c5 c10 c12 c14 c15 c16 c17 c18 c20 c25 c35 c40 c90 c100 c110 c120 c130 c140 c150 c152 c160 c170 c180 c190 c192 c200 c210 c220 c230 c240 c250 c260 c270 c280 c290 c300 c310a c310b c310c c310d c314a c314b c314c c314d c320a c320b c320c c324a c324b c324c c330 c332 c340 c350 c360 c370 c380 c390 c400 c410 c420 c430 c440 c450 c460 c490 c510a c510b c510c c510d c510e c510f c602 c604 c606 c608 c610 c612 c614 c616 c620 c640 c652 c654 c660 eof 20081201 NM 2008 12 1 USAA920082024 1 20081024 A 5313 6545800 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C20553006/006 LEVEL 2 EXFOLIATION CORROSION AT STRINGER 18R BETWEEN BS294 TO BS325. REPAIRED S TRINGER 18R BETWEEN BS294 TO BS325 IAW B737 SRM 53-00-03. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 ASAA0893789 1 20081115 A 5230 SKIN BOEING 737 737990 NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 FWD CARGO DOOR OUTER SKIN YELLOW DOT APPLIED AT DENT NOT ON SAD RUN 28 INCHES FROM AFT EDGE 22 INCHES FROM TOP. 2 L 7 4 4F RT A16WE 20081201 NM 2008 12 1 SWAA086608 1 20081125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086565 1 20081123 A 3350 411A2212 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 920WN 32460 FOUND R2 DOOR EGRESS LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 DL757081635 1 20081118 A 5340 146N85154 ATTACH ANGLE BOEING 757 757232 1384965 NM BS 1461 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 CORROSION ON ATTACH ANGLE BS 1461 RBL 22 WL 145, AFT CARGO COMPARTMENT OUT OF LIMITS. REMOVED AND REPLACED PART. 2 L 7 2 4F RT A2NM 20081201 NM 2008 12 1 AALA200820026 1 20081023 A 5320 TEE FITTING BOEING 757 757223 1384957 NM BS 1720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 663AM 53392 25279 TEE FITTING CORRODED AFT RT CORNER OF DECK PLATE. REPLACED TEE FITTING IAW SRM 53-60-51. 2 L 7 2 4F RT A2NM 20081201 NM 2008 12 1 AALA200820027 1 20081027 A 5340 415N400110 FITTING BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 604AA 43723 27055 AFT OUTBOARD RIGHT SIDE GALLEY FITTING CORRODED. REPLACED FITTING IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20081201 NM 2008 12 1 DLM88081598 1 20081120 A 7500 13277503 DUCT DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE DAMAGED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 980DL 53267 725545 RT ENGINE FIRE LIGHT CAME ON DURING FLIGHT. FOUND BLOWN DUCT AT AFT SIDE OF COWL ANTI-ICE VALVE. REPLACED DUCT FROM 13 TH STAGE SADDLE DUCT TO COWL ANTI-ICE VALVE. 2 L 7 2 4F 4 F RT A6WE E9NE 20081201 NM 2008 12 1 DL757081611 1 20081115 A 5320 143N51974 ANGLE BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 660 WL 208 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 724164 WL 208, BS 660 RBL 48, WEB UPPER ANGLE CRACKED. REMOVED AND REPLACED ANGLE. 2 L 7 2 4F 4 F RT A2NM E24NE 20081201 EA 2008 12 1 SWIA200820480 1 20081119 A 5241 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GALLEY DOOR NICKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 FLT 4852 - GALLEY SERVICE DOOR HARD TO OPEN FROM OUTSIDE. REMOVED BURR FROM OUTER HANDLE DOOR ALIGNMENT PIN. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 AALA200820031 1 20081024 A 5315 146N509131 FLOORBEAM BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 697AN 45632 26977 FLOORBEAM CORRODED. REPAIRED IAW EA B757-53-004789. 2 L 7 2 4F RT A2NM 20081201 WP 2008 12 1 AALA200810196 1 20081112 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT WEAK A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 584AA 53247 MID CABIN EMERGENCY LIGHT BATTERY PACK WEAK AT STATION 500R. INSTALLED NEW BATTERY PACK. 2 L 7 2 4F A6WE 20081201 NM 2008 12 1 AALA200820036 1 20081028 A 5320 146N8769U48 CHANNEL BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 663AM 53392 25297 HAT CHANNEL CORRODED. REPLACED HAT CHANNEL IAW SRM 51-21-03-7. 2 L 7 2 4F RT A2NM 20081201 EA 2008 12 1 SWIA200820454 1 20080830 A 5210 ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 961SW 7857 C-CHECK, PASSENGER DOOR ANGLE CRACKED. REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 SWAA086591 1 20081125 A 3350 81000 TRIM PANEL BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 DURING SCHEDULED MV2 CHECK, FOUND EEPLS TRIM LOOSE AT ROW 1. REMOVED AND REPLACED TRIM PER MM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 DL76G081622 1 20081122 A 2840 41817054 PRESSURE SWITCH BOEING 767 767332 1382001 NM NR 2 ENGINE FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1608 30573 2 RT ENG WOULD NOT START. RTB, RT ENG PRESS SWITCH POPPING C/B REPLACED FUEL PRESSURE SWITCH PER M/M. OP CKS GOOD RAN EN G AT IDLE, NO FAULTS NOTED. ETOPS CATEGORY 'D': INABILITY TO CTRL ENG OR GET DESIRED PWR. 2 L 7 2 4F RT A1NM 20081201 NM 2008 12 1 ASAA0893816 1 20081120 A 5320 146A7502 SUPPORT ANGLE BOEING 737 737990 NM BS 727-727I CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 CORROSION ON THE LOWER BULKHEAD SUPPORT ANGLE. REMOVED AND REPLACED SECTION BS 727I-772. 2 L 7 4 4F RT A16WE 20081201 NE 2008 12 1 ASAA0853779 2 20081115 A 7200 3370051180 SPINNER BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE NR 1 ENGINE WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 579AS 35187 894547 SPINNER FRONT CONE MISSING MORE THAN 20 PERCENT OF BLACK ANODIZED COATING. REMOVED AND REPLACED SPINNER CONE REF MM 72- 21-01. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081201 NM 2008 12 1 ASAA0893844 1 20081122 A 5320 146A7510 INTERCOSTAL BOEING 737 737990 NM BS 500J-500K BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 WHILE WORKING CARD (FUSE 5043 CUST CARD 5140481) FOUND BAFFLE INTERCOSTAL BENT FWD CARGO BAY STA 500S 500K. REMOVED FAB RICATED NEW AND INSTALLED INTERCOSTAL. 2 L 7 4 4F RT A16WE 20081201 CE 2008 12 1 GUUA10100802 1 20081010 A 5220 LOCK BEECH 1900 1900D 1154162 CE EMERGENCY EXIT LACK OF LUBE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 69549 UE194 AT SCHEDULED ROUTINE MAINT DISCOVERED LT AFT EMERGENCY EXIT FROZEN AND WILL NOT OPEN. APPLIED LUBRICANT TO LT AFT EMERG ENCY EXIT LOCKING ASSY. OPS CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081201 NM 2008 12 1 USAA2008112192102 1 20081105 A 5320 D53480043204 SILL AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 804AW 1043 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON LOWER SILL OF L-2 DOOR BETWEEN FR67 +17 INCHES AND FR68, Y1732 IN PASSEN GER CABIN. REPAIRED LOWER SILL OF L-2 DOOR BETWEEN FR67 +17 INCHES AND FR68, Y1732 IAW A319 SRM 53-41-14. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008112492119 1 20081121 A 2530 OVEN AIRBUS 320 A320232 3930326 EU GALLEY ODOR A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 648AW 770 FLT 138 LAS-SNA - BURNING SMELL - NR 2 OVEN EMITS ACRID SMELL WHEN OPERATED. MAINTENANCE COULD NOT DETERMINE CAUSE FOR ODOR - PULLED CIRCUIT BREAKER. MAINTENANCE CLEANED NR 2 OVEN AND NO ODOR NOTED. NO SUBSEQUENT EVENTS. 2 L 7 2 4F RT A28NM 20081202 EA 2008 12 2 MALA080199 1 20081126 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 8944B N8944B CAPTAIN CALLED-ADVISED THEY HAD AN AMBER CAUTION SMOKE IN THE LAVATORY. FLT ATTENDANT ADVISED SMOKE ALARM WAS GOING OFF AND THERE WAS A FIRE ODOR. FLIGHT RETURNED TO MSP BUT WHILE ON THE APPROACH CAUTION AND ALARM WENT OFF. FLIGHT DID NO T DECLARE AN EMERGENCY BUT DID LAND OVERWEIGHT. 2 L 7 2 4F RT A21EA 20081202 NM 2008 12 2 USAA2008112892141 1 20081112 A 5522 65C25746132 REPAIR BOEING 737 7373G7 138447J NM RT ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 SAL - C17 - MAJOR REPAIR - EXISTING REPAIR DELAMINATED ON RIGHT ELEVATOR UPPER SURFACE AT ELEVATOR STA 108.5. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW B737 SRM 51-70-03-0G. 2 L 7 2 4F RT A16WE 20081202 NM 2008 12 2 USAABB08172 1 20081126 A 3350 20121 CHARGER BOEING 767 767201 1385125 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 249AU 23901 BRU - DURING THE DAILY CHECK, THE EMERGENCY FLOOR PATH LIGHTING WAS FOUND INOPERABLE FROM ROW 1A/B TO ROW 8A/B. MAINTEN ANCE REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A1NM 20081202 NM 2008 12 2 USAA2008112892143 1 20081127 A 5754 65C25602223 REPAIR BOEING 737 7373G7 138447J NM LE SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 SAL - C17 - MAJOR REPAIR - EXISTING REPAIR DELAMINATED ON LEFT WING NR 2 SLAT UPPER SURFACE WS 251. REPAIRED NR 2 SLAT UPPER SURFACE IAW B737 SRM 51-70-10-2R. 2 L 7 2 4F RT A16WE 20081202 NM 2008 12 2 USAABB08173 1 20081125 A 3260 835606 PSEU BOEING 757 757225 1384959 NM FAILED A USAA K NONE N FALSE WARNING TO TAKEOFF 1 EA 19 920UW 22199 FLIGHT 882, LAS-BOS - AFTER TAKEOFF IN LAS, THE CREW RECEIVED "GEAR DOORS AND GEAR DISAGREE" MESSAGE ON EICAS. THE DOOR AND GEAR AMBER LIGHT ON FORWARD PANEL ILLUMINATED. ALL INDICATIONS WERE NORMAL AFTER RECYCLING THE GEAR. MAINTENANCE REPLACED PSEU CARD. 2 L 7 2 4F RT A2NM 20081202 NM 2008 12 2 UALA2008111305435 1 20080823 A 3350 363674 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 ROW 14 LT EEL STRIP INOP. REPLACED STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 20081202 NE 2008 12 2 UALA2008111305610 2 20080906 A 7321 53T424 THERMOCOUPLE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE RT ENGINE FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 206UA 30212 RIGHT ENG 2.9 STAB BLEED VALVE TC PROBE CHANNEL B SIGNAL OUT OF RANGE. REPLACED NR 2 ENG EEC PER MM 73-21-04. NO HELP CORRECTING PROBLEM. EEC OP CHECKS NORMAL. INSTALLED NEW GOOD PROBE IN 'B' POSITION, CHECKS OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081202 2008 12 2 UALA2008111306226 4 20081021 A 2565 101655305 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OVERWING EXIT NO TEST A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 642UA 25092 DURING LT OVERWING SLIDE DEPLOYMENT TEST, AFT HATCH STEP FAILED TO DROP DOWN, CABLE KINKED, STEP WILL NOT DROP FREELY. REPLACED AFT SUPPORT CABLE. OPS CHECKS GOOD. SLIDE FAULTY. AFTER CHECKING THE SLIDE SYS OUT, VERIFIED THE BOTTLE PRE SSURE AND WHITE DISK WERE CORRECT, THEY WERE PULLED AND SET UP THE SLIDE SYS IAW ROUTINE JIC 6-1950-50-1 0. WITH HYD PWR ON AND SPOILERS UP, THE LT AFT OVERWING HATCH WAS REMOVED, THE SPOILER BLOW DOWN ACTUATOR FIRED, PUSHING 85625, THE INB D SPOILER TO THE DOWN POSITION. LT OVERWING SLIDE COMPARTMENT DOOR OPENED TO THE FULL OPEN POSITION. THIS PULLED THE C ABLE THAT ACTUATES THE BOTTLE. AT THE INFLATION BOTTLE, THE BELL CRANK MOVED SLIGHTLY ENOUGH TO PULL THE CABLE FROM THE 2 L 7 2 4F 4 F RT A1NM E24NE 20081202 NM 2008 12 2 UALA2008111306339 1 20081031 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN LOOSE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 778UA 26940 EEL STRIP AT SEAT 2E IS LOOSE WITH WIRES SHOWING. SECURED LIGHT, CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081202 NM 2008 12 2 UALA2008111306369 1 20081103 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 548UA 25396 EMERGENCY LIGHT STRIP IN FRONT OF FC CLOSET IS LOOSE. SECURED LIGHT STRIP. 2 L 7 2 4F 4 F RT A2NM E17NE 20081202 NM 2008 12 2 UALA2008112406616 1 20081119 A 2421 S281T00137 GENERATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 643UA 25093 APU GENERATOR INOPERATIVE. CHECKED FEEDER CONNECTOR PER TIP 24-21-01-200A & FOUND OK. TRIED NEW GCU, NO HELP. BPCU BI TE SHOWS "REPLACE GEN-(DIODE)". NEEDS GENERATOR REPLACED. REPLACED APU GENERATOR. OPS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081202 NM 2008 12 2 UALA2008112406621 1 20081122 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 FUSELAGE SKIN DENT STA 760, AT STR 17L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081202 NM 2008 12 2 UALA2008112406623 1 20081122 A 5220 BACC2A4D00134JJ CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY EXIT KINKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 RT AFT EMERG EXIT HATCH STEP FWD CABLE IS KINKED. REPLACED CABLE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081203 NM 2008 12 3 AALA200820041 1 20081103 A 5330 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 604AA 43723 27055 AFT MAIN DECK PLATE CORRODED. REPAIRED IAW SRM 53-60-51-2R. 2 L 7 2 4F RT A2NM 20081203 EA 2008 12 3 BSY2008F00010 2 20081031 A 7414 1068291018 MAGNETO PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA RT ENGINE INTERMITTENT D BSYA O OTHER R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 07 3587P 318052120 RT ENGINE LOST POWER ON TAKE OFF, ABORTED TAKEOFF. (K) 1 L 7 2 3O 3 O A20SO E14EA 20081203 NM 2008 12 3 AALA200802733 1 20081013 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7667A 25301 MIA - EMERGENCY LIGHT AT SEAT ROW 5 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 5. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081203 NM 2008 12 3 AALA200802736 1 20081014 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 617AM 24525 DFW - EMERGENCY LIGHT AT SEAT ROW 11DEF BULL NOSE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 11DEF BULL NOSE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081203 SO 2008 12 3 FDKA2008111600296 1 20081116 A 3222 STRUT EMB 145 EMB145LR 3260212 SO NLG LOW A FDKA K NONE O OTHER CR CRUISE 1 SW 07 848MJ 145530 FRL FLT 6250 CLT-CVG - LANDING GEAR AIR GOUND FAIL. MX SERVICED NOSE STRUT AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081203 SO 2008 12 3 FDKA2008112800300 1 20081128 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 858MJ 145767 FRL FLT 6167 CVG-IND - AFT CEILING EXIT LOCATOR, FWD SIDE OUT. MX REMOVED AND REPLACED NR 3 AND NR 4 BATTERY PACKS. 2 L 7 2 4T RT T00011AT 20081203 NM 2008 12 3 AALA200802728 1 20081012 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW - EMERGENCY PROXIMITY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY PROXIMITY LIGHT AT SEAT 22C. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081203 NM 2008 12 3 AALA200802729 1 20081029 A 2930 6937317300 CONTROL MODULE BOEING 737 737823 13844BZ NM HYD SYSTEM FAULTED A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 905AN 29507 PIT INFLIGHT LAX TO IAD - DURING CRUISE, CREW REPORTED ENGINE NR 1 HYDRAULIC LOW PRESSURE INDICATION ILLUMINATED FOLLOWE D BY ENGINE NUMBER TWO HYDRAULIC LOW PRESSURE INDICATION. CREW TURNED OFF BOTH PUMPS AND LANDED PIT WITHOUT INCIDENT. EICAS SHOWED NORMAL HYDRAULIC PRESSURES AND QUANTITIES. FOUND HYDRAULIC PRESSURE INDICATING SYSTEM FAULTED. REPLACED H YDRAULIC RESERVOIR PRESSURE MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20081203 WP 2008 12 3 AALA200810199 1 20081110 A 5313 STRINGER DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 LONGERON 30 CORRODED FROM STATION 465-494. INSTALLED LONGERON REPAIR AT STATION 465-494 PER ESO 80559 DATED 11/04/2008. 2 L 7 2 4F A6WE 20081203 CE 2008 12 3 BSY2008F00018 1 20081023 A 3700 442CW12 PUMP BEECH 58 58 1152740 CE VACUUM SYSTEM FAILED E BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 9044V TH216 RT ENGINE DRIVEN VAC PUMP FAILED. THE SCREW FOR CHECKING WEAR ON VANES WAS MISSING, CAUSING PREMATURE FAILURE. (K) 1 L 7 2 3O 3A16 20081203 EA 2008 12 3 HNAA2008112000323 1 20081116 A 3251 89923 LINK DHAV DHC8 DHC8311 1386006 EA NLG STEERING BROKEN A HNAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 07 326EN 9769 5343 SAM0190106 234 IN PREPARATION FOR LANDING AT PHL THE FLIGHT CREW SELECTED THE GEAR DOWN AND THE NOSE GEAR INDICATOR WAS RED. THE MAIN GEAR INDICTED NORMAL. THE FLIGHT CREW DID THE ALTERNATE EXTENSION AND THE NOSE GEAR DID NOT COME DOWN. THE AIRCRAFT LA NDED WITH THE NOSE STILL RETRACTED, , THERE WERE NO INJURES REPORTED. UPON INSPECTION, LINK ON THE STEERING ACTUATOR FO UND BROKEN. STEERING ACTUATOR AND LINKS REPLACED. ACFT FERRIED TO SBY. DURING INSPECTION AFTER A NOSE GEAR UP LANDING, THE FRAME MEMBER AT X167.5 WAS BUCKLED BETWEEN STRINGERS 32S AND 32P.FRAME MEMBER WAS REPLACED IAW DEHAVILLAND STRUCTUR AL REPAIR MANUAL PROCEDURES. AIRCRAFT HAS NOT BEEN RELEASED YET DUE TO OTHER ONGOING WORK. 2 H 7 2 4T RT A13NM 20081203 NM 2008 12 3 HNAA2008120200326 1 20081124 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A HNAA K NONE O OTHER UK UNKNOWN 1 EA 07 938HA 152 EMERGENCY EXIT SIGN AT SEAT 4A REMAINS ILLUMINATED CONSTANTLY. INSPECTED AND FOUND LIGHT NOT TO BE ILLUMINATED. 2 H 7 2 4T RT A13NM 20081203 SO 2008 12 3 RAIA2008111500001 1 20081112 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 821HK 145068 PRE FLT INSPECTION REVEALED THAT THE EMERGENCY LIGHT AT SEAT 12A WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE LIGHT ASSEMBLY. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 20081203 SO 2008 12 3 RAIA2008112500004 1 20081122 A 3222 O-RING EMB 145 EMB145EP 3260221 SO NLG WORN A RAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 03 809HK 145187 DURING CLIMB, CREW RECEIVED A LG AIR/GND FAIL MESSAGE ON THE EICAS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A LEAK ING O-RING ON THE NLG SERVICING PORT. THE O-RING WAS REPLACED, NLG WAS SERVICED, AND AN OPERATIONAL CHECK OF THE EXTENS ION AND RETRACTION SYSTEM WAS PERFORMED. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 20081203 SO 2008 12 3 RAIA2008112400001 1 20081119 A 2930 300045021 THERMAL SWITCH EMB 145 EMB145LR 3260212 SO HYDRAULIC SYS FAULTY A RAIA B A EMER. DESCENT UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 812HK 145373 DURING CRUISE, CREW RECEIVED A HYDRAULIC SYSTEM 1 OVERHEAT MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE N R 1 SYSTEM HYDRAULIC THERMAL SWITCH. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081203 SO 2008 12 3 RAIA2008112500002 1 20081122 A 3350 LIGHT EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST TX TAXI/GRND HDL 1 CE 03 806HK 145112 CEILING EMERGENCY LIGHT IN CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE CEILING EMERGENCY LIGHT. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 20081203 NM 2008 12 3 HNAA2008120200329 1 20081123 A 3350 6013211X BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 07 846EX 37338 416 326 UPON ARRIVAL TO A/C, F/A FOUND EMERGENCY LIGHT TO HAVE BEEN LEFT ON. EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND R EPLACED CABIN EMERGENCY LIGHT BATTERIES, CABIN NUMBER S 3, 4, 5 AND 6 IAW 33-50-05R, OPS CHECK GOOD IAW 33-50-03Q BATTER Y S/N SBY-75 , SBY-1, $99088, ORF177. 2 H 7 2 4T RT A13NM 20081203 NM 2008 12 3 HNAA2008113000332 1 20081130 A 3150 7003652611 DISPLAY DHAV DHC8 DHC8102 2809003 NM COCKPIT DEFECTIVE A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 808EX 22868 4307 299 DURING GROUND HANDLING WITH APU AND ENGINES RUNNING, THE CREW NOTICED AN ELECTRICAL SMELL IN THE CABIN AND COCKPIT. MAI NTENANCE DISCOVERED THE PILOTS ADVISORY DISPLAY PANEL TO BE THE SOURCE OF THE ODORS. THE DISPLAY PANEL WAS PLACED ON TH E MEL LIST AND THE AIRCRAFT RELEASED FOR FURTHER FLIGHT. THE DISPLAY PANEL WAS SUBSEQUENTLY CHANGED AND OPS CHECKED GOO D. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 20081203 EU 2008 12 3 08FDEA04961 1 20081122 A 5347 R538D1042201 SEAT TRACK AIRBUS 310 A310304 3930339 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 817FD 552 MAIN DECK CARGO COMPT SEAT TRACK NR 2 RT, 12 IN AFT OF FR 43 HAS 2 DAMAGED SCALLOPS. REMOVED DAMAGED SECTION OF SEAT TR ACK NR 2 RT. FABRICATED REPLACEMENT SECTION AND INSTALLED BETWEEN FR 40 AND FR 45 IAW A310 SRM 53-10-16 AND SRM 51-40-2 1. 2 L 7 2 4F RT A35EU 20081203 EU 2008 12 3 08FDEA04963 1 20081124 A 5270 SWITCH AIRBUS 310 A310222 3930315 EU AFT CARGO DOOR FAULTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 455FE 331 AFT CARGO DOOR OPEN LIGHT IN FLIGHT. RETURNED TO KUL. VISUALLY CHECKED CLOSED AND LOCKED. VERIFIED INTEGRITY OF AFT C ARGO DOOR CLOSING AND LOCKING MECHANISM. ALL SATISFACTORY. SUSPECT FAULTY MICROSWITCH CAUSING ERRONEOUS DOOR INDICATIO N. APPLIED MEL 52-71-01. 2 L 7 2 4F RT A35EU 20081203 EU 2008 12 3 08FDEA04965 1 20081124 A 5320 FITTING AIRBUS 300 A300B4622 3930401 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 MAIN CABIN, AT FRAME 49 AND GANTRY 4 LT, SEAT TRACK, "LINKAGE FITTING" IS CRACKED, UNDER FLOOR. REMOVED AND REPLACED TH E SEAT TRACK LINK FITTING IAW A300-600 SRM 51-40-21, PARA 5, P/N A5381206720100, PO NR 640729.1. 2 L 7 2 4F RT A35EU 20081201 NM 2008 12 1 USAA920082035 1 20081022 A 5320 6545834256 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753005/015 LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL BS312 TO BS328, LBL11. REPLACED INTERC OSTAL BS312 TO BS328, LBL11 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAA920082026 1 20081106 A 5320 50794649 ATTACH ANGLE BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753006/012 INTERCOSTAL ATTACH ANGLE CRACKED AT BS296 BEHIND H STRAP. REPLACED INTERCOSTAL A TTACH ANGLE AT BS296 BEHIND H STRAP IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086597 1 20081125 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 23. REMOVED AND REPLACED LAMP PER MM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086627 1 20081125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086600 1 20081125 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 54. REPAIRED BEAM PER ER. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086602 1 20081125 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 DL757081636 1 20081118 A 5347 694557932 CARGO TRACK BOEING 757 757232 1384965 NM BS 1400-1405 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 CORROSION ON AFT CARGO TIE DOWN FITTING BS 1400-1405 RBL 25 WL 147 AT DOOR CUTOUT, NO ALLOWABLE LIMIT. REMOVED AND REPL ACED PART. 2 L 7 2 4F RT A2NM 20081201 NM 2008 12 1 DL757081641 1 20081118 A 5347 69455787 CARGO TRACK BOEING 757 757232 1384965 NM PWA JT8 JT8D219 52053 NE BS 1383 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 725866 CORROSION ON AFT CARGO TIE DOWN FITTING BS 1383 RBL 25 WL 147 AT DOOR CUTOUT, NO ALLOWABLE LIMITS. REMOVED AND REPLACED FITTING PER SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E9NE 20081201 NM 2008 12 1 DL76S081642 1 20081124 A 2781 TARGET BOEING 767 767332 1382001 NM NR 10 SLAT UNSERVICEABLE A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 130DL 24080 AFTER TAKEOFF APPROX 200FT AGL, THE STICK SHAKER ACTIVATED. AIRSPEED WAS NML AND FLAPS 15DEG. DURING FLAP RETRACTION R ECEIVED LEADING EDGE SLAT ASYM CAUTION MSG. PERFORMED QRH PROCEDURE. FOUND DAMAGED TARGET AT NR 10 SLAT INBD TRACK. R EPLACED SAME. REPLACED PROX BOX DUE TO NOT INDICATING TARGET PROBLEM. 2 L 7 2 4F RT A1NM 20081201 EA 2008 12 1 SWIA200820467 1 20081116 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 459SW 7782 AD INSPECTION, ENGINE SUPPORT BEAM INSPECTION PER AD CONFIRMED CRACKS. REPAIRED PER SB60R-53-065. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 DLM88081602 1 20081119 A 2710 CONTROL CABLE DOUG MD88 MD88 3023688 NM FLAP/SLATS FOD A DALA O OTHER W C F INADEQUATE Q C F.O.D. FLT CONT AFFECTED AP APPROACH 1 SO 27 952DL 49883 WHEN SLATS/FLAPS WERE EXTENDED FROM CLEAN POSITION, THE AIRCRAFT ROLLED APPROXIMATELY 20-30 DEGREES UNCOMMANDED. INSPEC TED AIRCRAFT, FOUND SCREWDRIVER STUCK IN CONTROL CABLES ABOVE E/E DOOR AT STA 116. REMOVED TOOL. RAN FLIGHT CONTROLS, FLAPS/SLATS, AILERON AND RUDDER TRIM. ALL CHECKS NORMAL. NO DAMAGE FOUND. OK FOR SERVICE. 2 L 7 2 4F RT A6WE 20081201 NM 2008 12 1 DLM88081603 1 20081120 A 4920 INLET DOUG MD88 MD88 3023688 NM APU CONTAMINATED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 963DL 17700 49982 BOTH AFT LAV SMOKE DETECTORS WENT OFF AFTER TAKEOFF FOR BUF BOTH ENG ANTI-ICE ON FOR TAKEOFF, NO SMOKE, SLIGHT ODOR DETE CTED, DISSIPATED RAPIDLY. SUSPECT DE-ICE FLUID INGESTION. APU INLET CLEAN PERFORMED ALT DUCT BURNOUT PER AIJC OPN 509 0 AND REPLACED WATER SEPARATOR BAGS PER AIJC 7904. ALL CHECKS GOOD. 2 L 7 2 4F RT A6WE 20081201 NM 2008 12 1 DL757081612 1 20081111 A 5320 146N54511 INTERCOSTAL BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 1538 LBL 11.4 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 724164 CORROSION ON LOWER FLANGE OF INTERCOSTAL COMMON TO SKIN BILGE AREA LBL 11.40 BS 1538. REPAIRED DAMAGE PER DELTA ER/A 47 1504-14 REV ORIG. 2 L 7 2 4F 4 F RT A2NM E24NE 20081201 WP 2008 12 1 AALA200810180 1 20081115 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 FRAME AT STATION 1418 CRACKED AT LONGERON 2L. REPAIRED PER ESO80559 DATED 11-14-08. 2 L 7 2 4F A6WE 20081201 EA 2008 12 1 SWIA200820469 1 20081123 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 810SK 15093 FLT 4530 - CEILING EMERGENCY LIGHT AFT CABIN INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 AALA200820029 1 20081028 A 5315 FLOORBEAM BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 697AN 45632 26977 FLOORBEAM CORRODED. REPAIRED IAW EA B757-53-004765 2 L 7 2 4F RT A2NM 20081201 EA 2008 12 1 SWIA200820475 1 20081118 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 455SW 7760 FLT 4425 - CEILING LEVEL EMERGENCY FLOODLIGHT OVER ROW 2 INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081201 SO 2008 12 1 SWIA200820477 1 20081117 A 6123 30005000052 SIGNAL COND UNIT EMB 120 EMB120ER 3260203 SO AUTOFEATHER SYS MALFUNCTIONED A SWIA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 NM 07 221SW 120290 FLT 5427 - ABORTED TAKEOFF DUE TO INADVERTENT AUTOFEATHER OF NR 1 ENGINE. REPLACED LEFT TORQUE PROBE AND TORQUE SIGNAL CONDITIONER PN ON 30005-0000-57, PN OFF 30005-0000-52, SN ON MM4720, SN OFF 4225. 2 L 7 2 4T RT A31SO 20081201 WP 2008 12 1 AALA200810190 1 20081118 A 5320 WEB DOUG DC9 DC983 3022083 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 965TW 53615 CANT FRAME 1485 UPPER LEFT WEB CRACKED AFT OF LEFT LOUVER BOX. INSTALLED DOUBLER PER AARD 53-10-00-32. 2 L 7 2 4F RT A6WE 20081201 WP 2008 12 1 AALA200810193 1 20081120 A 2761 CASTING DOUG DC9 DC982 3022082 WP SPOILER ACTUATOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 586AA 53249 GROUND SPOILER ACTUATOR CASTING CRACKED FORWARD INBD CORNER, LEFT GROUND SPOILER. INSTALLED REPAIR DOUBLER PER AARD 57- 20-00-15. 2 L 7 2 4F A6WE 20081201 NM 2008 12 1 AALA200820037 1 20081028 A 5320 146N8767U48 CHANNEL BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 663AM 53392 25297 HAT CHANNEL CORRODED. REPLACED HAT CHANNEL IAW SRM 51-21-03-7. 2 L 7 2 4F RT A2NM 20081201 EA 2008 12 1 SWIA200820445 1 20080827 A 5320 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 918SW 7645 C-CHECK SUPPORT AND CLIP AT FS 625 CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081201 EA 2008 12 1 SWIA200820447 1 20080827 A 5320 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 918SW 7645 C-CHECK, FS 280 LBL 9 SUPPORT CLIP CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081201 EA 2008 12 1 SWIA200820453 1 20080830 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 625 S14L CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 961SW 7857 C-CHECK, FS 625 LEFT STRINGER CLIP AT STRINGER 14L CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081201 EU 2008 12 1 RMXA11911708 1 20081031 A 5302 SKIN AGUSTA AGUSTA A109 A119 0261102 EU PWA PT6 PT6B37A 52179 NE TAILBOOM CRACKED E RMXA K NONE O OTHER AA AIR AMBULANCE 1 SW 05 820NA 14011 PU0008 A CRACK DEVELOPED IN THE TAILBOOM SKIN AT APPROXIMATELY STA 9725, WL 1895, LT SIDE EMANATING FROM A RIVET FORE AND AFT W ITH A TOTAL LENGTH OF APPROX 79 MM. 1 G 7 1 3U 4 U H7EU E4EA 20081201 NM 2008 12 1 DL757081619 1 20081118 A 5320 ANGLE BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 1480 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 724164 FOUND CORROSION ON INTERCOSTAL UPPER ATTACH ANGLE TO BE OUT OF LIMITS. FABRICATED REPLACEMENT ANGLE AND INSTALLED ANGLE BS 1480-1500 RBL 27. 2 L 7 2 4F 4 F RT A2NM E24NE 20081201 NM 2008 12 1 SWAA086574 1 20081124 A 5230 002354370 DOOR FRAME BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED HC2 CHECK, FOUND AFT CARGO DOOR FWD LOWER FRAME CRACKED. REMOVED AND REPLACED DOOR PER MM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086587 1 20081125 A 5610 141A481018 WINDOW BOEING 737 7377H4 1384404 NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 29 223WN 32492 R2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086589 1 20081125 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAA2008111792068 1 20081105 A 5315 D53472192200 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 804AW 1043 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON FLOORBEAM AT FR 69 - FR 70, +Y765. REPLACED FLOORBEAM AT FR 69 - FR 70, +Y 765 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081201 NM 2008 12 1 ASAA0893849 1 20081122 A 5320 146A7510 WEB BOEING 737 737990 NM BS 500I-500J BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 BAFFLE INTERCOSTAL BENT FWD CARGO BAY STA 500I, 500J LH 26 WL 154. REMOVED 2 L 7 4 4F RT A16WE 20081201 NM 2008 12 1 ASAA0843821 1 20081115 A 5320 65479575 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 787-793 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 AFT CARGO PIT CORRODED INTERCOSTAL STA 787 TO STA 793 STR 26R AREA. REMOVED DAMAGED INTERCOSTAL, LOCATED, DRILLED AND I NSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-40-02 AND 51-40-05. 2 L 7 2 4F RT A16WE 20081201 2008 12 1 JGV2008F00001 4 20081104 A 2561 82122Z CARTRIDGE AIRCRUISERS LEAR 35 31A 5170531 CE GARRTT TFE731 TFE731* 01518 WP LIFE VEST FAILED B JGVR K NONE O OTHER IN INSP/MAINT 1 CE 09 177JB L782100 161 DURING ROUTINE INSP OF NINE (9) LIFE VESTS FOUND MISSING CO2 CARTRIDGES ON ALL NINE (9) VESTS. ALL LIFE VESTS WERE RECE IVED IN SEALED, SEWN-SHUT BAGS WITH SIGNED MAINT RELEASE DOCUMENTS FROM PREVIOUS INSP ACCOMPANYING THEM. PREVIOUS INSPE CTION ACCOMPLISHED NOVEMBER 2003. CO2 CARTRIDGES ARE NORMALLY REMOVED FOR WEIGHT CHECK AND REINSTALLED AS PART OF ROUTI NE INSPECTION REQUIREMENTS. PROBABLE CAUSE FOR FAILURE TO RE-INSTALL IS LAPSE OF FOCUS ON DETAILS OF MAINT BEING PERFOR MED. (K) 2 L 7 2 4F 4 F RT A10CE E6WE 20081201 NM 2008 12 1 SWAA086539 1 20081122 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 244WN 34864 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY LIGHT LENS MISSING AT ROW 1. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086544 1 20081123 A 5330 6547952 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT UPPER AFT CORNER. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086545 1 20081123 A 3350 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED MV4 CHECK, FOUND R2 DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAASB08110 1 20081116 A 2121 6454051 FAN BOEING 737 7374B7 138449C NM CABIN NOISY A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 454UW 48929 3122 24996 MIA - FLT 741 - EN ROUTE PHL TO MIA. ON TAXI-OUT, THE FLIGHT CREW NOTICED THAT THE LEFT RECIRCULATION FAN WAS NOISY. T HE FAN WAS TURNED OFF AND THE FLIGHT PROCEEDED. DURING THE FLIGHT, THE FLIGHT CREW NOTICED AN OILY ODOR COMING FROM THE COCKPIT GASPER VENT. THE CREW SHUT-OFF THE RIGHT RECIRCULATION FAN, AND THE ODOR DISSIPATED. THE FLIGHT CONTINUED WIT HOUT FURTHER INCIDENT. MAINTENANCE PLACED AIRCRAFT ON MEL. MAINTENANCE REPLACED THE LEFT RECIRCULATION FAN. OPERATION ALLY CHECKS OK. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAASB08113 1 20081118 A 2751 2061141 INDICATOR BOEING 737 7374B7 138449C NM COCKPIT DEFECTIVE A USAA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 EA 19 432US 35934 2842 24554 DCA - FLT 1282 EN ROUTE PBI TO DCA. DURING PREPARATION FOR LANDING, THE TRAILING EDGE FLAPS ONLY DEPLOYED TO TWO DEGRE ES AND INDICATED UNEVENLY SPLIT. THE CREW EXECUTED A MISSED APPROACH. THE CREW RECYCLED THE FLAPS AND MADE A SECOND AP PROACH. THE FLAPS DEPLOYED NORMALLY AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FLAP POSI TION INDICATOR. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A16WE 20081201 2008 12 1 USAASB08111 4 20081116 A 2565 D31591479 SLIDE BOEING 737 737401 138449B NM PAX DOOR LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 46973 2626 23885 MCO - THE FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE PRESSURE WAS FOUND LOW. MAINTENANCE REPLACED THE FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAASB08112 1 20081117 A 2150 UNKNOWN BOEING 737 7374B7 138449C NM A/C PACK ODOR A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 19 430US 24552 FLT 1868. ON TAKEOFF & LANDING, CREW NOTICED AN ODOR COMING FROM A/C PACKS. MX PLACED ACFT ON MEL. ODOR DISSIPATED DU RING CLIMB. CLT MX PLACED LT PACK ON MEL 21-01A. WHILE ON MEL, ANOTHER REPORT OF ODOR COMING FROM A/C PACKS DURING HIG H POWER ON TAKEOFF OCCURRED ON 11/21/08, FLIGHT 1159. ODOR AGAIN DISSIPATED DURING CLIMB. MX INSPECTED LT & RT RAM AIR INLETS, LT & RT ENGINE INLETS & AIR MIX CHAMBER. ALL CHECK OK. RAN ENGINES ONE AT A TIME WITH EACH PACK FOR FIVE MINU TES EACH. REACTIVATED LT PACK & ACCOMPLISHED ADJUSTMENT TEST PER MM 21-61-00-5. TESTED NORMAL. CLEARED MEL 21-01A. N O FURTHER ODORS NOTED AS CONFIRMED WITH FLT CREW & MX. ACFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAA SB08112 1 20081117 A 2120 UNKNOWN BOEING 737 737400 138449A NM CABIN ODOR A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 19 430US 24552 FLIGHT 1868, PBI-CLT - ON TAKEOFF AND LANDING THE CREW REPORTED A SOUR ODOR COMING FORM THE AIR CONDITIONING PACKS. THE ODOR DISSIPATED IN CLIMB. MAINTENANCE INSPECTED THE LEFT AND RIGHT RAM INLET, THE LEFT AND RIGHT ENGINE INLETS AND AIR MIX CHAMBER. ALL CHECK OKAY. MAINTENANCE RAN THE ENGINES ONE AT A TIME WITH EACH SIDE PACK FOR FIVE MINUTES EACH. NO FURTHER ODORS NOTED. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAA SB08113 1 20081118 A 2751 2061141 INDICATOR BOEING 737 737400 138449A NM COCKPIT FAULTY A USAA L ABORTED APPROACH F FLT CONT AFFECTED LD LANDING 1 EA 19 432US 35934 33092 24554 FLIGHT 1282, PBI-DCA - DURING PREPARATION TO LAND IN DCA THE FLAPS STOPPED AT 2 DEGREES WITH ASSEMBLY INDICATION. THE C REW EXECUTED A MISSED APPROACH AND DID A GO AROUND. THE CREW RECYCLED THE FLAPS AND AFTER APPROXIMATELY THREE MINUTES T HE FLAPS EXTENDED NORMALLY AND THE INDICATION WENT AWAY. THE FLIGHT LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLA CED THE FLAP POSITION INDICATOR. 2 L 7 2 4F RT A16WE 20081201 EU 2008 12 1 USAA2008112092095 1 20081112 A 5347 D53371112005 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C07 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR41 & FR47, -Y1292. REPAIRED SEAT TRACK BETWEEN FR41 & FR47 , -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081201 NM 2008 12 1 USAA920082036 1 20081022 A 5320 6545834259 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753005/014 LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL BS328 TO BS344, LBL11. REPLACED INTERC OSTAL BS328 TO BS344, LBL11 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAA920082037 1 20081019 A 5320 6562175133 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753005/011 LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL BS294 TO BS312, RBL11. REPLACED INT ERCOSTAL BS294 TO BS312, RBL11 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081201 EU 2008 12 1 USAA920082057 1 20081112 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 649AW 803 LOG PAGE 4458139 FLT NR 157 STL-PHX EEL EMERGENCY LIGHT OPS TEST FAILED (EPSU INT LOAD EMER L). MX RESET THE POWER SUPP LY AT CABIN LT. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081201 NM 2008 12 1 NWAA084936309 1 20081004 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING OVERNIGHT CHECK FOUND EMERGENCY LIGHTS AT ZONE B RT INOP. MX R&R POWER SUPPLY. OPS CHECKED GOOD, AND ACFT WAS R ETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20081202 NM 2008 12 2 USAA2008112492121 1 20081120 A 5753 654648198 SPINDLE BOEING 737 737401 138449B NM TE FLAP CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 PHL - RON - MAJOR REPAIR - CORROSION ON RIGHT WING OUTBOARD MID FLAP CARRIAGE SPINDLE. REPLACED RIGHT WING OUTBOARD FLA P ASSEMBLY IAW US AIRWAYS TASK CARD 03C40727020. 2 L 7 2 4F RT A16WE 20081202 EU 2008 12 2 USAA2008112592122 1 20081124 A 3350 321454 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN NO TEST A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 603AW 37496 16334 661 FLT 383 CLT-LAS - EEL - FORWARD LEFT EMERGENCY CABIN POWER SUPPLY UNIT WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED THE FORWARD LEFT EMERGENCY CABIN POWER SUPPLY UNIT AND BATTERY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081202 NM 2008 12 2 USAA2008112492113 1 20081123 A 5320 STRUCTURE BOEING 767 7672B7ER 1385107 NM NLG WW CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AY 25257 BFM - C3 - MAJOR REPAIR - CRACK ON VERTICAL CHORD ON NOSE WHEEL WELL AT BS 287, RBL 25, WL 173.5. REPAIRED VERTICAL CHO RD ON NOSE WHEEL WELL AT BS 287, RBL 25, WL 173.5 IAW B767 SRM 51-70-12. 2 L 7 2 4F RT A1NM 20081202 NM 2008 12 2 USAA2008112492108 1 20081123 A 3350 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 828AW 1552 FLT 341 - MZT-PHX - EEL - CIDS EMERGENCY LIGHT OPERATIONAL TEST FAILS EMERGENCY POWER SUPPLY UNIT INITIAL LOAD ON FORWAR D LEFT. RESET EMERGENCY POWER SUPPLY UNIT FORWARD LEFT AND RIGHT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081202 SO 2008 12 2 SIMA200832203 1 20081115 A 2120 UNKNOWN EMB 135 EMB135KL 3260302 SO CABIN ODOR A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 806AE 145503 ON FLIGHT 3055, CREW REPORTED SMOKE DETECTED IN CABIN AND COCKPIT 30 SECONDS AFTER TAKEOFF. SMOKE WAS NOT VISIBLE. SME LLED LIKE PAPER, BREAD TOAST, AND RUBBER. AFTER ONE MINUTE WITH BOTH PACKS TURNED OFF WAS UNABLE TO RESET THEM. CREW D ECLARED A EMERGENCY AND LANDED UNEVENTFULLY. FLIGHT ATTENDANT REPORTED ODOR CONTINUED UNTIL JUST PRIOR TO LANDING THEN DISSIPATED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ENVIRONMENTAL SLEEVE AT CONTROL UNIT IAW MM 21-51-02. OPERATION CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081202 SO 2008 12 2 DJFA2008084 1 20081125 A 2120 UNKNOWN EMB 135 EMB135BJ 3260306 SO CABIN SMOKE E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 23 910LX 14500952 IMMEDIATELY AFTER DEPARTURE CREW NOTED THE CABIN FILLING WITH SMOKE. MAINT IS EVALUATING. 2 L 7 2 4F RT 20081202 SO 2008 12 2 Y9PA663P112508 1 20081125 A 2910 HYDRAULIC SYSTEM GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU ZONE 100 LOW PRESSURE E Y9PA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 663P 3868 1434 1600316369 ENROUTE, THE CREW DECLARED AN EMERGENCY AND LANDED. THE REPORT IS BOTH HYDR SYS QUANTITY WAS INDICATING LOW, LOCATED A L OCAL TECH IAW AIR CARRIER MM SECTION 3.02. CHECKED THE QUANTITY IN THE HYDR RESERVOIRS AND VERIFIED THAT THEY WHERE LOW , SERVICED IAW COMPUTERIZED MAINT PROGRAM (CMP) 291057. ACFT CONTINUED AFTER SERVICING TO FINAL DESTINATION. 2 L 7 2 4F 4 F RT A12EA E25NE 20081202 2008 12 2 ESPADJ2008-2 2 20081117 A 7597 WIRE LEAR 35 35A 5170602 CE BLEED SWITCH BROKEN E ESPA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 11 568PA 205 ON LIFT OFF, CREW NOTED FUMES AND SMOKE IN ACFT, AND THE ACFT PRESSURIZATION SYS WAS IN EMERGENCY. POWER WAS REDUCED AND ENGINE BLEED AIR SWITCHES WERE CYCLED, BUT LT ENGINE REMAINED IN EMERGENCY. CAPTAIN DECLARED AN EMERGENCY TO GET PRIORI TY LANDING AND RETURNED WITHOUT INCIDENT. A MECHANIC WAS DISPATCHED, AND TROUBLESHOOTING REVEALED A BROKEN WIRE ON THE L T ENGINE BLEED CONTROL SWITCH LOCATED ON THE CO-PILOT`S INSTRUMENT PANEL. WIRE WAS REPAIRED AND SYS TESTED NORMALLY ON T HE GROUND AND SUBSEQUENT TEST FLIGHT. 2 L 7 2 4F A10CE 20081202 WP 2008 12 2 IXXA08SMN183S 1 20080419 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C-CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 1731 LONGERON 35.5 LEFT. REMOVED FASTENERS AS NE EDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AN D CORROSION FOUND. FABRICATED REPAIR DOUBLER, FILLER, FINGER DOUBLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PAR TS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08197 DATED 04/25/08, SEMAN DRAWING ED-4775 DATE D 04/22/08, SRM 51-1-21, 51-1-20D, NDT SPM PART 06-10-01-001, SRM 51-1-8B, SRM 51-1-11, AND 51-3-1. 2 L 7 4 4F RT 4A25 20081202 EU 2008 12 2 USAA2008112692132 1 20081114 A 5315 D53472772201 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 +5 INCHES TO FR67 +16 INCHES, -Y1195. REPAIRED F LOORBEAM BETWEEN FR66 +5 INCHES TO FR67 +16 INCHES, -Y1195 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008112692135 1 20081112 A 5320 D5311282600100 DUMMY RAIL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON DUMMY RAIL AT FR16, Y503. REPLACED DUMMY RAIL AT FR16, Y503 IAW A320 SR M 51-72-11. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008112692137 1 20081113 A 5320 D53480043207 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON R2 DOOR LOWER SILL AT FR68, Y1732. REPAIRED R2 DOOR LOWER SILL AT FR68, Y1732 IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 YENA20081114111 1 20081113 A 3397 WIRE AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS SHORTED A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 580JB 20792 2136 EMERGENCY LIGHT AT 13, 17 AND 21 ABC ARE OUT. FOUND SHORTED WIRES TO AISLE LIGHT AT SEAT 25ABC, CAUSING EPSU TO SHORT O UT WHEN EMERGENCY LIGHTS TURNED ON. REPAIRED SHORTED WIRES WITH A SPLICE, TAPED AND SECURED BUNDLE. REMOVED AND REPLAC ED EPSU PER AMM 33-51-38, OPS CHECK OF EMERGENCY AISLE LIGHTS NORMAL. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008120192158 1 20081128 A 3397 WIRE AIRBUS 320 A320232 3930326 EU CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 619AW 527 FLT 460 PHX-IND - EEL - EMERGENCY EXIT LIGHT SEAT 19 LT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT EMERGENCY EXIT LIGHT SEAT 19 LT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008120192159 1 20081128 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A USAA K NONE L NO TEST NR NOT REPORTED 1 EA 19 651AW 33626 20546 866 FLT 504 ORD-PHX - EEL - EMERGENCY EXIT SIGNS OVER 1L AND 1R DO NOT ILLUMINATE IN THE ARMED POSITION. MAINTENANCE REMOVE D AND REPLACED THE EMERGENCY POWER SUPPLY UNIT AND BATTERY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 20081202 NM 2008 12 2 USAA2008112892140 1 20081112 A 5754 65C26601197 REPAIR BOEING 737 7373G7 138447J NM LE SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 SAL - C17 - MAJOR REPAIR - EXISTING REPAIR DELAMINATED ON LEFT WING NR 1 SLAT UPPER SURFACE WS 254.53 TO WS 389. REPAIR ED NR 1 SLAT UPPER SURFACE IAW B737 SRM 51-70-10-2R. 2 L 7 2 4F RT A16WE 20081202 NM 2008 12 2 USAA2008112892142 1 20081112 A 5522 65C557A13 REPAIR BOEING 737 7373G7 138447J NM LT ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 SAL - C17 - MAJOR REPAIR - EXISTING REPAIR DELAMINATED ON LEFT ELEVATOR UPPER SURFACE AT ELEVATOR STA 53. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW B737 SRM 51-70-03-0G. 2 L 7 2 4F RT A16WE 20081202 EU 2008 12 2 USAA2008112892148 1 20081113 A 5315 D5311141420000 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT FR20, -Y200. REPLACED FLOORBEAM AT FR20, -Y200 IAW A320 SR M 51-72-11. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008112892149 1 20081114 A 5347 DAN2001179511 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON RAIL SEAT BETWEEN FR64 TO FR66, -Y1292. REPLACED RAIL SEAT BETWEEN FR64 TO FR66, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081202 NM 2008 12 2 USAA2008112892138 1 20081126 A 5755 SPOILER BOEING 737 7373G7 138447J NM RT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 CLT - RON - MAJOR REPAIR - RIGHT WING NR 7 SPOILER DELAMINATED AT UPPER TRAILING EDGE APPROX 5 INCHES CIRCULAR DIAMETER. REPLACED NR 7 SPOILER IAW B737 AMM 27-61-11. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086588 1 20081124 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 265WN 32522 FOUND FWD EEPLS LIGHT COVER MISSING. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 20081201 2008 12 1 USAASB08109 4 20081116 A 2565 D37022101 BOTTLE AIRCRUISERS BOEING 737 737401 138449B NM EVAC SLIDE LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 1227 23885 MCO - MAINTENANCE REPORTED THE FORWARD ENTRY DOOR ESCAPE SLIDE BOTTLE PRESSURE WAS LOW. MAINTENANCE REMOVED AND REPLACE D THE FORWARD ENTRY DOOR ESCAPE SLIDE ASSEMBLY PER MM 25-61-00. 2 L 7 2 4F RT A16WE 20081104 WP 2008 11 4 UPS08853748 1 20081002 A 5320 CUSP WEB DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATION REPAIR EFN 70219971243 ORIGINAL NRC 750796 CUSP MEMBRANE CRACKED AT TRACK G FS 1470. PREV IOUSLY REPAIRED IAW 53-02-00 FIG 025. 2 L 7 4 4F RT 4A25 20081201 EA 2008 12 1 COMA0860463 1 20081113 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 784CA 7319 RT WING FUEL ACCESS PANEL CUTOUT AT 640BB HAS PITTING CORROSION AROUND EDGES. REMOVED CORROSION IN THE NON CRITICAL ARE A AT FUEL ACCESS PANEL 640BB CUTOUT AND FOUND THAT MATERIAL REMOVED WAS WITHIN LIMITS PER REO 601R-57-21-030 REV G. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 SWAA086569 1 20081124 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 788SA 30603 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 38 TO RBL 40. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086578 1 20081124 A 5311 654580744 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 291, STR 17R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081201 EA 2008 12 1 SWIA200820472 1 20081111 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 913EV 7731 AD INSPECTION, ENGINE SUPPORT BEAM INSPECTION PER AD CONFIRMED CRACKS. REPAIRED PER SB60R-53-065. 2 L 7 2 4F RT A21EA 20081201 EA 2008 12 1 SWIA200820458 1 20080810 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 959SW 7840 C-CHECK, RIGHT ENGINE AFT THRUST MOUNT FITTING CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081201 EA 2008 12 1 SWIA200820463 1 20081120 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 494CA 7765 FLT 2642 - ENTRY DOOR FLOOR LEVEL EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRE. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 SWAA086593 1 20081125 A 3350 81000 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 499WN 32481 DURING SCHEDULED HC2 CHECK, FOUND FWD EEPLS LIGHT COVER MISSING. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086594 1 20081125 A 3350 65C27095 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 499WN 32481 DURING SCHEDULED HC2 CHECK, LT EMERGENCY BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081201 2008 12 1 JGV2008F00004 4 20081104 A 2561 82122Z CARTRIDGE AIRCRUISERS LEAR 35 31A 5170531 CE LIFE VEST MISSING B JGVR K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 09 177JB L782069 161 DURING ROUTINE INSP OF NINE (9) LIFE VESTS FOUND MISSING CO2 CARTRIDGES ON ALL NINE (9) VESTS. ALL LIFE VESTS WERE RECE IVED IN SEALED, SEWN-SHUT BAGS WITH SIGNED MAINT RELEASE DOCUMENTS FROM PREVIOUS INSP ACCOMPANYING THEM. PREVIOUS INSPE CTION ACCOMPLISHED NOVEMBER 2003. CO2 CARTRIDGES ARE NORMALLY REMOVED FOR WEIGHT CHECK AND REINSTALLED AS PART OF ROUTI NE INSPECTION REQUIREMENTS. PROBABLE CAUSE FOR FAILURE TO RE-INSTALL IS LAPSE OF FOCUS ON DETAILS OF MAINT BEING PERFOR MED. (K) 2 L 7 2 4F RT A10CE 20081201 2008 12 1 USAAEMB08019 4 20081113 A 2565 STITCHING EMB ERJ190 ERJ190100IGW 3260408 NM ESCAPE SLIDE LOOSE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 946UW 3768 19000072 ORF - MAINTENANCE FOUND THE FORWARD PASSENGER DOOR EVACUATION SLIDE LACING CORD UNRAVELED. MAINTENANCE REMOVED AND REPL ACED THE SLIDE. 2 L 7 2 4F RT A57NM 20081201 NM 2008 12 1 ASAA0893804 1 20081117 A 5320 143A751022 INTERCOSTAL BOEING 737 737990 NM BS 500K CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 SIDEWALL SUPPORT INTERCOSTAL CRACKED AT FASTENER HOLE. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT INTERCOSTAL BETWE EN BS 500J AND 500K IAW SRM 51-40-02 STEP 4B AND C 2 L 7 4 4F RT A16WE 20081201 NM 2008 12 1 ASAA0893805 1 20081119 A 5320 146A8127 SHIELD BOEING 737 737990 NM BS 767-787 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 CORROSION ON SIDEWALL SUPPORT PLATE SHIELD STA 767 787 RBL 23. REMOVED, FABRICATED NEW SUPPORT AND INSTALLED. 2 L 7 4 4F RT A16WE 20081201 NM 2008 12 1 ASAA0893815 1 20081120 A 5320 143A9485Y35 SUPPORT ANGLE BOEING 737 737990 NM BS 500L CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 CORROSION ON THE LOWER BULKHEAD SUPPORT ANGLE. REPLACED LOWER SUPPORT ANGLE AT BS 500L LBL 25 RBL 25 PER SRM 51-20-05 A ND 51-40-01. 2 L 7 4 4F RT A16WE 20081201 NM 2008 12 1 SWAA086540 1 20081120 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 461 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED MV1 CHECK, FOUND STRINGER CRACKED AT BS 461, STR 18L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081201 CE 2008 12 1 GUUA10100803 1 20081010 A 5220 LOCK BEECH 1900 1900D 1154162 CE EMERGENCY EXIT LACK OF LUBE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 69549 UE194 AT SCHEDULED ROUTINE MAINT, DISCOVERED RT AFT EMERGENCY EXIT FROZEN AND WILL NOT OPEN, APPLIED LUBRICANT TO RT AFT EMER GENCY EXIT LOCKING ASSY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081201 NM 2008 12 1 USAA2008112092097 1 20081105 A 5320 D5347112420300 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 804AW 1043 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 & FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR6 9 & FR70, S23R IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081201 CE 2008 12 1 ZESA2008008 1 20081013 A 5730 FUEL DOOR CESSNA 560 560XL 2076702 CE RT WING OPEN E ZESA A UNSCHED LANDING W INADEQUATE Q C TX TAXI/GRND HDL 1 EA 03 228Y 5342 FUEL DOOR AND CAP WERE NOT SECURED PRIOR TO FLIGHT. UPON TAKE OFF, CREW HEARD A BANGING FROM ACFT AND RETURNED TO POINT OF ORIGIN. INSPECTED AND FERRIED ACFT FOR REPAIRS. REMOVED AND REPLACED RT INBD LEADING EDGE AND POLISHED OUT FUSELAG E PANEL. 2 L 7 2 4F RT A22CE 20081201 NM 2008 12 1 USAA920082039 1 20081022 A 5320 65C46812169 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q5 MAJOR REPAIR NR 03C10853028/030 LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL AT BS967 TO BS986,5, RBL17. REPLACE D INTERCOSTAL AT BS967 TO BS986.5, RBL17 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081201 WP 2008 12 1 NWAA084969969 1 20081107 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 8-10 AND THE LT OVERWING EMERGENCY EXIT SIGN WERE INOPERATIVE. 2 L 7 2 4F A6WE 20081202 NM 2008 12 2 USAA2008112592123 1 20081123 A 5330 6552988 SKIN BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 CLT - C1 - MAJOR REPAIR - FUSELAGE SKIN CRACKED AT AFT RIGHT SERVICE DOOR LOWER DOOR HINGE CUTOUT AT BS 951 BELOW S14R. REPAIRED FUSELAGE SKIN AT AFT RIGHT SERVICE DOOR LOWER DOOR HINGE CUTOUT AT BS 951 BELOW S14R IAW B737 SRM 53-60-01 REP AIR 7. 2 L 7 2 4F RT A16WE 20081202 NM 2008 12 2 USAA2008112692128 1 20081125 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 805AW 1049 FLT 160 - PHX-LAS - EEL - AFT RECHARGEABLE EMERGENCY FLASHLIGHT HAS DEAD BATTERY. REMOVED AND REPLACED EMERGENCY FLASHL IGHT BATTERY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081202 NM 2008 12 2 KCSA081602 1 20081126 A 5312 PRESSURE BLKHD BOEING 747 747212B 1384886 NM ZONE 100 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 CORROSION ON PRESSURE DECK AFT T-CHORD AT BS 1480, WL187, RBL5 TO LBL30. 2 L 7 4 4F RT A20WE 20081202 NM 2008 12 2 DXTA2008112403367 1 20081122 A 3150 WARNING LIGHT GULSTM 200 200 4500308 NM MULTIPLE FAIL E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 739QS 198 IMMEDIATELY AFTER TAKEOFF POWER SET WE GOT THE RED DITCH LIGHT THE YELLOW AUTO PRESS FAULT LIGHT AND THE FOLLOWING EICAS MESSAGES CABIN ALT HIGH AUTO PRESSURE. 2 L 7 2 4F RT A53NM 20081202 EU 2008 12 2 USAA2008112892146 1 20081113 A 5320 D53480043207 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON LOWER SILL AT R2 DOOR, FR66, -Y1732. REPAIRED LOWER SILL AT R2 DOOR, FR 66, -Y1732 IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 20081202 NM 2008 12 2 USAA2008112892156 1 20081112 A 5320 143N80216 INTERCOSTAL BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 MCN - C12 - MAJOR REPAIR - INTERCOSTAL WEB CRACKED AT BS 550, RBL 54.5. REPAIRED INTERCOSTAL WEB AT BS 550, RBL 54.5 IA W B757 SRM 51-70-10-0G. 2 L 7 2 4F RT A2NM 20081202 NM 2008 12 2 YENA200811240119 1 20081123 A 2782 5914054 PDU EMB ERJ190 ERJ190100IGW 3260408 NM LE SLAT FAILED A YENA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 15 247JB 1188 190000042 ORD-JFK, SLAT FAIL ON APPROACH TO LANDING, QRH ITEMS COMPLETED. AFTER EMBRAER ANALYZED THE FHDB FOR SLAT FAIL EVENT (RE PEAT ITEM) IT WAS DETERMINED THAT THE SLAT SURFACES JAMMED IN FLIGHT DURING APPROACH. FIM TASK 27-81-00-810-802-A. PER FORMED FIM TASK 27-83-00-810-804-A. REPLACED NR 1 SLAT LT ELECTRIC PDU MOTOR. REF AMM 27-83-04. ALSO C/W FIM TASK 27- 81-00-810-802-A. OPS CHECK OK. 2 L 7 2 4F RT A57NM 20081202 2008 12 2 UALA2008112106605 4 20081119 A 2565 660431 CYLINDER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EVAC SLIDE LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 772UA 0113 26930 INFLATION CYLINDER OUT OF GREEN BAND. IMPROPER CYLINDER FILL. TOP OFF CYLINDER. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081202 NM 2008 12 2 UALA2008111305431 1 20080823 A 3350 363674 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 ROW 1 LT EEL STRIP INOP. REPLACED LUMINESCENT STRIP. OPS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081202 NM 2008 12 2 UALA2008111305438 1 20080823 A 3350 363674 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 ROW 5 LT EEL STRIP INOP. FOUND LIGHTS INOP. REPLACED STRIP. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081202 NM 2008 12 2 UALA2008111306324 1 20081030 A 5220 CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ESCAPE HATCH FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 RT OVERWING ESCAPE HATCH(S) OFFWING MANUAL BACKUP CABLE CHECK FAILED. REPLACED RT OVERWING EXIT PRESSURE BOTTLE MANUAL BACKUP CABLE AND ADJUSTED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081202 EA 2008 12 2 ASOA200801511 1 20081115 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 713EV 10081 CORROSION DAMAGE ON NUT PLATE SUPPORT ANGLE ATTACHED TO AFT SIDE OF FS 280.00 IN A/E/B (MARKED). REMOVED CORRODED NUT P LATE SUPPORT ANGLE FROM AFT SIDE OF F.S. 280.00 IN A/E/B CORRION ON RADIUS OF ANGLE, ANGLE FOUND TO BE NO GOOD. ALL WORK DONE IAW 51-42-06. PICKED UP EXISTING FASTENER HOLES AND INSTALLED ANGLE FOR FLOORBOARD IN AVIONICS BAY AFT OF FS 280 PER SRM 51-42-06. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 DL777081621 1 20081122 A 2530 OVEN BOEING 777 777232 1385232 NM PWA 4060 PW4060 52119 NE GALLEY ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 863DA 29735 724164 GALLEY 401 OVEN 2 AFTER COOKING 8 MINS MADE HIGH PITCH BUZZ THEN QUIT W/ASSOCIATED BURNT WIRE ODOR NO FAULT LIGHT. 2 L 7 2 4F 4 F RT T00001SE E24NE 20081201 2008 12 1 JGV2008F00007 4 20081104 A 2561 82122Z CARTRIDGE AIRCRUISERS LEAR 35 31A 5170531 CE LIFE VEST MISSING B JGVR K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 09 177JB L782063 161 DURING ROUTINE INSP OF NINE (9) LIFE VESTS FOUND MISSING CO2 CARTRIDGES ON ALL NINE (9) VESTS. ALL LIFE VESTS WERE RECE IVED IN SEALED, SEWN-SHUT BAGS WITH SIGNED MAINT RELEASE DOCUMENTS FROM PREVIOUS INSP ACCOMPANYING THEM. PREVIOUS INSPE CTION ACCOMPLISHED NOVEMBER 2003. CO2 CARTRIDGES ARE NORMALLY REMOVED FOR WEIGHT CHECK AND REINSTALLED AS PART OF ROUTI NE INSPECTION REQUIREMENTS. PROBABLE CAUSE FOR FAILURE TO RE-INSTALL IS LAPSE OF FOCUS ON DETAILS OF MAINT BEING PERFOR MED. (K) 2 L 7 2 4F RT A10CE 20081201 2008 12 1 JGV2008F00006 4 20081104 A 2561 82122Z CARTRIDGE AIRCRUISERS LEAR 35 31A 5170531 CE LIFE VEST MISSING B JGVR K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 09 177JB L782064 161 DURING ROUTINE INSP OF NINE (9) LIFE VESTS FOUND MISSING CO2 CARTRIDGES ON ALL NINE (9) VESTS. ALL LIFE VESTS WERE RECE IVED IN SEALED, SEWN-SHUT BAGS WITH SIGNED MAINT RELEASE DOCUMENTS FROM PREVIOUS INSP ACCOMPANYING THEM. PREVIOUS INSPE CTION ACCOMPLISHED NOVEMBER 2003. CO2 CARTRIDGES ARE NORMALLY REMOVED FOR WEIGHT CHECK AND REINSTALLED AS PART OF ROUTI NE INSPECTION REQUIREMENTS. PROBABLE CAUSE FOR FAILURE TO RE-INSTALL IS LAPSE OF FOCUS ON DETAILS OF MAINT BEING PERFOR MED. (K) 2 L 7 2 4F RT A10CE 20081201 NM 2008 12 1 USAA BB08169 1 20081119 A 3350 BATTERY BOEING 767 767201 1385125 NM EMERGENCY LIGHTS INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246AY 23898 CLT - RIGHT EMERGENCY ESCAPE SLIDE SQUIP LIGHT FAILED TO ILLUMINATE DURING TEST ONE. MAINTENANCE REPLACED THE RIGHT OFF WING ESCAPE SYSTEM EMERGENCY BATTERY. 2 L 7 2 4F RT A1NM 20081201 EU 2008 12 1 USAA2008112092092 1 20081119 A 2120 UNKNOWN AIRBUS A321 A321211 3930370 EU CABIN FUMES A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 179UW 1521 FLT 904 CLT-ORD - RETURN TO FIELD - APPROXIMATELY 10 MINUTES INTO FLIGHT, FUMES WERE REPORTED IN THE REAR OF THE AIRCRAF T. THE CREW BEGAN A RETURN TO CLT AND WHEN AIRCRAFT STOPPED CLIMBING, THE FUMES DISSIPATED. IT WAS DECIDED TO CONTINUE TO ORD, BUT WHEN AIRCRAFT BEGAN TO CLIMB AGAIN, THE FUMES RETURNED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO CLT . THE AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT PER THE TSM (TROUBLESHOOTING MA NUAL) 71-00-00-810-802 WITH NO FAULTS NOTED. RAN BOTH ENGINES AND APU BLEEDS AND PACKS TO TAKEOFF POWER. NO SMOKE OR S MELL NOTED. 2 L 7 2 4F RT A28NM 20081201 CE 2008 12 1 ZESA2008014 1 20080925 A 7712 8184873 SENSOR CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE RT ENGINE OUT OF LIMITS E ZESA K NONE O OTHER TO TAKEOFF 1 EA 03 511TH 5600561 PCEDC0044 CREW IDENTIFIED DURING TAKEOFF THAT THE THROTTLE POSITION WHEN MATCHED SHOWED THE LT ENGINE AT 88 PERCENT AND THE RT ENG INE AT 37 PERCENT. RT ENGINE TOOK APPX 4-5 SECONDS TO CATCH UP TO THE LT. MAINT TROUBLESHOT AND REPLACED THE RT ENGINE T1 SENSOR. OPS CHECKS SATISFACTORY. 2 L 7 2 4F 4 F RT A22CE E00053EN 20081201 NM 2008 12 1 USAA920082070 1 20081020 A 5320 6546812169 INTERCOSTAL BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL C21 MAJOR REPAIR NR 6136496 CORROSION ON INTERCOSTAL BETWEEN BS967 TO BS986.5, WL208.1, RBL17.5 IN PASSENGER CABIN. REPAIRED INTERCOSTAL BETWEEN BS967 TO BS986.5, WL208.1, RBL17.5 IAW B737 SRM 51-40-02-0G. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 NWAA084986310 1 20081108 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING OVERNIGHT FOUND 2 EACH RT OVER WING EMERGENCY LIGHTS INOP. MX R&R POWER SUPPLY. OPS CHECKED GOOD, AND ACFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20081202 NM 2008 12 2 USAA2008112492109 1 20081114 A 5320 SUPPORT ANGLE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 804AW 1043 SAL - C7 - MAJOR REPAIR - CORROSION ON SUPPORT ANGLE AT INTERNAL STRUCTURE OF FORWARD CARGO COMPARTMENT FR29 + 2.5 INCHE S, S43R. REPLACED SUPPORT ANGLE AT INTERNAL STRUCTURE OF FORWARD CARGO COMPARTMENT FR29 + 2.5 INCHES, S43R IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081202 NE 2008 12 2 ASMF 20081102 2 20081121 A 7230 JT8D219 FAN BLADE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE RT ENGINE NICKED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 754RA 43964 10798 49641 718193 DURING OVERNIGHT CHECK, FOUND A NICK OF 0.005 INCHES DEPTH ON THE LEADING EDGE OF ONE FAN BLADE AT .4375 INCHES FROM THE ROOT, AND A NICK OF 0.0035 INCHES OUT OF LIMITS ON THE LEADING EDGE OF THE OTHER FAN BLADE AT .7500 INCHES FROM THE ROO T. RT ENG WAS REPLACED AND OPERATIONAL TEST WAS PERFORMED IAW MM 71-00-02 AND CM 71-00-01, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 20081202 EU 2008 12 2 USAA2008112692134 1 20081114 A 5315 D5347279220000 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT FR68, Y765. REPLACED FLOORBEAM AT FR68, Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081202 NM 2008 12 2 YENA200811260121 1 20081125 A 2120 UNKNOWN EMB ERJ190 ERJ190100IGW 3260408 NM CABIN ODOR A YENA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 279JB 190000090 FLT 623, JFK-HOU - AFTER TAKEOFF CALL RECEIVED FROM FLIGHT ATTENDANT AT 1500FT , A STRONG SMELL OF SMOKE IN THE CABIN. BELIEVED TO BE ELECTRICAL SMELL. AT THAT TIME CREW COULD SMELL SMOKE IN COCKPIT BUT NOT AS STRONG. PERFORMED QRH SMOKE COCKPIT/CABIN SMOKE/FUMES PROCEDURE. RETURNED TO JFK FOR EMERGENCY LANDING. THE SMOKE WAS NEVER VISIBLE TO THE FLIGHT OR INFLIGHT CREW. AFTER PERFORMING THE QRH PROCEDURE WHICH LEAD TO SHUTTING OFF THE BLEEDS AND RECIRCULATION FAN, NO L ONGER COULD SMELL THE BURNING ODOR. THERE WAS NO FURTHER INCIDENT AFTER TOUCHDOWN. TAXIED TO GATE NORMALLY WITH ARFF V EHICLES FOLLOWING AS PRECAUTION. PERFORMED TASK 21-20-00-810-801A SMOKE AND/OR ABNORMAL SMELL IN PASSENGER COMPARTMENT 2 L 7 2 4F RT A57NM 20081202 NM 2008 12 2 NWAA084996624 1 20081107 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 624US 21706 DURING OVERNIGHT FOUND EMERGENCY EXIT SIGNS AT DOOR 2 RT INOP. MX R&R BATTERY PACK. OPS CHECKED GOOD AND ACFT WAS RETU RNED TO SERVICE. 2 L 7 4 4F RT A20WE 20081202 NE 2008 12 2 UALA2008112106611 2 20081121 A 7397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUEL FLOW FAULTY A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 648UA 25285 CREW REPORT: FUEL CONFIGURATION EICAS ON DESCENT. 2 L 7 2 4F 4 F RT A1NM E24NE 20081202 EU 2008 12 2 YENA200811240117 1 20081123 A 3350 312431 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN FAILED A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 570JB 1627 2099 EMERGENCY LIGHT TEST FAILED FWD EPSU. REMOVED AND REPLACED EPSU, OPS CHECK NORMAL IAW AMM 33-51-38-04. 2 L 7 2 4F RT A28NM 20081203 WP 2008 12 3 AALA200810216 1 20081105 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 CORROSION ON RIGHT CUSP AT STATION 1281 TO 1309. REMOVED AND REPLACED CUSP FROM STATION 1250 TO 1309 RIGHT SIDE PER AAR D 53-20-00-16. 2 L 7 2 4F A6WE 20081203 NM 2008 12 3 AALA200810237 1 20081120 A 5343 TRUNNION BOEING 737 737800* NM RT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948AN 30086 RIGHT MAIN GEAR FORWARD TRUNNION INBOARD LUG FACE HAS CORROSION THAT MEASURES .107 IN DEPTH. REPAIRED PER SRM 57-20-2R- 2. 2 L 7 2 4F RT A16WE 20081203 NM 2008 12 3 AALA200820044 1 20081103 A 5347 141N51301 SEAT TRACK BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 604AA 43723 27055 LT OUTBOARD SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW SRM 51-10-02. 2 L 7 2 4F RT A2NM 20081203 WP 2008 12 3 AALA200810200 1 20081110 A 5313 STRINGER DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 LONGERON 29 LEFT CORRODED FROM STATION 484 TO 494. INSTALLED LONGERON REPAIR PER ESO 80559 DATED 11/04/2008. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200802734 1 20081014 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 561AA 53091 LGA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23D INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081203 CE 2008 12 3 BSY2008F00011 1 20080911 A 3411 PITOT SYSTEM CESSNA 208 208B 2073701 CE CONTAMINATED E BSYA O OTHER O OTHER TO TAKEOFF 1 GL 07 3RY 208B0436 ON TAKEOFF, PILOTS ALTIMETER AND VSI WERE FLUCTUATING. MAINT FOUND WATER IN PITOT/STATIC SYSTEMS. (K) 1 H 7 1 3T A37CE 20081203 SO 2008 12 3 FDKA2008111600297 1 20081116 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FRL FLT 6268 JFK-IAD - EMERGENCY LIGHTS INOP. MX REPLACED EMERGENCY BATTERY PACKS 2 AND 3. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 20081203 SO 2008 12 3 FDKA200811298 1 20081119 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 833MJ 145327 FRL FLT 6265 JFK-RIC - AFT MOST FLOOR ESCAPE PATH LIGHTS INOPERATIVE. MX REMOVED AND REPLACED FLOOR STRIP, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081203 SO 2008 12 3 FDKA2008111200293 1 20081112 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FRL FLT 8910 JFK - LT EMERGENCY EXIT OVERWING DOOR EXIT SIGN OUT. MX RESECURED LOOSE CONNECTOR, OPS GOOD. 2 L 7 2 4T RT T00011AT 20081203 SO 2008 12 3 FDKA2008112300299 1 20081123 A 5241 DOOR EMB 145 EMB145LR 3260212 SO GALLEY DOOR LACK OF LUBE A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 860MJ 145773 FRL FLT 6283 CVG-DAY - GALLEY DOOR DIFFICULT TO CLOSE. MX CLEANED AND LUBED DOOR, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081203 NM 2008 12 3 UALA2008112406626 1 20081122 A 2797 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE T/E BYPASS VALVE MISINSTALLED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 CONNECTOR ON T/E BYPASS VALVE V105 ALSO HAS INSULATOR DAMAGE FROM CONNECTOR NOT BEING INSTALLED PROPERLY. REPLACED VALV E ASSY. ALSO FOUND T/E FLAP BYPASS VALVE CONNECTOR D1716 NOT CONNECTED AT LT WHEEL WELL WHILE DOING OPS TEST FOR FLAP A ND SLAT ALTERNATE DRIVE SYS ON A-11 CHECK. ALSO CONNECTOR D1716 HAS CRACKS IN INTERNAL SHIELDED AREA. REPLACED CONNECT OR D1716. 2 L 7 2 4F 4 F RT A2NM E17NE 20081203 NM 2008 12 3 HNAA2008102900321 1 20081017 A 3233 8300101 ACTUATOR DHAV DHC8 DHC8102 2809003 NM NLG BYPASSING A HNAA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 EA 07 815EX 41157 321 FLIGHT 4165 LGA TO ROA. THE GEAR WAS SELECTED DOWN ON APPROACH. THE MAIN GEAR INDICATION WAS NORMAL AND THE NOSE GEAR INDICATION WAS RED. THE ALTERNATE INDICATION WAS NOT INDICATING AND THE APPROACH WAS MISSED. THE GEAR WAS THEN CYCLED FOR A SECOND TIME AND ALL INDICATIONS WERE NORMAL. ALL THREE GEAR DOWN AND LOCKED INDICATED WERE ILLUMINATED BY THREE G REEN LIGHTS. THE PLANE LANDED WITHOUT INCIDENT. IN ROA THE NOSE GEAR WAS SWUNG. IT WAS REPORTED THAT THE NOSE GEAR WA S SLOW AND THE DOORS WOULD STUTTER WHEN OPENING. FLUID COULD ALSO BE HEARD BYPASSING IN THE GEAR WELL. THE NOSE RETRAC TION ACTUATOR WAS REMOVED AND REPLACED IN ACCORDANCE WITH MM 32-30-31. THE GEAR WAS AGAIN CYCLED AND THE OPERATIONAL CH 2 H 7 2 4T RT A13NM 20081203 NM 2008 12 3 HNAA2008102900320 1 20081029 A 5320 85310346S104A DOUBLER DHAV DHC8 DHC8102 2809003 NM NLG WW CRACKED A HNAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 07 815EX 21233 321 UPON GEAR EXTENSION DURING FINAL APPROACH TO RUNWAY 35, NOSE GEAR RED UNSAFE LIGHT INDICATION ILLUMINATED. BOTH MAIN GEA RS LOCKED AND ILLUMINATED GREEN INDICATIONS. CREW DISCONTINUED APPROACH AND PERFORMED ALTERNATE GEAR EXTENSION PROCEDUR ED. GEAR WAS NOT CYCLED PRIOR TO PERFORMING THE ALTERNATE GEAR EXTENSION. THE FLIGHT LANDED AND TAXIED TO THE GATE WITH OUT INCIDENT. OUT OF SERVICE. THE AIRCRAFT WILL MTC FERRY TO SBY FOR FURTHER INSPECTION. UPON INSPECTION AT SBY AIRCR AFT DAMAGE RECORDING DESCRIPTION: LT SIDEWALL AT J-BEAM DOUBLER CRACKED. LOCATION: X97.00 AND Z110.00 APPROX. DIMENSION S: WIDTH-N/A, LENGHT-3.5IN, DEPTH-N/A. DISTANCE FROM FASTENER 1.0IN, STRINGER 1.0IN, FRAME 1.0IN. TYPE OF NDT PERFORMED: 2 H 7 2 4T RT A13NM 20081203 2008 12 3 JRA2008F00000 1 20081114 A 2710 240723006513 SPRING ASSY CVAC STC STC440 CONTROL CABLES STRETCHED A JRAA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 11 587CA 463 AILERON CONTROL CABLES BINDING TO THE RIGHT FROM FULL LEFT POSITION. INSPECTION OF AILERON CONTROL CABLES REVEALED STRE TCHED SPRING AT RUDDER INTERCONNECT. REMOVED AND REPLACED SPRING IAW 440 MM, SEC 8-2, PAGE 26. OPS CHECK OK. (K) 2 L 7 2 4R T 6A6 20081203 SO 2008 12 3 BSY2008F00002 1 20080926 A 3600 CS11C6231951 CLAMP PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA INTERCOOLER FAILED E BSYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 3587P 318052120 L63668A AFTER TAKEOFF AT 4,000 FT RT ENGINE FAILED AND ACFT RETURNED WITH NO PROBLEMS. MAINT FOUND INDUCTION TUBE CAME OFF INTE R-COOLER REDUCING MANIFOLD PRESSURE TO A NORMALLY ASPIRATED ENGINE. REPLACED WITH NEW DUCT AND CLAMP. (K) 1 L 7 2 3O 3 O A20SO E14EA 20081203 NM 2008 12 3 DXTA2008120203382 1 20081201 A 2780 SLAT SYSTEM GULSTM 200 200 4500308 NM MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 705QS 061 FOLLOWING A NORMAL TAKEOFF, SLATS WERE RETRACTED. KRUGERS INDICATED UNBALANCED, IN AMBER. 2 L 7 2 4F RT A53NM 20081203 CE 2008 12 3 BSY2008F00013 1 20080926 A 7721 10200007 PROBE BEECH 58 58 1152740 CE CHT MALFUNCTIONED E BSYA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 07 62500 TH1347 LT CYLINDER HEAD TEMP, WENT ABOVE RED LINE ON TAKEOFF, PILOT THEN RETURNED TO DEPARTURE. REMOVED AND REPLACE CHT PROBE. (K) 1 L 7 2 3O 3A16 20081203 NM 2008 12 3 DXTA2008120103374 1 20081126 A 3150 WARNING LIGHT GULSTM 200 200 4500308 NM ILLUMINATED E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 738QS 204 FLIGHT AIR BRAKE DEPLOYED ANNUCIATOR ILLUMINATED DURING TAKEOFF ROLL CAUSING A TAKE OFF UNSAFE EICAS MESSAGE. THE TAKE O FF WAS ABORTED. 2 L 7 2 4F RT A53NM 20081203 NE 2008 12 3 HNAA2008120200327 2 20081121 A 7310 3036432 FILTER ELEMENT DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 2 ENGINE CLOGGED A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 333EN 221 ON TAKEOFF ROLL NR 2 FUEL FILTER BYPASS CAUTION LIGHT ILLUMINATED. ABORTED TAKEOFF. REMOVED, INSPECTED & REPLACED HP & LP FUEL FILTER REF (WORK) CARD 73-10-02R AND 73-10-04R AND MAINT MANUAL 72-00-01 AND REPLACED HP FILTER BYPASS SWITCH R EF P&W MAINT, RUNUP CHECKS GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 20081203 SO 2008 12 3 RAIA20081200003 1 20081130 A 3350 LIGHT EMB 145 EMB145EP 3260221 SO CABIN LOOSE A RAIA K NONE O OTHER TX TAXI/GRND HDL 1 CE 03 803HK 145077 DURING PRE FLIGHT INSPECTION, EMERGENCY LIGHT AT SEAT 12A WAS FOUND TO BE LOOSE. MAINTENANCE RESECURED THE LOOSE LIGHT ASSEMBLY. 2 L 7 2 4F RT T00011AT 20081203 SO 2008 12 3 RAIA2008120100004 1 20081130 A 2150 A/C PACK EMB 145 EMB145EP 3260221 SO NR 1 MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 804HK 145082 DURING CLIMB, CREW RECEIVED A NR 1 PACK OVERLOAD MESSAGE ON THE EICAS. MAINTENANCE DEFERRED THE NR 1 PACK PER MEL INSTR UCTIONS. 2 L 7 2 4F RT T00011AT 20081203 NM 2008 12 3 HNAA2008111800331 1 20081118 A 6120 V319 BETA SWITCH DHAV DHC8 DHC8102 2809003 NM NR 2 BROKEN A HNAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 07 911HA 58513 58513 034 DURING TAKEOFF AND AFTER GEAR RETRACTION, THE NR 2 ENGINE STARTED TO SURGE BETWEEN 60 TO 100 PERCENT TORQUE. AFTER TURN ING BACK TO FIELD, THE CONDITION CLEARED. MAINTENANCE CLEANED AND RESEATED THE ECU CONNECTOR, GROUND RAN AIRCRAFT AND N OTED NO DEFECTS. AIRCRAFT WAS THEN RELEASED FOR SERVICE AND DURING TAKEOFF AND GEAR RETRACTION, AGAIN THE NR 2 ENGINE T ORQUE SURGED BETWEEN 40 AND 100 PERCENT. AFTER RPM REDUCTION, THE CONDITION CLEARED. DURING TROUBLESHOOTING BY MAINTEN ANCE, THE NR 2 ENGINE BETA BACKUP SWITCH (6141-S4) WAS FOUND TO BE BROKEN. THE SWITCH WAS CHANGED OUT AND THE AIRCRAFT WAS GROUND RUN AND OPS CHECKED GOOD PENDING AN EVALUATION FLIGHT. THE AIRCRAFT FLEW SATISFACTORILY AND WAS THEN RELEASE 2 H 7 2 4T RT A13NM 20081201 NM 2008 12 1 USAA920082031 1 20081105 A 5320 507945178 PAN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10552010/012 BOTTOM DOOR PAN BEAM HAS 2 CRACKS, 1 INCH AND 1.5 INCHES AT FORWARD LOWER DOOR ST OP AT FORWARD ENTRY DOOR. REPAIRED BOTTOM DOOR PAN BEAM AT FORWARD LOWER DOOR STOP AT FORWARD ENTRY DOOR IAW BOEING DRAW ING NR 50-7945 AND B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAA920082029 1 20081105 A 5210 507945178 SKIN BOEING 737 737301 1384611 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10552010/007 INTERIOR SKIN CRACKED AT NR 6 STOP PIN CUTOUTS AT FORWARD ENTRY DOOR. REPAIRED I NTERIOR SKIN CRACKED AT NR 6 STOP PIN CUTOUTS AT FORWARD ENTRY DOOR IAW US AIRWAYS TYPICAL REPAIR NR 52-10-16. 2 L 7 2 4F RT A16WE 20081201 EA 2008 12 1 COMA0860461 1 20081112 A 2131 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 938CA 7046 RECEIVED CABIN ALTITUDE WARNING AT 11,500 FT. RETURNED TO BWI, LANDED WITHOUT INCIDENT. PERFORMED OPS TEST OF CABIN P RESSURE CONTROLLER NR 1 AND NR 2 IAW CRJ AMM. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 ASAA0843878 1 20081029 A 5320 65C323946 BEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 MAIN CABIN STUB BEAM CRACKED RT STA 601 RBL 65. TRIMMED OUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND ST IFFENING ANGLE IAW ASA EA 400 53EA 00269. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086624 1 20081125 A 5330 65457665 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 500D, BETWEEN STR 12R TO STR 18R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086604 1 20081125 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14R TO STR 15R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086566 1 20081124 A 5210 6545768 SKIN BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR SKN CRACKED AT BS 305, WL 236. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 QXEA2008112601199 1 20081121 A 3397 CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY LIGHTS DISCONNECTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 400QX 4030 RDM - EMERGENCY EXIT LIGHT AFT REAR SERVICE DOOR INOP. PARTIALLY REMOVED SURROUND TO RT REAR SERVICE DOOR. FOUND CONNE CTOR TO EMERGENCY EXIT LIGHT (LOWER) UNPLUGGED. CONNECTED CONNECTOR AND RE-INSTALLED RT REAR SERVICE DOOR SURROUND. OP S CHECK GOOD. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081201 NM 2008 12 1 QXEA2008112601201 1 20081122 A 3350 6138001 POWER SUPPLY BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY LIGHTS MALFUNCTIONED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 19 400QX 1193 802 4030 PDX - EMERGENCY EXIT SIGN LOWER AFT PAX DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AT WS X692.22, PAN EL 245EZ IAW AMM TASKS 33-51-01-000-801, 33-51-01-400-801. OPS CHECK GOOD. NO DEFECTS NOTED. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081201 NM 2008 12 1 SWAA086610 1 20081125 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14R TO STR 15R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081202 WP 2008 12 2 NWAA085029881 1 20081009 A 4930 O-RING DOUG DC9 DC951 3022051 WP APU FUEL SYS LEAKING A NWAA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 676MC 47652 SHORTLY AFTER TAKEOFF FLIGHT ATTENDANT REPORTED STRONG FUEL ODOR IN CABIN. A SLIGHT FUEL ODOR WAS NOTICED IN THE COCKPI T. FLIGHT CREW LANDED AT DESTINATION. MX NOTICED APU INTAKE PLENUM WET WITH FUEL AND ALSO A FUEL LEAK AT THE APU FUEL HEATER. THE APU AND AN O-RING ON THE APU FUEL HEATER WERE REPLACED. PACK BURNOUT AND COALESCER BAG REPLACEMENT COMPLIE D WITH. 2 L 7 2 4F RT A6WE 20081202 NM 2008 12 2 NWAA085006743 1 20081108 A 3350 BATTERY PACK BOEING 747 747249F 1384849 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 643NW 22245 DURING LINE CHECK FOUND UPPER DECK EMERGENCY LIGHT INOP. MX R&R BATTERY PACK. OPS CHECKED GOOD AND ACFT WAS RETURNED T O SERVICE. 2 L 7 4 4F RT A20WE 20081202 NM 2008 12 2 USAA920082072 1 20081116 A 5330 6545775 SKIN BOEING 737 7373G7 138447J NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 PHX RON MAJOR REPAIR NR 4451797 FUSELAGE SKIN CRACKED BETWEEN BS727E TO BS747, S23R. REPAIRED FUSELAGE SKIN BETWEEN BS7 27E TO BS747, S23R IAW SRM 53-00-01-2R31. 2 L 7 2 4F RT A16WE 20081202 NM 2008 12 2 YENA200811200115 1 20081117 A 2782 1703909 ACTUATOR EMB ERJ190 ERJ190100IGW 3260408 NM LE SLAT FAILED A YENA B EMER. DESCENT F FLT CONT AFFECTED AP APPROACH 1 EA 15 193JB 7987 190000017 FLT 1219, BOS-BUF, AOA FAIL EICAS MESSAGE, SLAT FAIL EICAS MESSAGE QRH COMPLIED WITH EMERGENCY LANDING ACCOMPLISHED. T /S PER FIM TASK 27-81-00-810-802-A. FOUND NR 6 RT SLAT ACTUATOR TRIPPED DUE TO PREVIOUS HISTORY, REMOVED & REPLACED NR 6 RT SLAT ACTUATOR PER 27-81-01-000-801-A AND 27-81-01-400-801-A, PERFORMED MECHANICAL RIG OF NR 567 RT SLAT ACTUATORS P ER 27-80-820-801-A. NO ADJUSTMENT NEEDED. PERFORMED ELECTRICAL RIGGING PER 27-80-00-820-802-A. OPS CHECK GOOD. NO FA ULTS NOTED AT THIS TIME. PERFORMED FIM TASK 27-03-00-810-89L-A. NO FAULTS NOTED AT THIS TIME. 2 L 7 2 4F RT A57NM 20081202 NM 2008 12 2 DXTA2008120103378 1 20081129 A 2612 WARNING LIGHT GULSTM 200 200 4500308 NM APU FIRE FALSE ACTIVATION E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 745QS 170 15 MINS AFTER APU SHUTDOWN APU FIRE CAS MSG CAME ON IN FLIGHT. NO INDICATION OF FIRE VISIBLE ON GROUND. 2 L 7 2 4F RT A53NM 20081202 NM 2008 12 2 DXTA2008120103379 1 20081130 A 3230 LANDING GEAR GULSTM 200 200 4500308 NM INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 712QS 073 ON DEPARTURE APA, UNABLE TO GET LT AND RT MAIN TO RETRACT. 2 L 7 2 4F RT A53NM 20081202 CE 2008 12 2 BSY2008F00015 1 20081020 A 2421 649305R ALTERNATOR BEECH 58 58 1152740 CE ENGINE INTERMITTENT E BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 696BD TH352 LT ALTERNATOR INTERMITTENT, COULD NOT DUPLICATE, CHANGED AS PRECAUTIONARY MEASURE, OPS GOOD. (K) 1 L 7 2 3O 3A16 20081202 CE 2008 12 2 BSY2008F00016 1 20081029 A 3060 353801327 SWITCH BEECH 58 58 1152740 CE PROP HEAT BURNED E BSYA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 9044V TH216 ACFT ENROUTE, WHEN PILOT SMELLED SMOKE AND SAW FLAMES COMING OUT OF PROPELLER HEAT CIRCUIT BREAKER SWITCH. PILOT THEN D IVERTED TO AIRPORT WITH NO OTHER PROBLEMS. (K) 1 L 7 2 3O 3A16 20081202 NE 2008 12 2 BSY2008F00005 2 20081003 A 7200 ENGINE CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE FAILED E BSYA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION NR NOT REPORTED 1 GL 07 1115M 208B0356 PCE17008 ACFT ENROUTE, WHEN THE ENGINE FAILED. PILOT WAS ABLE TO LAND ON A HIGHWAY WITH NO PROBLEMS. CAUSE UNKNOWN AT THIS TIME . (K) 1 H 7 1 3T 3 T A37CE E4EA 20081202 CE 2008 12 2 BSY2008F00006 1 20080927 A 5210 DOOR BEECH 58 58 1152740 CE UNSECURE E BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 2064V TH1004 ACFT ENROUTE, WHEN THE CABIN DOOR POPPED OPEN, PILOT THEN LANDED. SECURED DOOR AND CONTINUED. (K) 1 L 7 2 3O 3A16 20081202 NM 2008 12 2 UALA2008111306307 1 20081029 A 3610 REGULATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE BLEED AIR SYSTEM BLOCKED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 777UA 26916 LOSS OF ALL WATER PRESSURE. FLIGHT DIVERTED. FOUND BLEED AIR PRESSURE REGULATOR BLOCKED. CLEANED AND NOW WATER PRESSU RE TO LAV AND GALLEY NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081202 CE 2008 12 2 BSY2008F00007 1 20081016 A 5210 DOOR BEECH 58 58 1152740 CE UNSECURE E BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 2064V TH1004 ACFT ENROUTE, HAD TO LAND AT BECAUSE CABIN DOOR POPPED OPEN SECURED DOOR AND CONTINUED TO DEPARTURE. (K) 1 L 7 2 3O 3A16 20081202 NM 2008 12 2 UALA2008111306361 1 20081103 A 4960 32908144 CONTROLLER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 213UA 30219 APU BLEED AIR APUC DETECTED LOSS OF ABILITY TO PNEUMATICALLY LOAD APU. MESSAGE IS TRIGGERED BY IGV OR SURGE CONTROL SY STEM FAULTS. STATUS MSG01- NOT ACTIVE ENGINE START MODE DEPENDENT; SURGE CONTROL VALVE (PNEUMATIC CLUSTER) DOES NOT FO LLOW COMMAND. DB- APU CONTROLLER (APUC) MSG-4911180 INACTIVE MODE. REPLACED APU CONTROLLER. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081202 EU 2008 12 2 YENA200811200116 1 20081117 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 597JB 2307 FLT 760, SJU-BOS, 30 MINUTES AFTER TAKEOFF F/A REPORTED A BURNING PLASTIC ODOR. COUNTING FROM THE LAST THREE ROWS, TURNE D OFF (LIVE TV) AND THE ODOR WENT AWAY. COMPLIED WITH TSM 24-00-00-810-823. NO DAMAGE FOUND. PERFORMED INSPECTION PER TSM 23-39-00-819-801 SECTION B. NO ABNORMALITIES FOUND. MONITORED FOR 2 HOURS. OPS NORMAL. 2 L 7 2 4F RT A28NM 20081202 NM 2008 12 2 UALA2008112406618 1 20081121 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 AFT PIT AT STA 1560, STR 26R, FRAME DENTED AT INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FR AME AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081202 NM 2008 12 2 UALA2008112406620 1 20081121 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 MAIN CABIN FLOORBEAM STA 1640, RBL 57 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF T-CAP, RBL 0 TO RBL 64. FAB NEW SECTION AND SPLICES. 2 L 7 2 4F 4 F RT A2NM E17NE 20081201 NM 2008 12 1 SWAA086616 1 20081125 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 362, STR 4R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086617 1 20081125 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND SKIN CORRODED AT BS 515, BETWEEN LBL 2 TO RBL 2. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086583 1 20081124 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BETWEEN BS 506D TO 512D, STR 28L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081201 SO 2008 12 1 SWIA200820479 1 20081121 A 5210 MECHANISM EMB 120 EMB120ER 3260203 SO PAX DOOR LACK OF LUBE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 298SW 120328 FLT 5710 - PASSENGER DOOR DIFFICULT TO OPEN. CLEANED AND LUBE LOCKING MECHANISM. 2 L 7 2 4T RT A31SO 20081201 SO 2008 12 1 SWIA200820470 1 20081107 A 3233 1959500007 ACTUATOR EMB 120 EMB120ER 3260203 SO MLG FAULTY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 584SW 18592 18592 120352 FLT 5711 - RIGHT MAIN GEAR WOULD NOT RETRACT. REPLACED RIGHT MAIN GEAR ACTUATOR, P/N 1959-000-07, S/N ON 685, S/N OFF: B118. 2 L 7 2 4T RT A31SO 20081201 WP 2008 12 1 AALA208810181 1 20081115 A 5330 SKIN DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 2 CRACKS IN SKIN AT STATION 1380 RT BETWEEN LONGERON 13R AND 14R. INSTALLED DOUBLER PER SRM 53-01-00. 2 L 7 2 4F A6WE 20081201 WP 2008 12 1 AALA200810184 1 20081121 A 5320 STRUCTURE DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 594AA 53284 CORROSION ON LOWER SIDE OF CABIN SUBFLOOR BELOW G1 GALLEY. INSTALLED REPAIR PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081201 NM 2008 12 1 AALA200820032 1 20081027 A 5320 STRUCTURE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 640A 56247 24597 AFT GUTTER BOX CORRODED. REPAIRED IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081201 WP 2008 12 1 AALA200810197 1 20081112 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT WEAK A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 584AA 53247 EMERGENCY LIGHT BATTERY PACK WEAK AT STATION 160L. INSTALLED NEW BATTERY PACK. 2 L 7 2 4F A6WE 20081201 EA 2008 12 1 SWIA200820457 1 20080810 A 5420 RISER CNDAIR CL600 CL6002B19 1900309 EA NACELLE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 959SW 7840 C-CHECK, FRETTING CORROSION AT RIGHT PRODUCTION RISER. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 ASAA0893881 1 20081104 A 5320 147A571235 SHEAR WEB BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 CORROSION ON SHEAR WEB BS 986.5 RBL 30 WL 208. REMOVED CORROSION, PERFORMED NDI TO ENSURE NO CRACKS. ALODINED AND PRIM ED. NO ESTABLISHED SRM LIMITS REPAIR WAS DONE PER EA 900 53EA 00246. 2 L 7 4 4F RT A16WE 20081201 NM 2008 12 1 SWAA086595 1 20081125 A 3350 65C27095 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 499WN 32481 DURING SCHEDULED HC2 CHECK, RT EMERGENCY BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086584 1 20081124 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727C BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 DL757081623 1 20081115 A 5320 146N539148 SUPPORT BOEING 757 757232 1384965 NM BS 1530 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 2 CORROSION ON INBD LOWER FLANGE OF FLOOR TO SIDEWALL SUPPORT COMMON TO LOCK FASTENER, BS 1530, LBL 16.5 OUT OF LIMITS. R EPAIRED PER DELTA ER/A 471507-14 REV ORIGINAL. 2 L 7 2 4F RT A2NM 20081201 CE 2008 12 1 GUUA10100801 1 20081010 A 5260 1294000321 DOOR BEECH 1900 1900D 1154162 CE AIRSTAIR STIFF A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 29 81556 UE239 PILOT REPORTED CABIN DOOR HARD TO CLOSE. CLEANED AND LUBRICATED AIRSTAIR DOOR LOCKING CAMS AND ADJUSTED DOOR SUPPORT CA BLES. OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 20081201 NM 2008 12 1 ASAA0893850 1 20081122 A 5320 146A7510 INTERCOSTAL BOEING 737 737990 NM BS 500K-500L CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 BAFFLE INTERCOSTAL CRACKED AT STA 500K 500L LT 26 WL 154. REMOVED FABRICATED NEW AND INSTALLED INTERCOSTAL. 2 L 7 4 4F RT A16WE 20081201 2008 12 1 JGV2008F00003 4 20081104 A 2561 82122Z CARTRIDGE AIRCRUISERS LEAR 35 31A 5170531 CE LIFE VEST MISSING B JGVR K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 09 177JB L782101 161 DURING ROUTINE INSP OF NINE (9) LIFE VESTS FOUND MISSING CO2 CARTRIDGES ON ALL NINE (9) VESTS. ALL LIFE VESTS WERE RECE IVED IN SEALED, SEWN-SHUT BAGS WITH SIGNED MAINT RELEASE DOCUMENTS FROM PREVIOUS INSP ACCOMPANYING THEM. PREVIOUS INSPE CTION ACCOMPLISHED NOVEMBER 2003. CO2 CARTRIDGES ARE NORMALLY REMOVED FOR WEIGHT CHECK AND REINSTALLED AS PART OF ROUTI NE INSPECTION REQUIREMENTS. PROBABLE CAUSE FOR FAILURE TO RE-INSTALL IS LAPSE OF FOCUS ON DETAILS OF MAINT BEING PERFOR MED. (K) 2 L 7 2 4F RT A10CE 20081201 2008 12 1 JGV2008F00002 4 20081104 A 2561 82122Z CARTRIDGE AIRCRUISERS LEAR 35 31A 5170531 CE LIFE VEST MISSING B JGVR K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 09 177JB L782065 161 DURING ROUTINE INSP OF NINE (9) LIFE VESTS FOUND MISSING CO2 CARTRIDGES ON ALL NINE (9) VESTS. ALL LIFE VESTS WERE RECE IVED IN SEALED, SEWN-SHUT BAGS WITH SIGNED MAINT RELEASE DOCUMENTS FROM PREVIOUS INSP ACCOMPANYING THEM. PREVIOUS INSPE CTION ACCOMPLISHED NOVEMBER 2003. CO2 CARTRIDGES ARE NORMALLY REMOVED FOR WEIGHT CHECK AND REINSTALLED AS PART OF ROUTI NE INSPECTION REQUIREMENTS. PROBABLE CAUSE FOR FAILURE TO RE-INSTALL IS LAPSE OF FOCUS ON DETAILS OF MAINT BEING PERFOR MED. (K) 2 L 7 2 4F RT A10CE 20081201 NM 2008 12 1 SWAA086541 1 20081121 A 3350 65C27095 BATTERY PACK BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086542 1 20081120 A 5754 65C2660297 SKIN BOEING 737 7373H4 1384600 NM NR 2 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT LOWER T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086543 1 20081120 A 3350 PL22300 LIGHT BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY LIGHT STRIP WORN BETWEEN ROW 8 TO ROW 13. REMOVED AND REPLACED STRIP PER MM . 2 L 7 2 4F RT A16WE 20081201 2008 12 1 USAA BB08170 4 20081119 A 2565 BATTERY BOEING 767 767201 1385125 NM ZONE 200 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 246AY 23898 CLT - LEFT EMERGENCY ESCAPE SPOILER SQUIB LIGHT FAILED TO ILLUMINATE DURING TEST TWO. MAINTENANCE REPLACED THE LEFT ESC APE SYSTEM EMERGENCY BATTERY. 2 L 7 2 4F RT A1NM 20081201 NM 2008 12 1 USAASB08114 1 20081119 A 3397 WIRE BOEING 737 7373G7 138447J NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 154AW 23776 PHX - SEAT TWO, LEFT FORWARD ESCAPE PATH LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONALL Y CHECKS OK. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAA2008112092094 1 20081119 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 816AW 31343 17067 1350 FLT 548 - PHX-DFW - EEL - EMERGENCY BATTERY PACK FAULTING ON LEFT OVERWING EMERGENCY EXIT LOCATION 11WL. REMOVED AND RE PLACED POWER SUPPLIES 11WL AND 12WL. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081201 NM 2008 12 1 USAA2008112192101 1 20081119 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 816AW 28339 1443 1350 FLT 548 - PHX-DFW - EEL - EMERGENCY BATTERY PACK FAULTING ON LEFT OVERWING EMERGENCY EXIT LOCATION 11WL. REMOVED AND RE PLACED POWER SUPPLIES 11WL AND 12WL. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081201 NM 2008 12 1 USAA2008111992089 1 20081116 A 5523 65C2638428 TRIM TAB BOEING 737 7374B7 138449C NM RT ELEVATOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 24781 CLT - RON - MAJOR REPAIR - RIGHT ELEVATOR TRIM TAB HAS CRACKS COMING FROM HINGE CUTOUTS (2 PLACES). REPLACED RIGHT ELEV ATOR TRIM TAB IAW US AIRWAYS TASK CARD 03C71227004. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAA2008111992090 1 20081116 A 5523 65C2638427 TRIM TAB BOEING 737 7374B7 138449C NM LT ELEVATOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 24781 CLT - RON - MAJOR REPAIR - LEFT ELEVATOR TRIM TAB DELAMINATED AT NR 2 HINGE CUTOUT AREA AND HAS CRACKS AT THE NR 1 HINGE CUTOUT. REPLACED LEFT ELEVATOR TRIM TAB IAW US AIRWAYS TASK CARD 03C71127007. 2 L 7 2 4F RT A16WE 20081201 EU 2008 12 1 USAA920082066 1 20081116 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 3930316 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 123UW 26508 3581 1310 LOG PAGE 4440750 FLT NR 1145 PHL-SAN EEL L3 EMERGENCY LIGHT POWER SUPPLY FAILED OPS CHECK. MX R&R THE L3 EMERGENCY POWE R SUPPLY UNIT. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081201 EU 2008 12 1 USAA920082067 1 20081114 A 3350 321454 POWER SUPPLY AIRBUS A319 A319112 3930323 EU CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 746UW 1297 LOG PAGE 4394365 FLT NR 1458 PIT-CLT EEL DURING EMERGENCY LIGHT TEST CFDS FAULT MSG EMERGENCY POWER SUPPLY UNIT BATTERY FORWARD LT. R&R BATTERY. OPS TEST WAS GOOD. 2 L 7 2 4F RT A28NM 20081201 NM 2008 12 1 USAA920082040 1 20081023 A 5320 65C10592146 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10853028/025 LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL AT BS964, BETWEEN RBL25 TO RBL8. RE PLACED INTERCOSTAL AT BS964, BETWEEN RBL25 TO RBL8 IAW B737 SRM 53-60-15. 2 L 7 2 4F RT A16WE 20081201 WP 2008 12 1 NWAA084979862 1 20081109 A 3397 CONNECTOR DOUG DC9 DC951 3022051 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 771NC 47769 DURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 14-18 OF THE CABIN WERE INOPERATIVE. MX CORRECTE D A LOOSE CONNECTION AND THEN OPS CHECKED THE SYSTEM. 2 L 7 2 4F RT A6WE 20081202 NM 2008 12 2 USAASB08115 1 20081122 A 2751 2061141 INDICATOR BOEING 737 7374B7 138449C NM COCKPIT FAULTY A USAA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 EA 19 460UW 2054 1575 25024 CREW REPORTED A SPLIT FLAP CONDITION WHEN EXTENDING FLAPS FROM 10 TO 15 UNITS. AFTER GO-AROUND, FLAPS CORRECTED TO NORM AL. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT CLT. CLT MAINTENANCE REMOVED AND REPLACED THE TRAILING EDGE FLAP POSITIO N INDICATOR PER MM 27-58-41. ACCOMPLISHED SATISFACTORY FLAP ASYMMETRY CHECK AND TEST OF THE TRAILING EDGE POSITION INDI CATION SYSTEM. 2 L 7 2 4F RT A16WE 20081202 EU 2008 12 2 USAASB08116 2 20081123 A 7230 COMPRESSOR BOEING 737 7374B7 138449C NM CFMINT CFM56 CFM563B2 13802 EU LT ENGINE LEAKING A USAA O OTHER J WARNING INDICATION TO TAKEOFF 1 EA 19 430US 24552 ON TAKEOFF FROM ORD, EN ROUTE TO CLT, CREW REPORTED A STRONG ODOR WITH SMOKE DETECTORS SOUNDING OFF. NO VISUAL INDICATI ON OF SMOKE WAS NOTED. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT CLT. CLT MAINTENANCE FOUND OIL RESIDUE IN APU DISTRIB UTION DUCT. CLEANED AND BURNED OUT SMELL. ALSO, DUE TO AIRCRAFT HISTORY FOR STRONG ODORS, CLT MAINTENANCE BOROSCOPED T HE NR 1 ENGINE FOR OIL IN THE HPC STAGES 1-3 PER MM 71-00-00-6. OIL WAS FOUND IN THE HPC STAGES 1-3. MAINTENANCE REMOV ED AND REPLACED THE NR 1 ENGINE PER JOB CARD. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 20081202 NM 2008 12 2 USAA2008112492112 1 20081106 A 5315 BAC1518399 FLOORBEAM BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 SAL - C17 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT BS 986.5 BETWEEN RBL 43 TO LBL 8. REPLACED FLOORBEAM AT BS 986.5 B ETWEEN RBL 43 TO LBL 8 IAW B737 SRM 53-00-51 2R2. 2 L 7 2 4F RT A16WE 20081202 NM 2008 12 2 USAA2008112492116 1 20081122 A 5330 65C32355 SKIN BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 CLT - C1 - MAJOR REPAIR - CRACK ON FUSELAGE SKIN AT BS 484.5, S1R. REPAIRED FUSELAGE SKIN AT BS 484.5, S1R IAW B737 SRM 53-00-01. 2 L 7 2 4F RT A16WE 20081202 NM 2008 12 2 USAA2008112492117 1 20081121 A 5752 6546845521 TAB BOEING 737 7374B7 138449C NM AILERON DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 CLT - C1 - MAJOR REPAIR - LEFT AILERON TAB DISBONDED ON LOWER SIDE 1.5 INCHES FROM OUTBOARD END AND 1 INCH FROM TRAILING EDGE. REPLACED LEFT AILERON TAB IAW US AIRWAYS TASK CARD 03I30627002L. 2 L 7 2 4F RT A16WE 20081202 EA 2008 12 2 SIMA200833602 2 20081125 A 7200 ENGINE EMB 135 EMB135KL 3260302 SO RROYCE AE3007 AE3007A1 54165 EA NR 1 SMOKE A SIMA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 830AE 162 145615 CAE311351 ON FLIGHT 4553, AFTER 80 KTS ON TAKEOFF ROLL COCKPIT BECAME HAZY WITH SMOKE ACCOMPANIED BY ODOR. ABORTED TAKEOFF. SMOK E DISSIPATED FAIRLY RAPIDLY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 ENGINE OPERATION CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081202 CE 2008 12 2 DXTA2008112403366 1 20081122 A 3150 WARNING LIGHT RAYTHN DH125 HAWKER800XP 7150012 CE NR 1 COMPUTER ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 893QS 258393 NR 1 COMPUTER LIGHT ILLUMINATED ON TAKEOFF ROLL AT APPROX 60KTS. ABORTED TAKEOFF. 2 L 7 2 4F RT A3EU 20081202 2008 12 2 SIMA200832901 4 20081123 A 3420 DISPLAY EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 21 630AE 145132 ON FLIGHT 4286, DURING DESCENT CREW RECEIVED A PFD FAILED MESSAGE FOLLOWED BY SLIGHT ELECTRICAL BURNING ODOR. CREW PULL ED PFD NR 1 CB AND ODOR SLOWLY EXTINGUISHED. ACFT REMOVED FROM SERVICE, ISSUED MEL 34-01. REMOVED AND REPLACE NR 1 PFD IAW EMB-145 MM 34-22-01. OPERATIONAL CHECK GOOD MEL ITEM RESTORED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081202 WP 2008 12 2 IXXA08SMN186S 1 20080605 A 5310 FINGER DOUBLER DOUG DC8 DC871F 302199D WP ZONE 700 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 823BX 91810 2850 46064 DURING ROUTINE D CHECK INSPECTION, FOUND TOP SURFACE OF MAIN LANDING GEAR WHEEL WELL PRESSURE PANEL FINGER DOUBLER CORRO DED AT STATION 941.000 TO STATION 958.000 LEFT BOTTOM LINE 5 TO RIGHT BOTTOM LINE 5. REMOVED CORROSION. FOUND OUT OF L IMITS. REMOVED FINGER DOUBLER. FABRICATED FINGER DOUBLER. CLEANED TREATED AND PRIMED AREA AND FINGER DOUBLER. INSTAL LED NEW FINGER DOUBLER IAW SRM 51-1-21, SRM 51-1-8 PAGES 17-18, SRM 53-2-0 PAGE 2P, SRM 51-1-21, SRM 53-7-1 PAGE 21 FIGU RE 10, AND SRM 51-1-8B. 2 L 7 4 4F RT 4A25 20081202 WP 2008 12 2 IXXA08SMN182S 1 20080419 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 1694 LONGERON 27 RIGHT. REMOVED FASTENERS AS NEE DED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8100-9 D ATED 05-09-08, AD 2007-02-02, SB DC8-53A080 DATED 06-22-04, DRAWING SR08530032, MESSAGE 1-819144906-11 DATED 05/07/08, 1 -819144906-13 DATED 05-05-08, AND DRAWING ED-4754 DATED 05-10-08. 2 L 7 4 4F RT 4A25 20081202 EA 2008 12 2 MALA080197 1 20081123 A 3350 BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MALA O OTHER O OTHER CR CRUISE 1 GL 15 933XJ 15196 CABIN EMERGENCY LIGHTS CYCLING INTERMITTENTLY DURING FLIGHT. REPLACED BATTERY AND RELAY. 2 L 7 2 4F RT A21EA 20081202 EU 2008 12 2 USAA2008120192160 1 20081128 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU CABIN INOPERATIVE A USAA K NONE L NO TEST NR NOT REPORTED 1 EA 19 642AW 584 FLT 687 PHX-EWR - EEL - LAV D ALL LIGHTS INOPERATIVE INCLUDING EMERGENCY LIGHTS. CYCLED LAV POWER SWITCH ON FORWARD ATT ENDANT PANEL WITH NO HELP. MAINTENANCE RELAMPED LIGHTS AND RECONNECTED MIRROR LIGHT CONNECTOR. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008112892154 1 20081114 A 5320 D53471124200 SHEAR PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, Y1340. REPLACED SHEAR PLATE BETWEEN F R69 TO FR70, Y1340 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081202 NM 2008 12 2 UALA2008112106606 1 20081120 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 AFT PIT AT STA 1500, STR 26L FRAME DENTED AT INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081202 NM 2008 12 2 UALA2008112106608 1 20081121 A 3510 MC1019101 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT DEFECTIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 564UA 26666 PILOTS O2 MASK HAS DEFECTIVE AIRFLOW. REPLACED MASK & OP CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081202 WP 2008 12 2 NWAA084959867 1 20081106 A 3397 CONNECTOR DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT LOOSE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 776NC 47786 DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING FROM ROWS 22 AND AFT WERE INOPERATIVE. MX FOUND AND COR RECTED A LOOSE CONNECTION AND THEN OPS CHECKED THE SYSTEM. 2 L 7 2 4F RT A6WE 20081201 NM 2008 12 1 USAA2008111992091 1 20081118 A 5315 SUPPORT ANGLE BOEING 767 7672B7ER 1385107 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 253AY 24894 BFM - C4 - MAJOR REPAIR - FLOORBEAM SUPPORT ANGLE CRACKED AT BS 287, LBL 82. REPAIRED FLOORBEAM SUPPORT ANGLE AT BS 287 , LBL 82 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081202 CE 2008 12 2 BSY2008F00004 1 20081007 A 8011 STARTER CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE ENGINE NOISY E BSYA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 105AN 208B0956 PCEPC0911 AFTER TAKEOFF, AT 5,000 FT, ENGINE STARTER TO MAKE A SQUEALING NOISE WITH A RISE IN EGT, LOW TORQUE AND NO. PILOT THEN RETURNED TO DEPARTURE NO PROBLEMS. CAUSE UNKNOWN AT THIS TIME. (K) 1 H 7 1 3T 3 T A37CE E4EA 20081203 NM 2008 12 3 AALA200820043 1 20081103 A 5347 141N51301 SEAT TRACK BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 604AA 43723 27055 LT INBOARD SEAT TRACK CORRODED, REPLACED SEAT TRACK IAW SRM 51-10-02. 2 L 7 2 4F RT A2NM 20081203 CE 2008 12 3 BSY2008F00000 1 20081015 A 3010 442CLU12 PLUG BEECH 58 58 1152740 CE CONT O520 IO520* 17032 SO VACUUM PUMP MISSING E BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 525GW 417 TH557 ACFT WING BOOTS WON`T INFLATE TO FULL PRESSURE. FOUND INSP PLUG MISSING CAUSING PREMATURE PUMP FAILURE. (K) 1 L 7 2 3O 3 O 3A16 E5CE 20081203 SO 2008 12 3 FDKA2008111500295 1 20081115 A 5610 163500115 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT CRACKED A FDKA B EMER. DESCENT O OTHER CR CRUISE 1 SW 07 830MJ 145259 FDL FLT 6173 JFK-PIT - EMERGENCY DECLARED DUE TO LT WINDSHIELD SHATTERED. MX REMOVED AND REPLACED WINDSHIELD, OPS CHECK ED GOOD. 2 L 7 2 4T RT T00011AT 20081203 NM 2008 12 3 AALA200820040 1 20081103 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 604AA 43723 27055 AFT MAIN DECK PLATE CORRODED. REPAIRED IAW SRM 53-60-51-2R. 2 L 7 2 4F RT A2NM 20081203 NE 2008 12 3 AALA200802731 2 20081013 A 7261 OIL SYSTEM DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 1 ENGINE LOW PRESSURE A AALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 441AA 49460 728218 PHL INFLIGHT JFK TO DFW - DURING CLIMB NUMBER ONE ENGINE OIL PRESSURE LOW LIGHT ILLUMINATED. OIL PRESSURE DROPPED TO ZE RO ON GAUGE AND OIL TEMPERATURE DROPPED. CREW SHUT DOWN ENGINE AS PRECAUTION. LANDED PHL WITHOUT INCIDENT. SINGLE ENG INE TIME 15 MINUTES. FOUND METAL IN FILTER. REPLACED NUMBER ONE ENGINE ON 13 OCT AT PHL DUE TO OIL PRESSURE OUT OF LIMI TS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 20081203 2008 12 3 UALA2008112406627 4 20081122 A 2565 H2052K3833 LATCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 RT OVERWING ESCAPE SLIDE COMPARTMENT DOOR LATCHES FAIL TORQUE CHECK AT 225 IN LBS. REMOVED AND REPLACED 4 EA LATCHES AT RT OVERWING SLIDE COMPT DOOR. PRELIMINARY ADJUSTMENT AND LATCHING SYSTEM ADJUSTMENT CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081203 2008 12 3 UALA2008112406628 4 20081122 A 2565 H2052K3833 LATCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 LEFT OVERWING ESCAPE SLIDE DOOR LATCH NR 3 SLIDER WORN. REMOVED AND REPLACED NR 3 LATCH. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081203 EU 2008 12 3 AALA200802730 1 20081012 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 50051 459 MIA - EMERGENCY LIGHTS AT SEAT ROWS 1G TO 5G INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 1G TO 5G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081203 WP 2008 12 3 AALA200810198 1 20081110 A 5311 FRAME DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 FRAME AT STA 1418 L-2L TO L-2R HAS CRACKS. INSTALLED DOUBLER AND RADIUS BLOCK PER AARD 53-10-00-17. 2 L 7 2 4F A6WE 20081203 NM 2008 12 3 AALA200820048 1 20081105 A 5320 141N5160U46 FLOOR SUPPORT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 666A 52891 25300 FLOORBOARD SUPPORT HAT CHANNEL CORRODED. REPLACED FLOOR SUPPORT HAT CHANNEL IAW SRM 53-10-51-01. 2 L 7 2 4F RT A2NM 20081203 2008 12 3 BSY2008F00017 2 20080925 A 7261 DIPSTICK LEAR 35 35LEAR 5170600 CE LT ENGINE UNSECURE E BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 900JC 178 ACFT DEPARTED, WHEN PILOT NOTICED HIS LT ENGINE OIL PRESSURE DROPPING, HE THEN NOTIFIED TOWER AND RETURNED TO DEPARTURE. FOUND OIL DIP STICK NO SECURED CAUSING OIL LOSS. (K) 2 L 7 2 4F A10CE 20081203 NM 2008 12 3 HNAA2008112300324 1 20081121 A 2611 PU90461S SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM LAVATORY MALFUNCTIONED A HNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 07 908HA * 59520 015 LAV SMOKE DETECTOR SOUNDED ABOUT 10 TIMES AND STOPPED, NO EVIDENCE OF SMOKE OR FUMES. LAV SMOKE DETECTOR DEACTIVATED IA W SP 26.2 REFERENCE LP 279923 ITEM 2. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW 26-12-05 AND REACTIVATED SYSTEM OPS C HECK GOOD. P/N ON/OFF PU90-461S S/N OFF 08243 S/N ON 09254. 2 H 7 2 4T RT A13NM 20081203 SO 2008 12 3 RAIA2008112500003 1 20081122 A 3297 WIRE EMB 145 EMB145EP 3260221 SO LANDING GEAR BROKEN A RAIA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 805HK 145096 DURING CLIMB, CREW RECEIVED A LG AIR/GROUND FAILURE MESSAGE ON THE EICAS. MAINTENANCE REPAIRED WIRING AT THE LT AFT A/G SWITCH. SYSTEM OPS CHECKED GOOD FOLLOWING REPAIR. 2 L 7 2 4F RT T00011AT 20081203 SO 2008 12 3 RAIA2008120100001 1 20081126 A 3260 PROXIMITY SENSOR EMB 145 EMB145EP 3260221 SO LT MLG OUT OF ADJUST A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 809HK 145187 DURING CLIMB FROM TAKEOFF, CREW RECEIVED AN AIR/GROUND FAIL MESSAGE ON THE EICAS AND GEAR WOULD NOT RETRACT. MAINTENANC E INSPECTED AND FOUND THAT THE LT MLG WOW PROXIMITY SENSOR REQUIRED ADJUSTMENT. ADJUSTMENT WAS MADE AND LANDING GEAR SY STEM, OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 20081201 2008 12 1 JGV2008F00005 4 20081104 A 2561 82122Z CARTRIDGE AIRCRUISERS LEAR 35 31A 5170531 CE LIFE VEST MISSING B JGVR K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 09 177JB L782066 161 DURING ROUTINE INSP OF NINE (9) LIFE VESTS FOUND MISSING CO2 CARTRIDGES ON ALL NINE (9) VESTS. ALL LIFE VESTS WERE RECE IVED IN SEALED, SEWN-SHUT BAGS WITH SIGNED MAINT RELEASE DOCUMENTS FROM PREVIOUS INSP ACCOMPANYING THEM. PREVIOUS INSPE CTION ACCOMPLISHED NOVEMBER 2003. CO2 CARTRIDGES ARE NORMALLY REMOVED FOR WEIGHT CHECK AND REINSTALLED AS PART OF ROUTI NE INSPECTION REQUIREMENTS. PROBABLE CAUSE FOR FAILURE TO RE-INSTALL IS LAPSE OF FOCUS ON DETAILS OF MAINT BEING PERFOR MED. (K) 2 L 7 2 4F RT A10CE 20081201 NM 2008 12 1 DU4R2008264 1 20081123 A 5711 111A1141 REPAIR BOEING 737 737800* NM LT WING CRACKED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 171LF 30637 DURING SCHEDULED INSPECTION, FOUND A TEMPORARY REPAIR AT LBL 33 AND LBL 41 CRACKED AND REQUIRING REPAIR. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAA2008112092096 1 20081114 A 5320 FLOOR SUPPORT BOEING 767 7672B7ER 1385107 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 253AY 24894 BFM - C4 - MAJOR REPAIR - CABIN FLOOR SUPPORT INBOARD ANGLE IS CRACKED IN HALF AT BS 303, RBL 54.75. REPAIRED CABIN FLO OR SUPPORT INBOARD ANGLE AT BS 303, RBL 54.75 IAW B737 SRM 51-40-02 & 51-21-01. 2 L 7 2 4F RT A1NM 20081201 CE 2008 12 1 ZESA2008007 1 20081016 A 3243 CV02259AND9R3864 CHECK VALVE CESSNA 500 550 2076604 CE NLG WW CHATTERING E ZESA K NONE E VIBRATION/BUFFET CL CLIMB 1 EA 03 824CB 0824 VIBRATION EVIDENT WITH CHANGES IN AIRSPEED, PRESSURIZATION AND GEAR RETRACTION. TROUBLESHOT SYS WITH TECH REP AND FOUND BRAKE RESERVOIR PRESSURIZATION CHECK VALVE VIBRATING DURING OPERATION. CHANGED CHECK VALVE AND RELIEF VALVE THEN PRESS URIZED CABIN. NO FAULTS NOTED. OPS CHECK FLIGHT PERFORMED AND ALL SYS CHECKED GOOD. 1 L 7 2 4F A22CE 20081202 NM 2008 12 2 USAA2008112492114 1 20081122 A 5330 6545776 SKIN BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - RON - MAJOR REPAIR - CRACK FUSELAGE SKIN AT BS 727E +9 INCHES, S26R. REPAIRED FUSELAGE SKIN IAW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 20081202 CE 2008 12 2 AWKA7741118 1 20081114 A 2150 73838433 ACM CESSNA 750 750 2076810 CE ZONE 200 LEAKING E AWKA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 WP 25 774XJ 28 7500274 SHORTLY AFTER TAKEOFF, 3 TO 5 MINUTES. A PASSENGER REPORTED STEAM/SMOKE VAPOR WAS ACCUMULATING IN THE CABIN. THE COCKPIT CREW BEGAN DETECTING ODOR AND LOOKING BACK IN THE CABIN SEEING INCREASING SMOKE/VAPOR LEVELS. THE PILOTS DECIDED TO RE TURN AND NOTIFIED DEPARTURE OF INTENTIONS. WHILE ON VECTORS FOR RETURN, THE CREW PLACED BOTH PACKS IN MANUAL TEMP CONTR OL AND WERE ABLE TO CONTROL BOTH PACKS MANUALLY. THE SMOKE BEGAN TO DIMINISH AS ENGINE POWER WAS REDUCED FROM CLIMB TO I DLE FOR DECENT. AN EMERGENCY WAS NOT DECLARED DUE TO SMOKE DIMINISHING, BUT, A RETURN FOR PRECAUTIONARY REASONS WAS DE CLARED. THE COCKPIT AIRCYCLE MACHINE WAS FOUND TO BE FAULTY AND WAS REPLACED. OPS CHECKS NORMAL, NO SMOKE WAS DETECTED 2 L 7 2 4J RT T00007WI 20081202 CE 2008 12 2 DJFA2008081 1 20080710 A 3241 42901 CONTROL UNIT BEECH MU300 400A 1155402 CE ANTI-SKID SYSTEM FAILED E DJFA H DEACTIVATE SYST/CIRCUITS O OTHER LD LANDING 1 EA 23 464LX RK453 ON LANDING BRAKES DID NOT RESPOND WHEN INITIALLY APPLIED. BRAKES ENGAGED AFTER A FEW MOMENTS BUT FAILED AGAIN WHILE DEC ELERATING BETWEEN 10 AND 15 KNOTS. CREW DISENGAGED THE ANTI-SKID SYS AND BRAKING RETURNED TO NORMAL. MAINT FOUND THE AN TI-SKID CONTROL BOX FAILED. THE UNIT WAS REPLACED. 2 H 7 2 4F RT A16SW 20081202 NM 2008 12 2 YENA200811180112 1 20081111 A 2150 17018554401 SUPPORT EMB ERJ190 ERJ190100IGW 3260408 NM NR 2 PACK BROKEN A YENA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 EA 15 289JB 3090 19000002 FLT 1114, MCO-RIC, AIR RETURN TO MCO AT FL 390, HEARD LOUD NOISE SIMILAR TO NOISE REDUCTION HEADSETS TURNING ON AND OFF. FLIGHT ATTENDANTS REPORTED LOUD BANG COMING FROM AFT OF AIRPLANE. CABIN ALT WAS RISING RAPIDLY WITH A HIGH CABIN RATE OF CLIMB. SHORTLY EICAS SHOWED CABIN ALT HIGH WITH MASTER WARNING. OFC WAS FULL CLOSED AND PACK (PSI) WAS NORMAL WITH GREEN LINES ON MFD ECS PAGE. PERFORMED QRH CABIN ALTITUDE HI PROCEDURES. CABIN ALT REACHED APRX 13,500 FT. REACHING 10,000 MSL, FLIGHT ALT CABIN PRESSURIZATION STABILIZED AND STARTED TO PRESSURIZE TO APRX 500 FT. FOUND NR 2 PACK OUTLET DUCT BELLOWS SLIPPED OFF AND A BROKEN PACK OUTLET DUCT SUPPORT ROD ASSY. RESECURED NR 2 PACK BELLOWS AND REMOVED AND R 2 L 7 2 4F RT A57NM 20081202 NM 2008 12 2 YENA200811190113 1 20081111 A 2120 19055782401 DUCT EMB ERJ190 ERJ190100IGW 3260408 NM NR 2 PACK CRACKED A YENA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 289JB 3091 19000002 FL 662, MCO-BUF, AIR RETURN TO MCO. CLIMBING THROUGH 32,000 CABIN ALT WAS 8400 AND CLIMBING. CREW EXECUTED CABIN ALT H IGH PROCEDURE. CABIN ALT HIT 10,000 WITH A CABIN ALT EICAS. OUTFLOW VALVE WAS CLOSED. NO NOISES. PACK INDICATION NOR MAL. ON DESCENT CABIN ALT STAYED BELOW 10,000 THROUGH THE REMAINDER OF THE FLIGHT. THE CABIN ALT AND CABIN RATE FLUCTU ATED. PERFORMED FIM TASK 21-31-00-810-818-A. FOUND NR 2 PACK OUTLET DUCT CRACKED AND CONDITIONER AIR CHECK VALVE BELLO WS RUPTURED. REMOVED AND REPLACED NR 2 PACK OUTLET DUCT AND CHECK VALVE BELLOWS PER AMM 21-51. OPS CHECKS AND LEAK CHE CKS OK. PRESSURIZATION CHECKS GOOD. REF 21-31-00. 2 L 7 2 4F RT A57NM 20081202 EU 2008 12 2 USAA2008112692133 1 20081114 A 5320 D5348004320 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON LOWER SILL OF L2 DOOR AT FR66 , Y1732. REPAIRED LOWER SILL OF L2 DOOR A T FR66, Y1732 IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008120192162 1 20081118 A 5320 D53471124201 SHEAR PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, -Y1732. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, -Y1732 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081202 WP 2008 12 2 NWAA084849853 1 20081103 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 762NC 47710 DURING LINE CHECK MX FOUND THAT THE RT SIDE EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MX REPLACED THE BATTERY PAC K AND THE LIGHTS RETURNED TO AN OP CONDITION. 2 L 7 2 4F RT A6WE 20081202 NM 2008 12 2 UALA2008111305437 1 20080823 A 3350 363674 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 ROW 1 RT EEL STRIP INOP. FOUND LOOSE LIGHTS. ADJUSTED LOOSE LIGHTS. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081202 NM 2008 12 2 UALA2008111305439 1 20080823 A 3350 363674 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 ROW 5 RT EEL STRIP INOP. FOUND LIGHTS INOP. SPLICED IN EEL POWER STRIP. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081202 NM 2008 12 2 DXTA2008120103380 1 20081130 A 2700 UNKNOWN AMD FALC50 FALCON2000 2730170 NM UNKNOWN E DXTA A UNSCHED LANDING F FLT CONT AFFECTED DE DESCENT 1 GL 07 275QS 075 ACFT WAS DESCENDING THROUGH FL 380 WHEN FLYING PILOT MOMENTARILY LOST PITCH CONTROL. 2 L 7 2 4F RT A50NM 20081202 CE 2008 12 2 DXTA2008120103381 1 20081130 A 2120 UNKNOWN CESSNA 560 560XL 2076702 CE COCKPIT ODOR E DXTA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 07 639QS 5605139 WITH APU OPERATING AND AVIONICS SWITCH ON I NOTICED A BURNING ODOR. 2 L 7 2 4F RT A22CE 20081202 GL 2008 12 2 S8Y2008F00001 1 20081110 A 7820 14836001 MUFFLER CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO ENGINE WARPED E S8YA O OTHER O OTHER NR NOT REPORTED 1 EA 27 519SR 284 2072 689850 ORIGINAL EQUIPMENT INSTALLED NEW AT FACTORY. FUND BY VISUAL INSPECTION AT THIRD 100 HR INSPECTION CYCLE. MUFFLER CONE/ BAFFLE SAGGING AND WARPED. DOWN LOAD OF RECENT ENGINE DATA, EGT/CHT, SHOWS NO ANOMALIES THAT WOULD HAVE CAUSED DEFECT. (K) 1 L 7 1 3O 3 O NT A00009CH E3SO 20081202 2008 12 2 BSY2008F00009 2 20080925 A 8550 S9413117 O-RING LEAR 35 35A 5170602 CE DIP STICK CUT E BSYA O OTHER K FLUID LOSS NR NOT REPORTED 1 GL 07 25AN 35A259 AIRCRAFT ENROUTE, WHEN PILOT NOTICED A DROP IN OIL PRESSURE LT ENGINE. SHUTDOWN ENGINE LANDED, NO PROBLEMS. MAINT FOUN D OIL DIP STICK, O-RING CUT, REMOVED AND REPLACED O-RING. (K) 2 L 7 2 4F A10CE 20081202 CE 2008 12 2 BSY2008F00008 1 20081021 A 3700 442CW12 PUMP BEECH 58 58 1152740 CE VACUUM SYSTEM FAILED E BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 21ES TH1123 LT ENGINE DRIVEN VAC PUMP FAILED THE SCREW FOR CHECKING WEAR WAS MISSING CAUSING PREMATURE FAILURE. (K) 1 L 7 2 3O 3A16 20081202 2008 12 2 BSY2008F00003 4 20080910 A 3421 060001700 INDICATOR CESSNA 208 208B 2073701 CE ATTITUDE ERRATIC E BSYA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 104AN 208B0918 AFTER TAKEOFF, PILOTS ATTITUDE INDICATOR WOULD NOT STAY ERRECT, RETURNED TO DEPARTURE, REMOVED AND REPLACED INDICATOR. OPS CHECKED GOOD. (K) 1 H 7 1 3T A37CE 20081202 NM 2008 12 2 UALA2008112106610 1 20081121 A 3397 794640 POWER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 EMERGENCY FLOOR PATH LIGHTING LEFT AISLE FIRST LIGHT IN FIRST CLASS CABIN IS INOP. REPAIRED POWER FEED LINE. OPS CHECK S GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081202 NM 2008 12 2 UALA2008111306373 1 20081104 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 528UA 25018 FLIGHT ATTENDANT REPORTED EEL TRACK COVER BROKE. FOUND EEL LIGHT OUT BETWEEN ROW 14ABC TO 20ABC. REPLACED MISSING EEL SEGMENT AND SECURED LOOSE CONNECTORS. REPLACED BROKEN COVER. 2 L 7 2 4F 4 F RT A2NM E17NE 20081202 NM 2008 12 2 UALA2008111306374 1 20081104 A 5210 ROLLER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT UPPER DOOR DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 RT UPPER DECK DOOR WILL NOT ARM FOR DEPARTURE. CLEANED ROLLERS AND SLIDE OF ARMING TEE. CLEANED ARMING FORK. CYCLED D OOR AND ARMING IS NOW NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081202 NM 2008 12 2 UALA2008112406614 1 20081118 A 5312 PRESSURE PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT PRESSURE DECK BS 1681.8 AT RBL 42" AND RBL 52" HAS CORROSION DAMAGE. MAJOR REPAIR ACCOMPLISHED. REMOVED PREVIOUSL Y INSTALLED REPAIR DOUBLER-TRIPLER. FABRICATED A NEW REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 20081202 NM 2008 12 2 UALA2008112406619 1 20081121 A 3350 363674 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 648UA 25285 EEL FLOOR PATH LIGHTING AT RT MID LAV ARE INOP. REPLACED EEL LIGHT, CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081202 NM 2008 12 2 UALA2008112406624 1 20081122 A 5315 STIFFENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 CABIN FLOORBEAM STIFFENER CRACKED AT BS 246, APPROX LBL 40, ABOVE CONTROL CABLE A1A. MAJOR REPAIR ACCOMPLISHED. INSTAL LED NEW STIFFENER, P/N 141T5282-2. 2 L 7 2 4F 4 F RT A1NM E24NE 20081202 2008 12 2 UALA2008112406625 4 20081122 A 2565 HOUSING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 RT OVERWING ESCAPE SLIDE DISCONNECT HOUSING CRACKED. REPLACED DISCONNECT HOUSING. 2 L 7 2 4F 4 F RT A1NM E24NE 20081202 CE 2008 12 2 BSY2008F00014 1 20080917 A 3230 9581001723 GEARBOX BEECH 58 58 1152740 CE LANDING GEAR FAILED E BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 62500 TH1347 PILOT SELECTED GEAR DOWN AND THE CIRCUIT BREAKER POPPED, PILOT THEN HAND CRANKED GEAR DOWN WITH DIFFICULTY. MAINT FOUND GEAR BOX HAD A LOT OF FRICTION INSIDE GEAR BOX. REMOVED AND REPLACED GEAR BOX AND MOTOR. OPS CHECKS GOOD. (K) 1 L 7 2 3O 3A16 20081203 NM 2008 12 3 AALA200820045 1 20081103 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 604AA 43723 27055 AFT MAIN DECK PLATE DOUBLER CORRODED. INSTALLED NEW DOUBLER IAW SRM 53-60-51-2R. 2 L 7 2 4F RT A2NM 20081203 NM 2008 12 3 AALA200820046 1 20081103 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 604AA 43723 27055 AFT MAIN DECK PLATE CORRODED. INSTALLED REPAIR DOUBLER IAW SRM 53-60-51-2R. 2 L 7 2 4F RT A2NM 20081203 WP 2008 12 3 AALA200702732 1 20081013 A 2750 4956160 SPRING DOUG DC9 DC983 3022083 WP FLAP CONTROL BROKEN A AALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 9624T 53594 DFW - FLAP/SLAT HANDLE WOULD NOT LOCK IN THE UP/RETRACT POSITION. TRIGGER ON LEFT SIDE OF HANDLE WILL NOT GO DOWN. RET URNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED BROKEN SPRING ON LEFT SIDE OF FLAP HANDLE. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A6WE 20081203 NM 2008 12 3 AALA200802735 1 20081014 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 617AM 24525 DFW - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081203 SO 2008 12 3 FDKA2008111400294 1 20081114 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 837MJ 145367 FRL FLT 6217 ROC-CVG - EMERGENCY EXIT LIGHT ABOVE OVERWING DOORS AND FLOOR STRIPS AT ROW 8-10 ARE INOP. AIRCRAFT FERRIE D TO CVG WHERE MAINTENANCE REPLACED ALL BATTERIES. 2 L 7 2 4T RT T00011AT 20081203 NM 2008 12 3 AALA200802727 1 20081012 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW - EMERGENCY PROXIMITY LIGHTS AT SEAT ROWS 20G TO 26G FAILED TEST. REPLACED BATTERY PACK AT RIGHT NUMBER THREE DOOR FOR EMERGENCY PROXIMITY LIGHTS AT SEAT ROWS 20G TO 26G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081203 NM 2008 12 3 AALA200802737 1 20081014 A 3350 SIGN BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 617AM 24525 DFW - EMERGENCY LIGHT EXIT PLACARD DAMAGED AT RIGHT AFT OVERWING. REPLACED EMERGENCY LIGHT EXIT PLACARD AT RIGHT AFT OV ERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081203 NM 2008 12 3 AALA200820047 1 20081103 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 604AA 43723 27055 AFT MAIN DECK PLATE CORRODED. REPAIRED IAW SRM 53-60-51-2R. 2 L 7 2 4F RT A2NM 20081203 2008 12 3 BSY2008F00001 4 20080904 A 2300 069102000 RADIO BEECH 58 58 1152740 CE COMM SYSTEM MALFUNCTIONED E BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 78DM TH281 ACFT COMING IN, NR 1 COMM INAUDIBLE AND NR 2 COMM RECEIVER FAOS. REMOVED AND REPAIRED NR 1 AND NR 2 COMM. OPS CHECKS G OOD. (K) 1 L 7 2 3O 3A16 20081203 SO 2008 12 3 VOX2008F00000 1 20081125 A 2421 BELT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA LT ALTERNATOR BROKEN E VOXA O OTHER O OTHER NR NOT REPORTED 1 NM 03 850ST 317305080 RT ALTERNATOR BELT BROKE, LT BELT LOOSE TO CARRY ELECTRICAL LOAD. (K) 1 L 7 2 3O 3 O A20SO E14EA 20081203 NM 2008 12 3 DXTA2008120103375 1 20081127 A 2120 UNKNOWN AMD FALC50 FALCON2000 2730170 NM COCKPIT ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 213QS 113 ON DESCENT BOTH PILOTS NOTICED STRONG ELECTRICAL BURNING ODOR IN COCKPIT. 2 L 7 2 4F RT A50NM 20081203 NE 2008 12 3 HNAA2008120200325 2 20081108 A 7261 311289501 FILTER ELEMENT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE SLOW A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 933HA 47742 3784 134 120709 NR 1 OIL PRESSURE LIGHT ILLUMINATED ON TAKEOFF ROLL WITH FLUCTUATION ON PRESSURE GAUGE. REJECTED TAKEOFF, LIGHT EXTINGU ISHED REMAINED NORMAL. CONTRACT MAINTENANCE REPORTS SAFETY ON TRANSMITTER BROKEN AND CONNECTOR OIL SOAKED. CLEANED AND SERVICED ENGINE WITH 2 QTS OF OIL. PERFORMED HIGH POWER AND HIGH SPEED TAXI ALL INDICATIONS REMAIN NORMAL THROUGH ALL ABOVE STEPS. PLANE RELEASED FOR FERRY FLIGHT FROM ROC TO MDT. C/W LOW OIL PRESS IN PWMM 05-50-00. NO DEBRIS FOUND. I NSTALLED NEW OIL FILTERS, NO EXTERNAL LEAKS FOUND ON ENGINE AFTER GROUND RUN. OPS AND LEAK CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E20NE 20081203 SO 2008 12 3 RAIA2008112500001 1 20081121 A 3610 S2D226 SEAL EMB 145 EMB145 3260210 SO BLEED AIR SYS WORN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 820HK 145064 DURING CLIMBOUT, CREW RECEIVED A NR 1 BLEED LEAK MESSAGE ON THE EICAS AND A LOUD POPPING NOISE IN BACK OF THE AIRCRAFT W ITH ASSOCIATED BAD SMELL IN CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A LEAKING BLEED COUPLING AND SEAL. THE SEAL WAS REPLACED AND NO OTHER DEFECTS NOTED. 2 L 7 2 4F RT T00011AT 20081203 NM 2008 12 3 08FDEA04956 1 20081121 A 5315 65208371 FLOORBEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 469FE 21581 CORROSION ON FLOORBEAM BETWEEN BL0 AND RBL25 STA 1110. FOUND CORROSION OUT OF LIMITS, CUT OUT DAMAGED SECTION DIMS 2 3/ 4 INCH BY 2 1/2 INCH. FABRICATED REPAIR ANGLES USING BAC1490-2785 PO NR 9007702 DIMS 11 3/4 INCH BY 2 1/2 INCH AND BAC 1490-2831 PO NR 9006081 DIMS 7 1/2 INCH BY 3 INCH, FILLER USING BAC1505-100617 PO NR 8270109 DIMS 2 3/4 INCH BY 2 1/2 IN CH REPAIR STRAPS USING 7075-T6 .050 PO NR 9007861 DIMS 11 3/8 INCH AND 8 1/2 INCH. INSTALLED REPAIR PARTS IAW FEDEX DWG SR27-53-034. 2 L 7 3 4F A3WE 20081203 EU 2008 12 3 08FDEA04958 1 20081121 A 5321 FLOOR PANEL AIRBUS 300 A300B4622 3930401 EU CARGO BAY PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 THE BULKPIT FLOOR PANEL 161 GF IS PUNCTURED. 2 L 7 2 4F RT A35EU 20081203 NM 2008 12 3 08FDEA04959 1 20081121 A 5322 65561222 SHEAR TIE BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 FOUND AFT PIT FRAME SHEAR TIE REPAIR LOCATED AT APPROX BS 950D STR S-29L TO S-28L. REPAIR REQUIRES EVALUATION FOR MAJOR /MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING APPROVED DATA. ACCOMPLISHED REPAIR AT BS 950D STR 29L TO S28L FRAME SHEAR TIE. ACCOMPLISHED USING FAA APPROVED DATA AS A MAJOR REPAIR. REF SRM 53-10-4 PG 58-60 FIG 15 AND REPA IR 3. HFEC C/S HOLES AT SKIN SHEAR TIE IAW 727 NDT MAN, PART 6,53-39-00 FIG 3 (NO EFECTS NOTED). THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 UALA2008120906794 1 20081209 A 5210 2603830004 CABLE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE R3 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 795UA 26927 DOOR 3R WOULD NOT DISARM ON ARRIVAL. DOOR DISARMED AND ARMED NORMALLY AFTER 10 MINUTES. DOOR HAS HISTORY AND WAS LIBER ALLY COATED IN ICE RELEASE AND DOOR HEATER TEST NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081203 NM 2008 12 3 08FDEA04964 1 20081124 A 5730 648342 SKIN PANEL BOEING 727 7272D4 138407U NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 WHILE ACCOMPLISHING "OK TO WORK" STEP ON SNRM (N00791)) FOUND WING L/E SKIN CRACKED (LT WING) AT FSS 122, LWR SURFACE OF SKIN. REMOVED AND REINSTALLED ANTI-ICE DUCT (LT L/E WING ROOT) REF MM 36-00-001-2, LEAK CHECK GOOD. REPAIRED CRACK RE F SRM 57-30-4 FIG 8. THIS IS CLASSIFIED AS A MINOR REPAIR TREATED AND PRIMED REF SRM 51-10-2. 2 L 7 3 4F A3WE 20081203 EU 2008 12 3 08FDEA04967 1 20081124 A 5320 FITTING AIRBUS 300 A300B4622 3930401 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 MAIN CABIN, AT FRAME 48 AND GANTRY 4 RT, SEAT TRACK, "LINAGE FITTING" IS CRACKED, UNDER FLOOR. 2 L 7 2 4F RT A35EU 20081203 NM 2008 12 3 08FDEA04971 1 20081124 A 5347 BAC1520792 SEAT TRACK BOEING 757 75728A 1384976 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 912FD 24260 SEAT TRACK BS 418-440, RBL 45, IS GOUGED AND CORRODED. REMOVED CORROSION FROM SEAT TRACK, BS 418-440, RBL 45, IAW SRM 53 -00-52. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-52. .021 INCH MATERIAL REMOVED. REMOVED SEAT TRACK, BS 418-4 40, RBL 45, IAW SRM 51-40-02. RECEIVED NEW SEAT TRACK ON MAE TRAVELER NR T8/769433. LOCATED, DRILLED, TREATED AND PRIM ED AND PAINTED NEW SEAT TRACK, BS 418-440, RBL 45, IAW SRM 51-40-02/51-20-01. INSTALLED NEW SEAT TRACK, BS 418- 440, R BL 45, IAW SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING. 2 L 7 2 4F RT A2NM 20081203 NM 2008 12 3 FDEA200811254976 1 20081125 A 5320 65198615 BEAM BOEING 727 727225 1384077 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 469FE 21581 E/E COMPT HORIZ WALKWAY BEAM HAS CORROSION WITH EXFOLIATION LBL 12 BS 32. REMOVED CORROSION AND FOUND OUT OF LIMITS, RE MOVED LT LWR CHORD AND INSTALLED NEW LWR CHORD PART NUMBER 5715216 PO NR 827075 AT E/E COMPT STA 328 LBL12 IAW SRM 51- 30-02. 2 L 7 3 4F A3WE 20081203 EU 2008 12 3 FDEA200811264982 1 20081126 A 5711 A5724196000500 FITTING AIRBUS 300 A300B4622R 3930312 EU LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 LEFT WING HOLE " D " OF EO 6-5710-7-5005 P1 SHOWS A CRACK INDICATION APPROX 1/16 LONG. COMPLIED WITH FEDEX EA 6-5710-12 3673, WINGS - AD 99-16-01 - EO 6-5710-7-5005 - LT WING REAR SPAR, MLG FWD PICK-UP FITTING BOLT HOLE "D". 2 L 7 2 4F RT A35EU 20081203 NM 2008 12 3 FDEA200811264978 1 20081126 A 5315 6516338180 BEAM BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 CABIN FLOORBEAM, UPPER CAP LOWER SURFACE, CORRODED AROUND NUTPLATE, STA 950 RBL 5 BLENDED AREA TO REMOVE CORROSION, ORIG INAL MAT .150, LOSS .035 REMAINING .115 AND FOUND TO BE OUT OF LIMITS REF SRM 53-10-1. OBTAINED EA 7-5310-123812. FOUN D MORE CORROSION DURING FLAP PEEN. REMOVED CORROSION ORIG .150 LOSS .046 REMAINING .104, OBTAINED REVISION TO EA 7-5310 -123812 FLAP PEENED AREA TREATED AND PRIMED AREA REF EA 7-5310-123812. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081203 EU 2008 12 3 FDEA200811295035 1 20081129 A 5531 A5517770320200 SPAR AIRBUS 300 A300B4622 3930401 EU VERTICAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 RT THS REAR SPAR UPPER TEE CAP UPPER SURFACE HAS CORROSION BETWEEN RIB 14 - 15. REMOVED CORROSION IAW A300-600 SRM 51-7 4-10. ORIG THICKNESS .080 IAW AIRBUS DWG A55177703. MAT REMAINING .054. FOUND AREA TO BE OUT OF LIMITS IAW A300-600 S RM 55-10-00 PG 106 TOOL: T8225T, REPAIRED AREA IAW A300-600 SRM 55-11-21 FIG 212. 2 L 7 2 4F RT A35EU 20081203 NM 2008 12 3 FDEA200812015036 1 20081201 A 7931 1163P182 PRESSURE SWITCH BOEING 727 727227 1384078 NM PWA JT8 JT8D15A 52051 NE ENGINE MALFUNCTIONED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 21 492FE 41798 41798 21530 695358 NR 1 ENGINE SHUT DOWN IN FLIGHT DUE TO LOW PRESSURE/FILTER BYPASS LIGHT. COMPLIED WITH QRH ENGINE WINDMILLED 2 MIN PRI OR TO SHUT DOWN. OIL PRESSURE AT APPROX 40 PSI. FOUND FAULTY LOW OIL PRESS SWITCH, REMOVED AND REPLACED SWITCH IAW MM 79-34-001-4, ALSO CLEANED CONNECTORS ON LOW OIL PRESS SWITCH AND FILT BYPASS PRESS DIFF SWITCH RAN ENGINE AND PERFORMED LEAK CHECK OF SWITCHES, NO LEAKS NOTED AND LIGHT IS OPERATING NORMALLY AT THIS TIME. 2 L 7 3 4F 4 F A3WE E2EA 20081203 NM 2008 12 3 FDEA200812025038 1 20081202 A 5720 65249661 ANGLE BOEING 727 7272S2F 1384O81 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 213FE 22935 CRACKED LOWER ANGLE FALSE SPAR AT SPOILER NR 8 RT WING. REMOVED SPAR DOUBLER & INBD WEB SECTION IAW SRM 51-30-2. FABBE D NEW DOUBLER IAW SRM 51-30-2 & DWG NR SR 27-57-038 REV C. FABBED NEW INBD WEB SECTION IAW DWG NR SR 27-57-038 REV C & SRM 51-30-2. FABBED 2 ANGLES IAW DWG NR SR 27-57-038 REV C & 51-30-5. HEAT TREATED NEW DOUBLER & HEAT TREATED NEW ANGL ES IAW NDTM PT 6 51-00-00 FIG 20 & ER 2-37153-801 REV A. CUT LOWER SECTION IAW DWG NR SR27-57-038 REV C. FABBED INBD L OWER SECTION IAW DWG NR SR 27-57-038 REV C & SRM 51-30-5. FABBED NEW STRAP IAW DWG NR SR 27-57-038 REC C & SRM 51-30-5. TREATED PRIMED REPAIR PART IAW SRM 51-10-2 & INSTALLED REPAIR PART IAW DWG NR SR27-57-038 REV C. 2 L 7 3 4F A3WE 20081203 2008 12 3 FDEA200812025040 4 20081202 A 3414 2083121 INDICATOR BOEING 727 727233 138408A NM COCKPIT FAILED A FDEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 21 285FE 22622 REJECTED T/O AT 90KTS DUE TO NO AIRSPEED INDICATION ON CAPT SIDE. REMOVE AND REPLACED CAPTAINS AIRSPEED INDICATOR. REM OVE AND REPLACED CAPTAINS AIRSPEED INDICATOR. 2 L 7 3 4F RT A3WE 20081203 NM 2008 12 3 FDEA200812025046 1 20081202 A 5320 141N5160152 FLOOR SUPPORT BOEING 757 75723A 1384967 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 CABIN FLOOR, BS 310-324, RBL 43, CHANNEL IS CORRODED AROUND FASTENER HOLES. REMOVED FLOOR SUPPORT/CHANNEL IAW SRM 51-40- 02. FABRICATED NEW SUPPORT/CHANNEL ON MAE TRAVELER T8/759071. TREATED, PRIMED AND TOP COATED NEW SUPPORT/CHANNEL IAW S RM 51-20-01 AND AMM 51-21-00. LOCATED AND DRILLED NEW SUPPORT/CHANNEL IAW SRM 51-40-02. INSTALLED NEW SUPPORT/CHANNEL, BS 310-324, RBL 43, IAW SRM 51-10-02. CORROSION WAS OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3. (L=2.2 INCH, W= 2.0 INCH, D=.018 INCH). THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20081203 EU 2008 12 3 FDEA200812025048 1 20081202 A 5730 A5724240920000 PANEL AIRBUS 300 A300B4622 3930401 EU LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 LT WING T/E PANEL NR 575DB HAS FRETTING CORROSION, WORN AREAS, AROUND FASTENER MATTING SURFACE AFT OF RIB 7A. REPAIRED LT WING T/E PANEL 575DB BY BONDING A PICTURE FRAME DOUBLER TO PANEL IAW EA 6-5750-123683 AND SRM 51-77-10. REMOVED AND REATTACHED PANEL TO ACFT IAW SRM 51-40-21 PARA 5. 2 L 7 2 4F RT A35EU 20081203 NM 2008 12 3 AALA200810238 1 20081120 A 3211 TRUNNION BOEING 737 737823 13844BZ NM LT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948AN 30086 LEFT FORWARD TRUNNION FITTING OUTBOARD FACE ON LEFT MAIN LANDING GEAR HAS CORROSION. ACCOMPLISHED REPAIR IAW SRM 57-20- 90-2R-2. 2 L 7 2 4F RT A16WE 20081203 NM 2008 12 3 AALA200810239 1 20081120 A 3211 TRUNNION BOEING 737 737823 13844BZ NM LT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948AN 30086 LEFT FORWARD MAIN LANDING GEAR TRUNNION UPPER FACE OUTBOARD SIDE HAS CORROSION. ACCOMPLISHED REPAIR IAW SRM 57-20-90-2R -2. 2 L 7 2 4F RT A16WE 20081203 WP 2008 12 3 AALA200810220 1 20081106 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 WEB CRACKED AT NUTPLATE, STATION 1215 LONGERON 28R. STOP DRILLED CRACK AND REPAIRED PER ESO 80559 DATED 11-06-08. 2 L 7 2 4F A6WE 20081203 NM 2008 12 3 AALA200810241 1 20081120 A 3211 TRUNNION BOEING 737 737823 13844BZ NM LT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948AN 30086 LEFT FORWARD TRUNNION FITTING INBOARD UPPER FACE ON LEFT HAND MAIN GEAR CORRODED. REPAIRED PER SRM 57-20-90-2R-2. 2 L 7 2 4F RT A16WE 20081203 EU 2008 12 3 08FDEA04966 1 20081124 A 5320 FITTING AIRBUS 300 A300B4622 3930401 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 MAIN CABIN, AT FRAME 48 AND GANTRY 4 LT, SEAT TRACK, "LINKAGE FITTING" IS CRACKED, UNDER FLOOR. REMOVED AND REPLACED TH E SEAT TRACK LINK FITTING IAW SRM 51-40-21, PARA 5. 2 L 7 2 4F RT A35EU 20081203 NM 2008 12 3 08FDEA04969 1 20081124 A 5210 DOOR FRAME BOEING 757 757236 1384971 NM L1 DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 L-1 DOOR, AFT -SIDE, FRAME EXFOLIATED BELOW DOOR ASSIST HANDLE. REPAIRED DAMAGED FRAME, L-1 DOOR, AFT-SIDE, BELOW DOOR ASSIST HANDLE, IAW SRM 51- 70-11. ALL PARTS REMOVED FOR ACCESS WERE RE-INSTALLED IAW SRM 51-40-02. ALL REPAIR PARTS INSTALLED IAW SRM 51-70-11. THIS IS A CAT "A" MAJOR REPAIR, WITH NO FOLLOW UP TRACKING. 2 L 7 2 4F RT A2NM 20081203 SO 2008 12 3 RAIA2008120100002 1 20081130 A 3610 DUCT EMB 145 EMB145LR 3260212 SO BLEED AIR SYS LOOSE A RAIA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 CE 03 840HK 145341 DURING CLIMB FROM TAKEOFF, CREW RECEIVED A BLEED NR 1 AND NR 2 LEAK MESSAGE ON THE EICAS. MAINTENANCE RESECURED LOOSE A NR 2 BLEED LINE DUCT UNDER THE CARGO FLOOR. BLEED SYSTEM, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081203 EU 2008 12 3 08FDEA04957 1 20081121 A 5321 FLOOR PANEL AIRBUS 300 A300B4622 3930401 EU CARGO BAY PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 THE BULKPIT FLOOR PANEL 161 BF IS PUNCTURED. REPAIRED PUNCTURE ON FLOOR PANEL 161 BF IN REF TO A300-600 SRM 53-10-20, S TEP 10A. 2 L 7 2 4F RT A35EU 20081203 NM 2008 12 3 08FDEA04960 1 20081122 A 5320 651633512 BRACKET BOEING 727 7272D4 138407U NM RT MLG WW CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 RT MLG W/W CUTOUT SEAL BEAM (STR 19R), AREAS OF CORROSION ON TOP SIDE OF BEAM FROM FS 906 TO FS 930, RBL 74, WL 105 REMO VED CORROSION FROM BRACKET, STA 920 ORIG T .094, REMAINING T .071, .023 MATERIAL LOSS OUT OF LIMITS. REPLACED BRACKET STA 920. REMOVED CORROSION FROM BEAM, ORIG T .080' REMAINING T .076. .004 MATERIAL REMOVED WITHIN ALLOWABLE DAMAGE. R EF SRM 51-30-2 PG 1-7, SRM 53-10-1 PG 2A, AMM 51-20-021-7 PG 1-3, AMM 51-20-151-7 PG 1, THIS IS CLASSIFIED AS A MINOR RE PAIR. 2 L 7 3 4F A3WE 20081203 EU 2008 12 3 FDEA200812015032 1 20081201 A 5321 A4600003434100 FLOORBOARD AIRBUS 300 A300B4622 3930401 EU CABIN BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 CABIN FLOOR BOARD BROKEN IN 3 PIECES, BETWEEN FR 47 - 51, 4TH BOARD FROM LEFT. FABRICATED NEW FLOOR BOARD USING OLD BOA RD AS TEMPLATE IAW FEDEX DWG SRZ 25- 005 REV G. 2 L 7 2 4F RT A35EU 20081203 NM 2008 12 3 FDEA200812025037 1 20081202 A 5270 ACTUATOR BOEING 727 7272S2F 1384O81 NM DOOR WARNING BROKEN A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 21 204FE 22926 AFT AIRSTAIR LIGHT ILLUMINATED IN-FLIGHT CLIMBING THROUGH 4,500 FEET. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B. A MBER AFT AIRSTAIR DOOR WARNING LIGHT INOP." REPLACED WARN RT HAND UPLOCK ROLLER FITTING PER SMP, FOUND SWITCH S395 ROLL ER ACTUATOR BROKEN AND SWITCH INOP. REPLACED S395 AND ROLLER ACTUATOR PER WDM 52-71-01 AFT AIRSTAIR OPERATION AND ALL INDICATIONS CK OK PER MM 52-62-001-5 2 L 7 3 4F A3WE 20081203 EU 2008 12 3 FDEA200812025039 1 20081202 A 5230 A5237416020800 SKIN AIRBUS 300 A300B4622R 3930312 EU AFT CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 AFT CARGO DOOR INTERNAL SKIN CORRODED AT FWD LWR CORNER. THIS SDR IS GEN TO REFLECT CORRECTIONS MADE IN CORRECTIVE ACTI ON BLOCK FROM ORIG SDR 08-4756. REMOVED CORROSION IAW A300-600 SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW A300-600 SR M 51-30-00. ORIGINAL MATERIAL 0.063. REMAINING MATERIAL 0.051. MATERIAL REMOVED 0.011. USED UT GAUGE T8225Q. REMOVE D AND RE-INSTALLED PANELS 812 AR AND BR; 154 AR; BR; CR IAW A300-600 AMM 52-72-11-5. REMOVED AND RE-INSTALLED SEAL RETA INER IAW A300-600 AMM 52-30-18-4. REMOVED AND REINSTALLED CAPS AND INSTALLED NEW SKIN IAW A300-600 SRM 51-72-10. MATER IAL ID 2024-T3, 0.063, PO 633758.6 IAW A300-600 SRM 52-32-00. ALODINED IAW A300-600 SRM 51-21-10. PRIMED IAW A300-600 2 L 7 2 4F RT A35EU 20081203 NM 2008 12 3 FDEA200812025042 1 20081202 A 5320 141N5160322 FLOOR SUPPORT BOEING 757 75723A 1384967 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 CABIN FLOOR, BS 297, RBL 20-36.2, CHANNEL IS CORRODED AROUND FASTENER HOLES. REMOVED FLOOR SUPPORT AT BS 297, RBL 20-36 .2, IAW SRM 51-40-02. FABRICATED NEW SUPPORT ON MAE TRAVELER T8/759390. TREATED, PRIMED AND TOP COATED SUPPORT IAW SRM 51-20-01 AND AMM 51-21-00. LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-40-05. INSTALLED NEW SUPPORT, BS 297, RBL 20-36 .2, IAW SRM 51-40-02. CORROSION WAS DETERMINED TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3 (L=1.9 INCH, W=1 .0 INCH, D=.033 INCH). THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20081203 WP 2008 12 3 FDEA200812025047 1 20081202 A 3260 WARNING SYSTEM DOUG MD10 MD1010F 3022112 WP COCKPIT ACTIVATED A FDEA K NONE J WARNING INDICATION LD LANDING 1 CE 21 556FE 46710 LANDING MEM, 18R 3 UNSAFE (RED) GEAR LIGHTS WITH GEAR HANDLE DOWN, 3 UNSAFE ON CONFIG PAGE, QRH PROCEDURE DEPLOY ALT GEA R EXTENSION AND RECEIVED 3 GREEN SAFE (CONFIG AND GEAR). NOSEWHEEL STEERING RIGHT LIMITED TO 25 DEG. 2 L 7 3 4F RT A22WE 20081203 WP 2008 12 3 AALA200810218 1 20081106 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 CABIN FLOOR SUPPORT, INTERCOSTAL CRACKED AT STATION 1287 TO 1209. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-00. 2 L 7 2 4F A6WE 20081203 NM 2008 12 3 08FDEA04968 1 20081124 A 5712 64834219 RIB BOEING 727 7272D4 138407U NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 LT WING L/E RIB LWR CHORD HAS 2 CRACKS AT 5 INCH AND 18 INCH FROM SPAR, FSS 122. REMOVED PNL 6301 TO FOM. FABRICATED A NGLE REF DWG 64-8342-19 DRILLED-UP, TREATED, PRIMED, AND INSTALLED ANGLE REF SRM 51-30-5, MM 51-20-021, MM 51-20-051, AN D SRM 51-30-2. INSTALLED PANEL 6301 REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081203 NM 2008 12 3 08FDEA04970 1 20081124 A 5347 BAC1592792 SEAT TRACK BOEING 757 75728A 1384976 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 912FD 24260 SEAT TRACK BS 418-440, RBL 24, GOUGED AND CORRODED. AFTER EVALUATION, DAMAGE ON SEAT TRACK, RBL 24, BS 418-440, FOUND T O BE OUT OF LIMITS IAW SRM 53-00-52. REMOVED SEAT TRACK IAW SRM 51-40-02. RECEIVED NEW SEAT TRACK ON MAE TRAVELER NR T 8/769432. LOCATED AND DRILLED NEW SEAT TRACK, TREATED AND PRIMED AND PAINTED NEW SEAT TRACK IAW SRM 51-20-01. INSTAL LED NEW SEAT TRACK, BS 418-440, RBL 24, IAW SRM 51-40-02/53-00-52. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAI R WITH NO FOLLOW UP TRACKING. 2 L 7 2 4F RT A2NM 20081203 EU 2008 12 3 FDEA200811244967 1 20081124 A 5320 A5381206720000 FITTING AIRBUS 300 A300B4622 3930401 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 MAIN CABIN, AT FRAME 48 AND GANTRY 4 RT, SEAT TRACK, "LINAGE FITTING" IS CRACKED, (UNDER FLOOR) REMOVED SEAT TRACK SPLIC ES AND DAMAGED LINKAGE FITTING IAW A300-600 SRM 51-30-00. LOCATED AND DRILLED NEW LINKAGE FITTING IAW A300-600 SRM 51-3 0-40. INSTALLED NEW LINKAGE FITTING AND OLD SEAT TRACK SPLICES IAW A300-600 SRM 51-30-00 PART NR A5381206720000 PO NR 6 40729.3. 2 L 7 2 4F RT A35EU 20081203 WP 2008 12 3 FDEA200811254972 1 20081125 A 5210 62963 SOLENOID DOUG MD10 MD1010F 3022112 WP L1 DOOR DEFECTIVE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 46631 L-1 DOOR TORQUE TUBE SOLENOID NOT OPERATING PROPERLY. REMOVED AND REPLACED L-1 DOOR TORQUE TUBE SOLENOID AND ADJUSTED. OPS CHECKED GOOD IAW FEDEX MD 10 AMM 52-11-13-2 AND 52-11-00-5. 2 L 7 3 4F RT A22WE 20081203 EU 2008 12 3 FDEA200811264980 1 20081126 A 5712 A5724196000400 RIB AIRBUS 300 A300B4622R 3930312 EU RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 RIGHT WING RIB 5; HOLE "E", THE EXISTING HOLE SIZE IS LARGER THAN THE FINAL HOLE SIZE CALLED OUT IN FEDEX EO 6-5710-7-5 005 P1. COMPLIED WITH FEDEX EA 6-5710-123672, WINGS - AD 99-16-01 - EO 6-5710-7-5005, RT WING REAR SPAR MLG FWD PICK-UP FITTING BOLT "E". 2 L 7 2 4F RT A35EU 20081203 NM 2008 12 3 AALA200820042 1 20081103 A 5347 141N51301 SEAT TRACK BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 604AA 43723 27055 LT OUTBOARD SEAT TRACK CORRODED, REPLACED SEAT TRACK IAW SRM 51-10-02. 2 L 7 2 4F RT A2NM 20081203 NM 2008 12 3 FDEA200812025044 1 20081202 A 5320 141N5160188 FLOOR SUPPORT BOEING 757 75723A 1384967 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 CABIN FLOOR, BS 297-310.5, RBL 30, CHANNEL CORRODED AROUND FASTENER HOLES. REMOVED FLOOR SUPPORT, BS 301-310.5, RBL 30, IAW SRM 51-40-02. FABRICATED NEW FLOOR SUPPORT (CHANNEL) ON MAE TRAVELER T8/759040. TREATED, PRIMED AND TOP COATED NE W SUPPORT/CHANNEL IAW SRM 51-20-01 AND AMM 51-21-00. LOCATED AND DRILLED NEW SUPPORT/CHANNEL IAW SRM 51-40-05. INSTALL ED NEW SUPPORT/CHANNEL, BS 301-310.5, RBL 30, IAW SRM 51-40-02. CORROSION WAS 100 PERCENT EXFOLIATED THRU PART AND OUT OF LIMITS IAW SRM 53-00-51, FIG 101. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20081203 EU 2008 12 3 FDEA200812025045 1 20081202 A 5711 A5724453123200 ANGLE AIRBUS 300 A300B4622 3930401 EU LT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 LT WING AFT OF REAR FALSE SPAR APPROX RIB 6A AREA HAS VERTICAL WEB GOUGED AND DOUBLE DRILLED HOLES. REMOVED LOWER SKIN PANEL AND DAMAGED ANGLE REF SRM 51-40-21 PARA 6 AND 13. FABRICATED NEW ANGLE REF SRM 57-51-11 AND DWG A57244531. ALOD INED REF SRM 51-21-10. PRIMED AND PAINTED REF SRM 51-23-10. PARTS MARKED REF GMM 7-0-1000. INSTALLED NEW ANGLE AND LO WER SKIN REF SRM 51-40-21 PARA 6, 7, AND 13. 2 L 7 2 4F RT A35EU 20081203 NM 2008 12 3 ZZDA2008172 1 20081117 A 2421 PCDU BOEING 717 717200 1383700 NM RIGHT MALFUNCTIONED A ZZDA K NONE H ELECT. POWER LOSS-50 PC AP APPROACH 1 SO 37 947AT 55010 ON DESCENT LOST RT GEN TRIED ONE RESET - STARTED APU BUS AC BUS TIE WOULD NOT CLOSE. REMOVED AND REPLACED RT PCDU, GEN CONTROL RELAY & EXT PWR MAIN BTR REF AMM 24-21. APU BUS, OPS CHECK GOOD. 2 L 7 2 4F TR A6WE 20081203 NM 2008 12 3 ZZDA2008173 1 20081113 A 2120 UNKNOWN BOEING 737 73776N 13844CH NM CABIN ODOR A ZZDA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 37 168AT 32653 BURNING RUBBER SMELL VERY STRONG IN AFT CABIN. UPON INITIAL OBSERVATION NO SMOKE, FUMES, OR RUBBER SMELL IN AFT CABIN. ACCOMPLISHED CHECK OF CABIN EQUIPMENT, IFE SYSTEM AT PAX SEATS, RECIRC FANS, LIGHTING, CARGO COMPARTMENTS. PERFORMED V ISUAL INSPECTION OF ENGINE INLETS AND EXHAUSTS. NO DEFECT NOTED. CANNOT DUPLICATE BURNING RUBBER SMELL REF FIM 21-00 T ASK 806. 2 L 7 2 4F RT A16WE 20081203 EA 2008 12 3 VNAA2008111700003 1 20081116 A 2742 BOLT CNDAIR CL600 CL6002C10 1390015 EA HORIZ STAB LOOSE A VNAA K NONE O OTHER IN INSP/MAINT 1 GL 05 718PS 10175 DURING ROUTINE MAINTENANCE ON THE HORIZONTAL STABILIZER TRIM ACTUATOR (HSTA), LOOSE BOLTS WERE FOUND IN THE UPPER BOLT L OCATIONS OF THE UPPER HSTA FITTING ASSEMBLIES (LT AND RT). THE BOLTS WERE RETORQUED TO THE PROPER SPECIFICATION. CHECK S WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 MASA2008111600777 1 20081116 A 3230 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA K NONE J WARNING INDICATION CL CLIMB 1 SW 07 27314 7314 ASH FLT 7263 ABE-ORD. GEAR DISAGREE ON DEPARTURE AND NLG DOOR WARNING. MX REPLACED NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 20081203 NM 2008 12 3 MASA2008111400774 1 20081114 A 5210 STRUT DHAV DHC8 DHC8202 2809007 NM PAX DOOR BROKEN A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 437YV 437 ASH FLT 2896 PHX-DRO. PASSENGER DOOR AFT SUPPORT STRUT BROKEN. MX REMOVED AND REPLACED AFT SUPPORT STRUT. 2 H 7 2 4T RT A13NM 20081203 WP 2008 12 3 UPS08853910 1 20081025 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV EVALUATION EFN 70019951018 ORGINIAL NRC 282430. REPAIRED SRM 53-02-03 FIG 6. 2 L 7 4 4F RT 4A25 20081203 WP 2008 12 3 UPS08853911 1 20081024 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV EVALUATION REPAIR ESN 70019951009 ORIGINAL NRC 282404. REPAIRED DC8 SRM 53-02-03 FIG 6. 2 L 7 4 4F RT 4A25 20081203 WP 2008 12 3 AALA200810222 1 20081124 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN UNSERVICEABLE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 WITH ELECTRICAL POWER OFF THE EMERGENCY LIGHTS IN THE AFT ACCESSORY BAY ARE ON. TURNING MAIN AIRCRAFT BATTERY SWITCH ON CAUSES LIGHTS TO GO OFF. LIGHT RETURNS ON WHEN BATTERY SWITCH IS OFF. INSTALLED SERVICEABLE 8130 BATTERY PACKS IN B5- 27 AND B5-28 POSITIONS, SYSTEM OPERATIONS TESTS GOOD. 2 L 7 2 4F RT A6WE 20081203 WP 2008 12 3 AALA200810225 1 20081108 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 CORROSION ON CUSP BETWEEN STATION 256 TO 275 LEFT SIDE. INSTALLED NEW CUSP MEMBRANE FROM STATION 237 TO 313. 2 L 7 2 4F A6WE 20081203 NM 2008 12 3 AALA200810244 1 20081120 A 3211 TRUNNION BOEING 737 737823 13844BZ NM RT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948AN 30086 RIGHT MAIN GEAR FORWARD TRUNNION LUG BORE HAS CORROSION AT OUTBOARD LOWER LUG. REPAIRED PER SRM 57-20-90-2R-2. 2 L 7 2 4F RT A16WE 20081203 WP 2008 12 3 AALA200810203 1 20081103 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 CRACKED TANG ON WEB AFT OF THE FWD ENTRY DOOR STATION 208 AT LONGERON 11 LEFT. FABRICATED AND INSTALLED DOUBLER PER AAR D 53-10-00-11. 2 L 7 2 4F A6WE 20081203 SO 2008 12 3 CHQA200800231 1 20081122 A 2610 JEHX0520150B REGULATOR EMB 135 EMB135KL 3260302 SO ALLSN AE3007 AE3007A 03030 GL NR 2 BLEED SYS CLOGGED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 371SK 145535 CAE311660 FLIGHT 5374, STL TO DSM - DURING CLIMB IN ICING CONDITIONS THE FLIGHT CREW RECEIVED A BLD 2 LOW TEMP MESSAGE ON EICAS SH ORTLY AFTER THE ANTI-ICING SYSTEM TURNED ON. THE QRH WAS FOLLOWED AND IT WAS DECIDED TO RETURN TO STL DUE TO WEATHER CO NDITIONS AT THE DESTINATION AIRPORT. MAINTENANCE TROUBLESHOT THE FAULT TO A CLOGGED PNEUMATIC REGULATOR FOR THE BLEED 2 THERMOSTAT. THE REGULATOR WAS REPLACED AND THE SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081203 SO 2008 12 3 CHQA200800228 1 20081118 A 3350 RPS1B BATTERY PACK EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CABIN DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 270SK 9494 9494 145304 CAE311866 DURING INSPECTION MAINTENANCE FOUND THAT THE FLOOR EMERGENCY LIGHTS FROM SEATS 7A TO 12A WERE INOPERATIVE WHEN TESTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081203 EA 2008 12 3 SWIA200820481 1 20080909 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 604SK 10249 DURING C-CHECK, LEFT SIDE OF BEAM AT FS 280 CORRODED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820486 1 20080912 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 905SW 7437 DURING C-CHECK, FS 280 RBL9 OUTBOARD CLIP CRACKED. REPLACED PER REO. 2 L 7 2 4F RT A21EA 20081203 EU 2008 12 3 FDEA200811264984 1 20081126 A 5720 A5724081021400 FITTING AIRBUS 300 A300B4622R 3930312 EU RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 RIGHT WING RIB 5; HOLE "L" SHOWS A CRACK INDICATION APPROX , WINGS - AD 99-16-01 EO 6-5710-7-5005-RT WING REAR SPAR, RIB 5 FITTING BOLT HOLE "L". 2 L 7 2 4F RT A35EU 20081203 NM 2008 12 3 FDEA200812025041 1 20081202 A 5320 69471112 ANGLE BOEING 727 7272D4 138407U NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 EXTERIOR LWR FUSELAGE INSIDE DELTA BEAM BS 740 LBL5 TO RBL 5 WL 148.5 LOWER ANGLE UPPER SURFACE CORRODED. REMOVED AND R EPLACED T-ANGLE REF SRM 51-30-2 ORIGINAL MATERIAL THICKNESS .125. REMOVED .025 MATERIAL REMAINING .100 OUT OF LIMITS RE F SRM 53-10-1 FIG 1. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081203 EU 2008 12 3 FDEA200812025043 1 20081202 A 5720 A5724453120000 INTERCOSTAL AIRBUS 300 A300B4622 3930401 EU RT WING WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 RIGHT WING LOWER INTERCOSTAL ANGLE INBD OF AILERON WORN SEVERAL PLACES. REMOVED DAMAGED ANGLE, FABRICATED NEW ANGLE IAW DWG A57244531 AND SRM 51-70-12 PG 1-8. LOCATED AND DRILLED IAW DWG A57244531. ALODINED AND PRIMED NEW ANGLE IAW SRM 5 1-21-10 PG 8 AND 11 AND 51-23-10. PART MARKED NEW ANGLE A5724453120000 IAW GMM 7-0-1000. INSTALLED NEW ANGLE IAW SRM 5 1-40-21 PARA 8. 2 L 7 2 4F RT A35EU 20081203 WP 2008 12 3 AALA200810217 1 20081106 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 CORROSION ON T-ANGLE AT STATION 1155 AT LONGERON 28R. REMOVED AND REPLACED T-ANGLE PER SRM 51-30-5. 2 L 7 2 4F A6WE 20081203 NM 2008 12 3 AALA2008100240 1 20081120 A 3211 TRUNNION BOEING 737 737823 13844BZ NM LT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948AN 30086 LEFT MAIN GEAR FORWARD TRUNNION FITTING LOWER FACE IS CORRODED. REPAIRED PER SRM 57-20-90-2R-2. 2 L 7 2 4F RT A16WE 20081203 WP 2008 12 3 AALA200810219 1 20081106 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 VERTICAL ANGLE ABOVE VAULT DOOR JAMB FORWARD SIDE OF AFT PRESSURE BULKHEAD CRACKED AT STATION 1338. REMOVED AND REPLACE D ANGLE PER SRM 53-30-00. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200810201 1 20081031 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 RIGHT CUSP MEMBRANE CORRODED FROM STATION 1174 TO 1193. INSTALLED NEW CUSP MEMBRANE. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200810221 1 20081106 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 CORROSION ON CUSP AT STATION 598 TO 617 RIGHT SIDE. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081203 NM 2008 12 3 R61A20080037 1 20081113 A 2751 WARNING SYSTEM EMB ERJ170 ERJ170200LR 3260121 NM COCKPIT MALFUNCTIONED A R61A O OTHER N FALSE WARNING DE DESCENT 1 GL 11 106HQ 17000164 DURING DESCENT CREW REPORTED, RECEIVED A FLAP FAIL MESSAGE. FOLLOWED QRH PROCEDURES DECLARED AN EMERGENCY AND LANDED AI RCRAFT WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO AIRCRAFT CLEARED SF-ACE INHIBITS SYSTEM OPERATIONAL CHECK WAS CO MPLETED OPERATIONAL CHECK GOOD, AIRCRAFT WAS RETURN TO SERVICE. 2 L 7 2 4F RT A56NM 20081203 2008 12 3 R61A20080036 4 20081114 A 2312 VHF COMM EMB ERJ170 ERJ170100SE 3260406 NM COCKPIT MALFUNCTIONED A R61A O OTHER O OTHER CR CRUISE 1 GL 11 873RW 17000144 CREW REPORTED VIA ACARS, LOST COMMUNICATIONS WITH ATC. DISPATCHED CALLED ATC BY PHONE AND RELAYED ALL COMMUNICATIONS VI A ACARS. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO AIRCRAFT TROUBL ESHOT RESET POWER AND PERFORMED OPERATIONAL CHECK OF SYSTEM OPERATIONAL CHECK WAS GOOD. MAINTENANCE ALSO REMOVED AND RE PLACED FLIGHT ATTENDANT HANDSET AND CRADLE AS A PRECAUTION. 2 L 7 2 4F RT A56NM 20081203 NM 2008 12 3 NOCA08308 1 20081111 A 2560 1317 LIGHT BOEING 757 75728A 1384976 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 752NA 28174 EMERGENCY LIGHTS OUT BY 18, 22, 25, 30FED AND 32, 33, 35ABC. RELAMPED EMERGENCY LIGHTS STOWAGE BINS / BULLNOSE TYPE, LO CATED AT 18, 22, 25, 30FED AND 32, 33, 35ABC IAW AMM. ALL OPS NORMAL, CLEARED CI WITH MCC. 2 L 7 2 4F RT A2NM 20081203 EA 2008 12 3 MASA2008111400771 1 20081114 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A MASA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 715SF 7115 ASH FLT 7209 IAD-SYR - CAPTAIN RECEIVED A FLAP FAIL AT "0" IN CRUISE. FLIGHT ORIGINALLY SCHEDULED TO LGA AND DIVERTED D UE TO WEATHER. CAPTAIN DECLARED AN EMERGENCY AND LANDING WAS UNEVENTFUL. MX COMPLIED WITH PART A RESET SUCCESSFUL. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 MASA2008111400772 1 20081114 A 2622 BRACKET CNDAIR CL600 CL6002C10 1390015 EA FIRE BOTTLE BROKEN A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 504MJ 10066 ASH FLT 7211 ORD-EWR. AFT FIRE EXTINGUISHER HOLDER BROKEN. MX RE-SECURED THE FIRE EXTINGUISHER TO THE BRACKET. 2 L 7 2 4F RT A21EA 20081203 WP 2008 12 3 UPS08853898 1 20081025 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV REPAIR EFN 700200001086 REQUIRES EVALUATION AND DISPOSITION ORIGINAL N RC 145820 RT WING L/E STA XRS 6.22 LOWER RIB IS CRACKED. NO REPAIR AT STATION STA XRS 6.22 REPAIR IS AT XAS 62.2 FOUND REPAIR TO HAVE BEEN ACCP IAW D C8 SRM 57-02-00-0. 2 L 7 4 4F RT 4A25 20081203 WP 2008 12 3 UPS08853912 1 20081024 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV EVALUATION EFN 70019941018 ORGINIAL NRC 018803. REPAIRED DC8 53-2-00 1B. 2 L 7 4 4F RT 4A25 20081203 SO 2008 12 3 CHQA200800230 1 20081121 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL LAVATORY FALSE ACTIVATION A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 569RP 145816 CAE312591 FLIGHT 6159, MKE TO CVG - DURING TAKEOFF CLIMB AT 1,000 FT, THE FLIGHT CREW RECEIVED A LAV SMOKE EICAS WARNING. THE QRH WAS FOLLOWED AND THE AIRCRAFT RETURNED TO LAND. THE FLIGHT ATTENDANT CONFIRMED THAT THERE WAS NO SMOKE OR FIRE. MAINT ENANCE RAN THE ENGINES WITH THE FLIGHT CREW WITH NO FURTHER OCCURRENCES AND THE LAV SMOKE DETECTOR WAS DEFERRED. THAT E VENING THE DEFERRAL WAS CLEARED WHEN THE LAV SMOKE DETECTOR WAS REPLACED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081203 EA 2008 12 3 CHQA200800232 1 20081124 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CABIN SMOKE A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 645BR 7383 GEE872681 FLIGHT 5570, IAH TO SDF - WHILE CLIMBING THROUGH 20,000 FT, THE FLIGHT CREW WAS NOTIFIED BY THE FLIGHT ATTENDANT OF SMOK E RISING FROM THE FLOOR DISTRIBUTION DUCTS AROUND ROW TEN AND A SMOKY SMELL FROM THE GASPER VENTS. THE FLIGHT CREW OPEN ED THEIR GASPERS AND CONFIRMED THE SMOKE SMELL. THE MEMORY ITEMS WERE RUN FOR SMOKE AND THE QRH CHECKLISTS WERE FOLLOWE D AND THE FLIGHT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED HIGH POWER ENGINE RUNS WITH B OTH BLEEDS SELECTED, WITH NO SMOKE SMELL NOTED FROM THE PACKS. THE ENGINE AND APU OIL LEVELS WERE CHECKED, NO OIL CONSU MPTION NOTED. THE APU WAS VISUALLY INSPECTED, ALONG WITH E1 AND E2 WITH NO DEFECTS NOTED. THE FORWARD AND AFT BAYS WER 2 L 7 2 4F 4 F RT A21EA E15NE 20081203 EA 2008 12 3 SWIA200820482 1 20080909 A 3213 PISTON CNDAIR CL600 CL6002C10 1390015 EA LT MLG CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 604SK 10249 DURING C-CHECK, LEFT MLG PISTON ASSEMBLY LOWER AFT TOP OF AXLE SUPPORT CORRODED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820483 1 20080909 A 3213 TORQUE LINK CNDAIR CL600 CL6002C10 1390015 EA RT MLG CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 604SK 10249 DURING C-CHECK, RIGHT MLG PISTON ASSEMBLY LOWER INBOARD TORQUE LINK CORRODED. REPAIRED PER CMM. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820484 1 20080912 A 5312 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 905SW 7437 DURING C-CHECK, LOWER INBOARD CORNER OF LINTEL FITTING, REAR PRESSURE BULKHEAD, CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820485 1 20080912 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 905SW 7437 DURING C-CHECK, FS 280 LBL9 INBOARD AND OUTBOARD CLIPS CRACKED. REPLACED PER REO. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820490 1 20080912 A 5312 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 903SW 7425 DURING C-CHECK, REAR PRESSURE BULKHEAD LINTEL FITTING UPPER AND LOWER INBOARD CORNERS CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820492 1 20080913 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 471CA 7655 DURING C-CHECK, FS 460 RIGHT SIDE FLOOR SUPPORT FITTING CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820493 1 20080913 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 471CA 7655 DURING C-CHECK, RIGHT WING PLANK AT WS54 HOLE NR 1 CORRODED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820495 1 20080913 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 471CA 7655 DURING C-CHECK, LEFT WING PLANK AT WS 54 HOLE NR 1 CORRODED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820498 1 20080913 A 7120 LINK CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 471CA 7655 DURING C-CHECK, RIGHT ENGINE FORWARD MOUNT UPPER LINK CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820503 1 20081121 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER NR NOT REPORTED 1 NM 07 443SW 7638 FLT 5800 - EMERGENCY EXIT SIGN AT ROW 8D INOP. RESECURED CONNECTOR. 2 L 7 2 4F RT A21EA 20081203 SO 2008 12 3 C2XA08SH130 1 20081014 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11193 14500938 SHV - DURING C CHECK LT OMEGA BEAM LOWER FLANGE HAS CORROSION BETWEEN FR 20-24. MX REPAIRED LT OMEGA BEAM BETWEEN FR 20 -24 IAW EMB 145XR SRM 53-00-10. THE ACFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 20081203 WP 2008 12 3 AALA200810211 1 20081105 A 5320 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 CORROSION ON FORWARD CARGO DOOR PAN STATION 370-427. SPLICED IN NEW SECTION OF PAN STATION 370-427. 2 L 7 2 4F A6WE 20081203 NM 2008 12 3 KCSA081604 1 20081129 A 3211 TRUNNION BOEING 747 747212B 1384886 NM LANDING GEAR CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 STA 1480 LT INBOARD LANDING GEAR TRUNNION CORRODED. 2 L 7 4 4F RT A20WE 20081203 NM 2008 12 3 KCSA081592 1 20081118 A 3350 LIGHT BOEING 747 747122 1384872 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 712CK 19754 EMERGENCY EXIT LIGHT IN LIGHTED DOME INOP. 2 L 7 4 4F RT A20WE 20081203 NM 2008 12 3 KCSA081593 1 20081118 A 3350 LIGHT BOEING 747 747122 1384872 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 712CK 19754 EMERGENCY LIGHT ABOVE EMERGENCY SLIDE INOP. 2 L 7 4 4F RT A20WE 20081203 EA 2008 12 3 SWIA200820487 1 20080912 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 903SW 7425 DURING C-CHECK, FS 280 RBL9 INBOARD AND OUTBOARD CLIPS CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820488 1 20080912 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 903SW 7425 DURING C-CHECK, FS 280 RBL9 UPPER FLOOR SUPPORT CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820489 1 20080912 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 903SW 7425 DURING C-CHECK, FS 621 BULKHEAD WEB CRACKED ABOVE LINTEL FITTING. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820491 1 20080913 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 471CA 7655 DURING C-CHECK, LEFT AND RIGHT OBLIQUE ANGLES AT FS 625 CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820494 1 20080913 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 471CA 7655 DURING C-CHECK, RIGHT WING PLANK AT WS 136 HOLE NR 8 CORRODED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820497 1 20080913 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 471CA 7655 DURING C-CHECK, LEFT ENGINE AFT THRUST FITTING CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820499 1 20080919 A 3213 TORQUE LINK CNDAIR CL600 CL6002C10 1390015 EA RT MLG CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 716SK 10180 DURING C-CHECK, RIGHT MLG OUTER CYLINDER UPPER TORQUE LINK CORRODED. REPAIRED PER CMM. 2 L 7 2 4F RT A21EA 20081203 WP 2008 12 3 AALA200810210 1 20081104 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 SUB FLOOR WEB CORRODED, STATION 160-200, JUST INBOARD OF THE FORWARD SERVICE DOOR. INSTALLED DOUBLER STATION 160-200 PE R AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200810212 1 20081105 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 CRACK IN CUSP MEMBRANE STATION 219 UNDER SEAT TRACK NUMBER 5. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200810213 1 20081105 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE SEPARATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 FUSELAGE SKIN SEPARATED AT BOTTOM FORWARD CORNER OF THE AFT LAVATORY SERVICE PANEL. INSTALLED DOUBLER ON BOTTOM HALF OF SKIN AT AFT LAVATORY SERVICE PANEL CUT-OUT PER ESO 80559 DATED 11/05/2008. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200802738 1 20081015 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 427AA 49339 LGA - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081203 NM 2008 12 3 KCSA081603 1 20081129 A 5315 FLOORBEAM BOEING 747 747249F 1384849 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 STA 330 FLOORBEAM WEB CRACKED 3.5 INCHES AT LBL 63. 2 L 7 4 4F RT A20WE 20081203 NM 2008 12 3 KCSA081589 1 20081118 A 5730 SKIN BOEING 747 747212B 1384886 NM LT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 LT WING UPPER SURFACE ILES-472 AT L/E RIB HAS CORROSION. 2 L 7 4 4F RT A20WE 20081203 NM 2008 12 3 KCSA081597 1 20081120 A 5414 SKIN BOEING 747 747212B 1384886 NM NR 1 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 NR 1 PYLON HAS CHAFING ON O/B SKIN UPPER SURFACE AT NAC STA-215 TO 220. 2 L 7 4 4F RT A20WE 20081203 NM 2008 12 3 KCSA081598 1 20081120 A 5210 WEB BOEING 747 747212B 1384886 NM L5 DOOR CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 L-5 DOOR INNER WEB CORRODED STA 2226. 2 L 7 4 4F RT A20WE 20081203 NM 2008 12 3 KCSA081601 1 20081121 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 FORWARD BILGE FUSELAGE FRAME IS DAMAGED AT STA 820, RBL 27. 2 L 7 4 4F RT A20WE 20081203 NM 2008 12 3 KCSA081594 1 20081119 A 5720 ATTACH FITTING BOEING 747 747212B 1384886 NM LT WING CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 LT WING L/E RIB ATTACH CLIP CRACKED AT FRONT SPAR UPPER CHORD FSSI 336. 2 L 7 4 4F RT A20WE 20081203 NM 2008 12 3 KCSA081595 1 20081118 A 5312 PRESSURE BLKHD BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 PRESSURE DECK AFT EDGE CORRODED AT BS 1480, RBL 13 TO RBL 30, WL 187. 2 L 7 4 4F RT A20WE 20081203 NM 2008 12 3 KCSA081607 1 20081202 A 5751 SKIN BOEING 747 747212B 1384886 NM LT AILERON GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 LT INBOARD AILERON LOWER L/E IS GOUGED. 2 L 7 4 4F RT A20WE 20081203 NM 2008 12 3 KCSA081605 1 20081201 A 5312 BULKHEAD BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 AFT PRESSURE BULKHEAD LWR SKIN PILLOWING AND APPROX .500 INCH CRACK, AT BS 2360 LBL 7 WL 186, APU CUTOUT FWD SIDE. 2 L 7 4 4F RT A20WE 20081203 NM 2008 12 3 KCSA081606 1 20081202 A 5751 RIB BOEING 747 747212B 1384886 NM LT AILERON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 LT INBOARD AILERON INBOARD RIB CRACKED. 2 L 7 4 4F RT A20WE 20081204 SO 2008 12 4 C2XA08CL124 1 20081127 A 2621 336000575 FIRE BOTTLE EMB 145 EMB145LR 3260212 SO NR 1 ENGINE FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 16919 13789 145393 EWR - FLIGHT 2400 - THE CREW REPORTED A ENGINE 1/2 EXTBTL A INOP MESSAGE ON THE EICAS INFLIGHT. THE AIRCRAFT DIVERTED I NTO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE ENGINE NR 1 FIRE BOTTLE A. OPERATI ONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20081204 SO 2008 12 4 C2XA08CL121 1 20081117 A 2910 HYDRAULIC SYSTEM EMB 145 EMB145LR 3260212 SO NR 1 CONTAMINATED A C2XA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SW 27 13970 145146 MKE - FLIGHT 2948 - THE CREW REPORTED THE NR 1 HYDRAULIC SYSTEM FLUID SHOWED 1/4 LEVEL AFTER 43 MINUTES IN FLIGHT. THE SYSTEM WAS SERVICED PRIOR TO DEPARTURE FROM IAH. RECEIVED A HYD SYS 1 LOW QUANTITY ON FINAL APPROACH. EMERGENCY WAS DE CLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED VISUAL INSPECTION AND NO LEAKS WERE NOTE D. THE SYSTEM WAS SERVICED AND OPERATIONAL CHECKS AND LEAK CHECKS WERE GOOD. CLE MAINTENANCE PERFORMED INSPECTION AND FOUND AIR IN THE NR 1 HYDRAULIC SYSTEM. THE NR 1 HYDRAULIC SYSTEM WAS BLED OF AIR AND SERVICED. THE AIRCRAFT WAS RELEA SED FOR SERVICE. 2 L 7 2 4T RT T00011AT 20081204 SO 2008 12 4 C2XA08IA241 1 20081120 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO AC BAY SEIZED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 13979 10495 10495 145181 RSW - FLIGHT 3146 - THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN AND PASSENGERS REPORTED HEARING A LOUD POPPING SOUN D WHILE CLIMBING THROUGH 14,000 FEET. THE CREW FOLLOWED THE QRH PROCEDURES, AND THE AIRCRAFT RETURNED TO RSW WHERE IT L ANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NUMBER TWO PACK ON MEL 21-24-01/1 CAT C CTL N R 158685, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RON'D AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ACM, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081204 SO 2008 12 4 C2XA08SH151 1 20081202 A 5320 14523171003 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24103 145645 SHV - DURING C-CHECK RT OMEGA BEAM CORRODED AT NUT PLATE AREAS AT FR 59-61. MAINTENANCE REPAIRED RT OMEGA BEAM BETWEEN FR 59-61 IAW EC 5320-01434. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081204 SO 2008 12 4 C2XA08TY133 1 20081120 A 5514 14521939000 HINGE BRACKET EMB 145 EMB145 3260210 SO HORIZ STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16911 145446 RT HORIZONTAL STAB HINGE PIN RETENTION EAR IS CRACKED. REMOVED AND REPLACED RT HORZ STAB HINGE PIN BRACKET IAW EMB 145 SRM 51-40-02. AIRCRAFT STILL IN C CHECK. 2 L 7 2 4F RT T00011AT 20081204 EU 2008 12 4 UPS08153920 1 20081027 A 5420 A5401043600164Y COVER AIRBUS A300 A300F4622R 3930360 EU NR 2 NACELLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 142UP 0825 INSPECTION TYPE:1C3C SEAL SUPPORT CRACKED AT CORNER ON NR 2 ENGINE BLEED AIR PRECOOLER COVER 423BL. REPAIRED NR 2 ENGIN E PRECOOLER SEAL SUPPORT COVER REF EO A300-5430-3114 6-A AND EA 300-5452-01-A1553. 2 L 7 2 4F RT A35EU 20081204 WP 2008 12 4 UPS08853924 1 20081111 A 5755 SKIN DOUG DC8 DC871F 302199D WP SPOILER DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:SV LT WING I/B SPOILER UPPER SURFACE HAS AN EXTERNAL REPAIR DOUBLER INSTALLED SURVEY SEQ 729-W3-34 STA X W 57. PREVIOUSLY REPAIRED SRM 57-2-0 FIG 2 REV 76. 2 L 7 4 4F RT 4A25 20081204 NM 2008 12 4 K11A2008120372214 1 20080903 A 5330 DOUBLER BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 AFT LAV SERVICE PANEL SKIN DOUBLER CORRODED ON INSIDE LOWER CORNER. 2 L 7 3 4F RT A3WE 20081204 EU 2008 12 4 PNSA02 1 20081118 A 7931 WARNING SYSTEM SAAB SF340 340B 7860101 EU COCKPIT ACTIVATED A PNSA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 AL 03 675P 206 LEFT OIL PRESSURE LIGHT CAME ON DURING TAKEOFF. 2 L 7 2 4T RT A52EU 20081204 NM 2008 12 4 R61A20080044 1 20081118 A 2752 C1583911 ACTUATOR EMB ERJ170 ERJ170200LR 3260121 NM TE FLAP MALFUNCTIONED A R61A O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 106HQ 4335 4335 17000164 CREW REPORTED ON APPROACH HAD A FLAP/SLAT FAIL MESSAGE. MAINTENANCE REMOVED AND REPLACED NR 4 FLAP ACTUATOR AND FLAP/SL AY POWER DRIVE UNIT WAS REPLACED AS PRECAUTIONARY. COMPLIED WITH OPERATIONAL CHECK OF SYSTEM ALL CHECK WERE GOOD. AIRC RAFT HAD AN OPERATIONAL CHECK FLIGHT AND THE CHECK FLIGHT WAS SATISFACTORY. 2 L 7 2 4F RT A56NM 20081204 NM 2008 12 4 R61A20080045 1 20081124 A 2750 FLAP EMB ERJ170 ERJ170200LR 3260121 NM WING MALFUNCTIONED A R61A O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 106HQ 17000164 CREW REPORTED ON APPROACH RECEIVED A FLAP FAIL MESSAGE ON EICAS. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MA INTENANCE TROUBLESHOT AIRCRAFT CLEARED INHIBITS AND RESET BRAKE. COMPLETED OPERATIONAL CHECK, ALL CHECKS GOOD. RETURNE D AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A56NM 20081204 NM 2008 12 4 UPS08553941 1 20081115 A 3350 LIGHT BOEING 757 75724APF 1384969 NM EXIT SIGN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 473UP 28846 INSPECTION TYPE:N/A EMERGENCY EXIT SIGN HAS 3 LAMPS OUT. RELAMPED PER AMM 33-51-01-2. 2 L 7 2 4F RT A2NM 20081204 NM 2008 12 4 UPS08M53932 1 20081117 A 5730 ARB75801 SKIN PANEL DOUG MD11 MD11F 3023600 NM LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C SURVEY SEQUENCE NUMBER 254-W3-006 LT WING INBOARD FIXED L/E PNL UPPER SURFACE STA XIS 244 HAS LOOSE F ASTENERS AND WRINKLING SKIN EO MD11-5110-30530 APPENDIX C AND NO SRM REF APPENDIX E. REMOVED EXISTING DOUBLER, FABRICAT ED AND INSTALLED DOUBLER IAW MD11 SRM VOL 1 57-00-01 FIGURE 24. 2 L 7 3 4F RT A22WE 20081204 NM 2008 12 4 UPS08M53931 1 20081114 A 7830 491B1330011 WEB DOUG MD11 MD11F 3023600 NM THRUST REVERSER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C NR 2 ENGINE RT T/R LOWER FWD WEB FOUND CRACKED AND 2 EA FASTENERS BROKEN AT 5 O'CLOCK POSITION. STOP DRILLED CRACK, FABRICATED, AND INSTALLED DOUBLER IAW CF6-80C2 CMM 78-32-02, REPAIR 24. 2 L 7 3 4F RT A22WE 20081204 NM 2008 12 4 UPS08M53938 1 20081117 A 5753 NRC6055507 WEDGE DOUG MD11 MD11F 3023600 NM TE FLAP DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 256UP 48405 INSPECTION TYPE:N/A LT INBOARD FLAP T/E WEDGE DAMAGED. REPAIRED PER MD11 SRM 57-20-00 FIG 3. 2 L 7 3 4F RT A22WE 20081204 NM 2008 12 4 UPS08M53943 1 20081109 A 5330 ADA70301 DOUBLER DOUG MD11 MD11F 3023600 NM FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C SURVEY SEQUENCE NUMBER 254-F1-003 OF MD11-5100-30530 APPENDIX C ITEM 3, GOUGE FOUND ON AFT EDGE OF RE PAIR DOUBLER RT 879 TO 889 L38R TO L42R. REMOVED EXISTING DOUBLER 1, 2 AND 3, FABRICATED AND INSTALLED REPAIR DOUBLER 1 , 2 AND 3 IAW MD11 VOL 1 SRM 53-50-00 FIG 17. 2 L 7 3 4F RT A22WE 20081203 SO 2008 12 3 C2XA08RI168 1 20081109 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT SMOKE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 16183 14500914 FLIGHT 3053 - EWR - FLIGHT CREW REPORTED SMOKE IN COCKPIT AND EICAS INDICATION FOR LAV SMOKE. EWR MX RAN ENGINES AND BO TH PACKS, INSPECTED DUCTS AND NO FAULTS OR SMOKE NOTICED. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081204 WP 2008 12 4 22AA20081101 1 20081118 A 2150 9788403 ANTI-ICE VALVE DOUG DC10 DC1010F 3022111 WP NR 1 INOPERATIVE A 22AA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 29 68041 5 5 46900 STRONG BURNING SMELL COMING FROM NR 1 AIR CONDITIONING PACK AFTER TAKEOFF AT HIGH POWER SETTINGS, PACK INLET & DISCHARGE TEMPERATURE NORMAL NR 1 AIR CONDITIONING PACK OPERATION NORMAL ON GROUND. REMOVED AND REPLACED WATER SEPARATOR CONICAL COALESCER IAW MM 21-54-03. ALSO REMOVED AND REPLACED NR 1 ANTI-ICE VALVE IAW MM 21-54-04, OPERATION CHECKED NORMAL. 2 L 7 3 4F A22WE 20081204 NM 2008 12 4 UPS08653929 1 20081117 A 5321 BMS423TYPEII FLOOR PANEL BOEING 767 76734AF 1385212 NM CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 318UP 27746 INSPECTION TYPE: IN .75 INCH HOLE IN ONE SKIN WITH NO CORE DAMAGE. REPAIRED IAW EO B767-5300-31210-A. 2 L 7 2 4F RT A1NM 20081204 NM 2008 12 4 R61A20080047 1 20081124 A 5330 SKIN EMB ERJ170 ERJ170200LR 3260121 NM FUSELAGE DENTED A R61A K NONE O OTHER IN INSP/MAINT 1 GL 11 110HQ 17000172 DENT/GOUGE ON THE AFT FUSELAGE BY THE LAVATORY SERVICE PANEL. ACCOMPLISHED MAJOR REPAIR PER EMBRAER ENGINEERING INSTRUC TION. 2 L 7 2 4F RT A56NM 20081204 2008 12 4 SWAA086660 4 20081128 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 L1 DOOR SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081204 2008 12 4 SWAA086666 4 20081127 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 761RR 27875 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086668 1 20081127 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 761RR 27875 DURING SCHEDULED HC1 CHECK, FWD LT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081204 2008 12 4 SWAA086670 4 20081124 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 913WN 29840 L1 DOOR SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086671 1 20081201 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086707 1 20081201 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086708 1 20081202 A 5310 6547978 CREASE BEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR CREASE BEAM CORRODED AT BS 986, RBL 49, WL 208. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081203 NM 2008 12 3 KCSA081591 1 20081118 A 3350 SIGN BOEING 747 747122 1384872 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 712CK 19754 EMERGENCY EXIT SIGN ABOVE UPPER DECK ESCAPE DOOR INOP. 2 L 7 4 4F RT A20WE 20081203 NM 2008 12 3 KCSA081599 1 20081120 A 5414 SKIN BOEING 747 747212B 1384886 NM NR 4 PYLON WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 NR 4 PYLON LOWER EDGE SKIN ON I/B AT NAC STA 180 TO 220 SIDE IS WORN. 2 L 7 4 4F RT A20WE 20081203 NM 2008 12 3 KCSA081590 1 20081118 A 5313 STRINGER BOEING 747 747212B 1384886 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 STR 49R AT STA 2614 DENTED. 2 L 7 4 4F RT A20WE 20081203 NM 2008 12 3 KCSA081608 1 20081202 A 5411 RIB BOEING 747 747212B 1384886 NM NR 2 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 NR 2 NAC STA 211 I/B RIB CRACKED 1 INCH, BELOW MIDSPAR. 2 L 7 4 4F RT A20WE 20081204 SO 2008 12 4 C2XA08RI171 1 20081111 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO GALLEY SMOKE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 11194 14500940 FLIGHT 2756 - EWR - FLIGHT ATTENDANT AND PASSENGER IN SEAT 2A REPORTED WHAT THEY THOUGHT WAS SMOKE COMING FROM AFT TRASH BIN IN GALLEY. FLIGHT ATTENDANT DISCHARGED HALOGEN FIRE EXTINGUISHER INTO BIN AND PASSENGERS WERE EVACUATED. EWR MX I NSPECTED THE AREA NO SIGNS OF BURNING OR SMOKE FOUND. MX REMOVED AND REPLACED FIRE EXTINGUISHER. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081204 SO 2008 12 4 C2XA08CL125 1 20081129 A 3232 21180100401 ACTUATOR EMB 145 EMB145LR 3260212 SO NLG DOOR FAULTY A C2XA K NONE J WARNING INDICATION DE DESCENT 1 SW 27 12922 19584 145338 CLE - FLIGHT 2775 - THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE ON THE EICAS AFTER SELECTING GEAR DOWN. THE MESSAGE CLEARED IMMEDIATELY AND NO OTHER INDICATIONS WERE NOTICED. MAINTENANCE INSPECTED AND REPLACED THE RIGHT NOSE G EAR DOOR ACTUATOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20081204 NE 2008 12 4 COMA2008111970002 2 20081119 A 7230 FAN BLADE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE LT ENGINE DEFECTIVE A COMA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 27 369CA 10079 965504 EN ROUTE ATL-MKE THE LEFT ENGINE VIBRATION INDICATION REACHED 1.8 AMBER, REDUCED THRUST TO INDICATE GREEN. CREW DIVERTE D TO MKE AND LANDED WITHOUT INCIDENT. REPLACED ALL FAN BLADES ON THE LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E00063EN 20081204 NM 2008 12 4 UPS08M53895 1 20081110 A 5720 DOUBLER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C RT WING FIXED L/E COMPT AT XORS 506 HAS CRACK 4 EA AROUND FASTENERS HOLE ON BEADED DOUBLER. REMOVED DAMAGE, FABRICATED FILLER, ANGLES, AND DOUBLER, AND INSTALLED IAW MD-11 SRM 57-10-00 VOL 1 FIG 2. 2 L 7 3 4F RT A22WE 20081204 NM 2008 12 4 UPS08M53916 1 20081113 A 7160 2242101567 ACOUSTIC PANEL DOUG MD11 MD11F 3023600 NM NR 1 ENGINE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C 2 EA DENTS AT 6 O'CLOCK POSITION 6 INCHES AND 18 INCHES FROM NOSE LIP IN NR 1 ENG INLET ACOUSTIC PANE L. REMOVED DAMAGE, FABRICATED AND INSTALLED PLUGS AND APPLIED FIBERGLASS IAW MD-11 SRM 54-10-00 REPAIR 18 STEPS C-F AND G-O. 2 L 7 3 4F RT A22WE 20081204 EU 2008 12 4 UPS08153919 1 20081029 A 5751 A57661001179 AILERON AIRBUS A300 A300F4622R 3930360 EU RT WING DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 142UP 0825 INSPECTION TYPE:1C3C RT WING ALL SPEED AILERON UPPER T/E NUMEROUS DENTS. REPAIRED RT WING ASA UPPER T/E REF EO C-5750-3 1147-A AND EA 300- 5751-01-A1554. 2 L 7 2 4F RT A35EU 20081204 WP 2008 12 4 UPS08853925 1 20081106 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV LT WING LEADING EDGE AT STA 700 DOES NOT HAVE REPAIR DOUBLER INSTALLED AS PER APPENDIX H (3)(4) OF EO DC8 5100 30418. INSTALLED DOUBLER AS IAW 57-02-01 FIG 38 2 L 7 4 4F RT 4A25 20081204 NE 2008 12 4 UPS08B53921 2 20081114 A 7321 HMU BOEING 747 74745E 1384947 NM GE CF6 CF680C2B2 30025 NE NR 1 ENGINE MALFUNCTIONED A IPXA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 SO 01 579UP 26062 704664 INSPECTION TYPE:N/A ENG NR 1 FAILURE ON FINAL WITH SUCCESSFUL AUTO RELIGHT. NR 1 FAILED AGAIN ON GROUND WITH ENG 1 CONT ROL MESSAGE. WIND ON FINAL APPROACH TO 26L WAS OUT OF NORTH UP TO 50 KNOTS. REMOVED AND REPLACED NR 1 ENG HMU IAW MM 7 3-21-14, REMOVED AND REPLACED ECU IAW MM 73-21-15. REF Q141548 & K141559. OPS CK GOOD. 2 L 7 4 4F 4 F RT A20WE E13NE 20081204 NM 2008 12 4 UPS08M53926 1 20081109 A 5330 ADA70301 DOUBLER DOUG MD11 MD11F 3023600 NM FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C SURVEY SEQUENCE NUMBER 254-F1-004 OF MD11-5100-30530 APPENDIX C SECTION C ITEM 3, FOUND 2 GOUGES ON F WD EDGE OF DOUBLER REPAIR STA 999 L-39R- L-42R. REMOVED PREVIOUS REPAIR DOUBLER, FABRICATED, AND INSTALLED NEW REPAIR D OUBLER 1 AND REPAIR DOUBLER 2 IAW MD11 SRM 53-50-00 VOL 1 FIGURE 17 SHEETS 1-5. 2 L 7 3 4F RT A22WE 20081204 NM 2008 12 4 UPS08M53927 1 20081106 A 5712 ATTACH FITTING DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C LT WING AT STA XORS 562 FIXED L/E RIB ATTACH STRAP CRACKED. REMOVED, FABRICATED, AND INSTALLED STRAP IAW MD11 SRM 51-33-01 AND DWG ARB3954. 2 L 7 3 4F RT A22WE 20081204 NM 2008 12 4 UPS08M53934 1 20081116 A 3350 LIGHT DOUG MD11 MD11F 3023600 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A EMERGENCY LIGHTING SYSTEM INOP. PERFORMED ADJUSTMENT / TEST IAW 33-50-00-5. SYSTEM OPERATIONAL TES T CHECKED GOOD. THIS CLEARS M388756. 2 L 7 3 4F RT A22WE 20081204 NM 2008 12 4 UPS08M53936 1 20081116 A 3350 6044115 BATTERY PACK DOUG MD11 MD11F 3023600 NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED & REPLACED EMERGENCY LIGHTS BATTERY PACK IN REF TO MD11 MM 33 51, NO HELP. CYCLED C/B B1-382 SYSTEM. OPS OK PER AMM 33 51 01. 2 L 7 3 4F RT A22WE 20081204 NM 2008 12 4 K11A2008120372213 1 20080808 A 5310 WINDOW POST BOEING 727 7272H3 138368N NM FUSELAGE CRACKED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 THE E-H WINDOW POST CRACKED 4 INCHES ABOVE LOWER CORNER. 2 L 7 3 4F RT A3WE 20081204 NM 2008 12 4 R61A20080049 1 20080401 A 5311 FRAME EMB ERJ170 ERJ170100SU 3260403 NM FUSELAGE DAMAGED A R61A K NONE O OTHER IN INSP/MAINT 1 GL 11 802MD 17000013 DENT/SCATCH ON FUSELAGE FRAME 32 TO 34. PERFORMED MAJOR REPAIR PER EMBRAER ENGINEERING INSTRUCTION. 2 L 7 2 4F RT A56NM 20081204 WP 2008 12 4 UPS08853945 1 20081010 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV FUSELAGE SKIN REPAIR AT BS 55- BS61 L25R-L26R DOES NOT MEET SRM CRITERIA REF UPS EO REPAIR EVAL SURVE Y SEQ 702-F1-11. REPAIRED DC SRM 53-203 AND SRM 53-2-0 FIG 7 SHT 5. 2 L 7 4 4F RT 4A25 20081204 NM 2008 12 4 UPS08M53930 1 20081116 A 5210 ACA3822511V DOUBLER DOUG MD11 MD11F 3023600 NM NR 2 DOOR MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C SURVEY SEQUENCE NUMBER 254-F1-002 OF MD11-5100-30530 APPENDIX E SECTION D REPAIR DOES NOT CONFORM TO MD11 VOL 1 SRM 52-00-01 FIG 4 SHEET 2. REMOVED EXTERNAL DOUBLER, FABRICATED AND INSTALLED 1 EXTERNAL DOUBLER 1 INTERNAL DOUBLER, AND 1 FILLER IAW MD11 SRM 52-10-00 VOL 1 FIG 1. 2 L 7 3 4F RT A22WE 20081204 NM 2008 12 4 R61A20080040 1 20081117 A 2781 1702288A SENSOR EMB ERJ170 ERJ170100SU 3260403 NM LE SLAT DEFECTIVE A R61A O OTHER N FALSE WARNING AP APPROACH 1 GL 11 806MD 8344 17000019 CREW REPORTED SLAT FAIL/AOA LIMIT FAIL ON FINAL APPROACH, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANC E REMOVED AND REPLACED RIGHT HAND OUTBOARD SKEW SENSOR AND COMPLETED OPERATIONAL CHECK SYSTEM OPERATIONAL CHECK GOOD AND A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A56NM 20081204 NM 2008 12 4 R61A20080041 1 20081113 A 2780 SLAT EMB ERJ170 ERJ170200LR 3260121 NM WING MALFUNCTIONED A R61A O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 106HQ 17000164 CREW REPORTED SLAT/FLAP FAIL MESSAGE ON EICAS. CREW DECLARED AN EMERGENCY, FOLLOWED QRH PROCEDURES AND LANDED WITHOUT I NCIDENT. MAINTENANCE WAS DISPATCHED TO AIRCRAFT TROUBLESHOT CLEARED INHIBITS AND COMPLETED AND OPERATIONAL CHECK, SYSTE M CHECK GOOD. RETURNED A/C TO SERVICE. 2 L 7 2 4F RT A56NM 20081204 NM 2008 12 4 R61A20080042 1 20081113 A 2782 ACTUATOR EMB ERJ170 ERJ170200LR 3260121 NM LE SLAT MALFUNCTIONED A R61A O OTHER O OTHER AP APPROACH 1 GL 11 106HQ 17000164 CREW REPORTED FLAP/SLAT FAIL ON APPROACH. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 2 AN D NR 3 ACTUATOR TRIPPED. MAINTENANCE RESET ACTUATORS AND SYSTEM OPERATIONAL CHECK COMPLETED, SYSTEM OPERATIONAL CHECK G OOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A56NM 20081204 NM 2008 12 4 UPS08M53946 1 20081117 A 5730 ARB2886503 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C RT WING ON TELESCOPIC ANTI-ICE DUCT AT SLAT NR 3 HAS CRACK ON DOOR CUTOUT UPPER LEFT CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD11 VOL 1 SRM 57-10-00 FIG 43. 2 L 7 3 4F RT A22WE 20081203 WP 2008 12 3 AALA200810202 1 20081103 A 5320 STRAP DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 TEE STRAP CRACKED STATION 207 AT LONGERON 11 LEFT. FABRICATED AND INSTALLED DOUBLER PER AARD 53-10-00-011. 2 L 7 2 4F A6WE 20081203 NM 2008 12 3 R61A20080039 1 20081113 A 2752 LIMITER EMB ERJ170 ERJ170200LR 3260121 NM FLAP ACTUATOR TRIPPED A R61A O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 106HQ 17000164 CREW REPORTS ON DESCENT AT FLIGHT LEVEL 7000 FEET CREW RECEIVED A FLAP FAIL MESSAGE FOLLOWED QRH PROCEDURES, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO AIRCRAFT TROUBLESHOT. FOUND NR 2 LEFT AND NR 3 R IGHT ACTUATOR TORQUE LIMITER TRIP PINS TRIPPED. RESET PINS, OPERATIONAL CHECK WAS GOOD. ALSO PERFORMED FLAP LUBE, RETU RNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A56NM 20081203 EA 2008 12 3 MASA2008111400773 1 20081114 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT DIRTY A MASA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 07 923FJ 15023 ASH FLT 2719 PHX-SBA. LT AFT EMERGENCY DOOR CAUTION MESSAGE INTERMITTENT. MX CLEANED PROXIMITY SENSOR. 2 L 7 2 4F RT A21EA 20081203 WP 2008 12 3 UPS08853908 1 20081025 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV EVALUATION REPAIR EFN 70019951020 TRACK 8 AFT END COMPARTMENT 2. REPAIRED TRACK SPLICE AT STA 338 SR M 53-02-03 FIG 6. 2 L 7 4 4F RT 4A25 20081203 WP 2008 12 3 UPS08853909 1 20081025 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV EFN 7001199510 NEEDS EVALUATION ORGINIAL NRC 282432. REPAIRED IAW DC8 SRM 53-02-03 FIG 6. 2 L 7 4 4F RT 4A25 20081203 SO 2008 12 3 CHQA200800226 1 20081118 A 2750 FLAP EMB 135 EMB135LR 3260305 SO ALLSN AE3007 AE3007A 03030 GL WING FAILED A CHQA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 840RP 145725 CAE311921 FLIGHT 6054, CMH TO LGA - ON APPROACH, FLAPS 9 WERE SELECTED AND CREW RECEIVED A FLAP FAIL MESSAGE AND FLAPS REMAINED AT ZERO. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RESET POWER TO THE FLAP SYSTEM AND THE FLAPS OPERATED NORMALL Y. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081203 SO 2008 12 3 C2XA08RI169 1 20081110 A 2611 FAU751A4 PANEL EMB 145 EMB145XR 3260214 SO SMOKE DETECTION DEFECTIVE A C2XA K NONE N FALSE WARNING CL CLIMB 1 SW 27 14204 14500968 FLIGHT 2761 - EWR - FLIGHT CREW REPORTED LAV SMOKE INDICATION ON EICAS DURING CLIMBING, BUT NO SMOKE NOTICED. EWR MX RE MOVED AND REPLACED LAV SMOKE DETECTION PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. MX ALSO PERFORMED BORESCOPE INSPECTION THROUGH ENGINE INLET AND NO OIL NOR WETNESS NOTICED. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081203 SO 2008 12 3 C2XA08TY135 1 20081126 A 3350 82301 SIGN EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26545 145558 FWD CEILING EXIT LIGHT LOCATOR SIGN IS NOT FULLY LIT. REMOVED AND REPLACED FWD EXIT LOCATOR SIGN ASSEMBLY IAW EMB 145 A MM 33-50-15. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081204 NM 2008 12 4 SWAA086709 1 20081202 A 5310 6547978 CREASE BEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR CREASE BEAM CORRODED AT BS 986, RBL 47, WL 208. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086676 1 20081201 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 401WN 29813 DURING SCHEDULED MV1 CHECK, FOUND EEPLS LIGHT INOP AT ROW 1. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086677 1 20081201 A 3350 81000 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 EEPLS LIGHT LENS MISSING AT ROW 11A. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086678 1 20081201 A 3350 300432 LIGHT BOEING 737 7373A4 1384585 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EGRESS LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086679 1 20081201 A 5310 6547952 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER STOP FITTING. REMOVED AND REPLACED F RAME PER ACO. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086682 1 20081201 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086683 1 20081201 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086710 1 20081202 A 5330 6545768 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO SKIN CRACKED AT BS 518, STR 28L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086711 1 20081202 A 5315 6545855 FLOORBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, RBL 48. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086712 1 20081202 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 27L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086713 1 20081202 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 9R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086694 1 20081201 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 8L TO STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086653 1 20081126 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 455WN 32462 FOUND FWD EEPLS COVER MISSING. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086657 1 20081201 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 498WN 32480 DURING SCHEDULED HC2 CHECK, LT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086658 1 20081201 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 498WN 32480 DURING SCHEDULED HC2 CHECK, RT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086659 1 20081126 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 793, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086689 1 20081201 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086692 1 20081201 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086693 1 20081201 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086737 1 20081202 A 2560 6557463 BRACKET BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 491WN 33867 FOUND R1 DOOR SLIDE GIRT BAR AFT BRACKET LOOSE. INSTALLED BRACKET FASTENER PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086738 1 20081202 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086700 1 20081201 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086701 1 20081201 A 5311 6546595 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086702 1 20081201 A 5311 6546590 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086718 1 20081202 A 5322 6546569 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 986, STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086651 1 20081129 A 3350 3071BPEGL LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 439WN 29834 DURING SCHEDULED MV1 CHECK, FOUND FWD ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086652 1 20081129 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 444WN 29839 DURING SCHEDULED MV2 CHECK, FOUND AFT EEPLS LIGHT INOP. REMOVED AND REPLACED EEPLS PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086641 1 20081130 A 5311 6546534 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 520, RBL 28. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086642 1 20081130 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 500D, STR 27L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 ASAA0843915 1 20081122 A 5340 653535214 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 STRINGER CLIP CRACKED. REPLACED CLIP PER ASA DWG A53100265816. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 ASAA0893890 1 20081128 A 5320 111A72026 SUPPORT BOEING 737 737990 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 PNEUMATIC DOOR SUPPORT CHORD DAMAGED REPAIRED CHORD REF ER 08 3633. 2 L 7 4 4F RT A16WE 20081204 NM 2008 12 4 ASAA0873904 1 20081129 A 5315 147A55068 FLOORBEAM BOEING 737 737790 13844CN NM BS 986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON BS 986.5 FLOORBEAM UPPER FLANGE. REPAIRED FLOORBEAM IAW SRM 53-70-51. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 ASAA0843882 1 20081030 A 5311 654659315 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION INSTALLED REPAIR ANGLES AND FILLERS PER ASA EA 400 53EA 00267. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 ASAA0843883 1 20081029 A 5311 654655243 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION INSTALLED REPAIR ANGLES AND FILLERS PER ASA EA 400 53EA 00267. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 ASAA0843896 1 20081029 A 5311 654655520 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400 53EA 00267. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 ASAA0843898 1 20081029 A 5311 654653226 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400 53EA 00267. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008120301119 1 20081202 A 5754 65C26686 SKIN BOEING 737 7373T0 1384582 NM LE SLAT DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14336 23574 RT WING NR 5 SLAT T/E WEDGE NOT SEALED AND NEEDS INSPECTION FOR DELAM. FOUND TO BE DELAMINATED, REMOVED AND REPAIRED DE LAMINATED AREA, INSTALLED UPPER SKIN AND DOUBLER ON NR 5 SLAT T/E RT WING PER SRM 51-70-10 AND APPLIED PROTECTIVE FINISH PER CAL SPEC 5100S00128 REV Q AND SEALED WEDGE PER SRM 51-70-10. 2 L 7 2 4F RT A16WE 20081205 SO 2008 12 5 HYIA818AN 2 20081129 A 8550 25102 GARLOCK SEAL CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO ZONE 500 LEAKING E HYIA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NE 01 818AN 1001 1001 402C0501 832114R LEFT ENGINE LEAKING OIL IN FLIGHT CREW SHUT DOWN ENGINE. MAINTENANCE INSPECTED FOUND VACUUM PUMP'S GARLOC SEAL WAS LEAK ING. MX REMOVED AND REPLACED GARLOC SEAL AND VACUUM PUMP ASSY. MX CLEAN OIL SEPARATOR FILTER AND LINES. MX PERFORMED FULL POWER RUN UP. OPS AND LEAK CHECK GOOD AFTER RUN UP AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 20081205 NM 2008 12 5 CALA2008120201114 1 20081202 A 5320 BAC1509100146 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14336 23574 AFT BAG PIT TRANSITION INTERCOSTAL (U CHANNEL) RT STA 767-787 IS DAMAGED ON UPPER LEG. REMOVED DAMAGED INTERCOSTAL IAW B737 SRM 51-40-02 MATERIAL ID, 7075-T6, .050", IC 0647302 IAW B737 SRM 53-60-04. FABRICATED INTERCOSTAL IAW B737 SRM 5 3-60-04. ALODINED AND PRIMED INTERCOSTAL IAW B737 SRM 51-20-01. INSTALLED INTERCOSTAL IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008120201115 1 20081202 A 5320 6547690 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14336 23574 AFT CARGO BAY RT SIDE TRANSITION ANGLE CORRODED AND DAMAGED FROM STA 747 TO 787. REMOVED DAMAGED SECTION OF TRANSITION ANGLE IAW B737 SRM 51-40- 02 MATERIAL ID EXTRUSION BAC149637X707576 IC 0648981 IAW B737 SRM 53-60-53. FABRICATED NEW AN GLE IAW B737 SRM 53-60-53. ALODINED AND PRIMED ANGLE IAW B737 SRM 51-20-01 INSTALLED ANGLE IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA0801085 1 20081118 A 5312 148A22813 PRESSURE BLKHD BOEING 737 737824 13844BZ NM FUSELAGE CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 26226 28935 MECHANICAL SCUFFING FOUND ON AFT DOME PRESS BULKHEAD BETWEEN STR 12L AND STR 13L 5 INCHES AFT. REPAIRED PER ECRA 5311-0 1429, ISSUED A DIP TO ACCOMPLISH A HEFC INSPECTION OF THE AFT PRESSURE BULKHEAD REPAIR PER ECRA 5311-01429, PART 2, TABL E 1 REQUIREMENT ALPHA AT OR BEFORE AIRCRAFT REACHES 47,406 TOTAL FLIGHT CYCLES ACCOMPLISH REPEAT INSPECTIONS AT INTERVAL S NOT TO EXCEED 12000 FLIGHT CYCLES PER NON-ROUTINE 6063466 FOR 2ND DIP. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008111901088 1 20081118 A 5315 141N51221 FLOORBEAM BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19141 30354 CABIN FLOORBEAM AT STA 365 RBL 8 HAS SMALL AREA OF SURFACE CORROSION. PERFORMED PERMANENT REPAIR TO CABIN FLOORBEAM AT STA 365 RBL 8 REF ECRA 5320-01913 STEPS 1 THRU 6. 2 L 7 2 4F RT A2NM 20081205 NM 2008 12 5 CALA2008112501101 1 20081125 A 5311 146N1006 FRAME BOEING 757 757224 1384958 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19141 30354 TOP OF FRAME HAS DEEP GOUGE STA 1300 STR 25R (APPROX). REPAIRED FRAME STA 1300 STR 25R REF ECRA 5311-01436. 2 L 7 2 4F RT A2NM 20081205 EA 2008 12 5 SWIA200820522 1 20080916 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 465SW 7845 DURING C-CHECK, LEFT ENGINE THRUST MOUNT CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 ASAA0843891 1 20081029 A 5311 654659683 FRAME BOEING 737 7374Q8 138447Q NM BS 727 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER EA 400 53EA 00267. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008120301123 1 20081203 A 5315 147A5506 FLOORBEAM BOEING 737 737924 13848A1 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 38403 30120 STA 986.5 FLOORBEAM HAS CORROSION AT FASTENER HOLES LOCATED AT LBL 4 AND AT RBL 4 FWD FLANGE. REPAIRED FLOORBEAM 986.5 PER SRM 53-0051. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008120101104 1 20081127 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 66051 29446 DOOR R4 EMERGENCY LIGHT AFT WALL AND DOOR LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY CHARGER PER AMM 33-51-07 AND OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 20081205 NM 2008 12 5 CALA2008120101106 1 20081129 A 3350 D71702030 CHARGER BOEING 737 737724 13844BY NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 39728 28944 OVERHEAD BIN BULLNOSE AT ROWS 17 AND 20 AND SEAT ROWS 22 TO 25 EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTE RY PACK AND CHARGER, OPS CHECKS GOOD. 2 L 7 2 4F RT A16WE 20081203 SO 2008 12 3 C2XA08TY137 1 20081126 A 3350 251005 FUSE EMB 145 EMB145LR 3260212 SO BATTERY BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26545 145558 RT & LT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY TRAY FUSE IAW RADIANT POWERCO RP VCMM 25-60-03. OPS CHECK GOOD AND AIRCRAFT RELEASE FOR SERVICE. 2 L 7 2 4T RT T00011AT 20081203 SO 2008 12 3 C2XA08RI174 1 20081104 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145XR 3260214 SO LANDING GEAR DEFECTIVE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 23139 145731 FLIGHT 2859 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS AND ENGINE 1/2 REV DISAGREE AFTER SELECTING GEAR UP. CREW PERFORMED AIR RETURN AND LANDED AIRCRAFT UNEVENTFULLY. MESSAGES DISAPPEARS WHEN SELECTED GEAR DOWN. EWR MX REMOVED AND REPLACED PROXIMITY SWITCH AND SERVICED NOSE LANDING GEAR. MX PERFORMED OPERATIONAL CHECKS SU CCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081203 SO 2008 12 3 C2XA08SH 1 20081202 A 5544 12033817005 ATTACH FITTING EMB 145 EMB145LR 3260212 SO RUDDER DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13955 145075 SHV - DURING C-CHECK RUDDER 1 UPPER ACTUATOR ATTACHMENT LOWER HINGE UPPER HAT BUSHING MIGRATED. 2 L 7 2 4T RT T00011AT 20081203 SO 2008 12 3 C2XA08SH154 1 20081203 A 5512 14552201402 SKIN EMB 145 EMB145XR 3260214 SO HORIZ STAB CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24103 145645 RT HORIZONTAL STAB L/E HAS CORROSION AROUND RIVETS. RT HORIZONTAL STAB L/E WAS REPAIRED IAW EC 5510-01195. THE AIRCRAF T WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081204 SO 2008 12 4 C2XA08TY134 1 20081123 A 4920 M4504113A APU EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A C2XA F ACTIVATE FIRE EXT. J WARNING INDICATION IN INSP/MAINT 1 SW 27 16976 145171 BNA - MX WAS IN THE COCKPIT OF THE A/C TROUBLESHOOTING THE APU, AND RECEIVED AN APU FIRE MESSAGE AND DISCHARGED THE FIRE BOTTLE. THE APU FIRE BOTTLE WAS REMOVED AND REPLACED IAW EMB 145 AMM 26-22-01 AND OPS CHECKED GOOD. THE APU WAS REMOV ED AND REPLACED IAW T/C 6849001 AND THE OPS AND LEAK CHECK WERE GOOD. A/C HAS BEEN RELEASED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081204 NM 2008 12 4 R61A20080048 1 20081119 A 5320 STRUCTURE EMB ERJ170 ERJ170100SU 3260403 NM FUSELAGE DENTED A R61A K NONE O OTHER IN INSP/MAINT 1 GL 11 821MD 17000042 DENT AT FRAME 91 TO FRAME 92, STRINGER 21 RT AND 23 RT. PERFORMED MAJOR REPAIR PER EMBRAER ENGINEERING INSTRUCTION. 2 L 7 2 4F RT A56NM 20081204 NM 2008 12 4 SWAA086732 1 20081202 A 2560 25270017 GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN DETERIORATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 788SA 30603 DURING SCHEDULED 8Y CHECK, FOUND CABIN FLOOR PHOTOLUMINESCENT LIGHT STRIP IN POOR CONDITION. REMOVED AND REPLACED STRIP PER SWA DWG. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086661 1 20081126 A 5312 6517582 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED SPV CHECK, FOUND LT VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17, WL 232. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086662 1 20081126 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 631SW 27706 AFT I/B FLASHLIGHT BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086663 1 20081126 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086664 1 20081126 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086669 1 20081127 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 902WN 36615 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086672 1 20081201 A 5753 65C26320 SUPPORT FITTING BOEING 737 7373H4 1384600 NM TE FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND LT OUTBOARD MIDFLAP INBOARD SUPPORT FITTING CORRODED. REPAIRED FITTING PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086673 1 20081130 A 5310 65C807351 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM CORRODED AT BS 954, RBL 53. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081204 2008 12 4 SWAA086733 4 20081202 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 255WN 32513 R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081204 2008 12 4 SWAA086734 4 20081202 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR SLIDE OUT OF POSITION. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086704 1 20081201 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086705 1 20081201 A 3350 MS2537 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND EMERGENCY AISLE LIGHT INOP AT ROW 13. REPLACED LAMP PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086706 1 20081201 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 27L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086674 1 20081130 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086675 1 20081201 A 3350 MS25237 LIGHT BOEING 737 737317 138447P NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. RESEATED LAMP PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086680 1 20081201 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086681 1 20081201 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086714 1 20081202 A 5322 6546546 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, RBL 3, WL 149. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086735 1 20081201 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 401WN 29813 DURING SCHEDULED MV1 CHECK, FOUND EEPLS STRIP INOP AT ROW 1. REPAIRED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081204 2008 12 4 SWAA086654 4 20081201 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 498WN 32480 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081204 2008 12 4 SWAA086655 4 20081201 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 498WN 32480 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081204 2008 12 4 SWAA086656 4 20081201 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 498WN 32480 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086688 1 20081201 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727B, BETWEEN STR 8R TO STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086690 1 20081201 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086691 1 20081201 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086703 1 20081201 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008112401094 1 20081123 A 5320 65C3397053 FLOOR SUPPORT BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14652 28913 CABIN BETWEEN STA 340 AND 360 BL 0 FLOOR SUPPORT CRACKED. REMOVED AND REPLACED FLOOR SUPPORT REF 51-40-02. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008112401095 1 20081123 A 5315 141T5108 SUPPORT BOEING 767 767224 1385170 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 67158 30437 CABIN - BS 325 LBL 27- LBL 60 FLOOR SUPPORT FOUND CORRODED. CABIN BS 325 LBL 16- LBL 62 FLOORBEAM SUPPORT REPAIRED PER SRM 53-00-51 REPAIR 1, FIG 201. HFEC NO CRACK FOUND. 2 L 7 2 4F RT A1NM 20081205 NM 2008 12 5 FDEA200812035072 1 20081203 A 5320 140N51501 SHEAR WEB BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 BS 1020, RBL 65, CREASE BEAM WEB IS CORRODED. REMOVED CORROSION, BS 1020, RBL 65, ON CREASE BEAM WEB IAW SRM 51-10-02 A ND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13. L=.50, W=.50, D=.015. FABRICATED NEW WEB ON MAE TRAVELER T8/759905, TREA TED, PRIMED WEB IAW SRM 51-20-01. INSTALLED NEW WEB, BS 1020-1040, RBL 65, IAW RM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20081205 NM 2008 12 5 UPS08M53948 1 20081118 A 5320 ACA37951 PAN DOUG MD11 MD11F 3023600 NM NLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 281UP 48538 INSPECTION TYPE:SPV DURING SPECIAL VISIT- SAA, FOR MLG CHANGE, NLG DOOR JAMB AFT LT WAS FOUND TO BE BENT AND CRACKED. T RIMMED OUT DAMAGED AREA 3 INCHES, REPAIRED PERFORMED PER EO -MD11- 5320-31154-A AND PER INSTRUCTIONS IN EA 011-5320-01-A 1555. 2 L 7 3 4F RT A22WE 20081203 NM 2008 12 3 ZZDA2008171 1 20081114 A 3210 3790055102 CYLINDER BOEING 717 717200 1383700 NM LANDING GEAR LEAKING A ZZDA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 37 944AT 55007 RIGHT HYDRAULIC PRESSURE LOW. REMOVED & REPLACED THE MAIN LANDING GEAR TRANSFER CYLINDER PER M/M REFERENCE 32-33, SERVI CED HYDRAULIC SYSTEM AND SAFTIED RIGHT SPOILER BYPASS PER M/M REFERENCE 12-13 AND PERFORMED FUNCTIONAL CHECK OF THE MAIN LANDING GEAR EXTENSION AND RETRACTION PER M/M REFERENCE 32-30. 2 L 7 2 4F TR A6WE 20081203 NM 2008 12 3 KCSA081588 1 20081117 A 5320 SUPPORT BOEING 747 747212B 1384886 NM FUSELAGE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 APU AFT HORIZONTAL SUPPORT CHAFED ON UPPER SIDE RBL 3 TO RBL 12 STA 2722. 2 L 7 4 4F RT A20WE 20081203 WP 2008 12 3 UPS08853899 1 20081025 A 5230 WEB DOUG DC8 DC871F 302199D WP CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV EVALUATE EFN 700200081061 ORGINIAL NRC 212907 B-PIT DOOR WEB STA 280. REPAIR ACCOMPLISHED DC8 SRM 52 -2-00-0 FIG 3. 2 L 7 4 4F RT 4A25 20081203 WP 2008 12 3 UPS08853915 1 20081113 A 5210 DOOR DOUG DC8 DC873F 302199F WP L1 OUT OF RIG A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:N/A L1 DOOR EXTREMELY HARD TO OPEN OR CLOSE. RERIGGED L-1 DOOR. OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 20081203 WP 2008 12 3 AALA200810228 1 20081107 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 CORROSION ON CUSP AT STATION 503 TO 617. REPLACED CUSP PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081203 NM 2008 12 3 AALA200810242 1 20081120 A 3211 TRUNNION BOEING 737 737823 13844BZ NM RT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948AN 30086 RIGHT MAIN GEAR FORWARD TRUNNION LUG BORE HAS CORROSION. REPAIRED PER SRM 57-20-90-2R-2. 2 L 7 2 4F RT A16WE 20081203 NM 2008 12 3 AALA200810243 1 20081120 A 3211 TRUNNION BOEING 737 737823 13844BZ NM RT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948AN 30086 RIGHT MAIN GEAR FORWARD TRUNNION LUG BORES HAVE CORROSION AT UPPER OUTBOARD LUG. REPAIRED PER SRM 57-20-90-2R-2. 2 L 7 2 4F RT A16WE 20081203 WP 2008 12 3 AALA200810226 1 20081108 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 CORROSION ON SUBFLOOR, STATION 200 TO 218 BETWEEN NUMBER 4 AND NUMBER 5 SEAT TRACKS. REPAIRED PER AARD 53-20-00-16, INS TALLED DOUBLER. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200810229 1 20081107 A 5330 FINGER DOUBLER DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 CORROSION ON SKIN SPLICE FINGER DOUBLER STATION 1245 TO 1310 AT LONGERON 26L. REMOVED AND REPLACED SKIN SPLICE FINGER D OUBLER AND INSTALLED LONGERON SPLICES AT STATION 1240 AND 1310 PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200810206 1 20081031 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 RIGHT CUSP MEMBRANE CORRODED STATION 655-674. INSTALLED CUSP DOUBLER STATION 654-670. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200810207 1 20081103 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 RIGHT CUSP MEMBRANE CORRODED STATION 886-905. INSTALLED CUSP DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200810208 1 20081104 A 5320 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 MID CARGO DOOR BEAM CORRODED STATION 637-693. INSTALLED DOOR BEAM DOUBLER PER AARD 53-10-00-3. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200810209 1 20081104 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 LEFT CUSP MEMBRANE CRACKED AT STATION 1250 BELOW THE NUMBER 2 SEAT TRACK. INSTALLED NEW SECTION OF CUSP FROM STATION 11 74-1250 PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081203 EA 2008 12 3 SWIA200820500 1 20080923 A 5320 BEAM CNDAIR CL600 CL6002D24 1390016 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 802SK 15061 DURING C-CHECK, FS 280 BEAM CORRODED AT LBL9 AND RBL9. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820502 1 20080923 A 5312 BULKHEAD CNDAIR CL600 CL6002D24 1390016 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 802SK 15061 DURING C-CHECK, FS 280 LEFT BULKHEAD WEB CORRODED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081203 SO 2008 12 3 C2XA08IA246 1 20081125 A 3350 7287580503 LIGHT EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14933 145018 IAH - FLIGHT 2819 - DURING POST FLIGHT INSPECTION THE CREW REPORTED THE 3RD AISLE PATH EMERGENCY LIGHT TO BE INOPERATIVE . MAINTENANCE REMOVED AND REPLACED THE AFFECTED AISLE PATH LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20081203 WP 2008 12 3 AALA200810230 1 20081110 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 CORROSION ON RIGHT CUSP MEMBRANE STATION 560-579. INSTALLED NEW CUSP MEMBRANE STATION 503-598. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200810231 1 20081111 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 LONGERON 30 CORRODED AT STATION 446-465. INSTALLED LONGERON "U" CHANNEL SPLICE IN LONGERON 30 PER SRM 53-02-00. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200810214 1 20081105 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 LONGERON 4 LEFT CRACKED AT STATION 180 AND 200. SPLICED IN A NEW SECTION OF LONGERON. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200810236 1 20081106 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 SEAT TRACK NR 2 CORRODED STATION 1221 TO 1307. REPLACED SEAT TRACK SECTION FROM STATION 1031 TO 1309 PER AARD 51-010-00 -012. 2 L 7 2 4F A6WE 20081203 SO 2008 12 3 C2XA08IA238 1 20081114 A 3350 74441 SIGN EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12967 145133 IAH - DURING A-CHECK INSPECTION THE EMERGENCY EXIT SIGN ABOVE THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SIGN, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081203 SO 2008 12 3 C2XA08IA239 1 20081114 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 27 16951 3361 3361 145063 LRD - FLIGHT 2858, THE CREW REPORTED SEVERAL EMERGENCY LIGHTS WOULD NOT TEST. THE CREW CHARGED THE EMERGENCY LIGHT BATT ERIES, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081203 SO 2008 12 3 C2XA08RI173 1 20081102 A 2913 971533 PUMP EMB 145 EMB145LR 3260212 SO NR 1 LEAKING A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 14902 15357 145496 FLIGHT 2554 - RIC - FLIGHT CREW REPORTED HYDRAULIC SYSTEM NR 1 LOW QTY INDICATION IN FLIGHT, SYSTEM INDICATION IN AMBER AND DECREASING. CREW DECIDED TO DIVERT FLIGHT TO RIC AND LANDED AIRCRAFT UNEVENTFULLY. RIC MX REMOVED AND REPLACED HYDR AULIC PUMP NR 1 AND PERFORMED OPERATIONAL TESTS SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081203 SO 2008 12 3 C2XA08RI172 1 20081101 A 2460 MASTER SWITCH EMB 145 EMB145LR 3260212 SO COCKPIT DIRTY A C2XA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SW 27 16571 145633 FLIGHT 2706 - GSO - FLIGHT CREW REPORTED DURING CLIMBOUT LOST PFD NR 2, MFD NR 1, RRMU NR 2, TRANSPONDER, RA ON EICAS ME SSAGE. PFD NR 2, FMS NR 2 ALSO WAS LOST. AVIONICS SWITCH LIGHT ON DESCENT. CREW PERFORMED AIR RETURN AND LANDED AIRCR AFT UNEVENTFULLY. MX CLEANED AVIONICS MASTER SWITCH NR 2 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS AP PROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081203 GL 2008 12 3 C2XA08IA240 2 20081117 A 7200 AE3007A1E ENGINE EMB 145 EMB145XR 3260214 SO ALLSN AE3007 AE3007A 03030 GL NR 2 MALFUNCTIONED A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 14148 15286 5050 145751 CAE312474 IAH - FLIGHT 2574, THE CREW REPORTED A LAV SMOKE DETECTOR WARNING DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT L ANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 20081203 NM 2008 12 3 SWAA086684 1 20081201 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 787, STR. 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081203 NM 2008 12 3 SWAA086736 1 20081202 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 446WN 29842 FOUND, OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081204 EA 2008 12 4 COMA2008111950001 1 20081119 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 807CA 21930 7364 FOUND DAMAGE TO FUSELAGE SKIN BETWEEN FS 235.00 AND FS 250.00 BETWEEN STR 25R AND STR 26R. REPAIRED FUSELAGE SKIN AT FS 235.00 - FS 250.00 STR 25- STR 26 RT IAW REO 601R-53-11-1490. 2 L 7 2 4F RT A21EA 20081204 NM 2008 12 4 UPS08553937 1 20081115 A 5610 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT OUT OF ADJUST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 469UP 25485 INSPECTION TYPE:N/A CAPTAIN L2 WINDOW HARD TO CLOSE WHEN LATCH REACHED NEAR CLOSE POSITION. REMOVED TRIM AND WINDOW HEA T DISCONNECTED. ADJUSTED WINDOW AND INSTALLED TRIM AND WINDOW HEAT PER MM 56-11-2-5. 2 L 7 2 4F RT A2NM 20081204 NM 2008 12 4 UPS08M53923 1 20081115 A 5240 ACA3822512 SKIN DOUG MD11 MD11F 3023600 NM DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP 48768 INSPECTION TYPE:N/A CRACK IN DOOR SKIN AND PAN. REPAIRED PER EO MD11-5240-31188-A. 2 L 7 3 4F RT A22WE 20081205 NM 2008 12 5 CALA2008120301118 1 20081202 A 5311 6546549 FRAME BOEING 737 7373T0 1384582 NM FRAME DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14336 23574 AFT CARGO BAY FRAME DENTED AT STA 767, S-25R. REPAIRED FRAME AT STA 767 RT STRINGER 25R IAW B737 SRM 51-70-11. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 R61A20080046 1 20081124 A 2752 C1583901 ACTUATOR EMB ERJ170 ERJ170200LR 3260121 NM TE FLAP DEFECTIVE A R61A O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 106HQ 4383 4383 17000164 ON APPROACH CREW REPORTED THEY HAD A FLAP/SLAT FAIL MESSAGE ON EICAS. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT . MAINTENANCE REMOVED AND REPLACED RIGHT NR 2 FLAP ACTUATOR AND COMPLETED CHECKS SYSTEM OPERATIONAL CHECK WAS GOOD. AI RCRAFT THEN COMPLETED A OPERATIONAL CHECK FLIGHT AND OPERATIONAL CHECK FLIGHT WAS SATISFACTORY. AIRCRAFT WAS RETURNED T O SERVICE. 2 L 7 2 4F RT A56NM 20081204 NM 2008 12 4 UPS08M53933 1 20081115 A 5330 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C SURVEY SEQUENCE NUMBER 254-F1-008 OF MD11-5100-30530 APPENDIX C ITEM 2 CORROSION FOUND ON FASTENER HO LE ON REPAIR DOUBLER RT SIDE STA 2134 L33R- L35R. REMOVED REPAIR, FABRICATED, AND INSTALLED NEW REPAIR DOUBLER IAW MD-1 1 SRM VOL 1 53-00-01 FIG 13. 2 L 7 3 4F RT A22WE 20081204 2008 12 4 SWAA086739 4 20081202 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 FOUND L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086742 1 20081202 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 914, STR 25L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086743 1 20081202 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BETWEEN BS 967 TO BS 987, STR 25L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086744 1 20081202 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 26L TO 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086745 1 20081202 A 5320 6545819 WEB BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND VERTICAL WEB CRACKED AT BS 227, BL 0. REPAIRED WEB PER PAE DWG. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086749 1 20081202 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 16L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086752 1 20081202 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 520, STR 23L. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086753 1 20081202 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 23L TO STR 24L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086695 1 20081201 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR. 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086636 1 20081126 A 2560 65C16820 FITTING BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 251WN 32510 R1 DOOR EMERGENCY EXIT SLIDE GIRT BAR FWD CLIP LOOSE. SECURED CLIP PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086640 1 20081130 A 5322 6546529 SHEAR TIE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED SPV CHECK, FOUND FWD CARGO SHEAR TIE CORRODED AT BS 500C, BETWEEN STR 26L TO STR 25L. REPAIRED SHEAR T IE PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086632 1 20081130 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 229WN 32498 FOUND FWD EEPLS LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086715 1 20081202 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086716 1 20081202 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086717 1 20081202 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086723 1 20081202 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086628 1 20081127 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 203WN 32483 DURING SCHEDULED MV3 CHECK, FOUND LT EEPLS LENS LOOSE. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 ASAA0843917 1 20081122 A 5340 653535214 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 STRINGER CLIP CRACKED. REPLACED CLIP PER ASA DWG A53100265816. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 ASAA0843918 1 20081030 A 5330 65458001203 BEAR STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 L1 DOOR UPPER HINGE CUTOUT SKIN AND BEARSTRAP CRACKED. REMOVED DAMAGE FABRICATED AND INSTALLED BEARSTRAP FILLER REPAIR DOUBLER REPAIR FILLER IAW ASA EA 400 53EA 00284. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 ASAA0843884 1 20081029 A 5311 654655244 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400 53EA 00267. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 ASAA0843885 1 20081029 A 5311 65C32961503 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLERS PER EA 400 53EA 00267. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 ASAA0843897 1 20081029 A 5311 6546525112 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER EA 400 53EA 00267. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 ASAA0843900 1 20081029 A 5311 65465311 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400 53EA 00267. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 CALA2008120301117 1 20081203 A 3350 ADD71701100 BATTERY PACK BOEING 737 737824 13844BZ NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26215 28775 L-1 DOOR BATTERY PACK FAILED TEST. REMOVED AND REPLACED L-1 DOOR BATTERY PACK PER AMM 33-51-06, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008112601102 1 20081126 A 3350 S283W6032 POWER SUPPLY BOEING 757 757224 1384958 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17104 27294 PASSENGER EMERGENCY LIGHT AT ROW 32 ABC OUT. NO POWER TO RECEPTACLE. REPLACED RECEPTACLE, NO HELP. TROUBLESHOT PER WD M 33-51-15. FOUND M736 POWER SUPPLY INOPERATIVE. REMOVED AND REPLACED M736 POWER SUPPLY. OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 20081205 NM 2008 12 5 CALA2008111901086 1 20081117 A 5320 141A541059 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 79279 31597 FORMED INTERCOSTAL BETWEEN STA 328 AND 344 AT LBL46 IS CRACKED AT FASTENER HOLE. REMOVED AND REPLACED INTERCOSTAL REF S RM 51-40-02. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008111901087 1 20081118 A 5315 141N51221 FLOORBEAM BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19141 30354 CABIN FLOORBEAM AT STA 365 RBL 40 HAS SMALL AREA OF SURFACE CORROSION. PERFORMED PERMANENT REPAIR TO CABIN FLOORBEAM AT STA 365 RBL 40 REF ECRA 5320-01913 STEPS 1 THRU 6. 2 L 7 2 4F RT A2NM 20081204 NM 2008 12 4 SWAA086647 1 20081126 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED MV4 CHECK, FOUND SKIN CRACKED AT BS 438, STR 31L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086648 1 20081130 A 3350 101331 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED MV2 CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086649 1 20081130 A 3350 6574550 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED MV3 CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 20 TO ROW 21. REMOVED AND REPLACED LIG HT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086650 1 20081125 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT LOOSE AT ROW 1. REMOVED AND REPLACED EEPLS PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086725 1 20081202 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086726 1 20081202 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT E/E EXHAUST PORT OPENING AT BS 379, LBL 2, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086727 1 20081202 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 660, BL 0. REPAIRED BEAM PER SI. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086728 1 20081202 A 5330 6545800219 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR SKIN CUTOUT CRACKED AT BS 305, BELOW WL 236. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086730 1 20081202 A 5330 6545765 SKIN BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 500D, STR 27L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086731 1 20081202 A 5512 65C25727 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 787SA 29812 DURING SCHEDULED 8Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 142. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NE 2008 12 4 U5QA06014 2 20081116 A 7261 31B406704 ENGINE LEAR 60 60LEAR 5170707 CE PWA 305 PW305 NE RIGHT LEAKING E U5QA B EMER. DESCENT K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 923SK 7093 050 PCE305217 SUNDAY MORNING 11-16-08 ON A PART 91 FLIGHT FROM KCLL TO KDAL APPROXIMATELY 20 MIKES SOUTH OF KDAL PILOT REPORTED SMOKE IN CABIN. AT THAT POINT THE CREW DECLARED AN EMERGENCY, AND WERE GIVEN PRIORITY LANDING. LANDED WITHOUT INCIDENT AT KD AL. MAINT RAN ENGINES AND FOUND RT ENGINE OIL LEAK INTO BYPASS AIR TO BE IN BLEED AIR DUCTS. 2 L 7 2 4F 4 F RT A10CE E35NE 20081204 WP 2008 12 4 AALA200802344 1 20081016 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AA 49338 LGA - EMERGENCY FLASHLIGHT AT AFT JUMPSEAT HAS MISSING STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT JUMPSEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081204 WP 2008 12 4 AALA200802345 1 20081016 A 3350 LENS DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7550 53032 DFW - EMERGENCY DOUBLE ARROW EXIT MARKER AT FORWARD ENTRY HAS DAMAGED LENS. REPLACED LENS FOR EMERGENCY DOUBLE ARROW EX IT MARKER AT FORWARD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081205 NM 2008 12 5 ASAA0843892 1 20081029 A 5311 6546596164 FRAME BOEING 737 7374Q8 138447Q NM BS 727 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400-53EA-164. 2 L 7 2 4F RT A16WE 20081204 EA 2008 12 4 RU3A004 1 20081020 A 2910 601R7514785 HYDRAULIC LINE CNDAIR CL600 CL6002B16 1900305 EA PYLON CHAFED E RU3A O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 15 87 5350 5190 NUMBER 2 HYDRAULIC SYSTEM LOST PRESSURE ON APPROACH. FOUND PRESSURE HOSE ASSY IN PYLON CHAFED BY HOSE CLAMP WHERE RUBBE R LINER WAS ERODED AND THE CLAMP AND HOSE WERE METAL TO METAL. REPLACED HOSE, CLAMP, AND ENGINE DRIVEN HYDRAULIC PUMP. INSPECTED FILTERS, LEAK AND OPS CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 20081204 NM 2008 12 4 SWAA086665 1 20081129 A 3350 8200048801 LENS BOEING 737 7373T5 1384608 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED MV2 CHECK, FOUND OVERHEAD EMERGECY EXIT LIGHT LENS MISSING AT ROW 19. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086667 1 20081127 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 761RR 27875 DURING SCHEDULED HC1 CHECK, AFT RT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086719 1 20081202 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086720 1 20081202 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086721 1 20081202 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086633 1 20081129 A 3350 284A01215 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 238WN 34713 DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086634 1 20081130 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 239WN 34714 DURING SCHEDULED MV3 CHECK, FOUND FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086635 1 20081127 A 3350 81000 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 247WN 32508 RT AFT EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008120201113 1 20081202 A 3233 65448106 UPLOCK ACTUATOR BOEING 737 737524 1384721 NM LT MLG INOPERATIVE A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 19621 38723 20787 27334 LEFT LANDING GEAR WOULD NOT REMAIN IN UP AND LOCKED POSITION AFTER TAKEOFF, LANDING NORMAL SINK RATE. OVERWEIGHT LANDIN G 114.9. REMOVED AND REPLACED LEFT INBOARD MAIN LANDING GEAR UPLOCK ACTUATOR, AND LUBED LEFT MAIN LANDING GEAR PER AMM 32-32-41. OPERATIONAL CHECKS GOOD, OK TO CONTINUE. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008112501100 1 20081125 A 5311 6558240 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14652 28913 AIR CONDITIONING SUPPORT BRACKET ATTACHED TO THE FRAME BETWEEN STRINGER 8 AND 9 CRACKED AROUND HOLE STA 360 L. REPAIRED CRACK AROUND HOLE AT STA 360 L, REMOVED DAMAGED AREA (CUT OUT IN ITEM 1, 2, 3) AND MADE REPAIR ANGLES "A" & AMP; "B" AN D INSTALLED AS REF EA5310-04498. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008120301122 1 20081202 A 5315 141T5107 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 68159 30438 CABIN - FLOOR SUPPORT FOUND CORRODED AT BS 303 BETWEEN LBL 20-35. CABIN FLOOR SUPPORT BEAM STA 303 LBL 20 TO LBL 60 REP AIRED PER SRM 53-00-51 REPAIR 1 FIG 201 AND HFEC NO CRACK FOUND. 2 L 7 2 4F RT A1NM 20081205 SO 2008 12 5 CHQA200800225 1 20081117 A 2130 UNKNOWN EMB 135 EMB135KL 3260302 SO ALLSN AE3007 AE3007A 03030 GL CABIN PRESSURE UNKNOWN A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 374SK 145544 CAE311206 FLIGHT 5319, EWR TO STL - CREW REPORTED THAT DURING CLIMB AT ABOUT 5,000 FT THE CABIN DIFFERENTIAL, CABIN RATE OF CLIMB, AND CABIN ALTITUDE INDICATIONS DASHED OUT. THE CREW TRIED MANUAL MODE WITH NO HELP. THE AIRCRAFT RETURNED TO EWR AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET POWER TO THE AIRCRAFT AND ALL PRESSURIZATION INDICATIONS RETURNED TO NORMAL. PRESSURIZATION CHECKS WERE PERFORMED WITH NO FURTHER DEFECTS NOTED. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081205 NM 2008 12 5 ASAA0843902 1 20081029 A 5311 6546548120 FRAME BOEING 737 7374Q8 138447Q NM BS 747 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER EA 400 53EA 00267. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0843893 1 20081029 A 5311 654659684 FRAME BOEING 737 7374Q8 138447Q NM BS 727 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400 53EA 00267. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008120101107 1 20081126 A 5412 311N50054 FITTING BOEING 757 757224 1384958 NM RT PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17128 27567 NR 2 PYLON TORQUE BULKHEAD FITTING IS CRACKED AT HOLES 19 AND 20. REF EA 5440-01234, REEC. REMOVED AND REPLACED NR 2 P YLON TORQUE BULKHEAD FITTING PER EC/RA 5440-01304 AND 5450-01753. 2 L 7 2 4F RT A2NM 20081205 NM 2008 12 5 CALA2008120101112 1 20081201 A 5320 141A541012 INTERCOSTAL BOEING 737 737924 13848A1 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 38403 30120 CABIN FLOOR INTERCOSTAL CRACKED BETWEEN STATION 312 AND 328 LBL 40. REMOVED AND REPLACED INTERCOSTAL AT STATION 312 - 3 28 PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008112401092 1 20081122 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14652 28913 AIR CONDITIONING SUPPORT BRACKET ATTACHED TO THE FRAME BETWEEN STRINGER 8 & AMP; 9 CRACKED AROUND RIVET HOLE STA 867L. REPAIRED FRAME AT STA 867L STRINGER 8 & AMP; 9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008112401096 1 20081123 A 5330 141T32317 SKIN BOEING 767 767224 1385170 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 67158 30437 FOUND FASTENER AT STA 368 AROUND S-30 DAMAGED BY LIGHTNING STRIKE. TOTAL DAMAGE 0,250 IN RIVET HEAD DAMAGE 0,091 IN. PE R SRM 53-00-01 P103 TABLE III DETAIL IV NEEDS FASTENER REPLACEMENT WITHIN 50 FLIGHT CYCLES. PERFORMED INTERIM REPAIR PE R PART 1-2. PERFORM INSPECTIONS AT INTERVALS NOT TO EXCEED 30 DAYS AND ACCOMPLISH A PERMANENT REPAIR WITHIN 90 DAYS. R EFERENCE L/P 9100380 FOR INTERIM REPAIRS AT STATION 325, 347 AND 412. ALL WORK WAS PERFORMED FROM ECRA 5330-03837. INS PECTED INTERIM REPAIR AT STATION 368 IAW ECRA 5330-03837, PART 2, NO DEFECTS NOTED. INSPECTED AREA, REF ECRA 5330-03837 PART II, REPAIR SECURE. NO FURTHER DAMAGE. DIP REMAINS. FUSELAGE SKIN STA 368 S30L REPAIRED AS PER ECRA 5330-03837 RE 2 L 7 2 4F RT A1NM 20081205 2008 12 5 UPS08M53958 4 20081119 A 2565 BATTERY DOUG MD11 MD11F 3023600 NM EVAC SLIDE DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A L-1 DOOR SLIDE PRESSURE NO PTT REF M388837. REPLACED BATTERIES. OPS CHECKS GOOD PER MM 25-61-04-5. THIS CLEARS M388837, PLACARDS REMOVED. 2 L 7 3 4F RT A22WE 20081205 NM 2008 12 5 UPS08M53959 1 20081118 A 3350 LIGHT DOUG MD11 MD11F 3023600 NM COCKPIT MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:N/A EMERGENCY LIGHT SWITCH IS SUSPECTED TO BE FAULTY. EMERGENCY LIGHTS WILL NOT COME ON. BATT PACK ALR EADY REPLACED. REPLACED LIGHT SWITCH PER MM 33-41-01, NO HELP. CYCLED EMERGENCY LIGHTS CONTROL CIRCUIT BREAKER. ALL E MERGENCY LIGHTS OPS NORMAL PER MM 33-50-00-5. 2 L 7 3 4F RT A22WE 20081205 NM 2008 12 5 UPS08M53960 1 20081116 A 3350 6044115 POWER SUPPLY DOUG MD11 MD11F 3023600 NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY PER MM 33-51-01-4. REQUIRES FURTHER TROUBLESHOOTING. DEFERRAL M388782. 2 L 7 3 4F RT A22WE 20081205 EA 2008 12 5 COMA2008112450002 1 20081121 A 2752 854D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 408CA 16784 7440 FLAPS FAILED AT 0 DEG ON APPROACH INTO JFK. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED RIGHT OTBD FLA P OTBD ACTUATOR. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 COMA2008112450003 1 20081121 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 940CA 7048 FLAPS FAILED AT 0 DEG ON APPROACH INTO DTW. EMERGENCY DECLARED, A/C LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I000 2, FLAPS FAIL CAUTION MESSAGE FOLLOW UP MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 20081205 SO 2008 12 5 CHQA200800233 1 20081128 A 3350 RPS1B BATTERY PACK EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL EMERGENCY LIGHT INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 561RP 4860 1249 145447 CAE311826 DURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOP. THE NR 4 EMERGENCY POWER SUPPLY WAS REPLACED AND THE OVERWING EMERGENCY LIGHTS OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081205 NM 2008 12 5 ASAA0843905 1 20081029 A 5311 654655819 FRAME BOEING 737 7374Q8 138447Q NM BS 907 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400 53EA 00267. 2 L 7 2 4F RT A16WE 20081205 EA 2008 12 5 MASA2008111700781 1 20081117 A 2197 CONNECTOR CNDAIR CL600 CL6002D24 1390016 EA TEMP SENSOR DIRTY A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 904FJ 15004 ASH 2889 BUR-PHX. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE DUE TO SMOKE IN THE COCKPIT. MX CLEANED AND TIGHTENED RT INLET TEMP SENSOR CONNECTOR. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 MASA2008120200733 1 20081202 A 3350 1317 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 503MJ 10058 ASH FLT 7172 ATW-ORD. CREW REPORTED AN OVERHEAD EMERGENCY EXIT FLOOD LIGHT INOPERATIVE AT ROW NINE. MX RELAMPED. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 ASAA0843914 1 20081128 A 5340 653535214 STRINGER CLIP BOEING 737 7374Q8 138447Q NM BS 380 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 STRINGER CLIP CRACKED. REPLACED CLIP PER ASA DWG A53100265816. 2 L 7 2 4F RT A16WE 20081205 EA 2008 12 5 MASA2008120100732 1 20081201 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 77195 7195 ASH FLT 7083 ORD-SBN. FOUR EMERGENCY FLOOR LIGHT STRIPS ARE INOPERATIVE. MX REPLACED THE WIRING HARNESS AND OPS CHECKE D GOOD. 2 L 7 2 4F RT A21EA 20081205 2008 12 5 SWIA200820505 3 20081123 A 6140 PROPELLER EMB 120 EMB120ER 3260203 SO RIGHT SURGES A SWIA K NONE O OTHER CL CLIMB 1 NM 07 561SW 120335 FLT 7802 - RIGHT PROP NP ABOVE TOLERANCES ON CLIMB-OUT. RAN ENGINES, UNABLE TO DUPLICATE. 2 L 7 2 4T RT A31SO 20081205 EA 2008 12 5 MASA2008112000788 1 20081124 A 7830 SWITCH CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER OUT OF RIG A MASA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SW 07 593ML 7463 ASH FLT 7229 CAE-LEX. EN ROUTE TO ORD CAPTAIN DIVERTED TO LEX DUE TO A RT REV UNLOCK CAUTION MESSAGE. CAPTAIN DECLARED EMERGENCY. MX RE-RIGGED STOW MICRO SWITCHES. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 MASA2008112200787 1 20081122 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAP MALFUNCTIONED A MASA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 77302 7886 7302 ASH FLT 1004 HNL-LIH. CREW REPORTED FLAPS FAIL AT 2 DEGREES, DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. MX REPLA CED BPSU AND RT OUTBOARD ACTUATOR. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 MASA2008112500789 1 20081125 A 3230 LANDING GEAR CNDAIR CL600 CL6002D24 1390016 EA MALFUNCTIONED A MASA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 929LR 15029 ASH FLT 2679 CLT-SAT. CREW RETURNED TO THE FIELD AND DECLARED AND EMERGENCY DUE TO LANDING GEAR WOULD NOT RETRACT. MX OPS CHECKED SYSTEM AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 CALA2008120301120 1 20081202 A 5310 6520723054 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14336 23574 FWD CARGO DOOR CUTOUT AFT FRAME IS CRACKED AT STRINGER 24 AT TOP OF FOOT PRINT FOR DOOR STOP, FWD SIDE OF FRAME. REMOVE D CRACKED FRAME. DRILLED UP NEW FRAME AND INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008112501099 1 20081125 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14652 28913 AIR CONDITIONING SUPPORT BRACKET ATTACHED TO THE FRAME BETWEEN STRINGER 8 AND 9 CRACKED AROUND RIVET HOLE STA 827L. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED ALL REPAIR PARTS PER ECRA 5311-01435. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008120301121 1 20081202 A 5315 147A5506 FLOORBEAM BOEING 737 737924 13848A1 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 38403 30120 STA 986.5 FLOORBEAM HAS CORROSION AT FASTENER HOLE, AFT FLANGE, LBL 17. CUT OUT DAMAGED AREA AND REPAIRED PER SRM 53-00 -51 REPAIR 1 PAGE 204. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 UIEA200800344 1 20081126 A 5730 65B1162930 PANEL BOEING 747 74747UF 1384812 NM ZONE 600 DEPARTED A UIEA O OTHER D E INFLIGHT SEPARATION VIBRATION/BUFFET AP APPROACH 1 EA 15 497MC 29258 ON SHORT FINAL APPROACH, THE AIRCRAFT WAS ADVISED BY DXB ATC THAT THERE WAS A HOLE IN THE LEFT WING. DXB SAFETY RECOVER ED AND BOUGHT PANEL THAT LIBERATED ITSELF FROM THE AIRCRAFT TO THE DXB MAINTENANCE OFFICE. REPLACED PANEL AND PERFORMED RIB REPAIR PER SB 747-57-2269R1. 2 L 7 4 4F RT A20WE 20081205 EA 2008 12 5 SWIA200820521 1 20080914 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 964SW 7868 DURING C-CHECK, LEFT ENGINE AFT THRUST MOUNT CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081205 SO 2008 12 5 CHQA200800229 1 20081120 A 2430 30086011 GENERATOR EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL NR 2 FAILED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 271SK 14064 2 145305 CAE311922 FLIGHT 7875, CMH TO IAD - AFTER TAKEOFF, THE FLIGHT CREW RECEIVED A GENERATOR NR 2 BEARING FAIL MESSAGE ON EICAS. THE F LIGHT RETURNED TO CMH AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE GENERATOR NR 2 HARNESS W402 BUT THE MESSAGE WOULD INTERMITTENTLY APPEAR DURING OPS CHECKS. THE NR 2 GENERATOR WAS THEN REPLACED AND THE SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081205 NM 2008 12 5 CALA2008120101103 1 20081127 A 3350 76005 FUSE BOEING 737 737824 13844BZ NM POWER SUPPLY BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 77258 30802 AFT RIGHT OVERWING EMERGENCY EXIT SLIDE LIGHT INOPERATIVE WHEN TESTED. REPLACED LAMP, NO HELP. REPLACED FUSE AT POWER SUPPLY M1671 AND LAMP (767 BULB) SHORTED BULB, REPLACED FUSE P/N 76005 AGAIN PER W/D 33-51-14 PG 1, SH 2. OPERATION CHE CKS GOOD. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008120101111 1 20081201 A 5320 141A541012 INTERCOSTAL BOEING 737 737924 13848A1 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 38403 30120 CABIN FLOOR INTERCOSTAL CRACKED BETWEEN STATION 312 AND 328 RBL 20. REMOVED AND REPLACED INTERCOSTAL AT STATION 312-328 RBL 20 PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008112401089 1 20081121 A 5315 141T5107 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 67158 30437 CABIN - BS 303 LBL 26-44 FLOOR SUPPORT FOUND CORRODED. CABIN - BS 303 LBL 7 TO LBL 62 FLOOR SUPPORT BEAM UPPER FLANGE R EPAIRED PER SRM 33-00-51 REPAIR 1, FIG 201. HFEC NO CRACK FOUND. 2 L 7 2 4F RT A1NM 20081205 NM 2008 12 5 CALA2008112401090 1 20081121 A 5347 151W1294 SEAT TRACK BOEING 777 777224 1385225 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 78004 27580 CABIN STA 414 TO 420 RBL 70 SEAT TRACK CORROSION FOUND. STA 414 TO 476 RBL 70" SEAT TRACK REPLACED PER SRM 51-10-02. 2 L 7 2 4F RT T00001SE 20081205 NM 2008 12 5 CALA2008112401093 1 20081122 A 5313 BAC1498203 STRINGER BOEING 757 757224 1384958 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17128 27567 STR 21R GOUGED AT FUSELAGE STATION 1580. REPAIRED STR 21R AT FUSELAGE STATION 1580 PER SRM 53-00-03 REPAIR 1. 2 L 7 2 4F RT A2NM 20081205 WP 2008 12 5 FDEA200812035067 1 20081203 A 5720 ARB1066 ANGLE DOUG DC10 DC1030F 3023504 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 317FE 46835 LT WING LEADING EDGE FOUND NR 1 CRACK ON TEE ANGLE. 2 L 7 3 4F RT A22WE 20081205 WP 2008 12 5 FDEA200812035068 1 20081203 A 5320 ADA33537 STANCHION DOUG DC10 DC1030F 3023504 WP ZONE 100 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 317FE 46835 FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. 2 L 7 3 4F RT A22WE 20081205 WP 2008 12 5 FDEA200812035070 1 20081203 A 5320 ADA335328 STANCHION DOUG DC10 DC1030F 3023504 WP ZONE 100 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 317FE 46835 FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. 2 L 7 3 4F RT A22WE 20081203 EA 2008 12 3 VNAA2008111700002 1 20081109 A 2742 BOLT CNDAIR CL600 CL6002C10 1390015 EA HORIZ STAB LOOSE A VNAA K NONE O OTHER IN INSP/MAINT 1 GL 05 705PS 10144 DURING ROUTINE MAINTENANCE ON THE HORIZONTAL STABILIZER TRIM ACTUATOR (HSTA), LOOSE BOLTS WERE FOUND IN THE UPPER BOLT L OCATIONS OF THE UPPER HSTA FITTING ASSEMBLIES (LT AND RT). THE BOLTS WERE RETORQUED TO THE PROPER SPECIFICATION. CHECK S WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 MASA2008111500776 1 20081115 A 3350 1317 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 917FJ 15017 ASH FLT 2633 STL-CLT. EMERGENCY FLOOD LIGHT ROW 7 INOPERATIVE. MX RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 MASA2008112000783 1 20081120 A 2421 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 1 ENGINE MALFUNCTIONED A MASA E B ENGINE SHUTDOWN EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 27314 7314 ASH FLT 7163 PIT-CLE. EMERGENCY DECLARED DUE TO NR 1 ENGINE OIL PRESSURE WARNING AND ENGINE SHUTDOWN IN FLIGHT. MX REP LACED IDG, EDP AND ATS GARLOCK SEALS, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 MASA2008111700780 1 20081117 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAP MALFUNCTIONED A MASA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 SW 07 651ML 10204 7139 ASH FLT 7044 PWM. CREW DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY DUE TO A FLAPS FAIL CAUTION MESSAGE AT ZERO DEGREE S. MX REMOVED AND REPLACED PDU, FLAP LEVER AND RIGGED BPSU'S OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 MASA2008112900791 1 20081129 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH 2328 PHX. CREW REPORTED A CEILING EMERGENCY FLOODLIGHT INOPERATIVE. MX RELAMPED. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 ASAA0853922 1 20081130 A 3040 8300005604 CONTROLLER BOEING 737 737890 1384527 NM WINDOW HEAT INTERMITTENT A ASAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 02 583AS 5517 35681 WHILE EN ROUTE RIGHT SIDE WINDOW HEAT OVERHEAT LIGHT CAME ON CYCLED IT OFF PER THE CHECKLIST (AND BACK ON) BUT OVERHEAT WOULD NOT EXTINGUISH. SWITCH REMAINS OFF PER THE CHECKLIST. OPS CHECK BITE CHECK INTERMITTENT SENSOR FAULT OPS CK IAW FIM 30 41 00 810 801 30 41 00 760 801. VERIFICATION NO FURTHER FAULTS NOTED. OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0853923 1 20081130 A 3040 8300005604 CONTROLLER BOEING 737 737890 1384527 NM WINDOW HEAT FAULTED A ASAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 02 583AS 5524 35681 WHILE EN ROUTE RIGHT SIDE WINDOW OVERHEAT LIGHT CAME ON FOLLOWED QRH PROCEDURE AND OVERHEAT LIGHT CAME BACK ON BITE CHEC KED WHCU CURRENT BIT PASSED. RT SIDE WHCU LOGGED SENSOR FAULT FOR PAST 7 LEGS. MEASURED RESISTANCE OF SENSOR REF MM 30 41 21 760 801 PRIMARY 320 OHM SPARE 317 OHM WITH IN LIMITS. ALSO MEASURED WINDOW HEAT FILM REF MM 30 41 21 CHECKED NOR MAL. WINDOW HARNESS CHECKED NO FAULT NOTED. DUE TO HISTORY REMOVED AND REPLACED RT SIDE WHCU REF MM 30 41 11. OPS NOR MAL, PART VERIFIED WITH SEAMC ROB. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0873924 1 20081126 A 5321 453A261013 FLOORBOARD BOEING 737 737790 13844CN NM BS 727D-767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON AFT CARGO BAY FLOORBOARD. REMOVED AND REPLACED AFT CARGO BAY FLOORBOARD PER SRM 53 00 53. 2 L 7 2 4F RT A16WE 20081205 EA 2008 12 5 ASOA200801491 1 20081112 A 5347 SEAT TRACK CNDAIR CL600 CL600* 1900302 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 INSTALLED NEW SERVICEABLE SIDEWALL SEAT TRACK AT SEAT AREA 10CD IAW AMM TASK 53-01-11-400-802. REF JOB 8719625 OP 81 FO R INITIAL REMOVAL. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 USAA2008120392177 1 20081202 A 5753 SKIN BOEING 737 73733A 1384673 NM RT WING TE FLAP DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 19730 5510 1810 23634 PHX - DAILY - MAJOR REPAIR - RIGHT OUTBOARD AFT FLAP DISBOUNDED. REPLACED RIGHT OUTBOARD AFT FLAP IAW US AIRWAYS TASK C ARD R3M27034. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 USAA2008120392179 1 20081123 A 5315 D53472189204 FLOORBEAM AIRBUS A319 A319132 3930340 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 808AW 1088 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT FR 68, -Y1292. REPLACED FLOORBEAM AT FR 68, -Y1292 IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081205 NM 2008 12 5 ZZDA2008174 1 20081119 A 5320 PAN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 967AT 55028 AFT CARGO DOOR PAN CORRODED BEYOND LIMITS. CUT OUT CORRODED SECTION & REPLACED WITH SPLICE REPAIR PER B717 SRM 53-20-15 REPAIR 7. 2 L 7 2 4F TR A6WE 20081205 EU 2008 12 5 MALA080207 1 20081118 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE GOUGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 340B433 NUMEROUS DENTS AND GOUGES NOTED IN LT AND RT OUTER FUSELAGE SKIN. REPAIRED IAW EO NR S53640, S53005. 2 L 7 2 4T RT A52EU 20081205 NM 2008 12 5 USAA2008120292166 1 20081125 A 5312 BULKHEAD BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - CRACK ON VERTICAL BEAM WEB AT BS 178 BULKHEAD, RBL 17, WL 232. REPAIRED VERTICAL BEAM WEB AT BS 178 BULKHEAD, RBL 17, WL 232 IAW SRM 53-10-08 REPAIR 12. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0843920 1 20081120 A 5330 65C329541 SKIN BOEING 737 7374Q8 138447Q NM BS 832-844 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 FUSELAGE SKIN DENTED BELOW AFT CARGO DOOR. REMOVED DAMAGED SECTION. INSTALLED REPAIR DOUBLER AND TRIPLER PER SRM 53-00 -01. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0873906 1 20081119 A 5320 141A8550533 CHANNEL BOEING 737 737790 13844CN NM BS 360 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 E/E BAY DOOR CUTOUT AFT FRAME BS 360 BL 0 HAS MECHANICAL DAMAGE ON FITTING SUPPORT. R&R LOCK SUPPORT FITTING. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 USAA2008120292168 1 20081123 A 5310 D53471123202 SUPPORT FRAME AIRBUS A319 A319132 3930340 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 808AW 1088 SAL - C7 - CORROSION ON WEB SUPPORT FRAME AT FR 64 TO FR 70, S23R TO S24R. REPAIRED WEB SUPPORT FRAME AT FR 64 TO FR 70 , S23R TO S24R IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081205 WP 2008 12 5 UPS08853977 1 20081107 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV FLUSH SKIN REPAIR DOES NOT MEET SRM. REPAIRED BY DRW 3804041. 2 L 7 4 4F RT 4A25 20081205 2008 12 5 HALA2008112500875 4 20081125 A 3444 066500070101 TRANSCEIVER BOEING 767 76733A 1385209 NM RADAR ALTIMETER FAILED A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 581HA 28141 CAPT RADAR ALTIMETER FAIL FLAG ILLUMINATED SEVERAL TIMES DURING GLT. REMOVED AND REPLACED NR 1 RADIO ALTIMETER T/R UNIT GROUND CHECK OK PER AMM34-33-01. TEST 30 PASSED ACFT REMAINS IN LAND 3 STATUS. 2 L 7 2 4F RT A1NM 20081205 EA 2008 12 5 SWIA200820510 1 20081126 A 3233 17008115 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA RT MLG SLUGGISH A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 403SW 1848 1848 7028 FLT 2871 - RIGHT MAIN GEAR RETRACTION TIME LONGER THAN NORMAL. REPLACED RIGHT MAIN GEAR ACTUATOR, P/N: 17008-115, S/N O N, 01021 S/N OFF: 01753. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 ZZDA2008177 1 20081125 A 5220 CABLE BOEING 717 717200 1383700 NM TAILCONE MISROUTED A ZZDA K NONE W J INADEQUATE Q C WARNING INDICATION IN INSP/MAINT 1 SO 37 991AT 55135 TAIL CONE UNLOCK LIGHT ILLUMINATED. FOUND EXTERNAL HANDLE FOR TAIL CONE RELEASE, CABLE MIS-ROUTED IN BLOCK. REINSTALLE D CABLE PER B717 AMM 53-52-01. TAIL CONE WARNING LIGHT OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F TR A6WE 20081205 EA 2008 12 5 SWIA200820512 1 20081128 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 869AS 7479 FLT 4489 - EMERGENCY LIGHT NR 2 INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820513 1 20081126 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 417SW 7400 FLT 5835 - ENTRANCE FLOOR EMERGENCY LAMP ONE LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081205 SO 2008 12 5 SWIA200820515 1 20081123 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO CABIN/COCKPIT SMOKE A SWIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 585SW 120353 FLT 5702 - STRONG ODOR OF SMOKE IN COCKPIT AND CABIN. RAN ENGINES AND APU, OPERATING BOTH PACKS, NO DISCREPANCIES NOTED . 2 L 7 2 4T RT A31SO 20081205 EA 2008 12 5 SWIA200820524 1 20080916 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 465SW 7845 DURING C-CHECK, FS 280 FLOORBEAM CLIP AT LBL 9 CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 ZZDA2008176 1 20081107 A 5210 STRUCTURE BOEING 737 73776N 13844CH NM AIRSTAIR DOOR DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 175AT 32652 AIRSTAIR DOOR HAS HOLE IN THE UPPER RIGHT CORNER. REF: 08-0678 (C/W REPAIR 1 REF; SRM 52-00-01 ON AIRSTAIRS). C/W N/R 00003 MDDR 142112T ACCOMPLISHED PERMANENT REPAIR AS PER EA 37-52-01129A SECTION 3 AND SRM 52-00-01. AAR W/O 28461 N/R 3 292. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 USAA2008120292169 1 20081123 A 5320 D53112827201 DUMMY RAIL AIRBUS A319 A319132 3930340 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 808AW 1088 SAL - C7 - CORROSION ON DUMMY RAIL AT FR16, Y503. REPAIRED DUMMY RAIL AT FR16, Y503 IAW A319 SRM 51-74-00 AND 53-11-14. 2 L 7 2 4F RT A28NM 20081205 NM 2008 12 5 UPS08M53978 1 20081024 A 5330 ACA3108501 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C DENT ON RT EXTERIOR FUSELAGE SKIN STA 512 2 INCHES ABOVE S28R. CUT OUT DENT, FABRICATED AND INSTALLE D REPAIR DOUBLERS IAW MD-11 SRM 53-20-00 FIG 2. 2 L 7 3 4F RT A22WE 20081205 NM 2008 12 5 USAA2008120292170 1 20081201 A 5320 6545834U69 STIFFENER BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - FLOORBEAM STIFFENER CRACKED AT BS 312, LBL 10. REPLACED FLOORBEAM STIFFENER AT BS 312, LBL 1 0 IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 USAA2008120292171 1 20081201 A 5320 65C80735353 INTERCOSTAL BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - INTERCOSTAL CRACKED AT BS 360, BL 0. REPLACED INTERCOSTAL AT BS 360, BL 0 IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 UPS08M53979 1 20081025 A 5522 NLC67412 SKIN DOUG MD11 MD11F 3023600 NM RT ELEVATOR ERODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C AREA AT BOTTOM OF RT ELEVATOR AT O/B DAMPER HAS EROSION THRU COMPOSITE. REMOVED EXTERIOR COATING, DA MAGED COMPOSITE AND REPAIRED RT O/B ELEVATOR L/E IAW UPS EO MD11-5520-31233-A, SAA EA 011-5512-01 -A1559, MD-11 SRM 55-9 0-00 AND MD-11 SRM 51-62-01. 2 L 7 3 4F RT A22WE 20081205 NM 2008 12 5 USAA2008120292173 1 20081201 A 5315 6545834U70 FLOORBEAM BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - FLOORBEAM STABILIZER CRACKED AT BS 328, BL 0. REPLACED FLOORBEAM STABILIZER CRACKED AT BS 3 28, BL 0 IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 UPS08M53980 1 20081025 A 5753 ARC43602 SKIN PANEL DOUG MD11 MD11F 3023600 NM TE FLAP DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C RT WING O/B FLAP LOWER SURFACE 18.5 INCHES O/B OF PANEL 657FB 36 INCHES FROM T/E FOUND DENT. REMOVED DAMAGE AND BONDED REPAIR PLIES IAW UPS EO MD11-5750-31247 -A AND SAA EA 011-5750-01-A1563. 2 L 7 3 4F RT A22WE 20081205 NM 2008 12 5 ASAA0843943 1 20081201 A 5753 65C348126 FLAP TRACK BOEING 737 737490 1384715 NM NR 7 FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 ALL BEARING SURFACES OF NR 7 FLAP TRACK CORRODED. REMOVED CORROSION FLAP PEENED AND APPLIED TEMPORARY COATING PER OHM 5 7-53-15 EA 400-57EA-00291 AND EA 5750-01485. 2 L 7 2 4F RT A16WE 20081205 EA 2008 12 5 COMA2008120150015 1 20081126 A 5320 6013501252 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FS 621.00 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 971CA 30007 7145 RT INTERCOSTAL CLIP AT FS 621.00 IS CRACKED. INSTALLED NEW ANGLE BRACKET IAW SRM 51-42-20. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 COMA2008120150016 1 20081129 A 5210 601R317725 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 971CA 30007 7145 PAX DOOR CRACKED ON REAR STEP RISER ANGLE. REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 COMA2008120150017 1 20081130 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA ZONE 600 DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 442CA 19194 7483 RIGHT WING LOWER PLANK BOOST PUMP NR 8 SCREW HOLE IS DAMAGED. REMOVED DAMAGE AND INSTALLED A SERVICEABLE FREEZE PLUG BU SHING IAW REO 601R-57-21-169 REV (D). 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 ASAA0843959 1 20081201 A 5210 652999413 GUIDE ARM BOEING 737 7374Q8 138447Q NM L1 DOOR STIFF A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 L1 DOOR HARD TO CLOSE FROM INSIDE FOUND WHILE REPOSITIONING JETWAY AFTER ARRIVAL. ADJUSTED L1 DOOR GUIDE ARM REF M/M 52 -11-00-705-007-B00. OPERATED NORMALLY OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0873944 1 20081203 A 5320 147A56602 INTERCOSTAL BOEING 737 737790 13844CN NM BS 947.5-967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 BS 951 RBL 52 FLOOR SUPPORT INTERCOSTAL IS CORRODED. R&R FLOOR SUPPORT INTERCOSTAL. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0873945 1 20081123 A 5320 143A7501 SUPPORT CHANNEL BOEING 737 737790 13844CN NM BS 500A CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 500-500D, CORROSION CLEANUP AT BS 500A + 10 OUT OF LIMITS. REPAIR DOUBLER INS TALLATION ACCOMPLISHED PER SRM 53-00-53 REP 6. 2 L 7 2 4F RT A16WE 20081205 2008 12 5 ASAA0853889 2 20081126 A 7261 FILTER BOEING 737 737890 1384527 NM NR 2 SCAV PUMP FOD A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 559AS 31177 35178 WHILE ACCOMPLISHING TSR 904551 FOUND PACKING DEBRIS IN THE NR 2 ENGINE SCAVENGE OIL FILTER. VERIFIED LUBE UNIT S/N NR Y T006763 4 GS 96274 11/26/2008 SEAMC ROB NOTIFIED. REMOVED AND REPLACED NR 2 ENGINE LUBRICATION UNIT PER MM 79 21 01. P ERFORMED IDLE LEAK CHECK. NO LEAKS NOTED. OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0893948 1 20081112 A 5720 115A29532 BRACKET BOEING 737 737990 NM RT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 RT WING T/E PANEL SUPPORT BRACKET CRACKED. REMOVED AND REPLACED BRACKET. 2 L 7 4 4F RT A16WE 20081205 NM 2008 12 5 ASAA0843953 1 20081118 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 9 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 RT WING NR 9 SPOILER UPPER SURFACE CLUSTER OF 5 DENTS 5 INCHES FROM END AND 15 INCHES FROM INBD END. DEEPEST DENT MEASU RES A=.200 Y=.008 A/Y=25. REPAIRED NR 9 SPOILER UPPER SURFACE DENTS IAW SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0893947 1 20081115 A 7830 BRACKET BOEING 737 737990 NM THRUST REVERSER CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 302AS 30017 NR 2 ENG OUTBOARD TR HEAT SHIELD BRACKET BROKEN. REMOVED AND REPLACED BRACKET. 2 L 7 4 4F RT A16WE 20081205 NM 2008 12 5 UPS08M53949 1 20081118 A 5343 AEA7051502 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM CLG TRUNNION GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 281UP 48538 INSPECTION TYPE:SPV DURING SPECIAL VISIT FOR GEAR CHANGE AT SAA, CORROSION WAS FOUND ON THE CLG TRUNNION SUPPORT FITTING , RT SIDE. WHILE PERFORMING MACHINING TO SUPPORT FITTING FAYING SURFACE, PER SRM 53-40-00 FIG 16, THE SET SCREWS FOR TH E CUTTER TOOL CAME LOOSE AND THE RADIUS WAS DAMAGED. BLENDED AREA REPAIRED PER EO MD11-5310-31226 AND PERFORMED ON EA S AA-011-5310-01-A1558. REPEAT INSPECTIONS EVERY CLG REMOVAL, NOT TO EXCEED 7,500 CYCLES. METHOD- HFEC. 2 L 7 3 4F RT A22WE 20081205 EA 2008 12 5 MASA2008120200734 1 20081202 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN MALFUNCTIONED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 903FJ 15003 ASH 2766 PHX-SAT. CEILING EMERGENCY LIGHT AFT FACE INOPERATIVE. MX OPS CHECKED EMERGENCY LIGHT AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 MASA2008112100784 1 20081121 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA AC BAY DIRTY A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 651ML 7139 ASH FLT 7141 GSP-IAD. CREW REPORTED SMOKE IN CABIN DUE TO RT PACK OVERTEMP. MX REMOVED AND REPLACED COALESCER BAG. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 ASAA0843938 1 20081118 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 3 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 NR 3 SPOILER HAS A SHARP DENT ON UPPER SURFACE 5 INCHES FROM T/E AND 6 INCHES FROM OUTBOARD END. PREPPED DAMAGED AREA, FABRICATED DOUBLER AND BONDED REPAIR IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0843941 1 20081201 A 5753 65C348122 FLAP TRACK BOEING 737 737490 1384715 NM NR 1 FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 ALL BEARING SURFACES OF NR 1 FLAP TRACK CORRODED. REMOVED CORROSION FLAP PEENED AND APPLIED TEMPORARY COATING PER OHM 5 7-53-15 EA 400-57EA-00291 AND EA 5750-01485 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0843942 1 20081201 A 5753 65C348126 FLAP TRACK BOEING 737 737490 1384715 NM NR 2 FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 ALL BEARING SURFACES OF NR 2 FLAP TRACK CORRODED. REMOVED CORROSION FLAP PEENED AND APPLIED TEMPORARY COATING PER OHM 5 7-53-15-EA-400-57EA-00291 AND EA 5750-01485. 2 L 7 2 4F RT A16WE 20081205 EA 2008 12 5 SWIA200820518 1 20080914 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 964SW 7868 DURING C-CHECK, FS 280 LOWER FLOOR SUPPORT CRACKED AT LBL 11. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 VNAA2008111700008 1 20081121 A 2421 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 LOW A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 228PS 7897 CREW REPORTED ON TAKEOFF ROLL FROM CLT, IDG 2 CAUTION MSG CAME ON, ABORTED TAKEOFF. AIRCRAFT RETURNED TO GATE WITHOUT I NCIDENT. A RESET OF GEN 2 WAS ACCOMPLISHED & ALL MSG'S WERE CLEARED. MAINTENANCE SERVICED THE NR 2 IDG. NO DEFECTS NO TED AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 COMA2008112450008 1 20081121 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B16 1900305 EA TE FLAPS FAILED A COMA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 SO 27 815CA 7397 FLAPS FAILED AT 20 DEG WHEN SELECTED TO 30 DEG. ACFT LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL C AUTION MESSAGE FOLLOW UP MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 20081205 EU 2008 12 5 NWAA085133318 1 20081114 A 2140 HEATER AIRBUS 330 A330323 3940030 EU CABIN MALFUNCTIONED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 818NW 0857 FLIGHT ATTENDANTS REPORTED BURNING SMELL IN LDMCR, INCREASED IN STRENGTH OVER TIME AND WAS CONFIRMED BY PURSER AND CAPTA IN. 5 FLIGHT ATTENDANTS EXPERIENCED SYMPTOMS OF HEADACHES, BURNING NOSE, EYES AND TIGHTNESS OF CHEST WITH 1 FLIGHT ATTE NDANT BEING ADMINISTERED OXYGEN BY A PHYSICIAN. LANDING WAS UNEVENTFUL. THE LDMCR HEATER AND RECIRCULATION FILTER WERE REPLACED AND SEALANT BELOW THE STAIRWAY THAT WAS FOUND NOT CURED WAS REMOVED. 2 L 7 2 4F RT A46NM 20081205 EA 2008 12 5 REX2008F00056 1 20081024 A 2750 860D10018ABCD ECU CNDAIR CL600 CL6002B19 1900309 EA TE FLAP FAILED A REXA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 25 8907A 7907 FLAPS FAILED AT ZERO WHEN SELECTED TO 8 DEGREES. QRH FOLLOWED. EMERGENCY DECLARED FOLLOWED BY AN UNEVENTFUL LANDING. FLAP SYSTEM TROUBLESHOOTING PERFORMED PER BOMBARDIER FIM AND AMM PULLED CODES FROM FLAP ELECTRON CONTROL UNIT FECU. PER FIM CODES SHOWED FAILED FECU. FECU REPLACED PER BOMBARDIER AMM SYSTEM. OPS TESTED GOOD. 2 L 7 2 4F RT A21EA 20081205 WP 2008 12 5 NWAA085129926 1 20081115 A 3320 BALLAST DOUG DC9 DC932 3022066 WP AFT LAVATORY BURNED A NWAA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 GL 01 826NW 47425 NOTE THAT NO REPORT WAS RECEIVED OF VISIBLE SMOKE BEING OBSERVED BY A CREW MEMBER OR PASSENGER. THE AFT LT LAVATORY SMO KE ALARM ACTIVATED DURING APPROACH FOR LANDING AT MSP. THE INTERPHONE COMMUNICATIONS WAS LOST TO THE AFT CABIN. THE PI LOT DECLARED AN EMERGENCY AND CFR MET THE ACFT AFTER TOUCHDOWN, VERIFIED THAT NO FIRE, SMOKE, SMELL OR HEAT PER INFRARED SCAN AND ESCORTED THE ACFT TO THE GATE. MX FOUND THE LIGHT BALLAST FOR THE AFT LT LAVATORY WAS CHARRED AND SHOWED EVID ENCE OF INTERNAL DAMAGE. THEY WERE NOT ABLE TO DETERMINE CAUSE FOR LOST OF CABIN INTERPHONE, FAILURE OF AFT SECTION OF CABIN LIGHTING, OR THE INTERMITTENT TAIL CONE LIGHTS. LAV LIGHT BALLAST WAS REPLACED, COALESCER SOCKS REPLACED AND THOS 2 L 7 2 4F A6WE 20081205 NM 2008 12 5 NWAA085096305 1 20081015 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 665US 23820 UPPER DECK OVERHEAD EMERGENCY EXIT SIGN INOP. MX R&R POWER SUPPLY AND BATTERY PACK. OPS CHECKED GOOD AND ACFT WAS RETU RNED TO SERVICE. 2 L 7 4 4F RT A20WE 20081205 NM 2008 12 5 UALA2008112406634 1 20081123 A 3397 794640 CONNECTOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 671UA 30026 SEAT 5H EEL LIGHT IS INOP. SECURED SEAT CONNECTOR. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081205 NM 2008 12 5 UALA2008112406635 1 20081123 A 3350 582233 BATTERY BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 671UA 30026 SEATS 20A THRU 22A EEL IS INOP. REPLACED BATTERY, CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081205 NM 2008 12 5 UALA2008112406643 1 20081124 A 3350 20131A BATTERY BOEING 767 767222 1385122 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 595UA 28748 EEL LIGHTS INOP AT FWD COACH CABIN ALONG WITH 1 EA STOW BIN LIGHT AND HATCH LIGHTS. REPLACED BATTERY FOR POWER SUPPLY M 10567. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E17NE 20081205 NM 2008 12 5 WRLA2008093 1 20081124 A 5330 SKIN DOUG MD11 MD11F 3023600 NM BS 595-615 DAMAGED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHK + 4C, EGAT MECH FOUND FUSELAGE SKIN HAD WRINKLE FROM STA 595-615 AND STR 43R-47R. REPAIR FUSELAGE SKI N STA 595 TO STA 615 PER MD-11 SRM 53-20-00 FIG 11 REV 46. 2 L 7 3 4F RT A22WE 20081205 NM 2008 12 5 WRLA2008095 1 20081124 A 5712 RIB DOUG MD11 MD11F 3023600 NM LT WING CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHK + C4 CHK, EGAT MECH FOUND LT WING FIXED LE INTERNAL SUPPORT RIB CRACK AT STA XORS=484. REPAIRED AREA IAW ENGINEERING INSTRUCTION W2008A57B-1288 REV 00 AND EI W2008A57B-1288 REV 01. 2 L 7 3 4F RT A22WE 20081205 NM 2008 12 5 FDEA200812015027 1 20081201 A 5322 6516314111 SHEAR TIE BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 CE 21 495FE 21669 NLG W/W SHEAR TIE AT STA 312 BETWEEN STR 24R - 25R IS CRACKED AT BOTTOM HOLE. REMOVED FASTENERS A ND CUT OUT SHEAR TIE IAW B727 SRM 51-30-2 AND 53-10-4 FIG 15. REPAIRED NLG W/W SHEAR TIE AT BS 312 BETWEEN STR 24R AND STR 25R IAW B727 SRM 53-10-4 FIG 15. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2. INSTALLED SHEAR TIE, REPAIR IAW B727 SRM 51-30-2 AND 53 -10-4 FIG 15. 2 L 7 3 4F A3WE 20081205 EA 2008 12 5 ASOA200801572 1 20081126 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 859AS 7421 MAIN PASSENGER DOOR IS DIFFICULT TO CLOSE THE MOTOR IS HAVING TROUBLE CLOSING THE DOOR. 2 L 7 2 4F RT A21EA 20081205 NE 2008 12 5 C8GA20080032 2 20081120 A 7200 PW2037 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 DAMAGED A C8GA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 29 620DL 63061 17298 22910 716435 FLT 201 FROM MIA TO CCS - AFTER TAKEOFF WITH FLAPS RAISED APPROX 1800 FEET AND CLIMB THRUST SELECTED, 3 QUICK COMPRESSOR STALLS WERE HEARD AND FELT FROM THE NR 1 ENGINE. APPROPRIATE CHECKLIST WAS PERFORMED, EMERGENCY WAS DECLARED AND THE A IRCRAFT RETURNED TO MIA WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT BOROSCOPE INSPECTION REVEALED DAMAGE TO THE HIGH PRESSURE COMPRESSOR WHICH WAS DEEMED UNSERVICEABLE. THE NR 1 ENGINE WAS REMOVED AND REPLACE. OPERATIONAL AND LEAK CHEC KS GOOD. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081205 EA 2008 12 5 ASOA200801573 1 20081126 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 844AS 7317 CABIN FORWARD MOST CEILING EMERGENCY LIGHT INOP, CABIN EMERGENCY LIGHTS - CEILING LEVEL EMERGENCY FLOOD LIGHTS. REMOVED AND REPLACED CHARGER. CHECK GOOD. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 MASA2008111600778 1 20081116 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A MASA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 651ML 7139 ASH FLT 7212 BTV-IAD. CREW DECLARED AN EMERGENCY FOR FLAPS FAIL AT ZERO DEGREES. LANDING WAS UNEVENTFUL. MX COMPLIED WITH THE FLAPS FAIL PART A PROCEDURE AND SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 MASA2008111500775 1 20081115 A 3260 BRACKET CNDAIR CL600 CL6002B19 1900309 EA NLG DEFECTIVE A MASA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SW 07 27173 7173 ASH FLT 7044 IAD-PWM. CREW DECLARED AN EMERGENCY DUE TO NLG WARNING AND DISAGREE MESSAGES. MX REMOVED AND REPLACED NLG CENTERED/EXTENDED PROXIMITY SENSOR BRACKET. 2 L 7 2 4F RT A21EA 20081203 WP 2008 12 3 UPS08853917 1 20081002 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATION AND DISPOITION OF REPAIR EFN 70219961004 ORIGINAL NON ROUTINE 445615 FLOOR WEB REPAIR CRAC KED LEFT CORNER. REPAIRED 53-02-00 FIG 25. 2 L 7 4 4F RT 4A25 20081203 WP 2008 12 3 AALA200810224 1 20081106 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 AFT CARGO, CRACK IN INTERCOSTAL AT STATION 1271 TO 1287. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-00. 2 L 7 2 4F A6WE 20081203 NM 2008 12 3 AALA200820049 1 20081030 A 5320 146N8731 INTERCOSTAL BOEING 757 757223 1384957 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 694AN 47963 26974 INTERCOSTAL CRACKER; REPAIRED INTERCOSTAL IAW SRM 53-60-51-2R1. 2 L 7 2 4F RT A2NM 20081203 WP 2008 12 3 AALA200810204 1 20081103 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 BROKEN TANG ON SEAT TRACK NUMBER 3 AT STATION 1060. REPAIRED WITH SEAT TRACK PLUG PER AARD 53-20-00-10. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200810205 1 20081031 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 RIGHT CUSP MEMBRANE CORRODED AT STATION 1197 - 1200. INSTALLED CUSP DOUBLER STATION 1197-1200 PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081203 NM 2008 12 3 AALA200820050 1 20081106 A 5312 144N8006365 PRESSURE PANEL BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 604AA 43723 27055 PRESSURE DECK CORRODED 11 INCHES TO 21 INCHES OUTBOARD OF CENTER LINE. REPAIRED PRESSURE DECK IAW EA B757-53-004896. 2 L 7 2 4F RT A2NM 20081203 EA 2008 12 3 SWIA200820496 1 20080913 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 471CA 7655 DURING C-CHECK, RIGHT ENGINE AFT THRUST FITTING CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820501 1 20080923 A 5312 BULKHEAD CNDAIR CL600 CL6002D24 1390016 EA FUSELAGE CORRODED A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 802SK 15061 DURING C-CHECK, FS 280 RIGHT BULKHEAD WEB CORRODED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081203 EA 2008 12 3 SWIA200820504 1 20081125 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 917SW 7641 FLT 6387 - SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081203 SO 2008 12 3 C2XA08SH155 1 20081203 A 5512 14552201401 SKIN EMB 145 EMB145XR 3260214 SO HORIZ STAB CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24103 145645 LT HORIZONTAL STAB L/E HAS CORROSION AROUND RIVETS. LT HORIZONTAL STAB L/E WAS REPAIRED IAW EC 5510-01195. THE AIRCRAF T WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081203 SO 2008 12 3 C2XA08IA244 1 20081126 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14972 6501 2927 145151 IAH - FLIGHT 2998, THE CREW REPORTED EMERGENCY LIGHTS INOP ON THE BACK LEFT SIDE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081203 SO 2008 12 3 C2XA08IA243 1 20081120 A 2131 22250N030301 CONTROLLER EMB 145 EMB145EP 3260221 SO CABIN PRESSURE MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION DE DESCENT 1 SW 27 14937 16356 16356 145026 OKC - FLIGHT 2176, THE CREW REPORTED THAT PRESSURIZATION FAILED ON DESCENT INTO OKC. THE AIRCRAFT LANDED IN OKC WITHOUT INCIDENT WHERE MAINTENANCE PLACED PRESSURIZATION ON MEL 21-30-00/3 CAT C, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. THE AIRCRAFT TON'D AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE DIGITAL CONTROLLER, OPERATIONALLY TESTED W ITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20081203 GL 2008 12 3 C2XA08CL122 2 20081120 A 7321 23078830 FADEC EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL NR 1 ENGINE FAULTY A C2XA K NONE O OTHER CL CLIMB 1 SW 27 14993 23417 145289 CLE FLIGHT 2733 - THE CREW REPORTED, LOST NR 1 ENGINE INDICATION SEVERAL TIMES. THE CREW PERFORMED PROCEDURES FROM THE CFM. MAINTENANCE INSPECTED AND REPLACED THE 1B FADEC. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081203 SO 2008 12 3 C2XA08RI170 1 20081107 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO LAVATORY DEFECTIVE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 14204 5932 14500968 FLIGHT 2943 - EWR - FLIGHT CREW REPORTED LAV SMOKE IND ON EICAS. CREW PERFORMED AIR RETURN AND LANDED AIRCRAFT UNEVENTF ULLY. EWR MX REMOVED AND REPLACED LAV SMOKE DETECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROV ED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081205 NM 2008 12 5 UIEA2008341 1 20081116 A 5330 SKIN BOEING 747 74747UF 1384812 NM GE CF6 CF680 30025 NE ZONE 200 PUNCTURED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492MC 29253 AT DEPARTURE FOUND TAIL PUNCTURED THRU FUSELAGE EXTERNAL SKIN JUST FWD OF STA 2598 AT 6 O'CLOCK POSITION APPROX 11.5 FT BY 16 INCHES. CUTOUT FUSELAGE SKIN DAMAGE AND LOWER CHORD AT STA 2598 AS PER SRM 53-00-01 AND 51-70-12. REPAIR NOT COM PLETED AT THIS TIME. INFORMATION WILL FOLLOW. 2 L 7 4 4F 4 F RT A20WE E13NE 20081205 EA 2008 12 5 MALA080200 1 20081124 A 3350 CHARGER CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS MALFUNCTIONED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 933XJ 15196 CABIN EMERGENCY LIGHTS CYCLING INTERMITTENTLY. REPLACED NR 1 FWD BATTERY CHARGER. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 MALA080201 1 20081122 A 3397 CIRCUIT BREAKER CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS MALFUNCTIONED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 933XJ 15196 EMERGENCY LIGHTS ON STATUS MESSAGE WITH LIGHTS IN THE CABIN CYCLING. CYCLED U3 CIRCUIT BREAKER. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 MALA080202 1 20081122 A 3397 CIRCUIT BREAKER CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS MALFUNCTIONED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 933XJ 15196 EMERGENCY LIGHTS ON STATUS MESSAGE CYCLES ON AND OFF, FA REPORTS LIGHTS NOT ON IN CABIN. CYCLED U3 CIRCUIT BREAKER. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 UALA2008112406633 1 20081123 A 3350 78941 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 671UA 30026 SEAT 3A & 4A EEL LIGHTS ARE MISSING. RELAMPED 3A & 4A. OPS CHECK OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081205 WP 2008 12 5 AALA200810253 1 20081107 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CRACK IN CUSP AT LEFT SIDE BETWEEN STATION 218 AND 237. REPLACED SECTION OF CUSP. 2 L 7 2 4F RT A6WE 20081205 WP 2008 12 5 AALA200810265 1 20081109 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION ON LEFT CUSP. REMOVED AND REPLACED CUSP SHEET FROM STATION 598 TO STATION 712 PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081205 NM 2008 12 5 AALA200820052 1 20081106 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 666A 52891 25300 AFT MAIN DECK PLATE CORRODED, REPAIRED AFT DECK PLATE IAW SRM 53-60-51-2R2. 2 L 7 2 4F RT A2NM 20081205 WP 2008 12 5 AALA200810251 1 20081106 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION ON LOWER SIDE OF LEFT CUSP AT STATION 503 TO 522. REMOVED CORROSION PER SRM 51-10-03 AND INSTALLED DOUBLER PE R AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081205 WP 2008 12 5 AALA200810248 1 20081104 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION ON CUSP AT AFT SERVICE DOOR AFT GIRT BAR ATTACH FITTING. INSTALLED DOUBLER PER AARD 53-20-00-16 2 L 7 2 4F RT A6WE 20081205 WP 2008 12 5 AALA200810275 1 20081111 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 FUSELAGE FRAME UPPER SIDE FORWARD RADIUS HAS THREE EACH HOLES AT STATION 1231 BETWEEN LONGERONS 29 LEFT AND 30. INSTALL ED J ANGLE FILLER. 2 L 7 2 4F RT A6WE 20081205 WP 2008 12 5 AALA200810262 1 20081107 A 5320 PANEL DOUG DC9 DC983 3022083 WP LAV SERVICE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 AFT LAVATORY SERVICE PANEL HAS CORROSION ALONG LOWER EDGE OF SKIN TO FLANGE. REPAIRED AFT LAVATORY SERVICE PANEL PER SR M 51-10-9 AND ESO 80559 DATED 11/05/08. 2 L 7 2 4F RT A6WE 20081205 2008 12 5 ASAA0853886 4 20081125 A 2210 8221567102 CONTROL PANEL BOEING 737 737890 1384527 NM COCKPIT BURNED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 557AS 9547 35176 DIGITAL COURSE WINDOW (CAPT'S) HAS A BURN SPECK IN IT. VERIFIED BURN SPECK ON CAPTS COURSE WINDOW. REPLACEMENT MODE CO NTROL PANEL P/N VERIFIED BY SEAMC ROB. REMOVED AND REPLACED MCP REF AMM 22 11 34/401. ACCOMPLISHED LRU PELACEMENT TEST GRP NR 32 LAND VERIFY GRP NR 49 AND HGS SENSOR TEST FOR FCC/AT. ALL TESTS PASS REF AMM 22 11 00/201 AND 34 36 00/501. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0853887 1 20081127 A 2421 761574B IDG BOEING 737 737890 1384527 NM NR 1 ENGINE MALFUNCTIONED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 577AS 6758 35186 NR 1 ENGINE IDG FILTER DELTA P POPPED IDG HAS HISTORY 3 TIMES REQUIRES REPLACING. VERIFIED PART NR AND AFFECTIVITY WITH SEAMC ROB. REMOVED AND REPLACED NR 1 ENG IDG AS REQUIRED. RAN ENG LEAK CKD GOOD VOLTS AND FREQS GOOD. ALL WORK DONE IAW AMM 24 11 11 000 801 24 11 11 400 801. 2 L 7 2 4F RT A16WE 20081205 EA 2008 12 5 ASOA200801562 1 20081125 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 INDICATION NOTED AT LOWER WING PLANK ACCESS HOLE 640CB WHILE PERFORMING ASA TASK NR 000-57-600-610. INDICATION APPEARS TO BE CORROSION APPROX .040 DEEP, INDICATION IS MAPPED ON AIRCRAFT. REPAIRED LOWER WING PLANK ACCESS HOLE 640CB IAW REO 601R-57-21-1033. ASA EC/TC NEEDS C/W. C/W EC/TC REO 601R-57-21-1033 IAW REO 601R-57-21-1033. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 ASOA200801584 1 20081130 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 27 680BR 7679 FLAPS FAIL MSG ON EICAS AT 200 KAS FLAPS INDICATING 0. EN ROUTE TO CID A/C DIVERTED TO MLI DUE TO MTC, EMERGENCY DECLAR ED. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 ASOA200801585 1 20081130 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 855AS 7395 FWD OVERWING EMERGENCY LIGHT ON RT SIDE IS INOP. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 ASOA200801575 1 20081127 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 909EV 7658 FWD LT OVERWING EMERGENCY LIGHT IS INOP. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 COMA2008112570003 1 20081124 A 5610 601R3303320 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 658CA 12039 10148 EN ROUTE FROM MCI TO CVG RECEIVED RT WINDOW HEAT CAUTION MSG. A/C DIVERTED TO STL, LANDED SAFELY. REMOVED AND REPLACED RT WINDOW. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 COMA2008120150020 1 20081201 A 5330 600330521 SKIN PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 960CA 31308 7117 COMPLIED WITH MODIFICATION K601R36009-3 ON LT FS 640.00 FRAME AND DOUBLER PER S/B601R-53-061 KIT DRWG K601R36009 REV B, 601R-53-61-506 REV C AND 601R53-61-569. REMOVED AND REPLACED SKIN PANEL BETWEEN LT AND RT TRU DOORS IAW CRJ SRM 51-42-0 6. DAMAGED SKIN JUST AFT OF LT TRU DOOR REPAIRED IAW REO 601R-53-1538. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 ASOA200801529 1 20081117 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 713EV 10081 RT 280 FLOORBEAM CORRODED. R/R FLOORBEAM. 2 L 7 2 4F RT A21EA 20081208 NM 2008 12 8 DHLA2008745692 1 20081114 A 5743 SUPPORT BEAM BOEING 727 727224 1384076 NM ZONE 600 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 RIGHT MLG TRUNNION BEAM LOWER FAIRING PANEL ATTACH HOLES CORRODED. ACCOMPLISHED REPAIR TO SUSPECT HOLES IAW EO COO-2-57 -391-08 DATED 10/27/08. REF FAA FORM 8110-3 DATED 11/06/08 AND EVA B257-00059 FOR REPAIR APPROVAL. DOCUMENTED ON N/R 1 -661. 2 L 7 3 4F A3WE 20081208 NM 2008 12 8 SWAA086771 1 20081203 A 5754 65C26602312A SLAT BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT DELAMINATED AT O/B EDGE. REPAIRED SLAT PER MM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 NOCA08208001 1 20081112 A 2550 033638 MOTOR BOEING 767 767306 1385148 NM BLOWER INOPERATIVE A NOCA K NONE N FALSE WARNING NR NOT REPORTED 1 EA 15 760NA 28098 FWD DET FAN MESSAGE DISPLAYED ON EICAS MAINT PAGE. REMOVED AND REPLACED FWD CARGO SMOKE DETECTOR BLOWER NR 1 PER AMM 26 -16-02. OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 20081208 NM 2008 12 8 SWAA086772 1 20081203 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 11. REMOVED AND REPLACED BULB PER MM. 2 L 7 2 4F RT A16WE 20081208 WP 2008 12 8 NWAA085069852 1 20081112 A 5321 STIFFENER DOUG DC9 DC951 3022051 WP FLOOR PANEL CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 761NC 47709 DURING H CHECK FOUND CRACKS IN 2 STIFFENERS FOR FLOOR PANEL NR 28. REPAIRED PER EA 214491. 2 L 7 2 4F RT A6WE 20081208 EA 2008 12 8 ASOA200801521 1 20081116 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 581-613 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 713EV 10081 RT SIDEWALL SEAT RAILS HAVE SCATTERED CORROSION BETWEEN FS 581.00 TO FS 613.00. EXCEED THE ALLOWABLE DAMAGE IAW SRM 5 3-31-49 MA 7026048. REMOVED AND REPLACED SEAT TRACK PER AMM 53-00-49. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 A6WA200840605 1 20081105 A 2740 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INTERMITTENT A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 31 439AW 7753 FIRST OFFICERS STAB TRIM SWITCH INTERMITTENT IN FLIGHT. R&R FIRST OFFICERS STAB TRIM SWITCH IAW AMM 27-41-05. OPS CHEC K GOOD. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 ASOA200801522 1 20081116 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 708-761 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 713EV 10081 RT SIDEWALL SEAT RAILS HAVE SCATTERED CORROSION BETWEEN FS 708.00 TO FS 761.00. BLENDED CORROSION IAW SRM 53-31-49. EX CEED ALLOWABLE LIMITS. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 VNAA2008111700007 1 20081121 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A VNAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 05 207PS 7873 ON APPROACH TO LGA WHEN FLAPS WERE SELECTED TO 30 A FLAP FAIL CAS MESSAGE ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT . MAINTENANCE TESTED SYSTEM AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 VNAA200811177A 1 20081121 A 2421 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 FAILED A VNAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 05 207PS 7873 CREW REPORTED ON TAKEOFF ROLL FROM CLT, IDG 2 CAUTION MSG CAME ON. ABORTED TAKEOFF. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. A RESET OF GEN 2 WAS ACCOMPLISHED & ALL MSG'S WERE CLEARED. MAINTENANCE SERVICED THE NR 2 IDG. NO DEFECTS N OTED AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 A6WA200840604 1 20081102 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ODOR A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 438AW 7748 PRE FLIGHT SMELL OF SMOKE IN COCKPIT WITH LT PACK ON. UPON BOARDING ACFT FOUND APU RUNNING WITH BOTH LT AND RT PACKS ON AND OPERATING NORMALLY. INSPECTED ALL WINDOW HEAT CONNECTIONS, TERMINALS, COCKPIT CB`S AND LIGHTS. ALL APPEAR NORMAL. NO ODOR OR SMOKE NOTED AT THIS TIME. ACFT OK FOR SERVICE. 2 L 7 2 4F RT A21EA 20081203 SO 2008 12 3 C2XA08IA245 1 20081125 A 3350 78241 INVERTER EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13936 145025 IAH - FLIGHT 2524, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE 2ND AND 3RD AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT W AS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20081203 SO 2008 12 3 C2XA08RI166 1 20081113 A 2810 SWITCH EMB 145 EMB145XR 3260214 SO REFUEL PANEL OUT OF POSITION A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 14105 145649 FLIGHT 2539 - RIC - FLIGHT CREW REPORTED FUEL XFER CRITICAL MESSAGE ON EICAS. FLIGHT CREW PERFORMED AIR RETURN AND LAND ED AIRCRAFT UNEVENTFULLY. RIC MX FOUND POWER SELECTION SWITCH ON REFUEL PANEL IN BATT POSITION. MX REPOSITION SWITCH T O NORMAL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081203 SO 2008 12 3 C2XA08IA242 1 20081118 A 3350 66368 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13965 145125 MCI - DURING MAINTENANCE INSPECTION, THE LAST THREE AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE EMERGENCY LIGHT STRIP JUST AFT OF ROW 12, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081203 SO 2008 12 3 C2XA08RI167 1 20081114 A 3230 LANDING GEAR EMB 145 EMB145LR 3260212 SO NLG MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13970 145146 FLIGHT 2361 - EWR - FLIGHT CREW REPORTED NLG WOULD NOT RETRACT NORMALLY, CREW HAD TO USE DOWNLOCK RELEASE TO RETRACT GEA R, THEN GEAR EXTENDED NORMALLY. EWR MX PERFORMED A FLIGHT TEST AND COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT PASSED OP ERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081203 WP 2008 12 3 AALA200810232 1 20081111 A 5322 MOUNT FITTING DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 GALLEY MOUNT FITTING CORRODED STATION 218 OUTBOARD OF NR 5 SEAT TRACK. INSTALLED NEW GALLEY MOUNT FITTING. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200810233 1 20081106 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 SEAT TRACK NR 2 CORRODED FROM STATION 1031-1221. REPLACED SEAT TRACK. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200810234 1 20081110 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 RIGHT CARGO TIE DOWN TRACK CORRODED STATION 1231-1271. REPLACED TIE DOWN TRACK FORM STATION 1212 TO 1322. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200802739 1 20081015 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 427AA 49339 LGA - EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081203 WP 2008 12 3 AALA200810215 1 20081105 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 LEFT CUSP MEMBRANE CORRODED STATION 1022. INSTALLED NEW CUSP SHEET PER AARD 51-00-00-12. 2 L 7 2 4F A6WE 20081203 NM 2008 12 3 AALA200802340 1 20081016 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 199AN 32393 TPA - EMERGENCY LIGHTS AT SEAT ROWS 16D TO 21D INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 19DEF FOR EMERGENCY LIGHT S AT SEAT ROWS 16D TO 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081203 WP 2008 12 3 AALA200810235 1 20081111 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 CORROSION ON OUTFLOW VALVE SUPPORT STRUCTURE AT STATION 1275 NEAR LONGERON 21 LEFT. REMOVED AND REPLACED INTERCOSTAL FR OM STATION 1271-1287 PER SRM 51-30-05. 2 L 7 2 4F A6WE 20081203 EA 2008 12 3 C2XA08CL123 2 20081127 A 7200 23070401 ENGINE EMB 145 EMB145LR 3260212 SO RROYCE AE3007 AE3007A1P 54571 EA NR 2 FAULTY A C2XA K NONE O OTHER CL CLIMB 1 SW 27 16951 19960 145063 CAE311298 CLE - FLIGHT 2311 - THE CREW REPORTED AT FL320 THE NR 2 ENGINE ITT STARTED INCREASING SLOWLY TO 860 WITHOUT FULL THRUST. ASSENTING AT 91PERCENT N2 THE ENGINES HAD A 30 DEGREE DIFFERENCE. THE FUEL FLOW WAS ALSO NOTED TO BE 30 PPH HIGH. MAI NTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081203 NM 2008 12 3 SWAA086685 1 20081201 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787 BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081203 NM 2008 12 3 SWAA086686 1 20081201 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND RT WING NR 5 SLAT O/B UPPER SURFACE DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20081203 NM 2008 12 3 SWAA086687 1 20081201 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 8L TO STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 EA 2008 12 4 COMA200811170001 1 20081117 A 2780 SLAT CNDAIR CL600 CL6002C10 1390015 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION TO TAKEOFF 1 SO 27 398CA 10112 AFTER TAKEOFF FROM JFK RECEIVED A SLAT FAIL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND CONTINUED TO BWI, AIRCRAFT LANDED WITHOUT INCIDENT. PERFORMED SYSTEM RESET. 2 L 7 2 4F RT A21EA 20081204 NM 2008 12 4 UPS08M53894 1 20081108 A 5720 DOUBLER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C RT WING FIXED L/E COMPT AT XORS 562 HAS CRACK 4 EA AROUND FASTENERS HOLE ON BEADED DOUBLER. REMOVED DAMAGE, FABRICATED FILLER, ANGLES AND DOUBLER, AND INSTALLED IAW MD-11 SRM 57-10-00 VOL 1 FIG 27. 2 L 7 3 4F RT A22WE 20081204 EU 2008 12 4 UPS08153922 1 20081107 A 7830 22141261145CV PANEL AIRBUS A300 A300F4622R 3930360 EU THRUST REVERSER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 142UP 0825 INSPECTION TYPE:C DURING MAINTENANCE CHECK INSP FOUND NR 1 ENGINE RT T/R INNER BARREL PANEL HAD A 0.4 INCH CRACK AT UPPE R FORWARD AREA. CUT OUT AND REPAIRED DAMAGED AREA PER UPS EO A300-7830-31176-A AND SAA EA 300-7830-01-A1556. 2 L 7 2 4F RT A35EU 20081204 EU 2008 12 4 UPS08153928 1 20081116 A 5330 SKIN AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 150UP 0833 INSPECTION TYPE:N/A SKIN PLATE DAMAGED BETWEEN FR 78 AND 79 STR 44L AND 45L. REPAIRED IAW EO A300-5330-31201. 2 L 7 2 4F RT A35EU 20081204 2008 12 4 UPS08M53935 4 20081116 A 2565 60289117 SLIDE DOUG MD11 MD11F 3023600 NM L1 DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A L-1 DOOR ESCAPE SLIDE INOP. REMOVED AND REPLACED ESCAPE SLIDE ASSY PER MM 25-61-15-4. THIS CLEARS M388750. 2 L 7 3 4F RT A22WE 20081204 NM 2008 12 4 R61A20080043 1 20081117 A 2782 1702885C ACTUATOR EMB ERJ170 ERJ170100SU 3260403 NM LE SLAT MALFUNCTIONED A R61A O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 829MD 8241 8241 17000049 ON APPROACH CREW REPORTED A SLAT/FLAP FAIL MESSAGE ON EICAS. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TROUBLESHOT. REMOVED AND REPLACED THE NR 5 SLAT ACTUATOR COMPLETED OPERATIONAL CHECK OF THE SYSTEM, OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A56NM 20081204 NM 2008 12 4 UPS08M53944 1 20081115 A 5330 NFA6712 DOUBLER DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C SURVEY SEQUENCE NUMBER 254-F1-007 OF MD11-5100-30530 APPENDIX C SECTION D, BLEND ON DOUBLER AT FWD LW R SIDE STA 1984 L39L. REMOVED EXISTING DOUBLER AND FILLER, FABRICATED FILLER AND DOUBLER 1 AND REPAIR DOUBLER 2 AND INS TALLED IAW MD11 VOL 1 SRM 53-50-00 FIG 17. 2 L 7 3 4F RT A22WE 20081204 NM 2008 12 4 UPS08M53947 1 20081117 A 5720 DOUBLER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C RT WING FIXED L/E COMPT XORS 622 HAS CRACK 2 EA AROUND FASTENERS HOLE ON BEADED DOUBLER. REMOVED DAM AGE, FABRICATED AND INSTALLED DOUBLER, FILLER, AND ANGLES IAW MD11 VOL 1 SRM 57-10-00 FIG 27. 2 L 7 3 4F RT A22WE 20081204 NM 2008 12 4 SWAA086740 1 20081202 A 3350 417S5900 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 703SW 27837 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY FAILED TEST AT ROW 16. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086741 1 20081202 A 3350 417S5900 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 703SW 27837 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY FAILED TEST AT ROW 11. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086746 1 20081202 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 18L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086747 1 20081202 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 19L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086748 1 20081202 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 460, BETWEEN STR 14R TO STR 15R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086750 1 20081202 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BETWEEN BS 360 TO BS 440, STR 23R. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086751 1 20081202 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BETWEEN BS 360 TO BS 440, STR 24R. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086696 1 20081201 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086697 1 20081201 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086698 1 20081201 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 787, STR. 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086699 1 20081201 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, BETWEEN STR 8L TO STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 2008 12 4 SWAA086637 4 20081129 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 306SW 22946 L1 DOOR EMERGENCY EXIT SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086638 1 20081129 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BETWEEN BS 375 TO BS 378, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086639 1 20081130 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND KEEL BEAM CORRODED AT BS 500D, STR 27L. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086629 1 20081127 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 203WN 32483 DURING SCHEDULED MV3 CHECK, FOUND RT EEPLS LENS LOOSE. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081204 2008 12 4 SWAA086630 4 20081128 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 209WN 32484 FOUND L1 DOOR EMERGENCY EXIT SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086631 1 20081130 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 229WN 32498 FOUND FWD EEPLS LIGHT BROKEN. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086643 1 20081130 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 7L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086644 1 20081130 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 9L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086645 1 20081130 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086646 1 20081128 A 2121 215201 GASPER FAN BOEING 737 7373H4 1384600 NM CABIN FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 306SW 22946 DECLARED EMERGENCY, SMOKE IN CABIN - ACRID SMELL NEAR AFT GALLEY CONCENTRATED IN REAR WITH SOME VISIBLE SMOKE. F/O TURN ED DOWN RT PACK AFTER CALL - IT HELPED. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086724 1 20081202 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086729 1 20081202 A 5314 6545866 KEELBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED SPV CHECK, FOUND RT KEEL BEAM CORRODED AT BETWEEN 500D TO BS 520. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081204 EA 2008 12 4 VNAA2008112000006 1 20081116 A 2150 GG670950093 ACM CNDAIR CL600 CL6002C10 1390015 EA AC BAY SEIZED A VNAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 05 720PS 5579 5474 10178 AFTER LANDING AND TAXI TO GATE AT CLT, SMOKE STARTED COMING FROM VENTS IN COCKPIT. CREW ELECTED TO STOP SHORT OF GATE A ND EVACUATE THE AIRCRAFT. AIRCRAFT WAS EVACUATED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND LT AIR CYC LE MACHINE SEIZED. LT AIR CONDITIONING PACK WAS DEFERRED. NO OTHER DEFECTS WERE NOTED AND AIRCRAFT WAS RELEASED FOR SE RVICE. ON 081117 MAINTENANCE CHANGED THE AIR CYCLE MACHINE AND NO OTHER DEFECTS WERE NOTED. 2 L 7 2 4F RT A21EA 20081204 EA 2008 12 4 VNAA2008111900004 1 20081114 A 5350 RADOME CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 708PS 10160 CREW REPORTED THE AIRCRAFT EXPERIENCED STATIC DISCHARGE FROM THE FRONT RIGHT, WHICH WAS VISIBLE AND AUDIBLE FROM THE COC KPIT WHILE FLYING THROUGH A RAIN SHOWER. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE RIGHT WINGLET, THE RIGHT SIDE OF THE FUSELAGE AND THE RADOME. THE LEFT AND RIGHT WIPER ARMS WERE FOUND TO BE MAGNETIZED. REPAIRS WERE MADE TO THE WIN GLET AND FUSELAGE. THE RADOME WAS REMOVED AND REPLACED. THE WIPER ARMS WERE DEMAGNETIZED. NO FURTHER DEFECTS WERE NOT ED. CHECKS WERE PERFORMED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081204 2008 12 4 VNAA2008111900005 4 20081114 A 2360 STATIC WICK CNDAIR CL600 CL6002B19 1900309 EA HORIZ STAB MISSING A VNAA O OTHER O OTHER DE DESCENT 1 GL 05 229PS 7898 CREW REPORTED A LIGHTNING STRIKE DURING DESCENT. MAINTENANCE INSPECTED AND FOUND A STATIC WICK MISSING FROM THE RIGHT H ORIZONTAL STABILIZER AND DAMAGE TO THE FUSELAGE, HORIZONTAL STABILIZER, NR 2 ATC ANTENNA AND NR 2 VHF ANTENNA. THE MISS ING STATIC WICK WAS REPLACED. REPAIRS WERE MADE TO THE FUSELAGE AND THE HORIZONTAL STABILIZER. THE NR 2 ATC ANTENNA AN D THE NR 2 VHF ANTENNA WERE REMOVED AND REPLACED. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081204 WP 2008 12 4 AALA200802346 1 20081016 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7550 53032 DFW - EMERGENCY DOUBLE ARROW EXIT MARKER AT FORWARD ENTRY INOPERATIVE. REPAIRED DAMAGED WIRING FOR EMERGENCY DOUBLE ARR OW EXIT MARKER AT FORWARD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081204 NM 2008 12 4 AALA200802347 1 20081016 A 3350 1000679 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 336AA 22334 LAX - EMERGENCY PORTABLE LIGHT AT COCKPIT DOOR INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT ASSEMBLY AT COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081204 WP 2008 12 4 AALA200802348 1 20081017 A 2170 COALESCER BAG DOUG DC9 DC982 3022082 WP AC BAY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 291AA 49303 ATL INFLIGHT - DURING CLIMB-OUT BETWEEN 4000 AND 10000 FEET, FLIGHT ATTENDANT REPORTED WHITE SMOKE IN CABIN. ACCOMPLISH ED CABIN SMOKE AND FIRE CHECKLIST AND SMOKE BEGAN TO DISSIPATE. RETURNED TO ATL AND LANDED WITHOUT INCIDENT. ACCOMPLIS HED BURN OUT OF HIGH PRESSURE PNEUMATIC DUCTING, AND REPLACED TAIL COMPARTMENT COALESCER BAGS. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F A6WE 20081204 WP 2008 12 4 AALA200810245 1 20081125 A 5230 3926046509 TEE FITTING DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 554AA 53084 FORWARD CARGO DOOR, LOWER FORWARD STOP, TEE FITTING CRACKED. REMOVED AND REPLACED TEE FITTING. 2 L 7 2 4F A6WE 20081205 EA 2008 12 5 SWIA200820523 1 20080916 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 465SW 7845 DURING C-CHECK, RIGHT ENGINE THRUST MOUNT CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 ASAA0843894 1 20081029 A 5311 65465293 FRAME BOEING 737 7374Q8 138447Q NM BS 440 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER EA 400 53EA 00267. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008120101109 1 20081127 A 5330 141A31131 BEAR STRAP BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14249 28809 L1 DOOR HAS CORROSION ON INNER DOOR FRAME SKIN UPPER AFT INITIATED "DIP" TO ACCOMPLISH PERMANENT REPAIR WITHIN 12 MONTHS REF ECRA 5330-03849. L1 DOOR CUTOUT BEAR STRAP CORRODED. PER ECRA 5330-03849 COMPLETED INTERIM REPAIR. COMPLY WITH P ERMANENT REPAIR WITHIN 12 MONTHS. PLANNING TO CONTACT ESC AFTER 10 MONTHS BUT PRIOR TO 11 MONTHS FOR PERMANENT REPAIR. ISSUED DIP CONTROL NR D090804 1. 2 L 7 2 4F RT A16WE 20081204 NM 2008 12 4 SWAA086722 1 20081202 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008120201116 1 20081202 A 5320 69434771 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14336 23574 AFT CARGO BAY RT SIDE TRANSITION ANGLE CORRODED FROM STA 787 TO 807. REMOVED AND REPLACED TRANSITION ANGLE STA 787 TO 8 07 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081205 WP 2008 12 5 FDEA200812035066 1 20081203 A 5230 NDA6066545 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 800 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 FWD LOWER CARGO DOOR, DEFORMED FWD LOWER SKIN CORNER. 2 L 7 3 4F RT A22WE 20081205 NM 2008 12 5 ASAA0843895 1 20081029 A 5311 65465269 FRAME BOEING 737 7374Q8 138447Q NM BS 400 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400 53EA 00267. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008120101105 1 20081129 A 3350 ADD71701100 BATTERY PACK BOEING 737 737724 13844BY NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 39728 28944 LEFT WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPS CHECKS GOOD. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008120101108 1 20081126 A 5322 6546548 SHEAR TIE BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14652 28913 CORROSION ON SHEAR TIE AT STATION 747, STR 27R (BILGE AREA). REMOVED AND INSTALLED REPAIRED SHEAR TIE AND DOUBLER AT ST ATION 747 STR-27R (BILGE) REF SRM 53-00-07. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008120101110 1 20081130 A 5230 146A611013 PLATE BOEING 737 737824 13844BZ NM AFT CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14249 28809 AFT CARGO DOOR HAS 2 SPOTS OF CORROSION AT INNER PANEL, LOWER FWD CORNER. REPAIRED DAMAGED AREA ON AFT CARGO DOOR INNER SKIN PER ECRA 5232-01105. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 CALA2008112401091 1 20081121 A 5315 65C33950 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14652 28913 MINOR CORROSION ON FLOORBEAM, STA 986 AT FASTENER HOLES, RBL 40-RBL 50. BURNISHED CORROSION FOUND TO BE OUT OF LIMITS A T RBL 40 AND INSTALLED REPAIR STRAP AT RBL 40 REF SRM 53-00-51 REPAIR 3. 2 L 7 2 4F RT A16WE 20081205 WP 2008 12 5 FDEA200812035069 1 20081203 A 5320 ADA33538 STANCHION DOUG DC10 DC1030F 3023504 WP ZONE 100 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 317FE 46835 FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. 2 L 7 3 4F RT A22WE 20081205 WP 2008 12 5 FDEA200812035071 1 20081203 A 5320 ADA335327 STANCHION DOUG DC10 DC1030F 3023504 WP ZONE 100 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 317FE 46835 FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. 2 L 7 3 4F RT A22WE 20081205 NM 2008 12 5 EIAA2008120300074 1 20081202 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM ZONE 200 INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486EV 20888 DURING PREFLIGHT FOUNG CEILING U/D EMERGENCY EXIT LIGHT OVER THE STAIRS INOP. REPLACED LIGHT PER B747 MM 33-51-00, OPS CHECKED SATISFACTORLY. 2 L 7 4 4F RT A20WE 20081205 NM 2008 12 5 ASAA0873903 1 20081117 A 5320 141A850528 WEB BOEING 737 737790 13844CN NM BS 327-352 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 E/E DOOR CUTOUT SURROUND STRUCTURE LT FRAME WEB DAMAGED FROM CLOSING PARTIALLY LOCKED DOOR. R&R E&E DOOR CUTOUT SURROUN D STRUCTURE LT FRAME WEB. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0853932 1 20081201 A 3040 SENSOR BOEING 737 737890 1384527 NM COCKPIT WINDOW FAILED A ASAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 02 583AS 5529 35681 RIGHT SIDE WINDOW OVERHEAT CONDITION 10 MIN AFTER TAKEOFF TURNED HEAT OFF FOR 5 MINUTES PER QRH UPON TURNING HEAT ON THE OVERHEAT LAMP ILLUMINATED IMMEDIATELY. TURNED HEAT OFF FOR REMAINDER OF FLIGHT. RT SIDE WHCU FAULTS SENSOR. W/RT SID E WINDOW HEATED FOUND PRIMARY SENSOR AT 364 OHMS. SPARE AT 352 OHMS. MAX IS 330 OHMS PER MM 30-41-21-760-801 TABLE 502 . CHECK OF HEAT FILM RESISTANCE GOOD PER MM 30-41-21-000-801. VERIFIED WINDOW IS TAPPED PROPERLY REF WD 30-41-11 PG 3. REMOVED AND REPLACED R2 WINDOW. 2 L 7 2 4F RT A16WE 20081205 NE 2008 12 5 COMA2008120290001 2 20081201 A 7220 4114T15P02 FAN BLADE CNDAIR CL600 CL6002D24 1390016 EA GE CF34 CF348C5 30050 NE NR 2 ENGINE DAMAGED A COMA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 SO 27 679CA 2950 15132 194594 EN ROUTE FROM ORD TO JFK NR 2 ENGINE N1 VIBE. ACFT IN ICING CONDITIONS. FOLLOWED QRH FOR ICING BUT VIBE CONTINUED TO C LIMB, PERFORMED IFSD OF NR 2 ENGINE. EMERGENCY DECLARED, ACFT DIVERTED TO FWA LANDED SAFELY. REMOVED AND REPLACED 3 SE TS OF DAMAGED FAN BLADES. VIBE AND OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E00063EN 20081205 EA 2008 12 5 COMA2008120270004 1 20081201 A 3250 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA NLG STEERING FALSE INDICATION A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 398CA 10112 ON APPROACH INTO CVG, RECEIVED STEERING INOP CAUTION MSG AFTER GEAR WAS SELECTED DOWN. EMERGENCY DECLARED, ACFT LANDED SAFELY. POWERED DOWN ACFT AND BACK UP, PERFORMED NWS SYSTEM OPERATIONAL CHECKS, NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 MASA2008111900782 1 20081119 A 7997 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA PRESSURE SWITCH CONTAMINATED A MASA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SW 07 17175 7175 ASH FLT 7304 IAD-JAX. CAPTAIN DECLARED AN EMERGENCY AND DIVERTED TO RDU DUE TO LOW OIL PRESSURE MASTER WARNING IN FLIGH T. MX FOUND OIL ON CONNECTOR FOR PRESSURE SWITCH, CLEANED AND RE-SECURED. PERFORMED ENGINE RUNS, OIL TEMP AND OIL PRES SURES NORMAL. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820506 1 20081122 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 746SK 10202 CLT 6663 - CEILING EMERGENCY FLOOD LIGHT, AFT CABIN, INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820507 1 20081120 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT LOOSE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 740SK 10196 FLT 6547 - NR 4 EMERGENCY LIGHT INOP. RESEATED BULB. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820508 1 20081125 A 3697 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA BLEED LOOP SHORTED A SWIA B EMER. DESCENT S AFFECT SYSTEMS CR CRUISE 1 NM 07 738SK 10195 FLT 6285 - LEFT BLEED WARNING, PACKS SHUTDOWN AUTOMATICALLY, PERFORMED EMERGENCY DESCENT. REPOSITIONED LEFT BLEED LOOP A, CLEANED CONNECTORS LEFT BLEED LOOP B. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820509 1 20081123 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 705SK 10145 FLT 6570 - SERVICE DOOR EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 MASA2008113000793 1 20081130 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN OUT OF POSITION A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 592ML 7410 ASH FLT 7144 IAD-PHL. OVERHEAD EMERGENCY EXIT SIGN FELL DOWN. MX SECURED SIGN AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 ASAA0843901 1 20081029 A 5311 6546548119 FRAME BOEING 737 7374Q8 138447Q NM BS 747 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER EA 400-53EA-00267. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0873910 1 20081118 A 5347 146A750125 CARGO TRACK BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 AFT CARGO BAY TIE DOWN TRACK CORRODED. REMOVED AND REPLACED CARGO BAY TIE DOWN RACK IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081205 EA 2008 12 5 MASA2008113000731 1 20081130 A 5210 LANYARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNKNOWN A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 7264V 7264 ASH FLT 2791 FAT-ROM. MAIN CABIN DOOR WILL NOT OPEN. MX REMOVED HAND RAIL QD LANYARD FROM MECHANISM. OPS CHECKED GOOD . 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 TSAA0853030 1 20081116 A 5330 6545767 SKIN BOEING 737 7372X6C 1384552 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 840AL 23124 APPROX 3 INCH CRACK DISCOVERED AT BS 533 TO BS 536 STR 16R. REPAIRED IAW SRM 53-30-3 FIG 48 DETAIL IX. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 USAA2008120392178 1 20081123 A 5320 D53480019217 PLATE AIRBUS A319 A319132 3930340 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 808AW 1088 SAL - C7 - MAJOR REPAIR - CRACK ON COVER PLATE BETWEEN FR 68 TO FR 69, S23R. REPLACED COVER PLATE BETWEEN FR 68 TO FR 6 9, S23R IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081205 EU 2008 12 5 MALA080206 1 20081120 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 340B433 SEVERAL FUSELAGE FRAMES INNER FLANGES CHAFED. REPAIRED IAW EO NR S53641, S53642, S53152. 2 L 7 2 4T RT A52EU 20081205 EU 2008 12 5 USAA2008120392180 1 20081203 A 3211 D3215303000800 PIN AIRBUS A319 A319112 3930323 EU ZONE 700 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 713UW 1040 PIT - LRN - MAJOR REPAIR - LEVEL 2 PITTING CORROSION ON RIGHT MAIN LANDING GEAR AFT PINTLE PIN FLANGE FACE. REPLACED RI GHT MAIN LANDING GEAR AFT PINTLE PIN IAW US AIRWAYS TASK CARD 26T00032001. 2 L 7 2 4F RT A28NM 20081205 WP 2008 12 5 WX0A070246 1 20081023 A 3350 60030451 POWER SUPPLY DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 948MA 49778 REPORTED BY FLIGHT CREW, THE EMERGENCY EVACUATION LIGHTING SYSTEM FOUND TO BE DEFECTIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOM PLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 20081205 NM 2008 12 5 USAASB08118 1 20081130 A 2560 MV10 MEGAPHONE BOEING 737 7373G7 138447J NM FORWARD CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 322AW 25400 PHX - MAINTENANCE REPORTED THE FORWARD MEGAPHONE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD MEGAPHONE. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 USAA2008120292163 1 20081126 A 5315 6545815 FLOORBEAM BOEING 737 7374B7 138449C NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM UPPER T-CAP AT BS 344, LBL 19 TO RBL 8. REPAIRED F LOORBEAM UPPER TEE CAP AT BS 344, LBL 19 TO RBL 8 IAW SRM 53-30-51. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 USAA2008120292164 1 20081126 A 5311 6546525 FRAME BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - FUSELAGE FRAME CRACKED AT BS 380, BETWEEN S8L AND S9L. REPAIRED FUSELAGE FRAME AT BS 380, BET WEEN S8L AND S9L IAW EA NR 100749. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 USAA2008120292165 1 20081129 A 5322 SHEAR TIE BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - SHEAR TIE CRACKED AT FRAME BS 344 BETWEEN S19R TO S20R. REPAIRED SHEAR TIE AT FRAME BS 344 BE TWEEN S19R TO S20R IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 USAA2008120292167 1 20081125 A 5312 BULKHEAD BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - CRACK ON VERTICAL BEAM WEB AT BS 178 BULKHEAD, LBL 17, WL 232. REPAIRED VERTICAL BEAM WEB AT BS 178 BULKHEAD, LBL 17, WL 232 IAW SRM 53-10-08 REPAIR 12. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 UPS08553972 1 20081031 A 5330 SKIN BOEING 757 75724APF 1384969 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 455UP 25476 INSPECTION TYPE:N/A LIGHTNING STRIKE DAMAGE TO FASTENER LOCATED AT FUSELAGE BS 395.0 STRINGER 3 LEFT. DAMAGE BEYOND SRM LIMITS. DAMAGED REPAIRED PER EO B757-5330-31068-A. 2 L 7 2 4F RT A2NM 20081205 NM 2008 12 5 ASAA0843921 1 20081030 A 5330 65458001203 BEAR STRAP BOEING 737 7374Q8 138447Q NM BS 297-307 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 L1 DOOR LOWER HINGE CUTOUT SKIN AND BEARSTRAP CRACKED REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR TRIPLER, REPAIR D OUBLER, REPAIR FILLERS, STRUCTURAL FILLER IAW ASA EA 400-53EA-00284. 2 L 7 2 4F RT A16WE 20081205 WP 2008 12 5 UPS08853973 1 20081107 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV FLUSH SKIN REPAIR 1740 DOES NOT MEET SRM REQUIREMENTS. PREVIOUSLY REPAIRED DRW 3804041. 2 L 7 4 4F RT 4A25 20081205 WP 2008 12 5 UPS08853975 1 20081031 A 5720 STRUCTURE DOUG DC8 DC871F 302199D WP LT WING MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV LEFT WING STA XRS 431 HAS A DOUBLER THAT IS WRONG THICKNESS. REPAIRED DOUBLER IAW 57-2-1 FIG 2Q. 2 L 7 4 4F RT 4A25 20081205 NM 2008 12 5 WRLA2008091 1 20081124 A 3213 STRUT DOUG MD11 MD11F 3023600 NM RT MLG CHAFED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 CHAFING - DURING BRIDGE CHECK+4C CHECK, EGAT MECHANIC FOUND RT MAIN GEAR SHOCK STRUT UPPERSIDE HAD CHAFED L=3" AT STA Y= 1240 (REFER TO EGAT NRC NO. U05124) IAW EGAT EI NR W2008A32B-1088 REV OO, EGAT EI NR W2008A32B-1088 REV 01 AND APPROVED RDR DATED 11/11/08. 2 L 7 3 4F RT A22WE 20081205 2008 12 5 SWIA200820511 4 20081124 A 2210 6224404101 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA AILERON SERVO BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 479CA 7675 FLT 2626 - AILERON CONTROL EXTREMELY DIFFICULT TO MOVE. REPLACED AILERON SERVO ACTUATOR, PN 622-4404-101, SN ON 1284, S N OFF HX6P. 2 L 7 2 4F RT A21EA 20081205 WP 2008 12 5 UPS08853981 1 20081119 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV WEB CRACK FWD CARGO DOOR JAMB AT STA 1400. REPAIRED 53-02-00 FIG 23. 2 L 7 4 4F RT 4A25 20081205 EA 2008 12 5 SWIA200820514 1 20081126 A 3230 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA L ABORTED APPROACH O OTHER AP APPROACH 1 NM 07 433SW 7550 FLT 4865 - 'GEAR DISAGREE' FROM NOSE GEAR. REPLACED THE PRIORITY VALVE FOR THE NOSE LANDING GEAR. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 UPS08M53974 1 20081121 A 3213 CYLINDER DOUG MD11 MD11F 3023600 NM MLG CONTAMINATED A IPXA K NONE S AFFECT SYSTEMS CL CLIMB 1 SO 01 256UP 48405 INSPECTION TYPE:N/A GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. ALTERNATE PROCEDURE DID NOT BRING THE GEAR HANDLE UP . AIR TURNBACK. PERFORMED FIM 32-30-23-00 STEP GEAR HANDLE WOULD NOT RETRACT. BLEED TRUCK BEAM CYLINDER PER MM 32-37- 01. AFTER BLEEDING CYLINDER, BEAM TRIM INTERLOCK TEST IAW MM 32-37-00-5. GEAR HANDLE INTERLOCK OPS CHECKS GOOD. ACFT OK FOR SERVICE. 2 L 7 3 4F RT A22WE 20081205 NM 2008 12 5 USAA2008120292172 1 20081201 A 5315 6545810 FLOORBEAM BOEING 737 7374B7 138449C NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT BS 312, LBL 14 TO RBL10. REPAIRED FLOORBEAM AT BS 312, LBL 14 TO RBL 10 IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 USAA2008120292174 1 20081130 A 5311 6546540 FRAME BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - FRAME CHORD CRACKED AT BS 639, S18L. REPAIRED FRAME CHORD AT BS 639, S18L IAW TYPICAL REPAIR NR 53-62-01. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 USAA2008120292175 1 20081018 A 5320 6547958 WEB BOEING 737 7373G7 138447J NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL - C21 - MAJOR REPAIR - CORROSION ON WEB BETWEEN BS 847 TO BS 867, RBL 21. REPAIRED WEB BETWEEN BS 847 TO BS 867, RB L 21 IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 USAA2008120292176 1 20081010 A 5320 6546812169 INTERCOSTAL BOEING 737 7373G7 138447J NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL - C21 - MAJOR REPAIR - CORROSION ON INTERCOSTAL BETWEEN BS 967 TO BS 986.5, WL 208.1, LBL 17.5. REPAIRED INTERCOSTA L BETWEEN BS 967 TO BS 986.5, WL 208.1, LBL 17.5 IAW SRM 51-40-02-0G. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 UPS08M53982 1 20081025 A 5753 ARC4005810 SKIN DOUG MD11 MD11F 3023600 NM TE FLAP DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C RT WING O/B FLAP LOWER SURFACE 22 INCHES O/B OF PANEL 657FB 39 INCHES FROM T/E FOUND DENT. REMOVED D AMAGE AND BONDED REPLIES IAW UPS EO MD11-5750-31266-A AND SAA EA 011-5750-01-A1564. 2 L 7 3 4F RT A22WE 20081205 EA 2008 12 5 COMA2008120150018 1 20081130 A 5730 601R10045 PANEL CNDAIR CL600 CL6002B19 1900309 EA ZONE 500 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 442CA 19194 7483 LEFT WING PLANK FUEL PANEL CUTOUT AT 540BB HAS FRETTING CORROSION ON INBOARD SIDE. BLENDED OUT AND REMOVED FRETTING DAM AGE ON FUEL PANEL CUTOUT 540BB INBD SIDE PER REO 601R57-21-030. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 COMA2008120150019 1 20081130 A 5311 6013600121 FRAME CNDAIR CL600 CL6002B19 1900309 EA ZONE 400 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 442CA 19194 7483 LEFT FS 640.00 FRAME AND BONDED SKIN DOUBLER ARE CRACKED BETWEEN STR 9 AND 13. COMPLIED WITH MODIFICATION K601R36009-3 ON LT FS 640.00 FRAME AND DOUBLER PER S/B601R-53-061 KIT DRWG K601R36009 REV B, 601R-53-61-506 REV C AND 601R53-61-569. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 ASAA0873950 1 20081125 A 5320 453A16115 STRUCTURE BOEING 737 737790 13844CN NM BS 400-440 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 FWD CARGO BAY CORROSION ON THE FWD RT CAPSTRIP AROUND FASTENER HOLES BOTTOM SIDE. REMOVED AND REPLACED RT CAPSTRIP IN F WD CARGO BAY. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 UPS08M53983 1 20081026 A 7830 683L219G07 WEB DOUG MD11 MD11F 3023600 NM THRUST REVERSER GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C NR 2 ENGINE RT T/R CENTER FWD WEB FOUND WITH GOUGE AT 3 O`CLOCK POSITION. GOUGE FOUND OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-7830-31193-A AND CF6-80C2 CMM 78-32-02 REPAIR 24. 2 L 7 3 4F RT A22WE 20081205 NM 2008 12 5 ASAA0843919 1 20081117 A 5753 SKIN BOEING 737 7374Q8 138447Q NM LT WING TE FLAP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 LEFT WING OUTBOARD AFT FLAP TE IS DELAMINATED AT INBOARD CORNER. REMOVED DELAMINATED SECTION. INSTALLED FILLER DOUBLER AND BONDED REPAIR PER SRM 51-70-10. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0873949 1 20081121 A 5720 115A29532 SUPPORT BOEING 737 737790 13844CN NM RT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 FWD WEB SUPPORT FOR SEAL RETAINER IS CRACKED AT FASTENER RSS 269 RIGHT WING COMMON TO SUPPORT FOR UPPER TRAILING PANEL. REMOVED AND REPLACED SEAL RETAINER PER SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0843952 1 20081118 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 8 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 RT WING NR 8 SPOILER HAS MULTIPLE PROTRUDING DENTS 8 INCHES FROM T/E HIGHEST DENT MEASURES A=.800 Y=.008 A/Y= 80 MARKED. REPAIRED DENT DAMAGE AT INBD AND OTBD UPPER SURFACE OF NR 8 SPOILER IAW B737 400 SRM 51 70 10 REPAIR 2. 2 REPAIR DOUB LERS INBD END AT 2" ,12" FROM EDGE OTBD END 2", 12" FROM EDGE. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0843954 1 20081201 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 9 SPOILER PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 NR 9 SPOILER HAS A PUNCTURE ON LOWER SIDE 9 INCHES FROM INBD END. REPAIRED NR 9 SPOILER LOWER SKIN PUNCTURE IAW SRM 51- 70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0843955 1 20081119 A 5753 6546430189 SKIN BOEING 737 7374Q8 138447Q NM LT FOREFLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 LT WING INBD FORE FLAP UPPER SURFACE DENTED 8 INCHES FROM T/E AND 47 INCHES FROM INBD SIDE. DENT MEASURES A=1.3 Y=.033 FOR A/Y 39.39, REPAIRED DENT DAMAGE ON LT WING INBD FOREFLAP UPPER SURFACE IAW SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0843957 1 20081118 A 5753 6546434352 SKIN BOEING 737 7374Q8 138447Q NM RT TE FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 RT WING INBD T/E AFT FLAP SEGMENT SMALL GOUGE ON T/E UPPER SURFACE 5 INCHES FROM OTBD END. REPAIRED RT WING INBD T/E AF T FLAP IAW SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081205 EA 2008 12 5 COMA2008112450007 1 20081122 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 806CA 18997 7359 FLAPS FAILED AT 0 DEG ON APPROACH INTO PHL. EMERGENCY DECLARED, ACFT LANDED SAFELY. REMOVED AND REPLACED FLAP SYSTEM P DU. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820538 1 20081125 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 FLT 5937 - CEILING EMERGENCY FLOOD LIGHT NEXT TO LAV INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 COMA2008112450005 1 20081122 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 971CA 7145 FLAPS FAILED AT 0 DEG ON APPROACH INTO YYZ. EMERGENCY DECLARED, A/C LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0002 , FLAPS FAIL CAUTION MESSAGE FOLLOW UP MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820539 1 20081127 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710BR 7852 FLT 6701 - LAST EMERGENCY LIGHT IN CABIN INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 P5CA2008112001579 1 20081119 A 5280 DOOR BOEING 747 74746NF 13848BT NM LT MLG DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 453PA 30811 DAMAGE TO LT WING LANDING GEAR DOOR. TIME LIMITED REPAIR AS PER EO 4452A056. REPEAT DVI'S AT EVERY FLIGHT CYCLE AND A PERMANENT REPAIR AT NEXT "A" CHECK." 2 L 7 4 4F RT A20WE 20081205 NM 2008 12 5 MWEA080133 1 20081121 A 5320 59107845 CHANNEL BOEING 717 717200 1383700 NM FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 926ME 55192 LT MLG DOOR JAMB FWD CHANNEL HAS A .5 INCH CRACK. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F TR A6WE 20081205 NM 2008 12 5 ASAA0843937 1 20081003 A 5753 6546430189 SKIN BOEING 737 7374Q8 138447Q NM LT FOREFLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 LT INBD FOREFLAP HAS 2 DENTS 18 INCHES FROM OTBD EDGE ON UPPER CAMBER. PREPPED DAMAGED AREA FABRICATED DOUBLER AND BOND ED THE REPAIR IAW SRM 51-70-10 REP 2. 2 L 7 2 4F RT A16WE 20081205 EA 2008 12 5 SWIA200820516 1 20080914 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 964SW 7868 DURING C-CHECK, AFT PRESSURE BULKHEAD CRACKED AT FITTING UPPER INBOARD CORNER. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820517 1 20080914 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 964SW 7868 DURING C-CHECK, FS 280 LOWER FLOORBEAM CRACKED AT RBL 12. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820519 1 20080914 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 964SW 7868 DURING C-CHECK, FS 280 UPPER FLOORBEAM ANGLE CRACKED AT RBL 10 AND LBL 11. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820520 1 20080914 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 964SW 7868 DURING C-CHECK, RIGHT ENGINE THRUST MOUNT CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 COMA2008112450006 1 20081123 A 2750 965D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 814CA 30655 7387 RECEIVED FLAP FAIL MSG, WHEN SELECTING FLAPS TO 8 DEG AT 200 KNOTS. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED FLAP SYSTEM PDU. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 ASAA0873899 1 20081126 A 5320 111A11411 VAPOR BARRIER BOEING 737 737790 13844CN NM BS 663 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 6 INCH CRACK FOUND AT LBL 10.5 ON FWD LT VAPOR BARRIER. REPAIRED LT VAPOR BARRIER. 2 L 7 2 4F RT A16WE 20081205 EA 2008 12 5 COMA2008120150011 1 20081126 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 27 819CA 2587 7415 RECEIVED GEAR DISAGREE MSG, NOSE GEAR DID NOT LOCK DOWN. EMERGENCY DECLARED, QRH FOLLOWED. A/C LANDED SAFELY. REMOVED AND REPLACED NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 PNSA110804 2 20081121 A 7314 LW15473 PUMP PIPER PA32 PA32301 7103207 SO LYC O540 IO540K1G5 41532 EA ENGINE FAILED E PNSA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 AL 03 8259V 2078 2078 328006097 AFTER TAKEOFF PILOT SHUT THE FUEL BOOST PUMP (ELECTRIC) AND NOTICED AN IMMEDIATE FUEL FLOW REDUCTION, AND ENGINE BEGAN T O SHUT DOWN. PILOT TURNED BOOST PUMP BACK ON AND POWER WAS RESTORED FULLY. PILOT MADE A UNEVENTFUL LANDING AT THE DEPA RTURE AIRPORT. MAINTENANCE FOUND THE MECHANICAL ENGINE DRIVEN FUEL PUMP HAD FAILED. PUMP WAS REPLACED AND SYSTEM OPERA TED NORMALLY. 1 L 7 1 3O 3 O A3SO 1E4 20081205 NM 2008 12 5 CALA2008112401098 1 20081124 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14652 28913 AIR CONDITIONING SUPPORT BRACKET ATTACHED TO THE FRAME BETWEEN STRINGERS 8 & AMP; 9 CRACKED AROUND RIVET STA 747L. FABR ICATED AND INSTALLED REPAIR DOUBLERS PER ECRA 5310-04498. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 NWAA085106305 1 20081115 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 665US 23820 DURING OVERNIGHT CHECK FOUND UPPER DECK EMERGENCY EXIT SIGN OVER RT EMERGENCY EXIT DOOR IS INOP. MX R&R POWER SUPPLY AN D BATTERY PACK. OPS CHECKED GOOD AND ACFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20081205 2008 12 5 NWAA085043358 4 20081109 A 4500 PRINTER AIRBUS A330 A330223 3930374 EU COCKPIT FAILED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 858NW 22717 14319 00718 PRINTER FAILED AND SMOKE CAME FROM PRINTER, TURNED OFF PRINTER AND SMOKE STOPPED. PRINTER REPLACED AND TEST NORMAL. 2 L 7 2 4F RT A46NM 20081205 WP 2008 12 5 NWAA085039870 1 20081108 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 779NC 48101 DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 2 L 7 2 4F RT A6WE 20081205 2008 12 5 UALA2008112406639 4 20081123 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 DOOR 1R, HAS LANYARD HANGING FROM DOOR SLIDE. RE-INSTALLED LANYARD INTO SLIDE PACK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081205 NM 2008 12 5 WRLA2008094 1 20081124 A 5320 WEB DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHK + 4C CHK, EGAT MECH FOUND FWD CARGO COMP LONGERON L43L SUPPORT WEB CRACKED AT STA 6-60. REPAIRED CRAC K IAW ENGINEERING INSTRUCTION W2008A53B-1314 REV 00 AND EI NO W2008A53B-1314 REV 01. 2 L 7 3 4F RT A22WE 20081205 2008 12 5 ASOA200801576 4 20081126 A 3400 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA MULTIPLE FAIL A ASOA O OTHER G MULTIPLE FAILURE CR CRUISE 1 SO 27 875AS 7559 FLT 4999 - RADIO ALTIMETER FAULT FOLLOWED BY GPWS FAIL, WINDSHEAR FAIL, TCAS FAIL, SPOILERONS FAULT, FLT SPOILERS FAULT, OTBD GND SPOILERS FAULT, INBD GND SPOILERS FAULT, EMERGENCY VEHICLES ROLLED AS A PRECAUTION. 2 L 7 2 4F RT A21EA 20081205 EU 2008 12 5 UALA2008112406646 1 20081121 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 403UA 442 LT DOOR SILL HAS SEVERAL AREAS OF CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED SILL SHAPE FROM SILL PLATE AT DOOR 2L. INSTALLED NEW SILL SHAPE ON SILL PLATE. NEEDS 2 FASTNERS DRILLED AND INSTALLED ON SHAPE. REPLACED 3 FASTENE RS ON SILL SHAPE. REMOVED CORROSION ON SILL PLATE, PRIMED AND PAINTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081205 EA 2008 12 5 ASOA200801577 1 20081128 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 853AS 7374 HAD ELECTRIC BURNING ODOR IN FLIGHT (ATL-SRY). DIVERTED INTO KCRW UPON LANDING F/A TOLD US THE INDICATOR LIGHTS FOR THE POT-WATER WERE OFF AND COFFEE POT WAS INOP. CAPTAINS MFD FLICKERED 3 TIMES IN FLIGHT. ENROUTE TO SYR A/C DIVERTED TO CRW DUE TO MTC, EMERGENCY DECLARED. POTABLE WATER SYSTEMS, LAVATORY POTABLE WATER CONSIDERED INOPERATIVE AND SINK PLACA RED. 2 L 7 2 4F RT A21EA 20081205 EU 2008 12 5 UALA2008112406647 1 20081122 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 403UA 442 FLOORBEAM 200 HAS TWO SMALL SPOTS OF CORROSION (MARKED). MAJOR REPAIR ACCOMPLISHED. STARTED REPLACING BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081205 NM 2008 12 5 HALA2008112600876 1 20081126 A 5512 SKIN BOEING 767 76733A 1385209 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 582HA 28139 11 AREAS OF LEVEL 11 CORROSION, ON HORIZONTAL STABILIZER UPPER SURFACE OF CENTER SECTION SKIN. REWORKED IAW AIRNZ TI 19 0120092-0001. 2 L 7 2 4F RT A1NM 20081205 EA 2008 12 5 ASOA200801578 1 20081129 A 2560 BATTERY CNDAIR CL600 CL6002C10 1390015 EA MEGAPHONE UNKNOWN A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 708EV 10060 MEGAPHONE NEEDS BATTERIES. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 ASOA200801579 1 20081129 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 841AS 7300 CAPT FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 ASOA200801581 1 20081129 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 FLT 5311 - EXIT PLACARD MISSING ON PAX ENTRY DOOR. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 ASOA200801582 1 20081129 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 821AS 7194 ASD TOP STEP BROKEN. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 FDEA200810294604 1 20081029 A 5315 65863561 FLOORBEAM BOEING 727 7272D4 138407U NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 UPPER LOBE INTERIOR STATION 804 LBL68" FLOORBEAM LOWER CHORD CORRODED. REMOVED CORROSION OVER 50 PERCENT MATERIAL LOSS OUT OF LIMITS REF SRM 53-10-1 FIG 1. REMOVED AND REPLACED BEAM LOWER CHORD REF SRM 51-30-2 P8. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081205 NM 2008 12 5 FDEA200811044697 1 20081104 A 5310 65595341 BEAM BOEING 727 7272D4 138407U NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 LWR FUSELAGE DELTA BEAM LT LWR CHORD IS CRACKED ON LWR INBD FLANGE AT BS 740 TO 743 LBL 6 INCHES. REMOVED DAMAGE, NDT T RIMMED EDGES, MADE INSURANCE CUT, FABRICATED REPAIR ANGLE AND FILLER, FABRICATED ONE T-CLIP, FABRICATED INTERCOSTAL, ALO DINED AND PRIMED AND INSTALLED ALL PARTS, REF FED EX EA 7- 5310-123817. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081205 EA 2008 12 5 ASOA200801569 1 20081126 A 2560 BATTERY CNDAIR CL600 CL6002B19 1900309 EA FLASHLIGHT UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 681BR 7680 CAPTAINS FLASHLIGHT NEEDS BATTERIES. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 WRLA2008096 1 20081124 A 5712 RIB DOUG MD11 MD11F 3023600 NM LT WING CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 CRACK- DURING BRIDGE CHECK + C4 CHECK, EGAT MECH FOUND LT WING FIXED L/E RIB CRACK ON FUELING PANEL OTBD LOWER SIDE AT X ORS=538. REPAIRED CRACK AREA IAW ENGINEERING INSTRUCTION W2008A57B-1290 AND EI W2008A57B-1290 REV 01. 2 L 7 3 4F RT A22WE 20081205 EA 2008 12 5 ASOA200801570 1 20081124 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 TWO CRACKS ON INNER SKIN AT PAX DOOR HANDLE. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 ASOA200801571 1 20081125 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA WING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 INDICATION NOTED AT LOWER WING PLANK ACCESS HOLE 640CB WHILE PERFORMING ASA TASK NR 000-57-900-610 AFT SIDE OF HOLE. IN DICATION APPEARS TO BE CORROSION APPROX .040 IN DEPTH. INDICATION IS MAPED IN AIRCRAFT. REMOVED DAMAGE AT RT LOWER WIN G PLANK ACCESS HOLE 640CB IAW REO 601R-57-21-1033. ASA EC/TC NEEDS C/W. C/W EC/TC REO 601R-57-21-1033 IAW REO 601R-57- 21-1033. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 HALA2008112200867 1 20081122 A 3010 32157341 VALVE BOEING 717 717200 1383700 NM WING UNKNOWN A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 478HA 55123 WING MANIFOLD FAIL LIGHT CAME ON FOR 5 SEC THEN DISAPPEARED. REMOVED AND REPLACED WING PRESSURE REGULATOR AND SHUTOFF V ALVE PER AMM 30-11-01. LEAK AND OPS CHECK GOOD. 2 L 7 2 4F TR A6WE 20081205 NM 2008 12 5 UALA2008112406657 1 20081123 A 2497 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GENERATOR DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 643UA 25093 APU GENERATOR TRIPPED OFF. FLIGHT CANCELLED. APU GENERATOR TRIPPED OFF AND WILL NOT RESET. SEE PREVIOUS FOR FAULT "GE N DIODE". THE GEN HAS ALREADY BEEN REPLACED RECENTLY FOR THE SAME PROBLEM AND "GEN DIODE" WAS THE FAULT REPORTED BY AMS MM. ALSO AMSMM REPORTED INTERMITTENT "FIELD OFF" LIGHT WHEN SHAKING WIRES FROM FIREWALL TO GEN. 2 L 7 2 4F 4 F RT A1NM E24NE 20081205 NM 2008 12 5 UALA2008112406658 1 20081122 A 2150 8102044 CONTROL VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT AC PACK FAULTY A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 780UA 26944 LOSS OF RIGHT PACK. FLIGHT DIVERTED. REPLACED RIGHT PACK LOWER FLOW CONTROL VALVE. ACP AIR ON TESTS ON MAT. ALL OPS CHECK SATISFACTORILY. MSGS NOT ACTIVE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081205 2008 12 5 UALA2008112406629 4 20081122 A 3140 S242N701603 DISPLAY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EICAS FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 663UA 27160 LOSING UPPER EICAS DISPLAY INTERMITTENT NO COLOR AND DISPLAY MSG. REPLACED UPPER EICAS DISPLAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081205 EU 2008 12 5 UALA2008112406632 1 20081123 A 5320 PLATE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 403UA 442 PLATE UNDER SHEAR PLATE LOCATED BETWEEN FRAME 69 AND 70 RIGHT SIDE OF AIRCRAFT CORRODED. REMOVED PLATE AND FWD ATTACH A NGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081205 WP 2008 12 5 AALA200810266 1 20081110 A 5320 DIAPHRAGM DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION ON SUBFLOOR DIAPHRAM. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081205 WP 2008 12 5 AALA200810267 1 20081110 A 5310 BEAM DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 LOWER DOOR BEAM CORRODED FROM STATION 1162 TO STATION 1207 ON BOTH VERTICAL AND HORIZONTAL LEGS. INSTALLED REPAIR DOUBL ER PER AARD 53-10-00-03. 2 L 7 2 4F RT A6WE 20081205 NM 2008 12 5 AALA200820053 1 20081106 A 5320 146N56601 FLOOR SUPPORT BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 666A 52891 25300 FLOORBOARD SUPPORT CORRODED, REPAIRED IAW SRM 53-60-51-2R1. 2 L 7 2 4F RT A2NM 20081205 WP 2008 12 5 AALA200810249 1 20081104 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 FORWARD ENTRY DOOR AFT DOOR JAM WEB CRACKED AT L15 STATION 209. INSTALLED 3 INCH BY 6 INCH T SHAPED DOUBLER OF .040 707 5 T6 PER AARD 53-10-00-11. 2 L 7 2 4F RT A6WE 20081205 NM 2008 12 5 AALA200820051 1 20081105 A 5315 146N509131 FLOORBEAM BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 666A 52891 25300 FLOORBEAM CORRODED, REPAIRED IAW AARD 53-60-51-5. 2 L 7 2 4F RT A2NM 20081205 NM 2008 12 5 ASAA0843926 1 20081029 A 5311 65465553 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED STA 867 STR 8 9L. CUTOUT DAMAGE FABRICATED AND INSTALLED REPAIR ANGLES AND FILLER IAW ASA EA 400 53EA 002 67. 2 L 7 2 4F RT A16WE 20081205 EA 2008 12 5 ASOA200801557 1 20081106 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 WHILE PERFORMING FS 559 BULKHEAD INSPECTION, AN INDICATION WAS NOTED APPROX .500 INCH OTBD OF RBL 9, WL 58.70 APPROX .25 0 IN LENGTH VERTICALLY. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 ASOA200801583 1 20081130 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR TORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 EXIT STICKER ON PAX DOOR TORN. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 COMA2008120150012 1 20081128 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 27 408CA 7440 ON APPROACH INTO BOS, RECEIVED FLAPS FAIL CAUTION MSG. FLAPS FAILED AT 0 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW UP MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 COMA2008120150013 1 20081130 A 3020 SENSING ELEMENT CNDAIR CL600 CL6002B19 1900309 EA ENGINE OUT OF POSITION A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 916CA 7014 EN ROUTE FROM RDU TO BOS, RECEIVED A/I DUCT WARNING MSG. A/C DIVERTED TO ORF, LANDED SAFELY. INSPECTED A/C, FOUND SENS ING ELEMENT RESTING ON FLANGE FOR 14TH STAGE BLEED DUCT. REPOSITIONED SENSING ELEMENT. SYSTEM OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 WRLA2008098 1 20081124 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHK + 4C CHK, EGAT MECH FOUND MAIN DECK SEAT TRACK CRACK AT STA 635 AND STR LBL 40. REPAIRED SEAT TRACK A REA PER MD-11F SRM VOL 1 51-21-01 REV 40. 2 L 7 3 4F RT A22WE 20081205 NM 2008 12 5 WRLA2008099 1 20081124 A 5320 STANCHION DOUG MD11 MD11F 3023600 NM FWD CARGO BAY CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHK + 4C CHK, EGAT MECH FOUND FWD CARGO STA 6-73 STANCHION LWR END HAD CORROSION. REPAIRED CRACK AREA IAW ENGINEERING INSTRUCTION W2008A53B-1305 REV 00 AND EI W2008A53B-1305 REV 01, INSTALLED REPAIR STANCHION PER SRM VOL 2 51 -35-01 REV 40. 2 L 7 3 4F RT A22WE 20081205 NM 2008 12 5 WRLA2008097 1 20081124 A 5720 ANGLE DOUG MD11 MD11F 3023600 NM LT WING CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHECK + 4C CHECK, EGAT MECH FOUND ANGLE OF LT WING FIXED L/E CRACK AT STA XORS=488. REPAIRED CRACK AREA I AW ENGINEERING INSTRUCTION W2008A57B-1301 REV 00 AND EI W2008A57B-1301 REV 01. 2 L 7 3 4F RT A22WE 20081205 NM 2008 12 5 UALA2008112506663 1 20081124 A 2421 GENERATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 643UA 25093 APU GENERATOR TRIPPED OFF AND WILL NOT RESET. 2 L 7 2 4F 4 F RT A1NM E24NE 20081208 EA 2008 12 8 ASOA200801526 1 20081117 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 713EV LT BS 280 WEB HAS SURFACE CORROSION ON AFT LOWER WEB. REMOVED AND REPLACED BS 280 LT WEB REFER TO M-234 FORM FOR WORK A CCOMPLISHED. 2 L 7 2 4F RT A21EA 20081208 NM 2008 12 8 KCSA081560AA 1 20081120 A 5320 BEAM BOEING 747 747212B 1384886 NM BS 1480 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 STA 1480 BL 0 WL 187 PRESSURE DECK BEAM CORRODED. 2 L 7 4 4F RT A20WE 20081208 EA 2008 12 8 A6WA200840600 1 20081021 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 447AW 7812 AFT PRESSURE BULKHEAD WEB AT FS 621.00 AT THE LINTEL INSTALLATION IS CRACKED. AFT PRESSURE BULKHEAD WEB AT FS 621.00 LIN TEL INSTALLATION REPAIRED IAW CRJ 200 REO 601R-53-61-1230 REV D. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 A6WA200840601 1 20081020 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 412AW 7582 AFT PRESSURE BLKHD WEB AT FS 621.00 AT THE LINTEL INSTALLATION AREA IS CRACKED. REPAIRED IAW REO 601R53-61-1230 REV D. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 A6WA200840598 1 20081022 A 4920 APU CNDAIR CL600 CL6002B19 1900309 EA FAULTY A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 31 441AW 7777 SMOKE IN FLIGHT DECK AFTER LANDING. SMOKE DISSIPATED AFTER PACKS SELECTED OFF. OPERATED BOTH PACKS ON APU AIR AND DETE RMINED APU TO BE CONTAMINATING PACKS WITH OIL ODOR . 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 A6WA200840603 1 20081031 A 2910 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA LT SPOILER LEAKING A A6WA K NONE K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 401AW 7280 RECEIVED HYDRAULIC 2 LOW PRESSURE WARNING MSG ON GROUND. COMPLIED WITH QRH. ENGINE DRIVEN PUMP 2A RAN 2 MINUTES WITH Q UANTITY ZERO. NOTED TEMPERATURE OF 46C. R&R LT OTBD SPOILER HOSE ASSEMBLY AND LT INBD SPOILER RETRACT HOSE ASSEMBLY IA W 51-10. R&R HYD NR 2 SYSTEM PRESSURE AND RETURN FILTER IAW 29-11. LEAK AND OPS CHECK GOOD. SERVICED NR 2 SYSTEM. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 A6WA200840599 1 20081029 A 3310 LIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A A6WA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 463AW 7878 SMOKE IN COCKPIT WHEN FO TURNED FLOODLIGHT ON. TURNED OFF FLOODLIGHT AND SMOKE WENT AWAY. 2 L 7 2 4F RT A21EA 20081208 SW 2008 12 8 ZESA2008009 1 20080613 A 6520 GEARBOX BELL 407 407 1182206 SW TAIL ROTOR MAKING METAL E ZESA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 03 70AP 53409 DURING FLIGHT, TAIL ROTOR CHIP LIGHT ILLUMINATED. THE PILOT LANDED ASAP AND COMPLIED WITH LJ AVIATION SOP BY REMOVING A ND INSPECTING CHIP DETECTOR. FOUND SMALL HAIRLIKE SLIVER. CLEANED AND REINSTALLED CHIP DETECTOR WITH NEW O-RINGS, GROU ND RUN PERFORMED SATISFACTORILY. 1 G 7 1 3U O H2SW 20081208 WP 2008 12 8 NWAA085059852 1 20081112 A 5321 FLOOR PANEL DOUG DC9 DC951 3022051 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 761NC 47709 DURING H CHECK FOUND CRACK ON THE EDGE OF FLOOR PANEL NR 18 AND 4 STIFFENERS. REPAIRED PER EA 98-213662. 2 L 7 2 4F RT A6WE 20081208 NM 2008 12 8 SWAA086809 1 20081203 A 5311 6547959 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME PER SR M. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086778 1 20081203 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT RADIO ALTIMETER SKIN CUTOUT, BS 410. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081208 EU 2008 12 8 MALA080204 1 20081117 A 5310 FRAME SAAB SF340 340B 7860101 EU BS 294 CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 340B433 TOP FRAME, WHERE AIR STAIR SLIDES HAS TWO DEEP CHAFES AT STA 294. REPAIRED IAW EO NR S53362. 2 L 7 2 4T RT A52EU 20081208 EU 2008 12 8 MALA080205 1 20081116 A 5100 PANEL SAAB SF340 340B 7860101 EU UNKNOWN DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 340B433 PANEL 193AL HAS COMPOSITE DAMAGE. REPAIRED IAW EO NR S51031. 2 L 7 2 4T RT A52EU 20081208 NM 2008 12 8 UIEA200800342 1 20081121 A 5730 PANEL BOEING 747 7472D7B 1384803 NM ZONE 100 DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 RT WING PREVIOUS REPAIR ON UPPER WING SURFACE L/E PANEL AN AREA OF 6.0 BY 38.0 INCHES IS DELAMINATED AT ILES 522.06 AND 7.5 INCHES FROM PANEL FRONT EDGE. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18, SHEETS 2, 5 AND SR M 51-40-12. REF. ATLAS AIR EO 4757A467. 2 L 7 4 4F RT A20WE 20081208 NM 2008 12 8 HALA2008112100866 1 20081121 A 3610 MS289343 SENSOR BOEING 767 76733A 1385209 NM AIR TEMP MALFUNCTIONED A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, APU FAULT LIGHT AND AUTO SHUTDOWN AT FL 340. RESTART AND RAN OK AT FL 300 PRIOR TO AUTO SHUTD OWN, APU DID START AND RUN FOR APPROX 10 MIN AT FL 340. PERFORMED FIM 49-11-00, NO DEFECTS NOTED. PRECAUTIONARY REPLAC ED AIR TEMP SENSOR PER AMM49-94-01. OPS CK LEAK CK OK. WIRING CHECKED ON PINS E4 AND E5 AND PINS A AND B NORMAL AT ECU CONNECTOR D408B. 2 L 7 2 4F RT A1NM 20081208 NM 2008 12 8 WRLA2008101 1 20081124 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 1721 L44L CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA DURING BRIDGE CHK + 4C CHECK, EGAT MECH FOUND LONGERON BASE CORRODED AT CENTER CARGO STA 1721 AND STR 44L. REMOVED CORR ODED LONGERON SECTION, MANUFACTURED REPAIR PARTS PER SRM VOL 1 53-10-00 REV 40 AND REPAIRED DAMAGED AREA PER SRM VOL 1 5 3-10-00 REV 40. 2 L 7 3 4F RT A22WE 20081208 NM 2008 12 8 SWAA086813 1 20081203 A 5311 6546541 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 663, STR 3R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086814 1 20081203 A 3350 101114 LIGHT BOEING 737 737317 138447P NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND FWD LAV AFT WALL EMERGENCY EXIT LIGHT ASSY CRACKED. REMOVED AND REPLACED LIGHT ASSY P ER MM. 2 L 7 2 4F RT A16WE 20081020 WP 2008 10 20 ABXA080239 1 20080909 A 3350 60030451 POWER SUPPLY DOUG DC9 DC941 302207N WP EMERGENCY LIGHTS DEFECTIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 970AX 1183 47494 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW DC9 MM CHAPTER 33. 2 L 7 2 4F A6WE 20081020 EA 2008 10 20 COMA0860392 1 20080916 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 940CA 35923 7048 FLIGHT NR 6274 ON T/O FROM CVG RECEIVED NOSE GEAR DISAGREE MSG. EMERGENCY DECLARED. A/C RETURNED BACK TO CVG AND LANDE D SAFELY. R&R NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 20081020 WP 2008 10 20 AALA200802280 1 20080906 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7540A 49994 MSP EMERGENCY LIGHT AT SEAT ROW 25 HAS BROKEN LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 25. SYSTEM GROUND CH ECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081020 NM 2008 10 20 AALA200802307 1 20080908 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 912AN 29513 TPA EMERGENCY LIGHT AT SEAT 7D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMA L OPS. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 F3LA200800615 1 20080919 A 5320 D5348004320600 SILL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 930FR 31 2241 REFERENCE NON ROUTINE CO51321. DURING C3 C CHECK INSPECTION NOTED THE L2 DOOR SILL AFT OTBD NUT PLATE HOLE WAS CORRODED . MX CUT CORRODED AREA OUT OF THE SILL WEB, FABRICATED REPAIR FILLER AND INSTALLED REPAIR IN ACCORDANCE WITH THE REQUIR EMENTS OF A319 SRM 51-73-00, 51-42-11 AND ENGINEERING AUTHORIZATION EA NR A9-53R-30617. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 2008 10 20 AALA2008022979 4 20080907 A 3417 ADC AIRBUS 300 A300B4605R 3930308 EU NR 2 FAILED A AALA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SW 21 50051 459 MIA INFLIGHT T937/07SEP. CREW REPORTED FIRST OFFICERS AIRSPEED STOPPED ACCELERATING AFTER TAKE OFF. BOTH CAPTAIN AND F IRST OFFICERS AIRSPEED FAILED TO ACCELERATE IN STANDBY. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 2 AIR DATA COMPUTER. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A35EU 20081020 WP 2008 10 20 AALA200802287 1 20080906 A 3397 CONTACT DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 290AA 49302 LGA EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 23 TO 30 INOPERATIVE. CLEANED AND ADJUSTED CONTACT AT ROW 28 FOR EMERGENCY L IGHTS AT OVERHEAD SEAT ROWS 23 TO 30. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081020 EA 2008 10 20 QXEA200800684 1 20080612 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 675-713 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK NUMEROUS CORROSION SPOTS ON LT SIDE SEAT RAIL FS 675 TO 713. REMOVED CORROSION FROM SEAT TRACK AT FS 675 T O 713. .010 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013 AND CRJ SRM 51-21-16. 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 COMA0860393 1 20080919 A 5311 6013600129 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 640 S10-11L CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 430CA 7461 LT FS640 FRAME DOUBLER CRACKED BETWEEN STR 10L AND 11L. C/W MOD K601R36009-3 ON LT FS640 IAW S/B601R 53-061 KIT DRWG. K601R36009 REV B. 2 L 7 2 4F RT A21EA 20081020 NM 2008 10 20 F3LA200800612 1 20080919 A 5320 D5348004220601 SCUFF PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 930FR 31 2241 REFERENCE NON ROUTINE C051324. DURING C3 C CHECK, INSPECTION NOTED THE L2 DOOR AFT OTBD SCUFF PLATE SUPPORT ATTACHMENT HAD A CORRODED FASTENER. MX REMOVED CORNER ANGLE, OVERSIZED 3 HOLES, FABRICATED 3 FREEZE PLUGS, INSTALLED CORNER ANGLE AND NEW SCUFF PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF ENGINEERING AUTHORIZATION EA NR A9-53R-30632 AND A319 SRM 51- 42-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 AALA200802304 1 20080907 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 794AN 30256 MIA EMERGENCY LIGHT AT OVERHEAD SEAT 22G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 22G. SYSTEM G ROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081020 SO 2008 10 20 SIMA200826606 1 20080917 A 5310 14532638401 BEAM EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 837AE 145647 DURING MBV INSPECTION THE CENTER BEAM AT FRAME 25 WAS FOUND CORRODED. DAMAGE WAS CUT OUT. FABRICATED A REPAIR DOUBLE A L2024T3 .071 FILLER AND 2 SHIMS. DRILLED, CLEANED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS IAW EMB SRM 51-00-10. ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081020 NM 2008 10 20 F3LA200800637 1 20080928 A 5320 D5347112420100 SHEAR PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON SHEAR PLATE LOCATED AT FRAME 69 TO FRAME 70 ON THE RIGHT SIDE OF THE PASSENGER CABIN. MX REMOVED AND REPLACED THE SHEAR PLATE IAW THE REQUIREMENTS OF A319 SRM 51-72-11. UPON COMPLETION O F THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800618 1 20080911 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 930FR 31 2241 REFERENCE NON ROUTINE CO51286. DURING C3 C CHECK, INSPECTION NOTED FLOOR PANEL 262FF HAD CORROSION ON AFT BOTTOM SURFAC E. MX REMOVED FLOOR PANEL AND INSTALLED NEW IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-12-400-002. UPON COM PLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 AALA200802291 1 20080906 A 3350 LIGHT BOEING 757 757223 1384957 NM SEAT 23D BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 693AA 26973 DFW EMERGENCY LIGHT AT SEAT 23D BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081020 EA 2008 10 20 HNAA0800292 1 20080917 A 2910 39671 CONTROL VALVE DHAV DHC8 DHC8311 1386006 EA HYD SYSTEM BROKEN A HNAA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 07 327EN 29897 261 NR 1 HYDRAULIC QTY DROPPED TO 1 QUART FOLLOWED BY ISO VALVE CAUTION LIGHT ILLUMINATED. LOST NORMAL BRAKES. R&R NR 2 AN TI-SKID CONTROL VALVE. IAW 32-46-11. LEAK CHECK AND OPS CHECKS GOOD. SERVICED HYDRAULIC SYSTEMS AND RETURNED ACFT TO SERVICE. 2 H 7 2 4T RT A13NM 20081020 NM 2008 10 20 AALA200802305 1 20080907 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 794AN 30256 MIA EMERGENCY LIGHT AT SEAT 33G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 33G. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081020 SO 2008 10 20 C2XA08RI139 1 20080909 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14920 145380 FLIGHT 2516 EWR FLIGHT CREW REPORTED FORWARD EMERGENCY LIGHTS VERY DIM AND STAYS ON WHILE SWITCH IS IN OFF POSITION. EW R MX R&R EMERGENCY LIGHT BATTERY NR 2 AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081020 NM 2008 10 20 F3LA200800613 1 20080918 A 5320 D5348004320600 SILL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 930FR 31 2241 DURING C3 C-CHECK, INSPECTION NOTED THE L2 FORWARD GIRT BAR ATTACH FITTING, AFT INBOARD HOLE HAD CORROSION. MX CUT CORR ODED AREA OUT OF THE SILL WEB, FABRICATED REPAIR FILLER AND INSTALLED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-41-14, 51-75-12 AND ENGINEERING AUTHORIZATION EA NR A9-53R-30629. UPON COMPLETION OF THE REPAIR, IT WAS INSPECT ED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 WP 2008 10 20 UPS08853504 1 20080922 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:CV EVALUATION AND DISPOSITION REPAIR SURVEY SEQUENCE NR: 894-W4-09. RIGHT UPPER LEADING EDGE DOUBLER RE PAIR STA XFS 512 MISSING 8 EACH FA FASTENERS. INSTALLED FASTENERS IAW DC-8 SRM 51-03-00. 2 L 7 4 4F RT 4A25 20081020 NM 2008 10 20 ASAA0843584 1 20080914 A 5320 65C333671 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 947-967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 AFT CABIN FLOOR INTERCOSTAL CORRODED AT STA 947 AT LBL 40. REMOVED DAMAGED INTERCOSTAL LOCATED DRILLED INSTALLED A REPL ACEMENT INTERCOSTAL IAW B737 400 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0843586 1 20080912 A 5322 65465349 SHEAR TIE BOEING 737 7374Q8 138447Q NM BS 520 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 FWD CARGO BAY SHEAR TIE CORRODED AT STA 520 BETWEEN STA 28R AND 28L. REMOVED DAMAGED SHEAR TIE, FABRICATED, LOCATED, DR ILLED AND INSTALLED REPLACEMENT SHEAR TIE IAW B737 400 SRM 51 40 02 PG 2 4 AND DRW 65 46534. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0843566 1 20080907 A 5330 65529888 SKIN BOEING 737 7374Q8 138447Q NM BS 989-1016 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 SKIN CREASE ON FWD SIDE OF STA 1016 1.5 INCHES ABOVE STR 13L. REMOVED DAMAGED SKIN PANEL PREPARED AND BONDED DOUBLER TO NEW SKIN LOCATED DRILLED AND INSTALLED NEW PANEL IAW SRM 51-70-10 & 51-40-02. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0843576 1 20081003 A 5512 SKIN BOEING 737 7374Q8 138447Q NM HORIZONTAL STAB GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 LEFT HORIZONTAL STABILIZER LEADING EDGE EXTERNAL SKIN IS GOUGED 92 INCHES FROM I/B. REPAIRED GOUGE IAW SRM 55-10-01. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0843579 1 20080923 A 5522 65C25746142 SKIN BOEING 737 7374Q8 138447Q NM RT ELEVATOR PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 RIGHT ELEVATOR UPPER SURFACE SMALL PUNCTURE 6 INCHES FROM TRAILING EDGE AND 4 FEET FROM I/B END. PREPARED REPAIR AREA, APPLIED RESIN AND BONDED TWO LAYERS OF GRAPHITE CLOTH IAW B737 400 SRM 51 70 03 REPAIR 2. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0843561 1 20080911 A 5755 SKIN BOEING 737 7374Q8 138447Q NM NR 2 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS MA15290 25101 LEFT WING NR 2 SPOILER DENTED ON UPPER SURFACE 12 INCHES FROM O/B END. PREPARED DAMAGED AREA, FABRICATED DOUBLER AND BO NDED IAW 737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0843570 1 20080912 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 9 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 RIGHT WING NR 9 SPOILER UPPER SURFACE 2 DENTS CLOSE TOGETHER. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER BONDED I AW SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0843571 1 20080911 A 5753 65C2631187 SKIN BOEING 737 7374Q8 138447Q NM LT WING TE FLAP WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 LEFT WING INBOARD AFT FLAP EXHAUST GATE WORN ON UPPER SURFACE. REMOVED DAMAGED UPPER PANEL, LOCATED, DRILLED AND INSTAL LED A REPLACEMENT UPPER PANEL IAW B737 400 SRM 51 40 02 51 40 05. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0843577 1 20080911 A 5753 6546434335 SKIN BOEING 737 7374Q8 138447Q NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 LEFT WING I/B AFT FLAP UPPER SURFACE AREAS OF DENTS. PREPARED DAMAGED AREA, FABRICATED DOUBLERS, TREATED, REPAIRED AND BONDED IAW SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0843580 1 20080911 A 5755 65464552584 SKIN BOEING 737 7374Q8 138447Q NM NR 5 SPOILER DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 RIGHT WING NR 5 SPOILER LOWER SURFACE DAMAGED. PREPARED DAMAGED AREA, FABRICATED REPAIR PARTS AND BONDED DOUBLERS IAW B 737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0853587 1 20081007 A 7720 TC29604 PROBE BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27B3 13054 NE NR 1 ENGINE MALFUNCTIONED A ASAA K NONE N FALSE WARNING IN INSP/MAINT 1 NM 02 583AS 35681 894763 GE DIAGNOSTICS REPORTS NR 1 ENGINE CRUISE DELTA EGT SHOWS GREATER THAN NORMAL SCATTER AND MOVEMENT. EGT INDICTION IS SU SPECT: PRI: 1 PERFORMED EGT PROBES CLEANING PER MM 77 21 00 201 PINS AND SOCKETS TENSION CHECKED NORMAL. VALUES S1 S4 PR E 205 176 176 214 POST 130 83 83 142 DURING RUN AFTER 3 MIN 380 430 415 410. NO FAULTS LOGGED. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081020 CE 2008 10 20 26N2008F00004 1 20080929 A 2710 70611107 SELECTOR CESSNA 510 510 2076617 CE AILERONS FROZEN E 26NA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 EA 05 83EM 5100026 ACFT FLIGHT CONTROLS FROZE AT ALTITUDE ENROUTE. THIS IS THE SECOND SITUATION WHERE THIS CONDITION HAS HAPPENED TO THIS A CFT. ACFT PREVIOUS REGISTRATION N1693L. A TECH WAS WITH THE ACFT. INSPECTED AREAS OF PREVIOUS CONCERN AND SERVICE PREVI OUSLY WORKED BY MFG, DRIED AFFECTED AREA AND ACFT REPOSITIONED FOR EVALUATION AND RESOLUTION. (K) 1 L 7 2 4F RT A00014WI 20081020 CE 2008 10 20 DXTA200803270 1 20080910 A 2720 WARNING LIGHT BEECH MU300 400A 1155402 CE RUDDER ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 117QS RK391 ON TAKEOFF ROLL BELOW 80 KTS AT TAKEOFF POWER, RUDDER BOOST FAIL ANNUNCIATOR LIGHT COMES ON. ABORTED TAKEOFF. (K) 2 H 7 2 4F RT A16SW 20081020 NM 2008 10 20 F3LA200800610 1 20080916 A 5320 D5347112420100 SHEAR PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 930FR 31 2241 REFERENCE NOT ROUTINE C051378. DURING C3 C-CHECK, INSP NOTED THE RT SHEAR PLATE FROM FR 69 TO FRAME 70 WAS CORRODED. MA INT REMOVED AND REPLACED SHEAR PLATE ASSY AND SUPPORT FRAME IAW THE REQUIREMENTS OF A319, SRM 51-42-11, PARA 6 AND 7. U PON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (K) 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 UPS08M53532 1 20080516 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A RT WING O/B FLAP I/B AFT HINGE O/B PIVOT BORE CORRODED. RT WING O/B FLAP I/B AFT HINGE O/B PIVOT BO RE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-52-04 REV 61. 2 L 7 3 4F RT A22WE 20081020 EA 2008 10 20 SWIA200820130 1 20080510 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA AFT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 417SW 7400 REAR PRESSURE BULKHEAD WEB HAS .5 INCH CRACK (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 SWIA200820132 1 20080510 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA AFT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 417SW 7400 REAR PRESSURE BULKHEAD WEB HAS .5 INCH CRACK (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081208 2008 12 8 SIMA200833601 2 20081125 A 7261 OIL SYSTEM EMB 135 EMB135KL 3260302 SO LT ENGINE OVERSERVICED A SIMA O OTHER W K B INADEQUATE Q C FLUID LOSS SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 21 807AE 145506 FLIGHT 3115, DURING DESCENT CREW REPORTED BURNING ODOR AND SMOKE IN THE COCKPIT. AIRCRAFT REMOVED FROM SERVICE. PERFO RMED EMB 140 FIM 21-20-00-810-801-A AND FIM 21-20-00-810-803-A. FOUND OIL OVERSERVICED AT LT ENGINE. CLEANED COWLING A ND ENGINE COMPONENTS. PERFORMED ENGINE RUN IAW EMB 140 AMM 71-00-00. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVI CE. 2 L 7 2 4F RT T00011AT 20081208 EA 2008 12 8 A6WA200840597 1 20081020 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAP FAILED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 31 455AW 7848 AT FL280 LANDING CONFIGURATION INDICATION APPEARED AND ACFT NOSED OVER AND BACKUP. FLAP DEGRADE STATUS MSG APPEARED. P ERFORMED FLAP FAULT ISOLATION PER AMM 27-50-00 WHICH INDICATED A FAULT WITH SKEW DETECTION SYS. PERFORMED TEST OF SDS S YS PER FIM. NO FAULTS INDICATED. PERFORMED FECU TEST PER AMM 27-51-05 AND CONTROL UNIT FAILED. PER MX CNTRL, DEACTIVA TE SDS SYS PER MEL 27-51-03 AND RETEST FECU. DEACTIVATION OF SDS, THE FECU TEST OK PER AMM 27-51-05. FLAPS OPS TEST GO OD PER AMM 27-54-00-710-801. HORIZ STAB CONTROL SYS ALSO TEST OK PER AMM 27-41-00. REPLACED SDU PER AMM 27-51-15. REA CTIVATED SKEW DETECTION SYSTEM PER AWAC SUPP 06-076A. SYSTEM TESTS GOOD. OK FOR SERVICE. 2 L 7 2 4F RT A21EA 20081208 WP 2008 12 8 NWAA085079858 1 20081114 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 767NC 47724 DURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 9-13 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 2 L 7 2 4F RT A6WE 20081208 NM 2008 12 8 SWAA086808 1 20081203 A 5311 6547959 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 747, BETWEEN STR 26R, TO STR 27R. REPAIRED FRAME PER S RM. 2 L 7 2 4F RT A16WE 20081208 EU 2008 12 8 MALA080203 1 20081113 A 5210 SKIN SAAB SF340 340B 7860101 EU PAX DOOR UNKNOWN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 340B433 PASSENGER ENTRANCE DOOR OUTER SKIN REPAIRED. REPAIRED IAW EO NR S52152. 2 L 7 2 4T RT A52EU 20081208 NM 2008 12 8 HALA2008112300870 1 20081123 A 5100 UNKNOWN BOEING 767 76733A 1385209 NM AIRFRAME VIBRATION A HALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 13 581HA 28141 ATB - OUT OF 18000 MSL FELT VIBRATION IN AIRFRAME. FLT CONTROLS NO VIBRATION. CONTINUED TO 25 MSL THEN SLOWED IN INTEN SITY. FL 320 STILL SLIGHT VIBRATION. RETURN TO LAS. INSPECTED AIRCRAFT PANELS, FOUND SECURED INSPECTED ALL DOOR SEAL AND PRESSURIZED TO 6 PSI, NO LEAKS NOTED. INSPECTED CARGO DOORS AND SEALS, NO LEAKS NOTED. INSPECTED ECS BAY FOR LEAKS , OPENED BOTH ENG NO LOOSE DUCTS, RAN ENG AND WING ANTI-ICE. NO ABNORMAL SOUNDS OR VIBRATION. 2 L 7 2 4F RT A1NM 20081208 NM 2008 12 8 SWAA086779 1 20081203 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT RADIO ALTIMETER SKIN CUTOUT, BS 390. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081208 EA 2008 12 8 SWIA200820545 1 20081017 A 3213 AXLE CNDAIR CL600 CL6002C10 1390015 EA RT MLG CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 727SK 10191 C-CHECK, RIGHT MLG PISTON AXLE ROOT CORRODED. REPAIRED PER SCR. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820546 1 20081017 A 3210 GLAND NUT CNDAIR CL600 CL6002C10 1390015 EA RT MLG CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 727SK 10191 C-CHECK, RIGHT MLG CYLINDER GLAND NUT CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081208 NM 2008 12 8 USAASB08117 1 20081129 A 2751 1817389 TRANSMITTER BOEING 737 7374B7 138449C NM TE FLAPS INOPERATIVE A USAA O OTHER F FLT CONT AFFECTED DE DESCENT 1 EA 19 432US 24554 ON DESCENT INTO BWI, CREW REPORTED A TRAILING EDGE FLAP ASYMMETRY PROBLEM VIA ACAR'S. MAINTENANCE OPERATIONS CENTER REC OMMENDED FLIGHT TO CONTINUE TO BWI. CREW DECLARED AN EMERGENCY AND NOTIFIED THE PASSENGERS TO BRACE THEMSELVES FOR LAND ING. WHEN FLAPS WERE PLACED TO 5 UNITS, THE LEFT FLAP INDICATED 1 UNIT AND THE RIGHT REMAINED AT 2 UNITS. AIRCRAFT LAN DED SAFELY AND TAXIED TO THE GATE. NO INJURIES WERE REPORTED. MAINTENANCE FOUND THE LEFT FLAP POSITION TRANSMITTER INO PERATIVE. REMOVED AND REPLACED THE LEFT FLAP POSITION TRANSMITTER PER MM 27-58-12. PERFORMED FLAP POSITION INDICATING SYSTEM FUNCTIONAL CHECK PER MM 27-58-01. ACFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20081020 NE 2008 10 20 AALA200802282 2 20080906 A 7321 EEC BOEING 767 767323 1385205 NM GE CF6 CF680C2B6 30025 NE NR 1 ENGINE INOPERATIVE A AALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 21 377AN 25446 690271 BDL INFLIGHT T160/06 SEP SAN TO JFK. CREW REPORTED UNCOMMANDED SHUTDOWN OF NR 1 ENGINE. LANDED BDL WITHOUT INCIDENT. REPLACED NR 1 ENGINE ELECTRONIC ENGINE CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F 4 F RT A1NM E13NE 20081020 WP 2008 10 20 ABXA080240 1 20080912 A 2450 CURRENT LIMITER DOUG DC9 DC941 302207N WP FAILED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 954AX 47612 CREW REPORTED SMOKE COMING FROM CIRCUIT BREAKER PANEL BEHIND CAPTAINS SEAT WHEN GROUND POWER WAS CONNECTED TO ACFT. FOU ND GROUND SERVICE BUS CONTROL AND A & C PHASE GROUND SERVICE BUSS BREAKERS TRIPPED. REPLACED BLOWN CURRENT LIMITERS FOR CROSS TIE RELAY T2. STARTED APU AND PERFORMED CROSSTIE CHECK. OPS CHECK NORMAL. 2 L 7 2 4F A6WE 20081020 NM 2008 10 20 AALA200802316 1 20080909 A 3350 LIGHT BOEING 767 767323 1385205 NM SEAT 6H INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AN 25451 JFK EMERGENCY LIGHT AT SEAT 6H INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 6H. SYSTEM GROUND CHEC KED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081020 EA 2008 10 20 QXEA200800683 1 20080612 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 713-784 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK NUMEROUS CORROSION SPOTS ON LT SIDE SEAT RAIL FS 713 TO 784. REMOVED CORROSION FROM SEAT TRACK AT FS 713 T O 784. .010 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013 AND CRJ SRM 51-21-16. 2 L 7 2 4F RT A21EA 20081020 NM 2008 10 20 AALA200802294 1 20080907 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW EMERGENCY LIGHTS AT SEAT ROWS 20 TO 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 20 TO 2 6. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081020 EU 2008 10 20 NWAA084303213 1 20080920 A 3350 LAMP AIRBUS 320 A320211 3930320 EU EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 313US 153 EMERGENCY EGRESS LIGHTING TEST FAILS. RELAMPED EXIT SIGN, RESET POWER SUPPLIES 11WL, 12WL, 13WL. REPLACED EPSU 10WL, C HECKS OK. 2 L 7 2 4F RT A28NM 20081020 EA 2008 10 20 SWIA200820133 1 20081005 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 930SW 7713 OVERHEAD CEILING EMERGENCY LIGHT INOP (FLT 5951). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 SWIA200820135 1 20081005 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 506CA 7793 CEILING LEVEL EMERGENCY FLOOD LIGHT INOP (FLT 2810). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081020 SO 2008 10 20 SWIA200820144 1 20081004 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCHARGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 290SW 120317 EMERGENCY LIGHTS ON FLOOR AFT OF ROW 9 INOP (FLT 5565). INSTALLED SERVICEABLE ELBP. 2 L 7 2 4T RT A31SO 20081020 SO 2008 10 20 SWIA200820145 1 20081004 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 563SW 120338 ENTRY EMERGENCY LIGHT INOP (FLT 5708). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4T RT A31SO 20081020 SO 2008 10 20 SWIA200820147 1 20081008 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 224SW 120294 FORWARD EMERGENCY DOME LIGHT INOP (FLT 5457). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4T RT A31SO 20081020 EA 2008 10 20 SWIA200820138 1 20080805 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 771SK 10244 FS 280 CROSSBEAM CRACKED AT LBL 9 AND RBL 9 (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081020 NM 2008 10 20 F3LA200800635 1 20080926 A 5315 D53480043205 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON PASSENGER CABIN FLOORBEAM Y1732 AT FRAME 66. MX REPAIRED FLOORBEAM Y1732 AT FRAME 66 IAW THE REQUIREMENTS OF A319 SRM 53-41-14, FIGURE 201. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTE D AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800632 1 20080924 A 5315 D53472090002 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON PASSENGER CABIN FLOORBEAM Y765 AT FRAME 66+3 INCHES. MX REMOVED AND REPLACED FLOORBEAM Y765 FROM FRAME 64 TO FRAME 66+6 IAW THE REQUIREMENTS OF A319 SRM 51-72-11, PAGE 1 AND 2. UPON COMP LETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800633 1 20080924 A 5315 D53472193200 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON PASSENGER CABIN FLOORBEAM Y765 AT FRAME 68. MX REMOVED AND REPLACED FLOORBEAM AT FRAME 66 TO FRAME 70 IAW THE REQUIREMENTS OF A319 SRM 51-72-11. UPON COMPLETION OF THE REPAIR, IT WAS INS PECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800634 1 20080924 A 5315 D535472189204 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON PASSENGER CABIN FLOORBEAM Y1292 AT FRAME 68. MX REMOVED AND REPLACE D FLOORBEAM Y1292 AT FRAME 68 IAW THE REQUIREMENTS OF A319 SRM 51-72-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTE D AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 USAA920081784 1 20080927 A 5754 65C26603157SP SKIN BOEING 737 7374B7 1384702 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - MAJOR REPAIR - Q5 CHECK, NR 3 SLAT LOWER TRAILING EDGE SURFACE CRACKED AT THE OUTBOARD AUXILIARY TRACK LOCATION. REPAIRED NR 3 SLAT LOWER TRAILING EDGE SURFACE CRACKED AT THE OUTBOARD AUXILIARY TRACK LOCATION IAW B737 SRM 57-43-01 RE PAIR 6. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 USAA920081783 1 20080924 A 5512 SKIN BOEING 737 7374B7 1384702 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - MAJOR REPAIR - Q5 CHECK, RT HORIZONTAL STABILIZER LOWER SURFACE SKIN CRACKED, STABILIZER STATION 157.10. REPAIRE D RT HORIZONTAL STABILIZER LOWER SURFACE SKIN, STABILIZER STATION 157.10 IAW US AIRWAYS TYPICAL REPAIR 55-10-07 REV C. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 F3LA200800646 1 20080922 A 5321 D5367221800000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE PERFORATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED FLOOR PANEL 132DG WAS PERFORATED. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMEN TS OF A319 SRM 53-02-00 PARA 8C. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800647 1 20080922 A 5321 5367221600000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE PERFORATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED FLOOR PANEL 131DG WAS PERFORATED. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMEN TS OF A319 SRM 53-02-00 PARA 8C. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 EU 2008 10 20 USAA920081794 1 20080921 A 5322 D5347112420300 SHEAR TIE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 PIT - MAJOR REPAIR - S4 CHECK, LEVEL 2 CORROSION ON RT SHEAR TIE PLATE, FR 69- FR 70, S23L. REPLACED RT SHEAR TIE PLATE , FR 69- FR 70, S23L IAW US AIRWAYS EO 5307Y284. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 USAA920081785 1 20080927 A 5753 65C263208 SPLICE PLATE BOEING 737 7374B7 1384702 NM T/E FLAP CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - MAJOR REPAIR - Q5 CHECK, RT WING OUTBOARD MIDFLAP UPPER SURFACE SPLICE PLATE AT THE AFT TRACK ACCESS OPENING IS CR ACKED. REPLACED RT WING OUTBOARD MIDFLAP UPPER SURFACE SPLICE PLATE AT THE AFT TRACK ACCESS OPENING IAW B737 SRM 51-20- 01 AND BOEING DWG 65-71949-73. 2 L 7 2 4F RT A16WE 20081021 NE 2008 10 21 USA2008F00034 2 20080927 A 7200 ENGINE EMB ERJ190 ERJ190100IGW 3260408 NM GE CF34 CF3410E6 30023 NE NR 2 VIBRATION A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 965UW 19000198 FLIGHT 1615, CLT - MCI, PASSING 16,000FT THE NR 2 ENGINE TRIGGERED A HP VIB WARNING LIGHT (REGISTERING 5.0 VIBRATION). AFTER CONSULTING THE CHECKLIST THE CREW RESTORED POWER TO THE ENGINE, SIMILAR RESULTS OCCURRED. THE CREW DECIDED TO RET URN TO CLT. THE ENGINE WAS NOT SHUTDOWN BUT WAS IDLED. THE FLIGHT LANDED UNEVENTFULLY. MX ACTION PENDING 2 L 7 2 4F 4 F RT A57NM E00070EN 20081021 NM 2008 10 21 USAA920081738 1 20080916 A 5510 697309603 HINGE PIN BOEING 737 7373G7 1384595 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - MAJOR REPAIR, RT HORIZONTAL STAB OUTER HINGE PIN CORRODED AT BS 1154. REPLACED HORIZONTAL STAB OUTER HINGE PINS A T BS 1154 IAW AMERICA WEST TASK CARD I6C55039. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081744 1 20080818 A 5512 65C27494 SKIN BOEING 737 7373G7 1384595 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 SAL - MAJOR REPAIR - C19 CHECK, LT HORIZONTAL STAB LOWER SURFACE SKIN CRACKED AT PREVIOUS REPAIR, STABILIZER STATIONS 13 2.1 - 175.5. REPAIRED LT HORIZONTAL STAB LOWER SURFACE SKIN AT PREVIOUS REPAIR, STABILIZER STATIONS 132.1 - 175.5. IAW ER 03-5516-02339-ES2. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081747 1 20080906 A 5310 507945272 DOOR FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT - MAJOR REPAIR, CRACK AT L1 DOOR CUTOUT AT AFT LOWER CORNER OF FRAME. REPLACED L1 DOOR CUTOUT LOWER FRAME IAW BOEIN G DRAWING NR 5007945. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081749 1 20080916 A 5510 69731201 HINGE PIN BOEING 737 7373A4 1384585 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - MAJOR REPAIR, LT HORIZONTAL STAB OUTER HINGE PIN CORRODED AT BS 1154. REPLACED LT HORIZONTAL STAB OUTER HINGE PIN AT BS 1154 IAW AMERICA WEST TASK CARD I6C55039. 2 L 7 2 4F RT A16WE 20081021 EU 2008 10 21 USAA920081751 1 20080927 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 640AW 448 FLT NR 182 - PHX - FLASHLIGHT AT FWD FLT ATTENDANT JUMPSEAT INOPERATIVE. MX REMOVED AND REPLACED THE FWD FLT ATTENDANT FLASHLIGHT BATTERY. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081020 EA 2008 10 20 QXEA200800687 1 20080612 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 379-483 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK NUMEROUS CORROSION SPOTS ON LT SIDE SEAT RAIL FS 379 TO FS 483. REMOVED CORROSION FROM SEAT TRACK AT FS 37 9 TO FS 483. .015 MATERIAL REMOVED TREATED IAW REO 670-53-00-013 AND SRM 51-21-16. 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 HNAA0800293 1 20080917 A 3350 6013211X BATTERY DHAV DHC8 DHC8311 1386006 EA EMERGENCY LIGHTS DISCHARGED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 326EN 16730 234 RT AFT EMERGENCY LIGHT INOP. R&R D BULB NO FIX. R&R BATTERY 3351 PS4 ROW 12 RT SIDE IAW AMM 31-51-05. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 20081020 NM 2008 10 20 AALA200802312 1 20080908 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 343AN 33082 MIA EMERGENCY LIGHTS AT SEAT ROWS 37 TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 37 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081020 EA 2008 10 20 QXEA200800686 1 20080612 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 483-573 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK NUMEROUS CORROSION SPOTS ON LT SIDE SEAT RAIL FS 483 TO FS 573. REMOVED CORROSION FROM SEAT TRACK AT FS 48 3 TO FS 573. .040 MATERIAL REMOVED, OUT OF LIMITS IAW REO 670-53-00-013. REMOVED CORRODED SEAT TRACK IAW CRJ 700 SRM 5 1-41-02 AND INSTALLED NEW SEAT TRACK IAW 51-41-02 AND 51-23-00. 2 L 7 2 4F RT A21EA 20081020 NM 2008 10 20 AALA200802276 1 20080905 A 5753 113W300314 WEDGE BOEING 777 777223 1385213 NM RT WING TE FLAP DELAMINATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 AFW RT OTBD FLAP TRAILING EDGE WEDGE ON TOP SIDE HAS DELAMINATION CUT OUT WITHIN 3.5 INCHES OF THE LEADING EDGE. AREA OF DISCREPANCY IS 12 INCH BY 6 INCH. REPAIRED PER SRM 57-53-01-2R TABLE 201. 2 L 7 2 4F RT T00001SE 20081020 WP 2008 10 20 AALA200802298 1 20080907 A 3297 WIRE HARNESS DOUG DC9 DC982 3022082 WP LANDING GEAR INOPERATIVE A AALA O OTHER J WARNING INDICATION LD LANDING 1 SW 21 458AA 49563 LGA INFLIGHT T712/07SEP. CREW REPORTED ANTI SKID FAILED DURING LANDING FOLLOWED BY NR 1 AND 2 TIRE FAILURE. ACFT TAXIE D TO GATE UNDER ITS OWN POWER. REPAIRED TRANSDUCER WIRING AND REPLACED NR 1 AND 2 TIRES. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081020 NM 2008 10 20 AALA200802299 1 20080907 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 181AN 29591 DFW EXTERIOR EMERGENCY LIGHTS AT LT OVERWING AFT POSITION INOPERATIVE. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIG HT AT LT OVERWING AFT POSITION. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081020 NM 2008 10 20 AALA200802261 1 20080903 A 2421 766088B GENERATOR BOEING 767 767323 1385205 NM LEFT FAILED A AALA A UNSCHED LANDING G H J MULTIPLE FAILURE ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SW 21 370AA 25197 YOW INFLIGHT T55/03SEP MAN TO ORD. CREW REPORTED LT GENERATOR FAILED AND UNABLE TO START AUXILIARY POWER UNIT APU. LAN DED YOW WITHOUT INCIDENT. REPLACED LT INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081020 NM 2008 10 20 UPS08553560 1 20081002 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 1500 S26R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 FRAME IS DENTED AT BS 1500 STR 26R. REPAIRED PER SRM 53-00-07-2R5, MPI 19906. 2 L 7 2 4F RT A2NM 20081020 NM 2008 10 20 UPS08553561 1 20081002 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 1480 S26L DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 FRAME IS DENTED AT BS 1480 STRINGER 26LT. REPAIRED FRAME WITH DOUBLER IAW SRM 53-00-07-24 MPI 19905 ISSUED. 2 L 7 2 4F RT A2NM 20081020 CE 2008 10 20 YAD2008F00003 1 20080920 A 3240 BRAKE SYS BEECH 1900 1900C 1154161 CE MLG WEAK E YADA O OTHER O OTHER TX TAXI/GRND HDL 1 AL 03 115AX UC2 PILOT REPORTED LT BRAKE FLAT ON TAXI AND LANDING. MX BLEED BRAKES. 2 L 7 2 4T RT A24CE 20081020 GL 2008 10 20 P5CA0801576 2 20080919 A 7200 ENGINE BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL NR 3 SURGES A P5CA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 EA 15 450PA 30808 NR 3 ENGINE SURGED ON TAKE OFF ROLL. TAKE OFF ABORTED AT 100 KTS. HIGH ENERGY STOP INSPECTION COMPLETED PER AMM 05-51- 10. NO TROUBLE FOUND. ALSO NR 3 ENGINE CIT SENSOR WAS REPLACED AND TESTED OK. ACFT DEPARTED WITH NO FURTHER ISSUES. 2 L 7 4 4F 4 F RT A20WE E23EA 20081020 NM 2008 10 20 AALA200802308 1 20080908 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 912AN 29513 TPA EMERGENCY LIGHT AT SEAT 19D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 AALA200802310 1 20080908 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 912AN 29513 TPA EMERGENCY LIGHT AT SEAT 16D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 QXEA200800995 1 20080917 A 6123 PROPELLER DHAV DHC8 DHC8202 2809007 NM NR 2 MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 19 357PH 504 PDX NR 2 PROPELLER TOOK LONGER THAN NORMAL TO COME OUT OF FEATHER. ALL COCKPIT INDICATIONS WERE NORMAL. AFTER ABOUT 40 SECONDS THE PROPELLER CAME OUT OF FEATHER. MX GROUND RAN THE ACFT AND PERFORMED NUMEROUS UNFEATHERS. COULD NOT DUPLIC ATE 40 SECOND TIME. TIME WAS ABOUT 15 SECONDS FOR BOTH PROPS. ACFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081020 EA 2008 10 20 MAL2008F00036 1 20080922 A 3350 110049 BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 926XJ 15184 CREW INFORMED MX THAT EMERGENCY LIGHTING WAS INOP. REPLACED BATTERY CHARGER AND BATTERY PACK. 2 L 7 2 4F RT A21EA 20081020 NM 2008 10 20 AALA200802283 1 20080906 A 2560 BATTERY BOEING 777 777223 1385213 NM FLASHLIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 775AN 29584 BDL EMERGENCY FLASHLIGHT AT RT NR 2 DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT RT NR 2 DOOR. SYSTE M GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081020 EA 2008 10 20 HNAA0800294 1 20080917 A 3350 DL3071 LAMP DHAV DHC8 DHC8311 1386006 EA EMERGENCY LIGHTS BURNED OUT A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 326EN 234 EMERGENCY EXIT SIGN BY MAIN CABIN DOOR HAS SEVERAL LAMPS INOP. REPLACED BURNT OUT LAMPS AND SECURED COVER. OPS CHECK G OOD. 2 H 7 2 4T RT A13NM 20081020 GL 2008 10 20 SIMA200826701 2 20080826 A 7321 23063131 FMU EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007A 03030 GL NR 1 ENGINE MALFUNCTIONED A SIMA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 SW 21 611AE 145074 ON FLIGHT 3576 CREW REPORTED ENGINE 1 POWER FLUX N1 ITT, N2, IGNITION A&B AUTO RELIGHT AND FADEC TRANSFER IN FLIGHT FOR ABOUT 30 SECONDS. THRUST SURGED UP/DOWN CONTINUED FROM ABOVE TRUST LEVERS AT FLT IDLE. ENGINE 1 STABILIZED NO ABNORMAL INDICATIONS AFTERWARDS. NO EICAS MSGS. ACFT REMOVED FROM SERVICE. C/A R&R FPMU AND OPS CHECKED GOOD. FSF PASSED. A CFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081020 NM 2008 10 20 PIDA08032 1 20080921 A 3350 20131A BATTERY PACK BOEING 767 767277 1385128 NM EMERGENCY LIGHTS NO TEST A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 767MW 22694 DURING PREFLIGHT MX CHECK RT EMERGENCY ESCAPE SLIDE SQUIB TEST WAS INOPERATIVE. R&R ESCAPE SLIDE BATTERY PACK IAW AMM 2 5-65-17. FUNCTIONAL CHECK WAS NORMAL 2 L 7 2 4F RT A1NM 20081020 NM 2008 10 20 AALA200802278 1 20080829 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 MIA EMERGENCY EXIT LIGHTS AT SEAT ROWS 20H AND 21H INOPERATIVE. REPLACED BATTERY PACK AT RT HAND OVERWING DOOR FOR EMER GENCY EXIT LIGHTS AT SEAT ROWS 20H AND 21H. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081020 NM 2008 10 20 AALA200802309 1 20080908 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 912AN 29513 TPA EMERGENCY LIGHT AT SEAT 19D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 AALA200802260 1 20080903 A 5410 311T2115 BUSHING BOEING 767 767323 1385205 NM PYLONS CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 380AN 25449 AFW RT UPPER SPAR FITTING HAD PITTING ON BUSHINGS. REPAIRED PER SRM 54 52 90 2R WITH THE FOLLOWING DEVATION. AFTER PER FORMING STEP 5 IT IS ACCEPTABLE TO SKIP TO STEP 16. 2 L 7 2 4F RT A1NM 20081020 NM 2008 10 20 F3LA200800614 1 20080919 A 5315 D534721220400 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 930FR 31 2241 DURING C3 C-CHECK INSPECTION NOTED FLOORBEAMS INBOARD OF THE L2 DOOR SILL CORRODED AND CORROSION IN ALL NUT PLATE HOLES. MX REMOVED FLOORBEAMS, REMOVED BARREL NUT FITTING AND SPLICE, DRILLED HOLES IN SERVICEABLE BEAM, INSTALLED BARREL NUT FITTING AND SPLICE AND INSTALLED BEAMS IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800616 1 20080918 A 3220 D64433 PIN AIRBUS A319 A319111 3930336 NM NLG FAILED A F3LA O OTHER O OTHER LD LANDING 1 NM 21 924FR 17606 40 2030 FLIGHT NR 3183. NR 1 ELECTRONIC CENTRALIZED ACFT MONITOR INDICATED LANDING GEAR CONTROL INTERFACE UNIT FAULT. ACFT VIB RATION WAS FELT AFTER LANDING AND ACFT STOPPED ON RUNWAY. MX FOUND NOSE GEAR TIRES TURNED 90 DEGREES AND SEVERAL BROKEN NLG PARTS ON THE RUNWAY. MX STRAIGHTENED OUT THE TIRES AND TOWED ACFT TO REMOTE SITE FOR INSPECTION AND REPAIR. THE N LG LEG ASSEMBLY WILL BE SENT TO THE MFG FOR EVALUATION. THE LABORATORY CONCLUDED THAT THE SHAFT FAILED BY OVERLOAD WHIC H OCCURRED FROM APPLIED TORQUE IN A COUNTERCLOCKWISE DIRECTION. 2 L 7 2 4F RT A28NM 20081020 WP 2008 10 20 AALA200802284 1 20080906 A 3397 CONTACT DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 290AA 49302 LGA EXTERIOR EMERGENCY LIGHTS AT LT HAND OVERWING EXIT INOPERATIVE. CLEANED AND ADJUSTED CONTACT FOR EXTERIOR EMERGENCY LIGHTS AT LT HAND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081020 NM 2008 10 20 AALA200802293 1 20080902 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 602AN 27053 SFO EMERGENCY LIGHT AT SEAT ROWS 16 TO 23 INOPERATIVE. REPLACED BATTERY PACK AT SECTION 3 FOR EMERGENCY LIGHTS AT SEAT ROWS 16 TO 23. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081020 NM 2008 10 20 AALA200802295 1 20080907 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 DFW EMERGENCY LIGHTS AT FORWARD GALLEY AND LT NR 1 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORW ARD GALLEY AND LT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081020 NM 2008 10 20 UHL2008F00005 1 20080918 A 3350 340022 BATTERY EMB ERJ170 ERJ170100SE 3260406 NM EMERGENCY LIGHTS DISCHARGED A UHLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 11 655RW 17000105 CREW RECEIVED A EMER LT BATT FAULT. MX PERFORMED EMERGENCY BATTERY CHARGING. DISCREPANCY HAS NOT REPEATED THIS DATE 09 /23/08. 2 L 7 2 4F RT A56NM 20081020 NM 2008 10 20 AALA200802300 1 20080907 A 3397 WIRE HARNESS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 181AN 29591 DFW EMERGENCY LIGHT AT SEAT 35D INOPERATIVE. REPAIRED WIRING AT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 35D. SYSTEM GROU ND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081020 SO 2008 10 20 C2XA08RI138 1 20080908 A 3350 66368 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13969 145141 RIC MX DURING ROUTINE INSPECTION RIC MX FOUND EMERGENCY LIGHT FLOOR STRIP INOPERATIVE. RIC MX R&R EMERGENCY LIGHT STRIP AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081020 SO 2008 10 20 C2XA08TY107 1 20080924 A 3350 2013BR BATTERY EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12157 7507 145787 A/C IS CURRENTLY IN C CHECK AND DURING AN OPS CHECK THE ROW 12 CEILING AND SIDEWALL EMERGENCY LIGHTS WERE INOP. MX R&R THE NR 3 POWER SUPPLY IAW EMB XR AMM 33-50-04 AND OPS CHECKED GOOD. A/C WILL BE RELEASED WHEN CHECK IS COMPLETE. 2 L 7 2 4F RT 20081020 NM 2008 10 20 AALA200802303 1 20080907 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 794AN 30256 MIA EMERGENCY LIGHT AT SEAT 20C HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081020 NM 2008 10 20 F3LA200800617 1 20080911 A 5321 D5367180500400 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 930FR 31 2241 REFERENCE NON ROUTINE CO51223. DURING C3 C CHECK INSPECTION NOTED FLOOR PANEL 261FF HAD CORROSION ON UPPER AND LOWER SU RFACES. MX REMOVED FLOOR PANEL AND INSTALLED NEW IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-12-400-002. UPO N COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800611 1 20080920 A 5321 D536175900000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 930FR 31 2241 REFERENCE NON ROUTINE CO51333. DURING C3 C CHECK, INSPECTION NOTED FLOOR PANEL 261EF HAD DAMAGED AREA AROUND INSERT ON OTBD EDGE. MX REMOVED FLOOR PANEL AND REPLACED WITH NEW IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-12-400-00 2. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 WP 2008 10 20 AALA200802279 1 20080906 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7540A 49994 MSP EMERGENCY LIGHT AT SEAT ROW 25 HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 25. SYSTEM GROUND CH ECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081020 WP 2008 10 20 UPS08853529 1 20080921 A 5531 RIB DOUG DC8 DC873F 302199F WP VERTICAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:CV EVALUATION AND DISPOSITION REPAIR EFN89419911115. ORIGINAL N/R 480 775. VERTICAL STABILIZER L/E LOW ER SECTION NR 25 RIB CRACKED AFT LT FLANGE. RFTS N894UP-9-20284 RIVETS INSTALLED IN FREE STANDING LEG OF REPAIR. REMOV ED RIVETS AND INSTALLED LOCK FASTENERS IAW UPS DC-8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 20081020 NM 2008 10 20 ASAA0843583 1 20080914 A 5310 THRESHOLD BOEING 737 7374Q8 138447Q NM BS 907-1006 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 AFT CABIN FLOOR R2 DOOR THRESHOLD INNER CHORD CORRODED STA 946 TO STA 992 AREA. REMOVED DAMAGED INNER CHORD, LOCATED DRI LLED AND INSTALLED REPLACEMENT INNER CHORD IAW B737 400 SRM 51 40 02 51 40 05. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0843585 1 20080920 A 5322 65C336411 SHEAR TIE BOEING 737 7374Q8 138447Q NM BS 380 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 ACCOMPLISH SHEAR TIE REPAIR AT STA 380 BETWEEN STA 25L AND 26L REF ASA EA 5310 02675 ITEM 7 IAW SRM 53-00-07 (EDGE DISTA NCE AT FASTENER HOLES BELOW MINIMUM). REMOVED DAMAGED SHEAR TIE, LOCATED DRILLED AND INSTALLED A REPLACEMENT SHEAR TIE IAW SRM 53-00-07 FIG 201. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0843564 1 20080913 A 5754 65C26603191 SKIN BOEING 737 7374Q8 138447Q NM NR 3 SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 LEFT WING NR 3 SLAT T/E WEDGE LOWER SURFACE CHAFED CENTER AREA. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER BON DED IAW B737 400 SRM REPAIR 4. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0843562 1 20080907 A 5755 SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 LEFT WING NR 0 SPOILER DENTED ON LOWER SURFACE NEAR CENTER AT TRAILING EDGE. REMOVED DAMAGED AREA, PREPARED AREA, FABRI CATED FILLER AND DOUBLER BONDED IAW 737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0843572 1 20080912 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 7 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 RT WING NR 7 SPOILER UPPER SURFACE AREAS OF MULTIPLE DENTS. REMOVED DAMAGED AREAS, FABRICATED FILLERS AND DOUBLERS BOND ED IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0843574 1 20080925 A 5753 SKIN BOEING 737 7374Q8 138447Q NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 LEFT WING I/B FOREFLAP UPPER SURFACE HAS DENT AT O/B CORNER. PREPPED DAMAGED AREA, FABRICATED DOUBLER AND BONDED REPAIR IAW B737 400 SRM 51 70 10 REPAIR 2 PAGE 201. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0843575 1 20080925 A 5753 SKIN BOEING 737 7374Q8 138447Q NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 LEFT WING O/B FORE FLAP LOWER SURFACE HAS MULTIPLE DENTS AT MID SECTION. PREPPED DAMAGED AREA, FABRICATED REPAIR DOUBLE RS AND BONDED REPAIR IAW B737 400 SRM 51 70 10 REPAIR 4 PAGE 201. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0853560 1 20081007 A 2840 3012803 INDICATOR BOEING 737 737890 1384527 NM FUEL QTY FAILED A ASAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 02 559AS 8092 35178 FUEL TOTALIZER WENT 1500 LBS HIGH ON ROTATION ON TAKEOFF FROM 29.2 TO 30.7. FUEL AT GATE WAS 29.4. TOTALIZER REMAINED AT 1300 HIGHER THAN FLT PLAN BURN AT CRUISE CURRENT STATUS AND INFLIGHT FAULTS OF FQIS REVEALED NO FAULTS. PERFORMED OPER ATIONAL AND SYSTEM TEST REF MM 28-41-00, ALL OPS NORMAL. PRECAUTIONARY REPLACED FUEL QUANTITY PROCESSOR UNIT REF MM 28- 41-81. OPS CHECK NORMAL . "SATISFACTORY VERIFICATION FLT" VERBAL FROM INBOUND FLT CREW. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 F3LA200800609 1 20080916 A 5315 D53472172220500 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 930FR 2241 DURING C3 C-CHECK, INSPECTION NOTED THE FLOORBEAM IB OF THE R2 DOOR SILL HAS CORROSION IN ALL NUT PLATE HOLES. MAINT RE MOVED AND REPLACED FLOORBEAM. Y1292 IAW THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE REPAIR, IT WAS I NSPECTED AND FOUND ACCEPTABLE. (K) 2 L 7 2 4F RT A28NM 20081020 2008 10 20 COMA0880016 2 20080904 A 7200 ENGINE CNDAIR CL600 CL6002D24 1390016 EA RIGHT VIBRATION A COMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 689CA 15133 ENROUTE, CREW REPORTS FAN VIBRATION ON RT ENGINE. AC DIVERTED AND LANDED SAFELY. INSPECTED RT ENGINE FAN BLADES NO DEF ECTS NOTED. PERFORMED ENGINE RUNS WITH NO DEFECTS NOTED. (K) 2 L 7 2 4F RT A21EA 20081020 CE 2008 10 20 DXTA200803277 1 20080919 A 3260 INDICATION SYS CESSNA 750 750 2076810 CE NLG UNKNOWN E DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 942QS 7500024 NO GREEN LIGHT NOSE GEAR INDICATION ON FINAL APPROACH. (K) 2 L 7 2 4J RT T00007WI 20081020 NM 2008 10 20 UPS08M53528 1 20080516 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 RT WING O/B FLAP I/B AFT HINGE O/B PIVOT I/B SPOTFACE CORRODED. RT WING O/B FLAP I/B AFT HINGE O/B PIVOT I/B SPOTFACE C ORROSION REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-52-04 REV 61. 2 L 7 3 4F RT A22WE 20081020 EA 2008 10 20 SWIA200820129 1 20080510 A 5230 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 417SW 7400 CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED (C-CHECK). REPLACED CARGO DOOR SUPPORT ANGLE. 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 SWIA200820131 1 20080510 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA AFT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 417SW 7400 REAR PRESSURE BULKHEAD WEB AT LINTEL ATTACHMENT HAS .2 INCH CRACK (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 SWIA200820134 1 20081005 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN DEFECTIVE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 FLOOR LEVEL EMERGENCY LIGHT BY MAIN CABIN DOOR DOES NOT ILLUMINATE (FLT 5929). REPLACED FLOOR LEVEL EMERGENCY LIGHT STR IP. 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 SWIA200820136 1 20081005 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 452SW 7716 OVERHEAD EMERGENCY LIGHT, THIRD FROM THE GALLEY, INOP (FLT 3966). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 SWIA200820137 1 20081007 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 947SW 7786 EMERGENCY OVERHEAD FLOODLIGHT ROW 2 INOP (FLT 5867). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 SWIA200820143 1 20081007 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 963SW 7865 CEILING EMERGENCY LIGHT AT ROW 2 INOP (FLT 6268). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081020 SO 2008 10 20 SWIA200820146 1 20081008 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO GALLEY SMOKE A SWIA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 07 567SW 120342 F/A SMELLED SMOKE IN GALLEY AND PILOT SMELLED FAINT ELECTRICAL SMOKE IN COCKPIT (FLT 5138). INSPECTED GALLEY AREA FOR S MOKE, NONE FOUND. ALL SYSTEMS OPERATING NORMAL IN GALLEY. 2 L 7 2 4T RT A31SO 20081020 NM 2008 10 20 F3LA200800629 1 20080925 A 5315 D5347209200000 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON PASSENGER CABIN FLOORBEAM Y765 AT FRAME 67+10 INCHES. MX REMOVED AN D REPLACED FLOORBEAM AT FRAME 67 IAW THE REQUIREMENTS OF A319 SRM 51-72-11, PAGE 1 AND 2. UPON COMPLETION OF THE REPAIR , IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800638 1 20080927 A 5321 D5347204900100 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED DELAMINATION ON FLOOR PANEL 162EF IN THE AFT CARGO COMPARTMENT. MX REMOVED AND R EPLACED THE FLOO PANLE IAW THE REQUIREMENTS OF A319 SRM 53-02-00, TABLE 105. UPON COMPLETION OF THE REPAIR, IT WAS INSP ECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800640 1 20080925 A 5321 D5367202700000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED DELAMINATION ON FLOOR PANEL 151TG. MX REMOVED AND REPLACED THE FLOOR PANEL IAW T HE REQUIREMENTS OF A319 SRM 53-02-00. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800645 1 20080922 A 5321 D5367225900000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE PERFORATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED FLOOR PANEL 132EG WAS PERFORATED. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMEN TS OF A319 SRM 53-02-00, PARA 8C. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800642 1 20080925 A 5321 D5367227100000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED FLOOR PANEL 151TG WAS DAMAGED. MX REMOVED AND REPLACED THE FLOOR PANEL IAW THE R EQUIREMENTS OF A319 SRM 53-02-00. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800636 1 20080923 A 5315 D53472190205 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON PASSENGER CABIN FLOORBEAM Y1292 AT FRAME 66. MX REMOVED AND REPLACE D FLOORBEAM Y1292 AT FRAME 64 TO FRAME 66 IAW THE REQUIREMENTS OF A319 SRM 51-72-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 EU 2008 10 20 F3LA200800619 1 20080925 A 5321 D5367431100000 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 808FR 29 3038 DURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY FLOOR PANEL 131CG HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANE L IAW THE REQUIREMENTS OF A318 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCE PTABLE. 2 L 7 2 4F RT 20081020 EU 2008 10 20 USAA920081790 1 20080924 A 5315 D5347219020300 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 PIT - MAJOR REPAIR - S4 CHECK, LEVEL 2 CORROSION ON FLOORBEAM FR 65 - FR 66, -Y765. REPLACED FLOORBEAM, FR 65 - FR 66, -Y765 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081020 EU 2008 10 20 USAA920081788 1 20080924 A 5315 D5347219021100 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 PIT - MAJOR REPAIR - S4 CHECK, LEVEL 2 CORROSION ON FLOORBEAM FR 64, -Y1292. REPLACED FLOORBEAM, FR 64, -Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800651 1 20080928 A 5754 D57460351204 SKIN AIRBUS A319 A319111 3930336 NM L/E SLAT DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED DENT ON TOP SKIN OF LT SLAT NR 3 BETWEEN RIB 3 AND 4. MX REPAIRED THE DENT IAW T HE REQUIREMENTS OF A319 SRM 57-40-00, FIGURE 224. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800639 1 20080922 A 5321 D5367324200000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED PERFORATION ON FLOOR PANEL 151VG IN THE AFT CARGO COMPARTMENT. MX REPAIRED THE F LOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARA 8C. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUN D ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 USAA920081780 1 20080825 A 5311 65465262 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS440, S9L. REPAIRED FRAME BS440, S9L IAW US AIRWAYS TASK CARD M1C53002. 2 L 7 2 4F RT A16WE 20081020 EU 2008 10 20 USAA920081793 1 20080921 A 5320 D5361018300200 ANGLE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 PIT - MAJOR REPAIR - S4 CHECK, LEVEL 2 CORROSION ON ANGLE, FR 12+4, IN FRONT OF RT SEAT TRACKS. REPLACED ANGLE, FR 12+4 , IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081020 EU 2008 10 20 USAA920081791 1 20080924 A 5347 D5311278220200 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 PIT - MAJOR REPAIR - S4 CHECK, LEVEL 2 CORROSION ON SEAT TRACK FR 20, -Y765. REPLACED SEAT TRACK, FR 20, -Y765 IAW A319 SRM 51-42-11. 2 L 7 2 4F RT A28NM 20081021 NM 2008 10 21 R5KB10131 1 20081013 A 3350 LIGHT BOEING 727 727227 1384078 NM ROW 14-23 LOOSE I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 422BN 20735 EMERGENCY PATH LIGHTING INOP FROM ROW 14 TO ROW 23. 2 L 7 3 4F A3WE 20081021 NM 2008 10 21 USA2008F00035 1 20080925 A 3233 65448105 UPLOCK ACTUATOR BOEING 737 7374B7 1384702 NM RT MLG FAULTY A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 443US 27891 1458 24842 PIT - FLT 864, AFTER TAKEOFF FROM TPA, ENROUTE TO PIT, THE RT MLG RED LIGHT REMAINED ON WITH GEAR HANDLE IN THE UP POSIT ION. LANDING GEAR APPEARED TO BE LOCKED UP. AFTER APPROXIMATELY 20 MINUTES, THE RED LIGHT EXTINGUISHED. FLIGHT CONTIN UED ON TO PIT AND LANDED WITHOUT FURTHER INCIDENT. LANDING GEAR OPERATED NORMALLY DURING APPROACH AND LANDING. MX REMO VED AND REPLACED THE RT MLG UPLOCK ACTUATOR PER MM 32-32-41-404-006. RETRACTION/EXTENSION CHECKS GOOD PER MM32-3200/501 . LEAK CHECK AND INDICATIONS GOOD. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081732 1 20080923 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST UK UNKNOWN 1 EA 19 836AW 2570 FLT NR204 - SMF-PHX, OUTBOARD 2L FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081021 NM 2008 10 21 USAA920081735 1 20080920 A 5320 654797321 CUSP WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - MAJOR REPAIR, 2 CRACKS ON CUSP WEB BETWEEN BS 634 & BS 637, LBL 70.5, 1 INCH & 1.5 INCHES LONG. REPLACED CUSP WEB , BS 634 & BS 637, LBL 70.5 IAW B737 SRM 51-40-02-00. 2 L 7 2 4F RT A16WE 20081020 WP 2008 10 20 UPS08853550 1 20080929 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV EVALUATION OF N/R 535858 LT WING L/E REPAIR BETWEEN NR 1 AND 2 PYLONS TENTH RIB FROM INBOARD END IS C RACKED. REPAIR WAS ACCOMPLISHED IAW DC8 SRM 57-2-0 SHEET 2 OF 2. 2 L 7 4 4F RT 4A25 20081020 WP 2008 10 20 UPS08853551 1 20080921 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV EVALUATION OF N/R 534213 RIGHT HAND LEADING EDGE AT STA XFS 804.00 UPPER LEFT RIB HAS A CRACK AFT END . REPAIR IS ACCOMPLISHED IAW DC8 SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 20081020 WP 2008 10 20 UPS08853533 1 20080921 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1470 RBL 46 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:CV EVALUATION AND DISPOSITION REPAIR EFN 89420081074. ORIGINAL N/R 14 7772 SEAT TRACK PLUG GOUGED FS 14 70 RBL 46. REPAIR FOUND TO BE IAW SRM DC-8 53-2-3 FIGURE 60. 2 L 7 4 4F RT 4A25 20081020 SO 2008 10 20 SIMA200826102 1 20080912 A 3350 2013BR BATTERY EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHTS DISCHARGED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 806AE 145503 ON FLIGHT, CREW REPORTED EMERGENCY LIGHTS ON FLOOR AND EXIT SIGNS WILL NOT ILLUMINATE. ACFT REMOVED FROM SERVICE. REMOV ED AND REPLACED NR 2 BATTERY PACK IAW WORK CARD NR 33-700-19. OPERATIONAL CHECK GOOD AT THIS TIME. ACFT RETURNED TO SER VICE. (K) 2 L 7 2 4F RT T00011AT 20081020 EU 2008 10 20 USAA920081662 1 20080910 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 620AW 18094 052 EMERGENCY LIGHTS INTERMITTENTLY INOPERATIVE. MAINT REMOVED AND REPLACED THE MID CABIN EMERGENCY POWER SUPPLY IAW MM 33- 51-38. OPS CHECK WAS GOOD. (K) 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 USAA920081660 1 20080910 A 5311 6546529 FRAME BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 FRAME CRACKED AT SUPPORT BRACKET BS440 BETWEEN S8R AND S9R. REPAIRED FRAME AT SUPPORT BRACKET BS 440 BETWEEN S8R AND S9R IAW REPAIR NR 53-10-20E. (K) 2 L 7 2 4F RT A16WE 20081020 CE 2008 10 20 DXTA200803271 1 20080910 A 3240 BRAKE ASSY BEECH MU300 400A 1155402 CE MLG WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 108QS RK382 BRAKING IS MUSHY DURING TAXI. (K) 2 H 7 2 4F RT A16SW 20081020 EA 2008 10 20 ASOA200801327 1 20081001 A 5343 PIN CNDAIR CL600 CL6002C10 1390015 EA MLG TRUNNION CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 CORROSION AT RT MLG FWD TRUNNION PIN. 2 L 7 2 4F RT A21EA 20081020 NM 2008 10 20 UPS08M53503 1 20080518 A 5753 STRUCTURE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A RT WING O/B FLAP O/B FWD HINGE BARREL NUT UPPER BORE CORRODED. RT WING O/B FLAP O/B FWD HINGE BARRE L NUT UPPER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09. 2 L 7 3 4F RT A22WE 20081020 NM 2008 10 20 UPS08M53505 1 20080518 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A RT WING O/B FLAP O/B FWD HINGE FWD MOUNT O/B ATTACHMENT LUG O/B SPOT FACE CORRODED. RT WING O/B FLA P O/B FWD HINGE FWD MOUNT O/B ATTACHMENT LUG O/B SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09. 2 L 7 3 4F RT A22WE 20081020 NM 2008 10 20 UPS08M53506 1 20080518 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A RT WING O/B FLAP I/B FWD HINGE UPPER MOUNT I/B BORE FWD SPOTFACE CORRODED. RT WING O/B FLAP I/B FWD HINGE UPPER MOUNT I/B BORE FWD SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08. 2 L 7 3 4F RT A22WE 20081020 NM 2008 10 20 F3LA200800649 1 20080928 A 5321 D5361060500000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON FLOOR PANEL 221FF, FWD GALLEY AREA. MX REMOVED AND REPLACED THE FLO OR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-12-12-000-001. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND A CCEPTABLE. 2 L 7 2 4F RT A28NM 20081021 NM 2008 10 21 YENA200810150099 1 20081014 A 2911 5116404 PUMP EMB ERJ190 ERJ190100IGW 3260408 NM NR 2 HYD SYSTEM FAILED A YENA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 15 229JB 4996 1758 19000035 HYD 2 EDP FAIL IN FLT LOSS OF HYD 2 WAS DUE TO EDP NR 2, HYD 2 LO QTY AND PRESSURE EICAS MSGS. VISIBLE GAUGE LOSS OF FL UID QTY AT 0. QRH PROCEDURES FOLLOWED MANUAL GEAR RELEASE. REMOVED AND REPLACED NR 2 HYD EDP IAW 29-11-01, SERVICED NR 2 HYD SYS IAW 12-12-01-03, PERFORMED RETURN TO SERVICE TEST IAW 27-00-00, CHECK HYD SYS NR 2 FILTERS, OPS CHECK GOOD. PERFORMED LANDING FREE-FALL INSP, OPS CHECK OK, PERFOMED NR 2 ENG RUN LEAK CHECK GOOD. OPS CHECK GOOD. 2 L 7 2 4F RT A57NM 20081021 NM 2008 10 21 USAA920081739 1 20080916 A 5510 69730963 HINGE PIN BOEING 737 7373G7 1384595 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 5510 24711 MCN - MAJOR REPAIR, LT HORIZONTAL STAB INNER HINGE PIN CORRODED AT BS 1154. REPLACED LT HORIZONTAL STAB INNER HINGE PIN AT BS 1154 IAW AMERICA WEST TASK CARD I6C55039. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081762 1 20080825 A 5311 90526911 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 787, S9R. REPLACED FRAME, BS 787, S9R IAW B737 US AIRWAYS TASK CARD M 1C53002. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 DHLA2008745519 1 20081013 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 FUSE SKIN CORRODED AT BS 720A + 1", BETWEEN STR 27L & 28L. ACCOMPLISHED SKIN REPAIR AS REQUIRED, IAW B727 SRM 53-30-3 F IG 1. REF N/R 4987-1-575. 2 L 7 3 4F A3WE 20081021 NM 2008 10 21 USAA920081745 1 20080911 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT - MAJOR REPAIR - Q1 CHECK, LEVEL 2 CORROSION ON CABIN FLOORBEAM T-CAP AT BS 328, LBL 51. REPAIRED CABIN FLOORBEAM T -CAP AT BS 328, LBL 51 IAW US AIRWAYS EA 100632 AND B737 SRM 53-10-51 REPAIR 5. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081748 1 20080911 A 5311 65C323941 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT - MAJOR REPAIR, CRACK ON FUSELAGE FRAME INNER CHORD AT LOWER END BS 601, 17L. REPAIRED FUSELAGE FRAME INNER CHORD B S 601, 17L IAW US AIRWAYS EA 100638, US AIRWAYS TYPICAL REPAIR 53-62-01 & B737 AMM 20-15-05. 2 L 7 2 4F RT A16WE 20081021 EU 2008 10 21 USAA920081750 1 20080926 A 3397 WIRE AIRBUS 320 A320232 3930326 EU CABIN DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 659AW 1166 FLT NR 231 - LAS - FLOOR AISLE EMERGENCY LIGHT INOP 22L. REPAIRED BROKEN WIRE UNDER SEAT. OPS CHECK GOOD 2 L 7 2 4F RT A28NM 20081021 EU 2008 10 21 USAA920081752 1 20080927 A 2560 P209003001 FLASHLIGHT AIRBUS A321 A321211 3930370 EU CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 177US 1517 FLT NR 1121 - CLT - CABIN FLASHLIGHT AT 3L DOOR IS NOT FLASHING. MX REMOVED AND REPLACED THE FLASHLIGHT AT 3L DOOR. OP S CHECK GOOD. 2 L 7 2 4F RT A28NM 20081021 EU 2008 10 21 USAA920081753 1 20080928 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 619AW 527 FLT NR 343 - PHX - FWD FLT ATTENDANT FLASHLIGHT STOPPED CHARGING. MX REMOVED AND REPLACED THE FWD FLT ATTENDANT FLASHLI GHT BATTERY. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081021 NM 2008 10 21 USAA920081755 1 20080818 A 5330 6545766 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 SAL - MAJOR REPAIR - C19 CHECK, CRACKED FUSELAGE SKIN, BS 375, S10L. REPAIRED FUSELAGE SKIN, BS 375, S10L IAW US AIRWAY S EA 100110A. 2 L 7 2 4F RT A16WE 20081020 EA 2008 10 20 COMA0860394 1 20080919 A 5311 6013600121S FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 430CA 7461 LT FS640 FRAME CRACKED AT STR 9L. REPLACED FRAME IAW SRM AND S/B601R 53-061. 2 L 7 2 4F RT A21EA 20081020 NM 2008 10 20 AALA200802290 1 20080906 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 348AN 33087 MIA EMERGENCY LIGHT AT SEAT 4H AFT POSITION INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 4H AFT POSITION. SY STEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081020 NM 2008 10 20 AALA200802292 1 20080906 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 184AN 29594 SFO EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT A2NM 20081020 CE 2008 10 20 YAD2008F00002 1 20080913 A 3260 72644654 RELAY BEECH 1900 1900C 1154161 CE LANDING GEAR CONTAMINATED E YADA O OTHER J WARNING INDICATION NR NOT REPORTED 1 AL 03 112AX UC45 PILOT REPORTED IT TOOK 3 ATTEMPTS TO GET THE LANDING GEAR MOTOR TO OPERATE. THEN IT WORKED FINE. MX VERIFIED THAT FREE ZING THE HYDRAULIC POWER PACK RELAY WOULD CAUSE THIS PROBLEM. REPLACED THE HYDRAULIC POWER PACK RELAY. 2 L 7 2 4T RT A24CE 20081020 NM 2008 10 20 AALA200802302 1 20080907 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 794AN 30256 MIA EMERGENCY LIGHT AT SEAT 20C HAS BROKEN LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081020 SO 2008 10 20 C2XA08RI140 1 20080916 A 2400 MS2774318 RELAY EMB 145 EMB145LR 3260212 SO BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 11565 145621 FLIGHT 2654 EWR FLIGHT CREW REPORTED STRONG ELECTRICAL BURNING ODOR IN COCKPIT NOTICED AFTER LANDING. EWR MX R&R RELAY KO437 AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081020 EU 2008 10 20 UPS08153569 1 20081010 A 2611 FIRE LOOP AIRBUS A300 A300F4622R 3930360 EU MALFUNCTIONED A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 134UP 0817 ON CLIMBOUT MID, MAIN DET LOOP B FAULT ILLUMINATED ON ECAM. ALTITUDE WAS 10,500. LEVELED 11,000 FT AS CARGO SMOKE LAND ASAP ILLUMINATED ON ECAM. ACCOMPLISHED ECAM PROCEDURE WHILE RETURNING TO BIL. PERFORMED MAIN CARGO COMPARTMENT SMOKE DETECTION TEST PER MM 26-19-00- 05. NO DEFECTS NOTED. SUSPECT CONDENSATION FROM SNOW ON TOP OF SHIPPING CONTAINERS IN POSITIONS 1 AND 2. UNLOADED CONTAINERS. NO EVIDENCE OF SMOKE. 2 L 7 2 4F RT A35EU 20081020 NM 2008 10 20 UPS08553562 1 20081002 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 1520 S25-26L DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 FRAME IS DENTED AT BS 1520 BETWEEN STRINGER 25 & 26 LT. REPAIRED FRAME WITH DOUBLER IAW SRM 53-00-07 -2R5 MPI 19904 ISSUED. 2 L 7 2 4F RT A2NM 20081020 NM 2008 10 20 UPS08553515 1 20080928 A 7830 FLANGE BOEING 757 75724APF 1384969 NM THRUST REVERSER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 DURING INSPECTION, FOUND NR 2 ENGINE OUTBOARD T/R, NR 11 CASCADE VANE SEGMENT, AND NR 2 ENGINE INBOAR D T/R, NR 2 CASCADE VANE SEGMENT TO BE CRACKED ON THE FWD MOUNTING FLANGE, UPPER EDGE. REMOVED & REPLACED NR 2 ENGINE O UTBOARD T/R, NR 11 CASCADE VANE SEGMENT, AND NR 2 ENGINE INBOARD T/R, NR 2 CASCADE VANE SEGMENT IAW UPS 757 AMM 78-31-12 -4. 2 L 7 2 4F RT A2NM 20081020 NM 2008 10 20 UPS08553516 1 20081001 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM ZONE 200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 FLOOR PANEL SUPPORT PLATE IS CORRODED AT BS 1020 LBL 50 WL 208. FABRICATED NEW SUPPORT PLATE & INSTA LLED. 2 L 7 2 4F RT A2NM 20081020 NM 2008 10 20 UPS08553517 1 20080930 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM BS 1054 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 CORROSION FOUND ALONG UPPER SURFACE OF FLOORBOARD SUPPORT AT FASTENER HOLES BS 1054 RBL 242 WL 208. REMOVED AND REPLACED PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081020 NM 2008 10 20 UPS08553520 1 20081002 A 5420 BRACKET BOEING 757 75724APF 1384969 NM NR 1 NACELLE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 UPPER CONDUIT BRACKET CRACKED AT I/B SIDE OF NR 1 ENGINE PYLON AT AFT EDGE OF HYDRAULIC BAY AND STA 2 78. REMOVED, FABRICATED & INSTALLED BRACKET PER SRM 51-40-02, DWG 313NB3033. 2 L 7 2 4F RT A2NM 20081020 NM 2008 10 20 UPS08553544 1 20080916 A 5321 A402H FLOOR PANEL BOEING 757 75724APF 1384969 NM BS 900-1020 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 424UP 25369 INSPECTION TYPE:N/A MCB FLOOR PANEL AT BS 900-1020, LBL 45-65 IS DAMAGED IN 5 AREAS (MARKED). FABRICATED MCB FLOOR PANE L BS 900-1020, LBL 45-65 FROM MATERIAL A402H .400" THICK LOT 840614 IAW UPS EO B757-5320-9692-F. 2 L 7 2 4F RT A2NM 20081020 NM 2008 10 20 UPS08553545 1 20080916 A 5321 A401H FLOORBOARD BOEING 757 75724APF 1384969 NM BS 1020 PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 424UP 25369 INSPECTION TYPE:N/A MCB STA 1020 RBL 64 FLOORBOARD MISSING INSERT AND LWR SURFACE IS PUNCTURED AND DISBONDED. FABRICATE D MCB FLOORBOARD BS 900 TO BS 1020 RBL 45 TO RBL 65 OUT OF MTL A402H .400 LOT 840614 IAW UPS REPAIR MANUAL EO B757-25320 -9692-F. 2 L 7 2 4F RT A2NM 20081020 NM 2008 10 20 UPS08553546 1 20080916 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM BS 920-1000 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 424UP 25369 INSPECTION TYPE:N/A MCB 920-1000 RBL 64 SEAT TRACK FLANGE CORRODED. BLENDED TO BEYOND SRM REPAIR LIMITS WITH AUTHORIZAT ION FROM ENGINEERING. 2 L 7 2 4F RT A2NM 20081020 NM 2008 10 20 ASAA0853563 1 20081008 A 2131 2193301AC CONTROLLER BOEING 737 737890 1384527 NM CABIN PRESSURE FAULTED A ASAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 02 587AS 3858 35684 PRESSURIZATION ERATIC IN AUTO + 400 FPM SPIKED 200 FPM ON LEVEL OFF OK IN ALTERNATE PERFORMED TASK 21 13 801 CONFIRMED N R 2 CABIN PRESS FAULT. FOUND NO LOGGED FAULTS IN NR 2 PRESS CONTROLLER HISTORY & NO CURRENT FAULTS. RAN PRESSURIZATION GROUND SYS TEST ON NR 1 & 2 CONTROLLER PER MM 21 31 00, NO FAULTS FOUND. SYS OPS CHECKS NORMAL. RESET NR 2 AUTO PRESS CONTROL. 2 L 7 2 4F RT A16WE 20081020 EA 2008 10 20 MAS2008F00078 1 20080916 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 925FJ 15025 CAPTAIN REPORTED THE 2 LOWER EMERGENCY EXIT LIGHTS AT ROW 15 INOP. MX REPLACED THE EMERGENCY BATTERY PACK NR 4 AND IT O PS CHECKED GOOD. (K) 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 MAS2008F00080 1 20080914 A 3320 BALLAST CNDAIR CL600 CL6002D24 1390016 EA CABIN LIGHTS BURNED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 912FJ 15012 CAPTAIN REPORTED FWD LAV DOOR HAS A FAINT BURN ODOR. MX TROUBLESHOT ODOR COMING FROM BALLAST AT CEILING AND SIDEWALL LI GHT AT ROW 1. MX REMOVED AND REPLACED BALLAST. (K) 2 L 7 2 4F RT A21EA 20081020 NM 2008 10 20 USAA920081656 1 20080910 A 5330 6545774 SKIN BOEING 737 7374B7 1384702 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 443US 24842 FUSELAGE SKIN CRACKED AT BS 727E+4, S22L AND BS 727E+16, S23L. REPAIRED FUSELAGE SKIN AT BS 727E+4, S22L AND BS 727E+16, S23L IAW SRM 53-00-01, REPAIR 31, TEMPORARY REVISION 53-27. (K) 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 USAA920081666 1 20080903 A 5755 SKIN BOEING 737 7374B7 1384702 NM SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 456UW 25020 LT WING NR 0 SPOILER DELAMINATED ON UPPER SURFACE. REPLACED LT WING NR 0 SPOILER IAW AMM27-62-91. (K) 2 L 7 2 4F RT A16WE 20081020 CE 2008 10 20 DXTA200803272 1 20080910 A 3150 WARNING LIGHT CESSNA 500 560CESSNA 2076750 CE ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 318QS 5600418 DURING TAKEOFF ROLL AT 50 KNOTS W/S AIR O-HEAT ANNUNCIATOR LIGHT ILLUMINATED, PERFORMED ABORT. (K) 2 L 7 2 4F RT A22CE 20081020 EA 2008 10 20 MAS2008F00079 1 20080913 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM MALFUNCTIONED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 75994 2433 2014 7367 CREW REPORTED A GEAR DISAGREE MESSAGE. MX REMOVED AND REPLACED 3A PUMP, PERFORMED GEAR SWINGS, OPS CHECKED GOOD. (K) 2 L 7 2 4F RT A21EA 20081020 NM 2008 10 20 UPS08M53518 1 20080518 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 RT WING O/B FLAP I/B FWD HINGE BARREL NUT LOWER BORE CORRODED. RT WING O/B FLAP I/B FWD HINGE BARREL NUT LOWER BORE COR ROSION REMOVED AND REPAIRED AS PER CMM 57-44-08. 2 L 7 3 4F RT A22WE 20081020 EA 2008 10 20 ASOA200801326 1 20081001 A 5343 PIN CNDAIR CL600 CL6002C10 1390015 EA MLG TRUNNION CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 CORROSION AT LT MLG FWD TRUNNION PIN. 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 ASOA200801328 1 20081001 A 5343 PIN CNDAIR CL600 CL6002C10 1390015 EA MLG TRUNNION CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 CORROSION AT LT MLG AFT TRUNNION PIN. 2 L 7 2 4F RT A21EA 20081020 WP 2008 10 20 UPS08853554 1 20081009 A 3397 WIRE DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 EMERGENCY EXIT LIGHT SWITCH DOES NOT ILLUMINATE THE AMBER LIGHT WHEN SWITCH IS IN THE DISARM POSITION. FOUND BROKEN WIR E AT EMERGENCY LIGHTS BATTERY PACK. REPAIRED AS REQUIRED AND TESTED PER M/M 33-50-02-2. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 20081022 NM 2008 10 22 DHLA2008745520 1 20081010 A 5754 RIB BOEING 727 727224 1384076 NM LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LT WING, NR 2 L/E SLAT HAS 3 CRACKED INTERNAL RIBS AT SLAT STA'S 246, 252, AND 255.5 (3 CONSECUTIVE). REMOVED AND REPLA CED CRACKED RIBS BY FABRICATION OF RIBS PER SRM 57-50-2 FIG 2, 51-20-1 FIG 3, 51-10-1, AND 51-30-2. REF N/R 4987-5-298. 2 L 7 3 4F A3WE 20081022 NM 2008 10 22 DHLA2008745521 1 20081012 A 5322 SHEAR TIE BOEING 727 727224 1384076 NM CORRODED CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 MAIN FRAME AT BS 1070 HAS A CORRODED SHEAR TIE BETWEEN STR 29R & 30. ACCOMPLISHED SHEAR TIE REPAIR AS REQUIRED IAW B727 SRM 53-10-4 FIG 15. REF N/R 4987-1-606. 2 L 7 3 4F A3WE 20081022 EA 2008 10 22 HNAA0800308 1 20081008 A 5240 85240168005 SEAL DHAV DHAV DHC8 DHC8311 1386006 EA SERVICE DOOR TORN A HNAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 07 343EN 32739 32739 340 AT 18K FEET AIRCRAFT 343EN LOST CABIN PRESSURE WITH A SQUEAL FROM THE REAR SERVICE DOOR. PGV INSPECTED CABIN DOORS. CL EANED AND RESEATED DOOR SEAL AND PLACED PRESSURIZATION ON MEL. ROA MAINT REMOVED AND REPLACED REAR SERVICE DOOR SEAL AS SY IAW AMM 52-36-00. PRESSURIZED AIRCRAFT TO 5.5 DIFF WITH NO LEAKS, CLEAR MEL. 2 H 7 2 4T RT A13NM 20081022 EA 2008 10 22 VNAA2008101600004 1 20081010 A 2781 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT MALFUNCTIONED A VNAA K NONE N FALSE WARNING UK UNKNOWN 1 GL 05 720PS 10178 CREW REPORTED SLATS FAIL CAS MESSAGE IN FLIGHT DURING RETRACTION. FLAPS WERE FULLY STOWED WHEN SLATS FAILED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED CHECKS. NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081022 NM 2008 10 22 DHLA080911001 1 20080911 A 5340 STRINGER CLIP BOEING 727 727224 1384076 NM ZONE 200 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 FRAME TO STRINGER CLIP CRACKED AT BS 720C & STR 5L. REMOVED, FABRICATED, AND REPLACED STR CLIP IAW B727 SRM 51-10-1, 51 -30-2, AND 51-20-1. REF N/R 4987-2-72. 2 L 7 3 4F A3WE 20081022 NM 2008 10 22 DHLA2008745530 1 20081012 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 FUSE FRAME O/B CHORD CRACKED AT BS 188, WL 208. ACCOMPLISHED ANGLE REPAIR TO FRAME CHORD IAW B727 SRM 51-40-3 FIG 1, AT BS 188, WL 183 TO WL 216. REF N/R 4987-2-421. 2 L 7 3 4F A3WE 20081022 EA 2008 10 22 VNAA2008101700005 1 20081014 A 2421 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 1 LOW A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 202PS 7858 CREW REPORTED AMBER CAS MESSAGE IDG 1 AT 60 KNOTS. CREW ELECTED TO ABORT TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND SERVICED NR 1 IDG. CHECKS GOOD. NO FURTHER DEFECTS. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081022 NM 2008 10 22 DHLA2008745531 1 20081008 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 FUSELAGE SKIN DENTED AT BS 529.5, BETWEEN STR 17R & 18R. SKIN FOUND CRACKED UPON HFEC INSPECTION. ACCOMPLISHED FUSE SK IN DOUBLER REPAIR PER B727 SRM 53-30-3 FIG 3, BS 524.25 TO 535.75, STR 17R TO 19R. REF N/R 4987-1-36. 2 L 7 3 4F A3WE 20081022 EA 2008 10 22 VNAA2008101700006 1 20081014 A 2421 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 LOW A VNAA A UNSCHED LANDING O OTHER TO TAKEOFF 1 GL 05 202PS 7858 CREW REPORTED GEN 2 TRIPS OFF LINE WHEN TAKEOFF POWER IS APPLIED. KVA, HZ AND V ALL READ ZERO. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NR 2 IDG OIL LEVEL LOW. MAINTENANCE SERVICED NR 2 IDG OIL LEVEL. CHECKS GOOD. NO FURTHER DEFECTS. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081022 NM 2008 10 22 2008UALA06064 1 20081010 A 3397 7845243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT CONTAMINATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 FLOOR EEL LIGHTS INOP SEAT 54 TO 60 HJK. FOUND CONNECTION AT DOOR 5 CROSSAISLE FOR EMERGENCY LIGHT, WET AND SHORTING CO NNECTION. DRIED AREA & CONNECTION. ALL OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081022 NM 2008 10 22 2008UALA06065 1 20081010 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 FLOOR EEL LIGHTS INOP SEAT 33 TO 43 HJK. FOUND SHORTED EMERGENCY LIGHT AT 36 HJK. REPLACED LIGHT. ALL OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081022 NM 2008 10 22 2008UALA06067 1 20081011 A 3397 CONNECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 311UA 23672 EMERGENCY LIGHTS OUT FROM ROW 15 BACK. CLEANED LIGHT CONNECTORS. CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 20081022 2008 10 22 2008UALA06074 4 20081013 A 2565 D31517109 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 433UA 589 CABIN EMERGENCY LIGHT TEST EXT LOADS AFT L FAILED 3SV CHECK. REPLACED DOOR 2L EMERGENCY ESCAPE SLIDE. EMERGENCY LIGHT CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20081023 EA 2008 10 23 ASOA200801231 1 20080927 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REPAIRED VERTICAL BEAM AT FS 559.00 RBL 9.00 IAW BOMBARDIER REO 601R-53-41-057. COMPLIED WITH EC/TC REO 601R-53-41-097. SUPPLEMENTAL SDR CLOSED 10/15/08. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 ASOA200801241 1 20080929 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED AND REPLACED PLACARDS IAW CRJ 200 AMM 11-30-00-400-801. SUPPLEMENTAL SDR CLOSED 10/15/08. 2 L 7 2 4F RT A21EA 20081023 2008 10 23 UIEA200800332 4 20081015 A 2210 AUTOPILOT SYS BOEING 747 7472D7B 1384803 NM COCKPIT MALFUNCTIONED A UIEA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 523MC 21782 AIR TURNBACK, WHEN A/P "A" IS ENGAGED THE AIRCRAFT STARTED UNCOMMANDED LEFT ROLL. DISENGAGED "A" A/P. "B" A/P WOULD NOT ENGAGE. CYCLED YOKE SWITCH NIETHER "A" OR "B" A/P WOULD ENGAGE. FINALLY GOT "B" TO ENGAGE BUT IT WOULD NOT FOLLOW ANY MODE CONTROL PANEL COMMANDS. ITEM IS OPEN AS TO THE AIRCRAFT IS ON THE GROUND IN WORK. 2 L 7 4 4F RT A20WE 20081023 NM 2008 10 23 HALA0800814 1 20081017 A 2824 UNKNOWN BOEING 767 7673G5 1385126 NM FUEL SYSTEM MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM - MAIN TANK XFERRED FUEL 3100LBS INTO CTR TANK. BOTH MAIN TANKS REMAINED BALANCED. TOTAL QTY IND ACCURATE (MATCHED FLT PLAN FUEL QTY) CENTER TANK QTY INCREASED TO 3100LBS OVER A 2 HR PERIOD. AS PER VERBAL FROM IN BD CREW CTR TANK INCREASED JUST AFTER T/O TO APPROX 1200 LBS THEN INCREASED TO 3100 LBS. FUEL PUMPED OUT DURING FLT THE N FUEL NEVER RE-ENTERED TANK. FUEL QTY BITE CKD W/NO FAULTS. FUEL XFERRED BETWEEN TANKS & NO UNWANTED XFER. MANIFOLDS PRESS FOR 1 HR NO UNWANTED XFER. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20081023 NM 2008 10 23 UPS08553595 1 20080930 A 5247 ATTACH ANGLE BOEING 757 75724APF 1384969 NM APU INLET DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 THE APU INLET DOOR LOWER ATTACH ANGLE IS CORRODED BS 1818 STR 6R. REPAIRED PER ER 08-3098 DATED 10-1 3-08 AND UPS REPAIR AUTHORIZATION B7 57-5310-30837A. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 UPS08553644 1 20081017 A 2740 800000000016 TRIM SWITCH BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE O OTHER UK UNKNOWN 1 SO 01 456UP 25477 DIVERSION - BOTH CONTROL WHEEL'S STAB TRIM SWITCHES INOP IN FLT. NO FAULTS BALL ON SMMS PRESENT CONTINUED T/S STAB TR IM MSG APPEARS WHEN GOING TO A/P NOSEDOWN DIRECTION & AT HALF SPEED. STOPPED T/S AT START 3 BLOCK 26 D. R&R'D BRAKE PRES S SWITCH PER FM - NO HELP. R&R'D STAB TRIM LIMIT SWITCH & POSITION PER MM 27-48-01-4. REQ ADJ TEST. ALL CHECKS NORMAL PE R MM 27-48-00-5. 2 L 7 2 4F RT A2NM 20081023 GL 2008 10 23 J7S2008F00001 1 20080909 A 3246 WHEEL BOMBDR BD100 BD1001A10 1390044 GL NLG VIBRATION E J7SA C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 SW 05 520FX 20056 CREW EXPERIENCED SEVERE VIBRATION FROM THE NOSE GEAR ON TAKEOFF ROLL. MULTIPLE CAS MESSAGES DISPLAYED, INCLUDING `AOA FA IL`. CAS MESSAGES CLEARED WHEN AIRCRAFT WAS SLOWED. PERFORMED A REJECTED TAKEOFF AND TAXIED BACK TO MAINTENANCE WITH NO ADDITIONAL PROBLEMS. MX PERFORMED DOWN LOAD FROM THE MDC AND REFERRED TO FIELD SERVICE. GAINED ACCESS TO THE MOISTURE TR APS AND FOUND WATER INT THE STANDBY MOISTURE TRAP. CLEARED. RETORQUED NOSE WHEEL ASSEMBLIES AND GREASED NOSE GEAR ASSEMB LY. ALL OPERATIONAL CHECKS SATISFACTORY. (K) 2 L 7 2 4F RT T00005NY 20081023 NM 2008 10 23 EIA2008050 1 20080917 A 3397 WIRE BOEING 747 747212B 1384886 NM EMERGENCY LIGHTS DAMAGED A EIAA O OTHER O OTHER NR NOT REPORTED 1 NM 19 486EV 20888 (2) EACH EMERGENCY LIGHT ON UPPER DECK CEILING ARE OUT. EMERGENCY LIGHT ASSY U/D AFT REPLACED IAW MM 33-51-00. OPS CHE CKED NORMAL. REPAIRED WIRE AT PIN NR 3 BROKEN AT KITE ASSY IAW STANDARD PRACTICES ALSO REPAIRED PIN IAW MANUAL OPS CHECK ED NORMAL. (K) 2 L 7 4 4F RT A20WE 20081023 NM 2008 10 23 2008UALA06072 1 20081012 A 3397 58791 POWER STRIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 340UA 24244 AFT CABIN SECTION EEL FLOOR LIGHTS INOP. REPLACED POWER FEEDER CABLE TO EEL STRIP. 2 L 7 2 4F 4 F RT A16WE E21EU 20081023 NM 2008 10 23 2008UALA06075 1 20081013 A 4920 380029817 APU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DEFECTIVE A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 598UA 28751 APU INOP. FOUND APU OIL TANK EMPTY. SERVICED TO FULL. STARTED APU AND FOUND HEAVY SMOKE COMING OUT OF TAIL PIPE. AFT ER APU SHUTDOWN FOUND HUGE QUANTITY OF OIL IN APU EXHAUST SECTION. REPLACED APU. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 NM 2008 10 23 2008UALA06126 1 20081015 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 THE 1J AFT EEL STRIP DAMAGED. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 NM 2008 10 23 2008UALA06127 1 20081015 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 LT OVERWING FWD EMERGENCY EXIT LIGHT INOP. FOUND LIGHT INOPERATIVE. REPLACED LAMP. OP CHECKED OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 NM 2008 10 23 2008UALA06129 1 20081015 A 3397 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT LIGHTS INOP ROW 45 ABC THRU 57ABC. FOUND CONNECTOR UNSECURE. RESECURED CONNECTOR, OP CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 EA 2008 10 23 ASOA200801361 1 20081018 A 5534 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 RT VERTICAL STAB DRAG ANGLE CRACKED. COMPLIED WITH REO 670-55-31-018. REMOVED FASTENERS AND CUT AWAY DAMAGED AREA IAW REO. RT SIDE FWD DRAG ANGLE, PER REO 670-55-31-018. PERFORMED EDDY CURRENT INSPECTION IAW NDTM 51-20-006. NO DEFECTS NOTED. FABRICATED DOUBLER AND FILLER IAW REO 670-55-31-018. COUNTERSUNK TO MATCH FASTENER IN REO 670-55-31-018 PER SRM 51-40-11. COMPLIED WITH REO 670-55-31-018. PAINTED RT VERTICAL STAB DRAG ANGLE IAW SRM 51-25-00. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 ASOA200801364 1 20081018 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 FLIGHT COMPT FLOORBOARD AFT SUPPORT ANGLE HAS CORROSION DAMAGE. REMOVED AND REPLACED AFT SUPPORT ANGLE AT FLIGHT COMPT FLOORBOARD. STARTED DRILLING UP NEW FWD COCKPIT FLOORBOARD LAND ALL HOLES AT PILOT SIZE DRILL UP NEW FWD FLOOR SUPPORT ANGLE EXCEPT CAM-LOCK FASTENER HOLES. FWD FLOOR SUPPORT ANGLE IS READY TO BE INSTALLED IAW SRM 51-40-11. INSTALLED FWD SUPPORT ANGLE EXCEPT FOR CAM-LOCKS, ALL WORK DONE IAW 51-42-06. INSTALLED GEA CAM-LOCKS AT FWD FLOOR SUPPORT ANGLE IAW SRM-51-42-06. 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 HALA0800820 1 20081020 A 3242 BRAKE BOEING 717 717200 1383700 NM RIGHT OVERHEATED A HALA K NONE M OVER TEMP LD LANDING 1 WP 13 481HA 55126 RIGHT BRAKE OVERHEAT. PERFORMED FIM 32-47-00-801 RIGHT BRAKES OVERHEAT. NO CURRENT FAULTS ON BCU. BRAKES COOLED WITHI N NORMAL TEMPS, OK FOR SERVICE. 2 L 7 2 4F TR A6WE 20081023 NM 2008 10 23 KCSA08068 1 20081012 A 2612 FIRE SUPPRESSION BOEING 747 7472B4B 138481B NM PWA JT9 JT9D7J 52054 NE NR 3 ENGINE MALFUNCTIONED A KCSA E ENGINE SHUTDOWN A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 GL 23 710CK 21097 685873 RECEIVED FIRE WARNING ON CLIMBOUT AT 3500 FT ON NR 3 ENG FILTER BYPASS LIGHT CAME ON. OIL PRESS WENT TO "0", OIL QTY WE NT TO "0", OIL TEMP 160, N1, N2 NORMAL. FIRE HANDLE PULLED, BOTTLES WOULD NOT DISCHARGE (BOTH) HELD OVER 1 MIN. 2 L 7 4 4F 4 F RT A20WE E20EA 20081023 EA 2008 10 23 SWIA200820167 1 20081008 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 494CA 7765 FIRST OVERHEAD AISLE EMERGENCY LIGHT INOP (FLT 2558). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081024 NM 2008 10 24 K11A2008102272001 1 20081017 A 2150 A/C PACK BOEING 727 7272B6 138407J NM AC BAY INOPERATIVE A K11A B EMER. DESCENT O OTHER CL CLIMB 1 GL 23 720CK 21298 DURING CLIMBOUT CABIN ALT BEGAN TO CLIMB AT 1500 FT/MIN RT AC PACK WAS FOUND TO BE INOPERATIVE, LT PACK WORKING BUT WOUL D NOT MAINTAIN CABIN PRESS. REMOVED AND REPLACED RIGHT AC PACK FLOW CONTROL MODULATING AND SHUTOFF VALVE. 2 L 7 3 4F A3WE 20081024 NM 2008 10 24 K11A2008102372211 1 20080825 A 5320 FLOOR SUPPORT BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 COCKPIT FLOOR PANEL SUPPORT RAIL HAS SURFACE CORROSION TO BE OUT OF LIMITS. 2 L 7 3 4F RT A3WE 20081024 EA 2008 10 24 MASA2008102000740 1 20081020 A 3350 1317 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 915FJ 15015 ASH FLT 2888 PHX-AUS. EMERGENCY EXIT LIGHT AT SEAT 15A OUT. MX REPLACED LIGHT. 2 L 7 2 4F RT A21EA 20081024 NM 2008 10 24 08FDEA04354 1 20081015 A 5340 69473752 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 270FE 22035 FWD PIT BILGE BODY FRAME STR CLIP IS CORRODED BS 700, STR 26L, WL 153. REMOVED STRINGER CLIP, CORROSION ON CLIP WAS EXF OLIATED BEYOND REPAIR. FABRICATED, TREATED, AND PRIMED NEW CLIP, P/N 69-47375-2. INSTALLED CLIP REF SRM 51-30-2, PG 1- 4/BOEING DWG NR 69-47375/SRM 51-10-2, PG 1-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20081024 EU 2008 10 24 08FDEA04484 1 20081022 A 7830 491B1313000220 FRAME AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 668FE 772 NR 2 ENG OTBD T/R FWD FLANGE FOR MOUNTING RING LATCH ASSY HAS 2.750 INCH CRACK AT 12 O'CLOCK POSITION. REPAIRED CRACK O N NR 2 OTBD T/R FLANGE IAW FEDEX EA 6-7830-124135, RELEASE DATE 8 OCTOBER, 2008. 2 L 7 2 4F RT A35EU 20081024 NM 2008 10 24 08FDEA04355 1 20081015 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 270FE 22035 MAIN CABIN UPPER LOBE STA 680 STR 4L CLIP CRACKED REMOVED CLIP STA 680 STR L4 REF SRM 51-30-02 P1. INSTALLED CLIP STA 6 80 STR L4 REF SRM 51-30-02 P1. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20081024 EU 2008 10 24 08FDEA04356 1 20081015 A 5230 A5237416020800 SKIN AIRBUS 300 A300B4622R 3930312 EU CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 AFT CARGO DOOR INTERNAL SKIN IS CORRODED AT THE FWD LOWER CORNER. REMOVED CORROSION IAW A300-600 SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 51-30-00. ORIGINAL MATERIAL 0.063. REMAINING MATERIAL 0.051. MATERIAL REMOVED 0.01 1. USED UT GAUGE T8225Q. REMOVED & RE-INSTALLED PANELS 812 AR & BR 154 AR, BR, CR IAW A300-600 AMM 52-72-11-5. REMOVE D & RE-INSTALLED SEAL RETAINER IAW A300-600 AMM 52-30-18-4. REMOVED & RE-INSTALLED CAPS & SKIN IAW A300-600 SRM 51-72-1 0. MATERIAL ID 2024-T3, 0.063, PO 633758.6 IAW A300-600 SRM 52-32-00. ALODINED IAW A300-600 SRM 51-21-10. PRIMED IA W A300-600 SRM 51-23-10. REMOVED & RE-INSTALLED NR 1; NR 7 & NR 8 DOOR STOPS. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 08FDEA04485 1 20081022 A 5347 A5381206720100 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 THE 3RD LEFT SEAT TRACK INBD TRACK SUPPORT IS CRACKED AT FRAME 48. REMOVED & REPLACED THE TRACK LINK FITTING IN REF TO SRM 51-40-21. APPLIED TOP COAT IN REF TO SRM 51-23-10. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 08FDEA04462 1 20081021 A 5753 A57970100003D SKIN AIRBUS 310 A310222 3930315 EU LT WING TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 418FE 01049 343 LT WING, INBD FLAP TRAIL EDGE LWR SKIN PREVIOUS REPAIR LOCATED 54.5 INCHES FROM INBD EDGE DELAMINATED APPROX 3.0 BY 3.0 INCHES IN SIZE. REMOVED THE EXISTING REPAIR AND REPLACED BY A NEW REPAIR PER SRM 57-52-12 FIG 204. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 08FDEA04463 1 20081021 A 5753 SKIN AIRBUS 310 A310222 3930315 EU RT WING TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 418FE 01049 343 RT WING, INBD FLAP TRAIL EDGE LWR SURFACE PREVIOUS REPAIR LOCATED 17.0 INCHES FROM INBD EDGE, DELAMINATED APPROX 22.0 BY 3.0 INCHES IN SIZE. REMOVED THE EXISTING REPAIR AND REPLACED BY A NEW REPAIR PER EA 6-5750-125477. 2 L 7 2 4F RT A35EU 20081021 EU 2008 10 21 USAA920081776 1 20080929 A 2560 P4010021 BATTERY AIRBUS 320 A320231 3930325 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 620AW 052 FLT NR612 - PHX-ATL, FORWARD GALLEY EMERGENCY FLASHLIGHT OUTBOARD SIDE INOPERATIVE. MX REMOVED AND REPLACED THE FORWARD GALLEY EMERGENCY FLASHLIGHT BATTERY. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081021 NM 2008 10 21 USAA920081777 1 20080919 A 5320 654587545 THRESHOLD BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - MAJOR REPAIR - C18 C-CHECK, LEVEL 2 CORROSION ON THE R1 DOOR THRESHOLD INNER CHORD, BS 277 - BS360, S17R, WL 208 I AW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 UPS08M53542 1 20080516 A 5753 HINGE DOUG MD11 MD11F 3023600 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A LT WING O/B FLAP I/B AFT HINGE LOWER MOUNTING FOUND 02 EA BORE RUSTY. LT WING O/B FLAP I/B AFT HING E LOWER MOUNTING 02 EA BORE CORROSION REMOVED AND REPAIRED AS PER EN 1288-08. 2 L 7 3 4F RT A22WE 20081022 NM 2008 10 22 UPS08M53543 1 20080403 A 5531 SPAR DOUG MD11 MD11F 3023600 NM VERTICAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:N/A VERTICAL STABILIZER FRONT SPAR RT CUTOUT AT STA ZFS 516-443 APPROX FOUND MINOR CORROSION AS MARKED. VERTICAL STABILIZER FRONT SPAR RT CUTOUT STA ZFS 516.443 APPROX MINOR CORROSION REMOVED AND REPROTECTED AS PER SRM 51-2 1-01 VOL II REV 35, MATL REMOVED 0.005", ORG THICKNESS 0.125". FOUND WITHIN LIMIT AS PER SRM 55-00-01 VOL I FIG 1A REV 35. 2 L 7 3 4F RT A22WE 20081022 EA 2008 10 22 SWIA200820142 1 20081005 A 2611 SMOKE WARNING CNDAIR CL600 CL6002B19 1900309 EA LAVATORY MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 934SW 7722 ON CLIMBOUT "SMOKE TOILET" CAUTION MESSAGE, F/A REPORTED SMOKE (FLT 6269). INSPECTED LAV AND COMPONENTS COULD NOT FIND ANY DEFECTS. RAN BOTH ENGINES AND PRESSURIZED AIRCRAFT WITH ENGINE BLEEDS, NO SMOKE OR SMOKE SMELL NOTED ANYWHERE IN CA BIN. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 HNAA2008161000311 1 20081010 A 2163 BYLF51514 SENSOR DHAV DHC8 DHC8311 1386006 EA COCKPIT DEFECTIVE A HNAA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 336EN 36755 336 EN ROUTE TO CLT, 40 MILES EAST OF FLO THE CREW SMELLED A STRONG BURNING SMELL. FLIGHT ATTENDANT REPORTED NO SMELL OR SM OKE. THE CREW TURN ON COCKPIT LIGHTS AND COULD SEE A SMALL AMOUNT OF SMOKE. DECLARED AND EMERGENCY AND DIVERTED TO FLO . DESENDING TO 10K FEET, CREW OPENED THE FORWARD OUT FLOW VALVE AND THE SMOKE AND SMELL WENT AWAY. CANCELLED THE EMERG ENCY AND CONTINUED ONTO CLT. ARRIVED IN CLT WITH NO PROBLEMS. MAINT FOUND CIRCUIT BREAKER POPPED, UPON TROUBLESHOOTING FOUND COCKPIT ZONE TEMP SENSOR (FAN) INOP. REMOVED AND REPLACED ZONE TEMP SENSOR IAW 21-60-45. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 20081022 EA 2008 10 22 MASA2008101600731 1 20081016 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT MALFUNCTIONED A MASA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 07 512MJ 10109 ASH FLT 7228 IAD-RON. PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE. MX TROUBLESHOT AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081022 NM 2008 10 22 AALA200802356 1 20080914 A 2611 CLAMP BOEING 757 757223 1384957 NM NR 1 ENGINE LOOSE A AALA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP NR NOT REPORTED 1 SW 21 692AA 26972 TUL INFLIGHT T9677/14SEP. CREW REPORTED LT STRUT OVERHEAT STATUS IN FLIGHT. CREW TURNED OFF NR 1 ENGINE BLEED. LANDED TUL WITHOUT INCIDENT. FOUND CLAMP LEAKING AT HIGH PRESSURE DUCT FORWARD OF PRECOOLER. TIGHTENED CLAMP AT HIGH PRESSURE DUCT FORWARD OF PRECOOLER. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081210 WP 2008 12 10 AALA200802357 1 20081019 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 12 TO 16 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 13DEF FOR INOPERAT IVE EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 12 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081022 NM 2008 10 22 F3LA200800654 1 20081002 A 3350 321430 BATTERY AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHTS FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 21 931FR 52 2253 REFERENCE NON ROUTINE CO51711. DURING C3 C-CHECK, INSPECTION NOTED AFT EMERGENCY POWER SUPPLY UNIT BATTERY FAILED CAPAC ITY CHECK. MX R&R BATTERY IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 33-51-38-000-001 AND 33-51-38-400-001. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081022 2008 10 22 UIEA200800318 4 20080922 A 2210 AUTOPILOT SYS BOEING 747 7472D7B 1384803 NM MALFUNCTIONED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 523MC 21782 ATB BOTH AUTOPILOTS A AND B WILL NOT ENGAGE. BOTH TESTED OK ON GROUND. A/P A AND B PITCH AND ROLL COMPUTERS, FLIGHT C TL HYD PWR SHUT OFF SWITCHES ALL CHECKED IN ON POSITION. ACCESS BOXES INSTALLATION OCCURRED OK. MSP ELECT CONNECTORS I NSPECTION NO FAULTS. 2 L 7 4 4F RT A20WE 20081022 NM 2008 10 22 2008UALA06062 1 20081010 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EEL LIGHT SEAT 42 ABC INOP. LIGHT INOPERATIVE. REPLACED LAMP, OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081022 NM 2008 10 22 2008UALA06112 1 20081014 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT LIGHT INOP, MAIN STAIRS ILLUMINATION LIGHT. RELAMPED EMERGENCY LIGHT. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081022 NM 2008 10 22 2008UALA06113 1 20081014 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT LIGHT INOP, AT ROW 6 LEFT CEILING LIGHT. LIGHT IS INOPERATIVE. REPLACED LAMP, CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081022 NM 2008 10 22 2008UALA06114 1 20081014 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT EEL LIGHT INOP AT ROW 2A AFT LIGHT ASSY. LIGHT FOUND DEFECTIVE. REPLACED LAMP, OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081022 NM 2008 10 22 2008UALA06115 1 20081014 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 57 RIGHT. LIGHT IS FAULTY. REPLACED LAMP, OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 EA 2008 10 23 ASOA200801228 1 20080926 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED FASTENERS LT FS 460 FLOOR SUPPORT FITTING IAW SRM CRJ 200 51-42-21. REMAINING FASTENERS AND FITTING NEED REMOVE D. REMOVED REMAINING FASTENERS AND FITTING. INSTALLED NEW SERVICEABLE FITTING AT FS 460, LBL 9.0 IAW CRJ 200 SRM 51-42 -21. FITTING REQUIRES EDGE SEAL, PAINT, AND WATER INHIBITOR. SEALED REPAIRED AREA IAW SRM 51-23-00, PAINTED REPAIRED A REA IAW CRJ 200 SRM 51-25-01, APPLIED WATER DISPLACING CORROSION INHIBITING COMPOUND IAW CRJ 200 AMM TASK 51-25-56-943-0 02. SUPPLEMENTAL SDR CLOSED 10/15/08. 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 UPS08553580 1 20081002 A 5311 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 FRAME IS DENTED AT BS 1580 BETWEEN STR 23 AND 24 LT. REMOVED DAMAGED SECTION OF FRAME AND REPAIRED P ER SRM 53-00-07-1A1. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 UPS08M53590 1 20081007 A 5720 STIFFENER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:1C RT WING FIXED L/E LOWER STIFFENER XFS600 CRACKED. REMOVED AND REPLACED STIFFENER IAW SRM 51-33-01, D WG ARB2933, 51-35-01. 2 L 7 3 4F RT A22WE 20081023 NM 2008 10 23 UPS08M53626 1 20081010 A 5720 SPLICE DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:1C RT WING FIXED L/E COMPT APROX STA 562 SPLICE FOUND CRACKED. REMOVED, FABRICATED, AND INSTALLED SPLIC E IAW DWG 3954 AND MD-11 SRM 51-33-01. 2 L 7 3 4F RT A22WE 20081023 EA 2008 10 23 COMA0860389 1 20080912 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DISLODGED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 21 810CA 7370 ON CLIMBOUT, RECEIVED PAX DOOR OUTER HANDLE MSG. ACFT RETURNED BACK AND LANDED SAFELY. FOUND OUTER HANDLE POPPED OUT ON ARRIVAL. INSPECTED DOOR HANDLE AND PERFORMED OPS CHECK NO DEFECTS NOTED. (K) 2 L 7 2 4F RT A21EA 20081020 NM 2008 10 20 UPS08M53501 1 20080518 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 RT WING O/B FLAP O/B FWD HINGE LOWER MOUNT O/B BORE CORRODED. RT WING O/B FLAP O/B FWD HINGE LOWER MOUNT O/B BORE CORRO SION REMOVED AND REPAIRED AS PER CMM 57-44-09. 2 L 7 3 4F RT A22WE 20081020 NM 2008 10 20 UPS08M53502 1 20080518 A 5753 STRUCTURE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A RT WING O/B FLAP O/B FWD HINGE BARREL NUT LOWER BORE CORRODED. RT WING O/B FLAP O/B FWD HINGE BARRE L NUT LOWER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09. 2 L 7 3 4F RT A22WE 20081020 NM 2008 10 20 UPS08M53507 1 20080518 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A RT WING O/B FLAP I/B FWD HINGE LOWER MOUNT I/B BORE CORRODED. RT WING O/B FLAP I/B FWD HINGE LOWER MOUNT I/B BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08. 2 L 7 3 4F RT A22WE 20081020 EU 2008 10 20 USAA920081786 1 20080924 A 5315 D5347218920400 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 PIT - MAJOR REPAIR - S4 CHECK, LEVEL 2 CORROSION ON FLOORBEAM FR 68 - FR 69, -Y1292. REPLACED FLOORBEAM, FR 68 - FR 69, -Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 USAA920081778 1 20080915 A 5210 5079454 SKIN BOEING 737 7373G7 1384595 NM L1 DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - MAJOR REPAIR - C18 CHECK, L1 DOOR INNER SKIN CRACKED AT BS 340, S11L. REPAIRED L1 DOOR INNER SKIN CRACKED AT BS 3 40, S11L IAW B737-300 SRM 51-70-13-0G FIGURE 1. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 F3LA200800643 1 20080922 A 5321 D5367302100000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE PERFORATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 19980 DURING C4/S1 C-CHECK, INSPECTION NOTED FLOOR PANEL 151AE WAS PERFORATED. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMEN TS OF A319 SRM 53-02-00, PARA 8C. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081021 NM 2008 10 21 USAA920081761 1 20080825 A 5311 90526911 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 520, S9R. REPAIRED FRAME, BS 520, S9R IAW US AIRWAYS TASK CARD M1C530 02. 2 L 7 2 4F RT A16WE 20081022 EA 2008 10 22 SWIA200820140 1 20081007 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 479CA 7675 THIRD EMERGENCY LIGHT BACK ON CEILING INOP (FLT 2815). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 SWIA200820141 1 20081008 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER NR NOT REPORTED 1 NM 07 957SW 7829 OVERHEAD EMERGENCY LIGHT NR 3 INOP (FLT 6031). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081022 NM 2008 10 22 HNAA20081016 1 20081012 A 5522 85520057104 SKIN DHAV DHC8 DHC8102 2809003 NM RT ELEVATOR DAMAGED A HNAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 07 911HA 034 RT INBOARD END CAP MISSING PART OF BOTTOM SKIN. FERRY FLIGHT 9310 FROM FLO TO SBY. REMOVED RT INBOARD END CAP AND TWO ASSOCIATED RIBS. INSTALLED TWO NEW RIBS AND NEW END CAP PANEL IAW DRAWING 85520002. 2 H 7 2 4T RT A13NM 20081022 NM 2008 10 22 HNAA2008101700314 1 20081009 A 2920 AN8186 B-NUT VICKERS DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYS LOOSE A HNAA O OTHER K FLUID LOSS UK UNKNOWN 1 EA 07 933HA 50749 495308 134 AIRCRAFT EN ROUTE FROM LGA TO ROA, THEN DIVERTED INTO LYH DUE TO WEATHER. IN LYH CREW FOUND FLUID DRIPPING FROM NR 2 NA CELLE. MAINT CLEANED SUSPECTED AREA, GROUND RAN AIRCRAFT OPERATED FLAPS, SPOILERS, AND BRAKES. NO LEAKS NOTED AT THIS TIME. 10/10/2008 AIRCRAFT DUE INTO RON AT ROA TO UNDER GO MORE INVESTIGATION OF POSSIBLE LEAK. ROA MAINT FOUND LOOSE B -NUTS ON THE STANDBY PUMP. TIGHTED B-NUTS AS REQUIRED, OPERATED HYD SYSTEM, OPS/LEAK CHECK GOOD. 2 H 7 2 4T RT A13NM 20081022 SO 2008 10 22 C2XA08TY116 1 20081005 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO S21L TORN A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 26549 145571 A/C WAS GROUND DAMAGED IN JAX AND FERRY FLOWN TO TYS FOR REPAIR. STR 21L AT FRM 66 WAS FOUND TORN. THE DAMAGED SECTION OF STR 21L AT FRM 64-68 WAS REMOVED AND A NEW SECTION WAS CUT AND DRILLED. THE NEW SECTION OF STR 21L AND STR SPLICE A T FRAMES 61-62 WERE INSTALLED. ALL IAW EMB 145 SRM 51-40-02 AND 53-00-03. 2 L 7 2 4T RT T00011AT 20081022 NM 2008 10 22 AALA200802355 1 20080914 A 3350 ML1315 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 650AA 24608 LGA EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081022 NM 2008 10 22 USAA9200816AA 1 20080825 A 5320 654580731 STIFFENER BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 ANGLE STIFFENER CRACKED AT BS 289, S12R, WL 241 ABOVE WEB ATR1 DOOR CUTOUT. REPLACED ANGLE STIFFENER AT BS 289, S12R, W L 241 ABOVE WEB AT R1 DOOR CUTOUT IAW EA 130111. (K) 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 2008UALA06068 1 20081011 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 AFT PIT FRAME DENTED STA 1420 AT STR 26L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081022 NM 2008 10 22 2008UALA06069 1 20081011 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 AFT PIT DENTED FRAME STA 1520 BETWEEN STR 24-25 LEFT. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION FOR FRAME AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081022 NM 2008 10 22 2008UALA06080 1 20081013 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY LIGHT SEAT 24ABC INOP. LIGHT IS INOPERATIVE. REPLACED EMERGENCY LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081022 NM 2008 10 22 2008UALA06081 1 20081013 A 3397 7945243 CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY LIGHT ROW 45-55 ABC INOP. CABLE HAS MALFUNCTIONED. REPLACED EEL CABLE. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 EA 2008 10 23 ASOA200801353 1 20081015 A 5230 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 934EV 8028 UPON FURTHER INVESTIGATION FOUND CORROSION ON CARGO DOOR FLOOR EDGE MEMBER TO BE WITHIN ALLOWABLE REPAIRABLE LIMITS IAW SRM 53-00-00. BLENDED CORROSION ON CARGO DOOR EDGE MEMBER IAW SRM 51-21-06. APPLIED CONVERSION COATING, PRIMER, AND PA INT IAW SRM 51-25-06 AND 51-25-16. 2 L 7 2 4F RT A21EA 20081023 SO 2008 10 23 GLBA200810201 1 20081015 A 5330 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE CHAFED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 71GL 120071 MAJOR REPAIR - DURING SCHEDULED MAINTENANCE A CHAFE IN AN EXISITING PATCH BETWEEN FRAME 6 & 7 AT STRINGER 15L WAS FOUND. MX REPLACED CHAFED INSERT PATCH IAW SRM 51-70. 2 L 7 2 4T RT A31SO 20081023 NM 2008 10 23 UPS08M53589 1 20081007 A 5730 SPLICE DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:1C RT WING L/E SKIN STRAP XFS994 CRACKED. REMOVED AND REPLACED SKIN SPLICE STRAP IAW, SRM DWG ARB3954, 51-21-2, 51-33-01. 2 L 7 3 4F RT A22WE 20081023 SO 2008 10 23 SWIA200820178 1 20081011 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 567SW 120342 OVERHEAD EMERGENCY LIGHT AT MAIN CABIN DOOR INOP (FLT 5459). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4T RT A31SO 20081023 NM 2008 10 23 2008UALA06066 1 20081010 A 2560 KI10112 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FLASHLIGHT DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 THE 1L FLASHLIGHT NO BLINKY. REPLACED BATTERY, OPS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 NM 2008 10 23 2008UALA06071 1 20081012 A 3397 58791 POWER STRIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 340UA 24244 FIRST CLASS SECTION EEL FLOOR LIGHTS INOP. REPAIRED POWER FEEDER CABLE STRIP. 2 L 7 2 4F 4 F RT A16WE E21EU 20081023 NM 2008 10 23 2008UALA06125 1 20081014 A 5210 CYLINDER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR MISALIGNED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 548UA 25396 DOOR 4L EMERGENCY POWER ASSIST RESERVOIR RED BAND ON EMERGENCY POWER SPRING CYLINDER NOT ALIGNED PROPERLY. ADJUSTED CHE CK NUT TO ACHIEVE DIMENSIONS INDICATED ON FIG 401 VIEW A-A PAGE 402. CABLE TRAVEL CHECKED PER MM 52-11-36. CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 NM 2008 10 23 2008UALA06128 1 20081015 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 DOORWAY 2R UPPER SILL, EMERGENCY EXIT LIGHT INOP. REPLACED LAMP. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 2008 10 23 HALA0800819 4 20081020 A 2565 WARNING SYSTEM BOEING 767 767332 1382001 NM EVAC SLIDE MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 AFTER CLOSING MAIN CABIN DOOR, SLIDE LIGHT STARTED FLASHING. OPS CHECKED R1 DOOR SLIDE ARM/DISARM SYSTEM PER AMM 52-73- 00, NO DEFECTS NOTED OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20081023 EA 2008 10 23 ASOA200801359 1 20081016 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 FLOORBEAM AT LBL 9 FS 589 TO FS 621 HAS CORROSION ON OUTBOARD FLANGE FLOORBOARD ATTACH HOLES. REMOVED FLOORBEAM CAP AT LBL 9, FS 589 TO FS 621 IAW SRM 51-42-06 AND 51-42-21. DRILLED NEW SERVICEABLE FLOORBEAM CAP IAW SRM 51-40-11. OK TO IN STALL. INSTALLED NEW SERVICABLE BEAM CAP IAW SRM 51-42-06 AND 51-42-21 AND 51-42-28. REINSTALLED SERVICEABLE LOWER WEB . INSTALLED ALTERNATE FASTENERS IN FLOORBEAM CAP IAW REO 601R-53-61-2849. EC/TC REO 601R-53-61-2849 INCORPORATED. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 ASOA200801360 1 20081018 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 CABIN ENTRY DOOR DIFFICULT TO OPEN FROM INSIDE. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 ASOA200801362 1 20081018 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 LT FS 280 BEAM HAS CORROSION DAMAGE. REMOVED AND REPLACED. REPLACED WITH NEW T-BRACKET P/N BA 670-30072-15B. PICK U P ALL FASTENER HOLES IN BEAM, EXCEPT INTERCOSTALS T-BRACKET AND FWD COCKPIT BOARD LAND. FABRICATED U-BRACKET. ALL WORK DONE IAW SRM 51-24-16. PERFORMED EDDY CURRENT INSPECTION OF U-BRACKET AND LT BEAM CUT LINE. NO DEFECTS NOTED. INSTA LLED NEW FITTING & BRACKET AT PER SB 670BA-53-026. REFER TO W/O 103067 N/R 00346 FOR LEAK CHECK OF LT STBY PITOT STATIC LINE AT FS 280. RESTORED FINISH, APPLY SEALANT AND PROTECTIVE TAPE. INSTALLED NEW U-BRACKET. INSTALLED 5 CLICK BOND STAND (0900) OFFS. PERFORMED CLEAN UP AT LT SIDE FS 280 BELLY. REAPPLIED CORROSION INHIBITING COMPOUND. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 ASOA200801363 1 20081018 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 RT FS 280 BEAM HAS CORROSION DAMAGE. R&R BEAM PER SRM 51-42-06. REINSTALLED RT DRIP TRAY IAW SRM 51-42-13 SB 670BA-53- 026. REINSTALLED INTERCOSTALS IAW SRM 51-42-21. REINSTALLED PITOT STATIC LINE THRU BEAM IAW AMM 34-11-02. REPLACED WI TH NEW T-BRACKET. REINSTALLED CABLE GUIDE IAW AMM 20-21-00. REINSTALLED PULLEY BRACKET IAW AM 20-21-00. DRILLED BEAM PER SRM 51-40-11. WORK DONE IAW SRM 51-24-16. PERFORMED EDDY CURRENT INSPECTION OF U-BRACKET AND BEAM CUT LINE IAW REO 670 -53-11-047 PER NDTM 51-20-006. NO DEFECTS NOTED. INSTALLED NEW CROSSBEAM. 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 2008UALA06084 1 20081013 A 3350 767 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 566UA 26670 DOOR 4 RT EMERGENCY EXIT LIGHT INOP (EXT). LAMPS INOP. RELAMPED EMERGENCY LIGHT, SYS IS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 NM 2008 10 23 2008UALA06102 1 20081011 A 2913 6613204 PUMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HYDRAULIC SYS FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 774UA 26936 STATUS MSG HYD PUMP PRI C2. PUMP OVERHEATING AND LEAKING. INSTALLED C2 HYD PUMP. OPS CHECKED GOOD WITH NO LEAKS. RES ET BREAKER AND FILLED RESERVOIR TO FULL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081023 NM 2008 10 23 QXEA200800927 1 20080817 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE NICKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 410QX 4053 PDX C4 CHECK LOWER FUSELAGE EXTERNAL SKIN HAS 2 NICKS AT APPROX STA X41.0 BETWEEN STRINGERS 31R AND 32R. BLENDED OUT DA MAGE WITH SCOTCH BRITE PAD. HFEC INSP IAW Q400 NDTM PT 6, 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECKED FWD BLEND HI .062 LO .059, AFT BLEND HI .061 LO .058 IAW Q400 NDTM PT 1, 51-00-04. OUT OF LIMITS IAW RD8/4-53-505. INSPECTED AREA OF BLENDS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-666. PAINTED IAW Q400 SRM 51-25-05 PG 206. 2 H 7 2 4T RT A13NM 20081023 SO 2008 10 23 FDKA2008101600274 1 20081016 A 5210 DOOR EMB 145 EMB145LR 3260212 SO PAX DOOR DIRTY A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 841MJ 145448 FRL FLT 8916 JFK. MAIN PASSENGER DOOR HARD TO OPEN AND CLOSE. MX CLEANED AND LUBED DOOR, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081023 EU 2008 10 23 MAL2008F00041 1 20080926 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 340B424 DURING THE 2Y AND N4K NOTED 3 DENTS NOTED IN TAIL SECTION STA 622-853. REPAIRED IAW EO#S53229. 2 L 7 2 4T RT A52EU 20081023 NM 2008 10 23 QXEA200801064 1 20081005 A 2910 82920590003 LINE BOMBDR DHC8 DHC8402 1390042 NM HYDRAULIC SYS LEAKING A QXEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 19 407QX 4049 RNO FLIGHT 2444 LAX-RNO DURING CRUISE NR 1 HYD ISO VALVE & ROLL SPLR INBD HYD CAUTION LIGHTS ILLUMINATED. NR 1 HYD QTY INDICATED APPROX 25%. WE RAN CHECK LIST. NR 1 HYD QUANTITY SLOWLY DECREASED TO OPSI IN APPROX 30 MINUTES. UNEVENTFUL LANDING. STOPPED A/C ON RUNWAY AND SHUT DOWN ENGINES. TOWED TO GATE. REMOVED CHAFED SPOILER HYD. TUBE PN 82920590-00 3 AND REPLACED WITH NEW. CHANGED ENGINE DRIVEN PUMP. OPS CHECKS GOOD. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081023 WP 2008 10 23 ARWA20080905 1 20080920 A 2400 RHEOSTAT DOUG DC10 DC1030 3023501 WP CHART HOLDER FAILED A ARWA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 29 526MD 46998 CAPTAINS CHART HOLDER LIGHT IS CAUSING C/B E-8 TO POP. ELECT SMOKE ODOR AROUND CAPTAINS CHART HOLDER. FOUND CAPTAINS C HART HOLDER RHEOSTAT BAD. TRANSFERRED TO DMI NR 22073 AS PER MEL 33-1-0. CAT C. REPAIRED WIRE AT CAPTAINS CHART HOLDER IN ACCORDANCE WITH M/M 20-30-01. CHECKED LIGHT IN ACCORDANCE WITH M/M 33-10-00. FOUND NORMAL, CLEARED DMI NR 22073 AN D REMOVED PLACARD. 2 L 7 3 4F A22WE 20081023 2008 10 23 USAA920081857 4 20081010 A 2565 LANYARD AIRBUS 320 A320214 3930316 EU ESCAPE SLIDE MISROUTED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 113UW 1141 PIT A12 EES LT FORWARD DOOR HAS IMPROPER ROUTING OF WHITE AND YELLOW LANYARDS ON ESCAPE SLIDE RAFT. REPLACED LT FORWARD DOOR SLIDE RAFT. IAW US AIRWAYS JOB CARD 26L00025011. 2 L 7 2 4F RT A28NM 20081023 EU 2008 10 23 MAL2008F00049 1 20080926 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 340B424 DURING THE 2Y AND N4K NOTED THE LOWER FUSELAGE CENTER WING FAIRING AT STA562 HAS SEVERAL DENTS. REPAIRED DENTS ON LOWER FUSELAGE CENTER TRAILING COVER FAIRING IAW MAL EO S51031. 2 L 7 2 4T RT A52EU 20081023 NM 2008 10 23 KCSA081508 1 20081002 A 5347 SEAT TRACK BOEING 747 747122 1384872 NM COCKPIT CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 CAPTAINS AFT O/B SEAT TRACK CRACKED .5" AT STOP. 2 L 7 4 4F RT A20WE 20081023 NM 2008 10 23 AALA200802363 1 20080914 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 696AN 26976 DFW EMERGENCY LIGHT AT SEAT 30D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 30D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A2NM 20081023 2008 10 23 SRO2008F00000 4 20080926 A 2565 D31355440 SLIDE BOEING 737 737205 1384456 NM R2 DOOR INOPERATIVE A SROM K NONE L NO TEST IN INSP/MAINT 1 AL 03 733PA 23466 DURING MINI EVACUATION DEMONSTRATION TRAINING SLIDE DEPLOYED BUT DID NOT INFLATE. WAITING ON TEAR DOWN REPORT FOR FINAL DISPOSITION. 2 L 7 2 4F RT A16WE 20081023 EA 2008 10 23 TRAX200801250 1 20080930 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 R/H FS 280 FLOOR SUPPORT BEAM CORRODED. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820152 1 20080529 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 460SW 7803 FLOORBEAM AT STA 286 RBL 9 CRACKED (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081023 SO 2008 10 23 C2XA08TY114 1 20081005 A 5313 STRINGER EMB 145 EMB145LR 3260212 SO S19L TORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26549 145571 A/C WAS GROUND DAMAGED IN JAX AND FERRY FLOWN TO TYS FOR REPAIR. STR 19L AT FRM 66 WAS FOUND TORN. THE DAMAGED SECTION OF STR 19L FRM 67 TO FRM 61 WAS REMOVED AND A NEW SECTION WAS CUT AND DRILLED. FWD SECTION OF STR 19L AND STR SPLICE A T FRM`S 66-67 WERE INSTALLED. ALL IAW EMB 145 SRM 51-40-02 AND 53-00-03. 2 L 7 2 4T RT T00011AT 20081023 EA 2008 10 23 TRAX200801251 1 20080930 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 FLOOR SILL STRUCTURE AT FS 280, RBL 45 CORRODED. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 ASOA200801365 1 20081018 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN FAILED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 820AS 7188 NR 1 EMERGENCY BATTERY PACK FAILED. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820168 1 20081010 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 803SK 15062 CEILING EMERGENCY LIGHT, 2ND ONE BACK, INOP (FLT 4110). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 ASAA0853589 1 20081013 A 2161 6228145 CONTROLLER BOEING 737 737890 1384527 NM CABIN TEMP MALFUNCTIONED A ASAA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 02 559AS 8152 35178 LEFT PACK LIGHT ILLUMINATED ON RECALL EXTINGUISHED ON RESET. BITE TESTED PACK ZONE TEMP CONTROLLERS IAW AMM 21 61 00 70 0 806 002, NO FAULTS NOTED. RANG OUT OVERHEAT THERMAL SWITCHES S938 S2 S934 IAW WDM 21 51 15, NO DEFECTS NOTED. RANG O UT T472 & T488 WDM 21 51 12 21 61 51, RANG GOOD. COULD NOT DUPLICATE DISCREPANCY. ACCOMPLISHED GND TESTS SATISFACTORY. 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 WX0A070239 1 20080922 A 5330 593022U29 SKIN DOUG MD80 MD83 3023681 NM FUSELAGE DENTED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 892G 49826 FUSELAGE SKIN REPAIR - REMOVED AND REPLACED FUSELAGE BELLY SKIN STATION 1088-1183 - REFERENCE AA E58, 6079765. 2 L 7 2 4F RT 20081024 WP 2008 10 24 08FDEA04414 1 20081017 A 5740 ARB0177755 BRACKET DOUG MD10 MD1010F 3022112 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 LEFT WING FUEL PRESSURE SWITCH BRACKET IS CRACKED INBD OF THE NR 15 SLAT TRACK. REMOVED CRACKED BRACKET IAW SRM 51-33-0 1. FORMED, LOCATED & DRILLED NEW BRACKET IAW DWG ARB 0177. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED BRACKET I AW DWG ARB 0177 & SRM 51-33-01. REMOVED & RE-INSTALLED LEFT PRECHECK VALVE REF AMM 28-21-17-2. LEAK CHECKED GOOD. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 K11A2008102372206 1 20080825 A 5320 FLOOR SUPPORT BOEING 727 7272H3 138368N NM COCKPIT CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 SURFACE CORROSION FOUND ON COCKPIT FLOOR PANEL SUPPORT RAIL TO BE OUT OF LIMITS. 2 L 7 3 4F RT A3WE 20081024 NM 2008 10 24 K11A2008102372209 1 20080818 A 5313 STRINGER BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 STRINGER ANGLE CORROSION OUT OF LIMITS. 2 L 7 3 4F RT A3WE 20081024 NM 2008 10 24 SWAA085671 1 20081021 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED BETWEEN BS 727 TO BS 727A, STR 27R. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081770 1 20080926 A 5340 69374112 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - MAJOR REPAIR - C18 CHECK, CRACKED STRINGER TIE CLIP, BS 277, S15R, WL233. REPLACED STRINGER TIE CLIP, BS 277, S15 R, WL233 IAW B737-300 SRM 51-40-02 AND BOEING DWG 69-37411. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081771 1 20080917 A 5755 SPOILER BOEING 737 7373G7 1384595 NM LT WING DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - MAJOR REPAIR - C18 CHECK, LT WING NR 2 SPOILER DEBONDED, WS 304.53 - WS 353.53. REPAIRED LT WING NR 2 SPOILER DEB ONDED, WS 304.53 - WS 353.53 IAW B737-300 SRM 51-70-10-2R4 FIGURE 201. 2 L 7 2 4F RT A16WE 20081022 SO 2008 10 22 SIMA200828902 1 20081015 A 2820 2810051104 VALVE EMB 145 EMB145LR 3260212 SO FUEL VENT LEAKING A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 691AE 14500860 ON FLIGHT4222 CREW REPORTED DURING CLIMBOUT NOTICED A CLEAR FLUID LEAKING OUT OF THE RIGHT WING. CREW DECLARED AN EMERG ENCY AND ELECTED TO RETURN TO THE FIELD. AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. AIRCRAFT REM OVED FROM SERVICE. REMOVED AND REPLACED VENT VALVE, NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081022 NM 2008 10 22 DHLA20087651016 1 20081016 A 5754 CASTING BOEING 727 727264 138408M NM KRUEGER FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 765AT 23014 23014 UPON VISUAL INSPECTION FOUND THE NR 6 K-FLAP CENTER HINGE CASTING OUTBOARD SIDE AT THE ATTACH POINT FOR THE ACTUATOR ROD END CRACKED APPROX 2 INCHES IN LENGTH. K-FLAP IS TO BE CHANGED. REMOVED PART NUMBER IS 65-16227-18 SERIAL NUMBER BN18 69. UNKNOWN IS THE TIME ON AIRCRAFT. 2 L 7 3 4F A3WE 20081022 SO 2008 10 22 SIMA200829103 1 20081016 A 3350 110049 CHARGER EMB 135 EMB135KL 3260302 SO CABIN DEFECTIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 845AE 145685 CREW REPORTED ON FLIGHT 4247 EMERGENCY LIGHT AT MAIN CABIN DOOR INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AN D REPLACED BATTERY CHARGER ASSEMBLY AS PER EMB AMM 33-50-04 OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081022 NM 2008 10 22 AALA200802343 1 20080911 A 3350 LENS BOEING 737 737823 13844CB NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 969AN 29546 MIA EMERGENCY LIGHT AT SEAT 10D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 2008UALA06109 1 20081014 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT LIGHT INOP UPPER DECK CEILING ROW 13. LAMP IS UNSERVICEABLE. REPLACED LAMP. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081022 NM 2008 10 22 2008UALA06110 1 20081014 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT LIGHT INOP UPPER DECK CEILING ROW 16. LIGHT IS INOPERABLE. REPLACED LAMP, CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 EA 2008 10 23 SWIA200820153 1 20080529 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 460SW 7803 STATION 280 BEAM LBL 12 AFT FACE LOWER RADIUS AND CLIPS CRACKED (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820154 1 20080529 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 460SW 7803 STA 280 BEAM RBL 12 AFT FACE CRACKED (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820155 1 20080606 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 367CA 10069 STA 280 COCKPIT FLOOR SUPPORT HEAVILY CORRODED (C-CHECK). REPLACED SUPPORT PER SRM. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 ASOA200801334 1 20081014 A 3297 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING DAMAGED A ASOA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 883AS 7504 AFTER TAKEOFF RECEIVED "STEERING INOP" CAUTION MSG. COMPLIED WITH QRH AND LANDED WITH NWS INOP. REMOVED STEERING WIRIN G HARNESS P/N 17300-233 & INSTALLED STEERING WIRING HARNESS P/N 17300-233 ALL WORK PERFORMED IAW AMM SECTION 32-61-25, O PS CHECK REQUIRED. PERFORMED OPS CHECK GOOD. PERFORMED OPS CHECK IAW SECTION 32-61-00 & FOUND NOSE WHEEL STEERING IN GOO D WORKING CONDITION. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820164 1 20081013 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN SMOKE A SWIA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 07 413SW 7102 SMOKE AND ACRID SMELL COMING FROM MID TO REAR CABIN CEILING AREA (FLT 6391). RAN PACKS FOR ABOUT ONE HOUR INDIVIDUALLY AND TOGETHER. COULD NOT DETECT ANY SMOKE OR SMELL. 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 ASAA0843597 1 20080918 A 5320 65C335821 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 CABIN FLOOR WEB CRACKED STA 986 LBL 30. REMOVED DAMAGED WEB, FABRICATED REPAIR PARTS, LOCATED, DRILLED, INSTALLED A REP LACEMENT PANEL FLOOR WEB IAW B737 400 SRM 51 40 02 PG 293. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085631 1 20081019 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 18R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085620 1 20081019 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT JUST ABOVE FWD END OF HINGE CUTOUT . REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 08FDEA04374 1 20081016 A 5410 BEARING DOUG MD11 MD11F 3023600 NM ZONE 400 MIGRATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 576FE 48501 NR 1 PYLON AFT MOUNT FOUND WITH BEARING MIGRATION. REMOVED AND REPLACED WITH NEW HIGHER FITTING ASSEMBLY AS PER SRM 51- 31-01. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 SWAA085623 1 20081019 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085612 1 20081019 A 5315 6556804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 782SA 29808 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, BETWEEN RBL 5 TO LBL 5. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081024 EU 2008 10 24 08FDEA04363 1 20081015 A 5311 A2577174620400 FRAME AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 AFT LOWER CARGO COMPARTMENT HAS CORROSION ON THE POWER ROLLER PAN AND SUPPORT BETWEEN FRAMES 61 AND 62; LBL 41 INCH (LOW ER SURFACE). REMOVED FRAME IAW SRM 51-40-21. REMOVED CORROSION IAW SRM 51-74-10. BOTH FOUND TO BE OUT OF LIMITS IAW S RM 53-10-00. MACHINED NEW FRAME IAW DWG NR A25771746204. ALODINED IAW SRM 51-21-10. PRIMED IAW SRM 51-75-10. PAINTED IAW SRM 51-75-10. LOCATED AND DRILLED HOLES IN NEW PAN AND FRAME IAW SRM 51-40-44 AND SRM 51-72-10. PART MARKED IAW G MM 7-0-1000. INSTALLED PAN AND FRAME IAW SRM 51-40-21. INSTALLED PDU IAW AMM 25-54-26-04. OPS CHECK IAW AMM 25-52-26- 4. 2 L 7 2 4F RT A35EU 20081024 WP 2008 10 24 08FDEA04381 1 20081016 A 5340 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 MAIN CARGO DOOR NR 3 SPOOL FITTING, INBD END HOLE HAS A CRACK EXTENDING AFT. REMOVED & REPLACED SPOOLBACK UP FITTING & CENTERLINE GUIDE AFT BACK UP FITTING IAW DWG NCA 6084. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 SWAA085650 1 20081021 A 3350 PL2230LH0 STRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 472WN 33831 FOUND EEPLS STRIP LOOSE AT ROW 1. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081024 EA 2008 10 24 VNAA2008102200007 1 20081018 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A VNAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 05 221PS 7889 CREW REPORTED FLAPS FAIL CAS MESSAGE WHEN SELECTING FLAPS 30 DEGREES. FLAPS FAILED AT 20 DEGREES AND WOULD NOT MOVE. A IRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED CHECKS. NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081024 NM 2008 10 24 08FDEA04472 1 20081022 A 5313 AFA7772501 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 CENTER CARGO, LEFT STA 1701 LONGERON 50 FOUND CRACKED. FABRICATED AS PER EA 1-5310-122601. INSTALLED AS PER SRM 53-10- 00. FABRICATED AS PER DRAWING AFA7772. LONGERON REMOVED AND REPLACED AS PER SRM 53-10-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081022 NM 2008 10 22 2008UALA06111 1 20081014 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT EEL LIGHT INOP UPPER DECK SEAT 17AB FWD LIGHT ASSY. LAMP FOUND INOPERATIVE. REPLACED LAMP, ALL CHECKS G OOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20081022 NM 2008 10 22 2008UALA06116 1 20081014 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT EEL LIGHT INOP AT DOOR 5 LEFT AFT LOWER WALL EEL. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 EA 2008 10 23 N6WA200810193 1 20081019 A 3350 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA CABIN MALFUNCTIONED A N6WA K NONE N FALSE WARNING UK UNKNOWN 1 CE 03 157GJ 10230 EMERGENCY LIGHTS ON STATUS MESSAGE. CYCLED POWER, ACCOMPLISHED EMERGENCY LIGHTS RESET IAW M/M 33-51-00. 2 L 7 2 4F RT A21EA 20081023 CE 2008 10 23 EGQ2008F00000 1 20080914 A 2612 DETECTION SYS BEECH 100 B100 1152919 CE GARRTT TPE331 TPE331* 01514 WP RT FIRE DETECT MALFUNCTIONED E EGQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 17 105VY BE109 APPROX 1 MINUTE AFTER DEPARTURE, RT ENGINE FIRE LIGHT CAME ON STEADY FOR ABOUT 30 SECONDS THEN OFF, ABOUT 30 SECONDS LAT ER RT ENGINE FIRE LIGHT CAME ON AGAIN FOR 30 SECONDS THEN OFF. CREW FOLLOWED FIRE DETERMINATION PROCEDURES AND DETERMINE D THERE WAS NO FIRE AND RETURNED TO DEPARTURE AIRPORT. ALL UNEVENTFUL. THE CAUSE OF THE INDICATION INVESTIGATED. A FU LL ENGINE COMPARTMENT INSPECTION PERFORMED WITH NO INDICATIONS OF SMOKE OR FIRE. ENGINE FIRE DETECTION SYSTEM TEST PERFO RMED, ALL OPERATION NORMAL. ENGINE FIRE SENSORS WERE TESTED INDIVIDUALLY AND ALL OPERATED NORMALLY. ACFT RETURNED TO SE RVICE WITH NO FURTHER OCCURRENCES FOR THE ENGINE FIRE LIGHT. (K) 1 L 7 2 4T 3 T A14CE E2WE 20081023 EU 2008 10 23 USAA920081908 1 20081019 A 5210 FE240004 CYLINDER AIRBUS A321 A321211 3930370 EU DOOR ASSIST BLOWN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 180US 27080 3676 1525 EMERGENCY EQUIPMENT - MAINT FOUND DOOR ASSIST BOTTLE BLOWN ON FWD LEFT DOOR. REMOVED AND REPLACED DOOR DAMPER CYLINDER IAW MM 52-11-14. (K) 2 L 7 2 4F RT A28NM 20081023 EA 2008 10 23 SWIA200820149 1 20080518 A 5320 SUPPORT FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 435SW 7555 STA 280.0 FRAME RBL 9.0 INBOARD AND OUTBOARD SUPPORT CLIPS CRACKED (C-CHECK). REPLACED CLIPS. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 COMA0860387 1 20080911 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 720SW 7297 EMERGENCY LIGHTS AFT OF ROW 8 WILL NOT ILLUMINATE. REPLACED LIGHT AFT OF ROW 8 AND REPLACED ASSOCIATED POWER CONNECTOR. NO FURTHER DEFECTS. (K) 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 2008UALA06119 1 20081014 A 3350 767 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 SLIDE EMERGENCY LIGHT NOT ON AT DOOR 1 LT. LIGHT FOUND INOPERATIVE. REPLACED LAMP, OP CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 NM 2008 10 23 YENA2008089 1 20080912 A 2150 10007004 ACM EMB ERJ190 ERJ190100IGW 3260408 NM NR 1 ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 15 267JB 6165 19000065 PACK 1 INOPERATIVE EICAS DISPLAYED IN FLIGHT. QRH RESET SUCCESSFUL. ON SHORT FINAL NOTICED BURNING ODOR, TURNED OFF PA CK 1 AND ODOR WENT AWAY. REMOVED AND REPLACED NR 1 ACM IAW AMM 21-51-00. NO LEAKS NOTED OK TO CONTINUE SERVICE. (K) 2 L 7 2 4F RT A57NM 20081023 NM 2008 10 23 UPS08M53624 1 20081008 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:1C RT WING FIXED L/E BELOW NR 8 SLAT TRACK CUTOUT STRINGER FOUND CRACKED. REMOVED STRINGER, FABRICATED, AND INSTALLED IAW MD-11 SRM 51-33-01, 51-35-01 AND DWG 2933. 2 L 7 3 4F RT A22WE 20081023 NM 2008 10 23 UPS08M53643 1 20081017 A 3620 MANIFOLD DOUG MD11 MD11F 3023600 NM FAILED A IPXA K NONE O OTHER UK UNKNOWN 1 SO 01 258UP 48416 INSPECTION TYPE:N/A ATB - AIR MANIFOLD NR 2 FAILURE MESSAGE. CHECKED WIRING FROM ENG 2 BACK UP MANIFOLD PRESS SENSOR T 2-1397 TO PSC-2. WIRING CHECK OK PER MM 20-30-01-2 & WDM 36-11-03. LABEL AT SENSOR INCORRECT, SWAPPED LABELS IAW WDM 36- 11-03. SYSTEM OPS CK NORMAL IAW 36-10-02/21-08-00 & 36-23-11. 2 L 7 3 4F RT A22WE 20081023 NM 2008 10 23 2008UALA06082 1 20081013 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY LIGHT FWD AFT AND LT WALL IN THE AFT GALLEY INOP. REPLACED FWD AND AFT LAMP, OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 NM 2008 10 23 2008UALA06091 1 20081011 A 4920 380029817 APU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 545UA 25323 APU HAS LOW BLEED AND HIGH EGT. REPLACED APU. NO LEAKS NOTED, NO FAULTS NOTED. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 NM 2008 10 23 2008UALA06099 1 20081013 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 ENGINE LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 793UA 26946 NR 2 IDG LEAKING FROM CASE. IDG FOUND LEAKING. REPLACED NR 2 ENG IDG, OPS & LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081023 NM 2008 10 23 2008UALA06100 1 20081009 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 1 ENGINE FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 226UA 30226 NR 1 ENGINE IDG (DIFFERENTIAL PRESSURE INDICATOR) DPI IS EXTENDED. DPI EXTENDED. REPLACED NR 1 IDG, OP TESTS GOOD. OK AY FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081023 NM 2008 10 23 2008UALA06101 1 20081013 A 8012 10011003 START VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 1 ENGINE FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 794UA 26953 ENGINE START VALVE L EICAS. ENG START VALVE FOUND FAULTY. REPLACED NR 1 ENGINE AIR STARTER VALVE. OPS CHECKED GOOD. VERIFIED & CLEARED ALL EICAS MESSAGES AS REQUIRED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081023 NM 2008 10 23 2008UALA06103 1 20081011 A 8011 8110503 STARTER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE RT ENGINE MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 224UA 30225 R ENG AUTO START MALFUNCTION, MANUAL START START VALVE EICAS MSG. RESET C/B'S, NO HELP. GOOD DUCT PRESS, NO ROTATION. APPEARS VALVE NOT OPENING. REPLACED STARTER ASSY. OP CHECKS NORMAL. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081023 EU 2008 10 23 2008UALA06120 1 20081014 A 5320 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 442UA 780 STR CLEAT FRAME 33 ST43L-R IS CORRODED IN FWD PIT. MAJOR REPAIR ACCOMPLISHED. REPLACED CLEAT. 2 L 7 2 4F 4 F RT A28NM E40NE 20081023 NM 2008 10 23 2008UALA06121 1 20081014 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 FWD CARGO PIT FUSELAGE FRAME AT STA 660 IS DENTED IN UPPER FLANGE AT STR 24L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAG ED SECTION & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 NM 2008 10 23 HALA0800821 1 20081021 A 3260 285T003117 MODULE BOEING 767 7673G5 1385126 NM LANDING GEAR FAULTY A HALA K NONE N FALSE WARNING LD LANDING 1 WP 13 585HA 24257 FROM TOP OF DESCENT UNTIL GEAR DOWN, INTERMITTENT MASTER WARNING AND EICAS MSG 'GEAR NOT DOWN'. T/S PER FIM 31-51-00 FI GURE 109A STEP 34 REPLACED LANDING CONFIGURATION MODULE PER AMM 31-51-04. 2 L 7 2 4F RT A1NM 20081023 NM 2008 10 23 QXEA200801108 1 20081009 A 6120 697072003 GOVERNOR BOMBDR DHC8 DHC8402 1390042 NM NR 2 ENGINE MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 19 408QX 16029 4050 SEA FLIGHT 2283. NR 2 PROP WAS SLOW TO COME OUT OF FEATHER DURING ENGINE START, 15-20 SECONDS. R&R NR 2 ENG OVERSPEED GOVERNOR IAW Q400 AMM 61-20-26-400-801. LEAK CHECK AND OPS CHECK GOOD. HEAT SHRINK IAW Q400 HS 61-0028. PERFORMED FUN CTIONAL TEST OF PROP TIME TO UNFEATHER IAW Q400 AMM 61-20-00-720-801. FUNCTIONAL TEST GOOD. NR 2 PROP UNFEATHER IN APP ROX 10 SECONDS. NO FURTHER DEFECTS. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081023 NM 2008 10 23 QXEA200800916 1 20080817 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 410QX 4053 PDX C4 CHECK. RT INBD SEAT TRACK NR 13 IS CORRODED BETWEEN X268. BLENDED CORROSION IAW RD8/4-53-884 PG 1,2,6 STEP 1. MAX MATERIAL REMOVED. .015" 8/4-53-884 PG 2 FIG A-A. HFEC INSPECTED IAW D8 400 NDTM PT 6, 51-00-01. NO CRACKS NOTED. ALODINED PER RD 8/4-53-884 STEPS 3-6. 2 H 7 2 4T RT A13NM 20081023 WP 2008 10 23 AALA200802423 1 20080923 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 242AA 49255 LGA EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 18 TO 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 18 TO 26. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081023 EU 2008 10 23 MAL2008F00046 1 20080926 A 5512 SKIN SAAB SF340 340B 7860101 EU HORIZONTAL STAB DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 340B424 DURING THE 2Y AND N4K NOTED 13 DENTS IN UPPER SKIN OF RT HORIZONTAL STABILIZER. REPAIRED IAW EO S55017 & S55160. 2 L 7 2 4T RT A52EU 20081023 NM 2008 10 23 AALA200802407 1 20080921 A 3350 LIGHT BOEING 767 767323 1385205 NM SEAT 20B INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 383AN 26995 MIA EMERGENCY LIGHT AT FORWARD SEAT 20B INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD SEAT 20B. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081023 NM 2008 10 23 AALA200802409 1 20080921 A 1100 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 601AN 27052 DFW EMERGENCY LIGHT EXIT PLACARD AT RT HAND OVERWING DAMAGED. REPLACED EXIT PLACARD FOR EMERGENCY LIGHT AT RT HAND OVER WING. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 QXEA200801110 1 20081006 A 2710 82410608007 CONTROL PANEL BOMBDR DHC8 DHC8402 1390042 NM AILERONS MALFUNCTIONED A QXEA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 19 407QX 4049 PDX FLIGHT 9850. RT AILERON TRIM SWITCH STUCK WHEN APPLYING TRIM. TRIM RAN AWAY TO THE RT. WAS ABLE TO NEUTRALIZE TRI M BY APPLYING LT AILERON TRIM FIRMLY. THE SWITCH APPEARED TO BE STUCK. MX R&R THE AILERON/RUDDER TRIM CONTROL-PANEL PE R Q400AMM TASKS 27-13-16-000-801 AND 27-13-16-400-801. OPS TEST GOOD. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081023 EU 2008 10 23 MAL2008F00047 1 20080926 A 5522 SKIN SAAB SF340 340B 7860101 EU RT ELEVATOR PUNCTURED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 340B424 DURING THE 2Y AND N4K THE RT ELEVATOR UPPER SKIN PUNCTURED AT HS68.66. REPAIRED IAW EO S53229. 2 L 7 2 4T RT A52EU 20081023 NM 2008 10 23 AALA200802426 1 20080923 A 3350 HOUSING BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 DFW EMERGENCY LIGHT AT LT NR 1 DOOR CLOSET DAMAGED. REPLACED LIGHT HOUSING ASSEMBLY FOR EMERGENCY LIGHT AT LT NR 1 DOOR CLOSET. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081023 CE 2008 10 23 GUU2008F00058 1 20080930 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 87557 UE246 DURING SCHEDULED ROUTINE MX DISCOVERED LT ELEVATOR OTBD HINGE BRACKET CORRODED. REPLACED LT OTBD ELEVATOR HINGE BRACKET . 2 L 7 2 4T RT A24CE 20081024 EA 2008 10 24 VNAA2008102200008 1 20081019 A 3411 DRAIN CNDAIR CL600 CL6002B19 1900309 EA NR 2 PITOT CONTAMINATED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 213PS 7879 CREW REPORTED DURING TAKEOFF ROLL, CAPTAIN'S PFD FLASHED AN AMBER MESSAGE NEAR AIRSPEED TAPE: "IAS". CREW ELECTED TO AB ORT TAKEOFF AT AROUND 100 KNOTS. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND ADC NR 2 PITOT DRAIN FULL OF WATER AND REMOVED WATER CONTAMINATION FROM P2 SYSTEM. MAINTENANCE PERFORMED CHECKS AND REJECTED TAK EOFF INSPECTION. NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081024 NM 2008 10 24 08FDEA04473 1 20081022 A 5311 651631836 FRAME BOEING 727 7272D4 138407U NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 CABIN BS 360 S4R FRAME INNER CHORD WORN. BLENDED AREA, FOUND OUT OF LIMITS IAW SRM 53-10-04. FABRICATED REPAIR PART IAW SRM 53-10-04, REMOVED DAMAGE AND INSTALLED FARICATED REPAIR PART IAW SRM 53-10-4. TREATED AND PRIMED. THIS IS CLASSIFI ED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081024 NM 2008 10 24 08FDEA04475 1 20081022 A 5347 SEAT TRACK BOEING 757 75723A 1384967 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 MAIN CABIN SEAT TRACK, BS 1540-1640, LBL 45, I/B FLANGE HAS SEVERAL MIS-DRILLED HOLES. REMOVED AND REPLACED SEAT TRACK ASSY, BS 1540-1640, LBL 45, IAW SRM 51-40-02. REPLACEMENT SEAT TRACK WAS DRILLED UP AND SCALLOPED ON MAE TRAVELER NR T8 /758323. 2 L 7 2 4F RT A2NM 20081024 NM 2008 10 24 08FDEA04478 1 20081022 A 5320 65295486 PAN BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 PASSENGER CABIN BULKHEAD 1183 DITCH PAN, LBL 28 CRACKED. 2 L 7 3 4F A3WE 20081024 NM 2008 10 24 WX0A070244 1 20081012 A 3350 L2019115 LIGHT DOUG MD80 MD83 3023681 NM CABIN INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 879GA 53486 EMERGENCY LIGHT ASSY AT 36C - DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPOR TED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REPLACED THE EMERGENCY LIGHT ASSEMBLY AS REQUIRED. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETUR NED TO SERVICE. 2 L 7 2 4F RT 20081024 NM 2008 10 24 DL76L081365 1 20081015 A 8012 START VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 192DN 28449 724715 AFTER PUSHBACK LEFT ENGINE WILL NOT START. MANUALLY OPENED START VLV AND HAD ROTATION. REPLACED NR 1 ENGINE START VALV E PER AMM. STARTED NR 1 ENGINE, VALVE OPERATES NORMALLY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081024 NM 2008 10 24 DL75A081366 1 20081015 A 4920 ENGINE BOEING 757 757212 1384951 NM APU INOPERATIVE A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 751AT 22702 23125 ATTEMPTED 3 APU STARTS AT FL 370, APU WOULD NOT START, DISPLAYED APU FAULT EICAS MSG AFTER EACH ATTEMPT, APU STARTED OK ON GRND. FWD APU TO MCO AND PLACARD PER MEL 49-11-01A. 2 L 7 2 4F RT A2NM 20081024 NM 2008 10 24 DL76G081346 1 20081011 A 2150 HEAT EXCHANGER 1942744 BOEING 767 767324 1385203 NM RIGHT CRACKED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 394DL 53453 27394 RT PACK INOP ON BOTH APU AND ENG BLEEDS. WORKED FINE ON APU AT GATE. FAILED WHEN SWITCHED TO ENG BLEED. AT GATE RT PA CK CHECKED NORMAL WITH APU AIR. FOUND TWO INCH CRACK IN RT HEAT EXCHANGER REHEATER. REMOVED AND REPLACED REHEATER PER AMM. LEAK CHECK GOOD, MPN 194274-4. 2 L 7 2 4F RT A1NM 20081022 NM 2008 10 22 ABXA200810170253 1 20080929 A 5312 148T31212 BULKHEAD BOEING 767 767281 1385109 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 DURING INSPECTION, LOWER TWO FASTENER HOLES OF RIGHT CHORD SHOWED CRACK INDICATION. CRACK LENGTH = .0625 INCH. REPLACE D CHORD IAW EA 53800002-003. 2 L 7 2 4F RT A1NM 20081022 SO 2008 10 22 CHQA200800199 1 20081015 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO RROYCE AE3007 AE3007A1P 54571 EA CARGO BAY FAULTY A CHQA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 11 296SK 15709 153 145514 CAE311464 FLIGHT 3048, RDU TO LGA. AT FL270 WHILE OVER RIC, THE FLIGHT CREW RECEIVED A BAGG SMOKE EICAS INDICATION. THE QRH WAS FOLLOWED, AND AFTER PRESSING THE BAGG SMOKE BUTTON THE MESSAGE WENT OUT AFTER TWENTY SECONDS. THE AIRCRAFT DIVERTED TO IAD AND LANDED WITHOUT INCIDENT. THE BAGGAGE COMPARTMENT WAS INSPECTED BY FIRE CREWS WITH NO SIGNS OF SMOKE OR FIRE PRE SENT. MAINTENANCE INSPECTED AND TESTED THE BAGGAGE COMPARTMENT SMOKE DETECTORS WITH NO DEFECTS NOTED AND THE AIRCRAFT W AS RETURNED TO SERVICE. EI003588 WAS ISSUED TO THE AIRCRAFT ON THE 16TH TO FURTHER TROUBLESHOOT THE BAGGAGE COMPARTMENT SMOKE DETECTION SYSTEM AND LED TO THE REMOVAL OF BOTH SMOKE DETECTORS ON THE 16TH. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081022 EA 2008 10 22 ASOA200801332 1 20081013 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA DOOR OUT OF POSITION A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 835AS 7258 FLIGHT ATTENDANT CLOSED DOOR, PLUNGER PULLED OUT, INNER HANDLE CAME OUT. GATE RETURN. 2 L 7 2 4F RT A21EA 20081022 EU 2008 10 22 ASOA200801333 1 20081014 A 3350 COVER AEROSP ATR72 ATR72 EU CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 EMERGENCY LIGHT COVER BROKEN BY PASSENGER. 2 H 7 2 4T RT 20081022 EA 2008 10 22 ASOA200801335 1 20081014 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR ACTIVATED A ASOA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 824AS 7203 PAX DOOR OUT HANDLE CAUTION DOOR VERY DIFFICULT TO OPEN. FLT 4919 DEL 26 MINS. 2 L 7 2 4F RT A21EA 20081022 NM 2008 10 22 SWAA085576 1 20081014 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085577 1 20081014 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085580 1 20081012 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 360, STR 28L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085581 1 20081014 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 402WN 29814 DURING SCHEDULED MV2 CHECK, FOUND EGRESS LENS COVER MISSING AT LT FLOOR ROW 10. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085582 1 20081014 A 3350 417A5700 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 408WN 27895 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT FLOOR LIGHT INOP AT ROW 23 ABC. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085583 1 20081014 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 472WN 33831 FOUND EMERGENCY EXIT LIGHT LENS COVER MISSING. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085589 1 20081014 A 3297 W6124052622 WIRE BOEING 737 7377H4 1384404 NM E&E BAY UNSECURE A SWAA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 SW 29 248WN 32509 AIR TURNBACK, LANDING GEAR WOULD NOT RETRACT AFTER T/O GEAR LEVER WOULD NOT GO PAST "OFF" POSITION. WHILE RAISING FLAPS GEAR WARNING HORN SOUNDED. WITH FLAPS FULLY RETRACTED, GEAR SYSTEM 100 PERCENT NORMAL. SECURED S1050 SENSOR WIRE PER MM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085590 1 20081016 A 5610 571761 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 29 389SW 26592 F/O R1 WINDOW ARCED DURING FLIGHT. REMOVED AND REPLACED R1 WINDOW PER MM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085591 1 20081015 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 782SA 29808 DURING SCHEDULED 8Y CHECK, FOUND AFT GALLEY FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 36 TO RBL 5. REPAIRED BEAM PER SW A EA. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085592 1 20081015 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 782SA 29808 DURING SCHEDULED 8Y CHECK, FOUND AFT GALLEY FLOORBEAM CORRODED AT BS 947, BETWEEN LBL 5 TO RBL 5. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081022 2008 10 22 SWAA085593 4 20081015 A 2565 416A2100 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 463WN 32467 FOUND L1 DOOR EMERGENCY EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085598 1 20081013 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 787, BETWEEN RBL 10 AND RBL 19. REPAIRED FRAME PER SRM . 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085599 1 20081014 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 986 BETWEEN RBL 50 TO LBL 50, WL 208. REPAIRED BEAM PER PAE ER. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085601 1 20081014 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 54. REMOVED AND REPLACED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085602 1 20081014 A 5753 6573732 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED 14Y CHECK, FOUND LEFT WING O/B AFT FLAP INBOARD SIDE DELAMINATED AT TRAILING EDGE. REMOVED AND REPLACE D FLAP PER MM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085603 1 20081014 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085604 1 20081014 A 5311 65C25228 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085609 1 20081014 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 2008UALA05853 1 20080920 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 817UA 873 FLOORBEAM 70 CORRODED IN AREA OF FRAME 66 AFT OF LAV LOCATED FORWARD DOOR 2 LEFT. REMOVED CORROSION. VERIFIED CORROSIO N WAS REMOVED AND IS WITHIN LIMITS. TREATED PRIMED AND PAINTED. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081023 NM 2008 10 23 QXEA200801111 1 20081006 A 3230 LANDING GEAR BOMBDR DHC8 DHC8402 1390042 NM MLG NOISY A QXEA O OTHER E VIBRATION/BUFFET CL CLIMB 1 NM 19 406QX 4048 SEA FLIGHT 2265. LOUD BANG HEARD FORWARD RT SIDE OF COCKPIT JUST AS NG BEGINS TO RETRACT. GEAR SEQUENCE NORMAL DURING RETRACTION AND EXTENSION WITH NO ABNORMAL POSITION INDICATION. UNEVENTFUL LANDING. FERRIED TO PDX FOR REPAIRS. BLED A LTERNATE EXTENSION SYSTEM, SOUND WAS DUPLICATED AND CORRECTION CONFIRMED. PERFORMED NORMAL AND ALTERNATE GEAR OPS CHECK S IAW Q-400 AMM 32-31-00-710-801 AND 32-34-00-710-801. ALL CHECKS NORMAL, NOISE NO LONGER PRESENT. RETURNED TO SERVICE . NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081023 NM 2008 10 23 AALA200802342 1 20080912 A 3350 0202503001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 784AN 29588 NRT EMERGENCY LIGHT AT FIRST CLASS CLOSET DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FIRST CLASS CLOSET DO OR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081023 NM 2008 10 23 KCSA081507 1 20081002 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 1720 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 CORROSION ON BS 1720 FUSE FRAME REINFORCEMENT CHORD I/B OF STR-42R. 2 L 7 4 4F RT A20WE 20081023 EA 2008 10 23 TRAX200801244 1 20080929 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 JOB 8752811 OPERATION 184 RT UPPER OBLIQUE ANGLE INTERCOSTAL IN AFT EQUIPMENT BAY FROM FS 621 TO FS 625 IS CRACKED IN RA DIUS. 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 AALA200802374 1 20080918 A 3397 CONNECTOR BOEING 767 767223 1385123 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 322AA 22323 JFK EMERGENCY LIGHT AT SEAT 11H INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 11H. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081023 EU 2008 10 23 MAL2008F00040 1 20080926 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 322-392 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 340B424 DURING THE 2Y AND N4K NOTED 32 DENTS NOTED IN THE LT FUSELAGE STA 322-392 AND 5 DENTS NOTED ON THE RT FUSELAGE STA 353-3 92. REPAIRED IAW EO#S53619. 2 L 7 2 4T RT A52EU 20081023 EA 2008 10 23 SWIA200820150 1 20080518 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 435SW 7555 INTERCOSTAL CRACKED APPROX 18 INCHES BELOW ENGINE BEAM LEFT SIDE BETWEEN FS 621 AND FS 625 (C-CHECK). RE-INSPECT AT EVE RY C-CHECK PER REO. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820151 1 20080518 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 435SW 7555 INTERCOSTAL CRACKED APPROX 12 INCHES BELOW ENGINE BEAM LEFT SIDE BETWEEN FS 621 AND FS 625 (C-CHECK). RE-INSPECT AT EVE RY C-CHECK PER REO. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 TRAX200801252 1 20080930 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA BS 310-349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 MINOR CORROSION ON FLOOR SUPPORT RAIL INBD OF ASD @ FS 310-349. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 TRAX200801254 1 20080930 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 R/H 280 WEB CORRODED. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 TRAX200801255 1 20080930 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 FWD FLOOR SUPPORT ANGLE AT FS 280 CORRODED. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820156 1 20080606 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 367CA 10069 STA 280 LOWER BULKHEAD WEB IS CORRODED (C-CHECK). REPLACED LOWER WEB PER REO. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820157 1 20080606 A 5320 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 367CA 10069 STA 280 CROSSBEAM IS CRACKED AT LBL 9 AND RBL 9 (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820158 1 20081010 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 760SK 10223 EMERGENCY LIGHT ROW 9 INOP (FLT 5971). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820159 1 20081011 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 925SW 7682 EMERGENCY LIGHTS INOP AFT OF WINDOW EXIT (FLT 6703). FOUND LOOSE CONNECTION AT ROW 8, TIGHTENED CONNECTION. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820160 1 20081009 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 986CA 7174 NR 1 CEILING EMERGENCY FLOOD LIGHT INOP (FLT 2771). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081022 NM 2008 10 22 2008UALA05863 1 20080924 A 2120 CD01109F2 FILTER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE E&E BAY FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 774UA 26936 EQUIPMENT COOLING EICAS. REPLACED EQ COOLING AIR FILTER. MESSAGE CLEARED. OKAY FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081022 NM 2008 10 22 2008UALA06085 1 20081013 A 5311 FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 AFT CARGO BS 1560 LBL 20-30 FRAME UPPER CHORD CRACKED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, INSTALLED ANGLE REPA IR. 2 L 7 4 4F 4 F RT A20WE E24NE 20081022 NM 2008 10 22 2008UALA06086 1 20081013 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 793UA 26946 BOTH EMERGENCY LIGHTS OUT ON SEAT 2F. BOTH LIGHTS INOP ON SEAT 2F. REPLACED LAMP, TESTED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081022 NM 2008 10 22 2008UALA06087 1 20081013 A 3260 SENSOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT MLG DEFECTIVE A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 346UA 24250 LEFT MLG UNSAFE "RED" LIGHT ILLUMINATED. RTFL. FOUND SENSOR S72 GROUND WIRE OPEN AND REPLACED SENSOR. RESISTANCE CK' D GOOD. INSPECTED SENSOR INSTALLATION. ACCMP GEAR EXT RETRACT TEST. 2 L 7 2 4F 4 F RT A16WE E21EU 20081022 NM 2008 10 22 2008UALA06092 1 20081012 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 EMERGENCY EEL LIGHT STRIP INOP FROM SEAT 5AB TO 6AB. REPLACED FLEX EMERGENCY LIGHT STRIPS. OPS CHECKED OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081022 NM 2008 10 22 2008UALA06094 1 20081012 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SEAT 1EF INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 EMERGENCY LIGHT FLEX STRIP LIGHT INOP AT SEAT 1EF. REPLACED EMERGENCY LIGHT STRIP. OPS CHECKED OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081022 NM 2008 10 22 2008UALA06095 1 20081011 A 3610 79027013 SHUTOFF VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE BLEED AIR SYS MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 674UA 29242 724652 LT ENG REACHED 490 DEG DURING SLUGGISH START. TAXI TEMPS ELEVATED ALSO CLIMB/CRUISE NORMAL. REPLACED NR 1 ENG HPSOV & HP CONTROLLER. OPS CHECK GOOD. REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081022 NE 2008 10 22 2008UALA06097 2 20081012 A 7261 CARBON SEAL BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 ENGINE LEAKING A UALA O OTHER W K INADEQUATE Q C FLUID LOSS NR NOT REPORTED 1 WP 29 215UA 30221 NR 2 ENGINE LEAKING OIL PAST IDG CARBON SEAL. REPLACED IDG & RELATED SEALS. VERIFICATION FLIGHT CONFIRMS NORMAL OPERAT IONS. OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081022 2008 10 22 2008UALA06104 4 20081013 A 3417 10621533 ADC BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NR 2 MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 938UA 26671 R INERTIAL REFERENCE SYSTEM FAILURE. RTFL. REPLACED NR 2 ADC. CHECKS OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 20081022 EU 2008 10 22 2008UALA06105 1 20081013 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 442UA 780 FUSELAGE DENT AT FRAME 1, LT SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 20081022 NM 2008 10 22 2008UALA06106 1 20081013 A 2913 6613204 PUMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HYDRAULIC SYS LEAKING A UALA O OTHER W K INADEQUATE Q C FLUID LOSS IN INSP/MAINT 1 WP 29 212UA 30218 CREW COMMENTS: HYD QTY LOW LEFT. AT 9 HOURS FLYING QTY .37 AT 8 HOURS WAS .40. UPON ARRIVAL FOUND COWLS DRIPPING WITH HYD FLUID, DRY MOTORED AND FOUND NR 1 ENGINE DRIVE PUMP LEAKING. REPLACED NR 1 ENGINE DRIVE PUMP. REPLENISHED LT HYDR AULIC SYSTEM TO FULL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081022 NM 2008 10 22 2008UALA06107 1 20081014 A 3350 COVER BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 MAIN DECK SEAT 5F EMERGENCY EXIT MISSING COVER PLATE. EEL STRIP REPLACED AND OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 CE 2008 10 23 GLBA200810171 1 20081016 A 5511 MS20470AD5 RIVET BEECH 1900 1900D 1154162 CE HORIZ STAB MISSING A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 173YV UE173 MAJOR REPAIR - DURING ROUTING SCHEDULED MAINTENANCE A CONFORMITY INSPECTION WAS PERFORMED AND FOUR RIVETS WERE FOUND MIS SING ON THE HORIZONTAL STABILIZER SPAR CENTER WEB. MAINTENANCE INSTALLED FOUR MS20470AD5 RIVETS IDENTIFIED AS "A" IN ST EP 23 OF THE BEECH SRM 55-91-02. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1. THE WEB REPAIR CONFORM WITH MAIN SPA R CENTER WEB REPAIR AS SHOWN IN BEECH 1900 SRM 55-91-02. 2 L 7 2 4T RT A24CE 20081023 NM 2008 10 23 HALA0800815 1 20081017 A 3610 2780539105 ISOLATION VALVE BOEING 767 7673G5 1385126 NM LEFT MALFUNCTIONED A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 585HA 14910 14910 24257 ETOPS SIGNIFICANT SYSTEM - BTB - 36100301 - BTB - AFTER ENG START CLOSING LEFT ISLN VLV LIGHT REMAINED ILLUMINATED WITH LEFT ISLN VLV EICAS MSG. COULD NO RESET. REMOVED & REPLACED LT ISOLATION VLV PER AMM 36-11-04. OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 20081023 EA 2008 10 23 SWIA200820161 1 20081008 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE O OTHER NR NOT REPORTED 1 NM 07 709SK 10159 LAST AFT EMERGENCY DOME LIGHT INOP (FLT 6366). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820162 1 20081010 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 956SW 7825 AFT CABIN EMERGENCY CEILING FLOOD LIGHT INOP (FLT 6504). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820163 1 20081008 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 927SW 7693 FORWARD EMERGENCY FLOOD LIGHT INOP (FLT 5970). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081024 WP 2008 10 24 08FDEA04352 1 20081015 A 5730 ARB1067 SKIN DOUG DC10 DC1030F 3023504 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 LT WING L/E CRACK ON EXT LOWER SKIN. 2 L 7 3 4F RT A22WE 20081024 EU 2008 10 24 08FDEA04464 1 20081021 A 5753 SKIN AIRBUS 310 A310222 3930315 EU LT WING TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 418FE 343 LT WING, INBD FLAP TRAILING EDGE UPPER SURFACE PREVIOUS REPAIR LOCATED 44.0 INCH FROM OTBD EDGE DELAMINATED APPROX 3.0 B Y 3.0 IN SIZE. REMOVED EXISTING REPAIR BY A NEW REPAIR PER SRM 57-52-12 FIG 204. 2 L 7 2 4F RT A35EU 20081024 WP 2008 10 24 08FDEA04373 1 20081015 A 3620 ABM7009813 SENSE LINE DOUG DC10 DC1030F 3023504 WP LEAKING A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 310FE 48299 PNEU SUPPLY RED FAIL LIGHT ILLUMLINATED. PRESS GAUGE SYS NR 2 VERY HIGH, 30 PSI WOULD NOT GO DOWN WITH THROTTLE TO IDLE , SUPPLY PNEU SWITCH OFF, FINALLY PSI WENT TO 20 PSI. FOUND LEAKS ON LINE GOING TO FAN AIR VALVE. REMOVED AND REPLACE D SENSE LINE PER SMP. LEAK CHECKS GOOD. FOUND LEAK ON LINE INSIDE PYLON GOING TO HP SENSOR, THIS LEAK IS IN THE BAY W ITH THE D1-29 SENSOR. REMOVED AND REPLACED LINE PER SMP LEAK CHECKS GOOD. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 SWAA085630 1 20081019 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085624 1 20081019 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 54. REPAIRED BEAM PER PAE ER. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 08FDEA04382 1 20081016 A 5330 65545772 SKIN BOEING 727 727227 1384078 NM BS 720-720D DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 491FE 21529 FUSELAGE LT/RT, FWD WING TO BODY ATTACHMENT AREAS, SCRIBE MARKS IN SKIN STA 700, 72D STR 19L TO STR 19R. BLEND OUT DAMA GE IAW SRM 51-10-1 AND UT AREA IAW NDTM 51-00-00. FOUND SKIN OUT OF LIMITS IAW SRM 53-30-1. CUT OUT DAMAGE AREA LT SID E & FABRICATED 1 DOUBLER AND 2 REPAIR FILLERS AND FILLER IAW SRM 53-30-3 FIG 1 & 53-30-2. INSTALLED REPAIR PARTS IAW S RM 53-30-3 & 51-30-2. 2 L 7 3 4F A3WE 20081024 NM 2008 10 24 SWAA085627 1 20081019 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14R TO STR 15R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085649 1 20081016 A 3350 417A5700 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 443WN 29838 DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY EXIT FLOOR TRACK LIGHT COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085652 1 20081016 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 434, STR 1. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 08FDEA04474 1 20081022 A 5320 CHANNEL BOEING 757 75723A 1384967 NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 RT UPPER LOBE, INTERNAL, BS 1280, RBL 60, FRAME AT S-10R, FWD SIDE IS GOUGED. CUT OUT DAMAGED AREA IAW SRM 53-00-07, RE PAIR NR 1. FABRICATED CHANNEL ON MAE TRAVELER NR T8/763184, LOCATED AN DRILLED IAW SRM 51-40-05, 53-00-07, REPAIR NR 1. INSTALLED FABRICATED CHANNEL IAW SRM 51-40-02 AND 53-00-07, REPAIR NR 1 AT BS 1280, RBL 60, S-10R. THIS REPAIR IS CLA SSIFIED AS A CATEGORY "A" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20081024 NM 2008 10 24 08FDEA04476 1 20081022 A 5320 652954825 PAN BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FUSELAGE UPPER LOBE INTERIOR STRUCTURE, DITCHING PAN CORRODED AT BS 1183 RBL 53. REMOVED PAN & FABRICATED NEW PAN HEA T TREATED, INSTALLED NEW PAN (CLASSIFIED AS A MINOR REPAIR ) REF DWG 65-29567 & SRM 51-40-02. 2 L 7 3 4F A3WE 20081024 NM 2008 10 24 08FDEA04477 1 20081022 A 5347 BAC1520792 SEAT TRACK BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 MAIN CABIN SEAT TRACK, BS 377.7-440, LBL 45, HAS CORROSION AND SCRATCHES. REMOVED SEAT TRACK ASSY AT CUSTOMER REQUEST I AW SRM 51-40-02. REPLACEMENT SEAT TRACK WAS DRILLED UP AND SCALLOPED ON MAE TRAVELER NR T8/760225. INSTALLED REPLACEME NT SEAT TRACK ASSY, BS 377.7 - 440, LBL 45, IAW SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20081024 NE 2008 10 24 DL75E081362 2 20081014 A 7320 SHUTOFF VALVE BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE FUEL SYSTEM FOD A DALA K NONE C F.O.D. IN INSP/MAINT 1 SO 27 722TW 25907 728739 29385 728739 DURING PREFLT FOR FUEL CONTROL CHANGE HAD LOW AIR FROM NR 1 ENG AFTER REMOVING HPSOV FOUND METAL STRIPS INSIDE VALVE. C ONSULTED ENGINE SHOP AND DETERMINED TO BE AIRSEAL FROM 12TH TO 13 STG COMPRESSOR SECTION. REPLACED NR 1 ENGINE PER TRAN S 6T103. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 NM 2008 10 23 2008UALA06070 1 20081012 A 3350 582240 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 EEL FLOOR MOUNTED LIGHT STRIP ON RIGHT FWD AISLE INOP BETWEEN DOOR 1 RT AND SEAT 1K. REPLACED LIGHT ASSY & BATTERY PACK . OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081023 CE 2008 10 23 DXT2008F00008 1 20080916 A 3240 BRAKE RAYTHN DH125 HAWKER800XP 7150012 CE MLG WEAK E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 845QS 258545 BRAKES ARE WEAK AND SPONGY. (K) 2 L 7 2 4F RT A3EU 20081023 NM 2008 10 23 2008UALA06136 1 20081015 A 3350 60243 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 644UA 25094 LIGHT BAR (EEL) AT AFT GALLEY. REPLACED EEL STRIP. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081023 NM 2008 10 23 2008UALA06137 1 20081015 A 5315 SPLICE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 CABIN, BS 365, RBL 5, T-CAP SPLICE CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED STRAP SPLICE. FABRICATED & INSTALLED A NEW STRAP SPLICE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 NM 2008 10 23 2008UALA06141 1 20081015 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR UNSECURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 543UA 25698 DOOR 1R WILL NOT ARM. FOUND GIRT BAR OFF DOOR. SECURED GIRT BAR. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 EU 2008 10 23 AALA200802371 1 20080916 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7083A 645 MIA EMERGENCY LIGHTS AT SEAT ROWS 6C TO 18C. RECHARGED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 6C TO 18C. SYSTE M GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A35EU 20081023 NM 2008 10 23 AALA200802360 1 20080914 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 646AA 24604 DFW EXTERIOR EMERGENCY LIGHT AT LT NR 2 DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LT NR 2 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 AALA200802410 1 20080922 A 3397 CONNECTOR BOEING 767 767223 1385123 NM EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 320AA 22321 JFK SEAT MOUNTED EMERGENCY LIGHT AT SEAT 33H INOPERATIVE. REPAIRED CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 3 3H. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081023 NM 2008 10 23 AALA200802361 1 20080914 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 696AN 26976 DFW EMERGENCY LIGHT AT OVERHEAD SEAT 11D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 QXEA200800924 1 20080817 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 410QX 4053 PDX C4 CHECK. LOWER FUSELAGE EXTERNAL SKIN HAS NICK AT STA X1.0 BETWEEN STRINGERS 28R AND 29R. BLENDED OUT DAMAGE BY H AND WITH SCOTCHBRITE PAD. HFEC INSP IAW Q400 NDTM PT 6, 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECK IAW Q400 NDTM PT 1, 51-00-04 HI .043 LO .038. OUT OF LIMITS IAW RD8/4-53-505. MAPPED FOR ENGINEERING. BLENDED AREA IS WITHIN LIMITS I AW RD 8/4-53-2450. PAINTED IAW 400 SRM 51-25-05. 2 H 7 2 4T RT A13NM 20081023 NM 2008 10 23 AALA200802418 1 20080922 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 187AN 32381 DFW EMERGENCY LIGHT EXIT SIGN AT LT NR 3 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT EXIT SIGN AT LT NR 3 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 USAA920081854 1 20081009 A 5330 65458001205 SKIN BOEING 737 7373G7 138447J NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN C18 MAJOR REPAIR NR 6123139. CRACK ON FUSELAGE SKIN AT L-1 DOOR CUTOUT LOWER AFT CORNER BS 328, WL 208. REPAIRED F USELAGE SKIN AT L-1 DOOR IAW SRM 53-10-01-02 2R FIGURE 201. 2 L 7 2 4F RT A16WE 20081023 EA 2008 10 23 TRAX200801256 1 20081001 A 5330 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 981EV 7768 RT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED RBL 27. 2 L 7 2 4F RT A21EA 20081210 NM 2008 12 10 AALA200802349 1 20081007 A 3350 CM767 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 397AN 29604 AFW - EMERGENCY LIGHT ON RIGHT SIDE FORWARD OF AFT CARGO IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT ON RIGHT SID E FORWARD OF AFT CARGO. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081023 NM 2008 10 23 AALA200802434 1 20080923 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 792AN 30253 EMERGENCY LIGHT AT SEAT 37G HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081023 NM 2008 10 23 ASAA0843600 1 20080915 A 5322 6545815272 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 E&E BAY SHEAR TIE CORRODED STA 344 RBL 12. REMOVED DAMAGED SHEAR TIE, FABRICATED SHEAR TIE AND DOUBLER, LOCATED, DRILLE D, INSTALLED IAW B737 400 SRM 53 00 07 FIG 201. 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 ASAA0843591 1 20080908 A 5330 65C3235719 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 EXT FUSELAGE DENTED AT STA 490 BETWEEN STR 21L AND STR 22L MEASURES A = 3.0 INCHES Y = 1.1 INCHES A Y=27. TRIMMED OUT D ENT DAMAGE, HFEC INSPECTED TRIMMED OUT, NO DEFECT NOTED. FABRICATED REPAIR PARTS, LOCATED, DRILLED, INSTALLED FILLER DO UBLER AND TRIPLER IAW AAR EA 12944 ASA EA 5330 02395. 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 ASAA0843596 1 20081003 A 5753 6546430130 SKIN BOEING 737 7374Q8 138447Q NM FOREFLAP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 RT WING AFT I/B FORE FLAP DELAMINTATED ON LOWER SURFACE. PREPARED DAMAGED AREA AND PREPARED 3 EACH REPAIR PLYS AND BOND ED IAW B737 400 SRM 51 70 16 PG 17. 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 ASAA0843599 1 20080916 A 5753 6546434370 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 RT WING AFT I/B TRAILING EDGE FLAP LOWER SURFACE DENTED IN 4 SPOTS. REMOVED DAMAGED SKIN, FABRICATED FILLER AND DOUBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 ASAA0843601 1 20080911 A 5753 65C2632018 SKIN BOEING 737 7374Q8 138447Q NM MID FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 RIGHT O/B MID FLAP LOWER SURFACED CHAFED BELOW NR 7 FLAP CARRIAGE. REMOVED DAMAGED AREA OF SKIN, FABRICATED REPAIR PART S IAW B737 400 SRM 51 70 10 PG 214 AND BONDED IAW B737 400 SRM 51 70 10 PG 254. 2 L 7 2 4F RT A16WE 20081023 EA 2008 10 23 SWIA200820169 1 20081012 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 707SK 10003 SECOND TO LAST EMERGENCY LIGHT INOP (FLT 6615). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820174 1 20081013 A 3234 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A SWIA K NONE J WARNING INDICATION AP APPROACH 1 NM 07 956SW 15685 230 7825 ON APPROACH TO LANDING, RECEIVED "NOSE GEAR" DISAGREE (FLT 6541). REPLACED NLG SELCTOR VALVE. P/N 75000-6000, S/N OFF 2029. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820175 1 20081011 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 953SW 7813 FIRST CEILING EMERGENCY LIGHT IS INOP (FLT 6450). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820176 1 20081014 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 506CA 7793 EMERGENCY LIGHT BAR HAS A BURNED OUT LIGHT (FLT 2631). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820177 1 20081014 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 909SW 7558 CEILING RECESSED EMERGENCY LIGHT, MOST FORWARD, INOP (FLT 6588). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081023 SO 2008 10 23 FDKA2008101700275 1 20081017 A 5210 DOOR EMB 145 EMB145LR 3260212 SO PAX DOOR MALFUNCTIONED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 841MJ 145448 FRL FLT 6215 CLT. MAIN CABIN DOOR HARD TO CLOSE. MX PERFORMED AN OPS CHECK OF DOOR CLOSING AND LOCKING SYSTEM. DOOR O PS NORMAL. 2 L 7 2 4T RT T00011AT 20081023 SO 2008 10 23 FDKA2008101800276 1 20081018 A 5210 DOOR EMB 145 EMB145LR 3260212 SO PAX DOOR DIRTY A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FRL FLT 6174 CVG. MAIN CABIN DOOR HARD TO CLOSE. MX CLEANED AND LUBED DOOR, OPS GOOD. 2 L 7 2 4T RT T00011AT 20081023 SO 2008 10 23 FDKA2008102000278 1 20081020 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN UNSECURE A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FRL FLT 6195 ROC-JFK. EMERGENCY LIGHT OVER GALLEY DOOR INOPERATIVE. MX RE-SECURED CONNECTORS. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 20081023 EA 2008 10 23 MASA2008101600732 1 20081016 A 4940 387762801 IGNITER CNDAIR CL600 CL6002B19 1900309 EA APU MALFUNCTIONED A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 650ML 11041 7137 ASH FLT 7044 IAD-LGA. SMOKE COMING FROM APU INLET. MX INSPECTED A/C AND FOUND NO EVIDENCE OF UNCONTAINED FIRE AND REPL ACED IGNITOR. 2 L 7 2 4F RT A21EA 20081024 NM 2008 10 24 DL757081360 1 20081014 A 5330 148N32145 SKIN BOEING 757 757232 1384965 NM BS 1720 BL 0 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 631DL 23612 THE AFT FUSELAGE SKIN PANEL AT STA 1720 SUFFERED SCRATCHES DUE TO THE AIRCRAFT SCRAPING THE GROUND ON TAKEOFF. THE SKIN DAMAGE WAS REPAIRED PER ER/A 06-216844-14. THE DAMAGE AND REPAIR OCCURRED DURING JANUARY 1989, BUT NO PREVIOUS MRR REC ORD WAS FOUND. 2 L 7 2 4F RT A2NM 20081024 SO 2008 10 24 CHQA200800207 1 20081019 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 280SK 145381 CAE312672 FLIGHT 3084, CMH TO DCA. DURING INSPECTION THE EMERGENCY EXIT SIDEWALL LIGHT AT SEATS 12 D&F WAS INOP. MAINTENANCE FOU ND THE NR 4 INVERTER INOP AND WAS REPLACED. AFTER REPLACEMENT, THE EMERGENCY LIGHT SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081024 NM 2008 10 24 K11A2008102372212 1 20080828 A 5320 MOUNT BRACKET BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER NR NOT REPORTED 1 GL 23 722CK 20948 APU INLET SCREEN DRAIN ASSY HORIZONTAL MOUNT BRACKET (CHORD) CORRODED ON INSIDE OF KEEL BEAM. 2 L 7 3 4F RT A3WE 20081024 NM 2008 10 24 SWAA085676 1 20081021 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085614 1 20081019 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085655 1 20081016 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 UPS08553578 1 20081001 A 5320 BEAM BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 LONGITUDINAL BEAM BS 1040-1180 LBL 25 WL 208 IS CORRODED AT NUT PLATES AND ON FASTENERS. REMOVED AND REPLACED PER SRM 51-40-02 BEAM CHORD P/N 144N8017-10 AND P/N 144N5024-5. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 UPS08M53627 1 20081010 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:1C RT WING FIXED L/E BELOW SLAT TRACK 14 SKIN CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW MD-11 SRM 57-10-00 FIG 21. 2 L 7 3 4F RT A22WE 20081023 NM 2008 10 23 UPS08M53628 1 20081008 A 5720 SPLICE DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:1C RT WING FIXED L/E COMPT APPROX STA 775 SPLICE FOUND CRACKED. REMOVED, FABRICATED, AND INSTALLED SPLI CE IAW SGW ARB3954 AND MD-11 SRM 51-33-01. 2 L 7 3 4F RT A22WE 20081023 NM 2008 10 23 2008UALA02685 1 20080507 A 2400 CONTROL UNIT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ELECTRICAL SYS MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C CL CLIMB 1 WP 29 597UA 28750 LOST GALLEY LOAD SHED ON CLIMBOUT. RELATED TO SDR 2008UALA02620. THIS ISSUE WAS VERY DIFFICULT TO DIAGNOSE AND REQUIRE D THREE WEEKS OF CONSTANT TROUBLESHOOTING. AFTER ALL WIRES WERE HAND OVER HAND CHECKED AND FOUND NORMAL, K1 AND K2 RELA YS WERE CHANGED, BUSS TIE BREAKERS WERE ALSO CHANGED - IT WAS FOUND THAT CHANGING THE ELCU WAS THE FINAL FIX. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 NM 2008 10 23 2008UALA06134 1 20081015 A 5322 141T132259 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DEFECTIVE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 644UA 25094 STA 368 BETWEEN STR 7L AND 8L IS OUT OF TOLERANCE. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081023 NM 2008 10 23 2008UALA06135 1 20081015 A 5315 SPLICE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 CABIN, BS 365, RBL 30, T-CAP SPLICE CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED OLD SPLICE STRAP, FABRICATED & INSTAL LED A NEW STRAP SPLICE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 NM 2008 10 23 USAA920081673 1 20080822 A 5320 6545409306 WEB BOEING 737 7373G7 138447J NM BS 665.75 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 PRESSURE WEB CRACKED AT BS 665.75 WL 200, LBL 32. REPAIRED PRESSURE WEB AT BS 665.75, WL 200. (K) 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 USAA920081674 1 20080912 A 5343 654611325 PIN BOEING 737 7373B7 1384580 NM RT MLG TRUNNION CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 RT MLG TRUNNION PIN THREADS AND NUT BADLY CORRODED. REPLACED RT MLG TRUNNION PIN IAW MM 32-11-11. (K) 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 UIEA200800310 1 20080918 A 5330 SKIN BOEING 747 747243B 1384830 NM BS 430 S37R PUNCTURED A UIEA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 EA 15 517MC 23300 DURING GROUND OPERATION IN FUSELAGE SKIN, STA 430, STRINGER 37R NEAR THE GROUND POWER RECEPTACLE WAS STRUCK CAUSING DAMA GE CONSISTING OF A PUNCTURE MEASURING 3X6 INCHES. INTERIM REPAIR ACCOMPLISHED IAW EO 4753B209. (K) 2 L 7 4 4F RT A20WE 20081023 NM 2008 10 23 2008UALA06140 1 20081015 A 2560 BRACKET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR OBSTRUCTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 565UA 26669 DOOR 1R WILL NOT ARM OR DISARM PROPERLY. CLEANED DEBRIS FROM GIRT BAR BRACKETS. ARMED AND DISARMED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 NM 2008 10 23 2008UALA06146 1 20081016 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EMERGENCY LIGHT SEAT 3J AFT INOP. REPLACED EMERGENCY LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 NM 2008 10 23 2008UALA06147 1 20081016 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EMERGENCY LIGHT SEAT 35 RT INOP. REPLACED EMERGENCY LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 EU 2008 10 23 2008UALA06148 1 20081016 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN ODOR A UALA D RETURN TO BLOCK W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 422UA 503 NEAR ROW 6, ELECTRICAL ODOR AND HAZE REPORTED IN AREA. NEED TO INVESTIGATE FOR SOURCE. PERFORMED INSPECTION, FOUND NO EVIDENCE OF ELECTRICAL BURNING. REMOVED AND INSTALLED PANELS IN CABIN AROUND ROW SIX. PERFORMED INSPECTION. CKD CEILIN G AT ROWS 5-6-7, ALL NORMAL. FOUND NO EVIDENCE OF ELECTRICAL BURNING. NO OIL CONTAMINATION FOUND INSIDE OR OUTSIDE APU B LEED DUCTS, APU INLET, NO OIL LEAKS. RAN NR 1 & 2 ENGS ISOLATED WITH BLDS & ELECTRICS, ALL NORMAL. CHECKED ALL E&E COMPT S NO ABNORMALITIES, CHECKED ENG INLETS & EXHAUST, NO OIL PRESENT. CHECKED GEN TIE BREAKERS DURING SWITCH OVER WITH ENGS, ALL OK. INBOUND FLT CREW REPORTED NO ABNORMAL ODORS DURING PREV FLT. WILL CONTINUE TO MONITOR. NFF. 2 L 7 2 4F 4 F RT A28NM E40NE 20081023 2008 10 23 2008UALA06149 4 20081015 A 2565 D31039202U1 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE UNSERVICEABLE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 553UA 25277 BOTTLE INADEQUATE. OUTSIDE SERVICE STATION MISTAKE. OVERHAUL AND REPACK SLIDE PER CMM. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 SO 2008 10 23 SWIA200820165 1 20081004 A 2722 3081401003 ACTUATOR EMB 120 EMB120ER 3260203 SO RUDDER MALFUNCTIONED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 237SW 17057 16242 120314 AFTER TAKEOFF, AT APPROXIMATELY 130 KTS, RIGHT RUDDER JAMMED (FLT 5416). REPLACED BLUE SYSTEM RUDDER ACTUATOR. VPN 308 140-1003, S/N ON 0581, S/N OFF 0701. 2 L 7 2 4T RT A31SO 20081023 EA 2008 10 23 SWIA200820166 1 20081010 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 947SW 7786 RIGHT AFT EXTERIOR EMERGENCY LAMP INOP (FLT 6152). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081024 WP 2008 10 24 08FDEA04396 1 20081017 A 5730 ARC0254501 PANEL DOUG MD10 MD1010F 3022112 WP RT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 RIGHT WING INBD LOWER T/E PANEL 641 KB IS CHAFED. REPAIRED RT WING INBD LOWER T/E PANEL 641 KB BY FABRICATING A DOUBLER & BONDING IT TO THE PANEL. SEALING & RESTORING THE FINISH IAW 51-71-00. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04398 1 20081017 A 5230 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 MAIN CARGO DOOR NR 3 SPOOL BACK UP FITTING HOLES "A"; "C" AND "D" HAVE CRACK INDICATIONS. REPAIRED FITTING HOLES IAW SRM 53-50-00. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04399 1 20081017 A 5230 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 MAIN CARGO DOOR NR 4 SPOOL BACK UP FITTING HOLES "A" AND "C" HAVE CRACK INDICATIONS, BACK UP FITTING REQUIRES REPLACEM ENT. REWORK OF BOLT BORES ACCOMPLISHED ON WC E9-5230-7-5000. REPAIRED MCD JAMB UPPER & LOWER BEAMS IAW SRM 53-50-00. RE MOVED & REPLACED NR 4 SPOOL BACK UP FITTING IAW DWG NCA6084 & SRM 51-33-01. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04400 1 20081017 A 5230 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 MAIN CARGO DOOR NR 6 SPOOL BACK UP FITTING HOLES "B" AND "D" HAVE CRACK INDICATIONS. REPAIRED MAIN CARGO DOOR SPOOL B ACK UP FITTING HOLES " B " & " D " IAW SRM 53-50-00. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04401 1 20081017 A 5230 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 MAIN CARGO DOOR NR 5 SPOOL BACK UP FITTING HOLES "A" AND "C" HAVE CRACK INDICATIONS, BACK UP FITTING REQUIRES REPLACEM ENT. WORK ACCOMPLISHED ON W/C E9-5230-7-5000. REPAIRED MCD. UPPER & LOWER BEAMS IAW SRM 53-50-00. REMOVED REPLACED FIT TING IAW DWG NCA 6084 & SRM 51-33-01. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 08FDEA04426 1 20081018 A 5347 SEAT TRACK BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 MAIN CABIN, SEAT TRACK BS 377.7- BS 440 LBL 24.75 CROWN HAS CORROSION AND GOUGES. REMOVED AND REPLACED SEAT TRACK IAW S RM 51-40-02 MAJOR REPAIR, NO FOLLOW-UP INSPECTION REQUIRED. 2 L 7 2 4F RT A2NM 20081024 NM 2008 10 24 08FDEA04427 1 20081018 A 5315 FLOORBEAM BOEING 757 75723A 1384967 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 MAIN CABIN FLOORBEAM, STA 1620 LBL25-45 HAS MISDRILLED SCREW HOLES. REPAIRED FLOORBEAM IAW SRM 53-00-51 REPAIR NR 1 FIG 201 AND SRM 51-40-02 MAJOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED. 2 L 7 2 4F RT A2NM 20081024 NM 2008 10 24 DL76L081339 1 20081009 A 8011 774860A4 STARTER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE UNKNOWN A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 191DN 28448 727654 THE LEFT ENG WENT TO 14 PERCENT N2 ON START AND THEN BEGAN TO DECREASE RPM. ALL OTHER INDICATIONS NORM. REMOVED AND RE PLACED LT ENG STARTER PER M/M. PERFORMED OPS CHK OF STARTER OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081024 NM 2008 10 24 UPS08653691 1 20081012 A 5720 BEAM BOEING 767 76734AF 1385212 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 331UP 27757 INSPECTION TYPE:N/A LT WING L/E LES670 FWD NOSE BEAM LWR WEB CRACK CRACK LENGTH 1.25 INCH. LT WING L/E LES670 FWD NOSE BEAM WEB LOWER AREA REPAIRED AS PER SRM 57-41-13-2R FIG 201. 2 L 7 2 4F RT A1NM 20081024 NM 2008 10 24 SWAA085633 1 20081020 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085639 1 20081020 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED BS 747, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085645 1 20081020 A 5753 6546486 WEDGE BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND LT WING I/B MID FLAP WEDGE PANEL DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 WX0A070245 1 20081015 A 3350 L2019115 LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 402NV 49763 L1 DOOR EMERGENCY LIGHT - DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REPLACED THE EMERGENCY LIGH T ASSEMBLY AS REQUIRED. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 20081024 NM 2008 10 24 WX0A070243 1 20081005 A 3350 201314 BATTERY PACK DOUG MD80 MD83 3023681 NM CABIN DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 861G 49557 OVERHEAD EMERGENCY LIGHTS IN TAIL CONE AREA. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-5 0-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT 20081024 NM 2008 10 24 UPS08653684 1 20081013 A 5315 141T514622 STIFFENER BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 331UP 27757 INSPECTION TYPE:N/A MAIN DECK FLOORBEAM ATTACH STIFFENER AT TWO SURFACE STA 246 RBL 10 CRACK FOUND, CRACK LENGTH 1.25 IN CH. MAIN DECK FLOORBEAM ATTACH STIFFENER AT FWD SURFACE STA 246 RBL 10" REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20081024 EU 2008 10 24 08FDEA04422 1 20081017 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 MAIN CABIN SEAT TRACK SUPPORT FITTING AT FRAME 49, STA 3089, LBL 48 IS CRACKED. 2 L 7 2 4F RT A35EU 20081022 EA 2008 10 22 ASOA200801338 1 20081014 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA ASD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 872AS 7542 ASD LOWER STEP CRACKED. 2 L 7 2 4F RT A21EA 20081022 NM 2008 10 22 SWAA085578 1 20081014 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 1010, STR 24R. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085579 1 20081014 A 5753 65C30462 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD FORE FLAP OUTBOARD AREA REPAIR DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085584 1 20081013 A 5743 161A15011 BEARING BOEING 737 73776Q 13845AA NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 550WN 30279 DURING SCHEDULED MV2 CHECK, FOUND RT MLG AFT TRUNNION BEARING RACE INNER SURFACE CORRODED. REMOVED AND REPLACED BEARING PER MM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085585 1 20081013 A 5743 115A5211 ATTACH FITTING BOEING 737 73776Q 13845AA NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 550WN 30279 DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION BEARING ATTACH FITTING LUG FACE CORRODED. REPAIRED FITTING PER SW A EA. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085594 1 20081015 A 3350 417A5700 STRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 472WN 33831 DURING SCHEDULED MV1 CHECK, FOUND EEPLS STRIP LOOSE AT ROW 1. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085595 1 20081015 A 3350 8210248801 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 205WN 34010 DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085596 1 20081015 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 328, STR 20L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085597 1 20081015 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 335, STR 20L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085600 1 20081014 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS. 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085605 1 20081014 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085606 1 20081014 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS. 827, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085664 1 20081021 A 5311 6520722 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 440, BETWEEN STR 26L TO 27L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081024 EU 2008 10 24 UPS08153703 1 20081014 A 5321 B5327079900100 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 140UP 0823 INSPECTION TYPE:1/3C MAIN CARGO DECK FLOORBOARD 242DQ AFT HALF HAS FIELD REPAIR. REPAIRED MAIN CARGO DECK FLOORBOARD 24 2DQ REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081024 EA 2008 10 24 COMA0806418 1 20081012 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 588SW 22045 7069 EMERGENCY FLOOR LIGHTS ROW 8 AFT INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK NR 1. 2 L 7 2 4F RT A21EA 20081024 EU 2008 10 24 UPS08153708 1 20081014 A 5321 B5327079800100 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 140UP 0823 INSPECTION TYPE:1C3C MAIN CARGO DECK FLOORBOARD 242CQ FWD HALF HAS FIELD REPAIR. REPAIRED MAIN DECK FLOORBOARD 242CQ RE F A300-600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 UPS08153710 1 20081014 A 5321 B5327077900000 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 140UP 0823 INSPECTION TYPE:1C3C MAIN CARGO DECK FLOORBOARD 251BN HAS FIELD REPAIR. REPAIRED MAIN CARGO FLOORBOARD 251BN REF A300-6 00 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081024 EA 2008 10 24 ASOA200801347 1 20081015 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 934EV 8028 RBL 27 OUTBOARD SIDE AT FS 484 INTERCOSTAL ANGLE IS CRACKED IN UPPER RADIUS. REMOVED CRACKED ANGLE, REPLACED WITH SERVI CEABLE ANGLE IAW CRJ 200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 20081024 EU 2008 10 24 08FDEA04429 1 20081019 A 5330 A53974206200 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 427FE 362 LOWER FUSELAGE EXTERNAL SKIN FR 59 TO 61, STRINGER 44L - 45L HAS GOUGE 26" BY 1/4 INCH BY .052 INCH RUNNING JUST BELOW L AP SEAM REPAIRED AREA AT LOWER FUSELAGE EXTERNAL SKIN FR 59 TO 61, STRINGER 44L - 45L IAW SRM 53-10-12 FIG 217. 2 L 7 2 4F RT A35EU 20081024 NM 2008 10 24 08FDEA04430 1 20081020 A 5340 65453132 STRINGER CLIP BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 CABIN BS 950B S4L STRINGER CLIP CRACKED. REMOVED DAMAGED STRINGER CLIP REF 51-30-02, LOCATED AND DRILLED FASTENER HOLES REF SRM 51-30-05, INSTALLED STRINGER CLIP 65-45313Y2/A23841 REF SRM 51-30-02 P1, APPLIED CORROSION INHIBITING COMPOUND REF SRM 51-10-02 P14 THIS REPAIR IS CLASSIFIED AS MAJOR 2 L 7 3 4F A3WE 20081024 EA 2008 10 24 ASOA200801352 1 20081015 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 934EV 8028 LT 621 OBLIQUE ANGLE CRACKED. REMOVED AND REPLACED LT OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 20081024 NM 2008 10 24 08FDEA04431 1 20081020 A 5340 65453132 STRINGER CLIP BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 CABIN BS 950B S5L STRINGER CLIP CRACKED. REMOVED STRINGER CLIP, TRANSFERED HOLES TO NEW CLIP AND INSTALLED REF SRM 51-3 0-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081024 NM 2008 10 24 08FDEA04436 1 20081020 A 5340 654531314 STRINGER CLIP BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 INTERIOR UPPER FUSELAGE BS 660 STR 9R STRINGER CLIP LOWER OB RADIUS CRACKED. REMOVED STRINGER CLIP, CLEANED AND FOUND N O CRACKS. REINSTALLED STRINGER CLIP REF SRM 51-30-02 THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081024 EA 2008 10 24 ASOA200801354 1 20081015 A 5210 INTERCOSTAL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 750EV 10161 PAX DOOR 318 INTERCOSTAL CRACKED. REMOVED CRACKED 318 INTERCOASTAL AND REPLACED WITH NEW 318 INTERCOASTAL IAW CRJ700 SR M 52-11-06 AND SRM 51-42-06. 2 L 7 2 4F RT A21EA 20081024 NM 2008 10 24 08FDEA04437 1 20081020 A 5340 654531314 STRINGER CLIP BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 INTERIOR UPPER FUSELAGE BS 640 STR 9R STRINGER CLIP LOWER OB RADIUS CRACKED. REMOVED CRACKED STRINGER CLIP REF: SRM 51- 30-02 P1. LOCATED AND DRILLED FASRENER HOLES IN CLIP REF SRM 51-30-05, INSTALLED STRINGER CLIP REF SRM 51-30-02 P1. APPL IED CORROSION INHIBITOR REF 51-10-02 P14. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081024 WP 2008 10 24 08FDEA04410 1 20081017 A 5415 AUB70833 ATTACH BRACKET DOUG MD10 MD1010F 3022112 WP NR 1 NACELLE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 NR 1 ENGINE PYLON, FWD APRON PANEL ATTACHING BRACKET AT STA YN 281 HAS A 1/2 INCH CHAFED HOLE ON THE EDGE. REMOVED & RE PLACED FAIRING SUPPORT PER DWG AUB 7083; REV " K " & SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04411 1 20081017 A 5720 ARC02951 SUPPORT DOUG MD10 MD1010F 3022112 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 LEFT WING T/E VERTICAL ATTACH SUPPORT IS CRACKED AT THE UPPER PART OF FRAME 33, OUTBD OF THE INBD EDGE. REMOVED & REPLA CED POST IAW DWG 3 ARC0295 & SRM 51-33-01. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04413 1 20081017 A 5753 ARC25943 CHANNEL DOUG MD10 MD1010F 3022112 WP LT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46626 LEFT WING INBD FLAP OUT HINGE AFT FAIRING STRUCTURE ATTACH CHANNEL IS CRACKED AT THE UPPER INBD BOLT. REMOVED CRACKED C HANNEL REF SRM 51-33-01. FORMED, LOCATED & DRILLED CHANNEL REF DWG ARC 2594 & SRM 51-33-01. ALODINED, PRIMED & APPLIE D TOP COAT REF SRM 51-21-01. INSTALLED CHANNEL REF SRM 51-33-01. PART MARKED PER GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20081022 NM 2008 10 22 SWAA085607 1 20081014 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085608 1 20081014 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085610 1 20081015 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 632SW 27707 FOUND FWD DOOR EMERGENCY EXIT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085611 1 20081015 A 3350 101331 LIGHT BOEING 737 7373Y0 1384671 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 FOUND LT EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 2008UALA06088 1 20081013 A 2150 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 654UA 25392 THE 'R PACK INOP' LIGHT ON. EICAS MSG 'R PACK TEMP' DISPLAYED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081022 NM 2008 10 22 2008UALA06089 1 20081011 A 2432 263BA1012 BATTERY BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE MAIN FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 788UA 26942 STATUS MESSAGE "MAIN BATTERY". REPLACED & OP CHECKED MAIN BATTERY. MESSAGE CLEARED. BATTERY INDICATIONS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081022 NM 2008 10 22 2008UALA06093 1 20081012 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 EMERGENCY EEL FLEX STRIP LIGHT INOP AT SEAT 5EF. REPLACED EMERGENCY LIGHT STRIP. OPS CHECKED OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081022 NM 2008 10 22 2008UALA06098 1 20081013 A 4990 BEARING BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE APU OIL PUMP FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 793UA 26946 APU CONTROL STATUS MESSAGE. FOUND METAL IN APU. FOUND OIL PUMP BEARING FAILED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081023 EA 2008 10 23 N6WA200810081 1 20081008 A 5220 SEAL CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY DOOR OUT OF POSITION A N6WA K NONE O OTHER UK UNKNOWN 1 CE 03 164GJ 10256 EMERGENCY DOOR OVERWING ON A/C RIGHT HAS A SEAL COMING OUT OF THE BOTTOM OF DOOR AND LATCH COVER IS NOT LATCHING CLOSED. SECURED DUST SEAL IAW M/M 51-22-61. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 ASOA200801238 1 20080927 A 5260 STEP CNDAIR CL600 CL6002C10 1390015 EA ASD DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED AND REPLACED ASD LOWER STEP IAW CRJ700 AMM 52-11-04. SUPPLEMENTAL SDR CLOSED 10/15/08. 2 L 7 2 4F RT A21EA 20081023 CE 2008 10 23 ZESA2008006 1 20080603 A 5280 661308111 DOOR CESSNA 560 560XL 2076702 CE LANDING GEAR BENT E ZESA K NONE O OTHER LD LANDING 1 EA 03 877R 5605219 ON ARRIVAL AT LSE AND UPON EXTENDING GEAR, AN UNUSUAL NOISE WAS APPARENT. GEAR DOWN INDICATION WAS NORMAL AND NO GEAR H ORN WAS HEARD WHILE THROTTLES WERE IDLE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LANDING GEAR SPADE DOOR DAMAG ED. FERRY FLIGHT PERMIT WAS ISSUED FROM LSE TO MKE WITH GEAR DOWN PROVISIONS. THE NOSE GEAR SPADE DOOR WAS REPLACED, N O DETERMINATION OF CAUSE WAS FOUND. 2 L 7 2 4F RT A22CE 20081023 NM 2008 10 23 HALA0800811 1 20081016 A 2842 300710607 PROCESSOR BOEING 767 76733A 1385209 NM FUEL SYSTEM MALFUNCTIONED A HALA K NONE O OTHER CR CRUISE 1 WP 13 587HA 1233 1233 33421 ETOPS SIGNIFICANT SYSTEM - OVERHEAD FUEL QUANTITY TOTALIZER INTERMITTENT. ACCOMPLISHED BITE OF FQ PROCESSOR PER FIM 28- 41-00 FIG 104 PROCESSOR FAULTED. REPLACED PROCESSOR PER AMM 28-41-08. OPS CHECK OK. 2 L 7 2 4F RT A1NM 20081023 WP 2008 10 23 NWAA084299861 1 20081017 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 770NC 47758 DURING LINE CHECK, MAINT FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATI VE. MAINT REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (K) 2 L 7 2 4F RT A6WE 20081023 NM 2008 10 23 UIEA200800334 1 20081014 A 5220 BOLT BOEING 747 747243B 1384830 NM EMERGENCY EXIT LOOSE A UIEA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 540MC 22508 AIR TURNBACK AFTER TAKEOFF LOUD NOISE FROM OVERHEAD HATCH. CARRIED OUT HATCH SEAL CHECK AND DOOR CUTOUT CHECK FOR ABNOR MALITIES ALL OKAY. FOUND HINGE BOLTS LOOSE. TIGHTENED SAME PER STANDARD PRACTICES. PRESSURIZED AIRCRAFT AND LEAK CHEC KED, NO LEAKS NOTED. 2 L 7 4 4F RT A20WE 20081023 NM 2008 10 23 UPS08553582 1 20081002 A 5311 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 FRAME IS DENTED AT BS 1560 BETWEEN STR 26 AND 27 LT. REMOVED DAMAGED SECTION OF FRAME AND REPAIRED P ER SRM 53-00-07-1A1. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 UPS08553592 1 20081001 A 5320 BEAM BOEING 757 75724APF 1384969 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 DURING CORROSION CLEAN UP FOUND ELONGATED FASTENER HOLE IN LONGITUDINAL L BEAM I/B FLANGE BS 1021 LBL 45.5 WL 208. REPAIRED PER ATS ER08-3117 DATED 13OCT08. 2 L 7 2 4F RT A2NM 20081024 WP 2008 10 24 AALA200802521 1 20080926 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 CORROSION ON ANGLE AFT SIDE OF DOOR JAMB IN AFT CARGO AT STATION 1155 RT LONGERON 27 IS BEYOND LIMITS. AREA OF DISCREPA NCY IS 4 INCHES BY 10 INCHES. INSTALLED NEW ANGLE PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081024 WP 2008 10 24 AALA200802468 1 20080930 A 2410 696233B CSD DOUG DC9 DC983 3022083 WP NR 2 ENGINE FAILED A AALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 9621A 53592 INFLIGHT T870/30SEP. BUR TO DFW. CREW REPORTED DISCONNECTION OF NR 2 ENGINE GENERATOR DUE TO HIGH CONSTANT SPEED DRIVE OIL PRESSURE. AUXILIARY POWER UNIT ALSO HAD TO BE SHUT DOWN DUE TO LOW OIL PRESSURE. LANDED LAS WITHOUT INCIDENT. RE PLACED NR 2 ENGINE CONSTANT SPEED DRIVE CSD, GENERATOR AND OIL COOLER. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081024 NM 2008 10 24 AALA200802457 1 20080927 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 DFW EMERGENCY PROXIMITY LIGHT AT FIRST CLASS GALLEY FORWARD CORNER INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY P ROXIMITY LIGHT AT FIRST CLASS GALLEY FORWARD CORNER. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081024 WP 2008 10 24 AALA200802454 1 20080927 A 2131 21171803 CONTROLLER DOUG DC9 DC982 3022082 WP CABIN PRESSURE FAILED A AALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 453AA 49558 LGA INFLT T766/27SEP. CREW REPORTED CABIN PRESSURE INDICATION AND PRESSURE CLIMB. PERFORMED EMERGENCY DESCENT AND CABI N PRESSURE STABILIZED. LANDED LGA WITHOUT INCIDENT. REPLACED BOTH CABIN PRESSURE CONTROLLERS AND THE OUT FLOW VALVE AC TUATOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081024 NM 2008 10 24 AALA200802456 1 20080927 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 DFW EMERGENCY PROXIMITY LIGHTS AT FIRST CLASS GALLEY FLOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY PROXIMITY L IGHTS AT FIRST CLASS GALLEY FLOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081024 NM 2008 10 24 AALA200802469 1 20080930 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 658AA 24616 LOWER RT AND LT EMERGENCY LIGHT EXIT SIGNS AT OVERWING EXIT DOORS AND SEAT ROWS 16DEF TO 25DEF INOPERATIVE. REPLACED BA TTERY PACK AT SEAT ROW 20DEF FOR LOWER RT AND LT EMERGENCY LIGHT EXIT SIGNS AT OVERWING EXIT DOORS AND SEAT ROWS 16DEF T O 25DEF. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081024 NM 2008 10 24 AALA200802455 1 20080927 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 DFW EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT T00001SE 20081024 EU 2008 10 24 AALA200802447 1 20080926 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 EMERGENCY LIGHTS AT RT NR 1 DOOR TO SEAT ROW 6 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RT NR 1 DOOR TO SEAT ROW 6. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A35EU 20081024 NM 2008 10 24 AALA200802466 1 20080930 A 3350 0202503001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT DETACHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 794AN 30256 EMERGENCY LIGHT LENS AT FIRST CLASS COAT CLOSET IS DETACHED. REPLACED LENS FOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081024 WP 2008 10 24 AALA200802445 1 20080926 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 411AA 49322 EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 18 TO 24 INOPERATIVE. REPLACED BATTERY PACK AT STATION 900 FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 18 TO 24. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081024 EA 2008 10 24 COMA0860422 1 20081012 A 3350 364911 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 588SW 7069 EMERGENCY FLOOR LIGHTS ROW 8 AFT INOP. R&R FLOOR LEVEL LIGHT STRIP ROW 2 THRU 8. 2 L 7 2 4F RT A21EA 20081024 EA 2008 10 24 COMA0860420 1 20081012 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 588SW 24515 7069 EMERGENCY FLOOR LIGHTS ROW 8 AFT INOP. R&R EMERGENCY BATTERY PACK NR 3. 2 L 7 2 4F RT A21EA 20081024 NM 2008 10 24 USA2008F00039 1 20080927 A 2751 2061141 INDICATOR BOEING 737 7374B7 138449C NM COCKPIT FAULTY A USAA L ABORTED APPROACH O OTHER AP APPROACH 1 EA 19 453UW 51668 300 24980 CLT - FLT 1706, ON APPROACH TO CLT, CAPTAIN REPORTED THE TRAILING EDGE FLAPS SHOWED A SPLIT CONDITION WHEN SELECTING FLA PS. NO ROLLING MOMENT WAS EXPERIENCED. CREW ACCOMPLISHED A GO-AROUND AND FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES. FLIGHT LANDED NORMALLY AT FLAPS 15. AFTER LANDING, INDICATOR RETURNED TO NORMAL. NO EMERGENCY DECLARED. MX REMOVED AND REPLACED THE FLAP POSITION INDICATOR PER MM 27-58-41. OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 QXEA200800988 1 20080912 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 413QX 4060 PDX - C CHECK. RT INBD SEAT TRACK NR 16 HAS SURFACE CORROSIONINSIDE AND ON TOP OF THE CLAW SECTION BETWEEN STATION X705 AND X710. BLENDED CORROSION, MAX DEPTH TO TOP CLAW IS .024 OUT OF LIMITS. REMOVED NR 16 SEAT TRACK REF Q400 SRM 51-40- 07, 51-42-05 AND 51-40-15. MATCH DRILLED, PREPPED AND INSTALLED NEW SEAT TRACK REF Q400 SRM 51-40-07, 51-42-05 AND 51-4 0-15. 2 H 7 2 4T RT A13NM 20081027 EU 2008 10 27 M7KA0709084020 1 20080804 A 6220 BUSHING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE STARFLEX LOOSE E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 814MH M2941 4020 23100 DURING ROUTINE INSPECTION A STAR ARM END BUSHING WAS FOUND LOOSE. STARFLEX REMOVED FOR REPAIR AND SERVICEABLE STARFLEX I NSTALLED. THIS IS A VERY COMMON FAILURE RECENTLY FOR THIS PART SUSPECT THAT AN ADHESIVE FAILURE IS THE PROBLEM THAT MAY BE HEAT RELATED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 EA 2008 10 27 A6WA200840593 1 20080929 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* 30015 NE AIR CON SYS ODOR A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 415AW 7593 NOTICED OILY ODOR COMING FROM AIR CONDITIONING, BOTH PACS IN ENGINE OR APU AS AIR SOURCE, STRONGER WHEN DUCT TEMP IS HOT TER. REMOVED AND REPLACED RT ACM WATER SEPARATOR COALESCER BAG, REACTIVATED LT AND RT PACKS AND OVERBOARD EXHAUST SOV, O PS CHECK GOOD IAW AMM 21-51-00. REMOVED FROM MEL. (K) 2 L 7 2 4F 4 F RT A21EA 20081023 NM 2008 10 23 2008UALA06077 1 20081013 A 3350 582240 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 DOOR FWD RT EMERGENCY EXIT SIGN INOP. REPLACED LIGHT ASSY & BATTERY PACK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081023 NM 2008 10 23 2008UALA06078 1 20081013 A 3350 GE1317 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 CEILING MOUNTED EMERGENCY LIGHT AT 6K IS INOP. LIGHT FOUND INOPERATIVE. REPLACED LIGHT ASSY & REPAIR WIRING. SYSTEM C HECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081023 NM 2008 10 23 2008UALA06079 1 20081013 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY FWD GALLEY LIGHT INOP. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 SO 2008 10 23 C2XA08TY106 1 20080916 A 5751 PE64042H6016050 BUSHING EMB 145 EMB145XR 3260214 SO AILERON WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 GL 23 14158 13739 145791 ACFT CURRENTLY IN C-CHECK STATUS. MAINTENANCE FOUND THE LT AILERON IB PCA HAD BUSHING MIGRATED. MAINT REMOVED AND REPL ACED THE HAT BUSIONS IAW EC5740-01152 AND WILL BE RELEASED AT THE END OF THE CHECK. (K) 2 L 7 2 4F RT 20081023 NM 2008 10 23 AALA200802375 1 20080918 A 3350 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 322AA 22323 JFK EMERGENCY LIGHT EXIT SIGN AT OVERHEAD SEAT 20H INOPERATIVE. REPLACED BATTERY PACK M732 FOR EMERGENCY LIGHT EXIT SIG N AT OVERHEAD SEAT 20H. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081023 WP 2008 10 23 AALA200802411 1 20080922 A 2120 DUCT DOUG DC9 DC982 3022082 WP CABIN AIR DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 410AA 49321 SAT INFLIGHT T9647/22SEP. CREW REPORTED SMOKE IN CABIN DURING CLIMB. RETURNED TO SAT AND LANDED WITHOUT INCIDENT. SMO KE CLEARED AFTER LANDING. ACCOMPLISHED BURN OUT OF LT AND RT HAND HIGH PRESSURE PNEUMATIC DUCTS. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081023 CE 2008 10 23 GUU2008F00057 1 20080915 A 5260 HANDLE BEECH 1900 1900D 1154162 CE AIRSTAIR DOOR OUT OF ADJUST A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 45AR UE12 FLIGHT PBI ASD DURING PREFLIGHT PILOT REPORTED RT EMERGENCY EXIT EXTERIOR HANDLE SUNK IN. PROPERLY ADJUSTED RT REAR EME RGENCY EXIT INTERNAL MECHANISM. 2 L 7 2 4T RT A24CE 20081023 WP 2008 10 23 AALA200802367 1 20080915 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 580AA 53157 DFW EMERGENCY LIGHT AT SEAT ROW 22 HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 22. SYSTEM GROU ND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081023 NM 2008 10 23 QXEA200801119 1 20081009 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM AFT PAX DOOR STUCK A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 19 428QX 4160 PDX FLIGHT 2232. UNABLE TO OPEN REAR PAX DOOR. FOUND DOOR JAMMED, UNJAMMED. OPS CHECK GOOD. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081023 NM 2008 10 23 USAA920081855 1 20081009 A 5311 FRAME BOEING 737 7373G7 138447J NM ZONE 200 FUSEL CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN C18 MAJOR REPAIR NR 6123120. FRAME DOUBLER WEB CRACKED AT BS 303.9, S16L. REPLACED FRAME DOUBLER AT BS 303.9, S16L . IAW EO NR 5311-01025 & EA NR 130129. 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 F3LA200800653 1 20080922 A 5330 D53111074200 SKIN AIRBUS A319 A319111 3930336 NM FUSELAGE BURNED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 REFERENCE NON ROUTINE 2008-196727. DURING C4/S1 C-CHECK, INSPECTION NOTED LIGHTNING STRIKE DAMAGE ON EXTERNAL SKIN LOCA TED AT FRAME 1 + 8 INCHES, RT HAND SIDE UPPER FUSELAGE AT VERTICAL REFERENCE AXIS Z O. MX PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-11-11, FIGURE 209. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081023 NM 2008 10 23 AALA200802430 1 20080923 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 DFW EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT T00001SE 20081023 NM 2008 10 23 AALA200802416 1 20080922 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 187AN 32381 DFW EMERGENCY LIGHT EXIT SIGN AT RT NR 7 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT EXIT SIGN AT RT NR 7 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 ASAA0843592 1 20081015 A 5751 SPAR BOEING 737 7374Q8 138447Q NM LT AILERON DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 LT WING AILERON FRONT SPAR DELAMINATED I/B CORNER. REMOVED AND REPLACED LT AILERON IAW B737 400 MM 27 11 11. 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 ASAA0843598 1 20080911 A 5753 6546434370 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 RT AFT FLAP LOWER SURFACE DENTED WITHIN EDGE BAND. REMOVED, DAMAGED SKIN, FABRICATED FILLER AND DOUBLER, BONDED IAW B73 7 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081023 SO 2008 10 23 SWIA200820170 1 20081013 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN MISSING A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 569SW 120344 FORWARD EMERGENCY LIGHT MISSING, PULLED OUT (FLT 5456). INSTALLED LIGHT ASSEMBLY. 2 L 7 2 4T RT A31SO 20081027 NE 2008 10 27 M7KA0807084142 2 20080901 A 7261 0292817460 LABYRINTH SEAL UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE LEAKING E M7KA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 19 822MH 5198 4142 23069 ENGINE SMOKING FOLLOWING SHUTDOWN WAS THE OBSERVED SYMPTOM. CLOSER INSPECTION REVEALED TRACES OF OIL STREAKING FROM POWE R TURBINE BLADE ROOTS. A SERVICEABLE LABYRINTH RING ASSEMBLY HAS BEEN INSTALLED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081024 WP 2008 10 24 08FDEA04460 1 20081021 A 5340 WSP0815514 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 MAIN CABIN RIGID BARRIER FITTING NR 6 IS WORN. REPAIRED IAW EA 8-5340-123670. 2 L 7 3 4F RT A22WE 20081024 EA 2008 10 24 ASOA200801366 1 20081019 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA CABIN CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 EMERGENCY LIGHT ON FWD BULKHEAD FOR PAX DOOR LENSE CRACKED. 2 L 7 2 4F RT A21EA 20081024 EA 2008 10 24 ASOA200801369 1 20081019 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 934EV 8028 PAX DOOR PLACARDS 1 EXIT, 2 OPEN, AND 3 RED ARROW ARE WORN. 2 L 7 2 4F RT A21EA 20081024 SO 2008 10 24 CHQA200800206 1 20081019 A 3397 WIRE EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CABIN DAMAGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 260SK 145128 CAE311802 FLIGHT 5838, IAH TO STL. THE FLIGHT CREW REPORTED THAT THE EMERGENCY EXIT ROW OVERHEAD LIGHT WAS INOP. MAINTENANCE INS PECTED THE EMERGENCY LIGHT SYSTEM AND FOUND A WIRE AT THE SIGN DAMAGED. THE WIRE WAS REPAIRED AND THE EMERGENCY LIGHTS OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081024 NM 2008 10 24 F3LA2008102200678 1 20081020 A 5753 ABS5043D006 SKIN AIRBUS A319 A319111 3930336 NM TE FLAP DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED DENT ON OUTBOARD FLAP TRAILING EDGE LOWER SURFACE BETWEEN RIB 16 AND RIB 17 ON TH E RIGHT WING. MAINTENANCE PERFORMED REPAIR IN ACCORDANCE WITH A319 SRM 57-53-00, PARAGRAPH 8N. 2 L 7 2 4F RT A28NM 20081024 NM 2008 10 24 K11A2008102372205 1 20081001 A 5313 STRINGER BOEING 727 7272H3 138368N NM FUSELAGE CRACKED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 CRACKED FUSELAGE STRINGER (NOSE WHEEL WELL) AT STA 270. 2 L 7 3 4F RT A3WE 20081024 NM 2008 10 24 K11A2008102372210 1 20080818 A 5311 FRAME BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 UPPER WEB FRAME BELOW SUB FLOOR CORROSION (WHERE CABLES PASS THRU). 2 L 7 3 4F RT A3WE 20081024 NM 2008 10 24 SWAA085674 1 20081021 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085675 1 20081018 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085621 1 20081019 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 08FDEA04375 1 20081016 A 5347 AEA7325519 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 MAIN DECK CARGO, CORROSION ON SEAT TRACK FLANGE AT STA 1260 TO STA 1273, X = -8. REPAIR CARRIED OUT AT STA 1271 TO STA 1331, X = -8 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 08FDEA04377 1 20081016 A 5730 ARB74023 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 CRACK FOUND ON 3 FASTENER HOLES ON LEFT WING AT LOWER WING SKIN OUTER ACCESS DOOR CUTOUT AT PANEL NR 536AB. 3 CRACKED F ASTENER HOLES ON LEFT HAND WING AT LOWER WING SKIN REPAIRED AS PER EA 1-5710-125557, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 08FDEA04380 1 20081016 A 5330 6518217163 SKIN BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 221FE 20932 CABIN STA 440 STR 10L HAS MIS-DRILLED FASTENER HOLES. CUT OUT DAMAGED AREA DIMS 2 INCH BY 7/8 INCH. FABRICATED DOUBLER USING 2024-T3 .090 PO NR 9007561 DIMS 12 5/8 BY 9 1/2 INCH, FILLER USING 2024-T3 .190 PO NR 314676 DIMS 2 INCH BY 7/8 I NCH, IAW B727 SRM 53-30-3 AND INSTALLED REPAIR PARTS IAW B727 SRM 53-30-3 FIG 6. 2 L 7 3 4F RT A3WE 20081024 WP 2008 10 24 08FDEA04386 1 20081017 A 5720 ARB29188 INTERCOSTAL DOUG DC10 DC1030F 3023504 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 RT WING LEADING EDGE FOUND INTERCOSTAL CRACK. 2 L 7 3 4F RT A22WE 20081024 EU 2008 10 24 08FDEA04388 1 20081017 A 5347 A53278424202 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 677FE 791 MAIN CARGO DECK SEAT TRACK NR 3 LEFT HAS 2 WORN SCALLOPS BETWEEN FRAMES 59 LEFT AND FRAME 63 LEFT. REMOVED DAMAGED AREA AND INSTALLED SPLICE REPAIR BETWEEN FRAMES 59 AND 63, AT SEAT TRACK 3 LEFT IAW FREIGHTER SRM 53-10-16. 2 L 7 2 4F RT A35EU 20081023 EA 2008 10 23 SWIA200820171 1 20081009 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 507CA 7796 THIRD EMERGENCY LIGHT AFT ON CEILING IS INOP (FLT 2826). OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820172 1 20081012 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 763SK 10228 NEXT TO LAST CEILING EMERGENCY FLOODLIGHT INOP (FLT 6452). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820173 1 20081014 A 3350 INVERTER CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 926SW 7687 EMERGENCY FLOOR PATH LIGHTING WILL NOT ILLUMINATE FROM ROW 2 TO ROW 5 (FLT 6060). REPLACED NR 2 INVERTER. 2 L 7 2 4F RT A21EA 20081023 CE 2008 10 23 HSYA20081001 1 20081020 A 2120 UNKNOWN CESSNA 208 208B 2073701 CE COCKPIT SMOKE E HSYA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 05 903FE 208B0003 STRONG SMELL OF BURNING OR BURNT INSULATION AND A SLIGHT HAZE OF SMOKE IN COCKPIT. BOTH THE LEFT AND RIGHT INSTRUMENT P ANELS AND WIRING WERE INSPECTED FOR OBVIOUS DAMAGE. PERFORMED GROUND RUNS WITH ALL COCKPIT INSTRUMENTS ON AND COULD NOT DUPLICATE THE PROBLEM. THE AIRCRAFT RETURNED TO SERVICE WITHOUT FURTHER INCIDENT. 1 H 7 1 3T A37CE 20081023 SO 2008 10 23 FDKA2008101900277 1 20081019 A 3350 1317 SIGN EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FRL FLT 8910 JFK. RT EMERGENCY EXIT DOOR SIGN OUT. MX RELAMPED AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081023 EA 2008 10 23 MASA2008101700733 1 20081017 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA NR 1 MALFUNCTIONED A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 17231 23879 7231 ASH FLT 2925 FAT-PHX. CAPTAIN REPORTED SMOKE IN FLIGHT DECK CAUSED BY LT PACK. MX REMOVED AND REPLACED NR 1 ACM, OPS C HECKED GOOD. 2 L 7 2 4F RT A21EA 20081024 NM 2008 10 24 DLM88081361 1 20081014 A 5311 9923406504 FRAME DOUG MD88 MD88 3023688 NM BS 886 L18R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 916DL 49591 THE RT FS 886 FRAME WAS FOUND CRACKED JUST BELOW THE PASSENGER FLOOR LINE. THE FRAME WAS REPLACED PER ER/A 09-097023-14 . THE REPAIR OCCURRED DURING MARCH 2005 BUT A PREVIOUS MRR RECORD COULD NOT BE FOUND. 2 L 7 2 4F RT A6WE 20081024 NE 2008 10 24 DL76L081363 2 20081014 A 7210 NOZZLE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 181DN 61256 25986 724415 FAILED INSPECTION OF MAIN GEARBOX OIL NOZZLES PER EA-51470869-12 ON NR 1 ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081024 NM 2008 10 24 08FDEA04348 1 20081014 A 5315 BAC1505100617 FLOORBEAM BOEING 757 757236 1384971 NM BS 1280 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 FLOORBEAM STA 1280 UPPER SURFACE LBL 60 TO RBL 60 HAS GOUGES. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00- 51, FIG 101 DETAIL III. REMOVED DAMAGED AREA OF FLOORBEAM UPPER CHORD, FABRICATED NEW CHORD, LOCATED AND DRILLED ANGLES AND STRAPS IAW SRM 53-00-51, FIG 201. TREATED AND PRIMED NEW CHORD AND INSTALLED CHORD, ANGLES AND STRAPS IAW SRM 51-2 0-01. THIS IS A CATEGORY "A" REPAIR "MAJOR REPAIR" 2 L 7 2 4F RT A2NM 20081024 EU 2008 10 24 08FDEA04349 1 20081015 A 7830 491B1313000299 FRAME AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 668FE 772 NR 2 ENG INBD THRUST REVERSER HAS A CRACK .225 INCH LONG ON UPPER FWD END FRAME ROUTED CRACK ON NR 2 ENG INBD T/R TORQUE BOX FWD FRAME AND REPAIRED IAW FEDEX EA 6-7830-124136, RELEASE DATE 8 OCTOBER, 2008. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 08FDEA04350 1 20081015 A 5347 A53274788204 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 677FE 791 MAIN DECK CARGO COMPT SEAT TRACK NR 1 HAS DAMAGED SCALLOP, FR 71, .30 INCH LONG BY .15 INCH WIDE BY .020 IN DEEP. REMOV ED DAMAGED SECTION OF SEAT TRACK NR 1 AND INSTALLED SEAT TRACK SPLICE. REPAIR BETWEEN FR 71 AND FR 72 IAW A300-600 SRM 53-10-16, FIG 201, PAGE 207/208. 2 L 7 2 4F RT A35EU 20081024 NM 2008 10 24 SWAA085648 1 20081016 A 3350 417A5500 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED HC2 CHECK, FOUND RT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085619 1 20081019 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUOUT BELOW FWD END OF HINGE CUTOUT. REP AIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085625 1 20081019 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM CORRODED AT BETWEEN RT BS 480 TO BS 492. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081024 EU 2008 10 24 USAABA08031 1 20081022 A 3350 32146210 EPSU AIRBUS 330 A330323 3930335 EU CABIN FAULTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AY 0375 PHL - THERE WAS AN EPSU FAULT FOR THE R3 DOOR. MAINTENANCE REPLACED THE R3 DOOR EMERGENCY POWER SUPPLY UNIT. OPERATION ALLY CHECKS OK. 2 L 7 2 4F RT A46NM 20081024 2008 10 24 USAA EMB08017 4 20081021 A 2565 1040031 SLIDE EMB ERJ190 ERJ190100IGW 3260408 NM L1 DOOR UNWANTED DEPLOY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 950UW 19000106 CLT - L1 DOOR SLIDE PARTIALLY DEPLOYED, LACING UNDONE. MAINTENANCE REPLACED THE L1 SLIDE. 2 L 7 2 4F RT A57NM 20081024 EU 2008 10 24 08FDEA04390 1 20080916 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU RT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 725FD 572 RT WING, INBD FLAP WITH ACCESS HOLE AT RIB 7 OVER DIMENSIONAL AT INNER LOWER SKIN SURFACE, IT WAS REPAIRED IAW EA 6-5750 -121702. 2 L 7 2 4F RT A35EU 20081024 WP 2008 10 24 08FDEA04391 1 20081017 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP BS 690 S50 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 FOUND 2 DENTS ON THE LOWER FUSELAGE AT STA 690, STRINGER 50. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04393 1 20081017 A 5730 ARC0254501 PANEL DOUG MD10 MD1010F 3022112 WP LT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 LEFT WING INBD LOWER T/E PANEL 541 KB IS CHAFED. REPAIRED PANEL BY BONDING A DOUBLER IAW SRM 51-71-00. REMOVED & RE-IN STALLED PANEL IAW SRM 51-31-01. 2 L 7 3 4F RT A22WE 20081024 EU 2008 10 24 08FDEA04357 1 20081015 A 5320 ANGLE AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 LEFT TRANSITION ANGLE IN THE BULK PIT IS CORRODED FROM FRAME 64 TO 67. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 08FDEA04362 1 20081015 A 5311 10A25771822208 FRAME AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 AFT LOWER CARGO COMPARTMENT HAS CORROSION ON THE POWER ROLLER PAN AND SUPPORT AT FRAME 58; LBL 41 INCH (LOWER SURFACE). REMOVED PAN AND FRAME IAW SRM 51-41-21. REMOVED CORROSION IAW SRM 51-71-10. BOTH FOUND TO BE OUT OF LIMITS IAW SRM 53 -10-00. FABRICATED NEW FRAME P/N 10A25771822-208 IAW DWG 3 10A25771822. ALODINED IAW SRM 51-21-10. PRIMED IAW SRM 51- 75-10. PAINTED IAW SRM 51-75-10. LOCATED AND DRILLED HOLES IN NEW PAN AND FRAME IAW SRM 51-40-44 AND SRM 51-72-10. PA RT MARKED IAW GMM 7-0-1000. INSTALLED PAN AND FRAME IAW SRM 51-40-21. INSTALLED PDU IAW AMM 25-54-26-04. 2 L 7 2 4F RT A35EU 20081024 NM 2008 10 24 SWAA085613 1 20081019 A 5315 6556804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 782SA 29808 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 43. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081024 EA 2008 10 24 VNAA2008102300009 1 20081020 A 3260 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A VNAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 05 207PS 8241 7873 CREW REPORTED A GEAR DISAGREE WARNING. CREW ELECTED TO RETURN TO PHL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE I NSPECTED AND FOUND A HYDRAULIC LEAK AROUND THE NLG AREA AND FOUND A BAD PROXIMITY SENSOR ELECTRONIC UNIT (PSEU). REPAIR S WERE MADE AND PSEU WAS REMOVED AND REPLACED. CHECKS WERE PERFORMED. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 20081024 NM 2008 10 24 UPS08653683 1 20081012 A 5315 141T514616 STIFFENER BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 331UP 27757 INSPECTION TYPE:N/A MAIN DECK FLOORBEAM ATTACH STIFFENER AT STA 246 LBL 50 CRACK FOUND CRACK LENGTH .875 INCH. MAIN DEC K STA 246 LBL 50 FLOORBEAM ATTACH STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20081024 NM 2008 10 24 UPS08653687 1 20081013 A 5711 SPAR BOEING 767 76734AF 1385212 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 331UP 27757 INSPECTION TYPE:N/A RT WING ILES677 FRONT SPAR D-NOSE I/B FOUND CRACK AS MARKED CRACK LENGTH .75 INCH. RT WING ILES677 FRONT SPAR D-NOSE BEAM WEB REPAIRED AS PER SRM 57-41-13-2R FIG 201. 2 L 7 2 4F RT A1NM 20081024 NM 2008 10 24 UPS08653689 1 20081010 A 5753 HINGE FITTING BOEING 767 76734AF 1385212 NM TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 331UP 27757 INSPECTION TYPE:N/A LT WING I/B MAIN FLAP AFT FLAP I/B HINGE FITTING CRACK. CRACK LENGTH .875 INCH APPROX. LT WING I/B MAIN FLAP AFT FLAP I/B HINGE FITTING REPAIRED AS PER SRM 57-53-02-2R FIG 201. 2 L 7 2 4F RT A1NM 20081024 NM 2008 10 24 SWAA085638 1 20081020 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED BS 727D, STR 9R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085665 1 20081021 A 5312 65485409 BULKHEAD BOEING 737 7373H4 1384600 NM LT MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND LT MAIN GEAR W/W FWD PRESSURE BULKHEAD CRACKED NEXT TO AILERON CONTROL SHAFT. REPAIRE D WEB PER AAR EA. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085680 1 20081021 A 3350 311500 LIGHT BOEING 737 7373H4 1384600 NM CABIN NOT SEATED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND AFT RT OVERHEAD EMERGENCY EXIT LIGHT INOP. RESEATED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085682 1 20081021 A 5330 6550570 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR LOWER FWD FUSELAGE SKIN CUTOUT CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081024 EU 2008 10 24 UPS08153702 1 20081014 A 5321 B5327079500000 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 140UP 0823 INSPECTION TYPE:1C3C MAIN CARGO DECK FLOORBOARD 241XK HAS FIELD REPAIR. REPAIRED MAIN CARGO DECK FLOORBOARD 241XK REF A 300-600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081104 WP 2008 11 4 UPS08853727 1 20081002 A 5720 STIFFENER DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATE EFN 70220061052 ORIGINAL NR 902713 CRACKED STIFFENER IN 2ND L/E LEADING EDGE ACCESS HOLE OUT BOARD OF NR 3 PYLON. REPAIRED BY 57-02-00. 2 L 7 4 4F RT 4A25 20081024 NM 2008 10 24 WX0A070242 1 20081001 A 3350 AD4002 BATTERY DOUG MD80 MD83 3023681 NM CABIN DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 876G 53469 OVERHEAD EMERGENCY LIGHT IN TAIL CONE AREA. DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLIS HED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT 20081024 NM 2008 10 24 DL76L081356 1 20081013 A 8012 START VALVE BOEING 767 767332 1382001 NM NR 1 ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 192DN 28449 RTB DUE TO LT ENG W/N START. START VALVE LIGHT W/N EXTINGUISH. EXERCISED START VALVE. SPUN NR 1 ENG OPS NML. STARTED ENG AT GATE. NORMAL START OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20081024 WP 2008 10 24 08FDEA04394 1 20081017 A 5730 ARC0358503 PANEL DOUG MD10 MD1010F 3022112 WP LT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 LEFT WING INBD LOWER T/E PANEL 541 FB IS CHAFED. REPAIRED CHAFED AREAS BY BLENDING AND FOUND OUT IF LIMITS. FABRICATE D REPAIR DOUBLER & BONDED IAW SRM 51-71-00, 51-21-01 & 51-31-01. ALODINED, PRIMED & SEALED IAW SRM 51-21-01. RE-INSTAL LED HINGE REMOVED TO F.O.M. IAW SRM 51-31-01. REMOVED & RE-INSTALLED PANEL IAW SRM 51-31-01. 2 L 7 3 4F RT A22WE 20081023 EA 2008 10 23 SWIA200820148 1 20080518 A 5315 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 435SW 7555 RIGHT LOWER FLOORBEAM 280 SUPPORT CRACKED (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 UPS08M53591 1 20081007 A 5730 SPLICE DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:1C RT WING L/E SKIN SPLICE STRAP XFS 791 CRACKED. REMOVED AND REPLACED SKIN SPLICE STRAP IAW SRM DWG AR B3954, 51-33-01, 51-21-01. 2 L 7 3 4F RT A22WE 20081023 NM 2008 10 23 2008UALA06083 1 20081013 A 3350 767 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 566UA 26670 DOOR NR 2 LT AND RT EMERGENCY EXIT LIGHT INOP (EXT). LAMPS INOP. RELAMPED, OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 NM 2008 10 23 2008UALA06130 1 20081015 A 2910 HYDRAULIC LINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HYDRAULIC SYS CRACKED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 648UA 25285 HYDRAULIC PROBLEM. RTFL. FOUND HYDRAULIC LANDING GEAR UP TUBE ASSY CRACKED. ALSO 2 OTHER TUBES INTERFERING AND DAMAG ING. REPLACED TUBES OKAY. LEAK CHECK CARRIED OUT NO FAULTS FOUND. SURROUNDING AREA CLEANED OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081023 NM 2008 10 23 2008UALA06133 1 20081015 A 2560 MECHANISM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GIRT BAR DEFECTIVE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 506UA 24627 DOOR 4R AFTER ARMING SLIDE GRIT BAR FEEL OFF. AFTER REPLACING SHEARED RIVET, REINSTALLED SLIDE. GIRT BAR STILL COMES O FF WHEN OPENING UNARMED DOOR, NEEDS T/S OF GIRT BAR MECHANISM. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 NM 2008 10 23 USAA920081677 1 20080822 A 5315 6546811 FLOORBEAM BOEING 737 7373G7 138447J NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CORROSION ON FLOORBEAM BETWEEN BS 986.5 TO 1006, RBL 15. REPAIRED FLOORBEAM IAW SRM 53-00-51. (K) 2 L 7 2 4F RT A16WE 20081023 EU 2008 10 23 USAA920081909 1 20081016 A 3230 664700500A4D CONTROL UNIT AIRBUS 320 A320232 3930326 EU MLG FAILED A USAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 19 654AW 26974 3428 1050 FLT 71 EMERGENCY LANDING - FLIGHT WAS ON APPROACH WHEN THE FLAPS FROZE AT 2 DEGREES. THE CAPTAIN DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINT DETERMINED FLAPS EXTENSION AND RETRACTION TO BE NORMAL. NO FAULTS WERE FOUND DURING TROUBLESHOOTING AND OPERATIONAL CHECKS. SUBSEQUENTLY DURING ROLLOUT ON LANDING, CREW RECEIVED A FLAP ATTACH SENSOR LGCI U 1 FAULT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL INTERFACE UNIT IAW MM 32-31-71. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081023 NM 2008 10 23 2008UALA06139 1 20081015 A 2560 69B528083 HOUSING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT OVERWING CRACKED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 644UA 25094 LT OVERWING DISCONNECT HOUSING IS CRACKED. REPLACED DISCONNECT HOUSING. FREEDOM OF MOVEMENT. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081023 EU 2008 10 23 2008UALA06142 1 20081015 A 3520 MF20010 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LAVATORY MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 442UA 780 LAVATORIES D AND F O2 MASKS IMPROPERLY PACKED. FOUND MASKS RE-STRAINED BY OXYGEN GENERATOR FABRIC HEAT SHIELD IN LAVS D & F PREVENTING PROPER DEPLOYMENT. REMOVED MASKS REPOSITIONED HEAT SHIELD AND PACKED MASKS PROPERLY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081023 NM 2008 10 23 2008UALA06143 1 20081015 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 LT OVERWING EMERGENCY LIGHT INOP. REPLACED EMERGENCY BATTERY PACK. OPS CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 NM 2008 10 23 2008UALA06144 1 20081016 A 3040 CONTROLLER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE WINDOW HEAT MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 215UA 30221 WINDOW HEAT L FWD LOSS OF LEFT FORWARD WINDOW HEAT. ADVISORY - REPLACED LT WINDOW HEAT CONTROLLER. TEST OK, MSG CLEARE D. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081023 NM 2008 10 23 2008UALA06145 1 20081016 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EMERGENCY LIGHT SEAT 5A AFT INOP. REPLACED EMERGENCY LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 2008 10 23 2008UALA06150 4 20081016 A 2330 7430193014 VIDEO UNIT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN SMOKE A UALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 WP 29 551UA 25399 SMOKE DETECTED AT MID GALLEY LAV. SMOKE COMING OUT OF VIDEO SYSTEM CONTROL UNIT DURING PREFLIGHT. STOPPED WHEN POWER T URNED OFF. REPLACED VIDEO CONTROL UNIT. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 NM 2008 10 23 USAABB08161 1 20081017 A 2450 CIRCUIT BREAKER BOEING 757 7572S7 1384962 NM ELECTRICAL SYS FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 905AW 23567 FLT 119- IN CRUISE, LT AC BUSS FAILED. GENERATOR RESET DID NOT CORRECT CONDITION. ATTEMPTS TO POWER LT AC BUSS FROM OT HER POWER SOURCES NOT SUCCESSFUL. FLT DIVERTED & LANDED WITHOUT INCIDENT. REPLACED GROUND POWER CONTACTOR, CURRENT XFOR MERS, & BUSS TIE C/B, NO EFFECT. PERFORMED FIM PROCEDURE 24-22-00. NO FAULTS FOUND. FOUND A SUSPECTED SHORTED AFT GAL LEY FEEDER WIRE. WIRES DISCONNECTED, ISOLATION STILL OCCURRED. PROBLEM ISOLATED TO LT XFER BUSS & CAPTAIN'S CDU. WITH CDU REMOVED, OPS OK. DETERMINED CAPTAIN'S CDU C/B HAD MALFUNCTIONED. REPLACEMENT FIXED THE CONDITION. WIRE CHECKED OK & REINSTALLED. COFFEEMAKERS & GALLEY POWER LOAD CONTROL UNIT REPLACED. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 USAASB08098 1 20081020 A 3350 1012721 LIGHT BOEING 737 73733A 1384673 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 166AW 23627 DFW - MAINTENANCE REPORTED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT 14L INOPERATIVE. MAINTENANCE REMOVED AND REPLACED TH E LIGHT ASSEMBLY AT SEAT 14L. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 ASAA0853588 1 20081009 A 4930 4419215 FUEL CONTROL BOEING 737 737890 1384527 NM APU LEAKING A ASAA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 02 556AS 9930 35175 CHEMICAL FUMES SMELL IN FLT DECK FWD GALLEY. FOUND OIL LEAKING FROM FWD DRAIN (5) AT RATE OF 1 DROP EVERY 10 SECONDS. ALSO FUMES IN CABIN WHEN SELECTED FOR PACK OPERATION FOUND LEAK FROM APU FUEL CONTROL DRAIN. REMOVED AND REPLACED APU F UEL CONTROL PER MM 49 31 11. OPS CHECK GOOD. NO LEAKS NOTED. 2 L 7 2 4F RT A16WE 20081024 EA 2008 10 24 ASOA200801368 1 20081019 A 2711 TRIM SYSTEM CNDAIR CL600 CL6002B19 1900309 EA AILERON MALFUNCTIONED A ASOA K NONE F FLT CONT AFFECTED CL CLIMB 1 SO 27 855AS 7395 A/C YAWED EXCESSIVELY TO THE RIGHT DURING FLIGHT, THE A/C WOULD NOT STAY TRIMMED. AFTER ENGAGING THE AUTOPILOT, THE AUT OPILOT HAD DIFFICULTY MAINTAINING THE FLIGHT CONTROL INPUTS. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. (AILERON TRIM SYSTEM) 2 L 7 2 4F RT A21EA 20081024 WP 2008 10 24 08FDEA04395 1 20081017 A 5753 ARC0267602 PANEL DOUG MD10 MD1010F 3022112 WP RT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 RIGHT WING INBD T/E FLAP PANEL 641 BR IS CHAFED. REPAIRED TWO AREAS OF CHAFING BY REMOVING DAMAGED AREAS & FABRICATING & BONDING A FILLER & DOUBLERS IAW SRM 51-71-00. REMOVED CAM LOCKS TO FACILITATE REPAIR & RE-INSTALLED IAW SRM 51-31-01. ALODINED, PRIMED, & SEALED THE REPAIRS IAW SRM 51-21-01 & 51-41-01. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04397 1 20081017 A 5230 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 MAIN CARGO DOOR NR 1 SPOOL BACK UP FITTING HOLES "A"; "B" AND "C" HAVE CRACK INDICATIONS. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 UPS08653686 1 20081010 A 5320 140T0130U38 SUPPORT FITTING BOEING 767 76734AF 1385212 NM CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 331UP 27757 INSPECTION TYPE:N/A AFT CARGO COMPT STA 1086 RBL 26 PARTITION FRAME BOTTOM SUPPORT CLIP CRACKED, CRACK LENGTH .75 INCH. SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081024 WP 2008 10 24 08FDEA04402 1 20081017 A 5230 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 MAIN CARGO DOOR NR 7 SPOOL BACK UP FITTING HOLES "A"; "B"; "C" AND "D" HAVE CRACK INDICATIONS. REPAIRED MAIN CARGO DOOR SPOOL FITTING IAW SRM 53-50-00. 2 L 7 3 4F RT A22WE 20081024 EU 2008 10 24 08FDEA04403 1 20081017 A 5420 A5461144120200 SUPPORT AIRBUS 300 A300B4622R 3930312 EU NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 NR 1 PYLON INBD SIDE PANEL SUPPORT IS CRACKED AT RIB 8A, (PANEL 414CR). REMOVED & REPLACED PYLON SIDE PANEL SUPPORT R EF SRM 51-40-21. LOCATED & DRILLED FASTENER HOLES IN THE NEW PYLON SIDE PANEL SUPPORT REF SRM 51-40-44. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 08FDEA04405 1 20081017 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 AFT PIT AT FRAME C 62, LBL 32, THE FLOOR ANGLE SUPPORT IS CRACKED. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 08FDEA04423 1 20081011 A 2800 UNKNOWN AIRBUS 310 A310203 3930313 EU UNKNOWN A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 21 425FE 264 LO TANK READ 1200 LBS LESS AFTER 1 HR T/O. GAUGE HAD DASH IN LAST DIGIT. DASH WENT AWAY. FQI CONTINUED TO DECREASE TO 1200 TOTAL. ON DESCENT FUEL INCREASED, AT LDG FQI READ OK. RELEASE FOR SVC/MEL 28-42-01-01 CAT: C EXP: 21OCT08 ALL LO TANK IND INOP. FUEL TO KNWN QTY/VERIFY TANK QTY WITH MAG STICKS. VERIFIED LO TANK STICK PER 12-11-28 6273LBS AT BLOCK IN. NO LEAKS ON LEFT WING EXT SURFACES. FQ ONBD FUEL USED = 55880LBS. PREV FUEL SLIP FUEL WAS 56.9KLBS. NO FAULTS FLT 1463 REPORTED FQID GOOD ON THIS LEG. FQIS NOTED, 322, 703, 704. PER TSM 28-42-00 CODE SHOULD NOT BE T/S, INTERMIT TENT ON BITE, AND SHOULD BE LOGGED, CHK AFTER NEXT FLIGHT. FQI CK OK ; 2 L 7 2 4F RT A35EU 20081024 NM 2008 10 24 08FDEA04424 1 20081018 A 5754 PANEL BOEING 757 75723A 1384967 NM NR 2 SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 NR 2 LEADING EDGE SLAT COVE PANEL, INBD OF OTBD MAIN TRACK IS CRACKED. REMOVED AND REPLACED COVE PANEL IAW SRM 51-40-02 AND DRAWING, NR 114N4076. 2 L 7 2 4F RT A2NM 20081024 NM 2008 10 24 08FDEA04425 1 20081018 A 5310 WINDOW FRAME BOEING 757 75723A 1384967 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 LIGHTNING STRIKE, LT CABIN WINDOW CUT OUT BS 395- BS 418. REPAIRED LIGHTNING STRIKE IAW SRM 56-20-02 REPAIR NR 1 FIGURE 201 SHT, 3 MAJOR REPAIR. NO FOLLOW-UP INSPECTION REQUIRED. 2 L 7 2 4F RT A2NM 20081024 NM 2008 10 24 08FDEA04480 1 20081022 A 5320 652954853 PAN BOEING 727 7272D4 138407U NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FUSELAGE UPPER LOBE INTERIOR STRUCTURE, DITCHING PANEL CRACKED AT STA 1183 RBL 70. REMOVED DAMAGED DITCHING PAN, FABRIC ATED AND HEAT TREATED NEW DITCHING PAN, INSTALLED NEW DITCHING PAN (CLASSIFIED AS A MINOR REPAIR ) REF DWG 65-29548-53 & SRM 51-30-02 2 L 7 3 4F A3WE 20081024 NM 2008 10 24 08FDEA04479 1 20081022 A 5320 652954817 ANGLE BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 PASSENGER CABIN, BULKHEAD 1183 DITCHING PAN, LBL 19 ATTACH BRACKET CRACKED. REPLACED ANGLE IAW SRM 51-30-02 & DWG 65-29- 567. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081024 WP 2008 10 24 UPS08853700 1 20081020 A 3350 BATTERY DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE:N/A DURING EMERGENCY LIGHT CHECK, EMERGENCY STANDBY LIGHTS FAILED TO ILLUMINATE. REMOVED & REPLACED EME RGENCY LIGHT BATTERY / RELAY ASSY PER MM 33-50 -01-2. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 20081024 NM 2008 10 24 UPS08M53693 1 20081017 A 5730 SKIN DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:1C LT WING FIXED L/E TELESCOPIC DUCT CUTOUT FOUND CRACKED AS MARKED. CUT OUT CRACK, FABRICATED, AND INS TALLED DOUBLER IAW MD-11 SRM VOL 1 57-10-00 PG 133. 2 L 7 3 4F RT A22WE 20081024 EU 2008 10 24 08FDEA04389 1 20081017 A 5311 FRAME AIRBUS 300 A300B4622R 3930312 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 MAIN CABIN FRAME 33 IS GOUGED AT APPROXIMATELY LONGERON 15 L. 2 L 7 2 4F RT A35EU 20081024 NM 2008 10 24 UPS08M53714 1 20081021 A 3350 6044115 BATTERY DOUG MD11 MD11F 3023600 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 273UP 48574 INSPECTION TYPE:N/A DURING AS-N FOUND EMERGENCY LIGHT BATTERY NR 1 LOW. REMOVED AND REPLACED NR 1 EMERGENCY BATTERY IAW AMM 33-51-01-4. TEST IAW 33-51-01-700- 802 SATIS. 2 L 7 3 4F RT A22WE 20081024 SO 2008 10 24 RAIA2008192300002 1 20081019 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 832HK 145771 DURING PRE FLIGHT INSPECTION, EMERGENCY LIGHT AT THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESECURED TH E CONNECTOR TO THE LIGHT ASSEMBLY. LIGHT OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081024 SO 2008 10 24 RAIA2008102300004 1 20081020 A 3397 WIRE EMB 145 EMB145 3260210 SO CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 821HK 145068 AFT EMERGENCY TRACK LIGHT AT ROW 17 PULLED OUT OF TRACK. MAINTENANCE REPAIRED THE BROKEN WIRES TO THE LIGHT STRIP AND I NSTALLED THE ORIGINAL LIGHT STRIP. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 20081024 SO 2008 10 24 RAIA2008102300005 1 20081020 A 3350 RPS1B BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 852HK 145353 DURING INSPECTION, EMERGENCY LIGHT AT ROW 12 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENC Y LIGHT BATTERY PACK. OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081024 NM 2008 10 24 AALA200802444 1 20080925 A 3597 CONNECTOR BOEING 757 757223 1384957 NM CREW O2 LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 194AA 32388 INFLIGHT T267/25SEP MIA TO LAX. CREW REPORTED CREW OXYGEN INOPERATIVE INDICATION DURING CRUISE. LANDED IAH WITHOUT INC IDENT. SECURED LOOSE CONNECTOR AT BOTTLE PRESSURE TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081024 WP 2008 10 24 AALA200802467 1 20080930 A 5280 5936791504 DOOR DOUG DC9 DC982 3022082 WP RT MLG SEPARATED A AALA O OTHER D J INFLIGHT SEPARATION WARNING INDICATION CL CLIMB 1 SW 21 14551 53033 INFLIGHT T376/30SEP. CREW REPORTED RT GEAR DOOR OPEN LIGHT REMAINED ON AFTER RETRACTION. RAN CHECKLIST AND LIGHTS WENT OUT. NO OTHER ABNORMAL INDICATIONS REPORTED. LANDED DFW WITHOUT INCIDENT AND FOUND RLG STRUT DOOR MISSING WITH HINGE STILL ATTACHED TO ACFT. BOTH SUPPORT RODS HAND THE ENDS THAT ATTACHED TO THE DOOR BROKEN OFF AND MISSING. REMOVED DAMA GED HINGE AND REPLACED RLG DOOR ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081024 NM 2008 10 24 AALA200802402 1 20080921 A 2432 425404 CHARGER BOEING 767 767323 1385205 NM MAIN BATTERY FAULTED A AALA O OTHER O OTHER DE DESCENT 1 SW 21 390AA 27450 MAN INFLIGHT T54/21SEP. PRIOR TO FLAP EXTENSION LEADING EDGE ASYMMETRY AND EICAS MSG ILLUMINATED. LANDED WITHOUT INCID ENT MAN WITH 20 DEGREE FLAPS NO SLATS. CLEANED NR 10 SLAT SENSOR AND REPLACED MAIN BATTERY CHARGER. SYSTEM GROUND CHEC KED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081024 WP 2008 10 24 AALA200802400 1 20080921 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 554AA 53084 DFW EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 11 TO 17 INOPERATIVE. REPLACED BATTERY PACK AT STATION 700 FOR EMERGENCY LIG HTS AT OVERHEAD SEAT ROWS 11 TO 17. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081027 EU 2008 10 27 M7KA0628084134 1 20080901 A 6797 WIRE HARNESS UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE POTENTIOMETER DAMAGED E M7KA E ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 WP 19 821MH 1580 4134 23319 FAILURE CODE AT SHUTDOWN INDICATED FAULT WITH THE COLLECTIVE POTENTIOMETER. A NEW POTENTIOMETER WAS INSTALLED AND NO FUR THER DEFECT REPORTED. IT WAS RECENTLY DISCOVERED THAT THE ROUTING OF AIR CONDITIONING SYSTEM WIRING IN CONTACT WITH THE UNSHIELDED ELECTRICAL HARNESS FOR THE POTENTIOMETER WAS CAUSING SPURIOUS SIGNALS IN THE CONTROL DATA WHICH WERE INTERPRE TED AS A PONTENTIOMETER FAILURE. DOZENS OF THESE PONTENTIOMETERS WERE REPLACED. REROUTING THE AIR CONDITIONING WIRING HA S ALMOST ENTIRELY ELIMINATED THE NEED TO REPLACE THESE POTENTIOMETERS. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 EU 2008 10 27 MK7A0811084266 1 20080901 A 5350 350A31201621 FAIRING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE MAIN ROTOR CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 817MH 912 4125 23416 FOUND CRACKS RADIATING FROM A SINGLE SCREW BORE DURING ROUTINE INSPECTION. INSTALLED NEWLY REPAIRED AND PAINTED ASSY. FO LLOWING DOUBLER INSTALLATION AT SCREW BORE POSITIONS. THIS PART HAS HAD A HISTORY OF SIMILAR CRACK DEVELOPMENT UNTIL DOU BLERS WERE APPLIED. CURRENTLY NEW ACFT ARE DELIVERED FROM THE FACTORY WITH DOUBLER INSTALLED AT THESE SCREW BORE POSITIO NS. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 EU 2008 10 27 M7KA0524083912 1 20080804 A 6320 S1130021089 PRESSURE SENSOR UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE M/R GEARBOX MALFUNCTIONED E M7KA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 807MH 3912 23473 OIL PRESSURE LIGHT ILLUMINATES AT GROUND IDLE. NEW SWITCH NORMALLY WORKS WELL BUT ON OCCASION LOSES INTERNAL CALIBRATION OR IS MISCALIBRATED AS NEW SWITCHES SOMETIMES EXHIBIT THE SAME PROBLEM. SUGGEST A MORE MODERN DESIGN BE CONSIDERED FOR THIS PART. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 EU 2008 10 27 M7KA0810084266 1 20080901 A 5210 350A581020 HINGE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE DOOR CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 847MH 4266 23416 FOUND SEVERAL HINGE SEGMENTS CRACKED ON ONE END OF THE HINGE LENGTH DURING ROUTINE INSPECTION. THIS IS FAIRLY COMMON DE FECT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 EU 2008 10 27 M7KA0817084022 1 20080901 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ECDS FAILED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 815MH 436 4022 4022 46079 AMBER GOVERNOR LIGHT ILLUMINATED IN FLIGHT AND SUBSEQUENT TO FAILURE REPORT GENERATION THE COLLECTIVE POTENTIOMETER WAS INDICATED TO BE DEFECTIVE. A NEW PART WAS INSTALLED AND NO FURTHER DEFECT NOTED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 EU 2008 10 27 M7KA0706084131 1 20080804 A 5344 350A58004523 HINGE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE FUSELAGE CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 818MH 4131 23322 DURING ROUTINE INSPECTION CRACKS ON THE HINGE SURFACE RADIATE FROM MOUNTING BORES. THIS IS A VERY COMMON FAILURE FOR THI S PART. SUGGEST PART BE MANUFACTURED FROM A MORE DURABLE MATERIAL SUCH AS STAINLESS STEEL OR TITANIUM. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 NE 2008 10 27 M7KA0716084038 2 20080901 A 7412 9550177760 EXCITER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE LEFT INOPERATIVE E M7KA K NONE L NO TEST IN INSP/MAINT 1 WP 19 816MH 4038 23096 DURING ROUTINE INSPECTION THE LT POSITION IGNITER WOULD NOT FIRE. SWAP OF BOX OUTPUT FEEDS TO THE IGNITERS VERIFIED THE BOX CIRCUIT WAS DEFECTIVE. THIS BOX GAVE GOOD SERVICE BUT SEVERAL OTHER HAVE HAD PROBLEMS WITH LOW SERVICE HOURS THESE B OXES ARE NON-REPAIRABLE. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 NM 2008 10 27 DHLA2008745541 1 20080905 A 5753 STRAP BOEING 727 727224 1384076 NM RT WING TE FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 RT WING I/B MID FLAP L/E INNER SECTION STRAP WITH CORROSION FROM WBL 127 TO 143. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DHLA2008745542 1 20080905 A 5753 ANGLE BOEING 727 727224 1384076 NM LT WING TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LT WING I/B MID FLAP T/E I/B SECTON AFT LOWER CHORD ANGLE CRACKED AT WBL 125. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DL757081367 1 20080819 A 5297 TERMINAL BOEING 757 757232 1384965 NM L2 DOOR TEST SWH BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 EMERGENCY LIGHT TEST SWITCH AT L2 DOOR HAS A BROKEN COVER AND TERMINAL. (OFF A/C PART). PROCURED EMERGENCY LIGHT TEST SWITCH FOR L2 DOOR. REPLACED SWITCH ON DELTA OPN 1818 AND TESTED ON DELTA OPN 6813. 2 L 7 2 4F RT A2NM 20081027 NM 2008 10 27 DL76L081368 1 20081016 A 3150 WARNING LIGHT BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENG FALSE ACTIVATION A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 191DN 28448 727654 AFTER LT ENG START AND APU SHUTDOWN LEFT GEN OFF LIGHT WITH LT ISOLATION BUSS TIE LIGHT. RAN ENG CYCLED POWER FOR LT EN G AND APU SEVERAL TIMES WITH LOAD ON GENERATORS. PERFORMED BITE AND BPCU HAD PILOT DUPLICATE POWER TRANSFER. WHEN PROB LEM OCCURRED NO FAULTS NOTED. LT GEN AND APU AND A/C POWER OPS CHEC K NORMAL AS PER AMM. 2 L 7 2 4F 4 F RT A1NM E24NE 20081027 NE 2008 10 27 DL738081370 2 20081016 A 7200 CFM567 ENGINE BOEING 737 737832 13844CF NM GE CFM56 CFM56* 13802 NE NR 1 SEIZED A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 3748Y 19037 30489 876675 DURING CRUISE AT FL 370 ENGINE SEIZED. BOTH N1 AND N2 RAPIDLY DECREASED TO ZERO. AUTOPILOT KICKED OFF AND SIGNIFICANT AILERON INPUT REQUIRED TO RETURN TO WINGS LEVEL. DIVERTED TO ORD. NO LOSS OF ENGINE OIL. NO PREVIOUS VIBRATIONS. NO WARNING OST FLIGHT CREW COULD NOT MOVE FAN IN ANY DIRECTION. NO METAL OR DEBRIS IN INLET OR EXHAUST. 2 L 7 2 4F 4 F RT A16WE E2GL 20081027 NM 2008 10 27 DHLA2008745548 1 20080902 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN AT BS 720 S-8R FRAME DOUBLE HOLE. REPAIRED FUSELAGE FRAME SECTION T BS 720 BETWEEN S-7R AND S- 9R IAW B727 SRM 53-10-4 FIG 2. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DHLA2008745549 1 20080902 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN AT BS 720B S-8R FRAME WITH DOUBLE HOLE. REPAIRED FUSELAGE FRAME SECTION AT BS 720B BETWEEN S-7 R AND S-9R IAW B727SRM 53-10-4 FIG 2. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DHLA2008745551 1 20080902 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN AT BS 720B BETWEEN S-13L AND S-14L FRAME WITH DOUBLE HOLE. REPAIRED FUSELAGE FRAME SECTION AT BS 720B BETWEEN S-11L AND S-14L IAW B727 SRM 53-10-4 FIG 1 AND DETAIL 1. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DHLA2008745552 1 20080904 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN BS 950 BETWEEN LBL64 FLOORBEAM UPPER CHORD UPPER AND LOWER FACE CORROSION. REPAIRED UPPER FUSE LAGE FLOORBEAM UPPER CHORD AT BS 950 BETWEEN RBL 30 TO RBL42 IAW COOPESA EO NR COO-2-52-268-08 DTD SEPT 11 2008 DOCUMENT ED ON FAA FORM 8110-3 DTD SEPT 29,2008 AND ASTAR AIRCARGO EVA B253-00108 DTD OCT 9,2008 REV IR. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DHLA2008745554 1 20080905 A 5347 CARGO TRACK BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN FROM STA 344 TO 600 RBL 25 CARGO TRACK WITH CORROSION. REPLACED TRACK AT RBL 25 FROM BS 480 TO BS 600 IAW B727SRM 51-10-1 PARA 7A AND REF. VENTURA AEROSPACE 9G CARGO BARRIER INSTALLATION B727-100/200 STRUCTURAL RE PORT NR 2489 REVA DTD 9/13/07 PARA 5.4 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DHLA2008745537 1 20080907 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 200 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN AT BS 670 BETWEEN STRINGER 14L AND 17L FRAME WITH WEAR. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DHLA2008745538 1 20081010 A 5313 STRINGER BOEING 727 727224 1384076 NM ZONE 100 MISINSTALLED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 480 STRINGER 28L WITH IMPROPER SPLICE. 2 L 7 3 4F A3WE 20081024 NM 2008 10 24 08FDEA04481 1 20081022 A 5320 652954811 SUPPORT ANGLE BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FUSELAGE UPPER LOBE INTERIOR STRUCTURE, DITCHING PAN FWD SUPPORT ANGLE AT BS 1176 RBL 53-70 IS CRACKED. REMOVED DAMAGED ANGLE, FABRICATED HEAT TREATED NEW ANGLE. INSTALLED NEW ANGLE (CLASSIFIED AS A MINOR REPAIR) REF DWG 65-29548-11& 51- 30-02. 2 L 7 3 4F A3WE 20081024 NM 2008 10 24 SWAA085635 1 20081020 A 5311 6546595 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED BS 727A, STR 8. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085636 1 20081020 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085637 1 20081020 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED BS 727D, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085640 1 20081020 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED BS 747, STR 7R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085641 1 20081020 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED BS 740, STR 9R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085642 1 20081020 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED BS 787, STR 7R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085643 1 20081020 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED BS 827, STR 7R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085658 1 20081018 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 211WN 34163 FOUND FWD EMERGENCY EXIT LIGHT COVER BROKEN. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085659 1 20081017 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 211WN 34163 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW ONE. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085662 1 20081021 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085667 1 20081021 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085678 1 20081021 A 5312 6549892 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND BULKHEAD CRACKED AT BS 1016, STR 6R. REPAIRED BULKHEAD PER AAR EA. 2 L 7 2 4F RT A16WE 20081024 EA 2008 10 24 COMA0860416 1 20081011 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 933CA 7040 DURING 640 FRAME INSPECTION FOUND FRAME CRACKED AT STRINGER 9 LT CUTOUT. REPAIRED 640 FRAME PER REO 601R-53-61-557. 2 L 7 2 4F RT A21EA 20081024 EA 2008 10 24 ASOA200801337 1 20081014 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 750EV 10161 LBL 9 OF TRANSVERSE BEAM 280 CORRODED ON T/E. REMOVED CORROSION ON FS 280 AT TRANSVERSE BEAM LBL 9 PER CRJ 700 SRM 51-2 1-06 SUBMIT TO BOMBARDIER FOR DISPOSITION OF REPAIR. 2 L 7 2 4F RT A21EA 20081024 NM 2008 10 24 DL764081341 1 20081010 A 5330 SKIN BOEING 767 767432ER 1385134 NM BS 610-654 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830MH 29701 FUSELAGE SKIN DAMAGE, STA 610 TO 654A+22 BETWEEN S-20R AND S-25R, REPAIR. 2 L 7 2 4F RT A1NM 20081024 NM 2008 10 24 DL76G081342 1 20081010 A 8011 775550A3 STARTER BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 2 ENGINE FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 152DL 24984 695442 NR 2 ENGINE FAILED TO START ON TAXI OUT. MANUALLY OPENED START VALVE. ENGINE DIDN'T ROTATE. REMOVED DAMAGED STARTER. DUE TO STARTER VALVE MAY HAVE CLOSED DURING START AND REOPENED. REPLACED VALVE ALSO AS PRECAUTION. STARTER AND VALVE REPLACED PER AMM. 2 L 7 2 4F 4 F RT A1NM E13NE 20081024 EA 2008 10 24 ASOA200801351 1 20081015 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 934EV 8028 RT 621 OBLIQUE ANGLE CRACKED. REMOVED AND REPLACED RH 621 OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 20081024 EU 2008 10 24 08FDEA04428 1 20081018 A 3610 6272484 CONTROLLER AIRBUS 300 A300F4605R 3930327 EU PNEUMATIC SYSTEM FAILED A FDEA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 CE 21 658FE 18066 18066 752 PASSING FL 240, BOTH PACKS FAULTED, C/W ECAM PROCEDURE. PACK WOULD NOT RESET, DESCENDED TO 10,000 FOR REMAINDER OF FLIG HT. PASSING 14,000 ON WAY BACK DOWN PACK FAULTS MAGICALLY WENT AWAY AND CABIN BEGIN TO STABILIZE PERFORMED SUCCESSFUL BITE TEST OF NR 1 AND NR 2 CABIN PRESSURE CONTROLLERS, REF TSM 21-30-00. PERFORMED SUCCESSFUL BITE TEST OF NR 2 PNEU S YS CONT, REF TSM 36-00-00. NR 1 PNEU SYS CONT FAILED SEVERAL LEGS- "CONTROLLER". REMOVED AND REPLACED NR 1 SYS PNEU C ONT REF AMM 36-11-19-4. PERFORMED SUCCESSFUL CABIN PRESSURE CONTROL AND MONITORING ADJ/TEST, REF AMM 21-31-00-5. 2 L 7 2 4F RT A35EU 20081031 NM 2008 10 31 08FDEA04432 1 20081020 A 5340 65453132 STRINGER CLIP BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 CABIN BS 950B S6L STRINGER CLIP CRACKED. REMOVED STRINGER CLIP AND INSTALLED NEW CLIP REF SRM 51-30-2. THIS IS CLASSIFI ED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081024 NM 2008 10 24 08FDEA04433 1 20081020 A 5340 65453135 STRINGER CLIP BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 CABIN BS 950B S7L STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2 & 51-30-5. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081024 NM 2008 10 24 08FDEA04434 1 20081020 A 5340 6072324 STRINGER CLIP BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 INTERIOR UPPER FUSELAGE BS 680 STR 10R STRINGER CLIP CRACKED. REMOVED STRINGER CLIP REF SRM51-30-2, DRILLED NEW CLIP R EF SRM 51-30-5. INSTALLED NEW CLIP REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR 2 L 7 3 4F A3WE 20081024 NM 2008 10 24 08FDEA04435 1 20081020 A 5340 6072324 STRINGER CLIP BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 INTERIOR UPPER FUSELAGE BS 480 STR 10R STRINGER CLIP OB RADIUS CRACKED. REMOVED STRINGER CLIP, TRANSFERED HOLES AND INS TALLED STRINGER CLIP REF SRM 51-30-2 PG 1-10. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081024 NM 2008 10 24 UPS08M53712 1 20081022 A 2611 SMOKE DETECTOR DOUG MD11 MD11F 3023600 NM CABIN INTERMITTENT A IPXA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 285UP 48457 INSPECTION TYPE:N/A ATB - CABIN SMOKE DETECTOR WARNING WAS INTERMITTENT AFTER LEVEL OFF. NO SMOKE INDICATION VISUALLY N OTED. INDICATION DID NOT OCCUR DURING LAST HALF HOUR OF FLIGHT. BRIEF WITH FLT CREW - NR 1 SMOKE DETECTOR MAIN DECK WA RNING INTERMITTENT. NR 1 SMOKE DETECTOR REPLACED PER MM 26-15-01, TEST OK. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04412 1 20081017 A 5753 ARC25685 ATTACH ANGLE DOUG MD10 MD1010F 3022112 WP LT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 LEFT WING INBD FLAP OTBD HINGE FAIRING STRUCTURE, FWD ATTACH ANGLE IS CRACKED FROM THE BOLT HOLES RUNNING TO THE OUTER E DGE. REMOVED ATTACH ANGLE REF SRM 51-33-01. FORMED, LOCATED & DRILLED NEW ATTACH ANGLE REF DWG ARC 2568. ALODINED & PRIMED ANGLE REF SRM 51-21-01. INSTALLED ANGLE REF SRM 51-33-01. REMOVED TO F.O.M. & INSTALLED ACCESS PANEL REF SRM 51-31-01. PART MARKED IAW GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20081024 EU 2008 10 24 08FDEA04404 1 20081017 A 5315 A5327541120300 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 AFT PIT AT FRAME C61; RBL 64 FLOOR ANGLE SUPPORT IS CRACKED. REMOVED & REPLACED FLOOR ANGLE IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20081024 2008 10 24 08FDEA04420 4 20081017 A 2230 2606270001 CABLE DOUG DC10 DC1010F 3022111 WP GE CF6 CF66D 30020 GL AUTOTHROTTLE INOPERATIVE A FDEA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 CE 21 68059 46201 46907 451460 NR 2 THROTTLE STUCK DURING CRUISE. ENGINE SHUTDOWN DURING DESCENT. NR 2 THROTTLE MOVED BACK ON SHORT FINAL AFTER LANDI NG NR 2 THROTTLE COULD BE MOVED TO IDLE. CABLE COMING FROM OAK. REPLACED #2 THROTTLE CABLE PER MM 76-11-01-2, OP'S CHE KS NORMAL. PERFORMED NR 2 FCC AUTOTHROTTLE RTS. 2 L 7 3 4F 4 F A22WE E23EA 20081024 WP 2008 10 24 AALA200802523 1 20080918 A 5311 9923407504 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70504 49798 CRACK IN THE UPPER RADIUS OF OVERWING FRAME TAB AT RT STATION 905. CRACK LENGTH IS .5 INCHES. INSTALLED NEW FRAME SECT ION PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081231 NE 2008 12 31 AALA200802522 2 20081113 A 7200 ENGINE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE NR 2 VIBRATION A AALA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 SW 21 666A 5611 25300 31332 DFW INFLIGHT - AT CRUISE NR 2 ENGINE VIBRATIONS WERE ABOVE 2.0. FLUX BETWEEN 3.0 AND 1.6. CREW SHUT DOWN ENGINE. LANDE D DFW WITHOUT INCIDENT. COMPRESSOR AND TURBINE BLADES CHECKED OKAY. REPLACED NR 2 ENGINE ON 14 NOV AT DFW DUE TO VIBRA TIONS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 20081024 NM 2008 10 24 AALA200802453 1 20080927 A 2916 7321124005 MODULE BOEING 737 737823 13844CB NM HYDRAULIC SYS FAILED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 925AN 29526 LAS INFLIGHT T1553/27SEP YYZ TO LAX. CREW REPORTED BOTH ENGINE DRIVEN PUMP LOW PRESSURE INDICATION. LANDED LAS WITHOUT INCIDENT. REPLACED HYDRAULIC RESERVOIR PRESSURE MODULE. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 AALA200802460 1 20080928 A 2560 BATTERY BOEING 767 767323 1385205 NM FLASHLIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 358AA 24039 SFO EMERGENCY FLASHLIGHT AT FIRST CLASS FLIGHT ATTENDANT JUMPSEAT WAS USED. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT A T FIRST CLASS FLIGHT ATTENDANT JUMPSEAT. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081024 WP 2008 10 24 AALA200802440 1 20080925 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 292AA 49304 EMERGENCY LIGHTS AT SEAT ROWS 1 TO 25 INOPERATIVE. REPLACED BATTERY PACK AT FORWARD DOOR FOR EMERGENCY LIGHTS AT SEAT R OWS 1 TO 25. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081024 WP 2008 10 24 AALA200802441 1 20080925 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 292AA 49304 EMERGENCY LIGHTS AT SEAT ROWS 25 TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD MID CABIN FOR EMERGENCY LI GHTS AT SEAT ROWS 25 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081024 WP 2008 10 24 AALA200802518 1 20080926 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 CORROSION ON LOWER SURFACE OF RT HAND CUSP AT AFT CABIN BETWEEN STATIONS 1287 AND 1309 IS BEYOND SRM LIMITS. INSTALLED NEW CUSP PER SRM 53-05-00. 2 L 7 2 4F A6WE 20081024 NM 2008 10 24 AALA200802465 1 20080929 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 EMERGENCY LIGHT AT SEAT 26G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED NORMAL O PS. 2 L 7 2 4F RT T00001SE 20081024 NM 2008 10 24 AALA200802439 1 20080924 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 762AN 31479 EMERGENCY LIGHT AT SEAT 44C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 44C. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081024 NM 2008 10 24 AALA200802463 1 20080929 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 EMERGENCY LIGHT AT EXTERIOR LT NR 1 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT EXTERIOR LT NR 1 DOO R. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081024 WP 2008 10 24 AALA200802450 1 20080926 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 588AA 53251 MIA EMERGENCY LIGHT AT SEAT 33D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 33D. SYSTEM GROUND CH ECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081024 NM 2008 10 24 AALA200802464 1 20080929 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NORMAL O PS. 2 L 7 2 4F RT T00001SE 20081024 NM 2008 10 24 AALA200802449 1 20080926 A 3350 LAMP BOEING 737 737823 13844CB NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 937AN 30082 EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL O PS. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 AALA200802451 1 20080926 A 2560 FLASHLIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 DFW EMERGENCY FLASHLIGHT AT RT MID CABIN INOPERATIVE. REPLACED FLASHLIGHT AT RT MID CABIN. SYSTEM GROUND CHECKED NORMA L OPS. 2 L 7 2 4F RT A1NM 20081024 SO 2008 10 24 SIMA200829605 1 20081020 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 651AE 145422 DURING MBV INSPECTION FOUND CENTER SERVICE DOOR SILL TO BE CORRODED. REPAIRED SILL BY REMOVING CORROSION AND INSTALLING A DOUBLER IAW EMB SRM 53-21-02 FIGURE 201. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081024 SO 2008 10 24 SIMA200829802 1 20081023 A 3350 74441 SIGN EMB 145 EMB145LR 3260212 SO COCKPIT INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 641AE 145191 ON FLIGHT 3574 - CREW REPORTED EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT JUMP SEAT WILL NOT ILLUMINATE. REMOVED AND RE PLACED EMERGENCY EXIT SIGN IAW EMB AMM 33-50-15 OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081024 SO 2008 10 24 SIMA200829803 1 20081022 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 639AE 145182 ON FLIGHT 4118 - CREW REPORTED EMERGENCY EXIT SIGN ON STEP UNDER COCKPIT WILL NOT ILLUMINATE. AIRCRAFT REMOVED FROM SER VICE. REMOVED AND REPLACED INVERTER NR 1 IAW EMB 145 AMM 33-50-11, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVIC E. 2 L 7 2 4T RT T00011AT 20081024 EA 2008 10 24 SIMA200829804 1 20081020 A 3320 WIRE CNDAIR CL600 CL6002C10 1390015 EA OXYGEN SYSTEM SHORTED A SIMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 21 512AE 10110 ON FLIGHT 3561 CREW REPORTED DURING TAXI "PASS O2" LIGHT ILLUMINATED FOLLOW BY "PASS OXY ON" EICAS MESSAGE. ALL O2 MASK S IN PASS CABIN DEPLOYED. AIRCRAFT REMOVED FROM SERVICE. INSTALLED NEW WIRE OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 20081027 NE 2008 10 27 M7KA0718084290 2 20080804 A 7532 9550164950 BLEED VALVE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE MALFUNCTIONED E M7KA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 19 848MH 4290 23460 DURING FLIGHT OPERATIONS BLEED VALVE WAS CLOSING LATE AND OPENING TOO EARLY. A SERVICEABLE BLEED VALVE WAS INSTALLED. NO FURTHER DEFECT NOTED. SUSPECT ANEROID BELLOWS LOST CALIBRATION. THIS IS A RARE FAILURE FOR THIS PART. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 EU 2008 10 27 M7KA0809084125 1 20080901 A 3340 704A46831015 LIGHT UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE NAV INOPERATIVE E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 817MH 1977 4125 23292 NAV LIGHT ASSY, FOUND INOPERATIVE DURING ROUTINE POST FLIGHT INSPECTION, INSTALLED NEW REPLACEMENT, OPERATIONAL CHECK WA S CORRECT. THIS PART HAS HAD VIBRATION RELATED FAILURES IN OUT FLEET ON SEVERAL OCCASIONS. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081024 WP 2008 10 24 08FDEA04459 1 20081021 A 5340 WSP0815515 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 MAIN CABIN RIGID BARRIER FITTING NR 7 IS WORN. REPLACED IAW EA 8-5340-123670. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 K11A2008102372207 1 20080919 A 5320 PANEL BOEING 727 7272H3 138368N NM NLG WW CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 NOSE WHEEL WELL PANEL 1104 HAS CORROSION ON ATTACH UNDER NUT PLATES. 2 L 7 3 4F RT A3WE 20081024 NM 2008 10 24 MASA2008102000741 1 20081020 A 3350 1317 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN BROKEN A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 989HA 427 ASH FLT 2805 PHX-HMO. ROW 4 LT SIDE EXIT LIGHT BROKEN. MX CHANGED LIGHT. 2 H 7 2 4T RT A13NM 20081024 NM 2008 10 24 SWAA085616 1 20081019 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 782SA 29808 DURING SCHEDULED 8Y CHECK, FOUND LT AFT EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY ASSY PER MM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085672 1 20081021 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, BETWEEN RBL 44 TO LBL 43, WL 208. REPAIRED BEAM PER PAE ER. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 08FDEA04376 1 20081016 A 5347 AEA7325513 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 MAIN DECK CARGO, CORROSION ON SEAT TRACK FLANGE AT STA 1481 TO STA 1531, X = -75. REPAIR CARRIED OUT AS PER SRM 53-70-0 0 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 08FDEA04378 1 20081016 A 5730 ARB74023 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 CHIPPED EDGE FOUND ON 1 FASTENER HOLE ON LEFT WING AT LOWER WING SKIN OUTER ACCESS DOOR CUTOUT AT PANEL NR 536AB. REPAI R CARRIED OUT AT LEFT HAND WING AT LOWER WING SKIN. 01 EACH HOLE AT OUTER ACCESS DOOR CUTOUT AT PANEL NR 536AB AS PER E.A. 1-5710-125559, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 08FDEA04379 1 20081016 A 5730 ARB74024 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 CRACK FOUND ON 7 EACH FASTENER HOLES ON RIGHT WING AT LOWER WING SKIN OUTER ACCESS DOOR CUTOUT AT PANEL NR 636AB. 7 C RACKED FASTENER HOLES ON RT WING LOWER WING SKIN REPAIRED AS PER E.A. 1-5710-125558, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 08FDEA04385 1 20081017 A 5415 AUB7525501 MOUNT DOUG MD11 MD11F 3023600 NM NR 1 PYLON WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 576FE 48501 WITH REFERENCE TO SNRM N01236, DURING BEARING REMOVAL AT NR 1 PYLON AFT MOUNT FITTING BORE FOUND WORN. REMOVED AND REP LACED AS PER SRM 51-31-01 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04387 1 20081017 A 5312 NCA624628 PRESSURE PANEL DOUG DC10 DC1030F 3023504 WP MLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 DURING INSPECTION NLG W/W FOUND CRACK ON VERTICAL WEB. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04392 1 20081017 A 5410 SR107800218 COWLING DOUG MD10 MD1010F 3022112 WP NR 1 NACELLE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 1 ENGINE INBD FAN COWL IS GOUGED ABOVE THE MID LATCH. CLEANED UP DAMAGE, CHECKED LIMITS, REQUIRES REPAIR. REMOVED SURF ACE FINISH, FABBED DOUBLER, ALODINED & PRIMED AREA IAW SRM 51-71-00. SEALED DOUBLER EDGES BOND LINE IAW SRM 51-71-00. 2 L 7 3 4F RT A22WE 20081024 EU 2008 10 24 08FDEA04449 1 20081020 A 5740 LUG AIRBUS 310 A310222 3930315 EU RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 418FE 343 WHILE COMPLYING WITH EO 6-5710-7-5010 CORROSION WAS FOUND ON BOTH LEFT AND RIGHT WING RIB 5 FORWARD LUG. COMPLIED WITH EA 6-5710-125482 IN THE REMOVAL OF CORROSION ON THE AFFECTED AREAS IN ACCORDANCE WITH EO 6-5710-7-5010. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 08FDEA04360 1 20081015 A 5320 A2577260600600 PAN AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 AFT LOWER CARGO COMPARTMENT HAS CORROSION ON THE POWER ROLLER PAN AND SUPPORT AT FRAME 54.2, LBL 3 INCH" (LOWER SURFACE ). REMOVED PAN AND FRAME IAW SRM 51-41-21. REMOVED CORROSION IAW SRM 51-71-10. BOTH FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. MACHINED NEW FRAME IAW DWG 310A25771822. ALODINED IAW SRM 51-21-10. PRIMED IAW SRM 51-75-10. PAINTED IA W SRM 51-75-10. LOCATED AND DRILLED HOLES IN NEW PAN AND FRAME IAW SRM 51-40-44 AND SRM 51-72-10. PART MARKED IAW GMM 7-0-1000. INSTALLED PAN AND FRAME IAW SRM 51-40-21. INSTALLED PDU IAW AMM 25-54-26-04. OPS CHECKED IAW AMM 25-52-26-0 4. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 08FDEA04361 1 20081015 A 5320 A2577260600600 PAN AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 AFT LOWER CARGO COMPARTMENT HAS CORROSION ON THE POWER ROLLER PAN & SUPPORT AT FRAME 54.2; LBL 41" (LOWER SURFACE). REMOVED PAN AND FRAME IAW SRM 51-40-21. REMOVED CORROSION IAW SRM 51-74-10. BOTH FOUND TO BE OUT OF LIMITS IAW SRM 53- 10-00. MACHINED NEW FRAME IAW DWG NR 10A25771745; REV E AND 10A25771823; REV G. ALODINED IAW SRM 51-21-10. PRIMED IAW SRM 51-75-10. PAINTED IAW SRM 51-75-10. LOCATED AND DRILLED HOLES IN NEW PAN AND FRAME IAW SRM 51-40-44 AND SRM 51-72 -10. PART MARKED IAW GMM 7-0-1000. INSTALLED PAN AND FRAME IAW SRM 51-40-21. INSTALLED PDU IAW AMM 25-54-26-04. 2 L 7 2 4F RT A35EU 20081024 NM 2008 10 24 SWAA085651 1 20081016 A 3350 417A56014 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 490WN 32476 FOUND R1 DOOR EMERGENCY EXIT SIGN DETACHED. ATTACHED LENS PER MM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085653 1 20081020 A 5315 6546804 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CRACKED AT BS 312, LBL 54. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085654 1 20081020 A 5754 65C26686 WEDGE BOEING 737 7373H4 1384600 NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 DURING SCHEDULED 12Y CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE O/B END DELAMINATED. REPAIRED WEDGE PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 UPS08653685 1 20081012 A 5720 113T163925 CHANNEL BOEING 767 76734AF 1385212 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 331UP 27757 INSPECTION TYPE:N/A LT WING LANDING GEAR W/W 551CB PANEL ATTACHMENT CHANNEL FOUND CRACK AS MARKED, CRACK LENGTH .75 INCH . LT WING LANDING GEAR W/W 551CB PANEL ATTACHMENT CHANNEL REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20081024 NM 2008 10 24 SWAA085660 1 20081017 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 257WN 32515 FOUND R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085661 1 20081021 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BETWEEN BS 415 TO BS 417, STR 1. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081024 EU 2008 10 24 UPS08153704 1 20081014 A 5321 B5327079900000 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 140UP 0823 INSPECTION TYPE:1C3C MAIN CARGO DECK FLOORBOARD 241DQ HAS FIELD REPAIR. REPAIRED MAIN CARGO DECK FLOORBOARD 241DQ REF A 300-600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 UPS08153706 1 20081014 A 5321 B5327075300100 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 140UP 0823 INSPECTION TYPE:1C3C MAIN CARGO DECK FLOORBOARD 242LJ HAS A FIELD REPAIR. REPAIRED MAIN CARGO FLOORBOARD 242LJ REF A300 -600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081029 NM 2008 10 29 08FDEA04552 1 20081026 A 5340 66124343 STRINGER CLIP BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 AFT PIT BILGE BODY FRAME STR CLIP IS CORRODED BS 950F, STR 27L WL 141. INSTALLED NEW STRINGER CLIP 65-12434-3 REF SRM 5 1-10-1 AND ARM 53-10-1. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081024 2008 10 24 UPS08853699 4 20081019 A 2565 SLIDE DOUG DC8 DC873F 302199F WP EVAC SLIDE OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:N/A THE SIGHT GAUGE FOR THE EMERGENCY SLIDE IS NOT IN VIEW TO READ PRESS AND EQUIPMENT DUE DATE. REPOSI TIONED THE EMERGENCY SLIDE PACK AS NEEDED. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 20081024 NM 2008 10 24 08FDEA04384 1 20081016 A 5310 CREASE BEAM BOEING 757 75723A 1384967 NM BS 450-660 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 CREASE BEAM INBOARD CHORD RT SIDE CORRODED FROM FR 450-660, RBL 58. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-3 0-13. REMOVED CREASE BEAM. FABRICATED NEW CREASE BEAM IAW DRAWING NR 143N5520 IAW SRM 51-40-05. LOCATED AND DRILLED I AW SRM 51-40-05. TREATED AND PRIMED IAW SRM 51-20-01. INSTALLED CREASE BEAM STA 450 TO 660 RBL 58 IAW SRM 51-40-02 AND DRAWING 143N5520. 2 L 7 2 4F RT A2NM 20081024 EU 2008 10 24 08FDEA04358 1 20081015 A 5320 A9242053522201 CHANNEL AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 MAIN BATTERY OTBD SUPPORT CHANNEL IS CRACKED AT THE CENTER ATTACH POINT. REMOVED BATTERY TRAY CANOPY; CRACKED SUPPORT C HANNEL & 4 EA CLIPS IAW SRM 51-40-21. LOCATED & DRILLED NEW CHANNEL IAW SRM 51-40-44. INSTALLED NEW CHANNEL 4 CLIPS & BATTERY TRAY CANOPY IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 08FDEA04359 1 20081015 A 5320 A9242053522201 CHANNEL AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA J DUMP FUEL O OTHER IN INSP/MAINT 1 CE 21 667FE 771 MAIN BATTERY INBD SUPPORT CHANNEL IS CRACKED AT THE CENTER ATTACH POINT. REMOVED CRACKED SUPPORT CHANNEL IAW SRM 51-40- 21. LOCATED & DRILLED NEW SUPPORT CHANNEL IAW SRM 51-40-11. INSTALLED NEW SUPPORT CHANNEL IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20081024 2008 10 24 UPS08M53713 4 20081021 A 2565 INDICATOR DOUG MD11 MD11F 3023600 NM LT DOOR SLIDE NO TEST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 LEFT ENTRY DOOR SLIDE PUSH TO TEST LIGHT WILL NOT ILLUMINATE. R&R L1 SLIDE PRESSURE INDICATOR ASSY IAW AMM 25-61-15-4. OPS CHECK SATISFACTORY. 2 L 7 3 4F RT A22WE 20081024 SO 2008 10 24 RAIA2008102300001 1 20081017 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN MALFUNCTIONED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 801HK 145053 DURING PREFLIGHT INSPECTION, ONE OF THE EMERGENCY LIGHT AT THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE IN SPECTED THE CONNECTOR AT THE LIGHT ASSEMBLY AND FOUND NO DEFECTS. OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WA S GOOD. 2 L 7 2 4F RT T00011AT 20081024 SO 2008 10 24 RAIA2008102300003 1 20081020 A 5540 FITTING EMB 145 EMB145LR 3260212 SO RUDDER WORN A RAIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 03 814HK 145046 DURING CLIMB OUT OF STL, CREW REPORT EXCESSIVE VIBRATION COMING FROM THE AFT END OF THE AIRCRAFT. MAINTENANCE INSPECTED THE RUDDER I AND RUDDER II SYSTEMS PER AD 2008-05-02 (H) AND FOUND SEVERAL ATTACHMENT POINTS WORN. WORN HARDWARE WAS R EMOVED AND REPLACED AS PER AD, APPLICABLE SERVICE BULLETIN, AND AMM PROCEDURES. SUCCESSFUL MAINTENANCE CHECK FLIGHT WAS PERFORM WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 20081024 2008 10 24 AALA200802462 4 20080929 A 2565 5A33075 SLIDE BOEING 737 737823 13844CB NM PAX DOOR OUT OF POSITION A AALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 948AN 30086 FLIGHT ATTENDANT REPORTED SLIDE AT FORWARD ENTRY DOOR WAS DISARMED BUT SLIDE HARDPACK CAME OPEN ENOUGH FOR SLIDE TO STAR T TO COME OUT WHEN DOOR OPENED. SLIDE DID NOT COME OUT ENOUGH TO DEPLOY. UNSURE IF LANYARDS WERE UNDER TENSION. REPLA CED SLIDE AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081024 WP 2008 10 24 AALA200802470 1 20080930 A 3350 SIGN DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 214AA 49162 EMERGENCY LIGHT DOUBLE ARROW EXIT SIGN AT FORWARD ENTRY DAMAGED. REPLACED DOUBLE ARROW EXIT SIGN AT FORWARD ENTRY. SYS TEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081027 NM 2008 10 27 DHLA2008745539 1 20080907 A 5310 BEAM BOEING 727 727224 1384076 NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE AFT CARGO COMPARTMENT 1183 BULKHEAD WL 190 BETWEEN RBL19 AND RBL47 HORIZONTAL BEAM CRACKED. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DHLA2008745540 1 20080904 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 928 S17L CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN STA 928 STRINGER 17L CRACKED. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DL76L081376 1 20081019 A 3320 LIGHT BOEING 767 767332 1382001 NM CABIN INTERMITTENT A DALA F ACTIVATE FIRE EXT. O OTHER CR CRUISE 1 SO 27 177DN 25122 FLICKERING LIGHT IN OVERHEAD NEAR MID GALLEY MISTAKEN FOR FIRE BY FA SHE GAVE HALON FE TO PAX WHO DISCHARGED SOME ON LIG HT. 2 L 7 2 4F RT A1NM 20081027 NM 2008 10 27 DL757081378 1 20081020 A 5330 SKIN BOEING 757 757232 1384965 NM BS 570-620 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 CORROSION FOUND AT STA 570 TO 620 AT RBL 21.5 IN FWD CARGO BAY. REPAIRED ON NR CARD 00062 PER 51-40-05. 2 L 7 2 4F RT A2NM 20081027 NM 2008 10 27 DL757081379 1 20081020 A 5320 HRAB53AN011 ANGLE BOEING 757 757232 1384965 NM BS 660 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 ANGLE AT BS 660 RBL 45 CRACK. REPLACED ON NR CARD 00078 PER 51-40-05. 2 L 7 2 4F RT A2NM 20081027 NM 2008 10 27 DHLA2008745543 1 20080905 A 5542 SKIN BOEING 727 727224 1384076 NM RUDDER CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 EMPENNAGE VERTICAL STABILIZER LOWER RUDDER L/E SURFACE WITH WEAR AND CORROSION FROM STA 127.5 TO 150.625 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DHLA20087521022B 1 20081022 A 5753 WEDGE BOEING 727 727223 1384074 NM RT WING TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 752DH 22466 RIGHT WING INBD T/E FLAP ASSY MID FLAP T/E HAS AREA OF DELAMINATION AT OUTER T/E. 337 FILED AND MP9 FILED NR 26945. AL L REPAIR WORK COMPLIED WITH IAW BOEING SRM 51-40-20 PARA 7, 8, 10, 14, 20, 22. REMOVED DAMAGED AREA APPROX 4 INCH BY 4 INCH AND FABRICATED FILLER AND DOUBLER 4 1/4 INCH BY 6 1/4 INCH. PO NR 9007617 MATERIAL 2024 T3 .016". FILLER AND DOUB LER HOT BONDED TO T/E. AREA PRIMED, PAINTED AND SEALED. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DL75E081347 1 20081011 A 2121 6457053 FAN BOEING 757 757231 1384950 NM RECIRC SMOKE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 705TW 126351 28479 LEFT RECIRC FAN CAUSING SMOKE IN THE CABIN. REMOVED AND REPLACED LEFT RECIRC FAN PER AMM. RESET UTILITY BUSSES. OPS C HK NML. NO SMELL OR VIBRATION, NO RAN FOR 3 HRS. 2 L 7 2 4F RT A2NM 20081027 NM 2008 10 27 08FDEA04444 1 20081020 A 5340 6072324 STRINGER CLIP BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 INTERIOR UPPER FUSELAGE BS 680 STR 10R CRACKED LOWER FLANGE RADIUS, OB OF CLIP. NDT VERIFIED CRACK, SPLICE ANGLES REMOV ED REF SRM 51-30-2, DRILLED NEW STRINGER CLIP REF SRM 51-30-5. INSTALLED NEW STRINGER CLIP REF SRM 51-30-2. APPLIED CI C TO INTERIOR AND RECONDITIONED EXTERIOR SURFACE OF REPAIR. THIS IS CLASSIFIED AS A MAJOR REPAIR 2 L 7 3 4F A3WE 20081027 WP 2008 10 27 08FDEA04445 1 20081020 A 2913 1489951 PUMP DOUG DC10 DC1030F 3023504 WP HYD SYSTEM FAILED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 21 317FE 25352 21046 46835 AT CRUISE FLT, NR 2 HYDRAULIC QTY AND PRESSURE WENT TO ZER0. NO HIGH TEMP INDICATED. COMPLIED WITH QRH AND RETURNED TO MEMPHIS. REMOVED AND REPLACED 2/1 NON-REV MOTOR PUMP SHUTOFF VALVE 2 L 7 3 4F RT A22WE 20081027 EU 2008 10 27 08FDEA04448 1 20081020 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU RT WING TE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 RIGHT OUTBD FLAP L/E INBD END IS GOUGED IN THE EXTERNAL SKIN. 2 L 7 2 4F RT A35EU 20081024 NM 2008 10 24 SWAA085628 1 20081019 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 23L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085629 1 20081019 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085622 1 20081016 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND RT WING O/B FLAP, AFT FLAP DELAMINATED AT INBOARD END ALONG T/E. REPAIRED FLAP PER SR M. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 08FDEA04452 1 20081021 A 5320 656720510 STRAP BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 PNL RACK, FWD PIT SIDEWALL TO FLOOR RT NR 2 STRAP IS CORRODED, STRAP IS CRACKED, CORROSION FOUND TO BE OUT OF LIMITS REF 53-10-1 PG 30 NOTE A. FABRICATED, TREATED, PRIMED, AND IDENTIFIED NEW STRAP REF DWG 65-67205, SRM 51-10-2, AND FED EX MM1805 SEC 11-0-2700. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081024 NM 2008 10 24 08FDEA04453 1 20081021 A 5320 65672057 STRAP BOEING 727 7272D4 138407U NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 PNL RACK, FWD PIT SIDEWALL TO FLOOR STRAP NR 5 IS CRACKED REPLACED STRAP ORIGINAL THICKNESS .063 2024 T3 A24170 PO NR 10 39696, TREATED AND PRIMED NEW STRAP REF DWG 65-67205 AND MM 51-20-151-7 PG 1-6. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081024 WP 2008 10 24 AALA200802399 1 20080921 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 554AA 53084 DFW EMERGENCY LIGHT EXIT SIGNS AT AFT LT AND RT OVERWING DOORS INOPERATIVE. REPLACED BATTERY PACK AT STATION 1100 FOR E MERGENCY LIGHT EXIT SIGNS AT AFT LT AND RT OVERWING DOORS. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081024 NM 2008 10 24 AALA200802458 1 20080928 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 383AN 26995 DFW EMERGENCY LIGHT AT SEAT 24B INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 24B. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A1NM 20081024 NM 2008 10 24 AALA200802438 1 20080924 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 762AN 31479 EMERGENCY LIGHT AT SEAT 20C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081024 WP 2008 10 24 AALA200802437 1 20080924 A 2421 GENERATOR DOUG DC9 DC983 3022083 WP HNYWL T53 T5313BHNYWL 33857 NE NR 1 ENGINE FAILED A AALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SW 21 9402W 53138 P180 INFLIGHT T1363/24SEP. LT ENGINE GENERATOR OFF LINE. AUXILIARY POWER UNIT (APU) WOULD NOT COME ON LINE. RETURNED TO DF W AND LANDED WITHOUT INCIDENT. REPLACED LT CONSTANT SPEED DRIVE AND GENERATOR. APU REPLACED ON 24 SEP AT DFW. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F 4 U RT A6WE E17EA 20081024 NM 2008 10 24 AALA200802443 1 20080925 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 347AN 33086 EMERGENCY LIGHT AT OVERHEAD SEAT ROW 11 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL O PS. 2 L 7 2 4F RT A1NM 20081024 NM 2008 10 24 USA2008F00038 1 20080927 A 3397 WIRE BOEING 757 757222 1384956 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 504UA 24625 CLT - MX REPORTED THE SEAT EMERGENCY LIGHT AT ROW 4, LT SIDE, INOPERATIVE. MX REPAIRED WIRING BENEATH ROW4, LT SIDE. O PS CHECK GOOD. 2 L 7 2 4F RT A2NM 20081027 WP 2008 10 27 U2R2008F00011 1 20081013 A 5720 STRAP DOUG DC8 DC871F 302199D WP RWS 430 CRACKED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 872SJ 83402 46040 DURING C-CHECK, FOUND RT WING XFS 430.000 CTR LEADING EDGE INTERIOR LOWER SURFACE STRAP HAS 18 INCH CRACK. (K) 2 L 7 4 4F RT 4A25 20081027 EU 2008 10 27 M7KA804084327 1 20080901 A 2913 S40 COUPLING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE HYD PUMP DAMAGED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 850MH 4327 23472 DURING ROUTINE 500 HOUR INSPECTION THE PULLEY SPINDLE ON WHICH THE INNER RACE OF THE BEARING IS PRESS FIT WAS FOUND VERY WORN WITH MORE THAN 10" OF THE PROPER SPINDLE DIAMETER WORN AWAY AND SOME CORRESPONDING WEAR ON THE BEARING INNER RACE AND WEAR ON THE HYDRAULIC PUMP DRIVE PULLEYS SPLINED COUPLING SLEEVE. THIS IS THE THIRD INSTANCE OF WHICH WE ARE AWARE O F THIS DEFECT OCCURRING. THE BEARING ITSELF HAD NO APPARENT ROUGHNESS WHEN TURNED BY HAND. SUSPECT SOME PULLEYS OR PERHA PS BEARINGS HAVE BEEN IMPROPERLY MACHINED, DIAMETERS WHICH ALLOW THE INITIAL SLIPPAGE AND SUBSEQUENT CHATTERING DEVELOP S WHICH REMOVES MATERIAL OVER TIME. THIS HAPPENED BETWEEN INSPECTIONS. BELT TENSION MUST BE RELEASED TO DETECT THIS DEFE 1 G 7 2 3U 3 U H9EU E00054EN 20081027 EU 2008 10 27 M7KA0811084266 1 20080901 A 5340 350A54112420 BRACKET UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE STARTER CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 847MH 4266 23416 FOUND CRACKED DURING ROUTINE INSPECTION. RECOMMEND THIS PART BE MFG OF A MORE DURABLE MATERIAL SUCH AS STAINLESS STEEL. THIS IS A FAIRLY COMMON DEFECT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 EU 2008 10 27 M7KA0625084142 1 20080804 A 6320 S1130021089 PRESSURE SENSOR UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE M/R GEARBOX INTERMITTENT E M7KA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 822MH 975 4142 23069 OIL PRESSURE LIGHT ILLUMINATES AT GROUND IDLE. NEW SWITCH INSTALLED. NO FURTHER DEFECT NOTED. THIS SWITCH NORMALLY WORKS WELL BUT ON OCCASION LOSES INTERNAL CALIBRATION OR IS MISCALIBRATED AS NEW SWITCHES SOMETIMES EXHIBIT THE SAME PROBLEM. SUGGEST A MORE MODERN DESIGN BE CONSIDERED FOR THIS PART. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 NE 2008 10 27 M7KA0729084290 2 20080901 A 7310 9550172000 PRESSURE SWITCH UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE FUEL FILTER OUT OF TOLERANCE E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 848MH 609 4290 23460 DURING ROUTINE 600 HOUR INSPECTION THE FUEL FILTER PREBLOCKAGE PRESSURE SENSOR WAS FOUND OUT OF TOLERANCE IAW MM DATA. A NEW SWITCH WAS INSTALLED. THIS IS A RARE FAILURE FOR THIS PART. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 EU 2008 10 27 M7KA0501083833 1 20080804 A 6230 ARM UROCOP EC130 EC130B4 8680989 EU STARFLEX LOOSE E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 806MH M2746 3833 DURING ROUTINE INSPECTION A STAR ARM END BUSHING WAS FOUND LOOSE. STARFLEX REMOVED FOR REPAIR AND SERVICEABLE STARFLEX I NSTALLED. THIS IS A VERY COMMON FAILURE RECENTLY FOR THIS PART. SUSPECT THAT AN ADHESIVE FAILURE IS THE PROBLEM THAT MAY BE HEAT RELATED. (K) 1 G 7 2 3U H9EU 20081027 NE 2008 10 27 M7KA0815083967 2 20080901 A 7261 790081 MAGNETIC SEAL UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE LEAKING E M7KA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 813MH 3000 3967 23183 ENGINE FOUND LEAKING FROM POWER SHAFT HOUSING SEAL VICINITY DURING OPERATION. A NEWLY REPAIRED, SERVICEABLE HOUSING WIT H A NEW MAGNETIC SEAL EMBODIED WAS INSTALLED WITH NO FURTHER LEAKAGE NOTED. THIS SEAL HAS LEAKAGE ISSUES FROM TIME TO TI ME BUT WILL MAKE IT TILL OVERHAUL ALMOST HALF THE TIME. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 NM 2008 10 27 DHLA2008745545 1 20081017 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 1148 BL-0 FLOORBEAM LOWER CHORD AFT FLANGE WITH CORROSION. REPAIRED FUSELAGE FLOORBEAM LOWER CHORD AFT FLANGE SECTION AT BS 1148 BETWEEN LBL10 AND RBL10 IAW B727SRM 53-10-8 FIG 8. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DHLA2008745546 1 20080901 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE CARGO CABIN FRAME SHEAR TIE WITH CORROSION AT BS 950E BETWEEN S-13R AND S-14R. REPLACED FUSELAGE FRAME S ECTION AT BS 950E BETWEEN S-13R AND S-15R AND SHEAR TIE SECTION BETWEEN 13R AND 14R IAW B727 SRM 51-10-1 PARA 7A AND 51- 30-1 PARA 4B. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DHLA2008745547 1 20080902 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN AT BS 400 BETWEEN S-5R AND S-6R FRAME WITH DOUBLE HOLE. REPAIRED FUSELAGE FRAME SECTION AT BS 400 BETWEEN S-5R AND S-8R IAW B727 SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DL76L081372 1 20081017 A 4920 APU BOEING 767 767332 1382001 NM APU BAY FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 187DN 27582 APU FAILED AFTER PUSHBACK. RESTARTED APU. LOAD CKS GOOD PWR AND PNEUMATICS. 2 L 7 2 4F RT A1NM 20081027 NM 2008 10 27 DL76L081373 1 20081018 A 8012 7755386 START VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 188DN 27583 727725 LEFT ENGINE START VALVE FAILED TO OPEN. CONFIRMED START VLV INOP. PERF MANUAL START FWD TO MCO AND PLC PER MEL 80-00-0 2. 2 L 7 2 4F 4 F RT A1NM E24NE 20081027 NM 2008 10 27 DHLA2008745550 1 20080902 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN AT BS 720D BETWEEN S-13L AND S-14L FRAME WITH HOLE. REPAIRED FRAME SECTION AT BS 720D BETWEEN S-11L AND S-14L IAW B727 SRM 53-10-4 FIG 1 DETAIL 1. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DHLA2008745555 1 20080907 A 5320 FLOOR SUPPORT BOEING 727 727224 1384076 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20065 UPPER FUSELAGE CARGO CABIN AT BS 865 RBL45 WL 190 LONGITUDINAL FLOORBEAM LOWER CHORD HAS CORROSION. REPAIRED FLOORBEAM LOWER CHORD SECTION FROM BS 848 TO BS 867 AT RBL 45 WL 190 IAW B727 RM 51-40-4 FIG 2. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DHLA2008745556 1 20081012 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE CARGO CABIN TRACK WITH CORROSION AT BS 1130 LBL45. REPAIRED CARGO TRACK FROM BS 1073 TO BS 1137 LBL45 IA W 727 SRM 53-10-5 FIG 1 PREFERRED REPAIR. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DLM88081392 1 20081021 A 5320 5914494501 PAN DOUG MD88 MD88 3023688 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 979DL 53266 C1 DOOR JAMB PAN WAS FOUND CORRODED BEYOND ALLOWABLE LIMITS AND WAS REPAIRED PER SRM 53-05D FIG 804D. 2 L 7 2 4F RT A6WE 20081027 NM 2008 10 27 DHLA2008745535 1 20081002 A 5754 RIB BOEING 727 727224 1384076 NM NR 6 SLAT OUT OF LIMITS A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 RT WING NR 6 SLAT STA 128, 161, 181, 208, 224.5 AND 232.5 INTERNAL RIBS WITH MISSING MATERIAL. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DHLA2008745534 1 20080923 A 5330 SKIN BOEING 727 727224 1384076 NM ZONE 200 DEFORMED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE FROM BS 314.5 TO BS 326 BETWEEN STRINGER 11 AND STRINGER 13 RIGHT SIDE PREVIOUS DOUBLER REPAIR HAS WRINKL ING AND DEFORMED. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DHLA2008745536 1 20080904 A 5340 6917929 SUPPORT BRACKET BOEING 727 727224 1384076 NM BS 869 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN STA 869 AT RBL 25 AND 45 BL0 LBL 25 AND LBL 45 FALSE CARGO TRACK SUPPORT BRACKETS WITH CORROSIO N. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DL757081374 1 20081018 A 5311 FAILSAFE BOEING 757 757232 1384965 NM BS 900 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 670DN 25331 CORROSION FAILSAFE STRAP AT FS 900 RT LOWER SIDE FITTING. REPLACED STRAP WITH NEW OR SERVICEABLE STRAP. 2 L 7 2 4F RT A2NM 20081027 NM 2008 10 27 DLM88081375 1 20081018 A 2450 RELAY DOUG MD88 MD88 3023688 NM ELECTRICAL FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 949DL 49880 DUE TO LONG HISTORY OF BREAKERS POPPING AND SOME ELECTRICAL ODOR IN CABIN, WE LOOKED FOR AND FOUND CONNECTORS AND CURREN T LIMITERS ON THE T1,T2,AND T3 SIDE OF THE AC BUSS TIE RELAY WITH SEVERE HEAT DAMAGE. REPLACED AC BUSS TIE RELAY TWO FE EDER WIRES AND CURRENT LIMITERS ON THE T1,T2 AND T3 SIDE. POWER CHECKS GOOD IN ALL MODES. 2 L 7 2 4F RT A6WE 20081027 NE 2008 10 27 DL777081377 2 20081020 A 7200 ENGINE BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 1 INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 862DA 37396 29734 051193 LEFT ENGINE START VALVE FAILED TO OPEN AFTER PUSHBACK. RTB AND APPLIED MEL AND PERFORMED A MANUAL START. 2 L 7 2 4F 4 F RT T00001SE E00050EN 20081027 NM 2008 10 27 DL757081380 1 20081020 A 5320 140N250615 ANGLE BOEING 757 757232 1384965 NM BS 660 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 VERTICAL ATTACH ANGLE BS 660 CRACKED. REPAIRED ON NR 00083 PER 51-40-05. 2 L 7 2 4F RT A2NM 20081027 NM 2008 10 27 DHLA2008745544 1 20080901 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE CARGO CABIN AT STA 360 BETWEEN STR 13L AND 14L FRAME WITH HOLE. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DL757081381 1 20081020 A 5320 146N543211 WEB BOEING 757 757232 1384965 NM BS 1500-1520 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 VERTICAL WEB AT 1520 TO 1500 IS CORRODED ON TOP OF WEB. REPAIRED PER 51-70-13 ON NR 00100. 2 L 7 2 4F RT A2NM 20081027 NM 2008 10 27 DL757081383 1 20081020 A 5320 146N543111 FLOOR SUPPORT BOEING 757 757232 1384965 NM BS 1530-1560 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 CORROSION ON FLOOR SUPPORT AT BS 1530 TO 1560 LT. REPAIRED ON ATS 00041 PER 51-40-02. 2 L 7 2 4F RT A2NM 20081027 WP 2008 10 27 08FDEA04446 1 20081020 A 5730 ARC110937 SKIN DOUG MD10 MD1010F 3022112 WP LT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 LEFT WING, OUTBD LOWER L/E NOSE PANELS ARE CHAFED ON THE INBD EDGE FROM 34 INCHES OUTBD. FOUND OUT OF LIMITS. REMOVED PANEL IAW SRM 51-35-01 & SRM 51-33-01. FABRICATED A NEW PANEL IAW TPS 1003. LOCATED & DRILLED HOLES IAW DWG ARC 1109- 37. ALODINED & PRIMED IAW SRM 51-21-01. PART MARKED IAW GMM 7-0-1000. INSTALLED IAW DWG ARC 1109 & SRM 51-35-01 & SRM 51-33-01. PAINTED IAW SRM 51-21-02. 2 L 7 3 4F RT A22WE 20081027 WP 2008 10 27 08FDEA04447 1 20081020 A 5347 NEA602213 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 1239 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 MAIN CABIN SEAT TRACK, STA 1239; BUTT LINE, 48R "2" GOUGES. DAMAGE OUT OF LIMITS. REMOVED DAMAGED SECTION IAW SRM 53-7 0-00. FABRICATED REPAIR PARTS IAW SRM 53-70-00. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED REPAIR PART IAW SRM 53- 70-00. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 SWAA085618 1 20081019 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM CORRODED AT BS 733. REMOVED AND REPLACED BEAM PER PAE ER. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085626 1 20081019 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM CORRODED BETWEEN RT BS 493 TO BS 500. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081024 EU 2008 10 24 08FDEA04383 1 20081016 A 5315 A53275349200 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 668FE 772 MAIN DECK CARGO COMPT FLOORBEAM CRACKED AT FR 64, BETWEEN SEAT TRACK NR 3 RT AND NR 4 RT, .25 INCH LONG. CUT OUT DAMAGE D AREA AND INSTALLED CROSSBEAM REPAIR AT FR 64, BETWEEN SEAT TRACKS NR 3 RT AND NR 4 RT IAW SRM 53-10-15, FIG 211, PAGE 389/390. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 08FDEA04465 1 20081021 A 5520 ARM AIRBUS 310 A310222 3930315 EU ELEVATOR HINGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 418FE 343 EMPENNAGE, RT ELEV NR 5 HINGE ARM FOUND CRACKED/CORROSION AT UPPER END REPLACED RT ELEV NR 5 HINGE ARM AS PER AMM 55-16- 45-4. 2 L 7 2 4F RT A35EU 20081024 WP 2008 10 24 08FDEA04450 1 20081021 A 5713 STRINGER DOUG MD10 MD1010F 3022112 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 RIGHT WING UPPER STRINGER 8 AT COMP PROBE LAND IS CRACKED. REPLACED COMP. PROBE DOUBLER IAW EA 8-5720-123508. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 08FDEA04451 1 20081021 A 5311 651634112 FRAME BOEING 727 7272D4 138407U NM BS 1010 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 AFT LOWER CARGO PIT STA 1010 BETWEEN STR 28R AND 27R FRAME CORRODED. REPAIRED FRAME BY INSTALLING REPAIR ANGLE REF SRM 51-40-03. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081024 WP 2008 10 24 08FDEA04415 1 20081017 A 5754 SLAT TRACK DOUG MD10 MD1010F 3022112 WP LT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 LEFT WING NR 18 SLAT TRACK UPPER CLOSE OUT PANEL IS GOUGED. REMOVED AND INSTALLED DOOR ASSY IAW SRM 51-31-01. CLEANED, WELDED & INSPECTED REF. DPS 10.225. ALODINED & PRIMED IAW SRM 51-21-01. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04416 1 20081017 A 5415 AUB708313 ATTACH ANGLE DOUG MD10 MD1010F 3022112 WP NR 3 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 NR 3 PYLON L/E HEAT EXCHANGER ACCESS AREA FWD ATTACH ANGLE IS CRACKED. REMOVED & INSTALLED PANEL IN REF TO SRM 51-31-01 . REMOVED & INSTALLED ANGLE IN REF TO SRM 51-35-01. FABRICATED ANGLE IN REF SRM 51-21-01. PART MARKED FX AUB 7083- 13 IN REF TO GMM 7-01000. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04417 1 20081017 A 5420 AUB70837 WEB DOUG MD10 MD1010F 3022112 WP NR 3 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 NR 3 PYLON L/E WEB BETWEEN PANELS 487 DL AND 487 DR IS CRACKED. REMOVED & INSTALLED WEB IAW SRM 51-31-01, 51-33-01 & 51 -35-01. CUT OUT DAMAGE, FABRICATED DOUBLER & INSTALLED DOUBLER IAW SRM 54-00-01. ALODINED & PRIMED IAW SRM 51-21-01. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04368 1 20081015 A 5730 ARC436835 PANEL DOUG MD10 MD1010F 3022112 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 RIGHT WING LOWER T/E PANEL 641 GB IS CRACKED. FABRICATED PANEL IAW DWG ARC 0389. ALODINED & PRIMED IAW SRM 51-21-01. PAINTED PANEL IAW SRM 51-21-02. PART MARKED PANEL AMM 7-0-1000. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04369 1 20081015 A 5414 21700416 FAIRING DOUG MD10 MD1010F 3022112 WP NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 NR 1 PYLON PANEL 438 CR IS CRACKED AT THE WELD. FABRICATED REPAIR DOUBLER IAW SRM 54-00-01. INSTALLED REPAIR DOUBLER I AW SRM 54-00-01 & SRM 51-35-01. 2 L 7 3 4F RT A22WE 20081024 NE 2008 10 24 08FDEA04371 2 20081015 A 7200 ENGINE AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4E 52054 NE NR 2 HUNG START A FDEA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CE 21 421FE 342 715842 NUMBER TWO ENGINE HUNG START AT 36 PERCENT N2, EGT 506'. ABORTED START FOLLOWED QRH PROCEDURES. SECOND START ATTEMPT NUMBER TWO ENGINE HUNG AT 38 PERCENT N2. START AIR PRESSURE 30 PSI. REJECTED START AT 529'. OBSERVED PEAK EGT 538'. ENGINE REMOVAL APPROVED BY PROPULSION ENGR. DUE TO HIGH DRAG OF THE N2 SPOOL. REPLACED NR 2 ENGINE IAW W/C 44T0704-2 REV 14 OPERATIONAL AND LEAK CHECKS GOOD PER JRM AND AMM 72-00 TEST 13. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A35EU E3NE 20081024 NM 2008 10 24 08FDEA04466 1 20081022 A 5320 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 DURING OPEN HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WIT H CRACK INDICATIONS AT HOLES NR A AND NR D. CARRIED OUT REPAIR AS PER SRM 53-50-00. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04488 1 20081022 A 7797 8TK34ABF2 LEAD DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL NR 3 ENGINE MALFUNCTIONED A FDEA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 CE 21 367FE 46605 451580 WHEN DESCENDING OUT OF FL240 FOR LANDING, GOT "ENG 3 EGT HI" AND ENG 3 EXCEEDANCE ALERTS EGT 3 INDICATION. SEQUENCED BE TWEEN HIGH INDICATIONS (1053) AND AMBER "X", NO SECONDARY INDICATIONS. SHUT DOWN ENGINE IAW QRH, EGT WAS HIGH APPROX 30 SEC ON LANDING CRASH CREW REPORTED NO HIGH TEMPS, NO FLUIDS LEAKING. NO DEFECTS FOUND IN INTAKE/EXHAUST AREA. AIU-3 F AULT REVIEW HAS IN AIR FAULT 314174 ENG 3 EGT OUT OF RANGE,PROBABLE CAUSE ENG 3 EGT SENSOR,THIS SHOWS AS A INTERMITTENT FAULT. REMOVED AND REPLACED FWD THERMOCOUPLE LEAD IAW MM 77-21-02-2. ALL INDICATIONS NORMAL. RESET EXCEDENCE ON ENGINE DISPLAY. OK FOR SERVICE. 2 L 7 3 4F 4 F RT A22WE E23EA 20081024 NM 2008 10 24 08FDEA04467 1 20081022 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 DURING OPEN HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WIT H CRACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D. CARRIED OUT REPAIR AS PER SRM 53-50-00. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 DL76G081340 1 20081009 A 3610 80217010 SHUTOFF VALVE BOEING 767 767332 1382001 NM NR 2 ENGINE UNSERVICEABLE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 176DZ 29697 727739 IN FLIGHT EICAS MESSAGE RIGHT HPSOV ALONG WITH BLEED RIGHT LIGHT ON OVERHEAD PANEL. FWD TO MCO AND PLAC PER MEL 36-11-0 2. 2 L 7 2 4F RT A1NM 20081024 NM 2008 10 24 SWAA085679 1 20081021 A 5312 6962104 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FWD BULKHEAD O/B STIFFENER CRACKED AT BS 663, RBL 6.15. REPLACED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 20081024 2008 10 24 SWAA085683 4 20081020 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081024 EA 2008 10 24 COMA0860417 1 20081011 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 933CA 7040 DURING 640 FRAME INSPECTION FOUND FRAME CRACKED AT STRINGER 9 RT CUTOUT. REPAIRED 640 FRAME PER REO 601R-53-61-557. 2 L 7 2 4F RT A21EA 20081024 EA 2008 10 24 COMA0860419 1 20081012 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 588SW 28133 7069 EMERGENCY FLOOR LIGHTS ROW 8 AFT INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK NR 2. 2 L 7 2 4F RT A21EA 20081024 EU 2008 10 24 UPS08153705 1 20081014 A 5321 B5327075100200 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 140UP 0823 INSPECTION TYPE:1C3C MAIN CARGO DECK FLOORBOARD 241EF HAS FIELD REPAIR. REPAIRED MAIN CARGO FLOORBOARD 241EF REF A300-6 00 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 08FDEA04482 1 20081022 A 5315 A53779699200 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 668FE 772 FWD CARGO COMPT FR 31 BETWEEN SEAT TRACK NR 4 LT AND TRACK NR 5 LT FLOORBEAM HAS .25 INCH CRACK. REMOVED CRACK AND INST ALLED CROSSBEAM REPAIR AT CRACKED STIFFENER AT FR 31, BETWEEN SEAT TRACK NR 4 LT AND NR 5 LT IAW SRM 53-10-15, FIG 212, PAGE 397/398. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 08FDEA04407 1 20080916 A 5711 A57110603202 SPAR AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 725FD 572 RT WING RIB 5 NEXT CENTER SPAR FWD ZONE FOUND WITH CRACK (RIB 5 TO TOP SKIN). RIB 5 REPAIRED IAW EA 6-5710-121705. 2 L 7 2 4F RT A35EU 20081024 WP 2008 10 24 AALA200802401 1 20080921 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 554AA 53084 DFW EMERGENCY LIGHTS AT SEAT ROWS 20 TO AFT CABIN ARE DIM. REPLACED BATTERY PACK AT STATION 1154 FOR EMERGENCY LIGHTS A T SEAT ROWS 20 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081027 EA 2008 10 27 A6WA200840595 1 20080926 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA MLG ILLUMINATED A A6WA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 GL 31 425AW 7663 ON GEAR EXTENSION AND RETRACTION RECEIVED ANTI-SKID OB CAUTION MESSAGE. COMPLIED WITH QRH. EMERGENCY LANDING DECLARED. B RAKE SYSTEM OPS CHECK GOOD IAW 32-43-00710-801. (K) 2 L 7 2 4F RT A21EA 20081027 EU 2008 10 27 M7KA0625084248 1 20080804 A 7921 BEARING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ARMATURE FAILED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 846MH 818 2259 4248 23399 PILOT REPORTED THAT ON PREFLIGHT INSPECTION THE OIL COOLER FAN IMPELLOR WOULD NOT TURN BY HAND. BEARINGS WERE SEIZED. I NSTALLED SERVICEABLE BLOWER ASSY. THIS PART IS FAILURE PRONE, SUSPECT ALTERNATIVE ARMATURE BEARINGS OR GREASE BE CONSID ERED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 NE 2008 10 27 M7KA0625084248A 2 20080804 A 7532 9550164950 BLEED VALVE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE INTERFERENCE E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 846MH 675 4248 23399 DURING FLIGHT OPERATIONS BLEED VALVE WAS STICKING OPEN INTERMITTENTLY. A SERVICEABLE BLEED VALVE WAS INSTALLED. NO FURTH ER DEFECT NOTED. SUSPECT ANEROID BELLOWS LOST PRESSURE. THIS IS A REAR FAILURE FOR THIS PART. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 NM 2008 10 27 DL757081382 1 20081020 A 5320 146N54462 WEB BOEING 757 757232 1384965 NM BS 1510 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 CORROSION ON LOWER SIDE OF FLOOR SUPPORT AT STATION 1510 RBL 12. REPAIRED ON NR 00044 PER 51-40-05. 2 L 7 2 4F RT A2NM 20081027 EA 2008 10 27 SWIA200820192 1 20081018 A 3210 ARM CNDAIR CL600 CL6002B19 1900309 EA RT MLG CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 RIGHT MLG TRAILING ARM CORRODED. C-CHECK, REPLACED RIGHT MLG TRAILING ARM. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 SWIA200820193 1 20081018 A 3213 AXLE CNDAIR CL600 CL6002B19 1900309 EA RT MLG CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 REMOVED RIGHT MLG AXLE DUE TO CORRSION. C-CHECK, REPLACED RIGHT MLG AXLE. 2 L 7 2 4F RT A21EA 20081027 SO 2008 10 27 SWIA200820195 1 20081019 A 3350 BULB EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 292SW 120319 FLT 5557 - EXIT SIGN AT MAIN CABIN DOOR, COVER MISSING AND BULBS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 20081027 NM 2008 10 27 DL757081388 1 20081020 A 5320 HFAB53AN011 STIFFENER BOEING 757 757232 1384965 NM BS 680 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 VERTICAL WEB STIFFENER CRACKED AT STATION 680 RBL 25. REAPAIRED ON NR 00096 PER 51-20-01. 2 L 7 2 4F RT A2NM 20081027 NM 2008 10 27 DL757081389 1 20081020 A 5320 HFAB53AN002 ANGLE BOEING 757 757232 1384965 NM BS 680 RBL 25 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 ANGLE CRACKED AT STATION 680 RBL 25. REPAIRED ON NR 0095 PER 51-20-01. 2 L 7 2 4F RT A2NM 20081027 EA 2008 10 27 SWIA200820198 1 20081013 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 EMERGENCY LIGHTS INOP AFT OF ROW 8. FLT 6644, REPAIRED BROKEN WIRE. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 SWIA200820201 1 20081015 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 929SW 7703 FLT 6529 - CEILING LEVEL ERMERGENCY FLOOD LIGHT, ROW 10 INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 SWIA200820204 1 20081016 A 2910 QUICK DISCONNECT CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM DISCONNECTED A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 07 912EV 7728 FLT 3981 - AFTER TAKEOFF "HYDRAULIC 1 LO PRESS" AND "HYD 1 EDP" CAUTION MESSAGES DISPLAYED. RECONNECTED NR 1 EDP QUICK CONNECT FITTING 'P' SAFETY FITTING. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 SWIA200820206 1 20081017 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 708SK 10156 FLT 5831 - LAST OVERHEAD CEILING EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 SWIA200820207 1 20081019 A 5610 NP13932114 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FRACTURED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 438SW 7574 FLT 3863 - RIGHT WINDSHIELD SHATTERED IN CRUISE. REPLACED RIGHT WINDSHIELD, PN NP-139321-14, SN ON 08137H6207, SN OFF 0 1157H9325. 2 L 7 2 4F RT A21EA 20081027 NM 2008 10 27 DL76G081343 1 20081011 A 2150 A/C PACK BOEING 767 767332 1382001 NM RIGHT INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 169DZ 29689 RT PACK INOP AFTER ENGINE START. MTC CYCLED BREAKER A28 RT FLOW CONTROL VALVE CHECKED FOR CONDITION OK. RT PACK FLOW C ONTROL C/B RESET. SYSTEM OK RT BITE CONTROLLER PERFORMED, FAULTS FOUND OPS OK. 2 L 7 2 4F RT A1NM 20081027 NM 2008 10 27 DL757081344 1 20081008 A 5320 114N51666 INTERCOSTAL BOEING 757 757232 1384965 NM BS 860-880 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 609DL 22816 INTERCOSTAL BS 860-880 BL 0 WL 208 HAS DAMAGED HOLES REMOVED AND REPLACED PER SRM 51-40-02 STEP 4. 2 L 7 2 4F RT A2NM 20081027 EA 2008 10 27 QXEA200800928 1 20080817 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK LOWER FUSELAGE EXTERNAL SKIN HAS NICK AT APPROX STA X52 BETWEEN STRINGERS 31R AND 32R. BLENDED OUT DAMAGE WITH SCRUB PAD. HFEC INSP IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECK IAW Q400 NDTM PART 1, 51 -00-04. HIGH .063" LOW .056". FOUND OUT OF LIMITS. MAPPED FOR ENGINEERING. BLEND FOUND IN LIMITS IAW RD8/4-53-2455. PAINTED IAW Q400 SRM 51-25-05 PG 206. 2 L 7 2 4F RT A21EA 20081027 NM 2008 10 27 KCSA081532 1 20081013 A 5720 SUPPORT BEAM BOEING 747 747249F 1384849 NM RT WING SPOILER CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 RT WING SPOILER SUPPORT BEAM UPPER CHORD CORRODED AT APPROX W.S. 528. 2 L 7 4 4F RT A20WE 20081027 NM 2008 10 27 KCSA081535 1 20081014 A 5711 SPAR BOEING 747 747249F 1384849 NM NR 1 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 NR 1 PYLON MID SPAR WEB STIFFENER HAS CHAFF DAMAGE AT NAC. STA-210 R/H TOP. 2 L 7 4 4F RT A20WE 20081027 NM 2008 10 27 QXEA2008102301081 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4- RT INBOARD SEAT TRACK HAS SCRATCHES INSIDE THE CHANNEL FROM STA X611 TO X620. BLENDED OUT SCRATCHES IAW RD 8/ 4-53-884, WITHIN LIMITS PER RD 8/4-53-884. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ETCHED AND ALODINED AREA IAW RD 8/4-53-884. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 QXEA2008102301084 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4- NR 6 SEAT TRACK HAS CORROSION AT STA X219. BLENDED OUT CORROSION IAW RD 8/4-53-884, WITHIN LIMITS PER RD 8/4- 53-884. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ETCHED AND ALODINED AREA IAW RD 8/4-53-884. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 QXEA2008102301094 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4- NR 19 SEAT TRACK HAS CORROSION IN THE BASE BETWEEN APPROX STA X624.500 TO X634.500. BLENDED OUT CORROSION IAW RD 8/4-53-884, WITHIN LIMITS PER RD 8/4-53-884. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ETCHE D AND ALODINED AREA IAW Q400 SRM 51-21-10. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 QXEA2008102301095 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4- RT INBOARD SEAT TRACK HAS SCRATCHES AND CHAFING IN CHANNEL AND TOP APPROX STA X245 TO X248. BLENDED OUT CORRO SION IAW RD 8/4-53-884, WITHIN LIMITS PER RD 8/4-53-884. HFEC INSPECTED IAW 1-84-7A PART 6, 51-00-02, NO CRACKS NOTED. ETCHED AND ALODINED AREA IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 QXEA2008102301096 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4- RT INBOARD SEAT TRACK HAS CHAFING AND SCRATCHES ALONG CHANNEL AND TOP APPROX STA X300 TO X305. BLENDED OUT CO RROSION IAW RD 8/4-53-884, WITHIN LIMITS PER RD 8/4-53-884. HFEC INSPECTED IAW 1-84-7A PART 6, 51-00-02, NO CRACKS NOTE D. ETCHED AND ALODINED AREA IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 20081027 2008 10 27 DXTA2008102403315 2 20081023 A 7200 ENGINE AMD FALC50 FALCON2000 2730170 NM NR 1 SHUTDOWN E DXTA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 GL 07 230QS 59 ENG NR 1 SHUT DOWN BY FADEC (LOW OIL PRESS FLICKERED ON). 2 L 7 2 4F RT A50NM 20081027 NM 2008 10 27 USAA920081707 1 20080909 A 5540 D5537131800200 HINGE FITTING AIRBUS A319 A319132 3930340 NM RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 813AW 1223 SAL - BC6 - MAJOR REPAIR, EXCESSIVE PLAY AT RUDDER HINGE FITTING NR 3. REPLACED RUDDER HINGE FITTING NR 3 IAW A319 AMM 55-36-41. 2 L 7 2 4F RT A28NM 20081027 NM 2008 10 27 USAA920081737 1 20080919 A 5753 6546486130 WEDGE BOEING 737 7373G7 138447J NM TE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MAJOR REPAIR, RT WING INBOARD MIDFLAP TRAILING EDGE WEDGE DELAMINATED AT WBL 108.5 THRU WBL 111.5. REPAIRED RT WING INB OARD MIDFLAP TRAILING EDGE WEDGE AT WBL 108.5 THRU 111.5 IAW 51-70-10-2R4. 2 L 7 2 4F RT A16WE 20081027 NM 2008 10 27 USAA920081716 1 20080921 A 5755 SPOILER BOEING 737 7373S3 1384711 NM NR 7 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 PHX - MAJOR REPAIR, NR 7 SPOILER IS DELAMINATED IN 2 SPOTS. REPLACED NR 7 SPOILER IAW B737 MM 27-61-11. 2 L 7 2 4F RT A16WE 20081027 NM 2008 10 27 USAA920081734 1 20080822 A 5320 655056813 STRAP BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 SAL - C19 - MAJOR REPAIR, CORROSION ON STRAP BETWEEN BS 947 TO 986.5, RBL48. REPAIRED STRAP BETWEEN BS 947 TO 986.5, RB L48 IAW B737 SRM 51-70-11-0G. 2 L 7 2 4F RT A16WE 20081027 NM 2008 10 27 USAA920081722 1 20080901 A 5311 6546532 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 SAL - C17 -MAJOR REPAIR, FRAME AT BS 480 HAS A .410 INCH CRACK BETWEEN S8L & S9L AND A .371 INCH CRACK BETWEEN S8R & S9R . REPAIRED FRAME AT BS 480 BETWEEN S8L & S9L, ALSO BETWEEN S8R & S9R IAW AMERICA WEST AIRLINES TASK CARD NR MIC53002. 2 L 7 2 4F RT A16WE 20081027 NM 2008 10 27 USAA920081704 1 20080921 A 5330 6545774 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 23381 CLT - C5 - MAJOR REPAIR, CRACK ON FUSELAGE SKIN AT BS 727E BELOW S23L. REPAIRED FUSELAGE SKIN AT BS 727E BELOW S23L IAW B737 SRM 53-00-01 REPAIR NR 31 TEMPORARY REVISION NR 53-33. 2 L 7 2 4F RT A16WE 20081027 NM 2008 10 27 USAA920081706 1 20080921 A 5330 6545774 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 CLT - RON - MAJOR REPAIR, CRACK IN FUSELAGE SKIN BETWEEN BS 747 & BS 767, S21L. REPAIRED FUSELAGE SKIN BETWEEN BS 747 & BS 767, S21L IAW B737 SRM 53-00-01 REPAIR DETAIL 12 FIGURE 201 & TEMPORARY REVISION 53-2. 2 L 7 2 4F RT A16WE 20081027 NE 2008 10 27 USAA920081714 2 20080919 A 7200 ENGINE AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE NR 1 VIBRATION A USAA O OTHER E VIBRATION/BUFFET CR CRUISE 1 EA 19 765US 1371 779579 FLT NR 2134 - LGA-BOS, EMERGENCY LANDING, AT CRUISE POWER, A BANG WAS HEARD AND SEVERE VIBRATION FELT. THE FLT CREW PUL LED POWER BACK TO IDLE AND VIBRATION STOPPED. ON ATTEMPT TO RESTORE POWER TO CLIMB, WHILE TRANSITIONING THRU 40-45% N1, VIBRATION AND BANG RESUMED. AIRCRAFT DIVERTED TO BDL. THE FLT LANDED NORMALLY AND TAXIED TO THE GATE. MX REMOVED AND REPLACED NR 1 ENGINE. *SUPPLEMENTAL* TO BE ISSUED UPON REVIEW OF VENDOR TEAR DOWN REPORT. 2 L 7 2 4F 4 F RT A28NM E37NE 20081027 EU 2008 10 27 USAA920081717 1 20080920 A 5315 D5347219020300 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 PIT - S4 -MAJOR REPAIR, LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT -Y765, BETWEEN FR 66 TO FR 68. REPLACED FLOORBEA M AT -Y765, BETWEEN FR 66 TO FR 68 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081024 NM 2008 10 24 UPS08653694 1 20081018 A 5753 113T220138G FLAP BOEING 767 76734AF 1385212 NM RT WING DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 323UP 27749 INSPECTION TYPE:N/A RIGHT I/B MAIN FLAP DENTED OUT OF SRM LIMITS. REPAIRED PER EO B767-5750-30895-A. 2 L 7 2 4F RT A1NM 20081024 WP 2008 10 24 AALA200802519 1 20080918 A 5313 3913291501 LONGERON SPLICE DOUG DC9 DC982 3022082 WP BS 1297 L25L CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 CRACK IN LONGERON PRODUCTION SPLICE IN AFT CARGO AT STATIONS 1297 LONGERON 25 LT. AREA OF DISCREPANCY IS 2 INCHES BY 6 INCHES. CRACK LENGTH IS 2 INCHES. INSTALLED NEW LONGERON SPLICE PER SRM 51-30-00. 2 L 7 2 4F A6WE 20081024 WP 2008 10 24 AALA200802436 1 20080924 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 292AA 49304 EXTERIOR EMERGENCY LIGHT REMAINED ON AFTER ENGINE SHUTDOWN. RECHARGED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHT. SYSTE M GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081024 EA 2008 10 24 QXEA200800931 1 20080817 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK RT INBD SEAT TRACK NR 16 IS PITTED AT APPROX X670, X673 AND X698. EVALUATED SEAT TRACK FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK PREPPED AND INSTALLED NEW NR 15 SEAT TRACK. IAW Q400 SRM 51-40-07, 51-40-15, 51-42-05 AND 5 1-25-10. 2 L 7 2 4F RT A21EA 20081024 EA 2008 10 24 QXEA200800929 1 20080817 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK LT INBD SEAT TRACK IS CORRODED AT X608, X619, X637 AND X645. BLENDED CORROSION REF RD8/4-53-884 FOUND OUT OF LIMITS. REMOVED SEAT TRACK IAW Q400 SRM 51-40-07. PREPPED AND INSTALLED NEW TRACK IAW Q400 SRM 51-40-07, 51-21-10, 51-42-00 AND 51-40-15. 2 L 7 2 4F RT A21EA 20081024 WP 2008 10 24 08FDEA04366 1 20081015 A 5712 ARB24075 RIB DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 LEFT WING UPPER L/E PANEL 517 CT HAS 2 CRACKED RIBS. REMOVED 2EA CRACKED RIBS IAW SRM 51-35-01 & SRM 51-33-01; VOL II. & FABRICATED IAW DWG ARB 2407; REV "G". ALODINED & PRIMED IAW SRM 51-21-01; PGS 21 - 24; VOL II. INSTALED IAW DWG ARB 2407; REV "G"; SRM 51-35-10 & 51-33-01; VOL II. 2 L 7 3 4F RT A22WE 20081024 EU 2008 10 24 08FDEA04370 1 20081015 A 5753 A5796069020000 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 LEFT OUTBD FLAP L/E IS GOUGED AT THE INBD END OF THE FLAP. BLENDED GOUGE SMOOTH IAW SRM 51-73-10. LT WING OUTBD FLAP LE NOSE SKIN BETWEEN RIB NR 1 & 2 FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00. FABBED & INSTALLED OUTBD FLAP LE REPAIR IAW SRM 57-50-00. TOP COAT PAINTED IAW SRM 51-23-10. 2 L 7 2 4F RT A35EU 20081231 WP 2008 12 31 AALA200802459 1 20081102 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 DFW - EMERGENCY LIGHT AT SEAT ROW 22 MISSING SHROUD. REPLACED SHROUD AT SEAT ROW 22 SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F A6WE 20081024 NE 2008 10 24 AALA200802452 2 20080927 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 1 LEAKING A AALA E A ENGINE SHUTDOWN UNSCHED LANDING K E J FLUID LOSS VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 21 3515 49892 728081 EWR INFLT T1323/27SEP JFK TO ORD CREW REPORTED VIBRATION IN AIRFRAME FOLLOWED BY NR 1 ENGINE OIL QUANTITY LOSS AND OIL TEMPERATURE INCREASE. CREW SHUT DOWN NR 1 ENGINE. LANDED EWR WITHOUT INCIDENT. SINGLE ENGINE TIME 15 TO 20 MINUTES. REPLACED NR 1 ENGINE ON 28 SEP AT EWR DUE TO OIL LEAK. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F 4 F A6WE E9NE 20081024 EU 2008 10 24 AALA200802448 1 20080926 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 EMERGENCY LIGHTS AT RT NR 2 DOOR TO SEAT ROW 18 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RT NR 2 DOOR TO SEAT ROW 18. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A35EU 20081024 NM 2008 10 24 AALA200802442 1 20080925 A 5610 WINDOW BOEING 737 737823 13844CB NM COCKPIT CRACKED A AALA K NONE O OTHER CR CRUISE 1 SW 21 968AN 30095 INFLIGHT T2127/25SEP MIA TO LIR. FIRST OFFICER WINDOW CRACKED DURING CRUISE. LANDED MGA WITHOUT INCIDENT. REPLACED WI NDOW AND WINDOW HEAT CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081024 WP 2008 10 24 AALA200802406 1 20080921 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 469AA 49599 PHX CREW REPORTED EMERGENCY EXIT SIGN NOT ILLUMINATED AT OVERWING EXITS. REPLACED BATTERY PACK IN AFT POSITION STATION 1100, FOR EMERGENCY SIGN AT AFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081027 EU 2008 10 27 M7KA0810084433 1 20080901 A 5200 PIN UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE HINGE DISLODGED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 854MH 4433 FOUND PIN FALLING OUT DURING ROUTINE INSPECTION. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 EU 2008 10 27 M7KA0709083967 1 20080901 A 8000 975UN01B4AA5P SWITCH UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE START/STOP DEFECTIVE E M7KA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 19 813MH 2869 3967 23183 DURING START ATTEMPT YELLOW AND AMBER GOVERNOR LIGHTS ILLUMINATED. FAULT CODE INDICATED START/STOP SWITCH AS DEFECTIVE. A NEW SWITCH WAS INSTALLED AND NO FURTHER DEFECT REPORTED. THIS IS A RARE FAILURE FOR THIS PART. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 SO 2008 10 27 XGN2008F00013 2 20080929 A 8530 CYLINDER CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO NR 1 CRACKED A XGNA O OTHER O OTHER NR NOT REPORTED 1 SW 05 3378Q 405 402B0334 182909R CASE CRACKED, TOP OF NR 1 CYL, FWD TOP STUD 3 INCHES LONG. GOING UP TO TOP OF CASE. (K) 1 L 7 2 3O 3 O A7CE E8CE 20081027 WP 2008 10 27 U2R2008F00010 1 20081014 A 5720 STRAP DOUG DC8 DC871F 302199D WP RWS 341 CRACKED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 872SJ 46040 DURING C-CHECK FOUND RT WING XFS 341.500 CENTER LEADING EDGE INTERIOR LOWER SURFACE STRAP HAS 12 INCHES CRACK. (K) 2 L 7 4 4F RT 4A25 20081027 EU 2008 10 27 M7KA0702084313 1 20080804 A 5344 350A58004523 HINGE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE CREW DOOR CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 818MH 4131 23069 DURING ROUTINE INSPECTION CRACKS ON THE HINGE SURFACE RADIATE FROM MOUNTING BORES. THIS IS A VERY COMMON FAILURE FOR THI S PART. SUGGEST PART BE MANUFACTURED FROM A MORE DURABLE MATERIAL SUCH AS STAINLESS STEEL OR TITANIUM. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 WP 2008 10 27 U2R2008F00012 1 20081013 A 7830 3052356596 FITTING DOUG DC8 DC871F 302199D WP THRUST REVERSER CORRODED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 872SJ 46040 DURING C-CHECK FOUND NR 1, 2, 3, 4 ENGINE THRUST REVERSER TRANSLATING COWL RAIL FITTINGS CORRODED. (K) 2 L 7 4 4F RT 4A25 20081027 EU 2008 10 27 M7KA0804084038 1 20080901 A 5340 350A54112420 BRACKET UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE STARTER CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 816MH 1501 4038 23096 FOUND CRACKED DURING ROUTINE PERIODIC INSPECTION. INSTALLED NEW BRACKET AS REQUIRED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 WP 2008 10 27 22AA20081002 1 20081015 A 2752 CYLINDER DOUG DC8 DC863F 302198F WP TE FLAPS MALFUNCTIONED A 22AA O OTHER J WARNING INDICATION AP APPROACH 1 SO 19 784AL 46135 ON APPROACH INTO MROC THE FLAPS WOULD NOT EXTEND BEHOND 23 DEGREES. FOUND OUTBOARD FLAP LOCKOUT CYLINDER RETRACTED; SER VICE FLAP LOCKOUT CYLINDERS IAW MM 27-51-10. OPERATIONAL CHECK FOUND NORMAL IAW MM 27-50-00. 2 L 7 4 4F 4A25 20081027 NM 2008 10 27 DHLA2008745520A 1 20080917 A 5340 69162691 FITTING BOEING 727 727224 1384076 NM ZONE 100 CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE AFT CARGO COMPARTMENT BS 950,WL 175 LBL 50 BULKHEAD LATERAL FITTING CRACKED. 2 L 7 3 4F A3WE 20081027 CE 2008 10 27 DXTA2008102203313 1 20081021 A 2750 FLAP SYSTEM CESSNA 560 560XL 2076702 CE TE FLAPS MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 681QS 5605181 AT 400FT AND SELECTING FLAPS FROM 15 TO ZERO DEGREES, FLAPS INDICATOR STOPPED AT 7 DEGREES. 2 L 7 2 4F RT A22CE 20081027 NM 2008 10 27 QXEA200800953 1 20080820 A 5720 INTERCOSTAL BOMBDR DHC8 DHC8402 1390042 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 410QX 4053 PDX - C-CHECK, LT WING VERTICAL INTERCOSTAL, LOCATED UNDER OUTBOARD SPOILER HAS A CRACKED LIGHTENING HOLE. REMOVED INTE RCOSTAL AT OUTBOARD SPOILER, MATCH DRILLED NEW FROM STOCK INTERCOSTAL AT YW 357.30. PAINTED AND INSTALLED NEW FROM STOC K INTERCOSTAL IAW 8-400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 QXEA200800973 1 20080831 A 5210 FITTING BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 414QX 4061 PDX - C-CHECK, AFT PAX DOOR AFT TRACK LATCH FITTING HAS A GOUGE ACROSS UPPER SURFACE. REPAIRED REF RD 8/4-52-145 STEPS 1, 3-7. HFEC INSPECTED IAW D8 400 NDTM PT 6, 51-00-01 & RD 8/4-52-145 STEP 2. NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 QXEA200800972 1 20080831 A 5320 FLOOR SUPPORT BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 414QX 4061 PDX - C-CHECK, AFT BAGGAGE COMPARTMENT AT X783.102 LT FLOOR SUPPORT HAS CORROSION UNDER N/P. REMOVED NUT PLATE AND REMO VED CORROSION FROM UNDER NUT PLATE IAW Q400 SRM 51-21-00. HFEC AS PER 1-84-7A, PT 6, 51-00-02, NO CRACKS NOTED. THICKN ESS CHECK AS PER 1-84-7A, PT 1, 51-00-04 MAX .048 MIN .046. ALODINED PRIMED REF Q400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 QXEA2008102401097 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX-C4- RT INBOARD SEAT TRACK HAS CHAFING FROM APPROX STA X310 TO X345 IN CHANNEL AND TOP. REMOVED CHAFING AND FOUND T O BE WITHIN LIMITS PER RD8/4-53-884. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. APPLIED ETCH AND ALODINE IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 20081027 CE 2008 10 27 DXTA2008102303314 1 20081022 A 3150 WARNING LIGHT CESSNA 750 750 2076810 CE ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 950QS 7500050 ON TAKEOFF ROLL <80 KNOTS AMBER YD OFF LOWER LIGHT. 2 L 7 2 4J RT T00007WI 20081027 NM 2008 10 27 QXEA2008102301078 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4- NR 6 SEAT TRACK HAS CORROSION INSIDE THE CHANNEL AT STA X179.0 TO X187.0. BLENDED CORROSION IAW RD 8/4-53-884 , WITHIN LIMITS PER RD 8/4-53-884. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ETCHED AND ALODINED AREA IAW RD 8/4-53-884. 2 H 7 2 4T RT A13NM 20081027 CE 2008 10 27 DXTA2008101703307 1 20081016 A 3234 WARNING LIGHT BEECH MU300 400A 1155402 CE MLG HANDLE MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 153QS RK490 UPON GEAR RETRACTION THE RED LIGHT IN THE GEAR HANDLE REMAINED ON AND THE GREEN LIGHT IN THE NOSE INDICATOR REMAINED ON. 2 H 7 2 4F RT A16SW 20081027 NM 2008 10 27 QXEA2008102301080 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4- NR 1 SEAT TRACK HAS CORROSION IN THE BASE BETWEEN APPROX STA X71.200 TO X196.00. BLENDED CORROSION IAW RD 8/4 -53-884, WITHIN LIMITS PER RD 8/4-53-884. HFEC INSPECTED IAW 1-84-7A, PART 6, 51-00-02, NO CRACKS NOTED. ETCHED AND AL ODINED AREA IAW RD 8/4-53-884. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 USAA920081705 1 20080919 A 5330 6545774 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 CLT - RON - MAJOR REPAIR, CRACK ON FUSELAGE SKIN AT 727G, S24L. REPAIRED FUSELAGE SKIN AT 727G, 24L IAW US AIRWAY EA NR 100654. 2 L 7 2 4F RT A16WE 20081027 NM 2008 10 27 USAA920081727 1 20080901 A 5311 6546548 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 SAL - C17 -MAJOR REPAIR, FRAME AT BS 747 HAS A .471 INCH CRACK BETWEEN S8L & S9L. REPAIRED FRAME AT BS 747 BETWEEN S8L & S9L IAW AMERICA WEST AIRLINES TASK CARD NR M1C53002. 2 L 7 2 4F RT A16WE 20081027 NM 2008 10 27 QXEA200800950 1 20080820 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 410QX 4053 PDX - C CHECK, CORROSION ON THE NR 9 SEAT TRACK FLANGE AT STA X734-X763.3. INSPECTED AND FOUND TRACK TO BE OUT OF LIMIT S. REMOVED SEAT TRACK IAW SRM 51-40-07. INSTALLED NEW TRACK REF 8-400 SRM 51-42-05 AND 51-40-15. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 USAA920081724 1 20080901 A 5311 65C25229 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 SAL - C17 -MAJOR REPAIR, FRAME AT BS 727D HAS A .389 INCH CRACK BETWEEN S8L & S9L AND A .496 INCH CRACK BETWEEN S8R & S9 R. REPAIRED FRAME AT BS 727D BETWEEN S8L & S9L, ALSO BETWEEN S8R & S9R IAW AMERICA WEST AIRLINES TASK CARD NR M1C53002. 2 L 7 2 4F RT A16WE 20081024 EU 2008 10 24 08FDEA04454 1 20081021 A 5730 A57340084203 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 725FD 572 SUB-SURFACE CORROSION FOUND ON THE RT WING SKIN UPPER PANEL COMPLIDE WITH EA NR 6-5710-125470. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 08FDEA04486 1 20081022 A 5340 A5381206720000 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 THE 3RD LEFT SEAT TRACK INBD TRACK SUPPORT IS CRACKED AT FRAME 49. REMOVED & REPLACED THE TRACK LINK FITTING IN REF TO SRM 51-40-21. APPLIED TOP COAT IN REF TO SRM 51-73-10. 2 L 7 2 4F RT A35EU 20081024 WP 2008 10 24 08FDEA04418 1 20081017 A 7830 4071M68G03 PANEL DOUG MD10 MD1010F 3022112 WP THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 NR 3 ENGINE RIGHT T/R UPPER HINGE CLOSE OUT PANEL IS CRACKED AT THE HINGE RELIEF. REPLACED DAMAGED HINGE ACCESS PANEL W ITH A NEW PANEL IAW SRM 51-31-01. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04419 1 20081017 A 5411 AUB710740 RIB DOUG MD10 MD1010F 3022112 WP NR 3 PYLON WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 NR 3 PYLON PANEL 489 AL HAS A WORN RIB. REMOVED & REPLACED RIB IN REF TO DAC DWG AUB 7107; REV " P '. 2 L 7 3 4F RT A22WE 20081024 EU 2008 10 24 08FDEA04364 1 20081015 A 5320 A2577260900800 PAN AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 AFT LOWER CARGO COMPARTMENT HAS CORROSION ON THE POWER ROLLER PAN AND SUPPORT BETWEEN FRAMES 61 AND 62; LBL 14 INCH (LOW ER SURFACE). REMOVED PAN AND FRAME IAW SRM 51-41-21. REMOVED CORROSION IAW SRM 51-71-10. BOTH FOUND TO BE OUT OF LIMI TS IAW SRM 53-10-00. MACHINED NEW FRAME IAW DWG NR 10A25771822 REV E; 10A25771747; REV K. ALODINED IAW SRM 51-21-10. PRIMED IAW SRM 51-75-10. PAINTED IAW SRM 51-75-10. LOCATED AND DRILLED HOLES IN NEW PAN AND FRAME IAW SRM 51-40-44 AND SRM 51-72-10. PART MARKED IAW GMM 7-0-1000. INSTALLED PAN AND FRAME IAW SRM 51-40-21. INSTALLED PDU IAW AMM 25-54-26 -04. OPS CHECKED. 2 L 7 2 4F RT A35EU 20081024 WP 2008 10 24 08FDEA04365 1 20081015 A 5720 AEA00266 INTERCOSTAL DOUG MD10 MD1010F 3022112 WP RT WING WW CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 RIGHT WHEEL WELL FWD OF STA 1521, THE OTBD INTERCOSTAL IS CORRODED. REMOVED INTERCOSTAL IAW SRM 51-35-01. FOUND CORROD ED TEE CAP. UPON REMOVAL OF THE INTERCOSTAL. REMOVED CORROSION & WORKED AREA IAW SRM 53-40-00 & E.A. 8-5310-123513. F ABRICATED INTERCOSTAL IAW DWG AEA 0026. ALODINED & PRIMED IAW SRM 51-21-01. PAINTED IAW SRM 51-21-01. INSTALLED IAW D WG AEA 0026. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04367 1 20081015 A 5720 ARB12613 STIFFENER DOUG MD10 MD1010F 3022112 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 LEFT WING UPPER L/E PANEL 516 DT HAS A CRACKED ANGLE. REMOVED BROKEN STIFFENER IAW SRM 51-31-01. FABRICATED NEW STIFFE NER IAW DWG ARB 1261 REV NC. HEAT TREATED NEW STIFFENER IAW TPS 1003 REV A, ARB 78/80 HT 102308-2. NEW STIFFENER REQ UIRES ALODINE & PRIMED IAW SRM 51-21-01 VOL II. PART MARKED IAW GMM 7-0-1001. INSTALLED STIFFENER IAW SRM 51-31-01 & D WG ARB 1261 REV NC. 2 L 7 3 4F RT A22WE 20081024 EU 2008 10 24 08FDEA04372 1 20081015 A 2750 FLAP SYSTEM AIRBUS 300 A300F4605R 3930327 EU TE FLAPS MALFUNCTIONED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 21 650FE 726 REPEAT, AFTER TAKEOFF, UPON ATTEMPTING TO RAISE THE FLAPS, FLAPS FAULTED. COMPLIED WITH ECAM AND RED TABS AND RETURNED TO KATL. UPON CONFIG FOR LANDING FLAPS DID GO TO 40 FOR A NORMAL LANDING. FLAPS THEN RETRACTED TO 0 UPON LANDING. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 08FDEA04421 1 20081017 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU BS 3036 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 THE MAIN CABIN SEAT TRACK SUPPORT FITTING AT FRAME 48, STA 3036, RBL 48 IS CRACKED. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 08FDEA04487 1 20081022 A 5347 5381206720000 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 THE 3RD LEFT SEAT TRACK INBD TRACK SUPPORT LINK IS CRACKED AT FRAME 48. REMOVED & REPLACED THE TRACK LINK FITTING IN RE F TO SRM 51-40-21. APPLIED TOP COAT IN REF TO SRM 51-73-10. 2 L 7 2 4F RT A35EU 20081024 NM 2008 10 24 08FDEA04468 1 20081022 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 DURING OPEN HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CR ACK INDICATIONS AT HOLES NR A AND NR C. CARRIED OUT REPAIR AS PER SRM 53-50-00. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 08FDEA04469 1 20081022 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 DURING OPEN HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CR ACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 REMOVED AND REPLACE D AS PER SRM 51-31-01 AND 51-33-01. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 08FDEA04470 1 20081022 A 5320 ACA72261 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 DURING OPEN HOLE HFEC INSPECTION, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 UPPER WEB FIRST LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 3 O'CLOCK POSITION) AT HOLE NR C. CARRIED OUT REPAIR AS PER EA 1-5310-125561. THIS REPAIR C LASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 08FDEA04471 1 20081022 A 5320 ACA72251 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 DURING OPEN HOLE HFEC INSPECTION, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 UPPER WEB SECOND LAYER FOUND WITH CRAC K INDICATION (APPROXIMATELY 8 O'CLOCK POSITION) AT HOLE NR D. CARRIED OUT REPAIR AS PER EA 1-5310-125561. THIS REPAIR C LASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 SWAA085615 1 20081019 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, RBL 14. REPAIRED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 UPS08653688 1 20081011 A 5753 HINGE FITTING BOEING 767 76734AF 1385212 NM TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 331UP 27757 INSPECTION TYPE:N/A RT WING I/B MAIN FLAP AFT I/B HINGE FITTING CRACK CRACK LENGTH .9375 INCH APPROX. RT WING I/B MAIN FLAP AFT FLAP I/B HINGE FITTING REPLACED AS PER SRM 57-53-02-2R FIG 201. 2 L 7 2 4F RT A1NM 20081028 CE 2008 10 28 GUU2008F00064 1 20080910 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE CABIN ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 29 87550 UE205 DURING APPROACH VERY STRONG ODOR COMING FROM CABIN VENTS REGARDLESS OF MODE CONTROL SETTING. RAN ENGINES FOR 30 MINUTES AT ALL POWER SETTINGS AND MODE CONTROL SETTINGS NO ODOR NOTED. (K) 2 L 7 2 4T RT A24CE 20081028 2008 10 28 DXTA2008102003310 4 20081020 A 2210 AUTOPILOT SYS BEECH MU300 400A 1155402 CE COCKPIT MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 108QS RK382 AT 14000FT AND AT 280 KTS WITH AP/FD SELECTED TO LEFT SIDE, RIGHT SIDE ONLY AP PITCH TRIM FAIL LIGHT CAME ON. 2 H 7 2 4F RT A16SW 20081028 NM 2008 10 28 NOC2008F00006 1 20080917 A 2120 UNKNOWN BOEING 757 75728A 1384976 NM CABIN SMOKE A NOCA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 15 754NA 29381 AT FL90 WITH AUTOPILOT ENGAGED ACFT HAD AN OVERSPEED OF 10 KTS AT THE SAME TIME F/A CALLED SMOKE IN CABIN. HAD AN UNEVEN TFUL LANDING, DECLARED AN EMERGENCY. INSPECTED ACFT EXTERIOR STRUCTURE, AFT FUSELAGE, BULKHEAD, STAB FITTINGS, JACKSCRE W AREA NO DAMAGE FOUND NO BUCKLES OR CRACKS. EXAMINED ENGINE PANELS, DOORS AND LOWER SURFACES IAW MM 05-51-04-212-019 U NABLE TO DUPLICATE THE SMOKE IN CABIN. CHECKED BOTH PACK BAYS, ALL CARGO BAYS, LAVS, E/E COMPARTMENTS NO SIGNS OF HEAT. AIRCRAFT OK FOR SERVICE. (K) 2 L 7 2 4F RT A2NM 20081028 SO 2008 10 28 GUU2008F00063 1 20080915 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 268AS 120202 DURING SCHEDULED ROUTINE MAINT DISCOVERED NR 1 EMERGENCY LIGHT BATTERY PACK INOPERATIVE. RECHARGED NR 1 EMERGENCY LIGHT BATTERY PACK. (K) 2 L 7 2 4T RT A31SO 20081028 NE 2008 10 28 ZES2008F00001 2 20080908 A 7230 30C4656C DIFFUSER AMD FALC50 FALCON2000 2730170 NM PWC PW308 PW308C 52182 NE ENGINE CORRODED E ZESA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 03 267BW 790 107 PCECF0243 DURING ENGINE START OIL PRESSURE REMAINED AT ZERO PSI WITH A LOW OIL PRESSURE LIGHT WHEN ENGINE REACHED IDLE. SHUT DOWN ENGINE. INVESTIGATION REVEALED THE ENGINE DRIVEN HYDRAULIC PUMP LOCKED UP DUE TO A PIECE OF METAL THAT HAD DETACHED FRO M THE DIFFUSER CASE THAT SUPPORTS THE NR3 MAIN BEARING. GOT INTO THE OIL SYS, SLIPPED BRG THE INLET SCREEN TO THE PUMP. (K) 2 L 7 2 4F 4 F RT A50NM E00065EN 20081028 NE 2008 10 28 IXXA080026O 2 20081018 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE NR 4 FLAMED OUT A IXXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CL CLIMB 1 SW 11 823BX 44887 9166 46064 693495 DURING CLIMBOUT FROM KPDX AT 39000 FT NUMBER 4 ENGINE FLAMED OUT, AIRSPEED UNKNOWN, MACH .78, ALT 36.0, RAT UNKNOWN, WT 220.0 WEATHER CLEAR NO FIRE WARNING. GENERATOR WENT OFF LINE, OIL PRESS LIGHT ON, IGNITION OFF, FUEL FEED NOT CHANGED, WINDMILLING OIL PRESS 5 PSI, FUEL PRESS UNKNOWN. BEFORE FLAME OUT N1, N2 AND F/F WAS FLUCTUATING FOR 20 TO 30 SECONDS. THE CREW ATTEMPTED RESTART AT 35000 AND WAS UNSUCCESSFUL. CREW PERFORMED ENGINE SHUTDOWN CHECK LIST. THE CREW LANDED IN KLAX WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED REMOVED AND REPLACED FUEL PUMP FILTER, NO CONTAMINATION OR DEBR IS. INSPECTED CDP TUBE, MAG CHIP, FUEL PUMP LOW PRESSURE IMPELLER ROTATION, NO DEFECTS NOTED. MAINTENANCE REMOVED WATE 2 L 7 4 4F 4 F RT 4A25 E2GL 20081028 NM 2008 10 28 HNAA2008102000316 1 20081018 A 3350 1013073 MODULE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 937HA 50098 148 THE 5TH FROM FWD-AFT FLOOR AISLE EMERGENCY LIGHT INOP. REMOVED AND REPLACED FLOOR AISLE EMERGENCY LIGHT MODULE. OPS CH ECK GOOD. 2 H 7 2 4T RT A13NM 20081028 NM 2008 10 28 22AA20081003 1 20081019 A 2710 MECHANISM DOUG DC10 DC1040F 3023507 NM AILERON LACK OF LUBE A 22AA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SO 19 140WE 46920 UPON RETRACTING FLAPS 2 1/2 UNITS OF AILERON TRIM TO THE RT MUST BE USED TO KEEP WINGS LEVEL. PERFORMED AILERONS SYSTEM TEST IN ACCORDANCE WITH M/M 27-10-00. FOUND NORMAL, FLAP SYSTEM TEST IN ACCORDANCE WITH M/M 27-50-00. FOUND NORMAL SP OILER SYSTEM OPERATIONAL CHECK IN ACCORDANCE WITH M/M 27-60-00, NO DEFECTS NOTED. LUBRICATED I/B AND O/B AILERONS MECHA NISM IN ACCORDANCE WITH M/M 12-21-04. OPERATIONAL CHECK AILERONS, FLAPS AND SPOILERS SEVERAL TIMES, FOUND NORMAL. 2 L 7 3 4F RT A22WE 20081028 2008 10 28 IXXA080027O 4 20081021 A 3425 2587934801 COMPARATOR DOUG DC8 DC871F 302199D WP COCKPIT DEFECTIVE A IXXA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 11 828BX 87900 1416 45993 DURING CLIMBOUT FROM KTOL, CAPT'S RMI, GYRO FLAG, AND F/O'S GLIDESLOPE IN HSI, FLIGHT DIRECTOR IN ASI FLAG ALL IN VIEW. THE CREW RETURNED TO KTOL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED SMART BOX. OPERATIONAL CHECK GOOD IAW DC8 MAINTENANCE MANUAL 34-20-0, 34-23-20, 34-31-0. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 20081028 CE 2008 10 28 DXTA2008102203312 1 20081021 A 3230 LANDING GEAR CESSNA 680 680CE 2076811 CE MALFUNCTIONED E DXTA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 07 384QS 6800110 PUT GEAR DOWN, ONLY HAD NOSE GEAR LIGHT. ON GO AROUND BLEW DOWN GEAR PER CHECKLIST. 2 L 7 2 4F RC T00012WI 20081028 NM 2008 10 28 QXEA2008102201065 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4 - CORROSION ON SEAT TRACK NR 10 ON TOP AND IN THE CENTER OF THE TRACK FROM STA X1.000 - X10.000. REMOVED CORRO SION, FOUND OUT OF LIMITS REF RD8/4-53-884. REMOVED SEAT TRACK IAW DHC8 400 SRM 51-40-07. INSTALLED NEW SEAT TRACK IAW DHC8 Q400 SRM 51-40-07, 51-40-15, 51-20-10 AND 51-80-00. 2 H 7 2 4T RT A13NM 20081028 NM 2008 10 28 ASM2008F00005 1 20080913 A 2910 AE70970110 HOSE BOEING 777 7772Q8 1385238 NM GE GE90 GE9092B 30036 NE HYD SYSTEM DAMAGED W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 776AM 28692 900354 DURING TRANSIT CHECK, MAINT DETECTED DAMAGE AND HYDRAULIC LEAK ON SUPPLY HOSE ASSEMBLY TO RT ENGINE EDP. THE HOSE ASSY, PN AE70970110 WAS REMOVED AND REPLACED AND PERFORMED LEAK CHECK IAW AMM 29-11-05, NO LEAKS WERE FOUND. (K) 2 L 7 2 4F 4 F RT T00001SE E00049EN 20081028 NM 2008 10 28 QXEA2008102201066 1 20081002 A 5320 PANEL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX- C4- CORROSION AROUND SOME OF THE FASTENERS FOR PANEL 144LZ. REMOVED MINOR SURFACE CORROSION AS PER Q400 SRM 51-14- 00. ALODINED AND PRIMED AREA IAW Q400 SRM 51-25-10 AND 51-21-10. 2 H 7 2 4T RT A13NM 20081028 EU 2008 10 28 USAA920081888 1 20081013 A 2560 P2070003001 FLASHLIGHT AIRBUS 320 A320232 3930326 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 657AW 1083 FLT NR 71 ATL-PHX EMERGENCY EQUIPMENT. FLASHLIGHT AT FORWARD FLIGHT ATTENDANT SEAT INOPERATIVE. MX R&R THE FORWARD FLI GHT ATTENDANT FLASHLIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081028 2008 10 28 USAA920081887 4 20081013 A 2565 DHE1141 PROXIMITY SWITCH AIRBUS 320 A320231 3930325 EU ESCAPE SLIDE DEFECTIVE A USAA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 19 637AW 099 FLT 9 SJC-PHX EMERGENCY EQUIPMENT. DOOR 2L SLIDE INDICATION ON ECAM IS INTERMITTENT. MX R&R PROXIMITY SWITCH ON L2 DOO R. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081028 NM 2008 10 28 USAA920081891 1 20081013 A 5754 SKIN BOEING 737 737301 1384611 NM NR 6 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 345 23739 CLT Q3 MAJOR REPAIR NR 5030879 AND NR 03C40257009/005. NR 6 SLAT DELAMINATED ON OTBD EDGE OF TRAILING EDGE WEDGE. REPL ACED NR 6 SLAT IAW US AIRWAYS TASK CARD NR 03C40227004. 2 L 7 2 4F RT A16WE 20081028 WP 2008 10 28 AALA200802512 1 20080924 A 5320 7075T6 CUSP WEB DOUG DC9 DC982 3022082 WP BS 218 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 TUL-LT CUSP CRACKED AT STATION 218 UNDER NR 2 SEAT TRACK. AREA OF DISCREPANCY IS 3 INCHES BY 3 INCHES WITH A CRACK LENG TH OF 2 INCHES. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081028 EU 2008 10 28 USAA920081858 1 20080927 A 5320 D53472188202 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 CLT C7 MAJOR REPAIR NR 6062500. CORROSION ON FLOOR SUPPORT AT FR68 TO FR69, Y1190. REPLACED FLOOR SUPPORT AT FR68 TO F R69, Y1190 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081028 SO 2008 10 28 SIMA200829606 1 20081020 A 5320 14521725025 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 651AE 145422 DURING MBV INSPECTION FOUND AFT SERVICE DOOR SILL TO BE CORRODED. REPAIRED SILL BY REMOVING CORROSION AND INSTALLING A DOUBLER IAW EMB SRM 53-21-10 FIGURE 201. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081028 NM 2008 10 28 USAA920081886 1 20081013 A 5220 D5227917520200 PIN AIRBUS A319 A319132 3930340 NM ZONE 800 DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 814AW 1281 FLT 72 SEA-PHX EMERGENCY EGRESS SYSTEM RT OVERWING ESCAPE DOOR LATCH PIN WILL NOT LOCK IN EXTENDED POSITION. MX R&R THE RELEASE PIN AND SPRING. IAW AIRBUS MX MANUAL 52-21-11-000-003 AND 52-21-11-400-003. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081028 2008 10 28 SIMA200829607 4 20081013 A 3425 SWITCH EMB 145 EMB145LR 3260212 SO AVIONICS MASTER DIRTY A SIMA O OTHER G MULTIPLE FAILURE CR CRUISE 1 SW 21 928AE 14500911 ON FLIGHT 3830 DURING CRUISE CREW REPORTED, LOST VARIOUS INSTRUMENTS AND BOTH TRANSPONDERS. ADVISED ATC THEY WERE RVSM UNABLE AND STOPPED CLIMB AT FL260. CONTACTED MAINTENANCE AND COULD NOT RESOLVE PROBLEM. AFTER ABOUT 20 MINUTES DISCOV ERED AVIONICS MASTER NR 1 HAD RELEASED HALF WAY OUT WITH NO INDICATION SUCH AS THE SWITCH ILLUMINATING. RESETTING THE S WITCH RESTORED ALL INSTRUMENTS. AIRCRART REMOVED FROM SERVICE. CLEANED SWITCH AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081028 WP 2008 10 28 AALA200802473 1 20080930 A 1100 PLACARD DOUG DC9 DC982 3022082 WP EMERGENCY EXIT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 214AA 49162 EMERGENCY LIGHT EXIT MARKER PLACARD AT LT OVERWING DAMAGED. REPLACED EXIT MARKER PLACARD FOR EMERGENCY LIGHT AT LT OVER WING. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081028 WP 2008 10 28 AALA200802478 1 20080930 A 3350 LAMP DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 973TW 53623 LGA EMERGENCY LIGHT AT SEAT 19D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT A6WE 20081028 CE 2008 10 28 RU3A003 1 20081022 A 2700 540501514 CONTROL CABLE LEAR 60 60LEAR 5170707 CE LT WING CHAFED E RU3A K NONE O OTHER IN INSP/MAINT 1 SW 15 1600 PROBLEM ON 3 AIRCRAFT WITH EXCESSIVE WEAR, WHERE THE CABLES GO THROUGH THE PHENOLIC RUB STRIPS. THIS WAS FOUND DURING C ABLE REMOVAL TO FACILITATE OTHER MAINTENANCE, WHEN THE CABLES ARE INSTALLED THE WEAR AREAS CAN'T BE SEEN. THERE IS NO I NSPECTION REQUIRED FOR THAT AREA. THE CABLES ARE HARD TIME REPLACEMENT AT 2400 HOURS. 2 L 7 2 4F RT A10CE 20081028 NM 2008 10 28 USAA920081868 1 20081012 A 5320 654583469 STRAP BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753005/007. STABILIZER STRAP CRACKED AT BS 312 TO BS 328, RBL 32. REPLACED STABILIZER STRA P IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081028 WP 2008 10 28 AALA200802475 1 20080930 A 3350 MODULE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 214AA 49162 DFW EMERGENCY LIGHTS AT OVERHEAD AFT CABIN INOPERATIVE. REPLACED MODULE FOR EMERGENCY LIGHTS AT OVERHEAD AFT CABIN. SY STEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081028 EU 2008 10 28 USAA920081861 1 20080927 A 5320 D5311209120009 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C7 MAJOR REPAIR NR 6109619. CORROSION ON FLOOR SUPPORT BETWEEN FR16 TO FR20, Y1292. REPLACED FLOOR SUPPORT BETWEEN FR16 TO FR20, Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081028 WP 2008 10 28 AALA200802472 1 20080930 A 3350 SIGN DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 214AA 49162 EMERGENCY LIGHT EXIT MARKER PLACARD AT RT OVERWING DAMAGED. REPLACED EXIT MARKER PLACARD FOR EMERGENCY LIGHT AT RT OVER WING. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081028 EU 2008 10 28 USAA920081863 1 20080927 A 5320 D53471123202 SUPPORT AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C7 MAJOR REPAIR NR 6062496. CORROSION ON SUPPORT FRAME BETWEEN FR69 TO FR70, S24L, Y1732. REPLACED SUPPORT FRAME B ETWEEN FR69 TO FR70, S24L, Y1732. IAW A320 SRM 51-72-11 AND AIRBUS DRAWING NR D53470100. 2 L 7 2 4F RT A28NM 20081028 NM 2008 10 28 HALA2008102300823 1 20081023 A 8011 35054367 STARTER BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE RT ENGINE MALFUNCTIONED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM - RETURNED TO GATE. RIGHT ENGINE STARTER FAILED TO ACCELERATE PAST N2 10 PERCENT. MAINT REQUE STED TO EXAMINE PROBLEM. REMOVED AND REPLACED STATER ASSY PER AMM 80-11-01. OPS CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081028 WP 2008 10 28 AALA200802511 1 20080924 A 5347 GALLEY TRACK DOUG DC9 DC982 3022082 WP BS 218 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 TUL, GALLEY TIE DOWN SUPPORT AT CABIN SUBFLOOR CORRODED BEYOND SRM LIMITS. INSTALLED NEW GALLEY TIE DOWN SUPPORT PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081028 NM 2008 10 28 AALA200802482 1 20080919 A 5743 115A521110 TRUNNION BOEING 737 737823 13844CB NM RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 TUL RT MLG TRUNNION FITTING CORRODED AT LOWER OTBD HOLE OUTER FACE. AREA OF DISCREPANCY IS 2 INCHES BY 2 INCHES WITH A .142 INCH DEPTH. REMOVED CORROSION, TREATED, PRIMED, AND INSTALLED NEW BUSHING PER SRM 57-20-90-R2-2. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 UPS08653690 1 20081014 A 5320 212T34181 SUPPORT CHANNEL BOEING 767 76734AF 1385212 NM AFT CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 331UP 27757 INSPECTION TYPE:N/A APU DUCT SUPPORT CHANNEL CRACK FOUND AT STA 1153 TO 1175 LBL 75 AREA CRACK LENGTH .25 INCH APPROX. NEW CHANNEL REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20081024 NM 2008 10 24 UPS08653692 1 20081012 A 5315 141T5814136 STIFFENER BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 331UP 27757 INSPECTION TYPE:N/A MAIN DECK FLOORBEAM ATTACH STIFFENER AT STA 246 LBL 26 CRACK FOUND CRACK LENGTH .75 INCH APPROX. MA IN DECK STA 246 LBL 26 FLOORBEAM ATTACH STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20081024 NM 2008 10 24 SWAA085634 1 20081020 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085646 1 20081020 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085647 1 20081016 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 424WN 29828 FOUND EEPLS LIGHT COVER BROKEN AT ROW 11. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085657 1 20081018 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR LWR FWD CUTOUT FUSELAGE SKIN CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085666 1 20081021 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 22L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085681 1 20081021 A 5753 65C26320 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED HC1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED AT I/B FWD SIDE. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20081024 EU 2008 10 24 UPS08153701 1 20081015 A 5321 B5327085800000 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 140UP 0823 INSPECTION TYPE:1/3C MAIN CARGO DECK FLOORBOARD 241TN CRACKED. REPAIRED MAIN CARGO DECK FLOORBOARD 241TN REF A300-600 S RM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081024 EA 2008 10 24 COMA0860415 1 20081011 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 819CA 3332 7415 EMERGENCY FLOOR LIGHTING INOP FROM ROW 9 AFT. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK NR 4. 2 L 7 2 4F RT A21EA 20081024 NM 2008 10 24 08FDEA04438 1 20081020 A 5340 654531314 STRINGER CLIP BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 UPPER INTER FUSELAGE BS 600 STR 9R STRINGER CLIP OTBD LOWER RADIUS CRACKED. REMOVED STRINGER CLIP REF. SRM 51-30-02 P1, LOCATED AND DRILLED FASTENERS HOLES REF SRM 51-30-05 P1 INSTALLED STRINGER CLIP 65-45313-14 A45966 REF SRM 51-30-02 P1, APPLIED CORROSION INHIBITOR REF SRM 51-10-02 P14. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081024 WP 2008 10 24 08FDEA04409 1 20081017 A 5751 ARC047241 BRACE DOUG MD10 MD1010F 3022112 WP LT WING AILERON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 LEFT WING INBD AILERON BAY, VERTICAL TEE BRACE LOCATED AT XW 373 AND 22 INCHES AFT OF THE REAR SPAR HAS A CRACK TO THE B OTTOM OF THE TEE ANGLE. REMOVED CRACKED TEE ANGLE IAW SRM 51-33-01. LOCATED & DRILLED HOLES IN NEW ANGLE & INSTALLED IAW DWG ARC 0472 & SRM 51-33-01. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04408 1 20081017 A 5753 ARC21473 SKIN DOUG MD10 MD1010F 3022112 WP LT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 LEFT WING OTBD FLAP, INBD HINGE, AFT LOWER FAIRING IS CRACKED. REMOVED PANEL 535 JL IAW SRM 51-31-01. PANEL 535JL WAS CRACKED; WELDED PANEL 535JL IAW RS DPS 10.301 & DWG ARC 2147; REV " M ". WELS WAS CHECKED IAW DWG ARC 2147; REV " M " & DPS 4.707, NO CRACKS NOTED. ALODINED & PRIMED IAW SRM 51-21-01. RE-INSTALLED PANEL 535 JL IAW SRM 51-31-01. 2 L 7 3 4F RT A22WE 20081024 EU 2008 10 24 08FDEA04439 1 20081020 A 5347 A53278424202 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 677FE 791 MDCC SEAT TRACK 4L (Y1456) AT FRAME 60 HAS WORN SCALLOP .30 INCH WIDE BY .20 INCH LONG BY .043 INCH DEEP. REMOVED SEAT TRACK SECTION AT FRAME 60 TO 63 AND INSTALLED NEW SECTION AND SPLICE REPAIR IAW SRM 53-10-16 FIG 201 PG 207/208. 2 L 7 2 4F RT A35EU 20081024 EU 2008 10 24 08FDEA04440 1 20081020 A 5330 A53778019202 SKIN AIRBUS 300 A300F4605R 3930327 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 677FE 791 LT FUSELAGE EXTERIOR SKIN AT FRAME 38.2 STRINGER 40L HAS A GOUGE MEASURING 1/2 INCH BY 1 INCH BY .015 INCH DEEP. CUT OU T DAMAGED SKIN AND INSTALLED A REPAIR DOUBLER AND FILLER IAW A300-600 SRM 53-10-12 FIG 207 SHT 3. 2 L 7 2 4F RT A35EU 20081024 NE 2008 10 24 AALA200802446 2 20080926 A 7321 EEC BOEING 777 777223 1385213 NM RROYCE RB211 RB211TRENT89 NE NR 1 ENGINE FAULTY A AALA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SW 21 762AN 31479 51173 INFLIGHT T46/26SEP ORD TO LHR. NR 1 ENGINE HIGH ENGINE GAS TEMPERATURE INDICATION. CREW SHUT DOWN NR 1 ENGINE. LANDED YYZ WITHOUT INCIDENT. SINGLE ENGINE TIME 15 MINUTES. REPLACED ELECTRONIC ENGINE CONTROL. SYSTEM GROUND CHECKED NORMA L OPS. 2 L 7 2 4F 4 F RT T00001SE E00050EN 20081027 SW 2008 10 27 JIK2008F00003 1 20080703 A 2911 223002 ACCUMULATOR SWRNGN SA227 SA227AC 8780603 SW HYD SYSTEM FAILED E JIKA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 01 423MA AC636 AFTER TAKEOFF, BOTH HYDRAULIC PRESSURE LIGHTS CAME ON RIGHT AFTER GEAR RETRACTION. PILOT DECLARED AN EMERGENCY, CONDUCTE D AN EMERGENCY GEAR EXTENSION PROCEDURE, AND MADE A LANDING WITHOUT FURTHER INCIDENT. UPON EXAMINATION, IT WAS DISCOVERE D THAT THE HYDRAULIC ACCUMULATOR END CAP ON THE HYDRAULIC SIDE HAD EXPERIENCED A CATASTROPHIC METALLURGICAL FAILURE, RES ULTING IN SIGNIFICANT LOSS OF HYDRAULIC FLUID AND THEREFORE PRESSURE. THIS ACCUMULATOR IS AN "ON CONDITION" PART, WITH N O OVERHAUL REQUIREMENTS. THIS COMPANY HAS EXPERIENCED TWO SIMILAR FAILURES IN 2005 AND 2003 ON THIS MAKE AND MODEL OF A IRCRAFT, AND AN ADDITIONAL FAILURE OF THIS TYPE ON AC WHICH HAS AN ACCUMULATOR PN 22300-3. IT WOULD SEEM PRUDENT TO INST 2 L 7 2 4T RT A8SW 20081027 EU 2008 10 27 M7KA0803084356 1 20080901 A 5320 365A21384520 STOP UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE DOOR FRAME CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 852MH 201 4356 23147 FOUND CRACKED DURING ROUTINE INSPECTION. THIS PART IS ALSO DAMAGED BY UV RAYS OVER TIME MAKING IT BRITTLE AND PRONE TO C HIPPING AND CRACKING. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 EU 2008 10 27 M7KA0804084327 1 20080901 A 2913 350A35109222 PULLEY UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE HYD PUMP WORN E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 850MH 499 4327 23472 DURING ROUTINE 500 HOUR INSPECTION THE PULLEY SPINDLE ON WHICH THE INNER RACE OF THE BEARING IS PRESSFIT WAS FOUND VERY WORN WITH MORE THAN .10 INCH OF THE PROPER SPINDLE DIAMETER WORN AWAY AND SOME CORRESPONDING WEAR ON THE BEARING INNER R ACE AND WEAR ON THE HYDRAULIC PUMP DRIVE PULLEYS SPLINED COUPLING SLEEVE. THIS IS THE THIRD INSTANCE OF WHICH WE ARE AWA RE OF THIS DEFECT OCCURRING. THE BEARING ITSELF HAD NO APPARENT ROUGHNESS WHEN TURNED BY HAND. SUSPECT SOME PULLEYS OR P ERHAPS BEARINGS HAVE IMPROPER MACHINED DIAMETERS WHICH ALLOW THE INITIAL SLIPPAGE AND SUBSEQUENT CHATTERING DEVELOPS WHI CH REMOVES MATERIAL OVER TIME. THIS HAPPENED BETWEEN INSPECTIONS. BELT TENSION MUST BE RELEASED TO DETECT THIS DEFECT AS 1 G 7 2 3U 3 U H9EU E00054EN 20081027 EA 2008 10 27 SWIA200820194 1 20081015 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 958SW 7833 EMERGENCY EXIT LIGHT NEXT TO SERVICE DOOR INOP. FLT 6492, RELAMPED. 2 L 7 2 4F RT A21EA 20081027 SO 2008 10 27 SWIA200820196 1 20081019 A 5415 MOUNT EMB 120 EMB120ER 3260203 SO LT MLG HYD PACK CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 582SW 120350 LEFT MLG HYDRAULIC PACK LOWER O/B MOUNT CRACKED. C-CHECK, REPLACED MOUNT. 2 L 7 2 4T RT A31SO 20081027 EA 2008 10 27 SWIA200820197 1 20081017 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 821SK 15109 TWO OVERHEAD CEILING EMERGENCY LIGHTS INOP. FLT 3658, RELAMPED. 2 L 7 2 4F RT A21EA 20081027 NM 2008 10 27 DHLA20087521022A 1 20081022 A 5753 WEDGE BOEING 727 727223 1384074 NM LT WING TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 752DH 22466 LEFT WING INBD T/E FLAP ASSY INBD MID FLAP T/E APPROX 64 INCHES FROM OUTBOARD EDGE HAS AREA OF DELAMINATION AT PREVIOUS REPAIR. 337 FILED AND MP9 NR 26944 FILED. ALL REPAIR WORK COMPLIED WITH IAW BOEING SRM 51-40-20 PARA 7, 8, 9, 10, 14, 20, 22. AREA OF DAMAGE WAS REMOVED INCLUDING CORE. NEW CORE HOT BONDED IN T/E. REPAIR FILLER AND DOUBLER FABRICATED A ND HOT BONDED TO T/E. PO NR FOR MATERIAL 9911845 AND 9007617. MATERIAL USED 5052-4-4 3/16 INCH CORE. FILLER AND DOUBL ER 2024 T3 .016 INCH AND .020 INCH. THIS IS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 DL757081384 1 20081020 A 5320 146N543144 SUPPORT BOEING 757 757232 1384965 NM BS 1530 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 CORROSION ON SUPPORT STATION 1530 TO STATION 1560 RT. REPAIRED ON NR 00040 PER 53-00-02. 2 L 7 2 4F RT A2NM 20081027 NM 2008 10 27 DL757081385 1 20081020 A 5340 146N54432 STRINGER CLIP BOEING 757 757232 1384965 NM BS 1500 S29R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 CORROSION ON SUPPORT CLIP AT STRINGER 1500 AND STRINGER 29R. REPAIRED ON ATS 00102 PER 51-40-02. 2 L 7 2 4F RT A2NM 20081027 NM 2008 10 27 DL757081386 1 20081020 A 5347 146N545841 CARGO TRACK BOEING 757 757232 1384965 NM BS 1475 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 CORROSION CARGO TIE DOWN STATION 1475 RBL 12. REPAIRED PER 51-40-02 ON NR 00130. 2 L 7 2 4F RT A2NM 20081027 NM 2008 10 27 DL757081387 1 20081020 A 5320 HFAB53AN011 STIFFENER BOEING 757 757232 1384965 NM BS 660 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 VERTICAL STIFFENER CRACKED AT STA 660 RBL 25. REPAIRED ON NR 00097 PER 51-20-01. 2 L 7 2 4F RT A2NM 20081027 NM 2008 10 27 DLM88081390 1 20081020 A 5330 593600419 SKIN DOUG MD88 MD88 3023688 NM FS 636, L29L/R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951DL 49882 FUSELAGE SKIN CORRODED AT FS 636, LONGERON 29L - 29R. DAMAGED SKIN CUTOUT AND EXTERNALLY REINFORCED WITH A DOUBLER AND TRIPLER. 2 L 7 2 4F RT A6WE 20081027 NM 2008 10 27 DLM88081391 1 20081020 A 5531 5911394504 SPAR DOUG MD88 MD88 3023688 NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 941DL 49814 VERTICAL STABILIZER FRONT SPAR RT CHORD CRACKED THROUGH THREE FASTENER HOLES AT ZFS=52. DAMAGE CUT OUT OF FLANGE AND RE INFORCED WITH A REPAIR ANGLE. 2 L 7 2 4F RT A6WE 20081027 EA 2008 10 27 SWIA200820199 1 20081015 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 915SW 7615 EMERGENCY LIGHT AT ROW 10 INOP. FLT 6307, RELAMPED. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 SWIA200820200 1 20081013 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA LAVATORY SMOKE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 932SW 7714 FLT 6586 - DURING TAKEOFF, RECEIVED "SMOKE TOILET" CAUTION MESSAGE. PERFORMED HIGH ENGINE POWER RUNS ON BOTH ENGINES, N O SMOKE AND OPERATION NORMAL. RAN PACKS WITH ENGINE BLEEDS, NO SMOKE NOTED. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 SWIA200820202 1 20081016 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 935SW 7725 FLT 6103 - EMERGENCY LIGHT IN OVERHEAD ROW 10 INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 SWIA200820203 1 20081015 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 973SW 7949 FLT 6664 - EMERGENCY FLOODLIGHT ROW 2 INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 SWIA200820205 1 20081017 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT MISSING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 938SW 7741 FLT 6014 - OVERHEAD EXIT SIGN IN CABIN MISSING RED/LENS COVER. REPLACED RED/LENS COVER. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 QXEA200800932 1 20080817 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK L/H INBD SEAT TRACK NR 5 HAS CORROSION AT STA X1 TO X20 ON OTBD FLANGE AND ATTACH ANGLE FOR FLOOR PANEL 131 CZ. TRACK FOUND TO BE OUT OF LIMITS AS PER RD 8/4-53-884. REMOVED TRACK AND INSTALLED NEW SEAT TRACK REF Q400 SRM 51-4 0-15 AND 51-42-05. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 QXEA200800912 1 20080817 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK LT INBD SEAT TRACK NR 6 HAS CORROSION AT X181 AND X196. BLENDED CORROSION REF 8/4-53-884 PG 6 STEP 1. MAX MATERIAL REMOVED NEGLIGIBLE AND .014" RESPECTIVELY. BLENDS WITHIN LIMITS. HFEC INSP IAW RD 8/4-53-884, D8-400 NDTM PA RT 6, 51-00-01, NO CRACKS NOTED. TREATED BLENDED AREA REF RD8/4-53-884. 2 L 7 2 4F RT A21EA 20081027 NM 2008 10 27 KCSA081528 1 20081012 A 5230 SKIN BOEING 747 747249F 1384849 NM CARGO DOOR CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 AFT CARGO DOOR SKIN INNER DOUBLER CORRODED AT AFT LOWER CORNER BS 1915. 2 L 7 4 4F RT A20WE 20081027 WP 2008 10 27 AALA200802405 1 20080921 A 2150 A/C PACK DOUG DC9 DC982 3022082 WP CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 410AA 49321 SAT INFLIGHT T620/21SEP. CREW REPORTED SMOKE IN CABIN WITH HEAVY SMOKE IN AFT CABIN DURING CLIMB. RETURNED TO SAT AND LANDED WITHOUT INCIDENT. UPON LANDING SMOKE DISSIPATED. FOUND RESIDUAL OIL FROM OVERNIGHT APU WORK. REPLACED BOTH COA LESCER BAGS AND ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081027 NM 2008 10 27 KCSA081533 1 20081013 A 5420 STIFFENER BOEING 747 747249F 1384849 NM NR 3 NACELLE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 NR 3 PYLON NAC STA 248 AFT, LOWER, I/B SIDE VERTICAL STIFFENER DAMAGED. 2 L 7 4 4F RT A20WE 20081027 EA 2008 10 27 QXEA200800894 1 20080728 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK LT OTBD SEAT TRACK HAS CORROSION AT STA X841 TO X860. BLENDED CORROSION IAW REO 670-53-00-013 SHT 2 STEPS 1-2. MAX MATERIAL REMOVED WAS .005". BLEND IS WITHIN LIMITS IAW REO 670-53-00-013 TABLE 1. ALODINED IAW SRM 51-21-11. 2 L 7 2 4F RT A21EA 20081027 NM 2008 10 27 QXEA2008102301082 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4- NR 6 SEAT TRACK HAS CORROSION INSIDE THE CHANNEL AT STA X206. BLENDED OUT CORROSION IAW RD 8/4-53-884, WITHIN LIMITS PER RD 8/4-53-884. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ETCHED AND ALODINED AREA IA W RD 8/4-53-884. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 QXEA2008102301083 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4- LT INBOARD SEAT TRACK HAS CORROSION INSIDE THE CHANNEL FROM STA X449 TO X464. BLENDED OUT CORROSION IAW RD 8/ 4-53-884, WITHIN LIMITS PER RD 8/4-53-884. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ETCHED AND ALODINED AREA IAW RD 8/4-53-884. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 QXEA2008102301085 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4- LT INBOARD SEAT TRACK HAS CORROSION INSIDE THE CHANNEL FROM STA X488 TO X500. BLENDED OUT CORROSION IAW RD 8/ 4-53-884, WITHIN LIMITS PER RD 8/4-53-884. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ETCHED AND ALODINED AREA IAW RD 8/4-53-884. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 QXEA2008102301093 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4- NR 3 SEAT TRACK HAS CORROSION IN THE BASE BETWEEN APPROX STA X570.500 TO X664.500. BLENDED OUT CORROSION IAW RD 8/4-53-884, WITHIN LIMITS PER RD 8/4-53-884. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ETCHED AND ALODINED AREA IAW Q400 SRM 51-21-10. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 QXEA200800978 1 20080831 A 5320 THRESHOLD BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 414QX 4061 PDX - C-CHECK, MCD THRESHOLD HAS CORROSION AROUND SCREW HOLES. REMOVED THRESHOLD BY DRILLING OUT RIVETS. DRILLED UP NE W THRESHOLD AND INSTALLED RUB STRIP IAW 51-40-07 AND 51-42-05. INSTALLED NEW THRESHOLD WITH SEALANT REF SRM 51-42-05. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 QXEA2008102201087 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX-C4- LT INBOARD SEAT TRACK HAS CORROSION INSIDE THE CHANNEL FROM STA X509 TO X529. BLENDED OUT CORROSION FOUND WITHI N LIMITS PER RD8/4-53-884. HFEC INSPECTED IAW Q400 NDTM PART 6 51-00-01, NO CRACKS NOTED. ETCHED AND ALODINED AREA IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 HALA0800822 1 20081022 A 7720 32916782 VALVE BOEING 717 717200 1383700 NM NR 2 ENGINE FAULTED A HALA D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 475HA 55121 BTB - NR 2 ENGINE HOT START, MAX TGT 700 DEG. INTERROGATED NR 2 EEC FOUND STARTER AIR VLV FAULT. START TEMP WITHIN LIM ITS PER MM 71-00-05. REPLACED START VLV PER M/M 80-11-03, OPS CHECK LEAK CHECK GOOD. P/N 3291678-2, S/N ON 182C OFF 37 8. 2 L 7 2 4F TR A6WE 20081027 EU 2008 10 27 USAA920081718 1 20080920 A 5315 D5347219020300 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 PIT - S4 -MAJOR REPAIR, LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT -Y765, AFT OF FR 64. REPLACED FLOORBEAM AT -Y765 , AFT OF FR 64 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081027 NM 2008 10 27 USAA920081709 1 20080917 A 5320 65528942 INTERCOSTAL BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - C18 - MAJOR REPAIR, INTERCOSTAL CRACKED BS 520, WL 208, RBL 2. REPLACED INTERCOSTAL BS 520, WL 208, RBL 2 IAW B73 7 SRM 51-40-05-0G & 51-40-04-0G. 2 L 7 2 4F RT A16WE 20081027 NM 2008 10 27 USAA920081710 1 20080917 A 5320 65528941 INTERCOSTAL BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - C18 - MAJOR REPAIR, INTERCOSTAL CRACKED BS 540, LBL 2. REPLACED INTERCOSTAL BS 540, LBL 2 IAW B737 SRM 51-40-05-0 G & 51-40-04-0G. 2 L 7 2 4F RT A16WE 20081027 EU 2008 10 27 USAA920081715 1 20080920 A 5315 D5347219020300 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 PIT - S4 -MAJOR REPAIR, CORROSION ON FLOORBEAM BETWEEN FR 64 & FR 66, Y765. REPLACED FLOORBEAM BETWEEN FR 64 & FR 66, Y765 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081027 NM 2008 10 27 USAA920081726 1 20080901 A 5311 6546555 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 SAL - C17 -MAJOR REPAIR, FRAME AT BS 867 HAS A .395 INCH CRACK BETWEEN S8L & S9L AND A .489 INCH CRACK BETWEEN S8R & S9R . REPAIRED FRAME AT BS 867 BETWEEN S8L & S9L, ALSO BETWEEN S8R & S9R IAW AMERICA WEST AIRLINES TASK CARD NR M1C53002. 2 L 7 2 4F RT A16WE 20081027 NM 2008 10 27 USAA920081728 1 20080901 A 5311 6545593 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 SAL - C17 -MAJOR REPAIR, FRAME AT BS 500A HAS A .451 INCH CRACK BETWEEN S8L & S9L. REPAIRED FRAME AT BS 500A BETWEEN S8 L & S9L IAW AMERICA WEST AIRLINES TASK CARD NR M1C53002. 2 L 7 2 4F RT A16WE 20081027 NM 2008 10 27 USAABB08153 1 20080921 A 5240 COUNTERBALANCE BOEING 767 7672B7 1385107 NM R1 DOOR OUT OF ADJUST A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AY 26847 ATH - THE FWD SERVICE DOOR, R1, CANNOT BE OPENED BY AN INDIVIDUAL CABIN CREW MEMBER. MX PLACED THE R1 DOOR ON MEL. ADJ USTED THE R1 DOOR COUNTERBALANCE SYSTEM. OPS CHECK OK. 2 L 7 2 4F RT A1NM 20081027 2008 10 27 USAABB08152 4 20080921 A 2565 BPS73 POWER SUPPLY BOEING 767 767201 1385125 NM EVAC SLIDE DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 246AY 23898 PHL - THE LT SLIDE, RT SPOILER SQUIB TEST FAILED TO ILLUMINATE. MX REPLACED THE LT , OFF-WING ESCAPE SYSTEM EMERGENCY B ATTERY POWER SUPPLY ASSEMBLY. OPS CHECK OK. 2 L 7 2 4F RT A1NM 20081027 2008 10 27 USAA920081730 4 20080923 A 2565 AD31517417 SLIDE AIRBUS 320 A320232 3930326 EU CABIN MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 648AW 770 FLT NR 220 - LAS, EMERGENCY LIGHT TEST, EPSU FAILED ON RT AFT EMERGENCY ESCAPE SLIDE. MX REMOVED AND REPLACED THE RIGHT AFT EMERGENCY ESCAPE SLIDE 2 L 7 2 4F RT A28NM 20081024 NM 2008 10 24 SWAA085632 1 20081012 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 FOUND L1 DOOR EGRESS LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085644 1 20081020 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED BS 867, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085663 1 20081021 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081024 EU 2008 10 24 UPS08153709 1 20081014 A 5321 B5327076400000 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 140UP 0823 INSPECTION TYPE:1C3C MAIN CARGO DECK FLOORBOARD 252NM HAS FIELD REPAIR. REPAIRED MAIN CARGO DECK FLOORBOARD 252NM REF A 300-600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081024 WP 2008 10 24 AALA200802516 1 20080925 A 5320 7075T6 CUSP WEB DOUG DC9 DC982 3022082 WP BS 1211 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 LT CUSP SHEET CRACKED AT STATION 1211 UNDER NR 2 SEAT TRACK. AREA OF DISCREPANCY IS 2 INCHES BY 3 INCHES. CRACK LENGTH IS 1 INCH. REMOVED DAMAGED AREA AND INSTALLED CUSP SHEET REPAIR PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081024 NM 2008 10 24 AALA200802404 1 20080921 A 3350 P4010051112 MODULE BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 695AN 26975 DFW SEAT MOUNTED EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK AND CHARGER FOR SEAT MOUNTED EMERGENCY LIGHTS AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081024 NM 2008 10 24 AALA200802403 1 20080921 A 3350 LAMP BOEING 737 737823 13844CB NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 932AN 29530 DFW EMERGENCY EXIT SPOT LIGHT AT SEAT 13A INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SPOT LIGHT AT SEAT 13A. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081024 EA 2008 10 24 COMA0860421 1 20081012 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS FAILED A COMA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 588SW 22314 7069 EMERGENCY FLOOR LIGHTS ROW 8 AFT INOP. R&R EMERGENCY BATTERY PACK NR 4. 2 L 7 2 4F RT A21EA 20081024 WP 2008 10 24 AALA200802461 1 20080929 A 3260 833704 PROXIMITY SENSOR DOUG DC9 DC983 3022083 WP RT MLG INOPERATIVE A AALA L ABORTED APPROACH N FALSE WARNING DE DESCENT 1 SW 21 567AM 53293 LAX INFLIGHT T1407/29SEP. CREW REPORTED RT RED MAIN LANDING GEAR WARNING REMAINED ON AFTER GEAR EXTENDED. EXTENDED GEA R MANUALLY AND PERFORMED FLY BY. LANDED LAX WITHOUT INCIDENT. REPLACED RT GEAR PROXIMITY SENSOR. SYSTEM GROUND CHECKE D NORMAL OPS. 2 L 7 2 4F RT A6WE 20081024 WP 2008 10 24 AALA200802517 1 20080925 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 CORROSION ON LOWER SURFACE OF LT HAND CUSP AT AFT CABIN BETWEEN STATIONS 1287 AND 1309 IS BEYOND SRM LIMITS. INSTALLED NEW CUSP PER SRM 53-05-00. 2 L 7 2 4F A6WE 20081024 WP 2008 10 24 AALA200802520 1 20080926 A 5320 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 CORROSION IN SEVERAL LOCATIONS OF CARGO DOOR BEAM IN AFT CARGO AT STATION 1155 TO 1211. AREA OF DISCREPANCY IS 1 INCHES BY 48 INCHES. INSTALLED DOOR BEAM DOUBLER PER AARD 53-10-00-3. 2 L 7 2 4F A6WE 20081027 EU 2008 10 27 M7KA0708084290 1 20080804 A 6220 BUSHING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE STARFLEX LOOSE E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 848MH 500 M3043 4290 23460 DURING ROUTINE INSPECTION A STAR ARM END BUSHING WAS FOUND LOOSE. STARFLEX REMOVED FOR REPAIR AND SERVICEABLE STARFLEX I NSTALLED. THIS IS A VERY COMMON FAILURE RECENTLY FOR THIS PART. SUSPECT THAT AN ADHESIVE FAILURE IS THE PROBLEM THAT MAY BE HEAT RELATED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 EU 2008 10 27 M7KA0825084313 1 20080901 A 6730 PICKUP UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ROTOR RPM INTERMITTENT E M7KA O OTHER N FALSE WARNING CR CRUISE 1 WP 19 849MH 4313 23458 PILOT REPORTS THAT HE HAD INTERMITTENT LOW ROTOR RPM WARNING SIGNALS WITH NORMAL ROTOR SPEED INDICATIONS. THE MAGNETIC P ICKUP HAD A LOW ROTOR WARNING CIRCUIT COB. CONTINUITY PROBLEM. A NEW SENSOR WAS INSTALLED AND NO FURTHER DEFECT WAS REPO RTED. SUGGEST A MORE ROBUST SENSOR BE DESIGNED AS THE COIL WIRES ARE HAIR THIN AND FAIL ROUTINELY. PERHAPS EVEN AN OPTIC SENSOR WOULD BE MORE RELIABLE. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 NM 2008 10 27 DHLA080904001 1 20080904 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN AT BS 700 S-8L FRAME WITH DOUBLE HOLE. REPAIRED FUSELAGE FRAME SECTION AT BS 700 BETWEEN S-6L AND S-9L IAW B727 SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 20081027 NM 2008 10 27 QXEA200800971 1 20080831 A 5320 RIVET BOMBDR DHC8 DHC8402 1390042 NM PANEL LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 414QX 4061 PDX - C-CHECK, UPPER APERTURE FOR PANEL 263CL HAS 2 LOOSE RIVETS IN THE FWD UPPER CORNER. REMOVED AND REPLACED RIVETS I AW Q400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 QXEA2008102301139 1 20081017 A 3230 468433 PIVOT BOMBDR DHC8 DHC8402 1390042 NM MLG MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 19 428QX 4160 SEA - BOTH MAIN LANDING GEAR CYCLED AT APPROX 20,000 FEET AND 280 KTS. PERFORMED ALT GEAR EXTENSION CHECKLIST. ALT GEA R EXTENSION WAS SUCCESSFUL. LANDED WITHOUT INCIDENT. TOWED TO GATE. FERRY TO PDX. ADJUSTED LGDRCL AND RGDRCL PROX SE NSOR. REPLACED LT MLG AFT DOORS LINK MECHANISM. C/W OPERATIONAL TEST OF THE LG EXT AND RET. OPS TEST GOOD. NO OTHER DEFECTS NOTED. CHECK FLIGHT GOOD. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 QXEA2008102301076 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX-C4- RT INBOARD SEAT TRACK HAS CORROSION INSIDE THE CHANNEL AT STA X480. BLENDED CORROSION IAW RD 8/4-53-884, BLEND WITHIN LIMITS IAW RD 8/4-53-884. HFEC INSPECTED IAW 1-84-7A, PART 6, 51-00-02, NO CRACKS NOTED. ETCHED AND ALODINED AR EA IAW RD 8/4-53-884. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 QXEA2008102301077 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4- RT INBOARD SEAT TRACK HAS CORROSION INSIDE THE CHANNEL AT STA X509 TO X529. BLENDED CORROSION IAW RD 8/4-53-8 84, WITHIN LIMITS PER RD 8/4-53-884. HFEC INSPECTED IAW 1-84-7A PART 6, 51-00-02, NO CRACKS NOTED. ETCHED AND ALODINED AREA IAW RD 8/4-53-884. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 QXEA2008102301079 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4- RT INBOARD SEAT TRACK HAS CORROSION INSIDE THE CHANNEL AT STA X547.0 TO X559.0. BLENDED CORROSION IAW RD 8/4- 53-884, WITHIN LIMITS PER RD 8/4-53-884. HFEC INSPECTED IAW 1-84-7A, PART 6, 51-00-02, NO CRACKS NOTED. ETCHED AND ALO DINED AREA IAW RD 8/4-53-884. 2 H 7 2 4T RT A13NM 20081027 2008 10 27 DXTA2008101703308 4 20081016 A 2210 AUTOPILOT SYS AMD FALC50 FALCON2000 2730170 NM MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 236QS 136 AUTOPILOT DISCONNECTED 6 TIMES IN 30 MINUTES. 2 L 7 2 4F RT A50NM 20081027 CE 2008 10 27 DXTA2008101703309 1 20081016 A 3210 LANDING GEAR CESSNA 750 750 2076810 CE MALFUNCTIONED E DXTA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 07 900QS 7500123 LANDING GEAR BUMP IN THE NIGHT MULTIPLE TIMES IN CLIMB, IN CRUISE, IN DESCENT ONCE. 2 L 7 2 4J RT T00007WI 20081027 NM 2008 10 27 USAA920081736 1 20080915 A 5315 654583470 STRAP BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - C18 - MAJOR REPAIR, 2 CRACKS ON FLOORBEAM STABILIZER STRAP AT BS 328, BL 0. REPAIRED FLOORBEAM STABILIZER STRAP A T BS 328, BL 0 IAW B737 SRM 53-10-51-2R4 2 L 7 2 4F RT A16WE 20081027 NM 2008 10 27 QXEA200800967 1 20080831 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 414QX 4061 PDX - C-CHECK, RT INBOARD SEAT TRACK NR 16 IS CORRODED AT X678, AND X683. BLENDED SEAT TRACK REF RD 8/4-53-884. FOUND OUT OF LIMITS. REMOVED TRACK AND INSTALLED NEW TRACK IAW DHC8 400 SRM 51-42-05 AND 51-40-15. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 USAA920081720 1 20080901 A 5311 6546526 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 SAL - C17 -MAJOR REPAIR, FRAME AT BS 400 HAS A .475 INCH CRACK BETWEEN S8L & S9L AND A .481 INCH CRACK BETWEEN S8R & S9R . REPAIRED FRAME AT BS 400 BETWEEN S8L & S9L, ALSO BETWEEN S8R & S9R IAW AMERICA WEST AIRLINES TASK CARD NR MIC53002. 2 L 7 2 4F RT A16WE 20081027 NM 2008 10 27 USAA920081703 1 20080821 A 5320 6545774 PLATE BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 SAL - C19 - MAJOR REPAIR, CRACK ON SUPPORT PLATE AROUND POTABLE WATER SERVICE PANEL BS 947.5, S25L. REPAIRED SUPPORT PL ATE AROUND POTABLE WATER SERVICE PANEL BS 947.5, S25L IAW B737 SRM 51-40-02 & BOEING DRAWING NR 65-51626. 2 L 7 2 4F RT A16WE 20081027 NM 2008 10 27 USAA920081708 1 20080918 A 5540 D5537131800900 HINGE FITTING AIRBUS A319 A319132 3930340 NM RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 813AW 1223 SAL - BC6 - MAJOR REPAIR, EXCESSIVE PLAY AT RUDDER HINGE FITTING NR 2. REPLACED RUDDER HINGE FITTING NR 2 IAW A319 AMM 55-36-41. 2 L 7 2 4F RT A28NM 20081027 NM 2008 10 27 USAA920081733 1 20080822 A 5330 6548500219 SKIN BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN - C18- MAJOR REPAIR, 2 CRACKS IN FUSELAGE SKIN ABOVE L1 DOOR CUTOUT UPPER FWD CORNER BS 312, AT S7L & S8L. REPAIRED FUSELAGE SKIN ABOVE L1 DOOR CUTOUT UPPER FWD CORNER BS 312, AT S7L & S8L IAW US AIRWAYS EA NR 130115. 2 L 7 2 4F RT A16WE 20081027 NM 2008 10 27 USAA920081719 1 20080917 A 5754 65C26601198 SKIN BOEING 737 7373G7 138447J NM L/E SLAT DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - C18 - MAJOR REPAIR, NR 6 SLAT DISBONDED ON UPPER SURFACE AT SLAT STA 326.80 TO 329.5. REPAIRED NR 6 SLAT AT SLAT STA 326.8 TO 329.5 IAW B737 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 20081027 NM 2008 10 27 USAA920081711 1 20080917 A 5340 69414372 STRINGER CLIP BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - C18 - MAJOR REPAIR, STRINGER TIE CLIP CRACKED BS 663.75, S10R. REPLACED STRINGER TIE CLIP BS 663.75, S10R IAW B73 7 SRM 51-40-02-0G. 2 L 7 2 4F RT A16WE 20081027 EU 2008 10 27 USAA920081713 1 20080917 A 5320 SUPPORT ANGLE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 PIT - S4 - MAJOR REPAIR, LEVEL 2 GALVANIC CORROSION ON SUPPORT ANGLE AT L2 DOOR SILL AFT DOOR FRAME. REPLACED SUPPORT A NGLE AT L2 DOOR SILL AFT DOOR FRAME IAW SRM 53-41-14 REPAIR NR 5. 2 L 7 2 4F RT A28NM 20081028 EA 2008 10 28 2008FA0000670 2 20081010 A 7310 3011849 FUEL LINE BEECH 90 E90 1152914 CE PWA PT6 PT6A28 EA RT ENGINE CRACKED E VQMA E J ENGINE SHUTDOWN DUMP FUEL K FLUID LOSS IN INSP/MAINT 1 NM 03 379VM 20 20 LW27 PCE50947 WHILE PERFORMING ENGINE RUNS FOR RIGHT ENGINE FLOW PACK CHANGE FOUND FUEL LEAK FROM FUEL LINE FROM FCU TO TOP OF START C ONTROL UNIT. FITTING CRACKED ABOVE SCU. REMOVED CRACKED FUEL LINE FROM FCU TO TOP OF START CONTROL UNIT. INSTALLED OV ERHAULED LINE P/N 3011849 FROM DALLAS AIRMOTIVE. PERFORMED LEAK AND OPERATIONAL CHECKS SATISFACTORY. WORK ACCOMPLISHED IN REF TO P&W PT6A-28 MAINT MANUAL CHAPTER 73-10-03. LESS THAN ONE MONTH AND 20 HOURS LATER SAME FUEL LINE CRACKED AGA IN, IN SAME PLACE. REMOVED AND REPLACED CRACKED FUEL LINE BETWEEN THE FCU AND THE SCU OF RT ENGINE. P/N 3011849, OVERH AULED BY DALLAS AIRMOTIVE, S/N N/A, SEE 8130-3 DATED 9/18/2007. PERFORMED LEAK CHECKS SATISFACTORY. SAFTIED BOTH B-NUT 1 L 7 2 3T 4 T 3A20 E4EA 20081028 NE 2008 10 28 IXX2008F00097 2 20080916 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE NR 2 FLAMED OUT A IXXA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 11 823BX 46064 DURING CRUISE, AT 36,000 FT WITH POWER REDUCTION NR 2 ENGINE FLAMED OUT WITH 1-2 PSI OIL PRESSURE ATTEMPTED INFLIGHT RES TART, NO FUEL FLOW AND NO IGNITION. THE CREW PERFORMED INFLIGHT ENGINE SHUTDOWN PROCEDURE. THE CREW LANDED WITHOUT FURTH ER INCIDENT. MAINT INSPECTED NR TWO ENGINE, NO DEFECTS NOTED. RAN ENGINE AT IDLE SETTING, ALL INDICATIONS NORMAL, TAXI A CFT AND PERFORMED HIGH POWER RUN WITH TWO DIFFERENT POWER ASSURANCE 55 PERCENT SETTING AND 70 PERCENT SETTING, NO DEFECT `S NOTED. MAINT INSPECTED TANK AND FUEL PUMP, NO DEFECTS NOTED. OPS CHECK GOOD IAW MM 71-00-00, 73-11-00, MM 28-22, ERH 70.01.01-07, ERH 91.04.4, 91.01.6. ACFT WAS RETURNED TO SERVICE. (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 20081028 SO 2008 10 28 GUU2008F00061 1 20080915 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 268AS 120202 DURING SCHEDULED ROUTINE MAINT DISCOVERED NR 2 EMERGENCY LIGHT BATTERY PACK INOPERATIVE. RECHARGED NR 2 EMERGENCY LIGHT BATTERY PACK. (K) 2 L 7 2 4T RT A31SO 20081028 CE 2008 10 28 GUU2008F00062 1 20080914 A 5220 DOOR BEECH 1900 1900D 1154162 CE EMERGENCY EXIT LACK OF LUBE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87551 UE206 DURING SCHEDULED ROUTINE MAINT DISCOVERED SEAT 6F EMERGENCY EXIT HARD TO OPEN. LUBED EMERGENCY EXIT. OPS CHECK GOOD. (K ) 2 L 7 2 4T RT A24CE 20081028 2008 10 28 IXXA080028O 4 20081021 A 3497 WIRE DOUG DC8 DC871F 302199D WP SMART BOX BROKEN A IXXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 11 828BX 87900 1416 45993 DURING TAKEOFF FROM KTOL F/O'S FLIGHT DIRECTOR FLAG IN ADI AND GYRO FLAG CAME IN VIEW. THE CREW REJECTED TAKEOFF AND RE TURNED TO BLOCKS. MAINTENANCE SMART BOX WIRE NUMBER 2TN49B22 BROKEN AT R50-972 PIN 35. MAINTENANCE REPAIRED WIRE 2TN49 B22. OPERATIONAL CHECK GOOD IAW DACO DC8 MAINTENANCE MANUAL 34-20-0. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 20081028 WP 2008 10 28 GLQ2008F00000 1 20080911 A 2700 AN365428 NUT HUGHES 269 269C 4470504 WP PULLEY DAMAGED E GLQA O OTHER O OTHER NR NOT REPORTED 1 NM 11 6143K 1096 S1750 ROUTINE INSPECTION OF TRANSIENT ACFT REVEALED BOTH UPPER PULLEY FWD BEARING RETAINER CAP ATTACH BOLT NUTS LOOSE-APPROX Q .5 THREADS ONLY ENGAGED. THESE WERE SERVICEABLE USED NUTS. THREAD MARKINGS NOTED IN LOCK AREA. NUTS STILL EXHIBIT LOCKIN G CAPABILITY. FRAME ASSY FOUND WORN AND LOOSE AT BEARING RECESSES. MFG NOTIFIED MANDATORY REPLACEMENT ORDERED FOR FRAME ASSY, UPPER AND LOWER PULLEY FRAME BEARING ASSEMBLIES. INSPECTION REQUIRED FOR TRANSMISSION PINION SHAFT TIR, BEARING J OURNALS AND SPLINES WORN BEYOND LIMITS. LOWER PULLEY INNER SPLINES WORN DRIVE SPLINED COUPLING, UPPER PULLEY BEARINGS, S PRAGE CLUTCH OR AFT PINION NUT. TRANSMISSION PINION TOTAL INDICATOR RUN OUT GOOD. =0001" TIR. (K) 1 G 7 1 3O 4H12 20081028 SO 2008 10 28 SIMA200829601 1 20081018 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 642AE 5000 145193 DURING A MBV INSPECTION THE CARGO DOOR SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CARGO DOOR SILL. POSITIONED NEW SILL AND DRILLED. REPAIR DONE IAW EMB SRM (SRM EMB-145/1142 REV 40) CHAPTERS 51-20-03 AND 51-40-02. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081028 EU 2008 10 28 SIMA200829602 1 20081019 A 5347 7253725191 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 400BR 5000 340B400 DURING A HMBV INSPECTION THE SEAT TRACK AT BL 0.00 WAS FOUND TO BE CORRODED. REMOVED THE SEAT TRACK AND CUT, CLEANED AL ODINED AND PRIMED ALL FASTENER HOLES. REPAIR DONE IAW SAAB SRM (SRM 72LKS3079 REV 50) CHAPTER 53-70-60. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4T RT A52EU 20081028 SO 2008 10 28 SIMA200829603 1 20081020 A 5320 14532636 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 651AE 145422 DURING IMBV INSPECTION FOUND LEFT OMEGA BEAM TO BE CORRODED JUST FORWARD OF FRAME 29. REPAIRED OMEGA BEAM BY CUTTING OU T DAMAGED AREA AND INSTALLING A DOUBLER IAW IMB SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081028 WP 2008 10 28 AALA200802515 1 20080924 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 TUL-CORROSION ON NR 2 GALLEY TIE DOWN SUPPORT FITTING. REPLACED NR 2 GALLEY SUPPORT FITTING PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081028 WP 2008 10 28 AALA200802477 1 20080930 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 973TW 53623 LGA EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 19 TO 22 INOPERATIVE. REPLACED BATTERY PACK AT STATION 900 FOR EMERGENCY LIGH T AT OVERHEAD SEAT ROWS 19 TO 22. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081028 WP 2008 10 28 AALA200802476 1 20080930 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 214AA 49162 EMERGENCY LIGHT AT OVERHEAD TAIL CONE CAT WALK INOPERATIVE. REPAIRED CONNECTOR FOR EMERGENCY LIGHT AT OVERHEAD TAIL CON E CAT WALK. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081028 EU 2008 10 28 USAA920081865 1 20081010 A 2560 P4010021 BATTERY AIRBUS 320 A320231 3930325 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 644AW 317 FLT 290 PHX-LAX EMERGENCY EQUIPMENT. FORWARD FLIGHT ATTENDANT FLASHLIGHT WAS NOT CHARGED, WAS NOT STOWED CORRECTLY IN C HARGER. MX R&R THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT BATTERY. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081028 EU 2008 10 28 USAA920081893 1 20081011 A 5320 D53470489000 WEB AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C7 MAJOR REPAIR NR 6062482. CORROSION ON WEB SHEAR PLATE AT FR 56 TO FR 57, S36L. REPLACED WEB SHEAR PLATE AT FR 5 6 TO FR 57, S36L IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081028 NM 2008 10 28 EIAA2008102200060 1 20081021 A 3350 S1356B37 LIGHT BOEING 747 747132 1384882 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481EV 19896 RIGHT UPPER DECK EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT UPPER EMERGENCY LIGHT ASSY, SYSTEM CHECKS NORMAL PER B747MM 33-51-00. 2 L 7 4 4F RT A20WE 20081028 2008 10 28 22AA20080903 4 20080918 A 2564 SWD230100101 SLIDE RAFT DOUG DC10 DC1030F 3023504 WP L1 DOOR DEPLOYED A 22AA K NONE O OTHER IN INSP/MAINT 1 SO 19 450ML 47831 L-1 DOOR SLIDE RAFT DEPLOYED. REMOVED L-1 DOOR SLIDE RAFT IN ACCORDANCE WITH DC-10 M/M 25-61-07; PERFORMED DOOR CHECK F OUND NORMAL IN ACCORDANCE WITH DC-10 M/M 52-11-07. TRANSFERRED TO DMI 22064 AS PER MEL 52-10-2, CAT "C". REMOVED & REP LACED L-1 DOOR RAFT SLIDE IN ACCORDANCE WITH DC10 M/M 25-61-01; CLEARED DMI 22064. 2 L 7 3 4F RT A22WE 20081028 WP 2008 10 28 AALA200802471 1 20080930 A 3350 LIGHT DOUG DC9 DC982 3022082 WP SEAT 7D MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 214AA 49162 EMERGENCY LIGHT AT SEAT 7D FORWARD MISSING. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081028 EU 2008 10 28 USAA920081885 1 20081013 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 602AW 565 FLT NR 251 PHL-PHX EMERGENCY EQUIPMENT. EMERGENCY FLASHLIGHT INOPERATIVE AT AFT RT FLIGHT ATTENDANT SEAT. MX R&R THE F LASHLIGHT BATTERY. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081028 NM 2008 10 28 HALA2008102300814 1 20081023 A 8011 35054367 STARTER BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE RT ENGINE MALFUNCTIONED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM - RETURNED TO GATE. RIGHT ENGINE STARTER FAILED TO ACCELERATE PAST N2 10 PERCENT. MAINT REQUE STED TO EXAMINE PROBLEM. REMOVED AND REPLACED STARTER ASSY PER AMM 80-11-01. OPS CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081028 WP 2008 10 28 AALA200802474 1 20080930 A 3350 MODULE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 214AA 49162 EMERGENCY LIGHTS AT COCKPIT AND FORWARD AISLE. REPLACED MODULE FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081028 NM 2008 10 28 AALA200802483 1 20080919 A 5743 115A521110 TRUNNION BOEING 737 737823 13844CB NM RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 RT MLG TRUNNION FITTING CORRODED AT UPPER OTBD HOLE OUTER FACE. AREA OF DISCREPANCY IS 2 INCHES BY 2 INCHES WITH A .107 INCH DEPTH. REMOVED CORROSION, TREATED, PRIMED AND INSTALLED NEW BUSHING PER SRM 57 20-90-R2-2. 2 L 7 2 4F RT A16WE 20081028 WP 2008 10 28 AALA200802479 1 20080930 A 3350 LIGHT DOUG DC9 DC983 3022083 WP SEAT 20D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 973TW 53623 LGA EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CH ECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081028 NM 2008 10 28 USAA920081867 1 20081011 A 5320 654583471 STRAP BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753005/008. STABILIZER STRAP CRACKED AT BS 328, RBL 47. REPLACED STABILIZER STRAP IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081028 EU 2008 10 28 USAA920081862 1 20080925 A 5347 D5311209220539 SEAT TRACK AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C7 MAJOR REPAIR NR 6062558. CORROSION ON SEAT TRACK AT FR21 + 10, Y765. REPLACED SEAT TRACK IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081028 NM 2008 10 28 ASAA0843609 1 20080914 A 5311 65465672 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 AFT CARGO COMPARTMENT STA 1006 FRAME CORRODED STR 22R AND 24R. CUT OUT DAMAGED AREA OF FRAME, FABRICATED REPAIR PARTS A ND SPLICE DOUBLER, LOCATED, DRILLED AND INSTALLED IAW B737 400 SRM 53 00 07 FIG 201 AND 51 40 02. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0843610 1 20080918 A 5311 651630444 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 COCKPIT RT FRAME WEB CHAFED STA 211.8 AFT SIDE ABOUT 21 INCHES ABOVE FLOOR LEVEL. BLENDED AREA TO REMOVE DAMAGE. HFEC INSPECTED, NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER AND INSTALLED IAW AAR EA 12950 AND ASA EA 5310 02821. 2 L 7 2 4F RT A16WE 20081028 EU 2008 10 28 USAA920081860 1 20080927 A 5320 D53112836200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C7 MAJOR REPAIR NR 6109611 CORROSION ON FLOOR SUPPORT BETWEEN FR20 TO FR23, Y190. REPLACED FLOOR SUPPORT BETWEEN FR 20 TO FR23, Y190. IAW SRM 51-72-11 AND DRAWING NR D53472035. 2 L 7 2 4F RT A28NM 20081028 NM 2008 10 28 ASAA0843614 1 20080912 A 5314 65C329536 KEELBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 FWD CARGO BAY KEEL BEAM CHORD CORRODED AT STA 500 AT 1.5 INCHES I/B OF DRAIN HOLE. CUT OUT DAMAGED AREA. HFEC INSPECTE D NO DEFECT NOTED. FABRICATED FILLER ANGLE SPLICE, LOCATED, DRILLED AND INSTALLLED IAW B737 400 SRM 53 30 12 REPAIR 2 F IG 201 AND ASA EA 5310 02822. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0843617 1 20080914 A 5315 6546809129 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 AFT CABIN FLOORBEAM STA 947 CORRODED AT EXISTING UPPER CHORD REPAIR LBL 40 TO RBL 40. REMOVED DAMAGED UPPER CHORD, FABR ICATED REPAIR TEE SECTION, REPAIR SPLICES AND STRAPS, LOCATED, DRILLED AND INSTALLED IAW AAR EA 12921 AND ASA EA 5310 02 824. 2 L 7 2 4F RT A16WE 20081219 SO 2008 12 19 FDKA2008121000310 1 20081210 A 3350 20191A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 831MJ 145273 FRL FLT 6222 CLT - EMERGENCY LIGHTS DEAD. MX REPLACED 4 BATTERY PACKS. 2 L 7 2 4T RT T00011AT 20080701 EA 2008 7 1 SWIA200819714 1 20080404 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 433SW EMERGENCY LIGHT STRIP IN CABIN IS INOP. (FOUND AT C-CHECK) REPAIRED LIGHTING WIRING PER ESPM 20-17-00 AND WDM 33-51-00. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819715 1 20080423 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 706SK 10149 PAX DOOR OUTER HANDLE IS CRACKED. (FOUND AT C-CHECK) COMPLIED WITH REPLACEMENT OF THE OUTER PAX DOOR HANDLE. 2 L 7 2 4F RT A21EA 20080701 2008 7 1 SWAA083162 4 20080610 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 SWAA083400 1 20080619 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 767, STR 17R. R&R SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 SWAA083399 1 20080619 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 13R. R&R STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 DL757080864 1 20080612 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 1640 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 MAIN CABIN STA 1640 LBL FLOOR STRUCTURE "T" CHORD REPAIR EXFOLIATED AT FASTENER HOLE. REPLACED DAMAGED FLOOR STRUCTURE IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20080701 NM 2008 7 1 DL757080865 1 20080612 A 5754 SKIN BOEING 757 757232 1384965 NM NR 3 SLAT CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 LT WING NR 3 SLAT AT T/E AREA HAS CHAFING 2 EA LOCATIONS. REPAIRED CHAF IAW SRM 51-70-10. 2 L 7 2 4F RT A2NM 20080701 NM 2008 7 1 SWAA083393 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 SWAA083390 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083374 1 20080619 A 5311 6546554 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083389 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083382 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 USAA920081225 1 20080528 A 5740 112N5136 FITTING BOEING 757 7572B7 1384964 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 942UW 27807 WINGLET MOD/ ETOPS MOD - NR 6110937, LEFT WING RIB 22 LOWER FITTING CRACKED, WS 681.5. REPLACED LEFT WING RIB 22 LOWER F ITTING, WS 681.5 IAW DWG 112N5136. (K) 2 L 7 2 4F RT A2NM 20080702 NM 2008 7 2 2008UALA03572 1 20080623 A 2560 F1314 SPRING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SERVICE DOOR WEAK A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 657UA 27112 AFT LT SVC DOOR DEPLOYMENT BAR GAS SPRING IS WEAK. REPLACED GAS SPRING IAW MM 25-66-03. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080702 NM 2008 7 2 2008UALA03571 1 20080623 A 2560 SPRING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SERVICE DOOR WEAK A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 657UA 27112 AFT RT SVC DOOR DEPLOYMENT BAR GAS SPRING IS WEAK. FOUND WEAK GAS SPRING IN DEPLOYMENT BAR SERVICE DOOR. REPLACED GAS S PRING IAW MM 25-66-03. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080702 NM 2008 7 2 2008UALA03568 1 20080624 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 LT OVERWING EMERGENCY EXIT LIGHTS INOP, 1ST & 2ND FROM FWD. FOUND BURNED OUT LAMPS AND FUSES. REPLACED LAMPS AND FUSES OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03565 1 20080623 A 2611 824PTY SMOKE DETECTOR BOEING 737 737322 1384676 NM LAVATORY INTERMITTENT A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION NR NOT REPORTED 1 WP 29 350UA 24301 SMOKE DETECTOR INTERMITTENTLY SOUNDING IN AFT RIGHT LAV. SUSPECT FAULTY SMOKE DETECTOR. REPLACED DETECTOR OP CHECKED G OOD. AC OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 2008UALA03563 1 20080623 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 DENT ONE FOOT AFT OF DOOR FOUR RIGHT ABOUT THREE FEET ABOVE DOOR SILL. DENT MEASURES 1.00 INCHES IN WIDTH AND .046 IN D EPTH. REMOVED DAMAGE FABRICATED AND INSTALLED NEW REPAIR IAW SRM 53-00-01. 2 L 7 2 4F 4 F RT A2NM E17NE 20080702 NM 2008 7 2 2008UALA03562 1 20080623 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 FOUND CORROSION ON FLOORBEAM UPPER FLANGE REPAIR DOUBLER AT BS 365 RBL 7. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW DOUBLER AND FILLER IAW SRM 53-00-98 2 L 7 2 4F 4 F RT A2NM E17NE 20080702 NM 2008 7 2 2008UALA03559 1 20080623 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 FWD LWR CARGO PIT FUSELAGE FRAME DENTED AT UPR CHORD STA 600, STR 23L-24L. REMOVED DAMAGE, FABRICATED AND INSTALLED REP AIR IAW SRM 53-00-07. THIS IS A CAT B RPR IN ZONE 2 AND REQUIRES SUPPLEMENTAL INSPECTIONS STARTING IN 25000FC AND 11000F C THEREAFTER. THIS INSP CONSISTS OF BOTH DETAIL VISUAL AND NDT PER SRM 53-00-07. 2 L 7 2 4F 4 F RT A2NM E17NE 20080702 NM 2008 7 2 2008UALA03558 1 20080623 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 AFT PIT AT BS 1520, APPROX STR 26L, FRAME HAS DENT AT INBOARD FLANGE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR I AW SRM 53-00-07. THIS IS A CAT B RPR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSPECTIONS STARTING AT 50000FC AND 12000FC THE RE AFTER. THIS INSP CONSISTS OF BOTH DETAIL VISUAL AND NDT PER SRM 53-00-07. 2 L 7 2 4F 4 F RT A2NM E17NE 20080702 NM 2008 7 2 2008UALA03553 1 20080623 A 5420 311T3110 WEB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 66885 27112 NR 2 PYLON UPPER WEB CRACKED, NAC STA 182 AT FWD OUTBD CORNER OF FEED THROUGH CUTOUT. FOUND CRACKED WEB SUSPECT NORMAL AC OPERATION. REPAIRED CRACK IAW SB 767-54-0091 FIG 10. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080702 NM 2008 7 2 2008UALA03551 1 20080623 A 5512 SKIN BOEING 737 737522 138449F NM RT STABILIZER DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 RT STABILIZER LEADING EDGE HAS A APPROX 1-2 IN DENT OR CRACK ON RIVET ROW. APRROX 11 RIBS OUT FROM FUSELAGE. 2 L 7 2 4F RT A16WE 20080702 NE 2008 7 2 2008UALA03550 2 20080620 A 7200 ENGINE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 BIRD INGESTION A UALA E A ENGINE SHUTDOWN UNSCHED LANDING C F.O.D. TO TAKEOFF 1 WP 29 194UA 26892 727887 BIRDSTRIKE TO NR 2 ENGINE. RTFL. CREW SUSPECTED A BIRDSTRIKE, AND SHUT THE ENGINE DOWN AS A PRECAUTION. BORESCOPE INSP ECTION REVEALED NO CORE DAMAGE; BIRDSTRIKE DAMAGE CONFINED TO FAN BYPASS AREA. FIVE FAN BLADES WERE BENT FORWARD, WITH MINOR NICKS TO OTHER BLADES. REMOVED AND REPLACED THE FAN BLADE SET. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03543 1 20080621 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY EXIT SIGN INOP:DR3R EEL EXIT SIGN FWD OF DOOR. FOUND FAULTY BATTERY PACK. REPLACED BATTERY PACK OP CHECKED GO OD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03542 1 20080621 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHTS INOP:ALL C ZONE CEILING LT AND RT SIDES. FOUND FAULTY BATTERY. REPLACED BATTERY PACK OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03541 1 20080621 A 3397 CONNECTOR BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY EXIT SIGN INOP, R1 DOOR EMERGENCY LIGHT EXIT SIGN AFT OF DOOR. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03539 1 20080621 A 3350 582011 LAMP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT INOP:DR5L DOOR BUSTLE LT. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03536 1 20080621 A 3350 78961 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EEL INOP:SEAT 3A AFT SECTION. FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVIC E. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03531 1 20080620 A 5320 ANGLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 UPON REMOVAL OF GALLEY TIE ROD ATTACH PLATE THE L-ANGLE STRINGER WAS DAMAGED, FASTNER REMOVAL CAUSED END OF ANGLE TO CRA CK OFF. REPAIRED IAW SRM 51-20-01 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E24NE 20080702 NM 2008 7 2 2008UALA03530 1 20080621 A 2560 LOCK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GIRT BAR WORN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 544UA 25322 DOOR 1R SLIDE LIGHT WILL NOT COME ON. FOUND LOCK ASSY WORN. REPLACED AFT GIRT BAR LOCK ASSY. AND ADJUST RECEIVER, SUSPE CT WORN. LOCK, CHECKED SEVERAL TIMES AND LIGHT COMES ON. 2 L 7 2 4F 4 F RT A2NM E17NE 20080702 NM 2008 7 2 2008UALA03529 1 20080620 A 2560 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR WEAK A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 598UA 28751 DOOR "ARMED" LIGHT NOT BRIGHT ENOUGH AT DOOR 2R. FOUND A WEAK LAMP. REPLACED LIGHT ASSY PER WDM 25-66-11 AND CLEANED P ROX SWITCHES AND OPS CK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080702 NM 2008 7 2 2008UALA03528 1 20080620 A 5210 SPRING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 514UA 24839 DOOR 2R EVAC SLIDE ARM-DISARM LEVER COVER DOOR HAS BROKEN RETURN SPRING. REPLACED ARM DISARM DOOR COVER. 2 L 7 2 4F 4 F RT A2NM E17NE 20080702 NM 2008 7 2 2008UALA03520 1 20080623 A 2100 UNKNOWN BOEING 737 737322 1384676 NM MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 364UA 24533 LOSS OF AIR MODE INFLIGHT. RTFL. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 2008UALA03519 1 20080623 A 3222 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 589UA 28707 GEAR DISAGREE WARNING PROMPTED RTFL. FOUND NOSE GEAR SAFETY VALVE BY-PASSING, FAILING. REPLACED NOSE GEAR SAFETY VALV E, PERFORMED GEAR SWINGS, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080702 2008 7 2 2008UALA03516 4 20080623 A 2350 MICROPHONE BOEING 737 737322 1384676 NM O2 MASK INOPERATIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 346UA 24250 CREW REPORTS THE CAPT'S O2 MASK MICROPHONE IS INOP. SUSPECT FAULTY MASK. REPLACED MASK OP CHECKED GOOD. AC OK FOR SER VICE. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800618 1 20080612 A 5320 6938780 ATTACH FITTING BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 FORWARD PIT STATION 380 S26L WEB ATTACH CLIP IS CRACKED. REPLACED CRACKED CLIP AT STATION 380 S28L WITH FABRICATED CLIP 7075-T6 .032 IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800628 1 20080622 A 5320 66235743 FITTING BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16646 28907 CLIP IS CRACKED AT STATION 706 SL1 11. REMOVED AND REPLACED CLIP AT STATION 706 SL1 11 REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800572 1 20080530 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 BODY STATION 827 LEFT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED F RAME AT STATION 827 A/C BRACKET BETWEEN S-8L AND S-9L PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800573 1 20080530 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 BODY STATION 907 RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 907 A/C BRACKET BETWEEN S-8 AND S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800610 1 20080527 A 5540 65C2584151 RUDDER BOEING 737 737524 1384721 NM DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 RUDDER TRAILING EDGE DAMAGED ON RIGHT-HAND SIDE 30 INCHES BELOW LOWER STATIC DISCHARGE WICK. REPAIRED RUDDER TRAILING E DGE AT STATION 220 PER CONTINENTAL EC/RA 5540-01251 INIT FIRST CALCULATED REBALANCE PER CONTINENTAL EC/RA 5100-02041 COM PLIED WITH, NEW MOMENT IS + 367.94, NO ADDITIONAL WEIGHTS REQUIRED. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800620 1 20080620 A 5315 65C33952 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 SIGNS OF CORROSION ON T-CAP STATION 1016 BL29RT. BLENDED CORROSION ON BS 1016 FLOORBEAM AT RBL 29 DAMAGE FOUND TO BE BE YOND LIMITATIONS PER 737-500 SRM 53-60-51 FIG 101, FABRICATED AND INSTALLED REPAIR PER 737-500 SRM 53-00-51 FIG 201. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800621 1 20080620 A 5322 69774763 MOUNT FITTING BOEING 737 737524 1384721 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 AFT GALLEY LOWER MOUNT FITTING CORRODED AT BODY STATION 1016 LBL 28. FABRICATED NEW FLOOR PAN IAW BAC DWG 65C33582, FAB RICATED T-CAP REPAIR STRAP IAW SRM 53-00-51. ALODINED AND PRIMED IAW SRM 51-20-01, INSTALLED FLOOR PAN DIP PAN GALLEY M OUNTS T-ANLGE AND REPAIR STRAP IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800629 1 20080622 A 5320 141A5410U3 FLOOR SUPPORT BOEING 737 737724 13844BY NM CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 15712 28783 MAIN DECK FLOOR SUPPORT CRACKED STATION 277 TO 294.5 RBL 1. REMOVED AND REPLACED FLOOR SUPPORT BODY STATION 277 TO 294. 5 RBL1 REF SRM 51-40-02, APPLIED CIC REF SRM 51-20-01. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800623 1 20080620 A 5320 6545875520 ANGLE BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 DOOR Z-ANGLE STRAP AT BODY STATION 227 TO 294 CORRODED. REMOVED AND REPLACED Z-ANGLE AND STRAP AT R-1 DOOR IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800562 1 20080601 A 5743 115A5211 BUSHING BOEING 737 737724 13844BY NM LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 LEFT MAIN LANDING GEAR FWD TRUNNION SUPPORT (INBOARD UPPER BUSHING FACE) HAS CORROSION. REWORKED INBOARD UPPER BUSHING FACE PER ECRA 5741-01106. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800564 1 20080605 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 BODY STATION 787 LEFT-HAND CRACKED AT AIR GRILL MOUNT BRACKET. INSTALLED FRAME REPAIR PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800574 1 20080605 A 5311 6546557 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 BODY STATION 869 RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 869 A/C BRACKET BETWEEN S-8 AND S-9 PER EA 5310-04198. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800575 1 20080605 A 5311 6546596 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 BODY STATION 727B RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. FABRICATED REPAI R PARTS FOR BODY STATION 727B RIGHT-HAND SIDE FRAME AT A/C BRACKET BETWEEN S-8 AND S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800593 1 20080612 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 BODY STATION 360 LEFT BETWEEN S-8 AND S-9 IS CRACKED. INSTALLED INTERIM REPAIR AT CABIN FRAME BODY STATION 360 LEFT BET WEEN S-8L AND S-9L PER ECRA 5310-04782 DIP CONTROL NUMBER 88780 FOR FRAME REPAIR AT BODY STATION 360 S-8L AND S-9L AT PA SSENGER SERVICE UNIT (PSU) BRACKET ACCOMPLISH A PERMANENT REPAIR BEFORE 10 JUNE 09 PER ECRA 5310-04782 PART 3. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800544 1 20080528 A 5320 65C3397335 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 INTERCOSTAL IS CRACKED AT BL48 LEFT BETWEEN BODY STATION 312-328. REMOVED & REPLACED INTERCOSTAL AT BODY STATION 312 TO 328 BL48 PER 737-500 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800545 1 20080601 A 5311 6546596 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 BODY STATION 727B RIGHT BETWEEN S8 AND S9 IS CRACKED. REMOVED DAMAGED SECTION OF FRAME, FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR PIECES PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800546 1 20080605 A 2560 ACREM1A MEGAPHONE BOEING 737 7373T0 1384582 NM CABIN DEFECTIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 A/C MEGAPHONE MISSING VOLUME KNOB AND LOW IN VOLUME. REPLACED MEGAPHONE, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800585 1 20080610 A 5754 65C26794 SKIN BOEING 737 737524 1384721 NM L/E SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 NUMBER 2 SLAT HAS CRACKS ON THE LOWER TRAILING EDGE AT AFT RIVETS FSS 454. TRIMMED OUT CRACKED SKIN AND INSTALLED REPAI R DOUBLER AND FILLER PER SRM 57-43-01, FIG 201 AND REINSTALLED INNER PANEL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800583 1 20080608 A 2130 8243921003 CABIN PRESSURE BOEING 737 737524 1384721 NM MALFUNCTIONED A CALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 27 16650 24712 1333 28911 AT FL70 CABIN ALT WARNING HORN SOUNDED, CHECKED CABIN ALT GOING ABOVE 10,000. DID AN EMERGENCY DESCENT AND RAN CHECKLIS T WAS NOT ABLE TO CONTROL CABIN IN MANUAL UNTIL BELOW 10,000 T/S PER AMM 21-31-25 FAULT CODE 030. PERFORMED HEALTH CHEC K REF AMM 21-30-00/601, TEST PASSED. REMOVED AND REPLACED O/H CONTROL MODULE PRECAUTIONARY PER AMM 21-31-25, CHECK OK. BITE & PRESS CHECKED AGAIN PRECAUTIONARY CHECK OK. PANEL, PRESS, C OFF 24-2131-9-0001 2845 ON 24-2131-9-0001 2019. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800615 1 20080620 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16646 28907 STATION 867 FRAME RIGHT CRACKED BETWEEN S8 AND S9 AFT SIDE OF AIR CONDITIONING (A/C) OUTLET ASSEMBLY SUPPORT BRACKET. R EPAIRED FRAME PER EA 5310-04498 OP 2. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800539 1 20080603 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17640 28901 BODY STATION 867 LEFT BETWEEN STR 8 AND STR 9 CRACKED. REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800547 1 20080602 A 5320 6545834551 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 INTERCOSTAL CRACKED AT NUT PLATE HOLES FROM BS 328-344 LBL 44. REMOVED AND REPLACED CRACKED INTERCOSTAL FROM BS 328-344 LBL 44 PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800565 1 20080531 A 5320 6552878125 ANGLE BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 THE Z-ANGLE AT L2 DOOR HAS CORROSION. REMOVED CORRODED Z-ANGLE AT L-2 DOOR, LOCATED AND DRILLED NEW ANGLE PER 51-60-02 AND INSTALLED NEW Z-ANGLE AT L-2 DOOR PER B737 SRM 51-60-02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800567 1 20080530 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 BODY STATION 907 LEFT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. CUT OUT CRACKED AR EA OF BODY STATION 907 LEFT SIDE FRAME BETWEEN S8 AND S9 AND INSTALLED REPAIR PARTS PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800612 1 20080619 A 5320 141A5410U16 FLOOR SUPPORT BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 15712 28783 CRACK IN MAIN DECK FLOOR SUPPORT STATION 328 TO 344 LBL 42. REMOVED AND REPLACED FLOOR SUPPORT STATION 328 TO 344 LBL 4 2 REF 51-10-02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800554 1 20080530 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 BODY STATION 827 RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 827 AT A/C BRACKET BETWEEN S-8R AND S-9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800555 1 20080530 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 BODY STATION 787 RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 787 AT A/C BRACKET BETWEEN S-8R AND S-9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800552 1 20080530 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 BODY STATION 380 RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 380 AT A/C BRACKET BETWEEN S-8R AND S-9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 2008 7 2 SWAA083409 4 20080620 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 200WN 32482 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083411 1 20080621 A 3350 MS155721 LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083350 1 20080618 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 SWAA083402 1 20080619 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080701 SW 2008 7 1 EGI2008F00001 1 20080508 A 6210 206015001115 BLADE BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL MAIN ROTOR DAMAGED E EGIA K NONE O OTHER IN INSP/MAINT 1 SW 09 2922 VISUAL INSPECTION OF M/R BLADE PRIOR TO INSTALLATION FOUND A .017 IN. DEEP DENT IN THE LOWER GRIP PLATE AT STATION 17.5. THIS M/R BLADE WAS PREVIOUSLY REMOVED IN SERVICEABLE CONDITION AND PLACED IN STOCK. COMMUNICATION WITH MFG PSE RECOMMEN DS SENDING TO RBI FOR REWORK. THIS M/R BLADE HAS 2921.6 TT SINCE NEW. THE CAUSE OF THE DAMAGE IS UNKNOWN. SUSPECT M/R BL ADE WAS DAMAGED IN HANDLING. (K) 1 G 7 1 3U 3 U H2SW E1GL 20080702 NM 2008 7 2 SWAA083323 1 20080618 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 420, STR 13R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083366 1 20080618 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083059 1 20080606 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 213WN 34217 R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083065 1 20080608 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 226WN 32494 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083067 1 20080608 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 251WN 32510 EEPLS LENS BROKEN AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083068 1 20080608 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 262WN 32519 EEPLS LENS BROKEN AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080703 SO 2008 7 3 RAIA00805009 1 20080509 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO LANDING GEAR MALFUNCTIONED A RAIA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 CE 03 840HK 145341 FLT 7997 - RIC - LANDING GEAR LEVER DISAGREE MESSAGE ON THE EICAS. LEFT GEAR DID NOT EXTEND. MAINTENANCE REMOVED AND R EPLACED THE PROXIMITY SWITCH ON THE LEFT GEAR. MAINTENANCE GEAR SWING WAS ACCOMPLISHED SUCCESSFULLY. 2 L 7 2 4T RT T00011AT 20080703 SO 2008 7 3 RAIA00805010 1 20080510 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN NOT SEATED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 841HK 145382 PRE FLT 794 - RIC - EMERGENCY LIGHT OUT AT OVERHEAD EXIT INDICATOR. MAINTENANCE RESEATED THE CONNECTOR AT THE EMERGENCY LIGHT INVERTER. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080703 NM 2008 7 3 SWAA082795 1 20080522 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 283WN 36610 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082797 1 20080523 A 5330 6546767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 455, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082800 1 20080524 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506A, STR 20R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082806 1 20080524 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER 14R CRACKED AT BS 887. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082807 1 20080524 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 14R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082808 1 20080524 A 5343 6546543 FITTING BOEING 737 7373H4 1384600 NM LT MLG W/W CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED MV2 CHECK, FOUND LT MLG SIDE SUPPORT FITTING LUG CORRODED AT BS 685. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082815 1 20080525 A 3397 W4142001220 WIRE BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 444WN 29839 EEPLS INOP AT ROW ABC. FOUND LOOSE WIRE. SECURED WIRE PER MM. 2 L 7 2 4F RT A16WE 20080703 2008 7 3 SWAA082816 4 20080526 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 463WN 32467 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082817 1 20080526 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 474WN 33861 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. FOUND LOOSE LIGHT ASSY. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082818 1 20080523 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 491WN 33867 EEPLS LIGHT LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082824 1 20080526 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 406, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082825 1 20080526 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 470, STR 1. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082858 1 20080527 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 217JC 34232 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082869 1 20080527 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, BETWEEN RBL 40 AND LBL 31. REPAIRED PRESSURE WEB PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082870 1 20080527 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER 15R CRACKED AT BS 400. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082848 1 20080526 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082850 1 20080526 A 5315 6546810 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 967, RBL 28 TO RBL 42. REMOVED AND REPLACED CHOR D PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082853 1 20080526 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 394, LBL 3 TO RBL 1. REPAI RED SKIN PER ER. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082871 1 20080527 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080703 2008 7 3 SWAA082860 4 20080527 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 463WN 32467 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082877 1 20080527 A 5312 6545819 PRESSURE PANEL BOEING 737 7375H4 138449D NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED BRDG CHECK, FOUND NLG W/W CEILING PANEL WEB CRACKED AT RBL 7.5. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082878 1 20080527 A 2560 P4010021 BATTERY BOEING 737 7375H4 138449D NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 513SW 24190 AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082872 1 20080527 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082879 1 20080527 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082836 1 20080527 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082835 1 20080527 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082834 1 20080527 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082866 1 20080527 A 2121 215201 GASPER FAN BOEING 737 7373H4 1384600 NM E&E BAY FAULTY A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 646SW 28331 DIVERSION - FLIGHT CREW REPORTED SMOKE SMELL IN CABIN. WITH GASPER FAN TURNED OFF SMELL DISSIPATED. REMOVED AND REPLAC ED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082837 1 20080525 A 2121 215201 GASPER FAN BOEING 737 7373H4 1384600 NM E&E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 29 655WN 28400 DECLARED EMERGENCY - FLIGHT CREW REPORTED ELECTRICAL FUMES IN THE CABIN. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 CALA0800580 1 20080609 A 2560 ACREM1A MEGAPHONE BOEING 737 737924ER 13848A3 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 47414 32827 FORWARD MEGAPHONE SIREN INOPERATIVE. REMOVED AND REPLACED MEGAPHONE WITH BORROWED PART FROM DELTA REF ECRA 2564-01027. 2 L 7 2 4F RT A16WE 20080707 SO 2008 7 7 RAIA00805012 1 20080510 A 5210 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF ADJUST A RAIA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 03 846HK 14500855 FLT 8006 - IAD - PASSENGER DOOR DIFFICULT TO OPEN FROM INSIDE. MAINTENANCE RE-INDEXED THE MAIN DOOR INTERNAL HANDLE. D OOR OPERATION CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080707 EA 2008 7 7 COMA0870018 1 20080502 A 5610 601R3303318 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A COMA B EMER. DESCENT O OTHER CR CRUISE 1 SO 01 690CA 8995 10182 FLIGHT 5289 - CO-PILOT'S WINDSHIELD CRACKED AT FL 390. DECLARED EMERGENCY, REDUCED ALTITUDE, DIVERTED TO ATL, LANDED WI THOUT INCIDENT. REPLACED WINDSHIELD. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 20080707 EA 2008 7 7 COMA0880007 1 20080508 A 2613 LOOP CNDAIR CL600 CL6002D24 1390016 EA OVERHEAT SYS OUT OF POSITION A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 678CA 15125 FLIGHT 5056- ON CLIMB-OUT FROM AUS TO ATL, RECEIVED LEFT BLEED DUCT WARNING MESSAGE. EMERGENCY DECLARED AND A/C RETURNE D BACK TO AUS AND LANDED SAFELY. REPOSITIONED INSULATION AND LOOPS AT HP GROUND DUCT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080707 EA 2008 7 7 COMA0860235 1 20080429 A 3230 601R102371 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 914CA 7012 FLIGHT 5052- AFTER TAKEOFF SELECTED GEAR UP AND RECEIVED GEAR DISAGREE MESSAGE. COMPLETED QRH, EMERGENCY DECLARED. A/C RETURNED TO FSD AND LANDED SAFELY. REMOVED AND REPLACED RT MLG SIDE BRACE SHAFT FITTING. 2 L 7 2 4F RT A21EA 20080707 NM 2008 7 7 USAA920081076 1 20080513 A 3397 3416302 CONNECTOR BOEING 757 7572S7 1384962 NM CABIN DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 902AW 23322 MCN - EEL - C12 CHECK - EMERGENCY ESCAPE PATH LIGHTS WILL NOT ILLUMINATE AT SEATS 19L AND 24L. REPLACED EMERGENCY ESCAP E PATH LIGHT HARNESS CONNECTORS AT SEATS 19L AND 24L IAW BSWPM 20-42-01 AND OPERATIONAL CHECKED IAW USAIRWAYS TASK CARD, A1C33606. 2 L 7 2 4F RT A2NM 20080707 NM 2008 7 7 USAA920081079 1 20080505 A 5320 65C3267723 SHEAR WEB BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 157AW 23779 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON SHEAR WEB, BS 986, RBL 35. REPAIRED SHEAR WEB, BS 986, RBL 35 IAW B737 SR M 51-70-13. 2 L 7 2 4F RT A16WE 20080707 NM 2008 7 7 ASAA0872966 1 20080510 A 3350 D71701100 BATTERY PACK BOEING 737 737790 13844CN NM CABIN FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 614AS 30343 DURING ACCOMPLISHMENT OF T C 78233000 EMERG LTS BATTERY PACK RESTORE FOUND BATTERY PACK M1675 FAILS CAPACITY CHECK. REP LACED SERVICED TESTED BATT M1675 REF MM33 51 06. 2 L 7 2 4F RT A16WE 20080707 WP 2008 7 7 UPS08852249 1 20080505 A 5340 5652580N FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 TAIL 62 COMPT POGO STICK FITTING CRACKED AT FWD END. REPLACED POGO STICK SUPPORT FITTING IN 62 COMPT IAW SRM 51-03-00, SRM 51-01-21, SRM 51-01-24-0 AND SRM 51-03-01-0. 2 L 7 4 4F RT 4A25 20080707 WP 2008 7 7 UPS08852250 1 20080423 A 5322 SHEAR TIE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 D-PIT AT STA 1420 LONGERON 36, SHEAR TIE IS CRACKED AT OUTBD LOWER EDGE. FABRICATED AND REPLACED L36 SHEAR-TIE AND SPLICE PLATE AT STA 1420 AND LONGERON 36 IAW SRM 51--01-20D, SRM 51-01-21, SRM 53-02-10 FIG 002 B AND SRM 53-04-01 FIG 051. 2 L 7 4 4F RT 4A25 20080707 WP 2008 7 7 UPS08852252 1 20080424 A 5711 FRAME DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 RT WING UPPER SURFACE NR 4 STUBWING INBD UPPER FRAME CRACKED, GOUGED AND CHAFED. REPAIRED RT NR 4 ST UBWING INBD UPPER FRAME IAW SRM 51-01-20D, SRM 51-01 -21, SRM 57-02-00-0 FIG 002 AND DWG 5769525. 2 L 7 4 4F RT 4A25 20080707 WP 2008 7 7 UPS08852256 1 20080423 A 5311 3754918U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 MAIN CABIN BELT FRAME END FITTING INSIDE TORQUE BOX CRACKED AT INBD BOLT HOLE STA 1170 AND L21R. REM OVED AND REPLACED BELTFRAME END FITTING AT STA 1179 AND L21R IAW SRM 51-01-20D, SRM 51-01-24-0, SRM 51-03-00. 2 L 7 4 4F RT 4A25 20080707 WP 2008 7 7 UPS08852258 1 20080423 A 5320 97537691 CUSP WEB DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT CUSP HEAVILY CORRODED AT STA 1000. REPAIRED LT CUSP AT STA 1000 IAW SRM 53-02-05 FIG 15. 2 L 7 4 4F RT 4A25 20080707 WP 2008 7 7 UPS08852259 1 20080417 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 ALT STRINGER 65 TO FRONT SPAR FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-24, 51-1-8, 51-1-20D, 51-1-1 2. 2 L 7 4 4F RT 4A25 20080707 WP 2008 7 7 UPS08852268 1 20080421 A 5347 DC853B007002 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 CABIN STA 1470 RBL46 SEAT TRACK PLUG GOUGED. REMOVED AND REPLACED SEAT TRACK PLUG AT STA 1470 AND RB L46 IAW SRM 51-03-00. 2 L 7 4 4F RT 4A25 20080707 WP 2008 7 7 UPS08852269 1 20080422 A 5347 DC853B007002 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 CABIN STA 1130 RBL 50 SEAT TRACK SCALLOP IS GOUGED. REPLACED SEAT TRACK PLUG AT STA 1130 AND RBL 50 IAW SRM 51-03-00. 2 L 7 4 4F RT 4A25 20080707 WP 2008 7 7 UPS08852275 1 20080421 A 5754 576993321 VANE DOUG DC8 DC873F 302199F WP LT SLOT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING CENTER LE, OUTBD END OF SLOT VANE HAS FRETTING WEAR. REPAIRED LT WING CENTER LE OUTBD END OF SLOT VANE IAW SRM 51-1-21, SRM 51-01-08, SRM 51-03-01. 2 L 7 4 4F RT 4A25 20080707 WP 2008 7 7 UPS08852277 1 20080422 A 5753 5655752201 FRAME DOUG DC8 DC873F 302199F WP T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT OUTBD FLAP LE SUPPORT FRAME CRACKED IN LOWER ATTACH ANGLE RADIUS INBD FROM STA 340 HINGE. FABRICA TED AND REPLACED LT OUTBD FLAP LE ATTACH ANGLE INBD OF STA 34 0 IAW DWG 5655752, SRM 51-01-24, SRM 51-01-24, SRM 51-01-2 0D. 2 L 7 4 4F RT 4A25 20080707 NM 2008 7 7 UPS08M52229 1 20080326 A 5720 STRUCTURE DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:4C LEFT WING LE ACCESS PANEL LANDING AT NR 9 SLAT TRACK CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLE R IAW MD-11 SRM 57-10-00 FIG.18. 2 L 7 3 4F RT A22WE 20080707 2008 7 7 UPS08M52261 4 20080513 A 2565 CONTACT DOUG MD11 MD11F 3023600 NM EVAC SLIDE DIRTY A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 279UP 48573 RT SLIDE REMOTE PRESS CK LIGHT INOP. DEFERRED PER MEL 25-61-2 DMP C/W. CLEANED CONTACTS. OPS CHECK GOOD. 2 L 7 3 4F RT A22WE 20080707 NM 2008 7 7 UPS08M52266 1 20080512 A 2560 STRAP DOUG MD11 MD11F 3023600 NM GIRT BAR WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 282UP 48452 L1 GIRT BAR STRAP WORN. SLIDE INOP. SLIDE DEFERRED PER MEL 52-10-3-2, M375594 ASSIGNED. INSTALLED L1 SLIDE ASSY PER 2 5-61-01-4 AND 25-61-15-4. 2 L 7 3 4F RT A22WE 20080707 NM 2008 7 7 UPS08M52267 1 20080514 A 2560 GIRT BAR DOUG MD11 MD11F 3023600 NM COCKPIT OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 GIRT BAR POPPED OUT OF SNAP RING. REINSTALLED GIRT BAR REF MM 25-61-01-4. 2 L 7 3 4F RT A22WE 20080707 SO 2008 7 7 C2XA08IA127 1 20080515 A 3231 8005701 PROXIMITY SWITCH EMB 135 EMB135LR 3260305 SO NLG FAULTY A C2XA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 27 24517 145332 IAH - FLIGHT 2649, THE CREW REPORTED THAT THE NOSE LANDING GEAR DOORS OPENED IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WH ERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR DOOR SEQUENCE PROXIMITY SWITCH. OPER ATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20080707 NM 2008 7 7 2008UALA02739 1 20080510 A 3397 362624 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY LIGHT ROW 4F AFT INOP. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 2008UALA02741 1 20080511 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY DOOR SLIDE LIGHT DR5 LT INOP. SUSPECT FAULTY LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 2008UALA02742 1 20080511 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY CEILING LIGHT ROW 54 RT INOP. SUSPECT FAULTY LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 2008UALA02751 1 20080512 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 226UA 30226 SEAT 2F EMERGENCY AISLE LIGHT STRIP NOT CONNECTED. REPLACED LIGHT. OPS CHK'D OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080707 NM 2008 7 7 2008UALA02765 1 20080512 A 3350 7024091001 SIGN BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 791UA 26933 EMERGENCY EXIT SIGN AT DOOR 4L IS LOOSE. REPLACED LIGHT ASSEMBLY LIGHT. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080707 EU 2008 7 7 2008UALA02772 1 20080513 A 3350 BR964421 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 416UA 479 15C EMERGENCY LIGHT INOP. RELAMPED. OP CK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080707 NE 2008 7 7 2008UALA02773 2 20080513 A 7532 BLEED VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 427UA 512 NR 1 ENGINE HIGH PRESSURE BLEED VALVE PROBLEM CAUSED A DIVERSION. 2 L 7 2 4F 4 F RT A28NM E40NE 20080707 NM 2008 7 7 2008UALA02774 1 20080514 A 2781 PROXIMITY SENSOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SLATS OUT OF ADJUST A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 676UA 30028 L/E SLAT ASSY PROBLEM AFTER FLAPS RETRACTED. RTFL. PROXIMITY SENSOR S285 OUT OF LIMITS. ADJUSTED SENSOR. 2 L 7 2 4F 4 F RT A1NM E24NE 20080707 NM 2008 7 7 2008UALA02775 1 20080514 A 2897 ELM4121 CIRCUIT CARD BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FUEL SYSTEM MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 793UA 26946 FUEL PRESSURE PROBLEM. AFTER TROUBLE SHOOTING FOUND FAULTY SIGNAL CONDITIONING CARD. REPLACED SIGNAL CONDITIONING CARD PER MM24-09-00 ALL OPS NORMAL. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080707 NM 2008 7 7 2008UALA02782 1 20080514 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 RIGHT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP, FIRST LIGHT ASSY AFT BULB. RELAMPED. OPS CHK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 2008UALA02784 1 20080514 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY EXIT LIGHT INOP, AT DOOR 3 RIGHT SLIDE LIGHT. SUSPECT FAULTY LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FO R SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 2008UALA02787 1 20080514 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST DE DESCENT 1 WP 29 173UA 24380 EMERGENCY EXIT EEL LIGHT INOP, AT SEAT 5E AFT LIGHT ASSY. REPLACED LIGHT ASSY. OP CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 EU 2008 7 7 2008UALA02793 1 20080515 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 446UA 834 CORROSION FOUND ON FLOORBEAM NR 255. 2 L 7 2 4F 4 F RT A28NM E40NE 20080707 NM 2008 7 7 2008UALA02802 1 20080515 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 CEILING EMERGENCY LIGHT NEAR SEAT ROW 5L IS INOP. RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 2008UALA02803 1 20080515 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 SEAT 5E FWD EMERGENCY LIGHT IS INOP. RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080808 NM 2008 8 8 08FDEA02778 1 20080709 A 5720 RETAINER BOEING 727 727233 138408A NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 RT WING REAR SPAR LWR CHORD, APPROX 12" IB OF FWD MLG TRUNNION, SEAL RETAINER CORRODED AT OB END. REMOVED FAIRING AND SEAL RETAINER REF SRM PG 2 LOCATED AND DRILLED NEW SEAL RETAINER REF SRM 51-30-5 PG 1, INSTALLED SEAL RETAINER AND FAI RING REF SRM 51-30-2 PG 2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080808 EU 2008 8 8 08FDEA02519 1 20080627 A 5321 B5327046101800 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 232 CF IS CRACKED AND WORN IN TO. REPAIRED FLOOR PANEL 232 CF BY FABBING A NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE, POTTED INSERTS, POTTED, CURED AND SANDED EDGES SMOOTH; APPLIED NON-SKID AND PART MARK ED PANEL IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 WP 2008 8 8 08FDEA02799 1 20080709 A 5522 SKIN DOUG MD10 MD1010F 3022112 WP LT ELEVATOR UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT OUTBD ELEVATOR LOWER SURFACE HAS A LIGHTNING STRIKE AT STA XE 474. 2 L 7 3 4F RT A22WE 20080808 EU 2008 8 8 08FDEA02524 1 20080627 A 5321 B5327047602800 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 232 YG IS CRACKED AND CRUSHED. FABBED A NEW PANEL 232 YG, POTTED INSERTS, POTTED, CURED 7 S ANDED EDGES, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02728 1 20080707 A 5420 FAIRING AIRBUS 300 A300F4605R 3930327 EU NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 NR 2 PYLON AFT FAIRING LT FWD OF 483 CL CUTOUT; METAL PLATING IS CRACKED AT THE LOWER END. REMOVED METAL PLATE REINFORC EMENT IAW A300-600 SRM 51-40-00. FABBED REPAIR DOUBLER IAW A300-600 SRM 54-50-10; PG 214. STOP DRILLED THE CRACK IAW A 300-600 SRM 54-50-00; PG 214. INSTALLED REPAIR DOUBLER ON METAL PLATE REINFORCEMENT IAW A300-600 SRM 54-50-00; PG 214. INSTALLED METAL PLATE REINFORCEMENT ON TO AIRCRAFT IAW A300-600 SRM 51-40-0. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02752 1 20080602 A 2550 A25771305 CARGO TRACK AIRBUS 300 A300B4622R 3930312 EU CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 FWD CARGO COMPT ROLLER TRACK NR 3 BETWEEN FR27-32 WITH CORROSION. NEW ROLLER TRACK INSTALLED AS PER AMM 25-52-21-4 01. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02691 1 20080703 A 5320 146N541613 FLOOR SUPPORT BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FLOOR SUPPORT FROM BS 1200 TO BS 1340, RBL 3, 6, 11, AND 16 HAS CORROSION AROUND NUTPLATE HOLES IN SEVERAL LOCATIONS. C ORROSION FOUND EXCEED DAMAGE LIMITS IN B757-200 SRM 53-00-53 FIG 101. STRINGER REMOVED AND REPLACED IAW B757-200 SRM 51 -10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080808 NM 2008 8 8 08FDEA02649 1 20080703 A 5241 6556150138 DOOR FRAME BOEING 727 727225 1384077 NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 FWD GALLEY DOOR LWR AFT CORNER CRACKED REMOVED FWD GALLEY DOOR AND OPENED UP LOWER AFT INNER SKIN FOR ACCESS. REMOVED LOWER AFT STOP FITTING REMOVED PRESSURE SEAL, LOWER GATE, AFT LOWER SEAL RETAINER, REMOVED DAMAGE SECTION OF FRAME, AND DRILLED AND INSTALLED FRAME REPAIR. REF BOEING DRAWING NR 69-69908. INSTALLED ITEMS THAT WERE REMOVED. INSTALLED AND RIGGED DOOR REF AMM 52-12-000-5. INSTALLED LEVELING COMPOUND IN THE LOWER PART OF DOOR. INSTALLED HANDLE BOX AND LOWER HINGE COVER PLATES, PAINTED REPAIR. OPS CHECK GOOD. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080808 EU 2008 8 8 08FDEA02518 1 20080627 A 5321 B5327048300600 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 232 SG IS CRACKED AND PUNCTURED. FABBED A NEW PANEL; POTTED EDGES; CURED; SANDED; POTTED IN SERTS; APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02709 1 20080705 A 5313 BAC1490141 STRINGER BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 CABIN S-6L LOWER SURFACE HAS CORROSION BETWEEN BS 720A AND 720D REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REF SRM 5 3-10-1 FIG 1. REMOVED DAMAGE SECTION OF STRINGER REF SRM 53-10-3, PG 6. VERIFIED ALL REPAIR MATERIALS. REF A TAG A932 13, AND A48139. ALL REPAIR MATERIALS ARE 2024-T3, .071 INCH AND .125'. STRINGER IS BAC-1498-141 7075 -T62. REMOVED ST RINGER CLIPS, STA 720B AND C, STR 6L. FABRICATED AND FIT STRINGER SECTIONS AND SPLICE PLATES REF SRM 53-10-3 ITEMS 5. INSTALLED WET STRINGER SECTION AND SPLICE PLATES REF SRM 53-10-3 PG-5. REFINISHED REPAIR AREA REF AMM 51-20 AND SRM 53 -10-3 PG 5 ITEM 8. REINSTALLED STRINGER CLIPS REF SRM 51-30-02 PG 1-10. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080811 EU 2008 8 11 M7K2008F00131 1 20080303 A 5350 350A25040501 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE INLET FAIRING CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 807MH 1001 3912 23130 DURING ROUTINE 100 HOUR INSPECTION, A CRACK WAS FOUND RADIATING ACROSS THE CORNER OF THE FIRST HOLE ON THE HINGE END WIT H A TOTAL SEPARATION OF THE HINGE CORNER METAL ON THE FAIRING ATTACHMENT FLANGE. A NEW PART WAS INSTALLED IAW THE REQUI REMENTS OF AD2004-01-14 AN INSPECTION DUE AT 110 HOUR INTERVAL. THIS IS A FAIRLY COMMON DEFECT FOR THIS PART. SUGGEST THE NEW IMPROVED PN ASSY BE MADE IN QUANTITIES SO ALL AC MAY BE UPDATED TO THE LATEST NON AD EFFECTED PN. THIS IS A MFG SUPPLY ISSUE THAT THE OEM REFUSES TO ADDRESS. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 CE 2008 8 11 Z5F2008F00003 1 20080717 A 5610 991438013 WINDSHIELD CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT BROKEN E Z5FA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 EA 63 549CS 3145 5605546 ENROUTE, PILOT`S WINDSHIELD SHATTERED WITHOUT WARNING. CREW DIVERTED AND LANDED WITHOUT INCIDENT. EMERGENCY VEHICLES W ERE STANDING BY. MAINT REPLACED THE LEFT WINDSHIELD. LEAK CHECK OK. (K) 2 L 7 2 4F 4 F RT A22CE E00059EN 20080811 EU 2008 8 11 M7K2008F00094 1 20080324 A 5340 350A54112420 BRACKET UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COOLING DUCT CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 813MH 320 3967 23183 BRACKET FOUND CRACKED DURING ROUTINE 100 HOUR INSPECTION. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 NE 2008 8 11 C4N2008F00000 2 20080721 A 7200 CONNECTOR SKRSKY S61 S61N 8142104 NE GE CT58 CT581402 30011 NE NR 1 ENGINE DISCONNECTED E C4NA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 612AZ A14F14781101 61297 MAIN TRANSMISSION CHIP DETECTOR ILLUMINATED IN FLIGHT. (K) AFTER LANDING, INSPECTION FOUND CHIP PLUG LEAD HAD FALLEN O FF CHIP DETECTOR. LEAD WAS REINSTALLED, ACFT WAS RETURNED TO SERVICE. 2 G 7 2 4U 4 U 1H15 1E3 20080811 SO 2008 8 11 XGN2008F00009 2 20080723 A 8530 CYLINDER CESSNA 402 402B 207590P CE CONT O520 TSIO520* 17040 SO ENGINE CRACKED E XGNA K NONE O OTHER IN INSP/MAINT 1 SW 05 3378Q 532 402B0334 CRACKED BETWEEN FIN NR 1 AND FIN NR 3 AFT OF THE INJECTOR. MFG REV E SERIES CYLINDER. ALL DEFECTIVE! (K) 1 L 7 2 3O 3 O A7CE E8CE 20080811 NE 2008 8 11 R612008F00002 2 20080710 A 7200 ENGINE EMB ERJ170 ERJ170200LR 3260121 NM GE CF34 CF348E5 30061 NE NR 2 MALFUNCTIONED A R61A E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 11 131HQ 17000215 DURING AC DESCENT CREW RECEIVED AN EICAS ENGINE CONTROL FAULT MESSAGE, AND ENGINE WAS DECELERATING. CREW FOLLOWED QRH P ROCEDURES AND SHUTDOWN NR 2 ENGINE. DECLARED AN EMERGENCY LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO AC RE SET POWER AND CLEARED ALL ENGINE CONTROL FAULTS IAW SB 170-73-A0005. MAINT AND CREW COMPLETED ALL REQUIRED OPS CHECKS. ALL OPS CHECKS WERE GOOD AND MAINT RETURNED AC TO SERVICE. (K) 2 L 7 2 4F 4 F RT A56NM E00063EN 20080811 NM 2008 8 11 AALA200801666 1 20080618 A 3350 LENS BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AA 24488 DFW - EMERGENCY LIGHT EXIT SIGN AT AFT LT OVERWING DAMAGED. REPLACED LENS FOR EMERGENCY LIGHT EXIT SIGN AT AFT LT OVERW ING. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 WP 2008 8 11 AALA200801698 1 20080625 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 402A 49313 LGA - EMERGENCY LIGHT AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 100 FOR EMERGENCY LIGHT AT FIRST CL ASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 WP 2008 8 11 MWE2008F00025 1 20080725 A 3350 2232 LAMP DOUG DC9 DC981 3022081 WP EMERGENCY LIGHT INOPERATIVE A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 813ME 48007 RT OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED RT OVERWING LIGHT. (K) 2 L 7 2 4F A6WE 20080811 NM 2008 8 11 AALA200801647 1 20080617 A 3350 SHROUD BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 925AN 29526 DFW - EMERGENCY LIGHT AT SEAT ROW 12 MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT TAT SEAT ROW 12. SYSTEM GROUN D CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A16WE 20080811 SO 2008 8 11 SIM2008F00018 1 20080722 A 3320 BR900022 BALLAST EMB 135 EMB135LR 3260305 SO CABIN LIGHTS BURNED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 738NR 145401 ON FLIGHT, CREW REPORTED PLASTIC BURNING ODOR THROUGH THE CABIN COMING FROM ABOVE 4A. AC REMOVED FROM SERVICE. FOUND L T SIDE WALL BALLAST BY ROW 2A, BURNED AND INOPERATIVE. REMOVED AND REPLACED BALLAST ABOVE ROW 2A IAW MM 33-71-03. OPER ATIONAL CHECK GOOD, AC RETURNED TO SERVICE. (K) 2 L 7 2 4F RT T00011AT 20080811 EA 2008 8 11 DJFA2008055 1 20080615 A 2120 3043110630 HEAT TAPE CNDAIR CL601 CL6012A12 1900303 EA BURNED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 664CW 13632 3064 WHILE REFUELING THE AC, THE CREW NOTED A SIGNIFICANT AMOUNT OF SMOKE IN THE COCKPIT. OPEN (A) 2 L 7 2 4F RT A21AE 20080811 NM 2008 8 11 AALA200801717 1 20080627 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 621AM 24579 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 11D. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 11D. SYSTEM GROUND CHEC KED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 CE 2008 8 11 DJFA2008060 1 20080628 A 2422 INVERTER BEECH MU300 400A 1155402 CE ELECTRICAL SYS FAILED E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 429LX RK265 CREW REPORTED DUAL INVERTER FAIL DURING FLIGHT WITH A FAINT ELECTRICAL BURNING SMELL. AIRCRAFT LANDED AT INTENDED DESTI NATION. DISCREPANCY WAS TROUBLESHOT TO THE INVERTER INDICATOR SELECTOR. THE SELECTOR WAS REPLACED ALONG WITH THE NR 1 AND NR 2 INVERTERS. (A) 2 H 7 2 4F RT A16SW 20080811 NM 2008 8 11 AALA200801667 1 20080618 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 758AN 32637 DFW - EMERGENCY LIGHT AT AFT GALLEY DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080811 NM 2008 8 11 AALA200801591 1 20080611 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 676AN 29426 DFW - EMERGENCY LIGHT AT OVERHEAD EXIT AT SEAT 18A INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD EXIT AT S EAT 18A. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 WP 2008 8 11 AALA200801699 1 20080625 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 402A 49313 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 12 TO 16 INOPERATIVE. REPLACED BATTERY PACK AT B5 102 FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 12 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 NM 2008 8 11 HNA2008F00010 1 20080530 A 3350 82410162003 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS MALFUNCTIONED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 804EX 227 EMERGENCY LIGHT TURN ON WHEN SWITCH TURNED OFF. REMOVED AND REPLACED EMERGENCY LIGHTS CONTROL BOX, OPS CHECK GOOD. (K) 2 H 7 2 4T RT A13NM 20080811 EA 2008 8 11 A6WA200840519 1 20080617 A 5210 601R3177457 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 444ZW 7788 PAX DOOR AFT SIDE PANEL STIFFENER (P/N 601R317745-7) CRACKED AT DOOR ASSIST MOTOR ASSY. STIFFENER (P/N 601R317745-7) RE PLACED IAW CRJ 200 SRM 51-42-06 AND SRM 51-42-13. (A) 2 L 7 2 4F RT A21EA 20080811 NM 2008 8 11 PID2008F00010 1 20080731 A 3350 20131A BATTERY PACK BOEING 767 767277 1385128 NM EMERGENCY LIGHTS INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 EA 39 767MW 22694 DURING PREFLIGHT, RT OVERWING ESCAPE HATCH SQUID TEST LIGHT DIM. REMOVED AND REPLACED RT OVERWING ESCAPE HATCH EMERGENC Y LIGHT BATTERY PACK. OPS CHECK WAS NORMAL IAW AMM. (K) 2 L 7 2 4F RT A1NM 20080811 EU 2008 8 11 M7K2008F00048 1 20080108 A 5302 350A23422220 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 812MH 1427 3956 23072 CRACK FOUND DURING ROUTINE INSP RADIATING FROM A SCREW HOLE ON MOUNTING FLANGE SURFACE AND ONTO REINFORCEMENT RIB SURFAC E. A NEW FITTING HAS BEEN MATCH DRILLED AND INSTALLED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 2008 8 11 MTN2008F00004 2 20080801 A 7310 3027039 LINE CESSNA 208 208B 2073701 CE ENGINE FUEL LEAKING E MTNA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 68 905FE 208B0005 AC ENROUTE, THE PILOT DETECTED FUEL ODOR IN THE COCKPIT, PILOT RETURNED THE ACFT TO DEPARTURE AFTER TROUBLESHOOTING. TH E MECHANIC FOUND AN ENGINE FUEL LINE LEAKING. (K) 1 H 7 1 3T A37CE 20080811 CE 2008 8 11 GUU2008F00016 1 20080621 A 3210 LANDING GEAR BEECH 1900 1900D 1154162 CE OUT OF RIG A GUUA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 17 190YV UE190 FLIGHT 9120, AFTER TAKEOFF, UPON LANDING GEAR RETRACTION RED INTRANSIT LIGHT REMAINED ILLUMINATED, RT LANDING GEAR APPEA RED TO RETRACT SLOWER THAN REST, RT "R" AND "H" REMAINED ILLUMINATED LONGER. ACCOMPLISHED MLG RIGGING AND SWITCH ADJUSTM ENTS. OPERATIONAL CHECK NORMAL. (A) 2 L 7 2 4T RT A24CE 20080811 CE 2008 8 11 GUU2008F00017 1 20080615 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 17 87554 UE227 FLIGHT 9286, DURING FLIGHT, BURNING ODOR OBSERVED. RAN ENGINES WITH ALL ELECTRICAL SYSTEMS ON AND ENVIRONMENTAL SYSTEMS ON NO ODOR NOTED. COULD NOT DUPLICATE. (A) 2 L 7 2 4T RT A24CE 20080811 CE 2008 8 11 GUU2008F00018 1 20080608 A 3230 RELAY BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A GUUA O OTHER O OTHER AP APPROACH 1 SO 17 87555 UE234 FLIGHT 9225, DURING APPROACH, LANDING GEAR RELAY POPPED ON EXTENSION OF LANDING GEAR, MOTOR RAN UNTIL IT POPPED AND RT D OWN AND LOCK ANNUNCIATOR ILLUMINATED. INSPECTED LANDING GEARS, ACTUATORS AND SWITCHES ALL SECURE. LANDING GEAR OPERATION AL CHECKS NORMAL. (A) 2 L 7 2 4T RT A24CE 20080811 EA 2008 8 11 A6WA200840514 1 20080616 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 444ZW 7788 BULKHEAD CLIPS CRACKED AT FS 280, RBL 9 AND WL 72. BULKHEAD CLIPS AT FS 280, RBL 9 AND WL 72 REPLACED IAW CRJ 200 SRM 5 1-42-06 AND SRM 51-42-21. (A) 2 L 7 2 4F RT A21EA 20080811 SO 2008 8 11 CHQA200800128 1 20080628 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007A 03030 GL EMERGENCY LIGHTS INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 264SK 145221 CAE311337 MAINTENANCE FOUND THE FLOOR BOARD EMERGENCY LIGHTS INOP BETWEEN ROW 3 AND 12. THE EMERGENCY LIGHT INVERTERS NR 2 AND NR 5 WERE REPLACED AND THE EMERGENCY LIGHT SYSTEM OPERATED NORMALLY. (A) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080811 EA 2008 8 11 A6WA200840517 1 20080617 A 5320 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 444ZW 7788 CARGO DOOR SURROUND STRUCTURE, CHANNEL CRACKED AT FS 574 LBL 45 AND WL 79.5. CARGO DOOR SURROUND STRUCTURE CHANNEL AT F S 574 LBL 45 WL 79.5 REPLACED IAW CRJ 200 SRM 51-42-06. (A) 2 L 7 2 4F RT A21EA 20080811 EA 2008 8 11 A6WA200840518 1 20080617 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE PUNCTURED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 444ZW 7788 COCKPIT BULKHEAD FS 280 PUNCTURED AT LBL 34 AND WL 124. COCKPIT BULKHEAD FS 280 AT LBL 34 AND WL 124 REPAIRED IAW REO 6 01R-53-11-1414. (A) 2 L 7 2 4F RT A21EA 20080811 WP 2008 8 11 AALA200801748 1 20080701 A 3350 LENS DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 587AA 53250 LGA - EMERGENCY LIGHT AT FORWARD SEAT 7D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FORWARD SEAT 7D. SYSTEM GR OUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 NM 2008 8 11 AALA200801769 1 20080703 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 SFO - EMERGENCY LIGHT AT LT OVERWING INOPERATIVE. REPAIRED SHORT CIRCUIT AT LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LT OV ERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080811 NM 2008 8 11 USAA920081331 1 20080709 A 2560 P4010021 BATTERY PACK BOEING 737 7373G7 1384595 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 307AW 24634 LOG 8055785 - SAN-FLT NR 191- AFT FLT ATTENDANT EMERGENCY FLASHLIGHT NOT BLINKING. MX REPLACED THE BATTERY PACK. OPERA TIONAL CHECK WAS GOOD. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081364 1 20080714 A 5344 65458001207 HINGE BOEING 737 7373B7 1384580 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 24515 CLT-C11-MAJOR REPAIR LOG 5030342- CRACK AT LOWER HINGE OF FORWARD SERVICE DOOR BS296. REPAIRED HINGE OF FORWARD SERVICE DOOR BS296 IAW US AIRWAYS EA 100568 (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081327 1 20080705 A 3397 BMS13311122 WIRE BOEING 737 7373G7 1384595 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 308AW 24710 LOG 4430835 LAS-FLT NR 199- EMERGENCY EXIT LIGHTS OUT AT SEAT ROW 2L, MAINTENANCE FOUND BROKEN WIRE, REPAIRED BROKEN WIR E. OPERATIONAL CHECK WAS GOOD. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081367 1 20080703 A 5320 6935352U14 TIE CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT- Q3 CHECK MAJOR REPAIR NR 03C10853043/011- TIE CLIP CRACKED AT BS 867, S5L. REPLACED TIE CLIP AT BS867, S5L IAW B737 SRM 52-10-02 AND SRM 52-40-02. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAABA08111 1 20080628 A 7334 21SN04223 PRESSURE SWITCH BOEING 767 7672B7 1385107 NM RT ENGINE FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 256AY 12561 5181 26847 PHL FLT 710 EN-ROUTE PHL TO ZRH. THE FLIGHT RETURNED TO FIELD DUE TO A NUMBER 2 ENGINE FUEL FILTER MESSAGE. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMBER 2 ENGINE FUEL PRESSURE SWITCH. OPERATIONALLY AND LEA K CHECKS OK. [SUPP-CLOSED] (B) 2 L 7 2 4F RT A1NM 20080811 NM 2008 8 11 USAA920081328 1 20080708 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 839AW 2669 LOG 7983375 LAS-FLT NR 473- AFT F/A EMER FLASHLIGHT NOT BLINKING. MAINTENANCE REPLACED FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD. (B) 2 L 7 2 4F RT A28NM 20080811 NM 2008 8 11 USAA920081374 1 20080714 A 3397 PIN BOEING 737 73733A 1384673 NM CONNECTOR BACKED OUT A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 164AW 23625 LOG 4299302 PHX FLT NR 199- EMERGENCY EXIT PATH LIGHT ROW 15 INOP. MX FOUND PUSHED OUT PIN AT ROW 15 EMERGENCY CONNECTO R. MX REINSERTED PIN. OPERATIONAL CHECK WAS GOOD. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081349 1 20080710 A 5320 6601693 SUPPORT ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT- MAJOR REPAIR Q3 CHECK NR 03C20853012/008, LEVEL 2 CORROSION ON SUPPORT ANGLE, BS 500G, RBL 17.7. REPLACED SUPPORT ANGLE, BS 500G, RBL 17.7 IAW BOEING DRAWING 66-01693. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081347 1 20080706 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT- MAJOR REPAIR Q3 CHECK NR 03C10863029/022, LEVEL 2 CORROSION ON CABIN FLOORBEAM "T" CAP, BS 967, LBL17. REPAIRED CA BIN FLOORBEAM "T" CAP, BS967, LBL17 IAW B737 SRM 53-60-51-FIG 201. (B) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 AALA200801510 1 20080604 A 1100 PLACARD BOEING 757 757223 1384957 NM CABIN PEELING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 636AM 24594 DFW - EMERGENCY LIGHT EXIT ARROW DECAL AT FORWARD SEAT 18A PEELING. REPLACED EXIT ARROW DECAL FOR EMERGENCY LIGHT AT FO RWARD SEAT 18A. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 NM 2008 8 12 AALA200801513 1 20080604 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AM 24594 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 18F INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 18F. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 NM 2008 8 12 AALA200801537 1 20080605 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 797AN 30012 DFW - EMERGENCY LIGHT AT SEAT 22G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 EA 2008 8 12 N6WA0080502A 1 20080619 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 156GJ 10227 5337-STL CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED CEILING FLOOD LIGHT BULB IAW MM 33-51-09. (S) 2 L 7 2 4F RT A21EA 20080808 EU 2008 8 8 08FDEA02516 1 20080627 A 5321 A5228536400600 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 221 GF IS GOUGED. FABBED NEW FLOOR PANEL; POTTED EDGES; CURED; SANDED; POTTED INSERTS; APP LIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20081028 NM 2008 10 28 ASAA0843613 1 20080925 A 5320 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 AFT CARGO FLOOR SUPPORT AT STA 727F LBL 8.10 1 EA HOLE AND 1 EACH DEEP DRILL START. REMOVED DAMAGED SECTION OF FLOOR SU PPORT, FABRICATED CHANNEL REPAIR PARTS, LOCATED, DRILLED AND INSTALLED IAW AAR EA 12953 AND ASA EA 5310 02826. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0843616 1 20080914 A 5315 654681180 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 AFT CABIN FLOORBEAM STA 986 CORRODED AT EXISTING UPPER CHORD REPAIR RBL 40 TO LBL 40. REMOVED DAMAGED UPPER CHORD, FABR ICATED REPAIR TEE SECTIONS REPAIR SPLICES, HEAT TREATED, LOCATED, DRILLED AND INSTALLED IAW AAR EA 12922 AND ASA EA 5310 02823. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0843618 1 20080917 A 5320 655287873 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 L2 DOOR THRESHOLD WEB STA 967 TO STA 980 CORRODED UNDER INNER CHORD. REMOVED DAMAGED WEB, FABRICATED HEAT TREATED, LOCA TED, DRILLED AND INSTALLED A REPLACEMENT WEB IAW B737 400 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081218 EU 2008 12 18 FDEA200812155157 1 20081215 A 5321 FLOOR PANEL AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 MAIN CABIN FLOOR PANEL NR 242 QJ IS DAMAGED. FABBED A NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED HOLE S, COUNTERBORED, POTTED & SANDED EDGE. INSTALLED INSERTS, APPLIED ANTI-SKID & PART MARKED IAW DWG SRZ25-005: REV "G". 2 L 7 2 4F RT A35EU 20081217 NM 2008 12 17 SWAA087086 1 20081213 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 731SA 27863 DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION BEARING O/B LOWER ATTACH LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081216 WP 2008 12 16 AALA200810478 1 20081211 A 5320 SHELF DOUG DC9 DC982 3022082 WP RT MLG WW CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 463AA 49593 SHELF ABOVE RIGHT WHEEL WELL DOOR ACTUATOR TOP MOUNT IS CRACKED AT AFT END IN RADIUS. INSTALLED REPAIR ANGLE PER ESO 80 559 DATED 12/11/08. 2 L 7 2 4F A6WE 20081216 WP 2008 12 16 AALA200810456 1 20081126 A 5322 MOUNT DOUG DC9 DC983 3022083 WP GALLEY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 CORROSION ON INBOARD AFT NUMBER 2 GALLEY MOUNT. INSTALLED SERVICEABLE GALLEY MOUNT. 2 L 7 2 4F RT A6WE 20081216 WP 2008 12 16 AALA200810477 1 20081210 A 5320 STIFFENER DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7541A 49995 STIFFENER AT STATION 1418 AND LONGERON 2 RIGHT CRACKED IN 2 PLACES. INSTALLED DOUBLER PER SRM 53-01 FIGURE 2. 2 L 7 2 4F A6WE 20081218 EU 2008 12 18 UALA2008120806788 1 20081207 A 3510 MXP401600U OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 487UA 1669 F/O O2 MASK WILL NOT TEST. REMOVED & REPLACED FIRST OFFICER'S O2 MASK STOWAGE BOX. LEAK CHECKED O2 LINE. LEAK CHECK O KAY. CREW O2 BOTTLE VALVE OPEN & SAFETIED MASK AND BOX. OPS CHECK OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080701 EA 2008 7 1 TRAX200800680 1 20080522 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 720EV 10115 CABIN AFT MOST CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED CABIN AFT MOST CEILING EMERGENCY LIGHT BULB. OPS CHE CK GOOD. 2 L 7 2 4F RT A21EA 20080701 NM 2008 7 1 AALA200801558 1 20080608 A 3230 PROXIMITY SENSOR BOEING 757 757223 1384957 NM LANDING GEAR MALFUNCTIONED A AALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 21 647AM 24605 MIA - DURING LANDING GEAR RETRACTION GEAR INDICATION ILLUMINATED. AIRCRAFT FLEW THROUGH WAKE OF AIRBUS WITH VIBRATION A ND INDICATIONS EXTINGUISHED. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. ACCOMPLISHED INSPECTION OF LANDING GEAR AND LEFT PROXIMITY SYSTEM. FOUND NO FAULTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080701 NM 2008 7 1 AALA200801575 1 20080609 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 648AA 24606 DFW - EMERGENCY LIGHT AT FORWARD SEAT 5E HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT FORWARD SEAT 5E. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 20080701 SO 2008 7 1 LR7A08079 1 20080604 A 5330 SKIN LKHEED 382 382G 526414U SO BS 134 DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 ANC - FLT 741 - DURING SCHEDULED A CHECK PER JOB CARD HA1200, FOUND FUSELAGE EXTERIOR SKIN DENT AT FS 134, WL 246, LBL 9 . REPAIR ACCOMPLISHED IAW SMP583 51-140-12 ON LOG PAGE 27957, ITEM M3. (M) 2 H 7 4 4T A1SO 20080701 NM 2008 7 1 AALA200801506 1 20080603 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 363AA 24044 DFW - EMERGENCY LIGHT AT OVERHEAD LEFT FORWARD GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD LEFT F ORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080701 EA 2008 7 1 SWIA200819730 1 20080529 A 3040 HEATER CNDAIR CL600 CL6002B19 1900309 EA WINDSHIELD MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 465SW 7845 RECEIVED A "R WSHLD HEAT" CAUTION. (FLT 6760) REPLACED THE CO PILOTS WINDSHIELD IAW MM 56-11-01. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819732 1 20080530 A 3320 BALLAST CNDAIR CL600 CL6002B19 1900309 EA LAVATORY LIGHT ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 939SW 7742 LAV HAS ELECTRICAL ODOR. REPLACED LAV LIGHTING BALLAST IAW MM 33-25-07. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080808 NM 2008 8 8 08FDEA02710 1 20080705 A 5330 65545803 SKIN BOEING 727 727225 1384077 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 RT EXT FUSE SKIN IS GOUGED FROM CONTACT WITH FASTENER TAIL BS 950D 11 INCHES, STR 26R. 2 L 7 3 4F A3WE 20080808 EU 2008 8 8 M7K2008F00102 1 20080328 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE DEFECTIVE A M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 850MH 75 4327 23472 PILOT REPORTS HAVING AN AMBER GOVERNOR LIGHT IN FLIGHT. UPON AC SHUTDOWN, A FAILURE CODE WAS GENERATED INDICATING THE C OLLECTIVE POTENTIOMETER WAS DEFECTIVE. A NEW PART WAS INSTALLED WITH NO FURTHER DEFECT REPORTED. THIS IS A RECURRING P ROBLEM FOR THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY FOR THIS MODEL AIRCRAFT. AS THIS DESIGN HAS SUCH A HIGH FAILURE RATE PERHAPS AN OPTIC DESIGN WITH NO CONTACT WITH A RESISTANCE RIBBON AS WITH THE CURRENT DESIGN SHOULD BE CONS IDERED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080808 EU 2008 8 8 M7K2008F00095 1 20080324 A 8000 350A54112420 BRACKET UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE STARTER CRACKED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 812MH 3956 FOUND CRACKED DURING ROUTINE 100 HOUR INSPECTION. THIS IS A VERY COMMON PROBLEM FOR THIS PART. SUGGEST A MORE ROBUST MA TERIAL SUCH AS SS BE UTILIZED TO REDUCE THE CRACKING OR PERHAPS A MACHINED PART. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00130 1 20080414 A 3397 WIRE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAIL LIGHT SHORTED E M7KA K NONE L NO TEST IN INSP/MAINT 1 WP 19 816MH 1976 4038 23096 DURING PREFLIGHT INSP POSITION LIGHTS FAILED TO ILLUMINATE. INVESTIGATION REVEALED CIRCUIT BREAKER HAD POPPED. A SHORT WAS LOCATED IN THE TAIL POSITION LIGHT WIRING AND A REPAIR EMBODIED. RESETTING THE BREAKER FOR A GROUND TEST REVEALED NO FUNCTION FOLLOWING WIRING REPAIR. FURTHER INVESTIGATION REVEALED THE PCB RIBBON FOR THE POSITION LIGHTS SWITCH HAD B URNED UP ON BACK OF THE SWITCH BOARD. THIS IS A COMMON FAULT FOR THIS PART AS THE CIRCUIT RIBBON FOR THIS PART IS NOT L ARGE ENOUGH TO CARRY THE CURRENT THAT THIS CIRCUIT USES WHEN A SHORT OCCURS AND THE BOARD RIBBON MELTS RAPIDLY MUCH LIKE A FUSE BEFORE THE BREAKER WILL POP WHEN A WIRING SHORT DOES OCCUR. SUGGEST THAT A REDESIGN OF THIS CIRCUIT SO THE PANE 1 G 7 2 3U 3 U H9EU E00054EN 20080811 2008 8 11 C8G2008F00008 4 20080722 A 3442 20675680501 ANTENNA BOEING 727 727225 1384077 NM PWA JT8 JT8D* NE WX RADAR SYS FAULTED A C8GA O OTHER P NO WARNING INDICATION CL CLIMB 1 SO 29 808EA 22439 AFTER TAKEOFF, THE RADAR WAS SPOKING AND WOULD NOT PAINT KNOWN BAD WEATHER. THE AC RETURNED TO DEPARTURE WHERE IT LANDE D WITHOUT INCIDENT. POST FLIGHT INSP REVEALED THE RADAR ANTENNA AT FAULT. REMOVED AND REPLACED RADAR ANTENNA, PERFORME D OPS CHECKS GOOD. NO OTHER DEFECTS WERE NOTED. AC WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F 4 F A3WE E2EA 20080811 CE 2008 8 11 DXTA200803118 1 20080613 A 3220 UNKNOWN CESSNA 750 750 2076810 CE NLG UNKNOWN E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 979QS 7500079 DURING TAKEOFF WHEN NOSE GEAR RETRACTED AN AUDIBLE BANG FOLLOWED BY LOSS OF ALL A SYS HYD QUANTITY. (B) 2 L 7 2 4J RT T00007WI 20080811 EA 2008 8 11 TRAX200800676 1 20080521 A 2910 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA HYDRAULIC SYS MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 755EV 10185 HYD NR 3 HI TEMP FOLLOWED BY HYD NR 3 LO PRESS. QRH COMPLIED WITH. HYD NR 3 PRESS RETURNED TO NORMAL WHEN GEAR EXTENDED ON FINAL APPROACH. TOWER DECLARED AN EMERGENCY TRUCKS ROLLED. REMOVED AND REPLACED PRESSURE MANIFOLD ON HYD NR 3 IAW CRJ-700 AMM 29-10-01. NO HELP. NEEDS MORE TROUBLESHOOTING. [SDR CLOSED](B) 2 L 7 2 4F RT A21EA 20080811 EU 2008 8 11 U302008F00000 1 20080604 A 7830 PIN AIRBUS 320 A320214 3930316 EU THRUST REVERSER OUT OF POSITION A U30A O OTHER W J INADEQUATE Q C WARNING INDICATION LD LANDING 1 EA 17 261AV 1615 AC WAS RELEASED FROM MAINT AFTER A HANGAR VISIT. ON LANDING, BOTH NR 1 AND NR 2 THRUST REVERSER T/R`S DID NOT DEPLOY. AC LANDED WITHOUT FURTHER INCIDENT. MAINT INSPECTED AND FOUND THE T/R HCU "QUICK RELEASE" PINS IN THE "MAINTENANCE" POS ITION. MAINTENANCE MADE BOTH T/R`S SERVICEABLE IAW AMM 78-30-081-041. C/W OPS CHECK IAW AMM 78-31-00-081-042. BOTH THRU ST REVERSERS OPS CHECKED OK. AC RETURNED TO SERVICE. (K) 2 L 7 2 4F RT A28NM 20080811 SO 2008 8 11 N582008F00000 2 20080711 A 8530 AEC631397 CYLINDER BEECH 58 58 1152740 CE CONT O550 IO550C SO LT ENGINE CRACKED E N58A O OTHER O OTHER NR NOT REPORTED 1 GL 09 58GE 768 TH1480 287391R CRACK FOUND BETWEEN FUEL INJECTION BOSS AND SPARK PLUG BOSS. (S) 1 L 7 2 3O 3 O 3A16 E3SO 20080811 EA 2008 8 11 TRAX200800679 1 20080521 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 976EV 7601 RT EMERGENCY EXTERIOR OVERWING FWD LIGHT INOP RELAMPED RT EMERGENCY EXTERIOR OVERWING FWD LIGHT IAW CRJ MM 33-51-21. OP S CHECK GOOD [SDR CLOSED](B) 2 L 7 2 4F RT A21EA 20080811 SO 2008 8 11 N932008F00000 1 20080628 A 5610 1159SCB51025 WINDSHIELD GULSTM GIVX GIVXG450 3980205 SO COCKPIT SMOKE E N93A O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 13 440QS 4025 PILOTS WINDSHIELD STARTED SMOKING FOLLOWED BY CRACKING IN NUMEROUS PLACES. (K) 2 L 7 2 4F RT A12EA 20080811 GL 2008 8 11 7KF2008F00000 2 20080722 A 7230 6890550 COMPRESSOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 1 ENGINE FOD E 7KFA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 EA 17 911LF S663 CAE835218 DURING FLIGHT WITH 2 MEDICAL PERSONNEL AND PILOT ABOARD HEADING BACK TO AIRPORT NR 1. ENGINE MADE A LOUD NOISE AND FLAM ED OUT, PILOT NOTED ENGINE INDICATIONS AND SECURED THAT ENGINE, DECLARED AN EMERGENCY WITH TOWER AND LANDED AC WITHOUT I NCIDENT. AFTER INVESTIGATION FOUND NR 1 ENGINE HAD INGESTED A CLOTH RAG, NR 1 ENGINE COMPRESSOR RECEIVED DAMAGE TO COMP RESSOR BLADES AND STATORS. (K) 1 G 7 2 3U 3 U H3EU E4CE 20080811 CE 2008 8 11 DXTA200803165 1 20080709 A 3246 WHEEL CESSNA 750 750 2076810 CE NLG VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 913QS 7500113 DURING TAKE OFF AT 40 KTS A SEVERE SHIMMY VIBRATION AT THE NOSE WHEEL THRU 55 KTS. IT WAS SO SEVERE THAT IT KICKED THE Y D LOWER. TAKEOFF GROSS WEIGHT 30,773. FUEL 8400. (A) 2 L 7 2 4J RT T00007WI 20080811 NM 2008 8 11 AALA200801761 1 20080703 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 347AN 33086 MIA - EMERGENCY LIGHT AT RT AFT CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080811 WP 2008 8 11 AALA200801715 1 20080626 A 3350 SHROUD DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7517A 49894 DFW - EMERGENCY LIGHT AT SEAT 15D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CH ECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 NM 2008 8 11 AALA200801688 1 20080623 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 381AN 25450 JFK - EMERGENCY LIGHT EXIT SIGNS AT LT AND RT OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT EXIT SIGN S AT LT AND RT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080811 NM 2008 8 11 AALA200801512 1 20080604 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AM 24594 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 18A INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 18A. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 EA 2008 8 11 A6WA200840523 1 20080618 A 5240 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BROKEN BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 444ZW 7788 BRACKET OF SERVICE DOOR INNER HANDLE MICRO SWITCH BROKEN. BRACKET OF SERVICE DOOR INNER HANDLE REPLACED. (A) 2 L 7 2 4F RT A21EA 20080811 NM 2008 8 11 USAA920081362 1 20080616 A 5311 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN C21 MAJOR REPAIR NR 6112049- FRAMES CRACKED AT BS867, S9L, WL216. REPAIRED FRAME AT BS867, S9L, WL216 IAW AWA TASKC ARD M1C53002. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081329 1 20080604 A 5330 65C3578617 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN-C21-MAJOR REPAIR-NR 6108144- CRACK IN FUSELAGE SKIN BS 500D, S12L, WL247. REPAIRED FUSELAGE SKIN BS 500D, S12L, WL 247 IAW US AIRWAYS EA 130052. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAASB08047 1 20080703 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 432US 24554 PHL MAINTENANCE REPORT THE FORWARD INTERIOR EMERGENCY LIGHTS INOPERATIVE (BATTERY DEAD). MAINTENANCE REMOVED AND REPLAC ED FORWARD EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (B) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 AALA200801525 1 20080604 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 762AN 31479 DFW - EMERGENCY LIGHTS AT SEAT 26C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 WP 2008 8 12 AALA200801533 1 20080605 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 218AA 49168 LGA - EMERGENCY LIGHT AT AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD FOR EMERGENCY LIGHT AT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801544 1 20080606 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 MIA - EMERGENCY LIGHT AT SEAT 5H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 5H. SYSTEM GROUND CHECKED NORM AL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080812 NM 2008 8 12 AALA200801546 1 20080606 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 643AA 24601 JFK - EMERGENCY LIGHT AT RT AFT OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT AFT OVERWING. SYSTEM GRO UND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 NE 2008 8 12 AALA200801602 2 20080613 A 7320 B-NUT BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4B3 NE FUEL GOVERNOR LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 613AA 24489 DEN INFLIGHT T225/13JUN BOS TO SAN. CREW REPORTED ENGINE PRESSURE RATIO INDICATION FOR NR ONE ENGINE. LANDED DEN WITHO UT INCIDENT. SECURED B-NUT ON P1 LINE FORWARD OF NR ONE ENGINE FUEL FLOW GOVERNOR. SYSTEM GROUND CHECKED NORMAL OPERAT ION. (A) 2 L 7 2 4F 4 F RT A2NM E12EU 20080812 NM 2008 8 12 AALA200801605 1 20080613 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 780AN 29956 DFW - EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801608 1 20080613 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 780AN 29956 DFW - EMERGENCY LIGHT AT SEAT 40C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 40C. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801669 1 20080619 A 2150 A/C PACK BOEING 757 757223 1384957 NM A/C BAY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 693AA 26973 MIA INFLIGHT T2107/19JUN. CREW REPORTED FUMES IN CABIN. FLIGHT ATTENDANTS REQUIRED OXYGEN. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. ACCOMPLISHED AIR CONDITIONING PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 WP 2008 8 12 AALA200801674 1 20080620 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 462AA 49592 LGA - EMERGENCY LIGHTS AT AFT TAIL COMPARTMENT INOPERATIVE. RESEATED BATTERY FOR EMERGENCY LIGHTS IN AFT TAIL COMPARTME NT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 WP 2008 8 12 AALA200801681 1 20080622 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 3507A 49801 MIA - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801632 1 20080616 A 3350 LIGHT BOEING 767 767323 1385205 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 DFW - EXTERIOR EMERGENCY LIGHT AT AFT LT DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT AFT LT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080812 NM 2008 8 12 AALA200801633 1 20080616 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 780AN 29956 DFW - EMERGENCY LIGHT AT SEAT 22G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801634 1 20080616 A 3350 PBS73 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 JFK - EMERGENCY EXIT SIGN LIGHT AT SEAT 17H INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT 17H. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080812 NM 2008 8 12 AALA200801705 1 20080625 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 24C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 24C. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 WP 2008 8 12 AALA200801622 1 20080615 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 454AA 49559 MSP - EMERGENCY LIGHTS AT SEAT ROWS 13 TO 16 INOPERATIVE. REPLACED BATTERY PACK AT B5 103 FOR EMERGENCY LIGHTS AT SEAT ROWS 13 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801625 1 20080615 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT LT NR FOUR DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LT NR FOUR DOOR. SYSTEM GR OUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801581 1 20080610 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 787AL 30010 DFW - EMERGENCY LIGHT AT LT NR ONE DOOR FORWARD CLOSET IS BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LT NR ONE DOOR FORWARD CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 WP 2008 8 12 AALA200801583 1 20080611 A 2910 HYDRAULIC LINE DOUG DC9 DC982 3022082 WP THRUST REVERSER LEAKING A AALA O OTHER K P FLUID LOSS NO WARNING INDICATION DE DESCENT 1 SW 21 460AA 49565 ORD INFLIGHT T2340/11JUN. CREW REPORTED LT HYDRAULIC QUANTITY LOSS ON DESCENT. CREW TURNED HYDRAULIC PUMP OFF FOR LT H YDRAULIC SYSTEM. LANDED ORD WITHOUT INCIDENT. AIRCRAFT TAXIED TO GATE UNDER ITS OWN POWER. REPLACED HYDRAULIC LINE ON LT THRUST REVERSER CONTROL VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 WP 2008 8 12 AALA200801586 1 20080611 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 207AA 49158 LGA - EMERGENCY LIGHT AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD ROW 20 FOR EMERGENCY LIGHT AT MID CAB IN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 WP 2008 8 12 AALA200801588 1 20080611 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 207AA 49158 LGA - EMERGENCY LIGHT AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD ROW 20 FOR EMERGENCY LIGHT AT MID CAB IN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801590 1 20080611 A 3350 LIGHT BOEING 757 757223 1384957 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 676AN 29426 DFW - EXTERNAL EMERGENCY LIGHT AT LEFT HAND AFT DOOR INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 NM 2008 8 12 AALA200801596 1 20080611 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 793AN 30255 DFW - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 WP 2008 8 12 AALA200801654 1 20080618 A 2120 SEAL DOUG DC9 DC982 3022082 WP A/C BAY LEAKING A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 423AA 49335 LAS INFLIGHT T670/18JUN. TAIL COMPARTMENT HIGH TEMPERATURE INDICATION ON CLIMBOUT INTERMITTENT. INDICATION EXTINGUISHE D WHEN POWER WAS REDUCED TO DESCEND. RETURNED TO LAS AND LANDED WITHOUT INCIDENT. REPLACED L-CLAMP AND LT AND RT PERI SEALS FROM LT AND RT VALVE TO PRIMARY HEAT EXCHANGERS. REPLACED LT AND RT TEMPERATURE SENSORS. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 SW 2008 8 12 WGEAFAA06001 1 20080625 A 2121 FAN ECLIPS EA500 ECLIPSEEA500 3350000 SW AIR CONDITIONER ODOR A WGEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 27 162DJ 000079 "BURNING ODOR COMING FROM A/C CONDENSER COOLING FAN" (A) 1 L 7 2 4J RT A00002AC 20080812 NM 2008 8 12 AALA200801782 1 20080705 A 3350 LIGHT BOEING 757 757223 1384957 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 682AA 25339 DFW - EXTERNAL EMERGENCY LIGHT AT LT NR TWO DOOR INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LT NR TWO D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 EU 2008 8 12 USAA920081393 1 20080719 A 2121 VD390100 FAN AIRBUS A321 A321211 3930370 EU CABIN ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 177US 1517 FLT 1418 LAX-PHL- DIVERSION - EN ROUTE FROM LAX TO PHL, CREW REPORTED SMOKE IN THE CABIN AND COULD NOT DETERMINE THE SOU RCE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO PIT. AFTER LANDING, THE CAPTAIN STATED THERE WAS A SULPHUR SMELL THAT BECAME MORE PRONOUNCED ON APPROACH INTO PIT. MAINTENANCE REMOVED AND REPLACED THE LT RECIRCULATION FAN. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 20080701 2008 7 1 SWIA200819733 4 20080527 A 2350 6229852106 TUNING UNIT CNDAIR CL600 CL6002B19 1900309 EA NR 1 ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 944SW 9819 9819 7764 CREW REPORTS ELECTRICAL ODOR IN COCKPIT. REPLACED RTU 1 IAW MM 23-81-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080701 NM 2008 7 1 SWAA083181 1 20080610 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULE 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 SWAA083189 1 20080610 A 3097 D648 WIRE BOEING 737 7375H4 138449D NM COCKPIT CHAFED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 519SW 25318 AIR TURNBACK/DECLARED EMERGENCY, AFTER ROTATION SMELLED SMOKE IN COCKPIT. INSPECTED AIRCRAFT FOUND WIRE BUNDLE AT P5 PA NEL CHAFFED. REPAIRED WIRE CONNECTOR AT PANEL PER WDM. 2 L 7 2 4F RT A16WE 20080701 NE 2008 7 1 SWIA200819720 2 20080601 A 7321 LINKAGE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF348C5B1 30052 NE NR 2 FCU STIFF A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 442SW 7609 NR 2 ENGINE WOULD NOT SHUT DOWN WITHOUT USING ABNORMAL FORCE ON THRUST LEVER. (FLT 3769) RIGGED NR 2 ENGINE FUEL CONTRO L LINKAGE IAW CRJ MM 76-10-00. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080701 NE 2008 7 1 SWAA083405 2 20080618 A 7230 CFM567B24 COMPRESSOR BOEING 737 7377H4 1384404 NM GE CFM56 CFM567B24 NE NR 1 ENGINE STALLED A SWAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 29 735SA 874933 27867 874933 DIVERSION/DECLARED EMERGENCY, CLIMBING THROUGH 3000' AGL NR 1 ENGINE COMPRESSOR STALLED, VIBRATION OCCURRED, ENGINE FLUC TUATED. R&R NR 1 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080701 NM 2008 7 1 SWAA083407 1 20080619 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500A, BL0 TO RBL 3, WL 148. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 SWAA083396 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 SWAA083395 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 DL76G080867 1 20080612 A 3245 TIRE BOEING 767 767332 1382001 NM MLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 SO 27 173DZ 29692 FLIGHT 74/12 MEDICAL DIVERTED INTO ORF AND IN THE PROCESS BLEW 4 MAIN TIRES. SENT AMT'S FROM ATL TO REPLACE AND INSPECT . 2 L 7 2 4F RT A1NM 20080701 NM 2008 7 1 DL757080868 1 20080613 A 5320 ANGLE BOEING 757 757232 1384965 NM BS 1540-1560 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 AFT CARGO PIT STA 1540-1560 STR 27R WEB "L" ANGLE CORRODED. REPLACED "L" ANGLE IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 20080701 NM 2008 7 1 SWAA083371 1 20080619 A 5315 6546810 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 968, RBL 28 TO RBL 45. REPAIRED FLOORBEAM PER SR M. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 SWAA083372 1 20080619 A 5311 65C25228 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083377 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083386 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083370 1 20080619 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 15 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083158 1 20080610 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 USAA920081383 1 20080711 A 3350 20120 CHARGER BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 533AU 24515 CLT-C3-EEL - AFT LT ENTRY DOOR EXTERIOR EMERGENCY LIGHT DOES NOT COME ON. RE-LAMPED AFT LT ENTRY DOOR EXTERIOR EMERGENC Y LIGHT, REPLACED LAMP SOCKET AND REPLACED FAILED BATTERY CHARGER ASSY. (A) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 USAA920081397 1 20080716 A 5320 69414372 TIE CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT - Q3 - MAJOR REPAIR - TIE CLIP CRACKED AT BS 663 S10L. REPLACED TIE CLIP AT BS 663 S10L IAW B737 SRM 53-60-08. (A) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 USAA920081384 1 20080714 A 5311 651630349 FRAME BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT - Q3-MAJOR REPAIR - LEVEL 2 CORROSION ON FORWARD SIDE OF FRAME WEB AT BS 203.3 RBL 4. REPLACED FRAME WEB BS 203.3 R BL 4, IAW US AIRWAYS EA 100558. (A) 2 L 7 2 4F RT A16WE 20080812 EU 2008 8 12 USA2008F00006 1 20080717 A 3350 32146210 EPSU AIRBUS 330 A330323 3930335 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 277AY 34901 0380 PHL - DOOR 2L EMERGENCY POWER SUPPLY UNIT FAULTED. MAINTENANCE REPLACED THE DOOR 2L EMERGENCY POWER SUPPLY UNIT. OPERA TIONALLY CHECKS OK. (A) 2 L 7 2 4F RT A46NM 20080812 NM 2008 8 12 USA2008F00007 1 20080717 A 2560 P2070003001 FLASHLIGHT BOEING 757 7572B7 1384964 NM CABIN DEFECTIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 PHL - THE FORWARD FLIGHT ATTENDANT FLASHLIGHT STATUS LIGHT DID NOT BLINK, BUT WAS OTHERWISE OPERATIONAL. MAINTENANCE RE PLACED THE FLASHLIGHT. OPERATIONALLY CHECKS OK. (A) 2 L 7 2 4F RT A2NM 20080812 NM 2008 8 12 USA2008F00010 1 20080712 A 2910 LJ38085 DRAIN BOEING 757 7572B7 1384964 NM HYDRAULIC SYS CRACKED A USAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 19 942UW 27807 PHL FLT 723 - EN ROUTE DUB TO PHL. DURING DESCENT INTO PHL, THE LT HYDRAULIC SYSTEM QUANTITY DECREASED TO ZERO AND THE SYSTEM PRESSURE LIGHT ILLUMINATED. ALSO, EICAS MESSAGE "G L HYD SYS PRESS" DISPLAYED. THE FLIGHT LANDED SAFELY AND WAS ABLE TO TAXI OFF THE RUNWAY, BUT WAS TOWED TO THE GATE. MAINTENANCE REPLACED A HYDRAULIC DRAIN TUBE. SYSTEM OPERATION ALLY AND LEAK CHECKS OK. (A) 2 L 7 2 4F RT A2NM 20080812 NM 2008 8 12 USAA920081438 1 20080730 A 5320 65496795 INTERCOSTAL BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT-C2-MAJOR REPAIR - CORROSION ON INTERCOSTAL WEB FLANGE AT BS 947 TO 953.5 BL 0. REPAIRED INTERCOSTAL WEB FLANGE AT B S 947 TO 953.5 BL 0 IAW B737 SRM 51-70-11. (A) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 USAA920081439 1 20080728 A 5330 6545774 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT-C2- MAJOR REPAIR - FUSELAGE SKIN CRACKED AT BS 727E BELOW S22L. REPAIRED FUSELAGE SKIN AT BS 727E BELOW S22L IAW B7 37 SRM 53-00-01 AND TYPICAL REPAIR, 53-27, REPAIR 31. (A) 2 L 7 2 4F RT A16WE 20080812 EU 2008 8 12 USAA920081445 1 20080708 A 5754 D5746002820600 BOLT AIRBUS 320 A320231 3930325 EU SLAT TRACK CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 627AW 66 SAL-C6 MAJOR REPAIR - CORRODED ON BOLT THREADS ON LT WING NR 9 SLAT TRACK. REPLACED BOLT ON LT WING NR 9 SLAT TRACK IAW A320 AMM 27-84-62. (A) 2 L 7 2 4F RT A28NM 20080812 WP 2008 8 12 AALA200801675 1 20080620 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 462AA 49592 LGA - EMERGENCY LIGHTS AT OVERHEAD LT NR ONE DOOR GALLEY INOPERATIVE. RESEATED BATTERY FOR EMERGENCY LIGHTS AT OVERHEAD LT NR ONE DOOR GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801618 1 20080615 A 3350 LENS BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 968AN 30095 DFW - EMERGENCY LIGHT AT SEAT 14F MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 14F. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 AAL200801719 1 20080627 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 672AA 25337 DFW - EMERGENCY LIGHT AT SEAT 4B BULLNOSE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 4B BULLNOSE. SYSTEM G ROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 NM 2008 8 12 AALA200801627 1 20080615 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 32G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 WP 2008 8 12 AALA200801599 1 20080612 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 416AA 49327 LGA - EMERGENCY FLASHLIGHT SAFETY STRAP AT FORWARD UPPER POSITION MISSING. REPLACED SAFETY STRAP FOR EMERGENCY FLASHLIG HT AT FORWARD UPPER POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801780 1 20080705 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 DFW - EMERGENCY LIGHT AT RT NR THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT NR THREE DOOR. SYSTEM G ROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801779 1 20080705 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 781AN 29586 DFW - EMERGENCY LIGHT ASSEMBLY AT LT NR ONE CLOSET LOOSE. SECURED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LT NR ONE CLOSE T. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 EU 2008 8 12 08FDEA02635 1 20080702 A 5320 A5378198422000 BRACKET AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN UNDER FLOOR PANEL 231 AH AT FRAME 28; THE SUB-FLOOR PANEL IS CORRODED. FOUND TO BE OUT OF LIMITS REF A300-60 0 SRM 53-14-15. REMOVED PANEL NR 131 DC TO FOM. REF A300-600 SRM 51-40-21. LOCATED AND DRILLED BRACKET REF A300-600 SRM 51-40-44. BRACKET WAS INSTALLED REF A300-600 SRM 51-40-21; PARA 4-7. APPLIED CIC REF A300-600 AMM 51-22-00-0. INS TALLED PANEL 131 DC PER AIRBUS PMS 01-05-17. 2 L 7 2 4F RT A35EU 20080811 EU 2008 8 11 M7K2008F00101 1 20080414 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE DEFECTIVE E M7KA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 812MH 3956 23036 PILOT REPORTS HAVING AN AMBER GOVERNOR LIGHT IN FLIGHT. UPON AC SHUTDOWN, A FAILURE CODE WAS GENERATED INDICATING THE C OLLECTIVE POTENTIOMETER WAS DEFECTIVE. A NEW PART WAS INSTALLED WITH NO FURTHER DEFECT REPORTED. THIS IS A RECURRING P ROBLEM FOR THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY FOR THIS MODEL AIRCRAFT. AS THIS DESIGN HAS SUCH A HIGH FAILURE RATE PERHAPS AN OPTIC DESIGN WITH NO CONTACT WITH A RESISTANCE RIBBON AS WITH THE CURRENT DESIGN SHOULD BE CONS IDERED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 CE 2008 8 11 DXTA200803111 1 20080611 A 3260 INDICATION SYS CESSNA 750 750 2076810 CE MLG MALFUNCTIONED E DXTA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 916QS 7500116 WHEN SELECTING THE LANDING GEAR DOWN DURING APPROACH, THE GREEN LIGHT FOR THE LEFT MAIN GEAR DID NOT COME ON. (B) 2 L 7 2 4J RT T00007WI 20080811 NM 2008 8 11 AALA200801580 1 20080610 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 787AL 30010 DFW - EMERGENCY LIGHT AT SEAT ROW 34C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 34C. SYSTEM GROUND CH ECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080811 WP 2008 8 11 AALA200801645 1 20080617 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 234AA 49181 LGA - EMERGENCY LIGHTS AT AFT OVERWING INOPERATIVE. RESECURED BATTERY PACK TO SEAT ROW 21 FOR EMERGENCY LIGHTS AT AFT O VERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 NM 2008 8 11 AALA200801611 1 20080613 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 636AM 24594 DFW - EMERGENCY LIGHT AT SEAT 20C BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECK ED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 NM 2008 8 11 MWE2008F00023 1 20080725 A 5350 LATCH BOEING 717 717200 1383700 NM TAILCONE FAILED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 927ME 55193 WHILE PERFORMING TAILCONE FUNCTIONAL CHECK, INTERIOR HANDLE FAILED TO PULL FROM THE CLIPS. CLEANED DEBRIS AND MINOR COR ROSION FROM INNER SURFACES OF RETENTION CUPS. INTERIOR TAILCONE RELEASE HANDLE FORCE CHECKS NOW. (K) 2 L 7 2 4F TR A6WE 20080811 WP 2008 8 11 MWE2008F00022 1 20080726 A 4990 OIL SYSTEM DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE APU LEAKING A MWEA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 13 809ME H10189C 48071 FAINT ODOR DETECTED AND RIGHT AFT LAVATORY SMOKE DETECTOR WENT OFF AND LIGHT GRAY SMOKE WAS VISUAL. FOUND THE OIL LEAK WAS NOT CLEANED ENOUGH FROM PREVIOUS ISSUE ON 7/25/2008, REMOVED AND REPLACED APU. (K) 2 L 7 2 4F 4 F A6WE E2EA 20080811 NM 2008 8 11 AALA200801768 1 20080703 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 SFO - EMERGENCY LIGHT AT LT AFT CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LT AFT CABIN. SYSTEM GROUND CH ECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080811 NM 2008 8 11 AALA200801707 1 20080625 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 DFW - EMERGENCY LIGHT AT FORWARD GALLEY AT RT FORWARD POSITION INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD GALLEY AT RT FORWARD POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080811 EA 2008 8 11 A6WA200840520 1 20080610 A 5320 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 444ZW 7788 NR 1 AND NR 2 HYDRAULIC SUPPORT BRACKETS CRACKED ON THE AFT LOWER EDGE. REPAIR PERFORMED ON NR 1 AND NR 2 HYDRAULIC MAN IFOLD SUPPORT BRACKETS IAW CRJ 200 REO 601R-53-61-031 REV A. (A) 2 L 7 2 4F RT A21EA 20080811 EU 2008 8 11 AALA200801743 1 20080701 A 2910 HYDRAULIC LINE AIRBUS 300 A300B4605R 3930308 EU KRUEGER FLAP LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 21 59081 639 MIA INFLIGHT (T1812/01JUL). CREW REPORTED GREEN SYSTEM HYDRAULIC PRESSURE LOW INDICATION ON APPROACH. MANUALLY LOWERED GEAR. LANDED MIA WITHOUT INCIDENT AND AIRCRAFT WAS TOWED TO GATE. SERVICED GREEN HYDRAULIC SYSTEM AND RESTORED FREE F ALL EXTENSION HANDLE. ON 6 JUL FOUND PIN HOSE IN KRUEGER FLAP PRESSURE LINE ON LT SIDE OF AIRCRAFT AT SEAT ROW 16AB. R EPAIRED KRUEGER FLAP PRESSURE LINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080811 NM 2008 8 11 USAA920081351 1 20080701 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT- MAJOR Q3 CHECK NR 03C10853029/010, LEVEL 2 CORROSION ON "Z" ANGLE FITTING, BS914, LBL54. REPLACED "Z" ANGLE FITTIN G, BS914, LBL 54 IAW B737 SRM 51-10-02. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAABB08113 1 20080709 A 4960 211734220 ECU BOEING 757 7572S7 1384962 NM APU FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 903AW 23323 HNL FLT 119 ENROUTE KOA-PHX FLIGHT DIVERTED TO HNL. APU AUTO SHUTDOWN BEFORE ETOPS MIDPOINT. CREW ELECTED TO DIVERT T O HNL. CREW STATES "FRM #49-11-XB-00, APU AUTO SHUTDOWN IN FLIGHT TWO ATTEMPTS (START) EICAS STATUS PAGE. APU OIL QTY O N DESCENT INTO HNL" MAINTENANCE STATES, "APU BITE INDICATED BAD ECU. REMOVED AND REPLACED ECU. (B) 2 L 7 2 4F RT A2NM 20080811 NM 2008 8 11 USAA920081359 1 20080606 A 5755 654645262A SPOILER BOEING 737 73733A 1384673 NM NR 5 DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN- C21 MAJOR REPAIR NR 6062981, 6111534, AND 6062978- NR 5 SPOILER DISBONDED AT WBL99. REPLACED NR 5 SPOILER AT WBL95 TO WBL99 IAW B737 AMM 27-62-15-4 AND 27-62-12-5. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081344 1 20080628 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT- MAJOR REPAIR Q3 CHECK NR 03C10753060/006, LEVEL 2 CORROSION ON CABIN FLOORBEAM "T" CAP, BS 328, BL0 - RBL36. REPLA CED CABIN FLOORBEAM "T" CAP, BS 328, BL0-RBL36 IAW B737 SRM 53-10-51 FIG 201. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081346 1 20080630 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT- MAJOR REPAIR Q3 CHECK NR 03C10863029/015, LEVEL 2 CORROSION ON THE ENTIRE CABIN FLOORBEAM "T" CAP, BS 985.5. REPLA CED THE ENTIRE CABIN FLOORBEAM "T" CAP, BS 985.5 IAW US AIRWAYS TR 53-60-10A. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081338 1 20080607 A 5330 6545776Y55 SKIN PANEL BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN- C21 MAJOR REPAIR NR 6064882- CORROSION ON SKIN PANEL BS 947.5 TO 967 S27L WL179. REPLACED SKIN PANEL BS 947.5 TO 9 67 S27L WL179 IAW B737 SRM 51-40-02-0G (B) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 AALA200801518 1 20080604 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 762AN 31479 DFW - EMERGENCY LIGHTS AT SEAT 23G MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801603 1 20080613 A 3350 PBS73 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 630AA 24588 JFK - EMERGENCY LIGHT AT OVERHEAD LT NR TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD LT NR TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 NM 2008 8 12 AALA200801635 1 20080616 A 3350 PBS73 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 JFK - EMERGENCY EXIT SIGN LIGHT AT SEAT 17B INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT 17B. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080812 NM 2008 8 12 AALA200801664 1 20080618 A 3350 SHROUD BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 698AN 26980 DFW - EMERGENCY LIGHT AT SEAT 15D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECK ED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 EU 2008 8 12 AALA200801690 1 20080623 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 80058 466 MIA - EMERGENCY LIGHTS AT SEAT ROWS 19A TO AFT OF CABIN DIM. CHARGED BATTERIES FOR EMERGENCY LIGHTS AT SEAT ROWS 19A TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080812 NM 2008 8 12 AALA200801593 1 20080611 A 3350 LENS BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 676AN 29426 DFW - EMERGENCY LIGHT AT SEAT 33D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 33D. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 NM 2008 8 12 USAA920081395 1 20080721 A 5330 6545776 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 PHX-WEEKLY- MAJOR REPAIR - CRACK IN FUSELAGE SKIN BS 877 S24R. REPAIRED FUSELAGE SKIN BS877 S24R IAW B737 SRM 53-00-01- 1A-1. (A) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 USAA920081385 1 20080722 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 PHX - DROP-IN - FUSELAGE SKIN CRACKED ABOVE BS 727D S24L. REPAIRED FUSELAGE SKIN ABOVE BS 727D S24L IAW B737 SRM 53-00- 01 FIG 201 DETAIL 10. (A) 2 L 7 2 4F RT A16WE 20080812 NE 2008 8 12 USA2008F00008 2 20080717 A 7230 FAN BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE OUT OF BALANCE A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 942UW 27807 30529 PHL - FLT 722 EN ROUTE (PHL TO DUB). DURING CLIMBOUT FROM PHL THE RT ENGINE INDICATED VIBRATION OF 2.5 WITH SPIKES UP T O 2.8. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A FAN TRIM BALANCE. VI BRATION LEVELS WITHIN ACCEPTABLE LIMITS. (A) 2 L 7 2 4F 4 F RT A2NM E12EU 20080812 EU 2008 8 12 AALA200801600 1 20080612 A 3350 LENS AIRBUS 300 A300B4605R 3930308 EU CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14065 508 JFK - EMERGENCY LIGHT AT SEAT 24C MISSING LENS. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080812 WP 2008 8 12 AALA200801746 1 20080701 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 587AA 53250 LGA - EMERGENCY LIGHT AT GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 WP 2008 8 12 AALA200801598 1 20080612 A 3350 P2010031303 LIGHT DOUG DC9 DC983 3022083 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 589AA 53252 ORD - EMERGENCY EXIT SIGN LIGHT AT RT SIDE OF AFT GALLEY EXIT DOOR BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT S IGN LIGHT AT RT SIDE OF AFT GALLEY EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A6WE 20080812 WP 2008 8 12 AALA200801714 1 20080626 A 3350 SHROUD DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7517A 49894 DFW - EMERGENCY LIGHT AT SEAT AT 13D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 08FDEA02837 1 20080712 A 5720 692043726 BRACKET BOEING 727 727225 1384077 NM RT WING MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 RIGHT WING TANK UNIT (PROBE) CONTACTING STRINGER 11 REPAIR AT WS 686.5. FABRICATED NEW QUANTITY INDICATOR BRACKET AND I NSTALLED. REF EA NR 7-5710-114010. THIS IS CLASSIFIED AS A MAJOR. 2 L 7 3 4F A3WE 20080812 NM 2008 8 12 08FDEA02840 1 20080712 A 5511 65382031 SPAR BOEING 727 727225 1384077 NM HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 CORROSION ON LT HORIZ STAB REAR SPAR LOWER CHORD, STAB STA 108.5 BLENDED CHORD, ORIGINAL THICKNESS .110 INCH, MATERIAL R EMOVED .027 INCH MATERIAL REMAINING .083 INCH. REPAIRED CHORD REF EA 7-5510-114006 DATED 7-11-08. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080812 NM 2008 8 12 USA2008F00019 1 20080724 A 5270 WARNING SYSTEM EMB ERJ190 ERJ190100IGW 3260408 NM COCKPIT ACTIVATED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 951UW 19000112 PIT FLT 1557 EN ROUTE PIT TO CLT. AT FL 290, RECEIVED EICAS MESSAGE "FWD CABIN DOOR OPEN" PRESSURIZATION WAS NORMAL. HOWEVER, ONLY PARTIAL GREEN DOOR LOCK INDICATION. FOLLOWED QRH PROCEDURES AND RETURNED TO FIELD PIT. FLIGHT LANDED WIT HOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. AIRCRAFT CURRENTLY ON MEL. (A) 2 L 7 2 4F RT A57NM 20080812 NM 2008 8 12 USAA920081406 1 20080630 A 5310 507945264 DOOR FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT-Q3- MAJOR REPAIR - EXTERIOR FRAME CRACKED ON AFT SIDE AT NR 7 STOP PIN ACCESS HOLE. REPAIRED EXTERIOR FRAME AT NR 7 STOP PIN ACCESS HOLE IAW US AIRWAYS EA 100547. (A) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 USAA920081409 1 20080630 A 5210 507945264 STRUCTURE BOEING 737 737401 1384701 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT-Q3- MAJOR REPAIR - PASSENGER DOOR CRACKED AT NR 5 STOP PIN ACCESS HOLE ON FORWARD SIDE. REPAIRED PASSENGER DOOR AT NR 5 STOP PIN ACCESS HOLE IAW US AIRWAYS EA 100547. (A) 2 L 7 2 4F RT A16WE 20080813 EU 2008 8 13 08FDEA02905 1 20080715 A 5311 FRAME AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 719FD 388 AIR COND BAY HAS CORROSION ON UPPER SURFACE OF "T" ON FR 39 BETWEEN STR 50 AND STR 51 RT SIDE. REMOVED AND REPLACED "T" SECTION FROM STRINGER 53 RHS TO STRINGER 49 RHS. THE NEW "T" SECTION HAS BEEN SPLICED WITH ANGLE ON AFT FACE AND PLATE ON FORWARD FACE. IN COMPLIANCE WITH EA 6-5310-110880 PT 1. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02656 1 20080703 A 5321 B5327071400400 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN DECK FLOOR BOARD NR 251 XH IS CRACKED. REPAIRED DAMAGED AREA IAW A300-600 SRM 51-77-11. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02657 1 20080703 A 5321 B5327071400400 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN DECK FLOORBOARD NR 251 XG EDGE IS DETERIORATED. REPAIRED EDGE IAW FEDEX DWG SRZ 25-005, REV F. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02665 1 20080703 A 5321 B5327048401800 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN FLOOR PANEL 231 WG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED IAW A300-600 SRM 53-10- 20; FIG 201. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02667 1 20080703 A 5321 B5327045900400 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN FLOOR PANEL 231 FG HAS NUMEROUS PUNCTURES IN THE UPPER SURFACE FROM BALL BEARINGS. REPAIRED DAMAGED AREAS IA W A300-600 SRM 53-10-20; FIG 201. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02674 1 20080703 A 5321 B5327048900200 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CARGO DECK FLOOR PANEL 232 RG HAS PUNCTURES AND BALL BEARINGS STUCK IN THE UPPER SURFACE. REPAIRED DAMAGED FLOOR P ANEL IN REF TO A300-600 SRM 53-10-20; FIG 202. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02676 1 20080703 A 5321 B5327051200200 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CARGO DECK FLOOR PANEL FROM FRAME 22 TO FRAME 26, RBL 37 TO RBL 57 HAS NUMEROUS BALL BEARINGS STUCK AND PUNCTURES ON THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202. 2 L 7 2 4F RT A35EU 20080813 NM 2008 8 13 08FDEA02876 1 20080715 A 3260 SWITCH BOEING 727 727233 138408A NM NLG MALFUNCTIONED A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 CE 21 266FE 21672 DURING NORMAL LANDING GEAR EXTENSION RECEIVED UNSAFE NLG INDICATION. C/W QRH, LIGHT TEST OK, USED MANUAL NLG GEAR EXT A ND RECEIVED SAFE NLG IND AFTER ONLY 1/4 TURN OF HAND CRANK. SWUNG NOSE GEAR SEVERAL TIMES PER 727-200 MM 07-11-000-2 CN D. REMOVED AND REPLACED NLG LOCK AND POSITION SWITCHES PER 727-200 MM 32-61-071-4, OPS CHECKS GOOD. ALSO COMPLIED WITH TSI 32-20/0003 NOSE GEAR LUBE. 2 L 7 3 4F RT A3WE 20080813 EU 2008 8 13 08FDEA02859 1 20080714 A 5755 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 5 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND DELAMINATION ON LT SPOILER NR 5 OUT OF SRM LIMIT. REPAIR PERFORMED BY REPLACEMENT OF SPOILER NR 3 RT IAW AMM 27-6 1-53 PAGE 401. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02856 1 20080605 A 5313 A53986212 STRINGER AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 AFT CARGO COMPT, STRINGER 54 LT WITH CORROSION BETWEEN FR 65 AND FR 66. STRINGER 54 LT WAS REPAIRED AS PER SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02894 1 20080715 A 5330 A53610945200 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND LIGHTNING STRIKE AT FRAME 5-7, 11 O`CLOCK POSITION. REPAIR PERFORMED BY BUSH INSTALLATION IAW SRM 53-10-12 FIG 22 1. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02677 1 20080703 A 5321 B5327048402200 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CARGO DECK FLOOR PANEL 232 NG HAS BALL BEARINGS (2 PLACES) STUCK IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02680 1 20080703 A 5321 B5327048402800 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CARGO DECK FLOOR PANEL 232 TG HAS PUNCTURES AND BALL BEARINGS IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02688 1 20080703 A 5321 B5327047600600 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CARGO DECK FLOOR PANEL 232 ZG HAS BALL BEARINGS STUCK AND PUNCTURES ON THE TOP SURFACE. REPAIRED DAMAGED FLOOR PAN EL IN REF TO A300-600 SRM 53-10-20, FIG 202. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02689 1 20080703 A 5321 B5327047601600 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CARGO DECK FLOOR PANEL 232 AH HAS BELL BEARINGS STUCK AND PUNCTURES ON THE TOP SURFACE. REPAIRED DAMAGED FLOOR PAN EL IN REF TO A300-600 FIG 202. 2 L 7 2 4F RT A35EU 20080813 NM 2008 8 13 08FDEA01963 1 20080522 A 5100 NONE BOEING 757 75723A 1384967 NM NO DAMAGE NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 919FD 24636 EXTERNAL PATCH REPAIR ON FUSELAGE FROM BS 1701 TO BS 1708, BETWEEN S-17L AND S-19L TO BE EVALUATED. EXISTING REPAIR EVA LUATED AS PER EO F-5100-7-5001 PT1 ATTACHMENT B, FOUND PREVIOUSLY ACCOMPLISHED BY ENGINEERING LIMITED REPAIR NO: MON/757 /53-252/REP/502 ISSUE B. REPAIR RE-INSPECTED AS PER FEDEX EA: F-5310-120564 AND EA F-5310-120565. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080813 EU 2008 8 13 08FDEA02869 1 20080701 A 5754 A5786452400200 BOLT AIRBUS 300 A300F4605R 3930327 EU SLAT TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 LEFT WING NR 2 SLAT, NR 7 TRACK LOWER BOLT ID CRACKED. REPLACED DAMAGED BOLT WITH A NEW LOWER BOLT IAW A300-600 AMM 27- 80-12-4. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02871 1 20080710 A 5754 A5786452400200 BOLT AIRBUS 300 A300F4605R 3930327 EU SLAT TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 RIGHT WING NR 2 SLAT, NR 7 TRACK LOWER MOUNT BOLT IS CRACKED. REMOVED RIGHT WING NR 2 SLAT, NR 7 TRACK LOWER MOUNT BOLT AND INSTALLED NEW NR 2 SALT; NR 7 TRACK LOWER MOUNT BOLT IAW FEDEX A300-600 AMM 27-80-12-4. 2 L 7 2 4F RT A35EU 20080813 WP 2008 8 13 08FDEA02507 1 20080626 A 5100 NONE DOUG MD10 MD1010F 3022112 WP NOT AN SDR NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 383FE 46616 FOUND A REPAIR LOCATED AT STA 1517-1527; STRINGER 46R THAT REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPA IR WAS INSTALLED USING FAA APPROVED DATA. EVALUATED REPAIR AND FOUND NO APPROVED FAA DATA. REPAIRED IAW FEDEX EA 8-531 0-118524 "FUSELAGE - STA 1521 BULKHEAD TEE CAP AT L-46R - REPAIR". 2 L 7 3 4F RT A22WE 20080813 NM 2008 8 13 NWAA082533118 1 20080605 A 2913 PUMP AIRBUS A319 A319114 3930350 NM HYD SYSTEM LEAKING A NWAA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 318NB 19088 769 1325 HYDRAULIC-G RSVR LO LVL, G ENG1 PUMP LOW PSI, GREEN HYDRAULIC QUANTITY ZERO, DETECTED STRONG SIMILAR ODOR DURING TAKEOFF ROLL THAT DISSIPATED DURING CLIMB. REPLACED NR 1 ENGINE DRIVEN PUMP, CHECKS OK. (A) 2 L 7 2 4F RT A28NM 20080813 WP 2008 8 13 NWAA082816743 1 20080618 A 2120 HOSE DOUG DC9 DC932 3022066 WP CABIN AIR DISCONNECTED A NWAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 945N 47664 FLT WAS PASSING THROUGH FL 280 WHEN THE RED "CABIN PRESS" LIGHT AND YELLOW "MASTER CAUTION" LIGHT BOTH ILLUMINATED. CRE W SAW CABIN PRESSURIZATION WAS AT 10,500 FT AND CLIMBING. COM PROCEDURES WERE APPLIED BUT CABIN PRESSURE WAS NOT CONTROL LABLE. COCKPIT CREW EXECUTED AN EMERGENCY DESCENT TO 10,00 FT. THE MAXIMUM INDICATED ALTITUDE THE CABIN REACHED WAS 12 ,500 FT BUT THE MASKS DID NOT DEPLOY. THE FLIGHT RETURNED TO A NORMAL LANDING BACK AT MSP. MAINTENANCE FOUND THE LT AC M OUTLET DUCT WAS DISCONNECTED FROM THE HOSE CONNECTION AND THE RT PACK PRECOOLER INLET HOSE WAS NOT COMPLETELY SECURED BY THE CLAMP. THE BOOT AND CLAP WERE REPLACED, LEAK CHECK PERFORMED AND SYSTEM RETURNED TO OPERATIONAL STATUS. (A) 2 L 7 2 4F A6WE 20080813 WP 2008 8 13 NWAA082859864 1 20080622 A 2161 CONTROLLER DOUG DC9 DC951 3022051 WP CABIN TEMP MALFUNCTIONED A NWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 773NC 21220 1622 47775 JUST AS THE AIRCRAFT TOOK OFF, THE COCKPIT CREW DETECTED SMOKE AND FWD LAVATORY SMOKE DETECTOR ACTIVATED. CREW REPORTED "EXTREME HEAT" AND SMOKE FILLED CABIN AREA. RED-BORDER COM PROCEDURES WERE COMPLIED WITH AND ACFT RETURNED TO CMH WITH CFR STANDING-BY. CREW PERFORMED AN OVER-WEIGHT LANDING AND BRAKES FUSED UPON STOPPING. PAX DID NOT EVACUATE BUT WERE DEPLANED THROUGH AFT STAIRS. NO FIRE OR EVIDENCE OF BURNING WAS FOUND. MAINTENANCE REPLACED THE RT PACK TEMPERATURE CO NTROLLER FOR FAILING TO RUN COLD, EXECUTED THE PACK BURN-OUT PROCEDURES BECAUSE OF SMOKE, REPLACED THE COALESCER BAGS, L EAK CHECKED AND FUNCTIONALLY CHECKED ALL APPLICABLE SYSTEMS AND RETURNED THE AIRCRAFT TO SERVICE. (A) 2 L 7 2 4F RT A6WE 20080813 2008 8 13 NWAA082899928 4 20080620 A 2565 SLIDE DOUG DC9 DC931 3022065 WP TAILCONE NO TEST A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8921E 45836 THE EMERGENCY ESCAPE SLIDE FOR THE TAIL CONE EMERGENCY EXIT HATCH FAILED TO INFLATE COMPLETELY DURING DEPLOYMENT CHECK F OLLOWING SLIDE REPLACEMENT AFTER AN ODI EVENT. THE ATTEMPT TO INFLATE THE SLIDE WAS AN ENGINEERING DECISION AS PART OF THE ON-GOING ODI EVENT INVESTIGATION. THE SLIDE WAS "SERVICEABLE OUT OF STOCK" AND HAD JUST BEEN INSTALLED ON THE AIRCR AFT TO REPLACE THE ORIGINAL SLIDE WHICH CAUSED THE ODI EVENT. (A) 2 L 7 2 4F A6WE 20080813 WP 2008 8 13 NWAA082969613 1 20080703 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 613NW 47438 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN LIGHT FOR BOTH OF THE AFT OVERWING HATCHES WERE INOPER ATIVE. MAINTENANCE REPLACE TWO OF THE BATTERY PACKS AND THE SIGN LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (A) 2 L 7 2 4F A6WE 20080813 WP 2008 8 13 NWAA082979762 1 20080602 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP EMERGENCY LIGHTS MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 762NW 47395 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 20-23 OF THE CABIN WERE INOPERATIVE. T HE BATTERY PACK WAS "RESET" BY MAINTENANCE AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (A) 2 L 7 2 4F A6WE 20080813 NM 2008 8 13 NWAA082993140 1 20080705 A 2913 PUMP AIRBUS A319 A319114 3930350 NM HYD SYSTEM FAILED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 340NB 25544 25544 01714 IN FLIGHT GOT "HYD RSVR LO LEVER" ECAM. CONFIRMED YELLOW HYDRAULIC LEVEL AT ZERO. COMPLIED WITH ECAM & COM PROCEDURES. LANDED AND TAXIED AND UNEVENTFULLY. REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP. CHECKS GOOD. (A) 2 L 7 2 4F RT A28NM 20080813 WP 2008 8 13 NWAA082959928 1 20080620 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8921E 45836 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING ARM AND CHARGE CIRCUIT BREAKERS WERE TRIPPED AN D WOULD NOT RESET. MAINTENANCE REPLACED THE R5-50 POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM. (A) 2 L 7 2 4F A6WE 20080813 WP 2008 8 13 NWAA082949753 1 20080701 A 3397 CONNECTOR DOUG DC9 DC941 302207N WP EEL POWER SUPPLY LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 753NW 47117 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 9-10 OF THE CABIN WERE INOPERATIVE. MA INTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND CORRECTED A LOOSE CONNECTION; THEN OPERATIONALLY CHECKED THE SYS TEM. (A) 2 L 7 2 4F A6WE 20080702 NM 2008 7 2 SWAA083159 1 20080610 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 2008UALA03574 1 20080624 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY LIGHT ROW 24 LT INOP. FOUND BURNED OUT LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03567 1 20080623 A 2611 824PTY SMOKE DETECTOR BOEING 737 737322 1384676 NM LAVATORY FAULTY A UALA O OTHER W N INADEQUATE Q C FALSE WARNING IN INSP/MAINT 1 WP 29 348UA 24252 FA REPORTS SMOKE DETECTOR IN AFT RT LAV GOING OFF FOR NO APPARENT REASON. SUSPECT FAULTY SMOKE DETECTOR. REPLACED SMOKE DETECTOR OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 2008UALA03566 1 20080622 A 2741 90G97600U PRESSURE SWITCH BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE COCKPIT FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 674UA 29242 EICAS MSG STAB TRIM DISPLAYED & STAB TRIM LIGHT ILLUMINATED. STABILIZER TRIM RATE NORMAL. FOUND FAULTY PRESSURE SWITCH. REPLACED RT STAB MODULE BRAKE PRESSURE SWITCH. PER MM 27-41-07. OPS CHECK GOOD, LEAK CHECK GOOD, AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080702 NM 2008 7 2 2008UALA03564 1 20080623 A 5320 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 811UA 847 BEAM 150 FOUND CORRODED. ACCOMPLISHED MAJOR REPAIR AT DEN-REMOVED BEAM 150, TRANSFERRED GALLEY MOUNT FITTING AND 5 CLAM P BRACKETS, PICKED UP HOLES FOR SPLICE AT FWD JOINT. COMPLETED BEAM 150 INSTALLATION. 2 L 7 2 4F 4 F RT A28NM E40NE 20080702 NM 2008 7 2 2008UALA03557 1 20080623 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 FWD PIT STA 660 STR 24 - 25R FRAME DENTED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 53-00-07. THIS IS A CAT B REPAIR IN ZONE 2 AND REQUIRES SUPPLEMENTAL INSPECTIONS STARTING IN 25000FC AND 11000FC THEREAFTER. THIS INSP C ONSISTS OF BOTH DETAIL VISUAL AND NDT PER SRM 53-00-07. 2 L 7 2 4F 4 F RT A2NM E17NE 20080702 NM 2008 7 2 2008UALA03556 1 20080623 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 MAIN CABIN BS 324 FLOORBEAM UPPER T -CAP CORRODED RBL 50. REPLACED T-CAP IAW SRM 51- 40-02. 2 L 7 2 4F 4 F RT A2NM E17NE 20080702 NM 2008 7 2 2008UALA03555 1 20080623 A 5320 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 FUSELAGE STA 540 HAS DENT BETWEEN STR 24 AND 25. REMOVED DAMAGE, FABRICATED RPR DOUBLER AND FILLER AND INSTALLED IAW SR M 53-00-01 2 L 7 2 4F 4 F RT A2NM E17NE 20080702 NM 2008 7 2 2008UALA03552 1 20080623 A 5320 STRUCTURE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE A/C BAY DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 DAMAGE TO LWR CHORD IN LT AC BAY ABOVE PLENUM. 2 L 7 2 4F 4 F RT A1NM E24NE 20080702 NM 2008 7 2 2008UALA03546 1 20080622 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY LIGHT ROW 2J AFT INOP. FOUND FAULTY LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03545 1 20080621 A 3350 80541 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 WALL EEL INOP:AFT GALLEY FWD LWR WALL ACROSS FROM DOOR 4L. FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY OP CHEC KED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03534 1 20080625 A 3397 WIRE HARNESS BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EEL INOP:ALL RT FIRST CLASS IB AND OB SEATS. SUSPECT WIRE HARNESS FAULTY. REPLACED HARNESS AT 1J, SECURED ALL DISTURBED AREAS. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03532 1 20080622 A 3350 362624 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 EMERGENCY ESCAPE PATH LIGHTING LOOSE AT ROW 1, RIGHT SIDE. FOUND LOOSE LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY OP CHEC KED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080702 EU 2008 7 2 2008UALA03525 1 20080622 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 478UA 1533 EMERGENCY FLOOR EXIT LIGHTS INOP AT FWD CABIN BULKHEAD AND ROW 9. ALL OTHER LIGHTS OPERABLE. FOUND CONNECTOR UNDER SEAT DISCONNECTED. RE-CONNECTED UNDER SEAT CONNECTION, ALL LIGHTS OPERATE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080702 NM 2008 7 2 2008UALA03524 1 20080622 A 3397 CONNECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN LOOSE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 848UA 1647 TWO INCANDESCENT EMERGENCY ESCAPE PATH LIGHTS INOP AT SEATS 20A & 23A. LOOSE CONNECTOR, RE-SET WIRE CONNECTOR ON THE BO X CK OK 2 L 7 2 4F 4 F RT A28NM E40NE 20080813 EU 2008 8 13 NWAA082913264 1 20080626 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHT INOPERATIVE A NWAA O OTHER O OTHER AP APPROACH 1 GL 01 364NW 6073 6073 0962 AFTER GEAR EXTENSION, EXIT SIGNS DID NOT ILLUMINATE FOR AFT DOORS. REPLACED EPSU 13WL, CHECKS GOOD. (A) 2 L 7 2 4F RT A28NM 20080811 EA 2008 8 11 A6WA200840491 1 20080608 A 2710 REGULATOR CNDAIR CL600 CL6002B19 1900309 EA AILERON OUT OF RIG A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 414ZW 7586 AIRCRAFT REQUIRES 50% LT AILERON TRIM FOR LEVER FLIGHT, THE YOKE HAS LT TO RT SLOP FEEL ON FINAL APPROACH. THE YOKE HAD TO BE MOVED APPROXIMATELY 2-3 INCHES BEFORE RESPONSE. (A) RIGGED LT AND RT AILERON TENSION REGULATORS & RIGGED LT AND RT AILERON OUTBOARD PCU`S IAW AMM CHP 27-11. OPS & RIG CK GOOD AT THIS TIME. RII YES 1-42. (A) 2 L 7 2 4F RT A21EA 20080811 EA 2008 8 11 A6WA200840521 1 20080618 A 5320 HINGE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 444ZW 7788 CARGO STOW PLATE HINGES (3) CRACKED. CARGO STOW PLATE HINGES (3) REPLACED IAW CRJ 200 STM 51-42-06. (A) 2 L 7 2 4F RT A21EA 20080811 NM 2008 8 11 AALA200801758 1 20080702 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 178AA 32398 DFW - EMERGENCY EXIT LIGHT SIGN AT RT NR TWO DOOR FAILS TEST. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT LIGHT SIGN AT RT NR TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 NM 2008 8 11 AALA200801757 1 20080702 A 3350 LIGHT BOEING 757 757223 1384957 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 178AA 32398 DFW - EXTERIOR EMERGENCY LIGHT AT RT NR FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RT NR FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 NM 2008 8 11 AALA200801771 1 20080704 A 3350 0201984002 LENS BOEING 767 767223 1385123 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 325AA 22326 JFK - EMERGENCY LIGHT AT AFT LAVATORY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT AFT LAVATORY. SYSTEM GROUND C HECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080811 NM 2008 8 11 USAA920081298 1 20080707 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 457UW 25021 CLT-FORWARD PRESSURE BULKHEAD MAJOR REPAIR 03-0553-8-0105/4- CRACK IN BS 178 FORWARD PRESSURE BULKHEAD WEB WL 210 TO 213 , RBL 6.5. REPAIRED BS 178 FORWARD PRESSURE BULKHEAD WEB WL 210-213, RBL 6.5 IAW B737 SRM 53-10-08 (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081336 1 20080610 A 5240 6545871515 DOOR FRAME BOEING 737 73733A 1384673 NM R1 DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN- C21 MAJOR REPAIR NR 6110569- AFT FRAME CRACKED PAST STOP DRILL, R-1 DOOR CENTER STOP BS328 WL244 RBL60. REPAIRED A FT FRAME OF R-1 DOOR BS328 WL244 RBL60 IAW US AIRWAYS EA 130058. (B) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 AALA200801522 1 20080604 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 762AN 31479 DFW - EMERGENCY LIGHTS AT SEAT 39G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 39G. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 WP 2008 8 12 AALA200801532 1 20080605 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 218AA 49168 LGA - EMERGENCY LIGHTS AT SEAT ROW 20 INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD BIN FOR EMERGENCY LIGHTS AT SEAT R OW 20. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 WP 2008 8 12 AALA200801676 1 20080620 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 462AA 49592 LGA - EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801677 1 20080620 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 363AA 24044 SFO - EMERGENCY LIGHTS AT SEAT 20H TO 21H INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT 20H TO 21H. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080812 EU 2008 8 12 AALA200801691 1 20080623 A 3350 LENS AIRBUS 300 A300B4605R 3930308 EU CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 80058 466 MIA - EMERGENCY LIGHT AT SEAT 2G MISSING LENS. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 2G. SYSTEM GROUND C HECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080812 WP 2008 8 12 AALA200801686 1 20080623 A 2150 REGULATOR DOUG DC9 DC982 3022082 WP A/C BAY MALFUNCTIONED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 468AA 49598 DEN INFLIGHT T1055/23JUN. CREW REPORTED ODOR AND HAZE IN CABIN. RETURNED TO DEN AND LANDED WITHOUT INCIDENT. NO EVIDE NCE OF FIRE FOUND. REPLACED RT AIR CONDITIONING PILOT PRESSURE REGULATOR AND ACCOMPLISHED PACK BURN. SYSTEM GROUND CHE CKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 WP 2008 8 12 AALA200801623 1 20080615 A 3350 P2010031303 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 LAX - EMERGENCY LIGHT AT AFT STAIRWAY FORWARD SIDEWALL BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT AFT STAIR WAY FORWARD SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 WP 2008 8 12 AALA200801624 1 20080615 A 2150 ACM DOUG DC9 DC982 3022082 WP A/C BAY LEAKING A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 467AA 49597 DFW INFLIGHT T2312/15JUN. CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE INDICATION. RETURNED TO DFW AND LANDED WITHO UT INCIDENT. LIGHT EXTINGUISHED PRIOR TO LANDING. FOUND RUBBER BOOT ON RT AIR CYCLE MACHINE LEAKING BETWEEN HEAT EXCHA NGER AND PACK CONTROL VALVE. REPLACED AIR CYCLE MACHINE AND TEMPERATURE TABS ON BOTH SIDES. SYSTEM GROUND CHECKED NORM AL OPERAION. (A) 2 L 7 2 4F A6WE 20080812 WP 2008 8 12 AALA200801589 1 20080611 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 207AA 49158 LGA - EMERGENCY FLASHLIGHT AT FORWARD LOWER POSITION HAS BROKEN STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT FORWA RD LOWER POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801770 1 20080703 A 3350 FUSE BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 SFO - EMERGENCY LIGHT AT AFT LEFT OVERWING INOPERATIVE. REPLACED FUSE ON BATTERY PACK FOR EMERGENCY LIGHT AT AFT LEFT H AND OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080812 NM 2008 8 12 AALA200801783 1 20080705 A 1100 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 682AA 25339 DFW - EMERGENCY LIGHT EXIT ARROW DECAL AT FORWARD SEAT 18A DAMAGED. REPLACED EXIT ARROW DECAL FOR EMERGENCY LIGHT AT FO RWARD SEAT 18A. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 NM 2008 8 12 AALA200801778 1 20080705 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 181AN 29591 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 16C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 16C. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 NM 2008 8 12 USAA920081401 1 20080722 A 2560 P4010021 BATTERY BOEING 737 7373B7 1384580 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 506AU 23381 FLT 1640 (CLT-EWR) - EMERG EQUIP - EMERGENCY FLASHLIGHT IN AFT GALLEY LIGHT NOT BLINKING. MAINTENANCE REMOVED AND REPLA CED THE BATTERY IN THE AFT GALLEY FLASHLIGHT. OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F RT A16WE 20080812 EU 2008 8 12 USAA920081392 1 20080718 A 3240 BRAKE SYS AIRBUS 320 A320231 3930325 EU MALFUNCTIONED A USAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 19 621AW 053 FLT 730 (PHX-SEA) - BRAKES AFTER LANDING AND HOLDING SHORT OF RUNWAY, HAD NO PARKING BRAKE PRESSURE. MANUAL BRAKES WORK ED. WHILE PARKING AT GATE LOST ALL BRAKE PRESSURE - NO NORMAL OR PARKING BRAKE PRESSURE. PARKING BRAKE PRESSURE RETURN ED AND NORMAL BRAKE PRESSURE RETURNED UPON DOOR OPEN. MAINTENANCE OPS CHECKED THE BRAKE SYSTEM PER AIRBUS MM 32-45-00-7 10-001. OPERATIONAL CHECK NORMAL AT THIS TIME. AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A28NM 20080812 NM 2008 8 12 USAA920081408 1 20080718 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT- MAJOR REPAIR - CRACKED INTERCOSTAL AT BS 380-400, BL 0. REPLACED INTERCOSTAL BS 380-400 IAW B737 SRM 53-30-51. (A ) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 USA2008F00009 1 20080712 A 2910 LJ38085 DRAIN BOEING 757 7572B7 1384964 NM HYDRAULIC SYS CRACKED A USAA H O DEACTIVATE SYST/CIRCUITS OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 19 942UW 27807 PHL FLT 723 EN ROUTE DUB TO PHL. DURING DESCENT INTO PHL, THE LT HYDRAULIC SYSTEM QUANTITY DECREASED TO ZERO AND THE SY STEM PRESSURE LIGHT ILLUMINATED. ALSO, EICAS MESSAGE "G L HYD SYS PRESS" DISPLAYED. THE FLIGHT LANDED SAFELY AND WAS A BLE TO TAXI OFF THE RUNWAY, BUT WAS TOWED TO THE GATE. MAINTENANCE REPLACED A HYDRAULIC DRAIN TUBE. SYSTEM OPERATIONAL LY AND LEAK CHECKS OK. (A) 2 L 7 2 4F RT A2NM 20080812 WP 2008 8 12 AALA200801790 1 20080707 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 984TW 53634 SFO - EMERGENCY LIGHT AT SEAT 5E INOPERATIVE. SECURED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHE CKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A6WE 20080813 EU 2008 8 13 08FDEA02658 1 20080703 A 5321 A5227049900200 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 FLOORBOARD PANEL NR 231 EP MAIN CABIN IS SCORED; GOUGED AND PUNCTURED. REPAIRED AREA PER A300-600 SRM 53-10-20; FIG 201 . 2 L 7 2 4F RT A35EU 20080813 NM 2008 8 13 08FDEA02841 1 20080712 A 5312 6523555 ANGLE BOEING 727 727233 138408A NM BULKHEAD CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 BS 740 BULKHEAD LOWER FWD SURFACE, ANGLE LBL 4.5 TO RBL 4.5, WL 146.5 HAS CORROSION ON AFT SURFACE FABRICATED NEW ANGLE REF SRM 51-10-2 PG 2, DWR 65-23555. TREATED AND PRIMED REF 51-10-2 PG 2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080813 EU 2008 8 13 08FDEA02662 1 20080703 A 5321 B5327045900400 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN FLOOR PANEL 231 FG UPPER SURFACE IS PUNCTURED IN MANY AREAS BY BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL I N REF TO A300-600 MSRM 53-10-20; FIG 202. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02666 1 20080703 A 5321 B5327046300400 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN FLOOR PANEL 231 PG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02675 1 20080703 A 5321 B5327046200600 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 BALL BEARINGS ARE EMBEDDED ON THE TOP SURFACE OF PANEL NR 232 GG, MAIN CARGO DECK. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02893 1 20080715 A 5315 A53978476202 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION SPOTS ON CROSSBEAM C 62 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02895 1 20080715 A 5313 A53980877201 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION AT STRINGER P 56 RT, C 76-77 OUT OF LIMIT. REPAIR PERFORMED BY CORROSION REWORK, NDT FOR CORROSION FREE CONDITION AND FLAP PEENING IAW RAS/EFW/9000064/2008 ISS A, APPROVED BY EA 6-5318-120098. 2 L 7 2 4F RT A35EU 20080702 EU 2008 7 2 2008UALA03522 1 20080622 A 3350 CHARGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 404UA 450 EMERG LIGHT TEST FAILED AFTER SLIDE CHANGE..."L EMERG BATT" FAULT. WEAK BATTERY, REPLACED LEFT OVERWING BATTERY & CHARG ER. TEST OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20080702 2008 7 2 2008UALA03518 4 20080621 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR OUT OF TOLERANCE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 513UA 24810 SLIDE PRESSURE AT DOOR 4L OUT OF GREEN BAND. REPLACED SLIDE ASSY, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080702 NM 2008 7 2 2008UALA03515 1 20080621 A 3510 MC1025154 OXYGEN MASK BOEING 737 737322 1384676 NM CREW O2 LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 305UA 23666 CREW REPORT: F-O O2 MASK INFLATABLE HARNESS LEAKING - NOTE: OBSERVER AND CAPT MASKS ARE GOOD. SWAPPED FO'S MASK WITH FI RST OBS MASK. FO'S MASK CHKS OK PER MM35-12-86. FIRST OBS SEAT INOP. REPLACED FIRST OBS SEAT MASK REF MM 35-12-86. AC OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800541 1 20080604 A 5230 65C36231 SKIN BOEING 737 737524 1384721 NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 NUMBER 2 CARGO DOOR EXTERIOR SKIN DENTED 21 INCHES FROM AFT EDGE AND 15 INCHES FROM THE TOP. CUT OUT DENT, FABRICATED A ND INSTALLED REPAIR DOUBLER PER SRM 52-00-01 FIGURE 201 REPAIR 3. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800556 1 20080605 A 5743 115A5211 BUSHING BOEING 737 737724 13844BY NM RT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 RIGHT MAIN LANDING GEAR FWD TRUNNION SUPPORT (INBOARD LOWER BUSHING FACE) HAS CORROSION. COMPLETED ECRA 5741-01106 REV D. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800609 1 20080616 A 5320 147A8540U8 STRUCTURE BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16217 28777 SURFACE CORROSION AT R-2 SERVICE DOOR, THRESHOLD STATION 927-947. REMOVED AND REPLACED R-2 DOOR CHORD PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800543 1 20080604 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 BODY STATION 747 LEFT CRACKED AT AIR GRILL MOUNT. INSTALLED REPAIR ANGLES AND COLD WORKED 6EA HOLES PER EA 5310-04498 O P 02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800560 1 20080601 A 5743 115A5311 BUSHING BOEING 737 737724 13844BY NM LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 LEFT MAIN LANDING GEAR FWD TRUNNION SUPPORT (OUTBOARD UPPER BUSHING FACE) HAS CORROSION. REWORKED OUTBOARD UPPER BUSHIN G FACE PER ECRA 5741-01106. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800561 1 20080601 A 5743 115A5211 BUSHING BOEING 737 737724 13844BY NM LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 LEFT MAIN LANDING GEAR FWD TRUNNION SUPPORT (OUTBOARD LOWER BUSHING FACE) HAS CORROSION. REWORKED OUTBOARD LOWER BUSHIN G FACE PER ECRA 5741-01106. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800577 1 20080530 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 BODY STATION 867 LEFT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FR AME AT BODY STATION 867 LEFT-HAND SIDE A/C BRACKET BETWEEN S-8 & S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA08569 1 20080530 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 BODY STATION 747 LEFT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. CUT OUT CRACKED AR EA OF BODY STATION 747 LEFT SIDE FRAME BETWEEN S8 AND S9 AND INSTALLED REPAIR PARTS PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800627 1 20080622 A 5320 147A8540U7 ANGLE BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 15712 28783 L2 DOOR Z-ANGLE HAS LITE CORROSION ENTIRE LENGTH OF DOOR CUTOUT. REMOVED AND REPLACED Z-ANGLE REF SRM 53-70-15 AND 51-4 0-02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800624 1 20080620 A 5315 65C33952 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 FLOORBEAM AT BODY STATION 1016 LBL 37 HAS CORROSION ON UPPER FLANGE. FABRICATED NEW FLOOR PAN IAW BAC DWG 65C33582 FABR ICATED T-CAP REPAIR STRAP IAW SRM 53-00-51, ALODINED AND PRIMED IAW SRM 51-20-01, INSTALLED FLOOR PAN DIP PAN GALLEY MOU NTS T-ANGLE AND REPAIR STRAP IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800617 1 20080620 A 5311 143A1113 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 15712 28783 FRAME STATION 440 RIGHT CRACKED AT S-9R. INSTALLED REPAIR ON FRAME AT STATION 440 S9R PER ECRA 5311-01410. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800626 1 20080616 A 5320 6545875U70 ANGLE BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 SIGNS OF CORROSION ON Z-ANGLE FORWARD AREA OF R1 DOOR LOWER FRAME. REMOVED AND REPLACED Z-ANGLE AND STRAP AT R-1 DOOR I AW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800553 1 20080530 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 BODY STATION 400 RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 400 AT A/C BRACKET BETWEEN S-8R AND S-9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800576 1 20080608 A 3350 20121 BATTERY PACK BOEING 737 737524 1384721 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17620 27333 FWD ENTRY DOOR EXTERIOR SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK MODULE, OPS CHECKS GOOD. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800566 1 20080530 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 BODY STATION 787 LEFT-HAND FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 787 LEFT-HAND AT A/C BRACKET BETWEEN S-8 AND S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800568 1 20080530 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 BODY STATION 747 RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING A/C BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FR AME AT STATION 747 RIGHT-HAND STRINGER S-8 AND S9 A/C BRACKET PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800632 1 20080623 A 5320 143A541011 ANGLE BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 15712 28783 MAIN DECK FLOOR SUPPORT WEB UPPER ANGLE CRACKED BODY STATION 380 TO 400 BL 0. REMOVED AND REPLACED UPPER L-ANGLE REF SR M 51-40-02. 2 L 7 2 4F RT A16WE 20080702 2008 7 2 CALA0800634 4 20080624 A 2330 RDKW777802 VIDEO MONITOR BOEING 757 757224 1384958 NM CABIN OVERHEATED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 19117 9904 1884 27559 FLIGHT DIVERSION TO TERCEIRA, AZORES PORTUGAL, DUE TO ELECTRICAL SMELL IN FORWARD GALLEY AND FLIGHT DECK. AFTER PERFORM ING SMOKE IN THE FLIGHT DECK/ CABIN INSPECTION, FOUND PAX SEAT VIDEO MONITOR 1E/F AT FAULT. DEACTIVATED IFE, PERFORMED OVERWEIGHT LANDING INSPECTION AND RELEASED AIRCRAFT. 2 L 7 2 4F RT A2NM 20080702 NM 2008 7 2 CALA0800636 1 20080625 A 3350 RPS1B CHARGER BOEING 737 7373T0 1384582 NM CABIN FAULTY A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12349 23587 ROWS 12 - 20 EMERGENCY SEAT LIGHTS INOPERATIVE. FOUND CHARGER PART NUMBER RPS1-B AT FAULT, LOCATED IN CEILING CENTER AR EA BETWEEN AFT GALLEYS. REMOVED AND REPLACED BATTERY CHARGER PER AMM 33-51-51. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800550 1 20080530 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 BODY STATION 440 LEFT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED F RAME AT STATION 440 AT A/C BRACKET BETWEEN S-8L AND S-9L PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 2008 7 2 SWAA083410 4 20080620 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 233LV 32501 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083446 1 20080623 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 244WN 34864 EEPLS LENS MISSING AT ROW 11 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083447 1 20080620 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 254WN 32512 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083448 1 20080620 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 297WN 32542 EEPLS END CAP LOOSE AT ROW 1 ABC. SECURED END CAP PER MM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083449 1 20080623 A 3350 MS155721 LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083351 1 20080618 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083317 1 20080618 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 980, STR 20L. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20080701 EA 2008 7 1 SWIA200819766 1 20080615 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS LOOSE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 432SW 7548 FORWARD SECTION OF EMERGENCY STRIP IS INOP. (FLT 4099) RESECURED FLOOR LIGHT CONNECTION. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819710 1 20080410 A 5220 SEAL CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT TORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 954SW RIGHT EMERGENCY EXIT DOOR SEAL IS TORN. (FOUND AT C-CHECK) REPLACED EMERGENCY EXIT DOOR SEAL AS PER AMM TASK 52-21-07-4 00. 2 L 7 2 4F RT A21EA 20080702 NM 2008 7 2 SWAA083318 1 20080618 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083326 1 20080618 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 13R. REPAIRED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083324 1 20080618 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 420, STR 13L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083222 1 20080612 A 5315 6546811 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 1006, LBL 10. REMOVED AND REPLACED CHORD PER SRM . 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083224 1 20080612 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 751SW 29803 DURING SCHEDULED HC1 CHECK, LEFT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083064 1 20080608 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 226WN 32494 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 2 DEF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082793 1 20080522 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 235WN 34630 EEPLS ASSY LOOSE AT ROW 5 ABC. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082798 1 20080526 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082799 1 20080526 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED RON CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082801 1 20080524 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731E, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082803 1 20080524 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 771, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082804 1 20080524 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082813 1 20080523 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED HC2 CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT CRACKED AT LOWER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082814 1 20080525 A 3350 311500 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 422WN 29826 DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 8 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080703 2008 7 3 SWAA082819 4 20080524 A 2565 4A33075F SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 498WN 32480 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080703 2008 7 3 SWAA082820 4 20080524 A 2565 D31354433 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082823 1 20080523 A 5320 6517853 STIFFENER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED SPV CHECK, FOUND VERTICAL STIFFENER AT BS 178, RBL 5.7. REPAIRED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082821 1 20080523 A 5522 65C25746 SKIN BOEING 737 7375H4 138449D NM RT ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED SPV CHECK, FOUND RT ELEVATOR UPPER SURFACE DELAMINATED. REPAIRED ELEVATOR PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082827 1 20080524 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 608SW 27928 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20080703 2008 7 3 SWAA082828 4 20080526 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 726SW 27858 DURING SCHEDULED RON CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082854 1 20080526 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 414, RBL 1. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082862 1 20080527 A 3397 8100022608 CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 474WN 33861 DURING SCHEDULED MV1 CHECK, FOUND LT FWD CABIN EEPLS INOP. FOUND LOOSE CONNECTOR AT LIGHT ASSY. SECURED CONNECTOR ON L IGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082876 1 20080527 A 5210 6569450 DOOR FRAME BOEING 737 7375H4 138449D NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED BRDG CHECK, FOUND FWD SERVICE DOOR LOWER FRAME CRACKED AT LOWER FWD CORNER. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082875 1 20080527 A 2560 PH22300L GLOWSTRIP BOEING 737 7375H4 138449D NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED BRDG CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT ROW 10 ABC. REMOVED AND REPLACED STRIP P ER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082864 1 20080527 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 755, STR 23L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082830 1 20080527 A 2560 P4010021 BATTERY BOEING 737 7375H4 138449D NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED 16Y CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082865 1 20080527 A 3350 311500 LENS BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED 16Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 20 DEF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082829 1 20080527 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 970, STR 21L. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20080703 2008 7 3 SWAA082832 4 20080523 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082833 1 20080523 A 3230 BACC2A3A00358 CONTROL CABLE BOEING 737 7373H4 1384600 NM NLG LOOSE A SWAA K NONE J WARNING INDICATION DE DESCENT 1 SW 29 625SW 27701 ON GEAR EXTENSION ALL THREE GEAR IN TRANSIT LIGHTS ILLUMINATED IN ADDITION TO DOWN AND LOCKED INDICATION. CYCLED GEAR A ND TRANSIT LIGHTS EXTINGUISHED. LANDING GEAR CONTROL CABLE LGVA TENSION LOOSE. ADJUSTED CABLE PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082874 1 20080527 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082839 1 20080524 A 3350 311500 LENS BOEING 737 7373Y0 1384671 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 6 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080813 EU 2008 8 13 08FDEA02683 1 20080703 A 5321 B5327046101800 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CARGO DECK FLOOR PANEL 232 CF HAS NUMEROUS PUNCTURES AND BEARINGS IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 201. 2 L 7 2 4F RT A35EU 20080813 2008 8 13 NWAA082493302 4 20080602 A 2565 EPSU AIRBUS 330 A330323 3930335 EU ESCAPE SLIDE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 802NW 00533 EPSU TEST FAULTED THE ESCAPE SLIDE LIGHT SW/EPSU (12WL) AND EPSU (19WL). REPLACED BOTH EPSU AND TESTED OK. (A) 2 L 7 2 4F RT A46NM 20080813 NM 2008 8 13 NWAA082876310 1 20080623 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING OVERNIGHT CHECK, FOUND FLOOR EMERGENCY LIGHT STRIP INOP FROM ROW 35HJK THRU 43 HJK. MAINTENANCE REMOVED AND REPL ACED POWER SUPPLY. OPERATIONAL CHECKED GOOD, AND AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 4 4F RT A20WE 20080813 WP 2008 8 13 NWAA082989989 1 20080705 A 3350 FUSE DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8945E 47181 DURING THE LINE CHECK, THE RT OVERWING EMERGENCY EXIT SIGN AND THE EMERGENCY PATHWAY LIGHTING FOR SEVERAL SEAT ROWS WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE ASSOCIATED FUSE BLOWN AND REPLACED IT. OPERATIONAL CHECK WAS GOOD. (A ) 2 L 7 2 4F A6WE 20080813 NM 2008 8 13 NWAA083056745 1 20080710 A 3350 POWER SUPPLY BOEING 747 747222B 1384904 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 645NW 23736 DURING OVERNIGHT CHECK FOUND UPPER DECK RT OUTSIDE EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 4 4F RT A20WE 20080813 WP 2008 8 13 NWAA083079865 1 20080710 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 774NC 47776 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAI LED. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONALLY CONDITION. (A) 2 L 7 2 4F RT A6WE 20080813 WP 2008 8 13 NWAA083089613 1 20080713 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 613NW 47438 DURING LINE CHECK, BOTH OF THE AFT OVERWING EMERGENCY EXIT SINGS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (A) 2 L 7 2 4F A6WE 20080813 WP 2008 8 13 NWAA083109880 1 20080714 A 3397 DIODE DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 675MC 47651 DURING THE LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 5-8 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE "DIODE IN THE FWD RT HAND OVERWING EXIT IDENT". OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F RT A6WE 20080813 WP 2008 8 13 NWAA083039853 1 20080709 A 3397 RELAY DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 762NC 47710 DURING THE LINE CHECK, MAINTENANCE FOUND THAT THE EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND RELAY R2-271 BUT NEITHER PROCEDURE CORRECTED THE FAULT. AFTER RELAY R2-49 WAS REPLACED THE EXTERIO R EMERGENCY LIGHT FUNCTIONED PROPERLY. (A) 2 L 7 2 4F RT A6WE 20080813 WP 2008 8 13 NWAA083449992 1 20080726 A 3397 FUSE DOUG DC9 DC931 3022065 WP EMERGENCY LIGHT FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8960E 45869 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN LIGHT FOR THE AFT RT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE ASSOCIATED FUSE IN THE PERTINENT CIRCUIT BOARD. OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F A6WE 20080813 WP 2008 8 13 NWAA083469874 1 20080727 A 2710 CRANK ASSY DOUG DC9 DC951 3022051 WP AILERONS WORN A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 783NC 48108 FLIGHT RETURNED TO DTW AFTER TAKEOFF DUE TO UNRESPONSIVE OR SLOW TO RESPOND FLIGHT CONTROLS (AILERONS). CREW NOTICED 2 TO 3 INCHES OF YOKE TRAVEL BEFORE ANY FLIGHT CONTROL INPUT RESULTED IN AIRCRAFT CONTROL. PER DISPATCH REPORT MAINTENANC E CONTROL WAS CONTACTED PRIOR TO RETURN TO BASE. CREW ACCOMPLISHED A ROUTINE LANDING BACK AT DTW AND THE ACFT TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE REPLACED THE LEFT AILERON CONTROL TAB IDLER CRANK FOR MINOR PLAY. NO OTHER PROBLEMS NOTED. (A) 2 L 7 2 4F RT A6WE 20080813 NM 2008 8 13 NWAA083386743 1 20080719 A 2611 AMPLIFIER BOEING 747 747249F 1384849 NM SMOKE DETECTORS MALFUNCTIONED A NWAA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 01 643NW 22245 NUMBER 3 MAIN DECK CARGO SMOKE DETECTOR ILLUMINATED ALONG WITH THE FIRE BELL. AFTER CHECKING MAIN DECK, THERE WAS NO SI GN OF SMOKE. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR AMPLIFIER. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETU RNED TO SERVICE. (A) 2 L 7 4 4F RT A20WE 20080813 EA 2008 8 13 COMA0880010 1 20080718 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT DISCHARGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 676CA 20631 15127 EMERGENCY LIGHTS WILL NOT COME ON. REPLACED BATTERY PACK NR 2. (S) 2 L 7 2 4F RT A21EA 20080813 EA 2008 8 13 COMA0880011 1 20080718 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT DISCHARGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 676CA 18890 15127 EMERGENCY LIGHTS WILL NOT COME ON. REPLACED BATTERY PACK NR 3. (S) 2 L 7 2 4F RT A21EA 20080813 EU 2008 8 13 NWAA083123253 1 20080712 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHTS MALFUNCTIONED A NWAA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 01 353NW 18907 9844 786 EMERGENCY EGRESS LIGHTING EPSU FAULTS "INT LOAD AFT L" AND "EXT LOAD AFT L". REPLACED EPSU 13WL, CHECKS GOOD. (S) 2 L 7 2 4F RT A28NM 20080813 EA 2008 8 13 REXA08028 1 20080717 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8631E 7631 FLAP FAIL AT ZERO ON APPROACH. QRH FOLLOWED, EMERGENCY DECLARED WITH UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH. (S) 2 L 7 2 4F RT A21EA 20080813 SO 2008 8 13 RAIA00807011 1 20080713 A 2131 22250N030301 CONTROLLER EMB 145 EMB145LR 3260212 SO CABIN PRESSURE MALFUNCTIONED A RAIA O OTHER J WARNING INDICATION CR CRUISE 1 CE 03 840HK 21107 17683 145341 FLT 7982 - IAD - DURING CRUISE AT FL260, ACFT LOST PRESSURIZATION ON THE AUTO SYSTEM. MAINTENANCE REMOVED AND REPLACED THE PRESSURIZATION DIGITAL CONTROLLER IAW AMM PROCEDURES. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080813 SO 2008 8 13 C2XA08IA167 1 20080717 A 3260 8005701 PROXIMITY SENSOR EMB 145 EMB145XR 3260214 SO RT MLG INOPERATIVE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 21154 145772 IAH FLIGHT 2097 - THE CREW REPORTED LG AIR/GND FAIL AFTER TO COULD NOT MOVE GEAR LEVER HANDLE INTO UP POSITION. THE ACF T RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 2 PROX SWITCH ON RT GEAR PER EM B -145 MM 32-61-01. OPS CHECK GOOD, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080813 SO 2008 8 13 C2XA08IA166 1 20080716 A 3297 W509000122 WIRE EMB 145 EMB145XR 3260214 SO LT MLG BROKEN A C2XA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 27 21154 145772 IAH - FLIGHT 2110, THE CREW REPORTED A LANDING GEAR AIR/GRND FAIL. THE ACFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTE NANCE REPAIRED A BROKEN WIRE ON CONNECTOR P0045. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR R ETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080813 SO 2008 8 13 C2XA08IA165 1 20080716 A 7810 23068890 DIFFUSER EMB 135 EMB135LR 3260305 SO ALLSN AE3007 AE3007A 03030 GL NR 1 ENGINE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11526 145410 CAE311680 IAH - FLIGHT 2346 DURING PREFLIGHT INSPECTION THE NR 1 ENG WAS FOUND TO BE MISSING PART OF THE EXHAUST DIFFUSER, WITH DA MAGE TO THE NR 1 THRUST REVERSER, EXHAUST CONE, AND CONE SUPPORT. MX REMOVED AND REPLACED ENG 1 EXHAUST CONE, FORCED MI XER CONE FLOWPATH SUPPORT AND FORCED CORE BYPASS MIXER. REF: ROLLS-ROYCE EMM 78-11-10, 78-11-12, AND 78-11-15, PLACED T HE THRUST REVERSER ON DMI, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. ON 07/14/08, THE ACFT LANDED IN SHV WHERE M X REMOVED AND REPLACED THE NR 1 THRUST REVERSER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RE TURN TO SERVICE. (S) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080813 SO 2008 8 13 C2X2008F00011 1 20080718 A 5240 FRAME EMB 145 EMB145LR 3260212 SO SERVICE DOOR PUNCTURED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29917 17582 17582 145414 ACFT IS PRESENTLY IN A C-CHECK STATUS AND THE SERVICE DOOR WAS FOUND WITH A PUNCTURE TO THE UPPER FRAME. MX CUT OUT THE AFFECTED AREA AND FABRICATED A L-SHAPE DOUBLER AFTER CONTOURING THE AREA. ALODINED, PRIMED AND PAINTED. INSTALL IAW E C52-40-01040 AND THE SRM. ACFT WILL BE RELEASED UPON COMPLETION OF WORK. (S) 2 L 7 2 4T RT T00011AT 20080813 SO 2008 8 13 C2X2008F00012 1 20080718 A 5320 110049 BRACKET EMB 145 EMB145LR 3260212 SO BATTERY HOLDER BROKEN A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 48901 16816 16816 145501 ACFT WAS IN FOR A SERVICE CHECK AND THE RT FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX REMOVED AND REPLACED THE N R 2 EMERGENCY BATTERY HOLDER ASSEMBLY IAW AMM 33-50-04. OPS CHECK GOOD AND WAS RELEASED. (S) 2 L 7 2 4T RT T00011AT 20080813 SO 2008 8 13 C2X2008F00013 1 20080718 A 5311 FRAME EMB 145 EMB145LR 3260212 SO RROYCE AE3007 AE3007A1 54165 EA FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17560 145605 CAE311901 ACFT 560 WAS IN FOR A 3C INSPECTION AND CORROSION WAS FOUND ON THE FRONT FRAME FORWARD FLANGE THAT HAD HOLES 9,24,24 AND 40 THAT WERE GREATER THAN THE R/R MANUAL LIMITS. EC 7220-01056 AND TVF5284 WAS ISSUED APPROVING THE REPAIR OF THE DAMA GE AND CONTINUED OPERATION OF THE ENG. MX REMOVED THE CORROSION TO A MINIMUM. CREATED A SMOOTH TRANSITION RADIUS FROM THE AFFECTED AREAS. INSPECT THE AREA WITH SPORT FLUORESCENT PENETRANT INSPECTION METHOD C SENSITIVITY LEVEL 3 IAW ROLLS ROYCE MANUAL. ALL WORK WAS ACCOMPLISHED IAW WITH EC7220-01057 AND TVF 5284 AND WILL BE RELEASED AT THE END OF THE C-CH ECK. (S) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080813 2008 8 13 RYN2008F00010 4 20080806 A 2310 RADIO BOEING 767 767332 1382001 NM RT HF SYSTEM FAILED A RYNA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 CE 07 123DN 23437 ACFT DIVERTED DUE TO LOSS OF THE RT HF COMMUNICATION SYSTEM. THE LT HF IS ALREADY ON DEFERRAL PER MEL 23-11-1-2. TROUB LESHOOTING IN WORK (ISSUED MEL 23-11-1-2OH DMI NR62632). (S) 2 L 7 2 4F RT A1NM 20080813 NM 2008 8 13 RYN2008F00011 1 20080806 A 5610 WINDSHIELD BOEING 757 757236 1384971 NM COCKPIT CRACKED A RYNA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 CE 07 526NA 24794 ACFT RETURNED TO BUD. FLIGHT CREW ADVISED THAT THE LT NR 1 WINDSHIELD IS CRACKED ALONG THE LOWER SECTON OF THE WINDOW. WAITING FOR PARTS. OPEN. (S) 2 L 7 2 4F RT A2NM 20080813 NM 2008 8 13 TSAA0852022 1 20080717 A 5297 CABLE BOEING 737 737290C 138448V NM DOOR WARNING UNSECURE A TSAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 842AL 23136 FLT 956: AFT CARGO DOOR LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED TO BASE. RE-SECURED DOOR CABLE AND TARGET. OPS CHE CK ON GROUND OK. (S) 2 L 7 2 4F A16WE 20080813 CE 2008 8 13 TSAA0852022A 1 20080721 A 5220 STOP BEECH 1900 1900D 1154162 CE EMERGENCY DOOR OUT OF ADJUST A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 81556 UE239 DURING SCHEDULED ROUTINE MX DISCOVERED SEAT 6A EMERGENCY DOOR HARD TO OPEN. ADJUSTED SIDE STOPS ON FUSELAGE FOR EMERGEN CY DOOR. (S) 2 L 7 2 4T RT A24CE 20080813 NE 2008 8 13 G6O2008F00000 2 20080726 A 7200 ENGINE DOUG MD11 MD11F 3023600 NM GE CF6 CF680C2D1F 30025 NE NR 1 MAKING METAL A G6OA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 27 705GC 48412 NR 1 ENG SHUTDOWN DUE TO FLUCTUATING PARAMETERS. N1 MAX 12035 N2 MAX 116.7 EGT MAX 1045. GROUND INSPECTION FOUND METAL SHAVINGS IN EXHAUST. (S) 2 L 7 3 4F 4 F RT A22WE E31N3 20080813 NM 2008 8 13 YEN2008F00017 1 20080729 A 2150 FILTER EMB ERJ190 ERJ190100IGW 3260408 NM A/C PACK CONTAMINATED A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 15 249JB 19000045 FLT 907, JFK-ORD, AIR RETURN TO JFK, RECEIVED LAV SMOKE WARNING IN FLIGHT. LANDED ACFT ASAP, FOLLOWED QRH PROCEDURES. SMOKE WAS VISIBLE IN CABIN INITIALLY AND THEN DISSIPATED WITH TIME. LAV SMOKE WARNING WENT OUT AFTER SMOKE DISSIPATED. NO VISIBLE SMOKE IN COCKPIT. PERFORMED LTV SMOKE ODOR INSPECTION PER 44-20-10. INSPECTION WAS GENERAL TO CABIN, NO FA ULTS NOTED. PERFORMED VISUAL INSPECTION OF NR1 AND NR2 PACK INLETS. FOUND EVIDENCE OF COFFEE RESIDUE ON NR 2 PACK INLE T. SMALL TRACES OF COFFEE STAINS ON NR 2 PACK INLET. CLEANED RESIDUE FROM PACK INLET NR 2 AND REMOVED AND REPLACED REC IRC FAN AIR FILTERS AS PER MM 21-24-02. ACFT OK FOR SERVICE. (S) 2 L 7 2 4F RT A57NM 20080813 WP 2008 8 13 WX0A070222 1 20080723 A 3350 AD4002 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 894GA 49660 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (S) 2 L 7 2 4F A6WE 20080813 WP 2008 8 13 WX0A070221 1 20080722 A 3350 20131A BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 864GA 49912 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MX DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATI ON LIGHTING SYSTEM WOULD NOT TEST. MX PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATI SFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (S) 2 L 7 2 4F RT A6WE 20080813 NM 2008 8 13 WX0A070220 1 20080719 A 3350 AD4002 BATTERY DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 872GA 53295 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MX DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATI ON LIGHTING SYSTEM WOULD NOT TEST. MX PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATT ERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (S) 2 L 7 2 4F RT 20080813 EU 2008 8 13 08FDEA02910 1 20080716 A 5313 A53971006 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON STRINGER P 54 LT, C55-56 AND P56 LT, C 57.2-57.3 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201A. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02912 1 20080716 A 5313 A53974202 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON STRINGER P 54 LT BETWEEN C59-61, P 53 LT AND P 48 LT BETWEEN C59-60 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201A. 2 L 7 2 4F RT A35EU 20080813 NM 2008 8 13 08FDEA02913 1 20080716 A 5320 65163517 CHANNEL BOEING 727 727233 138408A NM BS 423 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 E/E DOOR CUT-OUT FWD ANGLE CRACKED BY LATCH REPLACED CUT OUT FWD ANGLE AND RIGGED E/E DOOR REF BOEING DWR 65-16351, SRM 51-30-01 PG 1-10, SRM 51-30-5 PG 3, SRM 51-30-2 PG 2/3, AMM 51-20-151 PG 1-6, AMM 20-60-001 PG10, MM 52-40-011 PG 1. TH IS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080813 NM 2008 8 13 08FDEA02954 1 20080717 A 5320 6526173109 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 UNDER FWD LAV STA 328 TO 344 FLOOR SUPPORT RBL 52 HAS CORROSION AROUND NUTPLATES REMOVED AND REPLACED SUPPORT FROM STA 3 26-344 RBL REF SRM 51-30-2 PG 2, FLOOR SUPPORT AT RBL 52 STA 328-344. FOUND TO BE WITHIN LIMITS OF SRM 53-10-06, TREATE D AND PRIMED REF SRM 51-10-2. 2 L 7 3 4F RT A3WE 20080813 EU 2008 8 13 08FDEA02955 1 20080717 A 5340 A53812602202 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 ELONGATED HOLES FOUND AT STRINGER COUPLING 5 AND 13, C 40 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02956 1 20080717 A 5311 A53833127205 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND DAMAGED HOLE AT C 40, BETWEEN P 5-6 RT REPAIR PERFORMED BY ENLARGING THE HOLE TO 6MM. PERFORM NDT FOR CRACK FREE CONDITION AND INSTALLING HL11VF8/HL70-8 FASTENER IAW RAS/DAHAM/4025121/2008 ISS A , APPROVED BY EA 6-5315-120079. 2 L 7 2 4F RT A35EU 20080813 WP 2008 8 13 08FDEA02957 1 20080717 A 5730 ARC16541 SKIN DOUG DC10 DC1010 3022110 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 40061 46973 LT WING OUTBD FLAP CRACK ON LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 85 VOL I. 2 L 7 3 4F A22WE 20080813 NM 2008 8 13 08FDEA02901 1 20080715 A 2613 WARNING SYSTEM BOEING 727 7272D4 138407U NM OVERHEAT MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 21 287FE 21849 INFLIGHT, LOWER AFT BODY OVERHEAT LT ILLUMINATED. ACCOMPLISHED QRH PROCEDURES AND DETERMINED THAT THE LEAK IS BETWEEN N R 3 BLEED VLV AND PACK VALVE. HAD TO DESCEND TO FL250 TO CONTROL CABIN ALTITUDE AT 10000 FT. RAN ENGINES AT H/P. NO O VERHEAT LIGHT CHECKED PLUMBING IN AFT STAIR AND FOUND CLAMP LEAKING AT AIR CLEANER. TIGHTENED CLAMP. OHMED OUT SENSORS , CHECKING FOR SHORTS TO GROUND, NONE FOUND. CHECKED ALL DUCT WORK INSIDE AND OUT INCLUDING KEEL BEAM WITH HAND HELD FL IR IMAGING SYSTEM. ALL TEMPS WELL BELOW TRIGGER THRESHOLD OF OVERHEAT SYSTEM IAW TSM 26-14-000. REMOVED AND REPLACED C ONTROL UNIT. OPS CK GOOD IAW AMM 26-14-000-5. 2 L 7 3 4F A3WE 20080813 WP 2008 8 13 08FDEA02902 1 20080715 A 5730 AUB22084 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 RIGHT WING TIP, LOWER SURFACE HAS 2 DENTS, CENTER AREA. CHECKED WING TIP LOWER SURFACE, NOTED CREASES. FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 51-80-01, PARA 2-C, VOL II. CUT OUT DAMAGED AREA. MATERIAL ID FOR THE DOUBLER IS 2024-T3, 0.063, PO 614988.3. FABRICATED DOUBLER IAW DC/MD-10 SRM 57-00-01, FIG 4, VOL III. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-71-01, PGS 21 - 24, VOL II. INSTALLED DOUBLER IAW DC/MD-10 SRM 51-35-01, VOL II. 2 L 7 3 4F RT A22WE 20080813 EU 2008 8 13 08FDEA02914 1 20080716 A 5330 A53978152200 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 742FD 613 EDGE DISTANCE TO SMALL AT FOUR FASTENER LOCATION C 68, P 32-33 RT. EXTERNAL DOUBLER REPAIR PERFORMED IAW RAS/EFW/900006 9/2008 ISS A, APPROVED BY EA 6-5317-123002. 2 L 7 2 4F RT A35EU 20080813 NM 2008 8 13 08FDEA02915 1 20080716 A 5320 65261735 FLOOR SUPPORT BOEING 727 727233 138408A NM BS 305-312 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 FWD LAV FLOOR SUPPORT STA 305-312 RBL 42 NUTPLATES RUSTED AND FLOORBEAM CORRODED. REMOVED CORROSION FROM FLOORBEAM, O RIGINAL THICKNESS .070, REMAINING .066. REMOVED .004, FOUND TO BE WITHIN LIMITS, REMOVED CORROSION FROM FLOOR SUPPORT, ORIG THICKNESS.070, REMAINING .035. REMOVED .035, FOUND TO BE OUT OF LIMITS REF SRM 53-10-1 PG 2. TOOL ID AAR 9800 CAL DUE DATE 06/24/09. REMOVED AND REPLACED FLOOR SUPPORT AND "T" CLIP, TREATED AND PRIMED "T" CLIP AND AFFECTED AREAS ON AIRCRAFT REF SRM 51-10-2 PG2. INSTALLED SUPPORT AND T CLIP, REF SRM 51-30-2 PG 2. THIS IS CLASSIFIED AS A MINOR REPAIR . 2 L 7 3 4F RT A3WE 20080813 EU 2008 8 13 08FDEA02918 1 20080716 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND ELONGATED HOLES ON RT WING BOTTOM SKIN, RIB 8, IN AREA OF HYDRAULIC FITTINGS REPAIR PERFORMED BY REAM UP THE HOL ES AND INSTALL REPAIR BUSHES IAW DRAWING R571-50532, APPROVED BY EA 6-2910-120038. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02920 1 20080716 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION AT LT WING BOTTOM SKIN UPPER SURFACE RIB 8. REPAIR PERFORMED BY BLEND OUT THE CORROSION, NDT FOR CORROS ION FREE CONDITION INSTALLING STEEL PLATES IAW RAS/BAE/1007329/2008 ISS A, APPROVED BY EA 6-2910-120038. 2 L 7 2 4F RT A35EU 20080813 NM 2008 8 13 08FDEA02921 1 20080716 A 5320 6517593151 FLOOR SUPPORT BOEING 727 727233 138408A NM BS 305-320 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 FLOORBOARD SUPPORT NUTPLATES RUSTED STA 305-312 RBL 55 FWD LAV. REMOVED FLOOR SUPPORT ANGLE, REMOVED CORROSION, FOUND T O BE OUT OF LIMITS ORIG MATERIAL THICKNESS .040, REMAINING .033, REMOVED .007. INSTALLED NEW ANGLE REF SRM 51-30-2 PG 2, SRM 53-10-1 PG 1, BOEING DWG 65-17593-151, TOOL ID AAR 9800 CAL DUE DATE 6/24/09. THIS IS CLASSIFIED AS A MINOR REP AIR. 2 L 7 3 4F RT A3WE 20080814 WP 2008 8 14 UPS08852664 1 20080612 A 5311 FRAME DOUG DC8 DC871F 302199D WP PWA JT3D JT3D3 52039 NE BS 70 L29L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, AREA OF CORROSION EXFOLIATON ON AFT SIDE OF STA 70 FRAME, A PIT, BETWEEN L29L AND L30L. REMOVED DAM AGE AND FABRICATED DOUBLER IAW SRM 53-02-05 FIG 008C. 2 L 7 4 4F 4 F RT 4A25 1E8 20080812 WP 2008 8 12 AALA200801679 1 20080621 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 559AA 53089 LGA - EMERGENCY LIGHTS AT TAIL COMPARTMENT INOPERATIVE. SECURED LOOSE BATTERY FOR EMERGENCY LIGHTS AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 WP 2008 8 12 AALA200801680 1 20080621 A 3020 320115C ANTI-ICE VALVE DOUG DC9 DC982 3022082 WP NOSE COWL BROKEN A AALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 419AA 49331 DFW INFLIGHT T1205/21JUN. CREW REPORTED NR ONE ENGINE FIRE WARNING AFTER TAKEOFF. CREW SHUT DOWN NR ONE ENGINE. RETUR NED TO DFW AND LANDED WITHOUT INCIDENT. FOUND NOSE COWL ANTI ICE VALVE BROKEN OFF AT THE FLANGE. REPLACED NOSE COWL AN TI ICE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801661 1 20080618 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 673AN 29423 DFW - EMERGENCY LIGHT AT MID COACH CABIN INOPERATIVE. REPLACED BATTERY PACK AT STATION 1050 FOR EMERGENCY LIGHT AT MID COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 EU 2008 8 12 AALA200801655 1 20080618 A 2820 O-RING AIRBUS 300 A300B4605R 3930308 EU FUEL SYSTEM LEAKING A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 70054 461 PTY INFLIGHT T2110/18JUN LIM TO MIA. CREW REPORTED UNWANTED FUEL TRANSFER IN FLIGHT. LANDED PTY WITHOUT INCIDENT. FOU ND O-RING DAMAGED AND SPLIT AT LEFT INNER PUMP NUMBER ONE FUEL FEED OUTLET MANIFOLD. REPLACED O-RING AT LT INNER PUMP N R ONE FUEL FEED OUTLET MAINFOLD. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080812 NM 2008 8 12 USAA920081400 1 20080722 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 306AW 24633 FLT 421 (PHX-ELP) - EMERG EQUIP - VERTICAL FLASHLIGHT IN FORWARD GALLEY NOT FLASHING RED LIGHT. MAINTENANCE REMOVED AND REPLACED THE BATTERY IN THE FORWARD RT EMERGENCY FLASHLIGHT. OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 USAA920081394 1 20080721 A 2530 416000129 COFFEEMAKER AIRBUS A319 A319132 3930340 NM GALLEY DEFECTIVE A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 820AW 1397 FLT 350 PHX-LAX - BURNING SMELL - COFFEEMAKER WILL NOT BREW. COFFEEMAKER WENT OFF AND THERE WAS A SMELL OF WIRE BURNING . NO SMOKE WAS DETECTED. MAINTENANCE REMOVED AND REPLACED THE COFFEEMAKER. OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F RT A28NM 20080812 NM 2008 8 12 USAA920081410 1 20080717 A 5320 WEB BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT- Q3- MAJOR REPAIR - CRACK IN WEB AT BS 294 S16L. REPLACED WEB AT BS 294 S16L IAW B737 SRM 53-00-07. (A) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 AALA200801721 1 20080627 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 672AA 25337 DFW - EMERGENCY LIGHT AT SEAT 31D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31D. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 NM 2008 8 12 08FDEA02566 1 20080630 A 5730 APB74411 SKIN DOUG MD11 MD11F 3023600 NM WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 609FE 48549 MAIN DECK CARGO COMPARTMENT, CORROSION FOUND ON UPPER SURFACE OF PRESSURE BOUNDARY OVERWING AT STA Y=1228, XCW= 63.5-64. 5 RT. UPPER SURFACE CORROSION ON MAIN DECK CARGO COMPARTMENT AT STA Y=1228 XCW=63.5-64.5. REMOVED AS PER SRM 51-21-0 1 VOL II AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG 13 VOL I. ORIGINAL THICKNESS: 0.169 INCH, MATERIAL REMOVED: 0.0 14 INCH, REMAINING THICKNESS: 0.155 INCH. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080812 NM 2008 8 12 08FDEA02806 1 20080710 A 5320 ACA72241 FITTING DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 609FE 48549 MAIN DECK CARGO COMPARTMENT, UPPER DECK CARGO DOOR LOWER SILL SPOOL FITTING NR 2 FASTENER HOLES FOUND WITH CRACK INDICAT ION AT HOLE 'C' AND 'D' DURING OPEN HOLE HFEC INSPECTION. MAIN DECK CARGO COMPARTMENT, UPPER DECK CARGO DOOR LOWER SILL SPOOL FITTING NR 2 CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 VOL I FIG 10. REPAIR CLASSIFIED MAJOR AS PER FEDEX G MM 6-2-100. 2 L 7 3 4F RT A22WE 20080812 NM 2008 8 12 08FDEA02807 1 20080710 A 5320 ACA72241 FITTING DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 609FE 48549 MAIN DECK CARGO COMPARTMENT, UPPER CARGO DOOR LOWER SILL SPOOL FITTING NR 5 HOLES FOUND WITH CRACK INDICATIONS AT HOLE ' C' AND 'D' DURING OPEN HOLE HFEC INSPECTION. MAIN DECK CARGO COMPARTMENT, UPPER CARGO DOOR LOWER SILL SPOOL FITTING NR 5 CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 VOL I FIG 10. REPAIR CLASSIFIED MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080812 NM 2008 8 12 08FDEA02834 1 20080712 A 5312 6523558 FITTING BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 BS 740 BULKHEAD LOWER SURFACE, "T" ANGLE AT RBL 5" WL 146.5 CONNECTION TO DELTA BEAM "T" FLANGE IS CORRODED NEW T ANGLE FABRICATED ON SHOP NON-ROUTINE N00670. REMOVAL AND INSTALLATION ACCOMPLISHED ON N00167. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080812 WP 2008 8 12 08FDEA02835 1 20080712 A 5320 NJC6010 CHANNEL DOUG DC10 DC1030F 3023504 WP BS 879 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 FWD CARGO COMPT CHANNEL WITH SEVERE EXFOLIATION CORROSION. WORK COVERED BY NRC N00418. 2 L 7 3 4F RT A22WE 20080812 NM 2008 8 12 USAA920081382 1 20080717 A 5330 6545776 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 PHX-BJ- MAJOR REPAIR - DEEP CORROSION FOUND ON FUSELAGE EXTERNAL SKIN AT AFT AIRPHONE ANTENNA. REPAIRED FUSELAGE EXTERN AL SKIN AT AFT AIRPHONE ANTENNA LAW B737 SRM 53-00-01 REPAIR 31 AND US AIRWAYS TYPICAL REPAIR 53-00-53 REFERENCE 1-7. ( A) 2 L 7 2 4F RT A16WE 20080813 EU 2008 8 13 08FDEA02664 1 20080703 A 5321 B5327046402400 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN FLOOR PANEL 231 HG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02858 1 20080714 A 5755 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 3 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD TS0564 613 FOUND DELAMINATION ON RT SPOILER NR 3 OUT OF SRM LIMIT. REPAIR PERFORMED BY REPLACEMENT OF SPOILER NR 3 RT IAW AMM 27-6 1-51 PAGE 401. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02888 1 20080715 A 5330 A53974426202 SKIN AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND SCRATCHES AT SKIN PANEL C64-65 IN THE AREA OF RA ANTENNA. REPAIR PERFORMED BY REWORK OF AREA AND NDT FOR CRACK FR EE CONDITION IAW RAS RAS/EFW/9000071/2008 ISS A , APPROVED BY EA 6-5317-123028. 2 L 7 2 4F RT A35EU 20080813 NM 2008 8 13 08FDEA01961 1 20080522 A 5100 NONE BOEING 757 75723A 1384967 NM IAW SRM NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 919FD 24636 EXTERNAL PATCH REPAIR ON FUSELAGE BS 1717, BETWEEN S-20L AND S-21L, TO BE EVALUATED. EXISTING REPAIR EVALUATED AS PER EO F-5100-7-5001 PT.1 ATTACHMENT B, FOUND PREVIOUSLY ACCOMPLISHED IAW MESSAGE 1-730176994-3, WITH FAA FORM 8110-3. SUP PLEMENTAL INSPECTION REQUIRED NOT LATER THAN 08 JANUARY 2009. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 2 4F RT A2NM 20080813 NM 2008 8 13 NWAA082593168 1 20080606 A 5610 NP1653127 WINDSHIELD AIRBUS A319 A319114 3930350 NM COCKPIT FAILED A NWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 01 368NB 12380 02039 DURING TAKEOFF ROLL AT 100 KNOTS CAPTAINS SLIDING WINDOW OUTER PANE SHATTERED. ABORTED TAKEOFF AND RETURNED TO GATE. M SP MAINTENANCE REMOVED SLIDING WINDOW PER MM 56-12-11 AND INSTALLED NEW WINDOW. OPS CHECKED PER MM 30-42-00-710-001. T ESTED OK AND AIRCRAFT HAS RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A28NM 20080813 WP 2008 8 13 NWAA083459992 1 20080726 A 3397 FUSE DOUG DC9 DC931 3022065 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8960E 45869 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 14-17 OF THE CABIN WERE INOPERATIVE. M AINTENANCE REPLACED THE ASSOCIATED FUSE IN THE PERTINENT CIRCUIT BOARD AT THE AFT RIGHT EXIT SIGN. OPS CHECK WAS GOOD. (A) 2 L 7 2 4F A6WE 20080814 NM 2008 8 14 UPS08M52645 1 20080705 A 3110 LAMP DOUG MD11 MD11F 3023600 NM INSTRUMENT PANEL INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 EMERG POWER "OFF" , LIGHT DIM, RELAMPED EMERG POWER "OFF" LIGHT. OPS CHECKED GOOD. REF MM 33-11-17- 12-2. 2 L 7 3 4F RT A22WE 20080814 NM 2008 8 14 UPS08M52652 1 20080613 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 271UP 48572 INSPECTION TYPE-C, LT WING FUEL TANK UPPER STRINGER NR 11 END SUSPECT CRACK. STR NR11 SECTION CUT IAW SRM 57-20-00, FIG.10 V.1 REV.40 & EN1277-08. HFEC INSP C/OUT IAW NDT SPM R.13 PART 06-10-01.001 ON TRIMMED AREA FOUND NO CRACK EVIDENT . NEW STRINGER 11L & REP PARTS MACHINED IAW SRM 57-20-00 FIG. 10 V.1 R.40&EN1277-08 USING 10164 & 100425. HOLES ON NEW S TR 11 & REP PARTS P/UP IAW EN1277-08. OK TO INSTALL NEW STR 11, REP PARTS, SPLICE END. 2 L 7 3 4F RT A22WE 20080814 WP 2008 8 14 IXX2008F00045 1 20080609 A 5753 SKIN DOUG DC8 DC872F 302199E WP T/E FLAP WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND LT WING OUTBOARD FLAP UPPER SKIN WORN AT STATION XF 211.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 4 TR 57-94, DC8 SRM 57-1-0 PAGE 1, SRM 51-1-2 1, DC8 SRM 51-1-8B, DC8 SRM 57-7-1 FIGURE 4 ITEM "C" TR 57-94 DATED 10/01/02, DC8 SRM 51-1-11, SRM 51-3-0, AND SRM 51-3- 1. (S) 2 L 7 4 4F RT 4A25 20080814 NM 2008 8 14 UPS08M52671 1 20080328 A 5730 SKIN DOUG MD11 MD11F 3023600 NM WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE-C, CORROSION AROUND FASTENER HEADS ON O/WING CTR FUEL TANK UPPER SURFACE AT STA 1229 X=-87 TO -107. LO CK FASTENER ON AFFECTED AREA REMVD FOR ACCESS. CORROSION REMOVED, MEASURED THK: 0.170", MAT'L REMOVED:0.067", MAT'L REM N:0.103". FOUND OUT OF LMT FPI & 10X VISUAL INSP C/O ON REWK AREA, FOUND NO CORROSION OR CRACK. REWORK AREA REPROTECTED & PAINTED. LOCK FASTENERS INSTALLED FUEL VAPOR BARRIER SEAL APPLIED. FUEL LEAK CHECK C/O, SATIS. 2 L 7 3 4F RT A22WE 20080814 NM 2008 8 14 UPS08552794 1 20080720 A 2560 ESCAPE REEL BOEING 757 75724APF 1384969 NM COCKPIT UNSERVICEABLE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 468UP 25484 3 EMERGENCY ESCAPE TAPE TAMPER SEALS BROKEN. R&R 3 EMERGENCY ESCAPE DESCENT DEVICES IAW MM 25-61-02-2. 2 L 7 2 4F RT A2NM 20080814 WP 2008 8 14 IXX2008F00047 1 20080610 A 5754 SKIN DOUG DC8 DC872F 302199E WP SLOT VANE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON LT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095. 000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED A ND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-3-2 FIGURE 10 PAGE 22 ITEM "F", DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-1, SRM 51-3-0, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 NE 2008 8 14 ARWA20080707 2 20080731 A 7321 71128726 FUEL CONTROL DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 1 ENGINE MALFUNCTIONED A ARWA O OTHER R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 SO 29 661AV 45969 ENG NR 1 FAILED TO ACCELERATE BEYOND GROUND IDLE. REMOVED AND REPLACED FUEL CONTROL UNIT AT NR 1 ENG IAW DC8 MM 73-20-1 . PERFORMED ENG RUN UP IAW DC8 MM 77-00. FOUND NORMAL. (S) 2 L 7 4 4F 4 F 4A25 1E8 20080814 WP 2008 8 14 UPS08852788 1 20080630 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1870-1885 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, FUSELAGE SKIN AROUND TAIL-STAND HANGER FIN IN VERY POOR CONDITION, NUMEROUS DENTS, SKIN DEFORMED,PUS HED IN, DAMAGED REPAIR DOUBLER, BAD PAINT STA. 1870-1885. REMOVED AND INSTALLED REPAIR DOUBLER IAW SRM,51-1-20 FIG.45, 51-1-8, 5 2-3-0 FIG. 1D. 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 UPS08852731 1 20080628 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1306-150 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, MCC FLOOR SEAT TRACK LBL 59 CORROSION AND WEAR MARKS BS 1306 TO 1350. INSTALLED 1EA PLUG AND 1 CHAN NEL BS 1320-1326 LBL 59 IAW SRM 51-03- 01 (AREAS STA 1306-1319 AND 1326-1350 BLENDED AND WITHIN LIMITS IAW SRM 53-02-03 FIG 012). 2 L 7 4 4F RT 4A25 20080814 NM 2008 8 14 UPS08652669 1 20080702 A 5320 146T5651U5 FLOOR SUPPORT BOEING 767 76734AF 1385212 NM BS 1581 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 301UP 27239 AFT OF BULK CARGO COMPT STA 1581 LBL 75 MAIN DECK FLOOR SUPPORT ATTACH SPLICE DAMAGED. (CRACK LENGTH 1" APPROX) AFT OF B ULK CARGO COMPT BS 1581 LBL 75 FLOOR SUPPORT ATTACHMENT SPLICE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 AT MAIN DECK AREA. 2 L 7 2 4F RT A1NM 20080814 WP 2008 8 14 UPS08852749 1 20080629 A 5720 36475841 FITTING DOUG DC8 DC871F 302199D WP LT WING GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, LT WING FLAPWELL FITTING BENT AND GOUGED BELOW FLAP STA 98 ACTUATOR. REMOVED AND INSTALLED FITTING AT FLAP STA 98 IAW SRM 51-3-0, 51-1-8, 5 1-3-1. 2 L 7 4 4F RT 4A25 20080814 EA 2008 8 14 TRAX200800929 1 20080725 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 CANNOT CLOSE PAX DOOR. FLT 4451 DEL 551 MINS NC. CHECKED PAX DOOR PUSHRODS, OUTER AND INNER LOCKS. OPS CHECKED PAX DO OR OVER 20 TIMES, INSIDE AND OUTSIDE. PAX DOOR WORKS SMOOTHLY EVERY TIME IAW CRJ 100 AMM 52-11-00. NO DEFECTS NOTED AT THIS TIME. ACFT OK FOR SERVICE. (S) 2 L 7 2 4F RT A21EA 20080814 NM 2008 8 14 KCSA081360 1 20080729 A 5210 FRAME BOEING 747 747246B 1384864 NM R4 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 R4 MAIN ENTRY DOOR LOWER HORIZONTAL FRAME CRACKED AT FWD END. (S) 2 L 7 4 4F RT A20WE 20080814 NM 2008 8 14 USA2008F00011 1 20080730 A 3350 036000570010 FUSE BOEING 737 7373G7 1384595 NM BATTERY PACK BLOWN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 307AW 24634 PHX - MAINTENANCE REPORTED THE BULL NOSE EMERGENCY EXIT LIGHTS AT ROW 21L AND 22R INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE AT EMERGENCY LIGHT BATTERY PACK M1137. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A16WE 20080814 NM 2008 8 14 USA2008F00012 1 20080726 A 3350 1012721 LIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 435US 24557 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHT ASSEMBLY AT SEAT 12C (AISLE) NEEDS REPLACED. MAINTENANCE REMOVED AND REP LACED THE EMERGENCY LIGHT ASSEMBLY AT SEAT 12C. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A16WE 20080814 NE 2008 8 14 USAA920081437 2 20080728 A 7230 9115M31P06 PIN AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE NR 1 VSV STALLED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING E M VIBRATION/BUFFET OVER TEMP TO TAKEOFF 1 EA 19 749US 1313 FLT 792, ACFT EXPERIENCED NR 1 ENG FAILURE AFTER TAKEOFF. CAPTAIN REPORTED A LOUD BANG PRIOR TO FINAL FLAP RETRACTION P ROBABLY FROM A COMPRESSOR STALL. THEN EXPERIENCED ENG SURGING, VIBRATION AND A MAX ENG TEMP READING. THE CREW SHUTDOWN ENG AND RETURNED TO NAS AFTER DECLARING AN EMERGENCY. CAPTAIN ALSO REPORTED NO ECAM WARNINGS OF ENG PROBLEMS. FLIGHT L ANDED WITHOUT FURTHER INCIDENT. (S) MX R&R THE NR 1 ENGINE. ENGINE RUN/LEAK CHECK GOOD. VENDOR TEARDOWN REPORT INDICA TES THE ANTI ROTATION PIN AT THE VSV SHROUD LIBERATED CAUSING DAMAGE TO THE COMPRESSOR. 2 L 7 2 4F 4 F RT A28NM E37NE 20080814 EU 2008 8 14 USAA920081436 1 20080729 A 2560 P4010021 BATTERY AIRBUS 320 A320231 3930325 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AW 076 FLT 323 ORD-LAS - EMERGENCY EQUIPMENT - AFT LT FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE AFT EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A28NM 20080814 EU 2008 8 14 USA2008F00017 1 20080729 A 2560 P4010021 BATTERY AIRBUS 330 A330323 3930335 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 274AY 0342 LHR - THE CAPTAIN’S FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE CAPTAIN’S FLASHLIGHT BATTERY. OPERATION ALLY CHECKS OK. (S) 2 L 7 2 4F RT A46NM 20080814 NM 2008 8 14 USAA920081429 1 20080727 A 5347 SEAT TRACK BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT - Q3 - MAJOR REPAIR - SEAT TRACK CRACKED AT BS 727B RBL 48. REPAIRED SEAT TRACK CRACKED AT BS 727B RBL 48 IAW B737 SRM 53-00-52 AND SOPM 20-42-01. (S) 2 L 7 2 4F RT A16WE 20080814 NM 2008 8 14 USAA920081427 1 20080715 A 5712 RIB BOEING 737 737401 1384701 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT - Q3 - MAJOR REPAIR - CRACK LT WING TANK RIB AT WBL 135.5 WING ROOT. REPAIRED LT WING TANK RIB AT WBL 135.5 IAW EA NR100548. (S) 2 L 7 2 4F RT A16WE 20080814 2008 8 14 USAA92081431 4 20080725 A 2565 LANYARD AIRCRUISERS AIRBUS 320 A320214 3930316 EU EVAC SLIDE UNSECURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 117UW 1224 1224 PIT - EES - DROP IN MAINTENANCE - L2 DOOR SLIDE SAFETY LANYARD NOT SECURED. RE-RIG LANYARD. (S) 2 L 7 2 4F RT A28NM 20080814 2008 8 14 USAA920081430 4 20080725 A 2565 LANYARD AIRCRUISERS AIRBUS 320 A320214 3930316 EU EVAC SLIDE UNSECURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 117UW A6110 1224 PIT - EES - DROP IN MAINTENANCE - R2 DOOR SLIDE SAFETY LANYARD NOT SECURED. RE-RIG LANYARD. (S) 2 L 7 2 4F RT A28NM 20080814 EA 2008 8 14 A6WA200840543 1 20080714 A 5610 NP1393216 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A A6WA K NONE D INFLIGHT SEPARATION AP APPROACH 1 GL 31 434AW 17773 7322 IN DESCENT, AT FL130, 310K IAS, RT WINDSHIELD INNER PANE CRACKED. REMOVED AND REPLACED RT WINDSHIELD. OPS AND LEAK CHE CK GOOD. (S) 2 L 7 2 4F RT A21EA 20080814 CE 2008 8 14 DXTA200803203 1 20080729 A 2421 GENERATOR CESSNA 750 750 2076810 CE LT ENGINE MALFUNCTIONED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 929QS 7500129 ON TAXI OUT TOWER REPORTED SEEING SMOKE COMING FROM OUR RT ENG. STOPPED ACFT, SHUT BOTH ENG/APU DOWN. DETERMINED THE S MOKE WAS COMING FROM THE LT AC GEN. (S) 2 L 7 2 4J RT T00007WI 20080814 WP 2008 8 14 UPS08852750 1 20080701 A 5313 4772397U1 FITTING DOUG DC8 DC871F 302199D WP BS 1760 L10L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, END FITTING CRACKED L10L, STA 1760. REMOVED AND REPLACED FITTING IAW, SRM. 51-1-20D, 51-1-8, 51-3-1 . 2 L 7 4 4F RT 4A25 20080814 SO 2008 8 14 C2XA08RI108 1 20080728 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO RT MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 11539 145536 FLIGHT 2756 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GRD FAIL MESSAGE JUST AFTER LIFT OFF AND GEARS COULD NOT BE RE TRACTED. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED RT L/G TRAILING WOW PROXIMITY SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080814 WP 2008 8 14 UPS08852766 1 20080716 A 3350 LENS DOUG DC8 DC871F 302199D WP EMERGNECY LIGHT MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 COCKPIT EMERGENCY LIGHT LENSE MISSING. 2 L 7 4 4F RT 4A25 20080814 NM 2008 8 14 08FDEA03058 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL TANK ACCESS CUTOUT 641MB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080814 NM 2008 8 14 08FDEA02885 1 20080715 A 5753 652163197 SKIN BOEING 727 727233 138408A NM FORE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 275FE 22040 LT WING T/E O/B FOREFLAP HAS DEEP GOUGE ON UPPER SURFACE AT WS 450. REMOVED DAMAGED AREA IAW B727 SRM 51-40-20 PARAGRAP H 12 AND FABRICATED FILLER AND DOUBLER FROM 2024T3 .016 (3 BY 3) AREA IAW B727 SRM 51-40-20 GAUGE 59. BONDED FILLER AND DOUBLER, SEALED EDGES AND PRIMED AREA IAW B727 SRM 51-40-20 PARAGRAPH 7-22. 2 L 7 3 4F RT A3WE 20080814 EU 2008 8 14 08FDEA03046 1 20080724 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 455FE 331 MAIN DECK FLOOR LEVEL COURIER COMPT TRACK BETWEEN FR 15A - FR 16A, -Y450 WITH EXFOLIATION CORROSION. REMOVED CORROSION PER SRM51-74-10.MATERIAL LOSS WITHIN LIMIT PER SRM53-10-16/103. 2 L 7 2 4F RT A35EU 20080814 CE 2008 8 14 7282008N406CS 1 20080724 A 2731 S37792H38214 CONTROL CABLE CESSNA 525 525 2076601 CE ELEVATOR TRIM CHAFED E Z5FA K NONE O OTHER NR NOT REPORTED 1 EA 63 406CS 2430 525B0043 ELEVATOR TRIM CABLE CHAFED ON PULLEY BRACKET P/N 6361201-1 IN VERTICAL STABILIZER. ENGINEERING ORDER WRITTEN TO ADD FAI RLEADS TO PREVENT FURTHER CHAFING. (S) 1 L 7 2 4F RT A1WI 20080814 CE 2008 8 14 7302008N409CS 1 20080725 A 2731 S37792H38214 CONTROL CABLE CESSNA 525 525 2076601 CE ELEVATOR TRIM CHAFED E Z5FA K NONE O OTHER NR NOT REPORTED 1 EA 63 409CS 2355 525B0050 ELEVATOR TRIM CABLE CHAFED ON PULLEY BRACKET P/N 6361201-1 IN VERTICAL STABILIZER. ENGINEERING ORDER WRITTEN TO ADD FAI RLEADS TO PREVENT FURTHER CHAFING. (S) 1 L 7 2 4F RT A1WI 20080814 WP 2008 8 14 08FDEA03004 1 20080721 A 5720 FAIRING DOUG MD10 MD1010F 3022112 WP LT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING INBD FAIRING PANEL 535 DL IS CHAFED. REPAIRED THE LT WING INBD FLAP FAIRING PANEL 535 P/N ARC 0740-501 BY F ABRICATING & BONDING THE SKINS; CORE; DOUBLERS; PHENOLIC FILLERS & INSTALLED HARDWARE IAW EA 8-5750-116997; DWG ARC 07 40 & TPS - 1001; REV E. 2 L 7 3 4F RT A22WE 20080814 WP 2008 8 14 IXX2008F00033 1 20080609 A 5753 SKIN DOUG DC8 DC872F 302199E WP T/E FLAP WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP UPPER SKIN SHOWS WEAR AT STATION XF 211.000. REMOVED FAS TENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND R EPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 4 TR 57-94 DATED 10-01-02, DC8 SRM 57-1- 0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B AND DC8 SRM 51-1-11. (S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 IXX2008F00036 1 20080609 A 5754 SKIN DOUG DC8 DC872F 302199E WP SLOT VANE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK, FOUND IMPROPER REPAIR ON LT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095.000 AND XS 247.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREAT ED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND PLATING IAW DC8 SRM 57-3-2 FIGURE 10 PAGE 22 ITEM "F", DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-3-0, AND SRM 5-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 IXX2008F00044 1 20080611 A 5313 LONGERON DOUG DC8 DC872F 302199E WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE CRACKED AT STATION FS 1610.000 LONGERON 17 RIGHT. REMOVED DAMAGED LONGERON. CLEANED, TREATED AND PRIMED AREA. INSTALLED LONGERON IAW DC8 SRM 53-5-2 FIGURE 5 SHEET 1 PAGE 16 ITEM "B", DC8 SRM 51-1-8B, DC8 SRM 53-1-0 PAGE 1, SRM 51-1-21, 51-1-20D, SRM 51-2-0 FIGURE 50 SHEET 37, 51-3-0, AND SRM 51-3-1. ( S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 IXX2008F00046 1 20080611 A 5313 LONGERON DOUG DC8 DC872F 302199E WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE CRACKED AT STATION FS 1610.000 LONGERON 17LEFT. REMOVED DAMAGED L ONGERON. CLEANED, TREATED AND PRIMED AREA. INSTALLED LONGERON. IAW DC8 SRM 53-5-2 FIGURE 5 SHEET 1 PAGE 16 ITEM "B", DC8 SRM 51-1-8B, DC8 SRM 53-1-0 PAGE 1, SRM 51-1-21, 51-1-20D, SRM 51-2-0 FIGURE 50 SHEET 37, 51-3-0, AND SRM 51-3-1. ( S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 08FDEA02864 1 20080714 A 5720 ARC0504501 SUPPORT DOUG MD10 MD1010F 3022112 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING OUTBD FLAP, INBD HINGE, FAIRING ATTACH BRACKET IS CRACKED AFT OF THE FLAP TRANSMITTER IN THREE LOCATIONS. REM OVED FAIRING TO FOM REF DC/MD-10 SRM 51-31-01; VOL II. REMOVED THE -1 TEE, -19 CLIP, -51 CLIP AND -1 CRACKED BRACKET RE F DC/MD-10 SRM 51-31-01, VOL II. LOCATED AND DRILLED NEW STRUCTURE AND INSTALLED A NEW STRUCTURE REF DC/MD-10 SRM 51-31 -01, VOL II. REINSTALLED FAIRING REF DC/MD-10 SRM 51-31-01, VOL II. 2 L 7 3 4F RT A22WE 20080814 WP 2008 8 14 08FDEA03032 1 20080723 A 5420 2170004505 FAIRING DOUG MD10 MD1010F 3022112 WP NR 3 PYLON WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 NR 3 PYLON PANEL 488 CR IS WORN AT THE FASTENER HOLES. BLENDED WORN AREA OUT OF LIMITS. ORIGINAL MATERIAL 0.050. MATE RIAL REMOVED IS 0.011. MATERIAL REMAINING IS 0.039 REF DC/MD-10 SRM 54-00-01, VOL I. FABBED REPAIR DOUBLER AND INSTALL ED DOUBLER REF DC/MD-10 SRM 54-00-01, VOL I AND SRM 51-33-01, VOL II. 2 L 7 3 4F RT A22WE 20080814 NM 2008 8 14 08FDEA03053 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL TANK ACCESS CUTOUT 641FB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS C LASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080814 WP 2008 8 14 IXX2008F00056 1 20080612 A 5330 SKIN DOUG DC8 DC872F 302199E WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C-CHECK INSPECTION, FOUND FUSELAGE EXTERNAL PART PRIMARY HEAT EXCHANGER LOWER AFT CORNER CRACKED AT STATI ON 188.000 LONGERON 27LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPEC TION. NO CRACK, NO CORROSION FOUND. FABRICATED EXTERNAL REPAIR DOUBLER, EXTERNAL REPAIR TRIPLER, AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 08378 DATE 7/11 /08, SEMAN DRAWING ED-4804 DATED 06/23/08, DC8 SRM 51-1-21, SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, SRM 51-1-11, SRM 51-1-20D, SRM 51-3-0, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 08FDEA03007 1 20080721 A 5347 601096418 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 303FE 46802 MAIN CARGO, LUGS ON SEAT TRACK ARE WORN AT FOUR PLACES BETWEEN FS 1249 - 1319 LBL 8. INSPECTED FOUND AREAS TO BE OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED NEW TRACK AND SPLICE HAT/PLATE AND INSTALLED ALL REPAIR PARTS ALL ON MAE TRAV ILERS T8/748406, T8/748404 AND SRM 53-70-00 FIG 1 AND FIG 5. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR AND IS REPORTA BLE AND IS RII. 2 L 7 3 4F RT A22WE 20080814 CE 2008 8 14 DXTA200803210 1 20080731 A 3240 BRAKE SYS CESSNA 500 560CESSNA 2076750 CE MALFUNCTIONED E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 303QS 5600343 F/O BRAKE PEDALS ARE SOFT. (S) 2 L 7 2 4F RT A22CE 20080814 NM 2008 8 14 08FDEA03061 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL TANK ACCESS CUTOUT 642CB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS C LASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080814 CE 2008 8 14 DXTA200803211 1 20080801 A 2120 UNKNOWN CESSNA 750 750 2076810 CE CABIN SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 984QS 7500084 ON THE GROUND WITH THE APU RUNNING APU BLEED SWITCH ON SMOKE WAS OBSERVED IN THE CABIN. KDTS-KGNV. (S) 2 L 7 2 4J RT T00007WI 20080814 CE 2008 8 14 DXTA200803213 1 20080803 A 3260 WARNING SYSTEM CESSNA 560 560XL 2076702 CE COCKPIT ACTIVATED E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 588QS 5605721 ON A VISUAL APPROACH SELECTED GEAR DOWN AND GOT ONLY TWO GREEN INDICATORS. (S) 2 L 7 2 4F RT A22CE 20080814 WP 2008 8 14 08FDEA02929 1 20080716 A 5753 ARC1949501 SKIN DOUG MD10 MD1010F 3022112 WP LT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING OUTBD FLAP, INBD LOWER SKIN HAS TWO CREASES BETWEEN RIBS 3 AND 4 FROM THE INBD SIDE. REMOVED DAMAGED AREA IAW SRM 57-10-00, VOL I, FIG 85. FABRICATED A REPAIR DOUBLER IAW SRM 57-10-00, VOL I, FIG 85. ALODINE AND PRIMED REPAIR D OUBLER IAW SRM 51-21-01, VOL II. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00, VOL I, FIG 85. 2 L 7 3 4F RT A22WE 20080814 NM 2008 8 14 KCSA081370 1 20080804 A 5330 SKIN BOEING 747 747122 1384872 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FUSELAGE SKIN DAMAGED AT BS 1865, BETWEEN STR 50R AND 51R. (S) 2 L 7 4 4F RT A20WE 20080814 EA 2008 8 14 TRAX200800938 1 20080728 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 926EV 7843 FS 484.0, RBL 36.0 INTERCOSTAL CRACKED (NOT PREVIOUSLY REPAIRED). REPAIRED INTERCOSTAL AT FS 484.0 RBL 36.0 IAW REO 601 R-53-41-059. COMPLIED WITH REO 601R-53-41-059. PRESSURE CHECK DUE. PERFORMED PRESSURE CHECK IAW AMM 21-32-00-863-801. NO DISCREPANCIES NOTED AT THIS TIME. RII COMPLIED WITH 5300002. (S) 2 L 7 2 4F RT A21EA 20080814 EA 2008 8 14 TRAX200800941 1 20080728 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 GL 23 886AS 7531 NR 1 INTERIOR CEILING EMERGENCY LIGHT OUT. REMOVED AND REPLACED INTERIOR CEILING EMERGENCY LIGHT LAMP. OPS CHECK GOOD IAW AMM 33-51-16. (S) 2 L 7 2 4F RT A21EA 20080812 NM 2008 8 12 USAA920081421 1 20080702 A 5340 ATTACH ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT-Q3- MAJOR REPAIR - LEVEL 2 CORROSION ON FUSELAGE FRAME SKIN ATTACH ANGLE BS 787 BETWEEN S26R AND S27R. REPAIRED FUS ELAGE FRAME SKIN ATTACH ANGLE BS 787 BETWEEN S26R IAW B737 SRM 53-00-07. (A) 2 L 7 2 4F RT A16WE 20080812 EU 2008 8 12 USAA920081424 1 20080726 A 5720 D57252920200 ANCHOR FITTING AIRBUS 320 A320231 3930325 EU LT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 627AW 66 SAL-C6- MAJOR REPAIR - CORROSION ON ANCHORAGE FITTING LT WING. REPAIRED ANCHORAGE FITTING LT WING IAW US AIRWAYS EA 132 038. (A) 2 L 7 2 4F RT A28NM 20080813 EU 2008 8 13 08FDEA02659 1 20080703 A 5321 B5327051500200 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN FLOOR PANEL 231 DH IS WORN THROUGH THE TOP AND IS PUNCTURED. REPAIRED DAMAGED AREA IAW A300-600 SRM 53-10-20 ; FIG 201. 2 L 7 2 4F RT A35EU 20080813 NM 2008 8 13 08FDEA02861 1 20080714 A 5753 6521658369 RETAINER BOEING 727 727225 1384077 NM LT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 LT WING TE FLAP WELL LWR PNL BULB SEAL RETAINER IS CRACKED 15 INCHES OUTBOARD OF NR 2 FLAP TRANSMISSION (MKD). REMOVED SEAL RETAINER REF SRM 51-30-2. FABRICATED RETAINER REF DWG 65-21658 AND GMM 7-0-1001. INSTALLED SEAL RETAINER REF SRM 51-30-2 AND IDENTIFIED RETAINER. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080813 EU 2008 8 13 08FDEA02900 1 20080715 A 5230 A52374263212 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION AT AFT CARGO DOOR C 59-63A, INNER SKIN PANEL (BETWEEN LONGERON 3-4) OUT OF LIMIT. REPAIR PERFORMED BY S MOOTH BLEND OUT OF CORROSION, NDT FOR CRACK FREE CONDITION AND FLAP PEENING IAW RAS/DAHAM/4025300/2008 ISS A, APRROVED B Y EA 6-5232-123025. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02681 1 20080703 A 5321 B5327048300600 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CARGO DECK FLOOR PANEL 232 SG HAS PUNCTURES AND BALL BEARINGS STUCK TO THE TOP SURFACE. REPAIRED DAMAGED FLOOR PAN EL IN REF TO A300-600 SRM 53-10-20; FIG 202. 2 L 7 2 4F RT A35EU 20080813 WP 2008 8 13 NWAA082679755 1 20080609 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 755NW 47179 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE VENTRAL STAIRWAY WERE INOPERATIVE. MAIN TENANCE ATTEMPTED CORRECTION BY RELAMPING BUT ENDED UP REPLACING THE BATTERIES IN THE BATTERY PACK B5-28. THE LIGHTS RE TURNED TO AN OPERATIONAL CONDITION. (A) 2 L 7 2 4F A6WE 20080813 EU 2008 8 13 USAA920081419 1 20080726 A 3150 WARNING LIGHT AIRBUS A319 A319112 3930323 EU RT WING TANK FALSE ACTIVATION A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 703UW 0904 FLT 1062 CREW REPORTED `FUEL RT WING TANK LOW LVL` AND FUEL RT XFER VALVE FAULT WHILE ENROUTE. CAPTAIN ADVISED, COULD N OT GET FUEL TO TRANSFER FROM THE OUTER CELL TO THE INNER CELL OF BOTH WINGS. ACFT DIVERTED AND LANDED WITHOUT INCIDENT. MX ACCOMPLISHED TANK LEVEL SENSING TASK 28-46-00-810-819-0 THROUGH STEP 3B. NO FAULTS. OPS CHECKED INTERCELL FUEL TR ANSFER VALVES PER TASK 28-15-00-710-002-0, NO FAULTS. FUNCTIONAL BITE TESTED FLSCU PER TASK 28-46-00-810-819-0, NO FAUL TS. PERFORMED GROUND SCANNING OF CWS PER TASK 31-50-00-710-001. NO FAULTS. TROUBLESHOT INTERCELL TRANSFER SYSTEM IAW TSM 28-15-00-810-801 THRU 806 & 28-46-00-810-819, NO DISCREPANCIES FOUND. ALL FOUR TRANSFER VALVES VERIFIED TO OPERATE 2 L 7 2 4F RT A28NM 20080813 EU 2008 8 13 08FDEA02908 1 20080716 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD FH1126 630 FOUND CHAFING MARKS ON LT INBOARD FLAP TOP SKIN RIB 1C. REPAIR PERFORMED BY INSTALLING EXTERNAL PATCH IAW RAS/FOK/161/2 008 ISS B, APPROVED BY EA-5752-120086A. 2 L 7 2 4F RT A35EU 20080814 2008 8 14 UPS08M52644 4 20080703 A 2565 SWITCH DOUG MD11 MD11F 3023600 NM ESCAPE SLIDE INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 294UP 48472 REF M379214, R1 PUSH-TO-TEST SWITCH INOP. COMPLIED WITH DMP 25-61-2 SLIDE PRESSURE GOOD. ITEM REMAINS ON DEFERRAL. 2 L 7 3 4F RT A22WE 20080703 SW 2008 7 3 Z0A2008F00000 1 20080407 A 2910 70061H000A180A HYDRAULIC LINE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL HYDRAULIC SYSTEM DEFECTIVE E Z0AA O OTHER O OTHER CR CRUISE 1 WP 07 98AZ 2296 LOSS OF HYDRAULIC SYSTEM IN FLIGHT RESULTING IN PILOT RETURNING TO AIRPORT UNEVENTFULLY. HYDRAULIC SYSTEM HOSE WAS FOUN D DEFECTIVE. (K) 1 G 7 1 3U 3 U H2SW E4CE 20080703 NE 2008 7 3 NACA20080009 2 20080514 A 7200 JT8D15A ENGINE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE OUT OF TRIM A NACA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 AL 03 320DL 52373 23092 700533 NR 2 ENGINE NOT MAKING TAKEOFF THRUST. REJECTED TAKEOFF AT APPROXIMATELY 80 KNOTS. FOD INSPECTION COMPLETED WITH NO DE FECTS. FOUND ENGINES OUT OF TRIM. TRIMMED NR 1 AND NR 2 ENGINES BACMM 71-09-200. OPERATIONAL CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E2EA 20080703 NM 2008 7 3 CALA0800579 1 20080602 A 2560 ACREM1A MEGAPHONE BOEING 737 737924ER 13848A3 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 37419 31666 AFT MEGAPHONE ALARM DOES NOT WORK. REMOVED AND REPLACED MEGAPHONE. OPERATION CHECKS GOOD. 2 L 7 2 4F RT A16WE 20080707 WP 2008 7 7 U2RA290LP3020 2 20080514 A 7261 9AA110811B OIL SYSTEM BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UHR WP MCAULY 4HFR34 4HFR34C653 NE RT ENGINE DAMAGED A U2RA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 290MA 800 P66005C 080097 RIGHT ENGINE OIL LIGHT ALONG WITH RED ATTENTION LIGHT ILLUMINATED DURING FLIGHT NOTED WITH A RAPID DROP IN INDICATED OIL PRESSURE ON RIGHT ENGINE. PRECAUTIONARY ENGINE SHUT DOWN WAS SATISFACTORILY INITIATED WITHOUT FURTHER INCIDENT AS PER COMPANY QRH BY THE FLIGHT CREW. 2 L 7 2 4T 4 T RT A56EU E4WE 6 C 3PNE 20080707 EA 2008 7 7 COMA0860237 1 20080503 A 2140 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA POPPED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 937CA 7044 FLIGHT 5314 - EN ROUTE FROM PWM TO CVG, C/B 1B8 POPPED (CARGO BAY HEATER). EMERGENCY DECLARED AND A/C DIVERTED TO ALB A ND LANDED SAFELY. DUE TO ANIMAL IN CARGO BAY. TRANSFERRED TO DMI LIST PER MEL 21-55-05-1. 2 L 7 2 4F RT A21EA 20080707 EA 2008 7 7 COMA0860238 1 20080507 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 7038 DURING FS 640 FRAME INSPECTION FOUND FORWARD FRAME CRACKED ON RT SIDE BELOW ENGINE SUPPORT BEAM. CUT OUT DAMAGED SECTIO N OF FRAME AND REPLACED WITH SPLICED IN REPAIR TO FRAME AND BONDED DOUBLER PER REO 601R-53-61-506, REV C. 2 L 7 2 4F RT A21EA 20080707 2008 7 7 COMA0860239 4 20080511 A 3442 6229302003 RADAR CNDAIR CL600 CL6002B19 1900309 EA WEATHER RADAR FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 937CA 12878 7044 FLIGHT 5223- DURING CLIMB-OUT FROM CVG TO RDU RECEIVED RADAR FAULT MESSAGE. AIRCRAFT RETURNED BACK TO CVG AND LANDED SA FELY. REMOVED AND REPLACED WEATHER RADAR. 2 L 7 2 4F RT A21EA 20080707 SO 2008 7 7 C2XA08ON123 1 20080510 A 2611 M8353613008M RELAY EMB 145 EMB145LR 3260212 SO SMOKE WARNING BLOWN A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 19544 14554 14554 145557 FLT 0119 - ONT - FLIGHT CREW REPORTED BAGGAGE SMOKE DETECTOR WILL NOT TEST. MX REMOVED AND REPLACED RELAY K0630 OPERATI ONALLY CHECKED SATISFACTORY AIRCRAFT WAS RELEASED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20080707 SO 2008 7 7 C2XA08CL059 1 20080515 A 2131 22250N030301 CONTROLLER EMB 145 EMB145XR 3260214 SO CABIN PRESSURE FAULTY A C2XA B EMER. DESCENT O OTHER CR CRUISE 1 SW 27 11121 14435 145683 EWR FLIGHT NR 2753, THE CREW REPORTED AT FL370 THE PRESSURIZATION STARTED CLIMBING TO 14,000 FT. EMERGENCY DESCENT STAR TED AND THE PRESSURIZATION STARTED DESCENDING. THE FLIGHT DIVERTED TO CLE. MAINTENANCE INSPECTED AND REPLACED THE DIGI TAL PRESSURIZATION CONTROLLER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 20080707 EU 2008 7 7 SA08035 1 20080512 A 3397 WIRE HARNESS AIRBUS A319 A319112 3930323 EU CABIN SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 724UW 1122 TPA - EMERGENCY LIGHTS AT 18 LF INOP. MAINTENANCE REPLACED THE WIRE HARNESS FROM WALL TO SEAT. OPERATIONALLY CHECKS OK . 2 L 7 2 4F RT A28NM 20080707 WP 2008 7 7 UPS08852253 1 20080421 A 5711 576958961 FRAME DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING CENTER LE 3 INCH CRACK IN FRAME ABOVE PNEUMATIC DUCT XFS 410. REPAIRED LT WING CENTER LE AND FABRICATED INTERCOSTAL AND INSTALLED AT XFS 410 IAW DWG 57-69-589, SRM 51-01-21 AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 20080707 WP 2008 7 7 UPS08852254 1 20080422 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 RT SEAT TRACK DAMAGED RBL 46 FROM STA 380-STA 385. REPAIRED CABIN SEAT TRACK AT RBL 46 STA 380 TO ST A 385 IAW SRM 53-02-0 3-FIG 006D, SRM 51-01-08, SRM 51-03-00. 2 L 7 4 4F RT 4A25 20080707 WP 2008 7 7 UPS08852255 1 20080421 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING CENTER LE UPPER RIB CRACKED AT XFS 434. REPAIRED LT WING CENTER LE UPPER RIB AT XFS 434 IAW SRM 57-02-00-0 FIG 002, SRM 57-03-03-0 FIG 005. 2 L 7 4 4F RT 4A25 20080707 WP 2008 7 7 UPS08852273 1 20080428 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING CENTER LE INBD UPPER RIB GOUGED AT PNEUMATIC DUCT STA 494. REPAIRED LT WING CENTER LE INBD U PPER RIB AT STA XFS 494 IAW SRM 57-02-00 FIG 002, 57-03-03-0 FIG 005 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 20080707 NM 2008 7 7 UPS08M52264 1 20080428 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C CABIN-STA 839-899 SEAT TRACK CROWN AREA, X=-27.50 FOUND CORROSION AS MARKED. CORROSION AT CABIN STA 8 39-899 X=-27.5 ON SEAT TRACK CROWN SURFACE AREA REMOVED AS PER SRM 51-21-01 V.II R35. EXISTING SEAT TRACK SPLICE AT STA 816 REMOVED PER SRM 51-31-01 VII R35. HFEC INSP C/O PER DAC NDTSPM R1 3 06-10-01.001 ON TRIMMED OFF AREA AND FOUND NO CRACK. NEW SEAT TRACK REPAIR SECT AND SPLICES INSTALLED PER SRM 51-31-01 V.II REV 35. 2 L 7 3 4F RT A22WE 20080707 SO 2008 7 7 C2XA08IA128 1 20080514 A 3411 PITOT LINE EMB 145 EMB145LR 3260212 SO PITOT/STATIC SYS CONTAMINATED A C2XA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 SW 27 15912 145439 IAH - FLIGHT 2546, DURING FLIGHT IN IMC DESCENDING THROUGH FL320 THE CREW REPORTED A STRONG BURNING SMELL IN THE COCKPIT FOLLOWED BY AN SPS ADVANCED MESSAGE ON EICAS, IAS AND ALT ON BOTH PFD'S, CAPT AIRSPEED DOWN TO 147KTS, AND FO'S TO 157K TS, FOLLOWED BY LOSS OF F/O AIRSPEED AND ALT. FLEW AIRCRAFT BY ISIS TO BELOW 15000 FT WHEN THE INSTRUMENTS RETURNED TO NORMAL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, DRAINED WATER FROM THE PIT OT SYSTEMS, FOUND RT FWD AVIONICS COMPT SHUTOFF VALVE TO BE INOPERATIVE. REMOVED AND REPLACED RELAYS K0039 AND K0040, W ITH NO HELP, PLACED SHUTOFF VALVE ON MEL 21-26-00/1 CTL NR 145947. OPERATIONALLY CHECKED PITOT STATIC SYSTEM SATISFACTO 2 L 7 2 4T RT T00011AT 20080707 NM 2008 7 7 2008UALA02760 1 20080513 A 3397 362624 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY LIGHT ROW 4A FWD INOP. FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 2008UALA02761 1 20080513 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY LIGHT ROW 5J INOP. RELAMPED. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 EU 2008 7 7 2008UALA02780 1 20080513 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT ODOR A UALA O OTHER W E B INADEQUATE Q C VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 436UA 638 IN FLIGHT HAD NOISE AND VIBRATION BELOW FLT DECK (RUDDER PEDAL AREA) WITH BURNING RUBBER (ELECT) SMELL FOLLOWED BY AEVC VENT BLOWER FAULT. 2 L 7 2 4F 4 F RT A28NM E40NE 20080707 2008 7 7 2008UALA02791 4 20080513 A 2565 101651303 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 648UA 25285 LEAKING ASPIRATOR. SUPPLEMENTAL DATA UPDATE, POSSIBLE MANUFACTURER DEFECT. REPLACED ASPIRATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 20080707 NM 2008 7 7 2008UALA02799 1 20080515 A 5753 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE LT WING TE FLAPO DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 LT OTBD FLAP INBD EDGE DELAMINATED 4 INCH BY 7 INCH. MOISTURE IS PRESENT. REPLACED LT OUTBOARD AFT FLAP AND OPS CHECKE D REF MM 27-51-39-401. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 20080707 NM 2008 7 7 2008UALA02800 1 20080514 A 3350 20131A BATTERY BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 910UA 25254 MID CABIN EMERGENCY LIGHTING INOPERATIVE. REPLACED BATTERY AND OP CHK'D GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 20080707 NM 2008 7 7 2008UALA02801 1 20080515 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 CEILING EMERGENCY LIGHT NEAR SEAT ROW 3L IS INOP. RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080808 EU 2008 8 8 08FDEA02653 1 20080703 A 5754 A5786353300200 BOLT AIRBUS 300 A300F4605R 3930327 EU NR 1 SLAT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 RIGHT WING NR 1 SLAT; NR 2 TRACK FWD BOLT IS PITTED. REMOVED AND REPLACED THE BOLT ON THE RIGHT WING NR 1 SLAT; NR 2 TR ACK FWD BOLT IAW FEDEX A300-600 AMM 27-80-11-4. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02466 1 20080625 A 5330 651842016 SKIN BOEING 727 727227 1384078 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 LT FWD FUSELAGE STA 190 STR 27L REPAIR DOUBLER HAS SKIN BULGES AND DENTS. CUTOUT DAMAGED AREA DIMS 1 1/4 INCH BY 1 1/2 INCH IAW SRM 53-10-3 FIG 5. FABRICATED DOUBLER REPAIR USING 2024-T3 .050 PO NR 9006288 DIMS 10 1/2 INCH BY 13 1/2 INCH AND FILLER USING 2024-T3 .040 PO NR 9007107 DIMS 1 1/4 INCH BY 1 1/2 INCH IAW SRM 53-30-2 FIG 1, 53-30-3 FIG 3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20080808 NM 2008 8 8 08FDEA02493 1 20080626 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 609FE 48549 DURING OPEN HOLE HFEC INSPECTION, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR C AND NR D (3RD LAYER). MOUNTING HOLES NR A, NR C AND NR D ON MAIN CARGO DOOR NR 1 JAMB SUPPORT BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL I. CRACK FITTING ON NR 1 JAMB AREA REMOVED AND REPLACED WITH A NEW FITTING AS PER SRM 51-33-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080808 NM 2008 8 8 08FDEA02495 1 20080626 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 609FE 48549 DURING OPEN HOLE HFEC INSPECTION, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLES NR A AND NR B (3RD LAYER). MOUNTING HOLES NR A AND NR B ON THE MAIN CARGO DOOR NR 3 JAMB SUPPORT BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL I. CRACK FITTING ON NR 3 JAMB AREA REMOVED AND REPLACED WITH A NEW FITTING AS PER S RM 51-33-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080808 NM 2008 8 8 08FDEA02643 1 20080703 A 5320 146N5447U16 FLOOR SUPPORT BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 CORROSION FOUND ON FLOOR STRINGER FROM BS 1445 TO BS 1510, RBL16.21. CORROSION FOUND EXCEED ALLOWABLE LIMITS IN B757-20 0SRM 51-10-02. STRINGER REMOVED AND REPLACED IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080808 NM 2008 8 8 08FDEA02810 1 20080710 A 5414 311N504632 SKIN BOEING 757 75727B 1384921 NM ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 916FD 24137 SURFACE CORROSION FOUND ON PYLON NUMBER TWO LEFT SIDE INNER SKIN FORWARD OF ACCESS PANEL 443LL, PPS 126 TO PPS 181. EVALUATE AND RECTIFY. REPLACED LEFT SIDE INNER SKIN FORWARD OF ACCESS PANEL 443LL OF PYLON NUMBER TWO IN ACCORDANCE WIT H BOEING DRAWING 311N5046, BOEING DRAWING 311N5002 AND B757-200 SRM 51-10-02 REV 93. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-02-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080808 NM 2008 8 8 08FDEA02756 1 20080708 A 5312 6529567 BULKHEAD BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 FUSELAGE STA 1183 BULKHEAD RT LOWER MIDDLE FLOOR WEB CRACKED. REF EO 7-5320-7- 310 PT 1. REPLACED WEB AND ANGLE REF SR M 51-30-02 PG 4. 2 L 7 3 4F A3WE 20080808 EU 2008 8 8 08FDEA02600 1 20080701 A 5210 A52175004202 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 800 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 743FD 630 FOUND OLD DOUBLER REPAIR AT PAX DOOR NR 4 LT LOWER AFT CORNER NOT IAW SRM 52-10-00 FIG 203. PERFORMED (DOUBLER THICKNES S TO LESS) DOUBLER REPAIR RENEWED IAW SRM 52-10-00 FIG 203. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02717 1 20080706 A 5230 A52371015002 SKIN AIRBUS 300 A300F4605R 3930327 EU CARGO DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 660FE 759 EXTERNAL SURFACE OF MD CARGO DOOR HAS DENT 2" (L) BY 1.2 INCH WIDE BY .060" DEEP. EDGE OF NEAREST RIB TO DEEPEST POINT APROX. .950". LOCATED LONGERON 4, BELOW STR 14 AFT OF FR21. COMPLIED WITH EA6-5230-121322 BY INSTALLING EXTERNAL SKIN REPAIR IAW A300-600 SRM 53-10-12 FIG 208 SHEET 1. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02528 1 20080627 A 5321 B5327048401800 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 231 WG IS CRUSHED AND PUNCTURED. FABRICATED A NEW PANEL 231 WG, POTTED INSERTS, POTTED, CUR ED; SANDED EDGES, APPLIED NON-SKID TAPE AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02529 1 20080627 A 5321 B5327048402400 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 231 VG IS CRACKED AND CRUSHED. FABBED A NEW PANEL 231 VG BY POTTING INSERTS, POTTED, CURED, SANDED EDGES, APPLIED NON-SKID AND PART MARKED IAW FEDEX DG SRZ 25-005, REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 M7K2008F00110 1 20080324 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE DEFECTIVE E M7KA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 806MH 193 3833 23220 FAILURE CODE AT SHUTDOWN INDICATED A FAULT WITH THE COLLECTIVE POTENTIOMETER. INSTALLED NEW POTENTIOMETER AND NO FURTHE R PROBLEM NOTED. THIS IS A VERY COMMON FAULT FOR THIS PART THAT EFFECTS THE DISPATCH RELIABILITY FOR THIS MODEL AIRCRAF T. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080808 EU 2008 8 8 M7K2008F00082 1 20080414 A 5302 350A23422321 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM CRACKED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 807MH 3481 3912 23130 DURING ROUTINE INSPECTION A CRACK WAS DISCOVERED THROUGH THE STRENGTHENING RIB OF THE MOUNTING FLANGE. CRACK DEVELOPMEN T IS A VERY COMMON FAILURE FOR THIS PART. SUGGEST A MORE ROBUST MATERIAL SUCH AS SS OR TITANIUM BE UTILIZED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00107 1 20080414 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE DEFECTIVE E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 808MH 99 3914 23072 UPON AC SHUTDOWN A FAILURE CODE WAS GENERATED INDICATING THE COLLECTIVE POTENTIOMETER WAS DEFECTIVE. A NEW PART WAS INST ALLED WITH NOT FURTHER DEFECT REPORTED. THIS IS A REOCCURRING PROBLEM FOR THIS PART THAT HAS EFFECTED THE DISPATCH RELI ABILITY FOR THIS MODEL AIRCRAFT. AS THIS DESIGN HAS SUCH A HIGH FAILURE RATE PERHAPS AN OPTIC DESIGN WITH NO CONTACT WI TH A RESISTANCE RIBBON AS WITH THE CURRENT DESIGN SHOULD BE CONSIDERED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 CE 2008 8 11 DXT2008F00000 1 20080723 A 2120 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C 03047 GL CABIN SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 931QS 7500064 AFTER INITIAL START OF APU UPON OPENING BLEED AIR AND ISOLATION VALVE, LT LOWER COCKPIT AREA BEGAN FILLING WITH BLUE/GRE Y SMOKE AND UPON SHUTDOWN OF APU AND CLOSING ISOL VALVE/BLEED VALVE, SMOKE DISSIPATED. (K) 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080811 CE 2008 8 11 DXTA200803129 1 20080617 A 3244 TIRE CESSNA 500 560CESSNA 2076750 CE RT MLG FAILED E DXTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 837QS 5600685 RT MAIN TIRE BLEW ON TAKEOFF ROLL, ABORTED T/O. (B) 2 L 7 2 4F RT A22CE 20080811 EA 2008 8 11 MAL2008F00009 1 20080707 A 2163 SENSOR CNDAIR CL600 CL6002D24 1390016 EA A/C PACK TEMP MALFUNCTIONED A MALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 GL 15 923XJ 15177 THE CREW HAD A RT BLEED DUCT FAULT WARNING AND NOTED A SLIGHT SMELL OF SMOKE IN THE COCKPIT. CREW FOLLOWED QRH AND MADE SURE PACK WAS SHUTDOWN; DIVERTED. REPLACED TEMP SENSOR. (K) 2 L 7 2 4F RT A21EA 20080811 CE 2008 8 11 DXTA200803168 1 20080710 A 2800 FUEL SYS CESSNA 750 750 2076810 CE LEAKING E DXTA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 GL 07 921QS 7500241 DURING FUELING ON THE GROUND FUEL LEAKED OUT OF LT TANK OVERFLOW VENT AND AMBER CAS WING TANK O FULL L CAME ON APPROX 20 GALS OF FUEL LEAKED OUT ON RAMP. (A) 2 L 7 2 4J RT T00007WI 20080811 EA 2008 8 11 TRAX200800772 1 20080602 A 5220 HINGE FITTING CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 684BR 7708 JOB 8770831 OPERATION 152 CREW ESCAPE HATCH RIGHT HINGE ARM IS CRACKED. RESOLVED ON W/O: 91780 TASKCARD: N/R-00192. RE MOVED AND REPLACED RT HINGE ARM ON CREW ESCAPE HATCH IAW CRJ 200 AMM 20-21-00-910-801. OPS TEST GOOD IAW CRJ 200 AMM 52 -22-00-710-801. ASA RII C/W 5300010 [SDR CLOSED] 2 L 7 2 4F RT A21EA 20080811 WP 2008 8 11 AALA200801700 1 20080625 A 2613 CLAMP DOUG DC9 DC982 3022082 WP A/C BAY DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 7531A 49923 ORD INFLIGHT T1345/25JUN. CREW REPORTED TAIL COMPARTMENT OVERHEAT INDICATION DURING CLIMB. INDICATION EXTINGUISHED WHE N LT AIR CONDITIONING SWITCH PLACED TO OFF POSITION. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED CLAMP AND S HIM AT LT HEAT EXCHANGER INLET. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 WP 2008 8 11 AALA200801711 1 20080626 A 1100 PLACARD DOUG DC9 DC982 3022082 WP TAILCONE MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 474 49649 LGA - PLACARD AT TAIL CONE OUTER LT EMERGENCY EXIT MISSING. REPLACED PLACARD FOR AT TAIL CONE OUTER LT EMERGENCY EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 WP 2008 8 11 AALA200801791 1 20080707 A 3350 LENS DOUG DC9 DC983 3022083 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 984TW 53634 SFO - EMERGENCY LIGHT AT SEAT 5E MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NOR MAL OPERATION. (A) 2 L 7 2 4F RT A6WE 20080811 CE 2008 8 11 DJFA2008058 1 20080622 A 2150 11341041 MOTOR BEECH MU300 400A 1155402 CE AIR CON BURNED E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 23 785TA 6956 RK239 DURING AIR CONDITIONER OPERATION, UNIT PULLED HIGH AMPS AND POPPED AIR CONDITIONER CIRCUIT BREAKER. A BURNING SMELL WAS APPARENT NEAR THE REAR OF THE AC. THE AIR CONDITIONER COMPRESSOR MOTOR WAS FOUND BURNED UP. THE MOTOR WAS REMOVED AND R EPLACED. (A) 2 H 7 2 4F RT A16SW 20080811 NM 2008 8 11 AALA200801703 1 20080625 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 917AN 29518 JFK - EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 AALA200801671 1 20080619 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT SEAT 20C MISSING LENS. REPLACES LENS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080811 WP 2008 8 11 AALA200801713 1 20080626 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7520A 49897 LGA - EMERGENCY LIGHT AT SEAT 19D INOPERATIVE. CLEANED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROUND CHECKE D NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 EU 2008 8 11 M7K2008F00054 1 20080324 A 5300 350A58004523 HINGE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE INLET CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 817MH 105 4125 23292 DURING ROUTINE INSPECTION A CRACK WAS FOUND IN THE HINGE MOUNTING FLANGE RADIATING FROM THE OUTERMOST LT ATTACHMENT SCRE W BORE. THIS IS A VERY COMMON FAILURE FOR THIS PART. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 AALA200801553 1 20080606 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 JFK - EMERGENCY EXIT SIGN LIGHT AT RT NR THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT NR THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080811 WP 2008 8 11 AALA200801709 1 20080626 A 3350 6016125 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 418AA 49329 SFO - EMERGENCY LIGHTS AT SEAT ROWS 18 TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT FOR EMERGENCY LIGHTS AT SEAT ROWS 18 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 WP 2008 8 11 AALA200801708 1 20080626 A 3350 6016125 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 418AA 49329 SFO - EMERGENCY LIGHTS AT SEAT ROWS 18 TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT FOR EMERGENCY LIGHTS AT SEAT ROWS 18 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 CE 2008 8 11 DXTA200803173 1 20080714 A 3150 WARNING MESSAGE CESSNA 750 750 2076810 CE RUDDER LIMIT ILLUMINATED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 934QS 7500034 RUDDER LIMIT- A FAIL MESSAGE APPROXIMATELY 5 MINUTES AFTER TAKEOFF. RUDDER LIMITS TO 22 PERCENT. (A) 2 L 7 2 4J RT T00007WI 20080811 EA 2008 8 11 A6WA200840522 1 20080618 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 444ZW 7788 REPAIR CRACK ON PASSENGER DOOR. PASSENGER DOOR EDGE MEMBER REPAIRED IAW CRJ 200 REO 601R-53-11-279. (A) 2 L 7 2 4F RT A21EA 20080811 CE 2008 8 11 GUU2008F00019 1 20080525 A 5210 10151417617 PIN BEECH 1900 1900D 1154162 CE DOOR HANDLE BROKEN A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 81556 UE239 FLIGHT 9292, PILOT REPORTED CABIN DOOR HANDLE FELL OFF. HANDLE INNER PIN BROKEN. C/A REPLACED CABIN DOOR HANDLE. (A) 2 L 7 2 4T RT A24CE 20080811 CE 2008 8 11 GUU2008F00020 1 20080621 A 3260 H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE RT MLG FAILED A GUUA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 17 81556 UE239 FLIGHT 9270, PILOT REPORTED LANDING GEAR HANDLE LIGHT STAYED ILLUMINATED AFTER LANDING GEAR RETRACTED. REPLACED RT MLG U PLOCK SWITCH. OPERATIONAL CHECK NORMAL. (A) 2 L 7 2 4T RT A24CE 20080811 SO 2008 8 11 XGN2008F00008 2 20080723 A 8530 CYLINDER CESSNA 402 402B 207590P CE CONT O520 IO520* 17032 SO ENGINE CRACKED E XGNA O OTHER O OTHER NR NOT REPORTED 1 SW 05 5421M 811 402B0021 CRACKED BETWEEN FIN NR 1 AND FIN NR 3 AFT OF THE INJECTOR. MFG REV 3 E SERIES CYLINDER. ALL DEFECTIVE. (K) 1 L 7 2 3O 3 O A7CE E5CE 20080811 SO 2008 8 11 XGN2008F00006 2 20080723 A 8530 CYLINDER CESSNA 402 402B 207590P CE CONT O520 IO520* 17032 SO ENGINE CRACKED E XGNA O OTHER O OTHER NR NOT REPORTED 1 SW 05 5421M 811 402B0021 CRACKED BETWEEN FIN NR 1 AND FIN NR 3 AFT OF THE INJECTOR. ECI REV 3 E SERIES CYLINDER. ALL DEFECTIVE. (K) 1 L 7 2 3O 3 O A7CE E5CE 20080811 SO 2008 8 11 XGN2008F00007 2 20080723 A 8530 CYLINDER CESSNA 402 402B 207590P CE CONT O520 IO520* 17032 SO ENGINE CRACKED E XGNA O OTHER O OTHER NR NOT REPORTED 1 SW 05 5421M 811 402B0021 CRACKED BETWEEN FIN NR 1 AND FIN NR 3 AFT OF THE INJECTOR. MFG REV E SERIES CYLINDER. ALL DEFECTIVE. 1 L 7 2 3O 3 O A7CE E5CE 20080811 NM 2008 8 11 AALA200801752 1 20080701 A 3397 CONNECTOR DOUG MD80 MD83 3023681 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9412W 53187 SFO - EMERGENCY LIGHT AT SEAT ROW 9D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHEC KED NORMAL OPERATION. (A) 2 L 7 2 4F RT 20080811 NM 2008 8 11 AALA200801753 1 20080701 A 3397 CONNECTOR DOUG MD80 MD83 3023681 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9412W 53187 SFO - EMERGENCY LIGHT AT SEAT ROW 27D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 27D. SYSTEM GROUN D CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT 20080811 2008 8 11 DXTA200803171 4 20080713 A 3425 COMPUTER CESSNA 560 560XL 2076702 CE NR 2 AHRS FAILED E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 633QS 5605526 NR 2 AHRS FAILED IN FLIGHT. RT PFD DISPLAYED "ATT FAIL" AND "HDG FAIL" EMERGENCY CHECKLIST TAB V4 AND X1 COMPLIED WITH. (A) 2 L 7 2 4F RT A22CE 20080811 NM 2008 8 11 AALA200801772 1 20080704 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 175AN 32394 DFW - EMERGENCY LIGHT AT SEAT 16D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 2008 8 11 USAA920081332 4 20080709 A 2330 12748101 PCU AIRBUS A321 A321211 3930370 EU CABIN BROKEN A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 165US 1431 LOG PAGE 8094485-FLT NR 716 LAX-PHL - BURNING SMELL, FLIGHT ATTENDANT REPORTED LIGHT ELECTRICAL ODOR NEAR ROW 16. MAINT ENANCE FOUND A HEADSET PLUG BROKEN OFF AT SEAT 16D PLUG CONNECTION POINT. MALE END OF HEADSET IS STUCK IN PLUG. MAINTE NANCE REMOVED AND REPLACED THE PASSENGER CONTROL UNIT. OPERATIONAL CHECK GOOD. (B) 2 L 7 2 4F RT A28NM 20080811 NM 2008 8 11 USAA920081371 1 20080703 A 5320 6936656U9 INTERCOSTAL BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT-Q3 CHECK MAJOR REPAIR NR 03C10853029/013- INTERCOSTAL L-ANGLE CRACKED BS 927 TO 947, BL0. REPLACED INTERCOSTAL L-AN GLE BS 927 TO 947, BL0 IAW B737 SRM 51-10-02. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081355 1 20080710 A 2560 P2070001214 FLASHLIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 156AW 23778 LOG 8025703- IAH- FLT NR 280- FWD GALLEY AREA EMERG FLASHLIGHT INOP. MX REPLACED FLASHLIGHT. OPERATIONAL CHECK WAS GOO D. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAABB08116 1 20080712 A 2910 LJ38085 DRAIN BOEING 757 7572B7 1384964 NM HYDRAULIC SYS CRACKED A USAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 19 942UW 27807 PHL FLT 723 EN-ROUTE DUB TO PHL. DURING DESCENT INTO PHL, THE LEFT HYDRAULIC SYSTEM QUANTITY DECREASED TO ZERO AND THE SYSTEM PRESSURE LIGHT ILLUMINATED. ALSO, EICAS MESSAGE "G L HYD SYS PRESS" DISPLAYED. THE FLIGHT LANDED SAFELY AND WAS ABLE TO TAXI OFF THE RUNWAY, BUT WAS TOWED TO THE GATE. MAINTENANCE REPLACED A HYDRAULIC DRAIN TUBE. SYSTEM OPERATION ALLY AND LEAK CHECKS OK. (B) 2 L 7 2 4F RT A2NM 20080811 NM 2008 8 11 USAA920081369 1 20080702 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT-Q3 CHECK MAJOR REPAIR NR 03C10753007/013- FRAME CRACKED AT RADIUS OF CUTOUT BS380, S16R. REPAIRED FRAME AT RADIUS O F CUTOUT BS380, S16R IAW B737 SRM 53-00-07. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081368 1 20080701 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT-Q3 CHECK MAJOR REPAIR NR 03C10753041/001- FRAME 500A CRACKED BETWEEN S8R TO S9R. REPAIRED FRAME AT 500A BETWEEN S8R TO S9R IAW US AIRWAYS TYPICAL REPAIR 53-10-20. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081297 1 20080707 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 457UW 25021 CLT-FORWARD PRESSURE BULKHEAD MAJOR REPAIR 03-0553-8-0105/03- CRACK IN BS 178 FORWARD PRESSURE BULKHEAD WEB, WL 218, LBL 11. REPAIRED BS 178 FORWARD PRESSURE BULKHEAD WEB, WL 218, LBL 11 IAW B737 SRM 53-10-08 (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081294 1 20080708 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 23704 CLT RON MAJOR REPAIR LOG 4390633- FUSELAGE SKIN CRACKED AT BS 727E, S-24R. REPAIRED FUSELAGE SKIN AT BS727E, S-24R IAW B737 SRM 53-00-01 AND US AIRWAYS TYPICAL REPAIR 53-33. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081350 1 20080629 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT- MAJOR Q3 CHECK NR 03C10753007/006, LEVEL 2 CORROSION ON "Z" ANGLE, BS 328 ON THE FORWARD ENTRY DOOR THRESHOLD. REP LACED "Z" ANGLE, BS 328 ON THE FORWARD ENTRY DOOR THRESHOLD IAW B737 SRM 51-10-02 AND 51-40-02. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081363 1 20080714 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 PHX- B-CHECK MAJOR REPAIR TASKCARD 18M05026- FUSELAGE SKIN CRACKED AT BS727D TO 727E, S22R TO S23R. REPAIRED FUSELAGE S KIN AT BS727D TO 727E, S22R TO S23R IAW B737 SRM 53-00-01 REPAIR 31. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081360 1 20080604 A 5330 6552988 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN- C21 MAJOR REPAIR LOG PAGE 4018251- AFT LEFT HAND FUSELAGE CRACKED AT BS920,S23L,WL178. REPAIRED AFT LEFT HAND FUSE LAGE AT BS920, S23L, WL178 IAW US AIRWAYS EA 130054. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081370 1 20080702 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT- Q3 CHECK MAJOR REPAIR NR 03C10753038/002- FRAME INNER CHORD AT BOTTOM FASTENER LEFT HAND SIDE CRACKED AT BS616, S17 L. REPAIRED FRAME INNER CHORD AT BOTTOM FASTENER LEFT HAND SIDE AT BS616, S17L IAW US AIRWAYS TYPICAL REPAIR 53-62-01. ( B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081352 1 20080703 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT- MAJOR Q3 CHECK NR 03C10753060/011, LEVEL 2 CORROSION ON "Z" ANGLE, BS328, WL208.1. REPLACED "Z" ANGLE, BS328, WL20 8.1 IAW B737 SRM 53-60-15. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081348 1 20080703 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT- MAJOR REPAIR Q3 CHECK NR 03C10853029/018, LEVEL 2 CORROSION ON INTERCOSTAL, BS 967-986, RBL 16. REPLACED INTERCOST AL, BS 967-986, RBL 16 IAW B737 SRM 51-10-02. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081333 1 20080709 A 5310 652072354 DOOR FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 530AU 24412 PIT- RON MAJOR REPAIR LOG PAGE NR 4353032- WHILE ACCOMPLISHING THE REPETITIVE INSPECTIVE OF FORWARD CARGO DOOR OPENING, TWO CRACKS WERE FOUND AT S24R BS 492.4 REF US AIRWAYS EA 111238. REPAIRED FORWARD CARGO DOOR OPENING AT S24R BS 492.4 I AW US AIRWAYS EA 111238. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081335 1 20080616 A 5311 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN- C21 MAJOR REPAIR NR 6112049- FRAME CRACKED AT BS 480, S9R, WL216. REPAIRED FRAME AT BS480, S9R, WL216 IAW AWA TASK CARD M1C53002. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAASB08049 1 20080714 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 435US 24557 PHL MAINTENANCE REPORTED THE AFT LEFTHAND GALLEY EMERGENCY EXIT LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE ASSOCIATED BATTERY PACK PER MM 33-51-2-962-015. OPERATIONAL TEST GOOD. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081340 1 20080710 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT- MAJOR REPAIR Q3 CHECK NR 03C10763060/021, CRACKED INTERCOSTAL, BS 344, BL0. REPAIRED INTERCOSTAL, BS 344, BL0 IAW B737 SRM 51-70-11. (B) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 AALA200801509 1 20080604 A 3350 LIGHT BOEING 757 757223 1384957 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AM 24594 DFW EXTERNAL EMERGENCY LIGHT AT AFT LT OVERWING INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT AFT LT OVERW ING. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 NM 2008 8 12 AALA200801517 1 20080604 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 762AN 31479 DFW - EMERGENCY LIGHTS AT SEAT 26G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AAL200801519 1 20080604 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 762AN 31479 DFW - EMERGENCY LIGHTS AT SEAT 22G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801529 1 20080604 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 608AA 27446 LAX - EMERGENCY LIGHT AT OVERHEAD BULLNOSE BETWEEN SEATS 3AB AND 4AB INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY L IGHT AT OVERHEAD BULLNOSE BETWEEN SEATS 3AB AND 4AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 WP 2008 8 12 AALA200801530 1 20080605 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 218AA 49168 LGA - EMERGENCY LIGHT AT SEAT ROWS 21 AFT INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 20 FOR EMERGENCY LIGHT AT SEAT ROWS 21 AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801536 1 20080605 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 797AN 30012 DFW - EMERGENCY LIGHT AT OVERHEAD LT NR THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD LT NR THR EE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801538 1 20080605 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 797AN 30012 DFW - EMERGENCY LIGHT AT SEAT 22G MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801539 1 20080605 A 3397 WIRE BOEING 777 777223 1385213 NM CABIN EXPOSED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 797AN 30012 DFW - EMERGENCY LIGHT WIRING AT SEAT 24D EXPOSED. SECURED WIRING FOR EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHECKE D NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801540 1 20080606 A 3350 B21506 FUSE BOEING 777 777223 1385213 NM BATTERY PACK INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 793AN 30255 JFK - EMERGENCY LIGHTS AT SEAT ROWS 20 TO 26 INOPERATIVE. REPLACED BATTERY PACK FUSE FOR EMERGENCY LIGHTS AT SEAT ROWS 20 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 SO 2008 8 12 RAIA00807016A 1 20080722 A 5210 SEAL EMB 145 EMB145LR 3260212 SO CABIN DOOR DRY A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 822HK 145069 POST FLT 5548-STL MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE LUBED THE DOOR SEAL. (S) 2 L 7 2 4T RT T00011AT 20080808 EU 2008 8 8 08FDEA02608 1 20080701 A 5313 A53974203204 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION AT STRINGER P 44, C 70-71 LT OUT OF LIMIT STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02611 1 20080701 A 5313 A53778409208 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION AT STRINGER P 44, C 38.2-39 RT OUT OF LIMIT, STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 M7K2008F00108 1 20080303 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE DEFECTIVE E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 810MH 128 3949 23209 PILOT REPORTED THAT WHEN ADJUSTING POWER FOR CRUISE FLIGHT THE ENGINE HAD FLUCTUATIONS WHEN PASSING THROUGH A CERTAIN CO LLECTIVE POSITION THAT WERE REPEATABLE IF SELECTING THE POSITION IN QUESTION. UPON SHUTDOWN A FAULT CODE WAS GENERATED INDICATING THE COLLECTIVE POTENTIOMETER WAS FAULTY. A NEW POTENTIOMETER WAS INSTALLED AND NO FURTHER DEFECT NOTED. THIS IS A VERY COMMON FAULT FOR THIS PART THAT EFFECTS THIS MODEL AIRCRAFTS DISPATCH RELIABILITY. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 WP 2008 8 11 DHL2008F00030 1 20080723 A 7920 D81P5410115 LINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE OIL PRESS XMITER CRACKED A DHLA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 05 873SJ 46091 NR 2 ENGINE LOSS OIL QUANTITY AND PRESSURE SHUT ENGINE DOWN WITH OIL PRESSURE 13 PSI RESOLUTION. FOUND OIL LINE PN D81P 54101 FROM PRESSURE TRANSMITTER CRACKED. REPLACED LINE IAW MM 71-00-01 LK AND OPS CK GOOD. (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 20080811 WP 2008 8 11 ABX2008F00001 1 20080719 A 5610 ROD DOUG DC9 DC941 302207N WP COCKPIT WINDOW DETACHED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 F/O WINDOW WOULD NOT OPEN. FOUND LOWER AFT LINKAGE ROD NOT ATTACHED AT THE AFT LOCK BAR. SECURED ROD (ATTACHED) TO AFT LOCK BAR IAW AMM CHAPTER 56. (K) 2 L 7 2 4F A6WE 20080811 NE 2008 8 11 M7K2008F00124 2 20080414 A 7412 EXCITER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE IGNITION SYS FAILED E M7KA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 19 824MH 752 4173 23350 DURING ATTEMPTED START IGNITERS FAILED TO ACTIVATE. INVESTIGATION REVEALED CIRCUIT BREAKER HAD POPPED. RESETTING THE B REAKER FOR A GROUND TEST REVEALED AN UNEVEN IGNITER RHYTHM NO NORMALLY FOUND WITH THIS IGNITION SYSTEM, IGNITER BOX WAS CHANGED AS A PRECAUTION. THIS PART HAS BEEN DEEMED NON REPAIRABLE BY THE ENGINE MFG, AS NO SECOND BOX IS EMBODIED REPLA CEMENT OF ANY SUSPECT BOX IS PRUDENT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00092 1 20080324 A 6210 350A21491800 TUNING UNIT UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE BLADE CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 848MH 902 4290 23336 ROUTINE 100 HOUR INSPECTION REVEALED THAT HAMMER BLADE HAD CRACKED. AS THIS BLADE IS NORMALLY UNDER A 1200 FLEX PER MIN UTE OPERATION IT IS EXPECTED TO WORK HARDEN OR FATIGUE OVER TIME. SUSPECT A METAL DEFECT OF SOME NATURE AS MOST OF THES E BLADES LAST MUCH LONGER IN SERVICE. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00099 1 20080414 A 5340 350A54112420 BRACKET UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE CRACKED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 808MH 3914 23072 BRACKET FOUND CRACKED DURING 100 HOUR INSPECTION. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 NM 2008 8 11 MWE2008F00027 1 20080802 A 2611 V73168 SMOKE DETECTOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D* NE LAVATORY INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 701ME 49760 RT LAVATORY SMOKE DETECTOR SYSTEM IS INOPERATIVE WHEN TEST SWITCH WAS ACTIVATED. AFTER RESETTING RELEVANT CIRCUIT BREAK ER ONE TIME IN COCKPIT AND ACTIVATING TEST SWITCH AGAIN, ALL INDICATIONS ARE NORMAL. SMOKE DETECTOR SYSTEM IN RT LAVATO RY IS FULLY OPERATIONAL. (K) 2 L 7 2 4F 4 F RT A6WE E2EA 20080811 EA 2008 8 11 TRAX200800677 1 20080521 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 680BR 7679 FLAPS FAIL AT ZERO WHEN SELECTING 8 DEGREES. FLT 4349 CX EMERGENCY DECLARED. REMOVED AND REPLACED BPSU LT SIDE IAW CRJ 200 AMM 27-50-01. OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME. [SDR CLOSED](B) 2 L 7 2 4F RT A21EA 20080811 SO 2008 8 11 XGN2008F00011 2 20080723 A 8530 CYLINDER CESSNA 402 402B 207590P CE CONT O520 TSIO520* 17040 SO ENGINE CRACKED E XGNA O OTHER O OTHER NR NOT REPORTED 1 SW 05 3378Q 532 402B0334 CRACKED BETWEEN FIN NR 1 AND FIN NR 3 AFT OF THE INJECTOR. MFG REV 3 E SERIES CYLINDER. ALL DEFECTIVE! (K) 1 L 7 2 3O 3 O A7CE E8CE 20080811 NM 2008 8 11 UIEA200800266 1 20080718 A 2612 285U00721 CIRCUIT CARD BOEING 747 74747UF 1384812 NM FIRE WARNING FAILED A UIEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 EA 15 415MC 32837 MASTER CAUTION/ FIRE WARNING BELL ON GROUND. NO EICAS MESSAGE (NO OTHER LIGHTS OR WARNINGS). REPLACED A15 CARD AT THE M5206 MODULE. OPS CHECKED OK. (S) 2 L 7 4 4F RT A20WE 20080811 NM 2008 8 11 AALA200801695 1 20080624 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 788AN 30011 DFW - EMERGENCY LIGHT AT OVERHEAD ACROSS FROM RT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OV ERHEAD ACROSS FROM RT NR THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080811 NM 2008 8 11 AALA200801523 1 20080604 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 762AN 31479 DFW - EMERGENCY LIGHTS AT SEAT 24C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080811 NM 2008 8 11 AALA200801786 1 20080707 A 3397 CONNECTOR BOEING 757 757223 1384957 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 184AN 29594 SFO - EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKE D NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 NM 2008 8 11 GTIA0800076 1 20080712 A 3240 SELECTOR VALVE AIRBUS A319 A319132 3930340 NM MLG BRAKES MALFUNCTIONED A GTIA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 23 501NK 2424 LOSS OF NORMAL BRAKING WITH ECAM: BRAKE-NORMAL BRAKE FAULT. T/S SYS WITH NFF. ECAM: BRAKES NORMAL FAULT ON NEXT LEG. B RAKE SELECTOR VALVE CHANGED AS PRECAUTIONARY. (S) 2 L 7 2 4F RT A28NM 20080811 CE 2008 8 11 DXTA200803163 1 20080706 A 2120 UNKNOWN CESSNA 750 750 2076810 CE CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 907QS 7500201 PASSENGER NOTICED OILY ODOR IN CABIN. (A) 2 L 7 2 4J RT T00007WI 20080811 NM 2008 8 11 AALA200801766 1 20080703 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 SFO - EMERGENCY EXIT SIGN LIGHT AT LEFT NR TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT LEFT NR TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080811 WP 2008 8 11 AALA200801755 1 20080702 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 486AA 49679 LGA - EMERGENCY LIGHT AT SEAT 7D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORM AL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 EA 2008 8 11 A6WA200840524 1 20080612 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 444ZW 7788 FUNCTIONAL TEST OF CREW ESCAPE HATCH FAIL CORROSION FOUND ON OUTER HANDLE SHAFT. OUTER HANDLE REPLACED. (A) 2 L 7 2 4F RT A21EA 20080811 2008 8 11 USAABB08115 4 20080706 A 2565 D30656126 SLIDE BOEING 757 7572G7 1384963 NM L4 DOOR LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 909AW 24522 PHX- THE L4 DOOR EMERGENCY ESCAPE SLIDE PRESSURE WAS FOUND LOW. MAINTENANCE REPLACED THE L4 DOOR EMERGENCY ESCAPE SLIDE . OK FOR SERVICE. (B) 2 L 7 2 4F RT A2NM 20080811 NM 2008 8 11 USAA920081373 1 20080712 A 2560 P4010021 BATTERY PACK BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 308AW 24710 LOG 4299216 PHX FLT NR 199- FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOP. MX REPLACED FLASHLIGHT BATTERY PACK. O PERATIONAL CHECK WAS GOOD. (B) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 AALA200801528 1 20080604 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 762AN 31479 DFW - EMERGENCY LIGHT AT LT NR ONE DOOR CLOSET AREA DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LT NR ONE D OOR CLOSET AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 WP 2008 8 12 AALA200801531 1 20080605 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 218AA 49168 LGA - EMERGENCY FLASHLIGHT AT AFT ENTRY DOOR HAS BROKEN BAND. REPLACED STRAP FOR EMERGENCY LIGHT AT AFT ENTRY DOOR. SY STEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NE 2008 8 12 AALA200801541 2 20080606 A 7250 TURBINE BLADES DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE FAILED A AALA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 589AA 53252 709987 DFW INFLIGHT T1853/06JUN. CREW REPORTED LOUD NOISE FOLLOWED BY ENGINE GAS TEMPERTURE GOING TO 800 DEGREES. NR ONE ENGI NE WAS SHUTDOWN BY CREW. LANDED DFW WITHOUT INCIDENT. SINGLE ENGINE TIME SIX MINUTES. FOUND TURBINE BLADE FAILURE AND METAL IN TAIL PIPE. REPLACED NUMBER ONE ENGINE ON 07JUN AT DFW. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F 4 F RT A6WE E9NE 20080812 WP 2008 8 12 AALA200801542 1 20080606 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 405A 49316 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROW 28 TO 31 INOPERATIVE. CLEANED CORROSION ON BATTERY PACK AT SEAT ROW 28. SY STEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801642 1 20080617 A 3350 0201984002 LENS BOEING 767 767323 1385205 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AN 25446 JFK - EMERGENCY LIGHT AT RT MID GALLEY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080812 NM 2008 8 12 AALA200801643 1 20080617 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 342AN 33081 MIA - EMERGENCY LIGHT AT SEAT ROW 20B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT MID GALLEY. SYSTEM GROUND C HECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080812 WP 2008 8 12 AALA200801601 1 20080613 A 8012 9794104 START VALVE DOUG DC9 DC983 3022083 WP NR 1 ENGINE MALFUNCTIONED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 562AA 49344 DFW INFLIGHT T1106/13JUN. NR ONE ENGINE START VALVE OPENED IN FLIGHT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. RE PLACED NR ONE ENGINE START VALVE AND FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A6WE 20080812 NM 2008 8 12 AALA200801604 1 20080613 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 630AA 24588 JFK - EMERGENCY LIGHT AT MID LAVATORY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT MID LAVATORY. SYSTEM GROUND CH ECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 NM 2008 8 12 AALA200801607 1 20080613 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 780AN 29956 DFW - EMERGENCY LIGHT AT SEAT 40C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 40C. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801673 1 20080620 A 2740 ACTUATOR BOEING 737 737823 13844BZ NM STABILIZER TRIM FAILED A AALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SW 21 908AN 29501 IAD INFLIGHT T1572/20JUN. CREW REPORTED STABILIZER TRIM INDICATION FOLLOWED BY LOSS OF STABILIZER TRIM. LANDED IAD WIT HOUT INCIDENT. REPLACED STABILIZER TRIM ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A16WE 20080814 WP 2008 8 14 UPS08852663 1 20080611 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 270 L21L GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, MCD CUT OUT HAS WEB REPAIR GOUGED STA 270 ABOVE L21L (AFT LWR CORNER O F DOOR CUT-OUT). REMOVED, FA BRICATED, AND INSTALLED REPLACEMENT WEB FILLER IAW SRM 5 1-01-21 AND 51-01-04. 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 UPS08852786 1 20080712 A 5540 FITTING DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, RUDDER HINGE CUTOUT NR 2 FROM BOTTOM DAMPER ATTACH FITTING CRACKED. REMOVED AND REPLACED FITTINGS I AW SRM, 51-1-21, 51-1-8, 51=3-2. 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 UPS08852733 1 20080529 A 5340 5773844 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FS 1771 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-C2 POSSIBLE CRACK IN RADIUS OF INTERCOSTAL ATTACH ANGLE, AT BOTTOM J-BEAM, AFT SIDE OF APB, 60 COMPT RT BS 1771. REMOVED INTERCOSTAL ATTACH ANGLE, FABRICATED AND INSTALLED REPLACEMENT ANGLE. IAW DWG 5773844 AND SRM 51-1-2 1,51-3-00 AND 51-1-20D. 2 L 7 4 4F RT 4A25 20080814 NM 2008 8 14 USAA920081426 1 20080726 A 5754 114N4002156A SKIN BOEING 757 7572B7 1384964 NM L/E SLAT DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 930UW 27145 CLT - IRAN - MAJOR REPAIR - NR 10 SLAT HAS DISBONDING AT INBOARD AFT CORNER OF THE UPPER SKIN. REPAIRED NR 10 SLAT AT I NBOARD AFT CORNER OF THE UPPER SKIN IAW US AIRWAYS EA NR100580. (S) 2 L 7 2 4F RT A2NM 20080814 SO 2008 8 14 C2XA08CL090 1 20080727 A 3350 1317 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13118 145675 DURING ROUTINE MAINTENANCE THE OVERHEAD EMERGENCY LIGHT AT ROW 7A WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND RELA MPED THE OVERHEAD LIGHT AT SEAT 7A. OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4F RT 20080814 SO 2008 8 14 C2XA08CL091 1 20080727 A 3350 276005 FUSE EMB 145 EMB145LR 3260212 SO POWER SUPPLY INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26545 84584 145558 DURING ROUTINE MAINTENANCE BOTH AFT OVERHEAD EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACE D THE FUSE AT THE NR 4 EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4T RT T00011AT 20080814 EU 2008 8 14 08FDEA03048 1 20080724 A 5347 A53610798202 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 455FE 331 MAIN DECK COURIER COMPT TRACK AT FLOOR LEVEL BETWEEN FR 16A-FR 19, Y1560 WITH EXFOLIATION CORROSION. REPLACED THE SEAT TRACK PER DWG A53610 798202 & SRM 51-40-21. RESTORED FINISH PER SRM 51-75-10. 2 L 7 2 4F RT A35EU 20080814 CE 2008 8 14 7302008N401CS 1 20080725 A 2731 S37792H38214 CONTROL CABLE CESSNA 525 525 2076601 CE ELEVATOR TRIM CHAFED E Z5FA K NONE O OTHER NR NOT REPORTED 1 EA 63 401CS 2866 525B0030 ELEVATOR TRIM CABLE CHAFED ON PULLEY BRACKET P/N 6361201-1 IN VERTICAL STABILIZER. ENGINEERING ORDER WRITTEN TO ADD FAI RLEADS TO PREVENT FURTHER CHAFING. (S) 1 L 7 2 4F RT A1WI 20080814 EU 2008 8 14 MAL2008F00016 1 20080723 A 5753 SKIN SAAB SF340 340B 7860101 EU T/E FLAP DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 DURING INSTALLATION OF RT FLAP DAMAGE OCCURRED TO THE LEADING EDGE AT WS 174.3. DAMAGE WAS REPAIRED IAW EO57204 AND EO5 7060. (S) 2 L 7 2 4T RT A52EU 20080814 EU 2008 8 14 MAL2008F00017 1 20080723 A 5753 SKIN PANEL SAAB SF340 340B 7860101 EU T/E FLAP DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 THREE DENTS WERE FOUND ON RT FLAP UPPER SKIN PANEL 641AT FROM WS 94.5 TO WS 99. DENTS WERE REPAIRED IAW EOS57201. (S) 2 L 7 2 4T RT A52EU 20080814 EU 2008 8 14 MAL2008F00018 1 20080725 A 2150 MOTOR SAAB SF340 340B 7860101 EU CABIN MALFUNCTIONED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 416XJ 340B416 F/A REPORTS STRONG ODOR IN CABIN AGAIN. SMELLS LIKE AN ELECTRICAL SMELL. NOTED STRONG ELECTRICAL SMELL COMING FROM BUR NT UP SUPP AIR MOTOR. SYSTEM ON MEL (INOP). RAN ACFT SYSTEMS. NO FURTHER ELECTRICAL SMELL. (S) 2 L 7 2 4T RT A52EU 20080814 WP 2008 8 14 IXX2008F00034 1 20080609 A 5753 SKIN DOUG DC8 DC872F 302199E WP T/E FLAP DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND NICKS RT WING OUTBOARD FLAP UPPER SKIN AT STATION XF 345.000. REMOVED FASTENER S AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XF 345.000-360.000 IAW DC8 SRM 57-7-1 FIGURE 4 TR 57-94 DATE D 10-01-2002, DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-3-0, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 EA 2008 8 14 TRAX200800937 1 20080728 A 5230 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 926EV 7843 CARGO DOOR FWD, LOWER "C" CHANNEL IS CRACKED. REMOVED AND REPLACED CHANNEL IAW SRM 51-42-06. (S) 2 L 7 2 4F RT A21EA 20080814 EA 2008 8 14 TRAX200800948 1 20080730 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 926EV 7843 RT WING LOWER PLANK ACCESS HOLE 650BB HAS CORROSION AROUND ENTIRE LANDING IN CRITICAL AND NON-CRITICAL AREAS. FAILED ND T INSPECTION 60% FULL SCREEN HEIGHT. REPAIRED RT WING LOWER PLANK ACCESS HOLE NR10 650BB IAW REO 601R-57-21-030. COMP LIED WITH EC/TC EO 600-57-81. COMPLIED CONTACTED STRUCTURE ENGINEERING AND PROVIDED ALL FORMS. RII COMPLIED WITH. (S) 2 L 7 2 4F RT A21EA 20080814 EA 2008 8 14 TRAX200800950 1 20080731 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 723EV 10132 LT FUSELAGE MIDDLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LT FUSELAGE MIDDLE EMERGENCY LIGHT BULB. OPS CHEC K GOOD. (S) 2 L 7 2 4F RT A21EA 20080814 EA 2008 8 14 TRAX200800951 1 20080731 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 730EV 10141 CAPTAIN EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW CRJ 700 AMM 25-61-00. (S) 2 L 7 2 4F RT A21EA 20080814 NM 2008 8 14 WRLA2008065 1 20080802 A 5313 1D0554T LONGERON DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 275WA 48631 DURING "C" CHECK INSPECTION IN TPE, FOUND CENTER CARGO LONGERON 49R CORROSION AT STA Y=1707. REPAIRED THE CTR CARGO LON GERON 49R AT STA Y -1707 PER MD-11 SRM 53-10-00 REV. 40. CONDITION CHECK NORMAL AND JOB COMPLETED. (S) 2 L 7 3 4F 4 F RT A22WE E24NE 20080814 NM 2008 8 14 F3LA200800540 1 20080728 A 2560 D5348015800600 PLATE AIRBUS A319 A319111 3930336 NM GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2 2209 DURING C3 C-CHECK, INSPECTION NOTED THE L2 FORWARD GIRT BAR BLANKING PLATE HAD CORROSION. MAINTENANCE REMOVED AND REPLA CED CORRODED L2 DOOR FORWARD GIRT BAR FITTING BLANKING PLATE IAW THE REQUIREMENTS OF AMM 52-13-31-400-007. UPON COMPLET ION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080814 CE 2008 8 14 DJF2008F00011 1 20080706 A 2131 45AS630013 CONTROLLER BEECH MU300 400A 1155402 CE CABIN PRESSURE FAILED A DJFA G O2 MASK DEPLOYED O OTHER NR NOT REPORTED 1 EA 23 794TA RK282 TEMPORARILY LOST PRESSURIZATION AT FL300. OXYGEN MASKS DROPPED. EMERGENCY WAS DECLARED. ACFT LANDED SAFELY. THE PRES SURIZATION CONTROLLER WAS REPLACED. OPS CHECKS WERE GOOD AND THE ACFT WAS RETURNED TO SERVICE. (S) 2 H 7 2 4F RT A16SW 20080814 SO 2008 8 14 RAIA00807019 1 20080728 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAC DOOR OUT OF ADJUST A RAIA K NONE O OTHER NR NOT REPORTED 1 CE 03 831HK 145232 FLT 7916-STL - PASSENGER DOOR DIFFICULT TO OPEN. LAST 3" INCHES OF HANDLE TRAVEL DIFFICULT. MAINTENANCE PERFORMED AN A DJUSTMENT OF THE MAIN DOOR ROLLER. OPERATIONAL CHECK OF THE DOOR WAS GOOD. (S) 2 L 7 2 4T RT T00011AT 20080814 SO 2008 8 14 RAIA00807021 1 20080729 A 2150 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A RAIA O OTHER N FALSE WARNING CL CLIMB 1 CE 03 850HK 145003 FLT 7905-IAD-LEFT PACK OVERLOAD MESSAGE ON THE EICAS DURING CLIMB. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE SY STEM WITH NO DEFECTS NOTED. (S) 2 L 7 2 4T RT T00011AT 20080814 WP 2008 8 14 ABXA080213 1 20080728 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP COCKPIT DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 958AX 47760 EMERGENCY OVERHEAD LIGHTS IN COCKPIT WOULD NOT ILLUMINATE DURING TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-02-4. (S) 2 L 7 2 4F A6WE 20080814 NM 2008 8 14 KCSA081372 1 20080805 A 5330 FASTENER BOEING 747 747122 1384872 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STA 1700 TO STA 1740 AT STR 34R SKIN HAS NUMEROUS FASTENERS WITH HEADS PULLING. (S) 2 L 7 4 4F RT A20WE 20080814 NM 2008 8 14 KCSA081352 1 20080727 A 5320 DOUBLER BOEING 747 747246B 1384864 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 STA 400 STR 43R TO 45R NWW RT AFT. CUTOUT DOUBLER HAS A CRACK ON DOUBLER INSIDE RADIUS. (A) (S) 2 L 7 4 4F RT A20WE 20080814 NM 2008 8 14 KCSA081322 1 20080715 A 3350 LIGHT BOEING 747 747246F 1384850 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 705CK 21034 LT UPPER DECK ESCAPE DOOR AFT EMERGENCY LIGHT INOPERATIVE. (A) 2 L 7 4 4F RT A20WE 20080814 NM 2008 8 14 KCSA081353 1 20080727 A 5347 SEAT TRACK BOEING 747 747246B 1384864 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 SEAT TRACK UNDERSIDE AT STA 1220 RBL 10 HAS CORROSION ON INBOARD SIDE. (A) (S) 2 L 7 4 4F RT A20WE 20080814 NM 2008 8 14 USAA920081482 1 20080729 A 5315 D53472094008 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803AW 0931 SAL-C7- MAJOR REPAIR - CORROSION ON FLOOR BEAM AT FR 66, Y512. REPLACED FLOORBEAM AT FR66, Y512 IAW A318 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 USAA920081411 1 20080721 A 5512 65C27494 SKIN BOEING 737 7374B7 1384702 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 451UW 24934 CLT-C1- MAJOR REPAIR - CRACK 2 INCHES FORWARD OF REAR SPAR ON LT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 115. REPA IRED HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 115 IAW B737 SRM 55-10-01 AND TYPICAL REPAIR 55-10-07 REV C. (S) 2 L 7 2 4F RT A16WE 20080814 NM 2008 8 14 USAABB08121 1 20080721 A 3610 312N53061 DUCT BOEING 757 7572B7 1384964 NM RT ENGINE LEAKING A USAA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 19 937UW 27245 LAS FLT 790 LAS-CLT - RT ENG OVERHEAT WARNING ON TAKEOFF IN FLT SHUTDOWN, 30 MINUTES SINGLE ENG TIME. MAINTENANCE REPLA CED A LEAKING RT ENG HP2 DUCT. LEAK AND OPERATIONALLY CHECKS OK. (S) 2 L 7 2 4F RT A2NM 20080814 NM 2008 8 14 USAA920081463 1 20080721 A 5540 D5537131800000 HINGE FITTING AIRBUS A319 A319132 3930340 NM RUDDER EXCESS PLAY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803AW 0931 SAL-CY- MAJOR REPAIR - EXCESSIVE PLAY ON NR 1 HINGE OF RUDDER AT RIB 2 VERTICAL STABILIZER STA 760. REPLACED FITTING AS SEMBLY AT RIB 2 VERTICAL STABILIZER STA 760 IAW A319 AMM 55-36-41. (S) 2 L 7 2 4F RT A28NM 20080814 2008 8 14 USAABA08028 4 20080803 A 3441 46502003030316 ADIRU AIRBUS 330 A330323 3930335 EU NR 1 INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 276AY 11075 3017 0375 LGW FLT 705 FRA TO CLT - THE FLIGHT RECEIVED ECAM MESSAGES "ADR 1 FAULT" AND "IR 1 FAULT" PRIOR TO ENTERING THE ETOPS SE GMENT OF FLIGHT. THE FLIGHT COULD NOT CONTINUE ETOPS, PER PROCEDURES, WITHOUT IR 1. THE FLIGHT DIVERTED TO LGW AND LAN DED WITHOUT FURTHER INCIDENT. MAINTENANCE IN LGW SWAPPED THE NR 1 AND NR 2 ADIRUS, AND DEFERRED THE NR 2 ADIRU ON MEL. MAINTENANCE IN CLT REPLACED THE NR 2 ADIRU. OPERATIONALLY CHECKS OK. (S) 2 L 7 2 4F RT A46NM 20080814 NM 2008 8 14 USAA920081464 1 20080722 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803AW 0931 SAL-C7- MAJOR REPAIR - BEAM RAIL CORRODED AT FR66, Y1292. REPLACED BEAM RAIL AT FR66, Y1292 IAW A319 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 USAA920081476 1 20080803 A 5320 STIFFENER BOEING 737 737401 1384701 NM MLG WW CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 452US 23992 CLT-C2 -MAJOR REPAIR- VERTICAL Z-ANGLE STIFFENER CRACKED ACROSS WEB AND FLANGE IN MAIN WHEEL WELL AT BS 663 RBL 6.15 JUS T FORWARD OF B-HYDRAULIC PUMP. REPAIRED VERTICAL Z-ANGLE STIFFENER AT BS 663 RBL 6.15 IAW US AIRWAYS TYPICAL REPAIR 57- 10-03B. (S) 2 L 7 2 4F RT A16WE 20080814 NE 2008 8 14 USAA920081492 2 20080805 A 7532 5950041108 BLEED VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING M OVER TEMP TO TAKEOFF 1 EA 19 665AW 19978 19791 1644 FLT 569 PHX-MCO -AIR TURNBACK- CAPTAIN RECEIVED NR2 ENG SYSTEM FAULT ON TAKEOFF AND EXCEEDED EGT LIMITS REACHING 641 DEG REES. THE ENG THRUST WAS SUBSEQUENTLY REDUCED BUT CREW WAS UNABLE TO INCREASE THRUST TO CLIMB OR CRUISE WITHOUT EXCEEDI NG EGT LIMITS. THE ACFT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HPT/LPT ACTI VE CLEARANCE CONTROL VALVE ACTUATOR, 10TH STAGE BLEED VALVE AND VARIABLE STATOR VANE ACTUATOR. VENDOR TEARDOWN REPORT I NDICATES THE 10TH STAGE BLEED VALVE WAS A CONFIRMED FAILURE. TEARDOWN FOR THE HPT/LPT ACC VALVE ACTUATOR ALSO INDICATED LEAKAGE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080814 NM 2008 8 14 USAA920081480 1 20080808 A 5330 6518420 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 453UW 24980 CLT-RON -MAJOR REPAIR- FUSELAGE CRACKED AT UPPER OTBOARD CORNER OF PILOT`S WINDSHIELD BS 203.8, S2L. REPAIRED FUSELAGE AT UPPER OUTBOARD CORNER OF PILOT`S WINDSHIELD BS 203.8, S2L IAW B737 SRM 53-10-01. (S) 2 L 7 2 4F RT A16WE 20080814 NM 2008 8 14 USAABB08122 1 20080719 A 2460 CIRCUIT BREAKER BOEING 757 7572B7 1384964 NM ELECTRICAL SYS MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 206UW 27808 FLL FLT 811 EN ROUTE PHL TO CUN. DURING CRUISE, RECEIVED A LT UTILITY BUS OFF MESSAGE. ATTEMPTS TO RESET WERE UNSUCCES SFUL. THE CREW DECIDED TO STOP IN FLL TO HAVE MAINTENANCE REPAIR THE ACFT. THE FLIGHT DIVERTED TO FLL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LFT DC BUSS, SECTION 1 CIRCUIT BREAKER. OPERATIONALLY CHECKED OK. (S) 2 L 7 2 4F RT A2NM 20080815 EU 2008 8 15 08FDEA03094 1 20080727 A 5210 A5211131100300 FITTING AIRBUS 310 A310222 3930315 EU PAX DOOR HINGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 455FE 331 MAIN DECK RT FWD PAX/CREW DOOR LOWER HINGE ARM/FITTING WITH EXFOLIATION CORROSION. REPLACED RT FWD PAX/CREW DOOR LOWE R CONNECTION LINK PER AMM 52-11-21/4.OPERATION TEST THE RT CREW DOOR PER AMM 52-11-21/4.TEST OK. 2 L 7 2 4F RT A35EU 20080815 NM 2008 8 15 08FDEA03050 1 20080724 A 3230 106122615 SENSOR BOEING 727 727233 138408A NM MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 271FE 22036 LANDING LEVER HANDLE FAILED TO MOVE PAST THE OFF POSITION. FOLLOWED QRH PROCEDURES AND IT FAILED TEST NR 1. REINSTAL LED GROUND SENSE LOWER LINK TO SCISSORS LT GEAR, PER SMP AND SAFETIED BOLT. REMOVED AND REPLACED AIR SAFETY SENSOR IAW M/M 32-09-221-4. PERFORMED ADJUSTMENT TEST PER M/M 32-09-2215, COMPLYING WITH EA 7-3210- 122383. "LANDING GEAR SENSIN G ALTERNATE TEST PROCEDURE". 2 L 7 3 4F RT A3WE 20080815 WP 2008 8 15 08FDEA02930 1 20080716 A 5753 ARC23703 SKIN DOUG MD10 MD1010F 3022112 WP LT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING INBD FLAP LOWER SKIN IS DENTED. CHECKED DENT AND FOUND TO BE OUT OF LIMITS IAW SRM 57-10-00; VOL I, FIG 48. REMOVED DAMAGE AND FABRICATED A REPAIR DOUBLER IAW SRM 57-10-00, VOL I, FIG 85. ALODINED AND PRIMED REPAIR DOUBLER IAW SRM 51-21-01, VOL II. INSTALLED THE REPAIR DOUBLER IAW SRM 57-10-00, VOL I, FIG 85. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 08FDEA02931 1 20080716 A 5753 ARC27361 SKIN DOUG MD10 MD1010F 3022112 WP LT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING INBD FLAP LOWER SURFACE HAS DENTS. CHECKED DENT AND FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00, VOL I, FIG 48. REMOVED DAMAGE AND FABRICATED A REPAIR DOUBLER IAW DC/MD-10 SRM 57-10-00, VOL I, FIG 85. ALODINED AND PRIME D REPAIR DOUBLER IAW DC/MD-10 SRM 51-21-01, VOL II. INSTALLED THE REPAIR DOUBLER IAW DC/MD-10 SRM 57-10-00, VOL I, FIG 85. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 08FDEA02933 1 20080716 A 5753 ARC2122502 SKIN DOUG MD10 MD1010F 3022112 WP RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 RIGHT WING OUTBD FLAP LOWER SURFACE, OUTBD EDGE AREA SKIN HAS 6 EA DENTS. CHECKED DENTS AND FOUND THEM TO BE OUT OF LIM ITS IN 2 PLACES FROM STA XOFH 773 - 778, IAW DC/MD-10 SRM 57-10-00, FIG 48, VOL I. CUT OUT DAMAGED AREAS. MATERIAL ID FOR THE DOUBLER IS 2024-T3, 0.050, PO 623403.1. FABRICATED DOUBLER IAW DC/MD-10 SRM 57-10-00, FIG 48, VOL I. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01, PGS 21 - 24, VOL II. INSTALLED IAW DC/MD-10 SRM 51-35-02, VOL II. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 08FDEA03041 1 20080723 A 5320 AFA016177 SUPPORT ANGLE DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 MID CARGO CEILING WEB PANEL IS CRACKED AT THE DOOR MOTOR AREA. REMOVED CEILING SUPPORT ANGLE AT FS 1741 - 1761, BL 95. FABRICATED NEW SUPPORT ANGLE IAW DAC DWG AFA 0161, REV AV. MATERIAL ID 2024-0, 0.040, PO 548001.2. HEAT TREAT ANGLE I AW TPS 1003, REV A. LOCATED AND DRILLED ANGLE IAW DAC DWG AFA 0161, REV AV. ALODINED AND PRIMED IAW DC/MD-10 SRM 51- 21-01, VOL III. INSTALLED SUPPORT ANGLE IAW DC/MD-10 SRM 51-31- 01, VOL II. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 08FDEA02938 1 20080716 A 5754 6916241 PANEL BOEING 727 727233 138408A NM NR 3 SLAT DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 NR 3 SLAT UNDERWING PANEL NR 6224 HAS AREA OF DELAMINATION REPAIRED PANEL 6224 REF SRM 51-40-9 STEPS 3D, 4E, 4F PG3-7 AN D AMM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080815 NM 2008 8 15 08FDEA02942 1 20080716 A 5713 65C2613912 STRINGER BOEING 727 727225 1384077 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 LT WING STATION 686.5 STRINGER S-10 S CRACKED REPAIRED STRINGER S-10, AT STA 686.5 WITH REPAIR KIT 65C26139-12 REF EO NR 7-5710-7-4322 PT 1, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080815 NM 2008 8 15 08FDEA02945 1 20080716 A 5512 6517491 PANEL BOEING 727 727233 138408A NM ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 UPPER TAIL PANEL NR 9607, INNER FOIL DISBONDED REPAIRED TEDLAR COVERING ON INNER SURFACE REF SRM 51-40-9 STEP 11 PG 18. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080815 EU 2008 8 15 08FDEA02991 1 20080721 A 5542 A55471500022 SKIN AIRBUS 300 A300B4622R 3930312 EU RUDDER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FLUID INGRESS ON RUDDER RT SIDE PANEL NEAR LOWER RIB Z-PROFILE. REPAIR PERFORMED IAW SRM 51-77-10, TD/K4/S1/24567/2008 ISS B AND RAS/DAHAM/4024567/2008 ISS A, APPROVED BY EA 6-5540-117180. 2 L 7 2 4F RT A35EU 20080815 WP 2008 8 15 08FDEA02946 1 20080716 A 5322 ADA011223 SHEAR TIE DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 FWD PIT, ATTACH ANGLE ON LONGERON 52 IS CORRODED, BL O AT STA 959. CUT OUT DAMAGED SECTION OF ATTACH ANGLE (SHEAR TIE). FABRICATED A NEW SHEAR TIE SECTION AND 2 SPLICES IAW DC/MD-10 SRM 53-30-00, VOL I, FIG 9 AND 10. ALODINED, PRIMED A ND PAINTED SHEAR TIE SECTION AND SPLICES IAW DC/MD-10 SRM 51-21-01, VOL II, PGS 21 - 24 AND SRM 51-21-02, PG 8, VOL II. INSTALLED THE NEW SHEAR TIE SECTION AND SPLICES IAW DC/MD-10 SRM 51-33-01, VOL II, PG 34 AND SRM 51-35-01, VOL II, PG 1 . 2 L 7 3 4F RT A22WE 20080815 EU 2008 8 15 08FDEA02965 1 20080717 A 5753 SKIN AIRBUS 310 A310222 3930315 EU ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 01038 318 RT WING, INBD FLAP TRAIL EDGE UPPER AND LOWER SURFACE DELAMINATED AT 15.0 INCH FROM INBD EDGE, MEASURING 5.0 BY 2.0 INCH REPAIRED THE DELAMINATED WEDGE PER EA NR 6-5720-117366. 2 L 7 2 4F RT A35EU 20080812 NM 2008 8 12 AALA200801678 1 20080620 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 363AA 24044 SFO - EMERGENCY LIGHT AT SEAT 20H TO 21H INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 20H TO 21H. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080812 EU 2008 8 12 AALA200801682 1 20080622 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80084 675 JFK - EMERGENCY LIGHTS AT SEAT 29C TO 37C AND LT NR FOUR DOOR DIM. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT 2 9C TO 37C AND LT NR FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080812 WP 2008 8 12 AALA200801685 1 20080622 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70529 49921 LGA - EMERGENCY LIGHT AT AFT TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT TRAIL COMPA RTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801636 1 20080616 A 3260 841602 PSEU BOEING 757 757223 1384957 NM LANDING GEAR FAILED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 604AA 27055 SJU INFLIGHT T1312/16JUN. CREW REPORTED GEAR INDICATION AFTER RETRACTION. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SENSOR ELECTRONICS UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 WP 2008 8 12 AALA200801637 1 20080616 A 3350 LIGHT DOUG DC9 DC982 3022082 WP EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7539A 49993 LGA - EXTERNAL EMERGENCY LIGHT AT RT AFT INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT RT AFT. SYSTEM GRO UND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 WP 2008 8 12 AALA200801639 1 20080617 A 2424 947F9453 GCU DOUG DC9 DC983 3022083 WP NR 2 ENGINE FAILED A AALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 21 9402W 53138 STL INFLIGHT T2361/17JUN ORD TO DFW. CREW REPORTED LOSS OF RT AC BUD POWER AND RT ENGINE DRIVEN GENERATOR WOULD NOT HOL D A LOAD. LANDED STL WITHOUT INCIDENT. REPLACED GENERATOR CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A6WE 20080812 NM 2008 8 12 AALA200801653 1 20080618 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 JFK - EMERGENCY LIGHTS AT SEAT ROWS 20 TO 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 20 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801659 1 20080618 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 673AN 29423 DFW - EMERGENCY LIGHT AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK AT STATION 400 FOR EMERGENCY LIGHT AT FIR ST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 WP 2008 8 12 AALA200801718 1 20080627 A 7931 DDK3818501 TUBE DOUG DC9 DC982 3022082 WP NR 1 ENGINE CRACKED A AALA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 21 585AA 53248 MCI INFLIGHT T358/27JUN PHX TO ORD. CREW REPORTED LOSS OF OIL AND PRESSURE ON NR ONE ENGINE. CREW SHUT DOWN ENGINE. L ANDED MCI WITHOUT INCIDENT. SINGLE ENGINE TIME APPROXIMATELY 20 MINUTES. FOUND CRACK IN OIL LOW PRESSURE SWITCH TUBE. REPLACED TUBE FOR OIL PRESSURE SWITCH ON NR ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801687 1 20080623 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 768AA 33540 DFW - EMERGENCY LIGHTS AT SEAT ROWS 20 TO 26 INOPERATIVE. REPLACED BATTERY PACK AT M33404 FOR EMERGENCY LIGHTS AT SEAT ROWS 20 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801615 1 20080613 A 3350 TRIM PANEL BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 636AM 24594 DFW - EMERGENCY LIGHT BULLNOSE TRIM AT SEAT ROW 16 LOOSE. SECURED BULLNOSE TRIM FOR EMERGENCY LIGHT AT SEAT ROW 16. SY STEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 WP 2008 8 12 AALA200801620 1 20080615 A 3350 SHROUD DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 454AA 49559 MSP - EMERGENCY LIGHT AT SEAT 30D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 30D. SYSTEM GROUND CH ECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 WP 2008 8 12 AALA200801621 1 20080615 A 3350 SHROUD DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 454AA 49559 MSP - EMERGENCY LIGHT AT SEAT 32D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 32D. SYSTEM GROUND CH ECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801626 1 20080615 A 3350 0219242005 LIGHT BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 338AA 22335 LAX - EMERGENCY LIGHT AT AFT CENTER FLIGHT ATTENDANT SEAT BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT AFT CE NTER FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080812 NM 2008 8 12 AALA200801629 1 20080615 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 26C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 WP 2008 8 12 AALA200801587 1 20080611 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 207AA 49158 LGA - EMERGENCY LIGHT AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD AFT GALLEY FOR EMERGENCY LIGHT AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801578 1 20080610 A 3350 8200037201ATS HOUSING BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 787AL 30010 DFW - EMERGENCY LIGHT WIRING AT LT NR THREE OVERHEAD SIGN EXPOSED. REPLACED HOUSING FOR EMERGENCY LIGHT AT LT NR THREE OVERHEAD SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801781 1 20080705 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 DFW - EMERGENCY LIGHT AT FIRST CLASS GALLEY CLOSET INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FIRST CLASS GALLEY CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801820 1 20080709 A 3397 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39365 24046 MIA - EMERGENCY LIGHTS AT MID GALLEY INOPERATIVE. SECURED CONNECTION FOR EMERGENCY LIGHTS AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080812 NM 2008 8 12 USAA920081402 1 20080722 A 2560 P4010021 BATTERY BOEING 737 73733A 1384673 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 166AW 23627 FLT 486 (PHX-DEN) - EMERGENCY EQUIP - AFT EMERGENCY FLASHLIGHT NOT WORKING. MAINTENANCE REMOVED AND REPLACED THE BATTER Y ON AFT EMERGENCY FLASHLIGHT. (A) 2 L 7 2 4F RT A16WE 20080812 EU 2008 8 12 USAA920081386 1 20080711 A 3350 Z040H0005110 DECODER AIRBUS A319 A319112 3930323 EU CABIN FAILED A USAA O OTHER L NO TEST IN INSP/MAINT 1 EA 19 725UW 1135 PIT-CII-EEL- EMERGENCY LIGHT BIT TEST FAILS. REPLACED FORWARD DECODER/ENCODER UNIT-B. (A) 2 L 7 2 4F RT A28NM 20080812 NM 2008 8 12 USAA920081388 1 20080715 A 5755 6546452 SKIN BOEING 737 737401 1384701 NM NR 9 SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 CLT-C2- MAJOR REPAIR - RT WING NR 9 SPOILER UPPER SURFACE DELAMINATED. REPLACED RT WING NR 9 SPOILER IAW B737 AMM 27-62 -91. (A) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 USAA920081391 1 20080718 A 3350 321454 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A USAA K NONE L NO TEST UK UNKNOWN 1 EA 19 819AW 40697 20830 1395 FLT 580 LAS-JFK - EEL - EMERGENCY EXIT LIGHTS INOP. BATTERY DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE RT AND LT BATTERY CHARGERS AND BATTERIES. OPERATIONAL CHECK WAS NORMAL. POWER SUPPLE/MFGR DIEHL / P/N 3214-54 / S/N 6067 / DISC HARGED / ZONE 200 FUSELAGE-TOP TIME 50454 / TOTAL CYCLES 20306 / TIME SINCE REPAIR 20830. POWER SUPPLY / MFGR DIEHL / P /N 3214-54 / S/N 6420/ DISCHARGED / ZONE 200 FUSELAGE-TOP TOTAL TIME 19531 / TOTAL CYCLES 8504 / TIME SINCE REPAIR 1443. (A) 2 L 7 2 4F RT A28NM 20080812 EU 2008 8 12 USAA920081405 1 20080720 A 2824 FRH28002 VALVE AIRBUS A321 A321211 3930370 EU FUEL SYSTEM FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 181UW 25822 2728 1531 FLT 1532 (SEA-PHL) - AIR TURNBACK - THE CREW REPORTED AN EXAM AUTO XFR FAULT IN FLIGHT. PERFORMED EXAM ACTION WITH NO C HANGE. UNABLE TO TRANSFER FUEL TO THE LT ENGINE CAUSING A LARGE FUEL IMBALANCE. THE CREW WAS ADVISED TO RETURN TO FIEL D AND AN EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE AIR RELEASE VALVE. OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F RT A28NM 20080812 NM 2008 8 12 USAA920081396 1 20080718 A 5320 69414372 TIE CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT - Q3-MAJOR REPAIR - TIE CLIP CRACKED AT BS 663 S10R. REPLACED TIE CLIP AT BS 663 S10R IAW B737 SRM 53-60-08. (A) 2 L 7 2 4F RT A16WE 20080812 EU 2008 8 12 USAA920081387 1 20080708 A 3213 201581001 STRUT AIRBUS 320 A320214 3930316 EU LT MLG CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 110UW 1112 PIT- C11- MAJOR REPAIR - LT STRUT UPPER LEG HAS CORROSION AT BASE BLENDED CORROSION ON LT STRUT UPPER LEG FOUND TO BE OU T OF LIMITS. REPLACED LEFT GEAR ASSEMBLY IAW US AIRWAYS ROUTINE TASK CARD 26-3200-9-004. (A) 2 L 7 2 4F RT A28NM 20080812 NM 2008 8 12 USAA920081407 1 20080717 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 517AU 23703 CLT- MAJOR REPAIR - CRACKED FUSELAGE SKIN AT BS 219.8 AT PILOTS WINDOW UPPER CORNER, REPAIRED FUSELAGE SKIN AT BS 219.8 AT PILOTS WINDOW UPPER CORNER IAW B737 SRM 53-10-01, REPAIR 10. (A) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 USAA920081403 1 20080629 A 5320 ANGLE BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT-Q3- MAJOR REPAIR - LEVEL 2 CORROSION ON FORWARD ENTRY THRESHOLD Z-ANGLE AT BS 328. REPLACED FORWARD ENTRY THRESHOLD Z-ANGLE AT BS 328 IAW B737 SRM 51-10-02 AND 51-40-02. (A) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 USAA920081381 1 20080712 A 5330 6545766 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 PHX-B-CHECK- MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT BS 500C, S10L. REPAIRED FUSELAGE SKIN AT BS 500C, S10L IAW US AIR WAYS EA120828. (A) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 USAA920081440 1 20080722 A 5315 D53472188202 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 5315 931 SAL-C7- MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR 68, Y1292. REPLACED FLOORBEAM AT FR 68, T1292 IAW A319 SRM 51-72-11 . (A) 2 L 7 2 4F RT A28NM 20080812 NM 2008 8 12 USAA920081442 1 20080722 A 5347 D531128130051 SEAT TRACK AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803AW 0931 SAL-C7- MAJOR REPAIR - CORROSION ON SEAT TRACK AT FR 16, BL-Y1292. REPLACED SEAT TRACK AT FR 16, BL-Y1292 IAW A319 SRM 51-72-11. (A) 2 L 7 2 4F RT A28NM 20080812 NM 2008 8 12 AALA200801628 1 20080615 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 21G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801594 1 20080611 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 676AN 29426 DFW - EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 WP 2008 8 12 AALA200801619 1 20080615 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 253AA 49286 MSP - EMERGENCY LIGHT AT SEAT 23D BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECK ED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801616 1 20080613 A 3350 TRIM PANEL BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 636AM 24594 DFW - EMERGENCY LIGHT BULLNOSE TRIM AT SEAT ROW 20 LOOSE. SECURED BULLNOSE TRIM FOR EMERGENCY LIGHT AT SEAT ROW 20. SY STEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 NM 2008 8 12 AALA200801720 1 20080627 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 672AA 25337 DFW - EMERGENCY LIGHT AT SEAT 18A INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 18A. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 WP 2008 8 12 AALA200801764 1 20080703 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 479AA 49654 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 21 TO 24 INOPERATIVE. RE-SECURED BATTERY PACK FOR EMERGENCY LIGHTS AT OVER HEAD SEAT ROWS 21 TO 24. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 08FDEA02565 1 20080630 A 5730 APB74411 SKIN DOUG MD11 MD11F 3023600 NM WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 609FE 48549 MAIN DECK CARGO COMPARTMENT, CORROSION FOUND ON PRESSURE BOUNDARY OVERWING UPPER SURFACE AT STA Y= 1227 TO 1228, XCW= 96 -97 RT UPPER SURFACE CORROSION ON MAIN DECK CARGO COMPARTMENT AT STA Y=1227 TO STA 1228 XCW 96- 97. REMOVED AS PER SRM 51-21-01 VOL II AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG 13 VOL I. ORIGINAL THICKNESS:0.175 INCH, MATERIAL REMOV ED:0.026 INCH, REMAINING THICKNESS:0.149 INCH. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080811 NM 2008 8 11 DXTA200803104 1 20080607 A 5300 UNKNOWN GULSTM 200 200 4500308 NM AIRFRAME VIBRATION E DXTA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 07 724QS 100 CLIMBING THROUGH 5000 FT/250KTS/SMOOTH AIR VIBRATION FELT THROUGH OUT FLIGHT DECK. VIBRATION NOTICED DURING DESCENT AS W ELL. (B) 2 L 7 2 4F RT A53NM 20080811 EU 2008 8 11 M7K2008F00098 1 20080414 A 2910 MA12500 PRESSURE SWITCH UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE HYD SYSTEM FAILED E M7KA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 808MH 3914 23100 HYDRAULIC PRESSURE LIGHT FAILED TO EXTINGUISH ALTHOUGH SYS WAS PRODUCING NORMAL PRESSURE AND OPERATING NORMALLY IN ALL O THER RESPECTS. A NEW SWITCH WAS INSTALLED AND DEFECT WAS CORRECTED. THIS PART HAS BEEN FOUND VERY RELIABLE. IF IT HAS A WEAKNESS IT IS THE MOLEX TYPE CONNECTOR UTILIZED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EA 2008 8 11 HNA2008F00023 1 20080619 A 6123 AUTOFEATHER SYS DHAV DHC8 DHC8311 1386006 EA INOPERATIVE A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 330EN 274 AUTOFEATHER WOULD NOT ARM DURING TAKEOFF. RETRIMMED BOTH ENGINES AUTOFEATHER ARMED AT 40 DEGREES OF P/LEVER ANGLE WITH A TORQUE OF 74 PERCENT. OPS CHECK GOOD. (K) 2 H 7 2 4T RT A13NM 20080811 CE 2008 8 11 GUU2008F00022 1 20080714 A 3260 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE NLG OUT OF ADJUST A GUUA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 17 81556 UE239 FLIGHT 9216, DURING FLIGHT, LANDING GEAR HANDLE LIGHT ILLUMINATED MOMENTARILY. ADJUSTED LT, RT AND NOSE GEAR UPLOCK SWI TCHES. (S) 2 L 7 2 4T RT A24CE 20080811 SO 2008 8 11 XGN2008F00010 2 20080723 A 8530 CYLINDER CESSNA 402 402B 207590P CE CONT O520 TSIO520* 17040 SO ENGINE CRACKED E XGNA O OTHER O OTHER NR NOT REPORTED 1 SW 05 4165G 295 402B1212 CRACKED BETWEEN FIN NR 1 AND FIN NR 3, AFT OF THE INJECTOR. MFG REV 3 E SERIES CYLINDER. ALL DEFECTIVE! (K) 1 L 7 2 3O 3 O A7CE E8CE 20080811 CE 2008 8 11 J7S2008F00000 1 20080713 A 2131 2119830 CONTROLLER LEAR 60 60LEAR 5170707 CE CABIN PRESSURE MALFUNCTIONED E J7SA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 05 261FX 319 CABIN LOST PRESSURIZATION AT FL410. CABIN ALTITUDE REACHED 14,500 FT. EXECUTED EMERGENCY DESCENT TO 15,000 FT IFE DECL ARED WITH EMERGENCY DESCENT. AIR DIVERSION WITH UNEVENTFUL LANDING AND TAXI. REPLACED PRESSURE CONTROLLER WITH REPAIRE D UNIT. SYSTEM OPS AND LEAK CHECK OK. RII C/W 6/16/2008 - MX CHECK FLIGHT SATISFACTORY. (K) 2 L 7 2 4F RT A10CE 20080811 NM 2008 8 11 HNA2008F00022 1 20080704 A 3350 6104789 BATTERY DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHT DISCHARGED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 839EX 226 EMERGENCY LIGHT ABOVE AIRSTAIR DOOR INOPERATIVE. ALSO, LT FWD EXTERIOR EMERGENCY LIGHT OUT. REMOVED AND REPLACED 3351P S1, CHECK GOOD BY OBSERVING LIGHT ILLUMINATE. (K) 2 H 7 2 4T RT A13NM 20080811 EA 2008 8 11 VNA2008F00002 1 20080626 A 2133 1037708 OUTFLOW VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CABIN PRESSURE FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 229PS 10328 7898 CREW REPORTED A CABIN ALTITUDE AMBER MESSAGE AFTER TAKEOFF AND THE CABIN WOULD NOT PRESSURIZE. CREW ELECTED TO RETURN T O CLT AND LANDED WITHOUT INCIDENT. MAINT REMOVED AND REPLACED THE PRIMARY OUTFLOW VALVE AND THE MAIN CABIN DOOR SEAL IA W THE AC MM. OPS CHECK WERE GOOD. AC WAS RELEASED FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 20080811 EA 2008 8 11 VNA2008F00001 1 20080624 A 5200 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE GROUND POWER OPEN A VNAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 05 712PS 10168 CREW REPORTED THE GROUND POWER DOOR LEFT OPEN AFTER TAKEOFF. CREW ELECTED TO RETURN TO DEPARTURE AND LANDED WITHOUT INC IDENT. MAINT INSPECTED AND FOUND DEFECTS. OPS CHECK GOOD AT THIS TIME. MAINT SECURED THE DOOR CLOSED. AC WAS RELEASE D FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A21EA E00063EN 20080811 NM 2008 8 11 F3L2008F00001 1 20080722 A 5210 D5211064320100 BUSHING AIRBUS A319 A319111 3930336 NM GE CFM56 CFM56* 13802 NE R1 DOOR UNSECURE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 938FR 2406 FLIGHT CREW NOTED THE R1 DOOR WOULD NOT LATCH IN THE OPEN POSITION. MAINT RESECURED THE GUST LOCK BUSHING IAW THE AMM 5 2-11-00-PB501. UPON COMPLETION OF THE REPAIR. IT WAS INSPECTED AND FOUND ACCEPTABLE. (K) 2 L 7 2 4F 4 F RT A28NM E2GL 20080811 NM 2008 8 11 AALA200801617 1 20080614 A 3350 LENS BOEING 767 767323 1385205 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 352AA 24033 JFK - EMERGENCY LIGHT AT LT NR FOUR DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LT NR FOUR DOOR. SYSTEM GR OUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080811 CE 2008 8 11 DXTA200803162 1 20080706 A 3150 WARNING MESSAGE CESSNA 680 680CE 2076811 CE ILLUMINATED E DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 362QS 6800051 FLAP FAIL CAS MESSAGE ILLUMINATED UPON ATTEMPTED TO FLAP RETRACTION. (A) 2 L 7 2 4F RC T00012WI 20080811 CE 2008 8 11 DXTA200803157 1 20080701 A 3150 WARNING LIGHT RAYTHN DH125 HAWKER800XP 7150012 CE ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 863QS 258463 REAR BAY OVERHEAT MASTER WARNING CAME ON. T/O ABORTED AT 115KTS. (A) 2 L 7 2 4F RT A3EU 20080811 NM 2008 8 11 AALA200801702 1 20080625 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 917AN 29518 JFK - EMERGENCY LIGHT AT SEAT 19D INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A16WE 20080811 WP 2008 8 11 AALA200801722 1 20080627 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9304C 49530 STL - EMERGENCY LIGHT AT SEAT ROW 22DEF INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 22DEF. SYSTEM G ROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A6WE 20080811 EU 2008 8 11 HDN2008F00000 1 20080717 A 2612 B332M FIRE DETECTOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 1 NACELLE CORRODED B HDNR O OTHER N FALSE WARNING CR CRUISE 1 SW 03 911EB S812 CAE831133 NR 1 ENG FIRE DETECTOR WARNING LIGHT ILLUMINATED DURING CRUISE FLIGHT. AC DIVERTED FROM FLIGHT PATH AND LANDED ON THE S HOULDER OF THE ROAD. IT WAS DETERMINED THAT THERE WAS NOT A FIRE. MAINT WAS DISPATCHED TO THE LZ. IT WAS DETERMINED T HAT CORROSION WAS EVIDENT BETWEEN THE WIRE TERMINAL AND THE FIRE DETECTOR. THE TERMINAL AND THE FIRE DETECTOR WERE CLEA NED, AND AN OPERATIONAL CHECK OF THE FIRE DETECTION SYS WAS SATISFACTORY. (K) 1 G 7 2 3U 3 U H3EU E4CE 20080811 SW 2008 8 11 EGI2008F00002 1 20080626 A 6410 206016201135 BLADE BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL TAIL ROTOR DAMAGED E EGIA K NONE O OTHER IN INSP/MAINT 1 SW 09 255EV 86 51488 DURING SCHEDULED 100 HOUR INSP OF AC, INSP OF TAIL ROTOR BLADES REVEALED THAT ONE T/R BLADE HAD MECHANICAL DAMAGE. THE DAMAGE WAS CONFINED TO THE T/E WHICH CONSISTED OF A DENT AT T/R BLADE STA 16.5 APPROXIMATELY .010 INCH DEEP AND THE T/E BENT IN A SPAN OF APPROX 2 INCHES LONG WITH A .030 INCH DEFLECTION. THE T/R BLADE WAS REPLACED. THE T/R BLADE WILL BE SHIPPED FOR EVALUATION AND POSSIBLE REPAIR. PROBABLE CAUSE OF THIS DAMAGE COULD HAVE BEEN CAUSED BY A MAINTENANCE STAND STRIKING THE BLADE OR THE BLADE FLAPPING INTO A MAINTENANCE STAND. (K) 1 G 7 1 3U 3 U H2SW E1GL 20080812 NM 2008 8 12 AALA200801606 1 20080613 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 780AN 29956 DFW - EMERGENCY LIGHT AT SEAT 21C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 WP 2008 8 12 AALA200801694 1 20080624 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 567AM 53293 LGA - EMERGENCY LIGHT AT OVERHEAD SEAT 26D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT OVERHEAD SEAT 26D. SYSTEM GR OUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A6WE 20080812 NE 2008 8 12 AALA200801582 2 20080611 A 7230 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 2 ENGINE STALLED A AALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 21 7519A 49896 709951 DFW INFLIGHT T1413/11JUN. CREW REPORTED NR TWO ENGINE COMPRESSOR STALL ON CLIMB. CREW REDUCED POWER TO IDLE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NR TWO ENGINE ON 11JUN AT DFW. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F 4 F A6WE E9NE 20080812 NM 2008 8 12 AALA200801777 1 20080705 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 370AA 25197 SFO - EMERGENCY LIGHT AT OVERHEAD SEAT 5B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 5B. SYSTEM G ROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080812 EU 2008 8 12 USAA920081443 1 20080702 A 2560 SURVIVAL KIT AIRBUS A319 A319112 3930323 EU L2 DOOR OUT OF POSITION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 1019 PIT - DROP IN -EES - L2 DOOR SURVIVAL KIT LANYARD VELCRO PULLED APART AND DROPPED OUT OF TRIGGER ASSY. REROUTED LANYARD VELCRO END THRU TRIGGER ASSY PER - (JOB CARD JA-25-62-02). (A) 2 L 7 2 4F RT A28NM 20080812 NM 2008 8 12 AALA200801776 1 20080705 A 3397 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 625AA 24583 SFO - EMERGENCY LIGHT AT RT NR ONE DOOR INTERIOR AND EXTERIOR AND EXIT SIGN NEXT TO MID LAVATORY INOPERATIVE. SECURED C ONNECTOR FOR EMERGENCY LIGHTS AT RT NR ONE DOOR INTERIOR AND EXTERIOR AND EXIT SIGN NEXT TO MID LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 EU 2008 8 12 08FDEA02636 1 20080702 A 5320 A53778198422200 BRACKET AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN, UNDER FLOOR PANEL 231 BH; THE SUB-FLOOR PANEL IS CORRODED BETWEEN FRAME 29 AND FRAME 30. CHECKED THE LIMITS FOR FLOOR PANEL 231 BH SUB-FLOOR PANEL AND FOUND IT TO BE OUT OF LIMITS REF A300-600 SRM 51-74-10 AND SRM 53-14-15. RE MOVED PANEL 131 NW REF A300-600 SRM 51-40-21; PARA 5. REMOVED THE SUB-FLOOR PANEL BETWEEN FRAMES 29-30 REF A300-600 SRM 51-40-21; PARA 6. LOCATED AND DRILLED BRACKET REF A300-600 SRM 51-40-44. INSTALLED BRACKET REF A300-600 SRM 51-40-44. APPLIED CIC REF A300-600 AMM 51-20-00- 0. INSTALLED PANEL 131 NW PER AIRBUS PMS 01-05-12. 2 L 7 2 4F RT A35EU 20080812 NM 2008 8 12 08FDEA02808 1 20080710 A 5320 ACA72241 FITTING DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 609FE 48549 MAIN DECK CARGO COMPARTMENT, UPPER CARGO DOOR LOWER SILL NR 6 SPOOL FITTING FASTENER HOLES FOUND WITH CRACK INDICATIONS AT HOLE 'A' AND 'D' DURING OPEN HOLE HFEC INSPECTION. MAIN DECK CARGO COMPARTMENT, UPPER CARGO DOOR LOWER SILL NR 6 SPO OL FITTING CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 VOL I FIG 10. REPAIR CLASSIFIED MAJOR AS PER FEDEX GMM 6-2-10 0. 2 L 7 3 4F RT A22WE 20080812 EU 2008 8 12 08FDEA02820 1 20080710 A 3610 A2121121100000 FITTING AIRBUS 310 A310203 3930313 EU BLEED AIR SYS LOOSE A FDEA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 CE 21 431FE 316 ON CLIMB-OUT PASSING 15000 FT GOT NR 2 BLEED FAULT. COMPLIED WITH ECAM, RETURNED TO DFW. FOUND SENSE LINE FOR NUMBER 2 ENG PNEU PRESSURE REGULATOR LOOSE AT PYLON FITTING SECURED FITTING. PERFORMED FUNCTIONAL CHECK OF THE NUMBER 2 ENG BLE ED REF MM 36-11-00-6. 2 L 7 2 4F RT A35EU 20080812 EU 2008 8 12 08FDEA02828 1 20080711 A 5320 A5378198422200 WEB AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN METAL PANEL UNDER FLOOR PANEL 231 WG FROM FRAME 26 TO FRAME 28 IS CORRODED. REMOVED THRUST BRACKETS IAW A300 -600 SRM 51-40-21; PARA 6. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 51-70-10. RECEIVED 2 NEW THRUST BRACKETS P/N A53 78198422200, PO 624015.1 AND A5378198423400, PO 623903.1. PART MARKED THRUST BRACKETS IAW FEDEX GMM 7-0-1001. LOCATED AND DRILLED HOLES IAW A300-600 SRM 51-40- 44. ALODINED; PRIMED AND PAINTED THE THRUST BRACKETS IAW A300-600 AMM 51-23 -10-0. INSTALLED THRUST BRACKETS IAW A300-600 SRM 51-40-21; PARA 6. APPLIED CIC TO THRUST BRACKETS IAW A300-600 AMM 51 -22-00-0. 2 L 7 2 4F RT A35EU 20080812 NM 2008 8 12 08FDEA02833 1 20080712 A 5713 65185702 STRINGER BOEING 727 727225 1384077 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 GENERATED BY EO 7-5710-7-4322 RT WING STA 686.5, VENT STRINGER STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS REF EO NR 7-5710-7-4322. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080812 NM 2008 8 12 USAA920081390 1 20080718 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 303AW 24010 FLT 287 PHX-SJL - EE - FORWARD VERTICAL FLASHLIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY. OPERATIONAL CHE CK WAS GOOD. (A) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 USAA920081399 1 20080722 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 512AU 23595 FLT 1465 CLT-IND- EEL - AFT EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR THE AFT EM ERGENCY EXIT LIGHT. OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F RT A16WE 20080812 EU 2008 8 12 USAA920081425 1 20080723 A 3350 33511314 LIGHT AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 627AW 66 SAL-C6- EEL - EMERGENCY EXIT LIGHT AT R1 DOOR IS INOP. REPAIRED EMERGENCY EXIT LIGHT AT R1 DOOR IAW AIRBUS AMM 33-51-00 . (A) 2 L 7 2 4F RT A28NM 20080812 EU 2008 8 12 USAA920081420 1 20080727 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A USAA K NONE L NO TEST NR NOT REPORTED 1 EA 19 601AW 18543 1071 1935 FLT 351 PHX-MSP - ELL- FLIGHT ATTENDANT REPORTS AFT EMERGENCY LIGHTS NOT WORKING PROPERLY. MAINTENANCE REMOVED AND REPL ACED THE AFT RT EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL TEST WAS GOOD. (A) 2 L 7 2 4F RT A28NM 20080812 NM 2008 8 12 USAA920081417 1 20080718 A 5753 6546430122 SKIN BOEING 737 7374B7 1384702 NM FOREFLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 451UW 24934 CLT- MAJOR REPAIR-C1 CHECK - RT WING INBOARD FOREFLAP UPPER RT SURFACE IS DELAMINATED. REPLACED RT WING INBOARD FOREFLA P IAW B737 AMM 27-51-07. (A) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 USAA920081389 1 20080720 A 5330 6545774 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 CLT- DROP IN- MAJOR REPAIR - FUSELAGE SKIN CRACK AT BS 727E S23L. REPAIRED FUSELAGE SKIN AT BS 727E S23L IAW B737 SRM 5 3-00-01 REPAIR 31. (A) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 USAA920081404 1 20080630 A 5210 507945264 DOOR BOEING 737 737401 1384701 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT-Q3- MAJOR REPAIR - PASSENGER DOOR INTERIOR SKIN CRACKED ON AFT SIDE AT NR 4, 5, 6 AND 7 OF STOP PIN ACCESS HOLES. R EPAIRED PASSENGER DOOR INTERIOR SKIN AT NR 4, 5, 6 AND 7 STOP PIN ACCESS HOLES OF IAW US AIRWAYS EA 100547. (A) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 USAA920081423 1 20080715 A 5320 INTERCOSTAL BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT-Q3- MAJOR REPAIR - CRACK IN RADIUS OF INTERCOSTAL WEB BS 294 S15L. REPAIRED INTERCOSTAL WEB BS 294 S15L IAW B737 SR M 51-40-00 AND BOEING DRAWING 65-17684-635 AND B737 SRM 51-40-00. (A) 2 L 7 2 4F RT A16WE 20080813 NM 2008 8 13 08FDEA02884 1 20080715 A 5330 65545836 SKIN BOEING 727 727233 138408A NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 275FE 22040 FUSELAGE EXTERIOR SKIN GOUGED STA 1090 STR 22R. BLENDED OUT DAMAGE AND FOUND OUT OF LIMITS IAW SRM 51-10-1 AND 53-30-1 FIG 1 AND 2. REPAIRED SKIN FUSELAGE STA 1090 STRINGER 22R IAW EA 7-5330-122334. 2 L 7 3 4F RT A3WE 20080813 EU 2008 8 13 08FDEA02660 1 20080703 A 5321 B5327046101600 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN FLOOR PANEL NR 231 CF IS PUNCTURED IN MANY AREAS BY BALL BEARINGS. REPAIRED PER A300-600 SRM 53-10-20; FIG 2 01. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02661 1 20080703 A 5321 B5327046501000 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN FLOOR PANEL NR 231 GH IS PUNCTURED ON THE UPPER SURFACE AREAS BY BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 201. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02668 1 20080703 A 5321 B5327080300600 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN FLOOR PANEL 231 JG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02669 1 20080703 A 5321 B5327046200400 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN FLOOR PANEL 231 GG UPPER SURFACE HAS PUNCTURES FROM BALL BEARINGS AND THE EDGING COMPOUND IS MISSING FROM THE INBD CORNER. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02670 1 20080703 A 5321 B5327051300000 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN FLOOR PANEL 231 UG UPPER SURFACE HAS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A3 00-600 SRM 53-10-20; FIG 202. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02671 1 20080703 A 5321 B5327048300400 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN FLOOR PANEL 231 TG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02672 1 20080703 A 5321 B5327048300400 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN FLOOR PANEL 231 SG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02673 1 20080703 A 5321 B5327049902200 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CARGO DECK FLOOR PANEL 232 PF HAS BALL BEARINGS STUCK IN THE TOP SURFACE AND PUNCTURES FROM FRAME 19 TO 22; RBL 57 TO RBL 77. REPAIRED DAMAGED AREAS PER A300-600 SRM 53-10-20; FIG 201. 2 L 7 2 4F RT A35EU 20080813 NM 2008 8 13 08FDEA02842 1 20080712 A 5511 65382051 SPAR BOEING 727 727225 1384077 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 CORROSION ON LT HORIZ STAB FRONT SPAR UPPER CHORD, STAB STA 4.5 BLENDED CORROSION, ORIGINAL THICKNESS IS .120 INCHES. M ATERIAL REMOVED .052 INCHES. MATERIAL REMAINING .088 INCH REPAIRED UPPER CHORD REF EA NR 7-5510-114204 DATED 7-11-08. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080813 EU 2008 8 13 08FDEA02860 1 20080714 A 5755 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 5 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD TS0570 613 FOUND DELAMINATION ON RT SPOILER NR 5 OUT OF SRM LIMIT. REPAIR PERFORMED BY REPLACEMENT OF SPOILER NR 3 RT IAW AMM 27-6 1-53 PAGE 401. 2 L 7 2 4F RT A35EU 20080813 NM 2008 8 13 08FDEA02821 1 20080711 A 2910 LINE BOEING 727 727227 1384078 NM HYD SYSTEM CRACKED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 21 487FE 21490 AT FL 320 "A" SYS QUANITY DECREASED TO ZERO. RAN QRH FOR HYD SYS "A" LEAK CHECKS PERFORMED. MANUAL GEAR EXT AND ALT FL APS LANDING. SYS "A" FLUID SHUTOFF WAS CLOSED AT 05:09, ENGINE SHUT DOWN AT 05:51. FOUND THE NR 2 SPOILER RETURN LINE CRACKED. WORKING ON FABRICATING LINE. SPLICED IN NEW SECTION OF HYD LINE FROM THE RETURN LINE OF THE NR 2 SPOILER ACT UATOR OPS AND LEAK CHECK GOOD IAW B-727-200 MM 20-10-005-8. SERVICED "A" SYSTEM HYD TO FULL IAW B-727-200 MM 12-12-000- 2. 2 L 7 3 4F A3WE 20080813 EU 2008 8 13 08FDEA02897 1 20080715 A 5330 A53974207200 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND OLD REPAIR (REWORKED AREA) ON SKIN PANEL C 67, P 48 RT RELATED TO RAS- DA/HAM1376.2/96, WHICH IS SMALLER THAN DET ECTED. REPAIR RENEWED IAW RAS/EFW/9000065/2008 ISS A (REWORK OF THE AREA, PERFORM FLAP PEENING, ENSURE CORROSION FREE C ONDITION), APPROVED BY EA 6-5316-120100. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02898 1 20080715 A 5315 A53974343200 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON CROSSBEAM C 72 OUT OF LIMIT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02682 1 20080703 A 5321 B5327046200600 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CARGO DECK FLOOR PANEL 232 GG HAS NUMEROUS PUNCTURES AND BEARINGS STUCK IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02684 1 20080703 A 5321 B5327046000200 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CARGO DECK FLOOR PANEL 232 FG HAS NUMEROUS PUNCTURES AND BALL BEARINGS STUCK TO THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 201. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02685 1 20080703 A 5321 B5327052200000 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN FLOOR PANEL 231 JH UPPER SURFACE HAS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A3 00-600 SRM 53-10-20, FIG 202. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02686 1 20080703 A 5321 B5327080500000 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN FLOOR PANEL 231 XG UPPER SURFACE HAS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A3 00-600 SRM 53-10-20, FIG 202. 2 L 7 2 4F RT A35EU 20080813 NM 2008 8 13 08FDEA02874 1 20080714 A 5310 143N8328U54 CREASE BEAM BOEING 757 757236 1384971 NM BS 680-740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 MAIN CABIN CREASE BEAM CHORD BS 680 -740, RBL 66 HAS CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CRE ASE BEAM, RECEIVED NEW PART NR 143N8328U54 IAW SRM 53-30-13. INSTALLED NEW CREASE BEAM PART IAW SRM 51-40-02, AND 51- 10-02, FS 680-740, RBL 66. 2 L 7 2 4F RT A2NM 20080813 NM 2008 8 13 08FDEA02875 1 20080714 A 5347 SUPPLIED SEAT TRACK BOEING 757 757236 1384971 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 STA 1046, LBL 47, LUG SCALLOP IS MISSING ON SEAT TRACK. REMOVED SEAT TRACK SECTION IAW SRM 53-00-52. FABRICATED NEW O N MAE TRAV NR T8/750424. INSTALLED NEW SEAT TRACK REPAIR PARTS IAW SRM 51-40-02, AND 53-00-52. 2 L 7 2 4F RT A2NM 20080813 WP 2008 8 13 NWAA082709751 1 20080612 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 751NW 47115 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 13-15 OF THE CABIN WERE INOPERATIVE. M AINTENANCE FOUND IMPROPER INSTALLATION OF THE BATTERIES. BATTERIES HAD BEEN INSTALLED BACKWARDS. REINSTALLED BATTERIES AND OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F A6WE 20080813 2008 8 13 NWAA082729928 4 20080612 A 2565 SLIDE DOUG DC9 DC931 3022065 WP TAILCONE INOPERATIVE A NWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 01 8921E 45836 THE AIRCRAFT ARRIVED AT EAU AS A DIVERTED FLIGHT NUMBER DUE TO CABIN PRESSURIZATION FAILURE. DURING GROUND OPERATIONS A T EAU, RAMP PERSONNEL INADVERTENTLY DROPPED THE TAIL CONE AND THE SLIDE DID NOT DEPLOY, AS DESIGNED. (A) 2 L 7 2 4F A6WE 20080813 NM 2008 8 13 NWAA082625649 1 20080520 A 5414 SKIN BOEING 757 757251 1384970 NM NR 2 NACELLE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 549US 26496 DURING "M" CHECK FOUND CRACKS IN NR 2 PYLON RT SKIN AT NAC STA 132. REPAIRED PER EA 56-212996 SECT 1. SECTION 2 REQUIR ES FOLLOW UP INSPECTION BY 19 MAY 09. (A) 2 L 7 2 4F RT A2NM 20080813 NM 2008 8 13 NWAA082645514 1 20080523 A 5330 SKIN BOEING 757 757251 1384970 NM BS 1310 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 514US 23202 DURING INSPECTION FOUND DAMAGE TO FUSELAGE SKIN AT BS 1310 S2R-S3R. REPAIRED PER EA 55-213052. (A) 2 L 7 2 4F RT A2NM 20080813 WP 2008 8 13 NWAA082659881 1 20080606 A 5330 SKIN DOUG DC9 DC951 3022051 WP BS 1266 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 676MC 47652 DURING LINE CHECK FOUND CRACK IN FUSELAGE SKIN AT BS 1266 LT BELOW VERTICAL STABILIZER ATTACH ANGLE. REPAIRED PER EA 98 -213119. (A) 2 L 7 2 4F RT A6WE 20080813 NM 2008 8 13 NWAA082806743 1 20080620 A 2910 HYDRAULIC SYSTEM BOEING 747 747249F 1384849 NM NR 1 LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 643NW 22245 DURING FLIGHT, HYDRAULIC SYSTEM NR 1 FLUID BEGAN DECREASING AND WENT TO 0. FLIGHT CONTINUED ON TO ANC. FOLLOWED COM PR OCEDURE AND SYSTEM NR 1 WAS SHUT DOWN. CFR WAS CALLED OUT TO MEET THE FLIGHT AND LANDING WAS UNEVENTFUL. AIRCRAFT WAS THEN TOWED TO THE CARGO RAMP. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE ADP, EDP AND PRESSURE AND CASE DRAIN MODULE FILTERS. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 4 4F RT A20WE 20080813 WP 2008 8 13 NWAA082849851 1 20080621 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NC 47708 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 19-22 OF THE CABIN AND IN THE TAIL COMP ARTMENT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIO NAL CONDITION. (A) 2 L 7 2 4F RT A6WE 20080813 WP 2008 8 13 NWAA082889613 1 20080623 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 613NW 47438 DURING LINE CHECK, THE RT AND LT HAND OVERWING EMERGENCY EXIT SIGNS AT ROW 12 AND THE EMERGENCY PATHWAY LIGHTING AT ROWS 11, 12 & 13 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR EXIT ROW 12ABC WITH A SERVICEABLE UNIT AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (A) 2 L 7 2 4F A6WE 20080813 NM 2008 8 13 NWAA083006746 1 20080704 A 3350 POWER SUPPLY BOEING 747 747222B 1384904 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 646NW 23737 DURING OVERNIGHT CHECK FOUND UPPER DECK COCKPIT EMERGENCY LIGHT WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED POWER S UPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 4 4F RT A20WE 20080813 NM 2008 8 13 NWAA082933132 1 20080704 A 3350 BATTERY PACK AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 322NB 1434 EMERGENCY LIGHT BATTERY PACK AT LT OVERWING EXIT INOP. REPLACED BATTERY POWER SUPPLY UNIT, CHECKS GOOD. (A) 2 L 7 2 4F RT A28NM 20080813 EU 2008 8 13 NWAA082923230 1 20080702 A 3350 POWER SUPPLY AIRBUS 320 A320211 3930320 EU EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 330NW 6521 6521 307 DURING TESTING OF THE EMERGENCY EGRESS LIGHTING, EPSU COMM EMER L ANNUNCIATED. REPLACED POWER SUPPLY 11WL, CHECKS GOOD. (A) 2 L 7 2 4F RT A28NM 20080811 NM 2008 8 11 AALA200801665 1 20080618 A 3350 LENS BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 612AA 24488 DFW - EMERGENCY LIGHT EXIT SIGN AT FORWARD LT OVERWING DAMAGED. REPLACED LENS FOR EMERGENCY LIGHT EXIT SIGN AT FORWARD LT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 EA 2008 8 11 A6WA200840513 1 20080616 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 444ZW 7788 BULKHEAD CLIPS CRACKED AT FS 280, LBL 9 AND WL 72. BULKHEAD CLIPS AT FS 280, LBL 9 AND WL 72 REPLACED IAW CRJ 200 SRM 5 1-42-06 AND SRM 51-42-21. (A) 2 L 7 2 4F RT A21EA 20080811 SO 2008 8 11 GUU2008F00021 1 20080531 A 5210 SWITCH EMB 120 EMB120ER 3260203 SO PAX DOOR OUT OF ADJUST A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 282AS 120226 FLIGHT 9209, MAIN CABIN FWD DOOR WILL NOT CLOSE WHEN CONTROL BUTTON IS PRESSED BOTH INSIDE AND OUTSIDE. CLEAN AND ADJUST ED PASSENGER CREW ENTRY DOOR LIFTING AND LOWER SUBSYSTEMS SWITCH. (A) 2 L 7 2 4T RT A31SO 20080811 NM 2008 8 11 USAA920081296 1 20080708 A 5240 6545871132 STOP FITTING BOEING 737 737401 1384701 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT- Q3 MAJOR REPAIR 03C10652003/001 AND 03C10652003/002- FORWARD SERVICE DOOR INBOARD STOP FITTING CRACKED DIRECTLY ABO VE AND BELOW CENTERING GUIDE. REPAIRED FORWARD SERVICE DOOR INBOARD STOP FITTING DIRECTLY ABOVE AND BELOW CENTERING GUI DE IAW US AIRWAYS TYPICAL REPAIR 52-10-11 (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081295 1 20080705 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT- Q3 MAJOR REPAIR 03C10753041/006- FRAME CRACKED AT BS 500A BETWEEN S-8L AND S-9L. REPAIRED FRAME AT BS 500A BETWEEN S-8L AND S-9L IAW TYPICAL REPAIR 53-10-20E.(B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAABB08114 1 20080709 A 3350 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 915AW 22209 PHX- ROW 6L EMERGENCY LIGHT ON SEAT INOP. MAINTENANCE REPLACED EMERGENCY LIGHT ASSEMBLY ON SEAT 6L. OPS CHECKS OK. 2 L 7 2 4F RT A2NM 20080811 NM 2008 8 11 USAASB08048 1 20080706 A 2560 P2070003001 FLASHLIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 454UW 24996 BOS MAINTENANCE REPORTED THE FORWARD CABIN EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWA RD CABIN EMERGENCY FLASHLIGHT. OPERATIONAL CHECK NORMAL. (B) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 USAA920081361 1 20080616 A 5311 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN- C21 MAJOR REPAIR NR 6112049-FRAME CRACKED AT BS847, S9R,WL216. REPAIRED FRAME AT BS847, S9R,WL216 IAW AWA TASKCARD M1C53002. (B) 2 L 7 2 4F RT A16WE 20080812 NM 2008 8 12 AALA200801520 1 20080604 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 762AN 31479 DFW - EMERGENCY LIGHTS AT SEAT 30C AFT POSITION INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 30C AFT POSITION . SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801640 1 20080617 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 NRT - EMERGENCY LIGHT AT FIRST CLASS GALLEY NEAR CLOSET INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FIRST CLASS G ALLEY CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801684 1 20080622 A 3350 LENS BOEING 767 767323 1385205 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 39356 24037 DFW - EMERGENCY LIGHT AT LT NR FOUR DOOR AT LAVATORY AREA MISSING LENS. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LT NR FOUR DOOR AT LAVATORY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080812 NM 2008 8 12 AALA200801663 1 20080618 A 3350 LENS BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 698AN 26980 DFW - EMERGENCY LIGHT AT SEAT 15D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 EU 2008 8 12 AALA200801584 1 20080611 A 3260 LINK ASSY AIRBUS 300 A300B4605R 3930308 EU LANDING GEAR DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 80052 460 JFK INFLIGHT T1299/11JUN. CREW REPORTED RED MAIN LANDING GEAR DOOR INDICATION AFTER TAKEOFF. RETURNED TO JFK AND LANDE D WITHOUT INCIDENT. REPLACED LANDING GEAR PROXIMITY SENSOR LINK ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080812 NM 2008 8 12 AALA200801595 1 20080611 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 793AN 30255 DFW - EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801597 1 20080611 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 793AN 30255 DFW - EMERGENCY LIGHT AT SEAT 34C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 34C. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NM 2008 8 12 AALA200801767 1 20080703 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39367 25194 SFO - EMERGENCY EXIT SIGN LIGHT AT RT NR ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT RT NR ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080812 WP 2008 8 12 AALA200801747 1 20080701 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 587AA 53250 LGA - EMERGENCY LIGHT AT FORWARD SEAT 7D MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT FORWARD SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801631 1 20080615 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT LT NR ONE CLOSET AREA DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LT NR ONE CLOSET AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 EU 2008 8 12 08FDEA02829 1 20080711 A 5320 A5378198423400 WEB AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN METAL PANEL UNDER FLOOR PANEL 231 WG FROM FRAME 26 TO FRAME 28 IS CRACKED. REMOVED THRUST BRACKETS IAW A300- 600 SRM 51-40-21; PARA 6. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 51-70-10. RECEIVED 2 NEW THRUST BRACKETS P/N A537 8198422200, PO 624015.1 AND A5378198423400, PO 623903.1. PART MARKED THRUST BRACKETS IAW FEDEX GMM 7-0-1001. LOCATED A ND DRILLED HOLES IAW A300-600 SRM 51-40-44. ALODINED; PRIMED AND PAINTED THE THRUST BRACKETS IAW A300-600 AMM 51-23-10- 0. INSTALLED THRUST BRACKETS IAW A300-600 SRM 51-40-21; PARA 6. APPLIED CIC TO THRUST BRACKETS IAW A300-600 AMM 51-22 -00-0. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02663 1 20080703 A 5321 B5327046200400 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN FLOOR PANEL 231 GG IS PUNCTURED ON THE UPPER SURFACE IN MANY AREAS BY BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 201. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02679 1 20080703 A 5321 B5327048400400 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CARGO DECK FLOOR PANEL 232 UG HAS BALL BEARINGS (4 PLACES) STUCK IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02857 1 20080714 A 5100 NONE AIRBUS 300 A300B4622R 3930312 EU NOT AN SDR NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 742FD 613 FOUND OLD DOUBLER REPAIR ON LT KRUEGER FLAP INNER SKIN WITHOUT ANY OLD DOCUMENTATION. REPAIR PERFORMED BY REPLACEMENT OF KRUEGER FLAP IAW AMM 278711 PAGE 401. 2 L 7 2 4F RT A35EU 20080813 NM 2008 8 13 NWAA082516314 1 20080604 A 3350 CHARGER BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 674US 30269 DURING OVERNIGHT CHECK, FOUND ZONE A & B RT SIDE EMERGENCY PATH LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED BATTERY C HARGER. OPERATIONAL CHECKED GOOD, AND AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 4 4F RT A20WE 20080813 NM 2008 8 13 NWAA082546740 1 20080603 A 3240 BRAKE BOEING 747 747251F 1384898 NM MLG FIRE A NWAA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 GL 01 640US 23888 ON TAXI IN BRAKE TEMP OVERHEAT LIGHT ILLUMINATED AND LT WING AND BODY GEAR TEMP GAUGES INDICATED IN RED ZONE. LT WING A ND BODY BRAKES CAUGHT FIRE. THE FIRE DEPARTMENT WAS DISPATCHED AND EXTINGUISHED THE FIRE. MAINTENANCE REMOVED AND REPL ACED LT SIDE 1-8 WING ANYBODY GEAR BRAKES AND ALL 16 MAIN LANDING GEAR WHEELS. (A) 2 L 7 4 4F RT A20WE 20080813 WP 2008 8 13 NWAA082689928 1 20080611 A 2131 CONTROLLER DOUG DC9 DC931 3022065 WP CABIN PRESSURE MALFUNCTIONED A NWAA B G A EMER. DESCENT O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 8921E 45836 FLT LOST CABIN PRESSURIZATION AT CRUISE AT FL 335. FULL ANIT-ICE PROTECTION WAS OPERATING. CREW DECLARED AN EMERGENCY WITH ATC, ACCOMPLISHED AN EMERGENCY DESCENT TO 10,000FT, AND DIVERTED TO A SAFE LANDING AT EAU. COM PROCEDURES INCLUDING RED-BORDER CHECK LIST ACCOMPLISHED BUT DID NOT CORRECT PROBLEM. CABIN MASKS AUTOMATICALLY DEPLOYED WHEN CABIN ALTITUDE REACHED 14,000 FT. MAXIMUM ALTITUDE CABIN ATTAINED WAS 17,000 FT AS ACFT DESCENDED THROUGH FL 310. MX COMPLETED A BIT E CHECK OF THE DIGITAL COMPONENTS AND ALSO PERFORMED EXTENSIVE SYSTEM LEAK AND VESSEL LEAK CHECKS. BOTH CABIN PRESSURE CONTROLLERS AND THE OUTFLOW VALVE WERE ALL REPLACED IN ADDITION TO NUMEROUS CLAMP AND DUCT DISCREPANCY CORRECTIONS. (A) 2 L 7 2 4F A6WE 20080813 WP 2008 8 13 NWAA082699863 1 20080612 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 772NC 47774 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN LIGHT PACK FOR THE AFT RT OVERWING HATCH WAS BROKEN. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (A) 2 L 7 2 4F RT A6WE 20080813 WP 2008 8 13 NWAA082839759 1 20080620 A 3350 BATTERY DOUG DC9 DC941 302207N WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 759NW 47287 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAI LED. MAINTENANCE REPLACED THE ASSOCIATED FUSE AND INSTALLED NEW BATTERIES IN THE POWER SUPPLY. OPERATIONAL CHECK WAS G OOD. (A) 2 L 7 2 4F A6WE 20080813 WP 2008 8 13 NWAA083159759 1 20080718 A 3397 WIRE DOUG DC9 DC941 302207N WP EMEGENCY LIGHTS SHORTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 759NW 47287 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 12-15 AND THE AFT LT OVERWING EMERGENCY EXIT SIGN WERE INOPERATIVE. MAINTENANCE FOUND A SHORTED WIRE, REPAIRED IT, REPLACED THE FUSE, AND REPLACED THE APPLICA BLE POWER SUPPLY. OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F A6WE 20080813 WP 2008 8 13 NWAA083019921 1 20080707 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 943N 47647 DURING LINE CHECK, THE "LOWER" OVERWING EMERGENCY EXIT LIGHTS AND THE EMERGENCY PATHWAY LIGHTING AT ROWS 8, 9, & 10 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. ( A) 2 L 7 2 4F A6WE 20080813 NM 2008 8 13 NWAA083416624 1 20080726 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 624US 21706 DURING OVERNIGHT CHECK, FOUND ZONE-E FLOOR EMERGENCY LIGHTS LEFT SIDE INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPP LY AND BATTERY PACK. OPERATIONAL CHECKED GOOD, AND AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 4 4F RT A20WE 20080813 WP 2008 8 13 NWAA083429876 1 20080726 A 3350 BATTERY DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 785NC 48110 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 23-26 OF THE CABIN WERE INOPERATIVE. M AINTENANCE REPLACED THE ASSOCIATED FUSE AND INSTALLED NEW BATTERIES IN THE POWER SUPPLY. OPERATIONAL CHECK WAS GOOD. ( A) 2 L 7 2 4F RT A6WE 20080813 EA 2008 8 13 COMA0880012 1 20080718 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT DISCHARGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 676CA 10754 15127 EMERGENCY LIGHTS WILL NOT COME ON. REPLACED BATTERY PACK NR 4. (S) 2 L 7 2 4F RT A21EA 20080813 EA 2008 8 13 COMA0880013 1 20080718 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT DISCHARGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 676CA 15439 15127 EMERGENCY LIGHTS WILL NOT COME ON. REPLACED BATTERY PACK NR 5. (S) 2 L 7 2 4F RT A21EA 20080813 WP 2008 8 13 NWAA083119758 1 20080713 A 2133 OUTFLOW VALVE DOUG DC9 DC941 302207N WP CABIN PRESSURE MALFUNCTIONED A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 758NW 47286 WHILE EN ROUTE TO DTW THE ACFT EXPERIENCED A LOSS OF CABIN PRESSURIZATION CONTROL WHICH REQUIRED AN EMERGENCY DESCENT TO FL140. OXYGEN MASK DID NOT DEPLOY AND THE FLIGHT CONTINUED TO A NORMAL SAFE LANDING AT DTW AS SCHEDULED. MAINTENANCE IS CONDUCTING A THOROUGH SYSTEM FUNCTIONAL CHECK AS WELL AS A DETAILED VESSEL PRESSURE DECAY CHECK. MAINTENANCE COMPLET ED BITE OF BOTH CONTROLLERS AND FAULTS DID DISPLAY. ACCOMPLISHED REPLACEMENT OF THE OUTFLOW VALVE AS WELL AS "REWORKING " ALL CLAMPS AND HOSE CONNECTIONS IN TAIL COMPARTMENT. "REWORKED" ALL DOOR SEALS AND DRAIN MAST. DETAILED VESSEL PRESS URE DECAY CHECK RESULTS WERE SATISFACTORY. SYSTEM RETURNED TO OPERATIONAL CONDITION. (S) 2 L 7 2 4F A6WE 20080813 NM 2008 8 13 NWAA083135533 1 20080716 A 3350 LAMP BOEING 757 757251 1384970 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 533US 24264 DURING OVERNIGHT MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE FROM ROW 33 TO ROW 39, THE SECTION AFT OF DOOR 3. MAINTENANCE RELAMPED THE EFFECTED LIGHTS AND ALL OPERATIONS CHECKED GOOD. (S) 2 L 7 2 4F RT A2NM 20080813 EA 2008 8 13 REXA08029 1 20080717 A 2611 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY FALSE ACTIVATION A REXA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SO 25 819AY 8617 8019 CARGO SMOKE WARNING IN FLIGHT, QRH FOLLOWED FIRE EXTINGUISHING SYSTEM ACTUATED. REMOVED AND REPLACED THE NR 2 CARGO SMO KE DETECTOR IAW BOMBARDIER AMM 26-10-00. (S) 2 L 7 2 4F RT A21EA 20080813 SO 2008 8 13 RAIA00807012 1 20080714 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHT UNSECURE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 804HK 145082 PRE FLT 3507-RIC-RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR AT THE INVERTER. SY STEM OPS CHECKED GOOD. (S) 2 L 7 2 4F RT T00011AT 20080813 SO 2008 8 13 C2XA08ON157 1 20080715 A 3350 20131A BATTERY EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12201 6188 3993 14500959 FLT 7751 - LAX - FLIGHT CREW REPORTED EXIT LIGHT CEILING SIGN AT ROW 12 INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED EXIT LIGHT CEILING SIGN EMERGENCY BATTERY NR 4. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RE TURN FOR SERVICE. (S) 2 L 7 2 4F RT 20080813 SO 2008 8 13 C2XA08SH096 1 20080719 A 5755 14569009406 BRACKET EMB 145 EMB145LR 3260212 SO RT WING SPOILER DAMAGED A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 16919 145393 RT WINGS GROUND SPOILER OUTBOARD ATTACHMENT POINT HAS A MIGRATING HAT BUSHING. MX REMOVED AND REPLACED RT WING`S GROUND SPOILER OUTBOARD ATTACHMENT POINT IAW AMM 57-51-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080813 CE 2008 8 13 GUU2008F00027 1 20080724 A 3243 9038000133 MASTER CYLINDER BEECH 1900 1900D 1154162 CE BRAKES BYPASSING A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 17 190YV UE190 FLIGHT 9282 EYW/TPA DURING TAXI CAPTAIN`S LT BRAKE PEDAL WENT TO THE FLOOR. REPLACED CAPTAIN`S LT BRAKE PEDAL MASTER CY LINDER. (S) 2 L 7 2 4T RT A24CE 20080813 NE 2008 8 13 WRLA2008069 2 20080716 A 7311 16622000 FUEL/OIL COOLER DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 3 ENGINE CRACKED A WRLA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 11 275WA 48631 PRECAUTIONARY SHUT DOWN OF NR 3 ENG DUE TO OIL QUANTITY IN THE RESERVOIR, 2 QUARTS, BOXED IN YELLOW ON SHUT DOWN. OIL T EMP 105C OIL PRESSURE 148 PSID AT FL 280 THROTTLE IDLE, N2 69.3. RAN ENG AND FOUND LEAK AT EXISTING WELD ON FUEL/OIL CO OLER. REMOVED AND REPLACED COOLER PER MM 79-21-01. OPS CHECK, NO LEAK NOTED. (S) 2 L 7 3 4F 4 F RT A22WE E24NE 20080813 NM 2008 8 13 UIEA200800270 1 20080726 A 7797 9037M17P04 WIRE HARNESS BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE EGT DAMAGED A UIEA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 EA 15 506MC 21252 528412 NR 2 ENG SHUT DOWN IN FLIGHT DUE TO HIGH EGT INDICATION - EGT WAS READING 1047C FOR 70 SECONDS. FOUND EGT HARNESS DAMAG ED. REMOVED AND REPLACED HARNESS AND OPS CHECKED OK PER MM 77-21-01. (S) 2 L 7 4 4F 4 F RT A20WE E23EA 20080813 2008 8 13 RYN2008F00012 4 20080730 A 3442 RADAR BOEING 757 7572G5 1384912 NM WX SYSTEM FAILED A RYNA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 CE 07 929RD 23929 WEATHER RADAR FAILED, AIRPLANE DIVERTED. TROUBLESHOOTING AND PARTS SOURCING IN WORK. (S) 2 L 7 2 4F RT A2NM 20080813 CE 2008 8 13 GLB2008F00012 1 20080724 A 3297 G15G22 WIRE BEECH 1900 1900D 1154162 CE MLG CHAFED A GLBA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 NM 03 255GL UE255 ACFT 255GL - AIR RETURN - FLIGHT 5063 - PILOTS REPORTED GEAR WOULD NOT MOVE TO THE UP POSITION. TRIED J-HOOK A COUPLE O F TIMES AND IT WOULDN’T COME UP AT FIRST, THEN THE HANDLE MOVED UP BUT THE GEAR WOULDN’T COME UP. LANDING GEAR RELAY CI RCUIT BREAKER POPPED. PUSHED IN , GEAR CAME UP, THEN PUT BACK DOWN AND CIRCUIT BREAKER POPPED AGAIN. MX REMOVED, CLEAN ED AND RE-INSTALLED CONNECTOR TO RT MAIN GEAR ACTUATOR. PERFORMED 10 EXTENSION/RETRACTIONS GEAR CYCLES. ALL CHECKS GOO D IAW 1900D MM 32-30-00. INSPECTED WIRING BEHIND GEAR HANDLE AND ON AIRFRAME SIDE OF RT MAIN GEAR ACTUATOR, CONNECTOR. NO DISCREPANCIES NOTED. MX THEN FOUND AND REPAIRED CHAFED WIRE NRG15G22 AT APPROXIMATELY POSITION SEAT 3A IN SIDEWALL 2 L 7 2 4T RT A24CE 20080813 SO 2008 8 13 CHQ2008F00000 1 20080725 A 5610 163500116 WINDSHIELD EMB 135 EMB135KL 3260302 SO ALLSN AE3007 AE3007A 03030 GL COCKPIT CRACKED A CHQA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 11 376SK 3475 3475 145578 CAE311852 FLIGHT 5349, MSY TO STL. DURING CRUISE THE FLIGHT CREW REPORTED HEARING A LOUD BANG AND NOTICED THAT THE FIRST OFFICER’ S WINDSHIELD HAD CRACKED. THE FLIGHT THEN DIVERTED TO CGI WHERE THE ACFT LANDED WITHOUT INCIDENT. THE ACFT WAS THEN FE RRIED TO STL WHERE THE NR 2 WINDSHIELD WAS REPLACED. (S) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080813 SO 2008 8 13 CHQ2008F00001 1 20080725 A 3350 66367 LIGHT EMB 135 EMB135KL 3260302 SO ALLSN AE3007 AE3007A 03030 GL CABIN INOPERATIVE A CHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 382SK 145624 CAE312609 MAINTENANCE FOUND THE EMERGENCY PROXIMITY LIGHT FORWARD OF THE WING EXIT TO BE INOPERATIVE. THE EMERGENCY LIGHT STRIP W AS REPLACED AND THE EMERGENCY LIGHTS OPERATED NORMALLY. (S) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080813 SW 2008 8 13 WGEA2008000666 1 20080730 A 2621 FX002002 CARTRIDGE ECLIPS EA500 ECLIPSEEA500 3350000 SW LEFT ENGINE LEAKING A WGEA O OTHER O OTHER NR NOT REPORTED 1 EA 27 142DJ 208 208 000056 REMOVED AND REPLACED LT ENG CARTRIDGE WITH SERVICEABLE UNIT IAW EA500 AMM 26-20-10. CLEANED ENG AND ENG NACELLE PANELS IAW EA500 AMM 26-20-00. INSPECTED ENG COMPONENTS SUBJECTED TO AGENT FOR CORROSION IAW P&WC LMM 05-50-00. NO DEFECTS NO TED AT THIS TIME. (S) 1 L 7 2 4J RT A00002AC 20080813 WP 2008 8 13 WX0A070219 1 20080708 A 3350 AD4002 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 878GA 53487 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MX DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATI ON LIGHTING SYSTEM WOULD NOT TEST. MX PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATT ERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (S) 2 L 7 2 4F RT A6WE 20080813 NM 2008 8 13 WX0A070218 1 20080708 A 3350 AD4002 BATTERY DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 872GA 53295 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MX DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATI ON LIGHTING SYSTEM WOULD NOT TEST. MX PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATT ERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (S) 2 L 7 2 4F RT 20080813 WP 2008 8 13 WX0A070217 1 20080701 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 887GA 49932 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MX DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATI ON LIGHTING SYSTEM WOULD NOT TEST. MX PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATI SFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (S) 2 L 7 2 4F A6WE 20080813 WP 2008 8 13 WX0A070216 1 20080701 A 3350 60030451 POWER SUPPLY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 879GA 53486 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MX DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATI ON LIGHTING SYSTEM WOULD NOT TEST. MX PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATI SFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (S) 2 L 7 2 4F RT A6WE 20080813 EU 2008 8 13 08FDEA02953 1 20080717 A 5730 A57340085 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON LT WING TOP SKIN RIB 26-27 LT REPAIR PERFORMED BY BLEND OUT CORROSION, NDT FOR CORROSION FREE CONDITI ON IAW RAS/BAE/1007630/2008 ISS A, APPROVED BY EA 6-5720-123019. 2 L 7 2 4F RT A35EU 20080813 NM 2008 8 13 08FDEA02958 1 20080717 A 5312 656725010 BULKHEAD BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 CORROSION AT BS 1166 BULKHEAD RT SIDE "T" ANGLE (AT BOTTOM NUTPLATE AFT SIDE OF BULKHEAD). REPLACED T-CHORD AT AFT PIT BULKHEAD BS 1166 RBL 25 INCHES. REMOVED CORROSION AND FOUND NOT WITHIN ALLOWABLE LIMITS ORIG MATERIAL THICKNESS IS .063 , MATERIAL LOSS IS .038, AND REMAINING MATERIAL IS .025, REF SRM 51-10-1 PG 5. FABRICATED NEW T-CHORD, REF BOEING DWR 6 5-67250-10 SHEET 2/3. TREATED AND PRIMED NEW T-CHORD REF 51-10-2 PG 1-7 AND 25. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080813 EU 2008 8 13 08FDEA02889 1 20080715 A 5321 B5327047600600 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO FLOOR PANEL 242 RG IS CRACKED. FABRICATED A NEW FLOOR PANEL, POTTED EDGES, CURED, SANDED, POTTED INSERTS, AP PLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080813 NM 2008 8 13 08FDEA02916 1 20080716 A 5321 65489610 FLOOR PANEL BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 21449 MAIN DECK LAV FLOOR WEB PANEL, UPPER LWR SURFACES ARE CORRODED BS 304 - 340, RBL 40 - 60, WL 208. REMOVED CORROSION, OR IGINAL MATERIAL THICKNESS .042 INCH, REMAINING .035', REMOVED .007. FOUND TO BE OUT OF LIMITS REF DRM 53-10-1 PG 2, TO OL ID AAR 9800 CAL DUE 6-28-09. CUT DRAIN OPENINGS IN NEW PANEL, TREATED AND PRIMED, REF SRMM 51-10-2 PG 2, FED EX GMM 7-0-1001 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080813 NM 2008 8 13 08FDEA02917 1 20080716 A 5330 6554571 SKIN BOEING 727 727233 138408A NM BS 680-682 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 C1 PIT BILGE AREA-STR 28R STA 680 LEVELING COMPOUND BULGING WITH CORROSION ON SKIN. REMOVED DAMAGED COMPOUND. FOUND CO RROSION AT SKIN AND NDT FOR LIMITS ORIGINAL "T" .070 LOSS AT LOWEST POINT IS .034, REMAINING T IS .036 IS OUT OF LIMITS REF SRM 53-30-3. REMOVED DAMAGE AREA REF SRM 53-30-3 FIG 3A. FABRICATED AND VERIFIED REPAIR DOUBLER AS 2024-T3 .080 RE F SRM 53-30-2 FIG 3A (A17124/PO NR 1038533). TREATED AND PRIMED REF SRM 51-30-2 PG 7. INSTALLED REF SRM 53-30-3 FIG 3A . RESTORED COMPOUND REF MM 51-40-00-0. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080813 EU 2008 8 13 08FDEA02919 1 20080716 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND ELONGATED HOLES ON LT WING BOTTOM SKIN, RIB 8, IN AREA OF HYDRAULIC FITTINGS. REPAIR PERFORMED BY REAM UP THE H OLES AND INSTALL REPAIR BUSHES IAW DRAWING R571-50532, APPROVED BY EA 6-2910-120038. 2 L 7 2 4F RT A35EU 20080814 WP 2008 8 14 UPS08852665 1 20080611 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 520 LBL 60 WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, BS 520 LBL 60 MAIN CABIN SEAT TRACKS WORN. REMOVED AND REPLACED PLUG ON SEAT TRACK I.A.W. SRM 53-0 2-03 FIG 006. 2 L 7 4 4F RT 4A25 20080812 WP 2008 8 12 AALA200801543 1 20080606 A 2560 1001191 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 405A 49316 LGA - EMERGENCY FLASHLIGHT AT FIRST CLASS EXIT INOPERATIVE. REPLACED FLASHLIGHT AT FIRST CLASS EXIT. SYSTEM GROUND CHE CKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 NM 2008 8 12 AALA200801660 1 20080618 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 673AN 29423 DFW - EMERGENCY LIGHT AT FORWARD COACH CABIN INOPERATIVE. REPLACED BATTERY PACK AT STATION 690 FOR EMERGENCY LIGHT AT F ORWARD COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 NM 2008 8 12 AALA200801630 1 20080615 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 39G INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 39G. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080812 NE 2008 8 12 AALA200801585 2 20080611 A 7200 ENGINE BOEING 767 767223 1385123 NM GE CF6 CF680A 30025 NE NR 1 SHUTDOWN A AALA O OTHER Y ENGINE STOPPAGE DE DESCENT 1 SW 21 324AA 22325 580154 JFK INFLIGHT T20/11JUN. AT FLIGHT LEVEL 230 NR ONE ENGINE UNCOMMANDED SHUT DOWN. LANDED JFK WITHOUT INCIDENT. SINGLE ENGINE TIME 20 MINUTES. REPLACED NR ONE ENGINE ON 11JUN AT JFK. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F 4 F RT A1NM E13NE 20080812 NM 2008 8 12 AALA200801592 1 20080611 A 1100 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 676AN 29426 DFW - EMERGENCY LIGHT EXIT ARROW DECAL AT FORWARD SEAT 18A DAMAGED. REPLACED EXIT ARROW DECAL FOR EMERGENCY LIGHT AT FO RWARD SEAT 18A. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 NM 2008 8 12 AALA200801656 1 20080618 A 3350 LENS BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 673AN 29423 DFW - EMERGENCY LIGHT AT SEAT 31D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 31D. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080812 WP 2008 8 12 AALA200801788 1 20080707 A 3213 PISTON DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7540A 49994 DFW INFLIGHT T1347/07JUL. NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR PISTON AND ASSOCIATED SEALS. REPLACED UPPER AND LOWER SCISSOR LINKS. SERVICED STRUT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080812 EU 2008 8 12 AALA200801784 1 20080706 A 2810 ACTUATOR AIRBUS 300 A300B4605R 3930308 EU LT WING INOPERATIVE A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 70054 461 JFK INFLIGHT T837/06JUL, CREW REPORTED UNWANTED FUEL TRANSFER. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED L T WING OUTER TANK REFUEL AND DEFUEL VALVE ACTUATOR AND REFUEL DEFUEL VALVE CANNISTER. SYSTEM GROUND CHECKED NORMAL OPER ATION. (A) 2 L 7 2 4F RT A35EU 20080812 NM 2008 8 12 USAA920081398 1 20080719 A 2611 RA12800M0706 CONTROL UNIT AIRBUS A319 A319132 3930340 NM SMOKE DETECTION MALFUNCTIONED A USAA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 EA 19 837AW 10054 10054 2595 FLT 179 (ONT-LAS) FALSE FIRE WARNING-ON DESCENT INTO LAS, CREW REPORTED SMOKE/CARGO FAULT. AFTER FIRE SUPPRESSANT DISC HARGE, RECEIVED LAV/GALLEY DETECTION FAULT. MAINTENANCE REMOVED AND REPLACED THE SMOKE DETECTOR CONTROL UNIT, SMOKE DET ECTORS 3WH & 4WH AND FIRE EXTINGUISHER BOTTLE. OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F RT A28NM 20080812 NM 2008 8 12 USAA920081441 1 20080722 A 5347 D53112815202 SEAT TRACK AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803AW 0931 SAL-C7- MAJOR REPAIR- CORROSION ON SEAT TRACK AT FR16, BL-Y765. REPLACED SEAT TRACK AT FR16, BL-Y765 IAW A319 SRM 51-72 -11. (A) 2 L 7 2 4F RT A28NM 20080812 WP 2008 8 12 08FDEA02836 1 20080712 A 5420 AUB7063 WEB DOUG DC10 DC1010 3022110 WP NR 3 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 40061 46973 AFTER REMOVAL ACCESS PANEL ON PYLON NR 3 WITH OAN J/C 0600B430-1JR FOUND HORIZ WEB WITH CRACKS. REPAIRED CRACKS IAW SRM 54-00-01 FIG 2B SHT 2 & FIG 13 SHT 6 VOL I. 2 L 7 3 4F A22WE 20080812 NM 2008 8 12 USAA920081415 1 20080722 A 5330 6545774 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 451UW 24934 CLT - MAJOR REPAIR-C1 CHECK - CRACKED FUSELAGE SKIN AT BS 727F-BS 727G, S23L. REPAIRED FUSELAGE SKIN FUSELAGE SKIN AT B S 727G, S23L IAW B737 SRM 53-00-01 REPAIR 31 AND US AIRWAYS, EA 100575. (A) 2 L 7 2 4F RT A16WE 20080813 EU 2008 8 13 08FDEA02855 1 20080605 A 5313 A53986212 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 AFT CARGO COMPT, STRINGER 53 LT WITH CORROSION NEXT TO RIVETS BETWEEN FR 65 AND FR 66. STRINGER 53 LT WAS REPLACED AS P ER SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02687 1 20080703 A 5321 B5327047500400 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CARGO DECK FLOOR PANEL 232 XG HAS BALL BEARINGS STUCK AND PUNCTURES ON THE TOP SURFACE. REPAIRED DAMAGED AREA PER A300-600 SRM 53-10-20, FIG 201. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02868 1 20080701 A 5754 A5786452400200 BOLT AIRBUS 300 A300F4605R 3930327 EU SLAT TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 NR 4 GUIDE TRACK LOWER KNUCKLE BOLT (NR 10) IS CRACKED AT THE HEAD END. THE ECCENTRIC BOLT WASHER IS GROOVED. REMOVE D DAMAGED LOWER BOLT AND REPLACED WITH NEW. REMOVED DAMAGED WASHER AND REPLACED WITH NEW IAW A300-600 AMM 27-80-12-4. TORQUE WRENCH T8342M. 2 L 7 2 4F RT A35EU 20080813 NM 2008 8 13 08FDEA02845 1 20080712 A 5713 65185702 STRINGER BOEING 727 727232 1384082 NM RWS 656 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 497FE 20866 RT WING, STR 10 CRACKED AT WS 656.5, ITEM IS AD DRIVEN, IF CRACKS EXCEED LIMITS IN SECTION II, FIG 12, CONTACT FED EX ST RUCTURES ENGINEERING FOR REPAIR INSTRUCTIONS PER WORK CARD E7-5710-7-4322. STOP DRILLED CRACK, VERIFIED CRACK TERMINATI ON AT STOP DRILL, LOCATED AND DRILLED REPAIR ANGLES AND RADIUS FILLERS AND INSTALLED ALL REPAIR PARTS. REF EO NR 7-5710 -7-4322/FIG NR 18. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080813 WP 2008 8 13 NWAA082719863 1 20080612 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 772NC 47774 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN LIGHT PACK FOR THE FWD RT OVERWING HATCH WAS BROKEN. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (A) 2 L 7 2 4F RT A6WE 20080813 WP 2008 8 13 NWAA08249927 1 20080529 A 5310 STRUCTURE DOUG DC9 DC931 3022065 WP FUSELAGE LEAKING A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 8920E 45835 AT FL 310 RED "CABIN PRESS" WARNING LIGHT ILLUMINATED. BOTH ENGINE AND AIRFOIL ICE PROTECTION SYSTEMS OPERATING. COM P ROCEDURES TO REGAIN CONTROL OF CABIN PRESSURE COMPLETED BUT CABIN STILL CONTINUED TO CLIMB AT AN INCREASING RATE. DECLA RED AN EMERGENCY AND INITIATED AN EMERGENCY DESCENT TO 10,000 FT. CABIN PRESSURIZATION STARTED FOLLOWING PRESSURE CONTR OLLER COMMANDS AT ABOUT 3.5 PSI DURING DESCENT. NO MENTION OF MASK DEPLOYMENT AND ACFT LANDED SAFELY AT STL. MX DID BI TE CHECK BOTH PRESSURE CONTROLLERS AND NO EXISTING FAULTS SHOWED. TAIL COMPARTMENT INSPECTED FOR LOOSE OR BLOWN DUCTING WITH BOTH APU AND EACH PACK INDIVIDUALLY. NO LEAKS FOUND AND VESSEL PRESSURIZED NORMALLY ON GROUND. FURTHER MX FOUND 2 L 7 2 4F A6WE 20080814 NM 2008 8 14 USAASB08058 1 20080803 A 3350 20131ASMI BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 532AU 24479 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 12 THRU 16, LT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A16WE 20080814 NM 2008 8 14 UPS08M52650 1 20080620 A 5740 FITTING DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 271UP 48572 INSPECTION TYPE-C, LT WING LOWER WINGLET AFT FITTING FOUND CRACKED DURING BOROSCOPE INSPECTION. LT WING WINGLET FWD FIT TING REMOVED IAW SRM 51-31-01 V.2R.40 & EOMD 11-57-20-27 680 APP.D. NEW FWD & AFT FITTINGS HOLES PICKED UP IAW SRM 51-31 -01V.2 & EO MD11-5720-27680 APP D. NEW NUTPLATES INSTALLED ON FWD & AFT FITTINGS IAW SRM 51-31-01V.2R 40 & EOMD 11-5720 -27680 APP D. OK TO INSTALL NEW FWD & AFT FITTING ON LT WING WINGLET. 2 L 7 3 4F RT A22WE 20080814 WP 2008 8 14 IXX2008F00043 1 20080612 A 5313 LONGERON DOUG DC8 DC872F 302199E WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT LONGERON-36 CORRODED AT STATION 1320.000-1340.000. REMOV ED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEED TO PERFORM REPAIR. REMOVED DAMAGED LONGERON SEGMENT. FA BRICATED SPLICE OF EXTRUSION. CLEANED, TREATED AND PRIMED AREA AND SPLICE. INSTALLED NEW FASTENERS AND LONGERON SEGMEN T IAW DC8 SRM 53-2-2 PAGE 6 FIGURE 41, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 53-2-2 FIGURE 10 SHEE T 2, SRM 53-2-2 FIG 10 SHEET 4 TR 53-193 DATED 03/15/04, DC8 SRM 51-1-8B, SRM 51-2-0 FIGURE 52 SHEET 1, SRM 51-2-0 FIGUR E 50 SHEET 65, SRM 53-4-1 FIGURE 44B SHEET 2 ITEM "L", SRM 51-1-20D, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 EA 2008 8 14 TRAX200800932 1 20080725 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 926EV 7843 PAX DOOR AFT DRAG ANGLE IS CRACKED IN PREVIOUS REPAIR SPLICE. COMPLIED WITH REO 601R-52-11-513 AND ASA ECTC 601R-52-11- 513. SUPPLEMENTAL SDR CLOSED 7/31/08. (A) 2 L 7 2 4F RT A21EA 20080814 NM 2008 8 14 UPS08552797 1 20080719 A 3350 LIGHT BOEING 757 75724APF 1384969 NM EMERGENCY EXIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 445UP 27390 2 LAMPS INOP IN EMERGENCY EXIT LIGHT ABOVE ENTRY DOOR. RELAMPED - OPS CHECKED GOOD. 2 L 7 2 4F RT A2NM 20080814 WP 2008 8 14 UPS08852789 1 20080701 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 418 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, GOUGED ON THE BS 418 LT FRAME STRAP ABOVE THE UPPER SURFACE OF CUSP EXTRUSION IN MAIN CABIN. REMOVE D AND REPLACED FRAME STRAP IAW SRM, 51-1-20D, 51-1-8. 2 L 7 4 4F RT 4A25 20080814 NM 2008 8 14 UPS08M52734 1 20080430 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, LT WING FUEL TANK UPPER STRINGER NR14 END SUSPECT CRACK. HFEC C/OUT & FOUND CRACK 11.5" APPROX. DAMAGED PORTION LT WING FUEL TANK UPP STRINGER NR 14 TRIMMED OFF IAW EN NR 1189-08. HFEC CUTOUT FOUND NO CRACK EVIDENT. NEW REPAIR STRINGER & REPAIR PARTS FAB IAW EN NR1189- 08. FPI C/OUT ON FAB PARTS & FOUND NO CRACK EVIDENT. CAP SEALIN G CUTOUT ON NEW INSTALLED IAW SRM 51-41-01 VOL II REV35. 2 L 7 3 4F RT A22WE 20080814 NM 2008 8 14 UPS08M52735 1 20080430 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT WING FUEL TANK UPPER STRINGER NR 13 END SUSPECT CRACK. HFEC INSPECTED CUTOUT & FOUND CRACK APPR OX 10". DAMAGED PORTION RT WING FUEL TANK UPPER STRINGER NR 13 AREA TRIMMED OFF PER EN NR1189-08. HFEC CUTOUT ON TRIM MED EDGE & FOUND NO CRACK EVIDENT. NEW REPAIR STRINGER & 3 REPAIR STRAPS FAB IAW EN NR 1189-08. FPI CUTOUT ON FAB REP AIR FOUND NO CRACK EVIDENT. CAP SEALING CUTOUT ON NEW INSTALLED FASTENER IAW SRM. 2 L 7 3 4F RT A22WE 20080814 WP 2008 8 14 UPS08852730 1 20080701 A 5310 TORQUE BOX DOUG DC8 DC871F 302199D WP STA 1660 L-19R DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, MAIN CABIN, RT AFT SERVICE DOOR FRAME (TORQUE BOX) WEB HAS DOUBLE DRILLED AND EXTRA HOLES STA 1660 L-19R. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-02-00-0 FIG 001D, 5 1-01-21. 2 L 7 4 4F RT 4A25 20080814 NM 2008 8 14 KCS2008F00006 1 20080727 A 2612 FIRE LOOP BOEING 747 7472B4B 138481B NM PWA JT9 JT9D7J 52054 NE NR 4 ENGINE MALFUNCTIONED A KCSA J DUMP FUEL N FALSE WARNING NR NOT REPORTED 1 GL 23 710CK 21097 701672 FIRE FAULT INDICATED ON P2 PANEL AFTER FLAPS UP. B-LOOP INDICATION ON NR 4 ENG TEMP OFF SCALE HIGH (NACELLE). FOLLOWED AOM PROCEDURE FOR ENG FIRE. VISUALLY CHECKED FOR INDICATION OF FIRE. NONE NOTED. NO RESTART ATTEMPTS. JETTISONED FU EL AND LANDED. (S) 2 L 7 4 4F 4 F RT A20WE E20EA 20080814 NM 2008 8 14 USA2008F00013 1 20080726 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 322AW 25400 PHX - MAINTENANCE REPORTED THE FORWARD FLIGHT ATTENDANT STATION FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE FLASHLIGHT BATTERY. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A16WE 20080814 NM 2008 8 14 USA2008F00015 1 20080723 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 438US 24560 CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT OVER THE FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE FORWARD GALLEY. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A16WE 20080814 NM 2008 8 14 USAA920081432 1 20080725 A 5315 D53472192200 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803AW 0931 SAL - C7 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR66 TO FR70, Y765. REPLACED FLOORBEAM AT FR66 TO FR70, Y765 IAW SR M A319 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080814 EU 2008 8 14 USAA920081435 1 20080729 A 3350 BATTERY PACK AIRBUS A319 A319112 3930323 EU CABIN MALFUNCTIONED A USAA K NONE O OTHER DE DESCENT 1 EA 19 747UW 1301 FLT 1137 PHL-DFW - EEL - FLIGHT ATTENDANT REPORTED THAT THE CABIN EMERGENCY LIGHTS WERE FLASHING ON AND OFF DURING DESCE NT AND LANDING. MAINTENANCE PERFORMED A BITE TEST WHICH FAULTED THE LT AND RT BATTERY PACKS. RESET BATTERY PACKS. OPE RATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4F RT A28NM 20080814 NE 2008 8 14 A6WA200840544 2 20080715 A 7297 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 1 ENGINE DAMAGED A A6WA E ENGINE SHUTDOWN X P ENGINE FLAMEOUT NO WARNING INDICATION AP APPROACH 1 GL 31 445AW 7804 ENG NR 1 SHUTDOWN IN FLIGHT, NO ASSOCIATED EICAS MESSAGES ILLUMINATED BEFORE SHUTDOWN. THRUST LEVERS WERE ABOVE IDLE AT APPROXIMATELY 80%. RAN QRH, TRIED TO RELIGHT. ENG RELIT FOR 15-20 SECONDS THEN GOT LOW OIL PRESSURE RED WARNING. DID PRECAUTIONARY SHUTDOWN. ENG WAS SHUTDOWN FOR APPROXIMATELY 15 MINUTES. REF W/O 127068 FOR WORK PERFORMED CLEANED BROW N HARNESS AND T2 SENSOR. R&R RT ENGINE BROWN HARNESS IAW AMM 73-21. OPS CHECK GOOD. REMOVED PLACARD & MEL. 2 L 7 2 4F 4 F RT A21EA E15NE 20080814 CE 2008 8 14 DXTA200803206 1 20080729 A 3240 UNKNOWN CESSNA 500 560CESSNA 2076750 CE BRAKE SYSTEM MALFUNCTIONED E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 326QS 5600526 EXCESSIVE AMOUNT OF BRAKE PEDAL APPLICATION IS NEEDED TO STOP AIRPLANE. (S) 2 L 7 2 4F RT A22CE 20080814 CE 2008 8 14 DXTA200803205 1 20080729 A 2740 WARNING SYSTEM CESSNA 680 680CE 2076811 CE COCKPIT ACTIVATED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 381QS 6800097 AFTER TAKEOFF INFLIGHT ANYTIME PITCH TRIM IS ACTIVATED EITHER NOSE UP OR DOWN, AMBER "AP STAB TRIM INOP" & AMBER "PRIMAR Y STAB TRIM FAIL" & CYAN "AP FAIL A & B" CAS MESSAGES DISPLAYED. (S) 2 L 7 2 4F RC T00012WI 20080814 WP 2008 8 14 UPS08852753 1 20080630 A 5322 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 1800 L3L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, LARGE SHEER TIE BRACKET CRACKED AT LT END, 60 COMPARTMENT CEILING STA, 1800,L3L. REMOVED AND REPLA CED SHEER TIE IAW SRM 51-1-8, 53-2-0 FIG F ,51-1-20D. 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 UPS08852755 1 20080626 A 5740 ATTACH BRACKET DOUG DC8 DC871F 302199D WP RT WING GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, RT WING REAR SPAR AT IB HINGE OF NR4 SPOILER PARTITION RIB ATTACH BRACKET GOUGED AND BENT. REMOVED AND REPLACED GUSSET IAW SRM, 51-1-21,57-2-0, 51-1-8. 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 UPS08852756 1 20080709 A 5320 WEB DOUG DC8 DC871F 302199D WP RT MLG WW DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, RT MLG DOOR SWITCH STA 896.500 HAS 1 EACH ELONGATED HOLE AT SUPPORTING WEB. FABBED AND INSTALLED RE PAIR DOUBLERS IAW SRM 51-9-0,EO-DC8-3260-16914- A. 2 L 7 4 4F RT 4A25 20080814 EU 2008 8 14 08FDEA02997 1 20080721 A 5530 A5537214021600 SUPPORT ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 VERTICAL STABILIZER RIGHT TRAILING EDGE SUPPORT IS CRACKED BELOW THE NR 2 RUDDER HINGE FITTING. REMOVED DAMAGE IAW SRM 51-70-10, REPAIR I. FABRICATED A REPAIR ANGLE AND FILLER IAW SRM 51-70-10, REPAIR I. ALODINED AREA AND REPAIR PARTS IA W SRM 51-21-10. PRIMED AND PAINTED AREA AND REPAIR PARTS IAW SRM 51-23-10. INSTALLED REPAIR IAW SRM 51-70-10, REPAIR I AND SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080814 SO 2008 8 14 C2X2008F00015 1 20080729 A 5751 145690094095 BRACKET EMB 145 EMB145XR 3260214 SO LT AILERON GOUGED A C2XA K NONE O OTHER CR CRUISE 1 SW 27 14204 4745 4745 14500968 ACFT IS CURRENTLY IN A C-CHECK STATUS AND THE LT AILERON TO PCA ATTACHMENT POINT O/B LUG HAT BUSHION WAS FOUND MIGRATED. MAINTENANCE REMOVED AND REPLACED THE BRACKET AND REINSTALLED THE AILERON. OPS CHECKS GOOD IAW EMB 145XR EC 5750-01177 . ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. (S) 2 L 7 2 4F RT 20080814 CE 2008 8 14 7282008N430CS 1 20080725 A 2731 S37792H38214 CONTROL CABLE CESSNA 525 525 2076601 CE ELEVATOR TRIM CHAFED E Z5FA K NONE O OTHER NR NOT REPORTED 1 EA 63 430CS 854 525B0185 ELEVATOR TRIM CABLE CHAFED ON PULLEY BRACKET P/N 6361210-1 IN VERTICAL STABILIZER. ENGINEERING ORDER WRITTEN TO ADD FAI RLEADS TO PREVENT FURTHER CHAFING. (S) 1 L 7 2 4F RT A1WI 20080814 EU 2008 8 14 08FDEA03047 1 20080724 A 5347 A53611640200 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 455FE 331 MAIN DECK FLOOR LEVEL COURIER COMPT TRACK BETWEEN FR 15A - FR 16A Y950 WITH EXFOLIATION CORROSION. REPLACED THE SEAT TRACK PER SRM 51-75-10. 2 L 7 2 4F RT A35EU 20080814 EU 2008 8 14 MAL2008F00012 1 20080723 A 5220 SKIN SAAB SF340 340B 7860101 EU ESCAPE HATCH DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 DENT NOTED ON FWD LT CORNER OUTER SKIN OF CREW ESCAPE HATCH. REPAIRED IAW EONRS52028. (S) 2 L 7 2 4T RT A52EU 20080814 EU 2008 8 14 MAL2008F00013 1 20080723 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 UPPER FLANGE ON BOTTOM FUSELAGE FRAME STA 294, RBL 18.38. REPAIRED IAW EONRS53108. (S) 2 L 7 2 4T RT A52EU 20080814 EU 2008 8 14 MAL2008F00014 1 20080723 A 5753 STRUCTURE SAAB SF340 340B 7860101 EU T/E FLAP DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 FLAP FAIRING AFT BULKHEAD UPPER FLANGE TO REAR SPAR FASTENERS. REPLACED IAW EOS57051. (S) 2 L 7 2 4T RT A52EU 20080814 WP 2008 8 14 IXX2008F00029 1 20080617 A 5730 SKIN DOUG DC8 DC872F 302199E WP LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND LT WING CRACKED ON LEADING EDGE UPPER SKIN AT STATION XCW 69.500. REMOVED FAST ENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION, FABRICATED DOUBLER, FILLER PLUG. PERFORMED HEAT TREATMENT, CLEANED TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTE NERS AND REPAIR PARTS IAW DC8 SRM 57-2-1 FIGURE 20 SHEETS 1,2,3 DC8 SRM 51-1-20D, DCA SRM 57-2-1 FIGURE 20 SHEET 1, DC8 SRM 51-1-12 FIGURE 7, DC8 NDT SPM PART 06-10-01-001, SRM 57-3-2 FIGURE 15 ITEM "J", SRM 51-10-0 FIGURE 21, DC8 SRM 51-1- 1 PAGES 1,13 AND 17, DC8 SRM 51-1-8, AND SRM 51-1-11. (S) 2 L 7 4 4F RT 4A25 20080814 NM 2008 8 14 08FDEA02922 1 20080716 A 5753 SKIN BOEING 727 727233 138408A NM LT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 21449 LEFT WING INBD AFT FLAP, 3RD ATTACH FITTING OUTBD SKIN CRACKED FABRICATED REPAIR PARTS AT LEFT WING T/E AFT FLAP, THIRD ATTACH FITTING O/B SKIN, REF 27-50-4 FIG 11. TREATED, PRIMED AND INSTALLED, REF SRM 51-20-2 PG 1-7, 57-50-04 FIG 11, 51-30-2 PG 2-4. PAINTED REPAIR AREA REF MM 51-20-151-1, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080814 WP 2008 8 14 IXX2008F00038 1 20080612 A 5711 STIFFENER DOUG DC8 DC872F 302199E WP RT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND RT WING AUXILIARY SPARS STIFFENER CORRODED AT STATION XW 33.000. REMOVED CORRO SION. FOUND OUT OF LIMITS. REMOVED CORRODED STIFFENER. FABRICATED STIFFENER. CLEANED, TREATED AND PRIMED AREA AND ST IFFENER. INSTALLED STIFFENER IAW DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 57-2-0 PAGE 16, DC8 SRM 51-1-21, SRM 51-1-20D, DC8 SRM 57-2-0 PAGE 1, DC8 SRM 51-1-8B, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 IXX2008F00040 1 20080611 A 5320 FITTING DOUG DC8 DC872F 302199E WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROURTINE C CHECK INSPECTION, FOUND AFT FUSELAGE SPLICE FITTING CRACKED AT STATION FS 1610.000 LONGERON 17RIGHT. REMOVED CRACKED SPLICE FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-21, SR M 51-1-20D, DC8 SRM 51-1-8B, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 IXX2008F00048 1 20080613 A 5753 SKIN DOUG DC8 DC872F 302199E WP T/E FLAP MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP UPPER PANEL HAS IMPROPER REPAIR AND DENTS AT STATION XW 30 00 TO STATION XW 92.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, AND BONDED DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 1 PAGE 2, DC8 SRM 57-1-0 PAGE 1, SRM 51-3-0, SRM 51-1-21, DC8 SRM 57-7-1 FIG 1 ITEM "A", DC8 SRM 51-1-9 TR 51-142, SRM 51-1-9A TR 51-141, DC8 SRM 51-1-8B, DC8 SRM 51-1-1, SRM 51-3-0, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 IXX2008F00049 1 20080616 A 5720 STIFFENER DOUG DC8 DC872F 302199E WP RT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND RT WING TRAILING EDGE STIFFENER CRACKED AT STATION XW 19.000. REMOVED CRACKED STIFFENER. FABRICATED STIFFENER. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND STIFFENER. INSTALLED STIFFENER IAW DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATION 2003-05, ED SEMAN 4816 DATED 07 /14/2008, DACO DPS 4.707, DC8 SRM 51-1-8B, DC8 SRM 51-1-21, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 IXX2008F00050 1 20080620 A 5320 FITTING DOUG DC8 DC872F 302199E WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FRAME CLIP CRACK AT STATION XF 350.000 LONGERON 21. REM OVED CRACKED FRAME CLIP. FABRICATED FRAME CLIP. PERFORMED HEAT TREATMENT. PERFORMED NDT INSPECTION, NO CRACK NO CORR OSION. CLEANED, TREATED AND PRIMED AREA AND FRAME CLIP. INSTALLED FRAME CLIP DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATI ON 2003-05 AND SEMAN ED 4814, DC8 SRM 51-1-1 PAGE 1,13,17, DACO DPS 4.707, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-1-20 D AND 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 IXX2008F00051 1 20080614 A 5753 SKIN DOUG DC8 DC872F 302199E WP T/E FLAP WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND LT OUTBOARD FLAP SKIN ON EXHAUST GATE WORN AT STATION XF 250.000. REMOVED FAST ENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AAND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 4 TR 57-94 DATED 10-01-02, DC8 SRM 57 -1-0 PAGE 1, SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 4 ITEM "C" TR 57-94, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND SRM 51-1-21. (S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 IXX2008F00052 1 20080616 A 5730 SKIN DOUG DC8 DC872F 302199E WP RT WING MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND RT WING CENTER LEADING EDGE UPPER SKIN HAS IMPROPER REPAIR AT STATION 285.250. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTI ON. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, FILLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PAR TS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 08379 DATED 07/11/08, SEMAN DRAWING ED48-10 DATED 06/2 4/08, DC8 SRM 51-1-8B, DC8 SRM 51-1-21, SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-11, SRM 51-3-0, SRM 51-1 -20D, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 NM 2008 8 14 08FDEA03055 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL TANK ACCESS CUTOUT 641JB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS C LASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080814 NM 2008 8 14 08FDEA03057 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL TANK ACCESS CUTOUT 641LB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS C LASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080814 NM 2008 8 14 08FDEA02926 1 20080716 A 5320 6517593153 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 FLOORBOARD, FWD LAV SUPPORT NUT PLATES RUSTED STA 305 - RBL 44. REMOVED FLOOR SUPORT ANGLE, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. ORIG. MATERIAL THICKNESS .040 INCH. REMAINING .031 INCH REMOVED .009'. FABRICATED NEW ANGLE, PEN ATRANT INSP FOR CRACKS. NO DEFECTS, TREATED AND PRIMED AND INSTALLED NEW ANGLE REF SRM 51-10-2 PG 2, SRM 51-30-2, SRM 5 3-10-1 PG 2, TPPL ID AAR 9800 CAL DATED 6- 24-09, BOEING DWG 65-17593-153, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080814 NM 2008 8 14 08FDEA02927 1 20080716 A 5230 53FX1396101 DOOR BOEING 727 727233 138408A NM CARGO BAY GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 MAIN CARGO DOOR, AFT EDGE LOWER CORNER GOUGED LOWER AFT CORNER GOUGED BEYOND LIMIT. REMOVED DOUBLER FABRICATED NEW DOUB LER, TREATED AND PRIMED. INSTALLED NEW DOUBLER REF 727 P-FSRM 52-30-2 PG 1/2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080814 NM 2008 8 14 08FDEA03062 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL TANK ACCESS CUTOUT 642DB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS C LASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080814 NM 2008 8 14 08FDEA03063 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL TANK ACCESS CUTOUT 641DB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS C LASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080814 NM 2008 8 14 KCSA081366 1 20080803 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FUSELAGE SKIN CORRODED AT BS 1000, LBL 53, WL 91. (S) 2 L 7 4 4F RT A20WE 20080814 NM 2008 8 14 KCSA081367 1 20080803 A 5414 SKIN BOEING 747 747259B 1384804 NM NR 4 PYLON DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 NR 4 PYLON INBOARD LOWER SKIN DAMAGED AT NAC STA 215. (S) 2 L 7 4 4F RT A20WE 20080814 NM 2008 8 14 KCSA081369 1 20080804 A 5313 STRINGER BOEING 747 747122 1384872 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STR 38R DAMAGED AT BS 512. (S) 2 L 7 4 4F RT A20WE 20080814 NM 2008 8 14 KCSA081371 1 20080804 A 5330 SKIN BOEING 747 747122 1384872 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FUSELAGE SKIN CORRODED AT BS 1743, STR 40R. (S) 2 L 7 4 4F RT A20WE 20080814 EA 2008 8 14 TRAX200800942 1 20080728 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 GL 23 936EV 8038 FWD ASD ANCHOR FITTING CRACKED. REMOVED AND REPLACED FWD ASD ANCHOR FITTING. ALL WORK ACCOMPLISHED IAW SB 601R-52-093. OPS CHECK GOOD. TK 7025453. RII COMPLIED WITH SATISFACTORILY ON ADJUSTMENT AND RIG OF FWD ASD ANCHOR FITTING PER SP 607. (S) 2 L 7 2 4F RT A21EA 20080814 EA 2008 8 14 TRAX200800944 1 20080729 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 GL 23 880AS 7606 PAX DOOR HARD TO OPEN. OPERATED DOOR FROM OUTSIDE AND INSIDE. NO DEFECTS NOTED. ACFT OK FOR CONTINUED SERVICE. (S) 2 L 7 2 4F RT A21EA 20080812 WP 2008 8 12 08FDEA02831 1 20080711 A 5730 ARB220875 SKIN DOUG MD10 MD1010F 3022112 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 LEFT WING TIP T/E AREA EXTERNAL SKIN IS CRACKED. REMOVED DAMAGED AREA PER DC/MD-10 SRM 57-00-01;VOL I. FABRICATED A DO UBLER REPAIR PER DC/MD-10 SRM 57-00-01; VOL I. ALODINED AND PRIMED DOUBLER REPAIR PER DC/MD-10 SRM 51-21-01; VOL II. INSTALLED DOUBLER REPAIR PER DC/MD-10 SRM 51-35-01; VOL II AND DC/MD-10 SRM 57-00-01; VOL I; SHEET 2; FIG 4. 2 L 7 3 4F RT A22WE 20080812 NM 2008 8 12 08FDEA02838 1 20080712 A 5720 6516200306 CHANNEL BOEING 727 727225 1384077 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 GENERATED BY EO NR 7-5710-7-4322 RT WING, STA 686.5 WEB FWD ATTACH "Z" CHANNEL CRACKED, OUTBD. REMOVED DAMAGED "Z" CHAN NEL, LOCATED AND DRILLED NEW "Z" CHANNEL AND INSTALLED. REFERENCE SRM 51-30-2. CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080812 EU 2008 8 12 USAA920081422 1 20080726 A 5720 57252920200 ANCHOR FITTING AIRBUS 320 A320231 3930325 EU RT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 627AW 66 SAL-C6- MAJOR REPAIR- CORROSION ON ANCHORAGE FITTING RT WING. REPAIRED ANCHORAGE FITTING RT WING IAW US AIRWAYS EA 1320 38. (A) 2 L 7 2 4F RT A28NM 20080813 EU 2008 8 13 08FDEA02886 1 20080715 A 5340 A53974369005 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CONNECTING FITTINGS AT C 63 WITH CORROSION OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10 . 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02887 1 20080715 A 5210 A52175325301 FRAME AIRBUS 300 A300B4622R 3930312 EU PAX DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND ON RT AFT PAX DOOR FRAME SEGMENT UNDER BEAM 8 BROKEN REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02891 1 20080715 A 5315 A53974268200 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION SPOTS ON CROSSBEAM C 56 AND C 58 SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02896 1 20080715 A 5313 A53980877200 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION AT STRINGER P 56 LT, C 76-77 OUT OF LIMIT. REPAIR PERFORMED BY CUT OUT OF CORRODED FLANGE AND INSTALLIN G REINFORCEMENT PROFILE IAW RAS/EFW/9000063/2008 ISS A, APPROVED BY EA 6-5318-120098. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02899 1 20080715 A 5230 A52374160208 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION AT AFT CARGO DOOR C 59-63A, INNER SKIN PANEL (NEAR LONGERON 5) OUT OF LIMIT. REPAIR PERFORMED BY SMOOTH BLEND OUT OF CORROSION, NDT FOR CRACK FREE CONDITION AND FLAP PEENING IAW RAS/DAHAM/4025300/2008 ISS A, APPROVED BY EA 6-5232-123025. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02678 1 20080703 A 5321 B5327048401400 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CARGO DECK FLOOR PANEL NR 232 VH HAS BALL BEARINGS (2 PLACES) STUCK IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PAN EL IN REF TO A300-600 SRM 53-10-20, FIG 202. 2 L 7 2 4F RT A35EU 20080813 NM 2008 8 13 08FDEA01966 1 20080522 A 5100 NONE BOEING 757 75723A 1384967 NM IAW SRM NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 919FD 24636 EXTERNAL PATCH REPAIR ON AFT CARGO DOOR LOWER CENTER EDGE BEAM TO BE EVALUATED. EXISTING REPAIR FOUND PREVIOUSLY ACCO MPLISHED IAW B757-200 SRM 52-30-01 FIG 205. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080813 EU 2008 8 13 08FDEA02870 1 20080714 A 5754 A5786452400200 BOLT AIRBUS 300 A300F4605R 3930327 EU SLAT TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 RIGHT WING NR 2 SLAT, NR 5 TRACK LOWER BOLT IS CRACKED. REMOVED AND REPLACED BOLT ON THE RIGHT WING NR 2 SLAT, NR 5 TRA CK IAW FEDEX A300-600 AMM 27-80-12-4. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02872 1 20080714 A 5754 A5786452400200 BOLT AIRBUS 300 A300F4605R 3930327 EU SLAT TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 LEFT WING NR 1 SLAT, NR 2 TRACK LOWER BOLT IS CRACKED. REMOVED AND REPLACED IAW A300-600 AMM 27-80-12-4. 2 L 7 2 4F RT A35EU 20080813 NM 2008 8 13 NWAA082523160 1 20080605 A 3397 WIRE AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHT DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 360NB 01959 DURING LINE CHECK DISCOVERED ROW 1, 2, 5, 6 EMERGENCY EGRESS LIGHTS INOP. REPAIRED 2 WIRES BELOW SEAT 1 & 2 REPLACED EP SU (10WL), CHECKS NORMAL. (A) 2 L 7 2 4F RT A28NM 20080813 NM 2008 8 13 NWAA082586623 1 20080608 A 3350 BATTERY BOEING 747 747251B 1384892 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 623US 21705 DURING OVERNIGHT CHECK FOUND UPPER DECK FLOOR TRACK LIGHTING AND ZONE-B FLOOR TRACK LIGHTING INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 4 4F RT A20WE 20080813 NM 2008 8 13 NWAA082795637 1 20080604 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 537US 26484 DURING AN A-CHECK THE OVERWING EXIT SIGN AT 22 DEF WAS INOPERATIVE. RELAMPING THE EMERGENCY EXIT SIGN DID NOT CORRECT T HE DISCREPANCY. MAINTENANCE REPLACED THE CORRESPONDING BATTERY PACK, ALL OPERATIONS CHECKED GOOD. (A) 2 L 7 2 4F RT A2NM 20080813 WP 2008 8 13 NWAA083099975 1 20080712 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9339 47382 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 18-21 OF THE CABIN WERE INOPERATIVE. M AINTENANCE REPLACED THE ASSOCIATED FUSE AND THE BATTERY PACK. OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F A6WE 20080813 NM 2008 8 13 NWAA083403164 1 20080716 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 364NB 19711 11500 02002 DURING EMERGENCY LIGHT CHECK, RECEIVED EPSU EXIT LOAD EMER R FAULT MESSAGE. REPLACED RIGHT POWER SUPPLY, CHECKS GOOD. (A) 2 L 7 2 4F RT A28NM 20080813 WP 2008 8 13 NWAA083439884 1 20080726 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 677MC 47756 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 9-13 OF THE CABIN WERE INOPERATIVE. MA INTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (A) 2 L 7 2 4F RT A6WE 20080813 EU 2008 8 13 08FDEA02906 1 20080715 A 2910 571191 PTU AIRBUS 310 A310222 3930315 EU HYD SYSTEM LEAKING A FDEA A UNSCHED LANDING K S J FLUID LOSS AFFECT SYSTEMS WARNING INDICATION CR CRUISE 1 CE 21 450FE 3484 3484 162 WHILE ENROUTE AT FL370 GOT ECAM WARNING FOR GREEN HYD RESV LOW RESV QUANTITY ON ECAM WAS IN THE RED. PRESSURE INDICATED ZERO. DIVERTED TO KPHX. GEAR EXTENDED BY GRAVITY. REMOVED AND REPLACED GREEN YELLOW POWER TRANSFER UNIT PER MM 29-23 -11-4. REQUIRES BLEEDING, OPS AND LK CHECK PER STEP D.10. REMOVED AND REPLACED NR 1 ENG GREEN SYSTEM HYDRAULIC PUMP PE R M/M 29-11-32-4 AND PUMP CASE DRAIN FILTER PER M/M 29-11-36-4 LEAK AND OP'S CHECK GOOD. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02907 1 20080716 A 5320 A53973085210 SILL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON SILL BEAM IN AFT CARGO COMPARTMENT, C 59-63A REPAIR PERFORMED BY UPPER FLANGE REPLACEMENT WITH SMALL DEVIATIONS IAW RAS/EFW/9000066/2008 ISS A, APPROVED BY EA 6-5317-123013. 2 L 7 2 4F RT A35EU 20080813 EU 2008 8 13 08FDEA02909 1 20080716 A 5754 A53710007207 DOUBLER AIRBUS 300 A300B4622R 3930312 EU KRUEGER FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON KRUEGER FLAP DOUBLER AT C 38, P 28-33 RT REPAIR PERFORMED BY CORROSION REMOVAL, NDT FOR CORROSION FRE E CONDITION AND FLAP PEENING IAW RAS/EFW/9000060/2008 ISS A, APPROVED BY EA 6-5314-120076. 2 L 7 2 4F RT A35EU 20080814 NM 2008 8 14 UPS08M52641 1 20080613 A 5710 STRUCTURE DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 271UP 48572 INSPECTION TYPE-C, RT WING ANTI-ICE TELESCOPIC DUCT, L/E CUT OUT AREA SUSPECT CRACK AT IB AND OB SIDE AS MARKED. HFEC I NSP CARRIED OUT IAW DAC NDT SPM R.13,06-10-01.001 & FOUND CRACK AS MARKED. FASTENERS AT CRACKED AREA REMOVED IAW SRM57-3 1-01V.2 & SRM 57-33-01 V.2R.40. CRACKED AREA TRIMMED OUT IAW SRM 57-10-00 FIG.43V.1R.40. REP DOUBLER & FILLER FAB IAW SR M 57-10-00 FIG.43 V.1R.40. REP DOUBLER HEAT TREAT TO T62 IAW DPS 7.00-1, HARDNESS 83.83 FOUND WITHIN LIMIT IAW DPS 1.05 . 2 L 7 3 4F RT A22WE 20080814 NM 2008 8 14 UPS08M52651 1 20080613 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 271UP 48572 INSPECTION TYPE-C, RT WING NR 3 FUEL TANK STRINGER NR 11 END SUSPECT CRACK AS MARKED. STR 11 SECTION CUT IAW SRM 57-20 -00 FIG.10V.1R.40 & EN1277-08. HFEC C/OUT IAW NDT SPM R.13 PART 06-10-01.001 ON TRIMMED EDGE & FOUND NO CRACK EVIDENT. NEW STRINGER & REP PARTS FAB IAW SRM 57-20-00 FIG.10 V.1R.40. HOLES ON NEW STR 11 & REP PARTS P/UP IAW EN1277-08. NEW STR 11 & REP PARTS, CLIP & REP AREA FASTENERS OK TO INSTALL. 2 L 7 3 4F RT A22WE 20080814 NM 2008 8 14 UPS08M52670 1 20080326 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE-C, RT WING OB FLAP IB HINGE (FLAP MOUNTED) UPPER MOUNTING POINT FWD OB NR 2 BORE HOLE FOUND CORRODED AS MARKED. CORRODED IN AFFECTED AREA REMOVED. ORG DIA 0.599", FINAL DIA 0.6725". FPI C/O ON REWORK AREA & FOUND NO CORROS ION EVDNT. BORE FINAL DIA OF 0.6725" EVAL. & FOUND ACCEPTED IAW EN1182-08. FLAP PEENING, CADMIUM PLAT & PAINTING C/O ON REWORK AREA. BUSHING & WASHER FAB AND HEAT-TREATED. BUSHING INSTL WITH BUSHING LINE REAM TO DIA: 0.583". NEW WASHER INS TL. 2 L 7 3 4F RT A22WE 20080814 NM 2008 8 14 UPS08M52687 1 20080708 A 5310 DOOR FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 AFT LWR CARGO DOOR FRAME DAMAGED. 2 L 7 3 4F RT A22WE 20080814 NM 2008 8 14 USA2008F00016 1 20080728 A 3397 WIRE BOEING 737 7373G7 1384595 NM COCKPIT BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 306AW 24633 PHX - MAINTENANCE REPORTED THE FLIGHT DECK EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIR E 003-22. OPERATIONAL CHECK GOOD IN ASSOCIATION WITH MM 33-51-11 AND CHAPTER 20. (S) 2 L 7 2 4F RT A16WE 20080814 CE 2008 8 14 DXTA200803204 1 20080729 A 2840 WARNING LIGHT CESSNA 500 560CESSNA 2076750 CE COCKPIT ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 825QS 5600655 DURING TAKEOFF ROLL "L FUEL GAUGE" LIGHT ILLUMINATED PASSING 60 KTS. ABORTED TAKEOFF. (S) 2 L 7 2 4F RT A22CE 20080814 CE 2008 8 14 DXTA200803207 1 20080729 A 3240 BRAKE SYS BEECH MU300 400A 1155402 CE MALFUNCTIONED E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 117QS RK391 THE RT SEAT, THE RT BRAKE PEDAL WOULD LOSE PRESSURE AND DEPRESS FURTHER FROM THE LT PEDAL. (S) 2 H 7 2 4F RT A16SW 20080814 2008 8 14 C2XA08RI107 4 20080725 A 3140 701700082430 COMPUTER EMB 145 EMB145LR 3260212 SO COCKPIT INTERMITTENT A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 13949 17325 145057 FLIGHT 2882 - EWR - FLIGHT CREW REPORTED ELECTRICAL POWER LOSS IN FLIGHT AT 35,000 FT WITH A LOUD THUMP, MFD, PFD, EICAS ALL RED "X", AP FAIL. STALL TEST LIGHT ILLUMINATED BUT EVERYTHING CAME BACK A FEW SECONDS LATER. CREW LANDED ACFT AS PLANNED WITHOUT INCIDENT. EWR MX REMOVED AND REPLACED NR 1 INTEGRATED COMPUTER IC600 AND PERFORMED OPERATIONAL CHECK SU CCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080814 WP 2008 8 14 IXX2008F00042 1 20080609 A 5754 SKIN DOUG DC8 DC872F 302199E WP SLOT VANE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD SLOT VANE LEADING EDGE HAS ELONGATED HOLES AT STATION XS 247.00 0. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XILD 7095.000-XS 247.000 IAW DC8 SRM 57-3-2 FIGURE 10 PAGE 22 ITEM F, DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-3-0, AND S RM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 08FDEA03028 1 20080723 A 5347 AGA38555 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 DURING INSPECTION AFTER REMOVAL FLOOR PANEL WITH OAN J/C 0600C180-1JR FOUND SEVERE CORROSION ON SEAT TRACK. 2 L 7 3 4F A22WE 20080814 NM 2008 8 14 08FDEA02925 1 20080716 A 5220 50797890 FRAME BOEING 727 727233 138408A NM EMERGENCY HATCH CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 RT AFT EMERGENCY EXIT HATCH LOWER FRAME OUTER SURFACE HAS CORROSION. REMOVED CORROSION REF SRM 52-00-2 NDT THICKNESS OR IGINAL "T" .063, .005 LOSS, .058, DAMAGE WITHIN LIMITS REF SRM 53-10-1 FIG 1 SHEETS 1, 2, 3. TREATED PRIMED AND PAINTED REWORKED AREAS REF SRM 51-10-2 AND MM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080814 CE 2008 8 14 DXTA200803214 1 20080803 A 3240 BRAKE SYS CESSNA 500 560CESSNA 2076750 CE MALFUNCTIONED E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 398QS 5600522 CO-PILOT`S BRAKES ARE VERY SQUISHY. TAKES MUCH MORE THAN NORMAL PRESSURE WHEN APPLYING BRAKES. (S) 2 L 7 2 4F RT A22CE 20080814 NM 2008 8 14 NWAA083586311 1 20080801 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 671US 26477 EMERGENCY PATH LIGHTS INOPERATIVE FROM ROW 51 TO 61. MAINTENANCE CONNECTED WIRE. OPERATIONAL CHECKED GOOD, AND ACFT WA S RETURNED TO SERVICE. (S) 2 L 7 4 4F RT A20WE 20080814 NM 2008 8 14 F3LA200800534 1 20080731 A 5321 D5367314500000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2209 DURING C3 C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL, 152XG, WAS DAMAGED. MAINTENANCE REPAIRED THE PUNCTURE DAMAGE IN TRANSITION PANEL 152XG IAW THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. MAINTENANCE PREPARED AND PAINTE D THE TRANSITION PANEL IAW THE REQUIREMENTS OF AMM 25-00-00-370-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 F3LA200800535 1 20080731 A 5321 D5367302100000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2209 DURING C3 C-CHECK, INSPECTION NOTED THE AFT CARGO PIT TRANSITION PANEL, 152AE, WAS DAMAGED. MAINTENANCE REPAIRED THE PU NCTURE DAMAGE IN TRANSITION PANEL 152AE IAW THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. MAINTENANCE PREPARED AND PAINTED THE TRANSITION PANEL IAW THE REQUIREMENTS OF AMM 25-00-00-370-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECT ED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 F3LA200800544 1 20080803 A 1100 D5361060700000 PLACARD AIRBUS A319 A319111 3930336 NM R2 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2 2209 DURING C3 C-CHECK, INSPECTION NOTED R2 DOOR THRESHOLD SLIDE "ARMED" PLATE IS CORRODED ON THE BOTTOM. MAINTENANCE REMOVE D AND REPLACED R2 DOOR THRESHOLD SLIDE "ARMED" PLATE IAW THE REQUIREMENTS OF A319 AMM 53-42-12-400-002. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080814 SO 2008 8 14 C2X2008F00017 1 20080804 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14916 17737 17737 145415 ACFT CURRENTLY IN A C-CHECK STATUS AND THE LT FUSELAGE WAS FOUND GOUGED AND DENTED AT FR19. MAINTENANCE CUT OUT THE ARE A AND FABRICATED A NEW REPAIR IAW EC5330-01824. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. (S) 2 L 7 2 4T RT T00011AT 20080814 NM 2008 8 14 QXEA200800858 1 20080730 A 2530 COFFEEMAKER BOMBDR DHC8 DHC8402 1390042 NM GALLEY MALFUNCTIONED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 19 430QX 4163 PDX - FLIGHT 2335. CREW REPORTED A BURNING ODOR IN THE AFT GALLEY AREA. MAINTENANCE FOUND THE SOURCE TO BE THE LT JUG. REPLACED THE LT JUG. OPERATIONAL CHECKS GOOD. ACFT RETURNED TO SERVICE. (S) 2 H 7 2 4T RT A13NM 20080814 NM 2008 8 14 QXEA200800859 1 20080729 A 3231 483023 SEQUENCE VALVE BOMBDR DHC8 DHC8402 1390042 NM NLG DOOR MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 19 420QX 4072 4147 PDX - UPON DEPARTURE FROM PUW WHEN THE GEAR WAS SELECTED UP THE LT MAIN GEAR DOOR LIGHT STAYED ON. RAN CHECKLIST, NORMA L GEAR AND ALTERNATE GEAR INDICATIONS WERE NORMAL. FERRIED THE ACFT TO PDX FOR REPAIRS. IN PDX REPLACED THE SOLENOID S EQUENCE VALVE. OPERATIONAL CHECKS GOOD. RETURNED TO SERVICE. (S) 2 H 7 2 4T RT A13NM 20080814 EA 2008 8 14 QXEA200800860 1 20080729 A 2612 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA FIRE WARNING ACTIVATED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 19 608QX 10026 PDX - FLIGHT 2621, FIRE SYSTEM FAULT MESSAGE RECEIVED. PLACED ON MEL 26-00-1. RETURNED TO SERVICE. (S) 2 L 7 2 4F RT A21EA 20080814 EA 2008 8 14 COMA086336 1 20080731 A 2621 346000371 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 971CA 28158 7145 FLIGHT 5308 CARGO LOW BOTTLE MESSAGE CAME ON. PERFORMED QRH, RETURNED TO CMH. LANDED WITHOUT INCIDENT. REPLACED FIRE BOTTLE. NO FURTHER DEFECTS. (S) 2 L 7 2 4F RT A21EA 20080814 SO 2008 8 14 RAIA00807018 1 20080727 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 817HK 145058 PRE FLT 5510-STL- VARIOUS EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RESET THE ACFT POWER AND FOUND ALL LIGHTS TO BE FUN CTIONING PROPERLY. (S) 2 L 7 2 4T RT T00011AT 20080814 SO 2008 8 14 RAIA00807022 1 20080730 A 3610 O-RING EMB 145 EMB145 3260210 SO BLEED AIR SYS WORN A RAIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 CE 03 821HK 145068 FLT 5529-STL-BLEED NR 2 LEAK MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE BLEED DUCT O-RINGS. SYSTEM OPS CHECKED GOOD. (S) 2 L 7 2 4F RT T00011AT 20080814 EU 2008 8 14 YENA2008074 1 20080805 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU HNYWL T53 T5317BHNYWL 33860 NE CABIN ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 15 534JB 1705 FLT 308, FLL-IAD, SLIGHT RUBBER ODOR AROUND ROWS 14DEF. LTV MASTER SWITCH AND RACK POWER SWITCH TURNED OFF. SMELL DISS IPATED RAPIDLY. ACCOMPLISHED TSM 23-39-00-810-801 THROUGH STEP 4.B AT ROWS 12-16DEF. ODOR COULD NOT BE DUPLICATED. IN FLIGHT CREW REPORTED SUSPECT AREA AS 14DEF. VERIFIED BY SECOND INFLIGHT CREW MEMBER. NO REPORTED LOSS OF VIDEO, INSPEC TED ROWS 12-16 DEF FOR ABNORMALITIES, NO FAULTS FOUND. SYSTEM WORKING NORMALLY. REMOVED AND REPLACED SEB AT 14E AS PRE CAUTIONARY IAW LTV MM 23-39-000, OPS CHECK OK. 2 L 7 2 4F 4 U RT A28NM E17EA 20080814 NM 2008 8 14 YENA2008071 1 20080802 A 3350 340022 POWER UNIT EMB ERJ190 ERJ190100IGW 3260408 NM CABIN FAILED A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 267JB 4139 4139 19000065 ON MX INSP, ROW 11, RT LOWER EMERGENCY LIGHT INOP. REMOVED AND REPLACED RT CENTER EMERGENCY LIGHT POWER UNIT IAW AMM 33 -50-01. OPS CHECK GOOD. (S) 2 L 7 2 4F RT A57NM 20080814 NM 2008 8 14 WRLA2008066 1 20080805 A 5347 S4929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 275WA 48631 DURING "C" CHECK INSPECTION IN TPE FOUND CRACK IN THE MAIN DECK SEAT TRACK AT Y=760, X=47.5. (S) 2 L 7 3 4F 4 F RT A22WE E24NE 20080814 WP 2008 8 14 V0J2008F00000 2 20080625 A 7321 21190108000 EEC RAYTHN 850 HAWKER850XP 7150016 CE GARRTT TFE731 TFE7315BR WP ENGINE INOPERATIVE E V0JA O OTHER O OTHER NR NOT REPORTED 1 EA 03 1776A 258750 P31306 NEW DIGITAL ELECTRONIC ENGINE COMPUTER WAS INOPERABLE UPON INSTALLATION. (S) 1 L 7 2 4F 4 F RT A3EU E6WE 20080814 NM 2008 8 14 KCSA081376 1 20080811 A 5311 FRAME BOEING 747 747249F 1384849 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 FWD PIT BS640 FUSELAGE FRAME DENTED AT LBL26, WL112. (S) 2 L 7 4 4F RT A20WE 20080814 2008 8 14 KCSA081364 4 20080731 A 2565 LINKAGE BOEING 747 747259B 1384804 NM EVAC SLIDE BROKEN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 ESCAPE SLIDE RELEASE LINKAGE BROKEN ON LATCH SIDE (FWD). (A) 2 L 7 4 4F RT A20WE 20080814 NM 2008 8 14 KCSA081318 1 20080715 A 5315 FLOORBEAM BOEING 747 747246B 1384864 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 BS 1220 STUB FLOOR BEAM WEB CRACKED AT LBL-111. (A) 2 L 7 4 4F RT A20WE 20080814 NM 2008 8 14 USAASB08052 1 20080723 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 438US 24560 CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT OVER THE AFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE BATTERY CHARGER ASSEMBLY IN THE AFT GALLEY. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A16WE 20080814 2008 8 14 USAA920081461 4 20080701 A 2565 CABLE AIRBUS A319 A319112 3930323 EU EVAC SLIDE FRAYED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 1028AL 0885 PIT-S4-EES- R-1 DOOR SLIDE/RAFT ASSEMBLY ATTACH CABLE FOR GIRT SAFETY PIN FRAYED. FRAYED WIRES CUT THREAD WHICH SECURES SAFETY PIN. R-1 DOOR SLIDE/RAFT ASSEMBLY REPLACED. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 USAA920081471 1 20080804 A 5311 654653251 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 PHX-RON -MAJOR REPAIR- FRAME AT BS 460 S16R IS CRACKED AT SKIN ATTACHMENT. REPAIRED FRAME AT BS 460 S16R IAW B737 SRM 5 3-00-07-2R7 REPAIR 7. (S) 2 L 7 2 4F RT A16WE 20080814 EU 2008 8 14 USAA920081460 1 20080803 A 2560 P207003001 FLASHLIGHT AIRBUS 320 A320214 3930316 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 109UW 1065 FLT 973 PDX-CLT - EMERGENCY EQUIPMENT - BREAKAWAY FLASHLIGHTS AT 2L AND 1L JUMPSEATS NEED REPLACED. MAINTENANCE REMOVED AND REPLACED FLASHLIGHTS AT 2L AND 1L AND BREAKAWAY STRAPS. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 USAA920081470 1 20080803 A 5320 69353506 FITTING BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 PHX-RON -MAJOR REPAIR- STRINGER TO FRAME CLIP CRACKED AT BS 440 S16R. REPLACED STRINGER TO FRAME CLIP AT BS 440 S16R IA W B737 SRM 51-40-02. (S) 2 L 7 2 4F RT A16WE 20080814 NM 2008 8 14 USAA920081490 1 20080806 A 5311 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT-Q6 -MAJOR REPAIR- FRAME CRACKED AT BS 887 BETWEEN S8L AND S9L. REPAIRED FRAME AT BS 887 BETWEEN S8L AND S9L IAW US AIRWAYS TYPICAL REPAIR 53-10-20E. (S) 2 L 7 2 4F RT A16WE 20080814 NM 2008 8 14 USAA920081486 1 20080731 A 5315 D53472188204 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 833AW 1844 SAL-BC4 -MAJOR REPAIR- CORROSION ON FLOORBEAM AT FR68, Y1180. REPLACED FLOORBEAM AT FR68, Y1180 IAW A319 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 USAA920081455 1 20080715 A 5347 D5311278220200 SEAT TRACK AIRBUS A319 A319132 3930340 NM CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803AW 0931 SAL-C7- MAJOR REPAIR - CORROSION ON CABIN SEAT TRACK FR20, -Y1292. REPLACED CABIN SEAT TRACK FR20, -Y1292 IAW A319 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 USAASB08051 1 20080723 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 438US 24560 CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT OVER THE FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE FORWARD GALLEY. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A16WE 20080814 EU 2008 8 14 USAA920081489 1 20080806 A 3240 A253130021 SELECTOR VALVE AIRBUS A319 A319112 3930323 EU BRAKE SYSTEM DEFECTIVE A USAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 19 764US 1369 FLT 1210 DFW-PHL- BRAKES - ACFT RETURNED TO GATE WITH ECAM MESSAGE "AUTO BRAKE INOP" FOLLOWED BY NORMAL BRAKE SYSTEM 1 F AILURE. ATTEMPTED RESETS WITH NO CHANGE IN INDICATION. MAINTENANCE REMOVED AND REPLACED THE BRAKE/STEERING CONTROL UNI T AND BRAKE SELECTOR VALVE. BRAKE SELECTOR VALVE WAS A CONFIRMED FAILURE. BRAKE/STEERING CONTROL UNIT WAS NO FAULT FOU ND. 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 USAA920081466 1 20080722 A 5320 D53471124201 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803AW 0931 SAL-C7- MAJOR REPAIR - SHEAR PLATE CORRODED FR69 TO FR70, -Y1732, S23R. REPLACED SHEAR PLATE FR60 TO FR70, -Y1732, S23R IAW A319 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 USAASB08059 1 20080803 A 3397 SPLICE BOEING 737 7374B7 1384702 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 456UW 25020 FLL - MAINTENANCE REPORTED THE AFT LT ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND THE BUTT SPLICE DI SCONNECTED. RECONNECTED BUTT SPLICE. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A16WE 20080814 EU 2008 8 14 USAA920081452 1 20080730 A 5540 D5537123500800 HINGE FITTING AIRBUS 320 A320231 3930325 EU RUDDER LOOSE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 627AW 66 SAL-C6-MAJOR REPAIR - PLAY ON RUDDER HINGE FITTING NR 7 AT VERTICAL STABILIZER STA 5605 RIB NR 11. REPLACED RUDDER HING E FITTING NR 7 AT VERTICAL STABILIZER STA5605 RIB NR 11 IAW A320 AMM 55-36-41. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 USAA920081478 1 20080714 A 5315 6546812185 FLOORBEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 168AW 23629 MCN - C21 -MAJOR REPAIR- CORROSION ON DIAGONAL FLOORBEAM BS 996 TO BS 1006, WL 208.1, LBL 13. REPLACED DIAGONAL FLOORBE AM BS 996 TO BS 1006, WL 208.1, LBL 13 IAW B737 SRM 51-40-02-0G. (S) 2 L 7 2 4F RT A16WE 20080815 WP 2008 8 15 08FDEA03074 1 20080725 A 5755 SKIN DOUG MD10 MD1010F 3022112 WP NR 2 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 THE LEFT WING NR 2 SPOILER IS DELAMINATED ON THE LOWER SURFACE AT THE OUTBD CORNER. REMOVED & REPLACED THE NR 2 LT WING SPOILER PER AMM 27-60-01-4. OPS & GAP CHECKS ARE GOOD PER AMM 27-60-01-4 & 27-60-01-6. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 08FDEA02959 1 20080717 A 5330 NFA601321 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 FUSELAGE EXTERNAL SKIN HAS A DENT BETWEEN LONGERONS 45-L AND 46-L AND FS 1761 AND 1741. MEASURED THE MINOR AXIS OF THE DENT (D) D=3.5. MEASURED DEPTH (Y) Y = .085, D/Y = 41, DENT IS CREASED AND FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 5 3-20-00, FIG 13, SHEET 2, VOL I, PARA 1-B. CUTOUT DAMAGE AND FABRICATED A REPAIR DOUBLER, TRIPLER, FINGER DOUBLERS AND INSTALLED THE REPAIR IAW DC/MD-10 SRM 53-20-00, FIG 6, VOL I. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01, VOL II. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 08FDEA02934 1 20080716 A 5753 ARC1959502 SKIN DOUG MD10 MD1010F 3022112 WP RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 RIGHT WNG OUTBD FLAP LOWER SURFACE SKIN HAS A DENT, 1 FOOT OUTBD OF THE SPRING CARTRIDGE. CHECKED THE DENT AND FOUND IT TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00, FIG 48, VOL I. CUT OUT THE DAMAGED AREA. MATERIAL ID FOR THE DOUBLER IS 2024-T3, 0.050, PO 623408.1. FABRICATED DOUBLER IAW DC/MD-10 SRM 57-10-00, FIG 85, VOL I. ALODINED AND PRIMED IAW D C/MD-10 SRM 51-21-01, VOL II, PGS 21-24, VOL II. INSTALLED IAW DC/MD-10 SRM 51-35-02, VOL II. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 08FDEA02936 1 20080716 A 5753 ARC19492 SKIN DOUG MD10 MD1010F 3022112 WP RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 RIGHT WING OUTBD FLAP SURFACE SKIN HAS 6 DENTS IN THE INBD EDGE AREA. CHECKED DENTS AND FOUND TO BE OUT OF LIMITS AT ST A XOFH 478 AND 503 IAW DC/MD-10 SRM 57-10-00, FIG 48, VOL I. CUT OUT DAMAGED AREAS. MATERIAL ID FOR DOUBLERS 2024-T3, 0.050, PO 623403.1, FILLERS 2024-T3, 0.046, PO 600955.2. FABRICATED IAW DC MD 10 SRM 57-10-00, FIG 85; VOL I AND SRM 5 7-52-01, FIG 8, VOL III. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01, VOL II, PGS 21-24. INSTALLED IAW DC/MD-10 SRM 51-35-02, VOL II. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 08FDEA02937 1 20080716 A 5753 ARC27364 SKIN DOUG MD10 MD1010F 3022112 WP RT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 RIGHT WING INBD FLAP T/E LOWER SURFACE SKIN HAS LIGHTNING STRIKE DAMAGE 4 FEET FROM THE OUTBD EDGE. REPLACED SKIN P/N A RC 2736-4. THIS WAS ACCOMPLISHED ON N/R N00285, FOR DETAILS SEE SDR TRACKING NUMBER 08-3079. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 08FDEA03042 1 20080724 A 5320 6558504 CHANNEL BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 LOWER FUSE WING BODY FILLET FRG SUPPORT FRAME U CHANNEL IS CORRODED BS 773, LBL 9 - RBL 9, WL 140. REMOVED U CHANNEL R EF SRM 51-30-2. FABRICATED "U" CHANNEL ON SHOP SNRM NR N00692, DRILLED UP, TREATED, PRIMED AND PAINTED "U" CHANNEL REF DWR 65-58504, SRM 51-10-2. IDENTIFIED "U" CHANNEL REF GMM 7-0-1001. INSTALLED "U" REF SRM 51-30-2 APPLIED CIC TO NEW "U " CHANNEL REF SRM 51-10-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080815 WP 2008 8 15 08FDEA02941 1 20080716 A 5347 601096418 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 303FE 46802 MAIN CARGO, LUGS ON SEAT TRACK WORN AT FS 1406 LBL 47. REMOVED SEAT TRACK SECTION, FABRICATED NEW SECTION AND SPLICES I NSTALLED NEW SECTION IAW SRM 53-70-00 ON TRAVELER T8/748310. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 08FDEA03064 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL TANK ACCESS CUTOUT 641CB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS C LASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080815 WP 2008 8 15 08FDEA02865 1 20080714 A 5330 AEA03443 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 CENTER WHEEL WELL/SPACE, INTERIOR AFT BULKHEAD, FWD FACE, MID LOWER SECTION SKIN HAS CORROSION IN MULTIPLE SPOTS AROUND FASTENER HEADS AND RUNNING UNDER A HORIZONTAL STIFFENER, LBL 15, FS 1521. REMOVED CORROSION IAW DC/MD-10 SRM 53-00-01, VOL I. FOUND TO BE WITHIN ALLOWABLE LIMITS. ORIGINAL MATERIAL IS 0.063. MATERIAL LOSS 0.003. MATERIAL REMAINING 0.0 60 IAW DC/MD-10 SRM 53-14-01, VOL III. USED UT GAUGE T8225P. ALODINED AND PRIMED AREAS IAW DC/MD-10 SRM 51-21-01, VO L II. 2 L 7 3 4F RT A22WE 20080815 EU 2008 8 15 08FDEA02977 1 20080718 A 5347 R5327049020000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 686FE 804 MAIN CARGO DECK LT SIDE NR 4 SEAT TRACK BETWEEN FR 60 AND FR 61 HAS 3 EA ELONGATED SCALLOPS. REMOVED DAMAGED TRACK SECT ION AND INSTALLED SEAT TRACK SPLICE. REPAIR AT LT TRACK NR 4 BETWEEN FR 60 AND FR 61 IAW A300-600 SRM 53-10-16, FIG 201 , PG207/208. 2 L 7 2 4F RT A35EU 2008011700083 20080117 00083 NM 2008 1 17 UIEA200800008 1 20080110 A 5753 SKIN BOEING 747 74747UF 1384812 NM LT TE FLAP DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 412 30559 SMALL DENT ON THE LT I/B AFT FLAP LOWER SURFACE I/B OF NR 4 CANOE. DENT 0.250" DIAMETER, PIN HOLE IN CENTER 0.060" IS N OT NEAR AN EDGE IS MIDSPAN AND IS COVERED UNDER ALLOWABLE DAMAGE SRM 57-53-01 PAGE 102, C, D, F. 2 L 7 4 4F RT A20WE 2008010800342 20080108 00342 NM 2008 1 8 MWEA080001 1 20080101 A 3220 59404965005 LANDING GEAR BOEING 717 717200 1383700 NM NOSE SLOW A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 913ME 55176 ON GEAR RETRACTION, NOSE SLOW TO RETRACT. NO FAULTS FOUND. SERVICED HYDRAULIC SYSTEM AND PERFORMED FUNCTIONAL TESTS WI TH NO FAULTS NOTED. OK FOR SERVICE. 2 L 7 2 4F TR A6WE 2008010900016 20080109 00016 2008 1 9 SIMA200800302 4 20080102 A 3160 622771800462244 ADC SAAB SF340 340B 7860101 EU COCKPIT SMOKE A SIMA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 307AE 340B307 ON FLIGHT 3426 - AIRCRAFT DECLARED AN EMERGENCY WITH SMOKE AND FUMES IN COCKPIT AND RUDDER INOP. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED MFD UNIT IAW AMM 31-25-10. REMOVED AND REPLACED ADC IAW AMM 31-12-05. OPERATIONAL CHECK AND LEAK CHECK GOOD. AUTO PILOT AND YAW DAMPENER OPERATIONAL CHECK GOOD IAW AMM 22-10-00. AIRCRAFT RETURNED TO SERVIC E. 2 L 7 2 4T RT A52EU 2008010900044 20080109 00044 EU 2008 1 9 08FDEA00010 1 20080102 A 5320 Y5382971220000 WEB AIRBUS 300 A300B4622 3930401 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 FOUND LWR FUSELAGE FR 51 BETWEEN SEAT TRACK 3L AND 4L, CARGO LOADING SYS SUPPORT WEB IS BENT ALONG THE O/B LWR EDGE. RE MOVED AND REPLACED WEB IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008010900045 20080109 00045 EU 2008 1 9 08FDEA00011 1 20080102 A 5320 Y5382971220000 WEB AIRBUS 300 A300B4622 3930401 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 LWR FUSELAGE FR 48 BETWEEN SEAT TRACK 3L THRU 4L THE CARGO LOADING SYS SUPPORT WEB IS BENT ALONG THE O/B EDGE. REMOVED AND REPLACED SUPPORT WEB IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008010900046 20080109 00046 EU 2008 1 9 08FDEA00012 1 20080102 A 5320 A5381206720100 WEB AIRBUS 300 A300B4622 3930401 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 LT TRACK Y1456 FR 49 AFTER REMOVAL OF WEB FOUND 1 LINK TRACK WITH BENT TAB ON I/B SIDE. REMOVED AND REPLACED SUPPORT LI NK IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008010900047 20080109 00047 EU 2008 1 9 08FDEA00013 1 20080103 A 5320 A5381206720100 TRACK AIRBUS 300 A300B4622 3930401 EU ZONE 100 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 LT TRACK Y1456 FR 52 AFTER REMOVAL OF WEB FOUND 1 LINK TRACK WITH BENT TAB ON I/B SIDE. REMOVED AND REPLACED SUPPORT LI NK BRACKET AT LT TRACK Y1456 FR 52 IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008010900051 20080109 00051 EU 2008 1 9 08FDEA00018 1 20080103 A 5320 A5381206720100 BRACKET AIRBUS 300 A300B4622 3930401 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 LWR FUSELAGE FR53 L SIDE OF CENTER 55" TRACK SUPPORT LINK BRACKET HAS THE I/B TAB ATTACH POINT FOR WEB IS BROKEN OFF. R EMOVED AND REPLACED LINK IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008010900053 20080109 00053 EU 2008 1 9 08FDEA00020 1 20080103 A 5753 A57960306201 SKIN AIRBUS 300 A300B4622 3930401 EU RT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 AFTER REMOVAL OF RT WING CENTER FLAP CENTER UPPER RUB STRIP FOUND 1 EA CRACK 1 INCH LONG IN THE FLAP UPPER SKIN. REPAIR ED UPPER SKIN OF RT CENTER FLAP IAW EA 6-5750-113403 AND TD FOK 302/2007 ISSUE A. 2 L 7 2 4F RT A35EU 2008010900054 20080109 00054 EU 2008 1 9 08FDEA00021 1 20080103 A 5320 Y5382971220000 WEB AIRBUS 300 A300B4622 3930401 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 LWR FUSELAGE FR 54 LEFT OF CENTER 33" TO 55" CARGO LOADING SYS SUPPORT WEB IS BENT ALONG THE I/B EDGE. REMOVED AND REPL ACED LOADING SYS SUPPORT WEB IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008010900059 20080109 00059 EU 2008 1 9 08FDEA00026 1 20080103 A 7120 BEAM AIRBUS 310 A310221 3930310 EU NR 2 PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 NR 2 ENGINE PYLON AFT BEAM ATTACHMENT MOUNT AFT SIDE , 2 PLACES, UPPER END EMITTING RUST. REMOVED & REPLACED NR 2 ENG. MOUNT SHIM REF AMM 54-54-86-4 2B-3. PRIMED SHIM REF AMM 54-51-00-6 PG. 5. MATCH DRILLED SHIM REF SRM 51-4-44. REMOVED & REINSTALLED PRE COOLER REF AMM 36-11-15-4. REMOVED & REINSTALLED PRE COOLER INLET DUCT REF AMM 36-11-00-4. LEAK CHECK TO BE ACP. ON FEDEX J/C 40C0503 JPF STEP 9. 2 L 7 2 4F RT A35EU 2008010900095 20080109 00095 EA 2008 1 9 SWIA200819021 1 20080102 A 7603 GEARBOX CNDAIR CL600 CL6002B19 1900309 EA THROTTLE CONTROL BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 435SW 7555 FLT 4331 - LEFT THRUST LEVER WILL NOT COME OUT OF SHUTOFF POSITION. REPLACED LEFT ENGINE THROTTLE GEAR BOX. OPS CHECK GOOD, PN: 2100140-010, SN OFF: 2297. 2 L 7 2 4F RT A21EA 2008010800316 20080108 00316 NM 2008 1 8 HALA0800001 1 20080101 A 2710 285T0015116 MODULE BOEING 767 76733A 1385209 NM AILERONS MALFUNCTIONED A HALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 13 583HA 24431 ETOPS SIGNIFICANT SYSTEM, EICAS MESSAGE AILERON LOCKOUT ILLUMINATED ON DESCENT THRU 7000 FT 230 KTS FLAP 5 AUTOPILOT ON. REPLACED RT SAM PER AMM 27-09-00. PERFORMED TEST AMM 27-11-00 CK OK. PERFORMED MCDP TEST 60 CK OK GRND CK 1 AT 2 ADC OK, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008010900028 20080109 00028 NM 2008 1 9 NWAA080016306 1 20080101 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 666US 23821 DURING LINE CHECK, FOUND LT UPPER DECK EMERGENCY DOOR BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK PER AMM 52-23-14. 2 L 7 4 4F RT A20WE 20080815 EU 2008 8 15 08FDEA02966 1 20080718 A 5330 A53813303200 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND SEVERAL DAMAGES ON INNER SKIN C 40 AFT FITTING OUTER FLANGE (HOLE 15 AND 16). REPAIR PERFORMED BY SMOOTH REWORK O N INNER SKIN PANEL ABOVE HOLE 15, OVERSIZE HOLE 15, REWORK OF WHOLE FLANGE AT HOLE 16 IAW RAS/70511563/030/2008 ISS A, APPROVED BY EA 6-5340-120078. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA02978 1 20080710 A 5753 A57942174208 FITTING AIRBUS 300 A300B4622R 3930312 EU TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 RT WING, INTERIOR FITTING AT FRONT CARRIAGE NR 3 FLAP TRACK WITH CORROSION, DETECTED ON ACCOMPLISHMENT OF NR 0599. A NEW FITTING WAS FABRICATED SO AS TO REPLACE THE EXISTING ONE. 2 L 7 2 4F RT A35EU 20080815 NM 2008 8 15 08FDEA03065 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL TANK ACCESS CUTOUT 641BB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS C LASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008010800311 20080108 00311 NM 2008 1 8 08FDEA00004 1 20080102 A 5710 6521655 SUPPORT BEAM BOEING 727 727233 138408A NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 RT WING INBD UPPER WING PANEL SUPPORT BEAM IS CRACKED JUST FWD OF MLG BEAM 10" O/B OF UPLOCK T/T. REMOVED SUPPORT BEAM FROM A/C REF SRM 51-30-2. STOP DRILLED CRACK REF SRM 51-10-1. FABRICATED AND INSTALLED REPAIR ON SUPPORT REF SRM 51-40 -2. REINSTALLED SUPPORT BEAM ON A/C REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008010800320 20080108 00320 NM 2008 1 8 HALA0800002 1 20080101 A 2150 CONTROLLER BOEING 767 7673G5 1385126 NM RT PACK TEMP MALFUNCTIONED A HALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, RIGHT PACK TEMP EICAS PRIOR TO DEPARTURE. BITE CHECK PACK TEMP CONTROLLER RESET. NO FAULTS N OTED. 2 L 7 2 4F RT A1NM 2008010900040 20080109 00040 EU 2008 1 9 08FDEA00007 1 20080102 A 5320 Y5382971220000 WEB AIRBUS 300 A300B4622 3930401 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 FOUND LWR FUSELAGE FR 49 BETWEEN SEAT TRACK 3L AND 4L, CARGO LOADING SYS SUPPORT WEB IS BENT ALONG THE O/B LWR EDGE. RE MOVED AND REPLACED SUPPORT WEB AT FR 49 TRACK 3L THRU 4L IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008010900049 20080109 00049 EU 2008 1 9 08FDEA00016 1 20080103 A 5320 A5383210420600 WEB AIRBUS 300 A300B4622 3930401 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 LWR FUSELAGE FR 51 BETWEEN TRACK 3L AND 4L, 12" TO 24" BELOW FLOOR. THE STIFFENER WEB IS BENT AFT 3/8". REMOVED AND RE PLACED WEB IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008010900052 20080109 00052 EU 2008 1 9 08FDEA00019 1 20080103 A 5320 BRACKET AIRBUS 300 A300B4622 3930401 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 LWR FUSELAGE FR 54 CENTER LINE SEAT TRACK SUPPORT LINK BRACKET IS BROKEN INTO TWO PIECES. REMOVED AND REPLACED SUPPORT LINK IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008010900055 20080109 00055 EU 2008 1 9 08FDEA00022 1 20080103 A 5720 SUPPORT ANGLE AIRBUS 310 A310221 3930310 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 LEFT WING UPPER SURFACE TRAILING EDGE PANEL NR 575BT CUTOUT SUPPORT ANGLE CRACKED AT STATION 490. CLEANED AREA IAW FED EX A310-200 SRM 51-23-10 PG 1. ACCOM. HFEC INSP. PER A310 NTM 51-10-08. VERIFIED AREA IS CRACKED. USED TOOL TWS 8209A. U NABLE TO MARK END OF CRACK DUE TO CRACK RUNS TO BOTTOM OF WING T/E. RECEIVED FINAL RFTS N416FE-7-36189 W/ EA6-5750-11300 9. ACCOMPLISHED HFEC OF ADJACENT SKIN AREA IAW A310 NTM 51-10-08 USING T8257A. NO CRACKS NOTED. INSTALLED FASTENERS IAW A310-200 SRM 51-40-21 PG 24 AND PG 90. 2 L 7 2 4F RT A35EU 2008010900056 20080109 00056 EU 2008 1 9 08FDEA00023 1 20080103 A 5347 A53811910200 SEAT TRACK AIRBUS 300 A300B4622 3930401 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 LWR FUSELAGE FR 54 18" LEFT OF CENTER, SEAT TRACK SUPPORT LINK IS BROKEN INTO TWO PIECES. REMOVED AND REPLACED TRACK SU PPORT LINK IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008010900057 20080109 00057 EU 2008 1 9 08FDEA00024 1 20080103 A 5320 Y5382791220000 WEB AIRBUS 300 A300B4622 3930401 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 LWR FUSELAGE FR 53 LEFT OF CENTER 18 TO 55" CARGO LOADING SYS SUPPORT WEB IS BENT ALONG THE INBD AND OTBD LWR EDGE. REM OVED AND REPLACED WEB IAW A30-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008010900098 20080109 00098 SW 2008 1 9 WGEA200800001 1 20080103 A 3244 M16901 TIRE ECLIPS EA500 ECLIPSEEA500 3350000 SW NR 1 MLG FAILED E WGEA O OTHER O OTHER LD LANDING 1 EA 27 141DJ 20 1215 000055 NR 1 RT MAIN GEAR TIRE BLEW AT 60 KTS ON ROLLOUT ON LANDING, NO GRAB, NORMAL TOUCHDOWN. NR 1 REMOVED RIGHT MAIN WHEEL A SSY. INSPECTED AXLE, BRAKE ASSY AND HARD LANDING INDICATOR. PERFORMED A GENERAL VISUAL INSPECTION OF GEAR ASSY. INSTA LLED A SERVICEABLE WHEEL ASSY IAW AMM 32-42-00. NO DEFECTS AT THIS TIME. 1 L 7 2 4J RT A00002AC 2008010900058 20080109 00058 EU 2008 1 9 08FDEA00025 1 20080103 A 7120 MOUNT AIRBUS 310 A310221 3930310 EU NR 1 ENGINE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 NR 1 ENGINE PYLON AFT ENGINE MOUNT LOWER SURFACE LIGHT CORROSION AROUND LEFT AND RIGHT OUTBOARD SIDES. CLEANED ASSY IAW AMM 54-51-00 6.5 B.P1 REMOVED CORRSION FROM ASSY SURFACE IAW SRM 51-74-10 ITEM 7 B-2 & PMS 01-01-14-1, POLISHWED REWORK AREA IAW AMM 54-51-00-6. PERFORMED PFPI IAW NTM 51-90-00 ON BLENDED AREA ONLY. NO CORROSION NOTED. CLEANED REWORKED AREA IAW AMM 54-51-00- 6 P4. PRIMED REWORKED AREA IAW AMM 54-51-00-6 P4. 2 L 7 2 4F RT A35EU 2008010900093 20080109 00093 2008 1 9 SWIA200819019 2 20080101 A 7230 STATOR VANE CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 440SW 7589 FLT 3976 - LEFT ENGINE STATOR VANE REQUIRES REPLACEMENT. REPLACED STATOR VANE IAW GE MM SEI 756 SP-47. 2 L 7 2 4F RT A21EA 2008010900099 20080109 00099 EU 2008 1 9 TRBA2008002 1 20080103 A 3350 0341516 FUSE AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 431AT 431 FORWARD PART EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY FUSE. 2 H 7 2 4T RT A53EU 2008010900274 20080109 00274 NM 2008 1 9 SWAA080025 1 20080101 A 5755 6573730 BRACKET BOEING 737 7373H4 1384600 NM NR 4 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED MV2 CHECK, FOUND LEFT WING NR 4 SPOILER INBOARD ACTUATOR BRACKET BROKEN. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2008010900082 20080109 00082 NM 2008 1 9 QXEA200800001 1 20080102 A 2810 POPPET VALVE DHAV DHC8 DHC8202 2809007 NM FUEL SYSTEM LEAKING A QXEA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 345PH 476 PDX - FUEL DRIPPING FROM THE AREA AROUND THE REFUELING DOOR. MAINTENANCE FOUND THE FUEL DRIPPING FROM THE SPR POPPET. RESEATED THE POPPET VALVE. CHECKS GOOD, NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008031300117 20080313 00117 NM 2008 3 13 CALA08 1 20080305 A 5340 6916970501 ATTACH FITTING BOEING 737 7373T0 1384582 NM BS 384 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69333 23571 STA 384.2 LEFT SIDE S-15 ATTACH FITTING CRACKED. REMOVED AND REPLACED CRACKED ATTACH FITTING AT BS 348.2 STRINGER 15 LT PER ECRA 5310-04726. 2 L 7 2 4F RT A16WE 2008010900042 20080109 00042 EU 2008 1 9 08FDEA00009 1 20080102 A 5320 Y5382971220000 WEB AIRBUS 300 A300B4622 3930401 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 FOUND LWR FUSELAGE FR 52 BETWEEN SEAT TRACK 3L AND 4L, CARGO LOADING SYS SUPPORT WEB IS BENT ALONG THE O/B LWR EDGE. RE MOVED AND REPLACED SUPPORT WEB AT FR 52 BETWEEN TRACK 3L AND 4L IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008010900091 20080109 00091 SO 2008 1 9 SWIA200819017 1 20080101 A 7603 FLEX DRIVE EMB 120 EMB120ER 3260203 SO POWER LEVER BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 561SW 120335 FLT 3730 - RIGHT POWER LEVER IS DIFFICULT TO MOVE. REPLACED AND RIGGED FLEX CABLE AND HOUSING, IAW 76-10-02. OPS CHECK S GOOD. 2 L 7 2 4T RT A31SO 2008010900280 20080109 00280 SO 2008 1 9 RAIA00801001 1 20080101 A 3350 RPS1B BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 823HK 145475 PRE FLT 8032 - SYR - VARIOUS EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BA TTERY. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008010900320 20080109 00320 NM 2008 1 9 SWAA080065 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010900326 20080109 00326 NM 2008 1 9 SWAA080092 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008010900327 20080109 00327 NM 2008 1 9 SWAA080091 1 20080102 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008010900330 20080109 00330 NM 2008 1 9 SWAA080090 1 20080102 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 748D, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008010900336 20080109 00336 NM 2008 1 9 SWAA080081 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081205 EU 2008 12 5 UALA2008112406644 1 20081121 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 403UA 442 RT AFT DOOR SILL HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED 2R DOOR SILL. PICKING UP FASTENER HOLES, STARTED A SSY CLIPS AND PARTS. ASSEMBLED CLIPS AND CORNER CASTINGS, AND SERRATED PLATES TO SILL PAN. INSTALLED FASTENERS IN UPPE R ROW OF SKIN, AND FWD FRAME. CONTINUED TO INSTALL FASTENERS LWR ROW OF SKIN AND COMMON TO (PARTIAL). INSTALLED REMAIN ING FASTENERS. NEED TO INSTALL FWD SPLICE ANGLES. 2 L 7 2 4F 4 F RT A28NM E40NE 20081205 EU 2008 12 5 AALA200802353 1 20081016 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33069 512 JFK - EMERGENCY LIGHTS AT SEAT ROW 9C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 9C. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081205 NM 2008 12 5 AALA200810153 1 20081016 A 5320 INTERCOSTAL BOEING 737 737823 13844BZ NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 TUL - ATTACH FASTENER HOLES AT RIGHT BUTTLINE 30 BETWEEN STATIONS 312 AND 328 HAS ONE HALF INCH CRACK. AREA OF DISCREPA NCY IS ONE HALF INCH BY ONE HALF INCH. REPLACED INTERCOSTAL PER SRM 51 10 02 0G. 2 L 7 2 4F RT A16WE 20081205 WP 2008 12 5 AALA200810258 1 20081108 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 LEFT CUSP IS CRACKED AND HAS CORROSION AT STATION 1244. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081205 WP 2008 12 5 AALA200810252 1 20081104 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION ON FLOORBOARD SUPPORT AT STATION 200 13 INCH IS INBOARD OF NR 3 SEAT TRACK. INSTALLED NEW FLOORBOARD SUPPORT. 2 L 7 2 4F RT A6WE 20081205 WP 2008 12 5 AALA200810259 1 20081108 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CUSP CRACKED FROM LIGHTENING HOLE AT STATION 1305. INSTALLED CUSP REPAIR PER AARD 53-20-00-16 AND SRM 53-01 2 L 7 2 4F RT A6WE 20081205 NM 2008 12 5 ASAA0853888 1 20081128 A 2421 761574B IDG BOEING 737 737890 1384527 NM NR 2 ENGINE MALFUNCTIONED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 584AS 5166 35682 NR 2 GEN DRIVE LIGHT DOES NOT ILLUMINATE REPLACED NR 2 IDG REF MM 24 11 11 400 801. OPS CKS GOOD REF MM 24 11 00 700 80 3 ETOPS CRITICAL PART VERIFIED BY SEAMC MARK. 2 L 7 2 4F RT A16WE 20081208 EA 2008 12 8 VNAA2008113000009 1 20081125 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG LOW A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 207PS 7873 AFTER TAKE OFF IN CLT THE NOSE GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENAN CE INSPECTED AIRCRAFT, CHECKED SENSOR CLEARANCES, SERVICED NLG STRUT, AND CYCLED THE LANDING GEAR. NO OTHER DEFECTS WER E NOTED AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 A6WA200840607 1 20080414 A 5710 FAIRING CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 446AW 7806 LOG 196188/1 REQUEST INSPECTION OF LT WINGLET TRAILING EDGE FOR CRACK. REMOVED LT WINGLET T/E ASSY PER AMM 57-30092 REF LOG PAGE 196188/4 FOR INSTALLATION. INSTALLED NEW LT WINGLET T/E FAIRING ASSY PER AMM 57-30-02. 2 L 7 2 4F RT A21EA 20081208 NM 2008 12 8 FDEA200812035062 1 20081203 A 5330 65545837 SKIN BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 495FE 21669 BS 1183 - 1148 OB AND STR 26L HAS SURFACE CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG 1 AN D 2 AND 53-30-2 FIG 2. REPAIRED SKIN IAW EA NR 7-5330-126867 FUSELAGE SKIN AD 98-11-03 R1, STA 1152 STA 1175 STR 26L 65 -54583 LAP JOINT UPPER AND LOWER SKINS CORROSION REPAIR. 2 L 7 3 4F A3WE 20081208 NM 2008 12 8 SWAA086817 1 20081203 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086754 1 20081202 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BETWEEN BS 520 TO BS 530, STR 28R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086755 1 20081202 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 22R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086761 1 20081202 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086825 1 20081204 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 25R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086762 1 20081202 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086763 1 20081202 A 5753 6573731 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086768 1 20081203 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 FDEA200812035065 1 20081203 A 5315 652084010 FLOORBEAM BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 MAIN DECK FLOORBEAM LWR FLANGE IS CORRODED BS 1166, RBL 10-42, WL 200. REMOVED CORROSION FROM LOWER CHORD, ORIGINAL TEE .125 REMAINING .110. REMOVED .015 OUT OF LIMITS, REMOVED DAMAGED AREA, FABRICATED REPAIR PIECES, ALODINED, PRIMED AND INSTALLED REPAIR PIECES REF EA 7-5310-123823. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081208 EA 2008 12 8 SWIA200820561 1 20081003 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 862AS 7476 DURING C-CHECK, FS 280 FORWARD FLOOR SUPPORT AT RBL 9 RADIUS CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820547 1 20081017 A 3213 AXLE CNDAIR CL600 CL6002C10 1390015 EA LT MLG CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 727SK 10191 C-CHECK, LEFT MLG PISTON AXLE ROOT CORRODED. REPAIRED PER SCR. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820552 1 20080930 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 625 S14R CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 969SW 7876 DURING C-CHECK, FS 625 RIGHT STRINGER NR 14 CLIP CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820554 1 20080930 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 969SW 7876 DURING C-CHECK, LEFT ENGINE AFT THRUST MOUNT FITTING CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820555 1 20081001 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 919SW 7657 DURING C-CHECK, FS 280 LBL9 OUTBOARD WEB CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820556 1 20081001 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 919SW 7657 C-CHECK, FS 280 RBL9 CLIPS CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820557 1 20081001 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 919SW 7657 DURING C-CHECK, FS 280 LBL9 FLOORBEAM CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081208 NM 2008 12 8 SWAA086830 1 20081204 A 5711 6545400 FITTING BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND RT WING VERTICAL WEB CRACKED AT FWD SPAR FITTING. REMOVED AND REPLACED FITTING PER SR M. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086795 1 20081203 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FWD CARGO BAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FWD CARGO STRINGER CRACKED AT BS 491, STR 27R. REPAIRED STRINGER PER AAR EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086801 1 20081203 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM TEE CAP CORRODED AT BS 986, BETWEEN RBL 28 TO RBL 40. REPAIRED TEE CAP PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086837 1 20081204 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086842 1 20081204 A 5230 6547952 STRUCTURE BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO DOOR LOWER TEE CHORD CRACKED AT FWD END. REMOVED AND REPLACED CHORD PER SRM . 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086805 1 20081203 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086807 1 20081203 A 5310 6516352 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER STOP FITTING AT BS 432. REPAIRED FRA ME PER SRM. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0853940 1 20081201 A 4990 FILTER BOEING 737 737890 1384527 NM APU OIL COOLER UNKNOWN A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 557AS 60 35176 JUST PRIOR TO PUSH APU LOW OIL PRESS LIGHT ON THEN APU SHUT OFF PERFORMED FIM TASK 49-60-00-810-801 MX MSG 49-91007 LOP 49-91005 HIGH OIL TEMP SHUTDOWN. PERFORMED FIM 49-90-00-810-803 FOR LOW OIL PRESS. REMOVED AND REPLACED LOW OIL PRESS SWITCH REF AMM 49 94 22 400 801 FIM 49-90-00-810-801 HIGH OIL TEMP. REMOVED AND REPLACED TEMP CONT VALVE OIL COOLER LUB E FILTER REF AMM 49-91-21-400-801-49-91 41-000-801 AND 49-91-21-400-802. APU OPERATIONAL AND LEAK CHECK GROUND OPERATIO N TEST PASSED REF 49-11-00-710-801. VERIFICATION FLIGHT SATISFACTORY . 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0873927 1 20081118 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON FLOOR SUPPORT AFT CARGO BAY BS 772 RBL 7. REMOVED AND FABRICATED NEW CHANNEL AND INSTALLED. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0843912 1 20081122 A 5340 653535214 STRINGER CLIP BOEING 737 7374Q8 138447Q NM BS 887 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 STRINGER CLIP CRACKED. REPLACED CLIP PER DWG A53100265816. 2 L 7 2 4F RT A16WE 20081205 NE 2008 12 5 Q2SA753004 2 20081123 A 7314 PUMP BOEING 747 747228F 1384895 NM GE CF6 CF650E2 30018 NE NR 2 ENGINE DEFECTIVE A Q2SA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 EA 63 753SA 21787 517351 ON CLIMB-OUT FROM EBLG (LIEGE, BELGIUM), NR 2 ENGINE FILTER BYPASS LIGHT ILLUMINATED, THEN WENT OUT. APPROXIMATELY 3 MI NUTES LATER, NR 2 ENGINE FLAME OUT OCCURRED. IN FLIGHT ENGINE START COMPLETED. 3 HOURS, 20 MINUTES LATER AT FL350, FIL TER BYPASS LIGHT ILLUMINATED AGAIN. TROUBLESHOOTING DETERMINED NR 2 ENGINE FUEL PUMP REQUIRES REPLACEMENT. 2 L 7 4 4F 4 F RT A20WE E23EA 20081205 NM 2008 12 5 ASAA0843939 1 20081119 A 5330 654577870 SKIN BOEING 737 7374Q8 138447Q NM BS 1004-1016 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 RT FUSELAGE DENTED 19 INCHES AFT OF R2 DOOR CUTOUT. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER AND TRIPLER AND INSTALLED REPAIR IAW SRM 53-00-01 FIG 201 DETAIL 35. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0843933 1 20081120 A 5755 654645258 SKIN BOEING 737 7374Q8 138447Q NM NR 5 SPOILER DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 AFTER SEAL REMOVED FOUND DENT TO BE DELAMINATED IN THE CENTER OF NR 5 SPOILER. REMOVED DAMAGED AREA FABRICATED FILLER A ND DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REP 4. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0843913 1 20081031 A 5311 654653969 FRAME BOEING 737 7374Q8 138447Q NM BS 616 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 LT FUSELAGE FRAME INNER CHORD CRACKED AT STA 616. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR FILLER AND STIFFENING ANGLE IAW EO 5310 02528. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 HALA2008112500874 1 20081125 A 4990 1589353 BYPASS VALVE BOEING 767 76733A 1385209 NM OIL COOLER MALFUNCTIONED A HALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM - BTB - APU SHUTDOWN ON TOW OUT. BITE CK ECU FOUND OIL TEMP HOT FAULT. REPLACED OIL COOLER BY PASS VALVE PER MM49-27-10 REF FIM 49-11-00. 2 L 7 2 4F RT A1NM 20081205 EA 2008 12 5 MASA2008120200735 1 20081202 A 3350 1317 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 927LR 15027 ASH FLT 2758 PHX-RNO. CEILING OVERHEAD EMERGENCY LIGHT INOPERATIVE. MX RELAMPED. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 MASA2008112700790 1 20081127 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 37178 7178 ASH 2779 PHX. CREW REPORTED A CABIN EXIT LIGHT INOPERATIVE. MX WAS UNABLE TO DUPLICATE THE PROBLEM. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 MASA2008112100785 1 20081121 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A MASA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 75998 7336 ASH FLT 7044 IAD-PWM. DECLARED AN EMERGENCY DUE TO FLAPS FAIL AT 0 DEGREES. MX COMPLIED WITH PART A AND B RESET. CLEA NED AND LUBED FLEX SHAFTS AND REPLACED TEFLON SEALS. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 MASA2008112200786 1 20081122 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN CONTAMINATED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17358 7358 ASH 2818 DSM. DURING OVERNIGHT MAINTENANCE FOUND EMERGENCY FLOOR LIGHTS ON ROWS 2-5 AND 9-12 INOPERATIVE. MX FOUND MOI STURE IN LIGHT TRACKS, DRIED UP AND RE-SECURED. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 MASA2008112900792 1 20081129 A 7714 5071T98P02 AMPLIFIER CNDAIR CL600 CL6002B19 1900309 EA ENGINE MALFUNCTIONED A MASA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SW 07 571ML 7209 ASH FLT 7146 ORD-TYS. CREW DIVERTED TO SDF AND DECLARED AN EMERGENCY DUE TO NR ENGINE SPEED FLUCTUATING. MX PERFORMED ENGINE RUNS AND OPS CHECKED. MX REPLACED A BAD AMPLIFIER. 2 L 7 2 4F RT A21EA 20081205 EU 2008 12 5 UPS08154005 1 20081121 A 3350 CIRCUIT BREAKER AIRBUS A300 A300F4622R 3930360 EU COCKPIT DEFECTIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 130UP 0814 INSPECTION TYPE:N/A COURIER/SUPERNUMERARY AREA INTERIOR EMERGENCY LIGHT SYSTEM INOP. REMOVED AND REPLACED C/B 28WJ PER AMM 33-26-21 AND ESPM 20-46-10. OPS TEST PER AMM 33-51-00-05. CHECKS GOOD. CLEARS M389086. PLACARD REMOVED. 2 L 7 2 4F RT A35EU 20081205 NM 2008 12 5 UPS08553970 1 20081121 A 5610 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT OUT OF ADJUST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 474UP 28844 INSPECTION TYPE:N/A CAPTAIN'S SIDE WINDOW HARD TO OPEN. ADJUSTED L2 WINDOW W/REF TO AMM 56-11-02-5. WINDOW HANDLE OPER ATES NORMALLY. 2 L 7 2 4F RT A2NM 20081205 NM 2008 12 5 ASAA0843958 1 20081121 A 5311 654653981 FRAME BOEING 737 7374Q8 138447Q NM BS 616 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 BS 616 LT SIDE FRAME CRACKED BELOW WL 208 ACCOMPLISHMENT OF EC 5310-0258-5 REQUIRED. REPAIRED LT SIDE FRAME AT STA 616 IAW EC 5310-0258-5. 2 L 7 2 4F RT A16WE 20081205 EA 2008 12 5 SWIA200820525 1 20080916 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 465SW 7845 DURING C-CHECK, FS 280 FLOORBEAM AT RBL 9 OUTBOARD SIDE CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820527 1 20081007 A 5315 FLOORBEAM CNDAIR CL600 CL6002D24 1390016 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 806SK 15070 DURING C-CHECK, FS 280 FLOORBEAM CRACKED AT RBL 9. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820532 1 20081007 A 5343 PIN CNDAIR CL600 CL6002C10 1390015 EA LT MLG TRUNNION CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 718SK 10184 DURING C-CHECK, LEFT MLG TRUNNION PIN AND NUT CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081205 SO 2008 12 5 SWIA200820533 1 20081124 A 5322 SHEAR TIE EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 227SW 120304 DURING C-CHECK, SHEAR CLIP CORRODED BETWEEN STATIONS 36 AND 37 BELOW KEEL BEAM. REPLACED PER SRM. 2 L 7 2 4T RT A31SO 20081205 SO 2008 12 5 SWIA200820534 1 20081124 A 5322 SHEAR TIE EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 227SW 120304 DURING C-CHECK, SHEAR CLIP CORRODED AT STATION 35 BELOW KEEL BEAM. REPLACED PER SRM. 2 L 7 2 4T RT A31SO 20081205 EA 2008 12 5 SWIA200820535 1 20081129 A 3350 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCHARGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 946SW 7776 FLT 6704 - EMERGENCY LIGHTS INOP IN AFT CABIN. REPLACED NR 4 INVERTER. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 WRLA2008092 1 20081004 A 5730 SKIN DOUG MD11 MD11F 3023600 NM BS 595 DEFORMED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHK + 4C CHK, EGAT MECH FOUND NOSE GEAR TRUNNION FITTING SKIN DEFORMED AT STA Y=595, L50L, REFER TO EGAT N RC NR U05188. REMOVE TRUNNION FITTING AND DAMAGED DOUBLER PER MD-11F SRM VOL 2 51-35-01 REV 40. FABRICATED NEW DOUBLER IAW ENGINEERING INSTRUCTION W2008P53B-1311 REV 00. INSTALLED TRUNNION FITTING AND DOUBLER IAW EI W2008A53B-1308 REV 40 . 2 L 7 3 4F RT A22WE 20081205 SO 2008 12 5 LR7A08124 1 20081119 A 5320 STANCHION LKHEED 382 382G 526414U SO FS 770 WL 175 SCRATCHED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 4 4590 DURING POST FLIGHT INSPECTION, CREW NOTED A SCRATCHED STANCHION AT FS 770, WL 175. SCRATCH DETERMINED TO BE BEYOND SER VICEABLE LIMITS, REPAIRED STANCHION IAW SMP583 53-50-24. 2 H 7 4 4T A1SO 20081205 EA 2008 12 5 SWIA200820544 1 20081201 A 3397 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT FAULTY A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 728SK 10192 FLT 6684 - AFT OVERHEAD EMERGENCY LIGHT IN FRONT OF LAV INOP. REPLACED LIGHT ASSEMBLY CONNECTOR. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 QXEA2008120301213 1 20081124 A 2720 RUDDER PEDAL BOMBDR DHC8 DHC8402 1390042 NM LACK OF LUBE A QXEA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 19 405QX 4047 PDX - RUDDER PEDALS NOTICEABLE HARDER TO PUSH TO THE RIGHT SIDE. IT BINDS-UP AND THERE IS A SLIGHT RATCHETING, THEN IT PUSHES THROUGH AND FREES UP. INSPECTED UNDER COCKPIT BEHIND PANELS 121BL AND 122BR FOR ANY SIGNS OF BINDING OR FOREIGN OBJECT DEBRIS, NONE FOUND. LUBRICATED PIVOT POINTS OF RUDDER PEDAL LINKAGES WITH LPS. RUDDER PEDALS OPERATE NORMALLY. COULD NOT DUPLICATE. ALSO, TAXIED AIRCRAFT TO ENSURE NWS SYSTEM NOT AFFECTED. NO DEFECTS. CHECK FLIGHT PERFORMED, NO DEFECTS. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081205 2008 12 5 QXEA2008120301214 4 20081124 A 3418 C16177AC TRANSDUCER BOMBDR DHC8 DHC8402 1390042 NM STALL WARNING FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 19 408QX 4050 PDX - PUSHER SYSTEM FAIL LIGHT ILLUMINATES WHEN AC GENERATORS COME ON LINE. FOUND "L AOA VANE" CB POPPED, POPPED AGAIN WHEN RESET. REMOVED AND REPLACED THE LT AOA TRANSDUCER PER Q400 AMM TASKS 27-33-226-000-801 AND 27-33-26-400-801. FUNC TIONAL TEST GOOD. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081205 NM 2008 12 5 UPS08M53985 1 20081123 A 5321 WSP1133507 FLOORBOARD DOUG MD11 MD11F 3023600 NM AFT CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 272UP 48571 INSPECTION TYPE:N/A AFT LWR PIT FLOOR AT DOOR HAS DAMAGE BEYOND REPAIR. STARTED FABRICATION OF NEW FLOORBOARD FROM AER9 8-5320-0004-1 SP 13580 77 IAW UPS EO MD115320-27386A. COMPLETED REPAIR REF UPS EO MD11-5320-2 7386-A. 2 L 7 3 4F RT A22WE 20081205 NE 2008 12 5 ZZDA2008179 2 20081203 A 7200 BR700715A130 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NR 2 FAILED A ZZDA A UNSCHED LANDING Z Y SIGNIFICANT FAILURE REPORT ENGINE STOPPAGE CL CLIMB 1 SO 37 950AT 55012 DURING CLIMBOUT OF 14,500 HEARD A LOUD BANG. LOST NR 2 ENGINE. NORMAL DESCENT. RAN QRH. LANDING WEIGHT 102,400, MAX TGT 1148. REMOVED AND REPLACED NR 2 ENGINE ON TASK CARD 603 AS REQUIRED. LEAK AND OPS CHECKED GOOD. POWER ASSISTANCE TEST PASSED. 2 L 7 2 4F 4 F TR A6WE E00061EN 20081205 NM 2008 12 5 CALA2008112401097 1 20081123 A 5330 141T3231 SKIN BOEING 767 767224 1385170 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 67158 30437 LIGHTNING STRIKE DAMAGE AT 4 LOCATIONS SEE L/P 8072815 STA 111, 129, 412 STA 111 S-30 DMG DIAM 0.184 IN RIVET HEAD DMG 0 .066 IN. STA 129 S-30 DMG DIAM 0.170 IN RIVET HEAD DMG 0.056 IN. STA 412 S-30 DMG DIAM 0.147 IN RIVET HEAD DMG 0.071IN . WITHIN LIMITS PER SRM 53-00-01. BURNISHED, PUT ON DIP WILL NEED TO REPLACE WITHIN 50 FLIGHTS REFERNCE ECRA 5330-03837 CORRECT STATION NUMBERS ARE AS FOLLOWS (325, 347, AND 412) PERFORMED INTERIM REPAIR AT STATIONS (325, 347 AND 412) PERF ROM INSPECTIONS AT INTERVALS NOT TO EXCEED 30 DAYS AND ACCOMPLISH REPAIR WITHIN 90 DAYS . SEE L/P 8072815 FOR INTERIM RE PAIR ATE STATION 368. INSPECTED INTERIM REPAIRS IAW ECRA 5330-03837, STATORS 325 347 AND 412 NO DEFECTS NOTED. INSPECT 2 L 7 2 4F RT A1NM 20081205 NM 2008 12 5 NWAA085116732 1 20081116 A 3350 BATTERY BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 632NW 23112 DURING OVERNIGHT LINE CHECK FOUND UPPER DECK ESCAPE SLIDE LIGHTS INOP. MX R&R BATTERY. OPS CHECKED GOOD AND ACFT WAS R ETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20081205 EA 2008 12 5 REX2008F00057 1 20081028 A 3250 16735109 RVDT CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8525B 7525 ON CLIMB OUT GOING THROUGH FL270 RECEIVED A NOSE WHEEL STEERING INOPERATIVE CAUTION MASTER CAUTION. QRH FOLLOWED WITH N O FIX. WAS SCHEDULED FOR MEM ASKED FOR LONGEST RUNWAY. LANDING WAS UNEVENTFUL. TOWED TO GATE. R&R THE NOSE WHEEL STE ERING RT STEERING RVDT ROTARY VARIABLE DIFFERENTIAL TRANSFORMER RIGGED STEERING PER BOMBARDIER AMM. 2 L 7 2 4F RT A21EA 20081205 GL 2008 12 5 CVG2008F00002 1 20081006 A 2913 AP6VSC12204 PUMP BOMBDR BD100 BD1001A10 1390044 GL HYDRAULIC SYS FAILED E CVGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 620JF 1127 20059 WHILE CLIMBING OUT OF FL390 THE CREW NOTICED A VIBRATION SHORTLY FOLLOWED BY A CYAN L ENG HYD PUMP FAIL EICAS MSG. THE CREW VERIFIED THE PUMP FAILURE ON THE HYDRAULIC SYNOPTIC PAGE. SOON AFTER A L HYD PRESS LOW CAS MSG WAS RECEIVED. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO KMRY. MX REPLACED LT HYDRAULIC ENGINE DRIVE PUMP EDP AND FLUSHED HYDR AULIC SYSTEM. PERFORMED OPS AND LEAK CHECKS. ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00005NY 20081205 EU 2008 12 5 UALA2008112406642 1 20081124 A 3350 LANYARD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN OUT OF POSITION A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 461UA 1266 LT OVERWING EXIT, EMERGENCY EXIT SIGN INOP. LENS LANYARD OBSTRUCTING ELECTRICAL CONNECTION RE-ADJUSTED. OPS CHECK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20081205 NM 2008 12 5 UALA2008112406651 1 20081124 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 SHEAR TIES CORRODED AT BS 1197+44, AFT FACE AREA BETWEEN STRINGERS 38L & 37R. MAJOR REPAIR. REMOVED CORROSION SHEAR TI E 38L-39L, 39R-39L AND 38R-37R WITHIN LIMITS. SHEAR TIE 39R-38R REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081205 NM 2008 12 5 UALA2008112406652 1 20081124 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 CORRODED SHEAR TIE AT BS 1197-22 FWD FACE AREA BETWEEN STRINGER 39L & 38L. MAJOR REPAIR. REMOVED CORROSION SHEAR TIE 3 8L-39L, 39R-39L AND 38R-37R WITHIN LIMITS. SHEAR TIE 39R-38R REPLACED REF DWG 140T2102 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010900275 20080109 00275 NM 2008 1 9 SWAA080040 1 20080101 A 5330 6545800 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 294 AND BS 312, STR 23R AND STR 25R. REPAIRED SKIN P ER SWA EA. 2 L 7 2 4F RT A16WE 2008010900276 20080109 00276 NM 2008 1 9 SWAA080053 1 20080101 A 3211 654610914 TRUNNION PIN BOEING 737 7373T5 1384608 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 696SW 23064 DURING SCHEDULED C2 CHECK, FOUND RIGHT MLG BEAM CLEVIS TRUNNION PIN CORRODED. REMOVED AND REPLACED CLEVIS PER MT. 2 L 7 2 4F RT A16WE 2008010900277 20080109 00277 NM 2008 1 9 SWAA080050 1 20080101 A 5314 6562125 KEELBEAM BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 696SW 23064 DURING SCHEDULED C2 CHECK, FOUND RT KEEL BEAM CORRODED AT BS 500D TO BS 520. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2008010900278 20080109 00278 NM 2008 1 9 SWAA080018 1 20080101 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 718SW 27852 DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008010900279 20080109 00279 NM 2008 1 9 SWAA080026 1 20080101 A 3397 D40042P CONNECTOR BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 731SA 27863 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND BROKEN CONNECTOR. REMOVED AND REPLACED CONN ECTOR PER MM. 2 L 7 2 4F RT A16WE 2008010900304 20080109 00304 SO 2008 1 9 RAIA00801002 1 20080101 A 2150 CHECK VALVE EMB 145 EMB145LR 3260212 SO RT A/C PACK UNSECURE A RAIA I A I CABIN DEPRESSURIZATION UNSCHED LANDING CABIN DEPRESSURIZATION O OTHER CL CLIMB 1 CE 03 839HK 14500829 FLT 8018 - STL - DURING CLIMBOUT, PRESSURIZATION WAS INOPERATIVE IN AUTO AND MANUAL MODES. MAINTENANCE RESECURED THE RI GHT PACK AIR CHECK VALVE. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008010900310 20080109 00310 SO 2008 1 9 C2XA08IA006 1 20080102 A 7931 23057889 PRESSURE SENSOR EMB 145 EMB145LR 3260212 SO NR 2 ENGINE FAULTY A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 19966 145131 IAH - FLIGHT 2298, THE CREW REPORTED E2 HI OIL PRESSURE WHEN THROTTLES ADVANCED IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE OIL PRESSURE SENSOR, OPERATIO NALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008010900312 20080109 00312 SO 2008 1 9 C2XA08IA005 1 20080102 A 4950 BLEED VALVE EMB 145 EMB145XR 3260214 SO APU FAULTY A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 13123 145688 IAH - FLIGHT 2025, THE CREW REPORTED THAT THE APU CAUSES FUEL SMELL IN THE CABIN. MAINTENANCE PLACED THE APU ON MEL49-0 0-00 CTL 136251, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE R &R THE APU SERVO BLEED VALVE, OPE RATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND TEH AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008010900322 20080109 00322 NM 2008 1 9 SWAA080066 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010900324 20080109 00324 NM 2008 1 9 SWAA080067 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010900332 20080109 00332 NM 2008 1 9 SWAA080083 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010900334 20080109 00334 NM 2008 1 9 SWAA080082 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010900338 20080109 00338 NM 2008 1 9 SWAA080078 1 20080102 A 5754 65C26602 SKIN BOEING 737 7375H4 138449D NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 L/E SLAT SKIN CRACKED AT OUTBOARD T/E. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 UALA2008112406636 1 20081123 A 3350 60443 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 671UA 30026 LONG EEL FLOOR STRIP IN AFT GALLEY IS INOP. REPLACED EEL STRIP. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081205 NM 2008 12 5 UALA2008112406637 1 20081123 A 2560 KI10112 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FLASHLIGHT FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 FLASHLIGHT FWD GALLEY NEEDS BATTERIES REPLACED. REPLACED BATTERY AND RESEALED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081205 NM 2008 12 5 UALA2008112406653 1 20081124 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 TWO SHEAR TIES CORRODED AT BS 1197+22 AFT FACE AREA BETWEEN STRINGERS 39L & 38R. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS OF SRM 53-00-07. 2 L 7 2 4F 4 F RT A1NM E24NE 20081205 NM 2008 12 5 UALA2008112406654 1 20081124 A 5320 FLOOR SUPPORT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 MAIN CABIN STA 785.9, LBL 12 FLOOR SUPPORT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION, STA 785 TO 805, AT LBL 12. INSTALLED FILLER & ANGLE REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081205 WP 2008 12 5 AALA200810263 1 20081107 A 5320 SILL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 MIDDLE CARGO DOOR CUT-OUT LOWER SILL HAS CORROSION, STATION 636 TO STATION 693. REMOVED CORROSION FROM DOOR CUT-OUT LOWE R SILL, TREATED AND PRIMED AREA AND INSTALLED DOUBLER AND SEAL RETAINER PER AARD53-10-00-3. 2 L 7 2 4F RT A6WE 20081205 NM 2008 12 5 AALA200820054 1 20081106 A 5320 146N56511 FLOOR SUPPORT BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 666A 52891 25300 FLOORBOARD SUPPORT CORRODED, REPAIRED IAW SRM 53-60-51-2R1. 2 L 7 2 4F RT A2NM 20081205 WP 2008 12 5 AALA200810278 1 20081113 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 WORN AREA ON FORWARD SIDE LEFT 1380 FRAME. REMOVED DAMAGE AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 20081205 WP 2008 12 5 AALA200810264 1 20081109 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION ON LEFT CUSP. INSTALLED DOUBLERS ON CUSP AFTER CORROSION REMOVAL PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081205 WP 2008 12 5 AALA200810250 1 20081106 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION FOUND ON SCREW HOLE IN CUSP WEB. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER AARD 53-20-00-10. 2 L 7 2 4F RT A6WE 20081205 NM 2008 12 5 ASAA0843925 1 20081029 A 5311 65465553 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED STA 787 STR 8 9L. CUTOUT DAMAGE FABRICATED AND INSTALLED REPAIR ANGLES AND FILLER IAW ASA EA 400 53EA 002 67. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 UALA2008112506660 1 20081122 A 3350 7003121 SIGN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INTERMITTENT A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY EXIT SIGN AT 2L GOES ON AND OFF UNCOMMANDED. EXIT SIGN OPS CHECKED OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081205 NM 2008 12 5 UALA2008112506661 1 20081124 A 4960 211734220 CONTROLLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 543UA 25698 APU INOP. CAUSE WAS FOUND TO BE THE APU CONTROLLER. THIS PART HAS BEEN CHRONIC AND HAS A LONG HISTORY OF NFF. 2 L 7 2 4F 4 F RT A2NM E17NE 20081208 NM 2008 12 8 SWAA086773 1 20081202 A 3350 8210248801 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 446WN 29842 FOUND OVERWING EMERGENCY EXIT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081208 EA 2008 12 8 ASOA200801517 1 20081113 A 5320 SILL CNDAIR CL600 CL600* 1900302 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 FS 280 O/B LBL 9 UPPER SILL CRACKED APPROX .50 INCH LONG. REMOVED DAMAGED AREA OF FLOOR ANGLE AS SHOWN ON SH 3 AND MADE REPAIR ANGLE FROM PN 600-34017-595 IAW REO 601R-53-11-138. C/W STEPS 1-10 OF INC REO 601R-53-11-138 REV NC. PERFORMED L PI OF CUT FABBED PARTS AND INSTALLED. INSTALLED SAME SERVICEABLE ALTERNATE RELEASE CABLE PULLEY BRACKET AT FS 280 OTBD OF LBL 9 IAW SRM 51-41-02. C/W ECTC REO 601R-53-11-138. OPS TEST OF ALTERNATE RELEASE GOOD IAW AMM 32-34-00-710-801. 2 L 7 2 4F RT A21EA 20081208 SO 2008 12 8 C2XA08TY136AA 1 20081201 A 5521 14527273008 RIB EMB 145 EMB145XR 3260214 SO ZONE 300 BURNED A C2XA O OTHER O OTHER DE DESCENT 1 SW 27 21154 145772 RT ELEVATOR TIP FAIRING SUPPORT NUT PLATE FASTENER HOLE WAS ELONGATED FROM A LIGHTNING STRIKE. THE DAMAGED TIP WAS CUT OUT AND A FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW EC5520-01162. THE ELEVATOR WAS REMOVED, BALANCED, AND IN STALLED IAW EMB AMM 27-30-00. 2 L 7 2 4F RT 20081208 EA 2008 12 8 ASOA200801539 1 20081119 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 927EV 7844 PAX DOOR FWD WEB HAS CRACKS IN RADIUS WHERE STAIRS 832DT AND CT MEET, 832CT AND MIC FIXED STEPS MEET. REPAIRED PAX DOOR FWD WEB IAW REO 601R-52-11-702. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 ASOA200801542 1 20081119 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 PASSENGER DOOR INNER SKIN HAS CORROSION AROUND FASTENER HOLES UNDER ACCESS PANELS 832AL, 832BL, 832CL, AND 832EL. CORRO SION IS MINOR SURFACE CORROSION. REMOVED MINOR CORROSION IAW SRM 51-21-06. 2 L 7 2 4F RT A21EA 20081208 CE 2008 12 8 Z5FA111408N304CS1 1 20081114 A 2130 OUTFLOW VALVE CESSNA 500 550 2076604 CE CABIN PRESSURE MALFUNCTIONED E Z5FA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 63 304CS 5500847 AT FL 370 CABIN STARTED TO CLIMB AT 2000 FPM. CREW DECLARED AND EMERGENCY AND DIVERTED TO KBUR. PRESSURIZATION SYSTEM WAS DIFFERED PER MEL AND AIRCRAFT REPOSITIONED TO KLGB (CITATION SERVICE CENTER) FOR PRESSURIZATION MEL MAINTENANCE. FOU ND HARDWARE CONNECTING AIR LINES TO OUTFLOW VALVE STRIPPED. REPLACED ASSOCIATED HARDWARE, PRESSURE, LEAK AND OPERATIONA L CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4F A22CE 20081205 EU 2008 12 5 UALA2008112406638 1 20081123 A 5210 FE1740011 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 461UA 1266 THE 2R DOOR ASSIST BOTTLE PRESS LOW. SERVICED BOTTLE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081205 EU 2008 12 5 UALA2008112406645 1 20081122 A 5320 DOUBLER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 403UA 442 LT DOOR SILL DOUBLER OUTBOARD HAS 2 CRACKS (MARKED). MAJOR REPAIR ACCOMPLISHED. REPLACED SILL SHAPE (DOUBLER), AT DOOR 2L. 2 L 7 2 4F 4 F RT A28NM E40NE 20081205 NM 2008 12 5 AALA200802351 1 20081017 A 3397 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 196AA 32390 MIA - EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081205 WP 2008 12 5 AALA200810247 1 20081104 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 FORWARD ENTRY DOOR JAM AFT WEB CRACKED AT L-11 STATION 209. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW AARD 53-10-00-11. 2 L 7 2 4F RT A6WE 20081205 WP 2008 12 5 AALA200810256 1 20081108 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 RIGHT CUSP HAS CORROSION AT STATION 731 TO 750. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081205 WP 2008 12 5 AALA200810257 1 20081108 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 RIGHT CUSP HAS CORROSION AT STATION 712 TO 731. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081205 WP 2008 12 5 AALA200810260 1 20081108 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION ON OUTBOARD LEG OF SEAT TRACK NR 2, STATION 1150 TO STATION 1160. INSTALLED SEAT TRACK NR 2 SPLICE PER SRM 53 -05-01. 2 L 7 2 4F RT A6WE 20081205 WP 2008 12 5 AALA200810261 1 20081108 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION ON SEAT TRACK NR 5 INBOARD FLANGE AT STATION 200 TO STATION 204. INSTALLED SEAT TRACK SPLICE PER 53-05-01. 2 L 7 2 4F RT A6WE 20081205 WP 2008 12 5 AALA200810276 1 20081111 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION ON RIGHT CUSP. REMOVED AND REPLACED CUSP. 2 L 7 2 4F RT A6WE 20081205 WP 2008 12 5 AALA200810277 1 20081112 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION ON RIGHT CUSP. INSTALLED NEW CUSP. 2 L 7 2 4F RT A6WE 20081208 NM 2008 12 8 SWAA086815 1 20081203 A 3397 W998593020 WIRE BOEING 737 737317 138447P NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EXIT MARKER WIRE LOOSE. REPAIRED WIRE PER MM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086782 1 20081203 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086757 1 20081202 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, BETWEEN STR 27L TO 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081208 2008 12 8 SWAA086758 4 20081202 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086759 1 20081202 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081208 2008 12 8 SWAA086828 4 20081204 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081208 2008 12 8 SWAA086829 4 20081204 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086764 1 20081202 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081208 GL 2008 12 8 SWAA086765 2 20081203 A 7532 328255621 MOTOR BOEING 737 7373T0 1384582 NM CFMINT CFM56 CFM563B1US GL NR 1 ENGINE FAULTY A SWAA K NONE O OTHER CL CLIMB 1 SW 29 697SW 23838 DURING SCHEDULED OTS CHECK, FOUND NR 1 ENG UNABLE TO MAKE CLIMB POWER. REMOVED AND REPLACED VBV GEAR DRIVE MOTOR ASSY P ER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 20081208 NM 2008 12 8 SWAA086767 1 20081203 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 255WN 32513 FOUND R2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 HALA2008112300872 1 20081123 A 5751 STRUCTURE BOEING 767 7673CB 1385187 NM LT WING AILERON DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 592HA 28141 FOUND DAMAGE TO LT WING OTBD AILERON OTBD STATIC WICK. OK TO CONTINUE. 2 L 7 2 4F RT A1NM 20081208 EA 2008 12 8 SWIA200820558 1 20081001 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 919SW 7657 DURING C-CHECK, FS 280 RBL 11 ANGLE CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820559 1 20081001 A 5320 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 919SW 7657 DURING C-CHECK, FS 280 SUPPORT BRACKET RADIUS CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820560 1 20081003 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 862AS 7476 DURING C-CHECK, FS 625 LEFT AND RIGHT CLIPS CRACKED. REPLACED PER REO. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820562 1 20081003 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 862AS 7476 DURING C-CHECK, FS 280 LBL 9 LOWER FLOOR SUPPORT CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820563 1 20081003 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 862AS 7476 DURING C-CHECK, FS 280 RBL9 FLOOR SUPPORT AND CLIPS CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820564 1 20081003 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 862AS 7476 DURING C-CHECK, FS 280 UPPER FLOOR SUPPORT AT RBL9 CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820565 1 20081203 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 938SW 7741 FLT 6445 - RIGHT SIDE FORWARD EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820548 1 20081017 A 3210 BOLT CNDAIR CL600 CL6002C10 1390015 EA RT MLG CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 727SK 10191 DURING C-CHECK, RIGHT MLG INBOARD RETRACT ACTUATOR BRACKET BOLT CORRODED. REPLACED PER CMM. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820549 1 20080930 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 969SW 7876 C-CHECK, AFT PRESSURE BULKHEAD FORWARD FITTING CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820550 1 20080930 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 969SW 7876 C-CHECK, FS 280 RBL9 UPPER FLOOR SUPPORT ANGLE CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820551 1 20080930 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 969SW 7876 C-CHECK, FS 280 LBL9 LOWER FLOOR SUPPORT CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081208 SO 2008 12 8 SIMA200832201 1 20081112 A 3350 20131A POWER SUPPLY EMB 135 EMB135KL 3260302 SO SEAT 3 B/C UNKNOWN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 854AE 145743 ON FLIGHT 3023 CREW REPORTED EXIT SIGN FWD OF SEAT 3 B/C AND FLOOR PROX STRIPS FORWARD OF ROW 6 ARE INOPERATIVE. AIRCRA FT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY NUMBER 2 IAW EMB -140 AMM 33-50-04, OPERAT ION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081208 EA 2008 12 8 ASOA200801545 1 20081119 A 5320 SILL CNDAIR CL600 CL600* 1900302 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 FLOOR SILL AT 280 RBL 45 CORRODED. REPAIRED FLOOR SILL AT FS280 RBL45 PER REO 670-53-21-139 REFER TO M-234 FORM FOR WO RK ACCOMPLISHED JOB COMPLETED. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 A6WA200840602 1 20081028 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 450AW 7823 AFT PRESSURE BULKHEAD WEB FS 621.00 AT THE LINTEL ATTACHMENT INSTALLATION IS CRACKED. AFT PRESSURE BULKHEAD WEB FS 621. 00 LINTLE INSTALLATION REPAIRED IAW REO 601R-53-61-1230 REV D. 2 L 7 2 4F RT A21EA 20081208 NM 2008 12 8 SWAA086810 1 20081203 A 5311 6547959 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 807, BETWEEN STR 25L TO STR 26L. REPAIRED FRAME PER SR M. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086811 1 20081203 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086774 1 20081202 A 3350 41A2212A LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 497WN 32479 FOUND R2 DOOR EMERGENCY EXIT LENS BROKEN. REPAIRED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081208 EU 2008 12 8 MALA080208 1 20081123 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 433XJ 340B433 SEVERAL DENTS NOTED IN CARGO DOOR OUTER SKIN. REPAIRED IAW EO NR S52028, S52151. 2 L 7 2 4T RT A52EU 20081208 NM 2008 12 8 USAA2008120492182 1 20081106 A 5330 143N3691 SKIN BOEING 757 7572S7 1384962 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 904AW 23566 MCN - MAJOR REPAIR - C12 CHECK - LEVEL 2 CORROSION ON FUSELAGE SKIN AT BS 749, S22R. REPAIRED FUSELAGE SKIN AT BS 749, S22R IAW EA 130154. 2 L 7 2 4F RT A2NM 20081208 NM 2008 12 8 USAA2008120492183 1 20081123 A 5320 D534711240200 WEB AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 808AW 1088 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON SHEAR PLATE WEB AT FR 69 - FR 70, +Y1732. REPLACED SHEAR PLATE WEB AT FR 6 9 - FR 70, +Y1732 IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081208 NM 2008 12 8 USAA2008120492184 1 20081202 A 5320 65C10592155 FLOOR SUPPORT BOEING 737 7374B7 138449C NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - MAJOR REPAIR - Q2 CHECK - CORROSION ON FLOOR SUPPORT INTERCOSTAL AT BS 947 - BS 967, RBL 16. REPLACED FLOOR SUPPO RT INTERCOSTAL AT BS 947 - BS 967, RBL 16 IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081208 WP 2008 12 8 FDEA200812025049 1 20081202 A 5411 SPAR DOUG MD10 MD1010F 3022112 WP NR 3 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 387FE 46621 NR 3 PYLON HORIZONTAL UPPER SPAR WEB HAS 4 INCH CRACK, REFERENCE INSPECTION OF PYLON S177 WORKCARD 54X1201ALI-P2. COMP LIED WITH HFEC. VERIFIED NR 3 PYLON HORIZONTAL UPPER SPAR WEB HAS CRACKED INDICATION PER NDTSPM. REMOVED AND FABRICA TED NEW WEB REF DWG AUB7031 AND SRM 51-00-01 VOL 2. INSTALLED WEB REF DWG AUB7031 AND SRM 54-20-00 FIG. 27 SHT 1. 2 L 7 3 4F RT A22WE 20081229 SO 2008 12 29 C2XA08SH160 1 20081218 A 5751 SHROUD EMB 145 EMB145LR 3260212 SO ZONE 600 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 48901 501 SHV DURING C-CHECK RT AILERON LOWER SHROUD HAD CORRODED BONDING PLATE. MX REPAIRED RT AILERON LWR SHROUD IAW EC 5750-01 315 (E). THE ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081229 SO 2008 12 29 C2XA08SH162 1 20081218 A 5751 SHROUD EMB 145 EMB145LR 3260212 SO ZONE 500 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 48901 501 SHV DURING C-CHECK LT AILERON LOWER SHROUD HAD CORRODED BONDING PLATE. MX REPAIRED LT LOWER AILERON SHROUD IAW EC 5750- 01315 (E). THE ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081229 NM 2008 12 29 ASAA0844036 1 20081209 A 5512 657378212 SKIN BOEING 737 7374Q8 138447Q NM HORIZONTAL STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 RT STABILIZER LEADING EDGE SKIN HAS DENT ON STA 243 TO STA 254. REMOVED DAMAGE SECTION OF SKIN AND INSTALLED EXTERNAL DO UBLER WITH BLIND FASTENERS PER SRM 55 10 01 REPAIR 3. 2 L 7 2 4F RT A16WE 20081229 EA 2008 12 29 A6WA200840627 1 20081203 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 414ZW 7586 CRACK FOUND ON BRACKET FS 280 RBL 9 INBD CRACK LENGTH IS .200. BRACKET AT FS 280 RBL 9 REMOVED IAW SRM 51-42-13 AND 51- 42-21. NEW BRACKET AT FS RBL 9 INSTALL IAW 51-42-20. 2 L 7 2 4F RT A21EA 20081229 SO 2008 12 29 C2XA08RI181 1 20081217 A 3350 3025103 HOUSING EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT DETERIORATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16178 14500889 RIC - DURING ROUTINE INSPECTION, RIC MX FOUND LT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. MX R&R LT FORWARD OVERWI NG EMERGENCY LIGHT HOUSING AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081229 EA 2008 12 29 A6WA200840636 1 20081203 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 414ZW 7586 CRACK FOUND ON PILOT BULKHEAD FS 280 RBL 9. CRACK LENGTH IS .500. PILOT BULKHEAD FS 280 RBL 9 REPAIRED IAW CRJ 200 REO 601R-53-11-171 REV D. 2 L 7 2 4F RT A21EA 20081229 NM 2008 12 29 SWAA087331 1 20081222 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 462WN 32466 DURING SCHEDULED HC1 CHECK, FOUND RT EEPLS COVERS CRACKED. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081229 2008 12 29 SWAA087333 4 20081222 A 2565 LATCH BOEING 737 7377H4 1384404 NM EVAC SLIDE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 462WN BNG9330 32466 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR SLIDE SHROUD LATCH BROKEN. REMOVED AND REPLACED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087334 1 20081223 A 5330 6545800 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 258, BETWEEN STR 22L TO STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081229 WP 2008 12 29 AALA200810515 1 20081218 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS WEAK A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 465A 49595 BATTERY PACK TESTED DIM, REF- AMM 33-60-98-4. INSTALLED SERVICABLE BATTERY PACK. 2 L 7 2 4F A6WE 20081229 WP 2008 12 29 AALA200810511 1 20081211 A 3350 5016 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS WEAK A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 463AA 49593 EMERGENCY LIGHTING BATTERY PACK TESTED WEAK (AMM 33-60-98-4). INSTALLED A SERVICEABLE BATTERY PACK. 2 L 7 2 4F A6WE 20081229 WP 2008 12 29 AALA200810513 1 20081211 A 3350 5016 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT WEAK A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 463AA 49593 EMERGENCY LIGHTING BATTERY PACK TESTED WEAK (AMM 33-60-98-4). INSTALLED A SERVICEABLE BATTERY PACK. 2 L 7 2 4F A6WE 20081229 NM 2008 12 29 AALA200820096 1 20081205 A 5543 TAB BOEING 777 777223 1385213 NM RUDDER DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 761AJ 27651 31478 RUDDER HAS DAMAGE 1.25 INCH IN DIAMETER 11 INCH FROM LEADING EDGE AND 8 INCH FROM BOTTOM SIDE OF TAB RT SIDE. RUDDER RE PAIRED IAW SRM 51-70-04-2R AND EA NUMBER COMP 5T-00506 CURED PER FIG 211. 2 L 7 2 4F RT T00001SE 20081229 NM 2008 12 29 SWAA087297 1 20081222 A 5753 6573732 SKIN BOEING 737 7373L9 1384470 NM FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND LT WING O/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 AALA200820098 1 20081210 A 5340 146N52932 MOUNT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 609AA 45862 27447 LAVATORY MOUNT CORRODED, RERLACED MOUNT IAW SRM 51-10-02 2 L 7 2 4F RT A2NM 20081229 NM 2008 12 29 AALA200820099 1 20081210 A 5340 65B5783942 MOUNT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 609AA 45862 27447 CORROSION ON LAVATORY MOUNT FITTING RT SIDE AFT LAVATORY, REPLACED FITTING IAW SRM 51-00-02. 2 L 7 2 4F RT A2NM 20081229 NM 2008 12 29 AALA200810518 1 20081212 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 FLOORBOARD SUPPORT CORRODED AT STATION 953 NUT PLATE HOLE. INSTALLED A SERVICEABLE FLOOR SUPPORT PER SRM 51-10-02-0G. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087298 1 20081221 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 214WN 32486 EEPLS TRACK CRACKED AT ROW 11. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081229 WP 2008 12 29 AALA200810534 1 20081207 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 FLOORBOARD SUPPORT CRACKED UNDER BOARD C-14 STATION 1060. INSTALLED A SERVICEABLE SUPPORT PER SRM 51-01. 2 L 7 2 4F A6WE 20081229 NM 2008 12 29 AALA200820105 1 20081211 A 5320 141N516Y54 CHANNEL BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 609AA 45862 27447 CHANNEL CORRODED AT GALLEY MOUNT, REPLACED CHANNEL IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20081229 NM 2008 12 29 SWAA087302 1 20081221 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 982 STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 UALA2008122206953 1 20081221 A 2432 18550000 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE MAIN FAULTY A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION IN INSP/MAINT 1 WP 29 642UA 25092 BATTERY DISCHARGE LIGHT ILLUMINATED. REPLACED SHIP'S BATTERY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081229 NM 2008 12 29 UALA2008122206939 1 20081220 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY EXIT LIGHT INOP AT DOOR 3 RIGHT FWD SILL LIGHT. RELAMPED EMERGENCY LIGHT, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081229 NM 2008 12 29 UALA2008122306967 1 20081222 A 4990 38762112600U SENSOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE APU FAILED A UALA D RETURN TO BLOCK W INADEQUATE Q C IN INSP/MAINT 1 WP 29 227UA 30555 APU SHUTDOWN AT GATE FOR LOW OIL QTY MAT FAULTING OIL QUANTITY-SUMP TEMPERATURE SENSOR. REPLACED APU OIL QTY-SUMP SENSO R. OPS CHECK NORMAL. NO MESSAGES. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081229 NM 2008 12 29 UALA2008122306973 1 20081223 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 RT OVERWING EMERGENCY LIGHTS FWD AND AFT INOP. REPLACED BATTERY, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081229 NM 2008 12 29 UALA2008122306974 1 20081223 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 FWD EXIT SIGN LIGHT INOP DOOR 4L. REPLACED FEEDER CABLE, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081229 NM 2008 12 29 UALA2008122306975 1 20081223 A 3397 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 LT SEAT EEL LIGHTS INOP 45ABC TO 53ABC. REPLACED FEEDER CABLE, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081229 NM 2008 12 29 UALA2008122306976 1 20081223 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 LT B-ZONE EMERGENCY CEILING LIGHT INOP. RELAMPED EMERGENCY LIGHT, OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081229 2008 12 29 UALA2008111303713 4 20080703 A 3140 S243W0011201 MODULE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT INOPERATIVE A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 215UA 30221 HIGH GAIN AND SAT SYS STATUS MESSAGE. FOUND LEFT AIMS IOM 3 INOP. REPLACED IOM 3. MESSAGES CLEARED AND VERIFIED OPS S OFTWARE INSTALLED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081229 NM 2008 12 29 SWAA087305 1 20081222 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087313 1 20081222 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RT R1 DOOR LOWER HINGE CUTOUT, BS 290, WL 228. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 AALA200820093A 1 20081119 A 5340 146N87264 FITTING BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 56842 24599 BATHTUB FITTING CORRODED, REPLACED FITTING IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20081229 WP 2008 12 29 AALA200802389A 1 20081024 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 439AA 49457 LGA - EMERGENCY LIGHT OVER RIGHT AFT EMERGENCY EXIT INOPERATIVE. REPLACED BATTERY PACK AT B5105. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081229 EU 2008 12 29 AALA200802391A 1 20081023 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 18066 509 MIA - EMERGENCY LIGHTS AT RIGHT NUMBER TWO DOOR INOPERATIVE. CHARGED EMERGENCY LIGHT SYSTEM. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A35EU 20081229 NM 2008 12 29 UALA2008111302305 1 20080419 A 3230 CIRCUIT CARD BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LANDING GEAR FAULTY A UALA O OTHER W INADEQUATE Q C AP APPROACH 1 WP 29 374UA 24639 LANDED UNDER AMBER ALERT DUE TO NOSE GEAR PROBLEM. PER CREW, ONLY HAD A RED NOSE GEAR LIGHT ILLUMINATED ON APPROACH. D ID A FLY BY, TOWER ADVISED IT LOOKED LIKE ALL 3 GEAR WERE DOWN. CREW VERIFIED NOSE DOWN THROUGH VIEWPORT. CAPT WENT BA CK IN THE CABIN AND OPERATED MLG DOWN AFTER FINDING YELLOW INDICATOR STRIP. CAPT DID SAY AFTER CB RESET ALL INDICATIONS NORMAL. RANG OUT SENSORS S845 AND S846 ON NOSE LANDING GEAR. BOTH WITHIN LIMITS. FOUND BOTH LAMPS INOP ON GREEN LIGH T FOR NOSE GEAR, RELAMPED GREEN LIGHT OPS NORMAL WITH GEAR DOWN. SUSPECT M1215 CARD. CYCLED MLG AND NLG 6 TIMES FROZE SENSORS ON NLG. COULD NOT DUPLICATE PROBLEM, BUT SUSPECT M1215 CARD PER T-S MANUAL. REPLACED M1215 CARD. CYCLED NOSE 2 L 7 2 4F 4 F RT A16WE E21EU 20081229 NM 2008 12 29 UALA2008111302866 1 20080518 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 305UA 23666 STA 294.5 FRAME AT STR 11L HAS TOOLING MARK. REPAIRED PER UA-EVA-71570 AND REO-L01074. THIS IS A TIME LIMITED REPAIR F OR 12 MONTHS. BOEING MUST ISSUE A NEW 8100-9 ON OR BEFORE 17MAY2009. RECEIVED FIRST STAGE APPROVAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20081229 2008 12 29 AALA200802395A 4 20081025 A 2297 WIRE HARNESS DOUG DC9 DC982 3022082 WP DISPLAY SHORTED A AALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SW 21 214AA 49162 BOS INFLIGHT - DURING CLIMB AT 300 FEET ALTERNATE ALERT WINDOW WENT BLANK. AUTOPILOT AND AUTO THROTTLE ONE AND TWO INOP ERATIVE. CIRCUIT BREAKER POPPED. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. FOUND WIRING FAULTS. REPAIRED SHORTED WIRE IN AFT ACCESSORY COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081229 NM 2008 12 29 UALA2008122206931 1 20081219 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 554UA 26644 FWD CARGO COMPT, FRAME HAS A DENT BS 520 AND BETWEEN STR 24L-25L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTAL LED J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081229 NM 2008 12 29 ASAA0854073 1 20081217 A 2161 6228145 CONTROLLER BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 579AS 2110 35187 ON RECALL LT PACK LIGHT ILLUMINATED GROUNDED YES. BITE TEST ON ZONE TEMP CONT. NR 1 SHOWS TCV FAULT THIS PACK. PERFORM ED GROUND FUNCTIONAL TEST AND PACK ZONE TEMP CONTROLLER BITE TEST. NO FAULTS FOUND. OPS CHECK GOOD REF FIM TASK 21 00 00 800 REF AMM 21 61 00. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 ASAA0854080 1 20081218 A 2161 3989083 MODULE BOEING 737 737890 1384527 NM NR 2 PACK FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 566AS 21106 35181 NR 2 ZONE/TEMP CONTROLLER BITE TEST FAILS FLIGHT DECK TRIM VALVE GROUNDED YES. R&R FLIGHT DECK TRIM VALVE. BITE CHECK OK. REF MM 21 61 21/401. REQUIRES LEAK CHECK. 3922 INSTALLED PART NR VERIFIED BY SEAMC PAT. BATCH NR 867780. LEAK CH ECK GOOD. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 ASAA0854083 1 20081220 A 2430 115195211 PCU BOEING 737 737890 1384527 NM COCKPIT MALFUNCTIONED A ASAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 583AS 29626 35681 `ELEC` LIGHT ILLUMINATED ON OVERHEAD PANEL GROUNDED YES. TRIED TO CLEAR THE FAULT AND NO HELP. CYCLED NORMAL AND STAND BY SPCU C/B AND CLEARED FAULT REF MM FIM 24 34 00 810 802 SPCU. OPS CK GOOD. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 UALA2008122607012 1 20081226 A 4930 388250017 FUEL CONTROL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 547UA 25368 AIRCRAFT RTFL DUE TO APU NO START AT ALTITUDE. PILOT REPORTS: APU HUNG AT 27 PERCENT DURING ALTITUDE OF 34,000 MSL AND THEN FAULTED, SHUT DOWN. REPLACED APU FUEL CONTROL DUE TO FAULTY FUEL SOLENOID. 2 L 7 2 4F 4 F RT A2NM E17NE 20081230 NM 2008 12 30 UALA2008122306980 1 20081221 A 2621 3490000433601U EXTINGUISHER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CARGO BAY LOW PRESSURE A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 174UA 24381 PRIOR TO DEPT CREW REPORTED BTL LOW CARGO A DISPLAYED. FIRE EXTINGUISHER REPLACED. CMC GRD FIRE TEST PASS. 2 L 7 4 4F 4 F RT A20WE E24NE 20081230 NM 2008 12 30 UALA2008111302728 1 20080511 A 5320 CHANNEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 307UA 23668 THE FOLLOWING CRACKS WERE FOUND FROM SB737 -53A1204 INSPECTION. STR 14L CHANNEL STA360, CLIP STR 11L STA 360, CLIP STR 11L STA 294.5, CLIP STR 12L STA 294.5, INTERCOSTAL WEB STR 11L STA 294.5, STRAP STR 16L STA 348 AND CLIP STR 15L STA 348 . MAJOR REPAIRS. REPAIRS ACP PER UA-EVA-71543 AND REO-L01071. AREAS TO BE REINSPECTED WITHIN 6000 CYCLES AND EVERY 60 00 CYCLES THEREAFTER. CURRENT PTC 35911 41911 CYCLES IS FIRST REINSPECTION. PER SB737-53A1204. 2 L 7 2 4F 4 F RT A16WE E21EU 20081230 NM 2008 12 30 UALA2008111302758 1 20080512 A 5320 CHANNEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 308UA 23669 CRACKS WERE FOUND AT THE FOLLOWING LOCATIONS: STR 15L SPLICE CHANNEL STA 360, STR 11L & 10L CLIPS STA 360, STR 11L & 12 L CLIPS STA 294.5, INTERCOSTAL WEB STR 7L STA 294.5, INTERCOSTAL ATTACH ANGLE STR 15L STA 348, UPPER AND LWR INTERCOSTAL ATTACH ANGLES STR 16L STA 348 AND VERTICAL PLATE STR 16L STA 348. MAJOR REPAIRS. REPAIRS ACP PER UA-EVA-71542 AND REO -L01070. AREAS TO BE REINSPECTED WITHIN 6000 CYCLES AND EVERY 6000 CYCLES THEREAFTER. CURRENT PTC 35539. 41539 CYCLES IS FIRST REINSPECTION. PER SB 737-53A1204. 2 L 7 2 4F 4 F RT A16WE E21EU 20081230 NM 2008 12 30 UALA2008111303551 1 20080623 A 5512 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 RT STABILIZER LEADING EDGE HAS A APPROX 1-2 IN DENT OR CRACK ON RIVET ROW APRROX 11 RIBS OUT FROM FUSELAGE. REMOVED SKI N DAMAGE TO ACCESS RIB. FOUND RIB DENTED .040" WITH GOUGE. BLENDED AND REWORK. ACP HFEC INSPECTION AND CONFIRMED NO CR ACKS. INSTALLED INTERIM RPR ON SKIN REF SRM 55-10-01 REPAIR 3. 2 L 7 2 4F 4 F RT A16WE E21EU 20081230 NM 2008 12 30 UALA2008122406982 1 20081223 A 3610 79027013 SHUTOFF VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE NR 1 ENGINE FAILED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 675UA 29243 LEFT HPSOV EICAS ON TAKEOFF ROLL LOW SPEED ABORT. HP VALVE LOCKED CLOSED. HP VALVE REPLACED. REPLACED LEFT ENG HP CON TROLLER. 2 L 7 2 4F 4 F RT A1NM E24NE 20081230 NM 2008 12 30 UALA2008122206932 1 20081219 A 3397 58781 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 554UA 26644 G4A GALLEY EMERGENCY LIGHT FEEDER CABLE DAMAGED. RE-TERMINATED AND INSTALLED G4A GALLEY EMERGENCY LIGHT FEEDER CABLE A ND LIGHT ASSY, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081230 NM 2008 12 30 UALA2008122206942 1 20081220 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY EXIT EMERGENCY LIGHTS VERY DIM AT DOOR 5 RIGHT AFT. LOWER WALL GALLEY AND DOOR 5 RIGHT FWD EXIT SIGN. REPLAC ED POWER FEEDER CABLE. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081230 NM 2008 12 30 UALA2008122406995 1 20081223 A 5311 FRAME AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 807UA 798 CORROSION ON TOP OF FRAME 59, AFT PIT FLOOR JUST AFT OF PIT DOOR. MAJOR REPAIR. INSTALL STRAP REPAIR PER TIMCO REO-L01 119. OBTAINED APPROVAL FROM AIRBUS VIA RAS-DAHAM-4900705-2008. ON NR K0145C BY 310884 AND INSPECTED BY LC67. THIS IS A PERMANENT REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 20081230 NM 2008 12 30 UALA2008122206943 1 20081220 A 3350 20131A POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 RIGHT OVERWING EXTERIOR EMERGENCY EXIT LIGHTS INOP 4 EA LIGHT ASSY'S. REPLACED POWER SUPPLY. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081230 NM 2008 12 30 UALA2008122206933 1 20081219 A 3397 58781 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 554UA 26644 A-ZONE EEL SEAT CABLE DAMAGED. REPLACED CONNECTOR, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081230 NM 2008 12 30 UALA2008122206934 1 20081219 A 3397 58781 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A-ZONE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 554UA 26644 A-ZONE EMERGENCY LIGHT SEAT FEEDER CABLE DAMAGED. REPAIRED WIRES, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081230 NM 2008 12 30 AALA200802411A 1 20081026 A 8012 9798269 START VALVE BOEING 767 767323 1385205 NM NR 1 ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 355AA 24036 MIA INFLIGHT - CREW REPORTED ENGINE STARTER CUTOUT INDICATION 15 MINUTES AFTER TAKEOFF. RETURNED TO MIA AND LANDED WIT HOUT INCIDENT. REPLACED START VALVE FOR NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081230 WP 2008 12 30 AALA200802413A 1 20081027 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7525A 49917 LGA - EXTERIOR EMERGENCY LIGHTS AT AFT CARGO COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGH TS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081230 NM 2008 12 30 AALA200802414A 1 20081027 A 3350 LENS BOEING 737 737823 13844CB NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 961AN 30092 DFW - FORWARD GALLEY MOUNTED EMERGENCY EXIT IDENTIFIER LENS MISSING. REPLACED LENS FOR FORWARD GALLEY MOUNTED EMERGENCY EXIT IDENTIFER LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 AALA200802415A 1 20081027 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 26G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081230 EA 2008 12 30 COMA2008122450045 1 20081224 A 3010 11513361 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYSTEM FAULTY A COMA G O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SO 27 713CA 22356 7245 DURING CRUISE FLIGHT RECEIVED A LEFT WING ANTI-ICE MESSAGE, FLGIHT DIVERTED TO GSO. REPLACED THE ANTI-ICE CONTROLLER. 2 L 7 2 4F RT A21EA 20081230 EA 2008 12 30 COMA2008122350043 1 20081222 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 720SW 7297 ON CLIMBOUT FROM JFK RECEIVED FLAPS FAIL CAUTION MSG, AT 8 DEG. EMERGENCY DECLARED, A/C RETURNED TO JFK LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW UP MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 20081230 NM 2008 12 30 HNAA2008121000350 1 20081212 A 2434 23088008 GENERATOR DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE MALFUNCTIONED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 824EX 11749 345 387 NR 2 DC GENERATOR WOULDN'T COME ON LINE, NR 2 DC GENERATOR HOT CAUTION LIGHT ILLUMINATED AND SMOKE AND SPARKS CAME FROM NR 2 ENGINE. REMOVED AND REPLACED RELAY 3421K2, REMOVED AND REPLACED NR 2 DC GCU AND STARTER GENERATOR IAW 24-30-02R, O PS GOOD PERFORMED HIDDEN DAMAGE INSPECTION AND NO DAMAGE NOTED. 2 H 7 2 4T RT A13NM 20081230 SO 2008 12 30 RAIA2008122900002 1 20081224 A 2120 DUCT EMB 145 EMB145EP 3260221 SO AC PACK BLOWN A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 807HK 145119 CREW RECEIVED A WING ANTI ICE FAIL MESSAGE ON THE EICAS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT A DUCT AT TH E NR 2 PACK WAS BLOWN OFF. THE DUCT WAS RE-SECURED AND THE NR 2 PACK WAS DEFERRED PER MEL PROCEDURES. 2 L 7 2 4F RT T00011AT 20081230 SO 2008 12 30 RAIA2008122400001 1 20081220 A 3610 DUCT EMB 145 EMB145LR 3260212 SO BLEED AIR SYS LOOSE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 835HK 145670 CREW RECEIVED A NR 1 BLEED LEAK MESSAGE ON THE EICAS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 1 FAN AIR DUC T TO BE LOOSE. THE DUCT WAS RE-SECURED AND THE SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081230 SO 2008 12 30 RAIA2008122400003 1 20081222 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 821HK 145068 DURING DAILY INSPECTION BY MAINTENANCE, THE EMERGENCY LIGHT AT THE GALLEY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND RECONNECTED THE CONNECTOR AT THE POWER SUPPLY AND ADJUSTED THE LIGHT ASSEMBLY. OPERATIONAL CHECK FOUND NO ADDIT IONAL DISCREPANCIES. 2 L 7 2 4F RT T00011AT 20081230 NM 2008 12 30 USAA2008122392306 1 20081216 A 5311 6546548 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - NR 6136276 - CRACK ON FRAME AROUND HOLES FOR SUPPORT BRACKET AT BS 747 BETWEEN S8L & S9L. RE PAIRED FRAME AROUND HOLES FOR SUPPORT BRACKET AT BS 747 BETWEEN S8L & S9L IAW US AIRWAYS TASK CARD M1C53002. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 USAA2008122392307 1 20081216 A 5311 6546549 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - NR 6136277 - CRACK ON FRAME AROUND HOLES FOR SUPPORT BRACKET AT BS 767 BETWEEN S8R & S9R. RE PAIRED FRAME AROUND HOLES FOR SUPPORT BRACKET AT BS 767 BETWEEN S8R & S9R IAW US AIRWAYS TASK CARD M1C53002. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 USAA2008122392309 1 20081216 A 5311 6546555 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - NR 6136279 - CRACK ON FRAME AROUND HOLES FOR SUPPORT BRACKET AT BS867 BETWEEN S8R & S9R. REP AIRED FRAME AROUND HOLES FOR SUPPORT BRACKET AT BS867 BETWEEN S8R & S9R IAW US AIRWAYS TASK CARD M1C53002. 2 L 7 2 4F RT A16WE 20081230 EU 2008 12 30 USAA2008122692329 1 20081225 A 2910 AE7094593 HOSE AIRBUS 320 A320214 3930316 EU HYDRAULIC SYS CHAFED A USAA O OTHER K FLUID LOSS CR CRUISE 1 EA 19 118US 1264 LOG PAGE 8316449 - FLT 1584 PHX-PIT - EMERGENCY LANDING - CREW REPORTED LOSS OF GREEN HYDRAULIC SYSTEM. FLIGHT CONTINUE D TO PIT AND AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT AND WAS TOWED TO GATE DUE TO LOSS OF NOSE WHE EL STEERING. MAINTENANCE REMOVED AND REPLACED CHAFED CASE DRAIN FILTER HOSE ASSEMBLY AND SERVICED HYDRAULIC SYSTEM. LE AK CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081230 NM 2008 12 30 USAAEMB08024 1 20081224 A 3350 34002210 BATTERY EMB ERJ190 ERJ190100IGW 3260408 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 954UW 1688 1688 19000139 EMERGENCY LIGHT INOP. MAINTENANCE INSTALLED SERVICEABLE BATTERY. 2 L 7 2 4F RT A57NM 20081230 NM 2008 12 30 USAA2008122392304 1 20081217 A 5311 6546525 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - NR 6136274 - CRACK ON FRAME AROUND HOLES FOR SUPPORT BRACKET AT BS 380 BETWEEN S8R & S9R. RE PAIRED FRAME AROUND HOLES FOR SUPPORT BRACKET AT BS 380 BETWEEN S8R & S9R IAW US AIRWAYS TASK CARD M1C53002. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 USAA2008122392311 1 20081201 A 5544 STRUCTURE BOEING 737 7373G7 138447J NM RUDDER DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - NR 6135795 - DEBOND OF TRAILING EDGE OF RUDDER STA 233.09 +12 INCHES. REPAIRED RUDDER TRAILI NG EDGE IAW B737 SRM 51-20-05-06. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 USAA2008122992332 1 20081124 A 5320 69434452 SUPPORT ANGLE BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - MAJOR REPAIR - C19 CHECK - NR 6130865, CORROSION ON AFT CARGO DOOR CUTOUT LOWER SILL SUPPORT ANGLE AT BS 767 + 5, S25R. REPLACED AFT CARGO DOOR CUTOUT LOWER SILL SUPPORT ANGLE AT BS 767 + 5, S25R IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 USAASB08125 1 20081223 A 3350 036000570010 FUSE BOEING 737 7373G7 138447J NM POWER SUPPLY BLOWN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 303AW 24010 PHX - MAINTENANCE REPORTED THE LEFT FUSELAGE EMERGENCY EXIT LIGHT, AFT OF WING, INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE FUSE ON BATTERY POWER SUPPLY PER MM 33-51-21. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 USAA2008122292293 1 20081123 A 5347 6546875 SEAT TRACK BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - NR 6135762 - CORROSION ON SEAT TRACK BETWEEN BS 907 TO BS 927, RBL 26. REPAIRED SEAT TRACK B ETWEEN BS 907 TO BS 927, RBL 26 IAW B737 SRM 53-00-52-2R 3. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 USAA2008122292294 1 20081124 A 5315 6546811 FLOORBEAM BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - NR 6130902 - CORROSION ON FLOORBEAM UPPER FLANGE AT BS 986.5, S17R, BETWEEN BL 0 TO RBL 19. REPAIRED FLOORBEAM AT BS 986.5, S17R, BETWEEN BL 0 TO RBL 19 IAW US AIRWAYS EA 132131 & B737 SRM 53-00-51-2R 2. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 USAA2008122292295 1 20081124 A 5312 6545801512 BULKHEAD BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - NR 6135611 - CORROSION ON BULKHEAD LOWER CHORD AT BS 227.8, BETWEEN S28R TO S28L. REPAIRED B ULKHEAD LOWER CHORD AT BS 227.8, BETWEEN S28R TO S28L IAW US AIRWAYS EA 32138. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 USAA2008122292297 1 20081124 A 5320 6547957U3 SILL BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 CLT - C19 - MAJOR REPAIR - NR 6130870 - CORROSION ON SILL WEB AT AFT CARGO COMPARTMENT ENTRY RIGHT SIDE. CORROSION ON S ILL WEB AT AFT CARGO REPLACED SILL WEB AT AFT CARGO COMPARTMENT ENTRY IAW B737 SRM 51-40-02-0G. 2 L 7 2 4F RT A16WE 20081230 EU 2008 12 30 USAA2008122492314 1 20081204 A 5540 D5537131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - C8 - MAJOR REPAIR - NR 6138729 - EXCESSIVE PLAY ON RUDDER HINGE ARM NR 2 AT VERTICAL STABILIZER STA 1926. REPLACE D RUDDER HINGE ARM NR 2 FITTING AT VERTICAL STABILIZER STA 1926 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 20081230 NM 2008 12 30 USAASB08124 1 20081222 A 2751 1817389 TRANSMITTER BOEING 737 7374B7 138449C NM TE FLAP FAULTY A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 427US 48388 213 24549 ON APPROACH TO CLT, FROM BDL, CREW REPORTED AN ASYMMETRICAL FLAP CONDITION BETWEEN 10 - 15 UNITS. NO ROLL DIFFICULTY OR CONTROL ISSUES NOTED. CREW DECLARED AN EMERGENCY AND ACCOMPLISHED A GO-AROUND TO RESOLVE PROBLEM. FLIGHT LANDED WITHO UT FURTHER INCIDENT AND TAXIED TO THE GATE. CLT MAINTENANCE REMOVED AND REPLACED THE LEFT FLAP POSITION TRANSMITTER PER MM 27-58-12. OPERATIONAL CHECK GOOD PER MM 27-51-00. 2 L 7 2 4F RT A16WE 20081230 EU 2008 12 30 USAA2008122992333 1 20081204 A 5320 D5347228400800 BEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C8 CHECK - NR 6138922, CORROSION ON BEAM AT FR 64 - FR 67, -Y465. REPLACED BEAM AT FR 64 - FR 67, -Y465 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081230 EU 2008 12 30 USAA2008122992334 1 20081204 A 5320 D53112821200 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C8 CHECK - NR 6131243, CORROSION ON FLOOR SUPPORT AT FR 12 - FR 24, -Y254. REPLACED FLOOR SUPPORT AT FR 12 - FR 24, -Y254 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081230 EU 2008 12 30 USAA2008122992335 1 20081204 A 5320 D5311219820005 FITTING AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C8 CHECK - NR 6131240, CORROSION ON L1 DOOR CUTOUT LOWER SILL CENTER FITTING AT FR 16 - FR 20. REP LACED L1 DOOR CUTOUT LOWER SILL CENTER FITTING AT FR 16 - FR 20 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081230 NM 2008 12 30 USAASB08127 1 20081227 A 3350 20131ASMI BATTERY PACK BOEING 737 737401 138449B NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 409US 23879 FLL - MAINTENANCE REPORTED THE AFT EMERGENCY LIGHT, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LE FT BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 NOCA09308 1 20081220 A 3350 S417T5103 LIGHT BOEING 767 767324 1385203 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 767NA 27569 FWD GALLEY FLOOR EMERGENCY LIGHT FWD OF COMP NR 213 LT SIDE IS INOP. REMOVED AND REPLACED FLOOR LIGHT ASSY IAW AMM 33-5 1-00. 2 L 7 2 4F RT A1NM 20081230 NM 2008 12 30 NOCA09008 1 20081210 A 3350 767 LIGHT BOEING 757 75728A 1384976 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 R2 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT AS PER MM 33-51-07. 2 L 7 2 4F RT A2NM 20081230 NM 2008 12 30 ASAA0874076 1 20081205 A 5320 146A750225 SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION ON FLOOR TO SIDEWALL SUPPORT AROUND NUTPLATE HOLES STA 772 LBL 20. R&R FLOOR TO SIDEWALL SUPPORT STA. 772 LBL 20 WAS ACCOMPLISHED. 2 L 7 2 4F RT A16WE 20081231 SO 2008 12 31 C2XA08IA259 1 20081221 A 2611 SMOKE WARNING EMB 145 EMB145EP 3260221 SO LAVATORY MALFUNCTIONED A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 11176 14500881 FLIGHT 2072 RIC-IAH - THE CREW REPORTED A MOMENTARY LAVATORY SMOKE WARNING DURING CRUISE. NO SMOKE CONDITIONS WERE NOTE D AT THAT POINT AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE PERFORMED FUNCTIONAL TESTS OF THE LAVATORY SMOKE WARNING SYSTEM AND COULD NOT FIND AND COULD NOT DUPLICATE THE WARNING. 2 L 7 2 4F RT T00011AT 20081231 SO 2008 12 31 C2XA08IA260 1 20081220 A 2611 SMOKE WARNING EMB 145 EMB145LR 3260212 SO LAVATORY MALFUNCTIONED A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 48901 145501 FLIGHT 2220 SHV-IAH - THE CREW REPORTED A MOMENTARY LAVATORY SMOKE WARNING DURING CRUISE. NO SMOKE CONDITIONS WERE NOTE D AT THAT POINT AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE PERFORMED ENGINE GROUND RUNS AND COULD NOT DUPLICATE THE CONDITION. 2 L 7 2 4T RT T00011AT 20081231 SO 2008 12 31 C2XA08IA263 1 20081225 A 3350 14532843401 CONTROL PANEL EMB 145 EMB145XR 3260214 SO COCKPIT FAULTY A C2XA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 27 11191 9243 14500935 FLIGHT 2777 IAH-GSO - DURING TAXI THE EMERGENCY LIGHT PANEL LOCATED IN THE COCKPIT KEPT RE-ARMING AND TURNING ON THE EME RGENCY LIGHTS. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT CONTROL PANEL, OPERATIONALLY TESTED THE EMERGENCY L IGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2 L 7 2 4F RT 20081231 NM 2008 12 31 AALA200802511A 1 20081031 A 5320 143T85134 WEB BOEING 767 767323 1385205 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 366AA 25193 AFW - FORWARD CARGO DOOR SILL WEB HAD CORROSION BLENDED AT LOWER FORWARD OUTBOARD SIDE AT STATION 615. REPAIRED IN ACCO RDANCE WITH MRB 767 3336. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 AALA200802513A 1 20081030 A 5315 141T5113 FLOORBEAM BOEING 767 767323 1385205 NM BS 325 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 366AA 25193 AFW - FLOORBEAM AT STATION 325 HAS CORROSION REMOVAL ON UPPER AND LOWER SURFACES. MATERIAL REMAINING IS BEYOND SRM LIM ITS. REPAIRED IN ACCORDANCE WITH MRB 767 3334. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 AALA200802515A 1 20081106 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 782AN 30003 AFW - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD R2 DOOR FAILED TEST. REPLACED BATTERY PACK AT OVERHEAD R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 WP 2008 12 31 AALA200802523A 1 20081113 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 475AA 49650 DFW - EMERGENCY LIGHT SHROUD MISSING AT SEAT 31D. REPLACED SHROUD FOR SEAT 31D. SYSTEM GROUND CHECKED NORMAL OPERATION . 2 L 7 2 4F A6WE 20081231 EU 2008 12 31 AALA200802436A 1 20081030 A 2750 CHA1171006C GEARBOX AIRBUS 300 A300B4605R 3930308 EU TE FLAPS FAILED A AALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 21 18066 509 SDQ INFLIGHT - CREW REPORTED FLAPS WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO SDQ AND LANDED WITHOUT INCIDENT. REPLA CED RIGHT BEVEL GEARBOX STARBOAD SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081231 WP 2008 12 31 AALA200802441A 1 20081030 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DISLODGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 16545 53027 LGA - EMERGENCY LIGHTS AT SEAT ROWS 6 TO 12 INOPERATIVE. REPOSITIONED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081231 NM 2008 12 31 AALA200802466A 1 20081106 A 3040 S283W4013 CONTROL UNIT BOEING 777 777223 1385213 NM WINDSHIELD HEAT ARCED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 755AN 30263 NRT - R3 COCKPIT WINDOW DELAMINATING AT BOTTOM CENTER WITH ARCING DAMAGE OUT OF LIMITS. REPLACED R3 WINDOW AND WINDOW H EAT CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 MASA2008122600757 1 20081226 A 3350 1317 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 445YV 445 ASH FLT 7059 DEN-RAP. CENTER FLOOR AISLE EMERGENCY LIGHT INOP. MX REPLACED AISLE PATH STRIP. 2 H 7 2 4T RT A13NM 20081231 NM 2008 12 31 MASA2008122700758 1 20081227 A 7920 LINE DHAV DHC8 DHC8202 2809007 NM OIL COOLER LOOSE A MASA E B ENGINE SHUTDOWN EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SW 07 448YV 448 ASH FLT 7122 GCC-DEN. CREW DECLARED AN EMERGENCY AND SHUT DOWN NR 1 ENGINE ON FINAL DUE TO A LOW OIL PRESSURE WARNING. MX RE-SECURED OIL COOLER INLET LINE AND OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 20081231 NM 2008 12 31 NOCA09508 1 20081219 A 3350 BR9279103 COVER BOEING 767 767324 1385203 NM CABIN MISSING A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 767NA 27569 AFT GALLEY FWD WALL EXIT SIGN MISSING COVER. REPLACED FLOOR LIGHT COVER ASSY AS REQUIRED. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 DL76L081707 1 20081210 A 2530 FAN BOEING 767 767332 1382001 NM OVEN INOPERATIVE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 194DN 28451 MID GALLEY OVEN WOULD NOT SWITCH OFF. EMITTED BURNT ELECT SMELL. SECURED OVEN BY PULLING C/B LOCATED IN MID GALLEY. F OUND MID GALLEY OVEN FAN INOP. FWD TO NEF PER 253.00. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 DL77L081753 1 20081124 A 2822 568130080002 PUMP BOEING 777 777232 1385232 NM FUEL SYSTEM FAILED A DALA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 702DN 29741 058851 AFTER FUEL BALANCING COMPLETE RT FWD FUEL BOOST PUMP LIGHT REMAINED ON. SHORTLY AFTER RT AFT FUEL BOOST PUMP ILLUMINATE D. COMPLETED NON NORMAL PROCEDURE FOR FWD & AFT BOOST PUMP FAILS PER QAH. BOTH BOOST PUMP REPLACED VERIFICATION FLT C/ W ON 11/26/08 FLT 185. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 DL76L081771 1 20081219 A 2131 CONTROLLER BOEING 767 767332 1382001 NM CABIN PRESSURE MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 176DN 25061 RTB DUE TO CABIN AUTO PRESS CONTROLLER INOP. PROBLEM OCCURRED AFTER AC WAS DEICED. PERFORMED BIT ON AUTO1 AND AUTO2 CABIN PRESS CONTROL UNIT BOTH FAULTED. CONTROLLER PERFORMED, VERIFY NO FAULTS. RESET BOTH CONTROLLERS, NO FAULTS , NO MSGS, NO HISTORY ON AUTO PRESS. AC OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 DLM88081752 1 20081218 A 5711 SPAR DOUG MD88 MD88 3023688 NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 FOUND CRACK IN REAR SPAR LOWER CHORD AT O/B FLAP, I/B HINGE. CUT OUT DAMAGED SECTION OF CHORD AND SPLICED IN NEW SECTIO N. REPAIRED IAW ER/A 471595-14. 2 L 7 2 4F RT A6WE 20081230 NM 2008 12 30 AALA200802427A 1 20081028 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 680AN 29590 DFW - EMERGENCY LIGHT AT SEAT 17DEF INOPERATIVE. INSTALLED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 17DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081230 NM 2008 12 30 AALA200802430A 1 20081029 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 194AA 32388 DFW - EMERGENCY LIGHT AT SEAT ROW 17DEF AFT MISSING LENS. REPLACED LENS AT SEAT ROW AFT 17DEF. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081230 NM 2008 12 30 AALA200802432A 1 20081029 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 194AA 32388 DFW - EMERGENCY LIGHT AT SEAT ROW 17DEF AFT SHROUD BROKEN. REPLACED SHROUD AT SEAT ROW AFT 17DEF. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081230 EU 2008 12 30 AALA200802433A 1 20081030 A 3350 P4010051124 CHARGER AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14065 508 JFK - EMERGENCY LIGHTS IN FIRST CLASS RIGHT SIDE INOPERATIVE. REPLACED BATTERY PACK AND CHARGER UNIT OVERHEAD NUMBER ON E RIGHT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081230 NM 2008 12 30 AALA200802417 1 20081027 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081230 SO 2008 12 30 RAIA2008122900005 1 20081228 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 845HK 14500842 DURING PRE FLIGHT INSPECTION, THE EMERGENCY LIGHTS AT THE RIGHT AND LEFT OVERWING EXITS WERE FOUND TO BE INOPERATIVE. M AINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY FOR THESE LIGHTS AND PERFORMED A OPERATIONAL CHECK OF T HE EMERGENCY LIGHTING SYSTEM WITH NO ADDITIONAL DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 20081230 SO 2008 12 30 RAIA2008121500002 1 20081211 A 2797 CONNECTOR EMB 145 EMB145LR 3260212 SO FECU DIRTY A RAIA O OTHER N FALSE WARNING LD LANDING 1 CE 03 810HK 145231 THE CREW RECEIVED A FLAP FAIL MESSAGE ON THE EICAS. MAINTENANCE CLEANED AND RE-SECURED THE CONNECTOR TO THE FECU, INSPE CTED WIRES, AND PERFORMED AN OPERATIONAL CHECK OF THE FLAP SYSTEM WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 20081230 SO 2008 12 30 RAIA2008122300001 1 20081218 A 3610 CA33020 CLAMP EMB 145 EMB145 3260210 SO NR 1 BLEED DUCT BROKEN A RAIA E B A ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CE 03 820HK 145064 CREW RECEIVED A BLEED 1 LEAK MESSAGE ON THE EICAS AND THE FLIGHT ATTENDANT REPORTED THE PRESENCE OF SMOKE IN THE CABIN. MAINTENANCE INSPECTED AND FOUND THE NR 1 BLEED DUCT CLAMP IN THE BELOW ONE OF THE BELLY FAIRINGS TO BE BROKEN. MAINTEN ANCE ALSO FOUND THAT THE WIRE TO THE LEAK DETECTOR FOR THE SAME JOINT TO BE BROKEN. MAINTENANCE REPAIRED THE WIRE TO TH E LEAK DETECTOR AND REMOVED AND REPLACED THE BROKEN CLAMP. AN OPERATIONAL CHECK WAS OF THE NR 1 BLEED LEAK SYSTEM WAS P ERFORMED WITH NO ADDITIONAL FINDINGS. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 20081231 NM 2008 12 31 AALA200802496A 1 20081109 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 689AA 25731 MIA - EMERGENCY LIGHTS FROM SEAT ROW 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 20 AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 SO 2008 12 31 C2XA08IA258 1 20081218 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145EP 3260221 SO RT MLG OUT OF ADJUST A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 15926 145005 FLIGHT 2804 - IAH TO MEM- DURING CLIMB THE LANDING GEAR DID NOT RETRACT WHEN SELECTED. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. UPON INSPECTION THE RIGHT GEAR AIR GROUND PROXIMITY SWITCH WAS FOUND TO BE OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED THE PROXIMITY SWITCH, FUNCTIONALLY TESTED THE LANDING GEAR EXTENSION AND RETRACTION AND THE DISCREP ANCY WAS CLEARED. 2 L 7 2 4F RT T00011AT 20081231 NM 2008 12 31 AALA200802512A 1 20081103 A 5320 SILL BOEING 767 767323 1385205 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 366AA 25193 AFW - OUTER CHORD LOWER MAIN SILL AT FORWARD CARGO DOOR CORRODED. REMOVED AND REPAIRED CORROSION BY BLENDING AREA PER S RM 51-10-02 AND MRB 767-3335. 2 L 7 2 4F RT A1NM 20081231 SO 2008 12 31 C2XA08IA266 1 20081228 A 2611 SMOKE WARNING EMB 145 EMB145LR 3260212 SO LAVATORY MALFUNCTIONED A C2XA O OTHER N FALSE WARNING UK UNKNOWN 1 SW 27 13538 145527 IAH - FLIGHT 2356 - THE CREW REPORTED A LAV SMOKE INDICATION ON EICAS. THE CREW FOLLOWED THE QRH PROCEDURES WITH NO SMO KE NOTED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE OPERATIONALLY CHECKED THE LAV SMOKE DETECTOR WI TH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081231 NM 2008 12 31 AALA200802520A 1 20081113 A 3231 SEQUENCE VALVE BOEING 757 757223 1384957 NM MLG DOOR FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 647AM 24605 DFW INFLIGHT - GEAR WARNING INDICATION AFTER GEAR RETRACTION. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED L EFT DOOR SEQUENCE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 CALA2008122301163 1 20081222 A 5330 6545774 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69348 23586 STRINGER 24L, STATION 727E - 718 OUTER SKIN HAS 1 INCH CRACK. REPAIRED CRACK IN OUTER SKIN STRINGER 24L STATION 727 - 7 18 PER B737 SRM 53-00-01 FIG 201. TOTAL WEIGHT OF REPAIR, 9.84LBS FOR WEIGHT AND BALANCE CALCULATION. 2 L 7 2 4F RT A16WE 20081231 WP 2008 12 31 AALA200802471A 1 20081106 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 964TW 53614 LGA - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081231 EA 2008 12 31 MASA2008122600756 1 20081226 A 3350 1317 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 917FJ 15017 ASH FLT 2692 CLT-MDT. SECOND FROM LAST EMERGENCY LIGHTS INOP. MX RELAMPED LIGHTS. OPS GOOD. 2 L 7 2 4F RT A21EA 20081231 EA 2008 12 31 MASA2008122500754 1 20081225 A 5210 601R318712 RETAINER CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BENT A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 511MJ 10104 PERMANENT REPAIR - PERFORMED TEMP REPAIR TO PASSENGER DOOR LOWER FORWARD SEAL RETAINER FOR 1.25 INCH BEND. 2 L 7 2 4F RT A21EA 20081231 NM 2008 12 31 NOCA09608 1 20081224 A 2611 BS06374051 SMOKE DETECTOR BOEING 767 76736N 1385152 NM R4 LAVATORY MALFUNCTIONED A NOCA K NONE N FALSE WARNING UK UNKNOWN 1 EA 15 768NA 29898 SMOKE DETECTOR IN R4 LAV SOUNDING. RESET SMOKE DETECTOR, PERFORMED ADJ/TEST PER M/M 26-13-00 OPS CK'D NORMAL. P/N OFF AND ON - N/A. 2 L 7 2 4F RT A1NM 20081231 WP 2008 12 31 RYNA2008122200046 1 20081219 A 3230 59516395001 BUNGEE CYLINDER DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A RYNA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 CE 07 932RD 49233 DURING LANDING NLG FAILED TO EXTEND CHECKED TILLER ALIGNMENT MLG INDICATION WAS GREEN NLG INDICATION RED NLG PEDESTAL PI N WAS FLUSH. REACCOMPLISHED GEAR EXTENSION NLG INDICATED SAFE. AIRCRAFT WAS FERRIED TO HAMILTON IN TUS FOR TROUBLESHOO TING. JACKED FWD NOSE SECTION AND TROUBLESHOT FOUND DEFECTIVE BUNGEE CYLINDER, REMOVED AND REPLACED IAW MD-80 MM 32-32- 07. ACCOMPLISHED RETRACTION TEST SEVERAL CYCLES NLG EXTENDS AND RETRACTS NORMALLY WITHOUT BINDING ALL LIGHT INDICATIONS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 20081231 SO 2008 12 31 C2XA08IA268 1 20081228 A 2197 W101244722 WIRE EMB 145 EMB145LR 3260212 SO COCKPIT BROKEN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15973 145159 IAH - FLIGHT 2434, THE CREW REPORTED A PACK 1 VALVE CLOSED ADVISORY MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHE RE IT LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED WIRE W101-2447-22 AT THE BUSHBUTTON FOR PACK ONE, OPERATIONALLY TES TED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081231 SO 2008 12 31 C2XA08IA270 1 20081229 A 5610 AC251B12 SEALANT EMB 145 EMB145XR 3260214 SO WINDSHIELD SEPARATED A C2XA A UNSCHED LANDING B S SMOKE/FUMES/ODORS/SPARKS AFFECT SYSTEMS UK UNKNOWN 1 SW 27 11176 14500881 IAH - FLIGHT 2079, THE CREW REPORTED THE BLACK SEALER ON THE CAPT SIDE WINDOW PEELED OFF IN FLIGHT AND WENT THROUGH THE NUMBER ONE ENGINE CAUSING A BURNING SMELL. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED THE EXCESS SEALANT FROM THE CAPTAINS SIDE WINDOW, INSPECTED THE NUMBER ONE ENGINE WITH N O EVIDENCE OF INGESTION OF SEALANT NOTED, OPERATIONALLY CHECKED THE NUMBER ONE ENGINE WITH NO DEFECTS NOTED, REPAIRED TH E CAPTAINS HUMPSEAL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081231 NM 2008 12 31 AALA200802538A 1 20081120 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 781AN 29586 DFW - EMERGENCY LIGHT AT SEAT 23G INOPERATIVE. REPLACED LAMP AT SEAT 23G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 AALA200802542A 1 20081120 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 781AN 29586 DFW - EMERGENCY LIGHTS AT SEAT ROWS 41C TO 45C FAILED TEST. SECURED CONNECTION AT SEAT ROW 40 FOR EMERGENCY LIGHTS AT S EAT ROWS 41C TO 45C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 AALA200802546A 1 20081121 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AA 24593 DFW - EMERGENCY LIGHT EXIT MARKER AT LEFT OF AFT RIGHT PASSENGER DOOR BROKEN. REPLACED LIGHT ASSEMBLY AT RIGHT PASSENGE R DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 WP 2008 12 31 AALA200802505A 1 20081110 A 3350 LAMP DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971TW 53621 DFW - EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. REPLACED LAMP AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081231 NM 2008 12 31 AALA200802516A 1 20081112 A 2917 211C223520 PRESSURE SWITCH BOEING 767 767323 1385205 NM HYD SYSTEM FAULTED A AALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 39364 24045 INFLIGHT - LEFT HYDRAULIC SYSTEM LOW PRESSURE INDICATION. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED LEFT H YDRAULIC PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 AALA200802517A 1 20081112 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 DFW - EMERGENCY LIGHT AT SEAT 23C MISSING LENS. REPLACED LENS AT SEAT 23C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 AALA200802518A 1 20081112 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 795AN 30257 DFW - EMERGENCY LIGHT AT SEAT 23C MISSING LAMPS. REPLACED LAMPS AT SEAT 23C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 AALA200802443A 1 20081031 A 2822 RELAY BOEING 757 757223 1384957 NM HYD PUMP DAMAGED A AALA A UNSCHED LANDING K J G FLUID LOSS WARNING INDICATION MULTIPLE FAILURE CR CRUISE 1 SW 21 608AA 27446 INFLIGHT - CREW REPORTED RIGHT HYDRAULIC SYSTEM QUANTITY LOSS AND LEFT HAND FORWARD FUEL BOOST PUMP FAILURE WITH AFT EXH AUST FAN NUMBER ONE STATUS MESSAGE AT CRUISE. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED K102 AND K103 RELA YS. ALSO REPLACED RIGHT ENGINE DRIVEN PUMP PRESSURE DRAIN FILTERS AND SERVICED RIGHT HYDRAULIC SYSTEM TO FULL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081208 EA 2008 12 8 SWIA200820553 1 20080930 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 969SW 7876 DURING C-CHECK, RIGHT ENGINE AFT THRUST MOUNT CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081208 NM 2008 12 8 SWAA086788 1 20081203 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086791 1 20081203 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27L TO STR 26L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086792 1 20081203 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM . 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086794 1 20081203 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT AT BS 291, WL 253. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086799 1 20081203 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086838 1 20081204 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 786, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086804 1 20081203 A 5320 6545805 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND HORIZONTAL WEB CRACKED AT BS 277, STR 14R. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086844 1 20081204 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM CORROED AT BS 976, RBL 50, WL 208. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086845 1 20081204 A 5330 6545819 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND NOSE WHEEL WELL UPPER PRESSURE SKIN CRACKED AT BS 252, BETWEEN LBL 9 TO RBL 9. REPAIR ED SKIN PER ACO. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086846 1 20081204 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER CUTOUT, BS 430, BL 0. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086847 1 20081204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086855 1 20081204 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM VERTICAL WEB CRACKED AT BS 707, LBL 25. REPAIRED BEAM PER PAE ER. 2 L 7 2 4F RT A16WE 20081208 SO 2008 12 8 SIMA200833802 1 20081201 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCHARGED A SIMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 21 619AE 145101 ON FLIGHT 3570 CREW REPORTED ON PREFLIGHT FORWARD ZONE EMERGENCY LIGHTS NOT ON OVER FLIGHT ATTENDANT SEAT EXIT SIGN BELO W COCKPIT FLOOR, AND EXIT SIGN-CEILING GALLEY EXIT SIGN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 BATT ERY PACK IAW EMB 145 AMM 33-50-04-000-801-A, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081208 SO 2008 12 8 SIMA200833803 1 20081201 A 2460 23080013A GENERATOR EMB 135 EMB135KL 3260302 SO APU FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 812AE 145531 ON FLIGHT 4205, CREW REPORTED UPON STARTING APU COCKPIT FILLED WITH ELECTRICAL BURNING SMELL AND SMOKE. AIRCRAFT REMOVE D FROM SERVICE. FOUND APU STARTER GENERATOR TO BE DEFECTIVE AFTER REMOVING PIECES OF METAL FROM INSIDE GENERATOR. REMO VED AND REPLACED GENERATOR IAW AMM 24-800-01. APU CHECKS GOOD. NO SMELL OR SMOKE DETECTED. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F RT T00011AT 20081208 NE 2008 12 8 DL76L081625 2 20081022 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 198DN 40748 28455 727830 NR 2 ENGINE FAILED 25 CYCLE RE-INSPECT OF GEARBOX FOR BLAST CONTAMINANT. REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081208 NM 2008 12 8 DLM88081631 1 20081124 A 3030 HEATER DOUG MD88 MD88 3023688 NM PITOT TUBE INOPERATIVE A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 939DL 202373 49812 PITOT/STALL HEAT OFF MSG ON TAKEOFF ROLL. CAPT PITOT HEATER SHOWING ZERO CURRENT. REJECTED TAKEOFF AT 75KTS. REPLACED CAPTS PITOT PER M/M. PROBE NOW DRAWS A CURRENT AND IS HOT. PITOT LEAK CK PER MM CKS GOOD. 2 L 7 2 4F RT A6WE 20081208 2008 12 8 UALA2008120306728 4 20081202 A 2565 5A2901 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EVAC SLIDE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 664UA PF0192 29236 ASPIRATOR LEAK. BROKEN O-RING AND BARREL LEAK. REBUILT ASPIRATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081208 NM 2008 12 8 UALA2008120306735 1 20081203 A 3350 794640 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCONNECTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 173UA 24380 DOOR 2L EEL LIGHTS BLINK ON AND OFF. RECONNECTED PWR SUPPLY AND OP CHK'D OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081208 NM 2008 12 8 UALA2008120406744 1 20081203 A 5200 F1314 SPRING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DOOR WEAK A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 LT FWD MED DEPLOYMENT BAR GAS SPRING WEAK. REPLACED GAS SPRING. 2 L 7 2 4F 4 F RT A1NM E24NE 20081208 NM 2008 12 8 UALA2008120406745 1 20081203 A 5240 F1314 SPRING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SERVICE DOOR WEAK A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 RT FWD SERVICE MED DEPLOYMENT BAR GAS SPRING WEAK. REPLACED GAS SPRINGS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081208 NM 2008 12 8 UALA2008120406754 1 20081204 A 2121 732591F FAN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 180UA 25224 EXPERIENCED LOSS OF ALL GALLEY POWER AND BOTH UTILITY BUSSES TRIPPED OFF. FOLLOWED IRREG PROC NOW BOTH UTILITY BUSSES R ESTORED AND GALLEY POWER LEFT UNPOWERED. FLT ATT REPORTED A BURNING SMELL AT TIME OF GALLEY POWER TRIP WHICH THEN QUITE QUICKLY DISSIPATED WHEN POWER REMOVED. FLT ATT STATED SOURCE OF SMELL TO BE BUSINESS CLASS GALLEY ON MAIN DECK AND UPP ER DECK GALLEY. FOUND BREAKER POPPED FOR RECIRC FAN H518 UNDERFLOOR RECIRC FAN 2, RECIRC FAN INOP AND PRIMARY CAUSE OF BURN SMELL AND UTILITY BUSSES SHEDDING. NEED TO REPLACE FAN. REPLACED FAN 2 UNDER FLOOR AND VIB MONITOR, TEST OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081208 EU 2008 12 8 UALA2008120406755 1 20081204 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 405UA 452 AFT TRIANGLE SHEAR PLATE ATTACH FRAME TO FUSELAGE CORRODED. REMOVED FRAME, DRILLED NEW FRAME NEEDS INSTALL. FRAME AND PLATE REPLACED COMPLETE. INSPECTED INSTALLATION AFT RT TRIANGLE TO FUSELAGE SHEAR PLATE SUPPORT FRAME. 2 L 7 2 4F 4 F RT A28NM E40NE 20081208 EA 2008 12 8 A6WA200840611 1 20081119 A 2751 601R930303 TRANSMITTER CNDAIR CL600 CL6002B19 1900309 EA LT WING TE FLAP MALFUNCTIONED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 31 426AW 7669 LOG 189993/2 FLIGHT 3802, 3845, UNCOMMANDED FLAPS EXTENSION OF 8 DEGREES AT FL 31.0 TAT -23, SAT -48, MACH .74, IAS 275, INTERMITTENT INDICATION OF FLAPS EXTENDING TO 2 DEGREES FOLLOWED. DOWNLOADED FDR IAW AMM 31-31-01, CONFIRMED LT FLAP P OSITION TRANSMITTER SHOWS ERRATIC FLAP MOVEMENT TO 8 DEGREE DURING FLIGHT. REF W/O 129548 CARD 2 FOR REMOVED AND REPLAC EMENT OF LT FLAP TRANSMITTER. REMOVED AND REPLACED FLAP POS TRANSMITTER ASSY IAW AMM 27-55-01. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 20081208 NM 2008 12 8 UALA2008120206724 1 20081202 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 24 RIGHT. REPLACED LIGHT ASSY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081208 CE 2008 12 8 DXTA2008120103376 1 20081128 A 3260 WARNING LIGHT BEECH MU300 400A 1155402 CE COCKPIT ILLUMINATED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 180QS RK469 RED GEAR HANDLE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. 2 H 7 2 4F RT A16SW 20081208 NM 2008 12 8 FDEA200811194922 1 20081119 A 5347 B2753051 SEAT TRACK BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 SEAT TRACK CORRODED, MAIN DECK AT RBL 24 BS 1148 TO 1176 FABRICATED SEAT TRACK, LOCATED AND DRILLED HOLES, TREATED AND PRIMED NEW SEAT TRACK EXTENSION REF SNRM N00801 SRM 51-30-5, SRM 51-10-2 AND MM 51-20-151-07. CLASSIFIED AS A MAJOR REP AIR. 2 L 7 3 4F A3WE 20081208 NM 2008 12 8 UALA2008120106713 1 20081129 A 2421 7259825M IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE FAULTY A UALA D RETURN TO BLOCK W INADEQUATE Q C IN INSP/MAINT 1 WP 29 551UA 25399 LT GEN CAME OFF LINE 2 TIMES, SPOKE TO SAM, DURING RUN UP IS WHEN GEN CAME OFF AT =40% N1. REPLACED NR 1 IDG. 2 L 7 2 4F 4 F RT A2NM E17NE 20081208 2008 12 8 UALA2008120106689 4 20081127 A 2210 C12850AC02 FCU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AUTOPILOT SYS FAULTY A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 427UA 512 AUTOPILOT ISSUES. FLIGHT DIVERTED. AUTO FLT 'FCU 1+2 FAULT' DISPLAYED ON UPPER ECAM SCREEN. CYCLED CB B5 AND M21 AND FCU CHANNEL 1 RECOVERED BUT FCU CHANNEL 2 REMAINED INOP. REPLACED FCU. 2 L 7 2 4F 4 F RT A28NM E40NE 20081208 NM 2008 12 8 F3LA200800657 1 20081003 A 5321 D5367324200000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE PERFORATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 REFERENCE NON ROUTINE 2008-196522. DURING C4/S1 C CHECK, INSPECTION NOTED FLOOR PANEL 151VG HAD PERFORATION DAMAGE. MX REPAIRED FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C. UPON COMPLETION OF THE REPAIR, IT WAS IN SPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081208 EA 2008 12 8 A6WA200840610 1 20081117 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION AP APPROACH 1 GL 31 427ZW 7685 THRU 10,000 FT FLAPS FAIL MSG. FLAPS FAILED AT ZERO, AIRSPEED WAS 250 KIAS. COMPLIED WITH QRH LANDED NORMAL. COMPLIED WITH FLAPS RESET IAW AWAC SUPP 98-018B FLAPS OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 A6WA200840609 1 20081115 A 2613 SENSOR CNDAIR CL600 CL6002B19 1900309 EA OVERHEAT SHORTED A A6WA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 31 467AW 7900 RECEIVED LT STAGE DUCT MSG INFLIGHT. MSG STAYED ON AFTER RETARDING THRUST LEVER TO IDLE. C/W GVI OF LT 10TH STAGE DUCT ING WITH ENGINE RUNNING. NO LEAKS DETECTED. LT 10TH STAGE WARN MSG OCCURRED AGAIN WITH ENGINES SHUTDOWN. CONFIRMED BA D INDICATION. REF 193317/1 FOR NEW DISCREPANCY. FOUND 10TH STAGE DUCT SENSING ELEMENT A14WK SHORTED TO GROUND. R&R A1 4WK IAW AMM 36-21-04. REF L/P 193317/3 FOR LOOB A FAULT. 2 L 7 2 4F RT A21EA 20081208 EU 2008 12 8 USAA920082080 1 20081116 A 5347 F57110568202 SEAT TRACK AIRBUS 330 A330323 3940030 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AY 370 BFM C2 MAJOR REPAIR NR 6115044 CORROSION ON SEAT TRACK BETWEEN FR39.2 TO FR47, Y450. REPLACED SEAT TRACK BETWEEN FR39.2 TO FR47, Y450 IAW A330 SRM 51-42-11. 2 L 7 2 4F RT A46NM 20081208 NM 2008 12 8 USAA920082081 1 20081111 A 5320 65C3267753 SHEAR WEB BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 MCN LAV SPILL MAJOR REPAIR NR 6135587 FLOOR SHEAR WEB CRACKED AT BS986.5, WL207.8, BETWEEN LBL38 TO LBL40. REPAIRED FLO OR SHEAR WEB AT BS986.5, WL207.8, BETWEEN LBL38 TO LBL40 IAW BOEING DRAWING NR 65C32677. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 F3LA200800656 1 20081002 A 5315 D5347217220390 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 931FR 52 2253 REFERENCE NON ROUTINE C051966. DURING C3 C CHECK, INSPECTION NOTED FLOOR BEAM Y-1292 BETWEEN FRAME 66 AND FRAME 68 HAS CORROSION IN SEVERAL HOLES. MX R&R FLOOR BEAM IAW THE REQUIREMENTS OF A319 SRM 51-42-11 AND DRAWING D53472780. UPON CO MPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081208 EA 2008 12 8 A6WA200840608 1 20081115 A 5610 NP13932112 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A A6WA K NONE O OTHER DE DESCENT 1 GL 31 458AW 12453 7861 FIRST OFFICERS WINDSHIELD CRACKED DURING DESCENT. REF 186497/2 R&R RT WINDSHIELD. APPLIED AERODYNAMIC FILLER TO RT WIN DOW STRAP. APPLIED SPEED TAPE. TAPE MUST BE REMOVED AFTER 48 HRS. IAW AMM 56-11-01 PLACED ON DIL. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 A6WA200840616 1 20081124 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 402AW 7281 LOG 189664/2 ON CLIMBOUT RECEIVED PAX DOOR LATCH CAUTION AND PAX DOOR WARNING MSGS. COMPLIED WITH QRH. DURING DESCENT WARNING MSG CLEARED YET CAUTION REMAINED. AFTER LANDING ALL MSGS CLEARED AND DOOR INDICATES NORMAL. PSI NORMAL. INTER ROGATED PSEU AND FOUND S46 AND S47 DOOR CAM 1/2 CODES STORED. OPERATED PAX DOOR AND VERIFIED DOOR CAMS OPERATE NORMAL A ND WITNESS MARKS ALIGNED. NO MSG DISPLAYED AT THIS TIME. DOOR INDICATES NORMAL. 2 L 7 2 4F RT A21EA 20081208 NM 2008 12 8 F3LA200800655 1 20081002 A 3350 BR964424 LIGHT AIRBUS A319 A319111 3930336 NM CABIN INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 21 931FR 52 2253 REFERENCE NON ROUTINE C051883. DURING C3 C CHECK INSPECTION NOTED THE RED EMERGENCY FLOOR PATH INDICATOR ON ROW 11ABC I S NOT ILLUMINATING. MX R&R LIGHT ASSEMBLY IAW THE REQUIREMENTS OF A319 AWM 33-51-07, PAGE 003. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081208 EU 2008 12 8 UALA2008120106685 1 20081126 A 5320 SHEAR PLATE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 403UA 442 SHEAR PLATE AFT OF DOOR 2R LOCATED BETWEEN FRAMES 68 AND 69 CRACKED. REPLACED TRAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081208 EU 2008 12 8 UALA2008120106687 1 20081126 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 448UA 842 TWENTY ONE (21) STRINGERS CUT FOR REMOVAL ACCESS TO REAR PRESSURE BULKHEAD LOWER FRAME 70 SECTION 5.25 INCHES AFT OF FRA ME 70 BETWEEN STRINGERS 24L AND STRINGER 24R. MAJOR REPAIR ACP'D: ALL STRINGERS REINSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081208 NM 2008 12 8 USAA EMB02022 1 20081202 A 2750 1700591A GEARBOX EMB ERJ190 ERJ190100IGW 3260408 NM TE FLAPS INOPERATIVE A USAA L ABORTED APPROACH F FLT CONT AFFECTED DE DESCENT 1 EA 19 951UW 2763 19000112 FLIGHT 1649, RDU-PHL - THE FLAPS FAILED TO EXTEND PAST 2. THE CREW DECLARED AN EMERGENCY AND DID A GO AROUND. THE FLIG HT LANDED UNEVENTFULLY. MAINTENANCE REPLACED THE FLAP POWER DRIVE GEARBOX. 2 L 7 2 4F RT A57NM 20081208 NM 2008 12 8 USAASB08119 1 20081203 A 3397 CONNECTOR BOEING 737 7373S3 138449H NM EMERGENCY LIGHTS LOOSE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW 23713 PHX - MAINTENANCE REPORTED THE AISLE EMERGENCY EXIT LIGHT AT ROW 21, SEAT C, INOPERATIVE. MAINTENANCE RESEATED THE CONN ECTOR AT ROW 21. OPERATIONAL CHECK GOOD PER MM 33-51-02-735-02. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 USAA2008120492181 1 20081114 A 5340 140N200113 STRINGER CLIP BOEING 757 7572S7 1384962 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 904AW 23566 MCN - MAJOR REPAIR - C12 CHECK - LEVEL 2 CORROSION ON STRINGER CLIP AT BS 751, S21R. REPAIRED STRINGER CLIP AT BS 751, S21R IAW EA 130156. 2 L 7 2 4F RT A2NM 20081208 NM 2008 12 8 SWAA086820 1 20081203 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED BETWEEN BS 360 TO BS 440, STR 21R. REMOVED AND REPLACED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086821 1 20081203 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED BETWEEN BS 360 TO BS 440, STR 22R. REMOVED AND REPLACED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086822 1 20081203 A 5310 6547978 CREASE BEAM BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CRACKED AT BETWEEN BS 616 TO BS 639, RBL 65, WL 208. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086783 1 20081203 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086831 1 20081204 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 496WN 32478 DURING SCHEDULED HC2 CHECK, FOUND FWD LT EMERGENCY EXIT BATTERY FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086823 1 20081204 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, BETWEEN STR 21L TO STR 22L. REMOVED AND REPLACED SHEAR T IE PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 UALA2008120406747 1 20081203 A 5420 WEB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CRACKED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 NR 2 PYLON UPPER WEB, OUTBOARD DRAIN HOLE CRACKED. MAJOR REPAIR ACCOMPLISHED. STOP DRILL CRACK. INSTALLED REPAIR DOUB LER AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081208 EU 2008 12 8 FDEA200811264986 1 20081126 A 5712 A5724081021400 RIB AIRBUS 300 A300B4622R 3930312 EU LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 LEFT WING RIB 5; HOLE "I" HAS A CRACK INDICATION. COMPLIED WITH FEDEX EA 6-5710-123674 WINGS, AD 99-16-01 - EO 6-5710-7 -5005, LT WING REAR SPAR, RIB 5 FITTING BOLT HOLE "G", "I", "M", AND "O". ORIGINAL EA ATTACHED TO SNRM N00846. 2 L 7 2 4F RT A35EU 20081208 NM 2008 12 8 UALA2008120106700 1 20081130 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 795UA 26927 EXIT PATH LIGHT NOT SECURE. LIGHT HANGS BY WIRE. AFT EEL LIGHT AT SEAT 1F IS BROKEN AND REMOVED. REPLACED LIGHT EMERG ENCY EVACUATION. CHECKED OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081208 NM 2008 12 8 FDEA200812045073 1 20081204 A 5310 ADA37521 BEAM DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 CABIN LEFT DOOR NR 3 FORWARD STOP, 5TH FROM TOP, FOUND CRACK APPROXIMATELY 2 INCHES. CABIN LEFT DOOR NR 3 FORWARD CRACK ED STOP (BEAM) (5TH FROM TOP) REMOVED AS PER SRM 51-31-01 VOLUME II. NEW BEAM HOLES PICKED UP AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081208 EU 2008 12 8 UALA2008120106686 1 20081126 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 448UA 842 AFT PRESSURE BULKHEAD FRAME (LWR) IS CREASED AT FR70 BETWEEN STR 42L AND STR 43R. MAJOR REPAIR ACCOMPLISHED: REPLACED FRAME. 2 L 7 2 4F 4 F RT A28NM E40NE 20081209 NM 2008 12 9 UALA2008112506671 1 20081121 A 2432 18550000 BATTERY BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE MASTER FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 677UA 30029 EICAS MESSAGE, MAIN BATTERY CHARGER WILL NOT CLEAR. REPLACED MAIN BATTERY. OPS CHECKS GOOD. MESSAGE CLEARED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081209 NM 2008 12 9 UALA2008111304388 1 20080820 A 2421 CIRCUIT BREAKER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT GENERATOR FAULTY A UALA D RETURN TO BLOCK W INADEQUATE Q C IN INSP/MAINT 1 WP 29 655UA 25393 LEFT GEN DID NOT STAY ONLINE AFTER ENG START. REPLACED GCU, NO HELP. REPLACED IDG, NO HELP. REPLACED GENERATOR CONTRO L BREAKER C901 UP TO IDG PHASE CABLES. SYSTEM TEST GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081209 NM 2008 12 9 UALA2008111305443 1 20080823 A 4920 380029817 APU BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 664UA 29236 APU WILL NOT START. FADEC SHOWED NO FAULTS. STARTED AND RAN APU WITH AIR AND ELECTRICAL LOADS AT GATE. COULD NOT REPL ICATE FAULT. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081209 NM 2008 12 9 UALA2008111306499 1 20081112 A 2497 WIRE HARNESS BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 ENGINE FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 786UA 26938 NR 2 ENG IDG WILL NOT DISCONNECT. SWAPPED NR 1 AND NR 2 IDG DISCONNECT SWITCH ON OVERHEAD, NO HELP. REMOVED ALL IDG EL ECTRICAL CONNECTORS, NO BENT PINS OR DEFECTS NOTED. SUSPECT BAD IDG FROM STOCK. NEW IDG ON ORDER. REPLACED IDG, NO HE LP. GCU BITE TEST OK. CHECKED PWR & GND AT CONN DM24001A, CHECKS OK. SOLENOID CHECKS OK. RAN ENG 4 TIMES, GOT IDG TO DISCONNECT ONE TIME. NEED A HEA PAR (PARTIAL) REPLACED IDG, NO HELP. FOUND BAD HARNESS SHORTED TO GROUND. REPLACED H ARNESS. IDG DISCONNECT CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081209 EU 2008 12 9 UALA2008112406631 1 20081123 A 3397 WIRE HARNESS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SEAT 22 SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 486UA 1620 EMERGENCY LIGHTS FAIL TEST. SHOWS EPSU INT LOAD EMER L. FOUND SHORT O GROUND CONNECTOR 11WL SOCKET "T" REF AWM 33-51-0 4, CHASING WIRES. FOUND HARNESS SHORTED AT SEAT 22. REPLACED LIGHT ASSY, CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20081209 WP 2008 12 9 22AA20081102 1 20081201 A 2740 CONTROL CABLE DOUG DC8 DC863F 302198F WP STABILIZER BROKEN A 22AA O OTHER O OTHER DE DESCENT 1 SO 29 784AL 46135 ON DESCENT LONG TRIM SUITCASE HANDLE, RIGHT SUITCASE HANDLE JAMMED. FOUND BROKEN CABLE RUNNING NR 49B. REMOVED AND REP LACED 1/16 CONTROL CABLE RUNNING NR 49B IN ACCORDING WITH DC-8 MAINTENANCE MANUAL 27-40-01. RIGGING AND OPERATION CHECK ED, FOUND NORMAL IN ACCORDING WITH DC-8 MAINTENANCE MANUAL 27-40-01. 2 L 7 4 4F 4A25 20081209 CE 2008 12 9 J7SA4527120081130 1 20081130 A 2612 74412135 FIRE LOOP LEAR 45 45LEAR 5170805 CE LT ENGINE FAULTY E J7SA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 05 435FX 45271 ON CRUISE, LEFT ENGINE FIRE RED EICAS WARNING APPEARED. WARNING WOULD EXTINGUISH WHEN THROTTLE RETARDED. CREW DIVERTED AIRCRAFT TO KGSO. MX TROUBLESHOOTING FOUND FAULTY ENGINE FIRE LOOP SECTION E24. REPLACED LOOP AND COMPLIED WITH SB 45 -26-03. ALL OPERATIONAL CHECKS NORMAL. 2 L 7 2 4F RT T00008WI 20081209 EU 2008 12 9 FDEA200812045086 1 20081204 A 5720 A5734008722000 SUPPORT AIRBUS 300 A300B4622 3930401 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 LT WING L/E LOWER PANEL NR 513AB SUPPORT CRACKED, LT WING L/E LOWER PANEL NR 513AB SUPPORT FWD CRACK STOPPED ON EXISTING HOLE; REPAIRED AREA IAW A300-600 SRM 53-15-63 PG 201. 2 L 7 2 4F RT A35EU 20081231 EU 2008 12 31 AALA200802444A 1 20081031 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70074 517 JFK - SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081231 EU 2008 12 31 AALA200802445A 1 20081031 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70074 517 JFK - SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081231 EU 2008 12 31 AALA200802446A 1 20081031 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70074 517 JFK - SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081231 WP 2008 12 31 AALA200802447A 1 20081101 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 443AA 49469 LGA - EXTERNAL OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR EXTERNAL OVERWING EMERGENCY LIGHTS. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081231 NM 2008 12 31 AALA200802449A 1 20081101 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 358AA 24039 MIA - EMERGENCY LIGHT AT SEAT 2B INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR INOPERATIVE EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 DL75E081736 1 20081214 A 3610 SHUTOFF VALVE BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE BLEED AIR SYS MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 27 723TW 29378 36-11-01 RIGHT ENG BLEED INOP. FLT CREW PLAC PER MEL 36-11-01 MTC NOTIFIED 1530Z MTC COORD. FOUND PRSOV WOULD NOT FULL Y CLOSE WHEN MANUALLY OPENED PER FIM. REPLACED SAME ENGINE, RUN CKS GOOD. MCO/PLACARD REMOVED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081231 NM 2008 12 31 DL76L081738 1 20081215 A 8011 774860A4 STARTER BOEING 767 767332 1382001 NM NR 1 ENGINE FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 195DN 28452 070908 NO ROTATION WHEN TRYING TO START LEFT ENGINE. L ENG STARTER EICAS MSG. FOUND STARTER BAD. STARTER NIS ATL. INSTALLED ROBBED STARTER FROM A/C 171 PER AMM. STARTER CHECKS GOOD. MFG P/N 774860A4. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 AALA200802571A 1 20081122 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMPS AT SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 DLM88081742 1 20081118 A 5755 FITTING DOUG MD88 MD88 3023688 NM LT SPOILER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 972DL 53215 070908 CRACKED FITTING FOR LT WING I/B FLIGHT SPOILER TORSION BAR O/B SIDE STA XRS=233. CRACKED FITTING FOR LT WING I/B FLIGHT SPOILER TORSION BAR WAS REPLACED IAW DRAWING 5923264. 2 L 7 2 4F RT A6WE 20081231 NM 2008 12 31 DL76G081744 1 20081216 A 2913 731966 PUMP BOEING 767 767332 1382001 NM HYDRAULIC SYS DEFECTIVE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 1602 29694 070908 C HYD PRIM 1 ANNUNCIATOR ILLUMINATED DURING TAXI. FOUND ELECTRICAL CONNECTOR PITTED ON C1 PUMP. REMOVED AND REPLACED C 1 PUMP AND CONNECTOR PIN B BURNT. REPLACED CONNECTOR D482. ALL LEAK AND OPS CHECK GOOD. PUMP MFG P/N 731966. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 DL757081748 1 20081217 A 5753 SPAR BOEING 757 757232 1384965 NM TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 619DL 22909 DURING SHOP VISIT, GROUND DAMAGE WAS FOUND TO THE OUTBOARD MAIN FLAP FRONT SPAR. THE WEB AND UPPER CHORD WERE DAMAGED. REPAIRED PER ERA 467854-14. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 DLM88081755 1 20081215 A 5620 PAN DOUG MD88 MD88 3023688 NM CABIN WINDOW CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 972DL 53215 RT PASSENGER CABIN WINDOW RING PAN AT FS 1041 HAD THE TYPICAL CRACK AT THE FWD LWR FASTENER, AND AN ELONGATED HOLE NEARB Y. THE WINDOW BELT DOUBLER ALSO HAD A SLIGHTLY MISDRILLED HOLE. THE CRACK END FASTENER WAS TRIMMED OFF, AND A REPAIR A NGLE INSTALLED. THE ELONGATED HOLE WAS BUSHED AND THE MISDRILL MARK WAS BLENDED OUT. THE INSTALLED REPAIR WAS FAA APPR OVED BY THE OEM BOEING. 2 L 7 2 4F RT A6WE 20081231 NM 2008 12 31 DL76L081708 1 20081210 A 8010 774860A4 STARTER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DAMAGED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 175DN 24803 724144 ON FIRST START ATTEMPT ON LEFT ENGINE IT HUNG START AT ABOUT 48 PERCENT N2. SUBSEQUENT ATTEMPTS HAD NO N2 ROTATION AND A STARTER VALVE LIGHT AND L STARTER EICAS MESSAGE. REMOVED AND REPLACED NR 1 ENG STARTER PER AMM MFN 774860A4, FOUND ST ARTER/GEARBOX COUPLING SHEARED. REPLACED SAME PER M/M. STARTED ENG, ALL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081231 NM 2008 12 31 DL76L081709 1 20081210 A 2750 FLAP BOEING 767 767332 1382001 NM WING MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 197DN 28454 ON TAXI OUT WITH FLAPS 5 RECEIVED STATUS MESSAGE T/E FLAP SHUTDOWN. PERFORMED WALK AROUND. NO DAMAGE NOTED TO FLAPS. BIT FSEU. SHOWED NO CURRENT FAULTS. T/E FLAP SHUTDOWN SHOWED INTERMITTENTLY BUT FLAPS STILL MOVED. CHECKED FLAP HANDL E RVDTS M603 AND M604 ON FSEU ALL VALUES GOOD AND NOMINAL FROM ZERO TO THIRTY. REPLACED RELAYS K350 AND K623 AS PRECAUT ION. RAN FLAPS ELECTRICALLY AND HYDRAULICALLY CHECKS GOOD. MCC NOTIFIED. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 SWAA087357 1 20081225 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 348, STR 2L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087358 1 20081225 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 342, STR 2L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087389 1 20081228 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 DL757081719 1 20081212 A 5420 112N700352 FITTING BOEING 757 757232 1384965 NM NR 2 PYLON WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 638DL 23761 THE NR 2 PYLON INBOARD SIDE LOAD FITTING WAS FOUND WORN AT THREE LOCATIONS ALONG THE INBOARD EDGE. LOCALLY BLENDED, ROT O PEENED, AND REFINISHED EACH DAMAGE LOCATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 DL76L081720 1 20081213 A 2121 UNKNOWN BOEING 767 767332 1382001 NM E&E BAY MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 177DN 25122 RTB AFTER ENGINE START FWD EQ COOLING VLV EICAS MSG. C/B 11P13 AND 11P22 PULLED AND RESET SYST, CYCLED AUTO/STBY VALV, OPERATION NORMAL. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 DL76L081721 1 20081213 A 5610 141T480014 WINDSHIELD BOEING 767 767332 1382001 NM COCKPIT CRACKED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 194DN 28451 DIV RT WINDSHIELD ARCED AND SUBSEQUENTLY CRACKED. REMOVED AND REPLACED WINDSHIELD AS PER MM 56-11-01, INSTALLED HIGH SP EED TAPE ON TOP OF SEALANT FIRST TORQUE PERFORMED. 2 L 7 2 4F RT A1NM 20081231 NE 2008 12 31 DL777081722 2 20081212 A 7250 GUIDE VANE BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 1 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 863DA 29735 051149 BORO NR 1 ENG HPC DUE TO PARAMETER SHIFT ON TRENDS AMM 72-00-00-200-802-R00. FOUND DAMAGE TO IPT NOZZLE GUIDE VANES BEY OND LIMITS REF M/M 72-000-00-200-810-R00-00 CHANGED ENGINE NR 1 PER TRANSMITTAL 11T00. 2 L 7 2 4F 4 F RT T00001SE E00050EN 20081231 NM 2008 12 31 DL76G081723 1 20081213 A 2530 OVEN BOEING 767 7673P6 1385105 NM FWD GALLEY FOD A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 156DL 25354 F/A IN FWD GALLEY REPORTED A LITTLE SMOKE/ELECTRICAL BURNING SMELL COMING FROM OVEN LOCATION 407. REMOVED PAPER LABEL F ROM OVEN RACK. OPERATED OVEN WITH NO SMELL OR SMOKE. 2 L 7 2 4F RT A1NM 20081231 NE 2008 12 31 DL75E081725 2 20081212 A 7200 PW2037RTC ENGINE BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE NR 2 MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 718TW 22738 28486 728746 DURING A CK INSP OF NR 2 ENG OIL FILTER FOUND FULL OF METAL PARTICLES MAGNETIC AND NON-MAGNETIC. FURTHER INSP OF CHIP D ET FOUND METAL ON MASTER, ANGLE GEARBOX, AND NR 4 BEARING DET. A CK WAS BEING PERFORMED JFK ON 12/12/08. CHANGED NR 2 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081231 NM 2008 12 31 DL76L081726 1 20081213 A 8011 PW40603 STARTER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE RT ENGINE FAULTY A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 1201P 65130 28458 724145 RT ENG WILL NOT GET MORE THAN 5 PERCENT N2 ROTATION DURING START. UNABLE TO PERFORM MAN START DUE TO TOOL NOT ALIGNING WITH HOLE. REMOVED VALVE REALIGNED ADJACENT DUCTING AND RE-INSTALLED VALVE. CLEANED C/P. REMOVED AND REPLACED STARTE R AS PER AMM. SPUN ENGINE. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081231 NM 2008 12 31 SWAA087381 1 20081229 A 5753 6573731 SKIN BOEING 737 7373H4 1384600 NM TE FLAP PUNCTURED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED MV2 CHECK, FOUND LT WING I/B FORE FLAP PUNCTURED THROUGH LOWER SKIN AT CENTERLINE OF FORE FLAP. REPAIR ED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087388 1 20081225 A 5752 654645521C TAB BOEING 737 7375H4 138449D NM LT AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED HC2 CHECK, FOUND LT WING AILERON TAB DELAMINATED AT I/B AND O/B TRAILING EDGE. REMOVED AND REPLACED TA B PER MM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087345 1 20081228 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, BELOW STR 9L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087346 1 20081228 A 5312 6517853 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087347 1 20081227 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 218WN 32489 DURING SCHEDULED MV1 CHECK, FOUND LT EEPLS COVER LOOSE AT ROW 1. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 ASAA0874029 1 20081210 A 5320 144A19044 CHANNEL BOEING 737 737790 13844CN NM CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION ON ANTENNA SUPPORT STRUCTURE (FWD CARGO BAY) STA 500-500A BL 0 WL 149. REMOVED FABRICATED AND INSTALLED REPLAC EMENT STRUCTURE. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 ASAA0874094 1 20081222 A 5320 111A13087 STIFFENER BOEING 737 737790 13844CN NM CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 VERTICAL STIFFENER AT BS 663 LBL 27 WL 155 IS CRACKED. REMOVED AND REPLACED VERTICAL STIFFNER. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 DL757081780 1 20081223 A 5711 SPAR BOEING 757 757232 1384965 NM LT WING DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 FWD SPAR UPPER CHORD OVER SIZED HOLES FROM FACTORY. CLEANED HOLE NDT, INSTALLED OVERSIZED FASTENERS. 2 L 7 2 4F RT A2NM 20090102 SO 2009 1 2 CHQA200800254 1 20081223 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 291SK 145486 CAE312631 DURING INSPECTION THE EMERGENCY FLOOR STRIP LIGHTING FROM ROWS 12 TO 19 WERE FOUND TO BE INOP. THE NR 6 EMERGENCY LIGHT INVERTER WAS REPLACED AND THE SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20090102 SO 2009 1 2 CHQA200800252 1 20081220 A 3297 14521495403 WIRE HARNESS EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL NLG OPEN A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 265SK 145226 CAE312062 FLIGHT 5936, CLE TO BDL. AFTER TAKEOFF THE FLIGHT CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS AND THE LANDING GEAR WOULD NOT RETRACT. THE FLIGHT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPORTED CMC MESS AGES OF LGEU FAIL AND NOSE WOW PROX SWITCH FAILURE. IT WAS THEN FOUND THAT THE NOSE LANDING GEAR PROX SWITCH WAS NOT GE TTING POWER AND WHEN A NEW HARNESS WAS SLAVED IN THE SYSTEM OPERATED NORMALLY. THE HARNESS WAS THEN REPLACED AND THE SY STEM OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20090102 SO 2009 1 2 CHQA200800255 1 20081224 A 3320 5113WW LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 575RP 14500847 CAE311948 CREW REPORTED A SMOKE SMELL FROM EMERGENCY ROW AROUND SEAT 10A. THE FLIGHT DIVERTED TO LEX AND LANDED WITHOUT INCIDENT. FOUND SIDEWALL LIGHT AT 10A INOPERATIVE AND DEFERRED THE LIGHT. THE LIGHT WAS LATER RELAMPED, CLEARING THE MEL AND NO OTHER DEFECTS WERE NOTED. 2 L 7 2 4T RT T00011AT 20090102 EA 2009 1 2 A6WA200840648 1 20081220 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A A6WA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 432AW 7257 LOG 188020/1 STRONG ODOR IN CABIN AND COCKPIT WITH APU AND ENGINE AIR SELECTED ON. DOES NOT DISSIPATE. 2 L 7 2 4F RT A21EA 20081230 SO 2008 12 30 RAIA2008121500001 1 20081211 A 2760 SWITCH EMB 145 EMB145EP 3260221 SO SPOILER SYS OUT OF ADJUST A RAIA O OTHER J WARNING INDICATION LD LANDING 1 CE 03 808HK 145157 CREW RECEIVED A SPOILER FAIL IN FLIGHT MESSAGE ON THE EICAS. MAINTENANCE ADJUSTED THE THRUST LEVER MICRO SWITCHES IN TH E QUADRANT. SPOILER INDICATOR SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 20081230 SO 2008 12 30 RAIA2008121500003 1 20081213 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 820HK 145064 EMERGENCY LIGHT INOPERATIVE/DIM. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE AFFECTED LIGHT. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 20081230 EU 2008 12 30 USAA2008122492316 1 20081204 A 5320 D53112818200 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - C8 - MAJOR REPAIR - NR 6131242 - CORROSION AROUND HOLES ON FLOOR SUPPORT BEAM UPPER AND LOWER SURFACE BETWEEN FR12 TO FR24, -Y254. REPLACED FLOOR SUPPORT BEAM UPPER AND LOWER SURFACE BETWEEN FR12 TO FR24, -Y254 IAW A320 51-72-17. 2 L 7 2 4F RT A28NM 20081230 2008 12 30 USAABA08033 4 20081219 A 2565 7A1509119 SLIDE AIRBUS 330 A330323 3940030 EU R3 DOOR FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 277AY 29380 108 380 LHR - MAINTENANCE REPORTED LOW PRESSURE FOR THE R3 DOOR. MEL 23-73-02E WAS ASSIGNED. FURTHER TROUBLESHOOTING ON 12/24/ 08 BY PHL MAINTENANCE PER TSM 25-62-00-810-801, PER STEP 3B(3)(A), FOUND THE R3 DOOR SLIDE AT FAULT. REMOVED AND REPLAC ED SLIDE PER AMM 25-62-42-04. CHECKS OK. CLEARED MEL 23-73-02E. 2 L 7 2 4F RT A46NM 20081230 NM 2008 12 30 USAABB08176 1 20081221 A 3397 CONNECTOR BOEING 767 7672B7 1385107 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 252AU 24765 MXP - THE ESCAPE PATH LIGHTING IN THE FIRST MAIN AISLE, NEAR DOORS 1L AND 1R WERE FOUND INOPERATIVE. MAINTENANCE RESTOR ED AN ELECTRICAL CONNECTION ON BOTH LAMP HOLDERS. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A1NM 20081230 EU 2008 12 30 USAA2008122492317 1 20081204 A 5315 D53472195202 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - C8 - MAJOR REPAIR - NR 6131422 - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 TO FR70, -Y465. REPLACED FLOORBEAM BETWEEN FR67 TO FR70, -Y465 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081230 NM 2008 12 30 USAA2008122492319 1 20081212 A 5320 D53480043205 REPAIR AIRBUS A319 A319132 3930340 NM R2 SILL CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL - C7 - MAJOR REPAIR - NR 6142505 - GALVANIC CORROSION ON EXISTING REPAIR AT SILL OF R2 DOOR, FR66, -Y1732. REPAIRED SILL IAW A319 SRM 53-41-14. 2 L 7 2 4F RT A28NM 20081230 NM 2008 12 30 USAA2008122492322 1 20081212 A 5347 D53112782200 SEAT TRACK AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL - C7 - MAJOR REPAIR - NR 6142502 - GALVANIC CORROSION ON CABIN FLOORBEAM SEAT TRACK AT FR20, -Y1292. REPLACED CABIN FLOORBEAM SEAT TRACK AT FR20, -Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081230 NM 2008 12 30 USAA2008122492323 1 20081211 A 5347 D53472090005 SEAT TRACK AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL - C7 - MAJOR REPAIR - NR 6142378 - GALVANIC CORROSION ON BEAM SEAT RAIL BETWEEN FR64 TO FR66, -Y1292. REPLACED BEAM SEAT RAIL BETWEEN FR64 TO FR66, -Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081230 NM 2008 12 30 USAA2008122492324 1 20081211 A 5347 D53472090002 SEAT TRACK AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL - C7 - MAJOR REPAIR - NR 6142384 - GALVANIC CORROSION ON BEAM SEAT RAIL BETWEEN FR64 TO FR66, Y765. REPLACED BEAM S EAT RAIL BETWEEN FR64 TO FR66, Y765 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081230 NM 2008 12 30 USAA2008122492325 1 20081211 A 5315 D53472192200 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL - C7 - MAJOR REPAIR - NR 6142390 - GALVANIC CORROSION ON CABIN FLOORBEAM BETWEEN FR66 TO FR70, Y765. REPLACED CABIN FLOORBEAM BETWEEN FR66 TO FR70, Y765 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081230 NM 2008 12 30 USAA2008122692328 1 20081217 A 5311 FRAME BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - MAJOR REPAIR - Q2 CHECK - NR 03C20853011/007, CRACKED FRAME AT BS 500D, S20L - S21L. REPAIRED FRAME AT BS 500D, S 20L - S21L IAW US AIRWAYS EA 100778. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 R61A20080054 1 20081227 A 3232 17070760903 ROD EMB ERJ170 ERJ170200LR 3260121 NM NLG DOOR BROKEN A R61A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 125HQ 2702 2702 17000202 CREW REPORTED AFTER GEAR WAS RETRACTED AND HAD 3 GREEN, STILL HAD A NOSE GEAR DOOR OPEN. CYCLED GEAR AND STILL HAD MESS AGE. FOLLOWED QRH PROCEDURES, LANDED WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO PITTSBURGH. MAINTENANCE REPLACED NOSE LANDING GEAR DOOR ACTUATOR ROD AND SYSTEM OPERATIONAL CHECK COMPLETED. ALL CHECK WERE GOOD AIRCRAFT WAS RETURNED TO SER VICE. 2 L 7 2 4F RT A56NM 20081230 NM 2008 12 30 R61A20080051 1 20081219 A 2450 70244401901 MODULE EMB ERJ170 ERJ170100SU 3260403 NM ZONE 100 FAILED A R61A O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 814MD 11856 11856 170000033 CREW REPORTED ON APPROACH, RECEIVED A MAU2B FAIL MESSAGE ON EICAS AND A RT BRAKE FAULT. CREW FOLLOWED QRH PROCEDURES, D ECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM AND REMOVED AND REPLACED MAU POWER MOD ULE AND COMPLETED OPERATIONAL CHECK OF SYSTEM. ALL CHECKS, OPERATIONAL CHECKS WERE GOOD AND RETURNED A/C TO SERVICE. 2 L 7 2 4F RT A56NM 20081231 WP 2008 12 31 AALA200802458A 1 20081102 A 8012 9794104 START VALVE DOUG DC9 DC983 3022083 WP NR 1 ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 9403W 53139 DFW INFLIGHT - NUMBER ONE ENGINE START VALVE INDICATION. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE START VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081231 NM 2008 12 31 AALA200802438A 1 20081030 A 3240 BRAKE BOEING 767 767323 1385205 NM ZONE 700 OVERHEATED A AALA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SW 21 393AN 29430 LAX DURING TAXI - NR 4 BRAKE OVER TEMPERATURE. FLIGHT CREW REPORTED THE BRAKE BRIEFLY CAUGHT FIRE. A FIRE SUPPRESSOR A GENT WAS DISCHARGED INTO THE BRAKE. NO FIRE DEPARTMENT ACTION WAS REQUIRED AND NO EVIDENCE OF FIRE WAS PRESENT ON BRAKE , TIRES OR PRESSURE LINES. REPLACED NUMBER FOUR BRAKE ASSEMBLY AND MAIN WHEEL AND TIRE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 AALA200802501A 1 20081110 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 760AN 31477 MIA - SEAT MOUNTED EMERGENCY LIGHT LAMP IS MISSING AT SEAT 21C. REPLACED LAMP AT SEAT 21C. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT T00001SE 20081231 EU 2008 12 31 AALA200802468A 1 20081106 A 3350 BR964814 LIGHT AIRBUS 300 A300B4605R 3930308 EU SEAT 9C BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14065 508 JFK - EMERGENCY LIGHT ASSEMBLY AT SEAT 9C BROKEN. REPLACED LIGHT ASSEMBLY AT SEAT 9C. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A35EU 20081231 EU 2008 12 31 AALA200802469A 1 20081106 A 3350 BR964814 LIGHT AIRBUS 300 A300B4605R 3930308 EU SEAT 9G BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14065 508 JFK - EMERGENCY LIGHT ASSEMBLY AT SEAT 9G BROKEN. REPLACED LIGHT ASSEMBLY AT SEAT 9G. SYSTEM GROUND CHECKED NORMAL OP ERATION. 2 L 7 2 4F RT A35EU 20081231 EA 2008 12 31 MASA2008122600755 1 20081226 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA FWD CARGO BAY ODOR A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 502MJ 10050 ASH 7152 CLT. PILOT REPORTED SMOKE SMELL IN FORWARD CARGO. MX INSPECTED AND FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 20081231 NM 2008 12 31 AALA200802532A 1 20081119 A 4920 351N110126 APU BOEING 767 767223 1385123 NM ZONE 100 AUTO SHUTDOWN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 332AA 21115 9288 22331 SFO INFLIGHT - DURING CLIMB AUXILLIARY POWER UNIT (APU) AUTO SHUT DOWN WITH LEFT INTEGRATED DRIVE GENERATOR ON MEL. RET URNED TO SFO AND LANDED WITHOUT INCIDENT. REPLACED APU ON 20 NOV AT SFO. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 DLM88081733 1 20081119 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 972DL 53215 CRACK ON FUSELAGE SKIN AT STA Y=1437 LONG 2RT. DAMAGE WAS REMOVED IAW SRM 53-04D FIG 27. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-30-2 AND IDENTIFIED IAW PS 900-5-1 NR 4. 2 L 7 2 4F RT A6WE 20081231 NE 2008 12 31 DL76L081768 2 20081218 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 MALFUNCTIONED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 173DN 76682 24800 724165 NR 2 ENG CHANGE DUE TO STAGGER. INSTALLED S/N 724715. 2 L 7 2 4F 4 F RT A1NM E24NE 20081231 NM 2008 12 31 AALA200802547A 1 20081121 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AA 24593 DFW - EMERGENCY LIGHT AT LEFT AISLE BULL NOSE AT SEAT ROW 27 BROKEN. REPLACED LIGHT ASSEMBLY AT LEFT AISLE BULL NOSE SE AT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802548A 1 20081121 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AA 24593 DFW - EMERGENCY LIGHT SHROUD AT AFT SEAT 3E IS BROKEN. REPLACED SHROUD AT AFT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OP ERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802549A 1 20081121 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AA 24593 DFW - EMERGENCY LIGHT SHROUD AT AFT SEAT 13D IS BROKEN. REPLACED SHROUD AT AFT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 DL76L081737 1 20081214 A 3697 CONNECTOR BOEING 767 767332 1382001 NM BLEED AIR SYS NOT SEATED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 184DN 27111 AFTER ENGINE START NO BLEED AIR FROM LEFT ENGINE WITH THE BLEED AIR VALVE SELECTED TO OPEN. RESEATED CONN ON LT ENG PRV AND HP CONT. CHECKED CONNECTIONS ON PRV AND HP VALVES. RAN LT ENG TO BLEED SHIFT AFTER UNLOCKING HPSOV DUE TO MSU. S EE NEXT ITEM. ENG BLEED OPS CHECK NORMAL PER AMM. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 USAA2008122292292 1 20081215 A 5522 65C1638915A TRIM TAB BOEING 737 7373G7 138447J NM LT ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 DELAMINATION ON LT ELEVATOR TRIM TAB SKIN AT NR 1, 2, 3, & 4 HINGE AREA. REPAIRED LEFT ELEVATOR TRIM TAB SKIN AT NR 1 H INGE AREA IAW SRM 51-70-17-0G. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 ASAA0844072 1 20081218 A 5311 FRAME BOEING 737 7374Q8 138447Q NM BS 767F DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 AFT CARGO FRAME HAS 1 EA ELONGATED HOLE BS 767F LBL 28 MARKED. REPLACED BS 767F FRAME PER SRM 51-70-11, 51-30-01, 51-20 -01, 51-40-02. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 DL76L081728 1 20081214 A 3320 FUSE BOEING 767 767332 1382001 NM CABIN LOOSE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 182DN 25987 AFTER 6 HRS SMELLED BURNING ODOR IN THE AFT GALLEY. INSPECTED AFT GALLEY AREA, NO EVIDENCE OF BURNING OR SMOKE. INSPEC TED ALL LIGHT FITTINGS AND FOUND INBOARD RIGHT AFT CEILING LIGHT INOP. RELAMPED, NO HELP. FOUND FUSE LOOSE AT M0065 CO NNECTOR CAUSING INTERMITTENT OPN, DISCONNECTED M00655 AND FWD TO MCO AND PLAC PER MEL 33-21-01. ALSO INSPECTED BULK CAR GO AREA, NO TROUBLE FOUND. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 DL757081766 1 20081218 A 5320 146N852247 SILL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 663DN 24992 THE AFT CARGO DOOR CUTOUT LOWER SILL OUTER CHORD WAS CORRODED. REMOVED AND REPLACED THE LOWER SILL OUTER CHORD. THE ST A 1380 AND 1440 FRAME WEBS WERE CUT TO GAIN ACCESS. 2 L 7 2 4F RT A2NM 20081231 NE 2008 12 31 DL76L081767 2 20081218 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 MALFUNCTIONED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 173DN 66472 24800 724142 NR 1 ENG CHANGE FOR STAGGER, INSTALLED S/N 727678. 2 L 7 2 4F 4 F RT A1NM E24NE 20081231 NM 2008 12 31 SWAA087399 1 20081229 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087390 1 20081227 A 2560 65C16820 HOLDER BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 606SW 27926 L1 DOOR EMERGENCY EVAC GIRT BAR HOLDER LOOSE. SECURED HOLDER PER MM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087391 1 20081224 A 3350 101114 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED MV2 CHECK, FOUND LT SIDE OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087392 1 20081226 A 3350 101114 COVER BOEING 737 7373A4 1384585 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED MV2 CHECK, FOUND OVERWING RT EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER M M. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087350 1 20081225 A 3350 9250071 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 259WN 35554 EEPLS BULB BROKEN AT ROW 1. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087393 1 20081227 A 3350 101114 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 902WN 36615 EMERGENCY EXIT LIGHT COVER MISSING. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087400 1 20081229 A 5311 6545808 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 291, BETWEEN STR 5R TO STR 19R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087355 1 20081225 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 390, ABOVE STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087363 1 20081225 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 775, STR 14R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087364 1 20081225 A 5330 6546881 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 961, STR 5R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087374 1 20081227 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 244WN 34864 FWD EEPLS LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087375 1 20081229 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, STR 6R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087382 1 20081227 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 430WN 33659 FWD CABIN EEPLS STRIP LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 ASAA0874111 1 20081229 A 5320 146A81273 SUPPORT BOEING 737 737790 13844CN NM CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION ON FLOOR TO SIDEWALL SUPPORT LOWER SIDE. REMOVED AND REPLACED AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT. BS 767-792 RBL 20 WL 156. 2 L 7 2 4F RT A16WE 20090102 EA 2009 1 2 A6WA200840647 1 20081217 A 3241 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA ANTI SKID SYSTEM MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION AP APPROACH 1 GL 31 431AW 7256 LOG 188366/3 ANTI-SKID INBD CAUTION MSG ON GEAR EXTENSION. T/S PER FIM 32-40-00. ASCU BITE SKID CHECK W/N PASS, R&R AN TI-SKID CONTROL UNIT IAW AMM 32-44-06. OPS TEST GOOD. 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 A6WA200840637 1 20081205 A 5313 STRINGER CNDAIR CL600 CL6002B19 1900309 EA BS 333-349 S27 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 414ZW 7586 STRINGER 27 FOUND CORRODED BTW FS 333. TO FS 349. CORROSION ON STR 27 BTW FS 333 TO FS 349. REMOVED IAW SRM 51-12-00. EDDY CURRENT PERFORMED ON BLEND OUT AREA, NO CRACKS FOUND. SURFACE FINISH RESTORED. 2 L 7 2 4F RT A21EA 20090102 NM 2009 1 2 F3LA2008123000729 1 20081225 A 2920 D3237010700000 MANIFOLD AIRBUS A319 A319111 3930336 NM HYDRAULIC SYS LEAKING A F3LA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 NM 21 934FR 2287 PILOT RETURNED TO BLOCK DUE TO LOSS OF GREEN SYSTEM HYDRAULIC FLUID. MAINTENANCE REMOVED AND REPLACED LANDING GEAR SAFE TY VALVE MANIFOLD IAW A319 AMM 32-32-17 PB 401. OPERATION AND LEAK CHECK NORMAL. 2 L 7 2 4F RT A28NM 20090102 SO 2009 1 2 FDKA2008122500323 1 20081225 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 851MJ 145572 FRL FLT 6193 PWM-JFK. MAIN DOOR HARD TO OPEN. MX LUBED DOOR ROLLERS AND SEAL OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 20090102 SO 2009 1 2 FDKA2008122600324 1 20081226 A 3350 INVERTER EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 FRL FLT 6289 JFK-PHL. OVERHEAD EMERG LIGHTS INOP. RESET THE INVERTER OPS CK GOOD. 2 L 7 2 4T RT T00011AT 20090102 NM 2009 1 2 SWAA087376 1 20081229 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 SWAA087377 1 20081228 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 428WN 29844 EEPLS TRACK LENS MISSING AT EMERGENCY EXIT ROW. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 SWAA087387 1 20081225 A 5754 65C26602301A WEDGE BOEING 737 7375H4 138449D NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT UPPER T/E WEDGE DELAMINATED. REPAIRED WEDGE PER MM. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 SWAA087344 1 20081227 A 2121 215201 GASPER FAN BOEING 737 7373H4 1384600 NM CABIN FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 29 362SW 26573 DURING DESCENT THERE WAS A STRONG SULPHER SMELL. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 SWAA087356 1 20081225 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 316, ABOVE STR 4L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 SWAA087365 1 20081225 A 5330 6546881 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 982, STR 5R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 SWAA087366 1 20081222 A 3350 PL22300 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED MV2 CHECK, FOUND EEPLS STRIP LOOSE AT ROW 20. REMOVED AND REPLACED EEPLS PER MM. 2 L 7 2 4F RT A16WE 20090102 EA 2009 1 2 SWIA200820644 1 20081215 A 3350 AD20131A BATTERY CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 340CA 661 661 10062 AFT CEILING OVERWING EMERGENCY LIGHT INOP (FLT 4399). REPLACED NR 3 BATTERY CHARGER AND BATTERY. P/N: AD-2013-1A, S/N ON: 11467, S/N OFF: 83440. 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 SWIA200820647 1 20081208 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 932SW 7714 EMERGENCY LIGHT SIGN NEAR MAIN CABIN DOOR INOP (FLT 5837). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081209 CE 2008 12 9 GLBA2008120501 1 20081202 A 5210 1015141961 HANDLE BEECH 1900 1900D 1154162 CE ASD DETACHED A GLBA K NONE O OTHER TX TAXI/GRND HDL 1 NM 21 881SK UE88 SIG EVENT - UPON ARRIVAL IN DEN IT WAS REPORTED THAT THE EXTERIOR AIRSTAIR DOOR HANDLE DETACHED FROM THE DOOR. ACFT HAD FERRIED TO CYS FOR REPAIRS AND WAS SUBSEQUENTLY GROUNDED TO LEASING AGREEMENT ISSUES. MX RE-INSTALLED THE AIRSTAIR DOO R EXTERIOR HANDLE IAW BEECH 1900D 52-10. OPS CHECK WAS OK. RII INSPECTION FOR THE AIRSTAIR DOOR EXTERIOR HANDLE INSTAL LATION COMPLIED WITH PER TASKCARD 4.3.14 AND WORKED SATISFACTORY. 2 L 7 2 4T RT A24CE 20081209 EA 2008 12 9 SWIA200820575 1 20081004 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 466SW 7856 C-CHECK, RIGHT SIDE FS 621 ANGLE CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081209 NM 2008 12 9 YENA200812020123 1 20081127 A 2782 1703909 ACTUATOR EMB ERJ190 ERJ190100IGW 3260408 NM LE SLAT MALFUNCTIONED A YENA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 EA 15 247JB 6656 190000042 FLT 1150, MCO-PWM, DIVERTED TO BOS, SLAT FAIL IN FLIGHT. T/S PER FIM 27-81-00-810-802A, FOUND SLAT ACT NR 6 TORQUE LIMI TER TRIPPED. REMOVED AND REPLACED PER AMM 27-81-01, OPS CHECK NORMAL. 2 L 7 2 4F RT A57NM 20081209 NM 2008 12 9 FDEA200809053729 1 20080905 A 2910 CONNECTOR DOUG MD11 MD11F 3023600 NM HYD SYSTEM LEAKING A FDEA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 21 586FE 46472 23624 48487 AFTER SLAT RETRACTION ON CLIMB OUT, RECEIVED "HYD 3 ELEV OFF" ALERT. APPROX 5 MINUTES LATER, GOT "HYD 3 FAIL" ALERT. COMPLIED WITH QRH. MANUALLY EXTENDED GEAR ON APPROACH. HYD LEAK FROM NR 1 HORIZ STAB TRIM MOTOR BODY. REMOVED AND REP LACED STAB TRIM MOTOR, MM27-43-30-4. DURING OPS CHECK FOR HORIZ STAB HYD OPS SYS, FOUND "HORIZ STAB TRIM RATE CTRL 2" C/B POPPED. TROUBLESHOT AND C/B STAYED IN AFTER DISCON ELEC CON FROM M1-16, BUT IT TRIPS IMMEDIATELY WHEN STATES ABOVE CONNECTOR RECONNECTED. TROUBLESHOT AND FOUND SHORT INSIDE OF DUAL SOLINOID VALVE ON M1-16 TRIM MOT REF WDM 22-22-01 P5 01. REMOVED AND REPLACED PER MM 27-43-41-4 AND HORIZ STAB HYD OPS NORM WITH NO LEAK PER MM 27-40-00-5. 2 L 7 3 4F RT A22WE 20081209 SO 2008 12 9 C2XA08RI176 1 20081111 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13965 145125 RIC - MX - DURING ROUTINE INSPECTION, MX FOUND OVERHEAD EMERGENCY LIGHT AT 12BC SEATS INOPERATIVE. MX REMOVED AND REPLA CED LAMP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081209 NM 2008 12 9 HNAA2008113000333 1 20081130 A 4950 167301101 APU DHAV DHC8 DHC8102 2809003 NM ODOR A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 982HA 21046 14667 380 UPON APU FAILURE, SMOKE ODOR FILLED THE CABIN AND COCKPIT. MAINTENANCE INSPECTED THE APU BAY AND FOUND NO LEAKS. APU W AS RUN FOR 10 MINUTES WITH AND WITHOUT BLEEDS ON. NO DEFECTS WERE NOTED AND NO ODORS WERE DETECTED. AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 20081209 NM 2008 12 9 FDEA200810034195 1 20081003 A 5310 2024T30071C CREASE BEAM BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 MAIN CABIN , CREASE BEAM, INBD CHORD BS 391, RBL 58, THERE IS A MISDRILLED HOLE, AND BS 430-418 HAS CORROSION RT. REMOV ED AND REPLACED CREASE BEAM, INBD CHORD, RBL 58, STA 297-395 IAW SRM 51-40-02. FOUND CORROSION OUT OF LIMITS IAW SRM 53 -10-15, L=9.0", W=1.5", D=.018". FABRICATED NEW CREASE BEAM ON MAE TRAVELER NR T8/760162. INSTALLED NEW CREASE BEAM, B S 297-395, RBL 58, IAW SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR. AT BS 418-430, RBL 58, NO CORROSION WAS NOTED AFTER AREA WAS CLEANED. 2 L 7 2 4F RT A2NM 20081209 NM 2008 12 9 HNAA2008111400334 1 20081114 A 2612 82460017013 PANEL DHAV DHC8 DHC8102 2809003 NM APU DEFECTIVE A HNAA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING TX TAXI/GRND HDL 1 EA 07 981HA 32145 32145 378 AFTER PUSHBACK FROM THE GATE, STARTED THE NR 2 ENGINE, TAXIED FROM THE GATE, NOTICED THE APU FAILURE LIGHT WAS ILLUM. T HE FLT ATTENDANT WAS NOTIFIED OF THE PROBLEM AS THE AFCT WAS TAXIED BACK TO THE GATE. THE CAPTAIN THEN ELECTED TO ACTIV ATE THE APU FIRE BOTTLE, SHUT DOWN THE ENGINE AND EVACUATE THE ACFT. ALL PAX WERE DEPLANED WITHOUT INJURY. ARFF CREWS WERE DISPATCHED TO THE AIRCRAFT. AFTER INSP, NO EVIDENCE OF SMOKE OR FIRE WAS FOUND. MX INSPECTED THE APU AREA. THE A PU FIRE BOTTLE, YELLOW BLOW-OUT DISC, AND APU RELAY PANEL WERE REPLACED. PERFORMED APU FIRE TEST AND OPS CHECKED THE AP U. ALL LEAK AND OPS CHECKS WERE GOOD AT THIS TIME. AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 20081209 NM 2008 12 9 HNAA2008112100337 1 20081121 A 2611 PU90461S SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM LAVATORY DEFECTIVE A HNAA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING NR NOT REPORTED 1 EA 07 908HA 59516 59516 015 THE LAVATORY SMOKE DETECTOR SOUNDED OFF ABOUT 10 TIMES WITHOUT EVIDENCE OF SMOKE OR FUMES. THE SMOKE DETECTOR WAS DE-AC TIVATED IAW SPECIAL PROCEDURES. MAINTENANCE REPLACED THE DEFECTIVE UNIT, RE-ACTIVATED THE SYSTEM AND OPS CHECKED THE UN IT. OPS CHECKS WERE GOOD AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 20081209 SO 2008 12 9 C2XA08RI177 1 20081203 A 2611 FAU751A4 CONTROL PANEL EMB 145 EMB145XR 3260214 SO LAVATORY DEFECTIVE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 41104 145646 FLIGHT 2966 - EWR - FLIGHT CREW REPORTED LAVATORY SMOKE INDICATION ON EICAS DURING CLIMBING WITH A SLIGHT SMELL OF SMOKE . CREW PERFORMED AIR RETURN AND LANDED AIRCRAFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED LAV SMOKE DETECTOR PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081209 WP 2008 12 9 AALA200810271 1 20081110 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 OUT OF LIMITS CORROSION REMOVAL. LEFT CUSP BETWEEN BS 560-579 AROUND LIGHTNING HOLE. INSTALLED DOUBLER PER AARD 53-20- 00-16. 2 L 7 2 4F RT A6WE 20081209 WP 2008 12 9 AALA200810274 1 20081110 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION ON RIGHT CUSP, STATION 1098-1117. INSTALLED CUSP SHEET, STATION 1098 TO STATION 1174 PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081209 WP 2008 12 9 AALA200810279 1 20081112 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 FOUND CORROSION ON FLOORBOARD SUPPORT. INSTALLED NEW FLOORBOARD SUPPORT. 2 L 7 2 4F RT A6WE 20081209 WP 2008 12 9 AALA200810281 1 20081112 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 RIGHT CUSP CORRODED. INSTALLED NEW CUSP PER SRM 53-30 AND AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081209 NM 2008 12 9 AALA200820056 1 20081107 A 5347 CBE12641 GALLEY TRACK BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 666A 52891 25300 AFT GALLEY RT TIE DOWN CORRODED, REPAIRED TIE DOWN IAW SRM 53-60-51-2R. 2 L 7 2 4F RT A2NM 20081205 EA 2008 12 5 COMA2008112450004 1 20081121 A 2750 7805013 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 868CA 13392 7427 FLAPS FAILED AT 0 DEG ON APPROACH INTO DTW. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED FLAP CONTROL H ANDLE. 2 L 7 2 4F RT A21EA 20081205 EU 2008 12 5 NSVA2008044 1 20081129 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU CABIN ODOR A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 352CJ 352 SMOKE NOTICED IN CABIN AFTER NR 2 ENGINE START UP, AFTER STARTING ENGINE NR 2 (FIRST ENGINE START) SMOKE BEGAN ENTERING THE CABIN AT ROW 7. AFTER PERFORMING THROUGH INVESTIGATION OF CABIN, LOWER VENTS, COVE LIGHTS, ENGINE COMPARTMENT, AND RT BIRD CATCHER. FOUND NO EVIDENCE OF ANYTHING BURNING. RAN RT ENGINE W/ACM RUNNING WITH ALL BLEEDS ON FOR 30 MINUTES WITH NO INCIDENT. AIR SYSTEM OPS CHECK GOOD IN REF TO AMM 21-60-00. 2 L 7 2 4T RT A52EU 20081205 SO 2008 12 5 CHQA200800234 1 20081130 A 3397 WIRE EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL EMERGENCY LIGHTS BROKEN A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 286SK 145443 CAE311567 DURING INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOP. MAINTENANCE FOUND THE WIRE W102-8502-22 WIR E BROKEN AT ROW 13. THE WIRE WAS REPAIRED AND PIN 63 WAS REPLACED IN CONNECTOR P1060. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081205 NM 2008 12 5 UIEA200800343 1 20081121 A 5730 PANEL BOEING 747 7472D7B 1384803 NM ZONE 600 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 RT WING UPPER L/E PANEL HAS A 19 INCH COMPOSITE CRACK AT ILES 657.22, 5.0 INCHES FROM PANEL FRONT EDGE. PERMANENT REPAI R ACCOMPLISHED AS PER SRM 51-40-09 FIG 18, SHEETS 2 AND 5 AND SRM 51-40-12. REF ATLAS AIR EO 4757A467. 2 L 7 4 4F RT A20WE 20081205 NM 2008 12 5 ASAA0843907 1 20081029 A 5311 654655820 FRAME BOEING 737 7374Q8 138447Q NM BS 907 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAMED CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400-53EA-00267. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0843908 1 20081029 A 5311 654655018 FRAME BOEING 737 7374Q8 138447Q NM BS 787 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400-53EA-00267. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0843909 1 20081029 A 5311 65465264 FRAME BOEING 737 7374Q8 138447Q NM BS 400 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400-53EA-00267. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0873928 1 20081125 A 5320 453A161110 STRUCTURE BOEING 737 737790 13844CN NM BS 500 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 FWD CARGO BAY CORROSION ON AFT LT CAP STRIP ON BACKSIDE. REMOVED DAMAGED FCB AFT LT CAP STRIP AND FABRICATED REPLACEMEN T AND INSTALLED REPLACEMENT AFT LT CAP STRIP IN FCB. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0843911 1 20081029 A 5311 654652924 FRAME BOEING 737 7374Q8 138447Q NM BS 440 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME CRACKED. REMOVED DAMAGED SECTION. INSTALLED REPAIR ANGLES AND FILLER PER ASA EA 400-53EA-00267. 2 L 7 2 4F RT A16WE 20081205 EA 2008 12 5 COMA2008112650009 1 20081125 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 446CA 7546 ON APPROACH INTO YHZ, RECEIVED FLAPS FAIL CAUTION MSG, FLAPS FAILED AT 0 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY. C OMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW UP MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 COMA2008112650010 1 20081125 A 2916 73021 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA NR 2 HYD SYSTEM FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 958CA 31359 7111 EN ROUTE FROM CVG TO YYZ RECEIVED NR 2 EDP CAUTION MSG AND NR 2 HYDRAULIC SYSTEM LOW PRESSURE CAUTION MSG. A/C DIVERTED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED NR 2 HYDRAULIC SYSTEM RESERVOIR. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 ASAA0873929 1 20081125 A 5320 453A1611 STRUCTURE BOEING 737 737790 13844CN NM BS 497-500D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 FWD CARGO BAY CORROSION ON AFT RT CAP STRIP AROUND FASTENER HOLES BOTTOM SIDE. REMOVED AND REPLACED RT CAP STRIP. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0873930 1 20081124 A 5320 146A8123U6 WEB BOEING 737 737790 13844CN NM BS 795-847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON CENTER WEB CENTER THRESHOLD SCUFFPLATE AT AFT CARGO BAY. REMOVED REPLACED NEW CENTER WEB UNDER CENTER THRE SHOLD. 2 L 7 2 4F RT A16WE 20081205 SO 2008 12 5 CHQA200800227 1 20081118 A 2751 3633501003 SENSOR EMB 135 EMB135LR 3260305 SO ALLSN AE3007 AE3007A 03030 GL TE FLAPS INOPERATIVE A CHQA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 840RP 12764 12764 145725 CAE311921 FLIGHT 6010, LGA TO CMH - WHILE ON APPROACH TO CMH THE FLAPS WERE SELECTED TO 9 THE CREW RECEIVED A FLAP FAIL MESSAGE WI TH THE FLAPS REMAINING AT ZERO. MAINTENANCE REPLACED THE LEFT FLAP VELOCITY SENSOR AND THE FLAPS OPERATED NORMALLY. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081205 NM 2008 12 5 ASAA0843931 1 20081117 A 5755 654645258 SKIN BOEING 737 7374Q8 138447Q NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 NR 5 SPOILER LOWER INBOARD SURFACE HAS A CLUSTER OF DENTS APPROX 20. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLE R AND BONDED REPAIR IAW SRM 51-70-10 REP 10. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0843934 1 20081120 A 5755 654645258 SKIN BOEING 737 7374Q8 138447Q NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 NR 5 SPOILER HAS A DENT WITH A CREASE ON THE UPPER SURFACE OTBD END. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER AND BONDED IAW SRM 51-70-10 REP 4. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0843935 1 20081117 A 5755 654645258 SKIN BOEING 737 7374Q8 138447Q NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 NR 5 SPOILER DENTED ON LOWER SURFACE CENTER AREA 9 IN FROM T/E. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER AND BONDED IAW SRM 51-70-10 REP 4. 2 L 7 2 4F RT A16WE 20090102 SO 2009 1 2 SWIA200820700 1 20081221 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 581SW 12824 12824 120349 THE AFT EMERGENCY LIGHTS GO DARK IN LESS THAN A MINUTE (FLT 5529). REPLACE AFT ELBP. P/N D366-04-001, S/N ON 971, S/N OFF 811. 2 L 7 2 4T RT A31SO 20090102 EA 2009 1 2 SWIA200820669 1 20081118 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 923SW 7664 UPPER FLOORBEAM ANGLE CRACKED AT LBL 9 AND RBL 9 (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081231 WP 2008 12 31 AALA200802519A 1 20081113 A 3510 15830AB REGULATOR DOUG DC9 DC982 3022082 WP CREW OXYGEN FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 481AA 49656 STL - INFLIGHT DTW TO DFW - CREW REPORTED LOSS OF CREW OXYGEN. LANDED STL WITHOUT INCIDENT. REPLACED PRESSURE REGULATO R FOR CAPTAINS OXYGEN AND REPLACED OXYGEN BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081231 WP 2008 12 31 AALA200802434A 1 20081030 A 3350 P401003130 LIGHT DOUG DC9 DC982 3022082 WP ZONE 200 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 574AA 53151 LGA - EMERGENCY LIGHT EXIT SIGN AT LEFT AFT STAIRWAY INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F A6WE 20081231 NM 2008 12 31 AALA200802448A 1 20081101 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 761AJ 31478 LHR - CAPTAINS SIDE DOME LIGHT INOPERATIVE. REPLACED LAMP FOR CAPTAINS SIDE DOME LIGHT. SYSTEM GROUND CHECKED NORMAL O PERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 AALA200802568A 1 20081122 A 3350 LAMP BOEING 737 737823 13844CB NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 962AN 30858 DFW - EMERGENCY LIGHT AT LT OVERWING HATCH HANDLE INOPERATIVE. REPLACED LAMP AT LEFT OVERWING HATCH HANDLE. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 DLM90081735 1 20081212 A 5511 5918000533 SPAR DOUG MD90 MD9030 3023690 NM HORIZ STAB DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DA 53388 RT HORZ STAB UPPER SKIN AND REAR SPAR UPPER CHORD FLANGE COMMON TO XFS 165 HAD AN EDGE DENT AND GOUGE. THE DAMAGE WAS T RIMMED OUT, TREATED AND PAINTED. 2 L 7 2 4F RT A6WE 20081231 EU 2008 12 31 AALA200802570A 1 20081122 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU ZONE 200 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7083A 645 JFK - EMERGENCY LIGHT IN CABIN INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081231 NM 2008 12 31 R61A20080048A 1 20081211 A 2782 ACTUATOR EMB ERJ170 ERJ170100SE 3260406 NM SLATS FAILED A R61A O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 873RW 17000144 ON APPROACH CREW REPORTED, RECEIVED A SLAT FAIL MESSAGE ON EICAS. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDEN T. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. MAINTENANCE CLEARED SF-ACE INHIBITS PERFORMED OPERATIONAL CHECK OF SYST EM, SYSTEMS OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A56NM 20081231 NE 2008 12 31 DL76L081747 2 20081214 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 MALFUNCTIONED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 44270 27583 727678 DUE NR 2 ENG CHANGE, STAGGER. INSTALL 724164. REPLACED NR 2 ENG PER TANS 1T149 AD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081231 NM 2008 12 31 ASAA0874030 1 20081213 A 5320 FLOOR SUPPORT BOEING 737 737790 13844CN NM BS 947-967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION WHILE WORKING CARD 5155617. FOUND FLOOR SUPPORT CORRODED AT BS 947 TO 967 RBL 50 WL 208 FWD FASTENER HOLES. DAMAGED FLOOR SUPPORT 100% MATERIAL LOSS AND WAS R&R. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 DL76L081778 1 20081222 A 2420 UNKNOWN BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE ELECTRICAL SYS MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 189DN 25990 724688 ON ENGINE START LT GEN DROPPED OFF LINE, GEN OFF LIGHT AND FIELD LIGHT AT AFT PNL CAME ON. RESET FIELD BIT BPCU FOUND U NDER FREQ TRIP. CLEARED MESSAGE, RAN ENG CHECKS, OK NO HISTORY. FAULTS DID NOT REOCCUR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081231 NM 2008 12 31 USAA20081213001 1 20081213 A 2150 10014566 FLOW VALVE EMB ERJ190 ERJ190100IGW 3260408 NM A/C PACK INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 964UW 825 19000197 FLIGHT 1772, CLT-DFW - AFTER TAKEOFF THE AIRCRAFT WAS UNABLE TO PRESSURIZE. THE CREW WAS PERFORMING OPS PROC WITH ECS O FF THE APU BLEED CLOSED PROPERLY AT 500FT, LEFT BLEED OPENED MOMENTARILY BUT THEN CLOSED RESULTING IN THE FOLLOWING EICA S MESSAGES; "X BLEED FAIL", "BLEED 1 OFF", "PACK 2 OFF", AND "BLEED APU VALVE". THE FLIGHT REMAINED BELOW 15,000 FEET W ITH THE APU POWERING PACK 1. MAINTENANCE THE NR 2 PACK CONTROL VALVE. 2 L 7 2 4F RT A57NM 20081231 NM 2008 12 31 SWAA087398 1 20081229 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 C77A88994 1 20081215 A 3260 PROXIMITY SENSOR EMB ERJ170 ERJ170200LR 3260121 NM RT MLG OUT OF ADJUST A C77A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 603CZ 17000176 ON CLIMBOUT FROM MSP THE CAPTAIN SELECTED GEAR UP AND THE INDICATION WAS STILL SHOWING THE LEFT MAIN LANDING GEAR WAS ST ILL EXTENDED. CAPTAIN THEN SELECTED THE GEAR HANDLE DOWN AND IT SHOWED ALL THREE GEAR DOWN AND LOCKED. CAPTAIN DID A R ETURN TO FIELD. MX PERFORMED A DVDR AND FHDB DOWNLOAD, THAT WAS ANALYZED BY EMBRAER. IT SHOWED THAT THE GROUND PROX SE NSORS ON THE RT MLG SHOWED A MISCOMPARE. ADJUSTED THE PROX SENSORS ON THE RT MLG, LUBED AND INSPECTED STRUT SERVICING. PERFORMED FUNCTIONAL CHECK OF LANDING GEAR SYSTEM, NO FAULTS WERE NOTED. PER THE DVDR DOWNLOAD GEAR WAS PHYSICALLY UP AND LOCKED. 2 L 7 2 4F RT A56NM 20090102 SO 2009 1 2 CHQA200800253 1 20081220 A 3350 100865 BATTERY PACK EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CABIN DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 564RP 12160 95 145524 CAE312502 DURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. THE NR 4 EMERGENCY LIGHT BATTERY PACK WAS REPLACED AND THE EMERGENCY LIGHTS OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081205 NM 2008 12 5 ASAA0843936 1 20081117 A 5755 654645258 SKIN BOEING 737 7374Q8 138447Q NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 NR 5 SPOILER LOWER SURFACE DENTED OUTBOARD END 11 INCHES FROM T/E. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER A ND BONDED IAW SRM 51-70-10 REP 4. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 DHLA2008752001 1 20081121 A 5754 SKIN BOEING 727 727223 1384074 NM KRUEGER FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 752DH BN402 22466 NR 3 K-FLAP HAS TWO SEPARATE CRACKS AT BOTTOM CENTER JUST ABOVE BULLNOSE APPROX WS 171.5. REMOVED AND REPLACED NR 3 K-F LAP OPERATIONAL CHECK GOOD. IAW M/M 27-81-01. 2 L 7 3 4F A3WE 20081205 EA 2008 12 5 MASA2008111700779 1 20081117 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAP MALFUNCTIONED A MASA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SW 07 37208 16239 7208 ASH FLT 7130 ORD. EMERGENCY DECLARED DUE TO FLAPS FAILED AT ZERO DEGREES DURING DESCENT. MX REMOVED AND REPLACED RT BP SU, RIGGED FLAPS AND RIGGED BPSU'S OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 ZZDA2008175 1 20081119 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 967AT 55028 DAMAGE DONE TO AIRCRAFT BY BELT LOADER UNDERSIDE OF TAIL SECTION BY AFT CARGO DOOR. REMOVED DAMAGED SKIN AND INSTALLED NEW SKIN SECTION FROM STA 980-1053 L26LTO L26R IAW B717 SRM 53-00-01 FIG 201 AND DWG 5919707 ON AAR W/O 28493 NRWC 6468 FOR COMPLETE DETAILS. 2 L 7 2 4F TR A6WE 20081205 NM 2008 12 5 UPS08553969 1 20081121 A 5610 012N377113 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT FAULTY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 468UP 25484 INSPECTION TYPE:N/A L2 WINDOW WOULD NOT CLOSE AND LOCK. ACCOMPLISHED INSTALLATION OF CAPTAIN'S NR 2 WINDOW PER MM 56-11 -02-4 UP TO AND INCLUDING STEP D 98. 2 L 7 2 4F RT A2NM 20081205 NM 2008 12 5 ASAA0873951 1 20081203 A 5320 SUPPORT CHANNEL BOEING 737 737790 13844CN NM BS 500A-500D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON RT FLOOR TO SIDEWALL SUPPORT BS 500A-500D. REWORKED CORROSION ON FLOOR TO SIDEWALL SUPPORT RT BS 500A-500D 1 INCH BY 4 INCH BY .006 INCH ORIGINAL MAT THICKNESS .040 FOUND OUT OF LIMITS AND REMOVED AND REPLACED SUPPORT PER SRM 51-10-02 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 ASAA0873946 1 20081111 A 5344 411A2119175A HINGE BOEING 737 737790 13844CN NM BS 975 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 AFT ENTRY DOOR LOWER HINGE PANEL CRACKED. REMOVED AND REPLACED HINGE PANEL. 2 L 7 2 4F RT A16WE 20081205 EA 2008 12 5 SWIA200820526 1 20080916 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 465SW 7845 DURING C-CHECK, FS 625 FLOORBEAM CRACKED AT STRINGER 13. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820528 1 20081007 A 3213 PISTON CNDAIR CL600 CL6002D24 1390016 EA RT MLG CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 806SK 15070 DURING C-CHECK, RIGHT MLG PISTON BLISTERED BETWEEN AXLES. REPAIRED PER CMM. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820529 1 20081007 A 3211 NUT CNDAIR CL600 CL6002C10 1390015 EA LT MLG CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 718SK 10184 DURING C-CHECK, LEFT MLG OUTER CYLINDER GLAND NUT INTERFACE CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820530 1 20081007 A 3211 NUT CNDAIR CL600 CL6002C10 1390015 EA RT MLG CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 718SK 10184 DURING C-CHECK, RIGHT MLG OUTER CYLINDER GLAND NUT INTERFACE CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820531 1 20081007 A 5343 PIN CNDAIR CL600 CL6002C10 1390015 EA RT MLG TRUNNION CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 718SK 10184 DURING C-CHECK, RIGHT MLG AFT TRUNNION PIN CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820536 1 20081124 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 961SW 7857 FLT 5923 - LAST CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820537 1 20081126 A 3397 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS SHORTED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 948SW 7789 FLT 6615 - CABIN EMERGENCY LIGHTS BETWEEN ROWS 9-12 INOP. REPLACED HARNESS ASSEMBLY FOR AFT EMERGENCY LIGHT STRIP. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820540 1 20081125 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 760SK 10223 FLT 5890 - CENTER OVERHEAD CABIN EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820541 1 20081125 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 740SK 10196 FLT 6732 - RIGHT SIDE LOWER WALL MOUNTED EMERGENCY EXIT SIGN HAS ONE LIGHT BULB INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820542 1 20081116 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 915EV 7754 VISUALLY INSPECTED THE LEFT AND RIGHT SIDE FRAMES AS REQUIRED BY AD 2008-06-10/01. BOTH SIDE FRAME DOUBLERS AT FS 640 INDICATE CRACKS. (AD INSP) REPAIRED PER SB 601R-53-065 REV B. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 SWIA200820543 1 20081201 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 728SK 10192 FLT 6684 - AFT TWO EMERGENCY OVERHEAD LIGHTS INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 UPS08M53984 1 20081116 A 5754 NRB67311 SKIN DOUG MD11 MD11F 3023600 NM LE SLAT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 INSPECTION TYPE:1C SURVEY SEQUENCE NUMBER 254-W3-008 LT WING 5 SLAT STA XORS 585 INNER SKIN REPAIR DOUBLER. NO SRM REF FOUND. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW MD-11 SRM 57-00-01 FIG 8. 2 L 7 3 4F RT A22WE 20081205 2008 12 5 UHLA2008110700005 4 20081121 A 3140 70244401930 POWER SUPPLY EMB ERJ170 ERJ170100SE 3260406 NM MAU DEFECTIVE A UHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 649RW 10092 17000070 FLIGHT 7610 ORD TO MSP - IN CRUISE CREW RECEIVED MAU3 FAIL. THE DECISION WAS MADE TO RETURN TO FIELD; AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MAU 3A POWER SUPPLY. 2 L 7 2 4F RT A56NM 20081205 NM 2008 12 5 ANCF200800027 1 20081031 A 2780 114T01151 CONTROL ROD BOEING 767 767259 1385136 NM LE SLAT DEFECTIVE A ANCF A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 23 986AN 24835 AIR TURN BACK REPORT LEADING EDGE SLAT ASYM EICAS MSG, DISPLAYED AT 400 FT WITH LEADING EDGE LIGHT ON WITH FLAPS TO 5 D EGREE WHILE TURNING LT WITH 180KTS, 25 DEGREE BANK, WITHOUT FLAPS MOVEMENT STICK SHACKER WAS ACTIVATED WITH NO REASON AN D STOPPED FEW SECONDS AFTER. IAW AMM 27-81-01 PAG 401 TO 429 THE INBD LEADING EDGE SLAT NR 7 WAS REMOVED. SLAT CONTROL ROD WAS REPLACED AND IAW 27-81-01 PAG 430 OPS TEST IS SATISFACTORY AND IAW AMM 27-88-01 PAG 214 TO 224 THE LEADING EDGE SLAT SENSORS W SWITCH TEST IS SATISFACTORY. IT WAS FOUND CRACKED SKIN FIXED LEADING EDGE RT STA WS 197.4 AND INBD SLAT 7 WAS REMOVED. IAW SRM 57-41-01 AND SRM 51-70-17 ITEM 4A PAG 16 THE LEADING EDGE SKIN STA 197, 4 WAS REPAIRED PHASE I 2 L 7 2 4F RT A1NM 20081205 WP 2008 12 5 NWAA085089871 1 20081015 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 780NC 48102 DURING LINE CHECK MX FOUND THAT BOTH OF THE EXTERIOR EMERGENCY LIGHTS WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AN D BOTH OF THE LIGHTS RETURNED TO AN OP CONDITION. 2 L 7 2 4F RT A6WE 20081205 NM 2008 12 5 USAA920082074 1 20081109 A 5320 65C334191 SHEAR WEB BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 MCN LAV SPILL MAJOR REPAIR NR 6135577 CORROSION ON SHEAR WEB AT BS1016, WL207.8, LBL19. REPLACED SHEAR WEB AT BS1016, W L207.8, LBL19 IAW B737 SRM 51-40-02-0G. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 USAA920082075 1 20081109 A 5320 65C3267723 SHEAR WEB BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 MCN LAV SPILL MAJOR REPAIR NR 6135576 CORROSION ON SHEAR WEB AT BS986.5, WL207.8, BETWEEN RBL38 TO RBL40. REPAIRED SHEA R WEB AT BS986.5, WL207.8, BETWEEN RBL38 TO RBL40 IAW BOEING DRAWING NR 65C32677. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 USAA920082073 1 20081109 A 5315 654681138 FLOORBEAM BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 MCN LAV SPILL MAJOR REPAIR NR 6135575 CORROSION ON FLOOR BEAM AT BS986.5, WL207.8, BETWEEN RBL40 TO RBL4. REPAIRED FLOO R BEAM AT BS986.5, WL207.8, BETWEEN RBL40 TO RBL4 IAW US AIRWAYS EA NR 130147. 2 L 7 2 4F RT A16WE 20081205 NM 2008 12 5 UALA2008112406640 1 20081124 A 3350 101072101 SIGN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 EXIT SIGN FELL OFF BY 2L. INSTALLED EMERGENCY EXIT SIGN DOOR 2L. 2 L 7 2 4F 4 F RT A2NM E17NE 20081205 EU 2008 12 5 UALA2008112406641 1 20081124 A 3350 78941 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 486UA 1620 SEAT 4A IS MISSING ONE OF TWO SEAT MOUNTED ELECTROLUMINESCENT. RELAMPED 4A, OPS CHECK OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081205 NE 2008 12 5 UALA2008112406648 2 20081121 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE DAMAGED A UALA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 29 225UA 30554 222024 METAL FOUND IN MASTER CHIP DETECTOR AND NO ROTATION OF ENGINE WITH ASSOCIATED ENG CONTROL, EEC C1 AND PMA MESSAGES. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081205 NE 2008 12 5 UALA2008112406649 2 20081124 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 717552 NR 1 ENGINE - CRACK FOUND IN 6-7 AIR SEAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081205 NM 2008 12 5 UALA2008112406650 1 20081124 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 FWD CARGO PIT FRAME TEE CAP CORRODED AT BS 654 +121 LBL 40 WL 125. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED TEE CAP SECTION, FAB NEW TEE CAP AND INSTALLED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081205 NM 2008 12 5 UALA2008112406655 1 20081124 A 5320 FLOOR SUPPORT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 MAIN CABIN STA 785.9 AT RBL 12 FLOOR SUPPORT CORRODED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION STA 785 TO 8 05, RBL 12. INSTALLED FILLER AND ANGLE REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081205 EU 2008 12 5 UALA2008112406656 1 20081123 A 2130 VFT300A1AMDTA VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN PRESSURE FAULTY A UALA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 29 482UA 1584 PRESSURIZATION PROBLEM. RTFL. REPLACE SKIN OUTLET VALVE 22HQ, AEVC COMPUTER 10HQ AND NR 2 SDAC. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081205 EU 2008 12 5 UALA2008112406630 1 20081122 A 5312 BULKHEAD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 448UA 842 AFT PRESSURE BULKHEAD WEB AT FR70 IS BENT BETWEEN STRINGERS 42L TO 43R, (K8847B). MAJOR REPAIR ACCOMPLISHED. REMOVED & REPLACED AFT PRESSURE BULKHEAD LOWER CENTER SECTION WEB BETWEEN STR 42L & 43R. 2 L 7 2 4F 4 F RT A28NM E40NE 20081205 WP 2008 12 5 AALA200810254 1 20081107 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 INTERCOSTAL IN CEILING AT STATION 1287 TO 1307 UPPER FRAME IS CRACKED AT 4 EACH FASTENERS. REMOVED AND REPLACED INTERCO STAL BETWEEN FLOORBEAM AT STATION 1287 AND 1309 PER SRM 51-01. 2 L 7 2 4F RT A6WE 20081205 WP 2008 12 5 AALA200810255 1 20081107 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 INTERCOSTAL CRACKED AT STATION 1271 AND 1287. REMOVED AND REPLACED INTERCOSTAL BETWEEN FLOORBEAM STATION 1271 AND 1287 PER SRM 51-01. 2 L 7 2 4F RT A6WE 20081205 NE 2008 12 5 AALA200802350 2 20081017 A 7261 ENGINE BOEING 767 767323 1385205 NM GE CF6 CF680C2B6 30025 NE NR 2 LEAKING A AALA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 353AA 2091 24034 695652 JFK INFLIGHT, CREW REPORTED SMOKE IN CABIN. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. FOUND OIL IN EIGHTH STAGE ARE A OF NUMBER TWO ENGINE. REPLACED NUMBER TWO ENGINE ON 19 OCT 2008 AT JFK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 20081205 NM 2008 12 5 ASAA0843916 1 20081023 A 5230 SKIN BOEING 737 7374Q8 138447Q NM AFT CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 AFT CARGO DOOR HAS DENT ON EXTERNAL SKIN DOUBLER REMOVED AND REPLACED AFT CARGO DOOR IAW B737 400 AMM 52 31 404 022 B00. 2 L 7 2 4F RT A16WE 20081205 EA 2008 12 5 ASOA200801559 1 20081116 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 713EV 10081 LT SIDEWALL SEAT RAILS HAVE SCATTERED CORROSION BETWEEN FS 394.00 TO FS 565.00. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 ASOA200801560 1 20081125 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 RT FS 559.0 BULKHEAD WEB HAS AN INDICATION NOTED APPROX .3 INCHES IN LENGTH, 55 PERCENT FULL SCREEN HEIGHT OTBD OF RBL 9 WL 58.70. FAILED NDT INSPECTION. REPAIRED RT FS 559 BULKHEAD CRACKED WEB AT WEB 58.70 BY INCORP REPAIR REO 601R-53-41- 821 TO BOTH LT & RT OF BULKHEAD. ALTERATION TO DOUBLER 2 AND THE SHIM IS COMPLETED IAW ECT/TC REO 601R-53-41-821 AND T HE SHIM IS COMPLETED IAW EC/TC REO 601R-53-41-821 AND THE ALTERATION MEETS ALL THE REQUIREMENTS OF REO 610R-53-41-821. C/W EC/TC REO 610R-53-41-260 IAW REO 610R-53-41-260 REV C. 2 L 7 2 4F RT A21EA 20081205 EA 2008 12 5 ASOA200801561 1 20081125 A 5312 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 VERTICAL BULKHEAD BEAM AT FS 409.00+128, LBL 18.00 LOCAL TO WL 69.00 HAS AN INDICATION NOTED APPROX 0.2 INCH LONG AND SI GNAL AMPLITUDE OF 80 PERCENT FULL SCREEN HEIGHT ON THE OTBD C-CHANNEL AFT RADIUS APPROX .5 INCHES BELOW TOP OF POST. RE MOVED DAMAGED POST ASSY AND AIR FILTER BRACKETS IAW SRM 51-42-06. FABRICATED STIFFENER. HEAT TREATED STIFFENER IAW SRM 51-24-21 AND DWG 601R32208 AND HEAT TREATED TO AMS 2770H. LPI FABRICATED STIFFENER IAW NDM 51-20-08. NO INDICATIONS NOTE D. INSTALLED POST AND AIR FILTER BRACKET IAW REO 610R-53-41-820 REV A & SRM 51-42-06. 2 L 7 2 4F RT A21EA 20081205 NM 2008 12 5 WRLA2008100 1 20081124 A 5320 WEB DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHK + C4 CHK, EGAT MECH FOUND FWD CARGO COMP WEB UNDER FLOOR CRACKED AT STA 6-50. REPAIRED CRACK AREA IAW ENGINEERING INSTRUCTION W2008A53B-1315 REV 00 AND EI W2008A53B-1315 REV 01. 2 L 7 3 4F RT A22WE 20081205 NM 2008 12 5 UALA2008112506659 1 20081122 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INTERMITTENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY LIGHT STRIP JUST AFT DOOR 1L GOES ON AND OFF UNCOMMANDED. PERFORMED EMERGENCY LIGHT CHECK. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081205 NM 2008 12 5 UALA2008112506662 1 20081124 A 3350 CNN3165Y LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FAIRING INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 RT EMERGENCY SLIDE LIGHT INOP AT FAIRING. RELAMPED. OPS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081208 SO 2008 12 8 C2XA08TY136 1 20081129 A 3350 66901 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16911 145446 THE 1ST FLOOR EMERGENCY PROXIMITY STRIP WILL NOT ILLUMINATE. REMOVED AND REPLACED PROX LIGHT STRIP IAW EMB 145 AMM 33-5 0-08. OPS CHECK GOOD. AIRCRAFT STILL IN C CHECK. 2 L 7 2 4F RT T00011AT 20081208 EA 2008 12 8 ASOA200801541 1 20081119 A 5340 ANGLE CNDAIR CL600 CL6002B19 1900309 EA INTERCOSTAL CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 LT FS 484 LBL 27 INTERCOSTAL ANGLE CRACKED. REMOVED AND REPLACED CRACKED INTERCOSTAL ANGLE IAW SRM 51-40-11 AND 51-42-2 1. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 A6WA200840606 1 20081112 A 5210 2R5206B ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FAILED A A6WA O OTHER O OTHER UK UNKNOWN 1 GL 31 452AW 10686 7835 LOG 192011/1 PAX DOOR WILL NOT LOWER COMPLETELY. HELD DOOR DOWN TO UNLOAD PASSENGERS, POWER ASSIST MOTOR FAILED. ASSIS T SPRINGS ALSO BAD. R&R PAX DOOR ACTUATOR IAW AMM 52-10-00, OPS CHECK OK. 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 A6WA200840634 1 20081204 A 5753 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING TE FLAP GOUGED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 414ZW 7586 RT WING INBD FLAP VANE L/E SKIN AT STA 57.00 GOUGED OVER LIMITS IAW REO 601R-57-52-004. RT WING INBD FLAP VANE LEADING EDGE AT STA 57.00 REPLACED IAW SRM 51-42-13. 2 L 7 2 4F RT A21EA 20090102 NM 2009 1 2 ASAA0874086 1 20081221 A 5720 115A62602 SUPPORT BRACKET BOEING 737 737790 13844CN NM RT WING BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 RT WING T/E I/B DEFLECTOR ROLLER FITTING I/B PANEL SUPPORT BRACKET BROKEN. R&R DEFLECTOR ROLLER FITTING I/B PANEL SUPPOR T. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 DLM88081730 1 20081114 A 5310 BEAM DOUG MD88 MD88 3023688 NM AFT CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 972DL 53215 EXFOLIATION CORROSION ON LWR BEAM OF AFT CARGO COMPARTMENT LWR DOOR JAMB BTW STA Y=1155-1212. REMOVED CORROSION IAW SRM 51-10-3, AREA FOUND OUT OF LIMITS. INSTALLED REPAIR PARTS IAW SRM 53-05 FIG 123 AND IDENTIFIED IAW PS 900-5-1 NR 4. 2 L 7 2 4F RT A6WE 20090102 EU 2009 1 2 F3LA2008123000732 1 20081228 A 2910 D3237010900800 SAFETY VALVE AIRBUS A319 A319112 3930323 EU LANDING GEAR LEAKING A F3LA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 21 943FR 30 2518 PILOT RETURNED TO BLOCK DUE TO LOSS OF GREEN SYSTEM HYDRAULIC PRESSURE. MAINTENANCE REMOVED AND REPLACED LANDING GEAR S AFETY VALVE AND PERFORMED OPERATIONAL CHECK IAW A319 AMM 32-31-17 PB401 AND 32-31-00-710-005. 2 L 7 2 4F RT A28NM 20090102 NM 2009 1 2 F3LA2008123000730 1 20081226 A 3397 ABS0364A10S CONNECTOR AIRBUS A319 A319111 3930336 NM CABIN FAILED A F3LA K NONE O OTHER UK UNKNOWN 1 NM 21 923FR 43 2019 PILOT REPORTED THAT THE EMERGENCY PATH LIGHTING WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED CONNECTOR 7245VC I AW A319 ELECTRICAL STANDARDS PRACTICES MANUAL 20-44-29. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNI T AT FIN 13WL IAW A319 AMM 33-51-38-000-001 AND 33-51-38-400-001. 2 L 7 2 4F RT A28NM 20090102 EA 2009 1 2 SWIA200820676 1 20081118 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 607SK 10251 LEFT WEB CORRODED AT FS 280 (C-CHECK). REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 SWIA200820678 1 20081104 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 967SW 7872 FS 280 BEAM CRACKED ON UPPER SIDE OUTBOARD OF RBL 9 AND LBL 9 (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090102 NM 2009 1 2 ASAA0874101 1 20081227 A 5320 INTERCOSTAL BOEING 737 737790 13844CN NM BS 737-192 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 DAMAGED FASTENER IN WEB. REMOVED AND REPLACED INTERCOSTAL WEB BS 767 TO 792 RBL 22 WL 156 160. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 ASAA0844105 1 20081213 A 5753 65C2632036 SKIN BOEING 737 737490 1384715 NM RT WING TE FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 794AS 28889 RT OTBD MID FLAP LOWER SURFACE GOUGED. REMOVED DAMAGED AREA FABRICATED FILLERS AND DOUBLER INSTALLED REPAIR IAW SRM 57- 53-01 FIG 201 EA 13093. 2 L 7 2 4F RT A16WE 20090102 NE 2009 1 2 ASAA0854114 2 20081225 A 7200 ENGINE BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 1 MALFUNCTIONED A ASAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 557AS 9810 35176 892792 ON PREFLIGHT CHECK RED BOX AROUND ENGINE NR 1 DIGITAL. GROUNDED YES. R&R NR 1 ENGINE PER T/C'S 78471000 AND 78471001 NO RED BOX NOTED ON N1 DISPLAY. ETOPS P/N CHANGE VERIFIED WITH MX CONTROL REF. IPC 72-00-00-01. FVR FLIGHT SUCCESSFUL. 2 L 7 2 4F 4 F RT A16WE E00055EN 20090102 2009 1 2 ASAA0854115 2 20081227 A 7261 M832481226 PACKING BOEING 737 737890 1384527 NM OIL CAP LOOSE A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 583AS 35681 WHILE SERVICING NR 2 ENG OIL SERVICING CAP PACKING VERY LOOSE GROUNDED YES. R&R PACKING OIL CAP P NR M83248 1 226 2 L 7 2 4F RT A16WE 20090102 EA 2009 1 2 SWIA200820679 1 20081104 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 967SW 7872 FS 280 BEAM CRACKED ON LOWER SIDE OUTBOARD OF LBL 9 (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 SWIA200820680 1 20081104 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 967SW 7872 FS 280 BEAM CRACKED ON LOWER SIDE OF OUTBOARD RBL 9 (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 SWIA200820677 1 20081102 A 5753 FITTING CNDAIR CL600 CL6002B19 1900309 EA TE FLAP CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 920SW 7660 RIGHT INBOARD FLAP INBOARD HINGE/FLAP ACTUATOR FITTING INBOARD BEARING CORRODED (C-CHECK). REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 SWIA200820699 1 20081217 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 928SW CEILING LEVEL EMERGENCY FLOOD LIGHT, THIRD AFT, INOP (FLT 5970). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 VNAA2008122200010 1 20081218 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A VNAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 05 250PS 7929 AFTER TAKEOFF FROM FAY CREW RECEIVED FLAPS FAIL MESSAGE 20 DEG. CREW ELECTED TO CONTINUE TO CLT AND LANDED WITHOUT INCI DENT. MAINTENANCE INSPECTED AIRCRAFT AND CYCLED THE FECU CIRCUIT BREAKERS. CHECKS WERE PERFORMED PER THE MANUFACTURERS MAINTENANCE MANUAL WITH NO FAULTS FOUND. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20090102 NM 2009 1 2 ASAA0844098 1 20081223 A 5730 65C26272 SKIN BOEING 737 7374Q8 138447Q NM LWS 589 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 LT WING FIXED LE HAS FIBER DAMAGE AT NR 1 SLAT I/B AUX TRACK CUTOUT. 2 L 7 2 4F RT A16WE 20090102 EA 2009 1 2 VNAA2008122600011 1 20081222 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A VNAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 05 226JS 7895 ON APPROACH INTO AVP THE CREW REPORTED FLAPS FAIL CAS MSG, FLAPS FAILED AT 37 DEGREES. AIRCRAFT LANDED WITHOUT INCIDENT . MAINTENANCE CHECKED FAULT CODES AND RESET SYSTEM AND CYCLED SYSTEM CB'S IAW SERVICE LETTER 00-001. NO DEFECTS WERE N OTED AND AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20090102 NM 2009 1 2 ZZDA2008187 1 20081221 A 5350 BALL BOEING 717 717200 1383700 NM TAILCONE DISLODGED A ZZDA K NONE N FALSE WARNING TO TAKEOFF 1 SO 37 979AT 55038 TAIL CONE UNLOCK ALERT IN FLIGHT. FOUND INSIDE BALL ON CABLE TO TAIL CONE SWITCH DISLODGED. REINSTALLED CABLE, LIGHT E XTINGUISHED IN COCKPIT. NO OTHER DISCREPANCIES NOTED PER MM 52-73-01 & 53-52-01. 2 L 7 2 4F TR A6WE 20090102 NM 2009 1 2 ASMF 20081203 1 20081221 A 2120 UNKNOWN BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE CABIN SMOKE W ASMF A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 23 852AM 33787 ACFT RETURNED, DUE TO SMOKE IN THE CABIN. THE ACFT WAS SENT TO THE HANGAR AND MX PERFORMED RT ENGINE CLEANING PROCEDURE IAW AMM 72-00-00 AND AIR PRESSURIZATION OPS TEST IAW AMM 21-31-00, ALL CORRECT. THE OVERWEIGHT INSP WAS NOT NECESSARY DU E TO THE ACFT LANDED WITH 53,500 KG AND THE MAXIMUM LANDING WEIGHT IS 58,059 KG. 2 L 7 2 4F 4 F RT A16WE E00055EN 20090102 WP 2009 1 2 ASMF 20081202 1 20081219 A 7800 0711346003 CONTROL VALVE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE THRUST REVERSER LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 205AM 11326 11325 49405 725745 DURING TRANSIT CHECK, A HYD LEAK ON THE RT ENG WAS DETECTED. MX TIGHTENED HYDRAULIC LINE AND REPLACED AND TESTED THE RT ENG REVERSE CONTROL VALVE IAW AMM 78-31-04, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 20090102 EA 2009 1 2 ASOA200801713 1 20081215 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN LOOSE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 752EV 10166 EMER LIGHTING STRIP LOOSE FROM FLOOR IN GALLEY 2 L 7 2 4F RT A21EA 20090105 NM 2009 1 5 C8GA20080043 1 20080824 A 5310 STRUCTURE BOEING 727 727223 1384074 NM BS 1133 DAMAGED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE EXISTING REPAIR AT BS 1133 BETWEEN STR. 21R - 22R REQUIRES REPLACEMENT. REMOVED EXISTING REPA IR, CUT OUT DAMAGE, FABRICATED FILLER, FABRICATED DOUBLER. INSTALLED REPAIR IAW SRM 53-30-2, 53-30-8. NO OTHER DEFECTS N OTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090102 NM 2009 1 2 F3LA2008122700728 1 20081225 A 3350 LIGHT AIRBUS A319 A319111 3930336 NM CABIN MALFUNCTIONED A F3LA K NONE O OTHER UK UNKNOWN 1 NM 21 923FR 2019 PILOT REPORTED THAT WITH THE CABIN EMERGENCY EGRESS LIGHT SYSTEM SET TO THE "OFF" POSITION, THE SEAT MOUNTED AISLE PATH LIGHTS AT SEAT ROW 15 AND AFT ON LEFT SIDE OF AIRCRAFT REMAINED ILLUMINATED. MAINTENANCE PERFORMED COMPUTER RESET OF CA BIN INTERCOMMUNICATION DATA SYSTEM NR 1 AND 2, REFERENCE TROUBLESHOOTING MANUAL 24-00-00-810-818. FAULT CLEARED. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 20090102 NM 2009 1 2 SWAA087380 1 20081229 A 5311 6546533 FRAME SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND FRAME SPLICE CRACKED AT BS 500, BETWEEN STR 13L TO 14L. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 ASAA0854113 1 20081225 A 4990 INDICATION SYS BOEING 737 737890 1384527 NM APU OIL FILTER TRIPPED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 559AS P7222 35178 APU OIL FILTER BUTTON POPPED. REQUIRES OIL FILTER INDICATOR SERVICING REF MM 49 91 13 PB 301 GROUNDED YES. ACCOMPLISHE D OIL FILTER IND. SERVICE. LEAK/IND CHKS GOOD. 2 L 7 2 4F RT A16WE 20090102 EA 2009 1 2 ASOA200801719 1 20081216 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 923EV 7826 RT FS 484 FLOOR SUPPORT INTERCOSTAL CRACKED .1" LONG AT RBL 36. COMPLETED REPAIR AT RT FS 484 FLOOR SUPPORT BRACKET AT RBL 36 IAW BOMBARDIER REO 601R-53-41-059. WORK PERFORMED IAW ASA EC/TC 601R-53-41-059. 2 L 7 2 4F RT A21EA 20090105 NM 2009 1 5 C8GA20080060 1 20080929 A 5347 BAC1520841 SEAT TRACK BOEING 727 727223 1384074 NM ZONE 200 CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE MAIN CABIN SEAT TRACK LOCATED AT BS. 760-850, LB L 45.5 HAD CORROSION. REMOVED SEAT TRACK FROM STATION 760-850, FABRICATED NEW SEAT TRACK, INSTALLED NEW SEAT TRACK IAW S RM 53-10-2, 53-10-5 & 51-10-2. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090105 EA 2009 1 5 ASOA200801725 1 20081222 A 5230 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 923EV 7826 CARGO DOOR SUPPORT BEAM AFT LWR ANGLE IS VISIBLY CRACKED IN TWO PLACES APPROX LENGTH ARE 1 1/2" 3/4" ANGLE PN IS 601R-35 050-109. 2 L 7 2 4F RT A21EA 20090105 NM 2009 1 5 C8GA20080062 1 20080930 A 5313 BAC1498143 STRINGER BOEING 727 727223 1384074 NM ZONE 100 CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT STR 25R LOCATED AT BS 720E +4 , HAD EXFOLIATED CORRO SION. REMOVED DAMAGED SECTION OF STR. FABRICATED NEW STRINGER, FABRICATED SPLICE, INSTALLED NEW PARTS IAW SRM 53-10-3, 5 3-10-2 NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090105 NM 2009 1 5 C8GA20080042 1 20080816 A 5310 STRUCTURE BOEING 727 727223 1384074 NM BS 1010 CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING VISUAL INSPECTION CORROSION WAS NOTED BETWEEN STR. 29L & 29R AT BS 1010. CORROSIO N WAS BEYOND LIMITS, DAMAGE WAS REMOVED. FABRICATED FILLER, FABRICATED DOUBLER. INSTALLED REPAR IAW SRM 53-30-2, 53-30-3 . NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090105 CE 2009 1 5 DXTA2008122203409 1 20081219 A 3260 INDICATOR CESSNA 500 560CESSNA 2076750 CE LT MLG INOPERATIVE E DXTA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 825QS 560655 EXTENDED LANDING GEAR- NO GREEN LIGHT ON LT MAIN GEAR. 2 L 7 2 4F RT A22CE 20090105 EA 2009 1 5 ASOA200801723 1 20081221 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE O OTHER AP APPROACH 1 SO 27 855AS 7395 FLAP FAIL ON FINAL APPROACH TO RUNWAY 27 (24DEG) MISSED APPROACH FLAPS FAIL APPROACH CW LANDED SAFELY OUT 25 ALT 2300, E MERGENCY DECLARED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200801710 1 20081213 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 355CA 10067 RT OVERWING EMERGENCY EXIT DOOR LOWER EMERGENCY EXIT LIGHT HAS SEVERAL BULBS BURNED OUT. 2 L 7 2 4F RT A21EA 20090105 CE 2009 1 5 DXTA2008122203410 1 20081219 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE MLG WEAK E DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 343QS 5600444 LEFT BRAKE PEDAL ON PILOT'S SIDE WILL NOT HOLD PRESSURE. WITH STEADY SLOW PRESSURE APPLIED, THE PEDAL GOES TO THE FLOOR. 2 L 7 2 4F RT A22CE 20090105 EA 2009 1 5 ASOA200801711 1 20081213 A 5320 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 CORROSION FOUND AROUND NUTPLATES IN AFT CARGO BELOW FLOOR BOARD AT DOOR. 2 L 7 2 4F RT A21EA 20090105 NM 2009 1 5 DXTA2008122303430 1 20081221 A 3240 BRAKE GULSTM 200 200 4500308 NM LEFT LOCKED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 708QS 069 LEFT BRAKE LOCKED ON LANDING BOTH LEFT MAIN TIRES BLOWN, WHEELS AND RIMS DESTROYED. 2 L 7 2 4F RT A53NM 20090105 NM 2009 1 5 DXTA2008122303431 1 20081222 A 2120 UNKNOWN AMD FALC50 FALCON2000 2730170 NM COCKPIT SMOKE E DXTA A G UNSCHED LANDING O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 290QS 190 SMOKE IN COCKPIT ORIGINATING FROM CENTER CONSOLE/FMS NR 2 AREA. 2 L 7 2 4F RT A50NM 20090105 NM 2009 1 5 DXTA2008122303426 1 20081221 A 3246 TIRE AMD FALC50 FALCON2000 2730170 NM MLG FAILED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 226QS 126 DURING APPROACH THE LANDING GEAR HANDLE WAS PULLED TO THE 2 ND POSITION 3 TIMES ( NO BRAKE LIGHT INDICATIONS) THEN ON LA NDING ALL 4 MAIN TIRES BLEW. 2 L 7 2 4F RT A50NM 20090105 NM 2009 1 5 DXTA2008122303433 1 20081222 A 3150 WARNING LIGHT RAYTHN 400 400ARAYTHEON NM ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 106QS RK381 HORIZ STAB FAIL ANNUNCIATOR CAME ON. 2 H 7 2 4F RT A16SW 20090105 NM 2009 1 5 DXTA2008122303427 1 20081221 A 3246 TIRE AMD FALC50 FALCON2000 2730170 NM MLG FAILED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 226QS 126 DURING APPROACH THE LANDING GEAR HANDLE WAS PULLED TO THE 2 ND POSITION 3 TIMES ( NO BRAKE LITE INDICATIONS) THEN ON LAN DING ALL 4 MAIN TIRES BLEW. 2 L 7 2 4F RT A50NM 20090105 CE 2009 1 5 DXTA2008122903448 1 20081228 A 3150 WARNING LIGHT CESSNA 680 680CE 2076811 CE ILLUMINATED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 375QS 6800230 ACM OVERTEMP AND EMERGENCY PRESSURE ANNUNCIATORS ILLUMINATED. SMALL AMOUNT OF SMOKE IN CABIN. 2 L 7 2 4F RC T00012WI 20090105 NM 2009 1 5 DXTA2008122303416 1 20081220 A 2910 HYDRAULIC SYSTEM GULSTM 200 200 4500308 NM LOW E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 720QS 085 AT FL350 WE GOT THE RT HYD LEVEL LOW CAS MESSAGE. DID THE EMERGENCY GEAR EXTENSION PER CHECK LIST. 2 L 7 2 4F RT A53NM 20090105 EA 2009 1 5 ASOA200900002 1 20081229 A 5320 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 IN PASSENGER COMPARTMENT FLOOR STRUCTURE FS 460.00 RBL 9.00 OUTBD INTERCOSTAL ATTACHMENT FITTING CRACKED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200900003 1 20081229 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 IN PASSENGER COMPARTMENT FLOOR STRUCTURE FS 484.00 LBL 9.00 OUTBD ATTACHMENT ANGLE CRACKED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200900004 1 20081229 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 IN PASSENGER COMPARTMENT FLOOR STRUCTURE FS 484.00 LBL 27.00 OUTBD ATTACHMENT ANGLE CRACKED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200900005 1 20081229 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 IN PASSENGER COMPARTMENT FLOOR STRUCTURE FS 280.00 LBL 9.00 INBD ATTACHMENT ANGLE CRACKED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200900010 1 20081229 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 REAR PRESSURE BULKHEAD FLOOR SUPPORT ANGLE FS 621 LEFT SIDE IS CRACKED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200900012 1 20081229 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 IN CARGO COMPARTMENT FLOOR STRUCTURE FROM FS 559.00+112 TO FS 621.00 RBL 36.00 SILL PLATE HAS MINOR CORROSION AROUND FAS TENER HOLES. 2 L 7 2 4F RT A21EA 20090105 CE 2009 1 5 DXTA2008122303429 1 20081221 A 3246 TIRE CESSNA 750 750 2076810 CE MLG FAILED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 947QS 7500047 RIGHT INBOARD MAIN TIRE BLOWN. RIGHT OUTBOARD MAIN TIRE BLOW. 2 L 7 2 4J RT T00007WI 20090105 CE 2009 1 5 DXTA2008122303419 1 20081220 A 3230 LANDING GEAR CESSNA 750 750 2076810 CE INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 960QS 7500160 AFTER TAKE-OFF , GEAR WOULD NOT RETRACT. 2 L 7 2 4J RT T00007WI 20090105 2009 1 5 DXTA2008122303420 4 20081221 A 2210 AUTOPILOT SYS CESSNA 560 560XL 2076702 CE MALFUNCTIONED E DXTA O OTHER S AFFECT SYSTEMS AP APPROACH 1 GL 07 667QS 5605365 WHILE ADVANCING THROTTLES ON APPROACH AUTOPILOT KICKS OFF, FLIGHT DIRECTOR REVERTS TO GO AROUND MODE. 2 L 7 2 4F RT A22CE 20090105 NM 2009 1 5 DXTA2008122303421 1 20081221 A 3230 INDICATION SYS RAYTHN 400 400ARAYTHEON NM MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 175QS RK574 ON TAKEOFF PERFORMED GEAR RETRACTION. 3 GREEN INDICATOR LIGHTS EXTINGUISHED AND GEAR INTRANSIT LIGHT ILLUMINATED AND REM AINED. 2 H 7 2 4F RT A16SW 20090105 NM 2009 1 5 AALA200802768 1 20081220 A 3520 OXYGEN MASK BOEING 757 757223 1384957 NM CABIN FAILED A AALA B A EMER. DESCENT UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SW 21 187AN 32381 AMA INFLIGHT EGE TO DFW - AT FL410, RIGHT CIRCULATION FAN FAILED FOLLOWED BY RIGHT PACK OVERHEAT INDICATION FOLLOWED BY LEFT PACK OVERHEAT INDICATION. EMERGENCY DESCENT ACCOMPLISHED. OXYGEN MASKS IN CABIN DEPLOYED MANUALLY. FLIGHT ATTEND ANT REPORTED SLIGHT BURNING ODOR. REPORTED SOME OXYGEN MASKS IN CABIN DID NOT DEPLOY. INSPECTED AIRCRAFT AND PREPARED FOR FERRY FLIGHT TO DFW FOR REPAIRS AND REPLACEMENT OF OXYGEN GENERATORS. 2 L 7 2 4F RT A2NM 20090105 NM 2009 1 5 AALA200820564 1 20081122 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 785AN 30005 MIA - EMERGENCY LIGHT AT SEAT 37C MISSING LENS. REPLACED LENS AT SEAT 37C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20090105 NM 2009 1 5 AALA200802485 1 20081108 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 641AA 24599 LGA - EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20090105 NM 2009 1 5 SWAA087420 1 20081230 A 5311 6546540 FRAME BOEING 737 7373L9 1384470 NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND RT FRAME OUTER CHORD WEB CRACKED AT BS 639, WL 209. REPAIRED WEB PER PAE ER. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087421 1 20081230 A 5330 6562212 SKIN BOEING 737 7373L9 1384470 NM BS 303 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS. 303, WL 234. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087422 1 20081230 A 5330 6562212 SKIN BOEING 737 7373L9 1384470 NM BS 305 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 305, WL 238. REPAIRED SKIN P ER PAE ER. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 R5KB15927 1 20081220 A 5315 FLOORBEAM BOEING 727 727212 138407G NM FUSELAGE CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 FLOOR BEAM UPPER CHORD CORRODED AT NUTPLATE. 2 L 7 3 4F A3WE 20090105 NM 2009 1 5 UHLA2008110700013 1 20081228 A 2797 WIRE HARNESS EMB ERJ170 ERJ170100SE 3260406 NM LE SLAT FAULTY A UHLA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 647RW 17000067 CREW HAD A SLAT FAIL ON APPROACH AND DECLARED AN EMERGENCY. THE ACFT LANDED WITHOUT INCIDENT. MX RELEASED ELECTRONIC B RAKE AND CLEARED SF-ACE INHIBITS. SI 278016 HAS BEEN WRITTEN TO REPLACE THE 3 / 4 SLAT HARNESS PART NRS 170-10231-401 L T AND 170-10232-401 RT. THE ACFT IS SCHEDULED FOR THE HARNESS REPLACEMENT 12/31/2008. 2 L 7 2 4F RT A56NM 20090105 NM 2009 1 5 USAA2008123092347 1 20081221 A 5347 D5713014720202 SEAT TRACK AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL MAJOR REPAIR C7 CHECK NR 6141076, CORROSION ON CABIN SEAT TRACK AT FR 36 - FR 41, +Y1292. REPAIRED CABIN SEAT TRACK AT FR 36 - FR 41, +Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20090105 NM 2009 1 5 USAA2008123092349 1 20081227 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST UK UNKNOWN 1 EA 19 814AW 1281 LOGPAGE: 8371748 FLT NR 162 LAS-SJC. FLASHLIGHT UNDER FORWARD GALLEY JUMPSEAT IS INOPERATIVE. R&R FORWARD FLASHLIGHT B ATTERY. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20090105 EU 2009 1 5 USAA2008123092353 1 20081226 A 3397 ABS0375A CONNECTOR AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS DAMAGED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 620AW 52 FLT 231 PHX-DTW - ELECTRICAL ODOR - FLIGHT ATTENDANT REPORTED ELECTRICAL ODOR BETWEEN ROWS 3 AND 4 LT. READING LIGHTS A T ROW 3 WOULD NOT TURN OFF. HOWEVER WHEN ENGINES WERE SHUT DOWN AND ELECTRICAL POWER REMOVED, LIGHTS WENT OUT. MX R&R THE POWER SUPPLY AND CONNECTOR DUE TO EXCESSIVE HEAT DAMAGE. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20090105 2009 1 5 USAA EMB08026 4 20081229 A 2312 VHF COMM EMB ERJ190 ERJ190100IGW 3260408 NM COCKPIT MALFUNCTIONED A USAA O OTHER G MULTIPLE FAILURE CR CRUISE 1 EA 19 964UW 19000197 FLIGHT 1839, BDL-PHL. THE ACFT LOST THE ABILITY TO TRANSMIT OR RECEIVE ON BOTH THE CAPTAIN'S AND THE FIRST OFFICER'S RA DIOS. ACARS DID NOT FUNCTION THEN RESUMED OPERATION ALLOWING THE CREW TO TRANSMIT INSTRUCTIONS FROM ATC. A COMMUNICATI ONS EMERGENCY WAS DECLARED AND THE CREW WAS GIVEN LANDING PRIORITY. A CIRCUIT BREAKER WAS RESET FOR "COMM AUDIO 2" ALL OWING LIMITED VERBAL COMMUNICATION WITH ATC FOR ARRIVAL AND LANDING. THE FLIGHT LANDED UNEVENTFULLY. MX RESET THE RADI O COMMUNICATION SYSTEM AND PERFORMED A GROUND OPS CHECK. 2 L 7 2 4F RT A57NM 20090105 NM 2009 1 5 USAA2008123092348 1 20081210 A 5347 D53233436200 SEAT TRACK AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL MAJOR REPAIR C7 CHECK NR 6141071, CORROSION ON CABIN SEAT TRACK AT FR 32 - FR 35, +Y765. REPAIRED CABIN SEAT TRACK AT FR 32 - FR 35, +Y765 IAW A319 SRM 53-21-15. 2 L 7 2 4F RT A28NM 20090105 EU 2009 1 5 USAA2008123192357 1 20081230 A 5315 D53472193200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656AW 1079 SAL C7 MAJOR REPAIR NR 6129695 GALVANIC CORROSION ON FLOOR BEAM AT -Y765 BTW FR66+5" TO FR70 OF PAX CABIN. REPLACED FLO OR BEAM AT -Y765 BTW FR66+5" TO FR70 OF PAX CABIN IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20090105 NM 2009 1 5 USAA2008123092346 1 20081212 A 5320 D53112833200 DUMMY RAIL AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL MAJOR REPAIR C7 CHECK NR 6142503, CORROSION ON CABIN DUMMY RAIL AT FR 16, -Y1379. REPLACED CABIN DUMMY RAIL AT FR 1 6, -Y1379 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20090105 NM 2009 1 5 USAA2008123192362 1 20081226 A 5313 65516989 STRINGER SPLICE BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT Q5 MAJOR REPAIR NR 03C10725042/001 2 CRACKS IN STRINGER SPLICE AT BS907, S4L. REPLACED STRINGER SPLICE AT BS907, S4 L IAW B737 SRM 51-10-2. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 USAA2008123192367 1 20081211 A 5315 D53472090010 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL C7 MAJOR REPAIR NR 6142389 GALVANIC CORROSION ON FLOOR BEAM BETWEEN FR64 TO FR66, Y1292. REPLACED FLOOR BEAM BETWEE N FR64 TO FR66, Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20090105 NM 2009 1 5 HALA2008122500904 1 20081225 A 2820 PRESSURE SWITCH BOEING 767 76733A 1385209 NM FUEL SYSTEM MALFUNCTIONED A HALA K NONE O OTHER CR CRUISE 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, LEFT FORWARD FUEL PUMP PRESS LIGHT ILLUMINATED FRM 28220305. PERFORMED FIM 28-22-00 FIGURE 10 6. NO DEFECTS FOUND. REPLACED LT FWD BOOST PUMP RELAY, (K185) AS PRE-CAUTIONARY. REPLACED LT FWD BOOST PUMP PRESSURE SWITCH (S70) PER AMM 28-42-01 AS PRE-CAUTIONARY. 2 L 7 2 4F RT A1NM 20090105 NE 2009 1 5 HALA2008122900911 2 20081229 A 7261 OIL SYSTEM BOEING 767 7673G5 1385126 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE LOW A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 586HA 24259 OPEN, ETOPS SIGNIFICANT SYSTEM, NR 1 ENG REQUIRED 10 PTS OIL SERVICE (.366PPH). REPAIR IN WORK. 2 L 7 2 4F 4 F RT A1NM E24NE 20090105 NE 2009 1 5 HALA2008123100914 2 20081231 A 7200 ENGINE BOEING 767 7673G5 1385126 NM PWA PW4062 PW4062 NE NR 2 BIRD INGESTION A HALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 586HA 24259 SUSPECT BIRD STRIKE NR 2 ENGINE AFTER LIFT OFF(+- 100'). CONFIRMED BIRDSTRIKE NR 2 ENGINE. ACCOMPLISHED FIM 71-05 -00 FIG 102. A/C NOW OK FOR SERVICE PER FIM. 2 L 7 2 4F 4 F RT A1NM E24NE 20090105 NM 2009 1 5 HALA2008122700907 1 20081227 A 5100 UNKNOWN BOEING 717 717200 1383700 NM AIRFRAME VIBRATION A HALA K NONE E VIBRATION/BUFFET CR CRUISE 1 WP 13 487HA 55132 AIRFRAME VIBRATION ABOVE FL250 IN CLIMB AND LEVEL AT FL260. PERFORMED GENERAL VISUAL INSPECTION OF EXTERNAL AREAS OF AI RCRAFT. FLIGHT CONTROLS AND GEAR DOORS, FILLET PANELS ACCESS PANELS, NO DEFECTS NOTED OK FOR SERVICE. 2 L 7 2 4F TR A6WE 20090105 2009 1 5 HALA2008122500903 4 20081225 A 3441 IRU BOEING 767 767332 1382001 NM OUT OF ALIGNMENT A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, PRE DEPARTURE RADAR TEST WX RADAR FAIL INDICATION ON MAP DISPLAY. CYCLED POWER ON AIRCRAFT. REALIGNED IRU'S. PERFORMED BITE PER FIM 34-43-00. SYSTEM OPS NORMAL. 2 L 7 2 4F RT A1NM 20090105 NM 2009 1 5 HALA2008123100915 1 20081231 A 4940 IGNITER BOEING 767 76733A 1385209 NM APU FAULTY A HALA K NONE O OTHER CR CRUISE 1 WP 13 580HA 28140 ETOPS SIGNIFICANT SYSTEM, APU FAILED TO START FAULT LIGHT ILLUMINATED EICAS MSG. APU FAULT DISPLAYED 2ND ATTEMPT NO RPM RISE. FOUND NO LIGHT OFF FAULT. REPLACED APU IGNITER PLUG AND LEAD PER AMM 49-41-02 AND 49-41-04. GRD OPS CHECK OK. 2 L 7 2 4F RT A1NM 20090105 2009 1 5 HALA2008122200898 4 20081222 A 2211 6224591512 COMPUTER BOEING 767 767332 1382001 NM AUTOPILOT SYS MALFUNCTIONED A HALA K NONE J WARNING INDICATION CR CRUISE 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM, AUTOPILOT DISCONNECT LIGHT ILLUMINATED. EICAS MESSAGE-AUTOPILOT DISCONNECT DISPLAYED AND LAND 3 DISPLAYED ON ASA. WITH CENTER AP SYSTEM ENGAGED IN COMMAND 2202084 3863 5203 CTR. PERFORMED MCDP TEST, FAULTS NO IN FLT. FCC CENTER GROUND TEST 01 FLT 01 FAULTS NO LAND 3, FCC LT-CTR CHANNEL AND FCC RT-LT CHANNEL CODE 111010 AND 121000 . REMOVED AND REPLACED CENTER FCC AMM 22-11-01 2823692. ACCOMPLISHED MCDP TEST NR 40, TEST PASSED. AIRCRAFT RETAINS LAND 3 STATUS, PER AMM 22-00-02. 2 L 7 2 4F RT A1NM 20090105 EA 2009 1 5 SWIA200820657 1 20081114 A 7830 CHANNEL CNDAIR CL600 CL6002C10 1390015 EA THRUST REVERSER CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 728SK 10192 DURING C-CHECK, LEFT LOWER TRANSCOWL 'U' CHANNEL CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820671 1 20081118 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 923SW 7664 C-CHECK, FLOOR SUPPORT INBOARD AND OUTBOARD CLIPS CRACKED AT LBL9 AND RBL9 FS280. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820706 1 20081221 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 611SK 10035 FLT 4799 - AFT OVERHEAD EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090105 SO 2009 1 5 SWIA200820708 1 20081226 A 3230 LANDING GEAR EMB 120 EMB120ER 3260203 SO SLUGGISH A SWIA K NONE O OTHER TO TAKEOFF 1 NM 07 569SW 120344 FLT 5579 - GEAR TOOK OVER 30 SECONDS TO RETRACT. REPLACED LANDING GEAR BOX. 2 L 7 2 4T RT A31SO 20090105 EA 2009 1 5 SWIA200820709 1 20081227 A 3234 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 07 445SW 7651 FLT 4543 - ON GEAR EXTENSION, RECEIVED A NLG GEAR DISAGREE WARNING MESSAGE. REPLACED NLG SELECTOR VALVE ASSEMBLY PN ON 750006000, PN OFF 601R75146-1, SN ON 1063, SN OFF 1928. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820710 1 20081222 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 910EV 7727 FLT 4502 - EMERGENCY LIGHT FORWARD CABIN INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820711 1 20081223 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 699BR 7801 FLT 5917 - OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 8. REPAIRED WIRING. 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 SWIA200820681 1 20081104 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 967SW 7872 FS 280 BEAM CRACKED ON UPPER SIDE OF OUTBOARD LBL 9 (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 ASOA200801718 1 20081216 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 923EV 7826 LT FS 484 FLOOR SUPPORT INTERCOSTAL CLIP CRACKED .1" LONG AT LBL 27. REMOVED AND REPLACED LT FS 484, LBL 27 FLOOR SUPPO RT INTERCOSTAL CLIP WITH NEW PART IAW CRJ 200 SRM 51-23-00, 51-40-11, 51-42-06, 51-42-21 AND 51-21-16. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200801712 1 20081214 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 FWD PRESS BULKHEAD CRACKED AT PASS THROUGH FOR LANDING GEAR MANUAL RELEASE CABLE. 2 L 7 2 4F RT A21EA 20090105 NM 2009 1 5 C8GA20080053 1 20080823 A 5754 MOUNT BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE NR 7 SLAT ACT CRACKED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE NR 7 SLAT ACTUATOR IB MOUNTING BRACKET HAD A 1" C RACK. REMOVED CRACKED SUPPORT. FABRICATED NEW DOUBLER FROM 301 1/2 HD .100" (7.5 X 3) AND NEW STIFFNER FROM BAC 1503-100 145 (9" X 4"). INSTALLED NEW SUPPORT PARTS IAW SB 727-57-0130. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SER VICE. 2 L 7 3 4F 4 F A3WE E2EA 20090105 NM 2009 1 5 C8GA20080044 1 20080824 A 5347 BAC15207927178T6 SEAT TRACK BOEING 727 727223 1384074 NM ZONE 200 DAMAGED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION NOTED THAT THE MAIN CABIN SEAT TRACK HAS ELONGATED HOLES AT BS. 720A -7 20D LBL 24.75. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-30-2, 53-10-5. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED T O SERVICE. 2 L 7 3 4F A3WE 20090105 EA 2009 1 5 ASOA200801724 1 20081222 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 923EV 7826 LT 621 FLOOR SUPPORT ANGLE CRACKED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200801708 1 20081212 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 684BR 7708 FLAPS FAILED AT 8 WHEN SELECTING 20 ON APPROACH. 2 L 7 2 4F RT A21EA 20090105 NM 2009 1 5 C8GA20080050 1 20080825 A 5752 TAB BOEING 727 727223 1384074 NM AILERON DENTED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION LEFT WING OUTBOARD AILERON TAB HAD A DEEP DENT. REMOVED DAMAGE AND FABR ICATED CORE & HOT BONDED. FABRICATED DOUBLER, HOT BONDED AND SEALED DOUBLER IAW SRM 51-40-20. NO OTHER DEFECTS NOTED. AI RCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090105 NM 2009 1 5 C8GA20080063 1 20081016 A 5313 BAC1498141 STRINGER BOEING 727 727223 1384074 NM ZONE 100 CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT STR 28R LOCATED AT BS. 490-510 HAD CORROSION. REMOV ED DAMAGED SECTION OF STR 28R FROM BS 480-508. FABRICATED NEW STRINGER, FABRICATED 2 EA SPLICES. INSTALLED NEW PARTS IAW SRM 53-10-3, 51-30-5 NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090105 NM 2009 1 5 C8GA20080052 1 20080825 A 5753 SKIN BOEING 727 727223 1384074 NM LT WING FLAP GOUGED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LT IB FOREFLAP AT THE UPPER SURFACE HAS A 10" GOU GE. REMOVED DAMAGED SKIN, FABRICATED CORE. FABRICATED DOUBLER. HOT BONDED CORE AND DOUBLER SEALED EDGES IAW SRM 51-40-20 . NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090105 NM 2009 1 5 C8GA20080058 1 20080818 A 5322 SHEAR TIE BOEING 727 727223 1384074 NM ZONE 100 CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE AFT CARGO COMPARTMENT SHEAR TIE LOCATED AT S29-30 L CORRODED. CORROSION FOUND TO BE OUT OF LIMITS, DAMAGE WAS CUT OUT. FABRICATED SHEAR TIE, HEAT TREATED TO T6. FABRICATE D DOUBLER. INSTALLED REPAIR AT BS 950E BETWEEN S29 TO 30L IAW SRM 53-10-4, 53-10-2. NO OTHER DEFECTS NOTED. AIRCRAFT WA S RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090105 CE 2009 1 5 DXTA2008122303424 1 20081221 A 2750 WARNING LIGHT CESSNA 750 750 2076810 CE TE FLAPS ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 07 919QS 7500224 DURING APPROACH TO LAND, RECEIVED "FLAPS FAIL" MESSAGE WHEN SELECTING 15*. 2 L 7 2 4J RT T00007WI 20090105 EA 2009 1 5 ASOA200801722 1 20081221 A 5100 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA DAMAGED A ASOA K NONE C F.O.D. AP APPROACH 1 SO 27 355CA 10067 BIRDSTRIKE ON FINAL APPROACH, EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 20090105 2009 1 5 DXTA2008122203414 4 20081220 A 2210 AUTOPILOT SYS RAYTHN 400 400ARAYTHEON NM MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED DE DESCENT 1 GL 07 131QS RK431 ON DESCENT THE RUDDER BOOST FAILED. AUTO PILOT DISCONNECTED & COPILOTS FD FAILED. 2 H 7 2 4F RT A16SW 20090105 NM 2009 1 5 DXTA2008122403436 1 20081224 A 3230 LANDING GEAR GULSTM 200 200 4500308 NM LEFT INOPERATIVE E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 740QS 194 LEFT MAIN LANDING GEAR WOULD NOT EXTEND. GOT A RED UNSAFE INDICATION. 2 L 7 2 4F RT A53NM 20090105 CE 2009 1 5 DXTA2008122403438 1 20081224 A 3320 LIGHT CESSNA 750 750 2076810 CE CABIN OVERHEATED E DXTA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 GL 07 949QS 7500049 LIGHT BETWEEN SEATS 7 & 9 OVERHEATED AND MELTED RUBBER HEAT GUARD. 2 L 7 2 4J RT T00007WI 20090105 EA 2009 1 5 ASOA200900015 1 20081230 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 FLOOR SEAT TRACKS AT LBL9 HAVE MINOR CORROSION FROM FS349 TO 977. BLENDED ON 2 SEAT TRACKS ON LBL 9, FS 349-FS 581 BOTH WERE BLENDED OUT OF LIMITS. REMOVED 2 SEAT TRACKS ON LBL 9, FS 349-FS 581. ON REMOVAL, NOTICED THAT THERE WAS FURTHER MORE EXTENSIVE CORROSION ON INBOARD SIDE OF TRACK. RECOMEND THAT ALL SEAT TRACKS ON LBL9 BE PULLED UP TO CHECK FOR CORR OSION ON INBOARD SIDE. ALL WORK DONE IAW CRJ 700 SRM 51-41-02, CRJ SRM 51-21-06 SAND CRJ 700 SRM 51-21-09. REMOVED AND REPLACED FLOOR SEAT TRACKS AT LBL9 HAVE MINOR CORROSION FROM FS349 TO 977 IAW CRJ700 AMM 53-00-49. 2 L 7 2 4F RT A21EA 20090105 CE 2009 1 5 DXTA2008122903442 1 20081226 A 5270 WARNING LIGHT CESSNA 560 560XL 2076702 CE CABIN DOOR ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 692QS 5605092 CABIN DOOR LIGHT CAME ON AFTER TAKE OFF. 2 L 7 2 4F RT A22CE 20090105 CE 2009 1 5 DXTA2008122903443 1 20081226 A 2751 WARNING LIGHT CESSNA 750 750 2076810 CE TE FLAPS ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 904QS 7500210 AMBER FLAPS FAIL CAS 2 L 7 2 4J RT T00007WI 20090105 NM 2009 1 5 DXTA2008122903445 1 20081227 A 3260 INDICATION SYS GULSTM 200 200 4500308 NM LT MLG ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 720QS 085 LEFT MAIN GEAR RED CROSS HATCHES ON RETRACTION 2 L 7 2 4F RT A53NM 20090105 CE 2009 1 5 DXTA2008122203411 1 20081219 A 2751 WARNING MESSAGE CESSNA 750 750 2076810 CE TE FLAPS ILLUMINATED E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 986QS 7500086 AMBER CAS MESSAGE FLAPS FAIL ILLUMINATED IN FLIGHT AND WOULD NOT RESET. FLAPS FAILED IN THE UP POSTION. THE SLATS DID NO T EXTENDED. 2 L 7 2 4J RT T00007WI 20090105 CE 2009 1 5 DXTA2008122303418 1 20081220 A 2750 FLAP SYSTEM CESSNA 560 560XL 2076702 CE TE FLAPS MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 661QS 5605677 AUTO PILOT DISENGAGED 5 SECONDS AFTER SELECTING FLAPS TO 15 DEGREES. AUTO PILOT FAIL AMBER LIGHT SHOWED ON PFD'S. 2 L 7 2 4F RT A22CE 20090105 EA 2009 1 5 ASOA200900013 1 20081229 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 FS 559.0 BULKHEAD WEB AND CAP ANGLE HAS INDICATIONS NOTED AT L CAP ANGLE LBL 18 APPROX .4" IN LENGTH 70% FSH AND RT WEB WL 54.10, WL 58.70 WK 54.10 APPROX .3" AND .5" IN LENGTH 100% FSH ALL FAILED NDT INSP. COMPLIED WITH REO 601R-53-41-260 , REPAIRE TO PRESSURE BULKHEAD STRUCTURE AT FS 559 BL 23L TO 23R AND MAINTENANCE INSTRUCTION CARD TASK RJ2-53-1. COMPLIE D WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260, REV C. 2 L 7 2 4F RT A21EA 20090105 CE 2009 1 5 DXTA2008121903407 1 20081218 A 2840 WARNING LIGHT CESSNA 750 750 2076810 CE ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 961QS 7500061 FUEL MTV FAIL L AMBER CAS MESSAGE CAME ON WHEN RT WING TO LT ENGINE CROSSFEED WAS SELECTED IN FLIGHT. 2 L 7 2 4J RT T00007WI 20090105 CE 2009 1 5 DXTA2008122303428 1 20081221 A 3246 TIRE CESSNA 750 750 2076810 CE MLG FAILED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 943QS 7500043 RIGHT OUTBOARD TIRE IS FLAT. RIGHT INBOARD TIRE BLOWN. LEFT OUTBOARD TIRE HAS FLAT SPOT WITH CORDS SHOWING. 2 L 7 2 4J RT T00007WI 20090105 EA 2009 1 5 ASOA200900018 1 20081230 A 5312 FITTING CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 830AS 7236 RELEVANT INDICATIONS OF CRACKS NOTED AROUND THE LINTEL ATTACHMENT FITTING ON THE AFT PRESSUR BULKHEAD. CRACKS MIGRATE A PPROXIMATELY 3/16" FROM THE UPPER, LOWER AND THE INBD EDGE OF THE FITTING. 2 L 7 2 4F RT A21EA 20090105 2009 1 5 SIMA200835002 2 20081214 A 7200 241244013002 ENGINE EMB 135 EMB135KL 3260302 SO VIBRATION A SIMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 21 844AE 145682 ON FLIGHT 3971, CREW REPORTED DURING CLIMB NR 1 ENGINE LP VIBRATION CLIMBED RAPIDLY TO MAX VIBRATION. NO PHYSICAL VIBRA TION BY EITHER FLIGHT CREW MEMBER OR FLIGHT ATTENDANT WAS NOTICED. CREW PERFORMED AOM EMERGENCY CHECKLIST AND SHUTDOWN NR 1 ENGINE AS A PRECAUTION. CREW DECLARED A EMERGENCY WITH ATC. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT . AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ENGINE VIBRATION MONITOR CONTROL MODULE. OPERATIONAL CHECK GOOD . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20090105 SO 2009 1 5 SIMA200836404 1 20081223 A 5320 14525480603 SILL EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 801AE 5000 145469 DURING HMBV, THE CARGO DOOR SILL WAS FOUND CORRODED. REMOVED CORRODED CARGO DOOR SILL. POSITIONED NEW SILL AND DRILLED FOR FASTENERS. CLEANED, ANODIZED, PRIMED AND INSTALLED NEW CARGO DOOR SILL IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20090105 SO 2009 1 5 SIMA200836405 1 20081223 A 5313 STRINGER EMB 135 EMB135KL 3260302 SO CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 801AE 5000 145469 DURING HMBV A CHAFE WAS DISCOVERED ON A PREVIOUS REPAIR REINFORCEMENT ANGLE ON STRINGER 19L. REMOVED DAMAGED REINFORCEM ENT ANGLE AND CLEANED THE AREA. FABRICATED A 1.4 INCH BY 16.25 INCH REINFORCEMENT, TREATED AND INSTALLED REPLACEMENT RE INFORCEMENT IAW EMB SRM 51-40-02 AND 53-24-02 FIG 201. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20090105 NM 2009 1 5 HALA2008122600908 1 20081226 A 5754 DOOR BOEING 717 717200 1383700 NM LE SLAT DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 478HA 55132 OPEN, LEFT SLAT DROOPING. FOUND LEFT WING NR 3 SLAT OUTBOARD SLAT TRACK DOOR DAMAGED, OK TO CONTINUE PER CDL. REMOVED DOOR. 2 L 7 2 4F TR A6WE 20090105 NM 2009 1 5 SWAA087408 1 20081230 A 3350 100031 COVER BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 637SW 27710 LT MID CABIN EMERGENCY EXIT LIGHT COVER FELL OFF. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20090105 2009 1 5 SWAA087409 4 20081230 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 729SW 27861 R1 EMERGENCY EVAC DOOR SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087411 1 20081230 A 5311 6546567 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO AFT BULKHEAD FRAME CORRODED AT BS 1006, BETWEEN STR 22L TO STR 23L. REPAIR ED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087431 1 20081230 A 5314 6545866 KEELBEAM BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND KEEL BEAM WEB CORRODED AT BS 710, BETWEEN LBL 6 TO RBL R. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087432 1 20081230 A 3350 20121 CHARGER BOEING 737 7373L9 1384470 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, EMERGENCY EXIT LIGHT BATTERY CHARGER INOP. REMOVED AND REPLACED CHARGER PER MM. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087428 1 20081230 A 5322 6546529 SHEAR TIE BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BBL 0. REMOVED AND REPLACED SHEAR TIE PER SRM.. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087429 1 20081230 A 5322 6546529 SHEAR TIE BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, LBL 17.7. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087430 1 20081230 A 5310 6547978 CREASE BEAM BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND RT CREASE BEAM WEB CRACKED AT BETWEEN BS 639 TO BS 667, WL 208. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20090105 EA 2009 1 5 SWIA200820656 1 20081114 A 3222 LUG CNDAIR CL600 CL6002C10 1390015 EA NLG CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 728SK 10192 DURING C-CHECK, NLG STRUT RIGHT TORQUE LINK LUG CORRODED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820738 1 20081121 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA CRACKED CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 C-CHECK, RIGHT INTERCOSTAL AT FS 484 RBL 27 CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820739 1 20081121 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 C-CHECK, LEFT INTERCOSTAL AT FS 484 LBL27 CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820742 1 20081121 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 C-CHECK, FS 280 BEAM RBL9 OUTBOARD CORNER CLIP CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20090105 SO 2009 1 5 SWIA200820701 1 20081215 A 3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO RT MLG OUT OF ADJUST A SWIA K NONE O OTHER TO TAKEOFF 1 NM 07 578SW 120346 FLT 5792 - RIGHT LANDING GEAR WOULD NOT RETRACT. ADJUSTED RIGHT MLG PROX SENSORS. 2 L 7 2 4T RT A31SO 20090106 EU 2009 1 6 FDEA200812165175 1 20081216 A 5414 SKIN AIRBUS 300 A300B4622 3930401 EU NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 NR 1 PYLON SKIN PNL. CRACKED AT FASTENER, AT RIB 8 O/B SIDE. REPAIRED CRACKED SKIN IAW AIRBUS REPAIR DWG R54610124. 2 L 7 2 4F RT A35EU 20081208 NM 2008 12 8 SWAA086775 1 20081202 A 5330 6545778 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086776 1 20081202 A 5330 6562212 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086777 1 20081202 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 904WN 36616 FOUND EGRESS LIGHT LOOSE AT ROW 1. REPAIRED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 HNAA2008120200328 1 20081202 A 3040 NP15790113 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM COCKPIT ARCED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 937HA 233 233 148 BURNING SMELL DETECTED ON FLIGHT DECK IN FLIGHT. INSP AND FOUND WIRE ON TERMINAL L1 FOR CAPTS WINDSHIELD HEAT LOOSE AND WIRE TERMINAL END DAMAGED. REPAIRED WIRE AS REQUIRED AND RESECURED WIRE TO TERMINAL L1 AND REMOVED AND REPLACED CAPTS WINDSHIELD HEAT CONTROLLER FOR MX CONVENIENCE, GROUND RAN A/C NO DEFECTS NOTED IAW -8 MX RUN MANUAL. 2 H 7 2 4T RT A13NM 20081208 WP 2008 12 8 AALA10162008001 1 20081016 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 CORROSION ON RIGHT HAND CUSP AT STATION 1179-1189. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081208 WP 2008 12 8 AALA10292008001 1 20081029 A 5311 FRAME DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 CORROSION IN AFT CARGO COMPARTMENT AT BS 1309 FRAME AFT SIDE AT L29R TO 30. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-10-00-14 FIG 1. 2 L 7 2 4F A6WE 20081208 NM 2008 12 8 KCSA081596 1 20081120 A 5414 SKIN BOEING 747 747212B 1384886 NM NR 2 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 NR 2 PYLON UPPER SKIN AFT EDGE DOUBLER APPEARS TO BE CRACKED .5 INCH AT NAC STA 221 O/B SIDE. 2 L 7 4 4F RT A20WE 20081208 NM 2008 12 8 SWAA086780 1 20081203 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT RADIO ALTIMETER SKIN CUTOUT, BS 430. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086812 1 20081203 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 FDEA200812035050 1 20081203 A 5313 ACA37962 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 DURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT RIGHT SIDE NOSE LANDING GEAR TRUNNION FITTING TRIM OUT, F OUND LONGERON CRACKED. CRACKED LONGERON AT RIGHT SIDE NOSE LANDING GEAR TRUNNION FITTING REMOVED AS PER SRM 51-31-01 VO LUME II. NEW LONGERON HOLES PICKED UP AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GM M 6-2-100. 2 L 7 3 4F RT A22WE 20081229 NM 2008 12 29 ASAA0874034 1 20081214 A 5311 141A83717 FRAME BOEING 737 737790 13844CN NM GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 FSD CUTOUT FRAME STRUCTURE GOUGED 1.35" FWD OF CUTOUT FED FRAME JUST OTBD OF TOP FWD STOP PAD FTG (MARKED). REPAIRED FR AME IAW EA 700 53EA 00 345 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 ASAA0874021 1 20081207 A 5320 143A812619 SUPPORT BRACKET BOEING 737 737790 13844CN NM BS 492-500 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 492-500 RBL 20. REPLACED FLOOR TO SIDEWALL SUPPORT (SHIELD). 2 L 7 2 4F RT A16WE 20081229 EA 2008 12 29 A6WA200840630 1 20081208 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 421ZW 7346 MWC 18 FS 621 PRESSURE BULKHEAD WEB THAT SURROUNDS THE ATTACHMENT FITTING IS CRACKED. PERFORMED A REPAIR BY CUTTING OUT SECTION OF WEB, FABRICATING AND INSTALLING REPAIR PARTS IAW REO 601R-53-61-1230 REV D. 2 L 7 2 4F RT A21EA 20081229 EU 2008 12 29 NWAA085503318 1 20081210 A 2120 UNKNOWN AIRBUS 330 A330323 3940030 EU CABIN ODOR A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 818NW 0857 FLIGHT ATTENDANTS REPORT LDMCR HAS VERY STRONG ODOR, HARD ON THE EYES AND CAUSED HEADACHES. LANDING WAS UNEVENTFUL. 2 L 7 2 4F RT A46NM 20081229 NM 2008 12 29 SWAA087338 1 20081222 A 5312 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 184, LBL 17.5, WL 233. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087326 1 20081222 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20090106 NE 2009 1 6 ASAA0954124 2 20081230 A 7200 CFM567B273 ENGINE BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 1 OIL CONSUMPTION A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 557AS 518 35176 896760 A/C 557 TOPPED FOR ENG. OIL SPIKE FOR NR 1 ENG. INSUFFICIENT DATA AVAILABLE FOR RE CALCULATING SPIKE REC. GROUNDED YES. AC ENG NR 1 BACK DOWN TO ETOPS CONSUMPTION LIMITS AT .23 RELEASED FROM TOP DEFERRAL. SEAMC JERRY NOTIFIED. 2 L 7 2 4F 4 F RT A16WE E00055EN 20090106 EU 2009 1 6 COEA2009010202913 1 20081231 A 5315 WASB08 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 913FX 2276 250 MAJOR REPAIR: M7 AEROSPACE STC ST01189WI, LT OTBD LONGITUDINAL FLOOR BEAM IS CRACKED JUST FWD OF FRAME 30. 2 H 7 2 4T RT A53EU 20090106 2009 1 6 COEA2009010204912 4 20081230 A 3425 7003360947 AHRS AEROSP ATR42 ATR42300 8680920 EU NR 1 FAILED A COEA A UNSCHED LANDING J I WARNING INDICATION FLT. ATTITUDE INST. CR CRUISE 1 NM 13 912FX 047 AIR TURNBACK: FLT NR 8202 JNU-SIT. ENROUTE TO SIT FROM JNU THE CAPT'S EFIS (ELECTRONIC FLIGHT INSTRUMENTS SYSTEM) COMP H EADING, PITCH, AND ATTITUDE FAILED. SINCE COPILOT'S SYSTEM WAS OPERATING NORMALLY. A DECISION TO RETURN TO JNU WAS MADE SINCE PARTS WERE NOT AVAILABLE IN SIT AND MX COULD BE ACCOMPLISHED. R&R NR 1 AHRU (ATTITUDE HEADING REFERENCE UNIT). 2 H 7 2 4T RT A53EU 20090106 EU 2009 1 6 FDEA200812175188 1 20081217 A 3234 224TS05Y CONTROL HANDLE AIRBUS 310 A310222 3930315 EU MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 453FE 267 AFTER T/O LANDING GEAR WOULD NOT RETRACT. THIS WAS CONFIRMED ON OVHD PANEL AS WELL. INTERROGATED MTP AND GOT 28V GEAR P WR SUPPLY 1 LOSS. INTERROGATED MTP AND GOT 28V GEAR POWER SUPPLY 1 LOSS LOGGED AND LIKEWISE FOUND RELAYS & RETRACT CONT ROL C/B OF MLG PROX DETECTOR POPPED OUT. FOLLOWED T/S PER TSM 32-30-00 FIG 109 AND RESET SAID C/B, NO POPPING OUT AND U NABLE TO DUPLICATE THIS TIME. PERFORMED NORMAL EXTENSION AND RETRACTION ADJ/TEST USING MLG SAFETY RELAY SIMULATOR TEST SET AND DUPLICATED POPPING OF C/B IN FLIGHT CONFIGURATION. FURTHER T/S FOUND MLG CONTROL MODULE DEFECTIVE. R & R MLG CO NTROL MODULE PER MM32-31-11. PERFORMED OPS TEST PER MM 32-31-00-5, SATISFACTORYAND NO C/B POPPING OUT NOTICED ON BOTH 2 L 7 2 4F RT A35EU 20090106 NE 2009 1 6 HALA2008122000897 2 20081220 A 7230 FAN BLADE BOEING 767 76733A 1385209 NM PWA PW4062 PW4062 NE NR 2 ENGINE DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, NR 2 ENG HAS A NICK ON ONE OF THE N1 FAN BLADES. BLENDED BLADE PER AMM 72-31-02. EDDY CURREN T INSP. NO CRACKS NOTED. DIMENSIONS .093 BY 5/8 INCH IN AREA "D" OF BLADE. 2 L 7 2 4F 4 F RT A1NM E24NE 20090106 EU 2009 1 6 FDEA200812165181 1 20081216 A 2800 UNKNOWN AIRBUS 300 A300F4605R 3930327 EU FUEL SYSTEM UNKNOWN A FDEA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 CE 21 689FE 875 DURING CRUISE, RT OUTER FUEL TANK DROPPED AS LOW AS 7.04 LBS, WHILE LT OUTER TANK REMAINED AT 8.04 LBS & 2 CB'S WITH NO CORRECTION. ARRIVED AT ACFT, FOUND FUEL QTYS ALL NORMAL, L/O AT 8.3, R/O AT 8.3, ECAM AND OVERHEAD TOTALS AGREE WITH TA NKS. PRESSURIZED ALL PUMPS / SYSTEMS, INSPECTED ACFT FOR SIGNS OF LEAKS, NONE FOUND. FQIC "SYS MONITOR" SHOWS 'SOFT' C ODES 331, 431, 022, 502, 631. CLEARED FQIC, TEST GOOD. SYSTEM IS NOW IN "LA" MODE. TRANSFERED FUEL FROM R/O TO INNER S, ACCOMPLISHED MX STEPS FOR MEL 28-42-01-01. RELEASED FOR SERVICE PER MEL/CDL. ALL RT OUTER TANK INDICATIONS INOP EI THER FUEL TO KNOWN QTY OR, AFTER REFUELING VERIFY TANK QTY WITH MAG MEASURING STICKS, & STICK READINGS, ARE RECORDED IN 2 L 7 2 4F RT A35EU 20090106 SO 2009 1 6 FDKA2008123000327 1 20081230 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 FRL FLT 6189 JFK. OVERHEAD EMERGENCY EXIT ROW 12 INOP. MX RESECURED CONNECTOR AT LIGHT ASSY OPS GOOD. 2 L 7 2 4T RT T00011AT 20090106 NM 2009 1 6 K11A2008123172310 1 20080410 A 5210 SKIN BOEING 727 7272H3 138368N NM L1 DOOR DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 723CK 20545 L1 DOOR HAS INTERIOR SKIN DAMAGE. 2 L 7 3 4F RT A3WE 20090106 EU 2009 1 6 FDEA200812155158 1 20081215 A 2841 INDICATION SYS AIRBUS 300 A300F4605R 3930327 EU FUEL QTY MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 668FE 772 DURING CLIMB, THRU APPROX 18K, NOTICED LT OUTER FUEL QTY DECREASING AT APPROX 500-1000 LBS MIN, THIS WAS ON THE ECAM AN D OVHD PANEL. REF QRH UNDER "POSSIBLE FUEL LEAK" PULLED FQI CHAN SUPPLY 1 2 C/B'S. WHEN FUEL INDICATIONS RETURNED LT OU TER RESUMED IT'S STEADY DECREASE. AFTER LANDING (30K UNDER MAX LNG WT) ALL FUEL IND'S RETURNED TO NORMAL (IE FUEL IND IN OUTERS). T/S INFO MTSI 28-40/1374, PER MOCC REQUEST COMPLIED WITH STEP A: DURING BITE CHECK FOUND FAULTS 312 AND 32 2 ON FQI. COMPLIED WITH TSM 28-42-00 FAULT CODE TROUBLESHOOTING PAGE 127, NO DEFECTS FOUND. STEP B: LEFT OUTER TANK CA PACITANCE AND RESISTANCE CHECKS OK PER MM 28-42-00-5. STEP C: VERIFIED WIRING AND PINS FROM CONNECTORS 56VC AND 5073V 2 L 7 2 4F RT A35EU 20090106 NM 2009 1 6 FDEA200812155172 1 20081215 A 5311 70750071C FRAME BOEING 757 75728A 1384976 NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 912FD 24260 MAIN CABIN STA. 1280 STR.11-14L FRAME IS GOUGED. CUT, REMOVED, FABRICATE AND INSTALLED REPAIR PARTS AS PER MAE TRAVELER NR T8/769971 AND T8/769950 IAW SRM 53-00-07 FIG 201, SRM 51-40-05 AND AMM 51-21-00-7. REPAIRED GOUGED FRAME IAW SRM 53 -00-07, REPAIR NR 1 AT BS 1280, STR 11- 14L. THIS IS A MAJOR AND CATEGORY "A" REPAIR. 2 L 7 2 4F RT A2NM 20090106 EU 2009 1 6 FDEA200812165174 1 20081216 A 7830 9059M10P721A FRAME AIRBUS 310 A310203 3930313 EU THRUST REVERSER CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 NR 1 OTBD T/R AFT FRAME INNER SURFACE HAS CHAFED AREAS FROM CONTACT WITH CORE COWLS. REMOVED AFT CLOSE OUT FRAME IAW SR M 51-40-21, PARA 5 AND 6. FABRICATED AND PART MARKED NEW CLOSE OUT FRAME IAW EA 6-7830-123697. ALODINED 7 PRIMED FRAME IAW SRM 51-21-10 AND 51-75-10. INSTALLED FRAME IAW SRM 51-40-21, PG 7 AND PG 90; AND CMM 78-32-02; FIG 702. 2 L 7 2 4F RT A35EU 20090106 EA 2009 1 6 SWIA200820733 1 20081222 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 705SK 10145 FLT 6454 - OVERHEAD EMERGENCY LIGHT IN FRONT OF LAV INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820696 1 20081220 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 975SW 7951 FLT 5902 - OVERHEAD EMERGENCY LIGHT, 4TH BACK, IS BURNED OUT. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820698 1 20081222 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 928SW 7701 FLT 5828 - MOST AFT OVERHEAD EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820646 1 20081214 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 806SK 15070 FLT 4820 - EMERGENCY LIGHT AT RIGHT EXIT ROW INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820682 1 20081217 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 471CA 7655 FLT 2768 - OVERHEAD EMERGENCY LIGHT SECOND FROM BACK OF AIRCRAFT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820683 1 20081219 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT FAILED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 443SW 7638 FLT 4390 - FLOOR EMERGENCY LIGHTING INOP. REPLACED INVERTER AT EMERGENCY BATTERY NR 3. 2 L 7 2 4F RT A21EA 20090106 NM 2009 1 6 K11A2008123172309 1 20080504 A 5313 STRINGER BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 723CK 20545 STRINGER HAS CORROSION. 2 L 7 3 4F RT A3WE 20090106 NM 2009 1 6 K11A2009010172301 1 20080514 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM FUSELAGE CRACKED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 723CK 20545 SHEAR TIE CRACKED. 2 L 7 3 4F RT A3WE 20090106 NM 2009 1 6 K11A2009010272302 1 20080409 A 5313 STRINGER BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 723CK 20545 STRINGER CORROSION. 2 L 7 3 4F RT A3WE 20090105 NM 2009 1 5 C8GA20080045 1 20080824 A 5347 BAC1520792 SEAT TRACK BOEING 727 727223 1384074 NM BS 640-740 LBL 4 ELONGATED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION NOTED THAT THE MAIN CABIN SEAT TRACK HAS ELONGATED SLOTS AT BS. 720B-74 0 LBL 45.0. REMOVED 2 EA SEAT TRACK AT LBL 45 BS. 640-740 DISPLACED SPLICE PER DWS 2902 INSTALLED NEW SEAT TRACK IAW SRM 51-30-2, 53-10-5. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090105 NM 2009 1 5 HALA2008121900894 1 20081219 A 2611 SMOKE DETECTOR BOEING 717 717200 1383700 NM LAVATORY MALFUNCTIONED A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 486HA 55131 LAVATORY SMOKE DETECTOR WARNING LIGHT STAYS ON. FUNCTIONAL TEST OF THE LAVATORY SMOKE DETECTORS PER FIM 26-14-01. NO F AULTS FOUND. OPS CK GOOD OK FOR SERVICE. 2 L 7 2 4F TR A6WE 20090105 NM 2009 1 5 HALA2008122000895 1 20081220 A 2612 S533213016 ELEMENT BOEING 767 767332 1382001 NM FIRE LOOP SHORTED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, APU FIRE LOOP 2 MSG ON EICAS. REPLACED UPPER APU FIRE DETECTOR ELEMENT ASSY PER AMM 26-15-02. OPS CHECK PENDING. APU FIRE DECTECTOR BITE CHECKED OK PER FIM 26-15-00. 2 L 7 2 4F RT A1NM 20090105 EA 2009 1 5 SIMA200835201 1 20081214 A 2150 A/C PACK CNDAIR CL600 CL6002C10 1390015 EA LEFT SMOKE A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 522AE 10147 ON FLIGHT 4034, DURING ENGINE START CREW REPORTED SMOKE IN THE COCKPIT AND CABIN FOLLOWED BY A REALLY STRONG ODOR IN THE COCKPIT FOLLOWED BY A LEFT PACK AUTO FAIL AND DUCT TEMP AT 95C. ISSUED MEL 21-12. 2 L 7 2 4F RT A21EA 20090105 NM 2009 1 5 SWAA087412 1 20081230 A 5330 6562212 SKIN BOEING 737 7373L9 1384470 NM BS 303 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 303, WL 258. REPAIRED SKIN P ER ER. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087413 1 20081230 A 5330 6562212 SKIN BOEING 737 7373L9 1384470 NM BS 304 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, BS 304, WL 258. REPAIRED SKIN P ER ER. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087414 1 20081230 A 5330 6562212 SKIN BOEING 737 7373L9 1384470 NM BS 304 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS 304, WL 235. REPAIRED SKIN P ER ER. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087401 1 20081230 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM BS 867 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087402 1 20081230 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM BS 500C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087403 1 20081230 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 239WN 34714 FWD EMERGENCY LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087419 1 20081230 A 5311 6546540 FRAME BOEING 737 7373L9 1384470 NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND RT FRAME INNER CHORD WEB CRACKED AT BS. 639, WL 209. REPAIRED WEB PER PAE ER. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 ASAA0874118 1 20081214 A 5210 411A2129321 BRACKET BOEING 737 737790 13844CN NM L2 DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 L2 DOOR LOWER DUST SKIRT BRACKET ON AFT END IS CRACKED. R&R L2 DOOR LOWER DUST SKIRT BRACKET IAW SRM 51 40 02. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 ASAA0874119 1 20081217 A 5320 149A81136 BRACKET BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 WATER TANK SUPPORT BRACKET CRACKED AT BS 947.5 LBL 14 WL 155. REMOVED FABRICATED AND INSTALLED NEW WATER TANK SUPPORT. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 ASAA0874117 1 20081216 A 5321 147A5810137 FLOOR PANEL BOEING 737 737790 13844CN NM CABIN DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 FLOOR PANEL AT L2 DOOR SEALED TO STRUCTURE AND DAMAGED UPON REMOVAL. REMOVED FABRICATED NEW FLOOR PANEL INSTALLED. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 ASAA0854122 1 20081227 A 5210 147A61401 HINGE BOEING 737 737890 1384527 NM L2 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 508AS 35691 L 2 DOOR STIFF TO CLOSE LUBED L 2 DOOR HINGES OPS OK. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 ASAA0844116 1 20081213 A 5753 65C2632036 SKIN BOEING 737 737490 1384715 NM MID FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 794AS 28889 RT OB MID FLAP LOWER SURFACE SKIN GOUGED. REMOVED DAMAGE FABBED FILLERS AND DOUBLERS INSTALLED REPAIR IAW EA 13093 AND SRM 57 53 01 FIG 201. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 ASAA0874120 1 20081221 A 5753 115A6260 BRACKET BOEING 737 737790 13844CN NM RT WING BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 RT WING TE IB DEFLECTOR ROLLER FITTING IB PANEL SUPPORT BRACKET BROKEN. R&R RT WING TE IB DEFLECTOR ROLLER FITTING IB PA NEL SUPPORT BRACKET. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087427 1 20081230 A 5315 6546804 FLOORBEAM BOEING 737 7373L9 1384470 NM BS 639 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND RT STUB FLOORBEAM CORRODED AT BS 639, RBL 70, WL 137. REMOVED AND REPLACED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20090106 NM 2009 1 6 HALA2008122600912 1 20081226 A 2421 INDICATION SYS BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE IDG TRIPPED A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, R IDG VALVE STATUS MSG. CHECKED IDG FILTER DPI FOR POPPED CONDITION, CHECKED NORMAL. CHECKED SERVICE OF RT IDG, CHECKED GOOD. PERFORMED FIM 31-41-00, FIG 109, CLEARED EICAS MESSAGE. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20090106 NM 2009 1 6 K11A2008123172307 1 20080408 A 5230 FASTENER BOEING 727 7272H3 138368N NM C3 DOOR LOOSE A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 723CK 20545 C-3 DOOR HAS LOOSE FASTENERS. 2 L 7 3 4F RT A3WE 20090106 NM 2009 1 6 K11A2008123172308 1 20080409 A 5610 SUPPORT FRAME BOEING 727 7272H3 138368N NM COCKPIT WINDOW CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 723CK 20545 COCKPIT SLIDING WINDOW SUPPORT FRAME HAS AREA OF CORROSION. 2 L 7 3 4F RT A3WE 20090106 EA 2009 1 6 MASA2008122900761 1 20081229 A 5730 WINGLET CNDAIR CL600 CL6002C10 1390015 EA LT WING DAMAGED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 503MJ 10058 PERMANENT REPAIR TO LT WINGLET TIP FAIRING DUE TO LIGHTNING STRIKE DAMAGE. 2 L 7 2 4F RT A21EA 20090106 EU 2009 1 6 YENA200812190130 1 20081218 A 2133 2079001AA OUTFLOW VALVE AIRBUS 320 A320232 3930326 EU CABIN PRESSURE FAILED A YENA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 517JB 30568 29190 1327 FLT NR 1729, JFK-SDQ, RETURNED TO JFK, PRESSURIZATION-V/S VARIABLE FROM -1250 TO +1250 FPM IN SYS 1 & SYS 2 AS WELL AS M ANUAL-OUTFLOW VALVE FLUCTUATED IN CLIMB CRUISE AND DESCENT. V/S STABILIZED AFTER LEVELING AT 10,000. R&R OUTFLOW VALVE (10HL). ACCOMPLISHED IAW AMM 21-51-04, OPS CHECK OK, IN MAN & AUTO MODE. 2 L 7 2 4F RT A28NM 20090106 GL 2009 1 6 SIMA200835401 2 20081217 A 7200 ENGINE EMB 135 EMB135LR 3260305 SO ALLSN AE3007 AE3007A 03030 GL NR 1 FIRE A SIMA A UNSCHED LANDING A FLAME/FIRE CL CLIMB 1 SW 21 717AE 145272 ON TAKEOFF CREW REPORTED AIRCRAFT YAWED TO THE RIGHT AND THEN ON THE CLIMB, RIGHT ENGINE ITT WAS FLUXING/SPIKING ANY WHE RE FROM 800 TO 838. BOTH PACKS WERE RUNNING AND ONLY AFTER RETARDING POWER, (N1 65) THE PACKS HAD TO BE RESET A FEW TIM ES AFTER POWER WAS RETARDED BUT WERE NEVER TURNED OFF. WHEN CREW WAS TURNED OVER FROM TOWER TO DEPARTURES THEY WERE TOL D THERE WAS FLAMES COMING OUT OF THE NR 1 ENGINE ON TAKEOFF. CREW DECLARED AND EMERGENCY AND RETURNED SAFELY TO DTW. A IRCRAFT REMOVED FROM SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20090106 CE 2009 1 6 GUUA93832122208A 1 20081222 A 3260 H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE LT MLG DEFECTIVE A GUUA O OTHER O OTHER CR CRUISE 1 SO 29 81538 UE199 DURING FLIGHT, LANDING GEAR HORN WILL NOT SILENCE EVEN THOUGH SILENCE BUTTON IS PUSHED. REPLACED LT LANDING GEAR UPLOCK SWITCH. OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 20090106 NM 2009 1 6 USAA2008123092350 1 20081210 A 5530 D5537131800200 HINGE FITTING AIRBUS A319 A319132 3930340 NM VERTICAL STAB WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL - MAJOR REPAIR - C7 CHECK - NR 6141111, NR 4 RUDDER HINGE FITTING AT VERTICAL STABILIZER STATION 2632 / RIB6 HAS EX CESSIVE PLAY. REPLACED NR 4 RUDDER HINGE FITTING AT VERTICAL STABILIZER STATION 2632 / RIB6 I/A/W A319 AMM 55-36-41. 2 L 7 2 4F RT A28NM 20090106 EU 2009 1 6 USAA2008123092339 1 20081204 A 5320 D53480043202 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C8 CHECK - NR 6138918, CORROSION ON THE R2 DOOR CUT OUT LOWER SILL AT FR 68 - FR 69, S23R. REPAIRE D THE R2 DOOR CUT OUT LOWER SILL AT FR 68 - FR 69, S23R IAW US AIRWAYS EA 132184. 2 L 7 2 4F RT A28NM 20090106 NM 2009 1 6 USAA2008123092340 1 20081212 A 5320 D53470488002 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL - MAJOR REPAIR - C7 CHECK - NR 6142693, CORROSION ON SHEAR PLATE AT FR 54 - FR 55, S38L. REPLACED SHEAR PLATE AT FR 54 - FR 55, S38L IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20090106 NM 2009 1 6 FDEA200812265301 1 20081226 A 5321 2024T3063C FLOOR PANEL BOEING 757 75728A 1384976 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 912FD 24260 MAIN CABIN METAL FLOOR PANEL STA 1681 TO STA 1720 HAS CORRROSION SEVERAL SPOTS. ENTIRE AREA. REMOVED CORROSION ON IAW S RM 51-10-02, FOUND (2) SPOTS OUT OF LIMITS, FABRICATED. (2) DOUBLER REPAIRS FROM P/N2024T3.063C BATCH NR 0001536183 I AW SRM 53-60- 51; ALTERNATIVE 1-REPAIR 2, TREATED, PRIMED AND INSTALLED (2) DOUBLER REPAIRS IAW SRM 51-20-01 AND 51-40-0 2.THIS IS CATEGORY "A" AND MAJOR REPAIR AT STA 1680 TO 1720, LBL55 TO RBL55. 2 L 7 2 4F RT A2NM 20090106 NM 2009 1 6 C8GA20080069 1 20081024 A 5313 652427629 STRINGER BOEING 727 727223 1384074 NM PWA JT8 JT8D NE ZONE 100 CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STRINGER 22L STA, 1183 ATTACH FITTING HAS EXFOLIATION CORROSION. REM OVED AND REPLACED ATTACH FITTING. PN 65-24276-29 IAW SRM 51-30-2. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERV ICE. 2 L 7 3 4F 4 F A3WE E2EA 20090106 NM 2009 1 6 C8GA20080070 1 20081105 A 5313 65564417 STRINGER BOEING 727 727223 1384074 NM PWA JT8 JT8D NE ZONE 100 CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 WHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT STRINGER 29L STA 950C - 1000 IS CORRODED. REMOVED AND REPLACED STR INGER 29L P/N 65-56441-7. INSTALLED STRINGER IAW SB 727-53-0179. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVI CE. 2 L 7 3 4F 4 F A3WE E2EA 20090106 NM 2009 1 6 C8GA20080071 1 20081015 A 5313 BAC14981437075T6 STRINGER BOEING 727 727223 1384074 NM PWA JT8 JT8D NE ZONE 100 CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 WHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT STRINGER 26L STATION 540 - 560 IS CORRODED.CUT OUT DAMAGE AT STA 5 33-550. FABRICATED STRINGER FROM BAC 1498-143 7075T6, 16 INCH, FABRICATED 2 EA SPLICE PLATES FROM BAC 1498-132 7075 T6, 13 INCHES INSTALLED STRINGER IAW SRM 53-10-2 & 53-10-3. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 20090106 EU 2009 1 6 FDEA200812175227 1 20081217 A 3260 140FL01D3Y1 SWITCH AIRBUS 310 A310 EU NLG FAILED A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CE 21 815FD 638 ON APPROACH, BEFORE LANDING CHECK LIST COMPLETE, AT 200' ABOVE THE GROUND WE HAD A "TO LOW GEAR]" ALERT FWD PANEL SHOWE D 3 GREEN, OVERHEAD INITIALLY SHOWED 3 GREEN BUT NOW SHOWED NO NOSE GEAR GREEN. WENT AROUND AND THE ACFT SHOWED 3 GREE N ON BOTH PANELS THROUGH LANDING. ENT BY: 715474 RPT BY: 078544 SHGN 17DEC08 16:30 YVR R IN WORK. REPLACED SWITCH 79GB ON NOSE GEAR TELESCOPIC DRAG STRUT IAW MM 32-00-00-4, OPS CHECKED IAW MM 32-61-00-5. CHECKED GOOD, 3 GREEN ARROWS ON FWD PANEL AND ON OVERHEAD PANEL ARE ON. 2 L 7 2 4F RT A35EU 20090106 NM 2009 1 6 USAA2008123192365 1 20081230 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLSAHLIGHT DISCHARGED A USAA K NONE L NO TEST UK UNKNOWN 1 EA 19 819AW 1395 LOGPAGE: 8367520 - FLT 178 - SFO-LAS- EEL - FLASHLIGHT UNDER FORWARD INBOARD FLIGHT ATTENDANT JUMPSEAT INOPERATIVE. REM OVED AND REPLACED FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20090106 NM 2009 1 6 USAA2009010590011 1 20081211 A 5320 D53471124200 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL - C7 - MAJOR REPAIR - NR 6142383 - CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, -Y1732. REPLACED SHEAR PLATE BETW EEN FR69 TO FR70, -Y1732 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20090106 CE 2009 1 6 2008F00028 1 20081203 A 7110 COWLING BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60 52043 NE ZONE 400 CRACKED E QZ9A K NONE O OTHER IN INSP/MAINT 1 WP 09 300TN FA168 POSTFLIGHT RAMP INSP DISCLOSED THAT EACH ENG COWLING HAD SMALL CRACK FWD OF AND CONNECTING TO OTBD AFT LATCHING MECHANIS M. CRACKS REPAIRED AND ACFT RETUNED TO SERVICE. 2 L 7 2 4T 4 T A24CE E4EA 20090106 EU 2009 1 6 FDEA200812195242 1 20081219 A 5320 Y5382990420000 SUPPORT FITTING AIRBUS 300 A300B4622 3930401 EU SEAT TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 SEAT TRACK SUPPORT CRACKED, LOCATED BETWEEN FR 49 AND FR 50, OTBD OF NR 4 LT GANTRY. FABRICATED SEAT TRACK FITTING SUPP ORT IAW E.A. 6-5321-123539. SEAT TRACK FITTING INSTALLED IAW SRM 51-40-00; PARA 3. 2 L 7 2 4F RT A35EU 20090106 NM 2009 1 6 FDEA200812245282 1 20081224 A 5313 65562392 STRINGER BOEING 727 727233 138408A NM BS 676-686 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 FWD CARGO HAS CORROSION AT STRINGER 28R AND STA 680 ON STRINGER CHANNEL UNDER LEVELING COMPOUND. REMOVED STRINGER SPL ICE IAW SRM 51-30-2. FABRICATED NEW STR SPLICE IAW SRM 53-10-2FIG 9 AND 53-10-3 FIG 1. TREATED AND PRIMED AND INSTALLED NEW SPLICE AT FWD CARGO STRINGER 28R, BS 680 IAW SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 20090106 NM 2009 1 6 DHLA20087451226 1 20081226 A 5720 ANGLE BOEING 727 727224 1384076 NM ZONE 600 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPON VISUALLY INSPECTING THE RT WING A CRACK IN THE FALSE SPAR LOWER CHORD WAS FOUND AT APPROX WBL124.0. THE CRACK IS I N THE RADIUS APPROX 1.5 INCHES IN LENGTH. 2 L 7 3 4F A3WE 20090106 WP 2009 1 6 AALA200810492 1 20081208 A 5311 FRAME DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7542A 49996 FRAME CRACKED, STA 1510 BELOW RT LOWER TAIL CONE LATCH AT 2 EACH ALIGNMENT PINS. INSTALLED REPAIR DOUBLER IAW 53-005083 . 2 L 7 2 4F A6WE 20090106 NM 2009 1 6 C8GA20080072 1 20081016 A 5313 BAC14981417075T6 STRINGER BOEING 727 727223 1384074 NM PWA JT8 JT8D NE ZONE 100 CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STRINGER 28L STA 492 HAD CORROSION. CUT OUT DAMAGE AT STA 492 FABRI CATED NEW ANGLE SUPPORT FROM 7075 T6 18, .5 INCH, FABRICATED STRINGER REPAIR STA. 480 -510 FROM P/N BAC 1498-141 7075 T6 , FABRICATED 2EA SPLICES FROM BAC 1498-132 7075 T6. INSTALLED SUPPORT ANGLE AND REPAIR IAW SRM 53-10-2, 53-10-3. NO OTHE R DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 20090106 CE 2009 1 6 BKE2008F00004 1 20081211 A 3220 TORQUE LINK RAYTHN 390 390 7150030 CE NLG LOOSE E BKEA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 01 88EL RB157 ON THE RUNWAY WHEN POWER WAS ADVANCED AND ACFT +/- 45 KTS. THERE WAS A VIBRATION SENSED IN THE FRONT. EXITED THE RUNWAY AND RETURNED TO FBO TO ASCERTAIN PROBLEM. TIGHTENED TORQUE LINK CENTER BOLT IAW AMM 32-20-02-401. PERFORMED HIGHT SPE ED TAXI, NO DEFECTS NOTED. (K) 1 L 7 2 3F RT A00010WI 20090106 EU 2009 1 6 USAA2009010590012 1 20081219 A 5347 D57130147200 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656AW 1079 SAL - C7 - MAJOR REPAIR - NR 6072800 - CORROSION ON SEAT TRACK BETWEEN FR36 TO FR38, -Y765 AT 4 LOCATIONS. REPAIRED SEA T TRACK BETWEEN FR36 TO FR38, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081229 NM 2008 12 29 SWAA087342 1 20081223 A 5610 5893543139 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 29 610WN 27696 L1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087335 1 20081223 A 3350 101074 SIGN BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT SIGN INOP. RELAMPED SIGN PER MM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 AALA200810516 1 20081218 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM BS 328 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CORROSION ON FLOORBEAM AT STATION 328. FLOORBEAM UPPER CHORD REPLACED PER ESO 6100 DATED 12-16-08. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 AALA200810517 1 20081217 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 FLOORBOARD SUPPORT CRACKED AT STATION 610. INSTALLED A SERVICEABLE FLOOR SUPPORT. 2 L 7 2 4F RT A16WE 20081229 WP 2008 12 29 AALA200810514 1 20081211 A 3350 5016 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT WEAK A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 463AA 49593 EMERGENCY LIGHTING BATTERY PACK TESTED WEAK (AMM 33-60-98-4). INSTALLED A SERVICEABLE BATTERY PACK. 2 L 7 2 4F A6WE 20081229 NM 2008 12 29 AALA200810520 1 20081218 A 5320 WEB BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 AFT CARGO LOWER SCUFF PLATE WEB CORRODED STATION 827. INSTALLED A SERVICEABLE SCUFF PLATE WEB PER ESO 61000 DATED 12-10 -08. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087299 1 20081222 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CRACKED AT BS 484, STR 22R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087301 1 20081222 A 3350 3005931 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081229 WP 2008 12 29 AALA200810537 1 20081208 A 5320 ANGLE DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 CORROSION ON RIGHT CUSP TEE ANGLE STATION 220. INSTALLED A SERVICEABLE TEE ANGLE FROM STATION 180 TO 228 PER SRM 53-05- 00. 2 L 7 2 4F A6WE 20081229 WP 2008 12 29 AALA200810540 1 20081208 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 CRACKS IN INTERCOSTAL AT FASTENER HOLE STATION 1287 TO 1309, AFT CARGO. INSTALLED A SERVICEABLE INTERCOSTAL. 2 L 7 2 4F A6WE 20081229 WP 2008 12 29 AALA200810542 1 20081208 A 5310 STRUCTURE DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 CORROSION ON RIGHT SUBFLOOR STATION 218. REPAIRED PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081229 WP 2008 12 29 AALA200810543 1 20081208 A 5320 PAN DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 CORROSION ON LOWER VERTICAL AND HORIZONTAL PAN LEGS, FORWARD CARGO PAN STATION 370 TO 425. INSTALLED SERVICEABLE DOOR P AN AND SPLICES PER SRM 53-05-00 FIG 44. 2 L 7 2 4F A6WE 20081229 NM 2008 12 29 AALA200820100 1 20081210 A 5340 146N52432 MOUNT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 609AA 45862 27447 CORROSION ON LAVATORY MOUNT LT SIDE OF AFT LAVATORY, REPLACED FITTING IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20081229 NM 2008 12 29 ASAA0844096 1 20081218 A 2130 7638103 PRESSURE SWITCH BOEING 737 7374Q8 138447Q NM E/E BAY DEFECTIVE A ASAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 NM 02 774AS 25107 F/A REPORTED LOUD BANG AT 35000' CABIN ALTITUDE THEN SHOWED A 1000'/MIN CLIMB CABIN WENT FROM 8500' TO 11000' DURING OUR RAPID DESCENT GOT CONTROL AT APPROX 20000' IN MANUAL AC. AFTER LANDING CABIN WAS 500' BELOW SEA LEVEL. INSPECTED THE A PU DUCT SEALS [KEEL BEAM & AFT PRESSURE BULKHEAD] NO LEAKS NOTED. INSPECTED APU CHECK VALVE OPS & LEAK CK OK. PRESSURI ZED AC PER MM 21-00-05 PG. 201 [CONFIDENCE CK] ALL FUNCTIONS NORMAL PRESSURIZED TO 4.0 PSI NORMAL. NO DEFECTS NOTED. P ERFORMED CABIN PRESS LEAK TEST PER MM 05-51-91-702-001 OPS & LEAK CKS NORMAL. R&R CABIN PRESSURE CONTROLLER PRECAUTIONA RY IAW MM 21-31-21-004-003 & MM 21-31-21-404-404. PERFORMED PRESSURIZATION CONTROL SYST TEST IAW MM 21 31 00/201 & MM 21 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 UALA2008111303552 1 20080623 A 5720 STRUCTURE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT A/C BAY DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 DAMAGE TO LWR CHORD IN LT AC BAY ABOVE PLENUM. MAJOR REPAIR ACCOMPLISHED. AFTER HEAT TREAT AND CAD PLATING INSTALLED A NGLES, STRAP AND CHORD SECTION. LOWER CHORD REPAIRED PER UA-EVA-71685. 2 L 7 2 4F 4 F RT A1NM E24NE 20081229 NM 2008 12 29 UALA2008122206937 1 20081220 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY EXIT LIGHT INOP DOOR 5 LEFT FWD SILL LIGHT. RELAMPED EMERGENCY LIGHT, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081229 EU 2008 12 29 UALA2008122206955 1 20081220 A 3350 321431 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 448UA 842 EPSU BATTERY EMERGENCY RIGHT FAULT DISPLAYED AFTER EMERGENCY LIGHT TEST. REPLACED BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081229 NM 2008 12 29 UALA2008122206925 1 20081218 A 2421 520854 CONTROL UNIT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HMG NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 596UA 28749 HMG DOES NOT TEST. REPLACED HYDRAULIC MOTOR GENERATOR CONTROL UNIT. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081229 NM 2008 12 29 UALA2008122306972 1 20081223 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 AFT EXIT LIGHT INOP DOOR 4R. REPLACED FEEDER CABLE. CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081229 NM 2008 12 29 SWAA087306 1 20081222 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 4L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087309 1 20081222 A 5511 6573782 RIB BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND LT HORIZONTAL STABILIZER LOWER RIB CHORD CRACKED AT BS 129. REMOVED AND REPLACED CHOR D PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087310 1 20081222 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 15R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087311 1 20081222 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 627, STR 6R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 AALA200802383A 1 20081009 A 5322 SHEAR TIE BOEING 767 767223 1385123 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AA 22320 AFW - SHEAR TIE ON FORWARD AND AFT SIDE AT STATION 1562 AND BUTTLINE ZERO HAVE CORROSION. REPAIRED PER MRB 767 3322. 2 L 7 2 4F RT A1NM 20081229 NM 2008 12 29 AALA200802384A 1 20081002 A 5320 FLANGE BOEING 767 767223 1385123 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AA 22320 AFW - FORWARD CARGO DOOR CUTOUT OUTER CHORD OUTBOARD FLANGE AT STATION 615 HAD CORROSION. AREA OF DISCREPANCY WAS 5 INC H BY 1 INCH WITH A DEPTH OF .290 INCHES AT DEEPEST SPOT. REPAIRED IN ACCORDANCE WITH MRB 767 3314. 2 L 7 2 4F RT A1NM 20081229 NM 2008 12 29 AALA200802385A 1 20081023 A 3350 LIGHT BOEING 777 777223 1385213 NM ZONE 200 MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 793AN 30255 LHR - EMERGENCY LIGHT MISSING ON FIRST CLASS COAT COMPARTMENT NEAR LEFT NUMBER ONE DOOR. REPLACED EMERGENCY LIGHT. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081229 NM 2008 12 29 AALA200802402A 1 20081025 A 3350 LAMP BOEING 737 737823 13844CB NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 923AN 29524 DFW - OVERHEAD EMERGENCY LIGHT AT SEAT ROW 17ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 17 ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 AALA200802403A 1 20081026 A 3350 GUARD BOEING 757 757223 1384957 NM EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 192AN 32386 DFW - EMERGENCY LIGHT AT SEAT 18D GUARD DAMAGED. REPLACED GUARD FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081229 NM 2008 12 29 AALA200802404A 1 20081026 A 1100 PLACARD BOEING 757 757223 1384957 NM ZONE 200 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 192AN 32386 DFW - EMERGENCY LIGHT LEFT FORWARD OVERWING EXIT MARKER DECAL DAMAGED. REPLACED DECAL. SYSTEM GROUND CHECKED NORMAL OP ERATION. 2 L 7 2 4F RT A2NM 20081229 NM 2008 12 29 AALA200802405A 1 20081026 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 192AN 32386 DFW - EMERGENCY BULL NOSE LIGHTS AT SEAT ROW 16C INOPERATIVE. REPLACED LAMP AT SEAT ROW 16C. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 20081229 NM 2008 12 29 AALA200802406A 1 20081026 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 192AN 32386 DFW - EMERGENCY BULL NOSE LIGHTS AT SEAT ROW 17C INOPERATIVE. REPLACED LAMP AT SEAT ROW 17C. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 20081229 NM 2008 12 29 AALA200802392A 1 20081024 A 2560 P4010021 BATTERY BOEING 757 757223 1384957 NM FLASHLIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 657AM 24615 SFO - AFT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081229 2008 12 29 UALA2008122206927 4 20081219 A 2565 416T22919 LATCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L3 DOOR DEFECTIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 649UA 25286 LEFT OVERWING SLIDE COMPARTMENT DOOR NR 3 LATCH FAILED EDGE MARGIN CHECK. INSTALLED NEW NR 3 LATCH, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081229 2008 12 29 UALA2008122206928 4 20081219 A 2565 416T22918 LATCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L4 DOOR SCORED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 649UA 25286 LEFT OVERWING SLIDE COMPARTMENT DOOR LATCH NR 4 IS SCORED. INSTALLED NEW LATCH, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081229 NM 2008 12 29 ASAA0844090 1 20081218 A 5753 6546434336 SKIN BOEING 737 737490 1384715 NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 794AS 28889 RT IB AFT FLAP IS DENTED ON UPPER SURFACE 1.5" AFT OF FWD SPAR AND 51" IB OF OB END. REPAIRED DENT DAMAGE ON UPPER SURF ACE OF RT IB AFT FLAP 1.5" AFT OF FWD SPAR AND 51" IB OF OB END IAW SRM 51 70 10 REPAIR 4 PG 201. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 ASAA0874063 1 20081212 A 5320 111A11411 VAPOR BARRIER BOEING 737 737790 13844CN NM NLG WW CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 FOUND CRACK IN LT WW FWD VAPOR BARRIER. REPAIRED CRACK IN LT WW FWD VAPOR BARRIER. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 ASAA0874065 1 20081217 A 5320 149A81136 SUPPORT BRACKET BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 WATER TANK SUPPORT BRACKET CRACKED AT BS 947.5 LBL 14. REMOVED, FABRICATED AND INSTALLED NEW WATER TANK SUPPORT. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 ASAA0854084 1 20081220 A 2421 28B5457 GENERATOR BOEING 737 737890 1384527 NM APU UNKNOWN A ASAA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 NM 02 583AS 2291 35681 APU GENERATORS DROPPED OFFLINE WITHOUT WARNING GROUNDED YES. NO CIRCUIT BREAKERS OPEN NO FAULTS IN COMPUTER STARTED APU SWITCHED TO APU POWER LOADED UP SYSTEM NO DEFECTS NOTED. GOOD FOR SERVICE. SEAMC BILL NOTIFIED. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 UALA2008122306979 1 20081223 A 3222 STRUT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NLG LOW A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 833UA 1401 UNABLE TO MOVE LANDING GEAR HANDLE. NLG EXT PROX SENSOR 25GA TGT POS AND 24GA TGT POS WERE FLAGGED ON PFR. ACCOMPLISHE D GENERAL INSP OF NOSE GEAR AND TORQUE LINK ASSY, CHECKS OK. FOUND STRUT INFLATION LOW. ACCOMPLISHED FULL SERVICE OF N LG, NO LEAKS. STRUT LEVEL NOW CORRECT. WILL NEED NLG SWING AND PROX SENSOR GAP CHECK WHEN AIRCRAFT NOSE IS JACKED. LI NK ASSY THAT ATTACHES 24GA AND 25GA PROX SENSOR TARGET LEVER TO THE NLG UPPER TORQUE LINK IS BENT. REMOVED DAMAGED LINK ASSY. NEED TO INSTALL NEW LINK ASSY. REPLACED LINK ASSY. JACKED NOSE GEAR AND RETRACTED AND EXTENDED NOSE GEAR. OPS CHEC K OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081230 NM 2008 12 30 UALA2008122406993 1 20081223 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 501UA 24622 R2 DOOR REQUIRES REPAIR DOUBLER AT UPPER HINGE CUTOUT. PERFORMED HFEC INSPECTION PER NDT MANUAL 6-51-00-19 ON UPPER HIN GE CUTOUT, AND FOUND NO CRACKS NOTED AT THIS TIME AS DOCUMENTED ON NON ROUTINE 25462 BY IN SP QC077. THIS REPAIR WILL B E ACCOMPLISHED AS PREVENTATIVE MAINTENANCE. INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 20081230 NM 2008 12 30 UALA2008122406994 1 20081223 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 501UA 24622 MAJOR REPAIR: L2 DOOR REQUIRES REPAIR DOUBLER AT UPPER HINGE CUTOUT. PERFORMED HFEC PER NDT 6-5 1-00-19 ON UPPER HINGE CUTOUT AND FOUND NO CRACKS NOTED AT THIS TIME AS DOCUMENTED ON NON ROUTINE 25463 BY INSP QC077. THIS REPAIR WILL BE AC COMPLISHED AS A PREVENTATIVE REPAIR. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081230 NM 2008 12 30 UALA2008122206936 1 20081220 A 3397 7945243 POWER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY EXIT LIGHTS INOP SEAT ROWS 45 THRU 54 LT. DOOR 4 RT AFT EXIT SIGN. DOOR 4 LT FWD EXIT SIGN. LOWER WALL EMER GENCY LIGHT ACROSS DOOR 4 LT. DOOR 4 LT LOWER WALL EMERGENCY IN GALLEY AREA. REPLACED POWER CABLE, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081230 NM 2008 12 30 AALA200802412A 1 20081026 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 343AN 33082 DFW - EMERGENCY LIGHT LENS FELL OFF AT SEAT ROW 20. SECURED LENS AT SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATIO N. 2 L 7 2 4F RT A1NM 20081230 EA 2008 12 30 COMA2008122450046 1 20081224 A 7830 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA RIGHT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 451CA 7562 DURING CLIMB RECEIVED A RIGHT THRUST REVERSER UNLOCK MESSAGE, FLIGHT DIVERTED TO IND. DEFERRED THE RIGHT THRUST REVERSE R PER MEL 78-30-01. 2 L 7 2 4F RT A21EA 20081230 EA 2008 12 30 COMA2008122390002 1 20081222 A 5220 DOOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT MALFUNCTIONED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 695CA 15097 LEFT FWD OVERWING EMERGENCY EXIT DOOR WILL NOT CLOSE. RESTOWED AND SECURED LEFT FWD OVERWING EMERGENCY EXIT DOOR. NO F URTHER DEFECTS NOTED, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20081230 NM 2008 12 30 HNAA2008122700363 1 20081224 A 5610 NP15790714 WINDSCREEN DHAV DHC8 DHC8102 2809003 NM COCKPIT CRACKED A HNAA A B UNSCHED LANDING EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 975HA 15994 15994 176 FIRST OFFICES FRONT WINDSCREEN CRACKED, ARCHING AT THE INNER HEATER ELEMENT. REMOVED AND REPLACED FIRST OFFICERS WINDSH IELD REF MM 56-10-11, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 20081230 NM 2008 12 30 HNAA2008122200356 1 20081218 A 3242 21565 BRAKE DHAV DHC8 DHC8102 2809003 NM LT MLG SMOKE A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 EA 07 930HA 4662 4662 126 LEFT MAIN BRAKE ASSEMBLY WET, SMOKES AFTER LANDING. REMOVED AND REPLACED NUMBER ONE BRAKE ASSY IN ACCORDANCE WITH 32-4 2-11, LEAK AND OPS GOOD. 2 H 7 2 4T RT A13NM 20081230 NM 2008 12 30 HNAA2008121000347 1 20081213 A 3350 1317 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 908HA 59652 59652 015 THE 2ND CEILING EMERGENCY LIGHT INOP. RELAMP 2ND CEILING EMERGENCY LIGHT BULB. 2 H 7 2 4T RT A13NM 20081230 SO 2008 12 30 RAIA2008122300002 1 20081218 A 3320 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 829HK 145281 CREW REPORTED THAT 1ST WINDOW WASH LIGHT AT SEAT 1A WAS OUT AND THAT THERE WAS A SMELL OF HOT ELECTRICS. MAINTENANCE DE FERRED THE WINDOW WASH LIGHT AS PER MEL PROCEDURES. 2 L 7 2 4T RT T00011AT 20081230 SO 2008 12 30 RAIA2008122400002 1 20081222 A 3350 LIGHT EMB 145 EMB145EP 3260221 SO COCKPIT OUT OF ADJUST A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 809HK 145187 DURING PRE FLIGHT INSPECTION, THE COCKPIT ENTRY EMERGENCY LIGHT WAS FOUND TO INOPERATIVE. MAINTENANCE ADJUSTED THE LIGH T ASSEMBLY AND PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WITH NO DEFECTS NOTED. 2 L 7 2 4F RT T00011AT 20081230 SO 2008 12 30 RAIA2008122400004 1 20081222 A 2130 UNKNOWN EMB 145 EMB145 3260210 SO CABIN PRESSURE MALFUNCTIONED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 821HK 145068 DURING CRUISE, CREW WAS UNABLE TO CONTROL AIRCRAFT PRESSURIZATION IN AUTO AND/OR MANUAL MODE. MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED AN OPERATIONAL CHECK OF THE AIRCRAFT PRESSURIZATION SYSTEM WITH NO ADDITIONAL DEFECTS NOTED. 2 L 7 2 4F RT T00011AT 20081230 NM 2008 12 30 USAA2008122392305 1 20081217 A 5311 6546532 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - NR 6136275 - CRACK ON FRAME AROUND HOLES FOR SUPPORT BRACKET AT BS480 BETWEEN S8R & S9R. REP AIRED FRAME AROUND HOLES FOR SUPPORT BRACKET AT BS480 BETWEEN S8R & S9R IAW US AIRWAYS TASK CARD M1C53002. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 USAA2008122392308 1 20081216 A 5311 6546550 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - NR 6136278 - CRACK ON FRAME AROUND HOLES FOR SUPPORT BRACKET AT BS 787 BETWEEN S8R & S9R. RE PAIRED FRAME AROUND HOLES FOR SUPPORT BRACKET AT BS 787 BETWEEN S8R & S9R IAW US AIRWAYS TASK CARD M1C53002. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 USAA2008122992330 1 20081127 A 5311 6546558 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - MAJOR REPAIR - C19 CHECK - NR 6136281, CRACKED FRAME AT BS 907, S8R - S9R. REPAIRED FRAME AT BS 907, S8R - S9R IA W TASK CARD M1C53002. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 USAA2008122392302 1 20081208 A 5523 SKIN BOEING 737 7373G7 138447J NM ELEVATOR TAB DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - NR 6135805, 6135806, 6135807, & 6135808 - DELAMINATION ON RIGHT ELEVATOR TRIM TAB SKIN AT NR 1, 2, 3, & 4 HINGE AREA. REPAIRED LEFT ELEVATOR TRIM TAB SKIN AT NR 1, 2, 3, & 4 HINGE AREA IAW B737 SRM 51-70-17-0G. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 USAA2008122392303 1 20081217 A 5311 6558280 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - NR 6136273 - CRACK ON FRAME AROUND HOLES FOR SUPPORT BRACKET AT BS 360 BETWEEN S8L & S9L. RE PAIRED FRAME AROUND HOLES FOR SUPPORT BRACKET AT BS 360 BETWEEN S8L & S9L IAW US AIRWAYS TASK CARD M1C53002. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 USAA2008122392310 1 20081217 A 5311 6546557 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - NR 6136280 - CRACK ON FRAME AROUND HOLES FOR SUPPORT BRACKET AT BS 887 BETWEEN S8L & S9L. RE PAIRED FRAME AROUND HOLES FOR SUPPORT BRACKET AT BS 887 BETWEEN S8L & S9L IAW US AIRWAYS TASK CARD M1C53002. 2 L 7 2 4F RT A16WE 20081230 EU 2008 12 30 USAA2008122392312 1 20081204 A 5540 D5537131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - C8 - MAJOR REPAIR - NR 6138728 - EXCESSIVE PLAY ON RUDDER HINGE ARM NR 1 AT VERTICAL STABILIZER STA 780. REPLACED RUDDER HINGE ARM NR 1 FITTING AT VERTICAL STABILIZER STA 780 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 20081230 NM 2008 12 30 USAA2008122992331 1 20081129 A 5320 65479574 SILL BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - MAJOR REPAIR - C19 CHECK - NR 6130864, CORROSION ON AFT CARGO DOOR CUTOUT LOWER SILL WEB AT BS 767 - BS 787, S25R. REPLACED AFT CARGO DOOR CUTOUT LOWER SILL WEB AT BS 767 - BS 787, S25R IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081230 EU 2008 12 30 USAA2008122492313 1 20081223 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 624AW 39449 6127 55 FLT 614 - PHX-ATL - EEL - EMERGENCY LIGHTS INOP 26-L, 22-L, 15-L, 7-L AND 3-L SEAT ENDS. MAINTENANCE REMOVED AND REPLAC ED THE LEFT OVERWING EMERGENCY LIGHT POWER SUPPLY UNIT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081230 EU 2008 12 30 USAA2008122492315 1 20081223 A 2560 P2070001201 FLASHLIGHT AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A USAA K NONE O OTHER NR NOT REPORTED 1 EA 19 621AW 53 FLT 343 ORD-PHX - EEL - FIRST CLASS CABIN FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FIRST CLASS CABI N FLASHLIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 20081230 NM 2008 12 30 USAA2008122292296 1 20081126 A 5311 65C352436 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - NR 6130873 - CORROSION ON FRAME AT BS 847, BETWEEN S24R TO S26R. REPLACED FRAME AT BS 847, B ETWEEN S24R TO S26R IAW B737 SRM 51-40-02-0G. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 USAA2008122292298 1 20081124 A 5311 6547959 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - NR 6130869 - CORROSION ON FRAME AT AFT CARGO DOOR CUTOUT AT BS 794, BETWEEN S23R TO S27R. RE PLACED FRAME AT AFT CARGO DOOR CUTOUT AT BS 794, BETWEEN S23R TO S27R IAW B737 SRM 51-40-02-0G. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 USAA2008122292299 1 20081202 A 5312 651758350 BULKHEAD BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - NR 6130736 - CRACK ON VERTICAL CHORD WEB AT BS 178, WL 184, RBL 5.7. REPAIRED VERTICAL CHORD WEB AT BS 178, WL 184, RBL 5.7 IAW US AIRWAYS EA 132171. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 R61A20080053 1 20081226 A 2131 CONTROLLER EMB ERJ170 ERJ170100SU 3260403 NM CABIN PRESSURE OUT OF POSITION A R61A G O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 GL 11 816MA 17000037 ON CLIMB CREW REPORTED, RECEIVED A CABIN ALTITUDE HIGH MESSAGE. CREW FOLLOWED QRH PROCEDURES, DEPLOYED OXYGEN MASKS AND RETURNED TO FIELD. MAINTENANCE WAS DISPATCHED TO AIRCRAFT FOUND PRESSURIZATION CONTROLLER IN MANUAL MODE COMPLETED AN OPERATIONAL CHECK OF SYSTEM. ALL CHECKS WERE GOOD RESTOWED MASKS AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F RT A56NM 20081230 NM 2008 12 30 USAA2008122992336 1 20081220 A 5320 143N52641 SHEAR WEB BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 933UW 27199 MCN - MAJOR REPAIR - B1 CHECK - NR 6144141 AND 6141794, CORROSION ON SHEAR WEB AT BS 660 - BS 680, LBL 45. REPLACED SHE AR WEB AT BS 660 - BS 680, LBL 45 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081230 NM 2008 12 30 USAA2008122992337 1 20081204 A 5330 143N31511 SKIN BOEING 757 7572B7 1384964 NM FUSELAGE CANNING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 933UW 27199 MCN - MAJOR REPAIR - B1 CHECK - NR 6144082, FUSELAGE SKIN HAS A 4 INCH DIAMETER AREA THAT OIL CANS AT BS 650 - BS 660, S 5L - S6L. REPAIRED FUSELAGE SKIN AT BS 650 - BS 660, S5L - S6L IAW US AIRWAYS EA 130164. 2 L 7 2 4F RT A2NM 20081230 NM 2008 12 30 USAASB08128 1 20081229 A 3397 SPLICE BOEING 737 7373G7 138447J NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 154AW 23776 PHX - MAINTENANCE REPORTED THE EMERGENCY PATH LIGHT AT SEAT ROW 5 INOPERATIVE. MAINTENANCE REPAIRED A WIRE SPLICE PER S WPM 20-30-12. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 NOCA08908 1 20081210 A 3350 20131A BATTERY BOEING 757 75728A 1384976 NM CABIN DISCHARGED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 EMERGENCY OVERHEAD BIN LIGHT INOP AT SEAT 11 DEF. REPLACED THE R2 BATTERY ASSY AS PER MM 33-51-07. 2 L 7 2 4F RT A2NM 20081230 NM 2008 12 30 NOCA09208 1 20081216 A 2730 251N224131 ARM BOEING 757 75728A 1384976 NM ELEVATOR CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 755NA 30043 ELEVATOR FEEL AND CENTERING UNIT INPUT ARM HAS LEVEL 1 CORROSION. REPAIRED INPUT ARM UNIT AS PER MM 27-31-17-055 AND PE R ESO EAB757-27-005076. 2 L 7 2 4F RT A2NM 20081230 NM 2008 12 30 ASAA0874075 1 20081220 A 5320 111A13089 STRUCTURE BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 VERTICAL STIFFENER CHORD CRACKED. RECEIVED NEW CHORD LOCATED AND DRILLED UP. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 AALA200802477A 1 20081108 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 698AN 26980 DFW - EMERGENCY LIGHT SHROUD AT SEAT 14D IS BROKEN. REPLACED SHROUD AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATIO N. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802479A 1 20081108 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 698AN 26980 DFW - EMERGENCY LIGHT AT FORWARD SEAT 16D IS BROKEN. REPLACED LAMP AT FORWARD SEAT 16D. SYSTEM GROUND CHECKED NORMAL O PERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802450A 1 20081101 A 3350 SIGN BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 680AN 29590 DFW - EMERGENCY EXIT SIGN OVER SEAT 17F FELL OFF. SECURED EMERGENCY EXIT SIGN OVER SEAT 17F. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 WP 2008 12 31 AALA200802454A 1 20081101 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 259AA 49289 LGA - EMERGENCY LIGHTS AT RIGHT OVERWING INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 20 FOR INOPERATIVE EMERGENCY LI GHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081231 NM 2008 12 31 AALA200802461A 1 20081103 A 3397 WIRE BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 186AN 32380 SFO - EMERGENCY LIGHT AT SEAT ROW 21DEF INOPERATIVE. SECURED LOOSE WIRES AT SEAT ROW 21DEF. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A2NM 20081231 SO 2008 12 31 C2XA08CL138 1 20081228 A 3297 CONNECTOR EMB 145 EMB145XR 3260214 SO BRAKE SYSTEM FAULTY A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 15980 145202 CLE FLT 2538 - THE CREW REPORTED A "NO TAKEOFF CONFIG" MESSAGE ON TAKEOFF. ABORTED TAKEOFF AND TAXIED TO THE GATE. MAI NTENANCE INSPECTED AND REPLACED THE EMERGENCY BRAKE PRESSURE SWITCH CONNECTOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 20081231 SO 2008 12 31 C2XA08CL135 1 20081224 A 2131 92185A010200 CONTROLLER EMB 145 EMB145LR 3260212 SO CABIN PRESSURE FAULTY A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 16919 15251 145393 CLE FLIGHT 2150 - THE CREW REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE ON CLIMBOUT. THE AIRCRAFT RETURNED TO CLE AND LAN DED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE DIGITAL CONTROLLER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20081231 NM 2008 12 31 AALA200802561A 1 20081122 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 785AN 30005 MIA - EMERGENCY LIGHT AT SEAT 21C MISSING LAMP. REPLACED LAMP AT SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 AALA200802562A 1 20081122 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 785AN 30005 MIA - EMERGENCY LIGHT AT SEAT 21C MISSING LENS. REPLACED LENS AT SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 AALA200802566A 1 20081122 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 785AN 30005 MIA - EMERGENCY LIGHT AT SEAT 41C MISSING LENS. REPLACED LENS AT SEAT 41C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 AALA200802486A 1 20081108 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 181AN 29591 DFW - EMERGENCY LIGHT AT L4 DOOR INOPERATIVE. SECURED LAMP AT L4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 WP 2008 12 31 AALA200802506A 1 20081111 A 8012 9794104 START VALVE DOUG DC9 DC983 3022083 WP NR 1 ENGINE FAULTED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 963TW 53613 INFLIGHT - RIGHT AFTER TAKEOFF LT ENGINE START VALVE LIGHT STARTED FLICKERING. REDUCED ENGINE TO IDLE AND LIGHT STOPPED FLICKERING. REPLACED NUMBER ONE ENGINE START VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081231 EA 2008 12 31 MASA2008122100751 1 20081221 A 5420 DOOR CNDAIR CL600 CL6002B19 1900309 EA LEFT & RIGHT CHAFED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 75998 7336 LT & RT UPPER AND LOWER CORE COWL DOORS CHAFE DAMAGE AT AFT EDGE. REPAIRED WORN AFT SEAL. 2 L 7 2 4F RT A21EA 20081231 EA 2008 12 31 MASA2008122200753 1 20081222 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 27314 7314 ASH FLT 7108 ORD-CWA. MAIN CABIN DOOR WILL NOT SECURE PROPERLY. MX OPS CHECKED IT NORMAL AND FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 20081231 NM 2008 12 31 NOCA09708 1 20081224 A 3350 1317 LIGHT BOEING 767 76736N 1385152 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 768NA 29898 OVERHEAD EMERGENCY EXIT AISLE ILLUMINATION LIGHTS INOP AT FWD GALLEY LT, 1B, 14B, 29G,12G, 37F, AND AFT GALLEY RT SIDE. RELAMPED AS REQUIRED, OPS CK'D NORMAL PER M/M 33-51-05. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 AALA200802488A 1 20081108 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 181AN 29591 DFW - EMERGENCY LIGHT AT SEAT ROW D INOPERATIVE. SECURED LOOSE CONNECTOR AT SEAT ROW 35D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 DL76L081773 1 20081221 A 2120 20224324 ACTUATOR BOEING 767 767332 1382001 NM RT AC PACK FROZEN A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 173DN 24800 RIGHT PACK WAS PUTTING OUT EXCESSIVE TEMP AIR MAIN CABIN WAS 87. ONLY WAY TO CONTROL CABIN TEMP WAS TO SHUT OFF RIGHT P ACK. TEMP RETURNED TO NORMAL WITH PACK OFF. T/S IAW FIM BITE PERFORMED ON PACK TEMP CONTROL BOX ALL OK. INSP RT PACK FOUND RT RAM AIR EXT DOOR CLOSED. BAD ACTUATOR. REPLACED SAME IAW AMM. NOW OPS OK. RAN PACK ON GND ALL OK. CABIN TEM P IS CONTROLLABLE. A/C OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20081231 EU 2008 12 31 AALA200802530A 1 20081118 A 2780 LIMITER AIRBUS 300 A300B4605R 3930308 EU SLAT JACKSCREW POPPED A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 14068 511 JFK INFLIGHT - CREW REPORTED LEADING EDGE SLATS WOULD NOT DEPLOY. TRAILING EDGE FLAPS WORKED NORMALLY. LANDED JFK WITH OUT INCIDENT. FOUND SLAT JAM FAULT ON BOTH SLAT FLAP CONTROL COMPUTERS. ROUND RIGHT WING NUMBER FIVE JACK SCREW LIMITE R POPPED. REPLACED NUMBER FIVE JACK SCREW. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081231 NM 2008 12 31 AALA200802535A 1 20081120 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AN 25446 DFW - EMERGENCY LIGHT AT SEAT 41H MISSING LENS. REPLACED LENS AT SET 41H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081230 NM 2008 12 30 AALA200802428A 1 20081028 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 680AN 29590 DFW - EMERGENCY LIGHT AT SEAT ROW 10DEF INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 10DEF. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081230 NM 2008 12 30 AALA200802429A 1 20081029 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 NRT - EMERGENCY LIGHT AT FLOOR LEVEL FIRST CLASS CLOSET MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FIRST CLASS CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081230 NM 2008 12 30 AALA200802431A 1 20081029 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 194AA 32388 DFW - EMERGENCY LIGHT AT SEAT ROW 17DEF LAMPS BROKEN. REPLACED LAMPS AT SEAT ROW AFT 17DEF. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A2NM 20081230 NM 2008 12 30 UALA2008122306970 1 20081222 A 3397 58781 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 554UA 26644 G1B GALLEY EMERGENCY LIGHT FEEDER CABLE DAMAGED. REPAIRED G1B EMERGENCY LIGHT FEEDER CABLE AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081230 SO 2008 12 30 RAIA2008121500005 1 20081214 A 5210 MECHANISM EMB 145 EMB145LR 3260212 SO PAX DOOR DIRTY A RAIA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 03 814HK 145046 PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE CLEANED AND LUBED THE PASSENGER OPERATING MECHANISM. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081230 SO 2008 12 30 RAIA2008122900004 1 20081227 A 3350 7287100503 CONTROL PANEL EMB 145 EMB145LR 3260212 SO CABIN FAULTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 838HK 145321 DURING THE PRE FLIGHT INSPECTION, IT WAS FOUND THAT THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REMOVED AND REPLAC E THE FLIGHT ATTENDANT FORWARD CONTROL PANEL IAW AMM PROCEDURES. THE EMERGENCY LIGHTS FUNCTIONED PROPERLY AFTERWARDS. 2 L 7 2 4T RT T00011AT 20081230 SO 2008 12 30 RAIA2008121500004 1 20081214 A 5210 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR DIRTY A RAIA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 03 822HK 145069 PASSENGER DOOR DIFFICULT TO OPERATE. MAINTENANCE CLEANED AND LUBED THE PASSENGER DOOR HANDLE. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081231 NM 2008 12 31 AALA200802478A 1 20081108 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 698AN 26980 DFW - EMERGENCY LIGHT SHROUD AT SEAT 32D IS BROKEN. REPLACED SHROUD AT SEAT 32D. SYSTEM GROUND CHECKED NORMAL OPERATIO N. 2 L 7 2 4F RT A2NM 20081231 SO 2008 12 31 C2XA08IA257 1 20081216 A 7603 CU09625138 RESOLVER EMB 145 EMB145EP 3260221 SO NR 2 THROTTLE INTERMITTENT A C2XA A UNSCHED LANDING S AFFECT SYSTEMS AP APPROACH 1 SW 27 12934 16 145019 FLIGHT 2070 - IAH-BRO - ON APPROACH INTO BRO THE CREW REPORTED THAT THE "E2 TLA FAIL" MESSAGE ILLUMINATED AND THE NR 2 E NGINE REMAINED AT SET THROTTLE UNTIL THE FADEC CIRCUIT BREAKER WAS RESET PER THE COCKPIT QRH. THE AIRCRAFT DIVERTED TO HRL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A FAULTY NR 2 THROTTLE LEVEL THRUST RESOL VER. 2 L 7 2 4F RT T00011AT 20081231 SO 2008 12 31 C2XA08IA264 1 20081219 A 3230 355022002MOD4 ELECTRONIC UNIT EMB 145 EMB145EP 3260221 SO LANDING GEAR FAULTY A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 15926 10662 145005 FLIGHT 4922 - DURING CLIMB THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT . MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT, PERFORMED LANDING EXTENSION AND RETRACTION CHECKS THEN CLEARED THE DISCREPANCY. 2 L 7 2 4F RT T00011AT 20081231 NM 2008 12 31 CALA2008122301164 1 20081223 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24633 27901 FRAME CRACKED AT STATION 400 BETWEEN STRINGER 8 AND 9 RIGHT. REPAIRED FRAME AT STATION 400, STRINGER 8R - 9R, PER EA 53 10-04498. 2 L 7 2 4F RT A16WE 20081231 SO 2008 12 31 C2XA08IA274 1 20081220 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 11539 145536 IAH - FLIGHT 2883 THE CREW REPORTED A PITOT 3 HEAT INOP MESSAGE ON EICAS WITH A BURNT ELECTRICAL SMELL COMING FROM THE F /O'S SEATING AREA. IAH MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED THE PITOT HEAT ALL WITH NO DEFECTS OR O DORS FOUND, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081231 NM 2008 12 31 AALA200802540A 1 20081120 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 781AN 29586 DFW - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP AT SEAT 23C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 WP 2008 12 31 AALA200802545A 1 20081121 A 2560 STRAP DOUG DC9 DC983 3022083 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 967TW 53617 LGA - EMERGENCY FLASHLIGHT AT AFT RIGHT LAVATORY HAS BROKEN SAFETY STRAP. REPLACED STRAP FOR FLASHLIGHT AT AFT RIGHT LA VATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081231 NM 2008 12 31 AALA200802476A 1 20081108 A 3350 LAMP BOEING 737 737823 13844CB NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 902AN 29504 MIA - EMERGENCY LIGHT AT OVERHEAD SEAT 20C INOPERATIVE. REPLACED LAMP AT SEAT 20C. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 DL76G081712 1 20081210 A 4920 380029817 APU BOEING 767 767332 1382001 NM APU BAY MAKING METAL A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 174DZ 37510 29693 P1061 APU AUTO SHUTDOWN WITH FAULT LIGHT ILLUMINATED TWICE. RTB - BITE OF APU CONTROLLER SHOWS HIGH OIL TEMP LAST 2 S/D WITH NO MINI FLAGS. PULLED MCD FOUND METAL. PLUNGER STUCK ON APU AFTER CHIP REMOVAL. NO OIL IN APU. REPLACED APU PER AMM, OPS CHECKS GOOD. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 AALA200802550A 1 20081121 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AA 24593 DFW - EMERGENCY LIGHT SHROUD AT AFT SEAT 22D IS BROKEN. REPLACED SHROUD AT AFT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802551A 1 20081121 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AA 24593 DFW - EMERGENCY LIGHT SHROUD AT AFT SEAT 24D IS BROKEN. REPLACED SHROUD AT AFT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802553A 1 20081121 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AA 24593 DFW - EMERGENCY LIGHT SHROUD AT AFT SEAT 35D IS BROKEN. REPLACED SHROUD AT AFT SEAT 35D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802483A 1 20081108 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 641AA 24599 LGA - EMERGENCY LIGHT AT R2 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT R2 DOOR. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802487A 1 20081108 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 181AN 29591 DFW - EMERGENCY LIGHT LENS AT LEFT OVERWING EXITS IS LOOSE. SECURED LENS AT LEFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802504A 1 20081110 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 647AM 24605 LGA - EMERGENCY LIGHT LENS MISSING AT AFT RIGHT GALLEY. REPLACED LIGHT ASSEMBLY AT AFT RIGHT GALLEY. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802567A 1 20081122 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 653A 24611 MIA - EMERGENCY LIGHT AT R4 DOOR INOPERATIVE. REPLACED LAMP AT R4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 DL738081714 1 20081211 A 3610 1074847 REGULATOR BOEING 737 737832 13844CF NM BLEED AIR SYS DEFECTIVE A DALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 27 3747D 29665 888354 NR 1 ENG BLEED TRIP OFF LIGHT CAME ON AFTER T/O. RESET, NO HELP. FOUND HI STAGE REG CONTROLING HI STAGE VLV TO STAY OPEN, SLIGHTLY CAUSING PRSOV TO TRIP. PERFORMED PNEU SYS HEALTH CHECK EA 12-467086-12 REV B FOUND HS REG BAD NOT SHUTT ING OFF. HIGH STAGE SYS REPLACED HS REG. ALSO FOUND PRSOV REG WIRE SHORTING TO BASE, REPLACED PRS REG HIGH STAGE SYS A ND PRSOV NOW TEST GOOD. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 AALA200802569A 1 20081122 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 637AM 24595 DFW - EMERGENCY LIGHT AT SEAT 12DEF INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT ROW 12DEF. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 DL764081715 1 20081210 A 2597 WIRE HARNESS BOEING 767 767432ER 1385134 NM CABIN BURNED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 845MH 29719 888354 EN ROUTE TO ATL FLT ATTENDANTS NOTICED OR SMELLED SMOKE COMING FROM SEATS 4AB. MAINT OPENED SEAT AND DISCOVERED THAT ON E OF THE HARNESSES TO SDU WAS SHOWING CHAR MARKS. ERA USED TO DISCONNECT THE HARNESS 14-472162-14. REMOVED AND REPLACE D SDU HARNESS / PIN RD-KM 6264-11. HARNESS ASSEMBLY DISC TO SDU ARM CONNECTOR / P/N RD-KM 6263-01 AND DC-SEB / P/N RD- FA 3124-01. REMOVED MCO AND PLACARD. OPS CK GOOD. HARNESS REPLACED PER ERA 14-472162-14. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 DL76L081716 1 20081212 A 7714 CIRCUIT CARD BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 195DN 45589 28452 727774 STATUS MSG R ENG SPEED CARD. PERFORMED EICAS AUTO/ERASE. MSG CLEARED. RERACKED CARD AND PERFORMED RT ENG SPEED CARD T EST CH 1 AND CH 2. RAN ENG AT GATE. ALL OPS CHECK NORMAL NOW. 2 L 7 2 4F 4 F RT A1NM E24NE 20081231 NM 2008 12 31 DLM88081734 1 20081116 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 972DL 53215 A 0.562 INCH CRACK ON FUSELAGE SKIN AT STA Y=175 ON THE WD UPPER CORNER AT THE FWD SERVICE DOOR JAMB. CRACK WAS REMOVED IAW SRM 53-05 FIG 112. NO CRACKS FOUND. INSTALLED REPAIR PARTS IAW SRM 53-05 FIG 112. 2 L 7 2 4F RT A6WE 20081231 NM 2008 12 31 DL76G081740 1 20081215 A 2150 CONTROL VALVE BOEING 767 767332 1382001 NM AC BAY MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 1605 30198 070908 L PACK INOP MSG AND L PACK OFF LIGHT ANNUNCIATED ON A/C PNL BIT CONTLLR NO FAULTS. RESET L PACK, NOW OPERATES NORMAL. OK FOR SERVICE. REPLACED L PACK FLOW CONT VLV, LEAK CHECK NORMAL. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 DL75E081741 1 20081215 A 2997 BMS1360T4C01G22 WIRE BOEING 757 757212 1384951 NM P36 PANEL BROKEN A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 757AT 23127 070908 ON TAXI OUT CREW REPORTED A PTU XFER STATUS MSG. A/C RTB. T/S SYSTEM FOUND WIRE W1260-0407-22 BROKEN ON THE X1 LEG OF RELAY K10337. MSG ONLY SHOWS WITH BOTH ENGINES RUNNING. PERFORMED CHECK OF PTU PER MM TEST OK. REPLACED LT AND RT REL AYS K10398 LEF K10444 RIGHT, NO HELP. CONTINUITY CHECK AT LEFT EDP PRESSURE SWITCH IS GOOD. REPLACED K103338, K10399 A ND K10051 NO HELP. FOUND WIRE W1260-0407-22 BROKEN AT X1 OF K10337. REPAIRED SA PTU CHECKS NORMAL. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 DL757081743 1 20081216 A 5311 FRAME BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 070908 AFT CARGO PIT FRAME STA 1500 AT S25L DENT. REPAIRED IAW SRM 53-00-07 REPAIR NR 5 AT SAA ON NON ROUTINE 81608560001. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 DL757081746 1 20081217 A 5311 FRAME BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 AFT CARGO PIT FRAME STA 1500 AT S25L. REPAIRED AS PER SRM 53-00-07 REPAIR 5 AT SAA ON NON-ROUTINE 81608560001. 2 L 7 2 4F RT A2NM 20081231 NE 2008 12 31 DL76P081751 2 20081217 A 7530 80217010 PRIORITY VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 143DA 25991 724719 RIGHT ENG BLEED VALVE WOULD NOT OPEN. FOUND PRV VALVE LOCKED OUT. RETURNED TO NORMAL AND LOCKED OUT HPSOV. REPLACED V LV PER AMM BUT NOW NEEDS MUSCLE LINE AND ELBOW PAR NR 332T4340-3, ELBOW IS IN MCO POUCH MCO/PLC SOB. 2 L 7 2 4F 4 F RT A1NM E24NE 20081231 GL 2008 12 31 DL764081754 2 20081216 A 7200 CF680C2B8F ENGINE BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 2 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 839MH 23281 29712 704857 NR 2 ENGINE FAILED SCHEDULED BORO. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E23EA 20081231 NM 2008 12 31 DL757081776 1 20081222 A 5320 144N321011 STRAP BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 DURING HMV, CORROSION WAS FOUND ON A REINFORCING STRAP AT THE OVERWING ESCAPE HATCH CUTOUT AT STA 960 ON THE LT SIDE. T HE CORROSION WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED PER BOEING REPAIR INSTRUCTIONS. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 DLM88081718 1 20081211 A 2910 2TL113D CONTROL PANEL DOUG MD88 MD88 3023688 NM COCKPIT ARCED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 908DE 53417 BATTERY CIRCUIT BREAKER POPPED INFLIGHT ELECTRICAL ARCING AND FLASH FROM HYDRAULIC PANEL F/O RECEIVED SHOCK FROM YOKE EL ECTRICAL BURNING SMELL BUT NO SMOKE. FOUND BATTERY CHARGER C/B POPPED, REPLACED C/B, BATTERY CHARGER & BATTERIES, REPLA CED HYD AUX PUMP & TRANSFER PUMP SWITCHES, PERFORMED OPS 5088, ALSO CHK L1 & R1 DOOR DRAIN SYSTEM, FOUND OPS NORMAL. 2 L 7 2 4F RT A6WE 20081231 NM 2008 12 31 DL757081717 1 20081211 A 5210 STRUCTURE BOEING 757 757232 1384965 NM R1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 6701 30187 DURING SHOP VISIT, R1 PASSENGER DOOR WAS FOUND WITH TWO CRACKED FASTENER HOLES. REPAIRED PER ERA 467251-14. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 DL76L081764 1 20081218 A 2751 18195816 TRANSMITTER BOEING 767 767332 1382001 NM TE FLAP OUT OF LIMITS A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 197DN 28454 ON TAXI OUT RECEIVED FLAP T/E SHUTDOWN MSG. COULD NOT CLEAR MSG. FOUND THE NR 4 FLAP POSITION TRANSMITTER OUT LIMITS. REPLACED NR 4 FLAP POS T/E AND INSTALLED A -16 FSEU PER AMM PERFORMED ADJ TEST PER AMM CKS OK. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 SWAA087369 1 20081223 A 3350 417S5500 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 406WN 27894 MID CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087359 1 20081225 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 8L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087397 1 20081229 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 DL76L081724 1 20081213 A 2820 43367310044226 SWITCH BOEING 767 767332 1382001 NM COCKPIT DAMAGED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 199DN 28456 LT AFT FUEL BOOST PUMP SWITCH COVER BECAME DETACHED ON TAXI OUT. REPLACED LT AFT FUEL BOOST PUMP SWITCH PER MM, CHECKS OK. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 SWAA087394 1 20081229 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 355 TO BS 357, STR 16R. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087395 1 20081229 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPV CHECK, FOUND FWD FUSELAGE SKIN CRACKED AT CARGO DOOR CUTOUT, LOWER FWD CORNER. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 20081231 NE 2008 12 31 DL76S081727 2 20081213 A 7200 CF680A2 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 1 FAILED A DALA K NONE Y ENGINE STOPPAGE DE DESCENT 1 SO 27 127DL 54944 24077 580350 ON DESCENT INTO ATL THE LEFT ENGINE ROLLED BACK. PERFORMED IN FLIGHT SHUTDOWN OF ENGINE. INSP INLET AND EXHAUST NTF. CHECKED CHIP DETECTORS NTF. RAN ENG IDLE AND T/O POWER ALL PARAMETERS NORMAL. SUMPED LEFT TANK BEF RUN NTF. REMOVED F UEL PUMP AND MEC. REMOVED FUEL OIL COOLER, REMOVED AND REPLACED NR 1 ENGINE PER TRANS 1T144. 2 L 7 2 4F 4 F RT A1NM E13NE 20081231 2008 12 31 DL76G081777 4 20081222 A 3442 TRANSCEIVER BOEING 767 767332 1382001 NM WEATHER RADAR FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 16065 30199 WXR FAIL DURING CLIMBOUT. UNABLE TO RECOVER. A/C RETURNING TO GRU DUE WX FORECAST IN SA. REPLACED WXR TRANSCEIVER AND INDICATOR. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 SWAA087396 1 20081229 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087348 1 20081225 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 239WN 34714 LT FWD EGRESS LIGHT STRIP LOOSE. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087383 1 20081225 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 450WN 32470 EEPLS LENS BROKEN AT ROW 1. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087384 1 20081228 A 5311 65C25228 FRAME SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND FRAME SPLICE CRACKED AT BS 727C, BETWEEN STR 13L TO STR 14L. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 20090102 EA 2009 1 2 VNAA2008122900012 1 20081225 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAILED A VNAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 05 259PS 10834 7939 CREW REPORTED THE GEAR DISAGREE WARNING MSG ON APPROACH TO CVG. THE CREW CYCLED GEAR HANDLE & RECEIVED MSG AGAIN & THEN IT DISAPPEARED. MAINTENANCE REMOVED & REPLACED NLG PRIORITY VALVE AND GEAR SWING WAS ACCOMPLISHED. CHECKS WERE DONE P ER THE MANUFACTURERS MAINTENANCE MANUAL WITH NO DEFECTS NOTED. ACFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20090102 2009 1 2 CHQA200800259 4 20081226 A 3417 8220372445 ADC CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE E&E BAY FAULTY A CHQA A UNSCHED LANDING S AFFECT SYSTEMS TO TAKEOFF 1 GL 11 667BR 5882 5882 7535 GEE873066 JUST AFTER TAKEOFF THE CREW RECEIVED RED FLAGS FOR THE CAPTAIN'S AIRSPEED, ALTIMETER AND VSI MOMENTARILY. INDICATIONS R ETURNED TO NORMAL SHORTLY. THE FLIGHT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLA CED THE NR 1 ADC IAW 34-13-01. ALL CHECKS NORMAL AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 20090102 EA 2009 1 2 A6WA200840642 1 20081202 A 5320 SCUFF PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 414ZW 7586 SERVICE DOOR LOWER SCUFF PLATE FOUND CORRODED, 3 PLACES APPROX .500 X .500, .026 DEEP. 2 L 7 2 4F RT A21EA 20090102 NM 2009 1 2 ASAA0874104 1 20081227 A 5320 146A83416 THRESHOLD BOEING 737 737790 13844CN NM BS 845 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 AFT CARGO DOOR CUTOUT AFT CORNER THRESHOLD CRACKED. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 ASAA0844109 1 20081228 A 5340 65479588 ATTACH BRACKET BOEING 737 7374Q8 138447Q NM BS 794 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 INTERCOSTAL ATTACH BRACKET BS 794 RBL 6 WL 153 HAS CORROSION. R&R BRACKET. 2 L 7 2 4F RT A16WE 20081230 EA 2008 12 30 COMA2008122850051 1 20081228 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 591SW 7079 PRESSURE FLOOR SKIN IS CRACKED IN TWO PLACES, ONE ON EACH SIDE OF BL 0 AT FS 460.00. REMOVED DAMAGE AND APPLIED A TEMPO RARY REPAIR PER CRJ REO 301R-53-41-103 REV (D). 2 L 7 2 4F RT A21EA 20081230 EA 2008 12 30 COMA2008122850049 1 20081228 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 940CA 7048 DURING CLIMBOUT EN ROUTE BOS-CVG RECEIVED A NOSE GEAR DOOR AND GEAR DISAGREE MESSAGE, FLIGHT RETURNED TO BOS. PERFORMED A LANDING GEAR EXTENSION/RETRACTION CHECK, NO DISCREPANCIES NOTED, NO MESSAGES RECEIVED. 2 L 7 2 4F RT A21EA 20081230 EA 2008 12 30 COMA2008122150044 1 20081221 A 3697 3530358 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA AC BAY FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 934CA 7042 DURING CRUISE FLIGHT RECEIVED AN ANTI-ICE DUCT WARNING MESSAGE, FLIGHT DIVERTED TO LGA. REPLACED THE LEFT PACK DUCT LOO P SENSING CONNECTORS AT A49WK AND A48WK. 2 L 7 2 4F RT A21EA 20081230 2008 12 30 HNAA2008122200359 4 20081217 A 3450 066107804 RECEIVER DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A HNAA O OTHER O OTHER CR CRUISE 1 EA 07 931HA 39149 423 132 NUMBER ONE NAVIGATION RADIO FAILED IN FLIGHT, CONTROL HEAD DISPLAY WENT BLANK AND NAVIGATION FLAG SHOWING. REMOVED AND REPLACED NUMBER 1 NAVIGATION RECEIVER, CHECKED WITH TIC BOX, OPS CK'D GOOD IN ACCORDANCE WITH 34-55-00. 2 H 7 2 4T RT A13NM 20081230 NM 2008 12 30 USAASB08126 1 20081224 A 3350 LIGHT BOEING 737 7373G7 138447J NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 156AW 23778 PHX - MAINTENANCE REPORTED THE EMERGENCY LIGHT, ON THE SIDEWALL AFT OF LEFT GALLEY, INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE GALLEY EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20081230 EU 2008 12 30 USAA2008122492318 1 20081204 A 5315 D5347218920200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - C8 - MAJOR REPAIR - NR 6138920 - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081230 EU 2008 12 30 USAA2008122392300 1 20081218 A 3350 PROXIMITY SWITCH AIRBUS 320 A320214 3930316 EU EMERGENCY EXIT OUT OF ADJUST A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 117UW 1224 PIT - C11 - EEL - NR 6072591 - LEFT FORWARD EMERGENCY EXIT DOES NOT ACTIVATE OVERWING LIGHTS WHEN REMOVED. ADJUSTED PRO X SWITCH 1AWV1 IAW A320 AMM 33-51-15. 2 L 7 2 4F RT A28NM 20081230 NM 2008 12 30 USAA2008122492320 1 20081211 A 5320 D53471124200 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL - C7 - MAJOR REPAIR - NR 6142385 - GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, Y1732. REPLACED SHEAR P LATE BETWEEN FR69 TO FR70, Y1732 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081230 NM 2008 12 30 USAA2008122492321 1 20081214 A 3210 D3215303000800 PIN AIRBUS A319 A319132 3930340 NM RT MLG CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL - C7 - MAJOR REPAIR - NR 6143508 - CORROSION ON REAR PINTLE PIN OF RIGHT MAIN LANDING GEAR. REPLACED REAR PINTLE PI N OF RIGHT MAIN LANDING GEAR IAW US AIRWAYS TASK CARD R4M3211. 2 L 7 2 4F RT A28NM 20081230 NM 2008 12 30 USAA2008122492326 1 20081212 A 5315 D53472196200 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL - C7 - MAJOR REPAIR - NR 6142629 - GALVANIC CORROSION ON CABIN FLOORBEAM BETWEEN FR68 TO FR70, Y165. REPLACED CABIN FLOORBEAM BETWEEN FR68 TO FR70, Y165 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081230 NM 2008 12 30 USAA2008122692327 1 20081224 A 5330 6545774 SKIN BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 PHX - MAJOR REPAIR - B1 CHECK - NR 4516590, CRACKED FUSELAGE SKIN AT BS 727E, S22R. REPAIRED FUSELAGE SKIN AT BS 727E, S22R IAW US AIRWAYS EA 121059. 2 L 7 2 4F RT A16WE 20081230 EU 2008 12 30 MTNA1208001 1 20081211 A 5610 NP1588014 WINDSHIELD AEROSP ATR72 ATR72202 8680940 EU COCKPIT CRACKED A MTNA O OTHER O OTHER CL CLIMB 1 EA 68 811FX 283 DURING CLIMBOUT THE COPILOTS WINDSHIELD DEVELOPED A CRACK. THE PILOT DECLARED AN EMERGENCY AND MADE A SAFE LANDING IN M IA. THE WINDSHIELD WAS REMOVED AND REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 20081230 NM 2008 12 30 R61A20080052 1 20081223 A 2440 1701337D MODULE EMB ERJ170 ERJ170200LR 3260121 NM EXTERNAL POWER BURNED A R61A O OTHER B SMOKE/FUMES/ODORS/SPARKS EX EXTERNAL LOAD 1 GL 11 116HQ 3484 3484 17000183 WHEN A/C WAS AT THE GATE AND PASSENGERS WERE DEPLANING CREW RECEIVED A SMOKE IN CABIN MESSAGE ON EICAS. THE CREW REPORT ED THAT AFTER GROUND POWER WAS APPLIED AND RECIRCULATION FAN WAS TURNED ON, HAD SMOKE IN CABIN. EXTERNAL POWER WAS REMO VED AND ALL SYSTEM WERE SHUTDOWN AND REMAINING 4-7 PASSENGERS WERE RUSHED OUT OF AIRCRAFT. EMERGENCY WAS DECLARED. MAI NTENANCE FOUND EXTERNAL POWER MODULE BURNED AND DEFERRED THE EXTERNAL POWER SYSTEM PER THE MEL AND RETURNED AIRCRAFT TO SERVICE. THE EXTERNAL POWER MODULE WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A56NM 20081230 NM 2008 12 30 R61A20080050 1 20081212 A 3240 142071141 CONTROL MODULE EMB ERJ170 ERJ170200LR 3260121 NM NR 1 BRAKE SYS FAILED A R61A L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 11 104HQ 4952 4952 17000160 CREW REPORTED ON APPROACH, RECEIVED A RT AND LT BRAKE FAULT MESSAGE ON EICAS UPON GEAR EXTENSION. ABORTED APPROACH AND DECLARED AN EMERGENCY. LANDED AIRCRAFT WITHOUT INCIDENT AND TAXIED TO GATE. MAINTENANCE WAS DISPATCHED TO AIRCRAFT, TR OUBLESHOT AND REMOVED AND REPLACED NR 1 BRAKE CONTROL MODULE SYSTEM. OPERATIONAL CHECK GOOD, AIRCRAFT WAS RETURNED TO S ERVICE. 2 L 7 2 4F RT A56NM 20081230 NM 2008 12 30 ASAA0844077 1 20081206 A 5320 654769010 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON RT FLOOR TO SIDEWALL SUPPORT IN AFT CARGO BAY RBL 25 BS 727+4 BS 767 OUT OF LIMITS. REPLACED RT FLOOR TO S IDEWALL SUPPORT PER SRM 53 60 53 REPAIR 5. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 ASAA0844078 1 20081219 A 5320 654583470 STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 E BAY FLOORBEAM TENSION STRAP IS CRACKED BS 344 BL 0 STOPPED DRILLED CRACK AND ACCOMPLISHED REPAIR 4 PER SRM 53 10 51. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 AALA200802557A 1 20081122 A 2840 HG1057LR02 PROCESSOR BOEING 767 767323 1385205 NM FUEL QTY FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 39365 24046 BOS INFLIGHT JFK TO FCO - CREW REPORTED FUEL QUANTITY INDICATIONS WENT BLANK. LANDED BOS WITHOUT INCIDENT. REPLACED FU EL QUANTITY PROCESSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 AALA200802560A 1 20081122 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 785AN 30005 MIA - EMERGENCY LIGHT AT SEAT 18C MISSING LENS. REPLACED LENS AT SEAT 18C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 SO 2008 12 31 C2XA08IA267 1 20081227 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT & CABIN ODOR A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 16149 145753 BTR - FLIGHT 2050 - DURING CLIMB THE CREW REPORTED A SMOKE SMELL IN THE COCKPIT AND CABIN. THE AIRCRAFT DIVERTED TO BTR WHERE IT LANDED WITHOUT INCIDENT. LCH MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED THE ENGINES, PACKS, AND APU ALL WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081231 NM 2008 12 31 AALA200802563A 1 20081122 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 MIA - EMERGENCY LIGHT AT SEAT 37C MISSING LAMP. REPLACED LAMP AT SEAT 37C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 WP 2008 12 31 AALA200802473A 1 20081108 A 4930 FUEL FILTER DOUG DC9 DC983 3022083 WP APU DIRTY A AALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 21 9403W 53139 ORD INFLIGHT - AT TOP OF CLIMB RIGHT AND LEFT INLET FUEL PRESSURE LOW LIGHT ILLUMINATED INTERMITTENTLY. AFTER LEVEL OFF APU SHUT DOWN. NUMBER TWO ENGINE GENERATOR ON PLACARD. APU RESTARTED AT 10,000 FEET. RETURNED TO ORD AND LANDED WITH OUT INCIDENT. REPLACED APU LOW PRESSURE FUEL FILTER AND APU COMBUSTION LINER. ALSO, REPLACED GENERATOR CONTROL UNIT AS A PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081231 WP 2008 12 31 RYNA2008122300047 1 20081223 A 3230 LANDING GEAR DOUG DC9 DC982 3022082 WP NLG & MLG LACK OF LUBE A RYNA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 CE 07 932RD 49233 DURING LANDING NLG FAILED TO EXTEND, MLG INDICATION GREEN, NLG INDICATION LIGHT RED, GEAR WARNING HORN SOUNDED NLG PEDES TAL PIN WAS FLUSH. RECYCLED GEAR HANDLE ON SECOND ATTEMPT ALL GEAR DOWN AND IN LOCKED POSITION. JACKED A/C CYCLED GEAR ALL CHECKS NORMAL. LUBED NLG AND DOORS IAW WITH WC802A-001, ADJUSTED RT FWDV GEAR DOOR FIT REF AMM 32-22-01. CHECKED BYPASS VALVE RIGGING REF AMM 32-31-03M ALL CHECKS NORMAL. CHECKED FOR BINDING IN NLG LINKAGES NO DEFECTS NOTED. CYCLED GEAR APPROX 30 TIMES WITH DOORS DETACHED AND ATTACHED ALL CHECKS NORMAL. 2 L 7 2 4F A6WE 20081231 NM 2008 12 31 AALA200802503A 1 20081110 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 760AN 31477 MIA - SEAT MOUNTED EMERGENCY LIGHT LAMP IS MISSING AT SEAT 22C. REPLACED LAMP AT SEAT 22C. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 AALA200802531A 1 20081119 A 2530 8803010000 OVEN BOEING 757 757223 1384957 NM GALLEY SMOKE A AALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 636AM 24594 INFLIGHT - DURING CLIMB FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL AND SMOKE FROM OVEN IN AFT GALLEY. TURNED OFF OVEN A ND SMOKE STOPPED. PULLED CIRCUITS IN AFT GALLEY AND UTILITY BUSS TURNED OFF. REPLACED NUMBER ONE OVEN IN AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802533A 1 20081120 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 697AN 26977 DFW - EMERGENCY LIGHT AT SEAT ROW 31DEF HAS BROKEN LENS. REPLACED LENS AT SEAT ROW 31DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 WP 2008 12 31 AALA200802534A 1 20081120 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 495AA 49733 LGA - EMERGENCY FLASHLIGHT AT FORWARD CABIN UPPER POSITION HAS BROKEN SAFETY STRAP. REPLACED SAFETY STRAP AT FLASHLIGHT AT FORWARD CABIN UPPER POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081231 NM 2008 12 31 AALA200802537A 1 20081120 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 781AN 29586 DFW - EMERGENCY LIGHT AT SEAT 26G INOPERATIVE. REPLACED LAMP AT SEAT 26G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 AALA200802489A 1 20081108 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 181AN 29591 DFW - EMERGENCY LIGHT BULL NOSE AT SEAT 36DEF INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 36DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 DL76L081775 1 20081221 A 2130 CONTROL PANEL BOEING 767 767332 1382001 NM COCKPIT MALFUNCTIONED A DALA B EMER. DESCENT O OTHER CR CRUISE 1 SO 27 185DN 27961 AT FLT 350 LOST CABIN PRESSURE RECOVERED PRESSURE AT FL 260. DECLARED EMERGENCY FOR THE RAPID DESCENT PROCEEDED TO MXP AT FL200. PERFORM FIM PROCEDURE 21-31-00-101 FIG 103 FOUND FAILURE ON CABIN PRESSURE SELECTOR PANEL. SAME REMOVED REPL ACED AND TESTED AS TO AMM 21-31-01-704-014. ALL TEST IS FINE. PRESSURIZATION TEST AS TO AMM 05-51-24-782-001, PERFORME D NO FAULT, NO LEAKAGE. NO OTHER FAULT FOUND. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 HNAA2008122200358 1 20081218 A 2720 2379003001 REGULATOR DHAV DHC8 DHC8102 2809003 NM ZONE 300 FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 07 930HA 51791 51791 126 RUDDER PRESSURE AND RUDDER FULL PRESSURE CAUTION LIGHT'S ILLUMINATED AFTER TAKEOFF. QUANTITY’S AND PRESSURE WERE NORMAL . RUDDER PRESSURE WENT OUT BELOW 140 KNOTS, RUDDER FULL PRESSURE WENT OUT AT 120 KNOTS. REMOVED AND REPLACED RUDDER DU AL PRESSURE REGULATOR IAW 27-20-38, OPS CHECK GOOD OK FOR SERVICE. 2 H 7 2 4T RT A13NM 20081231 NM 2008 12 31 ASAA0844070 1 20081218 A 5311 65465575004 FRAME BOEING 737 7374Q8 138447Q NM BS 727F ELONGATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 AFT CARGO FRAME HAS 1 EA ELONGATED HOLE BS 727F LBL 22 MARKED. REPLACED BS 727F FRAME PER SRM 51-70-11, 51-30-01, 51-20 -01 & 51-40-02. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 ASAA0844071 1 20081218 A 5311 FRAME BOEING 737 7374Q8 138447Q NM BS 787F DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 AFT CARGO FRAME HAS 1 EA ELONGATED HOLE BS 787F LBL 22 MARKED. REPLACED BS 787F FRAME PER SRM 51-70-11, 51-30-01, 51-20 -01, 51-40-02. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 DL757081765 1 20081218 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 DURING HMV AT SAA, A TOTAL OF SIX DENTS AND TWO GOUGES WERE FOUND IN THE EXTERNAL SKIN BETWEEN STA 600 AND 640 AND S-16L AND S-18L. THREE DENTS AND THE TWO GOUGES WERE FOUND TO BE ACCEPTABLE AFTER BLENDING AND TREATING AND THREE DENTS WERE TRIMMED OUT AND REPAIRED WITH AN EXTERNAL DOUBLER. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 SWAA087351 1 20081225 A 3350 81000 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 259WN 35554 FWD EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087352 1 20081228 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 276WN 32530 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087353 1 20081225 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 338, ABOVE STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087370 1 20081229 A 5754 65C26602 SKIN BOEING 737 7373L9 1384470 NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE O/B END LOWER SURFACE DELAMINATED. REMOVED AND REPLACED S LAT PER SRM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087371 1 20081229 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087372 1 20081229 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, BETWEEN LBL 6 TO RBL 6. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087373 1 20081229 A 5311 6546533 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND FRAME CORRODED AT BS 500, BETWEEN LBL 3 TO RBL 3. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087354 1 20081225 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 350, ABOVE STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087362 1 20081225 A 5230 6547953 DOOR FRAME BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED HC2 CHECK, FOUND AFT CARGO DOOR MAIN FRAME CRACKED AT LOWER AFT STOP FITTING. REMOVED AND REPLACED DOO R PER MM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087343 1 20081223 A 5610 141A481024 WINDOW BOEING 737 7377H4 1384404 NM COCKPIT FAULTY A SWAA D RETURN TO BLOCK A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 247WN 32508 AIR TURNBACK - AT LIFTOFF A SMALL FLAME AND SPARKS FOLLOWED BY A BAD ODOR COMING FROM THE L2 WINDOW HEAT CONNECTION AT T HE WINDOW. REMOVED AND REPLACED WINDOW ASSY PER MM. 2 L 7 2 4F RT A16WE 20090102 EA 2009 1 2 CHQA200800260 1 20081226 A 3350 RPS1B BATTERY CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CABIN DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 478CA 26490 26490 7671 GEE873457 THE EXTERNAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE AT THE PASSENGER AND SERVICE DOOR. THE EMERGENCY BATTERY ASS EMBLY WAS REPLACED IAW AMM 33-51-04 AND THE OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 20090102 NM 2009 1 2 ASAA0844110 1 20081207 A 5320 69434561 STRAP BOEING 737 7374Q8 138447Q NM BS 830-846 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 FOUND CORROSION ON LOWER STRAP BS 830-846 RBL 25. R&R STRAP. 2 L 7 2 4F RT A16WE 20090102 EA 2009 1 2 A6WA200840650 1 20081222 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A A6WA O OTHER J WARNING INDICATION AP APPROACH 1 GL 31 434AW 7322 LOG 193677/1 FLAPS FAIL CAUTION MSG IN FLIGHT. COMPLIED WITH QRH LANDED FLAPS O DEGREES WITH NORMAL BRAKING. 2 L 7 2 4F RT A21EA 20090102 SO 2009 1 2 CHQA200800257 1 20081224 A 3040 SENSOR EMB 145 EMB145LR 3260212 SO WINDOW HEAT MALFUNCTIONED A CHQA O OTHER N FALSE WARNING DE DESCENT 1 GL 11 286SK 145443 CAE311567 IN FLIGHT THE CREW RECEIVED A WINDSHIELD HEAT FAIL MESSAGE WHEN TURNING ON THE WINDSHIELD HEAT ON INITIAL DESCENT AT HIG HER ALTITUDES. MAINTENANCE CHANGED THE HEAT SENSOR LEADS FROM 3 AND 4 TO LEADS 5 AND 6 AND ALL OPERATIONAL CHECKS ARE G OOD. 2 L 7 2 4T RT T00011AT 20090102 NM 2009 1 2 DLM88081729 1 20081112 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 972DL 53215 BLEND OUT WITHOUT ID TAG ON FUSELAGE SKIN BETWEEN STA Y=712 TO 732 AND LONG 24-26RT. BLEND OUT WAS FOUND OUT OF LIMITS IAW SRM 53-04D FIG 38 TABLE A. DAMAGE WAS CUT OUT IAW SRM 53-04 FIG 129. NEW SKIN AND DOUBLER WERE INSTALLED IAW SRM 5 3-04D FIG 126 AND WERE IDENTIFIED IAW PS 900-5-1 NR 04. 2 L 7 2 4F RT A6WE 20090102 NM 2009 1 2 ASAA0854106 1 20081227 A 2160 3989083 VALVE BOEING 737 737890 1384527 NM LT PACK INOPERATIVE A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 579AS 22861 35187 ON RECALL "AIR CONDITIONING" MASTER CAUTION ILLUMINATES "PACK" LIGHT ILLUMINATES. RESETTING MASTER CAUTION CANCELS ALL LIGHTS LT PACK. GROUNDED YES. REPLACED LT PACK ZONE TEMP CONTROL VALVE P/N 398908 3 VERIFIED WITH SEAMC ED ETOPS COMPAT IBLE PART. ALL BIT AND OPS CHECKS C/W PER BMM 21-51-10. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 F3LA2008123000731 1 20081226 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319111 3930336 NM CABIN FAILED A F3LA K NONE O OTHER UK UNKNOWN 1 NM 21 923FR 43 2019 PILOT REPORTED THAT THE EMERGENCY PATH LIGHTING WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED CONNECTOR 7245VC I AW A319 ELECTRICAL STANDARDS PRACTICES MANUAL 20-44-29. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNI T AT FIN 13WL IAW A319 AMM 33-51-38-000-001 AND 33-51-38-400-001. 2 L 7 2 4F RT A28NM 20090102 SO 2009 1 2 FDKA2008122200322 1 20081222 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 FRL FLT 6208 CVG. LT AND RT AFT EXTERNAL LIGHTS OUT. MX REMOVED AND REPLACED NR 4 BATTERY OPS GOOD. 2 L 7 2 4T RT T00011AT 20090102 NM 2009 1 2 ASAA0854107 1 20081225 A 2421 7588429101 OIL FILTER BOEING 737 737890 1384527 NM NR 1 IDG POPPED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 559AS AAAH004855 35178 NR 1 ENG IDG FILTER BUTTON POPPED GROUNDED YES. REPLACED FILTERS AND IDG OIL PER W/C 78424000. RAN NR 1 ENG IDG LEAK/IN D CHKS GOOD. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 SWAA087378 1 20081228 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 428WN 29844 EEPLS TRACK COVER MISSING AT EMERGENCY EXIT ROW. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 SWAA087367 1 20081228 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 45. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 SWAA087368 1 20081228 A 5310 6545855538 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND R2 CUTOUT LOWER CHORD CORRODED AT BS 985. REMOVED AND REPLACED CHORD PER SRM. 2 L 7 2 4F RT A16WE 20090102 EA 2009 1 2 SWIA200820645 1 20081214 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 611SK 10035 EMERGENCY LIGHTS IN CEILING NR 2 AND NR 5 INOP (FLT 4508). RELAMPED EMERGENCY LIGHTS. 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 SWIA200820648 1 20081210 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 980SW 7955 THIRD AFT EMERGENCY LIGHT INOP (FLT 5861). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 SWIA200820672 1 20081108 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 445SW 7651 RIGHT AFT ENGINE MOUNT THRUST FITTING CORRODED (C-CHECK). REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081231 NM 2008 12 31 DL76L081745 1 20081216 A 8011 774860A4 STARTER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 175DN 24803 724691 ON TAXI OUT NR 2 ENG DURING START NO ROTATION. ATTEMPTED MANUAL START - NO HELP. REMOVED AND REPLACED NR 2 ENG STARTER PER M/M. CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081231 EU 2008 12 31 MTNA1208002 1 20081219 A 2611 8930112B50L114 SMOKE DETECTOR AEROSP ATR72 ATR72202 8680940 EU ZONE 200 DEFECTIVE A MTNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 68 810FX 2469 220 ON CLIMBOUT OF MEM, THE NR 2 ZONE SMOKE DETECTOR LIGHT ILLUMINATED. NO SMOKE WAS FOUND. THE PILOT DID A PRECAUTIONARY TURNBACK INTO MEM. THE SMOKE DETECTOR WAS REMOVED AND REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 20081231 NM 2008 12 31 SWAA087349 1 20081225 A 3350 81000 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 243WN 34863 RT AFT EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LENS ASSY PER MM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087360 1 20081225 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 570, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 SWAA087361 1 20081225 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 578, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 DL76G081779 1 20081222 A 4990 SWITCH BOEING 767 767332 1382001 NM APU UNSERVICEABLE A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 1609 30574 APU WON`T START REPOSITION FROM PAD TO GATE 6. T/S PER FIM AUTO SHUTDOWN GEN FILTER ON BITE. REMOVED AND REPLACED GEN DIFF PRESS SWITCH PER AMM. RAN APU, OPS NORMAL. T/S PER FIM AUTO SHUTDOWN GEN FILTER ON BITE. REMOVED AND REPLACED GE N DIFF PRESS SWITCH PER AMM. RAN APU, OPS NORMAL. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 SWAA087385 1 20081228 A 5311 65C22909 FRAME SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND FRAME SPLICE CRACKED AT BS 500C, STR 13L. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 20090102 EA 2009 1 2 CHQA200800261 1 20081226 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 667BR 7535 GEE873066 THE EXTERIOR EMERGENCY LIGHT NEAR THE FORWARD PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. THE LIGHT WAS RELAMPED AND OP ERATIONALLY CHECKED GOOD IAW CRJ200 AMM 33-51-21. 2 L 7 2 4F 4 F RT A21EA E15NE 20090102 SO 2009 1 2 CHQA200800251 1 20081220 A 3260 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL MLG DIRTY A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 269SK 145293 CAE311782 FLIGHT 7794, YYZ TO IAD. AFTER TAKEOFF WHEN THE LANDING GEAR WAS SELECTED TO UP THE FLIGHT CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS AND THE LANDING GEAR WOULD NOT RETRACT. THE QRH WAS FOLLOWED AND THE AIRCRAFT RETURNE D TO YYZ AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND INSPECTED ALL OF THE MAIN LANDING GEAR PROX SWITCHES, RES ET POWER AND THE SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20090102 SO 2009 1 2 CHQA200800262 1 20081227 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO CARGO BAY MALFUNCTIONED A CHQA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 278SK 20017 20017 145370 CAE311143 DURING TAXI THE CREW RECEIVED A BAGGAGE COMPARTMENT SMOKE INDICATION. THE CREW DISCHARGED THE FIRE EXTINGUISHERS FOR TH E BAGGAGE COMPARTMENT AND RETURNED TO THE GATE WITHOUT INCIDENT. THE SYSTEMS AND THE BAGGAGE COMPARTMENT WERE THEN DEFE RRED. MAINTENANCE LATER REMOVED AND REPLACED THE SMOKE DETECTORS AND THE FIRE BOTTLES. THIS ACTION CLEARED THE MEL AND ALL SYSTEMS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20090102 NE 2009 1 2 ASAA0854074 2 20081217 A 7261 ENGINE BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 1 OIL CONSUMPTION A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 577AS 6951 35186 894540 NR 1 ENGINE OIL CONSUMPTION OVER THE LIMIT ACFT RESTRICTED FROM ETOPS SERVICE UNTIL OIL CONSUMPTION IS LOWER THAN THE LI MIT GROUNDED YES. ACCOMPLISHED ETOPS INSPECTION PER AMM 71-71-00-21-999 & NO LEAKS NOTED ALSO ACCOMPLISHED OIL DRAIN & V ENTS LEAK INSPECTION PER AMM 71-00-00-700-823 F00 NO LEAKS NOTED AFTER ENGINE RUN FOUND OIL TANK OVERSERVICED BY APPROX 1.5 QTS DRAINED TO FULL LIMIT. OVERSERVICING APPEARS TO BE THE CAUSE OF HIGH OIL CONSUMPTION DATA ACFT RESTRICTED FROM ETOPS SERVICE UNTIL OIL CONSUMPTION IS BELOW THE LIMITS. STATED NR 1 ENG. OIL CONSUMPTION LOWERED TO 0.14. A/C NR 1 ENG . CLEARED FOR ETOPS SERVICE. DEFERRAL HAS BEEN REMOVED. 2 L 7 2 4F 4 F RT A16WE E00055EN 20090102 EA 2009 1 2 A6WA200840622 1 20081201 A 2751 855D1009 SENSOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION LD LANDING 1 GL 31 406AW 19195 7402 FLAP FAIL AT ZERO DEGREES IB. PERFORMED ZERO FLAP LANDING. BRAKE TEMPS 3,2,1,2. R&R BPSU. BPSU OPS AND RIG CHECK GOO D AT THIS TIME. 2 L 7 2 4F RT A21EA 20090102 NM 2009 1 2 ASAA0844089 1 20081222 A 5754 65C26601359 SKIN BOEING 737 7374Q8 138447Q NM NR 1 SLAT CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 NR 1 SLAT LWR SKIN CRACKED I/B AUX TRACK AND 4 EA FASTENER HOLES. REPAIRED USING DOUBLER SPLICE PLATE AND FILLER PER SR M 57-43-01 FIG 201 2 L 7 2 4F RT A16WE 20090102 NE 2009 1 2 ASAA0854085 2 20081219 A 7261 ENGINE BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 2 OIL CONSUMPTION A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 577AS 42 35186 896771 PER SEAMC NR 2 ENGINE OIL CONSUMPTION OVER THE LIMIT. ACFT RESTRICTED FROM ETOPS SERVICE UNTIL OIL CONSUMPTION IS LOWER THAN LIMIT. GROUNDED YES. PER SEAMC BILL AFTER OIL SERVICING NR 2 ENG OIL CONSUMPTION NOW WITHIN LIMITS FOR ETOPS CON SUMPTION 0.19 THIS REMOVES ETOPS RESTRICTION. 2 L 7 2 4F 4 F RT A16WE E00055EN 20090102 EA 2009 1 2 CHQA200800256 1 20081224 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CABIN & COCKPIT SMOKE A CHQA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 GL 11 645BR 7383 GEE872681 IN FLIGHT THE CREW REPORTED A LAVATORY SMOKE CAUTION MESSAGE. THEN REPORTED LIGHT SMOKE IN THE CABIN AND SMOKE ODOR COM ING FROM THE VENTS IN THE COCKPIT. THE FLIGHT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED ENGINE RUNS, RAN THE PACKS AND NOTED NO DEFECTS. MAINTENANCE IS UNABLE TO DUPLICATE THE CONDITION. ALL SYSTEMS CHECK GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 20090102 SO 2009 1 2 CHQA200800258 1 20081225 A 3260 8005701 TARGET EMB 135 EMB135KL 3260302 SO LANDING GEAR OUT OF ADJUST A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 374SK 145544 CAE311207 JUST AFTER TAKEOFF THE CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE. THE FLIGHT RETURNED TO THE FIELD WITHOUT I NCIDENT. MAINTENANCE FOUND THE LT AFT PROXIMITY SWITCH TARGET OUT OF ADJUSTMENT. PROCEEDED TO REPLACE THE SWITCH AND C ORRECT THE ADJUSTMENT. ALL OPERATIONAL CHECKS ARE GOOD AT THIS TIME. 2 L 7 2 4F RT T00011AT 20090102 SO 2009 1 2 FDKA2008122600325 1 20081226 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FRL FLT 6207 ROC-JFK. ROW 12A EMERGENCY EXIT LIGHT INOP. DE-POWERED AND RE-POWERED AIRCRAFT OPS CK NORMAL. 2 L 7 2 4T RT T00011AT 20090102 SO 2009 1 2 FDKA2008122900326 1 20081229 A 5210 DOOR EMB 145 EMB145LR 3260212 SO PAX DOOR DIRTY A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 851MJ 145572 FRL FLT 6259 CVG. MAIN CABIN DOOR HARD TO OPEN FROM THE INSIDE. MX CLEANED AND LUBED OPS GOOD. 2 L 7 2 4T RT T00011AT 20090102 NM 2009 1 2 SWAA087379 1 20081223 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 483WN 32472 EEPLS COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 SWAA087386 1 20081224 A 5330 6552988 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20090102 EA 2009 1 2 SWIA200820695 1 20081219 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 960SW 7853 RIGHT OVERWING CENTER EMERGENCY EXIT LIGHT INOP (FLT 6735). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 SWIA200820670 1 20081118 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 923SW LOWER FLOORBEAM ANGLE CRACKED AT LBL 9 FS 280(C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 SWIA200820675 1 20081108 A 5312 FITTING CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 445SW 7651 AFT PRESSURE BULKHEAD FORWARD FACET CRACKED AT LINTEL FITTING (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090102 NM 2009 1 2 ASAA0874102 1 20081227 A 5320 143A83314 SCUFF PLATE BOEING 737 737790 13844CN NM BS 495 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 FWD CARGO DOOR CUTOUT AFT CORNER THRESHOLD CRACKED. REPAIRED PER ASA EA 5320 01456. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 ASAA0874112 1 20081211 A 5315 147A55048 FLOORBEAM BOEING 737 737790 13844CN NM BS 947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION ON FLOORBEAM BS 947 BL 0 WL 208. REPAIRED PER EA 08-3916 & SRM 53-70-57 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 ASAA0844097 1 20081223 A 5311 654795920 FAILSAFE BOEING 737 7374Q8 138447Q NM BS 794 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON FAILSAFE STRAP. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 ASAA0844099 1 20081223 A 5311 654795978 FRAME BOEING 737 7374Q8 138447Q NM BS 794 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON FRAME BS 794. 2 L 7 2 4F RT A16WE 20090102 NM 2009 1 2 ASAA0844100 1 20081223 A 5311 65C312403 DOUBLER BOEING 737 7374Q8 138447Q NM BS 794 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON INTERNAL DOUBLER ON FRAME BS 794 RBL 30 WL 160. 2 L 7 2 4F RT A16WE 20090102 EA 2009 1 2 VNAA2008122900013 1 20081225 A 3610 20035008067 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA BLEED AIR SYS FAILED A VNAA K NONE J WARNING INDICATION UK UNKNOWN 1 GL 05 229PS 11499 7998 CREW REPORTED IN TRI WING ANTI ICE SYS INOP, RT WING RED WITH WING A/I SELECTED OFF. MAINTENANCE REMOVED AND REPLACED T HE NR 2 BLEED AIR LEAK CONTROL UNIT ALONG WITH THERMAL SWITCHES WS 51, WS 73, WS 140, 149, AND 250. NO OTHER DEFECTS WE RE NOTED AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20090102 WP 2009 1 2 ASMF 20081204 1 20081221 A 2910 7936907553 LINE DOUG DC8 DC871 302199A WP HYDRAULIC SYS LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 754RA 49641 DURING TRANSIT CHECK, A HYD LEAK ON THE LT WHEEL WELL LANDING GEAR WAS DETECTED. MX REPLACED AND TESTED THE HYDRAULIC LI NE IAW AMM 20-50-00, ALL CORRECT. 2 L 7 4 4F 4A25 20090102 EU 2009 1 2 ANCF200800031 1 20081222 A 2910 AS25361910 RING AIRBUS 330 A330243 3930330 EU HYD SYSTEM CUT W ANCF O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 23 967CG 147 147 967 PILOT REPORT: HYD SYS LEAK DURING CRUISE AT FL 390 AFTER 1 HR AND 30 MIN FLIGHT TIME. IN RT ENGINE: ON DUMPER HYD PULS ATION (GREEN SYSTEM) THE SEAL WAS FOUND BROKEN PROCEDURES IAW TSM 29-11-00-810-820 WERE PERFORMED WITH ELEC PUMPS. IAW A MM 29-11-54-400-802 THE GREEN ENG MOUNTED HYD PULSATION DUMPER ON RT ENG WAS REPLACED ENGINE RUN UP IAW 71-00-00-860-810 (AMM) IS OK. 2 L 7 2 4F RT A46NM 20090102 EA 2009 1 2 ASOA200801717 1 20081216 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 923EV 7826 LT FS 484 FLOOR SUPPORT INTERCOSTAL CRACKED .1" LONG AT LBL 36. THE REPAIR ANGLE DESCRIBED IN REO 601R-53-41-059 STEP 5 WAS FABRICATED USING PRE-MANUFACTURED ANGLE P/N 56144A14, THEREFORE THERE IS NO NEED TO HEAT TREAT OF NDT. COMPLETED R EPAIR AT LT FS 484 FLOOR SUPPORT BRACKET IAW BOMBARDIER REO 601R-53-41-059. WORK PERFORMED IAW ASA EC/TC 601R-53-41-059 . 2 L 7 2 4F RT A21EA 20090105 NM 2009 1 5 DU4R2008272 1 20081212 A 5330 SKIN BOEING 757 75723APF 1384966 NM ZONE 600 DENTED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 868AN 24868 DURING SCHEDULED INSPECTION, FOUND DENT IN FWD LOWER FUSELAGE BELOW MAIN CARGO DOOR THRESHOLD SCUFF PLATE AT BS 522. 2 L 7 2 4F RT A2NM 20090105 EA 2009 1 5 ASOA200801721 1 20081223 A 4920 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY MALFUNCTIONED A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 906EV 7642 AFTER STARTING APU ON SHORT FINAL FLIGHT CREW NOTICED AND DETECTED STRONG ODOR OF GASOLINE, FLIGHT ATTENDANT CALLED AND SAID SHE THOUGHT SHE SMELLED THE ODOR OF SOMETHING BURNING...FLT 5059 DEL 36 MINS / ( AUXILIARY POWER UNIT APU -INTAKE DOOR DEACTIVATED CLOSED / ) 2 L 7 2 4F RT A21EA 20090105 NM 2009 1 5 C8GA20080056 1 20080820 A 5753 SKIN BOEING 727 727223 1384074 NM TE FLAP DENTED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE RIGHT WING IB AFT FLAP HAS 1 LARGE DENT NEAR CENT ER ON BOTTOM SIDE. REMOVED DAMAGED AREA, FABRICATED CORE. FABRICATED DOUBLER. INSTALLED REPAIR HOT BONDED & SEALED CORE AND DOUBLER. IAW SRM 51-40-20. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090105 NM 2009 1 5 C8GA20080064 1 20081105 A 5313 STRINGER BOEING 727 727223 1384074 NM ZONE 100 CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT STR. 27R LOCATED AT BS. 1010-1030 HAD EXFOLIATED CORR OSION. REMOVED CORROSION, CORROSION AFTER CLEAN UP FOUND TO BE BEYOND LIMITS. FABRICATED DOUBLER. INSTALLED REPAIR AT BS 950E-1010 PER EA EAAG52-2. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090105 NM 2009 1 5 C8GA20080065 1 20081219 A 2612 FIRE LOOP BOEING 727 727223 1384074 NM APU BAY SHORTED A C8GA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING DE DESCENT 1 SO 29 708AA 22465 FLT 716. ON DECENT THE APU FIRE LIGHT ILLUMINATED AND THE MASTER FIRE BELL SOUNDED. THE APPROPRIATE CHECKLIST ACCOMPLISH ED. THE APU FIRE BOTTLE WAS DISCHARGED. EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPEC TION REVEALED THAT THE APU FIRE LOOP SYSTEM WAS SHORTED. FURTHER TROUBLESHOOTING FOUND MINOR SURFACE CORROSION ON DIODE R421 CONNECTOR, CLEANED CONNECTOR, SYSTEM OPS CHECK GOOD. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090105 NM 2009 1 5 C8GA20080047 1 20080823 A 5347 40456 SEAT TRACK BOEING 727 727223 1384074 NM ZONE 200 CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION NOTED THAT THE MAIN CABIN SEAT TRACK HAS 3 EA AREAS OF CORROSION / GOUG E AT BS. 590-720 RBL 0.5. REMOVED SEAT TRACK AT RBL 0.5 BS 590-720, FABRICATED AND INSTALLED SEAT TRACK PER DWG AE727-2- 063, NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090105 NM 2009 1 5 C8GA20080048 1 20080823 A 5347 40456 SEAT TRACK BOEING 727 727223 1384074 NM ZONE 200 CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION NOTED THAT THE MAIN CABIN SEAT TRACK CORRODED AT BS. 860 RBL 0.5. REMOV ED SEAT TRACK AT RBL 0.5 BS 860, FABRICATED AND INSTALLED SEAT TRACK PER DWG. AE727-2-063 NO OTHER DEFECTS NOTED. AIRCRA FT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090105 NM 2009 1 5 C8GA20080061 1 20081013 A 5347 BAC1520841 SEAT TRACK BOEING 727 727223 1384074 NM ZONE 200 CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE MAIN CABIN SEAT TRACK LOCATED AT BS. 760-850, LB L 45.5 HAD CORROSION. REMOVED SEAT TRACK FROM STATION 760-850, FABRICATED NEW SEAT TRACK, INSTALLED NEW SEAT TRACK IAW S RM 53-10-2, 53-10-5 & 51-10-2. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090105 NM 2009 1 5 C8GA20080049 1 20080823 A 5347 40456 SEAT TRACK BOEING 727 727223 1384074 NM ZONE 200 GOUGED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION THE SEAT TRACK LOCATED AT BS. 760-850 RBL .5 HAD SEVERAL GOUGES. DAMAG ED SEAT TRACK WAS REMOVED AND NEW SEAT TRACK WAS FABRICATED. INSTALLED SEAT TRACK ALL WORK ACCOMPLISHED IAW DWG AEI 727 -2-063. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090102 NM 2009 1 2 DLM88081731 1 20081127 A 5310 BEAM DOUG MD88 MD88 3023688 NM CARGO BAY DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 972DL 53215 DURING BLEND OUT, FOUND ELONGATED HOLES ON C2 DOOR JAMB BEAM. ELONGATED HOLE WERE DRILLED UP IAW SRM 51-10-4. BUSHINGS WERE FABRICATED IAW ERA 471657-14 REV ORIG. BUSHINGS WERE INSTALLED IAW ERA 471657-14 REV ORIG. REPAIR WAS IDENTIFIED IAW PS 900-5-1 NR 4. 2 L 7 2 4F RT A6WE 20090102 SO 2009 1 2 FDKA2008122200321 1 20081222 A 3350 20191A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 847MJ 145517 FRL FLT 6172 IAD. LT AND RT EXTERNAL EMERGENCY LIGHTS OUT. MX REMOVED AND REPLACED BATTERY AND BATTERY CHARGER NR 4. 2 L 7 2 4T RT T00011AT 20090102 NM 2009 1 2 ASAA0854108 1 20081225 A 4920 MS280341 SENSOR BOEING 737 737890 1384527 NM APU INLET FAULTED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 565AS P7343 35181 APU FAULT LIGHT ILLUMINATED. GROUNDED YES. VERIFIED DISCREPANCY CURRENT STATUS SHOWS FAULT CODE 49 61223.FOLLOWED FIM 49-60 TASK 812 R&R INLET TEMP SENSOR GROUND VERIFICATION TEST PASSED REF FIM 49-60 TASK 801. 2 L 7 2 4F RT A16WE 20090102 EA 2009 1 2 VNAA2008121900009 1 20081216 A 3397 59465 PIN CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A VNAA K NONE O OTHER UK UNKNOWN 1 GL 05 248PS 7925 CREW IN GSP REPORTED THE AFT 3RD OF THE FLOOR EMERGENCY LIGHTS WAS INOP. MAINTENANCE INSPECTED AND FOUND BROKEN PINS ON CABLE CONNECTOR P40LY. MAINTENANCE REMOVED AND REPLACED THE CABLE AND PERFORMED CHECKS IN ACCORDANCE WITH THE MAINTENA NCE MANUAL. NO OTHER DEFECTS WERE NOTED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 ASOA200801720 1 20081222 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE O OTHER AP APPROACH 1 SO 27 930EV 8014 FLAP FAIL AT 20 DEGREES ON APPROACH. EMERGENCY DECLARED. FLT 5589X2,5528X2 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 ASOA200801714 1 20081216 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 923EV 7826 LT FS 621-625 INTERCOSTAL ANGLE CRACKED IN AFT EQUIP BAY. REMOVED ANGLE, TRANSFERED HOLES ONTO NEW ANGLE. INSTALLED AN GLE ON A/C IAW CRJ 200 SRM 51-40-11 AND 51-42-06. 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 ASOA200801715 1 20081216 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 923EV 7826 RT FS 621-625 INTERCOSTAL ANGLE CRACKED IN AFT EQUIP BAY. REMOVED ANGLE, LOCATED, AND TRANSFERED HOLES ONTO NEW PART. INSTALLED NEW ANGLE ON A/C IAW CRJ 200 SRM 51-42-06 AND 51-40-11. 2 L 7 2 4F RT A21EA 20090105 NM 2009 1 5 C8GA20080059 1 20080815 A 5322 SHEAR TIE BOEING 727 727223 1384074 NM ZONE 100 CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE AFT CARGO COMPARTMENT SHEAR TIE LOCATED AT BS 985 STR 30-29R CORRODED. FRAME CORROSION FOUND TO BE OUT OF LIMITS, REMOVED DAMAGED SECTION. FABRICATED FRAME. FABRICATED A NGLE. INSTALLED REPAIR PARTS IAW SRM 53-10-2, 51-40-3, 51-10-2. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE . 2 L 7 3 4F A3WE 20090105 EA 2009 1 5 ASOA200801726 1 20081226 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 EXIT SIGN MISSING BY MAIN CABIN DOOR. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200801727 1 20081226 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 920EV 7810 SERVICE DOOR CANNOT BE OPENED FROM OUTSIDE, HANDLE WILL NOT POP OUT 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200801706 1 20081202 A 5210 DOUBLER CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 PAX DOOR INNER FRAME DOUBLER (PN 600-31922-4) AT FS 338.90 CRACKED (INBD OF 318 FRAME, ACCESS PNL 832AR) 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200801709 1 20081213 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 355CA 10067 PAX DOOR LOWER EMERGENCY EXIT LIGHT HAS SEVERAL BULBS BURNED OUT 2 L 7 2 4F RT A21EA 20090105 NM 2009 1 5 DXTA2008122303432 1 20081222 A 3260 LIGHT RAYTHN 400 400ARAYTHEON NM GEAR HANDLE MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 141QS RK498 AFTER TAKEOFF RAISED LANDING GEAR THE RED LIGHT ON GEAR HANDLE STAYED ON. 2 H 7 2 4F RT A16SW 20090105 NM 2009 1 5 DXTA2008122603439 1 20081225 A 3260 INDICATOR GULSTM 200 200 4500308 NM MLG MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 720QS 085 UPON GEAR RETRACTION LEFT MAIN GEAR INDICATION WAS AMBER CROSS HATCHED THEN RED CROSS HATCHED AND STAYED THAT WAY. 2 L 7 2 4F RT A53NM 20090105 CE 2009 1 5 DXTA2008122603440 1 20081225 A 3260 INDICATOR CESSNA 750 750 2076810 CE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 983QS 7500083 THE LANDING GEAR TOOK ABOUT 1 MIN TO FULLY RETRACT. THE RED UNLOCK LIGHT REMAINED ILLUMINATED. 2 L 7 2 4J RT T00007WI 20090105 NM 2009 1 5 DXTA2008122603441 1 20081225 A 5270 WARNING MESSAGE GULSTM 200 200 4500308 NM PAX DOOR ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 722QS 093 CABIN DOOR EICAS MSG AFTER TAKE-OFF. 2 L 7 2 4F RT A53NM 20090105 CE 2009 1 5 DXTA2008122303425 1 20081221 A 3246 TIRE CESSNA 680 680CE 2076811 CE MLG FAILED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 315QS 6800220 BOTH RIGHT MAIN TIRES BLEW ON LANDING. LEFT INBOARD MAIN TIRE FLAT. LEFT OUTBOARD MAIN TIRE FLAT. RIGHT MAIN GEAR DOOR D AMAGED ON LANDING. 2 L 7 2 4F RC T00012WI 20090105 CE 2009 1 5 DXTA200812230342A 1 20081221 A 3246 TIRE CESSNA 680 680CE 2076811 CE MLG FAILED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 346QS 6800013 ALL 4 MAIN TIRES BLOWN UPON LANDING DUE TO FROZEN BRAKES. 2 L 7 2 4F RC T00012WI 20090105 NM 2009 1 5 DXTA2008122903447 1 20081228 A 2120 UNKNOWN RAYTHN 400 400ARAYTHEON NM LAVATORY ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 179QS RK578 STRONG BURNING ODOR COMING FROM THE LAV AREA. 2 H 7 2 4F RT A16SW 20090105 CE 2009 1 5 DXTA2008122403434 1 20081224 A 2730 ELEVATOR SYSTEM CESSNA 560 560XL 2076702 CE STIFF E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 630QS 5605130 ELEVATOR CONTROL FEELS STIFF. 2 L 7 2 4F RT A22CE 20090105 NM 2009 1 5 DXTA2008123003449 1 20081229 A 3230 LANDING GEAR RAYTHN 400 400ARAYTHEON NM INOPERATIVE E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 114QS RK469 LANDING GEAR WOULD NOT EXTEND. PERFORMED ALTERNATE GEAR EXTENSION PROCEDURE. 2 H 7 2 4F RT A16SW 20090105 EA 2009 1 5 ASOA200900006 1 20081229 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 IN PASSENGER COMPARTMENT FLOOR STRUCTURE FS 280.00 LBL 9.00 OUTBD ATTACHMENT ANGLE CRACKED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200900007 1 20081229 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 IN PASSENGER COMPARTMENT FLOOR STRUCTURE FS 349.00 INTERCOSTAL TOP CAP BETWEEN RBL 27.00 AND RBL 36.00 HAS SEVERAL NUTPL ATE FASTENERS AND ATTACHMENT FASTENERS CORRODED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200900008 1 20081229 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 IN PASSENGER COMPARTMENT FLOOR STRUCTURE FS 349.00 INTERCOSTAL TOP CAP BETWEEN LBL 27.00 AND LBL 36.00 HAS SEVERAL NUTPL ATE FASTENERS AND ATTACHMENT FASTENERS CORRODED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200900009 1 20081229 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 IN PASSENGER COMPARTMENT FLOOR STRUCTURE PASSENGER DOOR HANDRAIL CUPS FS 315.00 AND FS 343.00 LBL 36.00 HAS MINOR SURFAC E CORROSION. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200801728 1 20081222 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 F/A CANNOT GET PAX DOOR TO OPEN. FLT 4980 DEL 90 MINS. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200900014 1 20081229 A 5210 MOTOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 934EV 8028 MAIN PASSENGER DOOR WILL NOT CLOSE. FLT 5405 DEL 47 MINS. REMOVED AND REPLACED PAX DOOR POWER ASSIST MOTOR ASSY IAW CR J 200 AMM 52-11-01. OP'S CHECK GOOD. DMIL CLEARED PLACARD REMOVED. 2 L 7 2 4F RT A21EA 20090105 NE 2009 1 5 DXTA2008121803406 2 20081217 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT SHUTDOWN E DXTA O OTHER X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 GL 07 345QS 5600445 AFTER NORMAL ENGINE START LEFT ENGINE SHUT DOWN DURING THE SPEED BRAKE TEST. 2 L 7 2 4F 4 F RT A22CE E25EA 20090105 CE 2009 1 5 DXTA2008122203412 1 20081219 A 3260 WARNING LIGHT CESSNA 560 560XL 2076702 CE ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 602QS 5605518 AFTER TAKEOFF AND GEAR RETRACTED, THE GEAR UNLOCK LIGHT REMAINED ILLUMINATED. 2 L 7 2 4F RT A22CE 20090105 CE 2009 1 5 DXTA2008122203413 1 20081220 A 5270 WARNING LIGHT CESSNA 750 750 2076810 CE PAX DOOR ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 971QS 7500071 AMBER CABIN DOOR SEAL LIGHT CAME ON AFTER TAKEOFF. 2 L 7 2 4J RT T00007WI 20090105 NM 2009 1 5 DXTA2008122303422 1 20081221 A 3260 INDICATION SYS GULSTM 200 200 4500308 NM MLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 740QS 194 LEFT MAIN LANDING GEAR WAS VERY SLOW TO EXTEND TWICE. GOT A RED UNSAFE INDICATION FOR APPROX 1 MIN. BEFORE TURNING GREEN . 2 L 7 2 4F RT A53NM 20090105 CE 2009 1 5 DXTA2008122303423 1 20081221 A 2150 A/C PACK CESSNA 750 750 2076810 CE COCKPIT MALFUNCTIONED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 916QS 7500116 COCKPIT PAC IS STUCK ON AND WILL NOT DECREASE IN TEMP. CREW COULD DETECT A BURNING ODOR IN FLIGHT. 2 L 7 2 4J RT T00007WI 20090105 SO 2009 1 5 SIMA200835403 1 20081217 A 3240 142093 CONTROL UNIT EMB 135 EMB135KL 3260302 SO ZONE 200 MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 839AE 14550 145653 ON FLIGHT 4663 ON TAKE OFF CREW RECEIVED A BRAKE DEGRADE ON EICAS. CREW ABORTED TAKEOFF AND RETURNED TO BLOCK. AIRCRAF T REMOVED FROM SERVICE. TROUBLESHOT IAW FIM TASK 32-41-00-810-805A. REMOVED AND REPLACED ACU IAW AMM 32-41-02. OPERAT ION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20090105 SO 2009 1 5 SIMA200835003 1 20081215 A 3260 852701 PROXIMITY SWITCH EMB 135 EMB135KL 3260302 SO NLG MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 822AE 145581 ON FLIGHT 4706, CREW REPORTED AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED AND LANDED IN JFK SAFELY. REMOVED AND REPLACED LGEU, NOSE LANDING GEAR DOWN LOCK PROX SWITCH, AND LEFT MAIN LANDING GEAR DOWN LOCK PROX SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20090105 EA 2009 1 5 ASOA200900020 1 20081230 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 LT FS 621-625 INTERCOSTAL ANGLE CRACKED .3" LONG. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200900021 1 20081231 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 CORROSION ON FWD AND AFT LOWER FRAMES IN CARGO FIREX BOTTLES COMPT RT AFT FUSELAGE FS879.00 TO FS909.00. 2 L 7 2 4F RT A21EA 20090105 NM 2009 1 5 SWAA087423 1 20081230 A 5315 6546804 FLOORBEAM BOEING 737 7373L9 1384470 NM BS 352 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 352, LBL 50, WL 195. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 R5KB15916 1 20081220 A 3270 ANGLE BOEING 727 727212 138407G NM AUX GEAR CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 VERTICAL ANGLE CORRODED. 2 L 7 3 4F A3WE 20090105 EU 2009 1 5 USAA2008123092354 1 20081227 A 2560 P2070003001 FLASHLIGHT AIRBUS 320 A320232 3930326 EU CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 665AW 1644 LOG PAGE 8354245 FLT NR 390 LAS-CLT. EMERGENCY FLASHLIGHT UNDER FORWARD FLIGHT ATTENDANT SEAT DOES NOT SHOW CHARGING. MX R&R THE FORWARD FLIGHT ATTENDANT FLASHLIGHT. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20090105 NM 2009 1 5 USAA2008123092343 1 20081211 A 5320 D53472188202 BEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL MAJOR REPAIR C7 CHECK NR 6142387, CORROSION ON CABIN BEAM AT FR 68 - FR 69, +Y1292. REPLACED CABIN BEAM AT FR 68 - FR 69, +Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20090105 NM 2009 1 5 USAA2008123092345 1 20081211 A 5320 D53472172203 BEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL MAJOR REPAIR C7 CHECK NR 6142380, CORROSION ON CABIN BEAM AT FR 66 - FR 68, -Y1167. REPLACED CABIN BEAM AT FR 66 - FR 68, -Y1167 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20090105 NM 2009 1 5 USAA2008123092344 1 20081211 A 5315 D53472172204 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL MAJOR REPAIR C7 CHECK NR 6142388, CORROSION ON CABIN BEAM AT FR 66 - FR 68, +Y1292. REPLACED CABIN BEAM AT FR 66 - FR 68, +Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20090105 EU 2009 1 5 USAA2008123192358 1 20081221 A 5315 D53472189204 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656AW 1079 SAL C7 MAJOR REPAIR NR 6129694 GALVANIC CORROSION ON FLOOR BEAM AT -Y1165 BTW FR67+19" TO FR69+2" OF PAX CABIN. REPLACE D FLOOR BEAM AT -Y1165 BTW FR67+19" TO FR69+2" OF PAX CABIN IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20090105 EU 2009 1 5 USAA2008123192360 1 20081222 A 5320 D53480048000 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656AW 1079 SAL C7 MAJOR REPAIR NR 6129473 SHAPE SILL CORRODED AT L2 DOOR BETWEEN FR66 TO FR68, S23L. REPLACED SHAPE SILL AT L2 DOO R BETWEEN FR66 TO FR68, S23L IAW A320 SRM 57-72-11 AND AIRBUS DRAWING NR D53480505. 2 L 7 2 4F RT A28NM 20090105 EU 2009 1 5 USAA2008123192366 1 20081226 A 5320 D53480020342 WEB AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656AW 1079 SAL C7 MAJOR REPAIR NR 6131295 CRACK ON WEB BTW FR68+10" ABOVE STR 23L OF PAX CABIN AT REAR FUSELAGE. REPAIRED WEB BTW FR68+10" ABOVE STR 23L OF PAX CABIN IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20090105 NM 2009 1 5 USAA2008123192368 1 20081210 A 5540 D5537131800200 FITTING AIRBUS A319 A319132 3930340 NM RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL C7 MAJOR REPAIR NR 6141110 EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 3 AT HORIZONTAL STABILIZER STATION 2279. REPLA CED RUDDER HINGE FITTING NR 3 AT HORIZONTAL STABILIZER STATION 2279 IAW A319 AMM 55-36-41. 2 L 7 2 4F RT A28NM 20090105 NM 2009 1 5 USAA2009010290001 1 20081231 A 5330 6545778 SKIN BOEING 737 7373B7 138447F NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 531AU 24478 CLT RON MAJOR REPAIR LOG NR 4434942. 1.5" CRACK IN FUSELAGE SKIN AT STA 943 STRINGER 24L. VERIFIED CRACK AND MARKED EN DS USING HFEC INSPECTION. REPAIRED FUSELAGE SKIN AT STA 943 STRINGER 24L IAW EA NR 100794. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 HALA2008122800909 1 20081228 A 4940 5198588 STARTER BOEING 767 76733A 1385209 NM APU DEFECTIVE A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM, APU WILL NOT START. PER FIM NEEDED TO CHANGE APU BATTERY PER AMM 24-31-04. CONDITION SAME. REMOVED AND REPLACED APU CONTROL ECU PER AMM 48-61-05 CONDITION SAME. REMOVED AND REPLACED APU TEMP SENSOR PER AMM 49-9 4-01 AND APU PRESS SW PER AMM 49-94-02. CONDITION SAME. REPLACED APU STARTER CLUTCH PER AMM 49-41-06. REPLACED APU ST ARTER PER AMM 49-41-01, STARTED APU 3 TIMES ALL SUCCESSFUL OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20090105 NM 2009 1 5 HALA2008122600905 1 20081226 A 7711 7302143 CIRCUIT CARD BOEING 767 7673CB 1385187 NM EPR SYSTEM FAULTY A HALA K NONE O OTHER NR NOT REPORTED 1 WP 13 592HA 33468 ETOPS SIGNIFICANT SYSTEM , R ENG SPEED CARD DISPLAYED EICAS MSG R ENG EPR INDICATOR BLANKED L ENG EPR INDICATOR BLANKED L ENG EPR INDICATOR CAME BACK. REMOVED AND REPLACED R ENG SPEED CSRD PER AMM 77-12-01. SYSTEM CHECKS NORMAL. EPR L/R BACK TO NORMAL SPEED CARD MSG NO LONGER ON EICAS. 7302143 D04798 D02022 RT 2 L 7 2 4F RT A1NM 20090105 2009 1 5 HALA2008122900910 4 20081229 A 3441 IRU BOEING 767 767332 1382001 NM E&E BAY MALFUNCTIONED A HALA K NONE O OTHER AP APPROACH 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, ON APPROACH TO HNL "C" IRS FAULT EICAS MESSAGE WITH "FAULT" INDICATED ON IRS PANEL. RE-RACKED CENTER IRU. NO IRS FAULT DISPLAYED ON EICAS PAGE OR IRS PANEL. OPS CHECK OKAY PER MM 34-21-01. PERFORMED TEST 30 PAS S AC TO MAINTAIN LMP LAMD 3 STATUS. 2 L 7 2 4F RT A1NM 20090105 NM 2009 1 5 HALA2008122400901 1 20081224 A 8011 35054367 STARTER BOEING 767 76733A 1385209 NM LT ENGINE INOPERATIVE A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM - BTB - LEFT ENG N2 FAILED TO ROTATE WITH STARTER IN GND START VLV LIGHT WAS EXTINGUISHED AND D UCT PRESSURE WAS NORMAL. FOUND NR 1 ENG STARTER DEFECTIVE. REPLACED STARTER PER AMM 80-11-01. OPS AND LEAK CHECK GOOD . OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20090105 NM 2009 1 5 HALA2008122400900 1 20081224 A 5752 KP4R16FS428 BEARING BOEING 767 767332 1382001 NM AILERON TRIM FROZEN A HALA K NONE F FLT CONT AFFECTED CR CRUISE 1 WP 13 596HA 23276 ETOPS SIGNIFICANT SYSTEM, FLIGHT CONTROLS BINDING (AILERON) WILL NOT CENTER. NOTE; WITH AP OFF. REMOVED CONTROL ROD FR OM CAPT TO F/O AILERON DRUM ASSY. CLEANED INSPECTED, REINSTALLED PER AMM 27-11-03. CONDITION SAME, CONT FOUND BEARING P/N KP4R16FS428 ON LT AIL FEEL, CENTERING AND TRIM MECHANISM FROZEN. REMOVED AND REPLACED BEARING PER AMM 27-11-08, OPS CHECK PER AMM 27-11-00 OK. 2 L 7 2 4F RT A1NM 20090105 NM 2009 1 5 HALA2008122400899 1 20081224 A 2740 TRIM SYSTEM BOEING 767 767332 1382001 NM HORIZ STAB MALFUNCTIONED A HALA K NONE F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 WP 13 596HA 23276 ETOPS SIGNIFICANT SYSTEM, FRM: 27480300. EICAS MESSAGE "STAB TRIM" DISPLAYED AND STAB TRIM LIGHT ILLUMINATED. STABILIZE R TRIM OPERATES AT 1/2 SPEED. TROUBLESHOT PER FIM 27-48-00. NO MESSAGES OR FAULTS FOUND. SYSTEM OPERATES NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20090105 NE 2009 1 5 HALA2008122700912 2 20081227 A 7261 OIL SYSTEM BOEING 767 7673CB 1385187 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE LOW A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 592HA 33468 ETOPS SIGNIFICANT SYSTEM, NR 2 ENG REQ 4 PINTS OF OIL. ACP VISUAL INSP OF NR 2 ENG, NO LEAKS NOTED OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20090105 EA 2009 1 5 SWIA200820673 1 20081108 A 2710 LINK CNDAIR CL600 CL6002B19 1900309 EA AILERON CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 445SW 7651 C-CHECK, LEFT FLUTTER DAMPER SHEAR LINK ASSEMBLY CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820674 1 20081108 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 445SW 7651 C-CHECK, LEFT AFT ENGINE MOUNT THRUST FITTING CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20090105 SO 2009 1 5 SWIA200820707 1 20081223 A 2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203 SO LAVATORY MALFUNCTIONED A SWIA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 568SW 120343 FLT 5538 - DURING ENGINE START RECEIVED SMOKE WARNING. INSPECTED LAVATORY AREA, RESET SMOKE ALARM. 2 L 7 2 4T RT A31SO 20090102 2009 1 2 A6WA200840639 2 20081210 A 7261 SCREEN CNDAIR CL600 CL6002B19 1900309 EA SCAVE PUMP COKED A A6WA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 31 432AW 7257 RT ENGINE OIL PRESSURE WARNING MSG AT CRUISE. WARNING PERSISTED AT POWER SETTINGS ABOVE IDLE. CW QRH DIVERTED TO PHL. ENGINE REMAINED AT IDLE DURING THE 40 MINUTE FLIGHT TO PHL. LOWEST OIL PRESSURE SHOWN WAS 24 PSI. REMOVED RT LUBE SCA VENGE PUMP AND FOUND SCREENS COKED UP CAUSING RESTRICTING. CLEANED SCREEN IAW EO8/016/479 AND REINSTALLED PUMP IAW AMM 79-21-01 OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 20090102 NM 2009 1 2 ZZDA2008191 1 20081207 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 893AT 55045 FOUND DENT ON FUSELAGE SKIN STA 446 BETWEEN STR 24L AND 25L OUT OF LIMITS. INSTALLED REPAIR AS PER B717 SRM 53-00-01 RE PAIR 2. 2 L 7 2 4F TR A6WE 20090102 NM 2009 1 2 ZZDA2008192 1 20081226 A 5312 BULKHEAD BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 982AT 55041 RUDDER SUPPORT BULKHEAD CRACKED AT 3 O`CLOCK POSITION STA 1178. REPAIRED RUDDER SUPPORT BULKHEAD CRACK AT STA 1178 L18 IAW B717 SRM 51-70-11. COMPLETED AAR N/R 5837 W/O 2000274 - OK FOR SERVICE. 2 L 7 2 4F TR A6WE 20090102 NM 2009 1 2 ZZDA2008189 1 20081220 A 5270 WARNING SYSTEM BOEING 717 717200 1383700 NM MLG MALFUNCTIONED A ZZDA O OTHER N FALSE WARNING AP APPROACH 1 SO 37 997AT 55141 AFTER LANDING GEAR EXTENSION WAS SELECTED, RECEIVED A "GEAR DOOR OPEN" INDICATION AFTER THE MLG WAS DOWN AND LOCKED. AI RCRAFT FERRIED TO ATL. ATL MAINTENANCE PERFORMED INSPECTION AND OPS CHECKS WITH GEAR SWINGS. COULD NOT DUPLICATE THE P ROBLEM. NO DEFECTS NOTED. 2 L 7 2 4F TR A6WE 20090102 NM 2009 1 2 ZZDA2008190 1 20081223 A 5270 WARNING SYSTEM BOEING 737 737 UTILSYS NM EMERGENCY EXIT MALFUNCTIONED A ZZDA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 37 175AT 32652 AFTER T/O POWER APPLIED, RIGHT OVERWING LIGHT ILLUMINATED. OPENED & CLOSED RIGHT OVERWING EMERGENCY EXIT DOOR. PERFORM ED THE EMERGENCY EXIT DOOR SYSTEM TEST. ALL TEST PASSED. REF AMM 52-22. 2 L 7 2 4F RT A16WE 20090102 EA 2009 1 2 ASOA200801707 1 20081212 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 882AS 7503 FLAPS FAILED AT 20 WHEN SELECTING 8 AFTER TAKEOFF. AIRCRAFT RETURNED TO ATW AFTER T/O, EMERGENCY VEHICLES ROLLED AS A P RECAUTION. FLT 5476 CX 2 L 7 2 4F RT A21EA 20090102 EA 2009 1 2 ASOA200801716 1 20081216 A 5310 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA APU DOOR FRAME CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 923EV 7826 APU INLET DOOR FRAME SUPPORT P/N 601R35210-17 CRACKED .2" LONG AT FWD BOTTOM CORNER RADIUS BETWEEN FS 654.5 - FS 672.20 STR 4L IN AFT EQUIP BAY CEILING. REPLACED APU INLET DOOR FRAME SUPPORT IAW CRJ SRM 51-42-06 FOR SOLID RIVETS, CRJ 200 S RM 51-42-13 FOR CHERRYMAX RIVETS, AND CRJ SRM 51-40-11 FOR FASTENER HOLE PREPARATION. 2 L 7 2 4F RT A21EA 20090105 NM 2009 1 5 C8GA20080051 1 20080813 A 5754 MOUNT BOEING 727 727223 1384074 NM KRUEGER FLAP CRACKED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THE THE NR 2 KFLAP ACTUATOR UPPER MOUNT WAS CRACKED AT THE UPPER INBOARD CORNER. REMOVED DAMAGED MOUNT AND FABRICATED NEW. INSTALLED NEW MOUNT IAW SRM 57-20-02. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090105 CE 2009 1 5 DXTA2008122403435 1 20081224 A 2720 RUDDER CONTROL CESSNA 560 560XL 2076702 CE MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 589QS 5605810 RUDDER PEDALS HAVE GRINDING FEELING DURING TAKEOFF ROLL AND IN-FLIGHT. 2 L 7 2 4F RT A22CE 20090105 CE 2009 1 5 DXTA2008122403437 1 20081224 A 5210 SEAL CESSNA 560 560XL 2076702 CE PAX DOOR INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 694QS 5605194 DOOR SEAL LIGHT ANNUNCIATOR CAME ON IN FLIGHT. DOOR SEAL INOP. 2 L 7 2 4F RT A22CE 20090105 EA 2009 1 5 ASOA200900016 1 20081230 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 FLOOR SEAT TRACKS AT RBL9 HAVE MINOR CORROSION FROM FS349 TO 977. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200900017 1 20081230 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 LT SIDEWALL SEATTRACK HAS MINOR CORROSION FROM FS465 TO 510(MARKED). 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200900001 1 20081229 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 IN PASSENGER COMPARTMENT FLOOR STRUCTURE FS 484.00 RBL 27.00 OUTBD ATTACHMENT ANGLE CRACKED. 2 L 7 2 4F RT A21EA 20090105 CE 2009 1 5 DXTA2008122903444 1 20081227 A 2120 UNKNOWN CESSNA 680 680CE 2076811 CE COCKPIT SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 07 382QS 6800245 SMOKE IN COCKIT DURING APPROACH 2 L 7 2 4F RC T00012WI 20090105 CE 2009 1 5 DXTA2008122903446 1 20081227 A 2751 INDICATION SYS CESSNA 750 750 2076810 CE TE FLAPS ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 903QS 7500162 "FLAPS FAIL" MSG ILLUMINATED DURING FLAP RETRACTION. 2 L 7 2 4J RT T00007WI 20090105 CE 2009 1 5 DXTA2008121903408 1 20081218 A 3210 LANDING GEAR CESSNA 750 750 2076810 CE INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 960QS 7500160 AFTER TAKEOFF , LANDING GEAR WOULD NOT RETRACT. 2 L 7 2 4J RT T00007WI 20090105 CE 2009 1 5 DXTA2008123003450 1 20081229 A 2700 UNKNOWN CESSNA 750 750 2076810 CE UNKNOWN E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 983QS 7500083 EXCESSIVE LEFT RUDDER TRIM NEEDED TO MAINTAIN COORDINATED STRAIT LEVEL FLIGHT. 2 L 7 2 4J RT T00007WI 20090105 EA 2009 1 5 SIMA200835402 2 20081216 A 7200 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO RROYCE AE3007 AE3007A1 54165 EA LEFT SMOKE A SIMA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 677AE 19871 14500810 CAE311151 ON FLIGHT 3598, ON TAKEOFF CREW REPORTED SMOKE IN CABIN. CREW ABORTED TAKEOFF AND RETURNED TO BLOCK. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENGINE. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20090105 SO 2009 1 5 SIMA200836401 1 20081220 A 3260 WARNING LIGHT EMB 135 EMB135KL 3260302 SO NLG DOOR FALSE INDICATION A SIMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 833AE 145629 ON FLIGHT 4740 CREW REPORTED AFTER DEPARTURE NOSE LANDING GEAR DOOR NOT CLOSING. THE LANDING GEAR INDICATION WAS NORMAL WITH 3 GREEN AND NO WARNING MESSAGES. CREW PERFORMED A FLY BY AT JFK WHICH RETURNED UNREMARKABLE. CREW DECLARED AN EM ERGENCY AND LANDED SAFELY AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PERFORMED GE AR SWING IAW EMB AMM NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20090105 2009 1 5 SIMA200836402 4 20081222 A 3444 70001840937 ALTIMETER EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION LD LANDING 1 SW 21 617AE 145093 ON FLIGHT 3474, CREW REPORTED AT 300 FEET AGL THEY GOT AURAL GPWS WARNING AND LANDING GEAR WOULD NOT COME DOWN WITH GEAR TOO LOW. WITH GEAR DOWN AND CONFIGURED CORRECTLY CREW DID A GO AROUND AND RECYCLED GEAR. TOWER CONFIRMED GEAR DOWN. R EQUESTED CFR AND LANDED AIRCRAFT SAFELY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RADIO ALT UNIT IAW AMM 34 -31-01. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20090105 SO 2009 1 5 SIMA200836403 1 20081225 A 3240 429513 CONTROL UNIT EMB 145 EMB145LR 3260212 SO BRAKE MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION LD LANDING 1 SW 21 625AE 16956 639 145115 ON FLIGHT 4345, CREW REPORTED AFTER LANDING UPON GEAR EXTENSION THEY GOT 2 EICAS MESSAGES 1 FOR INBOARD BRAKES INOP AND 1 FOR OUTBOARD BRAKES INOPERATIVE. THEY RECYCLED GEAR WITH NO HELP. DECLARED EMERGENCY AND LANDED USING THRUST REVERSE RS BRAKES APPEARED TO WORK NORMALLY. AIRCRAFT TAXIED TO GATE SAFELY WITH NO FURTHER INCIDENT. CREW INSPECTION SHOWED N O APPARENT PHYSICAL DEFECTS. REMOVED AND REPLACED BRAKE CONTROL UNIT. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20090105 NM 2009 1 5 USAA2009010290002 1 20081231 A 5330 6545774 SKIN BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT RON MAJOR REPAIR LOG NR 4434952. 2 1/4" CRACK IN FUSELAGE SKIN BETWEEN STA 727D & 727E AT STR 24R. VERIFIED CRACK AND MARKED ENDS USING HFEC INSP. REPAIRED FUSELAGE SKIN BETWEEN STA 727D & 727E AT STR 24R IAW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087407 1 20081230 A 3350 8200048901 LENS BOEING 737 7377H4 1384404 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 480WN 33998 R1 EMERGENCY EXIT DOOR LIGHT LENS FELL OFF. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087410 1 20081229 A 5753 113A270016 FLAP BOEING 737 7377H4 1384404 NM RT WING PUNCTURED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 766SW 29806 DURING SCHEDULED MV2 CHECK, FOUND RT WING INBOARD T/E FLAP PUNCTURED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20090105 EA 2009 1 5 SWIA200820740 1 20081121 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 C-CHECK, FS 280 BEAM LBL9 INBOARD CORNER CLIP CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820741 1 20081121 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 C-CHECK, FS 280 BEAM RBL 9 INBOARD CORNER CLIP CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20090106 NM 2009 1 6 FDEA200812165176 1 20081216 A 5320 655612910 SILL BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 276FE 22041 C-2 DOOR SILL CHORD O/B FLANGE CORRODED. REMOVED CORROSION PER B727 SRM 51-10-6 AND PERFORMED UT INSP OF AREA IAW NDTM 51-00-00 FIG 3 PART 4. (ORIG: .220 REMAIN : .170 LOSS: .050). REPORTED FINDINGS TO ENGINEERING AND EA 7-5310-126874 D ATED 15 DEC 08 ISSUED FOR REPAIR. HFEC AREA IAW NDTM 51-00-00 FIG 23 PART 6 PER EA 7-5310-126874 NO DEFECTS NOTED. REM OVED FASTNERS IAW SRM 51-30-2 AND HFEC HOLES IAW NDTM 51-00-00 FIG 16 PT 6 PER EA 7-5310-126874 NO DEFECTS NOTED. FLAP PEENED AREA IAW BSOPM 20-10-03 AND EA 7-5310-126874. OVERSIZED FASTNER HOLES 1/64 IAW SRM 51-30-5 AND EA 7-5310-126874 AND TREATED AND PRIMED AREA IAW B727 SRM 51-10-2. INSTALLED OVERSIZE FASTNERS IAW SRM 51-30-2 AND APPLIED ONE COAT OF TY 2 L 7 3 4F RT A3WE 20090106 EU 2009 1 6 FDEA200812175184 1 20081217 A 5340 A5377881320200 FITTING AIRBUS 300 A300B4622 3930401 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 CRACKED FITTING UNDER FWD. CARGO FLOOR, FR 38.2 RBL 8 REMOVED & REPLACED FITTING UNDER THE FLOOR AT FRAME 38.2; RBL 8 I AW SRM 51-40-21; PG 7. 2 L 7 2 4F RT A35EU 20090106 EU 2009 1 6 FDEA200812165173 1 20081216 A 5322 A5377341420151 SHEAR TIE AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 38333 248 FWD PIT BILGE FR 36 BETWEEN STGR 51L AND 52L SHEAR TIE HAS CORROSION FWD AND AFT SURFACES. REMOVED SHEAR TIE FROM FRAME 36 BETWEEN STRINGER 51L & 52L IAW SRM 51-40-21. REMOVED CORROSION FROM SHEAR TIE IAW SRM 51-73-10. ORIGINAL MATERIAL 0 .055 IAW SRM 53-14-13. MATERIAL LOSS 0.043. FOUND TO BE OUT OF LIMITS IAW SRM 51-73-10. LOCATED & DRILLED NEW SHEAR TIE IAW SRM 51-40-44. ALODINED IAW SRM 51-21-10. PRIMED IAW SRM 51-23-10. INSTALLED SHEAR TIE IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20090106 NM 2009 1 6 FDEA200812165177 1 20081216 A 5330 651842010 SKIN BOEING 727 727233 138408A NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 276FE 22041 PREVIOUS REPAIR AT BS 312 STR 24R HAS IMPROPERLY INSTALLED FASTENERS, AND FOUND GOUGES, AND TOOLING MARKS. REMOVED PREV IOUS REPAIR AT BS 312 STR 24R IAW SRM 51-30-2. CUT OUT DAMAGED AREA IAW SRM 51-10-1. CUT OUT DIMENSIONS 3.8" X 4.1". F ABRICATED REPAIR FILLER. FABRICATED FILLER AND FABRICATED DOUBLE IAW SRM 53-30-2 FIG 2, 53-30-3 FIG 5, 51-30-5, AND 51 -30-8. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2 AND INSTALLED REPAIR PARTS IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 20090106 NM 2009 1 6 FDEA200812165182 1 20081216 A 5730 DMS15920063 DOUBLER DOUG MD11 MD11F 3023600 NM ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 RIGHT WING LEADING EDGE WING ANTI-ICE TELESCOPIC DUCT CUT OUT REPAIR DOUBLER FOUND CHAFED. DOUBLER REMOVED AS PER SRM 5 1-31-01 VOLUME II AND INSTALLED WITH A NEW REPAIR DOUBLER AS PER EA 1-5740-122639 PART 1. ADJUSTMENT AND TEST CARRIED O UT AS PER AMM 27-80-30-5. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090106 NM 2009 1 6 ASAA0844121 1 20081212 A 5210 652999413 NUT BOEING 737 7374Q8 138447Q NM L1 DOOR LOOSE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 557 25101 L1 DOOR WILL NOT CLOSE FOUND GUIDE ARM ROD END JAMB NUT LOOSE. SECURED LOOSE JAMB NUT. L1 DOOR OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 20090106 SO 2009 1 6 C2XA08IA275 1 20081228 A 2130 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN PRESSURE MALFUNCTIONED A C2XA B EMER. DESCENT O OTHER CR CRUISE 1 SW 27 13118 145675 COS - FLIGHT 2116, THE CREW REPORTED A RAPID DEPRESSURIZATION AT FL360. THE CREW PERFORMED AN EMERGENCY DESCENT AND LAND ED AT COS WITHOUT INCIDENT. MX INSPECTED THE ACFT, OPS CHECKED THE MANUAL AND AUTO PRESSURIZATION SYSTEMS WITH NO DEFEC TS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20090106 NM 2009 1 6 FDEA200812175187 1 20081217 A 2131 7909601 CONTROLLER BOEING 727 727225 1384077 NM CABIN PRESSURE MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 467FE 21449 CABIN PRESSURIZATION CONTROLLER WOULD NOT MAINTAIN CABIN ALTITUDE. CONSTANT CLIMB OF 1500 FT/MIN SETTING OFF CABIN ALT WARNING HORN AT 10000 AND CLIMBING TO 14000 WHILE LEVEL AT FL 250. PERFORMED DECAY CHECK OF ACFT IN REF TO JRH AND DECA Y PASSED, SO AS A PRECAUTION REMOVED AND REPLACED CABIN PRESSURE CONTROLLER IN REF TO AMM 21-31-010-4, OPS CHECKED GOOD. ACFT OK FOR SERVICE. 2 L 7 3 4F A3WE 20090106 NE 2009 1 6 HALA2008122700913 2 20081227 A 7261 OIL SYSTEM BOEING 767 7673CB 1385187 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE LOW A HALA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 13 592HA 33468 ETOPS SIGNIFICANT SYSTEM, NR 2 ENG REQ 4 PINTS OF OIL. ACP VISUAL INSP OF NR 2 ENG. NO LEAKS NOTED OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20090106 NM 2009 1 6 FDEA200810034188 1 20081003 A 5347 2024T3190C SEAT TRACK BOEING 757 75723A 1384967 NM BS 900-1076 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 MAIN CABIN, SEAT TRACK BS 900 TO BS 1076 LBL 45.50 CROWN GOUGED AND SCRATCHED. REMOVED AND REPLACED SEAT TRACK STA 900 TO 1076 LBL 45.50 IAW SRM 51-40-02, 53-00-52, REPAIR NR 4. THIS IS A MAJOR AND CATEGORY "A" REPAIR. 2 L 7 2 4F RT A2NM 20090106 NM 2009 1 6 FDEA200812165179 1 20081216 A 5310 143N552010 CREASE BEAM BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 MAIN CABIN FLOOR SUPPORT, RT CREASE BEAM, INBD CHORD, BS 600-620, HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. C ORROSION OUT OF LIMITS PER SRM 53-30-13, DETAIL 2; D=.025". REMOVED AND REPLACED BS 600-620, RBL 63-70, INBD CREASE BEA M WEB, THAT WAS FABRICATED ON MAE TRAVELER NR T8/763830, IAW SRM 51-40-02/51-20-05. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20090106 WP 2009 1 6 FDEA200812115180 1 20081211 A 3246 BEARING DOUG MD10 MD1010F 3022112 WP MLG WHEEL FAILED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 362FE 48261 NR 1 TIRE ASSY OUTSIDE BEARING FAILURE. REMOVED WHEEL AND BRAKE ASSY FROM NR 1 AXLE LT MLG TRUCK ASSEMBLY TAG NR 5023BO . REPLACED LEFT MAIN LANDING GEAR TRUCK BEAM AND AXLE ASSY PER M/M REF 32-12-01-2. AIRCRAFT OK FOR FURTHER SERVICE. 2 L 7 3 4F RT A22WE 20090106 NM 2009 1 6 WX0A070247 1 20081103 A 5340 59121415967059 ANGLE DOUG MD80 MD83 3023681 NM ZONE 200 CRACKED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 879GA 53486 VERTICAL STABILIZER TO FUSELAGE PRODUCTION ANGLE CRACKED. 2 L 7 2 4F RT 20090106 EA 2009 1 6 SWIA200820734 1 20081227 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 750SK 10207 FLT 6085 - NR 3 OVERHEAD EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820735 1 20081228 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 702SK 10136 FLT 6075 - CEILING EMERGENCY LIGHT (2ND FROM REAR) INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820736 1 20081121 A 5322 SHEAR TIE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 C-CHECK, LEFT WINDSHIELD SIDE POST SUPPORT BOTTOM SHEAR TIE CRACKED. REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820697 1 20081218 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 466SW 7856 FLT 6018 - SECOND AFT CABIN EMERGENCY CEILING LEVEL FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 NM 2009 1 6 K11A2009010272305 1 20080102 A 5210 FRAME BOEING 727 7272H3 138368N NM L1 DOOR DAMAGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 723CK 20545 HOLES IN FRAME ELONGATED, L 1 DOOR. 2 L 7 3 4F RT A3WE 20090105 NM 2009 1 5 C8GA20080057 1 20080825 A 5752 BAC15141617 SUPPORT BOEING 727 727223 1384074 NM ZONE 800 CRACKED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE RIGHT WING IB AILERON TAB HAS DELAMINATION. REMOV ED DAMAGED AREA, FABRICATED CORE. FABRICATED DOUBLER. INSTALLED REPAIR HOT BONDED & SEALED CORE AND DOUBLER. IAW SRM 51- 40-20. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090105 NM 2009 1 5 C8GA20080046 1 20080823 A 5347 BAC15201466 SEAT TRACK BOEING 727 727223 1384074 NM BS 740-760 LBL 4 GOUGED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION NOTED THAT THE MAIN CABIN SEAT TRACK HAS DEEP QOUGE AT BS 740-760 LBL 4 5.5. REMOVED SEAT TRACK AT LBL 45 BS 740-760 DISPLACED SPLICE PER VENTURA AEROSPACE DWS 2902 INSTALLED NEW SEAT TRACK IA W SRM 53-10-5, 53-10-2. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090105 EA 2009 1 5 ASOA200900011 1 20081229 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ODOR A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 847AS 8028 ON DESCENT INTO INTO ATL THROUGH FL 270 SMELLED BURNING SMELL LIKE ELECTRICAL OR BURNING HAIR. SMELL WAS ISOLATED TO CO CKPIT. NONE SMELLED IN PACKS OR BY FA STRONG SMELL LASTED ABOUT 45 SEC. NO INDICATION FROM CBS OR ELEC PAGE. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 ASOA200900019 1 20081230 A 5311 REPAIR CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 LT FS 718 FRAME PREVIOUS REPAIR CRACKED 2" LONG BETWEEN STRS 10L AND 11L. 2 L 7 2 4F RT A21EA 20090105 SO 2009 1 5 SIMA200835001 1 20081209 A 3040 HEATER EMB 145 EMB145LR 3260212 SO WINDSHIELD ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 620AE 145102 ON FLIGHT 3956, CREW REPORTED ELECTRICAL BURNING ODOR AT GATE FROM COCKPIT. AIRCRAFT REMOVED FROM SERVICE. OPERATED EL ECTRICAL SYSTEM AND WINDSHIELD HEAT IAW AMM 30-43-00. COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20090105 NM 2009 1 5 EIAA2008102800075 1 20081214 A 3350 900835A BATTERY PACK BOEING 747 747230B 1384889 NM EMERGENCY LIGHT NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487EV 23286 UPPER DECK LT SLIDE EMERGENCY LIGHT INOP RELAMP NO HELP. REPLACED BATTERY PACK AND RECHARGES, OPS CHECKED NORMAL IAW MM 33-51-00. 2 L 7 4 4F RT A20WE 20090105 NM 2009 1 5 SWAA087415 1 20081230 A 5330 6562212 SKIN BOEING 737 7373L9 1384470 NM BS 303 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, BS. 303 WL 236. REPAIRED SKIN P ER ER. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087416 1 20081230 A 5315 6545410 FLOORBEAM BOEING 737 7373L9 1384470 NM BS 706 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 706, BL 0, WL 140.5. REPAIRED WEB PER PAE E R. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087404 1 20081228 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 460 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087405 1 20081228 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 500A S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087406 1 20081229 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 466WN 30677 DURING SCHEDULED MV2 CHECK, FOUND FWD EMERGENCY LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087417 1 20081230 A 5315 6546804 FLOORBEAM BOEING 737 7373L9 1384470 NM BS 712-713 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BETWEEN BS 712 TO BS 713, BL 0, WL 202. REPAIR ED WEB PER PAE ER. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087418 1 20081230 A 5315 6546804 FLOORBEAM BOEING 737 7373L9 1384470 NM BS 708 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS. 708, RBL 24, WL 202. REPAIRED WEB PER PAE ER. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087424 1 20081230 A 3350 8100022608 LIGHT BOEING 737 7373L9 1384470 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087425 1 20081230 A 5315 6546804 FLOORBEAM BOEING 737 7373L9 1384470 NM BS 727B CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM L ANGLE CRACKED AT BS 727B, LBL 45, WL 206. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 ASAA0974125 1 20081231 A 3350 D71701100 BATTERY PACK BOEING 737 737790 13844CN NM CABIN FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 627AS 30794 REF T/C 78233001: EMERGENCY LIGHT BATTERY PACKS M1673 AND M1675 FAIL DEEP CYCLE CAPACITY TEST. R&R AND TESTED EMERGENCY LIGHT BATTERY PACKS M1673 AND M1675 PER MM33 51 06 960 805 OPS NORMAL. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 SWAA087426 1 20081230 A 5310 6547978 CREASE BEAM BOEING 737 7373L9 1384470 NM BS 616-639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND RT CREASE BEAM WEB CRACKED BETWEEN BS 616 TO BS 639, WL 208. REMOVED AND REPLACED WE B PER SRM. 2 L 7 2 4F RT A16WE 20090106 NE 2009 1 6 22AA20081203 2 20081231 A 7532 563883 BLEED VALVE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 1 ENGINE STUCK A 22AA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 19 784AL 46135 671443 LOG PAGE NR 128276. NR 1 ENGINE WOULD NOT ACCELERATE TO TAKE-OFF POWER; REJECTED TAKE OFF AT 80 KTS. - RETURNED TO GATE . FOUND NR 1 COMPRESSOR BLEED VALVE STUCK IN OPEN POSITION. R&R NR 1 ENGINE COMP. BLEED CONTROL VALVE IAW DC-8 M/M 75 -30-3; OPS CHECK NORMAL IAW M/M 5-50-0 UNSCHEDULED MX CHECK, NO DEFECTS NOTED. 2 L 7 4 4F 4 F 4A25 1E8 20090106 NM 2009 1 6 ASAA0954123 1 20081230 A 4950 32912142 BLEED VALVE BOEING 737 737890 1384527 NM APU MALFUNCTIONED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 559AS 8940 35178 DURING ENGINE START ENGINE NR 1 AIR PRESSURE NEVER ROSE ABOVE 15 PSI WITH STARTER ENGAGED. N2 VERY SLOW TO RISE START A BORTED GROUNDED YES. ACCOMPLISHED APU BITE PROCEDURE NO CURRENT FAULTS. STARTED APU RAN RT PACK & DRY MOTOTED NR 2 ENG APU BLEED INDICATIONS NORMAL. REF FIM 49 55 808. ACFT REMAINS ETOPS QUALIFIED SEAMC LANCE NOTIFIED. OAT 40F 2 L 7 2 4F RT A16WE 20090106 SO 2009 1 6 C2XA08IA276 1 20081230 A 3350 375921 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14904 145477 IAH - DURING MX INSPECTION THE EMERGENCY EXIT OVERHEAD LIGHT AT THE CENTER EXIT WAS FOUND TO BE INOPERATIVE. MX INSPECT ED THE ACFT AND RECONNECTED THE EMERGENCY LIGHT, OPS TESTS WERE SATISFACTORY, AND THE ACFT WAS APPROVED FOR RETURN TO SE RVICE. 2 L 7 2 4T RT T00011AT 20090106 NM 2009 1 6 K11A2009010272306 1 20080508 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE DENTED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 723CK 20545 DENT IN FUSELAGE. 2 L 7 3 4F RT A3WE 20090106 EA 2009 1 6 MASA2008123100764 1 20081231 A 2121 FAN CNDAIR CL600 CL6002D24 1390016 EA FWD LAVATORY MALFUNCTIONED A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 916FJ 15016 ASH FLT 2964 PHX-MZT. SMOKE FWD LAV WARNING - SMOKE FORWARD GALLEY. MX R&R GALLEY EXHAUST FAN. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 MASA2008122900759 1 20081229 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A MASA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SW 07 75993 7372 ASH 7299 GRB-ORD. CREW DECLARED AN EMERGENCY DUE TO A FLAP FAIL AFTER TAKEOFF. MX THAWED OFF ICE, RESET AND COMPLIED W ITH PART A AND B INSPECTION. 2 L 7 2 4F RT A21EA 20090106 NM 2009 1 6 YENA200812190129 1 20081216 A 2781 5913479 SENSOR EMB ERJ190 ERJ190100IGW 3260408 NM LE SLAT FAILED A YENA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 EA 15 284JB 2906 1900000144 FLT NR 1304, IAD-JFK, SLAT FAIL WHEN MOVING FLAP HANDLE TO 1. AFTER FOLLOWING QRH SLAT INDICATION OF ZERO AND AMBER FLA PS 2 (FLAP HANDLE 2) GREEN. OTHER MSGS, SHAKE ANTICIPATED, AOA LIMIT FAIL, SPOILER FAULT, SLAT FAIL. FOUND SLAT SENSOR A T FAULT OB, R&R PREVIOUSLY REPLACED OB SLAT SKEW SENSOR. R&R LT IB 1-2 SLAT SKEW SENSOR IAW 27-83-01. INSTALLED NEW SL AT WING ANTI-ICE BELLOW BETWEEN SLATS 3 & 4 IAW AMM 30-11-01, OPS CHECK OK. 2 L 7 2 4F RT A57NM 20090106 CE 2009 1 6 DJFA2008085 1 20081219 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 462LX 2250 407 RK423 DURING A SCHEDULED MX VISIT, WHILE PERFORMING A HORIZ STAB ROLLER INSP OF THE HORIZ STAB INBD RIB AND BRACKET ASSEMBLIES , THE LT INBD RIB WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. THE LT AND RT RIB ASSEMBLIES WERE REPLACED. 2 H 7 2 4F RT A16SW 20090106 CE 2009 1 6 GUUA92752122808 1 20081228 A 5220 HANDLE BEECH 1900 1900D 1154162 CE EMERGENCY EXIT LACK OF LUBE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 46AR UE27 DURING SCHEDULED ROUTINE MAINT, DISCOVERED LT EMERGENCY EXIT HARD TO OPEN. LUBRICATED LT EMERGENCY EXIT INNER AND OUTER HANDLES. OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 20090106 CE 2009 1 6 GUUA93532122808A 1 20081228 A 3234 1013841377 CONTROL HANDLE BEECH 1900 1900D 1154162 CE COCKPIT INOPERATIVE A GUUA O OTHER O OTHER CL CLIMB 1 SO 29 81535 5099 UE147 AFTER TAKEOFF, UNABLE TO MOVE THE LANDING GEAR HANDLE FROM EXTENDED POSITION TO RETRACTED POSITION. DIVERTED, LANDED WIT HOUT INCIDENT. REPLACED LANDING GEAR HANDLE. OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 20090106 NM 2009 1 6 USAA2008123092352 1 20081211 A 5320 D53480019216 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL - MAJOR REPAIR - C7 CHECK - NR 6142386, CRACKED SHEAR PLATE AT FR 68 - FR 69, +Y1732. REPLACED SHEAR PLATE AT FR 68 - FR 69, +Y1732 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20090106 CE 2009 1 6 DJFA2008086 1 20081221 A 2697 CONNECTOR RAYTHN DH125 HAWKER800XP 7150012 CE FIRE DETECTION UNSECURE E DJFA O OTHER N FALSE WARNING CR CRUISE 1 EA 23 813LX 258454 DURING FLIGHT BAGGAGE FIRE ANNUNCIATOR ILLUMINATED. NO EVIDENCE OF FIRE WAS FOUND. MX FOUND THE CONNECTOR TO THE FWD B AGGAGE FIRE DETECTOR NOT SECURED PROPERLY. THE CONNECTOR WAS RESEATED. 2 L 7 2 4F RT A3EU 20090106 NM 2009 1 6 ERAA200800002 1 20081127 A 5314 85320056 KEELBEAM DHAV DHC8 DHC8106 2809020 NM ZONE 100 CORRODED A ERAA K NONE O OTHER IN INSP/MAINT 1 AL 03 883EA 35864 4981 260 CORROSION ON KEELBEAM, STR 31P, FS 222.7 AND 222.7. CORROSION ON KEEL BEAM ,STR 31P, FS 222.7 AND 252.7, BLENDED IAW RD 8-53-10403. FOUND TO BE WITHIN LIMITS OF RD 8-53-10403. 2 H 7 2 4T RT A13NM 20090106 NE 2009 1 6 CVG2008F00004 2 20081202 A 7321 1240KDC03005 EEC LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE LT ENGINE FAILED E CVGA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 05 95AG 4989 079 305280 LT ENG FAILED ABOUT 10-15 MINUTES INTO FLIGHT AT FL190. CREW REPORTED HEARING A BOOM AND THE 1ST OFFICER NOTICED THE LT ENGINE ROLL BACK. AN AIR START WAS NOT ATTEMPTED AND THE ACFT DIVERTED. REPLACED EEC WITH REPAIRED UNIT. PERFORMED G ROUND RUNS AND TEST FLIGHT. AC RETURNED TO SERVICE. THIS ENG IS PRE SB 24-434 (EEC). SUSPECTS ONE CHANNEL OF THE EEC D EVELOPED A FAULT AND ATTEMPTED TO CHANGE CHANNEL. THE EEC HAS A LANE-CHANGE CHANEL. THE EEC HAS A LANE-CHANGE RELAY, W HICH IS AN ELECTROMECHANICAL RELAY (AND NOT A SOLID STATE RELAY AS IN THE NEWER EEC`S) WHICH HAS A TENDENCY TO STICK OR TO TOO SLOW TO SWITCH CONTACTS. WHEN THIS TYPE OF FAILURE OCCURS NEITHER CHANNEL IS IN CONTROL OF THE FUEL FLOW AND FLA 2 L 7 2 4F 4 F RT A10CE E35NE 20090106 NM 2009 1 6 USAA2008123092342 1 20081211 A 5320 D53480043205 SILL AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL - MAJOR REPAIR - C7 CHECK - NR 6142382, CORROSION ON R2 DOOR CUT OUT LOWER SILL AT FR 66 - FR 68, -Y1732. REPAIRED R2 DOOR CUT OUT LOWER SILL AT FR 66 - FR 68, -Y1732 IAW US AIRWAYS EA 132178. 2 L 7 2 4F RT A28NM 20090106 EU 2009 1 6 USAA2008123092355 1 20081227 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST UK UNKNOWN 1 EA 19 672AW 2193 LOGPAGE: 8316380 - FLT 672 - PHL-PHX - EEL - EMERGENCY FLASHLIGHT ON AIRCRAFT AFT LEFT INOPERATIVE. REMOVED AND REPLACE D EMERGENCY FLASHLIGHT BATTERY ON AIRCRAFT AFT LEFT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20090106 EU 2009 1 6 USAA2008123192369 1 20081221 A 2560 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 647AW 762 SAL - EES - C8 CHECK - NR 6142565 INOPERATIVE BATTERY IN FLASHLIGHT AT AFT LEFT HAND FLIGHT ATTENDANTS SEAT. REMOVED A ND REPLACED FLASHLIGHT BATTERY AFT LEFT HAND FLIGHT ATTENDANTS SEAT. 2 L 7 2 4F RT A28NM 20090106 NM 2009 1 6 FDEA200812205253 1 20081220 A 5315 BAC1505100617 FLOORBEAM BOEING 757 75728A 1384976 NM BS 365 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 912FD 24260 MAIN CABIN FLOORBEAM UPPER CHORD STA 365 FROM BL 0 TO RBL 65 HAS CORROSION. REMOVED PREVIOUS T-CHORD REPAIR FROM STA 365 LBL 17 TO RBL 70 IAW SRM 53-00-51 FIG 201 REPAIR NR 3. FABRICATED TEE CHORD AND REPAIR PARTS IAW SRM 53-00-51 FIG 20 1 AND TRAVELLER'S T8/766554 AND T8/766555. INSTALLED TEE CHORD AND REPAIR PARTS AT STA 365, LBL 17 TO RBL 70 IAW SRM 53 -00-51 FIG 201 REPAIR NR 3. THIS REPAIR IS CLASSIFIED AS CATEGORY "A" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20090106 NM 2009 1 6 FDEA200812225256 1 20081222 A 5320 AJC705070 STIFFENER DOUG MD11 MD11F 3023600 NM BS 2007 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 EMPENNAGE: AFT FUSELAGE COMPARTMENT PRESSURE BULKHEAD STA 2007 QUANTITY 01 STIFFENER X = -15.25 FOUND CRACKED APPROX 0.3 5 INCH AT UPPER CORNER AREA. AFT FUSELAGE COMPARTMENT PRESSURE BULKHEAD STATION 2007 X = -11.25 STIFFENER CARRIED OUT REPAIR AS PER EA 1-5310-122664 PART 1. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090106 NM 2009 1 6 FDEA200812225257 1 20081222 A 5712 ARB2850506 RIB DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 RT WING FIXED LEADING EDGE SLAT TRACK 16 INBD RIB FOUND CRACKED. RIB REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-35-01 VOLUME II AND SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090106 EU 2009 1 6 USAA2009010590018 1 20081221 A 5320 D53471124200 SHEAR PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656AW 1079 SAL - C7 - MAJOR REPAIR - NR 6129685 - GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, Y1732. REPAIRED SHEAR PL ATE BETWEEN FR69 TO FR70, Y1732 A320 SRM 51-42-11 & 51-72-11. 2 L 7 2 4F RT A28NM 20090106 EU 2009 1 6 USAA2009010590020 1 20081219 A 5347 D57130147202 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656AW 1079 SAL - C7 - MAJOR REPAIR - NR 6072793 - CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, -Y1292 AT 4 LOCATIONS. REPLACED SEA T TRACK BETWEEN FR36 TO FR41, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20090106 NM 2009 1 6 USAABB08177 1 20081228 A 3350 BATTERY BOEING 767 7672B7 1385107 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 252AU 24765 PHL - THE FLIGHT DECK EMERGENCY ESCAPE LIGHT ABOVE THE COCKPIT DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES ON THE EMERGENCY ESCAPE LIGHT MODULE. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A1NM 20090106 EU 2009 1 6 USAA2008123192363 1 20081230 A 3350 32145510 POWER SUPPLY AIRBUS A321 A321211 3930370 EU CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 190UW 26833 3732 1436 LOGPAGE: 4387073 - FLT 1151 - PHX-LAX - EEL - FORWARD EMERGENCY DOOR EXIT EMERGENCY POWER SUPPLY UNIT (14WL, 15WL) FAUL TING. REMOVED AND REPLACE EMERGENCY POWER SUPPLY UNIT (14WL, 15WL). OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20090106 2009 1 6 FDEA200812305319 4 20081230 A 2230 AUTOTHROTTLE SYS AIRBUS 300 A300B4622 3930401 EU MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 21 718FD 365 ON TAKEOFF ROLL (20 KTS AIRSPEED). PERFORMED RTO CHECKLIST IA QRH. MEL NON FLAGGED ITEM 22-30-01-C AUTO THROTTLE SYS RES ET IN FLIGHT, WORKED FINE. PERFORMED AUTOTHROTTLE ADJUSTMENT AND TEST IAW AMM 22-30-00-5-02 ITEM "B". TEST PASSED SATI SFACTORY ON GND. INTERROGATED AFS COMPUTER AND NO FAULTS RECORDED. NO HISTORY PER ATS DURING THE LAST 90 DAYS. OK FOR SV C. A/C DOWNGRADED TO CAT2 , NR 1 AND NR 2 AP'S CHECK 3A. (NO PARTS REMOVED OR REPLACED, BITE CK OK. 6 GOOD LEGS) 2 L 7 2 4F RT A35EU 20090106 EU 2009 1 6 USAA2008123192364 1 20081230 A 3350 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A USAA K NONE L NO TEST UK UNKNOWN 1 EA 19 672AW 2193 LOGPAGE: 8316389 - FLT 323 - GDL-PHX - EEL - AFT GALLEY FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED A FT GALLEY FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20090106 EU 2009 1 6 USAA2008123192356 1 20081230 A 5320 D5347112420100 SHEAR PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656AW 1079 SAL - C7 - MAJOR REPAIR - NR 6129693 - GALVANIC CORROSION ON SHEAR PLATE BTW FR69 TO FR70, -Y1732. REPLACED SHEAR PLATE BTW FR69 TO FR70, -Y1732 IAW A320 SRM 51-72-11 & 51-42-11. 2 L 7 2 4F RT A28NM 20090106 2009 1 6 A6WA200840640 4 20081211 A 2210 AUTOPILOT SYS CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A A6WA K NONE N FALSE WARNING TO TAKEOFF 1 GL 31 409AW 7447 AFTER TAKEOFF FROM WET RUNWAY, CLIMBED TO FL320 IN RAIN/SNOW. TEMP -48`C IN CRUISE. WHILE MAKING LT TURN, WITH AP, REC EIVED LT WING DOWN AUTOPILOT TRIM CAUTION MSG MOMENTARILY. PERFORMED VISUAL INSP AILERON SYS FROM BULKHEAD TO AILERONS WHILE OPERATING THE SYS. FOUND NO OBSTRUCTION. ALL PULLEYS AND QUADRANTS, OPS NORMAL. INSP FLUTTER. 2 L 7 2 4F RT A21EA 20090106 SO 2009 1 6 C2XA08SH163 1 20081219 A 5320 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 48901 145501 CENTER OMEGA BEAM HAS CORROSION IN RADIUS AT FR 20. CENTER OMEGA BEAM WAS REPAIRED IAW SRM 53-21-10. THE ACFT WAS APPR OVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20090106 GL 2009 1 6 C2XA08CL139 2 20081230 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL NR 2 MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13538 13130 470 145527 CAE311494 IAH FLT THE CREW REPORTED A LAV SMOKE MESSAGE ON THE ECIAS AFTER TAKEOFF AT 3000FT. THE MESSAGE CLEARED AFTER THE CB E11 AND 12 WERE PULLED. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX REPLACED THE NR 2 ENG AND OPS CHEC KS WERE GOOD. SUPPLEMENT TO FOLLOW. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20090106 SO 2009 1 6 C2XA09IA002 1 20081228 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY MALFUNCTIONED A C2XA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 27 13538 14110 14110 145527 THE CREW REPORTED A LAV SMOKE INDICATION RIGHT AFTER ROTATION. THE ACFT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE LAV SMOKE SENSOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081208 NM 2008 12 8 SWAA086843 1 20081204 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM UPPER CAP CORROED AT BS 986, LBL 5. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086848 1 20081204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086851 1 20081204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 21L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086853 1 20081204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 8R. REPAIRED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081208 SO 2008 12 8 SIMA200833801 1 20081128 A 2150 A/C PACK EMB 145 EMB145LR 3260212 SO NR 2 SMOKE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 645AE 145212 ON FLIGHT 3488, CREW REPORTED WITH APU RUNNING AND NR 2 PACK OPERATING SMOKE IN CABIN AND PACK 2 OVERHEAT. MEL ISSUED 2 L 7 2 4T RT T00011AT 20081208 NM 2008 12 8 DL757081632 1 20081118 A 5347 FITTING BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 CORROSION ON AFT CARGO TIE DOWN FITTING, BS 1437, RBL 25, WL 147 AT DOOR CUT OUT, NO ALLOWABLE LIMITS. REMOVED AND REPL ACED FITTING PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081208 2008 12 8 UALA2008120306739 4 20081201 A 3140 9670205001 COMPUTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 597UA 28750 ACMS SYSTEM FAULTY. ACCMP FLIGHT DATA ACQUISITION MGMT UNIT SOFTWARE UPLOAD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081208 NM 2008 12 8 UALA2008120306740 1 20081203 A 2913 731966 PUMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HYDRAULIC SYS FAULTY A UALA O OTHER J WARNING INDICATION UK UNKNOWN 1 WP 29 663UA 27160 EICAS "C HYD PRIM 1" DISPLAYED. REPLACED NR 1 ACMP AND CONNECTOR D482. CASE AND DRAIN FILTERS REPLACED. ALL CHECKS OK AY. NO FAULTS NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081208 NM 2008 12 8 UALA2008120306729 1 20081201 A 3233 293W23022 ACTUATOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NLG FAULTY A UALA O OTHER W INADEQUATE Q C CL CLIMB 1 WP 29 206UA 30212 LANDING GEAR - DOES NOT RETRACT WHEN LANDING GEAR LEVER MOVED TO UP POSITION. CREW COMMENTS: NOSE GEAR EXTREMELY SLOW RETRACTION. NLG DOOR EICAS DISPLAYED BRIEFLY, CHRONIC. REPLACED NLG EXTENSION AND RETRACTION ACTUATOR. ACCOMPLISHED N LG EXTENSION AND RETRACTION. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081208 NM 2008 12 8 UALA2008120306730 1 20081202 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 228UA 30556 EMERGENCY LIGHT AT 19C INOP. REPLACED LAMP. OP CHECKED OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081208 NM 2008 12 8 UALA2008120306733 1 20081202 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 FWD PIT FRAME DENTED AT BS 620 AND STR 24L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SECTION OF FLANGE AND FABRICATE D A REPAIR ANGLE AND INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081208 EU 2008 12 8 UALA2008120306738 1 20081203 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 405UA 452 BEAM 165 HAS 2EA HOLE CORRODED. REMOVED BEAM 165 AND TRANSFERRED BRACKETS TO NEW BEAM. JOINED BEAM BS 200 TO 165. INS TALLED BEAM 165 IN ACFT. 2 L 7 2 4F 4 F RT A28NM E40NE 20081208 NM 2008 12 8 UALA2008120406742 1 20081203 A 3320 81841 BALLAST BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 544UA 25322 INOP OVERWING LT EXIT LIGHT (INTERIOR). REPLACED BALLAST. 2 L 7 2 4F 4 F RT A2NM E17NE 20081208 NM 2008 12 8 UALA2008120406743 1 20081203 A 5240 F1314 SPRING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SERVICE DOOR WEAK A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 RT AFT SERVICE DOOR DEPLOYMENT BAR GAS SPRING WEAK. REPLACED GAS SPRINGS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081208 EA 2008 12 8 ASOA200801558 1 20081123 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 713EV 10081 EMERGENCY BATTERY NR 1 PACK WIRES PULLED OUT OF CR124. REMOVED AND REPLACED NR 1 BATTERY PACK DIODE PACK CR124. COMPLI ED WITH OPS TEST OF EMERGENCY LIGHT SYSTEM IAW AMM 33-51-00-710-80, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 20081208 NM 2008 12 8 UALA2008120406748 1 20081203 A 5420 BUSHING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 NR 2 ENGINE, FWD SECTION OF DIAGONAL BRACE, OUTBOARD LUG BUSHING HAS MIGRATED OUT. REPLACED INNER AND OUTER BUSHINGS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081208 NE 2008 12 8 UALA2008120406752 2 20081204 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 HOT START A UALA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 29 655UA 25393 NR 1 ENG HOT START, MAX EGT 768. (EXCEEDS 535). SEE EICAS ENG EXCD FOR MAX EGT AND DURATION. CREW COMMENTS: NO FUEL I NITIATED DURING START. INSPECTED ENGINE INLET AND EXHAUST. RAN ENGINE IN GATE START WAS NORMAL. CREW STATED IT HAD EG T INDICATION ON PUSHBACK BEFORE ATTEMPTING TO START. 2 L 7 2 4F 4 F RT A1NM E24NE 20081208 NM 2008 12 8 UALA2008120206727 1 20081201 A 5610 141T4835504 WINDOW BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE COCKPIT CRACKED A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 670UA 29240 CREW COMMENTS: F/O SLIDING WINDOW HAS LOUD SQUEAL. FOUND DIAGONAL CRACK ACROSS THE WIDTH OF F/O 'S SLIDING WINDOW. RE PLACED F/O'S SLIDING WINDOW REPLACED DAMAGED CONNECTOR D5848P BEHIND P61 PANEL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081208 NM 2008 12 8 DXTA2008120103377 1 20081128 A 3260 WARNING LIGHT GULSTM 200 200 4500308 NM COCKPIT ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 730QS 120 AFTER TAKEOFF, AFTER GEAR LEVER MOVED TO "UP" LT INDICATED AMBER IN TRANSIT LIGHT ON, 2 L 7 2 4F RT A53NM 20081208 SO 2008 12 8 SIMA200834301 1 20081203 A 3246 31641 WHEEL EMB 145 EMB145LR 3260212 SO MLG SEPARATED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 698CB 14500877 ON FLIGHT 3992 AFTER TAKEOFF DURING GEAR RETRACTION CREW RECEIVED A L/G DISAGREE AND RIGHT L/G RED. CREW RAN CHECKLIST AND NOTED NORMAL ONLY WHEN GEAR DOWN. CREW RETURNED FOR LANDING AND WAS ADVISED BY CONTROL TOWER THAT THE NR 3 TIRE WAS BLOWN. AFTER LANDING CREW RECEIVED L/G AIR/GND FAIL, BRAKE DISAGREE, PITOT 3 INOP, E1/2 IDLE STOP FAIL MESSAGES. ALSO WASN’T ABLE TO PUT GUST LOCK ON. A/C TOWED TO GATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 3 WHEEL/T IRE ASSEMBLY, RT GEAR BRAKE TEMP HARNESS, WOW HARNESS REPLACED SEVERAL HARNESS CLAMPS, RT MLG WHEEL SPEED TRANSDUCER HAR NESS, NUMBER 3 BRAKE LINES. RETRACTION CHECK COMPLETED. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081208 NM 2008 12 8 UALA2008120106699 1 20081129 A 4900 32908145 VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU DEFECTIVE A UALA D E RETURN TO BLOCK ENGINE SHUTDOWN W INADEQUATE Q C IN INSP/MAINT 1 WP 29 772UA 26930 777025 CREW REPORTS: FLIGHT ATTENDANT REPORTED ABNORMAL SOUND FROM ENG 1 DURING START, CREW SHUTDOWN ENG, RESTART WITH SAME RE SULTS, NO REPORT OF ANY ABNORMAL ENG PARAMETERS OR EICAS MESSAGES, ENGINE WAS RUN AT 50% N1 WITH ALL PARAMETERS NORMAL. ACCOMPLISH CHECKS WITH NO DEFECTS FOUND. T-S AND FOUND APU SURGE VLV BAD. REPLACED VALVE AND DID SEVERAL ENGINE START S, ALL NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081208 NM 2008 12 8 USAA920082082 1 20081116 A 5312 BULKHEAD BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 24893 PIT FPBH MAJOR REPAIR NR 4335082 5 CRACKS IN BEAM WEB AT BS178, BETWEEN WL225 TO 234 RBL17. CRACKS MEASURE 0.125, 0.250 , 0.50, 0.750 AND 0.250 INCHES IN LENGTH. REPAIRED BEAM WEB AT BS178, BETWEEN WL225 TO 234 RBL17 IAW B737 SRM 53-10-08. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 F3LA200800652 1 20080930 A 5330 D53476410202 SKIN PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 REFERENCE NON ROUTINE 2008-196216. DURING C4/S1 C CHECK, INSPECTION NOTED DENT ON FUSELAGE SKIN AT FRAME 63 + 9 INCHES AND LT STRINGER 43 + 1 INCH. MX REPAIRED DENT ON EXTERNAL SKIN AT FRAME 63 + 9 INCHES BETWEEN LT STRINGER 41 AND RT STR INGER 43, IAW THE REQUIREMENTS OF A319 SRM 53-00-11, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FO UND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081208 EA 2008 12 8 A6WA200840612 1 20081120 A 3230 UPLOCK CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 436AW 7734 ON DEPARTURE AFTER SELECTING GEAR UP GEAR DISAGREE AND NOSE DOOR WARNING AURAL AND EICAS WARNING MSGS. BOTH MAINS SHOWE D CROSS HASH AND NOSE GEAR SHOWED UP. C/W QRH. ALL 3 GEAR SHOWED DOWN AND GREEN, PERFORMED NORMAL LANDING. TROUBLESHO T AND FOUND PSEU TO FLAG THE LT NOSE DOOR AND NLG UPLOCK. SWUNG LG AND NLG WILL FREE FALL BY ITSELF. R&R NLG UPLOCK AS SY PER AMM 32-30 LEAK AND OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 A6WA200840613 1 20081121 A 3222 BUSHING CNDAIR CL600 CL6002B19 1900309 EA NLG TORQUE LINK OUT OF LIMITS A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 436AW 7734 AFTER TAKEOFF RECEIVED GEAR DISAGREE LT MAIN AND RT MAIN SHOWED HATCHES AND NOSE GEAR SHOWED UP. RESELECTED GEAR DOWN. LANDED NORMAL. FOUND LOWER NOSE TORQUE LINK BUSHING OUT OF LIMITS AT OPS POINT. R&R NOSE TORQUE LINK IAW AMM 32-21-10 , FUNCTION CHECK OF EXTENSION AND RETRACTION OF LANDING GEAR 12 TIMES GOOD. 2 L 7 2 4F RT A21EA 20081208 NM 2008 12 8 USAA920082079 1 20081116 A 5311 65C25229 FRAME BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT Q2 MAJOR REPAIR NR 03C10753039/004 FRAME CRACKED AT PSU RAIL ATTACH POINT AT BS727D, BETWEEN S8L AND S9L. REPAIRED FRAME AT PSU RAIL ATTACH POINT AT BS727D, BETWEEN S8L AND S9L IAW US AIRWAYS TYPICAL REPAIR NR 53-10-20E. 2 L 7 2 4F RT A16WE 20081208 EU 2008 12 8 UALA2008120106683 1 20081126 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 448UA 842 AFT LOWER FUSELAGE FR70 TO FR72 HAS TAIL STRIKE DAMAGE TO EXTERNAL SKIN BETWEEN STR 42R TO STR 41L. MAJOR REPAIR ACCOMP LISHED. CUT OUT DAMAGED SECTION OF SKIN. FABRICATED & INSTALLED EXTERNAL DOUBLER. 2 L 7 2 4F 4 F RT A28NM E40NE 20081208 2008 12 8 UALA2008120106684 4 20081126 A 2565 CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 554UA 26644 LT OFF WING BACK UP CABLE DIMENSION FROM SUPPORT SHROUD TO THE BACK UP CABLE THREADS FOUND OUT OF LIMITS. ADJUSTED THE SUPPORT SHROUD TO CABLE BACK UP CABLE THREAD DIMENSION NOW AT .060. 2 L 7 2 4F 4 F RT A2NM E17NE 20081209 NM 2008 12 9 UALA2008111304348 1 20080819 A 2611 SMOKE DETECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE E&E BAY FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 DET CHAN 2 E-E SMOKE ELECTRICAL EQUIPMENT (E-E) COOLING SMOKE DETECTOR CHANNEL 2 FAILS BITE CHECK. STATUS MSG01- ACTIV E CRUISE HARD; E-E COOLING SMOKE DETECTOR HAS NO OUTPUT OR IS FAILED. DB- CARGO SMOKE DETECTOR CH 2 (LWR FWD) MSG02- AC TIVE, CRUISE HARD; E-E COOLING SMOKE DETECTOR HAS NO OUTPUT OR IS FAILED. MSG-2620070 ACTIVE ER HARD, MSG-2620070 ACTIV E ER HARD. *S/D* REPLACED EE COOLING SMOKE DETECTOR. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081208 NM 2008 12 8 FDEA200812015028 1 20081201 A 5322 6516314111 SHEAR TIE BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 495FE 21669 NLG W/W WEB AT STA 312 UPPER SECTION OF SHEAR TIE WEB IS CORRODED AT LBL 22. CUT OUT DAMAGE AREA DIM: 5 1/2 BY 4 AND RE PAIRED NLG W/W WEB AT STA 312 SHEAR TIE LBL 22 IAW B727 SRM 53-10-4 FIG 11 AND 53-10-2 FIG 1. 2 L 7 3 4F A3WE 20081208 EA 2008 12 8 COMA2008120150014 1 20081130 A 3020 5399001 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 1900309 EA ZONE 400 FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 455CA 4482 7592 ON CLIMB-OUT FROM CVG, RECEIVED LEFT COWL A/I CAUTION MSG. A/C RETURNED BACK TO CVG, LANDED SAFELY. REMOVED AND REPLAC ED LEFT COWL A/I VALVE. 2 L 7 2 4F RT A21EA 20081208 NM 2008 12 8 HALA2008112200868 1 20081122 A 4920 38002981 APU BOEING 767 76733A 1385209 NM SHUTDOWN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, APU AUTOSHUTDOWN AT GATE. REMOVED AND REPLACED APU PER HAL M266-767. 2 L 7 2 4F RT A1NM 20081208 NM 2008 12 8 SWAA086816 1 20081203 A 3350 100031 LIGHT BOEING 737 737317 138447P NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 17. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086819 1 20081203 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 727C, STR 10R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086760 1 20081202 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086827 1 20081204 A 5753 654643490 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED HC2 CHECK, FOUND RT WING I/B AFT FLAP O/B FWD EDGE DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086784 1 20081203 A 5511 6573782 SPAR BOEING 737 737317 138447P NM HORIZ STAB DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND LT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD DELAMINATED AT BS 165. REMOVED AND REP LACED STABILIZER PER MM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086785 1 20081203 A 5330 6545765 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 518, STR 28L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086790 1 20081203 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086796 1 20081203 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086797 1 20081203 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086854 1 20081204 A 5311 6546804 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 294, BETWEEN STR 2R TO STR 3R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 UALA2008120306731 1 20081202 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 AFT PIT AT STA 1480, STR 26L FRAME DENTED AT INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SECTION OF FLA NGE AND FABRICATED A J-ANGLE REPAIR AND INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081208 NE 2008 12 8 UALA2008120306741 2 20081203 A 7314 825500 PUMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE LEAKING A UALA O OTHER W K INADEQUATE Q C FLUID LOSS CR CRUISE 1 WP 29 643UA 25093 NR 1 ENG FUEL PUMP LEAKING AT INLET TUBE FLANGE. ACCOMPLISHED NR 1 ENG FUEL PUMP REPLACEMENT. NOW HAVE A FUEL LEAK FRO M THE DRIVE FLANGE WILL NEED TO PULL PUMP AND RESEAL. REPLACED O-RING SEAL. RUN CHECKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081208 NM 2008 12 8 UALA2008120406751 1 20081203 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 552UA 26641 L-2 DOOR REQUIRES DOUBLER REPAIR AT UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED A REPAIR D OUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 20081208 NM 2008 12 8 UALA2008120206722 1 20081202 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT LIGHTS INOP ALL OF FIRST CLASS CEILING. REPLACED BATTERY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081208 EA 2008 12 8 A6WA200840615 1 20081122 A 3234 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 408AW 7568 LOG 197305/3 AFTER TAKEOFF LANDING GEAR DID NOT COME UP WHEN SELECTED UP. LANDING GEAR LIGHT REMAINED GREEN. ALSO GOT INBD ANTI-SKID CAUTION AND PARKING BRAKE SHUT OFF VALVE CAUTION. CLEARED WHEN GEAR SELECTED DOWN. INTERROGATED PSEU AN D FOUND DI 11 OFF FAULT CODE. R&R LANDING GEAR CONTROL HANDLE IAW AMM 32-31-01. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 20081209 NM 2008 12 9 UALA2008112506668 1 20081125 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE SEAT 3F INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 794UA 26953 SEAT 3F, AFT EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081209 NM 2008 12 9 UALA2008112506670 1 20081123 A 3610 79027013 VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT ENGINE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 665UA 29237 LEFT ENG HPSOV ON MOMENTARILY DURING DESCENT. PER FLT CREW, CAME ON WHEN PWR PULLED TO IDLE FOR DESCENT AND EXTINGUISHE D AFTER APPROX 1 MIN. FOUND HPSOV BAD ON HEALTH CHECK. REPLACED HPSOV. OPS AND LEAK CHECK OKAY. NO FAULTS OR MESSAGE S. 2 L 7 2 4F 4 F RT A1NM E24NE 20081209 NE 2008 12 9 UALA2008111406507 2 20081113 A 7261 810E102 SCAVENGE PUMP BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 ENGINE FAULTY A UALA O OTHER W K INADEQUATE Q C FLUID LOSS IN INSP/MAINT 1 WP 29 217UA 30550 RIGHT ENG TOOK 10 QUARTS OF OIL ON ARRIVAL. BORO'D NR 3 WEEP TUBE FOUND CLN, NO OIL. HOC ON RIGHT ENG. REPLACED SCAVE NGE PUMP. REPLENISHED OIL TANK TO FULL. ACCOMPLISHED ENGINE RUN. ENGINE OIL PRESSURE WITHIN LIMITS. NO LEAKS NOTED O N ENG RUN. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081209 2008 12 9 UALA2008111406509 4 20081114 A 2310 490S1 COUPLER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HF COMM FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 663UA 27160 HF INTERFERENCE FAULTS. REPLACED LT & RT COUPLER. OPS CHECKED. NO FAULTS. REPLACED LT TRANSCEIVER. 2 L 7 2 4F 4 F RT A1NM E24NE 20090106 NM 2009 1 6 USAASB08129 1 20081231 A 3397 SPLICE BOEING 737 7374B7 138449C NM CABIN DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 430US 24552 ORD MAINTENANCE REPORTED THE EMERGENCY EXIT PATH LIGHT AT ROW 19, LEFT-HAND SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BAD SPLICE AT ROW 19, LEFT-HAND SIDE, PER SWPM 20-30-12. OPERATIONAL CHECK GOOD PER MM 33-51-12. 2 L 7 2 4F RT A16WE 20090106 EU 2009 1 6 USAA2008123192359 1 20081224 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 633AW 58143 13868 82 LOGPAGE: 4407906 - FLT 350 - PHX-LAS - EEL - FORWARD CABIN EMERGENCY LIGHTS WILL NOT COME ON DURING TEST. REMOVED AND R EPLACED FORWARD EMERGENCY LIGHT POWER SUPPLY UNIT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20090106 EU 2009 1 6 USAA2008123192361 1 20081227 A 2560 FLASHLIGHT AIRBUS 320 A320232 3930326 EU COCKPIT MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 657AW 1083 LOGPAGE: 8355428 - FLT 371 - CLT-PHX - EEL - FLIGHT ATTENDANT DIRECT VIEW JUMPSEAT FLASHLIGHT INOPERATIVE. MAINTENANCE CHECKED FLASHLIGHT CHARGE AND ILLUMINATION AND FOUND OPERATIONAL WITH NO DEFECTS. 2 L 7 2 4F RT A28NM 20090106 NM 2009 1 6 FDEA200812245289 1 20081224 A 2797 WIRE HARNESS BOEING 727 727277 138408S NM TE FLAPS BURNED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 CE 21 245FE 22016 DURING CLIMB THROUGH 6,000 FT EXPERIENCED A PWR SURGE AND FOUND THE ALTERNATE FLAP MOTOR CIRCUIT BREAKERS (INBD AND OTBD ) HAD POPPED. FOUND BURNED WIRE BUNDLE IN E&E COMPARTMENT, STILL TROUBLESHOOTING. 2 L 7 3 4F RT A3WE 20090106 NM 2009 1 6 FDEA200812245290 1 20081224 A 5320 6517510120 WEB BOEING 727 727233 138408A NM BS 1218-1220 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 AFT AIRSTAIR, RT LWR TORQUE BOX INBD VERTICAL WEB IS CRACKED AT 02 PLACES AT LIGHTING HOLE STA 1218. REMOVED AFT AIRSTAI RS FLOOR PANEL AND ANGLE FOR ACCESS IAW SRM 51-30-2. CUTOUT DAMAGED AREA IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR PARTS FROM 2024T3, 0.032 INCH IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS AND AND ANGLE AND FLOOR PANEL IAW SRM 51-30-2 AT AFT AIRSTAIRS RT LWR TORQUE BOX INBD VERT WEB. 2 L 7 3 4F RT A3WE 20090106 NM 2009 1 6 2009F00003 1 20081231 A 3240 511531 HOUSING BOEING 737 737* NM BRAKE SYS CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 WP 01 3780 HOUSING FOUND CRACKED IN MOUNTING LUG DURING SHOP VISIT. 2 L 7 2 4F RT A16WE 20090106 WP 2009 1 6 15HA0858014 1 20081219 A 6123 6873725012 O-RING CVAC 580 580 2422806 WP ALLSN 501D 501D13 03004 GL ALLSN A6441 A6441FN606 GL AUTOFEATHER SYS LEAKING A I5HA C ABORTED TAKEOFF K FLUID LOSS TO TAKEOFF 1 GL 25 581P 29 501319 HC95 DURING THE TAKEOFF ROLL DEPARTING, ENROUTE, THE NR ONE ENG AUTO-FEATHERED. THE CREW ABORTED THE TAKEOFF AND RETURNED TO BASE. MX PERSONNEL OBSERVED A LARGE AMOUNT OF OIL AROUND THE FRONT OF THE PROPELLER. FURTHER INSP REVEALED A FAILED O ’RING BENEATH THE FEATHER RESERVOIR CAUSING A MASSIVE OIL LEAK RESULTING IN THE AUTO-FEATHER. THE O’RING WAS REPLACED A ND THE ENGINE OPERATED BY MX WITH NO LEAKS OBSERVED. THE ACFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT E282 6 C P898 20090106 WP 2009 1 6 I5HA0858015 1 20081226 A 5730 3401610003807 SKIN CVAC 580 580 2422806 WP LT WING DAMAGED A I5HA K NONE E VIBRATION/BUFFET CL CLIMB 1 GL 25 588X 52 DURING CLIMB OUT, EN-ROUTE, THE CREW FELT A "THUMP" POSSIBLY FROM THE LT WING. THE CREW COULD NOT SEE ANY DAMAGE AND DI D NOT EXPERIENCE ANY CONTROL PROBLEMS. THE CREW CONTINUED THEIR FLIGHT AND LANDED UNEVENTFULLY. EXAMINATION BY THE CRE W OF THE LT WING REVEALED A HOLE IN THE LT NR 3 L/E CONSISTENT WITH A BIRD STRIKE. AREA OF DAMAGE WAS APPROXIMATELY 20 INCHES ACROSS AND 6 TO 8 INCHES IN HEIGHT. A MX CREW WAS FLOWN TO ACFT LOCATION WITH A REPLACEMENT L/E. THE DAMAGED L/ E WAS REMOVED AND THE AREA INSPECTED. NO OTHER DAMAGE WAS DISCOVERED. THE REPLACEMENT L/E WAS INSTALLED AND THE ACFT R ETURNED TO SERVICE. 2 L 7 2 4T RT 20090106 EA 2009 1 6 A6WA200840643 1 20081203 A 5210 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 414ZW 7586 CRACK FOUND ON PAX DOOR MOTOR ASSIST STIFFENER AFT WEB. PAX DOOR MOTOR ASSIST STIFFENER AFT WEB REPLACED IAW SRM 51-42 -06 AND 51-42-13. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 A6WA200840644 1 20081211 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 415AW 7593 MWC 17. FS 621 PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING IS CRACKED. PERFORMED A REPAIR BY CU TTING OUT SECTION OF WEB, FABRICATING, INSTALLING REPAIR PARTS IAW REO 601R-53-61-1230 REV D. 2 L 7 2 4F RT A21EA 20090106 NM 2009 1 6 AALA200810551 1 20081219 A 5320 ANGLE BOEING 737 737823 13844CB NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 RT TRANSITION ANGLE CRACKED AT STA 432. INSTALLED A SERVICEABLE ANGLE IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20090106 SO 2009 1 6 C2XA08SH165 1 20081229 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145EP 3260221 SO NLG DEFECTIVE A C2XA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 27 14947 145054 ON DEPARTURE OUT, NLG WOULD NOT RETRACT. REMOVED AND REPLACED NLG UPLOCK PROXIMITY SWITCH IAW EMB 145 32-63-03. THE AC FT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20090106 NM 2009 1 6 C8GA20080066 1 20081013 A 5313 BAC1498131 STRINGER BOEING 727 727223 1384074 NM PWA JT8 JT8D NE FUSELAGE CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT RIVETS WERE PULLING THROUGH THE SKIN EXTERIOR AT BS 1010 STR 28R. CO RROSION ON STR 28R TO BE OUT OF LIMITS. CUT OUT DAMAGED STR 28R AT B.S 1010 TO + 11.375. FABRICATED NEW STRINGER REPAIR SPLICE FROM BAC 1498-131 7075 T6 (12 INCHES), BAC 1498-147 .090 INCH 7075 T6 (11.375 INCHES). INSTALLED STRINGER REPAIR IAW 53-10-3, 53-10-2 AND 51-10-2. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 20090106 NM 2009 1 6 C8GA20080067 1 20081105 A 5313 65564418 STRINGER BOEING 727 727223 1384074 NM PWA JT8 JT8D NE FUSELAGE CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT STRINGER 29R WAS CORRODED UNDER BS 950E FRAME EXTENDING TO BS 1000. CORROSION AT STR. 29R WAS OUT OF LIMITS. CUT OUT DAMAGED STR 29R AT BS 950 TO 1006. INSTALLED NEW STRINGER P/N 65-56441- 8. WORK PERFORMED IAW SB 727-53-0179. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 20090106 2009 1 6 CEDAN217CA121708 4 20081216 A 3422 25883023 GYRO AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE E&E BAY FAILED E CEDA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 SW 05 217CA 075 245G418 AFTER TAKEOFF, ENROUTE, DIRECTIONAL GYRO FAILED. PILOT ELECTED TO DIVERT DUE TO WEATHER CONDITIONS. 2 L 7 2 4F 4 F RT A7EU E7EA 20081209 NM 2008 12 9 UALA2008112506666 1 20081125 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 794UA 26953 SEAT 2F, AFT EEL LIGHT INOP. REPLACED EEL LAMP ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081209 CE 2008 12 9 GUUA9353212080801 1 20081208 A 3260 WARNING SYSTEM BEECH 1900 1900D 1154162 CE COCKPIT ACTIVATED A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 81535 UE147 FLIGHT 9290 - DUJ/FKL - DURING APPROACH SELECTED LANDING GEAR DOWN, NO GEAR INDICATION. RETURNED TO DUJ, MANUALLY PUMPE D LANDING GEAR DOWN GOT TWO GREEN MAIN GEAR LOCKED ANNUNCIATOR. NO NOSE GEAR ILLUMINATED ON LANDING, SHUT DOWN AND FEAT HERED BOTH ENGINES. CORRECTIVE ACTION: OPEN 2 L 7 2 4T RT A24CE 20081209 NM 2008 12 9 FDEA200812045085 1 20081204 A 5340 6519606253 SUPPORT BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 MAIN DECK BULKHEAD SUPPORT CORRODED AT AFT BULKHEAD FITTING STA 1183 LBL 18, WL 208. REMOVED CORROSION, OUT OF LIMITS . 018 MATERIAL REMOVED, ORIGINAL MATERIAL .063, .045 REMAINING. INSTALLED DOUBLER AND SPLICED FLOOR SUPPORT REF SRM 51-40 -3 PG 1, DWR 65-31774. THIS IS CLASSIFIED AS A MAJOR REPAIR. TREATED AND PRIMED REPAIR SPLICE AND DOUBLER REF SRM 51-1 0-2. 2 L 7 3 4F A3WE 20081209 EA 2008 12 9 SWIA200820577 1 20081004 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 466SW 7856 C-CHECK, FS 280 FLOORBEAM RBL9 LOWER SUPPORT RADIUS CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081209 SO 2008 12 9 C2XA08CL127 1 20081204 A 2150 M835366022M RELAY EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 12552 145583 CLE - FLIGHT 2006 - THE CREW REPORTED A WING ANTI-ICE AND A PACK 1 VALVE FAIL MESSAGE ON THE EICAS DURING CLIMBOUT. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 PACK VALVE AND RELAY KO187. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20081209 NM 2008 12 9 YENA200812020124 1 20081130 A 2913 5116403 PUMP EMB ERJ190 ERJ190100IGW 3260408 NM NR 2 ENGINE LEAKING A YENA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 15 247JB 4056 339 190000042 FLT 1419, BOS-JAX - AIR TURNBACK, HYD 2 LO QTY. REMOVED AND REPLACED NR 2 ENG DRIVEN PUMP IAW AMM 29-11-01. REMOVED AN D REPLACED HYD FILTERS, LEAK CHECK OK. 2 L 7 2 4F RT A57NM 20081209 NM 2008 12 9 YENA200812020125 1 20081126 A 2797 W51219106685401 WIRE HARNESS EMB ERJ190 ERJ190100IGW 3260408 NM LE SLAT DEFECTIVE A YENA B EMER. DESCENT F FLT CONT AFFECTED AP APPROACH 1 EA 15 265JB 6176 190000049 FLT 662, MCO-BUF, ON APPROACH SLAT FAIL WHEN EXTENDING FROM FLAPS 3 TO 5. TS PER FIM 27-81-00-810-805. FOUND DEFECTIVE HARNESS W512. REMOVED AND REPLACED LEFT SLAT HARNESS W512 191-06685-401 IAW E190 MM 27-83-07, OPS CHECK GOOD. 2 L 7 2 4F RT A57NM 20081209 NM 2008 12 9 HNAA2008111300336 1 20081113 A 3320 BR63031023 FIXTURE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A HNAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 07 908HA 59474 59474 015 DURING DESCENT FROM 24000 FEET, THE FLIGHT ATTENDANTS NOTICED A BURNING ODOR IN THE CABIN BUT NO VISIBLE SMOKE. UPON LA NDING, MAINTENANCE DEACTIVATED THE CABIN INTERIOR NORMAL LIGHTING SYSTEM, REMOVED THE BULB AND PLACED THE SYSTEM ON THE MEL LIST FOR THIS AIRCRAFT. A HIDDEN DAMAGE INSPECTION WAS PERFORMED AND FOUND THAT THE RIGHT HAND ROW 1 LIGHT FIXTURE WAS LOOSE. FURTHER INVESTIGATION FOUND THE LIGHT FIXTURE RECEPTACLE TO BE BROKEN AND BURNT. THE FIXTURE WAS REPLACED A LONG WITH THE LIGHTING BALLAST. SYSTEM WAS THEN RE-ACTIVATED AND OPS CHECKS WERE GOOD. THE SYSTEM MEL WAS CLEARED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 20081209 EU 2008 12 9 YENA200812020122 1 20081128 A 3350 321431 BATTERY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 639JB 1613 2814 EMERGENCY LIGHT TEST FAILED. "LEFT EPSU" ON WEEKLY CHECK. REMOVED AND REPLACED LEFT EPSU BATTERY (11W) IAW TSM 33-51-00 -810-808. OPS TEST OF EMERGENCY LIGHT SYS OK. 2 L 7 2 4F RT A28NM 20081209 WP 2008 12 9 UPS08854045 1 20081023 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQ 803-F1-139 F/S 558, L25L-L26L HAS NO SRM REFERENCE, & NEEDS APPX F OF EO DC8-5100-30418C. REMOVED EXISTING REPAIR, FABBED & INSTALLED DOUBLER SHT7075T6 .090 REF DWG5779913, 2779655, SRM 53-2-1 FIG 7 SHT 13, 51 -1-8, 51-1-26, 51-1-20D, SAA ENG 81427390001. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 AALA200810272 1 20081110 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 PUNCTURED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CUSP HAS PUNCTURED HOLE AT BS 1097 RIGHT UNDER SEAT TRACK NR 6. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081209 WP 2008 12 9 AALA200810287 1 20081117 A 5330 DOUBLER DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION UNDER LEFT STATIC PORT PLATE DOUBLER RING. INSTALLED DOUBLER AND LEFT PRIMARY STATIC PORT PLATE. 2 L 7 2 4F RT A6WE 20081209 NM 2008 12 9 AALA200820055 1 20081107 A 5347 CBE12641 CARGO TRACK BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 666A 52891 25300 AFT GALLEY FORWARD RT TIE DOWN CORRODED, REPAIRED IAW SRM 53-60-51-2R. 2 L 7 2 4F RT A2NM 20081209 WP 2008 12 9 AALA200810282 1 20081114 A 5322 SHEAR TIE DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 SHEAR TIE CRACKED. INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F RT A6WE 20081209 WP 2008 12 9 UPS08854054 1 20081106 A 5720 DOUBLER DOUG DC8 DC871F 302199D WP RT WING MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV RT WING XW388 DOUBLER DOES NOT CONFORM TO SRM. REPLACED DOUBLER 57-02- 00 FIG 2A SHEET 1. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854055 1 20081028 A 5512 DOUBLER DOUG DC8 DC871F 302199D WP HORIZ STAB DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV LT HORIZ STAB L/E HAS DOUBLER UNABLE TO VALIDATE PER SRM. INSTALLED NEW DOUBLER AS PER 55-2-1 FIG 4. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854056 1 20081108 A 5510 DOUBLER DOUG DC8 DC871F 302199D WP STABILIZER UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV RT STAB XFS 66.25 EXTERNAL REPAIR UNABLE TO VALIDATE PER SRM. REPLACED DOUBLER IAW 55-02-01. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854057 1 20081107 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV FLUSH REPAIR AT STA BS 577 DOES NOT MEET SRM REQUIREMENT. INSTALLED NEW DOUBLER 53-2-1 FIG 7 SHEET 3 CLASS 1. 2 L 7 4 4F RT 4A25 20081209 NM 2008 12 9 HNA2008F00057 1 20081029 A 5320 DOUBLER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE FUSELAGE CRACKED A HNAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 07 815EX 321 UPON GEAR EXTENSION DURING FINAL APPROACH TO RUNWAY 35, THE NOSE GEAR RED UNSAFE LIGHT INDICATION ILLUMINATED. BOTH MAI N GEARS LOCKED AND ILLUMINATED GREEN INDICATIONS. THE CREW DISCONTINUED THE APPROACH AND PERFORMED THE ALTERNATE GEAR E XTENSION PROCEDURE. THE GEAR WAS NOT CYCLED PRIOR TO PERFORMING THE ALTERNATE GEAR EXTENSION. THE FLIGHT LANDED AND TA XIED TO THE GATE WITHOUT INCIDENT. OUT OF SERVICE. THE ACFT WILL MAINT FERRY FOR FURTHER IINSPECTION. LT SIDEWALL AT J BEAM DOUBLER CRACKED. (K) 2 H 7 2 4T 4 T RT A13NM E20NE 20081209 SO 2008 12 9 C2XA08SH152 1 20081203 A 5320 14530642403 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24103 145645 CENTER OMEGA BEAM LOWER FLANGE HAS CORROSION AT FR 34. REPAIRED CENTER OMEGA BEAM LOWER FLANGE IAW EMB 145 SRM 53-00-10 . THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081209 EU 2008 12 9 UPS08154077 1 20081130 A 5210 ROLLER AIRBUS A300 A300F4622R 3930360 EU L1 DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 164UP 005 L1 DOOR ROLLER & TRACK DAMAGE. REMOVED & REPLACED FWD ENTRY DOOR SLIDE IAW AMM 20-21-12-00 AND AMM 52-11-11-04 2 L 7 2 4F RT A35EU 20081209 EA 2008 12 9 SWIA200820597 1 20081021 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 C-CHECK, RIGHT AFT THRUST FITTING CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081209 EA 2008 12 9 SWIA200820598 1 20081021 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 C-CHECK, LEFT AFT THRUST FITTING CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081209 WP 2008 12 9 UPS08854036 1 20081107 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV FLUSH SKIN REPAIR AT STA 156 LONG 21L DOES NOT MEET SRM CRITERIA REF SURVEY SEQ 700F1-01. REPAIRED I AW SRM 53-02-08 FIG 23. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854065 1 20081102 A 5753 DOUBLER DOUG DC8 DC871F 302199D WP TE FLAP CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV LEFT OUTBOARD FLAP UPPER SURFACE AT XF333 DOUBLER CHAFED. REPAIRED AS IAW UPS EO DC8 5720 31345. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854066 1 20081106 A 5720 STRUCTURE DOUG DC8 DC871F 302199D WP RT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV RIGHT WING LWR L/E DAMAGE ARE AT XFS 295 CUTOUT & STOP DRILL NOT VISIBLE REF APPENDIX H SEQ 700 W4 11 . REPAIR AS IAW UPS EO 5720 31347 A. 2 L 7 4 4F RT 4A25 20081209 NM 2008 12 9 UPS08M54000 1 20081122 A 5610 LINK DOUG MD11 MD11F 3023600 NM SLIDING WINDOW BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 284UP 0322 48541 INSPECTION TYPE:N/A F/O SLIDING WINDOW DRIVE MECHANISM BROKE. T/S FOUND DRIVE ASSY CHAIN LINK BROKEN, REPLACED DRIVE ME CHANISM ASSY AS PER M/M 56-12-03-4 & F/O'S SLIDING WINDOW OPS CHECKED SATIS AS PER M/M 56-12-03, OK FOR SERVICE. 2 L 7 3 4F RT A22WE 20081209 WP 2008 12 9 UPS08854040 1 20081107 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV FLUSH REPAIR AT BS 122 TO 138 L19R TO 20R DOES NOT MEET SRM CRITERIA. REPAIRED SRM 53-02-01-0 FIG 7 SHEET 1. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08853988 1 20081013 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQ 803-F1-130 AT STA 1788-1791, L28L-30L HAS NO SRM REF AND REQUIRES ENG DISPOSITION. REMOVE D AND REPLACED REPAIR DOUBLER IAW SRM 51-1-21, 51-1-8, 53-2-1 FIG 7 AND SAA EA 81426740001. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08853990 1 20081013 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQ 803-F1-124, FS 1718, L20L-21L HAS NO SRM REF AND REQUIRES ENG DISPOSITION. REMOVED AND RE PLACED REPAIR DOUBLER IAW SRM 53-2-1 FIG 7, 51-1-8, 51-1-21 AND SAA EA 81427030001. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08853994 1 20081013 A 5330 SKIN DOUG DC8 DC873F 302199F WP FS1672,L22-23L MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQ 803-F1-121, FS 1672, L22L-23L (FLUSH REPAIR 1-1.5 INCH) HAS NO SRM REF AND REQUIRES ENG DI SPOSITION. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 53-2-1 FIG 7, 51-1-8, AND SAA EA 81427360001. 2 L 7 4 4F RT 4A25 20081209 NM 2008 12 9 AALA200820061 1 20081118 A 5320 146N876945 CHANNEL BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 688AA 55898 25730 HAT CHANNEL CORRODED UNDER THRESHOLD OF R-4 PASSENGER/SERVICE DOOR, REPLACED CHANNEL IAW SRM 53-60-51-2R2. 2 L 7 2 4F RT A2NM 20081209 WP 2008 12 9 UPS08853997 1 20081007 A 5320 STRUCTURE DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP ROUND FLUSH REPAIR 0.500 INCH DIA AT FS 1601.5, L8L HAS NO MINIMUM ROWS OF RIVETS REQUIRED BY SRM REP AIR SEQ 803-F1-113. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 51-1-8, 53-2-1 FIG 7 AND SAA EA 81426050001. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854001 1 20081029 A 5534 STRUCTURE DOUG DC8 DC871F 302199D WP VERTICAL STAB MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV VERTICAL STAB ZR254 EXTERNAL DOUBLER DOES NOT MEET SRM GUIDELINES. INSTALLED NEW ROW OF RIVETS 51-3- 0 51-1-21. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854002 1 20081029 A 5534 STRUCTURE DOUG DC8 DC871F 302199D WP VERTICAL STAB UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV SSN 700-S4-02 RT SIDE VERTICAL STAB STATION 254 EXTERNAL REPAIR UNABLE TO VALIDATE. REPAIRED AS PER SRM 51-1-27. 2 L 7 4 4F RT 4A25 20081209 NM 2008 12 9 QXEA2008120401224 1 20081203 A 3230 ROD END BOMBDR DHC8 DHC8402 1390042 NM MLG ACTUATOR OUT OF RIG A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 19 417QX 4086 SEA - UPON GEAR RETRACTION LEFT GEAR DOOR LIGHT AND LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED FOR APPROX 20-30 SECONDS AFTER OTHER LIGHT EXTENSIONS LIGHTS WENT OUT. VISUALLY CONFIRMED GEAR UP. GEAR EXTENDED NORMALLY. FERRY TO PDX. C/W RIGGING OF LT MLG RETRACT ACTUATOR ROD END IAW AMM 32-31-11-830-801. OPS CHECK OF MLG PRIMARY EXTENSION AND RETRACTION , GOOD IAW Q-400 AMM 32-31-00-710-801. RETURNED TO SERVICE. NO PARTS. 2 H 7 2 4T RT A13NM 20081209 NM 2008 12 9 QXEA2008120401225 1 20081203 A 2421 11521062 GENERATOR BOMBDR DHC8 DHC8402 1390042 NM NR 1 FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 19 400QX 4030 MWH - NR 1 GEN DC CAUTION LIGHT ILLUMINATED IN FLT RAN CHECK LIST REMAINED ON ASSOCIATED NR 1 DC GEN HOT CAUTION LIGHT ALSO ILLUMINATED. DIVERTED TO MWH. LANDING UNEVENTFUL. REMOVED AND REPLACED NR 1 DC GEN IAW AMM 24-31-01 PG 401-414 C /W OPS CHECK OF 28V GEN SYSTEM IAW AMM 24-31-00-710-802. CHECKS GOOD, NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081209 NM 2008 12 9 QXEA2008120401215 1 20081125 A 7710 8211661 FILTER BOMBDR DHC8 DHC8402 1390042 NM PRECOOLER MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 19 417QX 4086 SEA - ON CLIMB BOTH ENGINE FLUX 3. FLUX WAS INDEPENDENT FOR EACH ENGINE. WHEN POWER PULLED OUT OF DETENT FLUX 1-2 PERC ENT OF SET POWER. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. REPLACED BOTH ENG NR 1 AND NR 2 PRECOOL ER FILTERS IAW AMM TASK 36-11-31-000-802 AND 36-11-31-400-802. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081210 WP 2008 12 10 AALA200810293 1 20081121 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 MID CARGO, CORROSION AT CLIP NUT ATTACH HOLES ON RIGHT TIE DOWN TRACK FROM STATION 693 TO 788. REMOVED AND REPLACED CAR GO TIE DOWN TRACK WITH SERVICEABLE PER SRM 51-10-3. 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810295 1 20081122 A 5320 WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CORROSION ON LOWER WEB STATION 363-434 (FORWARD CARGO). REPLACED LOWER WEB WITH SERVICEABLE PER SRM 51-02-00. 2 L 7 2 4F RT A6WE 20081210 NM 2008 12 10 CALA2008120901131 1 20081208 A 3350 1000679 LIGHT BOEING 767 767224 1385170 NM COCKPIT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 76151 39464 1944 30430 OVERHEAD EMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. REPLACED OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHEC KS NORMAL. 2 L 7 2 4F RT A1NM 20081210 NM 2008 12 10 QXEA2008120401227 1 20081127 A 5230 HANDLE BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR UNSECURE A QXEA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION NR NOT REPORTED 1 NM 19 419QX 4145 RNO - FWD BAG DOOR WARNING IN FLIGHT. ALL OTHER INDICATIONS NORMAL. OUTER HANDLE NOT SEATED COMPLETELY. RESEATED HAND LE CAUTION EXTINGUISHED. PERFORMED VISUAL INSP OF DOOR ON OBVIOUS DEFECTS NOTED. PERFORMED OPS TEST PER AMM 52-32-00-7 10-801. OPS CHECK GOOD. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081208 NM 2008 12 8 FDEA200812035052 1 20081203 A 5311 ACA73511 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 CABIN LEFT FRAME STATION 535 BETWEEN LONGERON 23 AND 24 FOUND WITH CHAFING MARKS. REPAIR CARRIED OUT AS PER DRAWING SRZ -53-503. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081208 NM 2008 12 8 FDEA200812035053 1 20081203 A 5347 AEA732515 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1289-1321 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 CABIN RIGHT SEAT TRACK STATION 1289 TO 1321 FOUND WITH CORROSION AS MARKED AT X = -75.5. REPAIRED BY SECTIONAL SEAT TRA CK REPLACEMENT FROM EXISTING SPLICE AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-10 0. 2 L 7 3 4F RT A22WE 20081208 NM 2008 12 8 FDEA200812035054 1 20081203 A 5730 ARB7402 SKIN DOUG MD11 MD11F 3023600 NM ACCESS DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 08 FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. EACH CRACKED FASTENER HOLES REAMED AND REPAIR CA RRIED OUT AS PER EA NR 1-5710-122654. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081208 NM 2008 12 8 FDEA200812035055 1 20081203 A 5730 ARB7402 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 07 FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RIGHT WING LOWER SKI N ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. REAMED AND REPAIR CARRIED OUT AS PER EA NR 1-57 10-122655. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081208 NM 2008 12 8 HALA2008111700877 1 20081117 A 5730 PANEL BOEING 767 76733A 1385209 NM LT WING DEBONDED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 582HA 28139 LT WING T/E PANEL AT WS314.3 TOP SURFACE RAISED AND RIVET PULLED. SUSPECTED CORROSION UNDER PANEL. FOUND TO BE DISBOND OF COMPOSITE PANEL. REPAIRED PANEL IAW SRM 57-51-01 AND 51-70-07, PARA 5K REV 77. 2 L 7 2 4F RT A1NM 20081208 NM 2008 12 8 SWAA086818 1 20081203 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086824 1 20081204 A 5310 6547978 CREASE BEAM BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM CRACKED AT BS 617, STR 17R. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086826 1 20081204 A 5753 6546435278 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED HC2 CHECK, FOUND RT WING O/B AFT FLAP TRAILING EDGE I/B DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086769 1 20081203 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 773, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 FDEA200812035064 1 20081203 A 5320 6529548 PAN BOEING 727 7272S2F 1384O81 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 BS 1166 RBL 45-60 DITCHING PAN HAS 3 CRACKS REPLACED DITCH PAN REF DWR 65-29548 AND SRM 51-30-2 PG 4. THIS IS CLASSIFIE D AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081208 NM 2008 12 8 SWAA086786 1 20081203 A 5310 6547959 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 794, STR 25R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086787 1 20081203 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086798 1 20081203 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086800 1 20081203 A 5311 6546595 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086835 1 20081203 A 5512 65C25727 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER CRACKED AT REAR SPAR, BS 125, FWD OF PANEL 9107L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086836 1 20081204 A 5330 65C337568 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SWA EA . 2 L 7 2 4F RT A16WE 20081208 EA 2008 12 8 SWIA200820566 1 20081201 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 932SW 7714 FLT 6715 - AFT EMERGENCY LIGHT BURNED OUT. RELAMPED. 2 L 7 2 4F RT A21EA 20081208 NM 2008 12 8 SWAA086840 1 20081204 A 5753 65C26320 FITTING BOEING 737 7373H4 1384600 NM MID FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND RT WING O/B MID FLAP O/B SUPPORT FITTING CORRODED. REPAIRED FITTING PER PAE ER. 2 L 7 2 4F RT A16WE 20081208 EA 2008 12 8 SWIA200820567 1 20081130 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 454SW 7749 FLT 4483 - AFT EMERGENCY CEILING FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081208 NM 2008 12 8 SWAA086841 1 20081204 A 5753 6573731 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FLAP PER PAE ER. 2 L 7 2 4F RT A16WE 20081208 EA 2008 12 8 SWIA200820568 1 20081201 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA WINDOW POST CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 RIGHT WINDSHIELD AFT POST LOWER AFT ANGLE IS CRACKED IN THE BEND RADIUS (AD INSP). REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081208 EA 2008 12 8 SWIA200820569 1 20081201 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA WINDOW POST CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 LEFT WINDSHIELD AFT POST LOWER AFT ANGLE IS CRACKED IN THE BEND RADIUS, AD INSP. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081208 SO 2008 12 8 SWIA200820571 1 20081203 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO COCKPIT ODOR A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 301YV 120301 FLT 5442 - BURNING ODOR IN COCKPIT AND CABIN ACCOMPANIED WITH SMOKE. CLEANED AIR CONDITIONING HEAT EXCHANGERS, RAN BOTH PACKS OFF ENGINE BLEEDS AND APU BLEED FOR OVER AN HOUR, NO DISCREPANCIES NOTED. INSPECTED WIRING AND CONTACTORS NO DIS CREPANCIES NOTED. 2 L 7 2 4T RT A31SO 20081208 EA 2008 12 8 SWIA200820574 1 20081129 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 442SW 7609 FLT 4739 - LEFT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081208 NM 2008 12 8 SWAA086806 1 20081203 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT EQUIPMENT COOLING DUCT CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086849 1 20081204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086852 1 20081204 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 UALA2008120306732 1 20081202 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 DENT IN FUSELAGE FRAME AT STA 1420, STR 26L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SECTION OF FLANGE AND FABRICAT ED A J-ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081208 NM 2008 12 8 UALA2008120406749 1 20081203 A 5420 BUSHING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 ON NR 2 ENGINE, UPPER LINK, FWD BUSHING HAS MOVEMENT-ROTATED. EVIDENCED BY BROKEN SEALANT AROUND THE BUSHING PERIMETER. REPLACED BUSHINGS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081208 NM 2008 12 8 UALA2008120406750 1 20081203 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 552UA 26641 FWD PIT FRAME DENTED STA 520 AT STR 24L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED I/B FLANGE AND INSTALLED J-ANGLE R EPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081208 2008 12 8 UALA2008120406758 4 20081204 A 2565 7A147913 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L2 DOOR LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 180UA 25224 THE 2L DOOR SLIDE PRESSURE LOW. REPLACED SLIDE PACK ASSY AT DOOR 2L. 2 L 7 4 4F 4 F RT A20WE E24NE 20081208 EU 2008 12 8 FDEA200811264985 1 20081126 A 5712 A5724081021400 RIB AIRBUS 300 A300B4622R 3930312 EU LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 LEFT WING RIB 5; HOLE "G" HAS A CRACK INDICATION. COMPLIED WITH FEDEX EA 6-5710-123674 WINGS - AD 99-16-01 - EO 6-5710 -7-5005 - LT WING REAR SPAR, RIB 5 FITTING BOLT HOLE "G", "I", "M", AND "O". ORIGINAL EA ATTACHED TO SNRM N00846. 2 L 7 2 4F RT A35EU 20081208 NE 2008 12 8 UALA2008120206726 2 20081129 A 7421 38882677 IGNITER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 ENGINE FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 223UA 30224 EICAS STATUS MSG ENGINE IGNITER R1. REPLACED IGNITER PLUG. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081208 NM 2008 12 8 UALA2008120106705 1 20081201 A 2730 162000105 COMPUTER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE ELEVATOR FEEL FAULTY A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 672UA 30027 CREW COMMENTS: ELEVATOR FEEL STATUS MESSAGE. REPLACED ELEVATOR FEEL COMPUTER. 2 L 7 2 4F 4 F RT A1NM E24NE 20081208 NM 2008 12 8 UALA2008120206717 1 20081201 A 2560 65B090944 TURNBUCKLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GIRT BAR OUT OF ADJUST A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 107UA 26900 DOOR 1R IS DIFFICULT TO ARM. ADJUSTED GIRT BAR ATTACH FITTING TURN BUCKLE. 2 L 7 4 4F 4 F RT A20WE E24NE 20081208 EA 2008 12 8 A6WA200840614 1 20081122 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 GL 31 438AW 7748 LOG 193206/3 FLAPS FAILED AT ZERO. COMPLIED WITH QRH. DIVERTED TO ALB. BRAKE TEMP 4,2,1,3. COMPLIED WITH RESET PROCE DURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4. FLAP SYSTEM RESET OK. NOTED BY MX. 2 L 7 2 4F RT A21EA 20081208 NM 2008 12 8 USAA920082077 1 20081110 A 5320 694122615 ANGLE BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 MCN LAV SPILL MAJOR REPAIR NR 6136798 CORROSION ON SPLICE ANGLE AT BS936.5, WL204, BETWEEN RBL34 TO LBL40. REPLACED SPL ICE ANGLE IAW B737 SRM 51-40-02-0G. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 USAA920082078 1 20081109 A 5310 6552878U97 CREASE BEAM BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 MCN LAV SPILL MAJOR REPAIR NR 6135573 CORROSION ON CREASE BEAM INNER CHORD BETWEEN BS984 TO BS1006, WL207.8, LBL60. REP LACED CREASE BEAM IAW B737 SRM 51-40-02-0G. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 UALA2008120106682 1 20081126 A 3350 58731 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 EMERGENCY LIGHTING STRIP STICKING UP FROM FLOOR AT SEATS 13ABC. RESECURED EEL LIGHTING STRIP, OPS CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081209 EU 2008 12 9 UALA2008112506665 1 20081125 A 5320 PLATE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 403UA 442 SHEAR PLATE AFT OF DOOR 2R LOCATED BETWEEN FRAMES 69 AND 70 HEAVILY CORRODED. CONTINUED INSTALLATION OF SHEAR PLATE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081209 NM 2008 12 9 UALA2008112506667 1 20081125 A 3397 80172424 FEEDER CABLE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE EMERGENCY LIGHT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 794UA 26953 SEAT 3E, AFT EMERGENCY LIGHT INOP. REPLACED CABLE & LIGHT ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081209 NM 2008 12 9 UALA2008111305461 1 20080825 A 5753 65B3901193E FLAP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LT WING PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 117UA 38933 28810 LEFT INBOARD FORE FLAP LEADING EDGE HAS A LARGE PUNCTURE. FOUND PUNCTURED FORE FLAP DAMAGED FROM TIRE TREAD. REPAIRED DAMAGED SPAR PER SRM 51-70-12, REPAIR 1. REPAIRED LOWER PANEL ON R61502 PER SM-80-57-53-17-JD. REPAIRED L/E BULLNOSE O N R61505 PER SRM 57-53-01. 2 L 7 4 4F 4 F RT A20WE E24NE 20081209 NM 2008 12 9 FDEA200812055087 1 20081205 A 5343 AEA7051501 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 CENTER LANDING GEAR WHEEL WELL FOUND LEFT TRUNNION AFT HOLE INTERIOR SURFACE CORRODED. CORROSION REPAIRED AS PER EA N R 1-5310-122650. REPAIR BUSHING FABRICATED AND INSTALLED AS PER SRM 53-40-00 FIGURE 16 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081209 EA 2008 12 9 SWIA200820581 1 20081004 A 7120 BUSHING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 466SW 7856 C-CHECK, RIGHT ENGINE YOKE LINK BUSHINGS ARE CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081209 SO 2008 12 9 C2XA08RI175 1 20081107 A 3350 66901 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15980 145202 RIC - MX - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT FLOOR STRIP INOPERATIVE. MX REMOVED AND REPLACED STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081209 CE 2008 12 9 COEA2008120101976 1 20081126 A 2730 263401783 TORQUE TUBE CESSNA CESSNA 208 208B 2073701 CE ELEVATOR LOOSE A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 976FE 9189 208B0103 THE LT INBOARD CONTROL HORN ATTACHMENT RIVETS FOUND WORKING ON ELEVATOR TORQUE TUBE ASSY. LT ELEVATOR CONTROL HORN EXHI BITED ROTATIONAL MOVEMENT ON TORQUE TUBE. UPON REMOVAL OF HORN FROM TORQUE TUBE, FOUND WEAR WAS LIMITED TO RIVETS. REMO VED AND REPLACED TORQUE TUBE ASSY ATTACHMENT RIVETS. 1 H 7 1 3T A37CE 20081209 CE 2008 12 9 COEA2008120102775 1 20081126 A 2730 263401783 TORQUE TUBE CESSNA CESSNA 208 208B 2073701 CE ELEVATOR CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 775FE 9290 208B0272 THE RT INBOARD CONTROL HORN ATTACHMENT RIVETS FOUND WORKING ON ELEVATOR TORQUE TUBE ASSY. RT ELEVATOR CONTROL HORN EXHI BITED ROTATIONAL AND LATERAL MOVEMENT ON TORQUE TUBE. RIVET HOLES, CONTROL HORN AND TORQUE TUBE EXHIBITED FRETTING CORR OSION. REMOVED AND REPLACED TORQUE TUBE ASSY. 1 H 7 1 3T A37CE 20081209 CE 2008 12 9 GLBA200812011 1 20081128 A 6123 AUTOFEATHER SYS BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3A NE NR 2 ENGINE MALFUNCTIONED A GLBA O OTHER O OTHER AP APPROACH 1 NM 21 173YV UE173 SIGNIFICANT EVENT - FLIGHT 5128 EN ROUTE FROM PIR TO DEN DURING APPROACH INTO DENVER ON FINAL AT ABOUT 6000FT & 160KTS. THE NR 2 ENGINE AUTOFEATHERED 3 TIMES WITH TORQUE AT 1200, GEAR DOWN AND PROPS 1700 RPM. MAINTENANCE PERFORMED AN OPER ATIONAL RUNUP OF THE LEFT AND RIGHT ENGINES AND PERFORMED A TEST OF AUTOFEATHER SYSTEM IAW 1900D MM 61-21-00. ALL CHECK S GOOD, COULD NOT DUPLICATE FAULT. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 20081209 WP 2008 12 9 AALA200810284 1 20081115 A 5311 FRAME DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION ON FRAME. INSTALLED FRAME SPLICE REPAIR PER SRM 53-03-00. 2 L 7 2 4F RT A6WE 20081209 WP 2008 12 9 AALA200810273 1 20081110 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION ON RIGHT CUSP, STATION 1174-1193. INSTALLED RIGHT CUSP SHEET, STATION 1174 TO STATION 1250 PER AARD 53-20-00- 16. 2 L 7 2 4F RT A6WE 20081209 WP 2008 12 9 UPS08854047 1 20081125 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQUENCE 803-F1-134 REQUIRES AN SDR 12 X 25 INCH EXTERNAL REPAIR DOUBLER AT STA 112-140 L34L-L 35L CORRELATES TO DC8 SRM 53-2-1 FIG 7 SHT 3. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854064 1 20081102 A 5753 DOUBLER DOUG DC8 DC871F 302199D WP TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV LEFT O/B FLAP TOP SURFACE DOUBLER GOUGED. REPAIRED AS PER UPS EO DC8 5720 31345A. 2 L 7 4 4F RT 4A25 20081209 NM 2008 12 9 UPS08654078 1 20081201 A 3350 LIGHT BOEING 767 76734AF 1385212 NM CABIN BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 318UP 27746 EMERGENCY DOME LIGHT ASSY BROKEN. LAMP HOLDER REPLACED. OPERATIONAL TEST OK. DOME LIGHT & EMERGENCY LIGHT. 2 L 7 2 4F RT A1NM 20081209 WP 2008 12 9 UPS08854044 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQ 803-F1-104, STA 1446 L31L-L32L HAS NO SRM REF & REQUIRES APPX F OF EODC8-5100-30418C. REM OVED OLD DOUBLER, FABBED & INSTALLED FILLER AND DOUBLER SHT7075T6 .071 & .080 REF SRM 53-4-1, 53-2-1 FIG 7, 51-1-8, 51-1 -20D, SAA ENG 81426590001. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08853996 1 20081013 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQ 803-F1-119, FS 1701, L16-17L (ROUND FLUSH REPAIR 1.25 INCH) HAS NO SRM REF AND REQUIRES EN G DISPOSITION. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 51-1-8, 53-2-1 FIG 7 AND SAA EA81426990001. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854008 1 20081030 A 5720 STRUCTURE DOUG DC8 DC871F 302199D WP LT WING UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV LEFT WING CENTER L/E HAS A STEEL DOUBLER INSTALLED. REPLACED DOUBLER UPS EO DC8 5710-31296-A. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854009 1 20081010 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EXTERNAL SKIN REPAIR AT BS 383 L11L DOES NOT MEET SRM REQUIREMENTS. REPAIRED AS PER UPS EO DC8 5100 30540. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854010 1 20081013 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV REPAIR AT BS 850 L21R DOES NOT MEET SRM CRITERIA. REPAIRED UPS EO 5320-31273A. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854011 1 20081105 A 5720 STRUCTURE DOUG DC8 DC871F 302199D WP LT WING UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV LT WING CENTER L/E LOWER OUTBOARD EDGE IS TRIMMED OUT AT ATTACHED FASTENER HOLES. REPAIR AS PER UPS EO DC8 5720 31291. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854012 1 20081011 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EXTERNAL SKIN DOUBLER FS 191.5 DOES NOT MEET SRM GUIDELINES. REPAIRED PER UPS EO DC8 5320 31294A. 2 L 7 4 4F RT 4A25 20081210 WP 2008 12 10 AALA200810292 1 20081121 A 5320 PAN DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 FORWARD CARGO DOOR PAN CORRODED. REMOVED AND REPLACED CARGO DOOR PAN WITH SERVICEABLE PER SRM 51-10-3. 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810294 1 20081120 A 5313 LONGERON DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CORROSION ON LONGERON 30 BETWEEN STATIONS 446 AND 484 (FORWARD CARGO). REPAIRED PER SRM 53-02-00. 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810297 1 20081123 A 5340 BRACKET DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 AFT CARGO TIE DOWN TRACK ATTACHED BRACKET BROKEN STATION 1287 LEFT SIDE AT LONGERON 28L. INSTALLED A SERVICEABLE BRACKE T PER SRM 51-10-1. 2 L 7 2 4F RT A6WE 20081210 NM 2008 12 10 AALA200820066 1 20081120 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 56842 24599 AFT MAIN DECK PLATE CORRODED, REPAIRED IAW SRM 53-60-51-2R2. 2 L 7 2 4F RT A2NM 20081210 NM 2008 12 10 QXEA2008120401222 1 20081130 A 3260 PROXIMITY SENSOR BOMBDR DHC8 DHC8402 1390042 NM LT MLG DOOR OUT OF RIG A QXEA O OTHER N FALSE WARNING AP APPROACH 1 NM 19 434MK 4227 STS - LEFT MAIN GEAR UNSAFE INDICATION AND LT MLG DOOR OPEN INDICATION AFTER GEAR SELECTED DOWN ON APPROACH. FERRY TO P DX FOR REPAIRS. INTERROGATED OF PSEU FOUND PRESENT FAULT LGDLK 1 UNREASONABLE FAR. INDUCTANCE VALUE OF LGDLK1 SENSOR W AS AT 7.960 MH BEFORE ADJUSTMENT. RIGGED THE PROXIMITY SENSOR IAW AM TASK 32-61-06-830-801. CHECKED THE INDUCTANCE VAL UE OF PROXIMITY SENSOR IAW TASK 32-61-00-280-801, CURRENTLY AT 8.296MH. OP'S TESTED OF THE LANDING GEAR PRIMARY EXTENSI ON/ RETRACTION SYSTEM IAW TASK 32-31-00-710-801. OP'S CHECKED GOOD. RETURNED TO SERVICE. NO PARTS. 2 H 7 2 4T RT A13NM 20081210 WP 2008 12 10 AALA200810308 1 20081108 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CABIN, CORROSION ON SEAT TRACK STATION 1130. INSTALLED REPAIR PLUG PER AARD 53-20-00-10. 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810311 1 20081108 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CABIN, CORROSION ON RIGHT CUSP AT STATION 1011. REPAIRED PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081210 NM 2008 12 10 CALA2008120901133 1 20081209 A 5512 182A4002 SKIN BOEING 737 737924 13848A1 NM HORIZONTAL STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 38403 30120 RIGHT HORIZONTAL LOWER SKIN FWD OF AFT SPAR AT STAB STATION 129 .50 HAS 3 INCH CRACK. REMOVED DAMAGE SECTION OF SKIN, I NSTALLED REPAIR DOUBLER PER ECRA 5510-01954. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 CALA2008120401125 1 20081203 A 5320 BAC15181211 BEAM BOEING 737 737924 13848A1 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 38403 30120 STA 986.5 HAS CORROSION AT FASTENER HOLES LOCATED AT RBL-29 AND RBL-43, UPPER AND LOWER SURFACES OF FWD FLANGE. INSTALL ED REPAIR AND FASTENERS PER ECRA 5321-01429 REV A. 2 L 7 2 4F RT A16WE 20081209 NM 2008 12 9 UALA2008112606676 1 20081126 A 2120 CLAMP BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CARGO HEAT DUCT BROKEN A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 219UA 30551 BURNING ODOR IN CABIN. FLIGHT DIVERTED. DUST AND FEATHER TYPE DEBRIS COMING OUT OF VENTS BY SEATS 39AB-42AB, INTERMITT ENTLY PER CREW. CREW LATER STATED THAT WHEN L DUCT PRESS DROPS TO 37 PSI FROM 42 PSI THERE IS A RUMBLE NOISE IN AFT CAB IN AND SIDEWALL IS GETTING VERY WARM. FOUND CLAMP FOR CARGO HEAT DUCT IN AFT PIT LT SIDE BROKEN AND DUCT SEPARATED. RE PLACED CLAMP AND INSULATION BLANKETS AS REQUIRED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081209 NM 2008 12 9 UALA2008112606677 1 20081125 A 2822 568129115004 PUMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT FUEL BOOST FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 778UA 26940 FUEL PUMP RT FWD EICAS ILLUMINATED. FOUND "R FWD FUEL BOOST PUMP L AC SECT 2" (C18 ON P110) AND "R FWD FUEL BOOST PUMP R XFR " (F27 ON P210) TRIPPED. COLLARED ALL PER MEL 2822F, ITEM A.3 REPLACED, REPLACED RT FWD FUEL BOOST PUMP. OPS NOR MAL. NO LEAKS. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081209 NM 2008 12 9 UALA2008112606679 1 20081125 A 2697 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SQUIB FAULTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 524UA 24977 NR 1 L FIRE BOTTLE WILL NOT TEST. ACCOMPLISHED LEFT ENGINE EXTINGUISHER BOTTLE SQUIB TEST CIRCUIT TEST. RANG OUT WIRIN G FROM M32 SQUIB TEST PANEL TO LEFT SQUIB CONNECTOR D2188 ON BOTTLE 1, B17. CHECKED GOOD. CONNECTOR D2188 ON SQUIB CHE CKED GOOD. REPLACED SQUIB TEST PANEL M32 DUE TO BAD SWITCH S1. TESTED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081209 NE 2008 12 9 UALA2008111305731 2 20080914 A 7321 8010003 FMU BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE FAULTY A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 655UA 25393 724465 NR 2 ENG, TURBINE CASE COOLING ACTUATOR IS LEAKING FUEL AT A RATE OF 30 DROPS PER MINUTE. FOUND CHUNKS OF RUBBER COVERI NG 10 PERCENT OF STRAINER. PERHAPS O-RING MATERIAL. NO METAL FOUND. CLEANED AND REINSTALLED STRAINER. COMPLETED INSP OF STRAINER INSTALLATION FOUND SECURE. REPLACED NR 2 ENG FUEL PUMP AND FMU. REPLACED CUT O-RING AT OIL COOLER OUTLET FUEL FLANGE. OP CHECKED AND LEAK CHECKS OKAY. REPLACED FUEL PUMP FILTER P/N 75912-102. ACCMP'D LEAK CHECK. CHECKS GO OD. REPLACED TCC ACTUATOR. REPLACED NR 2 ENG VSV ACTUATOR. LEAK CHECK AND OP CHECKS GOOD. RT ENGINE TURBINE CASE COO LING MANIFOLD AFT SUPPORT STANDOFFS SLIGHTLY WORN. REPLACED MANIFOLD P/N 50T120 AND CLAMPS P/N 53T422-01. 2 L 7 2 4F 4 F RT A1NM E24NE 20081209 NM 2008 12 9 UALA2008112606680 1 20081125 A 2620 G718505 CONTROL PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 348UA 24252 NO GREEN LIGHT NR 2 ENG LIGHT BOTTLE. REPLACED FIRE CONTROL PANEL. 2 L 7 2 4F 4 F RT A16WE E21EU 20081209 SO 2008 12 9 C2XA08CL126 1 20081204 A 5240 14525940403 SEAL EMB 145 EMB145XR 3260214 SO SERVICE DOOR LOOSE A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 17138 145727 CLE FLIGHT 2505 - THE CREW REPORTED A LOUD BANGING NOISE AT THE SERVICE DOOR ON CLIMBOUT FROM CLE. THE AIRCRAFT RETURNE D TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE SERVICE DOOR SEAL LOOSE AND HANGING OUT AT TH E BOTTOM. RESECURED THE SERVICE DOOR SEAL AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 20081209 EA 2008 12 9 SWIA200820576 1 20081004 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 466SW 7856 C-CHECK, LEFT SIDE FS 621 ANGLE CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081209 EA 2008 12 9 SWIA200820579 1 20081004 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 466SW 7856 C-CHECK, FS 280 FLOORBEAM LBL9 UPPER FLOOR SUPPORT CRACKED IN RADIUS. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081209 EA 2008 12 9 SWIA200820580 1 20081004 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 466SW 7856 C-CHECK, FS 280 FLOORBEAM LBL 9 LOWER SUPPORT RADIUS CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081209 SO 2008 12 9 C2XA08SH153 1 20081203 A 5320 14530646401 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24103 145645 SHV - DURING C-CHECK LT OMEGA BEAM CORRODED AT FR 54. MAINTENANCE REPAIRED LT OMEGA BEAM IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081209 SO 2008 12 9 C2XA08IA247 1 20081104 A 2530 500064001 COFFEEMAKER EMB 145 EMB145XR 3260214 SO GALLEY FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14153 11093 3489 145761 SDR C2XA08IA235, FLIGHT 2459 CREW REPORTED THAT THE NUMBER ONE COFFEEMAKER SMOKES WHEN TURNED ON. MAINTENANCE PLACED ON NEF GL-01 CAT D CTL NR 157681, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 11/07/08 MAINTENANCE REMOVED AN D REPLACED THE NUMBER ONE COFFEEMAKER, OPERATIONALLY CHECKED WITH NO DEFECTS, CLEARED THE NEF, AND THE AIRCRAFT WAS APPR OVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081209 SO 2008 12 9 C2XA08RI178 1 20081203 A 3350 7137215501 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13124 145689 EWR - MX - DURING ROUTINE MAINTENANCE, MX FOUND AISLE EMERGENCY LIGHT INOPERATIVE ABOVE ROW 3. MX REMOVED AND REPLACED AISLE SEAT LIGHT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081209 WP 2008 12 9 AALA200810285 1 20081117 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 RIGHT TIE DOWN TRACK CORRODED. REMOVED AND REPLACED RIGHT TIE DOWN TRACK FROM STATION 1212-1322 PER SRM 51-30. 2 L 7 2 4F RT A6WE 20081209 WP 2008 12 9 AALA200810270 1 20081109 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION ON LEFT CUSP, STATION 836-841. DOUBLER INSTALLED PER SRM 51-01-00. 2 L 7 2 4F RT A6WE 20081209 WP 2008 12 9 UPS08854046 1 20081125 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQ 803-F1-131 REQUIRES AN SDR 7 X 8 INCH EXTERNAL DOUBLER REPAIR AT STA 1882-1890 L28L-L34L C ORRELATES TO DC8 SRM 53-2-1 FIG 7 SHT 13. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 AALA200810223 1 20081105 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 954U 49426 CORROSION ON CUSP T AT RIGHT SIDE AT STATION 598. INSTALLED SPAR SECTION OF TEE. 2 L 7 2 4F A6WE 20081209 EA 2008 12 9 SWIA200820583 1 20081004 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 466SW 7856 C-CHECK, LEFT ENGINE THRUST MOUNT CORRODED AT BEARING. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081209 EA 2008 12 9 SWIA200820586 1 20081008 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 472CA 7667 C-CHECK, PASSENGER DOOR INNER FORWARD SKIN CRACKED IN STEP RADIUS AT ZONE 3. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081209 EA 2008 12 9 SWIA200820588 1 20081008 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 472CA 7667 DURING C-CHECK, FS 484 LBL 27.0 ANGLE CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081209 WP 2008 12 9 AALA200802364 1 20081020 A 3350 SHROUD DOUG DC9 DC982 3022082 WP LIGHT ASSY BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 476AA 49651 DFW - EMERGENCY LIGHT AT SEAT 17D HAS CRACKED SHROUD. REPLACED CLEAR PLASTIC SHROUD FOR EMERGENCY LIGHT AT SEAT 17D. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081209 WP 2008 12 9 AALA200802365 1 20081020 A 3350 SHROUD DOUG DC9 DC982 3022082 WP LIGHT ASSY BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 476AA 49651 DFW - EMERGENCY LIGHT AT SEAT 23D HAS CRACKED SHROUD. REPLACED CLEAR PLASTIC SHROUD FOR EMERGENCY LIGHT AT SEAT 23D. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081209 NM 2008 12 9 AALA200820057 1 20081110 A 5320 143N5366 PANEL BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 666A 52891 25300 SIDE PANEL CORRODED, REPAIRED SIDE PANEL IAW SRM 53-00-53-1A. 2 L 7 2 4F RT A2NM 20081209 EA 2008 12 9 SWIA200820589 1 20081019 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 970SW 7881 C-CHECK, FS 280 RBL 9 FLOOR SUPPORT ANGLE CLIPS CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081209 EA 2008 12 9 SWIA200820590 1 20081019 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 970SW 7881 C-CHECK, FS 280 RBL 12 FLOOR SUPPORT ANGLE CLIP CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081209 EA 2008 12 9 SWIA200820591 1 20081021 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 C-CHECK, FLOORBEAM FS 280 RBL 9 OUTBOARD CLIP CRACKED. REPLACED PER REO. 2 L 7 2 4F RT A21EA 20081209 EA 2008 12 9 SWIA200820596 1 20081021 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 C-CHECK, FS 625 LEFT AND RIGHT SIDE CLIPS CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081209 WP 2008 12 9 UPS08854038 1 20081107 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV FLUSH SKIN REPAIR AT STA BS 1333 L21R DOES NOT MEET SRM CRITERIA. REPAIRED 52-2-00 FIG 4 SHEET 3. 2 L 7 4 4F RT 4A25 20081209 NM 2008 12 9 UPS08553995 1 20081118 A 5532 SRM517010 SKIN PANEL BOEING 757 75724APF 1384969 NM VERTICAL STAB DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 414UP 23854 INSPECTION TYPE:C VERTICAL STAB LEADING EDGE PANEL 321BL DELAMINATED AT UPPER/INNER SURFACE. REMOVED DAMAGE, BONDED DOU BLERS, SEALED EDGES, PRIMED IAW SRM 51-70-10 F FIG 201 REPAIRS. 2 L 7 2 4F RT A2NM 20081210 WP 2008 12 10 AALA200810310 1 20081108 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CABIN, CORROSION ON LEFT CUSP AT STATION 602. REPAIRED PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810312 1 20081107 A 5411 RIB DOUG DC9 DC983 3022083 WP ZONE 400 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 LEFT ENGINE PYLON, CRACK IN LOWER FORWARD END OF THE INBOARD RIB JUST ABOVE PANEL NUMBER 8111C. REPAIRED PER SRM 54-21- 00 FIGURE 2 SHEET 1 AND 2, 54-01-00 FIGURE 2 SHEET 2 AND 51-60-00 FIGURE 1 SHEET 1. 2 L 7 2 4F RT A6WE 20081210 NM 2008 12 10 CALA2008120801130 1 20081207 A 5315 BAC14902811 FLOORBEAM BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 33264 31584 CABIN FLOORBEAM AT STATION 328 REQUIRES A SINGLE FLANGE REPAIR, AFT SIDE FROM RBL 28 TO RBL 38 DUE TO CORROSION. REPAIR ED AFT FLOORBEAM FLANGE IAW B737 SRM 53-00-51 AND MODIFIED INTERCOSTAL AT RBL 24 IAW ECRA-5321-01590. 2 L 7 2 4F RT A16WE 20081210 WP 2008 12 10 AALA200810300 1 20081121 A 5313 LONGERON DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 AFT CARGO, CORROSION ON LONGERON UNDER FRAME FROM STATION 1277 TO 1297. REPLACED SECTION OF LONGERON FROM 1277 TO 1297. 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810301 1 20081123 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 AFT CARGO, CRACK IN INTERCOSTAL BETWEEN STATIONS 1287 AND 1309. REMOVED AND REPLACED INTERCOSTAL WITH SERVICEABLE PER S RM 53-14-3. 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810325 1 20081113 A 5531 FRAME DOUG DC9 DC983 3022083 WP ZONE 300 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 LEADING EDGE FORMER CRACKED IN RADIUS AT FORWARD SPAR ATTACH FASTENER LEFT STATION ZFS 36.500. INSTALLED REPAIR DOUBLER PER AARD 55-30-00-2. 2 L 7 2 4F RT A6WE 20081210 NM 2008 12 10 USAA920082086 1 20081117 A 5311 65C25228 FRAME BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT Q2 MAJOR REPAIR NR 03C10753039/007 FRAME CRACKED AT PSU RAIL ATTACH POINT BS727D, BETWEEN S8R AND S9R. REPAIRED FRA ME AT PSU RAIL ATTACH POINT BS727D, BETWEEN S8R AND S9R IAW TYPICAL REPAIR NR 53-10-20E. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 USAA920082087 1 20081117 A 5311 6546596 FRAME BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT Q2 MAJOR REPAIR NR 03C10753039/006 FRAME CRACKED AT PSU RAIL ATTACH POINT BS 727B, BETWEEN S8R AND S9R. REPAIRED FR AME AT PSU RAIL ATTACH POINT BS 727B, BETWEEN S8R AND S9R IAW TYPICAL REPAIR NR 53-10-20E.. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 BINA081001 1 20081019 A 3350 767 LAMP BOEING 737 737400 138449A NM EMERGENCY LIGHT BURNED OUT A BINA K NONE L NO TEST IN INSP/MAINT 1 WP 11 43XA 24796 LT FORWARD EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RE-LAMPED EMERGENCY EXIT LIGHT IAW AMM 33-51-22. 2 L 7 2 4F RT A16WE 20081210 SO 2008 12 10 FDKA2008120300307 1 20081203 A 2621 337000271 FIRE BOTTLE EMB 145 EMB145LR 3260212 SO CARGO BAY INOPERATIVE A FDKA K NONE L NO TEST NR NOT REPORTED 1 SW 07 847MJ 25 145517 FRL FLT 6269 BHM-CVG. CARGO EXTINGUISH BOTTLE INOP DURING FIRE TEST. MX REMOVED AND REPLACED CARGO FIRE BOTTLES. 2 L 7 2 4T RT T00011AT 20081210 SO 2008 12 10 FDKA2008120300308 1 20081203 A 5220 SEAL EMB 145 EMB145LR 3260212 SO OVERWING EXIT LACK OF LUBE A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 FRL FLT 6273 CVG-ROC. RT OVERWING EXIT DOOR SQUEALS IN FLIGHT. MX LUBED DOOR SEAL. LEAK CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081210 SO 2008 12 10 FDKA2008120200303 1 20081202 A 5210 HINGE EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FRL FLT 6194 CVG-IAD. MAIN PAX DOOR HARD TO OPEN. MX LUBED HINGE POINTS, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 20081210 SO 2008 12 10 FDKA2008120200304 1 20081202 A 3350 20191A CHARGER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA K NONE L NO TEST NR NOT REPORTED 1 SW 07 857MJ 145765 FRL FLT 6189 JFK-RIC. ROW 12 LT EMERGENCY EXIT SIGN INOP. MX REMOVED AND REPLACED NR 3 BATTERY CHARGER, OPS CHECK GOOD . 2 L 7 2 4T RT T00011AT 20081210 WP 2008 12 10 UPS08854016 1 20081013 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV DOUBLER AT STA 608 DOES NOT MEET SRM GUIDELINE. REPAIRED PER UPS EO DC8 5320 31276. 2 L 7 4 4F RT 4A25 20081210 WP 2008 12 10 UPS08854017 1 20081113 A 2730 ELEVATOR DOUG DC8 DC871F 302199D WP RIGHT OUT OF BALANCE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV RIGHT ELEVATOR REQUIRES WEIGHT AND BALANCE. ACCOMPLISHED IAW 27-30-01-4. 2 L 7 4 4F RT 4A25 20081210 WP 2008 12 10 UPS08854018 1 20081013 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV DOUBLER DOES NOT MEET SRM REQUIREMENTS FS 184 L10R. REPAIRED AS PER UPS EO 5320 31298A. 2 L 7 4 4F RT 4A25 20081210 NM 2008 12 10 MZZA2008120400007 1 20081203 A 5320 141A5410 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 SW 27 26232 28942 FORMED INTERCOSTAL CRACKED IN FWD WET AREA BETWEEN STA 312 AND STA 328 AT RBL 31. INTERCOSTAL REMOVED, FABRICATED IAW E CRA 5321-01524. HOLES PICKED PER SRM 51-40-05 AND INSTALLED PER SRM 51-10-02 REV 33. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086878 1 20081204 A 5311 6546533 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086879 1 20081204 A 5311 6546526 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086867 1 20081204 A 5330 6562212 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086868 1 20081204 A 5311 6545808 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 291, STR 16R. REPAIRED FRAME PER AAR EA. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086869 1 20081204 A 5315 6546804 FLOORBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM TEE CAP CORRODED AT BS 986, BETWEEN LBL 2 TO RBL 16. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086870 1 20081204 A 5330 6545800 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 286, STR 13R. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086871 1 20081204 A 5330 6545800 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 227, RBL 15. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086872 1 20081204 A 5311 6545774 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 794, BETWEEN STR 24R TO STR 25R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086873 1 20081204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 16L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 FDEA200811264992 1 20081126 A 5314 6523555 KEELBEAM BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 LOWER AFT CARGO BAY LT KEELBEAM BS 950E 6 OTBD FLANGE IS CORRODED. INSTALLED REPAIR STRAP REF EA 7-5310-118316. THIS I S CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081210 SO 2008 12 10 RAIA2008120500002 1 20081204 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 851HK 145340 EMERGENCY FLOOD LIGHT AT AISLE IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE BULB. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081210 SO 2008 12 10 RAIA2008120800001 1 20081205 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 847HK 14500857 EMERGENCY EXIT LIGHT AT ROW 3BC INOPERATIVE. MAINTENANCE SPLICED IN A NEW CONNECTOR FOR THE LIGHT. OPERATIONAL CHECK W AS GOOD. 2 L 7 2 4T RT T00011AT 20081210 SO 2008 12 10 RAIA2008120300001 1 20081201 A 3610 O-RING EMB 145 EMB145LR 3260212 SO BLEED AIR SYS LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 822HK 145069 CREW RECEIVED A BLEED 2 LEAK MESSAGE ON THE EICAS DURING CLIMB. MAINTENANCE REMOVED AND REPLACED LEAKING O-RINGS IN THE BLEED DUCT SYSTEM. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081210 NM 2008 12 10 SWAA086859 1 20081204 A 5753 6573732 CAP BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND RT WING O/B AFT FLAP, I//B END CAP DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086860 1 20081204 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086862 1 20081204 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 WRLA2008105 1 20081208 A 5753 FLAP DOUG MD11 MD11 3023602 NM TE FLAP VANE DEBONDED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 272WA 48437 DURING 1C+12A CHECK, EGAT MECHANIC FOUND LEFT WING OUTBOARD FLAP VANE LOWER SKIN DISBOND AT XOFH=499 ~ XOFH=533 (34 X 9. 5 ), REFER TO EGAT NRC U01027. OPEN 2 L 7 3 4F RT A22WE 20081210 NM 2008 12 10 WRLA2008104 1 20081208 A 5753 REPAIR DOUG MD11 MD11 3023602 NM TE FLAP VANE DEBONDED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 272WA 48437 DISBOND-DURING 1C+12A CHK, EGAT MECHANIC FOUND LEFT WING INBOARD FLAP VANE LWR SKIN EXISTING REPAIR DISBOND & EXTEND TO THE ORIGINAL SKIN AT XIFH=152~XIFH=213(61 X 19), THE EXISTING REPAIR:(70 X31) AND XIFH=243~XIFH=258 (15X23) REFER TO EGA T NRC U01026. OPEN 2 L 7 3 4F RT A22WE 20081210 EA 2008 12 10 MASA2008120300736 1 20081203 A 3234 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR FAULTY A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 27314 19700 7314 ASH 7343 HSV-IAD. CREW RETURNED TO FIELD DUE TO NOSE GEAR DOOR WARNING MESSAGE AND GEAR DISAGREE MESSAGE DUE TO MAIN GE ARS WOULD NOT RETRACT ON TAKEOFF. FERRIED TO CAE WHERE MX REPLACED DOOR SELECTOR VALVE. 2 L 7 2 4F RT A21EA 20081210 NM 2008 12 10 NOCA08508 1 20081130 A 7711 7898301 TRANSMITTER BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE DEFECTIVE A NOCA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 15 750NA 26277 31652 ABNORMAL ENGINE PARAMETERS DURING CRUISE. REMOVED AND REPLACED LEFT ENG EPR TRANSMITTER PER MM 77-11-01 PERFORMED TEST 13 FOUND OK AS PER MM 71-00-00. FOUND LEFT ENGINE ETPU SENSE LINE LOOSE. SECURED LINE PER MM 70-51-00-912-001-ROO. AC COMPLISHED HIGH POWER RUNS AND ALL INDICATIONS WERE NORMAL. OPS CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E12EU 20081210 CE 2008 12 10 TIMA20080008 1 20081203 A 3230 MS24171 RELAY BEECH 1900 1900C 1154161 CE LANDING GEAR BURNED E TIMA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 NM 07 17ZV UC17 THE LANDING GEAR MOTOR DID NOT RUN WHEN THE PILOT SELECTED 'GEAR UP'. PILOT RETURNED TO AIRPORT AND LANDED WITHOUT INCI DENT. INVESTIGATION REVEALED THAT THE 60 AMP CIRCUIT BREAKER WAS OPEN AND THE LANDING GEAR MOTOR RELAY HAD BURNED CONTA CTS. CLOSING THE CB AND REPLACING THE RELAY RETURNED THE LANDING GEAR RETRACT SYSTEM TO NORMAL OPERATION. 2 L 7 2 4T RT A24CE 20081210 EU 2008 12 10 USAA2008121092212 1 20081209 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 634AW 91 FLT 541 DFW-PHX - EEL - EMERGENCY LIGHT FAULT DURING TEST. MAINTENANCE REMOVED AND REPLACED BATTERY FOR EMERGENCY POWER SUPPLY UNIT 13WL IAW AIRBUS MAINTENANCE MANUAL 33-51-38. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 20081210 EU 2008 12 10 USAA2008121092213 1 20081209 A 2120 UNKNOWN AIRBUS A319 A319112 3930323 EU CABIN ODOR A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 19 733UW 1205 FLT 1429 CLT-ATL - BURNING SMELL - SEVERAL PASSENGERS IN ROW 5 AREA COMPLAINED OF BURNING PLASTIC SMELL DURING TAKEOFF A ND SHORTLY BEFORE LANDING. MAINTENANCE INSPECTED LIGHTING, PSU PANELS AND UNDER-SEAT WIRING AND WERE UNABLE TO FIND ANY EVIDENCE OF BURNING OR PLASTIC SMELL. AIRCRAFT WAS CLEARED FOR CONTINUED SERVICE. 2 L 7 2 4F RT A28NM 20081210 NM 2008 12 10 USAASB08122 1 20081206 A 2822 20C1444 CHECK VALVE BOEING 737 7374B7 138449C NM CENTER FUEL TANK FAULTY A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 439US 24781 DURING CRUISE, EN ROUTE FROM CLT TO CZM, CREW REPORTED FUEL BURNED OUT OF NR 2 FUEL TANK WITH OVER 5,000 POUNDS IN CENTE R TANK. ALL PUMPS WERE ON. UNABLE TO DETERMINE THE REASON, FLIGHT DIVERTED TO FLL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT CENTER BOOST PUMP CHECK VALVE PER MM 28-22-71. OPERATIONAL CHECK GOOD. NO FURTHER FUEL MIGRATION. ALSO, ACCOMPLISHED CHECK OF FUEL DISTRIBUTION SYSTEM. CHECKS GOOD PER MM 28-20-00. 2 L 7 2 4F RT A16WE 20081210 NE 2008 12 10 USAABB08174 2 20081207 A 7200 ENGINE BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE NR 2 MALFUNCTIONED A USAA E ENGINE SHUTDOWN J W WARNING INDICATION INADEQUATE Q C DE DESCENT 1 EA 19 918UW 22196 31270 CLT FLT 816 EN ROUTE CUN TO CLT. DURING DESCENT INTO CLT, THE FLIGHT RECEIVED AN INDICATION OF NO OIL PRESSURE IN THE NUMBER TWO ENGINE. THE CREW SHUT DOWN THE NUMBER TWO ENGINE. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. SINGLE ENGI NE TIME WAS APPROXIMATELY 15 MINUTES. MAINTENANCE ACTION PENDING. OPEN 2 L 7 2 4F 4 F RT A2NM E12EU 20081210 WP 2008 12 10 AALA200810302 1 20081122 A 5311 FRAME DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 AFT CARGO, CORROSION ON STATION 1309 FRAME. INSTALLED FRAME SPLICE PER SRM 53-03-00 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810303 1 20081109 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CABIN, RIGHT SIDE CUSP IS CORRODED AT STATION 170. REPAIRED PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081210 NM 2008 12 10 CALA2008120501126 1 20081204 A 5347 141T5121 SEAT TRACK BOEING 767 767224 1385170 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 68159 30438 FWD CARGO STA 412 CABIN FLOORBEAM ATT SEAT TRACK CRACK LBL 20. CABIN STA 380 - 412 LBL 20 SEAT TRACK REPLACED PER SRM 5 1-10-02 AND FASTENER INSTALLED PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081210 SO 2008 12 10 FDKA2008113000301 1 20081130 A 7500 CLAMP EMB 145 EMB145LR 3260212 SO BLEED AIR SYS LOOSE A FDKA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 850MJ 145568 FDM FLT 6231 PHL-RON. EMERGENCY DECLARED AND AIRCRAFT DIVERTED DUE TO BLEED 1 LEAK MESSAGE. MX FOUND LOOSE CLAMP AT TH E BLEED VALVE. 2 L 7 2 4T RT T00011AT 20081210 SO 2008 12 10 FDKA2008120300305 1 20081203 A 5210 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF ADJUST A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 FRL FLT 6268 IAD. MAIN CABIN DOOR INNER HANDLE CATCHES ON DOOR TRIM. MX ADJUSTED HANDLE, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081210 WP 2008 12 10 UPS08854021 1 20081008 A 5753 PANEL DOUG DC8 DC873F 302199F WP TE FLAP DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP LT FLAP SURF BOARD PANEL HAS TWO DAMAGED SCREW HOLES. INSTALLED BONDED REPAIR IAW SRM 57-7-1, 51-1-9 A PAR 11 FIG 9, 51-1-15 PAR 2. 2 L 7 4 4F RT 4A25 20081210 WP 2008 12 10 UPS08854026 1 20081118 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP LT WING OUTBOARD LEADING EDGE INBOARD SECTION HAS CRACKED UPPER RIB ABOVE PANEL 579B XFS 584. FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-21, 51-1-20D, 57-2-0 FIG 002 SHT 2. 2 L 7 4 4F RT 4A25 20081210 WP 2008 12 10 UPS08854027 1 20081008 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP LT FUSELAGE SKIN STA 1506 BETWEEN L29-31L HAS NUMEROUS PULLED FASTENERS. REMOVED EXISTING REPAIR DOU BLER, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-20D, 53-2-1 FIG 7, 51-1-26. 2 L 7 4 4F RT 4A25 20081210 WP 2008 12 10 UPS08854030 1 20081106 A 5751 SKIN DOUG DC8 DC871F 302199D WP LT AILERON MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV LT WING OUTBOARD AILERON UPPER SURFACE AT STA XA685 HAS EXTERNAL DOUBLER SURVEY DOES NOT MEET SRM REQ UIREMENTS. REPAIRED AS PER UPS EO DC8 5720 31284 A. 2 L 7 4 4F RT 4A25 20081210 WP 2008 12 10 UPS08854028 1 20081104 A 5320 CHANNEL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP DURING REPAIR EVAL OF EFN 80320061044 FOUND ANOTHER CRACK ON CHANNEL D-PIT STA 1394 L34R. REMOVED D AMAGE AND FABBED AND INSTALLED REPAIR ANGLE AND DOUBLER IAW SRM 51-1-20D, 51-1-21, 53-2-0 FIG 1B AND DWG 5616674. 2 L 7 4 4F RT 4A25 20081210 NM 2008 12 10 MZZA2008120500011 1 20081204 A 3350 S417N5101057 COVER BOEING 737 737824 13844BZ NM EXIT SIGN MISSING A MZZA K NONE O OTHER IN INSP/MAINT 1 SW 27 14228 28792 R2 EMERGENCY EXIT LIGHT SIGN COVER MISSING. REMOVED AND REPLACED 2R EMERGENCY EXIT LIGHT. OPS CHECK GOOD PER AMM 33-51 -01-960-802. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 FDEA200812045076 1 20081204 A 5320 CHANNEL BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 OTBD HAT CHANNEL HAS CORROSION AROUND NUT PLATE HOLES. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. FABRICATED, LOCATE D AND DRILLED HOLES, TREATED, PRIMED AND INSTALLED NEW HAT CHANNEL, REFERENCE DWG NR 65-19606/ITEM NR 19, CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 FDEA200812045077 1 20081204 A 5320 69728463 FLOOR SUPPORT BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 FLOOR SUPPORT AT FS 1130 TO FS 1148, RBL 62, WL 206, HAS CORROSION AROUND SEVERAL NUT PLATES. REMOVED CORROSION AND FOU ND TO BE OUT OF LIMITS. FABRICATED, LOCATED AND DRILLED HOLES, TRIMMED, TREATED, PRIMED AND INSTALLED NEW FLOOR SUPPORT. REF BOEING DWR 69-72846/ ITEM 3 AND SRM 51-10-2. THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 FDEA200812045079 1 20081204 A 5320 69348321 FLOOR SUPPORT BOEING 727 7272S2F 1384O81 NM BS 1169-1172 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 MAIN DECK FLOOR STRUCTURE, BL 0 BEAM, RT ATTACH ANGLE IS CORRODED AT LWR EDGE AT 1169 TO 1172, RBL 1 WL 205. REMOVED, F ABRICATED NEW ANGLE REF DRAWING 69-34832 AND INSTALLED REF SRM 51-30-2. THIS IS CLASSIFED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 FDEA200812045082 1 20081204 A 5315 6520824 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 218FE 21101 STA 1166 FLOORBEAM, LOWER FLANGE CORRODED RBL 53-57 AT ADEL CLAMP. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMO VED DAMAGE, FABRICATED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR PARTS. REFERENCE SRM 53-10-8/ FIG 8. THIS IS CLASS IFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20081210 NM 2008 12 10 FDEA200812045080 1 20081204 A 5320 65672505 ANGLE BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 AFT PIT BULKHEAD UPPER ANGLE CORRODED CENTERLINE TO RBL 1166. REMOVED AND REPLACED UPPER CHORD ANGLE AT STA 1166 IN LWR AFT CARGO PIT REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 FDEA200812045083 1 20081204 A 5320 B275305107 FLOOR SUPPORT BOEING 727 7272S2F 1384O81 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 REWORK OF SNRM N00933, FLOOR SUPORT AT FS 1148 RBL 45 WAS MISSDRILLED FABRICATED NEW FLOOR SUPPORT REF DRAWING B27-53-01 5B. INSTALLED REF SRM 51-30-2 THIS IS CLASSIFED AS A MAJOR REPAIR 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 USAA2008120992208 1 20081130 A 3221 D64433 HINGE PIN AIRBUS A319 A319132 3930340 NM NLG CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 808AW 1088 SAL - C7 - MAJOR REPAIR - DURING PENETRANT INSPECTION, NOSE LANDING GEAR CENTER HINGE PIN WAS FOUND CRACKED. REPLACED N OSE LANDING GEAR CENTER HINGE PIN IAW A319 AMM 32-21-27. 2 L 7 2 4F RT A28NM 20081210 NM 2008 12 10 ASAA0873962 1 20081120 A 5315 147A55048 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 BS 947 RBL 53 FLOORBEAM IS CORRODED. BLENDED CORROSION ON BS 947 RBL 53 FLOORBEAM FLAP PEENED AREA AND RE-APPLIED FINIS H. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 USAA2008120992209 1 20081206 A 5320 ANGLE BOEING 767 7672B7ER 1385107 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 253AY 24894 BFM - C4 - MAJOR REPAIR - FLOOR SUPPORT ANGLES CRACKED AT BS 246, LBL 7 TO RBL 19 (8EA). REPLACED (8EA) FLOOR SUPPORT A NGLES AT BS 246, LBL 7 TO RBL 19 IAW B767 SRM 51-70-13. 2 L 7 2 4F RT A1NM 20081210 NM 2008 12 10 ASAA0873960 1 20081126 A 5310 453A26114 STRIP BOEING 737 737790 13844CN NM CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON CARGO BAY CAP STRIP. REMOVED AND REPLACED CAP STRIP IN CARGO BAY. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 AALA200802341A 1 20081015 A 2782 5006397R ACTUATOR BOEING 757 757223 1384957 NM ZONE 500 TRIPPED A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 619AA 24577 BOS INFLIGHT, DURING APPROACH CREW REPORTED SLAT DISAGREE INDICATION. LANDED BOS WITHOUT INCIDENT. FOUND LEFT INBOARD ROTARY ACTUATOR TRIPPED. REPLACED LEFT LEADING EDGE SLAT DRIVE INBOARD ROTARY ACTUATOR. SYSTEM GROUND CHECKED NORMAL O PERATION. 2 L 7 2 4F RT A2NM 20081210 EU 2008 12 10 FDEA200812065096 1 20081206 A 5343 12R53611094 BUSHING AIRBUS 310 A310304 3930339 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 817FD 552 MAIN FRAME RT NOSE LANDING GEAR BEARING FITTING INSPECTION PER EA T6-5310-99725A, REQUIRES REMOVAL OF REPAIR BUSHING FOR INSPECTION. REMOVED REPAIR BUSHING, FABRICATED REPLACEMENT REPAIR BUSHING AND INSTALLED IAW FEDEX EA 6-5310-99725A, RE LEASE DATE 07/20/06. 2 L 7 2 4F RT A35EU 20081210 NM 2008 12 10 ASAA0853975 1 20081204 A 2161 6228145 CONTROLLER BOEING 737 737890 1384527 NM E&E BAY FAULTY A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 579AS 6946 35187 LEFT PACK LIGHT ILLUMINATED DURING RECALL NR 1 PACK TEMP CONTROLLER SHOWED THIS PACK TCV FAULT WHICH CLEARED. BOTH PACK TEMP CONTROLS CHECK OK, REF AMM 21 61 20 400 801. 2 L 7 2 4F RT A16WE 20081210 NE 2008 12 10 ASAA0853964 2 20081202 A 7261 CFM567B27 ENGINE BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 1 OIL CONSUMPTION A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 579AS 6932 35187 894547 AIRCRAFT RESTRICTED FROM ETOPS SERVICE UNTIL NR 1 ENGINE OIL CONSUMPTION RATE IS CORRECTED NR 1 ENGINE OIL CONSUMPTION W ITHIN ETOPS LIMITS OF .09 REF ETOPS MANUAL 05 00 11. A/C RELEASED FROM TOP DEFERRAL. THE ETOPS STATUS OF THE AIRCRAFT HAS BEEN REINSTATED. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081210 NM 2008 12 10 ASAA0853976 1 20081206 A 2161 6228145 CONTROLLER BOEING 737 737890 1384527 NM E&E BAY FAULTY A ASAA K NONE J WARNING INDICATION CR CRUISE 1 NM 02 577AS 6848 35186 ZONE TEMP ON CONT CB LIGHT ON. QRH FOLLOWED, LIGHT REMAINED ON, WENT OUT WITH RECALL SELECTED REFERENCE AMM FIM TASK 21 62 00. PERFORMED BITE CHECK OF ZONE TEMP CONTROLLER AND RESET OPS NORMAL. AIRCRAFT OKAY FOR SERVICE. 2 L 7 2 4F RT A16WE 20081210 2008 12 10 ASAA0853977 4 20081205 A 2310 8220990004 TRANSCEIVER BOEING 737 737890 1384527 NM HF COMM FAULTY A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 559AS 7425 35178 CIRCUIT BREAKER FOR HF 1 POPPED. RESET C/B REF 20 60 01. FOUND HF NR 1 TRANSCEIVER BAD. REPLACED NR 1 HF TRANSCEIVER REF 23 11 00 710 801 & OPERATIONAL CHECK OK. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0843969 1 20081119 A 5330 6545890502 BEAR STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 FWD ENTRY DOOR BEAR STRAP IS CRACKED AT FASTENER HOLE UPPER HINGE CUTOUT. REPAIRED L! DOOR CUTOUT BEAR STRAP AT UPPER H INGE IAW AAR EA 13050 AND ASA EA 400 53EA 00289. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0893974 1 20081114 A 5320 141A5410459 INTERCOSTAL BOEING 737 737990 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 INTERCOSTAL CRACKED. REPLACED INTERCOSTAL PER SRM 51 40 02. 2 L 7 4 4F RT A16WE 20081210 NM 2008 12 10 ASAA0873973 1 20081203 A 5320 143A81263 SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE BS 492 500A RBL 20 WL 158. REMOVED AND REPLACED SIDEWALL SUPPORT PLATE AT BS 492 500A RBL 20 WL 158 DUE TO CORROSION WITH PART. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 USAA2008120892194 1 20081121 A 5320 141N83219 FITTING BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 904AW 23566 MCN - MAJOR REPAIR - C12 CHECK - FRAME CLIP IS CRACKED AT BS 350, S7L AT THE UPPER SIDE OF L1 DOOR CUTOUT UPPER FRAME. REPLACED PER B757 SRM 51-40-02 AND BOEING DWG 141N8321. 2 L 7 2 4F RT A2NM 20081210 NM 2008 12 10 USAA2008120892195 1 20081107 A 5754 114N407636 PANEL BOEING 757 7572S7 1384962 NM LE SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 904AW 23566 MCN - MAJOR REPAIR - C12 CHECK - RIGHT WING NR 9 SLAT COVE PANEL AT WS 653 CRACKED. REPLACED RIGHT WING NR 9 SLAT COVE PANEL AT WS 653 IAW BOEING DWG 114N4076. 2 L 7 2 4F RT A2NM 20081210 NM 2008 12 10 USAA2008120592188 1 20081203 A 5315 D53472284008 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 808AW 1088 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON FLOORBEAM AT FR 65 AND FR 66, -Y480. REPLACED FLOORBEAM AT FR 64 AND FR 67 , BETWEEN -Y465 AND -Y480 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081210 NM 2008 12 10 ASAA0843967 1 20081117 A 5753 65C2631026 SKIN BOEING 737 7374Q8 138447Q NM MID FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 RT WING I/B AFT MID FLAP TRAILING EDGE IS GOUGED PREVIOUS REPAIR AT AFT FLAP I/B CONTROL ROD. REMOVED PREVIOUS REPAIR, FABBED REPAIR DOUBLER AND BONDED REPAIR PARTS IAW B737 400 SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081210 WP 2008 12 10 AALA200810332 1 20081117 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CORROSION ON FLOORBOARD SUPPORT DIRECTLY FORWARD OF NR 6 SEAT TRACK. REMOVED AND REPLACED FLOORBOARD SUPPORT PER SRM 51 -01. 2 L 7 2 4F RT A6WE 20081210 NM 2008 12 10 FDEA200811084812 1 20081108 A 5315 652083938 FLOORBEAM BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 STA 1148 FLOORBEAM UPPER FLANGE CORRODED RBL 45-45 AFT SIDE AND 44-47 FWD SIDE WL 208. REPAIRED DAMAGED FLOORBEAM REF S RM 53-10-8 FIG 3, SUBSTITUTED "T" CHORD REF EA 7-5310-118313. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 FDEA200811084813 1 20081108 A 5315 652084010 FLOORBEAM BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 AFT FLOORBEAM CORRODED RBL 27 AND RBL 43 NUTPLATES STA 1166 WL 208. REPAIRED CORRODED FLOORBEAM REF SRM 53-10-8 FIG 3. SUBSTITUTED "T" CAP MATERIAL REF EA 7-5310-118313. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 ASAA0843968 1 20081118 A 5753 65C2632017 SKIN BOEING 737 7374Q8 138447Q NM MID FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 LT OUTBOARD MID FLAP LOWER SURFACE HAS A CHAFED SPOT JUST ABOVE NR 2 FLAP TRACK FAIRING. REPAIRED LT OUTBOARD MID FLAP LOWER SURFACE SKIN IAW B737 400 SRM 51 70 10 PG 214 & IAW B737 400 SRM 51 70 10 PG 249-256. 2 L 7 2 4F RT A16WE 20081210 EA 2008 12 10 REX2008F00058 1 20081118 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OUT OF RIG A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8623A 7623 ON APPROACH SELECTED FLAPS 20, RECEIVED FLAP FAILURE MSG WITH FLAPS STUCK AT ZERO. QRH FOLLOWED DECLARED EMERGENCY WITH AN UNEVENTFUL LANDING. FOUND FLAPS TO BE OUT OF RIG. RIGGED FLAPS PER AMM PERFORMED OPS CHECK WITH NO DEFECTS. 2 L 7 2 4F RT A21EA 20081210 NM 2008 12 10 ASAA0843979 1 20081129 A 5753 FLAP TRACK BOEING 737 737490 1384715 NM TE FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 NR 1 FLAP TRACK HAS EVIDENCE OF CORROSION. 2 L 7 2 4F RT A16WE 20081211 WP 2008 12 11 AALA200810323 1 20081120 A 5340 MOUNT DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 CABIN, G-1 GALLEY INBOARD MOUNT CORRODED AT STATION 160. REMOVED AND INSTALLED A SERVICEABLE MOUNT. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810324 1 20081119 A 5320 ANGLE DOUG DC9 DC983 3022083 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 AFT ACCESSORY, ANGLE CRACKED ON AFT END, ABOVE ELEVATOR ACCUMULATOR CUTOUT, CANT FRAME STATION 1474. REMOVED AND INSTAL LED A SERVICEABLE ANGLE PER SRM 51-01. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810344 1 20081119 A 5320 SUPPORT ANGLE DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 INTERCOSTAL SUPPORT ANGLE CRACKED UNDER CO-PILOTS BRIEF CASE HOLD AT STATION 120 LONGERON 19 RIGHT. REMOVED AND REPLACE D ANGLE. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810357 1 20081119 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 CORROSION ON CUSP STATION 201. REPAIRED PER AARD53-20-00-16. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810345 1 20081116 A 5320 SUPPORT ANGLE DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 INTERCOSTAL SUPPORT ANGLE IN FORWARD CARGO CRACKED AT STATION 237 BETWEEN LONGERON 27 RIGHT AND LONGERON 28 RIGHT. REPL ACED SUPPORT ANGLE PER SRM 51-01. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810347 1 20081120 A 5320 ANGLE DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CORROSION ON ANGLE IN AFT CARGO AT STATION 1155 LONGERON 28 RIGHT. REPLACED CORRODED ANGLE WITH SERVICEABLE ONE. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810354 1 20081120 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 CABIN, 2 CRACKS IN LEFT CUSP AT STATION 223 TO 227. INSTALLED SERVICEABLE CUSP SHEET. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810342 1 20081119 A 5311 FRAME DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CORROSION IN FRAME STATION 1231 LONGERON 29 RIGHT TO LONGERON 24 LEFT IN AFT CARGO. REMOVED AND REPLACED WITH NEW SECTI ON OF FRAME AND SPLICE STATION 1231 LONGERON 28 RIGHT TO LONGERON 29 LEFT. 2 L 7 2 4F RT A6WE 20081211 NM 2008 12 11 ASAA0844002 1 20081118 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 9 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 RT WING NR 9 SPOILER UPPER SURFACE DENTED CTR 3 INCH FROM 4E DENT. REPAIRED REMOVED DAMAGE FAB AND DRILLED DOUBLER AND INSTALLED REPAIR IAW B737 400 SRM 57 70 10 FIG 201. 2 L 7 2 4F RT A16WE 20081211 WP 2008 12 11 AALA200810355 1 20081120 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 AFT CARGO, INTERCOSTAL CRACKED AT FASTENER HOLES STATION 1287 TO 1309 (CEILING CENTER). INSTALLED A SERVICEABLE INTERCO STAL. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 ASOA200801637 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RT FLOOR SEAT RAIL FS 349.00 TO 485.00 HAS CORROSION DAMAGE (MARKED). INSTALLED SEAT TRACK P/N SH670-32159-1 PER AMM 53 -00-49-400-801-A03. 2 L 7 2 4F RT A21EA 20081211 WP 2008 12 11 AALA200810366 1 20081123 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 CORROSION ON NUMBER 2 SEAT TRACK STATION 1194 TO 1202. REPLACED SECTION OF SEAT TRACK FROM STATION 1183 TO 1224. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810322 1 20081113 A 5531 FRAME DOUG DC9 DC983 3022083 WP ZONE 300 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 VERTICAL STABLIZER, LEADING EDGE FORMER CRACKED IN RADIUS AT FORWARD SPAR ATTACH FASTENER RIGHT SIDE ZFS 30.00. REPAIRE D PER AARD 55-30-00-2. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810318 1 20081118 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 CABIN, CENTER FLOORBOARD SUPPORT IS CRACKED AT STATION 905. REMOVED AND REPLACED SUPPORT WITH SERVICEABLE SUPPORT. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 ASOA200801614 1 20081203 A 5347 CARGO TRACK CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 CARGO SEAT TRACK AT RBL 9 FS 559+96 IS CORRODED. REMOVED CORRODED CARGO SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802. LOCATED AND DRILLED HOLES IAW SRM 51-41-02. COUNTERSUNK HOLES IAW SR M 51-40-11. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 AALA200820067 1 20081112 A 5310 141N88002 DOOR FRAME BOEING 757 757223 1384957 NM ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 694AN 47963 26974 FORWARD AVIONICS DOOR FRAME CRACKED. REPAIRED IAW SRM 51-70-11. 2 L 7 2 4F RT A2NM 20081211 WP 2008 12 11 AALA200810335 1 20081117 A 5320 ANGLE DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 TEE ANGLE FROM BELOW LEFT CUSP STATION 1140 HAS CORROSION. INSTALLED NEW TEE ANGLE PER SRM 51-01. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 ASOA200801656 1 20081205 A 5312 ANGLE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 CORROSION DAMAGE FS 280 BULKHEAD LOWER ANGLE AT ENTRANCE TO FLT COMPT RBL 10. CORROSION AREAS OF RBL 10 OF FS 280 BULKH EAD WERE TREATED IAW REO 670-53-11-370,REO 670-53-11-369,REO 670-53-11-3698 SRM 51-42-06,51-11-00 .025, NDTM 51-20-06. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801658 1 20081205 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 854AS 7382 MID CABIN EMERGENCY EXIT LIGHT INOP. FLT 4933 DEL 213 MINS. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 AALA200820069 1 20081118 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 56842 24599 AFT MAIN DECK PLATE CORRODED. REPAIRED IAW SRM 53-60-51-2R2. 2 L 7 2 4F RT A2NM 20081211 NM 2008 12 11 NWAA085265501 1 20081129 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 501US 23190 DURING AN OVERNIGHT LINE CHECK THE EMERGENCY ESCAPE PATH LIGHTING IN THE FORWARD CABIN WAS INOPERATIVE. MX FOUND THE AS SOCIATED POWER SUPPLY TO BE DEFECTIVE. THE POWER SUPPLY WAS REPLACED AND THE SYSTEM OPERATED NORMALLY AFTER THE POWER S UPPLY WAS REPLACED. 2 L 7 2 4F RT A2NM 20081211 EA 2008 12 11 ASOA200801659 1 20081205 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 CONTINUATION OF JOB 8746315/154, VERTICAL BULKHEAD BEAM AT FS 409+128 LBL 18.00 LOCAL TO WL 69.00 HAS AN INDICATION NOTE D APPROX 0.2 INCH LONG AND SIGNAL AMPLITUDE OF 80 PERCENT FULL SCREEN HEIGHT ON THE O/B C-CHANNEL AT RADIUS APPROX .5 IN CH FROM TOP. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801662 1 20081205 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 LT WING LWR PLANK ACCESS HOLE 540CB HAS EDDY CURRENT INDICATION NOTED 60 PERCENT FULL SCREEN HEIGHT APPROX 0.1 INCH LONG ON LANDING OF I/B SECTION OF RADIUS, NON-CRITICAL AREA APPROX 1 INCH AFT OF CENTER LINE. FAILS NDT INSPECTION. REPAIR ED LT WING PLANK ACCESS HOLE 540CB IAW REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801663 1 20081205 A 5260 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 UPON REMOVAL OF PAX DOOR STEP 832CT FOR REPLACEMENT OF PAX DOOR OUTER HANDLE, FOUND AFT SKIN WEB CRACKED AT RADIUS FOR S TEP 832CT AND FIXED MID STEP INTERSECTION. REPAIRED PAX DOOR AFT SKIN WEB AT RADIUS FOR STEP 832CT AND FIXED MID STEP I NTERSECTION IAW ECTC REO 601R-52-11-702. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801648 1 20081204 A 5210 MECHANISM CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10185 F/A REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE AND FEELS AS THOUGH LOCKING MECHANISM IS BINDING. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801650 1 20081204 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MISINSTALLED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 F/A REPORTED EMERGENCY LIGHT FLOOR LEVEL LIGHT STRIP (REAR 1/2) ORANGE STRIP "EXIT DIRECTION" IS AT ROW 12 NOT BY AN EXI T. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801592 1 20081201 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 LT FLOOR SUPPORT STRUCTURE IS CRACKED AT FS 621, LBL 40, WL 73. REPAIRED CRACKED LT SIDE FLOOR SUPPORT STRUCTURE AT FS 621, LBL 40, WL 73 IAW REO 601R-53-61-117 REV C. COMPLIED WITH ECTC REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801594 1 20081201 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 FS 280 FLOOR SUPPORT CHANNEL IS CRACKED O/B OF LBL 9 BESIDE MLG MANUAL RELEASE PULLEY BRACKET. APPROX 1 INCH IN LENGTH. FS 280 FLOOR SUPPORT CHANNEL IS CRACKED O/B OF LBL 9 BESIDE MLG MANUAL RELEASE PULLEY BRACKET. APPROX 1" IN LENGTH. C OMPLIED WITH BOMBARDIER REO 601R-53-11-136. REPAIR TO PILOT'S BULKHEAD J-ANGLE AT FS 280 LBL 9, RBL 9. COMPLIED W ITH ASA EO 600-53-91. COMPLIED WITH EC/TC EO 600-53-91. C/W IN ACCORDANCE WITH REO 601R-53-11-16 REV.A. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801596 1 20081201 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 THE CLIP ON THE INTERCOSTAL AT FS 484 RBL 27 HAS A .250 INCH CRACK IN THE RADIUS AT THE TOP. REMOVED AND REPLACED CLIP ON INTERCOSTAL IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 20081211 WP 2008 12 11 NWAA085319852 1 20081201 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 761NC 47709 DURING LINE CHECK BOTH OF THE FORWARD OVERWING EMERGENCY EXIT SIGNS WERE FOUND TO BE INOPERATIVE. MX REPLACED THE BATTE RY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 ASOA200801597 1 20081201 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 THE CLIP AT FS 484 LBL 27.00 HAS A .250 INCH CRACK IN THE RADIUS AT THE TOP. REMOVED AND REPLACED CLIP IAW SRM 51-42-21 AND REO 601R-53-41-059, STEP 14. STEPS 1 THRU 13 OF REO 601R-53-059 NOT REQUIRED. COMPLIED WITH EC/TC REO 53-41-059. 2 L 7 2 4F RT A21EA 20081211 EU 2008 12 11 NWAA085293277 1 20081201 A 5210 HANDLE AIRBUS 320 A320211 3930320 EU PAX DOOR OUT OF POSITION A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 377NW 02082 UNABLE TO ARM BOTH AFT DOOR SLIDES PROPERLY PRIOR TO FLIGHT. MEM MX REPOSITIONED DOOR HANDLES FROM LT TO THE RT DOOR AN D RT TO THE LT DOOR PER MM 52-13-21. DOOR SLIDES WERE ARMED AND OPS CHECKED GOOD. ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 20081210 NM 2008 12 10 AALA200820064 1 20081120 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 56842 24599 AFT MAIN DECK PLATE CORRODED, REPAIRED IAW SRM 53-60-51-2R2. 2 L 7 2 4F RT A2NM 20081210 SO 2008 12 10 FDKA2008120300306 1 20081203 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO NR 2 INOPERATIVE A FDKA K NONE L NO TEST NR NOT REPORTED 1 SW 07 847MJ 15497 145517 FRL FLT 6176 CVG-PHL. SMOKE DETECTOR WILL NOT TEST. MX REMOVED AND REPLACED NR 2 SMOKE DETECTOR, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 20081210 WP 2008 12 10 UPS08854020 1 20081105 A 5720 STRUCTURE DOUG DC8 DC871F 302199D WP LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV STA 526.7 LT WING LOWER OUTBOARD EDGE IS TRIMMED OUT AT ATTACH FASTENER HOLES. REPAIR IAW UPS EO DC8 5720 31291. 2 L 7 4 4F RT 4A25 20081210 NM 2008 12 10 SWAA086861 1 20081204 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081210 WP 2008 12 10 FDEA200812085111 1 20081208 A 3150 003001003 PROBE DOUG MD10 MD1010F 3022112 WP FAILED A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 68052 7520 47806 DEPARTING TPA RW 18R AT 392.2 TOGW BETWEEN 200 FT AND 3000 FT MSL IN A RT TURN TO 350' (FLAPS AND SLATS RETRACTED) LAT F UEL UNBALANCE ALERT CAME ON THE EAD. ALSO, FUEL QTY/USED CHK ALERT CAME ON. FUEL OFF SKED ALERT ILLUMINATED ABNORMAL N ON ALERT FUEL LEAK. ALSO, ILLUMINATED ON EAD. FOB AT DEP 55.1 AFTER 1ST ALERT ILLUMINATED FOB 43.2. REQ FUEL FOR TRIP WAS 48.1. REPLACED NR 3 OUTBOARD MJP. SEALED ALL TANK ACCESS COVERS AND THE MJP'S THAT WERE INSTALLED. ALL WORK PER FORMED BY FFC W/O 5081158. 2 L 7 3 4F RT A22WE 20081210 NM 2008 12 10 FDEA200812095112 1 20081209 A 5347 BAC1520841124 SEAT TRACK BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 493FE 21531 UPPER CARGO COMPARTMENT STA 770 BL24L SEAT TRACK LOBE CORRODED REMOVED PANEL TO GAIN ACCESS IAW 51-30-2 AND REMOVED CORR ODED SEAT TRACK AT STA 760-848; BL 24L IAW SRM 53-10-5. FABRICATED NEW SEAT TRACK IAW SRM 53-10-5. TREATED AND PRIME D IAW SRM 51-10-2, AND INSTALLED NEW SEAT TRACK IAW SRM 53-10-5. INSTALLED FLOOR PANEL IAW SRM 51-30-2. MAJOR REPAIR R II. 2 L 7 3 4F A3WE 20081210 EU 2008 12 10 FDEA200812095113 1 20081209 A 7830 WARNING SYSTEM AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4E1 52054 NE ILLUMINATED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 21 449FE 217 715838 NR 2 ENGINE REVERSER UNLOCK ECAM AT ABOUT 60 KTS ON TAKEOFF. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 14 DEC 08. FOUND NR 2 ENGINE LT REVERSER STOW SWITCH FALLING OFF CAM WHILE SHAKING WIRES FOR T/S. DUPLI CATED UNLOCK LIGHT. ADJUSTED SWITCH PER A310-200 MM 78-31-18-4. RAN REVERSER SEVERAL TIMES, OPS CHECK GOOD. NOTED 5 G OOD LEGS. 2 L 7 2 4F 4 F RT A35EU E3NE 20081210 EU 2008 12 10 FDEA200812095115 1 20081209 A 5710 A5724464420000 STIFFENER AIRBUS 300 A300B4622 3930401 EU LT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 LEFT WING VERTICAL STIFFENER LOWER AREA IS GOUGED AFT OF THE FALSE SPAR AND RIB 6A. REMOVED DAMAGED STIFFENER, LOCATED AND DRILLED NEW STIFFENER IAW DWG A57244644. INSTALLED NEW STIFFENER IAW SRM 51-40-21, PARA 7. 2 L 7 2 4F RT A35EU 20081210 WP 2008 12 10 AALA200810319 1 20081111 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CABIN, FLOORBOARD SUPPORT CRACKED AT STATION 180 LEFT BODY LINE 32. REMOVED AND REPLACED SUPPORT WITH SERVICEABLE SUPPO RT. 2 L 7 2 4F RT A6WE 20081210 NM 2008 12 10 ASAA0843981 1 20081129 A 5753 FLAP TRACK BOEING 737 737490 1384715 NM TE FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 NR 7 FLAP TRACK HAS EVIDENCE OF CORROSION. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0843984 1 20081126 A 5753 FLAP TRACK BOEING 737 737490 1384715 NM TE FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 NR 2 FLAP TRACK HAS EVIDENCE OF CORROSION. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0843986 1 20081126 A 5753 FLAP TRACK BOEING 737 737490 1384715 NM TE FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 NR 8 FLAP TRACK HAS EVIDENCE OF CORROSION. 2 L 7 2 4F RT A16WE 20081210 WP 2008 12 10 ABXA200812050268 1 20081203 A 4920 360452411 BURNER CAN DOUG DC9 DC941 302207N WP APU DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 958AX 615 47760 STRONG SMELL OF FUEL IN COCKPIT/CABIN WITH APU RUNNING AND AIR FLOW ON. FOUND THE APU NOZZLE COKED UP. REPLACED THE AP U BURNER CAN ASSEMBLY IAW DC9 AMM 49-20-01-2. 2 L 7 2 4F A6WE 20081210 NE 2008 12 10 ABXA200812050267 2 20081126 A 7200 CF680A ENGINE BOEING 767 767281 1385109 NM GE CF6 CF680A 30025 NE RIGHT FAILED A ABXA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 23 798AX 6869 23431 AT APPROXIMATELY 600 FEET ON TAKEOFF, RIGHT ENGINE COMPRESSOR STALLED. EGT EXCEEDANCE OF 1053 DEGREES WAS RECORDED. EN GINE FAILED ON FINAL. REPLACED RIGHT ENGINE IAW JOB CARD 7010. 2 L 7 2 4F 4 F RT A1NM E13NE 20081210 NM 2008 12 10 ASAA0873988 1 20081208 A 5320 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION ON BULKHEAD FLOOR SUPPORT ANGLE. REMOVED FABRICATED NEW SUPPORT AND INSTALLED. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0873989 1 20081208 A 5320 141A5410U12 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CRACK IN INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F RT A16WE 20081209 WP 2008 12 9 UPS08854049 1 20081125 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQUENCE 803-F1-63 REQUIRES AN SDR 15 X 21 INCH EXTERNAL DOUBLER REPAIR AT STA 1326-1348, L9L- L11L CORRELATES TO DC8 SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854050 1 20081016 A 5512 SKIN DOUG DC8 DC871F 302199D WP HORIZ STAB DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV SURVEY SEQ NUMBER 702-S2-08 RT HORIZONTAL STAB UPPER SKIN DOUBLER REPAIR UNABLE TO VALIDATE PER SRM. REPAIRED AS PER UPS EO DC8 5510 31277A. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854052 1 20081128 A 5330 57503223 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 46007 INSPECTION TYPE:N/A AREA OF CORROSION CAUSING RIVET HEADS TO DEFORM ON A/C SKIN LOWER CENTERLINE LOCATED NEAR VHF BLADE ANTENNA. INSTALLED INTERIM REPAIR DOUBLER REF NRC 224311 REF E/O DC8-5330-3135 3-A FOR REPEAT INSP AND PERM REPAIR REQU IREMENTS. THIS IS A MAJOR REPAIR. TRANSFERRED TO D-389557. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854053 1 20081108 A 5230 DOUBLER DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV DOUBLER CRACKED ON UPPER AFT A PIT DOOR. REMOVED AND REPLACED DOUBLER IAW 52-02-00 FIG 2. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854059 1 20081011 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV FLUSH SKIN REPAIR AT STA FS 46.5 DOES NOT CORRELATE TO SRM REPAIR. REPAIRED PER EO DC8 5320 31350 A. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854061 1 20081113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV EXTERNAL SKIN AT BS 694 TO 706 AND L35R ON STRESS PANEL ACCESS DOOR DOES NOT MEET SRM CRITIA SEQ 700- F1-34. REPAIRED AS PER UPS EO DC8 8 5330 31343A. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854062 1 20081105 A 5210 DOUBLER DOUG DC8 DC871F 302199D WP L1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV SEQ 700F108 REPAIR DOUBLER L1 DOOR HAS A CRACK STA 28. REPAIRED IAW 52-02-00 FIG 4. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854063 1 20081106 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV RT WING L/E SKIN DOUBLER DOES NOT MEET SRM LIMITS XFS 623. REPAIR IAW UPS EO DC8 5720 31344 A. 2 L 7 4 4F RT 4A25 20081209 NM 2008 12 9 AALA200820060 1 20081118 A 5340 415N40029 MOUNT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 688AA 55898 25730 AFT LT GALLEY MOUNT FITTING CORRODED, REPLACED FITTING IAW SRM 53-60-51-2R. 2 L 7 2 4F RT A2NM 20081209 WP 2008 12 9 UPS08854067 1 20081107 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV FLUSH SKIN REPAIR BS 184.5 LONG 9R TO 10R DOES NOT MEET SRM CRITIERIA. REPAIRED AS PER EO DC8 5320 3 1349A. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854068 1 20081107 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV FLUSH SKIN REPAIR AT STA 184.5 LONG 9R TO 10R DOES NOT MEET SRM REQUIREMENTS. REPAIR AS PER DC8 5320 31349A. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854069 1 20081113 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV EXTERNAL REPAIR AT BS 348 TO 361 L24R TO L25R DOES NOT MEET SRM REQUIREMENTS. REPAIRED IAW UPS EO DC 8 5320 31346A. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854070 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REP SEQ 803-F1-105, STA 1477-1479, L31L-L32L HAS NO SRM REFERENCE AND REQUIRES APPX F OF EO DC8-5100- 30418C. REMOVED OLD REPAIR. REPAIRED AREA REF DC8 SRM 53-2-1 FIG 7 PER SAA ENGINEERING 81426600001. 2 L 7 4 4F RT 4A25 20081209 2008 12 9 UPS08M54004 4 20081122 A 3417 4059060901 ADC DOUG MD11 MD11F 3023600 NM COCKPIT MALFUNCTIONED A IPXA K NONE N FALSE WARNING CR CRUISE 1 SO 01 289UP 48455 INSPECTION TYPE:N/A DIVERSION - LOSS OF A/S INDICATION & STALL WARNING. T/S PER FIM 34-16-00-1. REPLACED NR 1 CADC PER AMM 34-16-01-4. PERFORMED RTS, PASSED. ALSO PERFORMED RTS ON FCC 1 & 2, PASSED. NO OTHER CURRENT FAULTS NOTED. OK F OR SERVICE. 2 L 7 3 4F RT A22WE 20081209 NM 2008 12 9 UPS08M54060 1 20081128 A 5210 ACA3822512 SKIN DOUG MD11 MD11F 3023600 NM RT DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP 48768 INSPECTION TYPE:N/A 11 INCH CRACK IN RT EDGE OF RT FWD A/C DOOR. REPAIRED PER EO C5240-31269 REPAIR DOUBLER. 2 L 7 3 4F RT A22WE 20081209 WP 2008 12 9 UPS08853989 1 20081013 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQ 803-F1-128, FS 1746, L21L-22L HAS NO SRM REF AND REQUIRES ENG DISPOSITION. REMOVED AND RE PLACED REPAIR DOUBLER IAW SRM 51-21-00, 51-1-8, 53-2-1 FIG 7 AND SAA EA 81427040001. 2 L 7 4 4F RT 4A25 20081210 NM 2008 12 10 ASAA0873990 1 20081208 A 5320 141A5410U16 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CRACK IN INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0873991 1 20081208 A 5320 141A5410U12 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 CRACK IN INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0873993 1 20081208 A 5312 143A948530 BRACKET BOEING 737 737790 13844CN NM BS 500D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION ON LT SIDEWALL TO BULKHEAD ANGLE. REMOVED SUPPORT FABRICATED NEW SUPPORT AND INSTALLED. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0873996 1 20081208 A 5312 143A948534 ANGLE BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON RT SIDEWALL TO BULKHEAD ANGLE. REMOVED AND REPLACED BULKHEAD ANGLE. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0844003 1 20081207 A 5210 REPAIR BOEING 737 7374Q8 138447Q NM L1 DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 L1 DOOR AT PREVIOUS REPAIR TOP AFT CORNER OF REPAIR IS CURLED UP. REMOVED PREVIOUS REPAIR, FABRICATED AND INSTALLED NEW FILLER AND DOUBLER IAW B737 400 SRM 52 00 01. 2 L 7 2 4F RT A16WE 20081211 WP 2008 12 11 AALA200810364 1 20081117 A 5313 LONGERON DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 CORROSION ON LONGERON 30 STATION 218 TO 225. REPLACED 18 INCHES OF LONGERON 30 PER SRM 53-14-01. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 ASOA200801586 1 20081201 A 3350 LENS CNDAIR CL600 CL6002C10 1390015 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 355CA 10067 RIGHT AFT EMERGENCY LIGHT LENS BROKEN. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801639 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RT FLOOR SEAT RAIL FS 485.00 TO FS 581.00 HAS CORROSION DAMAGE (MARKED). REPLACED SEAT TRACK P/N SH670-33426-1 PER AMM 53-00-49-400-801-A03. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801657 1 20081205 A 5320 SPLICE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 CORROSION ON FS 280 BEAM CENTER SPLICE. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801661 1 20081205 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 904EV 7628 AFTER T/O RECEIVED WOW INPUT CAUTION MSG, RETURNED TO GATE. AIRCRAFT RETURNED TO ATL AFTER T/O, EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 20081211 WP 2008 12 11 NWAA085359763 1 20081203 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 763NW 47396 DURING LINE CHECK THE AFT LT OVERWING EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MX REPLACED THE BATTERIES. OPS CHECK WAS GOOD. 2 L 7 2 4F A6WE 20081211 EA 2008 12 11 ASOA200801604 1 20081202 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RT 280 WEB, AFT SIDE HAS MINOR CORROSION. STARTED REMOVING CORROSION ON AFT SIDE OF RT BS 280 WEB PER SRM 51-12-00 AND REMOVED 4 FASTENERS FROM AFT INBOARD CORNER. REMOVED REMAINING CORROSION ON AFT FACE OF RT BS 280 WEB IAW SRM 51-12-00. MECHANICALLY MEASURED BLENDED AREAS ABOVE BS 280 FLOORBEAM, .005 MAX MATERIAL REMOVED. ALL BLENDS WITHIN LIMITS ON R T AFT SIDE OF BS 280 WEB PER SRM 53-11-10. REPLACED REMOVED RIVETS ON RT FS 280 WEB AND RESTORED A023 FINISH IAW SRM 51 -42-06, SRM 51-42-16. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801605 1 20081202 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LT 280 FLOORBEAM, UPPER SURFACE HAS MINOR CORROSION. REMOVED SURFACE CORROSION ON LT 280 FLOORBEAM, UPPER SURFACE PER S RM 51-12-00. PERFORMED UT THICKNESS MEASUREMENT OF BLEND AREA ON LEFT 280 FLOORBEAM IAW NDTM 51-20-004. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801606 1 20081202 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 REPAIR ANGLE AT FS 484, RBL 27 CRACKED. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 DU4R2008256 1 20081120 A 5320 147A5710 SHEAR WEB BOEING 737 7378Q8 13844BX NM BS 1010 CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION, FOUND CORRODED SHEAR DECK AT BS 1010 LBL 31 IN AFT CABIN. 2 L 7 2 4F RT A16WE 20081211 EA 2008 12 11 ASOA200801612 1 20081203 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 RT FS 625.0 ANGLE IS CRACKED. REMOVED AND REPLACED RT FS 625.00 ANGLE IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 DU4R2008250 1 20081120 A 5320 141A5505 FLOOR SUPPORT BOEING 737 7378Q8 13844BX NM BS 340 LBL 22 CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BS 340 LBL 22. 2 L 7 2 4F RT A16WE 20081211 NM 2008 12 11 DU4R2008259 1 20081120 A 5315 147A5505 FLOORBEAM BOEING 737 7378Q8 13844BX NM BS 967 LBL 16 CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION, FOUND CORRODED FLOOR BEAM AT BS 967 LBL 16 IN AFT CABIN. 2 L 7 2 4F RT A16WE 20081211 NM 2008 12 11 DU4R2008258 1 20081120 A 5315 147A5504 FLOORBEAM BOEING 737 7378Q8 13844BX NM BS 947 CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION, FOUND CORRODED FLOORBEAM AT BS 947 LBL 53 IN AFT CABIN. 2 L 7 2 4F RT A16WE 20081211 NM 2008 12 11 DU4R2008246 1 20081120 A 5315 141A5502 FLOORBEAM BOEING 737 7378Q8 13844BX NM BS 294 RBL 0-10 CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION, FOUND CORROSION ON BS 294 FLOORBEAM BL 0 TO BL 10R. 2 L 7 2 4F RT A16WE 20081211 EA 2008 12 11 VNAA2008120400001 1 20081202 A 3350 BA50933901 POWER SUPPLY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A VNAA K NONE L NO TEST UK UNKNOWN 1 GL 05 245PS 81 7919 CREW IN CLT, REPORTED THE FLOOR EMERG LIGHTS INOP IN AFT SECTION. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY BATTE RY & BATT CHARGER /PWR SUPPLY. NO OTHER DEFECTS NOTED AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 USAA920082085 1 20081117 A 5312 BULKHEAD BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 24893 PIT FPBH MAJOR REPAIR LOG NR 4335079 CRACK ON FORWARD SIDE OF FORWARD PRESSURE BULKHEAD SKIN AT BS 178, RBL10, WL234. R EPAIRED FORWARD SIDE OF FORWARD PRESSURE BULKHEAD SKIN AT BS 178, RBL10, WL 234 IAW SRM 53-10-08. 2 L 7 2 4F RT A16WE 20081211 NM 2008 12 11 NWAA085275501 1 20081129 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 501US 23190 DURING AN OVERNIGHT LINE CHECK, THE EMERGENCY EXIT LIGHTS AND EXTERIOR SLIDE ILLUMINATION AT DOOR 3L WERE FOUND TO BE IN OPERATIVE. MX FOUND THE ASSOCIATED POWER SUPPLY TO BE DEFECTIVE AND IT WAS REPLACED. THE SYSTEM OPERATED NORMALLY AFTE R THE DEFECTIVE POWER SUPPLY WAS REPLACED. 2 L 7 2 4F RT A2NM 20081211 EA 2008 12 11 VNAA2008120400010 1 20081130 A 2613 GG670800133 OVERHEAT SENSOR CNDAIR CL600 CL6002C10 1390015 EA RT WING FAILED A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 05 719PS 10177 DURING TAXI WITH WING HEAT ON, CREW RECEIVED MOMENTARY RIGHT WING OVERHEAT RED WARNING MSG. AIRCRAFT RETURNED TO GATE W ITHOUT INCIDENT. MAINTENANCE INSPECTED AND DEFERRED SYSTEM. AIRCRAFT WAS RELEASED FOR SERVICE. AIRCRAFT LEFT THE GATE AND DURING TAXI, CREW RECEIVED MOMENTARY RIGHT WING OVERHEAT RED WARNING MSG. AIRCRAFT RETURNED TO GATE WITHOUT INCIDE NT. MAINTENANCE REMOVED AND REPLACED TEMPERATURE SENSOR. SYSTEM WAS TESTED, DEFERRAL CLEARED AND NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081211 WP 2008 12 11 NWAA085259870 1 20081129 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 779NC 48101 DURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION. 2 L 7 2 4F RT A6WE 20081211 NM 2008 12 11 NWAA085446624 1 20081208 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 624US 21706 DURING AN OVERNIGHT LINE CHECK THE EMERGENCY EXIT SIGNAGE WOULD NOT ILLUMINATE WHEN TESTED. MX FOUND THE ASSOCIATED BA TTERY PACK DEFECTIVE AND REPLACED IT. SYSTEM OPS WAS NORMAL AFTER THE BATTERY PACK WAS REPLACED. 2 L 7 4 4F RT A20WE 20081211 SO 2008 12 11 SWIA200820602 1 20081201 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCHARGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 13723 13723 120287 FLT 5879 - EMERGENCY EXIT LIGHTS OUT. REPLACED AFT BATTERY PACK PN D366-04-001, SN ON 1199, SN OFF 77Y. 2 L 7 2 4T RT A31SO 20081211 WP 2008 12 11 AALA200810374 1 20081125 A 5311 FRAME DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 LEFT OVERWING FUSELAGE FRAME CRACKED STATION 864. REMOVED AND REPLACED LEFT STATION 864 FRAME PER SRM 51-01-00. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810369 1 20081124 A 5340 MOUNT DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 CABIN, CORROSION ON G-2 GALLEY AFT INBOARD FLOOR MOUNT. REPLACED GALLEY MOUNT. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810377 1 20081125 A 5320 ANGLE DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 FORWARD CARGO DOOR LOWER STOP ANGLE CRACKED. REMOVED AND REPLACED ANGLE. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 ASOA200801670 1 20081206 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 FLOORBEAM CAP HAS CORROSION AT RBL 9 BETWEEN FS 517.00 AND FS 533.00. BLENDED CORROSION ON FLOORBEAM CAP ON RBL 9 BETWE EN FS 517.00 & FS 533.00 IAW CRJ 700 SRM 51-21-06. REQUIRES THICKNESS CHECK. RBL 9 FLOORBEAM REPLACED DUE TO OUT OF LI MIT CORROSION. REFER TO W/O 105591 N/R-00390 FOR BEAM REPLACEMENT. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801673 1 20081206 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 469.00 AND FS 485.00. REMOVED AND REPLACED FLOORBEAM AT FS 477 TO 573 P ER REO 670-53-00-172 REV A, CRJ 700 SRM 51-21-06, CRJ 700 SRM 51-11-00, REO 670-53-00-029, CRJ 700 NDTM 51-20-006, CRJ 7 00 51-40-11, CRJ 700 SRM 51-21-11. 2 L 7 2 4F RT A21EA 20081211 WP 2008 12 11 AALA200810380 1 20081202 A 5240 BEAM DOUG DC9 DC983 3022083 WP ZONE 800 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 FORWARD SERVICE DOOR HAS A CRACKED UPPER BEAM AT FORWARD END. REMOVED AND STOP DRILLED CRACK REPLACED BEAM UPPER DOOR. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 ASOA200801676 1 20081206 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 REMOVE CABIN FLOOR SEAT TRACKS FROM FS 581.00 AND AFT (CORROSION FOUND UNDER ALL SEAT TRACKS FWD OF FS 581.00 WITH ALLUM CAPS). REMOVED CABIN FLOOR SEAT TRACKS FROM FS581.00 AND AFT IAW CRJ 700 AMM 53-00-49. VK7025976. REINSTALLED FLOOR SEAT TRACKS LEFT SIDE OF CENTER AISLE FROM VICINITY OF FS830 AFT, AND ALL TRACKS RIGHT SIDE OF CENTER AISLE FROM FS581. 00 AFT IAW CRJ700 AMM 53-00-49. INSTALLED CABIN SEAT FLOOR TRACKS ON LT SIDE OF CENTER AISLE FROM FS581.00 AFT TO FS830. 40 IAW CRJ700 AMM 53-00-49. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 AALA200820074 1 20081118 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 688AA 55898 25730 AFT MAIN DECK PLATE CORRODED. REPAIRED IAW SRM 53-60-51-2R2 2 L 7 2 4F RT A2NM 20081211 NM 2008 12 11 AALA200820076 1 20081122 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 56842 24599 AFT MAIN DECK PLATE CORRODED, REPAIRED IAW SRM 53-60-51-2R2. 2 L 7 2 4F RT A2NM 20081211 EA 2008 12 11 ASOA200801680 1 20081206 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 629.00 AND FS 645.00. BLENDED FLOORBEAM CAP LBL 9 BETWEEN FS629.00 & FS 645.00 IAW CRJ 700 SRM 51-21-06. LBL 9 FLOORBEAM REPLACED DUE TO OUT OF LIMIT CORROSION. REFER TO W/O 105591 N/R-0039 5 FOR BEAM REPLACEMENT. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801682 1 20081206 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 661.00 AND FS 677.00. BLENDED FLOORBEAM CAP LBL 9 BETWEEN FS 661.00 & FS 677.00 IAW CRJ 700 SRM 51-21-06. LBL 9 FLOORBEAM REPLACED DUE TO OUT OF LIMIT CORROSION. REFER TO W/O 105591 N/R-0039 5 FOR BEAM REPLACEMENT. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801685 1 20081206 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 720EV 10115 EMERGENCY EXIT FLOODLIGHT T PAX DOOR INOP. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801688 1 20081206 A 5320 SUPPORT FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 874AS 7551 RT FLOOR SUPPORT FITTING CRACKED AT FS 460.00 RBL 9. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801615 1 20081203 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 CARGO SEAT TRACK AT LBL 9 FS 559+96 IS CORRODED. REMOVED CORRODED CARGO SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-01-11-400-802. DRILLED HOLES IAW SRM 51-41-02. COUNTERSUNK HOLES IAW SRM 51-40-11. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801617 1 20081203 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 879AS 7600 AFT SECTION OF OVERHEAD EMERGENCY LIGHT, BOTH CENTER OVERWING EMERGENCY LIGHTS, AND NR 3 EMERGENCY FLOOD LIGHT INOP. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801621 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RT SIDEWALL SEAT RAIL FS 863.00 TO FS 969.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .007, WITH IN LIMITS PER SRM 53-51-49. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801624 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LT SIDEWALL SEAT RAIL FS 485.00 TO FS 565.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .005, WITHI N LIMITS PER SRM 53-31-49. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801626 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LT SIDEWALL SEAT RAIL FS 565.00 TO FS 661.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .005,WITHIN LIMITS PER SRM 53-31-49. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801627 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RT SIDEWALL SEAT RAIL FS 565.00 TO FS 661.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .010, WITH IN LIMITS PER SRM 53-31-49. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801629 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RT SIDEWALL SEAT RAIL FS 677.00 TO FS 708.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .009, WITHI N LIMITS PER SRM 53-41-49. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801635 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RT FLOOR SEAT RAIL FS 830.40 TO 985.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .010, WITHIN LIMI TS PER SRM 53-51-49. 2 L 7 2 4F RT A21EA 20081209 WP 2008 12 9 UPS08853992 1 20081013 A 5330 SKIN DOUG DC8 DC873F 302199F WP 1740-45,L17-18L MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQ 803-F1-122, FS 1740.5 - 1745.5, L17L-18L (FLUSH REPAIR 3.5- 6.5 INCH) HAS NO, SRM REF AND REQUIRES ENG DISPOSITION. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 51-1-8, 53-2-1 FIG 7, AND SAA EA 81427010001. 2 L 7 4 4F RT 4A25 20081209 NM 2008 12 9 AALA200820062 1 20081118 A 5320 146N5391 PANEL BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 688AA 55898 25730 TRANSITION PANEL CORRODED, REPLACED TRANSITION PANEL IAW SRM 53-60-53-2R. 2 L 7 2 4F RT A2NM 20081209 2008 12 9 HALA2008112400869 4 20081124 A 3400 FMC BOEING 767 76733A 1385209 NM NR 1 MALFUNCTIONED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM -ATB - MCP STUCK IN VERTICAL SPEED MODE WHILE BOTH LNAV AND VNAV INDICATE ENGAGED. UNABLE TO D ISENGAGE VERTICAL SPEED. ABLE TO DISENGAGE VNAV BUT NO EFFECT ON VERTICAL SPEED MODE. CHECK LAST FLT FAULTS WITH MCDP FOUND A/T DISC FMC L/TMC AND A/P CTN MODE ERR. NO PREVIOUS FLT FAULTS FOR LAST 15 FLTS. DURING TEST 1 L AND C NO INFO FCC FMC BUSS IN, RESET BOTH FMC COMPUTERS C/B'S. TEST 1 NOW CHECKS GOOD. TEST 30 CKS GOOD, PER FIM 22-00-031. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20081209 WP 2008 12 9 UPS08853998 1 20081003 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE MISINSTALLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP 12-12 INCH REPAIR DOUBLER INSTALLED WITH BLIND FASTENERS FS 53-65 L31R TO 34R REPAIR SEQ 803-F1-32. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 51-1-8, 53-2-1 FIG 7 AND SAA EA 81425920001. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08853999 1 20081003 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP EXTERIOR SKIN OVAL FLUSH REPAIR HAS 1 EACH RIVET WITH LESS THAN 1.5 E. D. AT STA 1445, L23R REPAIR SE Q 803-F1-46. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 51-1-8, 53-2-1 FIG 7 AND SAA EAA 81425910001. 2 L 7 4 4F RT 4A25 20081209 NM 2008 12 9 QXEA2008120401219 1 20081129 A 5230 417241 SEAL BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR FAILED A QXEA G O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 NM 19 413QX 4060 MFR- AT ABOUT 23,000 FT THE AIRCRAFT RAPIDLY DEPRESSURIZED CABIN PRESS CAUTION LIGHT ILLUMINATED. AFTER DONNING THE O2 MASKS AND STARTING EMERGENCY DESCENT. RAN THE CHECKLISTS. CABIN DESCENDED AT SAME RATE AS AIRCRAFT FOR REMAINDER OF FL IGHT. AFTER LANDING FOUND CARGO DOOR SEAL HANGING LOOSE ON LEFT SIDE COMPLETE DETACHED FROM AIRCRAFT. FERRY TO PDX FOR REPAIRS. REMOVED AND REPLACED AFT CARGO DOOR SEAL IAW Q400 AMM TASK 52-31-26-000-801 AND TASK 52-31-26-400-801. LEAK CHECK GOOD. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081209 NM 2008 12 9 QXEA2008120401221 1 20081128 A 5210 SEAL BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR DIRTY A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 406QX 4048 PDX - REAR PASSENGER DOOR IS HARD TO OPEN AND CLOSE. CLEANED/LUBED SEAL, CHECKS GOOD. RETURNED TO SERVICE. NO PARTS R EPLACED. 2 H 7 2 4T RT A13NM 20081209 NM 2008 12 9 QXEA2008120401220 1 20081128 A 3260 SENSOR BOMBDR DHC8 DHC8402 1390042 NM MLG DOOR OUT OF ADJUST A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 19 418QX 4143 BOI - "R DOOR" GEAR INDICATOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. FERRY TO PDX FOR REPAIR. PSEU - RGDRCL UNREASONABLE FAR, FLT LEG 03. RGDRCL RIGGING NEAR GAP TO O LARGE. ADJUSTED SENSOR S-20 IAW AMM TASK 32-61-06-830-801. FOUND NR 2 MLG FWD DOOR (LEFT DOOR) HAD A GAP BETWEEN FWD END + NACELLE. ADJUSTED DOOR IAW TASK 32-12-11-830-801. PERFORMED OPS TEST OF LANDING GEAR PRIMARY EXTENSION AND RETR ACTION IAW 32-31-00-710-801. TR 32-240. OPS TEST GOOD. GEAR LIGHTS INDICATE NORMALLY. RETURNED TO SERVICE. NO PARTS . 2 H 7 2 4T RT A13NM 20081209 NM 2008 12 9 QXEA2008120401223 1 20081202 A 3260 401020101 PROXIMITY SENSOR BOMBDR DHC8 DHC8402 1390042 NM ZONE 700 DAMAGED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 19 418QX 4143 PDX - RT MAIN GEAR AMBER GEAR DOOR LIGHT ON AFTER T/O. INSPECTED FOUND RT MLG DOOR CLOSED PROX SENSOR UNREASONABLE NEA R FAULT. FOUND EVIDENCE OF CONTACT WITH PROX SENSOR AND TARGET. REMOVED AND REPLACED RGDRCL PROX SENSOR WITH NEW IAW A MM TASKS 32-61-06-000-802 AND 32-61-06-400-802. INSPECTED RT SSV FILTERS NO CONTAMINATION FOUND. PERFORMED OPERATIONAL TEST OF LANDING GEAR IAW AMM TASK 32-31-00-710-801 TR 32-240. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081209 EA 2008 12 9 QXEA2008120401226 2 20081201 A 7532 304768306 BLEED VALVE BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA NR 1 MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 19 424QX 4006 PDX- ON CLIMB THRU 7000', NR 1 PROP SUDDENLY INCREASED TO 1020 RPM. AFTER RESETTING TO 850 RPM IT WAS NOTICED A 4 PERCE NT TRQ SPLIT AND INCREASING WITH ALT APPEARED NR 1 BLEED MAY NOT BE WORKING. NO CAUTION LIGHTS OR MESSAGES NOTICED. RE TURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. REMOVED AND REPLACED P 2.2 BLEED VALVE POWER ASSURANCE RUNS CHEC K GOOD. RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E00062EN 20081209 NM 2008 12 9 QXEA2008120401217 1 20081125 A 6100 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM NR 1 PROP UNKNOWN A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 19 411QX 4055 PDX- NR 1 PROP APPEARS SLOW TO COME OUT OF FEATHER. C/W AMM TASK 61-20-00-720-801 "FUNC TEST OF PROP TIME TO UNFEATHER" TWICE. NR 1 PROP UNFEATHERED AT AROUND 17 SECONDS BOTH TIMES (WITHIN 30 SECOND LIMIT). ALSO C/W OSG TEST IAW TASK 61- 20-00-710-804. OPS TEST GOOD. RETURNED TO SERVICE. COULD NOT DUPLICATE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081210 NM 2008 12 10 AALA200820063 1 20081118 A 5320 143N8001 INTERCOSTAL BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 688AA 55898 25730 INTERCOSTAL TOP ANGLE CRACKED, REPAIRED INTERCOSTAL IAW SRM 51-70-11-0G. 2 L 7 2 4F RT A2NM 20081210 WP 2008 12 10 AALA200810307 1 20081109 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CABIN, CORROSION ON RIGHT CUSP AT STATION 1287 TO 1309. REMOVED DAMAGED CUSP SHEET AND INSTALLED A SERVICEABLE CUSP SHE ET FROM STATION 1250 TO 1309. 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810326 1 20081114 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CORROSION ON LOWER SIDE OF CUSP, STATION 1136 TO STATION 1155. REMOVED CORROSION BY REMOVING DAMAGED DOUBLER AND REPLAC ING WITH NEW DOUBLER PER AARD 53-20-00-16 AND ESO 80559 DATED 11/11/2008. 2 L 7 2 4F RT A6WE 20081208 NM 2008 12 8 FDEA200812035051 1 20081203 A 5311 ACA73511 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 CABIN LEFT FRAME STATION 535 BETWEEN LONGERON 19 AND 20 FOUND WITH CHAFING MARKS. REPAIRED AS PER DRAWING SRZ-53-503. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081208 NM 2008 12 8 FDEA200812035056 1 20081203 A 5310 143N5520 CREASE BEAM BOEING 757 757204 13844CO NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 923FD 26266 EXISTING REPAIR WAS FOUND ON RT CREASE BEAM INNER CHORD BETWEEN BS 760 AND BS 780. EXISTING REPAIR EVALUATED AS PER EO F-5100-75001 PT1 AND FOUND PREVIOUSLY ACCOMPLISHED BY BRITANNIA AIRWAYS LIMITED REPAIR NR RS/757/53/694 ISSUE 1. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20081208 NM 2008 12 8 FDEA200812035057 1 20081203 A 5310 143N55207 CREASE BEAM BOEING 757 757204 13844CO NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 923FD 26266 EXISTING REPAIR WAS FOUND ON RT CREASE BEAM INBOARD CHORD AT BS 660. TO EVALUATE AND REPAIR AS REQUIRED. EXISTING REPA IR EVALUATED AS PER EO F-5100-7-5001 PT1 AND FOUND PREVIOUSLY ACCOMPLISHED BY BRITANNIA AIRWAYS LIMITED REPAIR NR RS/757 /53/727 ISSUE 1. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20081208 NM 2008 12 8 FDEA200812035058 1 20081203 A 5310 144N52103 CREASE BEAM BOEING 757 757204 13844CO NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 923FD 26266 EXISTING DOUBLER REPAIR WAS FOUND ON LT CREASE BEAM WEB BETWEEN BS 1060, LBL 70. TO EVALUATE AND REPAIR AS REQUIRED. E XISTING REPAIR EVALUATED AS PER EO F-5100-7-5001 PT1 AND FOUND PREVIOUSLY ACCOMPLISHED BY BRITANNIA AIRWAYS LIMITED REPA IR NR RS/757/53/732 ISSUE 1. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20081208 NM 2008 12 8 FDEA200812035059 1 20081203 A 5315 141N51121 FLOORBEAM BOEING 757 757204 13844CO NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 923FD 26266 EXISTING REPAIR WAS FOUND ON CABIN FLOORBEAM UPPER CHORD AT BS 365.25 BETWEEN RBL 18 AND RBL 54. TO EVALUATE AND REPAI R AS REQUIRED. EXISTING REPAIR EVALUATED AS PER EO F-5100-7-5001 PT1 AND FOUND REPAIR WAS PREVIOUSLY ACCOMPLISHED LIM ITED REPAIR NR RS/757/53/1099 ISSUE 1. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20081208 NM 2008 12 8 FDEA200812035060 1 20081203 A 5311 65564416 FAILSAFE BOEING 727 727227 1384078 NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 495FE 21669 AFT CARGO COMP BS 950 AT STR 29R OTBD SIDE HAS LEVELING COMPOUND CRACKED, BELOW FAILSAFE. CORROSION ON FAILSAFE BS 950 STR 29R TO STR 28R. REMOVED LEVELING COMPOUND AND FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1 FIG 1. CUT OUT DAMAGE AREA IAW SRM 51-10-1 AND 51-40-4 FIG 1. FABRICATED REPAIR ANGLE AND REPAIR FILLER IAW SRM 51-40-4 FIG 1 AND 53-10-2 FIG 5. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-40-4 FIG 1 AND 51-30-2. REAPPL IED LEVELING COMPOUND IAW SOPM 20-41-05. 2 L 7 3 4F A3WE 20081208 NM 2008 12 8 HALA08112300871 1 20081123 A 3340 LIGHT BOEING 767 7673CB 1385187 NM LT WING INOPERATIVE A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 592HA 28141 A/C GRD DAMAGE TO LT AFT WING TIP NAV LIGHT ASSY (BOTH BULBS WORK). REMOVED AND REPLACED LT WING AFT NAV LIGHT ASSY PER MM 33-43-00, OPS NML. 2 L 7 2 4F RT A1NM 20081208 NM 2008 12 8 SWAA086781 1 20081203 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT RADIO ALTIMETER SKIN CUTOUT, BS 450. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086756 1 20081202 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 24R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086766 1 20081203 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 221WN 34259 FOUND EMERGENCY EXIT LIGHT LENS COVER MISSING AT ROW 1. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086770 1 20081203 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 22L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 FDEA200812035063 1 20081203 A 5310 65198615 SPAR BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 495FE 21669 CORROSION IN NLG LT STRUT DOOR SPAR BOX, APPX FUSELAGE STA 290. REMOVED WEB IAW SRM 51-30-2 AND REMOVED CORROSION IAW S RM 51-10-6. FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. REMOVED 2ND WEB LT AREA FOR ACCESS IAW SRM 51-30-2 AND REMOVED NLG SPAR IAW SRM 51-30-2. REMOVED EXISTING CORROSION FROM SPAR IAW SRM 51-10-6 AND EA 7-5310-126865. TREATED AND PRIME D SPAR IAW SRM 51-10-2 & EA 7-5310-126865. FABRICATED REPAIR ANGLE FROM BAC 1503-101053 IAW FEDEX EA 7-5310-126865. TR EATED AND PRIMED ANGLE. INSTALL REPAIR PARTS IAW EA 7-5310-126865 AND SRM 51-30-2. 2 L 7 3 4F A3WE 20081208 NM 2008 12 8 SWAA086789 1 20081203 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086832 1 20081204 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 496WN 32478 DURING SCHEDULED HC2 CHECK, FOUND MID LT EMERGENCY EXIT BATTERY FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086793 1 20081203 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 996, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086802 1 20081203 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086833 1 20081204 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 496WN 32478 DURING SCHEDULED HC2 CHECK, FOUND AFT RT EMERGENCY EXIT BATTERY FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086834 1 20081203 A 5512 65C25727 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER CRACKED AT REAR SPAR, BS 97 FWD OF PANEL 9106L. REPAIRED SKI N PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086839 1 20081204 A 5753 65C26320 FITTING BOEING 737 7373H4 1384600 NM MID FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND RT WING O/B MID FLAP I/B SUPPORT FITTING CORRODED. REPAIRED FITTING PER PAE ER. 2 L 7 2 4F RT A16WE 20081208 EA 2008 12 8 SWIA200820570 1 20081201 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA WINDOW POST CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 WINDSHIELD CENTER POST LOWER RIGHT FITTING AT WL 110.0 IS CRACKED IN THE BEND RADIUS, AD INSP. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081208 SO 2008 12 8 SWIA200820572 1 20081008 A 5310 WINDOW FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 566SW 120341 C-CHECK, LEFT FRAME WEB CRACKED, AFT OF CENTER DV WINDOW FRAME. REPAIRED PER SRM. 2 L 7 2 4T RT A31SO 20081208 EA 2008 12 8 SWIA200820573 1 20081130 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 947SW 7786 FLT 6600 - AFT OVERHEAD EMERGENCY FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081208 NM 2008 12 8 SWAA086803 1 20081203 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, BETWEEN STR 26R, TO STR 27R. REPAIRED FRAME PER SR M. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086850 1 20081204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 859, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 SWAA086856 1 20081204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 18L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081208 EU 2008 12 8 UALA2008120306734 1 20081202 A 5320 BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 405UA 452 BEAM 210 NEEDS REPLACED. STARTED REMOVAL OF BEAM. INSTALLED NEW BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081208 EU 2008 12 8 UALA2008120306736 1 20081202 A 5320 BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 405UA 452 BEAM 95 HAS CORROSION. INSTALLED NEW BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081208 EU 2008 12 8 UALA2008120306737 1 20081203 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 405UA 452 DOOR 2R SILL PLATE HAS CORROSION IN SEVERAL PLACES. REMOVED SILL PLATE. REPLACED DOOR 2R SILL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081208 NM 2008 12 8 UALA2008120406746 1 20081203 A 5200 F1314 SPRING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DOOR WEAK A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 LT AFT MED DEPLOYMENT BAR GAS SPRING WEAK. REPLACED GAS SPRINGS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081208 NM 2008 12 8 UALA2008120406756 1 20081204 A 3350 3071BPEGPL LAMP BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 783UA 26950 SEAT EMERGENCY LIGHTS INOP AT SEATS 3F AND 24C. RELAMPED SEAT 24C AND REPLACED LENS. SEAT 3F NEEDS ELEC HARNESS 566-13 75 AOG T0501. SIDE OF SEAT REMOVED FOR ACCESS. REPLACED HARNESS AND LT ASSY AND CHECKED 3F EMERGENCY LIGHTS, WORKS NOR MAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081208 NE 2008 12 8 UALA2008120406757 2 20081203 A 7261 OIL SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE MALFUNCTIONED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 29 550UA 25398 726545 NR 2 ENGINE OIL PRESSURE LOSS. FLIGHT DIVERTED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081208 NM 2008 12 8 BJNA081101 1 20081118 A 3350 3071 LIGHT BOEING 737 737400 138449A NM CABIN INOPERATIVE E BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 42XA 25729 L1 DOOR INTERIOR EMERGENCY EXIT LIGHT AS BURNED OUT BULB. RE-LAMPED EMERGENCY EXIT LIGHT IAW AMM. (K) 2 L 7 2 4F RT A16WE 20081208 SO 2008 12 8 SIMA200833804 1 20081202 A 3040 3801D2 CONTROLLER EMB 145 EMB145 3260210 SO WINDOW HEAT MALFUNCTIONED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 613AE 145081 ON FLIGHT 9805 CREW REPORTED ON CLIMB-OUT STRONG ODOR OF SMOKE IN COCKPIT. CREW RETURNED TO FIELD WITHOUT INCIDENT. AI RCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT WINDSHIELD CONTROLLER IAW AMM 30-42-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081208 EU 2008 12 8 FDEA200811264987 1 20081126 A 5712 A5724081021400 RIB AIRBUS 300 A300B4622R 3930312 EU LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 LEFT WING RIB 5; HOLE "M" HAS A CRACK INDICATION. COMPLIED WITH FEDEX EA 6-5710-123674, WINGS - AD 99-16-01 - E.O. 6-5 710-7-5005, LT WING REAR SPAR, RIB 5 FITTING BOLT HOLE "G", "I", "M" AND "O". ORGINAL EA IS ATTACHED TO SNRM N00846. 2 L 7 2 4F RT A35EU 20081208 NM 2008 12 8 UALA2008120206723 1 20081202 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT LIGHTS INOP IN BUSINESS CLASS CEILING DOORS 1 THRU DOORS 2 LEFT AND RIGHT. REPLACED BATTERY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081208 2008 12 8 UALA2008120106698 4 20081129 A 2565 D31591478U1 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU R1 DOOR OUT OF ADJUST A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 929UA 26652 DOOR 1 RIGHT SLIDE NEEDS ADJUSTING AS PER FLIGHT CREW. ADJUSTED DOOR SLIDE IN SLIDE HOLDER. 2 L 7 2 4F 4 F RT A16WE E21EU 20081208 EU 2008 12 8 FDEA200811264988 1 20081126 A 5712 A5724081021400 RIB AIRBUS 300 A300B4622R 3930312 EU LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 LEFT WING RIB 5; HOLE "O" HAS A CRACK INDICATION. COMPLIED WITH FEDEX EA 6-5710-123674, WINGS, AD 99-16-01 - EO 6-5710 -7-5005, LT WING REAR SPAR, RIB 5 FITTING BOLT HOLE "G", "I", "M", AND "O". 2 L 7 2 4F RT A35EU 20081208 NM 2008 12 8 USAA920082083 1 20081008 A 5311 654795911 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL C21 MAJOR REPAIR NR 6056756 CORROSION ON FRAME UPPER FLANGE AT BS807 BETWEEN S16R TO S27R. REPAIRED FRAME UPPER FLA NGE AT BS807, BETWEEN S16R TO S27R IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081208 NM 2008 12 8 UALA2008120106681 1 20081126 A 2560 140N276217 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR LACK OF LUBE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 516UA 24860 DOOR 1L DIFFICULT TO ARM. LEVER VERY TIGHT. CHECKED GIRT BAR AREA AND LUBED, CK'D GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081209 CE 2008 12 9 GUUA93854112308A 1 20081123 A 5410 1181200363 KEELBEAM BEECH 1900 1900D 1154162 CE LT NACELLE CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81538 UE199 AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT NACELLE KEEL HAS A .75 INCH CRACK. STOP DRILLED CRACK AND INSTALLED RE PAIR DOUBLERS. 2 L 7 2 4T RT A24CE 20081209 NM 2008 12 9 UALA2008112506672 1 20081125 A 2750 667602 MODULE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAP NO TEST A UALA O OTHER W INADEQUATE Q C AP APPROACH 1 WP 29 550UA 25398 TRAILING EDGE FLAP ASYMMETRY ON FINAL APP BETWEEN 15 & 20. FOUND THE NR 8 JACKSCREW STOP OUT OF RIG. PERFORMED A COMPLE TE RE-RIG OF RT OUTBOARD FLAP. ACP FIM 27-51-60, FAILED DEPRESS MODULE OPS CHECK FOR UNCOMMANDED MOTION. REPLACED MODUL E MR 27597 ON CARD 33130. HAND ROLLED FLAPS IAW FIM 27-51-00, NO BINDING NOTED THROUGH FULL RANGE OF MOTION. ACP INSP OF RT OB FWD & AFT FLAP TRACKS AND ROLLERS, NO BINDING, FLAT SPOTS OR SIGNS OF WEAR NOTED, ADJUSTED LESA & LESB (SLAT FOLL OW UP) TO IN LIMITS. ACP FLAP-SLAT RIG CHECKED ALL GOOD. CHECKED WIRING FROM FSEU-1 AND FSEU-2 (ALL GOOD). NO INDICATOR POP NOTED ON ALL TRANSMISSION OR FLAP DISAGREE MESSAGES. 2 L 7 2 4F 4 F RT A2NM E17NE 20081209 NE 2008 12 9 UALA2008112606673 2 20081126 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 1 MAKING METAL A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 229UA 30557 222139 METAL IN NR 1 ENGINE CHIPS AND OIL SCREEN. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081209 EU 2008 12 9 FDEA200811255074 1 20081125 A 5730 A5734008722400 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 RT WING LWR SKIN CRACKED APPROX 3/16 INCH BEYOND PREVIOUS STOP PLUG REPAIR. CRACK IS PROGRESSING AFT TOWARD FASTENER HO LE NR 19 AND TRANSITION RADIUS BETWEEN RIBS 8 AND 9. COMPLIED WITH EA 6-5730-123509 PART 1, WINGS CRACK IN RT BOTTOM SK IN AT FRONT SPAR, 632BB RIB 8 - 9 REPAIR. 2 L 7 2 4F RT A35EU 20081209 EU 2008 12 9 FDEA200812045075 1 20081204 A 5730 A5734008722000 SKIN AIRBUS 300 A300B4622 3930401 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 RT WING LOWER LEADING EDGE CRACKED AT CUTOUT FOR PANEL 613AB, CRACK EXTENDS AT BOTH ENDS OF FASTENER HOLE. DRILLED CRAC K STOP HOLE IAW SRM 53-15-63 PG 202 STEP 2. FABRICATED DOUBLERS IAW SRM 53-15-63 PG 209-210. ALODINED, PRIMED, AND PAI NTED IAW AMM 51-23-10-0. INSTALLED DOUBLERS IAW SRM 53-15-63 PG 209-210. 2 L 7 2 4F RT A35EU 20081209 NM 2008 12 9 FDEA200812055088 1 20081205 A 5313 AFA7105513 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 AFT CARGO COMPARTMENT RIGHT TUNNEL, LONGERON SPLICE FITTING CRACKED AT STATION 1861 L-38. REMOVED AND REPLACED AS PE R SRM 51-33-01 VOLUME II WITH NEW FABRICATED LONGERON SPLICE AS PER DRAWING AFA7105. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081209 NM 2008 12 9 FDEA200812055089 1 20081205 A 5340 65C1612924 BRACKET BOEING 727 7272D4 138407U NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 RADAR R/T SHELF TRAY CRACKED AT AFT RT AND LT FOOT REMOVED AND REPLACED RT SHELF REF SRM 51-30-02. 2 L 7 3 4F A3WE 20081209 WP 2008 12 9 FDEA200812055092 1 20081205 A 5754 ARB1619501 SKIN DOUG DC10 DC1030F 3023504 WP NR 2 SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 DURING REPAIR ACCOMPLISHMENT PER NRC NR N00497 FOUND ON LT WING NR 2 SLAT CRACK ON INNER SKIN. 2 L 7 3 4F RT A22WE 20081209 NM 2008 12 9 FDEA200812045084 1 20081204 A 3230 656021123 ACCESSORY UNIT BOEING 727 727227 1384078 NM MLG ILLUMINATED A FDEA A UNSCHED LANDING J J WARNING INDICATION WARNING INDICATION CL CLIMB 1 CE 21 489FE 21492 LANDING GEAR HANDLE FAILED TO RETRACT ABOVE OFF POSITION AFTER TAKEOFF, ACCOMPANIED BY ILLUMINATION OF ALL LIGHTS ON GEA R ANNUNCIATOR LIGHT PANEL UP FRONT AND RT MAIN GEAR DOOR LIGHT ON S/O PANEL. RAN QRH BUT FAILED 1ST TEST STEP. RECONFI GURED FOR LANDING WITH NORMAL INDICATIONS. UNEVENTFUL LANDING. REPLACED LANDING GEAR ACCESSORY UNIT AND TEST GOOD IAW MM 32-09-122-5. 2 L 7 3 4F A3WE 20081209 EA 2008 12 9 SWIA200820578 1 20081004 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 466SW 7856 C-CHECK, FS 280 FLOORBEAM RBL9 UPPER FLOOR SUPPORT CRACKED IN RADIUS. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081209 NM 2008 12 9 HNAA2008120200338 1 20081202 A 2150 78279018 ACM DHAV DHC8 DHC8102 2809003 NM APU BAY CONTAMINATED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 814HA 24275 14 318 WHEN THE APU BLEED AIR WAS SELECTED 'ON', THE CABIN FOGGED UP AND SMELLED LIKE OIL. MAINTENANCE REMOVED AND REPLACED TH E AIR CYCLE MACHINE. THE APU WAS RUN UP AND THE SYSTEM CHECKED GOOD. NO ODORS OR FUMES NOTED AT THAT TIME AND THE AIRC RAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 20081209 WP 2008 12 9 AALA200810286 1 20081117 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 LEFT TIE DOWN TRACK CORRODED AT FASTENER HOLES, STATION 1220-1322. REMOVED AND REPLACED LEFT TIE DOWN TRACK, STATION 12 20-1322. 2 L 7 2 4F RT A6WE 20081209 WP 2008 12 9 AALA200810288 1 20081117 A 5330 DOUBLER DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 RIGHT STATIC PORT PLATE DOUBLER RING HAS SEVERAL SMALL AREAS OF CORROSION. REMOVED AND REPLACED RIGHT STATIC PORT DOUBL ER RING. 2 L 7 2 4F RT A6WE 20081209 WP 2008 12 9 AALA200810283 1 20081114 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION ON CUSP. REMOVED AND REPLACED CUSP. 2 L 7 2 4F RT A6WE 20081209 WP 2008 12 9 AALA200810289 1 20081126 A 5310 39240869 BEAM DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CARGO DOOR TOP BEAM HAS A CRACK. REMOVED AND REPLACED BEAM ASSEMBLY. 2 L 7 2 4F RT A6WE 20081209 WP 2008 12 9 UPS08854048 1 20081125 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQUENCE 803-F1-64 REQUIRES AN SDR 4 X 9 INCH EXTERNAL DOUBLER REPAIR AT STA 1334-1349 L11L CO RRELATES TO DC8 SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 20081209 EA 2008 12 9 N6WA200812021 1 20081202 A 5610 NP139321003 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FAILED A N6WA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 166GJ 282 10266 RIGHT WINDSHIELD SHATTERED. REPLACED RIGHT WINDSHIELD. 2 L 7 2 4F RT A21EA 20081209 WP 2008 12 9 UPS08854058 1 20081011 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EXTERNAL SKIN AT STA FS 380 DOES NOT MEET SRM REQUIREMENTS. REPAIR PER UPS EO DC8 5330 31348A. 2 L 7 4 4F RT 4A25 20081209 NM 2008 12 9 UPS08554051 1 20081125 A 2120 UNKNOWN BOEING 757 75724APF 1384969 NM COCKPIT ODOR A IPXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 438UP 25469 31506 INSPECTION TYPE:N/A NOTICED ODOR AND LIGHT HAZE IN COCKPIT DURING CLIMB. FOUND FUEL IN NR 2 ENGINE OIL SYSTEM. PER FIM CHANGED NR 2 ENGINE LOW PRESSURE AND HIGH PRESSURE FUEL PUMPS, FFG, FCOC AND FCOC BYPASS VALVE. ALSO PERFORMED DUCT BU RNOUT OF PNEUMATIC DUCT SYSTEM. 2 L 7 2 4F RT A2NM 20081209 WP 2008 12 9 UPS08854033 1 20081023 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQ 803-F1-136 AT STA 510, BETWEEN L29 TO 30L HAS NO SRM REF AND REQUIRES APPX F OF EO DC8-510 0-30418C. ACCOMPLISH APPX F, REMOVED OLD REPAIR, FABBED NEW REPAIR AND INSTALLED IAW TR53-203 OF SRM 53-2-1 PARG 16 AS PER SAA EA 81427420. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854034 1 20081023 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQ 803-F1-137 AT STA 518, BETWEEN L25L TO 26L HAS NO SRM AND REQUIRES APPX F OF EO DC8-5100-3 0418C. ACCOMPLISHED APPX F, REMOVED OLD REPAIR, FABBED AND INSTALLED NEW REPAIR IAW TR 53-203 OF SRM 53-2-1 PARG 16B A S PER SAA EA 81427410001. 2 L 7 4 4F RT 4A25 20081209 NM 2008 12 9 UPS08554029 1 20081125 A 2120 UNKNOWN BOEING 757 75724APF 1384969 NM COCKPIT ODOR A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 438UP 25469 INSPECTION TYPE:N/A AIR TURNBACK AT 1020Z DURING CLIMBOUT AT APPROX 15,000FT, NOTICED AN ODOR IN THE COCKPIT FOLLOWED A MINUTE OR TWO LATER BY THE PRESENCE OF A LIGHT HAZE. DURING THE SMOKE/FUMES CHECKLIST NOTICED THE RIGHT ENGINE OIL PRES SURE IN THE AMBER BAND (OIL QUANTITY WAS GOOD). MAINTAINED PRESS IN THE NORMAL. *SDR FILED OPEN* 2 L 7 2 4F RT A2NM 20081209 WP 2008 12 9 UPS08854006 1 20081122 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:N/A L1 DOOR HOLD OPEN LATCH AT FS 16 BETWEEN LONGERONS L-15L AND L-16L CRACK AT LOWER AFT CORNER OF PROD UCTION TRIMOUT. THE CRACK AND EXISTING STOP DRILL MEASURES 0.70 INCH LENGTH. COMPLIED WITH EO DC8-5330-31311-A. 2 L 7 4 4F RT 4A25 20081210 WP 2008 12 10 AALA200810304 1 20081107 A 5320 CASTING DOUG DC9 DC983 3022083 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 AFT ENTRY DOOR JAMB STATION 1338, RIGHT MID STOP CASTING CRACKED. INSTALLED SERVICEABLE CASTING PER SRM 51-01. 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810327 1 20081113 A 5321 FLOORBOARD DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CORROSION ON INBOARD SIDE STATION 1174. INSTALLED 8 INCH BY 14 INCH DOUBLER PER AARD 53-20-00-23. 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810298 1 20081121 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 AFT CARGO, CORROSION ON LIP OF LEFT TIE DOWN TRACK. REMOVED AND REPLACED SECTION OF TRACK FROM STATION 1090 TO 1212. 2 L 7 2 4F RT A6WE 20081209 NM 2008 12 9 UALA2008112606674 1 20081125 A 2432 425402 CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE APU BATTERY INOPERATIVE A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 173UA 24380 BATTERY CHARGER APU STATUS MSG. REPLACED APU CHARGER AND CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081209 EU 2008 12 9 UALA2008112506664 1 20081124 A 3350 321431 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 486UA 1620 FWD BATTERY PACK INOP ON PSU 10WL. REPLACED BATTERY PACK, CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20081209 EA 2008 12 9 A6WA200840596 1 20081014 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ODOR A A6WA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 401AW 7280 WHEN TURNING ON BOTH PACKS SMOKE ODOR IN COCKPIT. ACFT PARKED AT GATE AFTER PACKS TURNED OFF SMOKE ODOR SUBSIDED. INSP ECTED APU AND AIR CYCLE MACHINE ACM AREA, NO FAULTS FOUND. TESTED ACM TEST CONTROL SYSTEM, AIR SYSTEM CHECKS GOOD IAW A MM 21-51-00, NO SMOKE OR ODORS NOTED. 2 L 7 2 4F RT A21EA 20081209 NM 2008 12 9 UALA2008111304326 1 20080814 A 2820 32C171 CHECK VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT BOOST PUMP FAILED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 773UA 26929 UNWANTED FUEL TRANSFER INTO LEFT MAIN TANK FROM CENTER TANK. FUEL TRANSFER FROM RIGHT MAIN TANK INTO LEFT MAIN TANK ALS O WITH CROSS FEED OPEN. FOUND LEFT FWD BOOST PUMP DISCHARGE CHECK VALVE FAILED AND FOD'D OUT PUMP AND HOUSING. REPLACE D LEFT MAIN TANK FWD BOOST PUMP (P/N 568-1-29115-004). REPLACED FMU (P/N 808800-1). REPLACED FUEL CONTROL SWITCH (P/N D738-01-001), REPLACED RELAYS FUEL CONT LEFT TD L K76107 AND GEN IGN L K76104. RT OUTBOARD FILL VALVE LEAKING. REPLACE D PACKING IN RT OUTBOARD REFUEL CONTROL UNIT. LEAK CHECK NORMAL. REPLACED ENG NR 1 & NR 2 FUEL FILTER ELEMENTS. RAN E NGINE FOUR TIMES EACH TIME ENGINE SHUT DOWN NORMAL. VERIFICATION FLIGHT COMPLIED WITH BY FLIGHT CREW (FLT 109-23). 2 L 7 2 4F 4 F RT T0001SE E46NE 20081209 NM 2008 12 9 UALA2008112506669 1 20081125 A 5414 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 PYLON CRACKED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 NR 1 PYLON INBOARD SIDE SKIN CRACKED AT UPPER AFT CORNER OF CUTOUT FOR PANEL 416BR. MAJOR REPAIR ACCOMPLISHED. REMOVED HINGE FITTING, STOP DRILLED THE CRACK AND PERFORMED HFEC TO VERIFY CRACK CONTAINMENT. FABRICATED AND INSTALLED A REPAI R DOUBLER-TRIPLER. 2 L 7 2 4F 4 F RT A1NM E24NE 20081209 NM 2008 12 9 UALA2008112606675 1 20081125 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 B-ZONE EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY LIGHT. OPS CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081209 NM 2008 12 9 FDEA200812045081 1 20081204 A 5315 FLOORBEAM BOEING 727 7272S2F 1384O81 NM BS 1176 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 MAIN DECK FLOOR BS 1176.5 CHORD HAS CORROSION ON UPPER FWD FLANGE AND INSIDE FASTENER HOLES FROM RBL 1 TO 24. REPLACED CHORD REF SRM 51-30-02, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081209 2008 12 9 PIDA08035 4 20081126 A 2565 LIGHT BOEING 757 757256 1384925 NM CONTROL PANEL NO TEST A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 801DM 1 1 26240 RIGHT OVERWING SLIDE BOTTLE PRESSURE LIGHT DOES NOT TEST ON P-61 PANEL. 2 L 7 2 4F RT A2NM 20081209 EA 2008 12 9 SWIA200820582 1 20081004 A 7120 BUSHING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 466SW 7856 C-CHECK, LEFT ENGINE YOKE ATTACH BUSHINGS ARE CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081209 WP 2008 12 9 AALA200810268 1 20081110 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 LEFT CUSP CORRODED, STATION 789 TO STATION 804. INSTALLED NEW CUSP SHEET AT LEFT CUSP, STATION 789 TO STATION 804. 2 L 7 2 4F RT A6WE 20081209 WP 2008 12 9 AALA200810269 1 20081109 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CORROSION, BLENDED OUT OF LIMITS. PART REPLACED PER 51-00-00. 2 L 7 2 4F RT A6WE 20081209 NM 2008 12 9 AALA200802358 1 20081019 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 796AN 30796 DFW - EMERGENCY LIGHT AT SEAT 31G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081209 WP 2008 12 9 AALA200810290 1 20081120 A 5330 SKIN DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CORROSION INTERIOR SIDE OF FUSELAGE SKIN FORWARD OF STATION 731 BETWEEN LONGERON 30 AND LONGERON 29 RIGHT. SPLICED IN S ECTION OF SKIN PER SRM 53-04-00 12C SHEET 3. 2 L 7 2 4F RT A6WE 20081209 WP 2008 12 9 AALA2008102 1 20081110 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 FLOORBOARD SUPPORT CRACKED AT STATION 845. INSTALLED NEW FLOORBOARD SUPPORT PER SRM 51-01. 2 L 7 2 4F RT A6WE 20081209 NM 2008 12 9 AALA200802359 1 20080827 A 3350 PBS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 MIA - EMERGENCY EXIT LIGHTS AT RIGHT LEFT OVERWING AND EMERGENCY LIGHTS AT SEATS 20H AND 21H INOPERATIVE. REPLACED BATT ERY PACK FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081210 NM 2008 12 10 USAA2008120992200 1 20081209 A 2560 R2070001214 FLASHLIGHT BOEING 767 7672B7ER 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 253AY 24894 BFM - C4 - EEL - FORWARD FLIGHT ATTENDANT POSITION EMERGENCY FLASHLIGHT INOP. REPLACED FORWARD FLIGHT ATTENDANT POSITIO N EMERGENCY FLASHLIGHT. 2 L 7 2 4F RT A1NM 20081210 NM 2008 12 10 USAA2008120992201 1 20081208 A 3350 S283T0143 POWER SUPPLY BOEING 767 7672B7ER 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 253AY 24894 BFM - C4 - EEL - BATTERY PACK ASSEMBLY UNDER THE FORWARD ATTENDANT SEAT INOP. REPLACED M1206 EMERGENCY LIGHT POWER SUPP LY FUSE IAW B767 WDM 33-51-21 & AMM 33-51-07. 2 L 7 2 4F RT A1NM 20081210 NM 2008 12 10 USAA2008120992206 1 20081205 A 5320 INTERCOSTAL BOEING 737 7374B7 138449C NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - EXFOLIATION CORROSION ON INTERCOSTAL AT BS 967 TO BS 986.5, RBL 18. REPLACED INTERCOSTAL AT B S 967 TO BS 986.5, RBL 18 IAW B737 SRM 53-60-51 & SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 AALA200802343A 1 20081016 A 2750 FSEU BOEING 737 737823 13844CB NM TE FLAPS FAILED A AALA O OTHER O OTHER AP APPROACH 1 SW 21 917AN 29518 DFW INFLIGHT - ON APPROACH FLAPS WOULD NOT EXTEND. GAUGE SHOWED NEEDLE SPLIT AT ZERO DEGREES. LEADING EDGE DEVICES EXT ENDED BY ALTERNATE FLAP SWITCH. LANDED DFW WITHOUT INCIDENT. REPLACED FLAP SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20081210 WP 2008 12 10 AALA200802356A 1 20081019 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 418AA 49329 LGA - EMERGENCY LIGHTS AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT NUMBER O NE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081210 EU 2008 12 10 AALA200802367A 1 20081020 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU ZONE 200 DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14065 508 MIA - EMERGENCY LIGHTS AT SEATS 19C TO 28C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 19C TO 28C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081210 EU 2008 12 10 AALA200802368A 1 20081020 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14065 508 MIA - EMERGENCY LIGHTS AT SEATS 1G TO 5G INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 1G TO 5G. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081210 NM 2008 12 10 AALA200802352A 1 20081017 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 196AA 32390 MIA - EMERGENCY LIGHT AT SEAT 32D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 32D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 20081210 EU 2008 12 10 AALA200802354A 1 20081016 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33069 512 JFK - EMERGENCY LIGHTS AT SEAT ROW 9F INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 9F. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081210 NM 2008 12 10 AALA200802360A 1 20081019 A 2750 9004213 SENSOR BOEING 737 737823 13844CB NM FLAP SYSTEM FAILED A AALA O OTHER J WARNING INDICATION DE DESCENT 1 SW 21 923AN 29524 MSP INFLIGHT - TRAILING EDGE FLAPS ASYMMETRY. LANDED MSP WITHOUT INCIDENT. REPLACED NUMBER EIGHT FLAP POSITION SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 FDEA200812065097 1 20081206 A 5512 SKIN BOEING 727 7272S2F 1384O81 NM ZONE 300 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 216FE 22937 FOUND RT STAB UPPER SURFACE EXTERNAL REPAIR LOCATED AT APPROX SS 145 8 INCHES FWD OF AFT EDGE. REPAIR REQUIRES EVALUATI ON FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA FOUND REPAIR DOES NOT COMPLY WITH CURRENT SRM REPAIR. REMOVED PREVIOUS REPAIR, LAID OUT TWO ADDITIONAL ROWS OF FASTENERS ON INBD SIDE OF DAMAGE CUT OUT. FABRICATED NEW REPAIR DOUBLER, TREATED, PRIMED, AND INSTALLED REF SRM 55-10-3/FIGURE 3. THIS IS CLASSIFIED AS A M AJOR REPAIR. THIS IS CATEGORY "C" REPAIR, EA 7-5510-118322. 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 FDEA200812065098 1 20081206 A 5512 SKIN BOEING 727 7272S2F 1384O81 NM ZONE 300 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 216FE 22937 FOUND RT STAB UPPER EXTERNAL REPAIR LOCATED AT APPROX SS 180, 6 INCHES FWD OF AFT EDGE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. FOUND REPAIR DOES NOT COMPLY WIT H CURRENTS SRM REPAIR. REMOVED PREVIOUS REPAIR, LAID OUT TWO ADDITIONAL ROWS OF FASTENERS ON INBD SIDE OF DAMAGE CUTOUT . FABRICATED NEW REPAIR DOUBLER, TREATED, PRIMED AND INSTALLED, REF SRM 55-10-3/FIGURE 3, AND FED EX EA 7-5510-118314. THIS IS CLASSIFIED AS A MAJOR REPAIR. THIS IS A CATEGORY "C" REPAIR. 2 L 7 3 4F A3WE 20081210 EU 2008 12 10 FDEA200812065099 1 20081206 A 5320 A53612120202 WEB AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 429FE 364 FRAME 1 FWD FACE AT RADOME ACCESS HAS 4 EA AREAS OF SKIN CORROSION, APPROX 7 SQ INCHES REMOVED LEVEL 1 CORROSION AND INS TALLED REPAIR DOUBLER ON WEB FLANGE AT FRAME 1 IAW FEDEX EA 6-5310-124171, RELEASE DATE 12 NOVEMBER, 2008. 2 L 7 2 4F RT A35EU 20081210 WP 2008 12 10 FDEA200812045093 1 20081204 A 5210 HANDLE DOUG MD10 MD1010F 3022112 WP L1 DOOR UNSECURE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 381FE 12816 512 46615 INADVERTANT EMERGENCY DOOR HANDLE (DOOR L1) MOVED TO DEPLOY POSITION AFTER BLOCK IN. NO SLIDE DEPLOYMENT. INSTALLED S LIDE ASSEMBLY PER MM 25-61-01-2. OPERATIONAL CHECK NORMAL SLIDE PREVIOUSLY REMOVED CPN INSTALLED 2500311 MPN AWD7274-1L . 2 L 7 3 4F RT A22WE 20081210 WP 2008 12 10 FDEA200812085106 1 20081208 A 7830 900760G52 SLEEVE DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL THRUST REVERSER DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 46631 NR 2 ENGINE LEFT TRANSLATING COWL OUTER SKIN IS DENTED. REPAIRED NR 2 LEFT TRANSLATING SLEEVE/COWL OUTER SKIN BY DRILLI NG INJECTED HOLES AND INJECTING EA 934 ADHESIVE AND FILLING THE DENT WITH POTTING COMPOUND AND CURING IAW CF6-6 ENGINE M ANUAL 78-00-32; REPAIR NR 06. PRIMED IAW CF6-6 ENGINE MANUAL 78-00-32; REPAIR NR 06. PAINTED IAW FEDEX DC/MD-10 SRM 51 -21-02; VOL II. 2 L 7 3 4F 4 F RT A22WE E23EA 20081210 NM 2008 12 10 FDEA200812085108 1 20081208 A 5330 53FX130121 SKIN BOEING 727 727225 1384077 NM ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 469FE 21581 FASTENERS WITH IMPROPER SPACING STA 460 STR 10L. ACCOMPLISHED REPAIR IAW FEDEX EA 7-5330-126862 AD 98-11-03 R1 MAIN CAR GO DOOR TRIPLER, DOUBLER AND FUSELAGE SKIN THRU DAMAGE AT STA 460 S10L EO 7-5100-7-4304. 2 L 7 3 4F A3WE 20081209 EA 2008 12 9 SWIA200820584 1 20081004 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 466SW 7856 C-CHECK, RIGHT ENGINE THRUST MOUNT CORRODED AT BEARING. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081209 EA 2008 12 9 SWIA200820585 1 20081008 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 472CA 7667 C-CHECK, FLOOR SUPPORT CLIP CRACKED AT FS 280 INBOARD SIDE RBL 9. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081209 EA 2008 12 9 SWIA200820587 1 20081008 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 472CA 7667 PASSENGER DOOR INNER AFT SKIN CRACKED IN STEP RADIUS AT ZONE 3. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081209 WP 2008 12 9 AALA200802362 1 20081020 A 3350 SHROUD DOUG DC9 DC982 3022082 WP LIGHT ASSY BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 476AA 49651 DFW - EMERGENCY LIGHT AT SEAT 14D HAS CRACKED SHROUD. REPLACED CLEAR PLASTIC SHROUD FOR EMERGENCY LIGHT AT SEAT 14D. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081209 EA 2008 12 9 SWIA200820592 1 20081021 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7881 C-CHECK, FLOORBEAM FS 280 RBL 9 INBOARD CLIP CRACKED. REPLACED PER REO. 2 L 7 2 4F RT A21EA 20081209 EA 2008 12 9 SWIA200820593 1 20081021 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 C-CHECK, FLOORBEAM FS 280 LBL 9 INBOARD CLIP CRACKED. REPLACED PER REO. 2 L 7 2 4F RT A21EA 20081209 EA 2008 12 9 SWIA200820594 1 20081021 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 C-CHECK, FS 280 LBL 9 FLOORBEAM LOWER FLANGE CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081209 NM 2008 12 9 AALA200820058 1 20081118 A 5340 415N40029 MOUNT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 688AA 55898 25730 FORWARD RT GALLEY MOUNT FITTING CORRODED, REPLACED FITTING IAW SRM 53-60-51-2R. 2 L 7 2 4F RT A2NM 20081209 NM 2008 12 9 AALA200820059 1 20081118 A 5340 415N40026 MOUNT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 688AA 55898 25730 CENTER FORWARD GALLEY MOUNT FITTING CORRODED, REPLACED FITTING IAW SRM 53-60-51-2R. 2 L 7 2 4F RT A2NM 20081209 EA 2008 12 9 SWIA200820595 1 20081021 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 C-CHECK, FS 280 RBL 9 UPPER FLOOR SUPPORT ANGLE CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081209 WP 2008 12 9 UPS08854039 1 20081105 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV EXTERNAL SKIN FLUSH REPAIR DOES NOT MEET SRM REQUIREMENTS. REPAIRED SRM 53-02-00 FIG 13 SHEET 5. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854042 1 20081015 A 5320 STRUCTURE DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQ 803-F1-94 AT STA 1457 L21L HAS NO SRM REF AND REQUIRES APPX F. REMOVED OLD REPAIR, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-8, 53-4-1 FIG 21C, 53-2-0 FIG 1D AS PER SAA EA 81426840001. 2 L 7 4 4F RT 4A25 20081209 WP 2008 12 9 UPS08854043 1 20081012 A 5320 STRUCTURE DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQ 803-F1-05 AT STA 74-83 L15-17L HAS NO SRM REF AND REQUIRES ENG DISPOSITION. REMOVED REPAI R, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-0 FIG 22A, TR53-205 AS PER SAA EA 81427430001. 2 L 7 4 4F RT 4A25 20081209 EU 2008 12 9 UPS08154007 1 20081124 A 7110 2214050515 NOSE COWL AIRBUS A300 A300F4622R 3930360 EU NR 2 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 128UP 0812 INSPECTION TYPE:N/A NR 2 ENGINE NOSE COWL AT 6 O`CLOCK POS CRACKED. REPAIRED PER EO A300-7110-30481-B. 2 L 7 2 4F RT A35EU 20081210 WP 2008 12 10 AALA200810291 1 20081121 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 AFT CARGO, INTERCOSTAL CORRODED AT LONGERON 29L BETWEEN STATION 1212 AND 1231. REMOVED AND REPLACED INTERCOSTAL WITH SE RVICEABLE PER SRM 51-10-3 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810296 1 20081123 A 5320 WEB DOUG DC9 DC983 3022083 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 WEB CRACKED IN CANT FRAME LEFT SIDE, (AFT ACCESSORY) STATION 1463. INSTALLED REPLACEMENT WEB SECTION IN CANT FRAME PER SRM 51-02-00. 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810306 1 20081109 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CABIN, LEFT CUSP CORRODED AT STATION 390. REMOVED CORROSION AND INSTALLED REPAIR. 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810309 1 20081108 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CABIN, CORROSION ON NUMBER 3 SEAT TRACK AT STATION 1200. INSTALLED REPAIR PLUG PER AARD 53-20-00-10. 2 L 7 2 4F RT A6WE 20081210 NM 2008 12 10 CALA2008120901132 1 20081209 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 69059 29454 AFT EMERGENCY LIGHTS FROM ROW 39 BACK ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND CHARGER, RESEATED CONNECTO R TO AFFECTED AREA, OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 20081210 WP 2008 12 10 AALA200810314 1 20081110 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CABIN, CORROSION ON BOTTOM SIDE OF RIGHT CUSP AT STATION 1079 TO 1098. INSTALLED SERVICEABLE CUSP SHEET FROM STATION 10 22 TO 1098 PER SRM 51-01. 2 L 7 2 4F RT A6WE 20081210 NM 2008 12 10 CALA2008120801128 1 20081208 A 2530 72067752 OVEN BOEING 757 757224 1384958 NM MID GALLEY MALFUNCTIONED A CALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 13138 45161 112 30351 STRONG ELECTRICAL SMELL FROM MID GALLEY WHEN OVEN TURNED ON SMELL DISAPPEARED WHEN OVEN TURNED OFF. REMOVED AND REPLACE D OVEN AND CONTROLLER, OPS CHECK OK. FILED SMOKE IN CABIN REPORT FOR MAINTENANCE WITH SUPERVISOR, OK TO CONTINUE. ROTA TABLE PARTS CHANGE - OVEN, LARGE, OFF 99-2533-9-0002 S/N 0266 ON 99-2533-9-0002 S/N 0081. 2 L 7 2 4F RT A2NM 20081210 NM 2008 12 10 CALA2008120801129 1 20081206 A 5315 146N5089 FLOORBEAM BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17122 27564 B757-53-3-0448 FLOORBEAM AT STATION 1640 HEAVILY CORRODED. REMOVED DAMAGED SECTION OF UPPER T-CHORD, FABRICATED AND INS TALLED REPAIR SECTION PER SRM 53-00-01 FIG 201, REPAIR 3. 2 L 7 2 4F RT A2NM 20081210 WP 2008 12 10 AALA200810299 1 20081121 A 5322 SHEAR TIE DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 AFT CARGO, CORROSION ON SHEAR TIE STATION 1287. REMOVED AND REPLACED SHEAR TIE. 2 L 7 2 4F RT A6WE 20081210 CE 2008 12 10 AWK2008F00002 1 20081030 A 2150 73838433 ACM CESSNA 750 750 2076810 CE APU BAY SMOKE E AWKA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 25 774XJ 1388 7500274 DURING A REPOSITIONING FLIGHT FROM CHM TO TPA, THE CREW REPORTED A BAD ODOR AND SAW SMALL AMOUNTS OF SMOKE IN THE COCKPI T. CREW REPORTED THEY WERE ABLE TO ISOLATE THE COCKPIT PAC AND THE ODOR WENT AWAY. NO PASSENGERS WERE ABOARD THE ACFT. ACFT DIVERTED TO ILG, THE LOCATION OF AN MX BASE WHERE MX TECHNICIANS TROUBLESHOT THE SOURCE OF ODOR TO BE FROM THE CO CKPIT AIR CYCLE MACHINE. THE ACM WAS REPLACED AND OPS CHECKED NORMAL. 2 L 7 2 4J RT T00007WI 20081210 WP 2008 12 10 NWAA085519926 1 20081117 A 2120 CLAMP DOUG DC9 DC932 3022066 WP DUCT MISSING A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 926NW 47425 DURING CRUISE AT FL340, FLT CREW HEARD A THUMP & NOTICED CABIN ALTITUDE CLIMBING 500-700 FPM. CONFIRMED THAT OUTFLOW VA LVE WAS FULLY CLOSED & CABIN WAS AT 8000 FT & CLIMBING, INITIATED A DESCENT & COMPLIED WITH RED BORDERED CHECKLIST. DUR ING DESCENT TO 10,000 FT, CREW WAS ABLE TO STOP CABIN CLIMB. FLT LANDED AT DESTINATION WITHOUT FURTHER INCIDENT. MX FO UND THE LT WATER SEPARATOR INLET DUCT CLAMP WAS MISSING. CLAMP WAS LOCATED ON THE FLOOR AND REINSTALLED. ALL OTHER CLA MPS ON AFT SIDE OF BOTH THE LT & RT WATER SEPARATOR SYSTEM REPLACED. LT AFT CONNECTOR BOOT REPLACED. NUTS FOR EACH CLA MP ON FWD SIDE OF WATER SEPARATOR SYSTEM REPLACED. LEAK CHECK WAS SATISFACTORY AND ACFT RELEASED FOR SERVICE. 2 L 7 2 4F A6WE 20081210 WP 2008 12 10 UPS08854013 1 20081031 A 5751 DOUBLER DOUG DC8 DC871F 302199D WP LT AILERON DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV LT AILERON STA 454 HAS A REPAIR DOUBLER WITH EDGE DAMAGE. REPAIRED AS PER UPS EO DC8 5710-31295A. 2 L 7 4 4F RT 4A25 20081210 WP 2008 12 10 UPS08854014 1 20081008 A 5520 STRUCTURE DOUG DC8 DC871F 302199D WP X312 MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV REPAIR DOUBLER AT STA X312.5 DOES NOT MEET SRM GUIDELINES. REMOVED AND REPLACED TIP AS PER SRM 51-01 -21A. 2 L 7 4 4F RT 4A25 20081210 WP 2008 12 10 UPS08854015 1 20081013 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV REPAIR DOUBLER AT STA 951 RT DOES NOT MEET SRM GUIDELINES. REPAIRED AS PER UPS EO DC8 5320 31274A. 2 L 7 4 4F RT 4A25 20081210 NM 2008 12 10 MZZA2008120400010 1 20081203 A 5320 141A5410 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 SW 27 26232 28942 FWD WET AREA INTERCOSTAL CRACKED BETWEEN STA 312 & STA 328 AT LBL 36.5 INTERCOSTAL. REMOVED, FABRICATED IAW ECRA 53 21-01524, INSTALLED PER SRM 51-10-02 AND HOLES PICKED UP PER SRM 51-40-05 REV 33. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 MZZA2008120400006 1 20081203 A 5320 147A8540U8 SILL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 SW 27 26232 28942 SPOT CORROSION FOUND ON LOWER SILL OF AFT GALLEY DOOR CUTOUT FROM BS 951 TO 981 (R2 DOOR) AFT GALLEY LOWER SILL CHORD. REMOVED AND REPLACED IAW B737-800 S RM 51-10-02 & HOLES PICKED UP PER SRM 51-40-05 REV 33. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086876 1 20081204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 28L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086877 1 20081204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086866 1 20081204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 927, STR 21R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086874 1 20081204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086875 1 20081204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 15L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 DU4R2008265 1 20081204 A 5320 141A83166 STRAP BOEING 737 737800* NM FUSELAGE CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 171LF 30637 DURING SCHEDULED INSPECTION AT TIMCO-LCQ FOUND CORROSION ON CABIN FLOOR STRAP AT BS 299, LBL 53. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 FDEA200812015024 1 20081201 A 5240 6521632 SKIN BOEING 727 727227 1384078 NM ZONE 800 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 495FE 21669 E&E DOOR DENTED & HAS GOUGE MARKS AT LH EDGE OF DOOR EXTERIOR SKIN. DENTS FOUND TO BE OUT OF LIMITS BY MECHANICAL MEANS IAW SRM 52-100-2. CUT OUT DAMAGE (DIMS: 2 1/8 X 1 1/8) IAW SRM 52-00-3 FIG 1. FABRICATED DOUBLER AND FILLER REPAIR I AW SRM 52-00-3 FIG AND 52-40-1 FIG 2. TREATED AND PRIME REPAIR PARTS IAW SRM 51-10-2 AND INSTALLED PARTS IAW SRM 51-30 -2. 2 L 7 3 4F A3WE 20081210 2008 12 10 P5CA200812021580 2 20081129 A 7397 CONNECTOR BOEING 747 74746NF 13848BT NM NR 2 ENGINE UNSECURE A P5CA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 15 452PA 30810 RWY 07L HKG REJECTED T/O AT 80 KTS DUE TO NR 2 ENGINE FAILURE TO DEVELOP T/O THRUST SUBSEQUENT RUN-UP ON TAXIWAY MAX N1 68 PERCENT, RETURN TO BLOCKS. ENGINE 2 THRUST REVERSER RIGGING AND READING CHECK CARRIED OUT IAW AMM78-31-00-825-001-J0 0. RVDT CONNECTOR SECURITY CHECK OK. ENG 2 EEC ALL CONNECTORS RESECURED ENG 2 GROUND RUN AND THROTTLE RESPONSE UP TO 8 0 PERCENT N1 NORMAL. 2 L 7 4 4F RT A20WE 20081210 SO 2008 12 10 RAIA2008120500001 1 20081204 A 5210 CABLE EMB 145 EMB145EP 3260221 SO PAX DOOR WORN A RAIA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 03 809HK 145187 PASSENGER DOOR WOULD NOT OPEN FROM INSIDE THE AIRCRAFT (NO PASSENGERS ONBOARD). MAINTENANCE REMOVED AND REPLACED THE IN NER PASSENGER DOOR HANDLE CABLE. DOOR OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 20081210 NM 2008 12 10 SWAA086858 1 20081204 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086863 1 20081204 A 3350 411A2212 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND LT FWD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086864 1 20081204 A 5311 6546529 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 SWAA086865 1 20081204 A 5311 6546526 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 8L TO STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 WRLA2008103 1 20081112 A 5542 SKIN DOUG MD11 MD11F 3023600 NM RUDDER DAMAGED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHECK + 4C CHECK, EGAT MECHANIC FOUND LWR RUDDER BROKEN ON THE LWR EDGE. REPAIRED SKIN DAMAGE AREA IAW E NGINEERING INSTRUCTION W2008A55B-1172 REV 01. 2 L 7 3 4F RT A22WE 20081210 NM 2008 12 10 KCSA081609 1 20081204 A 5711 SPAR BOEING 747 747212B 1384886 NM LT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 CORROSION ON L/E SPAR WEB UNDER SPAR STIFFENER AT APPROX WS STA 1589. 2 L 7 4 4F RT A20WE 20081210 NM 2008 12 10 KCSA081610 1 20081204 A 5711 SPAR BOEING 747 747212B 1384886 NM LT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 CORROSION ON L/E SPAR WEB UNDER SUPPORT RIB AFT [VERTICLE] CORD AT APPROX WS 1574. 2 L 7 4 4F RT A20WE 20081210 EA 2008 12 10 MASA2008120500737 1 20081205 A 3260 PROXIMITY SWITCH CNDAIR CL600 CL6002D24 1390016 EA NLG OUT OF ADJUST A MASA K NONE N FALSE WARNING CR CRUISE 1 SW 07 905J 15005 ASH FLT 2627 CLT-SAV. CREW RETURNED TO THE FIELD DUE TO NLG HAD A GEAR DISAGREE MESSAGE ON RETRACTION. MX ADJUSTED NOS E WOW SWITCHES AND TARGETS. 2 L 7 2 4F RT A21EA 20081210 NM 2008 12 10 NOCA08608 1 20081202 A 2612 FIRE WARNING BOEING 767 76739H 1385311 NM RT ENGINE MALFUNCTIONED A NOCA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 15 760NA 26257 R ENG OH LP 1 STATUS MESSAGE. PERFORMED OPERATION TEST OF THE ENGINE FIRE DETECTION SYSTEM PER M/M 26-11-00, OPS NORMAL . 2 L 7 2 4F RT A1NM 20081210 NM 2008 12 10 FDEA200812085109 1 20081208 A 5330 6554577 SKIN BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 469FE 21581 FWD CARGO COMPT STR 26R IS CORRODED WITH EXFOLIATION BETWEEN STA 720E AND 720F. ACCOMPLISHED REPAIR IAW FEDEX EA 7-5330 -126860 FUSELAGE AD 98-03-01 SECTION 43 SKIN REPAIR OF SKIN CORROSION AT STA 720E-720F AND S26R-S27R EO 7-5100-7-4304. 2 L 7 3 4F A3WE 20081210 WP 2008 12 10 FDEA200812085110 1 20081208 A 2421 707304E CSD DOUG DC10 DC1030F 3023504 WP NR 2 LEAKING A FDEA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CE 21 315FE 12755 810 48313 ON TAKEOFF ROLL GOT NR 2 CSD OIL PRESS LOW LIGHT FLUCTUATING WITH ALTERNATING GEN 2 OFF AND AC BUS TIE 2 ISOL LIGHTS. N R 2 ENG INSTRUMENT GAUGES AND LANDING GEAR LIGHTS FLASHING ALONG WITH INTERMITTENT MASTER CAUTION. ABORTED TAKEOFF AND RAN QRH. CSD OIL LIGHT AND ALL ELECTRICAL INDICATIONS WENT OUT OR STABILIZED WHEN ACFT STOPPED. NOTICED ALL AC LOAD ME TERS FLUXING WITH GEN 2 ON. SHUT OFF NR 2 GEN AND DISCONNECTED CSD. LOW SPEED REJECT. OPENED PATIO DOORS AND NR 2 EN GINE FAN COWLINGS. REACTIVATED NR 2 CSD AND FOUND OIL LEVEL TO BE LOW, SERVICED CSD TO FULL. PERFORMED ENGINE RUN PER DC10 JRH CHAPTER 6 AND DISCOVERED SMALL OIL LEAK AT THE CHARGE FILTER CAP ASSY, REF IPC 24-11-10 -01, ITEM 470. REPLAC 2 L 7 3 4F RT A22WE 20081210 NM 2008 12 10 FDEA200812055094 1 20081205 A 5330 6518420483 SKIN BOEING 727 7272S2F 1384O81 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 216FE 22937 FOUND FLUSH SKIN REPAIR LOCATED AT APPROX BS 308 BETWEEN STR S-10L AND S-11L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINO R DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED FLUSH REPAIR, NDT'D ALL COMMON FAST ENER HOLES AND EDGE OF CUTOUT, AND ACCOMPLISHED INSURANCE CUT. FABRICATED DOUBLER, STRUCTURAL FILLER,AND FILLER. ALODI NED, PRIMED AND INSTALLED REF EA 7-5330-123826. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 ASAA0843971 1 20081120 A 5330 65C323591 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 EXTERNAL SKIN ON FUSELAGE DAMAGED BELOW FWD CARGO DOOR STA 480 BUTT LINE 0. CUT OUT DAMAGED AREA & REPAIRED AREA USING FABBED DOUBLER TRIPLER & FILLER IAW B737 400 SRM 53 00 01 FIG 201. 2 L 7 2 4F RT A16WE 20081211 WP 2008 12 11 AALA200810352 1 20081119 A 5310 DOOR FRAME DOUG DC9 DC983 3022083 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 FORWARD ENTRY DOOR JAMB, AFT WEB CRACKED AT STATION 208. REPAIRED PER AARD 53-10-00-11. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810367 1 20081121 A 5320 STRUCTURE DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 CRACK IN SUBFLOOR AT STATION 200. REPAIRED PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 ASOA200801587 1 20081201 A 5534 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LT VERTICAL FWD DRAG ANGLE APPEARS CRACKED. PERFORMED EDDY CURRENT INSPECTION OF LEFT FORWARD VERTICAL STAB TO FUSELAGE DRAG ANGLE IAW CRJ 700 NDTM 51-20-006. DRAG ANGLE CONFIRMED CRACKED AND MARKED. LT DRAG ANGLE REPAIRED PER REO 670-55 -31-018. REMOVED PAINT IAW CRJ SRM 51-12-00, VERIFIED CORROSION TO BE OUT OF LIMITS IAW CRJ 200 SRM 53-00-00 FIG 102. REPAIR OR REPLACEMENT REQUIRED. REMOVED FLOOR LANDING PLATE, LOCATED AND DRILLED NEW PLATE FS 559+112 - 621 IAW CRJ 200 SRM 51-42-06. CUT NEW FLOOR LANDING PLATE IAW BOMBARDIER REO 601R-53-61-593A STEPS 1 AND 2. 2 L 7 2 4F RT A21EA 20081211 WP 2008 12 11 AALA200810333 1 20081110 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 RIGHT CUSP MEMBRANE HAS CORROSION STATION 939 TO STATION 941. INSTALLED NEW CUSP SHEET RIGHT STATION 905 TO STATION 946 PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 ASOA200801640 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LT FLOOR SEAT RAIL FS 581.00 TO FS 693.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .009, WITHIN L IMITS PER SRM 53-31-49. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801641 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RT FLOOR SEAT RAIL FS 581.00 TO FS 693.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .011, WITHIN L IMITS PER SRM 53-31-49. 2 L 7 2 4F RT A21EA 20081211 WP 2008 12 11 AALA200810313 1 20081109 A 5347 GALLEY TRACK DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CABIN, CORROSION ON GALLEY TIE DOWN STATION 160 RIGHT BODY LINE 50. REMOVED AND REPLACED TIE DOWN WITH SERVICEABLE TIE DOWN PER SRM 51-00-00. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 ASOA200801646 1 20081204 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 CORROSION AT FWD SIDE OF THE BELLY FRAME LOWER FLANGE AT FS 317.00 BETWEEN STR 27 AND 26R. REMOVED CORROSION AT FWD SI DE OF THE BELLY FRAME LOWER FLANGE AT FS 317.00 BETWEEN STR 27 AND 26R IAW SRM 51-21-06 SKIN THICKNESS WITHIN LIMITS. A LODINED PRIMED AND PAINTED REWORKED AREA IAW SRM 51-21-16. WORK COMPLETED RG7026456. 2 L 7 2 4F RT A21EA 20081211 WP 2008 12 11 AALA200810305 1 20081110 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9401W 53137 CABIN, CORROSION ON RIGHT CUSP AT STATION 389 TO 503. REPLACED CUSP SHEET WITH SERVICEABLE CUSP SHEET. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 ASOA200801649 1 20081204 A 5210 MECHANISM CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 755EV 10185 F/A REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE AND FEELS AS THOUGH LOCKING MECHANISM IS BINDING. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801651 1 20081204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 920EV 7810 ON APPROACH RECEIVED FLAPS FAIL. FLAPS FAILED IN ZERO POSITION. REFER TO WO 106447, ALL FLEX SHAFTS, ALL FLAP ACTUATOR S, RT BPSU, CHANGED IAW AMM 27-53-10, 27-51-10, AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801595 1 20081201 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 LT/RT FS 625 OBLIQUE ANGLES ARE CRACKED. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 DU4R2008248 1 20081120 A 5315 141A5410 FLOORBEAM BOEING 737 7378Q8 13844BX NM BS 340 LBL 11 CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION, FOUND CORROSION ON BS 340 FLOOR SUPPORT LBL 11. 2 L 7 2 4F RT A16WE 20081211 NM 2008 12 11 DU4R2008251 1 20081120 A 5315 141A5503 FLOORBEAM BOEING 737 7378Q8 13844BX NM BS 312 LBL 13-30 CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION, FOUND CORROSION ON FLOOR BEAM BS 312 LBL 13-30. 2 L 7 2 4F RT A16WE 20081211 NM 2008 12 11 DU4R2008253 1 20081120 A 5320 146A8120 WEB BOEING 737 7378Q8 13844BX NM BS 787-847 S25R CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION, FOUND CORROSION ON UPPER SURFACE OF UPPER WEB BS 787 TO BS 847 S-25R IN AFT CARGO PIT. 2 L 7 2 4F RT A16WE 20081211 NM 2008 12 11 NWAA085345519 1 20081202 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 519US 23207 DURING AN OVERNIGHT LINE CHECK THE EMERGENCY ESCAPE PATH LIGHTING FROM ROWS 33 TO 41 WERE INOPERATIVE. MX FOUND THE ASS OCIATED BATTERY PACK TO BE DEFECTIVE AND REPLACED IT. SYSTEM OPS WERE NORMAL AFTER THE BATTERY PACK WAS REPLACED. 2 L 7 2 4F RT A2NM 20081211 NM 2008 12 11 DU4R2008249 1 20081120 A 5315 141A5505 FLOORBEAM BOEING 737 7378Q8 13844BX NM BS 344 LBL 22 CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION, FOUND CORROSION ON FLOOR BEAM BS 344 LBL 22. 2 L 7 2 4F RT A16WE 20081211 NM 2008 12 11 USAA920082084 1 20081118 A 5310 BEAM BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 24893 PIT FPBH MAJOR REPAIR LOG NR 4335081 4 CRACKS IN BEAM WEB AT BS178 BULKHEAD, LBL17, BETWEEN WL225 AND WL234. REPAIRED B EAM WEB AT BS178 BULKHEAD, LBL17, BETWEEN WL225 AND WL234 IAW B737 SRM 53-10-08. 2 L 7 2 4F RT A16WE 20081211 EA 2008 12 11 SWIA200820599 1 20081201 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 951SW 7795 FLT 6474 - NR 3 EMERGENCY CEILING FLOODLIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081211 SO 2008 12 11 SWIA200820603 1 20081205 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 586SW 120354 C-CHECK, LEFT LOWER WING STRINGER NR 10 CRACKED IN FUEL CELL BETWEEN RIBS 8 AND 9. REPAIRED PER SRM. 2 L 7 2 4T RT A31SO 20081211 EA 2008 12 11 ASOA200801668 1 20081206 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LT 280 FRAME UPON FURTHER INVESTIGATION FOUND CORROSION TO BE OUT OF LIMITS. LT 280 BEAM REMOVED AND REPLACED PER CRJ70 0 SRM 51-42-06 AND 51-42-21, PER MODSUM IS67053110026,SRM 51-42-13, SB670BA-53-026, CRJ 700 SRM 51-21-16 AND CRJ 700 SRM 51-21-11. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801669 1 20081206 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RT 280 FRAME UPON FURTHER INVESTIGATION FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED RT FS280 BEAM IAW CRJ 700 SRM 51-20-006, 51-24-28, 51-21-00, 51-42-06, 51-42-00, 51-42-21, 51-42-13, IS670531120026 AND IS670531100026, AD KM T ORD 10048994, BAT 372037 REF TO M-234 FORM FOR WORK ACCOMPLISHED. 2 L 7 2 4F RT A21EA 20081211 WP 2008 12 11 AALA200810381 1 20081203 A 5313 LONGERON DOUG DC9 DC983 3022083 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 971TW 53621 AFT ACCESSORY, LONGERON 2R CRACKED JUST AFT OF FRAME AT STATION 1418. REPAIRED PER AARD 55-30-00-2. 2 L 7 2 4F RT A6WE 20081211 NM 2008 12 11 AALA200820075 1 20081118 A 5320 146N52466 SUPPORT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 688AA 55898 25730 DRAIN SUPPORT CORRODED. REPLACED DRAIN SUPPORT IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20081211 EA 2008 12 11 ASOA200801678 1 20081206 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 597.00 AND FS 613.00. BLENDED FLOORBEAM CAP LBL 9 BETWEEN FS597.00 & FS 613.00 IAW CRJ 700 SRM 51-21-06. LBL 9 FLOORBEAM REPLACED DUE TO OUT OF LIMIT CORROSION. REFER TO W/O 105591 N/R-00395 FOR BEAM REPLACEMENT. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801679 1 20081206 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 613.00 AND FS 629.00. BLENDED FLOORBEAM CAP LBL 9 BETWEEN FS613.00 & FS 629.00 IAW CRJ 700 SRM 51-21-06. LBL 9 FLOORBEAM REPLACED DUE TO OUT OF LIMIT CORROSION . REFER TO W/O 105591 N/R-00395 FOR BEAM REPLACEMENT. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801683 1 20081206 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 FLOORBEAM CAP HAS CORROSION AT LBL 9 AT FS 708.00. COMPLIED WITH (BLENDING, NDT, AND FINISH RESTORATION) OF REO 670-52- 00-172 ON FLOOR SUPPORT BEAM LOCATED AT FS 708, LBL9, WL73 REFER TO ATTACHED M-234 FOR WORK ACCOMPLISHED. BLENDED FLOO RBEAM CAP LBL 9 FS 708.00 IAW CRJ 700 SRM 51-21-06. PERFORMED EDDY CURRENT INSPECTION OF BLEND AREA AT LBL9, FS 708 PER REO 670-53-00-172 I/A/W CRJ 700 NDTM 51-20-006. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801634 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LT FLOOR SEAT RAIL FS 830.40 TO 985.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .009 WITHIN LIMIT S PER SRM 53-51-49. 2 L 7 2 4F RT A21EA 20081210 NM 2008 12 10 USAA2008120592186 1 20081203 A 3350 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN NOT SEATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 833AW 1844 FLT 635 - RDU-PHX - EEL - FORWARD BATTERY POWER SUPPLY UNIT SHOWS BATTERY FAULT WITH A KNOWN SERVICEABLE BATTERY DURING TEST. RESEATED LEFT FORWARD EMERGENCY POWER SUPPLY UNIT AND BATTERY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081210 EU 2008 12 10 USAA2008120592187 1 20081203 A 2560 P4010021 BATTERY AIRBUS A319 A319112 3930323 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 723UW 1109 FLT 1197 - BUF-DCA - EEL - FORWARD FLIGHT ATTENDANT FLASHLIGHT SEAL BROKEN. REPLACED SEAL AND FLASHLIGHT BATTERY. OPER ATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081210 WP 2008 12 10 AALA200810328 1 20081113 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 RIGHT CUSP CORRODED STATION 564 TO STATION 575. INSTALLED CUSP REPAIR PER AARD 53-20-00-16, STATION 564 TO STATION 575. 2 L 7 2 4F RT A6WE 20081210 NM 2008 12 10 CALA2008120401124 1 20081203 A 5320 147A576213 FLOOR SUPPORT BOEING 737 737924 13848A1 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 38403 30120 FLOOR SUPPORT BETWEEN STA 947.5 AND STA 967 NEAR R-2 DOOR HAS CORROSION AT HOLES FOR NUT PLATE FASTENERS. REMOVED AND R EPLACED FLOOR SUPPORT PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 AALA200820065 1 20081120 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 56842 24599 AFT MAIN DECK PLATE CORRODED; REPAIRED IAW SRM 53-60-51-2R2. 2 L 7 2 4F RT A2NM 20081210 NM 2008 12 10 CALA2008120501127 1 20081204 A 5315 141T5108 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 68159 30438 CABIN - STA 325 LBL 25 - LBL 54 FLOOR SUPPORT FOUND CORRODED. CABIN STA 325 LBL 18 - LBL 59 FLOOR SUPPORT BEAM REPAIRED PER SRM 53-00-51, FIG 201, REPAIR 1 AND HFEC NO CRACK FOUND. 2 L 7 2 4F RT A1NM 20081210 WP 2008 12 10 UPS08854022 1 20081110 A 5720 STRUCTURE DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP RT LEADING EDGE JUST OUTBOARD OF NR 4 PYLON SKIN CRACKED AT SCREW HOLE ABOVE REPAIR DOUBLER (XFS 533) FOUND DURING BUYBACK OF NR 164463. REMOVED EXISTING DOUBLER, CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW SRM 57-2- 1, 51-1-21, 51-1-26. 2 L 7 4 4F RT 4A25 20081210 WP 2008 12 10 UPS08854023 1 20081119 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP LT WING OUTBOARD LEADING EDGE INBOARD SECTION HAS CRACKED UPPER RIB ABOVE PNL 520A XFS 476. INSTALLE D REPAIR DOUBLER IAW SRM 51-1-21, 51-1-20D, 57-3-3 FIG 6 SHT 2. 2 L 7 4 4F RT 4A25 20081210 WP 2008 12 10 UPS08854024 1 20081119 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP WHILE WORKING NR 164443 FOUND WEB TO BE CRACKED AT PIT TORQUE BOX AREA STA 1390. REMOVED DAMAGED WEB AND INSTALLED FABRICATED WEB SECTION IAW SRM, 51-1-21, 51-1-8, FABBED PER DWG 5616674. 2 L 7 4 4F RT 4A25 20081210 WP 2008 12 10 UPS08854025 1 20081118 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP LT WING OUTBOARD L/E INBOARD SECTION HAS CRACKED UPPER RIB ABOVE ACCESS PANEL 519A XFS 692. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-21, 51-1-20D, 57-3-3 FIG 006, 57-2-0 FIG 002. 2 L 7 4 4F RT 4A25 20081210 NM 2008 12 10 MZZA2008120400008 1 20081203 A 5347 143A5310 SEAT TRACK BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 SW 27 26232 28942 FOUND CORROSION ON SEAT TRACK AT STA 344 LBL 22.80 SEAT TRACK REMOVED &. REPLACED IAW B737-800 SRM 51-10-02 AND HOLE S PICKED UP AS PER SRM 51-40-05 REV 33. CROSS REF TO ECRA 5321-01379 FOR SEAT TRACK SUBSTITUTION. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 MZZA2008120400009 1 20081203 A 5347 143A5310 SEAT TRACK BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 SW 27 26232 28942 FOUND CORROSION ON SEAT TRACK AT STA 344, LBL 43.54. SEAT TRACK REMOVED IAW B737-800SRM 51-10-02 AND HOLES PICKED UP PE R SRM 51-40-05 REV 33 CROSS REFERNECE TO ECRA 5321-01379 FOR SEAT TRACK SUBSTITUTE. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 FDEA200812045078 1 20081204 A 5310 BAC1520792 SEAT TRACK BOEING 727 7272S2F 1384O81 NM BS 1148 CORRODED A FDEA O O O O OTHER OTHER OTHER OTHER O O O OTHER OTHER OTHER IN INSP/MAINT 1 CE 21 216FE 22937 AT RBL 45 STA 1148 FLOORBEAM UPPER FLANGE CORRODED DUE TO REPAIR ON SNRM NR N00516 1/4 INCH HOLE IN SEAT TRACK WILL NOT HAVE EDGE DISTANCE IF DRILLED IN SAME LOCATION AS ORIGINAL. DUE TO TEE CAP REPLACMENT A 1/4 INCH HOLE REQUIRED IN SEAT TRACK WOULD HAVE BEEN IN RADIUS OF TEE CAP. CUT OUT AND SPLICED IN NEW SECTION OF SEAT TRACK. REF SRM 53-10-5 FIG 1 AND RELOCATED AFFECTED FASTENER HOLE. EA 7-5310-123825 AUTHORIZES MATERIAL SUBSTITUTION ON STRAP. THIS IS CLASSIFED AS A M AJOR REPAIR. SECTION REPLACED IS FROM STA 1100-1148 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 KCSA081611 1 20081205 A 5411 RIB BOEING 747 747212B 1384886 NM NR 2 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 NR 2 PYLON O/B RIB CRACKED 1.5 INCH AT NAC STA 267. 2 L 7 4 4F RT A20WE 20081210 NM 2008 12 10 KCSA081612 1 20081205 A 5412 BULKHEAD BOEING 747 747212B 1384886 NM NR 2 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 NR 2 PYLON BULKHEAD HAS CHAFE DAMAGE FROM HYDRAULIC FITTING AT NAC STA 220. 2 L 7 4 4F RT A20WE 20081210 NM 2008 12 10 KCSA081613 1 20081205 A 5412 BULKHEAD BOEING 747 747212B 1384886 NM NR 3 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 NR 3 PYLON BULKHEAD HAS CHAFE DAMAGE FROM HYDRAULIC FITTING AT NAC STA 221. 2 L 7 4 4F RT A20WE 20081210 NM 2008 12 10 NOCA08408 1 20081128 A 2560 P2070003001 FLASHLIGHT BOEING 767 767306 1385148 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 765NA 28098 RT OVERWING EMERGENCY EXIT F/A FLASHLIGHT STATUS LIGHT NOT BLINKING. REMOVED AND REPLACED RT OVERWING EMERGENCY EXIT F/ A EMERGENCY FLASHLIGHT IAW AMM 25-64-00. OPS CK OK. 2 L 7 2 4F RT A1NM 20081210 NM 2008 12 10 AALA2008116001 1 20081106 A 5320 146N56511 FLOOR SUPPORT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 666A 52891 52891 FLOORBOARD SUPPORT CORRODED. REPAIRED IAW SRM 53-60-51-2R1. 2 L 7 2 4F RT A2NM 20081210 NM 2008 12 10 USAA2008120992207 1 20081205 A 5320 ANGLE BOEING 737 7374B7 138449C NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - EXFOLIATION ON Z-ANGLE AT BS 991, RBL 43. REPLACED Z-ANGLE AT BS 991, RBL 43 IAW SRM 51-60-51 & SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 USAASB08120 1 20081205 A 3350 20121 CHARGER BOEING 737 7373B7 138447F NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 532AU 24479 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT THE LAST TWO SEAT ROWS, LEFT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1197 BATTERY CHARGER ASSEMBLY PER MM 33-51-51. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 USAA2008120892190 1 20081128 A 5320 D534711242001201 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 808AW 1088 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON SHEAR PLATE AT FR 69 AND FR 70, -Y1732, S23R - S24R. REPLACED SHEAR PLATE AT FR 69 AND FR 70, -Y1732, S23R - S24R IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081210 NM 2008 12 10 USAA2008120892191 1 20081114 A 5313 654N0010127 STRINGER BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 904AW 23566 MCN - MAJOR REPAIR - C12 CHECK - LEVEL 2 CORROSION ON FORWARD CARGO COMPARTMENT STRINGER AT BS 760, S20R. REPAIRED FORW ARD CARGO COMPARTMENT STRINGER AT BS 760, S20R IAW US AIRWAYS EA 1301456 AND B757 SRM 53-00-03-2R1. 2 L 7 2 4F RT A2NM 20081210 NM 2008 12 10 FDEA200811264990 1 20081126 A 5314 6523555 KEELBEAM BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 AFT PIT BILGE KEELBEAM IS CORRODED BS 950E-950F, S29R, WL 139. REPAIR STRAP INSTALLED REF EA 7-5310-118316 PG 1-2. ORI GINAL MATERIAL THICKNESS .150, MATERIAL REMOVED .029, .121 REMAINING. OUT OF LIMITS, REF EA 7-5310-118316. THIS IS C LASSIFIED AS A MAJOR. 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 FDEA200812065095 1 20081206 A 5320 69436951 ANGLE BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 LWR EXTERIOR FUSELAGE BS 740, LBL6 TO LBL 10, WL 148.5 TO WL 150 JUST AFT OF GROUND A/C HOOK UP DUCT CORRODED REMOVED P ANEL, A/C DUCT AND BODY FAIRING, AND HYD LINES FOR ACCESS REF SRM 51-30-02. REMOVED AND FABRICATED L ANGLE AND INSTAL LED NEW L ANGLE REF 51-30-02 PGS 1-13. RE INSTALLED HYD LINES, A/C GROUND DUCT PANELS. REMOVED FOR ACCESS REF MM 21- 20-004-4, 20-10-005-4, SRM 51-30-1, HYD LEAK CHECK GOOD, PNEUMATIC LEAK. OPS CHECK ACP ON W/C 7-5100-7-4310 70C055-00, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 ASAA0873966 1 20081120 A 5320 147A56601 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 BS 951 LBL 52 FLOOR SUPPORT IS CORRODED. REMOVED AND REPLACED CORRODED FLOOR SUPPORT AT BS 951 BL 52 PER SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0843965 1 20081119 A 5330 655298812 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 771AS 25104 FUSELAGE SKIN CREASED 24 INCHES AFT OF L2 DOOR CUTOUT. CUT OUT DAMAGED AREA, REPAIRED AREA USING FABBED DOUBLER TRIPLER AND FILLER IAW B737 400 SRM 53 00 01 FIG 201 REPAIR 31. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0853978 1 20081204 A 2421 761574B IDG BOEING 737 737890 1384527 NM NR 1 ENGINE LEAKING A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 577AS 5317 35186 NR 1 ENGINE IDG LEAKING OIL FROM SWITCH MOUNTED ON FRONT OF IDG. REMOVED AND REPLACED NR 1 IDG PER AMM 24 11 11 000 801 24 11 11 400 801, OPS CHECK GOOD PER AMM 24 11 00 700 802. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0893972 1 20081115 A 5320 141A541012 INTERCOSTAL BOEING 737 737990 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 INTERCOSTAL CRACKED. REPLACED INTERCOSTAL PER SRM 51 40 02. 2 L 7 4 4F RT A16WE 20081210 NM 2008 12 10 ASAA0893970 1 20081114 A 5320 147A750118 SUPPORT BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 SIDEWALL SUPPORT PLATE IS CORRODED. REPLACED SUPPORT PLATE PER SRM 53 00 53. 2 L 7 4 4F RT A16WE 20081210 NM 2008 12 10 USAA2008120892192 1 20081117 A 5320 143N51578200 ANGLE BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 904AW 23566 MCN - MAJOR REPAIR - C12 CHECK - WEB REPAIR ANGLE CRACKED AT BS 860 - BS 878, BL 0, WL 207. REPLACED WEB REPAIR ANGLE C RACKED AT BS 860 - BS 878, BL 0, WL 207 IAW B757 SRM 51-40-02 AND 143N5157-8200. 2 L 7 2 4F RT A2NM 20081210 NM 2008 12 10 USAA2008120892193 1 20081117 A 5320 143N5260 ANGLE BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 904AW 23566 MCN - MAJOR REPAIR - C12 CHECK - CRACKED WEB REPAIR ANGLE AT BS 790, BL 0, WL 207. REPLACED WEB REPAIR ANGLE AT BS 790 , BL 0, WL 207 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081210 EU 2008 12 10 USAA2008120892189 1 20081207 A 3397 WIRE AIRBUS 320 A320232 3930326 EU CABIN DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 663AW 1419 FLT 252 PHX - EEL - SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE AT 9R. MAINTENANCE REPAIRED WIRING AT EMERGENCY LIGHT AT R OW 9 RIGHT. SYSTEM OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081210 NM 2008 12 10 USAASB08121 1 20081206 A 3397 GROUND WIRE BOEING 737 7374B7 138449C NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 432US 24554 DURING WEEKLY CHECK, BDL MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY LIGHTS ON SEAT ROWS 3, 4 AND 5, LEFT SIDE, INOP ERATIVE. BDL MAINTENANCE FOUND A BROKEN GROUND WIRE FROM SEAT 2, LEFT SIDE TO SIDEWALL BENEATH CARPET. REPAIRED WIRE I N ASSOCIATION WITH B737 SPM 20-10-13. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20081210 EU 2008 12 10 FDEA200811124868 1 20081112 A 5554 A55471611000 ATTACH FITTING AIRBUS 310 A310222 3930315 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 453FE 267 RUDDER, NR 1 ATTACH FITTING HAS CORROSION. REPLACED WITH NEW FITTING PER SRM 51-40-21. 2 L 7 2 4F RT A35EU 20081210 EU 2008 12 10 FDEA200811124869 1 20081112 A 5540 A2721206000060Z BELLCRANK AIRBUS 310 A310222 3930315 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 453FE 267 NR 1 RUDDER SERVO ACTUATOR BELLCRANK AT RIB 12 HAS CORROSION. REPLACED WITH NEW FITTING PER SRM 51-40-21. PERFORM RUDD ER MECHANICAL CONTROL OPERATIONAL AND FUNCTIONAL TEST PER AMM 27-21-00-5. 2 L 7 2 4F RT A35EU 20081210 EU 2008 12 10 FDEA200811134873 1 20081113 A 5553 A55371291208 ATTACH FITTING AIRBUS 310 A310222 3930315 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 453FE 267 VERTICAL STABILIZER ATTACH FITTING AT RIB 12 HAS CORROSION. REMOVED CORROSION PER SRM 51-74-10. APPLIED ALODINE TO THE REWORKED AREA PER SRM 51-21-10. FREE OF CRACK AT THE REWORKED AREA. REMAINING THICKNESS IS 0.481 INCH, IT IS WITHIN L IMIT PER SRM 55-30-00/101 CONFIG 1. RESTORED FINISH AND CIC THE REWORKED AREA PER SRM 51-75-10 AND SRM51-23-20. 2 L 7 2 4F RT A35EU 20081210 EU 2008 12 10 FDEA200811134874 1 20081113 A 5553 A55371296208 ATTACH FITTING AIRBUS 310 A310222 3930315 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 453FE 3500 267 VERTICAL STABILIZER ATTACH FITTING AT RIB 13 HAS CORROSION. COMPLIED WITH EA 6-5510-125488. 2 L 7 2 4F RT A35EU 20081210 EU 2008 12 10 FDEA200811134875 1 20081113 A 5553 A55371301208 ATTACH FITTING AIRBUS 310 A310222 3930315 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 453FE 267 VERTICAL STABILIZER ATTACH FITTING AT RIB 14 HAS CORROSION. COMPLIED WITH EA 6-5510-125488. 2 L 7 2 4F RT A35EU 20081210 NM 2008 12 10 FDEA200812035061 1 20081203 A 5330 53FX130122 SKIN BOEING 727 727227 1384078 NM BS 440 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 495FE 21669 NUMEROUS FASTENERS WITH IMPROPER ED AND SPACING STA 440 STR'S 8L TO 10L. REPAIRED THE AFFECTED AREA IAW FEDEX EA NR 7-5 330-126864, FUSELAGE SKIN AD 98-11-03R1. MCD CUTOUT REINFORCEMENT DOUBLER AND FUSELAGE SKIN LAP JOINT REPAIR AT STA 440 , S10L. 2 L 7 3 4F A3WE 20081210 EA 2008 12 10 REX2008F00059 1 20081115 A 7830 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER FALSE ACTIVATION A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 8432A 7432 DURING CLIMB FROM KDTW THE R REV UNLOCKED MSG ILLUMINATED. THE FLIGHT CREW PERFORMED THE QRH AND DECLARED AN EMERGENCY. THE ACFT WAS ROUTED BACK TO KDTW WHERE AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE. MX INSPECTED THE ACFT A ND DEFERRED THE RT THRUST REVERSER. THE ACFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081210 NM 2008 12 10 ASAA0873992 1 20081208 A 5311 147A1047 FRAME BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION ON FRAME BS 947.5 I/B FLANGE. REMOVED CORROSION ON FRAME AND FOUND OUT OF LIMITS AT LBL 12. REPAIRED BS 947 FRAME AT LBL 12. 2 L 7 2 4F RT A16WE 20081211 WP 2008 12 11 AALA200810337 1 20081117 A 5320 SUPPORT ANGLE DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 SUPPORT ANGLE CRACKED IN FORWARD CARGO AT STATION 237. REMOVED AND REPLACED SUPPORT ANGLE. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810339 1 20081118 A 5320 BRACKET DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CORROSION IN LOWER BRACKET AT INBOARD AFT CORNER OF AFT CARGO DOOR JAMB OPENING STATION 1212. INSTALLED SERVICEABLE BRAC KET PER SRM 51-30-2. 2 L 7 2 4F RT A6WE 20081211 NM 2008 12 11 ASAA0853963 1 20081203 A 4920 353A20802 FITTING BOEING 737 737890 1384527 NM APU MISSING A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 579AS P7808 35187 APU FAULT LIGHT WOULD NOT START WAITED 5 MINUTES WOULD NOT START ON RE ATTEMPT. ON INSPECTION OF APU FOUND PLENUM DOOR FASTENERS LOOSE ON RT AFT CORNER/ ONE RETAINER CLIP WAS MISSING FROM HOUSING (ON ORDER). PER FIM: REMOVED AND REPLACED INLET PRESSURE SENSOR (PER: AMM 49 52 31) & INLET TEMP SENSOR (PER: AMM 49 61 31). INSTALLED RECEPTACLE CLIP ON APU CO MPRESSOR INLET CASE PLENUM DOOR. SECURED DOOR REF MM 49 11 00 200 801. 2 L 7 2 4F RT A16WE 20081211 WP 2008 12 11 AALA200810340 1 20081119 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CORROSION IN AFT CARGO ON INTERCOSTAL ABOVE LONGERON 27 LEFT BETWEEN FRAME STATION 1271 TO STATION 1250. INSTALLED DOUB LER PER 51-10-3. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810341 1 20081119 A 5320 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 AFT CARGO FLOOR SUPPORT CRACKED AT LONGERON 28 LEFT AT STATION 1174. REMOVED DAMAGED SUPPORT AND REPLACED WITH NEW SUPP ORT PER SRM 51-30-5. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810356 1 20081120 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 CABIN, CRACK IN RIGHT CUSP STATION 218. REPAIRED PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810358 1 20081121 A 5340 MOUNT DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 CABIN, CORROSION ON G-2 GALLEY AFT INBOARD MOUNT UNDER SUBFLOOR. INSTALLED A SERVICABLE MOUNT PER SRM 51-01-00. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810359 1 20081121 A 5320 ANGLE DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 AFT ACCESSORY, CRACK IN TEE ANGLE BELOW PIVOT OF VENTRAL STAIRS TORQUE TUBE, LEFT SIDE BETWEEN CANT FRAME 1485 AND 1497. INSTALLED SERVICABLE ANGLE PER SRM 51-01-00. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810346 1 20081120 A 5330 SKIN DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 NOSE LANDING GEAR LEFT AFT STRUT DOOR AFT HINGE CUT-OUT CRACKED. INSTALLED DOUBLER PER SRM 53-05-00 SHEETS 1 AND 2. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810360 1 20081122 A 5340 TEE FITTING DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 AFT CARGO, CORROSION ON TEE FITTING STATION 1155 LONGERON 28R. INSTALLED SERVICEABLE TEE FITTING PER SRM 51-01-00. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810361 1 20081122 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 CABIN, NUMBER 5 SEAT TRACK OUT OF LIMITS AT STATION 233 TO 237. INSTALLED NEW SECTION OF SEAT TRACK FROM STATION 200 TO 245. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810348 1 20081120 A 5320 ANGLE DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CORROSION ON ANGLE ABOVE BOTTOM FORWARD CORNER OF AFT CARGO DOOR CUT-OUT, STATION 1155 BETWEEN LONGERON 28 RIGHT AND LON GERON 27 RIGHT. CORROSION ADDRESS CORRECTED BY REPLACING WITH SERVICEABLE COMPONENT PER SRM 51-10-1. 2 L 7 2 4F RT A6WE 20081211 NM 2008 12 11 ASAA0873997 1 20081204 A 5311 146A9403237 FRAME BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 AFT CARGO BAY DOOR CUTOUT FWD FRAME CLOSEOUT WEB CRACKED. REMOVED AND REPLACED WEB. 2 L 7 2 4F RT A16WE 20081211 NM 2008 12 11 ASAA0843999 1 20081206 A 5320 6547690 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON RT FLOOR TO SIDEWALL SUPPORT IN AFT CARGO BAY RBL 25 BS 727+4 BS 767. REPLACED RT FLOOR TO SIDEWALL SUPPOR T PER SRM 53 60 53. 2 L 7 2 4F RT A16WE 20081211 WP 2008 12 11 AALA200810365 1 20081124 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 CORROSION ON LEFT CUSP AT STATION 237 TO 256. REPAIRED PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 ASOA200801665 1 20081205 A 5260 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 UPON REMOVAL OF FIXED MID STEP FROM PAX DOOR FOR AFT WEB REPAIR FOUND FWD WEB TO BE CRACKED IN 832CT. FIXED MID STEP IN TERSECTION RADIUS. REPAIRED PAX DOOR FWD SKIN WEB AT RADIUS FOR 832CT, FIXED MID STEP INTERSECTION IAW ECTC REO 601R-52 -11-702. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801589 1 20081201 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA LLT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 LT WING BATT RIB ASSY AT WS 53.60 IS CRACKED .800 INCH LONG JUST AFT OF TOP AFT FASTENER BEFORE THE RADIUS. COMPLIED WI TH REPAIR TO LT BATT RIB AT WS 53.60 REPAIR IAW BOMBARDIER REO 601R-57-51-046. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801642 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LT FLOOR SEAT RAIL FS 693.00 TO FS 847.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .015 , WITHIN LIMITS PER SRM 53-41-49. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801643 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RT FLOOR SEAT RAIL FS 693.00 TO FS 847.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .014 , WITHIN LIMITS PER SRM 53-41-49. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801647 1 20081204 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA BS 349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 CORROSION AT AFT SIDE OF THE BELLY FRAME LOWER FLANGE AT FS 349.00 BETWEEN STR 27 AND 26R. REMOVED CORROSION AT AFT SI DE OF THE BELLY FRAME LOWER FLANGE AT FS 349.00 BETWEEN STR 27 AND 26R IAW SRM 51-21-06 SKIN THICKNESS WITHIN LIMITS. ALODINED, PRIMED AND PAINTED REWORKED AREA IAW SRM 51-21-16. WORK COMPLETED RG7026456. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801655 1 20081205 A 2560 MEGAPHONE CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 317CA 10055 F/A MEGAPHONE NOT WORKING. FLT 4995 DEL 61 MINS. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801590 1 20081201 A 5210 ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 925EV 7831 PAX DOOR INNER HANDLE MEET STRUCTURE HAS CRACKED ANGLE. REMOVED THE PAX DOOR INNER HANDLE STRUCTURAL ANGLE. LOCATED, S EALED AND INSTALLED A NEW ANGLE IAW SRM 51-40-11 AND 51-42-06. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801591 1 20081201 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 RT FLOOR SUPPORT IS CRACKED AT FS 621, RBL 40, WL 73. REPAIRED CRACKED RT FLOOR SUPPORT AT FS 621, RBL 40, WL 73 IAW RE O 601R-53-61-117 REV C. COMPLIED WITH ECTC REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801599 1 20081201 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 FS 280 FLOOR SUPPORT CHANNEL HAS CRACK IN WEB NEAR LOWER FLANGE O/B OF RBL 9.0. COMPLIED WITH REO 601R-53-11-171, REPAI R TO BULKHEAD AT FS 280 AND RBL 9. COMPLIED WITH EO 600-53-90. 2 L 7 2 4F RT A21EA 20081210 NE 2008 12 10 SWAA086880 2 20081202 A 7397 W80400400520 WIRE BOEING 737 7373H4 1384600 NM GE CFM56 CFM56* 13802 NE RT WING DAMAGED A SWAA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 SW 29 338SW 23960 IN FLT SHUTDOWN / DIVERSION / DECLARED EMERGENCY. NR 2 ENG FLAMED OUT, UNABLE TO RESTART. FOUND NR 2 ENG FUEL SHUT-OFF VALVE WIRING DAMAGED AT BUNDLE W804. REPAIRED WIRING PER WPM. 2 L 7 2 4F 4 F RT A16WE E2GL 20081210 NM 2008 12 10 SWAA086857 1 20081204 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND LT WING NR 1 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 FDEA200811144880 1 20081114 A 5321 6523638 FLOOR PANEL BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 MAIN CARGO FLOOR CORROSION ON SEAT TRACK AT STA 740 LBL46, REMOVED BEYOND LIMITS CORRODED SEAT TRACK REF SRM 51-30-2. F ABRICATED REPLACEMENT SEAT TRACK REF SRM 53-10-5. FABRICATED TRACK SPLICE REF SRM 53-10-5. INSTALLED SEAT TRACK AND SP LICE REF SRM 53-10-5, TREATED AND PRIMED REF SRM 51-10-2 PG 3. FABRICATED -3 SPLICE STRAP REF SRM 53-10-5 PG3, HEAT TRE AT SPLICE REF 8130 NR 418721, CADMIUM PLATE STRAP REF NR N00957, PRIMED STRAP REF 51-10-2. INSTALLED STRAP SPLICE REF S RM 53-10-5 P3 AND EA 7-5310-118312. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 FDEA200811264989 1 20081126 A 5314 6523555 KEELBEAM BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 AFT PIT KEELBEAM IS CORRODED BS 950F - 970, STR 29R, WL 139. INSTALLED REPAIR STRAP REF EA 7-5310-118316 P 1-2. THIS I S CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 FDEA200811264991 1 20081126 A 5314 6523555 KEELBEAM BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 LOWER AFT CARGO AREA CORROSION AT STA 950E - 950C ON LEFT KEELBEAM. INSTALLED REPAIR STRAP REF EA 7-5310-118316. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081210 EU 2008 12 10 FDEA200812095114 1 20081209 A 5730 A5734008821100 SKIN AIRBUS 300 A300B4622R 3930312 EU RT WING BULGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 33428 358 RIGHT WING LOWER SKIN, LOWER SURFACE OTBD OF RIB 11 (OTBD OF THE FLAP TRACK) 19 INCHES FWD OF THE REAR SPAR, THE SKIN IS BULGING, FWD SIDE OF THE FASTENERS. REMOVED CORROSION. FLAP PEENED AREA. ALODINED, PRIMED AND PAINTED IAW EA 6-5730- 123533. REMOVED AND REPLACED FASTENERS IAW SRM 51-41-21; PG 7. 2 L 7 2 4F RT A35EU 20081210 NM 2008 12 10 FDEA200812095116 1 20081209 A 5330 53FX15322 SKIN BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 469FE 21581 INNER AFT EDGE OF MCD CUTOUT HAS NUMEROUS AREAS DAMAGED BY GILL LINER FASTENERS. REPAIRED BY ACCOMPLISHING EA 7-5310- 126861 "FUSELAGE - AD 98-11-03 R1 - SSI 6.19A - P-F MOD MCD CUTOUT LOWER CORNER INNER SKIN, REPAIR OF GOUGE MARKS AT BS 620 S16L - EO 7-5100-7-4304". 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 FDEA200812095117 1 20081209 A 5720 66191041 SUPPORT BOEING 727 727225 1384077 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 469FE 21581 LT WING NR 1 SLAT ACTUATOR RIB SUPPORT INBD SIDE IS CRACKED REPAIRED BY ACCOMPLISHING EA 7-5750-126863 WINGS - LT NR 1 S LAT STA 390.9 ACTUATOR SUPPORT RIB. REPAIR OF DOUBLER CRACKS PER SB 727-57-0130. 2 L 7 3 4F A3WE 20081210 WP 2008 12 10 AALA200810315 1 20081110 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CABIN, CORROSION ON BOTTOM SIDE OF RIGHT CUSP AT STATION 1098 TO 1117. INSTALLED SERVICEABLE CUSP SHEET FROM 1098 TO 10 74 PER SRM 51-01. 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810329 1 20081113 A 5320 ANGLE DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CORROSION OUT OF LIMITS ON ANGLE STATION 1338, LONGERON 28 LEFT TO LONGERON 29 LEFT. REPLACED ANGLE STATION 1338, LONGE RON 28 LEFT TO LONGERON 29 LEFT PER 51-01 SRM. 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810317 1 20081111 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CABIN, CORROSION ON NUMBER 3 SEAT TRACK AT STATION 1174. REPAIRED PER AARD 53-20-00-10. 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810331 1 20081113 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CORROSION ON NR 6 SEAT TRACK OUT OF LIMITS STATION 1031 TO STATION 1307. REPLACED SEAT TRACK FROM SPLICE AT STATION 103 1 TO STATION 1307 PER 51-01 SRM. 2 L 7 2 4F RT A6WE 20081210 WP 2008 12 10 AALA200810320 1 20081113 A 5532 FRAME DOUG DC9 DC983 3022083 WP VERTICAL STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 VERTICAL STABILIZER, LEADING EDGE FORMER CRACKED IN RADIUS AT FORWARD SPAR ATTACH FASTENER RIGHT SIDE ZFS 49.625. REPAI RED PER AARD 55-30-00-2. 2 L 7 2 4F RT A6WE 20081210 NM 2008 12 10 ASAA0843980 1 20081129 A 5753 FLAP TRACK BOEING 737 737490 1384715 NM TE FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 NR 2 FLAP TRACK HAS EVIDENCE OF CORROSION. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0843982 1 20081129 A 5753 FLAP TRACK BOEING 737 737490 1384715 NM TE FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 NR 8 FLAP TRACK HAS EVIDENCE OF CORROSION. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0843983 1 20081126 A 5753 FLAP TRACK BOEING 737 737490 1384715 NM TE FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 NR 1 FLAP TRACK HAS EVIDENCE OF CORROSION. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0843985 1 20081126 A 5753 FLAP TRACK BOEING 737 737490 1384715 NM TE FLAP CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 NR 7 FLAP TRACK HAS EVIDENCE OF CORROSION. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0873987 1 20081208 A 5320 143A7501 SUPPORT BOEING 737 737790 13844CN NM BS 500B-500D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION ON FLOOR TO SIDEWALL SUPPORT (SIDEPLATE ASSY). REMOVED FABRICATED NEW SUPPORT AND INSTALLED. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0873995 1 20081120 A 5320 147A56602 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 FLOOR SUPPORT IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0843998 1 20081206 A 5312 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON AFT CARGO LOWER BULKHEAD SUPPORT RBL 12 (OUT OF LIMITS). FABRICATED AND INSTALLED NEW BULKHEAD SUPPORT. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 ASAA0874000 1 20081208 A 5320 147A56602 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 FLOOR SUPPORT IS CORRODED. 2 L 7 2 4F RT A16WE 20081211 WP 2008 12 11 AALA200810362 1 20081122 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 CABIN, CORROSION ON LEFT CUSP AT STATION 1055 TO 1060. INSTALLED A SERVICEABLE CUSP SHEET FROM 1022 TO 1098. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 ASOA200801638 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LT FLOOR SEAT RAIL FS 485.00 TO FS 581.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .009 ,WITH IN LIMITS PER SRM 53-31-49. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 AALA200820068 1 20081112 A 5320 148N31388000 STRUCTURE BOEING 757 757223 1384957 NM APU INLET CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 694AN 47963 26974 CORROSION AROUND NUT PLATE AFT. EDGE OF APU INLET DOOR, REPAIRED IAW EA 53-004951 DATED 11-12-08. 2 L 7 2 4F RT A2NM 2008011700084 20080117 00084 NM 2008 1 17 UIEA200800009 1 20080110 A 5753 SKIN BOEING 747 74747UF 1384812 NM LT TE FLAP CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 412 30559 LT INBD MID FLAP WITH MULTIPLE AREAS OF DAMAGE TO THE INBD L/E FAIRING ADJACENT TO THE CONCERTINA SEAL. THIS DAMAGE COM PRISES OF A HOLE 1.2" BY 0.9", WITH AN ASSOCIATED 8.0" CRACK RUNNING OUTBD. TOTAL SIZE OF DAMAGE IS 9.2" LONG. 2 L 7 4 4F RT A20WE 20081211 EA 2008 12 11 ASOA200801645 1 20081204 A 5320 STRAP CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 CORROSION AT BELLY STRAP JUST AFT OF FS 280.00 BETWEEN STR 26L TO 26R. STARTED TO REMOVE PAINT AND SOLID RIVITS FROM ST RAP JUST AFT OF FS280 FRAME IN BELLY OF A/C AT STR 27 TO STR 26R ALL WORK IAW CRJ 700 SRM 51-42-06 AND 51-21-06, CRJ 700 NDTM 51-20-004, REO 670-53-21-421 PER CRJ 700 NDTM 51-20-006, CRJ 700 SRM 51-21-16, CRJ 700 SRM 51-21-11. 2 L 7 2 4F RT A21EA 20081211 WP 2008 12 11 AALA200810336 1 20081115 A 5320 MOUNT DOUG DC9 DC983 3022083 WP LIGHT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 HOLE FROM CORROSION IN MOUNTING FLANGE FOR UPPER ANTI-COLLISION LIGHT. DOUBLER INSTALLED PER 53-04 PAGE 145. 2 L 7 2 4F RT A6WE 20081211 NM 2008 12 11 AALA200820070 1 20081118 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 56842 24599 AFT MAIN DECK PLATE CORRODED; REPAIRED IAW SRM 53-60-51-2R2. 2 L 7 2 4F RT A2NM 20081211 EA 2008 12 11 ASOA200801593 1 20081201 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 FS 280 FLOOR SUPPORT CLIP IS CRACKED O/B OF LBL 9. REMOVED CRACKED CLIP AT FS 280 FLOOR SUPPORT O/B OF LBL 9. INSTALLE D NEW SERVICEABLE CLIP IAW SRM 51-42-06 AND 51-42-21. PREP AND PAINT REQUIRED. PAINTED SUPPORT CLIP IAW SRM 51-25-01. 2 L 7 2 4F RT A21EA 20081211 WP 2008 12 11 NWAA085309987 1 20081130 A 2740 TRIM SYSTEM DOUG DC9 DC932 3022066 WP MALFUNCTIONED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 987US 47458 CREW DETERMINED THAT THE PRIMARY TRIM CONTROL WAS INTERMITTENTLY INOPERATIVE IN BOTH NOSE UP AND NOSE DOWN DIRECTIONS. THIS WAS TRUE FROM BOTH THE CAPTAINS AND FIRST OFFICERS POSITION. THE ALTERNATE TRIM FUNCTIONED OK. NO MENTION OF COM COMPLIANCE EXCEPT FOR THE NOTE THAT THE CREW DID NOT TROUBLESHOOT THE SUITCASE HANDLES. THE FLIGHT RETURNED TO A NORMAL SAFE LANDING BACK AT MSP. MX COULD NOT FIND ANY PROBLEMS OR FAILURES BUT DID CHANGE THE PRIMARY DRIVE MOTOR (SECOND ON E IN 2 DAYS) AND ALSO REPLACED THE BRAKE OVERRIDE SWITCH. 2 L 7 2 4F A6WE 20081211 EA 2008 12 11 ASOA200801598 1 20081201 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 FS 280 FLOOR SUPPORT CLIP AT RBL 9.0 O/B IS CRACKED. REMOVED CRACKED CLIP FLOOR SUPPORT AT RBL 9 O/B. FOR RE-INSTALLAT ION OF CLIP AT FS 280 FLOOR SUPPORT AT RBL 9 O/B, REF MWC JOB 8773721/254. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801600 1 20081201 A 5230 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 CARGO DOOR SUPPORT BEAM LWR ANGLE P/N: 601R-35050-109 HAS VISIBLE CRACK EXTENDING APPROX 0.5 INCH FROM FASTENER. REMOVE D CARGO DOOR SUPPORT BEAM LWR ANGLE. INSTALLED NEW CARGO DOOR SUPPORT BEAM LOWER ANGLE P/N 601R35050-109 IAW ASA CRJ 20 0 SRM 51-42-21. LEAK CHECK GOOD AT THIS TIME (DURING PRESSURIZATION) IAW CRJ 200 AMM 21-32-00-863-801. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801601 1 20081202 A 5320 ANGLE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 FWD FLOOR ANGLE OF FS 280 LBL9 - RBL 9 CORRODED. REMOVED FWD FLOOR ANGLE OF FS280 LBL9-RBL9 DUE TO CORROSION BEING OUT OF LIMITS. ALL WORK DONE IAW CRJ 700 SRM 51-42-06, SB670-53-026, CRJ 700 51-42-21 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 DU4R2008243 1 20081117 A 5315 147A5566 FLOORBEAM BOEING 737 7378Q8 13844BX NM BS 986 CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION, FL FOUND CORROSION ON FLOORBEAM AFT CABIN STA 986 RBL 39 TO LBL 44. 2 L 7 2 4F RT A16WE 20081211 EA 2008 12 11 ASOA200801602 1 20081202 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RT 280 BEAM HAS MINOR CORROSION ON UPPER SURFACE. REMOVED MINOR CORROSION ON UPPER SURFACE OF RT 280 FLOORBEAM PER SRM 51-12-00. PERFORMED UT THICKNESS MEASUREMENT OF BLEND AREA ON RT 280 FLOORBEAM IAW NDTM 51-20-004. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801603 1 20081202 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LT 280 WEB, AFT SIDE HAS MINOR CORROSION. REMOVED MINOR CORROSION ON LT WEB AFT SURFACE PER CRJ700 SRM 51-12-00. REMOV ED 4 RIVETS ON LOWER INBOARD CORNER. MEASURED BLENDED AREA OF 280 WEB AT 2 TO 6 INCHES OUTBOARD OF LBL 9 DEPTH AT .005 IAW SRM 53-11-10. RE-MEASURED BLENDED AREAS OF THE LT 280 WEB AFT SIDE MECHANICALLY. MAX MATERIAL REMOVED IS .005. BLE NDED AREA WITH IN LIMITS PER SRM 53-11-10. REPLACED REMOVED RIVETS ON LT FS 280 WEB AND RESTORED A023 FINISH IAW SRM 5 1-42-06, SRM 51-42-16. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801608 1 20081203 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 750EV 10161 F/A REPORTS MAIN CABIN DOOR IS DIFFICULT TO OPEN FROM INSIDE. FLT 5245 DEL 43 MINS. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 DU4R2008247 1 20081120 A 5315 141A5410 FLOORBEAM BOEING 737 7378Q8 13844BX NM BS 325 RBL 10 CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION, FOUND CORROSION ON BS 325 FLOOR SUPPORT RBL 10. 2 L 7 2 4F RT A16WE 20081211 NM 2008 12 11 DU4R2008257 1 20081120 A 5322 147A5506 SHEAR TIE BOEING 737 7378Q8 13844BX NM AFT CABIN CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION FOUND CORRODED SHEAR TIE AT BS 986 RBL 39 TO LBL 44 IN AFT CABIN. 2 L 7 2 4F RT A16WE 20081211 EA 2008 12 11 ASOA200801611 1 20081203 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 RT FS 484 RBL 36.0 INTERCOSTAL CRACKED PREVIOUS REPAIR. REMOVED OUTBOARD PULLEY AND BRACKET AND SLID FWD. REMOVED CRAC KED ANGLE. FABRICATED NEW ANGLE BRACKET. ANGLE BRACKET REQUIRES HOLE TRANSFERS AND FURTHER SHAPING. AFTER REPAIR OUTB OARD CONTROL CABLE PULLEY AND BRACKET ON FS 484 REQUIRES INSTALLATION. REPLACED RT FS 484 RBL 360 INTERCOSTAL CLIP IAW SRM 51-41-02 AND REO 610R-53-41-059. INSTALLED OUTBOARD CONTROL CABLE PULLEY BRACKET IAW SRM 51-41-02. C/W EC/TC REO 6 01R-53-41-059. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 DU4R2008254 1 20081120 A 5315 141A5504 FLOORBEAM BOEING 737 7378Q8 13844BX NM BS 328 RBL 9-31 CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION, FOUND CORROSION ON FLOOR SUPPORT AT BS 328 RBL 9 - RBL 31. 2 L 7 2 4F RT A16WE 20081211 EA 2008 12 11 ASOA200801613 1 20081203 A 5347 CARGO TRACK CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 CARGO SEAT TRACK AT LBL 9 FS 621 IS CORRODED. REMOVED CARGO BAY SEAT TRACK AY FS 621 LBL 9 AND INSTALLED SERVICEABLE SE AT TRACK IAW SRM 51-41-04. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 DU4R2008245 1 20081120 A 5320 141A5410 FLOOR SUPPORT BOEING 737 7378Q8 13844BX NM BS 316-324 RBL30 CRACKED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION, FOUND FLOOR SUPPORT CRACKED AT BS 316 TO BS 324 RBL 30. 2 L 7 2 4F RT A16WE 20081211 NM 2008 12 11 USAA920082088 1 20081117 A 5311 65C22909 FRAME BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT Q2 MAJOR REPAIR NR 03C10753039/005 FRAME CRACKED AT PSU RAIL ATTACH POINT BS 500C, BETWEEN S8L AND S9L. REPAIRED FR AME AT PSU RAIL ATTACH POINT BS 500C, BETWEEN S8L AND S9L IAW TYPICAL REPAIR NR 53-10-20E. 2 L 7 2 4F RT A16WE 20081211 CE 2008 12 11 FCP2008F00000 1 20081114 A 5740 1011100841 ATTACH FITTING BEECH 300 300BEECH 1152930 CE LT WING CRACKED B FCPR K NONE O OTHER IN INSP/MAINT 1 NM 09 898RJ 8875 FA90 WHILE COMPLYING WITH AD AD 91-12-10 AMENDMENT 39-7021, FOUND THE LT WING PANEL LOWER FORWARD ATTACH POINT HAD A .125 INC H CRACK. 2 L 7 2 4T A24CE 20081211 EU 2008 12 11 USAA920082065 1 20081115 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU ZONE 200 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 628AW 67 LOG PAGE 4377534 FLT NR 612 PHX-ATL EEL FORWARD CABIN SEVERAL EMERGENCY EXIT LIGHTS INOPERATIVE. MX R&R THE FORWARD EME RGENCY LIGHT BATTERY. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081211 NM 2008 12 11 DU4R2008242 1 20081117 A 5753 6014571 ANGLE BOEING 737 7378Q8 13844BX NM LT IB TE FLAP CHAFED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION, FOUND LT IB FLAP RIB CHAFED AT IB TRACK FOR FORE FLAP ROLLER. 2 L 7 2 4F RT A16WE 20081211 2008 12 11 SWIA200820601 2 20081201 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO RIGHT SLUGGISH A SWIA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 NM 07 569SW 120344 FLT 7790 - RIGHT ENGINE VERY SLOW TO SPOOL UP ON TAKEOFF; RECEIVED AN AUTOFEATHER AURAL WARNING WITH SWITCHES IN CORRECT POSITION. COMPLETED RIGHT ENGINE TRIM ADJUSTMENTS. 2 L 7 2 4T RT A31SO 20081211 WP 2008 12 11 AALA200810368 1 20081121 A 5313 LONGERON DOUG DC9 DC983 3022083 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 LONGERON 4L CRACKED AT STATION 200. REPAIRED PER SRM 53-02-00. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 VNAA2008120400011 1 20081130 A 3010 355862255 SENSING ELEMENT CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYS SHORTED A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 05 258PS 7941 ON CLIMBOUT FROM PHL CREW RECEIVED AN ANTI ICE WARNING MESSAGE. AIRCRAFT RETURNED TO PHL, LANDING WITHOUT INCIDENT. MA INTENANCE FOUND SENSING ELEMENT A15WK SHORTED TO GROUND. MAINTENANCE REMOVED AND REPLACED ELEMENT AND NO OTHER DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081211 WP 2008 12 11 AALA200810371 1 20081126 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 CORROSION AND HOLE PUNCTURE IN LEFT CUSP AT STATION 853 TO 864. REPAIRED PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810378 1 20081126 A 5320 PAN DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 AFT CARGO DOOR PAN CRACKED. DOUBLER INSTALLED. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810379 1 20081126 A 5210 BEAM DOUG DC9 DC983 3022083 WP ZONE 800 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 FORWARD ENTRY DOOR NR 2 BEAM AFT END CRACKED. STOP DRILLED, DOUBLER INSTALLED. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 ASOA200801674 1 20081206 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 533.00 AND FS 549.00. BLENDED FLOORBEAM CAP LBL 9 BETWEEN FS533.00 & FS 549.00 IAW CRJ 700 SRM 51-21-06. LBL 9 FLOOR BEAM REPLACED DUE TO OUT OF LIMIT CORROSION. REFER TO W/O 105591 N/R -003 91 FOR BEAM REPLACEMENT. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801675 1 20081206 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 565.00 AND FS 581.00. BLENDED FLOORBEAM CAP LBL 9 BETWEEN FS565.00 & 58 1.00 IAW CRJ 700 SRM 51-21-06. FWD & AFT LBL9 FLOORBEAM REPLACED DUE TO OUT OF LIMIT CORROSION. REFER TO W/O 105591 N/R-00391 + N/R-00395 FOR BEAM REPLACEMENT. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801677 1 20081206 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 581.00 AND FS 597.00. LBL 9 FLOORBEAM REPLACED BETWEEN FS 572.00 & 686. WORK DONE IAW CRJ 700 SRM 51-21-06, CRJ 700 SRM 51-11-00. LBL 9 FLOOR BEAM REPLACED REFER TO W/O 105591 N/R-00401 FO R WORK ACCOMPLISHED . 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801684 1 20081206 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 FLOOR SEAT TRACKS AT LBL AND RBL 9 BETWEEN FS 581.00 AND FS 677.00 BOTTOM SIDE CORRODED. REPLACED LBL 9 FLOOR SEAT TRAC KS BETWEEN FS581.00 AND FS677.00 IAW CRJ700 AMM 53-00-49-400-801. NO DEFECTS NOTED. REWORKED AND REINSTALLED RBL 9 FLO OR SEAT TRACKS BETWEEN FS581.00 AND FS677.00. REWORK WITHIN ALLOWABLE DAMAGE LIMITS PER CRJ 700 SRM 53-31-49. REINSTALL ATION IAW CRJ700 AMM 53-00-49-400-801. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801686 1 20081206 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 874AS 7551 LT FS 484 ANGLES CRACKED AT LBL 27 AND LBL 36 (PREVIOUS REPAIR). 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801625 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RT SIDEWALL SEAT RAIL FS 485.00 TO FS 565.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .008, WITHI N LIMITS PER SRM 53-31-49. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801653 1 20081204 A 2750 ECU CNDAIR CL600 CL6002B19 1900309 EA TE FLAP UNKNOWN A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 923EV 7826 AIRCRAFT RETURNED TO ATL AFTER T/O. FLT 5558 DEL 122 MINS. FLAP ELECTRONIC CONTROL UNIT FECU CHANNELS, A/C WITH SKEW D ETECTION SYSTEMS FLAP POWER DRIVE UNIT MOTORS. REMOVED AND REPLACED RT MOTOR AND BRAKE ASSY IAW AMM 27-52-05. OPS CHEC K GOOD IAW AMM 27-64-00. DEFER CLEARED PLACARD REMOVED. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801628 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LT SIDEWALL SEAT RAIL FS 677.00 TO FS 708.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .015, WITHI N LIMITS PER SRM 53-41-49. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801633 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RT SIDEWALL SEAT RAIL FS 785.15.00 TO FS 863.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .011, WI THIN LIMITS PER SRM 53-41-49. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801666 1 20081205 A 5312 ANGLE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 CORROSION DAMAGE FS 280 BULKHEAD LOWER ANGLE AT ENTRANCE TO FLT COMPT LBL 10. CORROSION LBL 10 OF FS 280 BULKHEAD WAS T REATED BY ACCOMPLISHING DAMAGE 1 SPOT A OF REO 670-53-11-370. REINSTALLED RIVETS AT LBL 10 280 DOOR POST 13" FROM 280 B EAM, ALL WORK IAW CRJ 700 SRM 51-42-06. MEASURED BLENDED AREA OF FOUND TO BE .010" OF MATERIAL REMOVED. WORK DONE IAW CRJ 700 SRM 51-11-00, NDTM 51-20-06 SUBMITTED DAMAGE TO CRC. 2 L 7 2 4F RT A21EA 20081210 NM 2008 12 10 USAA2008120992197 1 20081207 A 5315 D5311146100200 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 806AW 1056 PIT - C6 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT -Y1292, FR16. REPLACED FLOORBEAM AT -Y1292, FR16 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081210 NM 2008 12 10 USAA2008120992198 1 20081207 A 5315 D5311146100200 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 806AW 1056 PIT - C6 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT -Y1292, FR20. REPLACED FLOORBEAM AT -Y1292, FR20 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081210 NM 2008 12 10 USAA2008120992199 1 20081209 A 3397 BMS1348 WIRE BOEING 767 7672B7ER 1385107 NM CABIN BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 253AY 24894 BFM - C4 - EEL - EMERGENCY CEILING LIGHT WIRE BROKEN AT SEAT ROW 25AB. REPAIRED BROKEN WIRE IAW B757 SWPM 20-30-12. 2 L 7 2 4F RT A1NM 20081210 NM 2008 12 10 USAA2008120992202 1 20081208 A 3350 201310 BATTERY BOEING 767 7672B7ER 1385107 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 253AY 24894 BFM - C4 - EEL - EMERGENCY CEILING LIGHT BATTERY AT SEAT 29G IS INOP. REPLACED EMERGENCY LIGHT BATTERY IAW B767 AMM 33- 51-07. 2 L 7 2 4F RT A1NM 20081210 NM 2008 12 10 USAA2008120992203 1 20081204 A 5315 6545812 FLOORBEAM BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - CRACK ON FLOORBEAM VERTICAL STIFFENER AT BS 328, LBL 45. REPAIRED FLOORBEAM VERTICAL STIFFENE R AT BS 328, LBL 45 IAW B737 SRM 51-30-01 & BOEING DRAWING 65-45812. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 USAA2008120992204 1 20081130 A 5311 6546526 DOUBLER BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - CRACK ON FRAME REPAIR DOUBLER AT BS 400 BETWEEN S8R & S9R. REPLACED FRAME REPAIR DOUBLER AT B S 400 BETWEEN S8R & S9R IAW US AIRWAYS EA 100748. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 USAA2008120992205 1 20081203 A 5320 ANGLE BOEING 737 7374B7 138449C NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - CORROSION ON CREASE Z-ANGLE AT BS 958 TO BS 994, LBL 55. REPAIRED CREASE Z-ANGLE AT BS 958 TO BS 994, LBL 55 IAW B737 SRM 51-07-11. 2 L 7 2 4F RT A16WE 20081210 NE 2008 12 10 USAA2008120592185 2 20081202 A 7230 3353523030 BEARING AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565A1 NE NR 2 ENGINE FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 19 184US 1651 FLT 1419 PHL-LAX - EMERGENCY LANDING - CREW REPORTED A COMPRESSOR STALL AT FL310 ON THE NR 2 ENGINE. AIRCRAFT DESCENDED TO 280 AND VIBRATIONS CONTINUED. ENGINE WAS SHUT DOWN DUE TO BLUE ELECTRICAL SYSTEM FAILURE. CREW DECLARED AN EMERGEN CY AND DIVERTED TO COS. MX R&R THE NR 2 ENGINE DUE TO FAILED BOROSCOPE. ALSO REPLACED BLUE SYSTEM HYDRAULIC RESERVOIR PRESSURIZATION LINE AND HYDRAULIC LINE FROM PUMP TO ACOUSTIC FILTER DUE TO CHAFING. 2 L 7 2 4F 4 F RT A28NM E29NE 20081210 NM 2008 12 10 AALA200802342A 1 20081016 A 2560 P4010021000 BATTERY BOEING 777 777223 1385213 NM FLASHLIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 EMERGENCY FLASHLIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081210 NM 2008 12 10 AALA200802355A 1 20081018 A 2780 90004213 SENSOR BOEING 737 737823 13844CB NM SLAT SYS FAILED A AALA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SW 21 917AN 29518 IAD INFLIGHT - LEADING EDGE SLATS WOULD NOT EXTEND. LANDED AT IAD WITHOUT INCIDENT DUE TO LONGER RUNWAY. REPLACED NUMB ER FOUR LEADING EDGE RETRACT SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20081210 NM 2008 12 10 FDEA200811194920 1 20081119 A 5330 65545803 SKIN BOEING 727 7272S2F 1384O81 NM ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 LOWER RIGHT EXTERIOR FUSELAGE SKIN IS CHAFED AT AFT CARGO PIT DOOR CUTOUT FWD LWR CORNER STA 950E, STR 26-R REPAIRED FWD LOWER CORNER OF FUSELAGE SKIN AT AFT CAGO DOOR CUT OUT REF EA 7- 5330-123818. BLENDED FOUND OUT OF LIMITS. ORIGINA L .080" , REMAINING .038 . TREATED AND PRIMED. THIS IS CLASSIFIED AS A MAJOR REPAIR 2 L 7 3 4F A3WE 20081210 EU 2008 12 10 FDEA200812065100 1 20081206 A 5320 A5397823700200 FITTING AIRBUS 310 A310203 3930313 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 429FE 364 AFT CARGO DOOR NR 2 DOOR LOCK FITTING HAS 1 GOUGE ON OTBD MOUNT AND 2 GOUGES ON INBD MOUNT REMOVED AND REPLACED AFT CARG O DOOR FITTING AT FR 60A IAW A310 SRM 51-40-21. 2 L 7 2 4F RT A35EU 20081210 NM 2008 12 10 FDEA200812065101 1 20081206 A 5714 APB74411 SKIN DOUG MD11 MD11F 3023600 NM CENTER WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 MAIN DECK, UNDER FLOOR CENTER WING UPPER PANEL UPPER SURFACE FOUND CORROSION AT STATION 1229, -X97, RIGHT. REPAIR CAR RIED OUT AS PER EA 1-5710-122662. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081210 NM 2008 12 10 FDEA200812075102 1 20081207 A 5330 655458321 SKIN BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 495FE 21669 BS 1183 TO 1148 AT STR 26L HAS SURFACE CORROSION ON INNER SKIN REMOVED CORROSION AND FOUND OUT OF LIMITS REPAIRED SKIN I AW EA 7-5330-126867. 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 FDEA200812075103 1 20081207 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272S2F 1384O81 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 AT RBL 24 STA 1148 FLOORBEAM UPPER FLANGE CORRODED. DUE TO FLOOR SUPPORT REPAIR 1'4 INCH HOLE IN SEAT TRACK WILL NOT HA VE EDGE DISTANCE IF DRILLED IN SAME LOCATION AS ORIGINAL. SEE SNRM N00516 FOR FLOOR REPAIR DUE TO "T" CAP REPLACEMENT, A 1/4 INCH HOLE REQUIRED IN SEAT TRACK WOULD HAVE BEEN IN RADIUS OF "T" CHORD. CUT OUT AND SPLICED IN NEW SECTION OF SE AT TRACK FROM STA 100-1148 REF SRM 53-10-5 FIG 1 AND RELOCATED AFFECTED FASTENER HOLE. EA 7-5310-1232825 AUTHORIZES MAT ERIAL SUBSTITUTION ON STRAP. THIS IS CLASSIFIED AS A MAJOR REPAIR 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 FDEA200812085104 1 20081208 A 5311 6516312146 FRAME BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 469FE 21581 NOSE WHEEL WELL "T" ANGLE CORRODED STA 280 STR 26R. FABRICATED NEW "T" ANGLE FROM 60-10936 7075-0 EXTRUSION PO NR 82702 23 DIMS 19 INCH BY 3 INCH, HEAT TREATED EXTRUSION TO T-6 CONDITION INSTALLED NEW "T" ANGLE AT BS 280 STR 26R IAW MM 51-3 0-5 AND BOEING DWG 65-18414 AND SRM 51-30-2. 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 FDEA200812085105 1 20081208 A 5310 65198618 BEAM BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 469FE 21581 E AND E COMPT HORIZ WALKWAY BEAM HAS CORROSION WITH EXFOLIATION RBL 12 BS 344. REMOVED AND REPLACED LWR CHORD WALKWAY B EAM AT RBL12 BS 294-360 WITH NEW CHORD P/N 65-19861-8 PO NR 827074 IAW SRM 51-30-5 AND SRM 51-30-2. 2 L 7 3 4F A3WE 20081210 NM 2008 12 10 FDEA200812085107 1 20081208 A 5330 53FX130122 SKIN BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 469FE 21581 FASTENERS WITH IMPROPER SPACING STA 440 ABOVE AND BELOW STR 14L. REPAIRED AREA IAW EA 7-5330-126868 FUSELAGE SKIN AD 98 -11-03 MAIN CARGO DOOR CUTOUT FUSELAGE SKIN LAP JOINT THRU DAMAGE AT STA 440 S14L. 2 L 7 3 4F A3WE 20081211 WP 2008 12 11 AALA200810321 1 20081119 A 5340 MOUNT DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 CABIN, CORROSION ON G-2 GALLEY FORWARD INBOARD FLOOR MOUNT STATION 207. INSTALLED SERVICEABLE GALLEY MOUNT PER SRM 51-0 1. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810353 1 20081119 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 CABIN, NUMBER 4 SEAT TRACK HAS BROKEN EAR AT STATION 980. INSTALLED REPAIR PLUG PER AARD 53-20-00-10. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810343 1 20081119 A 5311 FRAME DOUG DC9 DC983 3022083 WP ZONE 200 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 AFT SIDE OF FRAME HAS DEEP WEAR MARK FROM CONTACT WITH G1 GALLEY STATION 148 LONGERON 4 RIGHT. INSTALLED DOUBLER PER ES O 80559 DATED 11-18-08. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810349 1 20081120 A 5311 FRAME DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 CORROSION IN FRAME 1287 BETWEEN LONGERON 25 LEFT AND LONGERON 29 RIGHT. INSTALLED JAY ANGLE. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810350 1 20081120 A 5310 BEAM DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 MID CARGO DOOR BEAM AND DOUBLERS BETWEEN STATION 636 AND STATION 693 ARE CORRODED, OUT OF LIMITS. INSTALLED DOOR BEAM D OUBLER PER AARD 53-10-00-3. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810351 1 20081120 A 5322 SHEAR TIE DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 SHEAR TIE CORRODED AT STATION 674 FROM LONGERON 29 LEFT TO LONGERON 29 RIGHT. INSTALLED NEW SHEAR TIE AND SPLICE AT STAT ION 674, FROM LONGERON 29 LEFT AND LONGERON 29 RIGHT PER SRM 53-03-00 FIGURE 3 SHEET 1. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810363 1 20081122 A 5320 ANGLE DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 MID-CARGO, CORROSION ON CARGO DOOR CUTOUT THRESHOLD CHORD ANGLE STATION 636 TO 680. REPAIRED PER AARD 53-10-00-3. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 ASOA200801664 1 20081205 A 5200 WEB CNDAIR CL600 CL6002B19 1900309 EA DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 FOUND CRACK IN INNER SKIN WEB PLATE UNDER OUTER HANDLE DETENT APPROX .25 INCH LONG. 2 L 7 2 4F RT A21EA 20081211 WP 2008 12 11 AALA200810373 1 20081126 A 5340 MOUNT DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 G2 GALLEY INBOARD GALLEY MOUNT CORRODED IN HOLE AND TOP. NEW GALLEY MOUNT WAS INSTALLED PER SRM 51-01. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 ASOA200801588 1 20081201 A 5534 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RT VERTICAL FWD DRAG ANGLE APPEARS CRACKED. PERFORMED EDDY CURRENT INSPECTION OF RIGHT FORWARD VERTICAL STAB TO FUSELAG E DRAG ANGLE IAW CRJ 700 NDTM 51-20-006. DRAG ANGLE CONFIRMED CRACKED AND MARKED. RT DRAG ANGLE REPAIRED PER REO 670-5 5-31-018. 2 L 7 2 4F RT A21EA 20081211 WP 2008 12 11 AALA200810334 1 20081116 A 5320 SUPPORT ANGLE DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 948TW 49575 INTERCOSTAL SUPPORT ANGLE CRACKED AT STATION 237 BETWEEN LONGERON 28 RIGHT AND LONGERON 27 RIGHT. INSTALLED INTERCOSTAL SUPPORT ANGLE AT STATION 237 BETWEEN LONGERON 28 RIGHT AND LONGERON 27 RIGHT PER SRM 51-30-5. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 ASOA200801654 1 20081119 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 PAX DOOR OUTER HANDLE IS CRACKED. 2 L 7 2 4F RT A21EA 20090105 NM 2009 1 5 C8GA20080054 1 20080823 A 5754 MOUNT BOEING 727 727223 1384074 NM SLAT ACTUATOR CRACKED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE NR 7 SLAT ACTUATOR OB MOUNTING BRACKET HAD A 1" C RACK. REMOVED CRACKED SUPPORT. FABRICATED NEW DOUBLER AND NEW STIFFNER. INSTALLED NEW SUPPORT PARTS IAW SB 727-57-0130. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20081211 WP 2008 12 11 NWAA085329852 1 20081201 A 3397 WIRE DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 761NC 47709 DURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 14-18 OF THE CABIN WERE INOPERATIVE. MX REPAIRED THE WIRING AND FUNCTIONALLY CHECKED THE SYSTEM. 2 L 7 2 4F RT A6WE 20081211 EU 2008 12 11 NWAA085333241 1 20081201 A 3350 LAMP AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 341NW 380 EMERGENCY EGRESS LIGHTING INOP ON ROWS 15, 16, 17, 21, 22, 23. RELAMPED AND REPLACED EPSU 11WL. CHECKS OK. 2 L 7 2 4F RT A28NM 20081211 EA 2008 12 11 ASOA200801609 1 20081203 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 PAX DOOR AFT DRAG ANGLE IS CRACKED AT DOOR ASSIST CABLE PULLEY BRACKET APPROX 1 INCH LONG. REPAIRED PAX DOOR AFT DRAG A NGLE IAW CRJ 200 PER REO 601R-52-11-513 ASA RII C/W: 5300014. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801610 1 20081203 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 LBL 36.0 FS 484 INTERCOSTAL CRACKED. REMOVED OUTBOARD PULLEY AND BRACKET AND SLID FWD. REMOVED CRACKED ANGLE. FABRICA TED NEW ANGLE BRACKET. ANGLE BRACKET REQUIRES HOLE TRANSFERS AND FURTHER SHAPING. AFTER REPAIR OUTBOARD CONTROL CABLE PULLEY AND BRACKET ON FS 484 REQUIRES INSTALLATION. REPLACED LBL 360 FS 484 INTERCOSTAL CLIP IAW REO 601R-53-41-069. I NSTALLED OUTBOARD CONTROL CABLE PULLEY BRACKET IAW SRM 51-41-02. C/W EC/TC REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 NWAA085286739 1 20081124 A 5330 SKIN BOEING 747 747251F 1384898 NM BS 674 S38 GOUGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 639US 23887 DURING GROUND OPS FUSELAGE SKIN WAS DENTED AND GOUGED AT AFT EDGE OF FORWARD CARGO DOOR CUTOUT AT BS 674 S38 AND FRAME C HORD WAS DENTED JUST BELOW S37. REPAIRED PER EA 67-214354 SECTION I AND SECTION II. SECTION III TO BE DETERMINED PER B OEING DATA TOLERANCE ANALYSIS. 2 L 7 4 4F RT A20WE 20081211 NM 2008 12 11 NWAA085436301 1 20081208 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING AN OVERNIGHT LINE CHECK THE AFT MOST 2 SLIDE ILLUMINATION LIGHTS ON THE ACFT RT WOULD NOT TEST. MX FOUND THE ASS OCIATED POWER SUPPLY MODULE AND BATTERY TO BE DEFECTIVE AND REPLACED THEM. SYSTEM OPS WAS NORMAL AFTER THE POWER SUPPLY AND BATTERY WERE REPLACED. 2 L 7 4 4F RT A20WE 20081211 NE 2008 12 11 PCSA2008120301 2 20081203 A 7230 BLADE PWA 17 BOEING 727 727233 138408A NM PWA JT8 JT8D17 52049 NE NR 1 ENGINE BROKEN A PCSA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 SO 17 495AJ 707212 20937 707212 AMERIJET FLIGHT SXM - SJU NUMBER ONE ENGINE VIBRATION FOLLOWED BY HIGH FUEL FLOW. PERFORMED A PRECAUTIONARY SHUTDOWN. MAINTENANCE DISCOVERED A BROKEN C2 BLADE AND COMPRESSOR DAMAGE. 2 L 7 3 4F 4 F RT A3WE E2EA 20081211 NM 2008 12 11 AALA200820073 1 20081118 A 5320 146N876948 CHANNEL BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 688AA 55898 25730 HAT CHANNEL CORRODED. REPLACED HAT CHANNEL IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20081211 EA 2008 12 11 SWIA200820600 1 20081206 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 FLT 6469 - LEFT WINDSHIELD CRACKED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 AALA200820072 1 20081118 A 5320 146N876948 CHANNEL BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 688AA 55898 25730 CORROSION ON HAT CHANNEL FLOOR THRESHOLD SUPPORT AT R NR 4 PASSENGER/SERVICE DOOR. REPLACED HAT CHANNEL IAW SRM 53-00-5 1. 2 L 7 2 4F RT A2NM 20081211 2008 12 11 VNAA2008120800002 4 20081203 A 3418 STALL WARNING CNDAIR CL600 CL6002C10 1390015 EA COCKPIT MALFUNCTIONED A VNAA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 GL 05 725PS 10186 CREW REPORTED ON TAKEOFF A 'STALL FAIL' CAS MSG. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANC E PERFORMED OPS CHECK OF SPS AND FOUND NO DEFECTS. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081211 WP 2008 12 11 AALA200810370 1 20081124 A 5320 ANGLE DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 AFT CARGO DOOR THRESHOLD CHORD ANGLE CORRODED FROM STATION 1155 TO 1212. REPLACED BEAM PER AARD 53-10-00-3. 2 L 7 2 4F RT A6WE 20081211 WP 2008 12 11 AALA200810372 1 20081126 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 CORROSION ON LOWER SIDE OF RIGHT CUSP STATION 560. REPAIRED PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081211 EA 2008 12 11 VNAA2008120900003 1 20081201 A 4920 APU CNDAIR CL600 CL6002B19 1900309 EA HUNG START A VNAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 05 260JS 7957 CREW REPORTED ON DESCENT INTO DAY, APU EXPERIENCED A HUNG START. MOMENTS LATER THE CREW TRIED TO START APU AND WAS SUCC ESSFUL. BLEED AIR WAS SELECTED TO APU AND A STRONG FUEL SMELL WAS EVIDENT IN COCKPIT AND CABIN. APU WAS SHUTDOWN AND A IRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED APU AND APU COMPARTMENT FOR LEAKS. NO LEAKS WERE EVIDENT. NO O THER DEFECTS WERE NOTED AND AIRCRAFT WAS RELEASED FOR SERVICE. NOTE: RESIDUAL FUEL WAS EVIDENT IN THE APU EXHAUST DRAI N. THIS WAS SUSPECTED TO BE EXCESS FUEL FROM THE HUNG START. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801672 1 20081206 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 FLOORBEAM CAP HAS CORROSION AT RBL 9 BETWEEN FS 485.00 AND FS 501.00. FLOORBEAM RBL 9 FS 485 THRU 565 REMOVED AND REPLA CED PER REO 670-53-00-172, REO 670-53-00-029, CRJ 700 SRM 51-21-06, CRJ 700 SRM 51-11-00, CRJ 700 NDTM 51-20-006, REO 67 0-53-31-124. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801687 1 20081206 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 874AS 7551 RT FS 484 ANGLE CRACKED AT RBL 27 (PREVIOUS REPAIR). 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801616 1 20081203 A 5320 ANCHOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 FIVE CARGO BAY PLATE ANCHORS ARE CORRODED. REMOVED AND REPLACED 5 EACH CARGO DOOR ANCHOR PLATES IAW SRM 51-41-04. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801636 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LT FLOOR SEAT RAIL FS 379.00 TO 485.00 HAS CORROSION DAMAGE (MARKED). REMOVED LHS FLOOR SEAT RAIL FS379.00 TO 485 WORK DONE IAW CRJ 700 SRM 51-41-02. INSTALLED NEW SEAT RAIL PER CRJ 700 AMM 53-00-49. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 COMA2008120850022 1 20081207 A 2760 SECU CNDAIR CL600 CL6002B19 1900309 EA SPOILER SYS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 597SW 7293 ON APPROACH INTO CVG, RECEIVED GND SPOILER DEPLOY, FLT SPOILERS AND SPOILERONS CAUTION MSG'S. EMERGENCY DECLARED, A/C L ANDED SAFELY. RESET SECU'S, OPS CHECK OF SPOILER SYSTEM GOOD. 2 L 7 2 4F RT A21EA 20081211 EU 2008 12 11 YENA200812090126 1 20081204 A 2131 2079102AB CONTROLLER AIRBUS 320 A320232 3930326 EU NR 1 FAILED A YENA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 633JB 8703 195 2671 FLT 215, JFK-LGB, DIVERTED RAP, CAB PRESS SYS 1, ECAM IN FLIGHT. CPC NR 1 FAILED BITE TEST. REMOVED AND REPLACED CPC N R 1 IAW 21-31-34. BOTH CPC BITE TEST GOOD. 2 L 7 2 4F RT A28NM 20081211 NM 2008 12 11 QXEA2008121001229 1 20081203 A 3233 ROD END BOMBDR DHC8 DHC8402 1390042 NM LT MLG ACTUATOR OUT OF RIG A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 19 417QX 4086 PDX - UPON GEAR RETRACTION LEFT GEAR DOOR LIGHT AND LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED FOR APPROX 20-30 SEC'S A FTER OTHER LIGHT EXTENSION LIGHTS WENT OUT. VISUALLY CONFIRMED GEAR UP. GEAR EXTENDED NORMALLY AT LANDING. C/W RIGGIN G OF LT MLG RETRACT ACTUATOR ROD END IAW AMM 32-31-11-830-801. OPS CHECK OF MLG PRIMARY EXTENSION AND RETRACTION, CHECK S GOOD IAW AMM 32-31-00-710-801. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081211 NE 2008 12 11 RYNA200800044 2 20081128 A 7230 FAN BLADE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE RT ENGINE OUT OF BALANCE A RYNA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 07 123DN 23437 DURING CLIMB AND LEVEL OFF AT F/L 370 RIGHT ENGINE VIBRATION REACHED 3.9 UNITS. THE AIRCRAFT DIVERTED TO ATLANTA FOR MA INTENANCE TO DELTA AIRLINES MAINTENANCE CENTER. ACCOMPLISHED BORESCOPE INSPECTION, FAN BLADE LUBRICATION, RIGGED VSV & VBV SYSTEM AND BALANCED THE FAN BLADES. PERFORMED ENGINE RUN AND ALL SYSTEMS & PARAMETERS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 20081211 EA 2008 12 11 SWIA200820605 1 20081206 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 706SK 10149 FLT 6487 - CEILING EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 QXEA2008121001212 1 20081125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 412QX 4059 PDX - C4 - AFT END OF SEAT TRACK NR 8 SEAT TRACK IS CORRODED AROUND FASTENERS ON OTBD FLANGE. REMOVED FRONT A HI LITES AND SOLID RIVETS FROM FRONT SPLICE IAW SRM 51-40-07 AND 51-40-15. MATCH DRILLED NEW TRACK FROM STOCK AND INSTALLED IAW SRM 51-41-05 AND 51-42-05 AND 51-40-15. 2 H 7 2 4T RT A13NM 20081211 WP 2008 12 11 15HA0858011A 1 20081015 A 7921 862501 OIL COOLER CVAC 340 340CVAC 242270A WP RT ENGINE LEAKING A I5HA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 25 584E 24 WHILE IN FLIGHT, THE CREW OBSERVED THE OIL QUANTITY ON THE RT ENGINE DECREASING. AS THE OIL QUANTITY CONTINUED TO DECRE ASE, THE CREW ELECTED TO SHUT DOWN THE ENGINE AS A PRECAUTIONARY MEASURE. THE CREW DIVERTED TO ST MARTIN SMX AND MADE A N UNEVENTFUL LANDING. MX INSPECTION REVEALED A LEAK IN THE RT OIL COOLER. THE OIL COOLER WAS REPAIRED IAW MM AND THE A CFT RETURNED TO SERVICE. 2 L 7 2 4R 6A6 20081211 WP 2008 12 11 AALA200802372D 1 20081021 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 955U 49427 LGA - EMERGENCY FLASHLIGHT STRAP BROKEN AT FORWARD GALLEY. REPLACED FLASHLIGHT STRAP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081211 NM 2008 12 11 UPS08M54092 1 20081206 A 5230 DOUBLER DOUG MD11 MD11F 3023600 NM FWD CARGO DOOR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP INSPECTION TYPE:N/A GOUGE IN PREVIOUS REPAIR ON FWD CARGO DOOR AFT LOWER SIDE. REPAIRED IAW EO MD11-5330-31459-A. 2 L 7 3 4F RT A22WE 20081211 NM 2008 12 11 DU4R2008267 1 20081207 A 5524 FITTING BOEING 757 75723APF 1384966 NM RT ELEVATOR CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 868AN 24868 DURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND CORRODED ANGLE FITTING ON RT ELEVATOR STRAKELET. 2 L 7 2 4F RT A2NM 20081211 EA 2008 12 11 COMA2008121050023 1 20081209 A 3234 555405 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 27 931CA 24339 7037 ON APPROACH INTO ORD RECEIVED GEAR DISAGREE MSG AND NOSE DOOR WARNING MSG ON GEAR EXTENSION. BOTH MSG'S EXTINGUISHED PR IOR TO RUNNING QRH. NO EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED NLG DOOR SELECTOR VALVE. 2 L 7 2 4F RT A21EA 20081211 SO 2008 12 11 C2XA08IA249 1 20081203 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14904 145477 IAH - DURING MAINTENANCE INSPECTION SEVERAL EMERGENCY LIGHTS IN THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS A PPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081211 NM 2008 12 11 DL764081649 1 20081126 A 2750 FLAP SYSTEM BOEING 767 767432ER 1385134 NM TE FLAPS MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 834MH 29707 ON TAXI OUT HAD T/E FLAP DISAGREE. FLAPS WERE SET TO 5 DEG IND SHOWED 1 DEG. RECYCLED UP AND BACK TO 5 DEG WITH SAME R ESULTS. PER FIM RAN BIT OF FSEU, EXISTING FAULT RT FLAP/STAB POS MSG 27-51103. RAN FLAPS IN ALT. RAN FLAPS IN NORMAL, FLAPS OPERATE NORMAL. BIT LT/CTR/RT FSPM, BIT GOOD. COMPLETED FIM PROCEDURE, SYSTEM IS OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20090105 NM 2009 1 5 C8GA20080055 1 20080820 A 5753 SKIN BOEING 727 727223 1384074 NM RT WING TE FLAP DAMAGED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE RIGHT WING IB AFT FLAP BOTTOM SIDE UNDERNEATH TEA RDROP AREA DELAMINATED. REMOVED DAMAGED AREA, FABRICATED CORE. FABRICATED DOUBLER. INSTALLED REPAIR HOT BONDED & SEALED CORE AND DOUBLER. IAW SRM 51-40-20. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2008022700224 20080227 00224 NM 2008 2 27 CALA0800138 1 20080213 A 5320 141T5190124 FLOOR SUPPORT BOEING 767 767424ER 1385270 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 66051 29446 STA 303 TO STA 325 LBL 30" FLOOR SUPPORT FOUND CORROSION. REMOVED AND REPLACED AFT FLOOR PANELS PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008022700254 20080227 00254 WP 2008 2 27 IXXA08SMN001S 1 20080111 A 5730 SKIN DOUG DC8 DC862F 3021972 WP LT WING CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LOWER SKIN CENTRAL LEADING EDGE CRACKED AT STATION XF 428.000. REMOV ED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION DETECT ED AFTER TEST. FABRICATED REPAIR DOUBLER AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08030 DATED 01-22-08, SEMAN DRAWING ED-4685 DATED 01-12-08, DC8 SR M 51-1-21, 51-1-20D, 51-3-0, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B,DC8 SRM 51-1-11, 51-1-20D, AND 51-3-1. 2 L 7 4 4F 4A25 2008022700279 20080227 00279 EA 2008 2 27 SWIA200819227 1 20080212 A 2913 6619004 PUMP CNDAIR CL600 CL6002D24 1390016 EA HYD SYSTEM LEAKING A SWIA O OTHER K FLUID LOSS AP APPROACH 1 NM 07 807SK 2115 2115 15082 THE HYDRAULIC SYSTEM 1 QUANTITY READ "0", FLIGHT NR 4089. REPLACED NR 1 ENGINE DRIVEN PUMP AND INSPECTED NR 1 HYDRAULIC SYSTEM PRESSURE MANIFOLD DELTA P INDICATORS IAW MM 29-11-01. OPS AND LEAK CHECK OK. 2 L 7 2 4F RT A21EA 2008022700296 20080227 00296 NM 2008 2 27 NWAA080615523 1 20080221 A 2530 OVEN BOEING 757 757251 1384970 NM GALLEY SMOKE A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 523US 23617 FAR RIGHT FORWARD OVEN STARTED SMOKING, TURNED IT OFF AND BACK ON, AND IT STARTED SMOKING AGAIN, SO TURNED IT OFF AND PU LLED THE C/B. MAINTENANCE REMOVED AND REPLACED FIRST CLASS OVEN, OPERATIONAL CHECKED GOOD, AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2008022700298 20080227 00298 NM 2008 2 27 08FDEA00603 1 20080226 A 5730 ARB74023 SKIN DOUG MD11 MD11F 3023600 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 FOUND SIX FASTENER HOLES CRACK INDICATION DURING HFEC, OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT OUT BE TWEEN STA XORS = 690 AND XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-118760 PART 1, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008022700313 20080227 00313 EA 2008 2 27 SIMA200805705 1 20080222 A 3230 533407 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA MLG MALFUNCTIONED A SIMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 21 511AE 10107 ON FLIGHT 3757, CREW REPORTED LANDING GEAR WOULD NOT EXTEND. PERFORMED MANUAL/EMERGENCY EXTENSION. ENGINE HYDRAULIC PU MP PRESSURE WAS NORMAL. CREW ATTEMPTED TO EXTEND GEAR 3 TIMES BUT FAILED. DID GET A LG DISAGREE WARNING. HAD TO DO A GO AROUND TO GET GEAR DOWN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE AS PER AMM 52-32-10. PERFORMED OPERATIONAL CHECK OF LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT A21EA 2008022700330 20080227 00330 NM 2008 2 27 UIEA200800054 1 20080215 A 5313 STRINGER BOEING 747 7472D7B 1384803 NM ZONE 100 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 AFT CARGO COMPARTMENT LEFT SIDE STRINGER 51 CORROSION AT STATION 1540, LEVEL 1 CORROSION. AFT CARGO STRINGER CORROSION REPAIRED IAW SRM 51-10-01. APPLIED FINISH IAW 51-21-00. 2 L 7 4 4F RT A20WE 2008022700348 20080227 00348 NM 2008 2 27 SWAA080869 1 20080217 A 5322 6546567 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 1006, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008022700356 20080227 00356 NM 2008 2 27 SWAA080904 1 20080218 A 2560 PH22300L GLOWSTRIP BOEING 737 7373G7 1384595 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 1 DEF. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008022800013 20080228 00013 NM 2008 2 28 HALA0800305 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 467 S38R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 467 BETWEEN LONGERONS S38R AND S39R. CLEANED, TREATED AND PRIMED PER SRM 53-00-01. PAINT PEND. AREA PAINTED AS PER SRM 51-22-01. 2 L 7 2 4F RT A1NM 2008022800016 20080228 00016 NM 2008 2 28 HALA0800288 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 396 S35-36R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 396.5 BETWEEN LONGERONS S-35R AND S-36R, MARKED NR 13. REPAIRED PER SRM 53-00-01-ZR -8 CAT C REPAIR (TEMP). REPETITIVE INSPECTIONS EVERY 1500 CYCLES. PERMANENT REPAIR AT 6000 CYCLES. 2 L 7 2 4F RT A1NM 2008022800017 20080228 00017 NM 2008 2 28 HALA0800290 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 322 S36-37R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 322 BETWEEN LONGERONS S-36R AND S-37R, MARKED NR 14. CLEANED PER SRM 53-00-01. ACC OMPLISHED INTERIM REPAIR PER HAL M105 580055. PERMANENT REPAIR BY 1000 CYCLES OR NEXT C-CHECK, WHICHEVER COMES FIRST. 2 L 7 2 4F RT A1NM 2008022800022 20080228 00022 NM 2008 2 28 HALA0800289 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 390 S38R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 390 AT LONGERON S-38R, MARKED NR 21. REPAIRED PER SRM 53-00-01-ZR-8 CAT C REPAIR (T EMP). REPETITIVE INSPECTIONS EVERY 1500 CYCLES. PERMANENT REPAIR AT 6000 CYCLES. 2 L 7 2 4F RT A1NM 2008022800028 20080228 00028 NM 2008 2 28 HALA0800281 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 654 S36R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 654 + 121 AT LONGERONS S-36R, MARKED NR 34, AREA INSPECTED. FASTENER DAMAGE W/I LIM ITS AS PER SRM 53-0001/101 FASTENER CLEANED/PRIMED/PAINTED. FASTENER REQ'D TO BE REPAIRED AS PER SRM 53-00-01, REPAIR A T OR BEFORE 50 FLT CYCLES. 2 L 7 2 4F RT A1NM 2008022800033 20080228 00033 NM 2008 2 28 HALA0800331 1 20080218 A 5510 STRUCTURE BOEING 717 717200 1383700 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION, ON LT HORIZ STAB INBD L/E LOWER INBD ATTACH AFT END. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800057 20080228 00057 NM 2008 2 28 HALA0800338 1 20080219 A 5414 SKIN BOEING 717 717200 1383700 NM LT NACELLE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION, ON LT ENGINE PYLON T/E ASSY LOWER SURFACE. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800079 20080228 00079 WP 2008 2 28 IXXA08SMN028S 1 20080122 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND LT WING UPPER SKIN CORRODED AROUND FASTENERS AT STATION XRS 420.000 STRINGER 5. REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR APPLI ED SEALANT ON BLEND OUT AREA. PERFORMED INSPECTION NDT NO CRACK, NO CORROSION. FABRICATED REPAIR DOUBLER TAPERED REPA IR DOUBLER CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 81 10-3 NUMBER 08030 DATED 01-22-08, SEMAN DRAWING NUMBER ED-4687 DATED 01-15-08, DC8 SRM 51-1-20D, DC8 SRM 51-1-8B PAGES 1 7-18, DC8 SRM 57-2-0 PAGE 16, DC8 SRM 51-1-14, DC8 NDT SPM PART 06-10-01.001, AND DC8 SRM 51-1-12 PAGE 7, 2 L 7 4 4F 4A25 2008022800081 20080228 00081 NM 2008 2 28 HALA0800315 1 20080218 A 5347 CARGO TRACK BOEING 717 717200 1383700 NM BS 851 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION IN AFT CARGO BAY, ON FASTENER ON LEFT CARGO TIE DOWN TRACK AT STA 851. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800087 20080228 00087 WP 2008 2 28 IXXA08SMN002S 1 20080111 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND CORROSION ON LEFT WING CENTER LEADING EDGE OUTER LOWER SKIN AT STATION XFS 304. 000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGE AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION DETECTED AFTER TEST. FABRICATED REPAIR DOUBLER AND FILLER CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08030 DATED 01-22-08, SEMAN DRAWING NUMBER ED-4686 DATED 01-12-08, DC8 SRM 51-1-21, 51-1-20D, 51-3-0, DC8 SRM 51-1-8 PAGES 17- 18, DC8 SRM 57-2-1, FIGURE 2G, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND 51-3-1. 2 L 7 4 4F 4A25 2008022800092 20080228 00092 NM 2008 2 28 SWAA080921 1 20080219 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800126 20080228 00126 NM 2008 2 28 SWAA080915 1 20080215 A 5315 6545834 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 360, RBL 45 TO RBL 60. REPAIRED FLOORBEAM CHORD PER SR M. 2 L 7 2 4F RT A16WE 2008022800150 20080228 00150 NM 2008 2 28 KCSA081094 1 20080221 A 5320 STRAP BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 BULK PIT STABILIZATION STRAP CRACKED BETWEEN BS 1980 AND 2000, LBL 70. 2 L 7 4 4F RT A20WE 2008022800188 20080228 00188 2008 2 28 DL76G080157 4 20080205 A 2565 SLIDE BOEING 767 767332 1382001 NM L1 DOOR DISCONNECTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 173DZ 29692 WHILE WORKING OPN 58118 FINAL ESCAPE SYSTEM CHECK FOUND FOUND SLIDE WAS PARTIALLY DE-LACED AND BOTH FWD AND AFT DEPLOYME NT CABLES AND AND DEPLOYMENT CABLE RETRACTORS WERE NOT INSTALLED ON THE A/C. PARTS WERE ORDERED AND DISCREPANCY CORRECT ED. 2 L 7 2 4F RT A1NM 2008022800210 20080228 00210 WP 2008 2 28 AALA200800314 1 20080213 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7520A 49897 LGA - EMERGENCY LIGHTS AT FORWARD CABIN OVERHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD CABI N OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022800230 20080228 00230 NM 2008 2 28 SWAA080975 1 20080221 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008022800232 20080228 00232 NM 2008 2 28 SWAA080977 1 20080221 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008022800238 20080228 00238 2008 2 28 SWAA080982 4 20080221 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008022800254 20080228 00254 NM 2008 2 28 KCSA081110 1 20080223 A 5320 FITTING BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE LOWER SPLICE FITTING IS CORRODED AT STA 970 TO 1000, STR 38L. 2 L 7 4 4F RT A20WE 2008022800255 20080228 00255 NM 2008 2 28 KCSA081111 1 20080223 A 5210 DOOR FRAME BOEING 747 747209B 138489B NM L1 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 L1 MAIN ENTRY DOOR HAS A 3 INCH LONG CRACK IN THE FORWARD LOWER CORNER OF THE HORIZONTAL FRAME RADIUS AT STA 446 BETWEEN WL 200 & 208. 2 L 7 4 4F RT A20WE 2008022800286 20080228 00286 NM 2008 2 28 DLM90080241 1 20080122 A 5310 591746311 DOOR FRAME DOUG MD90 MD9030 3023690 NM AFT CABIN CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 AFT MAIN ENTRY FOOL SHOWS EVIDENCE OF CORROSION. REPAIRED JAMB SECTION, IAW ERA 466167-14 REV ORIG 1-30-08. 2 L 7 2 4F RT A6WE 2008022800288 20080228 00288 NM 2008 2 28 DL764080167 1 20080201 A 3397 CONNECTOR BOEING 767 767432ER 1385134 NM EMERGENCY LIGHTS LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 839MH 29712 EMERGENCY LIGHTS INOP FROM 38A TO 41A, CABLE CONNECTOR AT SEAT 42A WAS LOOSE, RECONNECTED CABLE CONNECTOR AT SEAT 42A. PERFORMED GOOD OPS CK OF EMERGENCY LIGHTS FOR SEATS 38A-41A IAW DAL B767-400MM 33-51-00 AND 33-51-05. 2 L 7 2 4F RT A1NM 2008022800289 20080228 00289 NM 2008 2 28 DL764080169 1 20080201 A 3397 CONNECTOR BOEING 767 767432ER 1385134 NM EMERGENCY LIGHTS DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 839MH 29712 EMERGENCY LIGHTS INOP AT SEATS 38FG THRU 44FG, REMOVED AND REPLACED ELECTRICAL CONNECTOR AT SEAT ROW 44FG IAW SWPM 20-10 -13 AND OPS CHECKED GOOD IAW B767-400 MM 33-51-10. 2 L 7 2 4F RT A1NM 2008022800290 20080228 00290 NM 2008 2 28 DL764080170 1 20080202 A 3397 1722331 CONNECTOR BOEING 767 767432ER 1385134 NM EMERGENCY LIGHTS DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 839MH 29712 FOUND SEAT 7AB EEPL CONNECTOR IS DAMAGED. REPLACED CONNECTOR AT SEAT 7AB, OPERATIONALLY CHECKS GOOD IN ACCORDANCE WITH B767-400 MM 33-51-00-715-200. 2 L 7 2 4F RT A1NM 2008022800297 20080228 00297 WP 2008 2 28 UPS08851694 1 20080219 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DENTED A IPXA K NONE O OTHER CL CLIMB 1 SO 01 851UP 46051 INSPECTION TYPE:N/A DENT APPROX 12 INCHES ABOVE MAIN STATIC PORT ON RT SIDE OF A/C. INSPECTED PER EO DC8-5330-28630-A. NO FURTHER DEFECTS NOTED. A 30 DAYS PERM REPAIR ACCOMPLISHED HFEC OF AREA PER DC8 SPM 06-10-01-001, NO CRACKS DETECTED . OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2008022800303 20080228 00303 NM 2008 2 28 SWAA080992 1 20080223 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, STR 17L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008022800304 20080228 00304 2008 2 28 SWAA080993 4 20080224 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008022800307 20080228 00307 NM 2008 2 28 SWAA081001 1 20080222 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS BS 747C, STR 14L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800308 20080228 00308 NM 2008 2 28 SWAA081000 1 20080222 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 28R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008022800309 20080228 00309 NM 2008 2 28 SWAA080998 1 20080222 A 5754 65C26601 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND LT WING NR 3 L/E SLAT CRACKED AT LOWER OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008022800312 20080228 00312 NM 2008 2 28 SWAA080994 1 20080222 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENA CUTOUT BS 410, BL 0. REPAIRED SKIN PE R EA. 2 L 7 2 4F RT A16WE 2008022800314 20080228 00314 NM 2008 2 28 SWAA080999 1 20080222 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND RIGHT WING NR 4 L/E SLAT CRACKED AT LOWER OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008022800322 20080228 00322 NM 2008 2 28 SWAA081045 1 20080224 A 5311 6546541 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, BETWEEN STR 3L AND STR 2R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800323 20080228 00323 NM 2008 2 28 DHL2008749007 1 20080115 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 500-520 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 MAIN CABIN SEAT TRACK CORRODED FROM BS 500 TO 520 LBL25. FABRICATED NEW SEAT TRACK SECTION FROM P/N BAC 1520-792 7178-T 6 PO NR 9006152 APPROXIMATE LENGTH 210" IAW B-727 SRM 53-10-5 FIGURE 1 AND SRM 53-10-2 FIGURE 7. INSTALLED NEW SEAT TRA CK SECTION USING PREVIOUS GOOD CONDITION SPLICES AT BS 480 TO BS 690 IAW B-727 SRM 53-10-5 FIGURE 1. 2 L 7 3 4F A3WE 2008022800332 20080228 00332 NM 2008 2 28 SWAA081042 1 20080222 A 5754 62735 FUSE BOEING 737 7373H4 1384600 NM MLG W/W FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 338SW 23960 AIR TURNBACK, AFTER TAKEOFF LEADING EDGE FLAPS TRANSIT LIGHT ILLUMINATED, TRANSIT LIGHT INDICATED ON APPROACH. REMOVED AND REPLACED LEADING EDGE RETRACT FUSE PER MM. 2 L 7 2 4F RT A16WE 2008022800336 20080228 00336 NM 2008 2 28 SWAA081007 1 20080223 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 863, STR 25L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800339 20080228 00339 NM 2008 2 28 SWAA081009 1 20080224 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008022800340 20080228 00340 NM 2008 2 28 SWAA081010 1 20080224 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 404WN 27892 DURING SCHEDULED HC1 CHECK, RT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008022800341 20080228 00341 EU 2008 2 28 08FDEA00558 1 20080222 A 5311 B53770380200 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND SEVERAL CHAFING MARKS ON INNER FLANGE OF FRAME C28, P 9-12 LT. REPAIR PERFORMED BY BLEND OUT THE AREAS AND NDT FO R CRACK FREE IAW RAS/DABRE/7008942/2008 ISS A, APPROVED BY EA 6-5314-115244. 2 L 7 2 4F RT A35EU 2008022800343 20080228 00343 NM 2008 2 28 SWAA081011 1 20080224 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 404WN 27892 DURING SCHEDULED HC1 CHECK, LT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081211 EA 2008 12 11 ASOA200801618 1 20081203 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 916EV 7757 SERVICE DOOR DIFFICULT TO OPEN. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801619 1 20081203 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 916EV 7757 SERVICE DOOR DIFFICULT TO OPEN. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801620 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LT SIDEWALL SEAT RAIL FS 863.00 TO FS 969.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION, MAX DEPTH .006 WITH IN LIMITS PER SRM 53-51-49. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801622 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LT SIDEWALL SEAT RAIL FS 379.00 TO FS 485.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .015, WITHI N LIMITS PER SRM 53-21-49. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801623 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RT SIDEWALL SEAT RAIL FS 379.00 TO FS 485.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .009, WITHI N LIMITS PER SRM 53-31-49. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801652 1 20081204 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 680BR 7679 FLAP FAIL AT 0 DEGREES WHEN LANDING IN GRR, RAN QRH, DECLARED AN EMERGENCY AND A 0 FLAP LANDING UNEVENTFUL. EMERGENCY D ECLARED. FLT 5599. FOUND MOISTURE IN TORQUE TUBE. DRIED, LUBED, OP CHECKED IAW AMM 27-54-01. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801631 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 RT SIDEWALL SEAT RAIL FS 708.00 TO FS 761.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .005 WITH I N LIMITS PER SRM 53-41-49. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 FDEA200812105120 1 20081210 A 5330 2024T390100180 SKIN BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 493FE 21531 LWR FUSELAGE SKIN BETWEEN STA 950B AND 950C AT BL0 IS BULDGING WITH 2 EACH RIVET HEADS POPPED. COMPLIED WITH EA 7-5330- 124049 PART 1 BY MANUFACTURING FILLER, DOUBLER AND TRIPLER OUT OF2024T3 180/90/100C. REMOVED DAMAGE AND INSTALLED PARTS ALL IAW EA 7- 5330-124049 PART 1. MAJOR REPAIR RII. 2 L 7 3 4F A3WE 20081211 NM 2008 12 11 QXEA2008121001230 1 20081206 A 3233 465509 ACTUATOR BOMBDR DHC8 DHC8402 1390042 NM ZONE 700 MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 19 410QX 15806 4053 SEA - AFTER GEAR RETRACTION THE RED UNSAFE LIGHT AND LEFT DOOR AMBER LIGHT REMAINED ILLUMINATED FOR 6-8 SECONDS THEN WEN T OUT. FERRIED TO PDX FOR REPAIRS. PERFORMED NUMEROUS GEAR SWINGS AT VARIOUS HYD MULE FLOW RATES. NO ABNORMAL GEAR IN DICATIONS, BOTH MLG RETRACTED AT THE SAME RATE. REMOVED AND REPLACED NR 1 MLG RETRACTION ACTUATOR AS A PRECAUTIONARY ME ASURE REF W/O 72187 T/C SB84-32-55 FOR REPLACEMENT OF MLG RETRACTION ACTUATOR. C/W OPS TEST OF THE LG PRIMARY EXT AND R ET SYSTEM IAW MM TASK 32-31-00-710-801. ALSO C/W OPS TEST OF THE ALTERNATE EXTENSION SYSTEM IAW AMM TASK 32-34-00-710-8 01. BOTH OPS CHECK GOOD. NO DEFECTS NOTED. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081211 NM 2008 12 11 QXEA2008121001228 1 20081125 A 5330 DOUBLER BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 412QX 4059 PDX - C4 - LOWER TCAS ANTENNA DOUBLER PLATE HAS PITTING CORROSION. REMOVED LOWER TCAS ANTENNA DOUBLER PLATE IAW SRM 51- 42-05 PG 205 PARA 4E. MATCH DRILLED NEW DOUBLER TO AIRCRAFT, DEBURRED AND ALODINED REF SRM 51-42-00 AND 51-21-10. INST ALLED DOUBLER PLATE IAW SRM 51-42-05. 2 H 7 2 4T RT A13NM 20081211 NM 2008 12 11 QXEA2008121001209 1 20081125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 412QX 4059 PDX - C4 - NR 16 SEAT TRACK HAS CORROSION AT FUSELAGE STATION APPROX 708 TO 714. REMOVED CORROSION MAX MATERIAL REMOVED .020, TRACK OUT OF LIMITS IAW RD 8/4-53-884. REMOVED SEAT TRACK IAW SRM 51-42-05 AND 51-40-15. DRILLED NEW SEAT TRACK IAW SRM 51-40-07. INSTALLED NEW SEAT TRACK IAW SRM 51-40-15 AND 51-42-05. 2 H 7 2 4T RT A13NM 20081211 EA 2008 12 11 SWIA200820608 1 20081203 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 810SK 15093 FLT 4813 - THE SIXTH EMERGENCY CEILING FLOOD LIGHT AFT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 UPS08454082 1 20081129 A 3350 BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:N/A UPPER DECK EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK IN REF TO 747 MM 33-51-04. OPS CHECKS GOOD. THIS CLEARS M389277. PLACARD REMOVED. 2 L 7 4 4F RT A20WE 20081211 NM 2008 12 11 UPS08M54090 1 20081204 A 5210 COVER DOUG MD11 MD11F 3023600 NM L1 DOOR DEFECTIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE:N/A L1 DOOR EXTERNAL CONTROL SW COVER W/N LATCH. RE-SECURED L-1 LATCH COVER AS REQUIRED SRM 51 31 01 VO L II. 2 L 7 3 4F RT A22WE 20081211 WP 2008 12 11 UPS08854095 1 20081014 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR 803-F1-111, STA 1573-1595, L21L-L25L, WAS REPAIRED PER SRM 53-2-1 FIG 7 IS CAT B, AND REQUIRES ENGINEERING DISPOSITION. REMOVED EXISTING REPAIR. INSTALLED NEW REPAIR PER SRM 53-04-01 FIG 16 SHT 2 2 L 7 4 4F RT 4A25 2008011700082 20080117 00082 NM 2008 1 17 QXEA200800016 1 20080104 A 3060 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM PROP DE ICE SYS FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING DE DESCENT 1 NM 09 416QX 4083 STS- FLIGHT 2468. ON DESCENT OUT OF 16,000, THE PROP DE-ICE CAUTION LIGHT CAME ON. PER THE CHECKLIST, CYCLED THE SWITCH LIGHT DID NOT GO OUT. ONCE THE AIRCRAFT WAS LANDED, THE LIGHT WENT OUT, AND PERFORMED TWO TESTS ON TAXI IN. CHECKS GO OD BOTH TIMES. MAINTENANCE CHECKED THE CDS SYSTEM FOR FAULTS, NO FAULTS FOUND. PERFORMED FUNCTIONAL TEST OF THE PROP H EAT SYSTEM AND VISUAL INSPECTION OF THE PROPELLERS WITH NO FAULTS FOUND. COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SER VICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008022700219 20080227 00219 EA 2008 2 27 TRAX200800240 1 20080210 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 975EV 7599 FLAP FAIL AT 0 DEG. EMERGENCY DECLARED. FLT 4317 DEL 236 MINS. 2 L 7 2 4F RT A21EA 2008022700229 20080227 00229 NM 2008 2 27 KCSA081079 1 20080215 A 5320 WEB BOEING 747 747209B 138489B NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FORWARD BILGE TORQUE BOX UPPER WEB HAS A DENT AT STA 660, LBL 41. 2 L 7 4 4F RT A20WE 2008022700233 20080227 00233 EU 2008 2 27 08FDEA00602 1 20080225 A 7830 491B1360005002 SKIN PANEL AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 NR 1 INBD T/R UPPER FWD SKIN PANEL IS CRACKED. REMOVED DAMAGED SKIN PANEL IAW A300-600 SRM 51-40-21. FABRICATED NEW PANEL IAW A300-600 SRM 51-26-00 AND 51-40-40 AND PER FEDEX GMM N7-0-1001. INSTALLED NEW PANEL IAW A300-600 SRM 51-40-21 . 2 L 7 2 4F RT A35EU 2008022700240 20080227 00240 SO 2008 2 27 SIMA200805302 1 20080221 A 3297 14521492401 WIRE HARNESS EMB 135 EMB135KL 3260302 SO MLG CORRODED A SIMA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 21 809AE 145521 ON FLIGHT 3823, CREW REPORTED AT CRUSE AT FL360 A LOUD BANG WAS FELT AND HEARD, APPROX 5 MIN LATER ANOTHER BANG FELT AND HEARD FOLLOWED BY LOUD BUFFETING FELT THROUGHOUT AIRCRAFT. NOISE AND VIBRATION CEASED ON DESCENT THROUGH FL320 NOISE A ND BUFFET FELT LIKE NOSE LANDING GEAR DOORS HAD OPENED AT LEAST PARTIALLY BUT NO EICAS. AIRCRAFT REMOVED FROM SERVICE. WHILE PERFORMING TROUBLESHOOTING, FOUND NOSE LANDING GEAR RIGHT DOWN LOCK PROX SENSOR HARNESS NOT LOCKING PROPERLY ONTO PROX SENSOR AND FOUND CORROSION IN CONNECTOR. REMOVED AND REPLACED HARNESS ASSEMBLY AND PROX SENSOR IAW EMB 140 AMM 32 -00-03. PERFORMED OPERATIONAL CHECK GOOD OF LANDING GEAR. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008022700247 20080227 00247 WP 2008 2 27 IXXA080008S 1 20080115 A 5320 SUPPORT DOUG DC8 DC862F 3021972 WP BS 460 S29L CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO PANELS SUPPORT CRACK AT STATION 460 LONGERON 29LEFT. REMOVED FAS TENERS AS NEEDED TO PERFORM REPAIR. FABRICATED ANGLE DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INST ALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-20D, 51-1-21, DC8 SRM 53-2-0 PAGE 2E AND 2F, DC8 SRM 51-1-8B, AND 51-3-1. 2 L 7 4 4F 4A25 2008022700255 20080227 00255 NM 2008 2 27 CALA0800145 1 20080216 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 68061 29456 WHILE REPLACING EMERGENCY BATTERY AT STA 1010 CHARGER WOULD NOT TEST. REPLACED CHARGER PER AMM 33-51-07. 2 L 7 2 4F RT A1NM 2008022700261 20080227 00261 NM 2008 2 27 CALA0800147 1 20080205 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 STA 907 RBL 45 SEAT TRACK CORRODED. FABRICATED AND INSTALLED SEAT TRACK SECTION PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 2008022700303 20080227 00303 NM 2008 2 27 LYNX00008 1 20080215 A 3260 WARNING SYSTEM BOMBDR DHC8 DHC8402 1390042 NM COCKPIT ACTIVATED A 3LYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 21 504LX 536 4172 PILOT WRITE UP, AFTER TAKEOFF WHEN THE LANDING GEAR HANDLE WAS BROUGHT UP, THE ONLY INDICATION WAS THE RED LIGHTS, GEAR HANDLE LIGHTS, THE GREEN LIGHTS. CREW NEVER HEARD THE GEAR DOORS OR THE GEAR MOVE, REF QRH AND RETURNED TO FIELD, CYCLE D GEAR TWICE. MAINTENANCE COULD NOT DUPLICATE PROBLEM AND CHANGED THE LANDING GEAR SELECTOR VALVE AS A PRECAUTION. OPS CHECKS AND FUNCTIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 2008022700304 20080227 00304 NM 2008 2 27 UIEA200800063 1 20080221 A 5340 65B38174 FITTING BOEING 747 7472D3B 1384805 NM BS 1893 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 AFT CARGO DOOR FAILED TO CLOSE DURING NORMAL OPERATION. FOUND AFT POSITION ROTARY LIFT ACTUATOR FRAME REINFORCEMENT FIT TING CRACKED. REPLACED FITTING 65B38174-3 PER STANDARD PRACTICES IAW SRM 51-30-02 AND LIFT ACTUATOR 60B00305-1 PER AMM 52-34-03. OPS CHECK NORMAL. 2 L 7 4 4F RT A20WE 2008022800012 20080228 00012 NM 2008 2 28 F3LA200800070 1 20080217 A 5320 D53477154004 THRESHOLD AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE CARGO DOORWAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 903FR 5893 1560 DURING C5 C CHECK, INSPECTION REPORTED LEVEL 1 CORROSION OF AFT CARGO PIT DOOR THRESHOLD AT EIGHTEEN (18) LOCATIONS AROU ND ATTACHMENT HOLES AND ADJACENT TO THRESHOLD ITSELF. MAINTENANCE REMOVED CORROSION IN ACCORDANCE WITH REQUIREMENTS OF A319 SRM 51-74-00, PARAGRAPH 6 AND EA A9-53R-30055. HFEC (EDDY CURRENT) INSPECTION WAS PERFORMED. NO DEFECTS FOUND. R EPAIRED AREAS TREATED, PRIMED AND PAINTED IN ACCORDANCE WITH EA REQUIREMENTS. THIS WAS A MAJOR REPAIR. FOLLOWING COMPL ETION OF REPAIRS, THRESHOLD WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008022800043 20080228 00043 NM 2008 2 28 HALA0800276 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 412 S37-38R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 412 BETWEEN LONGERONS S-37R AND S-38R, MARKED NR 22, AREA INSPECTED. FASTENER DAMAG E W/I LIMITS AS PER SRM 53-00-01/101. FASTENER CLEANED/PRIMED/PAINTED. FASTENER TO BE REPAIRED PER SRM 53-00-01. REPA IR NR E AT OR BEFORE 50 FLT CYCLES. 2 L 7 2 4F RT A1NM 2008022800046 20080228 00046 NM 2008 2 28 HALA0800287 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 171 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 171 AT 6 O'CLOCK POSITION, MARKED NR 10, AREA INSPECTED. FASTENER DAMAGE W/I LIMITS AS PER SRM 53-00-01/101. FASTENER CLEANED/PRIMED/PAINTED. FASTENER REQ'D TO BE REPAIRED AS PER SRM 53-00-01. REPAIR 8 AT OR BEFORE 50 FLT CYCLES. 2 L 7 2 4F RT A1NM 2008022800056 20080228 00056 NM 2008 2 28 HALA0800337 1 20080219 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION, ON RADOME RT HINGE CUT OUT AREA (2 EA). REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800059 20080228 00059 EU 2008 2 28 08FDEA00605 1 20080226 A 5754 A53710007206 DOUBLER AIRBUS 300 A300B4622R 3930312 EU K FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND KRUEGER FLAP DOUBLER AT C 38, 28-33 LT WITH CORROSION. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008022800063 20080228 00063 NM 2008 2 28 HALA0800297 1 20080217 A 5410 PANEL BOEING 717 717200 1383700 NM NACELLE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 NUMEROUS BOLT HEADS CORRODED ON LT ENGINE, ON TRAPEZOIDAL PANEL ABOVE AND I/B SIDE OF FWD MOVEABLE VANE. REPAIR IN WORK . 2 L 7 2 4F TR A6WE 2008022800073 20080228 00073 NM 2008 2 28 KCSA081090 1 20080220 A 5320 INTERCOSTAL BOEING 747 747209B 138489B NM FUSELAGE PUNCTURED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 INTERCOSTAL PUNCTURED AT STR-30L BETWEEN BS 1700 AND 1720. 2 L 7 4 4F RT A20WE 2008022800096 20080228 00096 NM 2008 2 28 SWAA080919 1 20080219 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800119 20080228 00119 SO 2008 2 28 CHQA200800038 1 20080222 A 7500 7276045 FILTER ELEMENT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 BLEED CLOGGED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 846RP 145600 CAE312242 CMH TO DCA - AT APPROXIMATELY 1,200 FT THE CREW RECEIVED A BLEED 1 OVERTEMP MESSAGE. THE QRH WAS FOLLOWED AND THE NUMBE R 1 BLEED WAS CLOSED, BUT DUE TO THE AIRCRAFT BEING IN ICING CONDITIONS, IT WAS DECIDED THAT THE AIRCRAFT WOULD RETURN T O FIELD AT CMH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE BLEED 1 SYSTEM AND FOUND THE FAN AIR VALVE FILTER CLOGGED, AND AFTER REPLACING THE FILTER, THE BLEED SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008022800130 20080228 00130 NM 2008 2 28 AALA200800278 1 20080209 A 2751 INDICATOR BOEING 757 757223 1384957 NM TE FLAPS TRIPPED A AALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SW 21 674AN 29424 JFK INFLIGHT T1876/09FEB MIA TO LGA - CREW REPORTED FLAP FAULT DURING DEPLOYMENT. TRAILING EDGE DISAGREE INDICATION. EXTENDED FLAPS WITH ALTERNATE SYSTEM. LANDED JFK WITHOUT INCIDENT. FOUND LEFT TRANSMISSION NUMBER ONE OVERLOAD INDICAT OR TRIPPED. RESET INDICATOR AND SERVICED TRANSMISSION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008022800184 20080228 00184 NM 2008 2 28 SWAA080961 1 20080220 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER 27L CORRODED AT BS 445. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008022800197 20080228 00197 NM 2008 2 28 DL76S080163 1 20080201 A 5330 143T35214 SKIN BOEING 767 767332 1382001 NM FS 522-544 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FOUND FUSELAGE SKIN BLENDS/STA 522-540 AND STR 27R-32R. 2 L 7 2 4F RT A1NM 2008022800204 20080228 00204 CE 2008 2 28 U5QA06009 1 20080219 A 3260 63710029 SQUAT SWITCH LEAR 60 60LEAR 5170707 CE MLG FROZEN E U5QA D RETURN TO BLOCK F FLT CONT AFFECTED CL CLIMB 1 CE 05 8783 006 AFTER TAKEOFF FROM GYY THE LANDING GEAR WOULD NOT RETRACT AND THE CREW RETURNED FOR LANDING WITHOUT INCIDENT TO GYY. 2 L 7 2 4F RT A10CE 2008022800222 20080228 00222 NM 2008 2 28 CALA0800167 1 20080204 A 5320 69489854 ATTACH FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 ATTACHMENT CLIP CRACKED IN RADIUS AT BS 360 STRING 10L. REMOVED AND REPLACED PER ECRA 5310-04719. 2 L 7 2 4F RT A16WE 2008022800226 20080228 00226 NM 2008 2 28 SWAA080971 1 20080221 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 266WN 32523 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 21 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008022800237 20080228 00237 NM 2008 2 28 SWAA080979 1 20080221 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 111. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008022800250 20080228 00250 NM 2008 2 28 KCSA081106 1 20080222 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 EXTERNAL FUSELAGE SKIN IS CORRODED AROUND FASTENER AT STA 940, STR 3R. 2 L 7 4 4F RT A20WE 2008022800258 20080228 00258 NM 2008 2 28 KCSA081114 1 20080223 A 5347 SUPPORT BRACKET BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 AFT BILGE, CARGO RESTRAINT STOP SUPPORT BRACKET IS CRACKED (1") AT STA 1480 LBL 25. 2 L 7 4 4F RT A20WE 2008022800271 20080228 00271 EA 2008 2 28 TRAX200800248 1 20080212 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDS A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 PASSENGER DOOR DIFFICULT TO CLOSE AND LATCH. 2 L 7 2 4F RT A21EA 2008022800274 20080228 00274 EA 2008 2 28 TRAX200800250 1 20080213 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SO 27 916EV 7757 FLAP FAIL AT ZERO IN FLIGHT AT FLT 320. EMERGENCY DECLARED. FLT 4432 CX. 2 L 7 2 4F RT A21EA 2008022800292 20080228 00292 NM 2008 2 28 DLM88080172 1 20080204 A 5753 99359426 SKIN DOUG MD88 MD88 3023688 NM TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 THE RT WING INBD MAIN FLAP LOWER REMOVEABLE TRAILING EDGE SKIN WAS SPLICED TO REMOVE NICKS. 2 L 7 2 4F RT A6WE 2008022800346 20080228 00346 NM 2008 2 28 SWAA081013 1 20080224 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 412WN 29818 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008022800349 20080228 00349 EU 2008 2 28 08FDEA00564 1 20080222 A 5522 SKIN AIRBUS 310 A310324 3930206 EU RT ELEVATOR DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 RT ELEVATOR UPPER SURFACE IS DELAMINATED APPROX 8 INCHES FROM TE TO TE FROM NR 1 HINGE ARM TO NR 6 HINGE ARM APPROX 8 FT . UPON FURTHER INSPECTION; THE ELEVATOR WAS FOUND TO BE SERVICEABLE. THE AREA NOTED IN THE DISCREPANCY IS NOT DELAMI NATED. 2 L 7 2 4F RT A35EU 2008022800350 20080228 00350 EU 2008 2 28 08FDEA00565 1 20080222 A 5551 LUG AIRBUS 310 A310324 3930206 EU HORIZONTAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 RT HORIZIONTAL STAB NR 6 ELEVATOR HINGE ARM LUG AT THE ELEVATOR IS CORRODED UPPER INBD. REMOVED AND REPLACED IAW AMM 55 -16-45-1. FUNCTIONAL TEST GOOD IAW AMM 27-31-11. 2 L 7 2 4F RT A35EU 2008022800351 20080228 00351 EU 2008 2 28 08FDEA00566 1 20080222 A 2612 NSA932834C03BZ RELAY AIRBUS 310 A310324 3930206 EU FIRE DETECTION INOPERATIVE A FDEA K NONE L NO TEST IN INSP/MAINT 1 SO 25 803FD 378 DISCHARGE AGENT 2 LIGHT FOR THE CARGO FIRE BOTTLES FAILS TEST. DISCHARGE AGENT 2 LIGHT DID NOT ILLUMINATE UNTIL 75 MINU TES. REMOVED AND REPLACED RELAY 14WM REF ESPM 20-46-50. DISCHARGE AGENT 2 REMINDER LIGHT OPS CHECK GOOD REF AMM 26-2 3-00-5. 2 L 7 2 4F RT A35EU 2008022800354 20080228 00354 EU 2008 2 28 08FDEA00567 1 20080222 A 5753 A57965044200 FLAP TRACK AIRBUS 310 A310324 3930206 EU CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 PARTS RACK, FLAP TRACK FAIRING 632 CB, AFT WEB IS CRACKED. REMOVED AND REINSTALLED WEB ASSEMBLY AND REPLACED WEB IAW A3 10-300 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008022800359 20080228 00359 EA 2008 2 28 CHQA200800034 1 20080219 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS OUT OF RIG A CHQA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 GL 11 469SM 7650 GEE873397 IAH TO SDF - WHILE ON APPROACH TO SDF, THE FLAPS WERE SELECTED TO 8 THE CREW RECEIVED A FLAP FAIL MESSAGE AND THE FLAPS WERE FAILED AT ZERO DEGREES. THE FLIGHT LANDED WITHOUT INCIDENT IN SDF. MAINTENANCE TROUBLESHOT THE FLAP SYSTEM AND FO UND THE LEFT AND INBOARD FLAP FAILED THE BACKLASH TEST AND WAS OUT OF RIG. AFTER RE-RIGGING THE FLAP SYSTEM IT OPERATED NORMALLY AND WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008022800360 20080228 00360 SO 2008 2 28 CHQA200800035 1 20080220 A 2133 2099L021100 OUTFLOW VALVE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN PRESSURE MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 283SK 145424 CAE312071 CLE TO ATL - DURING CLIMB, THE FLIGHT ATTENDANT REPORTED THAT THERE WAS AN UNUSUALLY LOUD NOISE COMING FROM THE CABIN SE RVICE DOOR. THE FLIGHT CREW VERIFIED THAT THE DOOR WAS CLOSED ON THE MFD AND MONITORED THE CABIN PRESSURIZATION. THE A IRCRAFT LEVELED OFF AT FL200 WHEN IT WAS NOTICED THAT THE PRESSURIZATION INDICATIONS WERE ERRATIC FOR BOTH THE CABIN ALT ITUDE AND DIFFERENTIAL PRESSURE. THE FLIGHT DIVERTED TO CMH, AND DURING DESCENT IT WAS NOTED THAT THE CABIN RATE WOULD NOT DESCEND UNTIL APPROXIMATELY 200 FEET ABOVE THE CABIN ALTITUDE OF 5,900 FEET. MAINTENANCE TROUBLESHOT THE PRESSURIZA TION SYSTEM AND FOUND ONE OF THE PRESSURIZATION OUTFLOW VALVES WAS SLOW TO RESPOND. AFTER REPLACING THE OUTFLOW VALVE A 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008022800375 20080228 00375 NM 2008 2 28 SWAA081030 1 20080224 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008022800382 20080228 00382 NM 2008 2 28 SWAA081037 1 20080224 A 5311 6546536 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800387 20080228 00387 NM 2008 2 28 SWAA081021 1 20080224 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800390 20080228 00390 NM 2008 2 28 SWAA081018 1 20080224 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800397 20080228 00397 NM 2008 2 28 SWAA081028 1 20080224 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 765SW 29805 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 35 TO RBL 45. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800399 20080228 00399 NM 2008 2 28 ASAA0842651 1 20080118 A 5310 654580761 DOOR FRAME BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD GALLEY SERVICE DOORWAY FWD STUB FRAME CRACKED AT BOTTOM FASTENER HOLE ATTACHING TO LOWER SILL CHORD. ONE CRACK FOUN D AFTER SILL CHORD WAS REMOVED, REPAIRED WITH MADE REPAIR PART. 2 L 7 2 4F RT A16WE 2008022900001 20080229 00001 NM 2008 2 29 DLM88080265 1 20080213 A 5330 593600419 SKIN DOUG MD88 MD88 3023688 NM BS 628 S29-30R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 FUSELAGE SKIN REPAIR AT STA=628 BETWEEN LONGERONS 30 AND 29 RT. A REPAIR WAS PERFORMED IAW ER/A 457183-14 REV D. 2 L 7 2 4F RT A6WE 2008022900002 20080229 00002 EA 2008 2 29 TRAX200800254 1 20080213 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA OVERWING EXIT CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 889AS 7538 MILD CORROSION BOTTOM RT OVERWING EXIT. THOROUGHLY CLEAND AND RE-INSPECTED OVER WING EXIT SURROUND STRUCTURE. SUSPECTE D CORROSION WAS DETERMINED TO BE EXCESSIVE DIRT AND DEBRIS IN THE EXISTING CORROSION INHIBITING COMPOUND. NO FURTHER EVI DENCE OF CORROSION WAS FOUND. APPLIED NEW CORROSION PREVENTATIVE COMPOUND.ALL WORK DONE IAW SRM 51-21-00 AND 51-21-11. 2 L 7 2 4F RT A21EA 2008022800293 20080228 00293 GL 2008 2 28 DL764080175 2 20080206 A 7200 LINER BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 2 ENGINE FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831MH 22002 29702 706431 REPLACE RT ENG DUE TO FAILED BORO 50131. COMP INNER LINER AXIAL CRACKS. ON 25 CYCLE FLYBACK, REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E23EA 2008022800300 20080228 00300 EU 2008 2 28 Y2LA200800010 1 20080215 A 2120 UNKNOWN AIRBUS A319 A319112 3930323 EU CABIN SMOKE A Y2LA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 07 553SX 3171 SMOKE OBSERVED IN THE CABIN OVERHEAD UPON LANDING. PHYSICAL INSPECTION PERFORMED, SMOKE TESTS CONDUCTED, NO TROUBLE FOU ND. UNABLE TO DUPLICATE AT GATE. NO C/B POPPED AND NO POST FLIGHT REPORT FAULTS. AIRCRAFT DEPARTED AFTER INSPECTION A ND TEST. 2 L 7 2 4F RT A28NM 2008022800301 20080228 00301 EU 2008 2 28 Y2LA200800012 1 20080223 A 5330 SKIN AIRBUS A319 A319112 3930323 EU FUSELAGE DAMAGED A Y2LA K NONE O OTHER TX TAXI/GRND HDL 1 GL 07 552SX 1884 AIRCRAFT STRUCK BY JETWAY, DAMAGING AIRCRAFT. DAMAGE FORWARD OF L1 DOOR. PERFORMED INSPECTION OF AIRCRAFT AND ENGINES AS REQUIRED BY PARAGRAPH C OF THE SFP AUTHORIZATION FORM AND DETERMINED THAT THE AIRCRAFT IS SAFE FOR FLIGHT FROM CMH TO BFM, AND THE FLIGHT CREW HAS BEEN BRIEFED REGARDING ANY LIMITATIONS IMPOSED BY THE AUTHORIZATION, ORIGINAL DISCREPANCY HAS BEEN TRANSFERRED TO LOG PAGE 00006303 ITEM 1. REPAIRED IN ACCORDANCE WITH EA 19-53-0050RO0OT REPAIR ON FUSELAGE SKI N DENTS BETWEEN LT FRAME 11 TO FRAME 13. PERFORMED PERMANENT REPAIR SCHEME BEFORE 8731FC IE. 3000FC LIFE LIMITATION. 2 L 7 2 4F RT A28NM 2008022800305 20080228 00305 NM 2008 2 28 SWAA080997 1 20080222 A 5754 65C26601 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT LOWER OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008022800310 20080228 00310 NM 2008 2 28 SWAA080996 1 20080222 A 5230 6547953 SKIN BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT AFT UPPER CORNER. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800311 20080228 00311 NM 2008 2 28 SWAA080995 1 20080222 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800315 20080228 00315 NM 2008 2 28 HALA0800277 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 418 S37R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE STA 418 LONG 37R. FASTENER TO BE REPAIRED PER SRM 53-00-01ANT. REPAIR A AND REPAIR NR 8 A T OR BEFORE 50 FLT CYCLES. 2 L 7 2 4F RT A1NM 2008022800317 20080228 00317 NM 2008 2 28 SWAA081004 1 20080224 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008022800326 20080228 00326 NE 2008 2 28 DL76G080218 2 20080216 A 7200 CF680C2B6 ENGINE BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE NR 1 FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 156DL 62665 25354 695476 ENGINE FAILED BORO-ENGINE REPLACED. 2 L 7 2 4F 4 F RT A1NM E13NE 2008022800330 20080228 00330 WP 2008 2 28 08FDEA00553 1 20080221 A 5321 AEA0183503 FLOOR PANEL DOUG DC10 DC1030F 3023504 WP ZONE 200 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MAIN CABIN FLOORBOARD AT APPROX LBL-90, BETWEEN STA 1481 TO 1561 IS DELAMINATED. MAT ID A402H35039-003 PO 5990899.1. P OTTING COMPOUND 1619 A/B PO 606417.3, INSERT SLS 5094A3-400-2 PO 595225, INSERT SLP 5094A3-2 PO 595242. ADHESIVE EPIBON D 420 A/B PO 594846.4. LOCATED HOLES, POTTED EDGES AND INSERTS. INSTALLED ANTI-SKID IAW FEDEX DWG SRZ 25-005 REV F, MI NOR REPAIR. 2 L 7 3 4F RT A22WE 2008022900208 20080229 00208 NM 2008 2 29 08FDEA00524 1 20080220 A 5511 65206611 RIB BOEING 727 727233 138408A NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 LT HORIZONTAL STABILIZER MAIN BOX INTERIOR RIB CRACKED AT LIGHTENING HOLE STAB STA 188. CUT OUT DAMAGED AREA IAW SRM 5 5-10-5 FIG2 NAD 55-10-4 FIG2. FABRICATED REPAIR FOR FWD SPAR WEB IAW SRM 55-10-5 FIG 2 PARTS AND AFFECTED AREAS TREATE D AND PRIMED IAW SRM 51-10-2 FIG 1. INSTALLED REPAIR PARTS AT RIB STA 188 IAW SRM 55-10-4 FIG2. FWD SPAR WEB AND REPAIR INSTALLED IAW SRM 55-10-5 FIG 2. 2 L 7 3 4F RT A3WE 2008022800335 20080228 00335 NM 2008 2 28 SWAA081006 1 20080223 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800345 20080228 00345 EU 2008 2 28 08FDEA00561 1 20080222 A 5330 A53610317207 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND DENT ON SKIN C 15A-16, P 33 LT. REPAIR PERFORMED BY DRESS OUT THE DENT AND NDT FOR CRACK FREE CONDITION IAW RAS 7 0502446/009/2008 ISS A, APPROVED BY EA 6-5312-114873. 2 L 7 2 4F RT A35EU 2008022800347 20080228 00347 NM 2008 2 28 SWAA081014 1 20080224 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 412WN 29818 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008022800348 20080228 00348 EU 2008 2 28 08FDEA00563 1 20080222 A 5740 A57710115200 FITTING AIRBUS 310 A310322 3930334 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 LT WING, THREE CRACKS AT CENTRAL FITTING ATTACHMENT TO ACTUATOR AT NUMBER 4 LT SPOILER REPLACED FITTING IN ACCORDANCE WI TH EA 6-5750-115315, SB A310-57-2057, IPC 57-73-11-01 AND SRM 57-73-11. 2 L 7 2 4F RT A35EU 2008022900003 20080229 00003 EA 2008 2 29 TRAX200800255 1 20080213 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 889AS 7538 AFT CARGO SUPPORT BEAM ATTACH FITTING IS CRACKED. REMOVED AND REPLACED CARGO LINTEL AFT BOTTOM ATTACH FITTING IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 2008022900004 20080229 00004 EA 2008 2 29 TRAX200800256 1 20080214 A 2120 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 884AS 7513 CARGO SOV FAIL STATUS. CARGO CONDITION AIR SOV, DEFERRED CLOSED. REMOVED AND REPLACED CARGO RECIRCULATED AIR SOV IAW A MM 21-55-07 OPS CHECK GOOD AT THIS TIME. DEFER CLEARED, PLACARD REMOVED. 2 L 7 2 4F RT A21EA 2008022900007 20080229 00007 EA 2008 2 29 TRAX200800103 1 20080117 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 844AS 7317 AAR - 1016 - I/B CLIP AT FS 280 RBL 9 CRACKED. REMOVED CRACKED RBL 9 I/B CLIP AT FS 280. REF FORM 412 FOR FABRICATION OF SERVICEABLE CLIP FOR RBL 9 I/B AT FS 280. REF REO 601R-53-11-171 FOR MATERIAL TYPE. INSTALLED SERVICEABLE CLIP IAW CRJ 200 SRM 51-42-21. SUPPLEMENTAL SDR CLOSED 2/13/08. 2 L 7 2 4F RT A21EA 2008022900009 20080229 00009 EA 2008 2 29 TRAX200800262 1 20080215 A 3350 COVER CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 EMERGENCY LIGHTING COVER MISSING, LAST 20 INCHES LEFT FWD CABIN. EMERGENCY FLOOR LIGHT COVER. 2 L 7 2 4F RT A21EA 2008022900010 20080229 00010 EA 2008 2 29 TRAX200800263 1 20080204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 RT FWD INBOARD FLOOR TRACK AND LAV HOLD DOWN FITTINGS CORRODED. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINA TION OF AN APPROPRIATE CORRECTIVE ACTION. 2 L 7 2 4F RT A21EA 2008022900012 20080229 00012 EU 2008 2 29 TRAX200800265 1 20080214 A 5313 STRINGER AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 CORROSION FOUND ON STR 21L, AT FR 44. 2 H 7 2 4T RT 2008022900019 20080229 00019 EA 2008 2 29 TRAX200800272 1 20080214 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 889AS 7538 LEFT SIDE FRAME 384 LBL 27 INBOARD CLIP CRACKED. 2 L 7 2 4F RT A21EA 2008022700343 20080227 00343 NM 2008 2 27 SWAA080864 1 20080217 A 5311 65C34355 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700352 20080227 00352 NM 2008 2 27 SWAA080913 1 20080218 A 2560 100031 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED SPV CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2008022800006 20080228 00006 NM 2008 2 28 HALA0800282 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 676 S36R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 676 AT LONGERON S-36R, MARKED NR 35, AREA INSPECTED. FASTENER DAMAGE W/I LIMITS AS PER SRM 53-00-01/101. FASTENER CLEANED/PRIMED/PAINTED. FASTENER REQ'D TO BE REPAIRED AS PER SRM 53-00-01 REPAIR 8 AT O R BEFORE 50 FLT CYCLES. 2 L 7 2 4F RT A1NM 2008022800007 20080228 00007 NM 2008 2 28 HALA0800273 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 332 S39R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 332 AT LONGERON S-39R, MARKED NR 15. REPAIRED PER SRM 53-00-01-ZR-8 CAT C REPAIR (T EMP). REPETITIVE INSPECTIONS EVERY 1500 CYCLES. PERMANENT REPAIR AT 6000 CYCLES. 2 L 7 2 4F RT A1NM 2008022800008 20080228 00008 EU 2008 2 28 08FDEA00612 1 20080226 A 5311 A53611513 FAILSAFE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION FOUND ON LT FWD DOOR FAIL/SAFE RING, LOWER AFT CORNER. REPAIR PERFORMED BY BLEND OUT THE CORROSION, NDT FOR C RACK FREE CONDITION IAW. RAS 70503237/006/2008 ISS A, APPROVED BY EA 6-5312-114886. 2 L 7 2 4F RT A35EU 2008022800011 20080228 00011 NM 2008 2 28 HALA0800330 1 20080218 A 5510 STRUCTURE BOEING 717 717200 1383700 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION, NUMEROUS FASTENERS ON OTBD END OF LT HORIZ STAB INNER BOX AREA. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800015 20080228 00015 NM 2008 2 28 HALA0800299 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 139 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 139.0 AT 6 O'CLOCK POSITION, MARKED NR 8. CLEANED, TREATED AND PRIMED PER SRM 53-00 -01. AREA PAINTED AS PER 51-22-01. 2 L 7 2 4F RT A1NM 2008022800020 20080228 00020 NM 2008 2 28 HALA0800291 1 20080217 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 2 CRACKS ON RIGHT MLG DOOR CUTOUT JUST ABOVE DOOR SENSOR. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800024 20080228 00024 NM 2008 2 28 HALA0800283 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 1605 S38-39R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 1605.5 BETWEEN LONGERONS S-38R AND S-39R, MARKED NR 41, AREA INSPECTED. FASTENER DA MAGE W/I LIMITS AS PER SRM 53-00-01/101. FASTENER CLEANED/PRIMED/PAINTED. FASTENER REQ'D TO BE REPAIRED AS PER SRM 53- 00-01 REPAIR 8 AT OR BEFORE 50 FLT CYCLES. 2 L 7 2 4F RT A1NM 2008022800038 20080228 00038 NM 2008 2 28 F3LA200800075 1 20080223 A 5321 D5367520800600 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 949FR 5553 10 2857 DURING C1 C CHECK, INSPECTION REPORTED AFT CARGO PIT FLOOR PANEL 151VG WAS DAMAGED BEYOND REPARABLE LIMITS. MAINTENANCE REMOVED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-42-14-000-001 AND REPLACED IT WITH A NEW FLOOR PA NEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPH 5. FOLLOWING THE REPLACEMENT OF THE FLOOR PANEL IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008022800044 20080228 00044 NM 2008 2 28 HALA0800298 1 20080220 A 5280 STRUCTURE BOEING 767 76733A 1385209 NM NLG DOOR DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON RT FWD NOSE GEAR DOOR GAP SEAL FASTENERS, 17 EACH SCREW HEADS. CLEANED, TREATED AND PRIMED PER SRM 53-00-01 PAINT PEND. AREA PAINTED AS PER 51-22-01. 2 L 7 2 4F RT A1NM 2008022800053 20080228 00053 NM 2008 2 28 HALA0800320 1 20080218 A 5510 STRUCTURE BOEING 717 717200 1383700 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION, RT HORIZ STAB 1 RUSTED NUT O/B AFT SIDE OF HORIZ INTERNAL STRUCTURE AT STA XHS 221. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800145 20080228 00145 EA 2008 2 28 COMA0860141 1 20080220 A 2421 755469C IDG CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 932CA 11294 7038 FLIGHT 5279 - RECEIVED IDG NR 2 CAUTION MESSAGE. ABORTED APPROACH, PERFORMED QRH, LANDED WITHOUT INCIDENT. REPLACED NR 2 IDG. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008022800146 20080228 00146 NM 2008 2 28 CALA0800160 1 20080220 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 69063 29458 EMERGENCY LIGHT BATTERY FAILED TEST. REMOVED AND REPLACED BATTERY CHARGER PER AMM 33-51-07. 2 L 7 2 4F RT A1NM 2008022800147 20080228 00147 NM 2008 2 28 CALA0800161 1 20080220 A 2750 65522111 TORQUE TUBE BOEING 737 737524 1384721 NM T/E FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 RIGHT INBOARD MID FLAP BOTH I/B AND O/B TORQUE TUBES CORRODED. REMOVED AND REPLACED BOTH TORQUE TUBES PER CMM 57-53-17. 2 L 7 2 4F RT A16WE 2008022800173 20080228 00173 NM 2008 2 28 AALA200800294 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 39G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 39G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022800179 20080228 00179 NM 2008 2 28 SWAA080956 1 20080220 A 3350 MS155721 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 269WN 32526 DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008022800195 20080228 00195 NM 2008 2 28 SWAA080959 1 20080220 A 2560 65476827 DOOR BOEING 737 7373H4 1384600 NM COCKPIT LACK OF LUBE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED HC1 CHECK, CAPTAIN'S EMERGENCY EXIT ROPE DOOR WILL NOT OPEN. LUBRICATED DOOR PER MM. 2 L 7 2 4F RT A16WE 2008022800239 20080228 00239 NM 2008 2 28 SWAA080983 1 20080221 A 5523 REP4HE8 BEARING BOEING 737 7375H4 138449D NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, RIGHT ELEVATOR TAB NR 1 HINGE FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BEARI NG AND BOLT PER MM. 2 L 7 2 4F RT A16WE 2008022800324 20080228 00324 NM 2008 2 28 P5CA0801543 1 20080212 A 2400 BACC18AF60 RCCB BOEING 747 74746NF 13848BT NM MULTIPLE FAIL A P5CA L A ABORTED APPROACH UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 EA 15 454PA 30812 AIR TURN BACK DUE TO MULTIPLE ELECTRICAL FAILURES. NR 1 COMMUNICATION PANEL, E/E COOLING CARD, T/E FLAPS/FLAPS PRIMARY, ELEC BCU 1, ALL FUEL CROSSFEED MSG'S, CREW O2 LOW, YAW DAMPER LOWER, FUEL TANK TO ENGINE, TORQUE LIMITER, FUEL PUMP 2 S TATUS MESSAGES APPEARED. FWD FUEL PUMP 2 FAILED AND RESET. REPLACED RELAY NR R7224 IAW MM 24-33-01 AND RCCB NR C2243 I AW MM 24-33-01 AND 24-60-01. FUNCTIONAL CHECKS SATISFACTORY. REMOVED AND REPLACED BATTERY TFR RELAY AND RCCB, PN 9131- 8506 AND BACC18AF60; SN 12151 AND 50150. 2 L 7 4 4F RT A20WE 2008022800325 20080228 00325 NM 2008 2 28 DL76G080217 1 20080217 A 3150 221701528 CIRCUIT CARD BOEING 767 767332 1382001 NM E&E MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 171DZ 29690 T/O CONFIG MSG AFTER T/O WITH FLAPS RED WHEN THROTTLES ADVANCED. WITH THROTTLES RETARDED AND FLAPS 5, MSG OUT. TRIED S EVERAL DIFFERENT C/B RESETS, NO HELP. ATB TO FRA. REPLACED M620 CARD PER MM31-51-04. 2 L 7 2 4F RT A1NM 2008022800328 20080228 00328 WP 2008 2 28 08FDEA00546 1 20080221 A 3230 LANDING GEAR DOUG MD10 MD1010F 3022112 WP MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 373FE 46611 LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. WITH HANDLE UP, THE 3 RED GEAR LIGHTS WERE ILLUMINATED ALONG WITH SECONDARY RED LIGHTS ON CONFIG PAGE. FOLLOWED QRH PROCEDURES AND RECYCLED GEAR. ALL CAME UP NORMALLY AND LIGHT WENT OUT. INSPE CTED GEAR AREA FOR OBVIOUS DAMAGE OR INTERFERENCE. NO DEFECTS NOTED. PERFORMED RTS AND FAULT REVIEW ON PSEU. NO FAULT S LOGGED. ALSO CHECKED PSEU FOR MARGINAL RIGGING ON ANY GEAR SENSORS. NO MARGINAL RIGGING FOUND FOR ANY GEAR SENSORS F OR ANY PREVIOUS FLIGHTS. ALL GEAR SENSORS CHECK NORMAL FOR NEAR/FAR STATUS AT THIS TIME. SUSPECT BOGIE WAS NOT CENTERE D WHEN HANDLE WAS SELECTED UP. AIRCRAFT OK FOR SERVICE, REF M/M 31-71-01-2. 2 L 7 3 4F RT A22WE 2008022800344 20080228 00344 NM 2008 2 28 SWAA081012 1 20080224 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 404WN 27892 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2008022800364 20080228 00364 SW 2008 2 28 WGEA200800034 1 20080225 A 2731 271125681004 MOTOR ECLIPS EA500 ECLIPSEEA500 3350000 SW ELEVATOR TRIM FAILED E WGEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 146DJ 129 000058 ELEVATOR TRIM TAB SPLIT, UNABLE TO TRIM OFF PRESSURE DURING NORMAL FLIGHT THROUGH HAT SWITCH AND FLCS PAGE. SUPPLEMENTA L INFORMATION, VERIFIED DISCREPANCY AND TROUBLESHOT A BAD LT ELEVATOR TRIM ACTUATOR. REMOVED AND REPLACED LT ELEVATOR T RIM ACTUATOR. ALL OP'S CHECKS SATISFACTORY IAW EA 500 AMM 27-33-15. 1 L 7 2 4J RT A00002AC 2008022800365 20080228 00365 NE 2008 2 28 0126200801 2 20080126 A 7200 ENGINE BOEING 747 747236B 1384804 NM RROYCE RB211 RB211524D419 54555 NE NR 3 MALFUNCTIONED A OZYA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 29 362FC 22442 12604 ON TAKEOFF ROLL, NR 3 ENGINE N2 WENT TO 114 PERCENT FOR LESS THAN 2 SECONDS, EPR WAS 1.4, ALL OTHER ENGINE GAGES NORMAL, AIRSPEED WAS 70 KTS. ABORTED TO, RETURNED TO RAMP. 2 L 7 4 4F 4 F RT A20WE E12EU 2008022800367 20080228 00367 SO 2008 2 28 SWIA200819257 1 20080218 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCHARGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 582SW 12029 12029 120350 FLT 5544 - EMERGENCY LIGHTS ARE INOP. REPLACED BATTERY PACK. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2008022800385 20080228 00385 NM 2008 2 28 SWAA081019 1 20080224 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800395 20080228 00395 NM 2008 2 28 GTIA0800011 1 20080201 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 501NK 2424 FLOORBEAM AT Y765 BETWEEN FRAME 66 AND 70 SHOWS SIGNS OF CORROSION. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2008022900021 20080229 00021 EA 2008 2 29 TRAX200800274 1 20080217 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 933EV 8022 FLAPS FAIL CAUTION MSG ON APPROACH. FLAPS FAILED AT ZERO WHEN SELECTING EIGHT DEGREES. FLT 4503 DEL 390 MINS. 2 L 7 2 4F RT A21EA 2008022900036 20080229 00036 NM 2008 2 29 KCSA081118 1 20080226 A 5414 SKIN BOEING 747 747209B 138489B NM NR 4 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 NR 4 PYLON OUTBOARD SIDE EXTERNAL SKIN IS CHAFED AT FIREWALL AREA FROM NAC STA 180 TO 220. 2 L 7 4 4F RT A20WE 2008022900040 20080229 00040 NM 2008 2 29 DLM88080264 1 20080213 A 5542 SKIN DOUG MD88 MD88 3023688 NM RUDDER DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 DURING HMV, TWO METALIZED DAMAGES WERE FOUND BOTH RUDDER SURFACES AT THE LT SIDE IT WAS 87 INCHES LONG BY 34 INCHES WIDT H AT THE RT SIDE IT WAS 71 INCHES LONG AND 30 INCHES WIDTH. A PERMANENT REPAIR WAS PERFORMED IAW MD-80 SRM 51-70-1A D P ARAGRAPH 23A. 2 L 7 2 4F RT A6WE 2008022900044 20080229 00044 NM 2008 2 29 KCSA081120 1 20080227 A 5340 FITTING BOEING 747 747209B 138489B NM RT MLG WW CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 RIGHT BODY GEAR WHEEL WELL HAS A CRACKED (10") FITTING AT STA 1356 TO 1364, RBL 129, WL 130. 2 L 7 4 4F RT A20WE 2008022900052 20080229 00052 NM 2008 2 29 DLM88080275 1 20080213 A 5330 593643443 DOUBLER DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 DURING HMV, A .45 INCH LONG CRACK WAS FOUND ON INTERNAL DOUBLER P/N 5936434-43 AT STA Y=579 BETWEEN LONGERONS 28 AND 29 LT A REPAIR WAS PERFORMED IAW ER/A 465656-14. 2 L 7 2 4F RT A6WE 2008022900058 20080229 00058 NM 2008 2 29 DLM90080248 1 20080220 A 5330 5924802133 SKIN DOUG MD90 MD9030 3023690 NM BS 237 L17-18L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 909DA 53389 FUSELAGE SKIN AND FORMER DENTED AT STA 237 BETWEEN L17L AND L18L DAMAGE CUTOUT. AREA INSPECTED, FORMER REPLACED AND SKI N REPLACED. 2 L 7 2 4F RT A6WE 2008022900060 20080229 00060 NM 2008 2 29 DLM90080256 1 20080222 A 5510 59404851 STRUCTURE DOUG MD90 MD9030 3023690 NM HORIZONTAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 DURING CURRENT HMV, CORROSION WAS FOUND IN THE HORIZONTAL STABILILZER CENTER SECTION HINGE BORES, BOTH LT AND RT. SUBJE CT CORROSION WAS REMOVED BY SPOTFACING AND OVERSIZING THE BORES BEYOND THE SRM ALLOWABLE LIMITS. AS SUCH, BOEING WAS CO NTACTED FOR APPROVAL OF REPAIR, AND IS DOCUMENTED IN ER/A 466670-14. 2 L 7 2 4F RT A6WE 2008022900061 20080229 00061 NM 2008 2 29 DL757080258 1 20080221 A 5330 146N35112 SKIN BOEING 757 757232 1384965 NM BS 1420 S28R DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 DURING HMV AT SAA, A CREASE WAS FOUND IN THE FUSELAGE SKIN AT STA 1420, S-28R. THE CREASE EXCEEDED THE ALLOWABLE SRM LI MIT. A REPAIR WAS ACCOMPLISHED PER BOEING INSTRUCTIONS. STARTING AT 12,000 CYCLES AFTER REPAIR INSTALLATION AND EVERY 12,000 CYCLES THEREAFTER, THE PERIPHERAL ROW OF FASTENERS COMMON TO THE REPAIR MUST BE LFEC INSPECTED FOR CRACKS. 2 L 7 2 4F RT A2NM 2008022900063 20080229 00063 WP 2008 2 29 NWAA080669936 1 20080225 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1799U 47370 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE VENTRAL STAIRWAY WAS INOPERATIVE. MAINT ENANCE REPLACED THE POWER PACK AND OPERATIONALLY CHECKED THE SYSTEM. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2008022900064 20080229 00064 WP 2008 2 29 NWAA080659852 1 20080225 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 761NC 47709 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE VENTRAL STAIRWAY WAS INOPERATIVE. MAINT ENANCE REPLACED THE POWER PACK AND OPERATIONALLY CHECKED THE SYSTEM. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008022900066 20080229 00066 2008 2 29 TRAX200800289 4 20080220 A 2210 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 682BR 7691 IN FLIGHT RECEIVED STAB TRIM MACH TRIM AUTOPILOT TRIM AND AUTOPILOT NOSE UP CAUTION, A/P DISCONNECTED. DECLARED EMERGEN CY LANDED IN SDF. EN ROUTE TO ATL A/C DIVERTED TO SDF DUE TO MTC. FLT 4803 DE; 325 MINS. 2 L 7 2 4F RT A21EA 2008022900069 20080229 00069 NM 2008 2 29 08FDEA00628 1 20080227 A 5320 657517255 INTERCOSTAL BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 VERTICAL WEB AT FS 580 - 600, LBL 15 IS CORRODED REPLACED WEB AT STA 580 - 600, LBL 15 WITH NEW WEN REF SRM 51-30-2. TH IS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008022900070 20080229 00070 NM 2008 2 29 08FDEA00629 1 20080227 A 5320 65575671 FLOOR SUPPORT BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 AFT LWR CARGO BAY BS 1164 - 1166 FLOOR SUPPORT ANGLE AT LBL 11 HAS CORROSION ON UNDERSIDE. REMOVED DAMAGE AND FABED CHA NNEL AND SPLICE REPAIR AT STA 1144 TO 1166. APPLIED ALODINE, PRIMER AND PAINT. INSTALLED NEW CHANNEL AND SPLICE, REF S RM 51-10-06, 53-10-05, 51-10-02. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008022900073 20080229 00073 EA 2008 2 29 TRAX200800290 1 20080220 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 880AS 7606 CEILING EMERGENCY LIGHT 2ND FROM AFT INOP. 2 L 7 2 4F RT A21EA 2008022900075 20080229 00075 EA 2008 2 29 TRAX200800291 1 20080220 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 880AS 7606 LEFT EXTERNAL EMERGENCY LIGHT IN FRONT OF EMERGENCY EXIT INOP. 2 L 7 2 4F RT A21EA 2008022900076 20080229 00076 EU 2008 2 29 MALA080030 1 20080225 A 3350 PN330151 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS NO TEST A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 404XJ 340B404 EMERGENCY POWER SUPPLIES 23LN AND 24LN FAILED CAPACITY CHECK DURING COMPLETION OF TASK CARD 335003. REPLACED BOTH POWER SUPPLIES WITH SERVICEABLE UNITS PN 3301-51 SN ON 23 LN 2119 SN ON 24LN, OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 2008022900078 20080229 00078 EU 2008 2 29 NSVA2008008 1 20080227 A 3260 BULB SAAB SF340 340B 7860101 EU MLG INDICATOR INOPERATIVE A NSVA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 27 370PX 340B300 EMERGENCY DECLARED DUE TO LANDING GEAR UNSAFE INDICATION. CREW RAN ABNORMAL CHECKLIST AND LANDED WITHOUT INCIDENT. MX FOUND THE BULBS IN THE GEAR HANDLE TO BE INOP. REPLACED BULBS AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2008022900080 20080229 00080 GL 2008 2 29 3324 1 20080222 A 3150 7000006000 DISPLAY CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL COCKPIT MALFUNCTIONED E J4PA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 13 532SR 1009 2134 689792 FP5024B FLYING FROM CEU TO JZI, AT 7000 FT IN IMC AND MODERATE RAIN 40 MILES EAST OF JZI, FOUR RED X'S APPEARED ON THE PFD. BUR NING ELECTRICAL WIRE FUMES WERE ALSO DETECTED BUT REMAINED FAINT. PFD FAILURE AND SMOKE AND FUME CHECKLISTS WERE REVIEW ED. AN EMERGENCY WAS DECLARED AT 1745 WITH 2 HOURS AND 56 MINUTES OF FUEL ON BOARD AND REQUESTED DIRECT TO CAE NO PAX O NBOARD. RADAR VECTORS TO AN ILS 5 WITH AN UNEVENTFUL LANDING. EMERGENCY TERMINATED AT 1823. TERMINATION CONFIRMED WIT H VISIT FROM FIRE CAPTAIN. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2008022900087 20080229 00087 2008 2 29 18937 4 20080226 A 2312 127180518 VHF COMM CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL INOPERATIVE E J4PA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SO 13 1492C 1978 0567 687502 FP2265B FLYING FROM GMU TO PHF IN SERVER RAIN, THE PILOT DIVERTED TO GSO. THE PILOT REPORTED HEAVY STATIC ON THE RADIOS AND COU LD TRANSMIT BUT COULD NOT RECEIVE. LANDING WAS UNEVENTFUL. ONE PASSENGER ONBOARD. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2008022900089 20080229 00089 NM 2008 2 29 GTIA0800017 1 20080109 A 5320 FLOOR SUPPORT AIRBUS A321 A321231 3940032 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 FLOOR SUPPORT AT Y765 AT FRAME 67-69 HAS CORROSION. REPLACED FLOOR SUPPORT. 2 L 7 2 4F RT A28NM 2008022900091 20080229 00091 NM 2008 2 29 GTIA0800024 1 20080109 A 5220 LEVER AIRBUS A321 A321231 3940032 NM EMERGENCY EXIT BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 EMERGENCY EXIT DOOR R2 ESCAPE SLIDE RELEASE MECHANISM LEVER BROKEN IPC25-62-02 ITEM 50. REPLACED LEVER. 2 L 7 2 4F RT A28NM 2008022900094 20080229 00094 NM 2008 2 29 GTIA0800027 1 20080115 A 5315 FLOORBEAM AIRBUS A321 A321231 3940032 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 CORROSION ON FLOORBEAM AT Y-254 FRAME 20. FABRICATED AND INSTALLED PART IAW SRM 53-00-14. 2 L 7 2 4F RT A28NM 2008022900100 20080229 00100 EA 2008 2 29 QXEA200800208 1 20080218 A 2730 8221310104 DCU CNDAIR CL600 CL6002C10 1390015 EA NR 1 UNKNOWN A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 602QX 10032 10010 SEA - FLIGHT 2548 - ON CLIMB RECEIVED A ELEVATOR SPLIT CAUTION AND CAS MISCOMPARE MESSAGE. NO ABNORMAL INDICATIONS ON F LIGHT CONTROL PAGE. NO ABNORMAL FLIGHT CONDITIONS NOTED. MAINTENANCE PERFORMED A GVI OF THE ELEVATOR AND LINKAGE AND T ENSION CHECK OF THE CABLES WITH NO DEFECTS NOTED. AS A PRECAUTION REPLACED NR 1 DCU. OPERATIONAL CHECKS GOOD. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008022900101 20080229 00101 NM 2008 2 29 HALA0800314 1 20080218 A 5711 FRAME BOEING 717 717200 1383700 NM RT WING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 CRACK ON O/B SECTION OF FORMER NR 2 RIGHT WING BELOW CENTER SECTION, VIEWED FROM 2ND WITNESS HOLE. REPAIR IN WORK. REP AIR IN WORK. 2 L 7 2 4F TR A6WE 2008022900103 20080229 00103 NM 2008 2 29 DL76L080290 1 20080224 A 2997 WIRE BOEING 767 767332 1382001 NM PTU DISCONNECTED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 183DN 27110 ON TAXI OUT, EICAS CAUTION L HYD SYS PRESS ILLUMINATED. SELECTED DEMAND PUMP TO ON. LIGHT REMAINED ILLUMINATED. ON AR RIVAL LIGHT EXTINGUISHED. VERIFY LT PUMP WORKS BOTH IN AUTO AND IN ON. SUSPECT INTERMITTENT PRESS SWITCH. FWD TO MCO AND PLAC PER MEL 29-31-01A. ACTIVATED FLT CONTROLS PRESSURE CHKS OK. PTU SIGNAL WIRE HAS BEEN DISCONNECTED AND MUST BE RECONNECTED BEFORE MCO IS CLEARED. 2 L 7 2 4F RT A1NM 2008022900105 20080229 00105 NM 2008 2 29 QXEA200800209 1 20080218 A 3230 483023 SEQUENCE VALVE BOMBDR DHC8 DHC8402 1390042 NM MLG MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 411QX 4055 SEA - AFTER TAKEOFF, GEAR DOOR LIGHT FOR THE LEFT MAIN GEAR DOOR REMAINED ON. AFTER CHECKLIST, LIGHT STAYED ON. CONTIN UED TO DESTINATION. PERFORMED ALTERNATE EXTENSION AND ACCOMPLISHED A UNEVENTFUL LANDING. AIRCRAFT FERRIED TO PDX FOR R EPAIRS. REPLACED THE BUSHINGS AND LOC-LINK AND THE SOLENOID SEQUENCE VALVE. ALSO FLUSHED THE HYDRAULIC SYSTEM. EXTENSIO N AND RETRACTION OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008022900107 20080229 00107 NM 2008 2 29 DLM88080278 1 20080213 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE MISREPAIRED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 DURING HMV, AN INADEQUATE REPAIR WAS FOUND ON UPPER FUSELAGE SKIN BETWEEN STA Y=499 AND Y=507 LONGERON 6 AND 7 LT. A PE RMANENT REPAIR WAS PERFORMED IAW MD-80 SRM 53-04 FIG 12B. 2 L 7 2 4F RT A6WE 2008022900111 20080229 00111 EA 2008 2 29 QXEA200800222 1 20080219 A 3320 BR9500106 BALLAST CNDAIR CL600 CL6002C10 1390015 EA CABIN LIGHTS ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 614QX 10049 PDX - FLIGHT 2533, NOTICED A ELECTRICAL SMELL AROUND ROW 7 IN THE CABIN. MAINTENANCE FOUND THE BALLAST FOR THE OVERHEAD LIGHTS AT ROW 6 A/B VERY HOT. REPLACED BALLAST. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008022900112 20080229 00112 NM 2008 2 29 QXEA200800221 1 20080220 A 3231 ROD END BOMBDR DHC8 DHC8402 1390042 NM MLG DOORS OUT OF ADJUST A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 409QX 4051 LAX - ON TAKEOFF, MAIN GEAR DOOR AMBER LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CYCLED GEAR AND LIGHT WENT OUT . AIRCRAFT FERRIED TO PDX. REMOVED L/R MLG RETRACT ACTUATOR AND ADJUSTED THE ROD ENDS AND REINSTALLED ACTUATOR. OPERA TIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008022900114 20080229 00114 EA 2008 2 29 QXEA200800207 1 20080217 A 2730 3A2237B TRANSMITTER CNDAIR CL600 CL6002C10 1390015 EA ELEVATOR MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 602QX 10010 SEA - FLIGHT 2634, RECEIVED A ELEVATOR SPLIT CAUTION AND A "CAS MISCOMPARE" STATUS MESSAGE DURING CLIMB THROUGH 22,000. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE ELEVATOR POSITION TRANSMITTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008022900118 20080229 00118 NM 2008 2 29 HALA0800328 1 20080218 A 5280 DOOR BOEING 717 717200 1383700 NM MLG DOOR CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION ON INNER SURFACE OF RT MLG OUTBOARD DOOR. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022900120 20080229 00120 NM 2008 2 29 HALA0800310 1 20080218 A 5711 FRAME BOEING 717 717200 1383700 NM LT WING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 CRACK ON O/B SECTION OF NR 3 FORMER LT WING BELOW CENTER SECTION, VIEWED FROM 4TH WITNESS HOLE. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022900122 20080229 00122 NM 2008 2 29 GTIA0800010 1 20080201 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 501NK 2424 FLOORBEAM AT Y254 AT FRAME 70 SHOWS SIGNS OF CORROSION. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2008022900123 20080229 00123 EA 2008 2 29 TRAX200800298 1 20080222 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA ASD BINDS A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 686BR 7715 STATION REPORTS DIFFICULTY CLOSING ASD. 2 L 7 2 4F RT A21EA 2008022900126 20080229 00126 EA 2008 2 29 SWIA200819232 1 20080215 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA LACK OF LUBE A SWIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 07 958SW 7833 SERVICE DOOR HARD TO OPEN. CLEANED AND LUBED SERVICE DOOR SEAL. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2008022900127 20080229 00127 EA 2008 2 29 SWIA200819233 1 20080215 A 3250 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 907SW 7511 FLT 5983 - STEERING INOP CAUTION MESSAGE APPEARED AFTER TAKEOFF FOLLOWED BY A GEAR DISAGREE WARNING MESSAGE. REPLACED N LG PRIORITY VALVE ASSEMBLY REF CRJ 200 AMM 32-33-15 AND NLG SELECTOR VALVE IAW CRJ 200 AMM 32-33-10. OPS CHECK AND LEAK CHECK GOOD, PN 4622 SN/OFF 1609A PN 750006000, SN/OFF 0221T. 2 L 7 2 4F RT A21EA 2008022800136 20080228 00136 WP 2008 2 28 IXXA080006O 1 20080219 A 2612 FIRE LOOP DOUG DC8 DC871F 302199D WP NR 4 NACELLE LOOSE A IXXA O OTHER N FALSE WARNING CR CRUISE 1 SW 11 828BX 87323 839 45993 DURING CRUISE FROM KPHL TO KTOL, NUMBER FOUR ENGINE SHORT LIGHT CAME ON WITH NO FIRE TEST INDICATION, THE CREW ACCOMPLIS HED EMERGENCY PROCEDURES AND SHUT DOWN NUMBER FOUR ENGINE. THE CREW LANDED AT KTOL WITHOUT INCIDENT. MAINTENANCE INSPE CTED AND FOUND RIGHT FORWARD LOOP CONNECTOR LOOSE AND CORRODED. MAINTENANCE CLEANED AND RESECURED LOOP CONNECTOR OPERAT IONAL CHECK WAS GOOD IAW DC8 MAINTENANCE MANUAL 26-10-1. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2008022800141 20080228 00141 EA 2008 2 28 COMA0860137 1 20080216 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 811CA 7380 PAX DOOR INNER SKIN IS CRACKED AT DOOR DATUM 1 BETWEEN FS 338.90 AND 349.00. CUT OUT DAMAGE AND INSTALLED A REPAIR DOUB LER WITH SHIMS IAW EA 10-5210-02085. 2 L 7 2 4F RT A21EA 2008022800149 20080228 00149 NM 2008 2 28 HALA0800204 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 819 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS, AT RBL 54.75, MAX BLEND OUT WAS 0.004". BLENDED IAW SRM 51-10-02. ALL BLEND S WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022800151 20080228 00151 NM 2008 2 28 KCSA081095 1 20080221 A 5740 ATTACH ANGLE BOEING 747 747209B 138489B NM RT WING CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 RIGHT WING L/E RIB ATTACH ANGLE CRACKED AT FSSI 598. 2 L 7 4 4F RT A20WE 2008022800153 20080228 00153 NM 2008 2 28 KCSA081097 1 20080221 A 5740 ATTACH ANGLE BOEING 747 747209B 138489B NM RT WING CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 RIGHT WING L/E RIB ATTACH ANGLE CRACKED AT FSSI 512. 2 L 7 4 4F RT A20WE 2008022800162 20080228 00162 NM 2008 2 28 DLM88080207 1 20080214 A 2610 LINE DOUG MD88 MD88 3023688 NM GE CF6 CF680C2B6F 30025 NE HYD SYSTEM LEAKING A DALA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 907DE 53416 704749 DURING FLT AT FL370, SMELLED SMOKE IN ACFT CABIN AND COCKPIT. AFT LEFT SMOKE DETECTOR WENT OFF W/SIGNIFICANT HAZE IN CA BIN. RAN SMOKE FUMES CHECK LIST. LANDED IN KCHS. T/S PER M/M 05-50-01. RAN ENGINE AT HIGH POWER. PERFORMED DUCT BUR NOUT PER OP 5089 AND 5088. FOUND HYD SYSTEM OVERSERVICED AND OVERFLOW BOTTLES FULL. DRAINED LEFT AND RT HYD SYSTEM TO PROPER LEVEL EMPTIED OVERFLOW BOTTLES. FOUND HYD LEAK AT AUX PUMP RESEATED LINE, LK CKS GOOD. APU INLET CLEAN ENGINE I NTAKE CLEANED, NO SMELL OR SMOKE NOTED IN CABIN. 2 L 7 2 4F 4 F RT A6WE E13NE 2008022800175 20080228 00175 NM 2008 2 28 KCSA081101 1 20080221 A 5320 STRAP BOEING 747 747209B 138489B NM FUSELAGE BROKEN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 BULK PIT STABILIZATION STRAP BROKEN AT BS 1980, LBL 71. 2 L 7 4 4F RT A20WE 2008022800186 20080228 00186 2008 2 28 SWAA080957 4 20080220 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008022800193 20080228 00193 NM 2008 2 28 SWAA080958 1 20080220 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 415WN 29836 DURING SCHEDULED 6Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008022800205 20080228 00205 NM 2008 2 28 ASAA0842640 1 20080221 A 5210 507945178 PIN BOEING 737 737490 1384715 NM L1 DOOR MISSING A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 703AS 33428 33428 28893 COULD NOT OPEN FORWARD PAX ENTRY (L1) DOOR (PRESUMABLY FROM THE INSIDE). REPLACED MISSING DOOR GUIDE ARM RETAINING RING PIN. DOOR THEN FUNCTIONED OK. 2 L 7 2 4F RT A16WE 2008022800229 20080228 00229 NM 2008 2 28 SWAA080974 1 20080221 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008022800231 20080228 00231 NM 2008 2 28 SWAA080976 1 20080221 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008022800257 20080228 00257 NM 2008 2 28 KCSA081113 1 20080223 A 5210 DOOR FRAME BOEING 747 747209B 138489B NM L1 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 L1 MAIN ENTRY DOOR HAS A 5 INCH LONG CRACK IN FORWARD LOWER VERTICAL FRAME AT STA 445 BETWEEN WL 205 & 210. 2 L 7 4 4F RT A20WE 2008022800264 20080228 00264 EA 2008 2 28 TRAX200800244 1 20080211 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 680BR 7679 AAR - PAX DOOR STEP "EXIT" PLACARD WORN. 2 L 7 2 4F RT A21EA 2008022800275 20080228 00275 EU 2008 2 28 08FDEA00549 1 20080122 A 5753 A2757030100400 TRUNNION AIRBUS 310 A310222 3930315 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 LT WING, INBD FLAP NR 1 TRUNNION WITH CORRODED AREA AND EXCESSIVE WEAR. TRUNNION NR 1 LT WAS REPAIRED IN ACCORDANCE WIT H CMM 57-52-15. 2 L 7 2 4F RT A35EU 2008022800294 20080228 00294 NM 2008 2 28 UPS08651693 1 20080219 A 2761 CAP BOEING 767 76734AF 1385212 NM NR 6 SPOILER CRACKED A IPXA K NONE K FLUID LOSS CL CLIMB 1 SO 01 326UP 27752 INSPECTION TYPE:N/A ATB - COMPLETE LEFT HYD SYSTEM QTY LOST. AT BLOCK, FLUID REMAINING 0.06. FOUND NR 6 SPOILER ACTUAT OR FILTER HOUSING CAP TO BE CRACKED AND LEAKING. INSTALLED INTERIM FITTING AND CAP PER EO B767-2760-28637A. ENTERED IN DMI LOG AS D369563. 2 L 7 2 4F RT A1NM 2008022800299 20080228 00299 EU 2008 2 28 Y2LA200800011 1 20080215 A 2120 UNKNOWN AIRBUS A319 A319112 3930323 EU CABIN ODOR A Y2LA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 07 553SX 3171 CABIN FILLED WITH STRONG SMELL AND HAZE JUST BEFORE LANDING. ENGINE IDLE CHECK, OIL ADDED. NO LEAKS NOTED. NO POST FL IGHT REPORT MESSAGES. AIRCRAFT DEPARTED NORMALLY. 2 L 7 2 4F RT A28NM 2008022800318 20080228 00318 NM 2008 2 28 SWAA081044 1 20080224 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800319 20080228 00319 NM 2008 2 28 SWAA081043 1 20080224 A 5311 69353656 BELTFRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND BELTFRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800337 20080228 00337 NM 2008 2 28 SWAA081008 1 20080224 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 733D, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008022800362 20080228 00362 NM 2008 2 28 GTIA0800008 1 20080220 A 3397 WIRE AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 534NK 3395 R-2 DOOR EXIT LIGHT DID NOT ILLUMINITE IN DTW. FOUND LOOSE WIRE AT R2 DOOR EXIT LIGHT. SECURED LOOSE WIRE. OPS CHECK OK PER AMM CH 33-51-38-860-052A. 2 L 7 2 4F RT A28NM 2008022800377 20080228 00377 NM 2008 2 28 SWAA081031 1 20080224 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800380 20080228 00380 NM 2008 2 28 SWAA081039 1 20080224 A 5311 6546534 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800392 20080228 00392 2008 2 28 SWAA081025 4 20080223 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008022800396 20080228 00396 NM 2008 2 28 SWAA081027 1 20080223 A 3840 288237 COMPRESSOR BOEING 737 7377H4 1384404 NM AFT CARGO BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 762SW 27876 STRONG ELECTRICAL SMELL REPORTED IN CABIN. FOUND WATER AIR COMPRESSOR FAULTY. REMOVED AND REPLACED WATER AIR COMPRESSO R PER MM. 2 L 7 2 4F RT A16WE 2008022800400 20080228 00400 NM 2008 2 28 CALA0800176 1 20080226 A 5310 6520723U66 DOOR FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 FORWARD CARGO DOOR CUTOUT AFT FRAME CRACKED AT LOWER STOP FITTING FOOTPRINT. REMOVED AND REPLACED FORWARD CARGO AFT FRA ME PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008022900011 20080229 00011 EU 2008 2 29 TRAX200800264 1 20080214 A 5313 STRINGER AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 CORROSION FOUND ON STR 21R, AT FR 44. CORROSION REMOVED AS PER SRM 51-21-42 ON STRG 218 AT FR 44. STRINGER AT FR 44, 21R , REPAIRED AS PER SRM 51-25-01. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR. IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPE NDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01. OUT OF LIMITS AS PER SRM 53-81-00 FIG 301. 2 H 7 2 4T RT 2008022900030 20080229 00030 2008 2 29 DL777080288 2 20080224 A 7200 ENGINE BOEING 777 777232 1385232 NM NR 1 VIBRATION A DALA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 SO 27 860DA 33239 29951 051001 NR 1 ENGINE REPLACED DUE TO HOC AND N3 VIBS. 2 L 7 2 4F RT T00001SE 2008022900041 20080229 00041 NM 2008 2 29 CALA0800177 1 20080227 A 5210 507945266 DOOR FRAME BOEING 737 737524 1384721 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 L-1 DOOR PAN CRACKED ON AFT EDGE 6TH STOP FROM TOP. REPAIRED L-1 DOOR PAN PER ECRA 5210-02001. 2 L 7 2 4F RT A16WE 2008022900042 20080229 00042 NM 2008 2 29 CALA0800178 1 20080227 A 5210 5079454 SKIN BOEING 737 737524 1384721 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 L-1 DOOR INNER SKIN CRACKED AT AFT EDGE 6TH STOP FROM TOP. REPAIRED L-1 DOOR INNER SKIN PER ECRA 5210-02001. 2 L 7 2 4F RT A16WE 2008022900043 20080229 00043 NM 2008 2 29 KCSA081119 1 20080227 A 5313 STRINGER BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE STRINGER IS CORRODED AT STA 2220, STR 40L. 2 L 7 4 4F RT A20WE 2008022900051 20080229 00051 EA 2008 2 29 TRAX200800286 1 20080220 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 858AS 7417 FS 280 ATTACH FITTING O/B LBL 9 CRACKED. REMOVED CRACKED F/S 280 ATTACH FITTING. FABRICATED AND INSTALLED SERVICEABLE ATTACH FITTING IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 2008022900056 20080229 00056 NM 2008 2 29 DL757080287 1 20080224 A 5330 146N3531 SKIN BOEING 757 757232 1384965 NM BS 1515 S28-29R DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 TOOLING MARKS WERE FOUND AT THE AIRPHONE ANTENNA SKIN AT FS 1515 BETWEEN S-28R AND S-29R. THE ANTENNA IS NO LONGER IN U SE. BECAUSE THE ANTENNA HAD BEEN SUBJECT TO AN STC, THE ANTENNA WAS REMOVED, AND THE FASTENER PATTERN CUTOUT. AN EXTE RNAL REPAIR DOUBLER WAS INSTALLED. CUTOUT WAS 8.6" BY 5.2". 2 L 7 2 4F RT A2NM 2008022900072 20080229 00072 EU 2008 2 29 08FDEA00631 1 20080227 A 5320 A5398674320500 ANGLE AIRBUS 310 A310324 3930206 EU INTERCOSTAL BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 EMPENNAGE FR 87 TO 88 APPROX STRINGER 29, THE INTERCOSTAL IS BENT. REMOVED INTERCOSTAL FOR FOM IAW SRM 51-40-21. REMO VED DAMAGED ANGLE FROM THE INTERCOSTAL IAW SRM 51-40-21. RECEIVED ANGLE. INSTALLED ANGLE AND INTERCOSTAL IAW SRM 51-40- 21. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008022900132 20080229 00132 SO 2008 2 29 SWIA200819235 1 20080215 A 3350 SIGN EMB 120 EMB120ER 3260203 SO CABIN MISSING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 569SW 120344 FLT 5746 - FORWARD EXIT SIGN IS MISSING. INSTALLED MISSING EXIT SIGN. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008022900133 20080229 00133 EA 2008 2 29 TRAX200800303 1 20080221 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 858AS 7417 FUSELAGE FRAME AT FS 349.0 HAS CORROSION AT BL 0. REMOVED CORROSION, DAMAGE FOUND WITHIN LIMITS IAW SRM 51-21-06. 2 L 7 2 4F RT A21EA 2008022900136 20080229 00136 EA 2008 2 29 TRAX200800305 1 20080222 A 5210 SKIN PANEL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 681BR 7680 AAR - PAX DOOR STAIRS, FWD SKIN PANEL IS CRACKED IN RADIUS UNDER STEP 832CT. 2 L 7 2 4F RT A21EA 2008022900138 20080229 00138 EA 2008 2 29 VNAA0802005 1 20080211 A 2611 PU90421R3 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE AFT LAVATORY FAILED A VNAA O OTHER N FALSE WARNING AP APPROACH 1 GL 05 258PS 6155 7941 CREW REPORTED A SMOKE TOILET AMBER MESSAGE ON APPROACH. CREW COULD NOT VISUALLY SEE ANY SMOKE AND THE FLIGHT LANDED WIT HOUT INCIDENT. MAINTENANCE INSPECTED AND MEL'D THE LAV SMOKE DETECTION SYSTEM PER MEL 26-16-01. MAINTENANCE REMOVED AN D REPLACED THE LAVATORY SMOKE DETECTOR IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MEL WAS CLEARED. AIRCRAFT W AS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008022800352 20080228 00352 NM 2008 2 28 SWAA081015 1 20080224 A 3246 161A11501 BEARING BOEING 737 7377H4 1384404 NM RT MLG FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 442WN 32459 DURING SCHEDULED WALKAROUND INSPECTION FOUND, NR 4 MLG WHEEL BEARING FAILURE. REMOVED AND REPLACED RIGHT MLG INNER CYCL INDER PER MM. 2 L 7 2 4F RT A16WE 2008022800369 20080228 00369 SO 2008 2 28 SWIA200819240 1 20080215 A 3350 COVER EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 561SW 120335 FLT 3691 - EMERGENCY LIGHT COVER NEAR MAIN CABIN DOOR IS BROKEN. REPLACED LIGHT ASSEMBLY NEAR THE MAIN CABIN DOOR. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008022800371 20080228 00371 NM 2008 2 28 HALA0800326 1 20080218 A 5512 PANEL BOEING 717 717200 1383700 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION, LT HORIZ STAB, LOWER SURFACE OF L/E PANEL. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800372 20080228 00372 NM 2008 2 28 HALA0800308 1 20080218 A 5711 FRAME BOEING 717 717200 1383700 NM LT WING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 CRACK ON O/B SECTION OF L-2 FORMER LEFT WING BELOW CENTER SECTION, VIEWED FROM 2ND WITNESS HOLE. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800373 20080228 00373 NM 2008 2 28 SWAA081017 1 20080224 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 440, STR 14R. REPAIRED SHEAR TIE PER EA. 2 L 7 2 4F RT A16WE 2008022800374 20080228 00374 NM 2008 2 28 SWAA081033 1 20080224 A 5311 6546550 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800376 20080228 00376 NM 2008 2 28 SWAA081032 1 20080224 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800378 20080228 00378 NM 2008 2 28 SWAA081035 1 20080224 A 5311 65C33509 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800379 20080228 00379 NM 2008 2 28 SWAA081040 1 20080224 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800398 20080228 00398 NM 2008 2 28 SWAA081029 1 20080224 A 5315 147A5504 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 765SW 29805 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, RBL 53. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800402 20080228 00402 EA 2008 2 28 TRAX200800252 1 20080213 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 846AS 7328 EMERGENCY LIGHTS AT A/S/D ENTRANCE, FWD LT AND RT WING AND CEILING AFT SIDE OUT. FLT 4485 CX. 2 L 7 2 4F RT A21EA 2008022900013 20080229 00013 EU 2008 2 29 TRAX200800266 1 20080214 A 5311 FRAME AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 CORROSION FOUND ON FR 19 AT STR 17R (AFT SIDE OF FR). CORROSION IS REMOVED IAW SRM 51-21-42 AND FOUND WITHIN LIMITS SR M 53-61-00 FIG 301. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR. IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPA IR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-31-42. 2 H 7 2 4T RT 2008022900014 20080229 00014 EU 2008 2 29 TRAX200800267 1 20080214 A 5340 STRINGER CLIP AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 CORROSION FOUND ON STRINGER CLIP AT FR 17 AND SRINGER 16R. CORROSION IS REMOVED IAW SRM 51-21-42 AND FOUND WITHIN LIMIT S SRM 53-61-00 FIG 301. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-21-42. 2 H 7 2 4T RT 2008022900015 20080229 00015 EA 2008 2 29 TRAX200800268 1 20080216 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 867AS 7463 FLAP FAIL ON VISUAL APPROACH. FLT 4585 DEL 132 MINS -NC FLT 4585 CX. FAILED AT 0 DEG WHEN SELECTING 8. TOWER ROLLED T HE FIRE TRUCKS AND AMBULANCE FOR SAFETY. REMOVED AND REPLACED FLAPS SCEW DETECTION UNIT ASSY IAW AMM 27-51-15. OP'S CH ECK GOOD. DML CLEARED PLACARD REMOVED. 2 L 7 2 4F RT A21EA 2008022900017 20080229 00017 EA 2008 2 29 TRAX200800270 1 20080213 A 5220 SHAFT CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 889AS 7538 CREW ESCAPE HATCH OUTER HANDLE SHAFT HAS MOISTURE AND CORROSION. 2 L 7 2 4F RT A21EA 2008022700338 20080227 00338 NM 2008 2 27 SWAA080867 1 20080217 A 5311 6546548 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700349 20080227 00349 NM 2008 2 27 SWAA080870 1 20080217 A 5753 65C30462 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 DURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD FOREFLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2008022800055 20080228 00055 NM 2008 2 28 HALA0800336 1 20080219 A 5311 FRAME BOEING 717 717200 1383700 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION, ON RADOME INTERNAL FORMER RING. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800058 20080228 00058 NM 2008 2 28 08FDEA00604 1 20080226 A 5730 ARB74024 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 16 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RT WING, LOWER SKIN ACCESS DOOR CUT OUT BET WEEN STA XORS 690 AND XORS 700. REPAIR CARRIED OUT AS PER EA 1-5710-118761 PART 1, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008022800074 20080228 00074 NM 2008 2 28 KCSA081091 1 20080220 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 CORROSION ON FUSELAGE SKIN AT BS 1960, STR 23L. 2 L 7 4 4F RT A20WE 2008022800082 20080228 00082 NM 2008 2 28 SWAA080927 1 20080219 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800104 20080228 00104 NM 2008 2 28 HALA0800300 1 20080220 A 5280 SEAL BOEING 767 76733A 1385209 NM NLG DOOR DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON RT FWD NOSE GEAR DOOR GAP SEAL FASTENERS (17 EACH SCREW HEADS). CLEANED, TREATED AND PRIMED PER SRM 53-00-01 PAINT PEND. AREA PAINTED AS PER 51-22-01. 2 L 7 2 4F RT A1NM 2008022800124 20080228 00124 NM 2008 2 28 SWAA080937 1 20080217 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 744B AND BS 727C, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008022800135 20080228 00135 NM 2008 2 28 UIEA200800062 1 20080215 A 5330 SKIN BOEING 747 7472D7B 1384803 NM ZONE 200 SCRATCHED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 SURROUNDING M/D L-3 DOOR CUTOUT AFT LOWER DOUBLER EDGE FUSELAGE SKIN FOUND SCRIBE LINE. BLENDED PER BOEING LETTER NR 1- 749452899-5 AND EO4753B109. 2 L 7 4 4F RT A20WE 2008022800137 20080228 00137 NM 2008 2 28 SWAA080954 1 20080219 A 5322 6546569 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 986, STR 27R. REPAIRED SHEAR TIE PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800159 20080228 00159 NM 2008 2 28 HALA0800200 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 866 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT RBL 88.5, STA 866, MAX DEPTH BLENDOUT WAS 0.012". BLENDED IAW SRM 51-10-02 . ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022800174 20080228 00174 EU 2008 2 28 AALA200800282 1 20080210 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 JFK - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008022800194 20080228 00194 NM 2008 2 28 DL76S080162 1 20080205 A 5330 143T35214 SKIN BOEING 767 767332 1382001 NM FS 536 S27R DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FOUND SKIN BLENDS AT FS 536 - FS 625, AND S-27R TO S-33R. 2 L 7 2 4F RT A1NM 2008022800203 20080228 00203 EU 2008 2 28 U5QA06010 1 20080220 A 2780 SLAT SYSTEM ISRAEL 1125 ASTRASPX 4500205 EU WING MALFUNCTIONED E U5QA K NONE J WARNING INDICATION DE DESCENT 1 CE 05 115BR 099 AIRCRAFT FLYING FROM MTN TO RDG IN DESCENT HAD LEADING EDGE SLAT FAULT. SYSTEM SHUT OFF. PILOT OVERRIDE SYSTEM TO DEPL OY FLAPS. CHANGED DESTINATION TO TEB. NO EMERGENCY DECLARED. MADE NORMAL LANDING. ON THE GROUND COULD NOT RESET SYST EM. LATER HAD MAINTENANCE RESET SYSTEM WITH BREAKOUT BOX. MAINTENANCE CHECKED RIGGING AND VOLTAGES, ALL NORMAL. 2 L 7 2 4F RT A16NM 2008022800207 20080228 00207 NM 2008 2 28 AALA200800301 1 20080211 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 26C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 26C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008022800218 20080228 00218 NM 2008 2 28 CALA0800164 1 20080221 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 FOUND CORROSION ON FLOORBEAM AT BS 328 AND LBL 30.0 AS SEEN FROM E&E COMPARTMENT CEILING. INSTALLED REPAIR AND REPAIR P ARTS PER SRM 53-10-51. 2 L 7 2 4F RT A16WE 2008022800224 20080228 00224 NM 2008 2 28 SWAA080969 1 20080221 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 202WN 33999 LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008022900142 20080229 00142 NM 2008 2 29 DLM88080268 1 20080213 A 5753 SKIN DOUG MD88 MD88 3023688 NM TE FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 DURING HMV, IT WAS FOUND A DELAMINATION ON UPPER SKIN OF INBOARD GUIDE VANE AT RT OUTBOARD FLAP. A PERMANENT REPAIR WAS PERFORMED IAW MD-80 SRM 57-03D PARAGRAPH 8A FIGURE 9A AND SRM 51-70-2D PARAGRAPH 6A, 6C, 10B, 10D AND 10E 2 L 7 2 4F RT A6WE 2008022900145 20080229 00145 2008 2 29 SWIA200819261 4 20080222 A 3418 SENSOR CNDAIR CL600 CL6002C10 1390015 EA LT AOA DAMAGED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 368CA 10075 FLT 4029 - DURING TAKEOFF, RECEIVED A STALL WARNING MESSAGE ALONG WITH AN AURAL WARNING. REPLACED LEFT AOA VANE ASSEMBL Y IAW MM 27-35-05. OPS CHECK GOOD, PN C1625AA, SN OFF 532. 2 L 7 2 4F RT A21EA 2008022900148 20080229 00148 NM 2008 2 29 HALA0800353 1 20080222 A 5753 SKIN BOEING 767 7673G5 1385126 NM TE FLAP DENTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 DENT ON RT WING I/B T/E FLAP, ON UPPER SKIN 16" FROM I/B END IN MIDDLE OF WEDGE. ASSESSED DENT IAW SRM 57-53-01, DENT O UT OF SRM LIMITS. REPAIRED DENT IAW B767 SRM 51-70-10 REPAIR 4, REV 76. 2 L 7 2 4F RT A1NM 2008022900151 20080229 00151 NM 2008 2 29 HALA0800356 1 20080226 A 5730 SKIN BOEING 767 7673G5 1385126 NM RT WING CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION RT WING UPPER SURFACE, AROUND FASTENER AT WING STA 865 AND 4 INCHES AFT OF FRONT SPAR. CORROSION REMO VED IAW B767300 SRM 51-10-02 TO THE POINT OF CONFIRMATION WITH 10X MAGNIFING GLASS. NO OTHER DAMAGE EXISTS ON THIS LINE PERPENDICULAR TO REAR SPAR. REF SRM 57-20-01, FIG 101, "B". 2 L 7 2 4F RT A1NM 2008022900156 20080229 00156 NM 2008 2 29 GTIA0800018 1 20080109 A 5315 FLOORBEAM AIRBUS A321 A321231 3940032 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 FOUND Y 512 AT FRAME 66 CORRODED. REPLACE Y 512 AT FRAME 66. 2 L 7 2 4F RT A28NM 2008022900159 20080229 00159 NM 2008 2 29 GTIA0800026 1 20080124 A 5297 CONNECTOR AIRBUS A321 A321231 3940032 NM L4 DOOR DAMAGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 585NK 1438 L4 DOOR CONNECTOR 13WL-A PIN "C" TO M FAILED CONTINUITY CHECK. CLEANED AND REINSTALLED WIRE TERMINAL AT 6924VN. 2 L 7 2 4F RT A28NM 2008022900160 20080229 00160 NM 2008 2 29 GTIA0800016 1 20080109 A 5315 SPLICE AIRBUS A321 A321231 3940032 NM FLOORBEAM CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 Y-1292 AT FRAME 66 FLOORBEAM SPLICE HAS CORROSION. REPLACED FLOORBEAM SPLICE. 2 L 7 2 4F RT A28NM 2008022900167 20080229 00167 NM 2008 2 29 HALA0800313 1 20080218 A 5711 FRAME BOEING 717 717200 1383700 NM RT WING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 CRACK ON O/B SECTION OF MOST FWD FORMER RIGHT WING BELOW CENTER SECTION, VIEW FROM 2ND WITNESS HOLE. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022900173 20080229 00173 EA 2008 2 29 SWIA200819244 1 20080215 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA LIGHTS ARCED A SWIA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 07 418SW 7446 CONNECTOR PINS IN P167/J167 SHOW SIGNS OF ARCING. REPLACED P167 AND J167 CONNECTOR IAW MM 25-28-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008022900175 20080229 00175 SO 2008 2 29 SWIA200819246 1 20080217 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DAMAGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 294SW 120321 FLT 5576 - EXIT SIGN OVER SEAT 9B DOES NOT ILLUMINATE. REPAIRED WIRING AT EMERGENCY EXIT LIGHT ASSEMBLY. OPS CHECK GOO D. 2 L 7 2 4T RT A31SO 2008022900176 20080229 00176 EA 2008 2 29 SWIA200819247 1 20080219 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA ODOR A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 946SW 7776 FLT 5932 - RECEIVED A SMOKE TOILET CAUTION MESSAGE. REPLACED LEFT AND RIGHT COALESCER BAGS IAW 21-51-13 CMM. PERFORMED ENGINE RUNS IAW 71-00-00. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2008022900178 20080229 00178 EA 2008 2 29 MASA200800134 1 20080215 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 27173 11742 7173 FLT 7348, IAD NOSE GEAR DISAGREE ON GEAR EXTENSION. MX TROUBLESHOT TO A NOSE PRIORITY VALVE AND REPLACED, OP GOOD. 2 L 7 2 4F RT A21EA 2008022900179 20080229 00179 EA 2008 2 29 MASA200800135 1 20080216 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS DEFECTIVE A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 27173 11023 7173 FLT 7230, ORD - PILOT REPORTED A NOSE GEAR DISAGREE ON GEAR EXTENSION. REMOVED AND REPLACED 3A PUMP, LOW FLOW VOLUME CA USING GEAR DISAGREE. 2 L 7 2 4F RT A21EA 2008022900180 20080229 00180 NM 2008 2 29 MASA200800136 1 20080216 A 2560 2LA00734480 SIGN DHAV DHC8 DHC8202 2809007 NM CABIN BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 991HA 431 ASH FLT 2949 ASE-PHX, SEAT 1F EMERGENCY EXIT SIGN BROKE OFF. REMOVED AND REPLACED EXIT SIGN. 2 H 7 2 4T RT A13NM 2008022900181 20080229 00181 EA 2008 2 29 MASA200800137 1 20080216 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 933LR 15033 ASH FLT 2667 EWR-CLT, CEILING LEVEL EMERGENCY FLOOD LIGHT AT ROW 23 INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2008022900190 20080229 00190 EA 2008 2 29 MASA200800147 1 20080218 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27191 7191 FLT 2741, ICT-PHX, ALL EMERGENCY LIGHTS ARE INOP. RECHARGED BATTERY PACKS AND LIGHTS WORKED NORMAL. 2 L 7 2 4F RT A21EA 2008022900192 20080229 00192 2008 2 29 MASA200800149 4 20080218 A 2350 MC1035101 MICROPHONE CNDAIR CL600 CL6002C10 1390015 EA OXYGEN MASK INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 521LR 6186 10261 ASH FLT 7297 SAT-ORD. CAPTAINS OXYGEN MASK MIC INOP. REMOVED AND REPLACED MASK. 2 L 7 2 4F RT A21EA 2008022900194 20080229 00194 NM 2008 2 29 MASA200800151 1 20080218 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 5 DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 989HA 427 REPAIR TO LEFT NR 5 FLAP TRACK. 2 H 7 2 4T RT A13NM 2008022900207 20080229 00207 NM 2008 2 29 08FDEA00523 1 20080220 A 5520 65206611 RIB BOEING 727 727233 138408A NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 LT HORIZONTAL STABILIZER MAIN BOX INTERIOR RIB CRACKED AT LIGHTENING HOLE STAB STA 69. CUT OUT FWD WEB FOR ACCESS IAW S RM 55-10-3 FIG2. FABRICATED REPAIR DOUBLER FOR INTERNAL RIB IAW SRM 55-10-4 FIG 2 AND 55-10-2 FIG2. FABRICATED REPAIR DO UBLERS IAW SRM 55-10-5 FIG2, 55-10-2 FIG2. TREATED AND PRIMED ALL PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 55-10-4 FIG 2 55-10-5 FIG 2. 2 L 7 3 4F RT A3WE 2008030300008 20080303 00008 NM 2008 3 3 AALA200800366 1 20080220 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 176AA 32395 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT AFT OVERWING EXIT INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEF T AFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008030300012 20080303 00012 NM 2008 3 3 AALA200800378 1 20080221 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 JFK - EMERGENCY LIGHT AT SEAT 1G INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 1G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008030300013 20080303 00013 WP 2008 3 3 AALA200800368 1 20080221 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 492AA 49730 LGA - EMERGENCY LIGHTS AT AFT BULKHEAD CEILING INOPERATIVE. REPLACED BATTERY PACK AT RIGHT LAVATORY FOR EMERGENCY LIGHT S AT AFT BULKHEAD CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300015 20080303 00015 2008 3 3 2008UALA00916 4 20080216 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR SLIDE LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 585UA 26709 DOOR 1R SLIDE PACK HAS HANGING LANYARD. SECURED LOOSE SLIDE PACK LANYARD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030300016 20080303 00016 NM 2008 3 3 2008UALA00106 1 20080104 A 2133 OUTFLOW VALVE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN PRESSURE MALFUNCTIONED A UALA O OTHER O OTHER AP APPROACH 1 WP 29 338UA 24242 CREW REPORTS DURING SINGLE PACK OPERATION, THE A/C FAILED TO MAINTAIN PRESSURIZATION DURING THE APPROACH. AIRCRAFT HAS CHRONIC PRESSURIZATION ISSUE. REPLACED REAR OUTFLOW VALVE. REPLACED FIRST OFFICER'S ALTIMETER, REPAIRED MISCELLANEOUS FUSELAGE DRAINS, REPAIRED AFT CARGO DOOR SILL AREA, ETC. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300017 20080303 00017 NM 2008 3 3 2008UALA00881 1 20080215 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 S11L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 STRINGER CLIP ON FWD SIDE OF FRAME 294.5 STR 11L IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300020 20080303 00020 NM 2008 3 3 2008UALA00884 1 20080215 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM BS 360 S16L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 STR 16L BS 360 INTERCOSTAL WEB IS DAMAGED. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW INTERCOSTAL. AC OK F OR SERVICE. 2 L 7 2 4F RT A16WE 2008030300022 20080303 00022 NM 2008 3 3 2008UALA00886 1 20080215 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 SKIN LAP TAB END ROW FASTENERS DAMAGED JUST ABOVE STR 20R. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED INTERNAL S KIN REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300023 20080303 00023 NM 2008 3 3 2008UALA00887 1 20080215 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 S7L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FORWARD ENTRY DOOR SURROUND STRUCTURE STA 294.5 INTERCOSTAL AT STR 7L HAS TWO CRACKS. MAJOR REPAIR ACCOMPLISHED: REPLACE D INTERCOSTAL REF EA 080094 REV IR . 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300026 20080303 00026 NE 2008 3 3 2008UALA00640 2 20080201 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LEFT MAKING METAL A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 773UA 26929 777049 ENG OIL FILTER L DISPLAYED ON EICAS. ENGINE REPLACED AT SFO DUE TO FERROUS METAL FOUND ON ALL MAGNETIC CHIP DETECTORS ( MCD'S). AS OF 03/04/08 ENGINE IS IN UA'S ENGINE SHOP UNDERGOING TEARDOWN INVESTIGATION. EXPECT FINAL FINDINGS BY 03/31/ 08. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008022800291 20080228 00291 2008 2 28 DL738080171 2 20080206 A 7532 BLEED VALVE BOEING 737 737832 13844CF NM NR 2 ENGINE SLUGGISH A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 27 397DA 18344 30537 RIGHT BLEED TRIP OFF COMPLIED W/QRH PROCEDURE WILL NOT RESET DIVERTED FLT TO ATL NOTE; ATTEMPTED RESET AT FL300 WITH CRU ISE POWER SET APPROX 80 PERCENT N1. NO ENGINE OR WING ANTI-ICE WAS ON AT TIME OF TRIP. REMOVED AND REPLACED HIGH STAGE VALVE PER MM. LEAK CHECK GOOD, CHECKOUT OF HIGH STAGE, PRECOOLER AND PRSOV PER ERA 46272514MA CHECKS GOOD. 2 L 7 2 4F RT A16WE 2008022800306 20080228 00306 NM 2008 2 28 SWAA081002 1 20080222 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND KEEL BEAM CORRODED AT BS 538, RBL 6.5. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2008022800338 20080228 00338 EU 2008 2 28 08FDEA00557 1 20080222 A 5330 A53773487 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND NICK/DENT AT EXTERNAL SKIN PANEL, C22-23, P52-53 LT REPAIR PERFORMED BY DRESS OUT THE DENT IAW SRM 51-73-00 AND SK IN REPAIR BY BUSH IAW SRM 53-10-12 FIG 221 SHEET 1. 2 L 7 2 4F RT A35EU 2008022800342 20080228 00342 EU 2008 2 28 08FDEA00559 1 20080222 A 5311 B53770012200 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND SEVERAL CHAFING MARKS ON INNER FLANGE OF FRAME C28, P 13-22 LT. REPAIR PERFORMED BY BLEND OUT THE AREAS AND NDT F OR CRACK FREE IAW RAS/DABRE/7008942/2008 ISS A, APPROVED BY EA 6-5314-115244. 2 L 7 2 4F RT A35EU 2008022800381 20080228 00381 NM 2008 2 28 SWAA081038 1 20080224 A 5311 6546538 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800383 20080228 00383 NM 2008 2 28 SWAA081036 1 20080224 A 5311 65C34356 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800386 20080228 00386 NM 2008 2 28 SWAA081020 1 20080224 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800393 20080228 00393 NM 2008 2 28 SWAA081026 1 20080224 A 3350 20311A BATTERY BOEING 737 737317 138447P NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED MV2 CHECK, RT FWD CABIN EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008022900022 20080229 00022 EA 2008 2 29 TRAX200800275 1 20080217 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 889AS 7538 FS 333 FRAME IS CORRODED AT BL 0. 2 L 7 2 4F RT A21EA 2008022900028 20080229 00028 EA 2008 2 29 TRAX200800281 1 20080219 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 980EV 7759 FLAP FAIL AT ZERO ON APPROACH. EMERGENCY EQUIPMENT ON STANDBY. 2 L 7 2 4F RT A21EA 2008022900032 20080229 00032 NM 2008 2 29 08FDEA00621 1 20080226 A 5330 A6A7112507 SPLICE DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 HFEC INSPECTION CARRIED OUT AND FOUND CRACK AT L-1 RT SPLICE WITH CRACK LENGTH OF APPROX 1 INCH AT STA 6-100. REPAIR CA RRIED OUT AS PER EA 1-5330-118767, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008022900055 20080229 00055 EA 2008 2 29 TRAX200800288 1 20080220 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 681BR 7680 RIGHT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED REQ'D FASTNERS TO RT OBLIQUE ANGLE AT FS 625 DISCARDED. DUPLICATED, LOC ATED HOLES, DEBURRED, ALODINED, PRIME, TOPCOATED NEW ANGLE AND INSTALLED WET WITH FASTNERS PER SRM 53-61-17 PG3 51-21-11 , 51-25-06, 51-25-16, 51-23-00, AND 51-42-21. 2 L 7 2 4F RT A21EA 2008022900068 20080229 00068 NM 2008 2 29 08FDEA00627 1 20080227 A 5311 6556122 FRAME BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 AFT LWR CARGO BAY AT BS 950D BETWEEN STR S-29L AND S-28L, AFT SURFACE OF FRAME AND LWR SURFACE OF LWR CHORD HAVE CORROSI ON REMOVED FASTENERS FROM STA 950D STR 28L - 30L, BLENDED CORROSION, ORIGINAL MATERIAL .071". REMAINING MATERIAL .058 I NCH, MATERIAL REMOVED .031", OUT OF LIMITS, SRM 53-10-1 PG 2, TOOL ID NR IN22-0029, CAL DUE DATE 09/28/08. REMOVED STRI NGER CLIPS FROM STR 28L - 30, STR 28L -30. FABRICATED NEW SHEAR TIE, SUPPORT ANGLE AND SUPPORT CHANNEL, MEASURED MATE RIAL FOR FAIL/SAFE, ORIGINAL MATERIAL .071" REMAINING MATERIAL .067, LOSS OF .004. WITHIN LIMITS REF SRM 53-10-1 PG2. FABRICATED DOUBLER, TREATED AND PRIMED AND INSTALLED REF SRM 51-10-2, SRM 51-30-2, SRM 53-10-4, BOEING DWG 69-44109. 2 L 7 3 4F A3WE 2008022900071 20080229 00071 NM 2008 2 29 08FDEA00630 1 20080227 A 5330 53FX1301 SKIN BOEING 727 727227 1384078 NM BS 520-524 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 LT LWR FUSELAGE EXTERIOR SKIN SURFACE SHOWS CRACK AT STA 520, ABOVE STR 23L, FWD OF THE STATIC PORT. PERFORMED HFEC AND FOUND CRACK 2" IAW B727 NDTM PART 6 51-00-00 FIG23. REPAIRED FUSELAGE, MDCD SURROUND STRUCTURE TRIPLER AT STA 520, STR 23L IAW EA NR 7-5330-116956 PART 1, B727 SRM 53-30-3 FIG 23, SRM 53-30-3 FIG 1 B. PERFORMED RVSM INSP ON LT FUSELAGE A FFECTED AREA IAW MM 51-10-00. 2 L 7 3 4F A3WE 2008022900079 20080229 00079 EA 2008 2 29 TRAX200800293 1 20080221 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 901EV 7616 FLAP FAIL AT 0 DURING APPROACH. EN ROUTE TO PVD A/C DIVERTED TO BOS DUE TO MTC. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2008022900084 20080229 00084 EA 2008 2 29 TRAX200800296 1 20080221 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 331CA 10061 LEFT LOWER OVERWING EMERGENCY DOOR EXIT LIGHT INOP. 2 L 7 2 4F RT A21EA 2008022900131 20080229 00131 EA 2008 2 29 TRAX200800302 1 20080221 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 858AS 7417 AAR - BATH TUB FITTING AT FS 461, RBL 9, CRACKED. REMOVED UNSERVICEABLE BATH TUB FITTING . LOCATED HOLES IN NEW FITTIN G, IAW SRM 51-42-11. OK TO INSTALL INSTALLED NEW SERVICEABLE FITTING PER SRM 51-42-21. OK TO FILLET SEAL AND TOUCH-UP F INISH. APPLIED FILLET SEAL PER SRM 51-23-00 AND TOUCHED-UP FINISH A023 PER SRM 51-21-16. 2 L 7 2 4F RT A21EA 2008022900153 20080229 00153 NM 2008 2 29 GTIA0800029 1 20080115 A 5320 FLOOR SUPPORT AIRBUS A321 A321231 3940032 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 Y 765 FLOOR SUPPORT 18-24 HAS CORROSION BEYOND LIMITS. REPLACED FLOOR SUPPORT Y 765. 2 L 7 2 4F RT A28NM 2008022900168 20080229 00168 NM 2008 2 29 HALA0800312 1 20080218 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION ON BELLY, JUST LEFT OF MLG DOOR BY PASS CUTOUT. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022900171 20080229 00171 NM 2008 2 29 HALA0800322 1 20080218 A 5510 STRUCTURE BOEING 717 717200 1383700 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION, LOCK FASTENERS ON TOP OF LT HORIZ STAB, L/E PANEL. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022900174 20080229 00174 EA 2008 2 29 SWIA200819245 1 20080220 A 3230 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 432SW 10935 10935 7548 FLT 3919 - NOSE GEAR EXTENDED IN FLIGHT. REPLACED PSEU WITH A SERVICEABLE UNIT. OPS CHECKS GOOD IAW MM 32-30-00. 2 L 7 2 4F RT A21EA 2008022900183 20080229 00183 EA 2008 2 29 MASA200800140 1 20080217 A 5220 601R350353 SEAL CNDAIR CL600 CL6002D24 1390016 EA ESCAPE HATCH DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 907FJ 15007 ASH FLT 2626 CLT-JFK. WATER LEAKING FROM FLIGHT DECK EMERGENCY ESCAPE HATCH. REPLACED FLIGHT DECK ESCAPE HATCH SEAL, O PS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008030300009 20080303 00009 NM 2008 3 3 AALA200800379 1 20080221 A 3350 SIGN BOEING 737 737823 13844BZ NM EMERGENCY EXIT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 918AN 29519 DFW - OVERHEAD EMERGENCY EXIT SIGN LIGHT AT OVERWING EXIT IS MISSING. REPLACED CEILING PANEL WITH EMERGENCY EXIT SIGN F OR EMERGENCY LIGHT AT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008030300044 20080303 00044 NM 2008 3 3 2008UALA00889 1 20080215 A 5320 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 727E S20R NICKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 RT NICKED AT BS 727E STR 20R. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR DOUBLER/TRIPLER AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300048 20080303 00048 NM 2008 3 3 2008UALA00894 1 20080218 A 2120 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE COCKPIT ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 791UA 26933 AFTER ENG START CREW REPORTED STRONG OIL ODOR ON FLT DECK. SUSPECT OIL LEAK FROM ENGINE OR APU. CHECKED APU & BOTH E NGINES. NO LEAKS OR OIL CONTAMINATION NOTED. NO ABNORMAL OIL CONSUMPTION NOTED. OK PER FIM 21-00 TASK 808. ACFT OK FOR SERVICE. NO REPEAT OF PROBLEM THRU 3/15/2008. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008030300050 20080303 00050 EU 2008 3 3 2008UALA00717 1 20080209 A 2697 CIRCUIT BREAKER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO FIRE AGENT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 426UA 510 CARGO FIRE AGENT 2 DISCHARGE LIGHT ON. RESET CB FOR BOTTLE DISCHARGE SYSTEM AND INDICATION RETURNED TO NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030300051 20080303 00051 EU 2008 3 3 2008UALA00818 1 20080213 A 2913 PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD SYSTEM LEAKING A UALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 29 402UA 439 FLIGHT DIVERTED DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. HYDRAULIC LEAK AT PTU. REPLACED PTU AND ALSO FOUND NR 1 EDP LEA KING, REPLACED AS WELL. SERVICED HYDRO FLUID AND PUT GEAR SYSTEM BACK TO NORMAL CONFIG. ALL SYSTEM TEST GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030300052 20080303 00052 2008 3 3 2008UALA00917 4 20080216 A 2565 STRAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE DISLODGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 581UA 26701 D-RING AND STRAP HANGING FROM DOOR 2L SLIDE PACK. REATTACHED LANYARD TO DOOR SLIDE, OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030300058 20080303 00058 NM 2008 3 3 2008UALA00838 1 20080214 A 5511 SPAR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 HORIZONTAL STABILIZER CENTER SECTION REAR SPAR LT UPPER CLEVIS HAS CORROSION ON AFT SIDE OF THE AFT CLEVIS AND FWD SIDE OF THE FWD CLEVIS AROUND THE BUSHING. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300059 20080303 00059 NM 2008 3 3 2008UALA00839 1 20080214 A 5520 BOLT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ELEVATOR BUSS AS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 ELEVATOR BUSS ASSY (NO SERIAL NR) LT SIDE OF CRANK ASSEMBLY BOLT IS DAMAGED. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300063 20080303 00063 WP 2008 3 3 AALA200800346 1 20080217 A 3230 BUSHING DOUG DC9 DC982 3022082 WP NLG WORN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 400AA 49311 DFW INFLIGHT T1429/17FEB - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FO UND WORN ELECTRIC BUSHINGS ON LOWER SCISSOR LINK. REPLACED LOWER SCISSOR LINK BUSHINGS AND PIN. ACCOMPLISHED NOSE STRU T REPACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300064 20080303 00064 WP 2008 3 3 AALA200800347 1 20080217 A 3510 B-NUT DOUG DC9 DC983 3022083 WP OXYGEN SYSTEM LOOSE A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 563AA 49345 IAD INFLIGHT T1281/17FEB BOS TO DFW - AT FL320 CREW REPORTED AIRCRAFT LOST PRESSURIZATION. OXYGEN MASKS DEPLOYED. LAND ED IAD WITHOUT INCIDENT. SECURED LOOSE B NUT ON LEFT PACK SENSE LINE. FERRIED TO LGA. REPLACED ALL PASSENGER AND FLIG HT ATTENDANT OXYGEN CANISTERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008030300066 20080303 00066 NM 2008 3 3 AALA200800341 1 20080216 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 786AN 30250 NRT - EMERGENCY LIGHT IN FIRST CLASS GALLEY AT LOWER LEFT SIDE BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT IN FIRST CLASS GALLEY AT LOWER LEFT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008030300067 20080303 00067 WP 2008 3 3 AALA200800344 1 20080216 A 3350 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 969TW 53619 SFO - EMERGENCY EXIT LIGHTS AT OVERHEAD RIGHT AND LEFT OVERWING EXIT DOORS INOPERATIVE. RESEATED BATTERIES IN BATTERY P ACK FOR EMERGENCY EXIT LIGHTS AT OVERHEAD RIGHT AND LEFT OVERWING EXIT DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008030300072 20080303 00072 WP 2008 3 3 AALA200800369 1 20080221 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 492AA 49730 LGA - EMERGENCY LIGHT AT OVERHEAD SEAT 5E INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 5E. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300073 20080303 00073 NM 2008 3 3 AALA200800337 1 20080213 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 907AN 29509 TUL - EMERGENCY LIGHT BATTERY PACK FOR AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT STATION 952 FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008030300076 20080303 00076 NM 2008 3 3 AALA200800334 1 20080205 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 904AN 29506 TUL - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008030300077 20080303 00077 NM 2008 3 3 AALA200800335 1 20080208 A 5322 SHEAR TIE BOEING 767 767323 1385205 NM BS 742 S37-38L CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 384AA 26996 AFW - SHEAR TIE AT FORWARD CARGO STATION 742 BETWEEN STRINGER 38L AND 37L CORRODED BEYOND LIMITS. REPLACED SHEAR TIE AT FORWARD CARGO STATION 742 BETWEEN STRINGER 38L AND 37L. 2 L 7 2 4F RT A1NM 2008030300079 20080303 00079 WP 2008 3 3 AALA200800370 1 20080221 A 3350 P2010031701 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70529 49921 TPA - EMERGENCY LIGHT AT FORWARD BULKHEAD HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FORWARD BULKHEAD. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300083 20080303 00083 NM 2008 3 3 AALA200800377 1 20080221 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 918AN 29519 DFW - EMERGENCY LIGHT AT FORWARD LEFT EXTERIOR OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD LEFT HAND EXTERIOR OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008030300084 20080303 00084 WP 2008 3 3 AALA200800361 1 20080220 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 234AA 49181 STL INFLIGHT T515/20FEB, NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REPACK ED NOSE LANDING GEAR SHOCK STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300086 20080303 00086 NM 2008 3 3 AALA200800357 1 20080220 A 2597 10682 POWER SUPPLY BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 774AN 29581 NRT INFLIGHT T167/20FEB - POWER PORT AT SEAT 13D BEGAN TO SMOKE WHEN USED. DISCONTINUED USE OF POWER PORT. LANDED NRT WITHOUT INCIDENT. SECURED POWER PORT WIRE HARNESS AND REPLACED POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008030300087 20080303 00087 NM 2008 3 3 2008UALA00844 1 20080214 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 FUSELAGE DENTED AND CRACKED, APPROX 3 FEET AFT OF DOOR 2L, 3 TO 6 INCHES ABOVE WATER LINE. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030300088 20080303 00088 NM 2008 3 3 2008UALA00845 1 20080214 A 2612 SQUIB AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE AFT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 809UA 825 AFT SQUIB LIGHT WILL NOT TEST DISCHARGE. RERACKED SDCU AND TEST OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030300090 20080303 00090 NM 2008 3 3 2008UALA00830 1 20080214 A 5321 FLOORBOARD AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 821UA 944 A-PIT FLOORBOARD AND SKID PLATES FOUND WITH SEVERAL AREAS ON THE FLOOR SUPPORT WITH CORRISION. ACCOMPLISHED MAJOR REPA IR AT ORD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030300092 20080303 00092 NM 2008 3 3 AALA200800355 1 20080219 A 3350 1722331 SOCKET BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 646AA 24604 SFO - EMERGENCY LIGHTS AT SEAT ROWS 26 AND AFT INOPERATIVE. REPLACED SOCKETS AT SEAT ROW 29 FOR EMERGENCY LIGHTS AT SEA T ROWS 26 AND AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008030300094 20080303 00094 WP 2008 3 3 AALA200800376 1 20080221 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 DFW - EMERGENCY LIGHT AT SEAT 30D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 30D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300097 20080303 00097 WP 2008 3 3 AALA200800371 1 20080221 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 417AA 49328 DFW - EMERGENCY LIGHT AT SEAT 20D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300101 20080303 00101 EA 2008 3 3 SWIA200819252 1 20080222 A 2750 SHAFT CNDAIR CL600 CL6002C10 1390015 EA TE FLAPS DISCONNECTED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 611SK 10035 FLT 4003 - FLAPS FAIL CAUTION MESSAGE DISPLAYED AFTER TAKE OFF. RESECURED LEFT OUTBOARD FLAP TORQUE TUBE SPLINE SHAFT A ND SAFETIED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008030300103 20080303 00103 NM 2008 3 3 HALA0800323 1 20080218 A 5410 CHANNEL BOEING 717 717200 1383700 NM NR 1 NACELLE GOUGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 .25 INCH DEEP GOUGE ON NR 1 ENGINE, TOP COWL CHANNEL AT 1ST GUIDE PIN. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008030300105 20080303 00105 NM 2008 3 3 HALA0800325 1 20080218 A 5410 STRUCTURE BOEING 717 717200 1383700 NM NR 1 NACELLE GOUGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 3 GOUGES ON NR 1 ENGINE, TOP COWL INTERIOR, NEAR FAN AIR VALVE EXIT. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008030300108 20080303 00108 NM 2008 3 3 08FDEA00636 1 20080227 A 5315 143N501447 FLOORBEAM BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 MAIN CARGO DECK FLOORBEAM AT STA. 700, LBL 58 HAS CORROSION. REMOVED CORROSION, AREA IS L=8", W=2", D=.035". ORIGINAL MATERIAL THICKNESS, 0.140" AFTER REWORK, 0.105', FOUND TO BE OUT OF SRM 53-00-51, FIG 101, DETAIL III LIMITS. REMOVED DAMAGED AREA IAW SRM 53-00-51 REPAIR NR 3. FABRICATED REPAIR PARTS ON MAE TRAVELERS T7/711676 (CHORD), T7/711674 (ANGL E NR 2), T7/714488 (STUB FRAME), T7/711675 (ANGLE NR 3), T7/711672 (STRAP NR 4), T7/711673 (STRAP NR 5) AND T7/714135 (D OUBLER). INSTALLED REPAIR PARTS IAW SRM 53-00-51, REPAIR NR 3. 2 L 7 2 4F RT A2NM 2008030300110 20080303 00110 NM 2008 3 3 08FDEA00638 1 20080228 A 5720 FLANGE DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT WING LEADING EDGE APPROXIMATELY STATION XOS = 900 AT HINGE PANEL NR 526FB, INBOARD MOST LATCH MATING SURFACE FLANGE FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01, VOL.II, FOUND OUT OF LIMIT AS PER SRM 57-20- 00, FIG.17, VOL I . ORIGINAL THICKNESS 0.200", MATERIAL REMOVED 0.125" AND REMAINING THICKNESS 0.075". REPAIRED AS PER EA 1-5710-112584, PART 1. REPAIR CLASSIFIED AS CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008030300111 20080303 00111 NM 2008 3 3 08FDEA00639 1 20080228 A 5753 SKIN DOUG MD11 MD11F 3023600 NM TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 LEFT WING INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT A ND TEST CARRIED OUT FOUND 'SATISFACTORY' AS PER AMM 27-50-22-5. 2 L 7 3 4F RT A22WE 2008030300114 20080303 00114 2008 3 3 WGEA200800032 4 20080221 A 3400 UNKNOWN ECLIPS EA500 ECLIPSEEA500 3350000 SW UNKNOWN E WGEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 146DJ 000058 DURING T/O ROLL, CAS MESSAGE AIRSPEED DISAGREE AT 45KTS. REFERENCE DAYJET WORK ORDER 1434, NR-00002. CHECKED FOR WATER IN THE PITOT DRAINS IAW EA500 AMM 34-10-00. NO WATER FOUND. FOUND CODE 764 - AIRSPEED MISCOMPARE. C/W FLIGHT ENVIRO MENT DATA ADJUSTMENT/TEST IAW EA500 AMM 34-10-00. SYSTEM TEST AND CHECKS GOOD AT THIS TIME. NO DEFECTS NOTED. 1 L 7 2 4J RT A00002AC 2008030300118 20080303 00118 NM 2008 3 3 HALA0800349 1 20080220 A 5530 STRUCTURE BOEING 717 717200 1383700 NM VERTICAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION ON VERTICAL STAB FWD LOWER L/E NUT PLATES (9EA). REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008030400006 20080304 00006 EU 2008 3 4 MALA080028 1 20080223 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 340B424 LT AFT COVE EMERGENCY LIGHT INOP, DISCOVERED DURING LC1. REMOVED AND REPLACED DEFECTIVE LIGHT ASSY 2LA005115-20. 2 L 7 2 4T RT A52EU 2008040800019 20080408 00019 SO 2008 4 8 2008F00009 1 20080319 A 3230 LANDING GEAR PIPER PA32 PA32RT300 7103215 SO NOSE COLLAPSED E K NONE O OTHER LD LANDING 1 SW 17 360SB 32R7885159 NOSE LANDING GEAR COLLAPSED AFTER LANDING BUT WHILE STILL MOVING UNDER ITS OWN POWER. 1 L 7 1 3O A3SO 2008040800030 20080408 00030 EA 2008 4 8 COMA0860192 1 20080323 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SO 01 786CA 7333 FLIGHT 5108 - RECEIVED FLAP FAIL MESSAGE ON FLAP SELECTION. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH SI-2-27I001 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION. FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2008040800037 20080408 00037 WP 2008 4 8 CLCA0308 1 20080326 A 5244 ACCESS DOOR DOUG DC10 DC1030 3023501 WP UNLOCKED A CLCA A UNSCHED LANDING O OTHER IN INSP/MAINT 1 SO 29 279AX N47816 UNABLE TO MAINTAIN CABIN ALTITUDES IN ALL MODES. CABIN ALT FOLLOWED AIRCRAFT TO 12000. 2 L 7 3 4F A22WE 2008040800049 20080408 00049 WP 2008 4 8 DHLA200800037 1 20080403 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 2 ENGINE FALSE ACTIVATION A DHLA E ENGINE SHUTDOWN N FALSE WARNING TX TAXI/GRND HDL 1 GL 05 873SJ 46091 POST FLIGHT NR 951, DURING LANDING ROLLOUT NR 2 ENGINE FIRE WARNING ACTIVATED. PERFORMED EMERGENCY CHECKLIST. DISCHARG ED BOTH FIRE BOTTLES AND DISCONNECTED NR 2 CSD. REMOVED AND REPLACED NR 2 ENG FIRE DET LOOP CONNECTOR ON PYLON. CLEAN PYLON CONNECTOR P1-7000, P1-7008, P1-7007. ALL PER WDM 26-1-1. OPS CHECKS SERVICEABLE ON GROUND, P/N 878238-02 AIRCRAF T WAS GROUNDED. 2 L 7 4 4F RT 4A25 2008040800061 20080408 00061 NM 2008 4 8 HNAA0800097 1 20080309 A 3350 OL3071BPEGL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST NR NOT REPORTED 1 EA 07 804EX 42523 42523 227 ONE RED EMERGENCY LIGHT AT FLOOR LEVEL EXIT IS OUT. RELAMPED FOURTH RED LIGHT SEGMENT, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2008040800062 20080408 00062 NM 2008 4 8 HNAA0800114 1 20080327 A 3350 603844 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 806EX 263 FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY, OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2008040800074 20080408 00074 SO 2008 4 8 FDKA200803134 1 20080327 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM RON CLT (0317 PHX LCL). EMERGENCY EXIT LIGHT ROW 12C INOP. MX RE-SECURED CONNECTION AT LIGHT ASSY, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008040800082 20080408 00082 SO 2008 4 8 C2XA08RI038 1 20080321 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 41104 145656 RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND EMERGENCY LIGHT SIGN NOT ILLUMINATING AT SEAT 3BC. MX REMOVED AND REPLAC ED NR 3 INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2008040800103 20080408 00103 SO 2008 4 8 C2XA08IA096 1 20080328 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14522 145383 IAH - FLIGHT 2856, THE CREW REPORTED TWO EMERGENCY EXIT LIGHTS TO BE INOPERATIVE IN THE CABIN CEILING. MAINTENANCE RESE T THE EMERGENCY LIGHTS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008040800114 20080408 00114 NM 2008 4 8 SWAA081737 1 20080331 A 3350 100031 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2008040800121 20080408 00121 WP 2008 4 8 WRLA2008037 1 20080307 A 5544 PANEL DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE RUDDER DAMAGED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 138WA 47844 DURING C-CHECK INSPECTION FOUND UPPER FWD RUDDER PANEL 376VL HAS 2EA SCREW HOLES ELONGATED. REPAIRED UPPER FWD RUDDER P ANEL 376VL SCREW HOLES PER ECRA 242NW-55-DC10-014 AND ECRA, 242NW-55-DC10-015. 2 L 7 3 4F 4 F A22WE E23EA 2008040800152 20080408 00152 NM 2008 4 8 SWAA081779 1 20080402 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 336, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040800191 20080408 00191 SO 2008 4 8 C2XA08IA098 1 20080331 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14991 145278 MCI - DURING MAINTENANCE INSPECTION, THE LEFT HAND OVERWING EMERGENCY EXIT MARKER WAS FOUND TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE NUMBER FIVE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008040900038 20080409 00038 NM 2008 4 9 AALA200800657 1 20080316 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 DFW - EMERGENCY LIGHT AT SEAT 25G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900048 20080409 00048 NM 2008 4 9 AALA200800644 1 20080315 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 612AA 24488 MIA - EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900058 20080409 00058 NM 2008 4 9 AALA200800637 1 20080314 A 2797 CONNECTOR BOEING 757 757223 1384957 NM TE FLAPS DAMAGED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 662AA 25296 AMA INFLIGHT T2466/14MAR SFO TO DFW - CREW REPORTED LEADING EDGE FLAP ASYMMETRY MESSAGE. LANDED AMA WITHOUT INCIDENT. FOUND LEFT WING CONNECTOR DAMAGED. REPLACED LEFT WING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900070 20080409 00070 NM 2008 4 9 HALA0800495 1 20080401 A 5310 BEAM BOEING 767 76733A 1385209 NM BS 870 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 587HA 33421 LEVEL 1 CORROSION ON THE INNER-PANEL TEE SECTION P/A 145T8629-2 AT LWR BEAM STA 870 RBL 9.5 TO LBL 9.5, CORROSION AROUND ANCHOR NUT FASTENERS. TEE SECTION REPLACED. 2 L 7 2 4F RT A1NM 2008040900077 20080409 00077 NM 2008 4 9 08FDEA01276 1 20080403 A 5347 AEA732515 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK SEAT TRACK INBOARD FLANGE AT STA 1481 TO STA 1515, X = -75 FOUND CORROSION. REPAIRED BY SECTIONAL REPLACEME NT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008040900080 20080409 00080 EU 2008 4 9 08FDEA01279 1 20080403 A 5340 A53980047211 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND A CLIP AT C 76, P 33-34 RT WITH NOT ENOUGH EDGE DISTANCE. REPAIR PERFORMED BY MANUFACTURING AND INSTALLING OF NEW CLIP IAW RAS/EFW9000026/2008 ISS A, APPROVED BY EA 6-5318-117152. 2 L 7 2 4F RT A35EU 2008040900092 20080409 00092 EU 2008 4 9 08FDEA01285 1 20080403 A 5755 A57771000004 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 4 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND DELAMINATION ON SPOILER NR 4 RT . DELAMINATION IS OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 276151. 2 L 7 2 4F RT A35EU 2008040900107 20080409 00107 WP 2008 4 9 08FDEA00734 1 20080305 A 5755 NRC6050502 SKIN DOUG MD10 MD1010F 3022112 WP NR 5 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 LT WING SPOILER NR 5 UPPER EXTERIOR INBD SIDE IS DELAMINATED (2 PLACES). TAP TESTED MARKED AREAS IAW DC/MD-10 SRM 51-61 -01; VOL II. NO DELAMINATION NOTED AT THIS TIME. REINSTALLED LT NR 5 SPOILER IAW MD-10-10 AMM 27-60-01-4. CLEARANCE AND OPS CHECKS GOOD IAW MD-10-10 AMM 27-60-01-4 AND MD-10-10 AMM 27-60-01-4. 2 L 7 3 4F RT A22WE 2008040900113 20080409 00113 NM 2008 4 9 AALA200800669 1 20080319 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 782AN 30003 JFK - EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900138 20080409 00138 WP 2008 4 9 AALA200800683 1 20080320 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 431AA 49343 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROW 29 TO AFT GALLEY INOPERATIVE. RESECURED BATTERY PACK FOR EMERGENCY LIGHTS A T OVERHEAD SEAT ROW 29 TO AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008040900143 20080409 00143 NM 2008 4 9 AALA200800693 1 20080321 A 3350 PBS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 344AN 33083 LAX - EMERGENCY LIGHTS AT SEAT ROWS 38HJ TO AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEA T ROWS 38HJ TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008040900167 20080409 00167 NM 2008 4 9 DLM88080544 1 20080403 A 5712 RIB DOUG MD88 MD88 3023688 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV A CRACK WAS FOUND ON RT WING LEADING EDGE RIB AT STA XRS=271. RIB WAS REPAIRED IAW SRM 57-06 BD FIG 801D. 2 L 7 2 4F RT A6WE 2008040900175 20080409 00175 NM 2008 4 9 QXEA20080336 1 20080329 A 5210 BOLT BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR HANDLE UNDERTORQUED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 412QX 4059 RDM- FRONT PASSENGER DOOR IS JAMMED CLOSED AND UNABLE TO BE OPENED. MAINTENANCE OPENED THE DOOR AND RETORQUED THE INNER HANDLE MOUNT BOLTS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008040900191 20080409 00191 NM 2008 4 9 2008UALA01857 1 20080401 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1600 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 AFT PIT FRAME INBOARD FLANGE DENTED AT BS 1600 AND STR 26L. CUTOUT DAMAGE. NO CRACKED NOTED. INSTALLED DOUBLER REPAIR . 2 L 7 2 4F 4 F RT A2NM E17NE 2008041000002 20080410 00002 NM 2008 4 10 NWAA081396310 1 20080220 A 5311 FRAME BOEING 747 747451 1384940 NM BS 2664 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING "M" CHECK, FOUND CRACK IN FRAME WEB AT BS 2664 LT WL 310. REPAIRED PER EA 63-211713. 2 L 7 4 4F RT A20WE 2008041000011 20080410 00011 EA 2008 4 10 MASA200800264 1 20080327 A 3510 OXYGEN MASK CNDAIR CL600 CL6002D24 1390016 EA COCKPIT UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 913FJ 15013 ASH FLT 2812 PHX-OKC. F/O OXYGEN MASK NOT SECURED. MX SECURED OXYGEN MASK. 2 L 7 2 4F RT A21EA 2008041000012 20080410 00012 NM 2008 4 10 MASA200800266 1 20080328 A 2910 731840 SPU DHAV DHC8 DHC8202 2809007 NM HYDRAULIC SYS MALFUNCTIONED A MASA O OTHER O OTHER CR CRUISE 1 SW 07 437YV 2278 437 ASH FLT 2950 PHX-GJT. NR 2 HYDRAULIC QUANTITY LOSS IN FLIGHT. AC DECLARED AND EMERGENCY AND DIVERTED TO GJT. CHANGED NR 2 SPU. 2 H 7 2 4T RT A13NM 2008041000014 20080410 00014 EA 2008 4 10 MASA200800269 1 20080328 A 5210 SEAL CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR DIRTY A MASA O OTHER O OTHER CR CRUISE 1 SW 07 513MJ 10111 ASH FLT 7331 ORD-SBN. MAIN CABIN DOOR HIGH PITCH NOISE IN FLIGHT. MX CLEANED & LUBED PASSENGER DOOR SEAL. 2 L 7 2 4F RT A21EA 2008041000023 20080410 00023 NM 2008 4 10 UPS08651944 1 20080321 A 5280 SKIN BOEING 767 76734AF 1385212 NM LT MLG DOOR PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 314UP 27742 INSPECTION TYPE:C LEFT MLG DOOR INNER SURFACE FOUND PUNCH HOLE AT O/B AREA AS MARKED. COMPOSITE REPAIR CARRIED OUT AS P ER HX RS#R-52-80-35973A AND UPS ENGINEERING FILE 767-32-20012 THE REPAIR PROCEDURE REFER SRM 51-70-05 PAR 5A (1) AND HX PROCESS CARD CONTROL SEQ AWC504651-1. 2 L 7 2 4F RT A1NM 2008041000031 20080410 00031 WP 2008 4 10 IXXA080011O 1 20080402 A 2612 899865 FIRE LOOP DOUG DC8 DC871F 302199D WP NR 1 NACELLE SHORTED A IXXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SW 11 820BX 90332 1253 46065 DURING CRUISE FROM KBFI TO KPDX AT FL160 NUMBER ONE ENGINE FIRE WARNING BELL AND LIGHT CAME ON. THE MASTER FIRE WARNING WOULD NOT SILENCE BELL. THE FIRE LIGHT AND BELL BECAME INTERMITTENT WHILE THE CREW RAN THE APPROPRIATE CHECKLIST. THE CREW SHUTDOWN NUMBER ONE ENGINE AND THE LIGHT STAYED ON. THE CREW FIRED ONE AGENT AND AFTER 30 SECONDS THE LIGHT AND BE LL WERE STILL ON, THE CREW FIRED THE SECOND AGENT AND THE LIGHT AND BELL EXTINGUISHED. THE CREW LANDED THE AIRCRAFT WIT HOUT INCIDENT. MAINTENANCE INSPECTED NUMBER ONE ENGINE INTERNALLY AND EXTERNALLY AND FOUND NO EVIDENCE OF FIRE. MAINTE NANCE CHECKED ALL FIRE LOOP AND FOUND TOP LOOP AT HOT SECTION SHORTED. MAINTENANCE REPLACED LOOP AND NUMBER ONE AND NUM 2 L 7 4 4F RT 4A25 2008041000032 20080410 00032 WP 2008 4 10 08FDEA01313 1 20080405 A 5347 60450018 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 MCD SEAT TRACK STA 1321 LBL 27 FOUND PITTING CORROSION REMOVED DAMAGED TRACK SECTION IAW 53-70-00. FABBED NEW SECTION O N TRAVELER T8/732807, T8/732808 AND T8/732809. LOCATED AND DRILLED AND INSTALLED NEW TRACK AND SPLICES IAW SRM 53-70- 00 AND SRM 53-21-01. 2 L 7 3 4F RT A22WE 2008041000034 20080410 00034 SO 2008 4 10 RAIA00803024 1 20080328 A 3297 CONNECTOR EMB 145 EMB145LR 3260212 SO NLG DIRTY A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 834HK 145269 FLT 8071 OMA - LANDING GEAR AIR/GROUND FAILURE MESSAGE ON THE EICAS. MAINTENANCE CLEANED THE NOSE LANDING GEAR PROXIMIT Y SWITCH CONNECTOR. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008041000038 20080410 00038 NM 2008 4 10 08FDEA01318 1 20080406 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK CARGO DOOR LOWER JAMB SPOOL FITTING NR 3 FOUND THIRD LAYER CRACK INDICATION AFTER BORE TO MAXIMUM 0.519". REMO VED AND REPLACED PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041000047 20080410 00047 EU 2008 4 10 08FDEA01323 1 20080407 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT LT MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 IT EXISTS AN OLD RAS/BAE.310/97 FOR A FOLDING NOSE REPAIR ON SLAT NR 1 LT. THE EXISTING REPAIR ARE NOT PERFORMED IAW R AS REPAIR PERFORMED BY PERFORMING SB A300-57-6067 ON SLAT NR 1 FOLDING NOSE, APPROVED BY EA 6-5742-117181. 2 L 7 2 4F RT A35EU 2008041000049 20080410 00049 SO 2008 4 10 RAIA00803025 1 20080328 A 3397 TERMINAL EMB 145 EMB145 3260210 SO CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 809HK 145187 PRE FLT 5511 - STL - EMERGENCY LIGHT AT LEFT OVERWING EXIT INOPERATIVE. MAINTENANCE INSPECTED AND FOUND A BROKEN TERMIN AL END. TERMINAL WAS REPAIRED AND THE SYSTEM, OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2008041000053 20080410 00053 EU 2008 4 10 08FDEA01328 1 20080407 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT RT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CHAFING MARK ON SLAT NR 1 RT LOWER SKIN. REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW RAS/FOK/004/2008 ISS D, APPROVED BY EA 6-5742-114858. 2 L 7 2 4F RT A35EU 2008041000056 20080410 00056 SO 2008 4 10 RAIA00803026 1 20080328 A 3350 CONTACT EMB 145 EMB145 3260210 SO CABIN OUT OF ADJUST A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 803HK 145077 PRE FLT 3517 - PIT - EMERGENCY LIGHT AT ROW 16 INOPERATIVE. MAINTENANCE ADJUSTED THE LAMP CONTACT. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2008041000057 20080410 00057 WP 2008 4 10 08FDEA01331 1 20080407 A 5330 AEA01121 SKIN DOUG DC10 DC1010F 3022111 WP BS 1305 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION FOUND ON UPPER FUSELAGE AT STA 1305 JAMB DOOR R NR 3 NUMBER 2 CRACK 2 INCHES LONG ON THE WE B IN POSITION LOWER REPAIRED FOR SRM 53-50-00 FIG 19 VOL I. 2 L 7 3 4F A22WE 2008041000059 20080410 00059 WP 2008 4 10 MWEA080049 1 20080330 A 2560 P4010021 BATTERY DOUG DC9 DC982 3022082 WP FLASHLIGHT DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 809ME 48071 POTABLE EMERGENCY FLASHLIGHT AT FORWARD PASSENGER DOOR IS INOPERATIVE. REMOVED AND REPLACED BATTERY. 2 L 7 2 4F A6WE 2008041000069 20080410 00069 EU 2008 4 10 08FDEA01339 1 20080327 A 5400 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU NR 1 NACELLE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 PYLON NR 1, PYRAMID HOLE WITH CORROSION (FWD RT). 2 L 7 2 4F RT A35EU 2008041000072 20080410 00072 NM 2008 4 10 USAA920080718 1 20080328 A 5313 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 23935 CLT - MAJOR REPAIR-C-2-NR O3C21853002/10, CORROSION ON STRINGER 27L AT BS 962.2. REMOVED DAMAGED STRINGER & INSTALLED S TRINGER SPLICE REPAIR IAW SRM 53-00-03 REPAIR 1. 2 L 7 2 4F RT A16WE 2008041000075 20080410 00075 EU 2008 4 10 USAA920080717 1 20080331 A 3350 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AW 76 FLT 363 - PHX - SMF - EEL - FAA RAMP CHECK. EMERGENCY LIGHTS INOP L1, R1, ROW 1, 2, 11 RT. MAINTENANCE REMOVED AND REP LACED THE BATTERY PACK AT L1 AND REPAIRED WIRING AT 11 RT. EMERGENCY LIGHTS OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 2008041000079 20080410 00079 2008 4 10 BB08044 4 20080328 A 2211 6228757105 COMPUTER BOEING 767 7672B7 1385107 NM AUTOPILOT SYS INOPERATIVE A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 256AY 40387 15 26847 MUC FLT 707 - MUC TO PHL. AFTER TAKEOFF, ALL AUTOPILOT SYSTEMS WERE INOPERATIVE. AFTER SEVERAL ATTEMPTS TO RESET, THE FLIGHT RETURNED TO MUC WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CENTER FLIGHT CONTROL COMPUTER. OPERATIONAL LY CHECKS OK. 2 L 7 2 4F RT A1NM 2008041000082 20080410 00082 WP 2008 4 10 NWAA081439883 1 20080407 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 671MC 47660 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EXTERIOR EMERGENCY FLOOD LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED BA TTERY PACK AND LIGHTS. RETURNED TO AN OPERATIONAL CONDITION. 2 L 7 2 4F RT A6WE 2008041000084 20080410 00084 EU 2008 4 10 08FDEA01344 1 20080408 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND ON LT WING ELONGATED HOLES DURING INSPECTION IAW SB 29-6058. REPAIR PERFORMED BY OVERSIZING THE HOLES AND BUSH IN STALLATION IAW DRAWING R571-50532 AND SB 29-6058, APPROVED BY RAS/BAE/1006287/2008 ISS A AND EA 6-2910-115253. 2 L 7 2 4F RT A35EU 2008041000087 20080410 00087 EU 2008 4 10 08FDEA01347 1 20080408 A 5542 A55471500026 SKIN AIRBUS 300 A300B4622R 3930312 EU RUDDER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND WATER INGRESS DURING THERMOGRAPHIC INSPECTION ON RUDDER RT SIDE. REPAIR PERFORMED BY REMOVING SKIN AND CORE, DRY T HE AREA, PERFORM REPAIR IAW SRM 51-77-10 IAW RAS/DAHAM/4024380/2008 ISS A, APPROVED BY EA 6-5540-115259. 2 L 7 2 4F RT A35EU 2008041000095 20080410 00095 EU 2008 4 10 08FDEA01354 1 20080408 A 5415 A54611024003 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CORROSION IN PYLON NR 2 REAR ATTACH FITTING. REPAIR PERFORMED IAW SB A300-54-6018 (REAM UP THE HOLE, CADMIUM PLAT ING), APPROVED BY EA 6-5451-114851. 2 L 7 2 4F RT A35EU 2008041000097 20080410 00097 NM 2008 4 10 SWAA081739 1 20080331 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041000098 20080410 00098 EU 2008 4 10 SIMA200809801 1 20080406 A 7700 5066T52G05 TORQUE SENSOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 240DS 340B240 GEE785486 ON FLIGHT 3767, CREW REPORTED ON TAKEOFF CTOT SET TO 100 PERCENT LEFT ENGINE TORQUE WENT TO 120 PERCENT. CREW REDUCED P ROP BLADE ANGLE AND TORQUE WAS DECREASED. ITT MAX WAS 852. CREW PERFORMED TORQUE MOTOR LOCKOUT PER AOM. AIRCRAFT REMO VED FROM SERVICE. PERFORMED TROUBLESHOOTING IN IAW SAAB WM 77-13-00 AND CT7 ENGINE MANUAL 72-00-00. REMOVED AND REPLAC ED TORQUE AND OVER SPEED SENSOR IAW CT7-9 MM 74-00-00. OPERATIONAL CHECK GOOD. ALSO PERFORMED OPERATIONAL CHECK OF CTO T IAW SAAB MM 71-00-00. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2008041000100 20080410 00100 EU 2008 4 10 08FDEA01356 1 20080408 A 5514 A55176100255 WEB AIRBUS 300 A300B4622R 3930312 EU ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 THS - DURING INSTALLATION OF RT THS TIP SOME HOLES FOUND MISDRILLED. REPAIR PERFORMED BY INSTALLAING NEW WEB WITH LOCK FASTENERS DAN7-6 IAW RAS/CASA/6544/2008 ISS B, APPROVED BY EA 6-5514-117183. 2 L 7 2 4F RT A35EU 2008041000107 20080410 00107 2008 4 10 Q2SA746005 4 20080405 A 3416 INDICATOR BOEING 747 747206B 1384856 NM ALTITUDE INACCURATE A Q2SA J A DUMP FUEL UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 EA 63 746SA 21111 ERRONEOUS ALTITUDE INFORMATION AND AIRSPEED FROM FLIGHT OFFICER'S INDICATORS. AT 11,000 FEET, 600 FEET DIFFERENCE. AT 240 KTS, IT WAS 30 KTS FAST. COMPLETED LEAK CHECK AND STATIC CHECK ON PITOT STATIC SYSTEM IN ACCORDANCE WITH AMM 34-11- 01. COULD NOT DUPLICATE MALFUNCTION. 2 L 7 4 4F RT A20WE 2008041000109 20080410 00109 NM 2008 4 10 SWAA081738 1 20080331 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041000112 20080410 00112 NM 2008 4 10 SWAA081745 1 20080330 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041000113 20080410 00113 NM 2008 4 10 SWAA081743 1 20080330 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008041000114 20080410 00114 NM 2008 4 10 SWAA081744 1 20080330 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041000124 20080410 00124 NM 2008 4 10 SWAA081753 1 20080327 A 5330 65C381921 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 445, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008041000126 20080410 00126 CE 2008 4 10 135258032308 1 20080323 A 3213 51411022 AXLE CESSNA 402 402C 207590R CE RT MLG CRACKED E HYIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 61 258PB 402C0336 ON TAXI AFTER LANDING, PILOT REPORTED RIGHT BRAKE "LOCKED UP". UPON FURTHER INSPECTION BY MAINTENANCE IT WAS FOUND THAT THE RIGHT MAIN LANDING GEAR AXLE WAS CRACKED. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN LANDING GEAR LOWER AXLE ASSE MBLY. AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 3O A7CE 2008041000129 20080410 00129 NM 2008 4 10 SWAA081756 1 20080331 A 5311 6545815 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 344, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041000130 20080410 00130 NM 2008 4 10 SWAA081755 1 20080331 A 5311 6546525 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041000133 20080410 00133 NM 2008 4 10 SB08017 1 20080402 A 3397 WIRE BOEING 737 737401 1384701 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 420US 23987 PIT - MAINTENANCE REPORTED THE CABIN EMERGENCY LIGHTS AT SEATS 6 THROUGH 10, LEFT-HAND SIDE, INOPERATIVE. MAINTENANCE R EPAIRED BROKEN WIRING FROM SIDEWALL AT FLOOR AREA. OPERATIONAL CHECK OF LIGHTS GOOD. 2 L 7 2 4F RT A16WE 2008041000137 20080410 00137 NM 2008 4 10 08FDEA01300 1 20080404 A 5347 53FX9394 SEAT TRACK BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 AFT CABIN SEAT TRACK, (STA 1130 - 1168) RBL 45 IS CORRODED REMOVAL AND INSTALLATION OF RBL 45 SEAT TRACK FROM STA 1130 - 1177 IS ON SNRM NR N00493/JPF LINE ITEM NR 66 AND 67. FABRICATION OF SEAT TRACK IS ON SNRM NR N00839. DRILLED, TREATE D AND PRIMED SEAT TRACK. REFERENCE FED EX DRAWING NR 53-FX939 AND SNRM NR N00839. CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008041000138 20080410 00138 NM 2008 4 10 08FDEA01301 1 20080404 A 5320 53FX939136 FLOOR SUPPORT BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 MAIN DECK FLOOR SUPPORT, BS 1166 - 1177, RBL 45, UPPER SURFACE HAS CORROSION AND VERTICAL FLANGE IS GOUGED. REMOVAL AND INSTALLATION OF FLOOR SUPPORT BETWEEN STA 1166 - 1177/RBL 45 IS ON SNRM NR N00493/JPF LINE ITEM NR 178 AND 179. FABRIC ATED FLOOR SUPPORT AND FLOOR SUPPORT FILLERS, LOCATED HOLES, TREATED AND PRIMED ALL PARTS. REFERENCE FED EX DRAWING 53F X939/ITEM NR -136, -38 AND -40. CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008041000141 20080410 00141 NM 2008 4 10 ASAA0852803 1 20080401 A 5610 5893543130 WINDOW BOEING 737 737890 1384527 NM COCKPIT FAULTY A ASAA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 02 558AS 35177 RIGHT FWD WINDOW HEAT OVERHEAT ILLUMINATED ACCOMPANIED BY POPPED C/B. REPLACED R1 WINDOW AND RESET C/B. 2 L 7 2 4F RT A16WE 2008041000142 20080410 00142 EU 2008 4 10 08FDEA01342 1 20080408 A 5740 A57661024 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION FINDINGS ON RT ASA ACTUATOR ATTACH FITTING UNDER BUSHING IN OUTER LUG REPAIR PERFORMED BY INCREASING THE HOLE DIAMETER, NDT FOR CRACK FREE AND INSTALLING A BUSH PER DRAWING A576-61546-200 AND A576-61024 IAW RAS/FOK/067/2008 ISS A, APPROVED BY EA 6-5756-117174. 2 L 7 2 4F RT A35EU 2008041000145 20080410 00145 WP 2008 4 10 08FDEA01308 1 20080404 A 5330 2024T3125C SKIN DOUG DC10 DC1030F 3023504 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 FWD CARGO CUT OUT DOOR AFT LOWER EDGE HAS TWO DENTS, MEASURED DENTS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01. REPAIRE D IAW SRM 53-50-00 FIGURE 8 SHEET 1 AND 2 MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008041000147 20080410 00147 WP 2008 4 10 08FDEA01310 1 20080404 A 5512 ALC744312 SKIN DOUG MD10 MD1010F 3022112 WP HORIZONTAL STAB GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT HORIZONTAL STABILIZER UPPER SKIN INBD SECTION FWD OF THE AFT SPAR IS GOUGED. REPAIRED IAW SRM 55-00-01 VOL I. 2 L 7 3 4F RT A22WE 2008041000153 20080410 00153 WP 2008 4 10 UPS08851950 1 20080328 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 CORROSION ON FLOOR PANEL AT STA 580 AND RBL 24. REPAIRED CABIN FLOOR PANEL AT STA 580 AND RBL 24 IAW SRM 53-02-03 FIG 10. 2 L 7 4 4F RT 4A25 2008041000156 20080410 00156 WP 2008 4 10 UPS08851956 1 20080402 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. 2 L 7 4 4F RT 4A25 2008040800149 20080408 00149 NM 2008 4 8 SWAA081775 1 20080402 A 3350 311500 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 288WN 36611 R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2008040800158 20080408 00158 NM 2008 4 8 SWAA081785 1 20080402 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008040800167 20080408 00167 NM 2008 4 8 SWAA081790 1 20080403 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 246LV 32507 L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008040800177 20080408 00177 NM 2008 4 8 SWAA081799 1 20080403 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 907, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008040800208 20080408 00208 NM 2008 4 8 SWAA081828 1 20080403 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 FUSELAGE SKIN CRACKED AT BS 500, STR 21R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008040900014 20080409 00014 NM 2008 4 9 HALA0800481 1 20080401 A 7500 CIRCUIT CARD BOEING 767 7673G5 1385126 NM PWA 4060 PW4060 52119 NE BLEED SYSTEM MALFUNCTIONED A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, EICAS L ENG BLEED OFF ILLUMINATED. T/S PER FIM 36 -10 00 CHECKED CONNECTORS AND SENSE LINES A T PRSOV, PRV, HPSOV AND FAMV NO TROUBLE FOUND RE-SEATED BLEED AIR CONTROL CARD RAN LEFT ENG PRSOV, OP CK GOOD PNEUMATICS , OP NORMAL NO FAULTS OR MESSAGES. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040900023 20080409 00023 EU 2008 4 9 TRBA2008037 1 20080402 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 29 342AT 345 MAIN PAX DOOR EMERGENCY STAIR LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP IAW MM NR 33-51-25. PERFORMED OPT CK IAW JI C NR 33-50-00. 2 H 7 2 4T RT A53EU 2008040900024 20080409 00024 NM 2008 4 9 AALA200800659 1 20080316 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 785AN 30005 DFW - EMERGENCY LIGHT AT SEAT ROW 30 LENS BROKEN. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 30. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900044 20080409 00044 NM 2008 4 9 AALA200800625 1 20080313 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT AT SEAT 23G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900086 20080409 00086 2008 4 9 HALA0800487 4 20080401 A 3460 FMC BOEING 767 767332 1382001 NM MALFUNCTIONED A HALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 596HA 23276 ETOPS SIGNIFICANT SYSTEM, ON TAKEOFF, F/O F/D QUIT, NO FMA, NO LAND 3 FLAG. COMPLETED FLT W/FO INST SOURCE SEL ON LEFT POSITION, ON APPROACH NO ILS OR LOC CAPTURE ON EITHER SIDE. RESET FMC 1 AND 2 C/B. FMC OPS CHECK OK PER MM 34-61-00. ILS OPS CHECK OK PER MM 34-31-00. OPS CHECK F/D OK PER MM 22-10-00. 2 L 7 2 4F RT A1NM 2008040900088 20080409 00088 NM 2008 4 9 HALA0800484 1 20080403 A 2131 CONTROLLER BOEING 767 7673G5 1385126 NM CABIN PRESSURE FAULTED A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 584HA 33466 ETOPS SIGNIFICANT SYSTEM, CABIN ALT AUTO 2 ON LOWER STATUS PAGE. FAULTED CONTROLLER LOW FLOW. RESET, BITE CHECK NORMAL IAW FIM 21-31-00, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008040900116 20080409 00116 NM 2008 4 9 AALA200800671 1 20080319 A 3210 BOLT BOEING 757 757223 1384957 NM LT MLG FAILED A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 697AN 26977 MIA - INFLIGHT T295/19MAR - CREW REPORTED LEFT MAIN LANDING GEAR DOOR INDICATION AFTER TAKEOFF. RETURNED TO MIA AND LAN DED WITHOUT INCIDENT. FOUND LEFT MAIN LANDING GEAR OUTBOARD BOLT BROKEN. REPLACED LEFT MAIN LANDING GEAR OUTBOARD BOLT . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900121 20080409 00121 NM 2008 4 9 AALA200800676 1 20080319 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 661AA 25295 DFW - EMERGENCY LIGHT AT SEAT 6E MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 6E. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900132 20080409 00132 NM 2008 4 9 AALA200800677 1 20080319 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 DFW - EMERGENCY LIGHT PUSH BUTTON AT FORWARD FIRST CLASS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT PUSH BUTTON AT FORWARD FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900137 20080409 00137 NM 2008 4 9 AALA200800682 1 20080319 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 DFW - EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900159 20080409 00159 NM 2008 4 9 AALA200800666 1 20080318 A 3397 WIRE BOEING 767 767323 1385205 NM EMERGENCY LIGHTS SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 359AA 24040 MIA - EMERGENCY LIGHTS AT SEAT ROWS 31H TO 41H INOPERATIVE. REPLACED SHORTED LIGHT AT 36H FOR EMERGENCY LIGHTS AT SEAT ROWS 31H TO 41H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008040900176 20080409 00176 NM 2008 4 9 QXEA20080338 1 20080328 A 2612 WARNING LIGHT DHAV DHC8 DHC8202 2809007 NM FIRE DETECTION INTERMITTENT A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 356PH 502 SEA - ON TAXI, THE FIRE DETECTION LIGHT WAS FLASHING AND THE FAULT "B" LIGHT ILLUMINATED WITH A FLASHING INDICATION. RE TURNED TO THE GATE AND PLACED THE SYSTEM ON MEL 26-1. AIRCRAFT RETURNED TO SERVICE. 4/5 MEL CLEARED BY PERFORMING A RE SISTANCE AND QUANTITY CHECK OF THE SYSTEM WIRING WITH NO DEFECTS NOTED. ALSO APPLIED SUPER CORR A TO ALL CONNECTORS REM OVED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008041000166 20080410 00166 EU 2008 4 10 M7K2008F00001 1 20080204 A 6220 350A31182703 FREQ ADAPTER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B 60037 NE MAIN ROTOR HEAD CRACKED A M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 817MH 1199 M2869 4125 DURING ROUTINE 100 HOUR INSPECTION, A CRACK IN THE BLUE BLADE ELASTOMER WAS FOUND ON THE T/E LWR IB SURFACE RADIATING FR OM THE INSPECTION BORE. THIS CRACK HAD REACHED THE MM LIMITATION OF 10MM IN TOTAL LENGTH. THIS IS A VERY COMMON FAILUR E FOR A PART WITH A NEWLY PUBLISHED 20000 HOUR LIVE LIMIT. THE ORIGINAL LIFE LIMIT WAS 3000 HOURS WHICH NONE OF THESE P ARTS HAVE EVER LASTED. MFG EXPLANATION WAS THAT THE LIMIT WAS FOR THE METAL COMPONENTS OF THE PART. THE ELASTOMER FORM ULATION OF THE ORIGINAL PN WHICH HAD BEEN REPLACED BY THE CURRENT PN ALMOST NEVER FAILED. MFG HAS BEEN NOTIFIED OF BOTH THESE DETAILS WITH NO ACTION TAKEN. (K) 1 G 7 2 3U 3 U H9EU E00054EN 2008041000171 20080410 00171 GL 2008 4 10 EVAC032708 2 20080313 A 7321 25490927 FUEL CONTROL BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL ENGINE MALFUNCTIONED E EVCA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CE 03 79AE 733 45436 CAE890683 REPORTED AS UNCOMMANDED TORQUE FLUCTUATION LEADING TO TORQUE EXCEEDANCE OF 134.7 PERCENT FOR 1 SECOND. FUEL CONTROL AND GOVERNOR REMOVED AND TESTED BY APPROVED REPAIR STATION. NO DEFECTS NOTED. 1 G 7 1 3U 3 U H2SW E1GL 2008041000178 20080410 00178 SO 2008 4 10 N93A01042008 1 20080401 A 2910 1159SCH2225 SHUTTLE VALVE GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU HYD SYSTEM MALFUNCTIONED E N93A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 13 487QS 1287 AFTER TAKEOFF, CREW RECEIVED 'CHK HYD QTY" CAS MESSAGE AND VERIFIED BY QUANTITY LEVEL BEING LOW. MAINTENANCE FOUND THAT HYDRAULIC SHUTTLE VALVE ACTUATED DURING GEAR BLOW DOWN ON PREVIOUS FLIGHT AND DID NOT FULLY RESEAT. 2 L 7 2 4F 4 F RT A12EA E25NE 2008041000182 20080410 00182 NE 2008 4 10 DXTA20082982 2 20080406 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT BIRD INGESTION E DXTA A UNSCHED LANDING C B F.O.D. SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 343QS 5600444 DURING CLIMB OUT AT 500 FEET, EXPERIENCED BIRD STRIKE TO LT ENGINE. CREW REPORTED A VERY LOUD BANG, FOLLOWED BY A COUPLE OF MINUTES OF SMOKE/ODOR IN CABIN. 2 L 7 2 4F 4 F RT A22CE E25EA 2008041000187 20080410 00187 CE 2008 4 10 DELR200800001 1 20080207 A 7932 OIL SYSTEM LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE7313A 01518 WP ENGINE LOW E DELA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 122LX 030 P85164 DURING CLIMB, SMELLED LIGHT SMOKE ODOR IN A/C. OIL PRESSURE LIGHT CAME ON IN FLIGHT CLIMBING THROUGH FL300, REMAINED ON FOR APPROX 1 MIN. ANALOG GAUGE SHOWED 25 PSI. PULLED POWER TO IDLE TO START S/D PROCEDURE AND EVENTUALLY OIL PRESSURE BE CAME NORMAL. WAS MONITORED CAREFULLY UNTIL LANDING AND REMAINED NORMAL. INSPECTED ENGINE AFTER LANDING AND FOUND NO OIL IN SIGHT GLASS.. 2 L 7 2 4F 4 F A10CE E6WE 2008041000191 20080410 00191 EA 2008 4 10 MASA200800277 1 20080331 A 5320 SPLICE CNDAIR CL600 CL6002D24 1390016 EA CROSSBEAM CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 938LR 15038 REPAIRED CROSSBEAM SPLICE CRACK AT FS 280.0. 2 L 7 2 4F RT A21EA 2008041000198 20080410 00198 NM 2008 4 10 MASA200800280 1 20080331 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 4 WORN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 988HA 426 RIGHT NR 4 FLAP TRACK WORN UPPER, LOWER, AND MID. REPAIRED FLAP TRACK. 2 H 7 2 4T RT A13NM 2008041000204 20080410 00204 CE 2008 4 10 20061085 1 20080328 A 5311 1294004475 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 496 S3L BENT A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 261GL UE261 FRAME SECTION AT FS 469 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 469 STRINGER 3L IAW SRM 51-40. P/N 129-40044-75. 2 L 7 2 4T 4 T RT A24CE E26NE 2008041000209 20080410 00209 NM 2008 4 10 CALA0800299 1 20080402 A 5310 6547957U3 WEB BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 46625 27529 AFT CARGO DOOR CUTOUT LOWER WEB CORROSION MARKED. REMOVED AND REPLACED WEB REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041000212 20080410 00212 NM 2008 4 10 SWAA081786 1 20080402 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 701GS 27836 DURING SCHEDULED HC1 CHECK, LEFT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F RT A16WE 2008041000214 20080410 00214 NM 2008 4 10 SWAA081788 1 20080402 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 769SW 30588 DURING SCHEDULED HC1 CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008041000215 20080410 00215 NM 2008 4 10 CALA0800300 1 20080308 A 5320 6545834U551 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11641 28902 INTERCOSTAL FWD WET AREA BETWEEN FLOORBEAM 312 AND 328 LBL 46 IS CRACKED AT CLIP NUT HOLE. REMOVED AND INSTALLED NEW IN TERCOSTAL FWD WET AREA BETWEEN FLOORBEAM 312 AND 328 LBL 46 IAW B737-500 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041000220 20080410 00220 CE 2008 4 10 VQMA02132008001 1 20080213 A 3411 CM29337 STATIC PORT CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP LEAKING E VQMA K NONE O OTHER IN INSP/MAINT 1 NM 03 651PW 9335 400 6500090 FOUND RT SIDE LOWER STATIC PORT SLIGHTLY LOOSE. REMOVED BOTH RT SIDE STATIC PORTS, CLEANED AREA ON INSIDE AND OUTSIDE O F AC. APPLIED PRIMER TO AFFECTED AREAS. INSTALLED (2) STATIC PORTS P/N-CM2933-7 ON RT SIDE OF AC WITH (8) CM3827AD-4 RIVETS. 2 L 7 2 4F 4 F A9NM E6WE 2008041000224 20080410 00224 NM 2008 4 10 2008UALA01866 1 20080401 A 3520 417T410633 MODULE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LAVATORY BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 655UA 25393 LAV 124 OXYGEN MASK COMPARTMENT DOOR BROKEN OFF AND MASK FELL DOWN. REPLACED PASSENGER OXYGEN MODULE. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT A1NM E24NE 2008041000232 20080410 00232 CE 2008 4 10 YADA032708001 1 20080327 A 3245 G195X6758 TUBE BEECH 1900 1900C 1154161 CE TIRE SPLIT E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 112AX 93 UC45 NOSE TIRE LOOSING AIR PRIOR TO DEPARTURE. REPLACED NOSE TIRE ASSY (FOUND INNER TUBE SPLIT ON CENTER SEAM .1250 INCH). THIS IS AN ADDITIONAL FAILURE OF A MFG INNER TUBE. THIS WAS A CANADIAN MANUFACTURED TUBE AND THE DEFECT WAS AT THE CENT ER SEAM. 2 L 7 2 4T RT A24CE 2008041000236 20080410 00236 CE 2008 4 10 DXTA20082975 1 20080331 A 2150 A/C PACK CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 900QS 7500123 STRONG ODOR COMMING FROM PACS UNABLE TO ISOLATE WHICH PACK SMELLS LIKE BURNING OFF OF CHEMICALS . 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008041000245 20080410 00245 NM 2008 4 10 2008UALA01891 1 20080402 A 3397 CONNECTOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 795UA 26927 EMERGENCY ESCAPE PATH LIGHT (BOTH) AT SEAT 1E ARE INOP. FOUND LOOSE CONNECTION UNDER SEAT. SECURED CONNECTION. AC OK FO R SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008041000248 20080410 00248 SO 2008 4 10 GUUA03250801 1 20080325 A 3260 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE MLG OUT OF ADJUST A GUUA O OTHER J WARNING INDICATION CL CLIMB 1 SO 29 282AS 120226 FLIGHT:5201, AFTER TAKEOFF WITH LANDING GEAR UP THE RT MAIN GEAR (A) LIGHT ILLUMINATED. CONTINUED, LANDED WITHOUT INCID ENT. ADJUSTED (A) SYSTEM LOWER DOWNLOCK PROXIMITY SWITCH. 2 L 7 2 4T 4 T RT A31SO E20NE 2008041000253 20080410 00253 CE 2008 4 10 GUUA03300801 1 20080330 A 3260 404EN16 DOWNLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG FAILED A GUUA O OTHER N FALSE WARNING AP APPROACH 1 SO 29 17541 UE203 FLIGHT: 9164, DURING APPROACH, LANDING GEAR INDICATED DOWN AND LOCKED (3) GREEN. HOWEVER, FLAPS WOULD NOT EXTEND BEYOND 17 DEGREES WITHOUT GEAR WARNING HORN SOUNDING. UPON LANDING THE GEAR HANDLE LIGHT ILLUMINATED. GEAR HANDLE LIGHTS AND GEAR HORN WILL NOT EXTINGUISH OR SILENCE. REPLACED RT MLG DOWNLOCK SWITCH. 2 L 7 2 4T 4 T RT A24CE E26NE 2008041000254 20080410 00254 CE 2008 4 10 20061086 1 20080328 A 5311 12944004473 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 482 S3L BENT A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 261GL UE261 FRAME SECTION AT FS 482.75 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 482.75 STRINGER 3L IAW SRM 51-40. P/N 129-440044-73. 2 L 7 2 4T 4 T RT A24CE E26NE 2008041000287 20080410 00287 NM 2008 4 10 2008UALA01916 1 20080402 A 2560 BATTERY BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FLASHLIGHT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 FLASHLIGHT AFT CABIN INOP NOT BLINKING. FAULTY BATTERY. REPLACED BATTERY OPS CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008041000292 20080410 00292 NM 2008 4 10 2008UALA01921 1 20080403 A 3350 60243 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 594UA 28145 EEL LIGHT STRIP INOP AT MID AFT LAV. REPLACED EEL STRIP. OP CHKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041000298 20080410 00298 NM 2008 4 10 2008UALA01928 1 20080404 A 5753 PANEL BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE T/E FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 798UA 26928 WEAR WAS FOUND ON THE PANEL OF THE RT WING T/E OUTBOARD FLAP UPPER SURFACE NEAR MID POINT L=50". DID NDT INSP PER NDT M ANUAL PART1. 51-01-01 FIG 9, NO DELAMINATION. REPAIRED REF 777EN-57-0031-01, TOUCH-UP PAINT REF AMM 51-21-10P701.AC OK F OR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008041000299 20080410 00299 NM 2008 4 10 2008UALA01929 1 20080404 A 5753 PANEL BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE T/E FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 798UA 26928 WEAR WAS FOUND ON THE PANEL OF THE RT WING T/E OUTBOARD FLAP UPPER SURFACE, O/B END L=35". DID NDT INSP PER NDT MANUAL PART1. 51-01-01 FIG 9, NO DELAMINATION. REPAIRED REF 777EN-57-0031-01, TOUCH-UP PAINT REF AMM 51-21-10P701.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008041100002 20080411 00002 NM 2008 4 11 2008UALA01889 1 20080402 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 3E DETACHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 EEL LIGHT AT SEAT 3E HAS BEEN RIPPED OFF. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008041100004 20080411 00004 EU 2008 4 11 08FDEA01305 1 20080403 A 5322 A5397318022200 SHEAR TIE AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FOUND BULK PIT, FWD SIDE FR 67 S54L , HAS SURFACE CORROSION. REMOVED CORROSION IAW SRM 51-74-10; REMOVED CLIP IAW SRM 5 1-40-21 CHECKED LIMITS IAW SRM 51-31-20 AND FOUND TO BE WITHIN LIMITS IAW SRM 53-10-00; ALODINED IAW SRM 51-21-10 AND PR IMED AND PAINTED IAW SRM 51-23-10; RECIEVED NEW CLIP AND INSTALLED IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008041100011 20080411 00011 EA 2008 4 11 A6WA200840134 1 20080219 A 5230 PLATE CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 FOUND CARGO DOOR SCUFF PLATE IS CRACKED. REPLACED IAW SRM 51-41-02 AND AMM 53-60-31. (M) 2 L 7 2 4F RT A21EA 2008041100050 20080411 00050 EA 2008 4 11 A6WA200840228 1 20080319 A 3000 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE SYS ILLUMINATED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 412AW 7582 AFTER TAKEOFF RECEIED ANTI-ICE DUCT WARNING MESSAGE. COMPLIED WITH QRH, MESSGE PERSISTED ON SYNOPTIC PAGE, SHOWS LT WIN G RED. (M) 2 L 7 2 4F RT A21EA 2008041100052 20080411 00052 NM 2008 4 11 GTIA0800046 1 20080311 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 502NK 2433 FLOOR SUPPORT Y254 FROM FR 66 THROUGH FR 68 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT Y254 FROM FR 66 THROUGH FR 68. 2 L 7 2 4F RT A28NM 2008041100054 20080411 00054 NM 2008 4 11 DHL2008753516 1 20080324 A 2810 VENT BOEING 727 727223 1384074 NM LT WING TANK CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 L/WING TANK VENT TUBES CHAFED, WS 519, 546, 601, 629, AND 656. ACCOMPLISHED BLEND OUT AT CHAFED AREAS, FABRICATED 5 DOU BLER REPAIRS, AND INSTALLED AS PER ASTAR AIR CARGO EVA: B228-00050 REV IR DATED 3/13/08 AND COTNEY AEROSPACE ED: EDAF2 8-1 REV IR DATED 3/12/08, AT ALL LISTED LOCATIONS. 2 L 7 3 4F A3WE 2008041100056 20080411 00056 NM 2008 4 11 DHL2008753514 1 20080314 A 5720 ANGLE BOEING 727 727223 1384074 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 L/WING FIXED L/E VERT SPT ANGLE CRACKED, LWR END, AT WBL 92. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE FROM 7075T6, . 063 INCH BY 7.25 INCH BY 2.5 INCH, AND INSTALLED PER B727 SRM 51-10-1, 57-10-2 FIG 3, AND 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2008041100057 20080411 00057 NM 2008 4 11 DHL2008753515 1 20080302 A 5754 ANGLE BOEING 727 727223 1384074 NM KRUEGER FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 NR 2 K-FLAP ACTUATOR I/B MOUNT ANGLE CRACKED, AT WS 236.2. REMOVED, FABRICATED NEW WEB FROM 7075T6, .063 INCH BY 11 INC H BY 7.5 INCH, AND INSTALLED PER B727 SRM 57-50-2 FIG 1 AND 51-30-2. 2 L 7 3 4F A3WE 2008041100059 20080411 00059 SO 2008 4 11 SMIA200810002 1 20080405 A 5320 14522178005 SILL EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 831AE 145616 DURING A MBV INSP, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED CORRODED CENTER SILL AND INSTALLED NE W SILL. REPAIR DONE IAW EMBRAER SRM (SRM 145/1142 REV 38) CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008041100060 20080411 00060 SO 2008 4 11 SIMA200810001 1 20080408 A 3350 2013BR BATTERY EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHT DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 848AE 145710 ON 3197, FLIGHT CREW REPORTED MAIN ENTRANCE EMERGENCY EXIT SIGN ABOVE FASTEN SEAT FAILS TO ILLUMINATE AND EXIT SIGN ABOV E FLIGHT ATTENDANT STATIONS FAILS TO ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 EMERGENCY BA TTERY IAW EMB 140 AMM 33-50-04. OPERATIONAL CHECK GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008041100063 20080411 00063 NM 2008 4 11 08FDEA01362 1 20080409 A 5320 65196046 WEB BOEING 727 727227 1384078 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 MAIN DECK FLOOR SHEAR WEB IS CORRODED/MISDRILLED, BS 1130-1177, RBL 16-64, WL 208. REMOVED CORRODED/MISDRILLED RT SHEAR WEB. RECEIVED NEW SHEAR WEB, DRILLED AND INSTALLED. REFERENCE SRM 51-30-2/PAGE NR 2 CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008041100064 20080411 00064 EU 2008 4 11 MALA080056 1 20080410 A 5753 RIB SAAB SF340 340B 7860101 EU TE FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 445XJ 340B445 RT FLAP, AFT COVE FAIRING RIB IS CRACKED. REPLACED RT FLAP AFT COVE FAIRING RIB P/N 7257840-082 IAW SRM 51-40-23. REMO VED AND REPLACED TURTLE BACK FAIRING TO FACILITATE REPAIR IAW SRM 51-40-23. RT FLAP ASSEMBLY REMOVED AND INSTALLED TO F ACILITATE REPAIR PER AMM 27-51-30. FUNCTION TESTS GOOD. FROM CONTINUATION CARD 085349. REMOVED FLAP (RT) TO FOM. REI NSTALLED RT FLAP IAW AMM 27-51-30. FUNCTION CHECKS GOOD. COMPLY WITH FLAP RIGGING CHECKS IAW AMM 27-51-00. C/W FLAP R IG AND FUNCTION CHECKS IAW AMM 27-51-00. TESTS GOOD. RT FLAP AFT COVE FAIRING RIB IS CRACKED. REPLACED RT FLAP AFT CO VE FAIRING RIB P/N 7257840-082 IAW SRM 51-40-23. REMOVED AND REPLACED TURTLE BACK FAIRING TO FACILITATE REPAIR IAW SRM 2 L 7 2 4T RT A52EU 2008041100067 20080411 00067 EA 2008 4 11 A6WA200840230 1 20080319 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A A6WA O OTHER J WARNING INDICATION LD LANDING 1 GL 31 421ZW 7346 FLAPS FAILED OCCURRED ON APPROACH TO PHL, FLAPS FAILED AT 20 DEGREES, QRH PROCEDURE COMPLIED WITH OPS CHECK GOOD. COMPL IED WITH RESET PER SUPP 98-018B, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2008041100068 20080411 00068 EA 2008 4 11 A6WA200840177 1 20080310 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA FALSE ACTIVATION A A6WA O OTHER N FALSE WARNING LD LANDING 1 GL 31 417AW 7610 STAB AND MACH TRIM CAUTION IN FLIGHT. AUTOPILOT PITCH TRIM MESSAGE IN FLIGHT. PERFORMED OPS CHECK OF STAB SYSTEM, NO F AULTS NOTED. INTERROGATED HSTCU REF 27-41-00, NO FAULTS NOTED. (M) 2 L 7 2 4F RT A21EA 2008041100069 20080411 00069 EA 2008 4 11 A6WA200840248 1 20080227 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH SEIZED A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 410AW 7490 FAILURE OF FUNCTIONAL TEST OF CREW ESCAPE HATCH, OUTER HANDLE SEIZED DUE TO CORROSION, DURING C-CHECK. CREW ESCAPE HATC H OUTER HANDLE REPLACED. (M) 2 L 7 2 4F RT A21EA 2008041100070 20080411 00070 NM 2008 4 11 08FDEA01363 1 20080409 A 5347 AEA732523 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK SEAT TRACK FLANGE AT STA 1500, X = -8 FOUND CORROSION AT UPPER SURFACE. REPAIRED BY SECTIONAL SEAT TRACK REPL ACEMENT PER SRM 53-70-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041100071 20080411 00071 NM 2008 4 11 08FDEA01364 1 20080409 A 5347 AEA732523 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK SEAT TRACK FLANGE BELOW FLOOR PANEL NR 263EF AT STA 1361, X = 8 FOUND CORROSION AT LOWER SURFACE. CORROSION R EMOVED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. ORIGINAL MATERIAL T HICKNESS = 0.080", REMAINING THICKNESS = 0.075" AND MATERIAL REMOVED = 0.005". REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100. 2 L 7 3 4F RT A22WE 2008041100072 20080411 00072 NM 2008 4 11 08FDEA01365 1 20080409 A 5347 AEA732523 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK SEAT TRACK FLANGE BELOW FLOOR PANEL NR 271AF AND NR 271BF AT STA 1485 TO STA 1531, X = 8 FOUND CORROSION AT U PPER SURFACE AT 2 LOCATIONS. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 1431 TO STA 1531, X = 8 AS PER SRM 5 3-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041100076 20080411 00076 EA 2008 4 11 A6WA200840252 1 20080327 A 3010 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE SYSTEM MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 31 450AW 7823 RECEIVED LEFT AND RIGHT WING ANTI-ICE CAUTION MESSAGES, IN STANDBY RECEIVED LEFT AND RIGHT WING ANTI-ICE CAUTION MESSAGE S INTERMITTENTLY. LANDING WEIGHT 44,000 LBS. REMOVED AND REPLACED ANTI-ICE CONTROL PANEL IAW 20-12-21, OPS CHECK GOOD. AVIONICS REPORTS SWITCH P/N 66AT300-1 IDENT S2HA IS BAD. (M) 2 L 7 2 4F RT A21EA 2008041100078 20080411 00078 EA 2008 4 11 A6WA200840145 1 20080220 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 CRACK FOUND ON CARGO BAY FLOOR SILL FS 574 LBL 45 UNDER BRACKET RETAINER. NEW UNDER BRACKET RETAINER INSTALLED IAW CR J REO 601R-53-61-690 REV D. (M) 2 L 7 2 4F RT A21EA 2008040900099 20080409 00099 NM 2008 4 9 08FDEA01293 1 20080403 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 MAIN CARGO COMPARTMENT, CORROSION ON SEAT TRACK FORM STA 700-720 BL 0. REMOVED SEAT TRACK OUT LIMITS BTW STA 600-720 BL 0 IAW SRM 51-30-2. FABRICATED, LOCATED, AND DRILLED NEW SEAT TRACK IAW SRM EA-01-049 AND SRM 53-10-5 FIG 7. TREATED A ND PRIMED IAW SRM 51-10-2. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008040900108 20080409 00108 WP 2008 4 9 AALA200800688 1 20080321 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AA 49271 LGA - EMERGENCY FLASHLIGHT AT AFT SERVICE DOOR HAS BROKEN STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008040900109 20080409 00109 WP 2008 4 9 AALA200800689 1 20080321 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 955U 49427 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 29D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD SEAT 29D. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008040900112 20080409 00112 NM 2008 4 9 AALA200800668 1 20080319 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 782AN 30003 JFK - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900124 20080409 00124 NM 2008 4 9 DLM88080531 1 20080403 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV CORROSION WAS FOUND ON RIGHT CUSP WEB AT STA Y=277. CUSP WEB WAS REPAIRED IAW DOUGLAS DWG SG09530003. 2 L 7 2 4F RT A6WE 2008040900146 20080409 00146 SO 2008 4 9 SWIA200819430 1 20080331 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCONNECTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 292UX 120292 FLT 5544 - EMERGENCY LIGHT TRACK LIGHT IS INOP. RESECURED WIRING AT LIGHT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008040900148 20080409 00148 EA 2008 4 9 SWIA200819432 1 20080401 A 3231 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 403SW 7028 FLT 2555 - RECEIVED A NOSE DOOR OPEN MASTER WARNING. REPLACED NOSE DOOR SELECTOR VALVE AND CHECK VALVE PER AMM 33-22-20 . OPS CHECK GOOD, P/N 750006000, S/N OFF 1640. 2 L 7 2 4F RT A21EA 2008040900149 20080409 00149 SO 2008 4 9 SWIA200819433 1 20080402 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS LEAKING A SWIA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 07 223SW 120291 FLT 5423 - WHEN FLAPS WERE SELECTED TO 25 DEGREES, RECEIVED A FLAPS MESSAGE FOLLOWED BY LOSS OF BLUE HYDRAULIC SYSTEM FL UID. REPLACED THE RIGHT NACELLE ACTUATOR IAW AMM 27-50-08. OPS AND LEAK CHECKS GOOD, P/N: 343100-1001 S/N OFF: 0200. 2 L 7 2 4T RT A31SO 2008040900154 20080409 00154 2008 4 9 SWIA200819438 4 20080401 A 3417 ADC CNDAIR CL600 CL6002C10 1390015 EA NR 2 FAULTY A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 772SK 10235 FLT 6064 - FIRST OFFICERS ALTIMETER AND VSI IS FLUCTUATING WHILE IN FLIGHT. REPLACED NR 2 ADC IAW CRJ 700 MM 34-13-01. OPS CHECK GOOD, P/N 822-0372-436, S/N OFF 21VTY. 2 L 7 2 4F RT A21EA 2008040900156 20080409 00156 NM 2008 4 9 DLM88080539 1 20080403 A 5320 FLOOR SUPPORT DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, A CRACKED SUPPORT WAS FOUND FOR CABIN FLOOR PANEL 927A. SUPPORT WAS REPAIRED IAW ER/A 466354-14. 2 L 7 2 4F RT A6WE 2008040900160 20080409 00160 WP 2008 4 9 IXXA08SMN082S 1 20080215 A 5340 FITTING DOUG DC8 DC871F 302199D WP BS 879 L18R CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FRAME FITTING CRACKED AT STATION 879.000 LONGERON 18 RIGHT TO LONGER ON-19 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED FITTING. PERFORMED NDT INSPECTION. NO CR ACK NO CORROSION FOUND. PERFORMED STOP HOLE ON CRACK END. FABRICATED SPLICE ANGLE, FILLERS. PERFORMED HEAT TREATMENT TO REPAIR PARTS AS NEEDED. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IA W FAA FORM 8110-3 NUMBER 08086 DATED 02/27/08, DRAWING ED 4702 DATED 02/09/08, DC8 51-1-20D, DC8 NDT SPM PART 06-10-01-0 01, DC8 SRM 51-1-1 PAGES 1, 13, 17, ATI REPAIR SPECIFICATION 2003-05, DRAWING DOUGLAS NUMBER 3779874 AND 3779978, DRAWIN 2 L 7 4 4F RT 4A25 2008040900182 20080409 00182 NM 2008 4 9 QXEA20080355 1 20080406 A 6123 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM PROPELLER MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 430QX 4163 LAX- FLIGHT 2448 - DURING TAKEOFF ROLL, AUTO-FEATHER SYSTEM FAILED TO ARM. ABORTED TAKEOFF AT 80 KNOTS AND RETURNED TO THE GATE. MAINTENANCE FOUND FAULT CODES 402B AND 494 A/B. PERFORMED PEC FAULT CODE CLEARING PROCEDURE. OPERATIONAL CH ECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008040900183 20080409 00183 NM 2008 4 9 2008UALA01852 1 20080402 A 5530 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE VERTICAL STAB WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 CROWN AREA DORSAL FIN LANDING AT BS 867-883 WORN AT RBL 1-4. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND INSTALLED EXTER NAL DOUBLER AND STRAPS. REPAIR CONSISTED OF 0.050 INCH DOUBLER FROM BS 857 TO BS 907 FROM STRINGER S-2L TO S-2R. INSTA LLED WEAR STRIPS ON DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050500204 20080505 00204 NM 2008 5 5 DL76L080645 1 20080428 A 2530 COFFEEMAKER BOEING 767 767332 1382001 NM CABIN SHORTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 179DN 25144 REAR COFFEEMAKER ON RIGHT SIDE EMITTED SPARK AND SMOKE WHEN ACTIVATED. SMOKE DISSIPATED SHORTLY AFTER. PULLED REAR COF FEEMAKER AS PER INSTRUCTIONS FROM ATL MTC. THERE WAS A SHORT CIRCUIT BECAUSE OF WATER. CB TRIP RESET A BREWED OK. PLS OBSERVE NEXT FLIGHT. 2 L 7 2 4F RT A1NM 2008040900189 20080409 00189 NM 2008 4 9 2008UALA01855 1 20080402 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 STRUCTURE AT E/E COOLING EXHAUST DUCT IS INADEQUATE. MAJOR REPAIR ACCOMPLISHED: REMOVED EXISTING REPAIR. CUTOUT DAMAG E ON AFT SIDE OF E/E COMPARTMENT EXHAUST DUCT. ACCMP'D NDT OF OPEN HOLES AND FOR CRACKS. FABRICATED AND INSTALLED EXTE RNAL DOUBLER FROM BS 360-400. ACCMP PREVENTATIVE MOD AT RADIO ALTIMETER ANTENNA LOCATIONS AT BS 410, 430 AND 450. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040900193 20080409 00193 NM 2008 4 9 HALA0800501 1 20080407 A 4940 211734219 ECU BOEING 767 7673G5 1385126 NM APU MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 584HA 19555 19555 24258 ETOPS SIGNIFICANT SYSTEM, APU SHUT DOWN AT THE GATE. REMOVED AND INSTALLED APU ECU PER MM 49-61-05. OPS CK GOOD. 2 L 7 2 4F RT A1NM 2008041100079 20080411 00079 EA 2008 4 11 A6WA200840164 1 20080228 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 INTERCOSTAL AT FS 484 INBOARD CLIP AT RBL 27 IS CRACKED. REPLACED. (M) 2 L 7 2 4F RT A21EA 2008041100080 20080411 00080 EA 2008 4 11 A6WA200840166 1 20080304 A 5540 DIAPHRAGM CNDAIR CL600 CL6002B19 1900309 EA RUDDER MISSING A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 RUDDER LOWER CLOSURE RIB IS MISSING CLOTH DIAPHRAGM. REPAIRED IAW CRJ 200 REO 601R-55-41-018 REV A. (M) 2 L 7 2 4F RT A21EA 2008041100081 20080411 00081 EA 2008 4 11 A6WA200840167 1 20080302 A 5410 STRIP CNDAIR CL600 CL6002B19 1900309 EA NOSE COWL WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 RIGHT NOSE COWL UPPER DOOR AFT STRIP FOUND WORN. REPAIRED IAW CRJ 200 CMM 71-14-01-300-815- A01. (M) 2 L 7 2 4F RT A21EA 2008041100085 20080411 00085 NM 2008 4 11 070191 1 20080403 A 3110 36005700 SWITCH DOUG MD88 MD88 3023688 NM SMOKE A WX0A D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 19 403NV 49764 FLT 552, FLIGHT DECK PERSONNEL OBSERVED VISIBLE SMOKE FROM THE OVERHEAD PANEL DURING TAXI. THE CREW RETURNED TO THE GAT E AND MAINTENANCE DEPARTMENT PERSONNEL WERE NOTIFIED. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE OVERHEAD PANEL AND DETERMINED THE IGNITION ROTARY SWITCH WAS DEFECTIVE. REPLACING THE SWITCH AND PERFORMING A SYSTEM OPERATIONAL CHECK. SYSTEM CHECK WAS NORMAL AND THE ACFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008041100088 20080411 00088 NE 2008 4 11 DLM88080565 2 20080407 A 7230 COMPRESSOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE STALLED A DALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 922DL 43209 49646 725867 POSSIBLE COMPRESSOR STALL LT ENGINE ON TAKEOFF ROLL, REJECTED TAKEOFF ROLL AT 75 KTS. MTC IN PROGRESS REPLACING LT ENGI NE. 2 L 7 2 4F 4 F RT A6WE E9NE 2008041100089 20080411 00089 NM 2008 4 11 DL757080567 1 20080408 A 5330 146N35317 SKIN BOEING 757 757232 1384965 NM BS 1510 S28R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 644DL 23998 DURING HMV AT SAA, CORROSION WAS FOUND ON THE EXTERNAL SKIN AT STA 1510 BETWEEN S-28R AND S-29R WHERE AN AIRPHONE ANTENN A HAD PREVIOUSLY BEEN MOUNTED. SINCE THE ANTENNA IS NO LONGER USED, THE CORRODED SKIN WAS CUT OUT AND AN EXTERNAL REPAI R DOUBLER WAS INSTALLED PER BOEING REPAIR INSTRUCTIONS. 2 L 7 2 4F RT A2NM 2008041100090 20080411 00090 NM 2008 4 11 DLM88080568 1 20080408 A 2197 CONNECTOR DOUG MD88 MD88 3023688 NM TEMP CONTROLLER BROKEN A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 925DL 4117 49712 TAIL COMPT TEMP HI MSG FOUND RT TEMP CONTROL VLV FULL HOT WHEN TEMP CONTROL DECREASED/MSG WENT AWAY TRIED TO WARM CBN TA IL TEMP HI MSG ON AGAIN. QRH DIRECTED HP BLEED OFF. FOUND DUCT HOSE BLOWN OFF TEMP CONTROL VLV. ALSO FOUND ELECT CONN BROKEN. REMOVED AND REPLACED TEMP CONTROLLER VALVE. OPS/LK CKS OK. ALSO FOUND TAIL COMPT TEMP SENSOR FLAPPER DOOR CL OSED CLEANED SAME. REPLACED BLOWN DUCT RAN ENG AT PWR PRESSURIZED, A/C NO LKS NOTED. OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2008041100092 20080411 00092 NE 2008 4 11 DL76L080570 2 20080408 A 7210 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 187DN 63974 27582 724416 DEBRIS FOUND IN OIL FILTER DURING ROUTINE REPLACEMENT. DEBRIS DETERMINED TO BE ALUMINUM GEARBOX MATERIAL. REQUIRES ENG INE CHG PER PROP ENGINEERING (GEARBOX UNAVAIL). 2 L 7 2 4F 4 F RT A1NM E24NE 2008041100093 20080411 00093 NM 2008 4 11 DLM88080571 1 20080407 A 5523 SKIN DOUG MD88 MD88 3023688 NM RT ELEVATOR TAB DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 962DL 49981 DURING HMV, DENTS WERE FOUND ON LOWER AND UPPER SKIN OF RT ELEVATOR GEARED TAB. TAB WAS REPAIRED IAW SRM 51-70-2D. 2 L 7 2 4F RT A6WE 2008022800228 20080228 00228 NM 2008 2 28 SWAA080973 1 20080221 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND RT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 2008022800234 20080228 00234 NM 2008 2 28 SWAA080978 1 20080221 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 516D, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008022800259 20080228 00259 NM 2008 2 28 KCSA081115 1 20080224 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE SKIN DAMAGED AT BS 500, STR 46L. 2 L 7 4 4F RT A20WE 2008022800272 20080228 00272 EU 2008 2 28 08FDEA00548 1 20080121 A 5743 A2757038000400 TRUNNION AIRBUS 310 A310222 3930315 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 LT WING, FLAP OUTBD NR 4 TRUNNION WITH SPOTS OF CORROSION AND EXCESSIVE WEAR. TRUNNION NR 4 LT WAS REPAIRED IN ACCORDAN CE WITH CMM 57-53-12. 2 L 7 2 4F RT A35EU 2008022800273 20080228 00273 EA 2008 2 28 TRAX200800249 1 20080212 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 901EV 7616 LT EMERGENCY LIGHT BURNED OUT. 2 L 7 2 4F RT A21EA 2008022800280 20080228 00280 WP 2008 2 28 UPS08851679 1 20080109 A 5320 561229857 FINGER DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 COCKPIT STA -38 RBL 14, SUBFLOOR FINGER DOUBLER BULGING. REPAIRED COCKPIT SUBFLOOR AT STA -38 RBL 14 IAW EA 008-5320-01- A1265. 2 L 7 4 4F RT 4A25 2008022800327 20080228 00327 NM 2008 2 28 DL76G080220 1 20080217 A 3150 285T025921 MODULE BOEING 767 767332 1382001 NM M620 FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 171DZ 29690 ATB - TAKEOFF WARNING SOUNDING IN FLIGHT. 2 L 7 2 4F RT A1NM 2008022800353 20080228 00353 NM 2008 2 28 SWAA081016 1 20080224 A 5523 6959227 BUSHING BOEING 737 7375H4 138449D NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, LT ELEVATOR TAB NR 2 HINGE FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 2 HINGE BUSHING PER MM. 2 L 7 2 4F RT A16WE 2008022800357 20080228 00357 NM 2008 2 28 08FDEA00570 1 20080222 A 5320 65239463 THRESHOLD BOEING 727 727227 1384078 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 AFT ENTRY DOOR THRESHOLD HAS AREAS OF DAMAGE (BOTH BULLNOSE PIECES CRACKED) PARTS OF THRESHOLD SENT TO BE FABRICATED AND HEAT TREATED IN SHOP, 8130-3 TRACKING NR 2008-02-125 AND 126. HEAT TREATED TO T4 CONDITION. THRESHOLD RECEIVED FROM S HOP FABRICATED AND IN T4 CONDITION, N00731. LOCATED AND DRILLED FASTENER HOLES AND TREATED AND PRIMED THRESHOLD (1EA FX 65-23946-4/FX69-24780-2) REF BOEING DWG 65-23946 AND/SRM 51-10-1, PG 12/SRM 51-10-2. THIS IS CLASSIFIED AS A MINOR REPA IR. 2 L 7 3 4F A3WE 2008022800363 20080228 00363 EA 2008 2 28 SWIA200819259 1 20080224 A 3040 HEATER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT WINDOW INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 934SW 7722 FLT 5929 - "L WINDOW HEAT" CAUTION MESSAGE IN FLIGHT. REPLACED CAPTAINS SIDE WINDOW IAW AMM 56-12-01, P/N OFF: NP-13932 2-9, S/N OFF: 04023H4007. 2 L 7 2 4F RT A21EA 2008022800366 20080228 00366 SO 2008 2 28 SWIA200819256 1 20080222 A 5313 STRINGER EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 565SW 120340 FOUND MISSING RIVET AND CORROSION AT STRINGER 20R BETWEEN FRAMES 22 AND 23. REPAIRED AND TREATED CORRODED STRINGER IAW 120 CPM 51-14-00 AND 51-14-02 ALONG WITH SRM 51-40-02. 2 L 7 2 4T RT A31SO 2008022800370 20080228 00370 NM 2008 2 28 HALA0800327 1 20080218 A 5512 PANEL BOEING 717 717200 1383700 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION, NUMEROUS FASTENERS HOLES, ON LOWER SURFACE OF THE LT HORIZ STAB L/E PANEL. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800388 20080228 00388 NM 2008 2 28 SWAA081022 1 20080224 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800389 20080228 00389 NM 2008 2 28 SWAA081023 1 20080224 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380 STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800394 20080228 00394 2008 2 28 SWAA08041 4 20080224 A 2565 6949956 CABLE BOEING 737 7373TO 138447G NM EVAC SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2008022900006 20080229 00006 EA 2008 2 29 TRAX200800261 1 20080214 A 3350 COVER CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 753EV 10169 PLASTIC EXIT LIGHT COVER BY FRONT DOOR IS MISSING. FLT 4182 DEL 31 MINS. 2 L 7 2 4F RT A21EA 2008041100097 20080411 00097 EA 2008 4 11 A6WA200840144 1 20080220 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 460 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 CRACK FOUND ON MACHINE FITTING FS 460 RBL. NEW MACHINED FITTING, REPLACED IAW SRM 51-42-21 AND 51-23-00. (M) 2 L 7 2 4F RT A21EA 2008041100098 20080411 00098 NE 2008 4 11 C1HA200879001 2 20080316 A 7200 ENGINE BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 2 OVERHEATED A C1HA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 GL 15 679MG 46327 1346 22557 700537 ON TAKEOFF ROLL, ENGINES WERE BROUGHT TO 1.4 EPR THEN WERE BEING ADVANCED TO FLEX THRUST WHEN NR 2 ENGINE MADE A LOUD NO ISE, FE CONFIRMED NR 2 ENGINE WAS AT 1.65 EPR WHEN NOISE OCCURRED. NR 2 FUEL FLOW WENT TO 0, ENG FAIL LIGHTS ILLUMINATE D, THRUST LEVERS WERE BROUGHT BACK TO IDLE. NR 2 EGT WENT UP TO 750*, TAKEOFF WAS ABORTED AND RED BORDER CHECKLIST WAS RUN. RUNWAY 36R WINDS 020 AT 7 KTS FOUND METAL IN TAILPIPE. REPLACED NR 2 ENGINE PER TASK B727-7101-02, 02.1 2 L 7 3 4F 4 F A3WE E2EA 2008041100101 20080411 00101 EA 2008 4 11 A6WA200840161 1 20080228 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 CROSSBEAM AT FS 280 RBL 9.0, WL 72 IS CRACKED IN RADIUS. (M) REPAIRED IAW REO 601R-53-11-171, REV B. (K) 2 L 7 2 4F RT A21EA 2008041100104 20080411 00104 2008 4 11 ARWA20080403 4 20080407 A 2200 19787294 CONTROL PANEL DOUG DC10 DC1030F 3023504 WP DAMAGED A ARWA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 478CT 47819 HEADING KNOB WORKING IN FAST MODE ONLY. ENTERED ON DMI NR 21598 AS PER MEL 22-1-(L) CAT "C". REMOVED AND REPLACED HDG GUIDANCE CONTROL PANEL IN ACCORDANCE WITH M/M 22-00-00. CHECK GOOD IN ACCORDANCE WITH M/M 22-00-00. CLEARED DMI NR 215 98; PLACARD REMOVED. 2 L 7 3 4F RT A22WE 2008041100105 20080411 00105 EU 2008 4 11 NSVA2008018 1 20080409 A 3397 CONNECTOR SAAB SF340 340B 7860101 EU CABIN LIGHTS SMOKE A NSVA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 350CJ 340B350 FA SAW AND SMELLED SMOKE COMING FROM LIGHT AT 2A, CREW EVACUATED AIRCRAFT USING FORWARD MAIN CABIN DOOR. MX CALLED AND AIRCRAFT TOWED BACK TO GATE. TROUBLESHOT AND FOUND SOCKET FOR SEAT 2A WINDOW LIGHT BURNED, REMOVED BULB FOR SAFETY PURP OSE ITEM DEFERRED IAW MEL 33-20-1-1 CAT C. FOUND SMOKE WAS COMING FROM SEAT 2A BALLAST CONNECTOR DISCONNECTED POWER TO BALLAST FOR SEAT 2A HAD POWER ON AIRCRAFT NO SMOKE NOTICED SEAT 2A LIGHT SYSTEM REMAINS ON MEL. 2 L 7 2 4T RT A52EU 2008041100106 20080411 00106 EU 2008 4 11 MALA080055 1 20080410 A 5523 SKIN SAAB SF340 340B 7860101 EU ELEVATOR TAB PUNCTURED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 445XJ 340B445 LT ELEVATOR UPPER SKIN HAS THREE PUNCTURES OB OF TRIM TAB AS WELL AS 13 PREVIOUS REPAIRS NOT RECOGNIZED AS BEING IN COMP LIANCE WITH THE SRM. REPAIRED DAMAGE AND PREVIOUS COMPOSITE DAMAGE ON LT ELEVATOR IAW EO NR S55143 FOR MORE INFO SEE CO NT CARD 085348 FROM CONTINUATION CARD 085348. (1) LT ELEVATOR REQUIRES BALANCE. BALANCED LT ELEVATOR IAW SF3 SRM 51-60 -00 (2) LT ELEVATOR UPPER SKIN DAMAGE REQUIRES DIMENSIONAL EVALUATION FOR ENGINEERING DEPARTMENT. MAPPED LOCATIONS AND MEASURED ALL THREE PUNCTURE DIMENSIONS AND FORWARDED TO ENGINEERING. 13 PREVIOUS REPAIRS REQUIRE EVALUATION FOR SRM COM PLIANCE. MAPPED ALL PREVIOUS REPAIRS ADJACENT TO PUNCTURE DAMAGE. FORWARDED TO ENGINEERING. LT ELEVATOR REQUIRES PERM 2 L 7 2 4T RT A52EU 2008041100110 20080411 00110 EA 2008 4 11 SWIA200819442 1 20080404 A 4990 APU CNDAIR CL600 CL6002B19 1900309 EA LEAKING A SWIA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 407SW 7034 FLT 2666 - FUEL ODOR CAN BE NOTICED WHEN PACKS ARE OPERATING ON APU. CLEANED RESIDUAL FUEL IN THE APU COMPARTMENT AND A FT EQUIPMENT BAY. RAN AND INSPECTED APU FOR LEAKING. NO LEAKS NOTED. NO FUEL ODOR NOTED. 2 L 7 2 4F RT A21EA 2008041100112 20080411 00112 EA 2008 4 11 SWIA200819444 1 20080404 A 3397 WIRE CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 764SK 10229 FLT 6332 - EMERGENCY EXIT SIGN ABOVE SERVICE DOOR DOES NOT LIGHT UP. REPAIRED WIRING TO EXIT SIGN. OPS TEST GOOD. 2 L 7 2 4F RT A21EA 2008041100113 20080411 00113 EA 2008 4 11 SWIA200819445 1 20080403 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 913SW 7597 OVERHEAD EMERGENCY FLOODLIGHT IS INOP. RELAMPED OVERHEAD FLOODLIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008041100119 20080411 00119 EA 2008 4 11 SWIA200819452 1 20080405 A 3397 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS UNSECURE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 614SK 10051 FLT 4000 - FORWARD EMERGENCY LIGHT STRIP IS INOP. RESECURED CONNECTOR ON LIGHTING STRIP. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008041100123 20080411 00123 EA 2008 4 11 A6WA200840133 1 20080219 A 5320 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 718 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 AT FS 718, RBL 27 APPROX, HYDRAULIC MANIFOLD SUPPORT BRACKET FOUND CRACKED. REPAIRED IAW REO 601R-53-62-031. (M) 2 L 7 2 4F RT A21EA 2008041100124 20080411 00124 EA 2008 4 11 A6WA200840135 1 20080226 A 5246 STOP CNDAIR CL600 CL6002B19 1900309 EA DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 ON RT WING BUTEDOOR, STOP ASSY CRACKED. REPLACED IAW SRM 51-42-06, 51-42-113. REPLACED IAW SRM 51-42-06, 51-42-13. (M ) 2 L 7 2 4F RT A21EA 2008041100129 20080411 00129 EA 2008 4 11 TRAX200800479 1 20080329 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN SMOKE A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 682BR 7691 UNUSUAL ELEC SMOKE ODOR ON DESCENT. 2 L 7 2 4F RT A21EA 2008041100130 20080411 00130 EA 2008 4 11 TRAX200800480 1 20080329 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 EMERGENCY LIGHT ON LEFT WALL ENTRANCE IS BROKEN. FLT 4247 DEL 84 MINS. 2 L 7 2 4F RT A21EA 2008041100131 20080411 00131 EA 2008 4 11 TRAX200800481 1 20080329 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 SERVICE DOOR HANDLE INOP. 2 L 7 2 4F RT A21EA 2008041100132 20080411 00132 EA 2008 4 11 TRAX200800482 1 20080329 A 2430 RECTIFIER CNDAIR CL600 CL6002B19 1900309 EA SMOKE A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 682BR 7691 ELECTRIC ODOR IN CABIN. FLT 4533 DEL 80 MINS. EMERGENCY DECLARED. TRANSFORMER RECTIFIER UNITS (TRUS). 2 L 7 2 4F RT A21EA 2008041400030 20080414 00030 CE 2008 4 14 GLBA20061085 1 20080328 A 5311 12944004475 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 469 S3L BENT A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 261GL UE261 FRAME SECTION AT FS 469 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 469 STRINGER 3L IAW SRM 51-40. P/N NR 129-440044-75. 2 L 7 2 4T 4 T RT A24CE E26NE 2008041400033 20080414 00033 SW 2008 4 14 HEER119357 1 20080324 A 5343 407030450197 SUPPORT BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MLG CRACKED B HEER O OTHER O OTHER NR NOT REPORTED 1 SW 03 415PH 53390 3.5 INCH CRACK IN RADIUS RT SIDE ABOVE LANDING GEAR SUPPORT. REPLACED WITH SERVICEABLE SUPPORT. 1 G 7 1 3U 3 U O H2SW E1GL 2008041400037 20080414 00037 CE 2008 4 14 DJFA2008037 1 20080401 A 2130 CABIN PRESSURE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP MALFUNCTIONED E DJFA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 EA 23 817LX 258516 DURING CLIMB AT FL 320 THE CABIN PRESSURE BEGAN CLIMBING AT 2000 FPM. THE CREW FOLLOWED THERE EMERGENCY PROCEDURES AND M ADE A EMERGENCY DESCENT. DURING THE DESCENT THE CABIN PRESSURE RATE MATCHED THE AIRCRAFT DESCENT RATE. THE AIRCRAFT DIVE RTED AND LANDED SAFELY. (OPEN) 2 L 7 2 4F 4 F RT A3EU E6WE 2008041400045 20080414 00045 CE 2008 4 14 DJFA2008038 1 20080405 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE CABIN ODOR E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 755TA RK324 AC DIVERTED ON REPOSITION LEG FOR OILY ODOR IN CABIN WHEN TEMPERATURE WAS TURNED TO HOT. WITH TEMPERATURE TURNED DOWN, THE ODOR DISAPPEARED. MAINT RAN THE AC WITH TEMPERATURE IN FULL HOT AND FULL COLD. NO OILY ODOR WAS NOTICED. CABIN AI R OUTLETS WERE CHECKED FOR BLOCKAGE. TEMPERATURE SENSOR WAS CHECKED FOR PROPER OPERATION. THE DISCREPANCY COULD NOT BE DUPLICATED. 2 H 7 2 4F 4 F RT A16SW E25EA 2008041400047 20080414 00047 WP 2008 4 14 AMTA200800242 1 20080327 A 3397 CONNECTOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL EMERGENCY LIGHT DAMAGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 701TZ 46583 AISLE EGRESS LIGHT AT 12JH INOPERATIVE. REPINNED SEAT 12 JH AISLE FLOOR PATH MARKING LIGHT CONNECTOR (SOCKET SIDE) IAW SWP`S IN WDM CH 20, LIGHT CHECKS GOOD AT THIS TIME. (K) 2 L 7 3 4F 4 F A22WE A23EA 2008041400048 20080414 00048 CE 2008 4 14 GUUA04040801 1 20080404 A 5260 12951405925 CABLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA AIRSTAIR DOOR BROKEN A GUUA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 29 87555 UE234 FLIGHT: 9205, PILOT REPORTED (4) REAR CAMS ON FWD CABIN DOOR WILL NOT ROTATE WHEN DOOR IS SECURED. REPLACED AIRSTAIR DO OR DOWN AFT CABLE. 2 L 7 2 4T 3 T RT A24CE E4EA 2008041400056 20080414 00056 CE 2008 4 14 45357033108 1 20080331 A 2997 CONNECTOR LEAR 45 45LEAR 5170805 CE ECS CONTROLLER CRACKED E J7SA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 441FX 357 RED STAB OVERHEAT CAS MSG ILLUMINATED. PERFORMED CHECKLIST AND LIGHT WENT OUT AFTER SEVERAL MINUTES. IFE DECLARED BY AT C. AIR DIVERSION WITH UNEVENTFUL LANDING AND TAXI. PERFORMED GROUND RUNS WITH BOTH ENGINES AT VARIOUS POWER SETTING, CH ECKED CONNECTORS AT ECS CONTROLLER, ALL WITH NO DEFECTS NOTED. 2 L 7 2 4F RT T00008WI 2008041400068 20080414 00068 CE 2008 4 14 DXTA200802949 1 20080318 A 5523 ROD END RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP ELEVATOR TRIM OUT OF ADJUST E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 838QS 258338 DURING INTIAL CLIMB AT 17000 FT + 270 KIAS, MAX FWD ELEVATOR TRIM WAS REQUIRED. ADJUSTED ELEVATOR ROD ENDS OUT .5 TURN A ND LUBRICATED TRIM JACKS. PERFORMED ELEVATOR TRIM CONTROL SYS FUNCTIONAL TEST. ELECTRIC TRIM FUNCTIONAL CHECKS, TRIM RAT E CHECKS. TRIM SAFETY CHECKS OUT OF TRIM ANNUNCIATOR FUNCTIONAL CHECKS IAW MM 27-30-00. NO OTHER DISCREPANCIES FOUND. 2 L 7 2 4F 4 F RT A3EU E6WE 2008041400070 20080414 00070 CE 2008 4 14 DXTA200802960 1 20080323 A 5523 TRIM TAB CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE ELEVATOR OBSTRUCTED E DXTA A UNSCHED LANDING C F F.O.D. FLT CONT AFFECTED CL CLIMB 1 GL 07 374QS 5600475 JAMMED ELEVATOR TRIM TAB ON DEPARTURE. FOUND FOD WEDGED IN CHAIN SPROCKET AREA OF PEDESTAL. REMOVED FOD, NO DAMAGE NOTED , CLEANED AND LUBED TRIM COMPONENTS, OPS CHECK AND TRAVEL CHECKS GOOD AT THIS TIME. REF MM 27-31-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2008041400071 20080414 00071 2008 4 14 DXTA200802961 4 20080324 A 2210 A320101A SWITCH CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE AUTOPILOT INOPERATIVE E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 391QS 7324 5600493 AT FL430 ACCIDENTALLY HIT TURN KNOB, AUTO PILOT WOULD NOT WORK CORRECTLY. IN HEADING MODE IT WOULD ALWAYS STOP 10 DEG S HORT OF THE HEADING BUG. NO FAULT CODES REPORTED. DISCREPANCY RELATED TO INVERTER FAULT. INVERTER SELECT SWITCH REPLAC ED. OPERATIONAL CHECK GOOD. IAW MM CH 24-20-04. 2 L 7 2 4F 4 F RT A22CE E25EA 2008041400077 20080414 00077 CE 2008 4 14 DXTA200802967 1 20080327 A 2150 73838433 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LEAKING E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 900QS 766 7500123 STRONG ODOR FROM WATER SEPARATOR IN CABIN PAC. REMOVED CABIN AIR CYCLE MACHINE DUE TO OIL LEAK. CLEANED CABIN HEAT EXCHA NGE AND INSTALLED REPAIRED ACM IAW MM CH 21-51-00, OPS CHECKED GOOD AND LEAK CHECKED GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008041400078 20080414 00078 CE 2008 4 14 DXTA200802968 1 20080328 A 2750 99146153 PDU CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS INOPERATIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED DE DESCENT 1 GL 07 999QS 5615 7500203 UPON SELECTING FLAP 15 DEGREES, AMBER CAS MSG (FLAP FAIL) SLAT WERE EXTENDED FULL AND FLAPS SHOWED 7 DEGREES. FOUND PDU ONLY PULLING 108 AMPS. REMOVED PDU AND INSTALLED OVERHAULED UNIT IAW MM 27-52-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008041400081 20080414 00081 CE 2008 4 14 DXTA200802976 1 20080401 A 2160 73838433 ACM CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL AIR CON BAY FROZEN E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 932QS 7500032 CANNOT CONTROL TEMP ON CABIN PAC. CABIN FILLED WITH SMOKE. REMOVED & REPLACED FORWARD ACM IAW MM 21-51-00. OPS & LEAK C HECKS ARE GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008041400083 20080414 00083 2008 4 14 DXTA200802978 4 20080402 A 3414 INDICATOR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE AIRSPEED FAILED E DXTA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 GL 07 352QS 5600352 ABOVE 40 KTS, LT AIRSPEED FAILED WITH RED X ACCOMPANIED BY GPWS WINDSHEAR FAIL ANNUNCIATOR. INSPECTED GPWS SYSTEM PERFO RMED GPWS SELF TEST NO FAULTS FOUND CHECKE IAC FAULTS NONE FOUND PERFORMED OPS CHECK OPS CK GOOD IAW MM 34-41-04. 2 L 7 2 4F 4 F RT A22CE E25EA 2008041400085 20080414 00085 2008 4 14 DXTA200802980 4 20080405 A 2210 UNKNOWN AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE STAB CONTROL MULTIPLE FAIL E DXTA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED DE DESCENT 1 GL 07 284QS 185 DURING DESCENT, AP TRIM FAIL LIGHT ILLUMINATED WITH ASSOCIATED AMBER CAS MESSAGE. REPLACED STAB CONTROL RELAYS- 504CH, 505CH, 506CH & 507CH. REPLACED STAB CONTROL PCB'S 502CH & 503CH. OPS CHECKED STAB CONTROL RELAY BOX DUE TO RELAY AND PCB REPLACEMENT. INSPECTED HORIZONTAL STAB CONTROL BUSS. ALL ABOVE WORK ACCOMPLISHED PER MM 27-405-OPS CHECK GOOD.INSPECTED PILOT AND CO-PILOT TRIM SWITCHES IAW WDM27-41-00-CHECKED GOOD. PERFORMED AUTO-PILOT TRIM OPERATIONAL CHECK PER MM 22-10 0- OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A50NM E44NE 2008041400087 20080414 00087 NE 2008 4 14 DXTA200802982 2 20080406 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT BIRD INGESTION E DXTA A UNSCHED LANDING C B F.O.D. SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 343QS 5600444 DURING CLIMB OUT AT APPROX 500 FEET, EXPERIENCED BIRD STRIKE TO LT ENGINE. CREW REPORTED A VERY LOUD BANG, FOLLOWED BY A COUPLE OF MINUTES OF SMOKE/ODOR IN CABIN. REMOVED AND REPLACED LT ENGINE IAW MM 71-01-02. LEAK AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2008041400088 20080414 00088 CE 2008 4 14 DXTA200802983 1 20080406 A 3233 99125692 ACTUATOR CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE MLG MALFUNCTIONED E DXTA O OTHER N FALSE WARNING AP APPROACH 1 GL 07 806QS 5600614 AFTER SELECTING GEAR DOWN, RT MAIN GREEN LIGHT AND GEAR UNLOCKED RED LIGHT BEGAN TO FLICKER INTERMITTENT (3 GREEN NO RED ). TROUBLESHOT TO FAULTY RT MLG ACTUATOR DOWNLOCK SWITCH. REMOVED AND REPLACED RT MLG ACTUATOR. LEAK AND OPERATIONAL CH ECKS NORMAL IAW MM 32-11-02. 2 L 7 2 4F 4 F RT A22CE E00053EN 2008041400095 20080414 00095 CE 2008 4 14 DJFA2008040 1 20080409 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE CABIN ODOR E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 482LX RK413 AIRCRAFT DIVERTED, WHEN PASSENGER NOTICED AN ELECTRICAL BURNING ODOR COMING FROM THE AREA BETWEEN THE FWD RT SEATS. MAI NT REMOVED THE RT SIDEWALL PANEL. GROUND RUNS REVEALED NO DEFECT. THE SIDEWALL WAS REINSTALLED AND THE AC WAS RETURNED TO SERVICE. 2 H 7 2 4F RT A16SW 2008041400099 20080414 00099 WP 2008 4 14 I5HA0858002 1 20080410 A 5730 SKIN CVAC 440 440 2422902 WP ALLSN 501D 501D13A 03004 GL RT WING CORRODED A I5HA K NONE O OTHER IN INSP/MAINT 1 GL 25 582P 475 DURING A ROUTINE MAINT INSP THE UPPER RT OB WING SKIN TE WAS FOUND CORRODED WITH CRACKS COMING AROUND SEVERAL RIVETS. TH E RT UPPER OB WING SKIN WAS REMOVED, ALL THE CORROSION WAS REMOVED, THE WING STRUCTURE INSPECTED, AND THE SKIN WAS REPLA CED IAW THE SRM. 2 L 7 2 4R 4 T 6A6 E282 2008041400101 20080414 00101 CE 2008 4 14 GUUA04040803 1 20080404 A 2701 CONTROL COLUMN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE OBSTRUCTED A GUUA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 17 231YV UE231 FLT NR 9188, ON FINAL APPROACH CONTROL COLUMN JAMMED. REQUIRED STRENGTH OF BOTH CREW MEMBERS TO OVER COME. MAINT DETE RMINED THAT A WIRE BUNDLE FROM UNDER AND FWD OF THE INSTRUMENT PANEL WAS INTERFERING WITH THE CONTROL COLUMN. THE WIRE BUNDLE WAS POSITIONED AND SECURED UP AND OUT OF THE WAY. OPERATIONAL FLIGHT SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E26NE 2008041400102 20080414 00102 EU 2008 4 14 907204092008 1 20080409 A 2497 WIRE UROCOP EC135 EC135P1 8680990 EU TMECA ARRIEL ARRIEL1E 60034 NE C/B PANEL SHORTED E QMLA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 NM 03 145LF 9072 UPON LANDING, STRONG ACRID ODOR IN CABIN AND COCKPIT AREAS. MECHANIC CALLED IN AND UPON INSPECTION OF OVERHEAD CIRCUIT B REAKER PANEL, IT WAS DISCOVERED THAT THE STANDBY ATTITUDE INDICATOR CIRCUIT BREAKER WIRE HAD CONTACTED METAL FRAME RESUL TING IN ARCING. MECHANIC TIGHTENED WIRE LUG AT CIRCUIT BREAKER AND ADDED INSULATION ON FRAME. AIRCRAFT RETURNED TO SERVI CE. 1 G 7 2 3U 3 U O H88EU E19EU 2008041400117 20080414 00117 NM 2008 4 14 NWAA081475511 1 20080408 A 2120 UNKNOWN BOEING 757 757251 1384970 NM CABIN ODOR A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 01 511US 23199 APPROXIMATELY 4 MILES FROM LANDING, FLIGHT ATTENDANTS AND PASSENGERS REPORTED A STRONG WOOD SMOKE ODOR IN THE CABIN. FL IGHT CREW DECLARED AN EMERGENCY AS A PRECAUTIONARY ACTION. THE FLIGHT LANDED WITHOUT INCIDENT, AIRPORT FIRE DEPARTMENT AND MAINTENANCE INSPECTED THE AIRCRAFT UPON ARRIVAL TO THE GATE AND FOUND NO EVIDENCE OF SMOKE OR FIRE IN THE PASSENGER CABIN OR CARGO COMPARTMENTS. 2 L 7 2 4F RT A2NM 2008041400118 20080414 00118 NM 2008 4 14 P5CA0801554 1 20080410 A 2497 CABLE BOEING 747 74746NF 13848BT NM DAMAGED A P5CA O OTHER H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 EA 15 450PA 30808 LIGHTNING STRIKE WHILE SITTING ON THE GROUND IN ORD. ALL ELECTRICAL POWER LOST. COMPLETED CONDITIONAL INSPECTION ACCOR DING TO MM 05-51-13. REPLACED THE 2 BCUS IAW AMM 24-23-01. ALSO, FOUND BOTH EXTERNAL POWER RECEPTACLE NEUTRAL POWER CA BLES DAMAGED. REMOVED SAME CABLES AND DEFERRED EXTERNAL POWER ACCORDING TO MEL 24-41-1. 2 L 7 4 4F RT A20WE 2008041400119 20080414 00119 NM 2008 4 14 DHL2008752516 1 20080410 A 5740 MOUNT BOEING 727 727223 1384074 NM KRUEGER FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 WHILE AT C CHECK, NR 1 KRUEBER FLAP ACTUATOR O/B AND I/B MOUNT SUPPORT CRACKED. REMOVED, FABRICATED, AND INSTALLED NEW SUPPORT BRACKET IAW BOEING DWG 65-16275 REV D AND B727 SRM 51-20-1 FIG 2, 51-30-2, 51-10-2.7075 T6 .071 INCH 8 INCH BY 3 1/2 INCH. 2 L 7 3 4F A3WE 2008041400123 20080414 00123 EA 2008 4 14 A6WA200840219 1 20080318 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA WING DUCT FALSE ACTIVATION A A6WA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 31 431AW 7256 WING DUCT FAIL WARNING ON EICAS/WITH MASTER WARNING. COMPLIED WITH QRH. MESSAGE CLEARED. OPS CHECK OF WING ANTI-ICE G OOD IAW AMM 30-12-00. CHECKED RESISTANCE TO GROUND AT CONTROLLERS OF 14TH STAGE LEAK DETECTION SYSTEM, NO DEFECTS FOUND . 2 L 7 2 4F RT A21EA 20080826 EA 2008 8 26 REX2008F00035 1 20080807 A 2910 HYDRAULIC SYSTEM CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8554A 7554 ON APPROACH INTO KCLE, WHEN GEAR WAS LOWERED THE AURAL "GEAR DISAGREE" WARNING WENT OFF WITH A RED NOSE GEAR INDICATION. CREW DECLARED AN EMERGENCY AND MANUALLY LOWERED THE GEAR. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KCLE. MAINTENANCE PERFORMED A HYDRAULIC SYSTEM BLEED ON SYSTEM 3 AND PERFORMED A FUNCTIONAL CHECK OF THE LANDING GEAR EXTENSI ON AND RETRACTION. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F RT A21EA 20080826 SO 2008 8 26 C2XA08SH092 1 20080703 A 3232 21180100009 ACTUATOR EMB 145 EMB145LR 3260212 SO NLG DOOR LEAKING A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 27 13949 145057 FLIGHT 3082 - DIVERTED FROM IAH - HYD IN SYSTEM 1 LEAKED, HYD SYSTEM I FAILURE. MX REMOVED AND REPLACED NOSE LANDING GE AR DOOR ACTUATOR AND HOSES IAW EMB 145 32-33-03. OPS CHECK GOOD AND LEAK CHECK GOOD. THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080826 EA 2008 8 26 C2XA08CL077 2 20080702 A 7200 ENGINE EMB 145 EMB145XR 3260214 SO RROYCE AE3007 AE3007A1E 54169 EA NR 1 OVERTEMP A C2XA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 27 21154 14192 145772 CAE312423 CLE FLIGHT 2531 - THE CREW REPORTED ENGINE NR 1 HP INDICATION IN YELLOW RANGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO C LE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD. SUP PLEMENT TO FOLLOW. (A) 2 L 7 2 4F 4 F RT TE6CH 20080826 EA 2008 8 26 MASA200800468 1 20080614 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 77181 7181 ASH FLT 7329 ROC-ORD. RAMP PERSONNEL COULD NOT GET THE MAIN CABIN DOOR OPEN FOR MORNING DEPARTURE. MX LUBED THE OUTER DOOR HANDLE AND MECHANISM, OPERATIONAL CHECK NORMAL. (B) 2 L 7 2 4F RT A21EA 20080826 NM 2008 8 26 KCSA081383A 1 20080811 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 440 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 BS 440 S10R FRAME OUTBOARD FLANGE CRACKED IN RADIUS .375 INCH CRACK MARKED UPPER DECK. (S) 2 L 7 4 4F RT A20WE 20080826 EA 2008 8 26 MAL2008F00026 1 20080807 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A MALA O OTHER J WARNING INDICATION LD LANDING 1 GL 15 8965E 7965 FLAP FAIL CAUTION FLAP FAIL AT 30 DEG 6900/160 KTS/GEAR DOWN. COMPLETED WITH FLAP FAIL RESET PROCEDURE IAW CRJ POM SECT ION 3.8. (S) 2 L 7 2 4F RT A21EA 20080826 WP 2008 8 26 AALA200801878 1 20080714 A 3233 3937029501 ACTUATOR DOUG DC9 DC982 3022082 WP MLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 463AA 49593 DFW INFLIGHT T2372/14JUL - CREW REPORTED LT MAIN LANDING GEAR AND LT MAIN LANDING GEAR DOOR UNSAFE INDICATION. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED MAIN LANDING GEAR ACTUATORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (S ) 2 L 7 2 4F A6WE 20080827 NM 2008 8 27 ABXA080202 1 20080721 A 5410 311T106577 DOOR BOEING 767 767232 1385132 NM NR 2 PYLON MISSING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 741AX 22215 STA MIA, ON WALKAROUND MAINTENANCE FOUND CIRCULAR PANEL ON OUTBOARD SIDE OF NR 2 PYLON MISSING. DEFERRED DI 61151. CLE ARED DI, INSTALLED NEW CIRCULAR ACCESS PANEL ON OUTBOARD SIDE OF NR 2 PYLON. (A) 2 L 7 2 4F RT A1NM 20080827 NM 2008 8 27 KCS2008F00003 1 20080707 A 5100 NONE BOEING 747 747209B 138489B NM NONE NONE A KCSA O OTHER O OTHER NR NOT REPORTED 1 GL 23 714CK 22446 AT ABOUT 2:52 A.M. EDT ON JULY 7, THE CARGO AIRCRAFT (N714CK), CRASHED SHORTLY AFTER TAKEOFF FROM EL DORADO INTERNATIONA L AIRPORT, BOGOTA, COLOMBIA. (A) [THIS IS AN ACCIDENT(AP)] 2 L 7 4 4F RT A20WE 20080827 CE 2008 8 27 DXTA200803187 1 20080719 A 3240 BRAKE CESSNA 750 750 2076810 CE MLG MALFUNCTIONED E DXTA O OTHER B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET TX TAXI/GRND HDL 1 GL 07 964QS 7500164 ON LANDING ROLL OUT HAD TO APPLY MORE PRESSURE TO LT SIDE BRAKES. ON TAXI IN LT BRAKE GRABBED AND SHUDDERED. TWENTY MI NUTES LATER LT BRAKES WERE STILL SMOKING. WHOLE AREA WAS OIL AND BRAKE FLUID WAS OBSERVED DRIPPING ON CHALK. SUSPECT L T INBOARD. (A) 2 L 7 2 4J RT T00007WI 20080827 NM 2008 8 27 DXTA200803191 1 20080720 A 2612 FIRE WARNING GULSTM 200 200 4500308 NM APU FALSE ACTIVATION E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 745QS 170 APU FIRE EICAS MSG. ILLUMINATED ON T/O AT ABOUT 90-100 KTS. EICAS MSG. WENT OUT ON ROLL OUT WITH NO INDICATION OF FIR E. APU EGT WAS NORMAL. POST FLT INSPECTION REVEALS NO EVIDENCE OF FIRE, SIGN OR SMELL. (A) 2 L 7 2 4F RT A53NM 20080828 EA 2008 8 28 HNA2008F00036 1 20080612 A 5320 82540016101 ANGLE DHAV DHC8 DHC8311 1386006 EA FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 335EN 32270 32270 375 CORROSION FOUND ON THE RT SIDE OF LAV, BOTTOM ANGLE. REPLACED ANGLE. (S) 2 H 7 2 4T RT A13NM 20080828 EA 2008 8 28 HNA2008F00047 1 20080820 A 5330 SKIN DHAV DHC8 DHC8311 1386006 EA FUSELAGE DAMAGED A HNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 07 343EN 340 SBY-CLT, FLIGHT 4649. ABORTED TAKEOFF AFTER MULTIPLE BIRD STRIKES TO RIGHT SIDE OF ACFT. RETURNED TO GATE. FOUND BIRD STRIKE BELOW RT WINDSCREEN CLEANED AREA. NO DEFECTS NOTED. INSPECTED PROPS. NO DEFECTS NOTED. (S) 2 H 7 2 4T RT A13NM 20080828 EA 2008 8 28 A6WA200840536 1 20080703 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR DIRTY A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 450AW 7823 UNABLE TO OPEN SERVICE DOOR FROM OUTSIDE, HANDLE WILL NOT POP OUT WHEN PUSH BUTTON IS PUSHED. CLEANED SERVICE DOOR HAND LE AND LUBED IAW AMM 52-41-03, OPS CHECK GOOD. (A) 2 L 7 2 4F RT A21EA 20080828 2008 8 28 Q2SA783001 4 20080814 A 2565 SLIDE BOEING 747 747281F 13848AB NM GE CF6 CF650E2 30018 NE UNWANTED DEPLOY A Q2SA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 EA 63 783SA 23919 DURING MAINTENANCE ACTIVITY IN SBKP, ACFT DOOR OPENED WITH FLOOR MOUNTED ESCAPE SLIDE HANDLE IN "AUTO", WHICH INADVERTEN TLY ACTIVATED RT SIDE UPPER DECK SLIDE. NO DAMAGE CAUSED TO ACFT. SLIDE REMOVED IAW AMM 25-68-00/PG 201. TRANSFERRED TO DI 16944 IAW DDPG MEL 25-11(3), CAT C. ALL AD`S ARE CURRENT FOR THIS ACFT. 2 L 7 4 4F 4 F RT A20WE E23EA 20080828 NE 2008 8 28 PCS2008F00000 2 20080826 A 7230 COMPRESSOR BOEING 727 727227 1384078 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A PCSA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 17 794AJ 21243 DURING CLIMB BETWEEN 180 TO 210 FLIGHT LEVEL NR 1 ENG COMPRESSOR STALL FOLLOWED BY OIL TEMP RISE. AFTER SECOND COMPRESS OR STALL NR 1 ENG OIL PRESS LIGHT ILLUMINATED. ENG WAS SHUT DOWN PER AOM. NR 1 ENG OPERATED APPROX 9 MINUTES OIL PRESS ABOUT 20 PSI. POST FLIGHT INSPECTION REVEALED NO INLET OR EXHAUST DAMAGE. THE NR 1 AND NR2 COMPRESSORS WOULD NOT ROTA TE. THE ACFT WAS RELEASED FOR A TWO ENG FERRY TO KMIA. (S) 2 L 7 3 4F 4 F A3WE E2EA 20080828 NM 2008 8 28 F3LA200800573 1 20080819 A 5321 D5367202600000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 928FR 2236 DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 151UG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO TRANSITION PANEL 151UG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080828 EA 2008 8 28 QXEA200800598 1 20080530 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 752 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 610QX 10033 RFD-C4 CHECK - CORRODED SIDE SEAT TRACK ON LT SIDE AT FS 752. BLENDED CORROSION FROM LT SIDE SEAT TRACK AT FS 752. REM OVED .006 MATERIAL FOR BLEND, WITHIN LIMITS MAX ALLOWABLE BLEND IS .035 INCHES. ALL WORK DONE IAW CRJ BOMB REO 670-53-0 0-013. TREATED IAW CRJ BOMB REO 670-53-00-013. (S) 2 L 7 2 4F RT A21EA 20080828 NM 2008 8 28 KCSA081421 1 20080821 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1000 S39L DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STRINGER 39L DAMAGED AT STA 1000. (S) 2 L 7 4 4F RT A20WE 20080828 SO 2008 8 28 RAIA00808017 1 20080817 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 815HK 145048 PRE FLT 5581 - STL - EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CEILING EMERGENCY LIGHT. SYSTE M OPS CHECKED GOOD. (S) 2 L 7 2 4T RT T00011AT 20080828 NM 2008 8 28 USAA920081561 1 20080821 A 5311 6520723 FRAME BOEING 737 7373B7 1384580 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT-Q6 - MAJOR REPAIR - CRACK IN AFT FUSELAGE FRAME AT FORWARD CARGO DOOR CUTOUT AT LOWER DOOR STOP BS 492.4, S24R. REP LACED FUSELAGE FRAME AT FORWARD CARGO DOOR CUTOUT AT LOWER DOOR STOP BS 492.4, S24R IAW B737 SRM 51-40-02. (S) 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084434 1 20080810 A 5322 6546525 SHEAR TIE BOEING 737 7373Q8 1384670 NM BS 380 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 380, STR 15L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084590 1 20080819 A 5512 65C25727 SKIN BOEING 737 7375H4 138449D NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED BRDG CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 125. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084591 1 20080819 A 5315 BAC1409100146 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 767 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767, LBL 3 TO RBL 13. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084596 1 20080819 A 5312 6517583 VERTICAL BEAM BOEING 737 7373A4 1384585 NM BS 178 BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LT 5.7. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084734 1 20080826 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084695 1 20080825 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907,STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084697 1 20080825 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907,STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 2008 8 29 SWAA084698 4 20080825 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080829 EA 2008 8 29 REX2008F00037 1 20080815 A 2611 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO MALFUNCTIONED A REXA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SO 25 8694A 13856 7694 ON APPROACH INTO DTW RECEIVED "CARGO SMOKE" MASTER WARNING, QRH FOLLOWED. BOTTLES DISCHARGED, DECLARED EMERGENCY FOLLOW ED BY UNEVENTFUL LANDING. ACFT INSPECTED BY EMERGENCY VEHICLES WITH NO FIRE OR SMOKE FOUND "FALSE WARNING". REMOVED AN D REPLACED THE CARGO FORWARD DETECTOR IAW BOMBARDIER AMM. OPERATIONALLY CHECKED GOOD. (S) 2 L 7 2 4F RT A21EA 20080829 NM 2008 8 29 SWAA084705 1 20080825 A 3350 20131 BATTERY PACK BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED MV2 CHECK, FOUND L2 EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084709 1 20080825 A 5311 6546536 FRAME BOEING 737 7373T0 1384582 NM BS 559 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084712 1 20080825 A 2560 33500003 GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 775SW 30590 DURING SCHEDULED 8Y CHECK, FOUND MID CABIN EEPLS PHOTOLUMINESCENT STRIP WORN. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084440 1 20080810 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 685 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084713 1 20080825 A 5322 69353656 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 360 S28L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 360, STR 28L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080902 2008 9 2 SWAA084674 4 20080824 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 755SA 27871 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080902 2008 9 2 SWAA084673 4 20080824 A 2565 61620468 SLIDE BOEING 737 7373Q8 1384670 NM R1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPL ACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084672 1 20080822 A 5755 ATTACH FITTING BOEING 737 7375H4 138449D NM SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 89317 26569 DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 3 GROUND SPOILER INBOARD ATTACH FITTING CRACKED. REMOVED AND REPLACED SPOI LER PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084671 1 20080821 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 480WN 33998 EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084668 1 20080824 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084663 1 20080824 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 580, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084662 1 20080824 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 560, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084661 1 20080824 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084660 1 20080824 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084653 1 20080824 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084652 1 20080824 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080902 EA 2008 9 2 A6WA200840545 1 20080717 A 2131 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION CL CLIMB 1 GL 31 407AW 7424 ACFT WOULD NOT PRESSURIZE AFTER TAKEOFF, SWITCHED CONTROLLERS, TRIED MANUAL NO ABNORMAL INDICATION. DURING TROUBLESHOOT ING OF ACFT PRESSURIZATION SYS FOUND CABIN PRESSURE TUBE ASSY B NOT CROSS THREADED. R&R CABIN PRESS TUBE ASSY IAW MM 21 -31-00 REF W/C 9 FOR LEAK CHECK. 2 L 7 2 4F RT A21EA 20080902 2008 9 2 SWAA084649 4 20080823 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084642 1 20080821 A 3350 20121 CHARGER BOEING 737 737317 138447P NM CABIN FAULTY A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED MV2 CHECK, LT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084626 1 20080824 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 322, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084625 1 20080821 A 3350 417A5700 SIGN BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 210WN 34162 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084637 1 20080821 A 5330 65C381921 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084638 1 20080821 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 20L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084636 1 20080821 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084631 1 20080824 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 500, STR 26R. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084628 1 20080824 A 5313 BSC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND STRINGER 18R CORRODED AT BS 830. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084627 1 20080824 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084714 1 20080825 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 500D,STR 15R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084679 1 20080825 A 5310 6978062 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT LOWER CORNER. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084607 1 20080815 A 2121 215201 GASPER FAN BOEING 737 7377H4 1384404 NM E&E BAY FAULTY A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 743SW 29279 DURING FLIGHT GASPER FAN MADE A LOUD GRINDING NOISE. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084609 1 20080820 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AFT SERVICE DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084608 1 20080820 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080902 2008 9 2 SWAA084620 4 20080819 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 724SW 27856 DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084619 1 20080820 A 5311 65C27021 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 939, STR 9R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080902 EA 2008 9 2 A6WA200840548 1 20080722 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 448AW 7814 FLAP FAIL CAS MESSAGE ILLUMINATED AT 100FT AGL WITH FLAPS AT 45 DEGREES, MESSAGE ILLUMINATED APPROXIMATELY 1 MINUTE AFTE R FLAPS INDICATED AT 45 DEGREES. C/W AWAC SUPP 98-018B RESET C/B`S INTERROGATED FECU, RAN FLAP SYS NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 20080902 NM 2008 9 2 AALA200801898 1 20080718 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 DFW - EMERGENCY LIGHT AT FORWARD OVERHEAD SEAT 9D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FORWARD OVERHEAD SE AT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20080902 WP 2008 9 2 AALA200801826 1 20080709 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 594AA 53284 LGA - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 29DEF FOR EMERGENCY LIGHTS IN AFT CA BIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A6WE 2008022900018 20080229 00018 EA 2008 2 29 TRAX200800271 1 20080213 A 2560 GLOWSTRIP CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 EMERGENCY FLOOR PHOTOLUMINESCENT TRACK DAMAGED IN SEVERAL PLACES. REMOVED EMERGENCY FLOOR PHOTOLUMNESENT TRACK IAW AMM 33-51-01-000-801 DISCARED AND REBUILT IAW CRJ 700 AMM 33-51-01-961-801. INSTALLED AND OPS CHECKED EMERGENCY FLOOR PHOT OLUMNESENT TRACK IAW AMM 33-51-01-400-801 AND 33-51-01-710-801. 2 L 7 2 4F RT A21EA 2008022900020 20080229 00020 EU 2008 2 29 TRAX200800273 1 20080129 A 5260 PANEL AEROSP ATR72 ATR72 EU PAX STAIRCASE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 PAX DOOR STAIRCASE AFT SIDE PANEL CRACKED AT LAST STEP. 2 H 7 2 4T RT 2008022900025 20080229 00025 EA 2008 2 29 TRAX200800278 1 20080217 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 889AS 7538 FS 349 FRAME IS CORRODED AT BL 0. 2 L 7 2 4F RT A21EA 2008022900026 20080229 00026 EA 2008 2 29 TRAX200800279 1 20080204 A 5755 PANEL CNDAIR CL600 CL6002C10 1390015 EA RT SPOILER CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 RT MULTI FUNCTION SPOILER CLOSEOUT PANEL CRACKED AT INBOARD AFT CORNER. 2 L 7 2 4F RT A21EA 2008022900033 20080229 00033 NM 2008 2 29 08FDEA00622 1 20080226 A 5330 A6A7112511 SPLICE DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 HFEC INSPECTION CARRIED OUT AND FOUND CRACK AT L-2 RT SPLICE WITH CRACK LENGTH OF APPROX 1 INCH AT STA 6-100. REPAIR CA RRIED OUT AS PER EA 1-5330- 118769, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008022900034 20080229 00034 NM 2008 2 29 08FDEA00623 1 20080226 A 5330 A6A7112507 SPLICE DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 HFEC INSPECTION CARRIED OUT AND FOUND CRACK AT L-1 LT SPLICE WITH CRACK LENGTH OF APPROX .25 INCH AT STA 6-100. REPAIR CARRIED OUT AS PER EA 1-5330-118768, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008022900035 20080229 00035 NM 2008 2 29 KCSA081117 1 20080226 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE SKIN IS CORRODED AT STA 2015, ABOVE STR 47R. 2 L 7 4 4F RT A20WE 2008022900039 20080229 00039 NM 2008 2 29 NWAA080675523 1 20080226 A 2913 PUMP BOEING 757 757251 1384970 NM HYD SYSTEM MALFUNCTIONED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 523US 23617 JUST PRIOR TO DESCENT HAD EICAS MESSAGES, LEFT HYDRAULIC SYSTEM PRESSURE, LEFT HYDRAULIC SYSTEM QUANTITY, LEFT ELECTRIC AND LEFT HYDRAULIC ENGINE PUMP RUDDER RATIO. FOLLOWED COM PROCEDURE FOR LOSS OF LEFT HYDRAULIC SYSTEM. FLIGHT CONTINUE D ON TO LAX AND LANDING WAS UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED EDP. OPERATIONAL CHECKED GOOD AND AIRCRAFT WA S RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2008022900045 20080229 00045 NM 2008 2 29 KCSA081098 1 20080221 A 5313 STRINGER BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE STR 36L CORRODED AT BS 1696. 2 L 7 4 4F RT A20WE 2008022900046 20080229 00046 NM 2008 2 29 KCSA081093 1 20080220 A 5313 STRINGER BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 STR 39L CORRODED AT BS 1699. 2 L 7 4 4F RT A20WE 2008022900049 20080229 00049 EA 2008 2 29 TRAX200800284 1 20080220 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 858AS 7417 AAR - FS 280 LOWER WEB CRACKED O/B OF RBL 9 (MARKED). 2 L 7 2 4F RT A21EA 2008022900050 20080229 00050 EA 2008 2 29 TRAX200800285 1 20080220 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 858AS 7417 FS 280 AFT ANGLE CRACKED O/B OF LBL 9. PERFORMED REPAIR TO FS 280.0 AFT ANGLE IAW REO 601R-53-11-136. REV A. COMPLIE D WITH EO 600-53-0091. 2 L 7 2 4F RT A21EA 2008022900053 20080229 00053 EA 2008 2 29 TRAX200800287 1 20080220 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 858AS 7417 FS 280 ATTACH FITTING O/B RBL 9 CRACKED. REMOVED CRACKED FS 280 ATTACH FITTING. FABRICATED AND INSTALLED SERVICEABLE A TTACH FITTING IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 2008022900054 20080229 00054 NM 2008 2 29 DLM90080286 1 20080225 A 5330 5911401535 SKIN DOUG MD90 MD9030 3023690 NM BS 160 CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 DURING HMV AT OKC, THE AIRCRAFT SKIN AT THE FWD LOWER CORNER OF THE PASSENGER DOOR AIRSTAIR CUTOUT WAS FOUND CHAFED. TH E CHAFED AREA WAS INSPECTED AND TREATED PER BOEING INSTRUCTIONS. 2 L 7 2 4F RT A6WE 2008022900057 20080229 00057 NM 2008 2 29 08FDEA00625 1 20080226 A 5347 A6A70821 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 MAIN DECK, MID CABIN, SEAT TRACK AT STA 6-10 TO STA 6-50, X = 8, 02 EACH CRACK FOUND ON CHANNEL. REPAIRED BY SECTIONA L SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008022900059 20080229 00059 NM 2008 2 29 DLM90080255 1 20080222 A 5512 5922578521 SKIN DOUG MD90 MD9030 3023690 NM HORIZONTAL STAB DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 DURING ACCOMPLISHMENT OF SKIN PANEL SPLICE REPAIR PER SR09550000, TWO HOLES HAD SHORT EDGE DISTANCE CONDITION. A/C WAS AT HMV OKC AAR, WHO CONTACTED BOEING FOR APPROVAL OF CONDITION. SUBJECT CONDITION IS DOCUMENTED ON ERA 466169-14. 2 L 7 2 4F RT A6WE 20080902 NM 2008 9 2 AALA200801893 1 20080716 A 3350 CM1317 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 172AJ 32400 JFK - EXTERIOR EMERGENCY LIGHT AT OVERHEAD SEAT 3EF INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 3EF . SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A2NM 20080902 2008 9 2 SWAA084613 4 20080820 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080827 CE 2008 8 27 DXTA200803197 1 20080724 A 2700 UNKNOWN CESSNA 500 560CESSNA 2076750 CE VIBRATION E DXTA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 07 390QS 5600490 ON CLIMB FELT VIBRATION IN ALL CONTROLS AND COCKPIT SEATS. (A) 2 L 7 2 4F RT A22CE 20080827 EA 2008 8 27 MAS2008F00019 1 20080807 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A MASA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 77195 7195 ASH 7223 CHS-ORD FLAP FAIL ON APPROACH TO LANDING. MAINTENANCE RESET THE SYSTEM AND COMPLIED WITH PART A. (S) 2 L 7 2 4F RT A21EA 20080827 EA 2008 8 27 MAS2008F00027 1 20080811 A 2560 GLOWSTRIP CNDAIR CL600 CL6002D24 1390016 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 902FJ 15002 ASH FLT 2836 PHX. RT FLOOR PANEL EMERGENCY LIGHTING SECTION MISSING. CHANGED PHOTO ILLUMINESCENT STRIP. (S) 2 L 7 2 4F RT A21EA 20080827 EA 2008 8 27 MAS2008F00028 1 20080811 A 3350 BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 921FJ 15021 ASH FLT 2679 CLT-SAT. EMERGENCY LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. (S) 2 L 7 2 4F RT A21EA 20080827 EA 2008 8 27 MAS2008F00031 1 20080811 A 3350 BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 938LR 15038 ASH FLT 2686 CLT-SAT. EMERGENCY LIGHT W/N ILLUMINATED. MAINTENANCE REPLACED BATTERIES. (S) 2 L 7 2 4F RT A21EA 20080827 EA 2008 8 27 MAS2008F00037 1 20080813 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 7337 ASH FLT 2982 SBP-PHX. LT AND RT REARWARD EXTERIOR EMERGENCY LIGHTS INOPERATIVE. OPS CHECKED GOOD. COULD NOT DUPLICATE . (S) 2 L 7 2 4F RT A21EA 20080827 EA 2008 8 27 MAS2008F00042 1 20080818 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 922FJ 15022 ASH FLT 2836 PHX-BUR. EMERGENCY FLOOD LIGHT INOPERATIVE. MAINTENANCE RELAMPED. (S) 2 L 7 2 4F RT A21EA 20080827 EU 2008 8 27 MAS2008F00058 1 20080705 A 3350 AML21GBA2CD SWITCH SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS MALFUNCTIONED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 424XJ 340B424 FLIGHT ATTENDANT REPORTED THE EMERGENCY LIGHT ARMED STATUS LIGHT ON THE FA PANEL DID NOT ILLUMINATE; HOWEVER, FLIGHT DEC K VERIFIED EMERGENCY LIGHTS WERE ARMED. REMOVED AND REPLACED F/A CONTROL PANEL SWITCH. (S) 2 L 7 2 4T RT A52EU 20080827 NM 2008 8 27 F3LA200800575 1 20080819 A 5321 D5367223600000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 928FR 2236 DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 162CF WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO PANEL 162C F IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCE PTABLE. (S) 2 L 7 2 4F RT A28NM 20080827 EA 2008 8 27 A6WA200840363 1 20080418 A 2131 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE INTERMITTENT A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 407AW 7424 CABIN ALT CAUTION MESSAGE, RAN QRH AUTO 1&2 CONTROLLER INTERMITTENT AND MANUAL INOPERATIVE. REMOVED DEBRIS FROM EJECTO R JET PUMP. INSPECTED BOTH OUTFLOW VALVES. PER RELIABILITY AS PRECAUTIONARY REPLACED NR 1 CPC PER AMM 21-31-16. OPS C HECK GOOD. REMOVED PLACARD AND MEL. 2 L 7 2 4F RT A21EA 20080828 NM 2008 8 28 F3LA200800562 1 20080816 A 5330 SKIN AIRBUS A319 A319111 3930336 NM FUSLEAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 948FR 47 2836 MAINTENANCE NOTED LIGHTNING STRIKE DAMAGE AT LAP SEAM AT STRINGER 6L, .25 INCH FROM RIVET EDGE AT FRAME 31. ENGINEERING AUTHORIZATION A9-53R-30571 INDICATES MAJOR REPAIR. (S) MX COMPLIED WITH ENGINEERING AUTHORIZATION NR A9-53R-30571. U PON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. REQUIREMENT TO REINSPECT REPAIR AT 32,800 FLIGHT CY CLES. 2 L 7 2 4F RT A28NM 20080828 NM 2008 8 28 F3LA200800567 1 20080816 A 5330 SKIN AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 948FR 47 2836 MAINTENANCE NOTED LIGHTNING STRIKE DAMAGE AT LAP SEAM AT STRINGER 6L, .25 INCH FROM RIVET EDGE AT FRAME 26. ENGINEERING AUTHORIZATION A9-53R-30571 INDICATES MAJOR REPAIR. (S) MX COMPLIED WITH ENGINEERING AUTHORIZATION NR A9-53R-30571. U PON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. REQUIREMENT TO REINSPECT REPAIR AT 32,800 FLIGHT CY CLES. 2 L 7 2 4F RT A28NM 20080828 EA 2008 8 28 MAS2008F00029 1 20080811 A 5210 CABLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 7337 FLT 2748 - PHS-SBP - PAX DOOR WILL NOT CLOSE. MAINTENANCE WAS CALLED OUT AND RESECURED PAX DOOR CABLE. (S) 2 L 7 2 4F RT A21EA 20080828 EA 2008 8 28 MAS2008F00032 1 20080812 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 154SF 7154 FLT 7251 - IAD-CLT - ALL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE WAS CALLED OUT AND WAS ABLE TO CHARGE EMERGENCY BATT ERIES. (S) 2 L 7 2 4F RT A21EA 20080828 EA 2008 8 28 MAS2008F00040 1 20080817 A 5210 DOOR CNDAIR CL600 CL6002D24 1390016 EA MAIN PAX OBSTRUCTED A MASA O OTHER C F.O.D. NR NOT REPORTED 1 SW 07 942LR 15042 ASH FLT 2640 - CLT-IAD - IN FLIGHT MAIN PAX DOOR WARNING INDICATION ILLUMINATED WITH DOOR LOCKED. UPON LANDING WARNING EXTINGUISHED. MAINTENANCE INSPECTED AND REMOVED FOD (BAG ZIPPER) FROM AREA. DOOR OPS GOOD. (S) 2 L 7 2 4F RT A21EA 20080828 NM 2008 8 28 QXEA200800527 1 20080521 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 411QX 4055 PDX-C4 CHECK - COMPLIED WITH TASK CARD RD8/4-53-2198-3 FOR PERMANENT REPAIR OF LIGHTNING STRIKE DAMAGE. COMPLIED WITH R D8/4-53-2201 STEPS 1, 2. REMOVED -5 RIVET INSTALL -6 RIVET W/WASHER. HFEC IAW -8 400 NDTM PART 6 51-00-01 AROUND RIVET HOLE. NO CRACKS NOTED. COMPLIED WITH STEPS 4&5 OF RD8/4-53-2201. (S) 2 H 7 2 4T RT A13NM 20080828 NM 2008 8 28 F3LA200800574 1 20080819 A 5321 D5367302000000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 928FR 2236 DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 151BE WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO PANEL 151B E IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCE PTABLE. (S) 2 L 7 2 4F RT A28NM 20080828 NM 2008 8 28 QXEA200800534 1 20080521 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM BS 321 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 411QX 4055 PDX-C4 CHECK - GOUGE ON LT SIDE SKIN APPROX 3.5 INCHES AFT OF STA X321.00 AND 1 INCH ABOVE STR 18. BLENDED AND FOUND OU T OF LIMITS IAW RD 8/4-53-666, MAPPED FOR ENGINEERING. HFEC INSPECTED IAW Q400 NDTM PART 6 51-00-01. NO CRACKS NOTED. BLENDED AREA WITHIN LIMITS IAW RD 8/4-53-2360. ALODINED, PAINTED IAW Q400 SRM 51-25-05/PG 206/ PARA F-1-4 RD 8/4-53-23 60 STEPS 1-7. (S) 2 H 7 2 4T RT A13NM 20080828 EU 2008 8 28 USAA920081559 1 20080817 A 5315 D53472190211 FLOORBEAM AIRBUS A319 A319112 3930323 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 PIT-S4-MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, -Y1292. REPLACED FLOORBEAM AT FR66, -Y1292 IA W A319 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080828 NE 2008 8 28 YENA2008081 2 20080821 A 7532 6774E010000 BLEED VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE FAILED A YENA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 15 569JB 635 635 2075 FLT 785, MCO-BON, DIVERTED TO FLL, ENG NR 2 BLEED FAULT. ACCOMPLISHED ECAM QRH, NO PRESSURIZATION IN CABIN. LOST BOTH (1&2) EMERGENCY DESCENT REQUIRED. REMOVED AND REPLACED NR 2 ENG PRESSURE REGULATING VALVE 4001HA PER AMM 36-11-52. OPS CHECK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20080828 SO 2008 8 28 C2XA08RI113 1 20080801 A 3610 LINE EMB 145 EMB145XR 3260214 SO BLEED SYSTEM LEAKING A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 26141 145733 FLIGHT 2943 - EWR - FLIGHT CREW PERFORMED AIR RETURN DUE TO BLEED NR 2 LEAK ON EICAS DURING CLIMBOUT. MESSAGE CLEARED A FTER COMPLETION OF QRH PROCEDURES. CREW LANDED ACFT UNEVENTFULLY. EWR MAINTENANCE RESEALED BLEED LINE BETWEEN FRAME 70 AND 74. MAINTENANCE RAN THE ENG NR 2 AND PERFORMED NO LEAK CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE . (S) 2 L 7 2 4F RT 20080828 SO 2008 8 28 C2XA08RI112 1 20080814 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 13123 145688 FLIGHT 2897 - EWR - FLIGHT CREW REPORTED STRONG FUEL ODOR DURING CLIMBING. ODOR WENT AWAY AFTER APU SHUT DOWN. NO ODOR NOTICED ON CRUISE. EWR MAINTENANCE PERFORMED OPERATIONAL CHECK OF APU SUCCESSFULLY. NO ODOR WAS NOTICED. ACFT WAS AP PROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080829 NM 2008 8 29 SWAA084598 1 20080819 A 5310 6545833 CREASE BEAM BOEING 737 7373Q8 1384670 NM BS 188 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 188, STR 17R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084602 1 20080819 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 DURING SCHEDULED MV2 CHECK, FOUND LH OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084732 1 20080826 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084745 1 20080826 A 5313 6551698 STRINGER SPLICE BOEING 737 7373A4 1384585 NM BS 360 S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 27L. REMOVED AND REPLACED STRINGER SPLICE PE R SRM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084696 1 20080825 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400,STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084703 1 20080825 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 520 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 15R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 KCSA081410 1 20080820 A 5320 WEB BOEING 747 747122 1384872 NM BS 1480 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 A 1.5 INCH CRACK AT STA 1480 ON WEB AT LBL 114 WL 168. (S) 2 L 7 4 4F RT A20WE 20080829 SO 2008 8 29 C2XA08RI110 1 20080810 A 2133 2097K011100 OUTFLOW VALVE EMB 145 EMB145LR 3260212 SO CABIN PRESSURE DIRTY A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 13997 25054 145298 FLIGHT 3114 - RIC-AIR CREW REPORTED THAT DURING CRUISE, CABIN PRESSURE WAS AT 12,000 FT AT ALTITUDE OF 32,000 FT. FLIGH T WAS DIVERTED TO RIC. CREW LANDED ACFT UNEVENTFULLY. RIC MAINTENANCE CLEANED LT OUTFLOW VALVE AND PERFORMED OPERATION AL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080829 NM 2008 8 29 SWAA084435 1 20080810 A 5311 6546533 FRAME BOEING 737 7373Q8 1384670 NM BS 500 S28R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, STR 28R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084436 1 20080810 A 5311 6546533 FRAME BOEING 737 7373Q8 1384670 NM BS 460 S28R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 460, STR 28R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080829 EU 2008 8 29 USAA920081553 1 20080820 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 642AW 584 FLT 51 LAX-LAS- EMERGENCY EQUIPMENT - DOOR 1L EMERGENCY FLASHLIGHT REPORTED INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080902 NM 2008 9 2 SWAA084729 1 20080826 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 847 AND BS 867, RBL 70. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080902 2008 9 2 SWAA084723 4 20080826 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 242WN 32505 L1 DOOR EMERGECNY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080902 2008 9 2 SWAA084669 4 20080822 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 475WN 32474 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084655 1 20080824 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084722 1 20080825 A 5512 6573794 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084684 1 20080825 A 3350 20131A BATTERY PACK BOEING 737 737317 138447P NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED MV3 CHECK, FOUND LT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080902 2008 9 2 SWAA084610 4 20080820 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 AALA200801834 1 20080625 A 5320 143T80041 SILL BOEING 767 767223 1385123 NM BS 610-615 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AA 22327 AFW FORWARD CARGO DOOR CUT OUT, LOWER MAIN SILL, OUTER CHORD HAS CORROSION REMOVAL BETWEEN STA 615 AND 610. MATERIAL RE MAINING IS BEYOND SRM LIMITS. REPAIRED PER MRB 767 3213. AREA OF DISCREPANCY IS 2.7 INCHES LONG AND IS THE WIDTH OF TH E FLANGE WITH A DEPTH OF 0.230 INCHES. (S) 2 L 7 2 4F RT A1NM 20080902 NM 2008 9 2 SWAA084612 1 20080820 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED CV CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 19 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 AALA200801923 1 20080721 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 182AN 29592 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080902 NM 2008 9 2 AALA200801892 1 20080716 A 3350 GE767 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 172AJ 32400 JFK - EXTERIOR EMERGENCY LIGHT AT RT NR 4 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT NR 4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A2NM 20080902 NM 2008 9 2 ABXA080212 1 20080715 A 5320 143T500418 WEB BOEING 767 767281 1385109 NM BS 624 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 773AX 22788 WEB CORRODED ON BOTTOM SIDE AT FS 624 AT RIGHT BUTT LINE 38.5. REMOVED AND REPLACED CORRODED WEB IAW B767 SRM. (A) 2 L 7 2 4F RT A1NM 20080902 EA 2008 9 2 TRAX200800776 1 20080610 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA COCKPIT SMOKE A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 354CA 10064 BURNING SMELL IN FLT ACCOMPANIED BY RADIO ATL AT 20 FT GEAR HORN SINK RATE AND PULL UP AURAL. FLT 4268 DEL 104 MINS. (S ERVICE LIGHTS) REMOVED AND REPLACED PYLON SERVICE LIGHT ASSY IAW CRJ700 AMM33-31. CBP2M7 PUSH IN, STAYS CLOSED, NO SM OKE, NO POPPING. OPERATION CHECKED GOOD, NO OTHER DEFECTS NOTED AT THIS TIME. INSPECTED CBP-2 AROUND CB-M7 PER CRJ700 AMM 05-21-00-210-801-A01. NO DEFECTS NOTED. REMOVED AND REPLACED PYLON SERVICE LIGHT ASSY IAW CRJ700 AMM 33-31. CBP2 M7 PUSH IN, STAYS CLOSED, NO SMOKE, NO POPPING, OPERATION CHECKED GOOD. NO OTHER DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2008022900062 20080229 00062 NM 2008 2 29 DLM88080259 1 20080213 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 CRACK ON RT CUSP WEB AT STA Y=222, NEW CUSP WEB WAS INSTALLED IAW DOUGLAS DWG 9930538. 2 L 7 2 4F RT A6WE 2008022900074 20080229 00074 EU 2008 2 29 08FDEA00632 1 20080227 A 5510 A5517742100300 FAIRING AIRBUS 310 A310324 3930206 EU EMPENNAGE TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 EMPENNAGE RT LOWER FAIRING IS TORN. REMOVED AND REPLACED THE FAIRING IAW MM 55-15-11-4. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008022900077 20080229 00077 EA 2008 2 29 TRAX200800292 1 20080221 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 837AS 7271 F/O SIDE WINDOW SHATTERED AT FL250. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2008022900082 20080229 00082 NM 2008 2 29 NSVA2008005 1 20080219 A 3297 CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM MLG DIRTY A NSVA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 188WQ 4188 NOSE GEAR DOORS DID NOT CLOSE UPON GEAR RETRACTION, DOOR LIGHT ILLUMINATED. CLEANED ELECTRICAL CONNECTOR ON SSV, CLEANE D PROXIMITY SENSORS, NO PROBLEMS NOTED. 2 H 7 2 4T RT A13NM 2008022900083 20080229 00083 EA 2008 2 29 TRAX200800295 1 20080221 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 331CA 10061 RIGHT FWD WING EXTERIOR EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008022900085 20080229 00085 NM 2008 2 29 NSVA2008006 1 20080219 A 3297 CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM MLG DIRTY A NSVA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 188WQ 4188 NOSE GEAR DOORS DID NOT CLOSE UPON GEAR RETRACTION, DOOR LIGHT ILLUMINATED. CLEANED ELECTRICAL CONNECTOR ON SSV, CLEANE D PROXIMITY SENSORS, NO PROBLEMS NOTED. 2 H 7 2 4T RT A13NM 2008022900092 20080229 00092 NM 2008 2 29 GTIA0800023 1 20080109 A 5220 LEVER AIRBUS A321 A321231 3940032 NM L3 DOOR BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 EMERGENCY EXIT DOOR L3 ESCAPE SLIDE RELEASE MECHANISM LEVER BROKEN IPC25-62-02 ITEM 40. REPLACED LEVER. 2 L 7 2 4F RT A28NM 2008022900093 20080229 00093 NM 2008 2 29 GTIA0800025 1 20080114 A 5240 MECHANISM AIRBUS A321 A321231 3940032 NM L4 DOOR LACK OF LUBE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 585NK 1438 L4 DOOR FAILED STEP 4AS EMERGENCY CONTROL HANDLE CAN BE ARMED, LUBED AND RIGGED MECHANISM AND CHANGED SLIDE PACK. 2 L 7 2 4F RT A28NM 2008022900095 20080229 00095 EA 2008 2 29 SWIA200819241 1 20080217 A 7830 RELAY CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER FAULTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 866AS 7517 FLT 3936 - LEFT REVERSER UNLOCKED CAUTION MESSAGE DURING CLIMB OUT. INSPECTED THRUST REVERSER RIGGING AND REPLACED RELA Y 1K1KE AND 1K2KE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008022900096 20080229 00096 SO 2008 2 29 SWIA200819242 1 20080215 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 564SW 120339 FLOOR EMERGENCY EXIT SIGN IS BROKEN. REPLACED EMERGENCY EXIT SIGN. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008022900099 20080229 00099 SW 2008 2 29 WGEA200800036 1 20080218 A 2897 391088491005 WIRE HARNESS ECLIPS EA500 ECLIPSEEA500 3350000 SW APC CHAFED E WGEA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 145DJ 121 000057 FUEL GAUGING FAULT CAS MESSAGE. ASSIGNED TO MDDR CONTROL NR 421. A/C RELEASED PER MEL 28-01. OK FOR SERVICE. REFERENC E DAYJET WORK ORDER 1396, NR-00001. TROUBLE SHOT FUEL GAUGING FAULT, FOUND HARNESS 39A01P05 OFF THE LEFT APC CHAFED AND TO BE DEFECTIVE. REMOVED AND REPLACED HARNESS IAW EA500 WRM. PERFORMED OPERATIONAL CHECKS IAW EA500 AMM 28-40-00, 71-0 0-00, AND 31-10-00, NO DEFECTS WERE NOTED. FUEL GAUGING SYSTEM FUNCTION WITH NO DEFECTS NOTED. 1 L 7 2 4J RT A00002AC 2008022900104 20080229 00104 NM 2008 2 29 DL757080291 1 20080226 A 5330 143N33406 SKIN BOEING 757 757232 1384965 NM BS 628 MISREPAIRED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 603DL 22810 DURING HMV AT SAA, THE FUSELAGE SKIN AT STA 628 AND S-25L WAS FOUND WITH AN EXISTING REPAIR THAT DID NOT MEET SRM REQUIR EMENTS. THE REPAIR DOUBLER WAS REMOVED AND A BOEING DESIGNED REPAIR WAS INSTALLED. 2 L 7 2 4F RT A2NM 2008022900108 20080229 00108 NM 2008 2 29 DLM88080279 1 20080213 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 DURING HMV, TWO DENTS WERE FOUND CLOSE TO AN EXISTING REPAIR AT STA Y=250 AND BETWEEN LONGERON 19 AND 20 LT. EXISTING R EPAIR WAS REMOVED AND A PERMANENT REPAIR WAS PERFORMED IAW ER/A 095061-14 AND MD-80 SRM 53-04D FIG 12B VIEW AU. 2 L 7 2 4F RT A6WE 2008022900109 20080229 00109 NM 2008 2 29 DL738080281 1 20080224 A 2697 WIRE BOEING 737 737832 13844CF NM GE CFM56 CFM56* 13802 NE NR 2 FIRE LOOP BROKEN A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 3760C 30816 888578 AT CRUISE ALTITUDE, FIRE DETECTION FAULT LIGHT ILLUMINATED BOTH FIRE DETECT LOOPS ON NR 2 ENGINE FAILED. DURING DESCENT INTO KCVG, LIGHT WENT OUT. FOUND NR 2 ENGINE A-LOOP WIRE BROKEN. RETERMINATED WIRE. REPLACED ENG/APU DETECT MODULE P ER M/M. OPS NORMAL. CKD FOR DISCREPANCIES AT RT ENGINE B-LOOP NONE NOTED. REPLACED ENG/APU FIRE CONTROL PANEL PER AMM 26-10-00-710-801. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022900110 20080229 00110 SW 2008 2 29 WGEA200800031 1 20080219 A 2133 54115412003 OUTFLOW VALVE ECLIPS EA500 ECLIPSEEA500 3350000 SW ZONE 100 DEFECTIVE E WGEA O OTHER J WARNING INDICATION LD LANDING 1 EA 27 153DJ 44 000072 FIELD ELEVATION SET AT 200 FT', AIRCRAFT LANDED PRESSURIZED (2.0) PSI. USED MAN/DUMP BUT COULD NOT DEPRESSURIZE EVEN AF TER ENGINE OF, FINALLY DEPRESSURIZED. REFERENCE DAYJET WORK ORDER 1425, NRI 1. REMOVED AND REPLACED PRIMARY AND SECOND ARY OUTFLOW VALVES IAW EA500 AMM 21-30-12 AND 21-38-13. OPS CHECK GOOD. 1 L 7 2 4J RT A00002AC 2008022900115 20080229 00115 EA 2008 2 29 SWIA200819260 1 20080225 A 2710 GEAR CNDAIR CL600 CL6002C10 1390015 EA AILERONS LACK OF LUBE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 771SK 10244 FLT 6577 - AILERON ACTION IS NOT SMOOTH. LUBRICATED AILERON PRIMARY SERVO GEAR TEETH PER CRJ 700 SERVICE LETTER SL-22-0 04. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 TRAX200800780 1 20080611 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS UNSECURE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 970EV 7527 ELECTROLUMINESCENT "EXIT" SIGN BY SEAT 8A WILL NOT ILLUMINATE. RE-SECURED CONNECTOR, OPS CHECK GOOD PER CRJ200 AMM 33-5 1-00. 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 TRAX200800781 1 20080612 A 5210 HANDLE CNDAIR CL600 CL6002B16 1900305 EA PAX DOOR DIRTY A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 MAIN CABIN DOOR WILL NOT CLOSE THE OUTER HANDLE WILL NOT STOW. FLT 4328 DEL 19 MINS. OPS CHECKED MAIN DOOR, OPS NORMAL AFTER CLEANING OPS PER AMM 52-70-01. 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 TRAX200800976 1 20080807 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA DAMAGED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 686BR 7715 REAR PRESSURE BULKHEAD WEB THAT SURROUNDS LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX 1 INCH IN LENGTH AND 60 PERCENT FULL SCREEN HEIGHT. FAILED NDT INSPECTION. REPAIRED AFT PRESSURE BULKHEAD WEB AND LINTEL FITTING IAW ASA EC /ET REO 601R-53-61-1230. ASA RII COMPLIED WITH 5300002. (S) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 TRAX200800969 1 20080805 A 5343 TRUNNION CNDAIR CL600 CL6002C10 1390015 EA LT MLG CORRODED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 738EV 10146 CORROSION ON LT MLG FWD TRUNNION. THE LANDING GEAR WAS REMOVED AND REPLACED FOR EO 700-32-023. LANDING GEAR WAS SENT TO THE GEAR SHOP. (S) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 TRAX200800978 1 20080807 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 686BR 7715 ANGLE CLIPS AT FS 280 LBL 9 AREA CRACKED AT THE INBD AND OTBD POSITIONS. REMOVED INBD & OTBD DAMAGED CLIPS FROM LBL 9 AN D REPLACED WITH NEW SERVICEABLE CLIPS IAW CRJ 200 SRM 51-42-06. REMOVED ALTERNATE LANDING GEAR PULLEY BRACKET FROM FS 2 80 BEAM IAW CRJ 200 AMM 20-21-00-910-801. CABLE BLOCKS WERE PLACED FWD OF FS 280 PULLEY AND AT FS 292 BEAM. REINSTALLE D SAME SERVICEABLE BRACKET FOR MLG ALTERNATE EXTENSION AT FS 280 IAW CRJ 200 AMM 20-21-00-910-801. CABLE BLOCKS AT FWD SIDE OF FS 280 AND AT FS 292 WERE REMOVED. OPS CHECK FOR ALTERNATE MLG EXTENSION DUE. COMPLIED WITH THE MLG OPS TEST O F THE MANUAL RELEASE SYSTEM IAW 32-34-00-710-801. THE MANUAL RELEASE SYSTEM CHECKS GOOD AT THIS TIME. ASA RII COMPLIED 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 TRAX200800995 1 20080810 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 826AS 7210 LT EXTERIOR AFT EMERGENCY LIGHT INOPERATIVE. RELAMP LT AFT EMERGENCY EXTERIOR LIGHT IAW 33-51-21. (S) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 TRAX200800939 1 20080728 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA RIGHT SEIZED A ASOA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 839AS 7284 AFTER LANDING DURING TAXI IN HAD A RT PACK HIGH TEMP CAUTION MESSAGE (FROM DEFECT 423741-1; STRONG SMELL IN CABIN AFTER TAKEOFF. SMELL RESEMBLED SMOKE AND STARTED DISSIPATING. CHECKED ALL SYSTEMS AND RETURNED FOR PRECAUTIONARY OVERWEIGHT LANDING. (AIR RETURN-RELATED TO DEFECT REPORT 423714-1). T/S FOUND RT PACK FROZEN. REMOVED AND REPLACED RT ACM IAW CR J200 MM 21-51-10. OPS AND LEAK CHECK GOOD. (S) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 TRAX200800946 1 20080729 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 27 934EV 8028 CREW REPORTED FLAP FAIL. (ACFT RETURNED TO ATL AFTER TAKEOFF, EMERGENCY VEHICLES ON STANDBY AS A PRECAUTION). FLT 4615 DEL 150 MINS. REMOVED AND REPLACED FLAP CONTROL LEVER IAW CRJ 200 AMM 27-51-01. OPS CHECK GOOD. (S) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 TRAX200800940 1 20080728 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 936EV 8038 AFT ASD ANCHOR FITTING SERRATED PLATE SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED ANCHOR FITTING IAW SB 601R-52-093. NO DEFECTS NOTED AT THIS TIME. RII COMPLIED WITH SATISFACTORILY ON ADJUSTMENT AND RIG OF AFT ASD ANCHOR FITTING PER S P 607. (S) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 TRAX200800974 1 20080806 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 738EV 10146 THE 280 BEAM CORRODED AND CRACKED OUTBOARD OF LBL 9. REFER TO STEPS 2-15 ON ATTACHED M234 FOR WORK ACCOMPLISHED. INSTA LLED LT DRIP TRAY IAW CRJ 700 SRM 51-42-13. (S) 2 L 7 2 4F RT A21EA 20080902 SO 2008 9 2 C2XA08SH111 1 20080819 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 16183 14500914 SHV - DURING C-CHECK CENTER OMEGA BEAM FR 18-23 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM 18-23 IAW EMB 145 XR SRM 51-40-02 AND EC 5320-01140. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080902 SO 2008 9 2 C2XA08IA192 1 20080810 A 3350 7287580503 SIGN EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27523 145389 IAH - DURING MAINTENANCE INSPECTION THE MID CABIN CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE EXIT SIGN. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080902 SO 2008 9 2 C2X2008F00020 1 20080814 A 2913 PUMP EMB 145 EMB145LR 3260212 SO HYDRAULIC SYSTEM LEAKING A C2XA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 13990 MX623836 145277 ACFT EN ROUTE FROM EWR TO TYS WHEN THE HYD 1 SYSTEM MESSAGE WAS HYD LOW QUANTITY. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENG DRIVEN HYD PUMP IAW EMB 145AMM 29-10-03 AND REMOVED AND REPLACED THE NR 1 ELECTRIC DRIVEN PUMP IAW EMB 145 AMM 29-10-04. OPS AND LEAK CHECKS WERE GOOD AND WAS RELEASED AFTER A SERVICE ROUTINE WAS COMPLIED WITH. P/N FOR ELECTRIC D RIVEN HYD PUMP (971533, S/N MX683545). (S) 2 L 7 2 4T RT T00011AT 20080902 NM 2008 9 2 SWAA084586 1 20080819 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 486WN 33852 DURING SCHEDULED HC2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084585 1 20080819 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 SO 2008 9 2 C2XA08IA177 1 20080724 A 2130 2014ABREVC MODULE EMB 145 EMB145LR 3260212 SO CABIN PRESSURE MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION DE DESCENT 1 SW 27 13538 16105 145527 IAH - FLIGHT 2656, THE CREW REPORTED THAT THE CABIN PRESSURIZATION RATE BELOW 20,000 FLUCTUATES WILDLY UP +/- 2500FPM, A ND APPEARED TO BE AFFECTED BY THRUST LEVER SETTING. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPE CTED THE AIRCRAFT AND RESET THE CABIN PRESSURE ACQUISITION MODULE (CPAM), OPERATIONALLY TESTED WITH NO DEFECTS. THE AIR CRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080902 SO 2008 9 2 C2XAA08IA172 1 20080715 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15986 145254 IAH - DURING MAINTENANCE INSPECTION THE SECOND AND THIRD EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINT ENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080902 NM 2008 9 2 SWAA084569 1 20080819 A 3350 311500 LENS BOEING 737 7373Q8 1384670 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084580 1 20080819 A 5330 6551625 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 968, STR 27L. REPAIRED SKIN PER SRM AND BOEING DRAWING. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084574 1 20080817 A 2750 569670 DRIVE UNIT BOEING 737 7373H4 1384600 NM T/E FLAP FAULTY A SWAA D RETURN TO BLOCK F FLT CONT AFFECTED CL CLIMB 1 SW 29 324SW 23414 AIR TURNBACK, FLAPS STUCK AT 5 DEGREE ON CLIMBOUT OF OAK. REMOVED AND REPLACED HYDRAULIC FLAP DRIVE UNIT PER MM. 2 L 7 2 4F RT A16WE 20080902 2008 9 2 SWAA084573 4 20080815 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 797MX 27890 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080902 SO 2008 9 2 CHQA200800131 1 20080705 A 2840 028936006 SENSOR EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007A 03030 GL LT WING OPEN A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 264SK 145221 CAE311337 FLIGHT 5881, DCA TO CLE. WHILE CLIMBING THROUGH 17,000 FT A FUEL 1 LOW LEVEL MESSAGE APPEARED ON EICAS. THE LT TANK IN DICATED ZERO WITH THE RT TANK INDICATING 2,300 LBS. THE FLIGHT LEVELED OFF AS THE QRH PROCEDURES WERE FOLLOWED FOR "FUE L 1 LOW LEVEL" AND "FUEL IMBALANCE" WERE RUN. AFTER FOLLOWING THE QRH THE FLIGHT DIVERTED TO KPIT AND LANDED WITHOUT IN CIDENT. MAINTENANCE TROUBLESHOT THE FAULT AND PLACED THE LT FUEL QUANTITY INDICATION ON MEL. THE MEL WAS CLEARED ON JU LY 7TH WHEN THE REPEATER CODES WERE PULLED AND POINTED TO THE LT TANK UNIT NR 6 BEING AT FAULT. THE TANK UNIT WAS REPLA CED AND THE FUEL QUANTITY SYSTEM INDICATED NORMALLY. (A) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080902 NM 2008 9 2 SWAA084510 1 20080814 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 451WN 32495 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084503 1 20080813 A 5311 6546536 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084502 1 20080813 A 5311 6546557 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084501 1 20080813 A 5311 6546555 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084496 1 20080813 A 5330 6545766 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 FUSELAGE SKIN CRACKED AT BS 583, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 2008 9 2 SWAA084495 4 20080813 A 2565 61620468 SLIDE BOEING 737 7373L9 1384470 NM R1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084494 1 20080813 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SWA E A. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084493 1 20080813 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 EA 2008 9 2 CHQA200800142 1 20080713 A 2750 8004404 SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT WING TE FLAPS FAULTY A CHQA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 11 701BR 7448 GEE872845 FLIGHT 5994, RDU TO SDF. DURING CLIMB AT 3,000 FT THE FLAPS WERE SELECTED FROM 3 DEGREES TO ZERO AND THE CREW RECEIVED A FLAP FAIL MESSAGE. THE CREW REPORTED THAT THE LEFT FLAP STOPPED AT 3 DEGREES AND THE RIGHT FLAP STOPPED AT ZERO. MAI NTENANCE RIGGED THE FLAPS AND BPSU`S AND REPLACED THE INBOARD SKEW SENSOR ON THE RT OUTBOARD FLAP. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080902 EU 2008 9 2 COEA0805816 1 20080806 A 5714 S5241055700000A PANEL AEROSP ATR72 ATR72212 8680945 EU CENTER WING CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 816FX 347 LEVEL 2 CORROSION. SURFACE CORROSION ON MATTING SURFACE OF PANEL 521DT. BLENDOUT OF CORROSION BLENDED BEYOND SRM LIMIT S. S/D HC AT COE. REMOVED AND REPLACED DRY BAY ACCESS PANEL 521DT. (S) 2 H 7 2 4T RT A53EU 20080902 CE 2008 9 2 DXTA200803223 1 20080811 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE MLG WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 326QS 5600526 AFTER LANDING, AT ABOUT 20 KNOTS, THE BRAKES LOST ABOUT HALF THE CONTROL PRESSURE AND BRAKING EFFECTIVENESS. (S) 2 L 7 2 4F RT A22CE 20080902 EU 2008 9 2 EYD2008F00001 1 20080806 A 2131 10246429 CONTROLLER BRAERO DH125 HS125700A 4230170 EU CABIN PRESSURE MALFUNCTIONED A EYDA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 19 411PA NA0211 ON AUGUST 6TH, WHILE EN ROUTE AT AN ALTITUDE OF 35,000 FEET, THE CREW EXECUTED AN EMERGENCY DESCENT DUE TO A "CABIN ALTI TUDE" LIGHT. THE CREW CONTINUED ON TO FXE UNEVENTFULLY. AFTER TROUBLESHOOTING THE PRESSURIZATION SYSTEM, IT WAS DETERM INED THAT THE PRESSURIZATION CONTROLLER P/N 10-1443, THAT HAD BEEN INSTALLED IN OVERHAULED CONDITION THE PREVIOUS WEEK, HAD FAILED. THE CONTROLLER WAS REPLACED AND THE SYSTEM IS WORKING NORMALLY. (S) 2 L 7 2 4F A3EU 20080828 EA 2008 8 28 HNA2008F00035 1 20080612 A 5347 SEAT TRACK DHAV DHC8 DHC8311 1386006 EA BS 593-626 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 335EN 32270 32270 375 CORROSION - LITE SURFACE, SPOTS FOUND ON I/B SET RAILS BETWEEN FS 593 AND 626. HFEC PERFORMED, NO CRACKS. SEAT RAIL RE PAIRED BY SPLICE RD8-53-3886 AND FSR 07-3003. (S) 2 H 7 2 4T RT A13NM 20080828 CE 2008 8 28 GUU2008F00044 1 20080806 A 5520 1016200111BW HINGE BRACKET BEECH 1900 1900D 1154162 CE RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 87554 7924 UE227 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT OUTBOARD ELEVATOR HINGE BRACKET CORRODED. REPLACED RT OUTBOARD ELEVA TOR HINGE BRACKET. (S) 2 L 7 2 4T RT A24CE 20080828 SO 2008 8 28 C2XA08TY088 1 20080825 A 3350 2013BR BATTERY EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16149 145753 TYS - DURING C-CHECK THE LT WING EMERGENCY LIGHT WAS FOUND DIM DURING AN OPS CHECK. MAINTENANCE REMOVED AND REPLACED TH E EMERGENCY BATTERY FOR THE LT WING EMERGENCY LIGHT IAW EMB 145XR 33-50-04 AND OPS CHECKED GOOD. ACFT WILL BE RELEASED WHEN C-CHECK IS COMPLETE. (S) 2 L 7 2 4F RT 20080828 EU 2008 8 28 NWAA083993215 1 20080820 A 2910 O-RING AIRBUS 320 A320211 3930320 EU HYD SYSTEM LEAKING A NWAA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 GL 01 315US 171 AT CRUISE (FL360) ECAM MESSAGE "YELLOW HYD SYSTEM LO", COMPLIED WITH COM PROCEDURES. ACFT LANDED UNEVENTFULLY. REPLACE D O-RING ON YELLOW HP MANIFOLD, NO LEAKS NOTED. (S) 2 L 7 2 4F RT A28NM 20080828 EU 2008 8 28 USAA920081558 1 20080818 A 5320 D53480043207 BEAM AIRBUS A319 A319112 3930323 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 PIT-S4-MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON R2 DOOR SILL BEAM AT FR66 TO FR68. REPLACED R2 DOOR SILL BEAM AT FR66 TO FR68 IAW A319 SRM 53-41-14 AND BOEING DWG D53480009. (S) 2 L 7 2 4F RT A28NM 20080828 EU 2008 8 28 MAS2008F00060 1 20080814 A 3350 AM121GBA2CD SWITCH SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS FAILED A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 424XJ 340B424 ON SHUT DOWN CURRENT BREAKER L8 TRIPPED; EMERGENCY LIGHT STAYED ON; RESET BREAKER, THIS SHUT OFF EMERGENCY LIGHTS. REMO VED AND REPLACED EMERGENCY LIGHT SWITCH. (S) 2 L 7 2 4T RT A52EU 20080828 EU 2008 8 28 MAS2008F00059 1 20080813 A 3350 66362 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 424XJ 340B424 FLOOR TRACK LIGHTING INOPERATIVE ROWS 2 AND 3. REMOVED AND REPLACED FLOOR TRACK LIGHTING STRIP. (S) 2 L 7 2 4T RT A52EU 20080828 NM 2008 8 28 F3LA200800572 1 20080819 A 5321 D5367314700000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 928FR 2236 DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 152WG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO TRANSITION PANEL 152WG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080828 SO 2008 8 28 CHQA200800167 1 20080820 A 3240 39807 CONTROL VALVE EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL BRAKE SYSTEM DEFECTIVE A CHQA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 11 579RP 9655 9655 14500871 CAE311509 FLIGHT 6109, CMH TO CVG. ON THE TAKEOFF ROLL, THE BRAKES GRABBED AND THE ACFT VEERED LT. THE CREW REPORTED THAT THE BR AKES ON THE LT ACTUATED WITHOUT COMMAND. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO GATE. THE BRAKES WERE GRABBI NG WHEN APPLIED DURING TAXI BACK. MAINTENANCE TROUBLESHOT THE FAULT AND FOUND THAT BOTH INBOARD AND OUTBOARD BRAKE CONT ROL VALVES WERE AT FAULT. BOTH OF THE BRAKE CONTROL VALVES WERE REPLACED AND THERE WERE NO FURTHER FAULTS. (S) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080828 EA 2008 8 28 QXEA200800596 1 20080530 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 661 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 610QX 10033 RFD-C4 CHECK - CORRODED SIDE SEAT TRACK ON RT SIDE OF FS 661. BLENDED CORROSION ON RT SIDE SEAT TRACK AT FS 661. REMOV ED .005 INCHES MATERIAL, FOUND TO BE WITHIN LIMITS. MAT BLEND IS .035 INCHES IAW REO 670-53-00-013. TREATED BLENDED AR EA WITH ALUM PREP 33 ALODINE 1001 IAW REO 670-53-00-013. (S) 2 L 7 2 4F RT A21EA 20080829 NM 2008 8 29 SWAA084731 1 20080826 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 807 S27L/R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080829 EA 2008 8 29 VNAA0808009 1 20080816 A 5610 601R3303320 WINDOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE COCKPIT FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 05 251PS 10306 7931 CREW REPORTED A WINDOW HEAT CAS MESSAGE AND ELECTED TO DIVERT TO CLT. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPEC TED ACFT AND CHANGED RT WINDSHIELD. NO DEFECTS WERE NOTED AND ACFT RETURNED TO SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080829 SO 2008 8 29 SIMA200823402 1 20080819 A 5320 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 692AE 14500866 DURING AN IMBV INSPECTION A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FR 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPA IR AND CLEANED THE AREA. PREPARED A DOUBLER, FILLLER, TWO SHIMS AND BACK PLATE. CLEANED AND TREATED ALL REPAIR PARTS. REPAIR DONE IAW EMB 145 SRM (SRM EMB-145/1142 REV 40) CHAPTER 53-00-10 FIGURE 201. ACFT RETURNED TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080829 NM 2008 8 29 ABXA080220 1 20080801 A 5330 148T31211 SKIN BOEING 767 767232 1385132 NM BS 1654 S3-5R CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 745AX 22222 RT STA 1654 SEVERAL FUSELAGE SKIN CRACKS, STRINGERS 3-5. REPAIRED FUSELAGE SKIN IAW B767 SRM 53-80-01. (S) 2 L 7 2 4F RT A1NM 20080902 NM 2008 9 2 SWAA084728 1 20080826 A 5310 6547979 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 807 AND BS 827, RBL 70. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084644 1 20080821 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 723SW 27855 DURING SCHEDULED HC1 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084630 1 20080824 A 5310 6546554 DOOR FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 3 STOP FITTING. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084721 1 20080825 A 5320 6545834 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND FLOOR WEB CRACKED AT BS 247, RBL 24. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084611 1 20080820 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED CV CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 12 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084588 1 20080819 A 5230 6546921 SKIN BOEING 737 7375H4 138449D NM FWD CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED HC2 CHECK, FOUND FWD CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 2008 9 2 SWAA084587 4 20080819 A 2565 6949956 CABLE BOEING 737 7375H4 138449D NM EVAC SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 20080902 WP 2008 9 2 ABXA080217 1 20080812 A 3350 60030451 BATTERY PACK DOUG DC9 DC941 302207N WP EMERGENCY LIGHT DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 952AX 492 47615 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC9 MM. OPS CHECKED GOOD. (S) 2 L 7 2 4F A6WE 20080902 EA 2008 9 2 TRAX200800608 1 20080507 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 928EV 8006 THE PAX DOOR EXIT PLACARD IS WORN. REMOVED AND REPLACED WORN PAX DOOR EXIT PLACARD WITH A NEW EXIT PLACARD IAW CRJ AMM TASK 11-20-00-400-801. SUPPLEMENTAL SDR CLOSED 6/19/08. 2 L 7 2 4F RT A21EA 20080902 SO 2008 9 2 C2XA08SH112 1 20080819 A 5320 14525480603 THRESHOLD EMB 145 EMB145XR 3260214 SO CARGO DOORWAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16183 14500914 SHV - DURING C-CHECK CARGO DOOR THRESHOLD HAS CORROSION IN MULTIPLE AREAS AROUND AND BOTTOM CUT OUT ANGLE. MAINTENANCE REMOVED AND REPLACED CARGO DOOR THRESHOLD LOWER BEAM IAW EMB 145 XR SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO S ERVICE. (S) 2 L 7 2 4F RT 20080902 SO 2008 9 2 CHQA200800166 1 20080818 A 2750 3632001003 DRIVE UNIT EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL TE FLAPS FALSE INDICATION A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 573RP 14500837 CAE312348 FLIGHT 6097, CVG TO GSP. CREW RECEIVED A FLAP FAIL MESSAGE AND SPS ADVANCE MESSAGE WHILE CLIMBING THROUGH 1300 FEET. T HE ACFT RETURNED TO CVG AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CMC MESSAGING POINTING TO A FLAP FEEDBACK POSITI ON ERROR. ALL THE WIRING WAS CHECKED IAW THE FIM PROCEDURES WITH NO DEFECTS NOTED. THE FLAP POWER DRIVE UNIT WAS REPLA CED ALONG WITH THE FLAP HANDLE. THERE WERE NO FURTHER DEFECTS NOTED ON THE TEST FLIGHT THAT FOLLOWED. (S) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080902 NM 2008 9 2 SWAA084521 1 20080814 A 5313 6551698 STRINGER SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 28L. REPAIRED SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20080902 2008 9 2 SWAA084512 4 20080814 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080902 2008 9 2 SWAA084511 4 20080814 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 474WN 33861 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084508 1 20080814 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 451WN 32495 DURING SCHEDULED HC1 CHECK, FOUND EEPLS INOP LENS CRACKED AT ROW 22 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008022900117 20080229 00117 NM 2008 2 29 DLM88080267 1 20080213 A 5753 SKIN DOUG MD88 MD88 3023688 NM TE FLAPS ERODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 DURING HMV, EROSION WAS FOUND ON LOWER SKIN OF OUTBOARD GUIDE VANE OF RT INBOARD FLAP. A PERMANENT REPAIR WAS PERFORMED IAW MD-80 SRM 57-03D PARAGRAPH 8A FIG 9A. 2 L 7 2 4F RT A6WE 2008022900119 20080229 00119 NM 2008 2 29 HALA0800309 1 20080218 A 5711 FRAME BOEING 717 717200 1383700 NM LT WING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 CRACK ON O/B SECTION OF MOST FWD FORMER LEFT WING BELOW CENTER SECTION, VIEWED FROM 2ND WITNESS HOLE. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022900121 20080229 00121 NM 2008 2 29 HALA0800318 1 20080218 A 5414 SKIN BOEING 717 717200 1383700 NM NR 1 NACELLE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION AND PAINT PEEL NR 1 ENGINE, LOWER COWL, EXTERIOR. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022900125 20080229 00125 EA 2008 2 29 SWIA200819231 1 20080211 A 7830 SWITCH CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 866AS 7517 FLT 3927 - AFTER TAKEOFF, RECEIVED A LEFT REVERSER UNLOCKED CAUTION MESSAGE. INSPECTED AND CHECKED GAP AND RIG OF STOW SWITCH IAW 78-32-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008022800152 20080228 00152 NM 2008 2 28 KCSA081096 1 20080221 A 5740 ATTACH ANGLE BOEING 747 747209B 138489B NM RT WING CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 RIGHT WING L/E/ RIB ATTACH ANGLE CRACKED AT FSSI 540. 2 L 7 4 4F RT A20WE 2008022800166 20080228 00166 2008 2 28 DL757080214 4 20080216 A 2565 S416N2021025 SLIDE BOEING 757 757232 1384965 NM R4 DOOR UNWANTED DEPLOY A DALA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 27 669DN 25142 R-4 DOOR WAS IN THE ARMED POSTION CABIN SERVICE OPENED DOOR FROM OUTSIDE AND BLEW THE DOOR ASSIST BOTTLE AND DROPPED THE SLIDE ONTO THE TRUCK. THE SLIDE DID NOT FULLY DEPLOY BECAUSE THE TRUCK PREVENTED THE SLIDE FROM DROPPING ENOUGH TO DEP LOY. 2 L 7 2 4F RT A2NM 2008022800172 20080228 00172 WP 2008 2 28 AALA200800311 1 20080213 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 453AA 49558 LGA - EMERGENCY FLASHLIGHT AT FIRST CLASS FLIGHT ATTENDANT STATION HAS DAMAGED STRAP. REPLACED STRAP FOR EMERGENCY FLAS HLIGHT AT FIRST CLASS FLIGHT ATTENDANT STATION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022800182 20080228 00182 NM 2008 2 28 HALA0800261 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1370 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON SEAT TRACK CROWN/BASE AT LBL 1370, AREA HAS BEEN REWORKED BEFORE. SEAT TRACK REPLACED PER SRM. 2 L 7 2 4F RT A1NM 2008022800206 20080228 00206 NM 2008 2 28 CALA0800162 1 20080221 A 3350 59624 BATTERY PACK BOEING 737 737824 13844BZ NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 37255 30610 EMERGENCY LIGHT CHECK PER CARD 29-3350-1-7100 FAILED. REPLACED EMERGENCY BATTERY PACK AT FORWARD AND AFT GALLEY. 2 L 7 2 4F RT A16WE 2008022800208 20080228 00208 WP 2008 2 28 AALA200800317 1 20080214 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 463AA 49593 LGA - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 33 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 33. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022800220 20080228 00220 NM 2008 2 28 CALA0800165 1 20080221 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 FOUND CORROSION ON CABIN LATERAL FLOORBEAM UPPER CAP AT BS 344 AND LBL 6.0 AS VIEWED FROM E&E CEILING. INSTALLED REPAIR PER SRM 53-10-51. 2 L 7 2 4F RT A16WE 2008022800240 20080228 00240 NM 2008 2 28 SWAA080984 1 20080221 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800262 20080228 00262 EA 2008 2 28 TRAX200800242 1 20080211 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 878AS 7590 FLAP FAIL AT 20 WHEN SELECTING 30. FLT 4444 DEL 150 MINS-NC. FLT 4501 CX. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2008022800287 20080228 00287 NM 2008 2 28 HALA0800279 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 537 S37R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTENING STRIKE ON FUSELAGE STA 537 LONG 37R. FASTENER CLEANED/PRIMED/PAINTED. FASTENER REQUIRED TO BE REPAIRED AS P ER SRM 53-00-01. REPAIR NR 8 AT OR BEFORE 50 FLT CYCLES. 2 L 7 2 4F RT A1NM 2008022800295 20080228 00295 WP 2008 2 28 UPS08851690 1 20080102 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 INTERCOSTAL BETWEEN STA 320-340 RBL 45 HAS CORROSSION. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL REF TRAVELER 78441190001, SRM 51-1-24, SRM 51-1-8, SRM 51-1-21 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2008022800298 20080228 00298 NM 2008 2 28 UPS08M51688 1 20080119 A 5414 AVB7777 FAIRING DOUG MD11 MD11F 3023600 NM PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP 48768 INSPECTION TYPE:1C FROM DMI LOG D339585 TAIL ENG PYLON LOWER AFT FAIRING CRACK REPAIRS REF EO MD11-5450-25730. REMOVED INTERIM REPAIR DOUBLERS, CUTOUT DAMAGE/CRACKS, FABRICATED, AND INSTALLED REPAIR FILLERS & DOUBLERS IAW MD-11 SRM 54-00-0 1 FIG 4 , 51-31-01, AND 51-31-04. 2 L 7 3 4F RT A22WE 20080902 NM 2008 9 2 SWAA084500 1 20080813 A 5311 6546593 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 13L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 SO 2008 9 2 CHQA200800120 1 20080622 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO NR 1 SEIZED A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 278SK 19010 145370 FLIGHT 5588, CLE TO SDF. ON CLIMBOUT WHILE PASSING THROUGH 12,000 FT, THE FLIGHT CREW NOTICED A LIGHT HAZE ACCOMPANIED BY THE FAINT SMELL OF SMOKE. MEMORY ITEMS WERE FOLLOWED AND THE FLIGHT PREPARED TO RETURN TO CLE. ALL APPLICABLE CHECK LISTS WERE FOLLOWED AND THE FLIGHT LANDED WITHOUT INCIDENT. WHILE INSPECTING THE AIR CONDITIONING PACKS, THE ACM FOR TH E NR 1 PACK HAD SEIZED. THE PACK WAS DEFERRED AND THE ACM WAS REPLACED ON THE 23RD. (A) 2 L 7 2 4T RT T00011AT 20080902 SO 2008 9 2 FDK2008F00006 1 20080816 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 830MJ 145259 FDM 6195 JFK-BNA. CEILING EMERGENCY OVERWING EXIT SIGN INOPERATIVE. MAINTENANCE RESET LIGHT CONNECTOR, OPS GOOD. (S) 2 L 7 2 4T RT T00011AT 20080902 NE 2008 9 2 GLB2008F00017 2 20080817 A 7532 BLEED VALVE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MALFUNCTIONED A GLBA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NM 03 100UX UE100 114305 ON DEPARTURE FROM "STL" PILOTS REPORTED THAT WHILE FLYING LEVEL AT 7000, AS PILOTS ACCELERATED THROUGH 200KIAS, LT ENG T ORQUE BEGAN TO FLUTTER CONSTANTLY 50FT/LBS AND EXPERIENCED MULTIPLE DROPS OF +/-100 FT/LBS. ALL OTHER ENG INDICATIONS N ORMAL, +300 FT LB SURGE EXPERIENCED ON SHORT FINAL. MAINTENANCE REMOVED, INSPECTED, RE-INSTALLED THE COMPRESSOR BLEED V ALVE IAW P&W MM 75-30-00. OPERATIONAL CHECKS GOOD ON GROUND RUN. 2 L 7 2 4T 4 T RT A24CE E26NE 20080902 CE 2008 9 2 GUU2008F00037 1 20080809 A 5520 1016200131 HINGE BRACKET BEECH 1900 1900D 1154162 CE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 69549 25747 UE194 AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT CENTER ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED LT CENTER ELEVATOR HI NGE BRACKET. (S) 2 L 7 2 4T RT A24CE 20080902 NE 2008 9 2 HNA2008F00045 2 20080816 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 MALFUNCTIONED A HNAA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 EA 07 815EX 40738 40738 321 FLIGHT 4376 - LYH - DURING CRUISE FLIGHT, WHILE REDUCING PROPELLER SPEED TOWARD 900 RPM, NR2 CONDITION LEVER WENT BELOW MIN POSITION RESULTING IN A LOSS OF POWER. WHEN TORQUE RETURNED TO 0, A SUCCESFUL AIR START WAS ACCOMPLISHED. REMOVED FOR AND SENT TO ROA FOR READING RESULTING IN A NO OVERTORQUE CONDITION. INSPECTED ENG MOUNTS AND ECP FOR FLAGS. NO DEF ECTS NOTED. IT INSTALLED NEW FDR REFERENCE LOG PAGE 262163-1. PERFORMED POWER ASSURANCE RUN AND AUTOFEATHER CHECK. AL L CHECKS GOOD. (S) 2 H 7 2 4T 4 T RT A13NM E20NE 20080902 NE 2008 9 2 HNA2008F00046 2 20080818 A 7261 O-RING DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE ADAPTER LEAKING A HNAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 07 326EN 32682 32682 234 NR 1 ENG OIL PRESSURE WARNING LIGHT ILLUMINATED IN FLIGHT ALONG WITH A NR 1 ENG OIL PRESSURE OF 40 PSI. SHUTDOWN NR 1 E NG PER CHECKLIST. AFTER LANDING FOUND OIL DRIPPING FROM BOTTOM OF NR 1 ENG. 00 ESP HISTORY: NONE. FACT 19AUG08 05:05 CHS, FOUND PCU AND ADAPTER LEAKING. REPLACED ALL O-RINGS AND REINSTALLED AND RIGGED PCU IAW WORKCARDS 61-1-0-10R AND 7 6-00-02Q AND COMPLIED WITH MM 05-50-00 (EXCLUDING PATCH CHECK). NO DEBRIS OR DEFECTS FOUND. GROUND RAN, ENG LEAK AND O PS CHECK GOOD. (S) 2 H 7 2 4T 4 T RT A13NM E20NE 20080902 WP 2008 9 2 IXX2008F00063 1 20080616 A 5330 SKIN DOUG DC8 DC872F 302199E WP BS 1606-1604 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE EXTERNAL SKIN HAS A CRACK AT STATION 1606.000-1604.000 LONGERON 10 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, INTERNAL FINGER D OUBLER, AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC 8 SRM 53-2-1 FIGURE 7 SHEET 1, 3 AND 5 SRM 53-5-2 FIGURE 1 ITEM "D", DC8 SRM 51-1-8B, SRM 51-1-11, SRM 51-1-21, SRM 51-1 -20D, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080902 NM 2008 9 2 KCSA081375 1 20080811 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 700 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 BS 700 FUSELAGE FRAME WEB DENTED ABOVE STR 47R. (S) 2 L 7 4 4F RT A20WE 20080902 NM 2008 9 2 KCSA081363 1 20080731 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2130-2180 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STA 2130 TO STA 2180 AT STR 34L HAS CORROSION ON SKIN. (A) 2 L 7 4 4F RT A20WE 20080902 NM 2008 9 2 SWAA084484 1 20080813 A 5315 6545833 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED HC2 CHECK, FOUND FLOORBEAM CORRODED AT BS 270, LBL 8 TO RBL 8. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 KCSA081398 1 20080816 A 5210 FRAME BOEING 747 747249F 1384849 NM BS 442 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 MAIN DECK L1 DOOR VERTICAL FRAME IS CRACKED (1.5 INCHES) AT FORWARD LOWER CORNER IN RADIUS AT STA 442, WL 209. (S) 2 L 7 4 4F RT A20WE 20080902 NM 2008 9 2 KCSA081399 1 20080816 A 5330 SKIN BOEING 747 747249F 1384849 NM BS 182 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 FUSELAGE SKIN HAS A DENT AT STA 182 BETWEEN STR 45R & 47R. (S) 2 L 7 4 4F RT A20WE 20080902 NM 2008 9 2 SWAA084483 1 20080813 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKN CRACKED AT AIR CONDITIONING ACCESS DOOR BS 520. REPAIRED SKIN PER SWA EA . 2 L 7 2 4F RT A16WE 20080902 EU 2008 9 2 MAL2008F00027 1 20080730 A 5753 RIB SAAB SF340 340B 7860101 EU RT WING TE FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 RT FLAP, AFT COVE RIB CRACKED. INSTALLED NEW RT FLAP AFT COVE RIB IAW SRM 51-20-00 AND 51-40-00 AND EOS57051. REPLACED FASTENERS IN RT FLAP FAIRING AFT BULKHEAD UPPER FLANGE TO REAR SPAR IAW EOS57051. FLAP FAIRING AFT BULKHEAD UPPER FLAN GE TO REAR SPAR - ALTERNATIVE FASTENER REPLACEMENT AUTHORIZATION. STANDARD SRM REPAIR PROCEDURES. ADDENDUM FOR MISSING PART CONDITION INFORMATION. (S) 2 L 7 2 4T RT A52EU 20080902 NM 2008 9 2 SWAA084478 1 20080812 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 909WN 32458 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084477 1 20080812 A 3350 20131A BATTERY PACK BOEING 737 7373T5 1384608 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED SPV CHECK, AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080902 EA 2008 9 2 MAS2008F00010 1 20080802 A 2560 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 87353 7353 ASH FLT 1038 HNL-ITO. INFANT LIFE VEST MISSING. MAINTENANCE REPLACED THE LIFE VEST. (S) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 MAS2008F00013 1 20080804 A 5220 SEAL CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT LEAKING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 904FJ 15004 ASH FLT 2889 PHX-AUS - EMERGENCY EXIT 15F SQUEELS. MAINTENANCE INSPECTED, CLEANED AND LUBED SEAL. (S) 2 L 7 2 4F RT A21EA 20080902 NM 2008 9 2 SWAA084471 1 20080812 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 496WN 32478 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 18 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080902 EA 2008 9 2 MASA200800478 1 20080617 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 919FJ 15019 ASH FLT 2935 PHX-YYC. TWO AFT EMERGENCY CEILING FLOODLIGHTS INOP. MX REPLACED LAMPS, OPS CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 MASA200800471 1 20080615 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 513MJ 10111 ASH FLT 7248 ORD-CLT - EMERGENCY EXIT ROW 12 ACFT RIGHT EXIT SIGN HAS 3 OF 4 BULBS INOP. MX RELAMPED EXIT SIGN. (B) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 MAS2008F00061 1 20080801 A 5210 DOOR CNDAIR CL600 CL6002D24 1390016 EA MAIN PAX OBSTRUCTED A MASA O OTHER C J F.O.D. WARNING INDICATION NR NOT REPORTED 1 SW 07 918FJ 15018 ASH 2725 PHX-SBA. MAIN PAX DOOR CAUTION IN FLIGHT. MAINTENANCE INSPECTED AND DISCOVERED FOD ADJACENT TO PAX DOOR HINGE AREA. REMOVED DEBRIS AND CLEANED, LUBED AND ADJUSTED PAX DOOR LOCK ASSY. OPS CHECKED GOOD. (S) 2 L 7 2 4F RT A21EA 20080902 EU 2008 9 2 NWAA083333312 1 20080705 A 5230 STRUCTURE AIRBUS 330 A330323 3930335 EU CARGO DOOR DENTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 812NW 00784 DURING LINE CHECK FOUND DENT ON INSIDE OF AFT CARGO DOOR. INTERIM REPAIR ACCOMPLISHED PER EA 33-213392 SECT I, SECT II PERMANENT REPAIR TO BE ACCOMPLISHED NEXT "L" CHECK AFTER 05 JUL 08. (S) 2 L 7 2 4F RT A46NM 20080902 NM 2008 9 2 SWAA084470 1 20080812 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 401WN 29813 EEPLS LENS LOOSE AT ROW 5 ABC. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 20080902 EU 2008 9 2 PNS2008F00007 1 20080815 A 3320 6500111 SOCKET SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R390 R3904123F27 NE CABIN LIGHTS BURNED A PNSA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AL 03 676PA 316 ON 8-14-2008, SAAB 340B EN ROUTE, EXPERIENCED SMOKE IN THE CABIN ALONG WITH AN ELECTRICAL ODOR. FLIGHT CREW FOLLOWED EM ERGENCY PROCEDURES AND AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE FOUND THAT THE OVERHEAD LIGHT OVER SEAT 1A BURNT, TH E OVERHEAD LIGHTING SYSTEM WAS DEFERRED. ACFT WAS RETURNED TO ANCHORAGE MAINTENANCE BASE, THE AFFECTED PARTS WERE REPL ACED, AND A TEST OF THE SYSTEM WAS MADE WITH NO DEFECTS. (S) 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P31NE 20080902 EA 2008 9 2 QXEA200800593 1 20080530 A 5210 SKIN CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 610QX 10033 RFD-C4 CHECK - PAX DOOR SKIN BEHIND FWD AND AFT HANDRAIL RETAINING BRACKETS CRACKED. REMOVED DAMAGED MATERIAL, FABRICAT ED FILLERS AND DOUBLERS IAW BOMB. REO 670-52-11-104. PERFORMED LPI TO CUTLINE, NO DEFECTS NOTED IAW NDTM 51-20-008. T REATED IAW CRJ700 SRM 51-21-16, 51-21-06, 51-25-16, AND 51-25-01. INSTALLED REPAIR IAW CRJ REO 670-52-11-104. (S) 2 L 7 2 4F RT A21EA 20080902 NM 2008 9 2 R612008F00008 1 20080812 A 5270 PROXIMITY SENSOR EMB ERJ170 ERJ170100SU 3260403 NM PAX DOOR MALFUNCTIONED A R61A A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 11 802MD 17000013 CREW RECEIVED A CABIN DOOR OPEN MESSAGE ON EICAS. NO OTHER INDICATION THAT DOOR WAS OPENED. CREW FOLLOWED QRH PROCEDUR ES, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED. TROUBLESHOT SYSTEM AND FOUND PROXIM ITY SENSOR NOT WORKING DUE TO AN INOPERATIVE WIRING HARNESS. MAINTENANCE CONTROL PLACED DOOR INDICATION SYSTEM ON MEL A ND RETURNED THE ACFT TO SERVICE. (S) 2 L 7 2 4F RT A56NM 20080902 GL 2008 9 2 RAIA00808001 2 20080801 A 7314 23076363 PUMP EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007A 03030 GL ENGINE FUEL MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 821HK 22834 145068 FLT 5570-CLT - CREW REPORTED AN ENG NR 2 LOSS OF POWER IN FLIGHT ON INITIAL CLIMBOUT AND RECEIVED AN E2 NO DISPATCH MESS AGE ON LANDING. MAINTENANCE REMOVED AND REPLACED THE NR 2 FPMU AND PERFORMED AN OPERATIONAL CHECK OF THE ENG WITH NO OT HER DEFECTS NOTED. (S) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080902 SO 2008 9 2 RAIA00806023 1 20080627 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 840HK 145341 PRE-FLT 7970 - IAD - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REINSTALLED THE SIDEWALL EXIT IDENTIFIER SIGN. OPERATION AL CHECK WAS GOOD. WD:IN HD:O (A) 2 L 7 2 4T RT T00011AT 20080902 SO 2008 9 2 RAIA00807014 1 20080718 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 823HK 145475 FLT 7933 - CHS - SECTION OF FLOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REINSTALLED THE LIGHT STRIP AND SYSTEM OPS CHECKED GOOD. WD:IN. RE:03. AT:0 (A) 2 L 7 2 4T RT T00011AT 2008022800302 20080228 00302 EU 2008 2 28 Y2LA200800013 1 20080220 A 2120 DUCT AIRBUS A319 A319112 3930323 EU CABIN CONTAMINATED A Y2LA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 521VA 2773 SMOKE IN CABIN AND COCKPIT. VERBAL TURNOVER FROM CREW. SMOKE APPEARED AFTER LANDING AND EXITING RUNWAY. RAN APU, OPER ATED PACKS, FOG APPEARED BRIEFLY, FOG CLEARED, NO SMOKE, RAN NR 1 AND NR 2 ENGINES AT IDLE FOR 5 MINUTES. PER 71-00-00- 710-006, CLEARED PNEUMATIC DUCTS OF MOISTURE, BELIEVE CONDITION OCCURS DUE TO SNOW REMOVAL, ENGINES PICKING UP MOISTURE, AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2008022800316 20080228 00316 NM 2008 2 28 SWAA081003 1 20080222 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 580, STR 9R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008022800329 20080228 00329 WP 2008 2 28 08FDEA00552 1 20080221 A 5321 ACA3205549 FLOOR PANEL DOUG DC10 DC1030F 3023504 WP ZONE 200 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MAIN CABIN CABIN FLOORBOARD AT APPROX LBL-20, BETWEEN STA 495 TO 615 IS DELAMINATED. MAT ID A420H PO 590899.1 IAW FED EX DWG SRZ 25-005 REV F. FABBED FLOORBOARD PNL IAW FEDEX DWG SRZ 25-005 REV F. MAT ID POTTING COMP 1619 A/B PO 6064173 . INSERT SLS 5094A3-400-Z, PO595225, INSERT SLP 5094AA-2,PO 595242. ADHESIVE EPIBOND 420 A/B PO 594846.1 IAW FEDEX DWG SRZ 25-005 REV F. LOCATED AND POTTED INSERTS IAW FEDEX DWG SRZ 25-005-REV F. INSTALLED ANTI-SKID, POTTED AND SANDED E DGES IAW FEDEX DWG SRZ 25-005 REV F, MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008022800331 20080228 00331 WP 2008 2 28 08FDEA00554 1 20080221 A 5321 ADA3212509 FLOOR PANEL DOUG DC10 DC1030F 3023504 WP ZONE 200 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MAIN CABIN FLOOR PNL FROM STA 1341, LBL-20 FWD EDGE IS DELAMINATED. MAT ID A402H PO590899.1 IAW FEDEX DWG SRZ 25-005 RE V F. FABBED FLOOR PNL IAW FEDEX DWG SRZ 25-005 REV F. MAT ID POTING COMP 1619 A/B PO 606417.3. INSERT SLS 5094A3-40 0-2 PO 595225, INSERT SLP 5094AA-2 PO 595242. ADHESIVE EPIBOND 420A/B PO 594846.4 IAW FEDEX DWG SRZ 25-005 REV F. LOCA TED INSERTS AND POTTED INSERTS IAW FEDEX DWG SRZ 25-005 REV F. INSTALLED ANTI-SKID IAW FEDEX DWG SRZ 25-005 REV F. POT TED AND SANDED EDGES IAW FEDEX DWG SRZ 25-005 REV F, MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008022800333 20080228 00333 WP 2008 2 28 08FDEA00555 1 20080221 A 5321 AEA7315503 FLOOR PANEL DOUG DC10 DC1030F 3023504 WP ZONE 200 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MAIN CABIN FLOORBOARD AT APPROX LBL-60, BETWEEN STA 1239 TO 1321 IS DELAMINATED. MAT ID A402H35039-003 PO 590899.1. FA BRICATED NEW BOARD, MAT ID POTTING COMPOUND 1619 A/B PO 666417.3. INSERT SLS 5094A3-400-2 PO 595255, INSERT SLP 5094A 3-2 PO 595242. ADHESIVE EPIBOND 420 A/B PO 594846.4. LOCATED HOLES FOR INSERTS, POTTED EDGE AND STARTED CURE, CURE CO MPLETE. SANDED EDGE, POTTED INSERTS. INSTALLED ANTI-SKID IAW FEDEX DC10-30 DWG SRZ 02-005 REV F, MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008022800334 20080228 00334 2008 2 28 SWAA081005 4 20080223 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008022800355 20080228 00355 NM 2008 2 28 08FDEA00568 1 20080222 A 5311 53FX13501 FRAME BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 FWD CARGO PIT, FRAME EXTENSION AT BS 520 IS CRACKED IN UPPER RADIUS, ABOVE STRINGER 22L ON FWD SIDE OF FRAME, MARKED E ND OF CRACK WITH BLACK DOT, (CIRCLED) GENERATED FROM U/C 53F0020. REMOVED CRACKED FRAME EXTENSION. VERIFIED MATERIAL F OR FABRICATION OF NEW FRAME EXTENSION, 7075-O .063" A61578 PO NR 1026198. HEAT TREATED NEW FRAME EXTENSION PART NR 53FX 1350-1 TO T-6 CONDITION. TREATED AND PRIMED AND INSTALLED NEW FRAME EXTENSION REF SRM 51-30-2, 51-10-2, AND STC DWG 53F X1350. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008022800356 20080228 00356 WP 2008 2 28 08FDEA00569 1 20080222 A 5347 AZZ7342507 CARGO TRACK DOUG DC10 DC1030F 3023504 WP BS 775 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 WHILE ACCOMPLISHING "C" CHECK AT TIMCO, THE OUTBOARD RAIL OF THE CARGO LOADING SYSTEM AT 3L POSITION WAS FOUND WITH DAMA GE AT ITS FWD EDGE. TRIM AWAY THE FWD END OF THE SUBJECT RAIL TO REMOVE THE DAMAGE. RESTORE THE ORIGINAL END PROFILE BY COPING FROM THE RAIL AT 3R POSITION IAW EA 8-2550-118438, DATED 2/18/08. MINOR REPAIR PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008022800358 20080228 00358 EA 2008 2 28 CHQA200800033 1 20080218 A 3230 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE MLG MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 650BR 29356 16097 7418 GEE872770 IAH TO CRP - ON TAKEOFF, WHEN THE LANDING GEAR LEVER WAS SELECTED UP THE CREW RECEIVED A LANDING GEAR DISAGREE MESSAGE A ND THE NOSE LANDING GEAR RETRACTED AND LOCKED, BUT THE MAIN LANDING GEAR SHOWED RED AND UNLOCKED. THE LANDING GEAR WAS SELECTED DOWN AND THE LANDING GEAR INDICATED DOWN AND LOCKED. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAULT TO THE MAIN LANDING GEAR SELECTOR VALVE, AND AFTER REPLACING THE VALVE, THE LANDING GEAR OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2008022800401 20080228 00401 EA 2008 2 28 TRAX200800251 1 20080213 A 7830 SWITCH CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 873AS 7549 L REV UNLOCK MSG IN FLT. EMERGENCY STOW INDICATION ONLY NO FLT TO INDICATE REV ACTUALLY OPEN. EN ROUTE TO ATL A/C DIVER TED TO CVG DUE TO MTC - EMERGENCY TRUCKS ON STANDBY AS A PRECAUTION. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETE RMINATION OF AN APPROPRIATE CORRECTIVE ACTION. THRUST REVERSER SYSTEMS. REMOVED AND REPLACED THROTTLE LOCKOUT SWITCH I AW AMM 78-37-01, FOUND CONTACT BRACKET FOR LOCKOUT SWITCH AND STOW SWITCH LOOSE, RESECURED . OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008022800403 20080228 00403 EA 2008 2 28 TRAX200800253 1 20080213 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 889AS 7538 RIGHT FS 625 CLIP IN AFT EQUIP BAY CRACKED. 2 L 7 2 4F RT A21EA 2008022900029 20080229 00029 NM 2008 2 29 DLM88080276 1 20080213 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 DURING HMV AN INADEQUATE REPAIR WAS FOUND ON UPPER FUSELAGE SKIN BETWEEN STA Y=461 AND Y=469 LONGERONS 6 AND 7 LT. A PE RMANENT REPAIR WAS PERFORMED IAW MD-80 SRM 53-04 FIG 12B. 2 L 7 2 4F RT A6WE 2008022900031 20080229 00031 EU 2008 2 29 MAC020805 1 20080207 A 2821 1111084 FILTER AEROSP ATR72 ATR72202 8680940 EU FUEL SYSTEM CLOGGED A MTNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 68 810FX 220 ON DEPARTURE FROM MEM-BHM FLT 8375, THE NR 1 ENGINE FUEL CLOG LIGHT ILLUMINATED. THE PIC DECIDED TO RETURN TO MEM. MAI NTENANCE WAS NOT AVAILABLE IN BHM. MAINTENANCE REPLACED THE HP FUEL PUMP INLET FILTER. THE SYSTEM TESTED GOOD AND THE A/C WAS RETURNED TO SERVICE AND DEPARTED FOR BHM. 2 H 7 2 4T RT A53EU 2008022900037 20080229 00037 NM 2008 2 29 08FDEA00624 1 20080226 A 5347 A6A70821 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 MAIN DECK, MID CABIN, SEAT TRACK AT STA 6-10, X = -8, 01 EACH CRACK FOUND ON CHANNEL. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008022900048 20080229 00048 EA 2008 2 29 TRAX200800283 1 20080220 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 858AS 7417 AAR - FS 280 FWD FLOOR ANGLE BETWEEN LBL 9.0 & RBL 9.0 HAS MINOR SURFACE CORROSION. REMOVED FWD FLOOR ANGLE TO FACILITAT E CORROSION REMOVAL. REMOVED MINOR CORROSION TO 0.003" ON FWD FLOOR ANGLE AT F.S. 280.0 LBL9 TO RBL9. RETURNED TO FINI SH CODE A023. WORK ACCOMPLISHED IAW SRM 51-21-06, 51-21-11, 51-25-06, AND 51-25-16. OK TO REINSTALL FWD FLOOR ANGLE. REINSTALLED FWD FLOOR ANGLE IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008022900090 20080229 00090 NM 2008 2 29 GTIA0800030 1 20080109 A 5320 FLOOR SUPPORT AIRBUS A321 A321231 3940032 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 FLOORBEAM AT FRAME 67-68, Y-765 CORRODED. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2008022900139 20080229 00139 EA 2008 2 29 SWIA200819238 1 20080214 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN SMOKE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 909SW 7558 FLT 6755 - SMOKE IN CABIN AFTER TAKEOFF. INSPECTED CABIN FOR ODOR AND HEAT RELATED ISSUES. NO DEFECTS NOTED. ALL OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008022900140 20080229 00140 SO 2008 2 29 SWIA200819239 1 20080217 A 5210 DOOR EMB 120 EMB120ER 3260203 SO LACK OF LUBE A SWIA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 NM 07 561SW 120335 FLT 3699 - MAIN CABIN DOOR IS DIFFICULT TO OPEN AND CLOSE. CLEANED AND LUBED DOOR. OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 2008022900144 20080229 00144 NM 2008 2 29 MASA200800133 1 20080215 A 2520 PSU DHAV DHC8 DHC8202 2809007 NM CABIN UNSECURE A MASA O OTHER O OTHER CR CRUISE 1 SW 07 991HA 431 ASH FLT 2857 PHX-FLG, SEAT 1A OVERHEAD PSU FELL IN FLIGHT. MX RESECURED PSU. 2 H 7 2 4T RT A13NM 2008022900146 20080229 00146 NM 2008 2 29 DLM88080284 1 20080224 A 2780 833703 SENSOR DOUG MD88 MD88 3023688 NM SLATS DAMAGED A DALA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 SO 27 994DL 53346 SLAT DISAGREE LIGHT AT LANDING, ON GO-AROUND INDICATIONS NML AT FLAPS 15. RECONFIG AND SLATS NML AT FLAPS 23 AND 28. O PS CHECKS NML ALL CONFIGS. CHECKED CABLE DRUM, OK. FOUND D1-65 SENSOR DAMAGED. REPLACED SENSOR, CHECKS GOOD. 2 L 7 2 4F RT A6WE 2008022900147 20080229 00147 NM 2008 2 29 HALA0800352 1 20080226 A 5730 SKIN BOEING 767 7673G5 1385126 NM RT WING CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION, WING RT UPPER SKIN FASTENER AT WS 936 ON FWD SPAR CAP. REMOVED CORROSION IAW B767-300 SRM 51-10-02 T O THE POINT OF CONFORMATION WITH 10X MAGNIFYING GLASS. NO OTHER DAMAGE EXIST ON THIS LINE PERPENDICULAR TO REAR SPAR. REF SRM 57-20-01, FIG 101 "B". 2 L 7 2 4F RT A1NM 2008022900149 20080229 00149 NM 2008 2 29 HALA0800354 1 20080222 A 5753 SKIN BOEING 767 7673G5 1385126 NM TE FLAP DENTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 DENT, RT WING I/B AFT T/E FLAP, WS 237, ON UPPER SKIN IN MIDDLE OF FLAP WEDGE. REPAIRED DENT IAW B767300 SRM 51-70-10, REPAIR 4, REV 76. 2 L 7 2 4F RT A1NM 2008022900150 20080229 00150 NM 2008 2 29 HALA0800355 1 20080221 A 5754 SKIN BOEING 767 7673G5 1385126 NM NR 3 SLAT DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 CRACKING IN SKIN AND RIVET PULLING, WINGS SLAT NR 3, TOP SKIN FWD RIVET IN LINE WITH INBD TRACK. CUT OUT DAMAGE SKIN, F ABRICATED REPAIR PLATE, DOUBLERS AND STRAP AND LOCATED, DRILLED, AND COUNTER SUNK FOR FASTENER HOLES IAW B767300 SRM 57- 43-01, REPAIR 1 FIG 201. RE-PROTECTED BY ALODINE TREATING AND APPLYING ONE COAT OF BMS 10-11 PRIMER PER B767300 SRM 51- 20-01. INSTALLED REPAIR PARTS PER B767300 SRM 57-43-01 AND SEALED IAW SRM B767300 AND SRM 51-10-05. 2 L 7 2 4F RT A1NM 2008022900152 20080229 00152 NM 2008 2 29 GTIA0800028 1 20080115 A 5315 FLOORBEAM AIRBUS A321 A321231 3940032 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 CORROSION ON FLOORBEAM AT FRAME 20 AT Y-765, FABRICATED AND INSTALLED PART IAW SRM 53-00-14. 2 L 7 2 4F RT A28NM 2008022900154 20080229 00154 2008 2 29 GTIA0800022 4 20080109 A 2565 LEVER AIRBUS A321 A321231 3940032 NM ESCAPE SLIDE BROKEN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 EMERGENCY EXIT DOOR R3 ESCAPE SLIDE RELEASE MECHANISM LEVER BROKEN IPC25-62-02 ITEM 50. REPLACED LEVER. 2 L 7 2 4F RT A28NM 2008022900161 20080229 00161 NM 2008 2 29 GTIA0800014 1 20080109 A 5320 FLOOR SUPPORT AIRBUS A321 A321231 3940032 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 FLOORBEAM AT L4 DOOR THRESHOLD HAVE INTERGRANULAR CORROSION FROM FRAME 66.5 THRU 69. 2 L 7 2 4F RT A28NM 2008022900163 20080229 00163 NM 2008 2 29 HALA0800316 1 20080218 A 5414 SKIN BOEING 717 717200 1383700 NM NR 1 NACELLE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION ON TOP COWL NR 1 ENGINE, ALONG L/E AND HINGE EDGE. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022900164 20080229 00164 NM 2008 2 29 HALA0800311 1 20080218 A 5730 SKIN BOEING 717 717200 1383700 NM LT WING CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION AROUND FASTENER TAILS LEFT WING BELOW CENTER SECTION. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022900165 20080229 00165 NM 2008 2 29 GTIA0800015 1 20080109 A 5315 SPLICE AIRBUS A321 A321231 3940032 NM FLOORBEAM CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 Y+1292 AND FRAME 66 FLOORBEAM SPLICE HAS CORROSION. REPLACED Y+1292 FRAME 66 FLOORBEAM SPLICE. 2 L 7 2 4F RT A28NM 2008022900166 20080229 00166 NM 2008 2 29 HALA0800317 1 20080218 A 5414 SKIN BOEING 717 717200 1383700 NM NR 1 NACELLE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION AND PAINT PEEL, NR 1 ENGINE, TOP COWL EXTERIOR AT FAN AIR VALVE EXIT AND 1 PLACE AT COWL HALF. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022900170 20080229 00170 NM 2008 2 29 HALA0800321 1 20080218 A 5510 STRUCTURE BOEING 717 717200 1383700 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION L/E TIP OF RT HORIZ STAB. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022900177 20080229 00177 SO 2008 2 29 SWIA200819248 1 20080221 A 5210 ARM EMB 120 EMB120ER 3260203 SO PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 291SW 120318 FLT 5511 - MAIN CABIN DOOR IS DIFFICULT TO OPEN. CLEANED AND LUBED MAIN CABIN DOOR ACTUATING ARM AND GEARS AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008022900182 20080229 00182 EA 2008 2 29 MASA200800138 1 20080216 A 5220 ESCAPE HATCH CNDAIR CL600 CL6002C10 1390015 EA COCKPIT LEAKING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 510FJ 10101 ASH FLT 7173 ORD-PIT, FLIGHT DECK ESCAPE HATCH LEAKING. INSPECTED AND CLEANED, NO LEAKS NOTED. 2 L 7 2 4F RT A21EA 2008022900185 20080229 00185 EA 2008 2 29 MASA200800142 1 20080217 A 5210 HANDLE CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR OBSTRUCTED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 925FJ 15025 ASH FLT 2872 PHX-SAT, PAX DOOR OUTER HANDLE STOW CAUTION ON GROUND. MX CLEANED DEBRIS, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008022900186 20080229 00186 EA 2008 2 29 MASA200800144 1 20080217 A 5210 PANEL CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 915FJ 15015 PAX DOOR STAIR FWD/AFT PANEL HAS WEB CRACKS. C/W PERMANENT REPAIR. 2 L 7 2 4F RT A21EA 2008022900193 20080229 00193 EA 2008 2 29 MASA200800150 1 20080218 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 926LR 15026 ASH FLT 2764 PHX-RNO. EMERGENCY LIGHT 15DF & 16AC 1 BULB INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2008022900195 20080229 00195 NM 2008 2 29 MASA200800152 1 20080218 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 1 DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 989HA 427 REPAIR TO LEFT NR 1 FLAP TRACK. 2 H 7 2 4T RT A13NM 2008022900196 20080229 00196 NM 2008 2 29 MASA200800153 1 20080218 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 4 DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 989HA 427 REPAIR TO LEFT NR 4 FLAP TRACK. 2 H 7 2 4T RT A13NM 2008022900199 20080229 00199 EA 2008 2 29 TRAX200800306 1 20080222 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA CABIN WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 681BR 7680 AAR - EXIT PLACARD WORN ON PAX DOOR. 2 L 7 2 4F RT A21EA 2008022900202 20080229 00202 EA 2008 2 29 TRAX200800107 1 20080117 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 844AS 7317 AAR - RIGHT 484 O/B RBL 27 CLIP CRACKED. REMOVED CRACKED CLIP FROM RT 484 O/B RBL 27. REF FORM 412 FOR FABRICATION OF SERVICEABLE CLIP IAW CRJ SRM 53-41-43. INSTALLED SERVICEABLE CLIP IAW CRJ SRM 51-42-21. SUPPLEMENTAL SDR CLOSED 2/13/0 8. 2 L 7 2 4F RT A21EA 2008022900204 20080229 00204 NM 2008 2 29 GTIA0800013 1 20080108 A 5320 FLOOR SUPPORT AIRBUS A321 A321231 3940032 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 FLOOR SUPPORT AT R4 DOOR THRESHOLD HAVE INTERGRANULAR CORROSION FROM FRAME 66.5 THRU 69 \ REPLACED FLOOR SUPPORT. 2 L 7 2 4F RT A28NM 2008030300001 20080303 00001 WP 2008 3 3 08FDEA00634 1 20080227 A 5314 SR105300725 SUPPORT DOUG DC10 DC1030F 3023504 WP HORIZONTAL STAB MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 REWORK OF JOB CARD E8-5340-7-3305 PT4 (INSPECT HORIZONTAL STABILZER SECTION PIVOT SUPPORT AD 96-25-15) STEP 3-A. SHOULD HAVE HAS 6 EACH ADDED HOLES, ONLY 5 WERE DRILLED. REPAIRED HORIZONTAL STAB PIVOT SUPPORT IAW FEDEX EA 8-5340-116955. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008030300005 20080303 00005 EA 2008 3 3 A6WA20084018A 1 20080117 A 5420 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT NACELLE UNKNOWN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 RT ENGINE UPPER CORE COWL STA ROD PIN AND BRACKET (SPRING CLIP) FOUND. RT ENGINE UPPER CORE COWL STAY ROD PIN REPLACED AND BRACKET (SPRING CLIP) REPLACED IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008030300011 20080303 00011 WP 2008 3 3 AALA200800373 1 20080221 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 417AA 49328 DFW - EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300014 20080303 00014 NM 2008 3 3 2008UALA00880 1 20080215 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FWD LOWER NOSE COMPT, JUST AFT OF ACCESS DOOR, LOWER CHORD CORRODED, BS 227 LBL 2". MAJOR REPAIR ACCOMPLISHED: RMV'D CO RROSION. INSTALLED REPAIR ANGLE & INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300018 20080303 00018 NM 2008 3 3 2008UALA00882 1 20080215 A 5340 ATTACH ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 S7L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FORWARD ENTRY DOOR SURROUND STRUCTURE CRACK ON ATTACHING ANGLE TO STRINGER S-7L JUST BELOW INTERCOSTAL AT BS 294.5 AND S TRINGER S-7L. 2 L 7 2 4F 4 F RT A16WE E2GL 20080902 NM 2008 9 2 YENA2008077 1 20080809 A 3610 10012463 SHUTOFF VALVE EMB ERJ190 ERJ190100IGW 3260408 NM NR 1 NACELLE FAILED A YENA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 15 258JB 19000047 FLT 447, BOS-TPA, DIVERTED TO JFK, BLEED 1 FAIL EICAS AT FL300, BLEED 1 PSI ABOUT 7 PSI, UNABLE TO MAINTAIN CABIN ALTITU DE. CLIMBING 800 FPM WITH CRUISE THRUST. FAULT CODE 36111200AM1 FOUND ON CMC. REMOVED AND REPLACED NACELLE PRSOV IAW AMM 36-11-03. OPERATIONAL CHECK OK. NO FAULT NOTED ON NR 1 BLEED SYSTEM. (S) 2 L 7 2 4F RT A57NM 20080902 NM 2008 9 2 WRLA2008066A 1 20080804 A 5310 AEA0626 DOUBLER DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 48632 DURING "A4" CHECK INSPECTION IN ZRH FOUND TWO CRACKS IN THE LT AND RT MACHINED DOUBLERS IN THE CENTER LANDING GEAR BAY S TA Y=1381. THE CRACKS WERE LOCATED IN THE VERTICAL ROW OF RIVETS THAT ATTACH THE DOUBLER TO THE VERTICAL STIFFENER. TH E CRACKS STARTED AND ENDED IN RIVET HOLES. REMOVED AND REPLACED LT AND RT DOUBLERS REF SRM 51-30-00 VOL 2 (REV 40). (S ) 2 L 7 3 4F 4 F RT A22WE E24NE 20080902 SW 2008 9 2 WGEA200800069 1 20080715 A 3246 WHEEL ECLIPS EA500 ECLIPSEEA500 3350000 SW MLG DAMAGED A WGEA O OTHER O OTHER NR NOT REPORTED 1 EA 27 146DJ 000058 FLAP COVE IN AREA OF RT WHEEL BENT UP AND HAS A 5 INCH CRACK. REPAIRED DAMAGED TO LOWER RT TRAILING EDGE WING SKIN FROM WS 57.20 TO 73.00 IAW EA SEM 500-0105 REV A DATED JULY 23, 2008. COMPLIED WITH TSR 57071208D REV C DATED 8/4/08. AFTE R DAMAGE WAS CUT OUT NDT REPORTED NO INDICATIONS. SEE NDT REPORT FOR DETAILS. WEIGHT AND BALANCE FOR REPAIR NEGLIGIBLE . NOTE: SEE OTHER RELATED DOCUMENTS FAA FORM: 337 & 8110-3. (S) 1 L 7 2 4J RT A00002AC 20080902 EA 2008 9 2 VNAA0807003 1 20080711 A 5100 NONE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE NONE NONE A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 705PS 10144 CREW REPORTED A GROUND POWER DOOR LEFT OPEN. CREW RETURNED TO HSV AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED A ND FOUND NO DEFECTS. MAINTENANCE SECURED THE DOOR CLOSED. AIRCRAFT WAS RELEASED FOR SERVICE. (A) 2 L 7 2 4F 4 F RT A21EA E00063EN 20080902 NM 2008 9 2 USAABB08128 1 20080806 A 2120 UNKNOWN BOEING 767 767201 1385125 NM CABIN ODOR A USAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 245AY 23897 PHL FLT 742 EN ROUTE PHL TO BCN. ABOUT ONE HOUR INTO THE FLIGHT, THE CREW TWICE NOTICED A STRONG ELECTRICAL BURNING ODO R, WHICH TWICE DISSIPATED SHORTLY AFTERWARDS. THE CREW NOTED THAT TURNING OFF THE FIRST OFFICER`S FOOT HEATER ELIMINATE D THE ODOR ALTOGETHER. THE FLIGHT RETURNED TO FIELD PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE AI RCRAFT ON MEL. (S) 2 L 7 2 4F RT A1NM 20080902 NM 2008 9 2 SWAA084469 1 20080812 A 3350 8100022608 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 273WN 32528 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 USAA920081550 1 20080819 A 5330 6552988 SKIN BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT-C4 -MAJOR REPAIR- CRACK IN FUSELAGE SKIN AT BS 957 BETWEEN S13L & S14L. REPAIRED FUSELAGE SKIN AT BS 957 BETWEEN S1 3L & S14L IAW US AIRWAYS EA 100601 AND US AIRWAYS TYPICAL REPAIR 53-60-10. (S) 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084466 1 20080812 A 5330 6545767 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 26L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084460 1 20080812 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 344, STR 11R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084437 1 20080810 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM 716 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 716, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084654 1 20080824 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 EA 2008 9 2 A6WA200840511 1 20080616 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 444ZW 7788 INTERCOSTAL CLIP AT FS 484, RBL 27, WL 72 IS CRACKED. INTERCOSTAL CLIP AT FS 484, RBL 27, WL 72 REMOVED IAW CRJ 200 SRM 51-42-06. NEW CLIP FABRICATED WITH S-6144-33 IAW CRJ 200 SRM 51-24-36 AND REPLACED IAW CRJ 200 SRM 51-42-06 AND SRM 51 -42-21. (A) 2 L 7 2 4F RT A21EA 20080902 NM 2008 9 2 SWAA084643 1 20080821 A 3350 20121 CHARGER BOEING 737 737317 138447P NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED MV2 CHECK, RT AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084639 1 20080821 A 3350 20131A BATTERY PACK BOEING 737 737317 138447P NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED MV3 CHECK, FOUND LT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084720 1 20080825 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084715 1 20080825 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 15R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008030300019 20080303 00019 NM 2008 3 3 2008UALA00883 1 20080215 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FWD ENTRY DOOR CUTOUT STA 294.5 INTERCOSTAL ANGLE AT STR 11L. MAJOR REPAIR ACCOMPLISHED: REPLACED INTERCOSTAL ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300021 20080303 00021 NM 2008 3 3 2008UALA00885 1 20080215 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S10L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FWD ENTRY DOOR CUTOUT STA 360 STR 10L HAS AN ANGLE CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300024 20080303 00024 NM 2008 3 3 2008UALA00888 1 20080215 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 351 S15L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FWD ENTRY DOOR CUTOUT, INTERCOSTAL SUPPORT STRUCTURE CRACKED BS 351 STR 15L. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300025 20080303 00025 NM 2008 3 3 2008UALA00618 1 20080203 A 2780 3910014101600U SOLENOID BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FLAP-SLAT FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 211UA 30217 STATUS MESSAGE FLAP-SLAT CONTROL 2 DISPLAYED. SUSPECT VALVE SHUTOFF SOLENOID. CHECKED RESISTANCE AT PRIMARY CONTROL SHU TOFF VALVE SOLENOID (V27004). FOUND SOLENOID NEEDS REPLACEMENT. REPLACED SOLENOID. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008030300027 20080303 00027 NM 2008 3 3 2008UALA00656 1 20080205 A 2750 285T004950 FSEU BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE TE FLAPS FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 654UA 25392 STATUS MSG FLAP-SLAT ELEC. AFTER EXTENSIVE TROUBLESHOOTING OF THE FSEU SYSTEM. REPLACED FLAP SLAT ELECTRONICS UNIT PER MM 27-51-01. TEST PASS. NO GRIPS OF FLAP SLATE ELECTRICAL SYSTEM TO DATE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030300028 20080303 00028 NM 2008 3 3 08FDEA00633 1 20080227 A 5315 65208379 FLOORBEAM BOEING 727 727227 1384078 NM BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 MAIN DECK FLOORBEAM UPPER FLAG IS CORRODED/MISDRILLED BS 1110, LBL 27-34, WL 208. REMOVED CORROSION BS 1110, LBL 27 - L BL 31, MAT. THICK .125". REMOVED .116", REMAINING .009" OUT OF LIMITS REF 727-PF SRM 53-10-1 PG 25-41. AAR TOOL 1817 2, CAL DATE DUE 10/15/08. REMOVED DAMAGE AREA. FABRICATED TWO REPAIR ANGLE REF FED EX DWG SR 27-53-034 SHT 2 REPAIR NR 2. MAT ID 17-7PH-.090 A49316. P/O 102446. FAB`D FILLER MAT ID 7075-76 .125". HEAT TREATED REPAIR ANGLES 8130 NR 417 102. CAD PLATED, DRILLED AND TRIMMED ALODINED AND PRIMED ANGLES. PAINTED FILLERS AND ANGLES REF SRM 51-10-2. INSTALLE D REPAIR REF DWG SR27-53-036. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008030300029 20080303 00029 NM 2008 3 3 AALA200800342 1 20080216 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 773AN 29583 JFK - EMERGENCY LIGHT AT SEAT 21G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008030300030 20080303 00030 NM 2008 3 3 2008UALA00422 1 20080124 A 5340 ATTACH ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 344 S16L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 INTERCOSTAL WEB AT STA 344 STR 16L AND INTERCOSTAL ATTACH ANGLES STA 344 STR 16L AND STR 15L WERE FOUND CRACKED. SUPPLE MENTAL DATA UPDATE MAJOR REPAIR: REPLACED THE ATTACH ANGLES. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022800277 20080228 00277 WP 2008 2 28 UPS08851678 1 20080130 A 5730 PANEL DOUG DC8 DC871F 302199D WP RT WING DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 RIGHT WING O/B TRAILING EDGE PANEL UPPER FWD. SURFACE IS DELAMINATED. REPAIRED RIGHT WING O/B TRAIL ING PANEL SURFACE IAW DWG 5644654 AND SRM 51-1-9A. 2 L 7 4 4F RT 4A25 2008022800296 20080228 00296 2008 2 28 UPS08851691 4 20080218 A 2565 SLIDE DOUG DC8 DC871F 302199D WP COCKPIT OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:N/A ESCAPE SLIDE PRESSURE GAUGE NOT VISIBLE. REMOVED EVACUATION SLIDE AND CONTAINER PER MM 25-60-01-2. REPOSITIONED SLIDE IN CONTAINER AND INSTALLED PER MM 25-60-01-2. 2 L 7 4 4F RT 4A25 2008022800313 20080228 00313 NM 2008 2 28 DLM88080181 1 20080209 A 3230 MS22892 SCHRADER VALVE DOUG MD88 MD88 3023688 NM NLG DAMAGED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 909DL 49540 2SE GEAR UNSAFE LIGHT ON TAKEOFF. REPLACED SERVICE VALVE PERFORMED OPERATION 50006. JACKED AIRCRAFT, SWUNG GEAR OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2008022800361 20080228 00361 GL 2008 2 28 CHQA200800036 2 20080220 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 MAKING METAL A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 563RP 17892 9040 145509 CAE311620 CVG TO GSP - AFTER TAKEOFF, THE FLIGHT CREW REPORTED SMOKE IN THE CABIN AND THE AUTO SHUTDOWN OF ENGINE NR 1. THE AIRCR AFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED THE CMC FOR FAULT CODES AND FOUND MESSAGES FOR O IL DEBRIS, CONTROL SYS A AND B ALONG WITH ENG ITT SYS, E1 EXCEEDENCE. MAINTENANCE FOUND METAL DEBRIS ON THE CHIP DETECT OR AND AFTER FURTHER TROUBLESHOOTING THE NR 1 ENGINE WAS REPLACED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008022800368 20080228 00368 EA 2008 2 28 SWIA200819258 1 20080124 A 2497 RECEPTACLE CNDAIR CL600 CL6002D24 1390016 EA GROUND POWER SHORTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 800SK 15060 FLT 3780 - EXTERNAL GROUND POWER RECEPTICLE WAS SMOKING. COMPLIED WITH REPAIRS OF EXTERNAL POWER RECEPTICAL J150 PER CR J900 AMM 24-41-03-400-801-A01 AND CRJ900 SRM 51-42-06-001-001-A01. 2 L 7 2 4F RT A21EA 2008022800384 20080228 00384 NM 2008 2 28 SWAA081034 1 20080224 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800391 20080228 00391 2008 2 28 SWAA081024 4 20080222 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM EVAC SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2008022900005 20080229 00005 EA 2008 2 29 TRAX200800260 1 20080214 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 846AS 7328 EMERGENCY INTER. LIGHT AT MID CURE CEILING LIGHT AND OVERWING LIGHT AND BATTERY PACK NR 2 INOP. 2 L 7 2 4F RT A21EA 2008022900008 20080229 00008 EA 2008 2 29 TRAX200800104 1 20080117 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 844AS 7317 AAR - 1017 - I/B CLIP AT FS 280 LBL 9 CRACKED. REMOVED CRACKED LBL 9 I/B CLIP AT FS 280. REF FORM 412 FOR FABRICATION OF SERVICEABLE CLIP FOR LBL 9 I/B CLIP AT FS 280 REF REO 601R-53-11-171 FOR MATERIAL TYPE. INSTALLED SERVICEABLE CLIP I AW CRJ 200 SRM 51-42-21. SUPPLEMENTAL SDR CLOSED 2/13/08. 2 L 7 2 4F RT A21EA 2008022900016 20080229 00016 EA 2008 2 29 TRAX200800269 1 20080216 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 972EV 7534 RIGHT SIDE EXT EMERGENCY LIGHT HAS LIGHT BULB INOP. 2 L 7 2 4F RT A21EA 2008022900038 20080229 00038 EU 2008 2 29 NSVA2008007 1 20080224 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY MALFUNCTIONED A NSVA O OTHER N FALSE WARNING DE DESCENT 1 EA 27 251CJ 251 ON APPROACH LAV, SMOKE LIGHT ILLUMINATED, NO SMOKE OR FIRE NOTED. OPENED MEL 26-13-1. 2 L 7 2 4T RT A52EU 2008022900047 20080229 00047 EA 2008 2 29 VNAA0802001 1 20080203 A 3234 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 2 FAILED A VNAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 05 206PS 9769 7860 CREW REPORTED A GEAR DISAGREE MESSAGE ON APPROACH. CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE REM OVED AND REPLACED THE MLG SELECTOR VALVE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008022900065 20080229 00065 NM 2008 2 29 DHLA200800018 1 20080227 A 5753 SKIN BOEING 727 727227 1384078 NM TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 781DH 2693 977 BN55 21996 DURING PREFLIGHT WALKAROUND, FOUND TRAILING EDGE OF LEFT WING FLAP SPLIT OPEN. REMOVED AND REPLACED LT WING I/B TRAILIN G EDGE FLAP, OPS CK GOOD REF 727 MM 27-51-2. AIRCRAFT WAS GROUNDED. 2 L 7 3 4F A3WE 2008022900086 20080229 00086 EA 2008 2 29 TRAX200800297 1 20080221 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 867AS 7463 ON APPROACH TO LGA SELECTED FLAPS TO 8 AND RECEIVED FLAP FAIL CAUTION MSG. EN ROUTE TO LGA A/C DIVERTED TO JFK AFTER T/ O. EMERGENCY TRUCKS ROLLED. FLTS 4298, 4765 CX. 2 L 7 2 4F RT A21EA 2008022900098 20080229 00098 NM 2008 2 29 QXEA200800205 1 20080214 A 3350 6138001 BATTERY PACK BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY LIGHTS INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - EMERGENCY LIGHTS DO NOT COME ON WHEN SELECTED FROM THE FLIGHT DECK OR THE CABIN. MAINTENANCE REPLACED THE BATTERY PACKS AND THE RELAYS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008022900106 20080229 00106 NM 2008 2 29 DLM88080277 1 20080213 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE MISREPAIRED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 959DL 49978 DURING HMV AN INADEQUATE REPAIR WAS FOUND ON UPPER FUSELAGE SKIN BETWEEN STA Y=385 AND Y=393 LONGERON 8 AND 9 LT. A PER MANENT REPAIR WAS PERFORMED IAW SRM 53-04 FIG 12B. 2 L 7 2 4F RT A6WE 2008022900134 20080229 00134 EA 2008 2 29 TRAX200800304 1 20080222 A 5210 SKIN PANEL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 681BR 7680 AAR - PAX DOOR STAIRS, AFT SKIN PANEL IS CRACKED IN RADIUS UNDER STEP 832CT. 2 L 7 2 4F RT A21EA 2008022900135 20080229 00135 EA 2008 2 29 SWIA200819236 1 20080218 A 4940 IGNITER CNDAIR CL600 CL6002B19 1900309 EA APU UNKNOWN A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 495CA 7774 FLT 2585 - APU WOULD NOT START AND CABIN SMELLED OF FUEL. REPLACED BOTH IGNITER PLUGS WITH SERVICEABLE UNITS IAW AMM 49 -41-05. 2 L 7 2 4F RT A21EA 2008030300006 20080303 00006 WP 2008 3 3 AALA200800348 1 20080218 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 559AA 53089 LGA - EMERGENCY LIGHTS AT SEAT ROWS 14, 18, 21, AND 24 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT R OWS 14, 18, 21 AND 24. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300043 20080303 00043 NM 2008 3 3 2008UALA00528 1 20080130 A 5540 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LWR RUDDER DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 LOWER RUDDER DAMAGED. MAJOR REPAIR ACCOMPLISHED ON A/C. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030300045 20080303 00045 NM 2008 3 3 2008UALA00890 1 20080215 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 AFT CARGO DOOR CUTOUT LOWER FWD SIDE HAS INTERCOSTAL CORRODED AT FASTENER HOLES. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300046 20080303 00046 NM 2008 3 3 2008UALA00891 1 20080215 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 S7L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FORWARD ENTRY DOOR SURROUND STRUCTURE 2 CRACKS ON INTERCOSTAL AT BS 294.5 AND STRINGER S-7L. MAJOR REPAIR ACCOMPLISHED: REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300047 20080303 00047 NM 2008 3 3 2008UALA00892 1 20080215 A 3260 WARNING LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NLG FALSE INDICATION A UALA O OTHER N FALSE WARNING CL CLIMB 1 WP 29 382UA 24657 AFTER TAKEOFF, THE NLG DID NOT RETRACT. WITH THE GEAR HANDLE UP THE GREEN NOSE GEAR LIGHT WENT OFF BUT THE RED NOSE GEA R LIGHT STAYED ON. LOOKING THROUGH THE NOSE GEAR VIEWER, THE NOSE GEAR WAS STILL DOWN AND THE TWO RED ARROWS WERE STILL ALIGNED. THE GEAR HANDLE OPERATION WAS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300049 20080303 00049 EU 2008 3 3 08FDEA00649 1 20080228 A 5414 2210081167 SKIN AIRBUS 310 A310324 3930206 EU NR 1 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 ON THE NR 1 ENG AFT PYLON FAIRING, O/B MID SKIN PANEL ASSY IS CRACKED AT THE MID FRAME. REMOVED MID FRAME IAW SRM 51-40 -21; PGS 22 & 23; PARA 6. MATERIAL ID 2024- O .063 FOR THE PATCH & 2024-0 .071 FOR THE DOUBLER IAW SRM 54-55-51; P G 202. HEAT TREATED IAW TPS 1003 REV A. CUTOUT THE DAMAGE IAW SRM 54-55-51. FABRICATED DOUBLER & PATCH IAW SRM 54-55-51 . ALODINED IAW SRM 51-21-10. PRIMED IAW SRM 51-23-10. INSTALLED DOUBLER & PATCH IAW SRM 54-55-51 & SRM 51-41-21; PARA 6 HEAT TREAT LOAD NR HT0229081. 2 L 7 2 4F RT A35EU 2008030300053 20080303 00053 NM 2008 3 3 2008UALA00918 1 20080217 A 5753 FAIRING BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RIGHT WING PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 933UA 26659 RAMP REPORTS 5 MINS BEFORE DEPARTURE, RIGHT WING TRAILING EDGE FLAP TRACK FAIRING HAS PUNCTURE DAMAGE APPROX SIZE 5.5" B Y 5.5" APROX 30 INCHES FROM T-E. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300054 20080303 00054 EU 2008 3 3 2008UALA00834 1 20080214 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 424UA 506 EMERGENCY EXIT LIGHTS STUCK ON. RESET SYSTEM AND ACCOMPLISHED EMERGENCY LIGHT TEST, ALL OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030300055 20080303 00055 EU 2008 3 3 2008UALA00835 1 20080214 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 468UA 1363 MSG "ATA 33-51-38 EPSU BATTERY AFT L AND EPSU UNIT EMER R" CAME UP ON THE EMERGENCY LIGHT TEST PANEL AFTER THE EMERGENCY LIGHT TEST. RESET EMERGENCY LIGHT SYSTEM AND CIDS, ALL OPS TEST WERE PERFORMED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030300056 20080303 00056 EU 2008 3 3 2008UALA00836 1 20080214 A 2612 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AFT CARGO SMOKE FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 470UA 1427 AFT CARGO SMOKE LIGHT DOES NOT ILLUMINATE WHEN TESTED. DIRTY CONTACTS IN LIGHT ASSY. CLEANED CONTACT IN LIGHT ASSY, TE ST WORKS NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030300057 20080303 00057 2008 3 3 2008UALA00837 4 20080215 A 2565 D31591478U1 SLIDE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE R1 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 377UA 24642 FOUND DOOR 1R SLIDE COMING OUT OF HOUSING. FOUND GIRT RETAINER FLAP WAS DISLODGED FROM LOWER SIDE OF PACK BUSTLE. TUC KED FLAP BACK INTO PACK BUSTLE AND REINSTALLED DOOR SLIDE PACK ASSEMBLY. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300060 20080303 00060 NM 2008 3 3 2008UALA00840 1 20080215 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 116UA 26908 FOUND EMERGENCY LIGHT INOP, COCKPIT CEILING. RELAMPED. EMERGENCY LIGHT OP CHECKD GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030300061 20080303 00061 NM 2008 3 3 2008UALA00841 1 20080214 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 794-865 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FUSELAGE SKIN INTERNAL BEAR STRAP HAS 3 EA SMALL AREAS OF CORROSION AFT OF AFT PIT CARGO THRESHOLD BS 855-865 AND AT FWD SIDE OF THRESHOLD BTWN BS'S 794-807, JUST BELOW STR 25R LAP JOINT. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300062 20080303 00062 NM 2008 3 3 2008UALA00895 1 20080215 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 500 S28L/R CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FORWARD PIT BS 500+18 INCHES FUSELAGE INTERIOR SKIN CORRODED BETWEEN STRINGERS S-28L AND S-28R. MAJOR REPAIR ACCOMPLISH ED: FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300065 20080303 00065 NM 2008 3 3 AALA200800343 1 20080216 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 773AN 29583 JFK - EMERGENCY LIGHT AT SEAT 31C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 31C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008030300068 20080303 00068 NM 2008 3 3 AALA200800338 1 20080213 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 907AN 29509 TUL - EMERGENCY LIGHT BATTERY PACK FOR FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT STATION 500 FOR EMERGENCY LI GHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008030300069 20080303 00069 NM 2008 3 3 AALA200800340 1 20080216 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 361AA 24042 ORD - EMERGENCY EXIT LIGHT AT MID GALLEY RIGHT CEILING INOPERATIVE. REPLACED BATTERY LAMP FOR EMERGENCY EXIT LIGHT AT M ID GALLEY RIGHT CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008030300070 20080303 00070 NM 2008 3 3 AALA200800336 1 20080208 A 5311 FRAME BOEING 767 767323 1385205 NM BS 610 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 384AA 26996 AFW - CARGO FLOOR FRAME J INNER CHORD AT STATION 610 RIGHT BUTT LINE 7 TO 10 IN FORWARD CARGO HAS CORROSION ON BOTTOM SI DE AT NUTPLATE. REMOVED CORROSION FORM AFFECTED AREA PER SRM 59 00 07 1A AND APPLIED ALODINE AND PRIMER. REINSTALLED H ARDWARE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008030300071 20080303 00071 WP 2008 3 3 AALA200800339 1 20080216 A 2560 P4010021000 BATTERY DOUG DC9 DC982 3022082 WP FLASHLIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 477AA 49652 TPA - EMERGENCY FLASHLIGHT AT LOWER LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT LOWE R LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300074 20080303 00074 NM 2008 3 3 AALA200800345 1 20080217 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 349AN 33088 MIA - EMERGENCY LIGHTS AT SEAT ROWS 24B TO 32B INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT ROWS 24B TO 32B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008030300075 20080303 00075 NM 2008 3 3 AALA200800333 1 20080207 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 949AN 29537 TUL - EMERGENCY LIGHT BATTERY PACK FOR LEFT MID TO AFT CABIN FAILED TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT MID TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008030300078 20080303 00078 WP 2008 3 3 AALA200800367 1 20080221 A 3222 STRUT DOUG DC9 DC983 3022083 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 9409F 53121 DFW INFLIGHT T1033/21FEB, NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO DFW AND LANDED WITHOUT INCIDEN T. NOSE GEAR STRUT BOTTOMED OUT DURING TAXI TO GATE. ACCOMPLISHED NOSE LANDING GEAR SHOCK STRUT REPACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008030300080 20080303 00080 WP 2008 3 3 AALA200800363 1 20080220 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 477AA 49652 LGA - EMERGENCY LIGHTS AT OVERHEAD TAILCONE INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD RIGHT AFT LAVATORY FOR EMERG ENCY LIGHTS AT OVERHEAD TAILCONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300081 20080303 00081 WP 2008 3 3 AALA200800364 1 20080220 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 440AA 49459 TPA - EMERGENCY LIGHT AT FORWARD GALLEY IN FRONT OF FORWARD LAVATORY BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGH T AT FORWARD GALLEY IN FRONT OF FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300082 20080303 00082 EU 2008 3 3 AALA200800365 1 20080220 A 3350 321441 POWER SUPPLY AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 JFK - EMERGENCY EXIT LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED POWER SUPPLY UNIT FOR EMERGENCY EXIT LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008030300085 20080303 00085 WP 2008 3 3 AALA200800362 1 20080220 A 1100 PLACARD DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 477AA 49652 LGA - EMERGENCY EXIT PLACARD MISSING. REPLACED PLACARD FOR EMERGENCY EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300089 20080303 00089 EU 2008 3 3 2008UALA00846 1 20080214 A 2612 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO BAY NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 422UA 503 FAILED CARGO SMOKE TEST. IMPROPER TEST METHOD PER AMM. REPEATED TEST AND PASSED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030300091 20080303 00091 NM 2008 3 3 AALA200800358 1 20080220 A 3350 SOCKET BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 NRT EMERGENCY LIGHT AT FIRST CLASS COAT CLOSET INOPERATIVE. SECURED SOCKET FOR EMERGENCY LIGHT AT FIRST CLASS COAT CLOS ET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008030300093 20080303 00093 WP 2008 3 3 AALA200800375 1 20080221 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 577AA 53154 DFW - EMERGENCY LIGHT AT SEAT 8D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 8D. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300095 20080303 00095 WP 2008 3 3 AALA200800353 1 20080219 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70425 49337 LGA - EMERGENCY LIGHTS AT AFT LAVATORIES INOPERATIVE. RESEATED BATTERIES IN BATTERY PACKS FOR EMERGENCY LIGHT AT AFT LA VATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300096 20080303 00096 NM 2008 3 3 AALA200800352 1 20080219 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 768AA 33540 DFW - EMERGENCY LIGHTS AT RIGHT SEAT ROWS 20 TO 27 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 20 TO 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008030300098 20080303 00098 SO 2008 3 3 SWIA200819249 1 20080207 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS LOOSE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 297SW 120327 FLT 5465 - EMERGENCY EXIT SIGN ON FORWARD BULKHEAD IS INOP. RESECURED WIRING AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008030300099 20080303 00099 SO 2008 3 3 SWIA200819250 1 20080210 A 2897 WIRE EMB 120 EMB120ER 3260203 SO BURNED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 297SW 120327 AUXILLARY RELAY BOX SPLICE SPBG-08 SHOWS SIGNS OF OVERHEATING. REPLACED SPLICE SPBG-08 WITH A SERVICEABLE UNIT. 2 L 7 2 4T RT A31SO 2008030300100 20080303 00100 EA 2008 3 3 SWIA200819251 1 20080224 A 2913 PUMP CNDAIR CL600 CL6002D24 1390016 EA HYD SYSTEM LEAKING A SWIA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 807SK 15082 FLT 3785 - NR 2 EDP HYD CAUTION MESSAGE IN FLIGHT. QUANTITY AND PRESSURE AT ZERO. REPLACED RIGHT ENGINE DRIVEN HYDRAUL IC PUMP IAW AMM 29-11-01. OPS AND LEAK CHECK GOOD, P/N: 66190-05, S/N OFF: K0608. 2 L 7 2 4F RT A21EA 2008030300102 20080303 00102 EA 2008 3 3 SWIA200819253 1 20080220 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS LOOSE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 947SW 7786 FLT 6005 - LOWER EMERGENCY EXIT LIGHT BY THE MAIN CABIN DOOR DOES NOT WORK. RESECURED WIRING CONNECTORS FOR EMERGENCY L IGHTING. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008030300104 20080303 00104 NM 2008 3 3 HALA0800324 1 20080218 A 5420 CHANNEL BOEING 717 717200 1383700 NM NR 1 NACELLE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION NR 1 ENGINE SEVEN PLACES ON LOWER COWL CHANNEL NEAR GUIDE PIN HOLES. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008030300106 20080303 00106 WP 2008 3 3 AALA200800372 1 20080221 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 417AA 49328 DFW - EMERGENCY LIGHT AT SEAT 7D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300107 20080303 00107 NM 2008 3 3 08FDEA00635 1 20080227 A 5730 114N21041 PANEL BOEING 757 7572B7 1384964 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 LT WING L/E SKIN PANEL BY NR 2 SLAT O/B TRACK AREA IS CRACKED AT FASTENER HOLE. REMOVED SKIN PANEL IAW SRM 51-40-02. F ABRICATED NEW SKIN PANEL ON MAE TRAVELER NR T7/687621FROM 7075 - T6 - .050C IAW SRM 51-10-02. INSTALLED FABRICATED SKIN PANEL IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008030300109 20080303 00109 NM 2008 3 3 08FDEA00637 1 20080227 A 5320 146N542519 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 AFT CARGO COMPARTMENT AT STA 1400, LBL 2, THE FLOOR SUPPORT WEB IS CORRODED. REMOVED CORROSION, AREA IS L = 2", W = 1", D = 100 PERCENT OF MATERIAL THICKNESS. CORROSION IS OUT OF SRM 53-00-51, FIG 101, DETAIL III LIMITS. REMOVED WEB FROM STA 1400 TO 1420 IAW SRM 51-40-02. FABRICATED NEW WEB ON MAE TRAVELER NR T8/719345 FROM 7075-0 .032C, HEAT TREATED TO T3 IAW SRM 51-10-02. LOCATED, DRILLED TREATED AND PRIMED NEW WEB IAW SRM'S 51-40-05 AND 51-20-01. INSTALLED WEB IAW SR M 51-40-02. TOP COATED WEB IAW AMM 51-20-00. 2 L 7 2 4F RT A2NM 2008030300112 20080303 00112 NM 2008 3 3 08FDEA00640 1 20080228 A 5347 AFA7795501 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 CABIN BETWEEN STATION 1841 TO 1854, X = 8.5 , SEAT TRACK FOUND SURFACE CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPL ACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008030300113 20080303 00113 EU 2008 3 3 TRBA2008024 1 20080225 A 3350 3012000B POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 369AT 369 SEVERAL FLOOR PATH EMERGENCY LIGHTS STAYS ON WHILE SWITCH TURNED OFF. REMOVED AND REPLACED EMERGENCY POWER SUPPLY FIN N R 43WL IAW JIC NR 33-51-21. OPS CK OK. 2 H 7 2 4T RT A53EU 2008030300115 20080303 00115 NE 2008 3 3 ARWA20080204 2 20080223 A 7200 ENGINE DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 3 STALLED A ARWA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 19 478CT 79718 1899 47819 517171 DURING ROTATION, NR 3 ENGINE SUFFERED COMPRESSOR STALL AND THE TOWER AND VICINITY AIRCRAFT NOTED FIRE COMING OUT OF ENGI NE AFT END. REMOVED AND REPLACED NR 3 ENGINE IN ACCORDANCE WITH ARROW AIR WORK CARD 143R7101M AND DC-10 M/M 71-00-00. PERFORMED ENGINE RUN-UP AND LEAK CHECKED ALL NORMAL. ACCOMPLISHED BY F&E AIRCRAFT MAINTENANCE CRS F8ER232Y UNDER WORK OR DER 08-031. 2 L 7 3 4F 4 F RT A22WE E23EA 2008030300116 20080303 00116 NM 2008 3 3 QXEA200800226 1 20080220 A 3230 ROD END BOMBDR DHC8 DHC8402 1390042 NM MLG OUT OF ADJUST A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 409QX 4051 PDX - FLIGHT 2457, ON TAKEOFF, MAIN GEAR DOOR AMBER LIGHTS REMAINED ILLUMINATED. CYCLED THE GEAR PER THE CHECKLIST. TH E LIGHT WENT OUT. DIVERTED TO PDX AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REMOVED THE L/R MLG RETRACT ACTUA TOR AND ADJUSTED THE ROD ENDS AND RE-INSTALLED THE SAME ACTUATOR. PERFORMED EXTENSION AND RETRACTION IAW AMM 32-31-00-7 10-801. NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008030300117 20080303 00117 2008 3 3 WGEA200800030 4 20080219 A 2200 8350015016 AHRS ECLIPS EA500 ECLIPSEEA500 3350000 SW ZONE 200 MALFUNCTIONED E WGEA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 EA 27 142DJ 75 000056 ON CLIMB-OUT , AHRS FAILED AND STICK PUSHER FAILED. SUPPLEMENTAL INFORMATION, REMOVED AND INSTALLED AHRS NR 1 IAW EA 50 0 AMM 34-20-11. PERFORMED ATTITUDE AND DIRECTION SYSTEM ADJUSTMENT TEST FOR AHRS. SYSTEM CHECKS GOOD IAW 34-20-10. DU RING TROUBLESHOOTING ADC1 WAS ELECTRICALLY DISCONNECTED THEN RECONNECTED. PERFORMED FLIGHT ENVIRONMENT DATA ADJUSTMENT TEST FOR ADC IAW EA 500 AMM 34-10-00. ALL TESTS CHECK GOOD. VERIFIED TRANSPONDER NR 1 AND NR 2 COMPLIED WITH FAR 91.41 3 AND FAR PART 43 APPENDIX F. PERFORMED ALTITUDE REPORTING CORRELATION TEST PER PART (C) OF FAR 43 APPENDIX E. NO DATA CORRESPONDENCE ERRORS FOUND FOR TRANSPONDERS NR 1 OR NR 2. 1 L 7 2 4J RT A00002AC 2008030300119 20080303 00119 NM 2008 3 3 HALA0800347 1 20080221 A 5320 SILL BOEING 717 717200 1383700 NM FUSELAGE GOUGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 GOUGES ON NR 1,NR 2, NR 3 AND NR 4, AFT MED STOPS SILL SIDE. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008030400002 20080304 00002 NM 2008 3 4 2008UALA00898 1 20080215 A 2121 6455072 FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT RECIRC BURNED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 544UA 25322 ELECTRICAL BURNING ODOR IN FRONT HALF OF CABIN DURING PUSHBACK. RT RECIRC FAN BEARING FAILURE. REPLACED FAN. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030400004 20080304 00004 NM 2008 3 4 DL76G080269 1 20080222 A 2750 PSEU BOEING 767 767332 1382001 NM TE FLAPS MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 1602 29694 AFTER FLAPS UP AIRBORNE, GOT AN EICAS FLAP MSG AND A CONFIG WARNING LIGHT AND WARNING HORN. HORN AND LIGHT WENT OUT WHE N THROTTLES REDUCED BELOW 85 PERCENT. OPS NORMAL WITH FLAPS OUT OF UP POSITION. REMOVED AND REPLACED RELAY K215 AIR/GN D NLG SYS 2. BITE FSEU AND PSEU, NO FAULTS FOUND. CHECKED NOSE GEAR TARGET FOR DAMAGE ALL OK. REMOVED AND REPLACED PS EU PER AMM. NO FAULTS NOTED. ALL GND CHKS NORMAL. 2 L 7 2 4F RT A1NM 2008030400008 20080304 00008 WP 2008 3 4 IXXA08SMN017S 1 20080115 A 5420 FLANGE DOUG DC8 DC862F 3021972 WP RT NACELLE CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT COWLING AFT FLANGE CRACK STATION YN 181.000. REMOVED SPLICE CRACKED. FA BRICATED SPLICE. CLEANED, TREATED AND PRIMED REPAIR PART INSTALLED REPAIR PART IAW DC8 SRM 51-1-21, DC8 SRM 54-3-2 FIGU RE 33, BOEING MESSAGE NUMBER 1-763536571 DATED 02-05-08, AND DC8 SRM 51-1-8B. 2 L 7 4 4F 4A25 2008030400011 20080304 00011 WP 2008 3 4 IXXA08SMN020S 1 20080119 A 5753 SKIN DOUG DC8 DC863F 302198F WP TE FLAP MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD FLAP LOWER SURFACE HAS IMPROPER REPAIR AT STATION XW 59.000. REM OVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC 8 SRM 51-1-21, 51-1-11, DC8 SRM 57-7-1 FIGURE 1 ITEM "B" AND "L", DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, SRM 51-1-9 TR NUMB ER 51-142 DATED 04-05-06, DC8 SRM 51-1-9A TR NUMBER 51-141 DATED 04-03-06,AND DC8 SRM 51-1-8B. 2 L 7 4 4F 4A25 2008040800016 20080408 00016 SO 2008 4 8 FDKA200803119 1 20080319 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 852MJ 145567 FDM 5961 BUF-JFK (0645 PHX LCL). CREW REPORTED BURNING PLASTIC SMELL AT FLIGHT DECK WITH LEFT PACK ON. MX OPS CHECKED LEFT PACK NO EVIDENCE OF SMOKE. 2 L 7 2 4T RT T00011AT 2008040800022 20080408 00022 SO 2008 4 8 FDKA200803123 1 20080323 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 FDM 5967 JFK (1027 PHX LCL). THE 12A EMERGENCY LIGHT INOP. MX RE-SECURED CONNECTORS. 2 L 7 2 4T RT T00011AT 2008040800025 20080408 00025 EA 2008 4 8 COMA0860186 1 20080320 A 2610 355862255 LOOP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 477CA 7670 FLIGHT 5389 - RECEIVED ANTI-ICE WARNING MESSAGE, LEFT SIDE FUSELAGE. RETURNED TO CVG, LANDED WITHOUT INCIDENT. REPLACE D A15WK LOOP. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008040800031 20080408 00031 NM 2008 4 8 LYNX00010 1 20080321 A 3230 483023 SEQUENCE VALVE BOMBDR DHC8 DHC8402 1390042 NM NLG FAULTY A 3LYA O OTHER J WARNING INDICATION AP APPROACH 1 NM 21 501LX 4165 UPON LANDING AT DEN AND GO-AROUND, NOSE GEAR WOULD NOT CLEAR ON GEAR RETRACTION. ON SELECTION OF 'GEAR DOWN' NOSE GEAR INDICATOR DISPLAYED A RED GEAR UNSAFE LIGHT. GEAR EXTENDED AFTER MULTIPLE ATTEMPTS USING THE ALTERNATE LANDING GEAR EXT ENSION PROCEDURE. REMOVED AND REPLACED NOSE LANDING GEAR SOLENOID SEQUENCE VALVE IAW Q400 AMM 32-31-71-400-801. BLED N UMBER 2 HYD SYS IAW Q400 AMM 29-10-00-870-802. PERFORMED LG EXTENSION AND RETRACTION FC IAW Q400 AMM 32-31-71-720-002, 25 CYCLES. NO DEFECTS NOTED. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2008040800045 20080408 00045 SO 2008 4 8 FDKA200803126 1 20080324 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 860MJ 145773 FDM 6061 CVG-CHS (1348 PHX LCL). FUEL SMELL DURING BLEED TRANSFER TO APU. MX INSPECTED FOR FUEL LEAKS ON APU AND PERFO RMED BLEED OPERATIONAL CHECK, NO LEAKS OR EVIDENCE OF FUEL SMELL FOUND. 2 L 7 2 4T RT T00011AT 2008040800046 20080408 00046 NE 2008 4 8 DHLA200800038 2 20080404 A 7200 ENGINE BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 1 VIBRATION A DHLA C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 GL 05 742DH 36552 426 21290 700608 FLT NR 155 ON TAKEOFF ROLL LOUD BANG AUTO PACK TRIP AND ENG FAIL LIGHTS ILLUMINATE AT 70KTS. RTO, ALL ENG RUNNING W/IN NORM, PARAMETER. CLEARED AUTO PACK TRIP AND PERFORMED RTO FLOW CHART. NOTIFY MX CNTRL. ON TAXI BACK ENG NR 1 LOW OIL PRESS LIGHT ILLUMINATED W/PRESS AT 30 PSI. SECURED NR 1 ENG AND COMPLETED ENG FAIL EMERGENCY CHECK LIST (PENDING). AIR CRAFT WAS GROUNDED. 2 L 7 3 4F 4 F A3WE E2EA 2008040800048 20080408 00048 WP 2008 4 8 ARWA20080401 1 20080402 A 2424 GCU DOUG DC10 DC1030F 3023504 WP NR 1 MALFUNCTIONED A ARWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 29 450ML 47831 24-20-BD 1 BY 3 CHANNEL WILL NOT PARALLEL. RERACKED GCU 1 BY 3; OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH MM 24-20-00 . 2 L 7 3 4F RT A22WE 2008040800069 20080408 00069 SO 2008 4 8 C2XA08TY040 1 20080327 A 3350 375911 SIGN EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16918 145397 EMERGENCY EXIT SIGN AT ROW 12 INOP. REMOVED AND REPLACED EMERGENCY EXIT SIGN IAW EMB145 AMM 33-50-15. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008040800080 20080408 00080 NM 2008 4 8 HNAA0800119 1 20080322 A 3350 SIGN DHAV DHC8 DHC8102 2809003 NM CABIN DAMAGED A HNAA K NONE O OTHER UK UNKNOWN 1 EA 07 824EX 30313 30313 387 EMERGENCY EXIT SIGN BY AIRSTAIR DOOR FELL APART. MX REPLACED EMERGENCY EXIT SIGN. 2 H 7 2 4T RT A13NM 2008040800095 20080408 00095 EA 2008 4 8 COMA0860201 1 20080329 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A COMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 597SW 7293 FLIGHT 5301 - DURING DESCENT THROUGH 17,800FT AT 280 KTS INTO SRQ, RECEIVED FLAPS HALF SPEED MESSAGE FOLLOWED BY FLAPS F AIL CAUTION MESSAGE. FLAPS WERE AT 0 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. COMPLIED WITH TASK CARD SI- 2-27I0001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 2008040800126 20080408 00126 NM 2008 4 8 SWAA081765 1 20080401 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040800150 20080408 00150 NM 2008 4 8 SWAA081776 1 20080402 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040800153 20080408 00153 NM 2008 4 8 SWAA081778 1 20080402 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040800190 20080408 00190 SO 2008 4 8 C2XA08ON111 1 20080403 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO FWD CARGO BAY FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14177 7155 7155 14500888 FLT MX - ONT - WHILE PERFORMING 4 A-CHECK MX PERSONNEL WAS PERFORMING OP'S CHECKS ON FWD BAGGAGE SMOKE DETECTOR AND IT F AILED. MX PERSONNEL REMOVED AND REPLACED FWD CARGO SMOKE DETECTOR OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS REL EASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008040800198 20080408 00198 SO 2008 4 8 C2XA08SH058 1 20080407 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12136 145719 SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION ON FR 20. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FR 16-24 IA W EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008040900035 20080409 00035 NM 2008 4 9 AALA200800648 1 20080315 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 612AA 24488 MIA - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900050 20080409 00050 NM 2008 4 9 AALA200800631 1 20080313 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AA 24617 DFW - EMERGENCY LIGHT AT SEAT ROW 12DEF LENS BROKEN. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 12DEF. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900060 20080409 00060 NM 2008 4 9 AALA200800652 1 20080316 A 5220 416T28542 DOOR BOEING 767 767323 1385205 NM RT OVERWING MALFUNCTIONED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AA 25201 SFO - RIGHT OVERWING SLIDE DID NOT SUCCESSFULLY DEPLOY. UNABLE TO DEACTIVATE BOTTLE. OUTER DOOR DID NOT OPEN PROPERLY AT TIME OF SLIDE DEPLOYMENT. REPLACED RIGHT OVERWING SLIDE AND DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008040900063 20080409 00063 NM 2008 4 9 AALA200800653 1 20080316 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 DFW - EMERGENCY LIGHT AT SEAT 31C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900067 20080409 00067 2008 4 9 HALA0800492 4 20080404 A 2210 AUTOPILOT SYS BOEING 767 767332 1382001 NM MALFUNCTIONED A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, NO LAND 3 DISPLAYED ON ASA WITH CTR A/P SYS ENGAGED IN CMD, INTERMITTENT PROBLEM-RESETS AFTER ABOUT 5 MIN. PAST FAULTS. NO LAND 3 RA C AND NO LAND 3 R/A/FCC C BITE OF CENTER RADIC ALT CHECKS GOOD. PERFORMED TEST 40. ALL CHECKS GOOD. A/C LAND 3 STATUS. 2 L 7 2 4F RT A1NM 2008040900120 20080409 00120 EA 2008 4 9 SWIA200819439 1 20080329 A 3350 RELAY CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS FAULTY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 815SK 15101 FLT NR 4000 - THE EMERGENCY LIGHTS COME ON WHEN IN THE "ARMED" POSITION. REPLACED K135 RELAY IN JB11 IN ACCORDANCE WITH CRJ 900 MAINTENANCE MANUAL 20-00-00. CHECKS GOOD. 2 L 7 2 4F RT A21EA 2008040900127 20080409 00127 NM 2008 4 9 DLM88080534 1 20080403 A 5347 SEAT TRACK DOUG MD88 MD88 3023688 NM BS 641 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, BLEND OUT WAS FOUND OUT OF LIMIT ON SEAT TRACK AT STA Y=641 X=22. SEAT TRACK WAS REPAIRED IAW SRM 53-05 FIG 4A. 2 L 7 2 4F RT A6WE 2008040900155 20080409 00155 NM 2008 4 9 AALA200800694 1 20080321 A 2761 ACTUATOR BOEING 767 767323 1385205 NM NR 7 SPOILER LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 393AN 29430 SFO INFLIGHT T178/21MAR - CREW REPORTED RIGHT HYDRAULIC FLUID LOSS. RETURNED TO SFO AND LANDED WITHOUT INCIDENT. FOUND RIGHT WING INBOARD NUMBER SEVEN SPOILER ACTUATOR NUT BACKED OUT WITH LARGE FLUID LEAK. REPLACED NUMBER SEVEN SPOILER A CTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008040900164 20080409 00164 NM 2008 4 9 DLM88080541 1 20080403 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, GENERAL SURFACE CORROSION WAS FOUND ON FUSELAGE SKIN AT ANTENNA RADIO ALTIMETER SETTLING SURFACE. REMOVED C ORROSION IAW SRM 51-10-3D PARAGRAPH 35. REMAINING THICKNESS AT STA Y=655-750 WITHIN LIMIT IAW SRM 53-01 FIG 1 AT STA Y= 598-617 OUT OF LIMIT AND TO BE REPAIRED ON NRC T0088183. 2 L 7 2 4F RT A6WE 2008040900190 20080409 00190 NM 2008 4 9 2008UALA01856 1 20080402 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360-400 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 RADIO ALTIMETER ANTENNA CUTOUT IS INADEQUATE. ACCOMPLISHED COA 930011 REPAIR TO LOWER EXTERNAL FUSELAGE BS 360-400 & PR EVENTATIVE MODIFICATION TO RADIO ALTIMETER ANTENNA CUT-OUT AT BS 410, 430, AND 450. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041000001 20080410 00001 EU 2008 4 10 NSVA2008014 1 20080325 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 339-363 DAMAGED A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 249CJ 340B249 AFTER FLIGHT, ON-COMING CREW NOTICED FUSELAGE DAMAGE ON RT SIDE OF AIRCRAFT, HOLE IN THE SKIN, AND PROP BLADE DAMAGE. A IRCRAFT WAS FERRIED TO ALB FOR REPAIRS. RT PROP WAS REPLACED, EDDY CURRENT EXAMINATION OF IMPACT AREA ON FUSELAGE BETWE EN STATIONS 339 AND 363 SL 1615/1616. PERFORMED REPAIR TO FUSELAGE SKIN IAW SAAB REPAIR STATEMENT SDS014569 AND SAAB SR M 53-70-10. 2 L 7 2 4T RT A52EU 2008041000005 20080410 00005 CE 2008 4 10 NB089003 1 20080320 A 3397 WIRE HARNESS BEECH B300 B300 1159232 CE COCKPIT CHAFED B GSPD H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 05 143DK 2048 2048 FL309 WHEN THE PILOT WAS DOING A PREFLIGHT THE COCKPIT LIGHTING SYSTEM WAS TURNED ON, SMOKE AND FUMES COULD BE SEEN COMING FRO M THE COPILOTS EDGE LIGHTED C/B PANEL. POWER WAS TURNED OFF AND INVESTIGATION REVEALED ONE OF THE BRASS TRIM SCREWS THA T ATTACHES THE EDGE LIGHTED PANEL TO THE COCKPIT SIDE WALL WAS CHAFING THROUGH A POWER WIRE BEHIND THE PANEL. THIS CAUS ED THE SCREW TO GET HOT AND BURN THE LIGHTED PANEL ASSEMBLY P/N 90-364125-3. 2 L 7 2 4T RT A24CE 2008041000006 20080410 00006 EA 2008 4 10 MASA200800259 1 20080324 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 919FJ 15019 ASH FLT 2709 PHX-FAT. OVERHEAD EMERGENCY FLOOD LIGHT ROW 20 INOP. MX RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2008041000007 20080410 00007 EA 2008 4 10 MASA200800260 1 20080324 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 927LR 15027 ASH FLT 2609 EWR-CLT. CEILING EMERGENCY FLOOD LIGHT AT ROW 12 INOP & FLOOR LEVEL EMERGENCY FLOOD LIGHT AT PASSENGER DOO R HAS 1 BULB INOP. RELAMPED EMERGENCY LIGHTS. 2 L 7 2 4F RT A21EA 2008041000008 20080410 00008 EA 2008 4 10 MASA200800261 1 20080325 A 2560 0117981494 FIRST AID KIT CNDAIR CL600 CL6002C10 1390015 EA CABIN UNSERVICEABLE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 507MJ 4968 10077 ASH FLT 7191 IAD-CLT. FWD FIRST AID KIT SEAL BROKEN. MX CHANGED FIRST AID KIT. 2 L 7 2 4F RT A21EA 2008041000010 20080410 00010 EA 2008 4 10 MASA200800263 1 20080327 A 2560 SEAL CNDAIR CL600 CL6002B19 1900309 EA PBE BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 7337 ASH FLT 2721 PHX-SBA. AFT PBE SEAL WAS BROKEN. MX INSPECTED THE PBE AND INSTALLED A NEW SEAL. 2 L 7 2 4F RT A21EA 2008041000013 20080410 00013 EA 2008 4 10 MASA200800268 1 20080328 A 2560 MR10037N PBE CNDAIR CL600 CL6002B19 1900309 EA CABIN UNSERVICEABLE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 649BR 16558 7414 ASH FLT 7063 ORD-SBN. AFT AND FWD PBE VISUAL INDICATORS WERE POPPED. MX REPLACED BOTH PBE UNITS. 2 L 7 2 4F RT A21EA 2008041000016 20080410 00016 NE 2008 4 10 2008032701 2 20080327 A 7250 500310301 TURBINE BLADES PWA JT8D17A BOEING 727 727233 138408A NM PWA JT8 JT8D17A 52049 NE NR 3 ENGINE FAILED A PCSA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 17 495AJ 2929 709461 20937 709461 FLT 433 MIA-BLA - CREW REPORTED, LOSS POWER ON NUMBER NR 3 ENGINE ON TAKEOFF. THE CAPTAIN REJECTED TAKEOFF ROLL AT APPR OXIMATELY 10 KNOTS. AIRCRAFT RETURNED BACK TO AMERIJET LINE MAINTENANCE FACILITY WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MULTIPLE TURBINE BLADES FAILED AND ENGINE WAS BEYOND LINE MAINTENANCE REPAIR. ENGINE IS SCHEDULED FOR REPLACEMEN T AND DAMAGED ENGINE IS BEING SENT TO REPAIR FACILITY. SHOP BORESCOPE INSPECTION REVEALED T-1 VISIBLE BLADES ACCEPTABLE , T-2 BLADES DAMAGED, T-3 AND T-4 BLADES TOTALLY DESTROYED. CONCLUSION - BLADE FAILURES COMMENCED WITH T-3. 2 L 7 3 4F 4 F RT A3WE E2EA 2008041000017 20080410 00017 EA 2008 4 10 MASA200800271 1 20080329 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OBSTRUCTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77331 7331 FLT 7010, PIT-IAD. PAX DOOR WILL NOT CLOSE. MX REMOVED FOD AND GREASE FROM AREA, OP CHECK GOOD. 2 L 7 2 4F RT A21EA 2008041000019 20080410 00019 EA 2008 4 10 MASA200800273 1 20080329 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 902FJ 15002 ASH FLT 2934 FAT-PHX. CABIN CEILING LEVEL EMERGENCY FLOOD LIGHT 1 BULB INOPERATIVE. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2008041000024 20080410 00024 WP 2008 4 10 UPS08851942 1 20080229 A 5347 SAA78826011 SEAT TRACK DOUG DC8 DC873F 302199F WP CABIN GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 CABIN STA 1590 TO STA 1600 LBL 45 SEAT TRACK GOUGED. FABRICATED AND INSTALLED SEAT TRACK AT STA 1590 TO STA 1680 IAW DWG S-2400463, SRM 51-03-00, SRM 51-03-02, SRM 51-01-08, SRM 51-03-01, SRM 53-21-01-4. 2 L 7 4 4F RT 4A25 2008041000030 20080410 00030 SO 2008 4 10 RAIA00803022 1 20080325 A 3222 STRUT EMB 145 EMB145EP 3260221 SO NLG LOW A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 827HK 145021 FLT 5542 SPI - LANDING GEAR AIR/GROUND FAILURE MESSAGE ON THE EICAS AND THE GEAR WOULD NOT RETRACT. MAINTENANCE SERVICE D THE NLG STRUT AND PERFORMED SEVERAL GEAR SWINGS WITH NO FURTHER DEFECTS NOTED. 2 L 7 2 4F RT T00011AT 2008041000035 20080410 00035 NM 2008 4 10 08FDEA01316 1 20080406 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK CARGO DOOR LOWER DOOR JAMB SPOOL FITTING NR 1 FOUND THIRD LAYER CRACK INDICATION AFTER BORE TO MAXIMUM 0.519". REMOVED AND REPLACED PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041000037 20080410 00037 NM 2008 4 10 08FDEA01317 1 20080406 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK CARGO DOOR LOWER JAMB SPOOL FITTING NR 2 FOUND THIRD LAYER CRACK INDICATION AFTER BORE TO MAXIMUM 0.519". REM OVED AND REPLACED PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041000046 20080410 00046 EU 2008 4 10 08FDEA01322 1 20080407 A 5330 A53833104236 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND A DENT WITH TOOLING MARK BETWEEN C42-43, P10-11 LT REPAIR PERFORMED BY CUT OFF AFFECTED SKIN PART AND INSTALLING A INTERNAL DOUBLER IAW DRAWING R539-71110 AND SRM 53-10-14 FIG.201, APPROVED BY RAS/EFW/9000012/2008 ISS B AND EA 6-531 5-114872. 2 L 7 2 4F RT A35EU 2008041000051 20080410 00051 EU 2008 4 10 08FDEA01326 1 20080407 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT LT DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CHAFING MARK ON SLAT NR 1 LT LOWER SKIN, INNER RIB 20-22. REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW RAS /FOK/003/2008, APPROVED BY EA 6-5742-114860. 2 L 7 2 4F RT A35EU 2008041000064 20080410 00064 EU 2008 4 10 08FDEA01336 1 20080405 A 5330 A5377816020000 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 EXTERNAL FUSELAGE, FRAME 38, 4 INCHES ABOVE STRINGER 43 RIGHT, SMALL DENT ON RIVET. FOUND DENT TO BE OUT OF LIMITS IAW S RM 53-10-12, FABBED DOUBLER AND FILLER IAW SRM 53-10-12. REMOVED DAMAGE IAW SRM 53-10-12. ALODINED IAW SRM 51-21-10. PR IMED & PAINTED IAW SRM 51-23-10. INSTALLED REPAIR IAW SRM 53-10-12 & 51-40-21. NDT ACCOMPLISHED PER NTM 51-10-08. NO FUR THER DAMAGE NOTED. 2 L 7 2 4F RT A35EU 2008041000067 20080410 00067 NM 2008 4 10 08FDEA01337 1 20080407 A 5347 143N5080 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 640 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 SEAT TRACK DAMAGED AT BS 640, LBL 24.75, MAIN CABIN. REMOVED SEAT TRACK ASSY IAW SRM 51-40-02. FABRICATED REPLACEMENT SEAT TRACK ASSY FROM BAC1520-792/24 IAW SRM 53-30-02. INSTALLED REPLACEMENT SEAT TRACK ASSY, FROM BS 440-640, LBL 24.75 , IAW SRM 51-40-02. REPLACEMENT OF SEAT TRACK ASSY WAS REQUIRED DUE TO NUMEROUS AREAS AT SEAT TRACK LUGS WORN BEYOND LI MITS. THIS IS CLASSIFIED AS A MAJOR REPAIR DUE TO REPLACEMENT OF PSE BY FABRICATION MEANS. 2 L 7 2 4F RT A2NM 2008041000070 20080410 00070 EU 2008 4 10 08FDEA01340 1 20080402 A 5310 A53772636208 DOOR FRAME AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 FWD CARGO COMPT DOOR FRAME 20A FOUND DENTED BETWEEN STGR 31-32 RT. FRAME WAS REPAIRED IN ACCORDANCE WITH EA 6-5310-11732 3. 2 L 7 2 4F RT A35EU 2008041000073 20080410 00073 EU 2008 4 10 USAA920080715 1 20080331 A 2761 31077100 ACTUATOR AIRBUS 320 A320231 3930325 EU NR 3 SPOILER MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 621AW 32719 18325 53 FLT 343 - PHX - PVR - AIR TURNBACK - AFTER APPROXIMATELY 45 MINUTES INTO FLIGHT, CREW REPORTED LOSS OF BLUE HYDRAULIC SY STEM. AIRCRAFT RETURNED TO PHX. MAINTENANCE REMOVED AND REPLACED THE RIGHT NR 3 SPOILER ACTUATOR, SYSTEM OPERATIONAL C HECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008041000080 20080410 00080 NM 2008 4 10 NWAA081416303 1 20080405 A 3397 CONNECTOR BOEING 747 747451 1384940 NM EMERGENCY LIGHT LOOSE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 663US 23818 DURING INSPECTION, FOUND EMERGENCY EXIT SIGNS INOP OVER ROWS 22 THROUGH 30. MAINTENANCE CORRECTED THE PROBLEM BY SECURI NG A LOOSE CONNECTOR AT ROW 22. 2 L 7 4 4F RT A20WE 2008041000088 20080410 00088 NM 2008 4 10 08FDEA01348 1 20080408 A 5330 AJC7060506 SKIN DOUG MD11 MD11F 3023600 NM BS 2144-2164 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 AFT FUSELAGE, RIGHT EXTERNAL SKIN AT STA 2144 TO STA 2164, FOUND EXFOLIATION CORROSION AT LOWER EDGE OF FIXED FAIRING (347DF) MOUNTING AREA. CORROSION REMOVED PER SRM 51-31-01 VOLUME II. ORIGINAL THICKNESS = 0.095", MATERIAL REMOVED = 0.058", REMAINING THICKNESS = 0.037" AND FOUND EXCEEDED LIMIT PER SRM 53-20-00 FIGURE 13 VOLUME I. REPAIR CARRIED OUT PER SRM 53-20-00 FIGURE 13 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041000089 20080410 00089 NM 2008 4 10 08FDEA01349 1 20080408 A 5347 AEA73256 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1310-1365 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK SEAT TRACK FLANGE BELOW FLOOR PANEL NR 263LF AND 263FF AT STA 1310 TO STA 1365, X = -8 FOUND CORROSION AT UPPE R SURFACE AT 3 LOCATIONS. CORRODED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REP AIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041000092 20080410 00092 EU 2008 4 10 08FDEA01352 1 20080408 A 5711 A57110431200 SPAR AIRBUS 300 A300B4622R 3930312 EU WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CRACKS IN CENTER SPAR WEB VARIOUS LOCATION (HOLE 2, 3, 5, 7) REPAIR PERFORMED BY OVERSIZING THE HOLES AND INSTALLI NG A BUSH IN HOLE 5 IAW RAS057091/022/2007 ISS A, APPROVED BY EA 6-5710-114861. 2 L 7 2 4F RT A35EU 2008041000096 20080410 00096 EU 2008 4 10 NWAA081403230 1 20080406 A 3350 BATTERY AIRBUS 320 A320211 3930320 EU EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 330NW 307 COM EMERGENCY LIGHT FWD FAULT ON CIDS. REPLACED FWD LEFT EPSU BATTERY, EMERGENCY LIGHTS CHECK GOOD. 2 L 7 2 4F RT A28NM 2008041000105 20080410 00105 NM 2008 4 10 Q2SA746006 1 20080406 A 3411 0856CC12 PITOT TUBE BOEING 747 747206B 1384856 NM DEFECTIVE A Q2SA J A DUMP FUEL UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 EA 63 746SA 21111 ON DEPARTURE, CAPTAIN AND FIRST OFFICER'S ALTIMETER SPLIT 500 FEET, AIRSPEED SPLIT 30 KTS. WHEN ALTERNATE STATIC SELECT ED ON CAPTAIN'S SIDE, ALL INSTRUMENTS MATCHED UP. DURING ILS FLIGHT, ALTITUDE SHOWED 1800 FEET AT 6.3 DME (SHOULD HAVE BEEN 1600 FEET). REMOVED/REPLACED LOWER AUXILIARY PITOT TUBE IN ACCORDANCE WITH AMM 34-11-01. 2 L 7 4 4F RT A20WE 2008041000108 20080410 00108 NM 2008 4 10 SWAA081741 1 20080331 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041000110 20080410 00110 NM 2008 4 10 SWAA081742 1 20080331 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 456WN 32463 R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2008041000118 20080410 00118 NM 2008 4 10 SWAA081750 1 20080329 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED MV1 CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 28R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008041000119 20080410 00119 NM 2008 4 10 SWAA081751 1 20080329 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED MV1 CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 28L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008041000120 20080410 00120 NM 2008 4 10 NWAA081446310 1 20080327 A 5311 FRAME BOEING 747 747451 1384940 NM FUSELAGE MISMANUFACTURED A NWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 01 670US 24225 DURING "M" CHECK, THE BS 320 CROWN FRAME WEB WAS FOUND TO BE 0.080 INCH THICK INSTEAD OF BLUEPRINT THICKNESS OF 0.140. REPAIRED PER EA 63-212555 SECTION I SECTION II REQUIRES DAMAGE TOLERANCE ANALYSIS TO BE ACCOMPLISHED BY MARCH 2009. 2 L 7 4 4F RT A20WE 2008041000123 20080410 00123 NM 2008 4 10 SWAA081760 1 20080331 A 5310 6516352 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 2008041000125 20080410 00125 NM 2008 4 10 SWAA081759 1 20080331 A 5313 6551698 STRINGER SPLICE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 663, STR 3L. REPAIRED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2008041000131 20080410 00131 NM 2008 4 10 SWAA081746 1 20080331 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008041000134 20080410 00134 NM 2008 4 10 BB08045 1 20080330 A 2560 P4010021 BATTERY BOEING 757 7572B7 1384964 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 935UW 27201 CLT - EMERGENCY FLASHLIGHT AT DOOR 3R IS NOT FLASHING. MAINTENANCE REPLACED BATTERY IN FLASHLIGHT AT DOOR 3R. OPERATIO NALLY CHECKS OK. 2 L 7 2 4F RT A2NM 20080902 NM 2008 9 2 SWAA084678 1 20080825 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND STRINGER 25R CORRODED AT BS 727D. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084618 1 20080820 A 5311 6516301 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084617 1 20080820 A 3350 65C27093 LIGHT BOEING 737 7373Q8 1384670 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080902 WP 2008 9 2 AALA200801882 1 20080715 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 3515 49892 LGA - EMERGENCY LIGHT AT RT AFT LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RT AFT LAVATORY. SY STEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F A6WE 20080902 NM 2008 9 2 AALA200801880 1 20080715 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 319AA 22320 JFK - EMERGENCY LIGHT AT RT SIDE BUSINESS CLASS INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RT SIDE BUS INESS CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A1NM 20080902 NM 2008 9 2 AALA200801885 1 20080715 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AM 24594 DFW - EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. REPINNED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECK ED NORMAL OPERATION. (S) 2 L 7 2 4F RT A2NM 20080902 EU 2008 9 2 AALA200801888 1 20080621 A 3350 LENS AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 40064 507 MIA - EMERGENCY LIGHT AT SEAT 25C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED N ORMAL OPERATION. (S) 2 L 7 2 4F RT A35EU 20080902 NM 2008 9 2 AIEA200800263 1 20080708 A 5350 FAIRING BOEING 747 74747UF 1384812 NM FUSELAGE DAMAGED A AIEA O OTHER O OTHER NR NOT REPORTED 1 GL 11 408MC 29261 DURING ARRIVAL WALKAROUND INSPECTION FOUND LOWER RT AFT OF BODY GEAR FUSELAGE FAIRING DAMAGED. ACCOMPLISHED TIME LIMITED REPAIR AS PER EO 4453A188 DATED 7/8/08 ENTERED NON MEL DMI N08-037 FOR REPEAT INSPECTION OF PANEL AT EVERY A-CHECK. (A) 2 L 7 4 4F RT A20WE 20080902 NM 2008 9 2 ARWA20080801 1 20080805 A 5270 WARNING SYSTEM DOUG DC10 DC1040F 3023507 NM PAX DOOR MALFUNCTIONED A ARWA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 29 140WE 46920 ATC REPORT FOR DOOR OPEN ON ACFT. RETURN TO RAMP. INSPECTED ACFT. FOUND NO DOOR OPEN, NORMAL CONDITION IAW WITH MM 52 -00-00. ALL CLOSED AND LIGHT OFF. (S) 2 L 7 3 4F RT A22WE 20080902 SO 2008 9 2 C2XA08IA180 1 20080728 A 3320 BR90002 BALLAST EMB 145 EMB145EP 3260221 SO CABIN LIGHTS INOPERATIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 13929 145009 IAH - FLIGHT 2938 - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED A BURNING SMELL AT ROW 18. MAINTENANCE INSPECTED TH E AIRCRAFT, FOUND A BAD BALLAST AT SEAT 18A. THE BALLAST WAS DISCONNECTED AND THE LIGHT PLACED ON MAL 33-20-00/1 CAT C CONTROL NUMBER 151397 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 08/03/08 MAINTENANCE REMOVED AND REPLACED THE LIGHT BALLAST FOR ROW 18, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE ACFT WAS APPROVED FOR RET URN TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080902 SO 2008 9 2 C2XA08IA193 1 20080808 A 4920 APU EMB 145 EMB145LR 3260212 SO SMOKE A C2XA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 15985 145248 IAH - FLIGHT 2749 - DURING PRE-FLIGHT THE CREW REPORTED SMOKE IN THE COCKPIT WHEN THE APU WAS STARTED, AND THE CREW SHUT DOWN THE APU. MAINTENANCE INSPECTED ACFT, OPERATIONALLY CHECKED THE APU WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROV ED FOR RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080902 SO 2008 9 2 C2XA08SH109 1 20080819 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16183 14500914 SHV - DURING C-CHECK LT OMEGA BEAM LOWER FLANGE HAS CORROSION BETWEEN FR 20-24. MAINTENANCE REPAIRED LT OMEGA BEAM LOWE R FLANGE BETWEEN FR 20-24 IAW EMB 145 XR SRM 53-00-10 FIGURE 201 SHEET 2. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080902 SO 2008 9 2 C2XA08IA179 1 20080715 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15986 145254 MCI - DURING MAINTENANCE INSPECTION THE SECOND AND THIRD AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENA NCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080902 SO 2008 9 2 C2XA08ON167 1 20080809 A 2611 SMOKE WARNING EMB 145 EMB145XR 3260214 SO CARGO BAY FALSE ACTIVATION A C2XA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 27 14162 11268 6213 14500808 FLT 0023 - OKC - FLIGHT CREW REPORTED BAGGAGE SMOKE INDICATION ON EICAS. SYSTEM WAS RESET AS PER MAINTENANCE CONTROL IN STRUCTIONS. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4F RT 20080902 SO 2008 9 2 C2XA08SH095 1 20080711 A 5320 14521700007 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14514 145303 SHV - DURING C-CHECK LT OMEGA BEAM FR 21-23 HAS VARIOUS AREAS OF CORROSION ON LWR FLANGE WEB. MX REMOVED LT OMEGA BEAM FROM 17 SPLICE TO FR 26 AND INSTALLED WITH NEW IAW EC5320-01413 ANS CPM 51-21-06. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080902 NM 2008 9 2 SWAA084572 1 20080815 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 797MX 27890 DURING SCHEDULED HC2 CHECK, LT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084507 1 20080814 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CREASED AT BS 947, STR 25R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084520 1 20080814 A 5313 6551698 STRINGER SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 380, STR 28L. REPAIRED SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20080902 EA 2008 9 2 CHQA200800153 1 20080722 A 2910 601R7528655 LINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE HYD SYSTEM LEAKING A CHQA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 11 466CA 7627 GEE873331 FLIGHT 5581, IND TO IAH. DURING CRUISE THE FLIGHT CREW RECEIVED A HYD 2 SYS LOW PRESS MESSAGE. THE HYDRAULIC PAGE WAS BROUGHT UP IT WAS CONFIRMED THAT THE SYSTEM WAS INDICATING 0% QUANTITY AND VERY LOW PRESSURE. THE QRH PROCEDURES WERE F OLLOWED, AND THE FLIGHT DIVERTED TO KBNA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE HYDRAULIC SYSTEM A ND FOUND A PIN-HOLE IN THE SYSTEM 2 HYDRAULIC LINE GOING THROUGH THE AFT EQUIPMENT BAY. THE HYDRAULIC LINE WAS REPLACED ALONG WITH THE HYDRAULIC PUMP AND THE SYSTEM LEAK AND OPS CHECKED GOOD. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080902 NM 2008 9 2 SWAA084519 1 20080814 A 5313 6551698 STRINGER SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 380, STR 27L. REPAIRED SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084518 1 20080814 A 5313 6551698 STRINGER SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 27L. REPAIRED SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20080902 SO 2008 9 2 CHQA200800123 1 20080624 A 3397 WIRE EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL EMERGENCY LIGHT BROKEN A CHQA O OTHER O OTHER NR NOT REPORTED 1 GL 11 271SK 145305 CAE311922 FLIGHT 7805, IAW TO CMH. THE FLIGHT CREW NOTED THAT THE RIGHT EXTERIOR EMERGENCY LIGHT WAS INOP. MAINTENANCE SLAVED IN A NEW BULB, INVERTER AND BATTERY PACK WITH NO FIX. MAINTENANCE FOUND WIRE W122-8274-22 BROKEN. THE WIRE WAS REPAIRED AND THE EMERGENCY LIGHT OPERATED NORMALLY. (A) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080902 EU 2008 9 2 COEA0804816 1 20080805 A 5312 S53174000200 BULKHEAD AEROSP ATR72 ATR72212 8680945 EU FUSELAGE NICKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 816FX 26364 347 TOOL DAMAGE TO FWD SIDE OF FWD PRESSURE BULKHEAD. THREE SMALL NICKS FOUND AT THE LT UPPER RADOME BONDING CONTACT POINT. S/D HC AT COE. S/D SRM REPAIR, BLENDED OUT DAMAGE AND INSTALLED REPAIR DOUBLER TO THE BULKHEAD WEB. (S) 2 H 7 2 4T RT A53EU 20080902 CE 2008 9 2 DXTA200803208 1 20080730 A 2750 FLAP SYSTEM CESSNA 680 680CE 2076811 CE TE FLAPS MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 305QS 6800088 A "FLAPS FAIL" CAS MESSAGE ON FLAP RETRACTION, FLAPS WILL NOT EXTEND. (A) 2 L 7 2 4F RC T00012WI 20080902 NM 2008 9 2 F3LA200800538 1 20080728 A 5320 D5348015900700 BLANKING PLATE AIRBUS A319 A319111 3930336 NM GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2 2209 DURING C-CHECK, INSP NOTED THE R2 FWD GIRT BAR BLANKING PLATE HAD CORROSION. MAINT REMOVED AND REPLACED CORRODED R2 DOO R FWD GIRT BAR FITTING BLANKING PLATE IAW AMM 52-13-31-400-007. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUN D ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080902 CE 2008 9 2 GLB2008F00016 1 20080817 A 3610 REGULATOR BEECH 1900 1900D 1154162 CE PNEUMATIC SYS MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 03 240GL UE240 ACFT 240GL AIR RETURN FLT 5087 "DEN" 08/17/08 PILOTS REPORTED THE PNEUMATIC PRESSURE WAS EXCEEDING REDLINE DURING CLIMB OUT AT FULL POWER SETTINGS. MAINTENANCE ADJUSTED PNEUMATIC REGULATOR AS REQUIRED IAW 1900D MM 36-00-01. OPERATIONAL CH ECK WAS GOOD. 2 L 7 2 4T RT A24CE 20080902 NM 2008 9 2 KCSA081365 1 20080731 A 5414 SKIN BOEING 747 747259B 1384804 NM NR 3 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 NR 3 PYLON SKIN OUTBOARD SIDE EXTENDING FROM DOUBLER CRACKED 3 INCHES. (A) 2 L 7 4 4F RT A20WE 20080902 NM 2008 9 2 SWAA084479 1 20080813 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080902 EA 2008 9 2 MAS2008F00011 1 20080803 A 3597 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77331 7331 ASH FLT 7330 SAV-IAD. CARGO BOTTLE LOW CAUTION MESSAGE. RE-SECURED LOOSE CONNECTOR TO LT BOTTLE. (S) 2 L 7 2 4F RT A21EA 20080902 NM 2008 9 2 QXEA200800919 1 20080815 A 3240 216052 BRAKE BOMBDR DHC8 DHC8402 1390042 NM MLG SMOKE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 19 416QX 4083 SEA - LT SIDE BRAKE SMOKING AFTER TAXI TO THE GATE. MAINTENANCE REPLACED BOTH LT BRAKES AND TIRES. OPERATIONAL CHECKS GOOD. RETURNED TO SERVICE. (S) 2 H 7 2 4T RT A13NM 20080902 SO 2008 9 2 RAIA00806028 1 20080630 A 3150 WARNING LIGHT EMB 145 EMB145 3260210 SO THRUST REVERSER ILLUMINATED A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 803HK 145077 FLT 3562 - STL - ENGINE 1 THRUST REVERSER DISAGREE MESSAGE ON THE EICAS DURING CLIMB. MAINTENANCE DEFERRED THE NUMBER 1 THRUST REVERSER PER MEL PROCEDURES. WD:CL HD:J AT:A 2 L 7 2 4F RT T00011AT 20080902 NM 2008 9 2 SWAA084461 1 20080812 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 25L CORRODED AT BS 967. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084459 1 20080812 A 3350 101331 LENS BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084458 1 20080812 A 3350 65C27093 LIGHT BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084451 1 20080812 A 3350 65C27093 LENS BOEING 737 7373K2 13844BA NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080902 2008 9 2 SWAA084450 4 20080812 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084449 1 20080812 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 12R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 USAABB08129 1 20080806 A 2150 A/C PACK BOEING 767 7672B7 1385107 NM ZONE 100 MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 252AU 24765 PHL FLT 755 EN ROUTE PHL TO CLT, ON CLIMBOUT FROM PHL, THE "L PACK OFF" LIGHT ILLUMINATED WITH A CORRESPONDING "L PACK O FF" EICAS MESSAGE. THE CREW SELECTED STANDBY FOR THE LT PACK, BUT THE STATUS DID NOT CHANGE. SINCE THE RT PACK WAS ALR EADY ON MEL, THE ACFT WOULD NOT PRESSURIZE. THE FLIGHT RETURNED TO FIELD PHL AND LANDED WITHOUT FURTHER INCIDENT. MAIN TENANCE REPLACED THE LT PACK REHEATER. OPERATIONALLY AND LEAK CHECKS OK. (S) 2 L 7 2 4F RT A1NM 20080902 NM 2008 9 2 SWAA084442 1 20080810 A 5311 6546540 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084441 1 20080810 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 USAAEMB08010 1 20080812 A 2560 P4010030 BATTERY EMB ERJ190 ERJ190100IGW 3260408 NM FLASHLIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 960UW 19000173 PHL - FORWARD FLIGHT ATTENDANT FLASHLIGHT WOULD NOT CHARGE. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY. (S) 2 L 7 2 4F RT A57NM 20080902 NM 2008 9 2 USAA920081330 1 20080604 A 5522 SKIN BOEING BOEING 737 73733A 1384673 NM RT ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 7494 23627 MCN-C21-MAJOR REPAIR-NR 6108144- DELAMINATION ON RIGHT HAND ELEVATOR LOWER SURFACE AT ELEVATOR STATIONS 94 TO 121. REPA IRED RIGHT HAND ELEVATOR LOWER SURFACE AT ELEVATOR STATIONS 94 TO 121 IAW US AIRWAYS EA 130064 (B) 2 L 7 2 4F RT A16WE 20080903 EU 2008 9 3 USAA920081514 1 20080811 A 5320 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 PIT-S4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR18 & FR20, WL 208.10, Y254. REPLACED FLOORBEAM AT FR18 & FR20, WL 208.10, Y254 IAW A319 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080903 NM 2008 9 3 2008UALA03765 1 20080707 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26877 FOUND DENT IN SKIN FWD OF MED 1L APPROX 12 INCHES BELOW WATER LINE 119.8 (THRESHOLD) & 6 INCHES AFT OF SKIN JOINT AT STA 406. *S/D* MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL DOUBLER. 2 L 7 4 4F 4 F RT A20WE E24NE 20080903 NM 2008 9 3 2008UALA03486 1 20080619 A 5315 141T5814 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 246 LBL11 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 66885 27112 MAIN CABIN FLOORBEAM AT BS 246, AFT FACE UPPER ANGLE CRACKED, LBL 11. *S/D* FOUND UPPER CHORD CRACKED. REMOVED DAMAGE , FABRICATED NEW UPPER CHORD AND INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F 4 F RT A1NM E24NE 20080903 NM 2008 9 3 2008UALA03496 1 20080619 A 3610 32153024 VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 ENGINE FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 226UA 30226 NR 2 ENGINE PRSOV FAILED HEALTH CHECK. *S/D* NR 2 ENGINE PRSOV FAILED HEALTH CHECK. REPLACED PRSOV PER MM 36- 11-18 4 01, OPS TEST GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080903 NM 2008 9 3 2008UALA03497 1 20080620 A 3610 339910230 CONTROLLER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 1 ENG BLEED FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 226UA 30226 NR 1 ENG PRSOV CONTROLLER FAILED. *S/D* NR 1 ENGINE PRSOV CONTROLLER FAILED. INSTALLED NEW PRSOV CONTROLLER, OPS CHEC K GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080903 NM 2008 9 3 2008UALA03445 1 20080617 A 5315 143T5132 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE MAIN CABIN UPPER WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 66885 27112 MAIN CABIN FLOORBEAM UPPER SURFACE HAS WEAR MARKS AROUND FASTENER HOLE AT BS 764 BETWEEN RBL 20 AND RBL 54. *S/D* SUSP ECT TOOLING MARKS. REMOVED DAMAGE AREA, FABRICATED AND INSTALLED REPAIR IAW SRM 53-00-51 FIG 201 TABLE I. AC OK FOR SE RVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080903 NM 2008 9 3 2008UALA03455 1 20080616 A 4930 4417614 FUEL SYS BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE APU FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 794UA 26953 APU SYS MSG DISPLAYED PRIOR DEPT MNT MSG 49-1042- DISPLAYED FIM 49-30 TASK 802 FAULTS APU WIRE HARNESS OR FUEL CLUSTER. *S/D* FOUND FAULTY FUEL CLUSTER. REPLACED APU FUEL CLUSTER PER AMM 49-31-31. OP CHECKED GOOD. VERIFICATION FLIGHT C ONFIRMS NORMAL OPERATION OF THE SUBJECT SYSTEM. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080903 NM 2008 9 3 2008UALA03466 1 20080618 A 5280 STRUCTURE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT NLG DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 66885 27112 LT FWD NLG DOOR SKIN HAS A LIGHTNING STRIKE APROX 17 INCHES AFT OF LEADING EDGE OF DOOR AND 7.75 INCHES FROM INBOARD EDG E OF DOOR. *S/D* FOUND LIGHTNING STRIKE IN NOSE LANDING GEAR DOOR. REMOVED DAMAGE TO LT FWD NLG DOOR AND INSTALLED CO MPOSITE REPAIR PER SRM 52-80-02. PAINTED PER GN-MM 5-0-4-020. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080903 NM 2008 9 3 KCSA081413 1 20080820 A 5412 BULKHEAD BOEING 747 747132 1384882 NM NR 1 NACELLE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 709CK 20247 NR 1 PYLON HAS CHAFED DAMAGE AT NAC STA 221.9 AT HYDRAULIC PRESSURE LINE. (S) 2 L 7 4 4F RT A20WE 20080903 NM 2008 9 3 QXEA200800348 1 20080330 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAPS WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 356PH 502 PDX-C5 CHECK- LT NR 3 FLAP TRACK HAS SEVERAL AREAS OF WEAR ON THE LOWER HORIZONTAL TRACK UPPER SURFACE APPROX .500 INCHE S BY .300 INCHES BY .010 DEEP. BLENDED AFFECTED AREAS ON NR 3 FLAP TRACK LOWER HORIZONTAL UPPER IAW RD8-57-987. HFEC I NSPECTED BLENDED AREAS FOR CRACK IAW D8 200 NDTM PART 6 51-00-01, NO CRACKS NOTED. MEASURED BLENDED AREA AND FOUND TO B E WITHIN LIMITS. FORWARD BLEND 0.005 INCHES WAS REMOVED. 0.003 INCHES WAS REMOVED FROM AFT BLEND. APPLIED DRY FILM LU BE IAW RD8-57-987. (S) 2 H 7 2 4T RT A13NM 20080903 SO 2008 9 3 C2XA08SH108 1 20080817 A 5755 14567066401 BRACKET EMB 145 EMB145LR 3260212 SO LT SPOILER WORN A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 16571 145633 SHV - DURING C-CHECK, THE LT GROUND SPOILER CENTER HINGE BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHI NGS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080903 NM 2008 9 3 KCSA081414 1 20080820 A 5320 INTERCOSTAL BOEING 747 747249F 1384849 NM BS 660-680 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 INTERCOSTAL UPPER FLANGE BENT BETWEEN BS 660 TO BS 680. (S) 2 L 7 4 4F RT A20WE 20080903 EU 2008 9 3 USAA920081548 1 20080819 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 647AW 762 FLT 251 PHL-PHX-EEL- AFT CABIN EMERGENCY EGRESS LIGHTING INOPERATIVE DURING CABIN EMERGENCY LIGHTS TEST. MAINTENANCE RE MOVED AND REPLACED THE AFT EMERGENCY POWER SUPPLY BATTERY. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080903 EU 2008 9 3 USAA920081549 1 20080816 A 2913 4607 O-RING AIRBUS 320 A320231 3930325 EU HYD PUMP DEFECTIVE A USAA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 19 632AW 81 FLT 710 IND-PHX-HYDRAULIC LOSS- HYDRAULIC YELLOW ENG PUMP LOW PRESSURE INDICATION - YELLOW SYSTEM FLUID GONE. MAINTENAN CE REMOVED AND REPLACED O-RING ON CHECK VALVE 3094GM. OPERATIONAL AND LEAK CHECKS WERE GOOD. (S) 2 L 7 2 4F RT A28NM 20080903 NM 2008 9 3 USAA920081543 1 20080808 A 5320 PAN BOEING 737 7373B7 1384580 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT-Q6 -MAJOR REPAIR- LEVEL 2 EXFOLIATION CORROSION ON RT LAV PAN AT BS 1016, RBL 25 TO RBL 26. REPAIRED RT LAV PAN AT BS 1016, RBL 25 TO RBL 26 IAW B737 SRM 51-70-13. (S) 2 L 7 2 4F RT A16WE 20080903 NM 2008 9 3 USAASB08067 1 20080820 A 2560 P4010021 BATTERY BOEING 737 7374B7 1384702 NM FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 453UW 24980 PHL - MAINTENANCE REPORTED, THE FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE F LASHLIGHT BATTERY. OPERATIONAL CHECK NORMAL. (S) 2 L 7 2 4F RT A16WE 20080903 NM 2008 9 3 UIEA200800287 1 20080815 A 5311 FRAME BOEING 747 7472D7B 1384803 NM BS 380 CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 524MC 21784 BS 380 FRAME WEB AT STRINGER 17L & 17R CRACKED. REPAIRED IAW SERVICE REQUEST 1911068869 APPROVED BY FAA FORM 8100-9 DAT ED 6 AUG 2008, DETAILS OF WORK KEPT AT ENGINEERING ORDER EO 4753B184. (S) 2 L 7 4 4F RT A20WE 20080903 NM 2008 9 3 QXEA200800708 1 20080711 A 2130 8201003005 ECU BOMBDR DHC8 DHC8402 1390042 NM CABIN PRESSURE FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 09 409QX 1169 4051 PDX - FLIGHT 2461 (SEA-MDR) DIVERTED TO PDX FOR A CABIN PRESSURE WARNING LIGHT. UNEVENTFUL LANDING. MAINTENANCE COULD NOT GET ECS CODES TO COME UP. REPLACED THE ECS ECU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 H 7 2 4T RT A13NM 20080903 NM 2008 9 3 QXEA200800701 1 20080701 A 6123 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM NR 2 ENGINE MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 400QX 4030 PDX - FLIGHT 2241 - NR 2 ENGINE FAILS AUTO FEATHER TEST. FOUND PEC FAULT CODES 402, 422 AND 424. CLEARED BY FIM. PERF ORMED TWO GROUND RUNS AND 6 AUTO FEATHER TESTS WITH NO DEFECTS. RETURNED TO SERVICE. NO PARTS REPLACED. (A) 2 H 7 2 4T RT A13NM 20080903 SO 2008 9 3 C2XA08SH106 1 20080817 A 5320 14525480003 SILL EMB 145 EMB145LR 3260212 SO CARGO DOORWAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16571 145633 SHV - DURING C-CHECK THE CARGO DOOR LOWER SILL CUTOUT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE LO WER SILL CUTOUT STRUCTURE IAW EMB 145 SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080903 NM 2008 9 3 KCSA081415 1 20080820 A 5730 SKIN BOEING 747 747122 1384872 NM LT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 716CK 19753 LT WING LOWER SKIN HAS CORROSION ON UPPER SURFACE AT LES 884. (S) 2 L 7 4 4F RT A20WE 2008041000135 20080410 00135 WP 2008 4 10 08FDEA01297 1 20080404 A 5311 AFA00303 FRAME DOUG DC10 DC1010F 3022111 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION ON UPPER FUSELAGE AT STA 1781 LT STRINGER 13 FOUND FRAME WITH CRACK 5 INCHES LONG. REPAIRE D FOR SRM 53-30-00 FIG 5 SECT. 2 L 7 3 4F A22WE 2008041000146 20080410 00146 NM 2008 4 10 08FDEA01309 1 20080404 A 5347 BAC1520792 SEAT TRACK BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 MAIN DECK, SEAT TRACK I/B FLANGE CORRODED, BS; 1110 - 1130, RBL 45 REMOVED CORROSION AND SEAT TRACK IS OUT OF LIMITS. F ABRICATED NEW SEAT TRACK, DRILLED, TREATED AND PRIMED AND INSTALLED. REFERENCE BOEING DOCUMENT NR 65-86245/ID 000 FR AME NR 2 SRM 51-10-2/PAGE 2 AND SRM 51-30-2/ PAGE 2. CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008041000151 20080410 00151 NM 2008 4 10 UPS08551959 1 20080402 A 3350 CONTROL PANEL BOEING 757 75724APF 1384969 NM COCKPIT FAULTY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 448UP 27737 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS ILLUMINATED WITH SWITCH IN OFF POSITION, SWITCH LOOSE. REPLACED PILOT'S EMERG ENCY LIGHTS CONTROL PANEL, OPS NORMAL. REF AMM 33-51-08-4. 2 L 7 2 4F RT A2NM 2008041000154 20080410 00154 2008 4 10 UPS08851951 4 20080331 A 2565 LANYARD DOUG DC8 DC873F 302199F WP EVAC SLIDE DISCONNECTED A IPXA K NONE O OTHER UK UNKNOWN 1 SO 01 803UP 46073 INSPECTION TYPE:N/A EMERGENCY SLIDE WILL NOT ATTACH TO FLOOR. DEFERRED IAW MEL 52-7-4, M372513 INSTALLED. RECONNECTED INFLATION LANYARD TO QUICK - DISCONNECTION FITTING IAW MM 25-60-01-2. THIS CLEARS M372513. REMOVED PLACARD. 2 L 7 4 4F RT 4A25 2008041000157 20080410 00157 NM 2008 4 10 HALA0800517 1 20080406 A 3150 WARNING SYSTEM BOEING 767 767332 1382001 NM FALSE INDICATION A HALA O OTHER N FALSE WARNING DE DESCENT 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM, ON DESCENT-EICAS MESSAGE FWD CABIN TEMP DISPLAYED AND INOP DISCRETE ILLUM TEMP SW SELECTED OFF PER QRH. FOUND ZONE TEMP BITE MESSAGE, PER FIM 21-61-00 FIG 103 BITE ZONE TEMP CONTROLLER, VERIFIED RESET, MESSAGE CLE ARED, OPS CHK OK, NO FAULTS NOTED. 2 L 7 2 4F RT A1NM 2008041000165 20080410 00165 CE 2008 4 10 DXTA20082979 1 20080404 A 2120 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 921QS 7500241 DURING GEAR RETRACTION, CABIN SPIKED 4000 FPM (CLIMB) AND A STRONG ENVIROMENTAL BURNING SMELL APPEARED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008040800160 20080408 00160 EA 2008 4 8 COMA0860206 1 20080401 A 5610 NP13932110 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A COMA K NONE O OTHER CR CRUISE 1 SO 01 487CA 13384 7729 FLIGHT 5664 - F/O'S WINDSHIELD SHATTERED COMPLETELY EN ROUTE TO SAV. AIRCRAFT LANDED SAFELY IN SAV. REMOVED AND REPLAC ED F/O'S WINDSHIELD. 2 L 7 2 4F RT A21EA 2008040800172 20080408 00172 NM 2008 4 8 SWAA081795 1 20080403 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 444WN 29839 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008040800186 20080408 00186 NM 2008 4 8 SWAA081805 1 20080403 A 5311 6546543 BELTFRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 663, STR 2L. REPAIRED BELTFRAME PER SRM. 2 L 7 2 4F RT A16WE 2008040800192 20080408 00192 SO 2008 4 8 C2XA08IA100 1 20080331 A 3397 3025103 WIRE EMB 145 EMB145LR 3260212 SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12563 145612 MCI - DURING MAINTENANCE INSPECTION THE RIGHT SIDE OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENAN CE RE-SECURED THE WIRES ON THE AFFECTED EMERGENCY EXIT LIGHT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WA S APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008040800193 20080408 00193 SO 2008 4 8 C2XA08IA101 1 20080402 A 2910 792249 CONTROL PANEL EMB 135 EMB135LR 3260305 SO COCKPIT MALFUNCTIONED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14516 145323 IAH - FLIGHT 2339, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED SMOKE TO BE COMING FROM THE OVERHEAD HYDRAULIC PANEL. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC CONTROL PANEL, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT W AS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008040800205 20080408 00205 2008 4 8 SWAA081816 4 20080405 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 221WN 34259 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008040800215 20080408 00215 NM 2008 4 8 SWAA081822 1 20080406 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040900002 20080409 00002 EU 2008 4 9 MALA080051 1 20080331 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 294 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 457XJ 340B457 SEAT TRACK REPAIR ANGLES CORRODED STA 294 - BL 0 AND BL18.3 AND SUPPORT FRAME. SEAT TRACK REPAIR ANGLES REPLACED AT STA 294 - BL 0 AND BL 18.3 AND SUPPORT FRAME IAW EO NR S53342 AND SRM 51-40-21. 2 L 7 2 4T RT A52EU 2008040900027 20080409 00027 NM 2008 4 9 AALA200800628 1 20080313 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900042 20080409 00042 NM 2008 4 9 AALA200800621 1 20080221 A 5320 143T82053 SILL BOEING 767 767323 1385205 NM BS 592 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 359AA 24040 FORWARD CARGO DOOR LOWER SILL SECTION HAD CORROSION AT THE VERTICAL INBOARD SIDE AT STATION 592. REPAIRED CORROSION PER SRM 53-00-15 AND MRB 767 3140. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080903 NM 2008 9 3 USAA920081541 1 20080812 A 5320 654656018 PLATE BOEING 737 7373G7 1384595 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN-C19 -MAJOR REPAIR- EXFOLIATION CORROSION ON SEAL PLATE AT BS 947, S26L TO S26R. REPAIRED SEAL PLATE AT BS 947, S26L TO S26R IAW B737 SRM 51-40-02-0G. (S) 2 L 7 2 4F RT A16WE 20080903 EU 2008 9 3 USAA920081530 1 20080817 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 767UW 21692 2185 1382 FLT 1645 DCA-TPA- EMERGENCY EQUIPMENT- RT MID CABIN EMERGENCY POWER SUPPLY UNIT FAULT. REMOVED AND REPLACED POWER SUPPL Y. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080903 NM 2008 9 3 USAA920081546 1 20080817 A 5315 6545834 STIFFENER BOEING 737 7373B7 1384580 NM FLOORBEAM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT-Q6 -MAJOR REPAIR- CRACK ON FLOORBEAM WEB VERTICAL STIFFENER AT BS 328, BL 0. REPLACED FLOORBEAM WEB VERTICAL STIFFE NER AT BS 328, BL 0 IAW B737 SRM 51-10-02. (S) 2 L 7 2 4F RT A16WE 20080903 EA 2008 9 3 SIMA200823301 1 20080818 A 5610 601R3303318 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 522AE 10147 ON FLIGHT 4133 CREW REPORTED THE FIRST OFFICER`S SIDE WINDOW SHATTERED IN FLIGHT WHEN FLYING OVER STL. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED FIRST OFFICER`S SIDE WINDOW. ACFT RETURNED TO SERVICE. (S) 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 SWAA086466 1 20081121 A 5315 BAC1509100146 SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO BAY FLOORBEAM SUPPORT CORRODED AT BS 727D + 6, LBL 8. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086474 1 20081121 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086489 1 20081121 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086493 1 20081121 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 EU 2008 11 25 COEA0809917 1 20081024 A 5751 S57610170200 RIB AEROSP ATR42 ATR42300 8680920 EU LT AILERON CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 917FX 354 FOUND AT COE LEVEL 2 CORROSION. CORROSION ON LT WING AILERON HORN ATTACHMENT RIB. 2 H 7 2 4T RT A53EU 20081125 NM 2008 11 25 SWAA086464 1 20081121 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 26L TO 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086428 1 20081120 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STR 25L CORRODED AT BS 985. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843747 1 20081022 A 5230 65C329541 SKIN BOEING 737 7374Q8 138447Q NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 BELOW AFT CARGO DOOR LARGE DENTS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW B737 40 0 SRM 53 00 01 REPAIR 31. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843748 1 20081028 A 5347 65538449 CARGO TRACK BOEING 737 7374Q8 138447Q NM CARGO BAY DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 CARGO TRACK TIE DOWN HAS DAMAGED LUGS STA 787. REMOVED DAMAGED SECTION OF TRACK, FABRICATED AND INSTALLED REPLACEMENT T RACK PLATES ANGLES IAW B737 400 SRM 53 00 50 REPAIR 2 FIG 201. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0873712 1 20081109 A 5320 453A26111 PLATE BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 CORROSION ON AFT CARGO FWD RT FLOOR PLATE. REMOVED AND REPLACED FLOOR PLATE. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0853772 1 20081114 A 3040 8300005604 SENSOR BOEING 737 737890 1384527 NM WINDOW HEAT MALFUNCTIONED A ASAA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 NM 02 559AS 8473 35178 ON PREFLIGHT WINDOW HEAT OVERHEAT LIGHT ON RIGHT SIDE ILLUMINATES WITH SWITCH ON. CONFIRMED, WHCU SHOWS SENSOR FAULT. SWAPPED TO SECOND SENSOR REF MM 30 41 00 810 812. OPS CHECK R2 WINDOW HEAT GOOD REF MM 30 41 00 710 801. FVR FOR WINDO W HEAT SUCCESSFUL. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0853754 1 20081105 A 3040 8300005604 CONTROL UNIT BOEING 737 737890 1384527 NM WINDOW HEAT FAULTY A ASAA K NONE J WARNING INDICATION NR NOT REPORTED 1 NM 02 559AS 8418 35178 RIGHT SIDE WINDOW HEAT OVERHEAT LIGHT ILLUMINATED, TRIPPED MASTER CAUTION ANTI ICE. AMBER OVERHEAT LIGHT ILLUMINATED GR EEN ON LIGHT EXTINGUISHED. RIGHT SIDE WINDOW WAS COOL TO THE TOUCH. LEFT SIDE WINDOW WAS WARM TO TOUCH (APPROX 8 000 F T ALG). TURNED RIGHT SIDE HEAT OFF FOR APPROX 2 MIN. TURNED SWITCH BACK ON OVERHEAT LIGHT ILLUMINATED AGAIN, APPROX 3 TO 4 MIN LATER. VERIFIED FAULT NR 2 WINDOW HEAT INOP, PERFORMED FIM 30 41 00 810 801 FOUND P5 CONTROL POWER FAULT. CKD VOLTAGE ALL NORMAL. RERACKED WHCU SYSTEM OPS NORMAL. FVR FLIGHT FOR RIGHT SIDE WINDOW HEAT PASSED. 2 L 7 2 4F RT A16WE 20081126 NE 2008 11 26 ASAA0853756 2 20081111 A 7200 CFM567B27 ENGINE BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE NR 2 SURGES A ASAA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 02 559AS 8473 8473 35178 89227 RIGHT ENGINE N1 SURGE AT 32FL DURING CLIMB. REDUCED POWER AND RETURNED TO ANC. ENGINE REPLACEMENT IN PROCESS. WILL BE SENT TO GE FOR ANALYSIS. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081126 EA 2008 11 26 ASOA200801509 1 20081115 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 920EV 7810 FLT 5379 - EMERGENCY DECLARED, FLAP FAIL CAUTION MSG ON APPROCH WHEN SELECTING 8 DEG FLAP, FLAP FAIL AT ZERO. 2 L 7 2 4F RT A21EA 20081126 EA 2008 11 26 ASOA200801510 1 20081115 A 2560 BATTERY CNDAIR CL600 CL6002C10 1390015 EA MEGAPHONE LOW A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 379CA 10102 F/A REPORTS MEGAPHONE BATTERY IS LOW. 2 L 7 2 4F RT A21EA 20081126 NM 2008 11 26 DHLA2008745694 1 20081114 A 5743 SUPPORT BEAM BOEING 727 727224 1384076 NM LT MLG CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LT MLG TRUNNION SUPPORT BEAM HAS CORROSION IN AND AROUND LOWER PANEL ATTACH HOLES, LWBL 80.5 TO 124.2. ACCOMPLISHED REP AIR TO SUPPORT BEAM AS REQUIRED, IAW COOPESA EO COO-2-57-387-08 DATED 10/27/08. REF FAA FORM 8110-3 DATED 11/06/08 AND ASTAR EVA B257-00060 FOR REPAIR APPROVAL. DOCUMENTED ON COOPESA N/R 1-651. 2 L 7 3 4F A3WE 20081126 EA 2008 11 26 ASOA200801531 1 20081118 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION DE DESCENT 1 SO 27 680BR 7679 FLT 5575 - FLAPS FAIL MESSAGE ON DESCENT, WHEN SELECTING 8 DEGREES. FAILED AT ZERO. EMERGENCY VEHICLES ROLLED AS A PRE CAUTION. 2 L 7 2 4F RT A21EA 20081126 2008 11 26 SWAA086547 4 20081121 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086548 1 20081122 A 3350 101114 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 352SW 24888 FOUND LT EMERGENCY EXIT LIGHT INOP. R&R LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081126 EA 2008 11 26 ASOA200801540 1 20081119 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 927EV 7844 PAX DOOR AFT WEB IS CRACKED IN STEP JOINT RADIUS (832DT AND 832CT) AND (832CT AND FIX MID STEP). 2 L 7 2 4F RT A21EA 20081126 NM 2008 11 26 SWAA086549 1 20081123 A 3233 654491032 ACTUATOR BOEING 737 7373H4 1384600 NM RT MLG FAILED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 29 353SW 24889 AIRTURNBACK, AFTER TAKEOFF RT MLG DID NOT RETRACT. ONE ATTEMPT TO RECYCLE LANDING GEAR LEVER DID NOT FIX PROBLEM. R&R RT RETRACT ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086550 1 20081121 A 3350 PL22300 STRIP BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND LT EEPLS STRIP DAMAGED. R&R STRIP PER MM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086551 1 20081121 A 3350 PL22300 STRIP BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND R/H EEPLS STRIP DAMAGED. R&R STRIP PER MM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086552 1 20081123 A 3350 PL22300 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 455WN 32462 DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS STRIP COVER BROKEN AT ROW 1. R&R STRIP PER MM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086553 1 20081120 A 3350 101114 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 463WN 32467 FOUND LT EMERGENCY EXIT LIGHT COVERS LOOSE. R&R COVER PER MM. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 K11A2008112072302 1 20080409 A 5311 FRAME BOEING 727 7272H3 138368N NM BS 211 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 FRAME, CORROSION TO BE OUT OF LIMITS STA 211 APPROX 19 INCH FROM CABIN FLOOR. 2 L 7 3 4F RT A3WE 20081128 NM 2008 11 28 K11A2008112072303 1 20080417 A 5330 SKIN BOEING 727 7272H3 138368N NM BS 1362 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 SKIN CORROSION, 4 INCHES ABOVE NR 2 ENG RT SIDE. 2 L 7 3 4F RT A3WE 20081128 NM 2008 11 28 K11A2008112072305 1 20080410 A 5311 FRAME BOEING 727 7272H3 138368N NM BS 227 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 FRAME, CORROSION OUT OF LIMITS STA 227R 16 INCHES OFF CABIN FLOOR. 2 L 7 3 4F RT A3WE 20081128 NM 2008 11 28 K11A2008111772202 1 20080918 A 5320 TEE FITTING BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 722CK 20948 LOWER TEE CHORD OTBD FLANGE UPPER SURFACE CORRODED BETWEEN FRAME WEBS AT STA 302-312, LBL 16, WL 149. CORROSION 1 BY 2 INCHES. 2 L 7 3 4F RT A3WE 20081128 NM 2008 11 28 DL757081585 1 20081118 A 5610 141T480119 WINDOW BOEING 757 757232 1384965 NM COCKPIT CRACKED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 673DL 25978 WHILE SUPERTUG WAS TOWING A/T AND AMT WAS RIDING BRAKES L1 COCKPIT WINDOW SUDDENLY CRACKED FROM TOP TO BOTTOM. THERE WA S NO DEFINITE CAUSE. THERE WAS SOME DELAMINATION NEAR THE POINT THE CRACK STARTED. 2 L 7 2 4F RT A2NM 20081128 EA 2008 11 28 ASOA200801523 1 20081116 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 713EV 10081 SEAT TRACK HAS SCATTERED CORROSION THROUGH OUT CABIN AT LBL9. REMOVED AND REPLACED LBL 9 FORWARD SEAT TRACK IAW SRM 51- 41-06. 2 L 7 2 4F RT A21EA 20081128 NM 2008 11 28 08FDEA04948 1 20081120 A 5347 141N51313 SEAT TRACK BOEING 757 75728A 1384976 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 912FD 24260 SEAT TRACK STA 418-440 LBL 45 GOUGED AND CORRODED. REMOVED, REPLACED, TREATED AND PRIMED NEW FABRICATED SEAT TRACK ON M AE TRAVELER NR T8-769420 AND INSTALLED ON STA 418 -440 LBL 45 IAW SRM 51-40-02. THIS IS A NR 1 REPAIR CAT A. 2 L 7 2 4F RT A2NM 20081128 NM 2008 11 28 08FDEA04949 1 20081120 A 5347 141N51313 SEAT TRACK BOEING 757 75728A 1384976 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 912FD 24260 SEAT TRACK STA 418-440 LBL 24 GOUGED AND CORRODED. REMOVED, REPLACED, TREATED AND PRIMED NEW FABRICATED SEAT TRACK ON M AE TRAVELER NR T8-769431 AND INSTALLED ON STA 418-440 LBL24 IAW SRM 51-40-02 NR 1 REPAIR CATEGORY A. 2 L 7 2 4F RT A2NM 20081128 EU 2008 11 28 08FDEA04940 1 20081120 A 5270 WARNING LIGHT AIRBUS 310 A310203 3930313 EU MLG DOOR ILLUMINATED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 21 427FE 362 ON TAKEOFF ROLL KBDL LOWER ACCESS DOOR LT CAME ON AT 70KTS RTO AND RETURN TO RAMP WITH LTS ON ECAM AFT LOWER ACCESS DOOR OPENED AND CLOSED LIGHTS WENT OUT. DOOR IS CLOSED AND LOCKED. NOTE: TSI OPENED TO RECHECK DOOR 136AR. 2 L 7 2 4F RT A35EU 20081128 NM 2008 11 28 ASAA0843797 1 20081029 A 5320 6517688165 SILL BOEING 737 7374Q8 138447Q NM BS 277-360 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 L1 DOOR CUTOUT SILL BEAM CHORD IS CORRODED. REMOVED CORRODED CHORD REPLACED SILL BEAM CHORD IAW B737 400 SRM 51 40 02 B DRAWING 65 17688 AND ASA EA 400 53EA 00208. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0873836 1 20081118 A 5321 146A940121 FLOOR PANEL BOEING 737 737790 13844CN NM BS 887 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 AFT CARGO FLOOR PANEL SPLICE PLATE CORRODED. R&R FLOOR PANEL SPLICE STRIP AFT CARGO BAY BS 887 RBL 20 LBL 9. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0853866 1 20081121 A 2160 6228145 CONTROLLER BOEING 737 737890 1384527 NM CABIN TEMP WARNING LIGHT A ASAA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 02 577AS 6697 35186 UPON RECALL AIR COND LT ILLUMINATES AND RIGHT PACK LT ILLUMINATES. PERFORMED FIM TASK 21 62 00. BITE CK PACK ZONE TEMP CONTROLLER. BITE TEST CHECK OK. NO HISTORY PAST 30 NOTED. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0853873 1 20081121 A 2997 CONNECTOR BOEING 737 737890 1384527 NM NR 2 HYD PUMP DIRTY A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 587AS 4318 35684 WHILE ACCOMPLISHING OPS CHECK OF NR 2 ENGINE AFTER ENGINE CHANGE NOTED ENGINE DRIVEN PUMP WILL NOT SHUT OFF CLEANED CONN ECTOR PER SWPM 20-60-01. OPS CK GOOD. VERIFIED HYD PUMP SHUTS OFF DURING GROUND RUN REF AMM 29-11-11-710-015-002. 2 L 7 2 4F RT A16WE 20081128 EA 2008 11 28 ASOA200801552 1 20081123 A 2560 MEGAPHONE CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 748EV 10158 CABIN MEGAPHONE INOP. 2 L 7 2 4F RT A21EA 20081128 NM 2008 11 28 08FDEA04950 1 20081121 A 5311 6516343 FRAME BOEING 727 7272S2F 1384O81 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 216FE 22937 FOUND AFT PIT FRAME REPAIR LOCATED AT APPROX BS 1050 STR S-27L TO 26L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETER MINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EVALUATION DETERMINED INSUFFICIENT FASTENERS. REMOV ED REPAIR SRM 51-30-2, VERIFIED MATERIAL FOR REPLACEMENT AND FABRICATED REPLACEMENT REF DWR 65-16343 A35227 PO 1041113. HEAT TREATED NR 8130 2008-11-08. DRILLED AND FINAL TRIM DOUBLER REF SRM 51-30-3 FIG 1. TREATED AND PRIMED PARTS REF S RM 51-10-2. INSTALLED DOUBLER REF SRM 51-70-3. FAB REPAIR ANGLE REF DWR 65-67276-50 MATERIAL A 66622 PO 1008655 INSTAL LED REPAIR ANGLE SRM 51-30-6. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081128 EA 2008 11 28 ASOA200801553 1 20081123 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 GI GALLEY LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS. 2 L 7 2 4F RT A21EA 20081128 EA 2008 11 28 ASOA200801488 1 20081110 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 LOWER FUSELAGE SKIN FROM FS 559.00 TO FS 559.00+112 STR 23L TO 25R HAS CORROSION DAMAGE AROUND FASTENER HOLES ON EXTERNA L SURFACE AND EXTERNAL SKIN SURFACE APPROX DEPT .009. 2 L 7 2 4F RT A21EA 20081128 EA 2008 11 28 ASOA200801489 1 20081110 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 LT LOWER FUSELAGE SKIN HAS CORROSION DAMAGE AROUND FASTENER HOLES AT FS 559+80 TO 559.00+96 STR 19L - 20L, APPROX .003 D EEP. 2 L 7 2 4F RT A21EA 20081128 EA 2008 11 28 ASOA200801490 1 20081110 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 RT FUSELAGE LOWER SKIN HAS CORROSION DAMAGE AROUND FASTENER HOLES AT FS 559.00+80 TO 559+112 STR 21R TO 23R, APPROX DEPT .003. 2 L 7 2 4F RT A21EA 2008040900051 20080409 00051 WP 2008 4 9 AALA200800639 1 20080314 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7519A 49896 LGA - EMERGENCY LIGHT AT OVERHEAD FIRST CLASS LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHE AD FIRST CLASS LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008040900062 20080409 00062 WP 2008 4 9 IXXA08SMN084S 1 20080215 A 5330 564932975N1 SKIN DOUG DC8 DC871F 302199D WP BS 1690-1890 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 822BX 92877 2986 458133 DURING ROUTINE C CHECK, FOUND AT EXTERNAL DOUBLER AFT LOWER FUSELAGE BELLY TAIL SKID FAIRING HAS IMPROPER REPAIR AT STAT ION FS 1745 LONGERON 35.5 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAG ED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR P ARTS AT STATION FS 1690.000 TO STATION FS 1890.000 IAW DC8 SRM 53-5-1 FIGURE 1 ITEM "E", BOEING MESSAGE 1-756217773-2 DA TED 01/22/08, DC8 SRM 53-1-0 PAGE 1, DC8 SRM 51-1-21, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008040900069 20080409 00069 NM 2008 4 9 HALA0800493 1 20080401 A 5314 KEELBEAM BOEING 767 76733A 1385209 NM BS 960 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 587HA 33421 LEVEL 1 CORROSION FOUND O LWR KEEL BEAM CHEN-MILLED HORIZONTAL WEB AT STA 960, BETWEEN RBL 9.5 AND LBL 9.5. CORROSION R EMOVED WITHIN LIMITS IAW SRM 53-50-12/A01 REV 76 AND SURFACE AREA RESTORED, ALODINE, PRIMED, CPC APPLIED. 2 L 7 2 4F RT A1NM 2008040900075 20080409 00075 NM 2008 4 9 08FDEA01274 1 20080403 A 5347 AEA732515 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK SEAT TRACK FLANGE AT STA 1470, X = -75 FOUND EXFOLIATION CORROSION. REPAIRED BY SECTIONAL REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008040900115 20080409 00115 NM 2008 4 9 AALA200800667 1 20080318 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 756AM 30264 MIA - EMERGENCY LIGHT AT SEAT 22G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900128 20080409 00128 NM 2008 4 9 DLM88080535 1 20080403 A 5347 SEAT TRACK DOUG MD88 MD88 3023688 NM BS 455 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, BLEND OUT WAS FOUND OUT OF LIMIT ON SEAT TRACK AT STA Y=455 X=54 . SEAT TRACK WAS REPAIRED IAW SRM 53-05 FI G 4A. 2 L 7 2 4F RT A6WE 2008040900150 20080409 00150 EA 2008 4 9 SWIA200819434 1 20080402 A 3520 OXYGEN MASK CNDAIR CL600 CL6002D24 1390016 EA LAVATORY UNWANTED DEPLOY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 802SK 15061 FLT 3809 - AFT LAV O2 MASKS DROPPED INFLIGHT. INSPECTED MASKS AND O2 SYSTEM. RESTOWED O2 MASKS. CHECKS GOOD. 2 L 7 2 4F RT A21EA 2008040900161 20080409 00161 WP 2008 4 9 IXXA08SMN085S 1 20080215 A 5522 SKIN DOUG DC8 DC871F 302199D WP LT ELEVATOR DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR LOWER SKIN DENTED AT STATION XE 246.875. REMOVED FASTENERS AS NE EDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. BALANCED, AND FOUND TO BE WITHIN LIMITS MOMENT OF 1473.4 INCH-POUND. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XE 246.000 TO XH 285.000 IAW DC8 SRM 51-1-11, DC8 SRM 55-4-1 FIGUR E 1 SHEETS 1, 2 ITEMS "E" AND "F", DC8 SRM 55-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 51-4-4 PAGE 1-3, DC8 SRM 51-1-9 T/R 5 1-142, DC8 SRM 51-1-9A T/R 51-141, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008041000175 20080410 00175 CE 2008 4 10 VQMA032308001 1 20080323 A 2910 AE3663218G0150 HOSE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BRAKES RUPTURED E VQMA O OTHER K FLUID LOSS LD LANDING 1 NM 03 56GA 6777 6777 5600259 MAIN BRAKES FAILED ON LANDING, EMERGENCY BRAKES HAD TO BE USED, FLUID FOUND ON BOTTOM OF WING AND RT FLAP. SIGHT GAGE IN DICATES FLUID LEVEL EMPTY. 2 L 7 2 4F 4 F RT A22CE E25EA 2008041000183 20080410 00183 EU 2008 4 10 M7K2008F00002 1 20080204 A 5410 350A58004523 HINGE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE FAIRING CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 817MH 1199 4125 23292 DURING ROUTINE 100 HOUR INSP, A CRACK IN THE HINGE OF THE ENGINE FAIRING WAS FOUND RADIATING FROM THE 2ND HOLE FROM ONE END OF THE HINGE WITH THE CORNER HAVING SEPARATED FROM THE HINGE FROM CRACKS EMANATING FROM THE 1ST HOLE. THIS IS A COM MON FAILURE FOR THIS PART. THE SURFACE UNDER THE HINGE IS UNEVEN AND GIVES UNEVEN SUPPORT TO THE HINGE WHEN BOLTED DOWN . SUGGEST USING A STRONGER MATERIAL SUCH AS STAINLESS STEEL FOR THE HINGE OR IMPROVING THE SURFACE CONTOUR AND STRENGTH OF THE FAIRING HINGE MOUNTING SURFACE. (K) 1 G 7 2 3U 3 U H9EU E00054EN 2008041000195 20080410 00195 NM 2008 4 10 ASMF200804001 1 20080406 A 5730 SKIN BOEING 737 73776Q 13845AA NM LT WING DENTED W ASMF K NONE C F.O.D. IN INSP/MAINT 1 SW 23 997AM 30283 DURING TRANSIT CHECK, A BIRD STRIKE WAS DETECTED IN THE LT WING LEADING EDGE. MAINT PERFORMED A BIRD STRIKE INSPECTION I AW MM 05-51-18 DETECTING A DENT OF 0.562 INCH DEPTH, 11.5 INCH LENGTH AND 3.5 INCH WIDTH AT STATION WS 192, OUT OF LIMIT S IAW SRM 57-41-01. THE DENT WAS REPAIRED IAW MFG MESSAGE 1-8 05891937-3 DATED APRIL 07, 2008, TESTED CORRECT. 2 L 7 2 4F RT A16WE 2008041000196 20080410 00196 NM 2008 4 10 MASA200800279 1 20080331 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 5 WORN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 988HA 426 LEFT NR 5 FLAP TRACK WORN UPPER, LOWER AND MID. REPAIRED FLAP TRACK. 2 H 7 2 4T RT A13NM 2008041000197 20080410 00197 CE 2008 4 10 3302008N406CS 1 20080330 A 3260 631839721 PCB CESSNA 525 525 2076601 CE WILINT FJ44 FJ44 66000 GL MLG BURNED OUT E Z5FA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 63 406CS 2180 525B0043 DURING APPROACH, WHEN LANDING GEAR WAS SELECTED DOWN, THE DOWN AND LOCKED GREEN LIGHTS DID NOT ILLUMINATE ALTHOUGH THE G EAR FELT LIKE IT EXTENDED. THE GEAR WAS BLOWN DOWN BUT THE INDICATION DID NOT APPEAR. THE COCKPIT FLOOD LIGHTS WERE SELE CTED AND THE DOWN AND LOCKED GREEN LIGHTS APPEARED. A NORMAL LANDING FOLLOWED. TROUBLESHOOTING REVEALED A FAILED PCB NZ1 24 IN THE LT CONSOLE. REPLACED PCB NZ124 OPS CHECK OF LANDING GEAR WAS GOOD AND THE AC RETURNED TO SERVICE. 1 L 7 2 4F 4 F RT A1WI E3GL 2008041000200 20080410 00200 NM 2008 4 10 MASA200800282 1 20080331 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 5 WORN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 988HA 426 RIGHT NR 5 FLAP TRACK WORN UPPER, LOWER, AND MID. REPAIRED FLAP TRACK. 2 H 7 2 4T RT A13NM 2008041000206 20080410 00206 SO 2008 4 10 RAIA00804001 1 20080401 A 3297 5008701 CONNECTOR EMB 145 EMB145LR 3260212 SO NLG CORRODED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 834HK 145269 FLT 8055 MLI - LANDING GEAR AIR/GROUND MESSAGE ON THE EICAS AND GEAR WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACE D THE NOSE WOW SWITCH AND THE NOSE WOW SWITCH CONNECTOR. OPERATIONAL CHECK OF THE SYSTEM PROVED GOOD. 2 L 7 2 4T RT T00011AT 2008041000213 20080410 00213 NM 2008 4 10 SWAA081789 1 20080402 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 769SW 30588 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008041000217 20080410 00217 NM 2008 4 10 2008UALA01859 1 20080401 A 5210 DOOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 578UA 26694 SMALL DENT LOWER RIGHT CORNER DOOR 2L. A PERMANENT REPAIR HAS BEEN REPAIRED PER UA-EVA-71342 A AND APPROVED VIA FAA FOR M 8100-9 31 MARCH 2008 SR 1-795555670 2 L 7 2 4F 4 F RT A2NM E17NE 2008041000228 20080410 00228 NM 2008 4 10 2008UALA01870 1 20080402 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY LIGHT ROW 47 LT INOP. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041000238 20080410 00238 NM 2008 4 10 2008UALA01875 1 20080402 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 UPPER EXTERNAL FUSELAGE SKIN WORN AT BS 961-966 AND BS 988-994 AT RBL 12. BLENDED DAMAGE TO MATERIAL LOSS OF .003 IN TH E DEEPEST AREA. ACCOMPLISHED NDT INSPECTION WITH NO DEFECTS FOUND. INSTALLED WEAR STRIPS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008041000240 20080410 00240 2008 4 10 2008UALA01879 4 20080402 A 2565 CYLINDER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EVAC SLIDE LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 202UA 24717 AFT GALLEY DOOR EVAC SLIDE INFLATION CYLINDER PRESS GAUGE BELOW GREEN BAND. FAULTY RELEASE VALVE SEAL. REPLACED THE A FT GALLEY DOOR EVACUATION SLIDE REF MM 25-61-35 PAGE 202. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008041000243 20080410 00243 NM 2008 4 10 2008UALA01890 1 20080403 A 2621 4734743 FIRE BOTTLE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FWD CARGO BAY FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 793UA 26946 FIRE BOTTLE FOR FWD PIT, 1A, AFT CONNECTOR WILL NOT INSTALL ON BOTTLE. REPLACED BOTTLE. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008041000273 20080410 00273 NM 2008 4 10 2008UALA01882 1 20080402 A 5313 STRINGER SPLICE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 360 S15L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 UPPER FUSELAGE INTERIOR FORWARD ENTRY DOOR CUTOUT AT BS 360 STRINGER SPLICE CRACKED AT STRINGER S-15L. MAJOR REPAIR ACC OMPLISHED: REPLACED SPLICE CHANNEL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008041000274 20080410 00274 NM 2008 4 10 2008UALA01903 1 20080402 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EEL LIGHT INOP AT SEAT 3A AFT. REPLACED EEL LIGHT. OP CHK'D NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041000283 20080410 00283 NM 2008 4 10 2008UALA01912 1 20080403 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 AFT LOWER FUSELAGE SKIN UNDER NR 3 VHF ANTENNA HAS SMALL AREA OF CORROSION AROUND RIVET HEAD. MAJOR REPAIR ACCOMPLISHED , FABRICATED & INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008041000284 20080410 00284 NM 2008 4 10 2008UALA01913 1 20080403 A 5313 STRINGER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 FUSELAGE STRINGER 16L IS CRACKED AT STR END, BETWEEN BS 348-360, ABOVE DOOR 1L. MAJOR REPAIR ACCOMPLISHED, INSTALLED ST RINGER SPLICE CHANNEL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008041000285 20080410 00285 NM 2008 4 10 2008UALA01914 1 20080403 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 UPPER EXTERNAL FUSELAGE SKIN WORN FROM BS 907 TO 928 AND BS 945 TO 955 AT LBL 9. MAJOR REPAIR ACCOMPLISHED. BLENDED DA MAGE WITH .004" MATERIAL LOSS. INSTALLED WEAR STRIPS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008041000286 20080410 00286 NM 2008 4 10 2008UALA01915 1 20080404 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 809UA 825 FOUND BEAM 175 CORRODED. REPAIR WAS ACCOMPLISHED, REMOVED FLOORBEAM. INSTALLED AND SEALED BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041000293 20080410 00293 NM 2008 4 10 2008UALA01922 1 20080403 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 594UA 28145 EEL STRIP LIGHT BY FWD COAT CLOSET INOP. FOUND SHORTED WIRING. REPLACED LIGHT STRIP CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041000294 20080410 00294 NM 2008 4 10 2008UALA01924 1 20080403 A 3350 60243 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 594UA 28145 EEL LIGHT STRIP AT AFT LAV INOP. REPLACED LIGHT STRIP. CHK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041000295 20080410 00295 NM 2008 4 10 2008UALA01925 1 20080403 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 545UA 25323 RIGHT AFT OVERWING EXIT LIGHT INOP. FOUND BULB INOP. REPLACED BULB. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041000296 20080410 00296 NM 2008 4 10 2008UALA01926 1 20080404 A 5753 PLATE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE T/E FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 798UA 26928 HONEYCOMB PLATE WEAR WAS FOUND AT UPPER SURFACE OF LEFT WING OUTBOARD FLAP. DID NDT INSP PER NDT MANUAL PART1 51-01-01 F IG 9, NO DELAMINATION. REPAIRED REF 777EN-57-0030-01, TOUCH UP PAINT PER AMM 51-21-10P701. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008041000297 20080410 00297 NM 2008 4 10 2008UALA01927 1 20080404 A 5753 PANEL BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE T/E FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 798UA 26928 WEAR WAS FOUND ON THE PANEL OF THE RT WING T/E OUTBOARD FLAP UPPER SURFACE, INBOARD END L=31". DID NDT INSP PER 777 NDT MANUAL PART 1. 51-01-01 FIG 9, NO DELAMINATION, REPAIRED PER 777EN-57-0031-01, TOUCH UP PAINT REF TO AMM 51-21-10 P701. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008041000300 20080410 00300 EA 2008 4 10 MASA200800284 1 20080403 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27314 7314 FLT 1944, HNL-OGG. EXTERIOR FORWARD LEFT EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2008041100001 20080411 00001 NM 2008 4 11 2008UALA01887 1 20080402 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1197 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 AFT PIT AT BS 1197+88 AND LBL 40 FRAME T-CAP IS CORRODED UNDER AND AROUND NUT PLATE. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041100003 20080411 00003 EU 2008 4 11 08FDEA01298 1 20080404 A 2133 VST165D OUTFLOW VALVE AIRBUS 310 A310304 3930339 EU CABIN PRESSURE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 816FD 593 UPON CLIMB-OUT CABIN VERTICAL SPEED EXCEEDED 2000FPM, AT 15000 ALT CAB ALT EXCEEDED 10,000. OUTBOARD EXTRACT VALVE FAUL TED, UNABLE TO MANUALLY CONTROL CABIN PRESS. REACTIVATED SYSTEM. FAILED OPS CHECKED AS PER AMM 21-23-00-5, VALVE NEVER MOVED. T/S AS PER WDM, R&R RELAY 69HR, NO HELP. R&R OVERBOARD EXTRACT VALVE AS PER AMM 21-23-13-4, OPS CHECKED GOOD, OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2008041100010 20080411 00010 EU 2008 4 11 08FDEA01373 1 20080410 A 5755 A57771000004 SPOILER PANEL AIRBUS 300 A300B4622R 3930312 EU NR 4 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND DELAMINATION OUT OF LIMIT ON SPOILER NR 4 LT. REPAIR PERFORMED BY REPLACEMENT OF IAW AMM 25-61-51. 2 L 7 2 4F RT A35EU 2008041100047 20080411 00047 EA 2008 4 11 A6WA200840227 1 20080319 A 4990 CAP CNDAIR CL600 CL6002B19 1900309 EA APU OIL FAULTY A A6WA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 436AW 7734 ON TAXI OUT, STRONG BURNING ODOR FOLLOWED BY APU FAULT CAUTION AND APU AUTO-SHUTDOWN. COMPLIED QRH, PACKS SWITCHED TO 1 0TH STAGE BLEEDS AND ODOR DISSIPATED. TROUBLESHOT BURNING ODOR TO APU. APU OIL SERVICING CAP FOUND TO BE FAULTY. (M) 2 L 7 2 4F RT A21EA 2008041100048 20080411 00048 EA 2008 4 11 A6WA200840226 1 20080318 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM ILLUMINATED A A6WA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 31 402AW 7281 STAB TRIM CHANNEL 1 STATUS MESSAGE IN FLIGHT, COMPLIED WITH QRH AND MESSAGE DID NOT CLEAR. (M) 2 L 7 2 4F RT A21EA 2008041100049 20080411 00049 EA 2008 4 11 A6WA200840234 1 20080322 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY DOOR FALSE ACTIVATION A A6WA O OTHER N FALSE WARNING CR CRUISE 1 GL 31 440AW 7766 RIGHT EMERGENCY DOOR CAUTION MESSAGE ON CLIMB-OUT AT 13,000 FT, NORMAL PRESSURIZATION. COMPLIED WITH QRH. (M) 2 L 7 2 4F RT A21EA 2008041100051 20080411 00051 EA 2008 4 11 A6WA200840178 1 20080310 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 462AW 7875 AFTER TAKEOFF UPON GEAR RETRACTION NOSE GEAR SHOWED DOWN WITH GEAR DISAGREE, COMPLIED WITH QRH, PERFORMED MANUAL GEAR EX TENSION, RETURNED TO ROS. (M) 2 L 7 2 4F RT A21EA 2008041100053 20080411 00053 NM 2008 4 11 DHL2008753512 1 20080407 A 5410 NOSE COWL BOEING 727 727223 1384074 NM NR 1 NACELLE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 WHILE AT C CHECK, NR 1 ENG NOSE COWL IB SIDE UPPER, CRACKED AT FASTENER HEAD AT PANEL CUTOUT NAC STA 77. FABRICATED AND INSTALLED REPAIR, CUT-OUT AREA NAC 69-77 8 3/4 INCH BY 6 1/2 INCH 3 DOUBLERS 2 INNER 6 INCH BY 4 INCH OUTER 1 11 INCH B Y 8 1/2 INCH 1 FILLER 8.75 INCH BY 6.5 INCH AND 1 ANGLE 1 1/2 INCH BY 8 INCH IAW B 727 SRM 54-30-1 FIG 1, 54-30-3, 51-30 -2 AND 51-10-2. 2 L 7 3 4F A3WE 2008041100055 20080411 00055 NM 2008 4 11 DHL2008753513 1 20080310 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 590-740 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 MAIN CABIN SEAT TRACK GOUGED, BS 700, RBL 25. REMOVED SEAT TRACK SECTION, FABRICATED SEAT TRACK FROM BAC1503-792 PO NR 9006020, 172" LONG, AND REPAIR ANGLE FROM BAC1503-100122, PO NR 9006027, 12 INCH LONG, AND INSTALLED SEAT TRACK PER B727 SRM 53-10-5 FIG 1 AND 51-302. 2 L 7 3 4F A3WE 2008041100058 20080411 00058 EA 2008 4 11 A6WA200840235 1 20080324 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A A6WA O OTHER O OTHER AP APPROACH 1 GL 31 448AW 7814 ON DESCENT CAPTAINS WINDSHIELD CRACKED. COMPLIED WITH QRH, CYCLED HEAT `OFF`, THEN `ON` THEN BACK `OFF`, AFTER RECEIVIN G LT WINDSHIELD HEAT CAS MESSAGE. REMOVED AND REPLACED CAPTAINS WINDSHIELD IAW AMM 56-11-01. (M) 2 L 7 2 4F RT A21EA 2008041100061 20080411 00061 EU 2008 4 11 08FDEA01360 1 20080409 A 5740 A57111092202 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND ON C 47 IN VARIOUS HOLES LOWER JUNCTION FITTING CORROSION AND DAMAGES. REPAIR PERFORMED BY REWORK OF CORROSION AN D DAMAGE IN ALL HOLES, REAM UP, BUSH INSTALLATION WHERE NECESSARY IAW RAS 70503157/030/2008 ISS A, APPROVED BY EA 6-5710 -114882. 2 L 7 2 4F RT A35EU 2008041100062 20080411 00062 EU 2008 4 11 08FDEA01361 1 20080409 A 5740 A57111092203 FITTING AIRBUS 300 A300B4622R 3930312 EU WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND ON C 47 IN VARIOUS HOLES LOWER JUNCTION FITTING CORROSION AND DAMAGES. REPAIR PERFORMED BY REWORK OF CORROSION AN D DAMAGE IN ALL HOLES, REAM UP, BUSH INSTALLATION WHERE NECESSARY IAW RAS 70503157/030/2008 ISS A, APPROVED BY EA 6-5710 -114882. 2 L 7 2 4F RT A35EU 2008041100065 20080411 00065 SO 2008 4 11 CHQA200800072 1 20080404 A 2720 15793101 PRESSURE SWITCH EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL RUDDER INOPERATIVE A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 380SK 10353 10353 145613 CAE311970 FLIGHT 5284, STL TO BDL, DURING CRUISE AT FL340, THE CREW RECEIVED A RUDDER SYS 1-2 INOP EICAS MESSAGE, FOLLOWED BY AUTO PILOT AND YAW DAMPER FAIL. THE QRH WAS FOLLOWED AND THE RUDDER 2 BUTTON WAS RELEASED WHICH THEN RESTORED POWER TO THE R UDDER 1 SYSTEM. THE FLIGHT THEN DIVERTED TO CMH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE SYSTEM T O THE PRESSURE SWITCH FOR THE RUDDER SYSTEM 2. AFTER REPLACING THE PRESSURE SWITCH THERE WERE NO FURTHER MESSAGES, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008041100066 20080411 00066 EA 2008 4 11 A6WA200840170 1 20080303 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 OUTBOARD CLIP AT FS 484 RBL 36 FOUND CRACKED. REPLACED IAW CRJ 200 REO 601R-53-41-059 REV A. (M) 2 L 7 2 4F RT A21EA 2008041100073 20080411 00073 NM 2008 4 11 08FDEA01366 1 20080409 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK SEAT TRACK FLANGE BELOW FLOOR PANEL NR 271DF AT STA 5-83, X = 27 FOUND CORROSION AT UPPER SURFACE. REPAIRED B Y SECTIONAL SEAT TRACK REPLACEMENT FROM STA 5-0 TO STA 1531, X = 27 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLAS SIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041100074 20080411 00074 EU 2008 4 11 08FDEA01367 1 20080409 A 5330 A5397326420000 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FOUND SIX EDDY CURRENT INDICATIONS ON INNER SKIN LIP BETWEEN STA - 3620 TO 3726 (FR67 - 69 ) BULK CARGO DOOR. REWORKED IAW SRM 53-17-12. NDT AREA IAW. NTM53-30-52 PT 6 AND 51-10-08. FOUND 1 CORROSION INDICATION NO CRACKS IN SUB STRUCTURE. REMOVE CORROSION IAW SRM 53-17-12 ORIG MAT .238 OF .228 WITHIN LIMITS IAW SRM 53-17-12, REMOVED SECTION, LATERAL WEB, FLOOR SUPPORT AND CORNERS TO FOM IAW SRM 51-40-21 ALODINED IAW SRM 51-21-10, PRIMED AND PAINTED IAW SRM 51-23-10. INST ALLED NEW SECTION P/N A5397305720000, PO NR 614306.5, LATERAL WEB, FLOOR SUPPORT, AFT CORNER P/N A5397326420251, PO 6143 06.1 AND FWD CORNER P/N A5397325850251, PO 614306.3 IAW 1-40-21. 2 L 7 2 4F RT A35EU 2008041100075 20080411 00075 NM 2008 4 11 08FDEA01368 1 20080409 A 5347 BAC15201466 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 MAIN CARGO COMPATRMENT, SEAT TRACK IC CORRODED FROM BS 870-848, LBL 25. REMOVED SEAT TRACK AT MAIN CARGO COMPARTMENT IA W SRM 51-30-2. LOCATED AND DRIILED NEW TRACK, DIM 16 INCH LONG IAW SRM 51-30-5 AND 53-10-2 FIG 7. TREATED AND PRIMED A FFECTED AREAS IAW CSRM 51-1-2. INSTALLED NEW TRACK IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008041100077 20080411 00077 EA 2008 4 11 A6WA200840140 1 20080228 A 5260 PANEL CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR UNKNOWN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 REPAIR PAX DOOR AFT STAIR SIDE PANEL. REPLACED SIDE PANEL IAW SRM 51-42-06, 51-42-21 AND 51-23-00. (M) 2 L 7 2 4F RT A21EA 2008040900076 20080409 00076 NM 2008 4 9 08FDEA01275 1 20080403 A 5347 AEA732515 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK SEAT TRACK FLANGE AT STA 1395, X = -75 FOUND EXFOLIATION CORROSION. REPAIRED BY SECTIONAL REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008040900082 20080409 00082 EU 2008 4 9 08FDEA01281 1 20080403 A 5540 A55471500026 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU RUDDER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 WATER INGRESS FINDINGS DURING RUDDER THERMOGRAPHY INSPECTION -EO 6-5530-7-5004. REPAIR PERFORMED BY REMOVING OUTER SKIN AND CORE, DRY THE REPAIR AREA, REPLACE THE CORE AND PERFORM WET LAY UP- REPAIR IAW RAS/DAHAM/4024104/2008 ISS A, APPROV ED BY EA 6-5540-114923. 2 L 7 2 4F RT A35EU 2008040900085 20080409 00085 2008 4 9 HALA0800488 4 20080403 A 2210 AUTOLAND SYS BOEING 767 767332 1382001 NM MALFUNCTIONED A HALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM, ON FINAL APPROACH NO LAND 3 INDICATED. RESET ASA HOWEVER, LAND 2 INDICATED ON ASA AFTER PRELA ND TEST. SUCCESSFUL AUTOLAND USING LAND 2 ON RWY 340. MCDP LAST FLT FAULT NO LAND 3 ILS LOC L NCD CODE 11 2020 RESET L ILS C/B. PERFORMED A/L TEST 01, 30, AND 40. ALL TESTS SUCCESSFUL LMP IND REMAINS AT CAT 3. 2 L 7 2 4F RT A1NM 2008040900106 20080409 00106 WP 2008 4 9 08FDEA00733 1 20080305 A 5755 NRC6050505 SKIN DOUG MD10 MD1010F 3022112 WP NR 4 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 LT WING SPOILER NR 4 UPPER EXTERIOR IS DELAMINATED (3 PLACES). TAP TESTED MARKED AREAS IAW DC/MD-10 SRM 51-61-01; VOL I I. NO DELAMINATION NOTED AT THIS TIME. REINSTALLED LT NR 4 SPOILER IAW MD-10-10 AMM 27-60-01-4. CLEARANCE AND OPS CHECKS GOOD IAW MD-10-10 AMM 27-60-01-6 AND MD-10-10 AMM 27-60-01-4. 2 L 7 3 4F RT A22WE 2008040900131 20080409 00131 NM 2008 4 9 AALA200800684 1 20080321 A 2800 RELIEF VALVE BOEING 757 757223 1384957 NM RT WING POPPED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 671AA 25336 JFK INFLIGHT T1375/21MAR BDL TO SJU - TOWER REPORTED FUEL LEAKING FROM RIGHT WING. LANDED JFK WITHOUT INCIDENT. FOUND PRESSURE RELIEF VALVE POPPED IN PANEL NUMBER SIX POSITION FROM OUTBOARD. RELOCATED PRESSURE RELIEF VALVE TO NUMBER FIV E POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900141 20080409 00141 WP 2008 4 9 AALA200800687 1 20080321 A 5340 BRACKET DOUG DC9 DC982 3022082 WP FLASHLIGHT CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AA 49271 LGA - EMERGENCY FLASHLIGHT AT AFT RIGHT FORWARD BY LAVATORY HAS CRACKED BRACKET. REPLACED BRACKET FOR EMERGENCY FLASHLI GHT AT AFT RIGHT FORWARD BY LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008040900144 20080409 00144 EA 2008 4 9 SWIA200819428 1 20080402 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WINGLET DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 969SW 7876 LEFT WINGLET OUTBOARD SKIN WAS DAMAGED BY BAGGAGE CART. REPLACED WINGLET SKIN IAW CRJ SRM 51-40-11, REO 601R-57-31-330 AND BOMBARDIER DRAWING NR 600-15108. 2 L 7 2 4F RT A21EA 2008040900145 20080409 00145 EA 2008 4 9 SWIA200819429 1 20080331 A 5610 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 702SK 10136 FLT 6395 - CAPTAINS SIDE WINDOW CRACKED DURING DESCENT. REPLACED SIDE WINDOW IAW 56-12-01, P/N NP-139322-5, SN/OFF 0324 5H3457. 2 L 7 2 4F RT A21EA 2008040900169 20080409 00169 NM 2008 4 9 DLM88080546 1 20080403 A 5311 FRAME DOUG MD88 MD88 3023688 NM BS 1380 L28L-R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, CORROSION WAS FOUND ON FRAME Y=1380 BETWEEN LONGERON 28 LT AND 28 RT. FRAME WAS REPLACED IAW DOUGLAS DWG 99 12246. 2 L 7 2 4F RT A6WE 2008040900174 20080409 00174 NE 2008 4 9 NACA20080006 2 20080402 A 8530 356993 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 3 ENGINE CRACKED A NACA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 2907F 869 869 533265 P31943 NR 3 ENGINE SHUT DOWN DUE TO BACKFIRING DURING CRUISE. REPLACED NR 2 CYLINDER DUE TO A CRACKED HEAD, REF: DC-6MM SECT V PG 16-17. OP CHECK GOOD. 2 L 7 4 4R 4 R A781 5E8 2008040900180 20080409 00180 NM 2008 4 9 QXEA20080335 1 20080328 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM PAX STUCK A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 414QX 4061 GEG - AFT PASSENGER DOOR WILL NOT CLOSE. MAINTENANCE RESET THE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SER VICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008041000004 20080410 00004 EU 2008 4 10 PNSA080301 1 20080328 A 3350 6104789 BATTERY SAAB SF340 340B 7860101 EU CABIN FAILED A PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 364PX 340B262 DURING INSPECTION AND TESTING OF EMERGENCY POWER SUPPLY BATTERIES P/N 61-0478-9, FOUND ONE BATTERY WITH A SPLICE IN WIRE NOT ALLOWED IN CMM, FOUND ANOTHER THAT FAILED VOLTAGE CHECK. REMOVED BOTH BATTERIES FROM SERVICE AND SCRAPED. 2 L 7 2 4T RT A52EU 2008041100091 20080411 00091 NE 2008 4 11 DL76L080569 2 20080408 A 7260 GEARBOX BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 187DN 27582 724416 METAL FOUND ON THE NR 2 ENGINE CHIP DETECTOR. DURING INVESTIGATION FOUND TO BE METAL FROM GEARBOX. WILL REPLACE NR 2 E NG. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041100094 20080411 00094 NM 2008 4 11 DL75A080573 1 20080408 A 3244 B757M TIRE BOEING 757 757212 1384951 NM MLG CUT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 751AT 23125 NR 8 MLG TIRE HAS DEEP CUT. REPLACED NR 8 MLG WHEEL ASSY PER AMM. 2 L 7 2 4F RT A2NM 2008041100095 20080411 00095 EA 2008 4 11 A6WA200840136 1 20080225 A 3340 LENS CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 RIGHT WING TIP POSITION LIGHT LENSES FOUND CRACKED. REPLACED IAW AMM 57-30-61-400-801. (M) 2 L 7 2 4F RT A21EA 2008041100096 20080411 00096 EA 2008 4 11 A6WA200840141 1 20080226 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 CRACK FOUND ON AFT PRESSURE BULKHEAD WEB AT FS 621 BTW 113.33 AND WL 106.17 LBL 36. REPAIR TO PRESSURE BULKHEAD WEB CAR RIED OUT IAW REO 601R-53-61-1230 REV D. (M) 2 L 7 2 4F RT A21EA 2008041100099 20080411 00099 EA 2008 4 11 A6WA200840182 1 20080314 A 2710 AILERON CNDAIR CL600 CL6002B19 1900309 EA STUCK A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 427ZW 7685 IN FLIGHT, 4 SECONDS AFTER DISCONNECTION AUTOPILOT, AILERONS STUCK AND MOMENTARILY AILERONS COULD NOT BE TURNED LEFT OR RIGHT, ON 4 MILE FINAL. (M) 2 L 7 2 4F RT A21EA 2008041100100 20080411 00100 EA 2008 4 11 A6WA200840232 1 20080320 A 2760 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA SPOILERS ILLUMINATED A A6WA O OTHER J WARNING INDICATION AP APPROACH 1 GL 31 409AW 7447 OUTBOARD GROUND SPOILER FAULT MESSAGE AND SPOILERON FAULT MESSAGE IN FLIGHT. AFTER LANDING ONLY OUTBOARD GROUND SPOILER MESSAGE EVIDENT. PERFORMED RESET PER FIM PROCEDURE. MESSAGE CLEARED. FLIGHT CREW PERFORMED INITIAL RESET. PROBLEM C LEARED LOCAL MAINTENANCE NOTED NO MESSAGE. AIRCRAFT RELEASED. (M) 2 L 7 2 4F RT A21EA 2008041100102 20080411 00102 EA 2008 4 11 A6WA200840162 1 20080307 A 5753 FAIRING CNDAIR CL600 CL6002B19 1900309 EA TE FLAP DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 ABRASION FOUND ON LEFT FLAP STUB FAIRING EXTERNAL SURFACE. (M) REPLACED IAW SRM 51-42-06. (K) 2 L 7 2 4F RT A21EA 2008041100103 20080411 00103 EA 2008 4 11 A6WA200840165 1 20080308 A 5540 DIAPHRAGM CNDAIR CL600 CL6002B19 1900309 EA RUDDER MISSING A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 RUDDER UPPER CLOSURE RIB IS MISSING DIAPHRAGM CLOTH. REPAIRED IAW CRJ 200 REO 601R-55-41-037. (M) 2 L 7 2 4F RT A21EA 2008041100107 20080411 00107 EU 2008 4 11 MALA080053 1 20080404 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 288-399 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 421XJ 340B421 SEAT TRACK CORRODED. REPLACED AT STA 288 TO 399 ALONG IAW EO NR S530602. 2 L 7 2 4T RT A52EU 2008041100108 20080411 00108 EA 2008 4 11 SWIA200819440 1 20080402 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 936SW 7726 AFT CEILING EMERGENCY POD LIGHT IS INOP. RELAMPED THE EMERGENCY POD LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008041100109 20080411 00109 SO 2008 4 11 SWIA200819441 1 20080331 A 3350 SIGN EMB 120 EMB120ER 3260203 SO CABIN MISSING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 227SW 120304 FLT 5462 - EXIT SIGN MISSING ON THE EMERGENCY EXIT ROW. REPLACED EXIT SIGN COVER. 2 L 7 2 4T RT A31SO 2008041100111 20080411 00111 EA 2008 4 11 SWIA200819443 1 20080404 A 5220 SEAL CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT LEAKING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 407SW 7034 FLT 2876 - RIGHT OVERWING EMERGENCY EXIT DOOR SEAL IS LEAKING. REPLACED RIGHT EMERGENCY EXIT DOOR SEAL IAW CRJ MM 52-21 -07. 2 L 7 2 4F RT A21EA 2008041100114 20080411 00114 2008 4 11 SWIA200819446 2 20080403 A 7320 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE OUT OF ADJUST A SWIA E ENGINE SHUTDOWN O OTHER TX TAXI/GRND HDL 1 NM 07 439SW 7578 FLT 3919 - THE LEFT ENGINE SHUT DOWN WHILE TAXIING TO THE GATE. ADJUSTED THE LEFT ENGINE CONTROL RIGGING. OPS CHECK GO OD. 2 L 7 2 4F RT A21EA 2008041100115 20080411 00115 EA 2008 4 11 SWIA200819448 1 20080402 A 3350 AD20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 746SK 1479 1479 10202 FLT 6612 - EMERGENCY LIGHT IN FRONT OF CABIN IS INOP. REPLACED NR 1 ELBP AS REQUIRED. LIGHTS OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008041100116 20080411 00116 SO 2008 4 11 SWIA200819449 1 20080402 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 579SW 120347 FLT 5478 - EMERGENCY EXIT SIGN AT SEAT 6A IS BROKEN. REPLACED BROKEN SIGN. 2 L 7 2 4T RT A31SO 2008041100117 20080411 00117 EA 2008 4 11 SWIA200819450 1 20080403 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCONNECTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 417SW 7400 FLT 2522 - FLOOR LEVEL EMERGENCY LIGHT AT MAIN CABIN DOOR ENTRANCE IS INOP. RESECURED CONNECTOR TO EMERGENCY LIGHT. OP S CHECK GOOD. 2 L 7 2 4F RT A21EA 2008041100118 20080411 00118 EA 2008 4 11 SWIA200819451 1 20080407 A 5210 LATCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 498CA 7792 FLIGHT ATTENDANT WAS UNABLE TO OPEN MAIN CABIN DOOR. REPLACED DOOR LATCH MECHANISM BOX PER MM 52-11-25. OPS CHECK GOOD . 2 L 7 2 4F RT A21EA 2008041100125 20080411 00125 EA 2008 4 11 A6WA200840137 1 20080225 A 5280 DOOR CNDAIR CL600 CL6002B19 1900309 EA RT MLG WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 RIGHT MLG FIXED DOOR FOUND WORN ON L/E END SECTION. RIGHT MLG FIXED DOOR REPAIRED IAW REO 601R-52-82-016 SHEET 1 THROUG H 4. (M) 2 L 7 2 4F RT A21EA 2008041100127 20080411 00127 EA 2008 4 11 A6WA200840163 1 20080307 A 5753 FAIRING CNDAIR CL600 CL6002B19 1900309 EA TE FLAP DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 ABRASION FOUND ON RT FLAP STUB FAIRING EXTERNAL SURFACE. (M) REPLACED IAW SRM 51-42-06, 51-41-02, 51-42-11. (K) 2 L 7 2 4F RT A21EA 2008041100128 20080411 00128 EA 2008 4 11 A6WA200840171 1 20080227 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 PRESSURE BULKHEAD WEB AT FS 621, LINTEL AREA, IS CRACKED. REPAIRED IAW CRJ 200 REO 601R-53-61-1230 REV D. (M) 2 L 7 2 4F RT A21EA 2008041100145 20080411 00145 NM 2008 4 11 CALA0800294 1 20080331 A 5315 FLOORBEAM BOEING 767 767424ER 1385270 NM BS 303 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76055 29450 CABIN - STA 303 LBL 15 TO LBL 45 FLOORBEAM FOUND CORROSION. CABIN FLOORBEAM CORROSION AREA REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AT STA 303 LBL 4 IN TO LBL 63 IN. 2 L 7 2 4F RT A1NM 2008041100146 20080411 00146 NM 2008 4 11 CALA0800295 1 20080331 A 5315 141T5147 FLOORBEAM BOEING 767 767424ER 1385270 NM BS 246 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76055 29450 STA 246 FLOORBEAM LBL 40 MID CHORD AREA 1EA CRACK FOUND AT MID CHORD RADIUS APPROX .75 INCH LONG APART FROM O/B EDGE. S TA 246 FLOORBEAM LBL 40 MID CHORD CRACKED REPAIRED AS PER ECRA#5310-04737. 2 L 7 2 4F RT A1NM 2008041100147 20080411 00147 NM 2008 4 11 CALA0800614 1 20080408 A 5310 652072366 DOOR FRAME BOEING 737 737524 1384721 NM CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 46625 27529 FWD CARGO DOOR CUTOUT AFT FRAME HAS 1 INCH CRACK, AT BOTTOM DOOR STOP PAD FOOT PRINT. REMOVED & REPLACED FWD CARGO DOOR CUTOUT AFT FRAME REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041400021 20080414 00021 CE 2008 4 14 DJFA2008034 1 20080328 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE CABIN SMOKE E DJFA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 23 755TA RK324 REPORTED EXTREME HEAT COMING INTO AIRCRAFT ACCOMPANIED BY A BLUE HAZY TYPE SMOKE AND BURNING ODOR IN CABIN. AIR CONDITI ONING SYSTEM WAS PREVIOUSLY MEL'D. MAINT FOUND THE AIR CYCLE MACHINE CIRCUIT BREAKER PULLED AND COLLARED. THE CIRCUIT BREAKER WAS RESET. THE BLEED AIR SYSTEM WAS TESTED AND THE SYSTEM FUNCTIONED NORMALLY. 2 H 7 2 4F 4 F RT A16SW E25EA 2008041400023 20080414 00023 CE 2008 4 14 GUUA03150801 1 20080315 A 3260 1309091338 DOWNLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MLG MISINSTALLED A GUUA O OTHER W N INADEQUATE Q C FALSE WARNING TX TAXI/GRND HDL 1 SO 29 87552 UE216 FLIGHT:9253, DURING BOARDING LT (H) LIGHT AND LANDING GEAR HORN ARE BLINKING AND SOUNDING SIMULTANEOUSLY. ALL (3) GREEN LIGHTS ILLUMINATED WITH THE RED GEAR HANDLE LIGHT WITH GEAR HORN. INSTALLED MISSING BOLT ON LT DOWNLOCK SWITCH. 2 L 7 2 4T 3 T RT A24CE E2NE 2008041400024 20080414 00024 SO 2008 4 14 GUUA03240801 1 20080324 A 3260 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE MLG OUT OF ADJUST A GUUA O OTHER S N AFFECT SYSTEMS FALSE WARNING AP APPROACH 1 SO 29 282AS 120226 FLIGHT:0250, DURING APPROACH LANDING GEAR DONT OPERATE DOWN NORMAL. OVERIDE SWITCH USED TO EXTEND LANDING GEAR. READJ USTED PROXIMITY SENSOR ON RT MLG UPLOCK (A) SYSTEM. 2 L 7 2 4T 4 T RT A31SO E20NE 2008041400025 20080414 00025 CE 2008 4 14 GUUA03240802 1 20080324 A 5540 10164001415 HINGE BRACKET BEECH 1900 1900D 1154162 CE RUDDER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 45AR UE12 DURING ROUTINE SCHEDULED MAINTENANCE DISCOVERED RUDDER UPPER HINGE BRACKET HAS SEVERAL AREAS OF EXFOLIATION. REPLACED R UDDER UPPER HINGE BRACKET. 2 L 7 2 4T RT A24CE 2008041400026 20080414 00026 EA 2008 4 14 N6WA20080304 1 20080328 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* 30015 NE EMERGENCY LIGHT INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 152GJ 10218 LT AFT EMERGENCY LIGHT INOP. REPLACE BULB, IAW AMM 33-51-15. 2 L 7 2 4F 4 F RT A21EA 2008041400029 20080414 00029 CE 2008 4 14 GLBA20061087 1 20080328 A 5311 12944004471 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 495 S3L BENT A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 261GL UE261 FRAME SECTION AT FS 495.75 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 495.75 STRINGER 3L IAW SRM 51-40. P/N 129-440044-71. 2 L 7 2 4T 4 T RT A24CE E26NE 2008041400038 20080414 00038 CE 2008 4 14 DXTA20082976 1 20080401 A 2150 A/C PACK CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MALFUNCTIONED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 932QS 7500032 CANNOT CONTROL TEMP ON CABIN PAC. CABIN FILLED WITH SMOKE. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008041400049 20080414 00049 CE 2008 4 14 DXTA20082984 1 20080407 A 2750 FLAP SYSTEM CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE TE FLAPS MALFUNCTIONED E DXTA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 07 694QS 5605194 FLAPS WILL NOT RETRACT BEYOND 7 DEG WITH THE FLAP HANDLE IN THE 0 POSITION. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008041400069 20080414 00069 CE 2008 4 14 DXTA200802933 1 20080312 A 3234 049801001 CONTROL HANDLE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 671QS 1551 5605071 DURING GEAR RETRACTION RED UNLOCK LIGHT STAYED ILLUMINATED, FOLLOWED BY STAB MISCOMPARE AND HYD PRESS CAUTION LIGHTS. W ITH GEAR EXTENDED UNLOCK LIGHT WENT OUT. WHILE COMPLETING HYD PRESS CHECKLIST (GEAR RETRACTED), A LOUD THUNK WAS HEARD IN THE L WING ROOT AREA WHEN THE HYD CONTROL CB WAS PULLED. CB WAS RESET, GEAR WAS EXTENDED. THERE WERE NO UNUSUAL BUF FET OR FLIGHT CHARACTERISTICS DURING THE FLIGHT. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE IAW MM 32-30-01. ALSO REMOVED AND REPLACED LANDING GEAR PCB IAW MM 24-51-02. C/W LANDING GEAR FUNCTIONAL CHECKS IAW MM 32-01-00. OPERATIONA L CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008041400079 20080414 00079 CE 2008 4 14 DXTA200802974 1 20080330 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 399QS 5600510 CO-PILOT'S BRAKES FEEL MUSHY AND SOFT WITH MORE THEN USUAL TRAVEL DURING LANDING. BLED ANTISKID BRAKE SYS. OPS CHECKED G OOD. LEAK CHECKED GOOD. WORK DONE IAW MM, CHAPTER 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2008041400089 20080414 00089 CE 2008 4 14 DXTA200802984 1 20080407 A 2752 99120071 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE TE FLAPS STUCK E DXTA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 07 694QS 5605194 FLAPS WILL NOT RETRACT BEYOND 7 DEG WITH THE FLAP HANDLE IN THE 0 POSITION. RECEIVED ACFT WITH FLAPS STUCK HARD AT 15 D EGREES. ATTACHED HYDS AT EXTEND AND RETRACT LINES OFF OF FLAP CONTROL VALVE. FLAPS WOULD NOT EXTEND OR RETRACT WITH APPL IED HYD PRESSURE. MEASURED ACTUATOR ROD LENGTHS WITH HYD PRESSURE APPLIED, THE RT ACTUATOR WOULD MOVE 1/4 INCH WHILE THE LT ACTUATOR REMAINED LOCKED. REMOVED LT FLAP ACTUATOR AND INSTALLED CUSTOMER SUPPLIED P/N 9912007-2 S/N 2568. WORK WAS PERFORMED IAW MM 27-51-04. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008041400090 20080414 00090 CE 2008 4 14 DXTA200802985 1 20080407 A 3230 VALVE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP RT MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 873QS 258573 ON TO RT MLG DID NOT FULLY RETRACT. TROUBLESHOT BY REMOVING RT MLG REVERSING VALVE IN-LINE FILTER AND NON-RETURN VALVE. CLEANED AND INSPECTED. REASSEMBLED WITH NEW O-RINIG. NO DEFECTS NOTED. PERFORMED RETRACTION TEST. LUBED RT MLG. WORK IA W AMM 32-30 & AFMS. 2 L 7 2 4F 4 F RT A3EU E6WE 2008041400091 20080414 00091 NM 2008 4 14 DXTA200802986 1 20080407 A 3150 4AS7130020003 ACTUATOR GULSTM 200 200 4500308 NM PWC PW306 PW306C 52169 NE ELEVATOR FEEL MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 708QS 069 AFTER TAKEOFF ELEVATOR FEEL FAIL MESSAGE CAME ON. REMOVED DEFECTIVE Q-FEEL ACTUATOR AND INSTALLED NEW Q-FEEL ACTUATOR P /N 4012-0000-000 S/N IL-217 ALL WORK DONE IAW MM 27-30-10. 2 L 7 2 4F 4 F RT A53NM E35NE 2008041400108 20080414 00108 SW 2008 4 14 KLAL9290 1 20080409 A 3211 2751042176 TORQUE TUBE SWRNGN SA227 SA227BC 3377519 SW RT MLG CRACKED E KY7A O OTHER P NO WARNING INDICATION TX TAXI/GRND HDL 1 NM 03 779B 31759 BC779B RIGHT MAIN GEAR ACTUATOR TORQUE TUBE FAILURE. 2 L 7 2 4T RT A8SW 20080826 SO 2008 8 26 C2XA08CL083 1 20080710 A 2913 971808MODA PUMP EMB 145 EMB145LR 3260212 SO HYD SYSTEM FAULTY A C2XA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 27 16987 18869 145261 SYR FLIGHT 2589 - THE CREW REPORTED A ENGINE NR 1 HYDRAULIC PUMP FAIL MESSAGE IN FLIGHT. EMERGENCY DECLARED AND FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE HYDRAULIC PUMP AND NR 1 HYDRAULIC PUMP SUCT ION HOSE AND THE RETURN AND CASE DRAIN FILTERS. OPERATIONAL CHECKS WERE GOOD. (A) 2 L 7 2 4T RT T00011AT 20080826 2008 8 26 PID2008F00013 4 20080816 A 2565 416N222019 BOTTLE BOEING 757 757200 1384950 NM RT OWING SLIDE NO TEST A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 801DM 26240 RT OVERWING SLIDE BOTTLE LIGHT DOES NOT TEST ON P-61 PANEL. REMOVED RT OVERWING ESCAPE SLIDE BOTTLE AND SERVICED TO 295 0 PSI WITH DRY NITROGEN. REINSTALLED RT OVERWING ESCAPE SLIDE BOTTLE IAW AMM 25-85-00. SLIDE BOTTLE PRESSURE LIGHT TES TS NORMAL. (S) 2 L 7 2 4F RT A2NM 20080826 WP 2008 8 26 IXX2008F00078 1 20080609 A 5753 SKIN DOUG DC8 DC872F 302199E WP LT WING TE FLAP WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND LT WING OUTBOARD FLAP UPPER SKIN WORN AT STATION XF 211.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 4 TR 57-94, DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21 , DC8 SRM 51-1-8B, DC8 SRM 57-7-1 FIGURE 4 ITEM "C" TR 57-94 DATED 10/01/02, DC8 SRM 51-1-11, SRM 51-3-0, AND SRM 51-3-1 . (S) 2 L 7 4 4F RT 4A25 20080826 SO 2008 8 26 C2XA08IA173 1 20080721 A 2120 UNKNOWN EMB 145 EMB145EP 3260221 SO CABIN ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14943 145040 IAH - FLIGHT 2372 - THE FLIGHT ATTENDANT REPORTED A BURNING ODOR COMING FROM ROWS 8-10. THE AIRCRAFT LANDED AT IAH WITH OUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DEFECTS NOTED, AND COULD NOT DUPLICATE THE DISCREPANCY. T HE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080826 NM 2008 8 26 KCSA081397 1 20080816 A 5320 ANGLE BOEING 747 747122 1384872 NM BS 1446 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 716CK 19753 RT BODY WHEEL WELL LONGERON BOX ANGLE IS CORRODED AT STA 1446, RBL 120, WL 113. (S) 2 L 7 4 4F RT A20WE 20080826 NM 2008 8 26 KCSA081401 1 20080816 A 5313 STRINGER BOEING 747 747249F 1384849 NM BS 690 S38L DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 FUSELAGE STRINGER IS DENTED AT STA 690, STR 38L. (S) 2 L 7 4 4F RT A20WE 20080826 EA 2008 8 26 TRAX200800795 1 20080606 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 559 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 FS 559 BULKHEAD WEB AND CAP ANGLE HAS INDICATIONS NOTED IN WEB RBL 9.00 WL 58.70 APPROX .4 INCH IN LENGTH. RBL 18.0 WL 58.70 APPROX 1.7 INCH IN LENGTH, AND CAP ANGLE LBL 18.00 AND RBL 18.0 IN RADIUS APPROX .5 INCH IN LENGTH FAILED NDT INSP . REPAIRED FS 559 BULKHEAD WEB AND CAP ANGLES FROM LBL 18 AND LBL 9, RBL 18 AND RBL 9 IAW REO 601R-53-41-260 REV B. RE QUIRES SEALANT AND PAINT. SEALED FS 559 IAW CRJ 200 MM 51-23-00-390-809. PAINTED IAW CRJ SRM 51-25-01. COMPLIED WITH REO 601R-53-41-260. SUPPLEMENTAL SDR CLOSED 6/24/08. 2 L 7 2 4F RT A21EA 20080826 SO 2008 8 26 C2XA08CL084 1 20080713 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14950 145061 DURING ROUTINE MAINTENANCE THE EMERGENCY AISLE PATH LIGHTING WAS INOPERATIVE IN THE AFT CABIN. MAINTENANCE INSPECTED AN D REPLACED THE NR 6 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. (A) 2 L 7 2 4T RT T00011AT 20080826 SO 2008 8 26 C2XA08IA163 1 20080713 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26545 145558 MCI - DURING MAINTENANCE INSPECTION THE AFT OVERWING EMERGENCY EXIT LIGHTS ON THE LT AND RT SIDES WERE FOUND TO BE INOPE RATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY POWER SUPPLY, OPERATIONALLY CHECKED WI TH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080826 NM 2008 8 26 QXEA200800875 1 20080808 A 2120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 19 413QX 4060 PDX-FLIGHT 2291 - FLIGHT ATTENDANT REPORTED FEELING ILL DUE TO A PETROLEUM ODOR IN THE CABIN DURING FLIGHT. ALSO SOME O F THE PASSENGERS ALSO REPORTED FEELING ILL DUE TO THE SAME THING. MAINTENANCE PERFORMED A GROUND RUN AT HIGH POWER SETT INGS WITH NR1 AND NR2 BLEEDS IN INDEPENDENT OPERATION. NO ODORS NOTED. COULD NOT DUPLICATE. RELEASED FOR OPERATIONAL CHECK FLIGHT. PASSED FLIGHT WITH NO DEFECTS. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080826 NM 2008 8 26 AALA200801922 1 20080721 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 182AN 29592 DFW - EMERGENCY LIGHTS AT AFT COACH CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A2NM 20080827 NM 2008 8 27 ABXA080210 1 20080711 A 5321 96F66770272 FLOOR PANEL BOEING 767 767281 1385109 NM BS 412 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 773AX 22788 UPPER CARGO SUB FLOOR PANEL BENDED BEYOND LIMITS APPROXIMATELY STA 412, RT BUTT LINE 60. REMOVED AND REPLACED PANEL IAW B767 SRM 51-40-02. (A) 2 L 7 2 4F RT A1NM 20080827 NM 2008 8 27 ABXA080211 1 20080717 A 5347 96F6675763 SEAT TRACK BOEING 767 767281 1385109 NM BS 325-347 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 773AX 22788 TRACK CORRODED AT LT BUTT LINE 7.28, STA 325-347. REMOVED AND REPLACED TRACK IAW B767 SRM. (A) 2 L 7 2 4F RT A1NM 20080827 SO 2008 8 27 CHQA200800141 1 20080713 A 3350 SOCKET EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAULTY A CHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 271SK 145305 DURING INSPECTION, THE RT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. THE OVERWING EMERGENCY LIGHT SOCKET WAS REPLACED AND THE EMERGENCY LIGHTS OPERATED NORMALLY. (A) 2 L 7 2 4T RT T00011AT 20080827 CE 2008 8 27 DXTA200803198 1 20080725 A 2120 UNKNOWN CESSNA 560 560XL 2076702 CE CABIN SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 610QS 5605210 SMOKE IN CABIN. KMDW-KMKG. (A) 2 L 7 2 4F RT A22CE 20080828 EA 2008 8 28 MAS2008F00024 1 20080810 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA ILLUMINATED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 501MJ 10047 ASH FLT 7174 CLT-IAD. NWS INOPERATIVE CAUTION MESSAGE. MAINTENANCE TROUBLESHOT AND COULD NOT DUPLICATE PROBLEM. ALL O PS GOOD. (S) 2 L 7 2 4F RT A21EA 20080828 EA 2008 8 28 MAS2008F00015 1 20080804 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27191 7191 ASH FLT 2777 PHX-BFL. EMERGENCY LIGHTS WOULD NOT COME ON. MAINTENANCE RECHARGED THE BATTERIES, OPS CHECK GOOD. (S) 2 L 7 2 4F RT A21EA 20080828 NM 2008 8 28 QXEA200800367 1 20080330 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM LT WING TE FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 356PH 502 PDX-C4 CHECK - LT WING NR 5 FLAP TRACK OUTBOARD LOWER TRACK UPPER SURFACE HAS WEAR MARKS. BLENDED IAW RD8-57-989. HFEC INSPECTED IAW D8-200 NDTM PART 651-00-01. NO CRACKS NOTED. (S) 2 H 7 2 4T RT A13NM 20080828 EA 2008 8 28 HNA2008F00043 1 20080812 A 3150 1 WARNING HORN DHAV DHC8 DHC8311 1386006 EA FALSE ACTIVATION A HNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 07 337EN 34300 34300 284 ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN SOUNDED. RECONFIGURED TRIM AND FLAPS, RESET CB 4A FOR TAKEOFF WARNING HORN. NO HORN SOUNDED. (S) 2 H 7 2 4T RT A13NM 20081128 EA 2008 11 28 ASOA200801555 1 20081124 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX OBSTRUCTED A ASOA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 848AS 7339 PAX DOOR SHOW CAUTION MSG ILLUMINATED ON PUSHBACK. RAMPERS INDICATED A "PIN" WAS OBSTRUCTING ABILITY TO CLOSE HANDLE. GATE RETURN. 2 L 7 2 4F RT A21EA 20081128 EU 2008 11 28 08FDEA04951 1 20081121 A 5311 A53988401218 FRAME AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 EMPENNAGE FRAME 84 AT STRINGER 13 L, THE FRAME LOWER CHORD IS CORRODED AT AND UNDER THE CROSSBEAM. REMOVED CORROSION FR OM THE FRAME FLANGE IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00, FIG 105 AND TABLE 102. REMOVED THE F LANGE IAW SRM 51-40-21. FABRICATED A NEW FLANGE CHORD IAW AIRBUS DWG A53988401. ALODINED IAW SRM 51-21-10. PRIMED AND IAW SRM 51-23-10. INSTALLED FLANGE IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20081128 NM 2008 11 28 DHLA2008745700 1 20081119 A 5753 FLAP TRACK BOEING 727 727224 1384076 NM ZONE 600 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 NR 6 FLAP TRACK FWD LUGS CORRODED. REPAIRED FWD LUGS IAW EO COO-2-57-333-08 DATED 10/04/08 AND BAC MSG 1-1000848556-3 D ATED 10/02/08. REFERENCE FAA FORM 8100-9 DATED 11/18/08 AND ASTAR EVA B257-00143 FOR REPAIR APPROVAL. DOCUMENTED ON N/ R 6-210. 2 L 7 3 4F A3WE 20081128 NM 2008 11 28 DHLA2008745701 1 20081004 A 5753 652163261 SKIN BOEING 727 727224 1384076 NM TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LT INBD MID-FLAP T/E WEDGE SECTION DISBONDED/HONEYCOMB CORE DELAMINATED AND CRUSHED. ACCOMPLISHED REPAIR TO HONEYCOMB A ND SKINS IAW COOPESA EO COO-CMP-2-57-309-08 DATED 10/21/08. REFERENCE FAA FORM 8110-3 DATED 10/29/08 AND ASTAR EVA B257 -00127 FOR REPAIR APPROVAL. DOCUMENTED ON COOPESA N/R 13-1. 2 L 7 3 4F A3WE 20081128 NM 2008 11 28 AALA200820023 1 20081027 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 697AN 45632 26977 AFT DECK CORRODED. REPAIRED IAW 53-60-51-2R2. 2 L 7 2 4F RT A2NM 20081128 NM 2008 11 28 QXEA2008112101193 1 20081119 A 6123 30005000056 SIGNAL COND UNIT DHAV DHC8 DHC8202 2809007 NM AUTO FEATHER MALFUNCTIONED A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 19 357PH 6 504 PDX - TESTING THE AUTO FEATHER SYS NR 1 PROP WILL FEATHER IMMEDIATELY WHEN MOVING THE TEST SWITCH FROM OFF TO NR 1 WITHO UT RELEASING SWITCH. REMOVED NR 1 SIGNAL CONDITION UNIT, REF PWC 123 MM 72-01-10, PARA 5 A.1. INSTALLED SERVICEABLE SI G COND UNIT. OPS TEST GOOD. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081128 NM 2008 11 28 ASAA0843794 1 20081024 A 5753 6546435281 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 LT OTBD AFT FLAP LOWER SURFACE IS DENTED PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0873838 1 20081118 A 5320 146A94018 PLATE BOEING 737 737790 13844CN NM BS 727D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 FLOOR PANEL SPLICE PLATE CORRODED AFT CARGO BAY. REMOVED AND REPLACED SPLICE PLATE. 2 L 7 2 4F RT A16WE 20081128 WP 2008 11 28 UPS08853891 1 20081020 A 5210 SKIN DOUG DC8 DC871F 302199D WP PAX DOOR TORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV LT FORWARD DOOR MAIN ENTRY INTERIOR SKIN TORN IN FORWARD CORNER. REPAIRED 51-09-00-0 AND DRW 5615403 2 L 7 4 4F RT 4A25 20081128 WP 2008 11 28 UPS08853892 1 20081002 A 5320 CUSP WEB DOUG DC8 DC871F 302199D WP FS 260 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATE EFN 7021991231 NRC 751026 CUSP MEMBRANE TRACK 1 BETWEEN FS26 0 AND FS360. REPAIRED IAW 53-2 -00 FIG 25. 2 L 7 4 4F RT 4A25 20081128 WP 2008 11 28 UPS08853893 1 20081011 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 40 MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV BS 40 FWD PASSENGER DOOR EXTERNAL SKIN REPAIR AROUND DOOR HANDLE DOES NOT MEET SRM CRITIA 702-F1-20. REPAIRED IAW 52-03000 FIG 1. 2 L 7 4 4F RT 4A25 20081128 NM 2008 11 28 USAA920082046 1 20081022 A 5320 65C10592154 INTERCOSTAL BOEING 737 737301 1384611 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10853028/013 LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL AT BS 960, LBL 45. REPLACED INTERCOSTA L AT BS 960, LBL 45 IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 USAA920082047 1 20081022 A 5320 65C10592155 INTERCOSTAL BOEING 737 737301 1384611 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10853028/014 LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL AT BS 947 TO BS 967, LBL 8. REPLACED I NTERCOSTAL AT BS 947 TO BS 967, LBL 8 IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 USAA920082049 1 20081111 A 5330 6545775 SKIN BOEING 737 737401 138449B NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 CLT RON MAJOR REPAIR NR 8405463 AFT FUSELAGE SKIN CRACKED AT BS 874, S24R. REPAIRED AFT FUSELAGE SKIN AT BS 874, S24R I AW SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 USAA920082048 1 20081013 A 5312 BULKHEAD BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03055380105/001 WEB FORWARD FLANGE CRACKED AT BS 178, LBL17, WL234. REPAIRED WEB FORWARD FLANGE AT BS 178, LBL 17, WL 234 IAW SRM 53-10-08 REPAIR 12. 2 L 7 2 4F RT A16WE 20081201 EA 2008 12 1 COMA0860466 1 20081113 A 5346 601R5361366 REPAIR CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE BEAM CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 784CA 7319 LT SIDE OF ENGINE BEAM PREVIOUS REPAIR ON LOWER OTBD WEB IS CRACKED. REMOVED AND INSTALLED SERVICEABLE REPAIR PARTS PER REO 601R53-61-366. 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 SWAA086516 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, RBL 6. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086517 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 27R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086526 1 20081121 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086439 1 20081120 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086429 1 20081120 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STR 26L CORRODED AT BS 980. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086431 1 20081120 A 3350 D71701100 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT LAMP INOP. REMOVED AND REPLACED BATTERY PACK PER WDM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086440 1 20081120 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086393 1 20081119 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 461WN 32465 DURING SCHEDULED HC1 CHECK, FOUND LT AFT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086394 1 20081119 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 461WN 32465 DURING SCHEDULED HC1 CHECK, FOUND RT AFT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086450 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0893709 1 20081023 A 5230 143A611028 SKIN BOEING 737 737990 NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 FORWARD CARGO DOOR HAS NUMEROUS DENTS IN THE OUTER SKIN. REPLACED FORWARD CARGO DOOR OUTER SKIN WITH A NEW SOLID SKIN. 2 L 7 4 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843746 1 20081030 A 5320 65458278 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 CRACKED INTERCOSTAL AT STA 277. REMOVED CRACKED INTERCOSTAL, INSTALLED NEW INTERCOSTAL IAW B737 400 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843749 1 20081029 A 5754 65C26602302 SKIN BOEING 737 7374Q8 138447Q NM LE SLAT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NR 5 SLAT UPPER SURFACE HAS DENT. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20081126 2008 11 26 ASAA0853764 4 20081113 A 3460 1741010201 DISPLAY BOEING 737 737890 1384527 NM COCKPIT FAULTY A ASAA K NONE O OTHER NR NOT REPORTED 1 NM 02 557AS 9410 35176 RT FMC L2 BUTTON DOES NOT CLICK BUT FUNCTIONS CONFIRMED. REMOVED & REPLACED F/O'S MCDU REF MM 34 61 01 400 802. OPS NO RMAL PER SAME. P/N VERIFICATION CONFIRMED W/ SEAMC RON. ETOPS GROUND VERIFICATION SUCCESSFUL. 2 L 7 2 4F RT A16WE 20081126 EA 2008 11 26 SWIA200820440 1 20080823 A 3233 BRACKET CNDAIR CL600 CL6002C10 1390015 EA CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 715SK 10179 C-CHECK, RIGHT MLG RETRACT ACTUATOR BRACKET ASSEMBLY PIN CORRODED. REPLACED BRACKET AND PIN. 2 L 7 2 4F RT A21EA 20081126 EA 2008 11 26 SWIA200820441 1 20081114 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 937SW 7735 FLT 6703 - AFT MOST OVERHEAD EMERGENCY FLOOD LIGHT INOP. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 20081126 EA 2008 11 26 ASOA200801508 1 20081115 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 884AS 7513 EMERGENCY TRACK LIGHTING AT ROWS 6-8 INOP. 2 L 7 2 4F RT A21EA 20081126 NM 2008 11 26 SWAA086537 1 20081121 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 220WN 32491 FOUND RT EEPLS STRIP MISSING LENS. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081128 EA 2008 11 28 QXEA2008112001176 1 20081108 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 617QX 10130 PDX - C3 - FS 280 CROSSBEAM HAS CORROSION AROUND RIVETS AND NUTPLATE HOLES ON TOP SURFACE LEF TOF CENTERLINE. REMOVED T WO RIVETS AND BLENDED ALL OF THE CORROSION LEFT OF CENTERLINE OF THE 280 BEAM IAW REO 670-63-11-046. UT THICKNESS CHECK ED IAW NDTM PART 1, 51-20-004. HI=.040 AND LO=.038". HFEC INSPECTED FOR CRACKS IAW CRJ 700 NDTM, 51-20-006, NO CRACKS NOTED. FOUND WITHIN LIMITS IAW REO 670-53-11-046. REPLACED RIVET IAW 51-42-15, ALODINED PRIMED AND PAINTED IAW 51-25- 06. 2 L 7 2 4F RT A21EA 20081128 NM 2008 11 28 ASAA0843809 1 20081103 A 5311 65C3277410 FRAME BOEING 737 7374Q8 138447Q NM BS 616 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 RT FUSELAGE INNER FRAME CHORD CRACKED AT STA 616. REMOVED CRACKED SECTION FABRICATED AND INSTALLED FILLER AND STIFFENER ANGLE IAW ASA EO 5310 02528. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 DL75E081587 1 20081119 A 2530 OVEN BOEING 757 757231 1384950 NM FWD GALLEY DIRTY A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 723TW 29378 IR - FWD RT OVEN GIVING OFF EXCESSIVE SMOKE/FUMES WHEN HEATING. OVENS CLEANED THEN CKS OK. 2 L 7 2 4F RT A2NM 20081128 NM 2008 11 28 ASAA0873841 1 20081120 A 5320 141A5410U3 INTERCOSTAL BOEING 737 737790 13844CN NM CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 INTERCOSTAL CRACKED AT BS 294 270 BL 0. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0893842 1 20081124 A 5320 111A72026 FLANGE BOEING 737 737990 NM ACCESS PANEL WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 ACCESS DOOR HAS WORN THROUGH INBD FLANGE OF LOWER BEAM CHORD. TRIMMED OUT DAMAGE INSTALLED REPAIR IAW ATS ER 08-3633 EA 900-53EA-00276. 2 L 7 4 4F RT A16WE 20081128 NM 2008 11 28 ASAA0893843 1 20081121 A 5320 147A571235 WEB BOEING 737 737990 NM BS 986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 CORROSION ON SHEAR WEB BS 986.5 RBL 30 WL 208.1. REPAIRED PER EA 900 53EA 00246 BLENDED AND TREATED. 2 L 7 4 4F RT A16WE 20081128 NM 2008 11 28 ASAA0893845 1 20081120 A 5320 149A721415 SUPPORT ANGLE BOEING 737 737990 NM CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 FRETTING/CHAFING ON SUPPORT ANGLE FOR FAIRING. REMOVED AND REPLACED INBD SUPPORT ANGLE FOR FAIRING PANEL 193AL PER SRM 51 40 05. 2 L 7 4 4F RT A16WE 20081128 EA 2008 11 28 ASOA200801550 1 20081122 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 754EV 10173 G2 GALLEY EMERGENCY LIGHT HAS SEVERAL INOP BULBS. 2 L 7 2 4F RT A21EA 20081128 EA 2008 11 28 ASOA20081501 1 20081113 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED OTBD CLIP AT FS 280 LBL9 IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE CLIP AT FS 280 O/B LBL 9 IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 20081128 NM 2008 11 28 ASAA0843767 1 20081024 A 5754 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 9 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NUMBER 9 SPOILER UPPER SURFACE IS DENTED. INSTALLED REPAIR DOUBLER PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAA920082030 1 20081104 A 5310 507945178 DOOR FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10552010/009 AND 03C10552010/010 AFT FRAME HAS A 0.025 INCH CRACK AT NR 6 AND A 0.125 INCH CRA CK AT NR 7 STOP PIN ACCESS HOLE AT FORWARD ENTRY DOOR. REPAIRED AFT FRAME AT NR 6 AND NR 7 STOP PIN ACCESS HOLE AT FORW ARD ENTRY DOOR IAW US AIRWAYS EA NR 100722. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAA920082033 1 20081024 A 5347 6546814 SEAT TRACK BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753005/033 LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN BS326 TO BS360 RBL24.75. REP LACED SEAT TRACK BETWEEN BS326 TO BS360 RLB24.75 IAW B737 SRM 53-00-52. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAA920082028 1 20081031 A 5330 6545800219 BEAR STRAP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03055380550/001 2 CRACKS ON BEAR STRAP AT L1 DOOR UPPER HINGE CUTOUT BS303, S10L. 0.50 INCHES LO NG AND 0.187 INCHES LONG. REPAIRED BEAR STRAP AT L1 DOOR UPPER HINGE CUTOUT BS303, S10L, IAW US AIRWAYS EA NR 100723. 2 L 7 2 4F RT A16WE 20081201 2008 12 1 ASAA0853879 4 20081123 A 2310 G7404124 PANEL BOEING 737 737890 1384527 NM COCKPIT FAULTY A ASAA K NONE O OTHER CR CRUISE 1 NM 02 559AS 8573 35178 COMM 1 FREQUENCY TRANSFER SWITCH INOP SWAPPED 1 & 2 RADIO TUNING CONTROL PANELS. ACTUAL POSITIONS: NR 1 S/N 6440 & NR 2 S/N 6441. RELEASED PER MEL 23 3N. NR 2 RADIO TUNING PANEL INOP. SWAPPED RADIO TUNING PANELS TO ORIGINAL POSITIONS. REMOVED & REPLACED NR 1 RADIO TUNING PANEL REF MM 23 12 41 000 801 & 23 12 41 400 801. OPS NML PER SAME. NR 2 RTP OPS NORMAL PER SAME. 2 L 7 2 4F RT A16WE 20080828 NM 2008 8 28 QXEA200800528 1 20080521 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 697-670 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 411QX 4055 PDX-C4 CHECK- SEAT TRACK NR 9 HAS CORROSION AT THREE PLACES, TWO ON OUTBOARD FLANGE AT APPROX STA X697.00 AND 670.00 AND ONE INSIDE TRACK AND ON TRACK FROM STA X709.00 TO 705.00. REMOVED AND INSTALLED NEW SEAT TRACK NR 9 IAW 8/400 SRM 51-4 0-07, 51-42-05, 51-40-15. (S) 2 H 7 2 4T RT A13NM 20080828 NM 2008 8 28 QXEA200800530 1 20080521 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 411QX 4055 PDX-C4 CHECK - SEAT TRACK NR 5 HAS CORROSION ON OUTBOARD FLANGE AT APPROX STA X23.00. REMOVED NR 5 SEAT TRACK AND INSTA LLED NEW NR 5 SEAT TRACK REF DHC8-400 SRM 51-40-15 & 51-42-05. (S) 2 H 7 2 4T RT A13NM 20080828 EA 2008 8 28 QXEA200800601 1 20080530 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 785 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 610QX 10033 RFD-C4 CHECK - CORRODED SIDE SEAT TRACK ON RT SIDE AT FS 785. BLENDED CORROSION FROM RT SIDE SEAT TRACK AT FS 785. REM OVED .008 MATERIAL FOR BLEND, WITHIN LIMITS. MAX ALLOWABLE BLEND IS .035 INCHES. ALL WORK DONE IAW CRJ BOMB REO 670-53 -00-013. TREATED IAW CRJ 700 SRM 51-21-11. (S) 2 L 7 2 4F RT A21EA 20080828 EU 2008 8 28 USAA920081557 1 20080818 A 5315 D53472172205 FLOORBEAM AIRBUS A319 A319112 3930323 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 PIT-S4-MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 AND FR68, -Y1162 TO -1292. REPLACED FLOOR BEAM BETWEEN FR66 AND FR68, -Y1162 TO -1292 IAW A319 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080828 NM 2008 8 28 F3LA200800576 1 20080819 A 5321 D5367204701000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 928FR 2236 DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 161BF WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO PANEL 161B F IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCE PTABLE. (S) 2 L 7 2 4F RT A28NM 20080828 NM 2008 8 28 USAA920081555 1 20080816 A 5330 6545775 SKIN BOEING 737 7374B7 1384702 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT-C4-MAJOR REPAIR - FUSELAGE SKIN CRACKED 2 INCHES FORWARD OF BS 727F, S24R. REPAIRED FUSELAGE SKIN 2 INCHES FORWARD OF BS 727F, S24R IAW B737SRM 53-00-01. REPAIR 31 TEMPORARY REVISION 53-27. (S) 2 L 7 2 4F RT A16WE 20080828 SO 2008 8 28 C2XA08RI116 1 20080808 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 17138 145727 FLIGHT 2129 -EWR- FLIGHT CREW REPORTED THAT PASSENGER NOTICED BURNING ODOR FROM AIR VENTS ABOUT HALFWAY THROUGH FLIGHT, THEN ODOR WENT AWAY. EWR MAINTENANCE PERFORMED OPERATIONAL CHECK OF PACK 1 AND 2 SYSTEM AND NO ODOR WAS DETECTED. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080829 NM 2008 8 29 SWAA084427 1 20080809 A 5321 6545833 FLOOR SKIN BOEING 737 7373H4 1384600 NM COCKPIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND COCKPIT FLOOR SKIN CRACKED AT BS 248.8, RBL 25.5. REPAIRED FLOOR SKIN PER SRM & ER. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084693 1 20080825 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 ABXA080219 1 20080801 A 5330 148T31111 SKIN BOEING 767 767232 1385132 NM BS 1654 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 745AX 22222 LEFT STA 1654.5 SEVERAL FUSELAGE SKIN CRACKS STRINGERS 3-6. REPAIRED SKIN CRACKS AT STRINGERS 3-6 IAW B767 SRM. (S) 2 L 7 2 4F RT A1NM 20080829 SO 2008 8 29 C2XA08TY086 1 20080819 A 3350 20131A BATTERY EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 NR 1 EMERGENCY LIGHT BATTERY NOT CHARGING. REMOVED AND REPLACED BATTERY IAW EMB 145 AMM 33-50-04. OPS CHECK GOOD. ACF T RELEASED AND RETURNED TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080829 NM 2008 8 29 SWAA084707 1 20080825 A 5311 6546549 FRAME BOEING 737 7373T0 1384582 NM BS 767 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084708 1 20080825 A 5311 6546555 FRAME BOEING 737 7373T0 1384582 NM BS 867 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084711 1 20080825 A 5753 SKIN BOEING 737 7373Q8 1384670 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 1707 23254 DURING SCHEDULED 24Y CHECK, FOUND LT WING OUTBOARD T/E FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER M M. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084439 1 20080810 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 716 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 716, STR 4R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080829 EA 2008 8 29 REX2008F00042 1 20080814 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A REXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 8631E 7631 FLAP FAILURE MESSAGE IN CRUISE FL330. OVERSPEED WARNING SOUNDING THEN FLAP FAILURE AT ZERO. QRH FOLLOWED, DIVERTED TO IAD, DECLARED EMERGENCY WITH UNEVENTFUL LANDING. TROUBLESHOT PER BOMBARDIER FIM AND AMM. ALL LRUS PASSED. VERIFIED RI GGING OF THE LT AND RT BRAKE POSITION SENSING UNITS (BPSU), FOUND TO BE CORRECT. PERFORMED OPERATIONAL CHECKS OF THE FL AP SYSTEM IAW BOMBARDIER AMM WITH NO DEFECTS FOUND. (S) 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 SWAA086625 1 20081125 A 5210 652212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR SKIN CRACKED AT UPPER HINGE, BS 305, BETWEEN WL 258 TO WL 261. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086626 1 20081125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086606 1 20081125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086607 1 20081125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 DL757081633 1 20081118 A 5311 146N10426 FRAME BOEING 757 757232 1384965 NM BS 1480 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 CORROSION ON FRAME UPPER FLANGE AND SIDE BS 1480 RBL 28 WL 148. REPAIRED FRAME PER SRM 53-00-07. 2 L 7 2 4F RT A2NM 20081201 EA 2008 12 1 QXEA2008112601198 1 20081121 A 5210 601R317725 ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 601QX 10009 PDX - PAX DOOR STEP SUPPORT STRUCTURE AFT SIDE BOTTOM (CURVED) CLOSING ANGLE CRACKED APPROX MIDWAY UP DOOR, 6 INCHES LON G. REPLACED DRAY ANGLE IAW REO 670-52-11-072. RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 DL757081639 1 20081118 A 5340 146N5395820 STRINGER CLIP BOEING 757 757232 1384965 NM BS 1519.5 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 CORROSION ON STRINGER CLIP BS 1519.5, STR 27R OUT OF LIMITS. REMOVED AND REPLACED PART. 2 L 7 2 4F RT A2NM 20081201 NE 2008 12 1 DLM88081640 2 20081124 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 SMOKE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 963DL 44514 49982 725866 DURING CRUISE, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. BOTH AFT LAV SMOKE DETECTORS WERE GOING OFF. ENGINE ANTI-ICE ON, LT PACK TURNED OFF SMOKE OUT. CAPTAIN DECLARED EMERGENCY ON APPROACH. LANDED AT SCHEDULED DESTINATION. REPLACED N R 1 ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 20081201 NM 2008 12 1 DL757081643 1 20081124 A 5330 146N37505 SKIN BOEING 757 757232 1384965 NM FS 1652 S20L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 DURING AGING AIRCRAFT INSPECTION, A DENT WAS FOUND AT FS 1652 JUST ABOVE THE S-20L LAP JOINT. DUE TO THE CLOSE PROXIMIT Y TO THE SUBJECT LAP, IT WAS OUT OF LIMITS PER SRM REQUIREMENTS. AS SUCH, MANUFACTURER WAS CONTACTED FOR REPAIR INSTRUC TIONS. MANUFACTURER APPROVED REPAIR INSTALLED PER ERA 471508-14. 2 L 7 2 4F RT A2NM 20081201 NM 2008 12 1 DL757081644 1 20081124 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM BS 610, S17L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 DURING AN AGING AIRCRAFT INSPECTION, A DENT AND CREASE WERE FOUND IN THE FUSELAGE SKIN AT STA 610 BETWEEN S-17L AND S-18 L. THE DAMAGED SKIN WAS CUT OUT AND REPAIRED PER BOEING INSTRUCTIONS. 2 L 7 2 4F RT A2NM 20081201 EA 2008 12 1 SWIA200820468 1 20081119 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 776SK 10241 FLT 5867 - SECOND TO LAST OVERHEAD EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 SWAA086567 1 20081124 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND LT KEEL BEAM CRACKED AT O/B EDGE, BS 541. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086568 1 20081124 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 788SA 30603 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 3. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086570 1 20081121 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 220WN 32491 FOUND LT EEPLS LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086571 1 20081121 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 220WN 32491 FOUND RT EEPLS LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 DL757081613 1 20081111 A 5320 SUPPORT BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 1527-1530 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 724164 CORROSION ON FLOOR TO SIDEWALL SUPPORT RT LOWER FLANGE INBD COMMON TO FASTENERS. REPAIRED PER DELTA ER/A 471503-14 REV ORIG. 2 L 7 2 4F 4 F RT A2NM E24NE 20081201 NM 2008 12 1 SWAA086615 1 20081125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 18L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086579 1 20081123 A 2121 BCREFA1210 GASPER FAN BOEING 737 7373H4 1384600 NM CABIN FAULTY A SWAA K NONE O OTHER CR CRUISE 1 SW 29 385SW 26600 DIVERSION, UNIDENTIFIED ODOR IN PAX CABIN AT ALTITUDE. INSPECTED FOUND GASPER C/B POPPED. INSPECTED AREA, NO DAMAGE NO TED. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 20081201 EA 2008 12 1 SWIA200820471 1 20081119 A 3397 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS MALFUNCTIONED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 956SW 7825 FLT 6108 - FORWARD GREEN LIGHT SECTION OF EMERGENCY FLOOR LIGHTING INOP. REPLACED NR 2 EMERGENCY LIGHTING INVERTER. 2 L 7 2 4F RT A21EA 20081201 WP 2008 12 1 AALA200810192 1 20081118 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP ZONE 100 BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 NUMBER 6 SEAT TRACK TANG BROKEN AT STATION 672 TO 673. INSTALLED NEW SEAT TRACK PER AARD 53-20-00-10. 2 L 7 2 4F RT A6WE 20081201 WP 2008 12 1 AALA200810194 1 20081112 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 584AA 53247 EMERGENCY LIGHT BATTERY PACK BS-107 STATION 1190R INOP. REPLACED DEFECTIVE BATTERY PACK WITH SERVICEABLE PACK. 2 L 7 2 4F A6WE 20081201 WP 2008 12 1 AALA200810185 1 20081121 A 5313 LONGERON DOUG DC9 DC983 3022083 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 594AA 53284 LONGERON 2L CRACKED JUST AFT OF FRAME 1418. REPAIRED PER AARD 53-30-00-2. 2 L 7 2 4F RT A6WE 20081201 WP 2008 12 1 AALA200810186 1 20081121 A 5313 LONGERON DOUG DC9 DC983 3022083 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 594AA 53284 LONGERON 2R END FITTING CRACKED AT STATION 1420. REPAIRED PER AARD 53-30-00-2. 2 L 7 2 4F RT A6WE 20081201 WP 2008 12 1 AALA200810187 1 20081113 A 5320 PAN DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70529 49921 CORROSION ON FORWARD CARGO LOWER DOOR PAN. INSTALLED NEW LOWER SECTION OF THRESHOLD PAN, FOR FORWARD CARGO, PER SRM 53- 05-00. 2 L 7 2 4F A6WE 20081201 NM 2008 12 1 AALA200820034 1 20081029 A 5320 141N516153 SUPPORT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 663AM 53392 25297 G1-B GALLEY MOUNT SUPPORT CORRODED. REPLACED IAW SRB 53-10-5. 2 L 7 2 4F RT A2NM 20081201 EA 2008 12 1 SWIA200820443 1 20080810 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 959SW 7840 C-CHECK, LEFT AND RIGHT FS 625 ANGLES CRACKED IN RADIUS. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081126 WP 2008 11 26 AALA200802712 1 20081009 A 3350 P4010049 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 969TW 53619 SFO SEAT MOUNTED EMERGENCY LIGHT AT SEAT 32D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 32D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A6WE 20081126 NM 2008 11 26 AALA200820022 1 20081023 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 697AN 45632 26977 AFT MAIN DECK PLATE CORRODED. REPAIRED IAW SRM 53-60-51-2R2. 2 L 7 2 4F RT A2NM 20081126 NM 2008 11 26 SWAA086559 1 20081121 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED HC1 CHECK, AFT GALLEY RT BATTERY PACK FAILED LONG TEST. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086560 1 20081121 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED HC1 CHECK, FWD GALLEY LT BATTERY PACK FAILED LONG TEST. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0843769 1 20081025 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 7 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NUMBER 7 SPOILER LOWER SURFACE DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081128 EA 2008 11 28 QXEA2008112001175 1 20081108 A 5751 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA LT AILERON CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 617QX 10130 PDX - C3 - LT AILERON TOP LEADING EDGE IS CHAFED IN SEVERAL PLACES. BLENDED CHAFE IAW SRM 57-61-01-001-A01. UT THICKNE SS CHECKED BLENDED AREAS IAW NDTM 51-20-04 FOUND TO BE OUT OF LIMITS. REMOVED LT AILERON TOP LEADING EDGE IAW SRM 51-42 -06 PG 8 STEP 11 AND THE 4 HUCK BOLTS IAW SRM 51-42-21 PG 11 STEP 10. MATCH DRILLED, COUNTERSUNK, AND ALODINED NEW FROM STOCK LEADING EDGE. INSTALLED LEADING EDGE REF SRM 51-42-21, 51-21-11, 51-42-06 AND 51-72-22. 2 L 7 2 4F RT A21EA 20081128 NM 2008 11 28 ASAA0843811 1 20081101 A 5754 6526603191 SKIN BOEING 737 7374Q8 138447Q NM NR 3 SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NR 3 SLAT T/E WEDGE DELAMINATED AT INBD AND OTBD ENDS. PREPPED DELAMINATED AREAS FABRICATED AND INSTALLED REPAIR CORE F ILLER AND DOUBLER IAW SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081128 EA 2008 11 28 ASOA200801543 1 20081119 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 PASSENGER DOOR INNER SKIN HAS CORROSION AROUND FASTENER HOLES UNDER ACCESS PNLS 832AR, 832BR, 832CR, 832ER AND 832GR. C ORROSION IS MINOR SURFACE. 2 L 7 2 4F RT A21EA 20081128 NM 2008 11 28 DHLA2008745699 1 20081119 A 5753 FLAP TRACK BOEING 727 727224 1384076 NM ZONE 600 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 NR 7 FLAP TRACK FWD ATTACH LUGS CORRODED. REPAIRED FWD LUGS IAW COOPESA EO COO-2-57-334-08 DATED 10/04/08 AND BAC MSG 1 -1000865923-2 DATED 10/02/08. REFERENCE FAA FORM 8100-9 DATED 11/18/08 AND ASTAR EVA B257-00146 FOR REPAIR APPROVAL. D OCUMENTED ON COOPESA N/R 6-223. 2 L 7 3 4F A3WE 20081128 NM 2008 11 28 ASAA0873837 1 20081118 A 5320 146A940116 SPLICE BOEING 737 737790 13844CN NM BS 722 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON FLOOR SPLICE STRIP AFT CARGO BAY BS 772 RBL 20 TO LBL 20. REMOVED FABRICATED AND REPLACED SPLICE PLATE. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0843825 1 20081028 A 5320 654795711 STRAP BOEING 737 7374Q8 138447Q NM CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 AFT CARGO PIT DOOR OPENING SILL PLATE TAPERED STRAP CORRODED STA 775 TO STA 855 RBL 24. REMOVED DAMAGED STRAP LOCATED D RILLED INSTALLED A REPLACEMENT STRAP IAW B737 400 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0893862 1 20081120 A 5320 143A7510 INTERCOSTAL BOEING 737 737990 NM BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 BAFFLE INTERCOSTAL BENT FWD CARGO BAY STA 500G-500H. REMOVED FABRICATED NEW AND INSTALLED INTERCOSTAL. 2 L 7 4 4F RT A16WE 20081128 NE 2008 11 28 ASAA0853807 2 20081118 A 7200 ENGINE BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE NR 2 SURGES A ASAA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 02 587AS 4317 35684 895978 JUST PRIOR TO LEVEL OFF AT FL 340 NR 2 ENG BEGAN TO SURGE BETWEEN 80 PERCENT AND RED LINE ON N1 GAGES N1 INDICATION RED BOXED MOMENTARILY TWICE EGT N2 FUEL FLOW WERE SURGING AS WELL. E 1.5 CK LIST FOLLOWED AT POWER REDUCTION EVERYTHING SMOO THED OUT AND ENG RAN AS PER NORMAL WITH ALL GOOD INDICATIONS NOTES IN CLEAR SMOOTH SKYS ENG A/I OFF CENTER FUEL EMPTIED AND PUMPS OFF JUST PRIOR TO SURGING NO EXCESSIVE VIBRATION NOTED. NR 2 ENGINE REMOVED UNDER INVESTIGATION 2 L 7 2 4F 4 F RT A16WE E2GL 20081128 NM 2008 11 28 ASAA0873864 1 20081120 A 5347 CARGO TRACK BOEING 737 737790 13844CN NM BS 772 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON TIE DOWN TRACK DOOR SUPPORT AFT CARGO BAY BS 772 LBL 17. OUT OF LIMITS. REMOVED TIE DOWN TRACK. FABRICAT ED AND INSTALLED REPAIR PARTS. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0873865 1 20081120 A 5320 SUPPORT BOEING 737 737790 13844CN NM BS 754-847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON FLOOR TO SIDEWALL SUPPORT AFT CARGO BAY BS 754 847 LBL 20. REMOVED FLOOR TO SIDEWALL SUPPORT. FABRICATED NEW SUPPORT AND INSTALLED. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 AALA200820024 1 20081024 A 5315 14N6509131 FLOORBEAM BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 640A 56247 24598 FLOORBEAM CORRODED. REPAIRED IAW EA B757-53-004838 DATED 10/24/2008. 2 L 7 2 4F RT A2NM 20081128 NM 2008 11 28 AALA200820025 1 20081023 A 5320 STRAP BOEING 757 757223 1384957 NM ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 663AM 53392 25297 STRAP ATTACHED TO BOTTOM OF FLOORBEAM FORWARD OF NR 2 SEAT TRACK CRACKED. REPAIR DOUBLER INSTALLED IAW SRM 53-10-51-2R. 2 L 7 2 4F RT A2NM 20081128 EU 2008 11 28 AALA200802715 1 20081010 A 3350 BR964814 LIGHT AIRBUS 300 A300B4605R 3930308 EU ZONE 200 DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 18066 509 JFK - EMERGENCY LIGHT ASSEMBLY AT SEAT 21C DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GR OUND CHECKED NORMAL OPERATIONS. 2 L 7 2 4F RT A35EU 20081128 NM 2008 11 28 ASAA0873867 1 20081125 A 5320 147A571234 WEB BOEING 737 737790 13844CN NM BS 986-1016 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON UNDERSIDE OF WEB BS 986-1016 RBL 38. FOUND WHILE ACCESSING FOR BS 986 FLOORBEAM REMOVAL. REMOVED WEB FABR ICATED NEW WEB AND INSTALLED. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0843814 1 20081107 A 5755 654645262A SKIN BOEING 737 7374Q8 138447Q NM NR 5 SPOILER DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NR 5 SPOILER INSERTS CORRODED/SKIN DELAMINATED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLE RS IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0873819 1 20081119 A 5320 146A75026 SUPPORT BOEING 737 737790 13844CN NM BS 867-887 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT ZEE BS 867-887 RBL 20. REPLACED DAMAGED SECTION OF ZEE SUPPORT FRO M BS 867 887 RBL 20. 2 L 7 2 4F RT A16WE 20081128 EA 2008 11 28 QXEA2008112001177 1 20081108 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 617QX 10130 PDX - C3 - FS 280 CROSSBEAM HAS 1 INCH CRACK ON THE TOP RT SIDE, 3 INCHES OUTBOARD OF THE RT LONGITUDINAL BEAM AND A 1.5 INCH CRACK ON THE FWD SIDE AT THE RT LONGITUDINAL BEAM ATTACHMENT. REMOVED RT SIDE OF BEAM IAW SRM 51-42-06. REMOVED INTERCOSTALS AT RBL36 AND RBL 18 AND DRIP TRAY. LOCATED DRILLED AND DEBURRED NEW RT 280 BEAM, SPLICE PLATES AND CAMLOCK CHANNEL IAW REO 670-53-11-047 AND SRM 51-42-06. INSTALLED RT 280 BEAM WITH SOLID RIVETS REF REO 670-53-11-047 AND 51-4 2-06. INSTALLED SPLICE PLATE IAW REO 670-53-11-047. INSTALLED OUTBOARD INTERCOSTAL REF SRM 51-42-21. INSTALLED CAMLOC K CHANNEL AND DRIP TRAY IAW SRM 51-42-06 AND 51-42-13. 2 L 7 2 4F RT A21EA 20081128 NM 2008 11 28 ASAA0843795 1 20081113 A 5753 6546435281 SKIN BOEING 737 7374Q8 138447Q NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 LT OTBD AFT FLAP LOWER SURFACE DENTED PREPPED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 5 1 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0873856 1 20081117 A 5321 453A1610 FLOOR PANEL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 FWD CARGO BAY AFT FLOOR PANEL CORRODED. INVESTIGATED CORROSION ON FWD CARGO BAY AFT FLOOR PANEL ALONG OUTER EDGES. FAB RICATED NEW PANEL USING OLD PANEL AS TEMPLATE. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086623 1 20081125 A 5330 65457665 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 500D, STR 10L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086605 1 20081125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 DL757081634 1 20081115 A 5347 146N544018 CARGO TRACK BOEING 757 757232 1384965 NM BS 1520 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 CORROSION ON LOWER SURFACE OF TIE DOWN FITTING COMMON TO NUTPLATE LOCATIONS BS 1520 RBL 20 AND AFT NUT PLATES, OUT OF LI MITS. REMOVED AND REPLACED PART PER SRM 53-00-53/51-40-02/51-40-06. 2 L 7 2 4F RT A2NM 20081201 EA 2008 12 1 SWIA200820473 1 20081118 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 440SW 7589 FLT 4762, AFT EMERGENCY LAMP INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 SWAA086572 1 20081124 A 3350 81000 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED MV2 CHECK, FOUND RT AFT ENTRY EEPLS LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 DL76L081615 1 20081121 A 2530 COFFEEMAKER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE MID GALLEY ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 195DN 28452 724164 AT CRUISE F/A NOTICED ODOR IN MID GALLEY POSSIBLY ELECTRICAL, AFTER C/B PULLED FOR COFFEEMAKER, DISAPPEAR IN A FEW MINUT ES. ALL AREA INSPECTED, COFFEEMAKER LIGHT AND ALL EQUIPMENTS CHECKED WITH NO FAULTS FOUND. 2 L 7 2 4F 4 F RT A1NM E24NE 20081201 NM 2008 12 1 DL757081616 1 20081115 A 5320 143N51974 ANGLE BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 724164 WL 208 BS 660 RBL 48, WEB UPPER ANGLE CRACKED. REMOVED AND REPLACED ANGLE. 2 L 7 2 4F 4 F RT A2NM E24NE 20081201 NM 2008 12 1 SWAA086577 1 20081123 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086582 1 20081124 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM CORRODED AT BETWEEN BS 700 TO BS 714, RBL 24. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081201 SO 2008 12 1 SWIA200820478 1 20081118 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 562SW 120336 EMERGENCY EXIT SIGN AND LIGHT BROKEN AT ROW 6BC. REPLACED SIGN. 2 L 7 2 4T RT A31SO 20081201 WP 2008 12 1 AALA200810195 1 20081112 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS WEAK A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 584AA 53247 MID CABIN BATTERY PACK INOP RIGHT SIDE STATION 671. REPLACED WEAK BATTERY PACK . 2 L 7 2 4F A6WE 20081201 NM 2008 12 1 AALA200820033 1 20081027 A 5315 FLOORBEAM BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 640A 56247 24598 FLOORBEAM CORRODED. REPAIRED IAW EA B757-53-004738. 2 L 7 2 4F RT A2NM 20081201 EA 2008 12 1 SWIA200820446 1 20080827 A 5320 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 918SW 7645 C-CHECK, FS 280 RBL 9 SUPPORT CLIPS CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081201 EA 2008 12 1 SWIA200820448 1 20080827 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 918SW 7645 C-CHECK, FS 280 LEFT BRACKET, RIGHT SIDE OF COCKPIT FLOOR OPENING, CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20080829 NM 2008 8 29 USAA920081544 1 20080808 A 5320 6545834256 INTERCOSTAL BOEING 737 7373B7 1384580 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT-Q6 -MAJOR REPAIR- LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL AT BS 314, WL 208, RBL 10. REPLACED INTERCOSTAL AT BS 3 14, WL 208, RBL 10 IAW BOEING DRAWING 6545834 AND B737 SRM 53-00-04. (S) 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 USAASB08063 1 20080818 A 3397 SPLICE BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 PHX - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS FROM SEAT ROWS 18 TO 23, LT, INOPERATIVE. MAINTENANCE REPAIRED A S PLICE. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD. (S) 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084726 1 20080826 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED PM CHECK, FOUND RT AFT CABIN EMERGENCY EXIT LIGHT ILLUMINATED WITH SWITCH IN THE ON POSITION. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084724 1 20080826 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084666 1 20080820 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084665 1 20080824 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084659 1 20080823 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 780 AND BS 813, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084651 1 20080824 A 3350 20121 CHARGER BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND LT FWD CABIN EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM . 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084650 1 20080824 A 3350 20121 CHARGER BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND RT AFT CABIN EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM . 2 L 7 2 4F RT A16WE 20080902 EA 2008 9 2 A6WA200840549 1 20080723 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A A6WA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 31 448AW 7814 FLAPS FAILED AT ZERO AFTER TAKEOFF. DID NOT LAND OVERWEIGHT. CORRECTIVE ACTION IN PROGRESS. (A) 2 L 7 2 4F RT A21EA 20080902 NM 2008 9 2 SWAA084647 1 20080822 A 2560 65C16280 HOOK BOEING 737 7377H4 1384404 NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 233LV 32501 R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084646 1 20080821 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 253WN 32511 DURING SCHEDULED MV1 CHECK, FOUND EEPLS END CAP MISSING AT ROW 1 ABC. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084645 1 20080821 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 723SW 27855 DURING SCHEDULED HC1 CHECK, RT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080902 2008 9 2 SWAA084641 4 20080821 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084635 1 20080821 A 5330 6545766 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084677 1 20080825 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947, STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084676 1 20080825 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED BRDG CHECK, FOUND NOSE W/W CEILING PANEL SKIN CRACKED BETWEEN RBL 7.75 AND LBL 7.75. REPAIRED SKIN PER ACO. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084719 1 20080825 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 291.5, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084718 1 20080825 A 5310 6546956 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 400 AND BS 420, STR 17L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084717 1 20080825 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084716 1 20080825 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 28L CRACKED AT BS 360. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084683 1 20080823 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 892, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084681 1 20080821 A 5330 6545766 SKIN BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 502D, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 2008 9 2 SWAA084680 4 20080825 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084621 1 20080820 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 746SW 29798 DURING SCHEDULED HC2 CHECK, RT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080902 EA 2008 9 2 A6WA200840526 1 20080623 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 446AW 7806 CRACK FOUND ON CROSS BEAM AT FS 280.00 LBL 9.0. CROSS BEAM AT FS 280.00 LBL 9 REPAIRED IAW CRJ 200 REO 601R-53-11-171 R EV D SCHEME A. (A) 2 L 7 2 4F RT A21EA 20080902 NM 2008 9 2 SWAA084616 1 20080820 A 5311 6546548 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 EA 2008 9 2 A6WA200840546 1 20080720 A 7603 THROTTLE CABLE CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE LACK OF LUBE A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 425 7663 RT THRUST LEVER DIFFICULT TO MOVE, SHUT OFF THROUGH FULL THROTTLE RANGE. CLEANED AND LUBED RT THROTTLE CABLE CONTROL SY STEM IAW AWAC SUPP 05-028 AND IAW AMM 76-11-00. PERFORMED FUNCTIONAL TEST OF RT THROTTLE CONTROL GEARBOX ASSEMBLY, OPS CHECK NORMALLY IAW CRJ AMM 76-11-00. (A) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 A6WA200840532 1 20080627 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 446AW 7806 CORROSION FOUND ON SERVICE DOOR LOWER SILL PLATE. LOWER SILL PLATE OF SERVICE DOOR REPLACED IAW CRJ 200 SRM 51-41-04. (A) 2 L 7 2 4F RT A21EA 20080902 NM 2008 9 2 SWAA084615 1 20080820 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 AALA200801896 1 20080717 A 3350 BPS73 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 319AA 22320 JFK - EMERGENCY LIGHT SIGN AT FIRST CLASS RT AISLE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT SIGN AT FIRST CLASS RT AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A1NM 20080827 WP 2008 8 27 NWAA083959758 1 20080819 A 3350 POWER SUPPLY DOUG DC9 DC941 302207N WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 758NW 47286 DURING LINE CHECK, MAINTENANCE FOUND THAT THE LT EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED T HE POWER SUPPLY AND THE LIGHT RETURNED TO AN OPERATIONAL CONDITION. (S) 2 L 7 2 4F A6WE 20080827 NM 2008 8 27 F3LA200800568 1 20080819 A 5321 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 928FR 2236 DURING C3 C-CHECK, INSPECTION NOTED FORWARD PIT PANEL 131CF WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO PANEL 131CF IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080827 EU 2008 8 27 USAA920081556 1 20080817 A 5315 D53472089004 FLOORBEAM AIRBUS A319 A319112 3930323 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 PIT-S4- MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR68, -Y1182. REPLACED FLOORBEAM AT FR68, -Y1182 I AW A319 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080827 EA 2008 8 27 MAS2008F00016 1 20080807 A 2750 860D10018 FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 77195 14856 14416 7195 ASH FLT 7050 ORD-MDT. FLAPS FAIL AT 8 DEGREES IN FLIGHT. REPLACED FECU. (S) 2 L 7 2 4F RT A21EA 20080828 NM 2008 8 28 QXEA200800526 1 20080521 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 411QX 4055 PDX-C4 CHECK LT FUSELAGE SKIN HAS GOUGE ON EXTERNAL SURFACE AT APPROX STA X51.00 AND Z129.00. BLENDED GOUGE IAW 8-400 S RM 51-14-00. HFEC IAW 8-400 NDTM PART 6 51-00-01 NO CRACKS. NOTED BLENDED ARE FOUND WITHIN LIMITS IAW RD8/4-53-2356. ALODINED, PAINTED IAW RD8/4-53-2356 AND Q400 SRM 51-25-05 PG 206/PARA F-1-4. (S) 2 H 7 2 4T RT A13NM 20080828 EU 2008 8 28 MAS2008F00055 1 20080814 A 5220 SKIN SAAB SF340 340B 7860101 EU EMERGENCY EXIT DENTED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 411XJ 340B411 FWD RT EMERGENCY EXIT 814 HAS 10 DENTS IN OUTER SKIN. REPAIRED DENTS NR 1 AND NR 4 IAW EOS52133. FOR MORE INFO SEE CON TINUATION CARD 085396. CONTINUATION CARD 085396, NR 1 TEN DENTS IN OUTER SKIN FOR RT FWD EMERGENCY EXIT DOOR 814 REQUIR ES MAPPING, DIMENSION AND EVALUATION. (S) 2 L 7 2 4T RT A52EU 20080828 NM 2008 8 28 F3LA200800571 1 20080819 A 5321 D5367314500000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 928FR 2236 DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 152XG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO TRANSITION PANEL 152XG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080828 NM 2008 8 28 KCSA081417 1 20080821 A 5313 STRINGER BOEING 747 747249F 1384849 NM BS 695 S39L DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 STRINGER 39L DENTED AT STA 695. (S) 2 L 7 4 4F RT A20WE 20080828 NM 2008 8 28 KCSA081419 1 20080821 A 5312 BULKHEAD BOEING 747 747249F 1384849 NM BS 2360 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 AFT PRESSURE BULKHEAD AT STA 2360 DENTED WL340 LBL 35 AFT SIDE. (S) 2 L 7 4 4F RT A20WE 20080828 CE 2008 8 28 DXTA200803183 1 20080718 A 2750 FLAP SYSTEM CESSNA 750 750 2076810 CE TE FLAPS FAILED E DXTA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 07 918QS 7500223 FLAP FAILED TO RETRACT ON CLIMBOUT. COMPLETED CKLIST-FLAP WOULD NOT "RESET" AFTER LANDING, PER ACP, FOUND "FAULT CODE 2 - MOTOR FAULT CODE FAULT". RESET FAULT CODE, TESTED FLAPS; FLAPS STILL WOULD NOT RETRACT; FAULT CODE 2 DISPLAYED AGAIN . (A) 2 L 7 2 4J RT T00007WI 20080828 NM 2008 8 28 P5CA0801571 1 20080725 A 5300 STRUCTURE BOEING 747 74747UF 1384812 NM FUSELAGE DAMAGED A P5CA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 EA 15 416MC 32838 DURING GROUND HANDLING THE TAIL JACK STRUCK THE TAIL SECTION OF THE AIRCRAFT NEAR THE TAIL POST FITTING IN SECTION 48 AT BS 2602. ACCOMPLISHED INTERIM REPAIR ACCORDING TO EO 4453A189, SRM 53-00-01 FIG 201, REPAIR 11. INITIAL AND REPEAT IN SPECTIONS TO BE SCHEDULED PER DER 8110-3 DATED 25 JULY 2008. (A) 2 L 7 4 4F RT A20WE 20080829 NM 2008 8 29 SWAA084428 1 20080810 A 5311 6546533 FRAME BOEING 737 7373H4 1384600 NM BS 500D S26R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 26R. REPAIRED PER SRM & ER. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084592 1 20080819 A 5315 BAC1409100146 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727D CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 727D, LBL 12 TO RBL 8. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084593 1 20080819 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500C S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084604 1 20080819 A 5330 6545800 SKIN BOEING 737 7373A4 1384585 NM BS 303 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 303, BETWEEN WL 233 AND WL 238. REPAIRED SKIN PER SWA EA . 2 L 7 2 4F RT A16WE 20080829 EA 2008 8 29 REX2008F00043 1 20080813 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY FALSE ACTIVATION A REXA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 25 8694A 7694 RECEIVED CARGO SMOKE MESSAGE AT GATE, DETERMINED AFTER INSPECTION TO BE A FALSE WARNING. POWER RESET TO DATA CONCENTRAT OR UNIT (DCU) AND PERFORMED OPERATIONAL CHECK OF CARGO DETECTION SYSTEM IAW BOMBARDIER AMM. NO DEFECTS FOUND. (S) 2 L 7 2 4F RT A21EA 20080829 NM 2008 8 29 SWAA084706 1 20080825 A 5311 6546538 FRAME BOEING 737 7373T0 1384582 NM BS 597 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084710 1 20080825 A 5322 6546546 SHEAR TIE BOEING 737 7373Q8 1384670 NM BS 787 S27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084648 1 20080822 A 3350 8200048901 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 292WN 32538 R1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084634 1 20080821 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084682 1 20080821 A 5330 6545765 SKIN BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 512B, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084624 1 20080820 A 5322 6546546 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 847, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 AALA200801886 1 20080715 A 2910 HOSE BOEING 757 757223 1384957 NM HYD SYSTEM LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 21 677AN 29427 PTY INFLIGHT T2189/15JUL - CREW REPORTED LT HYDRAULIC SYSTEM QUANTITY DECREASED RAPIDLY. LANDED PTY WITHOUT INCIDENT. FOUND NOSE GEAR ACTUATOR LINE BROKEN FROM NOSE WHEEL WELL. REPLACED NOSE GEAR ACTUATOR LINE. SYSTEM GROUND CHECKED NOR MAL OPERATION. (S) 2 L 7 2 4F RT A2NM 20080902 NM 2008 9 2 AALA200801884 1 20080715 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 905AN 29507 MIA - EMERGENCY LIGHT AT LT NR 1 DOOR DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LT NR 1 DOOR. SYSTEM GRO UND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 AALA200801833 1 20080625 A 5314 146T3223 KEELBEAM BOEING 767 767223 1385123 NM BS 1219 S38L CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AA 22327 AFW - KEEL BEAM AT STATION 1219 HAD CORROSION REMOVED FROM THE VERTICAL AND HORIZONTAL FLANGES. REPAIRED PER MRB 767-32 37. VERTICAL FLANGE: 0.4 INCH BY 0.9 INCH WITH A DEPTH OF 0.050 INCH. HORIZONTAL FLANGE: 0.8 INCH BY 2.4 INCH WITH A D EPTH OF 0.160 INCH. (S) 2 L 7 2 4F RT A1NM 20080902 EU 2008 9 2 AALA200801889 1 20080621 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 40064 507 MIA - EMERGENCY LIGHT AT SEAT 29C MISSING LENS. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 29C. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A35EU 20080902 NM 2008 9 2 ABXA080209 1 20080710 A 5347 SEAT TRACK BOEING 767 767281 1385109 NM BS 412-423 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 773AX 22788 SEAT TRACK CORRODED LT BUTT LINE 13.28, STA 412-423. REMOVED AND REPLACED SEAT TRACK IAW B767-200 SRM 51-40-2. (A) 2 L 7 2 4F RT A1NM 20080902 EA 2008 9 2 TRAX200800784 1 20080613 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 FLIGHT ATTENDANT AND RAMPERS REPORT CABIN DOOR EXTREMELY DIFFICULT TO CLOSE. FLT 4900 DEL 27MINS. CYLCED PAX DOOR SEVE RAL TIMES. OPS CK GOOD IAW CRJ 200 AMM 52-11-01. 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 TRAX200800801 1 20080618 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 MAIN CABIN DOOR DIFFICULT TO OPEN, RAMP CREW COULD NOT OPEN FROM THE OUTSIDE. COMPLIED WITH CABIN HANDLE INSP, CLEANED AND LUBE, OK FOR SERVICE PER CRJ200AMM52-10. 2 L 7 2 4F RT A21EA 20080902 SO 2008 9 2 C2XA08IA191 1 20080810 A 3350 78241 INVERTER EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27523 145389 IAH - DURING MAINTENANCE INSPECTION THE FORWARD FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED THE NR 2 EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED F OR RETURN TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080902 NM 2008 9 2 SWAA084584 1 20080819 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084583 1 20080819 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 22R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084582 1 20080819 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 947, STR 19R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084581 1 20080819 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER 23L CORRODED AT BS 727E. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084577 1 20080819 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 213WN 34217 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084575 1 20080815 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 209WN 32484 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080902 SO 2008 9 2 C2XA08IA187 1 20080804 A 3234 8271013 CONTROL HANDLE EMB 145 EMB145XR 3260214 SO MLG INOPERATIVE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 12145 21526 21526 145745 IAH-FLIGHT 2352 - THE CREW REPORTED THAT AFTER TAKEOFF THE LANDING GEAR DID NOT INITIALLY RETRACT, AND HAD THE ASSOCIATE D DISAGREE MESSAGE ON EICAS. THE ACFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER. OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080902 EA 2008 9 2 CHQA20080165 1 20080818 A 2741 70623 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE STAB TRIM MOTOR FAULTED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 652BR 136 136 7429 E872797 FLIGHT 5338, IAH TO VPS. AFTER TAKEOFF THE CREW RECEIVED A STAB TRIM CHANNEL 1 FAIL MESSAGE AND RETURNED TO IAH AND LAN DED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND FAULT CODES POINTING TO THE MOTOR CONTROL UNIT. THE MOTOR CONT ROL UNIT WAS REPLACED AND THE TRIM SYSTEM OPS CHECKED GOOD DURING THE TEST FLIGHT. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080902 NM 2008 9 2 SWAA084525 1 20080814 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 783SW 29809 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PA CK PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084517 1 20080814 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518D, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084516 1 20080814 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND STRINGER 23R CRACKED BETWEEN BS 492 AND BS 500. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084515 1 20080814 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND STRINGER 22R CRACKED BETWEEN BS 492 AND BS 500. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084499 1 20080813 A 5311 65C22910 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 13R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084492 1 20080813 A 3350 D71701100 BATTERY PACK BOEING 737 7375H4 138449D NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 UPON ARRIVAL TO AIRCRAFT, EMERGENCY EXIT LIGHTS ON. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084491 1 20080813 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084489 1 20080813 A 5210 507945 DOOR BOEING 737 7373H4 1384600 NM FWD ENTRY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FWD ENTRY DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED DOOR PER ER. 2 L 7 2 4F RT A16WE 20080902 NE 2008 9 2 CHQA200800127 2 20080629 A 7200 CF343B1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 2 DAMAGED A CHQA O OTHER O OTHER NR NOT REPORTED 1 GL 11 701BR 14622 7448 GEE870845 FLIGHT 5531, SDF TO IAH. ON CLIMBOUT OF KSDF, AT APPROXIMATELY 4,000 FT, THE FLIGHT CREW HEARD A LOUD BAND AND THE E2 I TT CLIMBED INTO THE RED AREA ALONG WITH A TRIPLE CHIME. WHILE PREPARING TO RETURN TO KSDF, THE APPROPRIATE QRH CHECKLIS TS WERE FOLLOWED AND E2 WAS SHUT DOWN. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DURING INITIAL INSPECTION THAT MULTIPLE FAN BLADES ALONG WITH THE CORE COWL WERE DAMAGED ON E2. DURING A BORE SCOPE INSPECTION OF THE CORE DAMAG ED 1ST STAGE VG VANES WERE FOUND. THE AIRCRAFT IS CURRENTLY OUT OF SERVICE FOR E2 ENGINE CHANGE. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080902 EA 2008 9 2 CHQA200800140 1 20080712 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS FAULTY A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 701BR 14851 7448 GEE872845 FLIGHT 5994, RDU TO IAH. UPON FLAP RETRACTION FROM FLAPS 8 TO ZERO AFTER TAKEOFF FROM RDU, THE FLIGHT CREW RECEIVED A F LAPS FAIL MESSAGE ON EICAS. THE MESSAGE WAS CONFIRMED AND THE FLAPS WERE FAILED AT 3 DEGREES ON THE LEFT FLAP AND ZERO DEGREES ON THE RIGHT FLAP. THE QRH WAS FOLLOWED AND THE FLIGHT LANDED BACK AT RDU WITHOUT INCIDENT. MAINTENANCE INTERR OGATED THE FECU AND FOUND THE FAULT CODES FROM THAT FLIGHT POINTED TO THE FECU ITSELF AS BEING THE CAUSE OF THE FAULT. THE FECU WAS REPLACED ALONG WITH THE SKEW DETECTION UNIT AND THE NR 4 SKEW DETECTOR. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080902 EA 2008 9 2 CHQA200800135 1 20080710 A 2750 8004403 SENSOR CNDAIR CL600 CL6002B19 1900309 EA RT WING TE FLAPS INOPERATIVE A CHQA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 11 701BR 7448 FLIGHT 5716, IAH TO JAX. DURING CLIMB WHEN THE FLAPS WERE SELECTED FROM 8 TO 0 THE RT FLAP RETRACTED TO 0 AND LT FLAP F ROZE AT 3 DEGREES AND A FLAP FAIL MESSAGE APPEARED ON EICAS. THE APPROPRIATE CHECK LISTS WERE FOLLOWED AND THE FLIGHT R ETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A FLAP RE-RIG AND THE FLAP SYSTEM OPERATED NORMALLY. (A) 2 L 7 2 4F RT A21EA 20080902 SO 2008 9 2 CHQA200800158 1 20080804 A 3260 8005701 PROXIMITY SENSOR EMB 135 EMB135KL 3260302 SO ALLSN AE3007 AE3007A 03030 GL LT MLG FAULTY A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 376SK 145578 CAE311852 FLIGHT 5360, STL TO ATL. DURING CLIMB, AFTER RETRACTING THE LANDING GEAR, THE FLIGHT CREW RECEIVED A LG AIR/GND FAIL ME SSAGE ON EICAS ALONG WITH AURAL WARNINGS FOR FLAPS AND TRIM. THE FLIGHT LEVELED OFF AND THE APPROPRIATE QRH CHECKLISTS WERE FOLLOWED. THE FLIGHT RETURNED TO STL AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIR/GROUND SYSTEM A ND FOUND INCORRECT GAPS ON THE RT NR 2 PROXIMITY SWITCH AND NR 2 LT PROXIMITY SWITCH, AND THE GAPS WERE RESET PER AMM 3 2-63-05. THE LT NR 1 PROXIMITY SWITCH WAS FOUND BAD USING THE GSE TOOLING AND WAS REPLACED. AFTER CORRECTING THE PRECED ING FAULTS, THE AIR/GROUND SYSTEM FUNCTIONED NORMALLY. (S) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080902 EA 2008 9 2 COMA086351 1 20080809 A 5311 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 965CA 7131 RT SIDE FUSELAGE FRAME DOUBLER AT FS 640.00 IS CRACKED. COMPLIED WITH MODIFICATION K601R360094 AT FS 640 IAW S/B 601R-5 3-061. (S) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 COMA086356 1 20080817 A 5311 601R3500733 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 640 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 916CA 7014 DURING FS 640 FRAME INSPECTION FOUND 640 FRAME AND SKIN DOUBLER CRACKED, ON RT SIDE AT STRINGER 9. REMOVED DAMAGED SECT ION OF FRAME FROM STRINGER 6-20 AND REPLACED WITH SPLICED IN REPAIR FRAME AND SKIN DOUBLER, REF SB 601R-53-061 PART C, R EO 601R-53-61-366 AND REO 601R-53-61-569. (S) 2 L 7 2 4F RT A21EA 20080902 CE 2008 9 2 DXTA200803227 1 20080815 A 2711 TRIM SYSTEM CESSNA 750 750 2076810 CE AILERONS MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 950QS 7500050 CLIMBING THROUGH FL230 AT 270 KNOTS INDICATED, "RETRIM L WING DOWN" AT THE TIME THE AP WAS DISENGAGED, AND THE ACFT REQU IRED 50 PERCENT LT AILERON TRIM. (S) 2 L 7 2 4J RT T00007WI 20080902 EA 2008 9 2 EHS2008F00000 2 20080702 A 8520 PISTON GULSTM 500 500S 0141107 SW LYC O540 IO540E1B5 41532 EA HARTZL HCC3Y HCC3YR GL NR 3 CYLINDER BURNED A EHSA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 WP 07 4QS 17551 L808848 CK2602 WHILE FLYING A FIRE MISSION IN SUPPORT OF USFS, THE PILOT NOTICED THE RT ENG OIL PRESSURE FLOWLY STARTING TO DECREASE. THE DECISION WAS MADE TO RETURN TO THE AIRPORT. AS OIL PRESSURE CONTINUED TO DECREASE, THE DECISION WAS MADE TO SHUTDOW N, FEATHER, AND SECURE THE ENG. A SAFE LANDING WAS ACCOMPLISHED AND THE ACFT WAS TAKEN OUT OF SERVICE. UPON INSPECTION , IT WAS FOUND THAT THE NR 3 CYLINDER`S PISTON RINGS AND RING GROOVES WERE DAMAGED, WHICH PRESSURIZED THE CASE AND PUMPE D THE ENG OIL OVERBOARD. THE ENG WAS REMOVED AND SENT FOR OVERHAUL AS A PRECAUTION. PROBABLE CAUSE: POSSIBLE BROKEN R ING OR POSSIBLE DETONATION. (S) 1 H 7 2 3O 3 O 6A1 1E4 5 C P25EA 20080828 EA 2008 8 28 MAS2008F00035 1 20080813 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 154SF 7154 AIR SHUTTLE 7094 IN CWA. SEVERAL SECTIONS OF FLOOR PATH LIGHTING INOPERATIVE. REPLACED NR 2 BATTERY PACK INVERTER. (S ) 2 L 7 2 4F RT A21EA 20080828 EU 2008 8 28 MAS2008F00056 1 20080814 A 5280 STRUCTURE SAAB SF340 340B 7860101 EU LT MLG DOOR CHAFED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 411XJ 340B411 LEFT OUTBOARD MLG DOOR, WHERE SPADE DOOR MAKES CONTACT IS CHAFED. REPAIRED DAMAGE ON LT OUTBOARD MLG DOOR IAW MAL EO510 31. SEE 409 286973 FOR DOOR INSTALLATION AND OPS/RIG CHECK. CONTINUATION CARD 085449 LT OUTBOARD, MLG DOOR REMOVED TO FOM. SEE 409 286973 FOR INSTALLATION OF DOOR. (S) 2 L 7 2 4T RT A52EU 20080828 NM 2008 8 28 F3LA200800577 1 20080820 A 5320 D53112534200 BLANKING PLATE AIRBUS A319 A319111 3930336 NM GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 928FR 2236 DURING C3 C-CHECK, INSPECTION NOTED R1 FORWARD GIRT BAR BLANKING PLATE HAS CORROSION AT HOLES. MAINTENANCE FABRICATED N EW NUT PLATE ASSEMBLY FOR GIRT BAR BLANKING PLATE AND INSTALLED IAW THE REQUIREMENTS OF AIRBUS DRAWING D531 12534 AND A3 19 SRM 51-42-11, PARAGRAPH 7. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080828 EA 2008 8 28 QXEA200800603 1 20080530 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 797 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 610QX 10033 RFD-C4 CHECK - CORRODED SIDE SEAT TRACK ON LT SIDE FS 797. BLENDED CORROSION FROM LT SIDE SEAT TRACK AT FS 797. REMOVE D .006 MATERIAL FOR BLEND, WITHIN LIMITS. MAX ALLOWABLE BLEND IS .035 INCHES. ALL WORK DONE IAW CRJ BOMB REO 670-53-00 -013. TREATED IAW CRJ BOMB REO 670-53-00-013. (S) 2 L 7 2 4F RT A21EA 20080828 NM 2008 8 28 F3LA200800570 1 20080819 A 5321 D5367227100000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 928FR 2236 DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 152TG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO TRANSITION PANEL 152TG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080828 NM 2008 8 28 KCSA081416 1 20080821 A 5313 STRINGER BOEING 747 747249F 1384849 NM BS 700 S41L DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 STA 700 STRINGER TIE AT STRINGER 41L IS DENTED. (S) 2 L 7 4 4F RT A20WE 20080829 NM 2008 8 29 SWAA084432 1 20080809 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM BS 801 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 801, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080829 2008 8 29 SWAA084433 4 20080809 A 2565 D35154 SLIDE BOEING 737 7373Q8 1384670 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 L1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. RE-INSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084730 1 20080826 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 787 S27L/R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081201 EA 2008 12 1 SWIA200820449 1 20080828 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 699BR 7801 C-CHECK, FLOOR SUPPORT ATTACH CLIP AT FS 280 LBL 9 CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081201 EA 2008 12 1 SWIA200820450 1 20080828 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 699BR 7801 C-CHECK, FLOOR SUPPORT ATTACH CLIPS AT FS 280 RBL 9 CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081201 EA 2008 12 1 SWIA200820451 1 20080828 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 699BR 7801 C-CHECK, RIGHT ENGINE THRUST FITTING CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081201 EA 2008 12 1 SWIA200820456 1 20080810 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 959SW 7840 C-CHECK, FS 280 LBL9 INBOARD AND OUTBOARD TIE CLIPS CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081201 EA 2008 12 1 SWIA200820459 1 20080810 A 5420 RISER CNDAIR CL600 CL6002B19 1900309 EA NACELLE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 959SW 7840 C-CHECK, FRETTING CORROSION AT LEFT PRODUCTION RISER. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 AALA200820035 1 20081029 A 5320 146N5246U6 GUSSET BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 663AM 53392 25297 RIGHT NR 4 DOOR DRAIN GUSSET CORRODED. REPAIRED IAW SRM 51-21-03. 2 L 7 2 4F RT A2NM 20081201 SO 2008 12 1 SWIA200820460 1 20081117 A 2730 6225734002 SERVO EMB 120 EMB120ER 3260203 SO ELEVATOR BINDING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 17600 17600 120271 FLT 5749 - ELEVATOR BINDING. REPLACED NR 1 STICK PUSHER SERVO, PN 622-5734-002, SN ON 3079, SN OFF 3640. 2 L 7 2 4T RT A31SO 20081201 SO 2008 12 1 SWIA200820461 1 20081117 A 2710 SUPPORT EMB 120 EMB120ER 3260203 SO AILERON SYS BENT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 FLT 5790 - AILERONS BINDING. REPLACED BENT RVDT ROD SUPPORT ON AILERON BELLCRANK. 2 L 7 2 4T RT A31SO 20081201 EA 2008 12 1 SWIA200820462 1 20081123 A 5610 NP1393225 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER TX TAXI/GRND HDL 1 NM 07 495CA 7774 FLT 2871 - LEFT SIDE WINDSCREEN CRACKED ON LANDING. REPLACED WINDOW. 2 L 7 2 4F RT A21EA 20081201 CE 2008 12 1 DXTA2008112403371 1 20081123 A 3260 INDICATOR CESSNA 560 560XL 2076702 CE MLG INOPERATIVE E DXTA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 647QS 5605547 RT GEAR DOWN INDICATOR LIGHT FAILED TO ILLUMINATE WHEN GEAR SELECTED DOWN. 2 L 7 2 4F RT A22CE 20081201 NE 2008 12 1 ASAA0853880 2 20081123 A 7320 1754M36P01 GASKET BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE NR 2 ENGINE LEAKING A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 587AS 35684 RIGHT ENGINE HAS FUEL LEAK FOUND FUEL TUBE GASKET CONNECTING TO HMU LEAKING. VERIFIED FUEL LEAK DURING IDLE LEAK CHECK. REMOVED & REPLACED GASKET REF MM 73 21 10 400 801 F00 (ITEM 34) FIG 401. IDLE LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081201 NM 2008 12 1 SWAA086596 1 20081125 A 5753 65C26686 WEDGE BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND NR 2 L/E SLAT T/E WEDGE UPPER SURFACE DELAMINATED. REPAIRED WEDGE PER SRM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086561 1 20081122 A 5743 115A5211 FITTING BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 746SW 29798 DURING SCHEDULED MV3 CHECK, FOUND LT MLG FWD UPPER I/B TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086534 1 20081123 A 3350 20121 CHARGER BOEING 737 737301 1384611 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED SPV CHECK, FOUND FWD LT OVER HEAD EMERGENCY EXIT LIGHT INOP. R&R BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086535 1 20081121 A 2560 61020 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 220WN 32491 FOUND LT AFT FLASHLIGHT INOP. R&R BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086536 1 20081121 A 2560 61020 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 220WN 32491 FOUND RT AFT FLASHLIGHT INOP. R&R BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0873818 1 20081119 A 5320 146A750213 SHIELD BOEING 737 737790 13844CN NM CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON FLOOR TO SIDEWALL SUPPORT SHIELD IN AFT CARGO BAY BS 847 866 RBL 20. REMOVED AND REPLACED FLOOR TO SIDEWAL L SUPPORT BS 847-866 RBL 20. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0873839 1 20081123 A 5320 143A7501 SUPPORT BOEING 737 737790 13844CN NM BS 500-500D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 500-500D. CORROSION CLEAN UP AT BS 500A & 10.5 OUT OF LIMITS REPAIR DOUBLER I NSTALLATION ACCOMPLISHED PER SRM 53 00 53 REPAIR 6. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0843785 1 20081024 A 5753 6546486149 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 LEFT INBOARD MID FLAP TE WEDGE UPPER SURFACE IS DENTED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0853792 1 20081116 A 2131 2193301AA CONTROLLER BOEING 737 737890 1384527 NM CABIN PRESSURE MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 558AS 9284 35177 PRESSURIZATION CONTROLLER FAILED HAD AUTO FAIL AND ALTN LIGHTS CPC NR 2 LOGGED CODE 101 AND 006. FIM 21 31 TASKS 803 AND 804 NEED TO BE ACCOMPLISHED. NO FAULTS LOGGED ON CPC NR 1. CONFIRMED AUTO FAIL FLIGHT ILLUMINATED IN AUTO POSITION. PERFORMED FIM TASK 22 31 00 TASK 810-801 FOUND DADC NR1 FAULT LOGGED ON NR 2 CABIN PRESS CONTROLLER. RESET AND CLEARED FAULT. SYSTEM BITE TEST OK. NR 2 CABIN PRESSURE C/B RESET. 2 L 7 2 4F RT A16WE 20081128 EA 2008 11 28 ASOA200801516 1 20081105 A 5320 PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 OPERATION 76/PNL 444BT HAS A CRACK ABOUT 1 INCH LONG IN IT. 2 L 7 2 4F RT A21EA 20081128 EA 2008 11 28 ASOA200801518 1 20081115 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 409-559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 LT SIDE PRESSURE FLOOR SILL PLATE STILL HAS AREAS OF CORROSION FROM FS 409+128 TO FS 559, LBL 36 TO LBL 44, REF MWC 110. CORROSION IS IN DIFFERENT AREAS THAN PREVIOUSLY BLENDED. 2 L 7 2 4F RT A21EA 20081128 EA 2008 11 28 ASOA200801519 1 20081105 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 WARDROBE EMERGENCY EXIT LIGHTNING WIRE IS BROKEN AT SPLICE. THIS SDR WILL REMAIN OPEN PENDING MTC DETERMINATION OF AN A PPROPRIATE CORRECTIVE ACTION. 2 L 7 2 4F RT A21EA 20081128 EA 2008 11 28 ASOA200801520 1 20081116 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 693-708 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 713EV 10081 LT SIDEWALL SEAT RAILS HAVE SCATTERED CORROSION BETWEEN FS 693.00 TO FS 708.00. 2 L 7 2 4F RT A21EA 20081128 NM 2008 11 28 ASAA0843775 1 20081112 A 5340 69353527 STRINGER CLIP BOEING 737 7374Q8 138447Q NM BS 727 S25L CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 STRINGER CLIP IS CORRODED. REPLACED CLIP PER SRM 51-40-02 AND DWG 69-35352 B. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086585 1 20081125 A 5314 6545866 BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND LT KEEL BEAM CORRODED AT BS 545. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAA2008111792076 1 20081109 A 5310 6545855538 CREASE BEAM BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 MCN - MAJOR REPAIR - DROP IN MAINTENANCE, CORROSION ON RIGHT CREASE BEAM INNER CHORD AT BS 967, RBL 60, WL 207.8. REPLA CED CREASE BEAM INNER CHORD AT BS 967, RBL 60, WL 207.8 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 DL76P081624 1 20081123 A 5247 ACTUATOR BOEING 767 767332 1382001 NM APU DOOR MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 143DA 25991 RTB, DUE TO APU DOOR STATUS MESSAGE LOCKED DOOR OPEN PER MEL 49-15-01B. RECONNECTED APU INLET DOOR ACTUATOR CONNECTOR A ND PUT ACFT IN NORMAL CONFIG. OPERATED APU START/STOP THRU SEVERAL CYCLES W/NO DEFECTS. APU OPS NML, MCO AND PLACARD REMOVED. 2 L 7 2 4F RT A1NM 20081201 CE 2008 12 1 GUUA11200801 1 20081120 A 2913 11438800013 POWERPACK BEECH 1900 1900D 1154162 CE HYDRAULIC SYS SLUGGISH A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 29 87557 UE246 PILOT REPORTED LANDING GEAR EXTENSION AND RETRACTION TAKES EXTREME LONG TIME. REPLACED HYDR POWER PACK. OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 20081201 CE 2008 12 1 GUUA11070802 1 20081107 A 5411 1181200363 KEELBEAM BEECH 1900 1900D 1154162 CE LT NACELLE CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87557 UE246 DURING SCHEDULED ROUTINE MAINT DISCOVERED LT NACELLE INBD KEEL HAS A 1.0 INCH CRACK FWD OF LANDING GEAR TRUNION BOLT. R EMOVED AND REPLACED LT NACELLE INBD KEEL. 2 L 7 2 4T RT A24CE 20081201 NM 2008 12 1 USAA SB08114 1 20081119 A 3350 WIRE BOEING 737 737300 1384610 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 154AW 23776 PHX - SEAT 2 LEFT FORWARD ESCAPE PATH LIGHT INOPERATIVE. MAINTENANCE TERMINATED THE BROKEN WIRE. 2 L 7 2 4F RT A16WE 20081201 CE 2008 12 1 DXTA2008112503372 1 20081124 A 2150 A/C PACK CESSNA 750 750 2076810 CE ODOR E DXTA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 07 956QS 7500156 PREFLIGHT CABIN PAC HAS STRONG VERY STRONG, DIRTY SOCK/OIL ODOR WHEN APU RUNNING. 2 L 7 2 4J RT T00007WI 20081201 CE 2008 12 1 GLBA200811131 1 20081111 A 5313 STRINGER BEECH 1900 1900D 1154162 CE BS 177 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 21 237YV UE237 DURING CONFORMITY CHECKS A CRACK WAS FOUND AT STRINGER CUTOUT AT FS 177 AND 9R. CRACK RADIATES .2 INCH. REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW B1900D SRM 51-70 AT FS 177. REPAIR AREA APPROX 4.6 INCHES BY 2.6 INCHES. 2024 T3, .07 1 INCHES, MS20470 RIVETS. RII INSP COMPLIED WITH IAW TASKCARD 8.2.1. 2 L 7 2 4T RT A24CE 20081201 CE 2008 12 1 DJFA2008080 1 20081116 A 3240 BRAKE ASSY BEECH MU300 400A 1155402 CE MLG MALFUNCTIONED E DJFA H DEACTIVATE SYST/CIRCUITS O OTHER LD LANDING 1 EA 23 442FL RK334 ON LANDING CREW REPORTED NO BRAKING ACTION WHEN APPLYING BRAKES INITIALLY. PUSHING HARDER ON THE BRAKES YIELDED SLIGHT IMPROVEMENT IN BRAKING BUT ALSO RESULTED THE BRAKES GRABBING. CONTROL IMPROVED WHEN DEACTIVATING THE ANTI-SKID SYS. 2 H 7 2 4F RT A16SW 20081201 EU 2008 12 1 USAA2008112192103 1 20081118 A 5347 D53371110010 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - CORROSION ON SEAT TRACK ASSEMBLY BETWEEN FR41 TO FR47, -Y765. REPLACED SEAT TRACK ASSEMBLY BE TWEEN FR41 TO FR47, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081201 EU 2008 12 1 USAA2008112492104 1 20081121 A 3397 CONNECTOR AIRBUS A321 A321211 3930370 EU CABIN LOOSE A USAA K NONE L NO TEST NR NOT REPORTED 1 EA 19 188US 1724 FLT 960 SAN-PHX - EEL - EMERGENCY EXIT LIGHT INOPERATIVE BY ROW 9 (2 L&R). MAINTENANCE TIGHTENED LOOSE CONNECTION ON CE ILING. OPERATIONAL CHECK WAS NORMAL. 2 L 7 2 4F RT A28NM 20081201 NM 2008 12 1 USAA920082053 1 20081008 A 5320 6547957011 STRAP BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL C21 MAJOR REPAIR NR 6062390 CORROSION ON STRAP AT BS767 TO BS867, RBL21. REPLACED STRAP AT BS767 TO BS867, RBL21 IA W B737 SRM 51-40-02-09. 2 L 7 2 4F RT A16WE 20081201 EU 2008 12 1 USAA920082056 1 20081112 A 3350 32145410 POWER SUPPLY AIRBUS A321 A321211 3930370 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 184US 24569 3891 1651 LOG PAGE 4310910 FLT NR 788 CLT-TPA EEL EMERGENCY POWER SUPPLY UNIT FAILED AFT MID CABIN RT SIDE. MX R&R THE EPSU. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081201 NM 2008 12 1 USAA920082071 1 20081116 A 5330 6552988 SKIN BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 PHX - RON MAJOR REPAIR NR 4451796 FUSELAGE SKIN CRACKED BETWEEN BS927 TO BS947.5, S23L. REPAIRED FUSELAGE SKIN BETWEEN BS927 TO BS947.5, S23L IAW B737 SRM 53-00-01-2R 31. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAA920082069 1 20081010 A 5315 6546811 FLOORBEAM BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL C21 MAJOR REPAIR NR 6139584 INTERGRANULAR CORROSION ON FLOOR BEAM UPPER CHORD AT BS986.5, WL208.1, BETWEEN LBL44 TO RBL44 IN PASSENGER CABIN. REPAIRED FLOOR BEAM UPPER CHORD AT BS986.5, WL208.1, BETWEEN LBL44 TO RBL44 IAW US AIRWAYS EA NR 132084. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAA920082050 1 20081111 A 5330 6545775 SKIN BOEING 737 737401 138449B NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 CLT RON MAJOR REPAIR NR 8405462 AFT FUSELAGE SKIN CRACKED AT BS897, S25R. REPAIRED AFT FUSELAGE SKIN AT BS897, S25R IAW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 20081201 EU 2008 12 1 USAA920082064 1 20081114 A 3350 P4010021 BATTERY AIRBUS 320 A320231 3930325 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST NR NOT REPORTED 1 EA 19 626AW 65 LOG PAGE 8360664 FLT NR 239 PHX-DTW EMERGENCY EQUIPMENT FLIGHT ATTENDANT FLASHLIGHT AT 2R IS DISCHARGED / INOPERATIVE. MX R&R THE AFT FLIGHT ATTENDANT FLASHLIGHT BATTERY. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081201 NM 2008 12 1 USAA920082038 1 20081023 A 5320 69770651 INTERCOSTAL BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753005/022 LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL BETWEEN BS294 TO BS312, LBL11. REPL ACED INTERCOSTAL BETWEEN BS294 TO BS312, LBL11 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081201 EU 2008 12 1 USAA920082051 1 20081109 A 5347 SEAT TRACK AIRBUS 330 A330323 3940030 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AY 370 BFM C2 MAJOR REPAIR NR 6127118 CORROSION ON SEAT TRACK AT FR54 TO FR58, -Y450. REPAIRED SEAT TRACK AT FR54 TO FR58, -Y45 0 IAW A330 SRM 53-00-15, 51-42-11 AND 51-73-00. 2 L 7 2 4F RT A46NM 20081201 NM 2008 12 1 USAA920082041 1 20081018 A 5315 BAC1518399 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10853028/024 LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM T-CAP AT BS986.5, BETWEEN LBL50 TO RB L50. REPLACED FLOOR BEAM T-CAP AT BS986.5, BETWEEN LBL50 TO RBL50 IAW US AIRWAYS TYPICAL REPAIR NR 53-10-05-B. 2 L 7 2 4F RT A16WE 20081202 NM 2008 12 2 USAA2008112492120 1 20081122 A 5315 FLOORBEAM BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 253AY 24894 BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM AT BS 325, RBL 14 THRU RBL 20. REPAIRED FLOORBEAM AT BS 325, R BL 14 THRU RBL 20 IAW B767 SRM 53-00-51 & 51-40-02. 2 L 7 2 4F RT A1NM 20081202 NM 2008 12 2 USAA2008112492115 1 20081118 A 5210 507945272 DOOR BOEING 737 7374B7 138449C NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - FORWARD ENTRANCE DOOR CRACKED AT INTERIOR SKIN AT NR 7 STOP PIN HOLE ON AFT SIDE OF DOOR. REP AIRED FORWARD ENTRANCE DOOR INTERIOR SKIN AT NR 7 STOP PIN HOLE IAW US AIRWAYS TYPICAL REPAIR 52-10-16. 2 L 7 2 4F RT A16WE 20081202 NM 2008 12 2 USAABB08171 1 20081122 A 3260 WARNING SYSTEM BOEING 757 757225 1384959 NM COCKPIT FALSE ACTIVATION A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 920UW 22199 CLT - FLT 1556 EN ROUTE SXM TO CLT. AFTER TAKEOFF FROM SXM, EICAS MESSAGE "GEAR DOORS" AND THE GEAR LIGHTS CAME ON. T HE CREW RECYCLED THE GEAR AND ALL GEAR LIGHTS AND MESSAGES WENT OUT. THE FLIGHT CONTINUED TO CLT AND LANDED WITHOUT FUR THER INCIDENT. MAINTENANCE PERFORMED TROUBLESHOOTING AND MULTIPLE GEAR SWINGS. NO FAULTS WERE FOUND. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 20081202 NM 2008 12 2 USAA2008112492107 1 20081121 A 3350 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 825AW 1527 FLT 192 - IAD-PHX - EEL - EMERGENCY LIGHTS WILL NOT PASS TEST, LEFT EMERGENCY POWER SUPPLY UNIT FAILS. RESET EMERGENCY CIRCUIT BREAKERS; PERFORMED BITE TEST ON FORWARD FLIGHT ATTENDANT PANEL. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008112492105 1 20081121 A 5210 H384110 LEVER AIRBUS A321 A321211 3930370 EU R2 DOORS BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 194UW 3629 FLT 1579 PHX-LAX - EMERGENCY EQUIPMENT - SLIDE ARM LEVER BROKE OFF THE R2 DOOR. MAINTENANCE REMOVED AND REPLACED THE R2 DOOR EMERGENCY ESCAPE SLIDE MECHANISM PER AIRBUS MAINTENANCE MANUAL 52-22-22. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081202 NM 2008 12 2 MZZA0800005 1 20081116 A 3350 BPS73 CHARGER BOEING 737 737824 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A MZZA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14235 28947 SEVERAL EMERGENCY LIGHTS IN ACFT CABIN NOT ILLUMINATING DURING TEST. FOUND BATTERY CHARGER M1674 AND BATTERY IN FORWARD OVERHEAD PANEL AND BATTERY AT CHARGER M1694 BAD. REMOVED AND REPLACED SAME PER AMM 33-51-06. OPS CHECKS NORMAL. 2 L 7 2 4F RT A16WE 20081202 EA 2008 12 2 MALA080198 1 20081125 A 3230 SELECTOR VALVE CNDAIR CL600 CL6002D24 1390016 EA MLG FAULTED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 913XJ 15148 ON APPROACH GEAR DISAGREE WARNING MESSAGE CAME ON. WENT THROUGH THE PROCEDURES ON 7.10.03, WHICH LED UP TO PULL GEAR HA NDLE. ONCE PULLED GEAR CAME DOWN AND LANDING WAS NORMAL AND NOSE STEERING WORKED. FOUND MLG SELECTOR VALVE TO BE AT FA ULT, REMOVED AND REPLACED MLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 20081202 SO 2008 12 2 SIMA200833603 1 20081128 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 616AE 145092 ON FLIGHT 3389 CREW REPORTED SMOKE IN THE COCKPIT WITH BURNING ELECTRICAL ODOR AT GATE WITH PASSENGERS LOADED. AIRCRAFT REMOVED FROM SERVICE. PERFORMED ABNORMAL ODOR/SMOKE CHECK, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081202 NE 2008 12 2 DXTA2008112603373 2 20081125 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWC JT15 JT15D5D 52192 NE SHUTDOWN E DXTA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 393QS 5600393 DURING SPEED BRAKE CHECK, WHEN LT THROTTLE WAS BROUGHT FWD AND RETURNED TO IDLE, ENGINE ROLLED BACK AND SHUTDOWN. 2 L 7 2 4F 4 F RT A22CE E45NE 20081202 CE 2008 12 2 Z5FA111808N408CS1 1 20081118 A 3230 LANDING GEAR CESSNA 525 525B 2076616 CE INOPERATIVE E Z5FA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 63 408CS 525B0045 UPON DEPARTING, LANDING GEAR DID NOT RETRACT. AFTER CLIMBING TO A SAFE ALTITUDE AND EXECUTING THE PROPER CHECKLIST THE AIRCRAFT DIVERTED. THE AUX GEAR CONTROL SYS WAS USED TO MAKE SURE GEAR WAS DOWN AND LOCKED. AN EMERGENCY WAS NOT DECLA RED, ALTHOUGH, CRASH AND RESCUE WAS REQUESTED TO STANDBY FOR ARRIVAL. THE LANDING WAS WITHOUT INCIDENT. THE ACFT IS CU RRENTLY IN MAINT FOR REPAIR. RESET, SERVICED AND BLED EMERGENCY GEAR SYSTEM. CYCLED GEAR, PERFORMED LANDING GEAR SYSTE M FUNCTIONAL CHECKS, ALL CHECKS GOOD. CHECKED LANDING GEAR ELECTRICAL SYSTEM (WIRING, SWITCHES, PC BOARDS)ALL CHECKS GO OD IAW MM AND WDM. AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4F RT A1WI 20081202 SO 2008 12 2 Y9PAN663P102908 1 20081029 A 7120 WASHER GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU ZONE 400 WRONG PART E Y9PA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 09 663P 3868 1434 16997 UPON THE MID-LIFE REMOVAL OF NR1 ENG FOUND THAT THE WASHER USED AT THE TRUNNION TIE BOLT HAD A O/D THAT WAS TO LARGE FOR THE USE OF TOOL (T900175-1). THIS TOOL IS USED TO PREVENT THE TRUNNION CANISTER FROM MOVING. IAW CAUTION FOUND IN MM 7 1-00-00 PG. 405 B. 25. ANY MOVEMENT OF THE TRUNNION CANISTER ASSY DURING REMOVAL OR INSTALLATION WILL REQUIRE THAT IT BE REMOVED AND INSPECTED FOR DAMAGE. THE REPLACEMENT OF THE CANISTER MAY BE NECESSARY IF IT IS DAMAGED. THE CORRECT WASHER , P/N MS20002C14 WILL ALLOW THE USE OF THE REQUIRED TOOL (T900175-1)NOTE: THIS IS THE FIRST TIME THE ENGINE WAS REMOVED FROM THE ACFT. 2 L 7 2 4F 4 F RT A12EA E25NE 20081202 CE 2008 12 2 DJFA2008082 1 20081122 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 898TA 1513 387 RK295 DURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER INBD RI B AND BRACKET ASSEMBLIES, THE RT INBD RIB WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COM MUNIQUE' NR 70. THE LT AND RT RIB ASSEMBLIES WERE REPLACED. 2 H 7 2 4F RT A16SW 20081202 EU 2008 12 2 COEA2008112803908 1 20081125 A 2913 4019501 PUMP AEROSP ATR42 ATR42300 8680920 EU BLUE HYD SYS FAILED A COEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 13 908FX 023 AIR TURN BACK. DURING LANDING GEAR RETRACTION, THE CREW RECEIVED A HYDR WARNING LIGHT FOR THE BLUE HYDR SYS. THEY ALSO O BSERVED THE SYS INDICATED '0' PRESSURE. AFTER RETURNING TO THE AIRPORT THE CREW DISCOVERED THE CIRCUIT BREAKER POPPED. M AINT FOUND THE BLUE SYS PUMP CAUSED THE CIRCUIT BREAKER TO POP. BLUE HYD SYS, PUMP REPLACED. 2 H 7 2 4T RT A53EU 20081202 NE 2008 12 2 ZESA2008010 2 20080704 A 7320 81850033 FMU CESSNA 500 550 2076604 CE PWA 530 PW530A NE ENGINE FAULTY E ZESA O OTHER O OTHER NR NOT REPORTED 1 EA 03 889B 3 3 5501047 PCEDA0508 CREW WROTE UP THE LT ENGINE FOR ACCELERATING MUCH SLOWER THAN THE RT ENGINE. TROUBLESHOT TO THE HMU. REMOVED AND REPLAC ED WITH AN OVERHAULED UNIT. RAN ACFT AND COMPLETED A MAINT CHECK FLIGHT. ALL CHECKED OK. TWO FLIGHTS LATER, CREW WROT E UP LT ENGINE NOT MAKING POWER AT ALTITUDE. .5 THROTTLE KNOB SPLIT AT FL 350- LT ENGINE SLOW TO ACCELERATE. REPLACED THE HMU WITH A SERVICABLE ASSY, RAN AND COMPLETED CHECK FLIGHT. ALL CHECKS OK. 1 L 7 2 4F 4 F A22CE E00053EN 20081202 CE 2008 12 2 YADA112808 1 20081128 A 3060 4E256010 BOOT BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE HARTZL HCB4M HCB4MP3 GL PROP DEICE SHORTED E YADA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 AL 03 113AX UC41 FWA33624 OBSERVED SPARKS FROM RT PROP INFLIGHT, SPARKS STOPPED WHEN PROP DEICE WAS TURNED OFF. A/C LANDED UNEVENTFULLY. MAINT REP LACED PROP DUE TO SHORTED DEICE BOOT. 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P56GL 20081202 CE 2008 12 2 ZESA2008011 1 20080604 A 3411 PITOT LINE CESSNA 500 550 2076604 CE OBSTRUCTED E ZESA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 03 824CB 5500824 CREW IDENTIFIED AN INDICATED AIRSPEED MISCOMPARE ON TAKEOFF 15-20 KNOTS DIFFERENCE. THEY ABORTED THE TAKEOFF. MAINT RE MOVED BOTH PITOT LINES FROM BOTH ADC'S AND BLEW OUT THE LINES. RECONNECTED AND TESTED ALL SYSTEMS. 1 L 7 2 4F A22CE 20081202 CE 2008 12 2 DXTA2008112403369 1 20081123 A 2730 ELEVATOR CESSNA 560 560XL 2076702 CE JAMMED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 638QS 5605363 WHEN LEVEL AT 41,000 FT EXPERIENCED A, JAMMED ELEVATOR TRIM. 2 L 7 2 4F RT A22CE 20081202 CE 2008 12 2 DXTA2008112403370 1 20081123 A 3260 WARNING LIGHT CESSNA 560 560XL 2076702 CE LT MLG ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 633QS 5605526 AFTER TAKEOFF, GEAR WAS SELECTED TO THE UP POSITION. LT MAIN DOWNLOCK LIGHT (GREEN LIGHT) REMAINED ILLUMINATED. 2 L 7 2 4F RT A22CE 20081202 NM 2008 12 2 USAA2008112692129 1 20081125 A 5330 6545775 SKIN BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 CLT - C1 - MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT BS 727F, S24L. REPAIRED SKIN IAW SRM 53-00-01 REPAIR 31. UPON FURT HER REVIEW OF FORMS ME-0308, A 1.5 INCH ADDITIONAL CRACK AT BS 727E, S24L WAS DISCOVERED IN RELATED AREA AND WAS INCORPO RATED INTO THIS REPAIR. CHANGES WERE MADE TO THE DISCREPANCY, NUMBER OF CRACKS & BODY STATIONS. 2 L 7 2 4F RT A16WE 20081202 2008 12 2 USAA2008112692127 4 20081120 A 2565 CABLE AIRCRUISERS AIRBUS 320 A320231 3930325 EU EVAC SLIDE BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 637AW A7477 99 PIT - C11 - EES - RIGHT OVERWING SLIDE BOTTLE INFLATION SLIDE CABLE END BROKEN. REPLACED OVERWING SLIDE BOTTLE IAW A320 AMM 25-62-46-400-001. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008112692130 1 20081114 A 5347 D53472190202 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON SEAT RAIL AT FR65 +19 INCHES, Y765. REPLACED SEAT RAIL AT FR65 +19 INCH ES, Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008112692131 1 20081114 A 5315 D53472196200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, Y160. REPLACED FLOORBEAM BETWEEN FR68 T O FR70, Y160 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081202 2008 12 2 USAA2008112692126 4 20081125 A 2565 61639203 BOTTLE BOEING 757 757251 1384970 NM EVAC SLIDE LOW PRESSURE A USAA K NONE O OTHER NR NOT REPORTED 1 EA 19 507US 19 19 23196 FLT 9254 YVR-PHX - CIDS PANEL INDICATES R3 DOOR SLIDE BOTTLE HAS LOW PRESSURE. INDICATION ON BOTTLE IS AT MINIMUM ALLOW ABLE PRESSURE. MAINTENANCE REMOVED AND REPLACED R3 DOOR SLIDE ASSIST BOTTLE. 2 L 7 2 4F RT A2NM 20081202 EU 2008 12 2 USAA2008112692136 1 20081113 A 5347 D53112782200 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 AND FR20, Y1292. REPAIRED SEAT TRACK BETWEEN FR 12 AND FR20, Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081202 NM 2008 12 2 USAA2008112892144 1 20081112 A 5755 654675262A REPAIR BOEING 737 7373G7 138447J NM LT SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 SAL - C17 - MAJOR REPAIR - EXISTING REPAIR DELAMINATED ON LEFT WING NR 4 INBOARD SPOILER, WBL 87.75 TO WBL 180.7. REPAI RED NR 4 INBOARD SPOILER IAW B737 SRM 51-70-10-2R. 2 L 7 2 4F RT A16WE 20081202 EU 2008 12 2 USAA2008112892145 1 20081124 A 5320 D53712821200 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOOR SUPPORT AT FR12 TO FR24, -Y254. REPLACED FLOOR SUPPORT AT FR12 TO FR24, -Y254 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008112892147 1 20081113 A 5320 D53480043204 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON LOWER SILL AT L2 DOOR, FR68, Y1732. REPAIRED LOWER SILL AT L2 DOOR, FR6 8, Y1732 IAW A320 SRM 53-41-14 & US AIRWAYS EA 132116. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008112892151 1 20081114 A 5347 D53472133202 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON RAIL SEAT BEAM AT FR64 + 10 INCHES, -Y765. REPAIRED RAIL SEAT BEAM AT F R64 + 10 INCHES, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008112892157 1 20081126 A 3211 D3215303000800 PIN AIRBUS A319 A319112 3930323 EU LT MLG CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 713UW 1040 PIT - LRN - MAJOR REPAIR - LEFT MAIN LANDING GEAR AFT PINTLE PIN CORRODED. REPLACED LEFT MAIN LANDING GEAR AFT PINTLE P IN IAW US AIRWAYS JOB CARD 26T00032001. UPON FURTHER REVIEW, FOUND DISCREPANCY TO BE LEVEL 2 CORROSION. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008120192161 1 20081123 A 5320 D5347557525 THRESHOLD AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - CORROSION ON SHEET THRESHOLD AT FR52 +10 AND FR56, S38R. REPAIRED SHEET THRESHOLD AT FR52 +10 AND FR56, S38R IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081202 NE 2008 12 2 UALA2008112106607 2 20081121 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BIRD INGESTION A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 516UA 24860 726612 RTFL DUE TO BIRD STRIKE. PERFORM NR 1 ENG BURNOUT PROCEDURE DUE TO ODOR IN CABIN (BIRD STRIKE NR 1 ENGINE). REMOVE NR 1 ENGINE DUE TO LPC STG 1 BOOSTER DAMAGE AND LINER SEPARATION. 2 L 7 2 4F 4 F RT A2NM E17NE 20081202 NM 2008 12 2 UALA2008111305432 1 20080823 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EXTERIOR DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 LT FWD EXTERIOR GROUND ILLUMINATION EMERGENCY LIGHT INOP. CLEANED AND SECURED LAMP, AND CONTACT, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081202 2008 12 2 YENA200811240118 4 20081121 A 2330 ENTERTAIN SYS AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 559JB 1917 FLT 504, FLL-EWR, LTV SYSTEM SMELL OF SMOKE ROW 1 THRU 5, LTV DEACTIVATED. T/S PER TR 2400001, TSM 24-00-00-810-823 & 2 3-39-00-810-801. NO ABNORMALITIES FOUND. INSPECTED ROW 1-7 ABCDEF. UPDATED XEB S/W. ADJUSTED RSSI FROM 4.95 TO 2.50. MONITORED SYS FOR 3 HOURS. OPS NORMAL. NO SMELLS NOTED. 2 L 7 2 4F RT A28NM 20081202 2008 12 2 YENA200811240120 4 20081123 A 3160 7023460803 DISPLAY EMB ERJ190 ERJ190100IGW 3260408 NM COCKPIT FAILED A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 258JB 235 190000047 FLT 922, ORD-BOS, DIVERTED TO BUF, COCKPIT SMOKE SMELL AT FL LEVEL 380. EICAS WENT BLANK. FIRST GOT MFD 1 & 2 FAULT FO LLOWED QRH. SMOKE SMELL WAS NOT PRESENT IN CABIN. EMERGENCY LANDING AT BUF. PULLED OUT MFD 2. FOUND BURNED CIRCUIT B OARD SMELL AT REAR CONNECTORS. REMOVED AND REPLACED MFD 2 (DU4) PER AMM 31-61-01-04. OPS CHECK GOOD PER 31-61-00-710-8 01-A. OK FOR SERVICE. 2 L 7 2 4F RT A57NM 20080829 NM 2008 8 29 SWAA084736 1 20080826 A 3350 100031 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED SPV CHECK, FOUND FWD CABIN EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080829 2008 8 29 SWAA084737 4 20080826 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM L1 DOOR DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 L1 DOOR EMERGECNY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084738 1 20080826 A 2560 P4010021 BATTERY BOEING 737 7373A4 1384585 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084700 1 20080825 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 867-887 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 867 AND BS 887, RBL 70. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080829 EA 2008 8 29 VNAA0808004 1 20080807 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT WING DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 246PS 7920 CREW REPORTED A LIGHTNING STRIKE TO THE RT WING. MAINTENANCE PERFORMED AN EN ROUTE AND A DETAILED LIGHTNING STRIKE INSP ECTION. MAINTENANCE INSPECTED AND FOUND DAMAGE TO LT FUSELAGE AND RT WINGTIP. MAINTENANCE REPAIRED ALL DAMAGE PER REO 601R-53-00-115 AND IAW THE ACFT MAINTENANCE MANUAL. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080829 NM 2008 8 29 SWAA084438 1 20080810 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 616 S14L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 14L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084727 1 20080826 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084725 1 20080826 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 RIGHT AFT CABIN EMERGENCY EXIT LIGHTS REMAIN ILLUMINATED. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084675 1 20080824 A 2121 215201 FAN BOEING 737 7373H4 1384600 NM E&E BAY FAULTY A SWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 370SW 26597 AIR TURNBACK / DECLARED EMERGENCY. FLIGHT CREW REPORTED SMOKE IN CABIN. INSPECTED AIRCRAFT, FOUND GASPER FAN FAULTY. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084667 1 20080820 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084658 1 20080823 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 764 AND BS 774, STR 19L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084656 1 20080824 A 5523 65C26384 ROD END BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED CV CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR CONTROL ROD ENDS PE R SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084629 1 20080824 A 5315 6546809 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 947, LBL 6. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084623 1 20080820 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084622 1 20080820 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 746SW 29798 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084614 1 20080820 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L AND STR 8R. REMOVED AND REPLACED STRINGER CLI P PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 AALA200801830 1 20080618 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 919AN 29520 TUL - EMERGENCY LIGHT BATTERY PACK AT LT EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LT EXIT D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 AALA200801867 1 20080713 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 616AA 24524 DFW - EXTERIOR EMERGENCY LIGHT AT RT AFT OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT AFT OVERWING. S YSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A2NM 20080902 NM 2008 9 2 SWAA084576 1 20080819 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 213WN 34217 DURING SCHEDULED HC1 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084522 1 20080814 A 5754 65C26602 SLAT BOEING 737 7377H4 1384404 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 715SW 27849 DURING SCHEDULED 10Y CHECK, FOUND RT WING NR 8 L/E SLAT CRACKED AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084498 1 20080813 A 5330 65C22910 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 518D, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084497 1 20080813 A 5330 6545766 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 FUSELAGE SKIN CRACKED AT BS 700, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 SO 2008 9 2 CHQA200800129 1 20080702 A 3350 RPS1B BATTERY PACK EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL EMERGENCY LIGHT INOPERATIVE A CHQA O OTHER O OTHER NR NOT REPORTED 1 GL 11 271SK 10039 145305 CAE11922 MAINTENANCE FOUND THE CENTER EMERGENCY STRIP LIGHT INOP IN THE CABIN. THE NR 3 EMERGENCY BATTERY POWER SUPPLY WAS REPLA CED AND THE EMERGENCY LIGHTS OPERATED NORMALLY. (A) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080902 NM 2008 9 2 GTIA0800077 1 20080801 A 2611 SMOKE DETECTOR AIRBUS A319 A319132 3930340 NM LAVATORY MALFUNCTIONED A GTIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 501NK 2424 LAVATORY "F" SMOKE DETECTOR FAULTS T/S SYSTEM PER TSM. REMOVED AND REPLACED DETECTOR. OPS NORMAL. (S) 2 L 7 2 4F RT A28NM 20080902 WP 2008 9 2 IXX2008F00069 1 20080612 A 5330 SKIN DOUG DC8 DC872F 302199E WP BS 188 L27L CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE EXTERNAL PART PRIMARY HEAT EXCHANGER LOWER AFT CORNER CRACKED AT STATI ON 188.000 LONGERON 27LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTI ON. NO CRACK, NO CORROSION FOUND. FABRICATED EXTERNAL REPAIR DOUBLER, EXTERNAL REPAIR TRIPLER, AND FILLER. CLEANED, T REATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 08378 DATED 7/11/ 08, SEMAN DRAWING ED4804 DATED 06/23/08, DC8 SRM 51-1-21, SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, SR M 51-1-11, SRM 51-1-20D, SRM 51-3-0, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080902 WP 2008 9 2 IXX2008F00059 1 20080614 A 5751 SKIN DOUG DC8 DC872F 302199E WP RT WING AILERON MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD AILERON UPPER SKIN IMPROPER REPAIRS AT STATION XA 630.000-724. 000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR, REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, DOUBLER. BONDED PAR TS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. PERFORMED BALANCE, FOUND WITHIN LIMITS MOME NT = 3326.3 IN-LB. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XW 546.000-XA 724.000 IAW DC8 SRM 57-8-1 FIGURE 4 ITEM "F" AND "G", DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DOUGLAS DRAWING 5763133, DC8 SRM 51-1-9 TR 51-142, SRM 51-1-9A T R 51-141, DC8 SRM 51-1-8B, IAW DC8 SRM 51-4-3 PAGES 1-6, DC8 SRM 51-1-11, AND SRM 51-1-21. (S) 2 L 7 4 4F RT 4A25 20080902 WP 2008 9 2 IXX2008F00060 1 20080613 A 5753 SKIN DOUG DC8 DC872F 302199E WP RT WING TE FLAP MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP PANEL UPPER PART HAS IMPROPER REPAIR AT STATION 360.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PR IMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XF345.000-360.000 IAW DC8 SRM 57-1-0 PAG E 1, SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 4 ITEM "B" TR 57-94 DATED 10-01-2002, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-3 -0, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080902 NM 2008 9 2 KCS2008F00007 1 20080807 A 2120 UNKNOWN BOEING 747 747246F 1384850 NM COCKPIT ODOR A KCSA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 705CK 21034 STRONG ELECTRICAL SMOKE ODOR IN COCKPIT. IMMEDIATELY STOPPED WHEN FLIGHT DECK FAN WAS TURNED OFF. (S) 2 L 7 4 4F RT A20WE 20080902 NM 2008 9 2 KCSA081351 1 20080727 A 5347 SEAT TRACK BOEING 747 747246B 1384864 NM BS 1060-1080 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 SEAT TRACK FROM B-STA 1060 TO 1080, LBL 10 HAS CORROSION UNDERSIDE AROUND NUT PLATES. (A) 2 L 7 4 4F RT A20WE 20080902 NM 2008 9 2 KCSA081346 1 20080724 A 3350 LIGHT BOEING 747 747209B 138489B NM CABIN INOPERATIVE A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FLIGHT DECK CEILING EMERGENCY LIGHT IS INOP. (A) 2 L 7 4 4F RT A20WE 20080902 NM 2008 9 2 KCSA081331 1 20080718 A 5730 SKIN BOEING 747 747122 1384872 NM LT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 716CK 19753 LT WING SKIN AT WS 993 TO WS 995 HAS CORROSION. (A) 2 L 7 4 4F RT A20WE 20080902 NM 2008 9 2 KCS2008F00004 1 20080720 A 2432 401767 BATTERY BOEING 747 747212B 1384886 NM MASTER FUMES A KCSA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 703CK 21939 SMOKE AND FUMES IN COCKPIT. FOUND SHIP’S MAIN BATTERY EMITTING FUMES. REMOVE AND REPLACE MAIN BATTERY AND CHARGER WITH APU BATTERY AND CHARGER PER GMM 3-5-8. APU BATTERY P/N 40176-7, S/N 076021 INSTALLED IN MAIN POSITION PER AMM 24-31-01 . APU BATTERY CHARGER INSTALLED IN MAIN POSITION PER AMM 24-31-02. BATTERY CHARGER OPS CK GOOD. P/N 2-792-02, S/N 334 , MAIN BATTERY INSTALLED DEACTIVATED IN APU POSITION PER AMM 24-31-00. P/N 40176-7M, S/N 75852. MAIN BATTERY CHARGER IN STALLED DEACTIVATED IN APU POSITION PER AMM 24-31-07 P/N 2-792-02, S/N 1721. (A) 2 L 7 4 4F RT A20WE 20080902 NM 2008 9 2 KCSA081319 1 20080715 A 5730 SKIN BOEING 747 747122 1384872 NM LT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 716CK 19753 LT WING LOWER SKIN CORRODED AT APPROX 1300. (A) 2 L 7 4 4F RT A20WE 20080902 NM 2008 9 2 SWAA084480 1 20080813 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 KCA081323 1 20080715 A 3350 LIGHT BOEING 747 747246F 1384850 NM CABIN INOPERATIVE A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 EMERGENCY FLOOR LIGHT AT UPPER DECK LT DOOR INOP. (A) 2 L 7 4 4F RT A20WE 20080902 NM 2008 9 2 SWAA084476 1 20080812 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084474 1 20080812 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 312, STR 28L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080902 EA 2008 9 2 MAS2008F00014 1 20080804 A 7500 ELBOW CNDAIR CL600 CL6002D24 1390016 EA LT BLEED SYS LEAKING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 905J 15005 ASH FLT 2679 CLT-SAT - LT BLEED DUCT CAUTION, LT BLEED DUCT WARNING. NO PACK PRESSURE AFTER RUNNING OF BLEED DUCT PROCE DURES. REMOVED AND REPLACED MT138 CONNECTOR ELBOW. (S) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 MASA200800474 1 20080616 A 5220 COVER CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 935LR 15035 ASH FLT 2877 PHX-ELP. THE 16F EMERGENCY EXIT HANDLE WILL NOT STOW. RE-SECURED THE DOOR HANDLE COVER. (B) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 MASA200800475 1 20080616 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DIRTY A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 77260 7260 ASH FLT 2818 DSM - OVERNIGHT. FLOOR PATH EMERGENCY LIGHTS 2 THROUGH 3 AND THE FLOOR LEVEL EXIT SIGNS ARE INOP. MX CLEA NED INVERTER CONNECTIONS AND SECURED LIGHT STRIP CONNECTIONS. (B) 2 L 7 2 4F RT A21EA 20080902 EU 2008 9 2 NSV2008F00015 1 20080805 A 2697 CONNECTOR SAAB SF340 340B 7860101 EU TAIL PIPE CONTAMINATED A NSVA O OTHER N FALSE WARNING CL CLIMB 1 EA 27 202SR 340B202 TAIL PIPE HOT LIGHT (RT) CAME ON AFTER TAKEOFF THEN WENT OUT AND STAYED OUT. CLEANED CONNECTORS AT DISCONNECTS WITH CON TACT CLEANER TO REMOVE MOISTURE, PERFORMED ENG RUN, NO FAULTS NOTED AMM 30-12-00. (S) 2 L 7 2 4T RT A52EU 20080902 NE 2008 9 2 PL92008F00000 2 20080816 A 7250 J53D3B TURBINE BLADES BOEING 707 707330B 138366F NM PWA JT3D JT3D3B 52039 NE TURBINE WHEEL FAILED A PL9B A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 15 88ZL 18928 668235 DURING CLIMBOUT FROM PHX NR 4 ENG EGT BEGAN TO CLIMB RAPIDLY AND NR 1 & NR 2 SPOOLED DOWN. ENG WAS SHUT DOWN FOLLOWING PUBLISHED PROCEDURES AND THE ACFT RETURNED TO PHX AND LANDED WTIHOUT INCIDENT. AFTER LANDING THE ENG WAS INSPECTED AND FOUND THAT THERE WERE SEVERAL SECTIONS OF TURBINE BLADES HAD FAILED AND CAUSED ADDITIONAL DAMAGE TO THE TURBINE WHEELS A FT OF THE FAILED DISC BLADES. THE DAMAGE WAS CONTAINED WITHIN THE TAIL PIPE AND NO EXTERNAL DAMAGE WAS NOTED TO ANY ADJ ACENT AREAS. (S) 2 L 7 4 4F 4 F 4A26 1E8 20080902 NM 2008 9 2 QXEA200800872 1 20080808 A 3233 ROD BOMBDR DHC8 DHC8402 1390042 NM MLG ACTUATOR OUT OF ADJUST A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 19 408QX 4050 PDX - AFTER SELECTING THE GEAR HANDLE UP THE LT MAIN GEAR INDICATED RED AND THE LT DOOR SHOWED OPEN. IT REMAINED FOR AB OUT 20 SECONDS FOLLOWED BY THE LIGHT GOING OUT. SHORTLY AFTER, THE DOORS INDICATED SHUT AND THE GEAR RETRACTED NORMALLY . MAINTENANCE ADJUSTED THE LT MLG RETRACT ACTUATOR ROD END IAW 32-31-11-400-803 TR 32-238. CHECKS GOOD. ACFT RETURNED TO SERVICE. NO PARTS REPLACED. (S) 2 H 7 2 4T RT A13NM 20080902 EA 2008 9 2 QXEA200800595 1 20080530 A 5751 SKIN CNDAIR CL600 CL6002C10 1390015 EA RT AILERON CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 610QX 10033 RFD-C4 CHECK - RT AILERON CHAFED ON UPPER AND LOWER LEADING EDGE. BLENDED CHAFED AREA IAW CRJ SRM 57-61-01. LEADING ED GE FOUND TO BE OUT OF LIMITS IAW CRJ SRM 57-61-01. REMOVED UPPER LEADING EDGE PANEL IAW CRJ SRM 51-42-21, INSTALLED NEW LEADING EDGE IAW CRJ SRM 51-42-21, 51-42-13. TREATED IAW CRJ700 SRM 51-21-11. PRIMED AND PAINTED IAW CRJ 700 SRM 51-2 5-01. (S) 2 L 7 2 4F RT A21EA 20080902 SO 2008 9 2 RAIA00808019 1 20080819 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 817HK 145058 PRE FLT 5451 - CID - CABIN OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR TO THE LIGHT ASSEM BLY. OPS CHECKED GOOD. (S) 2 L 7 2 4T RT T00011AT 20080902 SO 2008 9 2 RAIA00808018 1 20080817 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 810HK 145231 PRE FLT 7945 -SGF- EMERGENCY LIGHT STRIP CAME LOOSE FROM THE FLOOR. MAINTENANCE DEFERRED THE APPLICABLE LIGHT STRIP IAW MEL PROCEDURES. (S) 2 L 7 2 4T RT T00011AT 20080902 SO 2008 9 2 RAIA00806025 1 20080629 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS LOOSE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 821HK 145068 PRE-FLT 5506 - JAX - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE SECURED 4 LOOSE CONNECTORS ON THE EMERGENCY LIGHT SYSTEM, OPS CHECKED GOOD. WD:IN HD:O (A) 2 L 7 2 4F RT T00011AT 20080902 SO 2008 9 2 RAIA00808009 1 20080810 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAILED A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 844HK 14500838 PRE-FLT 7878-STL - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE LIGHT ASSEMBLY AND PER FORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHTING SYSTEM WITH NO DEFECTS NOTED. (S) 2 L 7 2 4T RT T00011AT 20080902 SO 2008 9 2 RAIA00807013 1 20080718 A 3610 PRECOOLER EMB 145 EMB145LR 3260212 SO BLEED SYSTEM LEAKING A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 840HK 145341 FLT 7905 - IAD - DURING CLIMBOUT, CREW RECEIVED A BLEED 2 LEAK ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 2 PRECOOLER ASSEMBLY. SYSTEM OPS CHECKED GOOD. (A) 2 L 7 2 4T RT T00011AT 20080902 SO 2008 9 2 SIMA200823106 1 20080814 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 695AE 14500870 DURING MBV INSPECTION FOUND CARGO DOOR SILL BETWEEN FRAMES 65-68 TO BE CORRODED. REMOVED AND REPLACED CARGO DOOR SILL I AW EMB SRM 51-40-02. ACFT WAS RETURNED TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080902 NM 2008 9 2 WRLA2008067 1 20080805 A 5347 54929147 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 275WA 48631 DURING INSPECTION FOUND MAIN DECK CARGO SEAT TRACK CRACK AT Y=760, X=47.6. REPAIRED CRACK SET TRACK IAW MD-11SRM VOL 1 53-70-00 REV 40. JOB COMPLETED AND CONDITION CHECK NORMAL. (S) 2 L 7 3 4F 4 F RT A22WE E24NE 20080902 EA 2008 9 2 VNAA0807007 1 20080714 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FALSE ACTIVATION A VNAA O OTHER N FALSE WARNING TO TAKEOFF 1 GL 05 262PS 7962 CREW RECEIVED A LT HAND STATIC HEAT CAS MSG AND ELECTED TO RETURN TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE RE-SET T HE SYSTEM AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080902 EA 2008 9 2 VNAA0807004 1 20080712 A 5100 NONE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NONE NONE A VNAA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 GL 05 213PS 7879 CREW REPORTED A COMMUNICATION DOOR LEFT OPEN. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. MAINTENANCE SECURED THE DOOR CLOSED. AIRCRAFT WAS RELEASED FOR SERVICE. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080902 NM 2008 9 2 USAA920081506 1 20080808 A 3350 321454 POWER SUPPLY AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 805AW 50861 13538 1049 FLT 0573-SFO-LAS-EEL - EMERGENCY EXIT LIGHT OVERWING CEILING (AFT FACING) AND ACFT LT SIDEWALL INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY UNIT. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080902 NM 2008 9 2 USAA920081507 1 20080809 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 831AW 1576 FLT 0220-ANC-PHX- EMERGENCY EQUIPMENT - FLASHLIGHT INOPERATIVE AT F/A. REMOVED AND REPLACED FLASHLIGHT BATTERY. OPERAT IONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080902 NM 2008 9 2 SWAA084464 1 20080812 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084462 1 20080812 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKN CRACKED AT BS 801, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080829 EA 2008 8 29 VNAA0808006 1 20080808 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE FALSE ACTIVATION A VNAA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 05 712PS 10168 CREW REPORTED A RED WARNING "L BLEED DUCT" CAS MESSAGE IN FLIGHT. CREW ELECTED TO DIVERT TO TYS AND LANDED WITHOUT INCI DENT. MAINTENANCE INSPECTED ACFT AND FOUND NO DEFECTS. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E00063EN 20080902 NM 2008 9 2 SWAA084670 1 20080821 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 480WN 33998 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084664 1 20080824 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084657 1 20080823 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084640 1 20080824 A 3350 65C27093 LIGHT BOEING 737 7373Q8 1384670 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT ASSY CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084633 1 20080821 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AFT SERVICE DOOR LOWER FWD CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084632 1 20080824 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767, LBL 12.50. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 EA 2008 9 2 A6WA200840534 1 20080626 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 574-621 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 446AW 7806 CARGO DOOR SURROUND FLOOR LANDING PLATE (SILL) CORRODED AROUND NUT PLATE HOLES BETWEEN FS 574 TO FS 621. CORROSION REMO VED ON CARGO DOOR SURROUND FLOOR LANDING PLATE. AROUND NUT PLATE HOLE BETWEEN FS 574 AND FS 621 IAW CRJ 200 SRM 51-21-0 6. (A) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 A6WA200840547 1 20080722 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A A6WA O OTHER J WARNING INDICATION AP APPROACH 1 GL 31 447AW 7812 FLAPS FAIL CAUTION CAS MESSAGE IN FLIGHT WHEN SELECTING 8 DEGREES. LT AND RT INDICATE NORMAL LANDING, BRAKES ALL GREEN. PERFORMED FLANGE RELAY PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4. FLAPS RESET. ACFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20080902 NM 2008 9 2 SWAA084589 1 20080819 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 806, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080902 SO 2008 9 2 C2X2008F00014 1 20080728 A 3350 20131A BATTERY PACK EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15926 17582 145005 A/C WAS IN FOR A OVERNIGHT SERVICE CHECK AND NR 4 EMERGENCY LIGHT BATTERY WAS FOUND INOP. MAINTENANCE REMOVED AND REPLA CED THE NR 4 BATTERY IAW EMB 145 AMM 33-50-04. OPS CHECKS GOOD AND WAS RELEASED BACK TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080902 NM 2008 9 2 SWAA084570 1 20080819 A 5311 6546549 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, BETWEEN STR 25L AND STR 27L. REPAIRED FRAME PER SR M. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084578 1 20080819 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 213WN 34217 DURING SCHEDULED HC1 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20080902 SO 2008 9 2 C2XA08IA186 1 20080804 A 3231 22250100003 SOLENOID EMB 145 EMB145XR 3260214 SO NLG DOORS INOPERATIVE A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 11109 16795 16795 145657 IAH-FLIGHT 3044 - THE CREW REPORTED THAT THE NOSE GEAR DOORS WOULD NOT CLOSE. THE ACFT LANDED AT IAH WITHOUT INCIDENT W HERE MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOOR SOLENOID VALVE. OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080902 SO 2008 9 2 C2XA08RI115 1 20080803 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12957 145080 RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND EMERGENCY LIGHT STRIPS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EME RGENCY LIGHT INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080902 NM 2008 9 2 SWAA084524 1 20080814 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 783SW 29809 DURING SCHEDULED HC1 CHECK, RT AFT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PAC K PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084523 1 20080814 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 783SW 29809 DURING SCHEDULED HC1 CHECK, LT MID CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PAC K PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084505 1 20080813 A 5320 6545402 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 DURING SCHEDULED SPV CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 663, RBL 6.15. REPAIRED STIFFENER PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084504 1 20080813 A 3350 311500 LENS BOEING 737 7373Q8 1384670 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED MV3 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 23 DEF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080902 2008 9 2 GLB2008F00013 4 20080804 A 6122 ROD BEECH 1900 1900D 1154162 CE PROP GOVERNOR OUT OF ADJUST A GLBA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NM 03 192GL UE192 AIRCRAFT N192GL - 07/05/2008 - FLIGHT 5136 - ON APPROACH INTO "DEN" THE PILOTS REPORTED THAT THE NR 1 ENG/PROP AUTO FEAT HERED ON FINAL, LOW POWER, FLAPS 35, & GEAR DOWN. MAINTENANCE ADJUSTED PROP GOVERNOR IN INTERCONNECT ROD & CLEANED SOLE NOID. GROUND OPERATIONAL CHECKS WERE GOOD PER BEECH 1900D 76-10-00. (S) 2 L 7 2 4T RT A24CE 20080902 NM 2008 9 2 SWAA084486 1 20080813 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 21R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084481 1 20080813 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084475 1 20080812 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080902 EA 2008 9 2 QXEA200800594 1 20080530 A 5730 SKIN CNDAIR CL600 CL6002C10 1390015 EA RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 610QX 10033 RFD-C4 CHECK - CHAFING ON RT WING CUTOUT AT LEADING EDGE WS 220.00. BLENDED CHAFED AREA IAW REO 670-57-41-059. TREATED IAW CRJ-700 SRM 51-21-11. PRIMED AND PAINTED IAW CRJ 700 SRM 51-25-06 AND 51-25-01. (S) 2 L 7 2 4F RT A21EA 20080902 SO 2008 9 2 RAIA00806024 1 20080627 A 3350 66901 LIGHT EMB 145 EMB145 3260210 SO CABIN BROKEN A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 802HK 145066 PRE-FLT 3505 - RIC - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FLOOR PROXIMITY EMERGENCY LIGHT STRIP. OPERATIONAL CHECK OF THE SYSTEM WAS GOOD. WD:IN HD:O AT:O (A) 2 L 7 2 4F RT T00011AT 20080902 EA 2008 9 2 REX2008F00033 1 20080808 A 3230 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8623A 7623 ON APPROACH GEAR FAILED TO EXTEND. QRH FOLLOWED MANUALLY EXTENDED. DECLARED EMERGENCY WITH UNEVENTFUL LANDING. PERFOR MED GEAR SWING PER AMM. FOUND THE MAIN LANDING GEAR SELECTOR VALVE OPERATIONALLY CHECK GOOD PER AMM. (S) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 REX2008F00027 1 20080730 A 2612 FIRE LOOP CNDAIR CL600 CL6002B19 1900309 EA RT NACELLE SHORTED A REXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 8588D 7588 WHEN THE THRUST LEVERS WERE ADVANCED FOR TAKEOFF ON RUNWAY 22L AT KDTW, THE MASTER WARNING FOR THE RT 14TH STAGE DUCT OV ERHEAT ILLUMINATED. THE POWER WAS REDUCED AND THE TAKEOFF ABORTED. THE FLIGHT CREW PERFORMED THE QRH WHICH DID NOT COR RECT THE PROBLEM. THE FLIGHT CREW DECLARED AN EMERGENCY AND ASKED FOR CFR BECAUSE THE WARNING DID NOT GO AWAY WHEN THE RT ENG WAS SHUT DOWN. WITH THE ASSISTANCE OF CFR, THE PASSENGERS WERE EVACUATED TO A SAFE LOCATION ON THE TAXIWAY AND S HUTTLED TO THE TERMINAL BY BUS. CFR FOUND NO EVIDENCE OF FIRE AND THE ACFT WAS TOWED TO THE GATE. MAINTENANCE FOUND TH E RT 14TH STAGE DETECTION LOOP SHORTED. THE LOOP WAS REPLACED, THE ACFT WAS RUN UP AND RELEASED FOR SERVICE. (S) 2 L 7 2 4F RT A21EA 20080902 SO 2008 9 2 SIMA200823109 1 20080817 A 3320 BR900022 BALLAST EMB 135 EMB135LR 3260305 SO CABIN LIGHTS ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 719AE 145276 ON FLIGHT 4771 CREW REPORTED STRONG CHEMICAL FUMES COMING FROM GASPER ABOVE FLIGHT ATTENDANT`S TEMP CONTROL PANEL. ACFT REMOVED FROM SERVICE. INSPECTED AND FOUND 1ST BALLAST OF CEILING LIGHT INOPERATIVE WHICH CREATED CHEMICAL ODOR. REMOV ED AND REPLACED BALLAST AND PERFORMED OPERATIONAL CHECK IAW EMB AMM 135 33-21-05. OPERATIONAL CHECKED GOOD. ACFT RETUR NED TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080902 NM 2008 9 2 SWAA084463 1 20080812 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKN CRACKED AT BS 490, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080902 2008 9 2 SWAA084456 4 20080812 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 424WN 29828 L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084444 1 20080810 A 5312 6546568 BULKHEAD BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD FWD SIDE CRACKED AT BS 1016, STR 6R. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 20080902 EU 2008 9 2 USAA920081484 1 20080807 A 2910 238D0660507 LINE AIRBUS A319 A319112 3930323 EU HYD SYSTEM LEAKING A USAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 19 716UW 1055 FLT 2173 LGA-DCA- HYDRAULIC SYSTEM FAILURE - INBOUND TO DCA, THE YELLOW HYDRAULIC SYSTEM FAILED. CREW RECEIVED "HYD Y S YS RES LO LEVEL" AND LOW PRESSURE ECAM WARNINGS. NO EMERGENCY WAS DECLARED AND THE ACFT LANDED WITHOUT INCIDENT. MAINT ENANCE REMOVED AND REPLACED THE NR2 ENG PRESSURE TRANSDUCER LINE. LEAK CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080902 NM 2008 9 2 SWAA084443 1 20080810 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 EU 2008 9 2 USAA920081469 1 20080803 A 2820 35300001 SENSOR AIRBUS 320 A320214 3930316 EU FUEL CELL UNRELIABLE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 102UW 0844 FLT 977 CLT- PDX - AIR TURN BACK - AFTER TAKEOFF, OUTER FUEL TRANSFER OCCURRED WITH WINGS AT 12,000 EACH SIDE AND CENTER TANK WOULD NOT AUTO FEED. CENTER TANK PUMPS DID AUTO FEED DURING TAXI OUT. CREW DECLARED AN EMERGENCY AND RETURNED TO CLT. ACFT LANDED AND TAXIED TO GATE WITHOUT INCIDENT. MAINTENANCE FOUND WING TANK LEVEL SENSORS UNRELIABLE. REPLACED 15QJ1, 15QJ2, 16QJ1 & 16QJ2 PER AIRBUS MAINTENANCE MANUAL 28-46-15. OPERATIONAL TEST NORMAL. (S) 2 L 7 2 4F RT A28NM 20080902 EU 2008 9 2 USAA920081527 1 20080813 A 3260 666000077 SENSOR AIRBUS A321 A321211 3930370 EU LANDING GEAR DEFECTIVE A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 172US 1472 FLT 1544 PHX-CLT- LANDING GEAR - ON APPROACH INTO CLT, LANDING GEAR SYSTEM INDICATED LT MAIN UNSAFE. AT GATE RECEIVED E CAM MESSAGE LANDING GEAR SYSTEM DISAGREE. MAINTENANCE REMOVED AND REPLACED PROXIMITY SENSOR 15GA. (S) 2 L 7 2 4F RT A28NM 20080903 NM 2008 9 3 2008UALA03451 1 20080618 A 2421 745329D IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 FAULTY A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 652UA 25390 L GEN DRIVE LIGHT CONTINUOUSLY FLICKERS IN FLIGHT. GEN WORKS NORMALLY. *S/D* SUSPECT FAULTY INTEGRATED DRIVE GENERATO R. REPLACED LEFT IDG PER MM 24-11-01, ALL OPS AND INDICATE NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080903 NM 2008 9 3 2008UALA03457 1 20080616 A 8012 8088846 START VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 ENGINE FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 797UA 26924 RIGHT STARTER AIR VALVE POSITION DISAGREES WITH COMMANDED POSITION. ADVISORY MSG-8061562 INACTV TA MODE. *S/D* FOUND FAULTY STARTER AIR VALVE. REPLACED STARTER VALVE ASSEMBLY PER 80-11-02. ALL OPS AND STARTS NORMAL MSG ERASED. AC OK F OR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080903 NM 2008 9 3 2008UALA03463 1 20080619 A 3212 STRUCTURE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE RT NLG DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 226UA 30226 RT AFT NLG DOOR AFT LOWER CORNER CRACKED APPROX 3"X1" AREA. *S/D* SUSPECT NORMAL AC OPERATION. ACCOMPLISHED INTERIM REPAIR PER EVA-71532. ** MF2588 CREATED TO MONITOR ** AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080903 NM 2008 9 3 UIEA200800289 1 20080815 A 5280 SKIN BOEING 747 7472D7B 1384803 NM LT MLG DOOR CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 524MC 21784 LT WING LANDING GEAR INBOARD STRUT DOOR EXTERIOR SURFACE AND EXISTING DOUBLER CRACKED. REPAIRED IAW SRM 51-40-24 FIGURE 1&2, DETAILS OF WORK KEPT AT ATLAS ENGINEERING ORDER EO4752A149. (S) 2 L 7 4 4F RT A20WE 20080903 NM 2008 9 3 UIEA200800281 1 20080803 A 3610 227565112 RELIEF VALVE BOEING 747 7472D7B 1384803 NM NR 4 ENGINE LEAKING A UIEA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 EA 15 528MC 22472 AT CRUISE NR 4 ENG HAD MULTPLE FIRE WARNINGS ON BOTH A&B. PERFORMED IN FLIGHT SHUT DOWN AND AIR TURNBACK. MAINTENANCE FOUND LEAKING PRESSURE RELIEF VALVE, WHICH WAS BLASTING HOT AIR ON THE DETECTORS. REPLACED OVER PRESSURE RELIEF VALVE P ER 36-11-03, OPS CHECKED OK. (S) 2 L 7 4 4F RT A20WE 20080903 NM 2008 9 3 QXEA200800345 1 20080330 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 356PH 502 PDX-C5 CHECK- AFT BAG PIT UPPER SKIN AT A LIGHTENING HOLE HAS LIGHT CORROSION FORMING IN RECESS HOLE Z100 X557 AND 27L. BLENDED OUT CORROSION AND MEASURED BLENDED AREA IAW DASH 8 200 SRM 51-20-11. ALODINED, PRIMED, AND PAINTED BLENDED ARE A IAW DHC 8 200 SRM 51-20-16, AND 51-20-36. (S) 2 H 7 2 4T RT A13NM 20080903 NE 2008 9 3 A6WA200840557 2 20080804 A 7261 O-RING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT ENGINE MISSING A A6WA O OTHER J WARNING INDICATION CR CRUISE 1 GL 31 419AW 7633 AT CRUISE SPEED RECEIVED LT ENG OPERATION WARNING MESSAGE AND OIL PRESSURE INDICATED 25-36 PSI. MESSAGE RECURRED AND PR ESSURE DROPPED TO 25 PSI SEVERAL TIMES IN FLIGHT. INSPECTED NR 1 ENG AND FOUND OIL LEAKING FROM SCAVENGE FILTER. UPON REMOVING FILTER FOUND O-RING MISSING. REPLACED O-RING AND FILTER IAW AMM 79-21-05. LEAK CHECK GOOD. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080903 WP 2008 9 3 ARWA20080802 1 20080814 A 3200 UNKNOWN DOUG DC8 DC863F 302198F WP MLG AREA SPARKS A ARWA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 29 784AL 46135 AIR TURNBACK REPORTED SPARKS COMING FROM RT MAIN GEAR. DECLARED EMERGENCY AND RETURNED TO MIA. (S) 2 L 7 4 4F 4A25 20080903 NM 2008 9 3 UIEA200800291 1 20080815 A 5320 INTERCOSTAL BOEING 747 747400 13848AT NM GE CF6 CF680C2* GL BS 360-380 CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 429MC 24833 DURING C-CHECK UPPER DECK STATION 360-380 RBL 28 INTERCOSTAL CHANNEL FOUND CRACKED. REPLACED CHANNEL AS PER SRM 51-10-0 2 AND INTERCOSTAL AS PER SRM 51-40-02. (S) 2 L 7 4 4F 4 F RT A20WE E23EA 20080903 EA 2008 9 3 QXEA200800736 1 20080710 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 613 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 612QX 10042 PDX-C4 CHECK. CORROSION ON INBOARD RT SEAT TRACK AT STATION 613.00. REMOVED CORROSION BY BLENDING. REMOVED MATERIAL W ITHIN LIMITS. HFEC FOR CRACKS, NONE NOTED. ALODINED AREA IAW REO 670-53-013. (S) 2 L 7 2 4F RT A21EA 20080903 NM 2008 9 3 UIEA200800290 1 20080815 A 5230 SKIN BOEING 747 747400 13848AT NM GE CF6 CF680C2* GL CARGO DOOR DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 429MC 24833 DURING C-CHECK FORWARD CARGO DOOR EXTERNAL SURFACE SPLICE AREA FOUND 1 EA LIGHTNING STRIKE AT UPPER AFT SIDE OF MASTER L OCK HANDLE. REPAIRED AREA AS PER EO 4452A047. (S) 2 L 7 4 4F 4 F RT A20WE E23EA 20080903 NM 2008 9 3 USAA920081547 1 20080818 A 5320 69396581 STRAP BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT-Q6- MAJOR REPAIR - CRACK ON WEB SUPPORT STRAP AT BS 639, S16R. REPAIRED WEB SUPPORT STRAP AT BS 639, S16R IAW B737 SRM 51-40-02 AND BOEING DRAWING 65-46920. (S) 2 L 7 2 4F RT A16WE 20080903 NM 2008 9 3 USAA920081552 1 20080812 A 5320 6546812169 FLOOR SUPPORT BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN-C19 -MAJOR REPAIR- GALVANIC CORROSION ON FLOOR SUPPORT AT BS 967 TO BS 986.5 RBL 18. REPLACED FLOOR SUPPORT AT BS 9 67 TO BS 986.5 RBL 18 IAW B737 SRM 53-60-51-1A1. (S) 2 L 7 2 4F RT A16WE 20080903 NM 2008 9 3 USAASB08062 1 20080817 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 456UW 25020 FLL, MAINTENANCE REPORTED THE AFT EMERGENCY LIGHTS CYCLING ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE AFT LT EMER GENCY LIGHT BATTERY CHARGER. OPERATIONAL CHECK NORMAL. (S) 2 L 7 2 4F RT A16WE 20080903 EA 2008 9 3 REX2008F00041 1 20080815 A 2611 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY FALSE INDICATION A REXA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SO 25 8694A 13856 7694 ON APPROACH INTO DTW RECEIVED "CARGO SMOKE" MASTER WARNING. QRH FOLLOWED, BOTTLES DISCHARGED. EMERGENCY FOLLOWED BY UN EVENTFUL LANDING. ACFT INSPECTED BY EMERGENCY VEHICLES WITH NO FIRE OR SMOKE FOUND "FALSE WARNING". REMOVED AND REPLAC ED THE CARGO FORWARD DETECTOR IAW BOMBARDIER AMM. OPERATIONALLY CHECKED GOOD. (S) 2 L 7 2 4F RT A21EA 20080903 EA 2008 9 3 QXEA200800707 2 20080713 A 7200 312162701 ENGINE BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA NR 1 SHUTDOWN A QXEA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 09 425QX 12883 2122 4039 0074 PDX - ON CLIMBOUT AT ABOUT 3,500FT RECEIVED A NR 1 OIL PRESSURE LIGHT FOLLOWED BY A DROP IN ENGINE TORQUE. SHUTDOWN ENG INE AND ACCOMPLISHED FAILURE CHECKLIST. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLA CED THE NR 1 ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 H 7 2 4T 4 T RT A13NM E00062EN 20080903 NE 2008 9 3 PNSA044A 2 20080730 A 7250 TURBINE BLADES SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE SEPARATED A PNSA C ABORTED TAKEOFF E F J VIBRATION/BUFFET FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 AL 03 364PX 340B262 GE785350 ON 7-29-08 SAAB 340B N364PX - ON TAKEOFF ROLL WHEN PILOT HEARD A POP AND THE AIRCRAFT STARTED TO YAW TO THE LT, THE PILO T ABORTED THE TAKEOFF AND DETERMINED THAT THE LT ENGINE WAS CAUSING THE PROBLEM. THE LT ENGINE WAS SHUT DOWN AND AIRCRA FT RETURNED TO THE HANGER, UPON EXAMINATION WITH BORESCOPE AND VISUAL THROUGH THE EXHAUST WE FOUND ALL THE 3 1 TURBINE B LADE MISSING DAMAGE TO THE NR 2, 3, 4, AND 5 TURBINE NOZZLE AND DAMAGE TO THE TURBINE WHEELS. THE ENGINE HAS A TTSN 325 62,4 AND TOTAL CYCLES 27799 AND A TTSOH OF 4945. (A) 2 L 7 2 4T 4 T RT A52EU E8NE 20080903 EA 2008 9 3 QXEA200800734 1 20080710 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 572 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 612QX 10042 PDX-C4 CHECK. CORROSION ON INBOARD RT SEAT TRACK AT STATION 572.00. REMOVED CORROSION BY BLENDING. REMOVED MATERIAL W ITHIN LIMITS. HFEC FOR CRACKS, NONE NOTED. ALODINED AREA. (S) 2 L 7 2 4F RT A21EA 20080903 SO 2008 9 3 C2XA08SH107 1 20080817 A 5751 14569009410 BRACKET EMB 145 EMB145LR 3260212 SO RT AILERON WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16571 145633 SHV - DURING C-CHECK. THE RT AILERON TO PCA ATTACHMENT BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHIN GS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN T O SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080903 EA 2008 9 3 REX2008F00039 1 20080813 A 2611 DETECTION SYS CNDAIR CL600 CL6002B19 1900309 EA CARGO SMOKE FALSE ACTIVATION A REXA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SO 25 8694A 7694 RECEIVED CARGO SMOKE MESSAGE AT GATE, DETERMINED AFTER INSPECTION TO BE A FALSE WARNING. POWER RESET TO DATA CONCENTRAT OR UNIT (DCU) AND PERFORMED OPERATIONAL CHECK OF CARGO DETECTON SYSTEM IAW AMM. NO DEFECTS FOUND. (S) 2 L 7 2 4F RT A21EA 20080903 NM 2008 9 3 NWAA083795810 1 20080813 A 3350 SIGN BOEING 757 757351 1384991 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 590NW 32990 DURING OVERNIGHT MAINTENANCE THE LT OVERWING EMERGENCY EXIT SIGN AND BOTH FORWARD AND AFT SLIDE HANDLE LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE ASSOCIATED POWER SUPPLY M11487. ALL OPERATIONS CHECKED GOOD. (S) 2 L 7 2 4F RT A2NM 20080903 NM 2008 9 3 USAASB08066 1 20080818 A 5210 SCREW BOEING 737 737401 1384701 NM L1 DOOR LOCK ARM BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 23879 CLT - MAINTENANCE REPORTED THE SCREW WAS BROKEN ON THE FORWARD ENTRY DOOR LOCKING ARM. MAINTENANCE REMOVED AND REPLACED THE SCREW. OPERATIONAL CHECK NORMAL. (S) 2 L 7 2 4F RT A16WE 20080903 NM 2008 9 3 USAASB08061 1 20080816 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM EMERGENCY LIGHT FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 456UW 25020 CLT - MAINTENANCE REPORTED THE AFT ENTRY DOOR EMERGENCY EXIT LIGHT FLICKERS. MAINTENANCE REMOVED AND REPLACED THE LT AN D RT EMERGENCY LIGHT BATTERY PACKS IN THE AFT POWER SUPPLIES. OPERATIONAL CHECK NORMAL PER MM 33-51-51-2. (S) 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086467 1 20081121 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081125 EU 2008 11 25 COEA0807917 1 20081017 A 5315 S53172210200 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 917FX 354 FOUND AT COE MAJOR REPAIR FLOOR BEAM 10 IS CORRODED ON THE UPPER AND LOWER SURFACE OF THE INTERCOSTAL 10 INCHES LT AND R T OF BL 0. 2 H 7 2 4T RT A53EU 20081125 EU 2008 11 25 NWAA084903304 1 20081031 A 3350 BATTERY AIRBUS 330 A330323 3940030 EU EMERGENCY LIGHT NO TEST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 804NW 0549 BATTERY EPSU 11 WL FAILED CAPACITY CHECK, REPLACED BATTERY AND TESTS OK. 2 L 7 2 4F RT A46NM 20081125 2008 11 25 SWAA086502 4 20081121 A 2565 6557463 MOUNT BRACKET BOEING 737 7373H4 1384600 NM EVAC SLIDE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR SLIDE FWD MOUNT BRACKET BROKEN. REMOVED AND REPLACED BRACKET PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086521 1 20081121 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 5 SLAT I/B END TOP SIDE DELAMINATED. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086343 1 20081118 A 5310 6549889 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER STOP FITTING. REMOVED AND REPLACED F RAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0853751 1 20081105 A 3040 8300005604 CONTROLLER BOEING 737 737890 1384527 NM WINDOW HEAT MALFUNCTIONED A ASAA K NONE J WARNING INDICATION CR CRUISE 1 NM 02 558AS 286 35177 WINDOW HEAT LEFT SIDE OVERHEAT LIGHT ON. INFO CAME ON AT 30 MIN AFTER T/O, ALT 37000 (TAT 31C). FOLLOWED QRH SWITCH OF F. RESET LEFT SIDE WINDOW HEAT POWER C/B PER MM 20 60 01. ACCOMPLISHED FIM 30 41 00 810 801. NO FAULTS NOTED. GROUND VERIFICATION SUCCESSFUL. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843701 1 20081029 A 5755 654645170 SKIN BOEING 737 737490 1384715 NM RT SPOILER DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 RT OUTBOARD GROUND SPOILER HAS PROTRUSION ON UPPER SURFACE AT O/B END ABOVE LOWER BLADE SEAL RETAINER. PREPPED DAMAGED AREA, FABBED REPAIR DOUBLER AND BONDED DOUBLER IAW B737 400 SRM 51 70 10 REP 2. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843778 1 20081029 A 5315 6545808260 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FLOORBEAM CORRODED. REPLACED FLOORBEAM PER SRM 53 10 51. 2 L 7 2 4F RT A16WE 20081126 SO 2008 11 26 SWIA200820432 1 20081114 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 583SW 120351 FLT 5458 - OVERHEAD EMERGENCY LIGHT EXIT ROW 9 B AND C INOP. RELAMPED. 2 L 7 2 4T RT A31SO 20081126 NM 2008 11 26 DHLA2008745698 1 20081116 A 5753 FLAP TRACK BOEING 727 727224 1384076 NM NR 6 FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 NR 6 FLAP TRACK FWD SUPPORT FITTING CORRODED. REPAIRED FITTING ATTACH LUGS IAW COOPESA EO COO-2-57-340-08 DATED 10/07/0 8 AND BAC MSG 1-1002286730-4 DATED 11/06/08 AND 1-1002286730-11 DATED 11/12/08. REF FAA FORM 8100-9 DATED 11/14/08 AND ASTAR EVA B257-00145 FOR REPAIR APPROVAL. DOCUMENTED ON COOPESA N/R 6-200. 2 L 7 3 4F A3WE 20081126 EA 2008 11 26 QXEA2008112401196 1 20081120 A 3230 9752753 VALVE CNDAIR CL600 CL6002C10 1390015 EA ZONE 700 MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 19 603QX 4676 10011 PDX - PROX SYSTEM CAUTION (W/PROX SYS 2 STATUS MSG) MSG, RETURNED TO FIELD. INTERROGATED MDC, LDG GEAR HANDLE D106 AND LDG GEAR SEL VLV D043/D063 FAULTS NOTED ON NOV 21, 2008 AS SINGLE OCCURRENCES IN MDC HISTORY. TROUBLESHOT LANDING GEAR HANDLE IAW CRJ-700 FIM 32-31-05-810-802-A01, HANDLE PREVIOUSLY REMOVED AND REPLACED. RESISTANCE AND SHORT CHECKS OF WIR ING IN FIM TASK OK. TROUBLESHOT LANDING GEAR SEL VLV IAW CRJ-700 FIM TASK 32-32-10-810-801-A01, VALVE PREVIOUSLY REMOVE D AND REPLACED IN HISTORY. RESISTANCE AND SHORT CHECK OF WIRING IN FIM TASK OK. REMOVED AND REPLACED NR 3 SYSTEM PRIOR ITY BALANCE RELIEF VALVE, AS A PRECAUTIONARY MEASURE IAW CRJ-700 AMM TASKS 29-12-05-000-802-A01 AND 29-12-05-400-802-A01 2 L 7 2 4F RT A21EA 20081126 NM 2008 11 26 F3LA2008112100720 1 20081119 A 3520 G1R12425 CONTAINER AIRBUS A319 A319111 3930336 NM OXYGEN SYSTEM FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 21 902FR 9 1515 DURING COMPLIANCE OF EO A8-25EO-20453, THE OXYGEN CONTAINER AT THE NINTH ROW OF SEATS ON THE RIGHT FAILED DROP TEST. MA INTENANCE REMOVED AND REPLACED THE OXYGEN CONTAINER PER A318 AMM 35-21-10-000-001 AND AMM 35-21-41-400-001. OPERATIONAL CHECK PERFORMED WITH SATISFACTORY RESULTS IN ACCORDANCE WITH A318 AMM 35-23-00-710-001. 2 L 7 2 4F RT A28NM 20081126 EA 2008 11 26 ASOA200801512 1 20081115 A 5330 DOUBLER CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 713EV 10081 CORROSION DAMAGE INTERNAL BELLY DOUBLER JUST AFT OF FS 280.00, REMOVED FASTENERS TO ACCOMMODATE CORROSION REMOVAL, REMO VED ALL CORROSION IN MARKED AREAS ON INTERNAL BELLY DOUBLER JUST AFT OF FS 280. ALL WORK DONE IAW SRM 51-21-06. PERFORM ED ET INSPECTION OF REWORKED AREA PER REO 670-53-21-407 IAW NDTM 51-20-006. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 20081126 2008 11 26 SWAA086546 4 20081121 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 FOUND L2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 08FDEA04944 1 20081120 A 5322 65163391 SHEAR TIE BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 AFT PIT BILGE BODY FRAME SHEAR TIE IS CORRODED BS 970, STR 29L OB, WL 139. REMOVED FLOOR SUPPORT ANGLE AT FRAME 970 LBL 9 REF SRM 51-30-2 PG 1-9. REMOVED CORROSION ON SHEAR TIE REF SRM 53-10-1, ORIG THICK .073, REMAINING .011, OUT OF LIMI TS. REMOVED DAMAGED SHEAR TIE, HEAT TREATED ON 8130-3 2008011-052. FABRICATED NEW FLOOR SUPPORT CHANNEL STA 970 LBL4, REMOVED FLOOR SUPPORT STA 970 LBL8. INSTALLED NEW SHEARTIE, FAB NEW FLOOR SUPPORT STA 970 LBL 8. INSTALLED FLOOR SUPPO RT STA 970 LBL 8. INSTALLED FLOOR SUPPORT STA 970 LBL 4. INSTALLED FLOOR SUPPORT STA 970 LBL 9. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081126 NM 2008 11 26 SWAA086532 1 20081123 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND LT KEELBEAM CRACKED BETWEEN BS 500C TO BS 542. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086538 1 20081121 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 220WN 32491 FOUND LT EEPLS STRIP MISSING LENS. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0843813 1 20081029 A 5340 69353527 STRINGER CLIP BOEING 737 7374Q8 138447Q NM BS 727G S26R CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 STRINGER CLIP CORRODED. REMOVED CORRODED STRINGER CLIP FABRICATED AND INSTALLED REPLACEMENT CLIP IAW B737 400 SRM 51 30 01 AND 51 40 02. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0873817 1 20081118 A 5347 146A750110 CARGO TRACK BOEING 737 737790 13844CN NM BS 942 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON THE TIE DOWN TRACK FLOOR SUPPORT AFT CARGO BAY AT BS 942 RBL 13. R & R TRACK ASSY IAW SRM. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 K11A2008112072301 1 20080409 A 5330 SKIN BOEING 727 7272H3 138368N NM FUSELAGE GOUGED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 723CK 20545 EXTERNAL FUSELAGE SKIN, SKIN GOUGED OUT OF LIMITS. 2 L 7 3 4F RT A3WE 20081128 NM 2008 11 28 K11A2008111772201 1 20081105 A 5320 WEB BOEING 727 7272H3 138368N NM BS 312-340 CORRODED A K11A K NONE O OTHER IN INSP/MAINT 1 GL 23 722CK 20948 E AND E BAY WALKWAY WEB CORRODED AT STA 312 TO 340 AND LBL 38. CORROSION 4 BY 6 INCHES. 2 L 7 3 4F RT A3WE 20081128 2008 11 28 ASAA0853877 2 20081121 A 7320 442317 HMU BOEING 737 737890 1384527 NM NR 2 ENGINE LEAKING A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 587AS 23507 35684 DURING LEAK CK OF REPLACEMENT OF NR 2 ENGINE NOTED HMU TO BE LEAKING AT THE TOP SURFACE FITTING/ADJUSTING SCREW CAP JUST AFT OF THE SUPPLY FUEL LINE. LEAK IS COMING FROM THE PARTING LINE BETWEEN HMU AND CAP REPLACED NR 2 ENGINE HMU PER AMM 73 21 10 400. OPS AND TESTS CHECK GOOD NO LEAKS. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0843831 1 20081120 A 5320 654583471 STRAP BOEING 737 7374Q8 138447Q NM FLOOR SUPPORT CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FLOORBEAM STABILIZER STRAP BROKEN/CRACKED. REMOVED CRACKED SECTION OF STRAP FABRICATED REPAIR FILLER AND STRAP INSTALLE D FILLER AND STRAP IAW SRM 51-70-13 FIG 1. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 DL757081589 1 20081111 A 5320 146N545111 INTERCOSTAL BOEING 757 757232 1384965 NM BS 1500 LBL 2.9 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 CORROSION ON INTERCOSTAL BS 1500 LBL 2.9 INBD SIDE OF INTERCOSTAL, BILGE. REPLACED INTERCOSTAL. 2 L 7 2 4F RT A2NM 20081128 NM 2008 11 28 08FDEA04939 1 20081120 A 5753 65216826 SKIN BOEING 727 727227 1384078 NM NR 6 SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 495FE 21669 RT WING L/E SLAT NR 6 LOWER SURFACE SKIN IS CRACKED AROUND RIVET HOLE. REMOVED RT NR 6 SLAT COVE PNL FOR ACCESS IAW SRM 51-30-2. FABRICATED REPAIR DOUBLE IAW SRM 57-50-3 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR IAW SR M 57-50-3 FIG 1, REINSTALLED RT NR 6 SLAT COVE PNL IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20081128 NM 2008 11 28 ASAA0873840 1 20081120 A 5320 141A5410U12 INTERCOSTAL BOEING 737 737790 13844CN NM BS 312-328 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 INTERCOSTAL CRACKED BS 312 328 RBL 30. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0843790 1 20081026 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 9 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NUMBER 9 SPOILER UPPER SURFACE DENTED. INSTALLED REPAIR DOUBLER PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0853872 1 20081121 A 2421 761574B IDG BOEING 737 737890 1384527 NM NR 2 ENGINE OUT OF LIMITS A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 587AS 17636 35684 NR 2 ENGINE IDG FREQUENCY AT 390CPS REPLACED NR 2 ENGINE IDG PER AMM 24 11 11 400. OPS CHECK GOOD, IDG ETOPS VERIFIED. 2 L 7 2 4F RT A16WE 20081128 EA 2008 11 28 ASOA200801554 1 20081124 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A ASOA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 906EV 7642 CAPTS SIDE WINDOW CRACKED IN FLIGHT. EN ROUTE TO ATL A/C DIVERTED TO MEM DUE TO MTC, EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 20081128 EA 2008 11 28 ASOA200801269 1 20081002 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 C/W STEPS 1, 4, 5, 6, AND 7 OF REO 601-R52-11-1571. NDT REQUIRED. PERFORMED EDDY CURRENT INSP ON PAX DOOR AFT SIDE SKI N BETWEN STEPS 2 AND 3 (CUTOUT) AT CORNER OF BOTTOM STEP. NO REJECTABLE INDICATIONS FOUND AT THE TIME, REPORT ATTACHED IAW STEP 2 OF REO 601R-52-11-1571 AND NDTM 51-20-06. RESTORE FINISH IS REQUIRED. C/W STEPS 3-9 OF REO 601R-52-11-1571, STEPS 10 AND 11 PAINT REQUIRED. EDGE SEALED AND PAINTED REPAIR IAW REO 601R-52-11-1571 STEPS 10 AND 11. C/W STEPS 12- 15 OF REO 601R-52-11-1571. C/W ASA EC/TC REO 601R-52-11-1571. 2 L 7 2 4F RT A21EA 20081128 EA 2008 11 28 ASOA200801273 1 20081002 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 C/W STEPS 1, 4, 5, 6, AND 7 OF REO 601-R52-11-1571. NDT REQUIRED. PERFORMED EDDY CURRENT INSP ON PAX DOOR AFT SIDE SKI N BETWEEN STEPS 2 AND 3 (CUTOUT). NO REJECTABLE INDICATIONS FOUND AT THE TIME, REPORT ATTACHED IAW STEP 2 OF REO 601R-5 2-11-1571 AND NDTM 51-20-06. RESTORE FINISH IS REQUIRED. C/W STEPS 3-9 OF REO 601R-52-11-1571. STEPS 10 AND 11 PAINT REQUIRED. EDGE SEALED AND PAINTED REPAIR IAW REO 601R-52-11-1571 STEPS 10 AND 11. C/W STEPS 12-15 OF REO 601R-52-11-15 71. C/W ASA EC/TC REO 601R-52-11-1571. 2 L 7 2 4F RT A21EA 20081128 EA 2008 11 28 ASOA200801492 1 20081112 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 RT FWD EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 20081128 EA 2008 11 28 ASOA200801525 1 20081116 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 713EV 10081 THE AFT DRAG ANGLE ON THE ASD STEP RISER IS CRACKED LOCATION MARKED. 2 L 7 2 4F RT A21EA 20081128 EA 2008 11 28 ASOA200801546 1 20081119 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA BS 469-565 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 713EV 10081 LBL 9 FLOORBEAM CORRODED AND HAS TOOLING DAMAGE AT FS 469.00 - 565.00. REWORKED AREA PER REO 670-53-31-119. 2 L 7 2 4F RT A21EA 20081128 NM 2008 11 28 ASAA0893846 1 20081119 A 5320 146A5410 WEB BOEING 737 737990 NM BS 500H CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 WHILE WORKING CUSTOMER CARD 5140480 FOUND BAFFLE INTERCOSTAL CRACKED AT BS 500H AND 500I RBL26 WL154. R&R INTERCOSTAL. 2 L 7 4 4F RT A16WE 20081128 EA 2008 11 28 ASOA200801556 1 20081124 A 3350 BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS FAILED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 905EV 7632 NR 4 EMERGENCY BATTERY FAILED OPS CHECK. 2 L 7 2 4F RT A21EA 20081128 2008 11 28 DHLA200800132 2 20081119 A 7261 OIL FILTER BOEING 727 7272B7 138407L NM NR 3 BYPASSING A DHLA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 05 762AT 22162 NR 3 OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT PRESS TO TEST CAUSED LIGHT TO BE BRIGHTER SHUT DOWN ENGINE IN ACCORDA NCE WITH ABNORMAL PROCEDURES RESOLUTION: REMOVED AND REPLACED NR 3 MAIN OIL FILTER PER MM CH 79-00 OPS CHECK NORMAL. A/C WAS GROUNDED. 2 L 7 3 4F A3WE 20081128 NM 2008 11 28 ASAA0873869 1 20081121 A 5320 146A7502 SUPPORT BOEING 737 737790 13844CN NM CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON FLOOR TO SIDEWALL SUPPORT AFT CARGO BAY BS 887-945 RBL 20. REPLACED SECTION OF ZEE SUPPORT FROM BS 887 945 RBL 20. 2 L 7 2 4F RT A16WE 20081128 WP 2008 11 28 AALA200802716 1 20081010 A 2120 DUCT DOUG DC9 DC983 3022083 WP AIR CON LEAKING A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SW 21 571AA 49353 LAX INFLIGHT DFW TO PDX - TAIL COMPARTMENT HIGH TEMPERATURE INDICATION IN FLIGHT. CREW SHUT DOWN LEFT AIR CONDITIONIN G PACK AND LIGHT EXTINGUISHED. LANDED LAX WITHOUT INCIDENT. REPLACED BROKEN LEFT AIR CONDITIONING PACK DUCT CLAMP. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081128 NM 2008 11 28 ASAA0843768 1 20081024 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 8 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NUMBER 8 SPOILER HAS PROTRUDING DENT ON UPPER SURFACE. REMOVED DAMAGED AREA. INSTALLED REPAIR DOUBLER PER SRM 57 70 01 . 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 UPS08553918 1 20081114 A 5610 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 422UP 25324 CAPTAIN'S LEFT SIDE WINDOW CRACKED. WINDOW REMOVED FROM A/C PER MM 56-11-02-4. CAPTAIN'S WINDOW REPLACED PER 56-11-02-4 . PERFORMED ADJ/TEST PER 56-11-02-5. 2 L 7 2 4F RT A2NM 20081128 NM 2008 11 28 USAA920082044 1 20081023 A 5320 65C10592156 INTERCOSTAL BOEING 737 737301 1384611 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10853028/018 LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL AT BS 964, BETWEEN RBL 25 TO RBL 40. REPLACED INTERCOSTAL AT BS 964, BETWEEN RBL 25 TO RBL 40 IAW SRM 51-10-02 AND 53-60-15. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 USAA920082043 1 20081024 A 5320 65C10592155 INTERCOSTAL BOEING 737 737301 1384611 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q5 MAJOR REPAIR NR 03C10853028/020 LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL AT BS 947 TO BS 964, RBL 40. REPLAC ED INTERCOSTAL AT BS 947 TO BS 964, RBL 40 IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 USAA920082045 1 20081010 A 5320 ANGLE BOEING 737 737301 1384611 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10853028/016 LEVEL 2 EXFOLIATION CORROSION ON ZEE ANGLE AT BS 970, RBL 55. REPLACED ZEE ANGLE AT BS 970, RBL 55 IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAA920082027 1 20081124 A 5312 651758240 BULKHEAD BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03055380105/005 CRACK IN VERTICAL BEAM WEB FORWARD FLANGE BS178, RBL17, WL234. REPAIRED VERTICAL BEAM WEB IAW US AIRWAYS EA NR 100702. 2 L 7 2 4F RT A16WE 20081201 EA 2008 12 1 COMA0860462 1 20081113 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 784CA 7319 LT WING FUEL ACCESS PANEL CUTOUT AT 510AB HAS PITTING CORROSION AROUND EDGES. REMOVED CORROSION IN THE CRITICAL AREA AT FUEL ACCESS PANEL 510AB CUTOUT AND FOUND THAT MATERIAL REMOVED WAS WITHIN LIMITS PER REO 601R-57-21-030 REV G. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 NWAA084945804 1 20081101 A 2530 OVEN BOEING 757 757351 1384991 NM GALLEY MALFUNCTIONED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 584NW 32984 IN FLIGHT TO OGG 1 OF THE OVENS IN THE AFT GALLEY STARTED TO EMIT SMOKE. IT IS CURRENTLY UNKNOWN IF ANY PRECAUTIONARY P ROCEDURES WERE PERFORMED BUT THE FLIGHT LANDED UNEVENTFULLY. MX DEFERRED THE SUSPECT OVEN TO MEL AND WOULD REPLACE IT O N 02 NOVEMBER. OPS OF THE OVEN WERE NORMAL AFTER REPLACEMENT. 2 L 7 2 4F RT A2NM 20081125 NM 2008 11 25 SWAA086448 1 20081120 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086449 1 20081120 A 5755 65C25243 FITTING BOEING 737 7373H4 1384600 NM NR 5 SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SPOILER FITTING CRACKED AT FWD ATTACH HOLE. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20081125 EA 2008 11 25 ASOA200801243 1 20080929 A 3350 COVER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED CRACKED COVER AND REPLACED WITH NEW SERVICEABLE COVER IAW CRJ 200 AMM 35-51-01-400-806. SUPPLEMENTAL SDR CLOSED . 2 L 7 2 4F RT A21EA 20081125 EA 2008 11 25 ASOA200801280 1 20081003 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REPAIRED FS 280 FLOOR SUPPORT ANGLE LOWER FLANGE OUTBOARD SIDE LBL 9 IAW ASA REO 601R-53-11-926. NO FURTHER ACTION REQU IRED. SUPPLEMENTAL-SDR CLOSED 11/13/2008. 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 SWAA086363 1 20081119 A 5754 65C2668C WEDGE BOEING 737 737317 138447P NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 3 SLAT O/B TRAILING EDGE WEDGE DELAMINATED. REPAIRED WEDGE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086430 1 20081120 A 5322 65C27314 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 540, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086395 1 20081119 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 880, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086396 1 20081119 A 3350 101331 LIGHT BOEING 737 7375H4 138449D NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED HC1 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT FAULTY. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086397 1 20081119 A 5754 65C26602 WEDGE BOEING 737 7373H4 1384600 NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 L/E SLAT WEDGE DELAMINATED AT O/B EDGE. REPAIRED SLAT PER MM. 2 L 7 2 4F RT A16WE 20081125 2008 11 25 SWAA086398 4 20081118 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0893787 1 20081114 A 5320 143A7501 SUPPORT BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 CORROSION ON FLOOR TO SIDEWALL SUPPORT. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT. 2 L 7 4 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843830 1 20081028 A 5753 6546434370 SKIN BOEING 737 7374Q8 138447Q NM RT IB AFT FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 RT INBD AFT FLAP UPPER SURFACE HAS DENT. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SR M 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843758 1 20081102 A 5210 571411 GUST LOCK BOEING 737 7374Q8 138447Q NM L2 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 764AS 25101 L2 DOOR GUST LOCK INOP. THOROUGHLY CLEANED AND LUBED L 2 DOOR GUST LOCK. PERFORMED OPS CHECK APPROX 20 TIMES WITH NO F AILURE. OPS NORMAL. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 08FDEA04955 1 20081121 A 5347 53FX13981 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 469FE 21581 CORROSION ON SEAT TRACK STA 1090 TO 1130 ANS BL0. FOUND CORROSION OUT OF LIMITS, REMOVED SECTION OF SEAT TRACK FROM BS 1010 TO 1130 AT BL0. FABRICATED NEW SECTION OF SEAT AND INSTALLED SECTION IAW SRM 51-10-2 AND 53-10-5. 2 L 7 3 4F A3WE 20081126 EA 2008 11 26 SWIA200820435 1 20081112 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 624 S14L CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910EV 7727 STRINGER CLIP AT FRAME 624 TO STRINGER 14 LEFT SIDE CRACKED. AD INSP, REPLACED. 2 L 7 2 4F RT A21EA 20081126 NM 2008 11 26 ASAA0843861 1 20081104 A 5753 65C2632018 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 RT OB MID FLAP TE SKIN IS CHAFED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR GENERAL. 2 L 7 2 4F RT A16WE 20081126 EA 2008 11 26 ASOA200801514 1 20081115 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 AFT MOST CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 20081126 EA 2008 11 26 ASOA200801515 1 20081016 A 5210 PANEL CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 PAX DOOR TOP STEP VERTICAL PANEL CRACKED AT FWD SIDE (MARKED). 2 L 7 2 4F RT A21EA 20081126 EA 2008 11 26 ASOA200801535 1 20081119 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA SMOKE A ASOA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 906EV 7642 FLT 5480 - ON TAKEOFF RECEIVED RT PACK HI TEMP. CONTINUED THROUGH 8000 FT. NOTICED SMOKE ODOR OFF PACK RESET PROCEDURE S. SHORTLY THERE AFTER RECEIVED SMOKE CAUTION. AIRCRAFT RETURNED TO ATL AFTER T/O. 2 L 7 2 4F RT A21EA 20081126 NM 2008 11 26 08FDEA04943 1 20081120 A 5330 65545772 SKIN BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 469FE 21581 FWD CARGO COMPT CORROSION ON SKIN AT BS 680 STR 26L TO 27L. FOUND CORROSION OUT OF LIMITS CUT OUT DAMAGED AREA DIMS 2 5 /8 INCH BY 2 INCH. FABRICATED DOUBLER USING 2024-T3 .063 PO NR 9008017 DIMS 8 1/2 INCH BY 2 INCH INSTALLED REPAIR PARTS IAW SRM 51-10-2 AND 53-30-3. 2 L 7 3 4F A3WE 20081126 NM 2008 11 26 SWAA086554 1 20081120 A 3350 101114 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 463WN 32467 FOUND RT EMERGENCY EXIT LIGHT COVERS LOOSE. R&R COVER PER MM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086555 1 20081120 A 3350 PL22300 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 487WN 33854 DURING SCHEDULED MV1 CHECK, FOUND EEPLS STRIP LENS LOOSE BETWEEN ROW 1 TO ROW 3. R&R STRP PER MM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086556 1 20081122 A 2560 P4010021 BATTERY BOEING 737 7375H4 138449D NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 507SW 24184 FOUND AFT EMERGENCY FLASHLIGHT INOP. R&R BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0843808 1 20081030 A 5311 654653141 FRAME BOEING 737 7374Q8 138447Q NM BS 500D CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FRAME AT STA 500D IS CORRODED. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM 51-70-11 REPA IR 2. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 DL757081588 1 20081111 A 5321 146N5391424 FLOOR PANEL BOEING 757 757232 1384965 NM BS 1380-1460 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 AFT CARGO BAY BS 1380-1460 RBL 20 FIXED FLOOR PANEL CORRODED AT NUTPLATE LOCATIONS. AREAS OF CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FIXED FLOOR PANEL IAW SRM 51-40-05. 2 L 7 2 4F RT A2NM 20081128 NM 2008 11 28 ASAA0843798 1 20081029 A 5320 50826185 INTERCOSTAL BOEING 737 7374Q8 138447Q NM CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 INTERCOSTAL STA 295 STR 4L IS CRACKED REMOVED CRACKED INTERCOSTAL INSTALLED NEW INTERCOSTAL IAW B737 400 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0843799 1 20081029 A 5320 50826183 STRAP BOEING 737 7374Q8 138447Q NM GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 INTERCOSTAL TIE STRAP STA 295 IS GOUGED REMOVED GOUGED STRAP INSTALLED NEW STRAP IAW B737 400 SRM 51 40 02 ASA EA 400 53 EA 00199. 2 L 7 2 4F RT A16WE 20081128 EA 2008 11 28 ASOA200801548 1 20081122 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA NO TEST A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 758EV 10210 FLT 5531 - EMERGENCY EXIT LIGHTS W/N TEST. 2 L 7 2 4F RT A21EA 20081128 EA 2008 11 28 ASOA200801544 1 20081119 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 867AS 7463 CARGO BAY SEAT TRACK BETWEEN FS 559.00+86 AND FS 574.00 AT LBL 9 CORRODED ALONG WITH HARDWARE. REMOVED AND REPLACED SE AT TRACK IAW AMM 53-01-11. 2 L 7 2 4F RT A21EA 20081128 NM 2008 11 28 ASAA0843810 1 20081113 A 5753 6546435281 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NUMEROUS DENTS ON LT OTBD TE OF AFT FLAP LOWER SURFACE. PREPPED DAMAGED AREA FABRICATED AND INSTALLED REPAIR AND DOUBLE R AND FILLER IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081128 EA 2008 11 28 ASOA200801549 1 20081122 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 754EV 10173 RT OVERWING EMERGENCY EXIT LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS. 2 L 7 2 4F RT A21EA 20081128 EA 2008 11 28 ASOA200801551 1 20081122 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 907EV 7648 RT OVERWING FWD EMERGENCY LIGHT IS INOP. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 USAA920082025 1 20081015 A 5712 6545445 RIB BOEING 737 737301 1384611 NM RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C40557004/001 RT WING INTERIOR RIB 135.5 LOWER CHORD CRACKED AT LOWER AFT END. REPAIRED RT WIN G INTERIOR RIB 135.5 LOWER CHORD IAW US AIRWAYS EA NR 100733 AND US AIRWAYS TYPICAL REPAIR NR 57-25-20. 2 L 7 2 4F RT A16WE 20081201 EA 2008 12 1 COMA0860467 1 20081113 A 5210 601R31902 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 784CA 7319 PAX DOOR INNER SKIN IS CRACKED AT DOOR DATUM 1 BETWEEN FS340 AND DOOR DATUM 1. CUT OUT DAMAGE AND INSTALLED A PERMANENT REPAIR DOUBLER WITH SHIMS PER EA 10-5210-02412 DATED 10/06/08. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 NWAA084926301 1 20081104 A 3350 CHARGER BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING OVERNIGHT CHECK FOUND EMERGENCY LIGHTS EXTERIOR RT AFT 2 INOP. MX R&R BATTERY AND CHARGER. OPS CHECKED GOOD AND ACFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20081201 EU 2008 12 1 NWAA084913254 1 20081103 A 3350 EPSU AIRBUS 320 A320212 3930322 EU CABIN DISCHARGED A NWAA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 01 354NW 801 EPSU UNIT FWD L SHOWS FAULTED. 1ST CLASS PATH LIGHTING INOP. REPLACED EPSU 10WL AND BATTERY. REPLACED EGRESS LIGHTING HARNESS AT SEAT 4AB. CHECKS GOOD. 2 L 7 2 4F RT A28NM 20081201 EA 2008 12 1 COMA0860464 1 20081113 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 784CA 7319 FUEL DRAIN AFT OF LT WING FUEL PANEL 510AB CUTOUT HAS DAMAGE ON AFT SCREW ATTACH HOLE. REAMED AND INSTALLED A SERVICEAB LE FREEZE PLUG BUSHING FOR FUEL DRAIN AFT OF LT WING FUEL PANEL 510AB CUTOUT AFT SCREW ATTACH HOLE IAW COMAIR EA # 10-57 21-02413. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 SWAA086598 1 20081125 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086620 1 20081125 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND FRAME STUB BEAM CRACKED AT BS 706, RBL 45. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086621 1 20081125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 7L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086622 1 20081125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086599 1 20081125 A 5330 6547952 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR SKIN CUTOUT CRACKED AT UPPER AFT CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086601 1 20081125 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086603 1 20081125 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 DL757081637 1 20081118 A 5347 694557931 CARGO TRACK BOEING 757 757232 1384965 NM BS 1415-1420 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 CORROSION ON AFT CARGO TIE DOWN FITTING BS 1415-1420 RBL 25 WL 147 AT DOOR CUTOUT NO ALLOWABLE LIMITS IN SRM. REMOVED A ND REPLACED FITTING. 2 L 7 2 4F RT A2NM 20081201 NM 2008 12 1 DL757081638 1 20081116 A 5321 146N543142 FLOOR PANEL BOEING 757 757232 1384965 NM BS 1530-1560 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 WHILE WORKING CUSTOMER CARD 00040 FOUND RIGHT FIXED FLOOR PANEL TO BE CORRODED FROM BS 1530-1560 O/B EDGE. 2 L 7 2 4F RT A2NM 20081201 WP 2008 12 1 AALA200810178 1 20081112 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1418 S2R CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 584AA 53247 FRAME AT STATION 1418 AT LONGERON 2R AFT SIDE CRACKED. REPAIRED FRAME PER ESO80559 DATED 11-11-08. 2 L 7 2 4F A6WE 20081201 NM 2008 12 1 AALA200820028 1 20081029 A 5320 146N5246U6 GUSSET BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 663AM 53392 25297 RIGHT NR 4 DOOR DRAIN GUSSET CORRODED. REPAIRED AND REPLACED IAW SRM 51-21-03. 2 L 7 2 4F RT A2NM 20081201 NM 2008 12 1 DL76L081610 1 20081121 A 7932 TRANSMITTER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE ENGINE OIL QTY INOPERATIVE A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 1201P 28458 724164 LT ENGINE OIL QTY INDICATION 0 QUARTS AFTER ENGINE START. AFTER SHORT TAXI QTY INDICATON RETURNED TO NORMAL. FWD TO MC O AND PLACARD T/S PER FIM FOUND OIL QTY TRANSMITTER INOP. REMOVED AND REPLACED OIL QTY TRANSMITTER AS PER AMM. PERFOR MED OPS AND SYSTEM TEST ALL OK RAN ENGINE AT IDLE FOR 5 MINUTES OIL QTY STAYED WITHIN PARAMETERS OK FOR SVC. MCO AND PL ACARD REMOVED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081201 NM 2008 12 1 SWAA086611 1 20081125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 390, STR 15L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086612 1 20081125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 18L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086613 1 20081125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 18L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086614 1 20081125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 18L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081201 2008 12 1 SWAA086575 4 20081123 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 L1 DOOR SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086618 1 20081125 A 5312 6517582 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND LT VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REPAIRED WEB PER ER. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086619 1 20081125 A 5311 6546545 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND FRAME STUB BEAM CRACKED AT BS 685, RBL 45. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086576 1 20081124 A 3350 8210248801 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 740SW 29276 DURING SCHEDULED HC1 CHECK, FOUND EMERGENCY EXIT LIGHT LENS CRACKED AT L2 DOOR. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086581 1 20081124 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM CORRODED AT BS 500C + 12, STR 27R. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 DL757081617 1 20081114 A 5320 146N54514 WEB BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 1520 LBL 10.5 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 724164 CORROSION BS 1520 LBL 10.5 COMMON TO HORIZONTAL WEB OTBD FLANGE, FOUND OUT OF LIMITS. REMOVED AND REPLACED PART IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E24NE 20081201 WP 2008 12 1 AALA200810188 1 20081114 A 5320 ANGLE DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70529 49921 CORROSION ON HORIZONTAL LEG OF AFT CARGO DOOR BEAM AT STATION 1174 TO 1211. REMOVED CORROSION AND INSTALLED REPAIR DOUB LER PER AARD 53-10-00-3. 2 L 7 2 4F A6WE 20081201 EA 2008 12 1 SWIA200820474 1 20081119 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 929SW 7703 FLT 6189 - EMERGENCY LIGHT AT ROW 5 INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081201 WP 2008 12 1 AALA200810179 1 20081112 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 584AA 53247 FRAME AT STATION 1418 AT 2R FORWARD SIDE CRACKED. REPAIRED PER ESO80559 DATED 11-11-08 2 L 7 2 4F A6WE 20081201 WP 2008 12 1 AALA200810189 1 20081118 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP ZONE 100 BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 NR 4 SEAT TRACK ATTACH LUG BROKEN OFF AT STATION 672. INSTALLED SEAT TRACK PLUG PER AARD 53-20-00-10. 2 L 7 2 4F RT A6WE 20081201 CE 2008 12 1 ZESA2008012 1 20080716 A 3040 ANTI-ICE SYSTEM CESSNA 500 560CESSNA 2076750 CE WINDSCREEN MALFUNCTIONED E ZESA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 03 511TH 5600561 CREW IDENTIFIED THE WINDSCREEN OVERHEAT ANNUNCIATOR CAME ON AT TAKEOFF POWER WITH VALVES CLOSED AND SWITCH OFF. THE CRE W ABORTED TAKEOFF AND MAINT WAS CALLED IN. TROUBLESHOT ACFT WINDSHIELD HEAT SYS IAW MM, NO DEFECTS NOTED. ENGINE RUN A T FULL POWER, NO BLEED AIR DETECTED ACROSS WINDSCREEN. ALL CHECKS WERE NORMAL, COULD NOT DUPLICATE. 2 L 7 2 4F RT A22CE 20081201 EA 2008 12 1 SWIA200820476 1 20081115 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 AD INSPECTION, ENGINE SUPPORT BEAM INSPECTION PER AD CONFIRMED CRACKS. REPAIRED PER SB 601R-53-061. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 AALA200820030 1 20081024 A 5315 FLOORBEAM BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 697AN 45632 26977 FLOORBEAM CORRODED. REPAIRED IAW EA B757-53-004790. 2 L 7 2 4F RT A2NM 20081201 WP 2008 12 1 AALA200810191 1 20081118 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP ZONE 100 BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 NUMBER 4 SEAT TRACK TANG BROKE OFF STATION 948-949. INSTALLED NEW SEAT TRACK PER AARD 53-20-00-10. 2 L 7 2 4F RT A6WE 20081201 WP 2008 12 1 AALA200810182 1 20081117 A 5311 FRAME DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7537A 49991 CANT FRAME CRACKED AT LOWER TAILCONE ALIGNMENT PIN, STATION 1510, LEFT. REPAIRED PER ESO80559 DATED 11-17-08. 2 L 7 2 4F A6WE 20081201 WP 2008 12 1 AALA200810183 1 20081122 A 5320 PAN DOUG DC9 DC983 3022083 WP CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 594AA 53284 CORROSION ON HORIZONTAL FLANGE OF FORWARD CARGO DOOR PAN, STATION 500. REPAIRED PER ESO80559 DATED 11-20-08. 2 L 7 2 4F RT A6WE 20081201 EA 2008 12 1 SWIA200820444 1 20080827 A 5310 ISOLATOR CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 918SW 7645 C-CHECK, THREE ISOLATORS FORWARD SIDE OF AFT PRESSURE BULKHEAD CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081126 WP 2008 11 26 AALA200802709 1 20081009 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 460AA 49565 LGA EMERGENCY PATH LIGHTING AT SEAT 20D INOPERATIVE. RECONNECTED LOOSE CONNECTOR AT SEAT 20D FOR EMERGENCY PATH LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 20081126 WP 2008 11 26 AALA200802710 1 20081009 A 3397 WIRE HARNESS DOUG DC9 DC982 3022082 WP TAILCONE DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 460AA 49565 LGA EMERGENCY ESCAPE PATH LIGHT IN AFT SIDEWALL PANEL IN TAILCONE HAS WIRES DISCONNECTED. SECURED WIRES FOR EMERGENCY LIGHT IN AFT SIDEWALL PANEL IN TAILCONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 20081126 WP 2008 11 26 AALA200802711 1 20081009 A 3397 WIRE HARNESS DOUG DC9 DC983 3022083 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 969TW 53619 SFO EMERGENCY SEAT MOUNTED LIGHTS AT SEAT ROW 29D INOPERATIVE. REPAIRED WIRING AT SEAT ROW 29D FOR EMERGENCY SEAT MOUN TED LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A6WE 20081126 WP 2008 11 26 AALA200810132 1 20081027 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 CUSP CORRODED ON TOP SIDE UNDER GIRT BAR BRACKET AT STATION 1168. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-2 0-00-16. 2 L 7 2 4F A6WE 20081126 NM 2008 11 26 AALA200820019 1 20081014 A 5320 CPN4048194 BEAM BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 672AA 52528 25337 TOP OF LATERAL I BEAM CORRODED. REPAIRED IAW SRM 53-00-51-2R. 2 L 7 2 4F RT A2NM 20081126 EA 2008 11 26 SWIA200820433 1 20081113 A 7120 BUSHING CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910EV 7727 LEFT ENGINE FORWARD MOUNT YOKE UPPER LINK BUSHINGS CORRODED. AD INSP, REPLACED. 2 L 7 2 4F RT A21EA 20081126 NM 2008 11 26 08FDEA04942 1 20081120 A 5414 SKIN BOEING 727 727227 1384078 NM ZONE 400 ERODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 495FE 21669 NR 1 NOSE COWL L/E SKIN AT BOTTOM HAS AREAS OF EROSION AND 3 CRACKS. REMOVED ACCESS PANEL IAW B727 SRM 51-30-2, CUT OUT DAMAGE DIMS 9 3/4 BY 3/4 IAW B727 SRM 54-30-3 FIG 3. FAB DOUBLER MAT 2024T3 .050 PO NR 9007861 DIMS 19 3/8 BY 3 1/2 A ND FILLER MATERIAL 2024T3 .040 PO NR 9007927 DIMS 9 3/4 BY 3/4 IAW B727 SRM 54-30-3 FIG 3A AND 54-30-2 FIG 1. TREATED A ND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED PARTS IAW B727 SRM 51-30-2 AND REINSTALLED PANEL IAW B727 SRM 51 -30-2. 2 L 7 3 4F A3WE 20081126 EA 2008 11 26 SWIA200820442 1 20081116 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 FLT 6276 - CEILING LEVEL CABIN EMERGENCY LIGHT INOP SECOND FROM AFT POSITION. RELAMPED. 2 L 7 2 4F RT A21EA 20081126 EA 2008 11 26 ASOA200801537 1 20081119 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 THE RT PRESSURE FLOOR SILL ANGLE HAS CORROSION AT FS 484 RBL 45. THE REMAINING THICKNESS IS .060 IN TWO AREAS AND .063 IN TWO AREAS WHICH IS BEYOND THE LIMITS OF REO 601R-53-41-666. 2 L 7 2 4F RT A21EA 20081126 NM 2008 11 26 ASAA0843781 1 20081026 A 5755 654645262A SKIN BOEING 737 7374Q8 138447Q NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NUMBER 5 SPOILER UPPER SURFACE IS DENTED. INSTALLED REPAIR DOUBLER PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086564 1 20081121 A 3350 PL22300 STRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 902WN 36615 DURING SCHEDULED MV2 CHECK, FOUND EEPLS STRIP LOOSE AT ROW 1. R&R STRIP PER MM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086533 1 20081123 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS. 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0893857 1 20081123 A 5320 143A83314 SCUFF PLATE BOEING 737 737990 NM CARGO DOORWAY CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 FWD CARGO BAY DOOR CUTOUT AFT CORNER SCUFF PLATE CRACKED. REMOVED AND REPLACED WD CARGO BAY DOOR CUTOUT AFT CORNER SCUF F PLATE. 2 L 7 4 4F RT A16WE 20081128 2008 11 28 ASAA0853806 4 20081118 A 3460 1762000101 COMPUTER BOEING 737 737890 1384527 NM FLT MANAGEMENT MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 577AS 6662 35186 ON TAXI OUT IN HNL "FMC DISAGREE" LIGHT ILLUMINATED FOLLOWED QRH. NO HISTORY 10 DAYS PREFORMED FIM 34 61 TASK 835 NO FA ULT MESSAGE FAULT INTERMITTENT PER FIM TASK NOTIFIED, GROUND VERIFICATION SUCCESSFUL. 2 L 7 2 4F RT A16WE 20081128 EA 2008 11 28 ASOA200801524 1 20081116 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 914EV 7752 EMERGENCY LIGHTING FLOOR STRIP IN FRONT OF SEAT 1B BROKEN. 2 L 7 2 4F RT A21EA 20081128 EA 2008 11 28 ASOA200801547 1 20081121 A 2560 BATTERY CNDAIR CL600 CL6002B19 1900309 EA FLASHLIGHT DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 979EV 7737 CAPT'S, FO'S AND FA FLASHLIGHT BATTERY ARE WEAK. 2 L 7 2 4F RT A21EA 20081128 NE 2008 11 28 ASAA0873765 2 20081113 A 7200 CFM567B24 ENGINE BOEING 737 737790 13844CN NM GE CFM56 CFM56* 13802 NE NR 2 SURGES A ASAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 02 609AS 27945 29752 888267 APPROX 1500' AGL ON TAKEOFF RT ENG SURGE/STALL APPROX 3 TIMES RIGHT AFTER POWER REDUCTION. SLIGHTLY HIGH EGT RT ENG A/T OFF AND POWER REDUCTION PER QRH ENG RAN NORMALLY J HOOK INSPECTION FAILED. DAMAGE NOTED ON THE HPC BLADES. EVIDENCE O F BIRDSTRIKE. NR 2 ENGINE REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 20081128 NE 2008 11 28 ASAA0853773 2 20081114 A 7200 CFM567B27 ENGINE BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE NR 2 MAKING METAL A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 559AS 31124 35178 876334 FOUND MATERIAL IN AFT SUMP CHIP DETECTOR NR 2 ENGINE FOUND APPROX 4 PIECES ALL NON MAGNETIC. THE LARGEST APPROX 0.400". UNABLE TO DETERMINE MATERIAL. RAN ENGINE NR 2 AT HIGH PWR PER CHIP ANALYSIS MANUAL. SENT MATERIAL TO SEA FOR EVALUATI ON. NO PARTICLES NOTED AFTER ENG RUN. ENGINE IS CURRENTLY ON REINSPECT INTERVAL. 2 L 7 2 4F 4 F RT A16WE E2GL 20081128 EA 2008 11 28 ASOA20081540 1 20081119 A 5230 PANEL CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED FWD CARGO LINER PANEL ABOVE DOOR IAW SRM 51-41-02. OK TO CLOSE CARGO LINER PANEL ABOVE DOOR. INSTALLED NEW SER VICEABLE FWD CARGO LINER PANEL ABOVE ARGO DOOR CUTOUT IAW AMM 20-21-00-910-801. 2 L 7 2 4F RT A21EA 20081128 NM 2008 11 28 ASAA0843812 1 20081025 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 8 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NR 8 SPOILER LOWER SURFACE DENTED. PREPPED DENTED AREA FABRICATED AND INSTALLED REPAIR AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0843858 1 20081117 A 5320 69165004 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 747-767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 INTERCOSTAL CORRODED STA 747 767 STR 26R. REMOVED CORRODED INTERCOSTAL INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51 40 2. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0843859 1 20081123 A 5320 69353654 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 380-400 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 INTERCOSTAL CRACKED AND FASTENER HOLES STA 380-400. REMOVED CORRODED INTERCOSTAL INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0873863 1 20081120 A 5320 SUPPORT BOEING 737 737790 13844CN NM BS 727-767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON FLOOR TO SIDEWALL SUPPORT OF CARGO BAY BS 727-767 RBL 20. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT. 2 L 7 2 4F RT A16WE 20081128 EA 2008 11 28 ASOA20081543 1 20081119 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED MINOR CORROSION AROUND FASTENER HOLES UNDER PANELS 832AR, 832BR, 832CR, 832ER AND 832GR IAW SRM 51-21-06. 2 L 7 2 4F RT A21EA 20081128 EA 2008 11 28 QXEA2008112001178 1 20081108 A 5320 STIFFENER CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 617QX 10130 PDX - C3 - VERTICAL STIFFENER CRACKED AT FS 280 RBL 25.5. REMOVED CRACKED STIFFENER, FABRICATED REPLACEMENT STIFFENER O F 7075-T6 .032 MATERIAL TREATED AND PRIMED PART. PAINTED PART REF CRJ SRM 53-11-10-003-A01 PG 17 ITEM 81B. INSTALLED V ERTICAL STIFFENER IAW CRJ 700 SRM 51-42-06 AND SRM 51-42-21. 2 L 7 2 4F RT A21EA 20081128 NM 2008 11 28 ASAA0843796 1 20081024 A 5753 6546435281 SKIN BOEING 737 7374Q8 138447Q NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 LT OTBD AFT FLAP DENTED ON LOWER SURFACE. PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 1 0 REPAIR 2. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0893854 1 20081122 A 5321 453A2610 FLOOR PANEL BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 AFT CARGO BAY FLOOR PANEL BS 767 887 HAS CORROSION. REMOVED AND REPLACED AFT CARGO BAY FLOOR PANEL BS 767 887 IAW SRM 5 3 60 53. 2 L 7 4 4F RT A16WE 20081128 NM 2008 11 28 ASAA0873868 1 20081120 A 5320 146A7502 SUPPORT BOEING 737 737790 13844CN NM CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON FLOOR TO SIDEWALL SUPPORT AFT CARGO BAY BS 727+4 754 LBL 20. R&R FLOOR TO SIDEWALL SUPPORT. 2 L 7 2 4F RT A16WE 20081201 EA 2008 12 1 COMA0860465 1 20081113 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 784CA 7319 FUEL DRAIN FWD OF LT WING FUEL PANEL 510AB CUTOUT HAS DAMAGE ON FWD SCREW ATTACH HOLE. REAMED AND INSTALLED A SERVICEAB LE FREEZE PLUG BUSHING FOR FUEL DRAIN FWD OF LT WING FUEL PANEL 510AB CUTOUT FWD SCREW ATTACH HOLE IAW COMAIR EA # 10-57 21-02413. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 USAA920082034 1 20081016 A 5315 6545810 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753005/018 LEVEL 2 EXFOLIATION CORROSION ON FLOOR BEAM T CAP UPPER CHORD AT BS312, BETWEEN R BL24 TO LBL36. REPAIRED FLOOR BEAM T CAP UPPER CHORD AT BS312, BETWEEN RBL24 TO LBL36 IAW B737 SRM 51-70-12. 2 L 7 2 4F RT A16WE 20081201 EA 2008 12 1 SWIA200820466 1 20081124 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION LD LANDING 1 NM 07 906SW 9683 1151 7510 FLT 6629 - NOSE LANDING GEAR WOULD NOT EXTEND. REPLACED NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 20081201 WP 2008 12 1 AALA200810177 1 20081113 A 5300 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS WEAK A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 584AA 53247 CABIN EMERGENCY BATTERY PACK BS-104 AT STATION 902R ARMING VOLTAGE WEAK. REPLACED BATTERY PACK WITH SERVICEABLE PACK. 2 L 7 2 4F A6WE 20081201 EA 2008 12 1 QXEA2008112601202 1 20081123 A 5610 NP1393225 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A QXEA O OTHER O OTHER CR CRUISE 1 NM 19 603QX 10795 10011 PDX - CAPT'S SIDE WINDOW CRACKED DURING FLIGHT. REMOVED AND REPLACED CAPT'S SIDE WINDOW. RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 SWAA086573 1 20081124 A 3350 81000 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED MV2 CHECK, FOUND LT AFT ENTRY EEPLS LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086609 1 20081125 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081201 2008 12 1 DL76G081614 4 20081121 A 3418 PSEU BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE STALL WARNING NO TEST A DALA D RETURN TO BLOCK N S FALSE WARNING AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 27 178DZ 30596 724164 ON TAXI OUT WARN ELEX STATUS MESSAGE. STALL WARNING WILL NOT TEST. FOUND LT STALL WARNING TEST INTERMITTING BITE TEST ON WARNING ELEX MODULE A5 T/S PER M/M. REMOVED AND REPLACED PSEU PER AMM. TEST OK. WARN MSG CLEARED. STALL WARNING T EST OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081201 NM 2008 12 1 SWAA086580 1 20081124 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM CORRODED AT BETWEEN BS 500C + 14 TO BS 500C + 17. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081201 CE 2008 12 1 ZESA2008013 1 20080917 A 3040 99120864 PRESSURE VALVE CESSNA 500 560CESSNA 2076750 CE ANTI-ICE SYSTEM INTERMITTENT E ZESA K NONE J WARNING INDICATION CR CRUISE 1 EA 03 511TH 5600561 CREW IDENTIFIED WINDSCREEN OVERHEAT ANNUNCIATOR LIGHT ILLUMINATED INTERMITTENTLY DURING FLIGHT. MAINT REPLACED WINDSHIE LD ANTI-ICE VALVE WITH NEW STYLE VALVE. LEAK AND OPS CHECK WERE SATISFACTORY. AFTER CONTACTING THE OEM, THEY CONFIRMED AN IMPROVED VALVE WAS AVAILABLE. THIS IS THE PRODUCT WE INSTALLED. 2 L 7 2 4F RT A22CE 20081201 NM 2008 12 1 AALA200820038 1 20081103 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 604AA 43723 27055 AFT MAIN DECK PLATE CORRODED. REPAIRED IAW SRM 53-60-51-2R 2. 2 L 7 2 4F RT A2NM 20081201 EA 2008 12 1 SWIA200820452 1 20080828 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 699BR 7801 C-CHECK, LEFT ENGINE THRUST FITTING CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081201 EA 2008 12 1 SWIA200820455 1 20080810 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 959SW 7840 C-CHECK, FS 280 RBL9 INBOARD AND OUTBOARD CLIPS CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081201 EU 2008 12 1 RMXA119112008 1 20081120 A 5312 BULKHEAD AGUSTA A109 A119 0261102 EU PWA PT6 PT6B37A 52179 NE FUSELAGE CRACKED E RMXA K NONE O OTHER AA AIR AMBULANCE 1 SW 05 820NA 3913 14011 PU0008 A CRACK LOCATED AT STA 3627, WL 1235, BL 510 (LT SIDE) FWD BULKHEAD RADIATING INBD AND OTBD FROM A RIVET. THE CRACK MEAS URES APPROX 3.5 INCHES TOTAL. THE RIVET IS USED TO ATTACH A CAST FITTING TO THE BULKHEAD AND IS THE LOWER LT RIVET. THE CAST FITTING IS PART OF THE FWD LT MAIN GEAR BOX STRUT ATTACHMENT POINT. 1 G 7 1 3U 4 U H7EU E4EA 20081201 EA 2008 12 1 N6WA200811092 1 20081123 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A N6WA K NONE L NO TEST IN INSP/MAINT 1 CE 03 161GJ 10253 CEILING EMERGENCY LIGHT 14/15 INOP. DIFFERED CEILING EMERGENCY FLOODLIGHT IAW MEL 33-51-01-2. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 DL757081618 1 20081118 A 5340 ATTACH ANGLE BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 1440-1460 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 724164 FOUND CORROSION ON INTERCOSTAL UPPER ATTACH ANGLE TO BE OUT OF LIMITS. FABRICATED REPLACEMENT ANGLE AND INSTALLED, BS 1 440 TO BS 1460, RBL 27, WL 147. 2 L 7 2 4F 4 F RT A2NM E24NE 20081201 EA 2008 12 1 SWIA200820464 1 20081118 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 944SW 7764 FLT 6639 - NR 3 EMERGENCY FLOOD LIGHT IN CABIN INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081201 EA 2008 12 1 SWIA200820465 1 20081122 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 932SW 7714 FLT 6561 - OVERHEAD EMERGENCY LIGHT AISLE AT ROW 2 INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081201 NM 2008 12 1 SWAA086590 1 20081125 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 4R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086592 1 20081125 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 499WN 32481 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LIGHT LENS CRACKED AT ROW 11. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086562 1 20081122 A 5743 115A5211 FITTING BOEING 737 7377H4 1384404 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 746SW 29798 DURING SCHEDULED MV3 CHECK, FOUND RT MLG FWD UPPER I/B TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 DL757081590 1 20081111 A 5320 146N545112 INTERCOSTAL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 CORROSION ON INTERCOSTAL BS 1500 RBL 2.9 O/B SIDE OF INTERCOSTAL BILGE. REPLACED INTERCOSTAL. 2 L 7 2 4F RT A2NM 20081128 NE 2008 11 28 DL76L081591 2 20081114 A 7320 27105401 STATOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 197DN 28454 727620 DURING ACCOMPLISHMENT OF EA 51-470869-12 REV H MAINTENACE FOUND PMA STATOR HAD INTERNAL DAMAGE AND REPLACED THE STATOR, STATOR PN 2710540-1 WITH DEPT 335 AS PRIME SHOP. FAA HAS REQUESTED SDR AND QA FOLLOW-UP WITH VENDOR TO CONFIRM DAMAGE A ND DETERMINE IT'S SOURCE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081128 NM 2008 11 28 ASAA0843832 1 20081029 A 5315 65C3394320 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FLOORBEAM CORRODED STA 344. REMOVED CORRODED SECTION OF UPPER CHORD. FABRICATED AND INSTALLED REPLACEMENT CHORD REPAIR ANGLES CHORD AND STRAPS IAW ASA EA 40053EA 0227. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0843788 1 20081026 A 5753 6546434370 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 RIGHT INBOARD AFT FLAP LE IS DENTED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER AND SPLICE PLATE PER SRM 57-5 3-01. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0843793 1 20081116 A 3233 65C329563 ACTUATOR BOEING 737 7374Q8 138447Q NM RT MLG LEAKING A ASAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 02 769AS 51456 25103 RIGHT MAIN GEAR RED RIGHT GEAR LIGHT ON WITH GEAR HANDLE UP. HAD BOTH GREEN AND RED LIGHTS WITH GEAR HANDLE IN OFF POSI TION AFTER BEING UP. NORMAL GEAR EXTENSION CHECKED UPLOCK SENSOR GAP REF 32-61-21 WITHIN LIMITS. RANG OUT UPLOCK SENSO R AND 74 RESISTANCE NORMAL REF M/M 32-61-00. REPLACED RT UP LOCK ACTUATOR REF AMM 32-32-41. LUBED MLG (ALL) REF 12-21- 11. REMOVED AND REPLACED RT MLG ACTUATOR REF MM 32 32 11. COMPLIED WITH OPS OF MLG TEST REF 32-32-00/715 001. OPS LEA KS CHECKS GOOD. 2 L 7 2 4F RT A16WE 20081128 NM 2008 11 28 ASAA0853875 1 20081121 A 4900 38007021 APU BOEING 737 737890 1384527 NM APU BAY ODOR A ASAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 02 557AS 26675 35176 VERY STRONG ODOR ON CLIMB-OUT AND DESCENDING THROUGH 10000 (MAINLY REAR CABIN AND FLT DECK) ALSO PUTRID ODOR ON FLT DECK (ON GROUND WITH APU RUNNING) NOT COMING FROM GASPERS. THE AIRCRAFT APU IS CAUSING SIGNIFICANT CABIN ODOR. SUSPECT COM PRESSOR OIL CONTAMINATION. APU REMOVED & REPLACED COMPLETED OIL CONTAMINATION REMOVAL FROM AIR CONDITIONING AND PNEUMA TIC SYSTEM REF MM 21-00-01-100-801. 2 L 7 2 4F RT A16WE 20081128 EA 2008 11 28 ASOA200801493 1 20081112 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 LT AFT EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 20081128 NM 2008 11 28 ASAA0893791 1 20081114 A 5320 143A7501164 SUPPORT BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 CORROSION ON LT FLOOR TO SIDEWALL SUPPORT FORWARD CARGO BS 500H 500L. REPLACED FLOOR TO SIDEWALL SUPPORT. 2 L 7 4 4F RT A16WE 20081128 NM 2008 11 28 ASAA0843786 1 20081029 A 5754 65C266D3192 SKIN BOEING 737 7374Q8 138447Q NM NR 4 CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NUMBER 4 SLAT TE WEDGE LOWER SKIN IS CHAFED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR FILLER AND DOUBLERS PER SRM. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 SWAA086586 1 20081125 A 5322 6546529 SHEAR TIE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, RBL 18. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081201 2008 12 1 USAABB08168 4 20081114 A 2565 31253003 SQUIB BOEING 767 767201 1385125 NM LT WING DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 246AY 23898 PHL - THE COCKPIT SQUIB TEST ON THE LEFT WING, NUMBER TWO SPOILER OVER-RIDE ACTUATOR DOES NOT TEST PROPERLY. MAINTENAN CE REPLACED THE LEFT WING SPOILER, OVER-RIDE ACTUATOR SQUIB. SYSTEM TESTS OK. 2 L 7 2 4F RT A1NM 20081201 NM 2008 12 1 DL757081620 1 20081115 A 5320 146N54508 SUPPORT BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 1520 RBL 2.9 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 724164 CORROSION ON Z STRINGER SUPPORT BS 1520 RBL 2.9 O/B SIDE, OUT OF LIMITS, REMOVED AND REPLACED PART. 2 L 7 2 4F 4 F RT A2NM E24NE 20081201 2008 12 1 JGV2008F00008 4 20081104 A 2561 82122Z CARTRIDGE AIRCRUISERS LEAR 35 31A 5170531 CE LIFE VEST MISSING B JGVR K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 09 177JB L782068 161 DURING ROUTINE INSP OF NINE (9) LIFE VESTS FOUND MISSING CO2 CARTRIDGES ON ALL NINE (9) VESTS. ALL LIFE VESTS WERE RECE IVED IN SEALED, SEWN-SHUT BAGS WITH SIGNED MAINT RELEASE DOCUMENTS FROM PREVIOUS INSP ACCOMPANYING THEM. PREVIOUS INSPE CTION ACCOMPLISHED NOVEMBER 2003. CO2 CARTRIDGES ARE NORMALLY REMOVED FOR WEIGHT CHECK AND REINSTALLED AS PART OF ROUTI NE INSPECTION REQUIREMENTS. PROBABLE CAUSE FOR FAILURE TO RE-INSTALL IS LAPSE OF FOCUS ON DETAILS OF MAINT BEING PERFOR MED. (K) 2 L 7 2 4F RT A10CE 20081201 NM 2008 12 1 USAA2008112192099 1 20081114 A 5330 6545776 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 591US 23936 PHL - RON - MAJOR REPAIR, CRACK ON FUSELAGE SKIN FORWARD OF AFT CARGO DOOR BY EXTERIOR SERVICE LIGHT BS727D +10 INCHES, S22R TO S23R. REPAIRED FUSELAGE SKIN IAW B737 SRM 53-00-01. REPAIR COMPLETED CHANGED DISCREPANCY, ADDED CORRECTIVE ACT ION, PART NUMBER, SERIAL NUMBER, & STRINGER LOCATION. 2 L 7 2 4F RT A16WE 20081201 NM 2008 12 1 USAA2008112092098 1 20081105 A 5320 D5347112420000 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSLAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 804AW 1043 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON LATERAL SHEAR PLATE BETWEEN FR69 & FR70, S23L, Y1732. REPLACED LATERAL SHEAR PLATE BETWEEN FR69 & FR70, S23L, Y1732 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081201 CE 2008 12 1 SBAA200800003 1 20081105 A 2140 1H1014RX FLOW VALVE CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE MCAULY 3AF34C 3GFR34C703 GL ZONE 400 FAILED E SBAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 09 712FX 267 267 208B0435 PCE19325 993384 DURING TAKEOFF THE BLEED AIR HEAT CAME ON WITHOUT PILOT INPUT. PILOT ATTEMPTED TO TURN HEAT OFF WITH SYS SWITCH AND TEMP . CONTROL KNOB. NEITHER ACTION WORKED. COCKPIT WAS GETTING EXCESSIVELY HOT SO PILOT OPENED UP ALL AIR VENTS AND PULLED F IREWALL SHUTOFF VALVE FOR BLEED AIR HEAT. AFTER ACTUATING SHUTOFF VALVE POSSIBLE LIGHT SMOKE AND ODOR FROM A EXCESSIVELY WARM SYS WAS NOTED IN COCKPIT. PILOT DECLARED AN EMERGENCY AND RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. 1 H 7 1 3T 3 T A37CE E4EA 5 C P60GL 20081201 NM 2008 12 1 USAA2008112092093 1 20081119 A 3350 1012881 MOUNT AIRBUS A319 A319132 3930340 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 803AW 931 FLT 635 - RDU-PHX - EEL - LAST ROW AIRCRAFT LEFT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT SEAT MOUNT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081201 EU 2008 12 1 USAA2008112492106 1 20081122 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU CABIN NOT SEATED A USAA K NONE O OTHER NR NOT REPORTED 1 EA 19 662AW 1274 FLT 596 PHX-MCI - EEL - FLIGHT ATTENDANT REPORTED TO COCKPIT THAT EXIT SIGNS 2 LEFT AND 2 RIGHT WERE NOT ILLUMINATED. E MERGENCY EXIT LIGHT SWITCH IN ARMED POSITION. EXIT SIGNS DID ILLUMINATE IF SWITCH WAS PLACED IN THE ON POSITION. MAINT ENANCE RESEATED THE CONNECTOR ON THE EMERGENCY POWER SUPPLY UNIT, FIN 13WL, LEFT AFT. OPERATIONAL CHECK WAS NORMAL. 2 L 7 2 4F RT A28NM 20081201 EU 2008 12 1 USAA920082052 1 20081109 A 5347 SEAT TRACK AIRBUS 330 A330323 3940030 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AY 370 BFM C2 MAJOR REPAIR NR 6127115 CORROSION ON SEAT TRACK AT FR58 TO FR68, Y450. REPAIRED SEAT TRACK AT FR58 TO FR68, Y450 IAW A330 SRM 53-00-15 AND 51-42-11. 2 L 7 2 4F RT A46NM 20081201 NM 2008 12 1 USAA920082054 1 20081111 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 591US 23936 CLT MAJOR REPAIR NR 4370429, CRACKED FUSELAGE SKIN AT BS 727E + 18", S24R. REPAIRED FUSELAGE SKIN AT BS 727E + 18", S24 R IAW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 20081201 EU 2008 12 1 NWAA085013232 1 20081008 A 3350 EPSU AIRBUS 320 A320211 3930320 EU CABIN FAULTY A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 332NW 319 EMERGENCY EGRESS LIGHTING TEST FAILS, FAULTING EPSU EMER R. REPLACED EPSU 12WL, CHECKS OK. 2 L 7 2 4F RT A28NM 20081202 NM 2008 12 2 USAA2008112592124 1 20081125 A 5315 146T5141 FLOORBEAM BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 253AY 24894 BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM UPPER CHORD AT BS 1480, LBL 43 TO LBL 27. REPAIRED FLOORBEAM U PPER CHORD AT BS 1480, LBL 43 TO LBL 27 IAW B767 SRM 51-20-01 & 53-00-51. 2 L 7 2 4F RT A1NM 20081202 NM 2008 12 2 USAA2008112592125 1 20081121 A 5310 CREASE BEAM BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 253AY 24894 BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON CREASE BEAM AT BS 858, RBL 88, WL 200. REPLACED CREASE BEAM AT BS 858, R BL 88, WL 200 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081202 NM 2008 12 2 USAA2008112492110 1 20081112 A 5755 SKIN BOEING 737 7373G7 138447J NM SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW MA11032 24634 SAL - C17 - MAJOR REPAIR - EXISTING REPAIR DELAMINATED AT SPOILER NR 0 UPPER SURFACE WS 447.47 TO WS 499.93. REPAIRED S POILER NR 0 UPPER SURFACE WS 447.47 TO WS 499.93 IAW B737 SRM 51-70-10-2R. 2 L 7 2 4F RT A16WE 20081202 NM 2008 12 2 USAA2008112492111 1 20081123 A 5320 STRUCTURE BOEING 767 7672B7ER 1385107 NM NLG WW CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AY 25257 BFM - C3 - MAJOR REPAIR - CRACK ON VERTICAL CHORD AT LEFT NOSE WHEEL WELL BS 287, LBL 25, WL 173.5. REPAIRED VERTICAL C HORD AT LEFT NOSE WHEEL WELL BS 287, LBL 25, WL 173.5 IAW B767 SRM 51-70-12. 2 L 7 2 4F RT A1NM 20081202 2008 12 2 IXXA080033O 4 20081120 A 3422 1428302001 GYRO DOUG DC8 DC873F 302199F WP HSI FAILED A IXXA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 SW 11 605AL 99401 2840 46106 DURING CRUISE FROM KTOL TO KBFI, THE CAPTAINS ADI AND HSI FAILED. THE CREW DIVERTED TO KRFD AND LANDED WITHOUT INCIDENT . MAINTENANCE REPLACED THE FIBER OPTIC VG/DG GYRO. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SER VICE. 2 L 7 4 4F RT 4A25 20081202 2008 12 2 IXXA080034O 4 20081123 A 2370 6009580001 VIDEO MONITOR DOUG DC8 DC862F 3021972 WP CABIN BURNED OUT A IXXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 11 799AL 3141 45922 APPROXIMATELY 15 MINUTES AFTER TAKEOFF FROM KSUU, THE CREW DETECTED AN ELECTRICAL ODOR IN THE CABIN. THE CREW RETURNED TO KSUU AND LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED ELECTRICAL ODOR WAS COMING FROM THE FORWARD VIDEO MONITOR. T HE FORWARD VIDEO MONITOR WAS REMOVED TO PREVENT FURTHER ODOR. THE MONITOR WAS PLACED ON ORDER AND THE AIRCRAFT WAS RETU RNED TO SERVICE IAW DACO M/M 56-00-01. 2 L 7 4 4F 4A25 20081202 NM 2008 12 2 USAA2008112492118 1 20081121 A 5753 65464331279 FLAP BOEING 737 7374B7 138449C NM LT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 CLT - C1 - MAJOR REPAIR - LEFT FOREFLAP DELAMINATED ALONG TRAILING EDGE APPROX 85.5 INCHES FROM INBOARD END AND 25 INCHE S FROM INBOARD END. REPLACED LEFT FOREFLAP IAW B737 AMM 27-51-37. 2 L 7 2 4F RT A16WE 20081202 SO 2008 12 2 SIMA200832204 1 20081113 A 5320 14530628001 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 654AE 145437 DURING IMBV INSPECTION, FOUND RIGHT OMEGA BEAM CORRODED BY CROSSMEMBER AT FRAME 24-25. REPAIRED RIGHT OMEGA BEAM IAW SR M 53-00-10 FIGURE 203. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081202 SO 2008 12 2 GLBA200811261 1 20081116 A 2460 MS2536180 CIRCUIT BREAKER EMB 120 EMB120ER 3260203 SO ZONE 100 CONTAMINATED A GLBA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 NM 21 293UX 120293 ENROUTE, PILOTS REPORTED AN EMERGENCY BUSS OFF LIGHT ILLUMINATED IN FLIGHT. EMERGENCY ACTIONS WERE TAKEN. MAINT WAS DISP ATCHED TO THE ACFT AND SECURED A WIRE HARNESS IN THE OVERHEAD CIRCUIT BREAKER PANEL. MAINT CHECKED THE TORQUE OF THE RCC B AND FEED WIRING HARDWARE IN THE LT DC RELAY BOX AND PERFORMED FUNCTIONAL CHECKS OF THE AFFECTED SYS. OPS CHECKS WERE G OOD. THE ACFT WAS RAN, TAXIED, AND NO DEFECTS WERE NOTED. ALL IAW MM 24-51. AN OPS CHECK FLIGHT WAS PERFORMED AND THE OP S CHECK FLIGHT WAS SATISFACTORY. UPON ENTRY INTO A SCHEDULED MAINT CHECK MAINT REMOVED AND REPLACED THE EMERGENCY BUSS CIRCUIT BREAKER CB 0470 P/N MS25361-80 PRECAUTIONARY DUE TO EVIDENCE WHICH APPEARED TO BE A POSSIBLE COFFEE SPILL PREVIO 2 L 7 2 4T RT A31SO 20081202 2008 12 2 Y9PAN930LS82208 4 20080822 A 3452 6226523207 TRANSPONDER GULSTM G1159 G1159 3953505 SO RROYCE SPEY SPEY5118 54523 EU ATC INTERMITTENT E Y9PA O OTHER N FALSE WARNING CR CRUISE 1 SW 09 930LS 1176 133 8576 MODE C TRANSPONDERS READ 500 FT HIGH 99 PERCENT OF THE TIME (IN CRUISE). TROUBLESHOOTING IN PROCESS, WILL AMEND FORM WH EN DETERMINATION OF CAUSE 8/22/08. RAN PITOT/STATIC SYS TO 45,000 FT AND CHECKED OUT PUT OF TRANSPONDER SYS WITH ATC60 1 TEST SET AND INDICATED NORMAL, REMOVED AND REPLACED CTL92 CONTROL GROUND CHECKS GOOD, PERFORMED OPERATIONAL TEST FLIGH T AND ATC REPORTS NO ABNORMALITIES. 2 L 7 2 4F 4 F RT A12EA E2EU 20081202 SO 2008 12 2 FFSA200800007 1 20081118 A 7810 LW16697 EXHAUST PIPE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2B NE HARTZL HCE3Y HCE3YR2A GL LT ENGINE CRACKED E FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 137CS 1878 1878 318152137 RL27361A DURING SCHEDULED INSP MECHANIC NOTICED EXHAUST STAINING AROUND THE AFT SIDE OF THE V-BAND CLAMP AT THE OTBD SIDE OF THE TURBOCHARGER TRANSITION OF THE LT ENGINE. REMOVAL OF THE CLAMP REVEALED A 2.25 INCH CRACK IN THE RADIUS OF THE STACK FLA NGE ALONG THE AFT SIDE. NO EVIDENCE OF ANY DAMAGE TO ACFT OR ENGINE COMPONENTS RESULTING FROM CRACK. 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 20081202 CE 2008 12 2 DJFA2008083 1 20081122 A 2612 473054 FIRE DETECTOR RAYTHN DH125 HAWKER800XP 7150012 CE CARGO BAY FAILED E DJFA O OTHER N FALSE WARNING CR CRUISE 1 EA 23 805LX 258374 IN CRUISE CREW REPORTED INTERMITTENT BAGGAGE FIRE DETECTION LIGHT ILLUMINATION. NO EVIDENCE OF SMOKE OR FUMES. MAINT C OULD NOT DUPLICATE THE DISCREPANCY. THE BAGGAGE FIRE DETECTOR WAS REPLACE FOR PRECAUTIONARY PURPOSES. 2 L 7 2 4F RT A3EU 20081202 CE 2008 12 2 YADA111708 1 20081110 A 5330 SKIN BEECH 1900 1900C 1154161 CE BS 363-378 CORRODED E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 111AX UC81 DURING INSP, THE MECHANIC NOTICED THE BELLY BEACON FRONT FASTENER WAS LOOSE. UPON INSP, THE MECHANIC DETERMINED THAT TH ERE WAS CORROSION UNDER THE BEACON MOUNT. THE BELLY SKIN REQUIRED A PATCH REPAIR TO REMOVE THE DAMAGED AREA. 2 L 7 2 4T RT A24CE 20081202 NM 2008 12 2 DXTA2008112403365 1 20081121 A 3260 WARNING LIGHT GULSTM 200 200 4500308 NM NLG ILLUMINATED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 718QS 136 NOSEWHEEL UNSAFE INDICATED AFTER RETRACTION. 2 L 7 2 4F RT A53NM 20081202 NM 2008 12 2 DXTA2008112403368 1 20081123 A 3230 LANDING GEAR GULSTM 200 200 4500308 NM RT MLG INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 728QS 116 ON CLIMBOUT TOWER REPORTED RT MAIN GEAR NOT RETRACTED. 2 L 7 2 4F RT A53NM 20081202 NM 2008 12 2 UALA2008111305483 1 20080826 A 3222 STRUT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LANDING GEAR LOW A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 840UA 1522 NOSE GEAR VIBRATION. FLIGHT DIVERTED. SERVICED ALL THREE LANDING GEAR STRUTS, SHIMMED NLG LINKS, CHANGED NLG TIRES. F OUND LT MLG SHIMMEY DAMPNER WORN AND TORQUE LINKS AS WELL. REPLACED SAME. 2 L 7 2 4F 4 F RT A28NM E40NE 2008022900024 20080229 00024 EA 2008 2 29 TRAX200800277 1 20080217 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 889AS 7538 FS 319 FRAME IS CORRODED AT BL 0. 2 L 7 2 4F RT A21EA 2008022900027 20080229 00027 EA 2008 2 29 TRAX200800280 1 20080219 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 874AS 7551 FLAP FAIL AT ZERO ON APPROACH. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. 2 L 7 2 4F RT A21EA 2008022900067 20080229 00067 NM 2008 2 29 08FDEA00626 1 20080227 A 5320 65561695 THRESHOLD BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 SEVERAL CRACKS AND DENTS IN THRESHOLD PLATE, FWD LOWER CARGO COMPT. THRESHOLD PLATED REPAIRED ON SHOP N/R N00123. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008022900088 20080229 00088 2008 2 29 GTIA0800009 4 20080208 A 2565 030665309 SLIDE AIRBUS A319 A319132 3930340 NM R2 DOOR UNWANTED DEPLOY A GTIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 501NK 2424 PASSENGER DOOR R2 SLIDE PACK CAME APART DURING REMOVAL. REPLACED R2 DOOR SLIDE PACK. 2 L 7 2 4F RT A28NM 2008022900102 20080229 00102 NM 2008 2 29 HALA0800333 1 20080219 A 5312 BULKHEAD BOEING 717 717200 1383700 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 2 CORROSION, RADOME STA 37 PRESSURE BULKHEAD LT SIDE O/B INTERCOSTAL (STIFFENER). REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022900113 20080229 00113 2008 2 29 QXEA200800206 4 20080218 A 3416 4016341905 ALTIMETER DHAV DHC8 DHC8202 2809007 NM NR 1 MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 355PH 500 SEA - FLIGHT 2027, RETURNED TO THE FIELD FOR THE CAPTAIN'S ALTIMETER FLAGGING AT 420 FEET. MAINTENANCE REPLACED THE NR 1 ALTIMETER. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008022900124 20080229 00124 EA 2008 2 29 TRAX200800299 1 20080221 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 858AS 7417 AAR - FS 484 CLIP CRACKED I/B RBL 27. 2 L 7 2 4F RT A21EA 2008022900130 20080229 00130 EA 2008 2 29 SWIA200819234 1 20080213 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DAMAGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 925SW 7682 FLT 6456 - EMERGENCY LIGHT ADJACENT TO CABIN DOOR IS INOP. REPAIRED WIRE AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008022900155 20080229 00155 NM 2008 2 29 GTIA0800021 1 20080109 A 5315 FLOORBEAM AIRBUS A321 A321231 3940032 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 FLOORBEAM CORRODED AT Y-189 FRAME 20. FABRICATED AND INSTALLED NEW PART IAW SRM 53-00-14. 2 L 7 2 4F RT A28NM 2008022900157 20080229 00157 NM 2008 2 29 GTIA0800019 1 20080109 A 5320 FLOOR SUPPORT AIRBUS A321 A321231 3940032 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 FOUND FLOORBEAM AT Y-468 AT FRAME 67.5 THRU 69 HAS CORROSION. 2 L 7 2 4F RT A28NM 2008022900169 20080229 00169 NM 2008 2 29 HALA0800339 1 20080219 A 5414 SKIN BOEING 717 717200 1383700 NM LT NACELLE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION AND PAINT PEELING ON LT ENG UPPER COWL EXTERIOR SURFACE. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022900188 20080229 00188 NM 2008 2 29 MASA200800146 1 20080217 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 3 DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 989HA 427 REPAIR TO RIGHT NR 3 FLAP TRACK. 2 H 7 2 4T RT A13NM 2008022900191 20080229 00191 NM 2008 2 29 MASA200800148 1 20080218 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 447YV 11907 447 ASH FLT 7097 DEN-ASE. PASSENGER DOOR EMERGENCY LIGHT INOP, EMERGENCY FLOOD LIGHT NR 2 INOP & GALLEY EMERGENCY LIGHT INO P. MX CHANGED NR 2 POWER SUPPLY. 2 H 7 2 4T RT A13NM 2008022900201 20080229 00201 EA 2008 2 29 TRAX200800308 1 20080222 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 856AS 7404 WHEN SELECTING FLAPS FROM 0 DEG TO 8 DEG ON APPROACH, FLAPS FAILED AT 2 DEG. FLAPS FAIL MESSAGE. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2008022900205 20080229 00205 NM 2008 2 29 HALA0800348 1 20080221 A 5344 HINGE BOEING 717 717200 1383700 NM DOOR DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 CONTACT DAMAGE ON MED DOOR HINGE, FROM FUSELAGE FRAME.//REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008030300002 20080303 00002 NM 2008 3 3 08FDEA00645 1 20080228 A 2460 50086003 CIRCUIT BREAKER BOEING 727 727200 138407E NM FAILED A FDEA E ENGINE SHUTDOWN B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 243FE 12440 12440 21480 WITH ENGINE NR 2 RUNNING, SMOKE ENTERED COCKPIT FROM UNKNOWN SOURCE. GOT INTERMITTENT NR 3 MAIN CARGO BAY SMOKE ALARM & LIGHT. ALARM & LIGHT OCCURED 2 TIMES FOR 1 SEC. SHUTDOWN NR 2 ENGINE & POWERED ACFT WITH APU. SMOKE DISPERSED. ON APU & EXT POWER, NR 2 BUSS IS NOT POWERED. ANNUNCIATOR PANEL HAD UNDEREXCITATION LIGHT NR 2 SYSTEM. R & R NR 2 VOLTAGE REGUL ATOR. SMOKE CAUSED DUE TO LOST POWER TO BUSS TIE BREAKER TO RT PACK. R & R GCU . R & R GENERATOR BREAKER (C814) & BUSS TIE BREAKER. RAN ENGS AND TAXIED A/C NO SMOKE NOTED. 2 L 7 3 4F RT A3WE 2008030300007 20080303 00007 2008 3 3 AALA200800360 4 20080220 A 2565 60B1000316 RESERVOIR BOEING 757 757223 1384957 NM R1 DOOR SLIDE INOPERATIVE A AALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 626AA 24584 SAL - RIGHT NUMBER ONE DOOR SLIDE DEPLOYED BY CABIN SERVICE. SLIDE REPORTEDLY TOOK 25 MINUTES TO INFLATE. REPLACED RIG HT NUMBER ONE DOOR SLIDE AND RESERVOIR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008030300041 20080303 00041 2008 3 3 2008UALA00810 4 20080212 A 2565 60592101 BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LT OWING SLIDE READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 817UA 873 FA SIDS PANEL AT 1L CAUTION ILLUMINATED. CANT RESET. FOUND LT OVERWING BOTTLE PRESSURE LOW. UNKNOWN LEAK AT BOTTLE. REPLACED THE OVERWING SLIDE BOTTLE, PRESSURE CHECK OK AND LIGHT WENT OUT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030300042 20080303 00042 EU 2008 3 3 2008UALA00811 1 20080213 A 3350 321431 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 495UA 1842 LT EMERGENCY EXIT LIGHT BATTERY SHOW A FAULT AFTER EMERGENCY LIGHT TEST ON CIDS PANEL. FAULTY BATTERY. REPLACED LT EME RGENCY EXIT LIGHT BATTERY. OPS CHECKS ARE NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030400007 20080304 00007 WP 2008 3 4 IXXA08SMN022S 1 20080119 A 5730 SKIN DOUG DC8 DC862F 3021972 WP RT WING DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING DENTED AT UPPER LEADING EDGE AT STA XFS 7.5000. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK, NO CORROSION FOUND. PERFORMED MEASUREMENT DIAMETER FOUND WITHIN ALLOWABLE LIMITS APPLIED PRO-SEAL 735 IAW DC8 SRM 57-2-1 FIGURE 2, AND DC8 SRM 51-1-9 PAGE 13 FIGURE 13. 2 L 7 4 4F 4A25 2008030400009 20080304 00009 WP 2008 3 4 IXXA08SMN018S 1 20080115 A 5310 DOOR FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE NOSE SECTION CRACKED AT PNEUMATIC AIR INLET DOOR FRAME INNER REVERSE. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE AREA. FABRICATED FILLER AND DOUBLER. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PARTS. INSTALLED NEW FASTENERS AN REPAIR PARTS IAW DC8 SRM 51-1-21, DC8 SRM 53-2-0 FIGURE 1 B, AND DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 2008030400010 20080304 00010 WP 2008 3 4 NWAA080609872 1 20080120 A 3397 WIRE DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS LOOSE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 781NC 48121 THE EMERGENCY LIGHT CIRCUIT BREAKER WAS FOUND TRIPPED DURING A LINE CHECK AND IT WOULD NOT RESET. MAINTENANCE FOUND THE TERMINALS ENDS ON THE WIRES TO SWITCH S1-387 OF THE FORWARD FLIGHT ATTENDANT EMERGENCY LIGHT CONTROL PANEL WERE NOT SEC URED. THE SWITCH AND THE TERMINAL ENDS WERE ALL REPLACED AS WAS THE POWER SUPPLY AT 1L AFTER IT WAS FOUND SHORTED. SYS TEM FUNCTIONALLY CHECKS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008030400033 20080304 00033 NM 2008 3 4 DHL2008749002 1 20080112 A 5340 STRINGER CLIP BOEING 727 727223 1384074 NM BS 740 S26L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 FORWARD CARGO COMPARTMENT STRINGER CLIP CORRODED AT STRINGER 26L BS 740. REMOVED STRINGER CLIP IAW SRM 51-30-2. CORROS ION OUT OF LIMITS IAW SRM 53-10-1 FIGURE 1. CLEANED LOWER AREA IAW MM 12-40-00 NO CORROSION NOTED. FABRICATED NEW PART IAW SRM 53-10-2 FIGURE 9, 51-20-01, AND 51-30-5. ALODINED AND PRIMED PART IAW SRM 51-10-2. INSTALLED IAW SRM 51-40-4 FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 2008030400040 20080304 00040 NM 2008 3 4 DHL2008749010 1 20080131 A 5344 HINGE BOEING 727 7272J0 138407E NM BS 640 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 MAIN CARGO DOOR UPPER AFT MOST HINGE IS GOUGED IN CENTER OF HINGE BS 640. REMOVED DAMAGE IAW AEI MM CHAPTER 52. LOCATE D AND DRILLED IAW AEI MM CHAPTER 52 FIG 5201B AND SRM 51-30-5. PARTS AND AREA TREATED AND PRIMED IAW SRM 51-10-2 FIGURE 1. INSTALLED IAW MM CHAPTER 52 FIGURE 5201C. OPS CHECK MCD, NO DEFECTS NOTED IAW MM CHAPTER 52. 2 L 7 3 4F RT A3WE 2008030400041 20080304 00041 NM 2008 3 4 DHL2008749011 1 20080202 A 5410 SKIN BOEING 727 7272J0 138407E NM BS 1089 MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 749DH 22013 NR 2 ENGINE INLET COWL LEADING EDGE PREVIOUS REPAIR AT BS 1089 WL 314 AT 9 O'CLOCK POSITION DOES NOT CONFORM TO AERODYNA MIC SMOOTHNESS REQUIRED FOR CRITICAL AREAS. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER IAW SRM 54-30-3 FIGURE 3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED IAW SRM 54-30-3 FIGURE 2 AND 51-30-2. 2 L 7 3 4F RT A3WE 2008030400042 20080304 00042 NM 2008 3 4 DHL2008749012 1 20080204 A 5313 STRINGER BOEING 727 7272J0 138407E NM BS 950-1010 S29L CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 AFT PIT STRINGER 29L CRACKED AT SPLICE AFT OF BS 950. REMOVED AFT PIT STRINGER 29L, LOCATED AND DRILLED NEW STRINGER. INSTALLED NEW STRINGER IAW SB 727-53-0179. 2 L 7 3 4F RT A3WE 2008030400048 20080304 00048 NM 2008 3 4 AALA200800297 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 38C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 38C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008030400049 20080304 00049 NM 2008 3 4 AALA200800302 1 20080211 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AN 25451 MIA - EMERGENCY EXIT LIGHT AT RIGHT SIDE AFT CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT RIGHT SIDE AF T CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008030400050 20080304 00050 NM 2008 3 4 AALA200800289 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 26G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008030400052 20080304 00052 NM 2008 3 4 DL764080187 1 20080211 A 3233 273T11512 ACTUATOR BOEING 767 767432ER 1385134 NM PWA JT8 JT8D219 52053 NE MLG LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 830MH EFS0057 29701 725736 CENTER HYDRAULIC QUANTITY DROPPED AT 28 PERCENT IN FLIGHT FL 300. FOUND RT MLG RETRACT ACTUATOR LEAKING. REPLACED ACT PER M/M LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E9NE 2008030400054 20080304 00054 NM 2008 3 4 DL764080270 1 20080223 A 7700 SENSOR BOEING 767 767432ER 1385134 NM ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 841MH 29714 ON TAXI TO RUNWAY, THE FOLLOWING LIGHTS REMAINED ON AFTER ENG START, LEFT CTR FUEL PUMP/L ENG BLEED VALVE/LEFT EFIS CONT ROL. T/S PER FIM 77-12-0, EXAMINED CIRCUIT BETWEEN N2 SENSOR AND DCUS FOUND OK. VERIFIED RESISTANCE OF N2 SENSOR OK CL EANED AND REINSTALLED ELEC CONNECTORS RUN BOTH ENGS BY FLT CREW ALL INDS NORMAL. A/C OK FOR SERVICE, L N2 ANALOG AND L N2 SPEED CARD WAS ON STS PAGE. 2 L 7 2 4F RT A1NM 2008030400055 20080304 00055 NM 2008 3 4 DL76L080188 1 20080212 A 3397 WIRE BOEING 767 767332 1382001 NM EMERGENCY LIGHTS BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 180DN 25985 EPATH LIGHT INOP AT SEAT 16FG. REPAIRED BROKEN WIRE AT WALL CONNECTOR, CKS GOOD. 2 L 7 2 4F RT A1NM 2008030400056 20080304 00056 2008 3 4 DL764080189 4 20080212 A 2310 UNKNOWN BOEING 767 767432ER 1385134 NM VHF SYSTEM MALFUNCTIONED A DALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SO 27 825MH 29696 LEFT VHF PANEL STARTED DISPLAYING FAIL INTERMITTENTLY THEN CONTINUOUSLY. RESET CB, FAIL WENT AWAY BUT COULD NOT TRANSMI T OR RECEIVE ON VHF OR STACOM. RT VHF AND STACOM WAS ABLE TO RECEIVE BUT NOT TRANSMIT. AFTER 10 MIN, RT VHF COULD TRAN SMIT ON A HANDFULL OF FREQUENCIES ACARS COULD RECEIVE, BUT NOT TRANSMIT. ACARS AND ATC INTERMITTENT. OPN OF ALL RADIOS NORMAL ON GROUND IN GRU. SWAPPED LT AND CENTER TRANSCEIVER AND LT AND CENTER RTPS AS PRE-CAUTION. CLEANED LT/RT VHF A NTENNA CONNECTORS. PERFORMED LIGHTNING STRIKE AND OVWT LDG INSPECTION ATC/VHF/SATOM/ACARS ALL TESTS NORMAL. 2 L 7 2 4F RT A1NM 2008030400065 20080304 00065 NM 2008 3 4 F3LA200800074 1 20080223 A 5321 D5376520800600 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 949FR 5553 10 2857 DURING C1 C CHECK, INSPECTION REPORTED AFT CARGO PIT FLOOR PANEL 151ZG WAS DAMAGED BEYOND REPAIRABLE LIMITS. MAINTENANC E REMOVED AND REPLACED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-42-14-400-001. FOLLOWING THE REPLA CEMENT OF THE FLOOR PANEL, IT WAS INSPECTED AND FOUND ACCEPTABLE. CORRECTED C CHECK FROM C5 TO C1 ON 02/27/08/END/. 2 L 7 2 4F 4 F RT A28NM 2008030400071 20080304 00071 EU 2008 3 4 2008UALA00852 1 20080215 A 3250 715TS06Y11 TILLER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG STEERING FAULTY A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 415UA 475 A/C DOES NOT STEER WITH RUDDER PEDAL INPUT. FOUND SHORT TO GRD ON FO'S NWS PEDAL DISCONNECT SWITCH. REPLACED FO'S NWS TILLER (2GC), OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030400072 20080304 00072 NM 2008 3 4 2008UALA00853 1 20080217 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN SMOKE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 547UA 25368 RTFL WITH SMOKE IN THE CABIN. ODOR EMINATED FROM 1ST CLASS TOWARD BACK, TURNING VIDEO EQUIP OFF REDUCED THE ODOR FOR A WHILE, THEN RETURNED. LIGHT HAZE IN CABIN EVIDENT. RAN BOTH LT AND RT PACKS INDIVIDUALY NO SMOKE OR ODOR NOTICED. RAN E NTIRE VIDEO SYSTEM AND INSPECTED LIGHT BALLEST IN FWD CABIN NO SMOKE OR ODORS NOTICED. RAN ALL FWD AND MID GALLEY SYSTEM S NO DESCRIPANCIES. NEVER REPEATED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030400074 20080304 00074 NM 2008 3 4 2008UALA00855 1 20080216 A 2913 PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE LOW PRESSURE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 517UA 24861 RTFL DUE TO LEFT ENGINE HYD PUMP LOW PRESSURE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030400082 20080304 00082 EA 2008 3 4 SWIA200819222 1 20080211 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCONNECTED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 912SW 7595 REAR EMERGENCY LIGHTING STRIP IS INOP, FLIGHT NR 6046. SECURED AFT EMERGENCY LIGHT CONNECTORS AS REQUIRED. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2008030400083 20080304 00083 EA 2008 3 4 SWIA200819223 1 20080209 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN SMOKE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 454SW 7749 FLT 3790, AFTER TAKEOFF WITH BLEEDS OPEN CABIN FILLED WITH SMOKE. RAN BOTH ENGINES AT TAKEOFF POWER AND WITH APU ONLY. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008030400084 20080304 00084 EA 2008 3 4 SWIA200819224 1 20080213 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 956SW 7825 PASSENGER DOOR HANDLE WAS BROKEN OFF, FLIGHT NR 6607. REPLACED OUTER PAX DOOR HANDLE IAW CRJ 200 52-11-03. 2 L 7 2 4F RT A21EA 2008030400093 20080304 00093 NM 2008 3 4 HALA0800260 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1353 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1353, AREA HAS BEEN REWORKED BEFORE. SEAT TRACK REPLACED PE R SRM. 2 L 7 2 4F RT A1NM 2008030400098 20080304 00098 NM 2008 3 4 HALA0800234 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1003 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT LBL 11, STA 1003, MAX DEPTH OF BLEND OUT WAS 0.015". BLENDED IAW SRM 51-10 -02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008030400108 20080304 00108 NM 2008 3 4 HALA0800180 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1186 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION AT RBL 54.75, SEAT TRACKS, STA 1186, BASE OF TRACKS. CORROSION REMOVED IAW SRM 51-10-02, REV 76 AND S RM 53-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030400109 20080304 00109 NM 2008 3 4 HALA0800181 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION AT RBL 54.75, SEAT TRACKS AT STA 1197+22, BASE OF TRACKS. CORROSION REMOVED PER SRM 51-10-02, REV 76 AND SRM 53-00-52/101, REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030400111 20080304 00111 NM 2008 3 4 HALA0800183 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION AT RBL 54.75, SEAT TRACKS AT STA 1197+63, BASE OF TRACK. CORROSION REMOVED PER SRM 51-10-02, REV 76 A ND SRM 53-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030400124 20080304 00124 NM 2008 3 4 2008UALA00906 1 20080215 A 4900 018550000 BATTERY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE APU FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 672UA 30027 APU DOES NOT START. SHUTS DOWN AT AROUND 18 PERCENT. REPLACED APU BATTERY AND CHARGER. APU STARTS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030400127 20080304 00127 NM 2008 3 4 DLM88080272 1 20080213 A 2750 VANE DOUG MD88 MD88 3023688 NM LT WING WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 DURING HMV, FOUND WEAR ON THE SURFACE OF THE LT INBOARD FLAP INBOARD GUIDE VANE. A PERMANENT REPAIR WAS PERFORMED IAW M D-80 SRM 57-03D FIG 9A PARAGRAPH 8A. 2 L 7 2 4F RT A6WE 2008030400128 20080304 00128 NM 2008 3 4 DLM88080273 1 20080213 A 5753 VANE DOUG MD88 MD88 3023688 NM TE FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 DURING HMV, REPORTED A DELAMINATION ON UPPER SKIN OF INBOARD GUIDE VANE AT LEFT OUTBOARD FLAP. A PERMANENT REPAIR WAS P ERFORMED IAW MD-80 SRM 57-03D PARAGRAPH 8A FIG 9A AND SRM 51-70-2D PARAGRAPH 6A, 6C, 10B, 10D AND 10E. 2 L 7 2 4F RT A6WE 2008030400131 20080304 00131 NM 2008 3 4 HALA0800189 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1210 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION RBL 54.75, SEAT TRACKS, STA 1210, BASE OF TRACKS. CORROSION REMOVED PER SRM 51-10-02 REV 76 AND SRM 5 3-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030400138 20080304 00138 NE 2008 3 4 DL76G080222 2 20080217 A 7250 TURBINE WHEEL BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 ENGINE DAMAGED A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 1613B 46022 32776 704234 ON CLIMB-OUT, RT ENGINE EGT RAN AWAY AND HAD TO RETARD THROTTLE 2 KNOB WIDTH TO MAINTAIN EGT UNDER REDLINE. MTC IN PROG RESS. PERFORMED BORESCOPE OF HPC/HPT. FOUND MINOR DAMAGE ON THE 5TH AND 13TH STAGE AND IS WITHIN BLEND REPAIRABLE LIMI TS PER AMM 72-00-00-206-167-H00. ENGINE IS WITHIN OPERATION LIMITS AND GOOD FOR 10 FLT CYCLES. 2 L 7 2 4F 4 F RT A1NM E13NE 2008030400140 20080304 00140 EU 2008 3 4 TRBA2007019 1 20080211 A 6120 30048000018 CONTROL UNIT AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RT ENGINE MALFUNCTIONED A TRBA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 29 308AE 309 NR 2 ENGINE TQ WENT DOWN TO 0 PERCENT, NP TO 0 PERCENT AND THE ENGINE SHUT DOWN BY ITSELF. REMOVED AND REPLACED MULTI-F UNCTION COMPUTER (MFC) IAW JIC NR 31-48-81. REMOVED AND REPLACED TORQUE SIGNAL CONTROL UNIT(AFU) IAW JIC NR 77-13-62. PERFORMED GROUND POWER RUN-UP IAW W/C 055007-CS-20000-001. 2 H 7 2 4T 4 T RT A53EU E20NE 2008030400141 20080304 00141 NM 2008 3 4 HALA0800216 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1043 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS, AT LBL 88.5 STA 1043, MAX DEPTH BLENDED WAS 0.028". BLENDED IAW SRM 51-10-02 . ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008030400142 20080304 00142 NM 2008 3 4 DLM90080224 1 20080217 A 3230 CONTROL VALVE DOUG MD90 MD9030 3023690 NM MLG ICED A DALA O OTHER J WARNING INDICATION LD LANDING 1 SO 27 906DA 53386 WHEN ATTEMPTING TO LOWER THE LANDING GEAR FOR LANDING "LANDING GEAR HANDLE JAMMED UP." INSPECTED GEAR WELL AREA, FOUND ICE ON CABLES FOR LANDING GEAR CONTROL VALVE. FOUND RT AUTODRAIN VALVE AND TUBE PLUGGED. ALSO FOUND ALL FOUR EMERGENCY EXITS OVERWING DOOR SEALS ON POOR CONDITION AND CABIN FLOOR AREA WAS WET. REPLACED EMERGENCY DOOR SEAL REF ITEMS 004, 005, 006, 007, 008, 009, 016. PERFORMED GEAR SWING AFTER JACKING A/C. NO FURTHER TROUBLES FOUND. 2 L 7 2 4F RT A6WE 2008030400144 20080304 00144 NM 2008 3 4 HALA0800191 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1275 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION RBL 54.75, SEAT TRACK AT STA 1275, BASE OF TRACKS. CORROSION REMOVED PER SRM 51-10-02 REV 76 AND SRM 53-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030400145 20080304 00145 NM 2008 3 4 2008UALA00872 1 20080217 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 270-360 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 50863 24641 CREASE BEAM AT FWD GALLEY SERVICE DOOR FROM STATION 270 T0 360 IS CORRODED. SUSPECT MOISTURE CONTAMINATION. REPLACED CO RRODED BEAM WITH NEW CREASE BEAM. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030400158 20080304 00158 SO 2008 3 4 SIMA200805104 1 20080219 A 3350 276005 FUSE EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHTS BLOWN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 814AE 145541 ON FLIGHT 3900, CREW REPORTED EMERGENCY LIGHT INOP AT ROW 11C. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EME RGENCY BATTERY POWER SUPPLY FUSE IAW CMM 25-60-03. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008030400166 20080304 00166 SO 2008 3 4 SIMA200805102 1 20080219 A 5315 14521700003 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AE 145101 DURING MBV INSPECTION, FOUND LT OMEGA BEAM CORRODED AT FR 20 AT CARBON CROSS MEMBER AREA. INSTALLED NEW REPAIR DOUBLERS FROM PREVIOUS REPAIR IAW SRM 53-00-12. A/C WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008030400173 20080304 00173 NM 2008 3 4 HALA0800105 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1023 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45 SEAT TRACKS, AT RBL 11 AT STA 1023. CORROSION REMOVED,CONFIRMED BY 10X MAGNIFICATION IAW S RM 51-10-02, REV 75, BLENDED WITHIN LIMITS, IAW SRM 53-00-52/101 REV 76. 2 L 7 2 4F RT A1NM 2008030400174 20080304 00174 NM 2008 3 4 HALA0800106 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1045 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45 SEAT TRACKS, AT RBL 11, STA 1045. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SR M 51-10-02, REV 75, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101, REV 76. 2 L 7 2 4F RT A1NM 2008030400175 20080304 00175 NM 2008 3 4 HALA0800116 1 20080109 A 5300 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1065 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45 SEAT TRACK AT LBL 11, HAS DAMAGE TO SEAT TRACK CROWN AT STA 1065. CORROSION REMOVED, CONFI RMED BY 10X MAGNIFICATION, IAW SRM 51-10-02, REV 76. BLENDED WITHIN LIMITS, IAW SRM 53-00-52/101, REV 75. 2 L 7 2 4F RT A1NM 2008030400182 20080304 00182 NM 2008 3 4 HALA0800125 1 20080108 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 999 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 2 CORROSION SECTION 45 AT LBL 88.5, STA 999. SEAT TRACK REPLACED. 2 L 7 2 4F RT A1NM 2008030400183 20080304 00183 NM 2008 3 4 2008UALA00914 1 20080218 A 5210 STRUCTURE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L5 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 194UA 26892 FOUND DAMAGE TO DR 5L LWR FWD EDGE DURING WALKAROUND. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL DOUBLER & FI LLER R EPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030400184 20080304 00184 NE 2008 3 4 2008UALA00915 2 20080215 A 7261 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 LEAKING A UALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 539UA 25223 STRONG ODOR ON CLIMB-OUT FROM PACKS. ODOR HAS OIL ODOR IN COCKPIT. FOUND NR 1 ENGINE OIL LEAK INTO BLEED SYSTEM. ENGI NE CHANGE, PERFORMED PACK BURN OUT. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030400187 20080304 00187 NM 2008 3 4 HALA0800109 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 806 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45, SEAT TRACK AT LBL 11 HAS DAMAGE TO SEAT TRACK CROWN AT STA 806. CORROSION REMOVED, CONFIR MED BY 10X MAGNIFICATION IAW SRM 51-10-02 REV 76, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101 REV 75. 2 L 7 2 4F RT A1NM 2008030400191 20080304 00191 NM 2008 3 4 F3LA200800052 1 20080210 A 5320 D5367227420000 SILL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 902FR 5564 1515 DURING C7 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE SIDE WALL PROFILE AND SUPPORT STRINGER, LOCATED IN THE AFT CARGO PIT, LEFT SIDE AT FRAME 58A. MAINTENANCE BLENDED THE CORRODED STRINGER AND REMOVED AND REPLACED THE CORRODED SILL PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE INSTALLATION, THE WORK WAS INSP ECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008030400192 20080304 00192 NM 2008 3 4 2008UALA00874 1 20080217 A 5340 ATTACH ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 50863 24641 STRINGER 11R INTERCOSTAL ATTACH ANGLE IS CRACKED BS 294. REPLACED CRACKED ANGLE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030400193 20080304 00193 NM 2008 3 4 2008UALA00875 1 20080217 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S13L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 50863 24641 FOUND SHEAR TIE IS CRACKED BELOW STR 13L AT BS 360. REPLACED CRACKED SHEAR TIE WITH NEW PART. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030400201 20080304 00201 NM 2008 3 4 08FDEA00580 1 20080223 A 5311 651593320 FRAME BOEING 727 727227 1384078 NM BS 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 FRAME SHEAR TIE AT FS 600 LBL 12 HAS MISDRILLED HOLES FROM PREVIOUS WORKMANSHIP REMOVED DAMAGED SHEARTIE REF SRM 53-10-4 . FABRICATED NEW ANGLE REF SRM 53-10-4, TOP COAT ANGLE REF SRM 51-10-2 MM 51-20-151-7. INSTALLED ANGLE TIE REF SRM 53- 10-4 FIG 15. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008022900128 20080229 00128 EA 2008 2 29 TRAX200800300 1 20080221 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 858AS 7417 AAR - FS 484 CLIP CRACKED I/B LBL 27. 2 L 7 2 4F RT A21EA 2008022900143 20080229 00143 SO 2008 2 29 SWIA200819254 1 20080216 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 216SW 120285 SIGNS OF CORROSION FOUND ON FRAME 21. REPAIRED IAW IC2008-120/01433, AND IAW 51-40-02. 2 L 7 2 4T RT A31SO 2008022900172 20080229 00172 NM 2008 2 29 MALA080029 1 20080220 A 2741 CONTROL UNIT BOMBDR CL600 CL6002D15 NM STAB TRIM INOPERATIVE A MALA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 GL 15 613XJ 7965 STAB TRIM CAUTION CAME ON AT FL340. AS WE DESCENDED, AP TRIM FAILED. EMERGENCY CHECKLIST TO RESET DID NOT WORK. CREW DECLARED AN EMERGENCY. STAB TRIM WAS INOP. FLAPS 20 DEGREES LANDING TRIM AT 3.2. PERFORMED HORIZONTAL STAB ADJUSTMENT /TEST. FUNCTIONAL TEST OF HSTCU PER AMM 27-41-00, ALL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2008022900184 20080229 00184 EA 2008 2 29 MASA200800141 1 20080217 A 5240 HANDLE CNDAIR CL600 CL6002D24 1390016 EA SERVICE DOOR OUT OF ADJUST A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 942LR 15042 ASH FLT 2884 PHX-IAH, SERVICE DOOR OUTER HANDLE ISN'T FLUSHED WHEN CLOSED. ADJUSTED HANDLE. 2 L 7 2 4F RT A21EA 2008022900197 20080229 00197 EA 2008 2 29 MASA200800154 1 20080219 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17358 7358 ASH FLT 2741 PHX - AIRCRAFT EMERGENCY FLOOR PATH LIGHTING AFT SECTION INOP. RESECURED CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008022900203 20080229 00203 EA 2008 2 29 TRAX200800109 1 20080117 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 844AS 7317 AAR - O/B CLIP AT FS 280 RBL 9 CRACKED. REMOVED CRACKED RBL 9 O/B FS 280 CLIP. REF FORM 412 FOR FABRICATION OF SERVICE ABLE CLIP FOR RBL 9 O/B AT FS 280. REF REO 601R-53-11-171 FOR MATERIAL TYPE. INSTALLED SERVICEABLE CLIP IAW CRJ200 SR M 51-42-21. SUPPLEMENTAL SDR CLOSED 2/13/08. 2 L 7 2 4F RT A21EA 2008030500019 20080305 00019 NM 2008 3 5 QXEA200800170 1 20080130 A 5340 STRINGER CLIP DHAV DHC8 DHC8202 2809007 NM BS 387 S23R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - FOUND CORROSION ON STRINGER CLIP, STRINGER 23R AT FRAME 387 AFT SIDE. REMOVED AND INSTALLED NEW STRIN GER CLIP IAW DHC8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008030500038 20080305 00038 NM 2008 3 5 QXEA200800162 1 20080130 A 5320 INTERCOSTAL DHAV DHC8 DHC8202 2809007 NM BS 510-531 S24L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - SUSPECT CORROSION ON FLOOR PAN INTERCOSTAL AT STR 24P FROM STA X510 TO X531. REPAIRED IAW DHC8 200 SRM 51-20-11 AND 51-20-16. 2 H 7 2 4T RT A13NM 2008030500039 20080305 00039 NM 2008 3 5 QXEA200800164 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 545 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - NR 9 SEAT TRACK INBOARD AND OUTBOARD FLOORBOARD SUPPORT MOUNT FLANGES SUSPECTED CORROSION AT STATION X5 45.00. REPAIRED IAW DHC8 200 RD8-53-4936, NDTM PT-6 51-00-01 AND DHC8 200 SRM 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2008030500050 20080305 00050 NM 2008 3 5 QXEA200800123 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 428-439 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - LEFT SEAT TRACK NR 7 BETWEEN FRAME 428.5 TO 439.5 HAS MULTIPLE CHAFES/GOUGES. REPAIRED IAW RD8/4-53-88 4, Q400 NDTM PT-6 51-00-01, AND Q400 SRM 51-21-10. 2 H 7 2 4T RT A13NM 2008030500071 20080305 00071 NM 2008 3 5 QXEA200800219 1 20080208 A 5320 SILL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - MCD LOWER SILL PLATE HAS CORROSION AROUND NUTPLATES. REPAIRED IAW Q400 RD8/4-53-1660, NDTM PT-6 51-00- 01 AND PT-1 51-00-04 AND SRM 51-42-05. 2 H 7 2 4T RT A13NM 2008030500072 20080305 00072 NM 2008 3 5 QXEA200800223 1 20080208 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 379-382 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - SEAT TRACK 2 STATION 379-382 HAS CORROSION ON CENTER OF TRACK. REMOVED SEAT TRACK AND INSTALLED NEW SE AT TRACK IAW Q400 RD 8/4-53-884, SRM 51-42-05, 51-40-15 AND 51-40-45. 2 H 7 2 4T RT A13NM 2008030500078 20080305 00078 NM 2008 3 5 QXEA200800129 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 644 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - LEFT SEAT TRACK NR 8 BETWEEN FRAME 644.5 TO END OF TRACK HAS POSSIBLE CORROSION. REPAIRED IAW RD8/4-53 -884, Q400 NDTM PT-6 51-00-01. 2 H 7 2 4T RT A13NM 2008030500079 20080305 00079 NM 2008 3 5 QXEA200800130 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 624 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - LEFT SEAT TRACK NR 15 BETWEEN FRAME 624.5 TO FRONT OF TRACK HAS MULTIPLE CHAFES/GOUGES. REPAIRED IAW R D8/4-53-884, Q400 NDTM PT-6 51-00-01, AND Q400 SRM 51-21-10. 2 H 7 2 4T RT A13NM 2008030500082 20080305 00082 NM 2008 3 5 QXEA200802090 1 20080101 A 5320 BRACKET DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - RADIO RACK LOWER BRACKET HAS CORROSION ON LIP JUST OUTBOARD OF STRINGER 31L AT APPROXIMATELY STATION X1 82.00 - X194.00. REPAIRED IAW -8 200 SRM 51-40-11, -8 CPCM CHAPTER 4 PARA 8, AND NDTM PART 6 51-00-1, NDTM PART 1 51-00 -04. 2 H 7 2 4T RT A13NM 2008030500083 20080305 00083 NM 2008 3 5 QXEA200802083 1 20080101 A 5313 STRINGER DHAV DHC8 DHC8202 2809007 NM BS 467 S31R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - CORROSION ON STATION 467.000 ON LEFT SIDE OF STRINGER 31R. REPAIRED IAW -8 200 CPC CHAPTER 4 PG 4-16 8 B AND -8 200 SRM 51-20-16, 51-20-36, 51-20-11, 51-40-11, 51-20-51. 2 H 7 2 4T RT A13NM 2008030500084 20080305 00084 NM 2008 3 5 QXEA200802085 1 20080101 A 5310 FRAME DHAV DHC8 DHC8202 2809007 NM BS 182 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - CORROSION AT STATION 182.00 ON RIGHT VERTICAL FRAME JUST OUTBOARD AND LOWER CORNER OF FLIGHT DECK KICK PLATE. REPAIRED IAW -8 200 CPC CHAPTER 4 PARA 8 AND -8 200 SRM 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2008030500085 20080305 00085 NM 2008 3 5 QXEA200802088 1 20080101 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - MCD SHELL HAS SURFACE CORROSION ON FORWARD FLANGE FOR STEP ASSEMBLY SEAL APPROXIMATELY 7" BELOW FORWAR D CENTER PRESSURE STOP. REPAIRED BY REMOVING LIGHT CORROSION BY HAND WITH SCOTCH BRITE PAD AND IAW -8 200 SRM 51-20-16, 51-20-86. 2 H 7 2 4T RT A13NM 2008030500094 20080305 00094 NM 2008 3 5 QXEA200802079 1 20080101 A 5315 FLOORBEAM DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - CARGO PIT SUPPORT ANGLE FOR AFT END OF CARGO DOOR THRESHOLD IS CORRODED ON TOP AND BOTTOM SURFACES LOCA TED ON STRUCTURE UNDER PANEL 145DZ (X600.00, Y29L, Z101.842). REMOVED ANGLE AND INSTALLED NEW ANGLE FROM STOCK IAW -8 2 00 SRM 51-40-00 AND 51-40-11. 2 H 7 2 4T RT A13NM 2008030500095 20080305 00095 2008 3 5 QXEA200800229 4 20080226 A 3442 MI5853512 INDICATOR DHAV DHC8 DHC8202 2809007 NM RADAR SMOKE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 355PH 500 PDX - FLIGHT 2058 - WHEN APPLYING ELECTRICAL POWER TO THE IRU AND FMS. SMOKE NOTICED FROM THE AREA BETWEEN THOSE UNITS AND THE RADAR INDICATOR. MAINTENANCE POWERED UP EACH UNIT ON IT'S OWN. THE RADAR DISPLAY (INDICATOR) STARTED TO SMOKE. REPLACED THE RADAR INDICATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008030500096 20080305 00096 NM 2008 3 5 QXEA200800233 1 20080228 A 3150 WARNING MESSAGE BOMBDR DHC8 DHC8402 1390042 NM ICE DETECTION FALSE ACTIVATION A QXEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 09 407QX 4049 SEA - FLIGHT 2232 - ICE DETECTOR CAUTION IN CLEAR AIR AT 22,000. DIVERTED TO SEA AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE CHECKED THE CDS SYSTEM WITH NO FAULTS LOGGED. AIRCRAFT RETURNED TO SERVICE. FUNCTIONAL CHECKS GOOD. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008030500117 20080305 00117 NM 2008 3 5 QXEA200800220 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 565 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - NR 6 SEAT TRACK FLOORBOARD MOUNT FLANGE (INBOARD) SIDE OF FLANGE APPROXIMATELY STA X565.00 IS CORRODED. REPAIRED IAW DHC 8 200 RD8-53-784, NDTM PT-6 51-00-01 AND DHC8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008030500118 20080305 00118 NM 2008 3 5 QXEA200800153 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 468 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - AT APPROXIMATELY STATION X468 THE LEFT OUTBOARD SEAT TRACK NR 2 HAS A GOUGE ON THE EDGE OF THE CLAW ON TOP OF TRACK. REPAIRED IAW DHC8 200 RD8-53-1342, NDTM PT-6 51-00-01, AND THE DHC8 200 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2008030500122 20080305 00122 NM 2008 3 5 QXEA200800182 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 265 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - SEAT TRACK NR 10 HAS CORROSION AT STA Y265. REMOVED SEAT TRACK AND INSTALLED NEW TRACK IAW DHC 8 200 S RM 51-40-11, 51-40-00. 2 H 7 2 4T RT A13NM 2008030500123 20080305 00123 NM 2008 3 5 QXEA200800143 1 20080119 A 5420 DIAPHRAGM BOMBDR DHC8 DHC8402 1390042 NM CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - RIGHT OUTBOARD DIAPHRAM HAS A SUSPECTED CRACK AT LOWER END NEAR LOCK FASTENER. REMOVED DIAPHRAM AND AS SOCIATED WEB IAW Q400 SRM 51-42-05. LOCATED AND DRILLED/DEBURRED AND INSTALLED FASTENERS COVERED BY AFT WEB AND INBOARD SOLID RIVETS IAW Q400 SRM 51-40-15, 51-42-05. INSTALLED AFT WEB AND FINISHED INSTALLATION OF DIAPHRAM IAW SRM 51-40-15 , 51-42-05. 2 H 7 2 4T RT A13NM 2008030500128 20080305 00128 NM 2008 3 5 QXEA200800116 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - SEAT TRACK NR 18 HAS SEVERAL SPOTS OF MILD SURFACE CORROSION AT STATION X94.0, X136.0, X150.0, X170.0, X201.0, X216.0. REMOVED AND INSTALLED NEW TRACK IAW Q400 SRM 51-40-05, 51-40-15 AND 51-42-05. 2 H 7 2 4T RT A13NM 2008030500131 20080305 00131 NM 2008 3 5 QXEA200800218 1 20080208 A 5320 SILL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - MCD THRESHOLD IS CORRODED AROUND SEVERAL SCREW HOLES. REMOVED SILL PLATE AND INSTALLED NEW SILL PLATE I AW Q400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 2008030500135 20080305 00135 NM 2008 3 5 QXEA200800114 1 20080119 A 5320 STRUCTURE BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - NUMBER 1 AND 2 JUNCTION BOXES (UNDER FLOOR) AT STATION X32.0/Y9.2 RIGHT THRU Y9.2 LEFT HAVE MILD SURFAC E CORROSION ON BOXES, TRAYS AND GROUNDING LUGS. REPAIRED IAW Q400 SRM 51-21-00 PARA A (1&2), 51-21-10, 51-21-00 PARA 1- 4A(1&2), 1-84-7A, PT-6,51-00-02 AND 1-84-7A PT-1, 51-00-04. 2 H 7 2 4T RT A13NM 2008030500139 20080305 00139 NM 2008 3 5 QXEA200800173 1 20080130 A 5340 STRINGER CLIP DHAV DHC8 DHC8202 2809007 NM BS 424 S23R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - THE STRINGER CLIP AND RIVETS ON STRINGER 23R AT THE FORWARD SIDE OF THE REAR SPAR FRAME X424.124 IS COR RODED. REMOVED CLIP AND INSTALLED NEW CLIP IAW DHC8 200 SRM 51-40-11, 51-20-46, AND 51-20-51. 2 H 7 2 4T RT A13NM 2008030500142 20080305 00142 NM 2008 3 5 QXEA200800201 1 20080208 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - CORROSION ON SKIN UNDER NUT PLATE DOUBLER FOR PANEL 144 GZ IN AFT CARGO BAY. REPAIRED REF. Q400 SRM 51 -21-00, 1-84-7A PT-6 51-00-02, 1-84-7A PT-1 51-00-04 AND Q400 SRM 51-21-10, 51-25-10. 2 H 7 2 4T RT A13NM 2008030500164 20080305 00164 NM 2008 3 5 QXEA200800216 1 20080208 A 5711 SPAR CAP BOMBDR DHC8 DHC8402 1390042 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - RIGHT HAND WING, LOWER FRONT SPAR CAP HAS FRETTING CORROSION FORMING AT APPROXIMATELY YW57.00 TO YW67.0 0 (I/B CONTACT AREA FOR 611AR). REPAIRED IAW Q400 RD8/4-57-935 AND NDTM PART 6 51-00-01. 2 H 7 2 4T RT A13NM 2008030500169 20080305 00169 NM 2008 3 5 QXEA200800210 1 20080208 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM BS 331 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - FUSELAGE SKIN HAS LIGHT SURFACE CORROSION UNDER NR 3 COM ANTENNA AT FS 331.0. REMOVED DOUBLER AND REPL ACED WITH NEW DOUBLER FROM STOCK IAW Q400 SRM 51-42-05, 51-40-07, AND 51-20-10. 2 H 7 2 4T RT A13NM 2008030500176 20080305 00176 NM 2008 3 5 QXEA200800172 1 20080130 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 333 S23-24L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - FRAME CASTELLATION AT STATION X333.3 AFT FACE OF FRAME BETWEEN STRINGERS 23L AND 24L HAS SUSPECT CORRO SION. REPAIRED IAW DHC8 200 CPM CHAPTER 4 STEP 8, NDTM PT-1 51-00-04 AND PT-6 51-00-01, DHC8 200 SRM 51-20-11, 51-12-16 , 51-20-51 AND 51-40-11. 2 H 7 2 4T RT A13NM 2008030500177 20080305 00177 NM 2008 3 5 UIEA200800061 1 20080215 A 5330 SKIN BOEING 747 7472D7B 1384803 NM ZONE 100 SCRATCHED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 PERFORMED EO 4753B100 FOUND SCRIBE LINE DISCREPANCY. REPAIRED LAP JOINT BS 520-1000 LEFT AND RIGHT SEE NON ROUTINE CARD 9022 AND 9030. BUTT JOINT BS 1961 S46L-S12R PER NON ROUTINE CARD 7455. ALL OTHER SCRIBE LINE DEFECTS COVERED BY ATLAS EO4753B112, 4753B113, 4753B116. 2 L 7 4 4F RT A20WE 2008030500179 20080305 00179 NM 2008 3 5 UIEA200800066 1 20080229 A 5755 SPOILER PANEL BOEING 747 7472D7B 1384803 NM ZONE 500 DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 LT WING NR 2 SPOILER UPPER SURFACE HAS A PREVIOUS REPAIR DISBONDING AT I/B FWD END OF SPOILER. PERMANENT REPAIR ACCOMPL ISHED AS PER B747-200 SRM 51-40-06, FIG 1, SHEET 2, FIG 4 SHEET 1, ALUMINUM HONEYCOMB REPAIRS, 250 DEGREES F CURE PER SR M 51-40-20. REFERENCE ATLAS AIR EO NR 4757A419. 2 L 7 4 4F RT A20WE 2008030500182 20080305 00182 NM 2008 3 5 QXEA200802093 1 20080101 A 5751 SKIN DHAV DHC8 DHC8202 2809007 NM LT AILERON CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - LEFT AILERON OUTBOARD HINGE CUT OUT IS CRACKED. REPAIRED IAW -8 200 SRM 51-20-91, -8 NDTM PART 6, 51-0 0-01 AND RD8-57-3827. 2 H 7 2 4T RT A13NM 2008030500184 20080305 00184 NM 2008 3 5 QXEA200802070 1 20080101 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - THERE IS A GOUGE AT APPROXIMATELY 2" AFT OF STATION X300 ON THE FLANGE OF THE LEFT OUTBOARD SEAT. REPA IRED IAW RD8-53-1342 AND -8 200 SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2008030500188 20080305 00188 NM 2008 3 5 QXEA200800195 1 20080208 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - NR 17 SEAT TRACK HAS AN AREA OF CORROSION AT STATION X36.000. REMOVED SEAT TRACK AND INSTALLED NEW SEA T TRACK IAW Q400 SRM 51-40-15 AND 51-42-05 2 H 7 2 4T RT A13NM 2008030500190 20080305 00190 NM 2008 3 5 QXEA200800200 1 20080208 A 5320 FLOOR SUPPORT BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - CORROSION AROUND LEFT OUTBOARD SCREW HOLE ON ANGLE AT X783 FOR AFT CARGO BAY FLOORBOARD 145AZ. REMOVED AND INSTALLED NEW ANGLE IAW Q-400 SRM 51-14-00, 51-42-05, 51-21-10, 51-25-10, 51-42-45 AND 51-42-05 2 H 7 2 4T RT A13NM 2008030500195 20080305 00195 NM 2008 3 5 QXEA200802066 1 20080101 A 5230 TRACK DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - CARGO DOOR FORWARD TRACK OUTBOARD FACE IS CHAFED APPROXIMATELY 25" FROM BOTTOM OF TRACK. REPAIRED IAW E/C 2-52-266 AND -8 200 NDTM PART 6 51-00-01. 2 H 7 2 4T RT A13NM 2008030500200 20080305 00200 NM 2008 3 5 QXEA200800194 1 20080208 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - NR 11 SEAT TRACK HAS AN AREA OF CORROSION AT STATION X21.500. REMOVED SEAT TRACK AND INSTALLED NEW SEA T TRACK IAW Q400 SRM 51-40-15 AND 51-42-05. 2 H 7 2 4T RT A13NM 2008030500201 20080305 00201 NM 2008 3 5 QXEA200800217 1 20080208 A 5711 SPAR CAP BOMBDR DHC8 DHC8402 1390042 NM RT WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - RIGHT WING LOWER FRONT SPAR CAP HAS 4 EACH DAMAGED SLEEVES AT INBOARD MOST END OF 611AR. REPAIRED SLEE VES IAW TASK CARD 6-57-551 AND Q400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 2008030600003 20080306 00003 NE 2008 3 6 NACA20080002 2 20080228 A 8550 OIL SYSTEM DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 1 ENGINE LOW PRESSURE A NACA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 AL 03 6174C 1137 1137 44075 510065 NR 1 ENGINE SHUT DOWN DUE TO NO OIL PRESSURE. REMOVED AND REPLACED ENGINE DUE TO INTERNAL FAILURE, REF: NAC DC6MM SEC V PG 3. 2 L 7 4 4R 4 R 6A3 5E8 2008030600005 20080306 00005 NM 2008 3 6 DHL2008752607 1 20080223 A 5754 6517327U3 ATTACH FITTING BOEING 727 727223 1384074 NM NR 1 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 NR 1 SLAT ACTUATOR INBD ATTACHING RIB (AT SLAT) CRACKED. REMOVED RIB AND "U" CHANNEL FOUND CRACK IAW SRM 51-30-2. LOCA TED, DRILLED AND DEBURRED RIB IAW SRM 51-30-5. FABRICATED CHANNEL IAW BDW NR 65-17327 AND SRM 51-20-01, 51-20-2, 51-30- 5. INSTALLED RIB AND CHANNEL IAW SRM 51-30-2 AT NR 1 SLAT ACTUATOR. 2 L 7 3 4F A3WE 2008030600006 20080306 00006 NM 2008 3 6 DHL2008752608 1 20080206 A 5752 SKIN BOEING 727 727223 1384074 NM AILERON TAB DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 LT OB AILERON TAB UPPER SURFACE HAS DELAMINATED AREA. CUTOUT DELAMINATED AREA 2 INCHES DIA ON LT O/B AILERON. TAB UPPE R SURFACE FABRICATED FILLER AND DOUBLER IAW B727 SRM 57-50-2, BONDED FILLER AND DOUBLER IAW B727SRM 51-40-20. 2 L 7 3 4F A3WE 2008030600008 20080306 00008 WP 2008 3 6 ABXA080055 1 20080214 A 2740 920710296 RELAY DOUG DC9 DC932 3022066 WP STAB TRIM OVERHEATED A ABXA K NONE M OVER TEMP IN INSP/MAINT 1 GL 23 986AX 5250 47543 WHILE SETTING STABILIZER, CIRCUIT BREAKER FOR PRIMARY TRIM TRIPPED. WHILE INVESTIGATING ISSUE, FOUND STABILIZER TRIM RE LAY AND WIRING TO RELAY SHOWED SIGNS OF OVERHEATING. REPLACED UP TRIM RELAY R20-16 AND RE-TERMINATED ALL WIRES GOING TO R20-16 DUE TO OVERHEAT DAMAGE. PRIMARY TRIM, OPS CHECK GOOD IAW DC9 MM CHAPTER 27. 2 L 7 2 4F A6WE 2008030600013 20080306 00013 GL 2008 3 6 RAIA00802017 2 20080217 A 7530 8266101 CONTROL VALVE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 ENGINE MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 814HK 145046 FLT 5597 - STL - BLEED 2 OVERTEMP MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE BLEED FAN AIR CONTROL VALVE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008030600019 20080306 00019 NM 2008 3 6 MASA200800158 1 20080217 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 989HA 427 REPAIR TO NR 3 LEFT FLAP TRACK. 2 H 7 2 4T RT A13NM 2008030600032 20080306 00032 EU 2008 3 6 PNSA080201 1 20080207 A 3260 SAFETY SWITCH SAAB SF340 340B 7860101 EU MLG FAULTY A PNSA A UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 364PX 340B262 ON CLIMBOUT FROM ANC LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO ANC AND MX CLEANED WEIGHT ON WHEEL SWITCHES. THE NEXT DAY AIRCRAFT HAD A SIMILAR PROBLEM AND MX REPLACED THE LT WEIGHT ON WHEEL SWITCHES. NO FURTHER PROBLEMS HAVE BEEN NOTED SINCE. 2 L 7 2 4T RT A52EU 2008030600037 20080306 00037 EA 2008 3 6 MASA200800160 1 20080221 A 3350 COVER CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH FLT 2903 PHX-GJT, EMERGENCY FLOOR PATH LIGHTING COVER LOOSE AT ROW 1-3. MX REPLACED COVER. 2 L 7 2 4F RT A21EA 2008030600041 20080306 00041 EA 2008 3 6 SWIA200819037 1 20080108 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 707SK 10003 FLT 5962 - PAX DOOR HANDLE IS HARD TO OPEN. CLEANED AND LUBRICATED PAX DOOR MECHANISM. OPS CHECK GOOD IAW AMM 52-00-00 . 2 L 7 2 4F RT A21EA 2008030600043 20080306 00043 WP 2008 3 6 UPS08851701 1 20080110 A 5313 3645897501 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 HEAVY CORROSION INSIDE L33L AT STA 1414. REPAIRED LONG 33L AT SAT 1414 IAW EO DC8-5320-28559-A AND E A 008-5320- 1-A1264. 2 L 7 4 4F RT 4A25 2008030600058 20080306 00058 2008 3 6 2008UALA00920 4 20080218 A 3460 DISPLAY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT FAILED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 644UA 25094 RTFL DUE TO FAILURE OF THE MULTI-FUNCTION CONTROL DISPLAY UNIT. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030600071 20080306 00071 SO 2008 3 6 C2XA08SH036 1 20080224 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18557 145596 SHV - DURING C-CHECK LEFT OMEGA BEAM FR 20 CORRODED AT RAMP BASE. MX REMOVED AND REPLACED PREVIOUS REPAIRED ON LEFT OME GA BEAM AT FR 20 IAW EMB 145 SRM 53-00-10 FIG 203 & 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008030600074 20080306 00074 SO 2008 3 6 C2XA08SH038 1 20080224 A 5512 14532235601 SKIN EMB 145 EMB145LR 3260212 SO HORIZ STAB CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18557 145596 SHV - DURING C-CHECK LT HORIZONTAL STAB L/E HAS CORROSION ON SKIN AND AROUND RIVET & SCREW HOLE. MX REPAIRED LT HORIZON TAL STAB L/E ON SKIN AND AROUND RIVET & SCREW HOLE IAW EC 5510-01179 AND EC 5530-01116. THE AIRCRAFT WAS APPROVED TO RE TURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008030600076 20080306 00076 SO 2008 3 6 C2XA08IA062 1 20080217 A 3350 2013BR BATTERY EMB 145 EMB145XR 3260214 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12163 10891 10891 14500811 MCI - DURING MAINTENANCE INSPECTION THE GALLEY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED THE NUMBER 2 EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. 2 L 7 2 4F RT 2008030600082 20080306 00082 WP 2008 3 6 UPS08851709 1 20080222 A 3397 WIRE DOUG DC8 DC871F 302199D WP COCKPIT SHORTED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. FOUND SHORTED WIRE IN CHARGING CIRCUIT. REMOVED AND REPLACED C/B DUE T O NOT POPPED WHEN SHORTED TO GROUND AND REPAIRED WIRE AS REQ. 2 L 7 4 4F RT 4A25 2008030600091 20080306 00091 SO 2008 3 6 RAIA00802021 1 20080219 A 3260 TARGET EMB 145 EMB145LR 3260212 SO NLG OUT OF ADJUST A RAIA B A EMER. DESCENT UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 824HK 145498 FLT 5535 - STL - LANDING GEAR AIR/GROUND FAILURE MESSAGE ON EICAS. MAINTENANCE INSPECTED AND FOUND THE NLG PROXIMITY SE NSOR TARGET OUT OF ADJUSTMENT. TARGET AND SENSOR WHERE RE-ALIGNED AND AN OPERATIONAL CHECK WAS PERFORMED WITH NO DEFECT S NOTED. 2 L 7 2 4T RT T00011AT 2008030600098 20080306 00098 NM 2008 3 6 SWAA081060 1 20080222 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED AT UPPER SURFACE. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008030600103 20080306 00103 NM 2008 3 6 SWAA081062 1 20080225 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 AALA200801883 1 20080715 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 905AN 29507 MIA - EMERGENCY LIGHT AT RT NR 1 DOOR DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RT NR 1 DOOR. SYSTEM GRO UND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A16WE 20080902 SO 2008 9 2 C2XA08IA182 1 20080730 A 3320 BR90002 BALLAST EMB 145 EMB145 3260210 SO GALLEY BURNED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27962 145110 IAH - FLIGHT 2247 - DURING POST FLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING SMELL FROM THE GALLEY AREA. M AINTENANCE REMOVED AND REPLACED THE GALLEY LIGHT BALLAST, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080902 NM 2008 9 2 SWAA084579 1 20080819 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 213WN 34217 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 20080902 SO 2008 9 2 C2XA08IA156 1 20080707 A 3260 8005701 PROXIMITY SENSOR EMB 135 EMB135LR 3260305 SO NLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16520 145372 IAH - FLIGHT 2497 - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON ROTATION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SEN SOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080902 NM 2008 9 2 SWAA084513 1 20080814 A 5312 6517852 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND FWD PRESSURE BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084509 1 20080814 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 451WN 32495 DURING SCHEDULED HC1 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080902 NE 2008 9 2 DHLA200800088 2 20080815 A 7200 ENGINE BOEING 727 7272J0 138407E NM PWA JT8 JT8D15 52051 NE NR 3 MALFUNCTIONED A DHLA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 01 749DH 22013 REJECTED TAKEOFF, ENG NR 3 WAS 1.88 EPR WITH BUG OF 2.05. GROSS WEIGHT 173.4, AIR SPEED 70 KTS, PRESS ALTITUDE 2360FT, AIR TEMP 39C. TRIMMED ENG TO CORRECT PP AND IDLE PARAMETERS PER MM CH 71-00-87. PP STOP REMOVED AND SAFTIED. TO EPR 2 .07. ACFT WAS GROUNDED. FLIGHT 149. (S) 2 L 7 3 4F 4 F RT A3WE E2EA 20080902 CE 2008 9 2 DXTA200803230 1 20080816 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE MLG WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 398QS 5600522 FIRST OFFICER`S RIGHT PEDAL GOES TO THE FORWARD STOP WHEN INITIALLY DEPRESSED. WHEN BRAKE IS PUMPED, LIMITED BRAKING RE TURNS. FIRST OFFICER`S LT BRAKE PEDAL IS "SPONGY", REQUIRING GREATER THAN NORMAL (CON`T) BRAKE APPLICATION. (S) 2 L 7 2 4F RT A22CE 20080902 NE 2008 9 2 DXTA200803231 2 20080816 A 7230 COMPRESSOR CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE LT ENGINE STALLED E DXTA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 678QS 5605616 LEFT ENG EXPERIENCED COMPRESSOR STALL AS THROTTLES WERE ADVANCED FOR TAKEOFF. ABORTED TAKEOFF. (S) 2 L 7 2 4F 4 F RT A22CE E00059EN 20080902 WP 2008 9 2 IXX2008F00064 1 20080709 A 5730 SKIN DOUG DC8 DC872F 302199E WP RT WING DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND ELONGATED HOLES ON RT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095. 000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING. FABRICATED NEW SKIN. CLEANED, TREATED A ND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XILD 7095.000-XS 247.000 IAW DC8 S R 57-3-2 FIGURE 10 PAGE 22 ITEM F, DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-3-0 AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080902 WP 2008 9 2 IXX2008F00057 1 20080616 A 5330 SKIN DOUG DC8 DC872F 302199E WP BS 1604-1606 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE EXTERNAL SKIN HAS A CRACK AT STATION 1606.000-1604.000 LONGERON 10 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, INTERNAL FING ER DOUBLER, AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IA W DC8 SRM 53-2-1 FIGURE 7 SHEET 1,3, AND 5, SRM 53-5-2 FIGURE 1 ITEM "D", DC8 SRM 51-1-8B, SRM 51-1-11, SRM 51-1-20D, AN D SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080902 NM 2008 9 2 SWAA084485 1 20080813 A 5311 6517684 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 303, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084482 1 20080813 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND STRINGER 22R CORRODED BETWEEN BS 933 AND BS 943. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080902 EU 2008 9 2 MAL2008F00024 1 20080813 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 415XJ 340B415 EMERGENCY POWER SUPPLY AT 23LN INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AT LOCATION 23LN P/N 3301-51 OF F/ON S/N 2108 OFF S/N 2057 ON IAW SAAB AMM 33-50-10-04-1. (S) 2 L 7 2 4T RT A52EU 20080902 2008 9 2 SWAA084472 4 20080812 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080902 SO 2008 9 2 RAIA00808015 1 20080815 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 835HK 145670 PRE FLT 7961 -BTV- THE FORWARD FLOOR EXIT ROW LIGHT WITH RED ARROWS IN FRONT OF SEAT 12A IS LOOSE. MAINTENANCE RE-INSTA LLED THE FLOOR EMERGENCY LIGHT. SYSTEM OPS CHECKED GOOD. (S) 2 L 7 2 4T RT T00011AT 20080902 EA 2008 9 2 REX2008F00026 1 20080801 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG DISCHARGED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8623A 7623 ON APPROACH INTO KMEM, WHEN GEAR WAS LOWERED THE AURAL "GEAR DISAGREE" WARNING WENT OFF WITH A RED NOSE GEAR INDICATION. CREW DECLARED AN EMERGENCY AND A GO AROUND. WHILE PERFORMING THE QRH, THE NOSE GEAR LOCKED DOWN. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KMEM. MAINTENANCE INSPECTED THE GEAR AND SERVICED THE NOSE LANDING GEAR STRUT NITROGE N/HYDRAULICS, GEAR SWINGS PERFORMED WITH NO DEFECTS PER AMM. (S) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 REX2008F00024 1 20080802 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG DISCHARGED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8611A 7611 ON APPROACH INTO KMEM, WHEN GEAR WAS LOWERED THE AURAL "GEAR DISAGREE" WARNING WENT OFF WITH A RED NOSE GEAR INDICATION. CREW DECLARED AN EMERGENCY AND A GO AROUND. WHILE PERFORMING THE QRH, THE NOSE GEAR LOCKED DOWN. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KMEM. MAINTENANCE INSPECTED THE GEAR AND SERVICED THE NOSE LANDING GEAR STRUT NITROGE N/HYDRAULICS, GEAR SWINGS PERFORMED WITH NO DEFECTS PER BOMBARDIER AMM. (S) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 VNAA0807005 1 20080712 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FALSE ACTIVATION A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 05 220PS 7887 CREW ABORTED TAKEOFF BETWEEN 90-95 KIAS FOR FMS NAV RED FLAG AND MAP AMBER MSG ON PDF AND MFD. MAINTENANCE INSPECTED FM S AND FOUND NO DEFECTS AND ACCOMPLISHED AN ABORTED TAKEOFF INSPECTION WITH NO DEFECTS. AIRCRAFT WAS RELEASED FOR SERVIC E. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080902 EA 2008 9 2 VNAA0808001 1 20080801 A 5200 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE OPEN A VNAA A UNSCHED LANDING W INADEQUATE Q C NR NOT REPORTED 1 GL 05 706PS 10150 CREW ELECTED TO RETURN TO CLT FOR COM DOOR LEFT OPEN. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ACFT WITH NO DEFECTS NOTED. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E00063EN 20080902 NM 2008 9 2 USAASB08064 1 20080818 A 2560 MEGAPHONE BOEING 737 7374B7 1384702 NM AFT CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 453UW 24980 BOS - MAINTENANCE REPORTED THE AFT MEGAPHONE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT MEGAPHONE. OPERATIO NAL CHECK GOOD. (S) 2 L 7 2 4F RT A16WE 20080903 NM 2008 9 3 2008UALA03464 1 20080618 A 5315 111T5007 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 805 LBL 11 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 CORROSION FOUND AT BS 805, LBL 11, UNDER MAIN CABIN FLOOR. *S/D* SUSPECT MOISTURE CONTAMINATION. CUT OUT DAMAGED SECT ION OF T-CAP SPLICED IN NEW SECTION PER SRM 53-00-51, SRM 51-20-01 AND SRM 51-40-02. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080903 NM 2008 9 3 UIEA200800294 1 20080804 A 5330 SKIN BOEING 747 747400 13848AT NM GE CF6 CF680C2* GL BS 2080 S26-27R SCRATCHED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 429MC 24833 DURING C-CHECK FOUND FUSELAGE SKIN WITH DEEP SCRATCH AT STATION 2080 STR 26-27R. REPAIRED AS PER SRM 53-00-01 FIGURE 20 1. (S) 2 L 7 4 4F 4 F RT A20WE E23EA 20080903 EA 2008 9 3 QXEA200800908 1 20080814 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA MAIN PAX STIFF A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 19 604QX 10019 PDX-FLIGHT 2634. MAIN CABIN DOOR STIFF TO OPERATE. MAINTENANCE OPERATED DOOR SEVERAL TIMES AND WERE NOT ABLE TO DUPLIC ATE. RETURNED TO SERVICE. NO PARTS REPLACED. (S) 2 L 7 2 4F RT A21EA 20080903 NM 2008 9 3 USAABB08133 1 20080816 A 7334 21SN04333 PRESSURE SWITCH BOEING 767 767201 1385125 NM GE CF6 CF680C2B2 30025 NE FUEL SYSTEM FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 248AY 23900 690167 YQX FLT 716 EN ROUTE PHL TO MXP. DURING CRUISE, THE FLIGHT RECEIVED EICAS MESSAGE "LT ENG FUEL FILTER." THE FLIGHT DIV ERTED TO YQX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LT ENG FUEL DIFFERENTIAL PRESSURE SWITCH. O PERATIONALLY AND LEAK CHECKS OK. (S) 2 L 7 2 4F 4 F RT A1NM E13NE 20080903 SO 2008 9 3 C2XA08RI109 1 20080810 A 2133 2099L011100 OUTFLOW VALVE EMB 145 EMB145LR 3260212 SO CABIN PRESSURE DIRTY A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 13997 19586 145298 FLIGHT 3114 - RIC- AIR CREW REPORTED THAT DURING CRUISE, CABIN PRESSURE WAS AT 12,000 FT AT ALTITUDE OF 32,000 FT. FLIG HT WAS DIVERTED TO RIC. CREW LANDED ACFT UNEVENTFULLY. RIC MAINTENANCE CLEANED RT OUTFLOW VALVE AND PERFORMED OPERATIO NAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080903 NM 2008 9 3 ABXA080223 1 20080805 A 5730 114T0222 SKIN BOEING 767 767232 1385132 NM LT TRACK CUTOUT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 745AX 22222 FOUND CRACK AT NR 3 SLAT OUTBOARD TRACK CUTOUT ON LEADING EDGE OF LT WING. REPAIRED SPLICE PLATE IAW REA B65757685. (S ) 2 L 7 2 4F RT A1NM 20080903 EU 2008 9 3 ECP2008F00000 1 20080605 A 2720 Z4242100024 BLOCK ZLIN 242 Z242L 9970204 EU RUDDER CONTROL CRACKED E ECPA O OTHER O OTHER NR NOT REPORTED 1 SO 15 146FS 1976 734 FOUND PILOT`S OUTBOARD BUSH BLOCK ON RUDDER CONTROL CRACKED. 1 L 7 1 3O 0 A76EU 20080903 EA 2008 9 3 VNAA0808010 1 20080817 A 3200 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE MLG OUT OF POSITION A VNAA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 GL 05 246PS 7920 CREW REPORTED A GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOOR SWITCH NOT IN FLT/NORMAL POSITION. SWITCH WAS REPOSITIONED AND SYS TEM TESTED. NO OTHER DEFECTS NOTED. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080903 SO 2008 9 3 XGN2008F00012 2 20080801 A 8530 AEC631397 CYLINDER CESSNA 402 402B 207590P CE CONT O520 TSIO520* 17040 SO ENGINE CRACKED E XGNA K NONE O OTHER IN INSP/MAINT 1 SW 05 4165G 801 402B1212 REV 3, E=SERIES CYLINDER, CRACKED. (K) 1 L 7 2 3O 3 O A7CE E8CE 20080904 NM 2008 9 4 RYN2008F00005 1 20080620 A 5310 STRUCTURE BOEING 757 757236 1384971 NM TAIL SKID DAMAGED A RYNA O OTHER O OTHER NR NOT REPORTED 1 CE 07 526NA 24794 REPAIR SECTION 48 TAIL SKID DAMAGE. REPAIRED SECTION 48 IAW 6-1171-RE-01647. 2 L 7 2 4F RT A2NM 20080904 NM 2008 9 4 DHL2008F00015 1 20080626 A 5210 ANGLE BOEING 727 7272M7 138407S NM L2 DOOR CORRODED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 L-2 DOOR TAP INTERIOR ANGLE SUPPORT AND WEB ARE CORRODED (EXFOLIATION) BS 1040/1065. REMOVED AND REPLACED L-2 DOOR UPPE R ANGLE SUPPORT WEB BEAM IAW B727 SRM 51-30-2 AND BOEING DRAWING 65-56992 REV V DATED 3/26/01. (A) 2 L 7 3 4F A3WE 20080904 NM 2008 9 4 QXEA200800710 1 20080714 A 2120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM GALLEY ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 432QX 7868 4166 SEA - ELECTRICAL BURNING ODOR IN THE CABIN. STRONGEST IN THE AFT GALLEY. MAINTENANCE RAN THE NR 2 ENGINE AND TURNED ON ALL THE CABIN AND GALLEY EQUIPMENT WITH NO ODOR DETECTED. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACE D. (A) 2 H 7 2 4T RT A13NM 20080904 WP 2008 9 4 IXX2008F00022 1 20080716 A 2612 FIRE DETECTOR DOUG DC8 DC871F 302199D WP NR 4 NACELLE FALSE ACTIVATION A IXXA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 11 828BX 45993 FLT ATN 819/KDFW TO KTOL/TAT 87593/TAC 36428. DURING CLIMBOUT FROM KDFW NR 4 FIRE WARNING LIGHT CAME ON, THE CREW SHUTD OWN NR 4 ENGINE AND DISCHARGED BOTH FIRE BOTTLES THE LIGHT REMAINED ON. THE CREW RETURNED TO KDFW AND LANDED WITHOUT IN CIDENT. MAINTENANCE REPLACED LT CORE, AND LT FAN PYLON FIRE SENSING ELEMENTS, AND BOTH FIRE BOTTLES, OPERATIONAL CHECK GOOD IAW MM 26-10-1, 26-21-09. AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 4 4F RT 4A25 20080904 WP 2008 9 4 IXX2008F00017 1 20080722 A 2697 CONNECTOR DOUG DC8 DC871F 302199D WP FIRE DETECTION MALFUNCTIONED A IXXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 11 830BX 45973 FLT NR: ATN 801 / KLAX TO KTOL / TAT 81755.9 / TAC 32719. DURING CRUISE FROM KLAX NR 2 ENGINE FIRE WARNING LIGHT CAME O N. THE CREW ACCOMPLISHED EMERGENCY CHECKLIST AND SHUTDOWN NR 2 ENGINE. FIRE WARNING LIGHT EXTINGUISHED SHORTLY AFTER E NGINE SHUTDOWN, THE CREW DID NOT DISCHARGE FIRE BOTTLES. THE CREW LANDED IN KTOL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LT CORE ELEMENT, AND RT CORE FORWARD CONNECTOR. OPERATIONAL CHECK GOOD IAW MM 26-10-1, 20-50-1 AND 26-10-0. AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 4 4F RT 4A25 20080904 NM 2008 9 4 DHL2008F00004 1 20080701 A 5754 STRUCTURE BOEING 727 727225 1384077 NM NR 3 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 748DH 22440 NON-ROUTINE 068119 LT WING NR 3 I/E SLAT AT INBOARD TRACK HAS CRACK IN SKIN AT RADIUS. THIS IS A MINOR REPAIR. STOPPED DRILLED CRACK AND INSTALLED REPAIR DOUBLER. ALL WORK ACCOMPLISHED IAW SRM 51-40-2. NON-ROUTINE 068125 LT WING NR 3 I/ E SLAT AT OUTBOARD TRACK HAS SKIN CRACKED AT BOTH RADIAL. STOPPED DRILLED CRACKS AND INSTALLED REPAIR DOUBLER. ALL WOR K ACCOMPLISHED IAW SRM 51-40-2. THIS IS MINOR REPAIR. (A) 2 L 7 3 4F A3WE 20080904 EU 2008 9 4 SIMA200820304 1 20080721 A 5315 FLOORBEAM SAAB SF340 340B 7860101 EU BS 258 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 392AE 340B392 DURING MBV A PREVIOUS REPAIR ON GALLEY FLOOR FRAME FS 258.0 WAS FOUND CORRODED. REMOVED THE DAMAGED FILLER, FABRICATED A 26.0" X 2.0" FILLER. DRILLED, TREATED AND INSTALLED FILLER IAW SRM 53-70-30. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4T RT A52EU 20080904 WP 2008 9 4 IXX2008F00024 1 20080716 A 2612 FIRE WARNING DOUG DC8 DC871F 302199D WP NR 4 NACELLE ACTIVATED A IXXA F A ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 11 830BX 45973 FLT NR: ATN 229/PKMJ TO KHNL/TAT 81746.9/TAC 32717. DURING CRUISE FROM PKMJ NR 4 FIRE WARNING CAME ON THE CREW SHUTDOWN THE NR 4 ENGINE AND FIRED BOTH BOTTLES. THE CREW LANDED KHNL WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION IN WORK. (A ) 2 L 7 4 4F RT 4A25 20080904 EA 2008 9 4 TRAX200800911 1 20080715 A 5313 STRINGER CNDAIR CL600 CL6002B19 1900309 EA BS 310-349 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 682BR 7691 FOUND CORROSION ON LOWER FRAME STRINGER MIDWAY BETWEEN FS 310.0 AND FS 349.0. REFERENCE CONTROL INSPECTION CARD ASA-2-2 42001. REMOVED AND REPLACED STRINGER 601R31527-221 IAW CRJ 200 SRM 51-40-00. (A) 2 L 7 2 4F RT A21EA 20080904 WP 2008 9 4 IXX2008F00023 1 20080717 A 2612 FIRE WARNING DOUG DC8 DC873F 302199F WP NR 3 NACELLE ACTIVATED A IXXA F A ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SW 11 603AL 46003 FLT NR: 744/ETAR TO OJAM/. DESCENDING INTO OJAM NR 3 ENGINE FIRE WARNING LIGHT CAME ON AND RED LIGHT IN FIRE HANDLE CAM E ON. THE CREW DISCHARGED BOTH BOTTLES AND RED LIGHT IN FIRE HANDLE WAS STILL ON, AND FIRE WARNING WAS INTERMITTENT. T HERE LANDED IN OJAM WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION IN WORK. (A) 2 L 7 4 4F RT 4A25 20080904 CE 2008 9 4 GUU2008F00024 1 20080429 A 5540 10164001415 HINGE BEECH 1900 1900D 1154162 CE RUDDER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 87557 23060 UE246 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED UPPER RUDDER HINGE EXFOLIATED. REPLACED UPPER RUDDER HINGE. (A) 2 L 7 2 4T RT A24CE 20080904 CE 2008 9 4 GUU2008F00023 1 20080613 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 87557 23060 UE246 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT ELEVATOR OUTBOARD HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR OUT BOARD HINGE BRACKET. (A) 2 L 7 2 4T RT A24CE 20080904 NM 2008 9 4 QXEA200800810 1 20080723 A 3350 58401A2B5C5F4L30 SWITCH BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY LIGHT FAILED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 429QX 4161 PDX - FLIGHT 2450 - EMERGENCY LIGHTS STAY ILLUMINATED WHEN THE SWITCH IS IN THE ARM POSITION. MAINTENANCE REPLACED THE SWITCH. CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE. (A) 2 H 7 2 4T RT A13NM 20080904 CE 2008 9 4 GUU2008F00025 1 20080429 A 5540 10164001423 HINGE BEECH 1900 1900D 1154162 CE RUDDER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 87557 23060 UE246 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LOWER RUDDER HINGE EXFOLIATED. REPLACED LOWER RUDDER HINGE. (A) 2 L 7 2 4T RT A24CE 20080904 WP 2008 9 4 G412008F00001 1 20080603 A 2612 FIRE WARNING DOUG DC8 DC872F 302199E WP NR 1 NACELLE FALSE ACTIVATION E G41A A UNSCHED LANDING N E FALSE WARNING VIBRATION/BUFFET CR CRUISE 1 SW 01 721CX 46013 DURING CRUISE FROM KBWI NR 1 FIRE WARNING LIGHT AND BELL CAME ON MOMENTARILY THEN WENT OFF ENGINE WAS SHUTDOWN IAW COM P ROCEDURE. THE CREW RETURNED TO KBWI AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED HORSESHOE DETECTOR, LT CORE DETEC TOR, RT CORE DETECTOR, AND RT FAN DETECTOR. OPERATIONAL CHECK GOOD IAW MM 26-10-1. AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 4 4F RT 4A25 20080904 NM 2008 9 4 DHL2008F00022 1 20080612 A 5313 STRINGER BOEING 727 7272M7 138407S NM BS 720B S15R CRACKED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 STRINGER 15R IS CRACKED AT BS 720B + 5 INCHES. CUT OUT DAMAGE AREA DIMENSION .625 AT STRINGER 15R 720B IAW SRM 53-10-3 FIG 5. FABRICATED CHANNEL USING 7075-T6 040 PO 9007282 DIMENSION 5.125" X 1" X 1", RADIUS FILLER USING 7075-T6 .090 PO 9006162 DIMENSION 2.625" X .75" AND TAPERED FILLER USING 7075-T6 PO 9007294 DIMENSION 625" X .75" IAW B727 SRM 53-10-3 F IG 5. ALODINE AND PRIMED REPAIR PART IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 53-10-3 FIG 5. (A) 2 L 7 3 4F A3WE 20080904 SO 2008 9 4 SIMA200820305 1 20080721 A 5320 14522178005 SILL EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 842AE 145673 DURING MBV THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. REMOVED DAMAGED SILL AND INSTALLED NEW SILL IAW EMB 145 SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080904 NM 2008 9 4 QXEA200800589 1 20080607 A 3297 CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM MLG DAMAGED A QXEA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 414QX 4061 YUR - WHEN GEAR SELECTED DOWN ON APPROACH, THE LT GEAR DOOR LIGHT REMAINED ON. DID ALTERNATE EXTENSION AND ACCOMPLISHED UNEVENTFUL LANDING. FERRY YUR TO PDX. MAINTENANCE REPLACED THE J-24 CONNECTOR. OPERATIONAL CHECKS GOOD, AIRCRAFT RET URNED TO SERVICE. (A) 2 H 7 2 4T RT A13NM 20080904 NM 2008 9 4 BJN2008F00000 1 20080815 A 3350 1317 LAMP BOEING 737 737400 138449A NM EMERGENCY LIGHT BURNED OUT A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 42XA 25729 ONE EMERGENCY AISLE LIGHT, ROW 12, RT SIDE, BURNED OUT. REPLACED EMERGENCY LIGHT BULB. (K) 2 L 7 2 4F RT A16WE 20080905 EA 2008 9 5 TRAX200800704 1 20080530 A 3350 RELAY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 760EV 10212 THE "EMER LTS ON" WHITE STATUS MESSAGE CONTIOUSLY CYCLING ON AND OFF. FLT 4192 DEL 136 MINS. T/S SYSTEM - FOUND RELAY 135 JB11 BAD. REMOVED AND REPLACED RELAY. PERFORMED FUNCTIONAL TEST OF EMERGENCY LIGHTS IAW AMM 33-51-01 PG 526-532. (B) 2 L 7 2 4F RT A21EA 20080905 EA 2008 9 5 TRAX200800924 1 20080722 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 683BR 7692 FLOORBEAM CRACKED AT FS 621 LT OUTBOARD CORNER. REFER TO EC/TC REO 601R-53-61-117. SDR CLOSED. (A) 2 L 7 2 4F RT A21EA 20080905 EA 2008 9 5 TRAX200800598 1 20080505 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 920EV 7810 FS 484 LBL 36.0 PREVIOUS REPAIR ON INTERCOSTAL ANGLE CRACKED AROUND FASTENER HOLE. REPAIRED CRACKED INTERCOSTAL ANGLE A T FS 484 LBL 36 BY FABRICATING NEW ANGLE AND INSTALLING IAW BOMBARDIER REO 601R-53-41-059 STEPS 5-14. (B) 2 L 7 2 4F RT A21EA 20080905 EA 2008 9 5 TRAX200800599 1 20080505 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 920EV 7810 INBOARD AND OUTBOARD CLIPS AT FS 280.0 RBL 9.0 CRACKED IN RADIUS. REMOVED CRACKED INBOARD AND OUTBOARD CLIPS AT FS 280 RBL 9.0, REPLACED WITH NEW IAW CRJ 200 SRM 51-42-06. (B) 2 L 7 2 4F RT A21EA 20080905 EA 2008 9 5 TRAX200800701 1 20080523 A 2913 PUMP CNDAIR CL600 CL6002C10 1390015 EA HYD SYSTEM MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION DE DESCENT 1 SO 27 760EV 10212 RECEIVED NR 2 HYD LOW PRESS IN FLT FOLLOWED QRH OBSERVED NR 2 SYSTEM AT 0. FLT 4189 CX. EMERGENCY DECLARED. REMOVED A ND REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP IAW AMM 29-10-01, OPS AND LEAK CK GOOD OK FOR SERVICE. (B) 2 L 7 2 4F RT A21EA 20080905 EA 2008 9 5 TRAX200800597 1 20080505 A 5210 ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 920EV 7810 PAX DOOR VENT FLAP SUPPORT STRUCTURE HAS CRACKED ANGLE ON AFT SIDE AT THE LOWER RIVET. REMOVED AND REPLACED PAX DOOR VE NT FLAP SUPPORT STRUCTURE ANGLE ON AFT SIDE AS NEEDED IAW CRJ 200 SRM 51-42-06. (B) 2 L 7 2 4F RT A21EA 20080905 EA 2008 9 5 TRAX200800603 1 20080505 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA LT OVERWING INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 974EV 7594 LEFT FUSELAGE FWD OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LT FUSELAGE FWD OVERWING EMERGENCY LIGHT IAW CRJ 200 AMM 33-51-00. (B) 2 L 7 2 4F RT A21EA 20080905 EA 2008 9 5 TRAX200800815 1 20080621 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 SUSPECTED CRACK IN AFT LOWER LEG OF FS 280 FRAME AT RBL 12. WORK COMPLETED IN ACCORDANCE WITH: PERFORMED EDDY CURRENT INSPECTION OF SUSPECT AREA IAW CRJ 200 NDTM 61-20-06 PART 1 AND CONFIRMED CRACK MB7011995 06-21-08. PERFORMED EDDY CURR ENT INSPECTION OF CUT LINE IAW CRJ 200 NDTM 61-20-06 PART 1 AND NO CRACK NOTED MB7011995 06-21-08. (B) 2 L 7 2 4F RT A21EA 20080905 EA 2008 9 5 TRAX200800610 1 20080508 A 2613 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA NACELLE MALFUNCTIONED A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 874AS 7551 ON CLIMBOUT RECEIVED A 14TH STAGE BLEED DUCT MSG FOLLOWING THE QRH THE MSG WENT AWAY THEN CAME BACK ABOUT 30SEC LATER. RETARDED THE LEFT ENGINE LANDING SINGLE ENGINE CONFIGURATION. LANDING WEIGHT WAS APPROX 48,500 LBS. ALSO NOTED HYD 1 P RESSURE READOUT WAS 0 PSI. EN ROUTE TO ATL A/C DIVERTED TO MCO DUE TO MTC, EMERGENCY DECLARED. REMOVED AND REPLACED LT 14TH STAGE PYLON LOOP IAW CRJ 200AMM 36-21-04. OPS AND LEAK CHECK GOOD. SEE AFDL 378520 ITEM 1 FOR OVERWEIGHT LANDING . SEE AFDL 378519 ITEM 3 FOR CORRECTIVE ACTION FOR HYD SYSTEM 1. (B) 2 L 7 2 4F RT A21EA 20080905 EA 2008 9 5 TRAX200800871 1 20080630 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 861AS 7445 PAX DOOR HANDLE SUPPORT WELLS ARE CORRODED AT FS 319 AND FS 33, LBL 45. REMOVED PAX DOOR HANDLE SUPPORT WELLS. STARTED PICKING UP EXISTING HOLES IN NEW PAX DOOR HANDLE SUPPORT WELLS IAW CRJ 200 SRM 51-42-06 SP7025126 7/02/08. (B) 2 L 7 2 4F RT A21EA 20080905 EA 2008 9 5 TRAX200800658 1 20080518 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 907EV 7648 FS 621 RT SIDE FLOORBEAM ANGLE IS CRACKED AT RBL 40. REPAIRED PREVIOUS REPAIR AT FS 621 RT. LOCATED AND DRILLED NEW AN GLE AND REPAIR ANGLE IAW SRM 51-40-11. INSTALLED ANGLES IAW REO 601R-53-61-117 REV C. LEAK CHECK DUE. PERFORMED LEAK CHECK OF THE RT 621 FLOORBEAM ANGLE IAW AMM 21-32-00-863-801. LEAK CHECK GOOD AT THIS TIME. REPAIRED RT FS 621 FLOOR S UPPORT ANGLE IAW REO 601R-53-61-117 REV C AND REO 601R-53-61-117. 2 L 7 2 4F RT A21EA 20080905 EU 2008 9 5 TRAX200800659 1 20080518 A 3350 LIGHT AEROSP ATR72 ATR72212 8680945 EU PAX DOORWAY INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 PAX DOOR EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW ATR 72 JIC 33-51-04. CHECKED G OOD. (B) 2 H 7 2 4T RT A53EU 20080905 EA 2008 9 5 TRAX200800667 1 20080519 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 929EV 8007 INTERCOSTAL CRACKED RT FS 621.0-625.0 IN RADIUS APPROX 1 INCH IN LENGTH. REMOVED CRACKED ANGLE AND INSTALLED NEW SERVIC EABLE PART IAW SRM 51-42-06. (B) 2 L 7 2 4F RT A21EA 20080905 CE 2008 9 5 PI82008F00000 1 20080718 A 8120 4066109025 TURBOCHARGER CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO RT ENGINE FAILED A PI8A O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 EA 17 5205J 402B0892 2082027E 931952 TURBOCHARGER FAILED IN FLIGHT AT CRUISE. (A) 1 L 7 2 3O 3 O A7CE E8CE 20080905 EA 2008 9 5 TRAX200800666 1 20080519 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 929EV 8007 LT INTERCOSTAL CRACKED, FS 621.0-625.0 IN RADIUS APPROX 1 INCH IN LENGTH. REMOVED CRACKED ANGLE AND INSTALLED NEW SERVI CEABLE PART IAW SRM 31-42-08. (B) 2 L 7 2 4F RT A21EA 20080905 EA 2008 9 5 TRAX200800873 1 20080704 A 3230 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 905EV 7632 AFTER T/O "GEAR DISAGREE WARNING MESSAGE. AIRCRAFT RETURNED TO CLE AFTER T/O. EMERGENCY DECLARED. REMOVED AND REPLACE D NOSE LANDING GEAR PRIORITY VALVE IAW CRJ 200 AMM 32-30-01, OPS CHECK AND LEAK CHECK GOOD, DEFERRED CLEAR OK FOR SERVIC E. (B) 2 L 7 2 4F RT A21EA 20080905 EA 2008 9 5 TRAX200800764 1 20080605 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS484 RBL 27-36 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 684BR 7708 RIGHT FS 484 INTERCOSTAL AT RBL 27.00 AND RBL 36.00 IS CRACKED .25 INCH. REMOVED CLIP FROM FS 484.00, RBL 27.00 AND INS TALLED NEW SERVICEABLE CLIP ON INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND CRJ 200 SRM 51-40-11. CUT AWAY DAMAGED FLANGE AT RBL 36.00, FABRICATED NEW ANGLE FROM S MATERIAL AND INSTALLED ANGLE IAW BAS REO. (B) 2 L 7 2 4F RT A21EA 20080905 EA 2008 9 5 TRAX200800879 1 20080705 A 3350 CHARGER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 REFER TO AFDL 380596 NR 1 CABIN EMERGENCY SIGN INOP. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY CHARGER ASSY AS PER AMM 33-51-17, OPS CHECK AS PER AMM 33-51-17. (B) 2 L 7 2 4F RT A21EA 20080905 NM 2008 9 5 2008UALA03925 1 20080719 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 326UA 23958 AFT SECTION OF EEL STRIP LIGHTING INOP. REPLACED AFT EEL STRIP CABLE. OPS CKS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 20080905 NM 2008 9 5 2008UALA03888 1 20080712 A 3510 232N800198 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CAPTAIN'S DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 MIC ON CAPT O2 MASK HAS FRAYED WIRE. NEEDS TO BE REPLACED. *S/D* REPLACED CAPT O2 MASK ASSY, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080905 NM 2008 9 5 2008UALA03952 1 20080723 A 5310 STRUCTURE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 180UA 25224 DAMAGE FOUND ON FUSELAGE. LOCATION IS APPROX 2 FEET AFT OF DOOR 5L AND TWO FEET UP FROM BOTTOM OF DOOR. MAJOR REPAIR A CCOMPLISHED: CUTOUT DAMAGE. HFEC INSP OF AREAS AROUND CUTOUT OF DAMAGE REMOVAL. NO CRACKS FOUND. MFG & INSTALLED REPAIR DOUBLER & SOLID FASTENER. 2 L 7 4 4F 4 F RT A20WE E24NE 20080905 EU 2008 9 5 2008UALA03890 1 20080717 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 41UA 751 FUSELAGE DENT FRAME 30 STRINGER 25R. *S/D* ACCOMPLISHED MAJOR REPAIR AT LCQ. INSTALLED DOUBLER REPAIR PER SRM 53-21-1 1. 2 L 7 2 4F 4 F RT A28NM E40NE 20081202 EU 2008 12 2 YENA200811190114 1 20081118 A 3260 893301 PROXIMITY SENSOR AIRBUS 320 A320232 3930326 EU MLG FAULTY A YENA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 EA 15 510JB 590 1280 FLT 185, JFK-SAN, DIVERTED TO PIT, LEVEL FLT 34,000FT, ENG 1 REVERSER FAULT. NAV TCAS FAULT. ANTI-ICE F/O PITOT PROBE FAULT ILLUMINATED IN SERIES. CONTACTED MX CONTROL. PER QRH REDUCED ENG TO IDLE. CONTINUED TO PIT. FOUND MLG EXTENSIO N MLG EXTENSION PROX SENSOR 20GA FAULTING. REMOVED AND REPLACED PROX SENSOR GA IAW A320 AMM 32-31-73-04 TESTED SYSTEM I AW A320 AMM 32-69-00-05. ALL TESTS GOOD. NO FAULTS INDICATED. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 YENA20081114110 1 20081113 A 3350 1012881 LIGHT AIRBUS 320 A320232 3930326 EU CABIN INOPERATIVE A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 580JB 20792 2136 EMERGENCY LIGHT AT SEAT 25ABC IS OUT. REMOVED AND REPLACED EMERGENCY LIGHT ASSY AT SEAT ROW 25ABC PER 33-51-18. OPERAT ION CHECK OK. 2 L 7 2 4F RT A28NM 20081202 NM 2008 12 2 USAA2008112892139 1 20081112 A 5320 143N51951 ANGLE BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 904AW 23566 MCN - C12 - MAJOR REPAIR - WEB VERTICAL ANGLE CRACKED AT BS 680, RBL 45.5. REPAIRED WEB VERTICAL ANGLE AT BS 680, RBL 4 5.5 IAW B757 SRM 51-40-02-0G & BOEING DRAWING 143N5195. 2 L 7 2 4F RT A2NM 20081202 EU 2008 12 2 USAA2008112892150 1 20081114 A 5315 D53472284008 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR67, -Y460. REPLACED FLOORBEAM BETWEEN FR66 TO FR67, -Y460 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008112892152 1 20081114 A 5315 D53472188204 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT FR67 +18 INCHES, Y1162. REPLACED FLOORBEAM AT FR67 +18 INC HES, Y1162 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008112892153 1 20081114 A 5315 D5347217220400 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT FR67 +16 INCHES, Y1195. REPLACED FLOORBEAM AT FR67 +16 INC HES, Y1195 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081202 EU 2008 12 2 USAA2008112892155 1 20081126 A 5610 NP1653115 WINDSHIELD AIRBUS A319 A319112 3930323 EU FUSELAGE CRACKED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 705UW 19793 2985 929 FLT 1660 - CLT-BNA - AIR TURNBACK - CAPTAIN WINDSHIELD ARCED AND THEN CRACKED SHORTLY AFTER TAKEOFF. WINDSHIELD SHATTER ED IMMEDIATELY. REPLACED CAPTAIN WINDSHIELD. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081202 NM 2008 12 2 UALA2008112106604 1 20081118 A 3810 2920016101 VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE WATER SYSTEM MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 777UA 26916 NO WATER PRESSURE THROUGHOUT ACFT. FLIGHT DIVERTED. REPLACED PRESELECT OVERFLOW (V38102) ON ACCOUNT NOT FULLY CLOSING. WATER SYS PRESS CHECKS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081202 NM 2008 12 2 UALA2008112106609 1 20081120 A 3020 2790583108 ANTI-ICE VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 598UA 28751 WHEN LT ENG ANTI-ICE SWITCHED ON, VALVE INTRANSIT LIGHT FAILED TO COME ON BRIEFLY. REPLACED TAI VALVE. TESTED, WORKS F INE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081202 NM 2008 12 2 UALA2008112106612 1 20081121 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 FUSELAGE DENTED FROM STA 850-930 UP TO 0.125 DEEP. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 20081202 NM 2008 12 2 UALA2008112106613 1 20081121 A 7110 NOSE COWL BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 ENGINE DENTED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 769UA 26921 BIRD STRIKE NR 2 ENGINE INLET COWL AT 1 O'CLOCK POSITION. BAD COWL REMOVED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081202 NM 2008 12 2 UALA2008111305434 1 20080823 A 3350 363674 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 ROW 9 LT EEL STRIP INOP. REPLACED STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 20081202 NM 2008 12 2 UALA2008111306212 1 20081022 A 3010 RELAY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ANTI-ICE SYSTEM FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 654UA 25392 CREW REPORT: WING ANTI ICE DISAGREEMENT L-R. ACP T-S REF MM30-11-00 PG1 04 FIG 103 AND WD 30-11-11, REPLACED RELAYS K4 14, K520, K1156 AND K1155. REPLACED TEST SWITCH ON P61 PANEL. ALL TESTS AND OPS CHECKS SATISFACTORY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081202 NM 2008 12 2 UALA2008111305436 1 20080823 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 LT MID LAV EEL STRIP INOPERATIVE. REPLACED CROSS AISLE LIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022900023 20080229 00023 EA 2008 2 29 TRAX200800276 1 20080217 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 846AS 7328 EXIT PLACARD MISSING FROM INTERIOR ASD. FLT 4330 DEL 35 MINS. 2 L 7 2 4F RT A21EA 2008022900081 20080229 00081 EA 2008 2 29 TRAX200800294 1 20080221 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 331CA 10061 AFT SIDE EMERGENCY EXIT LIGHT CENTERLINE AT WING EXIT IS NOT ILLUMINATING. 2 L 7 2 4F RT A21EA 2008022900097 20080229 00097 2008 2 29 SWIA200819243 2 20080216 A 7200 ENGINE CNDAIR CL600 CL6002C10 1390015 EA LEFT FLUCTUATES A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 778SK 10242 FLT 5996 - OIL TEMPERATURE INDICATIONS ON LEFT ENGINE WERE FLUCTUATING IN FLIGHT. REPLACED LEFT ENGINE ASSEMBLY IAW CRJ MM 71-00-00. OPS CHECK GOOD, PN: CF34-8C5B1 SN OFF: 194323. 2 L 7 2 4F RT A21EA 2008022900116 20080229 00116 NM 2008 2 29 DLM88080266 1 20080213 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 DURING HMV, CORROSION WAS FOUND ON AFT CARGO COMPARTMENT DOOR JAMB DOUBLER AT STA Y=1154 P/N 5936433-5 BETWEEN LONGERONS 30 AND 29 RT. A REPAIR WAS PERFORMED IAW DWG AMR0953586 R2 DATED ON 15 JAN 08. 2 L 7 2 4F RT A6WE 2008022900129 20080229 00129 EA 2008 2 29 TRAX200800301 1 20080221 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 858AS 7417 AAR - FUSELAGE FRAME AT FS 333.0 HAS CORROSION BL 0 TO LBL 9. 2 L 7 2 4F RT A21EA 2008022900141 20080229 00141 NE 2008 2 29 MASA200800131 2 20080214 A 7261 4018T16P04 GARLOCK SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT ENGINE DEFECTIVE A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 75991 7422 872783 ASH FLT 7423 MDT-ORD, LEFT ENGINE OIL PRESSURE FLUCTUATING WARNING. CREW REDUCED THROTTLE AND PRESSURE STABILIZED. DEC LARED EMERGENCY. REPLACED STARTER GARLOCK SEAL. 2 L 7 2 4F 4 F RT A21EA E15NE 2008022900158 20080229 00158 NM 2008 2 29 GTIA0800020 1 20080109 A 5320 INTERCOSTAL AIRBUS A321 A321231 3940032 NM BS 4059 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 FS 4059 LT MOST OB INTERCOSTAL HAS CORROSION. REPLACED INTERCOSTAL. 2 L 7 2 4F RT A28NM 2008022900162 20080229 00162 NM 2008 2 29 QXEA200800225 1 20080220 A 3231 ROD END BOMBDR DHC8 DHC8402 1390042 NM MLG DOOR MISINSTALLED A QXEA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 NM 09 411QX 4055 PSC- FLIGHT 2297 - ON GEAR RETRACTION, THE LT MLG DOOR AMBER LIGHT REMAINED ILLUMINATED. COMPLIED WITH THE CHECKLIST. MTX CONTROL REQUESTED A DIVERSION TO PDX. ACCOMPLISHED AN ALTERNATE EXTENSION AND A UNEVENTFUL LANDING. MAINTENANCE RE MOVED THE NR 1 RETRACT ACTUATOR AT THE SHOCK STRUT AND A YOKE. USING RIG TOOL FOUND THE ROD END INCORRECTLY INSTALLED I N THE PISTON. THREADED ROD END TWO FULL TURNS INTO PISTON TO ACHIEVE DIMENSIONS IN CMM 32-31-06 PAGE 703. TORQUED AND SAFETIED ROD END JAM NUT. REINSTALLED ACTUATOR, DID 15 GEAR SWINGS WITH NO DEFECTS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008022900189 20080229 00189 EA 2008 2 29 MASA200800139 1 20080217 A 5210 601R319119 STRUT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DEFECTIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17358 7358 FLT 2985, PHX - PILOT REPORTED THAT THE PAX DOOR FREE FALLS WHEN OPENED. REMOVED AND REPLACED FWD DOOR STRUT. 2 L 7 2 4F RT A21EA 2008022900198 20080229 00198 EA 2008 2 29 MASA200800155 1 20080219 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17358 7358 ASH FLT 2741 PHX - PSP, DURING PREFLIGHT CAPT FOUND THE OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED THE OVERHEA D EMERGENCY LIGHT, OPS GOOD. 2 L 7 2 4F RT A21EA 2008022900200 20080229 00200 EA 2008 2 29 TRAX200800307 1 20080222 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA CABIN WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 877AS 7579 ASD EXIT PLACARD WORN. 2 L 7 2 4F RT A21EA 2008022900206 20080229 00206 EU 2008 2 29 08FDEA00615 1 20080226 A 5320 A5398111320051 INTERCOSTAL AIRBUS 310 A310324 3930206 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 .25 INCH CRACK IN MAIN CABIN INTERCOSTAL BETWEEN FRAME 79 AND FRAME 80/82 AND STRINGER 26L. REMOVED AND REPALCED WEB IA W A310-300 SRM 51-20-41. MINOR REPAIR 2 L 7 2 4F RT A35EU 2008030300003 20080303 00003 WP 2008 3 3 08FDEA00650 1 20080228 A 5321 AFA38585 FLOOR PANEL DOUG DC10 DC1030 3023501 WP BS 1521-1601 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 CENTER PIT PANEL "183 BG" IS PUNCTURED. FABBED NEW FLOOR PANEL 183 BG IAW DWG SRZ 25-005 REV E. MAJOR REPAIR. 2 L 7 3 4F A22WE 2008030300010 20080303 00010 WP 2008 3 3 AALA200800374 1 20080221 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 417AA 49328 DFW - EMERGENCY LIGHT AT LEFT EXTERIOR OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT EXTERIOR OVERWIN G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300040 20080303 00040 NM 2008 3 3 08FDEA00648 1 20080228 A 5330 6554574 SKIN BOEING 727 727227 1384078 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 FOUND FUSELAGE SKIN CORROSION AT FS 582, STR 28L, AFTER REMOVING WEB ON SNRM N00557 FOUND SERIES OF MISDRILLED HOLES ALO NG INTERCOSTAL NEAR BOTTON EDGE OF MAIN CARGO DOOR DOUBLER COMPLIED WITH EA NR 7-5330-118244 PART NR 1. REMOVED INTERNA L STRUCTURE TO GAIN ACCESS. REMOVED DAMAGE AND CORROSION, FABRICATED REPAIR DOUBLER/FILLERS. TREATED PRIMED AND INSTAL LED, REF SRM 53-30-3. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008030400005 20080304 00005 NM 2008 3 4 2008UALA00849 1 20080215 A 2910 7G7542 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE PRESSURE TRANSMI INTERMITTENT A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 548UA 25396 CENTER HYD "RSVR" LIGHT ILLUMINATED. PRESSURE TRANSMITTER SWITCH INTERMITTENT. REPLACED PRESSURE TRANSMITTER SWITCH, O PS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030400034 20080304 00034 NM 2008 3 4 DHL2008749003 1 20080114 A 5322 SHEAR TIE BOEING 727 727223 1384074 NM BS 720F CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 FORWARD CARGO COMPARTMENT SHEAR TIE AND FRAME CORRODED AT FORWARD SIDE OF BS 720F STRINGER 25L. REMOVED SHEAR TIE IAW S RM 51-30-2. CLEANED SKIN AREA IAW MM 12-40-00, NO CORROSION NOTED. FABRICATED NEW SHEAR TIE IAW SRM 53-10-2 FIGURE 3, 51-20-2 AND 53-10-4 FIGURE 15. ALODINED AND PRIMED PART IAW SRM 51-10-2. INSTALLED SHEAR TIE IAW SRM 51-30-2 AND 53-10- 4 FIGURE 15. 2 L 7 3 4F A3WE 2008030400035 20080304 00035 NM 2008 3 4 DHL2008749004 1 20080114 A 5322 SHEAR TIE BOEING 727 727223 1384074 NM BS 680 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 FORWARD CARGO COMPARTMENT SHEAR TIE CORRODED AT FORWARD SIDE OF BS 680 FRAME AND STRINGER 26R. REMOVED CORRODED SHEAR T IE IAW SRM 51-30-2. CLEANED AREA AROUND SHEAR TIE IAW SOPM 20-30-3. NO DEFECTS NOTED IAW SRM 51-10-6 PARA 3. FABRICAT ED NEW SHEAR TIE IAW SRM 53-10-2 FIGURE 3, 51-20-1, AND 51-305. ALODINED AND PRIMED PART IAW SRM 51-10-2. INSTALLED SH EAR TIE IAW SRM 51-30-2 AND 53-10-4 FIGURE 15. 2 L 7 3 4F A3WE 2008030400045 20080304 00045 NM 2008 3 4 08FDEA00538 1 20080220 A 5246 1060031116 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 WING FUEL PANEL 641GB HAS SURFACE CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORD ERED AND RECEIVED NEW PANEL. 2 L 7 2 4F RT A2NM 2008030400053 20080304 00053 NM 2008 3 4 2008UALA00905 1 20080218 A 5310 STRUCTURE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE BS 610 S31L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 671UA 30026 FUSELAGE DAMAGED AT APPROX STRINGER 31L STA 610, DENT APPROX .097 DEEP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030400057 20080304 00057 NM 2008 3 4 DL76L080194 1 20080213 A 3350 BATTERY PACK BOEING 767 767332 1382001 NM EMERGENCY LIGHTS INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 196DN 28453 3 EXTERIOR EMERGENCY LIGHTS INOP, 2 AFT OF RIGHT WING AND R2 DOOR. REPLACED BATTERY PACK. OPS CK GOOD. 2 L 7 2 4F RT A1NM 2008030400061 20080304 00061 NM 2008 3 4 08FDEA00529 1 20080220 A 5246 1060031120 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 WING FUEL PANEL 643AB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 643AB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-120. 2 L 7 2 4F RT A2NM 2008030400063 20080304 00063 NM 2008 3 4 08FDEA00531 1 20080220 A 5730 112N61015 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 WING FUEL PANEL 641MB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 641MB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 112N6101-5. 2 L 7 2 4F RT A2NM 2008030400064 20080304 00064 NM 2008 3 4 08FDEA00539 1 20080220 A 5730 1060031116 PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 WING FUEL PANEL 641KB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 641KB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-116. 2 L 7 2 4F RT A2NM 2008030400069 20080304 00069 NM 2008 3 4 DLM90080231 1 20080217 A 5320 PAN DOUG MD90 MD9030 3023690 NM CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 2 AREAS OF CORROSION AT RIVNUTS ON LWR PORTION OF FWD CARGO DOOR JAMB AT MIDDLE AND AFT END. REPAIRED CARGO DOOR JAMB, IAW MD80 SRM 53-08D FIG 44. 2 L 7 2 4F RT A6WE 2008030400075 20080304 00075 NM 2008 3 4 2008UALA00856 1 20080218 A 3210 LANDING GEAR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 175UA 24382 RTFL DUE TO A PROBLEM WITH LANDING GEAR RETRACTION. REPLACED RIGHT HAND BODY GEAR TRUCK TILT POSITION ACTUATOR. OSV SHO P - NO SHOP DATA FOR ROOT CAUSE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030400077 20080304 00077 NM 2008 3 4 2008UALA00858 1 20080217 A 3350 LAMP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 817UA 873 2R AISLE EMERGENCY LIGHT INOP. LAMP IS OUT IN ASSY. RELAMPED DOOR 2R, ALL OPS CHECKS ARE GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030400080 20080304 00080 EA 2008 3 4 SWIA200819220 1 20080208 A 2497 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA ARCED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 PIN E ON J141 SHOWS SIGNS OF ARCING. REPLACED CONNECTOR. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2008030400081 20080304 00081 EA 2008 3 4 SWIA200819221 1 20080212 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCONNECTED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 460SW 7803 FLOOR EMERGENCY LIGHT STRIP PLUG IS LOOSE, FLIGHT NR 3901. SECURED LIGHT STRIP CONNECTORS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008030400087 20080304 00087 NM 2008 3 4 DLM90080242 1 20080218 A 5310 BEAM DOUG MD90 MD9030 3023690 NM CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 CORROSION ON LWR LEG OF MID CARGO DOOR BEAM IN NUMEROUS PLACES ENTIRE LENGTH. REPAIRED DOOR BEAM, IAW MD80 SRM 53-05D F IG 63. 2 L 7 2 4F RT A6WE 2008030400089 20080304 00089 NM 2008 3 4 HALA0800259 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1339 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1339, AREA HAS BEEN REWORKED BEFORE. SEAT TRACK REPLACED PE R SRM. 2 L 7 2 4F RT A1NM 2008030400092 20080304 00092 NM 2008 3 4 HALA0800256 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1288 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON SEAT TRACK AT LBL 88.5, STA 1288, AREA HAS BEEN REWORKED BEFORE. SEAT TRACK REPLACED PER SRM. 2 L 7 2 4F RT A1NM 2008030400094 20080304 00094 NM 2008 3 4 HALA0800223 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 794 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT RBL 11, STA 794, MAX DEPTH OF BLEND OUT WAS 0.009". BLENDED IAW SRM 51-10- 02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008030400095 20080304 00095 NM 2008 3 4 HALA0800257 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1305 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1305, AREA HAS BEEN REWORKED BEFORE. SEAT TRACK REPLACED PE R SRM. 2 L 7 2 4F RT A1NM 2008030400105 20080304 00105 NM 2008 3 4 AALA200800268 1 20080208 A 3230 S293W1202 BYPASS VALVE BOEING 777 777223 1385213 NM NLG INOPERATIVE A AALA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 794AN 30256 LHR INFLIGHT T131/08FEB - NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO LHR AND LANDED WITHOUT INCIDEN T. REPLACED NOSE LANDING GEAR SELECTOR BYPASS VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008030400110 20080304 00110 NM 2008 3 4 HALA0800182 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION AT RBL 54.75, SEAT TRACKS AT STA 1197+49, BASE OF TRACK. CORROSION REMOVED PER SRM 51-10-02, REV 76 A ND SRM 53-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030400118 20080304 00118 EU 2008 3 4 2008UALA00861 1 20080215 A 2620 30903886 SQUIB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FIRE BOTTLE FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 431UA 571 'ENG FIRE EXTINGUISHING-SQUIB' LIGHT OF 'AGENT 1' PUSHBUTTON SWITCH IS OFF DURING 'LOOP-SQUIB TEST'. SQUIB IS FAULTY. REPLACED SQUIB, ALL OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030400125 20080304 00125 WP 2008 3 4 IXXA08SMN004S 1 20080114 A 5730 PANEL DOUG DC8 DC862 3021970 WP LT WING DELAMINATED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LOWER PANEL DELAMINATED AT STATION XF 219 TO XF 339.000. REMOVED DAM AGED PANEL. INSTALLED NEW PANEL IAW DC8 SRM 51-3-0, 51-3-1. 2 L 7 4 4F 4A25 2008030400129 20080304 00129 EU 2008 3 4 TRBA2008022 1 20080211 A 6120 30048000018 CONTROL UNIT AEROSP AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RT ENGINE MALFUNCTIONED A TRBA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 29 308AE 262 309 NR 2 ENGINE TQ WENT DOWN TO 0 PERCENT, NP TO 0 PERCENT AND THE ENGINE SHUT DOWN BY ITSELF. REMOVED AND REPLACED MULTI-F UCTION COMPUTER (MFC) IAW JIC NR 31-48-81. REMOVED AND REPLACED TORQUE SIGNAL CONTROL UNIT(AFU) IAW JIC NR 77-13-62. P ERFORMED GROUND POWER RUN-UP IAW W/C 055007-CS-20000-001. 2 H 7 2 4T 4 T RT A53EU E20NE 2008030400135 20080304 00135 EU 2008 3 4 2008UALA00868 1 20080218 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN ODOR A UALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 WP 29 464UA 1290 ON T/O, CABIN AND GALLEY BURNING ODOR DECREASED BY FL 180, RETURNED ON DESCEND FR 10-6K FT. NEW HEAT EXCHANGERS INSTALL ED PRIOR TO FLIGHT- SUSPECT SLIGHT ODOR FROM NEW EQUIPMENT (NORMAL). RAN PACKS AT FULL HOT FOR 15 MINUTES AND COULD ONL Y DETECT SLIGHT ODOR SUSPECT BURNOFF OF NEW HEAT EXCHANGERS INSTALLED JUST PRIOR TO FLIGHT. CKD E/E COMPARTMENTS, NO DE FECTS OR BURNING NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030400136 20080304 00136 NM 2008 3 4 2008UALA00869 1 20080216 A 3350 SIGN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE L2 DOOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 928UA 26651 EMERGENCY EXIT LIGHT SIGN DOES NOT ILLUMINATE AT DR 2 LEFT AND RIGHT. REPLACED DOOR 2 RIGHT LOWER EMERGENCY EXIT SIGN, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030400137 20080304 00137 NM 2008 3 4 2008UALA00871 1 20080217 A 5321 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 664 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 PRESSURE DECK AT BS 664 IS CRACKED ON FWD EDGE OF CORRIGATION LBL32. INSTALLED EXTERNAL DOUBLER & FILLER REPAIR COMMON TO PRESSURE DECK IAW MM 53-21-98. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030400147 20080304 00147 NM 2008 3 4 DLM88080260 1 20080213 A 2560 LATCH DOUG MD88 MD88 3023688 NM GIRT BAR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 CORROSION ON GIRT BAR LATCH SUPPORT STA Y=1140 X=57 LT SIDE, NEW SUPPORT WAS INSTALLED IAW BOEING DWG 9930612. 2 L 7 2 4F RT A6WE 2008030400156 20080304 00156 NM 2008 3 4 08FDEA00617 1 20080226 A 5320 143N54103 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 FLOOR SUPPORT BY THE L2 DOOR, STA 700-720, LBL 60, WL208 HAS CORROSION. REMOVED CORROSION FROM FLOOR SUPPORT, L=12.0, W= 1.7, D=0.015, ORIGINAL MATERIAL THICKNESS = 0.063. FOUND TO BE OUT OF SRM 53-00-51, FIG 101, DETAIL II AND III LIMITS. REMOVED AND REPLACED FLOOR SUPPORT (U CHANNEL) IAW SRM 51-40-02. REPLACEMENT PART FABRICATED ON MAE TRAVELER T7/713364 FROM 7075-0, 0.056B, HEAT TREATED TO T6 IAW SRM 51-10-02. 2 L 7 2 4F RT A2NM 2008030400159 20080304 00159 NM 2008 3 4 DLM88080243 1 20080219 A 7921 OIL COOLER DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE UNKNOWN A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 923DL 49705 725552 NR 1 ENG GEN/CSD OIL TEMP RUNNING IN YELLOW BAND IN CLIMB AND UPON REACHING RED BAND AT TOP OF CLIMB DISCONNECTED CSD. APU GEN ALREADY ON MCO- DIVERTED TO IAD. REMOVED AND REPLACED LEFT CSD AND GENERATOR PER AMM 426246 ENGINE DISCONNECT A ND RECONNECTED CSD LOADED A/C WITH ELECT REMOVED AND REPLACED LEFT ENG CSD OIL COOLER REF MM 71139. 2 L 7 2 4F 4 F RT A6WE E9NE 2008030400161 20080304 00161 SO 2008 3 4 SIMA200805106 1 20080218 A 3260 23092900001 UPLOCK EMB 145 EMB145LR 3260212 SO RT MLG INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 611AE 145074 ON FLIGHT 4104, CREW REPORTED RIGHT MAIN LANDING GEAR DID NOT SHOW UP AND LOCKED ONLY IN TRANSIT. CREW RETURNED TO MQT WITH NO FURTHER INCIDENTS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR UPLOCK BOX IAW EMB AMM 32-33-10 AND NR 8194;AND NR 8194;AND NR 8194; AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20080905 EU 2008 9 5 2008UALA03891 1 20080718 A 5320 PAN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR SILL DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 449UA 851 EXCESSIVE MATERIAL REMOVED FROM DOOR 2L DOOR SILL PAN AFT END AT 2EA NUT PLATE HOLES. *S/D* ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED DAMAGE MATERIAL, FABRICATED REPAIR PARTS. 2 L 7 2 4F 4 F RT A28NM E40NE 20080905 NM 2008 9 5 2008UALA03892 1 20080717 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 740-760 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 LEFT EXTERNAL FUSELAGE BETWEEN STA 740 AND 760 BETWEEN STR 15L AND 16L FUSLAGE SKIN HAS 3 DENTS IN ONE BAY REQUIRES SRM EVAL. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. REPAIRED IAW REO G12160 AN D EVA 70752 REPAIR IS INTERM PENDING COMPLET ION OF FATIGUE AND DTA BY OEM BOEING WHICH IS DUE BY 17OCT08 AIRCRAFT IS NOT AIRWORTHY AFTER 17OCT08 WITHOUT A NEW FAA F ORM 8100-9. 2 L 7 2 4F 4 F RT A2NM E17NE 20080905 NM 2008 9 5 2008UALA03893 1 20080717 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 520 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 DENT IN UPPER LEG (INBOARD FLANGE) OF FUSELAGE FRAME BS 520, LBL 36. *S/D* ACCOMPLISHED A MAJOR REPAIR AT GSO. TRIMME D OUT DAMAGE TO FRAME INNER FLANGE, REMOVED EXISTING PRODUCTION SPLICE, FABRICATED AND INSTALLED A REPAIR J-ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080905 EU 2008 9 5 NSV2008F00013 1 20080724 A 2697 CONNECTOR SAAB SF340 340B 7860101 EU FIRE LOOP DIRTY A NSVA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 27 338CJ 340B338 TAIL PIPE NOT ILLUMINATED. CLEANED SENSOR LOOP CONNECTORS. ENGINE RUN UP AND OPS CHECKS GOOD IAW AMM 26-11-00-06. (A) 2 L 7 2 4T RT A52EU 20080905 SO 2008 9 5 SIMA200821001 1 20080726 A 2930 300045021 THERMAL SWITCH EMB 145 EMB145LR 3260212 SO HYD OVERHEAT FAILED A SIMA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 SW 21 635AE 145158 ON FLIGHT 3839 CREW REPORTED AT CRUISE NUMBER 2 HYDRAULIC SYSTEM OVERHEAT FOLLOWED BY NUMBER 2 HYDRAULIC SYSTEM FAIL. A FTER AOM COOL DOWN PERIOD INITIALLY WOULD NOT TURN ON WITH EICAS SYSTEM OVER HEAT MESSAGE GONE. CREW TRIED 5 MIN LATER AND SYSTEM CAME ON. CREW DECLARED EMERGENCY AND LANDED WITH OUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED HYD RAULIC SYSTEM RESERVOIR 2 THERMAL SWITCH IAW EMB 145 AMM 29-30-05. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE . (A) 2 L 7 2 4T RT T00011AT 20080905 SO 2008 9 5 SIMA200820703 1 20080723 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 935AE 14500920 ON FLIGHT 3574 CREW REPORTED ALL EMERGENCY LIGHTS LT ON AND WILL NOT TEST. AIRCRAFT REMOVED FROM SERVICE. REPLACED ALL EMERGENCY BATTERIES IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080902 NM 2008 9 2 SWAA084453 1 20080812 A 5311 6546541 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084452 1 20080812 A 5311 6546541 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, BETWEEN STR 2R AND STR 3R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080902 2008 9 2 USAABB08130 4 20080810 A 2565 BPS73 BATTERY BOEING 767 767201 1385125 NM ESCAPE SLIDE FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246AY 23898 ARN - OPERATIONAL CHECK OF SQUIBS FOR EMERGENCY ESCAPE SLIDES FAILED. MAINTENANCE REPLACED THE RT OFF-WING SYSTEM POWER SUPPLY. OPERATIONALLY AND LEAK CHECKS OK. (S) 2 L 7 2 4F RT A1NM 20080903 NM 2008 9 3 2008UALA03626 1 20080628 A 3040 141T480149 WINDSHIELD AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE WINDSHIELD HEAT SHORTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 801UA 686 ODOR IN COCKPIT, FLIGHT DIVERTED. *S/D* FOUND WHC2 HAD OVERHEATED. REMOVED COVER AND FOUND CHARRED RESISTORS, THIS CA USED BY AN INTERNAL SHORT WITHIN THE RT (F/O) WINDSHIELD. REPLACED WHC2, AND AND F/O WINDSHIELD, ALL OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080903 NM 2008 9 3 QXEA200800347 1 20080330 A 5310 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 356PH 502 PDX-C5 CHECK. CORROSION ON FLANGE AT GALLEY OUTBOARD AFT ATTACH POINT AT STA X227.70. BLENDED SURFACE CORROSION APPROX .001 MATERIAL REMOVED IAW DHC 8 200 SRM. ETCHED, ALODINED AND PRIMED SURFACE IAW DHC 8 200 SRM 51-20-16. (S) 2 H 7 2 4T RT A13NM 20080903 EA 2008 9 3 A6WA200840552 1 20080725 A 2751 601R9310511 SENSOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A A6WA O OTHER F FLT CONT AFFECTED LD LANDING 1 GL 31 448AW 14278 7814 FLAPS FAIL MESSAGE FROM 30 TO 45 ON LANDING. FLAPS FAILED AT 30 DEGREES. REMOVED AND REPLACED LT BRAKE POSITION SENSOR UNIT PER AMM 27-54-01, OPS AND RIG CHECK GOOD. (S) 2 L 7 2 4F RT A21EA 20080903 NM 2008 9 3 QXEA200800351 1 20080330 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 190 S4L DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 356PH 502 BURNED RIVET AT STA X190.00 APPROX 1 INCH BELOW STR 4L. REMOVED RIVET AND FOUND DAMAGE LIMITED TO ONE RIVET ONLY. INST ALLED RIVET IAW D8-200 SRM 51-40-11. (S) 2 H 7 2 4T RT A13NM 20080903 EA 2008 9 3 QXEA200800732 1 20080710 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 909 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 612QX 10042 PDX-C4 CHECK. GOUGE ON RT INBOARD SEAT TRACK AT STATION 909.00. REMOVED GOUGE BY REO 670-53-00-013. REMOVED MATERIAL IS IN LIMITS. HFEC AREA WITH NO CRACKS FOUND. ALODINE AREA. (S) 2 L 7 2 4F RT A21EA 20080903 SO 2008 9 3 C2X2008F00021 1 20080818 A 5330 SKIN EMB 145 EMB145XR 3260214 SO FUSELAGE PUNCTURED A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 16178 14500889 EWR/TYS-ACFT WAS STRUCK IN EWR BY A BELTLOADER AND PUNCTURED THE SKIN UNDER THE CARGO BAY. THE ACFT WAS FERRY FLOWN TO TYS. TYS MAINTENANCE INSTALLED A DOUBLER, FILLER, AND SHIMS ON FUSELAGE SKIN BETWEEN FRAMES 64-65 AND STRINGERS 19L-21L IAW EC 5330-01830. THE PRESSURE CHECK WAS GOOD AND THE ACFT WAS RELEASED TO SERVICE. (S) 2 L 7 2 4F RT 20080903 NM 2008 9 3 ABXA080221 1 20080801 A 5330 148T31311 SKIN BOEING 767 767232 1385132 NM BS 1654 S13L CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 745AX 22222 LT STA 1654.5, 2 EACH SKIN CRACKS STRINGER 13 LT. REPAIRED LT STA 1654.5 AT STRINGER 13 LT ON REA B653-57700. (S) 2 L 7 2 4F RT A1NM 20080903 EA 2008 9 3 VNAA0808008 1 20080815 A 5350 RADOME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 257PS 7939 CREW REPORTED LIGHTNING STRIKE. MAINTENANCE INSPECTED ACFT AND REPAIRED DAMAGE ON RADOME AND LT WINGLET. NO OTHER DEFE CTS NOTED. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080904 NM 2008 9 4 QXEA200800808 1 20080723 A 2611 SMOKE DETECTOR BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY MALFUNCTIONED A QXEA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 09 425QX 4039 PDX - FLIGHT 2388. BAGGAGE AIR SMOKE TEST VALVE INLET LIGHT INTERMITTENTLY CAME ON DURING TEST. (TEST 1 AND 2 POSITION ). VALVE OUTLET DID NOT RESPOND AT ALL. BOTH LAMPS TEST OK. MAINTENANCE CLEANED THE INLET AND OUTLET SCREENS. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. (A) 2 H 7 2 4T RT A13NM 20080904 NM 2008 9 4 QXEA200800703 1 20080701 A 3350 61047811 BATTERY DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHTS FAILED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 347PH 480 PDX - EMERGENCY LIGHTS OCCASIONALLY TURN ON IN ARM MODE, SOMETIMES SETTING OFF SEATBELT SOUND. REPLACED ALL POWER SUPPL IES AND BATTERIES. OPERATIONAL CHECKS GOOD. RETURNED TO SERVICE. (A) 2 H 7 2 4T RT A13NM 20080904 EA 2008 9 4 TRAX200800927 1 20080725 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 MAIN PAX DOOR OUTER HANDLE DIFFICULT TO STOW FROM INSIDE ACFT ON 2 LEGS. COMPLIED WITH INSP OF PAX DOOR OUTER HANDLE, C LEANED AND LUBE. PERFORM OPERATIONAL CHECK GOOD PER AMM 52-11. OK FOR SERVICE. (A) 2 L 7 2 4F RT A21EA 20080904 NM 2008 9 4 PID2008F00007 1 20080714 A 3350 9721055 BATTERY PACK BOEING 737 737291 138448W NM EMERGENCY LIGHTS INOPERATIVE A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 583CC 21069 AFTER REMOVING AND REPLACING ALL 6 EPH BATTERIES. FOR TIME, FOUND 1 BATTERY PACK BAD. REMOVED AND REPLACED BATTERY PAC K, OPS CK GOOD REF STC-SA 3441NM. (A) 2 L 7 2 4F A16WE 20080904 NM 2008 9 4 QXEA200800590 1 20080611 A 3230 483003 SELECTOR VALVE BOMBDR DHC8 DHC8402 1390042 NM MLG MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 405QX 4047 SEA - FLIGHT 2211 (YUR-SEA). AFTER DEPARTURE, LANDING GEAR DID NOT RETRACT. CONTINUED TO SEA GEAR DOWN AND ACCOMPLISHE D AN UNEVENTFUL LANDING. FERRY TO PDX. REPLACED PSEU, NO HELP. REPLACED LG SELECTOR VALVE. OPERATIONAL CHECKS GOOD, RETURNED TO SERVICE. (A) 2 H 7 2 4T RT A13NM 20080904 NM 2008 9 4 DHLA200800076 1 20080623 A 3350 MISCO62 BATTERY PACK BOEING 727 727227 1384078 NM EMERGENCY LIGHT INOPERATIVE A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 783DH 21999 EMERGENCY EXIT LIGHT FOR MAIN ENTRY DOOR INOP. REMOVED AND REPLACED BATTERIES PRE MM 33-50-71, OPS CHECK GOOD P/N MISC0 62. FLIGHT NUMBER 2808. AIRCRAFT WAS GROUNDED. 2 L 7 3 4F A3WE 20080904 2008 9 4 DHLA200800070 4 20080617 A 2312 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 3 NACELLE MALFUNCTIONED A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 807DH 45990 FLT 916 - NR 3 ENGINE FIRE INDICATION IN CRUISE SHUTDOWN PER EMER CHECK LIST AND BLEW BOTH BOTTLES. INDICATION PERSISTE D OFF AND ON. LT BOTTLE SHOWED BLOWN AT SAME TIME AS FIRE. INSPECTED CONNECTORS AT FIREWALL AND INSIDE PYLON CHECKED W IRING ON ENGINE AND TO COCKPIT PER WDM 26-01-01. REPLACED CONNECTOR ON LT AND RT "A" LOOP FAN AND PYLON "A" LOOP CONNEC TOR P/N`S 878239-02, 878238-02. REPLACED LT, RT FIRE LOOPS AND PYLON FIRE LOOPS PER MM 26-10-1. OPS CHECKS NORMAL SEE N EXT LOG PAGE FOR LT, RT ENGINE FIRE BOTTLES REPAIR. AIRCRAFT WAS GROUNDED. (A) 2 OF 3. 2 L 7 4 4F RT 4A25 20080904 CE 2008 9 4 GLB2008F00010 1 20080724 A 3234 CONTROL HANDLE BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A GLBA O OTHER O OTHER NR NOT REPORTED 1 NM 03 255GL UE255 LANDING GEAR EXTENSION-AIRCRAFT N255GL FLIGHT 5212 "STL" - PILOTS REPORTED THE LANDING GEAR RELAY CIRCUIT BREAKER POPPED WHEN GEAR HANDLE WAS PUT TO THE DOWN POSITION. RE-SET, BROUGHT GEAR UP, THE PUMP KICKED IN AND BROUGHT THE GEAR UP. W HEN PUT HANDLE BACK DOWN THE CIRCUIT BREAKER POPPED AGAIN AND USED HAND PUMP TO BRING GEAR DOWN. MAINTENANCE REMOVED AN D REPLACED THE LANDING GEAR CONTROL HANDLE PER 1900D MM 32-30. OPERATIONAL CHECKS WERE GOOD. (A) 2 L 7 2 4T RT A24CE 20080904 NM 2008 9 4 DHL2008F00023 1 20080706 A 5330 SKIN BOEING 727 7272M7 138407S NM BS 931 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 750DH 21951 LT WHEEL WELL BS 931.5 ABOVE STRINGER 18A CORROSION SPOT SKIN BLOWN WBL 70.5. INSTALLED REPAIR PARTS AT LT WHEEL WELL B S 931 5 ABOVE STRINGER 18A AREA WBL 70 5 IAW EVA B253-00083 REV 01 DATED 1 JULY 08 AND AVENGER REPORT AAS-SSR-08-017 REV B DATED JUNE 30, 2008 AND 8110-3 DATED 7-1-08. (A) 2 L 7 3 4F A3WE 20080904 WP 2008 9 4 DHLA200800069 1 20080617 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 3 NACELLE MALFUNCTIONED A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 807DH 45990 FLT 916 - NR 3 ENGINE FIRE INDICATION IN CRUISE SHUT DOWN PER EMER CHECK LIST AND BLEW BOTH BOTTLES. INDICATION PERSIST ED OFF AND ON. LT BOTTLE SHOWED BLOWN AT SAME TIME AS FIRE. INSPECTED CONNECTORS AT FIREWALL AND INSIDE PYLON CHECKED WIRING ON ENGINE AND TO COCKPIT PER WDM 26-01-01. REPLACED CONNECTOR ON LT & RT "A" LOOP FAN AND PYLON "A" LOOP CONNECT OR P/N`S 878239-02, 878238-02. REPLACED LT, RT FIRE LOOPS AND PYLON FIRE LOOPS PER MM 26-10-01. OPS CHECKS NORMAL. SE E NEXT LOGPAGE FOR LT, RT ENGINE FIRE BOTTLES REPAIR. AIRCRAFT WAS GROUNDED. (A) 3 OF 3. 2 L 7 4 4F RT 4A25 20080904 WP 2008 9 4 DHLA200800071 1 20080617 A 2612 898475 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 3 NACELLE SHORTED A DHLA K NONE L NO TEST IN INSP/MAINT 1 SO 01 807DH 45990 ENG FIRE WARNING NR 3 COMPLIED WITH PHASE 1 EMERG CHECKLIST ABNORMAL PROCEDURES AGENT DISCHARGED. INSPECTED ENG, NO FIR E IS LOCATED FAULT AND DETERMINED "A" LOOP P/N 898475 AT FAULT ENTERED ON MEL 26-2-3 DMI 32800 M/C NOTED REMOVED AND REP LACED BOTTLE IAW 26-20-0. NO FIT, A/C WAS GROUNDED. (A) 2 L 7 4 4F RT 4A25 20080904 EU 2008 9 4 NSV2008F00012 1 20080724 A 5410 727110808 COWLING SAAB SF340 340B 7860101 EU NACELLE DAMAGED A NSVA O OTHER O OTHER NR NOT REPORTED 1 EA 27 202SR 340B202 LT ENGINE INBOARD COWLING DAMAGED. REMOVED AND REPLACED LT INBOARD COWLING IAW SAAB MM 71-10-05-08. (A) 2 L 7 2 4T RT A52EU 20080904 WP 2008 9 4 G412008F00002 1 20080617 A 2612 898988C CONTROL UNIT DOUG DC8 DC871F 302199D WP FIRE DETECTION DEFECTIVE E G41A F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 01 830BX 45973 DURING CRUISE FROM KRFD NUMBER ONE ENGINE FIRE BELL AND LIGHT CAME ON, THE CREW ACCOMPLISHED RUN ENGINE FIRE CHECK LIST, THE CREW DISCHARGED ONE AGENT, AND DISCHARGED THE SECOND AGENT AND THE SECOND AGENT WOULD NOT DISCHARGE, THE CREW LANDE D IN KTOL WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NUMBER ONE ENGINE FIRE EXTINGUISHING SYSTEM AND FOUND BROKEN GROU ND WIRE ON STUD, MAINTENANCE CONFIRMED SECOND AGENT DID DISCHARGED. MAINTENANCE ALSO REPLACED FIRE DETECTOR CONTROL UNI T, PYLON FIRE LOOP, CORE FIRE LOOP, LT FIRE ELEMENT, RT FIRE ELEMENT, RT FAN FIRE ELEMENT, AND LT FAN FIRE ELEMENT. OPE RATIONAL CHECK GOOD IAW DC8 MAINTENANCE MANUAL 26-10-4, DC8 MAINTENANCE MANUAL 20-50-1. AIRCRAFT WAS RETURNED TO SERVIC 2 L 7 4 4F RT 4A25 20080904 EA 2008 9 4 TRAX200800609 1 20080507 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BENT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 928EV 8006 THE PAX DOOR EXTERIOR HANDLE IS CRACKED AND THE FLAP HANDLE IS BENT. REMOVED AND REPLACED CRACKED PAX DOOR OUTER HANDLE WITH A NEW SERVICEABLE OUTER HANDLE IAW BOMBARDIER SB 601R-52-119 REV. A. REMOVED AND REPLACED BENT/CRACKED PAX DOOR OU TER HANDLE FLAP WITH A NEW SERVICEABLE FLAP IAW SRM 51-42-06. . OPS TEST DUE AND PAIN REQUIRED. PAINTED HANDLE ON PAX DO OR TO MATCH COLOR SCHEME IAW SRM 51-25-01. OPS TEST DUE. PERFORMED OPS TEST OF THE PAX DOOR OUTER HANDLE IAW AMM 52-11- 03-710-802. OPS CHECK IS GOOD AT THIS TIME. (A) 2 L 7 2 4F RT A21EA 2008030400162 20080304 00162 EA 2008 3 4 SIMA200805107 1 20080218 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA CABIN SMOKE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 21 518AE 10126 ON FLIGHT 3663, CREW REPORTED SMOKE IN THE CABIN, PASSENGERS CONFIRMED VISIBLE SMOKE. AIRCRAFT REMOVED FROM SERVICE. G ROUND RAN AIRCRAFT IN VARIOUS POWER CONFIGURATIONS USING BOTH ENGINE AND APU BLEEDS TO SUPPLY PACKS. INSPECTED ACM AREA . POSITIONED AIRCRAFT IN DIFFERENT HEADINGS WITH RESPECT TO WIND. COULD NOT DUPLICATE, SMOKE IN CABIN. AIRCRAFT RETUR N TO SERVICE. 2 L 7 2 4F RT A21EA 2008030400167 20080304 00167 NM 2008 3 4 HALA0800228 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 825 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45,SEAT TRACKS AT LBL 11, STA 825. MAX DEPTH OF BLEND OUT WAS 0.010". BLENDED IAW SRM 51-10 -02. ALL BLEND OUTS WITHIN SRM 53-00.52 LIMITS. 2 L 7 2 4F RT A1NM 2008030400168 20080304 00168 NM 2008 3 4 DLM88080274 1 20080213 A 5753 SKIN DOUG MD88 MD88 3023688 NM LT WING TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 DURING HMV ELONGATED HOLES WERE REPORTED ON UPPER SKIN OF LT OUTBOARD FLAP INBOARD SECTION. A NEW SKIN AND FINGER DOUBL ER WERE FABRICATED AND INSTALLED IAW BOEING PRODUCTION DWG 9935954-15. 2 L 7 2 4F RT A6WE 2008030400169 20080304 00169 NM 2008 3 4 F3LA200800053 1 20080206 A 5321 D5367324200000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 902FR 5564 1515 DURING C 7 C CHECK, INSPECTION REPORTED THE FORWARD CARGO PIT PANEL 131AF HAD ITS RIGHT EDGE DAMAGED. MAINTENANCE REPAI RED THE PANEL BY FABRICATING AN ALUMINUM COVER SHEET IN ACCORDANCE WITH THE REQUIREMENTS OF EO A9-53EO-20231. THE COVER SHEET WAS INSTALLED IN ACCORDANCE WITH AMM 53-22-14-400-001 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR AND INSTAL LATION OF THE PANEL, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008030400170 20080304 00170 NM 2008 3 4 F3LA200800050 1 20080213 A 5411 D54630334206 FRAME AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE LT NACELLE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 902FR 5546 1515 DURING C7 C CHECK AND LEAK CHECKING OF THE LEFT PYLON, INSPECTION REPORTED A CRACKED FRAME ON THE TOP, LEFT SIDE OF THE PYLON, JUST AFT OF THE PRE-COOLER. MAINTENANCE REPAIRED THE CRACK IN ACCORDANCE WITH THE REQUIREMENTS OF DRAWING D54630 462, A319 SRM 54-52-12, PARAGRAPH 5E AND SRM 51-42-11, PARAGRAPH 6B. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AN D FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008030400178 20080304 00178 NM 2008 3 4 HALA0800194 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1351 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION RBL 54.75, SEAT TRACKS AT STA 1351, BASE OF TRACKS. CORROSION REMOVED PER SRM 51-10-02, REV 76 AND SR M 53-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030400185 20080304 00185 NM 2008 3 4 HALA0800126 1 20080108 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1043 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 2 CORROSION SECTION 45,SEAT TRACK AT LBL 88.5, STA 1043. SEAT TRACK REPLACED. 2 L 7 2 4F RT A1NM 2008030400189 20080304 00189 NM 2008 3 4 DL757080225 1 20080218 A 2910 271N61192 LINE BOEING 757 757232 1384965 NM HYD SYSTEM LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 619DL 22909 LEFT HYD FAILURE AFTER T/O STT, AA MTC FOUND THE RT RETRACT ACT PRESSURE LINE LEAKING. AA MTC REPLACED SAME LEAK CHECKE D GOOD. AA MTC ALSO CHECKED THE CASE DRAIN FILTERS AND DIFFERENTIAL PRESSURE POP OUTS ALL OK. 2 L 7 2 4F RT A2NM 2008030400196 20080304 00196 NM 2008 3 4 2008UALA00878 1 20080215 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FUSELAGE SKIN CRACKED ABOVE AND BELOW FWD ENTRY DOOR UPPER HINGE CUT-OUT. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022900137 20080229 00137 EA 2008 2 29 SWIA200819237 1 20080218 A 5610 NP1393222 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 960SW 10960 10960 7853 FLT 5819 - FIRST OFFICERS SIDE WINDOW CRACKED. REPLACED FO'S SIDE WINDOW IAW MM 56-12-01. 2 L 7 2 4F RT A21EA 2008022900187 20080229 00187 NM 2008 2 29 MASA200800145 1 20080217 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 2 DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 989HA 427 REPAIR TO RIGHT I/B NR 2 FLAP TRACK. 2 H 7 2 4T RT A13NM 2008030500018 20080305 00018 NM 2008 3 5 QXEA200800169 1 20080130 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - RIGHT SIDE OF FUSELAGE EXTERNAL SKIN HAS GOUGE AT BASE OF V-STAB APPROXIMATELY 10 INCHES AFT OF FRAME 5 . REPAIRED IAW DHC8 RD8-53-2181 AND NDTM PT-6 51-00-01. 2 H 7 2 4T RT A13NM 2008030500041 20080305 00041 NM 2008 3 5 QXEA200802074 1 20080101 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - NUT PLATE ON FLANGE AT STATION 600.00 LEFT SIDE THE FIRST NUT PLATE IS CORRODED ON THE UNDERSIDE NUT PL ATE. REMOVED AND REPLACED NUT PLATE IAW -8 200 SRM 51-40-11, 51-20-11 AND -8 CPC CHAPTER 4 STEP 8. 2 H 7 2 4T RT A13NM 2008030500059 20080305 00059 NM 2008 3 5 QXEA200800127 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 529-547 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - LEFT SEAT TRACK NR 7 BETWEEN FRAME 529.5 TO 547.0 HAS MULTIPLE CHAFES/GOUGES. REPAIRED IAW RD8/4-53-88 4, Q400 NDTM PT-6 51-00-01, AND Q400 SRM 51-21-10. 2 H 7 2 4T RT A13NM 2008030500069 20080305 00069 NM 2008 3 5 QXEA200800157 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 545-549 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - AT APPROXIMATELY STATION X545 TO X549 ON LEFT OUTBOARD SEAT TRACK NR 3 THERE IS LIGHT CORROSION IN THE CENTER OF THE TRACK. REPAIRED IAW DHC8 200 RD8-53-3644, NDTM PT-6 51-00-01, AND DHC8 200 SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2008030500073 20080305 00073 NM 2008 3 5 QXEA200800224 1 20080208 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 709-714 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - LEFT EQUIPMENT TRACK, STATION 709-714 HAS BUBBLED PAINT SUSPECT CORROSION. REPAIRED IAW Q400 RD 8/4-53 -884, RD 8/4-53-2260, AND NDTM PART 6 51-00-01. 2 H 7 2 4T RT A13NM 2008030500088 20080305 00088 NM 2008 3 5 QXEA200802087 1 20080101 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAPS WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - RIGHT NR 4 FLAP TRACK HAS A WORN SPOT ON THE UPPER INBOARD TRACK BOTTOM SIDE OF THE TRACK. REPAIRED IA W RD8-57-988. 2 H 7 2 4T RT A13NM 2008030500089 20080305 00089 NM 2008 3 5 QXEA200802089 1 20080101 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 393 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 AT FS X393 HAS DAMAGE TO OUTBOARD FLANGE. REPAIRED IAW RD8-53-9958 A ND -8 200 SRM 51-20-26. 2 H 7 2 4T RT A13NM 2008030500093 20080305 00093 NM 2008 3 5 QXEA200800134 1 20080119 A 5753 SKIN BOMBDR DHC8 DHC8402 1390042 NM RT TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - RIGHT OUTBOARD FLAP, INBOARD END, LOWER SIDE OF LEADING EDGE IS LIGHTLY CHAFED FOR APPROXIMATELY 5 INCH ES. REPAIRED IAW RD8/4-57-0920, AND Q400 NDTM PT-6 51-00-01, Q400 SRM 51-25-10 AND 51-25-15. 2 H 7 2 4T RT A13NM 2008030500120 20080305 00120 NM 2008 3 5 QXEA200800190 1 20080130 A 5751 SKIN DHAV DHC8 DHC8202 2809007 NM LT AILERON DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - LEFT AILERON OUTBOARD TRAILING EDGE JUST OUTBOARD OF STATIC WICK APPEARS TO BE A LIGHTING EXIT POINT. REMOVED TRAILING EDGE AND INSTALLED NEW TRAILING EDGE IAW DHC8 200 SRM 51-40-00, 51-20-26, 57-60-71 PARA 2B. PERFORMED W ICK CHECK IAW DHC8 200 AMM 23-60-01-400-801. 2 H 7 2 4T RT A13NM 2008030500121 20080305 00121 NM 2008 3 5 QXEA200800191 1 20080130 A 5720 MOUNT DHAV DHC8 DHC8202 2809007 NM STATIC WICK DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - THE OUTBOARD STATIC WICK MOUNT PAD APPEARS TO HAVE LIGHTNING STRIKE DAMAGE ON THE RIGHT AILERON. REMOV ED AILERON TRAILING EDGE AND INSTALLED A NEW TRAILING EDGE IAW RD8-57-2269, DHC8 AMM 23-60-01, SRM 51-20-26 AND 57-60-71 PARA 2B. PERFORMED STATIC WICK CHECK 23-60-01-400-801. 2 H 7 2 4T RT A13NM 2008030500124 20080305 00124 NM 2008 3 5 QXEA200800144 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 644 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - SEAT TRACK 20 BETWEEN FRAME 644.5 TO END OF TRACK HAS POSSIBLE CORROSION. REPAIRED IAW RD8/4-53-884, Q 400 NDTM PT-6 51-00-01. 2 H 7 2 4T RT A13NM 2008030500126 20080305 00126 NM 2008 3 5 QXEA200800147 1 20080119 A 5320 THRESHOLD BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - MCD LOWER THRESHOLD MEMBER IS CORRODED AT ALL N/P BETWEEN X1.000 TO X32.400. REMOVED THRESHOLD AND INS TALLED NEW THRESHOLD FROM STOCK IAW Q400 SRM 51-21-10 PG 201-205, 51-25-10 PG 201-205, 51-42-05 PG 201-218, AND 51-42-05 . 2 H 7 2 4T RT A13NM 2008030500138 20080305 00138 NM 2008 3 5 QXEA200800122 1 20080119 A 5315 FLOORBEAM BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - CARGO FLOOR PANEL 144JZ HAS CORROSION ON FLOOR FRAME MARKED. REPAIRED IAW Q400 SRM 51-27-00 PG2 4 A (2 )(A)(B), Q400 NDTM PT-6 51-00-01, PT-1 51-00-04, Q400 SRM 51-21-10, 51-14-00 AND 51-42-15. 2 H 7 2 4T RT A13NM 2008030500140 20080305 00140 NM 2008 3 5 QXEA200800196 1 20080208 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 136 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - NR 18 SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION X136.000. REMOVED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW Q400 SRM 51-40-15, 51-40-07, 51-42-45 AND 51-42-05. 2 H 7 2 4T RT A13NM 2008030500143 20080305 00143 NM 2008 3 5 QXEA200800212 1 20080208 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 261 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - NR 19 SEAT TRACK HAS CORROSION INSIDE TRACK AT STATION X261.000. REPAIRED IAW Q400 RD8/4-53-2211, NDTM PART 6 51-00-01 AND RD8/4-53-884. 2 H 7 2 4T RT A13NM 2008030500145 20080305 00145 NM 2008 3 5 QXEA200800215 1 20080208 A 5711 SPAR CAP BOMBDR DHC8 DHC8402 1390042 NM RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - RIGHT WING LOWER SPAR CAP HAS FRETTING CORROSION FORMING AT APPROXIMATELY YW145.2 TO 155.2. REPAIRED I AW Q400 RD 8/4-57-935, AND NDTM PT-6 51-00-01. 2 H 7 2 4T RT A13NM 2008030500162 20080305 00162 NM 2008 3 5 QXEA200800167 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 593 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - NR 6 SEAT TRACK FLOORBOARD SUPPORT MOUNT FLANGE HAS CORRODED NUTPLATE AT STATION X593.00. REPAIRED IAW DHC8 200 RD8-53-784, NDTM PT-6 51-00-01 AND DHC8 200 SRM 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2008030500163 20080305 00163 NM 2008 3 5 QXEA200800166 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 545 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - NR 9 SEAT TRACK INBOARD AND OUTBOARD FLOORBOARD SUPPORT MOUNT FLANGES SUSPECTED CORROSION AT STATION X5 45.00 TO X600.00. REPAIRED IAW DHC8 200 RD8-53-4936, NDTM PT-6 51-00-01 AND DHC8 200 SRM 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2008030500167 20080305 00167 NM 2008 3 5 QXEA200800168 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 582-600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - NR 6 SEAT TRACK OUTBOARD FLOORBOARD SUPPORT MOUNT FLANGE SUSPECT CORROSION FROM STATION X582.00 - 600.0 0. REPAIRED IAW DHC8 200 RD8-53-4936, NDTM PT-6 51-00-01 AND DHC8 200 SRM 51-20-16, 51-20-36 2 H 7 2 4T RT A13NM 2008030500168 20080305 00168 NM 2008 3 5 QXEA200800202 1 20080208 A 5740 CRADLE BOMBDR DHC8 DHC8402 1390042 NM RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - RIGHT SIDE OUTBOARD FORWARD SPAR WING ATTACH BOLT BARREL NUT CRADLE AT YW42 IS CRACKED ON AFT SIDE. RE MOVED RIGHT FORWARD OUTBOARD BOLT, NUT AND WASHERS AND INSTALLED SERVICEABLE HARDWARE FROM STOCK, REF TASK CARD SB84-57- 19/B. 2 H 7 2 4T RT A13NM 2008030500172 20080305 00172 NM 2008 3 5 QXEA200800214 1 20080208 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 669 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - SUSPECT CORROSION ON RIGHT INBOARD SEAT TRACK TOP SIDE AT APPROXIMATELY STATION X669.0. REMOVED SEAT TRACK AND INSTALLED NEW TRACK IAW Q400 RD8/4-53-884, Q400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 2008030500175 20080305 00175 NM 2008 3 5 QXEA200800171 1 20080130 A 5314 KEELBEAM DHAV DHC8 DHC8202 2809007 NM BS 202 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - SUSPECT CORROSION UNDER BRACKET AT VERTICAL KEEL FRAME APPROXIMATELY STATION 202 X 31P. REPAIRED IAW D HC8 200 CPM CHAPTER 4 STEP 8, NDTM PT-1 51-00-04 AND PT-6 51-00-01, SRM 51-40-11, 51-20-11, 51-20-16, 51-20-36 AND 51-40 -00. 2 H 7 2 4T RT A13NM 2008030500178 20080305 00178 NM 2008 3 5 UIEA200800065 1 20080229 A 5730 PANEL BOEING 747 7472D7B 1384803 NM LWS 744 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 LT WING UPPER FIXED T/E PANEL AT WS 744.0 HAS A CRACK 6 INCHES FROM AFT EDGE OF PANEL. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 2, SHEET 1, 2 AND 5 PREPREG 250 DEGREES F CURE PER SRM 51-40-12. REF: ATLAS AIR EO NR 4 757A420. 2 L 7 4 4F RT A20WE 2008030500189 20080305 00189 NM 2008 3 5 QXEA200800199 1 20080208 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 706 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - LIGHT SURFACE GOUGES ON LEFT INBOARD SEAT TRACK, TOP SIDE AT APPROXIMATELY STATION X706. REMOVED OLD S EAT TRACK AND INSTALLED NEW SEAT TRACK IAW Q-400 SRM 51-40-15 AND 51-42-05. 2 H 7 2 4T RT A13NM 2008030500191 20080305 00191 NM 2008 3 5 QXEA200800188 1 20080130 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 5 TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - LEFT NR 5 FLAP TRACK HAS PITTING ON UPPER SURFACE OF THE LOWER OUTBOARD FLANGE AT THE ROLLERS ZERO DEGR EE POSITION. REPAIRED IAW DHC 8 200 RD8-57-989, AND NDTM PT-6 51-00-01. 2 H 7 2 4T RT A13NM 2008030600010 20080306 00010 NM 2008 3 6 08FDEA00474 1 20080218 A 5320 146N54462 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOOR BOARD SUPPORT R11.40, STA 1500-1520 TO EVALUATE EXISTING REPAIR. EXISTING REPA IR FOUND NOT IAW SRM 51-70-11 FIG1 DETAIL I, II STRINGER R11.40 FROM STA 1500 TO STA 1520 REPLACED IAW B757 SRM 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008030600011 20080306 00011 NM 2008 3 6 08FDEA00475 1 20080218 A 5320 146N544417 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD SUPPORT L7.55, STA 1500-1520. TO EVALUATE EXISTING REPAIR. EXISTING REPA IR FOUND NOT IAW SRM 51070-11 FIG 1 DETAIL I, II. STRINGER L7.55 FROM STA 1500 TO STA 1520 REPLACED IAW B757 SRM 51-10- 02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008030600022 20080306 00022 SO 2008 3 6 C2XA08ON092 1 20080215 A 3350 BA50933901 CHARGER EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12166 10501 10501 14500831 FLT MX - SAN - WHILE PERFORMING ROUTING CHECK MX PERSONNEL FOUND PILOT'S EMERGENCY LIGHT NR 1 AISLE EMERGENCY LIGHT AND FWD EMERGENCY LIGHTS DO NOT ILLUMINATE. MX PERSONNEL REMOVED AND REPLACED NR 1 BATTERY CHARGER ASSY. OPERATIONALLY CHE CKED SATISFACTORY. A/C WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008030600023 20080306 00023 SO 2008 3 6 C2XA08ON093 1 20080216 A 2810 EMB145N VENT LINE EMB 145 EMB145LR 3260212 SO FUEL SYSTEM CHAFED A C2XA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 27 15555 145594 FLT 0119 - ONT - MX PERSONNEL REPORTED LT WING FUEL PANEL LEAKING. MX PERSONNEL REMOVED AND REPLACED VENT VALVE LINE, O PERATIONALLY & LEAK CHECKED SATISFACTORY. A/C WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008030600030 20080306 00030 SO 2008 3 6 C2XA08RI024 1 20080124 A 3350 7287580505 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 14998 145302 FLIGHT 2882 - CREW REPORTED GALLEY IDENTIFIER EXIT SIGN INOPERATIVE. EWR MX REMOVED AND REPLACED NR 1 EMERGENCY FLOOR S TRIP IAW EMB145 AMM 33-50-12 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008030600033 20080306 00033 SO 2008 3 6 C2XA08SH033 1 20080221 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11544 145557 SHV - DURING C-CHECK THE NR 1 AND NR 5 CENTER AISLE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MX REMOVED AND REPLA CED THE NR 3 EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008030600035 20080306 00035 SO 2008 3 6 C2XA08SH034 1 20080221 A 5230 14523918001 DOOR FRAME EMB 145 EMB145LR 3260212 SO CARGO DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18557 145596 SHV - DURING C-CHECK THE BAGGAGE DOOR WAS FOUND TO HAVE CORROSION AROUND NUT PLATE HOLES ON VARIOUS INTERNAL FRAMES. MA INTENANCE PERFORMED DOUBLER REPAIRS TO THE AFFECTED AREAS IAW EXPRESSJET EC 5220-01028. THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008030600039 20080306 00039 2008 3 6 UPS08551698 4 20080220 A 3442 TRANSCEIVER BOEING 757 75724APF 1384969 NM WEATHER RADAR FAULTY A IPXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 470UP 25486 INSPECTION TYPE:N/A ATB - FOR PREVIOUS WX RADAR FAIL. WX FAIL ON BOTH HSI'S AFTER T/O. SOMETIME INTERMITTENT, SOMETIME S CONTINUOUS. RADAR WAS NOT TRANSMITTING IN EITHER CASE. T/S FOUND RADAR XCEIVER AT FAULT. REMOVED AND REPLACED WX RA DAR XCEIVER, OPS CK GOOD. REF MM 34-43-01-4. 2 L 7 2 4F RT A2NM 2008030600042 20080306 00042 NE 2008 3 6 UPS08851697 2 20080221 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 3 FLAMED OUT A IPXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 SO 01 807UP 46007 INSPECTION TYPE:N/A NR 3 ENGINE FLAMEOUT AT CRUISE. FLT LVL 360, SPEED MACH .81, FUEL NORMAL AND BALANCED. ATTEMPTED R ESTART AT FL 300 UNSUCCESSFUL. ATTEMPTED 2ND RESTART AT 16000 FT SUCCESSFUL. ENG OPERATED NORMALLY REMAINDER OF FLT. EMERGENCY WAS DECLARED. PERFORMED T/S PROCEDURE WRT MM 71-00-00-1 FIG 139 SHEET 1 & 2. FOUND NO ABNORMAL DEFECTS. REM OVED AND REPLACED NR 3 MAIN ENG FUEL FILTER WRT MM 73-10-02-4-2. NO ABNORMAL CONTAMINATION FOUND. IDLE LEAK CHECK WAS GOOD. PERFORMED HIGH POWER RUN WRT MM 71-00-00-5, ALL PARAMETERS NO DEFECTS FOUND. NO PREVIOUS HISTORY A/C OK FOR SERV ICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2008030600057 20080306 00057 NM 2008 3 6 2008UALA00919 1 20080215 A 5320 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 806UA 788 FOUND BEAM NR 150 DAMAGED BEYOND REPAIR. ACCOMPLISHED MAJOR REPAIR AT DEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030600060 20080306 00060 NM 2008 3 6 2008UALA00924 1 20080218 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 196UA 28715 FUSELAGE INTERNAL SKIN CORRODED, BS 2080 STR 35R AT WASTE VENT OUTLET. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER/TRI PLER REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030600061 20080306 00061 NM 2008 3 6 2008UALA00930 1 20080218 A 3397 58791 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 590UA 28708 CABIN EMERGENCY LIGHTS ON FLOOR AFT OF ROW 30 INOPERATIVE. DAMAGE (UNKNOWN) TO FEEDER CABLE. REPLACED FEEDER CABLE, OP S CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030600062 20080306 00062 NM 2008 3 6 2008UALA00932 1 20080218 A 4920 S343T00339 SHUTOFF VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE APU FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 666UA 29238 APU DOES NOT START. REPLACED APU SHUTOFF VALVE. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030600063 20080306 00063 NM 2008 3 6 2008UALA00934 1 20080218 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 194UA 26892 FUSELAGE INTERNAL SKIN CORRODED, BS 2080 STR 35R AT WASTE VENT OUTLET. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER/TRI PLER REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030600073 20080306 00073 EA 2008 3 6 S9BA200800014 1 20080303 A 3246 MS203929C33 CLEVIS PIN DHAV DHC6 DHC6 2802606 EA FLYING WIRE MISSING A S9BA C ABORTED TAKEOFF Z SIGNIFICANT FAILURE REPORT TO TAKEOFF 1 SO 29 573SA 182 573 FLT 170, HEARD A POP IN THE AREA OF THE FLYING WIRE. CLEVIS PIN AT LEFT UPPER FLYING WIRE FOUND MISSING UPON LANDING. REMOVED AND REPLACED FLYING WIRES PN 13A0200-079 UPPER FRONT DRAG FITTING 13A02469-001 AND DRAG WIRE SHIM PN 13A02078-0 02. EMERGENCY WAS NOT DELARED AND AIRCRAFT WAS NOT GROUNDED. 1 H 7 2 3T RT A9EA 2008030600085 20080306 00085 NM 2008 3 6 MWEA080035 1 20080223 A 3260 7939010636 DOWNLOCK SENSOR BOEING 717 717200 1383700 NM LT MLG FAULTY A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 904ME 55168 AFTER GEAR RETRACTION LEFT UNSAFE LIGHT ILLUMINATED ALONG WITH A PSEU ALERT. REMOVED AND REPLACED LEFT MAIN LANDING GEA R DOWN/LOCKED SENSOR. FUNCTIONAL TESTED GEAR OPERATION, ALL INDICATIONS ARE NORMAL. 2 L 7 2 4F TR A6WE 2008030600087 20080306 00087 SO 2008 3 6 RAIA00802024 1 20080222 A 2730 ELEVATOR EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A RAIA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 CE 03 834HK 145269 FLT 8025 - IAD - DURING TAKEOFF THE ELEVATORS SEEMED TO BE NON-RESPONSIVE WHEN THE YOKE WAS PULLED BACK. MAINTENANCE IN SPECTED THE AIRCRAFT'S ELEVATOR FOR STRUCTURAL DAMAGE, PERFORMED A DEFLECTION CHECK OF THE ELEVATOR CONTROL SURFACE, PER FORMED AN OPERATIONAL CHECK OF THE PITCH TRIM SYSTEM, PERFORMED AN OPERATIONAL CHECK OF THE FLAP AND SPOILER SYSTEMS. I N ADDITION, A GALE FORCE WIND INSPECTION WAS PERFORMED IAW AMM PROCEDURES. ALL INSPECTIONS AND CHECKS WERE COMPLETED WI TH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008030600089 20080306 00089 SO 2008 3 6 RAIA00802022 1 20080222 A 3610 CA33020 CLAMP EMB 145 EMB145 3260210 SO BLEED AIR SYS BROKEN A RAIA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 802HK 145066 FLT 3506 - PIT - ENGINE AND APU BLEED LEAK MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED A BLEED LINE O-RING A ND CLAMP. PERFORMED LEAK CHECK OF THE SYSTEM WITH NO DEFECTS NOTED. 2 L 7 2 4F RT T00011AT 2008030600095 20080306 00095 2008 3 6 SWAA081046 4 20080225 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 206WN 34011 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008030600096 20080306 00096 NM 2008 3 6 SWAA081058 1 20080225 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500B, STR 15L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008030600100 20080306 00100 NM 2008 3 6 SWAA081059 1 20080222 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 AALA200801895 1 20080717 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW - EMERGENCY LIGHT AT OVERHEAD MID GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD MID GALLEY. SY STEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20080902 NM 2008 9 2 SWAA084571 1 20080815 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 797MX 27890 DURING SCHEDULED HC2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084506 1 20080814 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 232WN 32500 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084514 1 20080814 A 5312 6517853 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED 10Y CHECK, FOUND FWD PRESSURE BULKHEAD VERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084490 1 20080813 A 3350 8100137901 LENS BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 419WN 29824 DURING SCHEDULED HC1 CHECK, FOUND LT OVERWING EMERGENCY EXIT EXTERIOR LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084488 1 20080813 A 5210 507945 DOOR BOEING 737 7373H4 1384600 NM FWD ENTRY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FWD ENTRY DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED DOOR PER ER. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084487 1 20080813 A 5311 6546538 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 KCSA081339 1 20080723 A 5420 STIFFENER BOEING 747 747209B 138489B NM NR 3 NACELLE SEVERED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 LOWER SIDE OF HORIZ FIREWALL WEB. CENTER LONGERON STIFFENER SEVERED NR 3 PYLON NAC STA 160. (A) 2 L 7 4 4F RT A20WE 20080902 NM 2008 9 2 SWAA084473 1 20080812 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 16 DEF. REMOVED AND REPLACED LIGHT BULB PE R MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084454 1 20080812 A 5311 65C22910 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084446 1 20080809 A 3211 6959886 FITTING BOEING 737 7377H4 1384404 NM RT MLG TRUNNION CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 726SW 27858 DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION SUPPORT LOWER LUGS CORRODED. REPAIRED PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084445 1 20080809 A 3211 6959886 FITTING BOEING 737 7377H4 1384404 NM RT MLG TRUNNION CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 726SW 27858 DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION SUPPORT UPPER & LOWER LUGS CORRODED. REPAIRED PER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 USAABB08127 1 20080721 A 7500 312N53217 DUCT BOEING 757 7572B7 1384964 NM BLEED SYS LEAKING A USAA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 19 937UW 27245 LAS FLT 790 LAS-CLT - THE CREW RECEIVED A RT ENG OVERHEAT WARNING ON TAKEOFF, RESULTING IN AN IN-FLIGHT SHUTDOWN. THE F LIGHT RETURNED TO FIELD LAS AND LANDED WITHOUT FURTHER INCIDENT. THERE WAS 30 MINUTES SINGLE ENG TIME. MAINTENANCE REP LACED A LEAKING RT ENG HP 6 DUCT. LEAK AND OPERATIONALLY CHECKS OK. (S) 2 L 7 2 4F RT A2NM 20080903 NM 2008 9 3 2008UALA03480 1 20080618 A 2421 1701768 GENERATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 776UA 26937 RT BACKUP ELECTRICAL POWER SYSTEM INOP. *S/D* FOUND RT BACK-UP GENERATOR HAS SHEARED SHAFT. REPLACED NR 2 ENGINE BACK UP GENERATOR PER MM-24-25-01. ACCOMPLISHED IDLE RUN NR 6 TEST, REF: MM-71-00-00-PAGE 543, REF: MM-24-25-01, PAGE 417 TESTED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080903 NM 2008 9 3 UIEA2008002272 1 20080801 A 5753 SKIN BOEING 747 7472D3B 1384805 NM LT WING TE FLAP CHAFED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 506MC 21252 LEFT WING INBOARD FLAP, AFT FLAP S/N 000204 UPPER SKIN HAS 4 EACH AREAS OF CHAFING CAUSED BY LONG BOLTS ON MID-FLAP. AR EAS ARE WBL 248.0, 297.0, 339.0 AND 425.0. CHAFE IS .500 INCH IN DIAMETER. PERMANENT REPAIR ACCOMPLISHED AS PER B747-2 00 SRM 51-40-09 FIG 5, SHEETS 4 & 10, ALUMINUM HONEYCOMB REPAIRS, 250 DEGREES F CURE PER SRM 51-40-20. LONG BOLTS ON MI D-FLAP WERE REMOVED AND REPLACED AS PER B747-200 SRM 51-30-02. ALSO REFERENCE ATLAS AIR EO4757A455. (S) 2 L 7 4 4F RT A20WE 20080903 CE 2008 9 3 DGCA175D081867 1 20080818 A 2913 PF24390615BCES52 PUMP RKWELL NA265 NA26565 7630107 CE HYD SYSTEM INOPERATIVE E DGCA O OTHER J WARNING INDICATION NR NOT REPORTED 1 CE 03 570R 46575 ON AUGUST 16, 2008, AT APPROXIMATELY 8:30 AM, ACFT N570R S/N 485-075, AFTER LANDING AT YIP, THE CREW HEARD AUDIBLE WARNI NG OF HYDRAULIC SYSTEM LOW PRESSURE. THE ACFT TAXIED TO THE RAMP OF DESTINATION, WITHOUT INCIDENT. UPON INVESTIGATION, THE HYDRAULIC PUMP WAS FOUND TO HAVE FAILED. (S) 2 L 7 2 4J A2WE 20080903 WP 2008 9 3 ARWA20080803 1 20080829 A 3040 NBA6045502 WINDSHIELD DOUG DC10 DC1010 3022110 WP COCKPIT SHORTED A ARWA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 29 68041 46900 FIRST OFFICER`S WINDSHIELD STARTED ARCING, POWER REMOVED. OUTER PANEL CRACKED, CHECK LIST COMPLETED. REMOVED AND REPLA CED FIRST OFFICER`S WINDSHIELD PANEL IAW DC-10 MM 56-11-00, OPERATIONAL CHECK NORMAL. REMOVED AND REPLACED RT WINDOW HE AT CONTROLLER IAW MM 30-42-01. GROUND TEST NORMAL IAW MM 30-42-00. (S) 2 L 7 3 4F A22WE 20080903 EA 2008 9 3 COMA086359 1 20080817 A 2910 601R752861 LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM CHAFED A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 710CA 7241 EN ROUTE FROM JAX TO LGA RECEIVED HYD SYS NR 1 LOW PRESS CAUTION MSG. FOLLOWED QRH, HYD QTY SHOWED, PRESS DROPPED TO 0 PSI. ACFT DIVERTED TO RIC AND LANDED SAFELY. FOUND LT ENG EDP SUPPLY LINE CHAFED. REPAIRED EDP SUPPLY LINE IAW CRJ AM M TASK 20-22-00-910-802. (S) 2 L 7 2 4F RT A21EA 20080903 NM 2008 9 3 USAA920081531 1 20080817 A 3397 D9299200900200 WIRE HARNESS AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 827AW 1547 FLT 655 - SNA-PHX- EEL - EMERGENCY PATH LIGHT AT SEAT 22C INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT HARNESS ON SEAT 22C. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080903 2008 9 3 VNAA0808007 4 20080810 A 3418 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FALSE INDICATION A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 05 218PS 7885 AFTER TAKEOFF CREW RECEIVED A STALL FAIL CAS MESSAGE. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINT ENANCE INSPECTED SYSTEM AND FOUND NO DEFECTS. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080903 NM 2008 9 3 ABXA080224 1 20080807 A 5313 148T9120 LONGERON BOEING 767 767232 1385132 NM EMPENNAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 745AX 22222 UPPER LONGERON ABOVE HORIZONTAL BOX WEB CRACKED AND DAMAGED STA 1734 LT SIDE. REPAIRED IAW REA B653-57691. (S) 2 L 7 2 4F RT A1NM 20080903 NM 2008 9 3 KCSA081411 1 20080820 A 5320 WEB BOEING 747 747122 1384872 NM BS 1480 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 A 1 INCH CRACK AT STA 1480 ON WEB T RBL 108 AT STR 34R. (S) 2 L 7 4 4F RT A20WE 20080903 EA 2008 9 3 VNAA0808005 1 20080808 A 5100 NONE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NOT AN SDR NONE A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 215PS 7880 CREW REPORTED A BIRD STRIKE ABOVE THE WINDSHIELD ON TAKEOFF ROLL. CREW ELECTED TO ABORT THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO DEFECTS OR DAMAGE. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080904 NM 2008 9 4 EIA2008027 1 20080708 A 3350 906835AB POWER SUPPLY BOEING 747 747230B 1384889 NM EMERGENCY LIGHT INOPERATIVE A EIAA O OTHER L NO TEST NR NOT REPORTED 1 NM 09 487EV 23786 EMERGENCY LIGHT U/D ABOVE SEAT INOPERATIVE. OPEN RT U/D CEILING PANEL STA 670 FOR ACCESS TO EMERGENCY LIGHT. POWER SUP PLY DM335 REMOVED AND REPLACED U/D EMERGENCY LIGHT PS DM 335, OPS CHECK NORMAL. (A) 2 L 7 4 4F RT A20WE 20080904 NE 2008 9 4 Q2S2008F00002 2 20080714 A 7200 ENGINE BOEING 747 747206B 1384856 NM GE CF6 CF650E2 30018 NE NR 3 FAILED A Q2SA C ABORTED TAKEOFF M Y J OVER TEMP ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 EA 63 746SA 92607 21111 DURING TAKEOFF, THE NR 3 ENGINE FIRE WARNING INDICATIONS (VISUAL/AURAL) WENT OFF AT 1,500 FT. PULLED BACK THE THROTTLE, INDICATIONS WENT OUT. ENGINE SHUT DOWN AND RETURNED TO LAGOS, NIGERIS (DNMM). FUEL WAS NOT DUMPED AS AIRCRAFT WAS NOT LOADED WITH CARGO AND WAS UNDER THE MAXIMUM LANDING WEIGHT. A VISUAL INSPECTION OF THE ENGINE FOUND UNCONTAINED ENGINE FAILURE WITH DAMAGE TO THE SIDE OF THE TURBINE CASE, BOTH CORE COWLS AND BLADES MISSING FROM THE LOW PRESSURE TURBINE ( LPT) WHEEL. FURTHER DAMAGE ASSESSMENT IS UNDERWAY. ALL AD`S ARE CURRENT FOR THIS ENGINE. 2 L 7 4 4F 4 F RT A20WE E23EA 20080904 SO 2008 9 4 SIMA200818904 1 20080706 A 3297 CONNECTOR EMB 145 EMB145LR 3260212 SO MLG LOOSE A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 675AE 14500806 ON FLIGHT 4402 - CREW REPORTED ON TAKEOFF, RECEIVED A LG AIR/GND FAIL CAUTION MESSAGE. LANDING GEAR WOULD NOT RETRACT A ND CREW ELECTED TO RETURN TO FIELD. AIRCRAFT REMOVED FROM SERVICE. FOUND CONNECTOR J0775 LOOSE. RETIGHTENED OPERATION AL CHECK GOOD IAW AMM 32-30-00 AND AMM 32-34-00. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080904 EA 2008 9 4 TRAX200800935 1 20080727 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 926EV 7843 LT SIDE FUSELAGE STATION 621 OBLIQUE ANGLE CRACKED. REPLACEMENT OF OBLIQUE ANGLES. REMOVED LT/RT FS 625 OBLIQUE ANGLES IAW CRJ 200 SRM 51-42-21. LOCATED HOLES IN NEW SERVICEABLE OBLIQUE ANGLE IAW CRJ 200 SRM 51-40-11. INSTALLED NEW SERV ICEABLE FS 625 OBLIQUE ANGLES IAW CRJ 200 SRM 51-42-21. (A) 2 L 7 2 4F RT A21EA 20080904 NM 2008 9 4 DHL2008F00012 1 20080611 A 5347 SEAT TRACK BOEING 727 7272M7 138407S NM BS 848-1166 CORRODED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 CABIN SEAT TRACK BS 1166 TO 848 LBL 24-25 LIGHT CORROSION IN SEVERAL AREA AND MISSING PRIMER. REMOVED CORROSION ON SEAT TRACK BETWEEN BS 1050 TO 848 LBL 24.25 IAW SRM 51-10-6. AREA OF SEAT TRACK WITH ORIGINAL THICKNESS OF .300, MATERIAL L OSS .002, MATERIAL REMAINING IS .298 FOUND WITHIN LIMITS IAW SRM 51-20-2 FIG, 21 AND 53-10-1 FIG 3, ALODINE AND PRIMED A REAS IAW SRM 51-10-2. FOUND CORROSION ON SEAT TRACK BS 1100 TO 1166 IAW SRM 53-10-4 FIG 3. REMOVED SEAT TRACK IAW SRM 51-30-2 AND FLOOR PANELS ROW B AND C BS 1100 TO 1166. FABRICATED NEW SEAT TRACK WITH BACK 1520-792 7178 T6 PO 9006864 I AW SRM 51-20-1 AND 53-10-5 FIG 1 AND 51-30-5. TREATED AND PRIMED SEAT TRACK IAW SRM 51-10-2. INSTALLED SEAT TRACK IAW 2 L 7 3 4F A3WE 20080904 WP 2008 9 4 IXX2008F00027 1 20080716 A 2612 FIRE WARNING DOUG DC8 DC871F 302199D WP NR 4 NACELLE ACTIVATED A IXXA F A ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 11 830BX 45973 FLT NR: ATN 229/PKMJ TO KHNL/TAT 81746.9/TAC 32717. DURING CRUISE FROM PKMJ NR 4 FIRE WARNING CAME ON THE CREW SHUTDOWN THE NR 4 ENGINE AND FIRE BOTH BOTTLES. THE CREW LANDED IN KHNL WITHOUT FURTHER INCIDENT. (A) 2 L 7 4 4F RT 4A25 20080904 SO 2008 9 4 SIMA200820301 1 20080716 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 614AE 145086 ON FLIGHT 3762 ON TAKEOFF CREW REPORTED A BURNING OIL ODOR. AIRCRAFT REMOVED FROM SERVICE. PERFORMED ETN EM-72-034R4, AND REMOVED AND REPLACED LT ENGINE PER WORK CARD 71-000-000 OPERATIONAL CHECKED GOOD. NO LEAKS NOTED. AIRCRAFT RETURNE D TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080904 EA 2008 9 4 TRAX200800917 1 20080717 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 719EV 10099 AFT GALLEY EMERGENCY LIGHT HAS SEVERAL INOP BULBS. RELAMPED AFT GALLEY FLOOR LEVEL EMERGENCY FLOOD LIGHT. OPS CHECK GO OD. (A) 2 L 7 2 4F RT A21EA 20080904 WP 2008 9 4 IXX2008F00021 1 20080718 A 2697 CONNECTOR DOUG DC8 DC873F 302199F WP FIRE DETECTION DAMAGED A IXXA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 11 602AL 45991 FLT NR: ATN 842/KTOL TO KPHL. DURING CLIMB FROM KTOL THE NR 4 FIRE WARNING CAME ON. THE CREW ACCOMPLISHED THE APPROPRI ATE CHECKLIST AND DISCHARGED BOTH FIRE BOTTLES. THE ACFT LANDED AT KPHL WITHOUT INCIDENT. MAINTENANCE INSPECTED NR 4 E NGINE FIRE DETECTION SYSTEM AND FOUND HIGH RESISTANCE AT PIN F, UPPER PYLON SOCKET PLUGS DISTORTED. MAINTENANCE REPLACE D PYLON FIRE DETECTOR ELEMENT, SOCKET PLUG, FIRE DETECTOR CONTROL UNIT AND BOTH FIRE BOTTLES. OPERATIONAL CHECK GOOD IA W MM 26-10-0, 26-10-1 AND 26-10-2. AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 4 4F RT 4A25 20080904 NM 2008 9 4 DHL2008F00018 1 20080625 A 5210 WEB BOEING 727 7272M7 138407S NM L1 DOOR CRACKED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 L-1 DOOR LOWER FORWARD CORNER OF WEB HAS CRACK. CUT OUT DAMAGE L-1 DOOR LOWER FORWARD CORNER WEB IAW B727 SRM 51-40-3 F IG 1. FABRICATED DOUBLER REPAIR AND INSTALLED IN L-1 DOOR IAW EVA B252-00082 REV IR DATED 6/19/08. (A) 2 L 7 3 4F A3WE 20080904 WP 2008 9 4 IXX2008F00018 1 20080718 A 2697 CONNECTOR DOUG DC8 DC871F 302199D WP FIRE DETECTION CONTAMINATED A IXXA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 11 821BX 45811 FLT NR: ATN 807/KBRI TO KMSP. DURING CRUISE FROM KBFI THE NR 1 ENGINE FIRE WARNING LIGHT AND BELL CAME ON. THE FIRE WA RNING LIGHT WENT OUT AND THE BELL STOPPED RINGING. THE CREW SUCCESSFULLY TESTED THE SYSTEM AND PERFORMED A PRECAUTIONAR Y ENGINE SHUTDOWN, AFTER AN ADDITIONAL HOUR OF FLT TIME THE FIRE WARNING LIGHT ILLUMINATED AND THE BELL SOUNDED, THE CRE W DISCHARGED BOTH FIRE BOTTLES. THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED NR 1 ENGINE FIRE WARNING SYSTE M AND FOUND A WET ELEMENT CONNECTOR, MAINTENANCE CLEANED AND DRIED CONNECTOR AND REPLACED BOTH BOTTLES. OPERATIONAL CHE CK GOOD IAW W/D 26-01-01, MM 26-21-09. AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 4 4F RT 4A25 20080904 SO 2008 9 4 SIMA200820303 1 20080720 A 2121 4611028900 FAN EMB 145 EMB145LR 3260212 SO COCKPIT FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 21 617AE 145093 ON FLIGHT 3989 CREW REPORTED ON SHORT FINAL, GOT A BURNING OR HOT ODOR IN THE FLIGHT DECK AND FORWARD PART OF CABIN. TU RNED THE RECIRCULATION FAN OFF AND FLIGHT ATTENDANT REPORTED NO ODOR AFT OF ROW 5. SMELL DISSIPATED AFTER LANDING WITHO UT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED COCKPIT RECIRCULATION FAN IAW EMB-145 AMM 21-24-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080904 EA 2008 9 4 MALA080127 1 20080723 A 3230 SELECTOR VALVE CNDAIR CL600 CL6002D24 1390016 EA MLG MALFUNCTIONED A MALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 15 928XJ 15190 GEAR EXTENSION FAILED ON APPROACH TO DTW. PERFORMED EMERGENCY LANDING GEAR EXTENSION AND LANDED IN DTW. (A) 2 L 7 2 4F RT A21EA 20080904 NM 2008 9 4 QXEA200800705 1 20080709 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM MAIN PAX STUCK A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 408QX 4050 SEA - FLIGHT 2274. AFT PASSENGER DOOR JAMMED. MAINTENANCE OPENED THE DOOR AND CLEANED AND LUBED. OPERATIONAL CHECKS G OOD. RETURNED TO SERVICE. NO PARTS REPLACED. (A) 2 H 7 2 4T RT A13NM 20080904 SO 2008 9 4 SIMA200818902 1 20080703 A 5320 14525480 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 689EC 14500853 DURING MBV INSPECTION FOUND CARGO DOOR SILL BETWEEN FRAMES 65-68 TO BE CORRODED. REMOVED AND REPLACED CARGO DOOR SILL I AW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080904 EA 2008 9 4 QXEA200800714 1 20080710 A 5347 58401A2B5C5F4L30 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 645 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 612QX 10042 PDX-C4 CHECK - CORROSION AND A GOUGE AT THE RT SEAT TRACK AT STATION 645.00. BLENDED CORROSION. MATERIAL REMOVED IS WI THIN LIMITS OF REO 670-53-00-013. ALODINED TRACK. (A) 2 L 7 2 4F RT A21EA 20080904 EA 2008 9 4 QXEA200800807 1 20080721 A 2120 SEAL CNDAIR CL600 CL6002C10 1390015 EA ENGINE DAMAGED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 617QX 10130 PDX-FLT 2561 (PDX-ONT) MASTER WARNING AND AFT LAVATORY SMOKE MESSAGE ILLUMINATED ON TAKEOFF. WENT OFF AFTER 10 SECONDS . LAVATORY WARNING SOUNDED BUT NO SMOKE PRESENT. CALLED CFR AND RETURNED TO THE FIELD AND ACCOMPLISHED AN UNEVENTFUL L ANDING. LANDING WAS OVER WEIGHT. MAINTENANCE PERFORMED AN OVERWEIGHT INSPECTION AND REPLACED THE E SEAL (ENGINE SEAL P RESSURE REGULATING VALVE). DOWNSTREAM E-RING MISSING. OPERATIONAL CHECKS GOOD. RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A21EA 20080904 EA 2008 9 4 COMA0860332 1 20080724 A 2910 PE4096G0060000 HOSE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM RUPTURED A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 594SW 7285 FLIGHT 5285 - AFTER TAKEOFF FROM CVG LOST ALL NR 3 SYSTEM HYDRAULIC FLUID, CREW DECLARED AN EMERGENCY AND RETURNED TO TH E FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED RUPTURED HYDRAULIC LINE ON ACMP 3B. (A) 2 L 7 2 4F RT A21EA 20080904 EA 2008 9 4 TRAX200800607 1 20080506 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 621-755 S14L CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 928EV 8006 LT INTERCOSTAL ANGLE BETWEEN FS 621.00 AND FS 755.00 AT STRINGER 14 IS CRACKED APPROX 1 INCH LONG. REMOVED AND REPLACED LT INTERCOSTAL BETWEEN FS 621 AT STRINGER 14 WITH NEW SERVICEABLE INTERCOSTAL IAW BOMBARDIER REO 601R-53-61-422 AND CRJ 200 SRM 51-42-21. SUPPLEMENTAL SDR CLOSED 6/24/08. (A) 2 L 7 2 4F RT A21EA 20080904 NM 2008 9 4 ASM2008F00002 1 20080805 A 5753 FAIRING BOEING 737 737* NM T/E FLAP PUNCTURED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 904AM 28262 DURING TRANSIT CHECK, MAINTENANCE PERSONNEL DETECTED A PUNCTURE OF 6"X7" IN THE LT INTERIOR FLAP FAIRING AT FWS LOWER AR EA AND A CRACK OF 6 INCHES IN LATERAL SIDE WITH THE BRACKET LOOSENED. THE INTERIOR FLAP FAIRING WAS REPLACED IAW MM 27- 61-18, TESTED CORRECT. 2 L 7 2 4F RT A16WE 20080905 NM 2008 9 5 DHLA200800075 1 20080617 A 3350 BATTERY PACK BOEING 727 727223 1384074 NM EMERGENCY LIGHTS INOPERATIVE A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 752DH 22466 EMERGENCY ENT LIGHTS INSIDE LIGHT INOP. REMOVED AND REPLACED BATTERIES IN LIGHT PACK, OPS CHECK GOOD IAW MM 33-50-71. FLT 119. A/C WAS GROUNDED. (A) 2 L 7 3 4F A3WE 20080905 EA 2008 9 5 TRAX200800928 1 20080724 A 2910 HOSE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A ASOA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 842AS 7304 HYD 1 LOW PRESS CAUTION MESSAGE IN FLIGHT. FLT 4258,4391 CX-(EMERGENCY DECLARED). REMOVED AND REPLACED HOSE ASSY NR 1 FOR RESERVOIR PRESS AND HOSE ASSY FOR AC PUMP SUCTION, OPS CHECK GOOD AT THIS TIME. WORK DONE IAW AMM 29-10-00 (SDR CLO SED). (A) 2 L 7 2 4F RT A21EA 20080905 EA 2008 9 5 TRAX200800807 1 20080620 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 930EV 8014 RIGHT FS 621 ANGLE CRACKED. JOB COMPLETED REPAIRED ITEM BY ACCOMPLISHMENT OF REO 601R-53-61-117. RII REQUIREMENTS MET PER SP 607. JOB COMPLETE [SUPPLEMENTAL SDR CLOSED 6/25/08] (B) 2 L 7 2 4F RT A21EA 20080905 NM 2008 9 5 2008UALA03926 1 20080723 A 2432 276005 FUSE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BATTERY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 642UA 25092 AIRCRAFT BATTERY IS INOP. AIRCRAFT WILL NOT POWER UP. INSTALLED NEW BATTERY. STILL DID NOT POWER UP. REPLACED INTERL OCK FUSES IN P34 PANEL. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20080905 EU 2008 9 5 2008UALA03927 1 20080722 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 496UA 1845 EPSU UNIT AFT L MESSAGE DISPLAYED AFTER EMERGENCY LIGHT CHECK. *S/D* EPSU FAILED. REPLACED EPSU, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080905 NM 2008 9 5 2008UALA03928 1 20080722 A 3350 362624 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 338UA 24242 FLOOR EEL INOP FROM ROW 16 TO AFT OF AIRCRAFT. FOUND LIGHT STRIP FAULTY. REPLACED LAMP STRIP OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080905 NM 2008 9 5 CALA0822739 1 20080723 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM BS 827 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14629 27533 FRAME CRACKED AT STATION 827 S-9LT. PERFORMED INTERIM REPAIR BY REMOVING DAMAGE, PERFORMING NDT INSPECTION, FABRICATING AND INSTALLING REPAIR DOUBLERS PER ECRA 5310-04807 PART 1. INITIATED DIP 089441 TO PERFORM THE INSPECTION PER ECRA 531 0-04807 PART 2 ON THE FRAME REPAIR BETWEEN S-8 AND S-9, ON LEFT SIDE STATION 827 BEFORE 56250 TOTAL AIRCRAFT CYCLES. 2 L 7 2 4F RT A16WE 20080905 NM 2008 9 5 2008UALA03960 1 20080723 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHTS FLASHING RIGHT AISLE SEAT 6 TO 8. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECK GOOD. AC OK FO R SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080905 EU 2008 9 5 2008UALA03895 1 20080717 A 5320 SHEAR PLATE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 449UA 851 FOUND RT SHEAR PLATE CORRODED BETWEEN FRAME 69 AND 70 REF EQ3700. *S/D* ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED SH EAR PLATE, INSTALLED SAME NEW. 2 L 7 2 4F 4 F RT A28NM E40NE 20080905 NM 2008 9 5 2008UALA03966 1 20080725 A 2121 FAN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EQUIP COOLING SMOKE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 646UA 25283 SMOKE ODOR IN CABIN. FLT DIVERTED. FOUND APU OPERATION NORMAL. REPLACED EQUIP COOLING EXHAUST FAN AS A PRECAUTION. 2 L 7 2 4F 4 F RT A1NM E24NE 20080905 EU 2008 9 5 2008UALA03911 1 20080717 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 441UA 751 FOUND 2 DENTS AT SECTION FR23 AT FLOOR LEVEL ON LEFT SIDE OF AIRCRAFT. *S/D* ACCOMPLISHED MAJOR REPAIR AT IAD. CLEANE D AREAS, CHECKED FOR CRACKS, NONE FOUND. TREATED AREAS, PRIMED AREAS, PAINTED AREAS. OK PER SRM 53-00-11. 2 L 7 2 4F 4 F RT A28NM E40NE 20080905 EU 2008 9 5 2008UALA03912 1 20080717 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 441UA 751 FUSELAGE DENT FRAME 30 STRINGER 25R. *S/D* ACCOMPLISHED MAJOR REPAIR AT LCQ. INSTALLED DOUBLER REPAIR PER SRM 53-21-1 1 FIG 215. 2 L 7 2 4F 4 F RT A28NM E40NE 20080905 NM 2008 9 5 2008UALA03859 1 20080713 A 5240 ARM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR OBSTRUCTED A UALA K NONE C F.O.D. IN INSP/MAINT 1 WP 29 512UA 24809 UNABLE TO ARM DOOR 3R. *S/D* DEBRIS UNDER DOOR LEDGE. REMOVED DEBRIS FROM UNDER DOOR LEDGE. DOOR ARMS/DISARMS NORMAL LY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080905 NM 2008 9 5 2008UALA03860 1 20080713 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 511UA 24799 EMERGENCY LIGHT AT SEAT ROW 27DEF INOP. *S/D* LAMPS INOP AT ROW 27. RE-LAMPED ASSY AT ROW 27, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080905 NM 2008 9 5 2008UALA03862 1 20080713 A 2612 330TS08Y PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE TEST SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 544UA 25322 RT ENGINE OVHT LIGHT ON CENTER PEDESTAL INOP DURING FIRE TEST. *S/D* SHORT IN ENG FIRE TEST PANEL. REPLACED ENG FIRE PANEL ON PEDESTAL, GROUND CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080905 EU 2008 9 5 2008UALA03863 1 20080711 A 3510 OXYGEN BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 464UA 1290 COCKPIT OXYGEN BOTTLE -LOW. *S/D* SERVICED CREW O2, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080905 EU 2008 9 5 2008UALA03873 1 20080714 A 5311 FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 441UA 751 R2 DOOR SILL CORROSION AT FASTENER HOLE FRAME 66. *S/D* ACCOMPLISHED MAJOR REPAIR AT LCQ. INSTALLED REPAIR PER SRM 53 -41-14. 2 L 7 2 4F 4 F RT A28NM E40NE 20080905 EU 2008 9 5 2008UALA03898 1 20080717 A 5310 BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 449UA 851 FOUND BEAM 205 CORRODED REF EQ3700. *S/D* ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED BEAM, PREPPED AND RE-INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080905 EU 2008 9 5 2008UALA03900 1 20080717 A 5310 BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 449UA 851 FOUND BEAM 210 CORRODED REF EQ3700. *S/D* ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED BEAM, PREPPED AND RE-INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080905 EU 2008 9 5 2008UALA03902 1 20080717 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 449UA 851 FOUND FLOORBEAM 235 CORRODED REF EQ3700. *S/D* ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED BEAM, ON WORKBENCH. INSTALL ED SPLICE ON BEAM AND PAINTED. INSTALLED BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20080905 EU 2008 9 5 2008UALA03903 1 20080717 A 5320 PAN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 449UA 851 EXCESSIVE MATERIAL REMOVED FROM DOOR 2L DOOR SILL PAN AFT END AT 2EA NUT PLATE HOLES REF SMC 28. *S/D* ACCOMPLISHED MA JOR REPAIR AT DEN. REMOVED DAMAGE MATERIAL, FABRICATED REPAIR PARTS, AND INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080905 NM 2008 9 5 2008UALA03954 1 20080723 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 L-2 DOOR REQUIRES DOUBLER AT UPPER HINGE ARM CUTOUT. ACCOMPLISHED MAJOR REPAIR AT GSO. CUT OUT DAMAGE AND INSTALLED D OUBLER REPAIR PER MM 52-11-87 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E17NE 20080905 NM 2008 9 5 2008UALA03918 1 20080723 A 2840 HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUEL FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 175UA 24382 FUEL IMBALANCE. FLIGHT DIVERTED. REPLACED LO-Z HARNESS IN NR 3 MAIN. 2 L 7 4 4F 4 F RT A20WE E24NE 20080902 CE 2008 9 2 GLB2008F00015 1 20080815 A 6123 AUTOFEATHER SYS BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3A NE MALFUNCTIONED A GLBA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 NM 03 211GL UE211 PS0077 ACFT 211GL SUSPECTED AUTOFEATHER FLT 5127 "PIR" 08/15/08 PILOTS REPORTED DURING FINAL DESCENT INTO LANDING, THAT POWER W AS REDUCED TO APPROX 500 LBS WITH PROPS FULL FORWARD. DURING POWER REDUCTION ONE OR BOTH PROPELLERS APPEARED TO FEATHER , THEN SURGE. POWER WAS INCREASED AFTER 10 SECONDS. ENGINES STABILIZED AND A SAFE LANDING MADE. DURING THE EVENT THE AFX DISABLE ILLUMINATED, THEN EXTINGUISHED WHEN POWER WAS REINTRODUCED. MAINTENANCE PERFORMED AFTER START CHECKLIST FI RST LIGHT ITEMS AS PER FSM 3.5.10 AND MM 61-10. OPERATIONAL CHECKS SATISFACTORY. (S) 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 20080902 WP 2008 9 2 IXX2008F00062 1 20080709 A 5730 SKIN DOUG DC8 DC872F 302199E WP RIGHT WING MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR RT WING OUTBOARD SLOT VANE LEADING EDGE AT STATION XOLDI 6.224. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECT ION. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLERS, FILLERS, AND INTERNAL DOUBLERS. CLEANED, TREATED AND P RIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XOLDI 6.224-XOLDO 67.000 IAW FAA FORM 8110-3 08378 DATED 07/11/2008, SEMAN DRAWING ED-4809 DATED 06/23/08, DC8 SRM 51-1-21, SRM 51-3-0, DC8 NDT SPM PART 06-10 -01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-1-20D AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080902 EA 2008 9 2 QXEA200800599 1 20080530 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 752 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 610QX 10033 RFD-C4 CHECK - CORRODED SIDE SEAT TRACK ON RT SIDE AT FS 752. BLENDED CORROSION FROM RT SIDE SEAT TRACK AT FS 752. REM OVED .006 MATERIAL FOR BLEND, WITHIN LIMITS, MAX ALLOWABLE BLEND IS .035 INCHES. ALL WORK DONE IAW CRJ BOMB REO 670-53- 00-013. TREATED IAW CRJ 700 SRM 51-21-11. (S) 2 L 7 2 4F RT A21EA 20080902 NM 2008 9 2 QXEA200800917 1 20080817 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM UNKNOWN A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 19 345PH 476 PDX - FLIGHT 2129. FLIGHT ATTENDANT REPORTS A "FOG" COMING FROM THE LAST 3 ROWS FROM ENG START THROUGH 10,000, THEN DIS APPEARED. MAINTENANCE PERFORMED A GROUND RUN OF THE ENGS WITH INDEPENDENT USE OF THE BLEED AIR. NO FOG, OR OTHER DEFE CTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED. (S) 2 H 7 2 4T RT A13NM 20080902 SO 2008 9 2 RAIA00808004 1 20080804 A 5210 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR DIRTY A RAIA O OTHER C F.O.D. TX TAXI/GRND HDL 1 CE 03 838HK 145321 POST FLT 7997 - RIC - PASSENGER DOOR DIFFICULT TO OPEN AND CLOSE. MAINTENANCE CLEANED AND LUBED THE DOOR SEAL. OPS CHE CKED GOOD. 2 L 7 2 4T RT T00011AT 20080902 SO 2008 9 2 RAIA00806022 1 20080626 A 2750 3631001011 CONTROL VALVE EMB 145 EMB145LR 3260212 SO TE FLAPS MALFUNCTIONED A RAIA O OTHER J WARNING INDICATION LD LANDING 1 CE 03 851HK 145340 FLT 7878 - DEN - DURING LANDING, CREW RECEIVED A FLAP LOW SPEED MESSAGE ON THE EICAS. MAINTENANCE REPLACED THE FECU SYS TEM, OPS CHECKED GOOD. WD:LD HD:J (A) 2 L 7 2 4T RT T00011AT 20080902 SO 2008 9 2 RAIA00808007 1 20080806 A 3320 LIGHT EMB 145 EMB145 3260210 SO CABIN SMOKE A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 807HK 145119 FLT 7884-ORD - DURING TAXI, BURNING ODOR STARTED COMING FROM THE SIDEWALL LIGHTS AT 18BC. MAINTENANCE REMOVED THE LIGHT BULBS AND PLACED THE READING LIGHT ON DEFERRAL IAW MEL PROCEDURES. (S) 2 L 7 2 4F RT T00011AT 20080902 NM 2008 9 2 SWAA084468 1 20080812 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 245WN 32506 DURING SCHEDULED MV3 CHECK, FOUND RT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 USAA920081505 1 20080811 A 5755 SKIN BOEING 737 7374B7 1384702 NM NR 3 SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 458UW 03671 25022 CLT-C6 -MAJOR REPAIR- LT WING NR 3 SPOILER DELAMINATED. REPLACED LT WING NR 3 SPOILER IAW B737 AMM 27-61-11. (S) 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084467 1 20080812 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 797, STR 26L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 USAA920081551 1 20080802 A 5320 D53471123202 PLATE AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 833AW 1844 SAL-BC4 -MAJOR REPAIR- GALVANIC CORROSION ON LATERAL SUPPORT PLATE FROM FR69 TO FR70, Y1732. REPLACED LATERAL SUPPORT P LATE FROM FR69 TO FR79, Y1732 IAW A319 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080902 NM 2008 9 2 SWAA084448 1 20080812 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 251WN 32510 DURING SCHEDULED MV2 CHECK, FOUND RT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084447 1 20080812 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 232WN 32500 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080902 EU 2008 9 2 USAA920081475 1 20080805 A 2820 L95F50603 DISC AIRBUS A321 A321211 3930370 EU ZONE 500 RUPTURED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 172US 1472 FLT 1508 SAN-PHL - DIVERSION/IFSD - FUEL SYSTEM BURNED FUEL ONLY FROM LT MAIN TANK. THE CAPTAIN REPORTED, UNABLE TO STO P THE TRANSFER. IMBALANCE STOPPED AT 6000 LBS WHEN THE ENGINE WAS SHUT DOWN. THE ACFT DIVERTED TO PHX AND LANDED WITHO UT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE OVERPRESSURE PROTECTOR. (S) 2 L 7 2 4F RT A28NM 20080902 NM 2008 9 2 USAA920081485 1 20080731 A 5320 D53472172204 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 833AW 1844 SAL-BC4 -MAJOR REPAIR- CORROSION ON FLOORBEAM AT FR66 TO FR67, Y1180. REPLACED FLOORBEAM AT FR66 TO FR67, Y1180 IAW A31 9 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080903 EA 2008 9 3 A6WA200840558 1 20080804 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 448AW 7814 FLAPS FAIL AT ZERO DURING APPROACH. FOUND REPEAT LT BPSU, FECU, WIRING FAULT CODES. CONTINUITY RESISTANCE & MEGGER CHE CKED LT BPSU WIRING. NO FAULTS FOUND. REPLACED FECU PER AMM CH 27-50. OPS CHECK AND RIG CHECKS GOOD. 2 L 7 2 4F RT A21EA 20080903 NM 2008 9 3 UIEA200800292 1 20080804 A 5330 SKIN BOEING 747 747400 13848AT NM GE CF6 CF680C2* GL FUSELAGE CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 429MC 24833 DURING C-CHECK AFT CARGO DOOR CUTOUT FORWARD UPPER CORNER FOUND CRACKED AT FASTENER HOLE. REPAIRED AS PER SRM 53-60-01 FIGURE 201. (S) 2 L 7 4 4F 4 F RT A20WE E23EA 20080903 NM 2008 9 3 KCSA081412 1 20080820 A 5730 SKIN BOEING 747 747132 1384882 NM RWS 1481 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 709CK 20247 RT WING STA 1481 HAS CORROSION ON UPPER SURFACE OF THE LOWER SKIN. (S) 2 L 7 4 4F RT A20WE 20080904 NM 2008 9 4 DHL2008F00014 1 20080622 A 5314 6947111Y2 KEELBEAM BOEING 727 7272M7 138407S NM BS 740 CORRODED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 SURFACE CORROSION FRONT LOWER CHORD CENTER OF KEEL BEAM BS 740. REMOVED AND REPLACED BS 740 LOWER CHORD T ANGLE P/N 69- 4711Y2, PO 8180132 IAW B727 SRM 51-30-2. T-ANGLE ORIGINAL EVALUATED OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. (A) 2 L 7 3 4F A3WE 20080904 WP 2008 9 4 G412008F00000 1 20080606 A 2697 GROUND WIRE DOUG DC8 DC871F 302199D WP NR 1 NACELLE BROKEN E G41A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 01 822BX 93049 173 45813 AFTER TAKEOFF FROM KIAH, NR 1 ENGINE FIRE WARNING SOUNDED, FIRE HANDLE LIGHT, AND MASTER FIRE WARNING LIGHT ILLUMINATED. WARNING HORN COULD BE SILENCED BUT CAME BACK ON THREE TIMES. ENGINE FIRE HANDLE SUBSEQUENTLY PLACED IN SELECT AGENT P OSITION; LIGHT AND HORN SILENCED. ACFT RETURNED TO KIAH WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND AND REPAIRED A BRO KEN GROUND WIRE ON RT SIDE UPPER HOT SECTION FIRE LOOP IAW MM 20-50-1. ADDITIONALLY, NR 1 ENGINE FIRE DETECTOR SYSTEM O PERATIONAL CHECK GOOD IAW MM 26-11-16. (A) 2 L 7 4 4F RT 4A25 20080904 EA 2008 9 4 TRAX200800926 1 20080724 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 681BR 7680 F/A REPORTS MAIN PAX DOOR OPENS AND CLOSES WITH DIFFICULTY. OPERATED PAX DOOR MULTIPLE TIMES, OPS CK GOOD IAW AMM 52-10 -00. (A) 2 L 7 2 4F RT A21EA 20080904 WP 2008 9 4 DHL2008F00016 1 20080716 A 2612 FIRE WARNING DOUG DC8 DC871F 302199D WP NR 4 NACELLE ACTIVATED A DHLA F A ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 828BX 45993 FLT NR ATN 819 / KDFW TO KTOL. DURING CLIMBOUT FROM KDFW NR 4 ENGINE FIRE WARNING LIGHT CAME ON, THE CREW DISCHARGED BO TH FIRE BOTTLES AND LIGHT REMAINED ON. THE CREW RETURNED TO KDFW AND LANDED WITHOUT INCIDENT. CORRECTIVE ACTION IN WOR K. (A) 2 L 7 4 4F RT 4A25 20080904 EA 2008 9 4 QXEA200800716 1 20080710 A 5347 58401A2B5C5F4L30 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 677 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 612QX 10042 PDX-C4 CHECK - CORROSION AT RT INBOARD SEAT TRACK AT STATION 677.00. BLENDED AREA. MATERIAL REMOVED WITHIN LIMITS OF R EO 670-53-00-012. ALODINED TRACK. (A) 2 L 7 2 4F RT A21EA 20080905 NE 2008 9 5 DHLA200800082 2 20080720 A 7230 COMPRESSOR BOEING 727 727227 1384078 NM PWA JT8 JT8D17 52049 NE ENGINE STALLED A DHLA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 01 781DH 21996 ENG FAIL LIGHT/AUTO PACK TRIP LIGHT FAILED AS THRUST APPLIED FOR T/O. RAN APPROPRIATE PROCEDURE IN AOM. CONTACTED MX A ND DISPATCH. ALL INDICATIONS NORMAL AFTER PROCEDURE, APPARENT COMPRESSOR STALL AS THRUST APPLIED. NOTE, CREW REPORTED HEAVY CROSSWINDS DURING T/O OUT OF ILN DURING APPARENT COMPRESSOR STALL. PERFORMED HIGH POWER ENGINE RUNS PER JRH 5.2 A ND FOUND TO BE OPERATIVE NORMALLY PER P&W MM 72-00-0. INLET INSP NO DEFECTS NOTED. FLT NR 1703. AIRCRAFT WAS GROUNDED . (A) 2 L 7 3 4F 4 F A3WE E2EA 20080905 NM 2008 9 5 USAA920081375 1 20080711 A 5310 6545807U79 DOOR FRAME BOEING 737 737401 1384701 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT-Q3 CHECK -MAJOR REPAIR- CRACK IN FRAME AT RIGHT FORWARD SERVICE DOOR CUTOUT AT FORWARD LOWER CORNER BS 294.5. REPLA CED FRAME AT RIGHT HAND FORWARD SERVICE DOOR CUTOUT AT FORWARD LOWER CORNER BS 294.5 IAW B737 SRM 51-10-02 AND BOEING DR AWING 65-45807. (B) 2 L 7 2 4F RT A16WE 20080905 NM 2008 9 5 USAA920081339 1 20080708 A 5313 03530030730 STRINGER BOEING 737 737401 1384701 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT-Q3 -MAJOR REPAIR- CRACK IN STRINGER SPLICE AT BS 908, S4L. REPLACED STRINGER SPLICE AT BS 908, S4L IAW B737 SRM 51- 10-02. (B) 2 L 7 2 4F RT A16WE 20080905 NM 2008 9 5 USAA920081376 1 20080712 A 5340 66244912 TEE FITTING BOEING 737 737401 1384701 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT-Q3 CHECK -MAJOR REPAIR- AFT T-FITTING CRACKED IN RADIUS AT UPPER DOOR STOP BS 332.1, S8R. REPLACED AFT T-FITTING IN RADIUS AT UPPER DOOR STOP BS 332.1, S8R IAW BOEING DRAWING 66-24491. (B) 2 L 7 2 4F RT A16WE 20080905 EA 2008 9 5 TRAX200800660 1 20080518 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 ASD BOTTOM STEP CRACKED. REMOVED AND REPLACED ASD BOTTOM STEP IAW AMM 52-11-04. OPS CK GOOD. (B) 2 L 7 2 4F RT A21EA 20080905 NM 2008 9 5 2008UALA03883 1 20080715 A 2497 CONTACTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE DC BUSS SHORTED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 810UA 843 ELECTRICAL PROBLEMS AFTER TAKEOFF. RTFL. ON CLIMBOUT ECAM DC ESS SHED DISPLAYED FOLLOWED BY ECAM CB LFT ELECT BAY. LO SS OF FAC1, FMGC1, AP1, NAVGPWS. DC SHED ESS BUSS CONTACTOR SHORTED. REPLACED CNTOR DC SHED ESS BUS, OPS CHECKED NORMA L. 2 L 7 2 4F 4 F RT A28NM E40NE 20080905 NM 2008 9 5 2008UALA03974 1 20080725 A 5730 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 174UA 24381 UPPER LT WING L/E SURFACE, JUST OUTBOARD OF NR 2 ENG, HAS CRACK APPROX 4 FEET IN LENGTH, ORIENTATED IN A FORE TO AFT DIR ECTION. DOUBLER MANUFACTURED. LAID UP & DRILLING FASTENER HOLES. DOUBLER REPAIR INSTALLED. 2 L 7 4 4F 4 F RT A20WE E24NE 20080905 SO 2008 9 5 SIMA200820701 1 20080724 A 3240 21707 BRAKE EMB 145 EMB145LR 3260212 SO MLG CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 683AE 14500833 ON WALK AROUND AFTER A PS-1 INSPECTOR NOTED THAT THE NUMBER ONE TIRE WAS WORN TO LIMITS. DURING REMOVAL OF TIRE MAINTEN ANCE NOTED THAT THE NUMBER 1 BRAKE BROKE APART DURING REMOVAL. REPLACED THE NUMBER ONE BRAKE ASSEMBLY. AIRCRAFT RETURN ED TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080908 EA 2008 9 8 TRAX200800870 1 20080703 A 3231 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 979EV 7737 DURING GEAR RETRACTION HEARD A CONSISTANT MECHANICAL BANKING UNDER COCKPIT FOR APP 8 SECONDS. NOISE OCCURED APP 2 TIMES /SECOND. FLT 4743 DEL 45 MINS. EMERGENCY DECLARED. REMOVED AND REPLACED NOSE LANDING GEAR ACTUATOR AND DOOR SELECTOR VALVE IAW AMM 32-22-10 AND AMM 32-22-20. OPS CHECK GOOD. OK FOR SERVICE. (B) 2 L 7 2 4F RT A21EA 20080908 EA 2008 9 8 TRAX200800852 1 20080630 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 202 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 861AS 7445 SUSPECT CRACK AT FWD PRESSURE BULKHEAD FS 202.75 AT THE PILOTS BRAKE CONTROL PUSH/PULL CABLE LOCATION. THIS SDR WILL RE MAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. (B) 2 L 7 2 4F RT A21EA 20080908 NM 2008 9 8 2008UALA03815 1 20080710 A 3350 90085 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 OVERWING EMERGENCY LIGHT LT TWO LOWER LIGHT INOP. FOUND FAULTY POWER SUPPLY. REPLACED POWER SUPPLY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03610 1 20080626 A 3350 BPS73 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 CABIN C-ZONE RT SEAT EEL'S ONLY STAY ILLUMINATED FOR A FEW SECONDS. SUSPECT FAULTY BATTERY PACK. REPLACED BATTERY PACK , OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03637 1 20080628 A 3350 BPS73 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EEL INOP: SEATS 32-34 ABC. FOUND FAULTY BATTERY. REPLACED BATTERY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03641 1 20080628 A 3350 GE209 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY CEILING LIGHT INOP AT ROW 39. FOUND BURNED OUT BULB. REPLACED BULB, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03644 1 20080630 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 4J AFT LIGHT ASSY. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03646 1 20080630 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 35 LEFT. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVI CE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 EA 2008 9 8 TRAX200800765 1 20080605 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FS 280 LBL 9 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 684BR 7708 BULKHEAD FS 280.00 LBL 9.0 HAS A CLIP CRACKED .5 INCH. REMOVED OLD CRACKED CLIP AT FS 280.00 LBL 9.0, INSTALLED NEW SER VICEABLE CLIP P/N 601R-31113-57 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (B) 2 L 7 2 4F RT A21EA 20080908 NM 2008 9 8 2008UALA03905 1 20080719 A 2133 OUTFLOW VALVE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN AIR INOPERATIVE A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 27UA 1022 LANDED ORD UNDER AMBER ALERT DUE TO AN ELECTRICAL ODOR IN THE COCKPIT. SKIN AIR VALVE FAILED. REPLACED SKIN AIR VALVE AND TWO FILTERS. 2 L 7 2 4F 4 F RT A28NM E40NE 20080908 NM 2008 9 8 2008UALA03655 1 20080701 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY LIGHT ROW 53 LT INOP. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 DHLA200800056 1 20080609 A 3246 31395 WHEEL BOEING 727 727225 1384077 NM NLG VIBRATION A DHLA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 01 748DH 22440 RTO DUE TO HEAVY VIBRATION THAT SEEMED TO EMANATE FROM NOSE WHEEL NOTE RTO AT 80 KIAS FULL REVERSE & MODERATE BREAKING U SED. REMOVED AND REPLACED BOTH NOSE WHEELS PER MM 32-45-11. FIT 520. AIRCRAFT WAS GROUNDED. (A) 2 L 7 3 4F A3WE 20080908 NM 2008 9 8 2008UALA03166 1 20080603 A 3350 GE209 BULB BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 DOOR 3 RIGHT FWD SILL EMERGENCY LIGHT IS INOP. FOUND BURNED OUT BULB. REPLACED BULB, OP CHECKED GOOD. AC OK FOR SERVI CE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03172 1 20080530 A 5311 FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 720 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 128UA 33421 30023 FWD PIT FRAME STA 720 HAS DAMAGE. SUSPECT GROUND EQUIPMENT DAMAGE. INSTALLED MANUFACTURED PARTS PER SRM 51-70-12, DETA IL III. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03868 1 20080712 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1400 S15-16L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 AFT PIT FRAME DENTED AT INBOARD FLANGE, BS 1400 BETWEEN STR 15L-26L. ACCOMPLISHED MAJOR REPAIR. CUT OUT FRAME DAMAGE A ND INSTALLED DOUBLER REPAIR PER SRM 53-00-07, REPAIR 5. 2 L 7 2 4F 4 F RT A2NM E17NE 20080908 NM 2008 9 8 USAA920081356 1 20080710 A 2560 P4010021 BATTERY BOEING 737 7373S3 1384711 NM FLASHLIGHT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 315AW 23734 SNA - FLT 126 - FWD EMERGENCY FLASHLIGHT INOP. MX REPLACED FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD. (B) 2 L 7 2 4F RT A16WE 20080908 2008 9 8 2008UALA03880 4 20080714 A 2340 MICROPHONE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CAPTAIN'S DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 569UA 26677 CAPT HAND MIC DEFECTIVE. SHORTED MIC. REPLACED CAPT HAND MIC ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080908 NM 2008 9 8 2008UALA03677 1 20080702 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 4A AFT LIGHT ASSY. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03678 1 20080702 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 5F AFT LIGHT ASSY. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03679 1 20080702 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 58 LEFT. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVI CE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03739 1 20080706 A 2560 65B549299 GIRT BAR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ESCAPE SLIDE LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 116UA 26908 DOOR 5L GIRT BAR HANGING FROM DOOR WHEN CLEANERS OPENED DOOR. SUSPECT IMPROPERLY STOWED. REPOSITIONED GIRT BAR, OPERAT ION CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03743 1 20080707 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 FWD EEL INOP SEAT 2J. FOUND LAMP INOP AT SEAT 2J. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03744 1 20080707 A 3350 582240 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EEL'S INOP, ZONE C RT COLUMN AT SEATS 32H, 33H, 34H, LAV 112 SIDEWALL, LAV 111 FRONT WALL. SUSPECT FAULTY BATTERY PACK. REPLACED BATTERY PACK, OP CHECK OK REF MM 33-51-04. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 WP 2008 9 8 WX02008F00001 1 20080701 A 7500 MANIFOLD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE 13TH STAGE BLEED LEAKING A WX0A A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 19 887GA 49932 708108 FLIGHT CREW PERSONNEL REPORTED ON THE INITIAL CLIMBOUT OF FLIGHT 883-3 FROM PIE, THE FIRE DETECTOR HANDLE AND LOOP "A" I LLUMINATED ON THE LT ENGINE. THE AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE DEPARTMENT PERSONNEL PERFO RMED A VISUAL INSPECTION OF THE LT ENGINE AND DETERMINED THE 13TH STAGE BLEED MANIFOLD LEAKING HOT BLEED AIR INTO THE EN GINE NACELLE. THE LT ENGINE WAS REPLACED IAW ALL AMM PROCEDURES. THE AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 2 4F 4 F A6WE E9NE 20080908 NM 2008 9 8 2008UALA03605 1 20080627 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 SEAT 5A AFT EMERGENCY LIGHT IS INOP. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 DHL2008F00005 1 20080627 A 5753 STRUCTURE BOEING 727 7272J0 138407E NM LT WING TE FLAP CRACKED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 749DH 1711 22013 POSSIBLE CRACK ON NR 1 K-FLAP AT BOTTOM INBOARD CORNER. STOP DRILLED CRACK AND FABRICATED DOUBLER FROM 2024-TS 2,375 Z 2,375 X .062 (PO 4-6686) TREATED, PRIMED AND PAINTED THEN INSTALLED WITH SEALANT AND NAS1097D6 RIVETS, IAW BOEING 727 SR M 57-60-3. THIS IS A MINOR REPAIR. (A) 2 L 7 3 4F RT A3WE 20080908 NM 2008 9 8 2008UALA03849 1 20080713 A 2421 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LACK OF LUBE A UALA A UNSCHED LANDING W Y J INADEQUATE Q C ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 WP 29 597UA 28750 FAILED ENGINE GENERATOR. RTFL. IDG SHUTDOWN DUE TO LOW OIL. SERVICED IDG, NO REPEATS ON SUBSEQUENT FLIGHTS. 2 L 7 2 4F 4 F RT A2NM E17NE 20080908 NM 2008 9 8 2008UALA03910 1 20080718 A 8011 35054367 STARTER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 1 ENGINE FAILED A UALA D RETURN TO BLOCK R Y J PARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 665UA 29237 ENG 1 HUNG START AT 43 PERCENT N2, EGT STABLE, START VALVE MESSAGE & START VALVE LIGHT DISAGREE ON OVERHEAD PANEL. ENGI NE SHUT DOWN. GROUND CREW REPORTED LOUD BANG. FOUND STARTER SOAKED WITH OIL. OPENED START VALVE AND THERE WAS A STEADY STREAM OF OIL OUT THE AIR EXIT VANES OF THE STARTER WITH NO ENG ROTATION. REPLACED STARTER. 2 L 7 2 4F 4 F RT A1NM E24NE 20080908 NM 2008 9 8 2008UALA03303 1 20080610 A 3350 417U52201 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 58 ABC INADEQUATE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 THE 58 ABC EMERGENCY PATH LIGHTS ARE INADEQUATE. FOUND LIGHT ASSEMBLY PROTRUDING. REPLACED LIGHT ASSEMBLY. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NE 2008 9 8 AIEA200800260 2 20080707 A 7261 ENGINE BOEING 747 74747UF 1384812 NM GE CF6 CF680 30025 NE NR 3 OIL CONSUMPTION A AIEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 408MC 29261 ENGINE NR 3 OIL QTY WENT TO 0 (3 HOURS AFTER TAKEOFF). ENGINE SHUT DOWN PRECAUTIONARY. FIM 79-00-00 FOLLOWED. INSPECT ED FOR OIL LEAK. NO WETTING FOUND. REPLENISHED 22 QTS OIL AND LEAK AND OPS CHECK PERFORMED. NO LEAK FOUND. IDG AND S TARTER DRAIN LINE CAPPED FOR MONITORING PER AMM 71-71-00. (A) 2 L 7 4 4F 4 F RT A20WE E13NE 20080908 NM 2008 9 8 AIEA200800256 1 20080707 A 2612 FIRE DETECTOR BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE CARGO BAY DIRTY A AIEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 517MC 23300 RETURN TO BLOCKS INTERMITTENT FIRE WARNING DURING TAXI. FOUND EVIDENCE OF DE-GERM IN CARGO SNIFFED TUBE. CLEANED SNUFF ER TUBES WITH CONTACT CLEANER. SYSTEM OPS CHECK NORMAL AS PER MM 26-16-00. (A) 2 L 7 4 4F 4 F RT A20WE E23EA 20080908 NM 2008 9 8 AIEA200800257 1 20080707 A 5311 FRAME BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE BS 280 S26R CRACKED A AIEA K NONE O OTHER IN INSP/MAINT 1 GL 11 540MC 22508 DURING C-CHECK FOUND FRAME CRACKED AT STATION 280 STRINGER 26R. FRAME REPAIRED AS PER SRM 53-10-04 FIGURE 10. (A) 2 L 7 4 4F 4 F RT A20WE E23EA 20080908 NM 2008 9 8 2008UALA03494 1 20080619 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT AFT GALLEY RT BOTTOM WALL INOP. FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECKED GOOD. AC OK FO R SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03846 1 20080710 A 4920 BLEED VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU FAULTED A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 642UA 25092 APU AUTO SHUTDOWN DURING TAXI OUT. APU AUTO SHUTDOWN DURING TAXI OUT. CONFIRMED APU SURGE BLEED CONTROL VALVE MALFUNCTI ONING. REPLACED BLEED VALVE. OPS CHECK OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20080908 NM 2008 9 8 2008UALA03858 1 20080713 A 7931 MR7937721 TRANSMITTER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OIL PRESSURE READS HIGH A UALA O OTHER N FALSE WARNING CL CLIMB 1 WP 29 663UA 65469 5303 27160 717550 DURING CLIMB LEFT ENG OIL PRESS PEGGED OUT AT 400 PSI AT LEVEL OFF PRESS JUMPED TO 200. REPLACED OIL PRESSURE TRANSMITT ER. 2 L 7 2 4F 4 F RT A1NM E24NE 20080908 EU 2008 9 8 2008UALA03908 2 20080717 A 7200 BEARING CAGE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU LT ENGINE FAILED A UALA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 WP 29 934UA 26662 LT ENG FAILED ON TAKEOFF. AFTER TAKEOFF APPROX 500 FT AGL LOUD BANG, ENG SPOOLED DOWN. LT ENG FAILED ON TAKEOFF. AFTE R TAKEOFF LOUD BANG ENGINE SPOOLED DOWN. IFSD. CREW SECURED ENGINE. INLET AND EXHAUST CHECKED CLEAN. LCL AMT REPORTS FWD CHIP DET (AGB-TGB) FULL OF METAL. MID CHIP DETECTOR FWD SUMP) ALSO METAL. BOTH CHIP DETS HAVE FERROUS & NON FERROUS METAL. ECM EGT EXCD 978DEGS. THE ENGINE WAS REPLACED. NO ADDITIONAL FINDINGS ARE EXPECTED DUE TO FLEET RETIREMENT. 2 L 7 2 4F 4 F RT A16WE E21EU 20080908 NM 2008 9 8 2008UALA03787 1 20080708 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EEL INOP: SEAT 51 RT. FOUND LAMP INOP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03476 1 20080619 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY LIGHT INOP: CEILING ROW 13. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03477 1 20080619 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EEL INOP: SEAT 56 RT. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03383 1 20080615 A 3397 80541 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 WALL EEL INOP: BETWEEN MID LAVS CROSS AISLE. FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03411 1 20080615 A 3350 417U50251 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW REST AREA INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT INOP: AFT CREW REST STAIRS ILLUM. SUSPECT FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03431 1 20080613 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 127UA 28813 THE 3A EEL STRIP MISSING. FOUND LIGHT STRIP MISSING. REPLACED LIGHT STRIP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 AIEA200800259 1 20080707 A 5311 FRAME BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE BS 320 S25R CRACKED A AIEA K NONE O OTHER IN INSP/MAINT 1 GL 11 540MC 22508 DURING C-CHECK FOUND FRAME CRACKED AT STATION 320 STRINGER 25R. FRAME REPAIRED AS PER SRM 53-10-04 FIGURE 10. (A) 2 L 7 4 4F 4 F RT A20WE E23EA 20080905 NM 2008 9 5 2008UALA03953 1 20080723 A 5240 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 R-2 DOOR REQUIRES DOUBLER AT UPPER HINGE ARM CUTOUT. ACCOMPLISHED MAJOR REPAIR AT GSO. ACP'D HFEC INSPECTION PER NDT 6 -51-00-19 AND FOUND CRACK APPROX .25 INCH LONG AT CUTOUT, CUTOUT DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 51-40-02, A ND MM 52-11-87. 2 L 7 2 4F 4 F RT A2NM E17NE 20080905 SO 2008 9 5 SIMA200820704 1 20080723 A 3240 15851 SWITCH EMB 135 EMB135KL 3260302 SO PARKING BRAKE MALFUNCTIONED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 844AE 145682 ON FLIGHT 3888 DURING CRUISE CREW REPORTED PARKING BRAKE LIGHT ON INDICATION WHILE IN FLIGHT SUBSEQUENTLY ON THE GROUND. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. NO PRESSURE NOTED ON PARKING BRAKE WHILE RELEASED. REPLACED PRE SSURE SWITCH EMERGENCY PARKING BRAKE IAW EMB AMM 32-44-07, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080905 NM 2008 9 5 USAA920081342 1 20080709 A 5340 STRINGER CLIP BOEING 737 737401 1384701 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT -MAJOR REPAIR- Q3 CHECK- CRACKED STRINGER CLIP, BS 460, S16L. REPLACED STRINGER CLIP, BS 460, S16L IAW B737 SRM 51- 10-02. (B) 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084457 1 20080812 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 497WN 32479 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 11 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080902 EU 2008 9 2 USAA920081498 1 20080810 A 2560 P4010021 BATTERY AIRBUS 320 A320231 3930325 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 620AW 052 FLT 180 PHX-SAN - EMERG EQUIP - FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE F LASHLIGHT BATTERY. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A28NM 20080903 CE 2008 9 3 DXTA200803224 1 20080814 A 3150 WARNING MESSAGE CESSNA 750 750 2076810 CE ILLUMINATED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 960QS 7500160 AFTER TAKEOFF "RUD LIMIT FAIL B" CAS MESSAGE CAME ON. FAILED AT 87 PERCENT. (S) 2 L 7 2 4J RT T00007WI 20080903 NM 2008 9 3 UIEA200800293 1 20080804 A 5330 SKIN BOEING 747 747400 13848AT NM GE CF6 CF680C2* GL BS 520-540 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 429MC 24833 DURING C-CHECK FOUND FORWARD CARGO COMPARTMENT STATION 520-540-STR 34-35L SKIN DAMAGED. SKIN REPAIRED AS PER SRM 53-00- 01 FIGURE 201. (S) 2 L 7 4 4F 4 F RT A20WE E23EA 20080903 NM 2008 9 3 QXEA200800352 1 20080330 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 356PH 502 UPPER COMM ANTENNA HAS CORROSION ON MOUNTING AREA ON ACFT SKIN. REMOVED LIGHT CORROSION IAW CPC MANUAL CHAPTER 4 AND SR M 51-20-11. NO MEASURABLE MATERIAL REMOVED. (S) 2 H 7 2 4T RT A13NM 20080903 2008 9 3 USAABB08134 4 20080815 A 2565 D30655123 SLIDE BOEING 757 7572B7 1384964 NM ZONE 200 MALFUNCTIONED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 934UW 42658 3501 27200 CLT - THE CABIN CREW FAILED TO DISARM THE L2 DOOR, RESULTING IN A PARTIAL EMERGENCY ESCAPE SLIDE DEPLOYMENT. MAINTENANC E REPLACED THE L2 DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. (S) 2 L 7 2 4F RT A2NM 20080904 NM 2008 9 4 EIA2008F00002 1 20080708 A 3350 900835AB POWER SUPPLY BOEING 747 747230B 1384889 NM EMERGENCY LIGHTS INOPERATIVE A EIAA O OTHER O OTHER NR NOT REPORTED 1 NM 09 487EV 23393 UPPER DECK CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND OPS CHECKED. (A) 2 L 7 4 4F RT A20WE 20080904 NM 2008 9 4 DHL2008F00009 1 20080616 A 5330 SKIN BOEING 727 7272M7 138407S NM BS 660 S27R BULGED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 BULGE AT BS 660 AND STRINGER 27R EXTERIOR SKIN. REMOVED FASTENERS AND SHEAR TIE, TEE AT BS 660 AND STRINGER 27R IAW B72 7 SRM 51-30-2. FOUND SHEAR TIE OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. INSTALLED NEW PART WITH P/N 6943683-5 AND PO 8180177 IAW B727 SRM 51-30-2. (A) 2 L 7 3 4F A3WE 20080904 NM 2008 9 4 QXEA200800587 1 20080610 A 3350 SWITCH BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY LIGHT FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 401QX 4031 PDX - WHEN EMERGENCY LIGHT SWITCH IN OFF, CAUTION LIGHT STAYS OFF, AND WHEN POWER REMOVED, THE LIGHTS COME ON. MAINTENA NCE REPLACED THE EMERGENCY LIGHT SWITCH P/N 58401A2B5C5F4L302N2GAP11. OPERATIONAL CHECKS GOOD. (A) 2 H 7 2 4T RT A13NM 20080904 EU 2008 9 4 NSV2008F00011 1 20080726 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT WEAK A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 299CJ 340B299 DURING OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM ON A LINE CHECK 7D AND 8D FLOOR PROXIMITY LIGHTS WERE NOT ILLUMIN ATING. EMERGENCY LIGHT POWER SUPPLY 23LN WAS REPLACED IAW COLGAN AIR WORK CAR 33-60-025 AND SYSTEM CHECKED GOOD. AIRCR AFT WAS RETURNED TO SERVICE. (A) 2 L 7 2 4T RT A52EU 20080904 NM 2008 9 4 NWAA083396743 1 20080722 A 2611 SMOKE DETECTOR BOEING 747 747249F 1384849 NM CARGO BAY MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CR CRUISE 1 GL 01 643NW 22245 DURING CRUISE, THE CARGO FIRE LIGHT AND FIRE BELL ACTIVATED AND THE MAIN DECK DETECTOR LIGHT NR 3 ILLUMINATED. NO INDIC ATION OF SMOKE, FIRE OR FUMES WERE NOTICED DURING INSPECTION OF THE MAIN DECK. FLIGHT CONTINUED ON AND LANDING WAS UNEV ENTFUL. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE . (A) 2 L 7 4 4F RT A20WE 20080904 CE 2008 9 4 YBS2008F00000 1 20080711 A 2823 9102011 SELECTOR VALVE CESSNA 402 402C 207590R CE CONT O520 TSIO520* 17040 SO LT WING FUEL DAMAGED A YBSA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 17 69SC 402C0041 832080R AT CLIMB POWER-RT FUEL FLOW DROPPED TO 90 PPH. AUX PUMP ON LOW FIXED PROBLEM TEMPORARILY. FUEL FLOW DROPPED AGAIN AND LT ENGINE SURGE. RETURNED TO DEPARTURE AIRPORT AND LANDING WITHOUT INCIDENT. MX REMOVED AND REPLACED LT FUEL SELECTOR VALVE. ALSO REPLACED AUX FUEL PUMP AND CROSSFEED VALVE AS A PRECAUTIONARY MEASURE. (A) 1 L 7 2 3O 3 O A7CE E8CE 20080904 WP 2008 9 4 DHLA200800064 1 20080617 A 2697 CONNECTOR DOUG DC8 DC873F 302199F WP FIRE DETECTION MALFUNCTIONED A DHLA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 807DH 45990 FLT 916 - NR 3 ENGINE FIRE INDICATION IN CRUISE SHUT DOWN PER EMER CHECK LIST AND BLEW BOTH BOTTLES. INDICATION PERSIST ED OFF AND ON. LT BOTTLE SHOWED BLOWN AT SAME TIME AS FIRE. AIRCRAFT WAS GROUNDED. INSPECTED CONNECTORS AT FIREWALL AN D INSIDE PYLON CHECKED WIRING ON ENGINE AND TO COCKPIT PER WDM 26-01-01. REPLACED CONNECTOR ON LT AND RT "A" LOOP FAN A ND PYLON "A" LOOP CONNECTOR P/N`S 878239-02, 878238-02. REPLACED LT, RT FIRE LOOPS AND PYLON FIRE LOOPS PER MM 26-10-1. OPS CHECKS NORMAL. SEE NEXT LOGPAGE FOR LT, RT ENGINE FIRE BOTTLES REPAIR. (A) 1 OF 3 2 L 7 4 4F RT 4A25 20080904 CE 2008 9 4 071808N304CSI 1 20080718 A 3260 327 BULB CESSNA 500 550 2076604 CE LT MLG INDICATOR BURNED OUT E Z5FA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 63 304CS 6717 5500847 ON APPROACH INTO PDK THE LT MAIN GEAR INDICATOR DID NOT ILLUMINATE WITH GEAR SELECTED DOWN. CREW FOLLOWED CHECKLIST AND USED THE EMERGENCY PNEUMATIC SYSTEM TO LOWER THE LANDING GEARS. AIRCRAFT LANDED UNEVENTFUL. MAINTENANCE TROUBLESHOT T HE DISCREPANCY TO A FAULTY LEFT GEAR INDICATOR BULB. REPLACED BULB, SERVICED THE EMERGENCY PNEUMATIC SYSTEM AND PERFORM ED SEVERAL GEAR SWINGS. SYSTEM OPERATES OK. (A) 1 L 7 2 4F A22CE 20080904 2008 9 4 ARWA20080705 4 20080724 A 3422 25883025 GYRO DOUG DC8 DC863F 302198F WP MALFUNCTIONED A ARWA O OTHER O OTHER CR CRUISE 1 SO 29 661AV 45969 NR 2 COMPASS PROCESSES 10 DEGREES. REMOVED AND REPLACED NR 2 DIRECTIONAL GYRO IN ACCORDANCE WITH DC8 M/M 34-21-1; OPERA TIONAL CHECK NORMAL IN ACCORDANCE WITH DC8 M/M 34-21-0. (A) 2 L 7 4 4F 4A25 20080904 2008 9 4 DHLA200800054 2 20080609 A 7200 ENGINE BOEING 727 727227 1384078 NM MALFUNCTIONED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 782DH 21998 ALL NR 2 ENGINE INSTRUMENTS FLUCTUATING. EPR BETWEEN 2.0 & 2.1 ON TAKEOFF. N2 FLUCT .2, N1 FLUCT .3, PERFORMED ABNORMA L PROC, SHUTDOWN ENGINE INFLIGHT. POSITIVE OIL PRESSURE ENTIRE TIME. INSPECTED NR 2 ENG INLET & EXHAUST IAW P&W MM 72- 00-00, INSPECTED NR 2 ENG FUEL FILTER FOR CONTAMINATION IAW P&W MM 73-11-01. INSPECTED NR 2 ENG FUEL CONTROL SYSTEM IAW P&W MM 73-00-00. NO DEFECTS NOTED AT THIS TIME. LUBRICATED NR 2 ENG FUEL CONTROL BURNER PRESSURE BELLOWS IAW P&W MM 7 3-21-01. PERFORMED MPA RUN ON NR 2 ENGINE PER JRH CH 7, ALL INDICATIONS NORMAL. NO LEAKS NOTED. AIRCRAFT WAS GROUNDED . (A) 2 L 7 3 4F A3WE 20080904 WP 2008 9 4 IXX2008F00028 1 20080717 A 2612 ELEMENT DOUG DC8 DC873F 302199F WP NR 3 NACELLE MALFUNCTIONED A IXXA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING DE DESCENT 1 SW 11 603AL 46003 FLIGHT NUMBER: 744/ETAR TO OJAM - DESCENDING INTO OJAM NUMBER THREE FIRE WARNING LIGHT AND RED LIGHT IN FIRE HANDLE CAME ON. THE CREW DISCHARGED BOTH BOTTLES AND RED LIGHT IN FIRE HANDLE WAS STILL ON, AND FIRE WARNING WAS INTERMITTENT. TH E CREW LANDED IN OJAM WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED FIRE DETECTOR ELEMENT, LT FAN SENSING ELEMENT, AND BOTH FIRE BOTTLES. OPERATIONAL CHECK GOOD IAW DACO DC8 MAINTENANCE MANUAL 26-10-1, AND 26-20-1. AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 4 4F RT 4A25 20080904 WP 2008 9 4 WRLA2008060 1 20080725 A 5313 18077887784 STRINGER DOUG DC10 DC1030 3023501 WP BS 755 S38L CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 137WA 48282 DURING INSPECTION FOUND LEVEL 2 CORROSION ON STR 38L AT FSTA 766. (A) 2 L 7 3 4F A22WE 20080905 NM 2008 9 5 2008UALA03894 1 20080717 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 540 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 DENT IN UPPER LEG (INBOARD FLANGE) OF FUSELAGE FRAME BS 540, LBL 36. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. TRIMMED OUT DAMAGE TO FRAME INNER FLANGE AND REMOVED EXISTING PRODUCTION SPLICE, FABRICATED A REPAIR ANGLE AND INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080905 EU 2008 9 5 2008UALA03897 1 20080717 A 5310 BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 449UA 851 FOUND BEAM NR 200 CORRODED REF EQ3700. *S/D* ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED BEAM, PREPPED AND RE-INSTALLED . 2 L 7 2 4F 4 F RT A28NM E40NE 20080905 NM 2008 9 5 2008UALA03920 1 20080722 A 2120 SHUTOFF VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 216UA 30549 TRIM AIR PRSOV R RIGHT TRIM AIR PRESSURE RELIEF SHUTOFF VALVE (PRSOV) FAILED. STATUS MSG-2124202 ACTIVE CL MODE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080905 2008 9 5 2008UALA03853 4 20080711 A 2565 5650047 SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR SLIDE FAILED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 408UA 457 LEFT AFT SLIDE INDICATION INOP ON DOOR-OXY SYSTEM ECAM PAGE - DOOR-OXY -SLIDE ARMS BUT INDICATION INOP. *S/D* SLIDE D OOR ARMING PROX SWITCH FAILED. REPLACED PROX SWITCH AT DOOR 2L. ALL INDICATIONS ARE NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080905 EU 2008 9 5 2008UALA03899 1 20080717 A 5310 BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 449UA 851 FOUND BEAM NR 175 CORRODED REF EQ3700 B. *S/D* ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED BEAM, PREPPED AND RE-INSTALL ED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080905 EU 2008 9 5 2008UALA03901 1 20080717 A 5310 BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 449UA 851 FOUND BEAM 230 CORRODED REF EQ3700. *S/D* ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED BEAM, PREPPED AND RE-INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080905 NM 2008 9 5 2008UALA03874 1 20080714 A 5320 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 812UA 850 R2 DOOR SILL CORRODED AT AFT GIRT BAR FITTING. *S/D* ACCOMPLISHED MAJOR REPAIR AT LCQ. REPLACED R2 DOOR SILL PER SRM 51-40-00. 2 L 7 2 4F 4 F RT A28NM E40NE 20080905 2008 9 5 2008UALA03915 4 20080721 A 2565 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR DISLODGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 905UA 25005 DOOR 1L ESCAPE SLIDE FELL OUT OF BUSTLE WHEN DOOR WAS OPENED. 2 L 7 2 4F 4 F RT A16WE E21EU 20080905 EA 2008 9 5 TRAX200800923 1 20080721 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 903EV 7621 LEFT EXTERIOR EMERGENCY LIGHT NR 5 OUT. REMOVED AND REPLACED LAMP AT NR 5 LIGHT ASSY OPS CK GOOD IAW AMM 33-51-21 (SDR CLOSED). (A) 2 L 7 2 4F RT A21EA 20080908 NM 2008 9 8 2008UALA03640 1 20080628 A 3350 GE209 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY LIGHT INOP: DOOR 2R FWD SILL. FOUND BURNED OUT BULB. REPLACED BULB, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080902 NM 2008 9 2 KCSA081334 1 20080722 A 3350 LIGHT BOEING 747 747209B 138489B NM CABIN INOPERATIVE A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 EMERGENCY EXIT SIGN ABOVE UPPER RT ESCAPE DOOR IS INOP. (A) 2 L 7 4 4F RT A20WE 20080902 WP 2008 9 2 NWAA083349928 1 20080711 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8921E 45836 DURING "L" CHECK FOUND CRACK IN FUSELAGE SKIN AT AFT UPPER CORNER OF AFT CARGO DOOR JAMB. REPAIRED PER EA 99-212156. ( S) 2 L 7 2 4F A6WE 20080902 EA 2008 9 2 QXEA200800597 1 20080530 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 693 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 610QX 10033 RFD-C4 CHECK - CORRODED SIDE SEAT TRACK ON RT SIDE AT FS 693. BLENDED CORROSION FROM RT SIDE SEAT TRACK AT FS 693. REM OVED .006 MATERIAL FOR BLEND, WITHIN LIMITS MAX ALLOWABLE BLEND IS .035 INCHES. ALL WORK DONE IAW CRJ BOMB REO 670-53-0 0-013. TREATED IAW CRJ 700 SRM 51-21-11. (S) 2 L 7 2 4F RT A21EA 20080902 SO 2008 9 2 RAIA00808012 1 20080811 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT FAILED A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 836HK 145695 PRE FLT 5470-STL - EMERGENCY LIGHT INOPERATIVE IN THE CABIN. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB AT THE AFF ECTED LIGHT. OPS CHECK GOOD. (S) 2 L 7 2 4T RT T00011AT 20080902 EA 2008 9 2 REX2008F00028 1 20080804 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8884E 7884 ON APPROACH INTO ERI FLAPS WERE SELECTED TO 30 DEGREES AND FAILED AT TWENTY DEGREES, QRH FOLLOWED. EMERGENCY DECLARED W ITH UNEVENTFUL LANDING. RESET FLAP SYSTEM IAW AD 2006-12-21 AND PLACED ON 72 HOUR WATCH. (S) 2 L 7 2 4F RT A21EA 20080902 EA 2008 9 2 VNAA0807009 1 20080717 A 5100 NONE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NONE NONE A VNAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 05 260JS 7957 CREW REPORTED THE PDF SHOWED FLAPS EXTENDED TO 2 DEG UNCOMMANDED AT 30,000FT WITH NO AURAL WARNING AT CRUISE. THE CREW DIVERTED TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO DEFECTS. AIRCRAFT WAS RET URNED TO SERVICE. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080902 EA 2008 9 2 VNAA0807006 1 20080714 A 5100 NONE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NONE NONE A VNAA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 GL 05 215PS 7880 CREW REPORTED A LOUD NOISE ON RT SIDE OF AIRCRAFT AND ELECTED TO RETURN TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE IN SPECTED AND FOUND THE OXYGEN SERVICE DOOR LEFT OPEN. MAINTENANCE SECURED THE DOOR CLOSED. AIRCRAFT WAS RELEASED FOR SE RVICE. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080902 NM 2008 9 2 USAA920081545 1 20080808 A 5315 6545810 FLOORBEAM BOEING 737 7373B7 1384580 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT-Q6 -MAJOR REPAIR- LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT BS 328, BL 0 TO RBL 44. REPAIRED FLOORBEAM AT BS 328, BL 0 TO RBL 44. REPAIRED IAW B737 SRM 53-10-51. (S) 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084465 1 20080812 A 5330 6545766 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 920 AND BS 943, STR 21L AND STR 23L. REPAIRED SKIN P ER SWA EA. 2 L 7 2 4F RT A16WE 20080902 NM 2008 9 2 SWAA084455 1 20080812 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 405WN 27893 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20080902 EU 2008 9 2 USAA920081511 1 20080811 A 2560 BATTERY AIRBUS 320 A320231 3930325 EU FLASHLIGHT DISCHARGED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 628AW 67 FLT 616 SEA-PHX - EMERG EQUIP - OUTBOARD EMERGENCY FLASHLIGHT BLINKING SLOW. MAINTENANCE REMOVED AND REPLACED THE OUTBO ARD EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A28NM 20080903 EU 2008 9 3 2008UALA03620 1 20080628 A 3350 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 433UA 589 THREE SERVICE EMERGENCY LIGHT TEST FAILS. FAULT MSG EXT LOADS AFT L DISPLAYED. *S/D* INTERNAL SHORT IN DOOR SLIDE 2L. REPLACED 2L DOOR SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080903 NM 2008 9 3 UIEA200800283 1 20080815 A 5210 SKIN BOEING 747 7472D7B 1384803 NM PAX DOOR CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 524MC 21784 RT NR 3 MAIN ENTRY DOOR FWD LOWER CORNER SKIN & STRAP FASTENER HOLE CRACKED. REPAIRED IAW BOEING SERVICE REQUEST 1-9170 61347 APPROVED BY FAA FORM 8100-9 DATED 13 AUGUST 2008, DETAILS OF WORK KEPT AT ATLAS ENGINEERING ORDER EO4753B181. (S) 2 L 7 4 4F RT A20WE 20080903 NM 2008 9 3 USAA920081554 1 20080820 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 814AW 1281 FLT 0526 - GDL-PHX- EMERGENCY EQUIPMENT- FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED FORWARD FLIGHT ATTENDANT FLASHLIGHT BATTERY. FLASHLIGHT OPERATES NORMALLY AND STOWS PROPERLY. (S) 2 L 7 2 4F RT A28NM 20080903 EA 2008 9 3 COMA086360 1 20080819 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 819CA 7415 ON APPROACH IN JAX, RECEIVED FLAPS FAIL CAUTION MSG AT 30 DEG. CREW DECLARED AN EMERGENCY, LANDED SAFELY. COMPLIED WIT H TASK CARD SI-2-2710001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION. (S) 2 L 7 2 4F RT A21EA 20080904 NM 2008 9 4 DHL2008F00011 1 20080619 A 5322 SHEAR TIE BOEING 727 7272M7 138407S NM BS 328 S29L CRACKED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 SHEAR TIE CRACKED AT HORIZONTAL WALKWAY BEAM AREA BS 328 STRINGER 26L. REPAIRED SHEAR TIE AT HORIZONTAL WALKWAY BEAM BS 328 STRINGER 26L IAW B727 SRM 53-10-4 FIG 15. (A) 2 L 7 3 4F A3WE 20080908 EU 2008 9 8 COEA0802821 1 20080715 A 3260 WARNING SYSTEM AEROSP ATR72 ATR72202 8680940 EU NLG MALFUNCTIONED A COEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 13 821FX 253 RETURN TO FIELD. FLIGHT 100 GEG TO GEG. THE NOSE WHEEL UNLOCK LIGHT ILLUMINATED IMMEDIATELY UPON ROTATION ALONG WITH T HE NOSE GEAR DOWN AND LOCKED LIGHT REMAINING ILLUMINATED. AFTER THE LANDING GEAR HANDLE WAS SELECTED "UP", BOTH MAINS R ETRACTED NORMALLY. THE NOSE GEAR DID NOT RETRACT AND THE DOUBLE INDICATION CONTINUED SHOWING BOTH NOSE GEAR LOCKED AND UNLOCKED. THE CREW ELECTED TO RETURN TO GEG FOR LANDING. THE LANDING GEAR WAS SELECTED "DOWN" GIVING ALL SIX NORMAL GE AR DOWN INDICATIONS AFTER GEAR EXTENSION. A NORMAL AND SAFE LANDING WAS MADE. THE NOSE LANDING GEAR STRUT WAS SERVICED AND A LANDING GEAR FUNCTION CHECK WAS PERFORMED. THE LANDING GEAR CHECK FOUND NO SYSTEM FAULTS. (A) 2 H 7 2 4T RT A53EU 20080908 CE 2008 9 8 070808N408CSI 1 20080708 A 2611 47359717 SMOKE DETECTOR CESSNA 525 525 2076601 CE CARGO BAY DEFECTIVE E Z5FA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 EA 63 408CS 2654 525B0045 ON APPROACH INTO BOS, CREW OBSERVED BAGGAGE SMOKE ANNUNCIATION. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT, FI RE DEPARTMENT PERSONNEL FOUND NO INDICATION OF SMOKE OR FIRE. MAINTENANCE PERSONNEL TROUBLESHOT SYSTEM AND REPLACED SUS PECTED DEFECTIVE SMOKE DETECTOR AND TESTED SYSTEM WITH "SMOKE IN A CAN" AND DETERMINED SYSTEM OPERATIONAL CHECK SATISFAC TORY. AIRCRAFT RETURNED TO SERVICE. (A) 1 L 7 2 4F RT A1WI 20080908 NM 2008 9 8 CALA0800743 1 20080725 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM BS 360 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14629 27533 FRAME CRACKED STATION 360 S-9L. REPAIED CABIN FRAME STATION 360 S-8L TO S-9L PER ECRA5310-04808 AND CREATED A DIP FOR IN TERCOSTAL CLIP ON N/R LOG 9695077 , DIP 89478 PER ECRA 5310-04808 STEP 11. CREATED A SECOND DIP FOR FRAME INSPECTION ON N/R LOG 9695078 DIP 89477 PER ECRA 5310-04808 REV A STEP 12. 2 L 7 2 4F RT A16WE 20080908 2008 9 8 RYN2008F00006 4 20080723 A 2397 7926140001 COUPLER BOEING 767 767332 1382001 NM HF ANTENNA INOPERATIVE A RYNA O OTHER O OTHER NR NOT REPORTED 1 CE 07 123DL 23437 NR 2 HF (RIGHT HF) NOT WORKING, NR 1 HF (LEFT HF) IS ALREADY ON DEFERRAL. REPLACED NR 1 HF ANTENNA COUPLER IAW AMM 23-1 1-01, OPS CHECKED NORMAL. (A) 2 L 7 2 4F RT A1NM 20080905 2008 9 5 2008UALA03919 4 20080723 A 3422 DISPLAY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT INTERMITTENT A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 658UA 27113 CAPTAINS ADI BLANKING INTERMITTENTLY. RTFL. 2 L 7 2 4F 4 F RT A1NM E24NE 20080908 NM 2008 9 8 2008UALA03138 1 20080531 A 3397 P10225027003 WIRE HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 SEAT 49ABC EMERGENCY LIGHT INOP. *S/D* SUSPECT WIRE HARNESS. REPLACED WIRE HARNESS, OP CHECKED GOOD. AC OK FOR SERVI CE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 EA 2008 9 8 TRAX200800602 1 20080505 A 3230 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 905EV 7632 AFTER T/O IN ATL - GEAR DISAGREE WARNING NOSE GEAR DID NOT RETRACT. RAN QRH, NOSE GEAR (AND MAINS) CAME DOWN AND LOCKED . AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLT 4785 DEL 137 MINS. REMOVED AND REPLACED NLG PRIORITY V ALVE, LK AND OPS CHECKD GOOD. REMOVED AND REPLACED NLG SELECTOR VALVE, LEAK AND OPS CHECKED. REF CRJ MM 32-33-10. (B) 2 L 7 2 4F RT A21EA 20080908 NM 2008 9 8 2008UALA03879 1 20080715 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 506UA 24627 EXTERIOR EEL LIGHTS INOP AT DOORS 1R AND 4L. LAMPS WERE INOPERATIVE. RELAMPED, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080908 NM 2008 9 8 2008UALA03742 1 20080707 A 3350 362624NA LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 FWD EEL INOP SEAT 4E. FOUND LAMP INOP AT SEAT 4E. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03848 1 20080712 A 2597 WIRE HARNESS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L1 DOOR SLIDE SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 805UA 783 DURING 3SV EMERGENCY LIGHTING SYSTEM TEST EPSU EXT LOAD FWD L DISPLAYED. TEST ON FWD L POWER SUPPLY HAS SAME FAULT. FO UND SHORT IN HARNESS IN DOOR 1L SLIDE PACK. REPLACED DOOR 1L SLIDE PACK, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080908 NM 2008 9 8 2008UALA03304 1 20080610 A 3397 81841 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 FOUND SEATS 4J, 5J SIDE WALL AND CEILING LIGHT INOP. FOUND WIRE SHORTED BETWEEN STOW BIN AND STRUCTURE ABOUT TWO FEET A FT OF BALLAST AT SPLICE, MARKED. RESPLICED WIRE W2885-015- 20, REPLACED BALLAST AND REPROGRAMMED OEU. LIGHTS OPERATE NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 CE 2008 9 8 DJFA2008056 1 20080619 A 7160 SKIN BEECH MU300 400A 1155402 CE LT ENG INTAKE CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 439LX RK284 DURING A ROUTINE SERVICE CHECK IT WAS NOTED THAT THE LT ENGINE INLET INNER SKIN WAS CRACKED AT THE 9 O’CLOCK POSITION. THE INLET WAS REMOVED, REPAIRED BY INTEGRITY AERO AND REINSTALLED. (A) 2 H 7 2 4F RT A16SW 20080908 NM 2008 9 8 2008UALA03602 1 20080627 A 3397 P10225027003 WIRE HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 SEAT 5E FWD EMERGENCY LIGHT IS INOP. FOUND FAULTY HARNESS. REPLACED HARNESS, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03475 1 20080619 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY LIGHT INOP: COCKPIT CEILING. FOUND LAMP BURNED OUT. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 TSAA0826023 1 20080725 A 3150 WARNING LIGHT BOEING 737 737* NM OVERHEAT FALSE ACTIVATION A TSAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 13 840AL 23124 FLT 320, HNL-OAK: LT WING-BODY OVERHEAT LIGHT ILLUMINATED IN FLIGHT DURING CRUISE AT ABOUT FL350. LIGHT WENT OUT AFTER . ACCOMPLISHED QRH PROCEDURES AND RETURNED TO HNL. INSPECTED AIR CONDITIONING BAY DUCTS, LEADING FLAP DUCTS AND OVERWI NG DUCTS. NO LEAKS DETECTED. ALSO PERFORMED HIGH POWER RUN; SYSTEM CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A16WE 20080904 2008 9 4 RYN2008F00003 4 20080630 A 2565 104681303 SLIDE BOEING 767 767332 1382001 NM L2 DOOR UNWANTED DEPLOY A RYNA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 CE 07 120DL 23279 FLIGHT ATTENDANT DEPLOYED L2 PASSENGER ENTRY DOOR SLIDE. ACFT MADE A FERRY FLIGHT KWI TO BAH FOR DOOR SLIDE REPLACEMENT . INSTALLED SERVICEABLE L2 DOOR SLIDE IAW AMM 28-66-08. (A) 2 L 7 2 4F RT A1NM 20080904 WP 2008 9 4 IXX2008F00026 1 20080717 A 2612 FIRE WARNING DOUG DC8 DC873F 302199F WP NR 3 NACELLE ACTIVATED A IXXA F A ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SW 11 603AL 46003 FLT NR: 744/ETAR TO OJAM/. DESCENDING INTO OJAM NR 3 ENGINE FIRE WARNING LIGHT CAME ON AND RED LIGHT IN FIRE HANDLE CA ME ON. THE CREW DISCHARGED BOTH BOTTLES AND RED LIGHT IN FIRE HANDLE WAS STILL ON AND FIRE WARNING WAS INTERMITTENT. T HE CREW LANDED IN OJAM WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION IN WORK. (A) 2 L 7 4 4F RT 4A25 20080904 NM 2008 9 4 RYN2008F00004 1 20080627 A 2130 CONTROL PANEL BOEING 757 757236 1384971 NM CABIN PRESSURE MALFUNCTIONED A RYNA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CE 07 526NA 24794 AIR TURNBACK TO RFD FOR PRESSURE CONTROLLER PROBLEM, BOTH AUTO 1 AND AUTO 2 ARE SPIKING 200 TO 300 CABIN DIFFERENTIAL DU RING CLIMB. REPLACED OVERHEAD CONTROL PANEL IAW AMM 21-31-01, OPS CHECKED NORMAL. IN ADDITION COMPLIED WITH FIM 21-30- 00 AND AMM 21-30-00 PRESSURE CONTROL SYSTEM, OPS CHECKED NORMAL. (A) 2 L 7 2 4F RT A2NM 20080904 EU 2008 9 4 TRAX200800925 1 20080723 A 5210 BEARING AEROSP ATR72 ATR72212 8680945 EU DOOR HANDLE FAILED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 ASD STUCK. FLT 4232 DEL 232 MINS. REPLACED BEARING IN HANDLE ASSEMBLE, OPS CHECKED GOOD PER JIC 52-00-10-CHK. (A) 2 H 7 2 4T RT A53EU 20080904 EA 2008 9 4 TRAC200800754 1 20080605 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 290-559 CORRODED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 824AS 7203 SEAT RAIL AT RBL 9 FS 290 TO 559 HAS AREAS OF CORROSION. BLENDED CORROSION TO REMOVAL IAW CRJ200 SRM 51-21-06. DEPTH O F BLEND RANGED FROM 0.001" TO 0.008". 390 AND 409+128 AREAS STILL NEED CORROSION REMOVED. REMOVED CORROSION FROM FS 39 0 TO 409+128. DEPTH RANGED FROM .001 TO.008 WHICH IS WITHIN REPAIRABLE LIMITS IAW SRM 53-21-4. DAMAGE WAS REMOVED IAW 51-21-06 AND UPON INVESTIGATION FOUND ITEM 2 TO BE WITHIN REPAIRABLE LIMITS OF SRM 53-21-49. NEEDS ALODINE. APPLIED AL ODINE IAW CRJ200 SRM 53-21-49. (A) 2 L 7 2 4F RT A21EA 20080905 EA 2008 9 5 TRAX200800880 1 20080705 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR DIRTY A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 SERVICE DOOR WILL NOT OPEN. FLT 4608 DEL 50 MINS. CLEANED AND LUBED SERVICE DOOR HANDLE ASSY, OPS CHECK GOOD PER CRJ 2 00 AMM 52-41-03. (B) 2 L 7 2 4F RT A21EA 20080905 NM 2008 9 5 USAA920081334 1 20080628 A 5313 655169817 STRINGER BOEING 737 73733A 1384673 NM BS 907 S25R CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN-C21 -MAJOR REPAIR- CORROSION ON LOWER SIDE OF STRINGER SPLICE CHANNEL AT BS 907, S25R. REPLACED STRINGER SPLICE CHA NNEL AT BS 907, S25R IAW B737 SRM 51-40-02-0G. (B) 2 L 7 2 4F RT A16WE 20080905 NM 2008 9 5 USAA920081354 1 20080701 A 5320 6545834 INTERCOSTAL BOEING 737 737401 1384701 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT -MAJOR- Q3 CHECK- LEVEL 2 CORROSION ON INTERCOSTAL STIFFENER, BS 312 - BS 328 RBL 11. REPLACED INTERCOSTAL STIFFENE R, BS 312 - BS 328, RBL 11 IAW B737 SRM 51-10-02. (B) 2 L 7 2 4F RT A16WE 20080905 NM 2008 9 5 USAA920081345 1 20080706 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT -MAJOR REPAIR- Q3 CHECK - LEVEL 2 CORROSION ON CABIN FLOORBEAM T-CAP, BS 328, LBL 24-LBL 48. REPLACED CABIN FLOORBE AM T-CAP, BS 328, LBL 24-LBL 48 IAW B737 SRM 53-10-51 FIG 201. (B) 2 L 7 2 4F RT A16WE 20080905 NM 2008 9 5 USAA920081341 1 20080710 A 5311 FRAME BOEING 737 737401 1384701 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT -MAJOR REPAIR- Q3 CHECK - CRACKED FRAME, BS 747, S8R -S9R. REPAIRED FRAME, BS 747, S8R - S9R IAW US AIRWAYS TYPICAL REPAIR 53-10-20E. (B) 2 L 7 2 4F RT A16WE 20080905 NM 2008 9 5 2008UALA03886 1 20080715 A 2810 LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUEL SYSTEM CRACKED A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 597UA 28750 SVA - OPEN LINE FROM FUEL CONTROL TO BIFURCATION PLATE IS LEAKING FUEL FROM B-NUT AT FUEL CONTROL. SUSPECT LINE CRACKED AT FLAIR. FATIGUE CRACK IN FUEL LINE. REPLACED FUEL LINE, LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080905 NM 2008 9 5 2008UALA03962 1 20080724 A 2421 IDG BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RIGHT MALFUNCTIONED A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 665UA 29237 EICAS MSG ON RIGHT ENGINE GEN DRIVE DISPLAYED. LIGHT ILLUM GEN DRIVE DISCONNECTED. REPLACED RIGHT IDG. 2 L 7 2 4F 4 F RT A1NM E24NE 20080905 NM 2008 9 5 CALA0800740 1 20080718 A 3040 HEATER BOEING 737 7373T0 1384582 NM COCKPIT WINDOW SHORTED A CALA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SW 27 47332 961 23570 DURING TAXI AND SHORTLY AFTER TURNING ON WINDOW HEAT, A SPARK WAS NOTED COMING FROM THE 1R WINDOW WHICH THEN CRACKED. R EMOVED AND REPLACED R-1 WINDOW PER MM 56-11-11. 2 L 7 2 4F RT A16WE 20080905 NM 2008 9 5 DHLA200800055 1 20080609 A 3246 31395 WHEEL BOEING 727 727225 1384077 NM MLG NOISY A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 748DH 22440 RTO DUE TO HEAVY VIBRATION THAT SEEMED TO EMANATE FROM NOSE WHEEL NOTE RTO AT 80 KIAS FULL REVERSE AND MODERATE BREAKING USED. REMOVED AND REPLACED BOTH NOSE WHEELS PER MM 32-45-11. FIT 520 AIRCRAFT WAS GROUNDED. (A) 2 L 7 3 4F A3WE 20080908 NM 2008 9 8 2008UALA03906 1 20080720 A 3150 WARNING LIGHT BOEING 737 737522 138449F NM CABIN PRESSURE ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 925UA 26646 RETURNED TO THE FIELD DUE TO A PRESSURIZATION INDICATION. 2 L 7 2 4F RT A16WE 20080908 EU 2008 9 8 2008UALA03792 1 20080708 A 2611 PPA120300 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LAVATORY FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 404UA 450 LAVATORY DETECTOR FAULT DISPLAYED ON UPPER ECAM SCREEN. FOUND SMOKE DETECTOR MALFUNCTIONED. REPLACED SMOKE DETECTOR, S YS OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080908 NM 2008 9 8 2008UALA03611 1 20080626 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LAVATORY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EEL INOP, LAV 117 SIDE WALL. FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE . 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 EU 2008 9 8 2008UALA03907 1 20080720 A 5540 BEARING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RUDDER WORN A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 446UA 834 DIVERTED TO JAX DUE TO AN EXTREME VIBRATION. REPLACED ALL RUDDER HINGE BEARINGS AND ALL ELEV HINGE BEARINGS. TEST FLIG HT NORMAL, NO VIBRATION NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080908 EA 2008 9 8 TRAX200800859 1 20080701 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 861AS 7445 AFT PRESSURE BULKHEAD FS 621 IS CRACKED AT THE LINTEL FITTING AREA. OPEN (B) 2 L 7 2 4F RT A21EA 20080908 NM 2008 9 8 DHL2008F00001 1 20080627 A 5752 652172630 TAB BOEING 727 7272B7 138407L NM AILERON DELAMINATED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 762AT 22162 A 3 X 1 INCH DELAMINATION ON RT WING O/B AILERON BALANCE TAB AT TRAILING EDGE. AILERON BALANCE TAB WAS REMOVED AND REPL ACED IAW BOEING 727 MAINTENANCE MANUAL 27-10-41. OPERATION CHECK NORMAL. (A) 2 L 7 3 4F A3WE 20080908 NE 2008 9 8 R612008F00005 2 20080614 A 7321 SOFTWARE EMB ERJ170 ERJ170100SU 3260403 NM GE CF34 CF348E5 30061 NE FADEC FAILED A R61A E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 GL 11 819MD 9706 LMDL0594 17000040 CREW REPORTED DURING CRUISE FLIGHT NUMBER 2 ENGINE HAD A HIGH VIBRATION MESSAGE. CREW FOLLOWED QRH PROCEDURE SHUTDOWN N R 2 ENGINE AND THEN DIVERTED TO PITTSBURGH LANDED WITHOUT INCIDENT, TAXIED TO GATE MAINTENANCE WAS DISPATCHED TO A/C. M AINTENANCE TROUBLESHOT REMOVED AND REPLACED ENGINE FADEC, SYSTEM OPERATIONAL CHECK GOOD, RETURN AIRCRAFT TO SERVICE. (A ) 2 L 7 2 4F 4 F RT A56NM E00063EN 20080908 EU 2008 9 8 2008UALA03785 1 20080708 A 3350 BULB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 429UA 539 DURING OP-TEST OF FLOOR EMERGENCY ESCAPE PATH SYSTEM, ONE INCANDESCENT LIGHT INOP AT SEAT 9C. FOUND BULB OUT. REPLACED LAMP AT ROW 9C. 2 L 7 2 4F 4 F RT A28NM E40NE 20080908 NM 2008 9 8 2008UALA03881 1 20080714 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROW 1 UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 577UA 26693 CABIN EMER LT STRIP COMING UP NEAR ROW 13. SECURED STRIP, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080908 NM 2008 9 8 2008UALA03674 1 20080702 A 3350 582240 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 174UA 24381 RIGHT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP, TWO MOST AFT LIGHT ASSY'S. FOUND FAULTY POWER SUPPLY. REPLACED PO WER SUPPLY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03740 1 20080705 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 5E BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 THE 5E EEL STRIP BROKEN. FOUND LIGHT ASSEMBLY BROKEN. REPLACE LIGHT ASSEMBLY. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03606 1 20080627 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 SEAT 43ABC EMERGENCY LIGHT IS INOP. FOUND BURNED OUT LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03608 1 20080626 A 3350 BPS73 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EEL'S VERY DIM, SEATS 35HJK THROUGH 44HJK. FOUND FAULTY BATTERY PACK. REPLACED BATTERY PACK, OP CHECKED GOOD. AC OK F OR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 DHL2008F00006 1 20080627 A 5753 6521788108A FAIRING BOEING 727 7272J0 138407E NM FLAP TRACK CRACKED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 749DH 22013 POSSIBLE CRACK AT LOWER AFT SIDE OF NR 8 FLAP TRACK FAIRING. REMOVED AND REPLACED FLAP TRACK FAIRING IAW BOEING 727 MM 27-51-31. OPERATIONAL CHECK OK. (A) 2 L 7 3 4F RT A3WE 20080908 NM 2008 9 8 2008UALA03790 1 20080708 A 3397 362624 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY LIGHTS LOOSE ON SUITES 2A, 5A, 4J, 5J. FOUND LOOSE CONNECTIONS. SECURED CONNECTIONS, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03788 1 20080708 A 3350 GE209 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY LIGHT INOP: CEILING ROW 12. FOUND LAMP INOP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03493 1 20080619 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT ROW 48 LT INOP. FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 EA 2008 9 8 N6WA0080703 1 20080724 A 3350 9EL40004211 LENS CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT CRACKED A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 153GJ 7437 10219 INSP - MX EXTERIOR OVERWING EMERGENCY EXIT LIGHT LENS CRACKED LT AND RT. ITEMS DEFERRED IAW CDL 33-50. 2 L 7 2 4F RT A21EA 20080908 CE 2008 9 8 072208N523CS2 1 20080722 A 2997 WIRE CESSNA 560 560XL 2076702 CE HYD CONNECTOR DAMAGED E Z5FA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 63 523CS 3749 5605507 AFTER T/O FROM KSTP MASTER CAUTION AND STAB TRIM WARNING LIGHTS ILLUMINATED. WHILE FOLLOWING CHECKLIST HYDRAULIC CONTRO L CIRCUIT BREAKER EXTENDED. AIRCRAFT DIVERTED TO KMSP AND AN EMERGENCY WAS DECLARED. LANDING GEAR WAS EXTENDED USING T HE EMER SYSTEM AS PER CHECK LIST. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED WIRE ON CONNECTOR FOR THE HYD RAULIC LOADING VALVE AND REPLACED THE HYDRAULIC CONTROL PCB. EMER GEAR AND BRAKE SYSTEM WAS RESET AND SERVICED. SEVERA L GEAR SWINGS WERE PERFORMED. HYD SYSTEM OPS CHKS GOOD. (A) 2 L 7 2 4F RT A22CE 20080908 2008 9 8 COEA0801752 4 20080719 A 3421 0600001700 GYRO CESSNA 208 208B 2073701 CE LT INSTR PANEL FAILED A COEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 13 752FX 208B0517 RETURN TO BLOCKS. THE PILOT’S SIDE ATTITUDE INDICATOR WILL NOT ERECT. DISCOVERED DURING TAXI TO THE RUNWAY. REMOVED A ND REPLACED, ARTIFICIAL HORIZON. (A) 1 H 7 1 3T A37CE 20080908 NM 2008 9 8 QXEA200800693 1 20080625 A 5210 SEAL BOMBDR DHC8 DHC8402 1390042 NM AFT PAX DOOR DIRTY A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 428QX 4160 SEA - AFT PASSENGER DOOR WILL NOT CLOSE. FOUND SEAL DIRTY. CLEANED. DOOR CHECKS GOOD. RETURNED TO SERVICE. NO PARTS REPLACED. (A) 2 H 7 2 4T RT A13NM 20080908 EA 2008 9 8 QXEA200800649 1 20080613 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA PAX MALFUNCTIONED A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 601QX 10009 SEA - FLIGHT 2534 - MAIN CABIN DOOR DIFFICULT TO RAISE AND LATCH CLOSED. MAINTENANCE PERFORMED NUMEROUS DOOR OPERATIONS WITH NO DEFECTS. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED. (A) 2 L 7 2 4F RT A21EA 20080908 NM 2008 9 8 QXEA200800651 1 20080616 A 3350 LAMP DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHTS INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 345PH 476 PDX - AUX BATTERY AND EMERGENCY DISARM LIGHTS DIM. REPLACED LAMPS, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVI CE. (A) 2 H 7 2 4T RT A13NM 20080908 EA 2008 9 8 N6WA0080708 1 20080730 A 3350 8EL4004211 LENS CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BROKEN A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 157GJ 8481 10230 FLMX-ORD - PAX DOOR EMERGENCY LIGHT LENS BROKEN. PLACED ON DMI CONTROL NUMBER 8477 PER CDL 33-60. (A) 2 L 7 2 4F RT A21EA 20080908 NM 2008 9 8 2008UALA03980 1 20080726 A 3397 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 331UA 24192 EMERGENCY EXIT LIGHTING INOP ROW 15 AFT. FOUND FAULTY LAMP STRIP AND DAMAGED FEEDER CABLE. REPLACED LAMP STRIP AND FEE DER CABLE OP CHECK GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080908 2008 9 8 2008UALA03981 4 20080725 A 2300 106209025 SELECTOR PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 309UA 23670 F/O OXYGEN MASK MIC IS INOP. AFTER TROUBLE SHOOTING FOUND AUDIO SELECT PANEL FAULTY. REPLACED FIRST OBSERVER'S AUDIO S ELECTOR PANEL OP CHECK GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080908 NM 2008 9 8 CALA0800750 1 20080725 A 5754 65C26602312SP SKIN BOEING 737 737524 1384721 NM NR 5 SLAT DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 NR 5 SLAT TRAILING EDGE WARPED AT OUTBOARD END AT PREVIOUS REPAIR. REPAIRED AT OUTBOARD END AT PREVIOUS REPAIR AND UPP ER SURFACE REFINISHED PER SRM 51-70-10 AND CAL 5100500128 REV Q. 2 L 7 2 4F RT A16WE 20080908 NM 2008 9 8 CALA0800745 1 20080725 A 5210 6552875 FRAME BOEING 737 737524 1384721 NM L2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 CORROSION ON L2 DOOR SUPPORT STRUCTURE JUST AFT OF LOWER AFT CORNER. FOUND CORROSION TO BE BEYOND LIMITS PER SRM 51-10- 02. FABRICATED AND REPLACED FRAME SECTION AND REPAIRED SPLICE PER SRM 51-70-11 AT L2 DOOR SUPPORT STRUCTURE JUST AFT OF LOWER AFT CORNER. 2 L 7 2 4F RT A16WE 20080909 WP 2008 9 9 08FDEA03715 1 20080903 A 5414 AUB70231 PANEL DOUG MD10 MD1010F 3022112 WP NR 2 NACELLE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 NR 2 PYLON APRON HAS EDGE DAMAGE AT THE FWD END WHERE THE LT FAN COWL MATES. REPAIRED NR 2 FAN COWL LT APRON IAW E.A. 8 -5480-123629. 2 L 7 3 4F RT A22WE 20080909 NM 2008 9 9 2008UALA03924 1 20080723 A 2697 WIRE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CONNECTOR LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 815UA 867 SQUIB ON AGENT 1 ENG 2 DOESN'T TEST. BULB OK BUT DOESN'T COME ON DURING FIRE TEST. *S/D* OPEN WIRE AT PIN NR 2 OF 5WE 2 CONNECTOR. REPLACED WIRE 2621-0003-20 BETWEEN CONN'S 5WE2 & 474VC PER WDM26-21-03. PERFORMED FIRE OPS TEST. CHECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA03961 1 20080723 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 505UA 24626 DOOR 1L EXTERIOR EMERGENCY LIGHT INOP. *S/D* LAMP INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 20080909 EU 2008 9 9 2008UALA04010 1 20080726 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 453UA 1001 EPSU BATTERY FWD L DISPLAYED AFTER EMERGENCY LIGHT TEST PER 3 SVC. *S/D* CONNECTOR LOOSE. RE-SEATED MATING CONNECTOR FOR LEFT FWD BATT PACK, NORMAL OPERATION RESTORED, OPS CHECKS OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080908 NM 2008 9 8 2008UALA03887 1 20080714 A 2120 UNKNOWN BOEING 737 737522 138449F NM COCKPIT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 936UA 26667 STRONG PUNGENT ODOR IN FLIGHT DECK. 2 L 7 2 4F RT A16WE 20080908 NM 2008 9 8 2008UALA03405 1 20080615 A 3350 GE209 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT INOP: DOOR 2L FWD SILL. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 AIEA200800258 1 20080707 A 5311 FRAME BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE BS 280 S26L CRACKED A AIEA O OTHER O OTHER NR NOT REPORTED 1 GL 11 540MC 22508 DURING C-CHECK FOUND FRAME CRACKED AT STATION 280 STRINGER 26L. FRAME REPAIRED AS PER SRM 53-10-04 FIGURE 10. (A) 2 L 7 4 4F 4 F RT A20WE E23EA 20080908 EU 2008 9 8 2008UALA03791 1 20080708 A 2497 FEEDER CABLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE IDG BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 493UA 1821 FOUND BURNED IDG FEEDER CABLE AT JUNCTION BOX IN PYLON. NR 1 ENG. REPLACED FEEDER CABLE HARNESS, ALL SYS CHECKS PERFOR MED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080908 EU 2008 9 8 COEA0802742 1 20080716 A 7997 CONNECTOR FOKKER F27 F27MK600 4990706 EU LT ENG OIL IND DIRTY A COEA E D ENGINE SHUTDOWN RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 13 742FE 10349 RETURN TO BLOCKS. FLT 8777. ON TAXI TO THE RUNWAY THE LT ENGINE OIL PRESSURE GAGE DROPPED TO AN INDICATION OF "0". TH E LT ENGINE WAS SHUT DOWN AND THE A/C TAXIED SAFELY BACK TO THE RAMP. DISCONNECTED CONNECTORS AT THE OIL PRESSURE GAGE AND OIL PRESSURE TRANSMITTER FOR THE LT ENGINE. CLEANED CONNECTIONS AND RECONNECTED REMOVED CONNECTORS. SYSTEM CHECK A ND ENGINE RUN FOUND SYSTEM OPERATION NORMAL. (A) 2 H 7 2 4T A817 20080908 CE 2008 9 8 071708N523CSI 1 20080717 A 3260 66426321 UPLOCK CESSNA 560 560XL 2076702 CE NLG OUT OF ADJUST E Z5FA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 63 523CS 3740 5605507 AFTER TAKEOFF FROM KMVY THE LANDING GEAR UNLOCK LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION. THE HYDRAULIC PRESSURE LIGHT REMAINED ON, STAB MISCOMPARE LIGHT ILLUMINATED FOLLOWED BY MASTER CAUTION. FOLLOWED CHECKLIST DIVERTED TO KBED AN D DECLARED AN EMERGENCY. RESET HYDRAULIC CONTROL CIRCUIT BREAKER AS PER CHECK LIST. LOWERED GEAR, HYD PRESS AND STAB M ISCOMPARE INDICATIONS WENT BACK TO NORMAL. LANDING WAS UNEVENTFUL. MAINTENANCE FOUND THE NOSE LANDING GEAR UPLOCK ASSE MBLY OUT OF ADJUSTMENT. ADJUSTED NLG UPLOCK ASSEMBLY. PERFORMED SEVERAL GEAR SWINGS. SYSTEM OPERATES NORMAL. (A) 2 L 7 2 4F RT A22CE 20080908 NM 2008 9 8 2008UALA03972 1 20080724 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE AFT GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 AFT GALLEY X AISLE INOP. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080908 SO 2008 9 8 SIMA200820302 1 20080719 A 2612 36011335002030C FIRE LOOP EMB 135 EMB135KL 3260302 SO LT NACELLE MALFUNCTIONED A SIMA O OTHER N FALSE WARNING LD LANDING 1 SW 21 813AE 145539 ON FLIGHT 4278 UPON LANDING CREW REPORTED, AN ENGINE 1 FIRE INDICATION. NO EMERGENCY DECLARED AND FIRE BOTTLE WAS NOT D ISCHARGED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER 1 ENGINE FIRE DETECTION LOOP IAW EMB 140 AMM 26- 11-01. FIRE DETECTION OPERATIONAL CHECK PERFORMED AND SYSTEM FUNCTIONS NORMALLY. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080908 NM 2008 9 8 2008UALA03643 1 20080630 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 4A FWD LIGHT ASSY. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 EA 2008 9 8 TRAX200800858 1 20080701 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 917EV 7769 FORWARD EMERGENCY EXIT LIGHT (CURVED) MOUNTED ON THE ADJACENT TO THE HATCHES IS INOP. REMOVED AND REPLACED NR 2 BATTERY CHARGER FOR EMERGENCY LT`S SYSTEM. CHECKS GOOD IAW RJ-200 33-51-00. (B) 2 L 7 2 4F RT A21EA 20080908 NM 2008 9 8 2008UALA03140 1 20080531 A 3397 362624 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 SEAT 50HJK EMERGENCY LIGHT INOP. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECKED GOOD. AC OK FOR SERVIC E. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03162 1 20080603 A 3350 BPS73 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 RIGHT SIDE C-ZONE SEAT EMERGENCY LIGHTS IS INOP. SUSPECT FAULTY BATTERY. REPLACED BATTERY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 2008 9 8 2008UALA03714 4 20080703 A 2565 7A146913 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DOOR 5L UNSECURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 128UA 30023 DOOR 5L SLIDE UNRAVELED IN BUSTLE. SUSPECT IMPROPERLY INSTALLED. REPLACED SLIDE ASSEMBLY PER MM 25-69-01 PG401. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 EU 2008 9 8 DHLA200800077 2 20080627 A 7200 ENGINE DOUG DC8 DC873 302199C WP CFMINT CFM56 CFM562AFR 13802 EU NR 3 FAILED A DHLA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SO 01 803DH 1964 46123 693474 AT TOP OF CLIMB NR 3 ENGINE FAILED FOLLOWED APPLICABLE PROCEDURES RELIGHT ATTEMPT UNSUCCESSFUL WIND MILLING OIL PRESSURE 2 PSI WIND MILLING TIME 2.55. PERFORMED T/S IAW DC8-70 M/M 71-00, ADJUSTED MEL SPECIFIC GRAVITY IAW MM 73-20-1. ADJUS TED PMC DROP IAW MM 73-20-3. PERFORMED MPA PER JRH CH13 CKS GOOD. FLIGHT 951 AIRCRAFT WAS GROUNDED. (A) 2 L 7 4 4F 4 F RT 4A25 E21EU 20080908 NM 2008 9 8 2008UALA03746 1 20080706 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EEL LIGHT INOP AT SEAT 32 ABC. FOUND LAMP INOP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03747 1 20080705 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EEL STRIP AT 2A INOP. FOUND LAMP INOP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03749 1 20080707 A 3350 582240 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EEL'S INOP AT DOOR R3 & L3 AISLEWAYS. FOUND FAULTY BATTERY PACK. REPLACED BATTERY PACK, OP CHECK OK REF MM 33-51-04. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 CE 2008 9 8 DJFA2008051 1 20080604 A 7160 45A35022601 INTAKE BEECH MU300 400A 1155402 CE LT ENGINE CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 482LX RK413 DURING ROUTINE MAINTENANCE THE LT INLET SKIN AT THE INLET TEMPERATURE PROBE WAS FOUND CRACKED. THE LT INLET WAS REPLACE D. (A) 2 H 7 2 4F RT A16SW 20080908 NM 2008 9 8 2008UALA03461 1 20080619 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 8 INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 121UA 29167 WALL EEL INOP: AFT OF ROW 8 LT AT COAT CLOSET. FOUND LIGHT ASSEMBLY TO BE FAULTY. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03865 1 20080711 A 3150 WARNING MESSAGE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE MAIN OIL FILTER ILLUMINATED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 648UA 25285 724371 CREW REPORTS: RT ENG "OIL FILTER MSG AT ENGINE START, MSG CLEARED AFTER ENG START TOOK 15 SEC , OAT WAS 15C & OIL TEMP WAS BELOW 35C". DEFERRED. MAIN OIL FILTER TO BE REPLACED WITHIN 50 FLIGHT HOURS. MAIN OIL FILTER SUBSEQUENTLY REPLACE D AT ORD. RAN ENGINE - NO LEAKS, NO FILTER MESSAGE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080908 WP 2008 9 8 IXX2008F00019 1 20080718 A 2612 FIRE DETECTOR DOUG DC8 DC871F 302199D WP NR 3 NACELLE MALFUNCTIONED A IXXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 11 820BX 46065 FLT NR: ATN 820/KDFW TO KIAH. DURING CRUISE FROM KDFW TO KIAH THE NR 3 FIRE WARNING CAME ON. THE CREW ACCOMPLISHED THE APPROPRIATE CHECK LIST AND DISCHARGED BOTH FIRE BOTTLES, AND CONTINUED TO KIAH AND LANDED WITHOUT INCIDENT. MAINTENANC E REPLACED LT FAN, RT CORE, PYLON FIRE SENSING ELEMENT, LT CORE CONNECTOR, AND BOTH FIRE BOTTLES. OPERATIONAL CHECK GOO D IAW MM 26-11-16, 26-11-15 AND 26-21-09. AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 4 4F RT 4A25 20080908 NM 2008 9 8 QXEA20800690 1 20080624 A 3230 483025 SEQUENCE VALVE BOMBDR DHC8 DHC8402 1390042 NM NLG MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 414QX 4061 PDX - FLIGHT 2308 (ACV-RDD). GEAR WOULD NOT RETRACT NORMALLY. NOSE GEAR UNSAFE LIGHT. DIVERT TO PDX AT 185 KNOTS. PE RFORMED ALTERNATE EXTENSION. UNEVENTFUL LANDING. REPLACED NLG SEQ VALVE AND DOOR ACTUATOR. FLUSHED HYD LINES. PERFOR MED OVER 35 OPERATIONAL SWINGS OF GEAR, AND 5 ALTERNATE EXTENSIONS. CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 H 7 2 4T RT A13NM 20080908 NM 2008 9 8 QXEA200800650 1 20080612 A 5210 HANDLE BOMBDR DHC8 DHC8402 1390042 NM AFT PAX DOOR LACK OF LUBE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 409QX 4051 PDX - FLIGHT 2451 - AFT PASSENGER DOOR HARD TO LATCH. MAINTENANCE LUBED THE DOOR HANDLE. OPERATIONAL CHECKS GOOD. RET URNED TO SERVICE. NO PARTS REPLACED. (A) 2 H 7 2 4T RT A13NM 20080908 NM 2008 9 8 QXEA200800665 1 20080619 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM COCKPIT ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 374PH 480 PDX - FLIGHT 2040 - AFTER FLIGHT NOTICED FISH ODOR ON FLIGHT DECK. LIKE AN INVERTER FAILURE. MAINTENANCE PERFORMED A 4 00HZ AC SYSTEM TEST. NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. (A) 2 H 7 2 4T RT A13NM 20080908 NM 2008 9 8 QXEA200800664 1 20080619 A 2910 LINE DHAV DHC8 DHC8202 2809007 NM HYD SYSTEM LEAKING A QXEA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 NM 09 348PH 484 EAT - ON APPROACH F/A AND PASSENGERS NOTICES A HAZE IN THE CABIN. ACCOMPLISHED UNEVENTFUL LANDING. MAINTENANCE FOUND N R 2 DOWN LINE FOR THE NOSE GEAR HAS A HOLE. WEDGED IN NEW SECTION IAW 20-50-55-360-801. CHECKS GOOD. AIRCRAFT RETURNE D TO SERVICE. (A) 2 H 7 2 4T RT A13NM 20080908 NM 2008 9 8 WRLA2008061 1 20080731 A 5751 ARC7212501 WEDGE DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE OUTBD AILERON DEBONDED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 275WA 48631 DURING 4C CHECK INSPECTION DISBOND WAS FOUND ON THE LT WING OUTBOARD AILERON BETWEEN T/E CORE AND THE UPPER SKIN ASSEMBL Y. BOEING HAS AUTHORIZED A TEMPORARY REPAIR WITH A-CHECK REINSPECTIONS AND C-CHECK PERMANENT REPAIR. (A) 2 L 7 3 4F 4 F RT A22WE E24NE 20080908 EA 2008 9 8 N6WA0080704 1 20080730 A 3350 9EL4004211 LENS CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT CRACKED A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 165GJ 6481 10257 FLMX-ORD. EXTERIOR EMERGENCY LENS CRACKED. INSTALLED NEW LENS IAW AMM 33-51-16. 2 L 7 2 4F RT A21EA 20080908 NE 2008 9 8 2008UALA03951 2 20080724 A 7200 PW4056 ENGINE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE NR 1 BIRD INGESTION A UALA A UNSCHED LANDING C E J F.O.D. VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 WP 29 665UA 34057 22573 29237 727788 NR 1 ENGINE VIBRATION/POSSIBLE BIRD STRIKE. RTFL. ENGINE NOT SHUT DOWN. AFTER RTF, BIRD STRIKE CONFIRMED. MM FOUND 2 DAMAGED FAN BLADES. REPLACED DAMAGED BLADES AND OPPOSITE BLADES. HP COMPRESSOR BORESCOPE OK. AIRCRAFT RETURNED TO S ERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080908 NM 2008 9 8 CALA0800751 1 20080729 A 5753 GIMBAL JOINT BOEING 737 737524 1384721 NM TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 RIGHT INBOARD MIDFLAP PART NUMBER 65C26310-26, S/N BN1829 BOTH INBOARD AND OUTBOARD CARRIAGES, TORQUE TUBES AND ONE GIMB AL CORRODED BEYOND LIMITS. PARTS REPLACED: CARRIAGE HALF'S 65-52246-16, S/N 12142, 65-52246-18, S/N 11485, 65C26343-3, S/N 12635, GIMBAL (SPINDLE) 65-51622-6 S/N 7068, TUBES 65-52211-1/ -2, 69-37206-14. 2 L 7 2 4F RT A16WE 20080908 NE 2008 9 8 2008UALA03956 2 20080723 A 7261 ENGINE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE RIGHT MAKING METAL A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 672UA 34650 1507 30027 727886 ACFT RETURN TO BLOCK WITH STATUS MSG: RT ENG OIL FILTER. OIL STATUS MESSAGE WENT OUT AFTER 1-MINUTE WITH NO CREW ACTIO N. MM REPLACED THE MAIN OIL FILTER. NO METAL CHIPS PRESENT. AIRCRAFT RETURNED TO SERVICE; NO FURTHER PROBLEMS. 2 L 7 2 4F 4 F RT A1NM E24NE 20080908 NE 2008 9 8 2008UALA03958 2 20080723 A 7261 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE RT ENGINE ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 677UA 54552 1708 30029 727337 RT OIL FILTER STATUS MESSAGE. OIL FILTER STATUS MESSAGE WENT OUT AFTER 1-MINUTE WITH NO CREW ACTION. MM REPLACED THE M AIN OIL FILTER, NO METAL CHIPS FOUND. AIRCRAFT RETURNED TO SERVICE AFTER 35 MINUTE FLIGHT DELAY. NO FURTHER PROBLEMS. 2 L 7 2 4F 4 F RT A1NM E24NE 20080909 NM 2008 9 9 2008UALA03979 1 20080725 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1600 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 AFT PIT STA 1600 FRAME INNER FLANGE DENTED BETWEEN S-25L AND 26L. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. CUT OUT DAM AGE AND INSTALLED FRAME DOUBLER REPAIR PER SRM 53-00-07, REPAIR 5. 2 L 7 2 4F 4 F RT A2NM E17NE 20080909 NM 2008 9 9 2008UALA03778 1 20080708 A 8012 8088846 START VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 ENGINE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 213UA 30219 ENG START VALVE L LEFT STARTER AIR VALVE POSITION DISAGREES WITH COMMANDED POSITION OR STARTER AIR VALVE POSITION INDIC ATION IS LOST. STATUS MSG01- NOT ACTIVE ENGINE START MODE DEPENDENT; STARTER AIR VALVE (SAV) (L ENG) IS NOT IN COMMANDE D POSITION. DB- ELECTRONIC ENGINE CONTROL (L ENG, CH B) MSG02- NOT ACTIVE ENGINE START MODE DEPENDENT; STARTER AIR VALV E (SAV) (L ENG) IS NOT IN COMMANDED POSITION. PROG TEXT: - ITEM ROLLED FORWARD. MSG-8061561 INACTV ES MODE MSG-806156 1 INACTV ES MODE. *S/D* SUSPECT FAULTY STARTER AIR VALVE. REPLACED START VALVE PER MM 80-21-44, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 2008 9 9 2008UALA04026 4 20080726 A 2397 COUPLING BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE NR 1 HF RADIO DAMAGED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 670UA 29240 NR 1 HF RADIO NO TRANSMIT. FOUND FAULTY COUPLER. REPLACED NR 1 HF COUPLER. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080909 EU 2008 9 9 2008UALA04029 1 20080728 A 5350 FAIRING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE WING TO BODY LOOSE A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 487UA 1669 LOOSE PANEL OR FAIRING ON LEFT MID WING AREA FLOATING APPROX 3 INCHES, REPORTED BY FLT ATTENDANTS AND PASSENGERS AND CON FIRMED BY FIRST OFFICER. NO ABNORMAL FLIGHT CHARACTERISTICS. RTFL. *S/D* REPLACED LEFT OUTBOARD RUB STRIP. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 CALA0800774 1 20080806 A 5311 FRAME BOEING 737 737524 1384721 NM BS 747 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16632 27900 FRAME CRACKED STATION 747 AT S-9L. REPAIRED FRAME PER EA 5310-04498, OP 2. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 CALA0800756 1 20080802 A 3350 BPS73 BATTERY PACK BOEING 737 737524 1384721 NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14668 28928 SEAT EMERGENCY LIGHTS AT ROWS 14 THRU 19 WILL NOT TEST. REPLACED BATTERY PACK AT ROW 19, OPERATION CHECKS NORMAL. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 2008UALA03780 1 20080708 A 3510 38001614 OXYGEN SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 CREW REPORT: CREW O2 LOW SHOWS 950LBS. *S/D* FOUND FLEX LINE CAPTAINS O2 MASK BOX LEAKING. REPLACED FLEX LINE, LEAK CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 2008UALA03984 1 20080726 A 4990 ACA645F25Y4 FILTER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU PLUGGED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 210UA 30216 APU CONTROL APUC DETECTED FAILURE OF REDUNDANT CONTROL FUNCTION OR LOSS OF ONE ARINC 629 CHANNEL. *S/D* FOUND PLUGGED OIL FILTER. APU OIL FILTER PER MM 49-27-03, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 NM 2008 9 9 2008UALA03985 1 20080725 A 3150 WARNING MESSAGE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 210UA 30216 STATUS MESSAGES PFCS INTERFACE & FLAP-SLAT CONTROL 1 WILL NOT ERASE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080903 EA 2008 9 3 TRAX200801011 1 20080816 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 836AS 7263 SERVICE DOOR WILL NOT CLOSE. OPS CHECKED SERVICE DOOR PER 52-40-01. CHECKS GOOD. (S) 2 L 7 2 4F RT A21EA 20080903 WP 2008 9 3 MEW2008F00000 1 20080806 A 3350 B523 BATTERY PACK DOUG DC9 DC981 3022081 WP PWA JT8 JT8D* NE EMERGENCY LIGHT INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 804ME 48030 EMERGENCY LIGHTS ABOVE, ON COCKPIT CEILING ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. (K) 2 L 7 2 4F 4 F A6WE E2EA 20080903 NM 2008 9 3 MZZA0800002 1 20080807 A 2560 ACREM1A MEGAPHONE BOEING 737 737824 13844BZ NM CABIN INOPERATIVE A MZZA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27246 28956 FORWARD MEGAPHONE FOUND INOPERATIVE. REMOVED AND REPLACED FORWARD MEGAPHONE IAW IFM 25-60-01. OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20080903 NM 2008 9 3 MWE2008F00030 1 20080810 A 2421 100201020752 STATIC INVERTER BOEING 717 717200 1383700 NM INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 912ME 55175 DURING INITIAL POWER UP OF AC, WHEN SELECTING EMERGENCY POWER TO ARM "BUSS AC EMERGENCY OFF" COMES ON AND BATTERY STARTS DISCHARGE. REMOVED AND REPLACED STATIC INVERTER. (K) 2 L 7 2 4F TR A6WE 20080903 CE 2008 9 3 26N2008F00002 1 20080804 A 2730 70611107 CONTROL CABLE CESSNA 510 510 2076617 CE PWC PW615 PW615FA 52282 NE ELEVATOR FROZEN E 26NA O OTHER O OTHER NR NOT REPORTED 1 EA 05 1693L 461 5100026 7/24/2008, AC TT: 461.8, TC:302 CREW REPORTED AILERONS FROZEN AFTER FLYING THROUGH MOISTURE (FROM FORM 26NA-210A, ATTACH ED) 7/25/2008, AC REPOSITIONED TO MFG SERVICE CENTER FOR FURTHER EVALUATION AND RESOLUTION. 8/1/2008, AC TT: 462.3 MFG MTR FOR RESOLUTION. (K) 1 L 7 2 4F 4 F RT A00014WI E00073EN 20080903 SO 2008 9 3 WWQ2008F00002 1 20080801 A 8010 YU10352 GEAR GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU RT STARTER WORN E WWQA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 07 995GG 9182 1519 1074 RT ENGINE FAILED TO START, FOUND THAT THE STARTER WAS BAD. DURING THE STARTER REPLACEMENT, NOTICED ABNORMAL WEAR ON THE ENGINE GEAR BOX STARTER GEAR. CONTACTED ENGINEERING DEPARTMENTS TO AS FOR LIMITATIONS. AFTER ENGINEERING DEPARTMENTS REV IEWED PICTURES, THEY DETERMINED THAT THE STARTER GEAR BOX GEAR REQUIRED FURTHER EVALUATIONS. SPECIAL FLIGHT PERMIT (FER RY FLIGHT) AND FLEW THE AC FOR FURTHER EVALUATION. ENGINEERS DETERMINED STARTER GEAR IN THE GEAR BOX REQUIRED REPLACEME NT. A RENTAL ENGINE IS BEING INSTALLED AND ENGINE SN 16257 GEAR BOX STARTER WILL BE REPLACED. (K) 2 L 7 2 4F 4 F RT A12EA E25NE 20080903 CE 2008 9 3 FOM2008F00000 1 20080809 A 3260 P624007 DOWNLOCK SWITCH LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP MLG INTERMITTENT E FOMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 19 395MY 395 ON FINAL APPROACH, DURING PART 91 FLIGHT FOR AC OWNER, CREW NOTED THA THE LT MLG WOULD NOT INDICATE REQUIRED "GREEN" DOW N-LOCK INDICATION. ALL OTHER GEAR INDICATED PROPERLY AFTER NORMAL EXTENSION. CREW PROCEEDED WITH EMERGENCY CHECKLIST I TEMS IAW MFG, INCLUDING EMERGENCY GEAR EXTENSION PROCEDURE, AND NO CHANGE IN SITUATION OCCURRED. LT MLG STILL DID NOT I NDICATE DOWNLOCKED. CREW CONDUCTED SEVERAL FLY-BY MANEUVERS TO HAVE ATC CONTROL TOWER VERIFY GEAR POSITION. ATC REPORT ED "GEAR APPEARS DOWN AND LOCKED". CREW COMPLETED ALL EMERGENCY CHECKLIST ITEMS AND BRIEFED OCCUPANTS ON UPCOMING "GEAR UNSAFE" LANDING. CREW DECLARED EMERGENCY AND PROCEEDED WITH APPROACH AND LANDING AT AIRPORT WITHOUT INCIDENT. GEAR HELD 2 L 7 2 4F 4 F A10CE E6WE 20080903 NM 2008 9 3 MWE2008F00031 1 20080814 A 3350 6011779 BATTERY PACK BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE EMERGENCY LIGHT INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 904ME 55168 CEILING LIGHTS FWD OF THE CABIN DID NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK. (K) 2 L 7 2 4F 4 F TR A6WE E00061EN 20080904 NM 2008 9 4 QXEA20800702 1 20080630 A 2160 8209143 BYPASS VALVE BOMBDR DHC8 DHC8402 1390042 NM CABIN AIR FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 09 415QX 4081 BOI - FLIGHT 2344 (SUN-SEA). UNABLE TO CONTROL CABIN TEMPS. UP TO 100 DEGREES IN CABIN. DIVERTED TO BOI. ACCOMPLISHE D UNEVENTFUL LANDING. CONFIRMED BOTH PACKS UNCONTROLLABLE ON GROUND RUN. REPLACED BOTH BYPASS VALVES. OPERATIONAL CHE CKS GOOD. RETURN TO SERVICE. (A) 2 H 7 2 4T RT A13NM 20080904 EA 2008 9 4 SIMA200818403 1 20080728 A 3240 METERING VALVE CNDAIR CL600 CL6002C10 1390015 EA LT BRAKE FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SW 21 505AE 13759 10053 ON FLIGHT 9807 AT FL 400 CREW REPORTED A "MLG BAY OVHT" WARNING ON ED1. THE CREW DECLARED AN EMERGENCY. DURING DESCENT A FUME/SMOKE ODOR BECAME APPARENT IN THE COCKPIT/CABIN. AIRCRAFT LANDED WITH OUT FURTHER INCIDENT. AIRCRAFT REMOVED F ROM SERVICE. REMOVED AND REPLACED BRAKE METERING VALVE, NR 3 TIRE ASSEMBLY, AND NR 3 BRAKE ASSEMBLY. PERFORMED A CHECK FLIGHT WITH NO FAULT FOUND. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A21EA 20080904 SO 2008 9 4 SIMA200818903 1 20080702 A 3260 852701 PROXIMITY SWITCH EMB 135 EMB135LR 3260305 SO LT MLG MALFUNCTIONED A SIMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 21 701MH 145162 ON FLIGHT 4834 CREW REPORTED ON TAKEOFF THAT THE LT LANDING GEAR WOULD NOT RETRACT CAPTAIN ELECTED TO RETURN TO FIELD. AIRCRAFT REMOVED FROM SERVICE. PERFORMED CMC DOWNLOAD REMOVED AND REPLACED LANDING GEAR NR 1 DOWNLOCK [A] PROXIMITY SWI TCH IAW EMB AMM 32-61-02. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080904 NM 2008 9 4 QXEA200800592 1 20080611 A 5210 STOP BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 418QX 4143 LAX - FLIGHT 2442 - MAIN CABIN DOOR HARD TO OPEN AFTER LANDING. MAINTENANCE LUBRICATED THE DOOR STOPS. OPERATIONAL CHE CKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. (A) 2 H 7 2 4T RT A13NM 20080904 NM 2008 9 4 QXEA200800662 1 20080617 A 3240 BRAKE BOMBDR DHC8 DHC8402 1390042 NM MLG WEAK A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 401QX 4031 PDX - FLIGHT 2339 - BRAKING ACTION SOFT WITH FIRM BRAKE PRESSURE ON RUDDER PEDALS. BLED BRAKES IAW 32-42-00-870-801. T AXI CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. (A) 2 H 7 2 4T RT A13NM 20080904 NM 2008 9 4 DHL2008F00020 1 20080607 A 5347 SEAT TRACK BOEING 727 7272M7 138407S NM BS 1029 CORRODED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 PITTING CORROSION ON SEAT TRACK UPPERMOST SURFACE AT BS 1029 AND RBL 24. BLEND OUT AREA AT SEAT TRACK FOUND OUT OF LIMI TS IAW SRM 53-10-1 FIG 3. FABRICATED NEW SECTION OF SEAT TRACK IAW SRM 53-10-5 FIG 1 AND 51-20-1 INSTALLED NEW SEAT TRA CK SRM 53-10-5 FIG 1. (A) 2 L 7 3 4F A3WE 20080904 NM 2008 9 4 RYN2008F00002 1 20080630 A 2913 PUMP BOEING 757 7572G5 1384912 NM HYD SYSTEM FAILED A RYNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 151GX 24451 AFTER TAKEOFF LT ENGINE DRIVEN HYDRAULIC PUMP LIGHT AND EICAS MESSAGE CAME ON. RETURNED TO AZA AND MADE OVERWEIGHT LAND ING. PERFORMED AN OVERWEIGHT LANDING INSPECTION IAW AMM 08-51-38 AND PLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP ON DE FERRAL PER MEL 29-31-1. (A) 2 L 7 2 4F RT A2NM 20080904 NM 2008 9 4 QXEA200800653 1 20080618 A 5210 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM DOOR UNKNOWN A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 413QX 4060 SEA - AFT GALLEY DOOR (R2) HARD TO LATCH. MAINTENANCE PERFORMED A VISUAL INSPECTION AND OPERATIONAL CHECK WITH NO DEFEC TS NOTED. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED. (A) 2 H 7 2 4T RT A13NM 20080904 EA 2008 9 4 QXEA200800715 1 20080710 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 667 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 612QX 10042 PDX - C4 CHECK - CORROSION AT RT INBOARD SEAT TRACK AT STATION 667.00 BLENDED AREA. MATERIAL REMOVED WITHIN LIMITS OF R EO 670-53-00-012. ALODINED TRACK. (A) 2 L 7 2 4F RT A21EA 20080904 EA 2008 9 4 QXEA200800695 1 20080626 A 3260 895303 PSEU CNDAIR CL600 CL6002C10 1390015 EA MLG FAILED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 605QX 11001 10022 PDX - FLIGHT 2590 - FOLLOWING GEAR RETRACTION, RECEIVED A GEAR DISAGREE MESSAGE. NOSE GEAR APPEARED SLOW TO RETRACT. M AINTENANCE ADJUSTED PX-22 IAW 32-61-05-820-804-A01. REPLACED PSEU AS PRECAUTION. RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A21EA 20080904 2008 9 4 J4P2008F00000 4 20080727 A 2200 135600025 AUTOPILOT SYS CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO FAILED E J4PA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 13 398SR 2102 689888 FLIGHT ORIGINATED AT PBI TO CCO AT 1319L WITH 2 PAX, WHILE EN ROUTE AUTO PILOT FAILED AND DIVERTED TO SGT AND WITHOUT IN CIDENT. (A) 1 L 7 1 3O 3 O NT A00009CH E3SO 20080904 2008 9 4 USAA920081372 4 20080712 A 2565 650261 CABLE AIRCRUISERS AIRBUS 320 A320231 3930325 EU ESCAPE SLIDE DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 622AW 2065 54 PHX-FLT 504-OPERATIONAL TEST OF THE EMERGENCY SLIDE LIGHTS FAILED. MX REPLACED AFT LT SLIDE. VENDOR REPORT INDICATES TH AT A DEFECTIVE CABLE ASSEMBLY CAUSED THE LIGHTS TO GO OFF AND ON. (S) 2 L 7 2 4F RT A28NM 20080904 EU 2008 9 4 USAABA08024 1 20080706 A 2752 ACTUATOR AIRBUS 330 A330323 3930335 EU TE FLAPS FAILED A USAA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 EA 19 277AY 0380 MAD FLT 740 ENROUTE PHL TO MAD. DURING APPROACH, THE TRAILING EDGE FLAPS WOULD NOT EXTEND. THE LEADING EDGE FLAPS OPERAT ED NORMALLY. THE FLIGHT MADE A MISSED APPROACH AND THEN LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING (B) MAINTENANCE REPLACED THE NUMBER TWO, LEFT HAND FLAP ROTARY ACTUATOR (FIN 5022CU). OPERATIONALLY CHECKS OK. [SUPP CLOSE D](B) 2 L 7 2 4F RT A46NM 20080904 EU 2008 9 4 USAA920081358 1 20080710 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 3930316 EU EMERGENCY LIGHTS FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 109UW 29128 2267 1065 LOG# 4288237 - LAX- C-9-FWD EMERGENCY POWER SUPPLY UNIT WILL NOT TEST. MX REPLACED THE EPSU. OPERATIONAL TEST WAS GOOD. (B) 2 L 7 2 4F RT A28NM 20080905 CE 2008 9 5 GLB2008F00011 1 20080724 A 3230 LANDING GEAR BEECH 1900 1900D 1154162 CE MALFUNCTIONED A GLBA O OTHER J WARNING INDICATION CL CLIMB 1 NM 03 255GL UE255 FLIGHT 5063 - PILOTS REPORTED GEAR WOULD NOT MOVE TO THE UP POSITION. TRIED J-HOOK A COUPLE OF TIMES AND IT WOULDN’T CO ME UP AT FIRST, THEN THE HANDLE MOVED UP BUT THE GEAR WOULDN’T COME UP. LANDING GEAR RELAY CIRCUIT BREAKER POPPED. PUS HED IN, GEAR CAME UP, THEN PUT BACK DOWN AND CIRCUIT BREAKER POPPED AGAIN. OPEN (A) 2 L 7 2 4T RT A24CE 20080905 EA 2008 9 5 TRAX200800663 1 20080519 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 929EV 8007 FS 621 ANGLE IS CRACKED .5 INCH RIGHT SIDE FLOOR SUPPORT. REPAIR TO FLOOR SUPPORT ANGLE FS 621 IAW REO 601R-53-61-117. WORK C/W IAW REO 601R-53-61-117. (B) 2 L 7 2 4F RT A21EA 20080905 NM 2008 9 5 USAA920081337 1 20080623 A 5330 6545765 SKIN BOEING 737 73733A 1384673 NM BS 360-540 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN-C21 -MAJOR REPAIR- CRACKS IN FUSELAGE SKIN AT LAP SEAM, BS 360 TO BS 540, S10R, RBL 60. REPAIRED FUSELAGE SKIN AT L AP SEAM, BS 360 TO BS 540, S10R, RBL 60 IAW US AIRWAYS EA 130056. (B) 2 L 7 2 4F RT A16WE 20080905 NM 2008 9 5 USAA920081353 1 20080701 A 5320 6545834260 INTERCOSTAL BOEING 737 737401 1384701 NM BS 312-326 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT -MAJOR- Q3 CHECK - LEVEL 2 CORROSION ON INTERCOSTAL STIFFENER, BS 312 -BS 326, LBL 10. REPAIRED INTERCOSTAL STIFFEN ER, BS 312 - BS 326, LBL 10 IAW B737 SRM 51-10-02. (B) 2 L 7 2 4F RT A16WE 20080905 NM 2008 9 5 CALA0800741 1 20080724 A 5310 BAC1515553X7075T CREASE BEAM BOEING 757 757224 1384958 NM BS 1180-1310 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18119 27561 RIGHT SIDE OF FLOOR STURCTURE CREASE BEAM LOCATED AT STATION 1200 TO 1320 CORRODED IN SEVERAL SPOTS. REMOVED DAMAGED SE CTION AND FABRICATED NEW INBOARD CHORD SECTION OF CREASE BEAM FROM STATION 1180 TO 1310, PERFORMED REPAIR TO RIGHT SIDE FLOOR STRUCTURE INBOARD CHORD OF CREASE BEAM FROM STATION 1180 TO 1310 PER SRM 51-70-12 AND DWG 146N5590. 2 L 7 2 4F RT A2NM 20080908 NM 2008 9 8 2008UALA03645 1 20080630 A 3350 GE209 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EMERGENCY EXIT LIGHT INOP AT CEILING ROW 14. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE . 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03866 1 20080711 A 5270 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 2R GIRT BAR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 598UA 28751 SLIDE LIGHT AT 2R IS DIM. GIRT BAR AFT SENSOR SHORTED. REPLACED GIRT BAR AFT SENSOR, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080908 NM 2008 9 8 2008UALA03673 1 20080702 A 3397 582011 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY EXIT EEL LIGHT INOP ACROSS DOOR 3 LEFT LOWER WALL. FOUND BROKEN FEEDER WIRE. REPAIRED FEEDER WIRE, OP CHECKE D GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03675 1 20080702 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY EXIT EEL LIGHT INOP AT DOOR 5 LEFT LOWER WALL CROSSAISLE. FOUND BURNED OUT LAMP. REPLACED LAMP OP CHECKED GO OD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03748 1 20080707 A 3350 20131A BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 DOOR 1L OVERHEAD EMERGENCY EXIT LIGHT INOP. FOUND FAULTY BATTERY PACK. REPLACED BATTERY PACK, OP CHECK OK REF MM 33-5 1-04. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03609 1 20080626 A 3350 80602 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EEL INOP, G5 GALLEY FWD WALL. FOUND FAULTY CABLE ASSEMBLY. REPLACED CABLE ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVIC E. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 WP 2008 9 8 DHL2008F00007 1 20080701 A 2697 CONNECTOR DOUG DC8 DC871F 302199D WP FIRE DETECTION DIRTY A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 830BX 45973 FLT NR: ATN 808, DURING CRUISE NR 2 ENGINE FIRE WARNING & BELL CAME ON INTERMITTENT FOR 1-2 SECONDS. CREW ACCOMPLISHED CHECK LIST AND SHUT DOWN NR 2 ENGINE. THE FIRE BELL STOPPED AFTER FIRE HANDLE WAS MOVED TO FULL FORWARD POSITION. THE FIRE BOTTLES WERE NOT DISCHARGED. THE CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED NR 2 FIRE WARNING SYSTEM AND FOUND LT FAN ELEMENT CONNECTOR WET, RT FIRE DETECTOR ELEMENT CONNECTOR DIRTY. MAINTENANCE CLEANED BOTH CONNECTORS, AND REPLACED LT AND RT FAN ELEMENT, AND LT AND RT FIRE DETECTOR ELEMENT. OPERATIONAL CHECK GOOD IAW MM 26-10-1, ERH 70-1-0 1. AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 4 4F RT 4A25 20080908 EU 2008 9 8 2008UALA03852 2 20080713 A 7230 COMPRESSOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 ENGINE DAMAGED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 29 338UA 24242 724431 NR 2 COMPRESSOR STALL. RTFL. TWO LPT 4TH STAGE BLADES WERE FOUND TO HAVE FRACTURE ABOUT .5 INCHES FROM BLADE PLATFORM . CHANGED ENGINE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080908 NM 2008 9 8 2008UALA03234 1 20080605 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 THE 5A AFT EEL LIGHT DETACHED. FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 AIEA200800262 1 20080708 A 3244 TIRE BOEING 747 74747UF 1384812 NM RT MLG FAILED A AIEA K NONE O OTHER IN INSP/MAINT 1 GL 11 408MC 29261 DURING ARRIVAL WALK AROUND INSPECTION FOUND NR 11 TIRE SEPARATION. REPLACED NR 11 AND 12 WHEEL ASSEMBLIES. ALSO ACCOMP LISHED TIRE TREAD LOSS CONDITIONAL INSPECTION AS PER 05-51-34-202-001. (A) 2 L 7 4 4F RT A20WE 20080908 NM 2008 9 8 R612008F00006 1 20080719 A 2133 2142501 OUTFLOW VALVE EMB ERJ170 ERJ170100SU 3260403 NM CABN PRESS SYS FAILED A R61A O OTHER O OTHER NR NOT REPORTED 1 GL 11 821MD 10493 17000042 CREW REPORTED AT FLIGHT LEVEL 31,000 FEET, RECEIVED A CABIN HIGH ALTITUDE MESSAGE. CREW DEPLOYED OXYGEN MASK AND DESCEN DED TO FLIGHT LEVEL 10,000 FEET AND DECLARED AND EMERGENCY AND DIVERTED TO TTS. MAINTENANCE REMOVED AND REPLACED THE OU TFLOW VALVE AND PLACED THE AIRCRAFT BACK INTO SERVICE. (A) 2 L 7 2 4F RT A56NM 20080908 2008 9 8 2008UALA03937 4 20080719 A 3442 RECEIVER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE WX RADAR SYS INOPERATIVE A UALA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 WP 29 804UA 759 WEATHER RADAR INOP. FLIGHT DIVERTED. REPLACED WX RADAR RECEIVER, TRANSMITTER OPS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20080908 NM 2008 9 8 R612008F00007 1 20080719 A 3150 WARNING LIGHT EMB ERJ170 ERJ170200LR 3260121 NM BRAKES FALSE ACTIVATION A R61A A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 11 118HQ 17000189 CREW RECEIVED A BRAKE FAULT MESSAGE MOMENTARILY IN FLIGHT AND MESSAGE WENT AWAY. CREW ADVISED ATC AND AN EMERGENCY WAS DECLARED. CREW FOLLOWED QRH PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT TROUBLE SHOT AND SYSTEM NO DEFECTS NOTED AND SYSTEM OPERATIONAL CHECKS COMPLETED AND AIRCRAFT WAS RETURNED TO SERVICE. NO FURTH ER FAULTS INDICATED AT THIS TIME. (A) 2 L 7 2 4F RT A56NM 20080908 NM 2008 9 8 YENA2008069 1 20080721 A 2150 10007004 ACM EMB ERJ190 ERJ190100IGW 3260408 NM NR 1 FAILED A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 15 203JB 6638 19000023 FLT 1082, CLT-JFK, SMOKE IN CABIN. APPROACH TO LANDING AT 2000`, SULPHUR ODOR NOTED IN COCKPIT. FLIGHT ATTENDANT CONFI RMED SMOKE IN CABIN AND ODOR OF SULPHUR. COMPLIED WITH SMOKE/FIRE QRH. UPON INSPECTION FOUND PHYSICAL PACK 1 FAILURE W ITH FRAGMENTS IN EXHAUST DUCTING GRILLE. TSD DATA PULLED FOR PACK 1 DATA. (AIR CONDITIONING PACKS-SINGLE). REMOVED AN D REPLACED NR 1 PACK ACM IAW AMM 21-51-05 AND HEAT EXCHANGER IAW AMM 21-51-04. OPS CHECK OK. (A) 2 L 7 2 4F RT A57NM 20080908 NM 2008 9 8 QXEA200800694 1 20080625 A 5240 DOOR BOMBDR DHC8 DHC8402 1390042 NM AFT SERVICE MALFUNCTIONED A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 405QX 4047 LAX - FLIGHT 2307 - RT REAR SERVICE DOOR WILL NOT CLOSE. RESET DOOR PER SERVICE LETTER. DH8-400-SL-52-003A. RETURNED TO SERVICE. NO PARTS REPLACED. (A) 2 H 7 2 4T RT A13NM 20080908 NM 2008 9 8 CALA0800746 1 20080725 A 5320 652072629 SILL BOEING 737 737524 1384721 NM FWD CARGO CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 FWD CARGO LOWER SILL PLATE HAS CORROSION ON TOP AND BOTTOM SIDES. INSTALLED NEW SILL PLATE IN FWD CARGO IAW B737 SRM51- 40-02. 2 L 7 2 4F RT A16WE 20080908 NM 2008 9 8 CALA0800747 1 20080725 A 5320 655483214 STIFFENER BOEING 737 737524 1384721 NM BS 1138 DEFORMED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 STIFFENER STATION 1138 DEFORMED. REMOVED OUT OF LIMITS STIFFENER AT STATION 1138, FABRICATED AND INSTALLED NEW STIFFENE R AND SPLICE AT STATION 1138 PER DWG 65-54832 AND B-737-500 SRM 51-70-11. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 CALA0800777 1 20080808 A 5320 143A812210 PAN BOEING 737 737724 13844BY NM CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 21723 28790 FORWARD CARGO COMPARTMENT DOOR CUTOUT LOWER PAN HAS SURFACE CORROSION IN THREE AREAS. REMOVED AND INSTALLED NEW WEB PER SRM 51-40-02 PARAGRAPH 5. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 CALA0800764 1 20080803 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 787 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16632 27900 FRAME CRACKED STATION 787 AT S-9L. REPAIRED FRAME PER EA 5310-04498 OP 2. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 CALA0800765 1 20080803 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM BS 967 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16632 27900 FRAME CRACKED STATION 867 AT S-9L. INSTALLED REPAIR DOUBLERS PER EA 5310-04498, OP 2. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 2008UALA04079 1 20080801 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ROW 9 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 399UA 24674 EEL LIGHT SECTION INOP FWD OF ROW 9. FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY OP CHECK GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 ZZDA2008135 1 20080807 A 3397 WIRE BOEING 717 717200 1383700 NM EMERGENCY LIGHT DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 906AT 55087 EMERGENCY LIGHTS INOP ON ROW 25-30. REPAIRED WIRING (EMERGENCY TRACK PATH) REF SWPM 20-10 AT SEAT 25. OPS CK GOOD REF MM 33-51. 2 L 7 2 4F TR A6WE 20080909 NM 2008 9 9 2008UALA03855 1 20080711 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ROW 16 INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 306UA 23667 EEL LIGHTS ARE INOP FROM ROW 16 AFT. *S/D* FOUND FAULTY LIGHT STRIP. REPLACED LIGHT STRIP, OP CHECKED GOOD. AC OK FO R SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 2008UALA03810 1 20080710 A 8011 8088846 START VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 ENGINE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 783UA 26950 NR 2 ENGINE START VALVE INOP. *S/D* FOUND FAULTY START AIR VALVE. REPLACED PER MM80-11-02, OP CHECKED GOOD. AC OK FO R SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 NM 2008 9 9 2008UALA04022 1 20080727 A 2697 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FIRE LOOP LOOSE A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 198UA 28716 THE 'ENG 1 FIRE LP B' EICAS STATUS MSG DISPLAYED. ENG 1 FIRE LOOP-B FIRE OR FAULT OUTPUT. FOUND LOOSE CONNECTION ON FW D LOOP. CLEANED AND SECURED LOOP CONNECTION. CLEANED AND SECURED THE OTHER B LOOP CONNECTIONS. OPS TEST NORMAL. AC OK F OR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080909 NM 2008 9 9 2008UALA04011 1 20080725 A 3510 TRANSDUCER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW OXYGEN SYS LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 CREW OXYGEN NEEDS SERVICING. FOUND TRANSDUCER LEAKING. REPLACED O2 TRANSDUCER OP CHECKS OK. SERVICED O2 TO 1750. AC O K FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 CALA0800778 1 20080728 A 5240 65C807351 ANGLE BOEING 737 7373T0 1384582 NM R2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 R2 DOOR Z-ANGLE CORRODED AND STRAP AFT OF Z=ANGLE IS CORRODED. REMOVED CORRODED R2 Z-ANGLE AND STRAP IAW B737 SRM 51-40 -02. CLEANED CORROSION FROM STRAP, FOUND TO BE WITHIN LIMITS PER B737 SRM 51-10-02. LOCATED AND DRILLED NEW Z-ANGLE PE R B737 SRM 51-40-05. REINSTALLED R2 Z-ANGLE AND STRAP PER B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 CALA0800758 1 20080801 A 5311 65C34355 FRAME BOEING 737 737524 1384721 NM BS 482 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16632 27900 FRAME CRACKED STATION 482 AT S-9 R. REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 CALA0800760 1 20080801 A 5320 65C333672 INTERCOSTAL BOEING 737 737524 1384721 NM BS 947-967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16632 27900 TOP OF INTERCOSTAL AT RBL 50 BETWEEN FLOORBEAMS 947 AND 967 HAS CORROSION ON TOP SURFACE IN MULTIPLE AREAS. REMOVED DAM AGED INTERCOSTAL REF SRM 51-40-02, LOCATED AND DRILLED NEW INTERCOSTAL P/N 65C33367-2 REF SRM 51-40-05. INSTALLED NEW I NTERCOSTAL REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 CALA0800761 1 20080802 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM BS 747 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16632 27900 FRAME CRACKED STATION 747 AT S-9R. REPAIRED FRAME PER EA 5310-04498 OP 2. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 CALA0800772 1 20080805 A 5311 6546596 FRAME BOEING 737 737524 1384721 NM BS 727B S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16632 27900 FRAME CRACKED STATION 727B AT S-9L. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLERS REF EA5310-04498. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 2008UALA03716 1 20080703 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ROW 22 BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 EEL STRIP LOOSE AT ROW 22. *S/D* FOUND BROKEN LIGHT STRIP. REPAIRED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVI CE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 CALA0800762 1 20080802 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM BS 907 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16632 27900 FRAME CRACKED STATION 907 AT S-9R. REPAIRED FRAME PER EA 5310-04498, OP 2. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 CALA0800763 1 20080803 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM BS 867 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16632 27900 FRAME CRACKED STATION 867 AT S-9R. INSTALLED REPAIR ANGLES PER EA 5310-04498, OP 2. 2 L 7 2 4F RT A16WE 2008022600222 20080226 00222 EA 2008 2 26 A6WA200840050 1 20080123 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE SERVICE DOOR FAULTY A A6WA K NONE O OTHER NR NOT REPORTED 1 GL 31 440AW 7766 REQUEST INSPECTION FOR OPERATION OF SERVICE DOOR. (DOOR OPENS ABNORMALLY). (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022700327 20080227 00327 NM 2008 2 27 UIEA200800052 1 20080215 A 5313 STRINGER BOEING 747 7472D7B 1384803 NM ZONE 100 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 AFT CARGO COMPARTMENT STRINGER 51 CORROSION WITH MARKING AT STATION 1800, LEVEL 1 CORROSION. AFT CARGO STRINGER CORROSI ON REPAIRED IAW 53-10-03. 2 L 7 4 4F RT A20WE 20080903 2008 9 3 K2D2008F00000 2 20080806 A 7320 369H81445 PRESSURE SWITCH HUGHES 369 369E 4470707 WP ENG FUEL PUMP LEAKING E K2DA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 500PH 0187E ON OR AROUND 5:00 PM, WEDNESDAY, 6 AUGUST, 2008, WHILE CONDUCTING A POST FLIGHT INSP, DISCOVERED SOME OIL LEAKAGE IN ENG INE COMPARTMENT. AS HE WAS INVESTIGATING LEAKAGE, NOTICED THAT THE FUEL FILTER PRESSURE SWITCH HAD PLAYED BETWEEN TWO B ODY HALVES AND HAD SOME FUEL LEAKAGE. AT WHICH TIME, GROUNDED HELICOPTER, RESCHEDULED OUR FLIGHTS FOR NEXT DAY, AND ORD ERED THE PART TO REPAIR THE FAULT. AT THIS TIME, HAVE NO PROBABLE CAUSE FOR THIS INCIDENT BUT DID INFORM THE MECHANIC T O USE CAUTION IN TORQUING THE LINES AND FITTINGS THAT CONNECT THIS PART TO THE ENGINE. (K) 1 G 7 1 3U H3WE 20080903 WP 2008 9 3 MWE2008F00032 1 20080819 A 3397 WIRE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217C 52053 NE EMERGENCY LIGHT BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 EMERGENCY FLOOR LEVEL LIGHTS INOPERATIVE FROM ROW 9 TO 20. REPAIRED BROKEN WIRE IN CENTER SECTION OF LIGHT TRACK. (K) 2 L 7 2 4F 4 F A6WE E9NE 20080903 EU 2008 9 3 PNS2008F00008 1 20080814 A 3320 BVO33000250 SOCKET SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN LIGHT BURNED A PNSA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AL 03 676PA 316 WHILE ENROUTE, FLIGHT CREW WAS NOTIFIED BY THE F/A THAT THERE WAS SMOKE AND AN ODOR IN THE CABIN, THE FLIGHT CREW PERFOR MED EMERGENCY PROCEDURES AND AN UNEVENTFUL LANDING WAS MADE AT THE DESTINATION AIRPORT. MAINT FOUND THE OVERHEAD LIGHT FIXTURE ABOVE SEAT 1A WAS BURNED AND MELTED. THE SYSTEM WAS DEFERED AND THE AC RETURNED TO THE MAINT BASE AND THE LAMP HOLDER WAS REPLACED AND THE LIGHTING SYS TESTED. WE HAVE HAD SIMILAR ISSUES WITH THESE LAMP HOLDERS WHICH ARE MADE OUT OF PLASTIC. IT WOULD BE BETTER IF THESE LAMP HOLDERS WERE MADE FROM CERAMIC OR ANOTHER MATERIAL THAT WOULD RESIST MELTI NG AND BURNING. (K) 2 L 7 2 4T 4 T RT A52EU E8NE 20080903 NM 2008 9 3 MWE2008F00033 1 20080817 A 2421 R25159 RELAY BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE EMERGENCY POWER FAILED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 916ME 55178 EMERGENCY POWER TEST FAILED. SHOWS NO POWER TO EMERGENCY AC. REMOVED AND REPLACED EMERGENCY POWER RELAY. (K) 2 L 7 2 4F 4 F TR A6WE E00061EN 20080904 NM 2008 9 4 QXEA200800698 1 20080629 A 3231 83232010007 SPRING DHAV DHC8 DHC8202 2809007 NM NLG DOOR BROKEN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 345PH 476 SEA - FLIGHT 2100. AFTER DEPARTURE, NOISE NOTED AFTER GEAR RETRACTION. TOWER REPORTED NOSE GEAR DOORS OPEN. RETURNED TO FIELD. UNEVENTFUL LANDING. FOUND RT FWD NLG DOOR SPRING AND CONTROL ROD BROKE. REPLACED. OPERATIONAL CHECKS GOOD. RETURNED TO SERVICE. (A) 2 H 7 2 4T RT A13NM 20080904 CE 2008 9 4 COEA0801775 1 20080728 A 3244 0253490 TIRE CESSNA 208 208B 2073701 CE RT MLG FAILED A COEA O OTHER O OTHER LD LANDING 1 NM 13 775FE 387 208B0272 TIRE WENT FLAT AFTER LANDING, FLT 7689 SLE TO PDX. UPON LANDING IN PDX THE PILOT NOTICE THE RT MLG TIRE FELT SOFT. AS THE AIRCRAFT SLOWED THE TIRE WENT FLAT. AIRCRAFT SAFELY CLEARED RUNWAY AND STOPPED. REMOVED AND REPLACED RT MAIN WHEEL ASSEMBLY. (A) 1 H 7 1 3T A37CE 20080904 NM 2008 9 4 QXEA200800588 1 20080606 A 3260 PROXIMITY SENSOR BOMBDR DHC8 DHC8402 1390042 NM MLG MALFUNCTIONED A QXEA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 414QX 4061 SEA - ON APPROACH WHEN GEAR SELECTED DOWN, LT GEAR DOOR LIGHT REMAINED ON. WENT OFF AFTER LANDING. FERRIED SEA-PDX. I N PDX REPLACED NR 1 MLG DOWNLOCK PROX SENSOR. OPERATIONAL CHECKS GOOD. (A) 2 H 7 2 4T RT A13NM 20080904 EA 2008 9 4 TRAX20800735 1 20080603 A 5320 VERTICAL BEAM CNDAIR CL600 CL6002B19 1900309 EA BS 409 CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 824AS 7203 FS 409.0+128 BULKHEAD VERTICAL STIFFENER BEAM AT LBL 18 CRACKED AT OUTBOARD SIDE LOWER RADIUS APPROX .5 INCH LONG. REMO VED BRACKET ASSY P/N 601R96611-057 FROM LBL 18 TO LBL 27 POST TO GAIN ACCESS TO AREA CRACKS IAW SRM 51-42-06. VERTICAL POST REQUIRES REPAIR. COMPLIED WITH REPAIR OF FS 409.0+128 BULKHEAD VERTICAL STIFFENER AT LBL 18 IAW REO 601R-53-41-056 AND REO 601R-53-41-059. BRACKET ASSEMBLY REQUIRES REINSTALLED. REINSTALLED BRACKET ASSEMBLY ON LBL 18 LBL 27 IAW SRM 51-42-06. ASA RII COMPLIED WITH. (A) 2 L 7 2 4F RT A21EA 20080904 SO 2008 9 4 SIMA200821002 1 20080728 A 5320 14522178005 SILL EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 839AE 145653 DURING MBV INSPECTION THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. REMOVED DAMAGED SILL, TREATED SILL AND INSTALLED NEW SILL IAW EMB 145 SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080904 NM 2008 9 4 DHL2008F00021 1 20080619 A 5310 BEAM BOEING 727 7272M7 138407S NM BS 312-328 MISINSTALLED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 HORIZONTAL WALKWAY BEAM LOWER CHORD LT SIDE, HAS SEVERAL FASTENERS BUCK TAIL FLAT, ALSO IMPROPER SIZE FASTENERS BETWEEN BS 312 AND BS 328. REMOVED AND REPLACED HORIZONTAL WALKWAY LOWER LT CHORD BS 312 TO 328 IAW B727 SRM 51-30-2. P/N 65-1 9861-7 (A) 2 L 7 3 4F A3WE 20080904 EA 2008 9 4 TRAX200800918 1 20080717 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 719EV 10099 SECOND FROM FRONT CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED 2ND FROM FRONT CABIN CEILING EMERGENCY FLOOD LIGHT BULB. OPS CHECK GOOD. SDR CLOSED. (A) 2 L 7 2 4F RT A21EA 20080904 WP 2008 9 4 ARWA20080706 1 20080724 A 2910 HYDRAULIC SYSTEM DOUG DC10 DC1030F 3023504 WP NR 1 LOW A ARWA O OTHER W INADEQUATE Q C CR CRUISE 1 SO 29 450ML 47831 NR 1 HYDRAULICS NEED SERVICING. SERVICED NR 1 HYDRAULIC SYSTEM AS REQUIRED IN ACCORDANCE WITH DC10 M/M 12-13-02; CHECKE D FOR LEAKS IN ACCORDANCE WITH DC10 M/M 29-00-00, NO LEAKS NOTED. (A) 2 L 7 3 4F RT A22WE 20080904 CE 2008 9 4 NSV2008F00014 1 20080724 A 3230 LANDING GEAR BEECH 1900 1900D 1154162 CE MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 27 191CJ UE19 WHEN GEAR PLACED IN DOWN POSITION AND GEAR RELAY POPPED AFTER 16 SEC WITH RED HANDLE ILLUMINATED AND NO GREEN LIGHTS, PE RFORMED MANUAL LANDING GEAR EXTENSION. MAINTENANCE INSPECTED AIRCRAFT HYD SYSTEM, NO LEAKS NOTED. CHECKED FLUID LEVEL, ALSO CHECKS GOOD. AIRCRAFT DETERMINED TO BE SAFE FOR FERRY FLIGHT FROM BOS TO ALB. (A) 2 L 7 2 4T RT A24CE 20080904 EA 2008 9 4 TRAX200800901 1 20080710 A 2560 GLOWSTRIP CNDAIR CL600 CL6002C10 1390015 EA CABIN DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 PHOTOLUMINESCENT FLOOR PROXIMITY EMERGENCY ESCAPE PATH TAPE DAMAGED AT FORWARD LAV ENTRANCE. (CABIN EMERGENCY LIGHTS-PH OTOLUMINESCENT FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING). REMOVED AND REPLACED EMERGENCY LIGHT STRIP PER AMM 33-51 -01. ACFT OK FOR SERVICE. (S) 2 L 7 2 4F RT A21EA 20080904 SO 2008 9 4 C2XA08CL089 1 20080723 A 2731 14563000401 SWITCH EMB 145 EMB145LR 3260212 SO PITCH TRIM STICKING A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 29906 145472 CLE FLIGHT 2018 THE CREW REPORTED A MAIN PITCH TRIM FAIL MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND FOUND THE FIRST OFFICER`S PITCH TRIM SWITCH WAS STICKING. THE SWITCH WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4T RT T00011AT 20080904 NM 2008 9 4 WRLA2008063 1 20080729 A 5754 STRUCTURE DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 1 SLAT CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 275WA 48631 DURING C CHECK INSPECTION CRACK-FOUND RT WING LE INBD SLAT NR 1 AFT SIDE HAD CRACK 11.5 INCHES LONG AT XIS 247. REMOVED THE RT INBD NR 1 SLAT ASSY COMPLETED PER AMM 27-80-20-000-801 REV 62. REPAIRED THE DAMAGED AREA IAW MD-11 SRM VOL ONE 57-10-00 REV. 40. INSTALLED THE RT INBD NR1 SLAT ASSY IAW 27-80-20-400-801 REV.62. FUNCTIONAL TEST OF THE RT INBD NR1 SLAT RANGE OF MOVEMENT CONDITION CHECK SATIS IAW AMM 27-80-00-710-802 REV. 62. (A) (S) 2 L 7 3 4F 4 F RT A22WE E24NE 20080904 NM 2008 9 4 WRLA2008062 1 20080730 A 5410 2214025513 FAIRING DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 3 ENGINE DENTED A WRLA O OTHER O OTHER NR NOT REPORTED 1 SO 11 275WA 48631 DURING C CHECK INSPECTION DENT FOUND NR 3 ENGINE NOZZLE FAIRING SKIN DENT AT NAC BETWEEN 3O`CLOCK AND 4O`CLOCK POSITION. (LOOKING FORWARD). REPAIRED NR3 ENG NOZZLE FAIRING SKIN IAW EI W2008 A54B-687 REV.00. JOB COMPLETED AND CONDITION CH ECK NORMAL. (A) (S) 2 L 7 3 4F 4 F RT A22WE E24NE 20080905 EA 2008 9 5 TRAX200800855 1 20080630 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 861AS 7445 FS 280 CLIPS ARE CRACKED AT LBL 9. REMOVED AND REPLACED FS 280 CLIPS AT LBL 9 IAW CRJ200 REO 601R-53-11-136 JOB COMPLET E RAP 7025969. (B) 2 L 7 2 4F RT A21EA 20080905 NM 2008 9 5 USAA920081365 1 20080703 A 5340 6935352U14 STRINGER CLIP BOEING 737 737401 1384701 NM BS 807 S10R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT-Q3 CHECK -MAJOR REPAIR- TIE CLIP CRACKED AT BS 807, S10R. REPLACED TIE CLIP AT BS 807, S10R IAW B737 SRM 52-10-02 A ND SRM 52-40-02. (B) 2 L 7 2 4F RT A16WE 20080905 EA 2008 9 5 TRAX200800878 1 20080705 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 CABIN EXIT SIGN INOP. FLT 4756 DEL 12 MINS NC FLT 4374 CX. REMOVED AND REPLACED NR 1 AND 2 BATTERIES FOR EMERGENCY LIG HT ASSY AS PER AMM 33-51-17. OPS CHECK AS PER AMM 33-51-17. (B) 2 L 7 2 4F RT A21EA 20080905 NM 2008 9 5 CALA0800742 1 20080724 A 5210 6552878125 ANGLE BOEING 737 737524 1384721 NM L2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 AFT CABIN L2 DOOR Z-ANGLE HAS CORROSION. CORROSION ON L2 DOOR Z-ANGLE FOUND TO BE BEYOND LIMITATIONS PER SRM 53-60-15 F IGURE 1, REMOVED AND REPLACED Z-ANGLE PRE SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080908 2008 9 8 2008UALA03701 4 20080702 A 2565 7A147914 O-RING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ESCAPE SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 LOW BOTTLE, FOUND BOTTLE PRESSURE LOW. REPLACED SLIDE AND RUPTURE PLUG O-RING. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 EA 2008 9 8 TRAX200800670 1 20080519 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 929EV 8007 FS 621 ANGLE IS CRACKED .5 INCH LEFT SIDE FLOOR SUPPORT. C/W REPAIR TO FLOOR SUPPORT ANGLE AT FS 621 IAW REO 601R-53-61 -117. ALL WORK C/W IAW REO 601R-53-61-117. (B) 2 L 7 2 4F RT A21EA 20080908 WP 2008 9 8 DHLA200800057 1 20080609 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 3 NACELLE FALSE INDICATION A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 807DH 45990 NR 3 ENG FIRE WARNING. COMPLETED CHECK LIST LIGHT REMAINED ON. PERFORMED NR 3 ENG RUN PER JRH 11.1 ALL SYSTEMS OPERATE NORMALLY. NO LEAKS NOTED SYS B-LOOP CHECKS NORMAL. LOOP-A CAUSES INTERMITTENT FALSE WARNINGS. PLACED A-LOOP ON DMI 3 2839 PER MEL 26-2-3 CAT C DDD 6/18/08. PLACARDS INSTALLED. FLIGHT 560. AIRCRAFT WAS GROUNDED. (A) 2 L 7 4 4F RT 4A25 20080908 NM 2008 9 8 2008UALA03347 1 20080613 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EEL INOP AT CLOSET WALL AFT OF DOOR 1L. FOUND EEL INOP AT CLOSET WALL AFT OF DOOR 1L. REPLACED BULB AND CABLE, OP CHEC K OK REF MM 33-51-12. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 EU 2008 9 8 2008UALA03871 2 20080714 A 7200 ENGINE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU LEFT MAKING METAL A UALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 WP 29 934UA 26662 724736 LT ENG FAILED ON TAKEOFF - AFTER TAKEOFF LOUD BANG ENGINE SPOOLED DOWN. RTFL. FOUND METAL IN CHIP DETECTOR. CHANGED E NGINE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080908 EU 2008 9 8 2008UALA03731 1 20080706 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 445UA 826 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED CREW O2 AND NO LEAKS NOTED AT TIME. 2 L 7 2 4F 4 F RT A28NM E40NE 20080908 NM 2008 9 8 2008UALA03676 1 20080702 A 3350 GE209 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY EXIT CEILING LIGHT INOP AT DOOR 4 FWD SIDE OF GALLEY AREA. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NE 2008 9 8 2008UALA03851 2 20080712 A 7200 PW4060 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEFT VIBRATION A UALA O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 29 662UA 66597 5753 27159 717590 LEFT ENGINE VIBRATIONS. *S/D* VIBRATION WAS NOT CONFIRMED BY ENGINE CONDITION MONITORING. GROUND RUN VIBRATION SURVEY WAS WELL WITHIN LIMITS. BORESCOPE INSPECTION REVEALED NOTHING ABNORMAL. LUBRICATED THE FAN BLADE ROOTS AND RERAN THE VIBRATION SURVEY. ALL STILL WELL WITHIN LIMITS. REPLACED VIBRATION ACCELEROMETER, PRECAUTIONARY. 2 L 7 2 4F 4 F RT A1NM E24NE 20080908 NM 2008 9 8 2008UALA03238 1 20080606 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY EXIT FLOOR LIGHT OUT AT COCKPIT DOOR. FOUND FAULTY LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03578 1 20080624 A 3350 GE209 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY CEILING LIGHT ABOVE ROW 19R INOP. FOUND BURNED OUT BULB. REPLACED BULB, OPS CHECKED GOOD. AC OK FOR SERVIC E. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03789 1 20080708 A 3350 UNK LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 THE 58M EXIT LIGHT INOP. SUSPECT FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OPS CHECKS NORMAL. AC OK FOR SERVICE . 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03409 1 20080615 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 WALL EEL INOP: AFT GALLEY FWD WALL. FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 CALA0800744 1 20080725 A 5753 SKIN BOEING 737 737524 1384721 NM LT WING TE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 LEFT OUTBOARD AFT FLAP HAS A DELAMINATED AREA ON LOWER INBOARD SURFACE. REMOVED LEFT OUTBOARD AFT FLAP PER MM 27-51-39, REPAIRED PER SRM 51-70-10, REINSTALLED LEFT OUTBOARD AFT FLAP PER MM 27-51-39. 2 L 7 2 4F RT A16WE 20080908 SO 2008 9 8 SIM2008F00016 1 20080724 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 928AE 14500911 ON FLIGHT 3567 - CREW REPORTED ALL EMERGENCY LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REPLACED ALL EMERGENCY BATTERIES IAW EMB AMM 33-50-04 OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080908 NE 2008 9 8 Q2SA751005 2 20080727 A 7532 BLEED VALVE BOEING 747 747228F 1384895 NM GE CF6 CF650E2 30018 NE NR 4 ENGINE MALFUNCTIONED A Q2SA O OTHER O OTHER NR NOT REPORTED 1 EA 63 751SA 22678 455280 VERBAL REPORT, AT 5,000FT CLIMB OUT FROM PHIK, NR 4 ENGINE HIGH NACELLE TEMP AND FIRE WARNING INDICATIONS WENT OFF. RE DUCED THRUST FOR 15 SECONDS, WARNING LIGHT WENT OUT. CLOSED BLEED VALVE AND TEMPERATURE DECREASED. AIRCRAFT OPERATED W ITH REDUCED THRUST AND RETURNED TO PHIK. NO FUEL WAS DUMPED. INSPECTION FOUND FAULT ENGINE BLEED AIR PRESSURE RELIEF V ALVE. ALL AD`S ARE CUTTING FOR THIS ENGINE. 2 L 7 4 4F 4 F RT A20WE E23EA 20080908 NM 2008 9 8 QXEA200800668 1 20080620 A 5210 85217555111 SEAL BOMBDR DHC8 DHC8402 1390042 NM AFT PAX DOOR DAMAGED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 411QX 4055 SEA - FLT 2220 - REAR CABIN DOOR HARD TO CLOSE. MAINTENANCE REPLACED THE SEAL IAW 52-12-21-000-802 AND 52-12-21-400-802 . CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 H 7 2 4T RT A13NM 20080908 EA 2008 9 8 QXEA200800713 1 20080710 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 629 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 612QX 10042 PDX-C4 CHECK - CORROSION ON RT INBOARD SEAT TRACK AT STATION 629. REMOVED CORROSION BY BLENDING AFFECTED AREA. MATERIA L REMOVED WITHIN LIMITS OF REO 670-53-00-013. NO CRACKS NOTED. ALODINED SEAT TRACK. (A) 2 L 7 2 4F RT A21EA 20080908 NM 2008 9 8 2008UALA03975 1 20080726 A 2421 GENERATOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LEFT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 668UA 30024 LEFT GENERATOR FAILURE. FLT DIVERTED. 2 L 7 2 4F 4 F RT A1NM E24NE 20080908 NM 2008 9 8 CALA0800752 1 20080729 A 5753 65C2631025 TORQUE TUBE BOEING 737 737524 1384721 NM TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 LEFT INBOARD MIDFLAP PART NUMBER 65C26310-25, S/N BN1835 BOTH INBOARD AND OUTBOARD CARRIAGES AND TORQUE TUBES CORRODED B EYOND LIMITS. PARTS REPLACED: CARRIAGE HALFS 65-52246-15 /-17, CARRIAGE ASSY 65-47856-13 /-14, TORQUE TUBES 65-52211-1 /-2, 69-37206-14. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 CALA0800770 1 20080804 A 5320 6941473US INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 500 S26L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INTERCOSTAL FOUND CRACKED AT FORWARD END BELOW TRANSITION ANGLE AT BODY STATION BS 500 STR 26L. REMOVED CRACKED ANGLE I NTERCOSTAL BS 500 STR 26L. DRILLED NEW ANGLE FOR INSTALL IAW B737 SRM 51-40-02, INSTALLED NEW INTERCOSTAL AT STATION 50 0 STR 26L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 ZZDA2008146 1 20080806 A 5315 9936534321 FLOORBEAM BOEING 717 717200 1383700 NM BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 FLOOR SUPPORT HAS CORROSION AT BS 200 LBL 22 OUT OF LIMITS. REMOVED AND REPLACED SUPPORT AT BS 200 LBL 22 IAW SRM 51-41 -01. 2 L 7 2 4F TR A6WE 20080909 NM 2008 9 9 ZZDA2008148 1 20080806 A 5320 9936534183 FLOOR SUPPORT BOEING 717 717200 1383700 NM BS 157-196 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 FLOOR SUPPORT HAS CORROSION AT BS 157 - BS 196 RBL 36 OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT AT BS 157 - BS 196 RBL 36 IAW B717 SRM 51-41-02. 2 L 7 2 4F TR A6WE 20080909 NM 2008 9 9 CALA0800773 1 20080805 A 5330 2024T3 SKIN BOEING 737 737824 13844BZ NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34222 28931 LEFT ALTERNATE STATIC PORT HAS LIGHTNING STRIKE DAMAGE INSIDE CRITICAL AREA. BURNISHED AREA FOUND TO BE WITHIN LIMITS I AW SRM 53-00-01 REPAIR13 AND SRM 51-10-01. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 2008UALA04075 1 20080730 A 2421 745329F IDG BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LEFT TRIPPED A UALA C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 677UA 30029 L GEN TRIPPED OFF AS POWER BROUGHT UP DURING INITIAL TAKEOFF ROLL. ABORTED TAKEOFF. IDG REPLACED AND TESTED. 2 L 7 2 4F 4 F RT A1NM E24NE 20080909 NM 2008 9 9 ZZDA2008150 1 20080808 A 5330 SKIN BOEING 717 717200 1383700 NM BS 1029 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 939AT 55099 SKIN DAMAGE CAUSED BY BELTLOADER AFT CARGO DOOR NEAR STATION 1029. REPAIRED PER EA-17-53-0120IR SECTION 1 STEPS 1 THRU 7 AND PERFORMED PRESSURE CK PER B717 MM 21-30, NO DEFECTS NOTED. 2 L 7 2 4F TR A6WE 20080909 NM 2008 9 9 2008UALA03856 1 20080712 A 3510 MC1025154 OXYGEN MASK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU 1ST OFFICER'S LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 F/O OXYGEN MASK HAS A LOW CONSTANT FLOW WHEN NOT STOWED IN ITS COMPARTMENT. *S/D* SUSPECT PRE FLIGHT CHECKS. REPLACED FIRST OFFICERS OXYGEN MASK, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 2008UALA03725 1 20080707 A 3610 23417441 PRECOOLER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 1 ENGINE LEAKING A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 794UA 26953 LEFT ENGINE PRECOOLER LEAKING AIR. *S/D* FOUND PRECOOLER LEAKING. REPLACED LEFT ENGINE PRECOOLER ASSEMBLY IAW MM 36-1 1-15, LEAK AND RUN CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 NM 2008 9 9 2008UALA03786 1 20080707 A 3350 767 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 340UA 24244 RIGHT OVERWING EXIT LIGHT INOP. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 2008 9 9 2008UALA03864 4 20080711 A 2565 D31354437 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 SLIDE DAMAGED AT 2L. *S/D* FOUND DAMAGED SLIDE ASSEMBLY. REPLACED SLIDE IAW MM 25-61-35, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 ZZDA2008142 1 20080806 A 5320 9936534Y165 FLOOR SUPPORT BOEING 717 717200 1383700 NM BS 157-190 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 FLOOR SUPPORT HAS CORROSION BS 157-190 RBL 46 OUT OF LIMITS. REPLACED FLOOR SUPPORT AT BS 157 - BS 190 AT RBL 46 PER B7 17 SRM 51-10-04. 2 L 7 2 4F TR A6WE 20080909 NM 2008 9 9 ZZDA2008145 1 20080806 A 5315 993653423 FLOORBEAM BOEING 717 717200 1383700 NM BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 FLOOR SUPPORT HAS CORROSION AT BS 200 & LBL 24 - 60 OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT AT BS 200 & LBL 2 4 - 60 IAW B717 SRM 51-41-05. 2 L 7 2 4F TR A6WE 20080909 NM 2008 9 9 CALA0800767 1 20080804 A 5315 65528941 FLOORBEAM BOEING 737 737724 13844BY NM BS 540 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 21723 28790 LEFT FLOOR SUPPORT CRACKED STATION 540 AT BL-0. REMOVED AND INSTALLED NEW CHANNEL PER SRM 51-40-02, PARAGRAPH 7, ECRA 5 321-01560. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 CALA0800769 1 20080804 A 5311 65C33512 FRAME BOEING 737 737524 1384721 NM BS 440 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16632 27900 FRAME CRACKED STATION 440 AT S-9L. REPAIRED CRACKED FRAME AT STATION 440 STR-9L REF EA 5310-04498 OP 02. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 2008UALA03809 1 20080709 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE RT GENERATOR FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 796UA 26931 ELEC BACKUP GEN R RIGHT BACKUP GENERATOR IS OFF OR HAS FAILED. ADVISORY MSG-2446010 ACTIVE DC MODE MSG-2447010 INACTV D C MODE MSG-2447010 INACTV DC MODE. *S/D* SUSPECT FAULTY IDG AND OR BUG. REPLACED BOTH IDG AND BUG OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 NM 2008 9 9 ZZDA2008138 1 20080806 A 5320 9957828U21 SILL BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 R-1 DOOR SILL WEB HAS CORROSION BEYOND LIMITS. REPLACED CLOSURE RIB IAW B717 SRM 51-41-01. 2 L 7 2 4F TR A6WE 20080909 NM 2008 9 9 2008UALA04034 1 20080729 A 5310 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 813UA 858 BEAM 170 CORRODED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600010 20080206 00010 NM 2008 2 6 USAA920080198 1 20080111 A 5340 6935352507 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 907 S3R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED STRINGER TIE CLIP, BS 907, S3R. REPLACED STRINGER TIE CLIP, BS 907, S3R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008011000083 20080110 00083 NM 2008 1 10 ASAA0852448 1 20080102 A 2130 WARNING SYSTEM BOEING 737 737890 1384527 NM CABIN PRESSURE MALFUNCTIONED A ASAA K NONE N FALSE WARNING UK UNKNOWN 1 NM 02 577AS 35186 UPON POWERING UP COLD PLANE ACFT PRESSURIZATION SYSTEM INDICATED AUTO FAIL & ALTN MODE. WHEN TRANSFERRING FROM APU TO G ROUND PWR AUTO FAIL & ALTN MODE FLASH ON AND GO OUT. COMPLIED WITH FIM 21 31 TASK 801. NO FAULTS FOUND. AIRCRAFT OK F OR SERVICE. 2 L 7 2 4F RT A16WE 2008011000109 20080110 00109 NM 2008 1 10 SWAA080095 1 20080102 A 5330 6545776 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1042, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008011500018 20080115 00018 NM 2008 1 15 2008UALA0037 1 20080102 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 AFT FUSELAGE SKIN CRACKED AT CHEM MILL STEP BS 727E + 3" STR 18L. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011500020 20080115 00020 EU 2008 1 15 2008UALA0039 1 20080103 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN SYSTEM FAILED A UALA K NONE K FLUID LOSS NR NOT REPORTED 1 WP 29 430UA 568 LANDED UNDER AMBER ALERT DUE TO A FAILED GREEN HYDRAULIC SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011500024 20080115 00024 NM 2008 1 15 2008UALA0043 1 20080103 A 3411 STATIC LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 567UA 26673 FOUND STATIC LINE OUT OF POCKET INTERFERING WITH GIRT BAR AND DOOR SEAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008011500027 20080115 00027 NM 2008 1 15 2008UALA0046 1 20080103 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT INOP: DOOR 2L AFT SILL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011500029 20080115 00029 NM 2008 1 15 2008UALA0048 1 20080103 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EEL INOP: SEAT 4A AFT SECTION. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011500030 20080115 00030 NM 2008 1 15 2008UALA0049 1 20080103 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHTS INOP: LT OVERWING FWD 2 ASSY'S. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011500031 20080115 00031 NM 2008 1 15 2008UALA0050 1 20080103 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EEL INOP: ROW 32 LT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011500059 20080115 00059 NE 2008 1 15 UPS08451374 2 20080104 A 7200 ENGINE BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 3 POWER LOSS A IPXA E ENGINE SHUTDOWN R M PARTIAL RPM/PWR LOSS OVER TEMP CR CRUISE 1 SO 01 672UP 20324 INSPECTION TYPE:N/A IFSD - AT FL360 AT CRUISE NR 3 ENG ROLLED BACK, CHECK FUEL PANEL ENG HAD PRESS VIA X FEED. ENG STIL L ROLLING BACK. PLACED IGN TO FLT START, TEMP STARTED TO OVERTEMP. SHUT ENG DOWN. DESCENDED TO 28000. DID INFLIGHT R ESTART AND ENG STARTED. PERFORMED INSPECTING OF NR 3 PER MM 71-00-42 AND 71-00-45 AND MM 71-00-00, 72-00-00. RAN ENG P ER MM 71-00-00, 71-00-46. NO DEFECT NOTED, OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E20EA 2008011500135 20080115 00135 2008 1 15 NSVA20070251 4 20080103 A 3497 WIRE BEECH 1900 1900D 1154162 CE PITOT HEAT CHAFED A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 152MJ UE52 DURING GEAR RETRACTION A BURST OF SPARKS LASTING ABOUT 5 SEC CAME FROM GEAR HANDLE. FOUND LANDING GEAR HANDLE CAN CHAFI NG INTO PITOT HEAT WIRE . REPAIRED AND REROUTED WIRES, PERFORMED GEAR SWING IAW BEECH 1900, 32-30-00, NO DISCREPANCIES NOTED. 2 L 7 2 4T RT A24CE 2008011500139 20080115 00139 EU 2008 1 15 NSVA20070252 1 20080104 A 3397 SOCKET SAAB SF340 340B 7860101 EU CABIN LIGHTS INOPERATIVE A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 27 338CJ 340B338 SMOKE ODOR IN CABIN, LIGHT BULB AT SEAT 10F CHATTERED AND CAUSED SOCKET TO BURN OUT. TROUBLESHOT SMOKE ODOR TO CHATTERI NG LIGHT BULB. REMOVED LIGHT BULB. DEFERRED IAW MEL 33-20-01-01 CAT C. ID 28794 2 L 7 2 4T RT A52EU 2008011500197 20080115 00197 NM 2008 1 15 08FDEA00034 1 20080104 A 5313 ACA37961 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 583FE 48421 LEFT SIDE NOSE LANDING GEAR TRUNNION FITTING FOUND CRACK AT LOWER LONGERON FASTENER HOLE. REPAIR CARRIED OUT AS PER S RM 51-33-01 VOLUME II AND FEDEX EA 1-5310-117251, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008011500198 20080115 00198 NM 2008 1 15 CALA0800004 1 20080104 A 5340 6935352U14 STRINGER CLIP BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 CLIP CRACKED AT STA 616, S6L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008011500199 20080115 00199 NM 2008 1 15 08FDEA00035 1 20080104 A 5420 311N522022 SHIM BOEING 757 7572B7 1384964 NM NR 1 PYLON MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 NR 1 PYLON MID BULKHEAD INBOARD AFT AND FWD LOWER SPAR HAS SHIM MIGRATION. REMOVED FWD AND AFT I/B BOLTS PER STEP 2.1 O F EA F-5450-110803 DATED 11/12/07. REMOVED AND REPLACED FWD I/B SHIM WITH NEW SHIM. REMOVED AND REPLACED AFT I/B SHIM WITH NEW SHIM PER STEPS 2.2 THRU 2.6 OF EA F-5450-110803 DATED 11/12/07. REAMED AFT I/B HOLE TO 0.3902" AND INSTALLED H ARDWARE PER STEP 2.7 OF EA F-5450-110803 DATED 11/12/07. REAMED FWD I/B HOLE TO 0.3925" WHICH IS OUT OF LIMITS. REAMIN G AND HARDWARE INSTALLATION OF FWD I/B HOLE WILL BE ACCOMPLISHED ON NON ROUTINE N00097, WORK ORDER 00037942. 2 L 7 2 4F RT A2NM 2008011500201 20080115 00201 NM 2008 1 15 08FDEA00036 1 20080104 A 5420 311N522022 SHIM BOEING 757 757200 1384950 NM NR 1 PYLON MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 NR 1 PYLON MID BULKHEAD O/B FWD LOWER SPAR HAS SHIM MIGRATION. REMOVED FWD O/B BOLT PER STEP 1.1 OF EA F-5450-110803 DA TED 11/12/07. REMOVED AND REPLACED FWD O/B SHIM WITH NEW SHIM PER STEPS 1.2 THRU 1.6 OF EA F-5450-110803 DATED 11/12/ 07. REAMED FWD O/B HOLE TO 0.3908" AND INSTALLED HARDWARE PER STEP 1.7 OF EA F-5450-110803, DATED 11/12/07. 2 L 7 2 4F RT A2NM 2008011500202 20080115 00202 NM 2008 1 15 08FDEA00037 1 20080105 A 5310 143N832854 CREASE BEAM BOEING BOEING 757 7572B7 1384964 NM BS 680-740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 R2 DOOR, CREASE BEAM BETWEEN STA 680 TO 740, RBL 60, S17, HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51- 10-02. ORIGINAL MATERIAL .100", AFTER REWORK BLENDED AREA IS L= 48", W= 1.5", D= .085", OUT OF LIMITS IAW SRM 53-30-13, FIG 101. REMOVED AND REPLACED CREASE BEAM IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A2NM 2008011500205 20080115 00205 EU 2008 1 15 08FDEA00040 1 20080105 A 5347 Y5382974900000 SEAT TRACK AIRBUS 300 A300B4622 3930401 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 FUS FR 53 SEAT TRACK 3L LOWER EDGE CRACKED, 1" WIDE REMOVED AND REPLACED SEAT TRACK 3L FROM FR 46 TO FR 54 IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008011500224 20080115 00224 NM 2008 1 15 WRLA2008004 1 20080105 A 5320 S292916912000 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 277WA 48743 DURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2007, X= 23.5. REPLACED AFT FLOOR SUPPOR T PER MD-11 SRM VOL.II 51-35-01 FIG.1 REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2008011500239 20080115 00239 NM 2008 1 15 CALA0800012 1 20080104 A 5320 147A8540U8 ANGLE BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 25705 28766 CORROSION ON UPPER INSIDE OF THRESHOLD Z-ANGLE MARKED R2. INSTALLED R2 DOOR CHORD PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008011500243 20080115 00243 NM 2008 1 15 CALA0800014 1 20080108 A 5320 6552878124 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 LEFT Z-ANGLE CORRODED AT STA 947-987. INSTALLED NEW LEFT Z-ANGLE PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008011500244 20080115 00244 NM 2008 1 15 CALA0800015 1 20080109 A 5311 65C25229 BELTFRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 ABB BELTFRAME STA 727D AT S-27R HAS CORROSION. REMOVED DAMAGED SECTION OF SHEAR TIE, FABRICATED AND INSTALLED PER SRM 5 3-00-07 REPAIR NR 4. 2 L 7 2 4F RT A16WE 2008011500285 20080115 00285 NM 2008 1 15 UPS08651369 1 20080103 A 2150 CONTROL VALVE BOEING 767 76734AF 1385212 NM A/C PACK MALFUNCTIONED A IPXA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 01 307UP 27760 INSPECTION TYPE:ETOP DIVERSION - TO SLC DUE TO CABIN PRESSURIZATION PROBLEM. THE RIGHT PACK FAILED WHILE EN ROUTE TO OA K. RECEIVED AN EQUIPMENT OVERHEAT WARNING AND COULD NOT MAINTAIN CABIN PRESSURE. DECLARED EMERGENCY. PER TECH SUPPORT REQUEST, REMOVED AND REPLACED RELAYS K2204 & K2205. AFTER BITE CHECK SHOWED NO FAULTS. TROUBLESHOOTING INDICATED GROU ND PATH INTERRUPTION, REF SSM 21-50-02 SCHEM 1 PAGE 101. REMOVED AND REPLACED LEFT FLOW CONTROL AND SHUTOFF VALVE IAW A MM 21-51-01-4. 2 L 7 2 4F RT A1NM 2008011500295 20080115 00295 NM 2008 1 15 ASAA0852456 1 20080107 A 4940 28B5457 STARTER GEN BOEING 737 737890 1384527 NM APU FAULTY A ASAA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 02 558AS 35177 APU "MAINT" LIGHT ILLUMINATED. VERIFIED FAULT CODE 49 41244. ACCOMPLISHED FIM 49 40 TASKS 805 806. REPLACED STARTER G ENERATOR (REF MM 49 41 21 PG 401). GROUND VERIFICATION GOOD. 2 L 7 2 4F RT A16WE 2008011100070 20080111 00070 NM 2008 1 11 2008UALA0027 1 20080101 A 2700 WARNING SYSTEM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 779UA 26941 THE "FLIGHT CONTROLS" EICAS APPEARED AFTER ENGINE START. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008011100076 20080111 00076 NM 2008 1 11 2008UALA0031 1 20080101 A 3350 LAMP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN INOPERATIVE A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 813UA 858 EPSU EXT LOAD EMER RIGHT MESSAGE ON EMERGENCY LIGHT TEST PANEL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011100099 20080111 00099 NM 2008 1 11 SWAA080100 1 20080103 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED C1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008011100175 20080111 00175 NM 2008 1 11 SWAA080131 1 20080104 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731C, STR 4L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011100197 20080111 00197 NM 2008 1 11 SWAA080155 1 20080106 A 5311 6546554 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011100198 20080111 00198 NM 2008 1 11 SWAA080156 1 20080106 A 5311 6546595 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011100247 20080111 00247 EA 2008 1 11 COMA0860025 1 20080102 A 2752 853D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 SO 01 685BR 7712 FLIGHT 5681 - RECEIVED FLAP FAIL CAUTION MESSAGE. DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED CVG WITHOUT INCIDEN T. REPLACED RIGHT SIDE NR 3 FLAP ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100256 20080111 00256 EA 2008 1 11 COMA0860034 1 20080103 A 2752 852D10021 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 924CA 4109 7026 FLIGHT 5483 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED RIGHT FLAP ACTUATOR NR 2. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100257 20080111 00257 EA 2008 1 11 COMA0860035 1 20080103 A 2752 853D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 924CA 9521 7026 FLIGHT 5483 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED THE RIGHT FLAP ACTUATO R NR 3. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100258 20080111 00258 EA 2008 1 11 COMA0860036 1 20080103 A 2752 854D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 924CA 564 7026 FLIGHT 5483 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED RIGHT FLAP ACTUATOR NR 4. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100259 20080111 00259 EA 2008 1 11 COMA0860037 1 20080103 A 2750 1104SD100201 FLEX DRIVE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP DAMAGED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 924CA 7026 FLIGHT 5483 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEFT NR 2 FLEX DRIVE S HAFT. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100280 20080111 00280 NE 2008 1 11 HALA0800007 2 20080103 A 7397 CONNECTOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE FUEL SYSTEM DIRTY A HALA K NONE O OTHER CR CRUISE 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM, LEFT ENG FUEL FLOW IS ZERO FUEL USED ALSO LOW. ALSO INTERMITTENT. CLEANED AND TIGHTENED PYLO N CONNECTOR D4210P REF WDM 73-31-11 PP TWO. RAN ENG ALL INDICATIONS NML. ACCOMPLISHED FIM 28-41-00 FIG 107, NO FAULTS NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008011400006 20080114 00006 CE 2008 1 14 DXTA200802757 1 20080109 A 3230 LANDING GEAR CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE INOPERATIVE E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 837QS 5600685 LANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF. PLACED AIRCRAFT ON JACKS. INSTALLED ROBO MULE TO RIGHT ENGINE TO PERFO RMED LANDING GEAR OPERATIONAL CHECKS. INSPECTED ALL LANDING GEAR ELECTRICAL CONNECTORS AND LANDING GEAR CONTROL VALVE. SYSTEM CHECKED GOOD.CYCLED THE LANDING GEAR SEVERAL TIMES. OPERATIONAL OF LANDING GEAR SYSTEM CHECKED GOOD. DOWN JACK ED AIRCRAFT AND REMOVED ROBO MULE. LEAK CHECK RIGHT ENGINE CHECKED GOOD. IAW CH 32-30-00 OF THE CITATION 560 MM. 2 L 7 2 4F 4 F RT A22CE E00053EN 2008011400007 20080114 00007 CE 2008 1 14 DXTA200802756 1 20080109 A 3260 SPRING RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP DOOR HOOK LACK OF LUBE E DXTA O OTHER N FALSE WARNING CL CLIMB 1 GL 07 870QS 258732 RT MAIN GEAR RED ANNUNCIATOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION AFTER TAKEOFF. REMOVED, CLEANED & LUBRIC ATED SPRING MECHANISM FOR RT DOOR HOOK., TESTED SPRING LOAD, INSTALLED ASSY & PERFORMED SATISFACTORY GEAR SWING, ALL TES TS GOOD. IAW HAWKER 800XP MM 32-30-00 &32-30-35. 2 L 7 2 4F 4 F RT A3EU E6WE 2008011400028 20080114 00028 NE 2008 1 14 TRBA2008003 2 20080105 A 7200 PW127 ENGINE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RIGHT FAILED A TRBA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 410AT 410 RT ENG NP WENT TO 108 PERCENT ENGINE WAS SHUT DOWN AND CAPTAIN DECLARED EMERGENCY. REMOVED AND REPLACED RT ENGINE IAW W ORK CARD 055006-CS-20000-001R1. PENDING MFG TEAR DOWN REPORT. 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400046 20080114 00046 CE 2008 1 14 DXTA200802749 1 20080105 A 2722 ACTUATOR CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE RUDDER MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 338QS 6800011 RUDDER BIAS FAULT CAS MESSAGE CAME ON AFTER ROTATION. R & R ACTUATOR NO FAULTS FOUND ON INSPECTION OF RUDDER BIAS COMPO NENTS. C/W SATISFACTORY OPERATIONAL CHECKS IAW MM 27-20-00 & FT-680-0022. 2 L 7 2 4F 4 F RC T00012WI E35NE 2008011400059 20080114 00059 CE 2008 1 14 HSYA20080102 1 20080106 A 5531 11463000053 RIB BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE VERTICAL STAB CRACKED E HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 101UE 27531 UC101 DURING SCHEDULED MX - SIM TASK 55-30-00 (1200 FLT HR/ 24 MO) REF. B1900 STRUCTURAL INSPECTION MANUAL, MX PERFORMED A VIS UAL INSPECTION OF THE VERTICAL STABILIZER STRUCTURAL COMPONENTS AND FOUND RIB, AT CANTED STAB. STA. 69.184, CRACKED ON T HE RT SIDE FLANGE AT THE 39.5 PERCENT CHORD REF. LINE AREA. MX INSTALLED REPAIR DOUBLERS ON THE UPPER AND LOWER PORTIONS OF THE DAMAGED AREA IAW THE MFG SRM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 T RT A24CE E4EA 2008011400076 20080114 00076 EU 2008 1 14 BAQA20080001 1 20080103 A 2597 LEAD AGUSTA A109 A109 0260109 EU SHORTED E BAQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 03 2MF 7277 PRIOR TO AIRCRAFT START WHEN THE BATTERY BUSS TIE SWITCHES WERE TURNED ON, THE CREW DETECTED AN ELECTRICAL BURNING ODOR IN THE CABIN. POWER WAS SHUTOFF AND THE MECHANIC INSPECTED THE AIRCRAFT AND FOUND THE PORTABLE SUCTION PUMP POWER LEAD S HORTED OUT AND GFI PLUG HAD HEAT DAMAGE. REPLACED SUCTION PUMP POWER LEAD WITH SERVICEABLE LEAD AND THE GFI PLUG WITH A NEW GFI PLUG P/N 7599-W. OPERATIONAL CHECK OF THE SYSTEMS WERE PERFORMED AND NO DEFECTS WERE NOTED. 1 G 7 2 3U H7EU 2008011500017 20080115 00017 NM 2008 1 15 2008UALA0036 1 20080102 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FUSELAGE EXTERIOR SKIN CRACKED AT BS 520 STR 12R. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011500200 20080115 00200 NM 2008 1 15 CALA0800005 1 20080105 A 5310 BAC15171470 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FWD ENTRY FRAME STA 310 L ABOVE L-1 DOOR CUTOUT CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-70-11 FIG 1. 2 L 7 2 4F RT A16WE 2008011500212 20080115 00212 NM 2008 1 15 CALA0800006 1 20080107 A 2530 8201110000A OVEN BOEING 777 777224 1385225 NM AFT GALLEY MALFUNCTIONED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 69020 398 398 31687 AFT GALLEY OVEN 810/809 STARTED TO SMOKE. PULLED C/B FOR OVEN 708-709-809-810 TO ISOLATE. SMOKE STOPPED. LEFT C/BS OU T FOR DURATION OF FLIGHT. SOURCE OF SMOKE/ODOR FOUND OVEN 809 FAN INOP. REMOVED OVEN 810/809. 2 L 7 2 4F RT T00001SE 2008011500218 20080115 00218 NM 2008 1 15 WRLA2008002 1 20080104 A 5730 ACCESS PANEL DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE RT WING CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 277WA 48743 DURING C-CHECK INSPECTION FOUND RT WING OUTBOARD SLAT DRIVE MECHANISM ACCESS PANEL SKIN CRACKED. REPAIRED RT WING ACTU ATOR ACCESS DOOR OUTER SKIN AT XOS STA 490.85 PER EGAT EI NR W2008A57B-022. 2 L 7 3 4F 4 F RT A22WE E24NE 2008011500248 20080115 00248 NM 2008 1 15 CALA0800017 1 20080110 A 3610 BACC10BN500LR CLAMP BOEING 737 7373T0 1384582 NM MLG WW LOOSE A CALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 17328 23458 AT FL340 APPROX 70 MILES SOUTH OF DFW GOT CABIN WARNING HORN, SAW CABIN AT 10,500 WENT TO STBY NO HELP. EMERGENCY DESCE NT TO LANDING IN DFW DUE TIME CONSTRAINTS AND TRYING TO KEEP CABIN BELOW 14000. LANDED SAFELY IN DFW. FOUND LEAK IN KE EL BEAM AREA (WHEEL WELL AFT WALL). APU PNEUMATIC DUCT WHICH HOLD SURROUNDING PRESSURE BOOT SLIPPED OFF. REALIGNED AFT CARGO FWD BULKHEAD TO DUCT BOOT AND REINSTALLED CLAMP PER MM 36-19-15, 21-31-25, 21-31-21 AND 21-31-11. 2 L 7 2 4F RT A16WE 20080908 NM 2008 9 8 2008UALA03909 1 20080717 A 5300 UNKNOWN BOEING 737 737322 1384676 NM AIRFRAME VIBRATION A UALA O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 29 303UA 23644 VIBRATION AT SLOWER SPEEDS, GREATER INTENSITY DURING MANUVERING AT HIGHER ANGLE. WENT AWAY AT HIGHER SPEED, VIBRATION R ETURNED DESCENDING FL 320-2 70 WITH SPEED INCREASING TO 300. LEFT TURN SLOWING TO 210 NOTICABLE VIBRATION. VIBRATION D IMINISHED AT FLAP 5. DID NOT FEEL VIBRATION AFTER GEAR EXTENSION. 2 L 7 2 4F RT A16WE 20080908 NM 2008 9 8 2008UALA03639 1 20080628 A 3350 GE209 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY LIGHT INOP: ROW 46 RT CEILING. FOUND BURNED OUT BULB. REPLACED BULB, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03642 1 20080628 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 55-61ABC DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EEL LIGHTS INOP AT SEAT 55 ABC TO 61 ABC. FOUND BROKEN LIGHT ASSEMBLY. SPLICED LIGHT SECTION, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 EA 2008 9 8 TRAX200800856 1 20080630 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 861AS 7445 FS 280 CLIPS ARE CRACKED AT RBL 9. REMOVED AND REPLACED I/B CLIP AT RBL 9 IAW CRJ200 REO 601R-53-11-136. FABRICATED O/ B CLIP FROM 2024-T3 .050" BATCH 845191 SAME AS 601R31113-58 AS INDICATED IN REO 601R-53-11-136 EXCEPT AS NEEDED TO CONFO RM TO EXISTING REPAIR DOUBLER CONTOUR. JOB COMPLETE RAP 7025969. (B) 2 L 7 2 4F RT A21EA 20080908 EA 2008 9 8 TRAX200800702 1 20080529 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 724EV 10138 GALLEY/ENTRANCE HAS SEVERAL EMERGENCY LIGHT BULBS OUT. REMOVED AND REPLACED GALLEY/ENTRANCE FLOOR LEVEL EMERGENCY FLOOD LIGHT BULBS. OPS CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080908 NM 2008 9 8 USAA920081343 1 20080708 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT -MAJOR REPAIR- Q3 CHECK- LEVEL 2 CORROSION ON CABIN FLOORBEAM T-CAP, BS 312, BL 0. REPLACED CABIN FLOORBEAM T-CAP, BS 312, BL 0 IAW B737 SRM 53-10-51. (B) 2 L 7 2 4F RT A16WE 20080908 WP 2008 9 8 WX02008F00000 1 20080701 A 2612 5938323503 FIRE LOOP DOUG DC9 DC982 3022082 WP LT NACELLE FAILED A WX0A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 19 887GA 49932 FLIGHT CREW PERSONNEL REPORTED ON THE INITIAL CLIMBOUT OF FLIGHT 883-1 FROM PIE, THE FIRE DETECTOR HANDLE AND LOOP "B" I LLUMINATED ON THE LEFT ENGINE. THE AIRCRAFT RETURNED TO ST. PETERSBURG, FL AND LANDED WITHOUT INCIDENT. MAINTENANCE DE PARTMENT PERSONNEL PERFORMED A VISUAL INSPECTION OF THE LT ENGINE FIRE DETECTION "B" SYSTEM AND DETERMINED A FIRE LOOP D ETECTOR WAS DEFECTIVE. THE "B" LOOP WAS DEFERRED IAW ALLEGIANT AIR MEL PROCEDURES AND THE AIRCRAFT WAS RETURNED TO SERV ICE. (A) 2 L 7 2 4F A6WE 20080908 NM 2008 9 8 2008UALA03735 1 20080706 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 824UA 965 CREW O2 PRESSURE IS SHOWING AT 50 PSI. SERVICED BOTTLE TO 1600 PSI AND CHECKED ALL CREW MASKS FOR LEAKS. VERIFIED NO L EAKS AND AFTER 1 HR BOTTLE PRESSURE STILL AT 1600 PSI, ACFT IS OK FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080908 CE 2008 9 8 DJFA2008062 1 20080706 A 2130 CABIN PRESSURE BEECH MU300 400A 1155402 CE FAILED E DJFA G O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 EA 23 794TA RK282 TEMPORARILY LOST PRESSURIZATION AT FL300. OXYGEN MASKS DROPPED. EMERGENCY WAS DECLARED. AIRCRAFT LANDED SAFELY. (A) 2 H 7 2 4F RT A16SW 20080908 NM 2008 9 8 2008UALA03825 1 20080710 A 3510 RCF6708 REGULATOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW O2 LEAKING A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 854UA 1731 OXYGEN LOST PSI INFLIGHT. FOUND LEAKING O2 REGULATOR. REPLACED O2 REGULATOR, SERVICED CREW O2 TO FULL AND LEAK CHECKED , ALL NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080908 NM 2008 9 8 CALA0800749 1 20080725 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM BS 360 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 LEFT SIDE STATION 360 FRAME CRACKED BETWEEN S-8 AND S-9 LT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REPAIRED CRACKE D FRAME AT BODY STATION 360 BETWEEN S-8 AND S-9 LEFT PER PACE EA647-53-001CAL AND EC/RA 5310-04812. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 CALA0800754 1 20080803 A 3350 276005 FUSE BOEING 737 737924 13848A1 NM BATTERY CHARGER BLOWN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 31412 30129 EMERGENCY EXTERIOR LIGHTS AT RIGHT WING AFT DID NOT ILLUMINATE ON TEST. REPLACED FUSE ON BATTERY PACK. OPERATION CHECK NORMAL PER AMM 33-51-06, REPLACE BATTERY PER AMM 33-51-06. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 CALA0800757 1 20080801 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM BS 400 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16632 27900 FRAME CRACKED STATION 400 AT S-9R. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLERS REF EA 5310-04498. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 CALA0800759 1 20080801 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM BS 440 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16632 27900 FRAME CRACKED STATION 440 AT S-9R. REPAIRED FRAME REF EA 5310-04498 OP 2. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 2008UALA03844 1 20080707 A 2421 BEARING BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 GENERATOR FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 228UA 30556 RIGHT BUG INOP. *S/D* SUSPECT FAULTY BEARING. REPLACED BACK UP GENERATOR, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 NM 2008 9 9 2008UALA03993 1 20080728 A 3150 WARNING LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 351UA 24319 LEFT EQUIP COOLING FAN LIGHT ILLUMINATED. RTFL. REPLACED BOTH SUPPLY FANS, RELAYS R347 & R401, AIR RESTRICTOR, LOW FLO W SENSOR, CLEANED CHECK VALVES. RAN SYSTEM FOR 3 HOURS, NO FAULTS. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 2008UALA04076 1 20080731 A 5310 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 813UA 858 BEAM 155 CORRODED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA03872 1 20080714 A 2560 MXP21000 SMOKE GOGGLES BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU 1ST OBSERVER'S DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 930UA 26655 SMOKE GOGGLES IN FLT DECK AT 1ST OBSERVER POSITION HAS A TORN FACE SEAL. *S/D* SUSPECT PRE FLIGHT CHECKS. REPLACED SMO KE GOGGLES. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 2008UALA03737 1 20080704 A 3510 38001614 LINE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU OXYGEN MASK LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. *S/D* FOUND CAPTAINS SUPPLY FLEX LINE TO MASK BOX LEAKING . REPLACED FLEX LINE, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 2008UALA03732 1 20080706 A 2560 3F17645501 GIRT BAR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 371UA 24540 DOOR 1L SLIDE PACK HAS FALLEN OUT. *S/D* SUSPECT IMPROPERLY INSTALLED. ADJUSTED GIRT BAR, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 2008UALA03955 1 20080723 A 8011 8110503 STARTER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 ENGINE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 213UA 30219 LEFT ENGINE WILL NOT START. *S/D* SUSPECT FAULTY STARTER. REPLACED STARTER IAW MM 80-11-01, OP CHECKED GOOD. AC OK F OR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 NE 2008 9 9 ZZDA2008134 2 20080803 A 7261 OIL SYSTEM BOEING 737 7377BD 1384511 NM CFMINT CFM567 CFM567B2US 13802 NE LT ENGINE LOW A ZZDA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 37 315AT 35788 OBSERVED LOW OIL QUANTITY IN LEFT ENGINE DURING CLIMBOUT. INDICATION AT 3 UNITS. ACCOMPLISHED FIM 79-05 TASK 809. INS PECTED ENG IAW B737 AMM 79-00-00 PG 601. SERVICED ENG OILS IAW B737 AMM 12-13-11. SECURED ACCESS OKAY FOR CONTINUED SE RVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 20080909 NM 2008 9 9 CALA0800768 1 20080804 A 5311 6546525 FRAME BOEING 737 737524 1384721 NM BS 380 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16632 27900 FRAME CRACKED STATION 380 AT S-9R. REPAIRED FRAME REF EA 5310-04498 OP 2. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 ZZDA2008137 1 20080806 A 5320 993653519 FLOOR SUPPORT BOEING 717 717200 1383700 NM BS 200-256 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 FLOOR SUPPORT HAS CORROSION AT STA 200-256 LBL 15 - OUT OF LIMITS. REPLACED FLOOR SUPPORT AT STA 200-256 LBL 15 IAW B71 7 SRM 51-41-02 & -05. 2 L 7 2 4F TR A6WE 20080909 NM 2008 9 9 ZZDA2008139 1 20080806 A 5320 9936534 FLOOR SUPPORT BOEING 717 717200 1383700 NM BS 160-258 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 FWD CABIN FLOOR SUPPORT CORRODED AT LBL 14 FROM BODY STA 160 TO BS 258 - OUT OF LIMITS. REPLACED FLOOR SUPPORT FROM BS 160 - 258 - LBL 14 PER B717 SRM 51-41-01. 2 L 7 2 4F TR A6WE 20080909 NM 2008 9 9 ZZDA2008140 1 20080806 A 5320 SE095300344 FLOOR SUPPORT BOEING 717 717200 1383700 NM BS 160-258 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 FWD CABIN FLOOR SUPPORT ANGLE IS CORRODED AT RBL 7 BS 160 TO BS 258. REPLACED FLOOR SUPPORT FROM BS 160 TO BS 258 LBL 7 IAW B717 SRM 51-41-01. 2 L 7 2 4F TR A6WE 20080909 NM 2008 9 9 ZZDA2008141 1 20080806 A 5315 993653415 FLOORBEAM BOEING 717 717200 1383700 NM BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 FLOOR SUPPORT HAS CORROSION AT STA 200 RBL 48-57 - OUT OF LIMITS. REPLACED FLOOR SUPPORT RBL 48 TO RBL 57 AT STA BS 200 PER B717 SRM 51-10-04. 2 L 7 2 4F TR A6WE 20080909 NM 2008 9 9 2008UALA01381 1 20080312 A 2450 3B391C CONTROL UNIT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE ELECTRICAL LOAD FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 670UA 29240 WORKING CHRONIC GALLEY PWR LOAD SHED. *S/D* AFTER EXTENSIVE TROUBLESHOOTING FOUND FAULTY ELECTRICAL LOAD CONTROL UNIT. REPLACED ELCU (M225) FWD GALLEY, PER MM25-31-03, OPS CHECKS NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080909 NM 2008 9 9 2008UALA04032 1 20080728 A 5310 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 813UA 858 BEAM 95 CORRODED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA04033 1 20080729 A 5310 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 813UA 858 BEAM 195 CORRODED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011000089 20080110 00089 NM 2008 1 10 SWAA080062 1 20080102 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011000103 20080110 00103 NM 2008 1 10 SWAA080086 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011500013 20080115 00013 NM 2008 1 15 2008UALA0033 1 20080102 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 UPPER EXTERNAL FUSELAGE SKIN IS WORN IN SEVERAL AREAS UNDERNEATH DORSAL FIN ON LT AND RT SIDE FROM STA 860-907. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011500025 20080115 00025 NM 2008 1 15 2008UALA0044 1 20080102 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 652UA 25390 AFT LEFT AND RIGHT LAV EEL LIGHT BARS ARE INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008011500026 20080115 00026 NM 2008 1 15 2008UALA0045 1 20080102 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 780UA 26944 EEL LIGHTS AT SEATS 12D AND 15D ARE BROKEN. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008011500060 20080115 00060 NM 2008 1 15 UPS08551366 1 20080102 A 3610 BLEED AIR SYS BOEING 757 75724APF 1384969 NM MLG WW LEAKING A IPXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 420UP 23907 INSPECTION TYPE:N/A DIVERSION - SHORTLY AFTER LVL OFF AT 370 MSTR WARNING BELL SOUNDED & EICAS W/W FIRE ILLUMINATED. LO WERED & DESCENDED IAW QRH. WHEEL WELL FIRE INDICATION STAYED ON FOR 8 MINUTES. AFTER INDICATION WENT OUT DUCT LEAK LP STATUS MSG ILLUMINATED. PERFORMED GENERAL VISUAL INSPECTION IN R/L WHEEL WELL AND L/R A/C BAYS AND BLEED AIR LEAKS FOUN D. ACCOMPLISHED FIM 26-18-00 FIG 103 AND FOUND CODE 84, ERASED CODE AND SYSTEM TEST NORMAL. 2 L 7 2 4F RT A2NM 2008011500063 20080115 00063 WP 2008 1 15 UPS08851362 1 20080102 A 2560 ATTACH FITTING DOUG DC8 DC873F 302199F WP GIRT BAR MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:N/A AFT GIRT BAR FITTING FOR ESCAPE SLIDE MISSING. DEFERRED ESCAPE SLIDE IAW DC8 MEL 52-7-4. D366115 AS SIGNED. LOCATED AND INSTALLED MISSING ATTACH FITTING AND HARDWARE. OPS CHECK OK. THIS CLEARS DMI. 2 L 7 4 4F RT 4A25 2008011500103 20080115 00103 NM 2008 1 15 DHLA200800002 1 20080105 A 5270 DOOR BOEING 727 7272Q9 138448M NM MAIN PAX OUT OF RIG A DHLA O OTHER N FALSE WARNING LD LANDING 1 GL 05 741DH 21931 FLT 505, ON LANDING ROLLOUT, FWD ENTRY LIGHT ON SO'S LIGHTS PANEL ILLUMINATED. RIG FRONT ENTRY DOOR PER M/M 52-11-01, O PS CHECK GOOD. ACFT GROUNDED. 2 L 7 3 4F RT A3WE 2008011500203 20080115 00203 EU 2008 1 15 08FDEA00038 1 20080105 A 5347 Y5382974600000 SEAT TRACK AIRBUS 300 A300B4622 3930401 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 LOWER FUSELAGE FR 53 SEAT TRACK 2L, LOWER EDGE IS CRACKED, 1" WIDE REMOVED AND REPLACED SEAT TRACK 2L FR 46 TO FR 54 IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008011500217 20080115 00217 NM 2008 1 15 CALA0800009 1 20080108 A 5347 BAC1520792 SEAT TRACK BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16632 27900 SURFACE CORROSION ON LEFT I/B SEAT TRACK UPPER FLANGE NEXT TO LAV MOUNT STA 916. INSTALLED NEW SEAT TRACK PER SRM 53-00 -52 FIG 101. 2 L 7 2 4F RT A16WE 2008011500227 20080115 00227 NM 2008 1 15 WRLA2008006 1 20080105 A 5320 S3932107012400 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 277WA 48743 DURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2007, X= -27.5. REPLACED AFT FUSELAGE FL OOR SUPPORT PER MD-11 VOL.II 51-35-01 FIG.1 REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2008011500228 20080115 00228 NM 2008 1 15 WRLA2008007 1 20080106 A 5320 S393210712400 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 277WA 48743 DURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2000, X= -56.65. REPLACED AFT FUSELAGE F LOOR SUPPORT PER MD-11 SRM VOL.II 51-35-01 FIG.1 REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2008011500230 20080115 00230 NM 2008 1 15 CALA0800011 1 20080105 A 5315 BAC1518399 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 STA 986.5 FLOORBEAM CORRODED RBL 22 TO LBL 9. REMOVED AND REPLACED UPPER T-CHORD PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008011500250 20080115 00250 NM 2008 1 15 CALA0800019 1 20080111 A 5313 65516981 STRINGER SPLICE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 STRINGER SPLICE IS CRACKED AT STA 907 STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008011500251 20080115 00251 NM 2008 1 15 CALA0800020 1 20080108 A 5320 BAC1518399 BEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 STA 947 BEAM CORRODED AROUND SCREW HOLES LBL 10 TO RBL 5. REPAIRED PER SRM 53-00-51. 2 L 7 2 4F RT A16WE 2008011500252 20080115 00252 NM 2008 1 15 CALA0800021 1 20080113 A 5313 6948948501 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 CORROSION IN CENTER OF STRINGER HAT SECTION STR 29RT APPROX STA 350 JUST BELOW FORWARDS OUTFLOW VALVE DUCT. REMOVED AND REINSTALLED STR CLIP AND SHIMS PER SRM 51-40-02. PICKER UP HOLES IN STR CAP REF 51-40-02. APPLIED EDGE SEAL REF AMM 5 1-31-00 APPLIED C.I.C. REF 51-20-01. 2 L 7 2 4F RT A16WE 2008011500284 20080115 00284 NM 2008 1 15 UPS08551377 1 20080105 A 2612 355782400 FIRE DETECTOR BOEING 757 75724APF 1384969 NM MLG WW SHORTED A IPXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 420UP 23907 INSPECTION TYPE:N/A WHEEL WELL FIRE INDICATION AT 30,000, GEAR EXTENDED AS PER QRH. FIRE INDICATION EXTINGUISHED AT APP ROX 10 MINS, DUCT LEAK LP DISPLAYED ON STATUS PAGE. INSPECTED DUCTING IN R/W/W, NO LEAKS FOUND. DUE TO PREVIOUS WRITE UP - REPLACED ALL 4 W/W ELEMENTS PER MM 26-17-01-4. REPLACED W/W FIRE DETEC T PWR SUPPLY CARD PER MM 26-10-01-4. REPLA CED FIRE/OVHT TEST PANEL PER MM 26-11-02-4. W/W FIRE DET SYS GOOD PER MM 26-17-00-5. 2 L 7 2 4F RT A2NM 2008011100095 20080111 00095 NM 2008 1 11 SWAA080114 1 20080103 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 15R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008011100111 20080111 00111 NM 2008 1 11 SWAA080115 1 20080103 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011100119 20080111 00119 NM 2008 1 11 SWAA080106 1 20080103 A 3230 6962289 ROLLER BOEING 737 7373H4 1384600 NM NLG W/W WORN A SWAA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 29 605SW 27956 MANUAL GEAR EXTENSION REQUIRED. ALL GEAR SAFE AND UNSAFE LIGHTS ILLUMINATED. FERRIED AIRCRAFT TO DAL FOR MAINTENANCE. FOUND LANDING CABLE OUT OF RIG, RIG CABLE PER MM. REMOVED AND REPLACED MANUAL RELEASE MECHANISM ROLLER ON NOSE GEAR PE R MM. 2 L 7 2 4F RT A16WE 2008011100125 20080111 00125 NM 2008 1 11 SWAA080117 1 20080101 A 3230 71784 TRANSFER VALVE BOEING 737 7377H4 1384404 NM MLG W/W FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 29 713SW 27847 AIR TURNBACK. DEPARTING PIT NLG WOULD NOT RETRACT. FERRIED TO MDW FOR MAINTENANCE. FOUND FAULTY NLG DOWNLOCK ACTUATOR AND NO POWER FROM PSEU. REMOVED AND REPLACED DOWNLOCK ACTUATOR PER MM. REMOVED AND REPLACED PSEU PER MM. REMOVED AND REPLACED GEAR TRANSFER VALVE PER MM. 2 L 7 2 4F RT A16WE 2008011100151 20080111 00151 2008 1 11 ZZDA2008003 4 20080104 A 2565 29982225 SLIDE BOEING 717 717200 1383700 NM R1 DOOR FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 991AT 55135 R-1 DOOR SLIDE FAILED TO DEPLOY DURING MAINT CHECK. REPLACED DOOR SLIDE ASSY. 2 L 7 2 4F TR A6WE 2008011100163 20080111 00163 NM 2008 1 11 SWAA080123 1 20080106 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011100219 20080111 00219 EA 2008 1 11 COMA0860015 1 20080102 A 2752 854D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 926CA 11844 7027 FLIGHT 5004 - FLAP FAIL CAUTION MESSAGE RECEIVED. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED RIGHT SIDE NR 4 FLAP ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100254 20080111 00254 EA 2008 1 11 COMA0860032 1 20080103 A 2752 854D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 924CA 2027 7026 FLIGHT 5483 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEFT FLAP ACTUATOR NR 4. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100255 20080111 00255 EA 2008 1 11 COMA0860033 1 20080103 A 2752 852D10021 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 924CA 4109 7026 FLIGHT 5483 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED RIGHT FLAP ACTUATOR NR 1. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100283 20080111 00283 NM 2008 1 11 08FDEA00029 1 20080103 A 5310 ACA00513 DOOR FRAME DOUG MD11 MD11F 3023600 NM BS 547 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 583FE 48421 NR 2 AIRCON PACK DOOR CUTOUT BS 547, S-33L FOUND FRAME CRACKED. REPAIR CARRIED OUT AS PER SRM 53-30-00 FIGURE 1. REPAI R CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008011100292 20080111 00292 EU 2008 1 11 QMLA010108001 1 20080101 A 2830 CANISTER SNIAS 350 AS350B3 8680954 EU TMECA ARRIUS ARRIUS2B1 NE FUEL PURGE FULL E QMLA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 397LG 3268 AFTER DEPARTURE FROM BASE HOSPITAL AND ENROUTE TO SENDING HOSPITAL, PILOT NOTICED A PERSISTENT FUEL ODOR IN THE CABIN. THE PILOT THEN ABORTED THE MISSION AND RETURNED TO BASE MAINTENANCE HELIPAD. TROUBLESHOT THE PROBLEM. FOUND THE FUEL PURGE CANISTER FULL OF FUEL, THE MECHANIC DRAINED THE CANISTER. CONDUCTED OPERATIONAL CHECK FLIGHT AND RETURNED AIRCRAF T TO SERVICE. 1 G 7 1 3U 3 U H9EU E34NE 2008011400008 20080114 00008 CE 2008 1 14 DXTA200802755 1 20080108 A 2731 ACTUATOR CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE STAB TRIM OUT OF ADJUST E DXTA O OTHER O OTHER CR CRUISE 1 GL 07 301QS 6800010 AUTOPILOT DISCONNECTS AND AUTOPILOT (FAIL A CAS) MSG COMES ON ONCE THE NOSEDOWN TRIM (PRIMARY) SETS TO +1.2. C/W HORIZ ONTAL STABILIZER TRIM ADJUSTMENT AND TEST IAW CE680 M/M 27-40-00. ADJUSTED ACTUATOR AS REQUIRED. TRAVEL AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RC T00012WI E35NE 2008011400015 20080114 00015 NE 2008 1 14 COEA0801819 2 20080102 A 7532 32149582 BLEED VALVE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE NR 1 ENGINE FAILED A COEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 13 819FX 300 359 FLIGHT NR 8091 ON 1/2/08, DURING TAXI TO RUNWAY, THE NR 1 ENGINE BLEED FAULTED. CREW ATTEMPTED TO RESET WITHOUT SUCCESS . AIRCRAFT RETURNED SAFELY TO BLOCKS. REPLACED NR 1 ENGINE HIGH PRESSURE BLEED AIR SHUTOFF VALVE. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400043 20080114 00043 NE 2008 1 14 TRBA2008103 2 20080105 A 7200 PW127 ENGINE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RT ENGINE FAILED A TRBA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 410AT 410 RT ENG NP WENT TO 108 PERCENT ENGINE WAS SHUTDOWN AND CAPTAIN DECLARED EMERGENCY. REMOVED AND REPLACED RT ENGINE IN PRO GRESS. 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400078 20080114 00078 EU 2008 1 14 HSYA20080101 1 20080101 A 2910 SD3730313XA LINE STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA HYDRAULIC SYS RUPTURED E HSYA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 05 330SB 25109 SH3013 JUST AFTER TAKEOFF, THE CREW REPORTED THAT THE NOSE LANDING GEAR WOULD NOT LOCK IN THE UP POSITION. SHORTLY AFTERWARDS B OTH OF THE HYDRAULIC SYSTEM LOW PRESSURE LIGHTS ILLUMINATED. THE CREW DECLARED AN EMERGENCY AND PERFORMED THE ABNORMAL P ROCEDURES LIST FOR HYDRAULIC FAILURE. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITH OUT FURTHER INCIDENT. MX FOUND THE NOSE LANDING GEAR UP HYDRAULIC ACTUATOR HYDRAULIC FLEX LINE BROKEN. MX REMOVED AND REPLACED THE HYDRAULIC LINE. AS A PRECAUTION MX REMOVED AND REPLACED BOTH LT AND RT ENGINE DRIVEN HYDRAULIC PUMPS BECAUSE OF POSSIBLE CAVITATIONS AND SER VICED THE HYDRAULIC SYSTEM. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T 4 T A41EU E4EA 2008011400090 20080114 00090 SW 2008 1 14 DUFA20080001 1 20080103 A 2613 434422122 OVERHEAT SENSOR SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE3311U 01514 WP LT NACELLE DEFECTIVE E DUFA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 27 159MC AC728B WHILE ON CLIMB OUT, THE PILOT NOTICED THAT THE LT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWING PROCEDURE, THE LT GENERATOR WAS SHUTDOWN, BLEED AIR TURNED OFF AND THE LANDING GEAR EXTENDED. AFTER 3 MINUTES THE LIGHT WAS STILL ILLUMINATED AND P ROCEDURES CALL OUT FOR ENGINE SHUTDOWN. SHORTLY AFTER ENGINE SHUTDOWN THE LIGHT EXTINGUISHED. THE PILOT INFORMED THE TOW ER OF HIS SITUATION AND WAS CLEARED TO RETURN TO DEPARTURE WHERE HE MADE AN UNEVENTFUL LANDING. UPON INVESTIGATION, NO E VIDENCE OF FIRE OR OVERHEATING COULD BE FOUND IN THE WING AND GEAR WELL AREAS. IT IS SUSPECTED THAT DUE TO HIGH WINDS DU RING THE PILOT’S BACK TAXI TO THE ACTIVE RUNWAY, HE MAY HAVE HAD TO APPLY CONSTANT BRAKE PRESSURE TO KEEP HIS TAXI SPEED 2 L 7 2 4T 3 T RT A8SW E3WE 2008011400196 20080114 00196 SW 2008 1 14 DUFA010308001 1 20080103 A 2613 WARNING LIGHT SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP WING OVERHEAT FALSE ACTIVATION E DUFA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 27 159MC AC728B WHILE ON CLIMB OUT, THE PILOT NOTICED THAT THE LT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWING PROCEDURE, THE LT GENERATOR WAS SHUTDOWN, BLEED AIR TURNED OFF AND THE LANDING GEAR EXTENDED. AFTER 3 MINUTES THE LIGHT WAS STILL ILLUMINATED AND P ROCEDURES CALL OUT FOR ENGINE SHUTDOWN. SHORTLY AFTER ENGINE SHUTDOWN THE LIGHT EXTINGUISHED. THE PILOT INFORMED THE TOW ER OF HIS SITUATION AND WAS CLEARED TO RETURN TO WHERE HE MADE AN UNEVENTFUL LANDING. UPON INVESTIGATION, NO EVIDENCE OF FIRE OR OVERHEATING COULD BE FOUND IN THE WING AND GEAR WELL AREAS. IT IS SUSPECTED THAT DUE TO HIGH WINDS DURING THE P ILOT’S BACK TAXI TO THE ACTIVE RUNWAY, HE MAY HAVE HAD TO APPLY CONSTANT BRAKE PRESSURE TO KEEP HIS TAXI SPEED LOW. THIS 2 L 7 2 4T 4 T RT A8SW E4WE 2008011500058 20080115 00058 2008 1 15 UPS08451372 4 20080103 A 3417 CADC BOEING 747 747200 1384847 NM NR 1 MALFUNCTIONED A IPXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 523UP 22381 INSPECTION TYPE:N/A ATB - RVSM - CAPTAINS ALTIMETER 1500' OF ALTITUDE AT 330, WENT TO ALT STATIC SOURCE. AS PER MM 34-1 1-00 AND 34-12-01 INSP NR 1 CADC AND PITOT STATIC SYS. DRAINED SOME WATER FROM STATIC LINES. REMOVED AND REPLACED NR 1 CADC PER MM 34-12-01 & LEAK CHECK GOOD. 2 L 7 4 4F RT A20WE 2008011500188 20080115 00188 SO 2008 1 15 C2XA08ON061 1 20080105 A 2130 CABIN PRESSURE EMB 145 EMB145XR 3260214 SO MALFUNCTIONED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 12195 14500943 FLT 103 - COS TO ONT - FLIGHT CREW REPORTED A/C WOULD NOT PRESSURIZE DURING WINDSHEAR ISSUES ON CLIMBOUT. BLEED WERE OF F, THEN TURNED ON. A/C RETURNED TO BLOCK WITHOUT INCIDENT. CONTRACT MX (ARNIC) RAN THE ENGINES WITH FLIGHT CREW AND OP ERATIONALLY CHECKED GOOD AND PRESSURIZATION PASSED SATISFACTORY. A/C WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008011500208 20080115 00208 EU 2008 1 15 08FDEA00042 1 20080105 A 5347 A5381206720100 SEAT TRACK AIRBUS 300 A300B4622 3930401 EU ZONE 200 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 LT TRACK Y1456 FR 51, AFTER REMOVAL OF WEB FOUND 1 LINK WITH BENT TAB ON I/B SIDE, REMOVED AND REPLACED SUPPORT LINK AT TRACK Y1456 FR 51 IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080908 EA 2008 9 8 TRAX200800661 1 20080519 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS INOPERATIVE A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 824AS 7203 FLAPS FAIL MSG WHEN SELECTING FLAPS FROM 20 DEG TO 30 DEG FLAPS FAILED AND 20 DEG. REMOVED AND REPLACED RT FLAPS BPSU A SSY AND FECU ASSY IAW AMM 21-51-10 AND 21-51-05. OPS CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080908 NM 2008 9 8 2008UALA03654 1 20080701 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY LIGHT ROW 36 LT INOP. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 USAA920081357 1 20080710 A 2560 P2070001214 FLASHLIGHT BOEING 737 7373G7 1384595 NM MAIN CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 154AW 23776 PHX - FLT 540 - FWD F/A EMERG FLASHLIGHT INOP. MX REPLACED FLASHLIGHT. OPERATIONAL CHECK WAS GOOD. (B) 2 L 7 2 4F RT A16WE 20080908 NM 2008 9 8 2008UALA03876 1 20080715 A 2910 272T3100216 LINE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE HYD SYSTEM CRACKED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 671UA 30026 LOST RIGHT HYDRAULIC SYSTEM. FOUND TUBE FROM REVERSER ISOLATION VALVE CRACKED. REPLACED TUBE WITH FLEX LINE. LEAK CHECK GOOD. OPS CHECKED OKAY FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080908 NE 2008 9 8 2008UALA03767 2 20080707 A 7261 FILTER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE ENGINE OIL WARNING MESSAGE A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 666UA 36067 7245 29238 727850 LT ENG OIL FILTER MSG APPEARED AFTER ENG START. MSG CLEARED WITHOUT ANY FLIGHT CREW ACTION. RETURNED TO BLOCKS. MAINT ENANCE REPLACED THE MAIN OIL FILTER PER AMM 79-21-05. NO METAL FOUND. FLIGHT TOOK AN 84 MINUTE DELAY. PROBLEM DID NO T RECUR. 2 L 7 2 4F 4 F RT A1NM E24NE 20080908 NM 2008 9 8 2008UALA03745 1 20080706 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EEL LIGHT INOP AT SEAT 47 ABC. FOUND LAMP INOP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NE 2008 9 8 Q2S2008F00004 2 20080711 A 7200 ENGINE BOEING 747 747300 1384920 GL PWA JT9 JT9D7R4G2 52054 NE NR 2 FAILED A Q2SA A UNSCHED LANDING R M J PARTIAL RPM/PWR LOSS OVER TEMP WARNING INDICATION CL CLIMB 1 EA 63 749SA 46052 24194 725302 AFTER TAKEOFF AND CLIMBING THROUGH FLIGHT LEVEL 220, NR 2 ENGINE COMPRESSOR STALLED VIOLENTLY, EGT 940 DEGREES C. REDUC ED THRUST AND NR 2 STABILIZER THEN STALLED VIOLENTLY AGAIN. AS EGT REACHED 700 DEGREES C, THRUST WAS REDUCED. COMPLETE D ENGINE FIRE/SEVERE DAMAGE QUICK REFERENCE HANDBOOK PROCEDURES & ACCOMPLISHED ENGINE SHUTDOWN. DUMPED 86,000 LBS OF FU EL AND RETURNED TO PANC. AWAITING ENGINE TO REPLACE WITH SERVICEABLE UNIT. (A) 2 L 7 4 4F 4 F RT A20WE E3NE 20080908 NM 2008 9 8 2008UALA03239 1 20080605 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26877 SEAT 4E EMERGENCY LIGHT STRIP BY SIDE OF SEAT IS MISSING. FOUND LIGHT STRIP MISSING. REPLACED LIGHT STRIP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03814 1 20080710 A 3350 582240 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 ALL EMERGENCY SEAT LIGHT IN FIRST CLASS INOP. FOUND FAULTY BATTERY PACK. REPLACED BATTERY PACK AND SECURED LOOSE WIRE CONNECTION. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080908 NM 2008 9 8 2008UALA03923 1 20080722 A 3510 OXYGEN BOTTLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU COCKPIT READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 700 PSI ON COCKPIT O2 GAUGE. PLS CHECK DIRECT GAUGE ON BOTTLE AND CONTACT SAM. 2 L 7 2 4F 4 F RT A16WE E21EU 20080908 NM 2008 9 8 RYN2008F00007 1 20080723 A 2913 3508806 PUMP BOEING 757 757231 1384950 NM LT HYD SYSTEM LOW PRESSURE A RYNA O OTHER J WARNING INDICATION NR NOT REPORTED 1 CE 07 151GX 24451 LT HYDRAULIC ENGINE DRIVEN PUMP LOW PRESSURE INDICATIONS IS INTERMITTENT. REPLACED THE LT ENGINE DRIVEN HYDRAULIC PUMP IAW AMM 29-11-05, SYSTEM OPS CHECKED NORMAL. (A) 2 L 7 2 4F RT A2NM 20080908 CE 2008 9 8 GUU2008F00026 1 20080721 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 81556 UE239 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT OUTBOARD ELEVATOR HINGE BRACKET CORRODED. REPLACED LT OUTBOARD ELEVA TOR HINGE BRACKET. (A) 2 L 7 2 4T RT A24CE 20080909 NM 2008 9 9 2008UALA04036 1 20080729 A 5320 SHEAR PLATE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 813UA 858 SHEAR PLATE CORRODED AT RT SIDE FRAME 69 TO 70. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA04040 1 20080730 A 5320 PLATE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SILL CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 813UA 858 RIGHT SILL PLATE FWD HOOK PLATE CORRODED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 EU 2008 9 9 2008UALA03994 1 20080727 A 3350 D9239003500060 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 465UA 1341 EMERGENCY LIGHTS FAILED TEST PER 3SVC. *S/D* EPSU FAILURE. REPLACED EPSU R & R BATTERY. EMERGENCY LIGHTS TEST OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 EU 2008 9 9 08FDEA03670 1 20080901 A 5340 A53974242200 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND IN AFT CARGO COMPARTMENT A CORNER FITTING C63 LT WITH CORROSION. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080909 NM 2008 9 9 08FDEA03665 1 20080901 A 5313 AJC7430506 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 594FE 48552 WASTE COMPARTMENT, AT ABOUT STA 1986 LONGERON 48 LEFT SPLICE FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01 VO LUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080909 EU 2008 9 9 08FDEA03681 1 20080901 A 5410 SUPPORT AIRBUS 310 A310222 3930315 EU NR 1 NACELLE BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 NR 1 ENGINE NOSE COWL ANTI-ICE PICCOLO TUBE SUPPORT LINKS AT THE 7; 12 & 2 O'CLOCK POSITIONS ARE BROKEN & DISCONNECTED. (TOTAL 8 LINKS) REMOVED & REPLACED THE NR 1 ENGINE NOSE COWL IAW AMM 71-11-00-4. 2 L 7 2 4F RT A35EU 20080909 NM 2008 9 9 08FDEA03494 1 20080818 A 5347 ACA7104511 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 MAIN DECK SEAT TRACK CORRODED AT STA 655, RBL 8. MAIN DECK CORRODED SEAT TRACK AT STA 655 RBL 8 REPAIRED BY SECTIONAL S EAT TRACK REPLACEMENT FROM STA 645 TO STA 765 RBL 8 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080909 NM 2008 9 9 08FDEA03495 1 20080818 A 5210 ADA00071 BEAM DOUG MD11 MD11F 3023600 NM L3 DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 L3 DOOR FWD BEAM NR 7 STOP BROKEN. L3 DOOR BROKEN BEAM REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLAS SIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080909 NM 2008 9 9 08FDEA03496 1 20080818 A 5714 APB74471 SKIN DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 MAIN DECK CARGO COMPARTMENT, CENTER WING TANK UPPER SKIN CORRODED AT STA 1232, LBL 47. MAIN DECK CARGO COMPARTMENT CENT ER WING TANK UPPER SKIN CORROSION AT STA 1232 LBL 47 REPAIRED AS PER FEDEX EA 1-5710-124343, TITLE: WINGS - BASIC WING S TRUCTURE - CORROSION AT CENTER TANK UPPER SKIN, STATION 1232 - REPAIR. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-1 00. 2 L 7 3 4F RT A22WE 20080909 NM 2008 9 9 08FDEA03643 1 20080829 A 5320 SUPPORT BOEING 727 727233 138408A NM BS 1253 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 LEFT LOWER TORQUE BOX, UPPER WEB SUPPORT HAS CRACK AT RIVET, STA 1253. CUT OUT AREA FOR ACCESS TO REMOVE SUPPORT ANGLE IAW SRM 51-40-2 & 51-10-1. REMOVED SUPPORT ANGLE IAW SRM 51-30-2. FABRICATED NEW SUPPORT ANGLE IAW DRAWING 65-17518. ALO DINED AND PRIMED ANGLE IAW SRM 51-10-2. INSTALLED ANGLE IAW SRM 51-30-2. FABRICATED 2(EA) DOUBLERS IAW SRM 51-40-2 FIG 1. ALODINED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED PARTS IAW SRM 51-40-2 FIG 1. 2 L 7 3 4F RT A3WE 20080909 NE 2008 9 9 08FDEA03645 2 20080829 A 7320 1820M99P08 ECU AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680 30025 NE NR 2 ENGINE FAILED A FDEA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 CE 21 681FE 799 DURING CLIMB NR 2 ENG N1, FF, EGT BECAME UNSTABLE, ASSOCIATED WITH ENGINE SURGING. FOLLOWING NR 2 ENG FADEC BITE DISPLA Y: BITE CHA CHB 270 84120 84120 271 99080 99080 272 20000 20000 273 274 ON 350-354. FADEC GROUND TEST: FOUN D FAULT CODE 352-21 ON CH A N1 SPEED SENSOR PERFORMED TSM PROCEDURE 73-21-30 352-21 FIG 102 SHEET 28. CHECKED BOTH CH A & B SYS GOOD. SPEED SENSOR IS 116 OHMS AT THE HARNESS. THE ECU CHECKED BAD PER STEP 12. REMOVED AND REPLACED ECU IA W AMM 73-21-01-4 05. ENGINE RUN AT HIGH POWER IAW JRH. ALL INDICATIONS STABLE. NO FAULT CODES AFTER RUN. ITEM CLEARE D. 2 L 7 2 4F 4 F RT A35EU E13NE 20080909 WP 2008 9 9 08FDEA03691 1 20080901 A 5350 ANB714311 BRACKET DOUG MD10 MD1010F 3022112 WP BS 1361 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 THERE IS A CRACKED BRACKET AT STA 1361 BETWEEN LONGERONS 31L & 32L. REMOVED ANGLE IAW SRM 51-31-01 VOL II. HEAT TREATE D IAW TPS 1003; REV " A ". ALODINED & PRIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II. INSTALLED IAW SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 20080909 NM 2008 9 9 08FDEA03655 1 20080831 A 5730 112N3101 SKIN BOEING 757 757223 1384957 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 RT WING TOP SURFACE REAR SPAR AREA APPROX WS 230-345, 3 SPOTS OF CORROSION ON TOP OF WING. REPAIR CARRIED OUT BY BLENDI NG OUT IAW B757-200 SRM 57-20-01 TABLE 1 AND EA F- 5730-124309. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 F3L2008F00004 1 20080822 A 5315 D5347217220500 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 928FR 2236 REFERENCE NON ROUTINE C050039. DURING C3 C-CHECK, INSP NOTED FLOOR BEAM Y1292 HAS CORROSION IN VARIOUS NUT CLIP HOLES F ROM RT HAND FRAME 66 TO FRAME 67. SUPPLEMENTAL INFORMATION WILL BE PROVIDED AS SOON AS CORRECTIVE ACTION INFORMATION BE COMES AVAILABLE. (OPEN) 2 L 7 2 4F RT A28NM 20080910 EU 2008 9 10 AALA200801927 1 20080722 A 2913 PUMP AIRBUS 300 A300B4605R 3930308 EU NR 1 HYD SYS INOPERATIVE A AALA O OTHER J WARNING INDICATION DE DESCENT 1 SW 21 70074 517 JFK INFLIGHT T1692/22JUL. CREW REPORTED PROBLEMS WITH GREEN HYDRAULIC SYSTEM INDICATIONS DURING FLIGHT. ON DESCENT CRE W REPORTED GREEN RESERVOIR LOW AND SYSTEM INOPERATIVE. LANDED JFK WITHOUT INCIDENT. REPLACED GREEN HYDRAULIC SYSTEM RE SERVOIR AND LT ENGINE DRIVE HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A35EU 20080908 2008 9 8 QXEA200800699 4 20080630 A 2350 AUDIO PANEL DHAV DHC8 DHC8202 2809007 NM COCKPIT MALFUNCTIONED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 346PH 477 YLW-GPU QUIT. AIRCRAFT LOST POWER AT GATE. DETECTED AN ELECTRICAL ODOR. SHUT OFF BATTERY. GOT NEW GPU. WHEN POWER R ESTORED, SQUEAL OVER SPEAKERS. MAINTENANCE SWAPPED AUDIO PANELS BETWEEN OBSERVER AND CAPTAIN. CHECKS GOOD. RETURNED T O SERVICE. NO PARTS REPLACED. (A) 2 H 7 2 4T RT A13NM 20080908 NM 2008 9 8 QXEA200800646 1 20080615 A 3240 FITTING DHAV DHC8 DHC8202 2809007 NM BRAKE ASSY LEAKING A QXEA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 357PH 504 PDX - FLIGHT 2123 - SMOKE REPORTED FROM LT MAIN GEAR ON TOUCHDOWN. FLUID LEAK NOTED FROM LT MAIN LANDING GEAR. MAINTEN ANCE FOUND A SMALL LEAK AT NR 1 BRAKE HYDRAULIC BLEED PORT. TIGHTENED FITTING. CHECKS GOOD. NO LEAKS. RETURNED TO SER VICE. NO PARTS REPLACED. (A) 2 H 7 2 4T RT A13NM 20080909 NM 2008 9 9 2008UALA03976 1 20080725 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 600 S24L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 FWD PIT AT STA 600, STR 24L FRAME DENTED AT INBOARD FLANGE. MAJOR REPAIR AT GSO. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 53-00-07 REPAIR 5, AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E17NE 20080909 NM 2008 9 9 2008UALA03977 1 20080725 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1660 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 UPPER T-CAP AFT FLANGE HAS CORROSION, CABIN FLOORBEAM, STA 1660, LBL 14. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. CUT OUT DAMAGED SECTION, LBL 13 TO LBL 15. INSTALLED FILLER AND 2 EA ANGLES PER MM. 2 L 7 2 4F 4 F RT A2NM E17NE 20080909 NM 2008 9 9 CALA0800779 1 20080728 A 5230 6547052524 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 AFT CARGO DOOR FOUND WITH CRACK APPROX 2.5 INCH ABOVE AFT EDGE OF EXTERNAL HANDLE. REMOVED EXISTING REPAIR DOUBLER PER SRM 51-40-02 FROM AFT CARGO DOOR, FABRICATED NEW REPAIR DOUBLER PER SRM 52-00-01, ALODINED AND PRIMED REPAIR DOUBLER AND BASE SKIN PER SRM 51-20-01. INSTALLED NEW REPAIR DOUBLER PER SRM 52-00-01. CRACK TERMINATED IN EXISTING FASTENER HOLE , NEW REPAIR DOUBLER INCORPORATED. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 ZZDA2008147 1 20080806 A 5320 9936535233 FLOOR SUPPORT BOEING 717 717200 1383700 NM BS 195-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 FLOOR SUPPORT HAS CORROSION AT BS 195 - 200 LBL 15 OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT AT BS 195 - 200 LB L 15 IAW B717 SRM 51-41-01. 2 L 7 2 4F TR A6WE 20080909 NM 2008 9 9 ZZDA2008149 1 20080806 A 5315 993653433 FLOORBEAM BOEING 717 717200 1383700 NM BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 FLOOR SUPPORT HAS CORROSION AT BS 200 BL-0 RBL 37. REMOVED AND REPLACED FLOOR SUPPORT AT BS 200 - BL-0 TO RBL 37 IAW B7 17 SRM 51-41-02. 2 L 7 2 4F TR A6WE 20080909 NM 2008 9 9 2008UALA04077 1 20080731 A 3350 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 817UA 873 RIGHT EMERGENCY POWER SUPPLY UNIT FAILED "A" CHECK BATTERY CAPACITY CHECK. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA04031 1 20080729 A 2121 FAN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EQUIPEMENT BAY FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 351UA 24319 EQ COOLING FAN FAILURE. RTFL. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 2008UALA04038 1 20080730 A 5311 FRAME AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 813UA 858 FRAME FOR SHEAR PLATE CORRODED AT RT SIDE FRAME 36 TO 70. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA04039 1 20080730 A 5320 PLATE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SILL CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 813UA 858 RT SILL PLATE AFT HOOK PLATE ASSY IS CORRODED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NE 2008 9 9 2008UALA03991 2 20080728 A 7412 MR74110 EXCITER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 CREW REPORTS LEFT ENGINE NR 2 IGNITON IS INOP. *S/D* IGNITION EXCITOR IS INOP. REPLACED IGNITION EXCITOR, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080909 NM 2008 9 9 2008UALA04150 1 20080806 A 2800 UNKNOWN BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE UNKNOWN A UALA O OTHER O OTHER CR CRUISE 1 WP 29 216UA 30549 UNWANTED FUEL TRANSFER. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 EU 2008 9 9 08FDEA03669 1 20080901 A 5320 A53974222212 STIFFENER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND IN AFT CARGO COMPARTMENT STIFFENER AT CROSS BEAM C 56 RT DENTED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080909 NM 2008 9 9 08FDEA03664 1 20080901 A 5330 NDA63135 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 594FE 48552 FUSELAGE EXTERIOR FOUND FORWARD CARGO DOOR CUTOUT FORWARD LOWER EDGE CHIPPED. CARRIED OUT REPAIR AS PER SRM 53-50-00 FI GURE 7 VOLUME I. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-20-100. 2 L 7 3 4F RT A22WE 20080909 EU 2008 9 9 08FDEA03680 1 20080901 A 5320 A53980212206 SUPPORT AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND DAMAGED Z-PROFILE (TO LESS EDGE MARGIN) AT C74, P26 LT. REPAIR PERFROMED BY DRILLING AN ADDITIONAL HOLE AND INSTA LLING ADDITIONAL FASTENER LN9198-4800CF IAW RAS/EFW/9000083/2008 ISS A, APPROVED EA 6-5318-123078. 2 L 7 2 4F RT A35EU 20080909 EU 2008 9 9 08FDEA03683 1 20080901 A 5753 FITTING AIRBUS 310 A310222 3930315 EU LT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 LEFT WING INBOARD FLAP OUTBOARD END; FOLLOW UP GUIDE FITTING IS CRACKED. REMOVED & INSTALLED FITTING IAW SRM 51-40-30. LOCATED & DRILLED IAW SRM 51-40-40. PAINTED IAW SRM 51-23-10. 2 L 7 2 4F RT A35EU 20080909 WP 2008 9 9 08FDEA03685 1 20080901 A 5720 ARB24047 CHANNEL DOUG MD10 MD1010F 3022112 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING INBOARD UPPER L/E PANEL 517 CT HAS A CRACKED CHANNEL. REMOVED STIFFENER IAW SRM 51-35-01 VOL II. FABRICATED STIFFENER IAW DWG ARB 2407; REV "G". ALODINED & PRIMED IAW SRM 51-21-01 VOL II PGS 21-24. INSTALLED IAW SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 20080909 NM 2008 9 9 08FDEA03459 1 20080817 A 5310 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM CARGO DOOR FRAME CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 DURING OPEN HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CR ACK INDICATIONS AT HOLES C AND D. MAIN CARGO DOOR LOWER JAMB CRACKED SUPPORT FITTING NR 2 REMOVED AND REPLACED AS PER S RM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080909 NE 2008 9 9 AALA200801951 2 20080724 A 7250 TURBINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE DAMAGED A AALA E A ENGINE SHUTDOWN UNSCHED LANDING M R J OVER TEMP PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 9626F 53596 718506 DFW INFLIGHT T2457/24JUL. CREW REPORTED NR 1 ENGINE MADE LOUD BANG FOLLOWED BY ENGINE GAS TEMPERATURE HIGH. CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND TURBINE DAMAGE. REPLACED NR 1 ENGINE ON 24 JUL AT DFW. SYSTEM GROUND CHECKED NORMAL OPS. (OPEN) 2 L 7 2 4F 4 F RT A6WE E9NE 20080909 NM 2008 9 9 08FDEA03462 1 20080817 A 5340 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM CARGO DOOR FRAME CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 DURING OPEN HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CR ACK INDICATIONS AT HOLES A AND B. MAIN CARGO DOOR LOWER JAMB CRACKED SUPPORT FITTING NR 6. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080909 NM 2008 9 9 08FDEA03493 1 20080818 A 5310 A6A70949 STANCHION DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 FWD CARGO: AFT BULKHEAD APPROXIMATE STA 6-73.5, LBL 8, STANCHION CORRODED. FORWARD CARGO AFT BULKHEAD APPROXIMATELY ST A 6-73.5, LBL 8 STANCHION CORRODED AREA. CARRIED OUT REPAIRED AS PER SRM 53-00-01 FIGURE 8 VOLUME I. THIS REPAIR CLASS IFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 2008UALA04116 1 20080802 A 3397 794640 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT FROM SEAT 46 TO 54 LT INOP. *S/D* RE-SECURED EEL CONNECTOR. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080909 NM 2008 9 9 08FDEA03647 1 20080831 A 5753 6521631202 SKIN BOEING 727 727227 1384078 NM RT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 CRACK ON DOUBLER AT RIGHT O/B FORE FLAP BY O/B TRUCK ATTACH FITTING AT WS 629. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED REPAIR PARTS, IAW SRM 57-50-4 FIG 7 AND 457-50-2 FIG 4. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAI R PARTS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20080909 NM 2008 9 9 08FDEA03648 1 20080831 A 5313 65562392 STRINGER BOEING 727 727227 1384078 NM BS 690 S27R CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 FWD CARGO COMPARTMENT, CORROSION ON STR AT BS 690, STR 27R. REMOVED CORROSION IAW SRM 51-10-6 AND FOUND OUT OF LIMITS I AW SRM 53-10-1. CUTOUT DAMAGED AREA DIM 11" AND FABRICATED NEW STRINGER SECTION AND 02 EA SPLICES IAW SRM 53-10-2 FIG 9 AND 53-10-3 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS AT FWD PIT STRINGER 27R AT STA 690 I AW SRM 53-10-3 FIG1. 2 L 7 3 4F A3WE 20080909 NM 2008 9 9 08FDEA03649 1 20080831 A 5313 65562392 STRINGER BOEING 727 727227 1384078 NM BS 720D S27R CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 FWD CARGO COMPARTMENT, STRINGER 27R CORRODED JUST FWD OF STA 720D APPROX 12 INCHES. REMOVED WEB IAW SRM 51-30-2. CUTOUT DAMAGED AREA OF STRINGER IAW SRM 53-10-3. FABRICATED STRINGER SECTION AND 2 SPLICES IAW SRM 53-10-3 FIG1. TREATED AND P RIMED REPAIR PARTS AND AREA IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 53-10-3 FIG 1. REINSTALLED WEB I AW SRM 51-30-2. 2 L 7 3 4F A3WE 20080909 WP 2008 9 9 08FDEA03690 1 20080901 A 5350 AEA055319 BRACKET DOUG MD10 MD1010F 3022112 WP BS 1401 S31-32L CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 THERE IS A CRACKED BRACKET AT THE LEFT OVERWING TO BODY FAIRING SUPPORT BETWEEN LONGERON 31L & 32L AT STA 1401. REMOVED ANGLE IAW SRM 51-33-01 VOL II. FABRICATED A NEW ANGLE, HEAT TREAT IAW TPS 1003, REV " A ". ALODINED & PRIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II. INSTALLED IAW SRM 51-33-01 & 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 20080909 WP 2008 9 9 08FDEA03693 1 20080901 A 5350 ANB70514 ANGLE DOUG MD10 MD1010F 3022112 WP BS 1421 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 THERE IS A CRACKED VERTICAL ANGLE AT THE RIGHT OVERWING TO BODY FAIRING SUPPORT AT STA 1421. REMOVED ANGLE IAW SRM 51-3 1-01 VOL II. FABRICATED IAW DWG AUB 7051; REV " C ". HEAT TREATED IAW TPS 1003 REV " A ". LOCATED & DRILLED HOLES IAW SRM 51-31-01 VOL II. ALODINED & PRIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II. INSTALLED NEW ANGLE IAW SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 20080909 NM 2008 9 9 08FDEA03651 1 20080831 A 5313 65562392 STRINGER BOEING 727 727227 1384078 NM BS 720D CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 FWD CARGO COMPARTMENT, STRINGER 27R CORRODED JUST FWD OF STA 720D APPROX 12 INCHES. REMOVED WEB IAW SRM 51-30-2. REMOVE D DAMAGED AREA OF STRINGER IAW SRM 53-10-3. FABRICATED STRINGER SECTION AND 2 SPLICES IAW SRM 53-10-3 FIG 1. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 53-10-3 FIG 1. REINSTALLED WEB IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20080909 NM 2008 9 9 08FDEA03653 1 20080831 A 5753 NRC6762501 VANE DOUG MD11 MD11F 3023600 NM LT WING TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 594FE 48552 LT WING INBOARD FLAP VANE INBOARD OF MID WAY TO TRAILING EDGE AREA FOUND DELAMINATED. REMOVED AND REPLACED AS PER AMM 2 7-50-22-4. ADJUSTMENT AND TEST CARRIED OUT FOUND SATISFACTORY AS PER AMM 27-50-22-5. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080910 NM 2008 9 10 AALA200802011 1 20080802 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 355AA 24036 JFK EMERGENCY LIGHT AT LT AND RT HAND OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK AT RT HAND OVERWING DOOR FOR EME RGENCY LIGHT AT LT AND RT HAND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20080910 NM 2008 9 10 AALA200802006 1 20080731 A 3350 1317 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39356 24037 ORD EMERGENCY LIGHT AT SEAT 10B OVERHEAD INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT SEAT 10B OVERHEAD. SYSTEM GROU ND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20080910 NM 2008 9 10 AALA200801960 1 20080725 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 751AN 30798 DFW EMERGENCY LIGHT AT SEAT 38G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 38G. SYSTEM GROUND CHECKED NORM AL OPS. (CLOSED) 2 L 7 2 4F RT T00001SE 20080910 NM 2008 9 10 USAA920081562 1 20080821 A 5311 65458073 FRAME BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 24479 CLT - C4 - MAJOR REPAIR - NR 5030599 - CRACK IN FRAME WEB CUTOUT AT BS 291.5, S16R. REPAIRED FRAME WEB CUTOUT AT BS 291 . 5, S16R IAW US AIRWAYS EA 100606. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 AALA200801949 1 20080724 A 3350 0201720101 LIGHT BOEING 767 767323 1385205 NM SEAT 2B DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 385AM 27059 JFK EMERGENCY LIGHT AT SEAT 2B DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20080910 EU 2008 9 10 AALA200801967 1 20080726 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 77080 626 JFK EMERGENCY LIGHT AT RT NR 3 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT NR 3 DOOR. SYSTEM GROUND CHEC KED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A35EU 20080910 SO 2008 9 10 CHQ2008F00002 1 20080822 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007A 03030 GL EMERGENCY LIGHTS INOPERATIVE A CHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 260SK 145128 CAE311802 DURING INSPECTION THE NR 1 PROXIMITY LIGHT STRIP AND THE EMERGENCY LIGHT OVER THE SERVICE DOOR WAS FOUND TO BE INOP. TH E NR 2 EMERGENCY LIGHT INVERTER WAS REPLACED IAW AMM 33-50-11. AFTER INVERTER REPLACEMENT, THE EMERGENCY LIGHTS OPERATE D NORMALLY. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080910 CE 2008 9 10 DXTA200803247 1 20080825 A 3260 INDICATOR RAYTHN DH125 HAWKER800XP 7150012 CE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 873QS 258573 RT RED GEAR IN TRANSIT LIGHT REMAINED ON AFTER RETRACTING THE GEAR ON TAKEOFF. 2 L 7 2 4F RT A3EU 20080910 NM 2008 9 10 USAA920081574 1 20080820 A 5320 6545834U107 STRAP BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT - Q6 - MAJOR REPAIR - NR # 03C10753005/012 - FLOOR STRAP CRACKED BETWEEN BS328 TO BS344, LBL45. REPLACED FLOOR STRAP BETWEEN BS328 TO BS344, LBL45 IAW B737 SRM 51-20-01. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 USAA920081575 1 20080822 A 5755 SKIN BOEING 737 7373B7 1384580 NM NR 2 SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT - Q6 - MAJOR REPAIR - NR 03C10753005/004 - NR 2 SPOILER DELAMINATED ON SKIN UPPER SURFACE. REPLACED NR 2 SPOILER I AW B737 AMM 27-61-11. 2 L 7 2 4F RT A16WE 20080910 CE 2008 9 10 DXTA200803236 1 20080822 A 2120 UNKNOWN CESSNA 750 750 2076810 CE CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 907QS 7500201 DURING APU RUN, ACFT FILLED WITH SMOKE. THE SMOKE HAD A BURNING RUBBER SMELL. KSAT. 2 L 7 2 4J RT T00007WI 20080910 NM 2008 9 10 AALA200801934 1 20080722 A 3350 1010427 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AM 24525 JFK EMERGENCY LIGHT AT SEAT 34A MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 34A. SYSTEM GROUND CHECKED NOR MAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 USA2008F00023 1 20080823 A 5497 FRFOE2822P03 CONNECTOR BOEING 737 737401 1384701 NM NR 2 PYLON BURNED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 409US 23879 CLT FLT1577 AFTER TAKEOFF FROM CLT, CREW REPORTED THE FIRST OFFICER’S GYRO AND IRU FAILING INTERMITTENTLY. ALSO, THE NR 2 AND NR 3 TRANSFORMER/RECTIFIER CIRCUIT BREAKERS WERE TRIPPED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FUR THER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE RESET THE NR 2 AND NR 3 TRANSFORMER/RECTIFIER CIRCUIT BREAKERS. OPS CHECK NORMAL. NO FAULTS NOTED. REMOVED AND REPLACED NR 2 AND NR 3 TRANSFORMER/RECTIFIERS, AS PRECAUTIONARY PER MM 24-21-31. FIRST OFFICER’S TRANSFORMER/RECTIFIER OPERATE PROPERLY PER MM 34-28-00. FURTHERMORE, FOUND PINS/SOCKETS BUR NED ON NR 2 ENGINE PYLON CONNECTORS D3026 AND D410 DUE TO A SUBSEQUENT EVENT THE FOLLOWING DAY. REPLACED CONNECTORS. A 2 L 7 2 4F RT A16WE 20080910 EA 2008 9 10 COMA086362 1 20080824 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA BS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 779CA 7306 UNDERFLOOR WEB BETWEEN FWD AND AFT U-CHANNELS AND LBL9-RBL9 AT STA 280 HAS CORROSION. CORRECTIVE ACTION: REPAIRED IAW E A NR 10-5310-02304. 2 L 7 2 4F RT A21EA 20080910 WP 2008 9 10 AALA200801932 1 20080722 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9621A 53592 AUS OVERHEAD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 105 FOR OVERHEAD EMERGENCY LIGHTS IN CA BIN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A6WE 20080910 NM 2008 9 10 AALA200801924 1 20080722 A 3350 P4010051112 MODULE BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 624AA 24582 EWR EMERGENCY LIGHTS AT SEAT ROWS 16 TO 26 AND OVERWING EXIT DOOR SIGNS INOPERATIVE. REPLACED MODULE FOR EMERGENCY LIGH TS AT SEAT ROWS 16 TO 26 AND OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 AALA200802021 1 20080804 A 3240 BRAKE BOEING 767 767323 1385205 NM MLG OVERHEATED A AALA O OTHER M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 353AA 24034 DFW INFLIGHT T2448/04AUG. CREW REPORTED NR THREE BRAKE OVERHEATED DURING TAXI FROM HANGAR TO TERMINAL. DRY CHEMICAL AP PLIED. INSPECTION FOUND NO INDICATION OF HEAT DAMAGE. REPLACED NR 3 AND 4 MAIN TIRE ASSEMBLIES. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20080910 NM 2008 9 10 AALA200801954 1 20080725 A 3241 CONTROLLER BOEING 737 737823 13844BZ NM ANTI-SKID SYS INOPERATIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 913AN 29514 JFK INFLIGHT T750/25JUL DFW TO LGA. CREW REPORTED ANTI-SKID INOPERATIVE INDICATION AFTER TAKE OFF. LANDED JFK WITHOUT INCIDENT DUE TO LONGER RUNWAY. REPLACED ANTI SKID AUTO BRAKE CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 AALA200801961 1 20080726 A 3350 OL1098BPEGPL LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 681AA 25338 JFK EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHECKED NORM AL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 USAA920081573 1 20080817 A 5320 6545834 STIFFENER BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT - Q6 - MAJOR REPAIR - NR 03C10753005/025 - FLOOR BEAM WEB VERTICAL STIFFENER CRACKED AT BS328, BLO. REPLACED FLOORB EAM WEB VERTICAL STIFFENER AT BS 328, BL 0 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20080910 EU 2008 9 10 USAA920081565 1 20080822 A 2121 EVT3454H FAN AIRBUS 320 A320232 3930326 EU ZONE 100 DEFECTIVE A USAA O OTHER O OTHER DE DESCENT 1 EA 19 655AW 33284 33275 1075 LOG PAGE 8061203 - FLT 454 PHX-SLC - SMOKE SMELL - CREW RECEIVED BLOWER EXTRACT FAN FAULT ON DESCENT, HEARD GRINDING SO UND AND SMELLED ELECTRICAL SMOKE. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE A VIONICS FAN 20HQ IAW MAINTENANCE MANUAL 21-26-51. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20080910 NM 2008 9 10 USAA920081582 1 20080826 A 5755 SKIN BOEING 737 7374B7 1384702 NM NR 7 SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 455UW 24997 CLT C1 MAJOR REPAIR NR 03C10025001/001 NR 7 FLIGHT SPOILER DELAMINATED ON AFT UPPER SURFACE. REPLACED NR 7 FLIGHT SPOIL ER IAW B737 AMM 27-61-11. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 USAA920081580 1 20080821 A 5320 6545855538 STRUCTURE BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN A1 MAJOR REPAIR NR 6123918 CORROSION ON INNER CHORD AT BS960 TO BS990. S17R, WL208. REPLACED INNER CHORD AT BS960 T O BS990, WL208 IAW B737 SRM 51-40-02-OG. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 AALA200801955 1 20080725 A 2422 INVERTER BOEING 767 767323 1385205 NM ODOR A AALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 363AA 24044 POS INFLIGHT T1668/25JUL. CREW REPORTED STANBY INVERTER STATUS MSG AND HEAVY ELECTRICAL SMOKE SMELL IN COCKPIT. RETURN ED TO POS AND LANDED WITHOUT INCIDENT. REPLACED STATIC INVERTER. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20080910 NM 2008 9 10 UIEA200800298 1 20080825 A 5730 PANEL BOEING 747 747341 13848AM NM RT WING CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 355MC 23395 RT WING FORWARD LEADING EDGE PANEL HAS A 2.5" CRACK LOCATED AT ILES 208.81 AND IS 18.25" FROM TOP EDGE OF PANEL. PERMAN ENT REPAIR ACCOMPLISHED AS PER B747-300 SRM 57-30-04 FIG. 2, SHEETS 1,2 & 3. ALSO, REFERENCE ATLAS AIR EO NO. 4757A459. 2 L 7 4 4F RT A20WE 20080908 WP 2008 9 8 IXX2008F00020 1 20080716 A 2697 CONNECTOR DOUG DC8 DC871F 302199D WP FIRE DETECTOR DAMAGED A IXXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 11 830BX 45973 FLT NR: ATN 229/PKMJ TO KHNL. DURING CRUISE FROM PKMJ NR 4 FIRE WARNING CAME ON, THE CREW SHUTDOWN NUMBER FOUR ENGINE A ND DISCHARGED BOTH BOTTLES. THE CREW LANDED IN KHNL WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED NR 4 FIRE WARNING SYSTEM AND FOUND LOW RESISTANCE. MAINTENANCE REPLACED P1-7037 CONNECTOR, AND BOTH FIRE BOTTLES. OPERATIONAL CHECK GOOD IAW MM 26-10-0, 26-21-09. AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 4 4F RT 4A25 20080908 NM 2008 9 8 QXEA200800692 1 20080625 A 5250 LATCH DHAV DHC8 DHC8202 2809007 NM COCKPIT DOOR STICKING A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 346PH 477 SEA - FLIGHT 2077 - COCKPIT DOOR HARD TO OPEN AND CLOSE. MAINTENANCE FOUND LATCH STICKY. CLEANED AND LUBED LATCH. CHE CKS GOOD. RETURNED TO SERVICE. NO PARTS. (A) 2 H 7 2 4T RT A13NM 20080908 NM 2008 9 8 QXEA200800652 1 20080617 A 5210 STOP BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR HANDLE OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 413QX 4060 PDX - RT REAR PASSENGER DOOR HARD TO OPEN. ADJUSTED THE LATCH CRANK STOP BOLT IAW 52-00-00-830-803. CHECKS GOOD. RETU RN TO SERVICE. NO PARTS REPLACED. (A) 2 H 7 2 4T RT A13NM 20080908 NM 2008 9 8 QXEA200800706 1 20080712 A 7797 CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA DISPLAY LOOSE A QXEA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 NM 09 406QX 4048 BOI-FLIGHT 2344 (LAX-SUN). DIVERTED TO BOI FOR THE NR 1 ENGINE ITT DISPLAY INOP, SHOWING ONLY DASHES. MAINTENANCE FOUN D CODE 805 ON A AND B CHANNELS. FOUND ITT TRIM CONNECTORS LOOSE, TIGHTENED CONNECTORS. OPERATIONAL CHECKS GOOD. AIRCR AFT RETURNED TO SERVICE. NO PARTS REPLACED. (A) 2 H 7 2 4T 4 T RT A13NM E00062EN 20080908 NM 2008 9 8 CALA0800748 1 20080725 A 5320 6547690 ANGLE BOEING 737 737524 1384721 NM BS 727B-787 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 AFT CARGO BAY RIGHT SIDE TRANSLATION ANGLE HAS CORROSION FROM STATION 727B TO 787. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED SECTION OF TRANSITION ANGLE FROM STATION 733-766 RIGHT SIDE PER SRM 53-60-53. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 2008UALA03978 1 20080725 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 700 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 FWD PIT STA 700 LBL 25 FLOORBEAM CRACKED. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. CUT OUT DAMAGE, INSTALLED FABBED T- CAP AND SPLICE AND INSTALLED REF MM 53-00-98. 2 L 7 2 4F 4 F RT A2NM E17NE 20080909 2008 9 9 2008UALA04006 4 20080724 A 2565 416N2002888 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 DOOR 1L SLIDE PRESSURE LOW. *S/D* UNKNOWN LEAK. REPLACED SLIDE ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 NM 2008 9 10 AALA200802005 1 20080731 A 3397 WIRE BOEING 767 767323 1385205 NM EMERGENCY LIGHT SEVERED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39356 24037 ORD EMERGENCY LIGHT AT SEAT 4B FORWARD INOPERATIVE. FOUND SEVERED WIRES. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT SE AT 4B FORWARD. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20080910 WP 2008 9 10 AALA200802027 1 20080805 A 3243 4062575 TRANSDUCER DOUG DC9 DC983 3022083 WP MLG INOPERATIVE A AALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 21 9629H 53599 DFW INFLIGHT T1115/05AUG. CREW REPORTED LT HAND ANTI SKID LIGHT ILLUMINATED ON APPROACH. LANDED DFW WITHOUT INCIDENT. REPLACED NR 2 WHEEL SPEED TRANSDUCER. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A6WE 20080910 NM 2008 9 10 AALA200801939 1 20080723 A 3350 LIGHT BOEING 767 767323 1385205 NM LAVATORY DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AN 25451 MIA EMERGENCY LIGHT MID NR 1 LAVATORY DAMAGED. REPLACED BASE FOR EMERGENCY LIGHT AT MID NR 1 LAVATORY. SYS GROUND CHEC KED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20080910 WP 2008 9 10 AALA200801931 1 20080722 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9621A 53592 AUS OVERHEAD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 104 FOR OVERHEAD EMERGENCY LIGHTS IN CA BIN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A6WE 20080910 EU 2008 9 10 AALA200801965 1 20080726 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 77080 626 JFK EMERGENCY LIGHT AT OVERHEAD LT NR 2 DOOR INOPERATIVE. REPLACED LAMP AT OVERHEAD LT NR 2 DOOR. SYSTEM GROUND CHECKE D NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A35EU 20080910 WP 2008 9 10 AALA200801963 1 20080726 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 498AA 49736 LGA EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 23 TO 26 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 25 FOR EMERGENCY LIGH TS AT OVERHEAD SEAT ROWS 23 TO 26. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F A6WE 20080910 NM 2008 9 10 F3LA200800584 1 20080823 A 5315 D5347218820400 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 928FR 2236 REFERENCE NON ROUTINE CO50117. DURING C3 C-CHECK, INSP NOTED LT FLOORBEAM Y1292 HAS CORROSION IN VARIOUS NUT CLIP HOLES FROM FRAME 66 TO FRAME 68 (L2 DOOR AREA). MX R&R THE FLOORBEAM IAW THE REQUIREMENTS OF ENGINEERING AUTHORIZATION NR 1 9-53R-30587. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20080910 NM 2008 9 10 AALA200801984 1 20080727 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AM 24594 DFW EMERGENCY LIGHT EXIT IDENTIFIER AT MID LAVATORY INOPERATIVE. REPLACED LAMP. SYSTEM GROUND CHECKED NORMAL OPS. (CL OSED) 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 AALA200801952 1 20080724 A 7931 21SN04340 PRESSURE SWITCH BOEING 777 777223 1385213 NM RT ENGINE OIL INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 793AN 30255 ORD INFLIGHT T70/24JUL DFW TO FRA. CREW REPORTED RT HAND ENGINE OIL SCAVENGE FILTER CLOG LIGHT ILLUMINATED. LANDED ORD WITHOUT INCIDENT. REPLACED DIFFERENTIAL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT T00001SE 20080910 NM 2008 9 10 AALA200801962 1 20080726 A 3350 0201804001 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 681AA 25338 JFK EMERGENCY LIGHT AT SEAT 26D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHECKED NOR MAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 AALA200801959 1 20080725 A 3397 WIRE HARNESS BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 699AN 27051 MIA EMERGENCY LIGHT AT SEAT 4E INOPERATIVE. SECURED WIRING HARNESS FOR EMERGENCY LIGHT AT SEAT 4E. SYSTEM GROUND CHECK ED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 AALA200801994 1 20080728 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 777AN 29585 DFW EMERGENCY LIGHT AT SEAT 32G BROKEN. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKED NORMAL OP S. (CLOSED) 2 L 7 2 4F RT T00001SE 20080910 NM 2008 9 10 USAA920081578 1 20080823 A 5240 WEB BOEING 737 7374B7 1384702 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 455UW 24997 CLT - C1 - MAJOR REPAIR - LOG NR 5030609 - FORWARD SERVICE DOOR LOWER WEB CRACKED. REPLACED FORWARD SERVICE DOOR IAW US AIRWAYS JOUVE TASK CARD 03C10652008. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 AALA200801958 1 20080725 A 3397 WIRE HARNESS BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 699AN 27051 MIA EMERGENCY LIGHT AT SEAT 17DEF INOPERATIVE. SECURED WIRING HARNESS FOR EMERGENCY LIGHT AT SEAT 17DEF. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 AALA200801953 1 20080725 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 342AN 33081 DFW EMERGENCY LIGHT AT OVERHEAD SEAT 9E INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 9E. SYSTEM GRO UND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20080910 NM 2008 9 10 USAA920081579 1 20080824 A 5752 654645521C TAB BOEING 737 7373B7 1384580 NM AILERON DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT - Q6 - MAJOR REPAIR - NR 03C30627004/001 - LEFT AILERON TAB OUTBOARD AFT CORNER DELAMINATED. REPAIRED LEFT AILERON TAB OUTBOARD AFT CORNER IAW B737 SRM 57-60-01 AND 51-70-16. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 AALA200802002 1 20080730 A 2421 GENERATOR BOEING 777 777223 1385213 NM LEFT FAILED A AALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SW 21 770AN 29578 MIA INFLIGHT T869/30JUL. CREW REPORTED LT INTEGRATED DRIVE GENERATOR FILTER BLOCK MESSAGE. DISCONNECTED LT INTEGRATED DRIVE GENERATOR. RT INTEGRATED DRIVE GENERATOR DROPPED OFF LINE. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACE D LT AND RT HAND INTEGRATED DRIVE GENERATORS AND LT HAND INTEGRATED DRIVE GENERATOR OIL COOLER. SYSTEM GROUND CHECKED N ORMAL OPS. (CLOSED) 2 L 7 2 4F RT T00001SE 20080910 NM 2008 9 10 AALA200802025 1 20080805 A 2597 WIRE BOEING 757 757223 1384957 NM PSU SHORTED A AALA G A O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 192AN 32386 LAX INFLIGHT T31/05AUG. CREW REPORTED SMOKE FILLING CABIN. DROPPED OXYGEN MASKS. FLIGHT ATTENDANTS REPORTED RT HAND S IDE OXYGEN MASKS DID NOT DROP. FLIGHT ATTENDANTS MANUALLY DROPPED MASKS AND OXYGEN DID NOT FLOW. RETURNED TO LAX AND L ANDED WITHOUT INCIDENT. DEPLOYED SIX SLIDES FOR EMERGENCY EVACUATION. FERRIED AIRCRAFT TO TUL FOR EVALUATION AND REPAI RS OF PASSENGER SERVICE UNITS (PSU). FOUND SHORED WIRE AFT OF MID GALLEY AND REPAIRED. AL PSUS SENT TO SHOP FOR INSPEC TION AND REINSTALLED. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 WP 2008 9 10 CNMA20080007 1 20080822 A 3397 WIRE DOUG DC10 DC1030 3023501 WP EMERGENCY LIGHT BURNED A CNMA K NONE O OTHER IN INSP/MAINT 1 SW 07 810AX 48265 ON PREFLIGHT FOUND FWD SECTION EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: EXTENSIVELY TROUBLESHOT SYSTEM R&R FAULTY BATT ERY POWER SUPPLY AND BATTERY PACK. PERFORMED CONTINUITY POWER GROUNDED CHECKS OF ALL FUNCTIONS AND SWITCHES. REPLACED CHARRED WIRE BETWEEN PIN M&N OF POWER SUPPLY CONNECTOR. TIGHTENED LOOSE POWER WIRE OF R1 DOOR OVERHEAD LIGHT ASSY IAW DC10 M/M DC 10-30 WDM 33-52 SYSTEM OPERATES NORMAL AND DC 10-30 33-51. 2 L 7 3 4F A22WE 20080910 WP 2008 9 10 AALA200801928 1 20080722 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9621A 53592 AUS OVERHEAD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5100 FOR OVERHEAD EMERGENCY LIGHTS IN CAB IN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A6WE 20080910 NM 2008 9 10 USAAEMB08012 1 20080828 A 5210 BRACKET EMB ERJ190 ERJ190100IGW 3260408 NM L1 DOOR BENT A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 948UW 19000081 CLT THE L1 DOOR PNEUMATIC ASSIST STRIKER BRACKET WAS FOUND BENT. MX REPLACED THE L1 DOOR PNEUMATIC ASSIST ASSEMBLY. OK FOR SERVICE. 2 L 7 2 4F RT A57NM 20080910 2008 9 10 USAAEMB08013 4 20080828 A 2565 1040031 SLIDE EMB ERJ190 ERJ190100IGW 3260408 NM L1 DOOR COLLAPSED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 948UW 19000081 CLT THE REPLACEMENT SLIDE FOR THE L1 DOOR WAS FOUND COMING APART. MX RETURNED THE DISCREPANT SLIDE TO STOCK AND INSTALL ED NEW SLIDE. OK FOR SERVICE. 2 L 7 2 4F RT A57NM 20080910 2008 9 10 USAABB08141 4 20080827 A 2565 D31041147 SLIDE BOEING 757 7572S7 1384962 NM R3 DOOR LOW A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 904AW 50626 23566 THE R3 DOOR EMERGENCY ESCAPE SLIDE PRESSURE WAS FOUND LOW. MX REPLACED THE R3 DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERV ICE. 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 AALA200802004 1 20080731 A 3350 8200008731 LIGHT BOEING 767 767323 1385205 NM FUSELAGE MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 39356 24037 ORD EMERGENCY LIGHT SIGN AT LT NR 1 DOOR MISSING LIGHT. REPLACED SIGN LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LT NR 1 DOO R. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20080910 WP 2008 9 10 AALA200801964 1 20080726 A 1100 PLACARD DOUG DC9 DC982 3022082 WP COCKPIT DOOR DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 LGA EMERGENCY PLACARD AT COCKPIT DOOR UNREADABLE. REPLACED EMERGENCY PLACARD AT COCKPIT DOOR. SYSTEM GROUND CHECKED NO RMAL OPS. (CLOSED) 2 L 7 2 4F A6WE 20080910 2008 9 10 USAA920081566 4 20080823 A 2565 D30664109 SLIDE AIRBUS 320 A320231 3930325 EU R1 DOOR LOW A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 622AW 48624 6909 054 LOG PAGE 4420739 - FLT NR 352 - PHX - EES -R-1 DOOR SLIDE/RAFT PRESSURE LOW (BELOW GREEN BAND). MAINTENANCE REMOVED AND REPLACED R-1 DOOR SLIDE/RAFT. 2 L 7 2 4F RT A28NM 20080910 EA 2008 9 10 COMA086366 1 20080823 A 2760 SPOILER SYS CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A COMA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 27 804CA 7352 RT FLT SPOILER MSG APPEARED ON APPROACH INTO JFK. EMERGENCY DECLARED, ACFT LANDED SAFELY. CORRECTIVE ACTION: RESET SPO ILER SYSTEM PER CRJ FIM FAULT RESET. NOR FURTHER DEFECTS NOTED. 2 L 7 2 4F RT A21EA 20080910 NM 2008 9 10 AALA200801992 1 20080728 A 3397 INSULATOR BOEING 777 777223 1385213 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW EXTERIOR EMERGENCY LIGHT AT RT NR 4 DOOR INOPERATIVE. SECURED INSULATOR SLEEVE FOR EXTERIOR EMERGENCY LIGHT AT RT N R 4 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT T00001SE 20080910 NM 2008 9 10 USAA920081569 1 20080811 A 5755 SKIN BOEING 737 7373G7 1384595 NM SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - C19 MAJOR REPAIR - NR 6124220 - NR 0 SPOILER DELAMINATED ON OUTBOARD LOWER SURFACE AT WS 492.93 TO 495.93. REPAI RED NR 0 SPOILER ON OUTBOARD LOWER SURFACE AT WS 492.93 TO 495.93 IAW B737 SRM51-70-10-2R4 REPAIR 4. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 USAA920081571 1 20080824 A 5523 65C2638428 TAB BOEING 737 7373B7 1384580 NM RT ELEVATOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT - Q6 - MAJOR REPAIR - NR 03C71227005/002 & JOB CARD 03C71227004 - SKIN CRACKED AND DISBONDED ON RT ELEVATOR TAB FOR WARD INBOARD LOWER SURFACE AT ELEVATOR STA. 124.047. REPLACED RT ELEVATOR TAB IAW JOB CARD 03C71227004. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 USA2008F00024 1 20080823 A 7711 EPR SYSTEM BOEING 757 7572S7 1384962 NM RROYCE RB211 RB211535E4 54555 NE INOPERATIVE A USAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 19 906AW 23568 30578 PHX FLT 146 ENROUTE PHX TO LIH. THE FLIGHT REJECTED TAKE-OFF DUE TO NO EPR INDICATION AND AUTO THROTTLES WOULD NOT ENGA GE. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MX CYCLED THE THRUST MANAGEMENT COMPUTER (TMC) CIRCUIT BREAKER. PERFORMED BITE CHECK OF TMC AND EPR SYSTEMS. SYSTEMS TEST OK. 2 L 7 2 4F 4 F RT A2NM E12EU 20080910 NM 2008 9 10 USAABB08139 1 20080823 A 3097 CONNECTOR BOEING 767 767201 1385125 NM WINDOW HEAT CORRODED A USAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 19 245AY 23897 CDG FLT 711 ENROUTE ZRH TO PHL. ABOUT TWENTY MINUTES AFTER DEPARTURE, THE COCKPIT CREW NOTED A STRONG ODOR. THE CREW A PPLIED QRH PROCEDURES, BUT THE ODOR DID NOT GO AWAY COMPLETELY. THE FLIGHT DIVERTED TO CDG AND LANDED WITHOUT FURTHER I NCIDENT. MX CLEANED CORROSION FROM CONNECTOR J5, D1670, FOR THE R1 OFFICER’S WINDOW HEAT SYSTEM. OPS CHECK O.K. 2 L 7 2 4F RT A1NM 20080909 NM 2008 9 9 2008UALA03843 1 20080710 A 2421 SHAFT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT AUX GENERATOR FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 214UA 30220 LEFT ELEC BACKUP GEN EICAS MESSAGE DISPLAYED. *S/D* SUSPECT SHEARED SHAFT. REPLACED BUG PER MM 24-25- 01, OPS CHECK G OOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 NM 2008 9 9 2008UALA03822 1 20080711 A 2133 27406504 ACTUATOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE OUTFLOW VALVE FAULTY A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 794UA 26953 OUTFLOW VALVE FWD AUTO CONTROL ON FORWARD OUTFLOW VALVE FAILED OR MANUAL MODE FOR FORWARD OUTFLOW VALVE SELECTED OR FAIL URE OF OUTFLOW VALVE FORWARD L AUTO CONTROL CHANNEL AND FAILURE OF OUTFLOW VALVE AFT R AUTO CONTROL CHANNEL OR FAILURE O F OUTFLOW VALVE FORWARD R AUTO CONTROL CHANNEL AND FAILURE OF OUTFLOW VALVE AFT L AUTO CONTROL CHA ADVISORY DB- AIR SUP MSG01- ACTIVE CRUISE MODE DEPENDENT; OUTFLOW VALVE CONTROL UNIT (FWD) OR ECU (R, FWD) MOTOR CONTROL CIRCUIT IS OPEN OR SHORTED. DB- AIR SUPPLY & CABIN PRESSURE R) MSG02- ACTIVE TAKEOFF ROLL MODE DEPENDENT; OUTFLOW VALVE (FWD) IS NOT IN CO MMANDED POSITION. DB- AIR SUPPLY. *S/D* FOUND VALVE CONTROL ACTUATOR ASSEMBLY FAULTY. REPLACED VALVE CONTROL ACTUATO 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 NM 2008 9 9 2008UALA03995 1 20080727 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ROW 16 INOPERATIVE A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 307UA 23668 CREW REPORT: DISCOVERED AFT EMERGENCY FLOOR LIGHTING INOP STARTING ROW 16. FOUND EEL STRIP WET AND STICKY. DRIED AND C LEANED STRIP. OPS CHKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 CALA0800775 1 20080806 A 5320 6545833435 CHANNEL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 CORROSION ON SUPPORT CHANNEL FOR NOSE LANDING GEAR VIEWER PANEL. REMOVED AND REPLACED SUPPORT CHANNEL WITH NEW CHANNEL AND REMOVED AND REINSTALLED UPPER VIEW TUBE PER BOEING DWG 65-45833 B737-300 SRM 51-40-02 AND B737-300 AMM 56-41-31. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 CALA0800776 1 20080806 A 5753 STRUCTURE BOEING 737 7373T0 1384582 NM RT WING TE FLAP DEFORMED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 RIGHT WING OUTBOARD MID FLAP DAMAGED ON TRAILING EDGE. REPAIRED DAMAGED AREA RT WING O/B MID FLAP TRAILING EDGE WEDGE R EF BOAC 737-300 SRM 51-70-10. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 2008UALA04004 1 20080726 A 2697 CONNECTOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FIRE LOOP FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 921UA 25388 CARGO DET FIRE LOOP 'B' RIGHT SIDE FAIL LIGHT. FOUND FAULTY SMOKE DETECTOR PLUG. REPLACED SMOKE DETECTOR PLUG OP CHECK GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 2008UALA04007 1 20080724 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 783UA 26950 AFT EMERGENCY LIGHT STRIP AT SEAT 1E MISSING. *S/D* FOUND LIGHT STRIP MISSING. REPLACED LIGHT STRIP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 NM 2008 9 9 2008UALA03959 1 20080722 A 2740 65860600U SHUTOFF VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 210UA 30216 EICAS STABILIZER R. *S/D* FOUND FAULTY SHUT OFF VALVE AND BAD CONNECTOR. REPLACED SHUT OFF VALVE AND CONNECTOR, OP CH ECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 EU 2008 9 9 2008UALA04078 1 20080731 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ROW 20C INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 407UA 456 EMERGENCY ESCAPE LIGHT INOP AT 20C. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA03867 1 20080712 A 2150 8102044 CONTROL VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FLOW CONTROL FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 778UA 26940 PACK R STATUS MESSAGE. *S/D* SUSPECT UPPER FLOW CONTROL SHUT OFF VALVE. REPLACED UPPER FLOW CONTROL AND SHUTOFF VALVE REF MM 21-51-01. OP CHECK NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 NM 2008 9 9 2008UALA03877 1 20080714 A 3350 58674 INVERTER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 382UA 24657 REPLACE LT OVERWING EXIT SIGN INVERTER MODULE. *S/D* FOUND LIGHT MODULE TO BE FAULTY. REPLACED THE LEFT OVERWING EXIT INVERTER MODULE, OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 2008UALA03351 1 20080612 A 2930 27802263 MODULE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RAT CHECKOUT FAULTY A UALA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 WP 29 210UA 30216 DURING LIGHT TEST GREEN ON LIGHT FOR RAT DID NOT COME ON. *S/D* SUSPECT FAULTY RAT CHECK OUT MODULE. REPLACED MODULE RERACKED A4 CARD, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 NE 2008 9 9 ASAA0853330 2 20080721 A 7200 3370051180 BULLET BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE NR 1 ENGINE WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 557AS 35176 892792 PER T C 78472000 NR 1 ENG HAS MORE 20 PERCENT BLACK ANODIZING COATING MISSING PER STEP 1(B) (2) (D) ON FWD SPINNER. NR 1 ENG FRONT SPINNER CONE TO BE REPLACED AT NEXT C-CHECK. REF AMM 72 21 01. REMOVED AND REPLACED NR 1 ENG FRONT SPINNER CONE REF MM 72 21 01. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080909 NM 2008 9 9 ASAA0853331 1 20080814 A 3097 286A2004001AS WIRE HARNESS BOEING 737 737890 1384527 NM WINDOW HEAT DAMAGED A ASAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 02 558AS 35177 EN ROUTE R SIDE WINDOW HEAT OVERHEAT LIGHT ILLUMINATED. SWITCH OFF PER QRH, THEN BACK ON, NORMAL OPS FOR DURATION OF FL T. FOUND PIN 1 ON COIL CORD TO BE INTERMITTENT OPEN. REMOVED AND REPLACED COIL CORD M2675. OPS TEST GOOD REF MM 30 41 00 WDM 30 41 11. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 2008UALA04091 1 20080804 A 2421 GENERATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FAILED A UALA C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 WP 29 588UA 26717 GENERATOR FAILURE INDICATION. TAKEOFF ABORTED AT 100 KNOTS. UNKNOWN IDG FAILURE. SHOP FINDINGS NFF. REPLACED IDG AND OPS CHECKED NORMAL. NO REPEATS. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 2008 9 10 USAAEMB08011 4 20080828 A 2565 1040031 SLIDE EMB ERJ190 ERJ190100IGW 3260408 NM L1 DOOR LOOSE A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 948UW 19000081 CLT THE L1 DOOR EMERGENCY ESCAPE SLIDE WAS FOUND PARTIALLY DEPLOYED. MX FOUND THE PRIMARY RELEASE PIN WAS FREED, AND TH E SLIDE DROPPED TO THE JETWAY. MX REPLACED THE L1 DOOR EMERGENCY ESCAPE SLIDE. 2 L 7 2 4F RT A57NM 20080908 EA 2008 9 8 QXEA200800666 1 20080622 A 2611 SENSOR CNDAIR CL600 CL6002C10 1390015 EA LAV SMOKE DETECT DIRTY A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 617QX 10130 SEA - FLIGHT 2514 - ON CLIMB RECEIVED A LAVATORY SMOKE WARNING. NO SMOKE OR FIRE NOTICED. WENT OUT IN 30 SECONDS. MAI NTENANCE FOUND THE SENSOR DIRTY. CLEANED AND OPERATIONAL CHECKED IAW 26-16-00-710-8D-A01. AIRCRAFT RETURNED TO SERVICE . NO PARTS REPLACED. (A) 2 L 7 2 4F RT A21EA 20080908 EA 2008 9 8 QXEA200800691 1 20080623 A 3310 LIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT SMOKE A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 608QX 10026 PDX - FLIGHT 2508 - F/O NOTICED PUFF OF SMOKE WHEN STOWING MAP LIGHT. DEACTIVATED BY PULLING C/B. PLACED ON MEL 33-11- 1. RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A21EA 20080908 NM 2008 9 8 QXEA200800700 1 20080630 A 3260 SENSOR BOMBDR DHC8 DHC8402 1390042 NM LT MLG DOOR OUT OF RIG A QXEA O OTHER N FALSE WARNING DE DESCENT 1 NM 09 410QX 4053 SEA - FLIGHT 2439 - DURING DESCENT AT 270 KIAS LT GEAR DOOR OPEN AND CLOSED UNCOMMANDED. AT 190 KIAS HAPPENED AGAIN. F ERRY SEA-PDX. RIGGED SENSOR RGD RCL IAW 32-61-06-830-801. RETURNED TO SERVICE. NO PARTS REPLACED. (A) 2 H 7 2 4T RT A13NM 20080908 2008 9 8 QXEA200800644 4 20080614 A 3420 42000332501 COMPUTER BOMBDR DHC8 DHC8402 1390042 NM NR 2 AHRS FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 430QX 2803 4163 BIL - FLIGHT 2598 (SEA-BIL) - RECEIVED A ELEVATOR CAUTION EN ROUTE. CONTINUE TO BIL. EMERGENCY DECLARED. LANDED WITHO UT INCIDENT. MAINTENANCE REPLACED THE NR 2 AHRU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 H 7 2 4T RT A13NM 20080908 NE 2008 9 8 QXEA200800663 2 20080620 A 7510 UNKNOWN DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE COCKPIT ODOR A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 09 347PH 480 PDX - UNUSUAL ODOR ON FLIGHT DECK ON THE GROUND. NOT MOVING FOR 10 MINUTES WITH BOTH ENGINES AND BLEEDS RUNNING. MAINT ENANCE RAN FOR 5 MINUTES BLEED ON, 5 MINUTES BLEED OFF. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED. (A) 2 H 7 2 4T 4 T RT A13NM E20NE 20080908 EA 2008 9 8 QXEA200800711 1 20080713 A 2611 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY MALFUNCTIONED A QXEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 602QX 7868 10010 SEA - FLIGHT 2544 - FIRE SYSTEM FAULT MESSAGE. PLACED THE SYSTEM ON MEL 26-00-1. RETURNED TO SERVICE. ON 7-14 REPLACE D THE NR 3 FORWARD BAGGAGE SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A21EA 20080908 EA 2008 9 8 TRAX200800936 1 20080727 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 926EV 7843 RT SIDE FUSELAGE STATION 621 OBLIQUE ANGLE CRACKED. REFERENCE MWC JOB 8784311, OP 48 FOR REPLACEMENT OF OBLIQUE ANGLES. REMOVED LT/RT FS 625 OBLIQUE ANGLES IAW SRM 51-42-21. LOCATED HOLES IN NEW SERVICEABLE OBLIQUE ANGLES IAW SRM 51-40-1 1. INSTALLED NEW SERVICEABLE FS 625 OBLIQUE ANGLES IAW SRM 51-42-21. (A) 2 L 7 2 4F RT A21EA 20080909 NM 2008 9 9 2008UALA03821 1 20080710 A 2750 15441007 PCU BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE LT WING TE FLAP FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 223UA 30224 STATUS MSG01- LATCHED INITIAL CLIMB MODE DEPENDENT; FLAPERON POWER CONTROL UNIT (LEFT OUTBOARD) DOES NOT FOLLOW COMMAND. DB-PRIMARY FLIGHT COMPUTER (RIGHT) MSG-2710301 LATCHD IC MODE. *S/D* FOUND FLAPERON POWER CONTROL UNIT FAULTY. REPL ACED LEFT O/B FLAPERON POWER CONTROL UNIT PER MM 27-11-12 PG 401. RIG AND OPS CK GOOD PER MM 27-11-00 PG 501. AC OK FO R SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 NM 2008 9 9 2008UALA04094 1 20080804 A 3233 1809308 ACTUATOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MLG FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 179UA 25158 GEAR RETRACTION PROBLEM. RTFL. REPLACED RT BLG TILT ACTUATOR. NO SHOP DATA FOR ROOT CAUSE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080909 NM 2008 9 9 2008UALA04028 1 20080726 A 3397 78941 WIRE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE EMERGENCY LIGHT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 786UA 26938 EMERGENCY LIGHT ON SEAT 3E AFT SIDE INOP. *S/D* FOUND BROKEN WIRE ON LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHEC KED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 NM 2008 9 9 CALA0800753 1 20080802 A 5240 654585103 ANGLE BOEING 737 737524 1384721 NM R2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 Z-ANGLE AT R2 DOOR HAS CORROSION. REMOVED AND REPLACED R2 Z-ANGLE REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 CALA0800755 1 20080802 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 66056 29451 DURING EMERGENCY LIGHT OPS CHECK, CENTER ROW SEAT LIGHTS DID NOT COME ON AT SEATS 5D THRU 7D. FOUND BAD POWER SUPPLY ON THE RT SIDE OF A/C AT SEAT ROW 6KL. REMOVED AND REPLACED POWER SUPPLY UNIT PER AMM 33051-07, OPERATION CHECKS GOOD. 2 L 7 2 4F RT A1NM 20080909 NM 2008 9 9 CALA0800771 1 20080805 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 787 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16632 27900 FRAME CRACKED STATION 787 AT S-9R. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLERS REF EA 5310-04498. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 2008UALA03878 1 20080714 A 3350 58674 INVERTER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 307UA 23668 LT OVERWING ESCAPE HATCH EXIT SIGN INOP. *S/D* FOUND INVERTER MODULE FAULTY. REPLACED EXIT SIGN INVERTER MODULE, OPS CHECKED OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 EU 2008 9 9 2008UALA04092 2 20080804 A 7200 1461M14P04 BEARING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 ENGINE SEIZED A UALA A UNSCHED LANDING R Y J PARTIAL RPM/PWR LOSS ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 WP 29 381UA 24656 724316 NR 1 ENGINE FAILURE. RTFL. ENG 1 STALLED AT 1,000' FOR 5 SEC, ENG SEIZED, OIL PRESS & N1 DROPPED TO ZERO, COMPLETED EN G SHUTDOWN. PROCEDURE, FLT AIRBORNE FOR 11 MIN, SMOKE IN CABIN, BLEEDS SHUTOFF WHICH CLEARED SMOKE, EMERGENCY DECLARED. NO EXCEEDANCE REPORTED, UPON ARRIVAL FOUND OIL DRIPPING FROM 7'0 CLK DRAIN HOLE AT TURB EXHAUST, UNABLE TO SEE OIL LEV EL IN TANK, FLT DECK ENG 1 OIL QTY IND READ 36, ENG 2 AT 100. SPINNER & TAIL PIPE HAVE NO EVIDENCE OF OIL LEAK. FBO RE PORTS FORWARD SUMP SCAVENGE CHIP DETECTOR (MIDDLE MAGNETIC C-D) IS FULL OF METAL. THE ENGINE WAS REPLACED. NO ADDITION AL FINDINGS DATA IS EXPECTED DUE TO RETIREMENT OF THE FLEET. FOUND FAILURE OF NR 3 BEARING. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 EU 2008 9 9 2008UALA03921 1 20080723 A 5753 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT WING TE FLAP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 433UA 589 RT WING O/B FLAP HAS A REPAIR OF 8 INCHES BY 15 INCHES ON LOWER TRAILING EDGE. THE TRAILING EDGE OF REPAIR IS SEPARATIN G FROM FLAP. *S/D* REPAIRED FLAP. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NE 2008 9 9 2008UALA04041 2 20080728 A 7532 D7532538000060 BLEED VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 485UA 1617 V10021 NR 1 ENGINE EGT OVERTEMP. RTFL. *S/D* FAULT 10TH BLD VLV SOL-HC-EEC1, NR 1 ENGINE. REPLACED 10TH BLD VLV SOL-NR 1 EN GINE. ACCOMPLISHED HIGH POWER RUNS, ALL CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA04070 1 20080730 A 5322 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1680 S28-29L CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 AFT PIT AT STA 1680 BETWEEN STR 28L AND 29L SHEAR TIE CORRODED. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. FABBED NEW SH EAR TIE REF BOEING DWG 140N2002 AND INSTALLED REF SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E17NE 20080909 NM 2008 9 9 ASAA0843338 1 20080801 A 5330 65C3576813 SKIN BOEING 737 737490 1384715 NM BS 366-377 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 REF SAD 6311478: DENT ON RT SIDE OF FUSELAGE AT APPROX STA 370 WL 206. DENT IS COMMON TO STR 17R. REMOVED DAMAGED AREA , FABBED FILLER DOUBLER & TRIPLER & INSTALLED REPAIR IAW ASA EA 5330 02379. REF LG PG 5130589 FOR REINSPECTION INFO. F LIGHT CYCLES AT INSTALL = 18874. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 ASAA0853344 1 20080817 A 2421 28B5457 GENERATOR BOEING 737 737890 1384527 NM APU FAULTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 558AS 5222 35177 APU MAINT LIGHT COMES ON WHEN SWITCHING APU GEN SWITCH 1 TO ON. VERIFIED FAULT APU SHOWED FAILED GEN DIODE MESS 49 4124 4. REMOVED AND REPLACED APU STARTER GEN PER MM 49 41 21 000 801. SYSTEM CHECK GOOD PER MM 49 41 21 000 801. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 ASAA0893346 1 20080816 A 5240 DOOR BOEING 737 737990 NM R2 STIFF A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 309AS 26820 30857 FLIGHT ATTENDANT REPORTS: R2 DOOR IS DIFFICULT TO OPERATE. OPS CHECK R2 DOOR. NO DEFECTS NOTED. NO HISTORY WITHIN 90 DAYS. REFERENCE AMM 52 41 00. 2 L 7 4 4F RT A16WE 20080909 NM 2008 9 9 ASAA0843339 1 20080808 A 5753 SKIN BOEING 737 737490 1384715 NM RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 RT INBOARD FORE FLAP HAS MULTIPLE SMALL DENTS ON LOWER SURFACE ABOVE NR 3 & 4 TIRES 2 DENTS ON PREVIOUS REPAIRS. REMOVE D DAMAGED AREA, FABBED FILLERS & DOUBLERS & BONDED REPAIRS IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 ASAA0843340 1 20080803 A 5753 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 LT OUTBOARD T/E AFT FLAP HAS NUMEROUS DENTS ON THE LOWER SURFACE. REMOVED DAMAGED AREA, FABBED FILLER & DOUBLER & BONDE D THE REPAIR PARTS IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 ASAA0843336 1 20080803 A 5755 SKIN BOEING 737 737490 1384715 NM NR 6 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 NR 6 SPOILER HAS SEVERAL DENTS ON TOP. PREPPED DAMAGED AREA, FABBED DOUBLERS 2 EA & BONDED REPAIRS IAW B737 400 SRM 51 70 10. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 ASAA0843341 1 20080812 A 5755 SKIN BOEING 737 737490 1384715 NM NR 7 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 NR 7 SPOILER IS DENTED ABOVE THE ACTUATOR ON THE UPPER SURFACE. REMOVED DAMAGED AREA, FABBED DOUBLER & INSTALLED REPAIR IAW B737 400 SRM 57 70 01 REPAIR 4. 2 L 7 2 4F RT A16WE 20080910 WP 2008 9 10 AALA200802001 1 20080730 A 3350 922710127 RELAY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 472AA 49647 LGA EMERGENCY LIGHT AT EXTERIOR OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK CONTROL RELAY FOR EMERGENCY LIGHT AT E XTERIOR OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F A6WE 20080910 NM 2008 9 10 AALA200802029 1 20080805 A 3350 MODULE BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 181AN 29591 DFW EMERGENCY LIGHT AT RT NR 1 EXIT DOOR INOPERATIVE. REPLACED EXIT SIGN MODULE FOR EMERGENCY LIGHT AT RT NR 1 EXIT DOO R. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 EU 2008 9 10 USAA920081564 1 20080824 A 3350 1013585 LIGHT AIRBUS A319 A319112 3930323 EU ROW 16A INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 714US 1046 LOGPAGE 7896719 FLT848 PHL EEL ROW 16A SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. R&R EMERGENCY LIGHT ASSEMBLY. OPS CHE CK WAS GOOD. 2 L 7 2 4F RT A28NM 20080910 NM 2008 9 10 AALA200801944 1 20080723 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 391AA 27451 MIA EMERGENCY LIGHT AT OVERHEAD SEAT 25B INOPERATIVE. CHARGED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT 25B. S YSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20080909 NM 2008 9 9 2008UALA03341 1 20080613 A 2421 745329A IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FAULTY A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 642UA 25092 AT TOC HAD LEFT ELEC BUSS POWER PROBLEM OF A TRANSITORY NATURE WHICH MOMENTARILY BLANKED CAPT'S EADI AND EHSI. *S/D* SUSPECT FAULTY BEARING IN IDG. REPLACED NR 1 IDG ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080909 NM 2008 9 9 2008UALA03837 1 20080710 A 3350 362624 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE SEATS 18C & 31C INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 220UA 30223 EMERGENCY LIGHT OUT AT SEATS 18C AND 31C. *S/D* SUSPECT LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 NM 2008 9 9 08FDEA03666 1 20080901 A 5311 AFA00273 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 594FE 48552 MAIN DECK CARGO AT STA 1661 JUST BELOW LONGERON 12 RIGHT HAND FRAME FOUND DAMAGED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION IS REQUIRED AT 14,500 CYCLES AND REPETITIVE INSPECTION AT EVERY 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080909 NM 2008 9 9 08FDEA03667 1 20080901 A 5311 AFA00203 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 594FE 48552 MAIN DECK CARGO AT STA 1701 JUST BELOW LONGERON 12 RT FRAME FOUND DAMAGED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INPSECTION REQUIRED AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080909 EU 2008 9 9 2008UALA04159 1 20080807 A 2910 DRAIN VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD SYSTEM LEAKING A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 427UA 512 HYDRAULIC GREEN SYSTEM LOW LEVEL DISPLAYED. FOUND DRAIN VALVE LEAKING. REPLACED DRAIN VALVE AND SERVICED HYD SYSTEM. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA04178 1 20080808 A 2421 734285E GCU BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LEFT FAILED A UALA C ABORTED TAKEOFF H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 668UA 30024 LT GEN FAILED TO ROLL ON POWER THRUST REJECTED AT 40 KNOTS. SUSPECT FAULTY IDG. REPLACED IDG. NO VOLTS OR FREQS. FOUND NR 1 GCU FAULTY. REMOVED AND REPLACED GCU. OP CKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20080909 2008 9 9 2008UALA03922 4 20080723 A 2565 D31517113 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 433UA 589 TEST OF EMERGENCY LIGHT SYSTEM SHOWS AFT EXTERNAL LOAD FAULT. *S/D* INTERNAL SHORT/HIGH RESISTANCE IN SLIDE 2L. REMOV ED AND REPLACED 2R DOOR SLIDE, OPS TEST ARE NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA04030 1 20080729 A 5330 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1500 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 AFT PIT STA 1500 FRAME INNER FLANGE DENTED IN 2 EACH PLACES AT S-25L AND 26L. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED PRODUCTION SPLICE AND TRIMMED OUT DAMAGED AREA, ACP'D HFEC INSP FOR DAMAGE REMOVAL AND NO DEFECTS FOUND PER NDT 6-51-00-16. ACP'D INSURANCE CUT, FABRICATED AND INSTALLED A REPAIR ANGLE PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 20080909 NM 2008 9 9 ASAA0843337 1 20080801 A 5330 65C357987 SKIN BOEING 737 737490 1384715 NM BS 911-922 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 REF SAD 6250170: FUSELAGE SKIN DENT 6' AFT OF AFT CARGO DOOR. DENT IS CREASED LOCATED AT STA 917 BELOW STR 23R. REMOV ED DAMAGED AREA, FABBED DOUBLER & INSTALLED REPAIR IAW ASA EA 5330 02378. REF LG PG 5130588 FOR REINSPECTION INFO. FLI GHT CYCLES AT INSTALL = 18874. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 ASAA0843334 1 20080801 A 5347 654652861 CARGO TRACK BOEING 737 737490 1384715 NM BS 480-500 BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 FWD CARGO PIT LT CARGO TIE DOWN TRACK HAS A BROKEN LUG FOR THE AFT NET ATTACHMENT. REMOVED DAMAGED SECTION OF TRACK, FA BBED REPLACEMENT TRACK & REPAIR PARTS & INSTALLED IAW B737 400 SRM 53 00 53 FIG 201. 2 L 7 2 4F RT A16WE 20080909 2008 9 9 ASAA0853343 4 20080818 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM MALFUNCTIONED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 577AS 5782 35186 FMC DISAGREE LIGHT CAME ON. RESET FMCS CMPTR 1 & 2 CBS. PERFORMED BITE CHECK OF FMC COMPUTERS L&R PER FIM 34 61 00, NO CURRENT FAULTS NOTED. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 ASAA0843345 1 20080815 A 5210 AN3167R NUT BOEING 737 7374Q8 138447Q NM L1 GUIDE ARM LOOSE A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 776AS 25109 L1 DOOR VERY STIFF HARD TO OPEN. PERFORMED VISUAL INSP OF L1 DOOR FOUND GUIDE ARM LOCK NUT LOOSE. TIGHTENED LOCK NUT I AW AMM 52 11 00 705 007 B00. PERFORMED FWD ENTRY DOOR TEST IAW AMM 52 11 00 755 051 B00. OPS CK GOOD. NO FURTHER DEFE CTS NOTED AT THIS TIME. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 ASAA0843335 1 20080803 A 5753 SKIN BOEING 737 737490 1384715 NM RT WING TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 RT INBOARD AFT FLAP UPPER SURFACE IS CHAFED AT WBL 82. PREPPED DAMAGED AREA, FABBED DOUBLER & BONDED REPAIR IAW B737 40 0 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 ASAA0843342 1 20080803 A 5755 SKIN BOEING 737 737490 1384715 NM NR 4 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 706AS 28894 LT WING INBOARD GROUND SPOILER NR 4 HAS SEVERAL DENTS ON THE LOWER SURFACE. PREPARED DAMAGED AREA, FABBED DOUBLERS & BO NDED THE REPAIRS IAW B737 400 SRM 51 70 10. 2 L 7 2 4F RT A16WE 20080909 CE 2008 9 9 DGC2008F00001 1 20080818 A 2913 PF24390615BCES62 PUMP RKWELL NA265 NA26565 7630107 CE GARRTT TFE731 TFE7313R1D 01518 WP HYD SYSTEM INOPERATIVE A DGCA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 CE 03 570R 4513 46575 ON AUGUST 16, 2008, AT APPROXIMATELY 8:30 AM, AFTER LANDING, THE CREW HEARD AUDIBLE WARNING OF HYDRAULIC SYSTEM LOW PRES SURE. THE AC TAXIED TO THE RAMP OF DESTINATION, WITHOUT INCIDENT. UPON INVESTIGATION, THE HYDRAULIC PUMP WAS FOUND TO HAVE FAILED. (K) 2 L 7 2 4J 4 F A2WE E6WE 20080909 NM 2008 9 9 08FDEA03650 1 20080831 A 5330 65545732 SKIN BOEING 727 727227 1384078 NM BS 662 S28L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 FWD CARGO COMPARTMENT, SKIN UNDER STRINGER 28L IS CORRODED AT STA 662 JUST I/B OF EXISTING REPAIR CUTOUT. REMOVED CORRO SION AND FOUND OUT OF LIMITS IAW SRM 51-10-6 AND 53-30-1 FIG 1. REMOVED EXISTING REPAIR IAW SRM 51-30-2. CUTOUT DAMAGE D AREA DIM 5" PER 1 3/4' AND FABRICATED NEW DOUBLER IAW SRM 53-30-3 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INS TALLED REPAIR DOUBLER AT FWD CARGO COMPARTMENT SKIN STRINGER 28L , STA 662 IAW SRM 53-30-3 FIG 1 AND 51-30-2. 2 L 7 3 4F A3WE 20080910 NM 2008 9 10 AALA200802015 1 20080802 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AA 24589 ORD EMERGENCY LIGHT SHROUD AT SEAT 17D MISSING. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 F3LA200800585 1 20080823 A 5320 D5347217220400 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 928FR 2236 REFERENCE NON ROUTINE CO50117. DURING C3 C-CHECK, INSP NOTED LT FLOOR SUPPORT Y1292 HAS CORROSION IN VARIOUS NUT CLIP H OLES FROM FRAME 66 TO FRAME 68 (L2 DOOR AREA). MX R&R THE FLOOR SUPPORT IAW THE REQUIREMENTS OF EA NR A9-53R-30587. UP ON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20080910 NM 2008 9 10 AALA200801950 1 20080724 A 3350 D71701002 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 915AN 29516 LAX SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 7 TO 11 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 7 TO 11. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 AALA200801945 1 20080723 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 391AA 27451 MIA EMERGENCY LIGHT AT OVERHEAD SEAT 28B INOPERATIVE. CHARGED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT 28B. S YSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20080910 NM 2008 9 10 AALA200801943 1 20080723 A 3350 7024092007 INDICATOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 391AA 27451 MIA EMERGENCY LIGHT AT SEAT 20A MISSING INDICATOR CAP. REPLACED INDICATOR CAP FOR EMERGENCY LIGHT AT SEAT 20A. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20080910 NM 2008 9 10 AALA200801987 1 20080727 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 794AN 30256 DFW EMERGENCY LIGHT AT OVERHEAD SEAT 1D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 1D. SYSTEM GRO UND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT T00001SE 20080910 NM 2008 9 10 AALA200801942 1 20080723 A 3397 WIRE BOEING 767 767323 1385205 NM EMERGENCY LIGHT SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 391AA 27451 MIA EMERGENCY LIGHTS AT SEAT ROWS 25B TO 31B INOPERATIVE. FOUND SHORTED WIRES AT SEAT 28B. REPLACED SOCKET AND CONNECT OR AT SEAT 28B FOR EMERGENCY LIGHTS AT SEAT ROWS 25B TO 31B. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20080910 NM 2008 9 10 USAA920081570 1 20080825 A 5330 6545775 SKIN BOEING 737 7373B7 1384580 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 23595 CLT - RON - MAJOR REPAIR - LOG 4393963 - FUSELAGE SKIN CRACKED AT BS761 & 765, S19R. REPAIRED FUSELAGE SKIN AT BS761 & 765, S19R IAW B737 SRM 53-00-01 REPAIR 31, TEMPORARY REVISION 53-33. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 USAA920081568 1 20080822 A 5754 SKIN BOEING 737 7373B7 1384580 NM ZONE 600 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 344 23702 CLT - Q6 - MAJOR REPAIR - NR 03C40257009/003 - DELAMINATION ON NR 5 SLAT LOWER SURFACE OUT BOARD TRAILING EDGE. REPLACE D NR 5 SLAT. 2 L 7 2 4F RT A16WE 20080910 NE 2008 9 10 COMA086369 2 20080822 A 7261 4138T09P03 CARBON SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30068 NE RT ENGINE WORN A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 957CA 7109 ENROUTE FROM CLE TO JFK RECEIVED RT ENGINE OIL PRESS WARNING MSG. FOLLOWED QRH, EMERGENCY DECLARED PERFORMED IFSD OF RT ENGINE. ACFT DIVERTED TO AVP AND LANDED SAFELY. CORRECTIVE ACTION: FOUND IDG CARBON SEAL (AGB AXIS BB) LEAKING. R&R CARBON SEAL. 2 L 7 2 4F 4 F RT A21EA E15NE 20080910 NM 2008 9 10 AALA20081986 1 20080727 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AM 24594 DFW SEAT MOUNTED EMERGENCY LIGHTS AFT OF FIRST CLASS TO SEAT ROW 15D INOPERATIVE. REPLACED BATTERY PACK M10798 FOR EMER GENCY LIGHTS AFT FIRST CLASS TO SEAT ROW 15D. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 AALA200801936 1 20080722 A 5320 145T87562 STIFFENER BOEING 767 767323 1385205 NM MLG WW DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7375A 25202 AFW MAIN LANDING GEAR PRESSURE DECK LONGITUDINAL STIFFENER HAS A HOLE IN THE UPPER OUT BOARD FLANGE AT RT BUTTLINE 5.75 STATION 1045. REPAIRED PER MRB 767 3250. (CLOSED) 2 L 7 2 4F RT A1NM 20080910 EU 2008 9 10 AALA200801995 1 20080729 A 7830 681L270G06 RVDT AIRBUS 300 A300B4605R 3930308 EU THRUST REVERSER SEPARATED A AALA O OTHER D INFLIGHT SEPARATION LD LANDING 1 SW 21 77080 626 JFK INFLIGHT T1892/29JUL. ON ROLL OUT LARGE SECTION OF NR 2 THRUST REVERSER DEPARTED ACFT. REPLACED NR 2 OUTBOARD REVE RSER. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A35EU 20080910 NM 2008 9 10 2008UALA04256 1 20080811 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY LIGHT DOOR 2R DAMAGED. REPAIRED WIRE AND LIGHT ASSEMBLY OP CHECK GOOD. ACFT OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080910 NM 2008 9 10 2008UALA04281 1 20080813 A 2800 UNKNOWN BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FUEL TRANSFER UNKNOWN A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 209UA 30215 CREW REPORT: FUEL APPEARS TO TRANSFER TO THE RT TANK AT 600-HR OR MORE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080910 NM 2008 9 10 USAA920081572 1 20080820 A 5320 BAC1493577 SUPPORT BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT - Q6 - MAJOR REPAIR - NR 03C10753005/005 - STABILIZER SUPPORT CRACKED BETWEEN BS312 & 328, BLO. REPLACED STABILIZER SUPPORT BETWEEN BS312 & 328, BLO IAW B737 SRM 53-10-51. 2 L 7 2 4F RT A16WE 20080910 2008 9 10 CNMA20080006 2 20080727 A 7200 AYG70555513 MANIFOLD DOUG DC10 DC1030 3023501 WP MALFUNCTIONED A CNMA O OTHER O OTHER NR NOT REPORTED 1 SW 07 621AX 48319 LOST NR 3 AND SYSTEM WITH EVEN OFF LIGHT. R & R NR 3 SYSTEM FILTER MANIFOLD. IAW MM 29-10 2 L 7 3 4F A22WE 20080910 EA 2008 9 10 COMA086368 1 20080824 A 2911 ACCUMULATOR CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM EMPTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 962CA 7123 ON APPROACH INTO DAY RECEIVED PARKING BRAKE SOV AND 1/B ANTI-SKID MSG WHEN GEAR WAS LOWERED. EMERGENCY DECLARED, ABORTE D APPROACH. ACFT LANDED SAFELY ON 2ND APPROACH. FOUND NR 3 HYD BRAKE ACCUMULATOR (I/B BRAKES) TO HAVE ZERO PRESS. SER VICED ACCUMULATOR. NO FURTHER DEFECTS NOTED. 2 L 7 2 4F RT A21EA 20080910 NM 2008 9 10 AALA200801926 1 20080722 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 386AA 27060 BOS SEAT MOUNTED EMERGENCY LIGHT AT SEAT 6B INOPERATIVE. SECURED CONNECTOR FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 6B. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20080910 EA 2008 9 10 COMA086363 1 20080824 A 5210 FRAME CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 779CA 7306 PAX DOOR INNER FRAME AT 335.7 IS CRACKED. CORRECTIVE ACTION: REPLACED FRAME AT FS335.7 PER CRJ SRM CH 51-42-06 PG 1-10 AND 51-42-20 PG 1-19. 2 L 7 2 4F RT A21EA 20080910 EA 2008 9 10 COMA086365 1 20080821 A 3230 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 27 451CA 7562 ON APPROACH, RECEIVED TWO MASTER WARNINGS, ONE FOR NOSE GEAR OPEN, THE OTHER FOR GEAR DISAGREE. ABORTED APPROACH, RAN Q RH, MANUALLY EXTENDED GEAR, LANDED WITHOUT INCIDENT WITH GEAR INDICATING GREEN. REPLACED NLG SELECTOR VALVE. NO FURTHE R DEFECTS. 2 L 7 2 4F RT A21EA 20080910 EU 2008 9 10 MAL2008F00029 1 20080822 A 7160 INTAKE DUCT SAAB SF340 340B 7860101 EU LEFT DAMAGED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 428XJ 340B428 IN FLIGHT THE ODOR OF BURNED RUBBER FILLED THE FLIGHT DECK FOLLOWED BY ICE PROTECTION LOOK UP LIGHT AND LEFT INTAKE LIGH T. R&R LT LOWER INTAKE DUCT. 2 L 7 2 4T RT A52EU 20080910 NM 2008 9 10 AALA200801925 1 20080722 A 2530 CHILLER BOEING 767 767323 1385205 NM GALLEY INOPERATIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 39367 25194 DEN INFLIGHT T073/22JUL ORD TO HNL. CREW REPORT SMOKE AND FUMES IN CABIN AT LT NR FOUR LAVATORY. CREW WAS ABLE TO CLEA R SMOKE. LANDED DEN WITHOUT INCIDENT. FOUND RT HAND AFT CHILLER CIRCUIT BREAKER POPPED AND HOT. REPLACED RT HAND AFT CHILLER. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20080910 NM 2008 9 10 AALA200802000 1 20080729 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 917AN 29518 DFS EMERGENCY FLOOD LIGHT AT FIRST CLASS OVERHEAD INOPERATIVE. REPLACED LAMP FOR EMERGENCY FLOOD LIGHT AT FIRST CLASS O VERHEAD. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 2008UALA04282 1 20080815 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 5A UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 SEAT 5A EEL LT STRIP NEEDS TO BE SECURED. FOUND LOOSE LIGHT ASSEMBLY. SECURED LIGHT ASSEMBLY OP CHECK GOOD. ACFT OK F OR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080910 NM 2008 9 10 2008UALA04284 1 20080814 A 3397 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 202UA 24717 EMERGENCY FLOOR MOUNTED STRIP LIGHTING ROWS 15-21 INOP. FOUND POWER FEEDER CABLE TO BE FAUTLTY. REPLACED POWER DISTRIB UTION STRIP AND ALL OPS NORMAL. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080910 NM 2008 9 10 2008UALA04285 1 20080814 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 5J UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 180UA 25224 SEAT 5J EMERGENCY LIGHT IS LOOSE. FOUND LIGHT UNSECURE. SECURED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 20080910 NM 2008 9 10 2008UALA04105 1 20080802 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 580 S24-25L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 FWD PIT STA 580 FRAME INNER FLANGE BETWEEN S-24L AND S-25L DENTED. ACCOMPLISHED MAJOR REPAIR AT GSO. CUT OUT DAMAGED F RAME SECTION AND INSTALLED DOUBLER REPAIR PER SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 NE 2008 9 10 2008UALA03992 2 20080728 A 7230 GUIDE VANE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE DAMAGED A UALA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 WP 29 647UA 45749 11602 25284 727366 BIRD STRIKE TO LT ENG. ABORTED TAKEOFF AT 120 KNOTS. *S/D* ACCOMPLISHED ENGINE CORE BORESCOPE INSPECTION, NO DAMAGE. FOUND 3 FAN EXIT GUIDE VANE BASES DAMAGED AT 4 O'CLOCK. REPAIRED PER AMM 72-33-02-801. SUBSEQUENT ENGINE GROUND RUNS OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080910 2008 9 10 2008UALA04292 4 20080812 A 2565 COVER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SLIDE CUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 807UA 798 FOUND DAMAGE TO SLIDE. BUSTLE TIE STRING CUT AND 3 INCH SLICE IN YELLOW SLIDE COVER. REPLACED DOOR 2L SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080910 NM 2008 9 10 2008UALA04283 1 20080814 A 5340 FITTING AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 803UA 748 AFT CARGO COMPARTMENT FLOOR SUPPORT FITTING CORRODED RT SIDE FRAME 59 UPPER FLANGE. ACCOMPLISHED MAJOR REPAIR AT LCQ-RE O-L01099 AND RAS-DAHAM-4 025656-2008 ON NR K8546B AND INSPECTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080910 NM 2008 9 10 2008UALA04288 1 20080815 A 3510 O-RING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW OXYGEN LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 CREW OXYGEN PRESSURE READ LOW. SUSPECT LEAKING O-RING. REPLACED O2 BOTTLE OP AND LEAK CHECK GOOD. ACFT OK FOR SERVICE . 2 L 7 4 4F 4 F RT A20WE E24NE 20080910 NM 2008 9 10 2008UALA00023 1 20080101 A 2611 8243 FIRE LOOP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 3 ENGINE FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 195UA 26899 THE 'ENG 3 FIRE LP B' EICAS STATUS MSG DISPLAYED. ENG 3 FIRE LOOP-B FIRE OR FAULT OUTPUT. *S/D* FOUND HIGH RESISTANCE LOWER AFT FIRE LOOP AND SHORT IN HARNESS. REPLACED LWR AFT FIRE LOOP, REPAIRED WIRE IN WIRE HARNESS, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080910 EU 2008 9 10 2008UALA04156 1 20080805 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 495UA 1842 CREW OXYGEN ON UPPER ECAM. *S/D* SERVICED CREW O2 TO FULL, NO LEAKS NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080910 NM 2008 9 10 2008UALA04266 1 20080813 A 5310 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 327UA 24147 FUSELAGE ON LEFT SIDE FWD OF ENGINE IS DENTED. 2 L 7 2 4F 4 F RT A16WE E21EU 20080910 NM 2008 9 10 2008UALA04267 1 20080813 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 L-2 DOOR REQUIRES REPAIR DOUBLER AT UPPER HINGE CUTOUT. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 NM 2008 9 10 2008UALA04268 1 20080813 A 3150 WARNING MESSAGE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 791UA 26933 FLIGHT CONTROL SYSTEM STATUS MESSAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080910 NE 2008 9 10 2008UALA04269 2 20080813 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LEFT HUNG START A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 666UA 29238 727850 LEFT ENGINE HUNG START AT 30 PERCENT N2. LEFT HYD QTY NOW LOW. 2 L 7 2 4F 4 F RT A1NM E24NE 20080910 NM 2008 9 10 2008UALA04271 1 20080813 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SEAT 3B MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 EMERGENCY EXIT LIGHT ASSEMBLY MISSING SIDE OF SEAT 3B. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 NM 2008 9 10 2008UALA03357 1 20080613 A 2530 2676 CHILLER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FWD GALLEY TRIPPED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 644UA 25094 SMOKE POSSIBLY ELECTRICAL IN BUSINESS GALLEY IN FLT. ALL POWER TO GALLEY SECURED. *S/D* FOUND CHILLER CIRCUIT BREAKER TRIPPED. REPLACED MID FWD GALLEY CHILLER, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080910 NM 2008 9 10 2008UALA04097 1 20080801 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 UPPER FUSELAGE SKIN PUNCTURED JUST AFT INBOARD SIDE OF THE TCAS ANTENNA. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. CUT OUT DAMAGE AND ACCOMP HFEC INSP PER NDT 51-00-19, PART 6, NO CRACKS NOTED. INSTALLLED DOUBLER AND FILLER REPAIR PER SRM 53-00-01, REPAIR 2. CURRENT PTC 18,24 5 CYC. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 NM 2008 9 10 CALA0800781 1 20080808 A 2121 4100941C FAN BOEING 767 767424ER 1385270 NM RIGHT NOISY A CALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 27 76062 28688 29457 LIGHT SMOKE AND FUMES ASSOCIATED WITH RIGHT RECIRCULATION FAN LEFT AND RIGHT RECIRCULATION FANS SELECTED OFF. CREW CONF IRMED RIGHT RECIRCULATION FAN THE CAUSE. PERFORMED CONDITIONAL INSPECTION PER 05-51-58 AND FOUND RIGHT RECIRCULATION FA N MAKING NOISE. FAN NIS LAX, PLACARD PER MEL 21-25-01C, ALSO COMPLIED WITH "SMOKE IN THE PLANE QUESTIONNAIRE. HNL REMO VED AND REPLACED RIGHT RECIRCULATION FAN PER AMM 21-25-01. OPERATIONAL AND LEAK CHECKS OK. 2 L 7 2 4F RT A1NM 20080910 NM 2008 9 10 2008UALA04235 1 20080810 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT EEL LIGHT INOP AT DOOR 4 LEFT FWD EXIT SIGN. FOUND FAULTY CABLE. REPLACED CABLE OP CHECK GOOD. ACFT OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080910 NM 2008 9 10 2008UALA04261 1 20080812 A 3150 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE INOPERATIVE A UALA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 WP 29 670UA 29240 NR 1 ENGINE GENERATOR DRIVE LIGHT NOT ILLUMINATED. 2 L 7 2 4F 4 F RT A1NM E24NE 20080910 2008 9 10 2008UALA04050 4 20080730 A 2565 416N2002843 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 588UA 26717 NR 1 RT MED SLIDE RAFT PRESSURE INDICATION NEEDLE IS AT LWR EDGE OF GREEN BAND. *S/D* UNKNOWN PRESSURE LEAK IN SLIDE. REPLACED NR 1 RT MED SLIDE RAFT. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 NM 2008 9 10 2008UALA04293 1 20080814 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 810UA 843 EMERGENCY LIGHTS TEST FAILED WITH EPSU L MESSAGE. FOUND FAULTY POWER SUPPLY. REPLACED LIGHT LENS ASSEMBLIES & LEFT EPS U UNDER LEFT OVERWING EMERGENCY EXIT. 2 L 7 2 4F 4 F RT A28NM E40NE 20080910 NM 2008 9 10 2008UALA04294 1 20080814 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 813UA 858 CAPTAIN'S OXYGEN HARNESS FAILS TO INFLATE (LEAKING). FOUND FAULTY OXYGEN HARNESS. REPLACED MASK ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080910 NM 2008 9 10 2008UALA04270 1 20080813 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT GALLEY FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 351UA 24319 AFT GALLEY EEL LIGHT STRIP NOT WORKING. 2 L 7 2 4F 4 F RT A16WE E21EU 20080910 EU 2008 9 10 2008UALA04157 1 20080804 A 3510 MF20010 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FO LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 415UA 475 F/O'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). *S/D* HARNESS IS CRACKED AND LEAKING. REPLACED F/O OXYGEN MASK, O PS CHECK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20080910 NM 2008 9 10 2008UALA04113 1 20080804 A 8011 784750A2 STARTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 COULD NOT START NR 1 ENGINE. RTBL. *S/D* STARTER FAILURE. REPLACED MAIN ENGINE STARTER AND REPLACED STARTER VALVE AN D SERVICED MAIN ENGINE STARTER PER. RAN UP ENGINE ALL INDICATIONS NORMAL AND NO LEAKS DETECTED AFTER ENGINE RUN. NO OT HER DEFECTS NOTED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 EU 2008 9 10 2008UALA04123 1 20080803 A 3510 6490376 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE 1ST OFFICER'S LEAKING A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 472UA 1435 F/O'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). CREW COMMENTS: MASKS DOES NOT TEST PROPERLY. *S/D* O2 BOX LEAKIN G AND TEST SWITCH IS STICKING. REPLACED 10RN3, 3RD OCCUPANT OXY BOX. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080910 EU 2008 9 10 2008UALA04124 1 20080803 A 3510 MR35114234 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE 1ST OBSERVER'S LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 472UA 1435 THE 1ST OBS MASK, LEAKS. *S/D* HARNESS NOT INFLATING/LEAKING. REPLACED 1ST OBS MASK, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20080910 NM 2008 9 10 2008UALA04241 1 20080812 A 5610 RETAINER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT WINDOW DEFORMED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 375UA 24640 PRESSURIZATION INDICATION. RTFL. FOUND FOUND ZEE RETAINER ON FO'S SLIDING WINDOW DEFORMED AT LOWER AFT CORNER. STRAIGH TENED RETAINER AND AREA OF DISBOND IS WITHIN LIMITS. INSTALLED SMALL AMOUNT OF SPEED TAPE AT AREA OF DISBOND. PRESSURIZE D ACFT AND FOUND NO LEAKS. INSPECTED WHEELWELL, FWD AND AFT E-E COMPARTMENTS-NOTHING UNUSUAL FOUND. REQUIRES SLIDING WIN DOW REPLACEMENT. REPLACED R2 WINDOW & ADJUSTED. 2 L 7 2 4F 4 F RT A16WE E21EU 20080910 NM 2008 9 10 2008UALA04243 1 20080812 A 3230 1809130 BRAKE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MLG SEIZED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 175UA 24382 LANDING GEAR NO RETRACT. RTFL. FOUND RT BLG FWD LT BRAKE SEIZED. REPLACED BRAKE. NO SHOP DATA FOR ROOT CAUSE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080910 NM 2008 9 10 2008UALA04258 1 20080812 A 3350 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 325UA 23957 AFT GALLEY EEL LIGHT DAMAGED. 2 L 7 2 4F 4 F RT A16WE E21EU 20080910 2008 9 10 2008UALA04259 4 20080813 A 2565 BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 LOW BOTTLE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080910 NM 2008 9 10 2008UALA04260 1 20080813 A 2421 GCU BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 787UA 26939 ELEC GEN OFF R RIGHT GENERATOR CONTROL BREAKER (GCB) OPEN OR GENERATOR CONTROL SWITCH OFF, AND ENGINE NOT SHUT DOWN. AD VISORY MSG01- LATCHED TAKEOFF ROLL MODE DEPENDENT; INTEGRATED DRIVE GENERATOR (R) EXCITER FIELD CURRENT IS OUT OF RANGE. DB- GENERATOR CONTROL UNIT (R) MSG-2431612 LATCHD TO MODE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080910 NM 2008 9 10 2008UALA04262 1 20080813 A 3350 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 918UA 25385 AFT DOOR GREEN EMERGENCY EXIT LIGHTS AND 2 STOW BIN LIGHTS STAYING ON. 2 L 7 2 4F 4 F RT A16WE E21EU 20080910 NE 2008 9 10 2008UALA04263 2 20080813 A 7261 ENGINE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LEAKING A UALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 835UA 1426 V10095 AFTER ENGINE SHUTDOWN AN UNUSUALLY LARGE AMOUNT OF SMOKE CAME FROM TAILPIPE. FOUND OIL RUNNING DOWN LAST STAGE OF LPT D ISK AND ONTO BLADES. 2 L 7 2 4F 4 F RT A28NM E40NE 20080910 NM 2008 9 10 2008UALA04074 1 20080731 A 2421 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 INOPERATIVE A UALA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 547UA 25368 RIGHT GENERATOR DROPPING OFF. *S/D* NO IDG HISTORY. REPLACED NR 2 ENG IDG -OPS AND LEAK CHECKED GOOD DURING RUNS, ALL GENERATION OUTPUT NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 2008 9 10 2008UALA04254 4 20080811 A 2565 D31591478U1 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 DOOR 1L SLIDE IS FALLING OUT. SUSPECT SLIDE IMPROPERLY INSTALLED. REINSTALLED SLIDE IAW MM 25-61-35 PG 201. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 2008UALA03882 1 20080714 A 2421 SHAFT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE BACK UP GEN SHEARED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 219UA 30551 CREW REPORTS RT BACKUP GENERATOR EICAS MSG. *S/D* FOUND SHAFT SHEARED. REPLACED BACK UP GENERATOR, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 NM 2008 9 9 2008UALA03738 1 20080705 A 3350 20131A BATTERY PACK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 309UA 23670 EEL TRACK DOES NOT ILLUMINATE AT SEAT ROW 17 THRU 21. *S/D* SUSPECT FAULTY BATTERY PACK. REPLACED BATTERY PACK, OP CH ECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 ZZDA2008151 1 20080810 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM EMERGENCY LIGHT UNSERVICEABLE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 932AT 55073 FIRST CLASS EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED B5-118 BATTERY AND BATTERY SUPPLY ASSY REF AMM 33-51. 2 L 7 2 4F TR A6WE 20080909 NM 2008 9 9 ZZDA2008136 1 20080806 A 5320 993653429 FLOOR SUPPORT BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 FWD GALLEY FLOOR HAS CORRODED ANGLE BETWEEN PANELS 221 BF & 221 CF. CORROSION OUT OF LIMITS. INSTALLED NEW FLOOR SUPPO RT ANGLE PER B717 SRM 51-41-02. 2 L 7 2 4F TR A6WE 20080909 NM 2008 9 9 2008UALA04043 1 20080730 A 2133 OUTFLOW VALVE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN PRESSURE FAULTED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 827UA 1022 VENT SKIN VALVE FAULT. RTFL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 EU 2008 9 9 2008UALA04044 1 20080730 A 2133 OUTFLOW VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN PRESSURE ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 494UA 1840 BLOWER FAULT DISPLAYED. RTFL. PFR SHOWS SKIN AIR OUTLET VALVE 22HQ FAULT. REPLACED SKIN VALVE. OPS CHECKS GOOD 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA04045 1 20080730 A 3260 SQUAT SWITCH BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 367UA 24536 TAKEOFF WARNING HORN SOUNDED. RTFL. REPLACED M991 AIR SENSING SQUAT SWITCH. PERFORMED TAKEOFF AURAL WARNING TEST. CHEC KED OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 EU 2008 9 9 2008UALA04053 1 20080729 A 3150 WARNING MESSAGE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ACTIVATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 478UA 1533 LAVATORY SMOKE DETECTOR DISPLAYED ON UPPER ECAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 2008 9 9 2008UALA04054 4 20080728 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 435UA 613 DOOR 1L ESCAPE SLIDE PRESS IS NOT IN GREEN BAND. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 EU 2008 9 9 2008UALA04055 1 20080728 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 472UA 1435 EMERGENCY LIGHT TEST FAILED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA04064 1 20080730 A 3260 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE MLG ILLUMINATED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 671UA 30026 MADE A TOWER FLYBY AND LANDED UNDER AMBER ALERT DUE TO LEFT LANDING GEAR INDICATION PROBLEM. 2 L 7 2 4F 4 F RT A1NM E24NE 20080909 NM 2008 9 9 2008UALA04065 1 20080731 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 816UA 871 CABIN EMERGENCY LIGHTS WILL NOT TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 EU 2008 9 9 2008UALA04067 2 20080731 A 7230 3053553220 BEARING BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NR 1 COMPRESSOR FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 935UA 26663 724509 NR 1 ENGINE COMPRESSOR STALL. RTFL. FOUND FAILURE OF NR 4 BEARING. CHANGED ENGINES. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 EU 2008 9 9 2008UALA04072 1 20080730 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OVERWING EXIT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 447UA 836 ON LAST 2 ENG SHUTDOWNS THE OVERWING EXIT LIGHTS ILLUMINATE WITH SWITCH IN OFF POSITION. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 EU 2008 9 9 08FDEA03682 1 20080901 A 5410 SUPPORT AIRBUS 310 A310222 3930315 EU NR 2 NACELLE BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 NR 2 ENGINE NOSE COWL ANTI-ICE PICCOLO TUBE SUPPORT LINK AT THE 12 O'CLOCK POSITION IS BROKEN & DISCONNECTED. REMOVED & REPLACED THE NR 2 NOSE COWL IAW AMM 71-11-00-04. 2 L 7 2 4F RT A35EU 20080909 NM 2008 9 9 ASAA0853332 1 20080815 A 2421 761574B IDG BOEING 737 737890 1384527 NM NR 2 ENGINE FAILED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 583AS 4310 35681 NR 2 GEN OFF BUSS LIGHT ILLUMINATED FOLLOWED SHORTLY BY NR 2 DRIVE LIGHT ILLUMINATION. DISCONNECTED DRIVE AND PUT APU O N BUSS. REMOVED AND REPLACED THE NR 2 ENG IDG REF MM 24 11 11 000 801 AND MM 24 11 11 400 801 LEAK CHECK AND OPS CHECKS GOOD REF MM 24 11 00 700 803. 2 L 7 2 4F RT A16WE 20080909 2008 9 9 ASAA0853333 4 20080815 A 3460 1741010201 CDU BOEING 737 737890 1384527 NM COCKPIT FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 584AS 3974 35682 NR 2 FMC "L2" BUTTON VERY DIFFICULT TO PRESS. REPLACED NR 2 FMCS CONTROL DISPLAY UNIT, OPS NML REF MM 36 61 01. 2 L 7 2 4F RT A16WE 20080909 WP 2008 9 9 AALA200801933 1 20080722 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9621A 53592 AUX OVERHEAD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT BS 106 FOR OVERHEAD EMERGENCY LIGHTS IN CA BIN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A6WE 20080909 NE 2008 9 9 AALA200802024 2 20080805 A 7200 RB211535E4B3735 ENGINE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE NR 1 FAILED A AALA G A O2 MASK DEPLOYED UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 192AN 32386 31790 LAX INFLT T31/05AUG. CREW REPORTED SMOKE FILLING CABIN. DROPPED OXYGEN MASKS. RETURNED TO LAX AND LANDED WITHOUT INC IDENT. DEPLOYED 6 SLIDES FOR EMERGENCY EVACUATION. FOUND EVIDENCE OF OIL ON NR 1 ENGINE INTERMEDIATE PRESSURE BLADES S TAGE 5 AND 6 AND HIGH PRESSURE BLADE STAGE 1. ALSO FOUND OIL LEAKING ON COMPRESSOR CASE AT 6 OCLOCK POSITION. REPLACED NR 1 ENGINE ON 07AUG AT LAX. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F 4 F RT A2NM E12EU 20080909 NE 2008 9 9 08FDEA03646 2 20080829 A 7320 441790 HMU AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680 30025 NE NR 1 ENGINE FAILED A FDEA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 CE 21 661FE 760 NR 1 ENGINE N1 INDICATION BECAME UNSTABLE DURING CLIMB. REPEAT WRITE-UP. THEN EGT EXCEEDED LIMITS AT 952 DEG. THEN FUE L FLOW INDICATION BECAME UNSTABLE WITH SURGING AND YAW. PULLED TO IDLE N-1 AND FF INDICATION REMAINED UNSTABLE BUT SURG ING STOPPED. PERFORMED FADEC BITE TEST AND PULLED FAULT CODES NOTHING ABNORMAL FOUND. REF TSM 73-21-30. BORESCOPED HP T STAGE 1 AND 2 PER 72-00-00-6, NO DEFECTS NOTED. REMOVED AND REPLACED HMU REF AMM 73-13-00-4. REMOVED AND REPLACED NR 1 CIT SENSOR REF MM 73-21-02-4. REMOVED AND REPLACED N1 SENSOR IAW MM 77-11-01-4 05. REMOVED AND REPLACED FUEL FILTER AND THE TEMP INLET SENSOR (T 1.2). REF AMM 73-12-02-4 AND 73-23-06-4. HIGH PWR RUN PER JRH. 2 L 7 2 4F 4 F RT A35EU E13NE 20080909 WP 2008 9 9 08FDEA03692 1 20080901 A 5350 ANB71427 BRACKET DOUG MD10 MD1010F 3022112 WP BS 1341 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 THERE IS A CRACKED BRACKET AT THE LEFT OVERWING TO BODY FAIRING PANEL SUPPORT AT STA 1341; BELOW LONGERON 31L. REMOVED ANGLE IAW SRM 51-31-01 VOL II. HEAT TREATED IAW TPS 1003; REV " A ". ALODINED & PRIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II. INSTALLED IAW SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 20080909 WP 2008 9 9 08FDEA03694 1 20080901 A 5350 ANB705114 BRACKET DOUG MD10 MD1010F 3022112 WP BS 1421 S32R CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 THERE IS A CRACKED BRACKET AT THE RT OVERWING TO BODY FAIRING SUPPORT AT BS 1421 L32R. REMOVED ANGLE IAW SRM 51-31-01 V OL II. FABRICATED IAW DWG ANB 7051 REV C . HEAT TREATED IAW TPS 1003 REV A. ALODINED & PRIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II. INSTALLED IAW SRM 51-31-01 VOL II. PART MARKED IAW GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20080910 NM 2008 9 10 AALA200801975 1 20080727 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 772AN 29580 JFK EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NORM AL OPS. (CLOSED) 2 L 7 2 4F RT T00001SE 20080910 NM 2008 9 10 USAA920081576 1 20080820 A 5320 SUPPORT ANGLE BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT - Q6 - MAJOR REPAIR - NR 03C10753005/008 - SUPPORT ANGLE CRACKED AT BS 312 TO BS 328, RBL32. REPLACED SUPPORT ANGLE AT BS 312 TO BS 328, RBL32 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 08FDEA03511 1 20080820 A 5730 ARB74023 SKIN DOUG MD11 MD11 3023602 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 15 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LH WING LOWER SKIN ACCESS DOOR CUTOU T BETWEEN STA XORS= 690 AND STA XORS= 700. 15 EACH FASTENER HOLES ON LEFT HAND WING LOWER SKIN ACCESS BETWEEN XORS = 690 TO XORS = 700 REPAIR CARRIED OUT AS PER E.A. #1-5710-122426A, THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080911 NM 2008 9 11 2008UALA03885 1 20080715 A 2780 4135T1003 MOTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SLATS FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 669UA 30025 INBOARD SLAT C-BREAKER POPPING. SLAT MOTOR FAULTY. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03829 1 20080710 A 3350 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 FLOOR EEL INOP CROSS AISLE FWD GALLEY AREA. FOUND BROKEN LEAD CABLE. REPAIRED LEAD CABLE IAW GNMM 2-0-15-005, OP CHECK ED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03827 1 20080710 A 3350 GE1317 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 EEL LIGHT INOP EXTERIOR LEFT WING SLIDE LIGHT (L396). *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. A C OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03840 1 20080710 A 3350 582240 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 647UA 25284 EEL LIGHTS AT LEFT HAND MID CABIN EMERGENCY EXITS INOP. FOUND POWER SUPPLY FAULTY. REPLACED POWER SUPPLY, OP CHECKED G OOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03969 1 20080723 A 3397 58791 CONNECTOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 675UA 29243 AFT GALLEY FLOOR EEL LIGHT INOP. *S/D* FOUND BROKEN CONNECTOR. SPLICED IN NEW CONNECTOR, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03986 1 20080725 A 2121 4100941C FAN BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 791UA 26933 EICAS STATUS MESSAGE EQUIP COOLING FAN LT. *S/D* FOUND FAULTY COOLING FAN AND FLOW SENSOR. REPLACED COOLING FAN AND F LOW SENSOR, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NM 2008 9 11 2008UALA03836 1 20080709 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE SEAT 22B BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 EEL LIGHT ON AISLE SEAT 22B BROKEN OFF SEAT. *S/D* FOUND LIGHT ASSEMBLY BROKEN. REPLACED LIGHT ASSEMBLY, OP CHECKED G OOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03947 1 20080720 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 58ABC FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY LIGHT ON SEAT 58ABC INBOARD AISLE BUMPER INOP. *S/D* FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03967 1 20080723 A 3350 362624 LAMP BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 675UA 29243 FWD GALLEY EEL LIGHT INOP. *S/D* FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03797 1 20080708 A 3350 582240 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 657UA 27112 LEFT SIDE A&B ZONE CEILING EMERGENCY AISLE LIGHTS ARE INOP. *S/D* FOUND FAULTY BATTERY PACK. REPLACED BATTERY PACK, O P CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03957 1 20080723 A 3510 MC1019151 OXYGEN MASK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FIRST OFFICER'S LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 F/O O2 MASK LEAKING FROM HEADBAND. *S/D* FOUND MASK LEAKING. REPLACED MASK, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03997 1 20080727 A 3350 GE1317 LAMP BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 LEFT AFT EXTERNAL EMERGENCY LIGHT INOP MED 2L. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FO R SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04018 1 20080728 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 55L FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EEL INOP 55L. *S/D* FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 2008 9 11 2008UALA04023 4 20080725 A 2565 H2052K3833 LATCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LH OWING SLIDE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 LT OVERWING SLIDE COMPARTMENT DOOR, NR 3 OPENING LATCH FAILS EDGE MARGIN MEASUREMENT. *S/D* FOUND WORN LATCH NR 3 DOOR . REPLACED NR 3 LATCH PER MM 25 -65-09, ADJ PER MM 25-65-09. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04025 1 20080727 A 3350 58791 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 EEL LT AT MID'S X-AISLE INOP. *S/D* FOUND POWER FEEDER CABLE BROKEN LIGHT ASSEMBLY INOP. REPLACED LIGHT ASSEMBLY REPA IRED FEEDER CABLE, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04020 1 20080728 A 3350 BPS73 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 ALL LT EEL INOP: D-ZONE. *S/D* FOUND FAULTY POWER SUPPLY. REPLACED POWER SUPPLY, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03999 1 20080727 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 EEL LT AT MID'S X-AISLE INOP. *S/D* FOUND BROKEN FEEDER CABLE. REPAIRED FEEDER CABLE, OP CHECK GOOD. AC OK FOR SERVI CE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04019 1 20080728 A 3350 FU305 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 RIGHT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP. TWO MOST AFT LIGHT ASSY'S. *S/D* FOUND FAULTY FUSE. REPLACED FUS E, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA04081 1 20080801 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERG LIGHT INOP: LT OVERWING 3RD ASSY AFT BULB. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECK GOOD. AC OK F OR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA04062 1 20080730 A 2910 3930021102 CONTROL VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE HYD SYSTEM FAULTY A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 794UA 26953 ON TAXI OUT HAD FLAP PRIMARY FAIL PRIMARY (HYDRAULIC FLAP DRIVE FAILURE). *S/D* SUSPECT FAULTY FLAP PRIMARY CONTROL VA LVE. REPLACED VALVE, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NM 2008 9 11 2008UALA04066 1 20080730 A 3610 32907449 VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 779UA 26941 NR 1 ENG FAMV STATUS MESSAGE. *S/D* FOUND FAULTY FAN AIR MODULATING VALVE. REPLACED FAMV, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NM 2008 9 11 2008UALA04140 1 20080805 A 3350 78671 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 2 BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 778UA 26940 THE 2E SEAT ARMREST MOUNTED EMERGENCY PATH LIGHT DAMAGED. *S/D* FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 2008 9 11 2008UALA04141 4 20080804 A 2565 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT OWING SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 662UA 27159 ASPIRATOR LEAKS FROM BARREL. *S/D* FOUND LEAKING ASPIRATOR SUSPECT PACKING. REPLACED SLIDE ASSEMBLY. AC OK FOR SERVI CE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04128 1 20080805 A 3350 78671 LAMP BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 THE EMERGENCY EXIT LIGHT MOUNTED ON THE SIDE OF SEAT 5B IS MISSING IN THE FWD POSITION. THE AFT LIGHT IS MISSING. *S/D * FOUND LIGHT ASSEMBLY MISSING. REPLACED LIGHT ASSEMBLY, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NE 2008 9 11 2008UALA04148 2 20080805 A 7532 79027013 BLEED VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT ENGINE FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 675UA 29243 LEFT ENGINE BLEED LIGHT ON W- LEFT ENG HPSOV ON EICAS. *S/D* SUSPECT HPSOV FAULTY. REPLACED HPSOV OP CHECKED GOOD. A C OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04149 1 20080806 A 2822 M259881151 O-RING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUEL PUMP LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 646UA 25283 EVIDENCE OF FUEL LEAK FROM RIGHT WING MAIN FUEL PUMP PANEL. *S/D* SUSPECT O-RING PACKING. REPLACED O-RING LEAK CHECKE D GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04161 1 20080806 A 2421 1701768 GENERATOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 1 ENGINE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 792UA 26934 LEFT BACKUP GENERATOR FILTER INDICATES BLOCKED ON ELECT SYNOPTIC PAGE. PRESS INDICATOR IS POPPED. *S/D* FOUND FAULTY BACK UP GENERATOR. REPLACED BUG OP AND LEAK CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NM 2008 9 11 2008UALA04162 1 20080806 A 8011 8088846 START VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 1 ENGINE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 784UA 26951 ENG START VALVE L LEFT STARTER AIR VALVE POSITION DISAGREES WITH COMMANDED POSITION OR STARTER AIR VALVE POSITION INDICA TION IS LOST. STATUS MSG01- NOT ACTIVE ENGINE SHUTDOWN MODE DEPENDENT; STARTER AIR VALVE (SAV) (L ENG) IS NOT IN COMMA NDED POSITION. *S/D* FOUND FAULTY STARTER VALVE. REPLACED STARTER PER MM 80-11-01, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NM 2008 9 11 2008UALA04168 1 20080806 A 3350 60443 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 EEL STRIP LOOSE ON FLOOR BY MID LAV. *S/D* FOUND LOOSE LIGHT ASSEMBLY. SECURED LIGHT ASSEMBLY, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NE 2008 9 11 2008UALA04274 2 20080814 A 7261 FILTER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ENGINE OIL UNKNOWN A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 652UA 32341 7170 25390 727787 LT ENGINE OIL FILTER STATUS MESSAGE. *S/D* REPLACED MAIN OIL FILTER. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 EU 2008 9 11 08FDEA03123 1 20080729 A 5740 A5724081021 LUG AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 CORROSION WAS FOUND ON THE MLG GEAR RIB 5 AFT PINTLE BEARING FORWARD LUG, RT WING. REPAIR PERFORMED BY OVERSIZING THE B ORE, REDUCING THE LUG THICKNESS, NDT INSPECTION (NIL FINDINGS), PERFORMING A FINISHING CUT AND INSTALLING OVERSIZE BUSHE S, ALL IAW REPAIR INSTRUCTIONS MENTIONED IN RAS/BAE/1007561/2008 ISSUE A AND EA 6-5720-120092. 2 L 7 2 4F RT A35EU 20080910 EU 2008 9 10 2008UALA04264 1 20080813 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 403UA 442 CREW O2 LEAKS 10 PSI EVERY 8 MINUTES. 2 L 7 2 4F 4 F RT A28NM E40NE 20080910 2008 9 10 2008UALA04265 4 20080813 A 2330 MONITOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE VIDEO SYSTEM LOOSE A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 550UA 25398 VIDEO MONITOR IN BACK CABIN IS LOOSE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 2008 9 10 2008UALA04048 4 20080730 A 2565 D31038201U1 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 LOW BOTTLE. LEAKING AT FILL VALVE. REPLACED FILL VALVE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 2008 9 10 2008UALA04049 4 20080730 A 2565 6499148 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 577UA 26693 NR 1 RT MED SLIDE PRESSURE INDICATOR IS AT LOW EDGE OF GREEN BAND. *S/D* UNKNOWN PRESSURE LEAK. REPLACED SLIDE ASSY, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 NM 2008 9 10 2008UALA04063 1 20080729 A 2700 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE UNKNOWN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 598UA 28751 CREW REPORT: W-RUDDER TRIM ZEROED, AIRCRAFT ROLLS RIGHT ON ROTATION. LEVEL FLIGHT REQ 2.5 UNITS LEFT RUDDER. *S/D* A CCOMPLISHED OPS CHK OF RUD PER AM 27-21-00. ALSO CHECKED SYS PER AMM 27-21-00 ITEM THRU PG 524 ITEM I ALL CHECKS NORMAL . REF AMIS PTT SEQ 0212016 AND 0212005. RUD TRIM WITHIN LIMITS PER AMM 27-01-00 PG 501 PARA A. NO REPEATS SINCE ORIGI NAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 NM 2008 9 10 2008UALA04068 1 20080730 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TAILCONE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 SKIN CREASE IN TAIL CONE SKIN STA 1820 TO 1840, STR 21L TO 23L. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. CUT OUT DAMAG ED SKIN AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 NM 2008 9 10 2008UALA04069 1 20080730 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1420-1440 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 CORROSION ON CREASE BEAM AT STA 1420 TO 1440, RBL 70.5. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. REPLACED WEB. REF BO EING DRW 146N5590 AND SRM 53-60-13 AND INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 NM 2008 9 10 2008UALA04253 1 20080812 A 3510 COUPLING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW OXYGEN LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. CREW COMMENTS: 1275 PSI AND SLOWLY DECREASING. FOUND THE JUMP SEAT MASK CONNECTION POINT TO ACFT O-RING DAMAGED. REPLACED WITH NEW MASK, OP CHECKED MASK, NORMAL. SERVICED O2 L EVELS. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 2008UALA03875 1 20080714 A 2622 SAFETY WIRE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE EXTING MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 373UA 24638 CREW REPORT: WATER EXTINGUISHER DOES NOT HAVE SAFETY WIRE. *S/D* FOUND SEAL BROKEN. REPLACED FIRE EXTINGUISHER. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 ZZDA2008143 1 20080806 A 5320 WEB BOEING 717 717200 1383700 NM BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 FLOOR WEB HAS CRACKS & CORROSION AT BS 200 RBL 22 CORROSION OUT OF LIMITS. FABRICATED WEB REPAIR PER B717 SRM 51-70-10. 2 L 7 2 4F TR A6WE 20080909 NM 2008 9 9 ZZDA2008144 1 20080806 A 5320 WEB BOEING 717 717200 1383700 NM BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 FLOOR WEB HAS CORROSION AT BL 0 - LBL 7 AT STA 200 OUT OF LIMITS. CUT OUT AFFECTED AREA, FABRICATED DOUBLER REPAIR, INS TALLED SAME PER B717 SRM 51-71-10. 2 L 7 2 4F TR A6WE 20080909 NM 2008 9 9 CALA0800766 1 20080804 A 5315 65528942 FLOORBEAM BOEING 737 737724 13844BY NM BS 540 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 21723 28790 RIGHT FLOOR SUPPORT CRACKED STATION 540 AT BL-0. REMOVED AND REPLACED FLOOR SUPPORT REF EC/RA 5321-01560. 2 L 7 2 4F RT A16WE 20080909 NM 2008 9 9 2008UALA04051 1 20080729 A 3320 SOCKET BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LAVATORY LIGHT BURNED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 776UA 26937 AFT LAV BLOCKED FOR LIGHT HAVING ELECTRIC SMELL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 NM 2008 9 9 2008UALA04056 1 20080728 A 2612 G718505 CONTROL PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE DETECTION ILLUMINATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 303UA 23644 FAIL LIGHT ILLUMINATED ON B-LOOP AFT CARGO COMPARTMENT. FOUND CONTROL PANEL TO BE FAULTY. REPLACED CONTROL PANEL CARGO FIRE DETECTION AND SUPPRESSION REF 26-00-02 OP CHECKS GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 2008UALA04060 1 20080728 A 3350 582240 BATTERY BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 667UA 29239 FWD CABIN X AISLE INOP. REPLACED BATTERY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 08FDEA02853 1 20080714 A 5753 ARC40091 SUPPORT DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 597FE 48596 DURING OPEN-HOLE HFEC INSPECTION, CRACK INDICATION FOUND AT OUTBOARD LOWER FASTENER HOLE COMMON TO ARC4008 AND ARC4009 S UPPORTS OF LEFT HAND SIDE WING OUTBOARD FLAP. LEFT HAND OUTBOARD FLAP REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJU STMENT AND TEST CARRIED OUT FOUND 'SATIS' AS PER AMM 27-50-00-830-805. 2 L 7 3 4F RT A22WE 20080911 NM 2008 9 11 08FDEA03122 1 20080729 A 5320 143N537036 FLOOR SUPPORT BOEING 757 757200 1384950 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FLOOR SUPPORT FROM BS 653 TO BS 700, LBL 8, HAS CORROSION. CORROSION FOUND EXCEED SRM LIMITS. REMOVED AND REPLACED STR INGER IAW SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080911 NM 2008 9 11 08FDEA03102 1 20080728 A 5320 143N5366Y72 PANEL BOEING 757 757200 1384950 NM BS 560-645 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 TRANSITION PANEL FROM BS 560 TO BS 645.75 HAS CORROSION. CORROSION FOUND BEYOND ALLOWABLE LIMITS IN B757-200 SRM 51-10- 02. PANEL REPLACED IAW B757-200 51-10-02 AND 51-40-02. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080911 NM 2008 9 11 08FDEA03103 1 20080728 A 5320 143N5366Y81 PANEL BOEING 757 757200 1384950 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 RIGHT TRANSITION PANEL FROM BS 640 TO BS 765 HAS CORROSION. CORROSION FOUND OUTSIDE ALLOWABLE SRM LIMITS. PANEL REMOVE D AND REPLACED IAW B757-200 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080911 NM 2008 9 11 08FDEA03104 1 20080728 A 5320 143N536677 PANEL BOEING 757 757200 1384950 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 RIGHT TRANSITION PANEL FROM BS 760 TO BS 845 HAS CORROSION. CORROSION FOUND OUTSIDE ALLOWABLE SRM LIMITS. PANEL REMOVE D AND REPLACED IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERI A. 2 L 7 2 4F RT A2NM 20080911 NM 2008 9 11 08FDEA03105 1 20080728 A 5320 146N5391U171 PANEL BOEING 757 757200 1384950 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 LEFT SIDE TRANSITION PANEL FROM BS 1200 TO BS 1310 HAS CORROSION. CORROSION FOUND OUTSIDE ALLOWABLE LIMITS IN SRM. PAN EL REMOVED AND REPLACED IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080911 NM 2008 9 11 2008UALA04296 1 20080818 A 3510 BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW OXYGEN LOW A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 175UA 24382 CREW OXYGEN PX READ 1560 PSI ON STS PAGE. REPLACED CREW OXYGEN CYLINDER. ACFT OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NE 2008 9 11 2008UALA04301 2 20080817 A 7421 IGNITER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE LT ENGINE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 224UA 30225 ENG IGNITOR L2 LEFT ENGINE FAILED TO IGNITE USING IGNITOR 2. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NM 2008 9 11 08FDEA03120 1 20080729 A 5320 143N537036 FLOOR SUPPORT BOEING 757 757200 1384950 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FLOOR SUPPORT FROM BS 653 TO BS 700, RBL 10, FOUND WITH CORROSION. CORROSION FOUND EXCEED ALLOWABLE LIMITS IN SRM. REM OVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080911 NM 2008 9 11 08FDEA03121 1 20080729 A 5320 143N534639 FLOOR SUPPORT BOEING 757 757200 1384950 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FLOOR SUPPORT FROM BS 653 TO BS 700, RBL 16, HAS CORROSION. CORROSION FOUND EXCEEDED SRM LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080911 NM 2008 9 11 2008UALA04306 1 20080815 A 3350 58781 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 642UA 25092 FIRST CLASS FWD EEL LIGHT INOP. REPAIRED EMERGENCY LIGHT CABLE. OP CHECKED OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NE 2008 9 11 2008UALA04308 2 20080815 A 7261 SCAVENGE PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE OIL LEAKING A UALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 551UA 25399 OILY ODOR NOTICED ON DESCENT. SCAVENGE PUMP SEAL LEAKING. REPLACED G-B OIL SCAVENGE PUMP REPLACED LUBRICATION AND SCA VENGE PUMP ACCOMPLISHED LT PACK BURNOUT PER SVC TIP 79-00-95. OPERATION AL AND LEAK CHECK GOOD. OIL ODOE NO LONGER PRES ENT AT ANY POWER SETTING. REACTIVATED HIGH STAGE BLEED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080911 EU 2008 9 11 2008UALA04309 1 20080815 A 2700 47145137 ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELAC FAULTED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 460UA 1248 ELAC 1 & 2 PITCH FAULT. RTFL. REPLACED THS ACTUATOR. ACCOMPLISHED SUCCESSFUL TEST FLIGHT. A/C OKAY FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA03964 1 20080724 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 525UA 24978 EMERGENCY LIGHT STRIP INOP ON LEFT SIDE OF A-C ROW 9. *S/D* LIGHT BATTERY PACK FAULTY, ALSO SUSPECT CHARGER IS WEAK. REPLACED EMERGENCY LIGHT BATTERY PACK CHARGER ASSY AND INVERTER, OP CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080909 2008 9 9 2008UALA04008 4 20080728 A 2565 MR25613023 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 402UA 439 FAILED EMERGENCY LIGHT TEST. *S/D* INTERNAL SHORT/RESISTANCE IN SLIDE 1L. REPLACED SLIDE 1L. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA04071 1 20080731 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 410-450 DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 330UA 24191 NEW CROWN SKIN IS MISSING INTERNAL DOUBLER FOR ATC ANTENNA AT STA 410-450 STR 1R TO 2R, ALSO HAS 4EA HOLES DRILLED IN TH E EDGE OF EXISTING INTERNAL DOUBLER 2 EA AT STA 420, 2EA AT STA 440. MAJOR REPAIR ACCOMPLISHED:ACCOMPLISHED A DOUBLER AND TRIPLER REPAIR. THE SKIN P/N INSTALLED 65-45765-98 WAS MODIFIED WITH THE DOUBLER AND TRIPLER AT THE ANTENNA LOCATIO N. WORK WAS ACCOMPLISHED ON E VA-71808. ACFT OK FOR FLIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 2008 9 9 2008UALA04073 4 20080730 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 417UA 483 CABIN EMERGENCY SLIDE CHECK DID NOT PASS. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 08FDEA03662 1 20080831 A 5340 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 594FE 48552 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION, ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITT ING AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MA JOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080909 EU 2008 9 9 08FDEA03684 1 20080901 A 5753 A5797033220300 FITTING AIRBUS 310 A310222 3930315 EU RT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 RIGHT WING INBOARD FLAP; OUTBOARD END; FOLLOW UP GUIDE FITTING IS CRACKED. REMOVED GUIDE FITTING IAW SRM 51-40-02; PG 1 & DRILLED NEW FITTING 1AW SRM 51-40-40 PG 2. INSTALLED NEW FITTING IAW SRM 51-40-02; PG 1. 2 L 7 2 4F RT A35EU 20080909 WP 2008 9 9 08FDEA03687 1 20080901 A 5720 ARB240713 STIFFENER DOUG MD10 MD1010F 3022112 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 RIGHT WING INBOARD UPPER L/E PANEL 617 CT HAS 2 CRACKED CHANNELS. REMOVED 2 EA STIFFENERS IAW SRM 51-35-01 VOL II. FAB RICARED IAW DWG ARB 2407; REV " G " (-13 & -9). ALODINED & PRIMED IAW SRM 51-21-01 VOL II PGS 21-24 AND INSTALLED IAW SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 20080909 NM 2008 9 9 2008UALA04100 1 20080801 A 2612 W20168 SWITCH BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE WARNING INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 302UA 23643 DURING FIRE TEST, THE F/O'S MASTER FIRE WARNING LIGHT WILL NOT ILLUMINATE. FOUND FAULTY SWITCH. REPLACED F-O MASTER WAR NING SWITCH. OPS CHECKED OK. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 ASAA0853329 1 20080811 A 4990 38809381 OIL FILTER BOEING 737 737890 1384527 NM APU POPPED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 558AS P7229 35177 WHILE ACCOMPLISHING TASKCARD 78349013, FOUND APU OIL FILTER DELTA P POPPED. ACCOMPLISHED OIL FILTER INDICATOR SERVICING PER MM 49 91 13. 2 L 7 2 4F RT A16WE 20080909 WP 2008 9 9 AALA200801989 1 20080727 A 3260 PROXIMITY SENSOR DOUG DC9 DC983 3022083 WP MLG INOPERATIVE A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 961TW 53611 SLC INFLIGHT T327/27JUL. CREW REPORTED NOSE LANDING GEAR UNSAFE LIGHT ON APPROACH. LANDED SLC WITHOUT INCIDENT. CLEAN ED NOSE LANDING GEAR DOWNLOCK PROXIMITY SENSOR. RESEATED PROXIMITY SENSOR ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMA L OPS. (CLOSED) 2 L 7 2 4F RT A6WE 20080909 2008 9 9 WWQ2008F00003 4 20080802 A 3442 MI5853511 TRANSCEIVER GULSTM G1159 G1159 3953505 SO RROYCE SPEY SPEY* NE WX RADAR SHORTED E WWQA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 WP 07 712AS 160 423 AC WAS DISPATCHED, THE CREW CAPTAIN AND F/O DEPARTED AT 13:40 ENROUTE. AT APPROX 13:50, WHILE CLIMBING OUT OF 8000 FEET , PILOTS NOTICED THE RADAR SCREEN START TO FLICKER. CAPT IMMEDIATELY SHUT THE RADAR OFF. A SHORT WHILE LATER PILOTS SM ELLED WHAT APPEARED TO BE SMOKE RELATED TO ELECTRICAL FIRE. PILOTS THEN SAW HEAVY SMOKE COMING OUT OF THE DASHBOARD. CA PT THEN DECLARED AN EMERGENCY, INITIALLY REQUESTED TO DIVERT, DUE TO THE AVAILABILITY OF LONGER RUNWAYS AND MUCH BETTER EMERGENCY EQUIPMENT IN CASE IT WAS NEEDED. AFTER PERFORMING CORRECT CHECKLIST AND ASSESSING THE SITUATION THE SMOKE HAD DISSIPATED AND CAPT DECIDED THAT THERE WAS NO LONGER AN EMERGENCY. AT THAT POINT REQUESTED TO FLY BACK TO DEPARTURE AN 2 L 7 2 4F 4 T RT A12EA E2EU 20080909 CE 2008 9 9 FPI2008F00000 1 20080821 A 5100 505530401 CABLE CESSNA 210 210M 2073450 CE CONT O520 IO520* 17032 SO UNKNOWN BROKEN E FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 778VK 21062895 MFG SERVICE KIT PN SK210174, CABLE ASSY BROKE AT THREADED END AFTER THE STOP NUT SEVEN WEEKS AFTER INSTALLATION APPEARS THREAD WALL IS TOO THIN LEADING TO FATIGUE. (K) 1 H 7 1 3O 3 O 3A21 E5CE 20080909 WP 2008 9 9 08FDEA03689 1 20080901 A 5350 ANB705113 BRACKET DOUG MD10 MD1010F 3022112 WP BS 1421 L32L CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 THERE IS A CRACKED BRACKET AT THE LEFT OVERWING TO BODY FAIRING SUPPORT STRUCTURE AT STA 1421 & LONGERON 32L. REMOVED A NGLE IAW SRM 51-33-01 & SRM 51-31-01 VOL II. HEAT TREATED IAW TPS 1003; REV " A ". ALODINED & PRIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II. INSTALLED IAW SRM 51-33-01 & SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 20080909 WP 2008 9 9 08FDEA03642 1 20080829 A 5753 ARC1475507 VANE DOUG MD10 MD1010F 3022112 WP TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 LEFT OUTBOARD FLAP VANE; INBOARD LOWER SKIN IS DELAMINATED. REMOVED DELAMINATED INBOARD LOWER SKIN ON LEFT OUTBOARD FLA P VANE INBOARD END. FABRICATED SKIN PLUG & REPAIR DOUBLER. PREPPED FOR BONDING; HOT BONDED REPAIR. ALODINED AREA & EDGE SEALED DOUBLER; PRIMED PER DC/MD-10 SRM 51-71-00; VOL II. PAINTED PER DC/MD-10 SRM 51-21-01; VOL II. REMOVED & R E-INSTALLED LEFT WING OUTBOARD FLAP VANE ASSEMBLY IAW MD-10-10 AMM 27-50-03-2. 2 L 7 3 4F RT A22WE 20080909 NM 2008 9 9 08FDEA03652 1 20080831 A 5754 ARB75821 SKIN DOUG MD11 MD11F 3023600 NM LT WING SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 594FE 48552 LT WING - LEADING EDGE AT SLAT NR 3, NR 8 TRACK AREA, 01 EA EDGE CRACK. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 2 1 VOLUME I. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080909 NM 2008 9 9 08FDEA03654 1 20080831 A 5753 NRC67622 VANE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 594FE 48552 RT WING INBOARD FLAP VANE LOWER SURFACE INBOARD OF MID WAY TO LEADING EDGE AREA FOUND DELAMINATED. REPAIRED IAW EA 1-57 50-124362, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080910 EU 2008 9 10 USAA920081583 1 20080826 A 2913 887673 PUMP AIRBUS A319 A319112 3930323 EU HYD SYSTEM INOPERATIVE A USAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 19 766US 23761 2203 1378 LOGPAGE 7907967 FLT 1045 DTW CLT AIR TURN BACK GREEN HYDRAULIC LOW LEVEL AND OVERHEAT. TOTAL LOSS OF GREEN SYSTEM WAS EXPERIENCED DURING CRUISE. THE FLIGHT DECLARED AN EMERGENCY AND RETURNED TO CLT. R&R NR 1 ENGINE HYDRAULIC PUMP. FLUS HED LINES AND REPLACED FILTERS. OPS AND LEAK CHECK WERE GOOD. 2 L 7 2 4F RT A28NM 20080910 NM 2008 9 10 F3L2008F00003 1 20080822 A 5320 D5347112420100 SHEAR PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 928FR 2236 REFERENCE NON ROUTINE C050055. DURING C3 C-CHECK, INSP NOTED INDICATIONS OF CORROSION ON TOP OF RIGHT AFT SHEAR PLATE B ETWEEN FRAME 68 AND FRAME 70. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE ASSEMBLY IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPH 6. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20080911 NM 2008 9 11 2008UALA03929 1 20080722 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 4A INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 4A AFT LIGHT ASSY. *S/D* EMERGENCY EXIT EEL LIGHT INOP AT SEAT 4A AFT LIGHT ASSY . REPLACED LIGHT ASSY, OPS CHECKS NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03943 1 20080719 A 3397 78961 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 4A AFT LIGHT ASSY. FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECK GOOD. A C OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03830 1 20080710 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 EEL CEILING AISLE LIGHTS INOP AT ROWS 20 AND 23. FOUND BROKEN WIRE ABOUT 10 INCHES FROM LIGHT ASSEMBLY. REPAIRED IAW G NMM02-0-15-001, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03831 1 20080710 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 FLOOR EEL INOP AT LEFT MID LAV. FOUND BROKEN LEAD CABLE. REPAIRED LEAD CABLE IAW GNMM2-0-15-005, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03842 1 20080710 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE 5B SEAT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 SEAT MOUNTED EEL STRIP INOP AT SEAT 5B. *S/D* FOUND LIGHT ASSEMBLY MISSING. REPLACED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03832 1 20080710 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 FLOOR EEL INOP LEFT AFT AISLE AFT LAV. *S/D* FOUND BROKEN LEAD CABLE. REPAIRED LEAD CABLE IAW GNMM2-0-15-005, OP CHEC KED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03938 1 20080719 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT LIGHT INOP UPPER DECK ROW 12 CEILING LIGHT. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03939 1 20080719 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT LIGHT INOP UPPER DECK DOORS AFT CEILING LIGHT. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECK GO OD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03940 1 20080719 A 3397 362624 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT EEL LIGHT INOP LOWER WALL EEL ACROSS LAV 100. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHE CK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03948 1 20080722 A 3350 582240 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 UD ROW 12 THRU 15 EMERGENCY EXIT PATH LIGHTS ARE INTERMITTENTLY COMING ON. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03811 1 20080710 A 2913 65057 PUMP BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE HYD SYSTEM FAULTY A UALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 675UA 29243 RIGHT ENGINE PRIMARY HYD PUMP PRESS LIGHT AFTER ENGINE START. *S/D* SUSPECT FAULTY HYDRAULIC PUMP. REPLACED HYDRAULIC IAW MM 29-11-05, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 2008 9 11 2008UALA03917 4 20080722 A 2565 7A146721 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L1 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 SWELLED-E-SLIDE RAFT AT LT 1 DOOR. *S/D* FOUND FAULTY SLIDE. REPLACED WITH SERVICEABLE SLIDE PER AMM 25-69-01 P401. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03769 1 20080707 A 3020 2790583108 ANTI-ICE VALVE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 ENGINE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 676UA 30028 NR 2 ENG ANTI ICE FAILED AGAIN AFTER ENGINE RUN UP. *S/D* FOUND FAULTY ANTI ICE VALVE. REPLACED NR 2 ENGINE ANTI VALV E IAW MMOV 30-21-03. CREW RAN ENGINE, OP CHECKS NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03970 1 20080724 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 EEL INOP AT SEAT 5EF TO 6EF. *S/D* FOUND FAULTY LEAD CABLE. REPLACED FEEDER, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03949 1 20080723 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 51C MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 194UA 26892 WFS REPORTED, EMERGENCY LIGHT IS MISSING AT SEAT 51C. *S/D* LIGHT ASSEMBLY MISSING. REPLACED LIGHT ASSEMBLY, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA04014 1 20080728 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R3 DOOR SLIDE BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT INOP: DOOR 3R SLIDE ILLUM. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECK GOOD. AC OK FOR SER VICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA04015 1 20080728 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EXIT LIGHT IN FLIGHT DECK INOP. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECK GOOD. AC OK FOR SERVI CE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA04017 1 20080728 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 53L FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EEL INOP SEAT 53L. *S/D* FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 2008 9 11 2008UALA04024 4 20080726 A 2350 MICROPHONE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OXYGEN MASK INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 648UA 25285 CAPTAIN'S OXYGEN MASK MIC INOP. *S/D* SUSPECT PRE FLIGHT CHECKS. REPLACED NR 1 O2 BOX. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04021 1 20080725 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 47C BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 193UA 26890 THE 47C EMERGENCY PATH LIGHTING STRIP BROKEN OFF. *S/D* FOUND LIGHT ASSEMBLY BROKEN. REPLACED LIGHT ASSEMBLY, OP CHEC K GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA04058 1 20080728 A 3350 582240 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 667UA 29239 ENTIRE FIRST CLASS CABIN LT SIDE EEL INOP. *S/D* FOUND FAULTY BATTERY PACK. REPLACED BATTERY PACK, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04059 1 20080728 A 3350 UNK WIRE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 667UA 29239 LEFT AFT OVERWING SLIDE LIGHT INOP. *S/D* FOUND BROKEN WIRE. REPAIRED WIRE, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04061 1 20080728 A 3350 D71702001 POWER SUPPLY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 774UA 26936 SEAT EMERGENCY EXIT LIGHTS INOP FROM SEAT 11 TO 15. *S/D* FOUND FAULTY POWER SUPPLY AND LIGHT ASSEMBLY. REPLACED POWE R SUPPLY AND LIGHT ASSEMBLY, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NM 2008 9 11 2008UALA04080 1 20080801 A 3350 FU305 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY LIGHT INOP: LT OVERWING 2 FWD ASSY'S. *S/D* FOUND FAULTY FUSE. REPLACED FUSE, OP CHECK GOOD. AC OK FOR SE RVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA04082 1 20080801 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 WALL EEL INOP: LWR WALL BETWEEN MID LAVS. *S/D* FOUND BURNED OUT LIGHT ASSEMBLY. REPLACED LAMP, OP CHECK GOOD. AC O K FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA04134 1 20080804 A 3350 61441 CAP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT DISLODGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 644UA 25094 EMERGENCY EXIT LIGHTS LOOSE L AISLE 1ST CLASS. *S/D* FOUND LOOSE END CAP LIGHT ASSEMBLY. INSTALLED END CAP. AC OK FO R SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04083 1 20080801 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY LIGHT INOP: DOOR 5R SLIDE ILLUM. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECK GOOD. AC OK FOR SER VICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA04099 1 20080801 A 2741 342381 MOTOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE STAB CONTROL LEAKING A UALA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 29 219UA 30551 HYDRAULIC FLUID LEAKING FROM AFT STAB COMP DRAINS. *S/D* FOUND LEAKING CENTER STABILIZER HYDRAULIC MOTOR. REPLACED CE NTER STAB HYD MOTOR, REF MM 27-41-11, OP AND LEAK CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NM 2008 9 11 2008UALA04142 1 20080806 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 501UA 24622 STRONG ELECTRICAL ODOR FROM MID CABIN. FLIGHT DIVERTED. *S/D* NO FAULT FOUND. 2 L 7 2 4F 4 F RT A2NM E17NE 20080911 NM 2008 9 11 2008UALA04214 1 20080809 A 2600 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FIRE BOTTLE IND INOPERATIVE A UALA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 WP 29 210UA 30216 FIRE BOTTLE ARMED AND BOTTLE DISCHARGED LIGHTS ON P-40 PANEL INOP. *S/D* FOUND CORRODED INDICATOR LIGHT SOCKETS. REPL ACED INDICATOR ASSEMBLY'S OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NE 2008 9 11 2008UALA04272 2 20080814 A 7321 RELAY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT ENG FUEL FAILED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 773UA 42510 4027 26929 777009 LEFT ENGINE DID NOT SHUT DOWN NORMALLY WHEN ON GATE. EICAS MSG ENG FUEL VALVE LEFT DISPLAYED. *S/D* REPLACED FUEL MAN AGEMENT UNIT (FMU), NO HELP. REPLACED FUEL CONTROL RELAYS, RAN ENGINE 4 TIMES, SHUTDOWN NORMALLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NE 2008 9 11 2008UALA04275 2 20080814 A 7261 FILTER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE ENGINE OIL UNKNOWN A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 665UA 62717 10543 29237 724627 R ENG OIL FILTER EICAS LIGHT ILLUM APPROX 1 MIN, WENT AWAY. R OIL FILTER STATUS MSG REMAIN. *S/D* REPLACED MAIN OIL F ILTER. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04250 1 20080811 A 4900 263BA1011 BATTERY BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE APU FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 799UA 26926 APU BATTERY STATUS MESSAGE. *S/D* FOUND FAULTY BATTERY. REPLACED APU BATTERY PER MM 24-31-05, OP CHECK GOOD. AC OK F OR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NM 2008 9 11 2008UALA04251 1 20080811 A 2432 263BC1012 CHARGER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 799UA 26926 BATTERY CHARGER APU STATUS MSG. *S/D* FOUND FAULTY BATTERY CHARGER. REPLACED BATTERY CHARGER PER MM 24 -31-06, OP CHE CK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 EU 2008 9 11 08FDEA03125 1 20080729 A 5330 A5397355400400 HOUSING AIRBUS 300 A300B4622R 3930312 EU RAD ALT ANTENNA CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 AFT LOWER EXTERIOR FUSELAGE; RADIO ALTIMETER ANTENNA DOME NUT RING IS CORRODED IN SEVERAL AREAS. REMOVED ANTENNA HOUSIN G IAW A300-600 SRM 51-40-21. LOCATED & DRILLED NEW ANTENNA HOUSING P/N A5397355400400, PO 627058.2 IAW SRM 53-17-12 & S RM 51-40-44. INSTALLED ANTENNA HOUSING IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080911 EU 2008 9 11 08FDEA03127 1 20080729 A 5311 FRAME AIRBUS 300 A300B4622R 3930312 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 DURING INSPECTION FOUND SEVERAL TOOL MARKS WERE FOUND ON FR47 RT FORWARD AND AFT FITTING, STR 21-26. REPAIR PERFORMED B Y DEPENDING PERFORMING SMOOTH REWORK AND SPOT FACING IAW RAS 70511944/017/2008 ISSUE A AND EA 6-5310-120093. 2 L 7 2 4F RT A35EU 20080911 NM 2008 9 11 2008UALA04297 1 20080816 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 DOOR 4 RT AFT EXIT LIGHT INOP. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECK GOOD. ACFT OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA04302 1 20080818 A 2910 LINE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HYDRAULIC SYSTEM FAILED A UALA O OTHER K FLUID LOSS AP APPROACH 1 WP 29 774UA 26936 CTR HYD QUANTITY WENT TO 0 ON 1 MILE FINAL APPROACH. FOUND NOSE STEERING FLEX LINE LEAKING IN NOSE WHEEL WELL. REPLACE D LINE. SERVICED CENTER HYD SYSTEM. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NM 2008 9 11 08FDEA02854 1 20080714 A 5712 ARB2850506 RIB DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 597FE 48596 RIGHT HAND WING LEADING EDGE NR 16 TRACK INBOARD RIB FOUND CRACKED. RIGHT HAND WING LEADING EDGE NR 16 TRACK INBOARD RI B REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. RIGHT NR 8 SLAT CABLE ADJUSTMENT AND TEST CARRIED OUT FOUND 'SATIS' AS PER AMM 27-80-00-5. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080911 EU 2008 9 11 08FDEA03118 1 20080729 A 5315 A53974268200 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 CORROSION ON CARGO FLOOR CROSSBEAM FR56 RT, AFT CARGO COMPARTMENT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 208 SHE ET 4. 2 L 7 2 4F RT A35EU 20080911 EU 2008 9 11 08FDEA03119 1 20080729 A 5330 A53973278202 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 OLD REWORKS AT SKIN PANEL AT AFT CARGO DOOR CUTOUT, FR63A, STR 29 RT. ONE IS OUT OF SRM LIMIT. REPAIR PERFORMED BY REW ORK AND FLAP PEENING IAW RAS/EFW/9000067/2008 ISSUE B, APPROVED BY EA 6-5317-120099. 2 L 7 2 4F RT A35EU 20080911 NM 2008 9 11 2008UALA04305 1 20080815 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L1 DOOR INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 642UA 25092 DOOR 1L LOWER EXIT LIGHT INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20080909 EU 2008 9 9 2008UALA04009 1 20080726 A 3150 WARNING LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ILLUMINATED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 448UA 842 THE "SLIDE PRESS LOW. CHECK SLIDE PRESS EMER R, EMER L" DISPLAYED ON PTP PANEL AFTER INSTALLATION OF AFT LEFT SIDE EMER GENCY OVERWING EXIT. *S/D* RESET AIRCRAFT PWR MSG DISAPPEARED. OPS TEST EMERGENCY LIGHTS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA04095 1 20080804 A 2841 INDICATION SYS BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FUEL QTY ERRATIC A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 782UA 26948 FUEL QTY SHOWS ERRATIC. RIGHT WING QTY IND. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080909 NM 2008 9 9 2008UALA04106 1 20080802 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 813UA 858 BEAM 145 CORRODED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA04107 1 20080802 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 813UA 858 BEAM 140 CORRODED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA04109 1 20080802 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 813UA 858 BEAM 80 CORRODED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA04121 1 20080802 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 198UA 28716 SEAT 4A EEL STRIP IS LOOSE. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080909 EU 2008 9 9 2008UALA04170 1 20080808 A 2133 OUTFLOW VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN PRESSURE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 411UA 464 PRESSURIZATION PROBLEMS. FLIGHT DIVERTED. FOUND PFR FAULTING OUTFLOW VALVE 81. REPLACED OUTFLOW VALVE. OPS CHECKED G OOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 EU 2008 9 9 2008UALA03988 1 20080726 A 2621 BA21758 FIRE BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LAVATORY OUT OF TOLERANCE A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 457UA 1146 LAV -A FIRE EXTINGUISHER SYSTEM - FOUND 1L LAV FIRE EXTINGUISHER IN THE RED. *S/D* REPLACED FWD LAV -A EXTINGUISHER. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA04171 1 20080808 A 5610 WINDOW BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT CRACKED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 914UA 25381 CREW REPORTS, THE CAPTAIN'S NR 4 WINDOW PANE IS CRACKED. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 EU 2008 9 9 2008UALA04172 1 20080808 A 2611 CG76011 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E/E BAY FALSE ACTIVATION A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 439UA 683 AVIONICS SMOKE ECAM DISPLAYED AFTER TAKEOFF, NO PERCEPTIBLE SMOKE DETECTED. RAN SUCCESSFUL TEST OF AEVC & RESET BOTH FL IGHT WARNING COMPUTERS (PRECAUTIONARY). INSTALLED NEW SMOKE DETECTOR 2WA. OPS CHECK SATISFACTORY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA04173 1 20080808 A 2100 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN AIR UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 398UA 24673 EQUIPMENT COOLING EXHAUST OFF LIGHT ILLUM. REPLACE MULTIPLE PARTS (ALT EXHAUST BLOWER, EXHAUST AIRFLOW DETECTOR, TURBOF AN VALVE) 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 2008UALA04165 1 20080806 A 2612 CONTROL PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE DETECTION MALFUNCTIONED A UALA O OTHER N FALSE WARNING CR CRUISE 1 WP 29 374UA 24639 CARGO DECT FWD PIT B-LOOP ON IN FLIGHT. TEST RESET SYSTEM, BEGAN TO FLICKER AGAIN. FOUND FAULTY FIRE PANEL. REPLACED FAULT ANNUNCIATION FIRE PANEL AS A PRECAUTIONARY ACTION. SYSTEM OPERATES NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 EU 2008 9 9 08FDEA03679 1 20080901 A 5320 A53980269201 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND DAMAGED ANGLE (ELONGATED HOLES) AT C75, P 26 RT. REPAIR PERFORMED BY REWORK THE HOLES AND INSTALLING RIVETS HL 10 VF8 IN AFFECTED HOLES IAW RAS/EFW/9000084/2008 ISS A, APPROVED BY EA 6-5318-123076. 2 L 7 2 4F RT A35EU 20080909 WP 2008 9 9 08FDEA03688 1 20080901 A 5350 ANB70513 ANGLE DOUG MD10 MD1010F 3022112 WP BS 1421 BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 THERE IS A BROKEN VERTICAL ANGLE AT THE LEFT WING TO BODY FAIRING SUPPORT AT STA 1421; ABOVE THE LEFT WING. REMOVED & R EPLACED ANGLE ANB 7051-3 IAW SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 20080909 SO 2008 9 9 NTB2008F00001 2 20080808 A 7414 SPRING PIPER PA28 PA28R201T 7102813 SO CONT O360 TSIO360F 17025 SO IMPULSE COUPLING BROKEN E NTBA O OTHER O OTHER NR NOT REPORTED 1 NM 05 5880V 14 D07HA272R 28R7703158 834910R IMPULSE COUPLING SPRING BROKEN. EVIDENCE OF PRE-EXISTING CRACK AND CORROSION. VERY LOW TIME IS SERVICE. MAG TO ENGINE TIMING LOST. BOTH MAGS EXPERIENCED THE SAME FAILURE ALMOST SIMULTANEOUSLY. (K) 1 L 7 1 3O 3 O 2A13 E9CE 20080911 NM 2008 9 11 2008UALA04307 1 20080815 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 642UA 25092 MED CABIN EEL LIGHT AT FRONT OF LAVS LEFT AND RIGHT INOP. FOUND DAMAGED CONNECTORS. REPAIRED LT & RT EMERGENCY LIGHT CABLE CONNECTORS. OP CHECKED OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20080909 NM 2008 9 9 2008UALA04037 1 20080730 A 5300 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 813UA 858 BEAM 150 CORRODED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA03950 1 20080724 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FUMES A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 556UA 26650 SMOKE IN CABIN. FLIGHT DIVERTED. *S/D* DUE TO REPORT OF SMOKE AND FUMES IN CABIN, WHICH TRIGGERED THE MID LAV SMOKE D ETECTOR TO GO OFF AND AFTER MANY SYSTEM AND COMPONENT CHECKS NOTHING WAS FOUND THAT WOULD HAVE CAUSED THIS PROBLEM. CHE CKED ALL LIGHTS IN CABIN AND LAVS FOUND NO FAULTS. RAN PACKS AND FOUND NO FAULTS WITH APU AIR. RAN RT PACK WITH NR 2 E NG AT IDLE AND FOUND NO PROBLEMS. CREW STATED THAT THERE MAY HAVE BEEN VERY MINIMAL SENT OF FUMES BUT NOT DEFINITIVE PR IOR TO THEM DAWNING O2 MASKS. 2 L 7 2 4F 4 F RT A2NM E17NE 20080909 EU 2008 9 9 2008UALA03963 1 20080724 A 3510 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CAPTAIN'S FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 455UA 1105 CAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. *S/D* SHORT IN BOX OR MASK (UNABLE TO DETEMERMINE). REMOVED AND REPL ACED CAPTS O2 BOX AND MASK ALONG WITH AMU- OPS CHECK GOOD, LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 08FDEA03663 1 20080901 A 5330 NDA63135 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 594FE 48552 FUSELAGE EXTERIOR FOUND FORWARD CARGO DOOR CUTOUT AFT LOWER EDGE CHIPPED. CARRIED OUT REPAIR AS PER SRM 53-50-00 FIGURE 7 VOLUME I. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080909 NM 2008 9 9 2008UALA04005 1 20080724 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 538UA 25222 CREW REPORTED EMERGENCY FLOOR LIGHTING LAST 2 FEET AFT CABIN INOP. *S/D* EEL DISCONNECTED AT STRIP. RECONNECTED LIGHT STRIP, OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080909 NM 2008 9 9 2008UALA04118 1 20080802 A 3397 3004071 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY EXIT SIGN ON DOOR 4L INOP. FOUND UNSECURE CONNECTOR. RESECURED CONNECTOR. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080909 NM 2008 9 9 2008UALA03965 1 20080724 A 2121 FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 551UA 25399 SMELL OF OIL IN CONDITIONED AIR IN DESCENT UNTIL ENGINE SHUTDOWN AT GATE. *S/D* RAN BOTH ENGINES AT IDLE AND HIGH POWE R, WITH PACKS ISOLATED. NO SMOKE OR FUMES NOTED PER FIM 21-00-01. NOTED MUSTY ODOR WITH LEFT RECIRCULATION FAN, REPLAC ED FILTER, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080909 EU 2008 9 9 08FDEA03668 1 20080901 A 5340 A53970709202 FITTING AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND IN AFT CARGO COMPARTMENT CORNER FITTING AT C56 LT WITH CORROSION. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080909 2008 9 9 2008UALA04111 4 20080803 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 492UA 1755 DOOR 2R SLIDE PRESSURE LOW. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 EU 2008 9 9 2008UALA04155 1 20080803 A 2612 FIRE LOOP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 NACELLE MALFUNCTIONED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 452UA 955 FIRE LOOP-A FAULT DISPLAYED ON UPPER ECAM SCREEN, ENG 2. REPLACED CORE LOOP ASSY. ACP FIRE TEST AND FDU TEST IN CFDS. O P CHKS NORMAL 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 NM 2008 9 9 2008UALA03983 1 20080725 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 569UA 26677 EXIT LIGHT DOOR 2L NEEDS RE-ATTACH. *S/D* REPLACED EXIT SIGN, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080909 NM 2008 9 9 2008UALA04093 1 20080804 A 2520 9F23535503 SEAT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ROW 3 ABC MISINSTALLED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 350UA 24301 SEAT ROW 3 ABC UNSECURE. RTFL. SEAT INSTALLED INCORRECTLY. INSTALLED SEAT CORRECTLY. 2 L 7 2 4F 4 F RT A16WE E21EU 20080909 NM 2008 9 9 2008UALA04098 1 20080801 A 5320 PROFILE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 813UA 858 THE 2T PROFILES DAMAGED AT STA 70 WHERE BEAM 155 ATTACHED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080909 2008 9 9 2008UALA03914 4 20080721 A 2350 MICROPHONE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OXYGEN MASK FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 418UA 485 THE O2 WORKS ON ALL 3 MASKS, MICROPHONE FOR ALL 3 MASKS ARE INOP. *S/D* AFTER FURTHER ANALYSIS, IT HAS BEEN DETERMINED THIS IS NOT AN SDR REPORTABLE EVENT. ALL FLT DECK MASKS OPS CK OK. NO EVIDENCE THAT THERE EVER WAS AN ISSUE WITH THE SYSTEM OF THE A/C. 2 L 7 2 4F 4 F RT A28NM E40NE 20080910 NM 2008 9 10 UIE2008F00028 1 20080825 A 5730 PANEL BOEING 747 747341 13848AM NM RT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 R/H WING UPPER SURFACE LEADING EDGE PANEL HAS A 3" CRACK LOCATED AT ILES 818.5 AND 9" FROM LEADING EDGE OF PANEL. ALSO , REFERENCE ATLAS AIR EO NO. 4757A458. UIEA200800297. 2 L 7 4 4F RT A20WE 20080910 NM 2008 9 10 AALA200802013 1 20080802 A 3350 SOCKET BOEING 757 757223 1384957 NM EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 631AA 24589 ORD, EMERGENCY LIGHT SOCKET AT SEAT 17D AFT DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 17D AFT. SYS TEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 WP 2008 9 10 AALA200801938 1 20080723 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9617R 53564 ORD EMERGENCY LIGHTS AT SEAT ROWS 19DEF TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT RO WS 19DEF TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A6WE 20080910 NM 2008 9 10 AALA200802034 1 20080805 A 2400 BUSS BOEING 767 767323 1385205 NM ELECTRICAL FAILED A AALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 378AN 25447 LHR INFLIGHT T93/05AUG DUB TO ORD. CREW REPORTED UTILITY BUSS FAULT. LANDED LHR WITHOUT INCIDENT. REPLACED RELAYS K1 AND K2 ON ELECTRONIC CONTROL PANEL. ALSO REPLACED BUSS POWER CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20080910 NM 2008 9 10 AALA200801940 1 20080723 A 3350 P4010051112 MODULE BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 609AA 27447 LAX SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 17 TO 26 INOPERATIVE. REPLACED MODULE FOR EMERGENCY LIGHTS AT SEAT ROWS 17 TO 26. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 WP 2008 9 10 AALA200801970 1 20080726 A 2120 UNKNOWN DOUG DC9 DC983 3022083 WP CABIN ODOR A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 9624T 53583 ABQ INFLIGHT T2457/26JUL DFW TO LAX. CREW REPORTED ELECTRICAL ODOR IN COCKPIT AND FLIGHT ATTENDANTS REPORTED HAZE NEAR AFT GALLEY. LANDED ABQ WITHOUT INCIDENT. COULD NOT DUPLICATE. NO HAZE OR ELECTRICAL ODOR NOTED. SYSTEM GROUND CHECKE D NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A6WE 20080910 EA 2008 9 10 N6WA0080804 1 20080824 A 3240 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA BRAKE FALSE ACTIVATION A N6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 156GJ 10227 5314 DAY. BRAKE OVHT ON TAKEOFF ROLL. RETURNED TO FIELD PER QRH. NR 2 BRAKE. DEFERRED BTMC FOR NR 2 BRAKE PER MEL 32 -46-01, CAT B ON DMI 6706. C/W REC 670-32-46-00-01. 2 L 7 2 4F RT A21EA 20080910 NM 2008 9 10 AALA200801948 1 20080724 A 3350 0201720001 LIGHT BOEING 737 737823 13844BZ NM SEAT 22D BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 915AN 29516 LAX EMERGENCY LIGHT AT SEAT 22D BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A16WE 20080910 EU 2008 9 10 USAA920081567 1 20080824 A 2530 COFFEEMAKER AIRBUS A319 A319112 3930323 EU GALLEY BROKEN A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 19 714US 1046 FLT 1062 ABE CLT BURNING ODOR FORWARD COFFEEMAKER HAD ELECTRICAL ODOR. TURNED OFF AND PULLED CIRCUIT BREAKER. NO FURTH ER PROBLEMS NOTICED. 2 L 7 2 4F RT A28NM 20080910 NE 2008 9 10 2008UALA04087 2 20080728 A 7261 OIL COOLER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 654UA 45208 11738 25392 727698 NR 2 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT. *S/D* SECURED OIL COOLER BYPASS INLET TUBE B-NUT. SUBSEQUENT OIL CONSUMP TION 0.28 QTS PER HOUR - WITHIN LIMITS. NO FURTHER PROBLEMS. 2 L 7 2 4F 4 F RT A1NM E24NE 20080910 NM 2008 9 10 2008UALA04104 1 20080802 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 660 S23L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 FWD PIT AT STA 660, STR 23L, FRAME DENTED AT INBOUND FLANGE. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. CUT OUT DAMAGE A ND INSTALLED DOUBLER REPAIR PER SRM 53-00-07, REPAIR 5. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 NM 2008 9 10 2008UALA03755 1 20080706 A 3350 GE1317 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 642UA 25092 EXT EMERGENCY LIGHT AT DOOR 2L INOP. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080910 NM 2008 9 10 2008UALA03758 1 20080706 A 3350 3015645 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT OVERWING INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 642UA 25092 EXT EMERGENCY LIGHT JUST AFT OF LT WING INOP. *S/D* FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080910 NM 2008 9 10 2008UALA03762 1 20080705 A 3350 582240 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 657UA 27112 L1 DOOR EMERGENCY EXIT LIGHT IS INOP. *S/D* FOUND FAULTY POWER SUPPLY. REPLACED POWER SUPPLY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008010900041 20080109 00041 EU 2008 1 9 08FDEA00008 1 20080102 A 5320 Y5382971220000 WEB AIRBUS 300 A300B4622 3930401 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 FOUND LWR FUSELAGE FR 50 BETWEEN SEAT TRACK 3L THRU 4L, CARGO LOADING SYS SUPPORT WEB IS BENT ALONG THE O/B LWR EDGE. R EMOVED AND REPLACED LOADING SYS SUPPORT WEB AT FR 50 IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008010900048 20080109 00048 EU 2008 1 9 08FDEA00015 1 20080103 A 5320 A5383210420600 WEB AIRBUS 300 A300B4622 3930401 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 LWR FUSELAGE FR 49 BETWEEN SEAT TRACK 3L AND 4L 12" TO 24" BELOW FLOOR . THE STIFFENER WEB IS BENT AFT 1/4". REMOVED A ND REPLACED WEB IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008010900343 20080109 00343 NM 2008 1 9 SWAA080089 1 20080102 A 5312 6545819 PRESSURE PANEL BOEING 737 7375H4 138449D NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND NLG W/W LEFT CEILING WEB CRACKED AT SNUBBER ATTACH NUT PLATE. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 2008010900368 20080109 00368 SO 2008 1 9 C2XA08RI004 1 20080102 A 3350 10049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16571 145633 RIC - DURING ROUTINE MAINTENANCE, MX FOUND RIGHT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED BATTERY POWER SUPPLY IAW EMB145 AMM 33-50-04 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008010900375 20080109 00375 EA 2008 1 9 TRAX200800017 1 20080101 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 906EV 7642 FLAP FAIL MESSAGE, EMERGENCY DECLARED. FLT 4313 DEL 80 MINS. 2 L 7 2 4F RT A21EA 2008010900378 20080109 00378 EA 2008 1 9 TRAX200800020 1 20080102 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 975EV 7599 FLAPS FAIL ZERO DEGREE AT 210 KNOTS >12000 FT, EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2008011000014 20080110 00014 NM 2008 1 10 SWAA080003 1 20080101 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 255WN 32513 EEPLS LENS MISSING AT ROW 3 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008011000027 20080110 00027 NM 2008 1 10 SWAA080012 1 20080101 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737E, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011000029 20080110 00029 NM 2008 1 10 SWAA080013 1 20080101 A 5512 65C25727 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 152. REPAIRED SKIN PER BOEING SB. 2 L 7 2 4F RT A16WE 2008011000033 20080110 00033 NM 2008 1 10 SWAA080045 1 20080101 A 5320 6551639 TEE FITTING BOEING 737 7375H4 138449D NM RT MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND RIGHT W/W SUPPORT RING LOWER TEE CHORD CRACKED AT STA 712. REPAIRED TEE CHORD PER SR M. 2 L 7 2 4F RT A16WE 2008011000035 20080110 00035 NM 2008 1 10 SWAA080043 1 20080101 A 5311 6546536 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011000037 20080110 00037 NM 2008 1 10 SWAA080022 1 20080101 A 7120 310A10212 MOUNT BOEING 737 7375H4 138449D NM LT WING WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED SERVICE CHECK, FOUND NR 1 ENGINE FWD OUTBOARD MOUNT WORN. REMOVED AND REPLACED MOUNT PER MM. 2 L 7 2 4F RT A16WE 2008011000039 20080110 00039 NM 2008 1 10 SWAA080038 1 20080101 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008011000044 20080110 00044 NM 2008 1 10 SWAA080054 1 20080101 A 5754 65C26602 SKIN BOEING 737 7373TO 138447G NM L/E SLAT DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 4 L/E SLAT OUTBOARD UPPER T/E SURFACE DISBONDED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008011000045 20080110 00045 NM 2008 1 10 SWAA080056 1 20080101 A 5310 6519603 CREASE BEAM BOEING 737 7373TO 138447G NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 364 TO BS 376, RBL 70. REMOVED AND REPLACED WEB PER SR M. 2 L 7 2 4F RT A16WE 2008011000046 20080110 00046 NM 2008 1 10 SWAA080055 1 20080101 A 5753 6573731 FLAP BOEING 737 7373TO 138447G NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND RT WING INBOARD MID FLAP DELAMINATED AT T/E. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2008010900256 20080109 00256 NM 2008 1 9 SWAA080002 1 20080101 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 231WN 32499 MID CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008010900257 20080109 00257 NM 2008 1 9 SWAA080021 1 20080101 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 281WN 36528 R1 DOOR EMERGENCY EXIT LIGHT ASSY LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008010900260 20080109 00260 NM 2008 1 9 SWAA080028 1 20080101 A 2730 656531014 TORQUE TUBE BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2008010900262 20080109 00262 NM 2008 1 9 SWAA080011 1 20080101 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED MV3 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008010900264 20080109 00264 NM 2008 1 9 SWAA080014 1 20080101 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 RIGHT OVERWING EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2008010900267 20080109 00267 NM 2008 1 9 SWAA080057 1 20080101 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 495WN 33869 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008010900269 20080109 00269 2008 1 9 SWAA080032 4 20080101 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008010900270 20080109 00270 NM 2008 1 9 SWAA080033 1 20080101 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED THRU CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 971, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011000016 20080110 00016 NM 2008 1 10 SWAA080020 1 20080101 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 275WN 36153 EEPLS ASSY LOOSE AT ROW 1 ABC. REMOVED AND REPLACED EEPLS ASSY PER MM. 2 L 7 2 4F RT A16WE 2008011000031 20080110 00031 NM 2008 1 10 SWAA080030 1 20080101 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011000041 20080110 00041 NM 2008 1 10 SWAA080039 1 20080101 A 5311 6545812 FRAME BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008011000050 20080110 00050 NM 2008 1 10 SWAA080019 1 20080101 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 774SW 27882 LEFT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008011000086 20080110 00086 NM 2008 1 10 ASAA0842451 1 20080102 A 5210 507945299 DOOR BOEING 737 737490 1384715 NM L1 DOOR BINDS A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 795AS 28890 FLT ATTENDANT HAS TROUBLE OPENING L1 DOOR. CARRIED OUT GENERAL VISUAL INSPECTION OF L1 DOOR. NO DEFECTS NOTED. OPERAT IONAL CHECK COMPLETED, NO FAULTS FOUND. OP CHECKS GOOD PER MM 52-11-00. 2 L 7 2 4F RT A16WE 2008011000090 20080110 00090 NM 2008 1 10 SWAA080063 1 20080102 A 5311 6546554 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011000093 20080110 00093 NM 2008 1 10 SWAA080069 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011000098 20080110 00098 NM 2008 1 10 SWAA080074 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011000105 20080110 00105 NM 2008 1 10 SWAA080080 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011000108 20080110 00108 NM 2008 1 10 SWAA080088 1 20080102 A 5312 6545819 PRESSURE PANEL BOEING 737 7375H4 138449D NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND NLG W/W RIGHT CEILING WEB CRACKED AT SNUBBER ATTACH NUT PLATE. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 2008011000019 20080110 00019 NM 2008 1 10 SWAA080008 1 20080101 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 RIGHT OVERWING EMERGENCY EXIT SIGN LENS FELL OFF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008011000026 20080110 00026 NM 2008 1 10 SWAA080009 1 20080101 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008011000030 20080110 00030 NM 2008 1 10 SWAA080031 1 20080101 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011000034 20080110 00034 NM 2008 1 10 SWAA080044 1 20080101 A 5311 6546543 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011000049 20080110 00049 NM 2008 1 10 SWAA080027 1 20080101 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 774SW 27882 LEFT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008011000091 20080110 00091 NM 2008 1 10 SWAA080064 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011000096 20080110 00096 NM 2008 1 10 SWAA080072 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011000100 20080110 00100 NM 2008 1 10 SWAA080075 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011100027 20080111 00027 EU 2008 1 11 2008UALA0005 1 20080101 A 5210 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR READS LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 497UA 1847 BOTTLE AT DOOR 2R INDICATES LOW. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011100039 20080111 00039 NM 2008 1 11 2008UALA0015 1 20080102 A 2751 WARNING MESSAGE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT ACTIVATED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 212UA 30218 DURING GROUND TEST OF RIGHT FLAPERON MSG 27-16039 OCCURS. ACCOMPLISHED TEST SEVERAL TIMES WITH SAME RESULT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008011100077 20080111 00077 NM 2008 1 11 2008UALA0032 1 20080102 A 5320 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 BS 291.5 INTERCOSTAL ATTACH ANGLE IS CRACKED BELOW STR 13R. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011100086 20080111 00086 NM 2008 1 11 ASAA0852452 1 20080102 A 3150 233A3101 WARNING SYSTEM BOEING 737 737890 1384527 NM COCKPIT MALFUNCTIONED A ASAA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 NM 02 577AS 35186 ON AFTER START RECALL MASTER CAUTION STAYED ON WITH AIR COND ZONE TEMP ON OVERHEAD PANEL. UNABLE TO DUPLICATE. BITE TE ST GOOD (REF FIM21 62 TASK 832). NO HISTORY LAST 30 DAYS. 2 L 7 2 4F RT A16WE 2008011100088 20080111 00088 EA 2008 1 11 TRAX200800021 1 20080102 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 975EV 7599 FLAPS FAIL AT 0 WHEN DEPLOYED AT 200 KNOTS AT 2000'. TOWER DISPATCHED EMERGENCY EQUIPMENT AS A PRECAUTION. FLT 4809 CX . 2 L 7 2 4F RT A21EA 2008011100089 20080111 00089 EA 2008 1 11 TRAX200800023 1 20080102 A 5260 STEP CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 755EV 10185 ASD LOWER STEP CRACKED. 2 L 7 2 4F RT A21EA 20080909 EU 2008 9 9 2008UALA03987 1 20080726 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT WEAK A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 416UA 479 BATTERY EMERGENCY R DISPLAYED AFTER CHECK OF CABIN EMERGENCY LIGHT TEST. *S/D* WEAK BATTERY. REPLACED BATTERY PER MM. TEST OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008010900036 20080109 00036 NM 2008 1 9 08FDEA00005 1 20080102 A 2910 54C54673D01 CONTROL VALVE BOEING 727 727227 1384078 NM HYD SYSTEM FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 483FE 21465 ARM LIGHT AND CARGO DOOR IN TRANSIT LIGHT ILLUMINATED IN FLIGHT. PRESSURIZATION REMAINED NORMAL. REPLACED HYDRAULIC SO LENOID SHUTOFF VALVE PER MM 52-34-129-4. REPLACED HYDRAULIC CONTROL VALVE PER MM 52-34-101-4. OPS OK PER MM 52-34-009- 5. 2 L 7 3 4F A3WE 2008010900037 20080109 00037 EU 2008 1 9 08FDEA00006 1 20080102 A 5320 A5381206720100 TRACK AIRBUS 300 A300B4622 3930401 EU ZONE 200 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 LT TRACK I/1456 FR 48 AFTER REMOVAL OF WEB FOUND 1 LINK TRACK WITH BENT TAB ON I/B SIDE. REMOVED AND REPLACED SUPPORT L INK AT LT TRACK I/1456 FR 48 IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008010900050 20080109 00050 EU 2008 1 9 08FDEA00017 1 20080103 A 5320 A5383210420600 WEB AIRBUS 300 A300B4622 3930401 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 LWR FUSELAGE FR 53 BETWEEN SEAT TRACK 3L AND 4L 12" TO 24" BELOW FLOOR, STIFFENER WEB BENT AFT 1/2" ALONG THE TOP EDGE. REMOVED AND REPLACED WEB IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008010900060 20080109 00060 EU 2008 1 9 08FDEA00027 1 20080103 A 5420 BEAM AIRBUS 310 A310221 3930310 EU NR 2 PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 NR 2 ENGINE PYLON AFT BEAM ATTACHMENT MOUNT HAS SEVERE RUST ON BOTTOM FACE OF MOUNT. CLEANED BEAM ASSY. IAW AMM 54-51- 00-6.5 B-1. REMOVED CORROSION FROM BEAM SURFACE IAW 54-51-00-6.5 B-1 & SRM 51-74-10 ITEM 7 B-2, ITEM 5 A-5 & PMS 01-01-1 4-1. POLISHED REWORKED AREA IAW AMM 54-51-00-6. PERFORMED PFPI IAW NTM 51-90-00 ON BLENDED AREA (NO CORROSION NOTED). CL EANED BEAM ASSY. IAW AMM 54-51-00-6 PG. 4. CALCULATED AMP HRS. IAW 51-21-10. ADHESION TEST OF DEPOSIT IAW SRM 51-21-10 ( ADHESION GOOD IN BOTH AREAS) & PRIMED REWORKED AREAS IAW AMM 54-51-00-6 01 PG. 5 (HIGH TEMP PRIMER). 2 L 7 2 4F RT A35EU 2008010900341 20080109 00341 NM 2008 1 9 SWAA080079 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010900345 20080109 00345 NM 2008 1 9 SWAA080093 1 20080102 A 5311 6554892 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 320, STR 18L. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008010900347 20080109 00347 NM 2008 1 9 SWAA080094 1 20080102 A 5311 6554892 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 336, STR 18L. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008010900348 20080109 00348 2008 1 9 SWAA080060 4 20080102 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 756SA 27872 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008010900349 20080109 00349 NM 2008 1 9 SWAA080061 1 20080102 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 774SW 27882 DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008010900364 20080109 00364 SO 2008 1 9 C2XA08ON057 1 20080102 A 3610 S2U2226 O-RING EMB 145 EMB145 3260210 SO BLEED AIR SYS BURNED OUT A C2XA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 27 16546 14500562 FLT 421 - SAN TO ONT - AFTER TAKEOFF FLIGHT CREW REPORTED BLEED LEAK. A/C DIVERTED TO ONT WITHOUT NOTIFICATION, BUT NO EMERGENCY WAS DECLARED, A/C LANDED WITHOUT INCIDENTS. MX PERSONNEL FOUND A BLEED LEAK IN THE CARGO COMPARTMENT, REMOVED AND REPLACED BOTH O-RINGS BEHIND PNL 272CRW. OPERATIONALLY CHECKED SATISFACTORY AND A/C WAS RELEASED TO RETURN FOR SER VICE. 2 L 7 2 4F RT T00011AT 2008010900366 20080109 00366 SO 2008 1 9 C2XA08RI002 1 20080102 A 3010 10006491 ANTI-ICE VALVE EMB 145 EMB145LR 3260212 SO WING INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13958 1494 145085 FLT 2708 - EWR - CREW REPORTED WING ANTI ICE FAIL MESSAGE ON EICAS AND PERFORMED AIR RETURN. ACFT LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 1 WING ANTI ICE VALVE IAW EMB145 AMM 30-11-01 AND PERFORMED OPERATIONAL CHECK SUCCESSFUL LY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008010900367 20080109 00367 SO 2008 1 9 C2XA08RI003 1 20080101 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13958 145085 EWR - DURING ROUTINE INSPECTION, MX FOUND EMERGENCY LIGHT FLOOR STRIP NR 1 INOPERATIVE. MX REMOVED AND REPLACED EMERGEN CY LIGHT AC/DC INVERTER IAW EMB145 AMM 33-50-11 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETU RN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008010900374 20080109 00374 EA 2008 1 9 TRAX200800016 1 20080101 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION DE DESCENT 1 SO 27 920EV 7810 FLAP FAIL, EMERGENCY DECLARED. FLT 4317 DEL 35 MINS. 2 L 7 2 4F RT A21EA 2008010900376 20080109 00376 EA 2008 1 9 TRAX200800018 1 20080101 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION TO TAKEOFF 1 SO 27 828AS 7213 FLAPS FAIL ON DEPARTURE AT 0 DEGREES, EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2008011100094 20080111 00094 2008 1 11 SWAA080098 4 20080103 A 2565 63550 SLIDE BOEING 737 737705 13844SC NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 270WN 29089 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008011100098 20080111 00098 NM 2008 1 11 SWAA080099 1 20080103 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504D, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011100113 20080111 00113 NM 2008 1 11 SWAA080097 1 20080103 A 2780 65C268692 CONTROL VALVE BOEING 737 7373H4 1384600 NM L/E SLAT FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 392SW 27379 AIR TURNBACK. DURING CLIMBOUT OF AMA WITH FLAP HANDLE UP AND T/E FLAPS UP NR 1 AND NR 6 L/E SLATS IN TRANSIT LIGHT ILLU MINATED. REMOVED AND REPLACED L/E SLAT CONTROL VALVE AND NR 2 L/E FLAP ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2008011100114 20080111 00114 NM 2008 1 11 SWAA080096 1 20080103 A 2780 4163DA CONTROL VALVE BOEING 737 7373H4 1384600 NM L/E SLAT FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 392SW 27379 AIR TURNBACK. DURING CLIMBOUT OF DEN L/E TRANSIT LIGHT ILLUMINATED. NR 6 L/E SLAT DID NOT MOVE WHEN FLAPS RETRACTED. NO ROLL NOTED. REMOVED AND REPLACED L/E DEVICE CONTROL VALVE PER MM. 2 L 7 2 4F RT A16WE 2008011100116 20080111 00116 NM 2008 1 11 SWAA080104 1 20080103 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011100117 20080111 00117 NM 2008 1 11 SWAA080103 1 20080103 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011100150 20080111 00150 NM 2008 1 11 ZZDA2008002 1 20080103 A 5310 J060228V3 DOOR FRAME BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 991AT 55135 FWD CARGO DOOR JAMB HAS SEVERAL AREAS OF CORROSION BEYOND LIMITS. INSTALLED FWD CARGO DOOR LOWER JAMB PAN CORROSION SPL ICE REPAIR BETWEEN STA 427.00 AND 370.00. 2 L 7 2 4F TR A6WE 2008011000028 20080110 00028 NM 2008 1 10 SWAA080029 1 20080101 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008011000032 20080110 00032 NM 2008 1 10 SWAA080046 1 20080101 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011000047 20080110 00047 NM 2008 1 10 SWAA080001 1 20080101 A 5310 6547978 CREASE BEAM BOEING 737 7373TO 138447G NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 616 TO BS 639, RBL 70. REMOVED AND REPLACED WEB PER SR M. 2 L 7 2 4F RT A16WE 2008011000097 20080110 00097 NM 2008 1 10 SWAA080073 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011000104 20080110 00104 NM 2008 1 10 SWAA080087 1 20080102 A 5753 65C30462 SKIN BOEING 737 7375H4 138449D NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND LT WING INBOARD FORE FLAP LOWER SURFACE DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2008011100157 20080111 00157 NM 2008 1 11 SWAA080125 1 20080106 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER 16L CRACKED AT BS 400. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008011100159 20080111 00159 NM 2008 1 11 SWAA080124 1 20080106 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011100162 20080111 00162 NM 2008 1 11 SWAA080122 1 20080106 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011100177 20080111 00177 NM 2008 1 11 SWAA080133 1 20080106 A 5310 6978062 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT BS NR 5 DOOR STOP. REMOVED AND REPLACED FR AME PER SRM. 2 L 7 2 4F RT A16WE 2008011100179 20080111 00179 NM 2008 1 11 SWAA080135 1 20080104 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 441WN 29837 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008011100181 20080111 00181 NM 2008 1 11 SWAA080157 1 20080106 A 3350 101073 LENS BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2008011100193 20080111 00193 NM 2008 1 11 SWAA080147 1 20080104 A 5610 5893543139 WINDOW BOEING 737 7373Y0 1384671 NM COCKPIT CRACKED A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 665WN 23497 FLIGHT DECK L1 WINDOW CRACKED AND ARCED INFLIGHT. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2008011100194 20080111 00194 NM 2008 1 11 SWAA080148 1 20080105 A 2560 P4010021 BATTERY BOEING 737 7373A4 1384585 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 676SW 23288 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008011100196 20080111 00196 2008 1 11 SWAA080150 4 20080105 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008011100206 20080111 00206 EA 2008 1 11 COMA0860002 1 20080101 A 2752 852D10021 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 924CA 3253 7026 FLIGHT 5682 - RECEIVED FLAP FAIL CAUTION AND STALL FAIL CAUTION MESSAGES. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEFT NR 2 FLAP ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100207 20080111 00207 EA 2008 1 11 COMA0860003 1 20080101 A 2752 853D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 924CA 4021 7026 FLIGHT 5682 - RECEIVED FLAP FAIL CAUTION MESSAGES. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEFT NR 3 FLA P ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100209 20080111 00209 EA 2008 1 11 COMA0860005 1 20080101 A 2752 852D10021 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 924CA 4109 7026 FLIGHT 5682 - RECEIVED FLAP FAIL CAUTION AND STALL FAIL CAUTION MESSAGES. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED RIGHT NR 1 FLAP ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100217 20080111 00217 EA 2008 1 11 COMA0860013 1 20080101 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 SO 01 685BR 7712 FLIGHT 5199 - RECEIVED FLAP FAIL CAUTION MESSAGE. DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED MSP WITHOUT INCIDEN T. COMPLIED WITH SI-2-2710002. PERFORMED FLAP REJUVE ON RIGHT SIDE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100239 20080111 00239 EA 2008 1 11 COMA0860018 1 20080102 A 3040 16591 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 436CA 30789 7482 FLIGHT 5526 - RECEIVED LEFT SIDE WINDOW HEAT CAUTION MESSAGE. RETURNED TO JFK, LANDED WITHOUT INCIDENT. REPLACED LEFT SIDE WINDOW HEAT TEMP CONTROLLER. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100240 20080111 00240 EA 2008 1 11 COMA0860020 1 20080102 A 2752 852D10021 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP CONTAMINATED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 675BR 367 7635 FLIGHT 5391 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEFT SIDE NR 2 FLAP AC TUATOR, DUE TO WATER CONTAMINATION. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100243 20080111 00243 EA 2008 1 11 COMA0860021 1 20080102 A 2752 1104SD100201 FLEX DRIVE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 675BR 7635 FLIGHT 5391 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED RIGHT SIDE NR 2 FLAP F LEX DRIVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100244 20080111 00244 EA 2008 1 11 COMA0860022 1 20080102 A 2752 1104SD100301 FLEX DRIVE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 675BR 7635 FLIGHT 5391 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEFT SIDE NR 3 FLAP FL EX DRIVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100253 20080111 00253 EA 2008 1 11 COMA0860031 1 20080103 A 2752 853D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 924CA 4021 7026 FLIGHT 5483 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEFT FLAP ACTUATOR NR 3. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100260 20080111 00260 EA 2008 1 11 COMA0860038 1 20080103 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 447CA 7552 UPON EDDY CURRENT INSPECTION FOUND AFT PRESSURE BULKHEAD CRACKED AROUND LINTEL ATTACHMENT FITTING. REPAIRED PRESSURE BU LKHEAD WEB FS 621.0 LINTEL INSTALLATION IAW REO 601R-53-61-1230. 2 L 7 2 4F RT A21EA 2008011100262 20080111 00262 EA 2008 1 11 COMA0860039 1 20080103 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 969CA 19904 7141 FLIGHT 5097 - RECEIVED GEAR DISAGREE WARNING MESSAGE. RETURNED TO GRR, LANDED WITHOUT INCIDENT. REPLACED NLG PRIORITY VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100287 20080111 00287 NM 2008 1 11 08FDEA00033 1 20080104 A 5753 SKIN DOUG MD11 MD11F 3023600 NM T/E FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 RIGHT WING, INBOARD FLAP LOWER SURFACE FOUND DENT AT XIFH 147. DENT AREA MEASURED AND DEPTH 0.038" FOUND ACCEPTABLE PE R SRM 57-10-00- FIGURE 17 VOLUME I. HFEC INSPECTION CARRIED OUT AS PER DAC NDT SPM REVISION 13 PART 6 06-10-01.001 O N DENT AREA FOUND NO CRACK EVIDENT. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008011100310 20080111 00310 CE 2008 1 11 DXTA200802738 1 20080101 A 3240 BRAKE ASSY CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG CONTAMINATED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 676QS 5605176 RT BRAKE PEDAL SOFT. GOES TO THE THE STOPS WHEN PRESSED. HOOKED UP BRAKE BLEEDER HOSES AND C/W LT & RT BRAKE BLEEDING. FOUND NUMEROUS AIR POCKETS ON LT & RT BRAKE SYSTEMS. C/W BRAKE BLEEDING ON LH & RH BRAKES. OPS CHECKED GOOD AND TAXI CHECKED GOOD IAW 560 XL M/M CH 32-42-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008011400009 20080114 00009 CE 2008 1 14 DXTA200802754 1 20080108 A 2731 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL PITCH FEEL FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 939QS 7500193 AMBER CAS MESSAGE (PITCH FEEL FAIL) ILLUMINATES IF SPEED EXCEEDS 250K. TROUBLE SHOT DISCREPANCY TO FAILED RT PITCH FEE L ACTUATOR. REMOVED & REPLACED RT PITCH FEEL ACTUATOR IAW 750 M.M. CH. 27-33-00. OPS AND TRAVEL CHECK GOOD 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011400010 20080114 00010 CE 2008 1 14 DXTA200802753 1 20080108 A 3297 WIRE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG WOW DAMAGED E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 374QS 5600475 ON INITIAL CLIMB OUT LANDING GEAR HANDLE WOULD NOT MOVE. REPLACED 5 EA WIRE SPLICES AT LT MAIN GEAR SQUAT SWITCH, REPA CKED LT MAIN GEAR STRUT, SERVICED STRUT, IAW 560 MM 32-11-02, 32-61-00, 32-42-01, 12-14-01 PERFORMED GEAR SWING, OPS CHE CKED GOOD, IAW 560 MM 32-61 2 L 7 2 4F 4 F RT A22CE E25EA 2008011400018 20080114 00018 NM 2008 1 14 AMTA200800004 1 20080101 A 3350 D71701100 BATTERY BOEING 737 73783N 13844HI NM EMERGENCY LIGHTS UNSERVICEABLE A AMTA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 11 305TZ 30706 L1 DOOR INT AND EXT. EGRESS LIGHTS FAIL TO ILLUM. REMOVED AND REPLACED L1 DOOR INT AND EXT EGRESS LIGHT BATT PACK. CHE CK GOOD IAW AMM 33-51-06. (K) 2 L 7 2 4F RT A16WE 2008011400031 20080114 00031 EA 2008 1 14 N6WA0080102 1 20080104 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE EMERGENCY LIGHTS BURNED OUT A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 165GJ 10257 EMERGENCY EXIT SIGN INOP AT ROW 12 LT SIDE. REPLACED BULB. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008011400039 20080114 00039 CE 2008 1 14 GUUA01050801 1 20080105 A 5524 1016200131 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 231YV 25579 UE231 DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOILATED. REPLACED RT ELEVATOR CTR HINGE BRACKET. 2 L 7 2 4T 3 T RT A24CE E2NE 2008011400044 20080114 00044 NM 2008 1 14 JJBA200825267 1 20080106 A 3350 61047811 BATTERY DHAV DHC8 DHC8201 2809001 NM PWA PW120 PW123 NE EMERGENCY LIGHTS DISCHARGED A JJBA K NONE L NO TEST IN INSP/MAINT 1 EA 01 361PH 9073 280 516 EMERGENCY LIGHTING INOP. FOUND THAT EMERGENCY LIGHTING’S BATTERIES (6 EA) WERE DISCHARGED. REPLACED BATTERIES OPS CK SA T. 2 H 7 2 4T 4 T RT A13NM E20NE 2008011600178 20080116 00178 NM 2008 1 16 SWAA080274 1 20080113 A 3350 1619 LIGHT BOEING 737 7375H4 138449D NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED SERVICE CHECK, FOUND LT FWD FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BU LB PER MM. 2 L 7 2 4F RT A16WE 2008011600183 20080116 00183 NM 2008 1 16 SWAA080288 1 20080113 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011600189 20080116 00189 NM 2008 1 16 SWAA080280 1 20080113 A 5311 6546539 FRAME BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 65. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008011600214 20080116 00214 NM 2008 1 16 SWAA080306 1 20080114 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011600215 20080116 00215 NM 2008 1 16 SWAA080305 1 20080114 A 5330 6545767 SKIN BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 427, LBL 1.2. REPAIRED SKI N PER EA. 2 L 7 2 4F RT A16WE 2008011600217 20080116 00217 NM 2008 1 16 SWAA080308 1 20080114 A 3350 311500 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 DURING SCHEDULED HC1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 22 ABC. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2008011600348 20080116 00348 NM 2008 1 16 08FDEA00064 1 20080107 A 5730 ARB74024 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 583FE 48421 06 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC, OPEN HOLE INSPECTION AT RT WING LWR SKIN ACCESS DOOR CUTOUT BETW EEN STA XORS=685 AND STA XORS=710. COMPLIED WITH EA 1-5710-117258, CLASSIFIED AS A MAJOR REPAIR AS PER FEDEX GMM 6-2-10 0. 2 L 7 3 4F RT A22WE 2008011600361 20080116 00361 EU 2008 1 16 MALA080006 1 20080106 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 DENTS LOCATED RT FUSELAGE IN ICE SHIELD AREA BETWEEN FRAME 298 AND FRAME 319. REPAIRED IAW EO NR S53005. 2 L 7 2 4T RT A52EU 2008011600380 20080116 00380 NM 2008 1 16 C8GA20080002 1 20080107 A 2910 BACH8C08NN0290 LINE BOEING 727 727225 1384077 NM HYD SYSTEM CHAFED A C8GA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 29 755DH 21875 FLT 246 FROM EWR TO BDA. DURING DESCENT INTO BDA, THE NR 2 HYDRAULIC "B" SYSTEM PUMP LOW PRESSURE LIGHT ILLUMINATED FOLL OWED BY A PRESSURE DROP TO ZERO PSIG. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FIGHT INSPECTION REVEALED THAT THE PR ESSURE AND RETURN LINES FROM THE RESERVOIR TO THE NR 2 "B" SYSTEM PUMP WERE CHAFED. REMOVED AND REPLACE BOTH PRESSURE A ND RETURN LINES, SERVICED "B" HYDRAULIC SYSTEM, PERFORMED OPS AND LEAK CHECK. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RET URNED TO SERVICE. 2 L 7 3 4F A3WE 2008011600381 20080116 00381 EA 2008 1 16 CHQA200800005 1 20080106 A 2910 601R7528657 LINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE HYD SYSTEM CRACKED A CHQA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 638BR 7311 GEE872506 IAH TO CMH - DURING CLIMB, THE CREW RECEIVED A HYDRAULIC SYSTEM 2 FAIL MESSAGE THEN CONFIRMED THAT THE SYSTEM 2 QUANTITY WAS ZERO. THE AIRCRAFT RETURNED TO FIELD AT IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE HYDRAULIC SYST EM AND FOUND A HAIRLINE CRACK ON THE HYDRAULIC TUBE FROM THE BACK OF THE SERVICING PORT. AFTER CHANGING THE TUBE AND SE RVICING THE HYDRAULICS, THE NR 2 SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2008011700042 20080117 00042 NM 2008 1 17 QXEA200800005 1 20080102 A 3150 WARNING MESSAGE BOMBDR DHC8 DHC8402 1390042 NM FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING LD LANDING 1 NM 09 421QX 4149 PDX - FLIGHT 2239 - PUSHER SYSTEM FAIL CAUTION ILLUMINATED ON LANDING. AFTER CHECKLIST, LIGHT STILL ON. MAINTENANCE CO MPLIED WITH SERVICE LETTER SL-31-005. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008011700044 20080117 00044 NM 2008 1 17 QXEA200800003 1 20080103 A 2620 FIRE BOTTLE BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY MALFUNCTIONED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 403QX 4037 SEA - FLIGHT 2264 - FORWARD BAGGAGE COMPARTMENT FIRE TEST BOTTLE WOULD NOT ARM. MAINTENANCE PLACED ON MEL 26-20-4B. AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008011700047 20080117 00047 EA 2008 1 17 QXEA200800002 1 20080103 A 3097 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA ANTI ICE SYS DAMAGED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 614QX 10049 PDX - FLIGHT 9820 - UPON SELECTING WING ANTI-ICE TO ON RECEIVED A SENSOR MESSAGE. MAINTENANCE REPLACED THE J814 CONNECT OR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008011700048 20080117 00048 NM 2008 1 17 HALA0800008 1 20080107 A 3150 FIRE WARNING BOEING 767 76733A 1385209 NM LT NACELLE FALSE ACTIVATION A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, DURING POWER UP OF ACFT, NOTED L/ENG FIRE LP 1 DISPLAYED ON EICAS. ACCOMPLISHED FIM 26-11-00, WHEN SWAPPING CARDS MSG CLEARED, RETURNED CARDS TO ORIGINAL POSITION, NO FAULTS INDICATED. 2 L 7 2 4F RT A1NM 2008011700055 20080117 00055 2008 1 17 HALA0800010 4 20080109 A 3416 S231T1011 ALTIMETER BOEING 767 76733A 1385209 NM MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 22563 22563 28141 ETOPS SIGNIFICANT SYSTEM, CAPTS BIOMETRIC ALTIMETER FLAG SHOWED UPON FLT DECK CHECK. REMOVED AND REPLACED CAPTS ALTIMET ER AS PER MM 34-13-01, OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2008011700081 20080117 00081 NM 2008 1 17 QXEA200800019 1 20080107 A 2430 DH103024600CS INVERTER DHAV DHC8 DHC8202 2809007 NM PRIMARY ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 356PH 502 PDX - FLIGHT 2172 - STRANGE ODOR FROM THE PRIMARY INVERTER. MAINTENANCE PLACED ON MEL 24-8. AIRCRAFT RETURNED TO SERVI CE. REPLACED THE INVERTER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008011800001 20080118 00001 NM 2008 1 18 NWAA080055640 1 20080104 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 540US 26487 DURING OVERNIGHT LINE CHECK, FOUND SEATS 4, 5, 6, LAV2L, AND F/A SEAT 2L EMERGENCY LIGHTS INOP WHEN TESTED. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2008011800022 20080118 00022 SO 2008 1 18 SIMA200801403 1 20080109 A 3250 1170A350001 POTENTIOMETER EMB 135 EMB135KL 3260302 SO NLG STEERING INOPERATIVE A SIMA O OTHER J WARNING INDICATION LD LANDING 1 SW 21 817AE 145554 ON FLIGHT 4614, CREW REPORTED THAT THEY HAD AN UNCOMMANDED SWERVING BACK AND FORTH OF THE STEERING SYSTEM, ALMOST RAN OF F RUNWAY. CREW WAS ABLE TO STOP ON TAXI WAY USING RUDDER AND DIFFERENTIAL BRAKING. AIRCRAFT TOWED TO THE GATE WITH A T UG. AIRCRAFT REMOVED FROM SERVICE. UPON FURTHER TROUBLESHOOTING FOUND FEEDBACK POTENTIOMETER INOPERATIVE. REMOVED AN D REPLACED FEEDBACK POTENTIOMETER IAW EMB AMM 32-50-07. OPERATIONAL CHECK GOOD. ALSO, ADJUSTED LOAD POTENTIOMETER IAW EMB AMM 32-50-05. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008011800030 20080118 00030 EA 2008 1 18 SWIA200819036 1 20080105 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 433SW 7550 FLT 3911 - EMERGENCY LIGHT COVER ON LEFT SIDE OF ENTRANCE FELL OFF. REPLACED LIGHTED SIGN ASSEMBLY IAW 33-00-00. OPS C HECK GOOD. 2 L 7 2 4F RT A21EA 2008011800129 20080118 00129 EA 2008 1 18 QXEA200800030 1 20080113 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA MAIN PAX STIFF A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 603QX 10011 PDX - FLIGHT 2616 - MAIN CABIN DOOR HARD TO CLOSE. MAINTENANCE PLACED THE DOOR POWER ASSIST ON MEL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008012200006 20080122 00006 NM 2008 1 22 KCSA081004 1 20080108 A 5412 BULKHEAD BOEING 747 747122 1384872 NM NR 4 PYLON GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 716CK 19753 NR 4 PYLON UPPER FORWARD ENGINE MOUNT BULKHEAD CHORD NAC STA 128.95 HAS A DEEP GOUGE ON INBOARD SIDE JUST AFT OF CHORD B END RADIUS AT NOSE COWL FORWARD FAIRING LATCH FITTING. 2 L 7 4 4F RT A20WE 2008010900377 20080109 00377 EA 2008 1 9 TRAX200800019 1 20080102 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION CL CLIMB 1 SO 27 884AS 7513 FLAPS FAIL - FLAPS 8 TO 0 DEGREES IN 8 DEGREE POSITION. COMPLIED W/ QRH LANDED KATL. A/C RETURNED TO ATL AFTER T/O. F IRE TRUCKS WERE ON STANDBY AS A PRECAUTION. FLT 4688 DEL 41 MINS - NC FLTS 4688, 4288 CX. 2 L 7 2 4F RT A21EA 2008010900380 20080109 00380 NM 2008 1 9 KCSA081000 1 20080104 A 5320 STIFFENER BOEING 747 747209B 138489B NM NLG WW CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 MAIN CABIN TOP OF NOSE WHEEL WELL STIFFENER BETWEEN STA 280 TO 300, LBL 10 IS CRACKED IN RADIUS 1 INCH LONG. 2 L 7 4 4F RT A20WE 2008010900385 20080109 00385 NM 2008 1 9 KCSA081001 1 20080104 A 5320 STIFFENER BOEING 747 747209B 138489B NM NLG WW CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 NOSE WHEEL WELL TUNNEL STA 260 TO 280, WL 150 HORIZONTAL STIFFENER IS CRACKED IN RADIUS IN 2 AREAS BOTH .5 INCHES LONG. 2 L 7 4 4F RT A20WE 2008010900386 20080109 00386 NM 2008 1 9 KCSA081002 1 20080104 A 5320 FLOOR SUPPORT BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 MAIN DECK FLOOR SUPPORT IS CRACKED .5 INCH ON OUTBOARD FLANGE AT STA 1480 RBL 77. 2 L 7 4 4F RT A20WE 2008011000015 20080110 00015 NM 2008 1 10 SWAA080004 1 20080101 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 275WN 36153 EEPLS LENS LOOSE AT ROW 7 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008011000020 20080110 00020 NM 2008 1 10 SWAA080049 1 20080101 A 5330 6545767 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 410 AND BS 448, ST R 28R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011000022 20080110 00022 NM 2008 1 10 SWAA080048 1 20080101 A 5322 6546569 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 887, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008011000036 20080110 00036 NM 2008 1 10 SWAA080042 1 20080101 A 5322 6546569 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008011000038 20080110 00038 NM 2008 1 10 SWAA080037 1 20080101 A 5330 6545767 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011000042 20080110 00042 NM 2008 1 10 SWAA080052 1 20080101 A 3211 656174011 BUSHING BOEING 737 7373T5 1384608 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 696SW 23064 DURING SCHEDULED C2 CHECK, FOUND RT MLG STRUT FWD TRUNNION LINK LUG HAT BUSHINGS CORRODED. REMOVED AND REPLACED MLG OUT ER CYLINDER AND COLLAR PER MT. 2 L 7 2 4F RT A16WE 2008011000048 20080110 00048 2008 1 10 SWAA080023 4 20080101 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 758SW 27873 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008011000056 20080110 00056 CE 2008 1 10 DXTA200802740 1 20080101 A 3150 CONTROL UNIT BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 125QS RK433 RED HSTAB FAIL WARNING LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. REPLACED 170 AND 180 KNOT AIRSPEED SWITCHES WITH NEW IA W HAWKER 400XP WIRING MANUAL CH 30-12-01. REPLACED OAT BIAS BOX WITH NEW IAW HAWKER 400XP MM CH 32-12-00. H-STAB DEICE S YSTEM OPS CHECK GOOD. LT AND RT PITOT/STATIC SYSTEMS LEAK CHECK GOOD IAW FAR 91.411. 2 H 7 2 4F 4 F RT A16SW E25EA 2008010900258 20080109 00258 NM 2008 1 9 SWAA080005 1 20080101 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008010900259 20080109 00259 NM 2008 1 9 SWAA080006 1 20080101 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008010900261 20080109 00261 NM 2008 1 9 SWAA080010 1 20080101 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008010900263 20080109 00263 2008 1 9 SWAA080024 4 20080101 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED THRU CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008012200040 20080122 00040 NM 2008 1 22 USAA920080136 1 20080101 A 5347 SEAT TRACK BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON SEAT TRACK, BS 1320 - BS 1340, BL 26, WL 208. REPAIRED SEAT TRACK, BS 1320 - BS 1340, BL 26, WL 208 IAW B757 SRM 53-00-052-2R. 2 L 7 2 4F RT A2NM 2008012200049 20080122 00049 NM 2008 1 22 USAA920080138 1 20080103 A 5330 6552988 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 460UW 25024 CLT - MAJOR REPAIR - C5 CHECK, CRACKED FUSELAGE SKIN, BS 940, S24L. REPAIRED FUSELAGE SKIN, BS 940, S24L IAW USAIRWAYS EA 100131. 2 L 7 2 4F RT A16WE 2008012200052 20080122 00052 EU 2008 1 22 USAA920080139 1 20080102 A 5320 D5347112420100 SHEAR PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 669AW 1792 PIT - MAJOR REPAIR - BC4 CHECK, CORROSION ON SHEAR PLATE, BS 3310 / FR 69 - BD 3366 / FR 70, -Y1732. REPLACED SHEAR PLA TE, BS 3310 / FR 69 - BD 3366 / FR 70, -Y1732 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008012200070 20080122 00070 CE 2008 1 22 DXTA200802772 1 20080116 A 3260 SQUAT SWITCH CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG INOPERATIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 319QS 5600519 IMMEDIATELY AFTER T/O GEAR HANDLE WOULD NOT RELEASE TO RETRACT GEAR. FOUND LEFT SQUAT SWITCH OUT OF ADJUSTMENT. ADJUST ED LT SQUAT SWITCH. SYSTEM OPERATION CHECKS GOOD. WORK PERFORMED IAW CH. 32-61-00 OF THE 560 CES. M.M. 2 L 7 2 4F 4 F RT A22CE E25EA 2008012200076 20080122 00076 EA 2008 1 22 TRAX200800043 1 20080103 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 904EV 7628 REAR PRESSURE BULKHEAD LEFT AND RIGHT STIFFENER CLIPS ARE CRACKED. 2 L 7 2 4F RT A21EA 2008012200081 20080122 00081 NM 2008 1 22 DXTA200802766 1 20080113 A 3260 C242450062 UPLOCK SWITCH AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE NLG MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 213QS 6749 113 GEAR SELECTED UP, GEAR RETRACTED NORMALLY, 3 RED DOOR LIGHTS REMAINED ON WITH RED GEAR UNSAFE LIGHT FLASKING. FOUND NL G UPLOCK WITH BROKEN INTERNAL SPRING. R & R NLG UPLOCK WITH MODIFIED UNIT. LEAK, OPS, AND ADJUSTMENT TEST GOOD I/A/W F ALCON 2000 MM 32-300, 32-214, 32-302, 32-200. 2 L 7 2 4F 4 F RT A50NM E44NE 2008011700011 20080117 00011 CE 2008 1 17 DXTA200702734 1 20080101 A 2150 73838433 ACM CESSNA 750 750 2076810 CE AFT SERVICE BAY FROZEN E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 984QS 5791 5791 7500084 COULD NOT CONTROL CABIN TEMP -THEN RAN ABNORMAL PROCEDURES. AFFECTED PAC WAS TURNED OFF. ONCE PARKED AT FBO CABIN FILLED WITH SMOKE. KHPN-KFLL.REMOVED DEFECTIVE CABIN PAC. INSTALLED REPAIRED UNIT. ALSO REPLACED BOTH CABIN & COCKPIT COALESCE R P/N 746451-3 OPS CK OF ECU'S GOOD. WORK DONE I/A/W CESSNA CITATION X M/M CHAPTER 21-51-00. 2 L 7 2 4J RT T00007WI 2008011700012 20080117 00012 CE 2008 1 17 DXTA200702735 1 20080101 A 2750 CONTROLLER CESSNA 750 750 2076810 CE TE FLAPS MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 933QS 7500133 AFTER TAKEOFF, FLAP FAIL CAS MESSAGE DISPLAYED WITH THE FLAPS AT 0*. FOUND BITS 2 TRIPPED ON FLAP CONTROLLER. RESET FLA P FAIL BUTTON ON SECOND ATTEMPT. THE FLAPS FULLY RETRACTED EXTENDED FLAPS TO 35* POSITION. INSPECTED FLAP TRACKS AND FOU ND ICE WAS KEEPING FLAPS FROM RETRACTING TO ZERO. LET ICE MELT FROM FLAP TRACKS AND WELLS. RESET BITE ON CONTROLLER, CYC LED FLAPS NUMEROUS TIMES. FLAPS OPS CHECK NORMAL IAW CESSNA 750 MM 27-50-00. 2 L 7 2 4J RT T00007WI 2008011700025 20080117 00025 NM 2008 1 17 08FDEA00031 1 20080104 A 5753 ARC2740 SKIN DOUG MD11 MD11 3023602 NM ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 RIGHT WING - INBOARD FLAP UPPER SURFACE FOUND DENT AT XIFH 193. REPAIR CARRIED OUT AT RIGHT HAND WING INBOARD FLAP UPPER SURFACE AT XIFH 193 AS PER SRM 57-10-00 FIGURE 38 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008011700026 20080117 00026 EU 2008 1 17 F3LA200800002 1 20080107 A 5210 FE240004 DAMPER AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE ZONE 800 INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 809FR 31 3092 WHILE PERFORMING HEAVY SERVICE CHECK, MECHANIC FOUND R-1 DOOR DAMPENING CYLINDER TO HAVE ZERO (0) PRESSURE. THE DOOR DA MPENING CYLINDER WAS REMOVED, REPLACED, INSPECTED (RII) AND OPERATIONS CHECKED OKAY IAW AMM 52-11-14 P 401 AND AMM 25-23 -46-000-01. 2 L 7 2 4F 4 F RT 2008011800011 20080118 00011 NM 2008 1 18 UIEA200800011 1 20080110 A 5730 PANEL BOEING 747 7472D7B 1384803 NM ZONE 500 DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 LT WING UPPER FIXED L/E PANEL HAS AREA OF DELAMINATION, 4.0 INCH WIDE BY 45.0 INCH LONG. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18 SHEET 3 AND 5, PREPREG 250 DEGREE CURE PER SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A409. 2 L 7 4 4F RT A20WE 2008011800027 20080118 00027 NM 2008 1 18 NWAA080096316 1 20080110 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 676NW 33002 DURING OVERNIGHT CHECK, FOUND ZONE E RIGHT SIDE PATH AND EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPL Y. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008011800126 20080118 00126 2008 1 18 HALA0800019 4 20080116 A 2370 1301273106 AUDIO VIDEO UNIT BOEING 767 76733A 1385209 NM SEAT 42C ODOR A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 589HA 33422 BURNING PLASTIC AND ELECTRICAL ODOR EMITTING FROM SEAT 42C. ODOR COMING FROM SEAT 41C REPLACED AVU AT 41C. VERIFIED ODO R NOT COMING FROM OVERHEAD OR OTHER SEATS. ALL CHECKS GOOD. 2 L 7 2 4F RT A1NM 2008012200009 20080122 00009 EA 2008 1 22 TRAX200800028 1 20080103 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 723EV 10132 CEILING LEVEL EMERGENCY LIGHT AT ROW 10 FAILED. FLT 4413 DEL 33 MINS. CABIN EMERGENCY LIGHTS, CEILING LEVEL FLOODLIGHT S. 2 L 7 2 4F RT A21EA 2008012200027 20080122 00027 SO 2008 1 22 XGN2008F00002 2 20080107 A 8530 TISN712ACA CYLINDER HEAD BEECH 36 36BEECH 1151602 CE CONT O520 IO520BA 17032 SO ENGINE CRACKED E XGNA K NONE O OTHER IN INSP/MAINT 1 SW 05 1194A 296 E159 ENGINE CYLINDER HEAD CRACKED. (K) 1 L 7 1 3O 3 O 3A15 E5CE 2008012200083 20080122 00083 CE 2008 1 22 DXTA200802767 1 20080113 A 3260 INDICATION SYS CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LT MLG MALFUNCTIONED E DXTA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 07 964QS 7500164 LT MAIN GEAR DOWN AND LOCK LIGHTS WILL NOT ILLUMINATE. LANDING GEAR WAS BLOWN DOWN. INSPECTED LANDING GEAR SYSTEM. NOT ED LEFT MAIN INDICATOR LIGHT ASSEMBLY UNSEATED. REMOVED INSPECTED AND NO DISCREPANCY NOTED. RESEATED LEFT MAIN INDICATOR LIGHT ASSY. OPS CHECK GOOD. RESET BLOW DOWN BOTTLE AND LANDING GEAR MANIFOLD. BLED GEAR SYSTEM. LANDING GEAR FUNCTIONAL TEST GOOD. WORK DONE IAW 750 MM CH 32-00-01 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008012200104 20080122 00104 EA 2008 1 22 TRAX200800054 1 20080106 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 904EV 7628 FS 319 FRAME IS CORRODED AT BL 0. 2 L 7 2 4F RT A21EA 2008012200109 20080122 00109 SO 2008 1 22 GLBA20061042 1 20080110 A 3610 BLEED AIR SYS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE CONTAMINATED A GLBA O OTHER C B F.O.D. SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 71GL 120071 SMOKE/SMELL, PILOTS REPORTED STRONG ODOR OF SMOKE IN CABIN FOLLOWED BY SMOKE AURAL WARNING FROM LAV SMOKE DETECTOR. MAIN TENANCE CLEANED BLEED DUCT AND BELLY PANEL OF GLYCOL FLUID. MAINTENANCE RAN ENGINES AND OPERATIONAL CHECKS WERE GOOD IAW MM 21-23. 2 L 7 2 4T 4 T RT A31SO E20NE 2008012200110 20080122 00110 EU 2008 1 22 TRAX200800033 1 20080104 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 RIGHT SEAT TRACK FOUND CORRODED BETWEEN FR 36-38. RIGHT SEAT TRACK CORROSION REMOVED BETWEEN FR 36-38 AS PER SRM 51-21- 42 & WITHIN LIMITS AS PER SRM 53-00-00 FIG 304. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AN D FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH 53-00-00 FIG 304 SRM MATERIAL THICKNESS: 0.090 MATERIAL RE MOVED: 0.003 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 304. SUPPLEMENTAL SDR CLOSED 1/10/08. 2 H 7 2 4T RT 2008012200115 20080122 00115 EU 2008 1 22 TRAX200800035 1 20080104 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 CORROSION FOUND ON LEFT SEAT TRACK BETWEEN FR 39 TO FR 41. CORROSION ON LEFT SEAT TRACK BETWEEN FR 39 TO 41 REMOVED IAW SRM 51-21-42. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACC OMPLISHED IN ACCORDANCE WITH SRM 53-00-00 FIG 304. MATERIAL THICKNESS: 0.090, MATERIAL REMOVED: 0.004 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 304. SUPPLEMENTAL SDR CLOSED 1/10/08. 2 H 7 2 4T RT 2008012200120 20080122 00120 EU 2008 1 22 TRAX200800042 1 20080104 A 5720 ANGLE AEROSP ATR72 ATR72 EU RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 ON TOP OF RIGHT WING BOX AT FR 23D AND RIB 1 ANGLE OF INTERCOSTAL FOUND CRACKED. FABRICATION OF ANGLE OF INTERCOSTAL ON RIGHT WING BOX AT FR 23D RIB 1 COVERED ON W/C 2000-161. ANGLE OF INTERCOSTAL ON TOP OF RIGHT WING BOX FR 23D RIB 1 REP LACED AS PER SRM 51-25-01. SUPPLEMENTAL SDR CLOSED 1/10/08. 2 H 7 2 4T RT 2008012200133 20080122 00133 CE 2008 1 22 AMWA89415BC 1 20080104 A 2424 51538001A GCU BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE INOPERATIVE A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 162ZV 19024 UE162 BATTERY CHARGE ANNUNCIATOR ILLUMINATED 8 TIMES IN FLIGHT, AMMETER SHOWED DISCHARGE DURING ILLUMINATION (NEEDLE DOWN ON A MMETER). MAINTENANCE PARALLELED GENERATOR CONTROL UNITS AND CLEARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2008012200165 20080122 00165 SO 2008 1 22 XGN2008F00001 2 20080107 A 8530 TISN712ACA CYLINDER HEAD BEECH 36 36BEECH 1151602 CE CONT O520 IO520BA 17032 SO ENGINE CRACKED E XGNA K NONE O OTHER IN INSP/MAINT 1 SW 05 1194A 993 E159 807201R ENGINE CYLINDER HEAD CRACKED. (K) 1 L 7 1 3O 3 O 3A15 E5CE 2008012200169 20080122 00169 NM 2008 1 22 CALS097001 1 20080118 A 5320 SHIELD BOEING 747 747409 13848AU NM CONT O520 IO520* 17032 SO CRACKED W SAJF K NONE O OTHER IN INSP/MAINT 1 WP 03 18275 24312 CHI FOUND A CRACKED DRIPSHIELD UNDER G1 FLOOR DURING AIRCRAFT B-18275 HEAVY MAINTENANCE OF 3D CHECK. THIS DRIPSHIELD HAD A 3 INCH DIAMETER HOLE WITH NUMEROUS CRACKS LOCATED IN AN AREA APPROXIMATELY 18 INCHES BY 8 INCHES. THE DRIPSHIELD IS I NTENDED TO PROTECT ELECTRONIC EQUIPMENT IN E1/E2 SHELVES FROM WATER. THE DRIPSHIELD ARE SHOWN IN THE 744 IPC SECTION (AL SO CALLED MOISTURE SHROUDS AND GUTTER ASSEMBLIES). 2 L 7 4 4F 3 O RT A20WE E5CE 2008012200177 20080122 00177 EU 2008 1 22 F3LA200800005 1 20080107 A 5320 D5347112420100 SHEAR PLATE AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FRAME CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 15198 5495 2051 DURING C-CHECK INSPECTION, AFT SHEAR PLATE ON THE RT, AFT SIDE OF FRAME 69 HAD CORROSION AT THE NUT PLATE CLIP HOLES. M AINTENANCE REPLACED THE SHEAR PLATE IAW THE REQUIREMENTS OF SRM 51-72-11, PARAGRAPH 6 AND SRM 51-42-11, PAGES 6 AND 7. FOLLOWING COMPLETION OF THE MAINTENANCE ACTION, THE REPLACEMENT WAS INSPECTED AND FOUND ACCEPTABLE. REFERENCE NON-ROUTI NE C035788. 2 L 7 2 4F 4 F RT 2008012200181 20080122 00181 EA 2008 1 22 TRAX200800061 1 20080108 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 317CA 10055 PAX DOOR OUTER HANDLE CRACKED. REMOVED OUTER HANDLE AND INSTALLED NEW HANDLE PER AMM 52-11-03. 2 L 7 2 4F RT A21EA 2008012200184 20080122 00184 EA 2008 1 22 TRAX200800062 1 20080108 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 317CA 10055 PAX DOOR "EXIT" PLACARD WORN. REPLACED PLACARD PER 11-30-00. 2 L 7 2 4F RT A21EA 2008012200185 20080122 00185 SO 2008 1 22 UG8A08P010901 1 20080109 A 5540 1159SCB2031 BEARING GULSTM GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE TORQUE TUBE CORRODED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 661GA 561 RUDDER TORQUE TUBE BEARING CORRODED AND SEAL LOOSE. 2 L 7 2 4F 4 F RT A12EA E00057EN 2008012200188 20080122 00188 SO 2008 1 22 UG8A08P011003 1 20080110 A 5230 1159B5144329 FRAME GULSTM GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE CARGO DOOR CRACKED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 661GA 561 561 BAGGAGE DOOR FRAME IS CRACKED. 2 L 7 2 4F 4 F RT A12EA E00057EN 2008012200200 20080122 00200 SO 2008 1 22 RAIA00801007 1 20080108 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN ODOR A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 814HK 145046 FLT NR 5599-STL-FLIGHT ATTENDANT REPORTED A STRONG ODOR OF SMOKE IN THE FORWARD CABIN. MAINTENANCE RAN BOTH ENGINES BLEE D AIR SYSTEMS AND PACKS. IN ADDITION THE CABIN AND GALLEY AREAS WERE INSPECTED. NO DEFECTS COULD BE FOUND AND NO FURTHER ODORS NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008010900265 20080109 00265 NM 2008 1 9 SWAA080015 1 20080101 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 431WN 29845 EEPLS LENS LOOSE AT ROW 3 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008010900266 20080109 00266 NM 2008 1 9 SWAA080016 1 20080101 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 480WN 33998 DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008010900268 20080109 00268 NM 2008 1 9 SWAA080041 1 20080101 A 5315 65C339504 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 30 TO LBL 47. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2008010900271 20080109 00271 NM 2008 1 9 SWAA080034 1 20080101 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008010900272 20080109 00272 NM 2008 1 9 SWAA080017 1 20080101 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008010900273 20080109 00273 NM 2008 1 9 SWAA080036 1 20080101 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008011000008 20080110 00008 NM 2008 1 10 UPS08651361 1 20080101 A 3350 COVER BOEING 767 76734AF 1385212 NM COCKPIT OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 308UP 27761 INSPECTION TYPE:N/A FLIGHT DECK EMERGENCY EXIT LIGHT COVER FELL OFF. REMOVED AND REPLACED LIGHT ASSEMBLY. OPS CHECK GO OD. 2 L 7 2 4F RT A1NM 2008011000017 20080110 00017 NM 2008 1 10 SWAA080007 1 20080101 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008011000043 20080110 00043 NM 2008 1 10 SWAA080051 1 20080101 A 3211 65633788 BUSHING BOEING 737 7373T5 1384608 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 696SW 23064 DURING SCHEDULED C2 CHECK, FOUND RT MLG TRUNNION LINK HAT BUSHINGS CORRODED. REMOVED AND REPLACED TRUNNION LINK PER MT. 2 L 7 2 4F RT A16WE 2008011000084 20080110 00084 2008 1 10 ASAA0852449 4 20080102 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 577AS 35186 FMC DISAGREE FAULT MESSAGE ON CAPT'S & F/O'S DISPLAYS. RESET NR 1 & NR 2 FMC'S CIRCUIT BREAKERS. FMC'S CHECK OK (REF F IM34 61 TASK 835). 2 L 7 2 4F RT A16WE 2008011000085 20080110 00085 NM 2008 1 10 ASAA0852450 1 20080102 A 5210 90787910 HANDLE BOEING 737 737890 1384527 NM R1 DOOR ICED A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 553AS 34594 R1 DOOR EXTERIOR HANDLE WILL NOT ENGAGE TO OPEN DOOR. R1 DOOR CANNOT BE OPENED FROM THE OUTSIDE. APPLIED HEAT TO R1 DO OR. POSSIBLE ICING. PERFORMED OPERATIONAL CHECK OF DOOR, AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A16WE 2008011000088 20080110 00088 NM 2008 1 10 SWAA080077 1 20080102 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 540, STR 10L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2008011000095 20080110 00095 NM 2008 1 10 SWAA080071 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011000099 20080110 00099 NM 2008 1 10 SWAA080076 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011000107 20080110 00107 NM 2008 1 10 SWAA080084 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011000146 20080110 00146 NM 2008 1 10 USAA920080122 1 20080102 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 453UW 24980 PIT - MAJOR REPAIR - FPBH INSPECTION, CRACKED BULKHEAD, BS 178, BL 5.7, WL 213. REPAIRED BULKHEAD, BS 178, BL 5.7, WL 2 13 IAW B737 SRM 53-10-08 AND EO 53000153. 2 L 7 2 4F RT A16WE 2008012200201 20080122 00201 SO 2008 1 22 RAIA00801008 1 20080108 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHTS LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 829HK 145281 PRE FLT NR 5527-STL-EMERGENCY LIGHT AT MID CABIN LOCATION INOPERATIVE. MAINTENANCE RESECURED THE FIXTURE CONNECTION. SYS TEM OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008012200206 20080122 00206 NM 2008 1 22 08FDEA00124 1 20080114 A 5730 112N61011 PANEL BOEING BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 RIGHT WING FUEL TANK PANEL 641FB HAS CORROSION ON THE LOWER SURFACE. REMOVED CORROSION ON PANEL 641FB PER SRM 57-20-01. FOUND TO BE OUT OF LIMITS PER SRM 57-20-01, FIG 201, DETAIL I SECTION AA, NOTE B. CORROSION WITHIN 0.10" OF SEAL. RE PLACED PANEL 641FB IAW AMM 28-11-01. 2 L 7 2 4F RT A2NM 2008012200207 20080122 00207 NM 2008 1 22 08FDEA00109 1 20080111 A 5315 BAC15123345 FLOORBEAM BOEING 757 757200 1384950 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 CORROSION AROUND SCREW HOLE ON STA 365, RBL3, RBL7, RBL11, RB15, RBL19, RBL23, RBL27, RBL31, RBL35, RBL39, RBL43, RBL4 7, RBL51. CORROSION FOUND EXCEED SRM LIMITS. FLOORBEAM REPAIR CARRIED OUT IAW SRM 53-00-51 REV. 93, FIG. 201, REPAIR 1. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008012200208 20080122 00208 EU 2008 1 22 08FDEA00110 1 20080111 A 5311 A5387006820000 FRAME AIRBUS 310 A310203 3930313 EU FUSLEAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 HOLE NR 5 FRAME 44 RT HAS CRACK INDICATION IN FRAME FOOT REAMED HOLE NR 5 LT TO .316 IAW FEDEX EA 6-5310-113006. COLD W ORKED HOLE IAW A310- 200 SRM 51-40-41 AND FEDEX EA6-5310-113006. REAMED HOLE TO .323 IAW FEDEX EA 6-5310- 113006. IN STALLED BUSHING IAW FEDEX EA 6-5310-113006. REMOVED AND INSTALLED FOOT FITTING AND BRACKETS IAW A310-200 SRM 51-40-21 P ARA 7 AND FEDEX EA 6-5310-113006. 2 L 7 2 4F RT A35EU 2008012200231 20080122 00231 NM 2008 1 22 KCSA081009 1 20080111 A 5210 HINGE BOEING 747 747209B 138489B NM L5 DOOR CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 L-5 DOOR JUST BELOW UPPER HINGE HAS SKIN PILLOWING AROUND FASTENERS. 2 L 7 4 4F RT A20WE 2008011800023 20080118 00023 SO 2008 1 18 SIMA200701405 1 20080112 A 3350 20131A110049 CHARGER EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 737MW 145396 ON FLIGHT 4806 - EMERGENCY FLOOR LIGHT FLOOR STRIP INOPERATIVE BY ROWS 7, 3, 4, 5. AIRCRAFT REMOVED FROM SERVICE. REMO VED AND REPLACED EMERGENCY BATTERY AND CHARGER NUMBER 2 IAW EMB AMM 33-50-04. EMERGENCY FLOOR STRIP LIGHTS OPERATIONAL CHECK GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE BATTERY. 2 L 7 2 4F RT T00011AT 2008011800072 20080118 00072 EA 2008 1 18 SWIA200819048 1 20080109 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG LOW A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 925SW 7682 FLT 1001 - RECEIVED "GEAR DISAGREE" WARNING MESSAGE AFTER TAKEOFF. SERVICED NOSE GEAR SHOCK STRUT WITH OIL AND NITROGEN IAW MM 12-12-32. 2 L 7 2 4F RT A21EA 2008011800113 20080118 00113 NM 2008 1 18 UIEA200800013 1 20080110 A 5753 SKIN BOEING 747 74747UF 1384812 NM RT WING TE FLAP DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 497MC 29258 RT TE MID FLAP UPPER SURFACE HAS DENT APPROX 1.0 INCHES IN DIAMETER LOCATED 28 INCHES FORWARD OF THE TRAILING EDGE AND 2 9 INCHES OUTBOARD OF THE CONTACT FACE OF THE ACCORDION SEAL. DENT BLENDED OUT FILLED OUT IN IAW SRM51-70-06 AND EO 4457 A116 2 L 7 4 4F RT A20WE 2008012200245 20080122 00245 NM 2008 1 22 AALA200800001 1 20080101 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 796AN 30796 MIA - EMERGENCY LIGHT AT SEAT 35G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 35G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008012200247 20080122 00247 NM 2008 1 22 KCSA081011 1 20080113 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 FWD PIT SEAT TRACK DAMAGED AT BS 560, RBL 48. 2 L 7 4 4F RT A20WE 2008012200262 20080122 00262 NM 2008 1 22 AALA200800007 1 20080101 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 797AN 30012 JFK - EMERGENCY LIGHT AT SEAT 22C MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008012200264 20080122 00264 NM 2008 1 22 AALA200800009 1 20080101 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 197AN 32391 MIA - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008012200273 20080122 00273 NM 2008 1 22 08FDEA00096 1 20080110 A 5412 311N50433 BULKHEAD BOEING 757 7572B7 1384964 NM NR 1PYLON DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 WHILE ACCOMPLISHING FX EO F-5450-7-5005 PT, THE NR 1 PYLON MID BULKHEAD FWD RT BOLT HOLE WAS REAMED PER STEP 3.C AND FI G. 9. TOLERANCE FOR MAX DIA SHOULD BE 0.3901- 0.3911". FINAL DIA AFTER REAMING IS 0.3925". HFEC INSPECTED MID BULKHEA D FWD RT BOLT HOLE PER NDT MANUAL PART 6 SECTION 51-00-00. REAMED HOLE AND INSTALLED BACB30YK12K8Y LOCK FASTENER AND VI SUALLY INSPECTED FOR PROPER INSTALLATION PER EA F-5450-110814 DATED 12/05/07. 2 L 7 2 4F RT A2NM 2008012200280 20080122 00280 NM 2008 1 22 08FDEA00125 1 20080114 A 5730 112N60081 PANEL BOEING 757 7572B7 1384964 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 RIGHT WING TANK ACCESS PANEL 641GB HAS SURFACE CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 641GB PER SRM 57-2 0-01. FOUND TO BE OUT OF LIMITS PER SRM 57-20-01, FIG 201, DETAIL I SECTION AA, NOTE B. CORROSION WITHIN 0.10" OF SEAL . REPLACED PANEL 641GB IAW AMM 28-11-01. 2 L 7 2 4F RT A2NM 2008012200281 20080122 00281 NM 2008 1 22 08FDEA00127 1 20080114 A 5730 112N60081 PANEL BOEING 757 757200 1384950 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 RT WING FUEL TANK ACCESS PANEL 641HB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 641HB PER SRM 57-20-01. FOUND TO BE OUT OF LIMITS PER SRM 57-20-01, FIG. 201, DETAIL I SECTION AA, NOTE B. CORROSION WITHIN 0.10" OF SEAL. REPLACED PANEL 641HB IAW AMM 28-11-01. 2 L 7 2 4F RT A2NM 2008012200290 20080122 00290 NM 2008 1 22 08FDEA00136 1 20080115 A 5311 BAC1570705 FRAME BOEING 727 727233 138408A NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 CABIN BS 560 FRAME INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT S11R INSTALLED DOUBLER IAW SRM 53-10-4 FIG 2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2008012200291 20080122 00291 NM 2008 1 22 08FDEA00137 1 20080115 A 5321 650489611 FLOOR PANEL BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 LAV FLOOR PANEL STA 303.6 -344 CORRODED IN NUMEROUS PLACES FABRICATED NEW FLOOR PANEL, PRIMED AND PAINTED REF AMM 51-20- 02, MM 51-20-31, 51-20-151. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008012200315 20080122 00315 WP 2008 1 22 UPS08851387 1 20080106 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK PER MM 33-50-01-2. CHECKS GOOD. 2 L 7 4 4F RT 4A25 2008012200316 20080122 00316 WP 2008 1 22 UPS08851390 1 20080108 A 2612 DETECTOR DOUG DC8 DC873F 302199F WP CARGO BAY MALFUNCTIONED A IPXA K NONE N FALSE WARNING NR NOT REPORTED 1 SO 01 803UP 46073 INSPECTION TYPE:N/A LIGHT ON THE LOWER CARGO FIRE MODULE ILLUMINATED. REPAIRED SDU AD1283 PER MM 26-18-01-5. SYSTEM OP S CHECKS NORMAL. 2 L 7 4 4F RT 4A25 2008012200326 20080122 00326 SO 2008 1 22 C2XA08RI014 1 20080108 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14959 145091 RIC - DURING ROUTINE MAINTENANCE, MX FOUND AFT EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED LIGHT BULB IAW EMB1 45 AMM 33-50-08 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008012200327 20080122 00327 SO 2008 1 22 C2XA08IA018 1 20080108 A 3260 M835366022M RELAY EMB 145 EMB145XR 3260214 SO COCKPIT INOPERATIVE A C2XA O OTHER N FALSE WARNING LD LANDING 1 SW 27 14105 145649 IAH - FLIGHT 2555, THE CREW REPORTED BRAKE INBOARD INOP ON EICAS DURING LANDING. THE AIRCRAFT LANDED AT IAH WITHOUT INC IDENT WHERE MAINTENANCE REMOVED AND REPLACED WOW RELAY K0200 IAW EMB 145 AMM 32-63-00, OPS CHECK GOOD. TEST FLEW SATISF ACTORILY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008012200331 20080122 00331 EU 2008 1 22 TRAX200800032 1 20080104 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 RIGHT SEAT TRACK FOUND CORRODED BETWEEN FR 39 TO FR 41. RIGHT SEAT TRACK CORROSION REMOVED BETWEEN FR 39 TO FR 41 AS PE R SRM 51-21-42 & WITHIN LIMIT AS PER SRM 53-00-00 FIG 304. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WIT H SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 53-00-00 FIG 304, MATERIAL THICKNESS: 0.090 , MATERIAL REMOVED: 0.004 WITHIN LIMITS AS PER SRM 53-00-00 FIG 304. SUPPLEMENTAL SDR CLOSED 1/10/08. 2 H 7 2 4T RT 2008012200335 20080122 00335 2008 1 22 ZZDA2008008 4 20080110 A 2565 D29981225 SLIDE BOEING 717 717200 1383700 NM R1 DOOR UNSERVICEABLE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 997AT 55141 R-1 DOOR SLIDE PRESSURE NOT IN GREEN BAND. REMOVED AND REPLACED R-1 DOOR SLIDE IN REF TO ATM 25-61-03. 2 L 7 2 4F TR A6WE 2008012200341 20080122 00341 NM 2008 1 22 08FDEA00148 1 20080115 A 5320 25FX1253119 SUPPORT ANGLE BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 MAIN DECK CEILING PNL SUPPORT ANGLE IS BUCKLED/CRACKED, BS 640, LBL 14. REPLACED SUPPORT ANGLE AT BS 640, LBL 14 REF S RM 51-30-2 PG 7. FABRICATED NEW SUPPORT REF SRM 25FX1253. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008012200343 20080122 00343 NM 2008 1 22 KCSA081016 1 20080115 A 5210 DOOR FRAME BOEING 747 747209B 138489B NM PAX DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 MAIN ENTRY DOOR NR 4R FWD FRAME WEB CRACKED AT UPPER O/B FLANGE. 2 L 7 4 4F RT A20WE 2008012200344 20080122 00344 NM 2008 1 22 08FDEA00149 1 20080115 A 5320 69477072 SUPPORT BRACKET BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 AIR CONDITIONING DISTRIBUTION BAG DUCT SUPPORT BRACKET IS CRACKED AT BOLT HOLES (3) STATION 740, LBL 5. REMOVED CRACKED BRACKET, FABRICATED NEW BRACKET AND INSTALLED. REFERENCE SRM 51-30-2 AND BOEING DOCUMENT NR 65-47707/ ITEM NR 2. CLA SSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008012200347 20080122 00347 NM 2008 1 22 DL738080005 1 20080104 A 5330 143A323212 SKIN BOEING 737 737832 13844CF NM BS 483 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3734B 30776 A SKIN DENT BELOW THE FWD CARGO DOOR AT FS 483 REQUIRED TRIM OUT. THE SRM 53-00-01 REPAIR 21 DOUBLERS APPLIED TO THIS C UTOUT, BUT INTERFERED WITH AN EXISTING 090750-14. REPAIR DOUBLER AT STR-22R/23R. THE SRM REPAIR WAS EXTENDED UP TO ENC OMPASS THE 090750-14 REPAIR. 2 L 7 2 4F RT A16WE 2008012200348 20080122 00348 NM 2008 1 22 DL757080006 1 20080104 A 5320 146N852249 SILL BOEING 757 757232 1384965 NM FS 1440 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 606DL 22813 FUSELAGE/C2 DOOR OPENING/LOWER SILL BEAM/INNER CAP, CRACKED FLANGE REPAIR. THE INNER CHORD OF THE LOWER SILL BEAM AT TH E C2 DOOR OPENING WAS DAMAGED BY CARGO LOADING EQUIPMENT RESULTING IN A ONE FOOT TEAR IN THE OUTER FLANGE OF THE CHORD. THE REPAIR CONSISTS OF REMOVING AND REPLACING OF THE DAMAGED PART PER BAC DRAWINGS AND ER/A 465925-14. 2 L 7 2 4F RT A2NM 2008012200350 20080122 00350 EU 2008 1 22 TRAX200800070 1 20080104 A 5260 PANEL AEROSP ATR72 ATR72 EU PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 PAX DOOR STAIRCASE, VERTICAL PANEL NR 1 FROM TOP, CORRODED UNDER LIGHT DOUBLER. 2 H 7 2 4T RT 2008012200352 20080122 00352 EA 2008 1 22 TRAX200800072 1 20080111 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA CABIN UNSECURE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 723EV 10132 F/A REPORTS MAIN DOOR-EXIT PLACARD AND OPEN SIGN UNSECURED. 2 L 7 2 4F RT A21EA 2008012200373 20080122 00373 NM 2008 1 22 KCSA081017 1 20080115 A 5210 DOOR BOEING 747 747209B 138489B NM L5 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 L-5 DOOR FWD LWR CORNER AROUND DOME NUTS HAVE CORROSION. 2 L 7 4 4F RT A20WE 2008011000094 20080110 00094 NM 2008 1 10 SWAA080070 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011000101 20080110 00101 NM 2008 1 10 SWAA080058 1 20080102 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 417WN 29822 EEPLS END CAP LOOSE AT ROW 1 ABC. SECURED END CAP PER MM. 2 L 7 2 4F RT A16WE 2008011000217 20080110 00217 EU 2008 1 10 2008UALA0001 1 20080101 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 407UA 456 RIGHT OVERWING EMERGENCY BATTERY FAILS TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011100033 20080111 00033 NM 2008 1 11 2008UALA0011 1 20080101 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 SEAT ROW 15 FWD & SEAT 40ABC EMERGENCY LIGHTS ARE INOPERATIVE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011100043 20080111 00043 NM 2008 1 11 2008UALA0017 1 20080101 A 2560 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FLASHLIGHT WEAK A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 F/A REPORTED DOOR 3L EMERGENCY FLASHLIGHT BATTERY WEAK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011100045 20080111 00045 NM 2008 1 11 2008UALA0018 1 20080101 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 THE EMERGENCY LIGHTS ON THE LEFT SIDE OF AIRCRAFT ARE ON. LIGHTS OVER THE DOORS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008011100066 20080111 00066 NM 2008 1 11 2008UALA0026 1 20080102 A 2425 WARNING LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ELECTRICAL SYS ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 508UA 24744 RTFL DUE TO GENERATOR DRIVE LIGHT ILLUM. 2 L 7 2 4F 4 F RT A2NM E17NE 2008011100075 20080111 00075 2008 1 11 2008UALA0029 4 20080101 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 408UA 457 CREW REPORT: SLIDE PACK 2R HAS FALLEN OFF. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011100087 20080111 00087 2008 1 11 ASAA0852453 4 20080103 A 2210 4082499903 AUTOLAND SYS BOEING 737 737890 1384527 NM COCKPIT MALFUNCTIONED A ASAA K NONE O OTHER LD LANDING 1 NM 02 577AS 35186 DURING AUTO LAND EVALUATION THE RIGHT MAIN LANDING GEAR TOUCHED DOWN TO THE LEFT OF THE RUNWAY CENTERLINE. EVALUATION U NSATISFACTORY. PERFORMED FIM 22 11 TASK 825. NO FAULTS LOGGED ON EITHER FCC. PERFORMED LAND VERIFY TEST PER FIM 22 11 00 TASKS 700 801 WITH NO FAULTS. PERFORMED HGS SYSTEM TEST (REF MM SUPP 34 36 00) WITH NO FAULTS. 2 L 7 2 4F RT A16WE 2008011100090 20080111 00090 EA 2008 1 11 TRAX200800024 1 20080102 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 846AS 7328 ASD BOTTOM STEP BROKEN. 2 L 7 2 4F RT A21EA 2008011100092 20080111 00092 EA 2008 1 11 TRAX200800025 1 20080102 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 852AS 7369 AFT MOST CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008011100096 20080111 00096 NM 2008 1 11 SWAA080113 1 20080103 A 5315 6545834 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 294, LBL 7. REPAIRED UPPER CHORD PER SRM. 2 L 7 2 4F RT A16WE 2008011100097 20080111 00097 NM 2008 1 11 SWAA080112 1 20080103 A 5315 6546816 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND TEE CHORD CORRODED AT BS 807, RBL 21. REMOVED AND REPLACED TEE CHORD PER SRM. 2 L 7 2 4F RT A16WE 2008011100110 20080111 00110 NM 2008 1 11 SWAA080101 1 20080103 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED C1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 6ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008011100120 20080111 00120 NM 2008 1 11 SWAA080107 1 20080103 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 629SW 27704 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008012300002 20080123 00002 WP 2008 1 23 08FDEA00155 1 20080115 A 5230 AFA71321 SUPPORT FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 UPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 1 IS CRACKED IN HOLE "C" BEYOND SRM LIMITS. REPLACED SUPPORT FITT ING NR 1 MAIN CARGO DOOR SPOOL LOCATION IAW SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2008012300028 20080123 00028 NM 2008 1 23 DL76L080010 1 20080105 A 2497 CONNECTOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE IDG LOOSE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 193DN 28450 724741 RIGHT GEN DRIVE LIGHT ILLUMINATED SHORTLY AFTER T/O. RETURNING TO JFK FOR REPAIRS. FOUND CONNECTOR LOOSE ON IDG, TIGHT EN SAME. RECONNECTED IDG. RAN R ENGINE AND LOADED RT IDG. OPS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012300030 20080123 00030 NM 2008 1 23 2008UALA00073 1 20080105 A 2750 S256W4028 MOTOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE TE FLAPS MALFUNCTIONED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 222UA 30553 FLAP-SLAT CONTROL 1 STATUS MESSAGE. SUSPECT ELECTRIC MOTOR. REPLACED ELECTRIC MOTOR. PERFORMED PRIMARY FLAP MAT TEST. TEST PASSED AND MSG CLEARED. IN ADDITION, PERFORMED SECONDARY FLAP TEST PASSED. RAN FLAPS IN ALT 3 TIMES NO FAULTS. ACF T OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008012300037 20080123 00037 SO 2008 1 23 SWIA200819060 1 20080107 A 2710 BRACKET EMB 120 EMB120ER 3260203 SO AILERON CONTROL BINDING A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 294SW 120321 ON APPROACH, AILERONS WERE VERY RESTRICTED IN THEIR MOVEMENT, FLIGHT NR 5446. REPLACED LEFT AILERON RVDT CONTROL ARM BR ACKET IAW SRM 51-10-02. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008012300038 20080123 00038 EA 2008 1 23 SWIA200819061 1 20080108 A 3250 PACKING CNDAIR CL600 CL6002B19 1900309 EA SELECTOR VALVE DAMAGED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 925SW 7682 RECEIVED "GEAR DISAGREE" WARNING MESSAGE AFTER TAKEOFF, FLIGHT NR 1001. REPLACED PACKING ON STEERING SELECTOR VALVE FIT TING IAW 32-51-25 CMM. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008012300054 20080123 00054 NM 2008 1 23 DL76L080015 1 20080108 A 5420 311T31571 ANGLE BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 191DN 28448 NR 2 PYLON MIDSPAR CLOSEOUT ANGLES WER CRACKED AT THE MIDSPAR FITTINGS. THE ANGLE WAS REPLACED. 2 L 7 2 4F RT A1NM 2008012300058 20080123 00058 NM 2008 1 23 DL757080024 1 20080109 A 5330 143N33206 SKIN BOEING 757 757232 1384965 NM BS 609 S15-19L PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 6707A 30395 FUSELAGE SKIN PUNCTURED BY JETWAY AT STA 609-619 BETWEEN STR 17L AND 18L. THE SKIN WAS ALSO FOUND DENTED AT STA 609 BET WEEN STR 15L AND 16L, STA 613 BETWEEN S16L AND 17L AND AT STA 609-619 AT STR 19L. ALL DAMAGE LOCATIONS WERE CUTOUT AND A SKIN REPAIR WAS INSTALLED. 2 L 7 2 4F RT A2NM 2008012300060 20080123 00060 EU 2008 1 23 08FDEA00111 1 20080111 A 5311 FRAME AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 HOLE NR 22 FRAME 45 LT HAS CRACK INDICATION IN FRAME, REAMED HOLE 22 FR 45L TO .376 IAW FEDEX EA 6-5310-113006 COLD WORK ED HOLE IAW FEDEX EA 6-5310-113006 AND A310-200 SRM 51-40-41. FINAL REAMED HOLE TO .401 IAW FEDEX EA 6-5310-113006. IN STALLED BUSHING IAW FEDEX EA 6-5310-113006. INSTALLED FASTENER NSA 5351-5-9 IAW FEDEX EA 6-5310-113006. ORIGINAL EA AT TACHED TO N/R N01419. ITEM 5A SHOULD READ FRAME AND ITEM 5C SHOULD READ A53870033200 FOR THE FRAME SECTION. 2 L 7 2 4F RT A35EU 2008012300085 20080123 00085 NM 2008 1 23 2008UALA00104 1 20080104 A 3397 CONNECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 339UA 24243 EEL FLOOR LIGHT STRIP INOP AT SEAT ROW 11. RESECURED CONNECTOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300087 20080123 00087 NM 2008 1 23 2008UALA00107 1 20080107 A 5297 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAV DOOR SHORTED A UALA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 WP 29 535UA 25130 FLIGHT DIVERTED DUE CABIN FIRE DETECTION FAULT. FOUND LAV DOOR SWITCH OVERHEAT CAUSED BY SUPPLY WIRES OVERHEATING DUE T O ELECTRICAL SHORT. FOUND PINCHED WIRES. REPLACED SWITCH AND REPAIRED LAV SWITCH WIRING. ALL OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300092 20080123 00092 NM 2008 1 23 2008UALA00112 1 20080106 A 3350 1317 LAMP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 DOOR 4 LEFT CEILING EMERGENCY LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012300095 20080123 00095 SO 2008 1 23 SWIA200819059 1 20080109 A 2197 CONNECTOR EMB 120 EMB120ER 3260203 SO TEMP SENSOR ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 565SW 120340 FLIGHT ATTENDANT NOTICED A BURNING ODOR COMING FROM THE VENTS AFTER TAKEOFF, FLIGHT NR5745. INSPECTED BOTH PACKS AND CL EANED CONNECTORS FOR RIGHT PACK DUCT TEMPERATURE SENSOR. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2008012300099 20080123 00099 NM 2008 1 23 2008UALA00114 1 20080105 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INTERMITTENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 DOOR 2L CLOSET EEL LIGHT INTERMITTENT. REPLACED EEL ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012300102 20080123 00102 NM 2008 1 23 DL76L080034 1 20080110 A 4920 380029817 APU BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE APU COMPARTMENT SHUTDOWN A DALA O OTHER O OTHER NR NOT REPORTED 1 SO 27 177DN 13815 25122 P2578 REPLACED APU DUE TO AUTO SHUT DOWN DUE TO LOW OIL PRESS AND WOULD NOT START AFTER SERVICING, SN OFF P2578, S/N ON P1078. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012300103 20080123 00103 NM 2008 1 23 2008UALA00116 1 20080106 A 3350 851307682073 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 532UA 25072 EMERGENCY LIGHT SWITCH INOPERATIVE AT L1 DOOR. FOUND DOOR 1L LIGHT SWITCH FAILED. REPLACED DOOR 1L EMERGENCY LIGHT SW ITCH. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008011100122 20080111 00122 NM 2008 1 11 SWAA080109 1 20080101 A 5322 6546546 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 747, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008011100124 20080111 00124 NM 2008 1 11 SWAA080111 1 20080103 A 5330 6545800 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008011100152 20080111 00152 2008 1 11 SWAA080118 4 20080106 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 230WN 34592 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008011000025 20080110 00025 NM 2008 1 10 SWAA080047 1 20080101 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2008011000040 20080110 00040 NM 2008 1 10 SWAA080035 1 20080101 A 5514 6549857 HINGE FITTING BOEING 737 7373G7 1384595 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND LT HORIZONTAL STABILIZER CENTER SECTION HINGE FITTING CORRODED AT BEARING FACE. REPA IRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008011000092 20080110 00092 NM 2008 1 10 SWAA080068 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011000102 20080110 00102 NM 2008 1 10 SWAA080059 1 20080102 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 431WN 29845 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008011000106 20080110 00106 NM 2008 1 10 SWAA080085 1 20080102 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011100155 20080111 00155 NM 2008 1 11 SWAA080120 1 20080104 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 277WN 32531 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008011100168 20080111 00168 NM 2008 1 11 SWAA080127 1 20080105 A 3234 A420060283 SOLENOID BOEING 737 7373H4 1384600 NM GEAR HANDLE FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 348SW 24375 DIVERSION/DECLARED EMERGENCY. DURING CLIMBOUT OF TUS LANDING GEAR HANDLE WOULD NOT MOVE FROM THE UP POSITION TO THE OFF POSITION. REMOVED AND REPLACED GEAR HANDLE SOLENOID PER MM. 2 L 7 2 4F RT A16WE 2008011100174 20080111 00174 NM 2008 1 11 SWAA080153 1 20080106 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011100176 20080111 00176 NM 2008 1 11 SWAA080132 1 20080106 A 5310 6516352 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT BS NR 5 DOOR STOP. REMOVED AND REPLACED FR AME PER SRM. 2 L 7 2 4F RT A16WE 2008011100186 20080111 00186 NM 2008 1 11 SWAA080142 1 20080106 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011100187 20080111 00187 NM 2008 1 11 SWAA080143 1 20080106 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008011100188 20080111 00188 NM 2008 1 11 SWAA080144 1 20080106 A 2560 6557463 FITTING BOEING 737 7375H4 138449D NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2008011100190 20080111 00190 NM 2008 1 11 SWAA080138 1 20080106 A 5310 6546817 CREASE BEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 360 TO BS 380, LBL 70. REMOVED AND REPLACED WEB PER SR M. 2 L 7 2 4F RT A16WE 2008012300115 20080123 00115 NM 2008 1 23 2008UALA00126 1 20080107 A 5712 RIB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 LT WING RIB BETWEEN WBL 135.5 AND WING STRINGERS S2 & S3 HAS APPROX 1 INCH CRACK ORIGINATING IN THE CUTOUT RADIUS OF THE RIB. REMOVED DAMAGE. FABRICATED AND INSTALLED TEE FITTING AND FILLERS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300120 20080123 00120 NM 2008 1 23 DLM90080044 1 20080102 A 5230 SKIN DOUG MD90 MD9030 3023690 NM AFT CARGO DOOR GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 AFT CARGO DOOR FWD LOWER INTERNAL SURFACE BELOW LATCH GOUGED. REPAIRED DOOR, IAW MD90 DRD 53-30-02 FIG 801D. 2 L 7 2 4F RT A6WE 2008012300122 20080123 00122 NM 2008 1 23 DLM90080045 1 20080111 A 2420 CONVERTER DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE LT AC POWER FAULTED A DALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 27 906DA 53386 020105 LT AC PWR FAULT. REMOVED AND REPLACED VSC CONVERTER PER AMM. OPS GOOD PART NO 1B189-5. 2 L 7 2 4F 4 F RT A6WE E40NE 2008012300127 20080123 00127 NM 2008 1 23 DLM88080049 1 20080112 A 2120 GASKET DOUG MD88 MD88 3023688 NM PNEUMATIC SYS BLOWN A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 930DL 49717 TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED IN FLIGHT. FOUND RT PNEU LOW TEMP SENSOR GASKET BLOWEN, REPLACED SAME. AL SO FOUND BLOWN SPIDER DUCT, REPLACED SAME. 2 L 7 2 4F RT A6WE 2008012300135 20080123 00135 NM 2008 1 23 2008UALA00136 1 20080107 A 5320 FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 BS 348 STR 16L INTERCOSTAL CLIP ANGLE & TIE CRACKED. REMOVED DAMAGED COMPONENTS. INSTALLED REPLACEMENT PARTS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300146 20080123 00146 2008 1 23 2008UALA00146 4 20080108 A 2565 101651303 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 647UA 25284 ASPIRATOR LEAKING. REPLACED ASPIRATOR, CKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012300147 20080123 00147 NM 2008 1 23 08FDEA00153 1 20080115 A 5320 25FX1253119 ANGLE BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 MAIN DECK CEILING PNL SUPPORT ANGLE IS BUCKLED/CRACKED, BS 600, LBL 14. REPLACED SUPPORT ANGLE AT BS 600, LBL 14, REF S RM 51-30-2 PG 7. FABRICATED NEW SUPPORT REF FED EX DWG 25FX1253. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008012300158 20080123 00158 NM 2008 1 23 2008UALA00151 1 20080108 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 FLOORBEAM UPPER CAP CORRODED AT BS 1640 BL 8L TO 57R WL 208. PERFORMED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300159 20080123 00159 2008 1 23 2008UALA00157 4 20080108 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR INCORRECT A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 307UA 23668 FORWARD GALLEY DOOR EMERGENCY SLIDE IS NOT PACKED CORRECTLY AT LOWER END OF CLAM SHELL. REPACKED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300165 20080123 00165 NM 2008 1 23 2008UALA00159 1 20080108 A 3350 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS WEAK A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 588UA 26717 EMERGENCY EEL STRIP LIGHT IS NOT WORKING FROM ROWS 16-23. FOUND BATTERY CHARGE WEAK. RECHARGED FOR 30 MIN, OPS CHECKED OK. NO REPEATS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300166 20080123 00166 NM 2008 1 23 2008UALA00160 1 20080108 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN UNSECURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 558UA 26654 EEL AT 13C NOT SECURED TO FLOOR. SECURED EEL TRACK TO FLOOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300169 20080123 00169 CE 2008 1 23 DXTA200802774 1 20080117 A 3213 STRUT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG UNDERSERVICED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 950QS 7500050 AFTER TAKEOFF THE RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. TROUBLESHOT. SERVICED THE HYD AND PNEUMATIC SIDE OF NOSE STRUT IAW CE 750 MM CHAP 12-10-38 GEAR SWINGS CHECK GOOD 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008012300170 20080123 00170 CE 2008 1 23 DXTA200802775 1 20080118 A 3340 LIGHT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE TAIL FIRE E DXTA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 GL 07 608QS 5605308 AFTER APU START AND TAIL FLOOD LIGHTS TURNED ON , BOTH PILOT AND FUEL LINEMAN OBSERVED BLUE FLAME AND SMOKE COMING FROM RT TAIL FLOOD LIGHT. RAN APU SEVERAL TIMES, TURNED FLOOD LTS. ON/OFF DURING START AND NORMAL OPERATION. NO INDICATION OF HIGH APU ITT. NO EVIDANCE OF FLASHES OR FLAMES NOTED FROM RIGHT TAIL SIDE OR APU EXHAUST AREA. ALL WORK PERFORMED I AW MM 49-80-00 & 33-40-00 AND AFM. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008012300180 20080123 00180 NM 2008 1 23 2008UALA00168 1 20080110 A 3350 276007 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY LIGHTS INOP: RIGHT OVERWING 2 AFT ASSEMBLIES. REPLACED FUSE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012300181 20080123 00181 NM 2008 1 23 2008UALA00169 1 20080110 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY LIGHT INOP: DOOR 2L CEILING. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012300186 20080123 00186 NM 2008 1 23 2008UALA00178 1 20080109 A 2820 LINE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 ENGINE BULGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 777UA 26916 777008 NR 2 ENG EVIDENCE OF FIRE AT FUEL HYDRAULIC DISCONNECT AREA. HEAT SHIELD IS BURNED AND LINERS ARE DAMAGED. DURING TRO UBLESHOOTING FOUND BURNED HEAT SHIELD BUT NO HYD FLUID RESIDUE. DISCOVERED BALLOON IN FUEL SUPPLY LINE. AFTER REPLACIN G FUEL & HYD LINES, HEAT SHIELD & INSULATION, PERFORMED MOTORING TO VERIFY FIX. REPLACEMENT FUEL LINE ALSO BALLOONED. SECOND REPLACEMENT LINE OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008012300189 20080123 00189 NM 2008 1 23 MWEA080007 1 20080109 A 5320 99579094 INTERCOSTAL BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 925ME 55191 FORWARD CARGO DOOR INTERCOSTAL DAMAGED FROM BELT LOADER, LOCATED BETWEEN LONGERON 23 RIGHT AND 24 RIGHT STATION 374. FA BRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F TR A6WE 2008012300190 20080123 00190 EA 2008 1 23 HNAA0800016 1 20080106 A 5697 WIRE TRIPLEX DHAV DHC8 DHC8311 1386006 EA WINDSCREEN LOOSE A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 EA 07 326EN 12335 11642 TTH2282 234 SMOKE COMING FROM F/O WINDSHIELD NEAR HEATER TERMINAL. MAINTENANCE INSPECTED WIRING AND FOUND A LOOSE WIRE ON THE FIRST OFFICERS WINDOW AT THE HEATER TERMINAL L2. WIRING INSPECTED FOR DAMAGE, NO DEFECTS NOTED. TIGHTENED CONNECTOR, OPERAT IONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2008012300191 20080123 00191 NM 2008 1 23 08FDEA00173 1 20080116 A 3251 1692RA12 METERING VALVE BOEING 727 7272S2F 1384O81 NM ZONE 700 FAILED A FDEA O OTHER O OTHER LD LANDING 1 SO 25 201FE 22924 ON TAXI IN OAK, TILLER WOULD NOT TURN TO THE LEFT, OK TO THE RIGHT. ALL HYD. PRESS GOOD. REMOVED AND REPLACED STEERIN G METERING VALVE IAW 727/200 MM 32-51-021-4. SYSTEM CKS NORMAL ALSO NO LEAKS. R/I FROM FACT PREMATURE REMOVAL/INSTALLA TION OFF MFG 1692RA12. 2 L 7 3 4F A3WE 20080911 WP 2008 9 11 08FDEA03700 1 20080901 A 5414 217000413 PANEL DOUG MD10 MD1010F 3022112 WP NR 3 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 3 PYLON PANEL 488 DL IS CRACKED. FABRICATED THE REPAIR DOUBLER IAW SRM 54-00-1 VOL I. INSTALLED DOUBLER IAW SRM 51 -31-01 VOL II & SRM 54-00-01 VOL I. 2 L 7 3 4F RT A22WE 20080911 WP 2008 9 11 08FDEA03701 1 20080901 A 5320 AUB7203148 WEB DOUG MD10 MD1010F 3022112 WP BS 1473 PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 THERE ARE PUNCTURES (2 PLACES) ON THE FAIRING SUPPORT WEB AFT OF THE RT MLG STRUT CUTOUT AT STA 1473. REMOVED WEB & A NGLE IN REF TO SRM 51-35-01 VOL II. FABRICATED ANGLE IN REF TO DWG ANB 7203; REV " BA ". ALODINED & PRIMED IN REF TO SRM 51-21-01; VOL II. INSTALLED WEB & ANGLE IN REF TO SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 20080911 EU 2008 9 11 08FDEA03702 1 20080901 A 3233 C231290043 ACTUATOR AIRBUS 300 A300B4605R 3930308 EU LEFT MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 656FE 745 LT MLG WOULD NOT RETRACT. "UNLK" AND "DOOR" LIGHTS ON BOTH DETECTION SYSTEMS. ACFT YAW ALSO CONFIRMED GEAR NOT UP. WHEN GEAR HANDLE PLACED IN NEUTRAL, GREEN DOWN LOCKED INDICATOR CAME BACK ON. RE-EXTENDED GEAR FOR LANDING, NO PROBLEMS WITH EXTENTION. SAFTIED BOLTS IN HOLLOW SHAFT AND INSTALLED COTTER PIN IN BOLT INTO STRUCTURE AND SAFTIED RESTRICTOR VALVE AND RIGGED CONTROL ROD. PERFORMED REMOVAL AND INSTALLATION OF LT MLG ACTUATOR AND VARIABLE RESTRICTOR PER AMM 32-31-46 -4. PERFORMED GEAR SWING PER AMM 32-31-00. 3 TIMES ALL INDICATION AND RETRACTION NORMAL LEAK CHECK OK. 2 L 7 2 4F RT A35EU 20080911 EU 2008 9 11 08FDEA03703 1 20080902 A 5315 A53974268200 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSION ON CROSSBEAM C 56 LT OUT OF LIMIT. SPLICE REPAIR PERFORMED IAW. SRM 53-10-15 FIG.207 2 L 7 2 4F RT A35EU 20080911 NM 2008 9 11 USAA920081602 1 20080829 A 5315 6546812 FLOORBEAM BOEING 737 7373G7 1384595 NM ZONE 200 FUSEL CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 SAL C19 MAJOR REPAIR NR 6097669 CORROSION ON FLOORBEAM BETWEEN BS 986.5 & BS 1006, RBL 15. REPAIRED FLOOR BEAM BETWEEN BS 986.5 & BS 1006, RBL15 IAW B737 SRM 53-00-51-2R. 2 L 7 2 4F RT A16WE 20080911 NM 2008 9 11 USAA920081600 1 20080829 A 5330 6545775 SKIN BOEING 737 737401 1384701 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 23876 CLT C5 MAJOR REPAIR 03C10053002/002 CRACK IN FUSELAGE SKIN AT BS727G, ABOVE S25R. REPAIRED FUSELAGE SKIN AT BS 727G. AB OVE S25R IAW US AIRWAYS EA NR 100617 & B737 SRM 53-00-01, REPAIR NR 31. 2 L 7 2 4F RT A16WE 20080911 NM 2008 9 11 QXEA200800398 1 20080418 A 5315 FLOORBEAM DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK ZONE 144 AFT FLOOR SUPPORT ANGLE AT STA X600 IS CORRODED AT Y29.5R. REMOVED CORROSION IAW CPM CHAP 4. UT T HICKNESS IAW -8 200 PT 1, 51-00-04, HI .083 LOW .077. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. REMOV ED .006" MATERIAL FOUND WITHIN LIMITS PER -8 200 SRM 51-20-11 STEP 3. PREP PRIMED, PAINTED IAW 51-20-16, 51-20-36 PARA F,1 AND 51-20-26 PG 8, PARA B(1-6). 2 H 7 2 4T RT A13NM 20080911 NM 2008 9 11 QXEA200800399 1 20080418 A 5315 FLOORBEAM DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK ZONE 144 AFT FLOOR SUPPORT ANGLE AT STA X600 IS CORRODED AT Y20L AND Y24L. REMOVED CORROSION IAW CPM CHAP 4. UT THICKNESS IAW -8 200 PT 1, 51-00-04, HI .083 LOW .061. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NOTED . REMOVED .022" MATERIAL FOUND OUT OF LIMITS PER -8 200 SRM 51-20-11 STEP 3. DRILLED AFFECTED FLOOR SUPPORT ANGLE OFF A ND INSTALL NEW ANGLE IAW -8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 20080911 NM 2008 9 11 QXEA200800407 1 20080418 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK CORROSION ON RT O/B SEAT TRACK AT APPROX X488.5. BLENDED OUT CORROSION IAW RD8-53-10103. ALODINE PRIMED I AW -8 200 SRM 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 20080911 NM 2008 9 11 QXEA200800409 1 20080418 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK BRACKET FOR NR 1 SEAT TRACK WEB AFT OF FRAME 354 IS DAMAGED. REMOVED BRACKET IAW -8 200 SRM 51-40-11. INS TALLED NEW BRACKET IAW -8 200 SRM 51-40-00, 51-40-11. 2 H 7 2 4T RT A13NM 20080911 NM 2008 9 11 USAA920081608 1 20080808 A 5320 6545834257 INTERCOSTAL BOEING 737 7373B7 1384580 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT Q6 MAJOR REPAIR NR 03C10753005/011 LEVEL 2 CORROSION ON INTERCOSTAL AT BS 332, RBL 11. REPLACED INTERCOSTAL AT BS33 2, RBL 11 IAW B737 SRM, 51-10-2. 2 L 7 2 4F RT A16WE 2008011100199 20080111 00199 NM 2008 1 11 SWAA080154 1 20080106 A 5752 6546455 TAB BOEING 737 7373TO 138447G NM LT AILERON DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND LT WING AILERON BALANCE TAB T/E DISBONDED. REPAIRED TAB PER SRM. 2 L 7 2 4F RT A16WE 2008011100205 20080111 00205 EA 2008 1 11 COMA0860001 1 20080101 A 2752 852D10021 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 924CA 9521 7026 FLIGHT 5682 - RECEIVED FLAP FAIL CAUTION AND STALL FAIL CAUTION MESSAGES. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED THE NR 1 FLAP ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100210 20080111 00210 EA 2008 1 11 COMA0860006 1 20080101 A 2752 852D10021 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 924CA 4109 7026 FLIGHT 5682 - RECEIVED FAIL CAUTION AND STALL FAIL CAUTION MESSAGES. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPL ACED RIGHT NR 2 FLAP ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100213 20080111 00213 EA 2008 1 11 COMA0860009 1 20080101 A 2432 17563 BATTERY CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 929CA 6825 7035 FLIGHT 5300 - RECEIVED INTERMITTENT BATTERY BUSS CAUTION MESSAGE. DIVERTED TO MCO, LANDED WITHOUT INCIDENT. REPLACED M AIN BATTERY. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100215 20080111 00215 2008 1 11 COMA0860011 4 20080101 A 3418 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING TRIPPED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 796CA 7338 FLIGHT 5440 - RECEIVED STALL FAIL CAUTION MESSAGE ON TAKEOFF. ABORTED TAKEOFF, RETURNED TO THE GATE. RESET TRIPPED CIR CUIT BREAKER FOR STALL FAIL SYSTEM. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100231 20080111 00231 CE 2008 1 11 DXTA200702737 1 20080101 A 2700 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LEAKING E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 627QS 5605227 ON TAKEOFF, GOT A STAB MISCOMPARE LIGHT AND THE HYDRAULIC PRESS LIGHT. REPLACED ACTUATOR DUE TO EXCESS LEAKAGE IN ACTUA TOR IAW 560XL M/M 23-40-00. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008011100234 20080111 00234 EA 2008 1 11 COMA0860016 1 20080102 A 2752 1104SD100201 FLEX DRIVE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP BENT A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 926CA 7027 FLIGHT 5004 - FLAP FAIL CAUTION MESSAGE RECEIVED. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED RIGHT SIDE NR 2 FLEX SHAFT. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100238 20080111 00238 EA 2008 1 11 COMA0860017 1 20080102 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 818CA 7408 FLIGHT 5220 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH CAR SI-2-27I0002, INCLUDING LEFT AND RIGHT FLAP REJUVE. 2 L 7 2 4F RT A21EA 2008011100241 20080111 00241 NM 2008 1 11 ZZDA2008004 1 20080105 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 924AT 55080 EMERGENCY LIGHTS OUT AT SEAT 1-3 AND 20-24. EMERGENCY LIGHT BATTERY PACK ASSEMBLIES WERE REMOVED AND REPLACED AS PER 33 -51. OPS CHECK NORMAL. 2 L 7 2 4F TR A6WE 2008011100242 20080111 00242 NM 2008 1 11 ZZDA2008005 1 20080104 A 3350 8039491 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 954AT 55016 EMERGENCY LIGHTS AT ROW 21 ABOVE OVERWING EXITS LT & RT INOP. REMOVED AND REPLACED E-BATTERY AT STA 715-737R (B5-230) I AW-AMM-33-51-10, OP CHECKS GOOD. 2 L 7 2 4F TR A6WE 2008011100246 20080111 00246 EA 2008 1 11 COMA0860024 1 20080102 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 SO 01 685BR 10958 7712 FLIGHT 5681 - RECEIVED FLAP FAIL CAUTION MESSAGE. DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED CVG WITHOUT INCIDEN T. REPLACED RIGHT SIDE NR 1 FLAP ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100263 20080111 00263 EA 2008 1 11 COMA0860040 1 20080102 A 3234 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 969CA 28641 7141 FLIGHT 5313 - RECEIVED GEAR DISAGREE MESSAGE. NOSE GEAR DID NOT RETRACT. PERFORMED QRH, DECLARED EMERGENCY, RETURNED T O IAD. REPLACED NLG SELECTOR VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100285 20080111 00285 NM 2008 1 11 08FDEA00032 1 20080104 A 5753 SKIN DOUG MD11 MD11F 3023600 NM T/E FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 RIGHT WING, INBOARD FLAP UPPER SURFACE FOUND DENT AT XIFH 184.5. DENT AREA MEASURED DEPTH = 0.050" FOUND WITHIN LIMIT PER SRM 51-80-01 VOLUME II. HFEC INSPECTION CARRIED OUT AS PER DAC NDT SPM REVISION 13 06-10-01.001 AND FOUND NO C RACK EVIDENT AT DENT REWORK AREA. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008011100302 20080111 00302 CE 2008 1 11 DJFA2008001 1 20080102 A 3260 MS243311 UPLOCK SWITCH BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LT MLG ERRATIC E DJFA O OTHER N FALSE WARNING CL CLIMB 1 EA 23 709TA 7844 RK180 DURING CLIMB-OUT CREW REPORTED RED LIGHTS IN GEAR SELECT HANDLE ILLUMINATED FOLLOWED BY SLIGHT DECELERATION AND A THUMP. CREW SUSPECTS THE GEAR EXTENDED AND RETRACTED UNCOMMANDED. MAINTENANCE FOUND THE LT MLG UPLOCK SWITCH ERRATIC IN COLD TEMPERATURES. THE SWITCH WAS REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2008011100309 20080111 00309 EU 2008 1 11 TRBA2008001 1 20080101 A 3350 3011210 BULB AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EMERGENCY LIGHTS FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 EMERGENCY LIGHT ON ON STAIRS. REPLACED EMERGENCY LIGHT BULB ON STAIRS IAW JIC 25-60-00. 2 H 7 2 4T 4 T RT A53EU E20NE 20080911 NM 2008 9 11 08FDEA03539 1 20080822 A 5753 ARC24434 SKIN DOUG MD11 MD11F 3023600 NM RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 RIGHT WING - INBOARD FLAP LOWER SURFACE FOUND DENT AT XIFH 255. RIGHT WING - INBOARD FLAP LOWER SURFACE DENT AT XIFH 25 5 DAMAGED CARRIED OUT REPAIR AS PER SRM 57-10-00 FIGURE 2 VOLUME I. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080911 NM 2008 9 11 08FDEA03516 1 20080820 A 5753 ARC24433 SKIN DOUG MD11 MD11F 3023600 NM LT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 LEFT WING - INBOARD FLAP LOWER SURFACE FOUND DENTS AT XIFH 249. LEFT WING INBAORD FLAP LOWER SURFACE DENT AREAS TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080912 NM 2008 9 12 USAA920081612 1 20080825 A 5340 69353502 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN C18 MAJOR REPAIR NR 6124318 CRACKED STRINGER CLIP AT BS 480, S16L. REPLACED STRINGER CLIP AT BS 460, S16R IAW SRM 5 1-40-02-OG. 2 L 7 2 4F RT A16WE 20080912 WP 2008 9 12 UPS08853098 1 20080720 A 5740 5803913519 ATTACH FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C2 AFTER REMOVAL FOUND 5803913-519 STRINGER 54 ATTACH FITTING BROKEN OFF A/C PART. LOCATED, DRILLED, RE PLACEMENT STRINGER 54 ATTACH FITTING TO BE INSTALLED ON NR 207274. 2 L 7 4 4F RT 4A25 20080915 NM 2008 9 15 08FDEA02883 1 20080715 A 5330 651842012 SKIN BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 275FE 22040 GOUGE IN SKIN AT FUSELAGE STA 265 FWD OF ELEC POWER RECEPTACLE ACCESS DOOR TRIMMED OUT DAMAGE SKIN (DIM 4 BY 1 1/4) IAW EA 7-5330-122320. HFEC INSPECTED AREA IAW NDTM 51-00-00 FIG 16 AND 2. NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER AND REPAIR FILLER IAW SRM 57-10-1 AND EA 7-5330-122320. TREATED AND PRIMED PARTS IAW SRM 51-10-2 AND INSTALLED REPAIR PART S IAW SRM 51-30-2 AND EA 7-5330-122320. 2 L 7 3 4F RT A3WE 20080915 NM 2008 9 15 08FDEA03159 1 20080730 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL ACCESS PANEL CUTOUT 541EB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIE D AS MINOR PER GMM 6-2-100. 2 L 7 2 4F RT A2NM 20080915 EA 2008 9 15 SWIA200819999 1 20080710 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 770SK FLOORBEAM CRACKED AT LBL AND RBL 9. FOUND AT C-CHECK. COMPLIED WITH REPAIRS TO FLOORBEAM IAW REO 670-53-11-047. 2 L 7 2 4F RT A21EA 20080915 NM 2008 9 15 UPS08553105 1 20080807 A 5340 ATTACH ANGLE BOEING 757 75724APF 1384969 NM BS 1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 453UP 25474 INSPECTION TYPE:C3 RT MLG WHEEL WELL BODY DOOR CUTOUT, CRACKED FWD BULB SEAL RETAINER ATTACH ANGLE TO BS 1060 FRAME 2ND I/B FROM O/B END. REPLACED RT MLG WHEEL WELL BODY DOOR CUTOUT 2ND I/B FROM O/B END SEAL RETAINER ATTACH ANGLE BRACKET. 2 L 7 2 4F RT A2NM 20080915 NM 2008 9 15 UPS08553114 1 20080808 A 5420 SUPPORT BOEING 757 75724APF 1384969 NM NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 453UP 25474 INSPECTION TYPE:MOD NR 1 PYLON UNDERWING FAIRING STRUCTURE LT FWD SUPPORT BRACE IS CRACKED AT PPS 185.0. REMOVED AND RE PLACED PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20080915 WP 2008 9 15 UPS08853134 1 20080728 A 5312 5612298341 PRESSURE PANEL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 PRESSURE WEB CRACKED AROUND RIVET HEAD, RT NOSE A/C TUNNEL CEILING STA -54, RBL 35. REPAIRED CRACK P ER SAA EA 008-5330-01-A1489. 2 L 7 4 4F RT 4A25 20080915 NM 2008 9 15 SWAA084780 1 20080828 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 242WN 32505 DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 SWAA084782 1 20080828 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 787 S26L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080915 EU 2008 9 15 08FDEA03438 1 20080815 A 5315 A53978267208 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSION ON CROSSBEAM C 67 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080915 NM 2008 9 15 08FDEA03114 1 20080729 A 5320 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTI NG AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB CRACKED NR 6 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-3 1-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080915 WP 2008 9 15 08FDEA03268 1 20080805 A 5313 ADA78981 STRINGER DOUG MD10 MD1010F 3022112 WP ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 FWD CARGO COMP LONGERON 52 AT STA 1026 IS MISSING FASTENERS AND IS GOUGED IN THE RADIUS. INSTALLED REPAIR CHANNEL AND R EPLACED MISSING FASTENERS IN REFERENCE TO DC/MD-10 SRM 53-10-00; FIG 2-A; VOL I. 2 L 7 3 4F RT A22WE 20080915 WP 2008 9 15 08FDEA03445 1 20080815 A 5311 AEA02733 FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 FRAME P/N AEA 0273-3 REQUIRES FABRICATION DUE TO BEING CORRODED BEYOND LIMITS. FABRICATED A NEW FRAME SECTION AND SHEAR TIE IAW DWG AEA 0273; REV "G". LOCATED AND DRILLED AEA 0273-3 FRAME AND AEA 0273-5 SHEAR TIE. ALODINED AND PRIMED I AW SRM 51-21-01; PGS 21 AND 24; VOL II. APPLIED TOP COAT OF PAINT IAW SRM 51-21-02; PG 1; VOL II. PART MARKED NEW PART S IAW GMM 7-0-1001. FRAME SECTION REMOVED AND INSTALLED ON SNRM N00567. 2 L 7 3 4F RT A22WE 20080915 EU 2008 9 15 08FDEA03382 1 20080812 A 5755 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 5 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND DELAMINATION AT SPOILER 5 LT CENTER HINGE ARM LOWER SURFACE OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF SPOI LER IAW AMM 27-61-53 /401. 2 L 7 2 4F RT A35EU 20080915 EU 2008 9 15 08FDEA03383 1 20080812 A 5755 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 5 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND DELAMINATION AT SPOILER 5 RT, LT/RT HINGE ARM LOWER SURFACE AND TOP SKIN OUT OF LIMIT. REPAIR PERFORMED BY REPLAC EMENT OF SPOILER IAW AMM 27-61-53 /401. 2 L 7 2 4F RT A35EU 20080915 NM 2008 9 15 08FDEA03594 1 20080826 A 5313 AEA76431 LONGERON DOUG MD11 MD11F 3023600 NM BS 1521 L29R CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 574FE 48499 RIGHT FUSELAGE EXTERNAL LONGERON END FITTING AT STA 1521.000 LONGERON 29 FOUND WITH CRACK. HFEC INSPECTION CARRIED OU T PER DAC NDT SPM REVISION 13.06-06-10-01.001, CRACK IS APPROXIMATELY 1 INCH LONG. CRACKED SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. NEW SPLICE REWORKED AS PER DRAWING AEA7643. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 08FDEA03596 1 20080826 A 5347 601096518 SEAT TRACK DOUG MD10 MD1030F 3024020 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 304FE 46992 MAIN CARGO DECK STA 1256-1276 RBL 48 SEAT TRACK IS DAMAGED REPLACED SEAT TRACK IAW SRM 51-70-00. 2 L 7 3 4F RT A22WE 20080915 EU 2008 9 15 08FDEA03597 1 20080826 A 2780 4907905 SLAT SYSTEM AIRBUS 310 A310324 3930206 EU SLATS MALFUNCTIONED A FDEA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 CE 21 805FD 456 DURING APPROACH WITH THE LDG GEAR DN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 A ND 2 FAULT LIGHTS ON O/H. DISCONTINUED AP AND FOLLOWED QRH. WHEN THE SLATS/FLAPS CYCLED PER QRH, THE LIGHT/FAULTS CL EARED CONFIGURED AGAIN THE SLATS STUCK AT 15 DEGREES. FOLLOWED QRH FOR SLATS STUCK LANDING. ON FINAL AP FLAP HANDLE AT 40 DEGREES THE SLATS BROKE FREE AND WENT TO 30 DEGREES SLATS WITH 40 DEG FLAPS. THE LANDING WAS UNEVENTFUL AND SLAT/ FLAP RETRACTON THE GROUND WAS NORMAL. REMOVED AND REPLACED SFCC'S, OFF MFG 49-079-05 POS 1 SRL 144 OFF MFG 49-079-05 P OS 2 SRL 692. GEK BAE SYSTEMS AVIONICS LTD. 2 L 7 2 4F RT A35EU 20080915 WP 2008 9 15 08FDEA03599 1 20080826 A 5311 AEA02733 FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 FRAME P/N AEA 0273-3 REQUIRES FABRICATION DUE TO EXISTING FRAME BEING CORRODED BEYOND LIMITS AT STA 1501. FABRICATED A NEW FRAME SECTION AND SHEAR TIE IAW DAC DWG AEA 0273; REV "G". LOCATED AND DRILLED AEA 0273-3 FRAME AND AEA 0273-5 SHEA R TIE. ALODINED AND PRIMED IAW SRM 51-21-01; PGS 21 AND 24; VOL II. APPLIED TOP COAT OF PAINT IAW SRM 51-21-02; PG 1; VOL II. PART MARKED NEW PARTS IAW FEDEX GMM 7-0-1001. FRAME SECTION REMOVED AND INSTALLED ON SNRM N00567. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 08FDEA03359 1 20080810 A 5330 65545753 SPLICE BOEING 727 727233 138408A NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 SKIN GOUGED LEFT FUSELAGE LAP SEAM FWD OF 720E AT STR 19L. FABRICATED REPAIR DOUBLER FROM 2024-T3 .071 PO NR 9006288 DI MS 14 INCH BY 7 1/2 INCH. FABRICATED STRUCTURAL FILLER FROM 2024-T3 .063 PO NR 9006773 DIMS 14 INCH BY 5 INCH. INSTALL ED REPAIR PARTS AT FUSELAGE LAP SEAM FWD OF 720E STR 19L IAW SRM 53-30-3 FIG 14 AND SRM 53-30-2 FIG 2. 2 L 7 3 4F RT A3WE 20080916 WP 2008 9 16 08FDEA03167 1 20080730 A 5411 AUB710739 RIB DOUG MD10 MD1010F 3022112 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 NR 1 PYLON ATTACH FLANGE FOR PANEL 438 GL IS CRACKED. REMOVED AND REPLACED RIB NR AUB 7107-39, PO 625780.4 IAW DAC DWG AUB 7107, REV "P" AND DC/MD-10 SRM 51-35-01, VOL II. 2 L 7 3 4F RT A22WE 20080916 NM 2008 9 16 08FDEA03728 1 20080905 A 5753 6521631201 SKIN BOEING 727 727227 1384078 NM LT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 LT WING O/B FORE FLAP I/B SEQUENCE CARRIAGE HAS ELONGATED BOLT HOLES AT AFT END WBL 348 REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 57-50-2 FIG 4, 57-50-4 FIG 7. TREATED AND PRIMED IAW SRM 51-10-2. INS TALLED REPAIR DOUBLER IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20080916 EU 2008 9 16 08FDEA03248 1 20080804 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 MAIN CABIN BETWEEN FRAME 63 AND FRAME 64, RBL 18 THE SEAT TRACK IS DAMAGED. SPLICED IN A NEW SEAT TRACK SECTION IAW A30 0-600 SRM 53-10-16, FIG 210. ALODINED, PRIMED AND PAINTED IAW A300-600 SRM 51-21-10. APPLIED CIC IAW A300-600 SRM 51-2 3-20, PARA 9. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03135 1 20080729 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 CABIN SEAT TRACK IS DAMAGED AT FRAME 38.1, RBL 67. SEAT TRACK FOUND TO BE OUT OF LIMITS PER A300-600 SRM 53-10-16. RE MOVED THE DAMAGED TRACK PER A300-600 51-41-21. MATERIAL ID FOR THE NEW TRACK P/N A5327400500053, PO 617932.1. MATERIAL ID FOR THE SPLICES P/N R5327049020000, PO 618090.2 PER A300-600 SRM 53-14-16. MARKED THE PARTS IAW GMM 7-0-1001. INST ALLED THE SEAT TRACK AND SPLICES PER A300-600 SRM 51-40-21. LOCATED AND DRILLED SEAT TRACK AND SPLICES PER A300-600 S RM 53-10-16. APPLIED CIC PER A300-600 AMM 51-22-00-0. 2 L 7 2 4F RT A35EU 20080916 SO 2008 9 16 LR7A08113 1 20080902 A 6120 582855 HOUSING LKHEED 382 382G 526414U SO PROP VALVE UNKNOWN A LR7A E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 403LC 1258 4590 DURING CRUISE FLIGHT, CREW REPORTED NR 4 PROPELLER RPM OUT OF LIMITS. PERFORMED ENGINE SHUT DOWN IAW ESP. NR 4 PROPELL ER VALVE HOUSING REPLACED IAW LACE JOB CARD HN61135, OPS CHECK GOOD. 2 H 7 4 4T A1SO 20080916 SO 2008 9 16 LR7A08114 1 20080905 A 6120 582855 HOUSING LKHEED 382 382G 526414U SO NR 1 PROP UNKNOWN A LR7A E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 AL 03 405LC 1087 5025 DURING SHORT FINAL, CREW REPORTED NR 1 PROPELER RPM OUT OF LIMITS. PERFORMED ENGINE SHUT DOWN IAW ESP. NR 1 PROPELLER VALVE HOUSING REPLACED IAW LAC JOB CARD HN61135, OPS CHECK GOOD. 2 H 7 4 4T A1SO 20080916 WP 2008 9 16 08FDEA03297 1 20080807 A 5311 ABA722113 FRAME DOUG DC10 DC1030F 3023504 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 AVIONIC COMPT FOUND CRACK ON FRAME. 2 L 7 3 4F RT A22WE 20080916 EU 2008 9 16 08FDEA03299 1 20080807 A 5415 A54610926000 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 CORROSION FOUND IN BOLT HOLES OF FORWARD PYLON TO ENGINE ATTACH FITTING. REPAIR PERFORMED BY REWORK OF CORROSION, NDT F OR CORROSION FREE CONDITION, AND PROTECT RIB 8 WITH CADMIUM PLATING IAW RAS/70511822/004/2008 ISS A, APPROVED BY EA 6-54 51-120089. 2 L 7 2 4F RT A35EU 20080916 SO 2008 9 16 LR7A08093 1 20080819 A 5312 3425828R BULKHEAD LKHEED 382 382G 526414U SO FS 880 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HC5315 FOUND AFT FUSELAGE INTERIOR BULKHEAD WEB CRACKED AT FS 880, WL206, RBL64 . REPAIRED IAW SMP583 FIG 51-140-17. 2 H 7 4 4T A1SO 20080916 SO 2008 9 16 LR7A08094 1 20080819 A 5230 SKIN LKHEED 382 382G 526414U SO CARGO DOOR DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HST5301 FOUND CARGO DOOR EXTERIOR SKIN DENT AT FS 880 TO 902, LBL 61TO RBL 61. REPAIRED BY REPLACING SKIN IAW SMP583 CHAP 51-60, 51-70, AND DRAWING 362005. 2 H 7 4 4T A1SO 20080916 NM 2008 9 16 2008UALA04364 1 20080820 A 2421 729825G IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 538UA 25222 LT GEN DRIVE LIGHT. RTFL. FOUND FAULTY IDG. INSTALLED NEW NR 1 IDG. ACCOMPLISHED OPS CHK & LEAK CHECK. ALL CHECKS G OOD. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080916 EU 2008 9 16 2008UALA04192 1 20080809 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ROW 20 ABC FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 432UA 587 DURING 3 SVC CHECK EMERGENCY SYSTEM TEST FAILED. MSG 33-51-38 "INT. LOADS AFT L" + "EXT. LOADS AFT L. T-S DOWN TO ROW 2 0ABC EGRESS LIGHTING, REMOVED BULB. OPERATION NORMAL. ALL OTHER EGRESS LIGHTING WORKING NORMALLY. REPLACED 20ABC SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY. ALSO PERFORMED CABIN EMERGENCY LIGHT TEST. TESTED OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080916 NM 2008 9 16 2008UALA04218 1 20080809 A 3397 90085 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY LIGHT DOOR 3R FWD EXIT SIGN INOP. FOUND LOOSE CONNECTOR. SECURED BATTERY CONNECTOR. EXIT SIGN OPS CKS NORMAL . 2 L 7 4 4F 4 F RT A20WE E24NE 20080917 WP 2008 9 17 08FDEA03713 1 20080903 A 5340 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 2 SPOOL BACK UP FITTING HOLES C & D HAVE CRACK INDICATIONS IN THE BACK UP FITTING. REQUIRES REMOVAL. REMOVED & R EPLACED BACK UP FITTING NR 2 IAW SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 20080917 NM 2008 9 17 ASAA0843353 1 20080716 A 5330 65C323585 SKIN BOEING 737 7374Q8 138447Q NM BS 400 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 FUSELAGE SKIN DENTED WITH CREASE STA 400 JUST BELOW STR 15R. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLED, LOCATED, DRILLED AND INSTALLED IAW SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 20080917 NM 2008 9 17 ASAA0843362 1 20080722 A 5340 STRINGER CLIP BOEING 737 7374Q8 138447Q NM BS 887 S4L CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 STRINGER CLIP STA 887 STRINGER 4L CRACKED. REMOVED DAMAGED STRINGER CLIP, LOCATED, DRILLED AND INSTALLED A REPLACEMENT STRINGER CLIP IAW SRM 51-40-02 PAR 4. 2 L 7 2 4F RT A16WE 20080917 NM 2008 9 17 ASAA0843373 1 20080723 A 5322 654653013 SHEAR TIE BOEING 737 7374Q8 138447Q NM BS 460 S28L/R CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 07 754AS 25095 SHEAR TIE AT STA 460 BETWEEN STRINGER 28 L TO 28R IS CORRODED. REMOVED AND REPLACED SHEAR TIE IAW B737 SRM 53 00 07. 2 L 7 2 4F RT A16WE 20080918 EU 2008 9 18 2008UALA05474 1 20080825 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 451UA 865 FLOORBEAM 235 CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. INSTALLED TIE DOWN FITTINGS FOR LAV AND GALLEY MODULES ONT O NEW FLOORBEAM 235. FITTED BEAM 235 TO ACFT (PICKED UP HOLES) AND FITTED 2EA. NEW SPLICES AT FWD END OF BEAM 235. IN STALLED FLOORBEAM 235 IN ACFT. NEW SPLICES AT FWD END HAVE TO BE INSTALLED FOR COMPLETION OF INSTALLATION. INSTALLED S PLICES ON BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20080918 NM 2008 9 18 2008UALA04353 1 20080819 A 3350 GUARD BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 EEL LIGHTING AT ROWS 6-8 RT SIDE TURN OFF AND ON RANDOMLY. FOUND LOOSE LIGHT GUARD. SECURED LIGHT GUARD OP CHECK GOOD. ACFT OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 EU 2008 9 18 2008UALA04355 1 20080820 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS CROSSED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 494UA 1840 CREW REPORT: EMERGENCY EXIT SIGN AT LEFT OVERWING EXIT INOP. 2 L 7 2 4F 4 F RT A28NM E40NE 20080918 NM 2008 9 18 CALA0800800 1 20080821 A 5320 6517688U165 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 Z-ANGLE AT L1 DOOR HAS CORROSION. REMOVED CORRODED Z-ANGLE AT L1 DOOR AND INSTALLED NEW Z-ANGLE IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 2008UALA04280 1 20080815 A 3350 20131A BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT AT DOOR 2R FLASHES INTERMITTENTLY. *S/D* REPLACED POWER SUPPLY BATTERY ASSY, OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 NM 2008 9 18 2008UALA04286 1 20080814 A 3350 20121 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 510UA 24780 LT SIDE MOST TWO AFT EMERGENCY LIGHTS OVERHEAD STOW BIN NO GOOD DURING CHECK. RELAMP, NO HELP. FURTHER TS NEEDED. *S/ D* REPLACED M10818 POWER SUPPLY BATTERY ASSY, EMERGENCY LIGHTS OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 2008 9 18 2008UALA04362 4 20080820 A 2350 MICROPHONE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE OXYGEN MASK FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 669UA 30025 F/O O2 MASK MICROPHONE INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20080918 EU 2008 9 18 2008UALA04365 1 20080821 A 5740 ATTACH BRACKET AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 3 FLAP TRACK BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 423UA 504 LEFT NR 3 FLAP TRACK AFT END STAY ASSY ATTACH BRACKET I/B LUG BROKEN. 2 L 7 2 4F 4 F RT A28NM E40NE 20080918 NM 2008 9 18 2008UALA04117 1 20080802 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 2A INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT SEAT 2A FWD INOP. *S/D* REPLACED EEL CABLE. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 NM 2008 9 18 2008UALA04290 1 20080813 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SEAT 15C BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 EMERGENCY EXIT LIGHT ASSEMBLY BROKEN AT SIDE OF SEAT 15C. *S/D* REPLACED EEL ASSY ON SEAT 15C. OPS CHECK OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NM 2008 9 18 2008UALA04163 1 20080806 A 5753 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT WING TE FLAP DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 LEFT WING INBOARD MID FLAP HAS DELAM. ON TOP SIDE. DAMAGE AREA IS APPROX. 4" X 6" AND MARKED IN RED. *S/D* REMOVED LT INBOARD MID FLAP TRAILING EDGE PANEL FOR IN SHOP REPAIR DUE TO DELAMINATION. REPAIR ACP BY SHOP, INSTALLED PANEL AND CH ECKED FIT AND FAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 20080918 NM 2008 9 18 2008UALA04373 1 20080821 A 3350 20121 CHARGER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 331UA 24192 FWD OVERHEAD EMERGENCY EXIT SIGN AND 1L EMERGENCY EXIT SIGNS INOP. *S/D* REMOVED & REPLACED BATTERY CHARGER LT FWD. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012200041 20080122 00041 EU 2008 1 22 TRBA2008004 1 20080111 A 3350 GE44 BULB AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EMERGENCY LIGHT FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 434AT 434 EMERGENCY LIGHT IN PASSENGER DOOR INOPERATIVE. RELAMPED AIRSTAIR EMERGENCY LIGHT BULB IAW MM 35-50-00. OPERATIONAL CHE CK GOOD. 2 H 7 2 4T 4 T RT A53EU E20NE 2008012200062 20080122 00062 NM 2008 1 22 F3LA200800003 1 20080110 A 3350 32146210 EPSU AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE ZONE 200 INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 940FR 9912 61 2465 DURING PERFORMANCE OF EPSU (12WL) FUNCTIONAL TEST, THE MECHANIC NOTED A POWER SUPPLY FAULT ON THE MDCU. THE EPSU WAS RE PLACED, IAW AMM 33-51-38 PB 401 AND OPERATIONS CHECKED OKAY. PART TOTAL TIMES AND TOTAL CYCLES WILL BE PROVIDED AT A LA TER DATE. REFERENCE LOG BOOK PAGE 308363, HOURS AND CYCLES FOR THE PART HAVE BEEN ADDED 01/11/08. 2 L 7 2 4F 4 F RT A28NM E37NE 2008012200077 20080122 00077 CE 2008 1 22 DXTA200802764 1 20080113 A 2750 SWITCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE TE FLAPS MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 671QS 5605071 AFTER TAKEOFF UPON FLAP RETRACTION THE "STAB MISCOMPARE ANNUNCIATOR LIGHT" ILLUMINATED. REPLACED SWITCHES SC050 AND SC051 PER MM 27-90-40. GROUND OPERATIONAL CHECK GOOD 2 L 7 2 4F 4 F RT A22CE E00059EN 2008012200078 20080122 00078 CE 2008 1 22 DXTA200802765 1 20080113 A 3297 WIRE HARNESS CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE ANTI SKID SYS SHORTED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 314QS 5600441 AT APPROXIMATELY 70 KNOTS THE ANTI-SKID INOP LIGHT CAME ON. ABORTED THE TAKEOFF. REMOVED THE LT ANTI-SKID TRANSDUCER W IRE BUNDLE FROM LEFT GEN TO WHEEL WELL CONNECTOR DUE TO OPEN. INSTALLED NEW WIRE BUNDLE IAW CE5650 M/M CH 32-42-00. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2008012200080 20080122 00080 EA 2008 1 22 TRAX200800045 1 20080105 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 904EV 7628 FS 280 WEB CRACKED AT RBL 9. 2 L 7 2 4F RT A21EA 2008012200098 20080122 00098 NM 2008 1 22 LYNX00003 1 20080108 A 3230 483025 SEQUENCE VALVE BOMBDR DHC8 DHC8402 1390042 NM MLG STICKING A 3LYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 21 507LX 39 4181 AFTER TAKEOFF LT DOOR AMBER LIGHT FAILED TO EXTINGUISH, FOLLOWED QRH PROCEDURE AND EXTENDED GEAR, LT GEAR DOOR AMBER LIG HT STILL DID NOT EXTINGUISH AND RED LT LANDING GEAR WARNING REMAINED ILLUMINATED. AFTER APPROX 5 MINUTES GEAR LOCKED DOW N AND GREEN LT LIGHT ILLUMINATED. FA REPORTED VERY SLOW EXTENSION OF LT GEAR. RETURNED TO DEPARTURE. MAINTENANCE PINNED GEAR AND FLEW AIRCRAFT ON A SPECIAL FLIGHT PERMIT. MAINTENANCE WAS ABLE TO DUPLICATE THE PROBLEM ON THE GROUND, TROUBLES HOT TO THE LT SOLENOID SEQUENCE VALVE, DFDR WAS DOWNLOADED AND CONFIRMED THAT THE LT GEAR TOOK 1 MINUTE AND 8 SECONDS TO EXTEND WHICH IS CONSISTENT WITH A SOLENOID SEQUENCE VALVE STUCK IN THE (OUT OF SEQUENCE) FAULT. MAINTENANCE ALSO CHANGE 2 H 7 2 4T RT A13NM 2008012200103 20080122 00103 SW 2008 1 22 WGEA200800003 1 20080109 A 5751 271093901002 BELLCRANK ECLIPS EA500 ECLIPSEEA500 3350000 SW PWC PW615 PW615FA 52282 NE AILERONS BINDING E WGEA O OTHER O OTHER CR CRUISE 1 EA 27 141DJ 95 000055 MX LOG PG. NR 0829 DISC NR 3 STICK BINDS TOP CENTER 3 DEGREES TO EITHER SIDE OF CENTER WHEN INITIATING ROLL. NOTED IN FL IGHT, BOTH LT AND RT STICKS. WO 1098, NRI 1. REMOVED AND REPLACED RT AILERON BELLCRANK AND JOINT ASSEMBLY IAW AMM 27-11 -17. PERFORMED RIG CHECK IAW AMM 27-00-00. CHECKED WITHIN LIMITS. 1 L 7 2 4J 4 F RT A00002AC E00073EN 2008012200106 20080122 00106 EA 2008 1 22 TRAX200800055 1 20080106 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 904EV 7628 LBL 9 INBOARD 280 CLIP FOUND CRACK. 2 L 7 2 4F RT A21EA 2008012200118 20080122 00118 EU 2008 1 22 TRAX200800040 1 20080104 A 5720 ANGLE AEROSP ATR72 ATR72 EU LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 ON TOP OF LEFT WING BOX AT FR 23D AND RIB 1 ANGLE OF INTERCOSTAL FOUND CRACKED. FABRICATION OF ANGLE OF INTERCOSTAL ON LEFT WING BOX AT FR 23D RIB 1 COVERED ON W/C 2000-146. ANGLE OF INTERCOSTAL ON TOP OF LEFT WING BOX AT FR 23D RIB 1 INS TALLED IAW SRM 51-25-01. SUPPLEMENTAL SDR CLOSED 1/10/08. 2 H 7 2 4T RT 2008012200124 20080122 00124 2008 1 22 2008UALA00072 4 20080104 A 3445 6228973001 ANTENNA BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE TCAS UNRELIABLE A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 670UA 29240 TCAS LWR ANTENNA, HARD FAULT. REMOVED & REPLACED LOWER TCAS ANTENNA PER MM34-45-01-401, OPERATIONAL CHECK PER MM34-45-0 0-501. RESET ENTIRE SYSTEM, GROUND CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012200144 20080122 00144 NE 2008 1 22 EGRR118593 1 20080117 A 5520 76020105002128 ANGLE SKRSKY S76 S76B 8143007 NE PWA PT6 PT6* 52043 EA HORIZONTAL STAB CRACKED B EGRR O OTHER O OTHER NR NOT REPORTED 1 EA 17 401CV 1155 760327 DURING 900 HR AIRFRAME INSPECTION WITH HORIZONTAL STABILIZER REMOVED, TECH FOUND AFT SPAR WEB P/N 76201-25002-101 CRACKE D NEAR THE TOP LT HORIZONTAL STABILIZER SUPPORT FITTING BOLT HOLE. REMOVED HORIZONTAL SUPPORT FITTING ASSY. AND FOUND TH E LT AFT SPAR CAP ANGLE P/N 76201-05002-128 CRACKED. PERFORMED DETAILED INSPECTION AND FOUND AFT SPAR DOUBLER PN 76201-0 5002-105 AND AFT SPAR CANTED BULKHEAD P/N 76201-04010-101 CRACKED AT THE ABOVE BOLT HOLE. THE REPAIR CONSISTED OF REPLAC EMENT OF THE FOLLOWING PARTS: LT AFT SPAR CAP ANGLE P/N 76201-05002-128 AFT SPAR DOUBLER 76201-06002-105 AFT SPAR WEB 7 6201-25002-101 UPPER SHEAR DECK 76202-04002-117 AFT SPAR CANTED BULKHEAD 76201-24010-101 RT UPPER BATH. 1 G 7 2 4U 3 T H1NE E2NE 2008012200151 20080122 00151 CE 2008 1 22 010808N341CS1 1 20080108 A 5311 65111312 FRAME CESSNA 500 550 2076604 CE PWA 530 PW530A NE BS 263 CRACKED E Z5FA K NONE O OTHER IN INSP/MAINT 1 EA 63 341CS 2407 5501106 FUSELAGE FRAME CRACKED AT FS 263.4 LBL 15.35 FRAME PN 6511131-2MFG AT ICT IN PROCESS OF REPAIR DEFINITION S-550-ATA53/1 6RD. 1 L 7 2 4F 4 F A22CE E00053EN 2008012200153 20080122 00153 EU 2008 1 22 TRBA2008006 1 20080114 A 3397 WIRE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE EXIT SIGN BROKEN A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 420AT 420 EMERGENCY EXIT LIGHT BY SERVICE DOOR ON FLOOR INOP. REPAIRED BROKEN WIRES AT SERVICE DOOR EMERGENCY EXIT SIGN IAW SRM 2 0-27-14 PERFORMED OPT CHK FOUND WORKING PROPERLYAT THIS TIME IAW JIC 33-50-00. 2 H 7 2 4T 4 T RT A53EU E20NE 2008012200189 20080122 00189 EA 2008 1 22 TRAX200800063 1 20080109 A 2560 GLOWSTRIP CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 PAX COMPARTMENT RIGHT SIDE OVERWING AFT EMERGENCY TRACK LIGHTING PHOTOLUMINESENT STRIP IS MISSING. 2 L 7 2 4F RT A21EA 2008012200195 20080122 00195 CE 2008 1 22 4533301062008 1 20080106 A 7540 CLAMP LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312 01518 WP HP BLEED LOOSE E J7SA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SW 05 438FX 333 RT BLEED OVERHEAT AMBER CAS MESSAGE POSTED. CREW DECLARED AN IFE AND LANDED. MX FOUND LOOSE CLAMPS ON THE LT HP BLEED VALVE AND LT LP DUCT PERRY SEALS. SEALS WERE REPLACED, CLAMPS RETORQUED AND LEAK CHECKS PERFORMED. NO DEFECTS NOTED 2 L 7 2 4F 4 F RT T00008WI E6WE 2008012200196 20080122 00196 CE 2008 1 22 6029501072008 1 20080108 A 2131 21198304 CONTROLLER LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE CABIN PRESSURE FAILED E J7SA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 05 259FX 295 LOST PRESSURIZATION IN AUTO MODE INFLIGHT, CREW REPORTED THAT THEY LOST PSI RAPIDLY AT 40K FT, CRUISE WITH DELTA P AT 9 .1. CABIN ALTITUDE INCREASED TO 10 FT WITH CABIN RATE MAXED OUT. EMER PSI ACTIVATED AND CREW COULD NOT RESET. PRESSURIZA TION FAULT LIGHT ILLUMINATED. CO-PILOT WAS ABLE TO GAIN CONTROL OF CABIN IN MANUAL MODE. MX REPLACED THE CABIN PRESSUR E CONTROLLER AND PERFORMED SATISFACTORY OPS CHECKS. 2 L 7 2 4F 4 F RT A10CE E35NE 2008012200197 20080122 00197 SO 2008 1 22 RAIA00801006 1 20080107 A 3230 230929000001 UPLOCK EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL MLG INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 819HK 19112 145062 FLT NR 5577-STL-NOSE LANDING GEAR FAIL TO RETRACT. MAINTENANCE REMOVED AND REPLACED THE NOSE UPLOCK BOX. OPS CHECKED GO OD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008012200212 20080122 00212 EU 2008 1 22 08FDEA00072 1 20080108 A 5347 A53774604202 SEAT TRACK AIRBUS 310 A310203 3930313 EU GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN CABIN SEAT TRACK Y1959 SCALLOPS GOUGED AND ELONGATED FRAME 20 TO 21. BLENDED SCALLOPS IAW FEDEX A310-200 SRM 53-10- 16. FOUND TO BE OUT OF LIMITS IAW FEDEX A310-200 SRM 53-10-16. REMOVED ENTIRE DAMAGED SEAT TRACK SECTION FR 18 -FR 26 MADE CUT IAW FEDEX A310-200 EA 6-5310- 109235 AND REINSTALLED NON DAMAGED PART OF SEAT TRACK FR 20 8 - FR 26 IAW FEDEX A310-200 SRM 51-40-21 PARA 7. FABRICATED NEW SEAT TRACK FR 18 TO FR 20, 8 AND REPAIR SPLICE IAW FEDEX A310-200 EA 6-531 0-109235. INSTALLED ALL REPAIR PARTS IAW FEDEX A4310-200 EA 6-5310-109235. APPLIED FR PRIMER IAW FEDEX A310-200 SRM 51 -21-10 AND TOP COATED IAW FEDEX A310-200 SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008012200251 20080122 00251 EU 2008 1 22 Y2PA200800027 1 20080104 A 5310 DOOR FRAME AMD FALCON FALCON20 2730103 EU FUSELAGE CRACKED A Y2PA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AA 67 DURING "A" CHECK INSPECTION FOUND 2 CRACKS ON CARGO DOOR FRAME AT THE AFT SCISSOR ASSY AREA. 2 L 7 2 4F RT A7EU 2008012200254 20080122 00254 NM 2008 1 22 AALA200800019 1 20080102 A 3350 D71701001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 AFW - EMERGENCY LIGHT BATTERY PACK AT LEFT NUMBER THREE DOOR FAILED TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008012200255 20080122 00255 NM 2008 1 22 AALA200800006 1 20080101 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 797AN 30012 JFK - EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008012200256 20080122 00256 NM 2008 1 22 AALA200800008 1 20080101 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 190AA 32384 DFW - EMERGENCY LIGHT AT AFT GALLEY INOPERATIVE. REPLACED LIGHT ASSEMBLY L762 FOR EMERGENCY LIGHT AT AFT GALLEY. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008012200258 20080122 00258 NM 2008 1 22 AALA200800016 1 20080102 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 977AN 29550 DFW - EMERGENCY LIGHT AT SEAT 16D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008012200259 20080122 00259 NM 2008 1 22 AALA200800017 1 20080102 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 977AN 29550 DFW - EMERGENCY LIGHT AT SEAT 27D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008012200260 20080122 00260 NM 2008 1 22 AALA200800014 1 20080102 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 355AA 24036 JFK - EMERGENCY EXIT LIGHT AT LEFT AND RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK M1208 FOR EMERGENCY LIG HT AT LEFT AND RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008011400002 20080114 00002 CE 2008 1 14 DXTA200802761 1 20080110 A 3260 DOWNLOCK SWITCH CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE MLG MALFUNCTIONED F DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 614QS 5605580 RT GEAR INDICATOR LIGHT SHOWED RT GEAR NOT DOWN AND LOCKED. PEFORMED GEAR SWING MANY TIMES WITH NO FAULTS. APPLIED FR EEZE-IT SPRAY TO RT GEAR DOWNLOCK SWITCH GIVING US A FAULTY LIGHT AT GEAR INDICATION. REMOVED RT MAIN ACTUATOR AND INST ALLED REPAIRED ACTUATOR IAW MM 32-30-04 AND CESSNA ENGINEER LETTER DATED 1/10/08. FUNCTIONAL CHECK AND LEAK CHECKS GOOD . SERVICED AND SAFETIED GEAR PNEUMATIC BOTTLE. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008011400003 20080114 00003 CE 2008 1 14 DXTA200802760 1 20080110 A 2120 UNKNOWN RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP CABIN FUMES E DXTA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 07 815QS 258705 AIRCRAFT INTERIOR HAS A TOXIC FUME ODOR TO IT, CAUSING BREATHING DISCOMFORT AND EYE IRRITATION. CLEANED AIRCRAFT CARPET . VENTILATED AIRCRAFT. NO TOXIC FUME ODOR NOTED AT THIS TIME. 2 L 7 2 4F 4 F RT A3EU E6WE 2008011400005 20080114 00005 CE 2008 1 14 DXTA200802758 1 20080110 A 3260 UPLOCK SWITCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 671QS 5605071 UPON GEAR RETRACTION - GEAR UNLOCK LIGHT WOULD NOT EXTINGUISH. REMOVED AND REPLACED ALL THREE UP LOCK SWITCHES WITH NEW PER CESSNA 560XL MAINT. MANUAL CHAP 32-30-05 & 32-60-02. SYS GROUND OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008011400047 20080114 00047 CE 2008 1 14 DXTA200802748 1 20080105 A 3240 BRAKE ASSY BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 151QS RK422 UPON LANDING WITH NORMAL BRAKING ON DRY RUNWAY THE BRAKES PULSED HEAVILY CAUSING THE A/C TO SKID CONTINUALLY. INSPECTE D WHEELS, TIRES, BRAKES, PERFORMED HUB CAP INSPECTION, CHECKED BRAKE ACCUMULATOR. TAXIED AIRCRAFT, NO DEFECTS FOUND, WOR K DONE IAW MM 32-00-00. 2 H 7 2 4F 4 F RT A16SW E25EA 2008011400050 20080114 00050 NE 2008 1 14 0102183945 2 20080102 A 7321 430128308 FUEL CONTROL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ENGINE MALFUNCTIONED E RMXA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 05 117AP 4982 214 7144 LE45665 ENGINE FLAMEOUT DURING POST MAINTENANCE EVALUATION FLIGHT. SAME ENGINE HAD FLAMED OUT DURING 135 OPERATION (2) DAYS PR IOR. SUSPECT FUEL CONTROL. ENTIRE ENGINE ASSEMBLY IS BEING REMOVED AT THIS TIME. 1 G 7 2 3U 3 U H13EU E5NE10 2008011400051 20080114 00051 EU 2008 1 14 550001062008 1 20080106 A 2120 UNKNOWN AEROSP AS355 AS355F2 8680812 EU ALLSN 250C 250C20 03013 GL COCKPIT ODOR E QMLA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 912KY 5500 AS PILOT STARTED DESCENT, CREW NOTICED STRONG SMOKE ODOR IN COCKPIT; FIRST ODOR WAS "CHEMICAL ODOR" WHICH QUICKLY BECAME "ELECTRICAL" IN NATURE. AS CREW LOOKED OUTSIDE TO CHECK FOR AN OUTSIDE SOURCE, PILOT CHECKED INSTRUMENTS & CAUTION LIG HT PANEL WITH NOTHING NOTED. CREW ANNOUNCED THAT THEY COULD SEE SMOKE COMING FROM BEHIND INSTRUMENT PANEL ON LT SIDE OF ACFT, PILOT COULD DETECT BUT NOT SEE SMOKE. LANDING AND SHUTDOWN UNEVENTFUL, & SUBSEQUENT POST FLT INSPECTION REVEALED NO EVIDENT DAMAGE. MECHANIC COULD FIND NO EVIDENCE OF FIRE/SHORT CIRCUITING IN ELECTRICAL SYS, AND ON ACFT COULD NOT R ECREATE ANY ODOR, SMOKE, OR SYSTEM INDICATIONS OF FIRE. ACFT WAS RETURNED TO SERVICE. 1 G 7 2 3U 3 U H11EU E4CE 2008011400055 20080114 00055 SO 2008 1 14 RAIA00801003 1 20080102 A 3350 1317 LAMP EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHTS FAILED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 831HK 145232 PRE FLT NR 7973-IAD-EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008011600193 20080116 00193 NM 2008 1 16 SWAA080297 1 20080114 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER 23R CORRODED AT BS 436 TO BS 439. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008011600202 20080116 00202 NM 2008 1 16 SWAA080295 1 20080114 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008011600203 20080116 00203 NM 2008 1 16 SWAA080294 1 20080114 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008011600222 20080116 00222 NM 2008 1 16 SWAA080313 1 20080114 A 5315 141A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 760SW 27874 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 43 TO LBL 43. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600287 20080116 00287 NM 2008 1 16 SWAA080207 1 20080109 A 5311 6546526 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600336 20080116 00336 EA 2008 1 16 MASA200800012 1 20080107 A 3350 BATTERY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 504MJ 10066 ASH FLT 7371 SBN - CABIN EMERGENCY LIGHTS INOP. RECHARGED BATTERIES OFF OF GROUND POWER, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008011600353 20080116 00353 EU 2008 1 16 08FDEA00069 1 20080108 A 5320 FLOOR SUPPORT AIRBUS 310 A310203 3930313 EU ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS REPAIR LOCATED ON MAIN CABIN COURIER AREA FLOOR SUPPORT "T" CAP RT SIDE BETWEEN FR 14 TO 15A , NR 5 LONGERON FR OM CENTER -Y1959 HAS 4 REPAIR ANGLES BOTH THE INBD AND OUTBD SIDE HAVE 2 STACKED REPAIR ANGLES THE BOTTOM ANGLE MEASURES 12" LONG AND THE STACKED ANGLES ARE 7.9" AND 1 REPAIR SECTION MEASURES 17.1" LONG REPAIR NOT IAW SRM REQUIREMENTS. REM OVED PREVIOUSLY INSTALLED REPAIR AND INSTALLED CORRECT REPAIR IAW A310 SRM 51-71-50, FIG 201. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008011600382 20080116 00382 EA 2008 1 16 CHQA200800006 1 20080106 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS FAILED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 639BR 13656 13656 7313 GEE872507 IAH TO TUL - DURING CLIMB CREW RECEIVED A FLAP FAIL MESSAGE ON EICAS. THE AIRCRAFT THEN RETURNED TO FIELD AND LANDED WI THOUT INCIDENT. MAINTENANCE INSPECTED THE FLAP SYSTEM AND INTERROGATED THE FECU FOR FAULT CODES AND FOUND A FECU BIT FA IL MESSAGE ON THE FECU. AFTER REPLACING THE FECU, THE FLAP SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2008012200268 20080122 00268 EU 2008 1 22 08FDEA00116 1 20080112 A 5347 A53832020204 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 685FE 803 MAIN DECK CARGO COMPARTMENT FR 44 SEAT TRACK L-2 IS GOUGED ON SCALLOP .250" DEEP REMOVED AND REPLACED DAMAGED SEAT TRACK L-2 SECTION FROM FRAME 40 TO 44.5 IAW A300-600 SRM 51-72-10 AND SRM 53-15-16. 2 L 7 2 4F RT A35EU 2008012200269 20080122 00269 EU 2008 1 22 08FDEA00117 1 20080112 A 5347 A5381310100100 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 685FE 803 MAIN DECK CARGO COMPARTMENT FR 38.2 TO FR 39 SEAT TRACK R-2 HAS GOUGES AT SCALLOPS IN 1 AREA, .250" DEEP REMOVED AND R EPLACED R-2 SEAT TRACK ASSEMBLY FROM FR 38.2 TO 39 IAW A300-600 SRM 51-72-10 AND SRM 53-15-16. 2 L 7 2 4F RT A35EU 2008012200270 20080122 00270 WP 2008 1 22 08FDEA00118 1 20080113 A 5330 2024T3100CLA SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 568FE 47827 RT PRIMARY STATIC PORT CONTROLLED AREA HAS NUMERIOUS AREAS ABOVE AND BELOW WAVINESS TOLERANCES DUE TO DENTS AND 3 EACH F LUSH REPAIRS. REPAIRED AREA IAW SRM 53-20-00 FIG 9. PEFORMED WAVINESS CHECK ON WORK CARD 34C1501. CHECK GOOD. 2 L 7 3 4F RT A22WE 2008012200275 20080122 00275 NM 2008 1 22 08FDEA00104 1 20080110 A 5310 146N56001 CREASE BEAM BOEING 757 757200 1384950 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 CORROSION FOUND ON LT CREASE BEAM OUTBD CHORD AT STA 1190, S17. REPAIR CARRIED OUT PER EAR P337-24137-C0014 AND EAR P33 7-24137-C0093 REV.A. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008012200277 20080122 00277 NM 2008 1 22 08FDEA00106 1 20080111 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 616FE 48747 MAIN DECK SEAT TRACK AT STA 1831 - 2007, -X107, SEVERAL CORROSION FOUND NEAR CLIPNUTS, VIEW FROM WASTE TANK COMPARTMEN T. REPAIR CARRIED OUT AS PER E.A. 1-5340-117264, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008012200287 20080122 00287 NM 2008 1 22 08FDEA00134 1 20080115 A 5320 6517593201 INTERCOSTAL BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 MAIN CABIN FLOOR STRUCTURE, STA 303, LBL 50, INTERCOSTAL SUPPORT CRACKED REPAIRED INTERCOSTAL SUPPORT AT BS 303, LBL 50 . REF SRM 5I-40-02. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008012200306 20080122 00306 NM 2008 1 22 2008UALA00062 1 20080104 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 LEFT OVERWING EMERGENCY EXIT LIGHTS INOP, 3RD & 4TH FROM FWD. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012200330 20080122 00330 SO 2008 1 22 C2XA08TY004 1 20080109 A 3350 BA50933901 CHARGER EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27506 145206 OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGING BASE IAW EMB135 AMM 33-50-04 . OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008012200332 20080122 00332 SO 2008 1 22 C2XA08TY005 1 20080108 A 5350 FAIRING EMB 135 EMB135ER 3260203 SO FUSELAGE DAMAGED A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 27506 145206 LEFT WING TO FUSELAGE FAIRING 193 GROUND DAMAGE REPAIR. PERFORMED PLY RESTORATION TO EACH SKIN, ONE AT A TIME INCLUDIN G CORE REPLACEMENT. EXPOXY PRIME AND FINISH PAINT REPAIR. REPAIR ACCOMPLISHED IAW EC5350-01104. EMB IC2008-145/00110; ENGINEERING PROJECT 08-1016, EC5330-01768 (ASSOCIATED REPAIR TO SKIN AND STRUCTURE). 2 L 7 2 4F RT T00011AT 2008012200345 20080122 00345 EU 2008 1 22 TRAX200800068 1 20080104 A 5320 ANGLE AEROSP ATR72 ATR72 EU RT MLG WW CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 RIGHT WHEEL WELL (MAIN) 2 ANGLES CRACKED AT FR 27 STR RT 17. 2 H 7 2 4T RT 2008012200349 20080122 00349 EU 2008 1 22 TRAX200800069 1 20080104 A 5320 BRACKET AEROSP ATR72 ATR72 EU FUSELAGE BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 OMEGA BRACKET & NUT PLATE BROKEN AT FR 39 BETWEEN STR LT 13 & 14. 2 H 7 2 4T RT 2008012200358 20080122 00358 EU 2008 1 22 TRAX200800078 1 20080110 A 5320 ANGLE AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 ANGLE CRACKED AT FR 26 STRINGER 4L (INTERNAL FUSELAGE). ANGLE AT FR 26 STR 4 LT REMOVED AS PER SRM 51-25-01. LT SHEAR WEB BTW FR 25 & 27 REMOVED IAW AMM 20-21-12. ANGLE AT FR 26 STR 4 LT INSTALLED AS PER SRM 51-25-01. LT SHEAR WEB RE-I NSTALLED IAW TECH INSTRUCTION 57-01-91. 2 H 7 2 4T RT 2008012200371 20080122 00371 2008 1 22 2008UALA00058 4 20080103 A 2565 D31865105 SLIDE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE OVERWING EXIT DELAMINATED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 831UA 1291 LEFT, OVERWING EXIT, SLIDE PACK, IS DELAMINATING IN TWO AREAS. DELAMINATION - REPLACED SLIDE ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012200375 20080122 00375 NM 2008 1 22 KCSA081019 1 20080115 A 5311 FRAME BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 CORROSION ON UPPER CHORD OF BS 800 CIRCUMFERENTIAL FRAME AT LBL-33 TO LBL-43. 2 L 7 4 4F RT A20WE 2008012200377 20080122 00377 EA 2008 1 22 TRAX200800085 1 20080111 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 683BR 7692 CRACK ON LT FRAME 640 BETWEEN STR 7L AND 8L. 2 L 7 2 4F RT A21EA 2008012300009 20080123 00009 EA 2008 1 23 SWIA200819069 1 20080117 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 957SW 7829 CENTER EMERGENCY EXIT LIGHT IS INOP, FLIGHT NR 6701. REPLACED LAMP WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008012300024 20080123 00024 2008 1 23 2008UALA00029 4 20080101 A 2565 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE UNSECURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 408UA 457 CREW REPORT: SLIDE PACK 2R HAS FALLEN OFF. RESECURED SLIDE COVER, NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012300026 20080123 00026 NM 2008 1 23 2008UALA00031 1 20080101 A 3350 GE1810 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN INOPERATIVE A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 813UA 858 EPSU EXT LOAD EMERGENCY RIGHT MESSAGE ON EMERGENCY LIGHT TEST PANEL. FWD LAMP RIGHT WING AFT OVERWING EMERGENCY LIGHT A SSY IN OUT. REPLACED RIGHT OVERWING EMERGENCY EXIT LIGHT, LAMPS OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012300032 20080123 00032 NM 2008 1 23 DL76G080012 1 20080107 A 5330 146T35313 SKIN BOEING 767 767332 1382001 NM FS 1346-1360 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1608 30573 BLENDS OF GOUGED SKIN BETWEEN STA 1346-1360, S 27R - 31R. 2 L 7 2 4F RT A1NM 2008012300042 20080123 00042 EA 2008 1 23 SWIA200819063 1 20080113 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA LAVATORY ILLUMINATED A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 915EV 7754 RECEIVED SMOKE TOILET CAUTION MESSAGE AFTER TAKEOFF, FLIGHT NR 3843. INSPECTED AND OPERATED BOTH PACKS WITH NO DISCREPE NCIES NOTED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008012300055 20080123 00055 NM 2008 1 23 DLM88080018 1 20080108 A 2120 UNKNOWN DOUG MD88 MD88 3023688 NM PWA 4060 PW4060 52119 NE CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 997DL 53364 724741 ELECTRIC ODOR IN OVERHEAD LIGHTS AROUND ROW 38. RAN APU TURNED. ON CABIN LIGHTS. MADE SEVERAL PASSES THRU CABIN. CHE CKED LOWER BB. NO SMOKE OR ODOR SOURCE NOTED. 2 L 7 2 4F 4 F RT A6WE E24NE 2008012300059 20080123 00059 NM 2008 1 23 DL764080025 1 20080109 A 3350 RELAY BOEING 767 767432ER 1385134 NM EMERGENCY LIGHTS MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 826MH 29697 AT DEPARTURE EMERGENCY LIGHT WOULD NOT TURN OFF. REPLACED BATTERY PACK M1208 AND M796. SYSTEM WORKED FOR A SHORT TIME AND THEN FAILED AGAIN. TROUBLESHOOTING IN PROGRESS. REPLACED RELAY K10361 ALL EMERGENCY LIGHTS CK NORMAL. 2 L 7 2 4F RT A1NM 2008012200014 20080122 00014 EA 2008 1 22 TRAX200800030 1 20080104 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 904EV 7628 AFT CARGO DOOR SUPPORT ATTACH ANGLE CRACKED AT AFT PRESSURE BULKHEAD. REMOVED AND REPLACED ATTACH ANGLE ON AFT CARGO DO OR SUPPORT AT AFT PRESSURE BULKHEAD IAW CRJ 200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 2008012200074 20080122 00074 NM 2008 1 22 KCSA081006 1 20080109 A 3350 LIGHT BOEING 747 7472B4B 138481B NM CABIN FAILED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 LEFT CEILING UPPER DECK EMERGENCY LIGHT COMES ON FOR APPROXIMATELY 1 TO 2 SECONDS. 2 L 7 4 4F RT A20WE 2008012200079 20080122 00079 EA 2008 1 22 TRAX200800044 1 20080105 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 904EV 7628 FS 280 FWD FLOOR ANGLE IS CORRODED. 2 L 7 2 4F RT A21EA 2008012200091 20080122 00091 NM 2008 1 22 KCSA081007 1 20080110 A 5347 SEAT TRACK BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 MAIN DECK SEAT TRACK INBOARD FLANGE IS CORRODED AT STA 420 TO 460, LBL 63. 2 L 7 4 4F RT A20WE 2008012200121 20080122 00121 EA 2008 1 22 TRAX200800022 1 20080102 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 AAR - CORROSION ON FLOOR SUPPORT SILL, JUST FWD OF SERVICE DOOR AT FS 349.00. CLEANED CORROSION ON FLOOR SUPPORT SILL, JUST FWD OF SERVICE DOOR AT FS 310.00 IAW CRJ-200 SRM 51-21-06. FOUND SURFACE CORROSION ONLY, NO MATERIAL LOSS. OK TO ALODINE, PRIME, AND PAINT. ALODINED, PRIMED, AND PAINTED FLOOR SUPPORT SILL, JUST FWD OF SERVICE DOOR AT FS 310.00 IAW CRJ-200 SRM 51-21-06. SUPPLEMENTAL SDR CLOSED 1/10/08. 2 L 7 2 4F RT A21EA 2008012200141 20080122 00141 EA 2008 1 22 N6WA0080103 1 20080110 A 3610 2873300 GASKET CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE SHUTOFF VALVE LEAKING A N6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 156GJ 10227 5387-STL-LT ENGINE FIRE MASTER WARNING. FOUND BLOWN GASKET ON PRESSURE REGULATING SHUTOFF VALVE. REPLACED GASKET, LEAK C HECK GOOD. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008012200158 20080122 00158 2008 1 22 WGEA200800002 4 20080109 A 3414 INDICATION SYS ECLIPS EA500 ECLIPSEEA500 3350000 SW PWC PW615 PW615FA 52282 NE AIRSPEED SPLIT E WGEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 158DJ 000074 MX LOG PG NR1404 DISC NR 1 AND WO NR1096 AIRSPEED DISAGREE CAS MESSAGE ON TAKEOFF ROLL. ABORTED TAKEOFF. SUPPLEMENTAL IN FORMATION- PERFORMED FLIGHT ENVIRONMENT DATA ADJUSTMENT TEST FOR NR 1, NR 2 ADC'S AND LT AND RT PITOT/AOA PROBES IAW MM 31-10-00. ALL TESTS CHECK GOOD. NO DEFECTS NOTED. NO MORE THAN 1 KNOT SPLIT BETWEEN NR 1, NR 2, AIRSPEEDS. SUSPECT PREVI OUS (AIRSPEED DISAGREE) TO BE CAUSED BY MOISTURE. 1 L 7 2 4J 4 F RT A00002AC E00073EN 2008012200178 20080122 00178 EA 2008 1 22 TRAX200800060 1 20080108 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 834AS 7254 F/A FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 2008011700006 20080117 00006 EA 2008 1 17 SWIA200819028 1 20080101 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 442SW 7609 FLT 3941, REAR MOST CEILING LEVEL EMERGENCY FLOODLIGHT IS NOT WORKING. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2008011700031 20080117 00031 SO 2008 1 17 SWIA200819032 1 20080102 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 393SW 120330 RIGHT WING FUEL PANEL ACCESS HAS A CRACK ON STRINGER 8 BETWEEN FRAMES 8 AND 9. REPAIRED STRINGER IAW SRM 57-20-03. 2 L 7 2 4T RT A31SO 2008011700032 20080117 00032 EA 2008 1 17 SWIA200819033 1 20080104 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 929SW 7703 TWO EMERGENCY LIGHT BULBS ARE INOP NEXT TO GALLEY DOOR. RELAMPED GALLEY EMERGENCY LIGHTS. OPS CK GOOD. 2 L 7 2 4F RT A21EA 2008011700043 20080117 00043 NM 2008 1 17 QXEA200800006 1 20080102 A 3080 PROBE BOMBDR DHC8 DHC8402 1390042 NM ICE DETECTOR MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 412QX 4059 PDX - FLIGHT 2364 - ICE DETECTOR FAIL CAUTION. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANC E PLACED ON MEL 30-80-2. AIRCRAFT RETURNED TO SERVICE. REPLACED NR 2 ICE DETECTOR PROBE. 2 H 7 2 4T RT A13NM 2008011700045 20080117 00045 EA 2008 1 17 QXEA200800004 1 20080102 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE CABIN ODOR A QXEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 614QX 10049 PDX - FLIGHT 2591 - GOING THROUGH 8000 FEET, FLIGHT ATTENDANT CALLED TO SAY THAT THERE WAS AN EXHAUST ODOR IN THE BACK O F THE AIRCRAFT. STRONGEST AFTER TAKEOFF, BUT DISSIPATED BY THE TIME SHE CALLED. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE PERFORMED A INSPECTION OF THE APU AND ENGINE GROUND RUN, WITH NO DEFECTS NOTED. AIR CRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008011700046 20080117 00046 NM 2008 1 17 QXEA200800007 1 20080103 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM FALSE ACTIVATION A QXEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 407QX 4049 SEA - FLIGHT 2483 - ON POWER UP, OBSERVED NR 3 HYDRAULIC PUMP CAUTION LIGHT ON. RETURNED TO THE GATE. MAINTENANCE CYCL ED THE PARKING BRAKE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008011800062 20080118 00062 SO 2008 1 18 SWIA200819038 1 20080108 A 2597 CONNECTOR EMB 120 EMB120ER 3260203 SO COFFEEMAKER ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 579SW 120347 ELECTRICAL BURNING ODOR IN CABIN.REPLACED FORWARD HOT JUG PLUG. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008012200007 20080122 00007 NM 2008 1 22 KCSA081005 1 20080108 A 5347 SEAT TRACK BOEING 747 747122 1384872 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 716CK 19753 FORWARD BILGE SEAT TRACK IS CRACKED BETWEEN STA 540 & 560, RBL 45. 2 L 7 4 4F RT A20WE 2008012200015 20080122 00015 EU 2008 1 22 TRAX200800037 1 20080104 A 5313 STRINGER AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 STR LEFT 17 CORRODED BETWEEN FR 38-39. CORROSION REMOVED ON STRG L/H 17 BTW FR 38 & 39 AS PER SRM 51-21-42. 2 H 7 2 4T RT 2008012200021 20080122 00021 2008 1 22 WGEA200800006 4 20080117 A 3414 INDICATOR ECLIPS EA500 ECLIPSEEA500 3350000 SW AIRSPEED MALFUNCTIONED E WGEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 142DJ 000056 AIRSPEED DISAGREE AT 45 KTS. AIRSPEED CHECK AT 25 KTS ON T/O ROLL WAS OK, WIND 160/9 LIGHT RAIN. USED RUNWAY 11. SUPPLEM ENTAL INFORMATION. INSPECTED PITOT/STATIC DRAIN LINES, NO WATER FOUND. PERFORMED PITOT STATIC LEAK CHECK AND PITOT/STAT IC PROBE VERIFICATION TEST IAW MM 31-10-00 ON BOTH ADC 1 AND ADC 2 SYSTEMS SIMULTANEOUSLY. ALL ALTITUDES AND AIRSPEEDS C HECKED GOOD. NO AIRSPEED DISAGREE CAS MESSAGE. NO DEFECTS NOTED. 1 L 7 2 4J RT A00002AC 2008012200022 20080122 00022 SO 2008 1 22 GUUA01070801 1 20080107 A 3350 25139915 SIGN EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE EMERGENCY LIGHTS MISSING A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 29 280AS 120231 FLIGHT: 1601 MIA/FLL ILLUMINATED EXIT SIGN MISSING BY SEAT 8F. INSTALLED NEW EXIT SIGN. 2 L 7 2 4T 4 T RT A31SO E20NE 2008012200035 20080122 00035 NM 2008 1 22 USAA920080132 1 20080102 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK, CRACKED STRINGER, BS 1720, S29R. REPAIRED STRINGER, BS 1720, S29R IAW B757 SRM 53-00-03 REPAIR 1. 2 L 7 2 4F RT A2NM 2008012200039 20080122 00039 NM 2008 1 22 USAA920080135 1 20080101 A 5347 SEAT TRACK BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON SEAT TRACK, BS 1320, RBL 26, WL 208. REPAIRED SEAT TRACK, BS 1320 , RBL 26, WL 208 IAW B757 SRM 53-00-052-2R. 2 L 7 2 4F RT A2NM 2008012200042 20080122 00042 2008 1 22 AMTA200800011 4 20080109 A 2310 NONE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211524B4 54555 NE HF RADIO NONE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 520AT 27976 UNABLE TO TRANSMIT OR RECEIVE ON LT HF RADIO. CALLED SFO ON 5574, TRANSMIT AND RECEIVE 5X5. NO FAULTS FOUND RECEIVER, OK FOR SERVICE, OPS CHECK NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008012200060 20080122 00060 NE 2008 1 22 GUUA01030801 2 20080103 A 7313 36100044 FUEL NOZZLE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE ENGINE LEAKING A GUUA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 282AS 120226 FLIGHT: 9227, DURING FLIGHT COCKPIT AND CABIN HAS STRONG FUEL ODOR. REPLACED APU FUEL NOZZLE AT 11 O CLOCK POSITION. 2 L 7 2 4T 4 T RT A31SO E20NE 2008012200063 20080122 00063 NM 2008 1 22 XV6A200800002 1 20080110 A 3260 BULB DORNER DO32 DO328300 NM PWA 306 PW306B NE RT MLG INDICATOR BURNED OUT E XV6A O OTHER P NO WARNING INDICATION AP APPROACH 1 WP 19 328DA 3171 RT MAIN LANDING GEAR DOWN INDICATION INOP. 2 H 7 2 4T 4 F RT A55NM E35NE 2008012200067 20080122 00067 WP 2008 1 22 AMTA200800010 1 20080107 A 3397 WIRE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE EMERGENCY LIGHTS SHORTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 162AT 1220 EMERGENCY LIGHT PATHWAY LIGHT AT FWD GALLEY AND RT FWD CABIN INOPERATIVE. DRIED OUT WET WIRES AND PLUGS BY A2 LAVATORY. OPS CHECK GOOD. (K) 2 L 7 3 4F 4 F A23WE E12EU 2008012200073 20080122 00073 CE 2008 1 22 DXTA200802762 1 20080111 A 2731 INDICATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ELEVATOR TRIM UNKNOWN E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 631QS 5605131 EXCESSIVE BACK PRESSURE (MORE THAN NORMAL) REQUIRED FOR ROTATION. REMOVED AND REPLACED ELEVATOR TRIM WHEEL POINTER IAW MM 27-32-01. CHECKED ELEVATOR TRIM RIGGING PER CE-5460XL M/M 27-31-00.CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008012200075 20080122 00075 NM 2008 1 22 DXTA200802763 1 20080112 A 3260 PROXIMITY SENSOR AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 265QS 165 AFTER TAKEOFF AND GEAR HANDLE SELECTED TO THE GEAR RETRACTION POSITION. NOSE GEAR RETRACTION MOVEMENT WAS FELT AND HEAR D. 2 RED MAIN GEAR LIGHTS (NO NOSE LIGHT) ALONG WITH A RED FLASHING HANDLE LIGHT OCCURRED. REMOVED AND REPLACED LT & R T MLG PROX SWITCHES AND INSTALLED NEW LT & RT MLG PROX SWITCHES PER MM 32-311 AND ACCOMPLISHED OPS AND LEAK CHECKS PER M M 32-300 WITH ALL OPS NORMAL NO FURTHER DEFECTS NOTED 2 L 7 2 4F 4 F RT A50NM E44NE 2008011600364 20080116 00364 EU 2008 1 16 MALA080004 1 20080106 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 MULTIPLE DENTS IN CARGO DOOR REQUIRES MAPPING AND EVALUATION. REPAIRED IAW MAL EO NR S52098. 2 L 7 2 4T RT A52EU 2008011600388 20080116 00388 EU 2008 1 16 08FDEA00077 1 20080109 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 56 LT BETWEEN FRAMES 68 TO 70 HAS 1 REPAIR SECTION MEASURIN G 16" LONG AND 2EA REPAIR SPLICES MEASURING 8" LONG REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTAL LED CORRECT STRINGER SPLICE REPAIR IAW A310 SRM 53-10-14,FIG 201. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008011600393 20080116 00393 EU 2008 1 16 08FDEA00078 1 20080109 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 56 LT BETWEEN FRAMES 62 TO 63 HAS 1EA REPAIR SPLICE MEASURIN G 14.1" LONG AND 1 REPAIR FILLER MEASURING 16.6" LONG AND 1 REPAIR SECTION FROM FRAME 55/58 TO 63 MEASURES 88.5" LONG RE PAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT STRINGER SPLICE REPAIR IAW A310 SRM 53-10- 14, FIG 201A. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION 2 L 7 2 4F RT A35EU 2008011700008 20080117 00008 EA 2008 1 17 SWIA200819030 1 20080103 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 668CA 10162 FLT 4052 - EMERGENCY POD LIGHT IS INOP. RELAMPED POD LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008011700010 20080117 00010 EU 2008 1 17 DHLA200800003 1 20080106 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 365DH 149 LOWER FORWARD CARGO DOOR FUSELAGE LOWER FORWARD FRAME IS SCUFFED. DEFERRED IAW GMM 3.5 CAT I & LETTER REF. 942-057506/ 014/2008 ACCEPTABLE FOR 10 F.C. PLACARD INSTALLED. 2 L 7 2 4F RT A35EU 2008011700027 20080117 00027 NM 2008 1 17 08FDEA00014 1 20080103 A 5230 54C54672D01 CYLINDER BOEING 727 727200 138407E NM CARGO DOOR LEAKING A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 483FE 21465 ON CLIMBOUT, "MCD ARM" LIGHT AND "CARGO DOOR IN-TRANSIT" LIGHT ILLUMINATED, REPEAT WRITE UP.PRESSURIZATION WAS NORMAL T HROUGHOUT FLIGHT. AT TIME OF LIGHT ILLUMINATION, PSID WAS 6. APPX ALTITUDE WAS 15,000. R & R MCD AFT LATCH CYLINDER PER 52-34-021-4. BLED AND OPS CHECKED NORMAL. RAN DOOR SEVERAL TIMES WITH PRESS IND. PLUMBED IN LINE AT PORT 2. PER D RAWING. NO LEAK DOWN NOTED. RESTORED A/C TO NORMAL. PRESSURIZED A/C TO CHECK FOR MIGRATION OF LOCK BAR. PRESS TO 5.0 D FOR APPROX 25 MIN. WITH NO LOCK BAR MOVEMENT NOTED. NO WARNING LIGHTS ILLUMINATED 2 L 7 3 4F RT A3WE 2008011800009 20080118 00009 NM 2008 1 18 TSAA0853003 1 20080108 A 5312 65458001000 BULKHEAD BOEING 737 737282 13844AT NM BS 1156 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 WHILE PERFORMING ECO 1822 PART I (REFERENCE AD 93-08-08 AND AD 90-06-02) A CRACK WAS DISCOVERED ON THE LT BULKHEAD BS 11 56 ALONG THE LAST ROW OF RIVETS APPROX WL 272-275. REPAIRED CRACK IN ACCORDANCE WITH ECO 1822 PART II (S/B 737-53-1-86 R3). 2 L 7 2 4F RT A16WE 2008011800013 20080118 00013 NM 2008 1 18 UIEA200800006 1 20080106 A 2910 9216787 O-RING BOEING 747 747228F 1384895 NM ZONE 200 LEAKING A UIEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 809MC 20887 APPROX 1 HOUR 15 MIN AFTER T/O NR 1 ENGINE OIL QTY IND ZERO, TEMP AND PRESS NORMAL ABOUT 2 HOURS 30 MIN AFTER T/O PRESSU RE BEGAN VERY SLOW DROP WITH SLOW FLUX 5 PSI DURING DESCENT WITH ENGINE AT IDLE OIL PRESSURE LIGHT ILLUMINATED OCCASIONA LLY BUT PRESS NEVER WENT BELOW 12 PSI. ENGINE REMAINED RUNNING AT ALL TIMES. PERFORMED LEAK CHECK INSPECTION ON ENGINE AND FOUND OIL LEAKING THROUGH DRAIN MAST ONLY, REPLENISHED THE OIL AND DRY CYCLED AND IDLE RUN PERFORMED IAW 71-00-00. LEAK CONFIRMED TO ENGINE HYD PUMP PAD DRAIN. HYD PUMP SHAFT O-RING REPLACED IAW 29-11-05 AND PERFORMED ENGINE RUN, NO F URTHER LEAKS EVIDENT. 2 L 7 4 4F RT A20WE 2008011800063 20080118 00063 EA 2008 1 18 SWIA200819039 1 20080113 A 2730 PCU CNDAIR CL600 CL6002B19 1900309 EA ELEVATOR INOPERATIVE A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 912SW 7595 FLT 6500 - RIGHT ELEVATOR DOES NOT MOVE WITH HYDRAULIC SYSTEM 3 PRESSURIZED. REPLACED RIGHT NR 3 HYD ELEVATOR PCU IAW 2 7-33-01. OPS CHECK GOOD.PN 27600-3, SN OFF 8783. 2 L 7 2 4F RT A21EA 2008011800125 20080118 00125 2008 1 18 HALA0800017 4 20080116 A 3420 H150AKM1 INDICATOR BOEING 767 76733A 1385209 NM STBY ATTITUDE PRECESSES A HALA O OTHER O OTHER CR CRUISE 1 WP 13 580HA 28140 ETOPS SIGNIFICANT SYSTEM, STBY ATTITUDE INDICATOR PRECESSING. REPLACED STANDBY ATTITUDE IND, OPS NORMAL. 2 L 7 2 4F RT A1NM 2008011800127 20080118 00127 EA 2008 1 18 CHQA200800008 1 20080113 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS MALFUNCTIONED A CHQA L ABORTED APPROACH O OTHER AP APPROACH 1 GL 11 469SM 7650 GEE873397 RDU TO CLE - ON DOWNWIND TO LAND AT CLE, FLAPS WERE SELECTED TO 8 AND CREW RECEIVED A FLAP FAIL MESSAGE WITH THE FLAPS F AILED AT ZERO. THE CREW RAN THE APPROPRIATE QRH CHECK LISTS AND LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE FECU AND MDC FOR FAULT CODES, BUT THERE WERE NONE PRESENT. AFTER RESETTING THE FLAP SYSTEM CIRCUIT BREAKERS, THE FLAP S YSTEM OPERATED NORMALLY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008011800130 20080118 00130 NM 2008 1 18 QXEA200800031 1 20080115 A 5210 4100S003 CHECK VALVE BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 400QX 4030 MSO - FLIGHT 2347 (MSO-SEA) - AIRCRAFT WILL NO PRESSURIZE IN AUTO OR MANUAL MODES. CFR CALLED BY CONTROL TOWER. AIRCRA FT RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. AIRCRAFT FERRIED TO PDX FOR REPAIRS. IN PDX REPLACED T HE MAIN CABIN DOOR SEAL CHECK VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008011800136 20080118 00136 NM 2008 1 18 NWAA080135515 1 20080114 A 2497 WIRE HARNESS BOEING 757 757251 1384970 NM LAVATORY DAMAGED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 515US 23203 DURING FLIGHT, ATTENDANT REPORTED ODOR OF BURNING WIRE OR SMOKE AT LAV 3L. DIVERTED AIRCRAFT TO MCO AND LANDING WAS UNEV ENTFUL. MAINTENANCE FOUND EXPOSED WIRES IN WIRE BUNDLE UNDER LAV 3L. STILL WORKING WIRING PROBLEM. 2 L 7 2 4F RT A2NM 2008011800138 20080118 00138 NM 2008 1 18 NWAA080153139 1 20080105 A 5320 SILL AIRBUS A319 A319114 3930350 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 339NB 1709 DURING "H" CHECK, FOUND CORROSION ON LT AFT PASSENGER DOOR SILL AT FRAME 66. REPAIRED PER EA 31-211442. 2 L 7 2 4F RT A28NM 2008012200010 20080122 00010 EA 2008 1 22 TRAX200800029 1 20080104 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 904EV 7628 AFT PRESSURE BULKHEAD IS CRACKED AT LINTEL FITTING. REPAIRED IAW SRM. 2 L 7 2 4F RT A21EA 2008012200036 20080122 00036 NM 2008 1 22 USAA920080133 1 20080103 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK, CORROSION ON STRINGER, BS 440, S29R. REPAIRED STRINGER, BS 440, S29R IAW B757 SRM 53-00- 03. 2 L 7 2 4F RT A2NM 2008012200057 20080122 00057 SW 2008 1 22 WGEA200800004 1 20080114 A 2621 FX002002 CARTRIDGE ECLIPS EA500 ECLIPSEEA500 3350000 SW PWC PW615 PW615FA 52282 NE LT EXTINGUISHER LEAKING E WGEA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 27 147DJ 70 000059 LT ENGINE FIRE EXTINGUISHER CARTRIDGE PRESSURE IN RED BAND. EVIDENCE OF LEAKAGE INSIDE COWLINGS AND ON NUMEROUS PARTS OF THE ENGINE. SUPPLEMENTAL INFORMATION- REMOVED AND REPLACED LT ENGINE PYLON FIRE EXTINGUISHER CARTRIDGE IAW MM 26-20-00 REV NR 11 FIRE SUPPRESSION AGENT CLEANUP PROCEDURES AND EMM 05-50-00 AND 71-00-00. 1 L 7 2 4J 4 F RT A00002AC E00073EN 2008012200068 20080122 00068 CE 2008 1 22 DXTA200802770 1 20080116 A 3260 INDICATION SYS RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 893QS 258393 WITH GEAR SELECTED UP AFTER T/O ALL 3 GEAR INDICATED UNSAFE WITH RED LIGHTS. JACKED AIRCRAFT CYCLED NOSE ONLY THEN UNPI NNED MAINS COMPLETED 2 MORE COMPLETE CYCLES WITH NO FAULTS. WORK COMPLETED IAW MM 29-10-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2008012200082 20080122 00082 EA 2008 1 22 TRAX200800046 1 20080105 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 904EV 7628 FS 349 FRAME IS CORRODED AT BL 0. REPAIRED IAW SRM. 2 L 7 2 4F RT A21EA 2008012200084 20080122 00084 CE 2008 1 22 DXTA200802768 1 20080114 A 3230 MECHANISM CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE MLG UPLOCK STICKING E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 820QS 5600650 RETRACTED GEAR ON T/O, 3 GREEN LIGHTS WENT OUT, RED UNLOCK LIGHT STAYED ON. TROUBLESHOT GEAR WARNING INDICATION, FOUND THAT RT MLG UPLOCK LATCHING MECHANISM IS STICKING PER CITATION 560 MM 32-30-00. CLEANED AND LUBED UPLOCK LATCHING MECHA NISM AND ROLLER. WORK DONE IAW CITATION 560 MM CH: 32-31-05. OPERATIONAL CHECK SATISFACTORY. 2 L 7 2 4F 4 F RT A22CE E00053EN 2008012200094 20080122 00094 EA 2008 1 22 TRAX200800050 1 20080102 A 5230 BEAM CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 AAR - CARGO DOOR LINTEL BEAM LWR AFT ATTACHMENT CLIP CRACKED. 2 L 7 2 4F RT A21EA 2008012200108 20080122 00108 EU 2008 1 22 TRAX200800031 1 20080104 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 RIGHT I/B SEAT TRACK BETWEEN FR 13 TO FR 17 FOUND CORRODED. RIGHT INBOARD SEAT TRACK BETWEEN FR 13 TO 17 CORROSION REMO VED IAW SRM 51-21-42. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REP AIR ACCOMPLISHED IN ACCORDANCE WITH SRM 53-00-00 FIG 304. MATERIAL THICKNESS: 0.090 MATERIAL REMOVED: 0.010 WITHIN LIMI TS AS PER SRM: 53-00-00 FIG 304. SUPPLEMENTAL SDR CLOSED 1/10/08. 2 H 7 2 4T RT 2008012200111 20080122 00111 EU 2008 1 22 TRAX200800034 1 20080104 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 RIGHT SEAT TRACK FOUND CORRODED BETWEEN FR 36-38. CORROSION REMOVED ON FLOORBEAM AT FR 36 AS PER SRM 51-21-42 & WITHIN LIMITS AS PER SRM 53-00-00 FIG 304. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, AP PENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH 53-00-00 FIG 304. MATERIAL THICKNESS: 0.063, MATERIAL REMOVED: 0.004 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 304. SUPPLEMENTAL SDR CLOSED 1/10/08. 2 H 7 2 4T RT 2008012200116 20080122 00116 EU 2008 1 22 TRAX200800036 1 20080104 A 5347 SEAT TRACK AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 CORROSION FOUND ON LEFT SEAT TRACK BETWEEN FR 36 TO FR 39. CORROSION ON LEFT SEAT TRACK BETWEEN FR 36 TO 39 REMOVED IAW SRM 51-21-42. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACC OMPLISHED IN ACCORDANCE WITH SRM 53-00-00 FIG 304. MATERIAL THICKNESS: 0.090, MATERIAL REMOVED: 0.004 WITHIN LIMITS AS PER SRM: 53-00-00 FIG 304. SUPPLEMENTAL SDR CLOSED 1/10/08. 2 H 7 2 4T RT 2008012200117 20080122 00117 EU 2008 1 22 TRAX200800039 1 20080104 A 5720 STRUCTURE AEROSP ATR72 ATR72 EU RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 RIGHT WING BOX AT FR 28A FOUND CRACKED. FR 28A OF RIGHT WING BOX REPLACED IAW SRM 51-25-01. REPAIR DETERMINED NOT TO B E A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01. SUPPLEMENTAL SDR CLOSED 1/10/08. 2 H 7 2 4T RT 2008012200137 20080122 00137 CE 2008 1 22 AMWA89426BC 1 20080104 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 162ZV 16409 91 UE162 BATTERY CHARGE ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED BATTERY AND CLEARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2008012200150 20080122 00150 NM 2008 1 22 2008UALA00090 1 20080106 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 EXTERIOR SKIN IS DENTED AT 7.25 INCHES AFT OF STA 1006 BELOW STR 12L. REMOVED EXISTING SKIN PANEL. FABRICATED AND INSTA LLED REPLACEMENT SKIN. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012200152 20080122 00152 NM 2008 1 22 IU6R229469 1 20080103 A 2721 69579073 SPRING BOEING BOEING 737 737 UTILSYS NM CENTERING UNIT BROKEN B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 9539 9539 3806 RUDDER CENTERING UNIT SPRING ASSY BROKEN. 2 L 7 2 4F RT A16WE 2008012200159 20080122 00159 NM 2008 1 22 2008UALA00100 1 20080107 A 3350 1619 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 382UA 24657 LEFT SIDE FUSELAGE AFT LOWER BODY FAIRING EMERGENCY LIGHT INOPERATIVE. RELAMPED. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012200168 20080122 00168 EA 2008 1 22 TRAX200800056 1 20080107 A 3397 LF47B22 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGNECY LIGHTS DAMAGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 883AS 7504 LEFT AFT MOST EXTERNAL EMERGENCY LIGHT INOP. EXTERIOR EMERGENCY LIGHTS - ONE OF TWO REARWARD ON EACH SIDE. FOUND WIRE (BETWEEN LIGHT AND TB107) BROKEN. REPAIRED WIRE IAW CRJ 200 ELECTRICAL/ELECTRONICS STANDARD PRACTICES MANUAL. OPS CK GOOD. 2 L 7 2 4F RT A21EA 2008012200170 20080122 00170 EA 2008 1 22 TRAX200800057 1 20080107 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 684BR 7708 WHITE EMERGENCY EXIT LIGHT BY PAX DOOR INOP. 2 L 7 2 4F RT A21EA 2008012200183 20080122 00183 SO 2008 1 22 UG8A08P011002 1 20080110 A 2910 1159HL5023623R2 LINE GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE BS 820 BENT E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 661GA 561 HYDRAULIC LINE IN TAIL COMPARTMENT JUST AFT OF LT ELT IS BENT/DENTED. 2 L 7 2 4F 4 F RT A12EA E00057EN 2008012200186 20080122 00186 SO 2008 1 22 UG8A08P011001 1 20080110 A 5540 1159B2160515 TORQUE TUBE GULSTM GULSTM GV GULFSTREAMGV 3980116 SO RROYCE BR700 BR700710A110 NE RUDDER CORRODED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 661GA 561 561 RUDDER TORQUE TUBE INNER AND OUTER TUBES ARE CORRODED AND PITTED. 2 L 7 2 4F 4 F RT A12EA E00057EN 2008012200202 20080122 00202 EA 2008 1 22 TRAX200800064 1 20080109 A 5534 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 317CA 10055 RIGHT VERTICAL STAB DRAG ANGLE CRACKED AT AFT END (MARKED). PERFORMED EDDY CURRENT INSPECTION OF RIGHT HAND VERTICAL ST AB DRAG ANGLE IAW NDTM 51-20-006 TO LOCATE END OF CRACK. END OF CRACK IS MARKED. INSTALLED AND SEALED RT DRAG ANGLE PE R REO 670-55-31-018. 2 L 7 2 4F RT A21EA 2008012200203 20080122 00203 EA 2008 1 22 TRAX200800065 1 20080109 A 5534 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 317CA 10055 LEFT VERTICAL STAB DRAG ANGLE CRACKED AT AFT END (MARKED). PERFORMED EDDY CURRENT INSPECTION OF LT VERTICAL STAB DRAG ANGLE IAW NDTM 51-20-006 TO LOCATE END OF CRACK. END OF CRACK IS MARKED. INSTALLED AND SEALED L/H DRAG ANGLE PER REO 67 0-55-31-018. 2 L 7 2 4F RT A21EA 2008012200204 20080122 00204 EA 2008 1 22 TRAX200800066 1 20080110 A 5210 INTERCOSTAL CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 317CA 10055 PAX DOOR INTERCOSTAL 318 CRACKED. REMOVED AND REPLACED 318 INTERCOSTAL IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008012200205 20080122 00205 NM 2008 1 22 08FDEA00123 1 20080114 A 5320 STRIP BOEING 757 7572B7 1384964 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 AFT CARGO DOOR SURROUND BETWEEN BS 1380-1440, AT RBL 24, NUT PLATE STRIP FOR DOOR SCUFF PLATE HAS SEVERAL AREAS OF CORRO SION. REMOVED NUT PLATES AND FASTENERS FOR ACCESS TO CORROSION ON STRIP IAW SRM 51-40-02. CHECKED AND VERIFIED LIMITS UPON REMOVAL OF STRIP, FOUND ENTIRE LENGTH TO BE EXFOLIATED. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15. FABRICATED NE W NUT PLATE STRIP IAW DWG. 146N8522. TREATED AND PRIMED IAW SRM 51-20-01. APPLIED TOP COAT IAW AMM 51-20-00-7. IN STALLED NUT PLATES IAW SRM 51-40-02. INSTALLED NUT PLATE STRIP IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008012200209 20080122 00209 EU 2008 1 22 08FDEA00112 1 20080111 A 5311 A5387006820000 FRAME AIRBUS 310 A310203 3930313 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 HOLE NR 5 FRAME 44 LT HAS CRACK INDICATION IN FRAME REAMED HOLE NR 5 TO .375 IAW FEDEX EA 6-5310-113006. COLD WORKED HO LE NR 5 AND REAMED TO .400 IAW FEDEX EA 6-5310-113006. INSTALLED BUSHING IAW FEDEX EA 6-5310-113006. INSTALLED NEW FOO T FITTING AND BRACKETS IAW A310-200 SRM 51-40-21 PAR 7, AND FEDEX EA 6-5310-113006AND FEDEX EA 6-5310-7-5020 PT1. 2 L 7 2 4F RT A35EU 2008012200213 20080122 00213 NM 2008 1 22 F3LA200800009 1 20080116 A 3350 BR964424 LIGHT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE CABIN INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 905FR 70 1583 DURING AN EARLIER FLIGHT, ROW 11, SEATS ABC EMERGENCY LIGHT ASSEMBLY WAS TESTED AND FOUND INOPERATIVE. IT WAS PLACED ON MEL 1031603 ON 01/15/2008. DURING RON MAINTENANCE, THE MEL WAS CLEARED BY THE REPLACEMENT OF THE EMERGENCY LIGHT ASSEM BLY AT ROW 11, SEATS ABC. THE REPLACEMENT WAS ACCOMPLISHED IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-19 PB 401. AFTER THE REPLACEMENT, THE ASSEMBLY WAS TESTED AND FOUND OKAY. MEL 1031603 WAS CLOSED ON 01/16/2008. REFERENCE LOG BO OK PAGE 32572, ITEM 1. 2 L 7 2 4F 4 F RT A28NM 2008012200215 20080122 00215 EA 2008 1 22 TRAX200800047 1 20080105 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 904EV 7628 FS 333 FRAME IS CORRODED AT BL 0. BLENDED FRAME OUT OF LIMITS PER CRJ200 SRM 53-21-15 AND 53-00-00. BAT23167 1/6/2008. CORROSION BLENDOUTS IN ITEM 1 ARE WITHIN LIMITS OF REO 601R53-21-840. REFER TO ATTACHED M-234 ITEMS 3 THRU 6 FOR WORK ACCOMPLISHED. JOB COMPLETE. MEASURE BLENDED AREA FOUND .008 REMOVED. MATERIAL WORK DONE IAW CRJ 200 SRM 53-00. PERF ORMED ET INSPECTION OF BLEND AREAS ON 333 FRAME IAW CRJ200 NDTM 51-20-06. NO DEFECTS NOTED. 1/9/08 ALODINED PRIME AND PAINTED FRAME 333 IAW REO 601R-33-21-840. EC/TC REO 601R-53-21-840 C\W, JOB COMPLETE. SUPPLEMENTAL SDR CLOSED 1/11/08. 2 L 7 2 4F RT A21EA 2008012200244 20080122 00244 NM 2008 1 22 KCSA081010 1 20080112 A 3350 SIGN BOEING 747 7472B4B 138481B NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 710CK 21097 UPPER DECK EMERGENCY EXIT SIGN WILL NOT LIGHT. 2 L 7 4 4F RT A20WE 2008012200180 20080122 00180 CE 2008 1 22 GUUA01130801 1 20080113 A 3260 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MLG OUT OF ADJUST A GUUA O OTHER J WARNING INDICATION CL CLIMB 1 SO 29 82539 UE168 AFTER TAKEOFF, LANDING GEAR UNSAFE LIGHT ON WHEN GEAR HANDLE PLACED IN THE UP POSITION. DIVERTED AND LANDED WITHOUT INCI DENT.ADJUSTED NOSE LANDING GEAR UPLOCK SWITCH. 2 L 7 2 4T 4 T RT A24CE E26NE 2008012200249 20080122 00249 NM 2008 1 22 AALA200800004 1 20080101 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 768AA 33540 JFK - EMERGENCY LIGHT AT SEAT 20G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008012200308 20080122 00308 NM 2008 1 22 2008UALA00064 1 20080103 A 5210 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 532UA 25072 DOOR 2R UPPER HINGE ARM CUTOUT ON FRAME REQUIRES DOUBLER INSTALLATION. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012200309 20080122 00309 NM 2008 1 22 2008UALA00065 1 20080103 A 5420 BRACE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 532UA 25072 NR 2 PYLON UPPER BRACE FUSE PIN SHOWS CRACK INDICATION IN SIDE INNER BORE. PERFORMED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012200346 20080122 00346 NM 2008 1 22 08FDEA00150 1 20080115 A 5311 65561011 FRAME BOEING 727 727233 138408A NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 CABIN BS 620 FRAME INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT S11R BLENDED DAMAGE ON FRAME INNER CHORD, S TA 620 STR 11R, FOUND TO BE OUT OF LIMITS ORIGINAL THICKNESS .056" .008" BLEND, .048" REMAINING. FABRICATED NEW DOUBLER REF SRM 51-40-3 AND INSTALLED DOUBLER REF 51-30-2. 2 L 7 3 4F RT A3WE 2008012200353 20080122 00353 EA 2008 1 22 TRAX200800073 1 20080111 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 840AS 7290 FLAPS FAIL AMBER CAUTION MSG AT FL320. EMERGENCY DECLARED - EN ROUTE TO ATW, A/C DIVERTED TO MKE DUE TO MTC. 2 L 7 2 4F RT A21EA 2008012200366 20080122 00366 EU 2008 1 22 TRAX200800038 1 20080104 A 5320 INTERCOSTAL AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 STR LEFT 17 + INTERCOSTAL CORRODED BETWEEN FR 36-38. CORROSION REMOVED ON STR LEFT 17, BETWEEN FR 36 & 38 + INTERCOSTAL AS PER SRM 51-21-42. U/T PERFORMED BY HEATHAIR AMO 46-90 W/O 38178 IAW NTM N=0.063" MIN=0.047" STR 17 LEFT WILL BE REP LACED ON W/C 100-65. MATERIAL THICKNESS: 0.063, MATERIAL REMOVED: 0.016 OUT OF LIMITS AS PER SRM: 53-61-00 FIG 301. SU PPLEMENTAL SDR CLOSED 1/15/08. 2 H 7 2 4T RT 2008012300019 20080123 00019 EU 2008 1 23 2008UALA00001 1 20080101 A 3350 321452 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 407UA 456 RIGHT OW EMERGENCY BATTERY FAILS TEST. BATTERY FAILURE. REPLACED BATTERY, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012300074 20080123 00074 NM 2008 1 23 2008UALA00084 1 20080105 A 5320 143T8510 SILL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 566-569 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 FWD PIT FLOOR LWR DOOR SILL CORRODED STA 566 TO 569 RBL 42 TO RBL 43. SUSPECT MOISTURE CONTAMINATION. CORRODED SILL. FW D CARGO DOOR LOWER SILL, STA 566-569, BL42R TO BL43R REPAIRED ON WU 35948 DURING C12 VISIT. UA-EVA-71016A.ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012300086 20080123 00086 NM 2008 1 23 2008UALA00105 1 20080105 A 5754 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L/E SLAT PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 NR 4 L/E SLAT, LOWER SKIN PUNCTURED JUST INBOARD OF ACTUATOR FROM UPSTOP PAD LODGED IN STRUCTURE. INSTALLED SPLICE PLAT E AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300100 20080123 00100 NM 2008 1 23 DL764080033 1 20080109 A 2730 2827001011 ACTUATOR BOEING 767 767432ER 1385134 NM PWA 4060 PW4060 52119 NE RT ELEVATOR LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 828MH 29699 724741 CENTER HYD RSVR LIGHT JUST AFTER LEVEL-OFF FOLLOWED CHECKLIST RETURNED FOR LANDING LND WT 398.0LBS. FOUND RIGHT ELEVATO R CENTER HYD PCA LEAKING. REPLACED PER AM LEAK CHECK OK. RII INSPECTION COMPLETED PER TOPP 40-30-05. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012300101 20080123 00101 NM 2008 1 23 2008UALA00115 1 20080106 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 532UA 25072 EEL LIGHT AT G4A GALLEY INOP. REPLACED EMERGENCY LIGHT ASSY, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300104 20080123 00104 NM 2008 1 23 2008UALA00117 1 20080106 A 3397 D6656 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXIT SIGN BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 532UA 25072 L2 DOOR EXIT SIGN FWD OF DOOR HAS A BROKEN CONNECTOR. REPLACED CONNECTOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300108 20080123 00108 NM 2008 1 23 2008UALA00121 1 20080105 A 3350 8283T0143 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 652UA 25390 THE M736 BATTERY FOR LEFT EXTERIOR EMERGENCY LIGHTS IS INOP. REPLACED BATTERY (M736), OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2008011800021 20080118 00021 EU 2008 1 18 SIMA200801404 1 20080109 A 6120 UNKNOWN SAAB SF340 340B 7860101 EU MULTIPLE FAIL A SIMA C ABORTED TAKEOFF G J MULTIPLE FAILURE WARNING INDICATION TO TAKEOFF 1 SW 21 394AE 340B394 ON FLIGHT 3050, CREW REPORTED DURING LOW SPEED TAKEOFF ROLL, RIGHT ENGINE PROP FEATHERED (AUTOCOARSEN EVENT). UPON FURT HER TROUBLESHOOTING, RIGHT TORQUE INDICATION WAS ZERO. WHEN SELECTING AUTOCOARSEN SWITCH TO OFF, PROPELLER UN-FEATHERED BUT TORQUE INDICATION WAS STILL ZERO. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. AIRCRAF T REMOVED FROM SERVICE. REMOVED AND REPLACED TORQUE SENSOR, DECU, PROP ACTUATOR, PCU, AUTOCOARSEN COMPUTER, AND AUTOCOA RSEN SWITCHER. FCF PASSED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2008011800112 20080118 00112 SO 2008 1 18 KL12726 1 20080115 A 3210 4550406 FORK PIPER PIPER PA31 PA31350 7103110 SO MLG STRUT CRACKED E KY7A K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 NM 03 411BJ 18340 317952043 LEFT MAIN GEAR FORK ASSEMBLY HAS VERTICAL CRACK AT CASTING SEAM WHERE STRUT PISTON INSERTS INTO FORK ASSEMBLY. 1 L 7 2 3O A20SO 2008012200246 20080122 00246 NM 2008 1 22 AALA200800002 1 20080101 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 796AN 30796 MIA - EMERGENCY LIGHT AT SEAT 25G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 25G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008012200248 20080122 00248 NM 2008 1 22 AALA200800003 1 20080101 A 3350 SWITCH BOEING 777 777223 1385213 NM EMERGENCY LIGHT TRIPPED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 796AN 30796 MIA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 1G TO 4J INOPERATIVE. RESET SYSTEM FOR EMERGENCY LIGHTS AT SEAT ROWS 1G TO 4J. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080909 WP 2008 9 9 08FDEA03686 1 20080901 A 5720 ARB12611 ANGLE DOUG MD10 MD1010F 3022112 WP LT WING BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING INBOARD UPPER L/E PANEL 516 DT HAS A BROKEN ANGLE. ANGLE FABRICATED IAW DWG ARB 1261. HEAT TREATED IAW TPS 1003, REV "A". PRIMED IAW SRM 51-21-01; VOL II. INSTALLED IAW SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 20080909 NE 2008 9 9 2008UALA03904 2 20080716 A 7261 COVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 5 BEARING FAILED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 577UA 26693 NR 2 ENGINE OIL PRESSURE READING 0 ON THE QUANTITY OIL TEMP READING NORMAL. PSI BETWEEN 100-140. FLIGHT DIVERTED. *S/ D* FOUND COVER SEAL DEFECTIVE AND BLOWN OUT OF GROOVE OF NR 5 BEARING COVER. CLEANED EXCESS OIL AND REPLACED SEAL AND SERVICED OIL. ACCOMPLISHED HIGH POWER RUNS AND NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 NM 2008 9 10 AALA200802008 1 20080731 A 3350 1317 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 620AA 24578 LGA EMERGENCY LIGHT AT OVERHEAD SEAT 16C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 16C. SYSTEM G ROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 DXTA200803235 1 20080821 A 2700 UNKNOWN GULSTM 200 200 4500308 NM UNKNOWN E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 721QS 092 ON DEPARTURE AFTER AUTOPILOT WAS DISCONNECTED AND AIRCRAFT HAD FLOWN TO LEVEL FLIGHT AILERON & ELEVATOR SEEMED TO BE LOC KED IN POSITION. 2 L 7 2 4F RT A53NM 20080910 EU 2008 9 10 QML2008F00008 1 20080821 A 2497 Z200CARD CIRCUIT BOARD UROCOP EC135 EC135T1 5620026 EU NR 1 GENERATOR BURNED E QMLA O OTHER O OTHER NR NOT REPORTED 1 NM 03 135TG 0298 NR 1 GENERATOR DISCONNECT CAUTION LIGHT ILLUMINATED, FOLLOWED BY NR 1 BUSS TIE OPEN CAUTION LIGHT. PILOT PLACED NR 1 GE NERATOR CONTROL SWITCH TO OFF POSITION. THE VOLTAGE AND LOAD FOR NR 2 GENERATOR APPEARED NORMAL. APPROXIMATELY TWO MIN UTES LATER, NR 2 BUSS TIE OPEN CAUTION LIGHT ILLUMINATED FOLLOWED BY BATTERY DISCONNECT CAUTION LIGHT. A SMELL OF ELECT RICAL FUMES WAS NOTED BY PILOT AND MEDICAL CREWMEMBERS. ACFT LANDED AND BATTERY DISCONNECTED. MX FOUND THE Z-200 CARD IN THE MASTER ELECTRICAL PANEL BURNT. 1 G 7 2 3U H88EU 20080910 NM 2008 9 10 AALA200801978 1 20080727 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 688AA 25730 DFW EMERGENCY LIGHT AT LT NR 1DOOR HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LT NR 1 DOOR. SYSTEM GROUND C HECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 AALA200801981 1 20080727 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AM 24594 DFW EXTERNAL EMERGENCY LIGHT AT RT HAND OVERWING AFT POSITION INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT A T RT HAND OVERWING AFT POSITION. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 F3LA200800583 1 20080822 A 5315 D53472780000 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 928FR 2236 REFERENCE NON ROUTINE CO50040. DURING C3 C-CHECK, INSP NOTED FLOOR BEAM Y1292 HAS CORROSION IN VARIOUS NUT CLIP HOLES F ROM RT HAND FRAME 67 TO FRAME 68. MAINTENANCE INSTALLED NEW FLOOR BEAM IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11 AND ENGINEERING AUTHORIZATION # A9-53R-30392. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPT ABLE. 2 L 7 2 4F RT A28NM 20080910 NM 2008 9 10 F3L2008F00002 1 20080821 A 5240 D53480043205 SEAL AIRBUS A319 A319111 3930336 NM R2 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 928FR 2236 REFERENCE NON ROUTINE C050131. DURING C3 C-CHECK, INSPECTION NOTED NUT PLATE HOLE ON R-2 DOOR SEAL, AFT AND OUTBOARD OF R-2 AFT GIRT BAR ATTACH FITTING WAS CORRODED. SUPPLEMENTAL INFORMATION WILL BE PROVIDED AS SOON AS CORRECTIVE ACTION I NFORMATION BECOMES AVAILABLE. (OPEN) 2 L 7 2 4F RT A28NM 20080910 NM 2008 9 10 F3LA200800582 1 20080822 A 5315 D5347217220500 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 928FR 2236 REFERENCE NON ROUTINE CO50039. DURING C3 C-CHECK, INSP NOTED FLOOR BEAM Y1292 HAS CORROSION IN VARIOUS NUT CLIP HOLES F ROM RT HAND FRAME 66 TO FRAME 67. SUPPLEMENTAL INFORMATION WILL BE PROVIDED AS SOON AS CORRECTIVE ACTION INFORMATION BE COMES AVAILABLE. MX R&R FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-41-14, 51-42-00 AND 51-42-11, PAGE 24. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20080910 NM 2008 9 10 AALA200801969 1 20080726 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 DFW EMERGENCY LIGHT AT SEAT 31G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED NORM AL OPS. (CLOSED) 2 L 7 2 4F RT T00001SE 20080910 NM 2008 9 10 AALA200801983 1 20080727 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 636AM 24594 DFW EMERGENCY LIGHT EXIT IDENTIFIER AT RT HAND FORWARD OVERWING ARROW DAMAGED. REPLACED LENS FOR EMERGENCY LIGHT EXIT I DENTIFIER AT RT HAND FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 2008012300109 20080123 00109 NM 2008 1 23 DLM90080035 1 20080110 A 5330 SKIN DOUG MD90 MD9030 3023690 NM IAE V2525 V2525D5 NE BS 788-883 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 P2578 RT FUSELAGE BENEATH LOWER FILLET FAIRING RUBSTRIP STATION 788 TO 883 HAS EVIDENCE OF CORROSION. NEED RUB STRIPS AND SEA LANT REMOVED FOR FURTHER EVALUATION. COMPLIED WITH DELTA ERA 460416-14 ISSUED 06JAN08. 2 L 7 2 4F 4 F RT A6WE A40NE 2008012300121 20080123 00121 NM 2008 1 23 2008UALA00129 1 20080107 A 2612 387 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE FIRE HANDLE FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 670UA 29240 LEFT ENGINE FIRE HANDLE NEEDS RELAMPING. RELAMPED, CKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012300136 20080123 00136 NM 2008 1 23 2008UALA00137 1 20080107 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 AFT PIT STA 1380, STR 26L FRAME HAS DENT. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300138 20080123 00138 NM 2008 1 23 2008UALA00139 1 20080107 A 5314 KEELBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FUSELAGE KEEL BEAM BS 723 RBL 6.3 LOWER CHORD OUTBOARD FLANGE IS WORN. ACP'D MAJOR REPAIR PER EA I071014. INSTALLED RE PAIR ANGLE WITH CUTOUT AND REPAIR FILLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300144 20080123 00144 NM 2008 1 23 08FDEA00151 1 20080115 A 5311 651593240 FRAME BOEING 727 727233 138408A NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 CABIN BS 580 FRAME INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT S11R. BLENDED WORN AREA ON 580 FRAME. VER IFIED MATERIAL BY NDT. ORIGINAL "T" AT .056" MATERIAL LOSS AT LOWEST POINT IS .011", .045 REMAINING. EXCEEDS 10 PERC ENT MAX LIMITS REFSRM 53-10-10. FABRICATED AND HEAT TREATED REPAIR DOUBLER (TRACKING NR 416821) TO T-6 FROM 7075-0. R EMOVED DAMAGE AREA FROM STA 580 FRAME, TREATED AND PRIMED REF SRM 51-10-2. INSTALLED REPAIR DOUBLER REF SRM 53-10-1 FIG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2008012300150 20080123 00150 NM 2008 1 23 2008UALA00148 1 20080108 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 AFT PIT AT BS 1480 BETWEEN STR 25L & STR 26L, FRAME HAS DENT IN 2 PLACES. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300154 20080123 00154 NM 2008 1 23 08FDEA00140 1 20080115 A 5347 53FX93925 SEAT TRACK BOEING 727 727233 138408A NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 SEAT TRACK CORRODED (3) THREE PLACES AT STA 1130, LBL, 47, WL 208 REMOVED CORROSION ON SEAT TRACK STA 1130, LBL 47, FOUN D TO BE WITHIN LIMITS. REMOVED DOUBLER AND CORROSION. DOUBLER FOUND TO BE OUT OF LIMITS. ORIGINAL MATERIAL THICKNES S .0132", REMAINING THICKNESS .0127''. MATERIAL LOSS .005". FABRICATED NEW DOUBLER. MATERIAL 2024- T3. .050". INSTA LLED NEW DOUBLER REF SRM 51-10-1, 51-30-2 PG 3. 2 L 7 3 4F RT A3WE 2008012300155 20080123 00155 NM 2008 1 23 08FDEA00142 1 20080115 A 5340 65404132 ANGLE BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 ELECTRIC HYD PUMP MOUNT TRAY CRACKED ON AFT SIDE, BS 955A, LBL 43 WL 143. REMOVED ANGLE FROM ELE HYD PUMP MOUNT TRAY AF T SIDE BS 955A, LBL 43. FABRICATED, TREATED, PRIMED AND INSTALLED. 2 L 7 3 4F RT A3WE 2008012300156 20080123 00156 NM 2008 1 23 2008UALA00149 1 20080108 A 5210 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 R-2 DOOR UPPER HINGE ARM CUTOUT REQUIRES A REPAIR DOUBLER, FRAME DAMAGE PREVIOUSLY ROUTED OUT. MAJOR REPAIR ACCOMPLISHE D. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300160 20080123 00160 NM 2008 1 23 08FDEA00169 1 20080116 A 5347 BAC1520792 SEAT TRACK BOEING 727 727200 138407E NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 FWD CABIN, RIGHT O/B SEAT TRACK, UPPER SURFACE HAS LIGHT CORROSION AS MARKED FROM STATION 420 -440, RBL 46" WL 208 REMOV ED CORROSION BS 420 - 440, RBL 46, WL 208, ORIGINAL THICKNESS .070", .063 REMAINING .007 MAT LOSS. OUT OF LIMITS REF SR M 51-10-1, BAC 1520-792. SEAT TRACK SECTION REMOVED AND NEW SECTION INSTALLED BS 390 TO BS 480, ALONG WITH -4 ANGLES - 5 STRAP REF SRM 53-10-5 (PF) FIG 1, PGS 1,2,4. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2008012300161 20080123 00161 NM 2008 1 23 08FDEA00170 1 20080116 A 5720 65192754 WEB BOEING 727 727200 138407E NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 LT WING , RIB ATTACH FTG FOR O/B AILERON AT NR 2 HINGE I/B AND O/B WEBS BROKEN OUT HINGE ATTACH BOLT. REMOVED O/B HINGE WEB NR 2 O/B, FABRICATED, TREATED AND PRIMED AND INSTALLED NEW WEB REF SRM 51-30-2 PG 4-5. BAC DOC 65-19275, BAC DWG 6 5-19260 REV G, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2008012300163 20080123 00163 NM 2008 1 23 08FDEA00171 1 20080116 A 5320 25FX1253119 SUPPORT ANGLE BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 MAIN DECK CEILING PNL SUPPORT ANGLE IS BUCKLED/CRACKED BS 600, LBL 14. REPLACED SUPPORT ANGLE AT BS 600, LBL 14, REF S RM 51-30-2, PG 7. FABRICATED NEW SUPPORT REF FED EX DRAWING DWG 25FX 1253. THIS IS CLASSIFIED A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008012300162 20080123 00162 NM 2008 1 23 2008UALA00158 1 20080109 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS WEAK A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 116UA 26908 EMERGENCY LIGHTS FLOOD LIGHT ON DOOR 1R IS VERY WEAK. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012300173 20080123 00173 NM 2008 1 23 F3LA200800008 1 20080106 A 5315 D5347217220400 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSLEAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 924FR 5350 2030 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON THE FLOORBEAM, AROUND THE NUT CLIP LOCATIONS (6 EACH) AT THE ATTACH PO INTS OF THE FLOOR PANEL, JUST INSIDE THE L2 DOOOR. THE FLOORBEAM WAS FOUND CORRODED (OUT OF LIMITS) IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-41-14. MAINTENANCE ACTIONS WERE TAKEN TO REMOVE AND REPLACE THE FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. FOLLOWING COMPLETION OF THE INSTALLATION, IT WAS INSPECTED AND FOUND TO BE ACCEPTABLE. REFERENCE NR 25796. 2 L 7 2 4F 4 F RT A28NM 2008012300175 20080123 00175 NM 2008 1 23 NWAA080116301 1 20080112 A 2697 TERMINAL BOEING 747 747451 1384940 NM APU FIRE DETECT DAMAGED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 661US 23719 DURING CLIMB HAD 2 VERY BRIEF (1-2 SECOND) INTERMITTENT APU FIRE WARNINGS (EICAS MESSAGE AND MASTER LIGHT/BELL). AFTER CONSULTING WITH DISPATCH, MC AND FLEET TRAINING CAPTAIN APU FIRE HANDLE WAS PULLED BUT NOT TURNED. APU HAD BEEN SHUT DO WN NORMALLY PRIOR TO TAXI AND WAS NOT OPERATIONAL AT THE TIME OF BRIEF FIRE INDICATIONS. MAINTENANCE REPLACED A TERMINAL LUG AND APU FIRE AFLOT CARD. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008012300182 20080123 00182 NM 2008 1 23 2008UALA00170 1 20080109 A 2560 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FLASHLIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 574UA 26686 EMERGENCY FLASHLIGHT AT DOOR 2 LEFT DOESN'T FLASH. FOUND BATTERY FAILED.REPLACED BATTERY, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300187 20080123 00187 NM 2008 1 23 PIDA08002 1 20080107 A 5315 FLOORBEAM BOEING 737 737228 13844AG NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 DURING MAINTENANCE CHECK, CORROSION NOTED ON BS 270 FLOORBEAM FROM LBL 10 TO RBL 10. REPAIRED DAMAGE AREA PER PACE AIRL INES' EA 53-344A DATED 12/17/07 WITH FAA DER APPROVED 8110-3 DATED 12/17/2007. 2 L 7 2 4F RT A16WE 2008012300209 20080123 00209 EA 2008 1 23 HNAA0800017 1 20080105 A 2910 82910009165 HYDRAULIC LINE DHAV DHC8 DHC8311 1386006 EA HYDRAULIC SYS LEAKING A HNAA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 07 337EN 33064 33064 284 A HEAVY CHEMICAL SMELL IN CABIN DURING FINAL PHASE OF FLIGHT WAS NOTICED. REMOVED AND REPLACED THE LEAKING SECTION OF H YDRAULIC LINE FOR LANDING GEAR DOWN SELECT UNDER THE CABIN FLOOR AT FORWARD EMERGENCY EXIT. LEAK CHECK GOOD. 2 H 7 2 4T RT A13NM 2008012300211 20080123 00211 NM 2008 1 23 ASAA0852462 1 20080110 A 2822 343A2801 PUMP BOEING 737 737890 1384527 NM CENTER FUEL TANK LEAKING A ASAA K NONE K FLUID LOSS UK UNKNOWN 1 NM 02 587AS 35684 LEFT CTR FUEL BOOST PUMP IS LEAKING. REPLACED ALL O-RINGS ON LEFT CTR BOOST PUMP. OP & LEAK CHECKS GOOD. 2 L 7 2 4F RT A16WE 2008012300215 20080123 00215 NM 2008 1 23 UPS08651392 1 20080109 A 2150 6259283 SENSOR BOEING 767 76734AF 1385212 NM A/C BAY FAULTY A IPXA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 01 327UP 27753 INSPECTION TYPE:ETOP EICAS MSG "FWD EQPT OVHT" DSPLYD & OVHT LT ILLUMINATED. AFTER SELECTOR WAS POSITIONED TO STBY LT R E-ILLUMINATED FOLLOWING FIVE MINS DLY. AFTER SELECTOR WAS POSITIONED TO OVRD, EICAS MSG "FWD EQPT COOLING" DSPLYD AND " NO COOLING" LT ILLUMNATED. RAN ALL APPROPRIATE CK LISTS. PERFORMED FIM 21-58-00 FIG116 REMOVED & REINSTALLED L AND R F AN CTRL CARDS & THE EQUPT COOLING INDICATION CARD AT P50. RUN BOTH PACKS & NOTICED THE RT PACK WILL ALWAYS OPERATE AT S UB FREEZING TEMPERATURES WHEN IN STBY N MODE. C/W AIR SUPPLY DIST TEST ADJ/TEST IAW MM 36-11-00-5. ALL OPS NORMAL. 2 L 7 2 4F RT A1NM 2008012300216 20080123 00216 2008 1 23 UPS08651393 4 20080111 A 3454 285T05545 SWITCH BOEING 767 76734AF 1385212 NM COCKPIT MALFUNCTIONED A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 311UP 27741 INSPECTION TYPE:ETOP VOR/DME AUTO MAN SELECTOR SWITCH DIDN'T ILLUM ON F/O SIDE WHEN PUSHED SMOKE CAME OUT FROM UNDER GLA RESHIELD ON RIGHT SIDE OF VOR. RAN SMOKE FIRE ELEC CHECKLIST. FOUND SWITCH BURNED OUT REMOVED AND REPLACED VOR CONTROL PANEL, OPS CHECK OK. 2 L 7 2 4F RT A1NM 2008012300219 20080123 00219 NE 2008 1 23 BB08002 2 20080108 A 7310 O-RING BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E437 54555 NE RT ENGINE BROKEN A USAA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 940UW 27805 030537 CUN FLT 816 EN ROUTE CLT TO CUN: FMC FUEL DISAGREE MESSAGE. RIGHT TANK QTY DECREASED AT A HIGHER RATE. AIRCRAFT USED 4000 LBS MORE THAN FLIGHT PLAN. AFTER ARRIVAL CAPT OBSERVED FUEL LEAKING FROM RT ENGINE ON GROUND. MAINTENANCE FOUND L EAK ON RT ENGINE AT FUEL PIPE BETWEEN HP FUEL PUMP TO FFG. FOUND BROKEN O-RING. REPLACED O-RING AND RAN ENGINE WITH NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A2NM E12EU 2008012300220 20080123 00220 NM 2008 1 23 BB08003 1 20080109 A 3350 FUSE BOEING 757 7572G7 1384963 NM CABIN BLOWN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 910AW 24523 PHX - EMERGENCY LIGHTS INOP ROW 1 THRU 8. MAINTENANCE REPLACED FUSE. OPS CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2008012300221 20080123 00221 WP 2008 1 23 MWEA080008 1 20080110 A 3260 833704 PROXIMITY SENSOR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 809ME 48071 THE NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED. REMOVED AND REPLACED PROXIMITY SENSOR. 2 L 7 2 4F A6WE 2008012200278 20080122 00278 NM 2008 1 22 08FDEA00107 1 20080111 A 5313 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 616FE 48747 CENTER CARGO COMPARTMENT, BILGE AREA, LONGERON SPLICE AT STA 5-123, L-52, FOUND CRACKED ABOUT 6 INCHES. CRACKED LONGERO N SPLICE AT CENTER CARGO COMPARTMENT BILGE AREA STA 5-123, LONGERON 52, REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUM E II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008012200299 20080122 00299 NM 2008 1 22 2008UALA00052 1 20080102 A 4940 27044425 STARTER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE APU MALFUNCTIONED A UALA O OTHER W A INADEQUATE Q C FLAME/FIRE IN INSP/MAINT 1 WP 29 786UA 26938 APU NO START WITH FLAMES, RESTART NO HELP WITH FAULT LIGHT ON. SUSPECT FAULTY STARTER. REPLACED ELECT STARTER. OP CHE CK NORMAL AC OK FOR SERVICE 2 L 7 2 4F 4 F RT T0001SE E46NE 2008012200300 20080122 00300 NM 2008 1 22 2008UALA00055 1 20080102 A 4920 APU BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SHUTDOWN A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 643UA 25093 CREW REPORT: APU SHUT DOWN DUE TO FAULT. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012200312 20080122 00312 NM 2008 1 22 MWEA080003 1 20080106 A 5230 49124581 FITTING BOEING 717 717200 1383700 NM CARGO DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 925ME 55191 FORWARD CARGO DOOR HAS INTERCOSTAL DAMAGE (T-FITTING). FABRICATED AND INSTALLED T-FITTING. 2 L 7 2 4F TR A6WE 2008012200320 20080122 00320 NM 2008 1 22 PIDA08001 1 20080103 A 3350 9721055 BATTERY PACK BOEING 737 737291 138448W NM CABIN DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 583CC 21069 EMERGENCY FLOOR PATH LIGHTING INOP. REPLACED EMERGENCY FLOOR PATH LIGHTING BATTERY PACKS AND CHECKED LIGHTING PER INTER VALVE MM. 2 L 7 2 4F A16WE 2008012200355 20080122 00355 EU 2008 1 22 TRAX200800075 1 20080110 A 5720 ANGLE AEROSP ATR72 ATR72 EU LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 LEFT ON TOP WING BOX AT FR 23D AND RIB 2 ANGLE OF FR FOUND CRACKED. 2 H 7 2 4T RT 20080910 WP 2008 9 10 AALA200801957 1 20080725 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 232AA 49179 ORD EMERGENCY LIGHTS AT OVERHEAD LT & RT HAND OVERWING EXITS INOPERATIVE. SECURED LOOSE CONNECTOR AT B1 103 FOR EMERGEN CY LIGHTS AT OVERHEAD LT & RT HAND OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F A6WE 20080910 CE 2008 9 10 DJF2008F00013 1 20080825 A 2120 UNKNOWN RAYTHN DH125 HAWKER800XP 7150012 CE CABIN SMOKE A DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 23 802TA 258454 THE A/C TAXIED IN AND CHALKED AS ENGINES WERE BEING SHUT DOWN. THE COCKPIT AND CABIN STARTED FILLING WITH SMOKE. THE C REW REPORTED THE SMOKE CLEARED AFTER ALL ELECTRICAL AND ENGINE AND APU WERE SHUT DOWN. OPEN 2 L 7 2 4F RT A3EU 20080910 NM 2008 9 10 AALA200801980 1 20080727 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 688AA 25730 DFW EMERGENCY LIGHT AT SEAT 16D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 WP 2008 9 10 AALA200801956 1 20080725 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 232AA 49179 ORD EMERGENCY LIGHT MISSING LENS IN CABIN. REPLACED LENS FOR EMERGENCY LIGHT IN CABIN. SYSTEM GROUND CHECKED NORMAL OP S. (CLOSED) 2 L 7 2 4F A6WE 20080910 NM 2008 9 10 AALA200801982 1 20080727 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 636AM 24594 DFW EMERGENCY LIGHT EXIT IDENTIFIER AT LT HAND OVERWING MISSING ARROW. REPLACED LENS FOR EMERGENCY LIGHT EXIT IDENTIFIE R AT LT HAND OVERWING. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 AALA200801979 1 20080727 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 688AA 25730 DFW EMERGENCY LIGHT AT SEAT 15D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 AALA200801977 1 20080727 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 688AA 25730 DFW SEAT MOUNTED EMERGENCY LIGHT AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIG HT AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 SO 2008 9 10 C2XA08CL097 1 20080824 A 2520 7281000501 MODULE EMB 145 EMB145LR 3260212 SO PSU ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 16918 145397 CLE FLIGHT NR2173 CREW REPORTED A STRONG ELECTRICAL SMELL NEAR THE MAIN CABIN DOOR. MX INSPECTED AND REPLACED THE PASSE NGER SERVICE UNIT CONTROL MODULE OPS CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20080910 NM 2008 9 10 AALA200801968 1 20080726 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 789AN 30252 DFW EMERGENCY LIGHT AT SEAT 31G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED NOR MAL OPS. (CLOSED) 2 L 7 2 4F RT T00001SE 20080910 EU 2008 9 10 AALA200801966 1 20080726 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 77080 626 JFK EMERGENCY LIGHT AT OVERHEAD RT NR 2 DOOR INOPERATIVE. REPLACED LAMP AT OVERHEAD RT NR 2 DOOR. SYSTEM GROUND CHECKE D NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A35EU 20080910 NM 2008 9 10 AALA200801935 1 20080722 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISINSTALLED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 617AM 24525 JFK SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 9A WRONG COLOR. REPLACED LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 9A. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 USAA920081563 1 20080822 A 3350 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 823AW 1463 LOGPAGE 8167374 FLT 407 LAS PHX EEL FLASHLIGHT AT FORWARD FLIGHT ATTENDANT STATION IS INOPERATIVE. MX R&R FLASHLIGHT BA TTERY. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20080910 NM 2008 9 10 USAA920081581 1 20080822 A 5320 65C3267723 WEB BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN A1 MAJOR REPAIR NR 6123918 CRACK ON SHEAR WEB AT BS986 TO 1016, S17R. WL208. REPLACED SHEAR WEB AT BS986 TO 1016, S17R. WL208 IAW B737 SRM 51-40-02-OG. 2 L 7 2 4F RT A16WE 20080910 WP 2008 9 10 AALA200801947 1 20080724 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9402W 53138 ORD EMERGENCY LIGHT AT RT HAND OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RT HAND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A6WE 20080910 NM 2008 9 10 2008UALA04101 1 20080802 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1440 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 AFT PIT STA 1440 FRAME INNER FLANGE DENTED IN 2 EACH PLACES BETWEEN S-25L TO 26L. *S/D* ACCOMPLISHED MAJOR REPAIR AT G SO. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 53-00-07, REPAIR 5. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 NM 2008 9 10 2008UALA04102 1 20080802 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1320-1340 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 AFT PIT, INTERCOSTAL WEB STRUCTURE BETWEEN STA 1320 TO STA 1340, RBL 10.5 R. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. AFT PIT, INTERCOSTAL WEB STRUCTURE BETWEE N STA 1320 TO STA 1340, RBL 10.5 R. INSTALLED NEW. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012200378 20080122 00378 EU 2008 1 22 TRAX200800086 1 20080112 A 3350 LIGHT AEROSP ATR72 ATR72 EU PAX DOOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 634AS 370 PAX DOOR LOWER STEP EMERGENCY FLOODLIGHT INOP. 2 H 7 2 4T RT 2008012200379 20080122 00379 EA 2008 1 22 TRAX200800087 1 20080112 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 843AS 7310 AAR - LIGHTED FLOOR LEVEL EXIT SIGN AT LEFT OVERWING EXIT DID NOT LIGHT DURING OPS CHECK OF NR 4 CHARGER ASSEMBLY. UPON FURTHER REVIEW OF INSERTS ON FLOOR PANEL 271ELF FOUND INSERT TO BE LOOSE AND NOT DAMAGE REBONDED SAME SERVICEABLE INSER T IAW CMM REPAIR. 2 L 7 2 4F RT A21EA 2008012300008 20080123 00008 EA 2008 1 23 SWIA200819068 1 20080117 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 957SW 7829 MAIN CABIN DOOR IS DIFFICULT TO OPERATE, FLIGHT NR 6701. CLEANED AND LUBED MAIN CABIN DOOR. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008012300031 20080123 00031 NM 2008 1 23 2008UALA00074 1 20080105 A 3020 S312T0018 ANTI-ICE VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE INOPERATIVE A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 657UA 27112 EICAS MSG ENG-ANTI ICE DISPLAYED. REPLACED NR 2 ENG ANTI ICE VALVE, AND OP CHECKED PER MM 30-21-03 -401. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012300039 20080123 00039 WP 2008 1 23 08FDEA00158 1 20080115 A 5230 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 UPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 6 IS CRACKED IN HOLE "A" BEYOND SRM LIMITS. REPLACED SUPPORT FITTI NG NUMBER 6 MAIN CARGO DOOR SPOOL LOCATION IN REF TO SRM 51-33-01 VOL II P/N AFA7132-1. 2 L 7 3 4F RT A22WE 2008012300057 20080123 00057 NM 2008 1 23 DLM90080023 1 20080109 A 5512 5922578521 SKIN DOUG MD90 MD9030 3023690 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 DURING HMV, A CRACK WAS FOUND IN THE HORIZONTAL STABILIZER RT UPPER AFT SKIN PANEL. THE SKIN PANEL WAS REPLACED PER ER/ A INSTRUCTIONS. 2 L 7 2 4F RT A6WE 2008012300061 20080123 00061 NM 2008 1 23 08FDEA00143 1 20080115 A 5311 53FX1445502 FRAME BOEING 727 727233 138408A NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 CABIN BS 680 FRAME INNER CHORD WORN FROM CONTACT WITH LT SIDEWALL FABRICATED DOUBLER, TREATED AND PRIMED AND INSTALLED DOUBLER IAW SRM 53-10-4. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2008012300093 20080123 00093 EA 2008 1 23 SWIA200819058 1 20080111 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY MALFUNCTIONED A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 440SW 7589 "SMOKE TOILET" CAUTION MESSAGE APPEARED ON CLIMB-OUT, FLIGHT NR 3986. REPLACED LAV SMOKE DETECTOR WITH A SERVICEABLE UN IT IAW M 26-16-00, PN: PV90-421R3, SN OFF: 07970. 2 L 7 2 4F RT A21EA 2008012300133 20080123 00133 NM 2008 1 23 2008UALA00134 1 20080107 A 5320 ATTACH FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 STA 344 INTERCOSTAL ATTACH CLIP AT STR 15L IS CRACKED AT STOP FITTING I/B LWR ATTACH BOLT. REMOVED DAMAGED INTERCOSTAL CLIP. INSTALLED REPLACEMENT CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300139 20080123 00139 NM 2008 1 23 2008UALA00141 1 20080108 A 5320 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 AFT PIT AT STA 1500 AND STR 26L HAS DENT. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300145 20080123 00145 NM 2008 1 23 08FDEA00152 1 20080115 A 5311 BAC1517705 FRAME BOEING 727 727233 138408A NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 CABIN BS 520 FRAME INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT S-11R, REMOVED DAMAGE FROM INNER CHORD REF SRM 51-10-1 PG 3. NDT ACCOMPLISHED ORG MAT. .056'' MAT. REMOVED UP TO .018'' EXCEEDED 10 PERCENT ALLOWABLE DAMAGE. FA BRICATED REPAIR DOUBLER IN REF TO SRM 53-10-4 PG 7 FIG 2, SENT REPAIR DOUBLER TO HEAT TREAT, 8130 -3 FORM TRACKING NR 41 6823 AFX3375 PN NR 132012000033. TREATED AND PRIMED REPAIR DOUBLER IN REF TO SRM 51-10-2 PG 7. REMOVED DAMAGE SECTION OF FRAME 520 RT BELOW STR 11 IN REF TO SRM 53-10-4 PG 7 FIG 2. INSTALLED DOUBLER REPAIR IN REF TO SRM 53-10-4 PG 7 FIG 2. 2 L 7 3 4F RT A3WE 2008012300157 20080123 00157 NM 2008 1 23 2008UALA00150 1 20080108 A 5210 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 L-2 DOOR UPPER HINGE ARM CUTOUT REQUIRES DOUBLER INSTALLATION, FRAME DAMAGE PREVIOUSLY ROUTED OUT. MAJOR REPAIR ACCOMPL ISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300183 20080123 00183 NM 2008 1 23 2008UALA00171 1 20080110 A 2820 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEAKING A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 550UA 25398 DISPATCH REPORTS LOSS OF LEFT GEN INFLIGHT. APU GEN ONLINE. RECURRED ON FLT 116-16JAN FOUND FUEL LEAK FROM NR 1 2.5 BL D ACT. REPLACED LT IDG, NR 1 ENG FUEL/OIL COOLER AND 2.5 BLEED ACTUATOR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300184 20080123 00184 NM 2008 1 23 2008UALA00173 1 20080110 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 598UA 28751 EMERGENCY ESCAPE PATH LIGHT AFT LAV DOOR THRESHOLD IS INOP. ACCOMPLISHED REPAIR OF ESCAPE LIGHT PATH LIGHTING. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300240 20080123 00240 EU 2008 1 23 USAA920080146 1 20080111 A 2752 791A000006 ACTUATOR AIRBUS 320 A320214 3930316 EU T/E FLAP FAILED A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 114UW 25730 740 1148 FLT 1161 - PHX - SLC - EL - ON APPROACH INTO SLC, SLAT/FLAP DISAGREE ECAM MESSAGE. CREW LANDED WITH ZERO FLAP LANDING A ND EMERGENCY WAS DECLARED WITH NO FURTHER INCIDENT. VISUAL INSPECTION OF FLAPS AND OPS CHECK NORMAL. AIRCRAFT WAS MAIN TENANCE FERRIED TO PIT WHERE THE NR 1 RIGHT FLAP ACTUATOR WAS REPLACED. 2 L 7 2 4F RT A28NM 2008012300244 20080123 00244 NM 2008 1 23 UPS08M51397 1 20080110 A 3010 SENSOR DOUG MD11 MD11F 3023600 NM ANTI-ICE SYSTEM FAILED A IPXA A O UNSCHED LANDING OTHER O OTHER NR NOT REPORTED 1 SO 01 254UP 48406 INSPECTION TYPE:N/A DIVERSION - ANTI ICE SENSOR FAIL (DIVERTED DUE TO ICING CONDITIONS) A/C IS OOS. PER FIM 30-82-00-1, FOUND SYSTEM IS OK. T/S IAW FIM 36-11-00-1, BUT COULDN'T DUPLICATE FAULT. PERFORMED VISUAL INSP OF THE NR 1 ENG HIGH S TAGE SENSE LINE AND SECURITY. C/OUT HIGH STAGE SENSE LINE LEAK TEST IAW MM 36-10-00-5, FOUND NO LEAK. HIGH PWR ENG RAN ON BOTH NR 1 AND NR 3 PER MM 71-00-00, ALSO NO FAULT FOUND. 2 L 7 3 4F RT A22WE 2008012400007 20080124 00007 SO 2008 1 24 LR7A08008 1 20080105 A 5230 LS2103 ANGLE LKHEED 382 382G 526414U SO CARGO DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 636 4698 DURING SCHEDULED B-1 CHECK, PER JOB CARD HB5302 FOUND INTERCOSTAL ANGLE CRACKED AT RS61, LBL3. REPAIR ACCOMPLISHED BY F ABRICATING AND REPLACING ANGLE IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008012400060 20080124 00060 NM 2008 1 24 SWAA080343 1 20080116 A 3397 D4044P CONNECTOR BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND EMERGENCY EXIT LIGHTS ILLUMINATED WITH SWITCH IN THE OFF POSITION. FOUND LOOSE CONNE CTOR. SECURED CONNECTOR PER WDM. 2 L 7 2 4F RT A16WE 2008012400062 20080124 00062 NM 2008 1 24 SWAA080319 1 20080115 A 5322 6546543 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 20L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008012400068 20080124 00068 NM 2008 1 24 SWAA080336 1 20080116 A 5322 6545646 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 807, STR 18L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008012400069 20080124 00069 NM 2008 1 24 SWAA080330 1 20080115 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008012400071 20080124 00071 NM 2008 1 24 SWAA080337 1 20080116 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 411WN 29821 EEPLS ASSY BROKEN AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008012400073 20080124 00073 NM 2008 1 24 SWAA080324 1 20080115 A 3350 101331 LENS BOEING 737 7375H4 138449D NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008012400075 20080124 00075 NM 2008 1 24 SWAA080326 1 20080115 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008012400076 20080124 00076 NM 2008 1 24 SWAA080325 1 20080115 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED MV2 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008012400079 20080124 00079 NM 2008 1 24 SWAA080327 1 20080115 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2008012400080 20080124 00080 NM 2008 1 24 SWAA080335 1 20080115 A 3350 20131A BATTERY PACK BOEING 737 7373G7 1384595 NM CABIN FAULTY A SWAA K NONE O OTHER CL CLIMB 1 SW 29 683SW 24008 DURING CLIMBOUT OF DAL ALL EMERGENCY EXIT LIGHTS ILLUMINATED. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008012400081 20080124 00081 NM 2008 1 24 SWAA080340 1 20080116 A 5755 MA2663 SKIN BOEING 737 7373Q8 1384670 NM RT SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED C2 CHECK, FOUND RIGHT WING NR 5 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM . 2 L 7 2 4F RT A16WE 2008012400084 20080124 00084 NM 2008 1 24 SWAA080341 1 20080116 A 3350 3071BPEGPL LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED MV1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 8 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008012400088 20080124 00088 NM 2008 1 24 SWAA080342 1 20080116 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008012400089 20080124 00089 NM 2008 1 24 ZZDA2008032 1 20080110 A 5347 5971207503 SEAT TRACK BOEING 717 717200 1383700 NM COCKPIT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 FIRST OFFICER'S AFT I/B SEAT TRACK CORRODED BEYOND LIMITS. REPLACED SEAT TRACK. 2 L 7 2 4F TR A6WE 2008012400090 20080124 00090 NM 2008 1 24 ZZDA2008033 1 20080114 A 5320 SUPPORT BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 HORIZONTAL GILL LINER SUPPORT CRACKED LBL 20", 2ND FROM BOTTOM AT STA 218. REPAIRED PER B717 SRM 51-70-11. 2 L 7 2 4F TR A6WE 2008012400093 20080124 00093 NM 2008 1 24 SWAA080348 1 20080117 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER 16R CRACKED AT BS 291. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008012400097 20080124 00097 NM 2008 1 24 SWAA080349 1 20080117 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 475, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008012400099 20080124 00099 NM 2008 1 24 SWAA080351 1 20080117 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 263.5, STR 9L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008012400101 20080124 00101 NM 2008 1 24 SWAA080352 1 20080117 A 3350 417A5701 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008012400103 20080124 00103 2008 1 24 SWAA080354 4 20080117 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 438WN 29833 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008012400111 20080124 00111 SO 2008 1 24 LR7A08021 1 20080115 A 5343 BEAM LKHEED 382 382G 526414U SO FS577 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 631 4590 DURING SCHEDULED B-3 CHECK PER JOB CARD HB5301, FOUND RT UPPER WHEEL WELL MLG FRAME OUTBD CAP CRACKED AT FS 577, WL230, RBL66. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-08-002. 2 H 7 4 4T A1SO 2008012400117 20080124 00117 NM 2008 1 24 SWAA080359 1 20080118 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510B, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008012400119 20080124 00119 NM 2008 1 24 SWAA080361 1 20080118 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 321SW 23342 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 433, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008012400120 20080124 00120 NM 2008 1 24 SWAA080384 1 20080120 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 928, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008012400121 20080124 00121 NM 2008 1 24 SWAA080383 1 20080120 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 928, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008012400123 20080124 00123 NM 2008 1 24 SWAA080362 1 20080119 A 3350 OL3071BPEGPL LIGHT BOEING 737 7373K2 13844BA NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 8 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008012400124 20080124 00124 NM 2008 1 24 SWAA080379 1 20080117 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 729D, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008012300196 20080123 00196 NM 2008 1 23 08FDEA00178 1 20080116 A 5322 146N101417 SHEAR TIE BOEING 757 7572B7 1384964 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 SHEAR TIE AT STA 1460, STRINGER 29 IS EXFOLIATED. SHEAR TIE WAS EXFOLIATED COMPLETELY THROUGH, 100 PERCENT. REMOVED AN D REPLACED SHEAR TIE IAW SRM 51-40-02. NEW SHEAR TIE FABRICATED ON MAE TRAVELER NR T7/710987, FROM 7075-0-0.056 B, HEAT TREATED TO T6 IAW AMS2770H. 2 L 7 2 4F RT A2NM 2008012300197 20080123 00197 NM 2008 1 23 08FDEA00179 1 20080116 A 5311 144N110123 FRAME BOEING 757 7572B7 1384964 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 STA 920 FRAME CHORD HAS 2 BROKEN OUT AREAS LOCATED UNDER THE 1ST AND 3RD LOCK FASTENERS BELOW THE CLIP AT S10R. DAMAGE IS SEEN ON AFT SIDE OF FRAME. REMOVED DAMAGED SECTION IAW SRM 51-70-12. FABRICATED REPAIR ANGLES, FILLER IAW SRM 51-70 -12. LOCATED, DRILLED AND DEBURRED PARTS IAW SRM 51-40-05. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-20-01. INSTALLE D REPAIR PARTS PER SRM 51-70-12. 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 2008UALA04103 1 20080802 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1480 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 AFT PIT STA 1480 FRAME INNER FLANGE DENTED AT S-26L. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. CUT OUT DAMAGE AND INSTA LLED DOUBLER REPAIR PER SRM 53-00-07, REPAIR 5. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 NM 2008 9 10 2008UALA03726 1 20080705 A 2150 3987505 CONTROL VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT A/C PACK FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 667UA 29239 LEFT PACK NOT PUTTING OUT COLD AIR. ACFT WILL NOT COOL DOWN. ON GND LEFT PACK OUT TEMP 40 VS 0. *S/D* RIGHT PACK CONTR OL BITE BOX SHOWS TEMP CONTROL VALVE AND LOW LIMIT VALVE FAULTS. REPLACED BOTH UNITS PER MM 21-51-12 AND MM 21-51-11. RIGHT PACK LEAK CHECKS OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080910 NM 2008 9 10 2008UALA03756 1 20080706 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LAVATORY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 642UA 25092 EEL LIGHT IN FRONT OF RT MID LAV INOP. *S/D* FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080910 NM 2008 9 10 2008UALA03757 1 20080706 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FWD GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 642UA 25092 FWD GALLEY XAISLE EEL LIGHT INOP. *S/D* FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECK GOOD. AC OK F OR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080910 NM 2008 9 10 2008UALA03759 1 20080703 A 3350 GE1317 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 655UA 25393 EXTERIOR EEL LT INOP AFT RT SIDE SLIDE LT. *S/D* FOUND FAULTY LAMP. REPLACED LAMP, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080910 NM 2008 9 10 2008UALA03760 1 20080703 A 3397 58791 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 655UA 25393 EMERGENCY EXIT LIGHT INOP RT MID LAV. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECK GOOD. AC OK FOR SER VICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080910 NM 2008 9 10 2008UALA03761 1 20080703 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 655UA 25393 CABIN EEL INOP AFT GALLEY. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080910 NM 2008 9 10 CALA0800785 1 20080813 A 5311 143A1110 FRAME BOEING 737 737724 13844BY NM BS 400 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 21723 28790 FRAME CRACKED STATION 400 AT S-9L. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04819. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 2008UALA03763 1 20080705 A 3350 FUSE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 657UA 27112 LEFT AND RIGHT AFT DOORS EMERGENCY EXIT LIGHTS ARE INOP. *S/D* FOUND FAULTY FUSE. REPLACED FUSE, OP CHECK GOOD. AC O K FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080910 NM 2008 9 10 CALA0800792 1 20080814 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM BS 360 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16632 27900 FUSELAGE FRAME CRACKED AT STATION 360 S9L. REPAIRED FUSELAGE FRAME STATION 360 BETWEEN S8L AND S9L PER ECRA5311-01416. INITIATED DIP ITEM 53-DIP, CONTROL NR 089838 AS FOLLOWS: BEFORE THE ACCUMULATION OF 79,104 TOTAL AIRCRAFT FLIGHT CYCLE S AND AT INTERVALS NOT TO EXCEED19, 000 FLIGHT CYCLES THEREAFTER, PERFORM AN INSPECTION PER PART 2 OF ECRA 5311-01416. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 CALA0800793 1 20080813 A 5311 143A1121 FRAME BOEING 737 737724 13844BY NM BS 500A S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 21723 28790 FRAME CRACKED AT STATION 500A S-9R. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04819. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 CALA0800794 1 20080815 A 3350 76005 FUSE BOEING 757 757224 1384958 NM EMERGENCY LIGHT BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 58101 27291 SEAT PATH LIGHTS OUT FROM SEAT 25 ABC TO LAST SEAT ROW WHEN EMERGENCY LIGHTS TESTED. FOUND BATTERY CHARGER FUSE BLOWN L OCATED AT AFT CABIN CEILING M736. REPLACED FUSE P/N 76005 PER CHAPTER 20 WIRE PRACTICES AND W/D 33-51-22, PG 902 SHT 1. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 20080910 NM 2008 9 10 CALA0800784 1 20080813 A 5311 143A1110 FRAME BOEING 737 737724 13844BY NM BS 400 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 21723 28790 FRAME CRACKED STATION 400 AT S-9R. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04819. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 CALA0800787 1 20080813 A 5311 65C33509 FRAME BOEING 737 737724 13844BY NM BS 480 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 21723 28790 FRAME CRACKED STATION 480 AT S9R. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04819. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 2008UALA04201 1 20080809 A 2822 PRESSURE SWITCH BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE FUEL BOOST FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 668UA 30024 LEFT AFT FUEL BOOST LOW PRESS LIGHT INOP WITH PUMP OFF. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012300199 20080123 00199 WP 2008 1 23 08FDEA00187 1 20080117 A 5710 ARB1066 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 RT WING LWR SIDE EXT ZONE FOUND DEEP WEAR ON SKIN. REPAIRED AREA IAW SRM 57-10-00 FIG 36 AND 39 VOL I. 2 L 7 3 4F RT A22WE 2008012300254 20080123 00254 NM 2008 1 23 UPS08M51407 1 20080112 A 3610 3399046 VALVE DOUG MD11 MD11F 3023600 NM NR 1 ENGINE DEFECTIVE A IPXA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 01 254UP 48406 INSPECTION TYPE:N/A ATB - LEVEL 1 ALERT; ANTI ICE FAIL MESSAGE. PER BOW#TS2220 998 WAN #1316400 PERFORMED LEAK TEST AND PROOF TEST NR 1 ENG HIGH STAGE VALVE SENSE LINE PER MM 36-10-00-5. NO LEAK NOTED. REPLACED HIGH STAGE PILOT VALVE PER MM 36-11-20. REPLACED PSC1 PER MM 36-10-02. 2 L 7 3 4F RT A22WE 2008012400009 20080124 00009 SO 2008 1 24 LR7A08010 1 20080105 A 5310 AMS5518 WINDOW FRAME LKHEED 382 382G 526414U SO FS 150 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 636 4698 DURING SCHEDULED B-1 CHECK, PER JOB CARD HB5301 FOUND RT SIDE WINDOW AFT FRAME CRACKED AT LOWER CORNER POST 5 FS150, WL2 33. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-30-32. 2 H 7 4 4T A1SO 2008012400010 20080124 00010 SO 2008 1 24 LR7A08011 1 20080105 A 5320 BRACKET LKHEED 382 382G 526414U SO FS 577 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 636 4698 DURING SCHEDULED B-1 CHECK, PER JOB CARD HB5301 - DURING REMOVAL OF THE OUTBD CAP FOR REPLACEMENT FOUND EXFOLIATION CORR OSION OF ATTACHMENT TEE BRACKET AT FS577, WL201, LBL66. REPAIR ACCOMPLISHED BY REPLACING TEE BRACKET IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008012400031 20080124 00031 SO 2008 1 24 LR7A08019 1 20080115 A 5311 FRAME LKHEED 382 382G 526414U SO FS 1012 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 631 4590 DURING SCHEDULED B-3 CHECK PER JOB CARD HB5302, FOUND AFT FUSELAGE INTERIOR LT SIDE BULKHEAD OUTBD CAP CRACKED AT FS 101 2, WL275, LBL80. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-08-003. 2 H 7 4 4T A1SO 2008012400058 20080124 00058 SO 2008 1 24 C2XA08TY007 1 20080114 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12921 145354 CENTER AISLE EMERGENCY CEILING LIGHT AT ROW 17 INOP. REPLACED BURNED OUT BULB IAW EMB AMM 33-50-05, OPS CHECK GOOD. AI RCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008012400065 20080124 00065 NM 2008 1 24 SWAA080318 1 20080115 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008012400102 20080124 00102 NM 2008 1 24 SWAA080353 1 20080117 A 3350 MS155721 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 437WN 29832 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008012400133 20080124 00133 NM 2008 1 24 SWAA080367 1 20080118 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 439WN 29834 DURING SCHEDULED HC1 CHECK, FOUND EEPLS LENS CRACKED AT ROW 21ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008012400134 20080124 00134 NM 2008 1 24 SWAA080368 1 20080118 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 439WN 29834 DURING SCHEDULED HC1 CHECK, FOUND EEPLS LENS CRACKED AT ROW 1ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008012400135 20080124 00135 NM 2008 1 24 SWAA080369 1 20080118 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 451WN 32495 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008012400137 20080124 00137 NM 2008 1 24 SWAA080370 1 20080118 A 2121 215201 GASPER FAN BOEING 737 7373H4 1384600 NM CABIN MALFUNCTIONED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 29 646SW 28331 DECLARED EMERGENCY. ON DESCENT INTO PHX CREW NOTED ODOR AT MID CABIN, TURNED OFF GASPER FAN ODOR DISSIPATED. REMOVED A ND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2008012400138 20080124 00138 NM 2008 1 24 SWAA080371 1 20080120 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 FWD CABIN EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2008012400139 20080124 00139 NM 2008 1 24 SWAA080372 1 20080118 A 3260 655825029 LOGIC CARD BOEING 737 7373Q8 1384670 NM E&E BAY FAULTY A SWAA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 29 663SW 23256 NLG RED LIGHT ILLUMINATED, CYCLED GEAR, LIGHT EXTINGUISHED. REMOVED AND REPLACED LOGIC CARD AND RELAY PER MM. 2 L 7 2 4F RT A16WE 2008012400140 20080124 00140 NM 2008 1 24 SWAA080373 1 20080119 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 701GS 27836 L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008012400142 20080124 00142 NM 2008 1 24 HNAA0800030 1 20080114 A 3010 M2SL060030583 THERMOSTAT DHAV DHC8 DHC8102 2809003 NM COCKPIT DEFECTIVE A HNAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 07 937HA 48308 48308 148 RIGHT ELEVATOR HORN HEAT CAUTION LIGHT ILLUMINATED JUST AFTER LIFT OFF. REMOVED AND REPLACED 3015-S2 THERMOSTAT, RAN AI RCRAFT, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2008012400147 20080124 00147 NM 2008 1 24 SWAA080386 1 20080121 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 732, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008012400148 20080124 00148 NM 2008 1 24 SWAA080396 1 20080121 A 5311 6546547 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727, STR 14R. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2008012400150 20080124 00150 2008 1 24 SWAA080397 4 20080118 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008012400154 20080124 00154 NM 2008 1 24 SWAA080394 1 20080121 A 5743 115A5211 FITTING BOEING 737 7377H4 1384404 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 709SW 27843 DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008012400157 20080124 00157 WP 2008 1 24 08FDEA00195 1 20080118 A 5310 SUPPORT FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 NR 5 MCD LOWER JAMB SUPPORT FITTING HOLES A AND D HAS CRACK INDICATIONS FOUND WITH BHEC. INSTALLED REPAIR BUSHINGS IAW SRM 53-50-00 VOL I PG 81 FIG 17 AT NR 5 FITTING LOCATION 2 L 7 3 4F RT A22WE 2008012400158 20080124 00158 EU 2008 1 24 08FDEA00196 1 20080118 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 56 LT BETWEEN FRAMES 54 TO 54.2 HAS 1 REPAIR SECTION MEASURING 27.5" LONG AND 4 REPAIR ANGLES, INBD BOTTOM ANGLE IS 20.4 INCH LONG, THE STACKED INBD ANGLE IS 16.3 INCH LONG, THE OUTB D BOTTOM ANGLE IS 19.2 INCH LONG AND THE STACKED OUTBD ANGLE IS 13.9 INCH LONG REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT STRINGER REPAIR IAW A310 SRM 53-10-14, FIG 201A. THIS IS AN AIRBUS REPAIR WITH N O ASSIGNED PART NUMBER AND IOS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008012400168 20080124 00168 NM 2008 1 24 ASAA0872467 1 20080112 A 5347 146A750125 CARGO TRACK BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 649AS 30663 CARGO TRACK IN AFT PIT AT RBL 13.84 FROM BS 787 - 827 IS CORRODED OUT OF LIMITS TO SRM 53 00 53 FIG 103. REMOVED AND RE PAIRED CARGO TRACK IN AFT PIT AT RBL 13.84 FROM STA 787 - 827 IAW B737 SRM 53 00 53 FIG 201 PG 202 - 205. 2 L 7 2 4F RT A16WE 2008012400169 20080124 00169 NM 2008 1 24 ASAA0852473 1 20080108 A 5330 FASTENER BOEING 737 737890 1384527 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 548AS 30020 LIGHTNING STRIKE ON FASTENER BS 440 & 12" AND STR 22 LT. REPAIRED IAW B737 800 SRM 53 00 01 REPAIR 1. 2 L 7 2 4F RT A16WE 2008012400174 20080124 00174 WP 2008 1 24 08FDEA00203 1 20080118 A 5347 S4929150 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 MCD STA 1239 RBL 48 SEAT TRACK GOUGED AND WORN EVALUATED SEAT TRACK; SEVERAL BROKEN SCALLOPS, OUT OF LIMITS IAW DC/MD10- 10 SRM 53-70-00 VOL I PG 21. REMOVED AND REINSTALLED 4 FLOOR PANELS AT STA 1199-1321 AND 1199-1259 RBL 27-76 IAW MD/DC 10-10 M/M 53-21-01-2. REMOVED DAMAGED SECTION OF TRACK AND INSTALLED NEW SECTION, IAW DC/MD10-10 SRM 53-70-00 VOL I PG 3/4 AT STA 1229 - 1249 RBL 48, MAT'L ID SECTION, HAT SPLICE AND PLATE ALODINED AND PRIMED IAW DC/MD10-10 SRM 51-21-01 PG 21 AND 24 VOL II. FABED SECTION IAW DC/MD10-10 SRM 53-70-00 VOL I PG 3 AND 4. 2 L 7 3 4F RT A22WE 2008012400178 20080124 00178 NM 2008 1 24 USAA920080145 1 20080109 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT - MAJOR REPAIR - C5 CHECK - CRACKED FUSELAGE SKIN, BS 500, S12L. REPAIRED FUSELAGE SKIN, BS 500, S12L IAW USAIRWAYS EA 100145. 2 L 7 2 4F RT A16WE 2008012400190 20080124 00190 NM 2008 1 24 USAA920080162 1 20080102 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 867, S9L. REPAIRED FRAME, BS 867, S9L IAW USAIRWAYS EO 5311-01019. 2 L 7 2 4F RT A16WE 2008012400191 20080124 00191 NM 2008 1 24 USAA920080163 1 20080102 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 887, S9L. REPAIRED FRAME, BS 887, S9L IAW USAIRWAYS EO 5311-01019. 2 L 7 2 4F RT A16WE 2008012400192 20080124 00192 NM 2008 1 24 USAA920080164 1 20080102 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 907, S9L. REPAIRED FRAME, BS 907, S9L IAW USAIRWAYS EO 5311-01019. 2 L 7 2 4F RT A16WE 2008012400193 20080124 00193 NM 2008 1 24 USAA920080165 1 20080102 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 480, S9R. REPAIRED FRAME, BS 480, S9R IAW USAIRWAYS EO 5311-01019. 2 L 7 2 4F RT A16WE 2008012400195 20080124 00195 NM 2008 1 24 USAA920080167 1 20080102 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 787, S9R. REPAIRED FRAME, BS 787, S9R IAW USAIRWAYS EO 5311-01019. 2 L 7 2 4F RT A16WE 2008012400200 20080124 00200 NM 2008 1 24 USAA920080172 1 20080102 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 907, S9R. REPAIRED FRAME, BS 907, S9R IAW USAIRWAYS EO 5311-01019. 2 L 7 2 4F RT A16WE 2008012400203 20080124 00203 NM 2008 1 24 USAA920080175 1 20080114 A 5754 114N4003184A WEB BOEING 757 757225 1384959 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK - RIGHT WING NR 9 SLAT WEB CRACKED, FSS 692. REPAIRED RIGHT WING NR 9 SLAT WEB, FSS 692 I AW USAIRWAYS EA 110393. 2 L 7 2 4F RT A2NM 2008012400221 20080124 00221 NM 2008 1 24 SWAA080406 1 20080122 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008012400236 20080124 00236 SO 2008 1 24 FDKA200801013 1 20080108 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM 6060 TYS (0630 PHX LCL) - EMERGENCY EXIT SIGN OUT OVER LT EXIT DOOR. MX RESET EMERGENCY LIGHT SYSTEM. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400251 20080124 00251 NM 2008 1 24 CALA0800023 1 20080114 A 5313 6545800122 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 CORROSION ON INBOARD FLANGE STRINGER 29R JUST FORWARD OF E&E DOOR CUTOUT APPROX STA 320. REMOVED AND REPLACED STRINGER REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008012400255 20080124 00255 SO 2008 1 24 FDKA200801018 1 20080109 A 3240 BRAKE EMB 145 EMB145LR 3260212 SO EMERGENCY LOW PRESSURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 832MJ 145310 FDM 6015 JFK (2154 PHX LCL) - EMERGENCY BRAKE LOW PRESSURE. MX CURRENTLY TROUBLESHOOTING. 2 L 7 2 4T RT T00011AT 2008012400304 20080124 00304 SO 2008 1 24 FDKA200801022 1 20080111 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 851MJ 145572 FDM 9966 MCO-ATL - MAIN CABIN DOOR DIFFICULT TO OPEN FROM THE INSIDE. MX ADJUSTED ROLLERS AND LUBED INNER CAM. 2 L 7 2 4T RT T00011AT 2008012400305 20080124 00305 NM 2008 1 24 08FDEA00204 1 20080119 A 5320 FLANGE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 RT W/W PRESSURE DECK FUEL SHROUD MOUNTING FLANGE IS CORRODED AT BS 890 TO 888, RBL 63", WL 200. REMOVED CORROSION SRM 5 1-10-1 PG 15,15. ORIG THICKNESS IS .100", REMAINING "T" IS .061, LOSS OF .039' REF SRM 53-10-1 FIG 1. MEASURED USING T OOL AAR 18172, DUE DATE OF 10/15/08. NDT INSPECTION USING HFEC IAW 727 NDT MANUAL PART 6 51-40-00 FIG 23 TOOL NR IN22-0 044 DUE DATE OF5/21/08. NO DEFECTS NOTED. FLAP PEENED BLENDED AREA SOPM 20-10-30 FIG 19. TREATED AND PRIMED AREA SRM 51-10-2 PG 7. APPLIED ONE COAT OF BMS3-23. THIS REPAIR IS WITHIN LIMITS OF FED EX EA 7-5310-113133 LEVEL 1 CORROSION. 2 L 7 3 4F RT A3WE 2008012400308 20080124 00308 2008 1 24 ASAA0852475 4 20080114 A 2310 8220987003 ANTENNA BOEING 737 737890 1384527 NM HF COMM DELAMINATED A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 577AS 35186 HF ANTENNA ABRASION COVERING DELAMINATING. VISUALLY INSP'D FIBERGLASS STRAP SURFACE. NO DEFECTS NOTED. APPLIED PRIMER & EROSION PROTECTION COATING TO HF ANTENNA. ACCOMPLISHED EA 5530 01146 OPTION 3. CREATED DEFERRAL TO REPLACE CAP COAT EROSION PROTECTION AT NEXT HEAVY. 2 L 7 2 4F RT A16WE 2008012400312 20080124 00312 NM 2008 1 24 08FDEA00207 1 20080119 A 5315 652083332 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 FLOORBEAM CORRODED AT STA 1030, LBL 19, WL 208, UPPER SURFACE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REF FE D EX PF SRM 53-10-1 PG 26 AND 38. ORIGINAL THICKNESS IS .125" MATERIAL REMOVED IS .030" MAT. REMAINING IS .095'. INSTALLED REPAIR ANGLE AND FILLER REF FED EX SRZ 53-034 REF REPAIR NR 2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2008012400313 20080124 00313 NM 2008 1 24 ASAA0872480 1 20080114 A 5210 141A6186 SKIN BOEING 737 737790 13844CN NM L1 DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 L1 OUTER DOOR SKIN PULLED FROM STRUCTURE FROM CONTACT WITH DOOR OPENING STRUCTURE (FRAME). REPAIRED IAW SRM 52 00 01 TO INSTALL EXTERNAL DOUBLER. 2 L 7 2 4F RT A16WE 2008012300205 20080123 00205 NM 2008 1 23 PIDA08003 1 20080110 A 5340 STRINGER CLIP BOEING 737 737228 13844AG NM FUSELAGE DAMAGED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 252TR 23001 DURING MAINTENANCE CHECK, DAMAGE NOTED ON STRINGER TIE CLIP AT BS 400 AT STR 15LT. FABRICATED REPLACEMENT CLIP PER BOEI NG DRAWING 69-35350 AND INSTALLED PER SRM 51-30-02. 2 L 7 2 4F RT A16WE 2008012300218 20080123 00218 NM 2008 1 23 BB08001 1 20080108 A 3397 WIRE HARNESS BOEING 757 7572S7 1384962 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 906AW 23568 PHX - ROW 19L EMERGENCY LIGHT INOP. MAINTENANCE REMOVED & REPLACED WIRE HARNESS & EMERGENCY LIGHT ON ROW 19L. OPS CHEC KS GOOD. 2 L 7 2 4F RT A2NM 2008012400001 20080124 00001 SO 2008 1 24 LR7A08001 1 20080105 A 5311 FRAME LKHEED 382 382G 526414U SO FS 122 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 636 4698 DURING SCHEDULED B-1 CHECK, PER JOB CARD HB5301 FOUND WINDSHIELD POST CRACKED AT FS 122, WL238, RBL44. REPAIR ACCOMPLIS HED IAW LAC MEA 382-53-07-089. 2 H 7 4 4T A1SO 2008012400006 20080124 00006 SO 2008 1 24 LR7A08007 1 20080105 A 5230 LS2103 INTERCOSTAL LKHEED 382 382G 526414U SO CARGO DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 636 4698 DURING SCHEDULED B-1 CHECK, PER JOB CARD HB5302 FOUND RAMP DOOR INTERIOR INTERCOSTAL WEB/ANGLE CRACKED AT RS61, BL0. RE PAIR ACCOMPLISHED BY FABRICATING AND REPLACING ANGLE AND WEB IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008012400008 20080124 00008 SO 2008 1 24 LR7A08009 1 20080105 A 5312 LS3872 BULKHEAD LKHEED 382 382G 526414U SO FS 573 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 636 4698 DURING SCHEDULED B-1 CHECK, PER JOB CARD HB5301 DURING REMOVAL OF INTERCOSTAL BEAM FOR ACCESS FOUND ATTACHMENT WEB EXFOL IATION CORROSION AT LT UPPER WHEEL WELL FS 573, WL220, LBL62.6. REPAIR ACCOMPLISHED BY REPLACING WEB FS529-576, WL200-2 24 IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008012400028 20080124 00028 SO 2008 1 24 LR7A08016 1 20080115 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 880 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 631 4590 DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5302, FOUND CABIN BULKHEAD WEB CRACKED AT FS 880, WL200, RBL66. REPAIR ACCOM PLISHED IAW SMP583 FIG 51-140-17. 2 H 7 4 4T A1SO 20080910 NM 2008 9 10 2008UALA04273 1 20080813 A 3610 79027013 SHUTOFF VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE FLUCTUATES A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 643UA 25093 DURING CLIMB R ENG HPSOV EICAS ON DUCT PRESS FLUCTUATES BETWEEN 25 - 40 PSI, OUT DURING CRUISE. FOUND HIGH PRESSURE SHU TOFF VALVE FAULTY. REPLACED VALVE. CHECKS OKAY FOR SVC. 2 L 7 2 4F 4 F RT A1NM E24NE 20080910 NM 2008 9 10 2008UALA04278 1 20080812 A 3150 WARNING MESSAGE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE ILLUMINATED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 220UA 30223 THE "APU CONTROL" STATUS MSG ON APU START. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NM 2008 9 11 2008UALA03941 1 20080719 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT EEL LIGHT INOP LOWER WALL EEL JUST AFT OF DOOR 1 LEFT. *S/D* FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIG HT ASSEMBLY, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03982 1 20080725 A 3350 1104441 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY EXIT LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 676UA 30028 EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR IS ILLUMINATED IN COCKPIT. *S/D* FOUND EXIT LIGHT LOOSE. SECURED LIGHT, OP CH ECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03968 1 20080723 A 3350 362624 LAMP BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 675UA 29243 MID GALLEY EEL LIGHT INOP. *S/D* FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SE RVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03833 1 20080710 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 FLOOR EEL INOP RIGHT AFT AISLE AFT LAV. *S/D* FOUND BROKEN LEAD CABLE. REPAIRED LEAD CABLE IAW GNMM2-0-15-005, OP CHE CKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03931 1 20080723 A 3397 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY EXIT EEL LIGHT INOP ACROSS LAV 100 LOWER WALL EEL. *S/D* FOUND FAULTY POWER FEED CABLE. REPLACED POWER FEED ER CABLE, OP CHECK NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03800 1 20080709 A 2421 745329D IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NR 1 ENG IDG FAILED DISC RESET TEST DOES NOT RESET MANUALLY AT DISC RING. *S/D* SUSPECT FAULTY BEARING. REPLACED IDG, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03799 1 20080709 A 3350 79411 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 657UA 27112 SEAT 9J EMERGENCY LIGHT INOP. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04002 1 20080727 A 3397 362624 CONNECTOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 EEL INOP AT AFT X-AISLE. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04046 1 20080728 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 1 FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 799UA 26926 ELEC GEN SYS L IDG HAS DISCONNECTED OR A PROTECTIVE TRIP OF THE GENERATOR CONTROL BREAKER HAS OCCURRED OR A PROTECTIVE T RIP OF THE BTB HAS OCCURRED. STATUS MSG01- LATCHED CRUISE MODE DEPENDENT; INTEGRATED DRIVE GENERATOR (L) FREQUENCY IS LOW. DB- GENERATOR CONTROL UNIT (L) MSG-2431631 LATCHED ER MODE. *S/D* SUSPECT FAULTY BEARING. REPLACED IDG IAW MM 24-22-00, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 2008 9 11 2008UALA04312 4 20080818 A 2565 RELAY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT OWING SLIDE FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 518UA 24871 RIGHT OVERWING SLIDE SQUIB TEST AT P61 FAILS. REPLACED 'R SLIDE TEST RELAY' K10487 AND TEST GOOD. ALSO REPLACED AND TES TED K10536 PRECAUTIONARY DUE TO AGE. OPS CK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080911 NM 2008 9 11 2008UALA04313 1 20080818 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 573UA 26685 EMERGENCY LIGHT ON LT SIDE OF AC BY PRESSURE RELIEF VALVES INOP. FOUND LIGHT INOP. REPLACED LAMP. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080911 EU 2008 9 11 2008UALA04324 1 20080816 A 3350 20131A BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 403UA 442 LEFT UNIT DISPLAYED ON 3SV EMERGENCY LIGHT TEST. FOUND FAULTY BATTERY PACK. REPLACED EMERGENCY LIGHT BATTERY PACK & UN IT AT LT OVERWING. MESSAGE NO LONGER DISPLAYED. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012400029 20080124 00029 SO 2008 1 24 LR7A08017 1 20080115 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 902 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 631 4590 DURING SCHEDULED B-3 CHECK PER JOB CARD HB5302, FOUND AFT FUSELAGE INTERIOR RT BULKHEAD WEB CRACKED AT FS902, WL260, RBL 66. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-1. 2 H 7 4 4T A1SO 2008012400032 20080124 00032 SO 2008 1 24 LR7A08020 1 20080115 A 5343 BEAM LKHEED 382 382G 526414U SO FS 577 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 631 4590 DURING SCHEDULED B-3 CHECK PER JOB CARD HB5301, FOUND RT UPPER WHEEL WELL MLG BEAM CRACKED AT FS 577, WL236, RBL64. REP AIR ACCOMPLISHED IAW LAC MEA 382-53-08-001. 2 H 7 4 4T A1SO 2008012400057 20080124 00057 SO 2008 1 24 C2XA08IA023 1 20080111 A 4930 49523162 SOLENOID VALVE EMB 145 EMB145LR 3260212 SO APU INOPERATIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 16963 6964 6964 145116 IAH - FLIGHT 2481, THE CREW REPORTED A FUEL SMELL ON T/O WITH THE APU RUNNING. THE AIRCRAFT LANDED AT IAH WITHOUT INCID ENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, AND PLACED THE APU ON MEL 49-00-00 CAT C, CTL NUMBER 137330, AND THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. ON 01/12/08 THE AIRCRAFT RON'D IN IAH WHERE MAINTENANCE REMOVED AND REPLACED TH E FUEL SOLENOID VALVE, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008012400110 20080124 00110 SO 2008 1 24 FDKA200801005 1 20080104 A 5210 GATE EMB 145 EMB145LR 3260212 SO PAX DOOR STUCK A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 832MJ 145310 FDM 6159 CVG (0555 PHX LCL) - MAIN DOOR UPPER FLAP WILL NOT CLOSE. MX FOUND INNER DOOR HANDLE STIFF. OPERATED SEVERAL TIMES, OPERATED GOOD. 2 L 7 2 4T RT T00011AT 2008012400118 20080124 00118 NM 2008 1 24 SWAA080360 1 20080119 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, BL 0. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008012400129 20080124 00129 NM 2008 1 24 SWAA080377 1 20080116 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 781, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008012400166 20080124 00166 NM 2008 1 24 ASAA0872466 1 20080112 A 5230 146A61121 SKIN BOEING 737 737790 13844CN NM CARGO DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 649AS 30663 AFT CARGO DOOR SKIN IS CREASED 22.5 INCHES AFT OF FWD EDGE AND 14 INCHES DOWN FROM TOP REF SAD 6128725. REPAIRED AFT CA RGO DOOR SKIN IAW ASA EA 5230 01397. 2 L 7 2 4F RT A16WE 2008012400173 20080124 00173 EU 2008 1 24 08FDEA00202 1 20080118 A 5320 SILL AIRBUS 310 A310221 3930310 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 BULK CARGO DOOR CUTOUT LOWER SILL CORROSION AFT SECTION. MARKED REMOVED AND REPLACED LOWER SILL BEAM IAW A310-200 SRM 5 3-17-18 FIG 6 SHT 8 AND 51-40-21. 2 L 7 2 4F RT A35EU 2008012400179 20080124 00179 NM 2008 1 24 USAA920080147 1 20080109 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT - MAJOR REPAIR - C5 CHECK - CRACKED FUSELAGE SKIN, BS 944, S27L. REPAIRED FUSELAGE SKIN, BS 944, S27L IAW USAIRWAYS EA 100140. 2 L 7 2 4F RT A16WE 2008012400306 20080124 00306 NM 2008 1 24 ASAA0872477 1 20080112 A 5347 146A750125 CARGO TRACK BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 649AS 30663 CARGO TRACK IN AFT PIT AT RBL 13.84 FROM BS 787 827 IS CORRODED OUT OF LIMITS TO SRM 53 00 53 FIG 103. REMOVED AND REPA IRED CARGO TRACK IN AFT PIT AT RBL 13.84 FROM STA 787 827 IAW B737 SRM 53 00 53 FIG 201 PG 202 205. 2 L 7 2 4F RT A16WE 2008012400318 20080124 00318 NM 2008 1 24 08FDEA00185 1 20080116 A 5730 112N60081 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 LT WING FUEL TANK ACCESS PANEL 541GB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 541GB PER SRM 57-20-01. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 201, DETAIL I, SECTION AA, NOTE B, WITHIN .1" OF SEAL. REPLACED PANEL 541GB IAW AMM 28-11-01. 2 L 7 2 4F RT A2NM 2008012400322 20080124 00322 WP 2008 1 24 08FDEA00222 1 20080122 A 5311 ADA00035 FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 FOUND CORROSION ON FRAME LOWER SURFACE, FS 1099 BETWEEN L34L AND L35L. REMOVED CORROSION IAW SRM VOL II 51-21-01 PG 28 A. FOUND TO BE OUT OF LIMITS IAW SRM VOL I 53-00-01 FIG 5 SHT 1. REMOVED AND REINSTALLED STRAP AND ANGLE IAW SRM VOLII 51-33-01. REMOVED AND REPLACED SHEAR TIE IAW SRM, VOL II 51-33-01. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008012400355 20080124 00355 CE 2008 1 24 DXTA200802786 1 20080122 A 2750 SWITCH BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE TE FLAPS OUT OF ADJUST E DXTA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 GL 07 131QS RK431 INITIAL SELECTION OF FLAPS 10DEG AT 200KIAS FLAP ASYM CAUTION LIGHT CAME ON. TROUBLESHOT, ADJUSTED LT AND RT FLAP FOLLO W UP SWITCHES, AND LT FLAP POSITION TRANSMITTER, ALSO ADJUSTED RT FLAP FOLLOW UP SWITCH LINK AREA AND CHECKED FLAP TRAVE L ANGLES. ALL CHECKED GOOD AT THIS TIME. NO ASSYM LIGHT ILLUMINATION AT THIS TIME. IAW MM 27-20 AND 27-50-00. 2 H 7 2 4F 4 F RT A16SW E25EA 2008012400356 20080124 00356 CE 2008 1 24 DXTA200802788 1 20080122 A 3233 99125692 ACTUATOR CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE RT MLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 839QS 2285 5600690 ON APPROACH AT 4000 FT AND 180 KIAS THE RT MAIN GREEN GEAR INDICATOR ILLUMINATED STEADY. JACKED AIRCRAFT AND T/S TO DE FECTIVE RT DOWNLOCK SWITCH. REMOVED & REPLACED RT MLG ACTUATOR AND ADJUSTED. OPS AND LEAK CHECKED GOOD IAW MM 32-01-00 D OWN JACKED AIRCRAFT. 2 L 7 2 4F 4 F RT A22CE E00053EN 2008012400357 20080124 00357 CE 2008 1 24 DXTA200802789 1 20080122 A 7330 3175653 SOLENOID VALVE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP NR 2 ENGINE INOPERATIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 838QS 258338 NR 2 ENGINE COMPUTER ANNUNCIATOR LIGHT ON STEADY. REPLACED LT ENGINE SURGE VALVE SOLENOID "A" IAW TFE 731-5BR LMM CH 76 -10-01. OPERATIONAL CHECK SATISFACTORY IAW TFE731-5BR LMM CH 72-00-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2008012400360 20080124 00360 SO 2008 1 24 GLBA20061052 1 20080121 A 5730 SKIN EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT WING CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 108UX 120108 MAJOR REPAIR, LT IB LOWER WING SKIN CRACKED APPROXIMATELY .250 INCH IN LENGTH AT THE FORWARD IB CORNER OF FUEL ACCESS PA NEL 522DB. MAINTENANCE STOP DRILLED CRACK AND PATCHED IAW SRM 57-20-01. 2 L 7 2 4T 4 T RT A31SO E20NE 2008012400362 20080124 00362 NM 2008 1 24 USAA920080185 1 20080114 A 5754 WEB BOEING 757 757225 1384959 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK - RIGHT WING 6 SLAT WEB CRACKED, FSS 550. REPAIRED RIGHT WING 6 SLAT WEB, FSS 550 IAW USA IRWAYS EA 110396. 2 L 7 2 4F RT A2NM 2008012400363 20080124 00363 EU 2008 1 24 USAA920080154 1 20080104 A 5315 D5347218920400 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 669AW 1792 PIT - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3043 / FR 64 - BS 3510 / FR 69, -Y1162. REPLACED CABI N FLOORBEAM, BS 3043 / FR 64 - BS 3510 / FR 69, -Y1162 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008012400365 20080124 00365 EU 2008 1 24 USAA920080156 1 20080104 A 5315 D5347209001100 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 669AW 1792 PIT - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3043 / FR 64 - BS 3510 / FR 69, -Y1162. REPLACED CABI N FLOORBEAM, BS 3043 / FR 64 - BS 3510 / FR 69, -Y1162 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008012400366 20080124 00366 EU 2008 1 24 USAA920080157 1 20080104 A 5315 D53472188200400 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 669AW 1792 PIT - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3158 / FR 66 - BS 3366 / FR 70, +Y1162. REPLACED CABI N FLOORBEAM, BS 3158 / FR 66 - BS 3366 / FR 70, +Y1162 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008012400374 20080124 00374 EU 2008 1 24 USAA920080182 1 20080112 A 5347 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 885 CLT - MAJOR REPAIR - RON, PILOT REPORT - CORROSION ON CABIN SEAT TRACK, BS 760 / FR 18, -Y1292. REPLACED CABIN SEAT TRA CK, BS 760 / FR 18, -Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008012400376 20080124 00376 NM 2008 1 24 2008UALA00075 1 20080106 A 2450 MR24534 BUSS TIE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE E&E BAY MALFUNCTIONED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 670UA 29240 ACFT HAS NUMEROUS GALLEY PWR AND LOAD SHED ISSUES. REPLACED BPCU M116 SEE PTT 7292007, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012500002 20080125 00002 EU 2008 1 25 NWAA080253217 1 20080114 A 5230 SKIN AIRBUS 320 A320211 3930320 EU CARGO DOOR PUNCTURED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 317US 197 DURING "H" CHECK, FOUND PUNCTURE AT AFT LOWER CORNER OF FORWARD CARGO DOOR INNER SKIN. REPAIRED PER EA 32-211429 SECTIO N I. SECTION II INSPECTION TO BE DETERMINED BUT NOT LESS THAN 180 DAYS AFTER SECTION I REPAIR. 2 L 7 2 4F RT A28NM 2008012500005 20080125 00005 EU 2008 1 25 F3LA200800024 1 20080115 A 5220 L32A319160001 RELEASE CABLE AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE ESCAPE HATCH INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION AND FUNCTIONAL TESTING, THE RIGHT, OVERWING, EMERGENCY ESCAPE HATCH RELEASE CABLE WAS BINDING AND WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED THE CABLE IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 25-62-43-4 00-001. UPON REPLACEMENT OF THE CABLE, IT WAS TESTED AND INSPECTED AND FOUND TO OPERATE IN ACCORDANCE WITH THE REQUIREM ENTS OF AMM 52-21-00 PB 501. 2 L 7 2 4F 4 F RT 2008012500007 20080125 00007 WP 2008 1 25 NWAA080209996 1 20080116 A 2133 REGULATOR VALVE DOUG DC9 DC931 3022065 WP CABIN PRESSURE MALFUNCTIONED A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 8932E 57743 9583 47141 WHILE IN CRUISE FLIGHT AT FL350, THE CREW WAS ALERTED THAT THE CABIN WAS LOSING PRESSURIZATION. AN EMERGENCY WAS DECLAR ED AND A RAPID DESCENT INITIATED. AT FL300, THE CREW STARTED TO REGAIN CONTROL OF THE CABIN PRESSURE AND THE AIRCRAFT C ONTINUED A NORMAL DESCENT TO 8000 FEET. THE FLIGHT COMPLETED ITS SCHEDULED ROUTING AND LANDED AT MSP WITHOUT FURTHER IN CIDENT. MAINTENANCE ACCOMPLISHED TROUBLESHOOTING AND ULTIMATELY REPLACED THE AIR PRESSURE REGULATOR VALVE, CORRECTED NU MEROUS SMALL SYSTEM LEAKS, AND REPLACED A MISSING SEAL FROM THE CABIN PRESSURE RELIEF VALVE. 2 L 7 2 4F A6WE 2008012500009 20080125 00009 NE 2008 1 25 NWAA080193245 2 20080116 A 7310 LINE AIRBUS 320 A320212 3930322 EU CFMINT CFM56 CFM565A3 NE HMU LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 345NW 399 733366 DURING CRUISE FLIGHT, ENGINE NR 2 FUEL BURN WAS EXCESSIVE. FLIGHT CREW DIVERTED TO MIA PERFORMING AN UNEVENTFUL LANDING . MAINTENANCE FOUND A FUEL LEAK AT NR 2 ENGINE HMU FUEL HEAT RETURN LINE CONNECTION. FUEL HEAT RETURN LINE AND GASKET REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 2008012500012 20080125 00012 EU 2008 1 25 F3LA200800011 1 20080107 A 5322 D534711242000 SHEAR PLATE AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION, CORROSION WAS FOUND ON THE BOTTOM OF THE AFT SHEAR PLATE AT FRAME 69, ON THE LEFT SIDE OF THE FUSELAGE. MAINTENANCE REMOVED AND REPLACED THE AFT SHEAR PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. F OLLOWING COMPLETION OF THE INSTALLATION, THE AFT SHEAR PLATE WAS INSPECTED AND FOUND TO BE ACCEPTABLE. 2 L 7 2 4F 4 F RT 2008012500013 20080125 00013 EU 2008 1 25 F3LA200800012 1 20080107 A 5320 D5361019720000 THRESHOLD AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION, CORROSION WAS FOUND ON THE BOTTOM SIDE OF THE L1 THRESHOLD STRIP. MAINTENANCE REMOVED AND RE PLACED THE THRESHOLD STRIP IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-12-12 PB 401. UPON COMPLETION OF THE INSTALLAT ION OF THE THRESHOLD STRIP IT WAS INSPECTED AND FOUND TO BE ACCEPTABLE. 2 L 7 2 4F 4 F RT 2008012500019 20080125 00019 EU 2008 1 25 F3LA200800013 1 20080108 A 5315 FLOORBEAM AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION, CORROSION WAS FOUND ON THE INBOARD, RIGHT SIDE OF THE FLOORBEAM, FORWARD OF THE SPLICE AT FRA ME 68 AND -Y1292, AT THE SECOND NUT PLATE HOLE. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AND RELATED COUPLINGS IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11, PARAGRAPH 7. THE MAINTENANCE ACTION REQUIRED TWO FLOORBEAMS, PART NU MBERS D5347217220500 AND D5347217220390. UPON COMPLETION OF THE MAINTENANCE ACTION, THE INSTALLATION WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT 2008012500020 20080125 00020 EU 2008 1 25 F3LA200800025 1 20080121 A 2130 101809 PRESSURE SWITCH AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE CABIN PRESSURE FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION AND FUNCTIONAL TEST, THE CABIN PRESSURE SWITCH (16WR) FAILED TO DROP THE OXYGEN MASKS. MAINTE NANCE REMOVED AND REPLACED THE CABIN PRESSURE SWITCH (16WR) IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 35-23-15-400-001. FOLLOWING ITS INSTALLATION AND INSPECTION IT WAS TESTED AND FOUND OKAY. 2 L 7 2 4F 4 F RT 20080911 2008 9 11 2008UALA04325 4 20080815 A 2565 D31517121 SLIDE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L2 DOOR MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 812UA 850 EMERGENCY LIGHT TEST FAILS. FAULTS EPSU EXT LOAD AFT L. FOUND SLIDE AT FAULT. REPLACED DOOR 2L SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080911 NM 2008 9 11 2008UALA04326 1 20080814 A 2800 UNKNOWN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE UNKNOWN A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 773UA 26929 UNWANTED FUEL TRANSFER INTO LEFT MAIN TANK FROM CENTER TANK. FUEL TRANSFER FROM RIGHT MAIN TANK INTO LEFT MAIN TANK ALS O WITH CROSS FEED OPEN. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NM 2008 9 11 2008UALA04327 1 20080815 A 3397 CONNECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT CONTAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 396UA 24671 FLOOR EMERGENCY EXIT LIGHTING INOP ROW 15 AND AFT. FOUND MOISTURE AT FLOOR STRIP CONNECTORS. DRIED AND CLEANED ALL CON NECTORS FROM ROWS 15 AFT. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 20080911 NM 2008 9 11 2008UALA04337 1 20080819 A 2560 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FLASHLIGHT DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 FLASHLIGHT AT 2L BATTERY LOW. BATTERY READS LOW. REPLACED BATTERY & SEAL. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04341 1 20080818 A 2611 PU90461R3 SMOKE DETECTOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE LAVATORY INTERMITTENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 796UA 26931 SMOKE ALARM INTERMITTENT AT LAV 3L FWD. FOUND FAULTY DETECTOR. REPLACED SMOKE ALARM AT LAV 3L. REACTIVATED LAV TO NOR MAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NM 2008 9 11 08FDEA02827 1 20080711 A 5311 65453137 FRAME BOEING 727 727200 138407E NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 275FE 22040 INTERIOR FUSELAGE STA 344 STRINGER TIE AT STR 7R HAS 02 FASTENERS WITH "O" ED. REMOVED STRINGER TIE IAW B727 SRM 51-30- 2, CUT OUT DAMAGE FRAME DIM 1.5 X 5/8 IAW B727 SRM 53-10-4 FIG 2. FABRICATED NEW STRINGER TIE FROM 7075T6 .032 DIM 3 X 3.75. FRAME REPAIR FROM 7075-0 .050 DIM 4 X 9 AND FILLER REPAIR FROM 7075-0 .050 DIM 1.5 X 5/8 IAW B727 SRM 53-10-4 FIG 2 & 53 -10-2 FIG 3 & 51-20-1. HEAT TREAT REPAIR PARTS FROM 7075- 0 TO 7075 T6 (FRAME REPAIR & FILLER) IAW FAS ENGINEE RING REPORT 237153-801 REV A. TREATED AND PRIMED PARTS IAW B727 SRM 51-30-2 AND INSTALLED PARTS IAW B727 SRM 51-10-2 & 53-10-4. 2 L 7 3 4F RT A3WE 20080911 EU 2008 9 11 08FDEA02843 1 20080712 A 3230 D226550003 DAMPER AIRBUS 300 A300B4605R 3930308 EU MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 680FE 794 UNABLE TO RETRACT GEAR IN EITHER SYS 1 OR SYS 2. PERFOMED BIT CHECK ON PROX BOX, GOT CODES P1, P2, 90, BL. REMOVED CL EANED AND LUBED BOGIE BEAM PIVOT PIN AND REINSTALLED. REPLACED PITCH DAMPNER. PERFORMED MLG SWING, OPS CHECKS NORMAL A LL INDICATIONS NORMAL. REF MM 32-11-15 AND 32-11-14. 2 L 7 2 4F RT A35EU 20080911 NM 2008 9 11 08FDEA02847 1 20080714 A 5230 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 597FE 48596 DURING OPEN-HOLE HFEC INSPECTION ON 0.460" HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDIC ATIONS AT HOLES A, C AND D. MAIN CARGO DOOR LOWER JAMB NR 2 FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. T HIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080910 EA 2008 9 10 COMA086361 1 20080824 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 779CA 7306 FLOOR SUPPORT FRAME JUST O/B OF RBL9 AT FS280 IS CRACKED ON LWR AFT SIDE. CORRECTIVE ACTION: CUT OUT DAMAGE AND INSTALL ED PERMANENT REPAIR PARTS PER REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 20080910 NM 2008 9 10 AALA200801937 1 20080722 A 5320 145T87562 STIFFENER BOEING 767 767323 1385205 NM MLG WW DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7375A 25202 AFW MAIN LANDING GEAR PRESSURE DECK LONGITUDINAL STIFFENER HAS A HOLE IN THE UPPER OUT BOARD FLANGE AT RT BUTTLINE 5.75 STATION 1060. REPAIRED PER MRB 767 3250. (CLOSED) 2 L 7 2 4F RT A1NM 20080910 NM 2008 9 10 AALA200801993 1 20080728 A 3350 OL1098BPEGPL LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW EMERGENCY LIGHT AT SEAT 32G BROKEN. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKED NORMAL OP S. (CLOSED) 2 L 7 2 4F RT T00001SE 20080910 NM 2008 9 10 AALA200801991 1 20080728 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 753AN 30261 MIA EMERGENCY LIGHT AT FORWARD COAT CLOSET INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD COAT CLO SET. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT T00001SE 20080910 NM 2008 9 10 2008UALA04174 1 20080807 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 640 S24-25R DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 FWD PIT STA 640 FRAME, INNER FLANGE BETWEEN S-25R-24R DENTED. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED PRODUCT ION SPLICE AND FABRICATED A REPAIR ANGLE AND INSTALLED PER SRM 53-00-07, REPAIR 5 ON NON ROUTINE. THIS IS A CAT B REPAI R IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSPECTIONS PER TABLE II AT 50,000C TOTAL AIRFRAME CYCLES. CURRENT PTC IS 18245. 2 L 7 2 4F 4 F RT A2NM E17NE 20080910 NM 2008 9 10 2008UALA03715 1 20080703 A 2560 MXP21000 SMOKE GOGGLES BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 196UA 28715 SMOKE GOGGLES DAMAGED OR MISSING. *S/D* SUSPECT PRE FLIGHT CHECKS. REPLACED SMOKE GOGGLES. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NE 2008 9 11 2008UALA03835 2 20080711 A 7532 79027013 VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BLEED SYSTEM STICKING A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 656UA 25394 RIGHT ENG OVERHEAT LIGHT & RT ENG BLD OVERHEAT EICAS MSG DURING CRUISE & ENG OR WING ANTI-ICE SW OFF. *S/D* FOUND HIGH PRESSURE SHUT OFF VALVE STICKING. REPLACED HPSOV IAW MM36-11-07 AS A PRECAUTIONARY, CHANGED CONTROLLER IAW MM36-11-08, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 2008 9 11 2008UALA03847 4 20080712 A 2397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE MASK MICROPHONE FRAYED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 SECOND OBSERVER O2 MASK MIC WIRE IS FRAYED. *S/D* FOUND MIC WIRE FRAYED. REPLACED 2ND OBS O2 MASK PER MM 35-11-51. A C OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03781 1 20080708 A 2150 20224324 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT A/C PACK FAULTY A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 655UA 25393 LT PACK TEMP MSG IN CRUISE. *S/D* SUSPECT RAM AIR DOOR ACTUATOR. REPLACED ACTUATOR, OP CHECK GOOD. AC OK FOR SERVICE . 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04012 1 20080728 A 3350 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EXIT EEL LIGHT INOP ACROSS DOOR 3L LOWER WALL EEL. *S/D* FOUND BROKEN POWER FEEDER CABLE. REPLACED FEEDER C ABLE, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 EU 2008 9 11 08FDEA02734 1 20080708 A 2611 CG7G011 SMOKE DETECTOR AIRBUS 300 A300F4605R 3930327 EU E/E BAY FAILED A FDEA O OTHER J WARNING INDICATION DE DESCENT 1 CE 21 685FE 803 ON SHORT FINAL TO KMEM RWY 36L, GOT AVIONICS SMOKE WARNING AND CRC. DECLARED EMERGENCY AND STOPPED ON RWY. RAN QRH PR OCEDURES. NO SMOKE NOTED, SHUTDOWN ENGINES STARTED APU AND ASKED FOR TOW-IN TO PARKING. T/S AVIONICS COMPARTMENT SMOKE DETECTION USING TSM 26-15-00. REMOVED AND REPLACED AVIONICS COMPARTMENT SMOKE DETECTOR 11WA AND 13WA. OPS CHECK GOOD REF A300 MM 26-15-12-4 T/S AVIONICS COMPARTMENT SMOKE DETECTION USING TSM 26-15-00. REMOVED AND REPLACED AVIONICS CO MPARTMENT SMOKE DETECTOR 11WA AND 13WA. OPS CHECK GOOD REF A300 MM 26-15-12-4. 2 L 7 2 4F RT A35EU 20080911 WP 2008 9 11 08FDEA03696 1 20080901 A 5350 AFA016320 ANGLE DOUG MD10 MD1010F 3022112 WP W-B FAIRING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 THERE IS A CRACKED ANGLE AT THE RT WING TO BODY FAIRING SUPPORT AT BS 1581 BOTTOM EDGE. HEAT TREATED IAW TPS 1003; RE V A. FABRICATED THE REPAIR IAW SRM 53-00-01 FIG 2 VOL I. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. INSTALLED THE REPAIR IAW SRM 51-35-01; VOL II. REMOVED & RE-INSTALLED FLOOR BOARD PANEL 183WF IAW AMM 53-21-01-2. 2 L 7 3 4F RT A22WE 20080911 WP 2008 9 11 08FDEA03697 1 20080901 A 5414 217000413 FAIRING DOUG MD10 MD1010F 3022112 WP NR 1 PYLON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 1 PYLON PANEL 438 FL IS CHAFED AT THE FWD END. REMOVED DAMAGE IAW SRM 54-00-01; VOL I. 2 L 7 3 4F RT A22WE 20080911 WP 2008 9 11 08FDEA03698 1 20080901 A 5414 AUB70373 PANEL DOUG MD10 MD1010F 3022112 WP NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 1 PYLON PANEL 438 CL IS CRACKED. FABBED A REPAIR DOUBLER & INSTALLED DOUBLER REF SRM 54-00-01 VOL I. 2 L 7 3 4F RT A22WE 20080911 WP 2008 9 11 08FDEA03699 1 20080901 A 5414 PANEL DOUG MD10 MD1010F 3022112 WP NR 3 PYLON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 3 PYLON PANEL 488 GL IS CHAFED AT & AROUND THE FASTENER HOLES. BLENDED CHAFED AREAS, FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01. FABRICATED IAW EA 8-5480-123637 & DWG AUB 7036 EV W. 2 L 7 3 4F RT A22WE 20080911 WP 2008 9 11 08FDEA03638 1 20080829 A 5753 ARC2232504 PANEL DOUG MD10 MD1010F 3022112 WP RT WING TE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 RIGHT WING OUTBOARD FLAP FAIRING INBOARD SIDE PANEL 635 GL HAS A GOUGE. BLENDED GOUGE; FOUND TO BE OUT OF LIMITS IAW DC /MD-10 SRM 57-52-01; VOL III & SRM 57-00-01; VOL I. PREPPED SURFACE; TREATED & PRIMED; FABRICATED DOUBLER; LAYED UP HO T BOND REPAIR & CURED. SEALED EDGES & APPLIED PRIMER COAT. 2 L 7 3 4F RT A22WE 20080911 EU 2008 9 11 08FDEA03706 1 20080902 A 5712 A57246401214 RIB AIRBUS 300 A300B4622R 3930312 EU LT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CHAFING MARKS ON LT WING, LEADING EDGE RIB, BETWEEN RIB 1-5 REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS, NDT F OR CRACK FREE CONDITION IAW RAS/BAE/1007859/2008 ISS.A , APPROVED BY EA 6-5741-123061. 2 L 7 2 4F RT A35EU 20080911 EU 2008 9 11 08FDEA03709 1 20080902 A 5740 A57140236 FITTING AIRBUS 300 A300B4622R 3930312 EU LT WING DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND NICKS ON LT WING, THRUST AND SIDE LOAD FITTING. REPAIR PERFORMED BY BLEND OUT, NDT FOR CRACK FREE CONDITION IAW R AS/BAE/1007700/2008 ISS.A, APPROVED BY EA 6-5720-123037. 2 L 7 2 4F RT A35EU 20080911 NM 2008 9 11 08FDEA03514 1 20080820 A 5753 ARC23701 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 LEFT WING - INBOARD FLAP LOWER SURFACE FOUND DENT AT XIFH 130. LEFT WING INBOARD FLAP LOWER SURFACE DENT AREA TRIMMED O FF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080911 WP 2008 9 11 08FDEA03714 1 20080903 A 5710 ARC074415 ANGLE DOUG MD10 MD1010F 3022112 WP LT WING WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LT WING LOWER T/E PANEL MATING SURFACE IS WORN OUT BY THE OUTBOARD FLAP; INBOARD HINGE FITTING. REMOVED ANGLE & ATTACH ANGLE IAW SRM 51-31-01 VOL II. FABRICATED A NEW ANGLE IAW DWG ARG 0744; REV "J ". ALODINED IAW SRM 51-21-01 VOL II. PRIMED IAW SRM 51-21-01; VOL II. TOP COATED IAW SRM 51-21-01 VOL II. INSTALLED ANGLE IAW SRM 51-21-01 VOL II. INST ALLED PANEL IAW SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 20080912 EU 2008 9 12 TRAX200801074 1 20080830 A 3397 GROUND WIRE AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 ASD EMERGENCY LIGHT INOP (RESOLVED ON W/O 98817 TASKCARD N/R 00003) R & R ASD EMERGENCY LIGHT IAW ATR72 AMM 33-50. INSP ECTED PLUG 253VC AND GROUND 19VN. FOUND BAD GROUND IN AIR STAIR DOOR. REPAIRED GROUND IAW ATR AVM SP 20-27-17. OPS CK GOOD. ITEM 1. R&R ASD EMERGENCY LIGHT IAW ATR72 AMM 33-50. INSPECTED PLUG 253VC AND GROUND 19VN. FOUND BAD GROUND IN AIR STAIR DOOR. REPAIRED GROUND IAW ATR AVM SP 20-27-17. OPS CK GOOD. 2 H 7 2 4T RT A53EU 20080912 SO 2008 9 12 C2XA08IA196 1 20080825 A 3350 78241 BALLAST EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13988 145265 IAH FLIGHT 2312 DURING POST FLIGHT INSPECTION THE GALLEY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX R&R THE GALLEY EMER GENCY LIGHT BALLAST, OPS CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20080912 NM 2008 9 12 USAA920081611 1 20080825 A 5340 69353502 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN C18 MAJOR REPAIR NR 6124320 CRACKED STRINGER CLIP AT BS 460 S16R. REPLACED STRINGER CLIP AT BS 460, S16R IAW B737 S RM 51-40-02-OG. 2 L 7 2 4F RT A16WE 20080912 NM 2008 9 12 QXEA200800413 1 20080418 A 5320 SUPPORT BRACKET DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK SUPPORT BRACKET UNDER MCD SILL IS CRACKED. R&R SUPPORT BRACKET WITH NEW FROM STOCK REF -8 200 SRM 51-40-11 FOR RIVETING. 2 H 7 2 4T RT A13NM 20080912 EA 2008 9 12 TRAX200801056 1 20080825 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 932EV 8016 LT 621 OBLIQUE ANGLE CRACKED. REPLACED LT 621 OBLIQUE ANGLE IAW REO 061R-53-61-422 AND SRM 51-42-21. 2 L 7 2 4F RT A21EA 20080912 NM 2008 9 12 USAA920081590 1 20080826 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CRACK IN BS 178 BULKHEAD WEB AT RBL 17, WL 234. REPAIRED BS 178 BULKHEAD WEB AT RBL 17, WL 234, IAW SRM 51-10-08 & SRM 51-70-13. 2 L 7 2 4F RT A16WE 20080912 NM 2008 9 12 SWAA084794 1 20080828 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 EEPLS END CAP LOOSE AT ROW 1 ABC. SECURED END CAP PER MM. 2 L 7 2 4F RT A16WE 20080912 EA 2008 9 12 SWIA200819973 1 20080817 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY FALSE ACTIVATION A SWIA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 910EV 7727 RECEIVED A CARGO SMOKE INDICATION ON TAXI IN AND BOTH BOTTLES DISCHARGED. INSPECTED SYSTEM AND REPLACED NR 2 SMOKE DETE CTOR IAW AMM 26-15-01. REMOVED AND REPLACED BOTH CARGO FIRE BOTTLE ASSEMBLIES IAW AMM 26-25-01. OPS CHECK GOOD. P/N 4 73547-19, S/N OFF 1861. 2 L 7 2 4F RT A21EA 20080912 SO 2008 9 12 SWIA200819975 1 20080817 A 3200 UNKNOWN EMB 120 EMB120ER 3260203 SO UNKNOWN A SWIA O OTHER G MULTIPLE FAILURE LD LANDING 1 NM 07 568SW 120343 FLT 3619, AIRPLANE WOULD NOT GO INTO REVERSE PITCH AND BRAKES FAILED AS THE AIRPLANE SLOWED BELOW 40 KTS. INSPECTED BRA KE SYSTEM IAW MM 32-45-00. INSPECTED ANTISKID SYSTEM IAW MM 32-41-00, PART A, B, C AND D. ALL SYSTEMS CHECKED GOOD. C OMPLIED WITH MAX REVERSE TEST IAW MM 71-00-00. NO DEFECTS FOUND. 2 L 7 2 4T RT A31SO 20080912 SO 2008 9 12 SWIA200819972 1 20080816 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN LOOSE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 227SW 120304 FLOOR LEVEL EMERGENCY LIGHT AT ROW 9 IS INOPERATIVE. FLIGHT 5577. RESECURED EMERGENCY FLOOR TRACK LIGHTING AS REQUIRED . OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080912 NE 2008 9 12 SWIA200819956 2 20080716 A 7320 LINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* 30015 NE LT ENG FUEL CHAFED A SWIA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 442SW 7609 LEFT ENGINE FUEL CONTROL AMBIENT SENSE LINE IS CHAFED THROUGH AT SUPPORT CLAMP. FOUND AT C-CHECK. REPLACED LEFT ENGINE FUEL CONTROL AMBIENT SENSE LINE AS PER CRJ200 AMM 73-21-15-400-803. 2 L 7 2 4F 4 F RT A21EA 20080912 SO 2008 9 12 SWIA200819958 1 20080616 A 3397 CONNECTOR EMB 120 EMB120ER 3260203 SO LAVATORY LIGHT UNSECURE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 215SW 120281 ELECTRICAL ODOR COMING FROM LAV. FLIGHT 3630. VERIFIED WIRING CONNECTIONS TO LAV LIGHT IAW EMB WDM 33-80-00 AND RESECU RED CONNECTORS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080912 SO 2008 9 12 SWIA200819959 1 20080817 A 3350 BULB EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 298SW 120328 EMERGENCY EXIT LIGHT AT ROW 9C INOP. FLIGHT 5561. REPLACED BULBS AS REQUIRED. 2 L 7 2 4T RT A31SO 20080912 SO 2008 9 12 SWIA200819960 1 20080814 A 2701 BEARING EMB 120 EMB120ER 3260203 SO CONTROL YOKE BINDING A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 578SW 120346 A SLIGHT DETENT CAN BE FELT WITH AILERON MOVEMENT. FLIGHT 3604. REPLACED RIGHT AND LEFT AILERON CONTROL YOKE BEARINGS. 2 L 7 2 4T RT A31SO 20080912 EA 2008 9 12 SWIA200819962 1 20080813 A 5210 CAM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 944SW 7764 MAIN CABIN DOOR WILL NOT OPEN. FLIGHT 5977. ADJUSTED UPPER DOOR CAM AND TORQUE TUBE PUSH PULL ROD IAW CRJ 200 MM 52-11 -21. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200819939 1 20080711 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 774SK 10240 FS 280 IS CRACKED AT LBL 9 AND RBL 9. FOUND AT C-CHECK. COMPLIED WITH REPAIRS AT RBL AND LBL 9 PER SB 670BA-53-026, RE V B. 2 L 7 2 4F RT A21EA 20080912 SO 2008 9 12 SWIA200819940 1 20080805 A 3230 LANDING GEAR EMB 120 EMB120ER 3260203 SO RIGHT MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 251YV 120251 THE RIGHT MAIN GEAR WOULD NOT RETRACT. CYCLED SYSTEM AND GEAR RETRACTED NORMALLY. FLIGHT 5719. REPLACED GEAR SELECTOR LEVER ASSEMBLY IAW MM 32-31-02. GEAR SWINGS CHECKS GOOD IAW MM 32-30-00. P/N OFF 120-38594-001, S/N OFF 120-241. 2 L 7 2 4T RT A31SO 20080912 EA 2008 9 12 SWIA200819941 1 20080806 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 863AS 7487 NR 3 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLIGHT 3888. INSTALLED A SERVICEABLE BULB. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 20080912 SO 2008 9 12 SWIA200819942 1 20080803 A 5210 GUIDE EMB 120 EMB120ER 3260203 SO PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 308SW 120326 MAIN CABIN DOOR WILL NOT OPEN. FLIGHT 5473. ADJUSTED GUIDE RETAINING HARDWARE AND OPS CHECKED DOOR PER AMM 52-10-00. 2 L 7 2 4T RT A31SO 20080912 EA 2008 9 12 SWIA200819943 1 20080805 A 3350 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 457SW 7773 FORWARD SECTION OF EMERGENCY LIGHTING IS INOPERATIVE. FLIGHT 4122. REPLACED NR 2 BATTERY INVERTER. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200819982 1 20080821 A 5241 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GALLEY DOOR UNKNOWN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 944SW 7764 GALLEY DOOR WOULD NOT OPEN FROM OUTER HANDLE. FLIGHT 6712. INSPECTED AND CLEANED DOOR. CYCLED NUMEROUS TIMES WITH NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200819948 1 20080716 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 442SW 7609 FOUND CORROSION ON FUSELAGE FRAME NEAR DOOR HINGE. REPAIRED DAMAGED AREA IAW CRJ200 SRM 51-42-06 AND 51-42-13. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200819949 1 20080807 A 5210 ACCESS PANEL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 PASSENGER DOOR SHOWS SIGNS OF CORROSION AROUND UPPER ACCESS PANELS. REPAIRED PAX DOOR PER REO 601R-52-11-1520. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200819950 1 20080811 A 3230 LANDING GEAR CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 765SK 10231 GEAR WOULD NOT RETRACT ON TAKEOFF. FLIGHT 6434. INSPECTED AND CYCLED GEAR SEVERAL TIMES. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200819951 1 20080810 A 2741 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM STICKING A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 471CA 7655 STAB TRIM WOULD NOT STOP AFTER COMMANDING FORWARD INPUT ON FIRST OFFICERS SIDE. SYSTEM FUNCTIONED CORRECTLY ON CAPTAINS SIDE. FLIGHT 2798. INSPECTED, CLEANED AND LUBED FIRST OFFICERS STAB TRIM SWITCH. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200819953 1 20080811 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 955SW 7817 WHILE SELECTING GEAR DOWN, NOSE GEAR WOULD NOT LOCK IN DOWN POSITION. CYCLED GEAR HANDLE AND ALL THREE LANDING GEAR LOC KED IN DOWN POSITION. FLIGHT 6473. INSPECTED AND CYCLED NOSE LANDING GEAR SEVERAL TIMES. OPS CHECK GOOD IAW CRJ MM 32 -30-00. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200819984 1 20080822 A 2421 FILTER CNDAIR CL600 CL6002B19 1900309 EA NR 1 IDG DIRTY A SWIA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 07 403SW 7028 ADG DEPLOYED AFTER RECEIVING GENERATOR 1 OFF CAUTION MESSAGE FOLLOWED BY GENERATOR 2 OFF MESSAGE. FLIGHT 2781. SERVICE D BOTH IDG'S IAW AMM 12-13-24. REPLACED NR 1 IDG FILTER IAW AMM 24-12-01. IDG'S OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080912 SO 2008 9 12 SWIA200819992 1 20080827 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 232SW 120306 EMERGENCY LIGHT STRIP HAS TWO LIGHT BULBS NOT WORKING. FLIGHT 3581. REPLACED EMERGENCY LIGHTING BATTERY PACK NR 1. OP S CHECK GOOD. P/N D366-04-001, S/N OFF 1164. 2 L 7 2 4T RT A31SO 20080912 EA 2008 9 12 SWIA200819993 1 20080827 A 5210 ROLLER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 916SW 7634 COULD NOT OPEN THE MAIN CABIN DOOR. FLIGHT 6724. LUBED LATCH PINS AND ROLLERS ON PAX DOOR. OPERATED PAX DOOR MULTIPLE TIMES. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200819963 1 20080813 A 3230 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 915SW 9689 9689 7615 RECEIVED A GEAR DISAGREE WARNING MESSAGE ON APPROACH. COMPLIED WITH MANUAL EXTENSION. FLIGHT 6657. REPLACED MAIN LAND ING GEAR SELECTOR VALVE PER AMM 32-32-25. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080912 NM 2008 9 12 UPS08553100 1 20080809 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM LBL 44.5 WL 207 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 CORROSION ON LONGITUDINAL FLOORBEAM TOP CHORD BETWEEN BS 1011-1015 LBL 44.5, WL 207. BLENDED DAMAGE AND REPAIRED PER EO 08-2597 AND UPS B757-5310-30207A. 2 L 7 2 4F RT A2NM 20080912 NM 2008 9 12 UPS08B53101 1 20080814 A 2560 12701564 SLIDE BOEING 747 747400 13848AT NM LEFT SIDE NO TEST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:N/A WHILE ATTEMPTING UPPER DECK SLIDE DEPLOYMENT FOR FAA, LEFT SIDE SLIDE FAILED TO DEPLOY IN THE AUTOMA TIC POSITION. FOUND DOOR ASSIST BOTTLE SQUIB PREVIOUSLY BLOWN. REMOVED AND REPLACED DOOR ASSIST BOTTLE. EMERGENCY ESC APE SLIDE DEPLOYED NORMALLY DURING 2ND AUTOMATIC TEST. 2 L 7 4 4F RT A20WE 20080912 NM 2008 9 12 UPS08553084 1 20080804 A 5754 BRACKET BOEING 757 75724APF 1384969 NM NR 1 SLAT CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 453UP 25474 INSPECTION TYPE:C3 NR 1 SLAT O/B AUX TRACK CLOSURE PANEL ATTACH BRACKET I/B AFT EDGE IS CHAFED. REMOVED CHAFED BRACKET. FABRICATED REPLACEMENT BRACKET. INSTALLED REPLACEMENT BRACKET PER OHM20-50-01, DWG 114N4146, M/M 51-21-10-7. 2 L 7 2 4F RT A2NM 20080912 NM 2008 9 12 UPS08553087 1 20080804 A 5320 SUPPORT BOEING 757 75724APF 1384969 NM BS 1200 PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 453UP 25474 INSPECTION TYPE:C3 BS 1200 RBL 10 WL 144 FLOOR TO BULKHEAD SUPPORT PUNCTURED. REPAIRED PER SRM 51-70-11-0G FIG 1. 2 L 7 2 4F RT A2NM 20080912 WP 2008 9 12 UPS08853067 1 20080730 A 5321 FLOORBOARD DOUG DC8 DC871F 302199D WP MAIN CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 COURIER AREA FLOORBOARDS 2EA ARE DELAMINATED AND CRACKING. SANDED, CLEANED AND REPAIRED 2EA COURIER AREA FLOORBOARDS AT DELAMINATED AND CRACKED AREAS IAW SRM 51-01-19. 2 L 7 4 4F RT 4A25 2008012500021 20080125 00021 EU 2008 1 25 NWAA080163240 1 20080115 A 2910 O-RING AIRBUS 320 A320212 3930322 EU HYD SYSTEM LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 340NW 372 DURING CRUISE FLIGHT HYD Y RSVR LO LVL, FOLLOWED COM PROCEDURE. AIRCRAFT LANDED UNEVENTFULLY WITH ZERO HYD QUANTITY. R EPLACED O-RING ON YELLOW HP MANIFOLD, LEAK CHECKS GOOD. 2 L 7 2 4F RT A28NM 2008012500023 20080125 00023 EU 2008 1 25 NWAA080183264 1 20080116 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320212 3930322 EU YELLOW SYSTEM EMPTY A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 364NW 0962 ALL HYDRAULIC FLUID GONE FROM YELLOW HYDRAULIC SYSTEM. PERFORMED HYD RSVR LO LVL PROC AS PER COM. AIRCRAFT LANDED UNEV ENTFULLY AND WAS TOWED TO GATE. 2 L 7 2 4F RT A28NM 2008012500037 20080125 00037 EU 2008 1 25 08FDEA00119 1 20080113 A 5330 SKIN AIRBUS 310 A310221 3930310 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 416FE 288 EVALUATION OF FUSELAGE NOSE REPAIR (AERODYNAMIC BODY FILLER) BETWEEN FRAMES 3 AND 4 CENTERLINE, JUST AFT OF LOWER EDGE O F RADOME. EVALUATED REPAIR, FOUND REPAIR NOT TO CONFORM TO FEDEX SRM. REMOVED DAMAGED AREA IAW 53-11-12 FIG 201. FABR ICATED AND INSTALLED REPAIR IAW SRM 53-11-12 FIG 201. MATERIAL P/N A57210234200. 2 L 7 2 4F RT A35EU 2008012500047 20080125 00047 SO 2008 1 25 FDKA200801003 1 20080101 A 2620 SEAL EMB 145 EMB145LR 3260212 SO FIRE EXTINGUISHE BROKEN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 FDM 6024 MCO (1669 PHX LCL) - SEAL ON FLIGHT DECK FIRE EXTINGUISHER WAS BROKEN. MX INSPECTED AND RESEALED THE EXTINGUIS HER AS REQUIRED. 2 L 7 2 4T RT T00011AT 2008012400030 20080124 00030 SO 2008 1 24 LR7A08018 1 20080115 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 1012 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 631 4590 DURING SCHEDULED B-3 CHECK PER JOB CARD HB5302, FOUND AFT FUSELAGE INTERIOR LT BULKHEAD UPPER WEB CRACKED AT FS 1012, W L275, LBL80. REPAIR ACCOMPLISHED BY REPLACING WEB IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008012400143 20080124 00143 NM 2008 1 24 SWAA080385 1 20080120 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 286WN 32471 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2008012400155 20080124 00155 2008 1 24 SWAA080395 4 20080120 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 756SA 27872 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008012400167 20080124 00167 NM 2008 1 24 ASAA0872468 1 20080112 A 5230 146A61121 SKIN BOEING 737 737790 13844CN NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 649AS 30663 FWD CARGO DOOR EXTERIOR SKIN IS DENTED WITH CREASE 16 INCHES AFT OF FWD EDGE AND 30 INCHES FROM LOWER EDGE REF SAD 60917 18. REPAIRED FWD CARGO DOOR EXTERIOR SKIN IAW ASA EA 5230 01396. 2 L 7 2 4F RT A16WE 2008012400207 20080124 00207 NM 2008 1 24 SWAA080407 1 20080122 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 907, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020600360 20080206 00360 EA 2008 2 6 COMA0860064 1 20080113 A 2133 OUTFLOW VALVE CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE OBSTRUCTED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 956CA 7105 FLIGHT 5228 - ON CLIMBOUT FROM CVG RECEIVED CABIN ALTITUDE WARNING MESSAGE, WITH PACKS ON, CABIN PRESS RISING. AIRCRAFT RETURNED TO CVG AND LANDED SAFELY. UPON INSPECTION, FOUND A 16" SQUARE PIECE OF INSULATION PROJECTING THROUGH PRIMARY OUTFLOW VALVE. REMOVED INSULATION FROM VALVE AND RESECURED BACK IN PLACE ON FUSELAGE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008012400213 20080124 00213 SO 2008 1 24 FDKA200801010 1 20080108 A 2750 FLEX DRIVE EMB 145 EMB145LR 3260212 SO TE FLAPS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 841MJ 145448 FDM RON MCO (1231 PHX LCL) - FLAP FAIL WITH 45 DEGREES SELECTED. MX REMOVED AND REPLACED FLEXSHAFT SECTION. 2 L 7 2 4T RT T00011AT 2008012400223 20080124 00223 NM 2008 1 24 SWAA080404 1 20080122 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008012400317 20080124 00317 NM 2008 1 24 08FDEA00184 1 20080116 A 5730 112N60081 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 LT WING FUEL TANK ACCESS PANEL 541HB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 541HB PER SRM 57-20-01. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 201, DETAIL I, SECTION AA, NOTE B, WITHIN .1" OF SEAL. REPLACED PANEL 541HB IAW AMM 28-11-01. 2 L 7 2 4F RT A2NM 2008012400319 20080124 00319 NM 2008 1 24 08FDEA00220 1 20080122 A 5712 69333281 RIB BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 NR 2 FLAP TRACK MID FRG AFT RIB IS CRACKED REMOVED CRACKED RIB REF SRM 51-30-2 P1, PRIMED AND PAINT FLAP TRACK FRG, REF 51-10-2 PG 1-4. INSTALLED REPLACEMENT RIB REF SRM 51-30-2 P 1-3. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008012400340 20080124 00340 2008 1 24 AMTA200800015 4 20080114 A 2310 TRANSCEIVER BOEING 737 73783N 13844HI NM RROYCE RB211 RB211* 54555 NE HF COMM MALFUNCTIONED A AMTA K NONE O OTHER CR CRUISE 1 GL 11 314TZ 30640 HF 2 RADIO INOPERATIVE. (K) PERFORMED HF COMM SYSTEM BITE IAW FIM 23-11-00-810-810 TEST PASSED NO FAULTS. SWAPPED HF T RANSCEIVER IAW AMM 23-11-21-4. HF NR 2 TRANSCEIVER IS NOW SN 0386. HF NR 1 TRANSCEIVER IS NOW SN 0025. 2 L 7 2 4F 4 F RT A16WE A12EU 20080912 WP 2008 9 12 UPS08853069 1 20080730 A 5321 FLOORBOARD DOUG DC8 DC871F 302199D WP FS 800-1000 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 MAIN CABIN FLOORBOARD AT STA 800-1000 RBL 25.44 HAS 1 EA MISSING & 3EA DAMAGED INSERTS. REMOVED AND REPLACED 4EA INSERTS PER B DPS 1902-3 REPAIR 4.3.1 PG 4. 2 L 7 4 4F RT 4A25 20080912 SO 2008 9 12 SWIA200820005 1 20080903 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 293SW 120320 ONE RED FLOOR PROXIMITY EMERGENCY LIGHT MISSING FROM ROW 9 AND MAIN CABIN DOOR, ROW 2. FLT 5702. ENTERED IN ERROR, SEE SDR 20006. 2 L 7 2 4T RT A31SO 20080912 EA 2008 9 12 SWIA200820007 1 20080901 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 770SK 10243 SECOND FROM LAST CEILING LEVEL EMERGENCY FLOOD LIGHT IS BURNED OUT. FLT 6363. RELAMPED LIGHT. 2 L 7 2 4F RT A21EA 2008012200263 20080122 00263 EU 2008 1 22 08FDEA00114 1 20080112 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 51 LT BETWEEN FRAMES 55/58 TO 63 HAS 2 EA REPAIR SECTIONS THE FWD REPAIR SECTION IS BETWEEN FRAMES 55/58 TO 61 MEASURING 46" LONG AND THE AFT REPAIR SECTION IS BETWEEN FRAMES 60 TO 6 3 MEASURING 46.7" LONG WITH 2EA REPAIR SPLICES MEASURING 7.8" LONG EACH REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIO US REPAIR AND INSTALLED CORRECT STRINGER REPAIR IAW A310 SRM 53-10-14,FIG 201. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNE D PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008012200265 20080122 00265 NM 2008 1 22 AALA200800011 1 20080102 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT SEAT 30C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 30C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008012200276 20080122 00276 NM 2008 1 22 08FDEA00105 1 20080111 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 616FE 48747 MAIN DECK SEAT TRACK AT STA 1831 - 2007, X107, SEVERAL CORROSION FOUND NEAR CLIPNUTS, VIEW FROM WASTE TANK COMPARTMEN T. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PE R GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008012200279 20080122 00279 NM 2008 1 22 08FDEA00108 1 20080111 A 5280 ARC28272 DOOR DOUG MD11 MD11F 3023600 NM MLG CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 616FE 48747 RT MLG FLIPPER DOOR FORWARD SIDE FOUND CHAFED. RT MLG FLIPPER DOOR FORWARD SIDE CHAFFED EDGE SMOOTHENED OFF AND FOU ND WITHIN LIMIT AS PER SRM 52-00-01 FIGURE 1 VOLUME I. RT MLG AND GEAR WHEEL DOOR OPERATION CHECK CARRIED OUT AS PER AMM 32-31-00-700-803. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008012200284 20080122 00284 NM 2008 1 22 KCSA081013 1 20080114 A 5347 SEAT TRACK BOEING 747 747209B 138489B NM CABIN CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 UPPER DECK SEAT TRACK CORRODED AT BS 600, LBL 65. 2 L 7 4 4F RT A20WE 2008012200285 20080122 00285 NM 2008 1 22 KCSA081014 1 20080114 A 5315 FLOORBEAM BOEING 747 747209B 138489B NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 AFT PIT FLOORBEAM UPPER CHORD DENTED AT BS 1740, RBL 20. 2 L 7 4 4F RT A20WE 2008012200286 20080122 00286 NM 2008 1 22 08FDEA00133 1 20080115 A 5311 BAC1507705 FRAME BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 CABIN BS 600 FRAME INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT S-11 REPAIRED FRAME AT STA 600, STR 11 R IN RE WITH SRM 51-40-3 FIG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2008012200301 20080122 00301 NM 2008 1 22 2008UALA00056 1 20080102 A 2621 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SQUIB TEST INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 513UA 24810 PER CREW, FIRE BOTTLE SQUIB TEST LIGHT DOES NOT ILLUMINATE. REPLACED CAP ASSY AS PRECAUTIONARY. TEST NORMAL. ENGINE DISCHARGE LIGHT ON PEDESTAL DOES NOT NORMALLY WORK WITH FIRE WARNING TEST. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012200302 20080122 00302 NM 2008 1 22 2008UALA00057 1 20080103 A 2421 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FAILED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 589UA 28707 RIGHT GENERATOR DRIVE LIGHT ILLUMINATED. IDG FAILED, SHOP FOUND 4 SUPPORT SCREWS HAD LOOSE INSERTS CAUSING FAILURE. REPLACED IDG. VERIFICATION FLIGHT ACCOMPLISHED, ALL NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012200303 20080122 00303 NM 2008 1 22 2008UALA00059 1 20080103 A 5330 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 919UA 25386 LAV SERVICE TRUCK STUCK ACFT, RT SIDE, NEAR F/O'S WINDOW AREA. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012200305 20080122 00305 NM 2008 1 22 2008UALA00061 1 20080103 A 3350 60243 LIGHT BOEING 737 737322 1384676 NM FWD GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 334UA 24229 FWD GALLEY EEL LIGHT INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F RT A16WE 2008012200310 20080122 00310 NM 2008 1 22 2008UALA00066 1 20080103 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L1 DOOR BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 652UA 25390 L1 DOOR LWR EMERGENCY EXIT IDENTIFIER SIGN L979 WIRES ARE BROKEN. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012400342 20080124 00342 EU 2008 1 24 EOX2008F00000 1 20080105 A 2435 23091002 STARTER GEN BRAERO 1000 HAWKER1000 7450005 EU PWA 305 PW305 NE RT ENGINE VIBRATION E EOXA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 EA 39 548LR 259048 AIRCRAFT WAS FL360 ENROUTE, FLIGHT CREW NOTED A VIBRATION IN THE RT ENGINE AND DID A PRECAUTIONARY SHUTDOWN OF THE RT EN GINE. THE AIRCRAFT DIVERTED AND MADE AN UNEVENTFUL LANDING WITH NO INJURIES TO PASSENGERS OR CREW. INSPECTED THE RT EN GINE AND FOUND THAT THE PROBLEM WAS THE RT STARTER GENERATOR FAN VIBRATING. THE RT STARTER GENERATOR WAS CHANGED OUT WI TH A SERVICEABLE UNIT AND OPERATIONAL CHECK PERFORMED WITH NO DISCREPANCIES NOTED. (K) 2 L 7 2 4F 4 F RT A3EU E35NE 2008012400354 20080124 00354 CE 2008 1 24 EOX2008F00001 1 20080105 A 3010 SEALANT BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE ANTI-ICE DUCT SMOKE E EOXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 39 527XP 183 RK527 AC EXPERIENCED SMOKE IN THE CABIN AT FL 22 ENROUTE, FLIGHT CREW FOLLOWED PROCEDURE WITH CAPTAIN DAWNING O2 MASK AND 2ND OFFICER INSPECTING CABIN. NO DISCREPANCIES WERE NOTED OTHER THAN SMOKE IN CABIN, WHICH WAS DISSIPATING. FLIGHT CREW FE LT THAT THE ISSUE WAS UNDER CONTROL AND CONTINUED TO THE INTENDED DESTINATION UNEVENTFULLY. INSPECTED AC, PERFORMED CAB IN TEMP SYSTEM CHECK, WING LEADING ANTI-ICE TEST, ALL TEST SATISFACTORY. BELIEVE GLUE IN ANTI-ICE DUCKS HEATING UP DUE TO HIGH POWER SETTINGS. COMMUNIQUÉ 77, ATA30-WING ANTI-ICE INSULATION. NO OTHER DISCREPANCIES NOTED AT THIS TIME. (K) 2 H 7 2 4F 4 F RT A16SW E25EA 2008012500001 20080125 00001 NM 2008 1 25 C1HA200892001 1 20080115 A 5330 SKIN BOEING 727 727212 138407G NM BS 1089 S28L CRACKED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 292AS 21458 FOUND CRACKED SKIN AND CORRODED STRINGER AT STA 1089 AT STR 28L. TRIMMED OUT DAMAGED TOP SKIN AND FABRICATED DOUBLER FR OM 2024-T3 .060" AND INSTALLED PER SRM 53-30-3 FIG 3 CAT B. REPAIR MUST BE REINSPECTED AT 45000 CYCLES THRESHOLD STARTS AT DATE OF REPAIR. RII ACCOMPLISHED AND VERIFIED DONE IAW SRM 53-30-3. A/C APPROVED. 2 L 7 3 4F A3WE 2008012500010 20080125 00010 NM 2008 1 25 F3LA200800010 1 20080116 A 2130 CABIN PRESSURE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FLUCTUATES A F3LA O OTHER J WARNING INDICATION CL CLIMB 1 NM 03 912FR 1803 THE FLIGHT CREW REPORTED, DURING CLIMB-OUT, PRESSURIZATION FLUCTUATED 200 FEET PER MINUTE BETWEEN FLIGHT LEVEL 350 UP TO AND LEVELING AT FLIGHT LEVEL 380. AT THE SAME TIME, THE R2 DOOR PRESSURE LIGHT FLASHED AND THE SLIDE "DISARM" ILLUMINA TED, ON THE LOWER ECAM SYSTEM DISPLAY, SHOWING THE DOOR PAGE. AFTER LEVEL OFF, PRESSURIZATION STABILIZED AND THE SLIDE DISARM INDICATOR RESET TO "ARMED." MAINTENANCE PERFORMED A VISUAL AND OPERATIONAL CHECK OF THE R2 DOOR IN ACCORDANCE WI TH THE REQUIREMENTS OF AMM 52-10-13 PB 501. MAINTENANCE THOROUGHLY CLEANED AND INSPECTED THE GIRT BAR FITTINGS, IN ACCO RDANCE WITH THE REQUIREMENTS OF AMM 52-13-22 PB 501. AN OPERATIONAL CHECK OF THE R2 DOOR WAS DONE AND THE DOOR CHECKED 2 L 7 2 4F 4 F RT A28NM 2008012500011 20080125 00011 EU 2008 1 25 F3LA200800022 1 20080115 A 5321 D5367180500400 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION, CARGO FLOOR PANEL 261FF, LOCATED BETWEEN FRAMES 66 AND 68, WAS FOUND TO HAVE CORROSION ON ITS LOWER SURFACE. MAINTENANCE REMOVED AND REPLACED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-42-12 PB 401. FOLLOWING THE COMPLETION OF THE INSTALLATION, THE NEW FLOOR PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT 2008012800047 20080128 00047 SO 2008 1 28 FDKA200801025 1 20080114 A 5344 BUSHING EMB 145 EMB145LR 3260212 SO PAX DOOR HINGE DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 851MJ 145572 FDM FLT 6206 FLL (0907 PHX LCL) MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. MX REMOVED AND REPLACED DOOR HINGE BUSHIN G AND BOLT, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008012800049 20080128 00049 SO 2008 1 28 FDKA200801002 1 20080101 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCONNECTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6137 ATL (1157 PHX LCL) - FLOOR PROXIMITY EMERGENCY LIGHT OUT AT ROW 7. MX RECONNECTED CONNECTOR. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012800050 20080128 00050 SO 2008 1 28 FDKA200801004 1 20080102 A 2750 FLAP SYSTEM EMB 145 EMB145LR 3260212 SO TE FLAPS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 841MJ 145448 FDM 6163 PNS (1710 PHX LCL) - FLAPS HALF SPEED. MX TROUBLESHOT TO CHANNEL 2 AND PLACED IT ON MEL. 2 L 7 2 4T RT T00011AT 2008012800066 20080128 00066 SO 2008 1 28 C2XAO8SH006 1 20080116 A 5310 14525480603 BEAM EMB 145 EMB145XR 3260214 SO CARGO DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13124 145689 SHV - DURING C-CHECK, CARGO DOOR CUT OUT LOWER SECTION HAS VARIOUS AREAS OF CORROSION. MX REMOVED AND REPLACED CUTOUT L OWER BEAM IAW EMB 145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008012800067 20080128 00067 SO 2008 1 28 C2XA08SH007 1 20080116 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13124 145689 SHV DURING C-CHECK, LT OMEGA BEAM LOWER FLANGE HAS VARIOUS AREAS OF CORROSION AT FR21-23. MX REPAIRED LT OMEGA BEAM LOW ER FLANGE AT FR 21-23 IAW SRM 53-21-10. THE AIRCRAFT WAS APPROVE TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008012400128 20080124 00128 2008 1 24 SWAA080378 4 20080116 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008012400159 20080124 00159 EU 2008 1 24 08FDEA00197 1 20080118 A 5330 LAP JOINT AIRBUS 310 A310203 3930313 EU ZONE 200 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS EXTERNAL LAP SEAM REPAIR LOCATED AT UPPER CROWN FUSELAGE SKIN AT FRAME 67 AND BETWEEN STRINGERS 4 TO 7 RT THE R EPAIR FILLER MEASURES 7.8 INCHES BY 11.9 INCHES WITH 2 ROWS OF FASTENERS PAST THE DOUBLER WITH A .900 INCH MILL STEP ARO UND THE OUTER ROW AND THE REPAIR DOUBLER MEASURES 8.5 INCH BY 9.8 INCH. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVI OUS REPAIR AND INSTALLED CORRECT SKIN REPAIR IAW A310 SRM 53-10-12, FIG 217, SHEET 3. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008012400177 20080124 00177 NM 2008 1 24 USAA920080144 1 20080105 A 5752 654645521C TAB BOEING 737 737301 1384611 NM LT AILERON DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT - MAJOR REPAIR - C5 CHECK - LEFT WING AILERON TAB TRAILING EDGE DELAMINATED. REPLACED LEFT WING AILERON TAB IAW USA IRWAYS JOB CARD 03C30627009. 2 L 7 2 4F RT A16WE 2008012400187 20080124 00187 NM 2008 1 24 USAA920080159 1 20080102 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 440, S9L. REPAIRED FRAME, BS 440, S9L IAW USAIRWAYS EO 5311-01019. 2 L 7 2 4F RT A16WE 2008012400206 20080124 00206 NM 2008 1 24 SWAA080405 1 20080122 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008012400209 20080124 00209 NM 2008 1 24 SWAA080416 1 20080122 A 5320 6545819 WEB BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND NLG W/W LT CEILING PANEL CUTOUT WEB CRACKED AT LOWER INBOARD END. REPAIRED WEB PER AC O. 2 L 7 2 4F RT A16WE 2008012400211 20080124 00211 NM 2008 1 24 SWAA080410 1 20080122 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 22R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2008012400217 20080124 00217 SO 2008 1 24 FDKA200801012 1 20080108 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO GALLEY ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 835MJ 145353 FDM RON CAE (1854 PHX LCL), ELECTRICAL ODOR FROM GALLEY OVERHEAD LIGHT. MX CURRENTLY TROUBLESHOOTING. 2 L 7 2 4T RT T00011AT 2008012400219 20080124 00219 NM 2008 1 24 SWAA080415 1 20080122 A 5320 6545819 WEB BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND NLG W/W RT CEILING PANEL CUTOUT WEB CRACKED AT LOWER OUTBOARD END. REPAIRED WEB PER A CO. 2 L 7 2 4F RT A16WE 2008012400228 20080124 00228 NM 2008 1 24 08FDEA00217 1 20080122 A 5320 FLOOR SUPPORT BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 AFT CARGO PIT CAP STRIP, 950D TO 990 LT, CRACKED AT FASTENER HOLE FABRICATED NEW CAP STRIP. REF BOEING DWG NR 65-67278/ SRM 51-20-1 FIG 2/SRM 51-10-1, PG 12. TREATED AND PRIMED CAP STRIP, REF SRM 51-10-2 PG 1, THIS IS CLASSIFIED AS MINOR R EPAIR. 2 L 7 3 4F RT A3WE 2008012400244 20080124 00244 SO 2008 1 24 FDKA200801015 1 20080109 A 2797 CONNECTOR EMB 145 EMB145LR 3260212 SO SPOILERS DIRTY A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6188 JFK (1223 PHX LCL) - SPOILER FAIL MESSAGE IN FLIGHT. MX CLEANED CONNECTORS AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012400274 20080124 00274 NM 2008 1 24 08FDEA00182 1 20080116 A 5730 112N61015 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 LEFT WING FUEL TANK ACCESS PANEL 543AB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 543AB PER SRM 57-20-0 1. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 201, DETAIL I, SECTION AA, NOTE B, WITHIN .1" OF SEAL. REPLACED PAN EL 543AB IAW AMM 28-11-01. 2 L 7 2 4F RT A2NM 2008012400275 20080124 00275 NM 2008 1 24 08FDEA00183 1 20080116 A 5730 65478504 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 LEFT WING FUEL TANK ACCESS PANEL 542AB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 542AB PER SRM 57-20-0 1. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 201, DETAIL I, SECTION AA, NOTE B, WITHIN .1" OF SEAL. REPLACED PAN EL 542AB IAW AMM 28-11-01. 2 L 7 2 4F RT A2NM 2008012400310 20080124 00310 NM 2008 1 24 08FDEA00205 1 20080119 A 5311 BAC15171062 FRAME BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 CABIN FRAME REPAIR INSTALLED AT BS 640, STR S-11R, FRAME HAS TOOLING DAMAGE ON AFT FACE OF FRAME WEB AT UPPER RIVET BUCK TAIL BLENDED DAMAGE AREA AT CABIN FRAME STA 640, STR 11R REF SRM 53-10-1 FIG 1. ORIGINAL MATERIAL .056 INCH. MATERIAL REMAINING .048 INCH'. MATERIAL LOSS OF .008 AND DAMAGE IS LESS THAN 1" FROM A HOLE IN RESPECTION NOTE "U" REF SRM 53- 10-1. FABRICATED REPAIR DOUBLER REF SRM 53-10-4 FIG 1. HEAT TREATED, TRACKING NR 2008-01-073, TREATED AND PRIMED REP AIR DOUBLER AND INSTALLED REF 51-10-2, 51-30-2, 53-10-4. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2008012400314 20080124 00314 NM 2008 1 24 ASAA0872479 1 20080112 A 5230 143A61121 SKIN BOEING 737 737790 13844CN NM CARGO DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 649AS 30663 FWD CARGO DOOR EXTERIOR SKIN IS DENTED WITH CREASE 16 INCHES AFT OF FWD EDGE AND 30 INCHES FROM LOWER EDGE REF SAD 60917 18. REPAIRED FWD CARGO DOOR EXTERIOR SKIN IAW ASA EA 5230 01396. 2 L 7 2 4F RT A16WE 2008012400316 20080124 00316 GL 2008 1 24 LR7A08022 2 20080116 A 7321 4409703 FUEL CONTROL LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL NR 3 ENGINE MALFUNCTIONED A LR7A O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 AL 03 402LC 4698 DURING DESCENT TO PANC, FLIGHT CREW REPORTED NR 3 ENGINE FLAMED OUT. NR 3 FUEL CONTROL AND COORDINATOR REPLACED PER ALL ISON MM 73-1-4 PG 201-203 AND 73-3-0 PG 201-202. OPS CHECK GOOD IAW LAC JOB CARD HN7101. 2 H 7 4 4T 4 T A1SO E282 2008012400369 20080124 00369 EU 2008 1 24 USAA920080177 1 20080112 A 5320 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 885 CLT - MAJOR REPAIR - RON, PILOT REPORT - CORROSION ON CABIN FLOOR SUPPORT, BS 808 / FR 20, -Y765. REPAIRED CABIN FLOOR SUPPORT, BS 808 / FR 20, -Y765 IAW A319 SRM 53-11-14. 2 L 7 2 4F RT A28NM 2008012800089 20080128 00089 SO 2008 1 28 FDKA200801027 1 20080115 A 2612 FIRE DETECTOR EMB 145 EMB145LR 3260212 SO NR 1 NACELLE FAILED A FDKA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 839MJ 145416 FDM 6173 TLH (1445 PHX LCL) - ABORTED TO DUE TO NR 1 ENGINE FIRE DETECT FAIL. MX PERFORMED GVI OF THE NR 1 ENGINE. NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008012800149 20080128 00149 NM 2008 1 28 08FDEA00225 1 20080122 A 5753 ARC40081 HINGE FITTING DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING, OUTBOARD FLAP INBOARD HINGE FITTING ARC4008 OUTBOARD FASTENER HOLE FOUND CORROSION. LT WING, OUTBOARD FLAP R & R AS PER AMM 27-50-30-4. FLAP ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00-830-805. TEST OF THE FLAP OPERATION/RANGE OF MOVEMENT CARRIED OUT AS PER AMM 27-50-00-710-801. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008012800180 20080128 00180 WP 2008 1 28 UPS08851409 1 20080102 A 5320 975407015 WEB DOUG DC8 DC871F 302199D WP BS 320-340 L23R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 WEB ABOVE A PIT DOOR CUT OUT BETWEEN STA 320-340 HAS CORROSION. REPAIRED WEB ABOVE A PIT DOOR CUT OU T BETWEEN STA 320-340 PER SRM 53-02-00 FIG 23. 2 L 7 4 4F RT 4A25 2008012200311 20080122 00311 NE 2008 1 22 200801091 2 20080106 A 7397 CONNECTOR EMB ERJ170 ERJ170100SE 3260406 NM GE CF34 CF348E5 30061 NE FMU DIRTY A UHLA L ABORTED APPROACH O OTHER AP APPROACH 1 GL 11 645RW 1700064 193245 FLIGHT 9405 DSM TO ATL ON FINAL APPROACH THE CREW EXPERIENCED AN UN-COMMANDED MAXIMUM THRUST ON ENGINE NR 1 LASTING FOR APPROXIMATELY 5 TO 10 SECONDS AND THEN THE THRUST ON THE ENGINE RETURNED TO NORMAL. THE CREW DISENGAGED THE AUTO THROTT LES AND CONTINUED THE APPROACH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED CONNECTOR PINS TO THE FMU. 2 L 7 2 4F 4 F RT A56NM E00063EN 2008012200314 20080122 00314 NM 2008 1 22 UPS08651388 1 20080108 A 3350 GUARD BOEING 767 76734AF 1385212 NM COCKPIT DEFECTIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 334UP 32844 INSPECTION TYPE:N/A PLACING GUARD DOWN ON EMERGENCY LIGHT SWITCH DISARMS EMERGENCY LIGHTS. RE-POSITIONED WIRE CLIP DEVI CE ON EMERGENCY LIGHTS SWITCH PER MM 33-50-00, OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2008012200321 20080122 00321 2008 1 22 SA08001 4 20080105 A 2215 31075440 CONTROL SERVO AIRBUS A319 A319112 3930323 EU ELEVATOR FAILED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 19 703UW 26395 0904 MCO FLT 1120 - EN ROUTE RSW TO DCA. AFTER TAKEOFF FROM RSW, THE AIRFRAME BEGAN TO SHUTTER FIVE TIMES. FLIGHT DIVERTED TO MCO WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT HAND ELEVATOR GREEN SYSTEM, AND RIGHT HAND ELEVATOR BLUE SYSTEM SERVOS. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2008012200333 20080122 00333 NM 2008 1 22 ZZDA2008006 1 20080108 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM CABIN UNSERVICEABLE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 947AT 55010 ARRIVED ON PLANE 2125Z. STANDBY LIGHTS ON. PLANE ARRIVED ON GATE AT 1900Z. REMOVED AND REPLACED EMERGENCY PWR PACKS A S PER M/M 33-51. 2 L 7 2 4F TR A6WE 2008012200334 20080122 00334 NM 2008 1 22 ZZDA2008007 1 20080106 A 3350 8039491 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 947AT 55010 E-PATH LIGHTS & OVERWING EXIT SIGNS (LOWER) INOP FROM ROW 20 TO ROW 24. INSTALLED SERVICEABLE EMER LIGHT POWER SUPPLY & BATTERY AT RIGHT ROW 25 IAW AMM 33-51-03. OPS CHECK GOOD. 2 L 7 2 4F TR A6WE 2008012200336 20080122 00336 NM 2008 1 22 08FDEA00144 1 20080115 A 5347 BAC15201466 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 SEAT TRACK CORRODED, STA 849 - 870, LBL 44-47 CORROSION DAMAGE EXCEEDED LIMITS SRM 53-10-1. REMOVED SEAT TRACK REF SRM 551-30-2 PG 1. FABRICATED REPLACEMENT TRACK REF DWG 69-4121. TREATED AND PRIMED REF SRM 51-10-2, INSTALLED REPLACEM ENT SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F RT A3WE 2008012200360 20080122 00360 EU 2008 1 22 TRAX200800080 1 20080110 A 5720 STRUCTURE AEROSP ATR72 ATR72 EU WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 ON TOP WING BOX AT RT SIDE BETWEEN FR 25 23D SUPPORT TUBULAR FOUND CRACKED. 2 H 7 2 4T RT 2008012200365 20080122 00365 NM 2008 1 22 DLM88080007 1 20080105 A 5330 5936003501 SKIN DOUG MD88 MD88 3023688 NM BS 637 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 955DL 49886 FUSELAGE SKIN AND DOUBLER AT THE FORWARD EDGE OF THE C2 CARGO DOOR CUTOUT WAS DAMAGED BY GROUND EQUIPMENT. CUTOUT DAMAG E AND INSTALLED A REPAIR DOUBLER/TRIPLER. 2 L 7 2 4F RT A6WE 2008012200380 20080122 00380 EU 2008 1 22 TRAX200800088 1 20080112 A 5730 SKIN AEROSP ATR72 ATR72 EU RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 CRACK FOUND ON RIGHT WING LOWER SKIN AT RIB 19. 2 H 7 2 4T RT 2008012300003 20080123 00003 WP 2008 1 23 08FDEA00156 1 20080115 A 5230 AFA71321 SUPPORT FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 UPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 3 IS CRACKED IN HOLE "B" BEYOND SRM LIMITS. REPLACED SUPPORT FITT ING NUMBER 3 MAIN CARGO DOOR SPOOL LOCATION IAW SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2008012300020 20080123 00020 EU 2008 1 23 2008UALA00002 1 20080102 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN CHAFED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 481UA 1559 EMERGENCY LIGHT TEST FAILS 3 SVC CK. FOUND WIRES CHAFED UNDER SEAT 4ABC. REPAIRED WIRES AT 4ABC, TESTS ALL NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012300027 20080123 00027 NM 2008 1 23 2008UALA00069 1 20080104 A 5230 6591700866 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FORWARD CARGO DOOR AFT FRAME CRACKED AT LOWER INBOARD FASTENER OF LOWER STOP FITTING. INSTALLED NEW FRAME. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300029 20080123 00029 NM 2008 1 23 2008UALA00070 1 20080104 A 5230 DOOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD CARGO BAY DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FWD CARGO DOOR HAS A DENT TOWARDS TOP PORTION OF DOOR. FOUND DENT AT AFT UPPER 1-3RD OF DOOR. DENT MEASURES 4"L X 2.5" W X .250"D. A OVER Y IS 10. REMOVED DAMAGE AND OLD DOUBLER. INSTALLED NEW LARGE AREA DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300040 20080123 00040 WP 2008 1 23 08FDEA00159 1 20080115 A 5230 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 UPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 7 IS CRACKED IN HOLES "A, B, D" BEYOND SRM LIMITS. REPLACED SUPPO RT FITTING NR 7 MAIN CARGO DOOR SPOOL LOCATION IAW SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2008012300041 20080123 00041 EA 2008 1 23 SWIA200819062 1 20080108 A 3310 LIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT SHORTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 710BR 7852 PILOT'S FLOODLIGHT IS SHORTED OUT. REPLACED PILOTS FLOOD LIGHT ASSEMBLY IAW CRJ200 AMM 33-11-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008012300043 20080123 00043 SO 2008 1 23 SWIA200819064 1 20080115 A 2731 ACTUATOR EMB 120 EMB120ER 3260203 SO ELEVATOR TRIM MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 297SW 120327 ELEVATOR TRIM IS DIFFICULT TO MOVE TOWARDS THE "NOSE UP" POSITION IN FLIGHT, FLIGHT NR 3677. REPLACED BOTH TRIM ACTUATO RS AS WELL AS THE LEFT DAMPENER ASSEMBLY. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2008012300070 20080123 00070 NM 2008 1 23 2008UALA00080 1 20080106 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 LEFT LWR FUSELAGE STRINGER CLIP DAMAGED, BS 787 STR 22L. INSTALLED NEW STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300078 20080123 00078 NM 2008 1 23 2008UALA00091 1 20080106 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 532UA 25072 FRAME AT STA 1280, STR 27L IS DAMAGED. A TIME LIMITED REPAIR AT FRAME STA 1280 AND STR 27L WAS REMOVED PER UAL EVA I MC-30128 FOR REPLACEMENT WITH A PERMANENT REPAIR. THE EXISTING REPAIR DID NOT PASS DTA ANALSYS. REMOVED EXISTING REPAI R AND TRIMMED OUT THE BS 1280 FRAME FLANGE TO REMOVE ALL DAMAGE AND FABRICATED A NEW REPAIR ANGLE AND FILLER AND INSTAL LED BETWEEN STR 26L -28L. THIS REPAIR IS TIME LI MITED FOR 12 MONTHS FROM 02JAN08 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300091 20080123 00091 NM 2008 1 23 2008UALA00111 1 20080106 A 3350 1317 LAMP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 DOOR 3R FWD SILL & DOOR 4L BOTH SILLS EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012300096 20080123 00096 NM 2008 1 23 DL76L080029 1 20080109 A 5412 311T32819 BULKHEAD BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 171DN 24759 DURING ACCOMPLISHMENT OF SB 767-54-0080, A CRACK WAS FOUND IN ONE OF THE FASTENER HOLES IN THE AFT BULKHEAD FITTING. TH E HOLE WAS REAMED TO REMOVE THE CRACK AND A BUSHING WAS INSTALLED TO RETURN THE HOLE TO THE DESIGN DIAMETER PER ER/A INS TRUCTIONS. 2 L 7 2 4F RT A1NM 2008012300112 20080123 00112 NM 2008 1 23 2008UALA00124 1 20080105 A 2611 21198356 SMOKE DETECTOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CARGO BAY FAULTY A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 787UA 26939 DETECTOR FAN 1 CARGO FWD STATUS MSG DISPLAY & DET CHANNEL 1 E-E SMOKE STATUS MSG DISPLAY. SUSPECT FAULTY SMOKE DETECTO R. REPLACED FWD LWR CARGO SMOKE DETECTOR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008012300131 20080123 00131 2008 1 23 DL76G080050 4 20080113 A 3414 4039891906 INDICATOR BOEING 767 767332 1382001 NM COCKPIT FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1608 99064100 30573 AT FL350 M.78 FLIGHT CREW DETECTED ACRID ODOR AND SAW A SMALL AMOUNT OF SMOKE COMING FROM ABOVE THE CENTER GLARE SHIELD. ALL OFF FLAGS APPEARED ON F/O`S IAS/MACH INDICATOR AND IAS/MACH C/B OPENED ON RT SIDE. REMOVED FO`S IAS/MACH INDICATO R. INDICATOR APPEARS TO BE SHORTED. SWAPPED F/O`S INDICATOR WITH CAPTS IAS/MACH INDICATOR. PERFORMED AIR DATA COMPUTE R TEST. ALL INDICATIONS NORMAL. REINSTALLED CAPTS INDICATOR IN ORIGINAL POSITION. NEEDS INDICATOR DPN 341002534 NIS D KR 478834. INSTALLED FOS IAS/MACH INDICATOR PER MM. OPS CK GOOD. 2 L 7 2 4F RT A1NM 2008012300132 20080123 00132 NM 2008 1 23 DLM90080053 1 20080113 A 3260 PROXIMITY SENSOR DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE LT MLG MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 901DA 53381 020105 LT MAIN GEAR RED LIGHT WAS SLOW TO EXTINGUISH AFTER TAKEOFF. ASSOCIATED OAP MESSAGE AUTO SPOILER FAIL. QRH PROCEDURE F OR AUTOSPOILER FAIL MESSAGE DID NOT EXTINGUISH MESSAGE. RETURN SLC AS DIRECTED BY COMPANY. CHECKED NOSE GEAR PROX SENS ORS WIRES AND TARGETS ALL CK GOOD REPLACED PROX ELECTRONICS UNIT PER M/M. REPLACED BOTH NOSE PROX SENSORS D1-32 D1-31 S WUNG GEAR PER M/M ALL OPS NML. 2 L 7 2 4F 4 F RT A6WE E40NE 2008012300137 20080123 00137 NM 2008 1 23 2008UALA00138 1 20080107 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 DOOR 1L, LOWER HINGE CUTOUT CRACKED IN AFT EDGE OF FUSELAGE SKIN BEARSTRAP, REF NR13042-8000-0004. REMOVED DAMAGE & ACP NDT & INSURANCE CUT. FABRICATED & INSTALLED REPAIR FILLERS & STAINLESS STEEL EXTERNAL DOUBLER IAW EA I070960. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR FILLERS AND STAINLESS STEEL EXTERNAL DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300141 20080123 00141 NM 2008 1 23 2008UALA00143 1 20080107 A 2611 824PTY SMOKE DETECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD LAVATORY FAULTY A UALA O OTHER W N INADEQUATE Q C FALSE WARNING IN INSP/MAINT 1 WP 29 337UA 24241 FWD LAV SMOKE DETECTOR ALARMS INTERMITTANTLY. REPLACED SMOKE DETECTOR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300143 20080123 00143 2008 1 23 2008UALA00145 4 20080108 A 2565 100000308 O-RING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE BOTTLE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 507UA 24743 LOW BOTTLE. FOUND CENTER SHAFT O-RING LEAKING. REPLACED O-RING, SERVICED O2 SYSTEM, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300151 20080123 00151 EU 2008 1 23 08FDEA00131 1 20080115 A 2133 VST165D OUTFLOW VALVE AIRBUS 310 A310324 3930206 EU CABIN PRESSURE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 815FD 638 AFTER T/O, OVERBOARD VALVE FAULTED. REMOVED AND REPLACED OVERBOARD EXTRACT VALVE (75HR) IAW MM 21-23-13-4. OPS CHK NOR MAL. 2 L 7 2 4F RT A35EU 2008012300171 20080123 00171 CE 2008 1 23 DXTA200802779 1 20080120 A 3260 1EN114N119 SQUAT SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 845QS 5223 258545 AFTER LANDING GEAR RETRACTION, RT MAIN GEAR UNLOCKED ANNUNCIATOR ILLUMINATED. REPLACED RT LANDING GEAR WOW SWITCH IAW RAC DWG. 25-8 NAS-2584. OPS.CK GOOD.REF: (HBS-LIT) W/O 19-1608. 2 L 7 2 4F 4 F RT A3EU E6WE 2008012300177 20080123 00177 NM 2008 1 23 2008UALA00165 1 20080110 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 SEAT EELS INOP: 4E & 5E BOTH SECTIONS. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012800184 20080128 00184 WP 2008 1 28 UPS08851419 1 20080104 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FS 1690 L28R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 AFTER REMOVAL OF EXISTING REPAIR AT L28R STA 1690, FOUND L28R CRACKED AND INTERNAL DOUBLER CUT. REMO VED AND REPLACED L28R AND INTERNAL DOUBLER AT STA 1690 IAW SRM 53-05-01 FIG 007 AND DWG 5649328. 2 L 7 4 4F RT 4A25 2008012800186 20080128 00186 NM 2008 1 28 08FDEA00126 1 20080114 A 5730 65507481 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 RIGHT WING FUEL TANK ACCESS PANEL 641JB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 641JB PER SRM 57-20- 01. FOUND TO BE OUT OF LIMITS PER SRM 57-20-01, FIG 201, DETAIL I SECTION AA, NOTE B. CORROSION WITHIN 0.10" OF SEAL. REPLACED PANEL 641JB IAW AMM 28-11-01. 2 L 7 2 4F RT A2NM 2008012900005 20080129 00005 SO 2008 1 29 RAIA00801009 1 20080109 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 850HK 145003 PRE FLT 7982 - IAD - LEFT OVERWING EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BULB. OPS CHECKED G OOD. 2 L 7 2 4T RT T00011AT 2008012900006 20080129 00006 SO 2008 1 29 RAIA00801011 1 20080110 A 2760 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO SPOILER CONTAMINATED A RAIA O OTHER N FALSE WARNING LD LANDING 1 CE 03 832HK 145771 FLT 7948 - IAD - CREW REPORTED A SPOILER FAIL MESSAGE ON THE EICAS. SPOILERS WERE INDICATED AS BEING OPEN. NO CONTROLL ABILITY ISSUES REPORTED BY CREW. MAINTENANCE REMOVED GREASE RESIDUE FROM THE LT SPOILER PROX SWITCH. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012900008 20080129 00008 SO 2008 1 29 RAIA00801014 1 20080111 A 3230 355022002 CONTROL UNIT EMB 145 EMB145EP 3260221 SO LANDING GEAR MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 827HK 12545 381 145021 FLT 5500 - STL - SPS ADVANCE MESSAGE ON THE EICAS DURING CLIMB. MAINTENANCE REMOVED AND REPLACED THE LGEU. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2008012900010 20080129 00010 SO 2008 1 29 RAIA00801016 1 20080111 A 2160 C1431232 CONTROL VALVE EMB 145 EMB145LR 3260212 SO CABIN TEMP MALFUNCTIONED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 818HK 145059 FLT 5524 - RIC - CREW REPORTED LOUD RUMBLE SOUND AFTER T/O. IT APPEARS TO COME FROM UNDERNEATH THE FLOOR OF THE COCKPIT . MAINTENANCE REMOVED AND REPLACED THE DUAL TEMP CONTROL VALVE, PERFORMED OPS CHECK WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008012900012 20080129 00012 SO 2008 1 29 RAIA00801017 1 20080112 A 3230 355022002 CONTROL UNIT EMB 145 EMB145LR 3260212 SO LANDING GEAR MALFUNCTIONED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 818HK 145059 FLT 5584 - RIC - NOSE GEAR DOORS WOULDN'T CLOSE. MAINTENANCE REMOVED AND REPLACED THE LGEU AND PERFORMED SEVERAL GEAR E XTENSIONS AND RETRACTIONS. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080910 NM 2008 9 10 CALA0800786 1 20080813 A 5311 143A1113 FRAME BOEING 737 737724 13844BY NM BS 440 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 21723 28790 FRAME CRACKED STATION 440 AT S-9L. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04819. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 CALA0800788 1 20080813 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM BS 400 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16632 27900 FRAME CRACKED STATION 400 AT STR 9LT. TRIMMED OUT CRACKED AREA AND INSTALLED REPAIR DOUBLERS PER EA 5310-04498 OP 2. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 CALA0800789 1 20080813 A 5347 6546813 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 328-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 RIGHT INBOARD SEAT TRACK HAS CORROSION FROM FS 328-344. REMOVED SEAT TRACK PER B737 SRM 51-40-02, FABRICATED SEAT TRACK SECTION PER B737 SRM 53-00-52, ALODINED AND PRIMED SEAT TRACK PER B737 SRM 51-20-01, INSTALLED SEAT TRACK PER B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 CALA0800790 1 20080813 A 5340 693535271 STRINGER CLIP BOEING 737 7373T0 1384582 NM BS 727D S23L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 STRINGER CLIP AT STATION 727D S23L CRACKED. REMOVED AND REINSTALLED STRINGER CLIP AT STATION 727D S23L PER B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 CALA0800791 1 20080813 A 5230 6546921 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 CRACK AT FORWARD CARGO DOOR HANDLE 22.25 INCHES FROM LOWER EDGE AND 17 INCHES FROM AFT EDGE. REMOVED FASTENER, VERIFIED CRACK CONTAINED AT FASTENER HOLE. REPAIRED DAMAGE PER 737-300 SRM 52-00-01 FIG 201. 2 L 7 2 4F RT A16WE 20080910 NM 2008 9 10 2008UALA04194 1 20080808 A 3510 O-RING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU OXYGEN MASK LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 CREW O2 INDICATES 680 PSI. FOUND THE JUMP SEAT MASK CONNECTION POINT TO ACFT O-RING DAMAGED. REPLACED WITH NEW MASK, OP S MASK NORMALLY, SERVICED O2. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080910 NM 2008 9 10 2008UALA04200 1 20080809 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 307UA 23668 EMERGENCY LIGHT STRIP IN AFT OF AC IS LOOSE. FOUND BROKEN LIGHT ASSEMBLY. REPAIRED LIGHTASSEMBLY OP CHECK GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080910 NM 2008 9 10 2008UALA04276 1 20080813 A 3150 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 673UA 29241 RIGHT ENG PRV EICAS AND BLEED LT CAME ON COMING OUT OF THRUST REVERSE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012300178 20080123 00178 NM 2008 1 23 2008UALA00166 1 20080110 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 WALL EEL INOP: RIGHT SIDE WALL AFT GALLEY. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012300192 20080123 00192 NM 2008 1 23 08FDEA00174 1 20080116 A 5311 BAC1517706 FRAME BOEING 727 727233 138408A NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 CABIN BS 500 FRAME INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT S11R BLENDED DAMAGE, REMOVED MAXIMUM OF .03 6" FROM ORIGINAL FRAME THICKNESS OF .056" WITH .020" REMAINING. OUT OF LIMITS. FABRICATED REPAIR DOUBLER AND INSTALLED . 2 L 7 3 4F RT A3WE 2008012300193 20080123 00193 EU 2008 1 23 08FDEA00175 1 20080116 A 5344 A5237161000000 HINGE AIRBUS 310 A310203 3930313 EU CARGO DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN CARGO DOOR HINGE SEGMENT DAMAGED FOWARD OF DOOR ACTUATOR. ACCOMPLISHED INTERIM REPAIR PER EA 6-5230-116948, PART 1. INSTALLED A STRAP IN PLACE OF HINGE NR 2 - 22 WITH BOLTS. MAIN CARGO DOOR AND ALL HINGES TO BE REPLACED AT A LATER DATE PER PART 2 OF EA 6-5230-116948. 2 L 7 2 4F RT A35EU 20080911 EU 2008 9 11 08FDEA03704 1 20080902 A 5311 A57111131200 FRAME AIRBUS 300 A300B4605R 3930308 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND DURING MODIFICATION IAW EO 6-5310-7-5015 PT. 2 FOUR ELONGATED HOLES IN FRAME FOOT AT C 43, P 36 LT. REPAIR PERFO RMED BY REAM UP THE HOLES , NDT FOR CRACK FREE CONDITION IAW RAS/70513493/2008 ISS. A, APPROVED BY EA 6-5315-123137. 2 L 7 2 4F RT A35EU 20080911 NM 2008 9 11 QXEA200800402 1 20080418 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK ZONE 144 SUBFLOOR IS CORRODED AT Y546 AND Y35.5L. REMOVED CORROSION IAW CPM CHAP 4. REMOVED .003 MATERIAL FROM .045 ORIGINAL THICKNESS, .042 MATERIAL REMAINING WITHIN LIMITS IAW -8 200 SRM 51-20-11 STEP 3. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. ALODINED PRIMED PAINTED IAW -8 200 SRM 51-20-16, 51-20-36 PG 6 PARA F(1) AND 5 1-20-26 PG 8 PARA B(1-6). 2 H 7 2 4T RT A13NM 20080911 NM 2008 9 11 QXEA200800410 1 20080418 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 333 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK FUSELAGE INTERIOR WEB THAT TIES INTO LT O/B SEAT TRACK HAS AN OVERSIZED HOLE LOCATED 2" AFT OF FRAME 333.30 0. REMOVED WEB BETWEEN FRAMES 333.30 AND 354.25 NEXT TO LH O/B SEAT TRACK. FABRICATED NEW WEB IAW T/C 2-53-836. INSTA LLED WEB IAW -8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 20080912 NM 2008 9 12 SWAA084748 1 20080827 A 3297 B06002 CIRCUIT CARD BOEING 737 7373H4 1384600 NM MLG FAULTY A SWAA O OTHER N FALSE WARNING DE DESCENT 1 SW 29 313SW 23335 WHEN GEAR EXTENDED FOR LANDING, NOSE GEAR DOWNLOCK WARNING LIGHT ILLUMINATED. REMOVED AND REPLACED M125 CIRCUIT CARD PE R MM. 2 L 7 2 4F RT A16WE 20080912 EA 2008 9 12 SWIA200819995 1 20080824 A 2697 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA FIRE DETECTION DIRTY A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 965SW 7871 LEFT FIRE FAIL CAUTION MESSAGE IS INTERMITTENT. FLIGHT 6541. CLEANED AND RE-INSTALLED CONNECTOR PINS AND PLUG. OPS CH ECK GOOD. 2 L 7 2 4F RT A21EA 20080912 NM 2008 9 12 UPS08M53095 1 20080731 A 5720 SUPPORT ANGLE DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 281UP 48538 INSPECTION TYPE:2C, LT WING FIXED L/E ANGLE SUPPORT AT STA XORS 346 FOUND CRACKED. REMOVED, FABRICATED AND INSTALLED AN GLE IAW MD-11 SRM 51-33-01 DWG ARB2918 AND SRM 51-21-01. 2 L 7 3 4F RT A22WE 20080912 WP 2008 9 12 UPS08853076 1 20080727 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FS 1500 LBL 29 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 MAIN CABIN, FLOOR PNL HAS CRUSHED HONEYCOMB STA 1500 LBL 29. REMOVED PNL, FABRICATED AND INSTALLED R EPLACEMENT FLOOR PNL IAW MM 53-21-02, EO DC8-5320-9691C. 2 L 7 4 4F RT 4A25 20080915 NM 2008 9 15 08FDEA03158 1 20080730 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL ACCESS PANEL CUTOUT 541DB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93, REPAIR 5. REPAIR IS CLASSIFI ED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080915 NM 2008 9 15 08FDEA03161 1 20080730 A 5753 SKIN BOEING 727 727233 138408A NM LT WING TE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 275FE 22040 T/E OF LT OB FOREFLAP HAS (2) EA DEEP GOUGES ON UPPER SURFACE. REMOVED DAMAGED AREA IAW SRM 51-40-20 PAGE 12. FABRICAT ED FILLER AND DOUBLER IAW SRM 51-40-20 PAGE 59. HOT BONDED FILLER AND DOUBLER ON SEALED EDGES AND PRIMED AREA IAW SRM 5 1-40-20 PARAGRAPH 7-22. 2 L 7 3 4F RT A3WE 20080915 EU 2008 9 15 08FDEA03124 1 20080729 A 5340 A53910530531 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 CE 21 743FD 630 DURING SB53-6123 INSPECTION, SEVERAL CRACKS AND TOOL MARKS WERE FOUND ON BOTH LT AND RT IN SPLICE, IN FR 47 FORWARD AND AFT FITTING. REPAIR PERFORMED BY DEPENDING OF AREA OVERSIZING HOLES, PERFORMING SMOOTH REWORK AND SPOT FACING IAW RAS 7 0511944/017/2008 ISSUE A AND EA 6-5310-120093. 2 L 7 2 4F RT A35EU 20080915 NM 2008 9 15 08FDEA03152 1 20080730 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL ACCESS PANEL CUTOUT 541LB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIE D AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080915 WP 2008 9 15 08FDEA03021 1 20080722 A 5414 AUB703625 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 NR 3 PYLON PANEL 488 AL IS CHAFED. FABRICATED DOUBLER AND FILLER IAW SRM 51-21-01;VOL II; FIG 2-B. ALODINED AND PRIMED FILLERS IAW SRM 51-21-01; VOL II. INSTALLED REPAIR PARTS IAW SRM 54-00-01; VOL I; FIG 2-B AND EA 8-5480-123601. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 08FDEA03023 1 20080723 A 5330 APB74471 SKIN DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 597FE 48596 MAIN DECK CARGO AT APPROXIMATELY STATION 1229, X = 75.5 TO X = 107.50, UPPER AUX TANK UPPER SURFACE FOUND CORROSION. MAIN DECK CARGO STATION 1229, X = 75.5 TO X = 107.50, UPPER AUX TANK UPPER SURFACE CORROSION AREA CARRIED OUT REPAIR AS PER EA NR 1-5710-122539 THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. CORROSION REMOVED AS PER SRM 51-21-01, VOL .II. FOUND EXCEEDED LIMIT AS PER SRM 57-20-00, FIG 13, VOL I. 2 L 7 3 4F RT A22WE 20080910 NM 2008 9 10 2008UALA04279 1 20080814 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 FAULTED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 775UA 26947 ELEC GEN DRIVE L LEFT IDG FAULT (LOW INTERNAL OIL PRESSURE). FOUND IDG FAULTY. REPLACED NR 1 IDG. OPS & LEAK CHECKS N ORMAL. OKAY FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 2008 9 11 2008UALA03841 4 20080711 A 2397 1203139 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SATCOM BROKEN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 656UA 25394 SATCOM UNAVAILABLE FOR ENTIRE FLIGHT. FOUND FAULTY CONNECTOR AT HIGH POWER RELAY, SHIELD BROKEN. REPLACED CONNECTOR, O P CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03996 1 20080727 A 3350 GE1317 LAMP BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT SLIDE LIGHT BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 AFT LT EXTERIOR SLIDE LT INOP FWD FAIRING. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECK GOOD. AC OK FOR SERV ICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04310 1 20080815 A 5210 BRACKET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR SLIDE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 SLIDE PACK AT DOOR 2L NEEDS SECURING. SLIDE FELL OFF SLIDE PACK SHELF DUE TO BROKEN BRACKET. REPLACED SLIDE ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080911 NM 2008 9 11 2008UALA04320 1 20080816 A 3510 2766008 REGULATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OXYGEN PRESS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 CREW O2 BOTTLE REG OUTPUT IS 9 PSI LOW, RANGE SHOULD BE BETWEEN 70 AND 85 PSIG. FOUND FAULTY REGULATOR. REPLACED CREW OXYGEN PRESSURE REGULATOR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080911 NM 2008 9 11 2008UALA04321 1 20080816 A 2421 729825G IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RIGHT FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 595UA 28748 RIGHT GENERATOR OFF LIGHT ILLUMINATED, THEN A SHORT TIME LATER RIGHT GENERATOR DRIVE LIGHT ILLUMINATED. FOUND FAULTY ID G. REPLACED NR 1 IDG. RAN, OP CHECKED & LEAKED CHECKED. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080911 2008 9 11 2008UALA04328 4 20080815 A 2565 143N61032 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR SLIDE DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 DOOR 2L SLIDE BOTTLE DISCHARGED. REPLACED DOOR ASSIST BOTTLE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080911 NM 2008 9 11 2008UALA04329 1 20080817 A 8012 7755386 START VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE STICKING A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 544UA 25322 CREW REPORT: LEFT START VALVE FAILED TO OPEN WITH EICAS MESSAGE. START VALVE INOP- SOLENOID CLOGGED, HARDWARE (INTERNA L) DAMAGED. REPLACED START VALVE AND OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080911 NM 2008 9 11 2008UALA04333 1 20080818 A 3000 ANTI-ICE VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 204UA 28713 ANTI ICE VALVE FAILURE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NM 2008 9 11 2008UALA04338 1 20080818 A 7700 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE FALSE ACTIVATION A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 643UA 25093 L OIL FILTER EICAS ON CLIMB FROM FL 320 TO 360 MESSAGE DISAPPEARED AT L-O STATUS MSG REMAINS. CHECKED & REPLACED FILTER , CHECKED CHIP DETECTORS. FOUND OKAY. ACCOMPLISHED 5 MIN RUN WITH NO FAULTS. REPLACED DIFFERENTIAL OIL PRESS SWITCH. LE AK CHECK OF SWITCH TESTS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NE 2008 9 11 2008UALA04340 2 20080819 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE RIGHT FOD A UALA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 29 792UA 26934 222026 RIGHT ENGINE MOMENTARY OVERTEMP AFTER TAKEOFF. THE ENGINE WAS SUBSEQUENTLY REMOVED FROM SERVICE AT SFO ON 8/23/08. SHO P TEARDOWN REVEALED A MISSING HPT STAGE-2 DUCT SEGMENT AT 7:00. SEGMENT HAD METALLIC MATERIAL LODGED IN ONE OF ITS OUTE R DIAMETER COOLING HOLES, INHIBITING COOLING AIR FROM ENTERING THE INTERNAL COOLING PASSAGES; SOURCE UNKNOWN. THE OVERT EMP WAS IN AREA "B"; THIS DOES NOT REQUIRE HPT BLADE SECTIONING. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NM 2008 9 11 2008UALA04342 1 20080818 A 2121 4100945A FAN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT SMOKE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 769UA 26921 SMOKE/FUMES IN COCKPIT. FLIGHT DIVERTED. FOUND RECIRC FAN FAILURE CAUSE OF SMELL. REPLACED UPPER FWD RECIRC FAN. REPL ACED EE SMOKE DETECTOR (P/N 2118860-4). A/C CLEARED FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NE 2008 9 11 08FDEA03093 2 20080726 A 7320 HMU DOUG MD11 MD11F 3023600 NM GE CF6 CF680 30025 NE NR 2 ENGINE FAILED A FDEA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 CE 21 576FE 43413 48501 702831 APPROACHING CRUISE ALTITUDE GOT A LEVEL 2 'ENG 2 N2 LOW' FOLLOWED BY A ROLL BACK ON ENG 2. ALL INDICATIONS INDICATED FL AME OUT. ACCOMPLISHED QRH PROCEDURES AND LANDED WITHOUT INCIDENT. DID NOT ATTEMPT A RESTART. PERFORMED ENGINE POST-WI NDMILLING INSPECTION PER MM 72-00-05-6 FOUND OK, RUN ENGINE NR 2 PER JRH FOUND ENGINE RUN NORMAL, ALL PARAMETERS IN LIMI TS. FUEL FILTER INSPECTED & FOUND CLEANED. REPLACED WITH NEW ONE. REMOVED AND REPLACED HMU AS PER 73-21-01-4 1 RUN UP & LEAK TEST OK. INSPECTED NR 2 MANIFOLD FOR CRACKED PIPING, NONE FOUND. ALSO ACCOMPLISHED FUEL SHROUD TEST PER MM 28- 25-00-5 CHECKED OK. ZERO FUEL AND NO LEAKS. 2 L 7 3 4F 4 F RT A22WE E13NE 20080911 NM 2008 9 11 08FDEA02846 1 20080714 A 5230 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 597FE 48596 DURING OPEN-HOLE HFEC INSPECTION ON 0.460" HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDIC ATIONS AT HOLES A, B, C AND D. MAIN CARGO DOOR JAMB NR 1 FITTING REMOVED AND REPLACED AS PER SRM 51-33-01, VOL II. THI S REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080911 NM 2008 9 11 08FDEA02848 1 20080714 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM DOOR FRAME CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 597FE 48596 DURING OPEN-HOLE HFEC INSPECTION ON 0.460" HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDIC ATIONS AT HOLES B. FITTING AT NR 3 MAIN CARGO DOOR LOWER JAMB REMOVED AND REPLACED AS PER SRM 51-33-01, VOL II. THIS R EPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080910 2008 9 10 COMA086367 4 20080823 A 3418 STALL WARNING CNDAIR CL600 CL6002C10 1390015 EA FALSE ACTIVATION A COMA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 27 669CA 10176 ENROUTE FROM JFK TO MSP RECEIVED STALL FAIL MSG. EMERGENCY DECLARED. ACFT LANDED SAFELY IN MSP. RESET STALL PROTECTIO N SYSTEM PER CRJ AMM. NO FURTHER DEFECTS NOTED. 2 L 7 2 4F RT A21EA 20080910 CE 2008 9 10 FFSA200800005 1 20080822 A 5610 1013840205 WINDSHIELD BEECH 1900 1900C 1154161 CE HARTZL HCB4M HCB4MP3 GL COCKPIT CRACKED A FFSA O OTHER O OTHER NR NOT REPORTED 1 AL 01 575X 9963 UC149 ATA 56-10-00 PILOT’S WINDSHIELD OUTER PANE CRACKED ENROUTE TO BRW. ACFT MADE NORMAL LANDING IN BRW AND RETURNED TO FAI , PART 91, IAW POH/AFM LIMITATIONS SECTION GUIDANCE, PAGE 2-16. 2 L 7 2 4T RT A24CE 6 C P56GL 20080910 EA 2008 9 10 COMA086364 1 20080824 A 5210 FRAME CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 779CA 7306 PAX DOOR INNER FRAME AT 338.9 IS CRACKED. CORRECTIVE ACTION: REPAIRED PER EO 601R 52-11-402. 2 L 7 2 4F RT A21EA 20080911 NM 2008 9 11 2008UALA03944 1 20080719 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT EEL LIGHT INOP LOWER WALL EEL ACROSS LAV 104. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHE CK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03945 1 20080719 A 3350 7945243 POWER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT EEL LIGHT INOP LOWER WALL EEL ACROSS LAV 102. *S/D* FOUND BROKEN POWER CABLE. REPLACED POWER CABLE, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03946 1 20080719 A 3397 7945243 POWER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT EEL LIGHT INOP AT DOOR 5L AFT LOWER WALL EEL. *S/D* FOUND BROKEN POWER FEEDER CABLE. REPLACED FEEDER C ABLE, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03934 1 20080723 A 3397 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY EXIT EEL LIGHT INOP JUST AFT OF SEAT 8 LEFT BELOW COAT CLOSET. *S/D* FOUND BROKEN POWER FEEDER CABLE. REPLA CED FEEDER CABLE, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA04013 1 20080728 A 3397 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 WALL EEL INOP RT SIDE LAV 112. *S/D* FOUND BROKEN POWER FEEDER CABLE. REPLACED FEEDER CABLE, OP CHECK GOOD. AC OK FO R SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA04000 1 20080727 A 3397 362624 CONNECTOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 EEL INOP AT L-AFT LAV. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04001 1 20080727 A 3397 362624 CONNECTOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 EEL INOP AT R-AFT LAV. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04052 1 20080729 A 2611 21188604 SMOKE DETECTOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CREW REST AREA FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 221UA 30552 SMOKE DETECTOR AT FLIGHT CREW REST LOWER BUNK HAS FAILED. *S/D* FOUND FAULTY SMOKE DETECTOR. REPLACED LOWER BUNK SMOK E DETECTOR TEST PASSED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NM 2008 9 11 08FDEA02849 1 20080714 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 597FE 48596 DURING OPEN-HOLE HFEC INSPECTION ON 0.460" HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDIC ATIONS AT HOLES A, C AND D. MAIN DECK CARGO DOOR LOWER JAMB FITTING NR 4 REMOVED AND REPLACED AS PER SRM 51-33-01 VOL I I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080911 NM 2008 9 11 08FDEA02850 1 20080714 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 597FE 48596 DURING OPEN-HOLE HFEC INSPECTION ON 0.460" HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CRACK INDIC ATIONS AT HOLES B AND D. HOLES B AND D AT MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 REPAIRED AS PER SRM 53-50-00, FIG 10, VOL I. REPAIR BUSHINGS, FABRICATED AS PER SRM 53-50-00, FIG 10, VOL I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2 -100. 2 L 7 3 4F RT A22WE 20080911 NM 2008 9 11 08FDEA02851 1 20080714 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 597FE 48596 DURING OPEN-HOLE HFEC INSPECTION ON 0.460" HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK IND ICATIONS AT HOLES A, C AND D. FITTING AT MAIN CARGO DOOR LOWER JAMB NR 7 REMOVED AND REPLACED AS PER SRM 51-33- 01 VOL II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080915 WP 2008 9 15 UPS08853080 1 20080727 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FS 1490 RBL 57 CRUSHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 MAIN CABIN FLOOR PANEL HAS CRUSHED HONEYCOMB STA 1490 RBL 57. REMOVED FLOOR PANEL, FABRICATED AND IN STALLED REPLACEMENT PANEL IAW MM 53-21-02, EO DC8-5320-9691. 2 L 7 4 4F RT 4A25 20080915 NM 2008 9 15 SWAA084768 1 20080827 A 5311 6546557 FRAME BOEING 737 7373T0 1384582 NM BS 887 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 SWAA084751 1 20080827 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 500D S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED HC2 CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 16R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 SWAA084752 1 20080827 A 5240 69457633 FITTING BOEING 737 7373H4 1384600 NM R2 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 UPS08M53097 1 20080810 A 5712 RIB DOUG MD11 MD11F 3023600 NM LEFT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 281UP 48538 INSPECTION TYPE:2C LEFT WING FIXED L/E RIB XFS 1024 CRACKED ON AFT SIDE BETWEEN FASTENERS. REMOVED, FABRICATED, AND INS TALLED RIB IAW MD-11 SRM 51-33-01 AND DWG ARB2920. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 UPS08553115 1 20080813 A 5420 SUPPORT BOEING 757 75724APF 1384969 NM NR 1 PYLON GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 453UP 25474 INSPECTION TYPE:MOD NR 1 PYLON UNDERWING FAIRING STRUCTURE, LT SUPPORT BRACE IS GOUGED AND DAMAGED PPS186.0. REMOVED AN D REPLACED PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20080915 NM 2008 9 15 UPS08553116 1 20080815 A 2560 INERTIA REEL BOEING 757 75724APF 1384969 NM SHOULDER HARNESS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 424UP 25369 INSPECTION TYPE:N/A CAPT'S SHOULDER HARNESS INERTIA REEL WILL NOT RETRACT. UNTWISTED SHOULDER STRAP AT INERTIA REEL, SH OULDER STRAPS RETRACT NORMALLY. 2 L 7 2 4F RT A2NM 20080915 EA 2008 9 15 SWIA200820012 1 20080430 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 424-559 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 RT AND LT CABIN FLOOR LINE STRUCTURE CORRODED FROM STA 424RT - 559RT. FOUND AT C-CHECK. REPAIRED PER REO 601R-53-41-72 4. 2 L 7 2 4F RT A21EA 20080915 NM 2008 9 15 UPS08M53118 1 20080817 A 3350 BATTERY PACK DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:N/A EMERGENCY LIGHTS TEST INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY RECHARGEABLE BATTERY PER MM 33-51-01-04, PERFORMED EMERGENCY LIGHTS TEST & OPS CHECK. FOUND SATIS PER MM 33-51-01-5. THIS CLOSES DMI & STIC KER REMOVED. 2 L 7 3 4F RT A22WE 20080915 2008 9 15 SWAA084778 4 20080828 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 214WN 32486 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080915 EA 2008 9 15 SWIA200819965 1 20080819 A 5210 WHEEL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 498CA 7792 FLIGHT ATTENDANT REPORTS THAT THE MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. FLIGHT 2803. INSPECTED, CLEANED AND ADJUS TED PAX DOOR SUPPORT WHEEL IAW 52-11-13. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080915 EU 2008 9 15 08FDEA03437 1 20080815 A 5315 A53974360200 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSION ON CROSSBEAM C 67 REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080915 EU 2008 9 15 08FDEA03384 1 20080812 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CHAFING MARKS ON SLAT NR 1 RT LOWER SKIN. REPAIR PERFORMED BY BLEND OUT THE DAMAGE IAW RAS/FOK/153/2008 ISS A, AP PROVED BY EA 6-5742-120090. 2 L 7 2 4F RT A35EU 20080915 NM 2008 9 15 08FDEA03593 1 20080826 A 5330 AJC70601 SKIN DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 574FE 48499 EMPENNAGE, AFT ACCESSORY COMPARTMENT INTERIOR RIGHT FUSELAGE SKIN AT AROUND BS 2154, (BELOW FIRE EXTINGUISHER BOTTLES) 01 LOCATION FOUND WITH CORROSION. REPAIRED AS PER SRM 53-20-00 FIGURE 13 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 08FDEA03313 1 20080808 A 5710 6521655440 SUPPORT BEAM BOEING 727 727233 138408A NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 275FE 22040 RT WING TRAILING EDGE SUPPORT BEAM CUT OUT ON SPOILER NR 8 IS CRACKED AT WBL 123 REMOVED "J" BEAM IAW B727 SRM 51-30-2 A ND FABRICATED NEW "J" BEAM FROM BAC1506-860 7075-T6. APPROX DIM 81 INCHES IN LENGTH IAW B727 SRM 51-30-5 AND SRM 57-20- 2 FIG 2. TREATED AND PRIMED "J" BEAM IAW B727 SRM 51-10-2 AND INSTALLED NEW "J" BEAM IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 20080915 EU 2008 9 15 08FDEA03330 1 20080808 A 5321 R532B381400000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 251 RT IS DAMAGED. REPAIRED CABIN FLOOR PANEL 251 RT BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARK ED AND APPLIED NON-SKID TAPE IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080915 EU 2008 9 15 08FDEA03342 1 20080808 A 5321 R532B364100000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 242 PF IS DAMAGED. REPAIRED CABIN FLOOR PANEL 242 PF BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARK ED AND APPLIED NON-SKID TAPE IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080915 NM 2008 9 15 08FDEA03595 1 20080826 A 5347 60109647075T6 SEAT TRACK DOUG MD10 MD1030F 3024020 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 304FE 46992 MAIN CARGO DECK STA 1119-1159 RBL 48 SEAT TRACK IS DAMAGED. REPLACED SEAT TRACK IAW SRM 53-70-00. 2 L 7 3 4F RT A22WE 20080915 EU 2008 9 15 08FDEA03598 1 20080826 A 2780 4907905 SLAT SYSTEM AIRBUS 310 A310324 3930206 EU FAILED A FDEA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 CE 21 805FD 9665 9665 456 DURING APPROACH WITH THE LDG GEAR DN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 A ND 2 FAULT LIGHTS ON O/H. DISCONTINUED AP AND FOLLOWED QRH. WHEN THE SLATS/FLAPS CYCLED PER QRH, THE LIGHT/FAULTS CL EARED CONFIGURED AGAIN THE SLATS STUCK AT 15 DEGREES. FOLLOWED QRH FOR SLATS STUCK LNDG. ON FINAL AP FLAP HANDLE AT 40 DEGREES THE SLATS BROKE FREE AND WENT TO 30 DEGREES SLATS WITH 40 DEG FLAPS. THE LANDING WAS UNEVENTFUL AND SLAT/FLA P RETRACTON THE GROUND WAS NORMAL. REMOVED AND REPLACED SFCC'S, OFF MFG 49-079-05 POS 1 SRL 144 OFF MFG 49-079-05 POS 2 SRL 692. GEK BAE SYSTEMS AVIONICS LTD. 2 L 7 2 4F RT A35EU 20080915 NM 2008 9 15 08FDEA03373 1 20080811 A 5320 SUPPORT BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 LT FUSELAGE BS 780-799, S-30 HAS CORROSION ON FWD SUPPORT FRAME AT SEVERAL PLACES. CORROSION FOUND EXCEEDED SRM LIMIT S. REMOVED AND REPLACED SUPPORT FRAME IAW SRM 51-40-02 REV. 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITER IA. 2 L 7 2 4F RT A2NM 20080916 EU 2008 9 16 08FDEA03453 1 20080816 A 5753 A57971445200 SKIN AIRBUS 310 A310203 3930313 EU RT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 430FE 394 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RT WING OUTBD FLAP LOWER MAIN SKIN AT MAIN SPAR TO REAR SPAR AND FROM THE IN BD EDGE TO BETWEEN RIB 2 AND TRACK NR 3, MEASURING 47.7 IN BY 19.9 IN. REMOVED EXISTING REPAIR AND REPAIRED IAW SRM 57- 53-12,FIG 210, PG 259/260. THIS IS AN REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080916 NM 2008 9 16 08FDEA03734 1 20080905 A 5330 6554571 SKIN BOEING 727 727233 138408A NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 SKIN PANEL DENTED STA 615 ON MAIN CARGO DOOR DOUBLER AND TRIPLER AT STR 24L TO 28L. REWORKED SKIN TO ORIGINAL CONTOUR A T BS 620 STR 24L TO 28L IAW FEDEX EA 7-5330-117028, FUSELAGE SKIN PANEL DENT AT STA 615 STR 24L TO 28L REPAIR. INSTALLE D DENT DOT IAW FEDEX GMM 6-3-101. 2 L 7 3 4F RT A3WE 20080916 EU 2008 9 16 08FDEA03246 1 20080804 A 5320 A5378105821500 WEB AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 RIGHT SIDE SUPPORT WEB IS CRACKED BETWEEN FRAME 38.1 AND FRAME 58.2, RBL 90 INCH, CREASE BEAM AREA. REPLACED CABIN RI GHT SIDE SUPPORT WEB BETWEEN FRAME 38.1 AND FRAME 38.2; RBL 90 IN REF TO TO AIRBUS A300-600 SRM 53-14-15. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03247 1 20080804 A 5320 A5378103821500 WEB AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 CABIN RIGHT SIDE SUPPORT WEB IS CRACKED BETWEEN FRAME 38 AND FRAME 38.1; RBL 90 INCH CREASE BEAM AREA. REMOVED BROKEN SUPPORT WEB, LOCATED AND DRILLED THE NEW SUPPORT WEB IAW A300-600 SRM 51-40-21. ALODINED HOLES IN THE WEB IAW A300-600 SRM 51-21-10. PRIMED HOLES IN THE WEB IAW A300-600 SRM 51-23-10. INSTALLED THE NEW SUPPORT WEB IAW A300-600 SRM 51-40- 21 AND DWG NR 14-A537-81963. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03249 1 20080804 A 5210 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 800 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 RIGHT CREW/COURIER EXTERIOR DOOR SKIN IS GOUGED AT THE LOWER FWD CORNER. BLENDED AND FOUND TO BE OUT OF LIMITS IAW A300 -600 SRM 52-11-00; DIF 102. ACCOMPLISHED A DOUBLER REPAIR IAW A300-600 SRM 52-11-00, FIG 206. ALODINED AND PAINTED IAW A300-600 SRM 51-21-10. 2 L 7 2 4F RT A35EU 20080916 NM 2008 9 16 08FDEA03087 1 20080725 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 577FE 48469 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT F ITTING AT HOLES A, C AND D. MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING AT HOLES A, C AND D BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL 1. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. REPAIR CLASSIF IED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080916 WP 2008 9 16 08FDEA03298 1 20080807 A 5711 ARB29187 FORMER DOUG DC10 DC1030F 3023504 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 LT WING L/E INT FOUND CRACK ON FORMER. 2 L 7 3 4F RT A22WE 20080916 WP 2008 9 16 08FDEA03250 1 20080805 A 5320 NGA6030 STRUT DOUG DC10 DC1030F 3023504 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 AFT FUSE WASTE TANK COMPT, FOUND EXFOLIATION CORROSION ON STRUT BULKHEAD. 2 L 7 3 4F RT A22WE 20080916 2008 9 16 08FDEA03276 2 20080806 A 7297 WIRE HARNESS AIRBUS 300 A300F4605R 3930327 EU NR 1 ENGINE FAILED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 21 661FE 760 SHORTLY AFTER T/O, AUTO THROTTLES DISENGAGED AND WOULD NOT RESET. SIMULTANEOUSLY, N1 FOR NUMBER 1 ENGINE FAILED (BOTH ANALOG AND DIGITAL). AUTO THROTTLE REMAINED OFF THE REST OF FLT. FOUND DUCT FOR T/R VALVE WITH A HOLE BLOWN THRU. ALS O, THE HARNESS FOR N1 SENSOR WAS BROKEN ON THE SMALL CONNECTOR, AND THE OTHER ONE WAS HEAT DAMAGED. ORDERED DUCT. REPL ACED ORANGE AND RED ELECTRICAL HARNESSES ON NR 1 ENG PER M/M 71-51-01-4 05. RAN NR 1 ENG PER JRH, ALL INDICATIONS NORMA L AT IDLE. 2 L 7 2 4F RT A35EU 20080916 SO 2008 9 16 LR7A08092 1 20080819 A 5312 3700326539 BULKHEAD LKHEED 382 382G 526414U SO BS 180 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, FOUND UNDERDECK BULKHEAD WEB CRACKED AT FS 180, WL178, RBL12 AND FS180, WL176, LBL24. REPAI RED IAW SB 382-53-51 R1 NR 2004. 2 H 7 4 4T A1SO 20080916 NM 2008 9 16 2008UALA04354 1 20080819 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 566UA 26670 EXTERIOR EMERGENCY LIGHT INOP AT DOOR 1L. RELAMPED DOOR 1L EMER LIGHT. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080916 NM 2008 9 16 2008UALA04361 1 20080820 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 579UA 26697 EXTERIOR EMERGENCY LIGHTS FOR DOORS 2LT & 4LT ARE INOP. RE-LAMPED DOORS 2L AND 4L, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080911 NM 2008 9 11 08FDEA02988 1 20080721 A 5330 AJC70602 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 597FE 48596 EMPENNAGE: UNDER RIGHT BODY FAIRING 347DF, SKIN FROM STATION 2150 TO 2164 FOUND SURFACE CORROSION EAR FASTENER HOLES. EMPENNAGE RIGHT HAND BODY FAIRING 347DF STATION 2150 TO STATION 2164 SKIN REPAIRED AS PER SRM 53-20-00, FIG 15 VOL I A ND SRM 51-33-01 VOL II. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. CORROSION REMOVED AS PER SRM 51-21-01 VOL II. ORIGINAL THICKNESS = 0.100", MATERIAL REMOVED = 0.045", MATERIAL REMAINING = 0.055" AND FOUND EXCEEDED LIMITS AS PE R SRM 53-00-01 FIG 2 VOL I. 2 L 7 3 4F RT A22WE 20080911 NM 2008 9 11 08FDEA03130 1 20080729 A 3260 859803 PROXIMITY SWITCH DOUG MD11 MD11F 3023600 NM RT MLG FAILED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 CE 21 598FE 49139 49139 48597 AFTER T/O DEL, RT MAIN GEAR UNSAFE INDICATION AFTER RETRACTION ON BOTH PRIMARY AND SECONDARY. CYCLE GEAR PER CK LIST, N O HELP. FELT VIBRATION AT 230KTS WHILE WORKING CK LIST AFTER APPROX 10 MIN VIBRATION STOPPED, INDICATION WENT TO SAFE, LIGHT OUT. CHECK ADJ OF RT MLG UP LATCH. RIGHT MLG DOOR LINK & BRACKET ASSY PER MM FOUND ON THE LIMITS. ADJUSTMENT MA DE AS PRECATIONARY MEASURE ONE NOTCH O/B WIRING, CONNECTORS CHECKED ALL FOUND NORMAL. PSEU FAIL TEST 31-71-04-00 ITEM 4 . TEST FAIL. REMOVED AND REPLACED PSEU PER MM 31-71-01, ALL TEST PASS. RETURN TO SERVICE. 2 L 7 3 4F RT A22WE 20080911 EU 2008 9 11 08FDEA03676 1 20080901 A 5330 A53778736204 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND SCRUB MARKS AT OUTER SKIN C 38.1-38.2, P 43-45 RT DOUBLER REPAIR PERFORMED IAW SRM 53-10-12 FIG.225 , APPROVED BY RAS/EFW/9000088/2008 ISS.A AND EA 6-5314-123093. 2 L 7 2 4F RT A35EU 20080911 WP 2008 9 11 08FDEA03695 1 20080901 A 5350 ANB70498 TEE FITTING DOUG MD10 MD1010F 3022112 WP BS 1441 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 THERE IS A CRACKED VERTICAL ANGLE AT THE RT OVERWING TO BODY FAIRING SUPPORT AT STA 1441. REMOVED TEE ANGLE IAW SRM 51- 31-01 VOL II. IAW DWG ANB 7049 REV E. ANNEALED IAW TPS 1003 REV A. FORMED NEW TEE IAW ANB 7049 REV E. LOCATED & DRIL LED IAW SRM 51-31-01 VOL II. ALODINED & PRIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II. INSTALLED IAW SRM 51-31-01 VOL II. PART MARKED IAW GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20080911 EU 2008 9 11 08FDEA03678 1 20080901 A 5330 A53978218200 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND DENT AND SCRATCH IN OUTER SKIN, C59-59A, P 37-38 RH. REPAIR PERFORMED BY REWORK THE DENT AND SCRATCH IAW SRM 51-7 3-10, APRROVED BY RAS/EFW/9000082/2008 ISS.A AND EA 6-5317-123075. 2 L 7 2 4F RT A35EU 20080911 EU 2008 9 11 08FDEA03705 1 20080902 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD FH1139 664 FOUND OLD DOUBLER REPAIR NOT PERFORMED IAW RAS/FOK/138/98 (TOP AND LOWER DOUBLER), LOWER DOUBLER MISSING, RIB 17A-18 TRA ILING EDGE. DOUBLER REPAIR RENEWED IAW RAS/224/2008 ISS.A, APPROVED BY EA 6-5752-123082. 2 L 7 2 4F RT A35EU 20080911 NM 2008 9 11 08FDEA03569 1 20080825 A 5330 AGA7418501 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 AFT LOWER FUSELAGE EXTERNAL SKIN FOUND A DENT WITH DIMENSIONS: D=1"/ Y=0.064" AND SCRATCH 8" IN LENGTH AT FUSELAGE STA 1940. AFT LWR FUSELAGE EXTERNAL SKIN DENT CLASS II REPAIR CARRIED OUT AS PER SRM 53-20-00 VOLUME I FIGURE 2. REQUIRED INITIAL INSPECTION AT 15,000 CYCLES AND REPETITIVE INSPECTION AT 9,800 FLIGHT CYCLES AS PER SRM 53-20-00 VOLUME I FIGUR E 2. REFER TO WRI 5310/26-73 AND OIL CONTROL NUMBER C/0341343. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080911 EU 2008 9 11 08FDEA03708 1 20080902 A 5230 A52378014204 SKIN AIRBUS 300 A300B4622R 3930312 EU CARGO DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND DENT IN BULK CARGO DOOR, C67-68, NEAR BEAM 1. REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR, NDT FOR CRACK FREE CONDITION IAW RAS/DAHAM/4025440/2008 ISS A, APPROVED BY EA 6-5234-123054. 2 L 7 2 4F RT A35EU 20080911 EU 2008 9 11 08FDEA03710 1 20080902 A 5310 FITTING AIRBUS 310 A310222 3930315 EU CARGO DOOR FRAME CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 THE DOOR FRAME FITTING IS CRACKED AT THE AFT CARGO DOOR LOWER AFT CORNER. COMPLIED WITH EA 6-5310-123646. 2 L 7 2 4F RT A35EU 20080911 WP 2008 9 11 08FDEA03712 1 20080903 A 5730 SKIN DOUG MD10 MD1010F 3022112 WP RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 40061 46973 RT WING UPPER SURFACE, LIGHT CORROSION ON UPPER SKIN BEVER TAIL. REPAIRED AREA IAW EA 8-5710-120494. 2 L 7 3 4F RT A22WE 20080912 NM 2008 9 12 USAA920081613 1 20080831 A 5320 65C333701 INTERCOSTAL BOEING 737 7374B7 1384702 NM ZONE 100 CONTAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03C10853030/005 LT AFT LAV SUPPORT INTERCOSTAL CORRODED AT BS 960, LBL 25. REPAIRED LT AFT LAV S UPPORT INTERCOSTAL CORRODED AT BS 960, LBL 25 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20080912 EA 2008 9 12 TRAX200801055 1 20080825 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 932EV 8016 PAX DOOR FWD ANCHOR FITTING IS CRACKED. REMOVED FWD PAX DOOR ANCHOR FITTING IAW AMM 52-11-17-000-804. PAX DOOR FWD ANC HOR FITTING REQUIRES INSTALL. INSTALLED PAX DOOR FWD ANCHOR FITTING IAW AMM TASK 52-11-17-400-804 THROUGH STEP 2A(3). C ABLE REQUIRES CONNECTION TO SWIVEL LEVER AND ADJUSTMENT OF THE PAX DOOR COUNTER BALANCE SYSTEM IS REQUIRED. RECONNECTED CABLE TO SWIVEL LEVER ASSY IAW AMM 52-11-17-820-801. ADJUSTMENT OF PAX DOOR COUNTER BALANCE AND OPS CHECK DUE IAW MM 5 2-11-17-820-801 AND 52-11-17-710-801. PERFORMED ADJ OF PAX DOOR COUNTER BALANCE IAW AMM 52-11-17-820-802. PERFORMED OP S CHECK OF PAX DOOR COUNTER BALANCE IAW AMM 52-11-17-710-802. PERFORMED OPS CHECK OF WHEEL ASSY (PAX DOOR) IAW AMM 52-1 2 L 7 2 4F RT A21EA 20080912 EU 2008 9 12 TRAX200801053 1 20080825 A 3350 COVER AEROSP ATR72 ATR72212 8680945 EU EMERGENCY SIGN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 EMERGENCY EXIT SIGN OVER AFT FA MISSING. FOUND SIGN IN AFT CLOSET, PRIOR RECOVERED, REINSTALLED PLASTIC SIGN COVER ON SI GN, LIGHT. OPS CK GOOD. REF 33-50-00 OPT 100000. 2 H 7 2 4T RT A53EU 20080912 EA 2008 9 12 TRAX200801069 1 20080828 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 682BR 7691 LT AFT EXT. EMERGENCY LIGHT INOP. RESOLVED ON W/O 98667 TASKCARD N/R 00007. R&R AFT BATTERY PACK NR 4 IAW AMM 33-51. OP CHECK GOOD. 2 L 7 2 4F RT A21EA 20080912 NM 2008 9 12 SWAA084790 1 20080828 A 3350 20121 CHARGER BOEING 737 7373T5 1384608 NM EMERGENCY LIGHT FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 RIGHT AFT CABIN EMERGENCY EXIT LIGHTS ON. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 20080912 NM 2008 9 12 SWAA084791 1 20080828 A 3350 417A5604 SIGN BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 711HK 27845 MID CABIN OVERHEAD EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 20080916 NM 2008 9 16 2008UALA04363 1 20080820 A 4920 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU COMPRESSOR LEAKING A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 537UA 25157 GENERATOR INDICATION AND APU EICAS MESSAGE. FLIGHT DIVERTED. FOUND FRONT LOAD COMPRESSOR SEAL LEAKING. REPLACED APU A SSY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080916 NM 2008 9 16 AALA200802009 1 20080801 A 3350 OL3071BPEGPL LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 JFK EMERGENCY LIGHT AT SEAT 25G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25G. SYSTEM GROUND CHECKED NORM AL OPS. (CLOSED) 2 L 7 2 4F RT T00001SE 20080916 NM 2008 9 16 2008UALA04368 1 20080820 A 3350 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 594UA 28145 FWD CLOSET EEL INOPERATIVE. TEST SWITCH IS SHORTED. REMOVED AND REPLACED FWD EMERGENCY LIGHT TEST SWITCH, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080916 NM 2008 9 16 2008UALA04380 1 20080821 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1640 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 MAIN CABIN STA 1640 FLOORBEAM TEE CAP CORRODED AT RBL 55. MAJOR REPAIR ACCOMPLISHED: CUTOUT CORRODED SECTION & INSTALLE D REPAIR PER MM 53-00-98. 2 L 7 2 4F 4 F RT A2NM E17NE 20080916 EU 2008 9 16 2008UALA04187 1 20080808 A 2910 PACKING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD SYSTEM LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 415UA 475 HYDRAULIC PROBLEM. FLIGHT DIVERTED. FOUND MANIFOLD ASSY LEAKING BELOW PRIORITY VALVE. REPLACED PACKING. NO LEAKS FOUN D. 2 L 7 2 4F 4 F RT A28NM E40NE 20080916 2008 9 16 2008UALA04208 4 20080809 A 2565 7A146912 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R5 DOOR OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 175UA 24382 UPPER DECK R DOOR WON'T ARM. IMPROPERLY INSTALLED SLIDE. REPOSITIONED SLIDE ASSEMBLY OP CHECK GOOD. AC OK FOR SERVIC E. 2 L 7 4 4F 4 F RT A20WE E24NE 20080917 NM 2008 9 17 2008UALA04221 1 20080809 A 3350 1013391 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE AFT CREW REST INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY LIGHT AFT CREW REST STAIRS ILLUMINATION LIGHT INOP. FOUND FAULTY LIGHT. REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080917 EU 2008 9 17 2008UALA04242 1 20080812 A 2910 B-NUT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD SYSTEM LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 443UA 820 HYDRAULIC PROBLEM. RTFL. FOUND LT MLG DOOR UPLOCK ASSY B-NUT ON FWD SIDE LEAKING AND 3-4'S OF THE WAY BACKED OFF AND LO OSE. SECURED B-NUT ON ON FWD SIDE OF LT MLG DOOR UPLOCK ASSY. SERVICED GREEN SYSTEM & LEAK CHECK ACCOMPLISHED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080917 NM 2008 9 17 2008UALA04248 1 20080811 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 814UA 862 FLOORBEAM CORRODED (MARKED ). REMOVED FLOORBEAM. TRANSFERRED BRACKETS ONTO NEW FLOORBEAM. INSTALLED FLOORBEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20080917 NM 2008 9 17 ASAA0843356 1 20080723 A 5322 654653170 SHEAR TIE BOEING 737 7374Q8 138447Q NM 500C S28L/R CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 AFT CARGO PIT SHEAR TIE CORRODED STA 500C BETWEEN STR 28L AND STR 28R. CUT OUT DAMAGED SHEAR TIE, FABRICATED SHEAR TIE AND REPAIR PARTS LOCATED, DRILLED AND INSTALLED IAW B737 400 SRM 53 00 07 REPAIR 3 PAGE 201. 2 L 7 2 4F RT A16WE 20080917 NM 2008 9 17 ASAA0843374 1 20080724 A 5313 65516989 STRINGER BOEING 737 7374Q8 138447Q NM BS 887 S4L CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 STRINGER 4L IS CRACKED AT STA 887. REMOVED AND REPLACED DAMAGED STRINGER IAW SRM. 2 L 7 2 4F RT A16WE 20080917 NM 2008 9 17 ASAA0843375 1 20080722 A 5313 65516989 STRINGER BOEING 737 7374Q8 138447Q NM BS 907 S4L CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 STRINGER 4L IS CRACKED FROM FASTENER HOLES AT STA 907. REMOVED AND REPLACED DAMAGE STRINGER IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 SWAA084795 1 20080828 A 5310 6546817 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 440-500A CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 440 TO BS 500A, LBL 70. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 SWAA084796 1 20080828 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 663 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 2008UALA04357 1 20080820 A 3350 EA30043233 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 326UA 23958 EXTERIOR EMERGENCY LIGHT AFT OF DOOR 1L IS INOP. *S/D* REPLACED LIGHT ASSEMBLY. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 20080912 EA 2008 9 12 SWIA200819974 1 20080821 A 2916 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 952SW 7805 AFTER TAKEOFF AND GEAR RETRACTION, RECEIVED A "GEAR DISAGREE" WARNING MESSAGE. RETURNED TO FIELD. FLIGHT 6640. REPLAC ED NR 3 HYDRAULIC RESERVOIR IAW AMM 29-12-30. LEAK CHECK AND OPS CHECK GOOD PER MM 32-30-00 P/N 7301-1, S/N OFF 052A. 2 L 7 2 4F RT A21EA 20080912 SO 2008 9 12 SWIA200819976 1 20080820 A 2710 BUSHING EMB 120 EMB120ER 3260203 SO AILERONS WORN A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 578SW 120346 AILERONS FEEL DIFFICULT TO MOVE. FLIGHT 3604. INSPECTED CABLE RUNS, PULLEYS AND BELL CRANKS. REPLACED AILERON CONTRO L QUADRANT BUSHINGS ON THE LEFT SIDE. OPS CHECK OF AILERON CONTROL SYSTEM IS NORMAL. 2 L 7 2 4T RT A31SO 20080912 SO 2008 9 12 SWIA200819977 1 20080819 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE COCKPIT SMOKE A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 07 221SW 120290 AFTER TAKEOFF, OIL PRESSURE DROPPED TO 0 AND HAD SMOKE IN THE COCKPIT. SHUTDOWN ENGINE AND RETURNED TO FIELD. FLIGHT 5 769. REPLACED LEFT ENGINE ASSEMBLY IAW EMB 120 MM 72-00-00. OPS CHECK GOOD. REPLACED OIL COOLER. NO LEAKS NOTED. S/ N OFF: 115629, P/N 160282-6, S/N OFF 105-823. 2 L 7 2 4T 4 T RT A31SO E20NE 20080912 SO 2008 9 12 SWIA200819981 1 20080822 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO TE FLAPS LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 232SW 120306 RIGHT HYDRAULIC QUANTITY WENT TO ZERO ON TAXI OUT AFTER SELECTING FLAPS. REPLACED RIGHT NACELLE FLAP ACTUATOR IAW MM 27 -50-00. P/N 343100-1001, S/N OFF 235. 2 L 7 2 4T RT A31SO 20080912 NE 2008 9 12 SWIA200819957 2 20080816 A 7497 IGNITION LEAD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* 30015 NE RT ENGINE ARCED A SWIA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 07 368CA 10075 RIGHT ENGINE IGNITION B-IGNITOR AND LEAD SHOW SIGNS OF ARCING. REPLACED THE IGNITION B IGNITOR AND LEAD IAW 74-20-03. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA 20080912 2008 9 12 SWIA200819961 3 20080809 A 6110 PROPELLER EMB 120 EMB120ER 3260203 SO LEFT MALFUNCTIONED A SWIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 NM 07 582SW 120350 PERFORMED GO-AROUND WHEN ENGINES WOULD NOT GO INTO GROUND IDLE. PERFORMED OPERATIONAL TEST OF FLIGHT IDLE STOP SYSTEM I AW AMM 76-13-00 WITH NO FAULTS. REPLACED LEFT PROP ASSEMBLY WITH SERVICEABLE UNIT IAW MM 61-10-00 DUE TO TORQUE. 2 L 7 2 4T RT A31SO 20080912 EA 2008 9 12 SWIA200819944 1 20080804 A 2497 WIRE CNDAIR CL600 CL6002C10 1390015 EA CONNECTOR BURNED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 710SK 10170 FOUND SEVERAL WIRES ON CONNECTOR P1 OF ADG POWER CENTER SHOWING SIGNS OF HEAT DAMAGE. REPAIRED WIRING IAW CRJ SPM 20-33 -00 AND 20-44-05. OPS CHECK GOOD IAW AMM 24-51-00. 2 L 7 2 4F RT A21EA 20080912 SO 2008 9 12 SWIA200819945 1 20080808 A 2621 FIRE BOTTLE EMB 120 EMB120ER 3260203 SO APU BAY EMPTY A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 393SW 120330 APU FIRE BOTTLE DISCHARGED. FLIGHT 5752. REPLACED APU FIRE BOTTLE ASSEMBLY WITH A SERVICEABLE ASSEMBLY. OPS CHECK GOO D. 2 L 7 2 4T RT A31SO 20080912 EA 2008 9 12 SWIA200819952 1 20080811 A 3350 CHARGER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 707SK 10003 FORWARD GALLEY EMERGENCY EXIT SIGNS ARE INOPERATIVE. REPLACED NR 1 BATTERY CHARGER PER AMM 33-51-17. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200819983 1 20080821 A 3230 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A SWIA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 07 927SW 7693 EXTENDED LANDING GEAR ON APPROACH AND RECEIVED A NOSE GEAR DISAGREE MESSAGE. WENT AROUND AND RECEIVED NORMAL GEAR DOWN INDICATIONS. FLIGHT 6831. REPLACED NOSE GEAR SELECTOR VALVE PER AMM 32-22-20. OPS AND LEAK CHECK GOOD. P/N 750006-00 0, S/N OFF 2029. 2 L 7 2 4F RT A21EA 20080912 NM 2008 9 12 SWAA084789 1 20080828 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20080912 EA 2008 9 12 SWIA200819990 1 20080826 A 2421 820465 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA ADG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 916SW 7634 ADG DEPLOYED AFTER TAKEOFF WITH BOTH GENERATORS OPERATING. RETURNED TO FIELD. FLIGHT 6701. REPLACED ADG AUTO DEPLOY C ONTROLLER PER CRJ 200 MM 24-23-15 AND STOWED ADG PER MM 24-23-1. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200819991 1 20080826 A 4930 LINE CNDAIR CL600 CL6002B19 1900309 EA FUEL MANIFOLD LEAKING A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 905SW 7437 STRONG JET FUEL ODOR IN COCKPIT AND CABIN WHEN APU BLEEDS ARE USED. FLIGHT 6099. REPLACED THE PRIMARY AND SECONDARY FU EL MANIFOLD LINES PER AMM 49-31-09. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200819964 1 20080812 A 3350 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 951SW 7795 AFT STRIP OF FLOOR EMERGENCY LIGHTS ARE INOP. FLIGHT 5846. REPLACED NR 4 EMERGENCY LIGHT POWER INVERTER AS REQUIRED. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 20080912 NM 2008 9 12 SWAA084757 1 20080827 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 457WN 33856 EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080912 EA 2008 9 12 SWIA200820000 1 20080830 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 944SW 7764 PAX DOOR LATCH HANDLE VERY DIFFICULT TO OPEN AND CLOSE. FLT 6018. INSPECTED DOOR AND PERFORMED OPS CHECK OF MAIN CABIN DOOR HANDLE IAW AMM 52-11-00, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080912 SO 2008 9 12 SWIA200819996 1 20080822 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT FAILED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 568SW 120343 FORWARD SECTION OF EMERGENCY LIGHTS ARE NOT WORKING. FLIGHT 3599. REPLACED NR 1 ELBP IAW MM 33-51-04. OPS CHECK GOOD. P/N D366-04-001, S/N OFF 1329. 2 L 7 2 4T RT A31SO 20080912 WP 2008 9 12 UPS08853099 1 20080626 A 5312 BULKHEAD DOUG DC8 DC871F 302199D WP BS 683 LBL21 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C2 FWD ACCESSORY COMPT BULKHEAD AT STA 683 LBL 21 BELOW FASTENER PATTERN ATTACHING BULKHEAD DOME TO WING LOWER FRONT SPAR WEB HAS 3 INCH CRACK. REMOVED WEB, REPLACED WEB IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 20080912 EA 2008 9 12 SWIA200820003 1 20080902 A 5210 ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 903SW 7425 CORROSION FOUND ON PAX DOOR LOWER ANGLE. REPLACED LOWER PAX DOOR ANGLE IAW SRM 53-21-13. 2 L 7 2 4F RT A21EA 20080912 SO 2008 9 12 SWIA200820006 1 20080903 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN MISSING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 BOTH FORWARD RED EMERGENCY LIGHTS, FLOOR STRIP, MISSING AT ROW 2. REMOVED 1 RED LIGHT FROM ROW 9 AND INSTALLED BY FORWA RD HATCH DOOR IAW 33-51-02. 2 L 7 2 4T RT A31SO 20080912 EA 2008 9 12 SWIA200820009 1 20080430 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 CRACK INDICATIONS NOTED AT AFT PRESSURE BULKHEAD LINTEL ATTACHMENT FITTING UPPER AND LOWER CORNER AREA. FOUND AT C-CHEC K. REPAIRED PER REO 601R-53-61-1230 REV C. 2 L 7 2 4F RT A21EA 20080915 WP 2008 9 15 08FDEA02999 1 20080721 A 5330 AFA30761 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 FUSELAGE EXTERNAL SKIN HAS A BULGING AREA AT FS 1781 AND LONGERON 49 L. THE BULGR HAS A CREASE AND IS OUT OF LIMITS PER SRM 53-20-00; FIG 13; SHEET 2; VOL I, PARA 1-B. CUT OUT THE DAMAGE AND FABRICATED A REPAIR DOUBLER; TRIPLER AND F INGER DOUBLERS PER SRM 53-20-00; FIG 6; SHEET 5; VOL I. INSTALLED THE REPAIR DOUBLER; TRIPLER AND FINGER DOUBLERS PER SRM 53-20-00; FIG 6; SHEET 5; VOL I. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 08FDEA03156 1 20080730 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL ACCESS PANEL CUTOUT 541GB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93, REPAIR 5. REPAIR IS CLASSIFI ED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080915 NM 2008 9 15 08FDEA03157 1 20080730 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL ACCESS PANEL CUTOUT 541FB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93, REPAIR 5. REPAIR IS CLASSIFI ED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080915 NM 2008 9 15 08FDEA03163 1 20080730 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 SURGE TANK ACCESS PANEL CUTOUT 643BB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01, REV 93, REPAIR 5. REPAIR IS C LASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080915 WP 2008 9 15 08FDEA03165 1 20080730 A 5754 ARB16192 SKIN DOUG DC10 DC1030F 3023504 WP RT NR 2 SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 DURING INSPECTION RT WING SLAT NR 2 FOUND CRACK ON INNER SKIN. 2 L 7 3 4F RT A22WE 20080915 EU 2008 9 15 08FDEA03177 1 20080730 A 5347 A5378193720100 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CABIN CROSS SEAT TRACK AT FRAME 30; LBL 30 IS CRACKED. REMOVED AND REPLACED THE ADAPTER ASSEMBLY IN REF TO SRM 51- 40-21; PARA 7. APPLIED CIC PROTECTION IN REF TO AMM SUP 51-22-00-0. 2 L 7 2 4F RT A35EU 20080915 WP 2008 9 15 08FDEA02962 1 20080717 A 5730 ARC0797509 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING FAIRING PANEL 536 BL HAS DENTS. REPAIRED THE DENTS ON THE LT WING OUTBD FAIRING PANEL 536 BL WITH REPAIR DOUB LERS IAW SRM 51-71-00; VOL II. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 08FDEA03180 1 20080730 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 906FD 27148 MAIN CARGO DECK SEAT TRACK STA 1540-1640 LBL 24 CORRODED REMOVED SEAT TRACK IAW SRM 51-41-02. RECEIVED AND FABRICATED N EW SEAT TRACK ON MAE TRAV NR T8/746699, MAT ID BAC1520-792, 7178T6511 IAW SRM 53-00-52 FIG 201, BATCH NR 00013400254 AND LOCATED, TRIMMED, AND DRILLED IAW SRM 51-41-02. TREATED AND PRIMED IAW SRM 51-21-00 AND INSTALLED NEW SEAT TRACK IAW S RM 51-41-02. 2 L 7 2 4F RT A2NM 20080915 EU 2008 9 15 08FDEA03219 1 20080803 A 5330 A53986101200 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 430FE 394 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT SIDE FUSELAGE SKIN BETWEEN FRAMES 80/82 TO 84 AND BETWEEN STRINGERS 29 TO 32 LT, THE REPAIR DOUBLER MEASURES 10.1 INCHES BY 12 INCHES WITH A SKIN CUTOUT MEASURING 2.5 INCHES BY 2.1 INCHES. R EPAIR NOT IAW SRM REQUIREMENTS. REMOVED REPAIR RIVETS AND INSTALLED CORRECT REAPAIR. REPAIR RIVETS ON REPAIR DOUBLER L OCATED ON LEFT SIDE FUSELAGE SKIN BETWEEN FRAMES 80/82 TO 84 AND BETWEEN STRINGERS 29 TO 32 LT IAW SRM 53-10-12 FIG 203 AND FIG 225 SHEET 1. 2 L 7 2 4F RT A35EU 20080915 NM 2008 9 15 08FDEA03181 1 20080730 A 3260 39140165505 UNLOCK CYLINDER DOUG MD11 MD11F 3023600 NM MLG MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 CE 21 598FE 48597 GEAR RETRACT AFTER T/O, RT MAIN UNSAFE A ON PRIMARY AND SECONDARY. TWR STATED RT MAIN GEAR STILL DOWN, OTHERS UP. RAN CHK LIST, NO HELP AFTER GEAR RECYCLE. SETTING UP FOR RTN TO ORIGIN, HEARD SOUND OF GEAR DOOR CLOSING, UNSAFE LIGHT OUT, GEAR NORMAL ON CONFIG SD IN WORK. PERFORMED TEST MAIN GEAR AND GEARWELL DOOR OPERATION AS PER MM 32-31-00-5. PERFORMED THIS TEST 3 TIMES AND 3 TIMES THE RT MLG DID NOT RETRACT. R & R RT MAIN LANDING GEAR UNLOCK CYLINDER AS PER MM 32-33- 02-4. PERFORMED TEST MAIN GEAR AND GEARWELL DOOR OPERATION AS PER MM 32-31-00-5. PERFORMED 6 TIMES LANDING GEAR RETRAC TION AND EXTENTION AND 6 TIMES THIS TEST WAS OK. 2 L 7 3 4F RT A22WE 20080915 EU 2008 9 15 08FDEA03129 1 20080729 A 5311 A57110531530 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 DURING INSPECTION FOUND DAMAGE ON FR 47 LT FORWARD AND AFT FITTING, S21-26L. REPAIR PERFORMED BY SMOOTH REWORK AND SPOT FACING IAW RAS 70511944/017/2008 ISSUE A AND EA 6-5310-120093. 2 L 7 2 4F RT A35EU 20080918 NM 2008 9 18 2008UALA05476 1 20080826 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ROW 16 UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 EMERGENCY LIGHT INOPERATIVE ROW 16 AND AFT. SECURED EMERGENCY LIGHT AND OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080918 NM 2008 9 18 2008UALA03884 1 20080715 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 259 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 FOUND DENT ON RT FUSELAGE STA 259.5 DENT IS 6 INCHES FWD OF FWD LAV SVC DOOR. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVE D DAMAGED FUSELAGE SKIN AND BEGAN LAYOUT OF REPAIR FASTENERS. COMPLETED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 20080918 NM 2008 9 18 2008UALA04359 1 20080820 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 520 S24-25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 FWD CARGO PIT, DENT ON FUSE FRAME UPPER FLANGE AT STA 520, STR 24L TO 25L. *S/D* MAJOR REPAIR ACCOMPLISHED: REPAIRED WITH J-SECTION REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NM 2008 9 18 2008UALA04287 1 20080814 A 3350 20121 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 510UA 24780 OUTSIDE SLIDE LIGHT IS INOP AT DOOR 4L. *S/D* REPLACED M10818 POWER SUPPLY BATTERY ASSY, OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NM 2008 9 18 2008UALA04360 1 20080820 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1701 S19L, DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 BS 1701 SKIN REPAIR S-19L AND S-20L IS INADEQUATE. *S/D* MAJOR REPAIR ACCOMPLISHED: REMOVED REPAIR FASTENERS AND TRIM MED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NM 2008 9 18 2008UALA04366 1 20080810 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 32H BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 SEAT 32H EMERGENCY LIGHT BROKEN. *S/D* REPLACED LIGHT & OP CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 NM 2008 9 18 2008UALA04370 1 20080820 A 5753 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT WING TE FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 RIGHT WING O/B FLAP 12 INCHES FROM I/B END AND 48 INCHES FROM AFT END, SKIN IS WORN. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080918 NM 2008 9 18 2008UALA04371 1 20080820 A 5753 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT WING TE FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 LT WING O/B FLAP 12 INCHES FROM I/B END AND 48 INCHES FROM AFT END, SKIN IS WORN. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080918 2008 9 18 2008UALA04133 4 20080804 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR SLIDE UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 580UA 26698 DOOR 2L DIFFICULT TO DISARM. *S/D* LANYARD AND D-RING -WERE INTERFERING WITH GIRT BAR. SECURED LANYARD AND D-RING WER E INTERFERING WITH GIRT BAR. DOOR ARMS AND DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NM 2008 9 18 2008UALA04377 1 20080821 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 575UA 26689 EXTERIOR EMERGENCY LIGHT BY DOOR 2L AND LT OVERWING ESCAPE HATCH FWD LIGHT INOP. FOUND BULBS INOP. RELAMPED BULBS, ALL OPS TEST NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 EU 2008 9 18 UPS08153220 1 20080820 A 5321 B5327076900400 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 138UP 0821 INSPECTION TYPE:1C MAIN CARGO FLOOR PANEL 252OJ HAS A FIELD REPAIR. REPAIRED MAIN CARGO FLOOR PANEL 252OJ REF SRM 53-10 -20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20080918 EU 2008 9 18 UPS08153221 1 20080820 A 5321 B5327078100000 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 138UP 0821 INSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 251SJ HAS FIELD REPAIR. REPAIRED MAIN CARGO FLOOR PANEL 251SJ REF SRM 53-10-2 0 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 2008012200005 20080122 00005 NM 2008 1 22 KCSA081003 1 20080108 A 5413 STRINGER BOEING 747 7472B4B 138481B NM NR 3 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 3 PYLON OUTBOARD SIDE CHORD IS CRACKED AT NAC STA 135, WL 164.58. 2 L 7 4 4F RT A20WE 2008012200072 20080122 00072 CE 2008 1 22 DJFA2008003 1 20080113 A 3240 BRAKE ASSY RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG WEAK E DJFA O OTHER O OTHER LD LANDING 1 EA 23 815TA 258534 CREW REPORTED THE BRAKES NEEDED EXCESSIVE FORCE TO APPLY BRAKING ACTION. PEDALS WENT NEARLY TO THE FLOOR. THE SAME PRO BLEM WAS REPORTED TWO DAYS PRIOR (REF SDR DJFA2008002) AND THE AIRCRAFT FLEW 5 FLIGHTS WITHOUT DISCREPANCIES. MAINTENAN CE BLED THE BRAKE CONTROL VALVE AND FOUND NO AIR IN THE SYSTEM. BRAKE SYSTEM CHECKED GOOD. 2 L 7 2 4F 4 F RT A3EU E6WE 2008012200093 20080122 00093 NM 2008 1 22 KCSA081008 1 20080110 A 5320 WEB BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 MAIN DECK FUSELAGE L1 DOOR THRESHOLD WEB IS CORRODED ON BOTTOM SIDE AT STA 461. 2 L 7 4 4F RT A20WE 20080915 NM 2008 9 15 08FDEA03200 1 20080731 A 5330 SKIN BOEING 757 75723A 1384967 NM BS 810 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 LIGHTNING STRIKE AT BS 810, S7L. LIGHTNING STRIKE DAMAGE REPAIR CARRIED OUT IAW SRM 53-00-01 REV 93, FIG 201 REPAIR 6, SECT II PARA 3. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080915 WP 2008 9 15 08FDEA02944 1 20080716 A 5210 NBA6062523 BEAM DOUG MD10 MD1010F 3022112 WP L1 DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 L-1 DOOR INTERIOR, NR 3 BEAM IS CRACKED AT THE UPPER FLANGE AFT SIDE. REPAIRED THE L-1 DOOR NR 3 BEAM USING 0.032, 7075 -T6, PO 577146.6; 0.050, 7075-T6, PO 565544.1 IAW DC/MD-10 SRM 52-00-01; VOL I. 2 L 7 3 4F RT A22WE 20080911 NM 2008 9 11 2008UALA03942 1 20080719 A 3350 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT EEL LIGHT INOP AT DOOR 4L GALLEY AREA LOWER WALL EEL. *S/D* FOUND DAMAGED FEEDER CABLE. REPAIRED CABLE , OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03826 1 20080710 A 3350 GE1317 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 EEL LIGHT INOP RIGHT AFT DOOR EXTERIOR SLIDE LIGHT. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03930 1 20080723 A 3397 362624 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY EXIT EEL LIGHT INOP JUST AFT OF DOOR 1L LOWER WALL EEL. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, O P CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03989 1 20080726 A 2150 20224324 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT A/C PACK FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 648UA 25285 RIGHT PACK INOP LIGHT ON. S/D* FOUND FAULTY ACTUATOR. REPLACED ACTUATOR PER MM 21-53-04, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03834 1 20080710 A 3350 362624 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 FLOOR EEL INOP AFT GALLEY CROSS AISLE. *S/D* FOUND BURNED OUT LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03935 1 20080723 A 3397 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY EXIT EEL LIGHT INOP JUST TO THE RIGHT OF LAV 100 LOWER WALL EEL. *S/D* FOUND BROKEN POWER FEEDER CABLE. REP LACED FEEDER CABLE, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03932 1 20080723 A 3397 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY EXIT EEL LIGHT INOP FROM SEATS 6L THRU 8L. *S/D* FOUND BROKEN POWER FEEDER CABLE. REPLACED FEEDER CABLE, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03933 1 20080723 A 3350 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY EXIT EEL LIGHT INOP ACROSS LAV 104 LOWER WALL EEL. *S/D* FOUND BROKEN POWER FEEDER CABLE. REPLACED POWER FE EDER CABLE, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 2008 9 11 2008UALA03861 4 20080713 A 2565 7A146724 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R4 DOOR OUT OF POSITION A UALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 WP 29 116UA 26908 THE 4R MED SLIDE-RAFT FELL OFF FROM ITS MOUNTS DURING TAKEOFF. SLIDE REMAINS JAMMED AGAINST F/A JUMP SEAT. *S/D* SUSP ECT PACK BOARD LATCH WORN OUT. DOOR 4R SLIDE REPLACED PER AMM 25-60-01. OPS CHECK NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03998 1 20080727 A 3397 58791 WIRE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 EEL LT AT FWD X-AISLE INOP. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NE 2008 9 11 2008UALA04003 2 20080727 A 7261 ACC434F65 OIL FILTER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE NR 2 ENGINE DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 664UA 29236 STATUS MESSAGE "R OIL FILTER" DISPLAYED ON EICAS. *S/D* REPLACED RIGHT ENGINE MAIN OIL FILTER ALONG WITH OIL FILTER DP SWITCH. REF MM 79-21-05 AND 79-35-01. OPS AND LEAK CHECK OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04084 1 20080801 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY LIGHT INOP: DOOR 4L AFT SILL. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECK GOOD. AC OK FOR SERVIC E. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012200119 20080122 00119 EU 2008 1 22 TRAX200800041 1 20080104 A 5720 PLATE AEROSP ATR72 ATR72 EU RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 RIGHT WING BOX AT FR 28A FACE PLATE FOUND CRACKED. FACE PLATE AT FR 28A RIGHT WING BOX REPLACED IAW SRM 51-25-01. REPA IR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDA NCE WITH SRM 51-25-01. SUPPLEMENTAL SDR CLOSED 1/10/08. 2 H 7 2 4T RT 2008012200125 20080122 00125 EU 2008 1 22 COEA0801911 1 20080108 A 3297 D227010001 WIRE HARNESS AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NLG UP RT WORN A COEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 13 911FX 045 AIR TURN BACK. FLT NR 8804. AFTER TAKE OFF THE LANDING GEAR WOULD NOT RETRACT. CREW ATTEMPTED SEVERAL CYCLES BEFORE EL ECTING TO RETURN. GEAR LIGHTS RED AND GREEN, WOULD CYCLE BETWEEN GEAR DOWN AND LOCKED AND UNLOCKED. NO EMERGENCY WAS D ECLARED AND THE PLANE LANDED NORMALLY AND SAFETY. REPLACED NOSE LANDING GEAR WIRE HARNESS. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008012200138 20080122 00138 CE 2008 1 22 AMWA89439BC 1 20080105 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 162ZV 16413 95 UE162 BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINTENANCE FOUND EACH CELL TO BE LOW VOLTAGE, CLEANED POSITIVE BATTER Y TERMINAL CORROSION, RETORQUED CELL LINKS, AND CHARGED BATTERY THEN CLEARED DISCREPANCY. 2 L 7 2 4T 4 T RT A24CE E26NE 2008012200162 20080122 00162 NM 2008 1 22 2008UALA00101 1 20080104 A 3510 STOWAGE BOX BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU O2 MASK CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 FIRST OFFICERS O2 MASK STORAGE BOX CRACKED ON LT DOOR. SUSPECT BROKEN DUE TO PRE FLIGHT CHECKS. REPLACED F-O O2 MASK ST ORAGE BOX. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012200164 20080122 00164 EU 2008 1 22 F3LA200800006 1 20080108 A 5320 D531128200101 DUMMY RAIL AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 15198 5495 2051 DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON THE DUMMY RAIL SURFACE AND IN NUT CLIP HOLE AT STATION Y503.2 (LT SIDE ) JUST FORWARD OF FRAME 16 ON THE IB SIDE OF THE BEAM. DRILLED A NEW DUMMY RAIL IAW THE REQUIREMENTS OF SRM 51-44-11 AN D INSTALLED THE DUMMY RAIL IAW THE REQUIREMENTS OF SRM 51-42-11. AFTER THE MAINTENANCE ACTION WAS COMPLETED IT WAS INSP ECTED AND FOUND ACCEPTABLE. REFERENCE NON-ROUTINE C035856. 2 L 7 2 4F 4 F RT 2008012200171 20080122 00171 EU 2008 1 22 TRAX200800058 1 20080107 A 5320 INTERCOSTAL AEROSP ATR72 ATR72 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 INTERCOSTAL AND CHORD ANGLE CORRODED BETWEEN FR 38-39 STR 17L. INTERCOSTAL REPLACED IAW SRM 51-25-01. 2 H 7 2 4T RT 2008012200172 20080122 00172 SW 2008 1 22 WGEA200800007 1 20080117 A 3244 M16901 TIRE ECLIPS EA500 ECLIPSEEA500 3350000 SW MLG FAILED E WGEA O OTHER O OTHER LD LANDING 1 EA 27 158DJ 13 000074 DISC NR 2-RT MAIN TIRE FAILED ON LANDING. SUPPLEMENTAL INFORMATION-REMOVED FAILED TIRE. INSPECTED RT AXLE, GEARDOOR,UNDE R WING, FUSELAGE AND RT ENGINE. NO DEFECTS NOTED. INSTALLED SERVICEABLE WHEEL ASSY IAW MM 32-42-00. OK FOR SERVICE. 1 L 7 2 4J RT A00002AC 2008012200175 20080122 00175 EA 2008 1 22 TRAX200800059 1 20080108 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR TORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 754EV 10173 EXIT STICKER ON AIRSTAIR DOOR IS TORN. 2 L 7 2 4F RT A21EA 2008012200176 20080122 00176 NM 2008 1 22 LYNX0005 1 20080109 A 5610 80260008 WINDSHIELD BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA COCKP;IT FAILED A 3LYA B EMER. DESCENT O OTHER CR CRUISE 1 NM 21 502LX 277 4168 AT FL 250, THE FO WINDSHIELD OUTER PANE SHATTERED. CREW DECLARED AN EMERGENCY AND DIVERTED TO COS. MAINTENANCE WENT TO C OS AND INSTALLED A NEW WINDSHIELD. 2 H 7 2 4T 4 T RT A13NM E00062EN 2008012200190 20080122 00190 CE 2008 1 22 DXTA200802769 1 20080115 A 3233 99125373 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 530 PW535A NE MLG INTERMITTENT E DXTA A UNSCHED LANDING P NO WARNING INDICATION LD LANDING 1 GL 07 631QS 6763 5605131 ON ILS APPROACH GEAR WAS EXTENDED BUT LT MAIN GEAR LIGHTS DID NOT ILLUMINATE. REMOVED LT MLG ACTUATOR AND INSTALLED RE PAIRED ACTUATOR I.A.W. CESSNA 560XL MAINT. MAN. CHAP. 32-30-04, OPS AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00053EN 2008012200252 20080122 00252 EU 2008 1 22 AALA200800010 1 20080101 A 2842 PROCESSING UNIT AIRBUS 300 A300B4605R 3930308 EU FUEL QTY FAILED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 41063 506 PTY INFLIGHT T960/01JAN - CREW REPORTED TOTAL FUEL QUANTITY SYSTEM FAILURE. RETURNED TO PTY AND LANDED WITHOUT INCIDEN T. REPLACED FUEL QUANTITY PROCESSOR UNIT AND RESET AND CLEANED CONNECTORS FOR FUEL PANEL INDICATORS. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008012200253 20080122 00253 2008 1 22 AALA200800018 4 20080102 A 3460 1762000101 COMPUTER BOEING 737 737823 13844BZ NM FLT MANAGE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 929AN 30078 MEX INFLIGHT T2114/02JAN - DURING CLIMB BOTH FLIGHT MANAGEMENT COMPUTERS FAILED. LANDED MEX WITHOUT INCIDENT. BOTH FL IGHT MANAGEMENT COMPUTERS WERE WORKING PRIOR TO ARRIVAL. REPLACED RIGHT AND LEFT FLIGHT MANAGEMENT COMPUTERS. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008012200257 20080122 00257 NM 2008 1 22 AALA200800015 1 20080102 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 977AN 29550 DFW - EMERGENCY LIGHT AT SEAT 11D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008012200261 20080122 00261 NM 2008 1 22 AALA200800012 1 20080102 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT SEAT 31G INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008012200266 20080122 00266 NM 2008 1 22 AALA200800013 1 20080102 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 355AA 24036 JFK - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080911 NM 2008 9 11 2008UALA04086 1 20080731 A 3397 80172424 WIRE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 782UA 26948 SEAT 1F BOTH EEL INOP. *S/D* FOUND BROKEN WIRE IN SPLITTER CABLE. REPAIRED WIRE, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 EU 2008 9 11 08FDEA03677 1 20080901 A 5411 A54611222500 SPAR AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 CORROSION FINDINGS AROUND PYLON NR 2 SPIGOT BEARING HOLES, UPPER SPAR RIB 12-13. REPAIR PERFORMED BY CORRSOION REMOVAL, NDT FOR CORROSION FREE CONDITION AND SURFACE PROTECTION IAW. RAS/70512899/009/2008 ISS.A, APPROVED EA 6-5451-123134. 2 L 7 2 4F RT A35EU 20080911 NM 2008 9 11 08FDEA03570 1 20080825 A 5330 AJC70602 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 EMPENNAGE: UPON AFT FUSELAGE BODY FAIRING REMOVED, FOUND RIGHT HAND FUSELAGE SKIN FAIRING MATING SURFACE WITH MINOR SUR FACE CORROSION. RIGHT FUSELAGE SKIN FAIRING MATING SURFACE CORROSION REMOVED AS PER SRM 51-21-01 VOL II AND FOUND OUT O F LIMIT AS PER SRM 53-00-01 FIG 2 VOL I ORIGINAL THICKNESS = 0.081", MATERIAL REMOVED = 0.042", MATERIAL REMAINED = 0.03 9". REPAIR CARRIED OUT AS PER SRM 53-20-00 FIG 13 VOL I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080911 NM 2008 9 11 08FDEA03519 1 20080820 A 5714 APB74471 SKIN DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 UPPER CARGO COMPARTMENT - CENTER WING TANK UPPER SKIN CORRODED AT STA 1232 LBL 17 UPPER CARGO COMPARTMENT. CENTER WING TANK UPPER SKIN AT STA 1232 LBL 17 CORRODED AREA REPAIRED AS PER FEDEX EA 1-5710-124344 TITLE: WINGS - BASIC WING STRUCT URE - CORROSION AT CENTER WING TANK UPPER SKIN, STATION 1232 - REPAIR. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080912 SO 2008 9 12 C2XA08TY089 1 20080825 A 5751 1456900941050 BRACKET EMB 145 EMB145XR 3260214 SO RT AILERON GOUGED A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 16149 7569 145753 A/C WAS IN A C CHECK STATUS AND THE O/B BUSHION HOLE ON THE PCA BRACKET ATTACH POINT WAS FOUND OVERSIZE ON THE RT AILERO N. MX REPLACED THE PCA BRACKET IAW EC 5750-01177. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED BACK TO SERVICE. 2 L 7 2 4F RT 20080912 NM 2008 9 12 QXEA200800404 1 20080418 A 5310 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK CORROSION ON FORE AND AFT LOWER CORNER COMBING PIECES, I/B FLANGE, ON PAX DOOR APERTURE LOWER EDGE. REMOVE D NUTPLATE FROM CASTING AND REMOVED CORROSION. REMOVED .002" MATERIAL REF CPM SECT 4. WITH IN LIMITS PER -8 200 SRM 51- 20-11. REINSTALLED NUT PLATE ON CASTING. 2 H 7 2 4T RT A13NM 20080912 EA 2008 9 12 TRAX200801048 1 20080823 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA ROW 4C INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 921EV 7819 EMERGENCY LIGHTING AT ROW 4C INOP R & R EMERGENCY LIGHTING STRIP AT 4C. IAW AMM 33-51-01. OPS CK GOOD. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 TRAX200801049 1 20080823 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 846AS 7328 RT INBD FLOOR SEAT TRACK CORRODED FROM FS 559+16 TO 559+80 (RESOLVED ON W/O 96197 TASKCARD N/R 00024) R&R RT INBD SEAT T RACK FROM FS559+16 TO 559+80. PER SRM 51-41-00. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 TRAX200801063 1 20080826 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 932EV 8016 PAX DOOR AFT DRAG ANGLE IS CRACKED. OPEN 2 L 7 2 4F RT A21EA 20080912 NM 2008 9 12 SWAA084792 1 20080828 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 727SW 27859 EEPLS LENS LOOSE AT ROW 16 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080912 NM 2008 9 12 SWAA084793 1 20080828 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 764SW 27878 L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080912 EA 2008 9 12 SWIA200819954 1 20080810 A 3520 OXYGEN MASK CNDAIR CL600 CL6002B19 1900309 EA CABIN UNWANTED DEPLOY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 934SW 7722 THE O2 MASKS IN PAX COMPARTMENT DROPPED WHILE AT THE GATE. FLIGHT 6759. RESTOWED ALL O2 MASKS AND PERFORMED OPERATIONA L TEST OF THE PASSENGER OXYGEN SYSTEM PER AMM 35-20-00-946-01. SYSTEM TEST GOOD. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200819955 1 20080809 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 708SK 10156 EMERGENCY LIGHT POD AT ROW 15 IS INOP. FLIGHT 6444. RELAMPED POD LIGHT, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200819986 1 20080820 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX LACK OF LUBE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 986CA 7174 MAIN CABIN DOOR WOULD NOT OPEN. FLIGHT 2531. LUBRICATED PAX DOOR IAW AMM 12-20-52. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200819988 1 20080824 A 3230 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAILED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 952SW 7805 ON APPROACH WHEN GEAR WAS SELECTED DOWN RECEIVED A GEAR DISAGREE WARNING MESSAGE AND BOTH MAINS DID NOT EXTEND. MANUALL Y EXTENDED GEAR. FLIGHT 5841. REPLACED MAIN GEAR SELECTOR VALVE IAW AMM 32-32-10. REPLACED MAIN GEAR PRIORITY VALVE I AW AMM 32-32-15. OPS CHECK GOOD. P/N 750005000, S/N OFF 0036T, P/N 4619-3. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200819989 1 20080825 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 986SW 7967 CEILING EMERGENCY EXIT LIGHT IS BURNED OUT. FLIGHT 6274. RELAMPED EMERGENCY LIGHT IAW AMM 33-51-16. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080912 NM 2008 9 12 SWAA084758 1 20080827 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 480WN 33998 EEPLS LENS LOOSE AT ROW 3 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080912 NM 2008 9 12 SWAA084746 1 20080827 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SKIN DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER S RM. 2 L 7 2 4F RT A16WE 20080912 NM 2008 9 12 SWAA084747 1 20080827 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND RT WING OUTBOARD FORE FLAP UPPER SKIN DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20080912 NM 2008 9 12 UPS08M53093 1 20080804 A 5730 ARB3954U5 SKIN DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 281UP 48538 INSPECTION TYPE:2C LEFT WING L/E SKIN SPLICE STRAP XFS 669 CRACKED. REMOVED SKIN SPLICE STRAP, REPLACED SKIN SPLICE STR AP IAW MD-11 SRM 51-33-01. 2 L 7 3 4F RT A22WE 20080912 WP 2008 9 12 UPS08853072 1 20080725 A 5330 SKIN DOUG DC8 DC871F 302199D WP FS 136 RBL 8 PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 NOSE FUSELAGE AT STA 136.0 HAS PUNCTURED SKIN ON TOP OF AFT SIDE RADOME COMP'T BULKHEAD RBL 8. FABRI CATED AND INSTALLED REPAIR ANGLE IAW SRM 51-02-00, AND 51-01-21. 2 L 7 4 4F RT 4A25 20080915 EU 2008 9 15 08FDEA03216 1 20080803 A 5730 A57971426202 SKIN AIRBUS 310 A310203 3930313 EU ZONE 500 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 430FE 394 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LT WING OUTBOARD FLAP UPPER MAIN SKIN UNDER RUB STRIP AREA BETWEEN RIBS 7 TO 8 MEASURES 4" BY 5.6" INCHES. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT EXTERNAL REPAIR DOUBLER LOCATED ON LT WING OUTBOARD FLAP UPPER MAIN SKIN UNDER RUB STRIP AREA BETWEEN RIBS 7 TO 8 IAW SRM 57-53- 12 FIG 210. 2 L 7 2 4F RT A35EU 20080915 EU 2008 9 15 08FDEA03095 1 20080728 A 5320 A5361221420001 FLOOR SUPPORT AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DECK FLOOR SUPPORT HAS CORROSION 4 INCH AFT OF FRAME 13; LBL 31 INCHES. REMOVED CORROSION IAW SRM 51-74-10. ORIGINAL MATERIAL THICKNESS 0.079. MATERIAL REMOVED 0.013. MATERIAL REMAINING 0.066. FOUND TO BE OUT OF LIMITS IAW S RM 53-10-00. REMOVED FLOOR SUPPORT IAW SRM 51-40-21; PG 6. LOCATED AND DRILLED THE HOLES IAW IAW SRM 51-40-44 AND 51-4 0-12. INSTALLED FLOOR SUPPORT IAW SRM 51-40-21; PG 6. APPLIED CIC IAW AMM 51-22-00. 2 L 7 2 4F RT A35EU 20080915 EU 2008 9 15 08FDEA03128 1 20080729 A 5311 A57110530531 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 DURING INSPECTION FOUND SEVERAL TOOL MARKS WERE FOUND ON FR 47 RT FORWARD AND AFT FITTING, S21-26R. REPAIR PERFORMED BY SMOOTH REWORK AND SPOT FACING IAW, RAS 70511944/017/2008 ISSUE A AND EA 6-5310-120093. 2 L 7 2 4F RT A35EU 20080915 EU 2008 9 15 08FDEA02022 1 20080529 A 3610 3985042 BLEED VALVE AIRBUS 310 A310222 3930315 EU NR 1 AC PACK FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 417FE 13247 13247 333 NR 1 PACK FAULT, XFEED WOULD NOT OPEN, RESET BREAKERS STILL INOP. THE NR 1 HP BLEED VALVE IS ON MEL 36-11-03. REPLACED THE PNEUMATIC CROSSBLEED VALVE 16HV PER AB MM 36-12-11-4, OPS CK OK, ALL ACCESS PANELS IN WHEEL WELL CLOSED UP. REMOVA L/INSTALLATION, OFF MFG 398504-2 POS ONL SRL 1826 TAG 4300C8 ON MFG 398504-2 SRL 2324 TAG 90755A. 2 L 7 2 4F RT A35EU 2008012900027 20080129 00027 NM 2008 1 29 2008UALA00127 1 20080108 A 4940 MR49408 STARTER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE APU INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 666UA 29238 APU FAILED TO START AFTER TWO ATTEMPTS, FAULT LIGHT ON LAST ATTEMPT. CHK'D MAG CHIP DETECTRS OK, BIT APU CONTROL OK. R EPLACED APU STARTER, OPS OK APU START. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900035 20080129 00035 NM 2008 1 29 2008UALA00183 1 20080110 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 SURFACE CORROSION ON INTERCOSTAL AT BS 1600-1612 BL 0 WL 138 TO WL 142. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012400334 20080124 00334 CE 2008 1 24 DXTA200802777 1 20080119 A 2612 FIRE LOOP CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE FIRE WARNING OUT OF POSITION E DXTA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 07 686QS 5605661 LT ENGINE FIRE WARNING LIGHT FLASHES INTERMITTENT IN CRUISE FLIGHT. NO SECONDARY INDICATIONS OBSERVED. REMOVED BOTH UP PER AND LOWER COWLINGS, INSPECTED FIRE LOOP, FOUND LOOP CONTACTING ENG. REPOSITIONED FIRE LOOP, CLEANED CONNECTORS, SWAP PED FIRE DETECTION CONTROL UNITS FOR CUSTOMER CONVENIENCE AND TROUBLESHOOTING PURPOSE, RAN LH ENG. NO DEFECTS NOTED, TAL KED WITH MCC NO PREV. WRITE UPS, OK FOR CONTINUED SERVICE. REINSTALLED BOTH ENG. COWLING. ALL WORK DONE IAW CE560 AMM 26 -11-00 AND AMM 26-11-02 2 L 7 2 4F 4 F RT A22CE E00059EN 2008012400336 20080124 00336 CE 2008 1 24 DXTA200802781 1 20080121 A 2750 99146153 PDU CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS FAILED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 978QS 299 7500187 FLAP FAIL AMBER CAS MESSAGE FAILURE OCCURED BETWEEN 15 AND 35 DEGREES. TROUBLESHOT TO BAD PDU CLUTCH. REMOVED REPLACE D AND OPS CHECK GOOD OF FLAP PDU IAW MM 27-51-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008012500006 20080125 00006 EU 2008 1 25 F3LA200800018 1 20080115 A 5321 D5367180500500 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION, CARGO FLOOR PANEL 262FF, LOCATED BETWEEN FRAMES 66 AND 68, WAS FOUND TO HAVE CORROSION ON ITS LOWER SURFACE. MAINTENANCE REMOVED AND REPLACED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-42-12 PB 401. FOLLOWING THE COMPLETION OF THE INSTALLATION, THE NEW FLOOR PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT 2008012500014 20080125 00014 EU 2008 1 25 F3LA200800023 1 20080115 A 5220 L32A319160001 RELEASE CABLE AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE ESCAPE HATCH INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION AND FUNCTIONAL TESTING, THE LEFT, OVERWING, EMERGENCY ESCAPE HATCH RELEASE CABLE WAS BINDING A ND WOULD NOT RETRACT. MAINTENANCE REMOVED AND REPLACED THE CABLE IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 25-62-43-40 0-001. UPON REPLACEMENT OF THE CABLE, IT WAS TESTED AND INSPECTED AND FOUND TO OPERATE IN ACCORDANCE WITH THE REQUIREME NTS OF AMM 52-21-00 PB 501. 2 L 7 2 4F 4 F RT 2008012200267 20080122 00267 EU 2008 1 22 08FDEA00115 1 20080112 A 5347 A5378193120800 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 685FE 803 MDCC, BETWEEN FRAMES 20 AND 21, SEAT TRACK L-5 IS BENT. REMOVED AND REPLACED SEAT TRACK NR 5 LT BETWEEN FRAMES 18 TO 26 IAW A300-600 SRM 51-75-10 AND SRM 53-13-16. 2 L 7 2 4F RT A35EU 2008012200271 20080122 00271 WP 2008 1 22 08FDEA00121 1 20080114 A 5512 ALC7439Y501 SKIN DOUG MD10 MD1010F 3022112 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 LT HORIZONTAL STAB UPPER REAR SKIN PANEL CRACKED, INITIATING FROM AFT EDGE OF SKIN AND PROCEDING FWD 21/4" (APPROXIMATEL Y). VERIFIED BY HFEC INSPECTION MARKED END OF CRACK. COMPLIED WITH AE 8-5510-116939. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008012200282 20080122 00282 NM 2008 1 22 KCSA081012 1 20080114 A 5347 SEAT TRACK BOEING 747 747209B 138489B NM CABIN DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 MAIN DECK SEAT TRACK DAMAGED BETWEEN BS 540 AND BS 550, RBL 33. 2 L 7 4 4F RT A20WE 2008012200289 20080122 00289 NM 2008 1 22 08FDEA00135 1 20080115 A 5311 BAC15171062 FRAME BOEING 727 727233 138408A NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 CABIN BS 640 FRAME, INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT S11R BLENDED DAMAGE AREA, FOUND TO BE OUT OF LIMITS. INSTALLED DOUBLER REPAIR REF SRM 53-10-4. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2008012200323 20080122 00323 SO 2008 1 22 C2XA08CL005 1 20080108 A 5210 14533967401 BELLCRANK EMB 145 EMB145LR 3260212 SO PAX DOOR BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13955 145075 YQM FLIGHT 2230 - THE CREW REPORTED THE MAIN CABIN DOOR WILL NOT CLOSE OR OPEN FROM INSIDE THE CABIN. MAINTENANCE INSPE CTED AND REPLACED THE INTERNAL HANDLE BELLCRANK ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008012200324 20080122 00324 SO 2008 1 22 C2XA08RI013 1 20080104 A 5210 14533225901 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR LOOSE A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 13989 145271 FLT 2486 EWR - CREW REPORTED MAIN CABIN DOOR HARD TO OPEN. EWR MX RE-SECURED MAIN CABIN DOOR HANDLE IAW EMB145 AMM 52-1 8-05 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008012200325 20080122 00325 SO 2008 1 22 C2XA08RI012 1 20080104 A 3350 CHARGER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11544 145557 RIC - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT OVERWINGS INOPERATIVE. MX REMOVED AND REPLACED NR 4 EMERGENC Y LIGHT BATTERY CHARGER IAW EMB145 AMM 33-50-00 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETU RN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008012200328 20080122 00328 SO 2008 1 22 C2XA08IA019 1 20080109 A 3246 14520682405 WHEEL EMB 145 EMB145LR 3260212 SO NLG WORN A C2XA A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 SW 27 21537 528 145523 IAH - FLIGHT 2431, THE CREW REPORTED AN EXCESSIVE NW VIBRATION ON T/O. MAINTENANCE REMOVED AND REPLACED BOTH NOSE WHEEL ASSEMBLIES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008012200329 20080122 00329 SO 2008 1 22 C2XA08IA020 1 20080109 A 3246 14520682405 WHEEL EMB 145 EMB145LR 3260212 SO NLG WORN A C2XA O OTHER E VIBRATION/BUFFET TO TAKEOFF 1 SW 27 21537 528 145523 IAH - FLIGHT 2431, THE CREW REPORTED AN EXCESSIVE NW VIBRATION ON T/O. MAINTENANCE REMOVED AND REPLACED BOTH NOSE WHEEL ASSEMBLIES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008012200337 20080122 00337 NM 2008 1 22 08FDEA00145 1 20080115 A 5321 656724516 SPLICE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 AFT PIT FLOOR BOARD SPLICE STRAP BETWEEN NR 3 AND 4 PANELS HAS LIGHT CORROSION ON BOTH SIDES. REMOVED CORROSION FROM AF T PIT FLOORBOARD SPLICE STRAP BETWEEN NR 3 AND 4 IAW SRM 51-10-1 FIG 1, AMOUNT EXCEED MAX ALLOWABLE LIMITS IAW SRM 53-10 -1 FIG 1, SHT 2. FABRICATED NEW PART USING ALTERNATE MATERIAL, 2024 -T3 .125" REF DWG 65-67245 ITEM 16, SRM 51-20-1 FIG 2, PG 13. ALODINED AND PRIMED REF SRM 51-10-2 PG 1. THIS IS CLASSIFIED A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008012200342 20080122 00342 NM 2008 1 22 KCSA081015 1 20080115 A 5210 WEB BOEING 747 747209B 138489B NM PAX DOOR CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 MAIN ENTRY DOOR NR 3R LOWER HINGE CUTOUT UPPER SURFACE OF LOWER WEB IS CORRODED. 2 L 7 4 4F RT A20WE 2008012200354 20080122 00354 EU 2008 1 22 TRAX200800074 1 20080110 A 5720 INTERCOSTAL AEROSP ATR72 ATR72 EU LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 LEFT ON TOP WING BOX AT FR 23D AND RIB 1, ANGLE OF INTERCOSTAL FOUND CRACKED. 2 H 7 2 4T RT 2008012200357 20080122 00357 EU 2008 1 22 TRAX200800077 1 20080110 A 5720 ANGLE AEROSP ATR72 ATR72 EU RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 RIGHT ON TOP WINGBOX FWD FR 23D AND RIB 3 ANGLE FOUND CRACKED. 2 H 7 2 4T RT 2008012200359 20080122 00359 EU 2008 1 22 TRAX200800079 1 20080110 A 5320 ANGLE AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 ANGLE CRACKED AT FR 26 STRINGER 4R (INTERNAL FUSELAGE). REMOVED AS PER SRM 51-25-01. RT SHEAR WEB BTW FR 25 & 27 REM OVED IAW AMM 20-21-12. ANGLE AT FR 26 STR 4 RT INSTALLED AS PER SRM 51-25-01. RT SHEAR WEB RE-INSTALLED IAW TECH INSTR UCTION 57-01-91. 2 H 7 2 4T RT 2008012200362 20080122 00362 EA 2008 1 22 TRAX200800082 1 20080111 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 843AS 7310 AAR - CLIP CRACKED O/B OF RBL 27. 2 L 7 2 4F RT A21EA 2008012200374 20080122 00374 NM 2008 1 22 KCSA081018 1 20080115 A 5320 TORQUE BOX BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 AFT BILGE TORQUE UPPER WEB HAS SEVERAL AREAS OF CORROSION FROM STA-1660 TO STA-1680 LBL-37 TO RBL-56. 2 L 7 4 4F RT A20WE 2008012800181 20080128 00181 WP 2008 1 28 UPS08851410 1 20080102 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 FITTING STA 340 RBL 46 HAS CORROSION IN A PIT. REMOVED FITTING, REPAIRED AND REINSTALLED PER SRM 51- 1-20D, SRM 51-1 -8 AND SRM 51-02-00. 2 L 7 4 4F RT 4A25 2008012900007 20080129 00007 SO 2008 1 29 RAIA00801010 1 20080110 A 3610 81662413 THERMOSTAT EMB 145 EMB145LR 3260212 SO BLEED AIR SYS MALFUNCTIONED A RAIA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CL CLIMB 1 CE 03 845HK 14500842 FLT 7908 - ORD - BLEED 1 OVERTEMP MESSAGE ON EICAS WHEN CLIMBING THROUGH FL150. MAINTENANCE REMOVED AND REPLACED THE FA N AIR CONTROL THERMOSTAT. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012900029 20080129 00029 NM 2008 1 29 2008UALA00077 1 20080104 A 2611 SMOKE DETECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CARGO BAY MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 844UA 1581 CARGO SMOKE DETECTOR FAILS TO TEST. FAILS LOOP-A FWD PIT. ALSO HAD CIDS LAV SMOKE DET FAIL MSG. RESET C/B'S FOR SDCU (C6 AND T18) AND PERFORMED CARGO SMOKE DET TEST. ALL PASSED AND ALL MESSAGES CLEARED AFTER RESET. NO REPEATS SINCE ORI GINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900030 20080129 00030 EU 2008 1 29 2008UALA00039 1 20080103 A 3230 S4340131003 SAFETY VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LANDING GEAR FAILED A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 430UA 568 LANDED UNDER AMBER ALERT DUE TO A FAILED GREEN HYDRAULIC SYSTEM. FAILED LANDING GEAR SAFETY VALVE. REPLACED LANDING GE AR SAFETY VALVE (49GA). PERFORMED GEAR CYCLES, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900056 20080129 00056 NM 2008 1 29 2008UALA00192 1 20080111 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS MISSING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 EEL MISSING AT SEATS 1J AFT, 4E AFT, 32A. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900064 20080129 00064 NM 2008 1 29 2008UALA00200 1 20080113 A 5610 WINDOW BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT UNDERTORQUED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 936UA 26667 RTFL DUE TO A POPPING SOUND FROM WINDOW R-4. RETORQUED ALL WINDOW BOLTS TO 60 LBS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900088 20080129 00088 NM 2008 1 29 2008UALA00208 1 20080111 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 AFT CARGO BAY BS 807 STRINGER CLIP 22L IS DAMAGED. REPAIRED AND INSTALLED STRINGER CLIP. REFERENCE SRM 53-00-03 & SRM 5 1-40-02 PG 1-7. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900095 20080129 00095 NM 2008 1 29 2008UALA00211 1 20080112 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 AFT GALLEY FLOORBEAM UPPER SURFACE IS CORRODED STA 1016, STR 17R, RBL 5 AND RBL 16, WL 208. INSTALLED UPPER FLOOR CAP D OUBLE FLANGE REPAIR PER MM 53-10-95 FIG 813 REPAIR XV. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900096 20080129 00096 NM 2008 1 29 2008UALA00212 1 20080112 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FWD ENTRY DOOR CUTOUT BS 360 SHEAR TIE CRACKED AT STRINGER 13L. FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE PER SRM 51-20-01 PG1 & SRM 51-40-01. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900101 20080129 00101 NM 2008 1 29 2008UALA00215 1 20080111 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 FUSELAGE FRAME AT BS 1420 STR 26L HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012900115 20080129 00115 NM 2008 1 29 2008UALA00222 1 20080112 A 2450 INSULATOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE POWER BREAKER MISSING A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 787UA 26939 P300 BACK PLANE AUXILARY POWER BREAKER (APB L9-C24335) HAS INSULATOR MATERIAL MISSING, ALSO C PHASE (BLUE) POWER FEEDER WIRE WAS DISCOLORED. RESISTANCE READING AT L9 C24335 C2 EXCEEDED LIMITS. SUSPECT SHORT AT POWER PANEL P300. REPLACED P 300 AUX PANEL AND PERFORMED CHECK'S IAW MM'S 24-09-01, 24-22-03, 24-22-05, & 24- 41-01. NO DEFECTS NOTED. ACFTOK FOR SE RVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008012900126 20080129 00126 NE 2008 1 29 2008UALA00097 2 20080103 A 7230 56A631 BLADE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE BENT A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 641UA 25091 727882 ONE BLADE ON LEFT ENGINE BENT OVER 90 DEGREES. REPLACED BLADE NR 37 DUE TO BENT AND OPPOSITE BLADE NR 18 PER MM 72-31-0 2. THREE OTHER BLADES NR 35, 36, 38 ARE CF'D. ACCOMPLISHED RII INSPECTION OF NR 35 36 AND 38 BLADES PER MM 72-31-02, O K FOR FINAL .020\ INSURANCE BLEND. ACCOMPLISHED BLENDING .020' PER MM 72-31-02. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900129 20080129 00129 EU 2008 1 29 2008UALA00053 1 20080102 A 3350 321454 EPSU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 456UA 1128 EMERGENCY EXIT SIGN AT DOOR 1L AT FLOOR LEVEL INOP DURING EMERGENCY LIGHT TEST. EPSU FAILED. REPLACED EPSU, LIGHTS TES T OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900142 20080129 00142 SO 2008 1 29 C2XA08SH004 1 20080116 A 5512 14532235602 SKIN EMB 145 EMB145LR 3260212 SO HORIZ STAB CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26549 145571 SHV - DURING C-CHECK RIGHT HORIZONTAL STAB L/E HAS PITTING CORROSION. MX REPAIRED RIGHT HORIZONTAL L/E IAW EC5530-01116 REV D. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008012900143 20080129 00143 SO 2008 1 29 C2XA08SH005 1 20080116 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26549 145571 SHV - DURING C-CHECK LEFT OMEGA BEAM HAS CORROSION AT FR 20. MX REPAIRED LEFT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00 -10. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008012900144 20080129 00144 NM 2008 1 29 2008UALA00086 1 20080107 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW O2 LOW PRESSURE A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 834UA 1420 FLIGHT DIVERTED DUE TO FLIGHT DECK OXYGEN PRESSURE. SERVICED CREW O2 SYSTEM AND LEAKED CHECKED THE ENTIRE SYSTEM THOROU GHLY. COULD FIND NO SOURCE OF LEAK. SUSPECT A CREW O2 MASK TO BE UNSTOWED/IMPROPERLY STOWED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900146 20080129 00146 NM 2008 1 29 CALA0800026 1 20080116 A 5310 6916970501 ANGLE BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 FORWARD ENTRYWAY (L1-DOOR OPENING) ANGLE ON BOTTOM FORWARD END OF INTERCOSTAL WEB AT FRAME STA 348.2 INLINE WITH S15L IS CRACKED AT INBOUND END. REMOVED AND REPLACED ANGLE PER ECRA 5311-01390. 2 L 7 2 4F RT A16WE 2008012900149 20080129 00149 EU 2008 1 29 F3LA200800030 1 20080123 A 5755 D5775002000118A HINGE FITTING AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE NR 3 SPOILER DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION, THE CENTER HINGE ANTI-ROTATION LUG FOR THE LEFT NUMBER 3 SPOILER WAS FOUND DAMAGED. MAINTENA NCE REMOVED THE DAMAGED ASSEMBLY AND PERFORMED A "MAJOR REPAIR" IN ACCORDANCE WITH THE REQUIREMENTS OF EA A8-57R-12379. UPON COMPLETION OF THE REPAIR, THE NUMBER 3 SPOILER WAS RE-INSTALLED, INSPECTED, TESTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT 2008012900152 20080129 00152 SO 2008 1 29 C2XA08CL009 1 20080114 A 4930 49523162 SOLENOID VALVE EMB 145 EMB145LR 3260212 SO APU FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16963 145116 EWR FLIGHT 2947 - THE CREW REPORTED A FUEL SMELL AFTER APU START ON THE GROUND. THE AIRCRAFT WAS RELEASED IAW MEL CONTR OL 137419. ON 1/16/08 CLE MAINTENANCE REMOVED AND REPLACED THE MAIN FUEL SOLENOID VALVE. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008012900153 20080129 00153 NM 2008 1 29 ASAA0842482 1 20080115 A 5210 65C80736354 UNKNOWN BOEING 737 737490 1384715 NM L1 DOOR BINDING A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 791AS 28886 L1 DOOR RELEASES INWARD OK VERY DIFFICULT TO PUSH OPEN. CHECKED DOOR FOR LOOSE OR DAMAGED PARTS, NO DEFECTS NOTED. PER FORMED OPERATIONAL CHECK OF L1 DOOR. DOOR OP CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2008012900156 20080129 00156 NM 2008 1 29 MWEA080009 1 20080115 A 3350 P4010021 BATTERY BOEING 717 717200 1383700 NM FLASHLIGHT DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 921ME 55183 FLIGHT ATTENDANT FLASHLIGHT NOT FLASHING. REMOVED AND REPLACED BATTERY. 2 L 7 2 4F TR A6WE 2008012900166 20080129 00166 EA 2008 1 29 TRAX200800091 1 20080113 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION DE DESCENT 1 SO 27 889AS 7538 ON DESCENT INTO ATW SELECTED FLAPS TO 8 AND FAILED AT ZERO. DIVERTED TO ORD AND DECLARED AN EMERGENCY INTO ORD. FLT 46 16 CX. 2 L 7 2 4F RT A21EA 2008012900177 20080129 00177 EU 2008 1 29 2008UALA00156 1 20080108 A 5210 FE240221001 DIAPHRAGM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 437UA 655 FOUND DOOR 2L DAMPNER AND EMERGENCY OPERATION CYLINDER READING "0" DURING 3 SVC. SUSPECT WEAK/LEAKING DIAPHRAGM AND/OR SEALS. REPLACED EMERGENCY OPERATION CYLINDER DIAPHRAGM AND SEALS. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900184 20080129 00184 EU 2008 1 29 2008UALA00224 1 20080113 A 3350 D9239003500060 EPSU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 408UA 457 LEFT AFT ENTRY DOOR EMERGENCY EXIT LIGHT HAS BATTERY FAULT. EPSU FAULTY. REPLACED EPSU. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900188 20080129 00188 NM 2008 1 29 2008UALA00230 1 20080113 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 LIGHTNING STRIKE AT STA 445, STRINGER 7L, IS BEYOND ALLOWABLE LIMITS. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012900190 20080129 00190 NM 2008 1 29 2008UALA00232 1 20080112 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 651UA 25389 LEFT EEL INOP IN FIRST CLASS AT LAV. SECURED CONNECTOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900192 20080129 00192 NM 2008 1 29 2008UALA00234 1 20080112 A 5330 146T3551 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 661UA 63328 27158 FUSELAGE DAMAGE AT STA 1197 +60 - +68. MANUFACTURED REPAIR DOUBLERS AND FILLERS. ACFT REPAIRED AND OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900203 20080129 00203 2008 1 29 2008UALA00245 4 20080113 A 2565 7A146724 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R4 DOOR OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 187UA 26877 DOOR 4R SLIDE PRESSURE GAUGE GREEN BAND NO IN VIEW. REPLACED SLIDE ASSEMBLY IAW 25-69-01. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012800147 20080128 00147 NM 2008 1 28 08FDEA00223 1 20080122 A 5730 ARB2886504 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RT WING, LEADING EDGE LOWER ACCESS PANEL 618FB INBOARD FORWARD CORNER CUTOUT FOUND CRACKED. REPAIR CARRIED OUT AT RT W ING LEADING EDGE LOWER ACCESS PANEL 618FB INBOARD FORWARD CORNER AS PER EA 1-5740-117298, REPAIR CLASSIFIED AS MAJOR PE R GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008012800161 20080128 00161 NM 2008 1 28 F3LA200800019 1 20080107 A 2560 P4010021 BATTERY AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FLASHLIGHT INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 924FR 233 2030 DURING C CHECK INSPECTION, THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY WAS FOUND DEAD. MAINTENANCE REMOVE D AND REPLACED THE FLASHLIGHT BATTERY IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 25-65-00. UPON COMPLETION OF THE BATTE RY REPLACEMENT, THE FLASHLIGHT WAS INSPECTED AND FOUND OPERATIONAL. 2 L 7 2 4F 4 F RT A28NM 2008012900037 20080129 00037 NM 2008 1 29 2008UALA00184 1 20080110 A 5210 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 L2 DOOR EXTERNAL SKIN HAS 2 DENTS ABOVE LOWER GATE. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012900054 20080129 00054 NM 2008 1 29 2008UALA00191 1 20080111 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 EEL INOP AT SEAT 5E, AFT. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900093 20080129 00093 NM 2008 1 29 2008UALA00210 1 20080112 A 5210 WEB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD ENTRY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FWD ENTRY DOOR LOWER WEB FWD CORNER IS CRACKED BELOW FITTING. REMOVED AND INSTALLED NEW LOWER DOOR FRAME CLOSURE WEB PE R SRM 51-40-05 PG1 & SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900163 20080129 00163 EU 2008 1 29 USAA920080188 1 20080107 A 5347 D53472178200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 622AW 54 SAL - MAJOR REPAIR - C6 CHECK - CORROSION ON CABIN SEAT RAIL, BS 2510 / FR 54, +Y765. REPAIRED CABIN SEAT RAIL, BS 2510 / FR 54, +Y765 IAW A320 SRM 53-00-15. 2 L 7 2 4F RT A28NM 2008012900179 20080129 00179 NM 2008 1 29 2008UALA00162 1 20080109 A 2560 256302008 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FLASHLIGHT DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 826UA 989 BOTH FWD EMERGENCY FLASHLIGHTS DEAD. REPLACED BOTH BATTERIES. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900183 20080129 00183 NM 2008 1 29 2008UALA00223 1 20080112 A 3320 Z250H2102110 BALLAST AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE GALLEY FAULTY A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 845UA 1585 AFT GALLEY ELECTRICAL SMELL REPORTED BY F/A. FAULTY BALLAST FOR AFT GALLEY WORK LIGHT. REPLACED AFT GALLEY WORK LIGHT BALLAST INSIDE PANEL G3. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900206 20080129 00206 WP 2008 1 29 UPS08851421 1 20080102 A 5313 37799191N STRINGER SPLICE DOUG DC8 DC871F 302199D WP FS 1340 L35L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 AT CARGO COMPT STA 1340 L35L SPLICE IS CRACKED. REMOVED AND REPLACED L35L SPLICE FITTING AT STA 1340 IAW SRM 51-01- 20D AND SRM 51-1-15. 2 L 7 4 4F RT 4A25 2008012900210 20080129 00210 2008 1 29 UPS08851428 4 20080112 A 2565 INDICATOR DOUG DC8 DC871F 302199D WP ESCAPE SLIDE OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 ESCAPE SLIDE PRESSURE GAUGE UNREADABLE, TOO LOW IN SIGHT WINDOW. REMOVED AND REPLACED SLIDE CONTAINER PER DC8 AMM 25 -60-01-2 2 L 7 4 4F RT 4A25 2008012900211 20080129 00211 WP 2008 1 29 UPS08851430 1 20080107 A 5511 RIB DOUG DC8 DC871F 302199D WP HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 CRACKED LOWER RIB ON HORIZ STAB RT LEADING EDGE. STOP DRILLED CRACK ON RT HORIZ STAB LEADING EDGE IA W SRM 55-02-00 FIG 002. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 55-02-00-0 FIG 002. 2 L 7 4 4F RT 4A25 2008012900214 20080129 00214 NM 2008 1 29 UPS08B51431 1 20080112 A 3350 LAMP BOEING 747 74744AF 13848B2 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 572UP 35669 L1 DOOR CEILING EMERGENCY LIGHT INOP. RELAMPED, INSPECTED. CHECKS OK. 2 L 7 4 4F RT A20WE 2008012900238 20080129 00238 NM 2008 1 29 2008UALA00255 1 20080114 A 5240 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FWD GALLEY DOOR, S/N 001301, LOWER FRAME CRACKED AT LOWER CORNER RADIUS NEAR THE INNER SKIN. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900253 20080129 00253 EU 2008 1 29 UPS08151458 1 20080111 A 5753 SKIN AIRBUS A300 A300F4622R 3930360 EU TE FLAP CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 167UP 0005 INSPECTION TYPE:1C LT CENTERFLAP IB UPPER SURFACE HAS HEAVY CHAFFING. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW A300-600 SRM 57-50-00. 2 L 7 2 4F RT A35EU 2008012900254 20080129 00254 WP 2008 1 29 UPS08851435 1 20080102 A 5313 3759258 LONGERON SPLICE DOUG DC8 DC871F 302199D WP BS 1280 L35R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 C CARGO COMPARTMENT STA 1280, LONGERON 35R AND SPLICE HAVE CORROSION. REPLACED LONGERON 35R SPLICE F ITTING REF SRM 51-01-20D AND SRM 51-01-24. 2 L 7 4 4F RT 4A25 2008012900260 20080129 00260 WP 2008 1 29 UPS08851446 1 20080116 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ASSY. OPS CHECK GOOD, REF AMM 33-50-01-2 , P/N ON 60-1223-5, S/N ON 341. 2 L 7 4 4F RT 4A25 2008012900262 20080129 00262 2008 1 29 UPS08851447 4 20080117 A 2565 INDICATOR DOUG DC8 DC871F 302199D WP ESCAPE SLIDE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 ESCAPE SLIDE PRESSURE UNREADABLE. REMOVED AND REPLACED ESCAPE SLIDE PER MM 25-60-01. OPS CKD, SLIDE GIRT BAR INSTALLED . THIS CLOSES DEFERRAL M367121. 2 L 7 4 4F RT 4A25 2008012900267 20080129 00267 NM 2008 1 29 2008UALA00266 1 20080113 A 2421 745329D IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT GENERATOR INOPERATIVE A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 651UA 25389 RT GENERATOR INOP. REPLACED RIGHT IDG. ACCOMPLISHED IDG PERFORMANCE CHECK . ALL NORMAL.. ACP BPCU BITE CHECK. ALL OK. VERIFICATION FLIGHT CONFIRMED NORMAL OPERATION. ACFT OK FOR SERVICE 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900280 20080129 00280 NM 2008 1 29 2008UALA00281 1 20080115 A 5753 HINGE BRACKET BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE T/E FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 667UA 29239 RIGHT WING INBOARD FLAP, FORE TO AFT FLAP CENTER HINGE BRACKET CRACKED. ACP EQ5256 TE FLAP FITTING INSPECTION. MANDATED BY AD 2003-13-01. REMOVED DAMAGED FLANGES. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR ANGLES. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900285 20080129 00285 NM 2008 1 29 2008UALA00289 1 20080115 A 2560 GIRT BAR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ESCAPE SLIDE LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 FORWARD ENTRY DOOR EMERGENCY SLIDE GIRT BAR FLOOR ATTACH FITTING SCREWS LOOSE. SECURED GIRT BAR FLOOR ATTACHMENT FITTIN G. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900286 20080129 00286 NM 2008 1 29 2008UALA00290 1 20080115 A 3350 1319 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 333UA 24228 EMERGENCY EXIT LIGHT AFT OF FORWARD ENTRY DOOR IS INOP. RELAMPED. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900291 20080129 00291 NM 2008 1 29 2008UALA00296 1 20080116 A 2621 GH3JHU1 EXTINGUISHER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DOGHOUSE LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 179UA 25158 THREE SVC CHECK FOUND 18GH DOGHOUSE HALON 1211 FIRE EXTINGUISHER PRESSURE LOW. REPLACED HALON EXTINGUISHER. AC OK FOR S ERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900293 20080129 00293 NM 2008 1 29 2008UALA00298 1 20080117 A 3510 OXYGEN SYSTEM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CREW NONE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 777UA 26916 O2 LOW. SERVICED CREW OXYGEN TO FULL. NO LEAKS NOTED. SUSPECT PERIODIC TESTS BY FLIGHT CREW DEPLETED PRESSURE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008013000013 20080130 00013 EU 2008 1 30 08FDEA00192 1 20080118 A 2910 HYDRAULIC SYSTEM AIRBUS 310 A310304 3930339 EU GREEN SYSTEM LOW A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 817FD 552 REJECT T/O DUE TO ECAM: GREEN SYSTEM HYD QTY LOW. VERY COLD OUTSIDE AIR TEMP. PERFORMED VISUAL INSPECTION AND NO LEAKS FOUND. SERVICED GREEN HYD SYS PER SMP AND A310-300 AMM REF 12-12-29, SERVICED TWO QTS. A/C OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2008013000016 20080130 00016 NM 2008 1 30 P5CA0801542 1 20080107 A 5347 SEAT TRACK BOEING 747 74746NF 13848BT NM BS 1850-1862 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 451PA 30809 MAIN CARGO DECK SEAT TRACK CRACKED AT STATION 1850-1862 RBL 11.33. SCL ACCOMPLISHED INTERIM REPAIR AND MIA ACCOMPLISHED PERMANENT REPAIR PER MA A4 5300-10-00. 2 L 7 4 4F RT A20WE 2008013000018 20080130 00018 EU 2008 1 30 TRBA2008007 1 20080115 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHTS FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 494AE 494 EMERGENCY LIGHT AT AFT F/A PANEL NOT WORKING PROPERLY. REMOVED AND REPLACED BATTERY PACKS AT POWER SUPPLY UNITS FIN NR 43WL, 61WL AND 62WL IAW MM NR 33-51-21. 2 H 7 2 4T RT A53EU 2008013000021 20080130 00021 EU 2008 1 30 MALA080008 1 20080109 A 5520 STRUCTURE SAAB SF340 340B 7860101 EU ELEVATOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 DENT LOCATED ON RT ELEVATOR 70.88" FROM INBOARD EDGE, 2.88" FROM FWD SPAR. REPAIRED IAW MAL EO NR S51031. 2 L 7 2 4T RT A52EU 2008013000028 20080130 00028 EU 2008 1 30 MALA080010 1 20080119 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 300-303 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 LT SEAT TRACK RAIL CORRODED ON IB WEB AT STA300 TO STA303, LBL 18. REPAIRED IAW MAL EO NR S53342. 2 L 7 2 4T RT A52EU 2008013000029 20080130 00029 EU 2008 1 30 CPCP20080001 1 20080107 A 5320 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 369AT 369 R/T INTERCOSTAL BETWEEN FRAME 36-38 CORRODED. RT INTERCOSTAL REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2008013000031 20080130 00031 2008 1 30 SMIA200802104 4 20080118 A 3418 C16258AA TRANSDUCER CNDAIR CL600 CL6002C10 1390015 EA AOA MALFUNCTIONED A SIMA B A EMER. DESCENT UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 518AE 10126 ON FLIGHT 3756 CREW REPORTED AOA VANE FAILED, AFTER TAKEOFF THE STICK PUSHER AND SHAKER CAME ON IN FLIGHT. CREW ELECTED TO RETURN TO THE GATE, DECLARED EMERGENCY AND LANDED WITH NO FURTHER PROBLEMS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT AND RIGHT AOA TRANSDUCERS IAW AMM 27-35-05. OPERATIONAL CHECK GOOD OF AOA VANES IAW 27-35-05. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008013000034 20080130 00034 SO 2008 1 30 FDKA200801034 1 20080117 A 5500 BONDING STRAP EMB 145 EMB145LR 3260212 SO CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 834MJ 145340 THE BONDING STRAPS ON PANEL NR 337DL, NR 321EL AND NR 321DR ARE CORRODED. THE STRAPS HAVE BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008013000041 20080130 00041 EA 2008 1 30 CHQA200800012 1 20080123 A 2133 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE OUTFLOW VALVE MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 639BR 7313 GEE872507 CMH TO IAH - AFTER A NORMAL TAKEOFF ON THE APU'S 10TH STAGE BLEED, THE BLEED SOURCE WAS TRANSFERRED OVER TO THE ENGINE'S 10TH STAGE BLEED. THE CABIN PRESSURE HELD FOR APPROXIMATELY 1 MINUTE THAN BEGAN TO RISE. AFTER LEVELING AT 11,000 FT, THE CABIN ALTITUDE GOT HIGH ENOUGH TO GENERATE THE AMBER "CABIN ALT" MESSAGE. THE FLIGHT CREW IMMEDIATELY RAN THE APPR OPRIATE QRH CHECKLISTS AND RETURNED TO FIELD AT CMH. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOU ND INBOARD EXHAUST VALVE MOVING IN THE OPPOSITE DIRECTION OF ITS DEFERRED POSITION WHEN PRESSURE WAS APPLIED. DURING SU BSEQUENT TROUBLESHOOTING THE PRESSURIZATION SYSTEM OPERATED NORMALLY WHEN THE OUTBOARD EXHAUST VALVE WAS IN THE DEFERRED 2 L 7 2 4F 4 F RT A21EA E15NE 2008012800163 20080128 00163 NM 2008 1 28 08FDEA00212 1 20080122 A 5720 652811542 BRACKET BOEING 727 727233 138408A NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 RT WING, NR 6 FLAP TRACK FAIRING, O/B SKATE ANGLE ATTACH BRACKET, CRACKED AT I/B AFT SIDE REMOVED RT WING NR 6, FLAP TRA CK FAIRING O/B SKATE ANGLE ATTACH BRACKET I/B AFT SIDE IAW SRM 51-30-2 PG3, VERIFIED MATERIAL AS MATERIAL 2024-T3 .071" IAW DWG 65-28115-5 SHT 2. FABRICATED NEW BRACKET IAW DWG 65-28116 ITEM -42 MATERIAL A TAG NR A70701/ PO NR 1028670. AL ODINED AND PRIMED IAW SRM 51-10-2 PG 3. INSTALLED BRACKET REF SRM 51-30-2 PG1, 51-30-2 PG4. THIS IS CLASSIFIED AS A MI NOR REPAIR. 2 L 7 3 4F RT A3WE 2008012800164 20080128 00164 SO 2008 1 28 C2XA08CL008 1 20080115 A 3097 CS500050D4A RELAY EMB 145 EMB145LR 3260212 SO CURRENT SENSOR BURNED A C2XA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 14923 145318 CMH FLIGHT NR 3142 - THE CREW REPORTED PITOT 2 INOP MESSAGE ON THE EICAS IN FLIGHT AT 25000. THEY ALSO REPORTED SMOKE I N COCKPIT AND CABIN. EMERGENCY DECLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FO UND PITOT 2 CURRENT SENSOR RELAY (K0054) AND SOCKET (XK0054) BURNED. THE RELAY AND SOCKET WERE REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008012800166 20080128 00166 SO 2008 1 28 N416RA 2 20080114 A 8530 631521 VALVE SPRING CONT CESSNA 414 414A 2075907 CE CONT O520 TSIO520NB 17040 SO NR 3 CYLINDER BROKEN E EAVA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 GL 09 416RA 223 223 AEC631397 414A0486 278454R ENGINE VIBRATION PROMPTED INFLIGHT SHUTDOWN OF ENGINE. 1 L 7 2 3O 3 O A7CE E8CE 2008012900023 20080129 00023 EU 2008 1 29 2008UALA00092 1 20080106 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 486UA 1620 CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. CREW COMMENTS: OXY PRESS 1090 DECREASED 400 PSI SINCE DEN . UNKNOWN INDICATION ISSUE. SERVICED CREW O2 SYSTEM, NO LEAKS NOTED ANYWHERE IN THE SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900047 20080129 00047 NM 2008 1 29 2008UALA00190 1 20080110 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE SCRATCHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 307UA 23668 EXTERNAL FUSELAGE SKIN SCRATCHED IN 4 LOCATIONS BS 294 STR 2L. FABRICATED AND INSTALLED EXTERNAL DOUBLER, TRIPLER & STR UCTURAL FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900057 20080129 00057 NM 2008 1 29 2008UALA00193 1 20080111 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 EEL WIRE BROKEN AT LAV 112 SIDE WALL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900059 20080129 00059 NM 2008 1 29 2008UALA00195 1 20080111 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY CEILING LIGHT ABOVE ROW 46 RT INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008020700114 20080207 00114 EA 2008 2 7 COMA0860098 1 20080124 A 3250 16736105 SERVO CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING FAILED A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 934CA 11617 7042 FLIGHT 5652 - STEERING INOP CAUTION MESSAGE DURING GEAR EXTENSION, FAILED TO CLEAR. QRH FOLLOWED, EMERGENCY DECLARED AN D A/C RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED EHSV ELECTRIC SERVO. 2 L 7 2 4F RT A21EA 2008012900104 20080129 00104 NM 2008 1 29 2008UALA00218 1 20080111 A 4920 EEC BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE APU ENGINE MALFUNCTIONED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 677UA 30029 APU WILL NOT START. SPEED SENSORS FAULTY DUE TO NORMAL OPERATIONS. REPLACED ENGINE CONTROL UNIT. FLIGHT CREW ACCOMPLISH ED VERIFICATION FLIGHT AND SENT APPROPRIATE MESSAGE FOR NORMAL OPERATION OF THE APU. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900117 20080129 00117 NM 2008 1 29 2008UALA00096 1 20080107 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW O2 LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 834UA 1420 LEAK CHECK O2 SYSTEM. SERVICED CREW O2 SYSTEM AND PERFORMED LEAK CHECKS OF ALL LINES AND MASKS. NO LEAKS WERE NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900180 20080129 00180 NM 2008 1 29 2008UALA00163 1 20080109 A 3260 893301 PROXIMITY SENSOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LANDING GEAR INTERMITTENT A UALA O OTHER W N INADEQUATE Q C FALSE WARNING AP APPROACH 1 WP 29 844UA 1581 THREE RED WITH NO ECAM ON FINAL. GEAR NOT DOWN RECYCLE OK GEAR DOWN. PROX SENSOR INTERMITTENT (38GA). REPLACED PROX SENSOR 38GA, PERFORMED GEAR SWINGS, ALL NORMAL, NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900185 20080129 00185 EU 2008 1 29 2008UALA00225 1 20080112 A 3350 BR964421 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 428UA 523 SEATS 11C, 20C & 21C ARE MISSING THE EMERGENCY LIGHT LENS COVER. UNKNOWN PASSENGER DAMAGE. REPLACED LENS ON EMERGENCY LIGHTS ASSY AT ROW 11C, 20C, 21C. ALL LIGHTS OPERATIONAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900233 20080129 00233 EU 2008 1 29 2008UALA00252 1 20080115 A 5320 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 444UA 824 UPPER FWD PART OF FUSELAGE DAMAGED WHERE IT MEETS RADOME. DAMAGE IS APPROX 1-4 IN BY 1-4 IN. PERFORMED MAJOR REPAIR AT LCQ. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900241 20080129 00241 NM 2008 1 29 2008UALA00257 1 20080114 A 5531 SPAR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU VERTICAL STAB GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 LEFT SIDE OF VERTICAL STABILIZER LOWER INTERSPAR SKIN IS GOUGED. REPLACED LOWER INTERSPAR SKIN. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900268 20080129 00268 NM 2008 1 29 2008UALA00267 1 20080114 A 2612 2156656 FIRE DETECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE AFT CARGO BAY INTERMITTENT A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 181UA 25278 THE 'FIRE CARGO AFT' EICAS WARNING MESSAGE DISPLAYED. REPLACED DETECTOR PER MM26-16-01-401, OPS NORMAL. AC OK FOR SERV ICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900279 20080129 00279 NM 2008 1 29 2008UALA00280 1 20080115 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 942 S24L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 EXTERNAL FUSELAGE SKIN IS CRACKED BS 942 STR 24L. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED EXTERNAL DOUBL ER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900283 20080129 00283 NM 2008 1 29 2008UALA00286 1 20080115 A 2612 CGAB140000 FIRE DETECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO BAY FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 377UA 24642 FWD CARGO PIT 'B' DETECTOR FAULT LIGHT ILLUMINATED. REPLACED DETECTOR OPS CHECK NORMAL PER MM 26-16-00. AC OK FOR SERVI CE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008013000007 20080130 00007 2008 1 30 HALA0800020 4 20080116 A 3140 UNKNOWN BOEING 767 7673G5 1385126 NM UNKNOWN A HALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, BLOCK TURN BACK, EICAS MSG ON STATUS: L EICAS COMPUTER. PERFORMED BITE TEST PER AMM 31-41-00. L EICAS COMPUTER, OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2008013000010 20080130 00010 NM 2008 1 30 08FDEA00074 1 20080108 A 5330 ACA3354501 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 583FE 48421 DURING TRANSFERRING OF HOLE FOUND EXTRA FASTENER HOLE. REPAIR CARRIED OUT AS PER FEDEX EA NR 1-5310-117263, TITLE "FUSE LAGE MAINFRAME LT AIR CONDITIONER DOOR JAMB SKIN REPAIR". REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008013000011 20080130 00011 NM 2008 1 30 08FDEA00141 1 20080115 A 2130 7791 MODULE BOEING 727 727233 138408A NM CABIN PRESSURE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 282FE 22349 PRESSURIZATION LOSS AT FL230, CABIN ALT 10,000' DESCEND TO (FL)10,000' PSID 0 (ZERO) LOSS OF HEAT. ACFT HARD TO HEAT O N GROUND. OUTFLOW VLV INDICATED CLOSED BUT DID NOT RESPOND IN "MAN D.C.". FOUND SMOKE CONTROL SWITCH ON P4-78 PANEL S TUCK IN THE "ON" POSITION WHICH WOULD NOT LET THE LEFT PACK FLOW CONTROL VALVE OPEN. REPLACED P4-78 PANEL AND OPS CHEC KED PANEL PER B727-200MM 26-16-001-5. LEFT PACK FLOW CONTROL VALVE OPS CHECK NORMAL. COMPLIED WITH DECAY CHECK. 2 L 7 3 4F RT A3WE 2008013000023 20080130 00023 EA 2008 1 30 QXEA200800038 1 20080121 A 3320 BR9500106 BALLAST CNDAIR CL600 CL6002C10 1390015 EA CABIN LIGHTS SMOKE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 604QX 10019 PDX - FLIGHT 2614. ELECTRICAL ODOR NOTED AT ROW FOUR. MAINTENANCE REPLACED THE LIGHTING BALLAST. OPERATIONAL CHECKS GO OD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008013000056 20080130 00056 2008 1 30 HALA0800026 4 20080124 A 2565 101656306 SLIDE BOEING 767 7673CB 1385187 NM RT OVERWING DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 592HA 33468 FOUND RT OVERWING SLIDE DOOR UNLATCHED. SLIDE PACK IS BECOMING UNLACED. REPLACED RT OVERWING SLIDE PACK PER AMM 25-65- 01. 2 L 7 2 4F RT A1NM 2008013000059 20080130 00059 2008 1 30 LR7A08023 4 20080121 A 6122 582855 HOUSING LKHEED 382 382G 526414U SO PROP VALVE DAMAGED A LR7A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 405LC 4322 5025 DURING CLIMB-OUT FLIGHT CREW REPORTED SEVERE NR 1 PROPELLER RPM FLUCTUATION. ENGINE SHUTDOWN PERFORMED IAW AFM. NR 1 P ROPELLER VALVE HOUSING REPLACED IAW LAC JOB CARD HN7101 WITH SATISFACTORY OPS CHECK. 2 H 7 4 4T A1SO 2008013000078 20080130 00078 NM 2008 1 30 F3LA200800035 1 20080110 A 5321 D5367151300000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 924FR 5350 2030 DURING C CHECK INSPECTION, CABIN FLOOR PANEL 241F, LOCATED IN THE COCKPIT, HAD THE SECOND SCREW HOLE, ON THE RIGHT FORWA RD SIDE, PULLED THROUGH. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF EA A8-53R-12384. FOLLO WING COMPLETION OF THE REPAIR AND THE INSTALLATION OF THE FLOOR PANEL, IT WAS INSPECTED AND FOUND TO BE ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008013000080 20080130 00080 EU 2008 1 30 F3LA200800032 1 20080107 A 5310 SHEAR PLATE AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE LOOSE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION, THE FORWARD SHEAR PLATE, JUST AFT OF FRAME 68, HAD 7 SOLID RIVETS SHEARED WHERE THE PLATE ATT ACHES TO THE FLOORBEAM. MAINTENANCE REMOVED THE SHEARED RIVETS AND REPLACED THEM WITH LOCK FASTENER IN ACCORDANCE WITH THE REQUIREMENTS OF EA A8-53R-12360. UPON COMPLETION OF THE MAINTENANCE ACTION, THE SHEAR PLATE WAS INSPECTED AND FOUND TO BE ACCEPTABLE. 2 L 7 2 4F 4 F RT 2008013000081 20080130 00081 EU 2008 1 30 F3LA200800033 1 20080107 A 5340 D534711242000 SHEAR PLATE AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION, THE AFT SHEAR PLATE ON THE LEFT SIDE OF THE FUSELAGE, JUST AFT OF FRAME 69, HAD FOUR BLIND FA STENERS SHEARED. MAINTENANCE REMOVED THE SHEARED FASTENERS, REPLACED THE SHEAR PLATE AND INSTALLED A NEW SHEAR PLATE AN D FASTENERS IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. FOLLOWING THE COMPLETION OF THE MAINTENANCE ACTION, TH E SHEAR PLATE INSTALLATION WAS INSPECTED AND FOUND TO BE ACCEPTABLE. 2 L 7 2 4F 4 F RT 2008013000084 20080130 00084 SO 2008 1 30 SIMA200802805 1 20080124 A 3297 14621495403 WIRE HARNESS EMB 135 EMB135KL 3260302 SO NLG PROX SWITCH DAMAGED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 838AE 145651 ON FLIGHT 3006, CREW REPORTED AIR/GND FAIL MESSAGE WHEN RETRACTING THE LANDING GEAR. GEAR REMAINED DOWN WITH 3 GREEN LI GHTS. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NOSE LANDING GEAR HARNESS IAW EMB140 AMM 32-61-02. PERFORME D OPERATIONAL CHECK ON LANDING G EXTENSION AND RETRACTION IAW EMB 140 AMM 32-30-00. OPERATION CHECK GOOD. FOUND PIN BR OKEN ON NOSE NLG PROX SWITCH AND REMOVED AND REPLACED NOSE LANDING GEAR PROX SWITCH IAW EMB 140 AMM 32-68-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008013000086 20080130 00086 SO 2008 1 30 SIMA200802804 1 20080123 A 2121 4611028900 FAN EMB 135 EMB135LR 3260305 SO NR 2 ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 716AE 145264 ON FLIGHT 4806, TAXI IN CREW NOTED A BURNED ODOR IN THE COCKPIT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED N R 2 REC FAN IAW EMB AMM 21-24-01. OPERATIONAL CHECK GOOD. REMOVED AND REPLACED NR 2 REC FAN MUFFLER DUCT IAW EMB AMM 2 1-22-06. OPERATIONAL CHECK AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008012200376 20080122 00376 NM 2008 1 22 KCSA081020 1 20080115 A 5311 FRAME BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 CORROSION ON BS 480 CIRCUMFERENTIAL FRAME UPPER CHORD AROUND NUT PLATES BETWEEN LBL-36 AND LBL-44. 2 L 7 4 4F RT A20WE 2008012200381 20080122 00381 NM 2008 1 22 2008UALA00302 1 20080117 A 5610 WINDOW BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT CRACKED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 364UA 24533 FLIGHT DIVERTED DUE TO CRACKED L4 WINDOW. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300004 20080123 00004 WP 2008 1 23 08FDEA00157 1 20080115 A 5230 AFA71321 SUPPORT FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 UPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 4 IS CRACKED IN HOLES "A, C, D" BEYOND SRM LIMITS. REPLACED SUPPO RT FITTING NR 4 MAIN CARGO DOOR SPOOL LOCATION IAW SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2008012300005 20080123 00005 EA 2008 1 23 SWIA200819065 1 20080116 A 2913 6619004 PUMP CNDAIR CL600 CL6002C10 1390015 EA HYDRAULIC SYSTEM LEAKING A SWIA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 07 776SK 2226 2226 10241 HYDRAULIC SYSTEM NR 2 RESERVOIR QUANTITY SHOWS 0 PERCENT, FLIGHT NR 5825. REPLACED NR 2 EDP IAW CRJ AMM 29-11-00. 2 L 7 2 4F RT A21EA 2008012300021 20080123 00021 EU 2008 1 23 2008UALA00005 1 20080101 A 5210 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 497UA 1847 BOTTLE AT DOOR 2R INDICATES LOW. SERVICED DOOR ASSIST BOTTLE, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012300025 20080123 00025 NM 2008 1 23 DL764080009 1 20080105 A 4900 33183001 BATTERY BOEING 767 767432ER 1385134 NM APU OVERHEATED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 833MH 29706 ON PRE-DEPARTURE CHECK ALL PASSENGERS OFF AIRCRAFT. FOUND SMOKE IN AFT CABIN. CORRECTIVE ACTION WAS TO REPLACE APU BAT TERY FOR SMOKE AND APU BATTERY CHARGER PRECAUTIONARY. 2 L 7 2 4F RT A1NM 2008012300033 20080123 00033 NM 2008 1 23 DL757080013 1 20080107 A 3150 WARNING LIGHT BOEING 757 757232 1384965 NM TE FLAPS FALSE ACTIVATION A DALA O OTHER N FALSE WARNING LD LANDING 1 SO 27 6712B 30484 T/E FLAP DISAGREE MSG ACCOMPLISHED 20 DEGREE FLAP LANDING IAW QRH. CK'D FSEU NO FAULTS. RAN FLAPS/SLATS SEVERAL TIMES ALL OPS NML.PER MCC CK'D AND LUBED ALL TRANSMISSIONS AND TORQUE LIMITERS. FOUND BOTH INBOARD TRANSMISSIONS LOW SERVICED FULL. LUBED ALL JACK SCREWS GIMBLE BEARINGS. RAN SEVERAL MORE TIMES ALL OPS NML. 2 L 7 2 4F RT A2NM 2008012300056 20080123 00056 NM 2008 1 23 DL76L080022 1 20080109 A 5412 311T32819 BULKHEAD BOEING 767 767332 1382001 NM NR 1 NACELLE MISREPAIRED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 171DN 24759 DURING ACCOMPLISHMENT OF S/B 767-54-0080, SEVERAL OVERSIZE HOLES WERE FOUND IN THE MIDSPAR WEB AND AFT BULKHEAD WEB. TH E HOLES WERE INSPECTED AND OVERSIZE FASTENERS WERE INSTALLED. 2 L 7 2 4F RT A1NM 2008012200008 20080122 00008 EA 2008 1 22 TRAX200800027 1 20080103 A 5260 STEP CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 PAX DOOR BOTTOM STEP IS CRACKED ON FWD SIDE. 2 L 7 2 4F RT A21EA 2008012200032 20080122 00032 CE 2008 1 22 ACE011208 1 20080112 A 3245 G195X6758 TUBE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA TIRE LEAKING E YADA O OTHER E VIBRATION/BUFFET LD LANDING 1 AL 03 111AX 6 UC81 PILOT REPORTED NOSE TIRE FLAT ON LANDING. REPLACED TIRE ASSEMBLY DUE FAILED INNER TUBE. WE ARE EXPERIENCING MULTIPLE F AILURES, BURST TUBES FROM THIS MFG. MFG PREVIOUSLY NOTIFIED. 2 L 7 2 4T 4 T RT A24CE E4EA 2008012200069 20080122 00069 CE 2008 1 22 DXTA200802771 1 20080116 A 3230 1106P59 RELIEF VALVE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG STICKING E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 671QS 7058 5605071 GEAR WOULD NOT RETRACT AFTER TAKEOFF. R & R LT UPLOCK ACTUATOR WITH NEW. FOUND HYD RELIEF VALVE OUT OF TOLERANCE, REPLAC ED WITH OVERHAULED UNIT FROM PNEUDRAULICS RS PD6R469J, PRESSURE SWITCH & LT MLG ACTUATOR WITH SERVICEABLE UNIT FROM CESS NA ICT RS CNQB9181 WORK PERFORMED IAW MM. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008012200071 20080122 00071 CE 2008 1 22 DJFA2008002 1 20080111 A 3240 BRAKE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG INOPERATIVE E DJFA O OTHER O OTHER LD LANDING 1 EA 23 815TA 258534 CREW REPORTED BREAKS REQUIRED EXCESSIVE PRESSURE TO ACTUATE. PEDALS NEEDED TO BE PUSHED NEARLY TO FULL TRAVEL TO OBTAIN BRAKING ACTION. MAINTENANCE BLED THE BRAKES AND CHECKED THE SYSTEM. THE SYSTEM CHECKED OK. 2 L 7 2 4F 4 F RT A3EU E6WE 2008012200090 20080122 00090 EA 2008 1 22 TRAX200800049 1 20080105 A 3241 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA ANTI-SKID SYS MALFUNCTIONED A ASOA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SO 27 738EV 10146 ANTI-SKID INBOARD CAUTION MSG ILLUMIMATED CYCLED ANTI-SKID CONTROL UNIT CIRCUIT BREAKERS. PERFORMED OPS CHK. MSG EXTIN GUISHED. EMERGENCY DECLARED. EN ROUTE TO EYW A/C DIVERTED TO NQX DUE TO MTC. FLT 4465 DEL 52 MINS. 2 L 7 2 4F RT A21EA 2008012200096 20080122 00096 EU 2008 1 22 TRAX200800051 1 20080104 A 5320 INTERCOSTAL AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 INTERCOSTAL CRACKED IN LEFT MLG W/W AT FR 27. 2 H 7 2 4T RT 2008012200147 20080122 00147 EU 2008 1 22 F3LA200800004 1 20080102 A 5330 D53112122206 SKIN AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 15198 42 2051 DURING C-CHECK MAINTENANCE ACTIONS, PREVIOUS, TEMPORARILY REPAIRED LIGHTENING STRIKE DAMAGE WAS PERMANENTLY REPAIRED. T HE REPAIR WAS ACCOMPLISH IAW TDI/RW 0000838 ON THE LT FORWARD FUSELAGE. THE REPAIR WAS ACCOMPLISHED IAW THE REQUIREMENT S OF EA A8-53R-10670, REV E. THIS ACTION CLOSES OUT TDI/RW 000478. HOLES 1, 2 AND 3 WILL BE PERMANENTLY REPAIRED WITHI N 4680 LANDINGS. SEE NON-ROUTINE C035074. 2 L 7 2 4F 4 F RT 2008012200166 20080122 00166 NM 2008 1 22 2008UALA00102 1 20080106 A 3350 58781 LIGHT BOEING 737 737322 1384676 NM CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 326UA 23958 EEL FLOOR LIGHTS FROM ROW 15 TO REAR OF PLANE IS INOP. REPLACED POWER STRIP. 2 L 7 2 4F RT A16WE 2008012200210 20080122 00210 NM 2008 1 22 08FDEA00113 1 20080111 A 5315 146N50042 FLOORBEAM BOEING 757 7572B7 1384964 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 FLOOR I BEAM STA. 1260 LOWER FLANGE HAS MISSING NUTPLATE WITH A DOUBLE DRILLED HOLE, RBL 18, FWD SIDE. REPAIRED FLOORBE AM IAW SRM 53-00-51, FIG 201 WITH REPAIR ANGLE FABRICATED ON TRAVELER NR T7/710125 AND FROM MATERIAL 7075T6 .125C FOR FI LLER AND .050 FOR STRAP. TREATED AND PRIMED AREA, PARTS IAW SRM 51-20-01. TOP COATED REPAIR AREA IAW SOPM 20-41-02. 2 L 7 2 4F RT A2NM 2008012200211 20080122 00211 NE 2008 1 22 Y2PA200800028 2 20080111 A 7200 B-NUT AMD FALC20 FALCON 2720302 EU GE CF700 CF700* 30010 NE P3 LINE LOOSE A Y2PA A UNSCHED LANDING R X J PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 23 822AA 195 304526B IN CRUISE NR 1 ENGINE SURGED THEN ROLLED BACK AND FLAMED OUT. CREW REQUESTED IMMEDIATE DESCENT FROM FL350 AND VECTORS T O NEAREST SUITABLE AIRPORT. CREW DECLARED AN EMERGENCY FOR THE NR 1 ENGINE WOULD NOT RELIGHT AND DIVERTED TO MLI. AIRC RAFT LANDED ON SINGLE ENGINE WITHOUT INCIDENT. USA JET MAINTENANCE CONTRACTED A MECHANIC WHO PERFORMED A FOD INSPECTION WITH NO DEFECTS FOUND. PERFORMED A VISUAL INSPECTION OF THE ENGINE AND FOUND P3 AIR LINE B-NUT LOOSE. SECURED B NUT A ND PERFORMED ALL REQUIRED ENGINE RUNS IAW GMM VOLUME 3 "STALL/FLAME OUT PROCEDURE CHECKS" ALL ENGINE PARAMETERS ARE WITH IN LIMITS, RESTRICTED ALTITUDE TO FL330. AIRCRAFT RETURNED TO MAIN BASE AT YIP ON 1/12/08 AND MAINTENANCE PERFORMED A 2 L 7 2 4F 4 F A7EU E7EA 2008012200228 20080122 00228 EA 2008 1 22 TRAX200800048 1 20080105 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 904EV 7628 PAX DOOR AFT SIDE DRAG ANGLE CRACKED JUST ABOVE MOTOR CABLE BOTTOM PULLEY. REPAIRED DAMAGED SECTION OF DRAG ANGLE PER R EO 601R-52-11-513. REPAIRED DAMAGED SECTION OF DRAG ANGLE PER REO 601R-52-11-513. CUT OUT DAMAGED SECTION PER REO 601R -52-11-513. FABRICATED REPAIR PARTS PER REO 601R-52-11-513. INSTALLED REPAIR PARTS PER REO 601R52-11-513. REPAIRED DA MAGED SECTION OF DRAG ANGLE PER REO 601R-52-11-513 CUT OUT DAMAGED SECTION PER REO 601R-52-11-513. PERFORMED EDDY CURRE NT INSPECTION OF CUT LINES ON AIRSTAIR DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513 PER CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. FABRICATED REPAIR PARTS PER REO 601R-52-11-513. INSTALLED REPAIR PARTS PER REO 601R52-11-513 2 L 7 2 4F RT A21EA 2008012200250 20080122 00250 NM 2008 1 22 AALA200800005 1 20080101 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 768AA 33540 JFK - EMERGENCY LIGHT AT SEAT 20G MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 20G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008012200274 20080122 00274 NM 2008 1 22 08FDEA00103 1 20080110 A 5310 143N832852 CREASE BEAM BOEING 757 757200 1384950 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 CORROSION ALONG RT CREASE BEAM INBOARD CHORD L ANGLE AT STA 660-686, S-17R. REPLACED AS PER EA F-5310-117337. REPAIR IS CLASSIFIED MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008012200283 20080122 00283 NM 2008 1 22 08FDEA00130 1 20080114 A 5754 WEDGE BOEING 757 757200 1384950 NM NR 6 SLAT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR, SLAT NR 6 TRAILING EDGE WEDGE EXTERNAL DOUBLER (REF: 4X-BY EXTERNAL DAMAGE RECORD SHEET ENTRY NR R4) TO EVALUATE EXISTING REPAIR. ACCOMPLISHED EVALUATION IAW ATTACHMENT B OF EO F-5100-7-5001 P1. EXISTING REPAIR DOUBLER AT NR 6 SLAT IS AN INTERIM REPAIR. REPLACED DOUBLER IAW B757-200 SRM 51-70-10, REPAIR 4, FIG 201 SHT 1 OF 5 REV 93. T HE NEW 7" BY 9" REPAIR DOUBLER IS CLASSIFIED AS A MAJOR REPAIR PER GMM 6-2-100 CRITERIA. THIS IS A PERMANENT REPAIR. N O FOLLOW-UP ACTION REQUIRED. 2 L 7 2 4F RT A2NM 2008012200307 20080122 00307 NM 2008 1 22 2008UALA00063 1 20080103 A 2560 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FLASHLIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 563UA 26665 FLASHLIGHT AT 2L POWER LIGHT INOPERATIVE. BATTERY FAILED. REPLACED FLASHLIGHT BATTERY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012200313 20080122 00313 NM 2008 1 22 MWEA080004 1 20080107 A 5330 5920323581 SKIN BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 925ME 55191 AFT OF FORWARD CARGO DOOR CAUSING DAMAGE. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED SKIN. 2 L 7 2 4F TR A6WE 2008012200322 20080122 00322 NM 2008 1 22 USAA920080142 1 20080105 A 5755 654645151 PANEL BOEING 737 7373B7 1384580 NM NR 2 SPOILER DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 332AW 23384 PHX - MAJOR REPAIR - B CHECK - LEFT WING NR 2 SPOILER PANEL DISBONDED. REPLACED LEFT WING NR 2 SPOILER PANEL. 2 L 7 2 4F RT A16WE 2008012200338 20080122 00338 NM 2008 1 22 08FDEA00146 1 20080115 A 5347 BAC1520792 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 MAIN CARGO SEAT TRACK IS CORRODED, BS 1090 - 1130 , RBL 46 REMOVED CORROSION ORG THICKNESS 1.36, LOSS OF .012" MIN THIC KNESS 1.348". FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK AND FABRICATED NEW TRACK. REF SRM 51-30- 02, SRM 53-10-2, BOEING DWG BAC1520-792. INSTALLED NEW SEAT TRACK REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008012200340 20080122 00340 NM 2008 1 22 08FDEA00147 1 20080115 A 5320 25FX1253119 SUPPORT ANGLE BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 MAIN DECK CEILING PNL SUPPORT ANGLE IS BUCKLED/CRACKED, BS 620, LBL 14. REPLACED SUPPORT ANGLE AT BS 620, LBL 14 REF SR M 51-30-2 PG 7. FABRICATED NEW SUPPORT REF FED EX DWG 25FX1253. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008012200351 20080122 00351 EU 2008 1 22 TRAX200800071 1 20080104 A 5260 PANEL AEROSP ATR72 ATR72 EU PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 PAX DOOR STAIRCASE, VERTICAL PANEL NR 1 FROM TOP, LIGHT DOUBLER CORRODED. 2 H 7 2 4T RT 2008012200361 20080122 00361 EA 2008 1 22 TRAX200800081 1 20080111 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 843AS 7310 AAR - CLIP CRACKED O/B OF LBL 27. 2 L 7 2 4F RT A21EA 2008012300006 20080123 00006 EA 2008 1 23 SWIA200819066 1 20080116 A 5610 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 715SK 10179 UPON INITIAL DESCENT, THE RIGHT WINDSHIELD CRACKED, FLIGHT NR 5927. REPLACED THE WINDSHIELD PER CRJ MM 56-11-01, PN: NP -139321-6, SN OFF: 0415CH6544. 2 L 7 2 4F RT A21EA 2008013000089 20080130 00089 2008 1 30 SIMA200802101 4 20080115 A 3425 HG2010A002 COMPUTER EMB 135 EMB135LR 3260305 SO AHRS MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 729AE 145343 ON FLIGHT 4914 CREW REPORTED ON CLIMB-OUT, AMBER ATT FAIL AND AMBER HDG FAIL ON CAPTAINS SIDE. AIRCRAFT REMOVED FROM SE RVICE. REMOVED AND REPLACED AHRS NR 1 COMPUTER IAW EMB-135 AMM 34-21-01. PERFORMED AHRS OPS CHECK IAW EMB-135 AMM 34-2 1-00. OPERATIONAL CHECK GOOD. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008013000091 20080130 00091 SO 2008 1 30 SIMA200802108 1 20080118 A 2720 15H0048PH PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO RUDDER MALFUNCTIONED A SIMA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 928AE 14500911 ON FLIGHT 3509 CREW REPORTED YAW DAMPER FAIL AND AUTO PILOT KICKED OFF DURING CLIMB FOLLOWED BY RUDDER SYSTEM 1/2 INOP E ICAS MESSAGE. CREW ELECTED TO RETURN TO DFW FOR MAINTENANCE DECLARED EMERGENCY PRIOR TO LANDING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RUDDER NR 2 PRESSURE SWITCH IAW EMB 145 AMM 27-23-04. PERFORMED OPERATIONAL CHECK OF TH E RUDDER SYSTEM, J2 AMM 27-23-00. OPERATIONAL CHECK GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008013000092 20080130 00092 SO 2008 1 30 SIMA200802111 1 20080118 A 3297 WIRE HARNESS EMB 145 EMB145LR 3260212 SO NLG WOW DAMAGED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 619AE 145101 ON FLIGHT 4370, CREW REPORTED LANDING GEAR DID NOT RETRACT AFTER TAKEOFF WITH ASSOCIATED AIR GROUND CAUTION MESSAGE ON E ICAS. AIRCRAFT REMOVED FROM SERVICE. PERFORMED GVI AND CONTINUITY TEST OF THE NLG WOW PROX SWITCH HARNESS FROM PIN C T O HARNESS SHIELDING AND VOLTAGE READINGS. CONTINUITY AND VOLTAGE READINGS NORMAL. NO DEFECTS NOTED. PERFORMED OPERATI ONAL CHECK OF AIR/GROUND SYSTEM IAW AE MTX WC NR 32-700-16. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008013000094 20080130 00094 EU 2008 1 30 SIMA200802113 1 20080103 A 5347 7253725191 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 273AE 25047 5000 340B273 AIRCRAFT WAS REMOVED FROM SERVICE. DURING A HMBV INSPECTION, THE SEAT TRACK AT B.L. 18.3L WAS FOUND TO BE CORRODED. RE MOVED CORRODED SEAT TRACK AND REPLACED WITH NEW PART NUMBER 7253725-193 IAW SAAB SRM CHAPTERS 53-70-60. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4T RT A52EU 2008013000095 20080130 00095 EU 2008 1 30 SIMA200802109 1 20080120 A 7930 8346501 SENSOR SAAB SF340 340B 7860101 EU ENG OIL PRESSURE MALFUNCTIONED A SIMA E ENGINE SHUTDOWN N FALSE WARNING AP APPROACH 1 SW 21 904AE 340B314 ON FLIGHT 9821 - CREW REPORTED WHILE DOING TRAINING FLIGHT E1 OIL PRESSURE SHOWED 30 LBS CREW SHUT E1 DOWN AND DECLARED EMERGENCY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENG OIL PRESS SENSOR AND OIL PRESS SWITCH IAW SAAB MM 79-30-05. OPS CHECK GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2008013000096 20080130 00096 SO 2008 1 30 SIMA200802110 1 20080113 A 2160 C143236 VALVE EMB 135 EMB135LR 3260305 SO TEMP CONTROL MALFUNCTIONED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 730KW 145346 ON FLIGHT 4891, CREW REPORTED DURING TAXI AND WITH APU ON RECEIVED EICAS PACK 2 OVERHEAT ACCOMPANIED BY A BURNING ODOR. AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF RIGHT PACK SYSTEM. NO DEFECTS NOTED. SUSPECT DUAL TEMP CONTROL VALVE. REMOVED AND REPLACED DUAL TEMP CONTROL VALVE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008013000103 20080130 00103 EU 2008 1 30 TRBA20080002 1 20080107 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 369AT 369 FOUND FLOORBEAM 39 CORRODED. FLOORBEAM 39 REPAIRED IAW SRM 53-00-00 FIG 436. 2 H 7 2 4T RT A53EU 2008013000107 20080130 00107 EU 2008 1 30 TRBA2008005 1 20080113 A 3350 30125000 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 538AT 538 EMERGENCY LIGHT FOR SERVICE DOOR INOP. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT AND OPERATIONALY TESTED IAW JI C 33-50-00 OPT 10000. TESTED SATISFACTORY. 2 H 7 2 4T RT A53EU 2008013000121 20080130 00121 NM 2008 1 30 08FDEA00234 1 20080123 A 5315 652083272 FLOORBEAM BOEING 727 727233 138408A NM BS 950D CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 MAIN DECK FLOORBEAM UPPER TEE CAP CORRODED, BS 950D, LBL 10-13. REMOVED CORROSION. FOUND OUT OF LIMITS IAW PF SRM 53-1 0-1 FIG 4C. REPAIRED DAMAGED FLOORBEAM IAW SRM 53-10-8 PG 18 FIG 3 UPPER CHORD REPAIR. THIS IS CLASSIFIED AS A MAJOR R EPAIR. 2 L 7 3 4F RT A3WE 2008013000122 20080130 00122 NM 2008 1 30 08FDEA00235 1 20080123 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 950D CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 MAIN DECK FLOORBEAM UPPER TEE CAP CORRODED, BS 950D, RBL 9-23. REMOVED CORROSION. OUT OF LIMITS IAW SM 53-10-8, SRM 51 -10-6. DISPLACED SEAT TRACK BS 950-950F RBL 25 IAW SRM 51-30- 2. REMOVED CHANNEL STIFFNER BS 950D, RBL 25. REMOVED CHA NNEL SUPPORT BS 950D-950E, RBL 25 IAW SRM 51-30-2. CUT OUT DAMAGE IAW SRM 53-10-8, TREATED AND PRIMED CUT OUT AREA, IA W SRM 51-10-2. FABRICATED REPAIR PARTS IAW SRM 53-10-8 FIG 1, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS, INSTALLED CHANNEL STIFFNER AT BS 950, RBL 25, INSTALLED CHANNEL SUPPORT, BS 950D-950E RBL 25. INSTALLED S EAT TRACK STA 950. 2 L 7 3 4F RT A3WE 2008013000128 20080130 00128 NM 2008 1 30 08FDEA00194 1 20080118 A 3020 DUCT BOEING 727 727227 1384078 NM ANTI-ICE SYS SEPARATED A FDEA J A DUMP FUEL UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 483FE 21465 DURING CLIMB-OUT WITH CLIMB POWER SET AND PASSING 3500 FT MSL, NR 2 ENG FIRE HANDLE AND BELL ACTIVATED. COMPLIED WITH Q RH AND DUMPED 400 LBS OF FUEL. LANDED AT MEM. FOUND NR 2 ENG COWL ANTI-ICE DUCT SEPARATED AFT OF VALVE DUCT DAMAGED. R EMOVED AND REPLACED NR 2 ENG LT A/I AFT DUCT SECTION PER MM 75-10-012-4. OPS AND LEAK CHECKS GOOD IN REFERENCE TO MM 75 -10-000-2. 2 L 7 3 4F A3WE 2008013000130 20080130 00130 NM 2008 1 30 QXEA200800035 1 20080117 A 3297 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM MLG DAMAGED A QXEA O OTHER O OTHER AP APPROACH 1 NM 09 409QX 4051 SEA - ON APPROACH AFTER GEAR EXTENSION, THE NOSE GEAR DOOR LIGHT REMAINED ILLUMINATED. EVERYTHING ELSE NORMAL. ACCOMPL ISHED A UNEVENTFUL LANDING. AIRCRAFT FERRIED TO PDX FOR REPAIRS. IN PDX, REPAIRED THE NLG ALTERNATE LOCK HARNESS. OPE RATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008013000139 20080130 00139 EA 2008 1 30 SWIA200819080 1 20080115 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DISCHARGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 773SK 10236 FLT 6550 - SEVERAL EMERGENCY LIGHTS ARE INOP. REPLACED NR 3 BATTERY PACK AS REQUIRED, OPS CHECK GOOD, PN: AD-2013-1A, S N OFF: 79415. 2 L 7 2 4F RT A21EA 2008013000143 20080130 00143 NM 2008 1 30 DLM88080069 1 20080116 A 5330 593600419 SKIN DOUG MD88 MD88 3023688 NM BS 731 L29-30R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 CORROSION CUTOUT TO THE SKIN AND INTERNAL DOUBLER AT FS 731 AND LONGERON 29R AND 30. REPAIR WAS ACCOMPLISHED WITH AN EX TERNAL DOUBLER AND TRIPLER. 2 L 7 2 4F RT A6WE 2008013000144 20080130 00144 NM 2008 1 30 DLM90080072 1 20080117 A 5313 LONGERON DOUG MD90 MD9030 3023690 NM BS 1475 L2L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 DURING HMV AT OKC, LONGERON 2L WAS FOUND CRACKED AT STA 1475. THE CRACK WAS REPAIRED PER BOEING INSTRUCTIONS PER ER/A 0 2-465751-14. 2 L 7 2 4F RT A6WE 2008012300034 20080123 00034 NM 2008 1 23 08FDEA00154 1 20080115 A 5315 B27530711 STRAP BOEING 727 727233 138408A NM FLOORBEAM CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 CABIN FLOORBEAM STABILIZER STRAP CRACKED AT STATION 344 AIRCRAFT CENTER LINE, WL 200. STOP DRILLED CRACKS AND FAB AND I NSTALLED A REPAIR PLATE REF SRM 53-10-8, FIG NR 6. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008012300069 20080123 00069 NM 2008 1 23 2008UALA00079 1 20080106 A 2781 SENSOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NR 2 LE FLAP OUT OF TOLERANCE A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 WP 29 933UA 26659 CREW REPORTS NR 2 LEADING EDGE FLAP TRANSIT LIGHT ON OVERHEAD AND TRANSIT LIGHT ON FWD PANEL ILLUMINATED WITH FLAPS EXTE NDED. NO ABNORMAL ROLL FELT. CYCLED FLAPS, NO HELP. FOUND NR 2 EXTEND PROXIMITY SENSOR GAP GREATER THAN ALLOWABLE LI MITS. ALSO FOUND OVER SPRAY ON BOTH THE SENSOR AND THE TARGET. CLEANED BOTH SENSOR AND TARGET AND SET GAP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300071 20080123 00071 NM 2008 1 23 2008UALA00081 1 20080106 A 5514 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU HORIZ STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 LEFT HAND SIDE HORIZONTAL STAB HAS DENT LEFT OF A PATCH. DENT MEASURES 6" X 2.5" AND IS .125" DEEP. LOCATED MIDSPAN ON LOWER SURFACE OF LEADING EDGE. A-Y RATIO IS 48. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300072 20080123 00072 NM 2008 1 23 2008UALA00082 1 20080105 A 5512 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 LEFT HORZ STAB LOWER SKIN CRACKED JUST FWD OF 2ND BALANCE PANEL BAY AT AFT SPAR. INSTALLED EXTERNAL SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300075 20080123 00075 NM 2008 1 23 2008UALA00085 1 20080104 A 2612 8242 FIRE LOOP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 NACELLE FAULTY A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 197UA 26901 NR 2 ENGINE HAS A FIRE LOOP "A" STATUS MESSAGE. REPLACED FIRE DETECTOR PER MM 26-11-02 PG401, OPS CKD GOOD. AC OK FOR S ERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012300076 20080123 00076 NM 2008 1 23 2008UALA00088 1 20080106 A 2520 CONTROL PANEL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN MALFUNCTIONED A UALA B F EMER. DESCENT ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 654UA 25392 THE 8F CONTROL PANEL STARTED SMOKING. REPLACED CONTROL PANEL. OPS CHECKED NORMAL. RAN FOR 10 MINUTES, COOL TO THE TOU CH. CHECKED ALL UNITS IN BUSINESS CLASS, ALL COOL TO THE TOUCH. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012300077 20080123 00077 NM 2008 1 23 2008UALA00089 1 20080107 A 3260 S26 SENSOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NLG FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 938UA 26671 AFTER GEAR RETRACTED NLG RED UNSAFE LIGHT REMAINED ON WITH GEAR HANDLE UP OR OFF. FOUND FAULTY GEAR DOWN SENSOR AND LOC K SWITCH. REPLACED SENSOR AND LOGIC CARD M1215. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300079 20080123 00079 2008 1 23 2008UALA00093 4 20080106 A 3416 ALTIMETER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT FAILED A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 668UA 30024 FIRST OFFICER'S ALTIMETER HAS FAILED. REPLACED AND TESTED F/O BARO ALTIMETER PER MM 34-13-01. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012300080 20080123 00080 NM 2008 1 23 DL764080026 1 20080109 A 2730 2827001011 ACTUATOR BOEING 767 767432ER 1385134 NM RT ELEVATOR LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 828MH 1332 29699 SHORTLY AFTER TAKEOFF FROM HNL FLIGHT 1282 NOTIFIED MCC THAT CTR SYS HYD WAS LOSING FLUID. HAD THE CREW SECURE CTR PUMP S AND QTY STABILIZED. CREW RETURNED TO HNL. TROUBLESHOOTING IN PROGRESS. FOUND RT ELV PCA LEAKING. REPLACE CK OK. 2 L 7 2 4F RT A1NM 2008012300081 20080123 00081 NM 2008 1 23 2008UALA00098 1 20080104 A 3350 58781 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 903UA 25003 AFT 3 EEL STRIPS INOPERATIVE IN CABIN. REPLACED POWER STRIP 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300082 20080123 00082 NM 2008 1 23 DL76G080027 1 20080109 A 2760 285T0017201 ELECTRONIC UNIT BOEING 767 767332 1382001 NM SPOILERS INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 177DZ 29698 RTB DUE TO SPOILER EICAS MSG. REPLACED RT CSEU OPS CK NML. 2 L 7 2 4F RT A1NM 2008012300083 20080123 00083 NM 2008 1 23 2008UALA00099 1 20080107 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 382UA 24657 DOOR 1L OUTSIDE EMERGENCY LIGHT & RIGHT WING OUTSIDE EMERGENCY LIGHT NEXT TO EMERGENCY EXIT DOOR ARE INOPERATIVE. RELA MPED. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300084 20080123 00084 NM 2008 1 23 2008UALA00103 1 20080104 A 5730 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT WING GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 RIGHT WING FIXED L/E GOUGED - PUNCTURED FROM DISLODGED UPSTOP JUST INBOARD OF NR 4 SLAT ACTUATOR. ACCOMPLISHED COMPO SITE SET-UP REPAIR PER SRM 51-70-17 REPAIR 7. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300088 20080123 00088 NM 2008 1 23 2008UALA00109 1 20080105 A 5514 65C25156501 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZONTAL STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 HORIZONTAL STAB CENTER SECTION INTERIOR, RT DIAGONAL I BEAM TRUSS, AFT SIDE OF UPPER FLANGE, GUSSET STIFFENER CRACKED IN RADIUS. REPLACED ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300089 20080123 00089 NM 2008 1 23 2008UALA00110 1 20080106 A 3350 1317 LAMP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 SEAT 3A FWD EMERGENCY LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012300090 20080123 00090 NM 2008 1 23 DL764080028 1 20080110 A 2934 291080111 MONITOR BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL HYD QTY MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 840MH 29718 724741 RTO DUE AT 60 KTS LT HYD QTY INDICATION DROPPED TO ZERO. MTC FOUND LT QTY IND AT TANK FULL. FWD LT QTY IND TO MCO AND PLACARD. INSPECTED AND SHOOK DOWN WIRING AND CP AT TRANSMITTER. NTF. CO NOT DUPLICATE REPLACED HYD QTY MONITOR M122 A S PRECAUTION DUE TO PREV. REINSTALLED PTU SIGNAL WIRE PER MEL. OPS CK GOOD, REMOVED MCO AND PLACARD. 2 L 7 2 4F 4 F RT A1NM E23EA 2008012300094 20080123 00094 NM 2008 1 23 2008UALA00113 1 20080106 A 3510 BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE OXYGEN SYSTEM LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 THE O2 LOW AT DOOR 5R. REPLACED BOTTLE AND MASKS. CHECKED OK. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012300097 20080123 00097 NM 2008 1 23 DL76G080030 1 20080108 A 5330 146T3541 SKIN BOEING 767 767332 1382001 NM BS 1346-1365 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1608 30573 FOUND FUSELAGE SKIN BLEND AT FS 1346-1365 AND STRINGERS 20-21R. 2 L 7 2 4F RT A1NM 2008012300106 20080123 00106 NE 2008 1 23 2008UALA00119 2 20080105 A 7200 PACKING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE LEAKING A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 590UA 28708 726668 INBOUND HIGH OIL CONSUMPTION NR 2 ENGINE. FOUND ENGINE STARTER DRIVE PAD LEAKING. REPLACED PACKINGS AND STARTER DRIVE PAD SEAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300119 20080123 00119 NM 2008 1 23 DLM90080043 1 20080104 A 5320 9911839029 STIFFENER DOUG MD90 MD9030 3023690 NM BS 1486 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 STIFFENER CRACKED AT CANT FRAME 1486 & 10.00 POSITION. REMOVED AND REPLACED STIFFENER IAW MD90 SRM 51-10-05 AND 51-30-0 5. 2 L 7 2 4F RT A6WE 2008012300124 20080123 00124 NM 2008 1 23 DL76G080047 1 20080111 A 2133 3964621 OUTFLOW VALVE BOEING 767 767332 1382001 NM RT A/C PACK UNSERVICEABLE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 175DZ 29696 ON TAXI OUT AFTER STARTING RIGHT ENGINE, RIGHT A/C PACK OFF LIGHT ILLUMINATED ACCOMPANIED BY R PACK OFF EICAS MSG. PACK WORKED ON APU AND LEFT ENGINE BLEED AIR AND POWER. SHUT DOWN RIGHT ENGINE AND PACK AGAIN WORKED AFTER ABOUT 10 MINUTES RE-STARTED RIGHT ENG AND PACK CONTINUED TO WORK FINE. RETURNED TO GATE PER DISPATCHER AND MAINTENANCE DIRECTION. PACK WORKED FINE DURING TAXI IN. CONTROLLER BITE NO FAULTS. REMOVED AND REPLACED RT PACK FLOW CTL VLV LEAK AND OPS CHK NML . RAN ENG W/PACK AS PRECAUTION ALL NML. 2 L 7 2 4F RT A1NM 2008012300126 20080123 00126 2008 1 23 2008UALA00130 4 20080107 A 2330 RDAV216801 MONITOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN MALFUNCTIONED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 215UA 30221 PAX REPORTED FUNNY SMOKE/SMELL AFTER T/O ROWS 22-25. ISOLATED SOURCE AS PERSONAL VIDEO DISPLAY & PULLED ALL C/B'S ASSOC IATED WITH MONITOR. SUSPECT VIDEO MONITOR SHORTED. REPLACED MONITOR OPS CHECK GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008012300128 20080123 00128 NM 2008 1 23 2008UALA00131 1 20080107 A 5712 RIB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 RIGHT WING RIB LOWER CHORD BETWEEN WBL 135.5 AND WING STRINGERS S2 & S3 HAS APPROX 1 INCH CRACK ORIGINATING IN THE CUTOU T RADIUS OF THE LOWER RIB. REMOVED DAMAGE. FABRICATED AND INSTALLED TEE FITTING AND FILLERS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300134 20080123 00134 NM 2008 1 23 2008UALA00135 1 20080107 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 BS 294.5 INTERCOSTAL WEB CRACKED AT STRINGER 7L AND AT STRINGER 16L. REMOVED DAMAGED PARTS. FABRICATED AND INSTALLED R EPLACEMENT INTERCOSTAL WEBS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300140 20080123 00140 NM 2008 1 23 2008UALA00142 1 20080107 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 651UA 25389 EEL LIGHT ADJACENT TO DOOR 1R INOP. REPAIRED EEL STRIP. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012300142 20080123 00142 2008 1 23 2008UALA00144 4 20080108 A 2565 100000308 O-RING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE BOTTLE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 564UA 26666 LOW BOTTLE. FOUND LEAK AT THE CENTER O-RING OF THE TANK. REPLACED O-RING ON CENTER SHAFT. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300148 20080123 00148 NM 2008 1 23 08FDEA00128 1 20080114 A 5280 NNB678619 FRAME DOUG MD11 MD11F 3023600 NM MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 LEFT MAIN LANDING GEAR DOOR, NEAR INBOARD STRUT FAIRING UPPER MOUNTING AREA FOUND CRACKED. CRACK AT LEFT MAIN LANDING GEAR DOOR, NEAR INBOARD STRUT FAIRING UPPER MOUNTING AREA. REPAIRED AS PER FEDEX EA NR 1-3210-116534, TITLE: LANDING G EAR MAIN GEAR DOOR LEFT MAIN LANDING GEAR DOOR FRAME, REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008012300149 20080123 00149 NM 2008 1 23 08FDEA00129 1 20080114 A 5280 NNB678620 FRAME DOUG MD11 MD11F 3023600 NM MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 592FE 48550 RIGHT MAIN LANDING GEAR DOOR, NEAR INBOARD STRUT FAIRING UPPER MOUNTING AREA, FOUND CRACKED. CRACK AT RIGHT MAIN LAND ING GEAR DOOR, NEAR INBOARD STRUT FAIRING UPPER MOUNTING AREA REPAIRED AS PER FEDEX EA NR 1-3210-116535, TITLE: LANDING GEAR, MAIN GEAR DOOR, RIGHT MAIN LANDING GEAR DOOR FRAME REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008012300152 20080123 00152 NM 2008 1 23 08FDEA00138 1 20080115 A 5311 651593630 FRAME BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 CABIN BS 660 FRAME INNER CHORD WORN FROM CONTACT WITH RT SIDEWALL SUPPORT AT STR 11R REMOVED DAMAGE FROM INNER CHORD AND FOUND AREA TO BE OUT OF LIMITS, REF SRM 51-10-1 PG 3, B727 NDT MANUAL PART 4, 51-00-0 FUG 2 TOOL NR IN 22-0028 DUE DATE 2/21/08 AND 53-10-3 PG 2, ITEM R. ORIGINAL THICKNESS IS .056. MATERIAL REMOVED IS .008". MATERIAL REMAINING IS .048" FABRICATED REPAIR DOUBLER REF SRM 53-10-4 PG 1-11. TREATED AND PRIMED DOUBLER AND REPAIR AREA REF SRM 51-10-2 PG 1. I NSTALLED REPAIR DOUBLER REF SRM 53-10-4. THIS IS CLASSIFIED AS MAJOR REPAIR . 2 L 7 3 4F RT A3WE 2008012300164 20080123 00164 NM 2008 1 23 08FDEA00172 1 20080116 A 5230 25FX1253 STRUCTURE BOEING 727 727233 138408A NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 MAIN CARGO DOOR CORNER TRIM CRACKED STOP DRILLED CRACK AND NDT, NO DEFECTS NOTED. VARIFIED MATERIAL FOR REPAIR REF DWG 25FX1253 FABRICATED DOUBLER REF SRM 51-40-3. TREATED AND PRIMED REPAIR REF MM 51-20-000. INSTALLED REPAIR REF SRM 51-4 0-3. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008012300167 20080123 00167 CE 2008 1 23 DXTA200802778 1 20080120 A 3230 LANDING GEAR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NOSE MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 970QS 7500070 AFTER TAKEOFF WHEN GEAR HANDLE WAS MOVED UP MAIN GEAR RETRACTED, NOSE GEAR DID NOT MOVE. JACKED AIRCRAFT & SWUNG GEAR 3 TIMES. OPS CHECKED GOOD. CHECKED NOSE GEAR & WW. ALL CHECKED GOOD. SWUNG GEAR 3 MORE TIMES. GEAR SWUNG NORMAL AND ALL INDICATIONS NORMAL. ALL WORK DONE IAW CE-750 AMM CHAPTER 32-30-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008012300168 20080123 00168 CE 2008 1 23 DXTA200802773 1 20080117 A 3260 WARNING LIGHT RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP RT MLG ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 896QS 258640 AFTER TAKEOFF AND GEAR RETRACTION, THE RT MAIN GEAR (RED ANNUNCIATOR) REMAINED ILLUMINATED. 2 L 7 2 4F 4 F RT A3EU E6WE 2008012300172 20080123 00172 NM 2008 1 23 F3LA200800007 1 20080106 A 5210 504529409 INERTIA REEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE R1 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 924FR 5350 2030 DURING C-CHECK INSPECTION, THE R1 DOOR SAFETY TAPE INERTIAL REEL WAS FOUND TO HAVE CORROSION ON IT. MAINTENANCE REMOVED AND REPLACED THE R1 DOOR SAFETY TAPE INERTIA REEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-40-00. FOLLOWING COMPLETION OF THE INSTALLATION, IT WAS INSPECTED AND FOUND TO BE ACCEPTABLE. REFERENCE NON-ROUTINE 25802. 2 L 7 2 4F 4 F RT A28NM 2008012300176 20080123 00176 NM 2008 1 23 NWAA080126301 1 20080114 A 2612 CIRCUIT CARD BOEING 747 747451 1384940 NM APU FIRE DETECT DAMAGED A NWAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 01 661US 23719 DURING TAKEOFF, APU FIRE WARNING ACTUATED. TAKEOFF WAS ABORTED AT LESS THAN 30 KNOTS. MAINTENANCE REMOVED AND REPLACED APU FIRE WARNING AND DETECTION CARDS. OPERATIONAL CHECKED GOOD, AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008012300185 20080123 00185 NM 2008 1 23 2008UALA00176 1 20080110 A 2150 8102099 ACM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LEFT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 768UA 26919 REPORT OF ODOR AND SLIGHT HAZE IN BUSINESS CLASS, ALSO NOTICED IN FLT DECK. ACCOMPLISHED TROUBLESHOOTING. REPLACED REC IRC FAN, BUT PROBLEM STILL EVIDENT. REPLACED LEFT SIDE AIR COND PACK AIR CYCLE MACHINE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008012300210 20080123 00210 NM 2008 1 23 ASAA0852461 1 20080110 A 2130 71231997303 CABIN PRESSURE BOEING 737 737890 1384527 NM MALFUNCTIONED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 570AS 35185 THE "AUTO FAIL" AMBER LIGHT ON PRESSURIZATION PANEL ILLUMINATED DURING PRE-FLIGHT. PERFORMED FIM 21 31 TASK 801. SYSTE M RESET, NO FAULTS NOTED. NO HISTORY. OP CHECKS GOOD. 2 L 7 2 4F RT A16WE 2008012300212 20080123 00212 NM 2008 1 23 UPS08551389 1 20080108 A 3260 MODULE BOEING 757 75724APF 1384969 NM RT MLG WARNING FAULTY A IPXA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 01 474UP 28844 INSPECTION TYPE:N/A ATB - RIGHT MLG INDICATING DOWN AND LOCKED WITH GEAR HANDLE IN NEUTRAL POSITION. *SUPPLEMENTAL SDR* T/S PER FIM 32-61-00 FIG 103. ALSO HAD MX MSG RT GEAR DOWN, T/S TO BLOCK 21. REMOVED AND REPLACED PSEU IAW MM 32-09- 04-4. TESTS GOOD IAW SAME MM. REMOVED RT GEAR LIGHT MODULE PER MM 33-16-02-2 AFTER RE-TERMINATING PINS 2 & 3. CHECKED GOOD ON GEAR SWINGS. REMOVED AND REPLACED RELAY K10370 PER WDM 32-61-00-5. PERFORMED GEAR SWING/ALT EXT IAW MM 32-35- 00-5. ALL CHECK GOOD. 2 L 7 2 4F RT A2NM 2008012300217 20080123 00217 NM 2008 1 23 UPS08651395 1 20080111 A 3240 91816EM81791 VALVE BOEING 767 76734AF 1385212 NM PARKING BRAKE MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 315UP 27743 INSPECTION TYPE:N/A BTB - A/C TURNS LEFT DURING BRAKING. REMOVED AND REPLACED PARKING BRAKE VALVE IAW AMM 32-44-04-4. 2 L 7 2 4F RT A1NM 2008012300222 20080123 00222 NE 2008 1 23 ASAA0892463 2 20080108 A 7200 CFM567B26 ENGINE BOEING 737 737990 NM CFMINT CFM56 CFM567B26US NE NR 2 OVERSPEED A ASAA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 02 320AS 33680 890571 DURING CLIMB AT APPROX 9000FT NR 2 ENGINE STARTED SURGING. N1 RANGED FROM 60% TO IN EXCESS OF 100%. ENGINE ANTI ICE ON . PULLED NR 2 ENGINE TO IDLE. ENGINE OPERATED NORMAL AT IDLE. ENGINE NR 2 EEC BITE SHOWS FAULT 73 20322. EEC EXC PAG E SHOWS NR 2 ENGINE N1 AT 106.4% (OVERSPEED) FOR .02 SECONDS. REFERENCE LOG 6308286 FOR ENGINE REPLACEMENT. 2 L 7 4 4F 4 F RT A16WE E00055EN 2008012200272 20080122 00272 WP 2008 1 22 08FDEA00122 1 20080114 A 5512 ALC7439Y502 SKIN DOUG MD10 MD1010F 3022112 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 1 5/8" CRACK LOCATED ON THE RT HORIZONTAL STABILIZER AT THE INBOARD AFT CORNER OF THE OUTER SECTION UPPER AFT SKIN PANEL . END OF CRACK MARKED AND VERIFIED WITH HFEC INSPECTION. REPAIRED SKIN PLANK IAW EA 8-5510-116939, MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008012200304 20080122 00304 NM 2008 1 22 2008UALA00060 1 20080103 A 5320 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 300 S10L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FUSELAGE INTERCOSTAL ATTACH ANGLE ABOVE STR 10L IS CRACKED BS 300. INSTALLED AUXILIARY INTERCOSTAL, ATTACH CLIPS AND "H " STRAP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012200356 20080122 00356 EA 2008 1 22 TRAX200800076 1 20080110 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 317CA 10055 FS 280 TRANSVERSE BEAM CORRODED BEYOND LIMITS AND CRACKED. 2 L 7 2 4F RT A21EA 2008012200363 20080122 00363 EA 2008 1 22 TRAX200800083 1 20080111 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 843AS 7310 AAR - CLIP CRACKED I/B OF RBL 36. 2 L 7 2 4F RT A21EA 2008012200372 20080122 00372 EU 2008 1 22 2008UALA00071 1 20080104 A 3350 D9239003500060 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 498UA 1865 EMERGENCY EXIT LIGHTS ABOVE DOORS FLASH ON-OFF. DISCO EFFECT ON ALL POWER TRANSFERS. WEAK BATTERY. FOUND AFT LEFT EME RGENCY EXIT BATTERY INOP. REPLACED BATTERY, CHECKS NORMAL AT THE GATE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012300001 20080123 00001 NM 2008 1 23 USAA920080143 1 20080107 A 3350 SWITCH BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 201UU 27810 MCN - EES - C4 CHECK - EMERGENCY SLIDE LIGHTS AT L1, R1, L2 & R2 DOORS ARE INOPERATIVE WHEN NLG EMER LT TEST SWITCH IS O PERATED. REPLACED AND FUNCTIONAL CHECKED L1 DOOR TEST SWITCH S10292 IAW B757 AMM 33-51-00. 2 L 7 2 4F RT A2NM 2008012300007 20080123 00007 EA 2008 1 23 SWIA200819067 1 20080116 A 4930 SOLENOID CNDAIR CL600 CL6002B19 1900309 EA APU LEAKING A SWIA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 409SW 7056 FUEL COULD BE DETECTED IN THE CABIN WHEN APU AUTO SHUTDOWN, FLIGHT NR 3946. REPLACED APU FUEL SOLENOID IAW MM 49-31-00. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2008012300036 20080123 00036 NM 2008 1 23 2008UALA00076 1 20080106 A 3510 OXYGEN MASK BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE COCKPIT FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 670UA 29240 CAPT'S OXYGEN MASK INHALATION VALVE FLUTTERS WHEN USED. REPLACED CAPT`S OXYGEN MASK ASSY PER MM 35-11-51. LEAK CHECK G OOD AND MIC OPS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012300052 20080123 00052 NM 2008 1 23 DL757080014 1 20080108 A 5330 146N853010 SKIN BOEING 757 757232 1384965 NM BS 1440 S28R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 612DL 22819 FUSELAGE SKIN, FRAME AND STRINGER FOUND CORRODED AT STA 1440 STR 28R. A SKIN DENT WAS ALSO FOUND AT STA 1425. DAMAGE W AS CUTOUT, STRINGER AND BEAR STRAP WERE SPLICED AND SKIN REPAIRS WERE INSTALLED. 2 L 7 2 4F RT A2NM 2008012300073 20080123 00073 NM 2008 1 23 2008UALA00083 1 20080105 A 5311 FITTING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 AFT CARGO BAY, STA 1285, RBL 42, AFT SIDE OF FRAME UPPER FITTING IS CRACKED. REPLACED FITTING REF SRM 51-40-02. FAB FI TTING REF BAC DWG 146T8068 AND REO-G1221 REV-A BY MECH, AND INSP QC. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012300098 20080123 00098 NM 2008 1 23 DLM88080032 1 20080110 A 2130 UNKNOWN DOUG MD88 MD88 3023688 NM PWA 4060 PW4060 52119 NE CABIN PRESSURE UNKNOWN A DALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 27 910DL 49541 724741 DURING CLIMB-OUT, CABIN WOULD NOT REPRESSURIZE. BOTH AUTO CONTROLLERS ATTEMPTED. DURING RETURN CABIN REPRESSURIZED BIT E BOTH CONTROLLERS NO FAULTS FOUND. RAN OUTFLOW VALVE, MANUALLY CKS GOOD OK FOR SERVICE. 2 L 7 2 4F 4 F RT A6WE E24NE 2008012300105 20080123 00105 NM 2008 1 23 2008UALA00118 1 20080106 A 3350 767 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 532UA 25072 L2 DOOR SLIDE LIGHT ASSY IS BROKEN. REMOVED AND REPLACED SLIDE LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300107 20080123 00107 NM 2008 1 23 2008UALA00120 1 20080104 A 2612 CONTROL PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE CONTROL INOPERATIVE A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 508UA 24744 DURING SQUIB TEST FWD AND AFT CARGO LIGHT SMOKING AND INOP. FOUND INTERNAL SHORT IN CONTROL PANEL FOR SQUIB TEST. REPL ACED SQUIB TEST CONTROL PANEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012300118 20080123 00118 NM 2008 1 23 DLM90080042 1 20080106 A 5740 ATTACH FITTING DOUG MD90 MD9030 3023690 NM RT ELEV FAIRING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 RT ELEV AFT FAIRING CLIP CRACKED. REMOVED AND REPLACED RT ELEV AFT FAIRING CLIP IAW 51-30-2. 2 L 7 2 4F RT A6WE 2008012300123 20080123 00123 NM 2008 1 23 DL76S080046 1 20080109 A 5330 SKIN BOEING 767 767332 1382001 NM BS 196 S21-24L DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 138DL 25409 THE FUSELAGE SKIN WAS FOUND WITH LIGHTNING STRIKE DAMAGE AT STA 196.5 BETWEEN S-21L AND S-24L. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED. 2 L 7 2 4F RT A1NM 2008012300125 20080123 00125 NM 2008 1 23 DL76G080048 1 20080112 A 2424 734284F GCU BOEING 767 767324 1385203 NM RIGHT ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 394DL 27394 JUST AFTER LEVELING OFF AT FL390 NOTICED A DISTINCT ELECTRICAL SMELL SHORTLY AFTER THE LEFT AND RIGHT UTILITY BUSS LIGHT S AND RT GEN DRIVE LIGHTS ILLUMINATED ON OVERHEAD PANEL WITH EICAS MESSAGES. NOTICED SLIGHT WHIFF OF SMOKE IN COCKPIT. FOLLOWED QRH PROCEDURES FIELD OFF LIGHT ON AUX PANEL ILLUMINATED SMOKE AND FUMES DISSIPATED SHORTLY THERE AFTER. REMOV ED RT GCU FOUND BAD BURNED ODOR. OPENED NR 2 ENGINE AND INSP FEEDER CABLES FROM GEN TO PYLON DISCONNECT. NO VISUAL TRO UBLE FOUND. REPLACED RT GEN CONTROL UNIT. REPLACED RT IDG PER AMM CHECKS GOOD. 2 L 7 2 4F RT A1NM 2008012300129 20080123 00129 NM 2008 1 23 2008UALA00132 1 20080107 A 5320 ATTACH FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 INTERCOSTAL ATTACH CLIP IS CRACKED AT STA 360 STR 10L. REMOVED DAMAGED CLIP. FABRICATED AND INSTALLED REPLACEMENT CLIP . 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300130 20080123 00130 NM 2008 1 23 2008UALA00133 1 20080107 A 5313 STRINGER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 STRINGER 15L AT STA 360 IS CRACKED. REMOVED DAMAGED STRINGER. FABRICATED AND INSTALLED REPAIR CHANNEL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012300153 20080123 00153 NM 2008 1 23 08FDEA00139 1 20080115 A 5321 65672055 FLOOR PANEL BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 FWD PIT NR 1 FLOOR PANEL HAS LIGHT CORROSION AROUND ALL FASTENER HOLES VERIFIED MATERIAL 2024 T3 .050" IAW DWG 65-67205 AND P/N 65-67205-5., A TAG NR A40813 AND PO NR 1022427. FABRICATED NEW FWD PIT NR 1 FLOOR PANEL P/N 65-67205-5 AND SRM 51-10-1 PG 12, ALODINED AND PRIMED REF SRM 51-10-2 PG 1. 2 L 7 3 4F RT A3WE 2008012300174 20080123 00174 NM 2008 1 23 2008UALA00164 1 20080109 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FLOORBEAM CORRODED STA 987, RBL 42, WL 207 ZONE 2422. CUT OUT DAMAGE AND INSTALLED REPAIR PARTS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008013000145 20080130 00145 NM 2008 1 30 DLM88080073 1 20080116 A 5320 9930503823 CUSP WEB DOUG MD88 MD88 3023688 NM BS 598-712 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 EXFOLIATION CORROSION ON RT CUSP WEB AT PAX CABIN AT STA Y=598 TO 712, NEW CUSP WEB WAS INSTALLED IAW DOUGLAS DWG 993053 8. 2 L 7 2 4F RT A6WE 2008013000146 20080130 00146 NE 2008 1 30 DL764080074 2 20080117 A 7230 COMPRESSOR BOEING 767 767432ER 1385134 NM GE CF6 CF680C2B6F 30025 NE NR 2 ENGINE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 829MH 25872 706102 29700 706102 ATB DUE NR 2 ENGINE SURGE ENGINE WAS NOT SHUTDOWN C/FOUND METAL IN TAILPIPE. REPLACED NR 2 ENG. REPLACED RIGHT ENGINE. 2 L 7 2 4F 4 F RT A1NM E13NE 2008013000152 20080130 00152 NM 2008 1 30 DLM88080080 1 20080116 A 5320 FLOOR SUPPORT DOUG MD88 MD88 3023688 NM BS 150-200 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 EXFOLIATION CORROSION ON PAX CABIN FLOOR SUPPORT BTW STA Y=150 AND 200 RBL 7. NEW FLOOR SUPPORT INSTALLED IAW SRM 51-30 -1. 2 L 7 2 4F RT A6WE 2008013000157 20080130 00157 EA 2008 1 30 SWIA200819090 1 20080119 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA LT WING DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 936SW 7726 LEFT WINGLET DAMAGED WHILE ON THE RAMP. INSTALLED NEW RIB AND PANEL PER SRM 57-31-31 AND CRJ DRAWING 600-15108. 2 L 7 2 4F RT A21EA 2008013000158 20080130 00158 EA 2008 1 30 SWIA200819091 1 20080122 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA CONTAMINATED A SWIA A UNSCHED LANDING C B F.O.D. SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 970SW 7881 FLT 5865 - RECEIVED A SMOKE TOILET INDICATION AFTER TAKEOFF. FOUND LEFT AND RIGHT PACKS SATURATED WITH DE ICING FLUID. CLEANED DUCTS AND REPLACED SOCKS, PER AMM 21-51-13. 2 L 7 2 4F RT A21EA 2008013000163 20080130 00163 WP 2008 1 30 08FDEA00264 1 20080124 A 5730 ARC70092 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 RIGHT WING TRAILING EDGE LOWER SKIN SURFACE DENTED INBD OF OUTBD MAIN FLAP INBD END. REMOVED PANELS TO FOM IAW MD/DC1 0 SRM 51-31-01 VOL II, CUTOUT DAMAGE AREA IAW MS/DC10 SRM 57-00-01 VOL I. MATERIAL ID FOR DOUBLER REPAIR 2024 T-3, .09 0 PO NR 575582.1, IAW MD/DC10 SRM 57-10-00 VOL I. FABRICATED REPAIR IAW MD/DC10 SRM 57-10-00 VOL I. ALODINED AND PRIM ED IAW MD/DC10 SRM 51-21-01 PAGE 24 AND PAGE 21 VOL II. INSTALLED DOUBLER REPAIR IAW MD/DC10 SRM 51-35-01 VOL II. INST ALLED ACCESS PANELS IAW MD/DC10 SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2008013000165 20080130 00165 NM 2008 1 30 08FDEA00246 1 20080123 A 5320 65B578392 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 INTERCOSTAL FLOOR SUPPORT BRACKET BETWEEN STA 333.45 AND STA 324.0 HAS CORROSION. REMOVED CORROSION FROM SUPPORT BRAC KET IAW SRM 51-10-02. UPON FURTHER INVESTIGATION FOUND SUPPORT TO BE OUT OF SRM 53-00-51 LIMITS, EXFOLIATED 100 PERCENT . REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-02 AND 51-40-05. TOP COATED SUPPORT IAW AMM 51-21-00-07. 2 L 7 2 4F RT A2NM 2008013000166 20080130 00166 EU 2008 1 30 08FDEA00247 1 20080123 A 7997 CONNECTOR AIRBUS 300 A300B4622R 3930312 EU NR 1 ENGINE DAMAGED A FDEA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 SO 25 725FD 572 ON DESCENT NR 1 ENG THRUST WOULD NOT INCREASE, FOLLOWED BY OIL PRESSURE LOW WARNING, PRESSURE SHOWED NEAR ZERO, SHUT DOW N ENG NR 1 (ENG NR 1 WINDMILL APPROX 10 MIN). PER FLIGHT CREW DEBRIEF: THEY WERE ON DESCENT WITH THROTTLES AT IDLE. ADVANCED THROTTLES TO LEVEL OFF, NR 1 ENG WOULD NOT RESPOND, ECAM WARNING FOR LOW OIL PRESSURE CAME ON, CREW SHUT DOWN NR 1 ENG. REMOVED AND REPLACED CONNECTOR DH10 AND BACKSHELL ASSY ON FMU IAW A300 HOOKUP LIST AND WDM 76-12-01. ACCOMPL ISHED POWER RUN BOTH ENG. ALL PARAMETERS WITHIN LIMITS. 2 L 7 2 4F RT A35EU 2008013000170 20080130 00170 NM 2008 1 30 08FDEA00251 1 20080124 A 5720 ARC2126501 STRUT DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 FOUND CORROSION, LT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING STRUT FORWARD FASTENER HOLE. CORROSION REPAIRED AS PE R EA 1-5750-117306, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008013000176 20080130 00176 NM 2008 1 30 DLM90080054 1 20080102 A 5511 991848827N RIB DOUG MD90 MD9030 3023690 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 RT ELEVATOR LEADING EDGE RIG CRACKED APPROXIMATELY STATION XE105. REMOVED, LOCATED AND DRILLED NEW -27 WEB AND REINSTAL LED -7 ANGLE. IAW MD90 SRM 51-30-01 AND 51-30-02. INSTALLED -27 WEB, IAW MD90 SRM 51-30-02. 2 L 7 2 4F RT A6WE 2008013000177 20080130 00177 NM 2008 1 30 DLM90080055 1 20080102 A 5330 5911401 SKIN DOUG MD90 MD9030 3023690 NM BS 218 L19L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 LT FUSELAGE STATION 218 AND LONGERON 191 DENTED. REPAIRED LT FUSELAGE AT STA 218 AND LONGERON 19L, IAW MD80 SRM 53-04D FIG 12B. 2 L 7 2 4F RT A6WE 2008013000184 20080130 00184 WP 2008 1 30 08FDEA00258 1 20080124 A 3246 NRG600231 WHEEL DOUG MD10 MD1010F 3022112 WP MLG FAILED A FDEA J A DUMP FUEL UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 25 365FE 406 406 46601 PDIS: DURING TAKEOFF FELT VIBRATION LEFT THE GEAR DOWN. CONFIRMED WITH TOWER FOUND RUBBER ON RUNWAY. DUMPED 82,000 POU NDS OF FUEL AND DID EMERGENCY RETURN. REMOVED AND REPLACED NR 4 MAIN WHEEL ASSY, WHICH BLEW UP AT 152 KTS ON TAKEOFF FR OM EWR. INSPECTED AREA AROUND RT GEAR, NO DAMAGE NOTED EXCEPT FOR A PIECE OF THE MLG FOLLOWUP DOOR IS MISSING. REMOVED AND REPLACED RT MAIN GEAR DOOR LOWER PANEL IAW AMM 20-50-02-2. NO ADJUSTMENT REQ FOR THIS PART ON THE MAIN GEAR DOOR. OK TO CONTINUE. 2 L 7 3 4F RT A22WE 2008013100005 20080131 00005 SO 2008 1 31 C2XA08SH006 1 20080116 A 5310 14525480603 BEAM EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13124 145689 SHV - DURING C-CHECK CARGO DOOR CUTOUT LOWER SECTION HAS VARIOUS AREAS OF CORROSION. MX REMOVED AND REPLACED CUTOUT LOW ER BEAM IAW EMB 145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008013100006 20080131 00006 EA 2008 1 31 MASA200800023 1 20080116 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37178 7178 ASH FLT 2722 PHX-SBA. AFT EMERGENCY LIGHTS ILLUMINATED WITH THE SWITCH IN ARM POSITION. MX OP CHECKED THE LIGHTING SYS TEM AND COULD NOT DUPLICATE THE PROBLEM. 2 L 7 2 4F RT A21EA 2008013100017 20080131 00017 EA 2008 1 31 MASA200800017 1 20080108 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH 2773 PHX - AFT EMERGENCY FLOOR LIGHTS 40% INOP. MX RESECURED CONNECTOR TO FLOOR LIGHTS. 2 L 7 2 4F RT A21EA 2008012300179 20080123 00179 NM 2008 1 23 2008UALA00167 1 20080110 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE AFT CREW REST INOPERATIVE A UALA K NONE O OTHER AP APPROACH 1 WP 29 174UA 24381 EMERGENCY LIGHT INOP: AFT CREW REST STAIRS ILLUM O/B LAMP. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2008012300188 20080123 00188 NM 2008 1 23 MWEA080005 1 20080109 A 5311 FRAME BOEING 717 717200 1383700 NM FUSELAGE BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 925ME 55191 STATION 427 FRAME BETWEEN RIGHT LONGERON 24 TO RIGHT LONGERON 25 AFT SIDE OF FRAME IS BENT. FABRICATED AND INSTALLED AN GLE. 2 L 7 2 4F TR A6WE 2008012300213 20080123 00213 NM 2008 1 23 UPS08551391 1 20080109 A 2613 OVERHEAT LOOP BOEING 757 75724APF 1384969 NM RT ENGINE MALFUNCTIONED A IPXA K NONE N FALSE WARNING NR NOT REPORTED 1 SO 01 452UP 25473 INSPECTION TYPE:N/A RT ENGINE OVHT LOOP 2 CAME ON FOR SEVERAL SECONDS IN FLIGHT THEN DISAPPEARED. STATUS MESSAGE NEVER RETURNED. PLACED ON DMI LIST MEL REF 26-11-2-1. PERFORMED TEST OF FIRE DET SYSTEM. OPS NORMAL PER MM 26-11-00-5. 2 L 7 2 4F RT A2NM 2008012300238 20080123 00238 NM 2008 1 23 2008UALA0028 1 20080101 A 2425 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE UNKNOWN A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 795UA 26927 ELEC BACKUP GEN R RIGHT BACKUP GENERATOR OFF DUE TO A PROTECTIVE TRIP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008012300243 20080123 00243 WP 2008 1 23 UPS08851406 1 20080108 A 5313 4641324U502 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 AFTER L28R WAS REMOVED FOUND END FITTING CRACKED AT STA 1690, AFT FITTING. REMOVED AND REPLACED LONG END FITTING AT STA 1690 AND L28R PER SRM 51-1-21 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2008012400004 20080124 00004 SO 2008 1 24 LR7A08005 1 20080105 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 477 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 636 4698 DURING SCHEDULED B-1 CHECK, PER JOB CARD HB5301, FOUND RT UPPER WHEEL WELL BULKHEAD WEB RISER CRACKED AT FS 477, WL220, RBL75. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-40-10. 2 H 7 4 4T A1SO 2008012400005 20080124 00005 SO 2008 1 24 LR7A08006 1 20080105 A 5312 LS3872 BULKHEAD LKHEED 382 382G 526414U SO FS 573 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 636 4698 DURING SCHEDULED B-1 CHECK, PER JOB CARD HB5301, DURING REMOVAL OF INTERCOSTAL BEAM FOR ACCESS, FOUND ATTACHMENT WEB COR ROSION AT FS573, WL230, LBL63. REPAIR ACCOMPLISHED REPLACING WEB IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008012400025 20080124 00025 SO 2008 1 24 LR7A08013 1 20080115 A 5310 WINDOW FRAME LKHEED 382 382G 526414U SO FS 150 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 631 4590 DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5301, FOUND LT SIDE WINDOW FRAME CRACKED AT AFT LOWER CORNER (POST 5) FS150, WL233, LBL52. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-30-32. 2 H 7 4 4T A1SO 2008012400026 20080124 00026 SO 2008 1 24 LR7A08014 1 20080115 A 5340 342589L FITTING LKHEED 382 382G 526414U SO FS 770 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 631 4590 DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5302, FOUND CABIN BHD TO SLOPING LONGERON TEE FITTING CRACKED AT FS 770, WL15 2, LBL62. REPAIR ACCOMPLISHED BY REPLACING TEE FITTING IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008012400055 20080124 00055 SO 2008 1 24 C2XA08SH001 1 20080115 A 5310 14564106001 STRIKER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15555 145594 SHV - DURING C-CHECK CARGO DOOR CUTOUT LINER DOOR STRIKER PLATE HAS CORROSION ON 2 SIDE. MX REPAIRED CARGO DOOR CUTOUT LINER DOOR STRIKER PLATE AT FR 65 IAW EC 5330-01767. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008012400059 20080124 00059 2008 1 24 2008UALA0051 4 20080103 A 2210 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE AUTOLAND SYS UNKNOWN A UALA O OTHER W INADEQUATE Q C DE DESCENT 1 WP 29 799UA 26926 NO LAND 3 DEGRADATION IN AUTOLAND SYSTEM PRIOR TO APPROACH (BEFORE LAND 3 AUTOLAND STATUS ANNUNCIATION). 2 L 7 2 4F 4 F RT T0001SE E46NE 2008012400063 20080124 00063 NM 2008 1 24 SWAA080320 1 20080115 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 634, RBL 70. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008012400064 20080124 00064 NM 2008 1 24 SWAA080321 1 20080115 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 618, RBL 70. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008012400070 20080124 00070 NM 2008 1 24 SWAA080322 1 20080115 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 464 TO BS 470, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008012400074 20080124 00074 NM 2008 1 24 SWAA080338 1 20080115 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, LBL 13.5. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008012400082 20080124 00082 NM 2008 1 24 SWAA080339 1 20080116 A 5230 6549889 SKIN BOEING 737 7373Q8 1384670 NM FWD CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT LOWER FWD CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008012400085 20080124 00085 NM 2008 1 24 SWAA080345 1 20080116 A 5534 6552274 BUSHING BOEING 737 7373TO 138447G NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND VERTICAL FIN LEFT REAR SPAR FAIL SAFE FITTING LUG BUSHING CORRODED. REMOVED AND REPLA CED BUSHING PER BOEING DRAWING. 2 L 7 2 4F RT A16WE 2008012400087 20080124 00087 NM 2008 1 24 SWAA080344 1 20080116 A 5534 6552274 BUSHING BOEING 737 7373TO 138447G NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND VERTICAL FIN LT REAR SPAR FITTING LUG BUSHING CORRODED. REMOVED AND REPLACED BUSHING PER BOEING DRAWING. 2 L 7 2 4F RT A16WE 2008012400091 20080124 00091 2008 1 24 SWAA080346 4 20080117 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008012400106 20080124 00106 NM 2008 1 24 SWAA080355 1 20080117 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER 26R CORRODED AT BS 480. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008012400113 20080124 00113 NM 2008 1 24 ZZDA2008035 1 20080120 A 3810 LINE BOEING 717 717200 1383700 NM GALLEY LEAKING A ZZDA B EMER. DESCENT K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 37 965AT 55026 SMOKE AND ACID SMELL IN COCKPIT. PUFF AND ELECTRICAL SMELL GALLEY AREA IE COFFEE POTS REPORTED BY A FLIGHT ATTENDANT. FOUND WATER LEAK IN GALLEY DRIPPING ON NR 3 COFFEEMAKER CONNECTOR CAUSING A SHORT AND SMALL AMOUNT OF SMOKE. REPLACED W ATER SUPPLY LINE. REF M/M 38-10. 2 L 7 2 4F TR A6WE 2008012400114 20080124 00114 2008 1 24 ZZDA2008036 4 20080120 A 2565 D29982225 SLIDE BOEING 717 717200 1383700 NM R1 DOOR UNSERVICEABLE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 934AT 55070 PIN SHOWING ON R1 SLIDE. REMOVED AND REPLACED R1 SLIDE ASSY. REF MM 25-61. 2 L 7 2 4F TR A6WE 2008012400116 20080124 00116 NM 2008 1 24 SWAA080374 1 20080120 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008012400122 20080124 00122 NM 2008 1 24 SWAA080375 1 20080117 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 912, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008012400125 20080124 00125 NM 2008 1 24 SWAA080376 1 20080116 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 914, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008012300194 20080123 00194 NM 2008 1 23 08FDEA00176 1 20080116 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 STRINGER CLIP CRACKED AT STATION 849 STR 7L REMOVED STRINGER CLIP STA 849, STR 7L, IAW SRM 51-30-2. MATCHED DRILLED NEW CLIP P/N 65-45313-2 REF IPC 53-10-00 FIG 35ZZ SHT 1 PG 1 ITEM 165 DWG 65 -45313. INSTALLED NEW CLIP IAW SRM 51-30-2 P 1. 2 L 7 3 4F RT A3WE 2008012300195 20080123 00195 NM 2008 1 23 08FDEA00177 1 20080116 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 STRINGER CLIP CRACKED STATION 804, STRINGER 7L REMOVED STRINGER CLIP, STA 804, STR 7, IAW SRM 51-30-2. MATCHED DRILLED NEW CLIP P/N 65-45313-2, REF IPC 53-10-00 IFG 35ZZ SHT 1, PG 1 ITEM 165 IAW DWG 65-45313. INSTALLED NEW CLIP IAW SRM 51 -30-2 P1. 2 L 7 3 4F RT A3WE 2008012300198 20080123 00198 EU 2008 1 23 08FDEA00186 1 20080117 A 3310 A9550042672695 CONTROL PANEL AIRBUS 300 A300F4605R 3930327 EU UNKNOWN A FDEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 25 677FE 791 DURING T/O ROLL AT KLAX WHEN SELECTING "LIGHTS ON" FOR TAKEOFF, RECEIVED "ELECTRICAL SHOCK" FROM OVERHEAD LIGHT PANEL. REMOVED AND REPLACED OVERHEAD LIGHT PANEL 426 VU, OP'S CHECKED ALL LIGHT SWITCHES 33-40-00-0. COMPLIED WITH EA 6-3000-1 18153 FOR PANEL INSTALLATION. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG A9550042672695. 2 L 7 2 4F RT A35EU 2008012300200 20080123 00200 EU 2008 1 23 08FDEA00188 1 20080117 A 3310 A9550042672695 CONTROL PANEL AIRBUS 300 A300F4605R 3930327 EU LIGHTS CHAFED A FDEA O OTHER O OTHER CL CLIMB 1 SO 25 677FE 791 DURING T/O ROLL AT KLAX WHEN SELECTING "LIGHTS ON "FOR TAKEOFF, RECEIVED "ELECTRICAL SHOCK" FROM OVERHEAD LIGHT PANEL. REMOVED AND REPLACED OVERHEAD LIGHT PANEL 426 VU, OP'S CHECKED ALL LIGHT SWITCHES 33-40-00-0. COMPLIED WITH EA 6-3000-1 18153 FOR PANEL INSTALLATION AND PART EFFECTIVITY, IPC, CANNED PANEL FROM A/C 725. 2 L 7 2 4F RT A35EU 2008012300201 20080123 00201 WP 2008 1 23 08FDEA00189 1 20080115 A 3260 SQUAT SWITCH DOUG DC10 DC1030F 3023504 WP MLG INACTIVE A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 301FE 46800 AFTER T/O RAISED GEAR AND NOSE GEAR REMAINED UNSAFE, BOTH PRIMARY AND SECONDARY INDICATIONS. RAN QRH CHECKLIST, CYCLED GEAR AND GOT GOOD UP AND LOCKED INDICATIONS, SO CONTINUED ON FLIGHT. WHILE GEAR WAS UNSAFE ALSO GOT PITOT AND TAT PRO BE HEAT OFF INDICATIONS, SO WEIGHT OFF WHEELS SWITCH WAS NOT ACTIVATED. REPACKED NLG STRUT REF MM 32-21-01-8. SERVICED REF 32-21-01-3. PERFORMED RETRACTION CHECK. ALL INDICATIONS CK GOOD. A/C OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2008013100019 20080131 00019 EA 2008 1 31 MASA200800018 1 20080108 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA EXIT SIGN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 909FJ 15009 ASH FLT 2702 TUS - THE 15AC, 15DF & 16AC EMERGENCY EXIT SIGN HAS MULTIPLE LIGHTS INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008013100021 20080131 00021 EA 2008 1 31 MASA200800020 1 20080110 A 2520 LATCH CNDAIR CL600 CL6002B19 1900309 EA F/A SEAT LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75998 7336 ASH FLT 7216 IAD-MDT. F/A SEAT WOULD NOT UNLOCK TO STOW. MX UNLOCKED THE SEAT AND LUBED THE LATCH. 2 L 7 2 4F RT A21EA 2008012900042 20080129 00042 NM 2008 1 29 2008UALA00188 1 20080110 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 OVERWING FRAME AT BS 616 RT SIDE IS CRACKED AT LOWER RIVET HOLE. FABRICATED AND INSTALLED NESTED ANGLE REPAIR ON FRAME PER MM 53-11-89-801. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900062 20080129 00062 NM 2008 1 29 2008UALA00198 1 20080110 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 SEAT EEL INOP AT 3A AFT SECT. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900066 20080129 00066 NM 2008 1 29 2008UALA00095 1 20080104 A 3510 MXP401600U STOWAGE BOX AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE OXYGEN SYSTEM DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 831UA 1291 RIGHT AFT CREW OXYGEN MASK BOX DOES NOT TEST AND DOOR DOES NOT CLOSE PROPERLY. UNKNOWN DAMAGE TO STOWAGE BOX. REPLACED CREW O2 (RT AFT) STOWAGE BOX AND OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900098 20080129 00098 EU 2008 1 29 2008UALA00213 1 20080114 A 3230 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MLG MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 439UA 683 CREW REPORTS LANDING GEAR DID NOT RETRACT AFTER T/O. PFR SHOWS 25GA FAULT, SERVICED NOSE GEAR STRUT, REPLACED LGCIU NR 2 ACCOMPLISHED A TEST FLIGHT WITH THREE SUCCESSFUL DEPLOY AND RETRACTIONS. A/C HAS NOT HAD THIS ISSUE SINCE JAN 15, 20 08. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900145 20080129 00145 NM 2008 1 29 2008UALA00087 1 20080107 A 3350 321430 BATTERY PACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 834UA 1420 EMERGENCY LIGHT TEST FAULTED EPSU L AND R. DUAL BATTERY PACK FAILURE. REPLACED BOTH LEFT AND RIGHT EPSU'S. OPS CHECKE D NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900160 20080129 00160 NM 2008 1 29 KCSA081022 1 20080117 A 5311 FRAME BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 BS 1880 FUSELAGE FRAME CRACKED ACROSS ENTIRE WIDTH, (APPROX 7 INCHES) AT STR 11R. 2 L 7 4 4F RT A20WE 2008012900162 20080129 00162 2008 1 29 MWEA080010 4 20080117 A 2565 375321385 LANYARD DOUG DC9 DC981 3022081 WP EVAC SLIDE FAILED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 813ME 48007 DURING TAIL CONE SLIDE DEPLOY OPERATIONAL CHECK, THE TAIL CONE DROPPED AWAY CLEAN BUT THE SLIDE COVER DID NOT AUTOMATICA LLY DEPLOY OR DEPLOY AND INFLATE EVACUATION SLIDE. REMOVED AND REPLACED TAIL CONE EVACUATION SLIDE. 2 L 7 2 4F A6WE 2008012900169 20080129 00169 SO 2008 1 29 C2XA08IA025 1 20080113 A 7810 23075866 EXHAUST MIXER ALLSN AE3007A EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL RT ENGINE BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 24128 CAE312139 145700 CAE312139 IAH - DURING MAINTENANCE INSPECTION THE EXHAUST MIXER ON THE NUMBER TWO ENGINE WAS FOUND TO BE MISSING HALF, AND HAD DAM AGED THE THRUST REVERSER HOUSING UPON DEPARTURE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, AND THRUST REV ERSER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2008012900170 20080129 00170 NE 2008 1 29 2008UALA00067 2 20080104 A 7261 4P0168 CARBON SEAL IAE V2527A5 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE IDG FAILED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 440UA 702 RTFL DUE TO UNIDENTIFIED FUMES ON CLIMBOUT. *S/D* IDG CARBON SEAL LEAKING MISTING OIL INTO BREATHER SYSTEM. REPLACED CARBON SEAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900178 20080129 00178 NE 2008 1 29 2008UALA00161 2 20080110 A 7261 2A2899 SEAL IAE V2522A5 AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 ENGINE FAILED A UALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 803UA 748 V12177 STRONG OIL SMELL NOT ELECTICAL SMELL IN CABIN. RAN ENGINE TO PWR, WITH ONE BLEED AND ONE PACK AT A TIME. BURN OIL SMEL L IS STRONGER WITH LEFT ENGINE BLEED. FOUND OIL IN EXTENSION SHAFT (NR 1 ENG). CLEANED OIL AND PERFORMED A PACK BURN A ND INSTALLED BLIND CAP SEAL AND NR 5 BEARING COMPARTMENT COVER. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900182 20080129 00182 EU 2008 1 29 2008UALA00180 1 20080110 A 3350 087021673 WIRE HARNESS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 495UA 1842 EEL LIGHT AT ROW 2 IS INOP. DAMAGE TO EEL SEAT HARNESS. REPLACED EEL LIGHT SEAT HARNESS AT ROW 2. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900191 20080129 00191 NM 2008 1 29 2008UALA00233 1 20080112 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 FIRST CLASS AND FWD X AISLE EEL LIGHTS INOP. SECURED CABLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900193 20080129 00193 NM 2008 1 29 2008UALA00235 1 20080112 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 DOOR 2L FWD EMERGENCY LIGHT IN UPPER SILL INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900202 20080129 00202 NM 2008 1 29 2008UALA00244 1 20080113 A 3350 276005 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 RIGHT OVERWING FWD TWO EMERGENCY LIGHTS IS INOP. REPLACED FUSES. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900250 20080129 00250 NM 2008 1 29 2008UALA00261 1 20080114 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 AFT PIT AT STA 1400 BETWEEN STR 25L AND STR 26L, FRAME HAS DENT 3 PLACES. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012900287 20080129 00287 NM 2008 1 29 2008UALA00291 1 20080115 A 2622 EXTINGUISHER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEAKING A UALA O OTHER W K INADEQUATE Q C FLUID LOSS IN INSP/MAINT 1 WP 29 658UA 27113 WATER FIRE EXTINGUISHER LEAKING FLUID. SUSPECT FAULTY EXTINGUISHING RELEASE VALVE. REPLACED AFT WATER FIRE EXTINGUIS HER. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008013000006 20080130 00006 NM 2008 1 30 HALA0800021 1 20080116 A 4940 1605441 IGNITER BOEING 767 76733A 1385209 NM APU FAILED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 ETOPS SIGNIFICANT SYSTEM APU FAILED TO START "FAULT" LIGHT ILLUMINATED AND EICAS MSG "APU FAULT" DISPLAYED, ADD'L START ATTEMPTS UNSUCCESSFUL. REPLACED APU IGNITER PER MM49-41-02. OPS CK GOOD. 2 L 7 2 4F RT A1NM 2008013000048 20080130 00048 WP 2008 1 30 DHLA200800006 1 20080120 A 2697 CONNECTOR DOUG DC8 DC873 302199C WP FIRE LOOP LOOSE A DHLA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 GL 05 806DH 46002 FLT 631, NR 1 ENGINE FIRE WARN COMES ON INTERMITTENTLY AT CRUISE FLIGHT FL 350 3 TIMES AND BOTH FIRE LOOPS CHECKED OK A ND IN DESCENT FIRE LIGHT CAME ON STEADY. COMPLETED ENG FIRE CHECKLIST (CONT) LIGHT REMAINED ON, BOTH BOTTLES DISCHARGED IN A LOOP. FOUND LOOSE CONNECTORS AT PYLON "A" AND "B" LOOPS. SECURED SAME IAW 26-10-01. OPS NORMAL. REPLACED BOTH FIRE EXT BOTTLES IAW DC-8 MM 26-20-01. NO EVIDENCE OF FIRE AT NR 1 ENGINE NOTED. AIRCRAFT RETURNED TO SERVICE. ACFT GR OUNDED. 2 L 7 4 4F RT 4A25 2008013000088 20080130 00088 EU 2008 1 30 SIMA200802802 1 20080121 A 5347 7253725193 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 320AE 21854 5000 340B320 DURING MBV INSPECTION, THE SEAT TRACK AT BL 18.3L WAS FOUND CORRODED. AIRCRAFT REMOVED FROM SERVICE. REPLACED SEAT TRA CK WITH NEW ONE PN 7253725-193 IAW SAAB 340 SRM 53-70-60. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2008013000097 20080130 00097 SW 2008 1 30 WGEA200800012 1 20080124 A 3233 EM411513 ACTUATOR ECLIPS EA500 ECLIPSEEA500 3350000 SW LT MLG DEFECTIVE E WGEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 153DJ 31 000072 "LANDING GEAR FAIL" CAS MESSAGE DISPLAYED IN FLIGHT AFTER GEAR RETRACTION. LEFT MAIN GEAR INDICATED UNSAFE AFTER SELECT ING GEAR HANDLE DOWN, THREE GREEN INDICATED (GEAR DOWN), LANDING UNEVENTFUL. DAYJET WORK ORDER 1218, NRI 1. TROUBLESHO T LANDING GEAR FOUND LEFT MLG ACTUATOR DEFECTIVE. REMOVED AND REPLACED LEFT MLG ACTUATOR WITH NEW UNIT IAW EA 500 AMM 3 2-30-20. PERFORMED ALL OPERATIONAL CHECKS OF LANDING GEAR SYSTEM IAW EA 500 AMM 32-30-00. ALL SYSTEM CHECK WERE SATISF ACTORY WITH NO DEFECTS NOTED. 1 L 7 2 4J RT A00002AC 2008013000127 20080130 00127 EU 2008 1 30 08FDEA00215 1 20080118 A 5340 A5237435120400 ATTACH FITTING AIRBUS 310 A310222 3930315 EU CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 AFT CARGO COMPARTMENT FLOOR, AFTER AN HFEC INSPECTION NTM 52-32-04 PART6, CRACKS WERE FOUND ON FLANGE OF DOOR ACTUATOR A TTACH FITTING. THE FRAME WAS SPLICED IN ACCORDANCE WITH EA 6-5230-117223. 2 L 7 2 4F RT A35EU 2008013000138 20080130 00138 EA 2008 1 30 SWIA200819079 1 20080117 A 2611 SMOKE WARNING CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE ACTIVATION A SWIA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 NM 07 411SW 7067 FLT 4114 - SMOKE TOILET CAUTION MESSAGE APPEARED. INSPECTED RIGHT ENGINE, AIR CYCLE MACHINE AND ASSOCIATED DUCTING FOR SIGNS OF CONTAMINATION WITH NO DISCREPANCIES NOTED. RAN ENGINES AT FULL POWER FOR 30 MINUTES AND COULD NOT DUPLICATE. OPS CHECK OF LAV SMOKE DETECTOR GOOD. 2 L 7 2 4F RT A21EA 2008013000141 20080130 00141 EA 2008 1 30 SWIA200819082 1 20080109 A 3310 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 403SW 7028 FLT 6474 - SMOKE REPORTED AT SIDEWALL AREA NEAR ROW 5. REPLACED SIDEWALL LIGHTING FIXTURE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008013000153 20080130 00153 NM 2008 1 30 DLM88080081 1 20080116 A 5315 FLOORBEAM DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 EXFOLIATION CORROSION ON PAX CABIN FLOORBEAM FOR GIRT BAR AT R1 LOWER DOOR JAMB. NEW FLOOR SUPPORT INSTALLED IAW SRM 51 -30-1. 2 L 7 2 4F RT A6WE 2008013000156 20080130 00156 NM 2008 1 30 DLM88080086 1 20080116 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 817 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 EXFOLIATION CORROSION ON RT CUSP WEB AT PAX CABIN STA Y=817. REPAIRED CUSP WEB IAW ERA 398191-14MA REV A. 2 L 7 2 4F RT A6WE 2008013100022 20080131 00022 EA 2008 1 31 MASA200800021 1 20080115 A 5210 MECHANISM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27318 7318 ASH FLT 7377 CAE. MAIN CABIN DOOR HARD TO OPEN FROM OUTSIDE, EXTERIOR HANDLE HARD TO TURN. CLEANED AND LUBED MAIN CAB IN DOOR MECH. 2 L 7 2 4F RT A21EA 2008013100024 20080131 00024 EA 2008 1 31 MASA200800022 1 20080115 A 3350 BATTERY CNDAIR CL600 CL6002D24 1390016 EA CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 910FJ 15010 ASH FLT 2629 JFK. EMERGENCY LIGHTS INOP. CHARGED EMERGENCY BATTERIES, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008012400002 20080124 00002 SO 2008 1 24 LR7A08003 1 20080105 A 5320 BRACKET LKHEED 382 382G 526414U SO FS 597 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 636 4698 DURING SCHEDULED B-1 CHECK, PER JOB CARD HB5302 FOUND CABIN OVERHEAD CLIP CRACKED AT FS 597, WL285, RBL23. REPAIR ACCOM PLISHED BY FABRICATION AND REPLACEMENT OF CLIP IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008012400027 20080124 00027 SO 2008 1 24 LR7A08015 1 20080115 A 5312 LS603451 BULKHEAD LKHEED 382 382G 526414U SO FS 617 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 631 4590 DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5301, FOUND LT MWW BHD WEB CRACKED AT FS 617, WL190, LBL73. REPAIR ACCOMPLIS HED IAW SMP583 FIG 53-40-10. 2 H 7 4 4T A1SO 2008012400051 20080124 00051 SO 2008 1 24 C2XA08CL007 1 20080110 A 2612 3601135470200 FIRE DETECTOR EMB 135 EMB135ER 3260203 SO APU FAILED A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 27506 145206 YOW FLIGHT 2762 - THE CREW REPORTED AN APU FIRE DETECT FAIL MESSAGE INFLIGHT WITH APU OFF. MAINTENANCE INSPECTED AND RE PLACED THE APU FIRE DETECTOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2008012400096 20080124 00096 NM 2008 1 24 SWAA080350 1 20080117 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505B, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008012400107 20080124 00107 NM 2008 1 24 SWAA080357 1 20080117 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008012400127 20080124 00127 NM 2008 1 24 SWAA080364 1 20080118 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 972, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008012400131 20080124 00131 2008 1 24 SWAA080365 4 20080118 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008012400136 20080124 00136 2008 1 24 SWAA080381 4 20080117 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 476WN 32475 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008012400141 20080124 00141 2008 1 24 SWAA080382 4 20080116 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 706SW 27840 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008012400145 20080124 00145 NM 2008 1 24 SWAA080388 1 20080121 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 744D, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008012400149 20080124 00149 2008 1 24 SWAA080390 4 20080121 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008012400151 20080124 00151 NM 2008 1 24 SWAA080391 1 20080121 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008012400152 20080124 00152 2008 1 24 SWAA080392 4 20080119 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008012400153 20080124 00153 NM 2008 1 24 SWAA080393 1 20080119 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008012400160 20080124 00160 WP 2008 1 24 08FDEA00198 1 20080118 A 5310 AFA71321 SUPPORT FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 NR 2 MCD LOWER JAMB SUPPORT FITTING HOLES A, B AND C HAS CRACK INDICATIONS, FOUND WITH BHEC. INSTALLED REPAIR BUSHINGS AT LOCATION NR 2 FITTING HOLES A, B AND C IAW SRM 53-50-00 VOL I PG 81 FIG 17. 2 L 7 3 4F RT A22WE 2008012400162 20080124 00162 WP 2008 1 24 08FDEA00200 1 20080118 A 5322 ADA000319 SHEAR TIE DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 LOWER FORWARD CARGO, STA 1099 BETWEEN L33L AND L35, SHEAR TIE HAS CORROSION ON LOWER FLANGE. REMOVED CORROSION IAW SR M VOLUME II, 51-21-01 PAGE 28. FOUND TO BE OUT OF LIMITS IAW SRM, VOLUME I, 53-00-01, FIGURE 1B. FABRICATED NEW -19 IAW DAC DGW ADA0003, REV M, INSTALLATION OF REPAIR ACCOMPLISHED ON NON-ROUTINE N00454. 2 L 7 3 4F RT A22WE 2008012400163 20080124 00163 NM 2008 1 24 ASAA0852471 1 20080111 A 3620 1296662 SENSOR BOEING 737 737890 1384527 NM BLEED AIR SYS FAULTY A ASAA K NONE O OTHER CR CRUISE 1 NM 02 577AS 35186 FIVE MINUTES AFTER REACHING FL350 NOTICED LARGE SPLIT IN DUCT PRESSURE. LEFT = 15PSI RIGHT = 45PSI. BEGAN RETURN TO HN L. THIRTY MINUTES LATER LT BLEED TRIP OFF LIGHT & WOULD NOT RESET. REMOVED AND REPLACED 390 SENSOR 450 THERMOSTAT HIGH STAGE VALVE HIGH STAGE REGULATOR & PRSOV SENSE LINE. ALL LEAK & OP CHECKS GOOD. 2 L 7 2 4F RT A16WE 2008012400164 20080124 00164 NM 2008 1 24 ASAA0872464 1 20080112 A 5230 146A61121 SKIN BOEING 737 737790 13844CN NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 649AS 30663 AFT CARGO DOOR EXTERIOR SKIN HAS SEVERAL SMALL DENTS 25 INCHES AFT OF FWD EDGE AND 14.5 UP. REPAIRED AFT CARGO DOOR EXT ERIOR SKIN IAW ASA EA 5230 01397. 2 L 7 2 4F RT A16WE 2008012400165 20080124 00165 NM 2008 1 24 ASAA0872465 1 20080112 A 5230 146A61121 SKIN BOEING 737 737790 13844CN NM CARGO DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 649AS 30663 AFT CARGO DOOR CREASED DENTED 3 INCHES AFT OF FWD EDGE 24 INCHES UP FROM BOTTOM REF SAD 6128724. REPAIRED AFT CARGO DOO R SKIN IAW ASA EA 5230 01397. 2 L 7 2 4F RT A16WE 2008012400170 20080124 00170 NM 2008 1 24 ASAA0852474 1 20080108 A 5330 RIVET BOEING 737 737890 1384527 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 548AS 30020 LIGHTNING STRIKE ON RIVET AT BS 480 1.3 INCH BELOW STR 21 LT. REPAIRED IAW ASA EA 5330 02286. 2 L 7 2 4F RT A16WE 2008012400175 20080124 00175 EU 2008 1 24 USAA920080140 1 20080102 A 5347 D5311278220200 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 669AW 1792 PIT - MAJOR REPAIR - BC4 CHECK, CORROSION ON SEAT TRACK, BS 709 / FR 16 - BS 808 / FR 20, -Y1292. REPLACED SEAT TRACK, BS 709 / FR 16 - BS 808 / FR 20, -Y1292 IAW A320 SRM 51-72-00. 2 L 7 2 4F RT A28NM 2008012400180 20080124 00180 EU 2008 1 24 USAA920080148 1 20080108 A 5347 D53472178200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 622AW 54 SAL - MAJOR REPAIR - C6 CHECK - CORROSION ON CABIN SEAT TRACK, BS 2403 / FR 52, +Y765. REPAIRED CABIN SEAT TRACK, BS 24 03 / FR 52, +Y765 IAW A320 SRM 53-00-15 FIGURE 201. 2 L 7 2 4F RT A28NM 2008012400181 20080124 00181 NM 2008 1 24 USAA920080149 1 20080108 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK - CRACKED STRINGER, BS 1640, S2R. REPAIRED STRINGER, BS 1640, S2R IAW B737 SRM 53-00-03 F IGURE 201. 2 L 7 2 4F RT A2NM 2008012400182 20080124 00182 SO 2008 1 24 FDKA200801009 1 20080107 A 2750 VELOCITY SENSOR EMB 145 EMB145LR 3260212 SO FLAPS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 841MJ 145448 FDM 6128 FLL (1750 PHX LCL) - FLAPS LOW SPEED MESSAGE. MX REMOVED AND REPLACED LT VELOCITY SENSOR. 2 L 7 2 4T RT T00011AT 2008012400196 20080124 00196 NM 2008 1 24 USAA920080168 1 20080102 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 807, S9R. REPAIRED FRAME, BS 807, S9R IAW USAIRWAYS EO 5311-01019. 2 L 7 2 4F RT A16WE 2008012400197 20080124 00197 NM 2008 1 24 USAA920080169 1 20080102 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 827, S9R. REPAIRED FRAME, BS 827, S9R IAW USAIRWAYS EO 5311-01019. 2 L 7 2 4F RT A16WE 2008012400198 20080124 00198 NM 2008 1 24 USAA920080170 1 20080102 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 847, S9R. REPAIRED FRAME, BS 847, S9R IAW USAIRWAYS EO 5311-01019. 2 L 7 2 4F RT A16WE 2008012400199 20080124 00199 NM 2008 1 24 USAA920080171 1 20080102 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 887, S9R. REPAIRED FRAME, BS 887, S9R IAW USAIRWAYS EO 5311-01019. 2 L 7 2 4F RT A16WE 2008012400201 20080124 00201 NM 2008 1 24 USAA920080173 1 20080110 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FLOORBEAM, BS 328, LBL 27. REPAIRED FLOORBEAM, BS 328, LBL 27 IAW BOEING 737 S RM 51-10-02. 2 L 7 2 4F RT A16WE 2008012400205 20080124 00205 NM 2008 1 24 SWAA080408 1 20080122 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008012400208 20080124 00208 NM 2008 1 24 08FDEA00216 1 20080122 A 5320 656097113 INTERCOSTAL BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 MAIN CARGO DECK INTERCOSTAL CORRODED, BS 1030-1050, LBL 19 REMOVED CORROSION AND FOUND OUT OF LIMITS. MATERIAL THICKNES S IS .071". REMAINING MATERIAL IS .051", AND MATERIAL LOSS AT .019'' REF SRM 53-10-1. BACKED DRILLED NEW INTERCOSTA L AT BS 1030-1050, LBL 19 REF SRM 51-30-2 PG 1-12, MADE 2 EA. FILLERS FOR INTERCOSTAL TO ALLOW FOR .090" REPAIR ANGLES AT STA 1030, LBL 19, REF SRM 5-20-1, PG 21. TREATED AND PRIMED FILLERS, REF SRM 51-10-2, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008012400210 20080124 00210 NM 2008 1 24 SWAA080409 1 20080122 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008013100028 20080131 00028 WP 2008 1 31 UPS08851454 1 20080102 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 MAIN CABIN FLOOR PNL LT INBD STA 540-660 IS DAMAGED. REMOVED, FABRICATED, AND INSTALLED FLOOR PNL AT LT INBD STA 540 TO 660 REF EO DC8-5320-9691-C. 2 L 7 4 4F RT 4A25 2008013100031 20080131 00031 WP 2008 1 31 UPS08851457 1 20080102 A 5320 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 D-PIT STA 1380, L31R FLOOR BOARD SUPPORT IS CRACKED. STOP DRILLED CRACKS ON FLOOR SUPPORT IN D-PIT A T STA 1380, L31R IAW EO DC8-5320-6176. 2 L 7 4 4F RT 4A25 2008013100074 20080131 00074 SO 2008 1 31 RAIA00801020 1 20080117 A 3297 WIRE EMB 145 EMB145LR 3260212 SO NLG BROKEN A RAIA A UNSCHED LANDING O OTHER TO TAKEOFF 1 CE 03 844HK 14500838 FLT 8018-STL - GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE REPAIRED WIRES AT THE NLG WOW PROXIMITY SWITCH CONNECT OR. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008013100075 20080131 00075 SO 2008 1 31 RAIA0801023 1 20080119 A 3350 09339821 BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 818HK 145059 PRE FLT 5515 - STL - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. O PS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008013100079 20080131 00079 EU 2008 1 31 YENA2008007 1 20080118 A 2720 810A000005 SERVO CONTROL AIRBUS 320 A320232 3930326 EU RUDDER SYS EXCESS PLAY A YENA O OTHER E VIBRATION/BUFFET DE DESCENT 1 EA 15 558JB 20841 1915 FLT 501, EWR-FLL, ON DESCENT LATERAL VIBRATION FELT IN COCKPIT, APPLICATION OF RUDDER INPUT CAUSED VIBRATION TO CEASE. VIBRATION FELT FROM 340 TO -100. ACCOMPLISHED AMM TASK 05-50-00-02 (AIRFRAME VIBRATION SURVEY) FOUND EXCESSIVE PLAY ON RUDDER TRAILING EDGE PLAY CHECK, FOUND GREEN SYSTEM RUDDER SERVO WITH 14MM OF PLAY. REMOVED AND REPLACED GREEN SYS RUDD ER SERVO CONTROL (1025GM) IAW 27-24-51, OPS CHECK NORM, NO LEAKS NOTED. 2 L 7 2 4F RT A28NM 2008013100083 20080131 00083 NM 2008 1 31 SWAA080434 1 20080123 A 2560 6557463 BRACKET BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR BRACKET CORRODED. REMOVED AND REPLACED BRA CKET PER SRM. 2 L 7 2 4F RT A16WE 2008013100090 20080131 00090 NM 2008 1 31 SWAA080425 1 20080123 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 951, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008013100102 20080131 00102 EU 2008 1 31 YENA2008008 1 20080119 A 2150 10007004 TURBINE BLADES EMB ERJ190 ERJ190100IGW 3260408 EU ACM DAMAGED A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 249JB 3923 19000045 STRONG BURNING SMELL IMMEDIATELY AFTER TAKEOFF. SMELL DISSIPATED AFTER 5 MIN. ODOR BEGAN IN CABIN. DECLARED EMERGENCY AND RETURNED TO BASE. FOUND ACM TURBINE BLADES DISINTEGRATED. REMOVED AND REPLACED RT ACM PER AMM 21-51-05. REF LP 3 10785 ITEM NR 1. OPS CHECK OF RT ACM REQUIRED TASK 21-51-00-710-801. 2 L 7 2 4F RT A57NM 2008013100104 20080131 00104 NM 2008 1 31 SWAA080436 1 20080124 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008013100114 20080131 00114 NM 2008 1 31 SWAA080440 1 20080124 A 5330 6545767 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA BETWEEN BS 434 AND BS 413, LBL 2 AND LBL 3. REPAIRED SKIN PER SB. 2 L 7 2 4F RT A16WE 2008013100116 20080131 00116 2008 1 31 SWAA080441 4 20080124 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 761RR 27875 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPL ACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008013100117 20080131 00117 EU 2008 1 31 YENA2008009 1 20080123 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU COCKPIT ODOR A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 633JB 2671 FLT 9, JFK-MCO, DIVERTED TO RDU, ODOR NOTICED IN FLIGHT DECK BY CREW. PERFORMED SMOKE INSP PER TSM 23-39-00-810-801 AND TSM 71-00-00-810-801 & 21-21-00-810-801. NO SMOKE SMELL NOTED. INSPECTED ASSOCIATED COMPONENTS, NO DEFECTS NOTED. FL T CREW RAN ENGINES & PACKS. NO SMELL NOTED. 2 L 7 2 4F RT A28NM 2008013100121 20080131 00121 SO 2008 1 31 RAIA00801026 1 20080122 A 3610 B-NUT EMB 145 EMB145LR 3260212 SO BLEED AIR SYS LOOSE A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 842HK 14500830 FLT 8003 - IAD - NR 1 BLEED LEAK MESSAGE ON THE EICAS DURING CRUISE. MAINTENANCE RESECURED A LOOSE B-NUT AT THE NR 1 EN GINE FAN AIR VALVE REFERENCE LINE. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008013100128 20080131 00128 EU 2008 1 31 YENA2008010 1 20080124 A 2150 A/C PACK EMB ERJ190 ERJ190100IGW 3260408 EU A/C BAY MALFUNCTIONED A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 249JB 19000045 FLT 430, MCO-BOS, AFTER TAKEOFF DETECTED AN ODOR THROUGHOUT CABIN. INITIAL THOUGHT WAS ELECTRICAL ODOR. AFTER REFERENC E TO QRH & DISCUSSION WITH MX CONTROL. ODOR WAS ISOLATED TO PACK NR 2. AS PACK NR 2 WAS TURNED PACK NR 2 ON/OFF THE OD OR CAME/DISSIPATED. CONTINUED FLT TO BOS WITH PACK NR 2 OFF. PERFORMED FIM TASK 21-20-00-810-801-A FOR ABNORMAL ODOR A ND ISOLATED TO RT PACK OPERATION. 2 L 7 2 4F RT A57NM 2008013100135 20080131 00135 EU 2008 1 31 YENA2008012 1 20080122 A 3240 CIRCUIT CARD EMB ERJ190 ERJ190100IGW 3260408 EU BRAKE SYS FAULTY A YENA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 15 281JB 19000103 FLT 38, JFK-ROC, AIR RETURN TO JFK, BRK RT FAULT AND BRK LT FAULT POST UPON GEAR DOWN ON APPROACH. BRAKE FAIL MSG AFTER LANDING. TROUBLESHOT AS PER 32-41-00. REMOVED AND REPLACED BCM MODULE 2 L0 CARD AS PER AMM 32-41-00, NO FAULTS NOTED. OPS CHECK GOOD. 2 L 7 2 4F RT A57NM 2008012900274 20080129 00274 NM 2008 1 29 2008UALA00274 1 20080115 A 3350 1317 LAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 209UA 30215 EEL(S) INOP AT FIRST CLASS SEAT 3E AFT & BUSINESS CLASS SEATS 11F & 13D. RELAMPED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008012400215 20080124 00215 NM 2008 1 24 SWAA080413 1 20080122 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 23R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008012400218 20080124 00218 NM 2008 1 24 SWAA080414 1 20080122 A 5315 6545874 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 251 TO BS 277, BL 0. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008012400229 20080124 00229 NM 2008 1 24 08FDEA00218 1 20080122 A 5340 65453132 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 CABIN BS 660, S 5L STRINGER CLIP TORN. REMOVED STRINGER CLIP, TRANSFERRED HOLD TO NEW CLIP. INSTALLED NEW STRINGER CLI P REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2008012400230 20080124 00230 NM 2008 1 24 SWAA080398 1 20080121 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008012400231 20080124 00231 SO 2008 1 24 FDKA200801007 1 20080107 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6088 MCO - EMERGENCY LIGHT SIGN OUT AT GALLEY. MX RESECURED LOOSE CONNECTOR. OPS CK GOOD. 2 L 7 2 4T RT T00011AT 2008012400233 20080124 00233 2008 1 24 SWAA080399 4 20080122 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 437WN 29832 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008012400235 20080124 00235 SO 2008 1 24 FDKA200801008 1 20080107 A 2760 SPOILER SYS EMB 145 EMB145LR 3260212 SO FAILED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 853MJ 145464 FDM 6047 MSY (1346 PHX LCL) - SPEED BRAKE FAIL. MX RESET SYSTEM AND PERFORMED OPS CHECK. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400253 20080124 00253 NM 2008 1 24 CALA0800025 1 20080114 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 LEFT INBOARD TRACK SEAT TRACK CORRODED AT STA 887 TO STA 927. REPAIRED SEAT TRACK PER SRM 53-00-52 REPAIR 3 FIG 201. 2 L 7 2 4F RT A16WE 2008012400271 20080124 00271 NM 2008 1 24 08FDEA00219 1 20080122 A 5311 65672505 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 CORROSION AT SEVERAL AREAS ON AFT WALL GILL LINER PANEL UPPER FRAME AT STA 1166, AROUND CAM LOC RECEPTACLE HOLES FRONT AND BACK FABRICATED UPPER FRAME AT STA 1166 WL 200, AFT CARGO COMP BULKHEAD, REF SRM 51-30-2 PG 4. REF BOEING DWG 65-67 250-5 SHEET 1-5. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008012400307 20080124 00307 NM 2008 1 24 ASAA0842481 1 20080112 A 2410 735511A OIL SYSTEM BOEING 737 737490 1384715 NM CSD OVERTEMP A ASAA E ENGINE SHUTDOWN M OVER TEMP CR CRUISE 1 NM 02 796AS 28891 IN FLIGHT NR 2 ENGINE CSD OIL HIGH TEMP LIGHT ILLUMINATED. CSD OIL TEMP WAS PEGGED TO RIGHT. NOTE: FLIGHT CREW SHUTDO WN NR 2 ENGINE THEN RESTARTED. ENGINE OPS NORMAL AFTER RESTART. RESET GENERATOR NR 2 PER MM 24 11 00 PGS 101 104. PER FORMED MAINT ON OIL FILTERS PER TC 48524002. OP CHECKS GOOD. RESAFTIED GENERATOR DISCONNECT. 2 L 7 2 4F RT A16WE 2008012300214 20080123 00214 NM 2008 1 23 UPS08651381 1 20080106 A 3620 DETECTOR BOEING 767 76734AF 1385212 NM BLEED AIR SYS MALFUNCTIONED A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 317UP 27745 INSPECTION TYPE:ETOP DIVERSION - RT BLEED DUCT MSG AND LIGHT INTERMITTENT 5 TIMES DURING T/O, THEN ON STEADY. FOLLOWED QRH AND DIVERTED TO AVOID ICING CONDITIONS. REMOVED AND REPLACED RIGHT BLEED LEAK DETECTION LOOPS TS214, TS215, TS216, TS217, TS218, TS219 PER 26-18-00-5. OPS CHECK GOOD PER SAME MM. 2 L 7 2 4F RT A1NM 2008012300226 20080123 00226 SO 2008 1 23 C2XA08TY006 1 20080114 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15910 145455 TYS EMERGENCY CEILING LIGHTS AT ROW 7 AND 12 WERE FOUND TO BE INOP ON A ROUTINE A CHECK. BOTH BULBS WERE CHANGED IAW EM B 145 AMM 33-50-08. OPS CHECKS WERE FOUND GOOD. A/C RETURNED TO SEVICE. 2 L 7 2 4T RT T00011AT 2008012300239 20080123 00239 NM 2008 1 23 2008UALA0030 1 20080102 A 3800 LAVATORY BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU UNKNOWN A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 341UA 24245 FLIGHT DIVERTED DUE TO FORWARD LAVATORY OVERFLOW. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012400003 20080124 00003 SO 2008 1 24 LR7A08004 1 20080105 A 5343 BEAM LKHEED 382 382G 526414U SO FS 577 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 636 4698 DURING SCHEDULED B-1 CHECK, PER JOB CARD HB5301 FOUND LT MLG BEAM AND OUTBD CAP CRACKED AT FS 577, WL236, LBL62. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-07-09. 2 H 7 4 4T A1SO 2008012400024 20080124 00024 SO 2008 1 24 LR7A08012 1 20080115 A 5310 WINDOW FRAME LKHEED 382 382G 526414U SO FS 150 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 631 4590 DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5301, FOUND RT WINDOW FRAME CRACKED AT AFT LOWER CORNER (POST5) FS 150, WL233 , RBL 52. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-30-32. 2 H 7 4 4T A1SO 2008012400052 20080124 00052 SO 2008 1 24 C2XA08ON064 1 20080104 A 2612 3601133500230 FIRE DETECTOR EMB 145 EMB145LR 3260212 SO NR 1 ENGINE DEFECTIVE A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 17560 11738 11738 14500605 FLT 209 - SMF TO ONT - CREW REPORTED E1 FIRE DETECTION FAIL. MX PERSONNEL REMOVED AND REPLACED ENG FIRE DETECTION MODUL E OPERATIONALLY CHECKED SATISFACTORY. A/C WAS RELEASED TO RETURN FOR SERVICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4T RT T00011AT 2008012400077 20080124 00077 NM 2008 1 24 SWAA080328 1 20080115 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED HC1 CHECK, FOUND KEEL BEAM SKIN CRACKED AT BS 715, RBL 5. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008012400078 20080124 00078 NM 2008 1 24 SWAA080329 1 20080115 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED HC1 CHECK, FOUND KEEL BEAM SKIN CRACKED AT BS 698, RBL 5 TO LBL 5. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008012400104 20080124 00104 NM 2008 1 24 SWAA080356 1 20080117 A 5322 6546546 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, RBL 15, WL 150. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008012400112 20080124 00112 SO 2008 1 24 FDKA200801006 1 20080106 A 2760 CONTROL UNIT EMB 145 EMB145LR 3260212 SO SPOILERS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 FDM 6134 PNS-MCO (1905 PHX LCL) - SPEED BRAKE FAIL CAUTION. MX REMOVED AND REPLACED SPOILER CONTROL UNIT, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400115 20080124 00115 NM 2008 1 24 SWAA080358 1 20080118 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 212WN 32485 L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008012400126 20080124 00126 NM 2008 1 24 SWAA080363 1 20080118 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 972, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008012400130 20080124 00130 NM 2008 1 24 SWAA080380 1 20080116 A 2750 655160250 CONTROL UNIT BOEING 737 7373H4 1384600 NM T/E FLAP FAULTY A SWAA K NONE J WARNING INDICATION AP APPROACH 1 SW 29 392SW 27379 ON APPROACH TO HOU L/E SLATS DID NOT EXTEND. REMOVED AND REPLACED FLAP CONTROL UNIT PER MM. 2 L 7 2 4F RT A16WE 2008012400146 20080124 00146 NM 2008 1 24 SWAA080387 1 20080121 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 759, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008012400161 20080124 00161 EU 2008 1 24 08FDEA00199 1 20080118 A 5311 FRAME AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS FRAME REPAIR LOCATED IN AFT CARGO ON FRAME 54.2 UNDER FLOOR BETWEEN STRINGERS 54 LT AND 57 HAS 1 REPAIR ANGLE O N THE LOWER AFT SIDE MEASURING 11.7" BY 3" WITH A LOWER FLANGE CUT OUT OF 2.6" BY 1" REPAIR NOT IAW SRM REQUIREMENTS. R EMOVED PREVIOUS REPAIR AND INSTALLED CORRECT FRAME REPAIR IAW FED-EX EA 6-5310-117993, DATED 31 DEC 07. THIS IS AN AIRB US REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008012400171 20080124 00171 WP 2008 1 24 08FDEA00201 1 20080118 A 5322 ADA00107 SHEAR TIE DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 FWD PIT AT STA 808 BETWEEN LONG 34R AND LONG 35R SHEAR TIE DAMAGED ON RADIUS. REMOVED, FABRICATED, AND INSTALLED SHER TIE PER SRM 53-13-01, VOL III FIG 8A AND SRM 53-30-00 VOL I FIG 10 AND SRM 53-30-00 VOL I PAGE 34 FIG 9 MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008012400172 20080124 00172 NE 2008 1 24 ASAA0852470 2 20080107 A 7321 2042M67P02 EEC BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 2 ENGINE FAULTY A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 583AS 35681 DURING TASKCARD 78273000 NR 2 ENGINE FAULT 73 20012 WAS FOUND. REPLACED NR 2 EEC (REF 73 21 60 PG 401 408 & MM SUPP 73 21 60 PG 401&408). ALL OP CHECKS GOOD. NO FAULTS. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008012400183 20080124 00183 NM 2008 1 24 USAA920080150 1 20080109 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK - CRACKED STRINGER, BS 1681, S2L. REPAIRED STRINGER, BS 1681, S2L IAW B737 SRM 53-00-03 F IGURE 201. 2 L 7 2 4F RT A2NM 2008012400194 20080124 00194 NM 2008 1 24 USAA920080166 1 20080102 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 767, S9R. REPAIRED FRAME, BS 767, S9R IAW USAIRWAYS EO 5311-01019. 2 L 7 2 4F RT A16WE 2008012400237 20080124 00237 SO 2008 1 24 FDKA200801014 1 20080108 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6033 JFK (0630 PHX LCL) - EMERGENCY LIGHT PANEL NOT ILLUMINATING. MX CLEANED AND REPAIRED CONNECTOR. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400256 20080124 00256 SO 2008 1 24 FDKA200801017 1 20080109 A 2751 CONTROL UNIT EMB 145 EMB145LR 3260212 SO TE FLAPS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 841MJ 145448 FDM 6132 MCO (1624 PHX LCL) - FLAPS LOW SPEED MESSAGE. MX PLACED THE FLAP CHANNEL 2 ON MEL. 2 L 7 2 4T RT T00011AT 2008012900276 20080129 00276 NM 2008 1 29 2008UALA00277 1 20080115 A 5320 65458078 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 277 S14R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FWD GALLEY DOOR CUTOUT BS 277 INTERCOSTAL CRACKED AT STRINGER 14R. MAJOR REPAIR: REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900292 20080129 00292 NM 2008 1 29 2008UALA00297 1 20080117 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY LIGHT AT SEATS 1A AFT, 35H, 37A & 41H ARE INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900295 20080129 00295 NM 2008 1 29 2008UALA00299 1 20080117 A 3510 HOSE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CREW O2 LOOSE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 662UA 27159 CREW O2 REPORTED LOW ON ARRIVAL. CHECKED ALL FLT DECK MASK CONNECTIONS. FOUND LOOSE CONNECTION AT 1ST OFFICER POS. SECU RED HOSE ASSY 192-2103, SERVICED OXYGEN AND PERFORMED LEAK CHECK, NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900296 20080129 00296 NM 2008 1 29 2008UALA00300 1 20080117 A 3510 OXYGEN MASK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 662UA 27159 SECOND OBSERVERS O2 MASK FOUND DAMAGED DURING LEAK CHECKS. SUSPECT DAMAGED FROM PRE FLIGHT CHECKS. REPLACED 2ND OBSERVE RS O2 MASK OPS CHECKS NORMAL. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900297 20080129 00297 NM 2008 1 29 2008UALA00301 1 20080116 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 523UA 24932 FLIGHT CREW REPORTS SMOKE IN COCKPIT. UNABLE TO DUPLICATE ON GROUND. PERFORMED TEST OF RT AND LT RECIRCULATION FANS, OPS CHECKED EQUIPMENT COOLING FANS, RAN APU WITH AI ON, TRIED DIFFERENT CROSSBLEED CONFIGS, NO ODOR EVER NOTED. THIS IS SUE NEVER APPEARED AGAIN AFTER 1/16/08. 2 L 7 2 4F 4 F RT A2NM E17NE 2008013000003 20080130 00003 NM 2008 1 30 DHLA200800005 1 20080118 A 3350 LIGHT BOEING 727 7272B7 138407L NM CABIN DISLODGED A DHLA O OTHER O OTHER TO TAKEOFF 1 GL 05 762AT 22162 FLT 577, EMERGENCY EXIT LIGHT OVER MAIN ENTRY DOOR FELL OFF DURING TAKEOFF ROLL. REINSTALLED EMERGENCY EXIT LIGHT OVER MAIN ENTRY DOOR. OPS CK. GOOD PER MM 33-50-01. ACFT GROUNDED. 2 L 7 3 4F A3WE 2008013000019 20080130 00019 WP 2008 1 30 IXXA080002O 1 20080117 A 3241 420531B CONTROL BOX DOUG DC8 DC871F 302199D WP ANTI SKID SYS DEFECTIVE A IXXA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 11 821BX 88742 2847 45811 DURING TAXI OUT FROM KFLL, THE CREW NOTICE THAT WITH THE ANTI-SKID SYSTEM ON THE AIRCRAFT HAD NO BRAKE'S, WHEN THE CREW TURNED THE ANTI-SKID SYSTEM OFF THE AIRCRAFT HAD BRAKE'S. THE CREW RETURNED TO BLOCK'S AT KFLL. MAINTENANCE AT KFLL DE FERRED ANTI-SKID SYSTEM IAW MRL -32-1. THE CREW FLEW THE AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE AT KTOL REMOVED AND REPLACED THE ANTI-SKID CONTROL BOX, TAXI THE AIRCRAFT AND PERFORMED OPERATIONAL CHECK ON THE BRAKES WIT H THE ANTI-SKID ON AND OFF BRAKES CHECKED GOOD ALL TIMES IAW DACO DC8 MAINTENANCE MANUAL 32-43-6 AND ATI ERH 09.01. AIR CRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2008013000049 20080130 00049 NM 2008 1 30 DHLA200800007 1 20080119 A 3350 37067001 BATTERY BOEING 727 7272B7 138407L NM EMERGENCY LIGHTS INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 GL 05 762AT 22162 FLT 152, EMERGENCY EXIT LIGHTS DON'T WORK. REMOVED AND REPLACED BATTERIES IN FWD AND AFT EMERGENCY EXIT LIGHTS, OPS CHE CK GOOD IAW B727 MM 33-50-71, P/N 37067-001 4 EACH. ACFT GROUNDED. 2 L 7 3 4F A3WE 2008013000051 20080130 00051 2008 1 30 ARWA20080102 4 20080124 A 3414 2594466902 INDICATOR DOUG DC10 DC1030 3023501 WP AIRSPEED MALFUNCTIONED A ARWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 526MD 46998 FIRST OFFICER'S AIRSPEED INDICATOR DISPLAYS FAIL-FLAG IN VIEW; REVISED AND PERFORMED EXPANDED CHECKLIST UNABLE TO RESTOR E. REMOVED AND REPLACED FIRST OFFICER'S MACH AIRSPEED INDICATOR IN ACCORDANCE WITH M/M 34-13-01. OPERATIONAL CHECK TES T FOUND NORMAL IN ACCORDANCE WITH M/M 34-13-00. 2 L 7 3 4F A22WE 2008013000052 20080130 00052 2008 1 30 ARWA20080103 4 20080125 A 2212 CONTROLLER DOUG DC10 DC1010 3022110 WP ATTITUDE HOLD MALFUNCTIONED A ARWA O OTHER O OTHER DE DESCENT 1 SO 19 68041 46900 ALTITUDE HOLD SLOW TO ENGAGE. PERFORMED ALTITUDE HOLD SYSTEM OPERATIONAL CHECK IN ACCORDANCE WITH M/M 22-00-03, FOUND N ORMAL AT THIS TIME. 2 L 7 3 4F A22WE 2008013000062 20080130 00062 SO 2008 1 30 FDKA200801033 1 20080117 A 5751 BONDING STRAP EMB 145 EMB145LR 3260212 SO AILERON CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 834MJ 145340 AILERON COVE PANEL NR 6731, O/B BONDING STRAP IS CORRODED. THE CORRODED STRAP HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008013000075 20080130 00075 SW 2008 1 30 WGEA200800008 1 20080118 A 3243 10100 MASTER CYLINDER ECLIPS EA500 ECLIPSEEA500 3350000 SW LT BRAKES WEAK E WGEA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 27 161DJ 18 000078 LEFT BRAKE ON PILOT AND COPILOT FEELS SPONGY. SUPPLEMENTAL INFORMATION, REMOVED AND REPLACED PILOTS LT BRAKE MASTER CYL INDER WITH NEW MASTER CYLINDER IAW EA 500 M/M 32-40-00. OP'S CHECK GOOD. 1 L 7 2 4J RT A00002AC 2008013000102 20080130 00102 2008 1 30 WGEA200800005 4 20080117 A 3417 1008555 ADC ECLIPS EA500 ECLIPSEEA500 3350000 SW NR 1 MALFUNCTIONED E WGEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 152DJ 35 000071 AIR SPEED DISAGREE CAS MESSAGE AT 80 KTS. 15 KTS SPLIT, CAPTAIN SIDE FASTER. REMOVED AND REPLACED NR 1 ADC IAW EA500 M M 34-10-15, 34-10-00, OPS CHECK GOOD. 1 L 7 2 4J RT A00002AC 2008013000120 20080130 00120 NM 2008 1 30 08FDEA00233 1 20080123 A 5347 BAC1520792 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 SEAT TRACK CORRODED, STA 880-950, RBL 47 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED SEAT TRACK. FABRICATED N EW SEAT TRACK, ALODINED AND PRIMED AND INSTALLED AT STA 870-950. REF BAC DWG 65-19601, SRM 51-10-2, SRM 51-30-2. REMOV ED FUEL SHROUD IN W/W TO FOM REINSTALLED AND SEAL FUEL SHROUD. REF MM 28-11-00. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008013000126 20080130 00126 EU 2008 1 30 08FDEA00214 1 20080117 A 5315 A53275336200 FLOORBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 FLOORBEAM CRACKED AT FR 54.3 AND Y-680. FLOORBEAM REPAIRED IAW EA 6-5310-115317. 2 L 7 2 4F RT A35EU 2008012400309 20080124 00309 NM 2008 1 24 ASAA0852476 1 20080114 A 2421 5910292 COUPLING BOEING 737 737890 1384527 NM NR 2 IDG LEAKING A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 577AS 35186 FOLLOW UP TO FREQUENT NR 2 IDG SERVICING. ACCOMPLISHED TSR 0811692. CLEANED ALL LUBE CONNECTIONS PLUMBING SERVICE FITT INGS & VENT VALVE. NO LEAKS NOTED AT ENGINE IDLE. REPLACED FILL PORT AS REQUESTED BY TECH SERVICES. 2 L 7 2 4F RT A16WE 2008012400323 20080124 00323 SO 2008 1 24 FDKA200801020 1 20080112 A 2710 CONTROL UNIT EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 833MJ 145327 FDM 6181 CLT (0406 PHX LCL) - CONTROL RESISTANT/GRINDING WITH AILERON AND ELEVATOR CONTROL INPUT. MX IS CURRENTLY TROUB LESHOOTING. 2 L 7 2 4T RT T00011AT 2008012400324 20080124 00324 SO 2008 1 24 FDKA200801021 1 20080111 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6148 MCO (0738 PHX LCL) - RT OVERWING EMERGENCY LIGHT SIGN INOP. MX CAN NOT DUPLICATE DISCREPANCY. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400327 20080124 00327 SO 2008 1 24 FDKA200801023 1 20080112 A 2731 SWITCH EMB 145 EMB145LR 3260212 SO YOKE INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 833MJ 145327 FDM 6181 CLT (0355 PHX LCL) - TRIM SWITCH ON YOKE INOP. MX REPLACED SWITCH, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008012400330 20080124 00330 EU 2008 1 24 08FDEA00209 1 20080121 A 5712 R5724912800300 RIB AIRBUS 310 A310221 3930310 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 CRACKED, R/WING SPOILER NR 3 IBD BOX HINGE RIB. REMOVED PANEL IAW A310-200 SRM 51-40-21 PG 7. CUT AND REMOVED CRACKED END RIB IAW A310-200 SRM 57-51-11 PG 227 AND 228. LOCATED, DRILLED AND DEBURRED ITEM 1, ITEM 2, AND ITEM 3 IAW A310-200 SRM 57-51-11 PG 222 STEP 3 (A) - 3(K), PG 223 3(L)- 3(V), PG 227, 228 AND 229. INSTALLED ITEM 1 RIB INSERT, ITEM 2 SPL ICE CHANNEL, ITEM 3 JOINT STRAP AND PANEL IAW A310-200 SRM 57-51-11 PG 223 AND A310-200 SRM 51040-21 PG 7. 2 L 7 2 4F RT A35EU 2008012400331 20080124 00331 WP 2008 1 24 08FDEA00210 1 20080121 A 5322 ADA01117 SHEAR TIE DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 CAC, CORROSION, SHEAR TIE, FS 1099 BETWEEN L51 R AND L50R REMOVED CORROSION IN REFERENCE WITH DC/MD10-10 SRM, VOLUME II, 51-21-01, PAGE 28A. ORIGINAL THICKNESS IA .071 INCH IAW DC/MD10-10 SRM, VOL III 53-13-01, FIGURE 8A, SHEET 1, ITEM 3 3. MATERIAL REMOVED IS .011. MATERIAL REMAINING IS .060" PER TIMCO TOOL T8225C. FOUND TO BE WITHIN LIMITS IAW DC/MD10 -10 SRM, VOLUME I, 53-00-01, FIGURE 1B. CUT OUT SHEAR CLIP AND REINSTALLED WITH SPLICE REPAIR IAW DC/MD10-10 SRM, VOLUM E I, 53-30-00, FIGURE 10. MATERIAL ID FOR SPLICE IS 7075-T6, .071 INCH, PO NR 596629.4 IAW DC/MD10-10, SRM, VOLUME I , 53-30-00, FIGURE 10. 2 L 7 3 4F RT A22WE 2008012400338 20080124 00338 CE 2008 1 24 DXTA200802783 1 20080121 A 3233 218262 ACTUATOR CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE COCKPIT ACTIVATED E DXTA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 GL 07 378QS 1189 6800103 ON GEAR EXTENTION THE RT GEAR INDICATED NOT DOWN AND LOCKED. REMOVED AND INSTALLED A RENTAL ACTUATOR PER MM 32-30-40 AN D OPERATIONAL CHECKED PER MM 32-00-00 GROUND OPERATIONAL CHECKED GOOD. 2 L 7 2 4F 4 F RC T00012WI E35NE 2008012400339 20080124 00339 2008 1 24 DXTA200802784 4 20080121 A 3414 INDICATOR CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE COCKPIT INOPERATIVE E DXTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 834QS 5600669 ON TAKEOFF CAPT'S AIRSPEED GAVE NO INDICATION, RED AIRSPEED ENUNCIATION SHOWED ON AIRSPEED INDICATOR. SIMULATED AIRSPE ED WITH PITOT/STATIC TEST SET AND COULD NOT DUPLICATE DISCREPANCY. CHECKED NR 1 PITOT HOSE FOR MOISTURE, NO MOISTURE FOU ND. BLEW OUT NR 1 PITOT LINES FROM ADC END. RE-ATTACHED HOSE. NR 1 PITOT SYTEM LEAK CHECKED GOOD. NR 1 AIRSPEED FUNCTION CHECKED GOOD. MAINTENANCE ACCOMPLISHED IAW MM 34-11-26. 2 L 7 2 4F 4 F RT A22CE E00053EN 2008012400358 20080124 00358 CE 2008 1 24 DXTA200802790 1 20080122 A 2701 CONTROL COLUMN CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT VIBRATION E DXTA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 07 639QS 5605139 VERY HIGH DEGREE OF VIBRATION IN CONTROL COLUMN AND YOKE AT ALL SPEEDS ABOVE 250 KNOTS AND AT ALL ALTITUDES ABOVE THAT S PEED. PERFORMED ELEVATOR AND ELEVATOR TRIM CABLE TENSION CHECK, PERFORMED FREE PLAY CHECK ON RT/LT AILERON, ALSO PERFOR MED INSPECTION OF CABLES, PULLEYS, BELL CRANK AND ROD ENDS WITH NO DEFECTS NOTED AT THIS TIME. IAW MM 27-31-00 2 L 7 2 4F 4 F RT A22CE E00059EN 2008012500003 20080125 00003 EU 2008 1 25 NWAA080233224 1 20080120 A 2910 LINE AIRBUS 320 A320211 3930320 EU HYD SYSTEM LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 324US 273 HYDRAULIC "G" LOW QUANTITY, ALSO LOW ON ECAM. FOLLOWED COM, LANDING GEAR GRAVITY EXTENDED AND LANDED UNEVENTFULLY. AIR CRAFT TOWED TO GATE. REPLACED HYDRAULIC LINE ON NR 1 THRUST REVERSER. CHECKS GOOD. 2 L 7 2 4F RT A28NM 2008012500016 20080125 00016 EU 2008 1 25 F3LA200800016 1 20080107 A 5321 D5347217220400 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION, FLOOR PANEL 222FF WAS FOUND TO HAVE CORROSION ON THE BOTTOM SIDE. THE FLOOR PANEL WAS REMOVE D AND REPLACED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11, PARAGRAPH 7. FOLLOWING THE COMPLETION OF THE INSTAL LATION OF THE FLOOR PANEL, THE INSTALLATION WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT 2008012500017 20080125 00017 EU 2008 1 25 F3LA200800029 1 20080123 A 5755 D57745013012 HINGE BRACKET AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE NR 2 SPOILER DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION, THE CENTER HINGE ANTI-ROTATION BRACKET FOR THE LEFT NUMBER 2 SPOILER WAS FOUND DAMAGED. MAIN TENANCE REMOVED THE DAMAGED ASSEMBLY AND PERFORMED A "MAJOR REPAIR" IN ACCORDANCE WITH THE REQUIREMENTS OF EA A8-57R-123 81. UPON COMPLETION OF THE REPAIR, THE NUMBER 2 SPOILER WAS RE-INSTALLED, INSPECTED, TESTED AND FOUND TO BE ACCEPTABLE. 2 L 7 2 4F 4 F RT 2008012500018 20080125 00018 NM 2008 1 25 NWAA080225507 1 20080119 A 2121 COOLING FAN BOEING 757 757251 1384970 NM E/E BAY FAILED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 507US 23196 DURING CLIMB, THERE WAS AN ELECTRICAL BURNING ODOR IN THE FLIGHT DECK. TURNED RECIRC FANS OFF AND SMELL SUBSIDED. AFTE R 50 MINUTES THE ODOR FAINTLY RETURNED. PERFORMED COM PROCEDURE FOR SMOKE AND FUMES. UTILITY BUSSES OFF, RECIRC FANS O FF, AND EQUIPMENT COOLING TO ALTERNATE, ODOR HAS NOT RETURNED. FLIGHT CONTINUED ON AND LANDING WAS UNEVENTFUL. MAINTEN ANCE REMOVED AND REPLACED 2 EQUIPMENT COOLING FANS, AND AN AIR RECIRC FAN. OPERATIONAL CHECKED GOOD, AND AIRCRAFT WAS R ETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2008012500024 20080125 00024 EU 2008 1 25 F3LA200800014 1 20080107 A 5320 D5361019720100 THRESHOLD AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION, CORROSION WAS FOUND ON THE BOTTOM SIDE OF THE R1 THRESHOLD STRIP. MAINTENANCE REMOVED AND RE PLACED THE THRESHOLD STRIP IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-12-12 PB 401. UPON COMPLETION OF THE INSTALLAT ION OF THE THRESHOLD STRIP, IT WAS INSPECTED AND FOUND TO BE ACCEPTABLE. 2 L 7 2 4F 4 F RT 2008012500025 20080125 00025 EU 2008 1 25 F3LA200800017 1 20080110 A 5320 D5347217220400 FLOOR SUPPORT AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION, THE FLOOR SUPPORT AT Y1292, BETWEEN FRAME 66 THROUGH FRAME 69, HAS CORROSION AT VARIOUS NUT C LIP HOLE LOCATIONS. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42 -11, PARAGRAPH 7. INSTALLATION OF HARDWARE WAS DONE IN ACCORDANCE WITH THE REQUIREMENTS OF EA A8-53R-12360. UPON COMPL ETION OF THE INSTALLATION, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT 2008012500036 20080125 00036 NM 2008 1 25 08FDEA00211 1 20080122 A 5210 69242491 LINK BOEING 727 727233 138408A NM L1 DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 MAIN DECK 1L DR CUTOUT LWR HINGE RADIUS LINK IS CORRODED. INSTALLED NEW RADIUS LINK, REF MM 52-11-001-PG 2, OPS CHECKE D GOOD THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008012500038 20080125 00038 EU 2008 1 25 08FDEA00120 1 20080114 A 2913 3508806 PUMP AIRBUS 300 A300F4605R 3930327 EU HYDRAULIC SYS LEAKING A FDEA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 686FE 20443 13564 804 APPROXIMATELY ONE HOUR IN FLIGHT, ECAM WARNING: GREEN PUMP 2 LO PR" FOLLOWED BY "GREEN PUMP 1 LO PR". OBSERVED GREEN R ESERVOIR OVERHEAT LIGHT ON. COMPLIED WITH ECAM AND QRH AND TURNED OFF BOTH GREEN PUMPS. ON APPROACH AND LANDING. ON S HORT FINAL, GREEN NR 2 LO PR LIGHT ILLUMINATED. LEAK FOUND BY GROUND CREW. REMOVED AND REPLACED NR 1 ENG GREEN SYS HY D PUMP PER MM 29-11-32-4 AND REMOVED AND REPLACED BOTH CASE DRAIN FILTERS PER MM 29-11-36-4. STILL NEEDS LEAK CK AND SA FETY WIRE. SLIGHT DISCOLORATION BUT LOOKED NORMAL. REMOVED ENG NR 2 GREEN SYS HYD PUMP AND COULD NOT ROTATE PUMP AND FOUND THE PRESSURE SIDE HYD FLUID HAD THE SAME SLIGHT DISCOLORATION BUT LOOK NORMAL WHEN REMOVED SUCTION HOSE FOUND A VE 2 L 7 2 4F RT A35EU 2008012500051 20080125 00051 SO 2008 1 25 RAIA00801013 1 20080111 A 3397 CONNECTOR EMB 145 EMB145EP 3260221 SO CABIN DIRTY A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 826HK 145016 PRE FLT 5450 - STL - EMERGENCY LIGHTS TURN ON WHEN PUT IN ARMED MODE. MAINTENANCE REMOVED THE FLIGHT ATTENDANT LIGHTING PANEL AND CLEANED THE CONNECTION. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2008012800013 20080128 00013 SO 2008 1 28 FDKA200801029 1 20080105 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 829MJ 145228 THE RT AFT FUSELAGE IS DENTED AFT OF FRAME NR 68 AND BETWEEN STRINGER 18R AND 19R. THE DAMAGE HAS BEEN RE-CONTOURED. 2 L 7 2 4T RT T00011AT 2008012300241 20080123 00241 SO 2008 1 23 C2XA08CL006 1 20080112 A 3150 WARNING SYSTEM EMB 145 EMB145XR 3260214 SO COCKPIT MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 11107 145654 IAH FLIGHT 2140 - THE CREW REPORTED A ELECTRICAL EMERGENCY ABNORMAL MESSAGE ON THE EICAS. THE CREW DIVERTED INTO CLE AN D LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND AFTER RESET COULD NOT DUPLICATE. THE NR 1 AND NR 2 BUSS TIE CONTA CTORS AND ESSENTIAL TIME RELAY AND POWER SWITCH WERE REPLACED FOR PRECAUTIONARY REASONS. OPERATIONAL CHECKS OF THE DC D ISTRIBUTION SYSTEM WERE GOOD. 2 L 7 2 4F RT 2008012400053 20080124 00053 SO 2008 1 24 C2XA08ON065 1 20080109 A 2750 FLAP EMB 145 EMB145XR 3260214 SO WING MALFUNCTIONED A C2XA K NONE J WARNING INDICATION LD LANDING 1 SW 27 14203 14500964 FLT 32 - OKC TO OKC - FLIGHT CREW REPORTED FLAP FAIL 0 DEGREE LANDING, ALSO DECLARED EMERGENCY UPON LANDING WHERE ACFT L ANDED SAFELY AND NO INCIDENTS. CONTRACT MX AAR AIRCRAFT SERVICES RESET FLAP SYSTEMS,OPERATIONALLY CHECKED SEVERAL TIME SATISFACTORY. A/C WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008012400056 20080124 00056 SO 2008 1 24 C2XA08IA024 1 20080110 A 3243 39807 VALVE EMB 145 EMB145LR 3260212 SO LT BRAKE FAULTY A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 29917 9685 152 145414 IAH - FLIGHT 2081, THE CREW REPORTED THE LEFT OUTBOARD BREAK TO BE LOCKED WITH FULL AMBER TEMP. MAINTENANCE REMOVED AND REPLACED THE O/B BRAKE CONTROL VALVE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. 2 L 7 2 4T RT T00011AT 2008012400061 20080124 00061 NM 2008 1 24 SWAA080332 1 20080115 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 22R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2008012400066 20080124 00066 NM 2008 1 24 SWAA080331 1 20080115 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 23R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2008012400067 20080124 00067 NM 2008 1 24 SWAA080333 1 20080115 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER 25R CORRODED AT BS 410 TO BS 420. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008012400072 20080124 00072 NM 2008 1 24 SWAA080323 1 20080114 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 16 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008012400086 20080124 00086 NM 2008 1 24 SWAA080334 1 20080115 A 5753 65C30462 FLAP BOEING 737 7373TO 138447G NM RT WING DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND RT WING FORE FLAP T/E DISBONDED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2008012400094 20080124 00094 NM 2008 1 24 SWAA080347 1 20080117 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 360, STR 15R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008012400144 20080124 00144 NM 2008 1 24 SWAA080389 1 20080121 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008012400186 20080124 00186 NM 2008 1 24 USAA920080153 1 20080103 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK - CORROSION ON STRINGER, BS 440, S29R. REPAIRED STRINGER, BS 440, S29R IAW B737 SRM 53-00 -03 FIGURE 201. 2 L 7 2 4F RT A2NM 2008012400212 20080124 00212 NM 2008 1 24 SWAA080411 1 20080122 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008012400214 20080124 00214 NM 2008 1 24 SWAA080412 1 20080122 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008012400227 20080124 00227 NM 2008 1 24 SWAA080401 1 20080122 A 5310 6546818 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 616 TO BS 639, RBL 70. REMOVED AND REPLACED WEB PER S RM. 2 L 7 2 4F RT A16WE 2008012400234 20080124 00234 NM 2008 1 24 SWAA080400 1 20080122 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008012400272 20080124 00272 NM 2008 1 24 08FDEA00180 1 20080116 A 5730 112N60081 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 LT WING FUEL TANK ACCESS PANEL 541FB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 541FB PER SRM 57-20-01. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 201, DETAIL I, SECTION AA, NOTE B, WITHIN .1" OF SEAL. REPLACED PANEL 541FB IAW AMM 28-11-01. 2 L 7 2 4F RT A2NM 2008012400273 20080124 00273 NM 2008 1 24 08FDEA00181 1 20080116 A 5730 112N60081 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 LT WING FUEL TANK ACCESS PANEL 541DB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 541DB PER SRM 57-20-01. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 201, DETAIL I, SECTION AA, NOTE B, WITHIN .1" OF SEAL. REPLACED PANEL 541DB IAW AMM 28-11-01. 2 L 7 2 4F RT A2NM 2008012400370 20080124 00370 EU 2008 1 24 USAA920080178 1 20080112 A 5315 D53610183002 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 885 CLT - MAJOR REPAIR - RON, PILOT REPORT - CORROSION ON CABIN FLOORBEAM, BS 709 / FR 16, -Y765 TO -Y1296. REPLACED CABIN FLOORBEAM, BS 709 / FR 16, -Y765 TO -Y1296 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008012500004 20080125 00004 NM 2008 1 25 NWAA080246312 1 20080118 A 5320 WEB BOEING 747 747451 1384940 NM BS 2300 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 672US 30267 DURING "L" CHECK AND ACCOMPLISHMENT OF CREW REST MODIFICATION FOUND FLOOR WEB AT BS 2300 RBL 60-RBL 80 WITH SHORT EDGE M ARGIN. REPAIRED PER EA 63-211481. 2 L 7 4 4F RT A20WE 2008012500008 20080125 00008 NM 2008 1 25 NWAA080215508 1 20080116 A 3350 SIGN BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 508US 23197 DURING OVERNIGHT, FOUND NR 2L DOOR EMERGENCY EXIT SIGN INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. OPERATIONA L CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2008012800039 20080128 00039 SO 2008 1 28 C2XA08SH008 1 20080116 A 5315 14521700007 FLOORBEAM EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13124 145689 SHV - DURING C-CHECK, LT OMEGA BEAM AT FR 20 CORRODED. MX REPAIRED LT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 51-40-02. TH E AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008012800056 20080128 00056 SO 2008 1 28 C2XA08SH009 1 20080116 A 5330 N6THKC51000 PANEL EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13124 145689 SHV - DURING C-CHECK 192 KL PANEL HAS COMPOSITE DAMAGE ON SCREW HOLE. MX REPAIRED 192 KL PANEL IAW 145 SRM 52-40-01 STE P 2 A THRU C AND EC 5750-01315 REV E. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICES. 2 L 7 2 4F RT 2008012800068 20080128 00068 SO 2008 1 28 C2XA08SH010 1 20080116 A 5751 N6THKC51000 SHROUD EMB 145 EMB145XR 3260214 SO LT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13124 145689 SHV- DURING C-CHECK, LT LOWER AILERON SHROUD HAS CORRODED BONDING PLATE. MX REPAIRED LT LOWER AILERON SHROUD IAW EC5750 -01315. THE AIRCRAFT WAS APPROVE TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008012800070 20080128 00070 SO 2008 1 28 FDKA200801001 1 20080101 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6137 DAY (0743 PHX LCL) - EMERGENCY FLOOR PROX LIGHTS OUT BETWEEN ROW 3 TO 7. MX RESECURED CONNECTOR ON FLOOR PROX LIGHT AT ROW 7. 2 L 7 2 4T RT T00011AT 2008012400132 20080124 00132 NM 2008 1 24 SWAA080366 1 20080117 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 422WN 29826 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 157. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008012400156 20080124 00156 NM 2008 1 24 ASAA0852469 1 20080108 A 2160 233A3101 CONTROLLER BOEING 737 737890 1384527 NM CABIN TEMP MALFUNCTIONED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 579AS 35187 ON RECALL "ZONE TEMP" LIGHT ILLUMINATED. LIGHT CLEARS WITH MASTER CAUTION RESET. PERFORMED FIM 21 62 TASK 842 & TEMP C ONTROLLER BITE PROCEDURE 21 62 TASK 801. OP CHECKS GOOD, NO FAULT FOUND. TESTS NORMAL. 2 L 7 2 4F RT A16WE 2008012400176 20080124 00176 NM 2008 1 24 USAA920080141 1 20080110 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FLOORBEAM, BS 328, RBL 32. REPAIRED FLOORBEAM, BS 328, RBL 32 IAW BOEING 737 S RM 51-10-02. 2 L 7 2 4F RT A16WE 2008012400184 20080124 00184 NM 2008 1 24 USAA920080151 1 20080109 A 5313 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK - CRACKED STRINGER, BS 1681, S2R. REPAIRED STRINGER, BS 1681, S2R IAW B737 SRM 53-00-03 F IGURE 201. 2 L 7 2 4F RT A2NM 2008012400188 20080124 00188 NM 2008 1 24 USAA920080160 1 20080102 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 480, S9L. REPAIRED FRAME, BS 480, S9L IAW USAIRWAYS EO 5311-01019. 2 L 7 2 4F RT A16WE 2008012400189 20080124 00189 NM 2008 1 24 USAA920080161 1 20080102 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 827, S9L. REPAIRED FRAME, BS 827, S9L IAW USAIRWAYS EO 5311-01019. 2 L 7 2 4F RT A16WE 2008012400204 20080124 00204 NM 2008 1 24 CALA0800022 1 20080113 A 5210 6552878U97 ANGLE BOEING 737 7373T0 1384582 NM L2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76354 23592 L2 DOOR Z-ANGLE HAS CORROSION TO AND BOTTOM (MKD). REMOVED AND REPLACED Z-ANGLE PER REF 737-300 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008012400216 20080124 00216 SO 2008 1 24 FDKA200801011 1 20080108 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO LAVATORY SMOKE A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 837MJ 145367 FDM 6032 DAY (1540 PHX LCL) - LAVATORY SMOKE WARNING AND SMOKE IN THE GALLEY AREA. MX INSPECTED GALLEY, LAV AND CABIN L IGHTS, FIXTURES AND BALLAST AND FOUND NO DEFECTS. 2 L 7 2 4T RT T00011AT 2008012400225 20080124 00225 NM 2008 1 24 SWAA080402 1 20080122 A 5311 6545805 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16R. REPAIRED FRAME PER BOEING DRAWING. 2 L 7 2 4F RT A16WE 2008012400232 20080124 00232 NM 2008 1 24 SWAA080403 1 20080122 A 5322 6546529 SHEAR TIE BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 420WN 29825 DURING SCHEDULED 6Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 15.04. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008012400254 20080124 00254 SO 2008 1 24 FDKA200801016 1 20080109 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX STIFF A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 835MJ 145353 FDM 6140 MCO (1250 PHX LCL) - PAX DOOR HARD TO OPEN. MX CURRENTLY TROUBLESHOOTING. 2 L 7 2 4T RT T00011AT 2008012400311 20080124 00311 NM 2008 1 24 08FDEA00206 1 20080119 A 5311 53FX13501 FRAME BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 FWD PIT STUB FRAME EXTENSION AT BS 540, 22L IS CRACKED OUT OF RADIUS. MARKED END OF CRACK WITH BLACK DOT ON FWD SIDE. REMOVED STUB FRAME EXTENSION AT STA 540, STR 22R, REF SRM 51-30-2. FABRICATED NEW STUB FRAME, HEAT TREATED ON NR N00785 , 8130-3 NR 2008-01-053. DRILLED UP NEW STUB FRAME REF SRM 51-30-2. TREATED AND PRIMED STUB FRAME REF 51-10-2, LABELED PART NUMBER FX53FX1350-1 REF FED EX GMM 7-0-1001. INSTALLED NEW STUB FRAME REF SRM 51- 30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2008012400315 20080124 00315 NM 2008 1 24 08FDEA00208 1 20080120 A 5754 2024730016 SKIN BOEING 757 757200 1384950 NM ZONE 600 NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 SLAT NR 7 TRAILING EDGE WEDGE EXTERNAL DOUBLER, REF: ENTRY NR R15 IN 4X-BY EXTERNAL DAMAGE RECORD SHEET. THE TEMPORAR Y REPAIR DOUBLER AT SLAT NR 7 TRAILING EDGE WEDGE OUTER SURFACE SKIN REMOVED. COMPLIED WITH ATTACHMENT B OF EO F-5100-7 -5001 P1. REPAIR DOUBLER, FABRICATED AND INSTALLED IN ACCORDANCE WITH B757-200 SRM 51-70-10 REPAIR 4, FIG 201 (SHEET 1 OF 5) REV 93. THE NEW 6.5 INCH BY 10 INCH REPAIR DOUBLER IS CLASSIFIED AS MAJOR REPAIR PER GMM 6-2-100 CRITERIA. THIS IS A PERMANENT REPAIR AND NO FOLLOW UP ACTION IS REQUIRED. 2 L 7 2 4F RT A2NM 2008012400320 20080124 00320 NM 2008 1 24 08FDEA00221 1 20080122 A 5320 69142991 INTERCOSTAL BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 LEFT LOWER FUSELAGE "B" SYSTEM HYD COMPARTMENT HYDRAULIC LINE SUPPORT INTERCOSTAL CRACKED 3 AREAS IN RADIUS, STA 950A PLUS 4, TO 950A PLUS 7 JUST O/B OF RESERVOIR REMOVED CRACKED INTERCOSTAL, FABRICATED NEW INTERCOSTAL, P/N 69-14299-1. T REATED AND PRIMED, AND INSTALLED NEW INTERCOSTAL. RECONNECTED HYD LINES AND CONNECTOR, REF AMM 29-12-001-4 PG 2, BOEING DWG 69-14299/SRM 51-10-2 PG 1, SRM 51-30-2 PG 2-3. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008012400337 20080124 00337 CE 2008 1 24 DXTA200802782 1 20080120 A 2150 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL A/C BAY MALFUNCTIONED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 978QS 7500187 CABIN PACK MAKING SMOKE AND BURNED RUBBER ODOR. REMOVED FAULTY ACM. INSTALLED ACM REPAIRED BY HAMILTON SUNDSTRAND. OPE RATIONAL & LEAK CHECKS GOOD. WORK DONE IAW 750 MM 21-51-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008012400368 20080124 00368 EU 2008 1 24 USAA920080176 1 20080112 A 5320 D53111460202 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 885 CLT - MAJOR REPAIR - RON, PILOT REPORT - NR 0014682, CORROSION ON CABIN FLOOR SUPPORT, BS 709 / FR 16 - BS 760 / FR 18, -Y254. REPLACED CABIN FLOOR SUPPORT, BS 709 / FR 16 - BS 760 / FR 18, -Y254 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008012400371 20080124 00371 EU 2008 1 24 USAA920080179 1 20080112 A 5320 D531182830202 DUMMY RAIL AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 885 CLT - MAJOR REPAIR - RON, PILOT REPORT - CORROSION ON CABIN DUMMY RAIL, BS 709 / FR 16 - BS 760 / FR 18, -Y4. REPLACED CABIN DUMMY RAIL, BS 709 / FR 16 - BS 760 / FR 18, -Y4 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008013000133 20080130 00133 NM 2008 1 30 TSAA0853004 1 20080122 A 5330 6545769 SKIN BOEING 737 737236 1384476 NM BS 470 S26-28R TORN A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 837AL 23169 SKIN DAMAGE AT BS 470 BETWEEN STR 26R AND STR 28R. REPAIRED DAMAGE IAW ECO 3705. 2 L 7 2 4F RT A16WE 2008013000135 20080130 00135 EA 2008 1 30 SWIA200819076 1 20080118 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 917SW 7641 FLT 6731 - LEFT WINDSHIELD SHATTERED. REPLACED PILOT'S WINDSHIELD IAW CRJ MM 56-11-01, PN NP-139321-13, SN/OFF 01355H56 50. 2 L 7 2 4F RT A21EA 2008013000137 20080130 00137 EA 2008 1 30 SWIA200819078 1 20080118 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA RIGHT SMOKE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 983SW 19985 3964 7961 FLT 5928 - RECEIVED SMOKE TOILET CAUTION MESSAGE AFTER TAKEOFF. REPLACED RIGHT AIR CYCLE MACHINE IAW 21-51-10. 2 L 7 2 4F RT A21EA 2008013000142 20080130 00142 NM 2008 1 30 DL76G080068 1 20080116 A 3350 21201 POWER SUPPLY BOEING 767 767332 1382001 NM ROW 4AB FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1612T 30575 EMERGENCY LIGHTS IN AFT SECTION OF BUSINESS CLASS INOP. REPLACED BATTERY POWER SUPPLY PACK M11558, LIGHTS NOW CHECK GOO D PER AMM. 2 L 7 2 4F RT A1NM 2008013000150 20080130 00150 NM 2008 1 30 DLM88080078 1 20080116 A 5315 FLOORBEAM DOUG MD88 MD88 3023688 NM BS 984 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 CRACKED FLOORBEAM AT PAX CABIN BTW STA Y=984 X=0,11. NEW FLOOR SUPPORT INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F RT A6WE 2008013000151 20080130 00151 NM 2008 1 30 DLM88080079 1 20080116 A 5315 FLOORBEAM DOUG MD88 MD88 3023688 NM BS 965 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 CRACKED FLOORBEAM ON PAX CABIN AT STA Y=965 AND X=0. NEW FLOOR SUPPORT INSTALLED IAW DOUGLAS DRW 5930544. 2 L 7 2 4F RT A6WE 2008013100002 20080131 00002 NE 2008 1 31 COMA0870001 2 20080110 A 7230 4414T15P02 FAN BLADE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE LT ENGINE LACK OF LUBE A COMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 655CA 10134 965326 FLIGHT 5448 - LEFT ENGINE VIBE AT 1.9 AT CLIMB, REDUCED POWER TO 68% TO GET TO GO GREEN. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED LEFT ENGINE FAN BLADES PER EO 72-017. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008013100004 20080131 00004 SO 2008 1 31 C2XA08IA022 1 20080109 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145EP 3260221 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14925 145004 IAH - DURING MAINTENANCE INSPECTION NUMEROUS EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE NUMBER 1 EMERGENCY LIGHT BATTERY POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFETCS NOTED, AND THE AIRCRAFT W AS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008013100020 20080131 00020 EA 2008 1 31 MASA200800019 1 20080110 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37342 7342 ASH 7186 ORD - AFT CABIN CENTER AISLE EMERGENCY FLOOD LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2008013100029 20080131 00029 WP 2008 1 31 UPS08851455 1 20080102 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 MAIN CABIN FLOOR PNL RIGHT INBD STA 660-760 IS DAMAGED AT END OF PLANK. REMOVED, FABRICATED, AND INS TALLED MAIN CABIN FLOOR PNL AT RIGHT INBD STA 660-760 REF EO DC8-5320-9691-C. 2 L 7 4 4F RT 4A25 2008013100076 20080131 00076 SO 2008 1 31 RAIA00801021 1 20080118 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 830HK 145313 PRE FLT 5587 - STL - EMERGENCY LIGHT AT AIRSTAIR HANDRAIL INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008013100081 20080131 00081 NM 2008 1 31 SWAA080417 1 20080123 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008013100082 20080131 00082 NM 2008 1 31 SWAA080433 1 20080123 A 2560 6557463 BRACKET BOEING 737 7373H4 1384600 NM BIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR BRACKET CORRODED. REMOVED AND REPLACED BRA CKET PER SRM. 2 L 7 2 4F RT A16WE 2008013100136 20080131 00136 2008 1 31 SWAA080447 4 20080123 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 238WN 34713 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008013100145 20080131 00145 NM 2008 1 31 SWAA080450 1 20080126 A 5743 6546543 SUPPORT FITTING BOEING 737 7373H4 1384600 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED MV2 CHECK, FOUND RT MLG SUPPORT FITTING CORRODED AT BS 685. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008012800146 20080128 00146 NM 2008 1 28 C1HA200883001 1 20080114 A 5330 SKIN BOEING 727 7272S7 138407Z NM BS 388 S33R DENTED A C1HA K NONE O OTHER IN INSP/MAINT 1 GL 15 683CA 22490 DENT AT BS 388 ON STR 22R TASK CARD E99683-1.4 DUE TEMP REPAIR AT DENT IN FUSE STA AT BS 338 AND S-22R VERIFIED HFEC INS PECTION OF DENT AND STRINGER HAS BEEN ACCOMPLISHED ON WO 122987 AND THAT NO CRACKS WERE FOUND. TEMP REPAIRED PER TASK C ARD E99683-14. ACCOMPLISH PERMANENT REPAIR AT NEXT C CHECK PLACED ON TLD T01351, M/C ADVISED. 2 L 7 3 4F A3WE 2008012800148 20080128 00148 NM 2008 1 28 08FDEA00224 1 20080122 A 5347 AFA7795501 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 MAIN DECK SEAT TRACK AT STA 1806 LBL 8 FOUND EXFOLIATION CORROSION. MAIN DECK SEAT TRACK REPAIR CARRIED OUT REPAIR AS P ER SRM 53-70-00 FIGURE 1 VOLUME I . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008012800150 20080128 00150 NM 2008 1 28 08FDEA00226 1 20080122 A 5753 ARC40091 HINGE FITTING DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING, OUTBOARD FLAP INBOARD HINGE FITTING ARC4009 FORWARD INBOARD FASTENER HOLE FOUND CORROSION. LT WING, OUTBO ARD FLAP R & R AS PER AMM 27-50-30-4. FLAP ADJUSTMENT CARRIED OUT AS PER AMM 27-50-00-830-805. TEST OF THE FLAP SYSTEM O PERATION/RANGE OF MOVEMENT CARRIED OUT AS PER AMM 27-50-00-710-801. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008012800165 20080128 00165 EU 2008 1 28 F3LA200800027 1 20080123 A 5755 D57750021000118A HINGE FITTING AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE NR 4 SPOILER DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION, THE CENTER HINGE ANTI-ROTATION LUG FOR THE LEFT NUMBER 4 SPOILER WAS FOUND DAMAGED. MAINTENA NCE REMOVED THE DAMAGED ASSEMBLY AND PERFORMED A "MAJOR REPAIR" ON ACCORDANCE WITH THE REQUIREMENTS OF EA A8-57R-12379. UPON COMPLETION OF THE REPAIR THE NUMBER 4 SPOILER WAS RE-INSTALLED, INSPECTED, TESTED AND FOUND TO BE ACCEPTABLE. 2 L 7 2 4F 4 F RT 2008012800178 20080128 00178 EU 2008 1 28 08FDEA00213 1 20080117 A 5315 FLOORBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 MDCC - ANGLE SUPPORT AT FR43 FLOOR LEVEL FOUND CRACKED AT Y 2860. THE ANGLE WAS REPLACED IAW SRM 51-72-10 AND EO51-40-2 1. 2 L 7 2 4F RT A35EU 2008012800179 20080128 00179 NM 2008 1 28 UPS08551429 1 20080112 A 3350 LAMP BOEING 757 75724APF 1384969 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 473UP 28846 EMERGENCY LIGHT DISARMED LIGHT BURNED OUT. RELAMPED, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2008012800183 20080128 00183 WP 2008 1 28 UPS08851414 1 20080102 A 5313 3754473501N LONGERON SPLICE DOUG DC8 DC871F 302199D WP BS 1270 L31L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 C CARGO COMPT STA 1270 AND L31L SPICE HAS CORROSION. REPLACED LONGERON SPLICE AT STA 1270 AND L31 L PER SRM 51-1-20D, SRM 53-2-0 FIG 1F AND SRM 51-3-2. 2 L 7 4 4F RT 4A25 2008012800187 20080128 00187 2008 1 28 08FDEA00132 4 20080115 A 3497 CONNECTOR BOEING 727 727223 1384074 NM BURNED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 223FE 20935 AT ROTATION OFF FLAG IN CAPT'S ALTIMETER AND ALT SELECT WINDOW APPEARED. FOUND RACK CONNECTOR D609 CENTER SECTION, BEHI ND NR 1 CADC BLACK FROM ELECTRICAL DAMAGE. INSTALLED WIRE NUMBERS W0007-162-22 AND W0007-9069-2 2 IN D609A PIN 12 PER BOEING HOOK UP LIST. INSTALLED WIRE NUMBERS W0007-9069-22 AND W0007-9070-22 IN PIN 42 IN D609A OF DADC NR 1. INSTALLED CONNECTOR ASSY PN NR DPD2MB-152-33S-2 PER BOEING STANDARD WIRING PRACTICES 20-71-11. REPLACED DADC NR 1 PER B727-200 A MM 34-11-051. NEEDS OPS CHECKED. INSTALLED CABIN PRESSURE CONTROLLER PER B727 AMM 21-31-010-4. PERFORMED SYS OPS CHEC K AND LEAK CHECK TO DADC, ALSO OPS CHECK AND LEAK CHECK TO CABIN PRESSURE CONTROLLER, SYS OPS CHECK NORMAL. 2 L 7 3 4F A3WE 2008012800193 20080128 00193 SO 2008 1 28 C2XA08TY010 1 20080115 A 5751 BUSHING EMB 145 EMB145XR 3260214 SO LT AILERON MIGRATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 21130 145704 LT AILERON PCA BRACKET HAS MIGRATED BUSHINGS AT O/B ATTACH. REMOVED AND REPLACED LT AILERON PCA BRACKET IAW EC 5750-011 77. AIRCRAFT STILL IN C CHECK. 2 L 7 2 4F RT 2008012900009 20080129 00009 SO 2008 1 29 RAIA00801015 1 20080111 A 3230 355022002 CONTROL UNIT EMB 145 EMB145LR 3260212 SO LANDING GEAR MALFUNCTIONED A RAIA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 818HK 19852 19851 145059 FLT 5524 - RIC - LOUD RUMBLE IN FLIGHT AT ALL ALTITUDES AND SPEEDS. MAINTENANCE REMOVED AND REPLACED THE LGEU AND PERFO RMED SEVERAL GEAR SWINGS. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012900016 20080129 00016 SO 2008 1 29 C2XA08SH002 1 20080116 A 5200 14534499002 DOOR FRAME EMB 145 EMB145LR 3260212 SO PAX DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26549 145571 SHV - DURING C-CHECK MAIN DOOR LOWER FRAME HAVE CORROSION AROUND NUT PLATE HOLES. MX REPAIRED MAIN DOOR LOWER FRAME IAW EMB 145 EC 5210-01154. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008012900018 20080129 00018 SO 2008 1 29 C2XA08SH003 1 20080116 A 5751 14569009409 ATTACH BRACKET EMB 145 EMB145LR 3260212 SO LT AILERON DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26549 145571 SHV - DURING C-CHECK LEFT WING AILERON HAS EXCESSIVE PLAY AT PCA RODS AND MIGRATED HAT BUSHING AT ATTACHMENT LUG. MX RE MOVED AND REPLACED LEFT AILERON PCA BRACKET IAW EMB 145 SRM 51-40-02 & EC5750-01177. THE AIRCRAFT WAS APPROVED TO RETUR N FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008012900028 20080129 00028 NM 2008 1 29 2008UALA00128 1 20080107 A 2720 Q0904 TRANSDUCER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE RUDDER FAULTY A UALA O OTHER W INADEQUATE Q C AP APPROACH 1 WP 29 671UA 30026 RUDDER RATIO LIGHT ILLUM IN FLIGHT. EICAS MSG RUDDER RATIO DISPLAYED. REPLACED LEFT ELEC HYD PUMP CONTROL PRESS SWITCH AND INSPECTED CONNECTOR, NO DEFECTS FOUND. REPLACED RUDDER RATIO LVDT. OP CHECK NORMAL, OSCILATION CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012400335 20080124 00335 CE 2008 1 24 DXTA200802780 1 20080121 A 3260 WARNING LIGHT BEECH MU300 400A 1155402 CE COCKPIT ILLUMINATED E DXTA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 07 141QS RK498 AFTER TAKEOFF, RED WARNING LIGHT IN GEAR HANDLE REMAINED ILLUMINATED WHEN GEAR WAS RETRACTED. INSPECTED LANDING GEAR A ND PERFORMED OPERATION CHECK OF LANDING GEAR SYSTEM. NO DEFECTS FOUND OPS CK GOOD IAW MM CH 32-10. 2 H 7 2 4F RT A16SW 2008012400359 20080124 00359 SO 2008 1 24 GLBA20061051 1 20080121 A 5730 SKIN EMB 120 EMB120ER 3260203 SO RT WING CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 108UX 120108 MAJOR REPAIR RT LOWER WING SKIN CRACKED APPROXIMATELY .9 INCH IN LENGTH AT THE FORWARD IB CORNER AND AFT OB CORNERS OF F UEL ACCESS PANEL 621AB. STOP DRILLED CRACKS AND PATCHED IAW SRM 57-20-01. 2 L 7 2 4T RT A31SO 2008012400361 20080124 00361 NM 2008 1 24 USAA920080184 1 20080114 A 5754 WEB BOEING 757 757225 1384959 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 22198 PIT - MAJOR REPAIR - C4 CHECK - RIGHT WING NR 9 SLAT WEB CRACKED, FSS 599. REPAIRED RIGHT WING 9 SLAT WEB, FSS 599 IAW USAIRWAYS EA 110393. 2 L 7 2 4F RT A2NM 2008012400364 20080124 00364 EU 2008 1 24 USAA920080155 1 20080104 A 5315 D5347217220390 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 669AW 1792 PIT - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3043 / FR 64 - BS 3510 / FR 69, -Y1162. REPLACED CABI N FLOORBEAM, BS 3043 / FR 64 - BS 3510 / FR 69, -Y1162 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008012400367 20080124 00367 EU 2008 1 24 USAA920080158 1 20080104 A 5315 D5347217220400 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 669AW 1792 PIT - MAJOR REPAIR - BC4 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3158 / FR 66 - BS 3366 / FR 70, +Y1162. REPLACED CABI N FLOORBEAM, BS 3158 / FR 66 - BS 3366 / FR 70, +Y1162 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008012500015 20080125 00015 EU 2008 1 25 F3LA200800015 1 20080107 A 5320 D5348004320601 SILL AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION, THE L2 DOOR SILL, AFT, OUTBOARD NUTPLATE HOLE FOR THE GIRT BAR BLANKING PLATE SHOWED SIGNS OF CORROSION. MAINTENANCE REMOVED THE L2 DOOR SILL IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-52-11. A NEW DOOR SILL WAS INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPLACEMENT OF THE L2 DOOR SI LL, THE INSTALLATION WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT 2008012500022 20080125 00022 NM 2008 1 25 NWAA080176301 1 20080116 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 661US 23719 DURING OVERNIGHT CHECK, FOUND EXTERIOR EMERGENCY LIGHT BELOW DOOR 3R 3RD AND 4TH POSITIONS WILL NOT ILLUMINATE. MAINTEN ANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008012900001 20080129 00001 WP 2008 1 29 DHLA200800008 1 20080122 A 2612 FIRE WARNING DOUG DC8 DC873F 302199F WP NR 1 NACELLE MALFUNCTIONED A DHLA O OTHER N FALSE WARNING AP APPROACH 1 GL 05 806DH 46002 FLT 403, NR 1 ENGINE FIRE WARNING FLASHED A COUPLE OF TIMES DURING FINAL APPROACH LOOP A HANDLE AND MASTER LIGHTS. DEF ERRED PER MEL 26-2-3 A-LOOP DMI NR 31485 PLACARD INSTALLED CAT C B-LOOP, OPS CK GOOD SP C/W 26-2. T/S SYS IAW MMS 26-10 -0. REMOVED AND REPLACED 5 EACH DETECTORS NR1 ENG IAW MMS 26-10-1. RAN NR 1 ENG PER JRH. SYSTEM TESTS GOOD. THIS ACT ION CLEARS MDDR NR 31485 PLACARDS REMOVED. 2 L 7 4 4F RT 4A25 2008012900003 20080129 00003 SO 2008 1 29 RAIA00801012 1 20080111 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 840HK 145341 PRE FLT 7949 - MKE - EMERGENCY LIGHT INOP. MAINTENANCE SECURED THE CONNECTOR TO THE LIGHT. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008012900024 20080129 00024 SO 2008 1 29 C2XA08TY009 1 20080116 A 4920 APU EMB 145 EMB145XR 3260214 SO CONTAMINATED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14188 14500929 TYS LAV SMOKE OCCURRED DURING CLIMBOUT IN THE LAV. CREW CHECKED LAV AREA, MESSAGE CLEARED AND RETURNED TO BLOCK. MAINT ENANCE FOUND VERY HEAVY DEICING FLUID RUNNING DOWN THE APU INLET. MAINTENANCE RAN THE BLEEDS AND ENGINE BLEEDS. PERFOR MED LAV SMOKE CHECKS AND OPS CHECKS GOOD. NO FURTHER MESSAGES, RELEASED BACK TO SERVICE IAW EMB 145XR AMM26-14-00. 2 L 7 2 4F RT 2008012900045 20080129 00045 NM 2008 1 29 2008UALA00189 1 20080110 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 CABIN FRAME BS 908 SHEAR TIE IS CRACKED AT UPPER FASTENER HOLE BETWEEN STR 13R AND 14R. CUT OUT DAMAGED AREA AND INSTAL LED REPAIR ANGLE WITH A FILLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900058 20080129 00058 NM 2008 1 29 2008UALA00194 1 20080111 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY CEILING LIGHT ABOVE ROW 5 INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900060 20080129 00060 NM 2008 1 29 2008UALA00196 1 20080111 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY CEILING LIGHT ROW 24 LT INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900063 20080129 00063 NM 2008 1 29 2008UALA00199 1 20080110 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 SEAT EEL INOP AT 32 HJK. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900065 20080129 00065 NM 2008 1 29 2008UALA00201 1 20080113 A 2910 FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HYDRAULIC SYS DAMAGED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 347UA 24251 DIVERTED UNDER AMBER ALERT DUE TO HYDRAULIC PROBLEM. FOUND LOOSE GROUND SPOILER PRESSURE FITTING AT THE NR 5 SPOILER IN BOARD ACTUATOR. REPLACED UNION AND PACKING. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900099 20080129 00099 NM 2008 1 29 2008UALA00214 1 20080111 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 EEL INTERMITTENT, D-ZONE LT COLUMN. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900102 20080129 00102 NM 2008 1 29 2008UALA00216 1 20080111 A 5210 HINGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 R2 DOOR UPPER HINGE ARM ASSY CUTOUT REQUIRES DOUBLER INSTALLATION. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012900105 20080129 00105 NM 2008 1 29 2008UALA00220 1 20080114 A 4920 APU BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE APU BAY ODOR A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 221UA 30552 SMOKE CREW REST F-D DETECTED SMOKE IN THE FLIGHT DECK CREW REST COMPARTMENT. FOUND APU OIL SYSTEM DEFECTIVE & CAUSED C ABIN OILY ODOR. REPLACED APU ASSY PER AMM49-11-01 PG401. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008012900106 20080129 00106 NM 2008 1 29 2008UALA00221 1 20080114 A 3510 MF20OO3 OXYGEN MASK BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE COCKPIT FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 782UA 26948 OXYGEN MASK WILL NOT STAY SNUG WHILE DEPLOYED. SUSPECT BROKEN STRAP. REPLACED DEMO MASK AT LOCATION 217. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008012900137 20080129 00137 NM 2008 1 29 2008UALA00174 1 20080110 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN LOOSE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 675UA 29243 LOOSE WIRE ATTACHED TO SMALL THIN PANEL FOUND LOOSE AT SEAT 28H. INSTALLED NEW EEL STRIP, OP CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900141 20080129 00141 EU 2008 1 29 08FDEA00193 1 20080118 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 404FE 233 AFT CARGO COMPT LT SIDE FRAME 58 FLOOR LEVEL CROSS MEMBER HAS CORROSION ON UPPER SURFACE REMOVED DAMAGED SECTION ON LT S IDE OF CROSSBEAM AT Y140 AND INSTALLED CROSSBEAM REPAIR IAW A310 SRM 53-10-15, FIG 201. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER 2 L 7 2 4F RT A35EU 2008012900147 20080129 00147 EU 2008 1 29 F3LA200800026 1 20080123 A 5755 D57750021000118A HINGE FITTING AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE NR 4 SPOILER DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION, THE CENTER HINGE ANTI-ROTATION LUG FOR THE RIGHT NUMBER 4 SPOILER ACTUATOR BOLT WAS FOUND DAM AGED. MAINTENANCE REMOVED THE DAMAGED ASSEMBLY AND PERFORMED A "MAJOR REPAIR" IN ACCORDANCE WITH THE REQUIREMENTS OF EA A8-57R-12379. UPON COMPLETION OF THE REPAIR, THE NUMBER 4 SPOILER WAS RE-INSTALLED, INSPECTED, TESTED AND FOUND TO BE ACCEPTABLE. 2 L 7 2 4F 4 F RT 2008012900148 20080129 00148 EU 2008 1 29 F3LA200800028 1 20080123 A 5755 D57750021000118A HINGE FITTING AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE NR 3 SPOILER DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK INSPECTION, THE CENTER HINGE ANTI-ROTATION LUG FOR THE RIGHT NUMBER 3 SPOILER WAS FOUND DAMAGED. MAINTEN ANCE REMOVED THE DAMAGED ASSEMBLY AND PERFORMED A "MAJOR REPAIR" IN ACCORDANCE WITH THE REQUIREMENTS OF EA A8-57R-12379. UPON COMPLETION OF THE REPAIR, THE NUMBER 3 SPOILER WAS RE-INSTALLED, INSPECTED, TESTED AND FOUND TO BE ACCEPTABLE. 2 L 7 2 4F 4 F RT 2008012900150 20080129 00150 NM 2008 1 29 CALA0800027 1 20080113 A 5320 6545874 SILL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76354 23592 CORROSION AT STA 296 RIGHT DOOR SILL WEB AT NUT PLATE HOLE CORROSION FOUND OUT OF LIMIT IAW SRM 53-10-15. REPAIRED IAW SRM 51-70-13, INSTALLED REPAIR IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2008012900157 20080129 00157 NM 2008 1 29 SB08002 1 20080117 A 3397 WIRE BOEING 737 737401 1384701 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 404US 23886 DFW - MAINTENANCE REPORTED THE ESCAPE PATH EMERGENCY LIGHTS AT SEAT ROWS 18, 19 AND 24 INOPERATIVE AND THE EMERGENCY EXI T LIGHT AT SEAT ROW 6 INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE 8 INCHES FROM LIGHT AT SEAT ROW 6 PER SWPWM 20-30 -12, REPLACED A BROKEN SPLICE AT SEAT ROW 24 PER SWPM 20-30-12 AND RECONNECTED A DISCONNECTED PLUG FOR SEAT ROWS 18 AND 19. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD. 2 L 7 2 4F RT A16WE 2008012900161 20080129 00161 NM 2008 1 29 KCSA081023 1 20080117 A 5412 DOUBLER BOEING 747 747209B 138489B NM NR 1 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 NR 1 PYLON NAC STA 128.95 LOWER O/B DOUBLER CRACKED AT LOWER END OF RADIUS. 2 L 7 4 4F RT A20WE 2008012900167 20080129 00167 SO 2008 1 29 C2XA08ON066 1 20080116 A 2611 FAU751A4 CONTROL PANEL EMB 145 EMB145XR 3260214 SO SMOKE DETECTION MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13161 10383 10383 14500805 FLT 54 - MCI TO TUS - LAV SMOKE DETECTOR DID NOT TEST. MX PERSONNEL AT ONT PERFORMED TROUBLESHOOTING OF LAV SMOKE DETEC TOR AND REMOVED AND REPLACED SMOKE DETECTION PANEL AND CONNECTOR. OPERATIONALLY CHECKED SATISFACTORY AND A/C WAS RELEAS ED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008012900168 20080129 00168 GL 2008 1 29 C2XA08ON067 2 20080116 A 7532 32158861 BLEED VALVE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL NR 2 ENGINE MALFUNCTIONED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 14188 6835 6835 1450929 FLT 1340 - TYS TO TYS - FLIGHT CREW REPORTED BLEED 1/2 LOW TEMP WITH WING 2 FAIL, IT WAS AN AIR RETURN AND DECLARED NO E MERGENCY AT THE TIME AND AIRCRAFT LANDED WITH NO INCIDENTS. MX PERSONNEL REMOVED AND REPLACED NR 2 ENG BLEED VLV AND OP ERATIONALLY CHECKED SATISFACTORY. A/C WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2008012900174 20080129 00174 NM 2008 1 29 2008UALA00153 1 20080108 A 3350 D9239003500060 EPSU AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 809UA 825 CIDS FAULTS, EPSU BATTERY EMER L, EPSU BATTERY, AFT L. EPSU FAILURE. REPLACED EPSU AT 11WL AND 13WL. ALL SYSTEMS TEST ED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900176 20080129 00176 2008 1 29 2008UALA00155 4 20080108 A 2565 D31516113 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 401UA 435 DOOR 1L SLIDE COVER HAS MOVED AND PREVENTS SEEING PRESSURE GAUGE. REPLACED ENTIRE SLIDE PACK ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900186 20080129 00186 EU 2008 1 29 2008UALA00226 1 20080113 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 444UA 824 LIGHTNING STRIKE AT FRAME 12 ON RIGHT SIDE IS AT FWD EDGE OF SKIN PANEL. HOLE IS BURNED 100% OF SKIN ABOUT .125". ABOU T 50% BURN THROUGH FOR .25". MORE THAN 10% BURN THROUGH FOR .625". INTEGRITY NOT COMPROMISED. REPLACED ELEVATOR AND P ERFORMED MAJOR REPAIR OF DAMAGED AREA AT FRAME 12. ALL OTHER AREAS ADDRESSED BY BURNISHING. ACCOMPLISHED AT LCQ. 2 L 7 2 4F 4 F RT A28NM E40NE 2008013100148 20080131 00148 NM 2008 1 31 SWAA080452 1 20080126 A 5753 6546434301 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED MV2 CHECK, FOUND LT WING INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2008013100158 20080131 00158 NM 2008 1 31 SWAA080458 1 20080127 A 5311 65C25228 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727C, STR 26L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008013100165 20080131 00165 NM 2008 1 31 SWAA080477 1 20080127 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 25R TO STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008013100166 20080131 00166 NM 2008 1 31 SWAA080476 1 20080127 A 5311 65C25230 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 25R TO STR 25L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008013100169 20080131 00169 NM 2008 1 31 SWAA080479 1 20080127 A 5311 6546554 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 27R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008013100178 20080131 00178 NM 2008 1 31 SWAA080466 1 20080127 A 3211 6546146 BOLT BOEING 737 7373G7 1384595 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND LT MLG BOTTLE BOLT CORRODED. REMOVED AND REPLACED BOTTLE BOLT PER MM. 2 L 7 2 4F RT A16WE 2008013100180 20080131 00180 NM 2008 1 31 SWAA080467 1 20080127 A 3350 20121 CHARGER BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER AND DIODE S PER MM. 2 L 7 2 4F RT A16WE 2008013100183 20080131 00183 NM 2008 1 31 SWAA080468 1 20080126 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 715SW 27849 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP AT ROW 20 DEF. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008013100184 20080131 00184 NM 2008 1 31 SWAA080471 1 20080127 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 756SA 27872 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008013100192 20080131 00192 NM 2008 1 31 SWAA080482 1 20080128 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 424, STR 17R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008013100194 20080131 00194 NM 2008 1 31 SWAA080484 1 20080128 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008013100195 20080131 00195 NM 2008 1 31 SWAA080483 1 20080128 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008013100199 20080131 00199 NM 2008 1 31 SWAA080502 1 20080128 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008013100201 20080131 00201 NM 2008 1 31 SWAA080501 1 20080128 A 5310 6547959 DOOR FRAME BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CORRODED AT NR 5 DOOR STOP. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008013100203 20080131 00203 NM 2008 1 31 SWAA080500 1 20080128 A 5315 6545834 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, RBL 1. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2008013100217 20080131 00217 NM 2008 1 31 SWAA080492 1 20080128 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 480, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008013100221 20080131 00221 2008 1 31 SWAA080494 4 20080128 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 788SA 30603 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008013100230 20080131 00230 EA 2008 1 31 TRAX200800094 1 20080115 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 843AS 7310 LEFT FS 640 BONDED SKIN DOUBLER WAS FOUND TO HAVE TWO CRACKS AS MARKED. COMPLIED WITH EC/TC REO 601R-53-61-2492. 2 L 7 2 4F RT A21EA 2008013100232 20080131 00232 EA 2008 1 31 TRAX200800096 1 20080115 A 2560 SIGN CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 EXIT SIGN MISSING AFT OF SVC DOOR. FLT 4425 DEL 42 MINS. 2 L 7 2 4F RT A21EA 2008013100233 20080131 00233 EA 2008 1 31 TRAX200800097 1 20080115 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 920EV 7810 CEILING 2ND FROM FRONT EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008013100237 20080131 00237 NM 2008 1 31 NOCA001 1 20080113 A 3350 767 LIGHT BOEING 757 75728A 1384976 NM EXTERIOR INOPERATIVE A NOCA K NONE O OTHER UK UNKNOWN 1 EA 15 752NA 28174 L-1 DOOR OUTSIDE EMERGENCY LIGHT DOESN'T ILLUMINATE. RELAMPED L1 EMERGENCY LIGHT, OPS CHECKS OK. 2 L 7 2 4F RT A2NM 2008013100240 20080131 00240 NM 2008 1 31 KCSA081025 1 20080118 A 5210 STRUCTURE BOEING 747 747209B 138489B NM R5 DOOR CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 R-5 DOOR FWD LOWER CORNER AROUND DOME NUT 2ND FROM CORNER. 2 L 7 4 4F RT A20WE 2008013100241 20080131 00241 NM 2008 1 31 KCSA081026 1 20080118 A 5312 SPLICE BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 BS 1480 BULKHEAD SPLICE BOLT HOLE LEFT NR 1 HAS A CRACK INDICATION. 2 L 7 4 4F RT A20WE 2008013100242 20080131 00242 NM 2008 1 31 KCSA081027 1 20080118 A 5312 SPLICE BOEING 747 747209B 138489B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 RIGHT BS 1480 BULKHEAD SPLICE FITTING, INNER SURFACE AROUND BOLT HOLE NR 7 DAMAGED AT STRINGER 33R. 2 L 7 4 4F RT A20WE 2008013100251 20080131 00251 SO 2008 1 31 C2XA08CL010 1 20080117 A 4930 4504616A FUEL CONTROL EMB 145 EMB145LR 3260212 SO APU LEAKING A C2XA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16963 145116 EWR FLIGHT 2756 - THE CREW REPORTED FUEL FUMES IN THE COCKPIT WHEN THE APU WAS STARTED AND SHUT DOWN. THE APU WAS MEL'E D CONTROL NR 137605. ON 1/18/08 CLE MAINTENANCE REMOVED AND REPLACED THE APU FUEL CONTROL ASSEMBLY P/N 4504616A, S/N 04 -02-63, AND THE APU FUEL FLOW DIVIDER P/N 4951486, S/N 0494 AND THE APU ANTI SURGE VALVE P/N 4950899, S/N 1206. OPERATI ONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008013000043 20080130 00043 NM 2008 1 30 QXEA200800042 1 20080123 A 2611 SMOKE DETECTOR BOMBDR DHC8 DHC8402 1390042 NM LAVATORY CONTAMINATED A QXEA O OTHER C N F.O.D. FALSE WARNING TX TAXI/GRND HDL 1 NM 09 425QX 4039 SEA - FLIGHT 2284 - LAVATORY SMOKE DETECTOR WENT OFF 6 TIMES. MAINTENANCE REMOVED DUST FROM THE SMOKE DETECTOR WITH A L IGHT BLAST OF NITROGEN. PERFORMED OPERATIONAL TEST WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPL ACED. 2 H 7 2 4T RT A13NM 2008013000074 20080130 00074 SO 2008 1 30 SIMA200802301 1 20080120 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG FAILED A SIMA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SW 21 939AE 14500923 ON FLIGHT 3869 - CREW DECLARED EMERGENCY DUE TO MOMENTARY LG AIR GND FAIL MESSAGE WHEN GEAR SELECTED DOWN. AIRCRAFT REM OVED FROM SERVICE. REMOVED AND REPLACED NOSE LANDING GEAR AIR GROUND PROXIMITY SWITCH IAW EMB 145 MM 32-63-02-000-801-A . OPS CHECK GOOD IAW 32-63-00-700-801-A. REMOVED AND REPLACED MAIN LANDING AIR/GROUND PROXIMITY SWITCH IAW 32-63-01-00 0-801-A. OPERATIONAL CHECK GOOD IAW EMB 145 MM 32-00-02-910-801-A. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008013000076 20080130 00076 NM 2008 1 30 08FDEA00241 1 20080123 A 5712 65172182 RIB BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 LT WING, FWD SPAR, STA 467, LE RIB, UPPER RADIUS CRACKED. REMOVED BLEED AIR DUCT TO GAIN ACCESS. REMOVE WEB AT STA 467 ON FWD SPAR. FABRICATED WEB REF BAC DWG 65-17218, HEAT TREATED ON FORM 8130-1 NR 2008-01-075, TREATED AND PRIMED AND I NSTALLED. REF SRM 51-10-2, SRM 51-30-2, RE INSTALLED BLEED AIR DUCT REF MM 36-00-001. THIS IS CLASSIFIED AS A MINOR RE PAIR. 2 L 7 3 4F RT A3WE 2008013000077 20080130 00077 2008 1 30 WGEA200800011 4 20080124 A 2297 CONNECTOR ECLIPS EA500 ECLIPSEEA500 3350000 SW CSP LOOSE E WGEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 139DJ 000054 AFTER LIFT OFF, ON GEAR RETRACTION, GOT FOLLOWING INDICATIONS: FULL STALL WARNING, AIRSPEED MISCOMPARE, STICK PUSHER FAI L, CAPT'S AIRSPEED APPEARED NORMAL, F/O'S AIRSPEED WAS INDICATING 10-15 KTS SLOWER AND MATCHED NR 3 AIRSPEED. STALL WAR NING CONTINUED TO TOUCHDOWN. AS PER PILOT THE 1ST OFFICERS DIGITAL READOUT WAS IN "RED" AND VARIED BETWEEN 120-115 KTS, AND STALL TAPE INDICATED UP TO 120 KTS, ALSO IN RED. SUPPLEMENTAL INFORMATION, INSPECTED CENTER SWITCH PANEL IAW EA 50 0 AMM 31-10-11. TIGHTENED CSP LT CONNECTOR 91A01P01 IAW EA 500 AMM 31-10-11. PERFORMED CSP TEST IAW EA 500 AMM 31-10-0 0. OP'S CHECK GOOD, NO DEFECTS NOTED. 1 L 7 2 4J RT A00002AC 2008013000079 20080130 00079 WP 2008 1 30 IXXA080003O 1 20080123 A 2697 CONNECTOR DOUG DC8 DC873F 302199F WP FIRE LOOP LOOSE A IXXA O OTHER N FALSE WARNING CR CRUISE 1 SW 11 603AL 98799 657 46003 DURING CRUISE FROM KTOL NUMBER THREE FIRE WARNING LIGHT STARTED TO FLICKER AND HORN SOUNDED. THE CREW TESTED NUMBER THR EE ENGINE FIRE WARNING NO BELL OR LIGHT, PERFORMED FIRE DAMAGED CHECK LIST PULL FIRE HANDLE FORWARD TEST FIRE WARNING TE STED GOOD ALL ENGINE PARAMETERS GOOD THE CREW SHUT DOWN ENGINE. THE CREW LANDED AT KMEM WITHOUT INCIDENT. MAINTENANCE INSPECTED NUMBER THREE ENGINE FIRE LOOP, NO ABNORMALITIES FOUND, CLEANED AND RECONNECTED FIRE LOOPS CONNECTORS, DEGREASE D SECTION OF LOOPS AS REQUIRED, ENSURE GOOD INSULATION ON ALL CONNECTION POINTS OPERATIONAL CHECK WAS GOOD IAW DC -8 MA INTENANCE MANUAL 26-10-1. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2008013000082 20080130 00082 2008 1 30 ANCF200800002 4 20080121 A 3420 ADI BOEING 767 7673Y0 NM COCKPIT FAILED W ANCF A UNSCHED LANDING O OTHER CL CLIMB 1 SO 23 948AV 24948 CAPT ADI IS BLANK. SELECTING ALT EFI DOES NOT CORRECT THE FAULT. REPLACED CAPT ADI AS PER AMM 34-22-00-601, CHECKS OK . IN ACCORDANCE WITH STANDARD WIRING PRACTICES MANUAL 20- 71-11 WAS REPLACED PINS 6, 7 AND 17 IN CONNECTOR D00107 CAP A DI ALSO FIM 34-22-0 0 FIG 104 BLOCKS 1, 2 AND 32 WAS ACCOMPLISHED OPERATIONAL CHECK SATISFACTORY. 2 L 7 2 4F RT A1NM 2008013000085 20080130 00085 2008 1 30 SIMA200802803 4 20080123 A 3400 UNKNOWN SAAB SF340 340B 7860101 EU COCKPIT MULTIPLE FAIL A SIMA O OTHER H ELECT. POWER LOSS-50 PC AP APPROACH 1 SW 21 253AE 340B253 ON FLIGHT 3006, CREW REPORTED DURING CRUISE AT 9000 FEET, THAT THEY WERE STRUCK BY LIGHTNING. CREW LOST BOTH EFIS SYSTE M, AUTOPILOT, AND MOST OF THE ALERTING SYSTEM. AFTER RESETTING BOTH GENERATORS CREW GOT ALL INDICATIONS BACK EXCEPT THE RT FUEL QUANTITY GAUGE. CREW DECLARED EMERGENCY. AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE WITHOUT FURTHER INCIDE NT. 2 L 7 2 4T RT A52EU 2008012900187 20080129 00187 NM 2008 1 29 2008UALA00228 1 20080115 A 5610 5717623096 WINDOW BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT CRACKED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 922UA 26642 RTFL DUE TO F/O'S SIDE CRACKED WINDOW. REPLACED WINDOW. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900189 20080129 00189 NM 2008 1 29 2008UALA00231 1 20080113 A 3350 362624 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 545UA 25323 DOOR 2L EXTERIOR EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012900194 20080129 00194 NM 2008 1 29 2008UALA00236 1 20080112 A 3350 276005 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 LEFT OVERWING EMERGENCY LIGHT FWD LAMP INOP. REPLACED FUSE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900197 20080129 00197 NM 2008 1 29 2008UALA00239 1 20080112 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT MALFUNCTIONED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHTS ON WITH C'PIT SW IN ARMED POSITION. RESET CB. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900198 20080129 00198 NM 2008 1 29 2008UALA00240 1 20080113 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 SEAT 4A FWD EMERGENCY LIGHT IS INOP. REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900201 20080129 00201 NM 2008 1 29 2008UALA00243 1 20080113 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 DOOR 5R FWD SILL EMERGENCY LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900205 20080129 00205 2008 1 29 2008UALA00249 4 20080112 A 2565 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 935UA 26663 DOOR 1L SLIDE PACK IS LAYING ON JET BRIDGE, NOT SECURED TO AIRCRAFT. REINSTALLED SLIDE PACK. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900220 20080129 00220 2008 1 29 USAA920080187 4 20080115 A 2210 C12850003108 COMPUTER AIRBUS A321 A321211 3930370 EU FLT CONTROLS ODOR A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 165US 22457 809 1431 FLT NR 1650, COCKPIT GLARESHIELD LIGHTING PANEL HAD AND ODOR OF ELECTRICAL HEAT AFTER ADJUSTING RHEOSTATS AREA FOR GLAR ESHIELD LIGHTING AND PULLED CB Z234 AND Y2345. FLIGHT LANDED WITHOUT INCIDENT AND NO EMERGENCY WAS DECLARED. CLT MAINT ENANCE REMOVED AND REPLACED THE FLIGHT CONTROL UNIT. FUNCTIONAL CHECK WAS NORMAL. 2 L 7 2 4F RT A28NM 2008012900231 20080129 00231 NM 2008 1 29 2008UALA00250 1 20080113 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 805UA 783 FOUND CORROSION BEYOND SRM LIMITS ON FLOORBEAM ITEMS 105, 170 & 175. MAJOR REPAIR ACCOMPLISHED AT DEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012800117 20080128 00117 SO 2008 1 28 FDKA200801031 1 20080117 A 7830 SKIN EMB 145 EMB145LR 3260212 SO THRUST REVERSER CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 834MJ 145340 THE O/B SIDE OF THE NR 1 THRUST REVERSER, EXTERNAL SKIN, BETWEEN THE UPPER AND LOWER BUCKETS IS DAMAGED. THE DAMAGE HAS BEEN REPAIRED. 2 L 7 2 4T RT T00011AT 2008012800162 20080128 00162 EU 2008 1 28 UPS08151408 1 20080113 A 5210 DOOR AIRBUS 300 A300F4605R 3930327 EU CREW ENTRY UNSECURE A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 138UP 0821 ATB - CREW ENTRY DOOR ECAM MESSAGE. A/C WAS SLOWLY LOSING PRESSURIZATION AND CREW WAS HEARING A LOUD SQUEAL. FLIGHT LA NDED WITH NO FURTHER INCIDENT. PERFORMED MAINTENANCE CHECK PER AMM A300-05-53-00-00. NO FAULTS NOTED. 2 L 7 2 4F RT A35EU 2008012900015 20080129 00015 SO 2008 1 29 C2XA08TY008 1 20080116 A 3350 1317 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18102 145643 TYS DURING A CURRENT A-CHECK INSPECTION A CABIN CEILING LIGHT WAS FOUND TO BE INOP. MAINTENANCE REMOVED AND REPLACED TH E LIGHT AND OPS CHECKS WERE GOOD. A/C PUT BACK IN SERVICE AT THE END OF THE CHECK. 2 L 7 2 4F RT 2008012900025 20080129 00025 SO 2008 1 29 RAIA00801018 1 20080115 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 815HK 145048 PRE FLT 5597 - EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE RESECURED WIRING TO THE FORWARD MOST LIGHTING STRIP. OPS CH ECK GOOD. 2 L 7 2 4T RT T00011AT 2008012900031 20080129 00031 NM 2008 1 29 2008UALA00181 1 20080110 A 5210 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 R1 DOOR EXTERNAL SKIN HAS A DENT BY LOWER HINGE ARM CUTOUT. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012900061 20080129 00061 NM 2008 1 29 2008UALA00197 1 20080110 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 WALL EEL INOP, UPPER DK STAIR WALL FWD SECT. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008013000106 20080130 00106 EU 2008 1 30 TRBA2008010 1 20080124 A 7930 810711100010AB TRANSMITTER AEROSP ATR72 ATR72212 8680945 EU LT ENG OIL PRESS FAILED A TRBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 29 426AT 426 AT 16000 HAD A SURGE RIGHT AFTER THE NR 1 OIL PRESS STARTS TO DROP AND THE OIL LOW LEVEL LIGHT CAME ON AND NO WARNING. THE NEEDLE DROPPED TO RED LINE BUT STILL NO WARNING CHIME, SHUT DOWN AS A PRECAUTION. REMOVED AND REPLACED LT ENG OIL P RESS TRANSMITTER IAW JIC 79-33-61. RUN-UP FOUND SATISFACTORY AND LEAK CK OK. 2 H 7 2 4T RT A53EU 2008013000116 20080130 00116 EU 2008 1 30 08FDEA00244 1 20080123 A 5522 SKIN AIRBUS 310 A310221 3930310 EU RT ELEVATOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 RT ELEVATOR APPROX STA 623 LOWER SKIN CORRODED. REPAIRED RT ELEVATOR LWR SKIN CORROSION BY REMOVING DAMAGED SKIN, AND F ABING SKIN PLUG AND DOUBLER, BONDING SKIN PLUG AND DOUBLER, EDGE SEALING REPAIR, AND REFINISHING IAW A310-200 SRM 51-77- 12 FIG 224. 2 L 7 2 4F RT A35EU 2008013000117 20080130 00117 EU 2008 1 30 MALA080007 1 20080109 A 5753 SKIN SAAB SF340 340B 7860101 EU TE FLAP CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 FLAP PANEL 641AT SKIN BENEATH NR 6 ANTI-CHAFE STRIP HAS AN AREA OF CHAFING/SCRATCHES. COMPLETED REPAIRS IAW EO NR S5717 2. 2 L 7 2 4T RT A52EU 2008013000119 20080130 00119 EU 2008 1 30 08FDEA00232 1 20080123 A 5522 SKIN AIRBUS 310 A310221 3930310 EU RT ELEVATOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 RT ELEVATOR APPROX STA 623 LOWER SKIN CORRODED. 2 L 7 2 4F RT A35EU 2008013000148 20080130 00148 NM 2008 1 30 DLM88080076 1 20080116 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 766 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 FOUND DENT ON LT CABIN CUSP WEB AT STA Y=766.5. REPAIRED IAW ERA 398191-14MA REV A. 2 L 7 2 4F RT A6WE 2008013000174 20080130 00174 NM 2008 1 30 08FDEA00256 1 20080124 A 5753 ARC198413 SUPPORT BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 FOUND CORROSION, LT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT INBOARD CENTER FASTENER HOLE. CORROSION REPAI RED AS PER EA 1-5750-117305, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008013000175 20080130 00175 NM 2008 1 30 08FDEA00257 1 20080124 A 5320 656725061 ANGLE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 CORROSION AT SEVERAL AREAS ON AFT WALL GILL LINER PANEL FRAME AT STA 1166 AROUND CAMLOC RECEPTACLE HOLES FRONT AND BACK SIDE. LOWER AFT CARGO COMPARTMENT REMOVED BULKHEAD SUPPORT ANGLE, IN REF TO SRM 51-30-2. VERIFIED MAT'L ID AS BAC 1506 -1707 7075-T6, A 84811 PO NR 10323033, REF DWG, 65-67250. FABRICATED NEW SUPPORT ANGLE IN REF TO SRM 51-30-5. INSTALLE D NEW SUPPORT ANGLE AND 5 RECEPTACLES IN REF TO SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008013000183 20080130 00183 NM 2008 1 30 DLM90080064 1 20080109 A 5280 SKIN DOUG MD90 MD9030 3023690 NM LT MLG DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 83528 53390 LMLG DOOR EXTERIOR SKIN CORRODED ALONG HINGE LINE. REPLACED LMLG DOOR. 2 L 7 2 4F RT A6WE 2008013100030 20080131 00030 WP 2008 1 31 UPS08851456 1 20080102 A 5320 FINGER DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 COCKPIT SUBFLOOR FINGER DOUBLER HAS 10EA POPPED RIVETS FROM CORROSION AT STA -32 TO -12 RBL 24. REMO VED CORROSION AT COCKPIT SUBFLOOR FINGER DOUBLER AT STA -32 TO -12 IAW SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUB LER AT STA -32 TO -12 RBL 24 IAW SRM 51-1-21 AND DWG 5612298. 2 L 7 4 4F RT 4A25 2008013100073 20080131 00073 SO 2008 1 31 RAIA00801019 1 20080116 A 3250 12302328407 TILLER EMB 145 EMB145LR 3260212 SO NLG STEERING FAULTY A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 838HK 145321 FLT 8036 - EWR - NOSE WHEEL STEERING GOES FULL DEFLECTION ERRATICALLY. NOT RESPONSIVE AFTER RESET AND THEN CAUSING HYDR AULIC BANGING NOISE FROM STEERING MANIFOLD WHENEVER TILLER IS DEPRESSED. MAINTENANCE REMOVED AND REPLACED TILLER. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008013100077 20080131 00077 SO 2008 1 31 RAIA00801022 1 20080119 A 2450 14521325407 CONTROL PANEL EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 830HK 145313 FLT 5576 - GSO - EMERGENCY LIGHTS NOT ARMED MESSAGE ON THE EICAS FOLLOWED BY AN EMERGENCY ABNORMAL MESSAGE. MAINTENANCE REMOVED AND REPLACED THE ELECTRICAL CONTROL PANEL. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008013100091 20080131 00091 NM 2008 1 31 SWAA080424 1 20080123 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 926, STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008013100134 20080131 00134 EU 2008 1 31 YENA2008011 1 20080121 A 5540 FITTING EMB ERJ190 ERJ190100IGW 3260408 EU RUDDER CRACKED A YENA O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 15 231JB 19000033 FLT 1264, AUS-BOS, AIRCRAFT REQUIRES EXCESSIVE RIGHT YAW TRIM AT HIGH SPEED. NEEDED 1/3 TO 1/2 RIGHT TRIM FOR COORDINATE D FLIGHT IN CRUISE. SEEMED TO TRIM BACK TO CENTER AT SLOW SPEED. ACFT IS CURRENTLY OUT OF SERVICE. REMOVED & REPLACED RUDDER PER EA E08-045 REVISION A PART 1, RUDDER RIGGING ACCOMPLISHED PER AMM 27-20-00, RUDDER BACKLASH PER AMM 27-20-00 -720-801-A/500 AND OPERATIONAL TEST OF THE RUDDER CONTROL SYSTEM PER AMM 27-20-00-710-801-A/500. ACCOMPLISHED CHECK FLT. ALL OPS CHECK OK. 2 L 7 2 4F RT A57NM 2008013100138 20080131 00138 NM 2008 1 31 SWAA080448 1 20080125 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 294WN 32540 EEPLS ASSY LOOSE AT ROW 1 ABC. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008013100139 20080131 00139 NM 2008 1 31 SWAA080449 1 20080124 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 700, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008013100140 20080131 00140 NM 2008 1 31 SWAA080470 1 20080124 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514B, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008012900103 20080129 00103 NM 2008 1 29 2008UALA00217 1 20080111 A 2560 G20213EFM SMOKE GOGGLES BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE COCKPIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 670UA 29240 F/O GOGGLES INOPERATIVE. SUSPECT BROKEN FROM PRE-FLIGHT CHECKS. REPLACED SMOKE GOGGLES. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900154 20080129 00154 NM 2008 1 29 ASAA0842483 1 20080115 A 5210 141A60752 GUIDE ARM BOEING 737 7374Q8 138447Q NM L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 762AS 25099 L1 DOOR IS DIFFICULT TO CLOSE. LENGTHENED FWD ENTRY DOOR GUIDE ARM (REF AMM52 11 00). LATCH OP CHECKS OK THIS DATE. 2 L 7 2 4F RT A16WE 2008012900158 20080129 00158 EU 2008 1 29 YENA2008003 1 20080112 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 608JB 2415 FLT 576, MCO-SWF, AT APPROX 15:00Z, F/A REPORTED STRONG BURNING RUBBER ODOR IN REAR OF A/C AND LAST TEN ROWS. RAN AIR C OND SYS AND UNABLE TO DUPLICATE ODOR OF ANY KIND. C/W AMM 24-00-00 STG 1 FOR AT LEAST 15 MINUTES, NO FAULTS. C/W TSM 2 4-00-00, NO ITEMS FOUND TO MEET CRITERIA OF SQUACK. 2 L 7 2 4F RT A28NM 20080912 WP 2008 9 12 UPS08853070 1 20080730 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 CRACKED FWD JAMB JUST ABOVE UPPER HINGE ON RT FWD SERVICE DOOR. BLENDED EDGE REMOVING CRACK IAW SRM 53-02-00, AND 51-01-08. 2 L 7 4 4F RT 4A25 20080912 WP 2008 9 12 UPS08853071 1 20080729 A 5755 SKIN DOUG DC8 DC871F 302199D WP NR 3 SPOILER GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 RT WING NR 3 SPOILER HAS TWO DEEP GOUGES AT LOWER SKIN AREA. REMOVED DAMAGE IAW SRM 51-01-09A. FABR ICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-07-01 AND 51-01-09A. 2 L 7 4 4F RT 4A25 20080912 2008 9 12 UPS08853075 4 20080812 A 3440 INU DOUG DC8 DC871F 302199D WP NR 1 FAILED A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 718UP 46018 INSPECTION TYPE:N/A EN ROUTE - CAPTAIN'S INS WARNING LIGHT ON EADI AND EHSI - LOST MULTIPLE SYSTEMS. CREW DECLARED EMER GENCY AND LANDED UNEVENTFULLY. REMOVED AND REPLACED NR 1 INU IAW MM 34-44-03. ADJUSTMENT TEST DUE. NR 1 INU CHECKS OK IN REF TO AMM 34-44-03. 2 L 7 4 4F RT 4A25 20080915 WP 2008 9 15 08FDEA03002 1 20080721 A 5730 ARC0267504 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 RIGHT WING T/E PANEL 641 BB HAS CORROSION AROUND FASTENER HOLES. REMOVED THE CORROSION IAW SRM 51-21-01; PG 28; VOL II. ORIGINAL MATERIAL 0.032 IAW SRM 57-32-01; FIG 2; VOL III. MATERIAL LOSS 0.010. REMAINING MATERIAL 0.022. FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01; FIG 1-A; VOL I. LOCATED AND DRILLED THE NEW PANEL P/N ARC 0267-504, PO 627171.2 IA W SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 20080915 WP 2008 9 15 08FDEA03003 1 20080721 A 5730 ARC0267503 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING T/E PANEL 541 BB IS WORN. BLENDED PANEL 541 BB IAW DC/MD-10 SRM 57-00-01; FIG 1-A; VOL I. FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-00-01; FIG 1-A; VOL I AND SRM 57-32-01; VOL I. LOCATED AND DRILLED HOLES IAW DC/MD-10 SRM 5 1-31-01, VOL II. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 08FDEA03149 1 20080730 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL PANEL ACCESS CUTOUT 542CB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIE D AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080915 WP 2008 9 15 08FDEA02960 1 20080717 A 5753 ARC0794509 PANEL DOUG MD10 MD1010F 3022112 WP LT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING OUTBD FLAP PANEL 535 AR HAS SEVERAL DENTS. REPAIRED DENTS IN THE LT WING OUTBD PANEL 535 AR WITH REPAIR DOUBL ERS IAW SRM 51-71-00; VOL II. 2 L 7 3 4F RT A22WE 20080915 WP 2008 9 15 08FDEA03170 1 20080730 A 5730 RB0975536 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 RIGHT WING FUEL PANEL 636 BB IS PITTING ON THE MATING SURFACES. FABRICATED A NEW FUEL PANEL IAW SRM 57-10-00; VOL I AND DWG ARB 0975-536, REV AY. 2 L 7 3 4F RT A22WE 20080915 WP 2008 9 15 08FDEA02961 1 20080717 A 5730 ARC07951 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING FAIRING PANEL 535BL HAS NUMEROUS DENTS. REPAIRED DENTS IN THE LEFT WING FAIRING PANEL 535 BL WITH REPAIR DOUB LERS IAW SRM 51-71-00; VOL II. 2 L 7 3 4F RT A22WE 20080915 EU 2008 9 15 08FDEA03178 1 20080730 A 5347 A5378193720100 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CABIN CROSS SEAT TRACK AT FRAME 28, LBL 35 IS CRACKED. REMOVED CROSS SEAT TRACK AT FRAME 28, RBL 35 IAW SRM 51-40- 21, PARA 7. DRILLED AND COUNTERSUNK HOLES FOR THE NEW CROSS SEAT TRACK ADAPTER P/N A5378193720100, PO 627374.2 IAW SRM 51-40-21, PARA 7. APPLIED CIC IAW AMM 51-22-00-0. 2 L 7 2 4F RT A35EU 20080915 WP 2008 9 15 08FDEA02904 1 20080715 A 5330 ADA31391 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 DENT AND GOUGE ON THE FUSELAGE SKIN APPROX FS 840 AT LONGERON 38 L. BLENDED OUT GOUGE PER SRM 53-00-01; FIG 1-A; SHEET 3; VOL I. ORIGINAL THICKNESS 0.068 PER SRM 53-33-01; FIG 1; VOL III. REMAINING THICKNESS IS 0.045. MAT REMOVED 0.023. AREA IS OUT OF LIMITS PER SRM 53-00-01; FIG 1-A; SHEET 3; VOL I. REMOVED DAMAGED AREA IAW SRM 53-20-00; FIG 6; VOL I. INSTALLED REPAIR PARTS REF SRM 53-20-00; VOL I; PGS 84 A, B, C. 2 L 7 3 4F RT A22WE 20080915 WP 2008 9 15 08FDEA03098 1 20080728 A 5230 AUB71321 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 100 WORN A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 372FE 46610 MAIN CARGO DOOR JAMB AT SPOOL FITTING NR 4; HOLE "D" IS OVERSIZED TO 0.519. VERIFIED HOLE "D" TO BE .5192 MEASURED WITH TOOL NR T8723K; MATERIAL ID FOR 3 EA FREEZE PLUGS FOR 4-"D" IS 7075-T6 AC BAR, PO 529774.6. FABRICATED AND LOCATED HOL E IAW SRM 53-50-00, VOL I, PG 81. FINAL HOLE SIZE 0.453.5. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 08FDEA03150 1 20080730 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL ACCESS PANEL CUTOUT 542AB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIE D AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008013100150 20080131 00150 NM 2008 1 31 SWAA080453 1 20080125 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 441WN 29837 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACKS FAIL LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008013100156 20080131 00156 NM 2008 1 31 SWAA080457 1 20080127 A 5311 6546596 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008013100159 20080131 00159 NM 2008 1 31 SWAA080459 1 20080127 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008013100171 20080131 00171 NM 2008 1 31 SWAA080460 1 20080126 A 5610 5717623122 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 651SW 27721 FLIGHT DECK R2 WINDOW ARCING. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2008013100189 20080131 00189 EU 2008 1 31 2008UALA00276 1 20080116 A 5250 AR47091 CONTROLLER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT DOOR FAULTY A UALA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CR CRUISE 1 WP 29 408UA 457 FLIGHT DIVERTED DUE FLIGHT DECK DOOR LOCK CYCLING OPEN, DOOR NOT SECURE. FAULT LIGHT ILLUMINATED. DOOR CONTROLLER MALF UNCTION. REPLACED DOOR CONTROLLER. 2 L 7 2 4F 4 F RT A28NM E40NE 2008013100215 20080131 00215 NM 2008 1 31 SWAA080493 1 20080128 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, STR 28L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008013100274 20080131 00274 NE 2008 1 31 VNAA0801006 2 20080120 A 7230 CF343B1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RIGHT FAILED A VNAA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 GL 05 209PS 9507 7874 CREW REPORTED A SMOKE TOILET CAUTION MESSAGE 5 SECONDS AFTER TAKEOFF. CREW ELECTED TO RETURN TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE RIGHT HAND ENGINE. MAINTENANCE FOUND EXTERIOR OIL LEAKAGE A T STAGES 2-5 OF THE COMPRESSOR ON OUTBOARD SIDE OF THE ENGINE. MAINTENANCE PERFORMED A BORESCOPE INSPECTION AND FOUND O IL ON STAGE 2 AND 3 VG VANES AND BLADES. MAINTENANCE REMOVED AND REPLACED THE ENGINE IN ACCORDANCE WITH THE AIRCRAFT MA INTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008013100293 20080131 00293 CE 2008 1 31 SBAA200800001 1 20080122 A 2435 200SGL119Q2RX STARTER GEN CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE MCAULY 3AF34C 3GFR34C703 GL ENGINE INOPERATIVE E SBAA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION AP APPROACH 1 GL 09 858FE 789 789 208B0178 19388 0222891 AIRCRAFT WAS ON A NORMAL SCHEDULED AM FLIGHT. AIRCRAFT WAS ON APPROACH ABOUT 8 MILES FROM AIRPORT WHEN GENERATOR FELL OF F LINE AND WOULD NOT RESET. STANDBY POWER SYSTEM PICKED UP ELECTRICAL LOAD AS DESIGNED AND AIRCRAFT LANDED AT WITHOUT F URTHER INCIDENT. STARTER/GENERATOR WAS REPLACED WITH OVERHAULED UNIT. OPERATIONAL TEST NORMAL. 1 H 7 1 3T 3 T A37CE E4EA 5 C P60GL 2008013100302 20080131 00302 EA 2008 1 31 A6WA200840012 1 20080114 A 2910 13E415 COOLER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE HYD SYSTEM VIBRATION A A6WA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 GL 31 466AW 18484 7289 AIRFRAME VIBRATION FELT AF VIBES FELT FROM T/O, TO DESCENT , WENT AWAY ON FINAL APPROACH. FELT IN REAR ON LT SIDE OF TH E AC EVIDENT AT ROW 13 BUT NOT EVIDENT IN LAV. REMOVE AND REPLACED HYDRAULIC COOLER REF AMM 29-11-42, OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008013100306 20080131 00306 SO 2008 1 31 SWIA200819083 1 20080108 A 5210 DOOR EMB 120 EMB120ER 3260203 SO MAIN PAX LACK OF LUBE A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 567SW 120342 FLT 3676 - FLIGHT ATTENDANT REPORTS DOOR IS HARD TO OPEN AND CLOSE. INSPECTED, CLEANED AND LUBRICATED THE DOOR. NO DEF ECTS NOTED. 2 L 7 2 4T RT A31SO 2008013100309 20080131 00309 NM 2008 1 31 DLM88080087 1 20080116 A 7120 K22199SA32 ISOLATOR DOUG MD88 MD88 3023688 NM LT ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 RUST ON AFT VIBRATION ISOLATOR AT LT ENGINE. VIBRATION ISOLATOR REPLACED AND WILL BE INSTALLED WITH OPN 7151 RC 805. 2 L 7 2 4F RT A6WE 2008013100310 20080131 00310 NM 2008 1 31 DLM88080088 1 20080116 A 5514 CHANNEL DOUG MD88 MD88 3023688 NM HORIZONTAL STAB DEFORMED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 DEFORMED "C" CHANNEL ON RT HORIZONTAL STABILIZER REAR SPAR AT STA XHS=207. INSTALLED NEW "C" CHANNEL IAW SRM 51-30-2, S RM 51-30-5 AND DOUGLAS DWG 9918401. 2 L 7 2 4F RT A6WE 2008013100311 20080131 00311 NM 2008 1 31 DLM88080089 1 20080116 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM PAX CABIN CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 EXFOLIATION CORROSION ON RT CUSP WEB AT PAX CABIN STA Y=507 TO 508. REPAIRED CUSP WEB IAW ERA 398191-14MA REV A. 2 L 7 2 4F RT A6WE 2008013100313 20080131 00313 NM 2008 1 31 DLM88080091 1 20080116 A 5347 SEAT TRACK DOUG MD88 MD88 3023688 NM BS 1141-1168 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 EXFOLIATION CORROSION ON LT GENERATION FLOOR SUPPORT AT STA 1141, 1168. INSTALLED NEW SECTION OF TRACK IAW SRM 53-05D F IG 4F. 2 L 7 2 4F RT A6WE 2008013100315 20080131 00315 NM 2008 1 31 DL757080093 1 20080118 A 2750 OIL SYSTEM BOEING 757 757232 1384965 NM FLAP TRANMISSION LOW A DALA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 SO 27 621DL 22911 ON APPROACH INTO LGA AS WE WERE CONFIG FROM 20 TO 25 FLAPS, TE FLAP DISAGREE EICAS MSG. PERFORMED NON-NORMAL CHECKLIST AND AFTER SELECTING 20 WITH ALT SW POSITION AND ALTN SELECTED FOR POWER TE CAUTION LIGHT WENT OUT. LANDED AT JFK WITH 20 FLAPS. T/S PER FIM 27-51-00, NO FAULTS NOTED. DURING TE FLAP DRIVE TX INSPECTION FOUND OIL LEVEL LOW AT RT WING 2 O B TXS LOW. SVCD SAME AND PERFORMED TE FLAP TX SYS LUBE. OPS NORM, NO FAULTS. 2 L 7 2 4F RT A2NM 2008013100318 20080131 00318 NM 2008 1 31 DL764080101 1 20080119 A 3350 CHARGER BOEING 767 767432ER 1385134 NM BS 841 LBL 94 INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 825MH 29696 BATTERY CHARGER M6759 STA 841 LBL 94 LIGHTS INOP AFTER 5 MINUTES. REMOVED AND REPLACED BATTERY CHARGER DURING HMV 1 AT TIMCO AT GSO ON NR 44973. 2 L 7 2 4F RT A1NM 2008013100320 20080131 00320 NM 2008 1 31 DL764080103 1 20080119 A 3350 CHARGER BOEING 767 767432ER 1385134 NM BS 1384 RBL 95 INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 825MH 29696 BATTERY CHARGER M734 STA 1384 RBL 95 LIGHTS INOP AFTER 5 MINUTES. REMOVED AND REPLACED BATTERY CHARGER M734 ON NR 44975 , DURING HMV 1 AT TIMCO IN GSO. 2 L 7 2 4F RT A1NM 2008013100325 20080131 00325 NE 2008 1 31 DL76G080109 2 20080117 A 7220 VANE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 ENGINE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1604R 36753 30180 704736 NR 1 ENGINE REPLACED DUE TO VSV WEAR. 2 L 7 2 4F 4 F RT A1NM E13NE 2008013100328 20080131 00328 EU 2008 1 31 08FDEA00262 1 20080124 A 4900 GTCP331250H APU AIRBUS 300 A300F4605R 3930327 EU APU BAY FIRE A FDEA F ACTIVATE FIRE EXT. F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 SO 25 670FE 777 AT TOUCHDOWN, APU FIRE LIGHT, AGENT AUTO FIRED. APU FIRE HANDLE PULLED. APU MASTER SW WAS OFF AND APU WAS NOT ON/RUNNI NG. UPON FURTHER INVESTIGATION, DISCOVERED EVIDENCE OF A FIRE IN THE APU COMPARTMENT. PLUG P18 FROM THE MONOPOLE ASSY IS MELTED AND BURNED. THE MONOPOLE ASSY C/P IS BLOWN APART AND BURNED. NUMEROUS WIRE BUNDLES ON APU HARNESS ARE BURNED AND SCORCHED. REMOVED AND REPLACED APU FIRE EXTINGUISHER BOTTLE. INSPECTED AREA FWD OF APU COMPT, THRU ACCESS DOOR 31 3AL, NO VISIBLE SIGNS OF HEAT OR FIRE DAMAGE, NO VISIBLE BLISTERING. REMOVED & REPLACED APU. SEE ALSO EA 6-4912-113204 FOR ADDITIONAL WORK C/W. 2 L 7 2 4F RT A35EU 2008013100330 20080131 00330 NM 2008 1 31 DLM88080094 1 20080119 A 4990 OIL SYSTEM DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE APU LEAKING A DALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 927DA 15972 49714 P80123 SMOKE IN CABIN, FOUND APU OIL LEAKING INTO APU INLET. FOUND OIL LEAK AT ATTA POINTS FOR OIL FILL/SIGHT GLASS, SECURED B OLTS THAT WERE FOUND LOOSE AND REPLACED OIL CAP. LEAK CKS OK REF ITEM 004 NEXT LOG PAGE FOR DUCT BURN OUT OPERATION. 2 L 7 2 4F 4 F RT A6WE E9NE 2008013100334 20080131 00334 NM 2008 1 31 DL75E080112 1 20080124 A 5330 143N3691 SKIN BOEING 757 7572Q8 1384972 NM BS 665 S19R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 713TW 28173 DURING THE WINGLET MOD AT SAA, A GOUGE WAS FOUND IN THE FUSELAGE SKIN AT STA 665, BETWEEN S-19R AND S-20R. THE DAMAGE W AS REPAIRED PER BOEING INSTRUCTIONS. 2 L 7 2 4F RT A2NM 2008013100338 20080131 00338 NM 2008 1 31 08FDEA00265 1 20080124 A 5414 311N504634 PANEL BOEING 757 7572B7 1384964 NM NR 1 NACELLE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 NR 1 NACELLE STRUT I/B SKIN PANEL ASSY PN: 311N5046-34 HAS AREAS OF CORROSION C/M TO THE INNER SKIN SURFACE BETWEEN PP S TA 153.9 AND PP 176 REMOVED CORROSION IAW SRM 54-50-01. ORIGINAL MATERIAL THICKNESS, 0.090", AFTER CORROSION REMOVAL, 0.063" AT PP STA 159, 0.019" AT PP STA 176. THIS IS OUT OF SRM 54-50-01 DETAIL V, FIG 101, SHEET 4 LIMITS. REMOVED AN D REPLACED I/B SKIN PANEL IAW DRAWING 757-311N5002, SHEET 14, SRM 51-40-02 AND BOEING SB 757-54-0035. 2 L 7 2 4F RT A2NM 2008013100339 20080131 00339 EU 2008 1 31 08FDEA00266 1 20080117 A 5310 CROSSBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 CROSSBEAM OF FR 54.3 CRACKED AT Y-680. 2 L 7 2 4F RT A35EU 2008013100342 20080131 00342 EU 2008 1 31 08FDEA00274 1 20080111 A 5330 SKIN AIRBUS 310 A310222 3930315 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 FUSELAGE LWR LOBE, FUSELAGE SKIN WITH SCRATCHES ON THE EDGE OF FR 20A - FWD CARGO COMPARTMENT DOOR FWD FRAME. FUSELAGE SKIN SURFACE REPAIRED IAW EA 6-5330-117222. 2 L 7 2 4F RT A35EU 2008013100343 20080131 00343 EU 2008 1 31 08FDEA00275 1 20080125 A 7120 A54612406601 MOUNT AIRBUS 300 A300F4605R 3930327 EU NR 1 ENGINE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 685FE 803 NR 1 ENGINE FWD MOUNT FITTING AFT UPPER I/B AND O/B HOLES HAVE A 2.5 SQ INCH AREA OF CORROSION EACH AT RECESS DIAMETERS AND AROUND UPPER SURFACE WORKED LEVEL 1 CORROSION ON NR 1 ENGINE FWD MOUNT HOLES AND REMOVED CORROSION AND REPAIRED IA W FED-EX EA NR 6-5450-118038, RELEASE DATE 4 JANUARY 2008. 2 L 7 2 4F RT A35EU 2008013100344 20080131 00344 WP 2008 1 31 08FDEA00276 1 20080125 A 5322 ADA00107 SHEAR TIE DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 FWD PIT AT STA.808 BETWEEN STRINGER 34R AND 35R SHEAR TIE DAMAGED ON RADIUS. REMOVED, FABRICATED AND INSTALLED SHEAR TI E PER DC/MD10-10 SRM 53-13-01 VOL III FIG 8A AND 53-30-00 VOL I FIG10 AND 53-30-00 VOL I PAGE 34 FIG 9. 2 L 7 3 4F RT A22WE 2008013100345 20080131 00345 NM 2008 1 31 08FDEA00277 1 20080125 A 5730 6524953 SKIN BOEING 727 727233 138408A NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 CRACK IN UPPER RIGHT WING OUTBD PANEL AT WBL 602.5, OF OUTBD AILERON REPAIRED UPPER WING OUTBD. PANEL AT WBL 602.5 REF EA NR 7-5720-113964. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008020100010 20080201 00010 NM 2008 2 1 CALA0800031 1 20080119 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 FUSELAGE FRAME IS CRACKED STATION 747 BETWEEN STRINGERS 8R AND 9R. INSTALLED REPAIR ANGLES ON FRAME AT STA 747 STRINGER 8R AND 9R PER ECRA 5310-04691. 2 L 7 2 4F RT A16WE 2008013100089 20080131 00089 2008 1 31 SWAA080423 4 20080123 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008013100094 20080131 00094 NM 2008 1 31 SWAA080426 1 20080123 A 5311 6546526 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008013100105 20080131 00105 NM 2008 1 31 SWAA080435 1 20080124 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008013100107 20080131 00107 NM 2008 1 31 SWAA080442 1 20080124 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 291, STR 14R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008013100147 20080131 00147 NM 2008 1 31 SWAA080451 1 20080126 A 5743 6567172 FITTING BOEING 737 7373H4 1384600 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED MV2 CHECK, FOUND RT MLG WALKING BEAM OUTBOARD FWD STABILIZER FITTING CORRODED. REMOVED AND REPLACED FI TTING PER SRM. 2 L 7 2 4F RT A16WE 2008013100177 20080131 00177 NM 2008 1 31 SWAA080465 1 20080127 A 3211 6546146 BOLT BOEING 737 7373G7 1384595 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND RT MLG BOTTLE BOLT CORRODED. REMOVED AND REPLACED BOTTLE BOLT PER MM. 2 L 7 2 4F RT A16WE 2008013100213 20080131 00213 NM 2008 1 31 SWAA080489 1 20080128 A 5330 6545765 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506, STR 17L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008013100227 20080131 00227 EA 2008 1 31 VNAA0801008 1 20080122 A 4990 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE APU LOW A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 05 202PS 7858 CREW REPORTED ON TAXI-OUT AN APU AUTO SHUTDOWN. CREW ELECTED TO RETURN TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSP ECTED AND DEFERRED THE APU PER MEL 49-10-01-1. MAINTENANCE PROPERLY SERVICED THE APU OIL LEVEL IN ACCORDANCE WITH THE A IRCRAFT MAINTENANCE MANUAL. OPS CHECKS OF THE APU WERE GOOD, NO DEFECTS WERE NOTED. MEL WAS CLEARED. AIRCRAFT WAS REL EASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008013100238 20080131 00238 NM 2008 1 31 NOCA002 1 20080113 A 3350 767 LIGHT BOEING 757 75728A 1384976 NM EXTERIOR INOPERATIVE A NOCA K NONE O OTHER NR NOT REPORTED 1 EA 15 752NA 28174 R-4 DOOR OUTSIDE EMERGENCY LIGHT DOESN'T ILLUMINATE. RELAMPED L1 EMERGENCY LIGHT, OPS CHECKS OK. 2 L 7 2 4F RT A2NM 2008013100239 20080131 00239 NM 2008 1 31 KCSA081024 1 20080118 A 5210 FRAME BOEING 747 747209B 138489B NM R5 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 R-5 DOOR HAS A 2 INCH CRACK FWD OF LOWER CORNER VERTICAL FRAME AT RADIUS. 2 L 7 4 4F RT A20WE 2008013100324 20080131 00324 NM 2008 1 31 DL76S080108 1 20080122 A 5315 FLOORBEAM BOEING 767 767332 1382001 NM BS 880 MISINSTALLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 121DE 23435 DURING AN IFE MOD AT BFM, AN EXISTING FLOORBEAM SPLICE REPAIR WAS FOUND TO BE INSTALLED INCORRECTLY. THE REPAIR WAS REM OVED AND A NEW SPLICE REPAIR WAS INSTALLED. 2 L 7 2 4F RT A1NM 2008013100332 20080131 00332 NM 2008 1 31 DLM88080096 1 20080120 A 3320 BALLAST DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE CABIN LIGHTS BURNED OUT A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 971DL 53214 725878 FLIGHT ATTENDANT REPORTED SMELLING SMOKE IN THE MID CABIN. OVERHEAD LIGHT AT 20ABC FLICKERED THEN WENT OUT FOLLOWED BY ODOR. DISCOVERED BALLAST AT 20ABC HOT. PULLED AND COLLARED C/B FOR LT O/H LIGHTS. C/W OPN 5088. FWD LIGHT TO MCO/PLA C PER MEL 33-00-02. REPLACED BALLAST CKS, OK MCO/PLAC REMOVED. 2 L 7 2 4F 4 F RT A6WE E9NE 2008013100337 20080131 00337 2008 1 31 DL76L080116 4 20080125 A 3440 IRU BOEING 767 767332 1382001 NM FAULTED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 192DN 28449 AFTER TAKEOFF, CREW REPORTS ALL IRU SYSTEMS SHOW 10NM ERROR DIVERT TO REALIGN IRU-S. SWAPPED RIGHT IRS WITH CENTER IRS, REALIGNED ALL IRUS. ALL INDICATIONS NORMAL NOW. RIGHT IRU INOP. PER MEL 34-21-01C. 2 L 7 2 4F RT A1NM 2008013100348 20080131 00348 EA 2008 1 31 SWIA200819092 1 20080121 A 3350 RELAY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS MALFUNCTIONED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 744SK 10200 FLT 6510 - EMERGENCY LIGHTS CYCLE ON AND OFF DURING FLIGHT. REPLACED RELAY K135 IN JB-11 ON PCB-5. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008013100360 20080131 00360 EU 2008 1 31 NSVA2008001 1 20080123 A 2612 WARNING LIGHT SAAB SF340 340B 7860101 EU RT FIRE LOOP FALSE INDICATION A NSVA O OTHER N FALSE WARNING CR CRUISE 1 EA 27 249CJ 340B249 R FIRE DET FAIL LIGHT ON CWP ON INTERMITTENTLY IN FLIGHT COME ON 7 TIMES, GOING OUT EACH TIME AFTER 10-15 SEC. OPENED R T COWL INSP FIRE LOOP ASSY AND HARDWARE. NO FAULTS FOUND, PERFORMED FIRE DETECTION TEST SYSTEM. OPS CHK NORMAL IAW SAA B AMM 26-13-00. 2 L 7 2 4T RT A52EU 2008020100007 20080201 00007 NM 2008 2 1 CALA0800028 1 20080118 A 5310 6547960 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 AFT BAG BIN DOOR CUTOUT AFT FRAME CRACKED AT LOWER STOP PAD. REPLACED FRAME PER EA 5310-04443, BAC DRAWING 65-47960 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020100020 20080201 00020 NM 2008 2 1 HNAA0800026 1 20080109 A 5220 82520335013 PANEL DHAV DHC8 DHC8102 2809003 NM EMERGENCY EXIT MISALIGNED A HNAA O OTHER O OTHER UK UNKNOWN 1 EA 07 937HA 48275 48275 148 FLOOR LEVEL EMERGENCY EXIT AT ROW 1 DF IS DIFFICULT TO OPEN. STRAIGHTENED THE FORWARD TRIM STRIP ON THE INTERIOR PANEL ON THE FORWARD EMERGENCY EXIT DOOR, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2008020100025 20080201 00025 NM 2008 2 1 KCSA081035 1 20080122 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 INTERNAL FUSELAGE SKIN CORRODED AT BS 1484 ABOVE STR 7L. 2 L 7 4 4F RT A20WE 2008020100026 20080201 00026 NM 2008 2 1 KCSA081036 1 20080122 A 5347 SEAT TRACK BOEING 747 747209B 138489B NM FUSELAGE BROKEN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 BS 2100 RBL 12 SEAT TRACK FLANGE BROKEN. 2 L 7 4 4F RT A20WE 2008020100029 20080201 00029 NM 2008 2 1 CALA0800036 1 20080119 A 3350 1010428 LIGHT BOEING 737 737724 13844BY NM CABIN SHORTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 21723 28790 STOWAGE BIN BULLNOSE EMERGENCY LIGHTS AT 1AC AND 2AC INOP. REPLACED F4 FUSE FOR BATTERY CHARGER M1675 AND REPLACED SHOR TED LIGHT ASSY AT SEAT 3AC. 2 L 7 2 4F RT A16WE 2008020100031 20080201 00031 NM 2008 2 1 CALA0800038 1 20080119 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 FUSELAGE FRAME CRACKED AROUND RIVET AT STATION 867 ABOVE STRINGER 9L. INSTALLED REPAIR ANGLES ON FRAME PER CERA 5310-04 691. 2 L 7 2 4F RT A16WE 2008020100032 20080201 00032 NM 2008 2 1 CALA0800039 1 20080119 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 FUSELAGE FRAME CRACKED AROUND RIVET AT STATION 827 ABOVE STRINGER 9L. INSTALLED REPAIR ANGLES ON FRAME PER ECRA 5310-04 691. 2 L 7 2 4F RT A16WE 2008020100034 20080201 00034 NM 2008 2 1 CALA0800041 1 20080119 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 FUSELAGE FRAME CRACKED AROUND RIVET AT STATION 787 ABOVE STRINGER 9L. INSTALLED REPAIR ANGLES ON FRAME PER ECRA 5310-04 691. 2 L 7 2 4F RT A16WE 2008020100039 20080201 00039 NM 2008 2 1 CALA0800046 1 20080119 A 5514 6547500155 FITTING BOEING 737 737524 1384721 NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 LEFT HORIZONTAL STAB FORWARD UPPER LUG HAS CORROSION AT BUSHING'S (FORWARD AND AFT). REMOVED BUSHINGS AND SLEEVE, CLEAN ED CORROSION AND INSTALLED NEW SLEEVE AND BUSHINGS PER SRM 55-10-10 REF ECRA 5510-01911. 2 L 7 2 4F RT A16WE 2008020100045 20080201 00045 NM 2008 2 1 CALA0800054 1 20080120 A 5320 6546595224 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76354 23592 STRAP DAMAGE UNDER AFT CARGO FLOORBOARD AT FRAME LOWER SURFACE STATION 727A LBL16. STRAP FOUND TO BE DAMAGED BEYOND REP AIR. INSTALLED NEW STRAP AT STATION 727A BL 0 TO LBL 16 AND RBL 22 PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020100048 20080201 00048 NM 2008 2 1 CALA0800057 1 20080107 A 5320 6545875U45 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76354 23592 R-1 ENTRY DOOR Z-ANGLE CORRODED FROM STA 294 TO STA 328 AT FLOOR LEVEL WL 207.5. REMOVED AND REPLACED PER SRM 51-40-2. 2 L 7 2 4F RT A16WE 2008020100057 20080201 00057 NM 2008 2 1 CALA0800065 1 20080106 A 3350 312BS1011 CHARGER BOEING 737 737824 13844BZ NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 24211 28771 EMERGENCY LIGHT RT AFT LOWER FUSE INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER. 2 L 7 2 4F RT A16WE 2008020100059 20080201 00059 NM 2008 2 1 CALA0800067 1 20080120 A 5330 6545775 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76354 23592 FUSELAGE SKIN CRACK AT BS 764 JUST ABOVE AND ADJACENT TO LAP AT STRINGER 25R. TRIMMED OUT DAMAGE, FABRICATED REPAIR, RE PAIRED SRM 53-00-01. 2 L 7 2 4F RT A16WE 2008020100065 20080201 00065 EA 2008 2 1 TRAX200800121 1 20080121 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 933EV 8022 DURING APPROACH TO (KBOS) REC'D "FLAPS FAIL" CAUTION MESSAGE WHEN SELECTING FLAPS TO "8" DEGREES, FLAP INDICATIONS ARE " 0" DEGREES. EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION. 2 L 7 2 4F RT A21EA 2008020100067 20080201 00067 EA 2008 2 1 TRAX200800129 1 20080122 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 916EV 7757 ASD EXTERNAL HANDLE CRACKED. 2 L 7 2 4F RT A21EA 2008020100070 20080201 00070 NM 2008 2 1 KCSA081041 1 20080125 A 5311 FRAME BOEING 747 747209B 138489B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 RIGHT FRAME AT STA 2674.85 APROX WL 304 FASTENERS HAVE ELONGATED HOLES ON FRAME STIFFENER. 2 L 7 4 4F RT A20WE 2008020100074 20080201 00074 NM 2008 2 1 CALA0800074 1 20080127 A 5320 6546554 SUPPORT ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 CORROSION ON SUPPORT ANGLE AT STA 847 RBL 8 TO RBL 4. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-40-02 AND SRM 51-70 -11. 2 L 7 2 4F RT A16WE 2008020100075 20080201 00075 NM 2008 2 1 CALA0800075 1 20080127 A 5230 6549889 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FORWARD CARGO DOOR SKIN CRACKED AT EXTERIOR HANDLE CUTOUT MARKED. INSTALLED DOUBLER, SEALED AND PAINTED PER SRM 52-00-0 1. 2 L 7 2 4F RT A16WE 2008020100077 20080201 00077 NM 2008 2 1 CALA0800077 1 20080127 A 5330 654576659 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FUSELAGE SKIN HAS A 2.5 INCH CRACK AT STA 500+16 STRINGER 12L. INSTALLED REPAIR PER ECRA 5331-01385. 2 L 7 2 4F RT A16WE 2008020100078 20080201 00078 NM 2008 2 1 KCSA081044 1 20080129 A 5315 FLOORBEAM BOEING 747 747209B 138489B NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 AFT PIT FLOORBEAM UPPER T-CHORD DENTED AT BS 1780, RBL 51. 2 L 7 4 4F RT A20WE 2008020100080 20080201 00080 NM 2008 2 1 KCSA081046 1 20080129 A 5311 FRAME BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FWD PIT FUSELAGE CIRCUMFERENTIAL FRAME UPPER CHORD CRACKED AT BS 840 ABOVE STR 40L. 2 L 7 4 4F RT A20WE 2008020100081 20080201 00081 NM 2008 2 1 KCSA081047 1 20080129 A 5511 STRINGER BOEING 747 747209B 138489B NM HORIZ STAB CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 HORZ STAB CENTER SECTION LOWER STR 9 CORRODED AT RBL 14.5. 2 L 7 4 4F RT A20WE 2008020100090 20080201 00090 NM 2008 2 1 CALA0800085 1 20080129 A 5311 BAC15171470 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FUSELAGE FRAME IS CRACKED AT STA 767 BETWEEN STRINGER 8L AND 9L. REPAIR PER ECRA 5310-04697. 2 L 7 2 4F RT A16WE 2008020100092 20080201 00092 NM 2008 2 1 KCSA081049 1 20080130 A 3350 LIGHT BOEING 747 7472B4B 138481B NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 710CK 21097 RIGHT UPPER DECK CEILING EMERGENCY LIGHT IS OUT. 2 L 7 4 4F RT A20WE 2008020100115 20080201 00115 WP 2008 2 1 08FDEA00283 1 20080125 A 5310 ACA72251 DOOR FRAME DOUG MD10 MD1010F 3022112 WP BS 633 S27L CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 NR 1 MCD LOWER JAMB SUPPORT FITTING HOLE "C" HAS CRACK INDICATIONS, FOUND WITH BHEC (SEE ATTACHED DRAWING). INSTALLED R EPAIR BUSHING IN REFERENCE WITH DC/MD10-10 SRM VOLUME I 53-50-00 PAGE 81 FIG 17 AT HOLE LOCATION C, TO CARGO DOOR JAMB B EAM ONLY. LOWER FITTING REPLACED ON NON-ROUTINE NR N00948. 2 L 7 3 4F RT A22WE 2008020100121 20080201 00121 EU 2008 2 1 08FDEA00290 1 20080126 A 5347 A5327828622200 ADAPTER AIRBUS 300 A300F4605R 3930327 EU SEAT TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 681FE 799 MAIN CARGO DECK FRAME 57.1 SEAT TRACK NR 3 LT SIDE CLS ADAPTER CRACKED APPROX 3.5 INCH IN LENGTH. REMOVED AND REPLACED CLS ADAPTER IAW A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008020100123 20080201 00123 NM 2008 2 1 08FDEA00292 1 20080126 A 3020 CLAMP DOUG MD11 MD11F 3023600 NM ANTI-ICE DUCT LOOSE A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 623FE 48794 NR 2 ENG ANTI ICE DUCT LIGHT, SHUT DOWN NR 2 ENG AS DIRECTED BY CHECKLIST. REMOVED AND REPLACED ENG 2 ANTI-ICE VLV LATC HING (R2-5527) IAW MD-11 SMP. REMOVED AND REPLACED NR 2 ENG COWL ANTI-ICE MANIFOLD FAILURE SENSING ALL 3 LOOPS (D1-89, D1-90, AND D1-91) IAW MD-11 MM 30-22-11-4. HOOKED UP EQUIPMENT FOR THE NR 2 ENG NOSE COWL ANTI-ICE DUCT LEAK CHECK IAW MD-11MM 30-22-09-5. LEAK CHECK C/W SMALL LEAK FOUND AT COUPLING ON DUCT GOING FROM ENGINE THROUGH FIREWALL. RETORQUED CLAMP LEAK CHECKS GOOD. REMOVED EQUIPMENT, REINSTALLED DUCTING CLOSED PANELS. REACTIVATED ANTI ICE VALVE, RAN ENGINE. OPS CHECKS GOOD. 2 L 7 3 4F RT A22WE 2008020100124 20080201 00124 WP 2008 2 1 08FDEA00293 1 20080126 A 5340 AFA71321 BRACKET DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MCD SPOOL BRACKET NR 3 HAS CRACK INDICATION ON HOLES A AND B. REPAIRED IAW EA 8-5310-113030. 2 L 7 3 4F RT A22WE 2008020100126 20080201 00126 WP 2008 2 1 08FDEA00295 1 20080126 A 5320 AFA71321 BRACKET DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MCD SPOOL BRACKET NR 5 HAS CRACK INDICATION ON HOLES B, C, AND D. REPAIRED IAW EA 8-5310-113030. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008020100130 20080201 00130 EU 2008 2 1 08FDEA00303 1 20080127 A 5347 A5381310620000 SEAT TRACK AIRBUS 310 A310221 3930310 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 NR 4 LT ARTICULATING SEAT TRACK IS CRACKED. REMOVED AND REPLACED LT NR 4 ARTICULATING SEAT TRACK PO NR 602215.2 REF FED EX A310-200 W/C E-6-5310-7-3322 PT2 SEAT AND DUMMY TRACKS ATTACHMENT FITTINGS INSPECTION. 2 L 7 2 4F RT A35EU 2008020100135 20080201 00135 EU 2008 2 1 08FDEA00308 1 20080128 A 5320 A53810967 DIAPHRAGM AIRBUS 300 A300B4605R 3930308 EU FUSELAGE SCRATCHED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND SCRATCHES ON BOTTOM SKIN OF DIAPHRAGM AT TRACK 4-5 LT, C48. REPAIR PERFORMED BY REWORK THE SCRATCHES IAW RAS 0575 41/004/2008 ISS A AND EA 5-5315-114877. 2 L 7 2 4F RT A35EU 2008020100136 20080201 00136 EU 2008 2 1 08FDEA00309 1 20080128 A 5330 A53986202200 SKIN AIRBUS 300 A300F4605R 3930327 EU FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 FOUND FUSELAGE EXT SURFACE SKIN DENTED BETWEEN FR 90 AND FR 91, BL 21L. CHECKED DENT LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-12, PAGE 109. CUT OUT DAMAGE AND FABBED 1 EA REPAIR DOUBLER AND FILLER IAW SRM 53-10-12, FIG 255 SHEET 2 , PAGES 357-362. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-10-12, FIG 225 SHEET 2. 2 L 7 2 4F RT A35EU 2008020100139 20080201 00139 EU 2008 2 1 MALA080016 1 20080128 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 CARGO EXTERIOR SKIN REQUIRES INSPECTION DUE TO FEW LIGHT SMOOTH DENTS AND MAPPING. INSPECTED CARGO DOOR AND REPAIRED DI SBOND AREA IAW MAL EO NR S52100. SEE CONT CARD 091672 FOR DETAILS. FROM CONTINUATION CARD 091672 NR 1 DENT IN CARGO DO OR EXTERIOR SKIN REQUIRES MAPPING. COMPLETED DENT MAPPING. SEE DENT MAP SHEET FOR DETAILS. 2 L 7 2 4T RT A52EU 2008013100163 20080131 00163 NM 2008 1 31 SWAA080478 1 20080127 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 25R TO STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008013100206 20080131 00206 NM 2008 1 31 SWAA080495 1 20080128 A 2612 896768 FIRE LOOP BOEING 737 7373H4 1384600 NM APU FAULTY A SWAA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 SW 29 611SW 27697 DECLARED EMERGENCY. APU FIRE WARNING INFLIGHT, FIRE BOTTLE DISCHARGED. REMOVED AND REPLACED APU LOWER FIRE DETECTOR LO OP PER MM. 2 L 7 2 4F RT A16WE 2008013100316 20080131 00316 NM 2008 1 31 DL764080099 1 20080119 A 3350 CHARGER BOEING 767 767432ER 1385134 NM STA 401 RBL 95 INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 825MH 29696 BATTERY CHARGER M730 STA 401 RBL 95 LIGHTS INOP AFTER 5 MINUTES. REMOVED AND REPLACED BATTERY CHARGER OPS CK GOOD. REP LACED DURING HMV1 ON N/R 44971 AT TIMCO IN GSO. 2 L 7 2 4F RT A1NM 2008013100336 20080131 00336 NM 2008 1 31 DLM88080114 1 20080124 A 2530 COFFEEMAKER DOUG MD88 MD88 3023688 NM GALLEY ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 920DL 49644 ELECTRICAL ODOR IN CABIN. REPLACED COFFEEMAKER, RAN A/C FOR SEVERAL HOURS. NO OTHER ODORS NOTED. 2 L 7 2 4F RT A6WE 2008020100015 20080201 00015 NM 2008 2 1 HNAA0800027 1 20080110 A 3397 MWSD20E2 DIODE DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 826EN 48275 265 389 CABIN ROW 7, FLOOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPAIRED WIRING AND REPLACED CONNECTOR/DIODE AT CR4, OPERAT IONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2008020100021 20080201 00021 NM 2008 2 1 HNAA0800028 1 20080115 A 3350 1013075 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN OUT OF POSITION A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 980HA 31685 115 376 NUMBER 1 RED FLOOR EMERGENCY ESCAPE PATH LIGHT PULLED AWAY FROM FLOOR EXPOSING WIRING. REPAIRED EMERGENCY LIGHT ASSEMBL Y. 2 H 7 2 4T RT A13NM 2008020100022 20080201 00022 NM 2008 2 1 HNAA0800029 1 20080114 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM CARGO BAY NO TEST A HNAA K NONE L NO TEST NR NOT REPORTED 1 EA 07 814EX 318 NR 1 BAG BAY SMOKE DETECTOR WILL NOT TEST. PULLED AND RESET CIRCUIT BREAKER K-7. THE SMOKE DETECTOR STILL WOULD NOT TE ST. SYSTEM IS STILL MEL'ED, MORE INFORMATION TO FOLLOW. 2 H 7 2 4T RT A13NM 2008020100094 20080201 00094 NM 2008 2 1 KCSA081051 1 20080130 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FUSELAGE SKIN CORRODED AT BS 1684, STR 42L. 2 L 7 4 4F RT A20WE 2008020100120 20080201 00120 WP 2008 2 1 08FDEA00288 1 20080126 A 5340 AFA71321 BRACKET DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MCD SPOOL BRACKET NR 1 HAS CRACK INDICATION ON HOLES A, B, C, AND D. REAMED ALL HOLES TO DIMENSIONS SHOWN IN TABLE 1 OF EA 8-5310-113030. PERFORMED HFEC OF ALL HOLES, NO DEFECTS NOTED. IAW NDT SPM 06-10-01-003. REPAIRED LOWER JAMB BEAMS IAW EA 8-5310-113030. REMOVED JAMB SUPPORT FITTING IAW SRM 51-33-01, VOL II ,PG 1. REMOVED AND REPLACED SUPPORT FITTING IAW SRM 53-50-00 VOL I, FIG 17 & 51-33-01, VOL II, PG 1. INSTALLED INTERCOSTAL FS 635-655 IAW SRM 51-33-01, VOL II ,P G 1. MAJOR REPAIR 2 L 7 3 4F RT A22WE 2008020100122 20080201 00122 WP 2008 2 1 08FDEA00291 1 20080126 A 3297 WIRE HARNESS DOUG MD10 MD1010F 3022112 WP LANDING GEAR OUT OF POSITION A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 397FE 46631 MAIN GEAR WOULD NOT RETRACT ON AFTER TAKEOFF CHECKLIST CYCLED GEAR AS PER QRH GEAR WENT DOWN 3 GREEN BUT MAIN GEAR STILL WOULD NOT RETRACT CONFIG PAGE CONFIRMED ALL THE ABOVE. FOUND LEFT AND RIGHT UPLATCH SENSOR WIRE HARNESS INTERFERING W ITH TRAVEL OF LINK ASSY'S. REPOSITIONED HARNESSES. LG POSITION SYSTEM CHECKS GOOD REF MD10-10 MM 32-61-15-4. JACKED A C SWUNG GEAR SEVERAL TIMES, OPS CHECK AND INDICATION CHECKS GOOD PER MD 10-10 MM 32-60-00-5. 2 L 7 3 4F RT A22WE 2008020100175 20080201 00175 NM 2008 2 1 QXEA200800047 1 20080128 A 3230 483023 SEQUENCE VALVE BOMBDR DHC8 DHC8402 1390042 NM NLG FAULTY A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 419QX 4145 BOI - FLIGHT 2403 AFTER TAKEOFF NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED, AFTER NORMAL RETRACTION OF NLG LOUD BANGING HEARD FROM UNDER COCKPIT FLOOR. PERFORMED EMERGENCY EXTENSION, RTF UNEVENTFUL LANDING. FERRY FLIGHT TO PDX FOR MAINTE NANCE. PDX MAINTENANCE REPLACED NOSE LANDING GEAR SOLENOID SEQUENCE VALVE, PERFORMED LANDING GEAR PRIMARY EXTENSION AND RETRACTION SYSTEM FUNCTIONAL TEST. OPS CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008020100176 20080201 00176 EU 2008 2 1 08FDEA00259 1 20080124 A 4920 GTCP331250H APU AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2* GL APU BAY FIRE A FDEA F ACTIVATE FIRE EXT. A J FLAME/FIRE WARNING INDICATION LD LANDING 1 SO 25 670FE 11056 777 P1377 AT TOUCHDOWN, APU FIRE, AGENT AUTO FIRED. APU FIRE HANDLE PULLED. APU MASTER SWITCH OFF, APU NOT ON. UPON FURTHER INV ESTIGATION, DISCOVERED EVIDENCE OF FIRE IN APU BAY. CONNECTOR P18 AT MONOPOLE ASSY IS MELTED/BURNED. NUMEROUS WIRE BUN DLES ON APU HARNESS ARE BURNED & SCORCHED. APU FIRE BOTTLE AUTO DISCHARGED UPON TOUCHDOWN. APU ENGR APPROVED. APU R & R GTCP331-250H, PERFORM STRUCTURAL INSPECT OF APU BAY AFTER APU REMOVED AND CLEANING PER MM 53-19-11-6 & SRM 53-19-12. PURGED APU DRAIN LINE WITH DRY N2. NO EVIDENCE OF BLOCKAGE. R & R OF APU BLEED VALVE, APU AIR INTAKE FLAP ASSY, FWD M OUNT ROD PER AMM. 2 L 7 2 4F 4 F RT A35EU E23EA 2008020100177 20080201 00177 WP 2008 2 1 08FDEA00282 1 20080125 A 5310 ACA72251 DOOR FRAME DOUG MD10 MD1010F 3022112 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 NR 3 MCD LOWER JAMB SUPPORT FITTING HOLES A, B, C AND D HAS CRACK INDICATIONS FOUND WITH BHE (SEE ATTACHED DRAWING). IN STALLED REPAIR BUSHINGS IN REFERENCE WITH DC/MD10-10 SRM VOLUME I, 53-50-00 PAGE 81 FIGURE 17 AT HOLE LOCATIONS A, B, C AND D TO CARGO DOOR JAMB BEAM ONLY. LOWER FITTING WAS REPLACED ON NON-ROUTINE NR N00949. 2 L 7 3 4F RT A22WE 2008020100178 20080201 00178 WP 2008 2 1 08FDEA00289 1 20080126 A 3297 WIRE HARNESS DOUG MD10 MD1010F 3022112 WP LANDING GEAR OUT OF POSITION A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 25 397FE 46631 MAIN GEAR WOULD NOT RETRACT ON AFTER TAKEOFF CHECKLIST CYCLED GEAR AS PER QRH GEAR WENT DOWN 3 GREEN BUT MAIN GEAR STIL L WOULD NOT RETRACT CONFIG PAGE CONFIRMED ALL THE ABOVE. FOUND LEFT AND RIGHT UPLATCH SENSOR WIRE HARNESS INTERFERING W ITH TRAVEL OF LINK ASSY'S. REPOSITIONED HARNESSES, LG POSITION SYSTEM CHECKS GOOD REF MD10-10 MM 32-61-15-4. REPOSITIO NED UPLATCH SENSOR HARNESS ROUTING AND GEAR SWING IAW MD-10-10 AMM 32-61-15-4. ALL OPERATION AND INDICATIONS CHECK S AR E GOOD. 2 L 7 3 4F RT A22WE 2008020100180 20080201 00180 EU 2008 2 1 08FDEA00299 1 20080126 A 5347 A53274005200 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K K NONE NONE O OTHER IN INSP/MAINT 1 SO 25 655FE 742 MAIN DECK SEAT TRACK HAS COROSION BETWEEN FR 69 AND FR 70, LBL18. INSTALLED NEW SEAT TRACK SECTION P/N NR A53274005. F ABRICATED FROM MATERIAL DAN200IT79511, BATCH NR 0000993114, IAW SRM 53-10-16 AND 53-23-00. 2 L 7 2 4F RT A35EU 20080911 NM 2008 9 11 2008UALA03990 1 20080727 A 2822 5006286C PUMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CENTER AUX TANK FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 657UA 27112 RIGHT MAIN FUEL QTY DECREASED WHILE FEEDING FROM CTR TANK. *S/D* SUSPECT FAULTY AUX OVERRIDE PUMP. REPLACED PUMP PER MM 28-22- 05, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03973 1 20080724 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 662UA 27159 FWD X AISLE EEL INOP. *S/D* FOUND LIGHT ASSEMBLY BROKEN. REPAIRED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE . 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA03916 1 20080721 A 3350 78961 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 SEAT 3A AFT EEL INOP. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03936 1 20080723 A 3350 78671 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 54 HJK. *S/D* FOUND FAULTY LIGHT. REPLACED LIGHT, OP CHECKED GOOD. AC OK FOR S ERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080911 NM 2008 9 11 2008UALA03971 1 20080724 A 3350 GE1317 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 AFT LT EXTERIOR EMERG LIGHT INOP 2L MED. *S/D* SUSPECT BURNED OUT LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SE RVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080911 NM 2008 9 11 2008UALA04027 1 20080727 A 3350 0YE4120A01G01 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE AFT LAVATORY FAULTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 776UA 26937 AFT LAV BLOCKED FOR LIGHT HAVING ELECTRIC ODOR. *S/D* FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 NM 2008 9 11 2008UALA04085 1 20080731 A 3397 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE EMERGENCY LIGHT DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 782UA 26948 SEAT 1E 1 EACH EEL INOP. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080911 EU 2008 9 11 08FDEA02735 1 20080708 A 2611 SMOKE DETECTOR AIRBUS 300 A300F4605R 3930327 EU E/E BAY MALFUNCTIONED A FDEA O OTHER N FALSE WARNING DE DESCENT 1 CE 21 685FE 6937 6937 803 ON SHORT FINAL TO KMEM RWY 36L, GOT AVIONICS SMOKE WARNING AND CRC. DECLARED EMERGENCY AND STOPPED ON RWY. RAN QRH PR OCEDURES. NO SMOKE NOTED, SHUTDOWN ENGINES STARTED APU AND ASKED FOR TOW-IN TO PARKING. T/S AVIONICS COMPARTMENT SMOKE DETECTION USING TSM 26-15-00. REMOVED AND REPLACED AVIONICS COMPARTMENT SMOKE DETECTOR 11WA AND 13WA. OPS CHECK GOOD REF A300 MM 26-15-12-4. 2 L 7 2 4F RT A35EU 20080911 NM 2008 9 11 08FDEA02759 1 20080708 A 5753 652163197 SKIN BOEING 727 727200 138407E NM LT WING TE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 275FE 22040 DEEP GOUGE IN LT O/B FOREFLAP, L/E CAP UPPER SURFACE APPROX 10 INCHES FROM I/B END IN PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. CUT OUT DAMAGED AREA DIM 1' X 5/8 IAW B727 SRM 57-50-4 FIG 1. FABRICATED REPAIR PLATE MA T USED 2024T3 .063' IAW B727 SRM 57-50-4 FIG 1. TREATED AND PRIMED REPAIR PLATE AND AREA IAW B727 SRM 51-10-2. INSTALL ED REPAIR PLATE IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 20080911 NM 2008 9 11 08FDEA02513 1 20080627 A 2130 32167441 VALVE BOEING 727 727200 138407E NM CABIN PRESSURE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 21 257FE 69 69 20939 CABIN PRESSURE WOULD NOT HOLD WITH ACFT AT 240. DESCENT TO 200 HELPED FOR ABOUT 1 HOUR, THEN CABIN CREAPED UP TO 9500'. FURTHER DESCENT TO 18000 ALLOWED CABIN TO HOLD STEADY. MAINTENANCE ACTIONS, REPLACED RT PACK VALVE. 2 L 7 3 4F RT A3WE 20080912 NM 2008 9 12 QXEA200800405 1 20080418 A 5314 KEELBEAM DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK SUSPECT CORROSION AT I/B BOTTOM OF VERTICAL KEELBEAM AT STA X370 AND STR 31P. REMOVED CORROSION AT BOTTOM OF VERTICAL KEEL BEAM STA 370.8. REF CPM CHAP 4 PG 4-25 PARA 9. ORIGINAL THICKNESS .050" REMAINING THICKNESS .046". M AX MATERIAL REMOVED .004 WITHIN LIMITS REF -8 200 SRM 51-20-11 PARA 3. HFEC INSP. IAW -8 200 NDTM PT6, 51-00-01 NO CRAC KS NOTED. ETCHED ALODINE PRIME REF -8 CPM CHAP 5, PARA 2C. 2 H 7 2 4T RT A13NM 20080912 SO 2008 9 12 SWIA200819985 1 20080822 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 236SW 120312 EMERGENCY LIGHT STRIP IN AFT CABIN IS BROKEN. REINSTALLED LIGHT STRIP. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080912 EA 2008 9 12 SWIA200819987 1 20080822 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 917SW 7641 RECEIVED A NOSE GEAR DISAGREE AFTER TAKEOFF. FLIGHT 6512. REPLACED NOSE GEAR SELECTOR VALVE WITH A SERVICEABLE UNIT. RE-ADJUSTED LEFT NOSE GEAR WOW PROX SENSOR IAW MM 32-61-05. PERFORMED SEVERAL GEAR SWINGS WITH NO DEFECTS NOTED. P/N O FF 55540-6, S/N OFF 1269. 2 L 7 2 4F RT A21EA 20080912 NM 2008 9 12 SWAA084759 1 20080827 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER AFT CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080912 2008 9 12 SWAA084760 4 20080827 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008020100181 20080201 00181 WP 2008 2 1 08FDEA00311 1 20080128 A 2810 APB70081 SKIN DOUG MD10 MD1010F 3022112 WP CENTER TANK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 LWW, CTR TANK UPPER SKIN CORRODED STA 1381, LBL 76. REMOVED AND REINSTALLED FASTENERS IAW 51-31-01 VOL II. REMOVED CORR OSION, FOUND TO BE WITHIN LIMITS IAW SRM 57-00-01 FIG 1A VOL I AND SRM 57-33-01 FIG 1 VOL III. ALODINED AND PRIMED IAW SRM 51-21-01 VOL II 2 L 7 3 4F RT A22WE 2008020100182 20080201 00182 EU 2008 2 1 08FDEA00312 1 20080128 A 5514 A5517860720000 BRACKET AIRBUS 310 A310221 3930310 EU HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 THS LEFT UPPER BODY FAIRING FWD ATTACH BRACKET ANGLE CORRODED, CENTER BOX AREA, ANGLE IS PART OF LEADING EDGE. REMOVED AND REINSTALLED UPPER APRON IAW A310-200 SRM 51-40-21. REMOVED AND REINSTALLED RIB ASSY IAW A310-200 51-40-21. REMOVED UPPER ATTACH PLATE IAW A310-200 SRM 51-40-21. REMOVED CORROSION ORIGINAL THICKNESS .252 REMOVED .050 REMAINING THICKNE SS .200, FOUND TO BE OUT OF LIMITS IAW A310-200 55-12-28 (NO REPAIR AUTHORIZED). RECEIVED NEW PART P/N A5517860720000 P /O 604175.1. INSTALLED NEW BRACKET IAW A310-200 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008020100186 20080201 00186 NM 2008 2 1 08FDEA00318 1 20080128 A 5320 141N84222 SILL BOEING 757 757200 1384950 NM BS 365-395 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND ON RI DOOR SILL BETWEEN STA 365 AND STA 395 FOUND WITH ELONGATED HOLES AND CORROSION. REMOVED EXIS TING REPAIR AND REPLACED IAW SRIM 51-10-02 REV. 93. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008020100188 20080201 00188 NM 2008 2 1 HALA0800029 1 20080128 A 3350 LIGHT BOEING 767 7673G5 1385126 NM CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 585HA 24257 EMERGENCY FLOOR TRACK LIGHT AT CROSS AISLE BETWEEN DOORS 2L AND 2R ARE INOP. REPLACED EMERGENCY TRACK LIGHT ASSY AT 2L DOOR SIDE OF FLOOR TRACK. ALL EMERGENCY FLOOR PATH LIGHTS, OPS CK GOOD. 2 L 7 2 4F RT A1NM 2008020100191 20080201 00191 CE 2008 2 1 WGEA200800013 1 20080112 A 5755 24920015 SPOILER LEAR 60 60LEAR 5170707 CE LT WING CORRODED E WGEA K NONE O OTHER IN INSP/MAINT 1 EA 27 268WS 268 LT AND RT SPOILERS HAVE CORROSION ON TRAILING EDGE; BLENDED CORROSION ON LT SPOILER PER BOMBARDIER ENGINEERING DISPOSITI ON 60268DAL0515. 2 L 7 2 4F RT A10CE 2008020100192 20080201 00192 CE 2008 2 1 WGEA200800015 1 20080112 A 5755 24920016 SPOILER LEAR 60 60LEAR 5170707 CE RT WING CORRODED E WGEA K NONE O OTHER IN INSP/MAINT 1 EA 27 268WS 268 LT AND RT SPOILERS HAVE CORROSION ON TRAILING EDGE; BLENDED CORROSION ON RT SPOILER PER BOMBARDIER ENGINEERING DISPOSITI ON 60268DAL0515. 2 L 7 2 4F RT A10CE 2008020100193 20080201 00193 SO 2008 2 1 CHQA200800013 1 20080126 A 3297 14544841401 WIRE HARNESS EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BRAKE SYSTEM DAMAGED A CHQA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 GL 11 273SK 145331 CAE312347 CVG TO STL. UPON ROTATION OF THE AIRCRAFT ON TAKEOFF, THE CREW RECEIVED A "BRAKE OVERHEAT" MESSAGE ON EICAS. THE FLIGH T LEVELED AT 6,000 FEET AND THE CREW RAN THE QRH CHECKLIST ITEMS. ACCORDING TO THE MFD THE RIGHT OUTBOARD BRAKE TEMPERA TURE WAS IN THE FULL YELLOW POSITION. AS A PRECAUTION, THE LANDING GEAR WAS LOWERED TO ALLOW THE BRAKE TO COOL IF IT WA S INDEED A HOT BRAKE. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT A ND FOUND THE HARNESS FOR THE BRAKE TEMPERATURE SENSOR WAS DAMAGED AND WAS THE CAUSE FOR THE ERRONEOUS BRAKE INDICATIONS. THE RIGHT OUTBOARD BRAKE TEMPERATURE INDICATION WAS DEFERRED. THE HARNESS WAS REPAIRED ON THE 26TH, THEN REPLACED ON 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008020400005 20080204 00005 EA 2008 2 4 CHQA200800015 1 20080128 A 3260 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE MLG FAULTED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 638BR 12398 7311 GEE872506 CMH TO IAH - DURING TAKEOFF, CREW RECEIVED A WOW INPUT AND WOW OUTPUT EICAS MESSAGE. AFTER RUNNING THE APPROPRIATE QRH CHECKLISTS, IT WAS DECIDED TO DIVERT TO SDF WHERE THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE PSEU FOR FAULT CODES WHICH POINTED TO THE PSEU BEING AT FAULT. MAINTENANCE REPLACED THE PSEU AND THE PROXIMITY SYSTEM OPERA TED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2008020400009 20080204 00009 EA 2008 2 4 REXA200800002 1 20080118 A 2610 7536893 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA CABIN DIRTY A REXA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 25 8747B 7748 AFTER TAKEOFF RECEIVED LAV SMOKE MESSAGE AND SMOKE IN CABIN. FOUND COALESCER BAG DIRTY. QRH FOLLOWED RETURNED TO AIRPOR T NO EVENT LANDING. 2 L 7 2 4F RT A21EA 2008020400011 20080204 00011 CE 2008 2 4 NSVA2008003 1 20080129 A 2612 LIGHT BEECH 1900 1900D 1154162 CE FIRE HANDLE INTERMITTENT A NSVA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 191CJ UE19 RIGHT "T" HANDLE FLICKERS MULTIPLE TIMES IN FLIGHT. INSPECTED RT ENG FIRE LOOP, NO DEFECTS NOTED AT THIS TIME. PERFORM ED FIRE HANDLE TEST IAW BEECHCRAFT AMM 26-10-01-101. 2 L 7 2 4T RT A24CE 2008020400016 20080204 00016 NM 2008 2 4 AALA200800031 1 20080105 A 2740 MODULE BOEING 757 757223 1384957 NM STAB ASYMMETRY INOPERATIVE A AALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 195AN 32389 BOS INFLIGHT T1501/05JAN - RETURNED TO BOS DUE TO STABILIZER TRIM MOVEMENT. LANDED WITHOUT INCIDENT. REPLACED THE STAB ILIZER ASYMMETRY MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020400019 20080204 00019 EU 2008 2 4 AALA200800036 1 20080106 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 JFK - EMERGENCY SEAT MOUNTED LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT 11OWL6 FOR EMERGENCY SEAT MOUNTED LI GHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008020400020 20080204 00020 EU 2008 2 4 AALA200800037 1 20080106 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 JFK - EMERGENCY SEAT MOUNTED LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT 11OWC5 FOR EMERGENCY SEAT MOUNTED LI GHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008020400021 20080204 00021 EU 2008 2 4 AALA200800038 1 20080106 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 JFK - EMERGENCY SEAT MOUNTED LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT 11OWC2 FOR EMERGENCY SEAT MOUNTED LI GHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008020400022 20080204 00022 NM 2008 2 4 AALA200800042 1 20080108 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 198AA 32392 JFK - EMERGENCY EXIT SIGN AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020400026 20080204 00026 WP 2008 2 4 AALA200800023 1 20080103 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7538A 49992 LGA - EMERGENCY LIGHT AT FIRST CLASS ENTRY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FIRST CLASS ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020400031 20080204 00031 WP 2008 2 4 AALA200800026 1 20080104 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 481AA 49656 LGA - EMERGENCY LIGHTS AT MID TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020400033 20080204 00033 WP 2008 2 4 AALA200800028 1 20080104 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 208AA 49159 LGA - EMERGENCY FLASHLIGHT AT AFT RIGHT FORWARD POSITION MISSING STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT RIGHT FORWARD POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020400034 20080204 00034 WP 2008 2 4 AALA200800029 1 20080104 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 208AA 49159 LGA - EMERGENCY FLASHLIGHT AT AFT RIGHT AFT POSITION HAS BROKEN STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT R IGHT AFT POSITION. 2 L 7 2 4F A6WE 2008020400039 20080204 00039 NM 2008 2 4 08FDEA00320 1 20080129 A 5322 146N101616 SHEAR TIE BOEING 757 7572B7 1384964 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 AFT PIT, STA 1500, STRINGER 29, SHEAR TIE IS 100 PERCENT EXFOLIATED. REMOVED AND REPLACED WITH FABRICATED SHEARTIE MADE ON MAE TRAVELER NR T7/689493 IAW SRM 51-10-1 AND 51-40-02. FOUND ADDITIONAL CORROSION ON FRAME AND ANGLE SUPPORT ON FWD SIDE OF FRAME AT STA 1500, S29. REMOVED ANGLE SUPPORT AND REPLACED WITH FABRICATED SUPPORT MADE ON MAE TRAVELER NR T7/691338IAW SRM 51-10-02 AND 51-40-02. ACCOMPLISHED TYPICAL REPAIR TO FRAME IAW SRM 51-70-11. REPAIR DOUBLER MADE ON MAE TRAVELER NR T7/691120 IAW SRM 53-00-07. 2 L 7 2 4F RT A2NM 2008020400060 20080204 00060 EA 2008 2 4 SWIA200819135 1 20080124 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER AP APPROACH 1 NM 07 930SW 7713 RIGHT SIDE WINDOW CRACKED ON APPROACH. REPLACED RIGHT SIDE WINDOW IAW MM 56-12-01, P/N OFF: NP139322-6W, S/N OFF: 02262 R6245. 2 L 7 2 4F RT A21EA 2008020400070 20080204 00070 EA 2008 2 4 SWIA200819145 1 20080128 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCONNECTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 938SW 7741 OVERWING EMERGENCY EXIT SIGN DOES NOT ILLUMINATE, FLIGHT NR 6369. INSPECTED AND SECURED CONNECTOR ON ELBP 2 CHARGER IAW CRJ 200 MM 33-51-05. 2 L 7 2 4F RT A21EA 2008020400072 20080204 00072 SO 2008 2 4 SWIA200819147 1 20080129 A 3040 HEATER EMB 120 EMB120ER 3260203 SO WINDSHIELD INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 565SW 120340 RIGHT WINDSHIELD HEAT IS INOP, FLIGHT NR 5477. REPLACED RIGHT WINDSHIELD IAW AMM 56-10-01, P/N NP-151311-2, S/N OFF 981 11H3490. 2 L 7 2 4T RT A31SO 2008020400074 20080204 00074 NM 2008 2 4 AALA200800053 1 20080112 A 2910 HOSE BOEING 757 757223 1384957 NM HYD SYSTEM LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 616AA 24524 LAX INFLIGHT T2454/12JAN - RECEIVED RIGHT HYDRAULIC LOSS INDICATION. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. FOU ND RIGHT HYDRAULIC LINE DAMAGED AT RIGHT WHEEL WELL REAR SPAR. REPLACED RIGHT HYDRAULIC LINE AT RIGHT WHEEL WELL REAR S PAR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020400079 20080204 00079 WP 2008 2 4 AALA200800063 1 20080114 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 214AA 49162 STL INFLIGHT T1186/14JAN - NOSE GEAR FAILED TO RETRACT AFTER TAKEOFF. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REP ACKED NOSE LANDING GEAR STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020400086 20080204 00086 NM 2008 2 4 AALA200800060 1 20080113 A 3350 P4010049 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 344AN 33083 ORD - EMERGENCY SEAT MOUNTED LIGHTS AT RIGHT SEAT ROW 30 TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT SEAT ROW 30 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008020400087 20080204 00087 NM 2008 2 4 AALA200800048 1 20080110 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AN 32396 DFW - EMERGENCY LIGHT AT SEAT 23D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020400094 20080204 00094 EU 2008 2 4 AALA200800062 1 20080113 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 JFK - EMERGENCY EXIT LIGHT IN CABIN CYCLED ON AND OFF. ADJUSTED AND TESTED EMERGENCY EXIT LIGHT IN CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008020400095 20080204 00095 NM 2008 2 4 AALA200800059 1 20080113 A 2820 ACTUATOR BOEING 767 767323 1385205 NM DEFUELING VALVE STUCK A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 39364 24045 LIM INFLIGHT T0957/13JAN - AIRCRAFT EXPERIENCED FUEL IMBALANCE DURING FLIGHT. LANDED LIM WITHOUT INCIDENT. FOUND RIGHT DEFUELING VALVE ACTUATOR STUCK IN OPEN POSITION DUE TO ICE FORMATION. CLEANED RIGHT DEFUELING VALVE ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008013100290 20080131 00290 NE 2008 1 31 183801212008 2 20080121 A 7314 9550178290 SOLENOID SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE IGNITION SYS LEAKING E QMLA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 03 257ST 1838 831 AT APPROX 01:30 MDT, MEDFLIGHT 2 WAS ATTEMPTING TO DEPART SCENE WITH PATIENT. PILOT DETECTED ODOR OF SMOKE IN THE COCKPI T AND ABORTED TAKEOFF. PILOT SECURED ENGINE AND ADVISED GROUND PERSONS THAT HE WAS UNABLE TO TRANSPORT PATIENT VIA HELI COPTER. PATIENT WAS THEN LOADED INTO A GROUND AMBULANCE AND DEPARTED. PILOT CALLED THE DISPATCH AT APPROX 01:50 MDT TO LET THEM KNOW HE HAD TO ABORT TRANSPORT. THERE WAS NO INJURIES OR DAMAGE. TROUBLESHOOTING SHOWED THAT THE IGNITION EL ECTRO SOLENOID WAS LEAKING CAUSING THE ODORS. 1 G 7 1 3U 3 U NC H9EU E19EU 2008013100291 20080131 00291 EU 2008 1 31 715801222008 1 20080122 A 2120 UNKNOWN BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE CABIN ODOR E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 440SL 7158 PILOT RECEIVED A REQUEST FOR A BABY FLIGHT. THE CREWMEMBERS AND PILOT PROCEEDED TO THE AIRCRAFT TO REPOSITION DOWNTOWN SO THEY COULD PICKUP THE CHILDREN'S TEAM. UPON TAKEOFF AT 11:02 A CREWMEMBER IN THE AFT CABIN ANNOUNCED SHE SMELLED SOM ETHING BURNING. ALL COCKPIT INSTRUMENT INDICATIONS WERE NORMAL. AS THE AIRCRAFT WAS TURNED TO RETURN TO BASE THE ODOR B ECAME STRONGER TO THE PILOT. AIRCRAFT WAS LANDED AT BASE WITH NO FURTHER PROBLEMS. AIRCRAFT TAKEN OUT OF SERVICE AND M AINT WAS CALLED. MAINTENANCE WAS UNABLE TO LOCATE THE SOURCE OF THE FUMES/SMELL, OR TO DUPLICATE THEM. AIRCRAFT RETUR NED TO SERVICE. 1 G 7 2 3U 3 U H13EU E5NE10 2008013100317 20080131 00317 NM 2008 1 31 DL764080100 1 20080119 A 3350 CHARGER BOEING 767 767432ER 1385134 NM BS 654A LBL 94 INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 825MH 29696 BATTERY CHARGER M7235 STA 654A PLUS 33 LBL 94 LIGHTS INOP AFTER 5 MINUTES. REMOVED AND REPLACED BATTERY CHARGER M7235 O N NR 44972, DURING HMV AT TIMCO IN GSO. 2 L 7 2 4F RT A1NM 2008013100319 20080131 00319 NM 2008 1 31 DL764080102 1 20080119 A 3350 CHARGER BOEING 767 767432ER 1385134 NM BS 1197 LBL94 INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 825MH 29696 BATTERY CHARGER M7236 STA 1197 PLUS 77 LBL 94 LIGHTS INOP AFTER 5 MINUTES. REMOVED AND REPLACED BATTERY CHARGER M7236 D URING HMV 1 AT TIMCO IN GSO ON NR 44974. 2 L 7 2 4F RT A1NM 2008013100326 20080131 00326 NM 2008 1 31 DLM88080111 1 20080123 A 3397 CONNECTOR DOUG MD88 MD88 3023688 NM EMERGENCY LIGHTS DISCONNECTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 937DL 49810 EMERGENCY LIGHTS OUT AT 2C AND 31-36 DEF FOUND BY FAA. RELAMPED 2C,NOW OPS NORMAL. FOUND CONNECTOR DISCONNECTED AT 36E . RECONNECTED AND SECURED NOW OPS NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A6WE 2008013100340 20080131 00340 EU 2008 1 31 08FDEA00267 1 20080110 A 5330 A53610567223 SKIN AIRBUS 310 A310222 3930315 EU FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 FOUND DENT ON FUSELAGE AT FR 49/50 AND STR 36/37 LT. THE DENT WAS REPAIRED IAW FEDEX EA 6-5330-115319. 2 L 7 2 4F RT A35EU 2008013100361 20080131 00361 EU 2008 1 31 NSVA2008002 1 20080129 A 3150 WARNING LIGHT SAAB SF340 340B 7860101 EU RT MAIN BUSS FALSE ACTIVATION A NSVA O OTHER N FALSE WARNING DE DESCENT 1 EA 27 321CJ 340B321 RT MAIN BUSS LIGHT CAME ON DURING DESCENT, RIGHT ESS BUSS LIGHT ON DURING DESCENT. RESET CB (5-I), RAN ENGINES OPS CHEC K GOOD PER MM 24-52-00 AND 24-50-00 VERIFIED AC/DC PWR SYSTEM. 2 L 7 2 4T RT A52EU 2008020100008 20080201 00008 NM 2008 2 1 CALA0800029 1 20080118 A 5330 6545800 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FWD FUSELAGE SKIN AT R-1 DOOR CUTOUT, LOWER AFT CORNER CRACKED. REMOVED DAMAGED SECTION OF SKIN, FABRICATED REPAIR PIEC ES, TREATED, PRIMED AND INSTALLED PER SRM 53-10-01 REPAIR 2. 2 L 7 2 4F RT A16WE 2008020100009 20080201 00009 NM 2008 2 1 CALA0800030 1 20080119 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 PAX CABIN FRAME 360 HAS CRACKS AROUND FASTENER HOLE JUST ABOVE STRINGER 8L. INSTALLED REPAIR ANGLES ON FRAME AT STA 360 STRINGER 8L PER ECRA 5310-04691. 2 L 7 2 4F RT A16WE 2008020100023 20080201 00023 NM 2008 2 1 HNAA0800031 1 20080109 A 6121 78249050 PCU DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE DEFECTIVE A HNAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 07 828EX 39645 243 392 NR 2 PROPELLER FLUX OF 20 RPM ASSOCIATED WITH TORQUE FLUX OF 6%, RETURNED TO FIELD, PROPELLER SYNC OFF AT TIME OF FLUX, CYCLED PROPELLER SYNC DURING FINAL AND SURGE SELF CORRECTED AND ENGINES OPERATE NORMAL. GROUND RAN AT TAKEOFF POWER, CO ULD NOT DUPLICATE DISCREPANCY. FOUND NR 1 SIDE SYNCHROPHASE CONNECTOR HOOKED WITH PCU, DISCONECTED CONNECTOR. RAN AIRC RAFT PER RUNUP MANUAL NO DEFECTS NOTED. ON 10 JANUARY 2008, NR 1 PROPELLER MAX RPM WENT TO 1214; REPLACED PCU, OPERATIO NAL AND LEAK CHECK GOOD. 2 H 7 2 4T RT A13NM 2008020100024 20080201 00024 NM 2008 2 1 KCSA081034 1 20080122 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FUSELAGE SKIN DENTED AT BS 1787 BETWEEN STR 31R AND STR 32R. 2 L 7 4 4F RT A20WE 2008020100030 20080201 00030 NM 2008 2 1 CALA0800037 1 20080119 A 5311 BAC15171147 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 FUSELAGE FRAME CRACKED AROUND RIVET AT STATION 727B ABOVE S-9L. INSTALLED REPAIR ANGLES OF FRAME AT STATION 727B STRING ER 9L PER ECRA 5310-04691. 2 L 7 2 4F RT A16WE 2008020100037 20080201 00037 NM 2008 2 1 CALA0800044 1 20080119 A 5311 6520723U54 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FORWARD BAG BIN DOOR CUTOUT AFT FRAME CRACKED AT LOWER STOP PAD. REMOVED DAMAGED FRAME AND INSTALLED A NEW ONE PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020100040 20080201 00040 NM 2008 2 1 CALA0800047 1 20080119 A 5514 6547501173 FITTING BOEING 737 737524 1384721 NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 LEFT HORIZONTAL STAB ATTACH LUGS INSPECTED FOR CORROSION. INSTALLED NEW SLEEVE PER SOPM 20-50-03. REF BUSHING AND SLEE VE INSTALLATION. 2 L 7 2 4F RT A16WE 2008020100041 20080201 00041 NM 2008 2 1 CALA0800048 1 20080119 A 5514 657378212 FITTING BOEING 737 737524 1384721 NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 RIGHT HORIZONTAL STAB AFT SPAR LOWER LUG HAS CORROSION IN BORE. REMOVED CORROSION IN BORE PER SRM 55-10-10 IAW ECRA 551 0-01912. 2 L 7 2 4F RT A16WE 2008020100047 20080201 00047 NM 2008 2 1 CALA0800056 1 20080118 A 5340 6938737501 STRINGER CLIP BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76354 23592 STRINGER TIE CLIP CRACKED AT STATION 344 R5-10. REMOVED AND INSTALLED NEW PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080912 NM 2008 9 12 SWAA084761 1 20080827 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 887-907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED FROM BS 887 TO BS 907, RBL 70. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080912 NM 2008 9 12 UPS08M53094 1 20080731 A 5321 USP0785Y501 FLOOR PANEL DOUG MD11 MD11F 3023600 NM CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 281UP 48538 INSPECTION TYPE:2C RCB FLOOR PANEL PART NUMBER WSPO785-501 HAS AREAS OF CORROSION. REMOVED AND REPLACED FLOOR PANEL IAW UPS EO MD11-5330-27218-C. 2 L 7 3 4F RT A22WE 20080912 WP 2008 9 12 UPS08853068 1 20080729 A 5240 INTERCOSTAL DOUG DC8 DC871F 302199D WP SERVICE DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 A HOLE DRILLED THROUGH INTERCOSTAL ON RT CTR SERVICE DOOR STRUCTURE 10, 10 INCHES BELOW UPPER HINGE. REMOVED DAMAGED INTERCOSTAL, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-01-21, DWG 5615762, AND SRM 51 -03-00, 51-1-20. 2 L 7 4 4F RT 4A25 20080912 EA 2008 9 12 SWIA200820004 1 20080903 A 3397 CONNECTOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT LOOSE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 803SK 15062 SECOND OVERHEAD EMERGENCY FLOOD LIGHT IS INOP. FLT 3912. FOUND BAD CONNECTION ON FIXTURE. TIGHTENED CONNECTION PER AM M 33-51-09. OPS GOOD. 2 L 7 2 4F RT A21EA 20080915 WP 2008 9 15 08FDEA03001 1 20080721 A 5753 ARC0797509 PANEL DOUG MD10 MD1010F 3022112 WP RT WING TE FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 RIGHT WING OUTBOARD FLAP PANEL 636 AR HAS SEVERAL DENTS. REMOVED THE SKIN AND CORE IN THE DAMAGED AREA. MATERIAL ID'D; CLEANED AND PREPPED FOR CORE BOND; BONDED CORE; CLEANED AND PREPPED DOUBLER FOR BOND. FABRICATED AND BONDED DOUBLER, S EALED DOUBLER EDGE BOND LINES, RESTORED FINISH IAW SRM 51-71-00, VOL II, PARA 17. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 08FDEA03148 1 20080730 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL PANEL ACCESS CUTOUT 542DB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93. REPAIR 5. REPAIR IS CLASSIF IED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080915 EU 2008 9 15 08FDEA03217 1 20080803 A 5310 A53974202476 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 430FE 394 PREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 52 LT BETWEEN FRAMES 59 TO 60 HAS 1 EACH REPAIR SECTION MEAS URING 29 INCHES LONG AND 1 EACH REPAIR SPLICE MEASURING 7.3 INCHES LONG. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREV IOUS STRINGER REPAIR AND INSTALLED CORRECT STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 52 LT BETWEEN FRAMES 59 TO 6 0 IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 20080915 NM 2008 9 15 08FDEA03155 1 20080730 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL ACCESS PANEL CUTOUT 541HB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93, REPAIR 5. REPAIR IS CLASSIFI ED AS MINOR PER GMM 6-2-100. 2 L 7 2 4F RT A2NM 20080915 NM 2008 9 15 08FDEA03151 1 20080730 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL ACCESS PANEL CUTOUT 541MB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIE D AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080915 NM 2008 9 15 08FDEA03153 1 20080730 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL ACCESS PANEL CUTOUT 541KB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93, REPAIR 5. REPAIR IS CLASSIFI ED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080915 WP 2008 9 15 08FDEA03020 1 20080722 A 5414 AUB703625 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 NR 1 PYLON PANEL 438 OL IS CHAFED IN 2 PLACES. FABRICATED DOUBLER AND FILLER IAW SRM 51-21-01; VOL II; FIG 2-B. ALO DINED AND PRIMED FILLERS IAW SRM 51-21-01; VOL II. INSTALLED REPAIR PARTS IAW SRM 54-00-01; VOL I; FIG 2-B AND EA 8-548 0-123601. 2 L 7 3 4F RT A22WE 20080915 WP 2008 9 15 08FDEA03072 1 20080725 A 5730 ARB25103 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING INBD L/E PANEL 516 HB IS WORN ON THE EDGE OF THE PANEL. BLENDED PANEL 516 NB AND FOUND TO BE OUT OF LIMITS IA W SRM 57-00-01; VOL I. FABRICATED DOUBLER IAW SRM 57-00-01; VOL I. ALODINED AND PRIMED IAW SRM 51-21-01; VOL II. P AINTED DOUBLER IAW SRM 51-21-02; VIL II. INSTALLED DOUBLER IAW SRM 51-35-01; VOL II AND 57-00-01; VOL I. 2 L 7 3 4F RT A22WE 20080915 EU 2008 9 15 08FDEA02813 1 20080709 A 5100 UNKNOWN AIRBUS 310 A310203 3930313 EU UNKNOWN UNKNOWN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 435FE 369 ON CLIMB-OUT, L INR PUMPS HOWEVER, LFT INR ISOLATION VALVE WAS AMBER, NO FUEL WAS BEING BURNED. GRAVITY FED FUEL MANUAL LY TO BALANCE. LANDED W/ 28.8 ON LT AND 24.8 ON RT. LANDED OVER MAX LANDING WT. 200 FPM DESCENT ON LANDING. LANDING W T 276.1 AND MAX LANDING WT LIMIT 267.9. T/S AUTO FUEL FEED SYS PER REVISED/AMM 28-21-00-5, NO DEFECTS, REMOVED AND REPL ACED RELAYS 139QA, 136QA, 89QA, 140QA, 131QA, 133QA, CONFIRMED WIRING CONFIG, OPS CHECK NORMAL. R & R RT NR 2 FUEL PUMP PRESS SW TANK ISO VLV TEST/AMM 28-22-00-5. R & R 73QU, 140QA RELAY, 154VD. R & R SDAC AND LEFT INNER ISOL VLV, NO F AULTS. ALL TESTS PASSED, RETURNED A/C TO SERVICE. NO PART CONFIRMED DEFECTIVE. 2 L 7 2 4F RT A35EU 20080915 NE 2008 9 15 08FDEA02982 2 20080718 A 7200 ENGINE DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 1 FAILED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 314FE 48312 530342 DURING DEPARTURE NR 1 ENGINE HAD LOUD BANG AND VIBRATION. NR 1 ENG TO IDLE AND THEN OIL QUANTITY WENT TO ZERO, NO N1. PERFORMED PHASE 1'S AND QRH PROCEDURE. RETURN TO MEM FOR ENGINE OUT LANDING. MX MEM, INSPECTED NR 1 ENGINE. FOUND O IL PUDDLED IN EXHAUST AREA. NO OIL QTY ON NR 1 ENGINE. CREW BLEW NR 1 ENGINE FIRE BOTTLE. REMOVED AND REPLACED ENGINE PER WORK CARDS 71T0101-1 AND 71T0701-1 RUN AND OPS CHECKS GOOD. 2 L 7 3 4F 4 F RT A22WE E23EA 20080915 WP 2008 9 15 UPS08853077 1 20080727 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FS 1490 RBL 36 CRUSHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 MAIN CABIN, FLOOR PANEL HAS CRUSHED HONEYCOMB STA 1490 RBL 36. REMOVED PANEL, FABRICATED AND INSTALL ED REPLACEMENT FLOOR PANEL IAW MM 53-21-02, AND EO DC8-5320-9691C. 2 L 7 4 4F RT 4A25 20080915 WP 2008 9 15 UPS08853078 1 20080729 A 5340 FITTING DOUG DC8 DC871F 302199D WP FS 1275 L36 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 C PIT STA 1275, LONGERON 36, FITTING HAS CORROSION. CORROSION ON FITTING OUT OF LIMITS IAW SRM 53-2- 0 FIG 1F. REMOVED FITTING IAW SRM 51-1020D, REPLACED FITTING IAW 51-01-24, 51-01-20D, AND 51-03-01. 2 L 7 4 4F RT 4A25 2008020100087 20080201 00087 NM 2008 2 1 CALA0800082 1 20080129 A 5311 BAC15171470 BELTFRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FUSELAGE CROWN INTERIOR BELT FRAME HAS CRACK AROUND FASTENER OF OVERHEAD GRILL MOUNTING BRACKET JUST ABOVE STRINGER S9L AT STA 480. 2 L 7 2 4F RT A16WE 2008020100089 20080201 00089 NM 2008 2 1 CALA0800084 1 20080129 A 5311 BAC15171470 BELTFRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 47332 23570 FUSELAGE CROWN INTERIOR BELT FRAME HAS CRACK AROUND FASTENER OF OVERHEAD GRILL MOUNTING BRACKET JUST ABOVE STRINGER S9R AT STA 480. 2 L 7 2 4F RT A16WE 2008020100095 20080201 00095 EA 2008 2 1 VNAA0801007 1 20080120 A 2421 O-RING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT IDG FAULTY A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 223JS 7892 CREW REPORTED ON TAKEOFF ROLL THE EICAS, STATUS DISPLAY AND PFD-MFD ON THE FIRST OFFICERS SIDE WENT DARK. IN ADDITION, A GEN 2 OFF CAS MESSAGE DISPLAYED AFTER EICAS CAME BACK ON. CREW ELECTED TO ABORT THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND SERVICED THE RIGHT HAND IDG IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MAN UAL. OPS CHECK WAS GOOD, LEAK CHECK WAS BAD. MAINTENANCE DEFERRED THE RT IDG PER MEL 24-11-01-1. MAINTENANCE REMOVED AND REPLACED FAULTY O-RINGS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MEL WAS CLEARED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008020100096 20080201 00096 EA 2008 2 1 VNAA0801001 1 20080106 A 4990 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE APU OVERSERVICED A VNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 05 256PS 7937 CREW REPORTED WHEN THE APU WAS TURNED ON FOR LANDING, IT CAUSED THE CABIN TO FILL WITH SMOKE. CREW FOLLOWED THE QRH, TU RNED OFF THE APU AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE OIL LEVEL TO BE OVERSERVICED. MAINTE NANCE PROPERLY SERVICED THE OIL LEVEL IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SER VICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008020100138 20080201 00138 EU 2008 2 1 MALA080015 1 20080128 A 5751 SKIN SAAB SF340 340B 7860101 EU LT AILERON DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 LT AILERON CONTROL SURFACE DISBONDED DENT 62 1/2 INCH FROM IB, 4 INCHES FROM TRAILING EDGE. REPAIRED DAMAGE ON LT AILER ON UPPER SKIN IAW MAL EO NR S51031. REFERENCE 409 NR 321696 FOR INSTALLATION. 2 L 7 2 4T RT A52EU 2008020100141 20080201 00141 EU 2008 2 1 MALA080017 1 20080125 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU COCKPIT ODOR A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 15 411XJ 340B411 ELECTRICAL TYPE SMELL NOTED IN FLIGHT (ONLY NOTED IN COCKPIT), LASTED FOR A SHORT PERIOD OF TIME. SMELLED LIKE "ENGINE ANTI-ICE DUCT" BURNING SMELL I HAD SMELLED BEFORE. VISUALLY INSPECTED DUCTS, FOUND NO PROBLEMS AT THIS TIME. ALL CHECK S GOOD. 2 L 7 2 4T RT A52EU 2008020100179 20080201 00179 EU 2008 2 1 08FDEA00298 1 20080126 A 5347 A53274005200 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 655FE 742 MAIN CARGO SEAT TRACK AT RBL 57 BETWEEN FR 58 AND FR 60 HAS 4 PLACES WITH CORROSION. REMOVED AND REPLACED WITH NEW SEAT TRACK FABRICATED FROM A532-74005-200, MATERIAL DAN200IT79511IAW SRM53-10-16 AND 51-23-00. 2 L 7 2 4F RT A35EU 2008020100183 20080201 00183 WP 2008 2 1 08FDEA00313 1 20080128 A 2810 SKIN DOUG MD10 MD1010F 3022112 WP CENTER TANK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 LWW, UPPER CTR TANK SKIN CORRODED, STA 1381, LBL 49. REMOVED AND REINSTALLED FASTENERS IAW SRM 51-31-01, VOL II. REMOV ED CORROSION, FOUND TO BE WITHIN LIMITS IAW SRM 57-00-01 FIG 1A VOL I, AND SRM 53-33-01 FIG 1 VOL III. ALODINED AND PR IMED IAW SRM 51-21-01 VOL II 2 L 7 3 4F RT A22WE 2008020400004 20080204 00004 SO 2008 2 4 CHQA200800014 1 20080127 A 3297 14544841401 WIRE HARNESS EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BRAKE TEMP CHAFED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 273SK 145331 CAE312347 STL TO CVG - DURING CLIMB CREW RECEIVED AN EICAS MESSAGE FOR BRAKE OVERHEAT ON EICAS. AFTER RUNNING THE QRH AND CONFERR ING WITH MAINTENANCE IT WAS DECIDED TO CONTINUE ON TO CVG. THE FLIGHT LANDED IN CVG WITHOUT INCIDENT. MAINTENANCE INSP ECTED THE AIRCRAFT AND FOUND THE HARNESS FOR THE RIGHT OUTBOARD BRAKE TEMPERATURE SENSOR AS CHAFED. THE BRAKE TEMPERATU RE INDICATION WAS PUT BACK ON DEFERRAL. THE HARNESS WAS CHANGED ON THE 29TH. AFTER REPLACING THE HARNESS, THE BRAKE TE MPERATURE INDICATION SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008020400012 20080204 00012 NE 2008 2 4 REXA200800003 2 20080118 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RIGHT LEAKING A REXA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 8747B 7747 GEE873642 ON CLIMB-OUT OF MSP THE FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. THE FLIGHT CREW PERFORMED QRH PROCEDURES, DECLARED AN EMERGENCY AND REQUESTED TO RETURN TO MSP. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT MSP. THIS AIRCRAFT HAD PREVIOUSLY HAD ITS LEFT ENGINE REPLACED ON 01/16/08 FOR AN OIL LEAK IN THE A SUMP AREA. SEE SDR REXA200800001. FUR THER TROUBLESHOOTING DISCOVERED THAT THE RIGHT ENGINE ALSO HAD AN INTERNAL LEAK IN THE B SUMP. THE AIRCRAFT WAS FERRIED TO A MAINTENANCE BASE WHERE THE RIGHT ENGINE WAS REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2008020400023 20080204 00023 NM 2008 2 4 AALA200800040 1 20080106 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 193AN 32387 DFW - EMERGENCY LIGHT AT LEFT AFT EXTERIOR SLIDE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT AFT EXTERIOR SL IDE. SYTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020400035 20080204 00035 NM 2008 2 4 AALA200800020 1 20080103 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 784AN 29588 NRT - EMERGENCY LIGHT EXIT SIGN AT LOWER LEFT PARTITION AFT OF SEAT ROW 45CEG MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT EXIT SIGN AT LOWER LEFT PARTITION AFT OF SEAT ROW 45CEG. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008020400069 20080204 00069 EA 2008 2 4 SWIA200819144 1 20080126 A 2130 10275B04C03 MODULE CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 960SW 8015 8015 7853 RECEIVED A MASTER WARNING "DIFF PRESSURE" MESSAGE ON CLIMB-OUT, FLIGHT NR 6621. REMOVED AND REPLACED CABIN PRESSURE ACQ UISITION MODULE IAW AMM 21-33-01. OPERATIONAL TEST GOOD. 2 L 7 2 4F RT A21EA 2008020400073 20080204 00073 NM 2008 2 4 AALA200800049 1 20080110 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 794AN 30256 DFW - EMERGENCY LIGHT AT SEAT 23G HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008020400083 20080204 00083 NM 2008 2 4 AALA200800072 1 20080114 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 945AN 30085 TUL - EMERGENCY LIGHTS AT RIGHT SEAT ROWS 15 TO 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT SEA T ROWS 15 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 SWAA084767 1 20080827 A 5311 65C25230 FRAME BOEING 737 7373T0 1384582 NM BS 727E S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 SWAA084769 1 20080827 A 5311 6546596 FRAME BOEING 737 7373T0 1384582 NM BS 727B S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 SWAA084770 1 20080827 A 5311 6546558 FRAME BOEING 737 7373T0 1384582 NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 SWAA084771 1 20080827 A 5311 6546557 FRAME BOEING 737 7373T0 1384582 NM BS 887 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 7L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 SWAA084773 1 20080827 A 5753 SKIN BOEING 737 7373Y0 1384671 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED 22Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED AT OUTBOARD END. REPAIRED FLAP PE R SRM. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 SWAA084753 1 20080827 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080915 EU 2008 9 15 UPS08153141 1 20080820 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 164UP 0853 EXIT LIGHT OVER DOOR REMAINS ON IN ALL SWITCH POSITIONS. ECAM SHOWS EXIT ON. PERFORMED ADJUSTMENT TEST OF SUPERNUMARY AREA EMERGENCY LIGHTS PER A300 MM 33-51-00-05. SYSTEM OPS CHECKED GOOD, CONTINUE IN SERVICE. 2 L 7 2 4F RT A35EU 20080915 WP 2008 9 15 UPS08853128 1 20080730 A 5240 INTERCOSTAL DOUG DC8 DC871F 302199D WP FWD SERVICE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 CRACKED CHANNEL AND GOUGED INTERCOSTAL AT THE SAME LOCATION ON RT FWD SERVICE DOOR LOWER AFT CORNER. REMOVED EDGE CRACK ON CHANNEL BY BLENDING IAW SRM 53-02-00. FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5615762 SRM 51 -01-21, AND 51-01-20D. 2 L 7 4 4F RT 4A25 20080915 NM 2008 9 15 UPS08M53107 1 20080726 A 5730 ARB39546 SKIN DOUG MD11 MD11F 3023600 NM RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 281UP 48538 INSPECTION TYPE:2C RT WING L/E SKIN SPLICE AT XFS669 IS CRACKED. REMOVED CRACKED SPLICE, FABRICATED AND INSTALLED REPLA CEMENT IAW DWG ARB3954 AND MD-11 SRM 51-33-01. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 UPS08M53111 1 20080805 A 5712 RIB DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:C LT WING L/E CAVITY AT 15 INCHES I/B OF SLAT TRACK NR 9, RIB SUSPECT CRACK. HFEC CARRIED OUT IAW NDT S PM REV13 PART 06-10-01.001 AND CRACK CONFIRM APPROX 3.75 INCH LONG. DAMAGE RIB REMOVED, NEW RIB FABRICATED & REPLACED A S PER SRM 51-31-01 VOL II REV 40. 2 L 7 3 4F RT A22WE 20080915 2008 9 15 UPS08M53117 4 20080817 A 2565 SLIDE DOUG MD11 MD11F 3023600 NM L1 DOOR MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 SLIDE REMOVED DUE TO NOT ABLE TO DISARM SLIDE WITH INSIDE OR OUTSIDE ARMING HANDLE. FOUND AFT ARMING LATCHING CATCHING ON INSPECTION VIEWING WINDOW AT BOTTOM OF LWR COVER. ADJUSTED VIEWING WINDOW AND REINSTALLED L1 SLIDE ASSY IAW AMM 25-6 1-15-4. OK FOR SERVICE CLEARS M382494. VERIFIED SAFETY PIN AND STOWED PRESSURE AND DATE GOOD. 2 L 7 3 4F RT A22WE 20080915 WP 2008 9 15 UPS08853131 1 20080731 A 5720 FITTING DOUG DC8 DC871F 302199D WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 NR 1 ALT Z-FITTING IS CRACKED. REMOVED Z-FITTING IAW SRM 51-01-20D. FABRICATED AND INSTALLED REPLAC EMENT FITTING IAW DWG 364046, SRM 51-01-20D. 2 L 7 4 4F RT 4A25 20080915 NM 2008 9 15 UPS08M53140 1 20080807 A 5754 SKIN DOUG MD11 MD11F 3023600 NM LT WING SLAT DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:C LT WING NR 6 SLAT EXTERIOR SURFACE FOUND DENTED AT 40.5 INCHES FROM I/B END AND 30.5 FROM T/E. LT WIN G NR 6 SLAT EXTERIOR SURFACE DENTED AREA MEASURED DEPTH 0.037 INCH AND FOUND EXCEED LIMIT AS PER SRM 57-10-00 FIG 16 VOL I REV 40. DENT AREA TRIM-OFF, HFEC INSP & NO CRACK EVIDENT. REPAIR PARTS FABRICATED AND INSTALLED AS PER SRM 57-10-00 FIG 5 VOL I REV 40. 2 L 7 3 4F RT A22WE 20080915 EA 2008 9 15 SWIA200819970 1 20080821 A 3520 OXYGEN MASK CNDAIR CL600 CL6002C10 1390015 EA LAVATORY UNWANTED DEPLOY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 368CA 10075 THE O2 MASK DEPLOYED IN FORWARD LAV. FLIGHT 3800. RESTOWED O2 MASK PER MM 35-20-00. 2 L 7 2 4F RT A21EA 20080915 SO 2008 9 15 SWIA200819971 1 20080812 A 7500 DUCT EMB 120 EMB120ER 3260203 SO LT BLEED SYS LEAKING A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 216SW 120285 RECEIVED A DUCT LEAK WARNING ON CLIMBOUT. SHUT DOWN LEFT ENGINE AND RETURNED TO FIELD. FLIGHT 3634. REPLACED LEFT ENG INE BLEED DUCT IAW 36-10-01. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080915 NM 2008 9 15 SWAA084779 1 20080828 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 214WN 32486 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20080915 2008 9 15 SWAA084783 4 20080828 A 2565 61621469 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED MV2 CHECK, L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED E VAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 SWAA084784 1 20080828 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 807 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, STR 26L TO 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 SWAA084786 1 20080828 A 5340 6936600 STRINGER CLIP BOEING 737 7373T0 1384582 NM BS 277 S10R/L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R AND STR 10L. REMOVED AND REPLACED STRINGER C LIP PER SRM AND BOEING DRAWING. 2 L 7 2 4F RT A16WE 20080915 EU 2008 9 15 08FDEA03434 1 20080815 A 5340 A53974223214 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORRODED CLIP AT C 67, P 55-56 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080915 EU 2008 9 15 08FDEA03436 1 20080815 A 5720 A57244856201 SHROUD AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND DENT ON LEADING EDGE SKIN, RIB 29 RT REPAIR PERFORMED BY NDT FOR CRACK FREE CONDITION AND LET THE DENT AS IT IS IA W RAS/BAE/1007864/2008, APPROVED EA 6-5741-123064. 2 L 7 2 4F RT A35EU 20080915 NM 2008 9 15 08FDEA03588 1 20080826 A 5711 ARB74132 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 574FE 48499 RIGHT WING, TRAILING EDGE SPAR UPPER CAP AT STA XORS 675 FOUND 01 EACH FASTENER HOLE ELONGATED. REPAIR CARRIED OUT AS PER E.A. 1-5710-122430, THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080915 EU 2008 9 15 08FDEA03439 1 20080815 A 5310 A53810967200 DIAPHRAGM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND NICKS AND DENTS IN DIAPHRAGM, TRACK 1-2, RT REPAIR PERFORMED SMOOTH BLEND OUT OF THE NICKS, PERFORM NDT INSPECTION FOR CRACK FREE CONDITION AND LEAVE THE DENTS AS IS IAW RAS/70512735/014/2008ISS. A, APPROVED BY EA 6-5315-123080. 2 L 7 2 4F RT A35EU 20080915 EU 2008 9 15 08FDEA03440 1 20080815 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CHAFING MARKS ON LT INBOARD FLAP, RIB 11-12, TOP SKIN REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS, NDT FOR CRA CK FREE CONDITION IAW RAS/FOK/228/2008 ISS A, APRROVED BY EA 6-5752-123079. 2 L 7 2 4F RT A35EU 20080915 NM 2008 9 15 08FDEA03592 1 20080826 A 5311 AFA00183 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 574FE 48499 MAIN DECK FRAME AT LEFT STA 1741 APPROXIMATELY LONGERON 11 TO LONGERON 12 FOUND WITH DENT. CARRIED OUT REPAIR AS PER SRM 53-30-00, FIGURE 1 VOLUME I. DUE TO CATEGORY B REPAIR, INITIAL INSPECTION TO BE CARRIED OUT AT 14,000 CYCLES AND THE REAFTER REPETITIVE INSPECTIONS AT EVERY 9,500 CYCLES. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 08FDEA03716 1 20080903 A 5311 146N1018 FRAME BOEING 757 75723A 1384967 NM STA 1540 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 MAIN CABIN, STA 1540, STR 11-13L FRAME HAS DRILL STOP. REMOVED STANDOFF IAW SRM 51-40-02, REMOVED DAMAGED FRAME IAW SRM 53-00-07 STEP 1 SHEET 1 REPAIR NR 3. RECEIVED NEW CHANNELS ON TRAVELER NR T8/755741 AND T8/755739. INSTALLED NEW REPA IR CHANNELS IAW SRM 53-00-07 REPAIR NR 3. REPAIR IS CATEGORY B REPAIR REF SRM 53-00-07 PG 201 REPAIR 3 PER NOTED. DO T HE INITIAL INSP BEFORE ACCUMULATION OF 10,000 FLT CYCLES AFTER THE REPAIR. 2 L 7 2 4F RT A2NM 20080915 WP 2008 9 15 08FDEA03717 1 20080903 A 2910 7G10471 PRESSURE SWITCH DOUG MD10 MD1010F 3022112 WP ENGINE FUEL FAILED A FDEA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 367FE 46605 DURING CLIMB-OUT, ABOVE 10,000 FT, RECEIVED LEVEL 1 HYD 2 OFF ALERT WITH SUBSEQUENT SHUTDOWN OF LT AND RT NR 2 ENGINE D RIVEN PUMPS. DURING APPROACH AND LANDING RMP'S REPRESSURIZED SYSTEM AND ACCOMPLISHED NORMAL FLAPS 35 LANDING. GVI DP INDICATORS ON NR 2 ENG HYD FILTER PCKG, NO FAULTS. REMOVED AND REPLACED NR 2 ENG RT PMP L PRESS SWITCH IAW 29-31-02-2 LK CK AND OPS CK NORMAL. PERFORMED HSC ADJ AND TEST IAW AMM 29-08-01-5 OPS CK NORMAL. PEFORMED AUTO FUNCTION OF NR 2 EDP'S IAW AMM 29-11-01-2 OPS CK NORMAL. REMOVED AND REPLACED ENG 2 LOW PUMP PRESS RELAY PRECAUTIONARY. CLOSED NR 2 EN G FAN COWL IAW AMM 71-00-00-2. 2 L 7 3 4F RT A22WE 20080915 WP 2008 9 15 08FDEA03168 1 20080730 A 5522 ALC730590 SKIN DOUG MD10 MD1010F 3022112 WP RT ELEVATOR CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 233FE 46610 RIGHT OUTBD ELEVATOR L/E BULL NOSE LOWER SURFACE IS CHAFED AT STA XE 400 TO 482 REMOVED RUB STRIP IAW DC/MD-10 SRM 55-21 -01; VOL II. ALODINED AND PRIMED NEW RUB STRIP IAW SRM 51-21-01; VOL II. INSTALLED NEW RUB STRIP IAW SRM 55-21-01; VO L II. RIGHT OUTBD ELEVATOR WAS DISPLACED TO ACCESS PANEL REMOVAL AND REINSTALLATION AND PERFORMED A BINDING AND GAP CHE CK WITH NO DEFECTS IAW AMM 27-30-02-4. 2 L 7 3 4F RT A22WE 20080915 EU 2008 9 15 08FDEA03179 1 20080730 A 5315 A5378196620000 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CABIN FLOORBEAM AT FRAME 30 IS CRACKED AT THE VERTICAL STIFFENER BETWEEN Y- 450 AND Y-953. REPAIRED FLOORBEAM IAW SRM 53-10-15; FIG 212. 2 L 7 2 4F RT A35EU 20080915 NM 2008 9 15 08FDEA03719 1 20080904 A 5330 655457534 SKIN BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 SCRIBE MARKS IN FUSELAGE SKIN BS 720 6 INCHES BETWEEN STR 23 RT AND 24 RT. FOUND AREA OUT OF LIMITS IAW SRM 53-30-01 FI G 1. CUT OUT DAMAGED AREA DIMS 3 INCH BY 2 INCH IAW SRM 51-6-01 AND 53-30-03 FIG 1. FABRICATED DOUBLER IAW SRM 53-30-0 3 FIG 2. FABRICATED FILLER IAW SRM 53-30-03 FIG 2. INSTALLED REPAIR PARTS IAW SRM 51-30-02 AND 53-30-03 FIG 2. 2 L 7 3 4F RT A3WE 20080915 EU 2008 9 15 08FDEA03291 1 20080806 A 5230 B5327027802000 PANEL AIRBUS 300 A300F4605R 3930327 EU CARGO DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DOOR PANEL NR 251 WHM IS CRACKED AND PUNCTURED. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; RE V "G". 2 L 7 2 4F RT A35EU 20080915 WP 2008 9 15 08FDEA03381 1 20080812 A 5410 AUB7063 ACCESS PANEL DOUG DC10 DC1010 3022110 WP NR 3 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 AFTER REMOVAL ACCESS PANELS OF PYLON NR 3 WITH OAN J/C 0600B430-1JR FOUND CRACK ON HORIZ WEB UPPER. REPAIRED CRACK IAW SRM 54-00-01 FIG 2B SHT 2 VOL I. 2 L 7 3 4F A22WE 20080916 EU 2008 9 16 08FDEA03134 1 20080729 A 5347 A5378197520900 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 CABIN SEAT TRACK HAS A GOUGE BETWEEN FRAMES 27 AND 28, RBL 87 INCH. REMOVED THE DAMAGED SECTION OF SEAT TRACK AND INSTA LLED THE NEW SECTION AND SPLICES IN REF TO SRM 53-10-16; FIG 201; 201A AND SRM 51-40-21, PARA 7; AND DWG A53781941. AL ODINED, PRIMED AND TOP COATED IAW AMM 51-27-00-0. REMOVED AND RE-INSTALLED CEILING PANEL 132 EC IN REF TO AMM 25-13-11- 4. 2 L 7 2 4F RT A35EU 20080916 WP 2008 9 16 08FDEA03166 1 20080730 A 5420 AUL70477 SUPPORT BRACKET DOUG MD10 MD1010F 3022112 WP NR 1 PYLON GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 NR 1 ENGINE PYLON, THROTTLE INTERLOCK ACTUATOR AFT SUPPORT BRACKET IS GOUGED. REMOVED DIRECTIONAL PILOT VALVE PUSH ROD IAW MD-10-10 AMM 76-10-03-02. REMOVED, FABRICATED AND INSTALLED AUL 7047-7 SUPPORT IN REF TO DAC DWG AUL 7047, REF "F" . ALODINED AND PRIMED IN REF TO DC/MD-10 SRM 51-21-01; VOL II. INSTALLED THE PUSH ROD IAW FEDEX MD-10-10 AMM 76-10-03 -02. 2 L 7 3 4F RT A22WE 20080911 NM 2008 9 11 08FDEA03657 1 20080831 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 594FE 48552 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTI NG AT HOLES A AND B. MAIN CARGO DOOR LOWER JAMB, CRACKED NR 2 SUPPORT FITTING R & R AS PER SRM 51-31-01 VOLUME II. RE PAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080911 NM 2008 9 11 08FDEA03660 1 20080831 A 5320 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 594FE 48552 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NO.4 SUPPORT FIT TING AT HOLES A, C AND D. 2 L 7 3 4F RT A22WE 20080911 NM 2008 9 11 08FDEA03661 1 20080831 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 594FE 48552 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTI NG AT HOLES A, B, C AND D. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJ OR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080911 NM 2008 9 11 08FDEA03458 1 20080817 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM DOOR FRAME CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 DURING OPEN HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NO. 1 FOUND WI TH CRACK INDICATIONS AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB CRACK SUPPORT FITTING #1 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080911 EU 2008 9 11 08FDEA03672 1 20080901 A 5712 A57240457200 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CHAFING MARKS ON RT WING TRAILING EDGE AREA ON RIB FOR ASA ATTACHMENT. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS , PERFORM NDT FOR CRACK FREE CONDITION IAW. RAS/BAE/1007863/2008 ISS.A , APPROVED BY EA 6-5751-1230 63 2 L 7 2 4F RT A35EU 20080911 EU 2008 9 11 08FDEA03673 1 20080901 A 5310 A53970890200 DOOR FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND SCRUB MARKS AT EMERGENCY EXIT C 55 AND C 57.2, P14-15 LT AND C 55, P 14-15 RT. REPAIR PERFORMED BY BLEND OUT , N DT FOR CRACK FREE CONDITION IAW RAS/EFW/9000079/2008 ISS.A, APPROVED BY EA 6-5316-123070, 2 L 7 2 4F RT A35EU 20080911 EU 2008 9 11 08FDEA03674 1 20080901 A 5310 A53970889200 DOOR FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND SCRUB MARKS AT EMERGENCY EXIT C 57.2, P14-15 LT REPAIR PERFORMED BY BLEND OUT , NDT FOR CRACK FREE CONDITION IAW. RAS/EFW/9000080/2008 ISS.A, APPROVED BY EA 6-5316-123071. 2 L 7 2 4F RT A35EU 20080911 EU 2008 9 11 08FDEA03675 1 20080901 A 5310 A53970890201 DOOR FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND SCRUB MARKS AT EMERGENCY EXIT C 55, P14-15 RT. REPAIR PERFORMED BY BLEND OUT , NDT FOR CRACK FREE CONDITION IAW RAS/EFW/9000086/2008 ISS.A, APPROVED BY EA 6-5316-123092. 2 L 7 2 4F RT A35EU 20080911 WP 2008 9 11 08FDEA03639 1 20080829 A 5753 ARC0747503 PANEL DOUG MD10 MD1010F 3022112 WP LT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING OUTBOARD FLAP; INBOARD FAIRING; OUTBOARD SIDE PANEL 535 DL IS CHAFED ON THE INNER SKIN. BLENDED GOUGE; FOUND TO BE OUT OF LIMITS; PREPPED AREA FOR REPAIR; TREATED 7 PRIMED; FABRICATED DOUBLER; LATED UP HOT BOND REPAIR & CURED; S EALED EDGES & PRIMED AREA IAW DC/MD-10 SRM 57-00-01; VOL I & SRM 51-71-00; VOL II. 2 L 7 3 4F RT A22WE 20080911 EU 2008 9 11 08FDEA03707 1 20080902 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD FH1114 664 FOUND SEVERAL DENTS AND IMPACTS ON RT INBOARD FLAP, LOWER SURFACE THREE DOUBLER REPAIRS (RIB 9-11, 12-16, 12-15) WERE PE RFORMED IAW RAS/FOK/233/2008 ISS.C, APPROVED BY EA 6-5752-123073. 2 L 7 2 4F RT A35EU 20080911 NM 2008 9 11 08FDEA03517 1 20080820 A 5754 ARB11271 SKIN DOUG MD11 MD11 3023602 NM LT WING SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 LEFT WING - NR 6 LEADING EDGE SLAT OUTBOARD TRACK CUTOUT CORNER FOUND SUSPECTED CRACK. LEFT WING NR 6 LEADING EDGE SLAT OUTBOARD TRACK CUTOUT OUTBOARD CRACKED CORNER TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I . REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080912 EA 2008 9 12 SWIA200819978 1 20080820 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX BINDING A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 417SW 7400 CREW COULD NOT OPEN MAIN CABIN DOOR FROM OUTSIDE. INSPECTED AND OPERATED MAIN CABIN DOOR SEVERAL TIMES. OPS CHECK GOOD . 2 L 7 2 4F RT A21EA 20080912 NM 2008 9 12 SWAA084749 1 20080827 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERVICE DOOR LOWER HINGE. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080912 NM 2008 9 12 SWAA084762 1 20080827 A 5322 6546543 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 727D S26L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020400096 20080204 00096 WP 2008 2 4 AALA200800058 1 20080112 A 2560 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 258AA 49288 LGA - EMERGENCY FLASHLIGHT AT AFT GALLEY CHARGE LIGHT INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT AT AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020400098 20080204 00098 NM 2008 2 4 AALA200800050 1 20080110 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHT AT SEAT 22C HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008020400160 20080204 00160 EA 2008 2 4 TRAX200800099 1 20080115 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 933EV 8022 FLAP FAIL AT ZERO ON APPROACH FIRE TRUCKS REQUESTED TO BE ON STANDBY AS A PRECAUTION. FLTS 4336, 4455 CX. 2 L 7 2 4F RT A21EA 2008020400161 20080204 00161 EA 2008 2 4 TRAX200800100 1 20080116 A 5210 STEP CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 PAX DOOR LOWER STEP BROKEN. 2 L 7 2 4F RT A21EA 2008020400165 20080204 00165 NM 2008 2 4 ERAA200800001 1 20080119 A 3233 10500103 ACTUATOR DHAV DHC8 DHC8106 2809020 NM MLG CRACKED A ERAA O OTHER K FLUID LOSS LD LANDING 1 AL 03 883EA 5950 260 NR 2 HYD SYSTEM PRSR DROPPED TO ALMOST ZERO UPON GEAR EXTENSION. LOUD BANG & NR 2 HYD ISO VALVE CAUTION LIGHT AND OUTBO ARD ROLL SPOILER LIGHT ILLUMINATED. LEFT MLG RETRACT ACTUATOR HOUSING CRACKED. REMOVED AND REPLACED LEFT MLG RETRACT A CTUATOR. 2 H 7 2 4T RT A13NM 2008020400168 20080204 00168 EA 2008 2 4 TRAX200800110 1 20080118 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 750EV 10161 ALL FORWARD EMERGENCY LIGHTS INOP. 2 L 7 2 4F RT A21EA 2008020400169 20080204 00169 2008 2 4 TRAX200800111 4 20080119 A 3450 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA FALSE INDICATION A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 878AS 7590 RECEIVED MULTIPLE EFIS COMP MON ON TAXI AND TAKEOFF. AT 12000 LOST FMS, AHRS; UNABLE TO FLY GREEN NEEDLES FOR 10 MINS. ABLE TO RETRIEVE GREEN NEEDLE CAPABILITY AFTER 10 MINS. A/C RETURNED TO ATL AFTER T/O. PILOT CANCELLED EMERGENCY DECL ARED/TOWER ROLLED EMERGENCY VEHICLES AS A PRECAUTION. 2 L 7 2 4F RT A21EA 2008020400171 20080204 00171 EA 2008 2 4 TRAX200800113 1 20080119 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 ASD FWD ANCHOR FITTING SERRATED PLATES CORRODED. 2 L 7 2 4F RT A21EA 2008020400173 20080204 00173 SO 2008 2 4 C2XA08IA028 1 20080120 A 3397 7287501601 WIRE HARNESS EMB 145 EMB145LR 3260212 SO SIDEWALL LIGHT BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 13992 145284 MAF - FLIGHT 2179 THE CREW REPORTED AN ELECTRICAL BURNING ODOR AT ROW 6 AND 7. THE AIRCRAFT LANDED AT MAF WITHOUT INCID ENT WHERE CONTRACT MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE SIDEWALL LIGHT AT ROW 6/7 ON MEL 33-20-00/1 CAT C C TL NR 137792, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 01/22/08 THE AIRCRAFT RON'D AT EWR WHERE MAINTENA NCE REMOVED AND REPLACED THE LIGHT ASSEMBLY HARNESS AT ROW 6/7, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008020400179 20080204 00179 EA 2008 2 4 TRAX200800118 1 20080120 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 27 975EV 7599 FLAP FAIL AT ZERO. EMERGENCY DECLARED - EN ROUTE TO SCE, A/C DIVERTED TO MDT DUE TO MTC. FLT 9951 DEL 109 MINS. 2 L 7 2 4F RT A21EA 2008020500004 20080205 00004 NE 2008 2 5 HALA0800027 2 20080128 A 7200 EN131 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NR 1 FAILED A HALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 WP 13 481HA 55126 13170 AIR TURN BACK AT KOA STATION DUE LOUD BANG, ENGINE SHUTDOWN, TGT 1149.5 DEGREES. PERFORMED CHECK LIST AND FIRED 1 FI RE BOTTLE. RETURN TO AIRPORT. REMOVED NR 1 ENGINE PER M144-717 REF LG PG 216722/75. INSTALLED NR 1 ENG PER HALM 143-717 GROUND RUNUP & LEAK CHECK OKAY. 2 L 7 2 4F 4 F TR A6WE E00061EN 2008020500006 20080205 00006 NM 2008 2 5 08FDEA00321 1 20080129 A 5310 CREASE BEAM BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 BS 1260, LBL 63, WL 208, CREASE ANGLE HAS CORROSION. REMOVED CORROSION ON CREASE ANGLE IAW SRM 53-60-13, FIG 101, DETAI L VIII, FOUND TO BE OUT OF LIMITS PER SRM 53-60-13, FIG 101. REMOVED AND REPLACED CREASE ANGLE FROM BS 1180 TO 1290 W ITH NEW CREASE ANGLE, IAW SRM 53-60-13, 51-40-02 AND 51-10-02. THIS IS A CATEGORY "A" REPAIR. 2 L 7 2 4F RT A2NM 2008020600001 20080206 00001 NM 2008 2 6 SWAA080531 1 20080130 A 3350 OL3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 2 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008020600002 20080206 00002 NM 2008 2 6 2008UALA00323 1 20080118 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 880 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 UPPER FUSELAGE DORSAL FIN SEAL CONTACT AREA AT STA 880 HAS EXCESSIVE MATERIAL LOSS. INSTALLED A DOUBLER AND TRIPLER REP AIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600003 20080206 00003 NM 2008 2 6 USAA920080206 1 20080112 A 5320 6916970501 ANGLE BOEING 737 7373Y0 1384671 NM BS 348 S15L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED L1 DOOR CUTOUT INTERCOSTAL ANGLE, BS 348.2, S15L. REPLACED L1 DOOR CUTOUT INT ERCOSTAL ANGLE, BS 348.2, S15L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600004 20080206 00004 SO 2008 2 6 C2XA08CL015 1 20080128 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12564 145618 CLE FLIGHT 2932 - THE CREW REPORTED LAV SMOKE DETECTOR OPERATION INTERMITTENT. MAINTENANCE INSPECTED AND PERFORMED OPE RATIONAL CHECKS ON THE LAV SMOKE DETECTOR AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008020600006 20080206 00006 NM 2008 2 6 USAA920080264 1 20080103 A 5347 SEAT TRACK BOEING 767 7672B7ER 1385107 NM BS 999-1065 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 999 - BS 1065, LBL 11. REPLACED CABIN SEAT TRA CK, BS 999 - BS 1065, LBL 11 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008020600007 20080206 00007 EA 2008 2 6 COMA0860044 1 20080102 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 806CA 7359 FLIGHT 5610 - FLAPS FAIL CAUTION MESSAGE ON APPROACH TO DCA. AIRCRAFT DIVERTED TO IAD AND LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 2008020600016 20080206 00016 NM 2008 2 6 200801233 1 20080121 A 3810 9631760001 FITTING EMB ERJ170 ERJ170100SE 3260406 NM POTABLE WATER CRACKED A UHLA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 11 654RW 17000104 FLIGHT 7702 DEN TO YYZ ON DESCENT THE AUTO PILOT KICKED OFF AND THE AIRCRAFT WAS HARD TO TURN. THE AILERONS FELT AS IF THEY WERE STUCK AND WERE GETTING PROGRESSIVELY WORSE. PILOT DECLARED AND EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTE NANCE LOCATED A POTABLE WATER LEAK WHICH FILLED THE BELLY OF THE AIRCRAFT WITH ICE CAUSING BINDING OF THE AILERON CONTRO L CABLES. ON-CALL MAINTENANCE THAWED THE ICE, DRAINED THE WATER AND REPLACED CRACKED POTABLE WATER T-FITTING. 2 L 7 2 4F RT A56NM 2008020600023 20080206 00023 NM 2008 2 6 SWAA080536 1 20080130 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 520 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020600024 20080206 00024 NM 2008 2 6 SWAA080537 1 20080130 A 3350 OL3071BPEGPL LAMP BOEING 737 7373L9 1384470 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 22Y CHECK, FOUND EEPLS INOP AT ROW 18 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008020600027 20080206 00027 NM 2008 2 6 USAA920080209 1 20080113 A 5320 69353654 ANGLE BOEING 737 7373Y0 1384671 NM BS 380-400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED MAIN CABIN FLOOR STRUCTURE SHEAR WEB ANGLE, BS 380- BS 400, BL 0, WL 208. RE PLACED MAIN CABIN FLOOR STRUCTURE SHEAR WEB ANGLE, BS 380- BS 400, BL 0, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600028 20080206 00028 NM 2008 2 6 USAA920080210 1 20080113 A 5340 69414372 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 663 S10R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED STRINGER CLIP, BS 663, S10R. REPLACED STRINGER CLIP, BS 663, S10R IAW B737 SR M 51-40-02. 2 L 7 2 4F RT A16WE 2008020600042 20080206 00042 NM 2008 2 6 SWAA080510 1 20080129 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 500D S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER 27L CORRODED AT BS 500D. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008020600043 20080206 00043 NM 2008 2 6 SWAA080511 1 20080129 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500 S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 18R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020600051 20080206 00051 NM 2008 2 6 2008UALA00306 1 20080117 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 867 S20R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 AFT PIT BS 867 STRINGER CLIP AT S20R CRACKED. MAJOR REPAIR: REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600056 20080206 00056 SO 2008 2 6 C2XA08IA035 1 20080125 A 3234 7455503 CONTROL LEVER EMB 145 EMB145XR 3260214 SO MLG INOPERATIVE A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 21129 19484 19484 145703 IAH - FLIGHT 2365, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE WARNING ILLUMINATED INFLIGHT WHILE THE LANDING GEAR W AS IN UP AND LOCKED POSITION. NORMAL INDICATIONS ACHIEVED WHEN GEAR WAS LOWERED. THE AIRCRAFT LANDED AT IAH WITHOUT IN CIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008020600057 20080206 00057 SO 2008 2 6 C2XA08IA034 1 20080129 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO FWD GALLEY SMOKE A C2XA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 27 11181 14500904 SLC - FLIGHT 7676, THE CREW REPORTED SMOKE COMING FROM THE FORWARD OUTBOARD GALLEY. THE INITIAL INDICATION WAS FROM LAV SMOKE, WITH THE SMOKE BEING BLUE IN COLOR AND HAVING AN ELECTRICAL ODOR. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT A ND MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE ENGINE & APU BLEED, PACKS SYSTEMS, ALL WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008020600060 20080206 00060 NM 2008 2 6 200802041 1 20080202 A 3260 LANDING GEAR EMB ERJ170 ERJ170100SE 3260406 NM LEFT WARNING MESSAGE A UHLA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 11 638RW 17000053 FLIGHT 7503 JFK TO IAD - ON APPROACH CREW SELECTED GEAR DOWN AND RECEIVED A RED "LG LEVER DISAGREE" MESSAGE ASSOC WITH A RED UP INDICATION ON THE LEFT MAIN. CREW ALSO RECEIVED A CYAN "BRAKE CONTROL FAULT" MESSAGE ASSOCIATED WITH THIS CONDI TION. ONCE ON THE RUNWAY HEADING THE CREW CYCLED THE GEAR 2 TIMES AND IT WORKED NORMALLY BOTH TIMES. THE CREW LANDED W ITHOUT INCIDENT. MAINTENANCE INSPECTED UPLOCK AND DOWNLOCK PROX SENSORS AND HARNESSES ON LT MLG, NOW DEFECTS NOTED. MA INT OBSERVED PSEM PARAMETERS ON DIAGNOSTIC PAGE OF CMC, NO DEFECTS NOTED. CMC NEVER SHOWED ANY ACTIVE EICAS MSG'S. HAS NOT REPEATED THIS DATE 02/04/2008. 2 L 7 2 4F RT A56NM 2008020100027 20080201 00027 NM 2008 2 1 KCSA081037 1 20080123 A 5347 SEAT TRACK BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 CAPTAIN'S I/B, AFT SEAT TRACK CRACKED ON WEB AT AFT END AT BS 540, LBL 20. 2 L 7 4 4F RT A20WE 20080912 EA 2008 9 12 SWIA200820002 1 20080829 A 2711 TRIM SYSTEM CNDAIR CL600 CL6002C10 1390015 EA AILERONS STUCK A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 702SK 10136 AILERON TRIM WOULD NOT MOVE RIGHT WING DOWN. FLT 6111. REPLACED AILERON/RUDDER TRIM PANEL IAW 27-12-4. OPS CHECKS GOO D IAW 27-11-00 AND 27-22-00. P/N: CC670-51114-3. 2 L 7 2 4F RT A21EA 20080912 SO 2008 9 12 SWIA200819994 1 20080825 A 2621 CARTRIDGE EMB 120 EMB120ER 3260203 SO APU FIRE BOTTLE MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 292UX 120292 APU FIRE BOTTLE "INOP" LIGHT IS ON. FLIGHT 5783. REPLACED APU FIRE BOTTLE AND CARTRIDGE IAW MM 26-22-01. OPS TEST GOO D. P/N 899170-1, S/N OFF 15840EK, P/N 897776-01, S/N OFF 57597. 2 L 7 2 4T RT A31SO 20080915 NM 2008 9 15 08FDEA03160 1 20080730 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL ACCESS PANEL CUTOUT 543BB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV, 93 REPAIR 5. REPAIR IS CLASSIFI ED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080915 NM 2008 9 15 08FDEA03215 1 20080802 A 5711 SPAR BOEING 757 75727B 1384921 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 916FD 24137 UNDOCUMENTED BLEND REPAIR FOUND ON THE AFT SIDE OF THE LT WING REAR SPAR WEB AT RSS 183. EVALUATE AND RECTIFY. LEFT WI NG REAR SPAR WEB CORROSION BLEND REPAIR CARRIED OUT IAW EA F-5710-118827 DATED MAY 24 2008. REPAIR IS CLASSIFIED AS MAJ OR PER GMM 6-02-100. 2 L 7 2 4F RT A2NM 20080915 NM 2008 9 15 08FDEA02654 1 20080703 A 3411 PITOT TUBE DOUG MD11 MD11F 3023600 NM OBSTRUCTED A FDEA C ABORTED TAKEOFF C J F.O.D. WARNING INDICATION TO TAKEOFF 1 CE 21 623FE 48794 ON TAKEOFF ROLL AIRSPEED INDICATORS DIFFERED BY 20 KNOTS REJECT T/O 04JUL08 09:12 TPE R. PERFORM PITOT TUBE PURGE ON AUX PITOT TUBE FOUND A BIG CLUNK OF MUD BLEW OUT THEN PERFORMED LEAK CHECK NORMAL PER MM 34-11-00-2. 2 L 7 3 4F RT A22WE 20080915 EU 2008 9 15 08FDEA03173 1 20080730 A 5347 A5378193620200 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CABIN SMALL LATERAL SEAT TRACK AT FRAME 30; LBL 56 INCH HAS A BROKEN SCALLOP. REMOVED SEAT TRACK ADAPTER IAW SRM 5 1-40-21. DRILLED AND COUNTERSUNK A NEW SEAT TRACK ADAPTER P/N A5378193620200, PO 627374.3 IAW A300-600 51-40-40. INSTA LLED SEAT TRACK ADAPTER IAW SRM 51-40-21; PARAGRAPH 7. APPLIED CIC IAW AMM 51-22-00-0. 2 L 7 2 4F RT A35EU 20080915 WP 2008 9 15 UPS08853086 1 20080727 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FS 1180 RBL14 CRUSHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 MAIN CABIN, FLOOR PANEL HAS CRUSHED HONEYCOMB STA 1180 RBL 14. REMOVED FLOOR PANEL IAW MM 53-21-02, FABRICATED AND INSTALLED REPLACEMENT PANEL IAW EO DC8-5320-9691C, AND MM 53-21-02. 2 L 7 4 4F RT 4A25 20080915 NM 2008 9 15 SWAA084772 1 20080827 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 277 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080915 2008 9 15 SWAA084754 4 20080827 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 UPS08M53102 1 20080802 A 5712 RIB DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:C LT WING LOWER WINGLET FWD RIB FOUND CRACKED AS MARKED. CRACKED REMOVED PER SRM 51-31-01 V2 R40. NEW RIB FAB PER BOEING DRAWING ARB7774 USING MATL 7075-0-0.040". RIB HEAT TREATED TO T6 PER DPS7.001 HARDNESS HRB80.1 PER D PS1.053. NEW RIB HOLES P/UP&NEW RIB PROTECTED PER SRM51-21-01 V2 R40. NEW RIB INSTALLED PER SRM 51-31-01 V2 R40. PAIN T TOUCH UP ON REPAIRED AREA PER SRM 51-21-02 V2 R40. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 UPS08553137 1 20080809 A 5210 LATCH BOEING 757 75724APF 1384969 NM PAX DOOR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 LWR CAM LATCH ON CREW ENTRY DOOR FWD FRAME IS GOUGED. BLENDED GOUGE ON CREW ENTRY DOOR LOWER LATCH CAM IAW SRM 51-10-02 . 2 L 7 2 4F RT A2NM 20080915 NM 2008 9 15 UPS08M53108 1 20080727 A 5730 ARB24342 SKIN PANEL DOUG MD11 MD11F 3023600 NM RT WING LE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 281UP 48538 INSPECTION TYPE:2C RT WING I/B FIXED L/E SKIN PANEL FOUND WITH CHAFE ON O/B EDGE CORNER JUST FWD OF PANEL 616HB. REMOVE D, FABRICATED AND INSTALLED RT WING I/B FIXED L/E SKIN PANEL IAW DWG ARB2434 AND MD-11 SRM 51-33-01 & 51-35-01. 2 L 7 3 4F RT A22WE 20080915 WP 2008 9 15 08FDEA03033 1 20080723 A 5412 AUB70803 RIB DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 NR 3 PYLON PANEL 487 CL HAS A CHAFED RIB. BLENDED RIB IAW SRM 54-00-01; VOL I. FOUND TO BE OUT OF LIMITS IAW SRM 54-00 -01; VOL I. LOCATED AND DRILLED HOLES IAW DWG AUB 7080; REV A. ALODINED AND PRIMED IAW SRM 51-21-01; VOL II. MARKE D PART AUB 7080-3 IAW GMM 7-0-1001. INSTALLED AUB 7080-3 IAW DWG AUB 7080, REV A. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 08FDEA03589 1 20080826 A 5320 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 574FE 48499 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTI NG AT HOLES A, B, C AND D. MAIN CARGO DOOR JAMB NR 6 SUPPORT FITTING REMOVE AND REPLACED AS PER SRM 51-31-01 VOL II. B USHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 08FDEA03591 1 20080826 A 5347 AFA7104521 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 574FE 48499 MAIN DECK SEAT TRACK AT STA 610, X = -8 FOUND CORRODED. CARRIED OUT REPAIR AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAI R CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080915 EU 2008 9 15 08FDEA03441 1 20080815 A 5740 A54611031201 FITTING AIRBUS 300 A300B4622R 3930312 EU RT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND OLD IMPACT MARKS ON INNER SURFACE OF RT PYLON TO WING LUG NEXT TO BRACKET A571-41040-001. REPAIR PERFORMED BY B LEND OUT THE MARKS TO SMOOTH CONTOUR , NDT FOR CRACK FREE CONDITION IAW RAS/BAE/1007776/2008 ISS A, APPROVED BY EA 6-572 0-123053. 2 L 7 2 4F RT A35EU 2008020100043 20080201 00043 NM 2008 2 1 CALA0800051 1 20080120 A 5312 655073333 STIFFENER BOEING 737 7373T0 1384582 NM LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 LEFT W/W UPPER PRESSURE BULKHEAD SUPPORT STIFFENER CRACKED JUST ABOVE GEAR UP LATCH AT STATION 706. REMOVED CRACKED ARE A, FABRICATED FILLER AND DOUBLER AND INSTALLED PER SRM 51-70-11. 2 L 7 2 4F RT A16WE 2008020100050 20080201 00050 NM 2008 2 1 CALA0800059 1 20080107 A 5320 6517688125 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76354 23592 L-1 ENTRY DOOR Z-ANGLE CORRODED. INSTALLED PER SRM 51-40-2. 2 L 7 2 4F RT A16WE 2008020100137 20080201 00137 EU 2008 2 1 MALA080014 1 20080128 A 5753 SKIN SAAB SF340 340B 7860101 EU T/E FLAP DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 SEVERAL DENTS IN RT FLAP UPPER SURFACE INCLUDING DENTS PARTIALLY COVERED BY 3 MOST OB CHAFE STRIPS REQUIRE MAPPING. REP AIRED DENT NR 12 IAW EO NR S51031. DENTS 1-11, 13-23 ACCEPTED AS IS IAW EO NR 57174. ENTERED INTO SCRATCH AND DENT LOG FROM CONTINUATION CARDS 091660 AND 091671. 2 L 7 2 4T RT A52EU 2008020100140 20080201 00140 EU 2008 2 1 MALA080018 1 20080128 A 3020 44730501 CONTROL MODULE SAAB SF340 340B 7860101 EU ANTI-ICE SYS MALFUNCTIONED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 15 402XJ 340B402 DURING CLIMB-OUT, RT ENGINE INTAKE LIGHT ILLUMINATED, WITH A STRONG SMELL OF MELTING RUBBER. THE F/O NOTICED GLOWING IN THE INTAKE. TURNED THE RT INTAKE SWITCH OFF, GLOWING WENT AWAY AND SMELL DISSIPATED. FOUND RT LOWER DUCT TO HAVE BURN SPOT. REMOVED AND REPLACED THE LOWER DUCT (INLET FWD) IAW AMM 71-60. REMOVED AND REPLACED RT DEICE CTRL MODULE IAW AC T MM 30-21, PN ON/OFF 44730-501, SN/ON A00491 SN/OFF A00632. DUCT PN ON/OFF NH24668-169, SN/ON L291146 SN/OFF L16236. OPS CHECK OF RT ENG INLET ANTI-ICE IAW MM 30-20, IS GOOD. 2 L 7 2 4T RT A52EU 2008020100189 20080201 00189 2008 2 1 HALA0800028 4 20080129 A 3416 06650007010 ALTIMETER BOEING 767 7673G5 1385126 NM COCKPIT MALFUNCTIONED A HALA K NONE O OTHER CR CRUISE 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, RA FLAG DISPLAYED INTERMITTENT ON THE CAPT ADI. REMOVED AND REPLACED LT RADIO ALTIMETER PER A MM 34-33-01, SYSTEM TEST NORMAL. ACCOMPLISHED MCDP TEST NR 30 PER AMM 22-00-02, TEST PASSED. AIRCRAFT RETAINS LMP STAT US LAND 3. 2 L 7 2 4F RT A1NM 2008020400024 20080204 00024 EU 2008 2 4 AALA200800039 1 20080106 A 5340 FITTING AIRBUS 300 A300B4605R 3930308 EU MLG WW BROKEN A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 14061 471 SJU INFLIGHT T1480/06JAN - WHEN RETRACTING LANDING GEAR CREW HEARD A LOUD NOISE FOLLOWED BY NOSE GEAR DOOR AMBER LIGHT. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR UPLOCK ACTUATOR ATTACHMENT FITTING. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008020400067 20080204 00067 EA 2008 2 4 SWIA200819142 1 20080124 A 7120 BEARING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 954SW 7815 ENGINE MOUNT LINK BEARING AND BUSHING HAS CORROSION. REPLACED FORWARD ENGINE MOUNT LINK IAW AMM 71-21-01, PN/OFF 600-37 016-5/00, SN/OFF 0066. 2 L 7 2 4F RT A21EA 2008020400099 20080204 00099 NM 2008 2 4 AALA200800070 1 20080114 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 945AN 30085 TUL - EMERGENCY SEAT MOUNTED LIGHTS AT RIGHT SEAT ROWS 22 TO 28 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY SEAT M OUNTED LIGHTS AT RIGHT SEAT ROWS 22 TO 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008020400182 20080204 00182 EA 2008 2 4 TRAX200800084 1 20080111 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 843AS 7310 RIGHT FS 625 OBLIQUE ANGLE IS CRACKED. REMOVED CRACKED RIGHT FS 625 OBLIQUE ANGLE. LOCATED NEW OBLIQUE ANGLE P/N 601-3 5012-52, IAW CRJ SRM 51-40-11. OK TO INSTALL. INSTALLED OBLIQUE ANGLE IAW CRJ SRM 51-42-21 AND REO 601R-53-61-985. OK TO TOP COAT FASTENERS FINISH A023. APPLIED FINISH A023 TO FASTENERS IAW CRJ SRM 51-21-16. SUPPLEMENTAL SDR CLOSED 1/2 3/08. 2 L 7 2 4F RT A21EA 2008020600008 20080206 00008 EA 2008 2 6 COMA0860054 1 20080107 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 815CA 16631 7397 FLIGHT 4982 - NOSE GEAR DISAGREE ON APPROACH INTO CVG. PERFORMED QRH, EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMO VED AND REPLACED NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2008020600029 20080206 00029 NM 2008 2 6 USAA920080211 1 20080113 A 5340 69414371 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 6663 S10L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED STRINGER CLIP, BS 663, S10L. REPLACED STRINGER CLIP, BS 663, S10L IAW B737 SR M 51-40-02. 2 L 7 2 4F RT A16WE 2008020600041 20080206 00041 NM 2008 2 6 SWAA080509 1 20080129 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 500 S26L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 26L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020600061 20080206 00061 2008 2 6 200802042 4 20080131 A 3140 70265421901 PROCESSOR EMB ERJ170 ERJ170100SE 3260406 NM MAU 1 FAULTED A UHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 642RW 6935 17000063 FLIGHT 7539 ORD TO IAH CREW REPORTS AN AVNX MAU 1A FAIL IN FLIGHT. DIVERTED TO DSM, DECLARED EMERGENCY, LANDING WAS NOR MAL, WITHOUT NOSE WHEEL STEERING. MAINTENANCE RESET AIRCRAFT POWER AND CLEARED AVNX MAU 1A FAIL MSG. NO HISTORY AND NO CORRELATIONS. SUSPECT NR 1 NIC/PROC IN MAU 1(NIC/PROC 1) AS THE PROBLEM SI: 314024 WRITTEN FOR AVNX MAU 1A FAIL MESSAG ES IN THE FHDB. SUSPECT NR 1 NIC/PROC IN MAU 1 (NIC/PROC 1) AS THE PROBLEM. SI ACCOMPLISHED ON 02/03/2008. 2 L 7 2 4F RT A56NM 2008020600062 20080206 00062 EA 2008 2 6 COMA0860047 1 20080102 A 2750 1104SD100201 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA LT TE FLAPS WORN A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 806CA 7359 FLIGHT 5636 - FLAPS FAIL CAUTION MESSAGE ON APPROACH INTO BOS. EMERGENCY DECLARED AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED LEFT SIDE NR 2 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2008020600072 20080206 00072 NM 2008 2 6 MWEA080013 1 20080123 A 3222 STRUT BOEING 717 717200 1383700 NM NLG DISCHARGED A MWEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 13 922ME 55184 THE NOSE GEAR DID NOT RETRACT FOR TWO MINUTES, RED NOSE GEAR UNSAFE LIGHT ILLUMINATED. SERVICED NOSE LANDING GEAR SHOCK STRUT AND DID NITROGEN SERVICING. 2 L 7 2 4F TR A6WE 2008020600077 20080206 00077 SO 2008 2 6 C2XA08SH016 1 20080202 A 5322 14525175001 SHEAR TIE EMB 145 EMB145EP 3260221 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14945 145049 SHV - DURING C-CHECK SHEAR CLIP AT FR 65 HAS CORROSION. MX REPAIRED FR 65 SHEAR CLIP IAW EC 5330-01458. THE AIRCRAFT W AS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 20080915 EU 2008 9 15 08FDEA03442 1 20080815 A 5330 A53610265205 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 744FD 664 FOUND OLD DOUBLER ON FUSELAGE C 2-3, RT NOT IAW SRM 53-11-12 FIG 201. DOUBLER REPAIR RENEWED IAW SRM 53-11-12 FIG 201. 2 L 7 2 4F RT A35EU 20080915 NM 2008 9 15 08FDEA03443 1 20080815 A 5315 65208371 FLOORBEAM BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 MAIN CABIN BS 1110 LBL 65 AND LBL 45 FLOORBEAM UPPER FLANGE HAS CORROSION. REPAIRED MAIN CABIN FLOORBEAM UPPER FLANGE B S 1110 LBL 57 CUTOUT AREA DIMS 3 1/2 INCH BY 1 INCH, FABRICATED REPAIR ANGLES (2EA). FABRICATED FILLER. INSTALLED REPA IR PARTS AT BS 1110 FLOORBEAM IAW SRM 53-10-8 FIG 3 AND SRM 53-10-2 FIG 7. 2 L 7 3 4F RT A3WE 20080916 EU 2008 9 16 08FDEA03450 1 20080816 A 5730 R57249152 SKIN AIRBUS 310 A310203 3930313 EU LT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 430FE 394 SKIN AFT OF REAR SPAR LT AT RIB 11 HAS PREVIOUS .5 IN CRACK REPAIR REMOVED PREVIOUS DOUBLER AND RE-INSTALLED IAW FEDEX E A 6-5710-73485, REV NO B, POS PT, RELEASE DATE 11/14/03. 2 L 7 2 4F RT A35EU 20080916 NM 2008 9 16 08FDEA03448 1 20080816 A 5740 652165826 ATTACH ANGLE BOEING 727 7272S2F 1384O81 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 RT WING, LOWER T/E PANEL BELOW NR 13 SPOILER ACTUATOR I/B ATTACH ANGLE CRACKED. REMOVED AND REPLACED CHANNEL REF SRM 51 -30-5, SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080916 NM 2008 9 16 08FDEA03451 1 20080816 A 5753 652678722 FAIRING BOEING 727 7272S2F 1384O81 NM NR 6 FLAP TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 RT WING NR 6 FLAP TRANSMISSION FAIRING IS CRACKED AT CENTER ATTACH HOLE REMOVED FAIRING REF 51-30-2, PG 1-7 STOP DRILLED CRACKS REF 727 SRM 51-10-1 PG 13. NDT VERIFIED CRACK CONTAINMENT. NDT MANUAL PART 6, 51-00-00 FIG 23. ORIGINAL AND R EPAIR MATERIAL IDENTIFIED REF SRM 57-20-2, PG 15 FIG 5 AND SRM 57-20-4, PG 7. WITH SRM 51-20-1, PG 13, ALSO A-TAG NR A8 4324. FABRICATED NEW REPAIR DOUBLER REF SRM 51-20-1 FIG 7. TREATED AND PRIMED REPAIR DOUBLER. REF SRM 51-10-2 PG 1 -2 7. INSTALLED DOUBLER REF SRM 51-30-2 PG 1-7, TOP COATED DOUBLER REF MM 51-20-151-7. REINSTALLED FAIRING REF SRM 51-30- 0. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080916 EU 2008 9 16 08FDEA03452 1 20080816 A 5210 A52175004200 SKIN AIRBUS 310 A310203 3930313 EU AFT PAX DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 430FE 394 RT AFT CREW DOOR LOWER AFT CORNER HAS DENT 1.5 IN LONG BY 2 IN W BY .033 IN DEEP CUT OUT DAMAGE AND INSTALLED SKIN REPAI R ON RT AFT DOOR LOWER AFT CORNER IAW A310-200 SRM 52-10-00, FIG 204, PG 217/218. 2 L 7 2 4F RT A35EU 20080916 NM 2008 9 16 08FDEA03455 1 20080816 A 5310 6522419 BEAM BOEING 727 7272S2F 1384O81 NM MLG WW CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 LT MLG W/W UPPER BOX BEAM LOWER WEBS AFT OF STA 910 AND 930 HAVE CORROSION REMOVED FASTENERS FOR ACCESS. REMOVED CORROS ION, ORIGINAL .080 REMAINING .070. REMOVED .010 OUT OF LIMITS, FABRICATED REPAIR DOUBLER 7075-O-100 HEAT TREAT T6. APP LIED ALODINE AND PRIMER, INSTALLED DOUBLER AND FASTENERS REMOVED FOR ACCESS. REF SRM 53-10-1 PG 1-6A, 53-10-1 PG 6B,C, 51-10-6 PG 1 AND 5. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080916 EU 2008 9 16 08FDEA03735 1 20080905 A 5347 A5361164020000 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 MAIN CABIN SEAT TRACK AT C 17; RBL 38 IS CRACKED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-21; PARA 7 & SRM 5 1-40-44. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03736 1 20080905 A 5220 RETAINER AIRBUS 310 A310222 3930315 EU EMERGENCY EXIT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 RIGHT OVER WING EMERGENCY EXIT; LOWER SEAL RETAINER OUTBD SURFACE HAS CORROSION AROUND THE BOLT HEADS. RECLEANED THE LOWER SEAL RETAINERS & HARDWARE. NO DEFECTS NOTED. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03737 1 20080905 A 5220 RETAINER AIRBUS 310 A310222 3930315 EU EMERGENCY EXIT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 RIGHT OVERWING EMERGENCY EXIT, LOWER SEAL RETAINER OUTBD HAS THREE TEE FITTINGS WITH LIGHT CORROSION. REMOVED LOWER SEA L RETAINER TO FOM. IAW SRM 51-40-20. REMOVED THE LOWER CHANNEL AND FOUND IT TO BE CORRODED BEYOND LIMITS IAW SRM 53-10- 00. RECEIVED NEW LOWER CHANNEL, INSTALLED NEW LOWER CHANNEL IAW SRM 51-40-02. REMOVED & CLEANED TEE FITTING ; NO DE FECTS NOTED. RE-INSTALLED LOWER SEAL RETAINER IAW SRM 57-40-02. RE-INSTALLED TEE FITTINGS IAW SRM 51-40-02. REMOVED & RE-INSTALLED DOOR IAW AMM 52- 23-11-4. 2 L 7 2 4F RT A35EU 20080916 NM 2008 9 16 08FDEA03722 1 20080904 A 5320 AFS71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 574FE 48499 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTI NG AT HOLE A. MAIN CARGO DOOR LOWER JAMB NO. 2 FITTING CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE 10 VOL UME I AT HOLE A. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080916 NM 2008 9 16 08FDEA03724 1 20080904 A 5330 148N371088 SKIN BOEING 757 7572B7 1384964 NM BS 1941 S5\R DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 906FD 27148 APU COMPT RT SIDEWALL HAS 10 INCH BY 12 INCH DELAMINATION. REMOVED AND INSTALLED SERVICABLE APU COMPT SKIN IAW SRM 51-4 0-02,STA 1941. MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20080916 NM 2008 9 16 08FDEA03725 1 20080905 A 5315 651631543 FLOORBEAM BOEING 727 727227 1384078 NM BS 328 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 TOOL MARK AT FLOOR SUPPORT MAIN CABIN STA 328 TOP OF FRAME APROX 11" FROM I/B EDGE OF LWR SILL. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. CUTOUT DAMAGE AREA DIM 9 1/2 PER 2 INCH IAW B727 SRM 53-10-8 FIG 9. FABRICATED FILLER MAT USED 7075T6 0.071 AND 04 EA ANGLES MAT USED 7075T6 0.071 AND 02 EA SHIMS IAW B727 SRM 53-10-8 FIG 9. TREATED AND PRIMED AFFE CTED PARTS IAW B727 SRM 51-10-2. INSTALLED ALL REPAIR PARTS IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 20080916 NM 2008 9 16 08FDEA03727 1 20080905 A 5754 65216823 SKIN BOEING 727 727227 1384078 NM NR 1 SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 NR 1 SLAT TRAILING EDGE IS GOUGED AND CRACKED AT I/B HOOK WS 716 TRIMMED OUT DAMAGED AREA DIM 1/2 PER 1/2 IAW SRM 57-50- 3 FIG 10. FABRICATED REPAIR DOUBLER MAT USED 7075T6 0.125, DIM 4 INCH PER 3 1/2 INCH IAW SRM 57-50-3 FIG 10. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PART IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20080916 EU 2008 9 16 08FDEA03220 1 20080803 A 5310 A5378193720100 ADAPTER AIRBUS 310 A310221 3930310 EU ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 430FE 394 MDCC BETWEEN SEAT TRACK 2R AND 3R FRAME 38 CARGO LOADING SYSTEM ADAPTER HAS 2 EACH AREAS OF WORN SCALLOPS. REMOVED WORN CLS ADAPTER AND INSTALLED NEW CLS ADAPTER BETWEEN SEAT TRACK 2R AND 3R FRAME 38 IAW A310-200 SRM 51-40-21 AND SRM 51-72 -10. 2 L 7 2 4F RT A35EU 20080916 NM 2008 9 16 08FDEA03222 1 20080803 A 5730 N112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 MINOR CORROSION FOUND ON WING LOWER INTERNAL SURFACE ACCESS 531AB WHILE CARRYING OUT TREATMENT. CORROSION REMOVED IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008020600086 20080206 00086 NM 2008 2 6 2008UALA00018 1 20080101 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 524UA 24977 THE EMERGENCY LIGHTS ON THE LEFT SIDE OF AIRCRAFT ARE ON. LIGHTS OVER THE DOORS. PERFORMED RESET OF EMERGENCY LIGHT SY STEM, ALL CHECKED OK AFTER RESET. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600087 20080206 00087 2008 2 6 2008UALA00019 4 20080101 A 2565 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE LIGHT DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 SLIDE ARMED LIGHT ABOVE DOOR 3R IS ILLUM WHEN SLIDE IS DISARMED. FOUND DIRTY SWITCH. CLEANED SWITCH, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600089 20080206 00089 NM 2008 2 6 2008UALA00042 1 20080102 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 2L OBSTRUCTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 SLIDE LT DOOR 2R INOPERATIVE. *S/D* GIRT BAR NOT ENGAGING FULLY DUE TO DEBRIS. CLEANED GIRT BAR FITTINGS AND DOOR ARM ING SYSTEM OPERATES NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600094 20080206 00094 WP 2008 2 6 ABXA080023 1 20080107 A 5310 99578608 ANGLE DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 COCKPIT WINDOW SILL RIGHT ANGLE CRACKED. REMOVED, REPAIRED, AND REINSTALLED ANGLE IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2008020600103 20080206 00103 EU 2008 2 6 FAA2508001 1 20080118 A 2497 WIRE PIAGIO P180 P180 6960204 EU CABIN BURNED E V2JA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 15 156SL 1397 127 1115 CREW SMELLED WHAT THEY DESCRIBED AS ELECTRICAL BURNING OR ARCING. NO SMOKE OR FLAMES SEEN. THEY LANDED WITHOUT INCIDEN T AND SECURED THE AIRCRAFT. WE WILL SEND A MAINTENANCE TEAM INTO INVESTIGAGE 1.20.08. 1 H 7 2 3O RT A59EU 2008020600105 20080206 00105 SO 2008 2 6 C2XA08TY014 1 20080120 A 2612 902081 CONTROL MODULE EMB 145 EMB145LR 3260212 SO FIRE DETECTION MALFUNCTIONED A C2XA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 27 11539 145536 ENGINE 2 FIRE DETECT FAIL. REMOVED AND REPLACED NR 2 FIRE DETECT CONTROL MODULE IAW EMB 145 AMM 26-11-03. OPS CHECK GO OD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008020600106 20080206 00106 SO 2008 2 6 C2XA08ON068 1 20080115 A 2611 APU EMB 145 EMB145XR 3260214 SO CONTAMINATED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14181 1450929 FLT 1363 - LAV SMOKE INDICATION DURING CLIMB AND CLEARED ON ITS OWN. AFTER LANDING MX FOUND DE-ICING FLUID RUNNING DOWN APU INLET. RAN APU BLEEDS AND ENGINE BLEEDS NO FURTHER MESSAGE NOTED. OPERATIONALLY CHECKED LAV SMOKE DETECTOR SATISF ACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008020600110 20080206 00110 WP 2008 2 6 ABXA08024 1 20080107 A 5320 99578607 ANGLE DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 COCKPIT WINDOW SILL LEFT ANGLE P/N: 9957860-7 CRACKED. REMOVED, REPAIRED, AND REINSTALLED ANGLE IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2008020600111 20080206 00111 WP 2008 2 6 ABXA08025 1 20080107 A 5320 591236067 ANGLE DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 CENTER AND SIDE WINDSHIELD LEFT ZEE P/N: 5912360-67 CRACKED. REPLACED LEFT ZEE IAW SR DWG 09530268, DC9 SRM 51-30-2, 51 -30-5 AND JOB CARD EA 53300036-014. 2 L 7 2 4F A6WE 2008020600114 20080206 00114 WP 2008 2 6 UPS08851523 1 20080113 A 5320 PANEL DOUG DC8 DC871F 302199D WP FS 920 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 KEEL BEAM PNL BETWEEN WHEEL WELLS BULGED AT FASTENER HOLE. FABRICATED REPAIR KEEL BEAM PNL AND INSTA LLED BETWEEN WHEEL WELLS IAW DWG 561606, AND SRM 51-09-22, SRM 51-01-22. 2 L 7 4 4F RT 4A25 2008020600135 20080206 00135 CE 2008 2 6 LX5R200800007 1 20080121 A 5610 10138402524 WINDSHIELD BEECH B300 B300 1159232 CE PWA PT6 PT6A60A 52043 NE HARTZL HCB4M HCB4MP3 GL COCKPIT CRACKED B LX5A K NONE O OTHER CR CRUISE 1 GL 19 981LL 870 FL265 IT WAS REPORTED WHILE AT 15000FT IN CRUISE FLIGHT FROM KSPI TO KMDW ON AN IFR FLIGHT PLAN WITH NO PASSENGERS ON BOARD, 1 0 MILES NORTH OF PONTIAC VOR. THE RIGHT HAND WINDSHIELD CRACKED IN SEVERAL PLACES ON THE OUTER PANE ONLY. AFTER REVIEW ING THE ABNORMAL PROCEDURES THE CREW RETURNED TO KSPI TO GET ANOTHER AIRCRAFT TO FINISH THE DAYS FLIGHT. THE AIRCRAFT L ANDED AT KSPI WITHOUT INCIDENT. THE MAINTENANCE DEPARTMENT INSPECTED THE AIRCRAFT AND FOUND NO OTHER DAMAGE. THE WINDS HIELD WAS REPLACED. 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P56GL 20080915 NM 2008 9 15 08FDEA03162 1 20080730 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL ACCESS PANEL CUTOUT 543AB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93, REPAIR 5. REPAIR IS CLASSIFI ED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080915 EU 2008 9 15 08FDEA03174 1 20080730 A 5347 R5307008820200 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 686FE 804 MAIN CARGO DECK LT SIDE NR 4 SEAT TRACK BETWEEN FR 57 AND FR 57.1 HAS 2 EA ELONGATED SCALLOPS. REMOVED DAMAGED SECTION OF TRACK AND INSTALLED SEAT TRACK SPLICE REPAIR AT TRACK NR 4 LT BETWEEN FR 57 AND FR 57.1 IAW SRM 53-10-16, FIG 201, PG 207/208. 2 L 7 2 4F RT A35EU 20080915 WP 2008 9 15 08FDEA03079 1 20080725 A 5753 ARC27362 SKIN DOUG MD10 MD1010F 3022112 WP RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 RIGHT WING INBD FLAP LOWER SURFACE SKIN HAS MULTIPLE DENTS INBD OF THE SPRING CARTRIDGE. CHECKED DENTS AND FOUND TO BE OUT OF LIMITS IAW SRM 57-10-00; VOL I; FIG 48 AT STA XIFH 250 AT 254. REMOVED THE LOWER SKIN WEDGE SKIN IAW SRM 51-35-0 2; VOL II. RECEIVED NEW SKIN ASSY. FABRICATED ON N01033. LOCATED; DRILLED AND INSTALLED NEW SKIN ASSY IAW SRM 51-31-0 1; 51-35-01; VOL II AND DWG ARC 2735, REV S. ALODINED AND PRIMED IAW SRM 51-21-01; VOL II. 2 L 7 3 4F RT A22WE 20080915 WP 2008 9 15 08FDEA03080 1 20080725 A 5414 AUB70387 PANEL DOUG MD10 MD1010F 3022112 WP NR 3 NACELLE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 NR 3 PYLON PANEL 437 DL HAS ELONGATED HOLES. REPAIRED PANEL 437 DL IN REF TO EA 8-5480-116998 P/N AUB 7038-7. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 08FDEA02761 1 20080708 A 5230 65561431 SKIN BOEING 727 727233 138408A NM ZONE 800 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 275FE 22040 FUSELAGE, C-3 DOOR HAS NUMEROUS DENTS AND BULGES ON EXTERIOR SKIN OF DOOR REMOVED C-3 DOOR ASSY AND HANDLE IAW MM 52-35- 051-4 AND SRM 51-30-2. REMOVED, FABRICATED AND INSTALLED NEW C-3 DOOR SKIN IAW EA 7-5230-22339. REINSTALLED C-3 DOOR H ANDLE AND ATTACHED PARTS IAW SRM 51-30-2. INSTALLED C-3 DOOR IAW MM 52-35-051-4. OPS CHECK GOOD IAW MM 52-35-051-4. R EF EA 7-5230-122339. 2 L 7 3 4F RT A3WE 20080915 NM 2008 9 15 CALA0800797 1 20080819 A 5311 650465255 FAILSAFE BOEING 737 7373T0 1384582 NM BS 380 S19-20R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 FRAME AT BODY STATION 380 BETWEEN S19R AND S20R APPEARS WAVY AT OLD REPAIR. EVALUATE AND REPAIR IF REQUIRED. REMOVED D AMAGED FAILSAFE AND REPAIRED IAW B737 SRM 51-70-11. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 CALA0800798 1 20080817 A 5320 BAC150510153 INTERCOSTAL BOEING 737 737524 1384721 NM BS 947-927 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 INTERCOSTAL BETWEEN FS 947-927 AT RBL 24 HAS POSSIBLE CRACK. REMOVED DAMAGED INTERCOSTAL CAP ANGLE IAW SRM 51-40-02. PE R SRM 51-20-01 AND EC/RA 5310-03585 MATERIAL ID EXTRUSION BAC1505-101353 FOR CAP ANGLE, PAC 40859, .190 INCH, 7075-76, I C 0654053 FOR FILLER, FABRICATED REPAIR PARTS, ALODINED, PRIMED AND INSTALLED REPAIR PARTS. 2 L 7 2 4F RT A16WE 20080915 WP 2008 9 15 UPS08853082 1 20080725 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 CRACKED FRAME AT FLIGHT COMP STA -67.000 BETWEEN LONGERON 10 AND 11 AT LT SIDE NEXT TO LT EYEBROW WIN DOW. REMOVED CRACKED FRAME IAW SRM 51-1-21, FABRICATED AND INSTALLED REPLACEMENT FRAME IAW DWG 5642814, SRM 51-1-20D, A ND 51-03-01. 2 L 7 4 4F RT 4A25 20080915 NM 2008 9 15 SWAA084765 1 20080827 A 5311 6546532 FRAME BOEING 737 7373T0 1384582 NM BS 480 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 UPS08M53092 1 20080803 A 5754 SLAT TRACK DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 284UP 48541 INSPECTION TYPE:C RT WING NR 11 SLAT TRACK I/B ENCLOSURE FOUND SKIN DOUBLER CRACKED. CRACKED SKIN DOUBLER AT RT WING NR 11 SLAT TRACK I/B ENCLOSURE TRIMMED OUT AS PER SRM 57-10-00 V1 R40 FIG 27. HFEC INSPECTION CARRIED OUT PER DAC NDTSPM REV 13 PART 06.10.01.001 ON TRIMMED OUT AREA, FOUND NO CRACK EVIDENT. HOLES TRANSFERRED ON TO NEW REPAIR FILLER 01EA, R EP DOUBLER 01EA &03EA REP ANGLES AS PER SRM 57-10-00V1 FIG 27 R40 & SRM 51-31-01 V2 R40. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 SWAA084766 1 20080827 A 5311 65C22908 FRAME BOEING 737 7373T0 1384582 NM BS 500C S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 SWAA084774 1 20080827 A 5312 6517582 BULKHEAD BOEING 737 7373Y0 1384671 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED 22Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 SWAA084775 1 20080827 A 5753 SKIN BOEING 737 7377H4 1384404 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 746SW 302 29798 DURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED FLA P PER MM. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 UPS08653109 1 20080810 A 5315 141T514616 FLOORBEAM BOEING 767 76734AF 1385212 NM BS 246 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 334UP 32844 INSPECTION TYPE:C FX - CABIN FLOORBEAM ATTACHMENT STIFFENER AT STA 246 LBL 50 FOUND CRACK. CRACK LENGTH 0.75 INCH. FX CABIN FLOORBEAM STA 246 LBL 50 ATTACHMENT STIFFENER WAS REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 20080915 NM 2008 9 15 SWAA084776 1 20080827 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 909WN 32458 EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 UPS08653110 1 20080808 A 5710 BEAM BOEING 767 76734AF 1385212 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 334UP 32844 INSPECTION TYPE:C LT WING LES 674 'D' NOSE SUPPORT WEB LOWER FLANGE FOUND CRACKED. CRACK LENGTH 1.125 INCH. LT WING LE S 674 'D' NOSE SUPPORT WEB LOWER FLANGE REPAIRED AS PER SRM 57-41-13-2R REPAIR 3 FIG 201. 2 L 7 2 4F RT A1NM 20080915 EA 2008 9 15 SWIA200820010 1 20080430 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW CRACK INDICATION NOTED ON AFT PRESSURE BULKHEAD LBL 36.20 JUST ABOVE LOWER LINER ATTACH CLIP. FOUND AT C-CHECK. REPAIR ED PER REO 601R-53-61-1285 SHEET 11. 2 L 7 2 4F RT A21EA 20080915 EA 2008 9 15 SWIA200820011 1 20080430 A 5751 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT AILERON CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 FS 559 UNDER RT SIDE LT AILERON HAS CRACKS IN WEB FOUND AT C-CHECK. REPAIRED PER REO 601R-53-41-260 STEP 13 A-E STEP 14 C,C REV "B". 2 L 7 2 4F RT A21EA 20080915 WP 2008 9 15 UPS08853133 1 20080726 A 5320 TORQUE BOX DOUG DC8 DC871F 302199D WP EMERGENCY EXIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 A FITTING CRACKED IN LEFT FWD EMERGENCY EXIT DOOR FWD JAMB TORQUE BOX STA 380 L19L. FABRICATED AND I NSTALLED REPAIR FITTING IAW SAA EA 008-5310-01-A1486-1. 2 L 7 4 4F RT 4A25 20080915 EA 2008 9 15 SWIA200819967 1 20080819 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA DIRTY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 946SW 7776 SERVICE DOOR IS HARD TO OPEN FROM OUTSIDE. FLIGHT 6490. INSPECTED, CLEANED AND LUBED SERVICE DOOR AND SEAL IAW AMM 52- 41-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008012900159 20080129 00159 NM 2008 1 29 KCSA081021 1 20080117 A 5311 FRAME BOEING 747 747209B 138489B NM FUSELAGE GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 BS 2320 FUSELAGE FRAME GOUGED BETWEEN STR 24L AND 25L. 2 L 7 4 4F RT A20WE 2008012900173 20080129 00173 EU 2008 1 29 2008UALA00152 1 20080108 A 5210 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 446UA 834 DOOR 2L ASSIST BOTTLE PRESSURE READS 7.0 PSI. SHOULD READ APPROX 1740 PSI. SERVICED DOOR ASSIST BOTTLE TO CORRECT PRESS URE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900196 20080129 00196 NM 2008 1 29 2008UALA00238 1 20080112 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 STAIR WELL CEILING EMERGENCY LIGHT BETWEEN MAIN DECK AND UPPER DECK & UPPER DECK CEILING EMERGENCY LIGHTS AT SEATS 13 & 17 ARE INOP. RESECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900207 20080129 00207 WP 2008 1 29 UPS08851422 1 20080109 A 5720 BRACKET DOUG DC8 DC871F 302199D WP LWS 28.00 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 LT AUX TANK MAIN PNUEMATIC MANIFOLD CENTER MOUNT BRACKET IS CRACKED. REMOVED, FABRICATED, AND INSTAL LED REPAIR MOUNT BRACKET AT LT AUX TANK STA XFS 28.000 IAW SRM 51-1-21 AND DWG 4766565. 2 L 7 4 4F RT 4A25 2008012900213 20080129 00213 2008 1 29 UPS08851433 4 20080108 A 2565 SLIDE DOUG DC8 DC873F 302199F WP PAX DOOR UNSECURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 MAIN DOOR ESCAPE SLIDE NEEDS TO BE REPACKED. RE-SECURED ESCAPE SLIDE. 2 L 7 4 4F RT 4A25 2008012900219 20080129 00219 NM 2008 1 29 HNAA0800022 1 20080101 A 3320 F18T5CWRS BULB DHAV DHC8 DHC8102 2809003 NM CABIN LIGHTS BROKEN A HNAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 07 839EX 41554 41554 226 OVERHEAD LIGHT AT 6DF CAME LOOSE AND BROKE IN FLIGHT, THOUGHT TO BE BROKEN BY PASSENGER OPENING OVERHEAD BIN. CLEANED B ROKEN GLASS FROM OVERHEAD BIN, FLOOR AND SEATS. REPLACED BULB, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2008012900235 20080129 00235 EU 2008 1 29 2008UALA00253 1 20080114 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 491UA 1741 R2 DOOR SILL PLATE HAS CORROSION AT FASTENER HOLE LOCATION FWD END AT FR66 AND AT AFT END AT FR 69 ON OUTER RADIUS. PER FORMED MAJOR REPAIR AT LCQ. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900244 20080129 00244 NM 2008 1 29 2008UALA00258 1 20080114 A 5330 146T3551 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 661UA 63328 27158 FUSELAGE DAMAGE AT STA 1197 +4 - +10. INSTALLED REPAIR DOUBLER AND FILLERS. ACFT REPAIRED AND OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900247 20080129 00247 NM 2008 1 29 2008UALA00259 1 20080114 A 5315 141T581410 STIFFENER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE BS 246 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 667UA 32928 29239 BS 246 CABIN FLOORBEAM AT RBL 11.53 HAS CRACKED VERTICAL STIFFENER FWD SIDE OF FLOORBEAM. REMOVED AND REPLACED STIFFENE R. ACFT REPAIRED AND OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900248 20080129 00248 NM 2008 1 29 2008UALA00260 1 20080114 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 L2 DOOR UPPER HINGE ARM ASSY CUTOUT HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012900255 20080129 00255 WP 2008 1 29 UPS08851441 1 20080109 A 5522 SKIN DOUG DC8 DC871F 302199D WP RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 RT ELEVATOR NR 5 HINGE CUTOUT IS CRACKED THROUGH FASTENER HOLE ON UPPER SIDE. FABRICATED AND INSTALL ED REPAIR DOUBLER ON RT ELEVATOR NR 5 HINGE CUTOUT IAW SRM 55-04-01, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2008012900264 20080129 00264 WP 2008 1 29 UPS08851449 1 20080102 A 5321 FLOORBOARD DOUG DC8 DC871F 302199D WP FS 880-1020 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 MAIN CABIN FLOOR PANEL CENTER RT STA 880-1020 HAS BAD INSERT AND DAMAGED HOLE. REMOVED, FABRICATED A ND INSTALLED MAIN CABIN FLOORBOARD PNL AT STA 880-1020 IAW EO DC8-5320-9691-C. 2 L 7 4 4F RT 4A25 2008012900265 20080129 00265 WP 2008 1 29 UPS08851450 1 20080102 A 5321 FLOORBOARD DOUG DC8 DC871F 302199D WP FS 660-760 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 MAIN CABIN FLOOR PNL LT INBD STA 660-760 IS DAMAGED AND CRUSHED. REMOVED, FABRICATED AND INSTALLED M AIN CABIN FLOOR PNL AT STA 660- 760 REF EO DC8-5320-9691-C. 2 L 7 4 4F RT 4A25 2008012900266 20080129 00266 WP 2008 1 29 UPS08851451 1 20080102 A 5321 FLOORBOARD DOUG DC8 DC871F 302199D WP FS 660-760 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 MAIN CABIN FLOORBOARD LT OUTBD STA 660-760 HAS DAMAGED INSERT. REMOVED, FABRICATED, AND INSTALLED MA IN CABIN FLOORBOARD AT STA LT OUTBD 660-760 REF E0 DC8-5320-9691-C. 2 L 7 4 4F RT 4A25 2008012900272 20080129 00272 NM 2008 1 29 2008UALA00272 1 20080114 A 2560 LINK ASSY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE DOOR GIRT BAR DIRTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 667UA 29239 NR 2 LEFT MED, AFT DEPLOYMENT BAR LINK ASSY IS STIFF. CLEANED GIRT BAR. DRY LUBRICATED ASSEMBLY. REASSEMBLED AND OPS CH ECKED. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080915 EA 2008 9 15 SWIA200819969 1 20080818 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 726SK 10190 THIRD OVERHEAD EMERGENCY LIGHT IS INOP. FLIGHT 6706. RELAMPED OVERHEAD EMERGENCY LIGHT AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080915 NM 2008 9 15 SWAA084781 1 20080828 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 967 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080915 EU 2008 9 15 08FDEA03435 1 20080815 A 5340 A53974225212 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORRODED CLIP AT C 69, P 55-56 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080915 EU 2008 9 15 08FDEA03584 1 20080825 A 5320 A53611640200 FLOOR SUPPORT AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 455FE 331 MAIN DECK FLOOR LEVEL FR 15 TO FR 19 Y450 FLOOR TRACK WITH EXFOLIATION CORROSION. REPLACED THE FLOOR TRACK PER SRM 51-4 0-21. RESTORED FINISH PER SRM 51-75-10. APPLIED CIC TO THE REWORKED AREA PER AMM 51-22-00-0. MINOR REPAIR AS PER GMM 6-2-100. 2 L 7 2 4F RT A35EU 20080915 NM 2008 9 15 08FDEA03585 1 20080826 A 5347 ADA7321519 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 574FE 48499 MAIN DECK SEAT TRACK CROWN AT STA 885, X = -8 FOUND CHAFED. MAIN DECK SEAT TRACK AT STA 849 TO STA 909, X = -8 CARRIED OUT REPAIR AS PER SRM 53- 70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 08FDEA03586 1 20080826 A 5711 ARB74132 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 574FE 48499 RIGHT WING, TRAILING EDGE REAR SPAR UPPER CAP AT STA XORS 897 FOUND 01 EACH FASTENER HOLE ELONGATED. FASTENER HOLE REP AIR CARRIED OUT AS PER EA 1-5710-122430, THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 08FDEA03587 1 20080826 A 5711 ARB74132 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 574FE 48499 RIGHT WING, TRAILING EDGE REAR SPAR UPPER CAP AT STA XORS 746 FOUND 01 EACH FOUND FASTENER HOLE ELONGATED. REPAIRED AS PER E.A. 1-5710-122430, THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080915 EU 2008 9 15 08FDEA03132 1 20080729 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CABIN SEAT TRACK AT APPROX RBL 37 INCH; BETWEEN FRAMES 43 AND 44 HAS CORROSION. SEAT TRACK FOUND TO BE OUT OF LIMI TS IAW A300-600 SRM 53-10-16. REMOVED SEAT TRACK IAW SRM 51-40-21. IN REF TO SRM 53-15-16 AND SM NSA348076. CUT SEA T TRACK AND DRILLED HOLES IN REF TO SRM 53-10-16. PART MARKED NEW SEAT TRACK IN REF TO GMM 7-0-1001. INSTALLED NEW SEA T TRACK IAW SRM 53-10-16. CIC'D SEAT TRACK IAW AMM 51-22-00-0. 2 L 7 2 4F RT A35EU 20080915 WP 2008 9 15 08FDEA03444 1 20080812 A 5330 ABA75181 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 RIGHT SIDE FUSELAGE SKIN AT STA 322 IS CRACKED 10 INCHES ABOVE THE FINGER DOUBLERS. REMOVED FIRST OFFICERS SEAT IAW AMM 25-11-01-4. REMOVED DAMAGE AND FABRICATED A REPAIR IAW SRM 53-20-00; FIG 6; VOL I. ALODINED AND PRIMED IAW SRM 51-21- 01; VOL II. INSTALLED THE REPAIR IAW SRM 53-20-00; VOL II; FIG 6. INSTALLED FIRST OFFICERS SEAT IAW AMM 25-11-01-4; OP S CHECK FOUND TO BE GOOD IAW AMM 25-11-01-4. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 08FDEA03720 1 20080904 A 5330 655457533 SKIN BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 SCRIBE MARKS IN FUSELAGE SKIN BS 720 6 INCH BETWEEN STR 23LT AND 24 LT. FOUND AREA OUT OF LIMITS IAW SRM 53-30-01 FIG 1 . CUT OUT DAMAGED AREA DIMS 2 1/2 INCH BY 1 5/8 INCH IAW SRM 51-10-01 AND 53-30-03 FIG 1. FABRICATED DOUBLER REPAIR IA W SRM 53-30-03 FIG 2 AND FILLER. INSTALLED REPAIR PARTS IAW SRM 51-30-02 AND 53-30-03 FIG 2. 2 L 7 3 4F RT A3WE 20080915 WP 2008 9 15 08FDEA03380 1 20080812 A 5311 ACA380825 FRAME DOUG DC10 DC1030F 3023504 WP BS 555 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 RT AIR COND COMPT FOUND CRACK ON CAP OF FRAME. 2 L 7 3 4F RT A22WE 20080915 EU 2008 9 15 08FDEA03133 1 20080729 A 5347 A5381231020001 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CABIN SEAT TRACK AT RBL 17 INCH HAS CORROSION BETWEEN FRAMES 47 AND 48. REMOVED OLD SEAT TRACK AND INSTALLED A NEW SEAT TRACK IAW A300-600 SRM 57-40-21. MATERIAL ID FOR THE NEW TRACK IAW A300-600 SRM 53-15-16. FABRICATED A NEW SEAT TRACK IAW DWG A53812922. ALODINED, PRIMED AND PAINTED IAW A300-600 AMM 51-75-10-8. 2 L 7 2 4F RT A35EU 20080916 NM 2008 9 16 08FDEA03446 1 20080816 A 5340 65C261432 BRACKET BOEING 727 7272S2F 1384O81 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 FWD NOSE COMPARTMENT WEATHER RADAR MOUNT BRACKET CRACKED REMOVED WEATHER RADAR R/T. REPLACED MOUNT BRACKET, INSTALLED W EATHER RADAR R/T AND PERFORMED GOOD OPS CHECK REF SRM 51-30-02, AMM 34-41-041-4 AND AMM 34-41-000-5. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080916 NM 2008 9 16 08FDEA03447 1 20080816 A 5740 652165828 ATTACH ANGLE BOEING 727 7272S2F 1384O81 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 RT WING LOWER T/E PANEL BELOW NR 13 SPOILER ACTUATOR O/B ATTACH ANGLE CRACKED. REMOVED AND REPLACED CHANNEL REF SRM 51- 30-5, SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080911 NM 2008 9 11 08FDEA03656 1 20080831 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 594FE 48552 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FIT TING AT HOLES A, C AND D. MAIN CARGO DOOR LOWER JAMB, CRACKED NR 1 SUPPORT FITTING R & R AS PER SRM 51-31-01 VOLUME I I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080911 NM 2008 9 11 08FDEA03658 1 20080831 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 594FE 48552 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FIT TING AT HOLES A, B, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MA JOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080911 NM 2008 9 11 08FDEA03659 1 20080831 A 5320 AFS71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 594FE 48552 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FIT TING AT HOLES A, B, C AND D. SUPPORT FITTING R&R AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6 -2-100. 2 L 7 3 4F RT A22WE 20080911 EU 2008 9 11 08FDEA03671 1 20080901 A 5712 A57240457200 RIB AIRBUS A300 A300F4622R 3930360 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CHAFING MARKS ON LH WING TRAILING EDGE AREA ON RIB FOR ASA ATTACHMENT. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS , PERFORM NDT FOR CRACK FREE CONDITION IAW. RAS/BAE/1007863/2008 ISS.A , APPROVED BY EA 6-5751-123063 2 L 7 2 4F RT A35EU 20080911 WP 2008 9 11 08FDEA03623 1 20080828 A 5712 AUB720347 RIB DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING T/E STRUCTURE VERTICAL WEB IS CRACKED AT THE INBOARD FWD CORNER OF THE INBOARD FLAP. REMOVED & REPLACED THE C RACKED WEB (ANGLE) IN REF TO DC/MD-10 SRM 51-35-01; VOL II & IN REF TO DAC DWG AUB 7203; REV "BA". 2 L 7 3 4F RT A22WE 20080912 EA 2008 9 12 SWIA200819979 1 20080819 A 3520 OXYGEN MASK CNDAIR CL600 CL6002B19 1900309 EA ROW 13 UNWANTED DEPLOY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 464SW 7827 THE O2 MASK DEPLOYED AT ROW 13. FLIGHT 3965. STOWED OXYGEN MASKS PER AMM 35-21-01. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200819980 1 20080820 A 3350 COVER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT MISSING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 719SK 10188 EMERGENCY EXIT LIGHT COVER IS MISSING NEAR SERVICE DOOR. FLIGHT 6343. REPLACED LENS FOR SERVICE DOOR. 2 L 7 2 4F RT A21EA 20080912 SO 2008 9 12 SWIA200819946 1 20080804 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 237SW 120314 LEFT WINDSHIELD SHATTERED DURING TAXI. FLIGHT 3418. REPLACED WINDSHIELD ASSEMBLY IAW 56-10-00. P/N: NP-151311-1, S/N OFF: 04114H2865. 2 L 7 2 4T RT A31SO 20080912 EA 2008 9 12 SWIA200819947 1 20080806 A 2913 PUMP CNDAIR CL600 CL6002C10 1390015 EA HYD SYSTEM FAILED A SWIA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 07 750SK 10207 HYDRAULIC EDP 2A CAUTION MESSAGE ALONG WITH QUANTITY INDICATION SHOWING 0 PERCENT. FLIGHT 6193. REPLACED NR 2 EDP IAW MM 29-11-01. NO LEAKS NOTED. P/N: 66190-03, S/N OFF: K0597. 2 L 7 2 4F RT A21EA 20080912 NM 2008 9 12 SWAA084750 1 20080827 A 5753 6546535335 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP P ER MM. 2 L 7 2 4F RT A16WE 20080912 NM 2008 9 12 SWAA084763 1 20080827 A 5311 6545807 FRAME BOEING 737 7373H4 1384600 NM BS 294 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 294, STR 15R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080912 EA 2008 9 12 SWIA200820001 1 20080831 A 2612 FIRE WARNING CNDAIR CL600 CL6002B19 1900309 EA APU BAY ILLUMINATED A SWIA F D ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 698BR 7799 UPON STARTING APU RECEIVED "APU BTL LO" CAUTION MESSAGE. REPLACED APU FIRE BOTTLE IAW AMM 26-22-07. OPS CHECK GOOD. P /N 897889-2, S/N OFF 6098ZEL, P/N 897776-01, S/N OFF 01842. 2 L 7 2 4F RT A21EA 20080912 EA 2008 9 12 SWIA200820008 1 20080430 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 410SW 7066 STA 621 LT - SUPPORT ANGLE FROM PRESS BLKHEAD TO FLOOR CRACKED AT OUTBOARD END. FOUND AT C-CHECK. REPAIRED PER REO 601 R-53-61-117. 2 L 7 2 4F RT A21EA 20080912 WP 2008 9 12 UPS08853073 1 20080807 A 3350 BULB DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE:ASE EMERGENCY LIGHTS VERY DIM OVER ENTRY DOOR. RELAMPED EMERGENCY LIGHTS. FOUND BAD BULB. BASE PARTIA LLY SEPARATED FROM LAMP. WORK DONE IAW MM 33-50-02-2. OPERATION CHECK GOOD AT THIS TIME. 2 L 7 4 4F RT 4A25 20080915 EU 2008 9 15 08FDEA02998 1 20080721 A 5720 A21040014000 DUCT AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 RT WING INBD FIXED L/E INLET SCOOP IS CRACKED ON THE FWD END APPROX 2 INCHES LONG. REMOVED PANEL IAW SRM 51-40-21, PG 7 ; SECT 5. WELDED CRACK IN THE RIGHT WING L/E INLET SCOOP IAW DWG A21040014. INSTALLED IAW SRM 51-40-21; PG 7. 2 L 7 2 4F RT A35EU 20080915 NM 2008 9 15 08FDEA03164 1 20080730 A 5311 651631633 FRAME BOEING 727 727233 138408A NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 275FE 22040 FRAME AT STA 344 DENTED AT STR 5L AT 9G BULKHEAD. CUT OUT DAMAGE FROM FRAME IAW SRM 53-10-4 FIG 2. FABRICATED NEW FRAM E REPAIR AND REPAIR FILLER IAW SRM 53-10-4 FIG 2 AND 53-10-2 FIG 3 AND 51-20-1. HEAT TREATED FRAME REPAIR IAW FAS ENGIN EERING REPORT 2-37153-801 REV A. TREATED AND PRIMED PARTS IAW SRM 51-30-2 AND INSTALLED NEW PARTS IAW SRM 51-10-2 AND 5 3-10-4. 2 L 7 3 4F RT A3WE 20080915 NM 2008 9 15 08FDEA03154 1 20080730 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL PANEL ACCESS CUTOUT 541JB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93, REPAIR 5. REPAIR IS CLASSIFI ED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080915 EU 2008 9 15 08FDEA03218 1 20080803 A 5340 A53611513224 FITTING AIRBUS 310 A310203 3930313 EU ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 430FE 394 PREVIOUS REPAIR LOCATED ON FUSELAGE CUTOUT AT L-1 FORWARD PAX DOOR FAILSAFE RING LOWER SECTION HAS 2 EACH EXTERNAL REPAI R DOUBLERS, AT FRAMES 14 AND 16A BETWEEN BEAMS 2 AND 5, EACH REPAIR DOUBLER MEASURES 16.1" INCHES LONG AND 3.1" INCHES W IDE. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED EXTERNAL REPAIR DOUBLERS AND INSTALLED CORRECT EXTERNAL REPAIR DOUBLERS AT FRAMES 14 AND 16A BETWEEN BEAMS 2 AND 5 IAW SRM 53-12-81 FIG 203 AND AIRBUS DWG R53610175. 2 L 7 2 4F RT A35EU 2008012900273 20080129 00273 NM 2008 1 29 2008UALA00273 1 20080115 A 3350 1317 LAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 209UA 30215 EMERGENCY LIGHT OUT AT MID GALLEY NR 2 RIGHT SIDEWALL. RELAMPED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008012900277 20080129 00277 NM 2008 1 29 2008UALA00278 1 20080115 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 727C S14L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 EXTERNAL FUSELAGE SKIN HAS A DRILL START DAMAGE BS 727C JUST BELOW STR 14L SKIN LAP. MAJOR REPAIR: REMOVED DAMAGE. FAB RICATED AND INSTALLED EXTERNAL DOUBLER, TRIPLER AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900278 20080129 00278 NM 2008 1 29 2008UALA00279 1 20080115 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 727C S14 GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 FUSELAGE BS 727C STRINGER CLIP AT STRINGER 14 IS GOUGED. REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900282 20080129 00282 NM 2008 1 29 2008UALA00283 1 20080115 A 2612 WARNING LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE WARNING NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 315UA 23947 ENGINE 2 OVERHEAT WARNING LIGHT DOES NOT ILLUMINATE DURING OVERHEAT - FIRE TEST. FOUND FAULTY ENGINE-APU FIRE CONTROL UNIT. REPLACED ENGINE-APU FIRE CONTROL UNIT. SHOP FOUND K201 ON A-6 FAILED. REPLACED K201. 2 L 7 2 4F 4 F RT A16WE E21EU 2008013000001 20080130 00001 WP 2008 1 30 UPS08851452 1 20080102 A 5321 FLOORBOARD DOUG DC8 DC871F 302199D WP FS 540-660 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 MAIN CABIN FLOORBOARD RT OUTBD STA 540-660 IS DELAMINATED AND CORRODED. REMOVED, FABRICATED, AND INS TALLED MAIN CABIN FLOORBOARD AT RT OUTBD STA 540-660 REF EO DC8-5320-9691-C. 2 L 7 4 4F RT 4A25 2008013000005 20080130 00005 NE 2008 1 30 HALA0800025 2 20080117 A 7261 UNKNOWN BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE OIL SYSTEM LEAKING A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM, DURING WALK AROUND NOTICED NR 1 ENG LEAKING OIL. CLEANED ENG COWL FOR NR 1 ENG RAN ENG FOR 5 MINUTES. NO LEAKS NOTED. NO OIL ADDED. QUANTITY CHECK OF IDG AND ENG OIL LEVEL CHECK GOOD. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E13NE 2008013000012 20080130 00012 NM 2008 1 30 08FDEA00191 1 20080117 A 5414 311N504631 SKIN BOEING 757 7572B7 1384964 NM NR 1 NACELLE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 NR 1 NACELLE STRUT O/B SIDE SKIN HAS TWO DENTS, AT CUT OUT AREA OF ACCESS PANEL 433BL, AT APPROXIMATELY NAC STA 136.675, OUTBOARD SKIN HAD TWO DENTS MEASURING 1.6" WIDE BY .126" DEEP AND 1.9" WIDE BY .10" DEEP. BOTH FOUND TO BE OUT OF LIMI TS IAW SRM 54-50-01, FIG 101, SHEET 4. REMOVED AND REPLACED OUTBOARD SKIN PER SRM 51-40-02 AND DWG, 311N5002, SHEET 14, REV E. 2 L 7 2 4F RT A2NM 2008013000014 20080130 00014 NM 2008 1 30 F3LA200800020 1 20080107 A 5220 FE240004 CYLINDER DAMPER AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE EMERGENCY DOOR INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 924FR 233 2030 DURING C CHECK INSPECTION, THE R2 EMERGENCY DOOR DAMPENER CYLINDER FAILED ITS TEST DUE TO LOW PRESSURE. MAINTENANCE CHA RGED THE CYLINDER IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 52-10-00-614-001. UPON COMPLETION OF THE CHARGING, TH E CYLINDER PRESSURE WAS VERIFIED TO BE WITHIN ACCEPTABLE LIMITS. 2 L 7 2 4F 4 F RT A28NM 2008013000020 20080130 00020 NM 2008 1 30 08FDEA00239 1 20080123 A 5311 BAC14902763 FRAME BOEING 727 727233 138408A NM BS 720D S26R CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 LWR FWD CARGO PIT FRAME UPPER FLANGE HAS SURFACE CORROSION, AFT SIDE STA. 720D ABOVE STR 26R. FOUND FRAME TO BE OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED FRAME. REINSTALLED Z-ANGLE, VERTICAL BULKHEAD SUPPORT IAW SRM 51-30-2 PG 1-16 S RM 51-40-2 PG 1-6, DWG 65-58677-17, 65-58352-54. HEAT TREAT FOR FRAME DONE ON 8130 TRACKING NR 2008-01-079. THIS IS CLAS SIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2008013000022 20080130 00022 NM 2008 1 30 QXEA200800036 1 20080121 A 3230 860TS09Y00 CONTROL PANEL BOMBDR DHC8 DHC8402 1390042 NM MLG MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 413QX 69 4060 LAX - AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT. LIGHTS REMAINED 3 GREEN. NO OTHER ABNORMAL INDICATIONS. RETU RNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE LANDING GEAR CONTROL PANEL. OPERATIO NAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008013000025 20080130 00025 NM 2008 1 30 QXEA200800039 1 20080123 A 2611 SMOKE DETECTOR BOMBDR DHC8 DHC8402 1390042 NM LAVATORY FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 418QX 4143 BOI- FLIGHT 2403 - LAVATORY SMOKE DETECTOR WENT OFF AFTER TAKEOFF FOR 30 SECONDS. FLIGHT ATTENDANTS NOTED NO SMOKE OR F IRE. MAINTENANCE COMPLIED WITH OPERATIONAL TEST OF THE SMOKE DETECTOR IAW 26-12-11-710-801. NO DEFECTS NOTED. COULD N OT DUPLICATE PROBLEM. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008013000026 20080130 00026 NM 2008 1 30 QXEA200800034 1 20080118 A 3297 471515 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM MLG WOW MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 411QX 4055 SEA - FLIGHT 2427 - AFTER TAKEOFF FROM YVR, THE LANDING GEAR WOULD NOT RETRACT. DIVERTED TO SEA AND PERFORMED A UNEVENT FUL LANDING. MAINTENANCE FERRIED THE AIRCRAFT TO PDX FOR REPAIRS. IN PDX, REPLACED THE NOSE GEAR WOW 2 HARNESS. OPERA TIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008013000027 20080130 00027 EU 2008 1 30 MALA080009 1 20080108 A 5753 STRUCTURE SAAB SF340 340B 7860101 EU RT TE FLAP DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 DENT LOCATED ON RT FLAP ASSY, IB PORTION OF LE, 9 INCH FROM FLAP PANEL AND 5 1/2 INCH FROM IB LE. REPAIRED IAW MAL EO N R S51031. 2 L 7 2 4T RT A52EU 2008013000030 20080130 00030 EU 2008 1 30 CPCP20080002 1 20080107 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 369AT 369 FOUND FLOORBEAM 39 CORRODED. FLOORBEAM 39 REPAIRED IAW SRM 53-00-00 FIG 436. 2 H 7 2 4T RT A53EU 2008013000032 20080130 00032 NE 2008 1 30 ANCF200800001 2 20080123 A 7261 FILTER DOUG DC9 DC983 3022083 WP PWA JT9 JT9D* NE RT ENGINE CLOGGED W ANCF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 23 160BS 53463 P726846D R OIL STRAINER CLOG ANNUNCIATION DISPLAYED ON EOAP DURING CRZ AT FL 350, ENG WAS OPERATED AT IDLE THRUST UNTIL LANDING; NO REVERSE WAS USED ON ENGINE. AS PER AMM 79-20-06 REMOVED AND REPLACED ENG OIL FILTER AND ENG OIL CHANGE PER AMM 12-12 -04. PERFORMED ENG CHECK ON GROUND OK. PER AMM 71-00-00, FILTER P/N 815345. 2 L 7 2 4F 4 F RT A6WE E20EA 20080915 EU 2008 9 15 08FDEA02996 1 20080721 A 5530 A5537214021600 SUPPORT ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 VERTICAL STABILIZER RIGHT TRAILING EDGE SUPPORT IS CRACKED BELOW THE NR 2 RUDDER HINGE FITTING. REMOVED DAMAGE IAW SRM 51-70-10, REPAIR I. FABRICATED A REPAIR ANGLE AND FILLER IAW SRM 51-70-10, REPAIR I. ALODINED AREA AND REPAIR PARTS IA W SRM 51-21-10. PRIMED AND PAINTED AREA AND REPAIR PARTS IAW SRM 51-23-10. INSTALLED REPAIR IAW SRM 51-70-10, REPAIR I AND SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080915 WP 2008 9 15 UPS08853079 1 20080727 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FS 1220 RBL 58 PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 MAIN CABIN, FLOOR PANEL PUNCTURED STA 1220 RBL 58. REMOVED FLOOR PANEL IAW MM 53-21-02, REPAIRED PER SRM 51-01-19, REINSTALLED PANEL IAW 53-21-02. 2 L 7 4 4F RT 4A25 20080915 NM 2008 9 15 SWAA084764 1 20080827 A 5310 6545871132 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED HC2 CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AT LOWER FRAME AFT LOWER STOP. REMOVED AND REPLACED DO OR PER MM. 2 L 7 2 4F RT A16WE 20080915 EA 2008 9 15 SWIA200819998 1 20080710 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 770SK 10243 COCKPIT FLOOR SUPPORT CRACKED. FOUND AT C-CHECK, REPLACED COCKPIT FLOOR SUPPORT PER SRM 51-42-06-001-001-A01, 51-42-21- 001-001-A01, 51-42-22-001-001-A01. 2 L 7 2 4F RT A21EA 20080915 NM 2008 9 15 UPS08M53074 1 20080811 A 3350 BATTERY DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:N/A EMERGENCY BATT/LO MESSAGE WHEN EMERGENCY LIGHT TESTED. REMOVED AND REPLACED EMERGENCY LIGHTS BATTER Y PER MM 33-51-01-4. OPS CHECK NORMAL. 2 L 7 3 4F RT A22WE 20080915 2008 9 15 SWAA084755 4 20080827 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080915 2008 9 15 SWAA084756 4 20080827 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 407WN 29817 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080915 WP 2008 9 15 UPS08853132 1 20080730 A 5340 ATTACH FITTING DOUG DC8 DC871F 302199D WP FS 520 L21R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 B-PIT STA 520 LONGERON 21R FLOORBEAM ATTACH FITTING HAS CORROSION. REMOVED FITTING IAW SRM 51-01-20D . INSTALLED REPLACEMENT FITTING IAW SRM 51-01-20D, AND 51-03-00. 2 L 7 4 4F RT 4A25 20080915 2008 9 15 SWAA084777 4 20080828 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 214WN 32486 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080915 SO 2008 9 15 SWIA200819966 1 20080819 A 5753 STRUCTURE EMB 120 EMB120ER 3260203 SO NACELLE FLAP CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 237SW 120314 CRACK IN LEFT NACELLE FLAP. REPLACED LEFT NACELLE FLAP IAW EMB 120 MM 27-50-03. 2 L 7 2 4T RT A31SO 20080915 NM 2008 9 15 SWAA084788 1 20080828 A 5311 6546529 FRAME BOEING 737 7373T0 1384582 NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 08FDEA03606 1 20080827 A 5330 65545732 SKIN BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 EXTERIOR SKIN OIL CANNED, BL0 STA 640-660. FABRICATED DOUBLER REPAIR FROM 2024T3 .050 PO NR 9007500 DIMS 10" BY 11 1/4 INCH IAW B727 SRM 53-30-3 FIG 1 AND INSTALLED REPAIR IAW B727 SRM 53-30-3 FIG 1 AND 51-30-2. 2 L 7 3 4F RT A3WE 20080916 EU 2008 9 16 08FDEA03454 1 20080816 A 5315 A2557217320200 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 430FE 394 BULK CARGO DOOR ENTRY FLOOR T-CAP ON INTERCOSTAL HAS 4 IN CRACK BEGINNING AT FR 68 REMOVED DAMAGED T-CAP AND SPLICE STRI PS AND INSTALLED NEW PARTS AT BULK CARGO DOOR FLOOR ENTRY BETWEEN FR 67 AND FR 69 IAW A310-200 SRM 51-40-21 AND 51-72-10 . 2 L 7 2 4F RT A35EU 20080916 NM 2008 9 16 08FDEA03456 1 20080816 A 5320 65271955 BRACKET BOEING 727 7272S2F 1384O81 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 AIRSTAIR COMPARTMENT LT BRACKET FOR FIRE LOOP SUPPORT IS CRACKED AT BULKHEAD STA 1183 NEAR FLOOR LEVEL. REMOVED OLD BRA CKET REF SRM 51-30-02 P 1-7, IDENTIFIED MATERIALS REF DWR 65-27195 FRAME 1 SHEET 3 REV E ALSO A-TAG NR A03329. FABRICAT ED NEW BRACKET REF DWR 65-27195 PAGE 1. TREATED AND PRIMED BRACKET REF SRM 51-10-2 PG 1-27. INSTALLED BRACKET REF SRM 51-30-02 PG 1-7. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080916 NM 2008 9 16 08FDEA03457 1 20080817 A 3260 862701 UPLOCK SENSOR DOUG MD11 MD11F 3023600 NM RT MLG MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 CE 21 599FE 48598 RT MAIN LDG GEAR WOULD NOT RETRACT ON FIRST ATTEMPT. SLOWED TO <230KIAS AND RECYCLED GEAR. 2ND RETRACT ATTEMPT WAS SUC CESSFUL. AS CREW BRIEF, DID NOT SEE SECONDARY MAIN LANDING GEAR INDICATION WHEN HAD NOT RETRACT. ALSO THEY COULD NOT F EEL ACTUAL DRAG. PERFORMED EXTERNAL VISUAL CK, FOUND NO DAMAGE AND NEED MORE T/S. FOUND CLEARANCE ON RT LANDING GEAR U P AND LOCK SENSOR OF 3.577MM (OUT OF LIMIT). REMOVED AND REPLACED RT LANDING GEAR UP AND LOCK SENSOR PER MM 32-61-15-4 AND ADJUSTED CLEARANCE PER MM 32-61-15-5. RT LANDING GEAR UP AND LOCK SENSOR R-T-S PASSED. A/C OK FOR SERVICE. 2 L 7 3 4F RT A22WE 20080916 EU 2008 9 16 08FDEA03175 1 20080730 A 5347 A5378193720000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CABIN SMALL LATERAL SEAT TRACK AT FRAME 30; LBL 30 FLANGE IS CRACKED. REMOVED CRACKED LATERAL SEAT TRACK IAW SRM 5 1-40-21; PARA 7. RECEIVED NEW LATERAL SEAT TRACK, PO 617060.2. LOCATED AND DRILLED THE LATERAL SEAT TRACK IAW SRM 51-4 0-40. INSTALLED NEW LATERAL SEAT TRACK REF DWG A53781937. 2 L 7 2 4F RT A35EU 2008013000033 20080130 00033 NE 2008 1 30 NACA20080001 2 20080126 A 8550 212734 PUMP DOUG DC6 DC6A 3021706 WP PWA R2800 R2800CB3 52026 NE NR 3 ENGINE POWER LOSS A NACA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 AL 03 6174C 1901 1901 44075 P35317 NR 3 ENGINE SHUT DOWN DUE TO LOSS OF BMEP. INSPECTION REVEALED FRONT OIL PUMP DRIVE FAILURE. REPLACED NR 3 ENGINE, REF : NAC DC6MM SECT V PG 3, 4 AND 5. CHECKED GOOD ON RUN-UP. 2 L 7 4 4R 4 R 6A3 5E8 2008013000035 20080130 00035 GL 2008 1 30 SIMA200802107 2 20080118 A 7261 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LEFT LEAKING A SIMA C ABORTED TAKEOFF K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 928AE 14500911 CAE312772 ON FLIGHT 3821 CREW REPORTED A ABORTED TAKE-OFF DUE TO STRONG SMOKE ODOR IN THE COCKPIT. NO VISIBLE SMOKE OBSERVED. DF W MTX CONFIRMED WAS OIL ODOR IN COCKPIT. NO ODOR IN CABIN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LT ENG INE IAW WC 71-000-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008013000036 20080130 00036 SO 2008 1 30 SIMA200802102 1 20080113 A 2510 747198412 HOLDER EMB 145 EMB145LR 3260212 SO COCKPIT SMOKE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 691AE 14500860 ON FLIGHT 4302, CREW REPORTED SHUTDOWN ENGINE AT THE GATE. A LITTLE BIT OF SMOKE WAS SEEN FROM UNDER THE F/O'S GLARE SH IELD. AIRCRAFT REMOVED FROM SERVICE. FOUND F/O`S CHART HOLDER SHORTING OUT AGAINST CHART ASSEMBLY CAUSING CIRCUIT BREA KER NR 2 COCKPIT READING TO TRIP. REMOVED AND REPLACED FIRST OFFICES CHART HOLDER ASSY IAW EMB145 25-12-11. OPS CHECK GOOD. NO DEFECTS NOTED, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008013000040 20080130 00040 SW 2008 1 30 WGEA200800009 1 20080123 A 3242 10100 MASTER CYLINDER ECLIPS EA500 ECLIPSEEA500 3350000 SW LT BRAKES WEAK E WGEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 27 161DJ 21 000078 LEFT BRAKE SPONGY ON BOTH PILOT AND COPILOT POSITIONS. REMOVED AND REPLACED CO-PILOTS LT MASTER CYLINDER WITH NEW MASTE R CYLINDER IAW EA500 AMM 32-41-11. BLED BRAKES IAW EA 500 AMM 32-40-00. OP'S CHECK AND LEAK CHECK GOOD. 1 L 7 2 4J RT A00002AC 2008021500061 20080215 00061 NM 2008 2 15 2008UALA00032 1 20080102 A 5320 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 BS 291.5 INTERCOSTAL ATTACH ANGLE IS CRACKED BELOW STR 13R. MAJOR REPAIR: FABRICATED AND INSTALLED REPLACEMENT ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900002 20080129 00002 NM 2008 1 29 HNAA0800023 1 20080104 A 3350 0L3071BPEGPL LAMP DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS BURNED OUT A HNAA O OTHER L NO TEST NR NOT REPORTED 1 EA 07 846EX 36311 36311 326 2 FLOOR EMERGENCY ESCAPE PATH LIGHTS ARE INOP IN FORWARD CABIN. RELAMPED AND TESTED GOOD. 2 H 7 2 4T RT A13NM 2008012900039 20080129 00039 NM 2008 1 29 2008UALA00186 1 20080110 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 AFT CARGO FLOOR STRINGER CORRODED AT STA 1358-1362 RBL 7. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012900040 20080129 00040 NM 2008 1 29 2008UALA00187 1 20080110 A 3350 58781 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU CABIN INOPERATIVE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 327UA 24147 AFT SECTION OF EEL LIGHTS INOP. CLEANED AND REPLACED SHORTED POWER STRIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900089 20080129 00089 NM 2008 1 29 2008UALA00209 1 20080112 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 UPPER FUESLAGE AFT GALLEY DOOR FUSELAGE EXTERIOR SKIN CRACKED AT UPPER FWD CORNER OF TORQUE TUBE CUTOUT. REMOVED DAMAG E. INSTALLED DOUBLER REPAIR PER AAR EA I060554 REV IR AND UA-EVA-60759. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900165 20080129 00165 NM 2008 1 29 USAA920080190 1 20080117 A 5330 141N3231 SKIN BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 903AW 23323 PHX - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 373, S21L. REPAIRED FUSELAGE SKIN, BS 373, S21L IAW B757 SRM 53-00-01-2R 2. 2 L 7 2 4F RT A2NM 2008012900181 20080129 00181 EU 2008 1 29 2008UALA00177 1 20080109 A 3234 215TS07Y00 CONTROL HANDLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT WORN A UALA O OTHER W INADEQUATE Q C CL CLIMB 1 WP 29 417UA 483 AFTER TAKEOFF TOOK 3 ATTEMPTS TO RAISE GEAR HANDLE. WEAR/PLAY IN THE LANDING GEAR CONTROL HANDLE. REPLACED THE LANDING GEAR CONTROL HANDLE. GEAR SWINGS ARE NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900195 20080129 00195 NM 2008 1 29 2008UALA00237 1 20080112 A 3350 276005 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 LEFT OVERWING EMERGENCY LIGHT 2ND AFT INOP. REPLACED FUSE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900200 20080129 00200 NM 2008 1 29 2008UALA00242 1 20080113 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 SEAT 56HJK EMERGENCY LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900271 20080129 00271 NM 2008 1 29 2008UALA00271 1 20080114 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 667UA 29239 EEL AT SEATS 6HJ AND 38AB ARE INOP. REMOVED AND REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900275 20080129 00275 NM 2008 1 29 2008UALA00275 1 20080114 A 3397 CONNECTOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 229UA 30557 EXIT PATH LIGHTS 2E-12F. FOUND CONNECTOR UNPLUGGED. RESECURED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008012900290 20080129 00290 NM 2008 1 29 2008UALA00294 1 20080115 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 775UA 26947 EEL LIGHT DAMAGED AT SEAT 11F. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008013000002 20080130 00002 NE 2008 1 30 REXA200800001 2 20080116 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LEFT LEAKING A REXA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 25 8747B 7747 GEE873643 ON CLIMB-OUT OF SGF,ON 01/15/08, THE CREW WAS ALERTED BY THE "SMOKE TOILET" WARNING. QRH PROCEDURES WERE COMPLETED, AN EMERGENCY DECLARED AND THE AIRCRAFT RETURNED TO SGF WHERE AN OTHERWISE NORMAL APPROACH AND LANDING WERE MADE. MAINTENAN CE INSPECTED THE AIRCRAFT BLEED AIR SYSTEM, PERFORMED OPERATIONAL TESTS, BUT COULD NOT DUPLICATE THE DISCREPANCY. THE A IRCRAFT WAS RETURNED TO SERVICE. THE FOLLOWING MORNING, THE AIRCRAFT DEPARTED SGF AND ON CLIMB-OUT AGAIN THE "SMOKE TOI LET" WARNING ILLUMINATED. THIS TIME THERE WAS VISIBLE SMOKE IN THE COCKPIT AND CABIN. THE CREW PERFORMED THE QRH PROCE DURES, DECLARED AN EMERGENCY AND RETURNED TO SGF. THE AIRCRAFT WAS TAKEN OUT OF SERVICE, INSPECTED AND FERRIED TO THE T 2 L 7 2 4F 4 F RT A21EA E15NE 2008013000008 20080130 00008 2008 1 30 HALA0800022 4 20080116 A 3422 H1501HK1 INDICATOR BOEING 767 76733A 1385209 NM STBY ATTITUDE FAILED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 580HA 28140 ETOPS SIGNIFICANT SYSTEM, STBY ATTITUDE GYRO FLAG CONTINUOUSLY POPPING IN/OUT OF VIEW (NOT SOLIDLY DISPLAYED). REPLACED STANDBY ATT INDICATOR. OPS CK OK PER MM 34-24-01. 2 L 7 2 4F RT A1NM 2008013000009 20080130 00009 NM 2008 1 30 HALA0800023 1 20080116 A 4950 ISOLATION VALVE BOEING 767 76733A 1385209 NM OPEN A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, NO APU BLEED AIR APU RUNS OK. OPERATED APU AIR. NO FAULTS NOTED. BLEED AIR PRESS NORMAL. O K FOR SERVICE. FOUND ISOLATION VALVE OPEN ON ARRIVAL. 2 L 7 2 4F RT A1NM 2008013000024 20080130 00024 EA 2008 1 30 QXEA200800037 1 20080121 A 5210 ROLLER CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 601QX 10009 PDX - FLIGHT 2520 - MAIN CABIN DOOR WILL NOT SWING OPEN WITHOUT DIFFICULTY FROM THE OUTSIDE. INSIDE OPENING NORMAL. MA INTENANCE CLEANED AND LUBED THE GUIDE ROLLERS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLAC ED. 2 L 7 2 4F RT A21EA 2008013000042 20080130 00042 EA 2008 1 30 QXEA200800040 1 20080123 A 5280 CC67010520951 DOOR CNDAIR CL600 CL6002C10 1390015 EA MLG MISSING A QXEA O OTHER D INFLIGHT SEPARATION CL CLIMB 1 NM 09 603QX 7090 10011 ONT- FLIGHT 2509 (PDX-ONT) - WHEN CLIMBING OUT OF 10,000 FEET AFTER DEPARTURE FROM PDX, A BANG WAS HEARD AND A SHUDDER W AS FELT FOR A MOMEMENT WHICH FELT LIKE IT WAS FROM THE FORWARD BELLY AREA. ALL INDICATIONS NORMAL. CONTINUED TO ONT AND ACCOMPLISHED A UNEVENTFUL LANDING. UPON ARRIVAL IT WAS NOTICED THAT THE LEFT MAIN GEAR DOOR HAD DEPARTED THE AIRCRAFT AND WAS MISSING. MAINTENANCE INSPECTED THE AIRCRAFT AND FERRIED THE AIRCRAFT TO PDX FOR REPAIRS. IN PDX, REPLACED THE LEFT GEAR DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008013000044 20080130 00044 NM 2008 1 30 QXEA200800041 1 20080123 A 2697 CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM FIRE LOOP DIRTY A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 406QX 4048 SEA - INTERMITTENT MASTER CAUTION FOR FIRE DETECTION. FAULT "A" FOR THE NUMBER 2 ENGINE. CYCLED OFF AND ON ABOUT 4 TIM ES OVER 3 MINUTES IN CRUISE, THEN NO FURTHER INDICATIONS FOR THE REST OF THE FLIGHT. MAINTENANCE INSPECTED THE FIRE LOO P FOR DAMAGE, NONE NOTED. CLEANED AND INSPECTED THE CONNECTOR FOR THE FIRE LOOP AND THE CONTROL AMPLIFIER. PERFORMED O PERATION CHECK WITH NO DEFECTS NOTED. RAN ENGINE AT 93 PERCENT FOR 15 MINUTES WITH NO DEFECTS. DISCREPANCY NOT DUPLICA TED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008013000050 20080130 00050 EU 2008 1 30 TRBA20080001 1 20080107 A 5320 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 369AT 369 RT INTERCOSTAL BETWEEN FRAME 36-38 CORRODED. RT INTERCOSTAL REPLACED AS PER SRM 51-25-01. 2 H 7 2 4T RT A53EU 2008013000053 20080130 00053 EA 2008 1 30 CHQA200800009 1 20080117 A 2150 32156222 PRESSURE VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 2 A/C PACK STUCK A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 486CA 1648 1648 7707 GEE873285 IAH TO MOB - WHILE CLIMBING THROUGH 1,500 FEET, CREW RECEIVED RIGHT PACK HIGH PRESSURE CAUTION MESSAGE ACCOMPANIED BY FA ULT LIGHT INDICATION ON RIGHT PACK BUTTON. CREW FOLLOWED QRH AND MESSAGE REMAINED. THE PACK WOULD NOT RECYCLE AND THE AIRCRAFT WOULD NOT PRESSURIZE DUE TO THE LEFT PACK BEING ON MEL. THE FLIGHT THEN RETURNED TO IAH AND LANDED WITHOUT INC IDENT. MAINTENANCE INSPECTED THE PACKS AND FOUND THE DUAL PRESSURE REGULATOR VALVE ON PACK 2 WAS STUCK OPEN. AFTER REP LACING THE DUAL PRESSURE REGULATOR VALVE THE RIGHT PACK OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2008013000054 20080130 00054 NM 2008 1 30 NWAA080266746 1 20080124 A 7603 POWER LEVER BOEING 747 747222B 1384904 NM NR 1 ENGINE MALFUNCTIONED A NWAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 01 646NW 23737 DURING THE TAKEOFF ROLL, THE NR 1 ENGINE WOULD NOT REACH TAKEOFF POWER. THE TAKEOFF WAS ABORTED AT 90KTS. DURING TAXI AFTER THE ABORTED TAKEOFF A BRAKE FIRE WAS REPORTED. MULTIPLE TIRES AND BRAKES WERE REPLACED. MAINTENANCE REPLACED THE NR 1 ENGINE POWER LEVER MIXING BOX AS CORRECTIVE ACTION FOR THE FAILURE TO REACH TAKEOFF POWER. ENGINE OPERATION WAS T HEN REPORTED AS NORMAL. 2 L 7 4 4F RT A20WE 2008013000058 20080130 00058 EU 2008 1 30 TRBA2008009 1 20080122 A 3350 E006478A50 SWITCH AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHTS FAILED A TRBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 29 541AT 541 AFTER BEGINNING TAXI, F/A CALLED AND SAID THAT THE EMERGENCY LIGHTS OVER BOTH F/A CONTROL PANELS WOULD NOT GO OUT. REMO VED AND REPLACED PUSH BUTTON SWITCH FIN NR 9LE AS PER ATR MM WIRING SCHEMATIC NR 33-12-02. PERFORMED OPT CK IAW JIC NR 33-20-00 AND FOUND OK. 2 H 7 2 4T RT A53EU 2008013000060 20080130 00060 2008 1 30 F3LA200800037 4 20080122 A 2565 D31516317 SLIDE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE R1 DOOR UNWANTED DEPLOY A F3LA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 03 922FR 566 2012 DURING THE TIME THE AIRCRAFT WAS ON THE GATE OVERNIGHT, A GATE AGENT INADVERTENTLY OPENED THE R1 DOOR AND DEPLOYED THE R 1 DOOR EMERGENCY ESCAPE SLIDE. MAINTENANCE REMOVED AND REPLACED THE DEPLOYED SLIDE WITH A NEW UNIT IN ACCORDANCE WITH T HE REQUIREMENTS OF AMM 25-62-44-400-006. FOLLOWING COMPLETION OF THE INSTALLATION, THE UNIT RIG CHECKED GOOD. CORRECTE D PART SN TO A12639 FROM A12679 AND ADDED TOTAL FLIGHT CYCLES. 2 L 7 2 4F 4 F RT A28NM 2008013000063 20080130 00063 EU 2008 1 30 TRBA20080011 1 20080127 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 377AT 377 MULTIPLE EMERGENCY LIGHTS ON ERRONEOUSLY. REPLACED EMERGENCY LIGHTS POWER SUPPLY 61WL AS PER 33-51-21 AND FOUND WORKING PROPERLY. 2 H 7 2 4T RT A53EU 2008013000064 20080130 00064 SO 2008 1 30 FDKA200801037 1 20080125 A 2120 DUCT EMB 145 EMB145LR 3260212 SO ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 852MJ 145567 FDM 6165 PNS-MCO - AC HAS AN ELECTRICAL BURNING ODOR IN THE CABIN AREA. MX REMOVED AND REPLACED AC DISTRIBUTION DUCT AS SY OPS GOOD AND CLEARED. 2 L 7 2 4T RT T00011AT 2008013000065 20080130 00065 SO 2008 1 30 FDKA200801038 1 20080125 A 3350 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 851MJ 145572 FDM 6015 JFK (1840 PHX LCL) - CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. MX RELAMPED AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2008013000066 20080130 00066 SO 2008 1 30 FDKA200801039 1 20080125 A 5340 ATTACH ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 834MJ 145340 THE FAIRING ATTACH ANGLE FOR PANEL 194 IS CRACKED ON THE RT SIDE OF THE FUSELAGE AT FRAME NR 49. THE DAMAGED ANGLE HAS BEEN REPAIRED. 2 L 7 2 4T RT T00011AT 2008013000067 20080130 00067 EU 2008 1 30 NWAA080273301 1 20080126 A 3350 BATTERY PACK AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 801NW 0524 CIDS 1 TEST OF EPSU FAILED, CARD 3351-7008 JOB 1-02, ATA 335100 BAT/EPSU (17WL) DOOR 4L. BATTERY PACK REPLACED. 2 L 7 2 4F RT A46NM 2008013000068 20080130 00068 NM 2008 1 30 UIEA200800017 1 20080114 A 2611 SMOKE DETECTOR BOEING 747 7472D3B 1384805 NM CARGO BAY DIRTY A UIEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 15 506MC 21252 AIRCRAFT DIVERTED TO SNN DUE TO NR 4 CARGO LIGHT SMOKE DETECTOR LIGHT CAME ON IN CRUISE. NR 4 A/B SMOKE DETECTORS CLEAN ED AND OPS CHECKED IAW 26-14-00, OPS CHECKED OK. 2 L 7 4 4F RT A20WE 2008013000071 20080130 00071 EU 2008 1 30 SIMA200802302 1 20080122 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 211NE 340B211 ON FLIGHT 3300, CREW DISCOVERED FOUR FLOOR EMERGENCY LIGHTS WERE INOP AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLAC ED EMERGENCY BATTERY NUMBER 24LN IAW SAAB 340 AMM 33-50-10. SYSTEM OPERATIONAL CHECK GOOD IAW SAAB 340 AMM 33-50-00. A IRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2008013000072 20080130 00072 SO 2008 1 30 SIAM200802304 1 20080122 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO MLG FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 675AE 14500806 ON FLIGHT 4372, CREW REPORTED THEY RETURNED TO FIELD FOR LANDING GEAR AIR GROUND FAIL MESSAGE. GEAR WOULD NOT RETRACT. CMC MESSAGE LAND GEAR PROX SW FAIL. AIRCRAFT REMOVED FROM SERVICE. FOUND NOSE GEAR AIR/GROUND PROX SWITCH HAD FAILED REMOVED AND REPLACED PROX SWITCH RETRACTION CHECK GOOD IAW 145 AMM 32-30-00-700-801-A. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008013000083 20080130 00083 EU 2008 1 30 SIMA200802801 1 20080118 A 5347 7253742407 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 320AE 21854 5000 340B320 DURING MBV INSPECTION, THE SEAT TRACK AT BL 36L WAS FOUND CORRODED. AIRCRAFT REMOVED FROM SERVICE. REPLACED SEAT TRACK WITH NEW ONE PN 7253742-407 IAW SAAB 340 SRM 51-40-21, 51-40-22, 51-40-25 AND 51-40-40. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2008013000090 20080130 00090 EU 2008 1 30 SIMA200802106 1 20080115 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 253AE 340B253 ON FLIGHT 3062 CREW REPORTED EMERGENCY EXIT LIGHTS DO NOT COME ON WITH SWITCH IN ON POSITION. AIRCRAFT REMOVED FROM SER VICE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AT LOCATION 20LN IAW SAAB AMM 33-50-10. OPERATIONAL CHECK GOOD AT TH IS TIME IAW SAAB AMM 33-50-00 AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2008013000093 20080130 00093 SO 2008 1 30 SIMA200802112 1 20080102 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 671AE 9733 5000 145793 AIRCRAFT WAS REMOVED FROM SERVICE. DURING IMBV INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND MANUAL L IMITS. REPAIRED OMEGA BEAM IAW SRM 53-00-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008013000098 20080130 00098 EU 2008 1 30 SIMA200802114 1 20080119 A 5347 7253725193 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 273AE 25047 5000 340B273 AIRCRAFT WAS REMOVED FROM SERVICE. DURING A HMBV INSPECTION, THE SEAT TRACK AT BL 18.3L WAS FOUND TO BE CORRODED. REMO VED CORRODED SEAT TRACK AND REPLACED WITH NEW PART NUMBER 7253725-193 IAW SAAB SRM CHAPTERS 53-70-60. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2008013000100 20080130 00100 EA 2008 1 30 CHQA200800011 1 20080120 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE SERVICE DOOR NOT CLOSED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 639BR 7313 GEE872507 IAH TO BTR - AFTER TAKEOFF CREW RECEIVED AN"OVBD COOL" EICAS MESSAGE. THE CREW NOTICED THAT THE CABIN PRESSURE WAS ABNO RMAL AND PROCEEDED TO THE UNPRESSURIZED FLIGHT PROCEDURE. WITH THE AIRCRAFT AT 4,000FT AND THE CABIN ALTITUDE AT 2,300F T THE "EMER DEPRESS SWITCH" WAS PRESSED AND THE CABIN PRESSURE EQUALIZED. THE FLIGHT RETURNED TO FIELD AND LANDED WITHO UT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE SERVICE DOOR HANDLE NOT PROPERLY STOWED. AFTER CYCLING THE DOORS THE PRESSURE SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2008013000104 20080130 00104 WP 2008 1 30 08FDEA00242 1 20080123 A 5230 AFA3805501 SKIN DOUG DC10 DC1030 3023501 WP CARGO DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 CENTER CARGO DOOR FWD LOWER EDGE IS DENTED. REPAIRED CENTER CARGO DOOR FWD LOWER EDGE IAW DC10 SRM 52-10-00 VOL I FIG 17 SHEET 1. 2 L 7 3 4F A22WE 2008013000111 20080130 00111 EU 2008 1 30 08FDEA00243 1 20080123 A 5522 SKIN AIRBUS 310 A310221 3930310 EU RT ELEVATOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 RT ELEVATOR APPROX STA 529 TOP SURFACE SKIN CORRODED. REPAIRED RT ELEVATOR UPPER SKIN CORROSION BY REMOVING DAMAGED SKI N, AND FABING SKIN PLUG AND DOUBLER, BONDING SKIN PLUG AND DOUBLER, EDGE SEALING REPAIR, AND REFINISHING IAW A310-20 0 SRM 51-77-12 FIG 224. 2 L 7 2 4F RT A35EU 2008013000112 20080130 00112 EU 2008 1 30 MALA080012 1 20080119 A 5320 RISER SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 RT BOTTOM CORNER OF FLIGHT DECK ENTRANCE RISER "T" SECTION CORRODED. REPAIRED IAW EO NR S53185. 2 L 7 2 4T RT A52EU 2008013000113 20080130 00113 WP 2008 1 30 IXXA080004O 1 20080124 A 3260 H2024B SWITCH DOUG DC8 DC873F 302199F WP MLG DOOR DEFECTIVE A IXXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 11 606AL 96268 363 46044 DURING CLIMB FROM KTOL, AFTER GEAR WAS RETRACTED DOOR NOT LATCH LIGHT CAME ON, THE CREW CYCLED THE GEAR THE LIGHT STAYED ON. THE CREW ACCOMPLISHED UPLATCH CHECK AND CYCLED THE GEAR A SECOND TIME THE LIGHT STAYED ON. THE CREW CLIMB TO 32,0 00 FEET CYCLED THE GEAR A THIRD TIME IN LEVEL FLIGHT AND LIGHT STAYED ON, THE LIGHT IS EXTINGUISHED WITH GEAR EXTENDED. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED GEAR DOOR SWITCH IAW DACO DC-8 MAINTENANCE MANUAL 32-60-0. OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2008013000123 20080130 00123 NM 2008 1 30 08FDEA00236 1 20080123 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 950D CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 MAIN DECK FLOORBEAM UPPER "T" CAP CORRODED, BS 950D, RBL 9-23 THIS SDR WAS ENTERED IN ERROR AND WILL NOT BE USED. THIS IS A DUPLICATE OF SDR NR 08-0235. THIS SDR ENTERED IN ERROR - ADMINISTRATOR. 2 L 7 3 4F RT A3WE 2008013000125 20080130 00125 EU 2008 1 30 08FDEA00237 1 20080122 A 3010 ABS104096 SEAL AIRBUS 300 A300F4605R 3930327 EU BLEED SYSTEM LEAKING A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 672FE 779 PHX - HAD AN ENGINE NR 1 BLEED LEAK ON T/O OUT OF DEN. ENGINE WING A/I WERE ON. FOUND A/I SUPPLY DUCT LEAKING AT FWD L T CONNER OF A/C BAY. REF A300-600 IPC 36-11-03-02A. ADDED MPN BA5614-5, CPN 3010434 QTY 1 SLEEVE ADDED MPN D40C60, CPN 2111350 QTY 2. REMOVED CLAMPS, LOOPS AND ROD SUPPORTS FROM PNEUMATIC DUCT IN FWD LT CORNER IN AIR CONDITIONING BAY. F OUND TWO SEALS LEAKING AT EXPANSION JOINTS. REF : IPC 36-11-03-02A SEALS ON ORDER. REMOVED AND REPLACED 2 SEALS IN DUC TING PER MM 36-11-00-4. INSULATION BLANKET PUT ON "OIL" WRI 30-10/8985. 2 L 7 2 4F RT A35EU 2008013000131 20080130 00131 NM 2008 1 30 DLM90080066 1 20080116 A 5512 5922578521 SKIN DOUG MD90 MD9030 3023690 NM HORIZONTAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 RIGHT HORIZONTAL STAB UPPER SKIN CRACKED APPROX 2 INCH LONG OUTBOARD OF STA XH 27.34 AND FORWARD OF REAR SPAR. REPAIRED RIGHT HORIZONTAL STAB UPPER SKIN IAW DELTA ERA 459896-14 REV ORIGINAL DATED 01--09-08 ON N/R 3400-0076 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008013000140 20080130 00140 EA 2008 1 30 SWIA200819081 1 20080120 A 2611 SMOKE WARNING CNDAIR CL600 CL6002C10 1390015 EA LAVATORY FALSE ACTIVATION A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 703SK 10139 FLT 5876 - RECEIVED A "SMOKE AFT LAV" WARNING MESSAGE. INSPECTED LAV AREA AND ASSOCIATED SYSTEMS WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2008013000154 20080130 00154 NM 2008 1 30 DLM88080084 1 20080116 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 737 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 EXFOLIATION CORROSION ON LT CABIN CUSP WEB Y=737. REPAIRED CUSP WEB IAW ERA 398191-14 MA REV A. 2 L 7 2 4F RT A6WE 2008013000159 20080130 00159 EU 2008 1 30 08FDEA00263 1 20080124 A 5420 A2611501200200 HEAT SHIELD AIRBUS 310 A310221 3930310 EU NR 1 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 PYLON NR 1 FWD ENG MOUNT, HEAT SHIELD CRACKED (MKD). REMOVED HEAT SHIELD NR 1 ENG PYLON IAW FEDEX A310-200 SRM 51-40-2 1 PAGE 1. RECEIVED NEW HEAT SHIELD P/N A2611501200200 S/N IC673554 PO 605041.1 FROM SUPPLY. INSTALLED NEW HEAT SHIELD IAW FEDEX A310-200 SRM 51-40-21 PAGE 7. 2 L 7 2 4F RT A35EU 2008013000164 20080130 00164 WP 2008 1 30 08FDEA00245 1 20080123 A 5322 ADA000319 SHEAR TIE DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 LOWER FORWARD CARGO, STA 1099 BETWEEN L33L AND L35L, SHEAR TIE HAS CORROSION ON LOWER FLANGE, PART ADA0003-19 REMOVED CO RROSION IAW DC/MD10-10 SRM, VOLUME II, 51-21-01 PAGE 28. ORIGINAL THICKNESS IS .071 IAW DAC DWG ADA0003, REV M, PARTS L IST, ITEM -19. MATERIAL REMOVED IS .030", MATERIAL REMAINING IS .041" PER TIMCO TOOL ( 8225B). FOUND TO BE OUT OF LIMI TS IAW DC/MD10-10 SRM, VOLUME I, 53-00-01, FIGURE 1B. FABRICATED NEW -19 IAW DAC DWG ADA0003, REV M. HEAT TREAT LOAD N UMBER FOR NEW -19 IS( HT011508-1). MATERIAL ID FOR NEW -19 IS 7075-O, .071", PO NR 591979.2. INSTALLATION OF NEW -19 ACCOMPLISHED ON FEDEX NON-ROUTINE NR N00454. 2 L 7 3 4F RT A22WE 2008013000167 20080130 00167 EU 2008 1 30 08FDEA00248 1 20080123 A 7830 THRUST REVERSER AIRBUS 300 A300F4605R 3930327 EU NR 1 INOPERATIVE A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 662FE 761 RTO AT 115 KTS FOR MASTER CAUTION LIGHT AND NR 1 TR UNLOCKED MESSAGE ON ECAM ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30 -01-A CATEGORY: C EXPIRATION: 03FEB08 "MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) NR 1 THRUST REVERSER, INOP. THRUST REV ERSER IS DEACTIVATED IN FORWARD THRUST POSITION." REACTIVATED NR 1 T/R. T/S AND PERFORMED NUMEROUS OPS CHECKS WITH NO F AULTS FOUND. CHECKED OPS PER M.M. 78-31-00-5 CHECKS GOOD. INSPECTED C/P'S AND PERFORMED SHAKE TESTS OF ALL ASSOCIATED W IRING WITH NO FAULTS NOTED. ITEM CLEARED, A/C RETURNED TO SERVICE. 2 L 7 2 4F RT A35EU 2008013000168 20080130 00168 NM 2008 1 30 08FDEA00250 1 20080124 A 5720 SUPPORT DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 FOUND CORROSION LEFT WING, OUTBOARD FLAP INBOARD HINGE AFT FAIRING SUPPORT INBOARD FORWARD FASTENER HOLE. MINOR CORROS ION REPAIRED AS PER SRM 51-21-01 VOLUME II AND FOUND WITHIN LIMIT AS PER DRAWING ARC1984. REPAIR CLASSIFIED AS MINOR P ER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008013000171 20080130 00171 NM 2008 1 30 08FDEA00252 1 20080124 A 5720 ARC2126501 STRUT DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 FOUND CORROSION, LT WING OUTBOARD FLAP INBOARD HINGE AFT FAIRING STRUT AFT FASTENER HOLE. CORROSION REPAIRED AS PER E A 1-5750-117306, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008013000181 20080130 00181 NM 2008 1 30 DLM90080059 1 20080112 A 5322 9953016429 SHEAR TIE DOUG MD90 MD9030 3023690 NM BS 1486 L3L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 FOUND STA 1486 L3L SHEAR TIE CRACKED. REMOVED AND REPLACED CRACKED SHEAR TIE, IAW MD90 SRM 51-30-5. 2 L 7 2 4F RT A6WE 2008013000182 20080130 00182 NM 2008 1 30 DLM90080063 1 20080109 A 5280 SKIN DOUG MD90 MD9030 3023690 NM RT MLG DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 RMLG DOOR EXTERIOR SKIN CORRODED OVER ENTIRE SURFACE. REPLACED RMLG DOOR. 2 L 7 2 4F RT A6WE 2008013100001 20080131 00001 SO 2008 1 31 C2XA08TY012 1 20080117 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16954 145072 TYS - DURING ROUTINE MX THE EMERGENCY FLOOR LIGHT STRIP BETWEEN ROWS 10 & 12 WAS FOUND INOP. MX RECONNECTED THE LIGHT S TRIP WIRES AND THE OPS CHECK WAS GOOD. A/C WAS RELEASED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008012900092 20080129 00092 EU 2008 1 29 2008UALA00054 1 20080102 A 2750 4911710 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SLAT FLAP CONTRL FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 410UA 463 FLAPS ARE SLOW TO EXTEND. SFCC FAULTY. REPLACED SLAT FLAP CONTROL COMPUTER. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900133 20080129 00133 2008 1 29 2008UALA00172 4 20080109 A 2312 284T022319 ANTENNA BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE VHF COMM FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 677UA 30029 NR 1 VHF COMM XMISSIONS ABNORMAL AT ALL CREW STAT'N (1= L VHF, 2=R VHF). CREW COMMENTS: ATC HAD POOR RECEPTION USING H EADSET AND HAND MIKE. REPLACED, AND OP CHECKED LT VHF ANTENNA REF MM 23-12-03, CKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20080916 EU 2008 9 16 08FDEA03176 1 20080730 A 5347 A5370617920000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CABIN CROSS SEAT TRACK AT FRAME 29; LBL 30 IS CRACKED. REMOVED THE CROSS SEAT TRACK AT FRAME 29 IAW A300-600 SRM 5 1-40-21. LOCATED AND DRILLED AND COUNTERSUNK HOLES FOR THE NEW CROSS SEAT TRACK P/N A5370617920000, PO 627372.1 IAW A 300-600 SRM 51-40-10. INSTALLED THE CROSS ADAPTER SEAT TRACK IAW A300-600 SRM 51-40-21 AND DWG A53781942, REV "D". AP PLIED CIC IAW A300-600 AMM 51-22-00-0. 2 L 7 2 4F RT A35EU 20080916 WP 2008 9 16 08FDEA02963 1 20080717 A 5730 ARC05851 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING T/E PANEL 541 IB IS GOUGED. REMOVED DAMAGE. FABRICATED REPAIR DOUBLERS AND FILLERS. PREPARED FOR BONDING. BONDED AND CURED REPAIR DOUBLERS AND FILLERS IAW DC/MD-10 SRM 51-71-00; VOL II. APPLIED SEALANT AND PRIMER IAW DC/MD-10 SRM 51-71-00; VOL II. 2 L 7 3 4F RT A22WE 20080916 WP 2008 9 16 08FDEA02964 1 20080717 A 5730 AUB126819 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING L/E PANEL 518 FB IS CHAFED. REPAIRED THE LT WING INBD L/E PANEL 518 FB BY REMOVING THE DAMAGED AREA AND BONDE D A FILLER AND DOUBLER IAW SRM 51-71-00; VOL II. PRIMED AND PAINTED IAW SRM 51-21-02; VOL II. 2 L 7 3 4F RT A22WE 20080916 WP 2008 9 16 08FDEA03730 1 20080905 A 5320 1299385 ANGLE DOUG MD10 MD1010F 3022112 WP BS 1505 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 RIGHT MLG WHEEL WELL STA 1505; AFT SHELF AREA, FWD WEB, LOWER ANGLE IS CRACKED. REMOVED & RE-INSTALLED PANEL 144 AZ IAW SRM 51-31-01; VOL II. REMOVED CRACKED ANGLE IAW SRM 51-31-01. HEAT TREATED 7075-0 TO T6 IAW TPS 1003; REV " A ". HRD 88-89, NT09210801. AODINED; PRIMED & PAINTED ANGLE IAW SRM 51-21-01. MARKED IAW FEDEX GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20080916 WP 2008 9 16 08FDEA03731 1 20080905 A 5730 ARB1066504 SKIN DOUG MD10 MD1010F 3022112 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 RIGHT WING L/E SKIN IS CRACKED AT THE NR 3 SLAT CENTER TRACK CUT-OUT. REMOVED 2 EA PANELS TO FOM IAW SRM 51-31-01. REM OVED OLD REPAIR DOUBLER IAW SRM 51-35-02. CUT PUT DAMAGED AREAS. FABRICATED IAW SRM 57-10-00. ALODINED & PRIMED IAW S RM 51-21-01. INSTALLED DOUBLER, FILLER & ACCESS PANELS IAW SRM 51-33-01 & 51-31-01. 2 L 7 3 4F RT A22WE 20080916 NM 2008 9 16 08FDEA03463 1 20080817 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 DURING OPEN HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CR ACK INDICATIONS AT HOLES C AND D. MAIN CARGO DOOR LOWER JAMB CRACKED SUPPORT FITTING NR 7 REMOVED AND REPLACED AS PER S RM 51-31-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080916 EU 2008 9 16 08FDEA03733 1 20080905 A 2611 CG7G011 SMOKE DETECTOR AIRBUS 300 A300B4622 3930401 EU E/E BAY FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 720FD 417 "AVIONICS SMOKE" WARNING ILLUMINATED AT 9000' ON CLIMB-OUT. ACCOMPLISHED ALL QRH PROCEDURES. INSPECTED AVIONICS COMPAR TMENT, MIN EQUIP BAY AND COCKPIT FOR EVIDENCE OF SMOKE OR FIRE. NO DISCREPANCIES FOUND. AVIONICS SMOKE DET WARNING, D ISPLAYS AND ALERT LIGHTS WOULD NOT CLEAR. FOUND DUCT SMOKE DETECTOR 11WA FAULTY. REMOVED AND REPLACED 11WA DETECTOR . 2 L 7 2 4F RT A35EU 20080916 NM 2008 9 16 08FDEA03464 1 20080818 A 5315 141N5150 FLOORBEAM BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 CORROSION ON CABIN FLOORBEAM AT BS 324, LBL 20. MINOR SURFACE CORROSION BLENDED OUT AND SURFACE TREATED, FOUND WITHIN A LLOWABLE LIMIT IAW B757-200 SRM 53-00-51 REV. 93 DETAIL III FIG 101. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRIT ERIA. 2 L 7 2 4F RT A2NM 20080916 NM 2008 9 16 08FDEA03721 1 20080904 A 5320 AFS71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 574FE 48499 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT F ITTING AT HOLE C. MAIN CARGO LOWER JAMB NO. 1 FITTING AT HOLE C CARRIED OUT BUSHING REPAIR AS PER SRM 53-50 -00 FIGU RE 10 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080916 NM 2008 9 16 08FDEA03723 1 20080904 A 5320 AFS71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 574FE 48499 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTI NG AT HOLES C AND D. MAIN CARGO DOOR LOWER JAMB NO. 3 AT HOLES C AND D CARRIED OUT BUSHING REPAIR AS PER SRM 53-50 -00 FIGURE VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080916 NM 2008 9 16 08FDEA03726 1 20080905 A 5330 651753073 SKIN BOEING 727 727227 1384078 NM BS 1214 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 CRACK TAIL SKID CUTOUT EXTERIOR SKIN STA 1214 TRIMMED OUT DAMAGED AREA DIM 1/4 PER 1/2 INCH IAW B727 SRM 53-10-3 FIG 1. FABRICATED REPAIR DOUBLER MAT USED 2024T3 0.050 IAW B727 SRM 53-30-2 FIG 3 AND 53-30-3 FIG 1. TREATED AND PRIMED AREA AND REPAIR PART IAW B727 SRM 51-10-2. INSTALLED COUNTERSINK WASHER IAW B727 SRM 51-30-8. INSTALLED REPAIR DOUBLER IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 20080916 NM 2008 9 16 08FDEA03729 1 20080905 A 2731 418575 ACTUATOR DOUG MD11 MD11F 3023600 NM STAB TRIM LEAKING A FDEA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 21 586FE 46472 23624 48487 AFTER SLAT RETRACT ON CLIMB-OUT, RECEIVED " HYD 3 ELEV OFF " ALERT. APPROX 5 MINS LATER, GOT "HYD 3 FAIL" ALERT. COMP LIED WITH QRH. MANUALLY EXTENDED GEAR ON APPROACH. HYD LEAK FROM NR 1 HORIZ STAB TRIM MOTOR BODY. R & R STAB TRIM MOTO R, MM 27-43-30-4. DURING OPS CHECK, FOUND "HOR STAB TRIM RATE CTRL 2" C/B POPPED. TROUBLESHOT & C/B STAY IN AFTER DISC ON ELEC CON FROM M1-16, BUT TRIPS WHEN STATES ABOVE. CONNECTOR RECONNECTED. TROUBLESHOT & FOUND SHORT INSIDE OF DUAL SO L VALVE ON M1-16 TRIM MOT. REF WDM 22-22-01 P501. R & R PER MM 27-43-41-4 & H-STAB HYD OPS NORM NO LEAKS PER MM 27-40- 00-5. FCC-1/-2 AFS RTS PER MM 22-01-01-5 & ALL TESTS PASS. ACFT RTS. PER MM 22-01-01-5 & ALL TESTS PASS. 2 L 7 3 4F RT A22WE 20080916 NM 2008 9 16 08FDEA03221 1 20080803 A 5350 2024T3 FRAME BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 LOWER FUSELAGE LEFT MID SUPPORT FRAME FOR FAIRING 197LL HAS SURFACE CORROSION. REPAIR CARRIED OUT ON WING-TO-BODY FUSEL AGE STRUCTURE LOWER CHORD IAW EA NR F-5320-124303. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 2 4F RT A2NM 20080916 NM 2008 9 16 08FDEA03224 1 20080803 A 5315 143N537035 FLOORBEAM BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 AT BS 650 RBL 8, CORROSION ON FLOOR SUPPORT BEAM. CORROSION FOUND EXCEEDED SRM LIMITS. STRINGER REMOVED AND REPLACED I AW B757-200 SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 2 4F RT A2NM 20080916 NM 2008 9 16 08FDEA03226 1 20080804 A 5330 BACR15BB5D4C SKIN BOEING 757 75723A 1384967 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 LT LWR FUSELAGE FROM BS 1460 TO 1480 BETWEEN STR 27L AND 28L HAS EXISTING LIGHTNING STRIKE REPAIR. EXISTING REPAIR EV ALUATED AS PER EO F-5100-7-5001 PT 1. FOUND ACCOMPLISHED IAW B757-200 REM 53-00-01 FIG 201, REPAIR 6 SECT 1, BASED ON E XTERNAL VISUAL EVALUATION OF THE REPAIR. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080916 NM 2008 9 16 08FDEA03465 1 20080818 A 5315 141N5111 FLOORBEAM BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 CABIN FLOORBEAM AT BS 350, LBL8, HAS CORROSION. MINOR SURFACE CORROSION BLENDED OUT AND SURFACE TREATED AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW B757-200, SRM 53-00-51 REV 93 DETAIL III, FIG 101. REPAIR IS CLASSIFIED AS MINOR PER GMM 6 -2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080916 EU 2008 9 16 08FDEA03467 1 20080818 A 5740 A57340086 SUPPORT BRACKET AIRBUS 300 A300B4622R 3930312 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 ELONGATED HOLE ON LT PYLON TO WING SUPPORT BRACKET AND BOTTOM SKIN. REPAIR PERFORMED BY OVERSIZING THE HOLES AND INSTAL LING FREEZE PLUGS IAW. DRAWING R571-50532 ISS A AND RAS/BAE/1007780/2008, APPROVED BY EA 6-2900-123041. 2 L 7 2 4F RT A35EU 20080916 WP 2008 9 16 08FDEA03097 1 20080728 A 5340 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP DOOR FRAME DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 MAIN CARGO DOOR JAMB AT SPOOL FITTING NR 2, HOLE "D" IS OVERSIZED TO 0.545 INCH. REMOVED WEB AND STRUCTURE IN REF TO D C/MD-10 SRM 51-33-01; VOL II AND 51-35-01; VOL II. REMOVED BACK UP FITTING IN REF TO DC/MD-10 SRM 51-33-01; VOL II. L OCATED AND DRILLED THE BACK UP FITTING IN REF TO DAC DWG AFA 7132; REV "B". INSTALLED BACK UP FITTING, REF TO DC/MD-10 SRM 51-33-01; VOL II. INSTALLED BUSHING ON THE BEAM IN REF TO EA 8-5310-117003 "FUSELAGE, MAIN DECK CARGO DOOR JAMB L OWER SEAL OVERSIZED HOLES AT THE NR 1 AND NR 2 SPOOL FITTINGS REPAIR". 2 L 7 3 4F RT A22WE 20080916 EU 2008 9 16 08FDEA03550 1 20080822 A 5414 A5461216200300 PANEL AIRBUS 300 A300F4605R 3930327 EU NR 1 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 THE NR 1 ENGINE PYLON PANEL NR 475 AL HAS A 3/8 INCH CRACK AT THE RADIUS. COMPLIED WITH FEDEX EA 6-5480-123386 "NACELL ES/PYLON, NR 1 ENGINE PYLON 475 AL EQUIPMENT ACCESS PANEL ASSY, CRACK WELD REPAIR". 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03472 1 20080818 A 5311 A53981311203 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND DEFORMED FRAME FLANGE, C 74, P 26-27 RT. REPAIR PERFORMED BY REWORK OF OUTER FLANGE AT RUN OUT TO ELIMINATE THE D EFORMATION IAW RAS/EFW/9000059/2008 ISS A, APPROVED BY EA 6-5318-123090. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03738 1 20080905 A 5220 E009240160 BONDING STRAP AIRBUS 310 A310222 3930315 EU RT OVERWING EXIT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 RIGHT OVERWING EMERGENCY EXIT, LOWER 2 EA BONDING STRAP SCREWS AND BONDING STRAPS HAVE CORROSION. CLEANED AREA IAW SRM 51-73-10. NO MATERIAL LOSS. ATTACHED THE BONDING STRAP TO BONDING POINT IAW SRM 51-40-21. BONDING CHECK GOOD IAW AMM 20-28-11-0. 2 L 7 2 4F RT A35EU 20080916 WP 2008 9 16 08FDEA03474 1 20080818 A 5522 NLC6039502 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 300 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 RT STAB INBD ELEV, XE 118, DENT ON UPPER SKIN. DIMENSIONS ARE 1 INCH BY 1 INCH BY .075 INCH. REPAIR SKIN IAW SRM 55-00 -01 VOL 1 FIG 3 SHEET 2. 2 L 7 3 4F RT A22WE 20080916 EU 2008 9 16 08FDEA03475 1 20080818 A 5754 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU NR 2 SLAT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 SLAT NR 2 LT WAS DAMAGED AT RIB 12-14 REPAIR PERFORMED IAW SRM 57-43-11 PARA 4A. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03739 1 20080905 A 5220 RETAINER AIRBUS 310 A310222 3930315 EU DOOR SEAL CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 LEFT OVERWING EMERGENCY EXIT, LOWER SEAL RETAINER OUTBD SURFACE HAS CORROSION AROUND THE FASTENERS ON 3 EA SECTIONS. REMOVED THE LOWER SEAL RETAINERS IAW SRM 51-40-21. REMOVED LOWER CHANNEL IAW SRM 51-40-21. REMOVED THE CORROSION IAW S RM 51-74-10. ALODINED IAW SRM 51-21-10. PRIMED IAW SRM 51-21-10. RCEIVED & INSTALLED THE LOWER CHANNEL IAW SRM 51-40- 01. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03742 1 20080905 A 5230 A5237204320200 SKIN AIRBUS 300 A300F4605R 3930327 EU CARGO DOOR CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 THE FWD LOWER CARGO DOOR INTERNAL SKIN IS CHAFFED AT DOOR FRAMES 7 AND 9. BLENDED IAW A300-600 SRM 51-74-10. UPON FURT HER INVESTIGATION MATERIAL REMAINING 0.050. FOUND TO BE WITHIN LIMITS IAW A300-600 52-30-00. ALODINED IAW A300-600 SRM 1-21-10; PARA 5-C. PRIMED AND PAINTED IAW A300-600 SRM 51-23-10, PARA 3-C. 2 L 7 2 4F RT A35EU 20080916 NM 2008 9 16 08FDEA03744 1 20080905 A 5330 655623610 SKIN BOEING 727 727233 138408A NM BS 680 S23L DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 OPEN HOLE IN SKIN AT BS 680 STR 23L. FABRICATED AND INSTALLED FREEZE PLUG IAW B727 SRM 51-10-7, FABRICATED RETAINING PL ATES USING 7075-T6 .040 PO NR 9007294 DIMS 3" BY 1" AND INSTALLED REPAIR PARTS IAW FEDEX EA 7-5330-117034, OPEN HOLE IN SKIN AT BS 680 STR 23L, REPAIR. 2 L 7 3 4F RT A3WE 20080916 WP 2008 9 16 08FDEA03745 1 20080905 A 5320 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 6 SPOOL BACK UP FITTING HOLE "B" HAS A CRACK INDICATION. INSTALLED BUSHINGS IN THE NR 6 BACK UP FITTING HOLE "B" AND REAMED UP TO SIZE (.453) IAW SRM 53-50-00; VOL II. 2 L 7 3 4F RT A22WE 20080916 WP 2008 9 16 08FDEA03746 1 20080905 A 5311 ACA72305 FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 THE SUB-FRAME AT STA 755 HAS A CRACK BELOW THE MCD AT LONGERON 29L. MATERIAL ID FOR DOUBLER 7075-T6511, PO 568806.2; SH IM 7075-T6 0.100, PO 584757.3 AND THE FILLER 7075-T6 0.071 PO 629996.2 IAW DAC DWG NR ACA 7230 AND DC/MD-10 SRM 51-10-01 ; VOL III. REMOVED DAMAGED AREA AND FABRICATED AND LOCATED HOLES IAW DC/MD-10 SRM 53-00-01;VOL I. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01; VOL II. INSTALLED DOUBLER, SHIM AND FILLER IAW DC/MD-10 SRM 51-33-01; VOL II. 2 L 7 3 4F RT A22WE 20080916 NM 2008 9 16 08FDEA03115 1 20080729 A 5310 ACA72261 DOOR FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 CRACK INDICATION FOUND ON FIRST LAYER DURING HFEC OPEN HOLE INSPECTION ON 0.520" HOLE AT MAIN CARGO DOOR NR 6 LOWER JAMB AT HOLE C. MAIN CARGO DOOR NR 6 LOWER JAMB AT HOLE C, CRACK ON FIRST LAYER REPAIRED AS PER FEDEX EA NR 1-5310-124331, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080916 WP 2008 9 16 08FDEA03005 1 20080721 A 5340 AGA32285 ATTACH ANGLE DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 AFT CARGO STA 1967 GILL LINER ATTACH ANGLE AT THE CARGO FLOOR AND ACROSS CEILING ATTACH ANGLE HAS CORROSION ON THE BACKS IDE AROUND CAMLOCK RECEPTICLES. REMOVED CAMLOKS FROM THE CEILING RETAINER TO FOM, CORROSION REMOVAL REF DC/MD-10 SRM 51 -35-01; VOL II. REMOVED CORROSION REF DC/MD-10 SRM 51-21-01, VOL II. ORIGINAL THICKNESS 0.040 RF DAC DWG AGA 3228. MA TERIAL REMOVED 0.002 (UT GAUGE T8253B). MATERIAL REMAINING 0.038 AND FOUND TO BE WITHIN LIMITS REF DC/MD-10 SRM 53-00-0 1; VOL I. ALODINED, PRIMED AND REPLACED CAMLOKS REF DC/MD-10 SRM 51-21-01 AND 51-35-01; VOL II. LOWER GILL LINER ATTAC H ANGLE FOUND TO BE CRACKED. REMOVED AND REPLACED ANGLE REF DAC DWG AGA 3228, REV AB AND SRM 51-21-01. 2 L 7 3 4F RT A22WE 20080916 EU 2008 9 16 08FDEA03131 1 20080729 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CABIN SEAT TRACK AT APPROX RBL 37 INCH, BETWEEN FRAMES 41 AND 42 HAS CORROSION IN THE TRACK. SEAT TRACK FOUND TO B E OUT OF LIMITS IAW A300-600 SRM 53-10-16. TOOL USED T8492F. REMOVED SEAT TRACK IAW A300-600 SRM 51-40-21. MATERIAL I D OR NEW SEAT TRACK IS A5327400500053, PO 624926.1 IN REF TO A300-600 SRM 53-15-16 AND AIRBUS SM NSA348076. CUT SEAT TR ACK AND DRILLED HOLES IN REF TO A300-600 SRM 53-10-16. PART MARKED NEW SEAT TRACK IN REF TO GMM 7-0-1001. INSTALLED NE W SEAT TRACK IAW A300-600 SRM 53-10-16. CIC'D SEAT TRACK IAW A300-600 AMM 51-22-00-0. 2 L 7 2 4F RT A35EU 20080916 NM 2008 9 16 08FDEA03294 1 20080806 A 5315 7075T60063 FLOORBEAM BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 AT BS 1630, 63LBL, FLOOR SUPPORT ANGLE HAS CORROSION. CORROSION FOUND EXCEED SRM LIMITS. REPAIR CARRIED OUT IAW B757-20 0 SRM 51-70-12 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080916 NM 2008 9 16 08FDEA03084 1 20080725 A 5320 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 577FE 48469 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLES A, B, C AND D BUSHING. R EPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL 1. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. R EPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080916 NM 2008 9 16 08FDEA03085 1 20080725 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 577FE 48469 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FITTING AT HOLES A, B, C AND D BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL. 1. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL . II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6- 2-100. 2 L 7 3 4F RT A22WE 20080916 NM 2008 9 16 08FDEA03269 1 20080805 A 2780 859803 PROXIMITY SWITCH DOUG MD11 MD11F 3023600 NM NR 2 SLAT MALFUNCTIONED A FDEA O OTHER N FALSE WARNING AP APPROACH 1 CE 21 599FE 27501 27501 48598 DURING APPROACH TO LFPG EXPERIENCED A LEVEL NR 2 "SLAT DISAGREE" ALERT DURING SLAT EXTENSION. COMPLIED WITH QRH AND C ONDUCTED A FLAP/RETRACT LANDING TO RUNWAY 26R AT LFPG. LANDING WEIGHT WAS REDUCED AS MUCH AS POSSIBLE AND NO FURTHER PR OBLEMS WERE ENCOUNTERED. CREW DECLARED A EMERGENCY. T/S AS PER FIM:31-71-07-00. SELF TEST ON PSEU SHOWED NO FAULT, LE G-1 WAS SHOWING A FAULT CODE 12. FOLLOWED T/S TREE, REMOVED AND REPLACED PSEU AS PER AMM:31-71-01-2. CARRIED OUT ADJ/T EST AS PER AMM:31-71-01-2 AND PERFORMED SLAT ELECTRICAL CONTROL ADJ/TEST AS PER AMM:27-86-00-5. ALL TESTS PASSED. A/C OK FOR SERVICE. RETURNED TO SERVICE. 2 L 7 3 4F RT A22WE 20080916 EU 2008 9 16 08FDEA03270 1 20080805 A 5314 KEELBEAM AIRBUS 300 A300F4605R 3930327 EU MLG GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN LANDING GEAR WHEEL WELL AFT OF THE KEEL BEAM BOX AT FRAME 54, THE RIGHT AFT SIDE OF THE BOX MARKED IN RED. THE FIT TING IS GOUGED. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03227 1 20080804 A 5315 A53978267202 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSIONN ON CROSSBEAM C 66 OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03231 1 20080804 A 5313 A53973320200 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON STRINGER P 54RH, C 71-72 OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03236 1 20080804 A 5210 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU L4 DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 DENT AND SCRATCH FOUND AT PAX DOOR 4 LT (DENT OUT OF LIMIT). REPAIR PERFORMED BY REWORK OF DAMAGED AREA, NDT FOR CRACK FREE CONDTION AND FLAP PEENING IAW RAS/DAHAM/4025321/2008 ISS A , APPROVED BY EA 6-5213-123026. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03237 1 20080804 A 5330 A53974207200 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON SKIN PANEL C 71-72, P 57 LT. REPAIR PERFORMED BY CORROSION REMOVAL, NDT FOR SKIN THICKNESS AND FLAP PEENING IAW RAS/EFW/9000068/2008 ISS A, APPROVED BY EA 6-5317-123009. 2 L 7 2 4F RT A35EU 2008011100118 20080111 00118 NM 2008 1 11 SWAA080105 1 20080103 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011100178 20080111 00178 NM 2008 1 11 SWAA080134 1 20080105 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 15 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008011100184 20080111 00184 NM 2008 1 11 SWAA080140 1 20080106 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011100185 20080111 00185 NM 2008 1 11 SWAA080141 1 20080106 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011100218 20080111 00218 EA 2008 1 11 COMA0860014 1 20080102 A 3620 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA ENGINE MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 926CA 7027 FLIGHT 5004 - RECEIVED ANTI-ICE DUCT WARNING MESSAGE. DECLARED EMERGENCY, RETURNED TO DSM, LANDED WITHOUT INCIDENT. PE RFORMED ENGINE RUN AND TROUBLESHOOTING. OPS CHECKS GOOD. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100250 20080111 00250 EA 2008 1 11 COMA0860028 1 20080103 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 924CA 15910 7026 FLIGHT 5483 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED PDU. NO FURTHER DEFEC TS. 2 L 7 2 4F RT A21EA 2008011100251 20080111 00251 EA 2008 1 11 COMA0860029 1 20080103 A 2752 852D10021 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 924CA 9521 7026 FLIGHT 5483 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEFT FLAP ACTUATOR NR 1. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100252 20080111 00252 EA 2008 1 11 COMA0870030 1 20080103 A 2752 852D10021 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 924CA 3253 7026 FLIGHT 5483 - RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEFT FLAP ACTUATOR NR 2. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008012900140 20080129 00140 NM 2008 1 29 2008UALA00175 1 20080109 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 EEL LIGHT TORN UP FIRST CLASS RIGHT SIDE. REPAIR EEL LIGHT ASSY, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900151 20080129 00151 SO 2008 1 29 C2XA08TY011 1 20080116 A 3610 8166011 VALVE EMB 145 EMB145XR 3260214 SO BLEED AIR SYS MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14188 14500929 BLEED 1 & 2 LOW TEMP WING ANTI ICE (2) FAIL WHILE IN ICING CONDITIONS. REMOVED AND REPLACED HIGH STAGE VALVE AND LOW PR ESSURE SWITCH IAW EMB 145 XR AMM 36-11-02 & 30-11-11, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. SWITC H P/N APS7-1000, S/N 730-2-255. 2 L 7 2 4F RT 2008012900155 20080129 00155 NM 2008 1 29 SB08001 1 20080108 A 3350 1012721 LIGHT BOEING 737 737401 1384701 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 418US 23985 CLT - MAINTENANCE REPORTED AN AFT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASS EMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008012900164 20080129 00164 NM 2008 1 29 USAA920080189 1 20080116 A 5330 6545775 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 422US 23989 CLT - MAJOR REPAIR - C2 CHECK - CRACKED FUSELAGE SKIN, BS 727D, S23R. REPAIRED FUSELAGE SKIN, BS 727D, S23R IAW B737 SR M 53-00-01. 2 L 7 2 4F RT A16WE 2008012900171 20080129 00171 EU 2008 1 29 2008UALA00125 1 20080107 A 2920 1211523239 PRESSURE SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RAT FAILED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 484UA 1609 HYD RAT UPPER ECAM, LOWER ECAM HYD PAGE SHOWS RAT IN AMBER. FAULT IS CLEAR BUT HAS MANY HITS. RAT PRESSURE SWITCH FAIL URE. REPLACED RAT PRESSURE SWITCH. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900172 20080129 00172 2008 1 29 2008UALA00147 4 20080108 A 2211 B546CCM0104 COMPUTER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE AUTOPILOT SYS FAULTY A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 824UA 965 FLIGHT DIVERTED DUE TO A FAULTING FMGC. FMGC FAILURE (SHOP FINDINGS NFF). REPLACED FMGC, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900175 20080129 00175 NM 2008 1 29 2008UALA00154 1 20080108 A 5210 BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L1 DOOR LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 809UA 825 DOOR 1 LEFT ACCUMULATOR BOTTLE PRESSURE LOW. SERVICED ACCUMULATOR TO FULL CHARGE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008012900199 20080129 00199 NM 2008 1 29 2008UALA00241 1 20080113 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 CEILING EMERGENCY LIGHT NEAR SEAT ROW 34HJK IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008012900204 20080129 00204 NM 2008 1 29 2008UALA00248 1 20080114 A 4930 4506353A600U FUEL CONTROL BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU APU LEAKING A UALA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 WP 29 924UA 26645 CREW REPORTED STRONG ODOR THRU OUT CABIN. ODOR DISSIPATED SOMEWHAT IN FLT BUT RETURNED UPON DESCENT AND LANDING. APU W AS NOT RUNNING AT TIME. FOUND APU INTERNALLY LEAKING FUEL FROM COMBUSTOR. REPLACED APU FCU. 2 L 7 2 4F 4 F RT A16WE E21EU 2008012900261 20080129 00261 NM 2008 1 29 2008UALA00262 1 20080114 A 3350 POWER SUPPLY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 768UA 26919 WHEN 6 CIRCUIT BREAKERS FOR EMERGENCY LIGHTS IN. ELECTRICAL ODOR C/B OUT NO ODOR. REPLACED EMERGENCY LIGHT POWER SUPPLY M33424 AND POWERED UP EMERGENCY LIGHTS. OPS TEST NOW OK, NO ODOR. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008012900269 20080129 00269 NM 2008 1 29 2008UALA00268 1 20080114 A 3350 362624 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 504UA 24625 RIGHT FWD OVERWING ESCAPE HATCH LIGHT IS INOPERATIVE. RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008012900270 20080129 00270 NM 2008 1 29 2008UALA00270 1 20080114 A 3350 1317 LAMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 667UA 29239 LEFT EXTERIOR EMERGENCY LIGHT BEHIND THE WING IS INOP. RELAMPED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900281 20080129 00281 NM 2008 1 29 2008UALA00282 1 20080115 A 5753 HINGE FITTING BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE T/E FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 667UA 29239 LT INBOARD FLAP CENTER HINGE FITTING CRACKED INBOARD SIDE. ACP EQ5256 TE FLAP FITTING INSPECTION. MANDATED BY AD 2003-1 3-01. REMOVED DAMAGED FLANGES. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR ANGLES. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900284 20080129 00284 2008 1 29 2008UALA00287 4 20080115 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L2 DOOR OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 399UA 24674 SLIDE AT DOOR 2L HAS MOVED. SECURED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008013000017 20080130 00017 NM 2008 1 30 F3LA200800021 1 20080107 A 5220 FE240004 CYLINDER DAMPER AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE EMERGENCY DOOR INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 924FR 233 2030 DURING C CHECK INSPECTION, THE R1 EMERGENCY DOOR DAMPENER CYLINDER FAILED ITS TEST DUE TO LOW PRESSURE. MAINTENANCE CHA RGED THE CYLINDER IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 52-10-00-614-001. UPON COMPLETION OF THE CHARGING, TH E CYLINDER PRESSURE WAS VERIFIED TO BE WITHIN ACCEPTABLE LIMITS. 2 L 7 2 4F 4 F RT A28NM 2008013000099 20080130 00099 SO 2008 1 30 SIMA200802115 1 20080108 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 614AE 20245 5000 145086 AIRCRAFT WAS REMOVED FROM SERVICE. DURING MBV INSPECTION THE BAGGAGE DOOR OPENING LOWER CENTER SILL WAS FOUND CORRODED. REMOVED AND REPLACE WITH NEW SILL PN 145-25480-603 IAW EMB 145 SRM 51-40-02 AND 51-20-03. AIRCRAFT RETURNED TO SERVIC E. 2 L 7 2 4T RT T00011AT 2008013000101 20080130 00101 NM 2008 1 30 F3LA200800036 1 20080123 A 3350 BR964424 LIGHT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE CABIN INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 947FR 435 2806 DURING RON MAINTENANCE, ROW 4, SEATS ABC AISLE MOUNTED EMERGENCY LIGHT FAILED ITS OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE ROW 4, SEATS ABC AISLE MOUNTED EMERGENCY LIGHT IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-19 PB 401. UPON COMPLETION OF THE INSTALLATION AND INSPECTION, THE LIGHT WAS TESTED AND FOUND TO BE ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008013000108 20080130 00108 NM 2008 1 30 F3LA200800034 1 20080106 A 5320 D53471124200 SHEAR PLATE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 924FR 5350 2030 DURING C CHECK INSPECTION, CORROSION WAS FOUND ON THE SHEAR PLATE ON THE RIGHT SIDE, OUTBOARD FLOOR SUPPORT BETWEEN FRAM ES 68 AND 70 AT STRINGER 23. MAINTENANCE REMOVED AND REPLACED THE SHEAR PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A3 19 SRM 51-42-11. FOLLOWING COMPLETION OF THE INSTALLATION, THE NEW SHEAR PLATE WAS INSPECTED AND FOUND TO BE ACCEPTABLE . 2 L 7 2 4F 4 F RT A28NM 2008013000114 20080130 00114 EU 2008 1 30 TRBA2008012 1 20080126 A 5410 S5411040400851 COWLING AEROSP ATR72 ATR72212A 8680902 EU LT NACELLE SEPARATED A TRBA E ENGINE SHUTDOWN D INFLIGHT SEPARATION TO TAKEOFF 1 SO 29 541AT 541 LOST LT ENGINE OUTBOARD COWLING ON TAKEOFF. ON APPROACH LT ENGINE GAVE FIRE WARNING. MADE PRECAUTIONARY ENGINE SHUT DO WN AND DISCHARGED FIRE BOTTLE. REMOVED AND REPLACED LT ENGINE HINGE COWLING AND UPPER BEAM IAW ATR JIC 54-00-00 AND 54- 12-61, FOR MORE INFO SEE NRWC NR 200402 AND 200554. REPLACED LEFT ENGINE FIRE EXTINGUISHER BOTTLE IAW JIC 26-21-71. AL SO REPLACED LT ENGINE FIRE BOTTLE AGENT NR 1 SQUIBB CARTRIDGE IAW JIC 26-21-72. OPT SATISFACTORY AT THIS TIME. 2 H 7 2 4T RT A53EU 2008013000115 20080130 00115 WP 2008 1 30 ARWA20080101 1 20080112 A 2780 ARH1664501 MECHANISM DOUG DC10 DC1030F 3023504 WP SLATS DAMAGED A ARWA O OTHER J WARNING INDICATION CR CRUISE 1 SO 19 450ML 47831 SLAT DISAGREE LIGHT ILLUMINATED WHEN SLATS SELECTED IN POST FLIGHT; INSPECTION FOUND LT INBOARD SLAT DEPLOYED. REMOVED AND REPLACED ASSEMBLY RUN NR 53A, NR 54A, NR 55A, AND NR 56A; NR 55C AND TWO (2) PULLEYS ASSEMBLY ON LT NR 7 AND NR 2 SL AT IN ACCORDANCE WITH M/M 27-80-00; REMOVED AND REPLACED INBOARD SLAT RETAINER MECHANISM IAW M/M 27-83-08. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F RT A22WE 2008013000129 20080130 00129 NM 2008 1 30 08FDEA00238 1 20080123 A 5311 BAC14902763 FRAME BOEING 727 727233 138408A NM BS 720D CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 LWR FWD CARGO PIT FRAME, UPPER FLANGE HAS SURFACE CORROSION, AFT SIDE OF STA 720D ABOVE STR 26L. FRAME DAMAGE FOUND TO B E OUT OF LIMITS, CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER. REMOVED AND REINSTALLED Z-ANGLE, BULKHEAD SUPPORT AND INTERCOSTAL TO GAIN ACCESS TO FRAME . IAW SRM 51-30-2, SRM 51-40-3, HEAT TREAT FOR REPAIR DONE ON 8130 TRACKING NR 2008-01-116. THIS IS CLASSIFIED MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2008013000173 20080130 00173 NM 2008 1 30 08FDEA00254 1 20080124 A 5347 ACA7399501 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 MAIN DECK STA 755, X = 48, SEAT TRACK FOUND CRACKED. CRACKED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008013100003 20080131 00003 EA 2008 1 31 COMA0870002 1 20080110 A 5210 601R318723 SEAL CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 656CA 10143 FLIGHT 5091 - AFTER TAKEOFF LOUD NOISE COMING FROM MAIN CABIN DOOR, PRESSURIZATION WOULD NOT WORK 43 PSI AND CABIN WAS C LIMBING. AIRCRAFT RETURNED TO CVG AND LANDED SAFELY. REMOVED AND REPLACED PAX DOOR SEAL. 2 L 7 2 4F RT A21EA 2008013100025 20080131 00025 EA 2008 1 31 MASA200800024 1 20080116 A 5240 DOOR CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR OUT OF ADJUST A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 501MJ 10047 ASH FLT 7197 IAD - SERVICE DOOR WILL NOT OPEN. MX ADJUSTED DOOR. 2 L 7 2 4F RT A21EA 2008013100026 20080131 00026 EA 2008 1 31 MASA200800014 1 20080105 A 5280 CC67010520965 FASTENER CNDAIR CL600 CL6002C10 1390015 EA LT MLG DOOR DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 503MJ 10058 DURING INSPECTION OF LT MLG DOOR PANEL FOUND LT PANEL DOOR AFT BRACKET FASTENER WORN/DAMAGED. REPLACED DOOR. 2 L 7 2 4F RT A21EA 2008013100027 20080131 00027 WP 2008 1 31 UPS08851453 1 20080102 A 5755 DOUBLER DOUG DC8 DC871F 302199D WP NR 3 SPOILER GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 NR 3 LT SPOILER BOARD REPAIR DOUBLER IS GOUGED INBD LWR EDGE. REMOVED AND REPLACED REPAIR DOUBLER ON NR 3 LT SPOILER BOARD IAW SRM 51-01-09A, AND SRM 57-07-01-0 FIG 005. 2 L 7 4 4F RT 4A25 2008013100042 20080131 00042 NM 2008 1 31 UPS08M51440 1 20080117 A 2710 ARH7057515 ACTUATOR DOUG MD11 MD11F 3023600 NM AILERON FAULTY A IPXA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 01 271UP 48572 INSPECTION TYPE:N/A ATB - ON DEPARTURE, LEVEL 2 AILERON DEFLECT DISAGREE. RAN CHECKLIST, LEVEL 2 ALERT RETURNED. T/S P ERFORMED AS PER FIM 27-10-00-1 & A/C DATA OBTAINED FROM AMC. FOUND LOB AILERON DEFLECTION ACTUATOR AT FAULT. SAME REPL ACED AS PER MM 27-16-00. ALL WITHIN LIMITS. 2 L 7 3 4F RT A22WE 2008013100043 20080131 00043 NM 2008 1 31 LYNX00005 1 20080109 A 5610 80260008 WINDSHIELD BOMBDR DHC8 DHC8402 1390042 NM COCKPIT CRACKED A 3LYA B EMER. DESCENT Z SIGNIFICANT FAILURE REPORT CR CRUISE 1 NM 21 502LX 277 4168 AT FL 250, THE FIRST OFFICERS WINDSHIELD OUTER PANE SHATTERED. CREW DECLARED AN EMERGENCY AND DIVERTED TO COS. MAINTEN ANCE WENT TO COS AND INSTALLED A NEW WINDSHIELD. 2 H 7 2 4T RT A13NM 2008013100046 20080131 00046 NM 2008 1 31 LYNX00006 1 20080114 A 3231 483023 SEQUENCE VALVE BOMBDR DHC8 DHC8402 1390042 NM NLG BYPASSING A 3LYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 21 503LX 259 4170 AFTER TAKEOFF FROM DEN, UPON LANDING GEAR RETRACTION, NOSE GEAR DOOR ANNUNCIATOR ILLUMINATED INDICATING THE NOSE GEAR DO ORS DID NOT CLOSE. CREW EXTENDED GEAR AND RETURNED TO DEN. MAINTENANCE REPLACED THE NOSE LANDING GEAR SOLENOID SEQUENC E VALVE P/N 48302-3, S/N FAH0428 WITH A NEW UNIT P/N 48302-5, S/N FAH0728. FUNCTIONAL CHECK OF GEAR CHECKS GOOD, PERFOR MED OPERATIONAL CHECK FLIGHT - CHECKS GOOD. DURING THE GROUND OPERATIONAL CHECK OF THE LANDING GEAR THE NOSE WHEEL STEE RING MOTOR CRACKED P/N RS1267-3, S/N 0261. NWS MOTOR WAS REPLACED. 2 H 7 2 4T RT A13NM 2008011100271 20080111 00271 SO 2008 1 11 CHQA200800002 1 20080102 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN SMOKE A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 575RP 145847 CAE312676 CVG TO IND, ON INITIAL CLIMB AT APPROXIMATELY 1500 FEET, THE CREW RECEIVED A "LAV SMOKE" EICAS MESSAGE. THE CREW RAN TH ROUGH THE APPROPRIATE QRH CHECK LISTS AND PREPARED TO RETURN TO FIELD. DURING THIS TIME THE FLIGHT ATTENDANT CALLED THE COCKPIT AND INFORMED THEM OF VISIBLE SMOKE IN THE CABIN. DURING APPROACH TO LAND, THE LAV SMOKE INDICATION DISAPPEARED AND THE SMOKE IN THE CABIN HAD CLEARED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, RAN BOTH ENGINES, AND COULD NOT DUPLICATE THE FAULT. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008011100276 20080111 00276 NM 2008 1 11 HALA0800006 1 20080102 A 2432 018550000 BATTERY BOEING 767 7673CB 1385187 NM DISCHARGED A HALA K NONE O OTHER CR CRUISE 1 WP 13 592HA 33468 ETOPS SIGNIFICANT SYSTEM, APU FAILED TO START. FAULT LT ILLUM AND EICAS MSG APU FAULT DISPLAYED TIME OAT -32 DEGREES FL 390 1S-3RD START ATTEMPTS UNSUCCESSFUL. ACCOMPLISHED FIM 49-11-00 FIG 103/106A, REPLACED APU BATTERY PER AMM 24-31-04 GRD OPS CHK OK. 2 L 7 2 4F RT A1NM 2008011400011 20080114 00011 2008 1 14 DXTA200802752 4 20080108 A 3417 ADC AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE NR 1 MALFUNCTIONED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 275QS 75 DURING TAKEOFF, TEN SECONDS AFTER FULL POWER WAS SET (AUTO SLATS) MESSAGE APPEARED. REPLACED ADC-850C AIR DATA COMPUTER NR 1 WITH AN OVERHAULED UNIT PER F2000 MM 34-103. COMPLETED LEAK CHECKS PER F2000 MM 34-100 & FAR 91.411 WITH NO LEAKS NOTED. OPS CHECKED GOOD PER F2000 MM 34-104. ASSISTED BY PRECISION STATIC TESTING CRS NO. QJAR856X REF. WO 4115. TRA NSPONDER INTEGRATION CHECK GOOD PER FAR 43 APP F PARA B 2 L 7 2 4F 4 F RT A50NM E44NE 2008011400060 20080114 00060 CE 2008 1 14 GLBA20061041 1 20080101 A 3350 1864 BULB BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA EMERGENCY LIGHTS BURNED OUT A GLBA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 210GL UE210 SMOKE/ODOR - PILOTS REPORTED THE GLARESHIELD INSTRUMENT EMERGENCY LIGHTS WERE SMOKING ON THE GROUND AFTER STARTING ENGIN ES. REMOVED EMERGENCY FUSE F127. MAINTENANCE REMOVED EMERGENCY FUSE F127 AND REMOVED AND REPLACED BULB IAW MM 33-10. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 3 T RT A24CE E4EA 2008011400072 20080114 00072 CE 2008 1 14 135762010708 1 20080102 A 3233 99101397 ACTUATOR CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO NLG FAILED E HYIA O OTHER J WARNING INDICATION CL CLIMB 1 EA 61 762EA 402C0061 NOSE GEAR DOWN AND LOCKED INDICATOR LIGHT WAS ILLUMINATED WITH GEAR UNSAFE AND HYDRAULIC PRESSURE LIGHTS OUT. PILOT PERF ORMED CHECK LIST, BLEW GEAR DOWN, AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED NOSE LANDING GEAR ACTUATOR AND REPLAC ED WITH SERVICE ABLE ACTUATOR, OPERATIONALLY CHECKED GOOD. 1 L 7 2 3O 3 O A7CE E8CE 2008020600136 20080206 00136 WP 2008 2 6 UPS08851493 1 20080110 A 5310 TORQUE BOX DOUG DC8 DC871F 302199D WP FS 1190 L33R GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 REPAIR DOUBLER IN C-PIT TORQUE BOX, STA 1190 L33R IS GOUGED. REMOVED, FABRICATED, AND INSTALLED REPA IR DOUBLER IN C-PIT TORQUE BOX STA 1190 L33R IAW SRM 51-01-20D, AND DWG 3753772. 2 L 7 4 4F RT 4A25 2008020600137 20080206 00137 WP 2008 2 6 UPS08851494 1 20080114 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FS 340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 CABIN, FLOOR PNL F27 HAS CORROSION BOTH SIDES AND POPPED RIVETS IN U CHANNEL. REMOVED TOP SKIN OF FL OOR PNL F27 IAW SRM 53-20-00 FIG 1F. FABRICATED AND INSTALLED REPAIR SKIN AND HAT CHANNELS ON FLOOR PANEL F27 IAW DWG 9 758942, AND SRM 51-3-2. 2 L 7 4 4F RT 4A25 2008020600151 20080206 00151 NM 2008 2 6 UPS08M51560 1 20080128 A 3350 BATTERY PACK DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 ON PDC, FOUND EMERGENCY LIGHTS FAILED TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. NO HELP DEFERRED PER ME L 33-50-4. PLACARD INSTALLED. AFTER BATTERY CHARGING COMPLETE, EMERGENCY LIGHTS OPERATIONAL CHECK GOOD PER AMM 33-50-0 0. 2 L 7 3 4F RT A22WE 2008020600152 20080206 00152 NM 2008 2 6 2008UALA00317 1 20080120 A 2780 SLAT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE WING MALFUNCTIONED A UALA O OTHER J W WARNING INDICATION INADEQUATE Q C NR NOT REPORTED 1 WP 29 669UA 30025 EICAS MSG L/E SLAT DISPLAYED WHEN FLAPS TO 30 DID NOT FULLY RETRACT AFTER LANDING. AFTER SEVERAL RESETS, SYMPTOMS REOCC URRED. EXTENSIVE DIAGNOSTIC SUGGESTED TARGET STABILITY PROBLEM. REPLACED NR 4 LE SLAT OUTBD UPPER TARGET, ROLLER AND BOLT. POST-REPAIR BITE TEST OF FLAPS & SLATS OK. AIRCRAFT RETURNED TO SERVICE. NO REPEAT OF ASSYM INDICATIONS. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020600156 20080206 00156 NM 2008 2 6 2008UALA00320 1 20080119 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 360 S14-15L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FUSELAGE FRAME SHEAR TIE CRACKED, BS 360 BETWEEN STR'S 14L-15L. MAJOR REPAIR: FABRICATED AND INSTALLED REPLACEMENT SHE AR TIE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600165 20080206 00165 NM 2008 2 6 UPS08451589 1 20080130 A 3010 69B400747 DUCT BOEING 747 747123F NIR NM ANTI ICE SYS DAMAGED A IPXA H DEACTIVATE SYST/CIRCUITS M J OVER TEMP WARNING INDICATION DE DESCENT 1 SO 01 677UP 20391 WITH WING ANTI-ICE ON, LOUD THUMP HEARD ON LEFT SIDE LEFT WING LE OVHT LIGHT ILLUMINATED. CLOSED LEFT ISOLATION VLV, SH UTOFF NR 1 AND NR 2 BLEED. WING OVHT LIGHT WENT OUT. FOUND MAIN PNEU SUPPLY DUCT WITH DAMAGED FLANGES AND CLAMPS, 2 EA LOWER SKIN PANELS HAVE EXTENSIVE HEAT DAMAGE. COMPLIED W/INTERIM REPAIR PER EO B747-5720-28529A. PERM REPAIR DUE BY 5 /17/08. LT WING L/E PNEUM DUCT REMOVED FROM STA 170-630 & 170-365. INSTALLED PNEU DUCT PER 36-11-00. LEAKS CHECKS GOOD. 2 L 7 4 4F RT A20WE 2008020600167 20080206 00167 NM 2008 2 6 UPS08451597 1 20080201 A 5210 DOOR BOEING 747 747212B 1384886 NM L1 OUT OF RIG A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 L1 ENTRY DOOR OUT OF RIG. FOUND LOWER HINGE BOLTS LOOSE, REPLACED BOLTS. GROUND OPS CHECKS GOOD PER MM 52-11-02. OK FOR SERVICE. 2 L 7 4 4F RT A20WE 2008020600168 20080206 00168 NM 2008 2 6 UPS08651477 1 20080119 A 5730 PANEL BOEING 767 76734AF 1385212 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 313UP 27764 LT WING LOWER T/E PANEL CRACKED AND WIGGLE PLATE BROKEN. REPLACED LT LWR WING PANEL 561 GB PER SRM 51-40-00, SEE LP 858 182/1. INSTALLED NEW WIGGLE PLATE IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008020600169 20080206 00169 NM 2008 2 6 2008UALA00329 1 20080120 A 5320 DOUBLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 LEFT FUSELAGE REPAIR DOUBLER HAS DENT BETWEEN FRAMES 600 AND 620LT, AND STRINGERS 17L AND 16L. ACCOMPLISHED MAJOR REPAI R. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600174 20080206 00174 WP 2008 2 6 UPS08851504 1 20080105 A 5347 3657502U509 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 1ST OFFICERS AFT OUTBD SEAT TRACK LOCK PIN HOLES ARE ELONGATED. REMOVED AND REPLACED 1ST OFFICERS AF T OUTBD SEAT TRACK IAW EO DC8- 5340-1815-B. 2 L 7 4 4F RT 4A25 2008013100056 20080131 00056 SO 2008 1 31 C2XA08IA026 1 20080117 A 3397 W741803120 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15985 145248 IAH - DURING MAINTENANCE INSPECTION THE LAST THREE AISLE PATH LIGHTING STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED A BROKEN WIRE AT SP9221, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WA S APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008013100058 20080131 00058 EU 2008 1 31 YENA2008005 1 20080113 A 2752 C1558161 ACTUATOR EMB ERJ190 ERJ190100IGW 3260408 EU T/E FLAP FAILED A YENA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 EA 15 197JB 5142 19000020 FLT 903, JFK-ORD, FLAP FAIL EICAS WHEN SELECTING FLAPS 1. RETURNED TO MCO, REMOVED AND REPLACED RIGHT OUTBOARD FLAP NR 4 ACTUATOR ASSY IAW AMM 27-51-01. OPS CHECK OK IAW AMM 27-51-01. 2 L 7 2 4F RT A57NM 2008013100062 20080131 00062 2008 1 31 ASAA0852487 4 20080117 A 2310 HF COMM BOEING 737 737890 1384527 NM COCKPIT MALFUNCTIONED A ASAA K NONE O OTHER NR NOT REPORTED 1 NM 02 587AS 35684 ACARS "NO COMM" WHEN HF NR 2 SELECTED TO DATA. ATTEMPTED SEVERAL TIMES AT ONE HOUR INTERVALS TO RE-ESTABLISH COMM. HF VOICE WORKED NORMAL. NR 1 HF DATA WORKED NORMAL. UNABLE TO VERIFY DISCREPANCY. ACFT ACARS USES HF DATA WHEN OUT OF VH F DATA RANGE. REPLACED NR 2 TRANSCEIVER PRECAUTIONARY. 2 L 7 2 4F RT A16WE 2008013100065 20080131 00065 NM 2008 1 31 ASAA0852486 1 20080117 A 4920 GTCP1319B APU BOEING 737 737890 1384527 NM APU BAY SHUTDOWN A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 579AS 35187 APU QUIT WHILE BEING DE ICED. SUSPECT GLYCOL INJESTION. RESTARTED AFTER APPROXIMATELY 5 MINUTES. RAN BOTH PACS CYCLED BETWEEN HOT AND COLD VERIFIED NO ODORS EXIST IN CABIN AND FLIGHT DECK. COMPLETED FIM 49 55 TASK 802. FOUND NO GLYCOL IN APU DUCTS, NO ODOR NOTICED. 2 L 7 2 4F RT A16WE 2008013100078 20080131 00078 SO 2008 1 31 RAIA00801024 1 20080120 A 3222 STRUT EMB 145 EMB145 3260210 SO NLG LOW A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 806HK 145112 FLT 3564 - STL - LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS. MAINTENANCE SERVICED THE NOSE LANDING GEAR STRUT AN D PERFORMED SEVERAL GEAR EXTENSIONS AND RETRACTIONS WITH NO DEFECTS NOTED. 2 L 7 2 4F RT T00011AT 2008013100080 20080131 00080 NM 2008 1 31 SWAA080418 1 20080123 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008013100085 20080131 00085 NM 2008 1 31 SWAA080419 1 20080123 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504D, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008013100086 20080131 00086 NM 2008 1 31 SWAA080420 1 20080123 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008013100087 20080131 00087 NM 2008 1 31 SWAA080421 1 20080123 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 402WN 29814 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008013100088 20080131 00088 NM 2008 1 31 SWAA080422 1 20080122 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 410WN 27897 EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008013100093 20080131 00093 NM 2008 1 31 SWAA080427 1 20080123 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008013100097 20080131 00097 NM 2008 1 31 SWAA080429 1 20080123 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 18L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008013100100 20080131 00100 NM 2008 1 31 SWAA080430 1 20080123 A 3350 OL301BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 719SW 27853 DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 23 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008013100108 20080131 00108 NM 2008 1 31 SWAA080439 1 20080124 A 5753 6573731 WEDGE BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED HC2 CHECK, FOUND LT WING INBOARD MID FLAP T/E WEDGE DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2008013100111 20080131 00111 NM 2008 1 31 SWAA080445 1 20080124 A 5313 6551698 STRINGER SPLICE BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 9R. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2008012900288 20080129 00288 NM 2008 1 29 2008UALA00292 1 20080115 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 666UA 29238 EEL LIGHTS INOP AT SEATS 30HJ & 39HJ. REPLACED EEL STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008012900289 20080129 00289 NM 2008 1 29 2008UALA00293 1 20080115 A 3350 1317 LAMP BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 666UA 29238 SEAT 3AB EEL LIGHT INOPERATIVE. RELAMPED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008013000004 20080130 00004 NM 2008 1 30 HALA0800024 1 20080116 A 3350 FUSE BOEING 767 76733A 1385209 NM BATTERY PACK FAILED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 593HA 33424 EXTERIOR EMERGENCY LIGHT AT STATION 1230 RT SIDE IS INOP. REPLACED FUSE IN BATTERY PACK. RELAMPED LIGHT. CHECKS OK. 2 L 7 2 4F RT A1NM 2008013000038 20080130 00038 NE 2008 1 30 SIMA200802105 2 20080119 A 7230 BLADES CNDAIR CL600 CL6002C10 1390015 EA GE CF700 CF700* 30010 NE NR 1 ENGINE DAMAGED A SIMA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 21 511AE 10107 ON FLIGHT 3714, CREW REPORTED IN CRUISE FLT ENGINE 1 N1 VIB IND STARTED TO CLIMB AND THEN WENT INTO AMBER AT 1.9 CREW RE DUCED POWER AND AT FIRST VIB IND WENT DOWN. IT THEN STARTED TO CLIMB AGAIN AND COULD BE FELT IN MAIN CABIN. CREW THEN DECLARED AN EMERGENCY AND LANDED IN XNA FOR MTX. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FAN BLADE SET IAW AMM 72-21-02. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E7EA 2008013000039 20080130 00039 EU 2008 1 30 MALA080011 1 20080108 A 5320 WEB SAAB SF340 340B 7860101 EU BS 294 CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 OB AFT CORNER OF AFT GALLEY FLOOR WEB IS CHAFED FROM AIRSTAIRS AT STA 294. REPAIRED IAW MAL EO NR S53362. 2 L 7 2 4T RT A52EU 2008013000069 20080130 00069 EU 2008 1 30 F3LA200800031 1 20080123 A 2130 101809 PRESSURE SWITCH AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE CABIN PRESSURE INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 804FR 5495 2051 DURING C CHECK AND FUNCTIONAL TEST, THE ALTITUDE PRESSURE SWITCH FAILED ITS FUNCTIONAL TEST. MAINTENANCE REMOVED AND RE PLACED THE ALTITUDE PRESSURE SWITCH IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 35-23-15 PB 401. FOLLOWING ITS INSTALLAT ION AND INSPECTION, IT OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F 4 F RT 2008013000070 20080130 00070 NM 2008 1 30 08FDEA00240 1 20080123 A 5730 6521657155 BRACKET BOEING 727 727233 138408A NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 RT WING O/B MOST UPPER TRAILING EDGE PANEL I/B SIDE SPOILER SEAL BRACKET CRACKED AT AFT EDGE AND AT SPOILER DOWN STOP PA D CUTOUT. REMOVED CRACKED BRACKET AND FABRICATED NEW SEAL DEPRESSOR BRACKET REF BOEING DRAWING 65-21657/ITEM NR 155 AND INSTALLED ON PANEL REF SRM 51-30-2 PG 4. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008013000105 20080130 00105 EU 2008 1 30 MALA080013 1 20080117 A 2613 DETECTOR SAAB SF340 340B 7860101 EU LT TAILPIPE MALFUNCTIONED A MALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 452XJ 340B452 LT TAILPIPE HOT LIGHT ILLUMINATED DURING TAXI. RETURNED TO GATE. CLEANED AND RESEALED LT TAILPIPE HOT DETECTORS IAW JC 2610-302. OPS CKS GOOD. OK FOR SERVICE. 2 L 7 2 4T RT A52EU 2008013000109 20080130 00109 EU 2008 1 30 TRBA2008008 1 20080121 A 3397 204 WIRE AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHTS OPEN A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 529AM 529 GALLEY FLOOR EMERGENCY LIGHTS ARE INOPERATIVE. REPAIRED OPEN WIRE AT EMERGENCY LIGHT STRIP 163WL AS PER STANDARD PRACTI CES JIC NR 20-00-00. PERFORMED OPERATIONAL CHECK IAW JIC NR 35-50-00. 2 H 7 2 4T RT A53EU 2008013000110 20080130 00110 EU 2008 1 30 CPCP20080003 1 20080107 A 5311 FRAME AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 369AT 369 FRAME 39 BETWEEN STRINGER 21L-21R CORRODED. FRAME 39, BETWEEN STRINGER 21L-21R REPAIRED IAW SRM 53-61-40 FIG 415. 2 H 7 2 4T RT A53EU 2008013000134 20080130 00134 SO 2008 1 30 SWIA200819075 1 20080121 A 5610 WINDOW EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 FLT 5510 - COCKPIT LEFT SIDE WINDOW IS CRACKED. REPLACED SIDE WINDOW IAW MM 56-11-01. 2 L 7 2 4T RT A31SO 2008013000136 20080130 00136 EA 2008 1 30 SWIA200819077 1 20080119 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 932SW 7714 FLT 6509 - SMOKE TOILET CAUTION MESSAGE ILLUMINATED AFTER TAKEOFF. REPLACED LAV SMOKE DETECTOR ASSEMBLY IAW CRJ 200 AMM 26-16-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008013000149 20080130 00149 NM 2008 1 30 DLM88080077 1 20080116 A 5347 SEAT TRACK DOUG MD88 MD88 3023688 NM BS 896 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 706102 GENERAL SURFACE CORROSION ON RT SEAT TRACK X=54 AT STA 896. REPAIRED IAW SRM 53-05D FIG 4A. 2 L 7 2 4F RT A6WE 2008013000169 20080130 00169 EU 2008 1 30 08FDEA00268 1 20080122 A 5310 CROSSBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 AFT CARGO COMPARTMENT, CROSSBEAM OF FR 61 WITH CORROSION AT Y 1004. CROSSBEAM REWORKED IAW EA 6-5310-115317. 2 L 7 2 4F RT A35EU 2008013000185 20080130 00185 WP 2008 1 30 08FDEA00260 1 20080124 A 5754 SKIN DOUG DOUG DC10 DC1030 3023501 WP NR 5 SLAT DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 RT WING, NR 5 L/E SLAT HAS DENTS 5EA ON L/E SKIN. CUT OUT DAMAGED AREA, FABERICATED DOUBLERS, SPLICE PLATE, BAFFLES, SE AL, FILLER AND INSTALLED REPAIR IAW SRM 57-10-00 FIG.II, VOL I, SRM51-21-01 VOL II AND SRM 51-35-02 VOL II. 2 L 7 3 4F A22WE 2008013100023 20080131 00023 EA 2008 1 31 MASA200800025 1 20080116 A 2560 NAS322C110516 CABLE ASSY CNDAIR CL600 CL6002C10 1390015 EA EXTINGUISHER MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 516LR 10258 ASH FLT 7281 IAD. FWD F/A FIRE EXTINGUISHER MISSING BREAK AWAY CABLE. MX INSTALLED BREAK AWAY CABLE. 2 L 7 2 4F RT A21EA 2008013100054 20080131 00054 SO 2008 1 31 C2XA08IA027 1 20080117 A 3350 7287580509 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15985 145248 IAH - DURING MAINTENANCE INSPECTION THE LAST THREE AISLE PATH LIGHTING STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NUMBER SIX AISLE PATH LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DE FECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008013100110 20080131 00110 NM 2008 1 31 SWAA080446 1 20080124 A 5754 65C26602 SLAT BOEING 737 7373TO 138447G NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD T/E EDGE. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008013100119 20080131 00119 SO 2008 1 31 RAIA00801025 1 20080121 A 5210 CABLE EMB 145 EMB145 3260210 SO PAX DOOR OUT OF ADJUST A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 802HK 145066 PRE FLT 3530 - EWR - PASSENGER DOOR WOULD NOT OPEN FROM THE INSIDE OF PLANE. MAINTENANCE LUBED AND ADJUSTED THE PASSENG ER DOOR CABLES. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2008013100141 20080131 00141 NM 2008 1 31 SWAA080472 1 20080127 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008013100142 20080131 00142 NM 2008 1 31 SWAA080473 1 20080127 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008013100153 20080131 00153 NM 2008 1 31 SWAA080455 1 20080127 A 2560 P4010021 BATTERY BOEING 737 7375H4 138449D NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008013100173 20080131 00173 NM 2008 1 31 SWAA080461 1 20080127 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 443, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008013100174 20080131 00174 NM 2008 1 31 SWAA080462 1 20080125 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008013100181 20080131 00181 NM 2008 1 31 SWAA080463 1 20080127 A 5311 65C22909 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008013100185 20080131 00185 NE 2008 1 31 SWAA080469 2 20080125 A 7314 8283005 PUMP BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE NR 1 ENGINE FAILED A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 29 782SA 29808 NR 1 ENGINE FAILED DURING TAXI. REMOVED AND REPLACED FUEL PUMP AND HMU PER MM. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008013100196 20080131 00196 NM 2008 1 31 SWAA080485 1 20080128 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008013100204 20080131 00204 NM 2008 1 31 SWAA080499 1 20080128 A 5315 6545834 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 11 TO RBL 14. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2008013100207 20080131 00207 NM 2008 1 31 SWAA080503 1 20080128 A 5330 6573745 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST CUTOUT BS 379, BL 0. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008013100208 20080131 00208 NM 2008 1 31 SWAA080487 1 20080128 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 443, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008020600176 20080206 00176 WP 2008 2 6 UPS08851506 1 20080105 A 5347 36575024U507 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 CAPT, AFT OUTBD SEAT TRACK LOCK PIN HOLES ARE ELONGATED. REMOVED AND REPLACED CAPT, AFT OUTBD SEAT T RACK IAW EO DC8-5340- 18315-B. 2 L 7 4 4F RT 4A25 2008020600183 20080206 00183 NM 2008 2 6 2008UALA00338 1 20080118 A 3320 BALLAST BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN LIGHTS OVERHEATED A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 666UA 29238 SUSPECT BALLAST OVERHEATING IN MID GALLEY. TURNED OFF LIGHTS, STRONG ACRID ODOR PRESENT. REMOVED MID GALLEY CEILING PA NEL AND NOTICED ODOR WAS EMANATING FROM SPEAKER DRIVE MODULE. REMOVED CONNECTOR AND ODOR DISSIPATED. REPLACED SPEAKER DR IVE MODULE. NO FURTHER REPORT OF ACRID ODOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020600188 20080206 00188 NM 2008 2 6 2008UALA00342 1 20080120 A 5210 RESERVOIR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE L2 DOOR ASSIST MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 786UA 26938 SLIDE GAUGE AT DOOR 2L ONE IS HIGH AND ONE IS LOW. REPLACED DOOR 2L EMERGENCY POWER ASSIST RESERVIOR PER MM. DOOR SLI DE PRESSURE SHOWS WITHIN ACCEPTABLE LIMITS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008020600196 20080206 00196 SO 2008 2 6 C2XA08TY016 1 20080122 A 2810 14563740405 BRACKET EMB 145 EMB145XR 3260214 SO FUEL TANK CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14117 145674 TYS - DURING THE CURRENT 3C INSPECTION THE VENTRAL TANK BRACKET SHOWS SIGNS OF CORROSION. MAINTENANCE REMOVED AND REPAI RED THE CORRODED AREA, PRIMED AND PAINTED IAW EC2810-01032. LEAK CHECKS WERE GOOD. A/C WILL BE RETURNED TO SERVICE AT THE END OF THE 3C CHECK. 2 L 7 2 4F RT 2008020600206 20080206 00206 2008 2 6 ASAA0852490 4 20080117 A 2310 8220990004 TRANSCEIVER BOEING 737 737890 1384527 NM HF COMM MALFUNCTIONED A ASAA K NONE O OTHER CR CRUISE 1 NM 02 587AS 35684 HR TRANSCEIVER MALFUNCTIONED CAUSING ACARS "NO COMM" ANNUNCIATION. REPLACED TRANSCEIVER. OP CHECKED OK. 2 L 7 2 4F RT A16WE 2008020600207 20080206 00207 NM 2008 2 6 UPS08M51551 1 20080119 A 2897 CONNECTOR DOUG MD11 MD11F 3023600 NM FUEL PUMP BURNED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 AFTER REFUELING MESSAGE "AUX LWR L PUMP OFF" APPEARED. DEFERRED AUX LWR L PUMP IAW MEL 28-22-6-1-1 M367263. DMP 28-22- 6-1 ACCOMPLISHED. REMOVED AUX LWR L PUMP. FOUND BURNT CONNECTOR IN HOUSING AND ON PUMP. REMOVED OLD HARNESS AND INSTA LLED NEW HARNESS THRU CONDUIT REF MM 20-22-10-8. COMPLETED HARNESS INSTALLATION IAW MM 28-22-10 AND INSTALLED NEW PUMP IAW 28-22-01. 2 L 7 3 4F RT A22WE 2008020600222 20080206 00222 EA 2008 2 6 MASA200800065 1 20080124 A 2720 274001 PCU CNDAIR CL600 CL6002B19 1900309 EA RUDDER MALFUNCTIONED A MASA O OTHER F FLT CONT AFFECTED LD LANDING 1 SW 07 17358 7358 ASH FLT 9700 PHX-PHX - RT RUDDER INPUT UNCOMMANDED ON LANDING WITH THE AUTO PILOT OFF. REMOVED AND REPLACED PCU RUDDER. 2 L 7 2 4F RT A21EA 2008020600224 20080206 00224 NM 2008 2 6 UPS08551579 1 20080129 A 2611 2156606A SMOKE DETECTOR BOEING 757 75724APF 1384969 NM COCKPIT INTERMITTENT A IPXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 464UP 28268 ATB DUE TO CAPT AND F/O ADI SCREENS BLANKING THEN LOSING COLOR. GOT A FLT DK EQUIP SMOKE AND RECIRC FAN EICAS MSG. THE N RECEIVED A EQUIP OVHT EICAS MSG. SELECTING "ALTN" ON THE EQUIP COOLING SWITCH RESTORED SCREENS T NORMAL. REF L/P 92 7415 NR 1 REPEAT ITEM. CONFIRMED FAULT TO BE NR 2 FLT DECK SMOKE DETECTOR AND REPLACED SAME PER 21-58-19-2. 2 L 7 2 4F RT A2NM 2008020600227 20080206 00227 EA 2008 2 6 MASA200800095 1 20080131 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 917FJ 15017 ASH FLT 2609 EWR-CLT - AFT CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 2008020600237 20080206 00237 2008 2 6 NOCA008 4 20080119 A 2230 948E310G2 AUTOTHROTTLE SYS BOEING 767 76736N 1385152 NM COCKPIT MALFUNCTIONED A NOCA O OTHER O OTHER CL CLIMB 1 EA 15 768NA 29898 AUTOTHROTTLE DISCONNECTED ON LANDING. ACCOMPLISHED MCDP TEST 02 & 10 PER FIM TASK 22-00-02 FIG 104 & FOUND TMC AT FAULT . ACCOMPLISHED BY AA E58D-3 9326553. REMOVED AND REPLACED TMC PER MM 22-31-01, OPS CHECK OK. NO FAULTS NOTED. 2 L 7 2 4F RT A1NM 2008020600238 20080206 00238 NM 2008 2 6 USAA920080200 1 20080111 A 5340 693535214 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED STRINGER TIE CLIP, BS 727E, S4R. REPLACED STRINGER TIE CLIP, BS 727E, S4R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020100174 20080201 00174 NM 2008 2 1 QXEA200800045 1 20080127 A 5230 HANDLE BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR UNSECURE A QXEA K NONE J WARNING INDICATION CR CRUISE 1 NM 09 431QX 4164 PDX - FLIGHT NR 2250 - DURING CRUISE A MASTER WARNING LIGHT ILLUMINATED INDICATING THE FORWARD BAGGAGE DOOR UNSAFE. CHE CK LIST RUN AND PRESSURIZATION WAS NORMAL. DIVERTED TO PDX FOR WORK. MAINTENANCE (INITIAL INSPECTION OF DOOR FOUND HAN DLE IMPROPERLY STOWED) INSPECTED THE DOOR LINKAGE NO DEFECTS WERE NOTED. CLEANED AND LUBRICATED THE DOOR HANDLE SHAFT. OPS CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE, NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008020100187 20080201 00187 EU 2008 2 1 08FDEA00319 1 20080129 A 5720 A57110531207 FITTING AIRBUS 300 A300B4605R 3930308 EU CENTER WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CENTER WING-TOOL MARK AND DAMAGED FASTENERS AT C 47 RT AFT FACE AT P26 REPAIR PERFORMED BY REWORK OF TOOL MARKS, HFEC IN SPECTION FOR CRACK FREE AND REMOVAL OF AFFECTED FASTENERS WITH HL112VF8 IAW, RAS 057234/008/2007 ISS A , APPROVED BY EA 6-5710-114864. 2 L 7 2 4F RT A35EU 2008020400027 20080204 00027 WP 2008 2 4 AALA200800043 1 20080108 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7526A 49918 LGA - EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS CABIN INOPERATIVE. SECURED BATTERIES FOR EMERGENCY LIGHTS AT OVERHEAD FI RST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020400028 20080204 00028 NM 2008 2 4 AALA200800030 1 20080105 A 2130 SHUTOFF VALVE BOEING 757 757223 1384957 NM CABIN PRESSURE INOPERATIVE A AALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 654A 24612 AUA INFLIGHT T1036/05JAN - LOST CABIN PRESSURE AND LIGHT SMOKE IN CABIN. OXYGEN MASKS WERE DEPLOYED. RETURNED TO AUA A ND LANDED WITHOUT INCIDENT. SMOKE IN CABIN CLEARED PRIOR TO LANDING. REPLACED RIGHT ENGINE PRESSURE REGULATING SHUT OF F VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020400030 20080204 00030 NM 2008 2 4 AALA200800021 1 20080103 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 669AA 25334 MIA - EMERGENCY LIGHT AT LEFT FORWARD DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT FORWARD DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020400032 20080204 00032 NM 2008 2 4 AALA200700024 1 20080104 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 386AA 27060 JFK - EMERGENCY LIGHT AT OVERHEAD AFT GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD AFT GALLEY. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008020400038 20080204 00038 NM 2008 2 4 AALA200800041 1 20080107 A 2910 MODULE BOEING 737 737823 13844BZ NM LT ENG HYD SYS DIRTY A AALA O OTHER N FALSE WARNING DE DESCENT 1 SW 21 952AA 30088 DEW IN-FLIGHT T1105/07JAN - LEFT ENGINE HYDRAULIC INDICATION FLICKERING FOLLOWED BY RIGHT ENGINE HYDRAULIC INDICATION FL ICKERING. LANDED DEW WITHOUT INCIDENT. FOUND RESERVOIR MODULE AND FILTER DIRTY. REPLACED RIGHT RESERVOIR PRESSURE MOD ULE AND FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008020400085 20080204 00085 WP 2008 2 4 AALA200800065 1 20080114 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 467AA 49597 LGA - EMERGENCY LIGHT AT OVERWING EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERWING EXIT SIG N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020400100 20080204 00100 WP 2008 2 4 AALA200800051 1 20080111 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7509 49803 LGA - EMERGENCY LIGHTS AT SEAT ROWS 28 TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROW S 28 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300004 20080303 00004 NM 2008 3 3 08FDEA00528 1 20080220 A 5753 ARC24441 SKIN DOUG MD11 MD11 3023602 NM TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 LEFT WING - INBOARD FLAP LOWER SURFACE FOUND SEVERAL DENTS AT XIFH 244. DENT AREA FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I AND REPAIR CARRIED OUT AT LEFT HAND WING INBOARD FLAP LOWER SURFACE AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008020400167 20080204 00167 EU 2008 2 4 TRAX200800108 1 20080110 A 5320 ANGLE AEROSP ATR72 ATR72 EU WHEEL WELL CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 FWD WHEEL WELL, ANGLE CRACKED AT FR 7 STR LEFT 20. 2 H 7 2 4T RT 2008020400180 20080204 00180 EA 2008 2 4 TRAX200800119 1 20080120 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 978EV 7723 FLAP FAIL AT ZERO ON APPROACH. THE TOWER INITIATED FIRE & RESCUE AS A PRECAUTION. 2 L 7 2 4F RT A21EA 2008020600025 20080206 00025 NM 2008 2 6 USAA920080207 1 20080112 A 5320 6545834107 STRAP BOEING 737 7373Y0 1384671 NM BS 312-328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED L1 DOOR CUTOUT LOWER SILL WEB STRAP, BS 312 - BS 328, LBL 45.6, WL 208. REPLA CED L1 DOOR CUTOUT LOWER SILL WEB STRAP, BS 312 - BS 328, LBL 45.6, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600035 20080206 00035 EU 2008 2 6 USAA920080193 1 20080120 A 3232 2271500002 ACTUATOR AIRBUS 320 A320231 3930325 EU MLG DOOR DEFECTIVE A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 632AW 32495 81 FLT 80 - LAS-MSP - LANDING GEAR DOORS - AFTER TAKEOFF, ECAM CAUTION LANDING GEAR DOORS DID NOT CLOSE. PERFORMED ECAM AC TIONS. AFTER THIRD ATTEMPT THE MESSAGE EVENTUALLY CLEARED. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOOR ACTUATOR CYLINDER PER AIRBUS MAINTENANCE MANUAL 32-31-16. LEAK CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008020600070 20080206 00070 WP 2008 2 6 ABXA080027 1 20080122 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP EMERGENCY LIGHTS DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 974AX 47623 EMERGENCY EVAC LIGHTS WOULD NOT ILLUMINATE WITH SWITCH ON. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 3 3-53-00-8. 2 L 7 2 4F A6WE 2008020600079 20080206 00079 SO 2008 2 6 C2XA08ON069 1 20080119 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 22909 1450459 FLT MX - ONT - WHILE PERFORMING 2A CHECK INTERVAL INSPECTION MX FOUND CEILING PANEL EMERGENCY EXIT SIGN BETWEEN SEAT 1A AND GALLEY DOES NOT ILLUMINATE. MX FOUND CONNECTOR TO BE LOOSE AND RECONNECTED AND OPERATIONALLY CHECK SATISFACTORY. A IRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008020600083 20080206 00083 SO 2008 2 6 C2XA08ON079 1 20080130 A 2120 2305591728 CLAMP EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL CUSTOMER AIR MISSING A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 12172 9636 9636 14500864 CAE312595 FLT 7765 - LAX TO LAX - DURING CLIMB FLIGHT CREW REPORTED E1 HIGH ITT. AIRCRAFT RETURNED TO BLOCK WITH NO INCIDENT. MX PERSONNEL FOUND COSTOMER SERVICE DISCHARGE TUBE CLAMP MISSING CAUSING GASKET ALSO MISSING. MX INSTALLED A NEW CLAMP AN D GASKET OPERATIONALLY CHECKED HIGH POWER RUNS SATISFACTORY. AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2008020600090 20080206 00090 NM 2008 2 6 2008UALA00043 1 20080103 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OBSTRUCTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 567UA 26673 FOUND STATIC LINE OUT OF POCKET INTERFERING WITH GIRT BAR AND DOOR SEAL. FLT ATT STUFFED PAPER TOWELS UNDER SLIDE COVER AND JAMMED SLIDE BUSTLE LOOSE. AFTER REMOVAL OF COVER FOUND DOOR WOULD NOT ARM. FOUND STATIC LINE OUT OF POCKET INTER FERING WITH GIRT BAR AND DOOR SEAL. STOWED STATIC LINE. CLEANED SEAL AND DOOR SILL AREA. PRESSURIZED AIRCRAFT, NO LEA KS FOUND. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600102 20080206 00102 EA 2008 2 6 TRAX200800128 1 20080122 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 EMERGENCY LIGHT FLOOR STRIP NEAR ROW 5 ON RIGHT SIDE DETACHED. 2 L 7 2 4F RT A21EA 2008013100210 20080131 00210 NM 2008 1 31 SWAA080491 1 20080128 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008013100211 20080131 00211 NM 2008 1 31 SWAA080490 1 20080128 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 840, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008013100219 20080131 00219 NM 2008 1 31 SWAA080496 1 20080128 A 3211 115A5211 FITTING BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 708SW 27842 DURING SCHEDULED MV2 CHECK, FOUND LEFT MLG TRUNNION FITTING LUGS CORRODED. REMOVED AND REPLACED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008013100220 20080131 00220 NM 2008 1 31 SWAA080497 1 20080128 A 3211 115A5211 FITTING BOEING 737 7377H4 1384404 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 708SW 27842 DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUGS CORRODED. REMOVED AND REPLACED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008013100228 20080131 00228 EA 2008 1 31 TRAX200800092 1 20080105 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 904EV 7628 FS 349 FRAME IS CORRODED AT BL 0.0. 2 L 7 2 4F RT A21EA 2008013100231 20080131 00231 EA 2008 1 31 TRAX200800095 1 20080115 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 843AS 7310 RIGHT FS 640 BONDED SKIN DOUBLER CRACKED. REPAIRED RT 640.00 BONDED SKIN DOUBLER IAW REO 601R-53-61-506. 2 L 7 2 4F RT A21EA 2008013100243 20080131 00243 NM 2008 1 31 KCSA081028 1 20080119 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FUSELAGE SKIN IS CORRODED IN TWO AREAS AT STA 1244 BETWEEN STR 2R & 1L. 2 L 7 4 4F RT A20WE 2008013100245 20080131 00245 NM 2008 1 31 KCSA081029 1 20080120 A 5414 SKIN BOEING 747 747259B 1384804 NM NR 3 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 NR 3 PYLON I/B SKIN HAS A CRACK AT AFT UPPER CORNER OF ACCESS PANEL OPENING AT NAC STA 208. 2 L 7 4 4F RT A20WE 2008013100249 20080131 00249 NM 2008 1 31 KCSA081031 1 20080120 A 5414 SKIN BOEING 747 747236B 1384804 NM NR 4 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 NR 4 PYLON I/B SKIN CRACKED AT UPPER AFT CORNER OF THE FWD LOWER ACCESS PANEL OPENING AT NAC STA 208. 2 L 7 4 4F RT A20WE 2008013100253 20080131 00253 WP 2008 1 31 UPS08851462 1 20080113 A 5313 37592581 LONGERON SPLICE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 C PIT STA 1260, LONG 35L SPLICE FITTING CRACKED. REPLACED CRACKED SPLICE FITTING AT STA 1260 AND LON G 35L PER SRM 51-01 20D AND SRM 51-03-00. 2 L 7 4 4F RT 4A25 2008013100257 20080131 00257 EA 2008 1 31 VNAA0801003 1 20080113 A 7830 LOCK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE THRUST REVERSER DIRTY A VNAA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 05 244PS 7912 CREW REPORTED A LEFT HAND THRUST REVERSER UNLOCKED CAS MESSAGE AFTER TAKEOFF. CREW FOLLOWED THE QRH AND RETURNED TO CAK WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CLEANED THE FLEX SHAFT LOCK UNIT. MAINTENANCE OPS CHECKED THE LEFT HAND T HRUST REVERSER IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008013000055 20080130 00055 NM 2008 1 30 C1HA200878001 1 20080121 A 2131 SWITCH BOEING 727 727225 1384077 NM A/C PACK MALFUNCTIONED A C1HA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 678MG 22555 AIRCRAFT (AT FL 290) CABIN ALT STARTED TO CLIMB. DESCENDED TO F200, THEN FL 160 DOWN TO 10,000 DIVERTED TO OKC. REMOVE D AND REPLACED RT PACK VALVE REF MM 21-55-71, NO HELP. PROBLEM VERIFIED RT PACK SWITCH. REMOVED AND REPLACED RT PACK S WITCH. OPERATIONAL CHECK REF MM 21-55-00 OK. PERFORMED PRESS CHECK REF MM 05-51-101. SYSTEM TESTS GOOD. 2 L 7 3 4F A3WE 2008013000061 20080130 00061 SO 2008 1 30 FDKA200801036 1 20080122 A 5320 14526436401 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 834MJ 145340 THE FLOOR SUPPORT AT Y-479 AND THE RT SILL IS CORRODED OUT OF LIMITS. THE DAMAGED SUPPORT HAS BEEN REMOVED AND REPLACED . 2 L 7 2 4T RT T00011AT 2008013000073 20080130 00073 GL 2008 1 30 SIMA200802303 2 20080121 A 7320 23083670 FADEC EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FAILED A SIMA E ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION NR NOT REPORTED 1 SW 21 614AE 145086 ON FLIGHT 3530 ,CREW REPORTED NUMBER 1 ENGINE FLAME OUT EN ROUTE AT 16,000 FT 310KTS. AIRCRAFT REMOVED FROM SERVICE. R EMOVED AND REPLACED 1A AND 1B FADEC IAW ROLLS ROYCE MM 73-22-01 AND REMOVED AND REPLACED LEFT ENGINE FPMU IAW ROLLS ROYC E MM 73-21-10. OPERATION CHECK GOOD. NO LEAKS NOTED. FOUND FADCU HARNESS AT CONNECTION P8 PIN A BURNED. REMOVED AND REPLACED NR 1 ENG BLUE FADEC A IAW ROLLS ROYCE MM 76-11-20. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008013000087 20080130 00087 SO 2008 1 30 SIMA200802806 1 20080126 A 3350 LIGHT EMB 135 EMB135KL 3260302 SO CABIN MALFUNCTIONED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 803AE 145483 ON FLIGHT 3482, CREW REPORTED EXIT ROW 12 EMERGENCY EXIT LIGHT IN THE CEILING DOES NOT ILLUMINATE. AIRCRAFT REMOVED FRO M SERVICE. PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM IAW EMB145 AMM 33-50-00. NO FAULTS NOTED. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008020600117 20080206 00117 NM 2008 2 6 UPS08M51549 1 20080114 A 5330 AGA74187383501 SKIN DOUG MD11 MD11F 3023600 NM BS 1925 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:SP FROM DMI D362760, FUSELAGE SKIN REPAIR AT BS 1925 BETWEEN L45R AND L48L. INSTALLED TRIPLER REPAIR PE R EO MD11-5330-28480-A AND EA 011- 5330-01-A1261. 2 L 7 3 4F RT A22WE 2008020600128 20080206 00128 EU 2008 2 6 USAA920080192 1 20080121 A 3350 32146220 POWER SUPPLY AIRBUS 330 A330323 3930335 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 270AY 315 BFM - EEL - C2 CHECK - EMERGENCY LIGHT POWER SUPPLY UNIT 14WL INOPERATIVE. REPLACED AND OPERATIONAL CHECKED EMERGENCY L IGHT POWER SUPPLY UNIT 14WL IAW A330 AMM 33-51-38. 2 L 7 2 4F RT A46NM 2008020600138 20080206 00138 NM 2008 2 6 2008UALA00308 1 20080117 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 AFT CABIN FLOORBEAM UPPER FLANGE IS CORRODED AT BS 1006 LBL 22 WL 208. MAJOR REPAIR: REPLACED FLOORBEAM TEE CAP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600154 20080206 00154 NM 2008 2 6 2008UALA00319 1 20080120 A 5340 ATTACH ANGLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 902UA 25002 CABIN, INTERCOSTAL CLIP CRACKED AT STA 360, STR 11L. MAJOR REPAIR: INSTALLED NEW INTERCOSTAL ATTACH ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600166 20080206 00166 NM 2008 2 6 UPS08451591 1 20080130 A 5751 SKIN BOEING 747 747123 1384873 NM LT O/B AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 676UP 20101 LT O/B AILERON UPPER SKIN HAS .5" BPT CRACK 4" FWD T/E, 11' IB OF OB END. APPLIED SPEED TAPE PER SRM 51-40-09 FIG 1 TAB LE 1 AND TABLE II. REINSPECT EVERY "A" CHECK. PERMANENT REPAIR AT NEXT "C" CHECK. TRANSFERRED TO D368106. 2 L 7 4 4F RT A20WE 2008020600208 20080206 00208 WP 2008 2 6 UPS08851588 1 20080129 A 3350 CIRCUIT BREAKER DOUG DC8 DC873F 302199F WP COCKPIT FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 ON PREFLIGHT, EMERGENCY EXIT LIGHTS CAME ON WHEN ARMED. FOUND EMERGENCY EXIT LIGHT CONTROL C/B BAD. REMOVED AND REPLAC ED SAME PER MANUAL 20-60-01. SYS OPS CKS PER MM 33-50-02-2. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2008020600214 20080206 00214 WP 2008 2 6 UPS08851603 1 20080110 A 5541 RIB DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 17TH RIB FROM BOTTOM OF RUDDER ON LE CAVITY CRACKED. RUDDER REPLACED ON N/R 123801. 2 L 7 4 4F RT 4A25 2008020600216 20080206 00216 EA 2008 2 6 MASA200800033 1 20080117 A 5210 HINGE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77181 7181 FLT 7223, IAD, LEFT LOWER PAX DOOR HINGE CRACKED. REPLACED FAIRING. 2 L 7 2 4F RT A21EA 2008020600219 20080206 00219 EA 2008 2 6 MASA200800036 1 20080117 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 926LR 15026 ASH FLT 2920 PHX - EMERGENCY FLOOR LIGHT 16A TWO LAMP INOP. RELAMPED. 2 L 7 2 4F RT A21EA 2008020600225 20080206 00225 NM 2008 2 6 UPS08M51580 1 20080117 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1341-1361 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C CABIN-SEAT TRACK CROWN AREA AT STA 1341-1361, X=-107 FOUND CORROSION AS MARKED. CORROSION AT CABIN ST A 1341-1361 X=-107 ON SEAT TRACK CROWN AND UPPER LEG AREA REMOVED PER SRM 51-21-01 V.II R35, FOUND EXCEEDED LIMITS PER S RM 5 3-70-00 FIG 3 V.I R35. EXCEED LIMIT SEAT TRACK REMOVED PER SRM 51-31-01 V.II R35. NEW SEAT TRACK REPAIR SECTION A ND SPLICES FAB AND INSTALLED PER SRM 53 -70-00D FIG 1 VOL I REV 35. 2 L 7 3 4F RT A22WE 2008020600239 20080206 00239 NM 2008 2 6 USAA920080201 1 20080112 A 5340 693535214 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED STRINGER TIE CLIP, BS 597, S8L. REPLACED STRINGER TIE CLIP, BS 597, S8L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600244 20080206 00244 NM 2008 2 6 USAA920080216 1 20080117 A 5320 146N52816 SUPPORT CHANNEL BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 MCN - MAJOR REPAIR - C11 CHECK - CORROSION ON FLOOR STRUCTURE SUPPORT CHANNEL, BS 1300 - BS 1320, RBL 22.75, WL 208. RE PLACED FLOOR STRUCTURE SUPPORT CHANNEL, BS 1300 - BS 1320, RBL 22.75, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008020600245 20080206 00245 NM 2008 2 6 USAA920080218 1 20080112 A 5340 693535214 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED STRINGER CLIP, BS 639, S1. REPLACED STRINGER CLIP, BS 639, S1 IAW B737 SRM 51 -40-02. 2 L 7 2 4F RT A16WE 2008020600250 20080206 00250 NM 2008 2 6 USAA920080224 1 20080113 A 5311 65458076 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 294.5, S10R. REPLACED FRAME, BS 294.5, S10R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600253 20080206 00253 NM 2008 2 6 USAA920080227 1 20080116 A 5320 65535953 REVEAL BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED R1 DOOR CUTOUT REVEAL, BS 305, S7R. REPLACED R1 DOOR CUTOUT REVEAL, BS 305, S 7R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600254 20080206 00254 WP 2008 2 6 UPS08851609 1 20080201 A 3350 BATTERY DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNITS. OPS CHECKED N ORMAL PER MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2008020600265 20080206 00265 NM 2008 2 6 USAA920080236 1 20080118 A 5320 SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED INTERCOSTAL SUPPORT, BS 360, S10L. REPLACED INTERCOSTAL SUPPORT, BS 360, S10L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008020600266 20080206 00266 NM 2008 2 6 USAA920080234 1 20080117 A 5312 BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACK EXTENDING THRU FASTENER HOLE IN VERTICAL BEAM, BS 178, RBL 17, WL 227. REPAIRED VERTICAL BEAM, BS 178, RBL 17, WL 227, IAW B737-300 SRM 51-17-13. 2 L 7 2 4F RT A16WE 2008020600268 20080206 00268 SO 2008 2 6 C2XA08TY015 1 20080124 A 3320 BR900022 BALLAST EMB 145 EMB145 3260210 SO CABIN BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 27962 145110 TYS - CREW REPORTED SMOKE AND A BURNING SMELL IN THE CABIN. MAINTENANCE REMOVED AND REPLACED THE LT SIDEWALL BALLAST IA W EMB 145 AMM 33-21-03, OPS CHECKS GOOD AND WAS RELEASED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008020600273 20080206 00273 NM 2008 2 6 08FDEA00327 1 20080130 A 3260 WARNING LIGHT DOUG MD11 MD11F 3023600 NM MLG FALSE ACTIVATION A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 618FE 48754 AFTER TAKEOFF GEAR LEVER RAISED AND RED LIGHT REMAINED ON IN RT MAIN INDICATOR (BOTH) PER QRH, REMAINED BELOW 230 KNOTS , EXTENDED GEAR RAISED GEAR AND ALL RED LIGHTS EXTINGUISHED. CONTINUED TO DESTINATION NO PROBLEM. T/S IAW FIM 32-30-0 3 AND 31-71-04-00. NOTHING FOUND A/C OK TO CONTINUE. 2 L 7 3 4F RT A22WE 2008020600274 20080206 00274 WP 2008 2 6 UPS08851534 1 20080113 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 COCKPIT FLOOR PNL 682A HAS AREAS OF CORROSION OUT OF LIMITS. REMOVED TOP SKIN OF FLOOR PNL 682A IAW SRM 51-1-21. FABRICATED AND INSTALLED REPLACEMENT SKIN ON FLOOR PNL 682A IAW DWG 5619357, AND SRM 52-2-O FIG 001F. 2 L 7 4 4F RT 4A25 2008020600275 20080206 00275 NM 2008 2 6 NOCA00108 1 20080113 A 3350 767 LIGHT BOEING 757 75728A 1384976 NM EXTERIOR INOPERATIVE A NOCA K NONE O OTHER UK UNKNOWN 1 EA 15 752NA 28174 L-1 DOOR OUTSIDE EMERGENCY LIGHT DOESN'T ILLUMINATE. RELAMPED L1 EMERGENCY LIGHT, OPS CHECKS OK. 2 L 7 2 4F RT A2NM 2008020600278 20080206 00278 NM 2008 2 6 SB08003 1 20080123 A 2560 MV10 MEGAPHONE BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 444US 24862 PBI FLT 1980 - PILOT REPORTED THE FORWARD MEGAPHONE WAS INOPERATIVE AND THE AFT MEGAPHONE BATTERY COVER WAS BROKEN. MAI NTENANCE REMOVED AND REPLACED BOTH THE FORWARD AND AFT MEGAPHONES. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008020600279 20080206 00279 NE 2008 2 6 NOCA00408 2 20080118 A 7321 07482CN182OM33P1 EEC BOEING 767 76736N 1385152 NM PWA 4060 PW4060 52119 NE RT ENGINE MALFUNCTIONED A NOCA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 15 768NA 29898 DURING CLIMBOUT HAD EXCESSIVE AIRFRAME VIBRATION, NO EICAS MSG. REDUCED THRUST VIBRATION WENT AWAY. RETURNED TO BAH. ENGINE LIMITS AND ENGINE INDICATIONS WAS NORMAL. AN EXTERIOR INSPECTION WAS ACCOMPLISHED PER M/M 05-51-38 TASK 201, NO FAULTS WERE FOUND. INSPECTED ENGINE PANELS AND DOORS ALL NORMAL. CARGO BINS ALSO INSPECTED ALL FOUND TO BE NORMAL. AC COMPLISHED ENGINE HIGH POWER RUN (VIBRATION SURVEY TEST 6) PER M/M 71-00-00-735-320-H00, ALL PARAMETERS WERE NORMAL WITH ENG NR 1 VIB .9 AND ENG NR 2 VIB 1.2 THE HIGHEST READING AT HIGH POWER. BOEING HAS DECODED THE DFDR DATA PROVIDED FOR BOTH THE BAHRAIN ATB ON 18-JAN-08 AND THE FLIGHT FROM NGU TO JFK ON 19-JAN-08. OUR REVIEW OF THE DATA SUPPORTS THE REF 2 L 7 2 4F 4 F RT A1NM E24NE 2008020600283 20080206 00283 EU 2008 2 6 USAA920080237 1 20080122 A 3240 C202163382D32 CONTROL UNIT AIRBUS 320 A320231 3930325 EU LANDING GEAR FAILED A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 627AW 36043 37 66 FLT 18 - SNA-PHX - EL - ON CLIMBOUT FROM SNA AND ON APPROACH INTO PHX, BSCU 1 FAILED RESULTING IN "BRAKES ANTISKID NOSEW HEEL STEERING" FAULT. BSCU 2 WAS ALREADY ON MEL. AN EMERGENCY WAS DECLARED AND THE PASSENGERS WERE BRACED. THE FLIGHT LANDED WITHOUT INCIDENT AND THE AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE BRAKING / STEERIN G CONTROL UNIT. BITE CHECK WAS GOOD. BSCU WAS A CONFIRMED FAILURE. UNIT FAILED OUTPUT TEST SYSTEM 2 DUE TO DEFECTIVE RELAYS AND TRANSISTORS ON INTERCONNECT 2 BOARD. IC 37,38 ON PROCESS BOARD HAD BROKEN PINS. RELAY MFG PN EFD2C26, IC MFG PN MK7726BQ. 2 L 7 2 4F RT A28NM 2008020600284 20080206 00284 2008 2 6 2008UALA00202 4 20080113 A 3460 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FLT MANAGEMENT MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 413UA 470 RTFL WITH A FLIGHT MANAGEMENT COMPUTER FAILURE. *S/D* RESET FMGC 1 AND 2 AND CROSS LOADED, OK- UPDATED FMS DATA UA3080 1001 17JAN TO 24FEB. OPS CHECKING NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600286 20080206 00286 EU 2008 2 6 2008UALA00205 1 20080111 A 3350 D9239003500060 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 424UA 506 EMERGENCY EEL LIGHTS INOP FROM FRONT OF AC TO ROW 6. FAULTY EPSU. REPLACED EPSU, GROUND TEST NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600288 20080206 00288 EU 2008 2 6 2008UALA00227 1 20080114 A 2932 501310000 PRESSURE SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYDRAULIC SYS FAILED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 430UA 568 FLIGHT DIVERTED DUE TO GREEN HYDRAULIC PUMP FAILURE. NR 1 ENG PUMP PRESS SWITCH FAILURE. REPLACED NR 1 ENG PUMP PRESS SWITCH, OPS CHECKED OK. ALSO REPLACED CASE DRAIN FILTER AS PRECAUTIONARY. FILTER WAS CLEAN WHEN REMOVED, NO CONTAMINAT ION. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600290 20080206 00290 NM 2008 2 6 2008UALA00246 1 20080115 A 3222 SEAL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NLG STRUT LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 804UA 759 RTFL UNDER AMBER ALERT DUE TO A LANDING GEAR RETRACTION MESSAGE. LEAKING STRUT SHOCK SEALS. REMOVED AND REPLACED SEALS ON NLG SHOCK STRUT SERVICED STRUT AND PERFORMED RETRACTION TEST, ALL NORMAL OPERATION. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600291 20080206 00291 EU 2008 2 6 2008UALA00247 1 20080112 A 2611 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LAVATORY FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 420UA 489 SMOKE LAVATORY DETECTOR FAULT ECAM. SWAPPED DETECTOR WITH AFT LAV AND RETESTED, ALL NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600297 20080206 00297 NM 2008 2 6 2008UALA00352 1 20080121 A 5514 FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 RIGHT HORIZ STAB CENTER SECTION FWD LUG FWD FACE CORRODED ON AFT SPAR UPPER ATTACH CLEVIS. MAJOR REPAIR: REMOVED CORRO SION. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600302 20080206 00302 2008 2 6 2008UALA00365 4 20080122 A 2565 720129101 HOSE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE COLLAPSED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 RIGHT EMERGENCY EXIT SLIDE INFLATION HOSE IN THE HYDRAULIC SERVICE BAY IS COLLAPSED AND SPONGY. REPLACED HOSE ASSY. HY DRAULIC SPLASH DURING SERVICING MAKES CONTACT WITH HOSE & PARTIALLY DISSOLVES IT, BECOMING SPONGY. HOSE THEN IS PRONE T O COLLAPSING. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020600306 20080206 00306 NM 2008 2 6 2008UALA00373 1 20080123 A 5230 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BULK CARGO DOOR CANNING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 BULK CARGO DOOR SKIN OIL CANNING AT FWD LWR AREA. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. INSTALLED EXTERNAL SKIN DOU BLER. 2 L 7 4 4F 4 F RT A20WE E24NE 2008020600307 20080206 00307 NM 2008 2 6 2008UALA00374 1 20080122 A 3500 9F4027507 OXYGEN BOTTLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE R2 DOOR LOW PRESSURE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 O2 BOTTLE AT DOOR 2R LOW. SUSPECT FAULTY VALVE. REPLACED O2 BOTTLE AT DOOR 2R. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020600316 20080206 00316 NM 2008 2 6 2008UALA00387 1 20080122 A 2432 263BA1012 BATTERY BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE MAIN DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 791UA 26933 A/C LOST POWER AT GATE PRIOR TO DEPARTURE. ACFT WILL NOT POWER UP. SUSPECT BATTERY VOLTAGE LOW. REPLACE MAIN AND APU BATTERYS. REPLACED APU BATTERY CHARGER. OPERATION NORMAL. REPLACED MAIN BATTERY CHARGER. GRD CHECKED NORMAL. ACFT OK F OR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008020600320 20080206 00320 NM 2008 2 6 2008UALA00394 1 20080123 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 AFT PIT FRAME DENTED JUST OUTBOARD OF STR 26L AT STA 1440, INBOARD FLANGE. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600323 20080206 00323 NM 2008 2 6 2008UALA00397 1 20080123 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 AFT PIT AT STA 1500, APPROX AT STR 26L FRAME DENTED ON INBOARD FLANGE. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600330 20080206 00330 NM 2008 2 6 ZZDA2008048 1 20080107 A 5311 SPLICE BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 A/C STRUCK BY BAG CART. HOLES ELONGATED ON SPLICE AT CANTED FRAME 1161 BL 0. INSTALLED NEW SPLICE AT CANTED FRAME STA 1161 BL 0 IAW B717 SRM 51-41-05 AND AIRTRAN ES17-53-00939A DATED 1/21/08. 2 L 7 2 4F TR A6WE 2008020600333 20080206 00333 SO 2008 2 6 C2XA08IA032 1 20080124 A 3232 23092700503 ACTUATOR EMB 145 EMB145EP 3260221 SO RT MLG MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 14937 21142 21142 145026 IAH - FLIGHT 2618, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE WHILE EN ROUTE FROM SHV TO IAH WITH A RED "X" ON THE RT MAIN GEAR INDICATOR. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE RIGHT MA IN LANDING GEAR MANEUVERING ACTUATOR, OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. 2 L 7 2 4F RT T00011AT 2008020600337 20080206 00337 EA 2008 2 6 HNAA08000036 1 20080121 A 3350 6104789 BATTERY DHAV DHC8 DHC8311 1386006 EA CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 331EN 32873 478 279 LAST TWO CEILING EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY. 2 H 7 2 4T RT A13NM 2008020600345 20080206 00345 EA 2008 2 6 COMA0880001 1 20080116 A 5240 SERVICE DOOR CNDAIR CL600 CL6002D24 1390016 EA OPEN A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 679CA 15132 FLIGHT 5545 - AIRCRAFT RETURNED BACK TO CVG FOR COMM SERVICE DOOR BEING LEFT OPEN. AIRCRAFT LANDED SAFELY. SECURED COM M SERVICE DOOR. NO OTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008020600353 20080206 00353 NM 2008 2 6 2008UALA00533 1 20080130 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 348-360 S17R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FUSELAGE STRINGER 17R CREASE BEAM WEB HAS ELONGATED HOLES, BS 348-360. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INS TALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600357 20080206 00357 GL 2008 2 6 C2XA08CL012 2 20080124 A 7532 32158861 BLEED VALVE EMB 145 EMB145EP 3260221 SO ALLSN AE300 AE3007A GL NR 1 ENGINE FAULTY A C2XA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 14943 8819 145040 BWI FLIGHT 2247 - THE CREW REPORTED A NR 1 ENGINE BLEED VALVE FAIL MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO THE G ATE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE BLEED VALVE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008020400162 20080204 00162 EA 2008 2 4 TRAX200800101 1 20080116 A 5210 STEP CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 PAX DOOR LOWER STEP CRACKED. 2 L 7 2 4F RT A21EA 2008020500002 20080205 00002 WP 2008 2 5 08FDEA00280 1 20080125 A 5311 ADA007313 FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 FWD PIT AT STA 919 BETWEEN STR 51R AND 51L LOWER FLANGE, FRAME HAS CORROSION. REPAIRED LOWER FLANGE AT STA 919, LONG 5 1R & 51L IAW DC/MD10-10 SRM 53-30-00, VOL I FIGURE 5 2 L 7 3 4F RT A22WE 2008013000118 20080130 00118 EU 2008 1 30 08FDEA00231 1 20080123 A 5522 SKIN AIRBUS 310 A310221 3930310 EU RT ELEVATOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 RT ELEVATOR APPROX STA 529 TOP SURFACE SKIN CORRODED. REPAIRED RT ELEVATOR UPPER SKIN CORROSION BY REMOVING DAMAGED SKI N, AND FABING SKIN PLUG AND DOUBLER, BONDING SKIN PLUG AND DOUBLER, EDGE SEALING REPAIR, AND REFINISHING IAW A310-200 SRM 51-77-12 FIG 224. 2 L 7 2 4F RT A35EU 2008013000147 20080130 00147 NM 2008 1 30 DLM88080075 1 20080116 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 897 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 EXFOLIATION CORROSION ON LT CABIN CUSP WEB AT STA Y=897. REPAIRED IAW ERA 398191-14MA REV A. 2 L 7 2 4F RT A6WE 2008013000155 20080130 00155 NM 2008 1 30 DLM88080085 1 20080116 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 566 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 EXFOLIATION CORROSION ON LT CABIN CUSP WEB AT STA Y=566. REPAIRED CUSP WEB IAW ERA 398191-14MA REV A. 2 L 7 2 4F RT A6WE 2008013000172 20080130 00172 NM 2008 1 30 08FDEA00253 1 20080124 A 5753 SKIN DOUG MD11 MD11F 3023600 NM TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 RT WING, INBOARD FLAP LOWER SURFACE FOUND DENTS AT XIFH 192. REPAIR CARRIED OUT AT RT WING INBOARD FLAP LOWER SURFACE D ENT AREA AT XIFH 192 AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008013000180 20080130 00180 NM 2008 1 30 DLM90080058 1 20080112 A 5322 995301643 SHEAR TIE DOUG MD90 MD9030 3023690 NM BS 1486 L1 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 STA1486 SWEAR CLIP AT L-1 CRACKED. REMOVED AND REPLACED CLIP AT STA1486 L-1, IAW MD90 SRM 51-30-05. 2 L 7 2 4F RT A6WE 2008013100099 20080131 00099 NM 2008 1 31 SWAA080432 1 20080123 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008013100113 20080131 00113 NM 2008 1 31 SWAA080444 1 20080124 A 5322 69353656 SHEAR TIE BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008013100151 20080131 00151 NM 2008 1 31 SWAA080454 1 20080125 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 449WN 32469 DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS MISSING AT ROW 13 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008013100154 20080131 00154 NM 2008 1 31 SWAA080456 1 20080127 A 5311 6545808 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294, STR 16R. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2008013100155 20080131 00155 NM 2008 1 31 SWAA080474 1 20080127 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 413, LBL 3. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008013100191 20080131 00191 NM 2008 1 31 SWAA080481 1 20080128 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 296WN 36613 DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER M M. 2 L 7 2 4F RT A16WE 2008013100214 20080131 00214 NM 2008 1 31 SWAA080488 1 20080128 A 5330 6545768 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 393, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008013100229 20080131 00229 EA 2008 1 31 TRAX200800093 1 20080113 A 5210 SKIN CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 317CA 10055 PAX DOOR INNER SKIN CRACKED 8 INCHES AFT OF FWD EDGE 4 INCHES UP FROM BOTTOM ON SKIN. REMOVED INNER SKIN AND INSTALLED NEW INNER SKIN PER CRJ 700 SRM 51-42-06,51-42-13 AND 52-11-01. 2 L 7 2 4F RT A21EA 2008013100247 20080131 00247 NM 2008 1 31 KCSA081030 1 20080120 A 5414 SKIN BOEING 747 747236B 1384804 NM NR 4 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 NR 4 PYLON I/B SKIN CRACKED AT FWD LOWER ACCESS PANEL OPENING AT NAC STA 197. 2 L 7 4 4F RT A20WE 2008013100268 20080131 00268 EA 2008 1 31 VNAA0801005 1 20080117 A 3010 6420002 PRESSURE SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE ANTI-ICE SYSTEM FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 05 216PS 9440 7882 CREW REPORTED A RIGHT HAND ANTI ICE DUCT FAIL RED MASTER WARNING ON TAKEOFF. CREW ELECTED TO RETURN TO GNV AND LANDED W ITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE WING ANTI ICE AND CONTROL INDICATION SYSTEM ALONG WITH THE BLEED AIR LEAK CONTROL UNIT AND ICE DETECTION SYSTEMS. MAINTENANCE REMOVED AND REPLACED THE PRESSURE SWITCH IN ACC ORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008013100312 20080131 00312 NM 2008 1 31 DLM88080090 1 20080116 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM PAX CABIN CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 957DL 49976 EXFOLIATION CORROSION ON LT CABIN WEB AT STA Y=546. REPAIRED CUSP WEB IAW ERA 398191-14MA REV A. 2 L 7 2 4F RT A6WE 2008013100322 20080131 00322 NM 2008 1 31 DL764080105 1 20080119 A 3350 BATTERY BOEING 767 767432ER 1385134 NM BS 1545 RBL 53 INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 825MH 29696 BATTERY AT CHARGER M12 STA 1545 RBL 53 BATTERY WON`T CHARGE. REMOVED AND REPLACED BATTERY, DURING HMV1 AT TIMCO IN GSO ON NR 44981. 2 L 7 2 4F RT A1NM 2008013100327 20080131 00327 EA 2008 1 31 CHQA200800010 1 20080119 A 2751 855D10011 POSITION SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS MALFUNCTIONED A CHQA O OTHER N FALSE WARNING AP APPROACH 1 GL 11 469SM 13958 7650 GEE873397 IAH TO CMH - ON DOWNWIND LEG TO LAND AT CMH, THE FLAPS FAILED AT ZERO DEGREES. CREW FOLLOWED QRH AND MADE AN UNEVENTFUL LANDING AT CMH. MAINTENANCE TROUBLESHOT THE FLAP SYSTEM DOWN TO THE RIGHT FLAP BRAKE POSITION SENSOR. AFTER REPLACING THE POSITION SENSOR, THE FLAP SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2008013100331 20080131 00331 NE 2008 1 31 DLM88080095 2 20080119 A 7230 FAN BLADE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE BENT A DALA A UNSCHED LANDING R A J PARTIAL RPM/PWR LOSS FLAME/FIRE WARNING INDICATION CL CLIMB 1 SO 27 919DE 41321 53422 725878 DURING CLIMB-OUT, NR 1 ENG HAD TWO COMPRESSOR STALLS AND FLAMES AS REPORTED BY F/A AND PASSANGERS. REPLACED 1ST STAGE F AN BLADES PER TRANS 9T133. 2 L 7 2 4F 4 F RT A6WE E9NE 2008013100341 20080131 00341 EU 2008 1 31 08FDEA00273 1 20080122 A 5340 A5397825620000 ATTACH FITTING AIRBUS 310 A310222 3930315 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 AFT CARGO COMPARTMENT, ATTACHMENT FITTING OF CROSSBEAM TO FR 64 AT Y-1400, FOUND CRACKED. THE FITTING WAS REPLACED IAW SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2008013100349 20080131 00349 EU 2008 1 31 UPS08151396 1 20080110 A 3260 SWITCH AIRBUS A300 A300F4622R 3930360 EU LANDING GEAR INOPERATIVE A IPXA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 164UP 005 INSPECTION TYPE:N/A ON FINAL APPROACH AT GEAR DOWN, GOT ECAM IND "LG POS DET SYS 2 FAULT". DID QRH PROC AND LANDED UNEV ENTFULLY. DEF "LG POS DET SYS 2", PER MEL 32-61-04. PLACARD INSTALLED DEF 366625. REMOVED AND REPLACED LANDING GEAR N ORMAL CONTROL MICROSWITCH UNIT (2GB) PER MM 32-31-11-04. 2 L 7 2 4F RT A35EU 2008013100362 20080131 00362 WP 2008 1 31 UPS08851459 1 20080118 A 5270 WARNING SYSTEM DOUG DC8 DC871F 302199D WP BELLLY DOOR MALFUNCTIONED A IPXA K NONE N FALSE WARNING TO TAKEOFF 1 SO 01 744UP 45944 INSPECTION TYPE:N/A ATB - AFTER ROTATION, MASTER WARNING LIGHT ALONG WITH BELLY DOOR ILLUMINATED. THE TOWER WAS INFORME D, RETURN FOR LANDING. LANDED IN THE SAME PATTERN WITHOUT ANY PROBLEMS AND TAXIED TO THE RAMP. OPENED AND CLOSED FWD B ELLY DOOR, PIT 32, LIGHT WENT OUT. PUSHED ON DOOR TO ENSURE LOCKED. 2 L 7 4 4F RT 4A25 2008020100003 20080201 00003 WP 2008 2 1 UPS08851469 1 20080103 A 5313 STRINGER SPLICE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 D-PIT STA 1340 L34L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED SPLICE FITTING AT STA 1340 L34L IAW SRM 51-01-20, AND SRM 51-03-02. 2 L 7 4 4F RT 4A25 2008020100011 20080201 00011 NM 2008 2 1 CALA0800032 1 20080119 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 FUSELAGE FRAME STATION 787 IS CRACKED BETWEEN STRINGERS 8R AND 9R. INSTALLED REPAIR ANGLES ON FRAME AT STATION 787, STR INGER 8R AND 9R PER ECRA 5310-04691. 2 L 7 2 4F RT A16WE 2008020100012 20080201 00012 NM 2008 2 1 CALA0800033 1 20080119 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 FUSELAGE FRAME CRACKED AROUND RIVET AT STA 867 ABOVE STRINGER 9R. INSTALLED REPAIR ANGLES ON FRAME AT STATION 867 STRIN GER 9R PER ECRA 5310-04691. 2 L 7 2 4F RT A16WE 2008020100013 20080201 00013 NM 2008 2 1 CALA0800034 1 20080119 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 FUSELAGE FRAME CRACKED AROUND RIVET AT STATION 747 STRINGER 9R PER ECRA 5310-04691. 2 L 7 2 4F RT A16WE 2008013100072 20080131 00072 NM 2008 1 31 MWEA080002 1 20080102 A 5320 9912455505 DOUBLER BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 925ME 55191 DOOR DOUBLER BETWEEN STATION 427 AND STATION 434.5 IS DAMAGED FROM THE BELT LOADER. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2008013100084 20080131 00084 NM 2008 1 31 SWAA080431 1 20080123 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 6 DEF. INSTALLED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008013100096 20080131 00096 NM 2008 1 31 SWAA080428 1 20080123 A 3350 20131A BATTERY PACK BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED SPV CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008013100103 20080131 00103 NM 2008 1 31 SWAA080437 1 20080124 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020500003 20080205 00003 WP 2008 2 5 08FDEA00281 1 20080125 A 5315 ADA00303 FLOORBEAM DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 FWD PIT AT STA 879 RBL 57 FLOORBEAM HAS CORROSION. FOUND TO BE OUT OF LIMITS AND REPAIRED BY SPLICING IN NEW SECTION OF FLOORBEAM IAW SRM 53-00-01 VOL I FIG 7. THIS REPAIR IS CLASSIFIED AS MAJOR. ROLLER TRAY AT STA 765-879 RBL 56 REMOVED FOR ACCESS AND REINSTALLED IAW SRM 51-31-01 VOL II PG1. 2 L 7 3 4F RT A22WE 2008020600014 20080206 00014 NM 2008 2 6 200801232 1 20080119 A 2797 17106276401 WIRE HARNESS EMB ERJ170 ERJ170100SE 3260406 NM TE FLAPS DEFECTIVE A UHLA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 652RW 17000075 FLIGHT 7501 DEN TO ABQ - ON APPROACH CREW SELECTED FLAPS POSITION 1. DURING TRANSITION CREW RECEIVED SLAT FAIL EICAS ME SSAGE. CREW RAN QRH CHECKLIST, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RT SLAT 3 A ND 4 SKEW SENSOR HARNESS. 2 L 7 2 4F RT A56NM 2008020600026 20080206 00026 NM 2008 2 6 USAA920080208 1 20080112 A 5340 693535214 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 639 S2L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED STRINGER CLIP, BS 639, S2L. REPLACED STRINGER CLIP, BS 639, S2L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600036 20080206 00036 EU 2008 2 6 USAA920080194 1 20080120 A 3230 C24730100 UPLOCK AIRBUS 320 A320231 3930325 EU MLG DEFECTIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 620AW 25809 3216 52 FLT 605 - ORD-LAS - AIR TURNBACK - AFTER TAKEOFF, CREW RECEIVED LANDING GEAR RETRACTION ECAM MESSAGE 'LANDING GEAR DOORS NOSE WILL NOT CLOSE COMPLETELY'. RECYCLED GEAR TWICE AND PROBLEM PERSISTED. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR UPLOCK ASSEMBLY. ALL FUNCTIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 2008020600039 20080206 00039 NM 2008 2 6 SWAA080507 1 20080129 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 500C S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020600040 20080206 00040 NM 2008 2 6 SWAA080508 1 20080129 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 927 S26L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, STR 26L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020600052 20080206 00052 NM 2008 2 6 2008UALA00307 1 20080117 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 807 S27L/R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 LOWER FUSELAGE SKIN CREASED AT STA 807 BETWEEN STR 27L AND STR 27R. MAJOR REPAIR: REMOVED DAMAGE. INSTALLED FILLER AND DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600080 20080206 00080 NM 2008 2 6 USAA920080265 1 20080107 A 5347 SEAT TRACK BOEING 767 7672B7ER 1385107 NM BS 380 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 380, LBL 88. REPLACED CABIN SEAT TRACK, BS 380 , LBL 88 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008020600096 20080206 00096 WP 2008 2 6 ABXA080025 1 20080107 A 5310 591236067 STRUCTURE DOUG DC9 DC941 302207N WP WINDOW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 CENTER AND SIDE WINDSHIELD LEFT ZEE P/N: 5912360-67 CRACKED. REPLACED LEFT ZEE IAW SR DWG 09530268, DC9 SRM 51-30-2, 51 -30-5 AND JOB CARD EA 53300036-014. 2 L 7 2 4F A6WE 2008020600115 20080206 00115 WP 2008 2 6 UPS08851587 1 20080129 A 3350 BATTERY DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS MALFUNCTIONED A IPXA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 852UP 46052 EMERGENCY LIGHTS CAME ON AT TAKEOFF WITH THE SWITCH IN THE "ARMED" POSITION. THE LEFT EMERGENCY BUSS WAS OPERATING NORM AL. T/S EMERGENCY EXIT LIGHT SYSTEM. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY AND RELAY UNIT PER MM 33-50-01- 2. SYSTEM OPS CKS GOOD ON GROUND. 2 L 7 4 4F RT 4A25 2008020600127 20080206 00127 WP 2008 2 6 MWEA080011 1 20080118 A 5320 993061237 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 810ME 48072 AFT CARGO COMPARTMENT HAS CORROSION ON BOTTOM OF CUSP MEMBRANE AT DOME NUT JUST AFT OF FRAME STATION 1174L. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2008020600148 20080206 00148 WP 2008 2 6 UPS08851559 1 20080125 A 3350 LAMP DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 FLIGHT DECK EMERGENCY LIGHTS INOP. RELAMPED, OPS CHECK GOOD PER MM 33-50-02-2-2. 2 L 7 4 4F RT 4A25 2008020600155 20080206 00155 EA 2008 2 6 MASA200800074 1 20080129 A 2520 SEAT CNDAIR CL600 CL6002B19 1900309 EA FLT ATTENDENT DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37178 7178 ASH FLT 2986 LAS - PHX - CAPT REPORTS THE FLIGHT ATTENDANT’S SEAT DOES NOT AUTOSTOW. CND, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008020600158 20080206 00158 NM 2008 2 6 2008UALA00321 1 20080120 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 GOUGE AND DENT 3 FT AFT OF LT FWD DOOR AND LEVEL WITH DOOR SILL. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED EXTERNAL DOUBLER, TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600201 20080206 00201 NM 2008 2 6 UPS08M51489 1 20080122 A 5210 DOOR DOUG MD11 MD11F 3023600 NM L1 INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 254UP 48406 CREW PREFLIGHT, L1 ENTRY DOOR WILL NOT OPEN, DEFERRED THE L1 DOOR PER MEL (M367452 ASSIGNED). REPLACED L1 DOOR UP LIMIT SWITCH S1-592 REF MD11 WDM 52-11-01 PG 1. OPS CHECK PER MD11 MM 52-12-00-0 AND 52-11-05-2. CHECKS OK, THIS CLEARS M36 7452. PLACARD REMOVED. 2 L 7 3 4F RT A22WE 2008013100106 20080131 00106 NM 2008 1 31 SWAA080438 1 20080124 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 25R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008013100109 20080131 00109 NM 2008 1 31 SWAA080443 1 20080124 A 5310 6545833 CREASE BEAM BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 344, LBL 70. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008013100198 20080131 00198 NM 2008 1 31 SWAA080486 1 20080128 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008013100205 20080131 00205 NM 2008 1 31 SWAA080498 1 20080128 A 5310 6547977 CREASE BEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CHORD CRACKED AT BS 560, LBL 65. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2008013100314 20080131 00314 NM 2008 1 31 DL757080092 1 20080118 A 5247 BOLT BOEING 757 757232 1384965 NM APU DOOR LOOSE A DALA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 27 693DL 29725 WHILE WORKING ELEVATOR ASSY MESSAGE, FOUND APU DOOR HINGE BOLT LAYING ON TOP OF HORIZONTAL STABILIZER. REINSTALLED BOLT IN DOOR HINGE. 2 L 7 2 4F RT A2NM 2008013100321 20080131 00321 NM 2008 1 31 DL764080104 1 20080119 A 3350 CHARGER BOEING 767 767432ER 1385134 NM BS 284 LBL 53 INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 825MH 29696 BATTERY CHARGER M1208 STA 284 LBL 53 INOP. REMOVED AND REPLACE BATTERY CHARGER ON N/R 44980 DURING HMV1 AT TIMCO IN GSO . 2 L 7 2 4F RT A1NM 2008013100323 20080131 00323 NM 2008 1 31 DL738080106 1 20080121 A 4920 ENGINE BOEING 737 737832 13844CF NM APU CONTAMINATED A DALA D RETURN TO BLOCK C B F.O.D. SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 378DA 30265 TAXI OUT FROM DEICE WITH APU BLEED OPEN AND LT ENG SHUTDOWN VISIBLE GREY SMOKE INTO COCKPIT. CLOSED APU BLEED AND SMOKE DISSIPATED. FOUND GLYCOL WAS SPRAYED INTO APU INTAKE. PACKS RAN, SMELL DISSIPATED. PACK CONTROLLERS HAD NO FAULTS. 2 L 7 2 4F RT A16WE 2008013100347 20080131 00347 NM 2008 1 31 08FDEA00279 1 20080125 A 5315 6520827162 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 CORROSION ON LOWER AFT SIDE OF FLOORBEAM TO CAP AT FLOORBOARD ATTACH FWD HOLE AT FS 720D, LBL 48, WL 208. REMOVED CORRO SION AND FLOORBEAM WAS FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS AND INSTALLED. REMOVED UPPER "T" CHORD CAP F ROM LBL 10 - LBL 68. REF FED EX DWG SR 27-53-034. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 2008013100359 20080131 00359 NM 2008 1 31 DHLA200800010 1 20080128 A 5330 SKIN BOEING 727 727225 1384077 NM FUSELAGE DAMAGED A DHLA O OTHER O OTHER NR NOT REPORTED 1 GL 05 742DH 21290 RT SIDE FUSELAGE HAS A 10 INCH GASH BY 1/4 INCH WIDE AT FUSELAGE STATION 720, 5 O'CLOCK POSITION. INSTALLED MAJOR REPA IR AT BS 700.00 AT RT STRINGER 27 IAW EVA B 253-00040 DTD 1/29/08 REV IR & IAW W/O 3473 TCN MXC10001 DTD 1-30-08. ACFT G ROUNDED. 2 L 7 3 4F A3WE 2008020100016 20080201 00016 NM 2008 2 1 KCSA081032 1 20080121 A 5210 DOOR FRAME BOEING 747 747209B 138489B NM L1 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 MAIN ENTRY DOOR L1 FWD LOWER CORNER VERTICAL FRAME CRACKED. 2 L 7 4 4F RT A20WE 2008020100017 20080201 00017 NM 2008 2 1 KCSA081033 1 20080121 A 5313 STRINGER BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 STR 40L CORRODED AT BS 1698. 2 L 7 4 4F RT A20WE 2008020100018 20080201 00018 NM 2008 2 1 HNAA0800024 1 20080102 A 2711 82740155007 LEVER DHAV DHC8 DHC8102 2809003 NM AILERON TABS WORN A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 906HA 58896 3975 9 IN FLIGHT AIRCRAFT IS DIFFICULT TO TURN LEFT AND SPOILER NR 1 PUSH OFF LIGHT ILLUMINATES WHEN MAKING RIGHT TURNS. FOUND WIRES ON RIGHT HAND SPOILER CLUTCH UPPER MICRO SWITCH, REPAIRED WIRES AND RIGGED MICRO SWITCH. INSPECTED LEFT AND RIGH T AILERONS AND SPRING TABS, FOUND SPRING TAB SPRINGS WORN. REPLACED AND RIGGED SPRING LEVER ASSEMBLIES FOR LEFT AND RIG HT AILERON TABS. EVALUATION FLIGHT SATISFACTORY. 2 H 7 2 4T RT A13NM 2008020100019 20080201 00019 EA 2008 2 1 HNAA0800025 1 20080106 A 2910 82960010181 HYDRAULIC LINE DHAV DHC8 DHC8311 1386006 EA HYDRAULIC SYS FAILED A HNAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 07 335EN 31288 31288 375 NR 1 HYDRAULIC ISO CAUTION LIGHT ILLUMINATED, NR 1 HYDRAULIC QUANTITY DROPPED TO 0 AND NR 1 HYDRAULIC PRESSURE DROPPED T O 0 PSI WITH CORRESPONDING CAUTION LIGHTS. NR 1 ENGINE HYDRAULIC PUMP OPERATED APPROXIMATELY 14 MINUTES WITH NO PRESSUR E. FOUND FLUID DRIPPING FROM RUDDER MANIFOLD AREA. FOUND HYDRAULIC LINE AT RUDDER PRESSURE REGULATOR LEAKING, INSTALLE D TEMP FLEX LINE. DURING INSPECTION FOUND THE DELTA-P TRIPPED. REMOVED AND REPLACED THE ENGINE DRIVEN HYDRAULIC PUMP, THE CASE DRAIN AND PRESSURE MANIFOLD FILTERS. OPERATIONAL AND LEAK CHECK GOOD. 2 H 7 2 4T RT A13NM 2008020100028 20080201 00028 NM 2008 2 1 CALA0800035 1 20080121 A 2612 M1759 TERMINAL BOEING 737 737824 13844BZ NM FIRE LOOP BROKEN A CALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 37252 30583 FIRE DETECTION FAULT LIGHT ILLUMINATED EN ROUTE. NR 1 ENG LOOP-B CAUSES STEADY FAULT LIGHT. LOOP-A CAUSES INTERMITTANT FAULT ILLUMINATION. FOUND 2 TERMINAL ENDS BROKEN OFF ON NR 1 ENGINE CORE LOOP A AND B REPLACED TERMINAL END. 2 L 7 2 4F RT A16WE 2008020100033 20080201 00033 NM 2008 2 1 CALA0800040 1 20080119 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 FUSELAGE FRAME CRACKED AROUND RIVET AT STATION 907 ABOVE STRINGER 9R. INSTALLED REPAIR ANGLES ON FRAME PER ECRA 5310-04 691. 2 L 7 2 4F RT A16WE 2008020100035 20080201 00035 NM 2008 2 1 CALA0800042 1 20080119 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 CRACKED FRAME BETWEEN STRINGER 8L AND 9L AT STATION 400. INSTALLED REPAIR ANGLES PER ECRA 5310-04691. 2 L 7 2 4F RT A16WE 2008020100038 20080201 00038 NM 2008 2 1 CALA0800045 1 20080120 A 5311 654656028 BELTFRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 ABB STATION 947.5 BELTFRAME HAS CORROSION LBL 4". REMOVED CORROSION, CUT OUT DAMAGE, INSTALLED FRAME REPAIR PER SRM 53- 00-07 REPAIR 2 FIG 201. 2 L 7 2 4F RT A16WE 2008020100044 20080201 00044 NM 2008 2 1 CALA0800053 1 20080120 A 5313 6545769 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FORWARD CARGO STRINGER 28R AT STATION 500 HAS CORROSION. REMOVED DAMAGED, FABRICATED PARTS, TREATED, PRIMED AND INSTALL ED PER SRM 53-00-02 FIG 201. 2 L 7 2 4F RT A16WE 2008020100049 20080201 00049 NM 2008 2 1 CALA0800058 1 20080107 A 5315 BAC1493577 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76354 23592 FOUND CRACK IN HORIZONTAL WEB BOTTOM OF FLOORBEAM STA 328 TO STA 312 RBL 31. FABRICATED REPAIRED AND INSTALLED PER SRM 53-10-51. 2 L 7 2 4F RT A16WE 2008020100051 20080201 00051 NM 2008 2 1 CALA0800060 1 20080122 A 5310 65479592 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 AFT BAG BIN CUTOUT FWD FRAME CRACKED AT LOWER STOP PAD REF EA5310-04443. REMOVED AND REPLACED FRAME IN REF TO SRM 51-40 -02, BOEING DRAWING 65 AND ECRA 5311-01386. 2 L 7 2 4F RT A16WE 2008020100052 20080201 00052 NM 2008 2 1 CALA0800061 1 20080109 A 5230 6547957U3 SEAL PLATE BOEING 737 7373T0 1384582 NM CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76354 23592 AFT CARGO DOOR SEAL PLATE FOUND CORROSION AROUND NUT PLATE HOLES. CORROSION ALSO FOUND ON LOWER SURFACE OF SEAL PLATE V IEWED THROUGH LIGHTNING HOLES. SILL WEB FOUND TO BE OUT OF LIMITS. INSTALLED NEW SILL WEB PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020100053 20080201 00053 NM 2008 2 1 CALA0800062 1 20080120 A 5313 65458001261 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76354 23592 FOUND CRACK AT STRINGER 10L BS 294.5. CUT OUT CRACKED PORTION OF STRINGER AND INSTALLED REPAIR PER SRM 51-70-11 FIG 1. ALSO FABRICATED AND INSTALLED NEW STRINGER CLIP AT STA 298 STRINGER 10L PER BOEING DRAWING 69-62054 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020100054 20080201 00054 NM 2008 2 1 KCSA081038 1 20080124 A 5315 FLOORBEAM BOEING 747 747209B 138489B NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 AFT PIT FLOORBEAM UPPER CHORD DENTED AT BS 1720, RBL 20. 2 L 7 4 4F RT A20WE 2008020100055 20080201 00055 NM 2008 2 1 CALA0800063 1 20080124 A 3350 78980 BATTERY PACK BOEING 737 737824 13844BZ NM CABIN DISCHARGED A CALA O OTHER O OTHER UK UNKNOWN 1 SW 27 37252 30583 EMERGENCY LIGHTING TEST SHOWED ROW 19D AND FWD GALLEY RT SIDE BATTERY PACK LOW. REPLACED BATTERY PACK PER CHECK CARD 29 -3350-1-710. 2 L 7 2 4F RT A16WE 2008020100060 20080201 00060 NM 2008 2 1 CALA0800068 1 20080113 A 3350 CONTROLLER BOEING 737 737824 13844BZ NM CABIN FAULTY A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 37267 31586 GATE RETURN FOR EMERGENCY EXIT LIGHTS ILLUMINATING & EXTINGUISHING INTERMITTENTLY. REPLACED CONTROLLER AT AFT FLIGHT AT TENDANT STATION. 2 L 7 2 4F RT A16WE 2008020100061 20080201 00061 NM 2008 2 1 CALA0800069 1 20080116 A 3350 ADD71701100 BATTERY PACK BOEING 737 737924 13848A1 NM L1 DOOR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 37409 30126 DURING RON L-1 DOOR EMERGENCY OVERHEAD LIGHT INOP. REPLACED BATTERY PACK PER MM 33-51-06. 2 L 7 2 4F RT A16WE 2008020100066 20080201 00066 EA 2008 2 1 TRAX200800122 1 20080121 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A ASOA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 861AS 7445 DOOR WILL NOT CLOSE/LOCK INDICATES PAX DOOR CAUTION MESSAGE PREVIOUS WRITE-UP. TAKES MULTIPLE ATTEMPTS TO CLOSE PROPERL Y. 2 L 7 2 4F RT A21EA 2008020100069 20080201 00069 NM 2008 2 1 KCSA081040 1 20080125 A 5230 SKIN BOEING 747 747209B 138489B NM CARGO DOOR DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 C-1 DOOR AFT LOWER CORNER, SKIN DAMAGED ALONG EDGE. 2 L 7 4 4F RT A20WE 2008020100072 20080201 00072 NM 2008 2 1 KCSA081043 1 20080125 A 5311 FRAME BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FRAME CRACKED 1 INCH AT STA 2690.85 LBL 36 WL 305. 2 L 7 4 4F RT A20WE 2008020100073 20080201 00073 NM 2008 2 1 CALA0800073 1 20080126 A 5313 6545774 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FUSELAGE AT STA 840 STRINGER 21L WAS CORRODED. REMOVED DAMAGED SECTION, FABRICATED AND VERIFIED REPAIR PART, TREATED, P RIMED AND INSTALLED IN REF TO SRM 53-00-03. 2 L 7 2 4F RT A16WE 2008020100076 20080201 00076 NM 2008 2 1 CALA0800076 1 20080127 A 5311 654654043 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 CABIN STA 639 FRAME WEB CRACKED JUST ABOVE CABIN FLOOR. REPAIRED CRACKED WEB PER ECRA 5311-01388. 2 L 7 2 4F RT A16WE 2008020100079 20080201 00079 NM 2008 2 1 KCSA081045 1 20080129 A 5347 SEAT TRACK BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 AFT PIT SEAT TRACK CRACKED AT BS 1839, RBL 46. 2 L 7 4 4F RT A20WE 2008020100082 20080201 00082 NM 2008 2 1 CALA0800078 1 20080128 A 5311 6546552 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FUSELAGE FRAME IS CRACKED AT STA 827 BETWEEN STRINGERS 8L AND 9L. INSTALLED REPAIR DOUBLERS PER ECRA 5310-04698. 2 L 7 2 4F RT A16WE 2008020100084 20080201 00084 NM 2008 2 1 CALA0800080 1 20080128 A 5210 147A85407 STRUCTURE BOEING 737 737724 13844BY NM L2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 54711 28782 CORROSION FOUND ON L-2 LOWER DOOR CHORD. REMOVED AND REPLACED L-2 DOOR CHORD PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020100085 20080201 00085 NM 2008 2 1 KCSA081048 1 20080129 A 5320 THRESHOLD BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 CORROSION ON BOTTOM OF L-1 MAIN ENTRY DOOR THRESHOLD WEB AT BS 461. 2 L 7 4 4F RT A20WE 2008020100086 20080201 00086 NM 2008 2 1 CALA0800081 1 20080129 A 5311 BAC15171470 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FUSELAGE FRAME IS CRACKED AT STA 867 BETWEEN STRINGER 8R AND 9R. REPAIR PER ECRA 5310-04697. 2 L 7 2 4F RT A16WE 2008020100088 20080201 00088 NM 2008 2 1 CALA0800083 1 20080129 A 5311 BAC15171470 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FUSELAGE FRAME STA 887 IS CRACKED BETWEEN STRINGERS 8R AND 9R. REPAIRED PER ECRA 5310-04697. 2 L 7 2 4F RT A16WE 2008020100091 20080201 00091 NM 2008 2 1 CALA0800086 1 20080129 A 5311 BAC15171147 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FUSELAGE FRAME IS CRACKED AT STA 727E BETWEEN STRINGER 8L AND 9L. REPAIRED PER ECRA 5310-04697. 2 L 7 2 4F RT A16WE 2008020100093 20080201 00093 NM 2008 2 1 KCSA081050 1 20080130 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 ONE FASTENER HOLE CRACKED IN FUSELAGE SKIN AT BS 800, STR 17R. 2 L 7 4 4F RT A20WE 2008020100114 20080201 00114 EU 2008 2 1 08FDEA00261 1 20080123 A 7997 21W4072537 CONNECTOR AIRBUS 300 A300B4622R 3930312 EU PWA 4158 PW4158 NE OIL SYSTEM DAMAGED A FDEA G O2 MASK DEPLOYED J X WARNING INDICATION ENGINE FLAMEOUT DE DESCENT 1 SO 25 725FD 572 717763 ON DESCENT NR 1 ENG THRUST WOULD NOT INCREASE, FOLLOWED BY OIL PRESS LOW WARNING. PRESS SHOWED NEAR ZERO, S/D ENG NR 1, ENG NR 1 WINDMILL APPROX 10 MIN, PER CREW DEBRIEF, ON DESCENT WITH THROTTLES AT IDLE. ADVANCED THROTTLES TO LEVEL OFF, NR 1 ENG W/N RESPOND, ECAM WARN FOR LOW OIL PRESS CAME ON, CREW S/D NR 1 ENG. BITE TEST ON NR 1 FADEC FOUND CODES 350- 18 AND 350-29 ON CH A AND B. BACKSHELL DAMAGED AT C/P DH10. REMOVED AND REPLACED NR 1 ENG OIL PRESS XMTR AND LOP SW. LEAK CK'S GOOD. REMOVED AND REPLACED NR 1 ENG FUEL FILTER. NO DEFECTS NOTED. REMOVED AND REPLACED TCC DUE FAULT CODES 350-18,350-29. REPLACED FUEL FILTER. PERF'D AFS/LAND TEST, OPS NORM. REMOVED AND REPLACED CONNECTOR DH10 AND BACKSHE 2 L 7 2 4F 4 F RT A35EU E24NE 2008020100117 20080201 00117 WP 2008 2 1 08FDEA00285 1 20080125 A 5310 ACA72251 DOOR FRAME DOUG MD10 MD1010F 3022112 WP BS 738 S27L CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 NR 6 MCD LOWER JAMB SUPPORT FITTING HOLES A, C AND D HAS CRACK INDICATIONS FOUND WITH BHEC (SEE ATTACHED DRAWING). INST ALLED REPAIR BUSHINGS IN REFERENCE WITH DC/MD10-10 SRM VOLUME I, 53-50-00, PAGE 81 FIG 17 AT HOLE LOCATIONS A, C, AND D TO CARGO DOOR JAMB BEAM ONLY. LOWER FITTING WAS REPLACED ON NON-ROUTINE N00951. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008020100118 20080201 00118 WP 2008 2 1 08FDEA00286 1 20080125 A 5310 ACA72251 DOOR FRAME DOUG MD10 MD1010F 3022112 WP BS 738 S27L CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 NR 6 MCD LOWER JAMB SUPPORT FITTING HOLES A, C AND D HAS CRACK INDICATIONS FOUND WITH BHEC (SEE ATTACHED DRAWING). INST ALLED REPAIR BUSHINGS IN REFERENCE WITH DC/MD10-10 SRM VOLUME I, 53-50-00, PAGE 81 FIG 17 AT HOLE LOCATIONS A, C, AND D TO CARGO DOOR JAMB BEAM ONLY. LOWER FITTING WAS REPLACED ON NON-ROUTINE N00951. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008020100125 20080201 00125 WP 2008 2 1 08FDEA00294 1 20080126 A 5340 AFA71321 BRACKET DOUG DC10 DC1030F 3023504 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MCD SPOOL BRACKET NR 4 HAS CRACK INDICATION ON HOLES A, B, C, AND D. REPAIRED IAW EA 8-5310-113030. 2 L 7 3 4F RT A22WE 2008020100127 20080201 00127 WP 2008 2 1 08FDEA00296 1 20080126 A 5340 AFA71321 BRACKET DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MCD SPOOL BRACKET NR 7 HAS CRACK INDICATION ON HOLES A, B, C, AND D. REPAIRED IAW EA 8-5310-113030. 2 L 7 3 4F RT A22WE 2008020100128 20080201 00128 WP 2008 2 1 08FDEA00297 1 20080126 A 5347 S4929147 SEAT TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MAIN CABIN SEAT TRACK HAS AREAS OF CORROSION STA 1481 TO 1531 LBL9. REMOVED, FABRICATED AND INSTALLED SEAT TRACK ATTACH LOBE AND SUPPORT STRUCTURE REPAIR IAW MD/DC10 -30 SRM 53-70-00 FIG 5 SHT 1 VOL 1,51-38-01 VOL II, 51-21-01 VOLII, 51-21 -02 VOLII AND 51-40-02 VOLII. 2 L 7 3 4F RT A22WE 2008020100129 20080201 00129 EU 2008 2 1 08FDEA00302 1 20080127 A 5347 A5381310620000 SEAT TRACK AIRBUS 310 A310221 3930310 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 NR 4 LT ARTICULATING SEAT TRACK IS CRACKED. REMOVED AND REPLACED LT NR 4 ARTICULATING SEAT TRACK PO NR 602215.2 REF FED EX A310-200 W/C E-6-5310-7-3322 PT2 SEAT AND DUMMY TRACKS ATTACHMENT FITTINGS INSPECTION. 2 L 7 2 4F RT A35EU 2008020600230 20080206 00230 EA 2008 2 6 MASA200800097 1 20080131 A 2120 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA COCKPIT ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 939FJ 15039 ASH FLT 2696 SDF-CLT - CAPTAIN REPORTED AN ODOR IN CABIN WHEN OPERATING NR 2 PACK. PERFORMED OPS CHECK AND NO DEFECTS F OUND. 2 L 7 2 4F RT A21EA 2008020600256 20080206 00256 NM 2008 2 6 UPS08M51525 1 20080117 A 5210 STRUCTURE DOUG MD11 MD11F 3023600 NM CREW DOOR LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 STRUCTURE ON LEFT CREW DOOR LOOSE. RE-ATTACHED SLIDE TO DOOR IAW 25-61-15-4. 2 L 7 3 4F RT A22WE 2008020600318 20080206 00318 NM 2008 2 6 2008UALA00392 1 20080123 A 2120 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN ODOR A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 651UA 25389 POSSIBLE ELECTRICAL ODOR FROM VENT IN AFT GALLEY LEFT SIDE. SAME ODOR REPORTED NEAR ROWS 5-6. REPLACED GEN CONTROL UN IT AS PER AMM 24 -22-02, ALSO INSP IDG WIRE BUNDLES, NO ABNORMALITIES OBSERVED& GALLEY FANS WORKING FINE. FOLLOWED SERV ICE TIP 21-00-00 FOR ODORS/ SMOKE IN THE CABIN & NO PROBS FOUND, ALSO APU BLEED AIR NOT IN USE WHEN FLT ATTENDANTS SMELL ED ODOR . COFFEEMAKERS WERE REMOVED FOR A COMPLETE CLEAN UP OF THE AFT GALLEY INCLUDING WARMING OVENS. SMC3 PROCEDURE FO LLOWED. THIS CONFIRMS NORMAL OPERATION OF THE A/C'S SYSTEMS. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020600332 20080206 00332 NM 2008 2 6 2008UALA00416 1 20080124 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 360 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FWD ENTRY DOOR CUTOUT BS 360 STRINGER CLIP AT STR 14L CRACKED AT ATTACH FASTENER LWR SIDE. MAJOR REPAIR: REPLACED STRIN GER 14L SPLICE CHANNEL AT STA 360. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600338 20080206 00338 NM 2008 2 6 HNAA0800038 1 20080125 A 3350 1317 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 942HA 48375 48375 163 INTERIOR EMERGENCY LIGHT INOP 2ND CEILING LIGHT AFT. REMOVED AND REPLACED BULB LIGHT OPS CHECK GOOD IAW M/M 33-51-00. 2 H 7 2 4T RT A13NM 2008020600341 20080206 00341 EA 2008 2 6 COMA0860055 1 20080109 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 931CA 7037 FLIGHT 5561 - FLAPS FAIL CAUTION MESSAGE AT 0 DEGREES. PERFORMED QRH, EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. COMP LIED WITH TASK CARD SI-2-27I001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 2008020600343 20080206 00343 EA 2008 2 6 COMA0860057 1 20080109 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 451CA 15355 7562 INTERCOSTAL ATTACH ANGLE CRACKED IN UPPER CORNER FS 484 RBL 27. REPLACED ANGLE IAW CRJ SRM 51-42-21. 2 L 7 2 4F RT A21EA 2008020600346 20080206 00346 EA 2008 2 6 COMA0870003 1 20080112 A 5240 PANEL CNDAIR CL600 CL6002C10 1390015 EA OPEN A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 669CA 10176 FLIGHT 5388 - EN ROUTE FROM PBI TO CVG, LOUD NOISE COMING FROM NOSE AREA. AIRCRAFT DIVERTED TO MCO AND LANDED SAFELY. FOUND AIRCRAFT SERVICE PANEL OPEN. RESECURED A/C PANEL IN SERVICEABLE CONDITION. 2 L 7 2 4F RT A21EA 2008020600347 20080206 00347 2008 2 6 2008UALA00436 4 20080125 A 2565 D31516113 SLIDE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE DOOR 1L FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 805UA 783 DOOR 1L SLIDE SHOWING INTERNAL CIDS FAULT. FOUND INTERNAL ELECTRICAL FAULT IN SLIDE 1L. REPLACED SLIDE ASSY, NO REPEATS . 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600365 20080206 00365 NM 2008 2 6 USAA920080247 1 20080123 A 5330 6545775 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FUSELAGE SKIN, BS 894, S25R. REPAIRED FUSELAGE SKIN, BS 894, S25R IAW B737 SRM 53-00-01-2R 31. 2 L 7 2 4F RT A16WE 2008020600372 20080206 00372 NM 2008 2 6 USAA920080254 1 20080124 A 5511 183N13055 SPAR BOEING 757 757225 1384959 NM HORIZ SATB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 MCN - MAJOR REPAIR - C11 CHECK - CORROSION ON RIGHT STABILIZER REAR SPAR, UPPER CHORD, STABILIZER STATION 318.949. REPL ACED RIGHT STABILIZER REAR SPAR, UPPER CHORD, STABILIZER STATION 318.949 IAW B757 51-40-02. 2 L 7 2 4F RT A2NM 2008020600373 20080206 00373 NM 2008 2 6 USAA920080262 1 20080109 A 5315 FLOORBEAM BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOORBEAM, BS 303, RBL 55, WL 200. REPAIRED CABIN FLOORBEAM, BS 303, RBL 55, WL 200 IAW B767 SRM 53-00-51 REPAIR 1 FIGURE 201. 2 L 7 2 4F RT A1NM 2008020700006 20080207 00006 NM 2008 2 7 ZZDA2008042 1 20080107 A 5320 STIFFENER BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 A/C STRUCK BY BAG CART. VERTICAL STIFFENERS 1 AT STA 1161 DAMAGED AT APPROX RBL 8 AND 1 AT APPROX RBL 18. INSTALLED 2 EACH VERTICAL STIFFENER AT STA 161, AT RBL 8 AND RBL 18 IAW B717 SRM 51-41-02, MATERIAL USED FROM S114-15595-12000. 2 L 7 2 4F TR A6WE 2008020700007 20080207 00007 NM 2008 2 7 ZZDA2008043 1 20080107 A 5313 LONGERON BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 A/C STRUCK BY BAG CART. LONGERON 25R DAMAGED BETWEEN STA 1145 TO 1178. INSTALLED NEW LONGERON 25R BETWEEN STATION 1145 AND STATION 1178 IAW B717 SRM 51-41-02. 2 L 7 2 4F TR A6WE 2008020700016 20080207 00016 NM 2008 2 7 SCNA08001 1 20080121 A 8011 35059459 STARTER BOEING 737 737800* NM NR 2 ENGINE FAILED A SCNA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 GL 15 PHHZI 8758 28380 CREW REPORTED, LOST OIL QUANTITY WHILE AT FL 400. ACCOMPLISHED NNC 7.15. MAINTENANCE REPORTED NR 2 ENGINE STARTER TURB INE FAILED. REPLACED NR 2 ENGINE STARTER & SERVICED TO FULL. PERFORMED ENGINE RUN AT THE GATE AND VERIFIED NO LEAKS. 2 L 7 2 4F RT A16WE 2008020700025 20080207 00025 NM 2008 2 7 HNAA0800041 1 20080121 A 3230 841005 PSEU DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A HNAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 07 914HA 37240 2879 53 AFTER TAKEOFF, WHEN THE LANDING GEAR WAS RETRACTED, THE CREW OBSERVED AMBER WARNING LIGHTS FOR BOTH RIGHT AND LEFT MAIN GEAR DOORS AND A RED UNSAFE INDICATION FOR THE NOSE GEAR. THE CREW THEN LOWERED THE GEAR AND LEFT IT IN THE DOWN POSITI ON FOR THE REMAINDER OF THE FLIGHT. THE FLIGHT THEN RETURNED TO THE FIELD AND DECLARED AN EMERGENCY WHERE CRASH RESCUE WAS DISPATCHED. THE AIRCRAFT THEN LANDED WITHOUT INCIDENT AND TAXIED NORMALLY. MAINTENANCE JACKED THE AIRCRAFT AND CYC LED THE LANDING GEAR WITHOUT DISCREPANCIES. THE PSEU WAS CHANGED AND SYSTEM WAS CYCLED SEVERAL MORE TIMES TO VERIFY SYS TEM OPERATION. NO FURTHER FAULTS WERE FOUND AND AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 2008020700030 20080207 00030 SO 2008 2 7 C2XA08CL013 1 20080127 A 7603 14535059401 CONTROL PANEL EMB 145 EMB145XR 3260214 SO COCKPIT STUCK A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 16112 14743 145660 EWR FLIGHT 2558 THE CREW REPORTED UNABLE TO SELECT CLIMB ON THE THRUST RATING PANEL. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE CLIMB BUTTON TO BE STUCK. REPLACED THE THRUST RATING PAN EL AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT 2008020700033 20080207 00033 EA 2008 2 7 COMA0860065 1 20080114 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 01 967CA 7134 FLIGHT 5516 - GEAR DISAGREE MESSAGE DISPLAYED UPON GEAR RETRACTION DURING TAKEOFF. NOSE GEAR REMAINED IN DOWN POSITION, MAINS SHOWED IN UP POSITION. FOLLOWED QRH, EMERGENCY DECLARED. AIRCRAFT RETURNED TO CVG AND LANDED SAFELY. ADJUSTED (S23) NLG STRUT EXTEND PROX SENSOR. 2 L 7 2 4F RT A21EA 2008020700038 20080207 00038 NM 2008 2 7 2008UALA00094 1 20080106 A 3040 6240663 CONTROLLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WINDOW HEAT FAILED A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 552UA 26641 FWD RIGHT WINDOW EXTREMELY COLD DURING FLIGHT. RIGHT FWD HEAT INDICATES NORMAL. WINDOW FROZE UP ON FINAL. WINDOW HEAT CONTROLLER FAILURE. REPLACED RT WINDOW HEAT CONTROLLER, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020700041 20080207 00041 NM 2008 2 7 2008UALA00407 1 20080122 A 2560 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FLASHLIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 534UA 25129 FLASHLIGHT DOOR 2L INOPERATIVE. FOUND FAULTY BATTERY. REPLACED ENTIRE FLASHLIGHT ASSY, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020700042 20080207 00042 NM 2008 2 7 2008UALA00414 1 20080124 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FUSELAGE LOWER HINGE CUTOUT AT FWD GALLEY DOOR HAS ONE FASTENER HOLE WITH CRACK INDICATIONS AT LOWER FWD CORNER OF THE C UTOUT. MAJOR REPAIR: REMOVED DAMAGE. INSTALLED STRUCTURAL FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700044 20080207 00044 NM 2008 2 7 2008UALA00417 1 20080124 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 294 S11L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 INTERCOSTAL AT BS 294.5 IS CRACKED AT STR 11L AT FRAME ATTACH ANGLE. REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700048 20080207 00048 NM 2008 2 7 2008UALA00421 1 20080124 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 294 S7-8L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 CRACKS WERE FOUND AT BS 294.5 INTERCOSTAL WEB STRINGER S-7L AND S-8L. MAJOR REPAIR: REMOVED AND REPLACED INTERCOSTAL W EBS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700052 20080207 00052 NM 2008 2 7 2008UALA00427 1 20080124 A 5340 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 294-303 S10L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 INTERCOSTAL BETWEEN BS 294.5 & 303 ABOVE STRINGER 10L HAS OUTER & FWD ATTACH ANGLES CRACKED. MAJOR REPAIR: REPLACED INT ERCOSTAL AND INSTALLED FRAME DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700057 20080207 00057 NM 2008 2 7 2008UALA00439 1 20080126 A 3350 D9239003500060 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMEGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 805UA 783 AFTER REPLACEMENT OF DOOR 2R SLIDE, ACFT FAILS THE EMERGENCY SYSTEM TEST WITH ERROR (EPSU UNIT EMER LT, 33-51-38). FOUN D EPSU FAILED. REPLACED EPSU (LT) OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020700058 20080207 00058 NM 2008 2 7 2008UALA00441 1 20080125 A 5522 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LT ELEVATOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 849UA 1649 LEFT ELEVATOR LOWER SKIN DENT REPAIR LOCATED 6 INCHES OUTBOARD OF ER5 AND 4 INCH AFT OF FWD SPAR REQUIRES VISUAL INSPECT ION OF TAPE SECURITY AND TAP TEST OF AREA BEYOND THE 6 X 6 REPAIR AREA. TEMP REPAIR REMOVED AND PERMANENT REPAIR INSTAL LED AS A MAJOR REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020700064 20080207 00064 NM 2008 2 7 2008UALA00450 1 20080126 A 5320 ATTACH FITTING BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU BS 360 S8L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 902UA 25002 INTERCOSTAL ATTACH FITTING CRACKED AT STA 360, STR 8L. MAJOR REPAIR: REPLACED INTERCOSTAL ATTACH FITTING. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700066 20080207 00066 2008 2 7 2008UALA00458 4 20080125 A 2565 INSERT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EVAC SLIDE DISLODGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 671UA 30026 RIGHT OVERWING SLIDE COMPARTMENT SLIDE PACK INFLATION HOSE CLAMP INSERT HAS COME OUT. LOCATED ON BACKSIDE OF SLIDE TRAY . REPLACED SLIDE. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020700067 20080207 00067 NM 2008 2 7 2008UALA00463 1 20080127 A 3510 LINE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW O2 LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 377UA 24642 CREW O2 PRESSURE IS GOING DOWN RAPIDLY. FOUND CAPTAINS O2 MASK STORAGE BOX SUPPLY LINE LEAKING. REPLACED THE SUPPLY LI NE, STORAGE BOX, AND MASK. NO FAULT FOUND. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020100131 20080201 00131 NM 2008 2 1 08FDEA00304 1 20080128 A 5311 AFA00293 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 523FE 48479 MAIN DECK CARGO: LT FRAME AT STA 1721, L12-13 FOUND WITH DENT. REPAIR CARRIED OUT AT MAIN DECK CARGO: LT FRAME AT BS 17 21, L12-L13 AS PER SRM 53- 30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008020100133 20080201 00133 EU 2008 2 1 08FDEA00306 1 20080128 A 5752 A579600000003 RIB AIRBUS 300 A300B4605R 3930308 EU T/E FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND ON RT INNER FLAP LOWER SKIN RIB 18-19 AN OLD DOUBLER REPAIR WITHOUT ANY DOCUMENTATION DOUBLER REPAIR RENEWED IAW R AS/FOK/006 2008 ISS A, APPROVED BY EA 6-5752-114854. 2 L 7 2 4F RT A35EU 2008020100134 20080201 00134 EU 2008 2 1 08FDEA00307 1 20080128 A 5320 A53810967 DIAPHRAGM AIRBUS 300 A300B4605R 3930308 EU FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND DENTS IN PRESSURE DIAPHRAGM AT TRACK 3-5,C48-54 LT AND TRACK 4-5, C51-53 RT REPAIR PERFORMED BY NDT-INSPECTION FOR CRACK FREE CONDITION AND LET THE DENTS AS IT IS IAW RAS 057541/004/2008 ISS A AND EA 6-5315-114877. 2 L 7 2 4F RT A35EU 2008013100162 20080131 00162 NM 2008 1 31 SWAA080480 1 20080127 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 27 TO STR 26L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008013100168 20080131 00168 NM 2008 1 31 SWAA080475 1 20080127 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, RBL 10. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008013100175 20080131 00175 NM 2008 1 31 SWAA080464 1 20080127 A 5311 65C22909 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008013100234 20080131 00234 NM 2008 1 31 USAA920080191 1 20080115 A 5313 STRINGER SPLICE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 444US 24862 CLT - MAJOR REPAIR - FPBH INSPECTION - CRACKED STRINGER SPLICE, BS 360, S15L. REPLACED STRINGER SPICE, BS 360, S15L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008013100333 20080131 00333 NM 2008 1 31 DL757080097 1 20080120 A 2121 216001033 FAN BOEING 757 757232 1384965 NM LEFT ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 652DL 24392 ODOR IN AREA 2C/D 3C/D AND ODOR STOPPED WHEN RECIRC FANS OFF CAME BACK WHEN TURNED ON. ALSO ODOR IN ROW 24 AREA. REMOV ED AND REPLACED LT RECIRC FAN IAW MM. 2 L 7 2 4F RT A2NM 2008020100036 20080201 00036 NM 2008 2 1 CALA0800043 1 20080119 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 CRACKED FRAME BETWEEN STRINGER 8R AND 9R AT STATION 400. INSTALLED REPAIR ANGLES ON FRAME PER ECRA 5310-04691. 2 L 7 2 4F RT A16WE 2008020100046 20080201 00046 NM 2008 2 1 CALA0800055 1 20080110 A 5320 654587512 ATTACH ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76354 23592 R1 DOOR SILL AREA THRESHOLD ATTACH ANGLE CORRODED. REMOVED CORROSION IAW 51-10-2, FOUND OUT OF LIMITS IAW SRM 53-10-15. REMOVED AND REPLACED ANGLE IAW SRM 51-40-2. 2 L 7 2 4F RT A16WE 2008020100116 20080201 00116 WP 2008 2 1 08FDEA00284 1 20080125 A 5310 ACA72251 DOOR FRAME DOUG MD10 MD1010F 3022112 WP BS 692 S27L CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 NR 4 MCD LOWER JAMB SUPPORT FITTING HOLES A, B, C AND D HAS CRACK INDICATIONS FOUND WITH BHEC (SEE ATTACHED DRAWING). I NSTALLED REPAIR BUSHINGS IN REFERENCE WITH DC/MD10-10 SRM VOLUME I, 53-50-00 PAGE 81 FIG 17 AT HOLE LOCATIONS A, B, C AN D D TO CARGO DOOR JAMB BEAM ONLY. LOWER FITTING WAS REPLACED ON NON-ROUTINE N00950. MAJOR REPAIR 2 L 7 3 4F RT A22WE 2008020100119 20080201 00119 WP 2008 2 1 08FDEA00287 1 20080126 A 5347 S4929405 SEAT TRACK DOUG DC10 DC1030F 3023504 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MAIN CABIN SEAT TRACK BETWEEN STA 1019 TO 1039 AT APPROX RBL - 48 IS CORRODED AND CRACKED. REMOVED AND REPLACED SEAT TR ACK FROM STA 949 TO STA 1049 RBL48 IAW MD/DC10 -10 SRM 51-40-02 VOL II. 2 L 7 3 4F RT A22WE 2008020100173 20080201 00173 NM 2008 2 1 QXEA200800046 1 20080128 A 2131 92146A010401 CONTROLLER BOMBDR DHC8 DHC8402 1390042 NM CABIN PRESSURE FAILED A QXEA K NONE O OTHER CL CLIMB 1 NM 09 402QX 4032 GEG FLIGHT 2347 ON CLIMB-OUT AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR MANUAL MODE. DIVERTED TO GEG FOR MAINTENANCE. MA INTENANCE INTEROGATED CDS NOTED CP CONTROLLER FAIL AND CPC/ADU ARINC FAIL. REPLACED CPC. GROUND RUN OPS CHECKS GOOD, A IRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008043000025 20080430 00025 NM 2008 4 30 ASAA0872842 1 20080406 A 5321 146A94014 TEE FITTING BOEING 737 737790 13844CN NM FLOOR PANEL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 609AS 29752 AFT CARGO BS 767+S FLOOR PANEL "T" SPLICE CORRODED COLLISION ON TEE ASSY IN AFT CARGO BS 767+5 BLENDED OUT BEYOND LIMITS . REPLACED WITH REPAIR PART IAW B737 700 SRM 53 60 53. 2 L 7 2 4F RT A16WE 2008020100185 20080201 00185 EU 2008 2 1 08FDEA00316 1 20080128 A 5514 A5517860720200 BRACKET AIRBUS 310 A310221 3930310 EU HORIZ STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 THS LEFT LOWER BODY FAIRING FWD ATTACH BRACKET ANGLE CORRODED LOWER SURFACE, CENTER BOX AREA, ANGLE IS PART OF LEADING EDGE. REMOVED AND REINSTALLED LOWER APRON IAW A310-200 SRM 51-40-21. REMOVED AND REINSTALLED RIB ASSY IAW A310-200 SRM 51-40-21. REMOVED LOWER ATTACH PLATE IAW A310-200 SRM 51-40-21. REMOVED CORROSION ORIGINAL THICKNESS .252 REMOVAL .060 REMAINING THICKNESS .192. FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 55-12-28 (NO REPAIR AUTHORIZED). RECEIVED NEW PART P/N A5517860720200 P/O 604456.1. INSTALLED NEW BRACKET IAW A310-200 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008020700074 20080207 00074 NM 2008 2 7 2008UALA00480 1 20080127 A 2721 658D1005 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RUDDER TRIM INTERMITTENT A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 655UA 25393 RUDDER TRIM INTERMITTENTLY INOP. SUSPECT FAULTY TRIM ACTUATOR. REPLACED RUDDER TRIM ACTUATOR. OP CHECKS NORMAL. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020700079 20080207 00079 EA 2008 2 7 COMA0860072 1 20080116 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA RT T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 675BR 9958 7635 FLIGHT 4940 - FLAPS FAILED AT 0 DEGREES ON APPROACH TO YUL. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND RE PLACED RIGHT I/B FLAP O/B ACTUATOR. 2 L 7 2 4F RT A21EA 2008020700082 20080207 00082 EA 2008 2 7 COMA0860075 1 20080117 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 629BR 8443 7251 FLIGHT 5653 - RECEIVED CONFIG SPOILERS WARNING MESSAGE. ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. REPLACE D RIGHT SECU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008020700084 20080207 00084 EA 2008 2 7 COMA0860077 1 20080117 A 3020 5399001 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 1900309 EA LT NACELLE FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 999CA 8202 7230 FLIGHT 4984 - RECEIVED LEFT COWL ANTI-ICE MESSAGE. PERFORMED QRH, RETURNED TO CVG, LANDED WITHOUT INCIDENT. LEFT PRESS RELIEVE VALVE OBSERVED EXTENDED DURING POST FLIGHT. REPLACED LEFT COWL ANTI-ICE VALVE AND RESET LEFT ENGINE PRESS RELI EVE VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008020700085 20080207 00085 NM 2008 2 7 HNAA0800054 1 20080128 A 7712 SEL0C2N INDICATOR DHAV DHC8 DHC8102 2809003 NM TORQUE FAILED A HNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 07 935HA 19278 1164 142 DURING TAKEOFF ROLL, NR 2 TORQUE INDICATOR DROPPED TO ZERO. SPEED WAS LESS THAT 40 KNOTS. CIRCUIT BREAKERS J5 & K5 (TQ IND & COND) WERE CYCLED AND AIRCRAFT WAS RUN UP. CHECKS WERE GOOD AND AIRCRAFT RELEASED FOR FLIGHT. UPON ARRIVAL AT A MAINTENANCE BASE, THE NR 2 TORQUE INDICATOR WAS REPLACED AND THE CONNECTOR AT THE ENGINE WERE CLEANED. CHECKS WERE GOO D AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 2008020700088 20080207 00088 WP 2008 2 7 MWEA080016 1 20080128 A 5320 SR095200089 SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 810ME 48072 CORROSION AROUND BOLT HOLE ALONG ENTIRE LENGTH OF AFT CARGO DOOR THRESHOLD PLATE SUPPORT STRUCTURE. FABRICATED AND INST ALLED SPACERS. 2 L 7 2 4F A6WE 2008020700090 20080207 00090 EA 2008 2 7 COMA0860081 1 20080118 A 2752 853D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SO 01 685BR 9764 7712 FLIGHT 5696 - FLAPS FAILED ON TAKEOFF UPON RETRACTION, FAILED AT 18 DEGREES. AIRCRAFT RETURNED TO DSM AND LANDED SAFELY . REMOVED AND REPLACED LEFT O/B FLAP I/B ACTUATOR. 2 L 7 2 4F RT A21EA 2008020700096 20080207 00096 EA 2008 2 7 COMA0860087 1 20080118 A 2752 853D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA LT T/E FLAP FAULTY A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 926CA 11953 7027 FLIGHT 5094 - FLAPS FAILED AT 0 DEGREES WHEN SELECTED TO 8 DEGREES ON APPROACH. EMERGENCY DECLARED. A/C LANDED SAFELY. REMOVED AND REPLACED LEFT O/B FLAP I/B ACTUATOR. 2 L 7 2 4F RT A21EA 2008020700098 20080207 00098 EA 2008 2 7 COMA0860089 1 20080119 A 2760 270007 PCU CNDAIR CL600 CL6002B19 1900309 EA SPOILER SYSTEM FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 629BR 20155 7251 FLIGHT 5661 - ON TAKEOFF ROLL RECEIVED TAKEOFF CONFIG SPOILER WARNING. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT FLIG HT SPOILER O/B PCU. 2 L 7 2 4F RT A21EA 2008020700099 20080207 00099 EA 2008 2 7 COMA0860090 1 20080120 A 2752 854D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA RT T/E FLAP FAULTY A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SO 01 915CA 11099 7013 FLIGHT 5348 - FLAPS FAILED ON FINAL WHEN SET TO 20 DEGREES. EMERGENCY DECLARED. A/C LANDED SAFELY. REMOVED AND REPLAC ED O/B FLAP O/B ACTUATOR. 2 L 7 2 4F RT A21EA 2008020700103 20080207 00103 EA 2008 2 7 COMA0860093 1 20080121 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 821CA 7420 FLIGHT 5294 - FLAPS FAIL CAUTION MESSAGE ON APPROACH. FLAPS FAILED AT 0 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED S AFELY. COMPLIED WITH TASK CARD SI-2-27I0001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 2008020700106 20080207 00106 EA 2008 2 7 COMA0860096 1 20080123 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 917CA 7017 FLIGHT 5620 - RECEIVED FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH TASK CARD SI-2-27I0001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 2008020700109 20080207 00109 NM 2008 2 7 ZZDA2008061 1 20080114 A 5320 STIFFENER BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 VERTICAL STIFFENER CRACKED 21" LBL 21 AND NR 5 O/B AT STA 218. INSTALLED FORMED CHANNEL REPAIR ON VERTICAL STIFFENER AT LBL 21" AND NR 5 FROM O/B AT STA 218 IAW B717 SRM 51-70-11 FIG 201. MATERIAL USED 7075-0 .063, HEAT TREATED TO 7075.T6 PER B717 SRM 51-32-01, FILLER 8" X 1" X 1" X 2.5", ANGLE 19" X 2" EACH. 2 L 7 2 4F TR A6WE 2008020600092 20080206 00092 NM 2008 2 6 PIDA08008 1 20080204 A 3350 20131A BATTERY PACK BOEING 737 737228 13844AG NM EMERGENCY LIGHTS INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 251TR 23792 AFT EMERGENCY EXIT LIGHTS OUT. REPLACED LEFT EMERGENCY EXIT BATTERY PACK. OPS CHECK GOOD PER MM 33-51-31. 2 L 7 2 4F RT A16WE 2008020600095 20080206 00095 WP 2008 2 6 ABXA080024 1 20080107 A 5310 99578607 ANGLE DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 COCKPIT WINDOW SILL LEFT ANGLE CRACKED. REMOVED, REPAIRED, AND REINSTALLED ANGLE IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2008020600098 20080206 00098 NM 2008 2 6 ABXA080022 1 20080118 A 2530 OVEN BOEING 767 767232 1385132 NM GALLEY SHORTED A ABXA O OTHER A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 744AX 21 070741518 22221 MICROWAVE SHORTED OUT WHEN IN USE. TOP RIGHT BACK SIDE SPARKED AND FIRE CAME OUT. CIRCUIT BREAKERS PULLED FOR GALLEY. REMOVED AND REPLACED MICROWAVE. OPS CHECKED GOOD IAW B767 MM 25-31-00. 2 L 7 2 4F RT A1NM 2008020600099 20080206 00099 NM 2008 2 6 USAA920080195 1 20080118 A 5322 SHEAR TIE BOEING 737 7373B7 1384580 NM BS 986 S27L/R CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 527AU 23862 CLT - MAJOR REPAIR - RON - CORROSION ON SHEAR TIE, BS 986, S27L - S27R. REPAIRED SHEAR TIE, BS S27L - S27R IAW B737 SRM 53-00-07. 2 L 7 2 4F RT A16WE 2008020600133 20080206 00133 EA 2008 2 6 MASA200800072 1 20080128 A 3350 AE20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 931LR 15031 ASH 2908 PHX - ALL FORWARD EMERGENCY FLOOD LIGHTS INOP. MX REPLACED THE NR 1 BATTERY PACK. 2 L 7 2 4F RT A21EA 2008020600144 20080206 00144 WP 2008 2 6 UPS08851499 1 20080109 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 COCKPIT FLOOR PANEL 676F 6 EA HAT CHANNELS ARE WORN, DAMAGED AND SKIN HAS ENLONGATED SCREW HOLES. RE PAIRED COCKPIT FLOOR PNL 676F IAW SRM 51-01-21, SRM 53-07-00 FIG 049B SHT 1, SRM 51-01-24 AND SRM 51-01-08. 2 L 7 4 4F RT 4A25 2008020600172 20080206 00172 NM 2008 2 6 2008UALA00330 1 20080120 A 5753 SUPPORT FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE T/E FLAP FAIRING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 RIGHT WING OUTBOARD FLAP FAIRING, SUPPORT FITTING CRACKED, LOCATED INBOARD OF AILERON. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600175 20080206 00175 WP 2008 2 6 UPS08851505 1 20080105 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 F/O'S AFT INBD SEAT TRACK LOCK PIN HOLES ARE ELONGATED. REMOVED AND REPLACED F/O'S INBD SEAT TRACK I AW EO DC8-5340-18315-B. 2 L 7 4 4F RT 4A25 2008020600177 20080206 00177 WP 2008 2 6 UPS08851507 1 20080105 A 5347 3657502U507 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 CAPT, AFT INBD SEAT TRACK LOCK PIN HOLES ARE WORN. REMOVED AND REPLACED CAPT AFT INBD SEAT TRACK IAW EO DC8-5340-18315 -B. 2 L 7 4 4F RT 4A25 2008020600179 20080206 00179 WP 2008 2 6 UPS08851524 1 20080121 A 5755 SKIN DOUG DC8 DC873F 302199F WP LT WING SPOILER CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 LEFT WING INBOARD LATERAL CONTROL SPOILER LOWER SURFACE IS CHAFFED ALONG T/E. INSTALLED NEW SPOILER ASSEMBLY IAW DC8 AM M 27-61-01-2, PARAGRAPH 3B STEPS 1 THROUGH 6. 2 L 7 4 4F RT 4A25 2008020600180 20080206 00180 NM 2008 2 6 2008UALA00331 1 20080120 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 AFT PIT AT STA 1440 STR 26L, FRAME HAS DENT. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600181 20080206 00181 WP 2008 2 6 UPS08851516 1 20080105 A 5347 36575031 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 COCKPIT STA -52 SEAT TRACK IS WORN AND LOCK PIN HOLES ARE ELONGATED. REMOVED AND REPLACED F/E'S FWD SEAT TRACK AT STA -52 IAW SRM 51-03-00, AND DC8 AMM 25-11-02-0 FIG 002. 2 L 7 4 4F RT 4A25 2008020600190 20080206 00190 WP 2008 2 6 UPS08851532 1 20080109 A 5311 FRAME DOUG DC8 DC871F 302199D WP FS 1100 L33R DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 DOUBLE DRILLED HOLES IN GUSSET AT STA 1100 FRAME L33R. REMOVED GUSSET AT STA 1100 L33R IAW SRM 51-01 -21D. FABRICATED AND INSTALLED REPAIR GUSSET IAW DWG 9754949, AND SRM 51-01-21D. 2 L 7 4 4F RT 4A25 2008020600202 20080206 00202 NM 2008 2 6 ASAA0852488 1 20080118 A 2150 A/C PACK BOEING 737 737890 1384527 NM A/C BAY MALFUNCTIONED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 549AS 30824 SETTING LEFTHAND AIRCON PACK TO HIGH FLOW CAUSES GENERATOR LOAD REDUCTION. TESTED, COULD NOT DUPLICATE. 2 L 7 2 4F RT A16WE 2008020600226 20080206 00226 WP 2008 2 6 UPS08851533 1 20080105 A 5730 DOUBLER DOUG DC8 DC871F 302199D WP RWS 467 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 R/WING, OUTBD STUB WING HAS DOUBLER AT LWR SURFACE WITH 2" CRACK. REMOVED CRACK DOUBLER AT R/WING OU TBD STUB WING IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPAIR DOUBLER ON R/WING OUTBD STUB WING STA XW 467.000 IAW SR M 57-02-01A-0 FIG 001. 2 L 7 4 4F RT 4A25 2008020600246 20080206 00246 NM 2008 2 6 USAA920080219 1 20080112 A 5320 69489856 FITTING BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED L1 DOOR CUTOUT INTERCOSTAL CLIP, BS 360, S11L. REPLACED L1 DOOR CUTOUT INTERC OSTAL CLIP, BS 360, S11L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600252 20080206 00252 NM 2008 2 6 USAA920080226 1 20080112 A 5340 693535214 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER TIE CLIP, BS 639, S2R. REPLACED STRINGER TIE CLIP, BS 639, S2R IAW B7 37 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600261 20080206 00261 NM 2008 2 6 USAA920080231 1 20080104 A 5322 140N20021150 SHEAR TIE BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 MCN - MAJOR REPAIR - C11 CHECK - CORROSION ON SHEAR TIE, BS 880, BL 0, WL 154. REPLACED SHEAR TIE, BS 880, BL 0, WL 154 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008020600294 20080206 00294 EU 2008 2 6 2008UALA00288 1 20080116 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 415UA 475 EMERGENCY LIGHTS FAIL TEST SHOW BATTERY AFT LEFT. LOOSE CONNECTOR. RESEATED CONNECTOR. LIGHTS TESTED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600296 20080206 00296 NM 2008 2 6 2008UALA00351 1 20080121 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU BS 986 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 AFT CABIN FLOORBEAM TEE CAP UPPER SURFACE CORRODED BS 986 LBL 46 - 48, 2 EA MISDRILL MARKS ON BOTH SIDES OF REPAIR FILLE R. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED NESTED ANGLE STRAP AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600298 20080206 00298 NM 2008 2 6 2008UALA00353 1 20080121 A 5514 FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 RIGHT HORIZ STAB CENTER SECTION, AFT FACE OF THE AFT LUG IS CORRODED ON THE AFT SPAR UPPER ATTACH CLEVIS. MAJOR REPAIR: REMOVED CORROSION. INSTALLED OVERSIZED BUSHING. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600301 20080206 00301 NM 2008 2 6 2008UALA00364 1 20080122 A 5330 146T3530 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 65357 27112 ON ARRIVAL FOUND SKIN DAMAGE AFT OF REAR CARGO DOOR. SUSPECT AC DAMAGE FROM GROUND EQUIPMENT. CUT-OUT DAMAGE TO EXTERN AL FUSELAGE AND FABRICATED REPAIR DOUBLERS AND FILLERS AND INSTALLED PER SRM 53-00-01, FIG. 201.REMOVED CRACK SHEAR 8562 5 TIE AND FABRICATED A NEW -818 SHEAR TIE PER BAC DWG 140T2103 AND INSTALLED PER SRM 51-40-2. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020600308 20080206 00308 NM 2008 2 6 2008UALA00375 1 20080122 A 5230 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 AFT CARGO DOOR LOWER AFT CORNER FRAME IS CRACKED AT STOP FITTING. FABRICATED AND INSTALLED FRAME REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600315 20080206 00315 NE 2008 2 6 2008UALA00384 2 20080121 A 7300 MR73236 ALTERNATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ENGINE MALFUNCTIONED A UALA K NONE J WARNING INDICATION DE DESCENT 1 WP 29 651UA 10714 25389 L ENG CONTROL EICAS ON DESCENT, CAME ON RIGHT AFTER TURNING OFF ENG ANTI ICE. REPLACED THE PERMANENT MAGNET ALTERNATO R FOR THE NR 1 ENGINE EEC. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020600321 20080206 00321 NM 2008 2 6 2008UALA00395 1 20080123 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 AFT PIT AT STA 1600, APPROX STR 26L, FRAME DENTED ON INBOARD FLANGE. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600329 20080206 00329 NM 2008 2 6 HNAA0800033 1 20080121 A 3242 21565 BRAKE ASSY DHAV DHC8 DHC8102 2809003 NM MLG DEFECTIVE A HNAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 934HA 2318 283 139 WHILE TAXING TO RUNWAY 36L, ANOTHER AIRCRAFT CREW SAID THE LEFT BREAKS WERE GLOWING RED. PULLED AIRCRAFT OFF TAXIWAY TO INSPECT. THE FIRST OFFICER NOTED SMOKE COMING FROM WHEEL ASSEMBLY, EVACUATED AIRCRAFT. REMOVED NR 1 AND NR 2 WHEEL AN D BRAKE ASSEMBLIES. INSPECED SRUT AND AXLE, NO DEFECTS NOTED. INSTALLED NEW BRAKE, WHEEL ASSEMBLIES AND FLEXIBLE BRAKE LINES. LEAK AND OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2008020600342 20080206 00342 EA 2008 2 6 COMA0860056 1 20080109 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 451CA 15355 7562 INBOARD BRACKET AT FS 280 RBL 9 CRACKED. REPLACED INBOARD BRACKET IAW CRJ SRM 51-42-21. 2 L 7 2 4F RT A21EA 2008020600362 20080206 00362 EA 2008 2 6 TRAX200800126 1 20080121 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A ASOA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 861AS 7445 DOOR WILL NOT CLOSE/LOCK, INDICATES AMBER PAX OUTER HANDLE CAUTION MSG. 2 L 7 2 4F RT A21EA 2008020700004 20080207 00004 NM 2008 2 7 ZZDA2008040 1 20080107 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 A/C STRUCK BY BAG CART. SKIN DAMAGED BETWEEN CANTED FRAME 1145.009 AND 1178. INSTALLED SKIN REPAIR AT CANTED FRAME FRO M STA 1145 TO STA 1178 IAW B717 SRM 51-41-02 AND DRG 9911840 AND AIRTRAN EA17-53-00939A DATED 01/21/08. MATERIAL USED 7 075 T6 .040. 2 L 7 2 4F TR A6WE 2008020700043 20080207 00043 NM 2008 2 7 2008UALA00415 1 20080124 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 UPPER FUSELAGE HINGE CUTOUT AT FWD ENTRY DOOR HAS TWO FASTENER HOLES WITH CRACK INDICATIONS. ONE ABOVE AND ONE BELOW FW D END OF THE CUTOUT. REMOVED DAMAGE. INSTALLED STRUCTURAL FILLER AND A DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700075 20080207 00075 NM 2008 2 7 MWEA080018 1 20080128 A 2560 P4010021 BATTERY BOEING 717 717200 1383700 NM FLASHLIGHT DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 925ME 55191 FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FORWARD EMERGENCY FLASHLIGHT BATTERY. 2 L 7 2 4F TR A6WE 2008020700081 20080207 00081 EA 2008 2 7 COMA0860074 1 20080117 A 7603 1603730007 THROTTLE CABLE CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE BROKEN A COMA L ABORTED APPROACH O OTHER AP APPROACH 1 SO 01 954CA 7100 FLIGHT 5175 - LEFT ENGINE WOULD NOT RESPOND WHEN POWER LEVER BROUGHT TO IDLE. ABORTED APPROACH, PERFORMED IFSD, DECLARE D EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED "S" CABLE ON LEFT ENGINE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008041800088 20080418 00088 EU 2008 4 18 USAA920080778 1 20080326 A 5320 D53347217220390 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 187US 1704 PIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 3950 / FR 68 - BS 4059 / FR 70, -Y1050 TO - Y1162. REPLACED CABIN FLOOR SUPPORT, BS 3950 / FR 68 - BS 4059 / FR 70, -Y1050 TO -Y1162 IAW A321 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008020100190 20080201 00190 SO 2008 2 1 SIMA200803001 1 20080127 A 2913 MPEV0086 PUMP EMB 135 EMB135KL 3260302 SO HYDRAULIC SYS FAILED A SIMA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 837AE 145647 ON FLIGHT 4376, CREW REPORTED RECEIVED HYDRAULIC 2 LOW QUALITY, SOON FOLLOWED BY HYDRAULIC 2 FAIL MESSAGE. CREW DECLARED EMERGENCY GOING INTO ORD. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER 2 EDMP. REMOVED AND REPLACED NU MBER 2 HYDRAULIC SYSTEM PRESSURE HYDRAULIC LINE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008020400006 20080204 00006 SO 2008 2 4 CHQA200800016 1 20080128 A 2750 3631001011 FCU EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL TE FLAPS MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 275SK 17004 145345 CAE312704 PNS TO IAH - DURING CLIMB AT APPROXIMATELY 12,000 FEET, THE FLIGHT CREW RECEIVED A FLAP FAIL EICAS MESSAGE. THE QRH WAS FOLLOWED AND THE FLIGHT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE CMC FOR FAULT CODES AND REPORTED AN FECU FAIL CODE. THE FECU WAS CHANGED AND THE FLAP SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008020400007 20080204 00007 SO 2008 2 4 FDKA200801040 1 20080128 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6059 TLH-MIA (0400 PHX LCL) - ROW 12 FWD OVERHEAD EMERGENCY LIGHT INOP. MX RESET EMERGENCY LIGHT SYSTEM, OPS CK GOO D. 2 L 7 2 4T RT T00011AT 2008020400010 20080204 00010 SO 2008 2 4 FDKA200801042 1 20080129 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6096 MCO (0738 PHX LCL) - EMERGENCY EXIT SIGN IN GALLEY WILL NOT ILLUMINATE. MX RESECURED CONNECTOR ON SIGN, OPS CH ECKED GOOD. 2 L 7 2 4T RT T00011AT 2008020400013 20080204 00013 NM 2008 2 4 NWAA080286311 1 20080129 A 3040 CONTROL UNIT BOEING 747 747451 1384940 NM WINDSHIELD HEAT MALFUNCTIONED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 671US 26477 DURING CLIMB-OUT, SMOKE BEGAN POURING OUT OF THE FIRST OFFICER FRONT WINDSHIELD AREA. PERFORMED FIRE/SMOKE CHECKLIST, R ETURNED TO MNL AND LANDING WAS UNEVENTFUL. AFTER LANDING FLIGHT ATTENDANT REPORTED SMELLING SMOKE AT DOOR 3 LEFT. MAIN TENANCE REMOVED AND REPLACED COCKPIT WINDOW AND WINDOW HEAT CONTROL UNIT. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RET URNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008020400015 20080204 00015 NM 2008 2 4 AALA200800033 1 20080105 A 3350 SIGN BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 964AN 30093 DFW - EMERGENCY EXIT LIGHT IDENTIFIER AT AFT RIGHT NUMBER FOUR DOOR MISSING. REPLACED IDENTIFIER FOR EMERGENCY EXIT LIG HT AT AFT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008020400017 20080204 00017 WP 2008 2 4 AALA200800034 1 20080105 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 293AA 49305 LGA - EMERGENCY LIGHT AT OVERHEAD AFT LAVATORY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD AFT LAVATORY . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020400018 20080204 00018 NM 2008 2 4 AALA200800035 1 20080105 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 757AN 32636 DFW - EMERGENCY LIGHT AT SEAT 22G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008020400036 20080204 00036 NM 2008 2 4 AALA200800025 1 20080104 A 2750 18173812 TRANSMITTER BOEING 737 737823 13844BZ NM TE FLAPS INOPERATIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 960AN 29542 IAD INFLIGHT T144/04JAN, ON APPROACH FLAPS WOULD NOT EXTEND. ACCOMPLISHED EMERGENCY EXTENSION OF FLAPS. LANDED IAD WIT HOUT INCIDENT. REPLACED LEFT TRAILING EDGE FLAP TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008020400037 20080204 00037 WP 2008 2 4 AALA200800027 1 20080104 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 481AA 49656 LGA - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABI N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020400040 20080204 00040 NM 2008 2 4 08FDEA00322 1 20080129 A 2612 10608776 POWER UNIT BOEING 727 727233 138408A NM APU FIRE DETECT MALFUNCTIONED A FDEA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SO 25 254FE 20936 SHORTLY AFTER TAKEOFF LIGHT IN APU FIRE HANDLE FLICKERED FOR SEVERAL MINUTES, FOLLOWED BY A STEADY LIGHT. NO OTHER FIRE INDICATIONS WERE NOTED. APU FIRE HANDLE PULLED, BOTTLE BLOWN. REMOVED AND REPLACED OPERATING POWER UNIT FOR APU FIRE DETECTION IAW B727-200 MM CH 26-15-003-4. FIRE TEST NOW CHECKS NORMAL. 2 L 7 3 4F RT A3WE 2008020400066 20080204 00066 SO 2008 2 4 SWIA200819141 1 20080124 A 5210 MECHANISM EMB 120 EMB120ER 3260203 SO PAX DOOR HANDLE BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 576SW 120345 PAX DOOR HANDLE WILL NOT LOCK AND STOW. LUBED HANDLE LOCKING MECHANISM, OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008020400071 20080204 00071 SO 2008 2 4 SWIA200819146 1 20080128 A 2497 CONTACTOR EMB 120 EMB120ER 3260203 SO UNKNOWN BURNED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 07 561SW 120335 ELECTRICAL ODOR COMING FROM FLIGHT DECK, FLIGHT NR 5539. REPLACED CONTACTOR K0519 WITH SERVICEABLE UNIT. OPS CHECKED G OOD. 2 L 7 2 4T RT A31SO 2008020400076 20080204 00076 NM 2008 2 4 AALA200800055 1 20080112 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 781AN 29586 DFW - EMERGENCY LIGHT AT SEAT 26C MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008020400078 20080204 00078 WP 2008 2 4 AALA200800057 1 20080112 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 583AA 53160 LGA - EMERGENCY LIGHT AT SEAT ROW 25DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 25DEF. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020400080 20080204 00080 NM 2008 2 4 AALA200800066 1 20080114 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 671AA 25336 DFW - EMERGENCY LIGHTS AT SEAT ROWS 16 TO 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 16 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020400082 20080204 00082 NM 2008 2 4 AALA200800068 1 20080111 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 978AN 30100 TUL - EMERGENCY SEAT MOUNTED LIGHTS AT SEAT ROWS 7 TO 11 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY SEAT MOUNTED LIGHTS AT SEAT ROWS 7 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008020400084 20080204 00084 NM 2008 2 4 AALA200800064 1 20080114 A 3350 P4010049 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 MIA - EMERGENCY SEAT MOUNTED LIGHT AT SEAT 21H INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY SEAT MOUNTED LIGHT AT S EAT 21H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008020400089 20080204 00089 NM 2008 2 4 AALA200800047 1 20080109 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975AN 29549 DFW - EMERGENCY LIGHT AT SEAT 19D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008020400090 20080204 00090 NM 2008 2 4 AALA200800045 1 20080109 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT FIRST CLASS COAT CLOSET INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FIRST CLAS S COAT CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008020400091 20080204 00091 WP 2008 2 4 AALA200800046 1 20080109 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 242AA 49255 LGA - EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 14 TO 19 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 14DEF FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 14 TO 19. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020400092 20080204 00092 NM 2008 2 4 AALA200800052 1 20080111 A 3397 WIRE BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 619AA 24577 MIA - EMERGENCY LIGHT AT SEAT 32D INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT SEAT 32D. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020400093 20080204 00093 NM 2008 2 4 AALA200800061 1 20080113 A 2150 6937319312 MODULE BOEING 737 737823 13844BZ NM A/C SYSTEM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 933AN 30080 MIA INFLIGHT T308/13JAN - RECEIVED WING TO BODY OVERHEAD INDICATION. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPL ACED AIR CONDITION MODULE AT COCKPIT OVERHEAD PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008013100301 20080131 00301 EA 2008 1 31 A6WA200840010 1 20080108 A 5240 SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE SERVICE DOOR OBSTRUCTED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 450AW 7823 SERVICE DOOR DIFFICULT TO OPEN. CLEANED DEBRIS FROM DOOR SEAL. DOOR OPERATES OK AT THIS TIME. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008013100329 20080131 00329 NE 2008 1 31 DL757080071 2 20080116 A 7200 UNKNOWN BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE UNKNOWN A DALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 27 605DL 22812 716377 PER THE CREW, AT CRUISE ALTITUDE, 380 LEFT ENGINE ROLLED BACK AND QUIT. CREW TRIED TO IN-FLIGHT START WITH NO JOY. REP LACED FUEL CONTROL AND FUEL PUMP PER MM. REPLACED EEC PE MM. INSPECTED PMG WIRING AND CONNECTORS. INSPECTED AND BLEW OUT PB SENSE LINE. NO PROBLEMS NOTED. LEAK CK GOOD. RAN ENG PER MM. 2 L 7 2 4F 4 F RT A2NM E17NE 2008013100346 20080131 00346 WP 2008 1 31 08FDEA00278 1 20080125 A 5322 AGA71339 SHEAR TIE DOUG DC10 DC1030F 3023504 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 AFT CARGO COMPT AT FS 1952 BETWEEN L47-48R SHEAR TIE IS CORRODED. REMOVED, FABERICATED AND INSTALLED SHEAR TIE IAW SRM 51-33-01, PG-1, VOL II & DWA AGA7133 REV.H. & SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2008020100083 20080201 00083 NM 2008 2 1 CALA0800079 1 20080128 A 5311 6546552 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FUSELAGE FRAME IS CRACKED AT STA 827 BETWEEN STRINGERS 8R AND 9R. INSTALLED REPAIR DOUBLERS PER ECRA 5310-04698. 2 L 7 2 4F RT A16WE 2008020100184 20080201 00184 WP 2008 2 1 08FDEA00315 1 20080128 A 5312 APB70801 ANGLE DOUG MD10 MD1010F 3022112 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 LWW, SLANT BULKHEAD PANEL LWR ATTACH ANGLE CORRODED AT SEVERAL AREAS BET LT AND RT CORNERS, FWD AND AFT FACES, STA 1381. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW MD/DC 10SRM 53-00-01 FIG 1A VOL I. MACHINED NEW SETION DWG APB7080 RE V. D. INSTALLED PER SRM 53-40-00 FIG. 1 VOL I. 2 L 7 3 4F RT A22WE 2008020100194 20080201 00194 NM 2008 2 1 DHL2008780001 1 20080129 A 5753 6521630187 FLAP BOEING 727 727223 1384074 NM LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 LT WING I/B FORE FLAP DELAMINATED BEHIND I/B FLAP TRACK AREA 7 INCH BY 3 INCH. 2 L 7 3 4F A3WE 2008020700089 20080207 00089 EA 2008 2 7 COMA0860080 1 20080118 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SO 01 685BR 9764 7712 FLIGHT 5696 - FLAPS FAILED ON TAKEOFF UPON RETRACTION, FAILED AT 18 DEGREES. AIRCRAFT RETURNED BACK TO DSM AND LANDED S AFELY. REMOVED AND REPLACED LEFT I/B FLAP O/B ACTUATOR. 2 L 7 2 4F RT A21EA 2008020700100 20080207 00100 EA 2008 2 7 COMA0860091 1 20080120 A 2752 853D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SO 01 915CA 11099 7013 FLIGHT 5348 - FLAPS FAILED ON FINAL WHEN SET TO 20 DEGREES. EMERGENCY DECLARED. A/C LANDED SAFELY. REMOVED AND REPLAC ED RIGHT O/B FLAP I/B ACTUATOR. 2 L 7 2 4F RT A21EA 2008020700115 20080207 00115 EA 2008 2 7 COMA0860099 1 20080124 A 5210 BUSHING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNKNOWN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 989CA 7215 FLIGHT 5652 - INFLIGHT AT 12000 FT RECEIVED PAX DOOR WARNING MESSAGE. QRH FOLLOWED AND AIRCRAFT RETURNED BACK TO CVG AN D LANDED SAFELY. REINSTALLED BUSHING IN UPPER FORWARD CAM LEVER OF PAX DOOR. 2 L 7 2 4F RT A21EA 2008020700119 20080207 00119 NM 2008 2 7 MWEA080019 1 20080130 A 5210 59100817 SKIN BOEING 717 717200 1383700 NM PAX DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 907ME 55171 FORWARD PASSENGER DOOR, AFT LOWER CORNER EXIT HAS SKIN DAMAGE. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2008020700120 20080207 00120 SO 2008 2 7 C2XA08IA040 1 20080129 A 5730 14567011012 SKIN EMB 145 EMB145LR 3260212 SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16911 145446 IAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE G ROUND SPOILER. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CRACK ON A 500FC DMI, WITH REINSPECTIONS TO BE MADE AT EVER 50FC, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE INSTALLED A TRIPLER REPAIR IAW EC5740-0114 8, REMOVED THE DMI, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008020700122 20080207 00122 SO 2008 2 7 C2XA08IA042 1 20080129 A 5730 14567011006 SKIN EMB 145 EMB145EP 3260221 SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15948 145056 IAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE G ROUND SPOILER. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CRACK ON A 500FC DMI, WITH RE-INSPECTIONS TO BE MADE A T EVER 50FC, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 05/01/08 TYS MAINTENANCE INSTALLED A TRIPLER REPA IR IN ACCORDANCE WITH EXPRESSJET ENGINEERING CHANGE AND REPAIR AUTHORIZATION 5740-01146, AND THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008020700127 20080207 00127 EA 2008 2 7 TRAX200800136 1 20080126 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 27 889AS 7538 ACFT DIVERTED INTO MSN FOR FLAP FAIL AT WHEN SELECTING 8, EMERGENCY DECLARED. FLT 4602 CX. 2 L 7 2 4F RT A21EA 2008020700129 20080207 00129 EA 2008 2 7 TRAX200800138 1 20080126 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 933EV 8022 ON APPROACH AT 2500 FT FLAPS FAIL MESSAGE WHEN MOVED TO 8 DEGREES. EMERGENCY VEHICLES ROLLED AS A PRECAUTION. 2 L 7 2 4F RT A21EA 2008020700131 20080207 00131 NM 2008 2 7 SWAA080512 1 20080129 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 EEPLS PHOTOLUMINESCENT STRIP BROKEN AT LT OVERWING EMERGENCY EXIT ROW. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008020700138 20080207 00138 NM 2008 2 7 SWAA080518 1 20080129 A 5753 654643099 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2008020700140 20080207 00140 NM 2008 2 7 SWAA080525 1 20080129 A 5312 6936642 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED SPV CHECK, FOUND FWD BULKHEAD RT LOWER CHORD CRACKED AT BS 178. REMOVED AND REPLACED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2008020700141 20080207 00141 NM 2008 2 7 SWAA080519 1 20080129 A 5312 6546541 BULKHEAD BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 22Y CHECK, FOUND MLG BULKHEAD CORRODED AT BS 663.75, LBL 2 TO LBL 4. REPAIRED BULKHEAD PER SRM. 2 L 7 2 4F RT A16WE 2008020700142 20080207 00142 NM 2008 2 7 SWAA080521 1 20080129 A 5311 6546543 FRAME BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008020700151 20080207 00151 SO 2008 2 7 C2XA08TY021 1 20080130 A 3350 20131A BATTERY EMB 145 EMB145XR 3260214 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14174 14500876 OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04, OPS CHECK G OOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT 2008020700155 20080207 00155 SO 2008 2 7 C2XA08ON078 1 20080129 A 2611 K0630 RELAY EMB 145 EMB145XR 3260214 SO SMOKE DETECTION FAILED A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 16183 7786 7786 14500194 FL 7753 - LAX TO LAX - DURING PRE-FLIGHT, FLIGHT CREW REPORTED BAGGAGE SMOKE DETECTION INOP. MX REMOVED AND REPLACED RE LAY K0630 OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008020700156 20080207 00156 SO 2008 2 7 C2XA08ON070 1 20080119 A 2760 SPOILER EMB 145 EMB145LR 3260212 SO WING DEPLOYED A C2XA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 27 11191 1450935 FLT 0054 - MCI TO TUS - SPOILERS DEPLOYED ON TAKEOFF ROLL ABORTED T/O AT 10KNOTS. FLIGHT CREW FULLY DISENGAGED GUSTLOCK AND AIRCRAFT DEPARTED NO MX ACTION WAS REQUIRED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008020700157 20080207 00157 EA 2008 2 7 HNAA0800050 1 20080127 A 2424 51539008D GCU DHAV DHC8 DHC8311 1386006 EA NR 2 ENGINE HOT A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 333EN 221 AN "ELECTRICAL SMELL" IN FLIGHT DECK ON F/O SIDE, FOUND NR 2 ENG GCU HOT. REPLACED GCU, OPS CHECK GOOD, "ELECTRICAL SME LL GONE", HIDDEN DAMAGE INSP C/W. 2 H 7 2 4T RT A13NM 2008020700160 20080207 00160 2008 2 7 WRLA2008013 4 20080122 A 3414 2594467901 INDICATOR DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE COCKPIT MALFUNCTIONED A WRLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 303WL 46917 KDOV/EDDP TAS/SAT INSTRUMENT OFF FLAGS APPEARED, 10 MINS LATER SMOKE EMINATED BRIEFLY FROM INSTRUMENT, TAS/SAT C/B PULLE D CONDITION WENT AWAY, MX CONTROL ADVISED. REMOVED AND REPLACED TAS/SAT GAUGE, OPS NORMAL MM 34-15-00. DMI'S CLOSED. 2 L 7 3 4F 4 F RT A22WE E23EA 2008020700162 20080207 00162 NM 2008 2 7 MWEA080021 1 20080130 A 5210 59100817 SKIN BOEING 717 717200 1383700 NM PAX DOOR BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 907ME 55171 FORWARD ENTRANCE DOOR, FORWARD LOWER CORNER SKIN IS BENT. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2008020700164 20080207 00164 NM 2008 2 7 SWAA080527 1 20080130 A 2730 251A2420 CONTROL VALVE BOEING 737 7377H4 1384404 NM ELEVATOR FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 216WR 32488 DURING SCHEDULED HC2 CHECK, ELEVATOR TAB CONTROL SYSTEM FAILED FUNCTIONAL CHECK. REMOVED AND REPLACED ELEVATOR TAB CONT ROL VALVE PER MM. 2 L 7 2 4F RT A16WE 2008020700165 20080207 00165 NM 2008 2 7 SWAA080528 1 20080130 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 294WN 32540 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008020700167 20080207 00167 2008 2 7 SWAA080530 4 20080130 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008020700168 20080207 00168 NM 2008 2 7 SWAA080538 1 20080130 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020700169 20080207 00169 NM 2008 2 7 SWAA080539 1 20080130 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020700171 20080207 00171 NM 2008 2 7 SWAA080545 1 20080130 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 988, STR 20L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008020700172 20080207 00172 NM 2008 2 7 SWAA080549 1 20080130 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, BL 0. REPAIRED SKIN P ER EA. 2 L 7 2 4F RT A16WE 2008020700177 20080207 00177 NM 2008 2 7 WRLA2008016 1 20080131 A 5753 SKIN DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FLAP VANE DEBONDED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 279WA 48756 DURING C-CHECK MECHANIC FOUND LEFT WING INBOARD FLAP VANE LOWER SKIN DISBONDED 2 PLACES. REPAIRED PER ENGINEERING INSTR UCTION W2008A57B-082 REV.00. REF NRC U01041. 2 L 7 3 4F 4 F RT A22WE E24NE 2008020700180 20080207 00180 EU 2008 2 7 TRAX200800139 1 20080127 A 3397 CONNECTOR AEROSP ATR72 ATR72 EU CABIN DAMAGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 637AS 383 UPON INSTALLATION OF FWD FLOORBOARDS, FOUND 2 EMERGENCY LIGHT TRACK CONNECTORS DAMAGED. 2 H 7 2 4T RT 2008020700186 20080207 00186 EU 2008 2 7 TRAX200800146 1 20080128 A 5720 FAIRING AEROSP ATR72 ATR72 EU RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 RIGHT SIDE WING BOX FAIRING FR 28 CRACKED. FAIRING FR 28 REMOVED AS PER SRM 51-25-01. INSTALLED IAW SRM 51-25-01. 2 H 7 2 4T RT 2008020700188 20080207 00188 EU 2008 2 7 TRAX200800148 1 20080128 A 5720 FAIRING AEROSP ATR72 ATR72 EU RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 RIGHT SIDE WING BOX FAIRING FR 28A CRACKED. FAIRING FR 28A REPLACED IAW SRM 51-25-01. 2 H 7 2 4T RT 2008020100195 20080201 00195 NM 2008 2 1 DHL2008780002 1 20080130 A 5753 66162255 FLAP BOEING 727 727223 1384074 NM WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 1 INCH CRACK ON I/B LOWER SIDE OF NR 3 K FLAP JUST ABOVE BULL NOSE. 2 L 7 3 4F A3WE 2008020400002 20080204 00002 NM 2008 2 4 HALA0800030 1 20080130 A 2841 WARNING MESSAGE BOEING 767 76733A 1385209 NM FUEL QTY INTERMITTENT A HALA O OTHER N FALSE WARNING CR CRUISE 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, DURING CRUISE EXPERIENCED INTERMITTENT STATUS MSG FOR FUEL QTY TOTALIZER. SYSTEM INFO RETURNE D. THEN OPS NORM. T/S PER FIM 28-41-00 FIG 106,108,104. NO FAULTS FOUND AT THIS TIME, SYS OPERATES NORMALLY. OK FOR SERVICE. NO EICAS MESSAGES, MAINTENANCE EICAS MSG FUEL QTY BITE CLEARED. 2 L 7 2 4F RT A1NM 2008020400003 20080204 00003 NM 2008 2 4 TSAA0877005 1 20080128 A 7711 2045061 INDICATOR BOEING 737 737230 1384401 NM NR 1 EPR INTERMITTENT A TSAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 823AL 23154 FLIGHT 48 HNL-ITO - AFTER THE CREW ADVANCED THE THROTTLES, THEY NOTED THE NR 1 EPR READ LOW AT 1.09. THE CREW ABORTED T HE TAKEOFF AT APPROXIMATELY 60 KNOTS. CREW OBSERVED THE NR 1 EPR INDICATION RETURN TO NORMAL AND ELECTED TO CONTINUE WI TH THE FLIGHT. THE FLIGHT OPERATED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 EPR INDICATOR P ER AMM 77-11-0 WITH ALL OPERATIONAL CHECKS SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2008020400014 20080204 00014 WP 2008 2 4 AALA200800032 1 20080105 A 2560 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 249AA 49269 DFW - EMERGENCY FLASHLIGHT AT FIRST CLASS FLIGHT ATTENDANT STATION INOPERATIVE. REPLACED FLASHLIGHT AT FIRST CLASS FLIG HT ATTENDANT STATION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020400075 20080204 00075 NM 2008 2 4 AALA200800054 1 20080112 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 781AN 29586 DFW - EMERGENCY LIGHT AT SEAT 26C HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008020400088 20080204 00088 NM 2008 2 4 AALA200800069 1 20080111 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 978AN 30100 TUL - EMERGENCY SEAT MOUNTED LIGHTS AT SEAT 19A INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY SEAT MOUNTED LIGHTS AT SEAT 19A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008020400097 20080204 00097 NM 2008 2 4 AALA200800071 1 20080114 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 945AN 30085 TUL - EMERGENCY LIGHTS AT RIGHT FIRST CLASS AND FORWARD SERVICE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT FIRST CLASS AND FORWARD SERVICE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008020400163 20080204 00163 EU 2008 2 4 TRAX200800102 1 20080117 A 3350 COVER AEROSP ATR72 ATR72 EU EMERGENCY LIGHTS WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 REFER TO DML 091378 EXIT ROW 1 (RIGHT SIDE) EMERGENCY EXIT LIGHT COVER WORN. 2 H 7 2 4T RT 2008020400170 20080204 00170 EA 2008 2 4 TRAX200800112 1 20080119 A 2751 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FALSE INDICATION A ASOA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 683BR 7692 FLAPS FAIL CAUTION MSG ON LANDING WHEN SELECTING FLAPS FROM 20 TO 30 DEGREES. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2008020400172 20080204 00172 EA 2008 2 4 TRAX200800114 1 20080119 A 5260 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 ASD AFT ANCHOR FITTING SERRATED PLATES CORRODED. 2 L 7 2 4F RT A21EA 2008020400176 20080204 00176 EA 2008 2 4 TRAX200800115 1 20080120 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 832AS 7243 EMERGENCY LIGHTS NOT WORKING PROPERLY. 2 L 7 2 4F RT A21EA 2008020400178 20080204 00178 EA 2008 2 4 TRAX200800117 1 20080120 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 935EV 8037 FLAP FAIL MSG AT 0 DEGREES ON APPROACH. EMERGENCY TRUCKS ON STANDBY AS A PRECATION. FLT 4781 DEL 593 MINS AND ON 1/21 FLTS 4717, 4414 CX. 2 L 7 2 4F RT A21EA 2008020400181 20080204 00181 EA 2008 2 4 TRAX200800120 1 20080120 A 5260 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 859AS 7421 AFT A/S/D ANCHOR FITTING ASSY IS CRACKED. 2 L 7 2 4F RT A21EA 2008020400183 20080204 00183 EA 2008 2 4 TRAX200800123 1 20080121 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 933EV 8022 DURING APPROACH TO (KBOS) REC'D "FLAPS FAIL" CAUTION MESSAGE WHEN SELECTING FLAPS TO "8" DEGREES, FLAP INDICATIONS ARE " 0" DEGREES. EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION. 2 L 7 2 4F RT A21EA 2008020400184 20080204 00184 2008 2 4 TRAX200800124 4 20080121 A 3416 SELECTOR KNOB CNDAIR CL600 CL6002B19 1900309 EA STBY ALTIMETER BROKEN A ASOA O OTHER O OTHER CL CLIMB 1 SO 27 972EV 7534 DURING CLIMB THRU FL 180 THE STBY ALTIMETER SELECT KNOB BROKE, KNOB WILL ONLY ROTATE COUNTER CLOCKWISE. EMERGENCY DECLA RED. A/C RETURNED TO ATL AFTER T/O. 2 L 7 2 4F RT A21EA 2008020600005 20080206 00005 NM 2008 2 6 SWAA080515 1 20080129 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 454WN 29851 DURING SCHEDULED MV2 CHECK, AFT CABIN EMERGENCY EXIT LIGHTS WILL NOT TURN OFF. REMOVED AND REPLACED BATTERY PACK PER MM . 2 L 7 2 4F RT A16WE 2008020700189 20080207 00189 EU 2008 2 7 TRAX200800149 1 20080128 A 5720 ANGLE AEROSP ATR72 ATR72 EU RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 RIGHT SIDE WING BOX FAIRING FR 28 ANGLE CRACKED. 2 H 7 2 4T RT 2008020700190 20080207 00190 EU 2008 2 7 TRAX200800150 1 20080128 A 5320 ANGLE AEROSP ATR72 ATR72 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 LEFT ANGLE CRACK AT FR 26 STR 5L. LT ANGLE AT FR 26 STRG 5L REMOVED IAW SRM 51-25-01. INSTALLED IAW SRM 51-25-01. FAB RICATION OF ANGLE COVER ON W/C 2000-20. 2 H 7 2 4T RT 2008020700195 20080207 00195 NM 2008 2 7 HNAA0800051 1 20080131 A 3350 OL3071BPEGPL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 804EX 227 CABIN EMERGENCY FLOOR LIGHT BY ROW 7 & 8 INOP. REPLACED LAMP, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2008020700196 20080207 00196 SO 2008 2 7 C2XA08SH015 1 20080202 A 5310 14525480603 BEAM EMB 145 EMB145EP 3260221 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14945 145049 SHV - DURING C-CHECK CARGO DOOR CUTOUT LOWER SECTION HAS VARIOUS ARES OF CORROSION. MX REMOVED AND REPLACED LOWER BEAM AT CARGO DOOR CUTOUT FR 65-68 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2008020700197 20080207 00197 SO 2008 2 7 C2XA08SH014 1 20080202 A 5311 14525369001 FRAME EMB 145 EMB145EP 3260221 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14945 145049 SHV - DURING C-CHECK FRAME 65 HAS CORROSION AT STR 17L. MX REPAIRED FR 65 STR 17 IAW EC 5310-01432. THE AIRCRAFT WAS A PPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2008020800002 20080208 00002 NM 2008 2 8 AALA200800167 1 20080125 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 344AN 33083 MIA - EMERGENCY LIGHT AT LEFT AFT DOOR INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT LEFT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008020800004 20080208 00004 2008 2 8 DLM90080142 4 20080131 A 2370 RDAV980501 MONITOR DOUG MD90 MD9030 3023690 NM PWA 2037 PW2037 NE PASSENGER CABIN INOPERATIVE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 909DA 53389 728705 VIDEO MONITOR AT 22F EMITTED SMOKE DURING VIDEO OPERATION. SYSTEM WAS TURNED OFF AND SMOKE DISSIPATED. REMOVED AND REP LACED VIDEO MONITOR AT SEAT 22A PER AMM. CHECKS REMOVED MCO/PLAC. 2 L 7 2 4F 4 F RT A6WE E17NE 2008020800005 20080208 00005 EU 2008 2 8 TRBA2008015 1 20080203 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN INOPERATIVE A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 451AT 451 ON POST FLIGHT, FOUND EMERGENCY LIGHT AT MAIN CABIN DOOR STEP INOPERATIVE. REMOVED AND REPLACED MAIN CABIN DOOR EMERGEN CY LIGHT ASSEMBLY IAW JIC NR 33-51-24. OP CK GOOD IAW JIC NR 33-51-10. 2 H 7 2 4T RT A53EU 2008020600270 20080206 00270 EA 2008 2 6 COMA0860045 1 20080102 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 806CA 12404 7359 FLIGHT 5636 - FLAPS FAIL CAUTION MESSAGE ON APPROACH INTO BOS. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED LEFT I/B FLAP I/B ACTUATOR. 2 L 7 2 4F RT A21EA 2008020600271 20080206 00271 EA 2008 2 6 COMA0860046 1 20080102 A 2752 1104SD100101 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP WORN A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 806CA 7359 FLIGHT 5636 - FLAPS FAIL CAUTION MESSAGE ON APPROACH INTO BOS. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED LEFT SIDE NR 1 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2008020600272 20080206 00272 EU 2008 2 6 08FDEA00326 1 20080130 A 3230 LANDING GEAR AIRBUS 300 A300F4605R 3930327 EU MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 680FE 794 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. TRIED SYS 1 AND SYS 2. SERVICED BOTH LANDING GEAR PITCH DAMPERS FOUND WI TH LOW PRESSURE AND REPLACED LANDING GEAR PROX BOX AS PRECAUTION. 2 L 7 2 4F RT A35EU 2008020600282 20080206 00282 NM 2008 2 6 NOCA00608 1 20080121 A 3350 59192 POWER STRIP BOEING 767 767304 NM CABIN DEFECTIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 769NA 28039 E-PATH LIGHTS INOP ADJACENT TO R2-LAV. INSTALLED NEW CROSSOVER STRIP PER MM 33-51-10, OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2008020600300 20080206 00300 NM 2008 2 6 2008UALA00362 1 20080121 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR OBSTRUCTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 546UA 25367 1R WILL NOT ARM. DEBRIS UNDER GIRT BAR FITTINGS. CLEANED DEBRIS FROM GIRT BAR AREA ON FLOOR. DOOR ARMS AND DISARMS N ORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600328 20080206 00328 NM 2008 2 6 2008UALA00404 1 20080123 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 UPPER FUSELAGE SKIN UNDER DORSAL FIN LEFT SEAL CONTACT AREA STA 986 AND 995 HAVE EXCESSIVE MATERIAL LOSS OF .006". BLEN DED DAMAGE. INSTALLED DOUBLER AND TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600358 20080206 00358 EA 2008 2 6 COMA0860062 1 20080112 A 3234 7179015 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 781CA 21813 7312 FLIGHT 5676 - DURING CLIMBOUT, LANDING GEAR HANDLE WOULD NOT MOVE TO RAISE THE GEAR. AIRCRAFT RETURNED BACK TO DCA AND LANDED SAFELY. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE. 2 L 7 2 4F RT A21EA 2008020600012 20080206 00012 NM 2008 2 6 PIDA08006 1 20080104 A 3350 BATTERY PACK BOEING 757 757200 1384950 NM EMERGENCY LIGHTS INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 801DM 26240 DURING MAINTENANCE CHECK, NOTED SEVERAL EMERGENCY EXIT LIGHTS INOP. RELAMPED AND REPLACED BATTERY PACKS PER MM 33-51-06 AND 33-51-07. LIGHTS OPS CHECKED GOOD PER MM 33-51-00. 2 L 7 2 4F RT A2NM 2008020600013 20080206 00013 NE 2008 2 6 200801231 2 20080120 A 7530 4120T03P05 ACTUATOR EMB ERJ170 ERJ170100SE 3260406 NM GE CF34 CF348E5 30061 NE VGV FAILED A UHLA E ENGINE SHUTDOWN O OTHER AP APPROACH 1 GL 11 640RW 2721 17000058 GEE193171 ON APPROACH CREW RECEIVED ENGINE 1 CONTROL FAULT EICAS MESSAGE AND A LOW/ABNORMAL N1 INDICATION. SHORTLY THEREAFTER ENG INE 1 ITT ROSE RAPIDLY AND PEAKED AT ABOUT 970 DEGREES. CREW SHUT ENGINE NR 1 DOWN INFLIGHT, DECLARED AN EMERGENCY, AND MADE A NORMAL LANDING. MAINTENANCE REPLACED THE VG ACTUATOR. 2 L 7 2 4F 4 F RT A56NM E00063EN 2008020600017 20080206 00017 NM 2008 2 6 USAA920080230 1 20080123 A 5320 6529818 SUPPORT ANGLE BOEING 737 7373S3 1384711 NM BS 335 S17-18L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - CRACKED SUPPORT ANGLE, BS 335.5, S17L - S18L. REPLACED SUPPORT ANGLE, BS 335.5, S17L - S18L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600018 20080206 00018 2008 2 6 SWAA080540 4 20080130 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008020600021 20080206 00021 NM 2008 2 6 SWAA080534 1 20080130 A 3350 20121 CHARGER BOEING 737 7375H4 138449D NM EMERGENCY LIGHTS FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND AFT LT LOWER FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTER Y CHARGER PER MM. 2 L 7 2 4F RT A16WE 2008020600022 20080206 00022 NM 2008 2 6 SWAA080535 1 20080130 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 360 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020600031 20080206 00031 NM 2008 2 6 USAA920080213 1 20080111 A 5340 693535214 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 727C S6L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED STRINGER CLIP, BS 727C, S6L. REPLACED STRINGER CLIP, BS 727C, S6L IAW B737 SR M 51-40-02. 2 L 7 2 4F RT A16WE 2008020600032 20080206 00032 NM 2008 2 6 USAA920080214 1 20080104 A 5340 146N519139 STRINGER CLIP BOEING 757 757225 1384959 NM BS 1660-1680 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 MCN - MAJOR REPAIR - C11 CHECK - CRACKED FLOOR STRUCTURE WEB UPPER CHORD CLIP ANGLE, BS 1660 - BS 1680, RBL 10.5, WL 208 . REPAIRED FLOOR STRUCTURE WEB UPPER CHORD CLIP ANGLE, BS 1660 - BS 1680, RBL 10.5, WL 208 IAW B757 SRM 53-00-51-2R4. 2 L 7 2 4F RT A2NM 2008020600033 20080206 00033 NM 2008 2 6 USAA920080215 1 20080112 A 5320 146N51905 WEB BOEING 757 757225 1384959 NM BS 1660 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 MCN - MAJOR REPAIR - C11 CHECK - CRACKED FLOOR STRUCTURE WEB, BS 1660, RBL 10.27, WL 208. REPLACED FLOOR STRUCTURE WEB, BS 1660, RBL 10.27, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008020600034 20080206 00034 NM 2008 2 6 SWAA080541 1 20080130 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM BS 727A S25L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008020600037 20080206 00037 NM 2008 2 6 SWAA080505 1 20080129 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 767 S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020600044 20080206 00044 NM 2008 2 6 PIDA08004 1 20080117 A 5320 FLOOR SUPPORT BOEING 737 7372K5 138448X NM BS 800-827 CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 DURING MAINTENANCE CHECK, NOTED CORROSION FROM BS 800 TO BS 827 ON THE FLOOR SUPPORT ANGLE AT RBL 17 IN THE AFT CARGO BI N. REPLACED FLOORBEAM FROM BS 787 TO BS 867 PER SRM 51-30-02 AND SRM 51-40-04. 2 L 7 2 4F RT A16WE 2008020600047 20080206 00047 2008 2 6 SA08003 4 20080121 A 2565 D31516121 SLIDE AIRBUS A319 A319112 3930323 EU ZONE 200 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 745VJ 21733 700 1289 CLT - DURING WEEKLY TEST, RECEIVED MAINTENANCE MESSAGE "EPSU EXT LOAD FWD L". MAINTENANCE REPLACED BOTH FORWARD EMERGEN CY ESCAPE SLIDE/RAFTS. EMERGENCY LIGHTS TEST NORMAL. 2 L 7 2 4F RT A28NM 2008020600049 20080206 00049 NM 2008 2 6 2008UALA00304 1 20080118 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 805UA 783 FOUND CORROSION ON FLOORBEAM ITEMS NR 145, 140 AND 90. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600058 20080206 00058 SO 2008 2 6 C2XA08IA036 1 20080121 A 3350 20131A BATTERY PACK EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 33182 1053 1053 14500909 MCI - FLIGHT 7684, SURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS IN THE GALLEY WERE INOPERAT IVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECT S NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008020600359 20080206 00359 EA 2008 2 6 COMA0860063 1 20080113 A 3020 12681 PRESSURE SWITCH CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 442CA 5673 7483 FLIGHT 5516 - DURING CRUISE FLIGHT RECEIVED LEFT COWL ANTI-ICE CAUTION MESSAGE. AIRCRAFT DIVERTED TO GSO AND LANDED SAF ELY. REMOVED AND REPLACED LEFT COWL ANTI-ICE PRESSURE SWITCH. 2 L 7 2 4F RT A21EA 2008020600374 20080206 00374 NM 2008 2 6 USAA920080263 1 20080107 A 5347 SEAT TRACK BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 871.5 - BS 1109, RBL 88.55, WL 200. REPLACED CABIN SEAT TRACK, BS 871.5 - BS 1109, RBL 88.55, WL 200 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008020700020 20080207 00020 SO 2008 2 7 C2XA08TY017 1 20080125 A 5534 1450498060160 BRACKET EMB 145 EMB145XR 3260214 SO VERTICAL STAB CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12122 145684 TYS - DURING A CURRENT 3C INSPECTION THE VERTICAL STAB SPHERICAL BEARING BRACKET WAS FOUND WITH PITTING CORROSION. MAIN TENANCE MEASURED THE AREA AND WAS FOUND TO BE OUT OF LIMITS. COMMENCE TO REAM TO FIRST OVERSIZE IAW EMB 14XR SRM 55-30- 02 AND EC 5510-01157. AIRCRAFT WILL BE RELEASED TO SERVICE AT THE END OF THE CHECK. 2 L 7 2 4F RT 2008020700035 20080207 00035 SO 2008 2 7 C2XA08IA033 1 20080122 A 3320 2LA00727830 LIGHT EMB 135 EMB135LR 3260305 SO CABIN MALFUNCTIONED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 12530 145533 IAH - DURING POST FLIGHT INSPECTION THE CREW REPORTED SMOKE COMING FROM THE READING LIGHT AT SEAT 2A. MAINTENANCE REMOV ED AND REPLACED THE READING LIGHT ASSEMBLY, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008020700039 20080207 00039 NM 2008 2 7 2008UALA00309 1 20080117 A 3510 MF20010 HARNESS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE O2 MASK LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 851UA 1664 F/O'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). BROKEN HARNESS (LEAKING). REPLACED F/O'S O2 HARNESS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020700072 20080207 00072 NM 2008 2 7 2008UALA00478 1 20080128 A 2612 FIRE WARNING BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 906UA 25006 CREW REPORTS ON PREFLT, NO BELL DURING FIRE TEST. APU HORN IN WHEEL WELL DOES COME ON. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700095 20080207 00095 EA 2008 2 7 COMA0860086 1 20080118 A 2760 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA SPOILER DIRTY A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 629BR 7251 FLIGHT 5155 - ON TAKEOFF RECEIVED TAKEOFF CONFIG SPOILER WARNING. ABORTED TAKEOFF. INSPECTED AND CLEANED GROUND SPOILE R PROX SENSORS. PERFORMED OPS CHECK OF SPOILER SYSTEM, ALL CHECKS GOOD. 2 L 7 2 4F RT A21EA 2008020700133 20080207 00133 NM 2008 2 7 SWAA080520 1 20080129 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008020700146 20080207 00146 NM 2008 2 7 HNAA0800046 1 20080123 A 3350 OL3071BPEGL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 914HA 53 EMERGENCY EXIT SIGN BY RIGHT SIDE AFT DOOR HAS INOP LAMP. REPLACED BURNED OUT LAMP, OPS CK'D GOOD. 2 H 7 2 4T RT A13NM 2008020700179 20080207 00179 NM 2008 2 7 WRNA200800004 1 20080131 A 2150 7192389 ACM BOEING 747 747230B 1384889 NM A/C BAY ACTIVATED A WRNA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 05 508MC 21644 DURING CRUISE, NR 3 PACK SHUTDOWN, LEAVING NO OPERATIONAL PACK, (NR 1 PACK WAS ON MEL, AND NR 2 PACK IS DEACTIVATED). A IRCRAFT DIVERTED TO IAH AND MADE A SAFE LANDING. REPLACED NR 3 ACM, NOTE: ALSO REPLACED NR 1 ACM AND REMOVED FROM MEL. A/C RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008020700193 20080207 00193 EA 2008 2 7 TRAX200800153 1 20080130 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 759EV 10211 CENTER LEVEL EMERGENCY EXIT SIGN FWD FACING SECTION INOP FOR OVERWING EXITS. 2 L 7 2 4F RT A21EA 2008020800018 20080208 00018 SO 2008 2 8 RAIA00801030 1 20080127 A 7830 SWITCH EMB 145 EMB145LR 3260212 SO THRUST REVERSER OUT OF ADJUST A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 815HK 145048 FLT 5577 - STL - ENGINE NR 2 THRUST REVERSER DISAGREE MESSAGE DURING TAKEOFF ROLL. MAINTENANCE ADDED SHIM TO BOTTOM STO W SWITCH. OPERATIONAL TEST OF SYSTEM CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008020800021 20080208 00021 SO 2008 2 8 RAIA00801028 1 20080125 A 3010 129502 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO ANTI-ICE SYSTEM MALFUNCTIONED A RAIA B EMER. DESCENT J WARNING INDICATION LD LANDING 1 CE 03 814HK 7259 534 145046 FLT 5468 - MSN - WING ANTI-ICE FAIL MESSAGE IN ICING CONDITIONS. MAINTENANCE REMOVED AND REPLACED THE NR 2 WING LOW PRE SSURE SWITCH. PERFORMED AN OPERATIONAL CHECK OF THE ANTI-ICE SYSTEM WITH NO ADDITIONAL DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008020800023 20080208 00023 EU 2008 2 8 08FDEA00345 1 20080203 A 5712 A5796011320000 RIB AIRBUS 300 A300B4622 3930401 EU LT IB FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 720FD 417 RIB NR 25 FOUND TO BE CRACKED. REPLACE DAMAGED RIB. 2 L 7 2 4F RT A35EU 2008020800025 20080208 00025 NM 2008 2 8 AALA200800133 1 20080121 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 674AN 29424 DFW - EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER THREE D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020600059 20080206 00059 SO 2008 2 6 C2XA08ON077 1 20080125 A 3350 66367 LIGHT EMB 145 EMB145LR 3260212 SO CABIN BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11547 13796 13796 14500563 FLT MX - ONT TO ONT - WHILE PERFORMING OVERNIGHT SERVICE CHECK MX PERSONNEL FOUND EMERGENCY PROXIMITY LIGHT STRIP INOP O N ROWS 8 & 9. MX PERSONNEL REMOVED AND REPLACED EMERGENCY PROXIMITY LIGHT STRIP ON ROW 8 & 9 OPERATIONALLY CHECKED SATI SFACTORY. AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008020100042 20080201 00042 NM 2008 2 1 CALA0800050 1 20080120 A 5320 65479599 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 ABB WEB AT STATION 787-794 ABOVE STRINGER 25R HAS CORROSION. REMOVED AND REPLACED INTERCOSTAL IN REF TO SRM 51-40-02 AN D BOEING DRAWING 65-47959. 2 L 7 2 4F RT A16WE 2008020100068 20080201 00068 NM 2008 2 1 KCSA081039 1 20080125 A 5312 STIFFENER BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 CORROSION ON TOP OF HORZ STIFFENER WEB ON AFT SIDE OF BS 1480 BULKHEAD BETWEEN RBL 33 AND RBL 69. 2 L 7 4 4F RT A20WE 2008020100071 20080201 00071 NM 2008 2 1 KCSA081042 1 20080125 A 5414 SKIN BOEING 747 747209B 138489B NM NR 1 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 PYLON NR 1 OUTER SKIN CHAFED WING L/E STA 1124 NAC STA 263. 2 L 7 4 4F RT A20WE 2008020100097 20080201 00097 NM 2008 2 1 KCSA081052 1 20080131 A 5320 INTERCOSTAL BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FUSELAGE FRAME INTERCOSTAL HAS .25 INCH CRACK BETWEEN STA 2725 & 2733, BL 0, WL 364.5. 2 L 7 4 4F RT A20WE 2008020100132 20080201 00132 NM 2008 2 1 08FDEA00305 1 20080128 A 5311 ACA73501 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 523FE 48479 MAIN DECK CARGO, LT FRAME AT STA 535 AT 9G NET YOKE FOUND EDGE GOUGED. REPAIR CARRIED OUT AT MAIN DECK CARGO LT FRAME, BS 535, 9G NET YOKE AS PER DWG SRZ53-503. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008020400008 20080204 00008 SO 2008 2 4 FDKA200801041 1 20080128 A 2700 701700082430 COMPUTER EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 846MJ 17883 145507 FDM 9963 ORF-JFK (1810 PHX LCL) - COMMAND AND INDICATION OF ROLL AND YAW TRIM NOT IN SYNC WITH ACTUAL CONTROL SURFACE PO SITION. MX REMOVED AND REPLACED IC-600. 2 L 7 2 4T RT T00011AT 2008020400025 20080204 00025 NM 2008 2 4 AALA200800022 1 20080103 A 2750 FCU BOEING 737 737823 13844BZ NM TE FLAPS INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SW 21 960AN 29542 LAX INFLIGHT T743/03JAN - ON APPROACH FLAPS WOULD NOT EXTEND. NO INDICATIONS. ACCOMPLISHED EMERGENCY FLAP EXTENSION. LANDED LAX WITHOUT INCIDENT. REPLACED FLAT SLAT ELECTRICAL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008020400159 20080204 00159 EA 2008 2 4 TRAX200800098 1 20080111 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 317CA 10055 LEFT 280 WEB CORRODED BEYOND LIMITS. 2 L 7 2 4F RT A21EA 2008020400174 20080204 00174 SO 2008 2 4 C2XA08IA030 1 20080122 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145EP 3260221 SO RUDDER INOPERATIVE A C2XA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 12934 145019 IAH - FLIGHT 2191, THE CREW REPORTED THAT THE AIRCRAFT VEERD SHARP LEFT, AND RECEIVED A RUDDER 1&2 INOP EICAS MESSAGE. THE AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE RUDDER 1&2 PRESSURE SWITCH ES, OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008020400177 20080204 00177 EA 2008 2 4 TRAX200800116 1 20080120 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 927EV 7844 FLAP FAIL AT ZERO ON APPROACH, EMERGENCY DECLARED. FLTS 4291, 4907 CX AND ON 1/22/08 FLT 4450 CX. 2 L 7 2 4F RT A21EA 2008020600019 20080206 00019 NM 2008 2 6 SWAA080532 1 20080130 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 440LV 29835 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008020600020 20080206 00020 NM 2008 2 6 SWAA080533 1 20080130 A 5330 6547955 SKIN BOEING 737 7375H4 138449D NM BS 847 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BEAR STRAP BS 847, RBL 15. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008020600030 20080206 00030 NM 2008 2 6 USAA920080212 1 20080113 A 5320 66142081 WEB BOEING 737 7373Y0 1384671 NM BS 294 S11L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED L1 DOOR CUTOUT INTERCOSTAL WEB, BS 294.5, S11L. REPLACED L1 DOOR CUTOUT INTER COSTAL WEB, BS 294.5, S11L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600066 20080206 00066 EA 2008 2 6 COMA0860051 1 20080104 A 3260 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA MLG UNKNOWN A COMA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 941CA 7050 FLIGHT 5262 - ON DESCENT INTO JFK RECEIVED PROX SYSTEM CAUTION MESSAGE. EMERGENCY DECLARED, MESSAGE WENT OUT BELOW 200 KTS AND BEFORE GEAR EXTENSION. ALL INDICATIONS WERE NORMAL DURING LANDING. INSPECTED PSEU NO FAULT CODES STORED. PERF ORMED SYSTEM SELF TEST. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2008020600067 20080206 00067 SO 2008 2 6 C2XA08SHO17 1 20080202 A 5540 14525008403 ATTACH BRACKET EMB 145 EMB145LR 3260212 SO RUDDER DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16559 145603 SHV - DURING C-CHECK ATTACHMENT BRACKET LOWER TO VENT HAS DAMAGE. MX REMOVED AND REPLACED ATTACHMENT BRACKET (LOWER-RUD DER 1 TO VENT) IAW EMB 145 SRM 51-40-02. 2 L 7 2 4T RT T00011AT 2008020600068 20080206 00068 SO 2008 2 6 C2XA08ON074 1 20080124 A 2910 LINE EMB 145 EMB145XR 3260214 SO HYD SYSTEM DISCONNECTED A C2XA A UNSCHED LANDING W K J INADEQUATE Q C FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 27200 14500956 FLT 0017 - TUS TO SAT - DURING CRUISE FLIGHT CREW REPORTED HYD SYS 1 INDICATED 0 PRESSURE AND 0 QUANTITY. CONTRACT AND ONT MX PERSONNEL WERE DISPATCHED. AIRCRAFT DIVERTED TO TUS AND DECLARED NO EMERGENCY AND LANDED SAFELY. MX PERSONNEL A FTER VISUAL INSPECTION FOUND HYD SERVICE LINE DISCONNECTED. MX RE-TIGHTENED SERVICE LINE OPERATIONALLY CHECK SATISFACTO RY AND AIRCRAFT WAS RELEASED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2008020600069 20080206 00069 SO 2008 2 6 C2XA08ON075 1 20080125 A 2120 2305591728 CLAMP EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL CUSTOMER AIR MISSING A C2XA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SW 27 16183 7762 7762 14500914 CAE312814 FLT 7650 - LAX TO LAX - DURING CRUISE FLIGHT CREW REPORTED E1 HIGH ITT. AIRCRAFT RETURNED TO BLOCK WITH NO INCIDENT. M X PERSONNEL FOUND COSTUMER SERVICE DISCHARGE TUBE CLAMP MISSING, CAUSING GASKET ALSO MISSING. MX INSTALLED A NEW CLAMP AND GASKET OPERATIONALLY CHECK HIGH POWER RUNS SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2008020600074 20080206 00074 NM 2008 2 6 MWEA080015 1 20080124 A 5330 991183915 SKIN BOEING 717 717200 1383700 NM BS 1178-1200 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 917ME 55179 AFT ACCESSORY COMPARTMENT LEFT SIDE HAS A 1 7/8" CRACK IN CANTED FRAME Y 1178.225, NEAR FRAME RADIUS AT APPROXIMATELY ST ATION 1200, 900, BETWEEN LONGERON 17 LEFT AND 18 LEFT. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2008020600076 20080206 00076 SO 2008 2 6 C2XA08SH019 1 20080202 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 SHV - DURING C-CHECK LEFT OMEGA BEAM AT FR 22 HAS A CRACK IN WEB THROUGH RIVET. MX REPAIRED LEFT OMEGA BEAM BETWEEN FRM 19 AND 23 IAW EC5320-01229. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008020600081 20080206 00081 NM 2008 2 6 USAA920080266 1 20080107 A 5347 SEAT TRACK BOEING 767 7672B7ER 1385107 NM BS 1098-1362 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 1098 - BS 1362, LBL 88.5. REPLACED CABIN SEAT TRACK, BS 1098 - BS 1362, LBL 88.5 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008020600082 20080206 00082 SO 2008 2 6 C2XA08TY020 1 20080130 A 3350 1317 BULB EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14174 14500876 MAIN DOOR EMERGENCY LIGHT FLICKERS ON/OFF. RESECURED BULB IAW EMB 145XR AMM 33-50-06. OPS CHECK GOOD, AIRCRAFT RELEASE D AND RETURNED TO SERVICE. 2 L 7 2 4F RT 2008020600084 20080206 00084 EA 2008 2 6 COMA0860041 1 20080102 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA RT WING TE FLAPS FAILED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 916CA 14160 7014 FLIGHT 5016 - FLAPS FAILED AT 0 DEGREES ON APPROACH INTO CVG. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED RIGHT BPSU. 2 L 7 2 4F RT A21EA 2008020600091 20080206 00091 NM 2008 2 6 USAA920080246 1 20080120 A 5511 183N150317 RIB BOEING 757 757225 1384959 NM HORIZONTAL STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 MCN - MAJOR REPAIR - C-11 CHECK - CORROSION ON L HORIZ STAB RIB 12, STAB STA 296.249. REMOVED AND REPLACED CHORD AT L H ORIZ STAB RIB 12, STAB STA 296.249 IAW B757-200 SRM 51-40-02-0G AND BAC DWG 183N1503. 2 L 7 2 4F RT A2NM 2008020600100 20080206 00100 NM 2008 2 6 USAA920080196 1 20080118 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 986 S27L/R CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 527AU 23862 CLT - MAJOR REPAIR - RON - CORROSION ON FUSELAGE SKIN, BS 986, S27L - S27R. REPAIRED FUSELAGE SKIN, BS S27L - S27R IAW USAIRWAYS EA 1000160. 2 L 7 2 4F RT A16WE 2008020600104 20080206 00104 NE 2008 2 6 16301 2 20080104 A 7200 80K347597801 BREATHER TUBE PIAGIO P180 P180 6960204 EU PWA PT6 PT6A66 52043 NE HARTZL HCE5N HCE5N3 GL ZONE 400 KINKED E V2JA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 15 163SL 633 61 1131 AT FL280, CREW CALLED INTO OPERATIONS CONTROL CENTER TO ADVISE OF AN UNKNOWN ODOR IN THE AIRCRAFT, AND SLIGHT VISIBLE S MOKE. THE CREW PULLED BACK ON THE THROTTLES AND THE SMOKE DISAPPATED. THEY THEN POWERED BACK UP AND THE SMOKE WENT AWA Y. THE ODOR REMAINED AND AT THAT POINT, THE SIC CONTACED ATC TO DELCARE AN EMERGENCY FOR SMOKE IN THE COCKPIT. THEY CH ANGED THEIR FLIGHT DESTINATION TO ELM FROM CYYZ IN THE PROCESS. THE PIC, NOT WANTING TO DOWN-GRADE THE EMERGENCY STATUS , GOT ON THE RADIOS AND ADVISED THAT ALL IS WELL AND THAT THE ROLLING OF EMERGENCY VEHICLES WAS NOT NECESSARY. FOUND BR EATHER TUBE KINKED. 1 H 7 2 3O 4 T RT A59EU E26NE 5 C PZONE 2008020600109 20080206 00109 WP 2008 2 6 ABXA08023 1 20080107 A 5320 99578608 ANGLE DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 COCKPIT WINDOW SILL RIGHT ANGLE P/N: 9957860-8 CRACKED. REMOVED, REPAIRED, AND REINSTALLED ANGLE IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 2008020600113 20080206 00113 WP 2008 2 6 ABXA08026 1 20080107 A 5320 591236068 ANGLE DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 CENTER AND SIDE WINDSHIELD RIGHT ZEE P/N: 5912360-68 CRACKED. REPLACED RIGHT ZEE IAW SR DWG 09530268, DC9 SRM 51-30-2, 51-30-5 AND JOB CARD EA 53300036-014. 2 L 7 2 4F A6WE 2008020600123 20080206 00123 NM 2008 2 6 ABXA08022 1 20080118 A 2530 400140901R OVEN BOEING 767 767232 1385132 NM GALLEY SHORTED A ABXA O OTHER A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 23 744AX 21 22221 MICROWAVE SHORTED OUT WHEN IN USE. TOP RIGHT BACK SIDE SPARKED AND FIRE CAME OUT. CIRCUIT BREAKERS PULLED FOR GALLEY. REMOVED AND REPLACED MICROWAVE. OPS CHECKED GOOD IAW B767 MM 25-31-00. 2 L 7 2 4F RT A1NM 2008020600134 20080206 00134 EA 2008 2 6 MASA200800071 1 20080128 A 5210 CAM CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR HANDLE DIRTY A MASA O OTHER O OTHER CR CRUISE 1 SW 07 503MJ 10058 ASH FLT 7237 BDL TO IAD - DIVERTED INTO BDL DUE PAX DOOR WARNING IN FLIGHT. MX FOUND INNER HANDLE CENTERING CAM DIRTY A ND FULL OF DEBRIS. MX CLEANED CAM DOOR, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008020600139 20080206 00139 WP 2008 2 6 UPS08851495 1 20080118 A 2560 GIRT BAR DOUG DC8 DC873F 302199F WP ESCAPE SLIDE DIRTY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 GIRT BAR JAMS ON RIGHT SIDE. CLEANED DEBRIS FROM GIRT BAR FLOOR LATCH AND LUBED. OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 2008020600140 20080206 00140 WP 2008 2 6 UPS08851496 1 20080107 A 5524 INTERCOSTAL DOUG DC8 DC871F 302199D WP LT ELEVATOR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 DAMAGED COUNTERSINK ON INBD AFT CORNER OF LT ELEVATOR. LT ELEVATOR INBD INTERCOSTAL AFT CORNER DAMAG ED COUNTERSINK REPAIRED IAW SRM 55-02-00-0 FIG 002, SRM 55-04-01-00 FIG 002, SRM 51-01-21 AND SRM 51-01-21A. 2 L 7 4 4F RT 4A25 2008020600141 20080206 00141 WP 2008 2 6 UPS08851497 1 20080108 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 1324 L21L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 WEB BROKEN ON AFT LOWER CORNER OF LT AFT ENTRY DOOR TORQUE BOX. REPAIRED LT AFT ENTRY DOOR TORQUE BO X WEB IAW DWG 9751060, SRM 53- 02-00 FIG 23, SRM 51-01-08, SRM 51-01-21 AND SRM 51-01-21D AT STA 1324 AND L21L. 2 L 7 4 4F RT 4A25 2008020600142 20080206 00142 WP 2008 2 6 UPS08851498 1 20080104 A 5753 RIB DOUG DC8 DC871F 302199D WP LT WING FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 PNL - 551 SUPPORT FRAME CRACKED AT O/B END OF LT I/B FLAP. REPAIRED LT I/B FLAP O/B RIB (PNL 551 LAN DING) IAW SRM 57-02-00, SRM 57-07-01-0, AND SRM 51-01-21-0. 2 L 7 4 4F RT 4A25 2008020600145 20080206 00145 WP 2008 2 6 UPS08851500 1 20080107 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 70 L21L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 MAIN CABIN L-1 DOOR TORQUE BOX WEB GOUGED AND CRACKED STA 70 ABOVE L21L. REPAIRED MAIN CABIN L-1 DO OR TORQUE BOX WEB AT STA70 ABOVE L21L IAW SRM 53-02-00-0 FIG 001D AND DWG 5597646. 2 L 7 4 4F RT 4A25 2008020600153 20080206 00153 2008 2 6 F3LA200800040 4 20080127 A 2565 D30665309 SLIDE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE R2 DOOR DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 948FR 140 2863 DURING C1 C CHECK, INSPECTION REPORTED THE R2 DOOR EMERGENCY ESCAPE SLIDE HAD A WORN AREA ON THE GIRT PANEL. MAINTENANC E REMOVED THE GIRT BAR FROM THE DAMAGED PANEL AND INSTALLED THE GIRT BAR IN THE NEW ESCAPE SLIDE ASSEMBLY IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 25-62-44-991-031. FOLLOWING INSTALLATION OF THE NEW ESCAPE SLIDE ASSEMBLY, THE INSTALLATIO N WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008020600157 20080206 00157 EA 2008 2 6 MASA200800077 1 20080130 A 5220 SEAL CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT LACK OF LUBE A MASA O OTHER O OTHER CR CRUISE 1 SW 07 930LR 15030 ASH FLT 2941 PHX-MEM - ROW 16AC EMERGENCY DOOR SQUEALING IN FLIGHT. MX LUBED THE SEAL. 2 L 7 2 4F RT A21EA 2008020600159 20080206 00159 NM 2008 2 6 2008UALA00322 1 20080118 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 LEFT EXTERNAL FUSELAGE HAS 2 DAMAGED FASTENER HOLES AT BS 887 ABOVE STR 20L. MAJOR REPAIR: REMOVED DAMAGE. INSTALLED DO UBLER AND TRIPLER WITH FILLERS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600160 20080206 00160 EA 2008 2 6 MASA200800078 1 20080130 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT OUT OF ADJUST A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 906FJ 15006 ASH FLT 2976 PHX-SJD - LT AFT EMERGENCY EXIT DOOR CAUTION MESSAGE INTERMITTENT. ADJUSTED DOOR PROX SENSOR. 2 L 7 2 4F RT A21EA 2008020600173 20080206 00173 WP 2008 2 6 UPS08851503 1 20080114 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FS 1120 RBL 50 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 MAIN CABIN FLOOR PNL CORRODED AT STA 1120 RBL 50. REMOVED FLOOR PNL AT STA 1120 RBL 50 IAW SRM 51-03 -00. FABRICATED AND INSTALLED REPAIR FLOOR PNL AT STA 1120 RBL 50 REF EO DC8-5320- 9691C. 2 L 7 4 4F RT 4A25 2008020600178 20080206 00178 2008 2 6 UPS08851521 4 20080122 A 2565 SLIDE DOUG DC8 DC871F 302199D WP EMERGENCY EXIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 CREW ENTRY DOOR WAS OPENED AFTER SECURED FOR FLIGHT BY DE-ICE; ESCAPE SLIDE WAS PULLED FROM CASE. INSTALLED SLIDE IN CA SE PER MM 25-60-01-2. 2 L 7 4 4F RT 4A25 2008021200101 20080212 00101 NM 2008 2 12 2008UALA00369 1 20080121 A 3510 MF20010 OXYGEN MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 837UA 1474 CAPTAIN'S O2 MASK LEAKING DURING TEST. UNKNOWN O2 LEAK. REPLACED CAPT O2 MASK. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600191 20080206 00191 NM 2008 2 6 UPS08B51479 1 20080120 A 3350 LAMP BOEING 747 74744AF 13848B2 NM GE CF6 CF680C2* GL EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 571UP 35668 L1 FWD DOOR FRAME EMERGENCY LIGHT INOP. RELAMPED, OPS CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E23EA 2008020600194 20080206 00194 WP 2008 2 6 UPS08851540 1 20080114 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 COCKPIT FLOOR PNL 676C HAS CRACKS AT RIVETS. REMOVED TOP SKIN OF COCKPIT FLOOR PNL 676C IAW SRM 51-1 -20D. FABRICATED AND INSTALLED TOP SKIN ON FLOOR PNL 676C IAW SRM 53-7-3 FIG 001. 2 L 7 4 4F RT 4A25 2008020600197 20080206 00197 NM 2008 2 6 UPS08B51481 1 20080121 A 2560 INERTIA REEL BOEING 747 74744AF 13848B2 NM COCKPIT DISLODGED A IPXA O OTHER O OTHER LD LANDING 1 SO 01 571UP 35668 INERTIAL REELS FELL OUT OF UNIT ON LANDING. NEED TO BE CHECKED FOR CORRECT STOWAGE. INSPECTED AND REPLACED ALL DESCENT DEVICES PER AMM 25-61-01-2. 2 L 7 4 4F RT A20WE 2008020600203 20080206 00203 NM 2008 2 6 UPS08M51490 1 20080122 A 3020 ANTI-ICE VALVE DOUG MD11 MD11F 3023600 NM NR 2 ENGINE STUCK A IPXA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 01 280UP 48634 ATB - NR 2 ENG ANTI-ICE LVL 1 ENG 2 ANTI-ICE OFF ALERT APPEARED. COULD NOT GET ENG 2 ANTI-ICE HEAT TO COWL. ACCOMPLISH ED FIM 30-22-007 AND 30-22-04, FOUND NR 2 ENG ANTI-ICE VALVE NOT RESPONDING AND STUCK IN MID POS. REMOVED AND REPLACED VALVE PER AMM 30-22-04. OPS CHECK GOOD. 2 L 7 3 4F RT A22WE 2008020600210 20080206 00210 2008 2 6 08FDEA00324 4 20080129 A 2565 SX657932 CHAIN DOUG MD11 MD11F 3023600 NM ZONE 200 FAILED A FDEA K NONE L NO TEST IN INSP/MAINT 1 SO 25 617FE 48748 DURING ESCAPE SLIDE/RAFT OPS CHECK, MED L1 FAILED TO DEPLOY IN EMERGENCY MODE. L1 DOOR AFT DRUM POWER DRIVE ROLLER CHAI N REMOVED AND REPLACED AS PER CMM 52-11-09. EMERGENCY OPERATIONAL TEST CARRIED OUT AS PER AMM 52-11-04-5. 2 L 7 3 4F RT A22WE 2008020600211 20080206 00211 WP 2008 2 6 UPS08851592 1 20080130 A 2560 GIRT BAR DOUG DC8 DC871F 302199D WP CABIN DOOR BENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:IN BRACKETS HOLDING GIRT BAR ARE BENT. STOWED GIRT BAR BUT WHEN OPENING DOOR, WIND CAUGHT DOOR AND GIRT BAR FELL OUT OF BRACKET AND SLIDE CAME OUT OF CONTAINER. REINSTALLED ESCAPE SLIDE PER M/M 25-60-04. 2 L 7 4 4F RT 4A25 2008020600212 20080206 00212 WP 2008 2 6 UPS08851593 1 20080131 A 5410 COWLING DOUG DC8 DC873F 302199F WP I/B FAN DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:IN NR 3 ENG I/B FAN COWL HAS 1 EA DENT AT L/E AT APPROX 7 O'CLOCK POS. INSPECTED DENT FOUND TO BE 2" DI A BY .045" DEEP WITH DISBOND. PERMANENT REPAIR WITHIN ONE WEEK PER EO DC8 7110 4284 C. TRANSFERRED TO D3681 89. 2 L 7 4 4F RT 4A25 2008020600217 20080206 00217 EA 2008 2 6 MASA200800034 1 20080117 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA MLG DOOR OUT OF ADJUST A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651ML 7139 FLT 7297, ORD, GEAR DISAGREE MASTER WARNING/NOSE DOOR OPEN AFTER GEAR RETRACTION. ADJUSTED S23 PROX SENSOR, OPS CHECK G OOD. 2 L 7 2 4F RT A21EA 2008020600218 20080206 00218 EA 2008 2 6 MASA200800035 1 20080117 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 926LR 15026 ASH FLT 2920 PHX - EMERGENCY FLOOR LIGHT 15A ONE LAMP INOP. RELAMPED. 2 L 7 2 4F RT A21EA 2008020600220 20080206 00220 EA 2008 2 6 MASA200800066 1 20080124 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 27314 7314 ASH FLT 7333 ORD-TVC - CREW REPORTED ODOR OF SMOKE IN COCKPIT. MX TROUBLESHOT AND COULD NOT FIND ANY FAULTS, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008020600221 20080206 00221 NM 2008 2 6 NOCA005 1 20080121 A 3350 59192 POWER STRIP BOEING 767 767304 NM CABIN MALFUNCTIONED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 769NA 28039 E-PATH LIGHTS INOP ON LEFT SIDE FROM ROW 25-28. INSTALLED NEW CROSSOVER POWER STRIP PER MM 33-51-10, OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2008020600228 20080206 00228 NM 2008 2 6 NOCA006 1 20080121 A 3350 59192 POWER STRIP BOEING 767 767304 NM CABIN MALFUNCTIONED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 769NA 28039 E-PATH LIGHTS INOP ADJACENT TO R2-LAV. INSTALLED NEW CROSSOVER STRIP PER MM 33-51-10, OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2008020600232 20080206 00232 2008 2 6 MASA200800069 2 20080127 A 7261 755469D IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 ENGINE LEAKING A MASA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 37208 16125 7208 ASH 7403 IAD-HSV - AIRCRAFT DIVERTED TO CHA FOR NR 2 ENGINE LOW OIL PRESSURE WARNING MESSAGE IN FLIGHT. ENGINE WAS SHUT DOWN IN FLIGHT. REPLACED IDG AND GARLOCK SEAL AND OIL PRESSURE O-RING. 2 L 7 2 4F RT A21EA 2008020600236 20080206 00236 NE 2008 2 6 NOCA004 2 20080118 A 7321 07482CN182OM33P1 EEC BOEING 767 76736N 1385152 NM PWA 4060 PW4060 52119 NE RT ENGINE MALFUNCTIONED A NOCA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 15 768NA 29898 DURING CLIMBOUT HAD EXCESSIVE AIRFRAME VIBRATION, NO EICAS MSG. REDUCED THRUST, VIBRATION WENT AWAY. RETURNED TO BAH. NO DOOR LIGHT INDICATIONS, ENGINE LIMITS AND ENGINE INDICATIONS WAS NORMAL. AN EXTERIOR INSPECTION WAS ACCOMPLISHED PE R M/M 05-51-38 TASK 201 TO INCLUDE THE FUSELAGE ALL WING SURFACES AND WING TIPS, VERTICAL FIN AND RUDDER WITH THE FLAPS EXTENDED AND AGAIN WITH THE FLAPS RETRACTED NO FAULTS WERE FOUND. INSPECTED ENGINE PANELS AND DOORS ALL NORMAL. CARGO BINS ALSO INSPECTED ALL FOUND TO BE NORMAL. ACCOMPLISHED ENGINE HIGH POWER RUN (VIBRATION SURVEY TEST 6) PER M/M 71-00- 00-735-320-H00, ALL PARAMETERS WERE NORMAL WITH ENG NR 1 VIB .9 AND ENG NR 2 VIB 1.2 THE HIGHEST READING AT HIGH POWER. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020400001 20080204 00001 SW 2008 2 4 WGEA200800014 1 20080129 A 3240 30266B BRAKE ECLIPS EA500 ECLIPSEEA500 3350000 SW MLG MALFUNCTIONED E WGEA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 27 161DJ 31 000078 LEFT BRAKE FEELS SPONGY ON BOTH PILOTS PEDALS. PUMPING THE PEDAL DOES NOT BRING THE PRESSURE BACK. ACCESSED ALL TUBIN G CONNECTIONS TO ALL LEFT BRAKE COMPONENTS, ALL TUBING RUNS CHECKED FOR SECURITY AND LEAKAGE, ALL CHECKED GOOD. VERIFIE D PROPER RESERVOIR SERVICE, REPLACED LEFT BRAKE WITH NEW UNIT AND PERFORMED A SATISFACTORY BLEED, LEAK AND OPS CHECK IAW EA500 MM 32-41-15. 1 L 7 2 4J RT A00002AC 2008020400029 20080204 00029 WP 2008 2 4 AALA200800044 1 20080108 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AA 49173 LGA - EMERGENCY LIGHT AT FORWARD GALLEY CEILING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT A FORWARD GALLEY CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020400068 20080204 00068 EA 2008 2 4 SWIA200819143 1 20080124 A 5241 HANDLE CNDAIR CL600 CL6002C10 1390015 EA GALLEY DOOR BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 613SK 10038 GALLEY DOOR OUTER HANDLE BROKE OFF WHILE OPENING, FLIGHT NR 4046. REPLACED SERVICE DOOR OUTER HANDLE AS PER AMM 52-41-0 3. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008020400077 20080204 00077 WP 2008 2 4 AALA200800056 1 20080112 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 481AA 49656 BOS - EMERGENCY LIGHT AT SEAT ROWS 20 TO AFT CABIN. REPAIRED WIRE FOR EMERGENCY LIGHT AT SEAT ROWS 20 TO AFT CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020400081 20080204 00081 NM 2008 2 4 AALA200800067 1 20080111 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 978AN 30100 TUL - EMERGENCY SEAT MOUNTED LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY SEAT MOUNTED LIGHTS AT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008020800026 20080208 00026 SO 2008 2 8 RAIA00801031 1 20080127 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 822HK 145069 PRE FLT 5504 - STL - EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE AFFECTED LIGHT. SYSTEM CHE CKED GOOD. 2 L 7 2 4T RT T00011AT 2008020800034 20080208 00034 EU 2008 2 8 AALA200800075 1 20080116 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 41063 506 JFK - EMERGENCY EXIT SIGN AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN AT LEFT NU MBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008020800038 20080208 00038 WP 2008 2 8 AALA200800078 1 20080116 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9403W 53139 LGA - EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD FIRS T CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800049 20080208 00049 WP 2008 2 8 DHL2007873507 1 20080101 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1595-1602 MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 89073 46091 REPAIR ON FUSELAGE EXTERIOR NOT IN ACCORDANCE WITH SRM (STA 1595.000 - 1602.000 L-21L TO L-23L) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1-5. REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-20D. CUT OUT DAMAGED S ECTION AND FABRICATED REPAIR DOUBLER FILLER AND INTERNAL FINGER DOUBLER IAW SRM 53-2-1 FIG 7 SHEET 1, 5, SRM 53-4-1 FIG 17A. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIG 7 SH EET 1, 2, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2008020800060 20080208 00060 NM 2008 2 8 USAA920080242 1 20080123 A 5320 69353521 TIE CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED TIE CLIP, BS 727D, S26L. REPLACED TIE CLIP, BS 727D, S26L IAW B737 SRM 51-40-0 2. 2 L 7 2 4F RT A16WE 2008020800062 20080208 00062 NM 2008 2 8 USAA920080244 1 20080115 A 5311 65C35243 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CORROSION ON FRAME, BS 847, S24R. REPLACED FRAME, BS 847, S24R IAW B737 SRM 51-40-00. 2 L 7 2 4F RT A16WE 2008020800064 20080208 00064 NM 2008 2 8 USAA920080255 1 20080117 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q5 CHECK - CRACKED FRAME WEB, BS 178, LBL 17, WL 230. REPAIRED CRACKED FRAME WEB, BS 178, LBL 17, WL 230 IAW B737 SRM 51-70-13. 2 L 7 2 4F RT A16WE 2008020800069 20080208 00069 NM 2008 2 8 USAA920080260 1 20080117 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q5 CHECK - CRACKED FRAME, BS 500A, S9R. REPAIRED FRAME, BS 500A, S9R IAW USAIRWAYS TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2008020800073 20080208 00073 NM 2008 2 8 NWAA080293125 1 20080130 A 2913 887673 PUMP AIRBUS A319 A319114 3930350 NM HYD SYSTEM LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 325NB 8123 1800 1483 EN ROUTE GREEN SYS HYD QUANTITY DECREASING, GOT GREEN HYD LOW PRESS ON ECAM. WENT THROUGH ECAM COM, SHUT-DOWN GREEN HYD SYSTEM PER COM. QUANTITY AMOUNT GRADUALLY DECREASED BELOW AMBER BOX WHEN GOT THE ECAM MESSAGE GREEN LOW PRESS. PER CO M LANDING GEAR ALTERNATE EXTENDED (VERIFIED ON AMMRS) WITH UNEVENTFUL LANDING AND TOWED TO GATE. 2 L 7 2 4F RT A28NM 2008020800074 20080208 00074 EU 2008 2 8 TRBA2008016 1 20080115 A 3222 D227001721 SHOCK ABSORBER AEROSP ATR72 ATR72212 8680945 EU NLG DAMAGED A TRBA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 29 407AT 407 VERY STRONG NOISE IN NOSE GEAR DURING RETRACTION. REMOVED AND REPLACED THE NOSE LANDING GEAR SHOCK ABSORBER IAW MM NR 3 2-21-00. REMOVED AND REPLACED LT NOSE WHEEL ASSEMBLY IAW JIC NR 12-37-32. 2 H 7 2 4T RT A53EU 2008020800075 20080208 00075 SO 2008 2 8 FDKA200802048 1 20080203 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM 6024 ATL (1005 PHX LCL) - EMERGENCY EXIT SIGN OUT OVER LT EXIT DOOR. MX COULD NOT DUPLICATE EMERGENCY LIGHT SYSTEM, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008020800077 20080208 00077 SO 2008 2 8 FDKA200802049 1 20080204 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM 6089 TLH (0618 PHX LCL), EMERGENCY EXIT SIGN OUT OVER LT EXIT DOOR. MX COULD NOT DUPLICATE, EMERGENCY LIGHT SYSTEM, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008020800080 20080208 00080 NM 2008 2 8 USAA920080275 1 20080115 A 5753 113N20033 FLAP BOEING 757 757225 1384959 NM LT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 MCN - MAJOR REPAIR - C11 CHECK - CORROSION ON LEFT WING INBOARD FLAP TRAILING EDGE, FLAP STATION 254.88 - FLAP STA 300. REPAIRED LEFT WING INBOARD FLAP TRAILING EDGE, FLAP STATION 254.88 - FLAP STA 300 IAW B757 SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A2NM 2008020800082 20080208 00082 EA 2008 2 8 QXEA200800044 1 20080125 A 3320 BALLAST CNDAIR CL600 CL6002C10 1390015 EA CABIN LIGHTS ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 605QX 10022 BOI - FLIGHT 2553 - AFTER LEAVING, THE CEILING LIGHT ON FOR A FEW HOURS, A ELECTRICAL ODOR WAS NOTICED AT ROW 4. MAINTE NANCE DISCONNECTED THE BALLAST AT ROW 4 (PS50) AND PLACED THE SYSTEM ON MEL 33-21-1. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008020800083 20080208 00083 NM 2008 2 8 USAA920080277 1 20080107 A 5340 AN5331001827 STRINGER CLIP BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 MCN - MAJOR REPAIR - C11 CHECK - CRACKED STRINGER CLIP, BS 686, S12R. REPLACED STRINGER CLIP, BS 686, S12R IAW TASCK CA RD M1C53607. 2 L 7 2 4F RT A2NM 2008020800086 20080208 00086 EU 2008 2 8 08FDEA00352 1 20080205 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 655FE 20414 742 MCD FLOORBEAM HAS CRACK AT FR23 RBL27 FWD SIDE REPAIRED FLOORBEAM IAW 53-10-15 FIG 212, RESTORE FINISH IAW 51-21-10. 2 L 7 2 4F RT A35EU 2008020800088 20080208 00088 NM 2008 2 8 USAA920080282 1 20080110 A 5347 146T52174 SEAT TRACK BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 1208 - BS 1428, RBL 88.5, WL 200. REPLACED CA BIN SEAT TRACK, BS 1208 - BS 1428, RBL 88.5, WL 200 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008020800089 20080208 00089 NM 2008 2 8 USAA920080283 1 20080112 A 5347 SEAT TRACK BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 347, RBL 85, WL 200. REPLACED CABIN SEAT TRAC K, BS 347, RBL 85, WL 200 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008020800094 20080208 00094 EU 2008 2 8 08FDEA00357 1 20080205 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 655FE 20411 742 MCD FLOORBEAM HAS CRACK AT FR31 LBL67 FWD SIDE REWORKED CRACKED AREA IAW SRM 53-10-15 AND SRM 51-22-0, FINISHED REWORKE D AREA IAW 51-75-10. 2 L 7 2 4F RT A35EU 2008020800096 20080208 00096 NM 2008 2 8 USAA920080285 1 20080113 A 5347 SEAT TRACK BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 347, LBL 55, WL 200. REPLACED CABIN SEAT TRAC K, BS 347, LBL 55, WL 200 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008020800105 20080208 00105 NM 2008 2 8 AALA200800085 1 20080118 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 JFK - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008020800106 20080208 00106 NM 2008 2 8 AALA200800092 1 20080118 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 637AM 24595 SJU - EMERGENCY LIGHTS AT SEAT ROWS 9D TO 15D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 9D T O 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020800109 20080208 00109 WP 2008 2 8 AALA200800095 1 20080118 A 3350 LIGHT DOUG DC9 DC983 3022083 WP SEAT 14D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 961TW 53611 DFW - EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800111 20080208 00111 EU 2008 2 8 SIMA200803101 1 20080128 A 5347 7253725191 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 320AE 21854 5000 340B320 DURING MBV INSPECTION, THE SEAT TRACK AT BL 0.0 WAS FOUND CORRODED. AIRCRAFT WAS OUT OF SERVICE. REMOVED AND REPLACED SEAT TRACK IAW SAAB 340 SRM 53-70-60. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2008020800115 20080208 00115 SO 2008 2 8 FDKA200801044 1 20080129 A 5420 14576590605 VENT EMB 145 EMB145LR 3260212 SO LOWER COWLING CHAFED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 834MJ 145340 THE LOWER VENT GRILL ON THE LT AND RT LOWER COWLING IS CHAFED OUT OF LIMITS. THE DAMAGED GRILL HAS BEEN REMOVED AND REP LACED. 2 L 7 2 4T RT T00011AT 2008020800126 20080208 00126 NM 2008 2 8 AALA200800102 1 20080119 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 957AN 29541 DFW - EMERGENCY LIGHT AT SEAT 12D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008020800129 20080208 00129 NM 2008 2 8 AALA200800109 1 20080119 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AA 22333 JFK - EMERGENCY LIGHT AT MID GALLEY BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT MID GALLEY. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008020800130 20080208 00130 NM 2008 2 8 AALA200800111 1 20080119 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 197AN 32391 DFW - EMERGENCY LIGHT AT AFT LEFT OVERWING EXIT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT AFT LEFT OVERWING EXI T. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020800132 20080208 00132 WP 2008 2 8 AALA200800124 1 20080121 A 3350 WIRE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9617R 53564 DFW - EMERGENCY EXIT MARKER AT FORWARD GALLEY WALL AT FLOOR LEVEL INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY EXIT MARKER AT FORWARD GALLEY WALL AT FLOOR LEVEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800133 20080208 00133 WP 2008 2 8 AALA200800125 1 20080121 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9617R 53564 DFW - EMERGENCY LIGHT AT SEAT 17D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800138 20080208 00138 NM 2008 2 8 AALA200800087 1 20080118 A 2560 STRAP BOEING 767 767323 1385205 NM FLASHLIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 360AA 24041 ORD - EMERGENCY FLASHLIGHT IN CABIN MISSING STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT IN CABIN. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008020800144 20080208 00144 NM 2008 2 8 AALA200800112 1 20080119 A 3350 LENS BOEING 767 767223 1385123 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 325AA 22326 JFK - EMERGENCY LIGHT AT SEAT 31B MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 31B. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008020800145 20080208 00145 NM 2008 2 8 USAA920080288 1 20080109 A 5315 FLOORBEAM BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOORBEAM, BS 347, RBL 10 - RBL 52, WL 200. REPAIRED CABIN S EAT TRACK, BS 347, RBL 10 - RBL 52, WL 200 IAW B767 SRM 53-00-51 REPAIR 1. 2 L 7 2 4F RT A1NM 2008020800146 20080208 00146 NM 2008 2 8 USAA920080289 1 20080109 A 5315 FLOORBEAM BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOORBEAM, BS 1480, LBL 30 - LBL 42, WL 200. REPAIRED CABIN SEAT TRACK, BS 1480, LBL 30 - LBL 42, WL 200 IAW B767 SRM 53-00-51. 2 L 7 2 4F RT A1NM 2008020800149 20080208 00149 NM 2008 2 8 USAA920080292 1 20080110 A 5315 FLOORBEAM BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK - CORROSION ON CABIN FLOORBEAM, BS 1540, RBL 12 - RBL 34, WL 200. REPAIRED CABIN FLOORBE AM, BS 1540, RBL 12 - RBL 34, WL 200 IAW B767 SRM 53-00-51. 2 L 7 2 4F RT A1NM 2008020800150 20080208 00150 NM 2008 2 8 USAA920080293 1 20080112 A 5315 FLOORBEAM BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK - CORROSION ON CABIN FLOORBEAM, BS 1480, RBL 44, WL 200. REPAIRED CABIN FLOORBEAM, BS 14 80, RBL 44, WL 200 IAW B767 SRM 53-00-51. 2 L 7 2 4F RT A1NM 2008020800159 20080208 00159 NM 2008 2 8 AALA200800120 1 20080121 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 368AA 25195 ORD - EMERGENCY LIGHT AT AFT ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT ENTRY DOOR. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008020800160 20080208 00160 NM 2008 2 8 AALA200800113 1 20080119 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 246 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 391AA 27451 AFW - ANGLE CRACKED ON THE FORWARD SIDE OF STATION 246 FLOORBEAM AT APPROXIMATELY LEFT BUTT LINE 45. REPLACED ANGLE AT FORWARD SIDE OF STATION 246 FLOORBEAM AT APPROXIMATELY LEFT BUTT LINE 45. 2 L 7 2 4F RT A1NM 2008020800161 20080208 00161 EU 2008 2 8 MALA080020 1 20080130 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS NO TEST A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 427XJ 340B427 DURING FUNCTION TEST OF EMERGENCY BATTERY CAPACITY, FOUND POWER SUPPLY 21LN FAILED TEST. REMOVED AND REPLACED POWER SUP PLY AT 21LN IAW AMM 33-50-10-04-1. 2 L 7 2 4T RT A52EU 2008020800163 20080208 00163 NM 2008 2 8 QXEA200800053 1 20080131 A 5270 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 419QX 4145 BOI- FLIGHT 2269 - RETURNED TO THE FIELD, BAGGAGE DOOR WARNING. MAINTENANCE FOUND THE HANDLE OUT 1/4" AT PARKING. PERF ORMED OPERATIONAL CHECK OF DOOR WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008020800165 20080208 00165 EA 2008 2 8 QXEA200800054 1 20080130 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA MAIN PAX STUCK A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 610QX 10033 YYC - AFTER PARKING, MAIN CABIN DOOR COULD NOT BE OPEN (HANDLE WON'T MOVE). WHILE WAITING FOR MAINTENANCE, RAMP PERSONE L WAS ABLE TO OPEN THE DOOR FROM THE OUTSIDE, SUSPECT ICE. MAINTENANCE INSPECTED DOOR WITH NO DEFECTS, AND PERFORMED OP ERATIONAL CHECK WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2008020800167 20080208 00167 NM 2008 2 8 QXEA200800055 1 20080131 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM MAIN PAX MALFUNCTIONED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 429QX 4161 HLN - GROUND CREW REPORTS UNABLE TO CLOSE THE AFT PASSENGER DOOR. MAINTENANCE COMPLIED WITH SERVICE LETTER DH8-400-SL-0 03A. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008020800169 20080208 00169 WP 2008 2 8 AALA200800135 1 20080122 A 3350 SHROUD DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 974TW 53624 DFW - EMERGENCY LIGHT AT SEAT 17D HAS MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020600363 20080206 00363 EA 2008 2 6 TRAX200800127 1 20080121 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 874AS 7551 RIGHT AFT EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008020700002 20080207 00002 NM 2008 2 7 ZZDA2008038 1 20080107 A 5311 FRAME BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 A/C STRUCK BY BAG CART. CANTED FRAME 1178 DAMAGED BETWEEN LONG 24R TP BL 0. INSTALLED NEW CANTED FRAME AND SPLICE REPA IR AT STATION 1178 BETWEEN LONGERON 24R AND BL 0 IAW B717 SRM 51-41-02 AND AIRTRAN EA17-53-00939A. MATERIAL USED 7075 T 6 .081. 2 L 7 2 4F TR A6WE 2008020700003 20080207 00003 NM 2008 2 7 ZZDA2008039 1 20080107 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 A/C STRUCK BY BAG CART. SKIN DAMAGE BETWEEN CANTED FRAME 1178 AND 1183. INSTALLED NEW SKIN SECTION AT CANTED FRAME BET WEEN STATION 1178 AND STATION 1200 IAW B717 SRM 51-41-02 AND DRG 9911840. 2 L 7 2 4F TR A6WE 2008020700009 20080207 00009 NM 2008 2 7 ZZDA2008045 1 20080107 A 5320 ANGLE BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 A/C STRUCK BY BAG CART. ANGLE SUPPORT DAMAGE BETWEEN STA 1178 AND 1189. INSTALLED NEW ANGLE SUPPORT FROM STA 1178 TO S TA 1189 IAW SRM 51-41-01 AND SRM 51-41-05 AND DRG 9911839. 2 L 7 2 4F TR A6WE 2008020400158 20080204 00158 NE 2008 2 4 ASAA0852484 2 20080117 A 7321 1853M33P06 EEC BOEING 737 737890 1384527 NM CFMINT CFM567 CFM567B2US 13802 NE NR 2 ENGINE FAULTY A ASAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 02 559AS 35178 894227 AUTO THROTTLE INDICATION "AT LIMIT" ON UPR DU DURING CLIMBOUT WITH THROTTLES NOT TO GREEN LINE (COMMANDED LIMIT) IN LVL CHG VNAV OR VS WITH AIRSPEED LESS THAN IAS WINDOW SETTING. 2ND CLIMB NR 2 EXCEEDED GREEN LIMIT LINE. PILOT DISCONNECTE D AUTOTHROTTLES BEFORE ANY ENGINE LIMIT EXCEEDANCE. REPLACED EEC. PERFORMED INSTALLATION TEST, PASSED. ACCOMPLISHED F IM 22 31 TASK 806. PASSED WITHOUT ERROR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008020400164 20080204 00164 EA 2008 2 4 TRAX200800105 1 20080117 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 844AS 7317 FWD FLOOR SUPPORT ANGLE AT FS 280 CRACKED LEFT SIDE. REMOVED FWD FLOOR SUPPORT ANGLE. LOCATED HOLES ON SERVICEABLE FWD ANGLE PN 600-34017-351 IAW SRM 51-40-11. OK TO INSTALL INSTALLED NEW SERVICEABLE ANGLE IAW SRM 51-42-06. OK APPLY FINIS H A023 TO FASTNERS. APPLIED FINISH TO FASTNERS IAW 200 SRM 51-21-16 2 L 7 2 4F RT A21EA 2008020400166 20080204 00166 SO 2008 2 4 C2XA08TY013 1 20080121 A 3350 602043 SIGN EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27962 145110 RIGHT EMERGENCY ESCAPE HATCH LOWER EXIT SIGN IS INOP. REPLACED RIGHT EMERGENCY ESCAPE HATCH LOWER EXIT SIGN IAW EMB 145 AMM 33-50-11- OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008020400175 20080204 00175 SO 2008 2 4 C2XA08IA029 1 20080117 A 3350 251005 FUSE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14953 145071 IAH - FLIGHT 2099 DURING PREFLIGHT INSPECTION SOME EMERGENCY LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED A FUSE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008020500001 20080205 00001 NM 2008 2 5 QXEA200800048 1 20080125 A 5210 SPRING BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR STUCK A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 426QX 4154 PDX - FLIGHT 2433 - AFT PAX DOOR WILL NOT UNLATCH UNABLE TO ROTATE HANDLE. INSPECTED DOOR, FOUND VENT DOOR SPRINGS NOT MOVING FREELY WITH VENT. CLEANED OLD GREASE FROM SPRINGS, FOUND ALL SPRINGS TO BE SERVICEABLE. APPLIED FRESH SYNTHETIC GREASE. DOOR OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2008020600015 20080206 00015 NM 2008 2 6 USAA920080222 1 20080115 A 5320 654587563 ANGLE BOEING 737 7373Y0 1384671 NM BS 294-312 S17R CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - CORROSION ON R1 DOOR CUTOUT LOWER SILL ANGLE, BS 294.5 - BS 312, S17R, WL 208. REPLACE D R1 DOOR CUTOUT LOWER SILL ANGLE, BS 294.5 - BS 312, S17R, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600046 20080206 00046 EU 2008 2 6 SA08002 1 20080119 A 3397 WIRE AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS SHORTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 717UW 1069 PHL - NUMEROUS SEAT MOUNTED EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED WIRE AT SEAT 20 LT, AND REPLA CED EMERGENCY POWER SUPPLY UNIT, FIN 11WL. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2008020600053 20080206 00053 SO 2008 2 6 C2XA08CL016 1 20080131 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG FAULTY A C2XA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SW 27 11536 145520 CLE FLIGHT 2409 THE CREW REPORTED A AIR/GROUND FAIL MESSAGE IN FLIGHT. THE LANDING GEAR WOULD NOT RETRACT, ALSO RECEIVE D A ENG REV 1&2 DISAGREE MESSAGE ON THE ECIAS. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR AIR/GROUND PROX IMITY SWITCH AND HARNESS. OPERATIONAL CHECKS WERE GOOD. HARNESS P/N 145-21495-405. 2 L 7 2 4T RT T00011AT 2008020600078 20080206 00078 SO 2008 2 6 C2XA08RI015 1 20080122 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG INOPERATIVE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 15980 145202 FLT 2652 - BNA - CREW REPORTED "LG AIR/GND FAIL" CAUTION MESSAGE CAME ON AFTER AIRBORNE AT 100' ARL AND MESSAGE WENT OFF UPON TOUCHDOWN (AIR RETURN). BNA MX FOUND "LG NOSE WOW SW FAIL" MESSAGE ON CMC. MX REMOVED AND REPLACED NLG WOW PROX SW AND PERFORMED TEST FLIGHT SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. AFTER T/O, CREW REPORTED "LG AIR/GN D FAIL" CAUTION MESSAGE CAME ON AFTER AIRBORNE AT 100' ARL AND MESSAGE WENT OFF UPON TOUCHDOWN (AIR RETURN)AGAIN. BNA M X ADJUSTED NLG WOW PROXIMITY SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVIC E. 2 L 7 2 4T RT T00011AT 2008020600085 20080206 00085 EA 2008 2 6 COMA0860042 1 20080102 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 916CA 7014 FLIGHT 5086 - FLAPS FAILED AT 0 DEGREES ON APPROACH INTO LAN. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. COMPLIED WIT H TASK CARD SI-2-27I001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 2008020600088 20080206 00088 NM 2008 2 6 2008UALA00026 1 20080102 A 2421 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 508UA 30909 24744 RTFL DUE TO GENERATOR DRIVE LIGHT ILLUM. *S/D* IDG FAILURE. NO SHOP FINDINGS OTHER THAN NOISY DISCONNECT TEST. UNKNO WN FAILURE ON AIRCRAFT. REPLACED IDG. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600097 20080206 00097 WP 2008 2 6 ABXA080026 1 20080107 A 5310 591236068 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 47612 CENTER AND SIDE WINDSHIELD RIGHT ZEE P/N: 5912360-68 CRACKED. REPLACED RIGHT ZEE IAW SR DWG 09530268, DC9 SRM 51-30-2, 51-30-5 AND JOB CARD EA 53300036-014. 2 L 7 2 4F A6WE 2008020600101 20080206 00101 NM 2008 2 6 USAA920080217 1 20080119 A 5753 6546431280 SKIN BOEING 737 7374B7 1384702 NM RT WING TE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 450UW 24933 CLT - MAJOR REPAIR - C1 CHECK - RIGHT WING OUTBOARD FORE FLAP, INBOARD TRAILING EDGE HAS 6 INCH AREA OF DELAMINATION. R EPLACED RIGHT WING OUTBOARD FOREFLAP IAW B737 AMM 27-51-37. 2 L 7 2 4F RT A16WE 2008020600108 20080206 00108 SO 2008 2 6 C2XA08ON071 1 20080119 A 3020 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO ANTI-ICE SYSTEM MALFUNCTIONED A C2XA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 27 16559 1450603 FLT 0511 - JAX TO MSY - FLIGHT CREW REPORTED A/I DISAGREE MSG ON EICAS. FLIGHT CREW ABORTED T/O AT 65 KNOTS THEN RESET CIRCUIT BREAKERS AND OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008020600119 20080206 00119 WP 2008 2 6 UPS08851607 1 20080111 A 5541 RIB DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 NR 5 RIB FROM BOTTOM OF RUDDER IS CRACKED THROUGH PREVIOUS REPAIR AT RT SIDE AT FRONT SPAR. RUDDER R EPLACED ON N/R 123801. 2 L 7 4 4F RT 4A25 2008020700013 20080207 00013 NM 2008 2 7 ZZDA2008052 1 20080123 A 5320 J066022809 THRESHOLD BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 994AT 55138 AFT CARGO DOOR THRESHOLD HAS CORROSION ALONG LOWER SECTION BEYOND LIMITS. REPAIRED LOWER SECTION AT AFT CARGO DOOR CUTO UT PAN AS PER B717 SRM 53-20-15 FIG 201 REPAIR 7. 2 L 7 2 4F TR A6WE 2008020700031 20080207 00031 NM 2008 2 7 NOCA00908 1 20080118 A 3350 LIGHT BOEING 757 75728A 1384976 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 EMERGENCY STRIP LIGHT OUT ROW 36L. RELAMPED LIGHT, OPS CHECK GOOD PER MM 33-51-05. 2 L 7 2 4F RT A2NM 2008020700051 20080207 00051 NM 2008 2 7 2008UALA00426 1 20080124 A 5313 STRINGER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 294 S10L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FUSELAGE JUST AFT OF STA 294.5 STR 10L UPPER FLANGE IS CRACKED. MAJOR REPAIR: REMOVED DAMAGE. INSTALLED REPAIR STRAP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700055 20080207 00055 NM 2008 2 7 2008UALA00434 1 20080124 A 5210 STRAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR UNSECURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 590UA 28708 DOOR 2L WOULD NOT ARM. FOUND RETAINER STRAP INTERFERENCE. SECURED RETAINER STRAP, DOOR FUNCTIONS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020700056 20080207 00056 2008 2 7 2008UALA00437 4 20080124 A 2565 O-RING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU SLIDE BOTTLE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 LOW BOTTLE. FOUND FILL VALVE O-RING LEAKING. REPLACED BOTTLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700063 20080207 00063 NM 2008 2 7 2008UALA00449 1 20080126 A 2530 3010000801 OVEN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE AFT GALLEY SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 798UA 26928 AFT GALLEY HAD SMOKE AND CONTROL PANEL VERY HOT. ALL AFT GALLEY C/B PULLED. SMOKE HAS DISSIPATED. OVEN SHORT -FOUND O VEN R52 SMOKING. REPLACED OVEN. TURNED ON ALL GALLEY EQUIPMENT NO SMOKE NOTED IN AFT GALLEY,CONTROL PANEL IS NORMAL. ACF T OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008020700065 20080207 00065 NM 2008 2 7 2008UALA00451 1 20080125 A 5230 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FWD CARGO DOOR BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 FWD CARGO DOOR SKIN BENT AT AFT LWR CORNER. MAJOR REPAIR ACCOMPLISHED: RMV'D DAMAGED SKIN. INSTALLED EXTERNAL DOUBLER. 2 L 7 4 4F 4 F RT A20WE E24NE 2008020700069 20080207 00069 NM 2008 2 7 2008UALA00473 1 20080126 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 DOOR R1 FAILS MIDWAY CHECK. FOUND GRIT BAR OUT OF ADJUSTMENT. ADJUSTED GIRT BAR. CHECKS NORAMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020700073 20080207 00073 2008 2 7 2008UALA00479 4 20080128 A 2565 61620468U1 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR DISLODGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 331UA 24192 WHILE OPENING 1L DOOR SLIDE RAFT FELL OUT. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700092 20080207 00092 EA 2008 2 7 COMA0860083 1 20080118 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SO 01 685BR 9764 7712 FLIGHT 5696 - FLAPS FAILED ON TAKEOFF UPON RETRACTION, FAILED AT 18 DEGREES. AIRCRAFT RETURNED BACK TO DSM AND LANDED S AFELY. REMOVED AND REPLACED LEFT I/B FLAP I/B ACTUATOR. 2 L 7 2 4F RT A21EA 2008020700108 20080207 00108 NM 2008 2 7 ZZDA2008060 1 20080114 A 5312 BULKHEAD BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 949AT 55003 FWD BULKHEAD WEB CRACKED ON STA 218 LBL 20". INSTALLED WEB SPLICE REPAIR AT FWD BULKHEAD STA 218 LBL 20" IAW B717 SRM 5 1-70-10. MATERIAL USED FOR FILLER AND DOULBER 7075T6.040 AND 7075T6.050, SIZE 15.5 X 9.75 AND 11.5 X 7.75. 2 L 7 2 4F TR A6WE 2008020700128 20080207 00128 EA 2008 2 7 TRAX200800137 1 20080126 A 2810 FUEL CAP CNDAIR CL600 CL6002C10 1390015 EA FUEL TANK UNSECURE A ASOA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 754EV 10173 FUEL CAP LEFT OFF IN FLT, PERFORMED AIR RETURN LANDED AT 72000 LBS. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2008020700134 20080207 00134 NM 2008 2 7 SWAA080513 1 20080129 A 2560 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 398SW 27692 RIGHT OVERWING EMERGENCY EXIT SIGN FELL OFF. INSTALLED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2008020700139 20080207 00139 NM 2008 2 7 SWAA080526 1 20080129 A 5312 6936642 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED SPV CHECK, FOUND FWD BULKHEAD LT LOWER CHORD CRACKED AT BS 178. REMOVED AND REPLACED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2008020700147 20080207 00147 NM 2008 2 7 HNAA0800044 1 20080119 A 3230 DSC1822 RELAY DHAV DHC8 DHC8102 2809003 NM LANDING GEAR SLOW A HNAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 07 933HA 48968 48968 134 WHILE CLIMBING THROUGH 11,000 FOOT ALTITUDE, THE AIRCRAFT CREW ELECTED TO TEST THE LANDING GEAR SYSTEM. ON EXTENSION, I T WAS NOTED THAT THE GEAR DOORS WERE TAKING A LONGER THAN NORMAL TIME TO CLOSE. MAINTENANCE WAS CONTACTED AND THE DECIS ION WAS MADE TO RETURN TO A MAINTENANCE BASE. MAINTENANCE CHANGED OUT THE TIME DELAY RELAY, 3261-K9, AND PERFORMED AN O PERATIONAL CHECK OF THE SYSTEM. CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008020700148 20080207 00148 NM 2008 2 7 HNAA0800047 1 20080123 A 3350 1317 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 914HA 53 AFT CEILING EMERGENCY LIGHT INOP. REPLACED BURNED OUT LAMP, OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2008020700181 20080207 00181 EA 2008 2 7 TRAX200800140 1 20080127 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 907EV 7648 TWO EXTERIOR EMERGENCY LIGHTS INOP ON RIGHT SIDE OF A/C. 2 L 7 2 4F RT A21EA 2008020700183 20080207 00183 EA 2008 2 7 TRAX200800143 1 20080127 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 878AS 7590 FLAPS FAILED AT 0 ON APPROACH. EMERGENCY EQUIPMENT WAS ON STANDBY AS A PRECAUTION. 2 L 7 2 4F RT A21EA 2008020700191 20080207 00191 EU 2008 2 7 TRAX200800151 1 20080128 A 5720 INTERCOSTAL AEROSP ATR72 ATR72 EU RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 RIGHT WING BOX BETWEEN FR 25-26 INTERCOSTAL CRACKED. RT WING BOX BTW FR 25-26 INTERCOSTAL REMOVED AND REPLACED IAW SRM 51-25-01. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH S.P. 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLI SHED IN ACCORDANCE WITH SRM 51-25-01 2 H 7 2 4T RT 2008020800014 20080208 00014 SO 2008 2 8 RAIA00801029 1 20080125 A 5270 SWITCH EMB 145 EMB145LR 3260212 SO CARGO DOOR LACK OF LUBE A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 839HK 14500829 FLT 7928 PHL-BAG DOOR MESSAGE DURING TAKEOFF ROLL. MAINTENANCE LUBRICATED CARGO DOOR INDICATION SWITCH. SYSTEM CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008020800033 20080208 00033 NM 2008 2 8 AALA200800100 1 20080118 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 944AN 29535 TUL - EMERGENCY LIGHT AT SEAT ROW 19ABC INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 19ABC. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008020800063 20080208 00063 NM 2008 2 8 USAA920080245 1 20080116 A 5711 SPAR BOEING 737 7373G7 1384595 NM RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - RIGHT WING AFT SPAR CHORD CRACKED, WS 135.5. REPAIRED RIGHT WING AFT SPAR CHORD, WS 13 5.5 IAW USAIRWAYS EA 100161. 2 L 7 2 4F RT A16WE 2008020800065 20080208 00065 NM 2008 2 8 USAA920080256 1 20080117 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q5 CHECK - CRACKED FRAME, BS 480, S8R - S9R. REPAIRED FRAME, BS 480, S8R - S9R IAW USAIRWAYS TYPIC AL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2008020800066 20080208 00066 NM 2008 2 8 USAA920080257 1 20080111 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q5 CHECK - CRACKED FRAME, BS 500A, S8R - S9R. REPAIRED FRAME, BS 500A, S8R - S9R IAW USAIRWAYS TYP ICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2008020800071 20080208 00071 NM 2008 2 8 USAA920080273 1 20080127 A 5330 6545775 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 157AW 23779 PHX - MAJOR REPAIR - OVERNIGHT - CRACKED FUSLAGE SKIN, BS 676, S19R. REPAIRED FUSELAGE SKIN, BS 676, S19R IAW B737 SRM 53-00-01-2R. 2 L 7 2 4F RT A16WE 2008020800072 20080208 00072 EU 2008 2 8 NWAA080303240 1 20080130 A 2910 MANIFOLD AIRBUS 320 A320212 3930322 EU HYD SYSTEM LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 340NW 372 YELLOW HYDRAULIC LOW LEVEL AT CRUISE. FOLLOWED ECAM AND COM PROCEDURES. AIRCRAFT LANDED UNEVENTFULLY. REPLACED YELLOW HP MANIFOLD, LEAK CHECKS OK. 2 L 7 2 4F RT A28NM 2008020800076 20080208 00076 NM 2008 2 8 USAA920080274 1 20080107 A 5511 183N15025 SPAR BOEING 757 757225 1384959 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 MCN - MAJOR REPAIR - C11 CHECK - CORROSION ON RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD, STABILIZER STATION 248. 249. REPLACED RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD, STABILIZER STATION 248.249 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008020800093 20080208 00093 EU 2008 2 8 08FDEA00355 1 20080205 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 655FE * 742 MCD FLOORBEAM HAS CRACK AT FR30 LBL 27 FWD SIDE REWORKED AREA IAW 51-75-10 53-10-15 FIG 212, FINISHED REPAIR IAW 51-75-1 0-8. 2 L 7 2 4F RT A35EU 2008020800104 20080208 00104 2008 2 8 WGEA200800018 4 20080201 A 3417 1004353940 PITOT HEAD ECLIPS EA500 ECLIPSEEA500 3350000 SW ZONE 200 FAILED E WGEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 145DJ 106 000057 AT ABOUT 300 FT AGL ON T/O EXPERIENCED STALL WARNING CAS MESSAGE, AND AURAL WARNING PFD NR 1 A/S WAS 120KTS, PFD NR 2 A/ S 145KTS AND MFD AS 145KTS, FOLLOWED BY A/S DISAGREE, STICK PUSHER CAS MESSAGE. DAYJET WO NR 1283 NRI 1. TROUBLESHOT S YSTEM FOUND BAD LEFT AND RIGHT PITOT. AOA PROBES IAW EA500 AMM 34-00-00. REPLACED PROBES IAW EA500 AMM 34-10-10. PERFO RMED LEAK CHECK AND STATIC VERIFICATION CHECK IAW EA500 AMM 34-00-00. ALL SYSTEMS CHECKED GOOD. 1 L 7 2 4J RT A00002AC 2008020800107 20080208 00107 NM 2008 2 8 AALA200800093 1 20080118 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 637AM 24595 SJU - EMERGENCY LIGHTS AT SEAT ROWS 16D TO 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 16D TO 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020800108 20080208 00108 NM 2008 2 8 AALA200800094 1 20080118 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 637AM 24595 SJU - EMERGENCY LIGHTS AT SEAT ROWS 26D TO 36D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 26D TO 36D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020600121 20080206 00121 2008 2 6 F3LA200800039 4 20080127 A 2565 D30665309 SLIDE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE L2 DOOR DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 948FR 140 2836 DURING C1 C CHECK, INSPECTION REPORTED THE L2 DOOR ESCAPE SLIDE HAD A WORN AREA ON THE GIRT PANEL. MAINTENANCE REMOVED THE GIRT BAR FROM THE DAMAGED PANEL AND INSTALLED THE GIRT BAR IN A NEW ESCAPE SLIDE ASSEMBLY IN ACCORDANCE WITH THE REQ UIREMENTS OF AMM 25-62-44-991-031. FOLLOWING INSTALLATION OF THE NEW ESCAPE SLIDE ASSEMBLY, THE INSTALLATION WAS INSPEC TED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008020600143 20080206 00143 NE 2008 2 6 2008UALA00313 2 20080121 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 LEAKING A UALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 663UA 27160 724652 RTFL UNDER AMBER ALERT DUE TO ELECTRICAL ODOR. REMOVED NR 2 ENGINE AFTER CONFIRMATION OF DIAGNOSTIC TEST FLT. LABEL ENG INE REMOVAL REASON AS CABIN OIL ODOR & CHRONIC HUNG START. OIL SMOKE ENTERING THROUGH THE BLEED INLETS. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020600150 20080206 00150 NM 2008 2 6 UPS08M51556 1 20080127 A 3350 BULB DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 LEFT EMERGENCY LIGHT BULB INOP. RELAMPED EMERGENCY LIGHT BULB PER AMM 33-13-01. OPS CHECK GOOD. 2 L 7 3 4F RT A22WE 2008020600184 20080206 00184 EA 2008 2 6 DATA200800001 2 20080119 A 7261 310079001 OIL CAP STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA RT ENGINE LOOSE E DATA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 13 2629P SH3079 PCE84295 DURING CRUISE ABOUT 30 NM OUT MYR, THE RIGHT ENGINE OIL PRESS LIGHT WAS FLICKERING BETWEEN 90-140 PSI ALL THE WHILE DECR EASING. WHEN IT DROPPED BELOW 90 PSI THE FLIGHT CREW REDUCED TORQUE TO 2000 PSI AND CONSULTED THE QRH. 46 NM FROM CAE, THE OIL PRESSURE GAUGE READ DECREASED BELOW 60 PSI AT THIS TIME THE FLIGHT CREW DECIDED TO SHUT DOWN THE ENGINE. THE L ANDING WAS UNEVENTFUL. 2 H 7 2 4T 4 T A41EU E4EA 2008020600193 20080206 00193 WP 2008 2 6 UPS08851539 1 20080105 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FS 8 RBL 54 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 INTERCOSTAL BROKEN IN MAIN CABIN SUBFLOOR, STA 8 RBL 54 AT MAIN A/C DUCT. STOP DRILLED CRACK ON INTE RCOSTAL AT MAIN CABIN STA 8 RBL 54. FABRICATED AND INSTALLED REPAIR DOUBLER ON INTERCOSTAL AT MAIN CABIN STA 8 RBL 54 I AW SRM 53-02-00, 53-02-00 FIG 001B, AND DWG 5888479. 2 L 7 4 4F RT 4A25 2008020600209 20080206 00209 WP 2008 2 6 08FDEA00323 1 20080129 A 5230 AFA71321 FITTING DOUG DC10 DC1030F 3023504 WP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 ACCOMPLISHED AN INITIAL BHEC INSPECTION OF THE NR 2 MCD SPOOL BRACKET BOLT BORES IAW NTSPM 06-10-01.003 AND EA 8-5230-11 7632, STEP C. ALL FOUR BORE HOLES (A, B, C AND D) HAVE CRACK/CORROSION INDICATIONS. REAMED BOLT BORES IAW SRM 53-50-0 0 VOL I FIG 17 PG 81 AND ACCOMPLISHED BHEC OF BOLT BORES IAW NTSPM 06-10-01.003 AND FOUND CRACK INDICATION REMAINING IN BORE HOLE D (LWR JAMB SUPPORT FITTING ONLY). REMOVED SUPPORT FITTING, LOCATED AND DRILLED NEW FITTING AND INSTALLED IAW SRM 53-50-00 VOL I FIG 17 PG 81 AND 51-33-01 VOL II PG 1. FABRICATED REPAIR BUSHINGS AND INSTALLED IAW SRM 53-50-00 VO L I FIG 17 PG 81. 2 L 7 3 4F RT A22WE 2008020600234 20080206 00234 NM 2008 2 6 NOCA003 1 20080111 A 5730 PANEL BOEING 767 767324 1385203 NM RT WING TORN A NOCA K NONE O OTHER UK UNKNOWN 1 EA 15 767NA 27569 LEADING EDGE PANEL ON RIGHT WING INBOARD BELOW INBOARD LEADING EDGE SLAT PANEL IS TORN / DELAMINATED. PERFORMED TEMP RE PAIR ON PANEL 611CB PER BOEING SERVICE REQUEST 1-750124783-5. PANEL SERVICEABLE FOR ONE TIME FLIGHT. 2 L 7 2 4F RT A1NM 2008020600240 20080206 00240 NM 2008 2 6 USAA920080202 1 20080112 A 5320 654797321 SHEAR WEB BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED SHEAR WEB, BS 639, S17L, WL 208. REPLACED SHEAR WEB, BS 639, S17L, WL 208 I AW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600241 20080206 00241 NM 2008 2 6 USAA920080203 1 20080112 A 5320 66244912 FITTING BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED R1 DOOR CUTOUT INTERCOSTAL CLIP / FITTING BS 328, S8R. REPLACED R1 DOOR CUTO UT INTERCOSTAL CLIP / FITTING, BS 328, S8R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600242 20080206 00242 NM 2008 2 6 USAA920080204 1 20080112 A 5320 69489852 FITTING BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED L1 DOOR CUTOUT INTERCOSTAL CLIP, BS 360, S8L. REPLACED L1 DOOR CUTOUT INTERCO STAL CLIP, BS 360, S8L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600251 20080206 00251 NM 2008 2 6 USAA920080225 1 20080112 A 5320 694898512 FITTING BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - CRACKED CLIP, BS 360, S13L. REPLACED CLIP, BS 360, S13L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600257 20080206 00257 EU 2008 2 6 08FDEA00325 1 20080130 A 2910 NSA93412101C MODULE AIRBUS 300 A300F4605R 3930327 EU HYD SYSTEM FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 669FE 774 AFTER POWER TO FLEX AROUND 40K HAD TO ABORT TAKEOFF DUE TO YELLOW HYD LOW AER ECAM, AFTER ABORT, ALL RESET TRIED AGAIN S AME OUTCOME ABORTED T/O AROUND 52K. REMOVED AND REPLACED YELLOW SYSTEM RESERVOIR CHECK VALVE. REMOVED AND REPLACED DIO DE MODULE 35VD. ALL ENGINE AND HYDRAULIC INDICATIONS CHECK NORMAL PER A 300 JRH. 2 L 7 2 4F RT A35EU 2008020600258 20080206 00258 NM 2008 2 6 UPS08M51478 1 20080119 A 7830 STRUCTURE DOUG MD11 MD11F 3023600 NM THRUST REVERSER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP 48745 NR 2 T/R RT UPPER ACT ATTACH POINT STRUCTURE CRACKED. DEFERRED NR 367364. REMOVED AND REPLACED 3 AND 4 O'CLOCK POSITIO N STIFFENERS PER ASSY DRAWING 491B1330033. ACCOMPLISHED PERMANENT REPAIR ON STIFFENERS AT 1 AND 2 O'CLOCK POSITIONS PER MRA CMM 78-33332-02 REPAIR 6. THIS CLEARS D367364. 2 L 7 3 4F RT A22WE 2008020600259 20080206 00259 NM 2008 2 6 USAA920080228 1 20080110 A 5753 6546435273 FLAP BOEING 737 7373Y0 1384671 NM LT WING DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - LEFT WING OUTBOARD AFT FLAP HAS 2 AREA OF DISBOND, WBL 232 - WBL 241 AND WBL 247 - WBL 250. REPAIRED LEFT WING OUTBOARD AFT FLAP, WBL 232 - WBL 241 AND WBL 247 - WBL 250 IAW B737 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2008020600264 20080206 00264 NM 2008 2 6 USAA920080235 1 20080117 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED STRINGER CLIP, BS 277, S11R. REPLACED STRINGER CLIP, BS 277, S11R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020800152 20080208 00152 NM 2008 2 8 USAA920080295 1 20080108 A 5320 140N250532 FITTING BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 MCN - MAJOR REPAIR - C11 CHECK - CRACKED CABIN FLOOR WEB CLIP, BS 1420 - BS 1440, BL 0, WL 208. REPAIRED CABIN FLOOR WE B CLIP, BS 1420 - BS 1440, BL 0, WL 208 IAW B757 SRM 53-0-51-2R FIGURE 1. 2 L 7 2 4F RT A2NM 2008020800158 20080208 00158 NM 2008 2 8 AALA200800118 1 20080120 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 689AA 25731 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 11D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020800162 20080208 00162 NM 2008 2 8 ASAA0842517 1 20080108 A 5210 507945 SKIN BOEING 737 737490 1384715 NM L1 DOOR DEFORMED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 L1 DOOR UPPER AFT CORNER DEFORMED INSTALLED EXTERNAL DOUBLER TO L1 DOOR AFT UPPER CORNER PER EA 5210 01238 AND SRM 52 00 01, 51 40 03. 2 L 7 2 4F RT A16WE 2008020800175 20080208 00175 NM 2008 2 8 AALA200800122 1 20080121 A 2910 DRAIN BOEING 757 757223 1384957 NM HYD SYSTEM CRACKED A AALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 21 626AA 24584 ORD INFLIGHT T538/21JAN - RIGHT HYDRAULIC QUANTITY INDICATION ILLUMINATED SHOWING DECREASE IN FLIGHT. LANDED ORD WITHOU T INCIDENT. FOUND HYDRAULIC DRAIN ON NR 2 ENGINE CRACKED. REPLACED HYDRAULIC DRAIN ON NUMBER TWO ENGINE. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020800178 20080208 00178 WP 2008 2 8 AALA200800130 1 20080121 A 3350 LAMP DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9617R 53564 DFW - EMERGENCY EXIT MARKER AT AFT GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT MARKER AT AFT GALLEY. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800191 20080208 00191 2008 2 8 BB08009 4 20080128 A 3140 8221033100 COMPUTER BOEING 757 7572S7 1384962 NM EICAS MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 905AW 70247 19338 23567 HNL FLT 125 HNL-PHX LEFT EICAS PROBLEM, FLIGHT CREW DECISION TO RETURN-TO-FIELD. MAINTENANCE REPLACED LEFT EICAS COMPU TER & LOADED SOFTWARE. 2 L 7 2 4F RT A2NM 2008020800193 20080208 00193 NM 2008 2 8 USAA920080298 1 20080130 A 5311 6546541504 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME UPPER CHORD, BS 663.75, S3L, S1, S2R, S3R. REPAIRED FRAME UPPER CHORD, B S 663.75, S3L, S1, S2R, S3R, IAW B737 SRM 53-00-07-2R9 FIGURE 201. 2 L 7 2 4F RT A16WE 2008020800194 20080208 00194 NM 2008 2 8 USAA920080300 1 20080130 A 5340 693535214 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - STRINGER TIE CLIP, BS 787, S9R. REPAIRED STRINGER TIE CLIP, BS 787, S9R, IAW BOEING 73 7 SRM 51-40-02-0G FIGURE 8, 12, 13 & 14. 2 L 7 2 4F RT A16WE 2008020800196 20080208 00196 NM 2008 2 8 SWAA080543 1 20080130 A 5340 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008020800198 20080208 00198 NM 2008 2 8 SWAA080542 1 20080130 A 5514 6547500 STIFFENER BOEING 737 7373TO 138447G NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 16Y CHECK, FOUND LT HORIZONTAL STABILIZER VERTICAL STIFFENER CRACKED AT STA 120. REMOVED AND REPLACED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2008020800200 20080208 00200 NM 2008 2 8 SWAA080552 1 20080130 A 5315 6546811 FLOORBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM TEE CAP CORRODED AT BS 689.5, LBL 45. REMOVED AND REPLACED TEE CAP PER SRM. 2 L 7 2 4F RT A16WE 2008020800201 20080208 00201 NM 2008 2 8 SWAA080553 1 20080130 A 5311 6545811 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 320, STR 21L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008020800202 20080208 00202 NM 2008 2 8 SWAA080554 1 20080130 A 5311 6545814 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 336, STR 21L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008020800203 20080208 00203 NM 2008 2 8 SWAA080555 1 20080130 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 28R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020800207 20080208 00207 NM 2008 2 8 SWAA080584 1 20080131 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM UPPER TEE CAP CRACKED AT BS 727B, LBL 45. REPAIRED FLOORBEAM TEE CAP PER S WA EA. 2 L 7 2 4F RT A16WE 2008020600267 20080206 00267 SW 2008 2 6 PNSA080103 1 20080118 A 2720 UNKNOWN SWRNGN SA227 SA227AC 8780603 SW RUDDER SYSTEM MALFUNCTIONED A PNSA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 AL 03 41NE AC741B ON CLIMBOUT REALIZED HAD LITTLE IF NO LT RUDDER. DECLARED EMERGENCY BECAUSE OF FLIGHT CONTROL MALFUNCTION. LANDING WAS UNEVENTFUL. 2 L 7 2 4T RT A8SW 2008020600269 20080206 00269 EA 2008 2 6 COMA0860043 1 20080102 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 933CA 7040 FLIGHT 5560 - FLAPS FAIL CAUTION MESSAGE DURING APPROACH TO BTV. AIRCRAFT DIVERTED BACK TO JFK AND LANDED SAFELY. COMP LIED WITH TASK CARD SI-2-27I001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 2008020600276 20080206 00276 NM 2008 2 6 NOCA00208 1 20080113 A 3350 767 LIGHT BOEING 757 75728A 1384976 NM EXTERIOR INOPERATIVE A NOCA K NONE O OTHER NR NOT REPORTED 1 EA 15 752NA 28174 R-4 DOOR OUTSIDE EMERGENCY LIGHT DOESN'T ILLUMINATE. RELAMPED L1 EMERGENCY LIGHT, OPS CHECKS OK. 2 L 7 2 4F RT A2NM 2008020600277 20080206 00277 NM 2008 2 6 NOCA00308 1 20080111 A 5730 PANEL BOEING 767 767324 1385203 NM RT WING DELAMINATED A NOCA K NONE O OTHER UK UNKNOWN 1 EA 15 767NA 27569 LEADING EDGE PANEL ON RIGHT WING INBOARD BELOW INBOARD LEADING EDGE SLAT PANEL IS TORN / DELAMINATED. PERFORMED TEMP RE PAIR ON PANEL 611CB PER BOEING SERVICE REQUEST 1-750124783-5. PANEL SERVICEABLE FOR ONE TIME FLIGHT. 2 L 7 2 4F RT A1NM 2008020600285 20080206 00285 NM 2008 2 6 2008UALA00204 1 20080113 A 5320 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 805UA 783 SILL AT DOOR 2R CORRODED AROUND GIRT BAR FITTINGS. ACCOMPLISHED MAJOR REPAIR AT DEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600287 20080206 00287 EU 2008 2 6 2008UALA00206 1 20080111 A 5210 CYLINDER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 405UA 452 DOOR 1L EMERGENCY CYLINDER PRESSURE GAUGE READS ZERO. SERVICED CYLINDER TO FULL. NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600292 20080206 00292 EU 2008 2 6 2008UALA00251 1 20080113 A 3510 MF100511 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 459UA 1192 FWD OXYGEN MASK-CAPT SIDE WILL NOT TEST IN CRADLE. MASK WAS NOT POSITIVELY STOWED, THUS STILL ON. SWITCHED OUT CAPT/FO AND STOWED PROPERLY. ALL NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600303 20080206 00303 NM 2008 2 6 2008UALA00366 1 20080121 A 5315 141T510410 STIFFENER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 671UA 30026 CRACKED VERTICAL STIFFENER ANGLE ON FLOORBEAM AT STA 246 LBL 26. REMOVED AND REPLACED STIFFENER. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020600304 20080206 00304 NM 2008 2 6 2008UALA00368 1 20080121 A 2432 BATTERY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE E&E BAY FAULTY A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 674UA 29242 MAIN BATTERY CHARGER EICAS MESSAGE WILL NOT CLEAR. REPLACED MAIN BATTERY AND CHARGER PER MM24-31-01 AND 24-31-02. MES SAGE CLEARED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020600309 20080206 00309 NM 2008 2 6 2008UALA00376 1 20080122 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FUSELAGE LOWER HINGE CUTOUT AT FWD ENTRY DOOR HAS TWO FASTENER HOLES WITH CRACK INDICATIONS. ONE ABOVE AND ONE BELOW FW D END OF THE CUTOUT. REMOVED DAMAGE. INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600313 20080206 00313 NM 2008 2 6 2008UALA00380 1 20080123 A 3510 OXYGEN MASK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW O2 LEAKING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 385UA 24660 CREW OXYGEN SYSTEM FAILS LEAK CHECK. REPLACED OBSERVERS MASK. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600314 20080206 00314 NM 2008 2 6 2008UALA00381 1 20080122 A 3510 CYLINDER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU OXYGEN SYSTEM INACCURATE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 385UA 24660 READING ON COCKPIT OXYGEN PRESSURE GAUGE OVER 100 PSI DIFFERENCE FROM CYLINDER GAUGE. REPLACED OXYGEN CYLINDER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600324 20080206 00324 NM 2008 2 6 2008UALA00398 1 20080123 A 2750 SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE JACKSCREW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 LEFT O/B FLAP I/B SIDE TRACK, FWD LWR JACK SCREW SUPPORT CRACKED. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600327 20080206 00327 NM 2008 2 6 2008UALA00401 1 20080124 A 2597 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COFFEEMAKER BURNED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 594UA 28145 F/A REPORTED HOT ODOR IN AREA OF AFT GALLEY SHORTLY AFTER TAKEOFF. FOUND COFFEE MAKER HEATER SHORTED WITH WIRES BURNED. REPAIRED WIRING, REPLACED HEATER, COFFEE MAKER OPS CHECKED NORMAL. NO REPEATS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600336 20080206 00336 SO 2008 2 6 C2XA08SH012 1 20080125 A 5210 14534499002 DOOR FRAME EMB 145 EMB145LR 3260212 SO MAIN DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18556 145595 SHV - DURING C-CHECK BOTTOM OF MAIN DOOR FRAME HAS CORROSION AROUND NUT PLATES. MX INSTALLED DOUBLER ON FWD DOOR HALF I AW EC 5212-01159. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008020800209 20080208 00209 NM 2008 2 8 SWAA080587 1 20080131 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 24R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008020800210 20080208 00210 NM 2008 2 8 SWAA080586 1 20080131 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CACKED AT BS 767, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020800211 20080208 00211 NM 2008 2 8 SWAA080585 1 20080131 A 5311 6546536 BELTFRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 616, STR 17L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008020800213 20080208 00213 NM 2008 2 8 SWAA080560 1 20080130 A 5754 65C26601 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED C4 CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008020800215 20080208 00215 NM 2008 2 8 SWAA080561 1 20080130 A 3350 OL3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 2 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008020800216 20080208 00216 2008 2 8 SWAA080562 4 20080131 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 454WN 29851 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008020800217 20080208 00217 2008 2 8 SWAA080563 4 20080131 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 492WN 33866 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008020800225 20080208 00225 NM 2008 2 8 SWAA080568 1 20080130 A 5754 65C26601 SLAT BOEING 737 7373L9 1384470 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 22Y CHECK, FOUND LT WING NR 3 L/E SLAT CRACKED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 2008020800232 20080208 00232 NM 2008 2 8 SWAA080571 1 20080131 A 2560 6557463 FITTING BOEING 737 737317 138447P NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2008020800235 20080208 00235 NM 2008 2 8 SWAA080572 1 20080131 A 5322 6546546 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020800247 20080208 00247 NM 2008 2 8 SWAA080590 1 20080202 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, STR 5R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008020800248 20080208 00248 2008 2 8 SWAA080611 4 20080201 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008020800258 20080208 00258 NM 2008 2 8 SWAA080595 1 20080201 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008020800260 20080208 00260 NM 2008 2 8 SWAA080596 1 20080203 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 382SW 26588 RIGHT AFT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008020800262 20080208 00262 WP 2008 2 8 AALA200800165 1 20080124 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 479AA 49654 LGA - EMERGENCY LIGHTS AT SEAT ROWS 20 TO 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 20 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020800264 20080208 00264 NM 2008 2 8 SWAA080597 1 20080201 A 3350 OL3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED SPV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008020600339 20080206 00339 EA 2008 2 6 COMA0860052 1 20080105 A 3260 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAILED A COMA K NONE N FALSE WARNING AP APPROACH 1 SO 01 912CA 24063 7011 FLIGHT 5367 - ON APPROACH TO CVG RECEIVED WOW INPUT AND OUTPUT CAUTION MESSAGE ALONG WITH NWS INOP CAUTION MESSAGE. EME RGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED PSEU. 2 L 7 2 4F RT A21EA 2008020600348 20080206 00348 EA 2008 2 6 COMA0870004 1 20080119 A 2710 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA AILERON MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 669CA 10176 FLIGHT 5448 - ABORTED TAKEOFF DUE TO CONFIG AILERON WARNING MESSAGE. COMPLIED WITH FAULT ISOLATION TASK FOR CONFIG AILE RON WARNING. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2008020600349 20080206 00349 EU 2008 2 6 2008UALA00447 1 20080125 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE 2R DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 437UA 655 R2 DOOR SILL PLATE HAS 3 SPOTS OF CORROSION AT FR 68. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600350 20080206 00350 EU 2008 2 6 USAA920080269 1 20080123 A 3350 LIGHT AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 632AW 81 FLT 455 - PHX-SLC - EEL - EMERGENCY LIGHTS AT SEAT ROW 9DEF INOP. MAINTENANCE RE-TERMINATED EMERGENCY LIGHT AT 9 RIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2008020600351 20080206 00351 EA 2008 2 6 COMA0860059 1 20080111 A 3010 CLAMP CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYSTEM LOOSE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 914CA 7012 FLIGHT 5045 - ANTI-ICE DUCT MESSAGE DISPLAYED DURING CLIMBOUT AT ABOUT 4000FT. ICE PAGE SHOWS LEFT FUSELAGE IN RED. AI RCRAFT DIVERTED TO TYS AND LANDED SAFELY. DURING INSPECTION OF ANTI-ICE SYSTEM FOUND LOOSE CLAMP ON DUCT ASSY LEFT SIDE AFT OF WING ATTACH POINT. RESECURED CLAMP, NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008020600352 20080206 00352 NM 2008 2 6 2008UALA00454 1 20080125 A 5210 ARM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR HINGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 L-2 DOOR UPPER HINGE ARM CUT OUT IS DAMAGED. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600354 20080206 00354 NM 2008 2 6 2008UALA00543 1 20080130 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1373 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 EXTERIOR FUSELAGE SKIN AT BS 1373 AND STR 28R DENTED. MAJOR REPAIR ACCOMPLISHED: CUT-OUT DAMAGE TO EXTERNAL FUSELAGE A ND FABRICATED REPAIR DOUBLERS AND FILLERS AND INSTALLED. REMOVED CRACKED SHEAR TIE AND FABRICATED A NEW -818 SHEAR TIE A ND INSTALLED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020500005 20080205 00005 NM 2008 2 5 DHLA200800011 1 20080130 A 5270 SWITCH BOEING 727 727214 138407R NM PAX DOOR LACK OF LUBE A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 05 788AT 21958 FLT 194, FWD ENTRY DOOR LIGHT DOES NOT ILLUMINATE WITH DOOR OPEN TEST. TRANSFERED TO DMI 31565 IAW MEL 52-4 CAT C PLAC ARD INSTALLED. CLEANED AND LUBED L1 DOOR WARNING SWITCH, OPS CHK GOOD IAW MM 52-11-01. DMI 31565 CLEARED PLACARDS REMOV ED. ACFT GROUNDED. 2 L 7 3 4F A3WE 2008020600009 20080206 00009 NM 2008 2 6 USAA920080197 1 20080111 A 5340 693535214 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 847 S4L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED STRINGER TIE CLIP, BS 847, S4L. REPLACED STRINGER TIE CLIP, BS 847, S4L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600011 20080206 00011 NM 2008 2 6 USAA920080199 1 20080111 A 5340 693535214 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 727E S3R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED STRINGER TIE CLIP, BS 727E, S3R. REPLACED STRINGER TIE CLIP, BS 727E, S3R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600038 20080206 00038 NM 2008 2 6 SWAA080506 1 20080129 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 887 S26L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 887, STR 26L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020600045 20080206 00045 NM 2008 2 6 PIDA08005 1 20080122 A 5312 BULKHEAD BOEING 737 7372K5 138448X NM BS 1016 CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 DURING MAINTENANCE CHECK, NOTED CORROSION ON THE AFT SIDE OF THE BS 1016 PRESSURE WEB AT THE FRAME ATTACHMENT BETWEEN ST R 26LT AND 27LT. CUT ACCESS HOLE IN FUSELAGE SKIN AND REPAIRED PRESSURE WEB AND SKIN PER BOEING SB 737-53A1075. 2 L 7 2 4F RT A16WE 2008020600050 20080206 00050 NM 2008 2 6 2008UALA00305 1 20080118 A 5320 WEB AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 805UA 783 AFT RIGHT CORNER FLOOR WEB BETWEEN FR 69 AND FR 70 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600054 20080206 00054 SO 2008 2 6 C2XA08IA037 1 20080126 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145XR 3260214 SO LT MLG INOPERATIVE A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 27 21129 145703 IAH - FLIGHT 2185, THE CREW REPORTED THAT THE LEFT MAIN LANDING GEAR DISAGREE LIGHT WHEN THE GEAR WAS EXTENDED. THE AIR CRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN GEAR DOWNLOCK PROXIMITY SWITCH , OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008020600055 20080206 00055 SO 2008 2 6 C2XA08IA038 1 20080123 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12996 145296 MCI - DURING MAINTENANCE INSPECTION THE FORWARD OVERWING CEILING EXIT LOCATOR SIGN WAS FOUND TO BE INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED THE NUMBER 6 EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008020600065 20080206 00065 EA 2008 2 6 COMA0860050 1 20080102 A 2750 1104SD100501 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA LT TE FLAPS WORN A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 806CA 7359 FLIGHT 5636 - FLAPS FAIL CAUTION MESSAGE ON APPROACH INTO BOS. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED LEFT SIDE NR 5 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2008020600093 20080206 00093 SO 2008 2 6 C2XA08IA039 1 20080127 A 3210 UNKNOWN EMB 145 EMB145EP 3260221 SO MLG UNKNOWN A C2XA O OTHER O OTHER DE DESCENT 1 SW 27 14939 145030 IAH - FLIGHT 2203, THE CREW REPORTED THAT THE LEFT MAIN GEAR COMES DOWN MUCH FASTER THAN NOSE OR RIGHT GEAR CAUSING YAW. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE OPERATIONALLY CHECKED THE LANDING GEAR EXTENSION & RETRACTIO N SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008020600107 20080206 00107 EU 2008 2 6 BA08001 1 20080121 A 3350 32145410 EPSU AIRBUS 330 A330323 3930335 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 270AY 0315 BFM - MAINTENANCE REPORTED THE EMERGENCY LIGHT EPSU 14WL INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EPSU 14WL. OPERATIONAL CHECK GOOD IAW WITH MM 33-51-38. 2 L 7 2 4F RT A46NM 2008020600131 20080206 00131 WP 2008 2 6 UPS08851488 1 20080123 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 EMERGENCY EXIT LIGHTS INOP. RELAMPED ALL EMERGENCY LIGHTS AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2. OPS C KS NORMAL. ALSO AS A PRECAUTIONARY, REPLACED 51-327 ARM DISARM SWITCH. 2 L 7 4 4F RT 4A25 2008020600146 20080206 00146 WP 2008 2 6 UPS08851555 1 20080102 A 5320 9754034235AAV INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 300-320 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 INTERCOSTAL BETWEEN STA 300-320 RBL48 IN A-PIT HAS EXFOLIATED CORROSION. REMOVED, FABRICATED AND INS TALLED INTERCOSTAL IN A-PIT BETWEEN STA 300 AND 320 AT RBL48 IAW WITH DWG 9754034, SRM 51-01-21, SRM 51-01- 20D, SRM 51- 3-0, SRM 51-1-8 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 2008020600147 20080206 00147 WP 2008 2 6 UPS08851558 1 20080127 A 5730 DOUBLER DOUG DC8 DC873F 302199F WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 WING INTERNAL DOUBLER CRACKED ABOVE NR 4 FILL VALVE. ACCOMPLISHED STEPS 6A1 THRU 6A4 ON PRELIMINARY EO NR DC8-5730-2850 0-A DATED 1-28-08. ACCOMPLISHED STEP 6AS-6AG. OK TO INSTALL REPAIR. COMPLETED REMAINING STEPS THRU 6A(9) OF EO DC8-57 30-28500. 2 L 7 4 4F RT 4A25 2008020600182 20080206 00182 WP 2008 2 6 UPS08851522 1 20080108 A 5320 CHANNEL DOUG DC8 DC871F 302199D WP FS 1766 LBL 8 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 MAIN CABIN "U" CHANNEL HAS HOLE IN RADIUS STA 1766 LBL 8. REMOVED, FABRICATED AND INSTALLED "U" CHAN NEL AT STA 1766 LBL 8 IAW SRM 51-01-21D, AND DWG 5755032. 2 L 7 4 4F RT 4A25 2008020600229 20080206 00229 WP 2008 2 6 UPS08851541 1 20080113 A 5730 SKIN DOUG DC8 DC871F 302199D WP LWS 501 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 LT WING OUTBD SLOT LWR ACCESS PNL HAS DOUBLE DRILLED HOLE. FABRICATED AND INSTALLED REPAIR DOUBLER O N LT WING OUTBD SLOT LWR ACCESS PNL IAW SRM 57-02-00 FIG 002A AND DWG 5769928. 2 L 7 4 4F RT 4A25 2008020600231 20080206 00231 EA 2008 2 6 MASA200800079 1 20080130 A 5270 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT FALSE INDICATION A MASA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 07 504MJ 10066 ASH FLT 7004 MKE-ORD - RT EMERGENCY EXIT CAUTION ON T/O ROLL. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008020600247 20080206 00247 NM 2008 2 6 USAA920080220 1 20080112 A 5320 65479737 SHEAR WEB BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - CRACKED SHEAR WEB, BS 578 - BS 597, LBL 70, WL 208. REPLACED SHEAR WEB, BS 578 - BS 59 7, LBL 70, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600248 20080206 00248 NM 2008 2 6 USAA920080221 1 20080113 A 5320 654587527 STRAP BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - CORROSION ON R1 DOOR CUTOUT LOWER SILL STRAP, BS 277 - BS 294.5, S17R, WL 208. REPLACE D R1 DOOR CUTOUT LOWER SILL STRAP, BS 277 - BS 294.5, S17R, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600249 20080206 00249 NM 2008 2 6 USAA920080223 1 20080115 A 5320 654587547 SILL BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - CORROSION ON R1 DOOR CUTOUT LOWER SILL WEB, BS 291 - BS 332, RBL 54, WL 208. REPLACED R1 DOOR CUTOUT LOWER SILL WEB, BS 291 - BS 332, RBL 54, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080916 NM 2008 9 16 08FDEA03223 1 20080803 A 5315 453N16071 FLOORBEAM BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 BS 1640 RBL 20 TO LBL 20 BULKHEAD FLOOR SUPPORT ANGLE HAS CORROSION. ANGLE ASSY AT BS 1640 BULKHEAD IS REPLACED UNDER E O F-2550-7-5001 PT 1: EQUIPMENT/FURNISHINGS, CARGO COMPARTMENT/LOADING SYSTEMS. REPLACE BS 1640 BULKHEAD, AFT CARGO C OMPARTMENT SB 757-25-0157 R1. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 2 4F RT A2NM 20080916 NM 2008 9 16 08FDEA03225 1 20080804 A 5330 BACR15BB5D4C SKIN BOEING 757 75723A 1384967 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 LT LWR FUSELAGE FROM BS 1480 TO BS 1500, STR 27L AND 28L HAS EXISTING LIGHTNING STRIKE REPAIR. EXISTING REPAIR EVALUATE D AS PER EO F-5100-7-5001 PT1 ATTACHMENT B, FOUND ACCOMPLISHED IAW B757-200 SRM 53-00-01 FIG 201 REPAIR 6 SECT 1, BASED ON EXTERNAL VISUAL EVALUATION OF THE REPAIR. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080916 EU 2008 9 16 08FDEA03468 1 20080818 A 5730 A57340084 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 CORROSION ON LT WING TOP SKIN, AFT OF REAR SPAR, RIB 3-6, AROUND HOLES 119, 120,121 (DRAWING R571-40141) AND CRACK FINDI NG AT HOLE 49. REPAIR PERFORMED BY CORROSION BLEND OUT IAW RAS/BAE/1007607/2008 ISS A , APPROVED BY EA 6-5720-123018. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03469 1 20080818 A 5730 A57340084 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 CORROSION ON RT WING TOP SKIN, AFT OF REAR SPAR, RIB 3-6, AROUND HOLES 118, 119, 120,121 (DRAWING R571-40141). REPAIR PERFORMED BY CORROSION BLEND OUT IAW RAS/BAE/1007607/2008 ISS A, APPROVED BY EA 6-5720-123018. 2 L 7 2 4F RT A35EU 20080916 WP 2008 9 16 08FDEA03096 1 20080728 A 5310 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP DOOR FRAME DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 MAIN CARGO DOOR JAMB AT SPOOL FITTING NR 1, HOLE "A" IS OVERSIZED TO 0.536 INCH. REMOVED SUB STRUCTURE AND WEB TO GAIN ACCESS TO THE NR 1 SPOOL BACK UP FITING IAW SRM 51-31-01;VOL II. LOCATED AND DRILLED NEW BACK UP FITTING AFA 7135-1IAW SRM 51-31-01; VOL II. INSTALLED NEW BACK UP FITTING IAW SRM 51-33-01; VOL II. INSTALLED SNU STRUCTURE AND WEB IAW SRM 51-33-01; VOL II. INSTALLED BUSHING IAW SRM 53-50-00, VOL I. 2 L 7 3 4F RT A22WE 20080916 EU 2008 9 16 08FDEA03551 1 20080822 A 5230 SKIN AIRBUS 300 A300F4605R 3930327 EU BS 1817 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DOOR LOWER AFT CORNED OF THE EXTERIOR SKIN IS GOUGED. REPAIRED THE GOUGED AREA IAW EA 6-5230-123389. 2 L 7 2 4F RT A35EU 20080916 WP 2008 9 16 08FDEA03031 1 20080723 A 5414 AUB7054501 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 NR 1 PYLON PANEL 437 DR INNER SKIN IS CRACKED. RECEIVED NEW PRECOOLER VENTILATOR ASSEMBLY P/N AUB 7054-501, PO 626793.1 . LOCATED AND DRILLED IN REF TO DC/MD-10 SRM 51-31-01; VOL II AND DAC DWG AUB 7054; REF "J". 2 L 7 3 4F RT A22WE 20080916 WP 2008 9 16 08FDEA03473 1 20080818 A 5512 NLC6039502 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 300 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 RT STAB INBD ELEV, XE 136, DENTED ON UPPER SKIN. DIMENSIONS ARE 1 INCH BY 1 INCH BY .075 INCH. REPAIR SKIN IAW SRM 55- 00-01 FIG 3 SHEET 2 VOL.1. 2 L 7 3 4F RT A22WE 20080916 EU 2008 9 16 08FDEA03740 1 20080905 A 5220 A5227106320200 ATTACH ANGLE AIRBUS 310 A310222 3930315 EU DOOR SEAL CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 LEFT OVERWING EMERGENCY EXIT, LOWER SEAL RETAINER OUTBD, 3 EA TEES AND ATTACH ANGLES HAVE CORROSION. CENTER PROFILE ANG LE BEYOND LIMITS IAW SRM 51-40-01. CLEANED 2 EA PROFILE ANGLES IAW SRM 52-53-11. NO DEFECTS NOTED. FABBED A NEW PROFI LE ANGLE IAW DWG A52241063. INSTALLED NEW PROFILE ANGLE IAW SRM 51-40-02. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03741 1 20080905 A 5220 BONDING STRAP AIRBUS 310 A310222 3930315 EU EMERGENCY EXIT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 LEFT OVERWING EMERGENCY EXIT, BONDING STRAPS AND ATTACHING SCREWS (2 EA) ARE CORRODED. REMOVED ANGLE IAW SRM 51-40-01. FABBED ANGLE IAW DWG A52271077, ISSUE "A". AODINED & PRIMED ANGLE IAW SRM 51-21-10. INSTALLED ANGLE & BONDING WIRE I AW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03743 1 20080905 A 5320 A5398038920400 WEB AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 CABIN RIGHT SIDE FLOOR WEB IS CRACKED AT FRAME 77; RBL 75. REMOVED THE CRACKED FLOOR WEB IAW SRM 51-40-21. LOCATED & DRILLED THE NEW WEB IAW DRAWING 18A53980389. INSTALLED WEB IAW SRM 53-18-18. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03295 1 20080807 A 5522 SKIN AIRBUS 300 A300B4622R 3930312 EU LT AILERON MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 743FD 630 FOUND OLD DOUBLER REPAIR ON LT AILERON UPPER SKIN, T/E, RIB 14-15, REPAIR WAS NOT PERFORMED IAW RELATED SRM. REPAIR REN EWED IAW RAS/FOK/163/2008, APPROVED BY EA 6-5761-120087. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03230 1 20080804 A 5313 A53974527224 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON STRINGER P 56 LT, C 64 OUT OF LIMIT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201A. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03232 1 20080804 A 5313 A53974232201 STRINGER SPLICE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON STRINGER COUPLING P 56RH, C 65 OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-1 0. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03233 1 20080804 A 5320 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION AT T-SECTION, C 93, P 23 REPAIR PERFORMED BY CUT OUT AND INSTALLING A REPAIR PROFILE IAW, RAS/EFW/900007 4/2008 ISS A, APPROVED BY EA 6-5319-123033. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03234 1 20080804 A 5753 A5796000720000 SKIN AIRBUS 300 A300F4605R 3930327 EU LT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 LEFT WING INBD FLAP LOWER SURFACE IS DENTED INBD OF THE FLAP TRACK. DENT WAS FOUND TO BE GOUGED. BLENDED GOUGE SMOOTH IAW A300-600 SRM 51-73-10. FLAP SKIN FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 57-50-00, PG 108. CUT OUT THE DAMAGED AREA IAW A300-600 SRM 57-50-00; PGS 220-226. FABRICATED A REPAIR DOUBLER AND BACKING STRIPS IAW A300-600 SRM 57-50-00, PGS 220-226. ALODINED REPAIR PARTS IAW A300-600 SRM 51-21-10. PRIMED AND TOP COATED THE REPAIR DOUBLER AND STRIPS IAW A300-600 SRM 51-23-10. INSTALLED REPAIR IAW A300-600 SRM 57-50-00, PGS 220-226. 2 L 7 2 4F RT A35EU 2008011100048 20080111 00048 2008 1 11 2008UALA0019 4 20080101 A 2565 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 524UA 24977 SLIDE ARMED LIGHT ABOVE DOOR 3R IS ILLUM WHEN SLIDE IS DISARMED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008011100093 20080111 00093 NM 2008 1 11 ZZDA2008001 1 20080101 A 3232 59713305001 ACTUATOR BOEING 717 717200 1383700 NM RT MLG FAILED A ZZDA O OTHER K FLUID LOSS DE DESCENT 1 SO 37 933AT 55071 RIGHT HYD SYS QTY WENT TO "0" ON DESCENT. QRH PROCEDURES FOLLOWED, TOWED TO GATE. REMOVED AND REPLACED RIGHT MLG RETRA CT CYC AND GLAND ASSY IAW AMM 32-33-01 AND C/W EA 17-32-009211R, OPS CHECKS GOOD. NO LEAKS NOTED C/W BOEING SERVICE BUL LETIN 717-31-0013. 2 L 7 2 4F TR A6WE 2008011100183 20080111 00183 NM 2008 1 11 SWAA080139 1 20080106 A 5310 6547980 CREASE BEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 807 TO BS 827, RBL 70. REMOVED AND REPLACED WEB PER SR M. 2 L 7 2 4F RT A16WE 2008011100189 20080111 00189 NM 2008 1 11 SWAA080145 1 20080106 A 2560 6557463 FITTING BOEING 737 7375H4 138449D NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2008020800268 20080208 00268 NM 2008 2 8 SWAA080617 1 20080203 A 5311 6546539 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, RBL 65. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008020800269 20080208 00269 NM 2008 2 8 SWAA080618 1 20080203 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND STRINGER 16L CRACKED AT BS 380. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008020800276 20080208 00276 NM 2008 2 8 SWAA080600 1 20080202 A 3350 MS155721 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008020800278 20080208 00278 2008 2 8 SWAA080601 4 20080201 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008020700118 20080207 00118 SO 2008 2 7 C2XA08IA041 1 20080129 A 2520 13501578537 INSULATION EMB 135 EMB135LR 3260305 SO CABIN LOOSE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 28529 145512 IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED A SMOKE SMELL IN THE CABIN. MAINTENANCE RESECURED INSULATION BLOCKI NG A COOLING FAN, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008020700123 20080207 00123 SO 2008 2 7 C2XA08IA043 1 20080129 A 5730 14567011006 SKIN EMB 145 EMB145EP 3260221 SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13935 145022 IAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE G ROUND SPOILER. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CRACK ON A 500FC DMI, WITH RE-INSPECTIONS TO BE MADE A T EVER 50FC, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008020700159 20080207 00159 NM 2008 2 7 MWEA080020 1 20080130 A 5311 5913537507 DOUBLER BOEING 717 717200 1383700 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 916ME 55178 CORROSION ON STAR DOUBLER LOCATED ON TOP OF FRAME AT STATION 944 AND LONGERON 29 RIGHT. BLENDED CORROSION, FABRICATED A ND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2008020700163 20080207 00163 EA 2008 2 7 HNAA0800049 1 20080127 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8311 1386006 EA CARGO BAY MALFUNCTIONED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 337EN 284 BAG BAY SMOKE WARNING LIGHT ILLUMINATED INTERMITTENTLY AFTER TAKEOFF. REPLACED NR 1 AND NR 2 SMOKE DETECTORS, OPS CK'D GOOD AT THIS TIME. 2 H 7 2 4T RT A13NM 2008020700182 20080207 00182 EA 2008 2 7 TRAX200800141 1 20080127 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 850AS 7355 LEFT SIDE EXTERIOR 2 EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008020800001 20080208 00001 NM 2008 2 8 AALA200800180 1 20080126 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 668AA 25333 DFW - EMERGENCY EXIT LIGHT AT RIGHT AND LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK AT M10758 FOR EMERGENCY LIGHT AT RIGHT AND LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020800011 20080208 00011 NM 2008 2 8 DL76L080122 1 20080126 A 3270 321002859 SKID BOEING 767 767332 1382001 NM AUX DAMAGED A DALA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 SO 27 177DN 25122 FYI - ATB WITH TAIL STRIKE ON TAKEOFF. FOUND TAIL SKID STRIKE DAMAGED. ACCOMPLISHED TIME LIMITED. REPAIR PER ERA 4663 38-14. REPLACED RT STAB POSITION MODULE PER M/M NEEDS CK OUT WHEN H PRESSURE IS AVAILABLE. RT STAB POSITION MODULE OP CKS GOOD AMM MFG NR 80000000-12. REMOVED TAILSKID ACTUATOR. TAILSKID ACTUATOR CHANGED PER AMM LEVER. REPLACED PER AMM AND DOOR FAIRING REPAIRED PER SRM. 2 L 7 2 4F RT A1NM 2008020800016 20080208 00016 NM 2008 2 8 DL738080129 1 20080129 A 5512 172A40025 SKIN BOEING 737 737832 13844CF NM HORIZONTAL STAB PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 374DA 29622 LT HORIZ STAB SKIN CONTACTED TAILDOCK. SKIN PUNCTURE AND UNDER LYING RIB BUCKLED. REPAIRED SKIN WITH DOUBLER AND RIB W ITH FITTINGS AND ANGLES. 2 L 7 2 4F RT A16WE 2008020800051 20080208 00051 NM 2008 2 8 ASAA0842504 1 20080108 A 5210 STRUCTURE BOEING 737 737490 1384715 NM PAX DOOR DEFORMED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 L1 DOOR UPPER AFT CORNER DEFORMED. RECONTOURED AND INSTALLED REPAIR DOUBLER PER EA 5210 01237 AND 5210 01238. 2 L 7 2 4F RT A16WE 2008020800057 20080208 00057 NM 2008 2 8 USAA920080239 1 20080116 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CORROSION ON CABIN FLOORBEAM "T" CAP, BS 312, RBL 10 - RBL 12. REPAIRED CABIN FLOOR BE AM "T" CAP, BS 312, RBL 10 - RBL 12 IAW B737 SRM 53-10-51. 2 L 7 2 4F RT A16WE 2008020800092 20080208 00092 EU 2008 2 8 08FDEA00354 1 20080205 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 655FE 20414 742 MCD FLOORBEAM HAS CRACK AT FR25 RBL27 FWD SIDE REWORKED REPAIR AREA IAW 53-10-15, SRM 51-21-10 AND SRM 51-75-10, FINISHE D REPAIR IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008020800131 20080208 00131 WP 2008 2 8 AALA200800123 1 20080121 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9617R 53564 DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 3 TO 6 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 3 TO 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800134 20080208 00134 NM 2008 2 8 NWAA080316316 1 20080201 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHTS NO TEST A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 676NW 33002 DURING LINE CHECK, FOUND RT UPPER DECK DOOR RIGHT BATTERY PACK FAILED TEST. REPLACED EMERGENCY POWER SYSTEM BATTERY PAC K PER MM 52-23-14. FUNCTION CHECKED GOOD AND AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008020800195 20080208 00195 NM 2008 2 8 USAA920080301 1 20080130 A 5320 65528948 CHANNEL BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - CRACKED MAIN CABIN FLOOR CHANNEL, BS 540, BL 0, WL 208. REPAIRED CRACKED MAIN CABIN FL OOR CHANNEL, BS 540, BL 0, IAW B737 SRM 51-40-04-0G FIGURE 2. 2 L 7 2 4F RT A16WE 2008020800271 20080208 00271 NM 2008 2 8 AALA200800147 1 20080123 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 767AJ 33539 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008020800272 20080208 00272 NM 2008 2 8 SWAA080619 1 20080203 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008020800273 20080208 00273 NM 2008 2 8 SWAA080598 1 20080203 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2008020800284 20080208 00284 NM 2008 2 8 SWAA080612 1 20080202 A 2612 6555707 FIRE LOOP BOEING 737 7373Y0 1384671 NM MLG W/W FAULTY A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 29 682SW 23496 AIR TURNBACK - MLG WHEEL WELL FIRE LIGHT ILLUMINATED DURING CLIMBOUT OF BWI. REMOVED AND REPLACED FIRE LOOP PER MM. 2 L 7 2 4F RT A16WE 2008020800289 20080208 00289 NM 2008 2 8 SWAA080625 1 20080203 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, LBL 7 TO LBL 13. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020800295 20080208 00295 NM 2008 2 8 08FDEA00344 1 20080202 A 5610 5893543109 WINDSHIELD BOEING 727 7272S2F 1384O81 NM COCKPIT CRACKED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 209FE 22931 AT FL310 PILOTS WINDSHIELD BEGAN TO CRACK ON INNER AND OUTER PANELS. REMOVED AND REPLACED CAPT'S WINDSHIELD IAW 727 MM 56-11-011-4. ALSO REPLACED WINDOW HEAT CONTROLLER IAW 30-41-033-4 AND 30-41-013-5. CHECKED WINDOW HEAT CONDUCTIVE COAT ING AND SENSOR PER MM 30-41-042-5 AND WDM 30-41-11 PIN 14 HAS 37.5 OHMS, WHICH IS CORRECT FOR THIS WINDOW A/C OK TO CONT INUE. 2 L 7 3 4F A3WE 2008020800299 20080208 00299 NM 2008 2 8 SWAA080626 1 20080203 A 5322 69353656 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 360, RBL 18. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020800300 20080208 00300 WP 2008 2 8 AALA200800138 1 20080123 A 3230 RING DOUG DC9 DC983 3022083 WP MLG MISSING A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 9615W 53562 ORD INFLIGHT T1715/23JAN - RECEIVED RED NOSE GEAR UNSAFE LIGHT AFTER RETRACTING GEAR ACCOMPANIED BY LOUD AIR NOISE FROM NOSE WHEEL WELL. RECYCLED GEAR AND GEAR CAME DOWN NORMALLY BUT LIGHT WOULD ILLUMINATE AFTER RETRACTION. RETURNED TO OR D AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. FOUND LOWER TWO SCRAPER RINGS MISSING FRO M BOTTOM STRUT SEAL. ACCOMPLISHED NOSE GEAR STRUT REPACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800301 20080208 00301 NM 2008 2 8 SWAA080606 1 20080201 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 711HK 27845 DURING SCHEDULED HC1 CHECK, FWD RIGHT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008020800303 20080208 00303 NM 2008 2 8 SWAA080608 1 20080202 A 3350 3071BPLEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 796SW 27889 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008020800311 20080208 00311 NM 2008 2 8 AALA200800101 1 20080119 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 773AN 29583 NRT - EMERGENCY LIGHT AT FIRST CLASS FORWARD CLOSET MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FIRST CLASS FOR WARD CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008020800317 20080208 00317 NM 2008 2 8 SWAA080630 1 20080204 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 291WN 32539 DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 2008020800318 20080208 00318 SO 2008 2 8 SIMA200803503 1 20080201 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COCKPIT ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 21 640AE 145183 ON FLIGHT 3735, CREW REPORT ON DESCENT BURNING ODOR IN COCKPIT. NOTED SMOKE AT FORWARD WINDSHIELD CENTER POST. SMOKE D ISSIPATED QUICKLY NO OTHER PROBLEMS NOTED AND LANDING WAS NORMAL. AIRCRAFT REMOVED FROM SERVICE. C/W ETN EM 72-034R2 C ABIN ODOR EVENT TROUBLESHOOTING CHECKLIST NO FAULTS OBSERVED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008020800320 20080208 00320 NM 2008 2 8 SWAA080631 1 20080204 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008020800321 20080208 00321 SO 2008 2 8 SIMA200803505 1 20080131 A 5320 14521725613 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 626AE 145117 DURING MBV INSPECTION, FOUND FWD SERVICE DOOR SILL BETWEEN FRAME 17-20 IS CORRODED. REPLACED SILL IAW SRM 51-40-02. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008020800327 20080208 00327 NM 2008 2 8 SWAA080635 1 20080204 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800328 20080208 00328 SO 2008 2 8 SIMA200803502 1 20080201 A 4920 APU EMB 145 EMB145LR 3260212 SO ICED A SIMA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 640AE 145183 ON FLIGHT 4224, CREW REPORT APU FIRE INDICATION DID NOT USE FIRE BOTTLE. PERFORMED APU SHUT DOWN AND INDICATION WENT AW AY, ABNORMAL ODOR NOTED INSIDE CABIN AND FLIGHT DECK. AFTER INSPECTION FOUND APU INLET ALMOST COMPLETELY COVERED WITH I CE. NO PASSENGERS ONBOARD AT THE TIME OF THE INCIDENT DISC-APU FIRE. PERFORMED DVI OF APU COWL INTERNAL AND EXTERNAL S URFACES AND ENGINE ASSEMBLY WITH NO EVIDENCE OF FIRE NOTED. FOUND APU INLET COVERED WITH ICE APU DEFERRED PER MEL 49-01 AUTH NR 020028DM. AIRCRAFT NOT REMOVED FROM SERVICE. PERFORMED OPS CHECK OF APU SYSTEM AND OPERATIONAL CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008020800329 20080208 00329 NM 2008 2 8 SWAA080636 1 20080204 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800330 20080208 00330 NM 2008 2 8 SWAA080637 1 20080204 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800331 20080208 00331 NM 2008 2 8 SWAA080638 1 20080204 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800335 20080208 00335 NM 2008 2 8 SWAA080641 1 20080204 A 5343 6546543 FITTING BOEING 737 7373H4 1384600 NM MLG W/W CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV2 CHECK, FOUND LT MLG SIDE SUPPORT FITTING LUG CORRODED AT BS 685. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800338 20080208 00338 WP 2008 2 8 DHL2007873517 1 20080115 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 719 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 LWR FUSELAGE END FITTING CRACKED 8" STA 719.000 L-34R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMO VED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW F ITTING IAW SRM 51-3-0, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2008020800343 20080208 00343 NM 2008 2 8 SWAA080652 1 20080204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020800345 20080208 00345 WP 2008 2 8 DHL2007873527 1 20080114 A 5751 SKIN DOUG DC8 DC873F 302199F WP AILERON MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 89073 46091 RT OUTBD AILERON UPPER SKIN HAS A NON-STANDARD REPAIR AT STA XA 653.000, MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 5 7-8-1 FIG 4 PG9. REMOVED PANEL PLATING WITH NON-STANDARD REPAIR ON IT IAW SRM 57-1-0 PG1 SRM 51-1-21. FABRICATED PLATI NG, DOUBLER IAW SRM 57-8-1 FIG 4 PG 9 ITEM"F" "G" BONDED BOTH PARTS WITH HYSOL IAW SRM 51-1-9 TR NR 51-142 SRM 51-1-9A T R NR 51-141. CLEANED TREATED PRIMED AREA + PANEL PLATING INNER FACE IAW SRM 51-1-8B. INSTALLED PANEL PLATING IAW SRM 5 1-1-11 SRM 51-1-21 REFER TO NR 107455 FOR BALANCING. 2 L 7 4 4F RT 4A25 2008020800350 20080208 00350 NM 2008 2 8 SWAA080642 1 20080203 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510D, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800356 20080208 00356 NM 2008 2 8 SWAA080649 1 20080204 A 2560 6557463 FITTING BOEING 737 7375H4 138449D NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2008020800363 20080208 00363 WP 2008 2 8 DHL2007873511 1 20080104 A 5720 FITTING DOUG DC8 DC873F 302199F WP NR 1 TANK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 NR 1 ALT TANK AFT FITTING CRACKED BETWEEN STA XW 408.000 AND S-58 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 57-1-0, SRM 51-1-20D. CLEANED AND APPLIED POLYURETHANE TOP YELLOW COATING IAW S RM 51-1-12 PG 7. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). REFER TO NR 107760 FOR FUEL LEAK CHECK. 2 L 7 4 4F RT 4A25 2008020800369 20080208 00369 EA 2008 2 8 SIMA200803106 1 20080129 A 2910 97571 VALVE CNDAIR CL600 CL6002C10 1390015 EA HYD SYSTEM LEAKING A SIMA L ABORTED APPROACH K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 21 505AE 10053 ON FLIGHT 4078, CREW REPORTED ON DESCENT WHEN SELECTING GEAR DOWN NR 3 HYD PRESSURE AND QUANTITY WENT TO ZERO, DECIDED T O DO A FLY BY AND DECLARED AN EMERGENCY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLOW LIMITER VALVE PER CR J AMM 29-12-13 AND 8194; AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008011100208 20080111 00208 EA 2008 1 11 COMA0860004 1 20080101 A 2752 854D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 924CA 2027 7026 FLIGHT 5682 - RECEIVED FLAP FAIL CAUTION AND STALL FAIL CAUTION MESSAGES. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEFT NR 4 FLAP ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100211 20080111 00211 EA 2008 1 11 COMA0860007 1 20080101 A 2752 853D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 924CA 12819 7026 FLIGHT 5682 - RECEIVED FLAP FAIL CAUTION AND STALL FAIL CAUTION MESSAGES. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED RIGHT NR 3 FLAP ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100230 20080111 00230 CE 2008 1 11 DXTA200702736 1 20080101 A 2720 LIMITER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RUDDER FAILED E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 998QS 7500198 THE AMBER (RUDDER LIMIT FAIL B) CAS MESSAGE ILLUMINATED IN FLIGHT AND REMAINED ON WITH SHUTDOWN. RUDDER LIMITER FAILED AT 67 PERCENT. REMOVED & REPLACED T.R. SWITCH. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011100248 20080111 00248 EA 2008 1 11 COMA0860026 1 20080102 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 SO 01 685BR 7712 FLIGHT 5681 - RECEIVED FLAP FAIL CAUTION MESSAGE. DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED CVG WITHOUT INCIDEN T. REPLACED RIGHT SIDE NR 2 FLAP ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100249 20080111 00249 EA 2008 1 11 COMA0860027 1 20080102 A 2752 854D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 SO 01 685BR 7712 FLIGHT 5681 - RECEIVED FLAP FAIL CAUTION MESSAGE. DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED CVG WITHOUT INCIDEN T. REPLACED RIGHT SIDE NR 4 FLAP ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100270 20080111 00270 SO 2008 1 11 CHQA200800001 1 20080101 A 2751 3633501003 VELOCITY SENSOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL T/E FLAP FAILED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 575RP 8894 145847 CAE312676 CVG TO IND - ATTEMPTED TO RETRACT FLAPS DURING CLIMB AND RECEIVED A FLAP FAIL EICAS MESSAGE. RAN ALL APPLICABLE QRH CHE CK LISTS, RETURNED TO FIELD, AND LANDED WITHOUT INCIDENT. MAINTENANCE DUPLICATED THE FLAP FAIL WITH A RIGHT TRANSMISSIO N BRAKE FAIL WHILE ON THE RAMP BUT ONCE THE AIRCRAFT WAS INSIDE THE HANGER THE FLAP SYSTEM OPERATED NORMALLY. MAINTENAN CE THEN FLUSHED AND SERVICED ALL FLAP ACTUATORS AND THE SYSTEM OPERATED NORMALLY. ON TAXI OUT, THE AIRCRAFT EXPERIENCED ANOTHER FLAP FAIL AND THE CMC HAD MESSAGES FOR THE RT VELOCITY SENSOR AND RT TRANSMISSION FAIL. THE VELOCITY SENSOR WA S THEN CHANGED AND THE FLAP SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008011100311 20080111 00311 CE 2008 1 11 DXTA200802739 1 20080102 A 3240 BRAKE ASSY CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE FAILED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 613QS 5605599 WHILE TAXIING, WE LOST OUR BRAKES AND USED EMERGENCY BRAKES TO STOP. FOUND PWR BRAKE CB PULLED. BLED BRAKES COMPLETED O PERATIONAL CHECK OF ANTI-SKID SYSTEM AND OPERATIONAL CHECK OF EMERGENCY BRAKE SYSTEM. TAXIED ACFT TO ACCOMPLISH OPS CEHC K OF BRAKES OPS CHECK GOOD. ALL WORK DONE IAW 32-44-00 OF THE CE-560XLMM. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008011400016 20080114 00016 EU 2008 1 14 COEA0802819 1 20080102 A 2435 8260121 STARTER GEN AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE NR 2 ENGINE FAILED A COEA D RETURN TO BLOCK J J WARNING INDICATION WARNING INDICATION TX TAXI/GRND HDL 1 NM 13 819FX 2269 1011 359 FLIGHT NR 8091 ON 1/2/08, DURING TAXI TO RUNWAY THE NR 2 DC GENERATOR FAULTED. CREW ATTEMPTED TO RESET WITHOUT SUCCESS. AIRCRAFT RETURNED SAFELY TO BLOCKS. REPLACED NR 2 ENGINE DC STARTER GENERATOR. NR 40670. 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400056 20080114 00056 SO 2008 1 14 RAIA00801005 1 20080103 A 3350 MS25231316 BULB EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHTS FAILED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 805HK 145096 PRE FLT NR 3565-PIT-EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY ON THE MAIN DOOR. OPS CH ECKED GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008011400057 20080114 00057 SO 2008 1 14 RAIA00801004 1 20080103 A 3297 D3899926KA98SN CONNECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C GL NLG UPLOCK CORRODED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 819HK 145062 FLT NR 5584-RIC-GEAR NOISES COMING FROM FRONT OF AIRCRAFT DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE CONNECTOR ON THE NLG UPLOCK BOX PROXIMITY SENSOR NR 2 WHICH WAS FOUND TO BE WORN, CORRODED AND BROKEN. OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008011400082 20080114 00082 CE 2008 1 14 DXTA200802743 1 20080103 A 3260 WARNING LIGHT CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE MLG UNKNOWN E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 814QS 5600776 WHEN THE GEAR WAS CYCLED DOWN NORMALLY (GEAR HANDLE TO DOWN POSITION) THERE WAS NONE OF THE 3 GREEN DOWN INDICATORS. JA CKED ACFT, CONNECTED HYDRAULIC MULE. EXTEND & RETRACTED GEAR 13 TIMES. ALL GEAR OPS NORMAL. DISCONNECTED MULE. ALL WOR K DONE IAW AMM 32-01-00 AND 7-10-01. SERVICED HYD FLUID TO PROPER LEVEL IAW AMM 12-12-01. DOWNJACKED A/C IAW AMM 07-10 -01 2 L 7 2 4F 4 F RT A22CE E00053EN 2008011400084 20080114 00084 2008 1 14 DXTA200802741 4 20080103 A 2210 7002800901 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 938QS 7500183 APPROX 5 TO 10 MINS AFTER T/O, CYAN FGC A FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED BOTH NR 1 & 2 LINEAR ACTUATOR. W ITH REPAIRED UNITS FROM HONEYWELL RS LV22992K PER MM CHAP 27-24-00. GROUND OP'S CHECKED GOOD 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011400086 20080114 00086 NE 2008 1 14 UIAA010208001 2 20080102 A 7531 2607MK2 ACTUATOR DOUG MD90 MD9030 3023690 NM IAE V2525 V2525D5 NE RT ENG VSV MALFUNCTIONED E UIAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 13 17921 1240 53554 V20125 DURING TAXI,THE (R ENG SYS FAIL) MSG SHOW ON EOAP. BITE RT ENGINE EEC FND (VSV ACT/HC/EEC2) CLM MSG. IAW AMM 75-31-01 REPLACED R ENG VSV ACTUATOR. PERFORM R ENG POWER ASSURANCE TEST AND CONDITION CHECK NORMAL. 2 L 7 2 4F 4 F RT A6WE A40NE 2008011400119 20080114 00119 NM 2008 1 14 DL757080001 1 20080101 A 2750 TLN1001W38 NUT BOEING 757 757232 1384965 NM FLAP DRIVE WORN A DALA O OTHER F FLT CONT AFFECTED LD LANDING 1 SO 27 602DL 22809 AT LANDING WHEN FLAPS LEVER PLACED TO 5, GOT TE FLAP DISAGREE CAUTION AND FLAPS LOCKED AT 1. FOUND RT INBD FLAP OUTBD J ACKSCREW DISCONNECTED FROM TRANSMISSION AT U JOINT. U JOINT PARTS FOUND IN FAIRING. REPLACED TRANSMISSION, U JOINT PAR TS, AND DAMAGED FAIRING. SUSPECT LOCKING FEATURE ON U JOINT ASSY NUT WORN. 2 L 7 2 4F RT A2NM 2008020800371 20080208 00371 WP 2008 2 8 08FDEA00328 1 20080130 A 5753 SKIN DOUG MD10 MD1010F 3022112 WP TE FLAP MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 374FE 46612 FOUND REPAIR DOUBLER R/W O/B FLAP LOWER SKIN STA XOF 458. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AN D IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED REPAIR AND FOUND NOT TO BE WITHIN THE LIMITS OF DC/MD10 SRM 57-10-00 FIG9 VOL I. REWORKED REPAIR IAW DC/MD10 SRM 57-10-00 FIG 9 VOL I. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008020800376 20080208 00376 WP 2008 2 8 UPS08851542 1 20080112 A 5320 FITTING DOUG DC8 DC871F 302199D WP FS 280 L21L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 FITTING L21L STA 280 IS CRACKED. REMOVED L21L END FITTING AT STA 280 IAW SRM 51-03-00-0. FABRICATED AND INSTALLED END FITTING AT L21L STA 280 IAW DWG 3773073, AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2008020800384 20080208 00384 NM 2008 2 8 WRLA2008019 1 20080202 A 2750 FLAP SYSTEM DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE WING JAMMED A WRLA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 11 274WA 48633 EDDF/CYYZ - FLAPS WOULD NOT EXTEND FOR APPROACH AND LANDING. FLAP HANDLE JAMMED PHYSICALLY. PERFORMED NO FLAP/SLAT EX TENDED LANDING CHECKLIST, DECLARED EMERGENCY. PERFORMED OPERATION OF FLAPS IAW MD-11 MM 27-50-00. ACTUATED FLAPS FROM 0-50 DEGREES THEN STOWED. INSPECTED FLAPS AT 50 DEGREES FOR ICE AND SNOW, NO ICE NOTED. SYSTEM OPERATES NORMAL. 2 L 7 3 4F 4 F RT A22WE E24NE 2008020800386 20080208 00386 NM 2008 2 8 WRLA2008018 1 20080202 A 2750 FLAP SYSTEM DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE WING MALFUNCTIONED A WRLA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 11 274WA 48633 CYYZ/EDDP - ACCOMPLISHED SLATS ONLY APPROACH AND LANDING. FLAPS WOULD NOT EXTEND WHILE ON APPROACH OR AFTER LANDING. P ERFORMED FUNCTIONAL TEST OF FLAP SYSTEM, PERFORMED RTS OF FLAP SYSTEM IN FCC 1 & 2, ALL TEST PASSED. NO DEFECTS NOTED. COULD NOT DUPLICATE ON GROUND PER MM 27-50-00. 2 L 7 3 4F 4 F RT A22WE E24NE 2008020800390 20080208 00390 NM 2008 2 8 SWAA080659 1 20080205 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800391 20080208 00391 NM 2008 2 8 SWAA080660 1 20080205 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800395 20080208 00395 NM 2008 2 8 SWAA080663 1 20080204 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 491WN 33867 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008020800399 20080208 00399 NM 2008 2 8 SWAA080673 1 20080205 A 5753 65C30462 SKIN BOEING 737 7373G7 1384595 NM FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2008020800400 20080208 00400 NM 2008 2 8 SWAA080672 1 20080205 A 5753 65C30462 SKIN BOEING 737 7373G7 1384595 NM FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND LT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2008020800402 20080208 00402 NM 2008 2 8 SWAA080668 1 20080204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008020800411 20080208 00411 NM 2008 2 8 SWAA080670 1 20080205 A 5310 6978062 DOOR FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 2008020800412 20080208 00412 NM 2008 2 8 SWAA080671 1 20080205 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008021100014 20080211 00014 2008 2 11 SWIA200819196 3 20080201 A 6111 SKIN EMB 120 EMB120ER 3260203 SO NR 1 PROP BLADE DELAMINATED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 576SW 120345 FLT 5543 - RIGHT PROPELLER TIP APPEARS TO BE DELAMINATED. REPLACED NR 1 BLADE ON RIGHT PROP WITH A SERVICEABLE UNIT IAW MM 61-11-01, P/N: RFC11M1-6A S/N OFF: 2172. 2 L 7 2 4T RT A31SO 2008021100017 20080211 00017 EA 2008 2 11 SWIA200819199 1 20080205 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 461SW 7811 FLT 3761 - SEVERAL EMERGENCY LIGHTS DO NOT ILLUMINATE. REPLACED NR 3 ELBP CHARGER WITH A SERVICEABLE UNIT IAW MM 33-51- 04,PN: BA5-0933-901, SN OFF: 000922. 2 L 7 2 4F RT A21EA 2008020800013 20080208 00013 EU 2008 2 8 USAA920080272 1 20080127 A 3350 321452 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A USAA K NONE O OTHER UK UNKNOWN 1 EA 19 637AW 58041 58041 99 FLT 518 - PHX-OMA - EMERGENCY EXIT LIGHTING - FIRST CLASS CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED POWER SUPPL Y AND BATTERY FOR FORWARD EMERGENCY LIGHTS (10WL). OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008011000219 20080110 00219 EU 2008 1 10 2008UALA0002 1 20080102 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN CHAFED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 481UA 1559 EMERGENCY LIGHT TEST FAILS 3 SERVICE CHECK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008011100115 20080111 00115 NM 2008 1 11 SWAA080102 1 20080103 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011100121 20080111 00121 NM 2008 1 11 SWAA080108 1 20080103 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008011100123 20080111 00123 NM 2008 1 11 SWAA080110 1 20080101 A 5322 6546569 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 887, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008011100156 20080111 00156 NM 2008 1 11 SWAA080121 1 20080106 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED BRDG CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED AT OUTBOARD T/E. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008011100170 20080111 00170 NM 2008 1 11 SWAA080128 1 20080106 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011100171 20080111 00171 NM 2008 1 11 SWAA080129 1 20080106 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011100172 20080111 00172 NM 2008 1 11 SWAA080130 1 20080106 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011100191 20080111 00191 NM 2008 1 11 SWAA080137 1 20080106 A 5754 65C20661 SLAT BOEING 737 7375H4 138449D NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 L/E SLAT INBOARD T/E DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008011400001 20080114 00001 NM 2008 1 14 AMTA200800009 1 20080105 A 2560 GLOWSTRIP BOEING 737 73783N 13844HI NM CABIN UNSERVICEABLE A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 F/A`S REPORT EGRESS LIGHTING BY RT AFT LAV IS INOPERATIVE. REMOVED AND REPLACED WITH SERVICEABLE PHOTOLUMINESCENT STRIP AT RT AFT LAV IAW AMM 33-51-15. (K) 2 L 7 2 4F RT A16WE 2008011400004 20080114 00004 EU 2008 1 14 DXTA200802759 1 20080110 A 2800 FLOAT VALVE ISRAEL GALAXY GALAXY 4500307 EU PWC PW306 PW306A 52165 NE WING FUEL TANK FAILED E DXTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 07 700QS 052 IN CRUISE FLIGHT AT FL380 WE NOTICED FUEL LEAKING OUT OVER THE LT AILERON. REMOVED DEFECTIVE LEFT WING VENT FLOAT VALVE AND INSTALLED NEW VALVE PER G200 CMP 28501. 2 L 7 2 4F 4 F RT A53NM E35NE 2008011400012 20080114 00012 CE 2008 1 14 DXTA200802751 1 20080108 A 2720 LIMITER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RUDDER MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 919QS 7500224 RUD LIMIT FAIL A AMBER CAS ILLUMINATED AFTER TAKEOFF AT APPROX 15000 FT. LIMIT WAS 22 PERCENT. R & R RUDDER TRAVEL LIM ITERS IAW MM CH 27-23-00. OPS CK GOOD IAW CE 27-20-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011500173 20080115 00173 NM 2008 1 15 USAA920080001 1 20080101 A 2611 100064904 SMOKE DETECTOR BOEING 737 7373B7 1384580 NM CARGO BAY FALSE ACTIVATION A USAA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 19 504AU 14584 706 23379 BOS - FFW - FLT 854 - CARGO FIRE MX LIGHT ON MX TEST SHOWS FALSE ALARM. MX REPLACED THE CARGO SMOKE DETECTOR. OPERATIO NAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2008011500206 20080115 00206 EU 2008 1 15 YENA2008002 1 20080102 A 2782 17003909 ACTUATOR EMB ERJ190 ERJ190100IGW 3260408 EU L/E SLAT MALFUNCTIONED A YENA O OTHER S AFFECT SYSTEMS AP APPROACH 1 EA 15 228JB 4682 19000030 FLT 1118, FLL-SYR, SLAT FAIL, AOA LIMIT FAIL, SPOILER FAULT, STICK SHAKER ANTICIPATED. EICAS MESSAGES UPON FLAP LEVER M OVEMENT FROM 0 TO 1, QRH PROCEDURES ACCOMPLISHED. LANDED SLAT 0, FLAPS 2. FAULT CODE 27811021ACE PRESENT. PERFORMED F IM TASK 27-81-00-810-802, FOUND LT NR 6 SLAT ACTUATOR TRIPPED. REMOVED AND REPLACED NR 6 LT SLAT ACTUATOR IAW 27-81-01, OPS CHECK OF SLAT SYS OK, NO FAULTS NOTED. 2 L 7 2 4F RT A57NM 2008011500207 20080115 00207 EU 2008 1 15 08FDEA00041 1 20080105 A 5320 A5383210420600 WEB AIRBUS 300 A300B4622 3930401 EU ZONE 200 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 FUS FR 50 BETWEEN SEAT TRACKS 3L AND 4L, STIFFENER WEB 12" TO 24" BELOW FLOOR BENT FABRICATED REPLACEMENT WEB IAW DRAWIN G A53832104. REMOVED AND REPLACED WEB IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008011500311 20080115 00311 NM 2008 1 15 R61A200800002 1 20080108 A 2120 UNKNOWN EMB ERJ170 ERJ170100SE 3260406 NM CABIN ODOR A R61A O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 873RW 17000144 DURING WEATHER DIVERSION CREW REPORTED ELECTRICAL SMELL IN THE AIRCRAFT. CREW DIVERTED TO MOSES LAKE WASHINGTON AND LAN DED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. CREW RAN AIRCRAFT AND MAINTENACE INSPECTED AIRCRAFT. NO DEFECTS WERE NOTED AND AIRCRAFT WAS RETURNED TO SERVICE. NO FURTHER CREW WRITE UPS HAVE BEEN REPORTED. 2 L 7 2 4F RT A56NM 2008011500317 20080115 00317 WP 2008 1 15 ABXA080003 1 20080103 A 5610 HOOK DOUG DC9 DC941 302207N WP COCKPIT WINDOW OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 956AX 47620 FIRST OFFICER'S CV WINDOW WOULD NOT OPEN. ADJUSTED UPPER HOOK ON FIRST OFFICER'S WINDOW IAW DC9 AMM 56-10-3. 2 L 7 2 4F A6WE 2008011500326 20080115 00326 SO 2008 1 15 C2XA08IA016 1 20080107 A 2432 14521325411 PANEL EMB 145 EMB145XR 3260214 SO COCKPIT DEFECTIVE A C2XA K NONE J WARNING INDICATION UK UNKNOWN 1 SW 27 12160 10944 10944 145799 IAH - FLIGHT 2785, THE CREW REPORTED RECEIVING AN "EMERGENCY LIGHTS NOT ARMED" MESSAGE IN FLIGHT. THE AIRCRAFT LANDED A T IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE MAIN BATTERY ELECTRICAL PANEL, OPERATIONALLY CHECKED W ITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008011500329 20080115 00329 SO 2008 1 15 C2XA08IA014 1 20080107 A 3350 M835366022M RELAY EMB 145 EMB145XR 3260214 SO COCKPIT INOPERATIVE A C2XA O OTHER J WARNING INDICATION UK UNKNOWN 1 SW 27 12160 145799 IAH - FLIGHT 2785, THE CREW REPORTED RECEIVING AN "EMERGENCY LIGHTS NOT ARMED" MESSAGE IN FLIGHT. THE AIRCRAFT LANDED A T IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED RELAY K0021, OPERATIONALLY CHECKED WITH NO DEFECTS, AND TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008011500331 20080115 00331 NM 2008 1 15 SWAA080180 1 20080108 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 237WN 34632 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008011100154 20080111 00154 2008 1 11 SWAA080119 4 20080103 A 2565 63550 SLIDE BOEING 737 737705 13844SC NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 270WN 29089 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008011100165 20080111 00165 NM 2008 1 11 SWAA080126 1 20080106 A 3350 417A5701 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 EEPLS LENS BROKEN AT ROW 5ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008011100182 20080111 00182 NM 2008 1 11 SWAA080136 1 20080106 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008011100214 20080111 00214 EA 2008 1 11 COMA0860010 1 20080101 A 3030 7858062 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 01 934CA 33305 7042 FLIGHT 5598 - RECEIVED RIGHT AOA, STATIC AND PITOT HEAT CAUTION MESSAGE. RETURNED TO CVG, LANDED WITHOUT INCIDENT. REP LACED ADHSC NR 2, NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100278 20080111 00278 NM 2008 1 11 HALA0800004 1 20080103 A 2697 CONNECTOR BOEING 767 7673G5 1385126 NM FIRE DETECTION DIRTY A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, ON PREFLIGHT: EICAS MESSAGE "APU FIRE LP2". CLEANED APU FIRE LP NR 2 PLUG. OPS CHECK OK IAW AMM 26-15-00. 2 L 7 2 4F RT A1NM 2008011100279 20080111 00279 NM 2008 1 11 HALA0800005 1 20080103 A 2612 WARNING SYSTEM BOEING 767 7673G5 1385126 NM PWA 4060 PW4060 52119 NE FIRE DETECTION MALFUNCTIONED A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM, EICAS STATUS MSG L ENG FIRE LOOP 1 DISPLAYED. OK FOR SERVICE PER FIM 26-11-00. NO DEFECTS NO TED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008011400038 20080114 00038 CE 2008 1 14 GUUA01050802 1 20080105 A 5524 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 231YV 25579 UE231 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT ELEVATOR OB HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR OB HINGE BRACKET. 2 L 7 2 4T 3 T RT A24CE E2NE 2008011400045 20080114 00045 CE 2008 1 14 DXTA200802750 1 20080107 A 2750 FLEX DRIVE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 953QS 7500153 FLAPS FAILED ANNUNCIATOR ILLUMINATED AFTER FLAP HANDLE SELECTED UP. FLAPS FAILED AT THE 0 INDICATION. REMOVED & REPLACE D LT & RT NR 5 FLAP FLEX DRIVE CABLE ASSYS. IAW MM. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011400049 20080114 00049 2008 1 14 DXTA200802746 4 20080104 A 2210 SERVO CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE MALFUNCTIONED E DXTA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 301QS 6800010 AUTO PILOT DISCONNECTS IN FLIGHT BY ITSELF. REMOVED AND REPLACED AILERON SERVO IAW MM 22-10-00. C/W AUTOPILOT SERVO D RIVE ADJUSTMENT AND TEST IAW MM 22-10-02. OPS CHECK GOOD. 2 L 7 2 4F 4 F RC T00012WI E35NE 2008011500015 20080115 00015 NM 2008 1 15 2008UALA0034 1 20080102 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FUSELAGE SKIN CRACKED AT FASTENER HOLE AFT OF E&E COOLING EXHAUST DUCT CUTOUT LBL 2 STA 378. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020800028 20080208 00028 EU 2008 2 8 USAA920080280 1 20080127 A 2120 87292325V06 COMPUTER AIRBUS A321 A321211 3930370 EU E&E BAY DEFECTIVE A USAA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION UK UNKNOWN 1 EA 19 174US 43 43 1492 FLT 921 - PHL-MJB - BURNING SMELL - AVIONICS SMOKE ECAM MESSAGE, SMELL OF LIGHT SMOKE IN COCKPIT. CLT MAINTENANCE REMOV ED AND REPLACED THE AVIONICS EQUIPMENT VENTILATION COMPUTER AND SMOKE DETECTOR. ECAM MESSAGE CLEARED AND NO FURTHER SME LL OF SMOKE IN THE COCKPIT. 2 L 7 2 4F RT A28NM 2008020800029 20080208 00029 NM 2008 2 8 HALA0800034 1 20080201 A 3241 761SUE22 CONTROL UNIT BOEING 717 717200 1383700 NM DCU FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 480HA 55125 ANTI-SKID FAIL AFTER GEAR EXTENSION - ATB. TROUBLESHOT IAW FIM 32-45, TASK 807. REMOVED AND REPLACED DCU IAW AMM 31-43 -02. OPS CHECK GOOD. MIC SHEET CLEARED. PLACARD REMOVED. 2 L 7 2 4F TR A6WE 2008020800030 20080208 00030 NM 2008 2 8 SB08004 1 20080128 A 3350 20131ASMI BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 421US 23988 CLT - MAINTENANCE REPORTED THE L1 AND R1 DOOR EMERGENCY EXIT LIGHTS ALONG WITH SEAT 1AC AND 2AC EMERGENCY LIGHTS INOPERA TIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008020800031 20080208 00031 WP 2008 2 8 ARWA20080202 1 20080203 A 8097 CONNECTOR DOUG DC10 DC1030F 3023504 WP START VALVE DIRTY A ARWA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 19 478CT 47819 UPON ADVANCING, THE POWER LEVERS FOR TAKEOFF, NR 3 START VALVE LIGHT ILLUMINATED, LIGHT EXTINGUISHED WHEN POWER LEVERS W ERE RETARDED TO IDLE. CLEANED AND SECURED CONNECTOR AT NR 3 ENGINE STARTED VALVE, OPERATIONAL CHECK AT BLAST FENCE TAKE OFF POWER IAW MM 71-00-00 AND 80-10-00. 2 L 7 3 4F RT A22WE 2008020800053 20080208 00053 WP 2008 2 8 DHL2007873510 1 20080108 A 5753 DOUBLER DOUG DC8 DC873F 302199F WP RT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 RT INBD FLAP FORMER ANGLE DOUBLER CRACKED 1" AT STA XW 125.000. REMOVED ANGLE DOUBLER IAW SRM 51-1-21. FABRICATED ANGL E DOUBLER 9AL7075T6 0.050") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2008020800087 20080208 00087 NM 2008 2 8 USAA920080281 1 20080109 A 5347 145T521344 SEAT TRACK BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 764 - BS 830, RBL 88.5, WL 200. REPLACED CABI N SEAT TRACK, BS 764 - BS 830, RBL 88.5, WL 200 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008020800099 20080208 00099 2008 2 8 HALA0800031 4 20080130 A 3442 RADAR BOEING 767 767332 1382001 NM WX SYSTEM MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 596HA 23276 ETOPS SIGNIFICANT SYSTEM, WX/TCAS SCREEN BLANK IN ALL MODES. REPLACED WXR DISPLAY. GND OPS CHK OK. 2 L 7 2 4F RT A1NM 2008020800102 20080208 00102 NM 2008 2 8 08FDEA00336 1 20080131 A 5315 652082757 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 MAIN DECK FLOORBEAM, UPPER CHORD FWD FLG, IS MISDRILLED, BS 480, LBL 62, WL 208 ACCOMPLISHED HFEC, NO DEFECTS NOTED. AP PLIED SEALANT TO AFFECTED HOLE. REF FED EX EA NR 7-5310-113134. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008020800119 20080208 00119 NM 2008 2 8 08FDEA00338 1 20080131 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 INTERCOSTAL AT BETWEEN STATION 440 - 460 AT STRINGER 24L IS CRACKED, 0.75" LONG. REMOVED AND REPLACED INTERCOSTAL IAW S RM 51-40-02. NEW INTERCOSTAL FABRICATED ON MAE TRAVELER NR T7/707194 IAW SRM 51-10-02, FROM 7075 - O - 0.063C, HEAT TRE ATED PER AMS 2770 H TO 87B. 2 L 7 2 4F RT A2NM 2008020800120 20080208 00120 WP 2008 2 8 08FDEA00339 1 20080131 A 5322 3F149181 SHEAR TIE DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 FWD PIT AT STA 808 BETWEEN STR 42L AND STR 43L SHEARTIE HAS TOOL MARKS. FABBED NEW SHEARTIE IN REF TO FEDEX GMM 7-0-100 1 AND DAC DWG RAM1470. REMOVED AND INSTALLED SHEARTIE AT STA 808 L42L - L43L IN REF TO DC/MD10-10 SRM 51-33-01 VOL II P G1. 2 L 7 3 4F RT A22WE 2008020800124 20080208 00124 NM 2008 2 8 AALA200800103 1 20080119 A 3350 SOCKET BOEING 737 737823 13844BZ NM EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 957AN 29541 DFW - EMERGENCY LIGHT AT SEAT 12D HAS DAMAGED SOCKET. REPLACED SOCKET FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008020800135 20080208 00135 NM 2008 2 8 AALA200800082 1 20080117 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 950AN 30087 LGA - EMERGENCY LIGHTS AT SEAT ROW 9 INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 9. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008020800147 20080208 00147 NM 2008 2 8 USAA920080290 1 20080115 A 5315 FLOORBEAM BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOORBEAM, BS 325, RBL 16 - RBL 56, WL 200. REPAIRED CABIN FLOORBEAM, BS 325, RBL 16 - RBL 56, WL 200 IAW B767 SRM 53-00-51. 2 L 7 2 4F RT A1NM 2008020800182 20080208 00182 SO 2008 2 8 FDKA200801046 1 20080131 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6068 JFK (1359 PHX LCL) - EMERGENCY LIGHT OUT AT ROW 12. MX RESECURED THE LOOSE CONNECTOR AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2008020800190 20080208 00190 NM 2008 2 8 SB08005 1 20080129 A 2450 941D3352 BUSS TIE BOEING 737 737401 1384701 NM ELECTRICAL SYS FAILED A USAA O OTHER H ELECT. POWER LOSS-50 PC AP APPROACH 1 EA 19 417US 23984 CLT FLT 1054 - AIRCRAFT DEPARTED WITH THE LEFT GENERATOR ON MEL AND THE APU GENERATOR SUPPLYING LEFT AC BUSS. DURING A PPROACH INTO CLT, THE AIRCRAFT LOST THE LEFT AC BUSS (DURING ILS COUPLE UP) AND THE APU WOULD NOT RESTORE LEFT BUSS POWE R. FLIGHT LANDED WITHOUT FURTHER INCIDENT. AFTER SEVERAL MINUTES ON THE GROUND, THE LEFT AC BUSS POWER RESTORED ON ITS OWN. CREW ALSO FOUND TR1 CIRCUIT BREAKER TRIPPED. MAINTENANCE REMOVED AND REPLACED THE LEFT SIDE GENERATOR BUSS TIE B REAKER PER MM 24-21-41. OPERATIONAL CHECK GOOD. ALSO, REMOVED AND REPLACED NR 1 GENERATOR AND CSD PER MM 24-11-11-04 A ND 24-21-11-04. OPERATIONAL CHECK GOOD. REMOVED MEL. 2 L 7 2 4F RT A16WE 2008020800197 20080208 00197 NM 2008 2 8 SWAA080544 1 20080130 A 5313 BAC1498 STRINGER BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 16Y CHECK, FOUND STRINGER 22L CRACKED AT BS 505. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008020800219 20080208 00219 NM 2008 2 8 SWAA080579 1 20080131 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 790, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008020800226 20080208 00226 NM 2008 2 8 SWAA080569 1 20080130 A 3350 65C27093 LIGHT BOEING 737 7373L9 1384470 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008020800233 20080208 00233 NM 2008 2 8 SWAA080573 1 20080131 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 27L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008020800241 20080208 00241 NM 2008 2 8 SWAA080609 1 20080201 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 248WN 32509 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008020800243 20080208 00243 NM 2008 2 8 SWAA080610 1 20080201 A 5753 6546430129 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED HC2 CHECK, FOUND LT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2008020800267 20080208 00267 NM 2008 2 8 SWAA080620 1 20080203 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020800294 20080208 00294 EU 2008 2 8 08FDEA00343 1 20080201 A 5330 A53771137200 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN DECK CARGO DOOR HINGE MOUNTING SURFACE (A/C FUSELAGE) HAS ELONGATED FASTENER HOLE ONE INCH FWD OF FRAME 23 (OUTBD) . REPAIRED ELONGATED FASTENER HOLE IAW FED EX A310-200 EA 6-5230-1169118, DOORS-MAIN DECK CARGO DOOR HINGE DAMAGE-INTER IM REPAIR FOR FERRY FLIGHT. 2 L 7 2 4F RT A35EU 2008020800341 20080208 00341 WP 2008 2 8 DHL2007873526 1 20080114 A 5320 57550583 FITTING DOUG DC8 DC873F 302199F WP BS 779 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 LWR FUSELAGE END FITTING CRACKED 8" AT STA 779.000 L-34L, MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. RE MOVED CRACKED FITTING IAW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2008020800351 20080208 00351 NM 2008 2 8 SWAA080643 1 20080203 A 5610 5716145 WINDOW BOEING 737 7375H4 138449D NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 513SW 24190 FLIGHT DECK L1 WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2008020800353 20080208 00353 WP 2008 2 8 DHL2007873530 1 20080122 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 CORROSION BETWEEN SKIN INSERT SURROUNDING "A" LWR CARGO DOOR JAMB AND PLATING AT BS 280 L-24R TO L-28R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-21-08 EVA D853-00036 REV IR, SEMAN DWG NR ED-4678-1. REMOVED FASTENERS IAW SRM 51- 1-21 SRM 51-1-20D. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18, FOUND OUT OF LIMITS IAW SRM 53-2-0. CUT OUT DAMAGE SECTI ON, FABRICATED REPAIR DOUBLER, REPAIR TRILLER IAW SEMAN DWG NR ED-4678-1. CLEANED TREATED PRIMED AREA & REPAIR PARTS I AW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SMN DWG ED-4678-1 SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D SRM 51-3-1. PERFOR MED NDT INSP AREA, REPAIR PARTS NO CRACK NO CORROSION FOUND ENCLOSED SMN-FORM 242-4 IAW EVA85300036.DPS 4.707-1. 2 L 7 4 4F RT 4A25 2008020800365 20080208 00365 WP 2008 2 8 ARWA20080201 1 20080203 A 2751 LIMIT SWITCH DOUG DC8 DC863F 302198F WP TE FLAPS MALFUNCTIONED A ARWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 19 784AL 46135 DURING TAKEOFF ROLL, TAKEOFF WARNING HORN CAME ON. REMOVED AND REPLACED SI-278 FLAP UPLIMIT SWITCH IN ACCORDANCE WITH M /N 27-52-1 AND SI-177 AND 176 SPOILERS SWITCH IN ACCORDANCE WITH 27-63-1, SYSTEM GROUND TEST NORMAL. 2 L 7 4 4F 4A25 2008020800393 20080208 00393 NM 2008 2 8 SWAA080661 1 20080205 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 772, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008020800394 20080208 00394 NM 2008 2 8 SWAA080662 1 20080203 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 382SW 26588 AFT CABIN OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2008021100018 20080211 00018 EA 2008 2 11 SWIA200819200 1 20080204 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY FALSE INDICATION A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 912EV 7728 FORWARD CARGO SMOKE DETECTOR GIVES FALSE WARNING. REPLACED SMOKE DETECTOR IAW MM 26-15-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008021100038 20080211 00038 SO 2008 2 11 SWIA200819180 1 20080123 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY EXIT BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 237SW 120314 FLT 3715 - EMERGENCY EXIT SIGN IS BROKEN AT ROW 6. REPLACED EXIT SIGN WITH A SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008011500021 20080115 00021 NM 2008 1 15 2008UALA0040 1 20080102 A 5320 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FWD GALLEY DOOR CUTOUT INTERCOSTAL ATTACH ANGLE CRACKED AT BS 277-294.5 BETWEEN STRINGERS 11R & 12R. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011500022 20080115 00022 2008 1 15 2008UALA0041 4 20080102 A 2565 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 642UA PA1268 25092 DAMAGED ASPIRATOR, LEAKING. 2 L 7 2 4F 4 F RT A1NM E24NE 2008011500051 20080115 00051 WP 2008 1 15 0801001 1 20080102 A 3260 LIGHT DOUG DC9 DC915F 3022037 WP COCKPIT INOPERATIVE A MJYA K NONE N FALSE WARNING AP APPROACH 1 SW 07 784TW 47014 ON APPROACH TO KGSO, RIGHT LANDING GEAR GREEN POSITION INDICATOR WOULD NOT ILLUMINATE. LANDING GEAR PHYSICALLY DOWN, VE RIFIED WITH GEAR HORN. AFTER THE PROCEDURE, BOTTOM SOCKET LIGHT ILLUMINATED BEFORE LANDING. RELAMPED RIGHT LANDING GEA R GREEN INDICATOR AS NECESSARY, OPS CHECK GOOD. 2 L 7 2 4F A6WE 2008011500102 20080115 00102 SO 2008 1 15 SIMA200800701 1 20080103 A 3240 15004191A LINE EMB 135 EMB135LR 3260305 SO NR 4 BRAKE DISCONNECTED A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 706RG 145194 ON FLIGHT 4611, DURING TAXI BRAKES SEIZED AND COULD NOT BE RELEASED. AIRCRAFT TOWED BACK TO GATE. AIRCRAFT REMOVED FRO M SERVICE. FOUND NR 4 NORMAL BRAKE LINE DISCONNECTED AND DAMAGED. REMOVED AND REPLACE NUMBER 4 NORMAL BRAKE LINE IAW E MB 32-10-01. OPERATIONAL CHECK GOOD AND TAXI CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008011500160 20080115 00160 NM 2008 1 15 USAA920080125 1 20080103 A 5330 6545774 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 23879 CLT - MAJOR REPAIR - RON - CRACKED FUSELAGE SKIN, BS 727E, S26L. REPAIRED FUSELAGE SKIN, BS 727E, S26L IAW B737 SRM 53- 00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008011500226 20080115 00226 NM 2008 1 15 WRLA2008005 1 20080105 A 5320 S393210712400 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 277WA 48743 DURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2007, X=27.5. REPLACED AFT FLOOP SUPPORT PER MD-11 SRM VOL.II 51-35-01 FIG.1 REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2008011500246 20080115 00246 NM 2008 1 15 WRLA2008012 1 20080110 A 5320 AGA72029 ANGLE DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 277WA 48743 DURING C-CHECK INSPECTION FOUND CORROSION ON LOWER CHORD AT STA Y=1964 L48L. BLENDED CORROSION, AREA MEASURED WITHIN L IMITS PER SRM VOL.1 53-00-01 FIG.3 REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2008011500247 20080115 00247 NM 2008 1 15 CALA0800016 1 20080111 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 BACKSIDE OF FUSELAGE FRAME IS CORRODED AT STA 787 BETWEEN STRINGER 27R AND 26R. REPAIRED PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2008011500322 20080115 00322 SO 2008 1 15 C2XA08IA011 1 20080106 A 2450 14528681401 BUSS EMB 135 EMB135LR 3260305 SO COCKPIT BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 28529 145512 IAH - FLIGHT 2963, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED A FAINT ELECTRIC BURNING SMELL. MAINTENANCE REMOVED A ND REPLACED THE RIGHT HAND DC ESSENTIAL BUSS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008011500349 20080115 00349 NM 2008 1 15 SWAA080206 1 20080109 A 5311 6546529 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011500355 20080115 00355 NM 2008 1 15 SWAA080162 1 20080107 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 522, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011500356 20080115 00356 NM 2008 1 15 SWAA080163 1 20080107 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 769, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008011500357 20080115 00357 NM 2008 1 15 SWAA080172 1 20080107 A 5311 6546529 BELTFRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELT FRAME CRACKED AT BS 482, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008011500360 20080115 00360 NM 2008 1 15 SWAA080169 1 20080107 A 5330 6545766 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 870, STR 24R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600004 20080116 00004 NM 2008 1 16 SWAA080174 1 20080107 A 5311 6546550 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021100039 20080211 00039 NM 2008 2 11 DL757080156 1 20080202 A 2530 COFFEEMAKER BOEING 757 757232 1384965 NM AFT GALLEY SMOKE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 670DN 25331 AT CRUISE ALT 39000, FLT ATTENDANTS REPORTED SMOKE IN THE WASTE CAN AREA OF THE REAR GALLEY. REPORTED NO VISIBLE FLAMES . MADE AN EMERGENCY LANDING AT BWI. UPON ARRIVAL AT THE GATE AN INSPECTION OF THE TRASH CAN REVEALED A COFFEE GROUND B AG HAD IGNITED. FIRE DEPT VERIFIED FIRE WAS CONTAINED IN TRASH BIN AND WAS EXTINGUISHED. PERFORMED INSP OF REAR GALLEY . NO DAMAGE NOTED. 2 L 7 2 4F RT A2NM 2008021100041 20080211 00041 NM 2008 2 11 ANCF200800003 1 20080203 A 2913 731966 PUMP BOEING 767 767259 1385136 NM HYD SYSTEM MALFUNCTIONED W ANCF O OTHER J WARNING INDICATION DE DESCENT 1 SO 23 986AN 34326 34326 24835 C ACMP 04=1 PRESS IS ZERO. EICAS MSG C HYD SYS MAINT IS DISPLAYED. PRESS NORMAL WHEN USING OTHER ACMP. EICAS MSG DOOR S DISPLAYED & DOOR AMBER LIGHT ILLUM WITH MLG DOWN MSG & LGT REMAINED ILLUM AFTER LANDING. NLG GREEN DOWN LIGHT FAIL TO ILLUM WITH MLG HANDLE DOWN, MLG DISAGREE DISPLAYED DOORS AMBER LIGHT ON, ALT MLG EXTENSION ACCOMPLISHED IAW AMM 29-11-0 2/401. ACMP 1 (M232) R & R. TEST SATISFACTORY. IAW FIM 32-30-00 FIG 105 BLOCKS 1, 10, 11, 21, & FIM 32-09-03 FIG 103 BL OCKS 1, 2, 3, 4, 5, 6, 7, 8, MLG IS IN CORRECT ADJUSTMENT & PSEU BITE PROCEDURE PERFORMED, NO FAULT DISPLAYED AFTER PSEU BITE IAW AMM 29-11-02-401, ACMP 1 M232 R & R TEST SATISFACTORY & IAW AMM 32-22-02 PAGE 502 PERFORMED, ADJUSTED OF MECHA 2 L 7 2 4F RT A1NM 2008021100044 20080211 00044 EA 2008 2 11 SWIA200819181 1 20080201 A 3244 TIRE CNDAIR CL600 CL6002B19 1900309 EA LT MLG FAILED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 963SW 7865 FLT 6737 - ABORTED TAKEOFF WHEN THE LEFT MAIN TIRE BLEW OUT. REPLACED NR 1 AND NR 2 WHEEL ASSEMBLIES IAW MM 32-41-01. REPLACED NR 2 BRAKE ASSEMBLY IAW MM 32-43-26. REPLACED 2 FAN BLADES IAW MM 72-20-00, AND REPLACED LEFT INBOARD FLAP IAW MM 27-54-01. 2 L 7 2 4F RT A21EA 2008021100057 20080211 00057 NM 2008 2 11 UPS08551543 1 20080124 A 3260 SENSOR BOEING 757 75724APF 1384969 NM MLG DIRTY A IPXA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 471UP 28842 INSPECTION TYPE:SEG1 ATB - AIR GROUND DISAGREE EXPERIENCED IN FLIGHT, RETURNED TO PAE. INVESTIGATED AND FOUND S10060, S 10064, AND S0062 RT/LT GEAR TRUCK TILT SENSORS CONTAMINATED WITH FOD. REMOVED FOD, PERFORMED PSEU SYSTEM TEST PER MM 32 -02-04 ON LT/RT TRUCK TILT SENSORS CHECK GOOD. 2 L 7 2 4F RT A2NM 2008021100063 20080211 00063 NM 2008 2 11 AALA200800145 1 20080123 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 630AA 24588 MIA - EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A2NM 2008021100068 20080211 00068 NM 2008 2 11 AALA200800153 1 20080123 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 767AJ 33539 DFW - EMERGENCY LIGHT AT SEAT 36C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 36C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021100071 20080211 00071 NM 2008 2 11 AALA200800144 1 20080123 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AA 27446 DFW - EMERGENCY LIGHT AT SEAT 24D LOOSE. SECURED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008021100073 20080211 00073 NM 2008 2 11 EIA2008009 1 20080125 A 5414 SKIN BOEING 747 747230B 1384889 NM NR 2 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 488EV 23287 NR 2 PYLON PRECOOLER EXHAUST CUTOUT EDGE, NR 3 STIFFENER NAC STATION 248 TO 234 HAS 2 EACH CRACKS IN SKIN DOUBLER TRIPLE R, CRACKS EXTEND FROM CUTOUT EDGE AND RUN UNDER STIFFENER. REMOVED DAMAGE AND STIFFENER, NDT AREA, FABRICATED REPAIR PA RTS AND INSTALLED PER ECRA 488-54-028-2. 2 L 7 4 4F RT A20WE 2008021100094 20080211 00094 WP 2008 2 11 UPS08851562 1 20080110 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FS1276 L33R TORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 LARGE HOLE TORN IN TOP OF INTERCOSTAL AT STA 1276 AND L33R. FABRICATED AND REPLACED INTERCOSTAL AT F S 1276 AND L33R REF DWG 9754949 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2008021100097 20080211 00097 WP 2008 2 11 UPS08851535 1 20080106 A 5314 KEELBEAM DOUG DC8 DC871F 302199D WP FS 870 RBL 12 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 RT WHEEL WELL KEEL BEAM WEB CRACKED STA 870, 2ND ACCESS HOLE AFT. STOP DRILLED END OF CRACK ON WEB A T STA 870 IAW SRM 53-02-00 FIG 23. FABRICATED AND INSTALLED REPAIR DOUBLER ON RT WHEEL WELL KEEL BEAM WEB AT STA 870 IA W SRM 53-02-00 FIG 23. 2 L 7 4 4F RT 4A25 2008021100105 20080211 00105 EU 2008 2 11 NWAA080363352 1 20080104 A 5712 RIB AIRBUS A330 A330223 3940031 EU RT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 852NW 0614 DURING INSPECTION PER AD 2006-22-14, FOUND CRACKS IN RT WING RIB 6. REPAIRED PER EA 33-211693. 2 L 7 2 4F RT A46NM 2008021100111 20080211 00111 WP 2008 2 11 08FDEA00329 1 20080130 A 5753 NRC60055IN SKIN DOUG MD10 MD1010F 3022112 WP TE FLAP FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 LT I/B FLAP LOWER EXTERNAL SURFACE HAS ERRODED DENT FILLER. REMOVED FILLER,FABRICATED AND INSTALLED NEW REPAIR IAW MD/D C10 SRM 57-10-00 FIG 85 VOLI , 51-21-01 VOLII. 2 L 7 3 4F RT A22WE 2008021100117 20080211 00117 NM 2008 2 11 EIA2008008 1 20080108 A 3350 900835AB BATTERY PACK BOEING 747 747212B 1384886 NM EMERGENCY LIGHTS DISCHARGED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 485EV 20712 RIGHT UPPER DECK SERVICE DOOR SEAL EMERGENCY LIGHT INOP. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT BATTERY PACK , OPS CHECKED NORMAL PER B747 MM 33-51-00. 2 L 7 4 4F RT A20WE 2008021100128 20080211 00128 NM 2008 2 11 UPS08551492 1 20080120 A 5270 PROXIMITY SWITCH BOEING 757 75724APF 1384969 NM RROYCE RB211 RB211535E4 54555 NE CARGO DOOR INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 468UP 25484 FOUND CARGO DOOR CONTROL CIRCUIT BREAKER POPPED AT P34. PANEL WILL NOT STAY IN. REMOVED AND REPLACED ELECTRONIC PROXIMI TY SWITCH UNIT PER MM 32-09-04-4. OPS CHECK NORMAL, PSEU SMOKED/BURNED. 2 L 7 2 4F 4 F RT A2NM E12EU 2008021100137 20080211 00137 NM 2008 2 11 08FDEA00330 1 20080130 A 5320 53FX13551 CHANNEL BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 MAIN CARGO DOOR SILL, HAT CHANNEL, ATTACHED TO FLOORBEAM HAS A CRACK AT FASTENER HOLE AS MARKED, LOCATED AT STA 540 8" , LBL 61", WL 208". REPLACED DAMAGED HAT CHANNEL AT MAIN CARGO DOOR SILL ATTACHED TO FLOORBEAM STA 4404 TO 560 LBL61. MATERIAL IS BAC1517 - 1511, 2024 T42 REF FED EX DWG 53-FX 1497, SHEET 1. TREATED AND PRIMED NEW FABRICATED PART REF S RM 51-10-2 PG 1-7 AND PAINTED REF SOPM 20-41-02 PG 1-6, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008021100140 20080211 00140 EU 2008 2 11 NWAA080353352 1 20080104 A 5712 RIB AIRBUS A330 A330223 3940031 EU LT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 852NW 0614 DURING INSPECTION PER AD 2006-22-14, FOUND CRACKS IN LT WING RIB 6. REPAIRED PER EA 33-211693. 2 L 7 2 4F RT A46NM 2008021100141 20080211 00141 WP 2008 2 11 UPS08851598 1 20080131 A 3350 LAMP DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 GLARESHIELD HAS ONE EMERGENCY LIGHT INOP. RELAMPED AND TESTED IAW MM 33-13-00-2. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2008021100142 20080211 00142 WP 2008 2 11 AALA200800191 1 20080128 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 579AA 53156 LGA - EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008021100148 20080211 00148 WP 2008 2 11 DHL2007873516 1 20080104 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 89073 46091 REPAIR ON FUSELAGE EXTERIOR NOT IN ACCORDANCE WITH SRM (STA 45.000 - 55.000, L-23R TO L-24R) MAJOR REPAIR. PERFORMED MA JOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 4. REMOVED EXISTING NON-STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OU T DAMAGED SECTION AND FABRICATED DOUBLER REPAIR 2 FILLERS AND 7 INTERNAL FINGER DOUBLER IAW SRM 53-2-1 FIG. 7 SHEET 1,4, SRM 53-3-3 FIG 1 ITEM "C". CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIG 7 SHEET 1, 4, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2008021100149 20080211 00149 WP 2008 2 11 UPS08851515 1 20080114 A 5753 37759062 FLAP TRACK DOUG DC8 DC871F 302199D WP LT WING TE FLAP DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 LT WING FLAP STA XW 340 FLAP TRACKS MISSING CHROME. REMOVED AND REPLACED L/WING FLAP TRACKS AT STA X W 340 IAW DC8 AMM 27-51-03-2. 2 L 7 4 4F RT 4A25 2008021100152 20080211 00152 WP 2008 2 11 AALA200800169 1 20080125 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 963TW 53613 LGA - EMERGENCY LIGHT AT SEAT 14D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008021100165 20080211 00165 NM 2008 2 11 AALA200800186 1 20080127 A 3350 0201984002 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 370AA 25197 JFK - EMERGENCY LIGHT AT LEFT AFT LAVATORY DOOR AISLE EXIT SIGN LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT AFT LAVATORY DOOR AISLE EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008021100171 20080211 00171 SW 2008 2 11 WGEA200800023 1 20080205 A 5270 PROXIMITY SWITCH ECLIPS EA500 ECLIPSEEA500 3350000 SW PAX DOOR OUT OF ADJUST E WGEA O OTHER N FALSE WARNING CR CRUISE 1 EA 27 163DJ 19 000081 DOOR CAS MESSAGE ON AT 17,200 FEET ALTITUDE, DP 6.2, CABIN ALTITUDE 1750 FEET. CAS MESSAGE OFF AT 10,000 FEET ALTITUDE, 1,000 FEET CABIN ALTITUDE AND 4 DP. ADJUSTED FORWARD DOOR SENSOR, AND PRESSURIZED AIRCRAFT IAW EA500 AMM 52-00-00 AND 21-30-03. NO CAS MESSAGE. ALL CHECKS GOOD. 1 L 7 2 4J RT A00002AC 2008021100184 20080211 00184 WP 2008 2 11 08FDEA00360 1 20080205 A 5310 ACA72261 DOOR FRAME DOUG DC10 DC1030F 3023504 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MCD DOOR JAMB, WEB CORRODED UNDER CENTERING GUIDE. REPAIRED AREA IAW EA 8-5710-116952. 2 L 7 3 4F RT A22WE 2008020800183 20080208 00183 SO 2008 2 8 FDKA200801047 1 20080131 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FDM RON MCO (1818 PHX LCL) - MAIN CABIN DOOR WAS DIFFICULT TO OPEN. MX CLEANED AND LUBED THE DOOR AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2008020800231 20080208 00231 NM 2008 2 8 SWAA080574 1 20080131 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020800253 20080208 00253 NM 2008 2 8 DL757080121 1 20080125 A 3210 ROD END BOEING 757 75726D 1384907 NM RT MLG DISCONNECTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 900PC 28446 FOUND ON L/O, RT MLG RT TRUNNION FAIRING DOOR OUTBOARD ROD END DISCONNECTED. RECONNECTED RT MLG TRUNNION FAIRING OB ROD END TO DOOR ASSY PER AMM. 2 L 7 2 4F RT A2NM 2008020800261 20080208 00261 WP 2008 2 8 AALA200800164 1 20080124 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 479AA 49654 LGA EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT FOWARD SEAT ROW 20 FOR EMERGENCY LIGHTS AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020800292 20080208 00292 WP 2008 2 8 AALA200800181 1 20080126 A 3350 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DISLODGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9409F 53121 LGA - EMERGENCY LIGHTS IN FIRST CLASS CABIN INOPERATIVE. RESEATED BATTERIES IN BATTERY PACK FOR EMERGENCY LIGHTS IN FIR ST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800302 20080208 00302 NM 2008 2 8 SWAA080607 1 20080203 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 713SW 27847 EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT ROW 8 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008020800310 20080208 00310 NM 2008 2 8 AALA200800119 1 20080121 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 788AN 30011 LHR - EMERGENCY LIGHT AT FIRST CLASS CLOSET DOOR JAMB IS BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FIRST C LASS CLOSET DOOR JAMB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008011600012 20080116 00012 NM 2008 1 16 SWAA080185 1 20080108 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011600013 20080116 00013 NM 2008 1 16 SWAA080186 1 20080108 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008011600018 20080116 00018 NM 2008 1 16 SWAA080202 1 20080108 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 489WN 33855 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008011600024 20080116 00024 NM 2008 1 16 SWAA080195 1 20080108 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011600025 20080116 00025 NM 2008 1 16 SWAA080196 1 20080108 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008011600029 20080116 00029 NM 2008 1 16 SWAA080200 1 20080108 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008011600030 20080116 00030 2008 1 16 SWAA080226 4 20080110 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 200WN 32482 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008011600031 20080116 00031 2008 1 16 SWAA080225 4 20080110 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 200WN 32482 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008011600033 20080116 00033 NM 2008 1 16 SWAA080227 1 20080110 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, STR 25R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008011600036 20080116 00036 NM 2008 1 16 SWAA080230 1 20080110 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED A2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008011600053 20080116 00053 NM 2008 1 16 SWAA080231 1 20080110 A 5751 6553391 ROD BOEING 737 7373H4 1384600 NM RT AILERON WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED BRDG CHECK, RT WING AILERON FAILED FREE PLAY CHECK. REMOVED AND REPLACED AILERON OUT PUT ROD PER MM. 2 L 7 2 4F RT A16WE 2008011600058 20080116 00058 NM 2008 1 16 SWAA080236 1 20080110 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 483WN 32472 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008011500176 20080115 00176 SO 2008 1 15 C2XA08IA007 1 20080103 A 7921 23077047 OIL COOLER EMB 145 EMB145LR 3260212 SO NR 2 ENGINE DIRTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 19966 145131 IAH - FLIGHT 2206, THE CREW REPORTED THAT ENGINE TWO HAD HIGH OIL PRESSURE IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHER E IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE FUEL OIL COOLER, OPERATIONALLY CHE CKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008011500185 20080115 00185 GL 2008 1 15 C2XA08IA004 2 20080102 A 7200 AE3007A1E ENGINE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL RIGHT LEAKING A C2XA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 11121 14243 14243 145683 GJT - FLIGHT 3029, THE CREW REPORTED SMOKE IN THE CABIN FROM THE NUMBER TWO PACK. THE AIRCRAFT DIVERTED TO GJT WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE NUMBER TWO PACK ON MEL 21-51-00 CTL NUMBER 136236. ON 01/02/08 MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE DUE TO INTERNAL OIL LEAKAGE, OPERATIONALLY C HECKED THE PACK SYSTEM WITH NO DEFECTS NOTED, CLEARED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2008011500213 20080115 00213 NM 2008 1 15 CALA0800007 1 20080107 A 5340 66235744 STRINGER CLIP BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19623 27527 FUSELAGE FRAME TO STRINGER CLIP IS CRACKED, CABIN STA 706 STRINGER 11R. INSTALLED NEW CLIP PER SRM 53-40-02. 2 L 7 2 4F RT A16WE 2008020800313 20080208 00313 NM 2008 2 8 AALA200800108 1 20080119 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 683A 25340 BOS - EMERGENCY LIGHT BATTERY PACK AT SEAT 9C INOPERATIVE. REPLACED BATTERY PACK AT SEAT 9C. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 2008020800344 20080208 00344 NM 2008 2 8 SWAA080653 1 20080204 A 5311 6545805 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 2R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008020800349 20080208 00349 NM 2008 2 8 SWAA080654 1 20080204 A 5315 6545610 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 661, LBL 25. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800361 20080208 00361 NM 2008 2 8 DL76S080126 1 20080122 A 5330 143T31521 SKIN BOEING 767 767332 1382001 NM FS 654 SCRATCHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FUSELAGE SKIN FS 654 + 24 TO 654 +37 AT VHF ANTENNA BLENDS. 2 L 7 2 4F RT A1NM 2008020800362 20080208 00362 NM 2008 2 8 SWAA080644 1 20080204 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008021100005 20080211 00005 EA 2008 2 11 SWIA200819176 1 20080131 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 411SW 21802 21802 7067 FLT 3767 - NOSE GEAR WOULD NOT EXTEND. REPLACED NOSE GEAR DOOR SELECTOR VALVE IAW AMM 32-22-20. 2 L 7 2 4F RT A21EA 2008021100053 20080211 00053 SO 2008 2 11 CHQA20080021 1 20080203 A 3610 40303920SD O-RING EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BLEED SYSTEM LEAKING A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 288SK 145451 CAE312717 IAH TO MCI - DURING CLIMB "BLEED 1 LEAK" MESSAGE APPEARED ON EICAS. THE CREW FOLLOWED THE QRH AND THE MESSAGE WENT AWAY . AFTER CONFERRING WITH MAINTENANCE CONTROL IT WAS DECIDED TO RETURN TO FIELD AT IAH. MAINTENANCE INSPECTED THE BLEED SYSTEM AND FOUND JOINT 19 LEAKING BEHIND THE CARGO COMPARTMENT SIDE WALL. THE O-RING WAS REPLACED AT JOINT 19 AND THERE WERE NO FURTHER BLEED LEAK MESSAGES. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008021100080 20080211 00080 WP 2008 2 11 DHL2007873525 1 20080110 A 5751 SKIN DOUG DC8 DC873F 302199F WP RT AILERON DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 RT OUTBD AILERON UPPER SKIN DENTED AT WS 737 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 4 PG 9. REMOVED DENTED PANEL PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING (AL2024T3 0.020") AND DOUBLER IAW SRM 57-8-1 FIG 4 PG 9 ITEM "F AND G". BONDED BOTH PARTS WITH HYSOL IAW SRM 51-1-9 TR NR 51-142, SRM 51-1-9A, TR NR 51-141. CLEAN ED, TREATED AND PRIMED AREA AND PANEL PLATING INNER FACE IAW SRM 51-1-8B. INSTALLED NEW PANEL PLATING (STA XA 700.000 - 737.000) IAW SRM 51-1-11, SRM 51-1-21. PERFORMED BALANCING IAW SRM 51-4-3 PG 1-3. INSTALLED COUNTERWEIGHT P/N 5764617 -47 AT XA 633.000. FOUND WITHIN TOLERANCE. 2 L 7 4 4F RT 4A25 2008021100082 20080211 00082 2008 2 11 MASA200800073 4 20080129 A 3418 C16258AA TRANSDUCER CNDAIR CL600 CL6002C10 1390015 EA AOA VAIN FAILED A MASA O OTHER O OTHER CR CRUISE 1 SW 07 504MJ 8258 10066 ASH FLT 7181 ORD- CID - PILOT DECLARED AN EMERGENCY AND DIVERTED TO MKE FOR STALL FAIL WARNING AND STICK SHAKER ACTIVATE D FOR THE ENTIRE FLIGHT. MX CHANGED RT AOA VANE. 2 L 7 2 4F RT A21EA 2008021100098 20080211 00098 WP 2008 2 11 UPS08851552 1 20080124 A 3350 LIGHT DOUG DC8 DC873F 302199F WP GLARESHIELD INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 GLARESHIELD HAS ONE EMERGENCY LIGHT INOP. RELAMPED AND TESTED IAW MM 33-13-00-2. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2008021100101 20080211 00101 NM 2008 2 11 AALA200800189 1 20080127 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 694AN 26974 DFW - EMERGENCY LIGHT AT SEAT 3E MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008021100108 20080211 00108 WP 2008 2 11 DHL2007873537 1 20080121 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 LT WING CTR L/E EXT SKIN SHOWS CORROSION AT STA XFS 341.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA-FORM 8110-3 DATED 01-14-08 EVA D857-00034 REV IR DATED 01-05-08 SEMAN DWG ED-4677-1 DATED 01-03-08. REMOVED FASTENERS IAW SRM 51-1- 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND WITHIN LIMITS IAW SRM 57-2-1 FIG 2G. VISUALLY INSPECTED AREA OF BLENDOUT. NO CRACK, NO CORROSION FOUND FILLER WITH SEALANT IAW SEMAN DWG ED-4677-1 SRM 51-1-15. FABRICATED REPAIR DO UBLER IAW SRM DWG ED-4677-1 NDT INSPECTED REPAIR PARTS CO CRACK FOUND IAW DPS 4.707-1 EVA D857-000034. CLEANED, TREATED , PRIMED AREA AND REPAIR DOUBLER INNER FACE IAW SRM 51-1-8B. INSTALLED REPAIR DOUBLER IAW SEMAN DWG ED-4677-1 SRM 51-1 2 L 7 4 4F RT 4A25 2008021100119 20080211 00119 WP 2008 2 11 AALA200800084 1 20080117 A 2560 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 402A 49313 LGA - EMERGENCY FLASHLIGHT IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT IN FIRST CLASS. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008021100163 20080211 00163 WP 2008 2 11 UPS08851568 1 20080129 A 3397 CIRCUIT BREAKER DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 ON PREFLIGHT, EMERGENCY LIGHTS WILL NOT DISARM. FOUND EMERGENCY EXIT LIGHT CONTROL C/B BAD. REMOVED AND REPLACED SAME PER DOUGLAS STANDARD MANUAL 20-60-01. SYS OPS CKS NORMAL PER MM 33-50-02-2. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 2008021100185 20080211 00185 SW 2008 2 11 WGEA200800024 1 20080205 A 2840 INDICATION SYS ECLIPS EA500 ECLIPSEEA500 3350000 SW FUEL MALFUNCTIONED E WGEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 132DJ 208 000034 FUEL IMBALANCE CAS MESSAGE, AUTO TRANSFER LEFT TO RIGHT RESULTED IN FUEL BEING PUMPED OVERBOARD THROUGH RIGHT WING VENT DURING TAXI. COMPLIED WITH WALK AROUND INSPECTION TO CHECK VENTS AND TANKS. CONNECTED AMC TO AIRCRAFT IAW EA500 AMM 25 -40-00 FOR GAUGING WET TEST ALL PROBES, CHECKED GOOD, ALSO COMPLIED WITH MFD FUEL SYNOPTIC TEST PAGE CHECK IAW EA500 AMM 31-10-00. WITH ENGINES RUNNING COMPLIED WITH EA500 AMM FUEL SYSTEM CHECK 28-00-00, CHECKED GOOD. 1 L 7 2 4J RT A00002AC 2008011500223 20080115 00223 NM 2008 1 15 WRLA2008003 1 20080105 A 5320 S292916912000 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 277WA 48743 DURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2007, X= -23.5. REPLACED AFT FUSELAGE FLO OR SUPPORT PER MD-11 SRM VOL.II 51-35-01 FIG.1 REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2008011500350 20080115 00350 NM 2008 1 15 SWAA080212 1 20080109 A 5322 6546546 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 807, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008011500353 20080115 00353 NM 2008 1 15 SWAA080161 1 20080107 A 5523 65C2628415M TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED HC1 CHECK, FOUND LT ELEVATOR TAB DELAMINATED AT OUTBOARD T/E. REMOVED AND REPLACED TAB PER MM. 2 L 7 2 4F RT A16WE 2008011600017 20080116 00017 NM 2008 1 16 SWAA080190 1 20080108 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 444WN 29839 DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008011600022 20080116 00022 NM 2008 1 16 SWAA080201 1 20080108 A 5313 BAC1498 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 13R CRACKED AT BS 500D. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008011600032 20080116 00032 2008 1 16 SWAA080249 4 20080110 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 241WN 32504 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008020600289 20080206 00289 EU 2008 2 6 2008UALA00229 1 20080112 A 3350 D9239003500060 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 451UA 865 EMERGENCY LIGHTS FAILS TEST. FAULTS EPSU UNIT LEFT. EPSU FAILURE. REPLACED EPSU, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600299 20080206 00299 NM 2008 2 6 2008UALA00354 1 20080121 A 5230 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 AFT CARGO DOOR LOWER FWD CORNER FRAME IS CRACKED AT STOP FITTING. MAJOR REPAIR: REMOVED DAMAGE. INSTALLED FILLER AND DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600311 20080206 00311 NM 2008 2 6 2008UALA00378 1 20080122 A 5712 RIB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 NR 2 MAIN FUEL TANK LOWER RIB WBL 135, ANGLE FWD UPPER RADIUS OF CUTOUT CRACKED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600319 20080206 00319 NM 2008 2 6 2008UALA00393 1 20080123 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 AFT PIT AT STA 1540, APPROX AT STR 26L, FRAME DENTED ON INBOARD FLANGE. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600325 20080206 00325 NM 2008 2 6 2008UALA00399 1 20080123 A 2750 SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE JACKSCREW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 RIGHT O/B FLAP I/B TRACK FWD LWR JACKSCREW SUPPORT CRACKED. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600326 20080206 00326 2008 2 6 2008UALA00400 4 20080123 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 LEFT OVERWING SLIDE SAFETY PIN STRING BROKEN. THIS PIN KEEPS SLIDE FROM UNRAVELING. REMOVED AND REPLACED LT OVERWING S LIDE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600331 20080206 00331 SO 2008 2 6 C2XA08CL011 1 20080123 A 5210 14533404403 STRUCTURE EMB 145 EMB145EP 3260221 SO MAIN DOOR LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14942 145037 CLE FLIGHT 2532 - THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. MAINTENANCE INSPECTED AND TIGHTENED BOLTS ON THE MAIN CABIN DOOR INNER HANDLE BOX. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2008020600340 20080206 00340 EA 2008 2 6 COMA0860053 1 20080105 A 2421 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE FAILED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 915CA 19221 7013 FLIGHT 5484 - DURING TAKEOFF ROLL RECEIVED IDG 2 CAUTION MESSAGE. ABORTED TAKEOFF. REMOVED AND REPLACED NR 2 IDG. 2 L 7 2 4F RT A21EA 2008020600355 20080206 00355 EA 2008 2 6 COMA0860060 1 20080111 A 3244 0274380 TIRE CNDAIR CL600 CL6002B19 1900309 EA LT MLG BLOWN A COMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 989CA 352 7215 FLIGHT 5030 - VIBRATION JUST BEFORE ROTATION SPEED. WOW INPUT CAUTION. AIRCRAFT RETURNED TO CVG AND LANDED SAFELY. RE MOVED AND REPLACED LEFT MLG I/B WHEEL ASSY. 2 L 7 2 4F RT A21EA 2008021100187 20080211 00187 WP 2008 2 11 UPS08851577 1 20080126 A 5210 SKIN DOUG DC8 DC873F 302199F WP L1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 SKIN CRACK AT UPPER EDGE NEAR AFT CURVE OF L1 DOOR APPROX 1/2 INCH LINEAR, PARALLEL TO T/E OF DOOR. PERFORMED INTERIM R EPAIR IAW UPS EO NR DC8-5210-28486-A PARAGRAPH 6A. PERM REPAIR OR PART REPLACEMENT WITHIN 25 FLIGHT CYLES. D367801 ASS IGNED BY AMC. 2 L 7 4 4F RT 4A25 2008021100193 20080211 00193 WP 2008 2 11 AALA200800174 1 20080126 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 431AA 49343 STL INFLIGHT T1605/26JAN - NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO STL AND LANDED WITHOUT INCIDE NT. ACCOMPLISHED STRUT REPACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008021100197 20080211 00197 NM 2008 2 11 ASAA0852499 1 20080125 A 2410 761574B IDG BOEING 737 737890 1384527 NM LT ENGINE INOPERATIVE A ASAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 NM 02 559AS 5187 5187 35178 EN ROUTE SEA HNL LEFT IDG DRIVE ANNUNCIATED. ATB TO SEA, REPLACED IDG AND IDG OIL COOLER. 2 L 7 2 4F RT A16WE 2008021200008 20080212 00008 EA 2008 2 12 A6WA200840043 1 20080111 A 5260 SUPPORT FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT HANDRAIL DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 LT HANDRAIL SUPPORT FITTING CHAFED AND BENT ON PAX DOOR. REPLACED LT HANDRAIL SUPPORT FITTING ON PAX DOOR. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200011 20080212 00011 EA 2008 2 12 A6WA200840040 1 20080114 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 CRACK ON FLOOR SUPPORT STRUCTURE FS 280, RBL 9. REPAIRED IAW REO 61R-53-11-171, REV D. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200015 20080212 00015 EA 2008 2 12 A6WA200840037 1 20080112 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 CRACK SUSPECTED ON LT FWD PRESSURE BULKHEAD FS 202.75 AT PARKING BRAKE FITTING CUTOUT. REPAIR PERFORMED ON FWD PRESSURE BULKHEAD FS 202.75 AT PARKING BRAKE CUTOUT IAW REO 601R-53-11-563. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200021 20080212 00021 EA 2008 2 12 A6WA200840031 1 20080115 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE HEAT EXCHANGER CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 ANGLE CRACK ON RT HEAT EXCHANGE SUPPORT STRUCTURE BTW FS 700 AND FS 718. ANGLE REPLACED ON RT HEAT EXCHANGER SUPPORT STR UCTURE BTW BS 700 AND BS 718 IAW SRM 51-24-16 AND SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200023 20080212 00023 EA 2008 2 12 A6WA200840028 1 20080114 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 FRETTING FOUND ON AFT OF FLIGHT COMPARTMENT OF BULKHEAD RBL 9, WL 97.50 (250 X 300) .002 DEEP. FRETTING REMOVED IAW SRM 51-12-00. SURFACE FINISH APPLY IAW SRM 51-25-16. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200024 20080212 00024 EA 2008 2 12 A6WA200840027 1 20080114 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 FS621.0 AT REAR PRESSURE BULKHEAD AND CARGO DOOR STRUCTURE JUNCTION, ONE CLIP CRACKED. LT FS 621.00 AT REAR PRESSURE BU LKHEAD AND CARGO DOOR STRUCTURE INTERCOSTAL QTY (1) ONE CLIP REPLACED IAW SRM 51-24-16 AND SRM 51-42-21. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200029 20080212 00029 EA 2008 2 12 A6WA20080014 1 20080118 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE WING FAILED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 438AW 7748 FLAPS FAILED AT 0 DEGREES ON APPROACH. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200031 20080212 00031 CE 2008 2 12 AIH2008F00000 1 20080117 A 2913 99123923 PUMP CESSNA 525 525 2076601 CE WILINT FJ44 FJ44 66000 GL HYDRAULIC SYSTEM SEIZED E AIHA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 11 940SW 3432 5250071 LT HYD PUMP LOW FLOW ANNUNCIATOR ILLUMINATED. MAINT FOUND THE LT HYD PUMP WAS SEIZED. PUMP WAS REPLACED WITH NEW AND PROBLEM WAS SOLVED. (K) 1 L 7 2 4F 4 F RT A1WI E3GL 2008021200043 20080212 00043 NE 2008 2 12 2008UALA00503 2 20080129 A 7200 BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 726576 FOUND METAL ON MASTER CHIP AND GEARBOX CHIP DETECTORS. FOUND BEARING FAILURE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200046 20080212 00046 NM 2008 2 12 2008UALA00498 1 20080129 A 3510 MC1019101 KNOB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OXYGEN MASK BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 549UA 25397 OBSERVERS O2 MASK EMERGENCY KNOB BROKEN. REPLACED OBS O2 MASK ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200052 20080212 00052 NM 2008 2 12 2008UALA00492 1 20080129 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 55 RIGHT. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008020600364 20080206 00364 NM 2008 2 6 USAA920080238 1 20080116 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 - LEVEL 2 CORROSION ON CABIN FLOORBEAM "T" CAP, BS 312, LBL 10 - LBL 12. REPAIRED CABIN FLOORB EAM, BS 312, LBL 10 - LBL 12 IAW B737 SRM 53-10-10-51. 2 L 7 2 4F RT A16WE 2008020600367 20080206 00367 NM 2008 2 6 USAA920080249 1 20080110 A 5320 654583469 STRAP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - CRACKED CABIN FLOOR STRUCTURE STRAP, BS 314, LBL 12, WL 198. REPAIRED CABIN FLOOR STRU CTURE STRAP, BS 314, LBL 12, WL 198 IAW B737 SRM 53-10-51-2R4. 2 L 7 2 4F RT A16WE 2008020600369 20080206 00369 NM 2008 2 6 USAA920080251 1 20080124 A 5753 654643099SP SKIN BOEING 737 7373Y0 1384671 NM T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - LEFT WING INBOARD FORE FLAP LOWER SURFACE HAS DELAMINATION, WBL 125 - WBL 127. REPAIRE D LEFT WING INBOARD FORE FLAP LOWER SURFACE, WBL 125 - WBL 127 IAW B737 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2008020600370 20080206 00370 NM 2008 2 6 USAA920080252 1 20080108 A 5320 140N250532 FITTING BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 MCN - MAJOR REPAIR - C11 CHECK - CRACKED CLIP, BS 1320 - BS 1340, BL 0, WL 208. REPAIRED CRACKED CLIP, BS 1320 - BS 134 0, BL 0, WL 208 IAW B757 SRM 53-00-51-2R4. 2 L 7 2 4F RT A2NM 2008020600371 20080206 00371 NM 2008 2 6 USAA920080253 1 20080107 A 5511 183N150317 SPAR BOEING 757 757225 1384959 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 MCN - MAJOR REPAIR - C11 CHECK - CORROSION ON RIGHT STABILIZER REAR SPAR, UPPER CHORD, STABILIZER STATION 296.249. REPL ACED RIGHT STABILIZER REAR SPAR, UPPER CHORD, STABILIZER STATION 296.249 IAW B757 51-40-02. 2 L 7 2 4F RT A2NM 2008020600375 20080206 00375 NM 2008 2 6 USAA920080267 1 20080107 A 5347 SEAT TRACK BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 871 - BS 1109, LBL 88.5. REPLACED CABIN SEAT T RACK, BS 871 - BS 1109, LBL 88.5 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008020600377 20080206 00377 NM 2008 2 6 USAA920080270 1 20080124 A 5753 113N20033 WEDGE BOEING 757 757225 1384959 NM T/E FLAP CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 MCN - MAJOR REPAIR - C11 CHECK - CORROSION ON LEFT WING INBOARD FLAP WEDGE, FLAP STATION 224.86 - 228.86. REPAIRED LEFT WING INBOARD FLAP WEDGE, FLAP STATION 224.86 - 228.86 IAW B757 SRM 51-70-10-2R. 2 L 7 2 4F RT A2NM 2008020700001 20080207 00001 NM 2008 2 7 ZZDA2008037 1 20080107 A 5311 FRAME BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 A/C STRUCK BY BAG CART. LOWER CHORD ON CANTED FRAME 1161.801 IS CRACKED BETWEEN LONG 24R AND BL 0. INSTALLED NEW CANTE D FRAME REPAIR ATA STATION 1161 BETWEEN LONGERON 24R AND BL 0 IAW B717 SRM 51-41-02 AND SRM 51-41-05 AND AIRTRAN EA17-53 3-00939 IR DATED 01/10/08. 2 L 7 2 4F TR A6WE 2008020700008 20080207 00008 NM 2008 2 7 ZZDA2008044 1 20080107 A 5320 WEB BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 A/C STRUCK BY BAG CART. WEB AT STA 1178 BETWEEN LONG 24L AND 24R DAMAGED. INSTALLED NEW WEB AT STA 1178 BETWEEN LONGER ON 24L AND LONGERON 24R IAW B717 SRM 51-41-02 AND MESSAGE 1-CEY7-MJ. MATERIAL USED 7075 T6 .032. 2 L 7 2 4F TR A6WE 2008020700010 20080207 00010 NM 2008 2 7 ZZDA2008046 1 20080107 A 5311 DOUBLER BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 A/C STRUCK BY BAG CART. DOUBLER DAMAGE BETWEEN LONG 25R AND LONG 25L ON CANTED FRAME 1178. INSTALLED NEW DOUBLER AT CA NTED FRAME 1178 BETWEEN LONGERON 25R AND LONG 25L IAW B717 SRM 51-41-02 AND DRG 9911839. MATERIAL USED 7075 T6 .063. 2 L 7 2 4F TR A6WE 2008020700011 20080207 00011 NM 2008 2 7 ZZDA2008047 1 20080107 A 5311 DOUBLER BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 A/C STRUCK BY BAG CART. DOUBLER DAMAGE BETWEEN LONG 25R AND LONG 25L ON CANTED FRAME 1161. INSTALLED NEW DOUBLER AT CA NTED FRAME 1161 BETWEEN LONGERON 25R AND LONG 25L IAW B717 SRM 51-41-02 AND DRG 99118401. MATERIAL USED 7075 T6 .080. 2 L 7 2 4F TR A6WE 2008020700014 20080207 00014 NM 2008 2 7 ZZDA2008056 1 20080107 A 5313 LONGERON BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 A/C STRUCK BY BAG CART. LONGERON DAMAGE AT 24R BETWEEN STA 1145 AND STA 1161. INSTALLED NEW LONGERON 24R BETWEEN STA 1 145 AND STA 1161 IAW B717 SRM 51-41-02. 2 L 7 2 4F TR A6WE 2008020700019 20080207 00019 EU 2008 2 7 WRNA200800003 1 20080125 A 3210 C230056 DAMPER AIRBUS 300 A300B4203 3930306 EU LT MLG FAILED A WRNA J A DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 SO 05 501TR 53 AFTER TAKEOFF FROM IND, GEAR FAILED TO RETRACT ON BOTH SYSTEM A AND B, DIVERTED TO GSO, DUMPED APPROX 15,000 POUNDS OF F UEL AND MADE A SAFE LANDING. FOUND LEFT INBOARD PITCH DAMPER AT FAULT, REPLACED INBOARD PITCH DAMPER IAW A300 MM 32-11- 15 PG 410, LEAK CHECKED IAW 12-12-32 PG 24. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A35EU 2008020700021 20080207 00021 SO 2008 2 7 C2XA08SH013 1 20080126 A 5751 C150 PLATE EMB 145 EMB145LR 3260212 SO LT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14562 145611 SHV - DURING C-CHECK LEFT AILERON UPPER SHROUD BONDING PLATE CORRODED. MX REPAIRED LT AILERON UPPER SHROUD BONDING PLAT E IAW EC5750-01315. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008020700024 20080207 00024 NE 2008 2 7 HNAA0800040 3 20080125 A 6197 CONNECTOR DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF7 NE WING ROOT CONTAMINATED A HNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 07 906HA 8383 6947 9 910918 WHEN PILOT ADVANCED POWER FOR TAKEOFF, THE NR 2 PROPELLER WENT INTO FEATHER UNCOMMANDED. THE PROP SPEED WAS APPROXIMATE LY 1200 RPM AND REACHED A TORQUE OF 100-105% FOR ABOUT 3 SECONDS. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT WAS RETURNED TO THE MAINTENANCE FACILITY. PLA SWITCHES 6121-S8, S9, S12 AND S13 WERE INSPECTED ALONG WITH NR 1 NAD AND NR 2 TSCU CO NNECTORS, AND STRUT HARNESS, WITH NO DEFECTS NOTED. INSPECTION OF THE NR 1 AND NR 2 WING ROOT CONNECTORS, 9811-P13 & P1 4, FOUND WATER IN THE P14 CONNECTOR, WHICH WAS REMOVED. THE NR 2 STRUT HARNESS AND NR 2 PROP ASSEMBLY WERE THEN CHANGED . ALL OPS CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 6 C P7NE 2008020700027 20080207 00027 NM 2008 2 7 HNAA0800042 1 20080121 A 5210 85210240005 STRUT DHAV DHC8 DHC8102 2809003 NM PAX DOOR BINDING A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 805EX 42280 42280 228 THE MAIN PASSENGER ENTRYWAY DOOR WAS FOUND TO BE BINDING SO THAT IT WOULD NOT OPEN OR CLOSE. AFTER MAINTENANCE OPENED T HE DOOR, A NEW UPPER DOOR STRUT WAS INSTALLED. DOOR WAS OPS CHECKED AND OPENED AND CLOSED NORMALLY AT THIS TIME. 2 H 7 2 4T RT A13NM 2008020700029 20080207 00029 NM 2008 2 7 HNAA0800045 1 20080124 A 3234 5352011 CONTROL HANDLE DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A HNAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 07 807EX 24090 14765 292 UPON SELECTING THE LANDING GEAR DOWN, THE LEFT MAIN GEAR WOULD NOT EXTEND AND THE RED GEAR UNSAFE CAUTION LIGHT ILLUMINA TED. THE CREW DECLARED AN EMERGENCY AND EXTENDED THE GEAR USING THE ALTERNATE EXTENSION SYSTEM. MAINTENANCE CHANGED TH E LANDING GEAR SELECTOR HANDLE ASSEMBLY AND PERFORMED EXTENSIVE CHECKS OF THE SYSTEM. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 2008020700032 20080207 00032 EA 2008 2 7 COMA0860058 1 20080110 A 3234 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG WW FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 588SW 19446 7069 FLIGHT 5354 - NOSE DOOR OPEN MESSAGE RECEIVED DURING GEAR RETRACTION, FOLLOWED BY GEAR DISAGREE. EMERGENCY DECLARED, AI RCRAFT RETURNED BACK TO CHS AND LANDED SAFELY. REMOVED AND REPLACED NOSE DOOR SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2008020700034 20080207 00034 WP 2008 2 7 MWEA080017 1 20080125 A 2421 976J2528 GENERATOR DOUG DC9 DC982 3022082 WP ENGINE FAULTY A MWEA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 GL 13 809ME 48071 CAPTAIN HAD FLICKERING ELECTRICAL COMPONENTS AND ON THE FIRST OFFICER'S SIDE LOST AP. REMOVED AND REPLACED AC GENERATOR . 2 L 7 2 4F A6WE 2008020700037 20080207 00037 EA 2008 2 7 COMA0860068 1 20080114 A 2751 8004403 SENSOR CNDAIR CL600 CL6002B19 1900309 EA RT T/E FLAP FAULTY A COMA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 916CA 549 7014 FLIGHT 5175 - FLAPS FAIL CAUTION MESSAGE WHEN SELECTING FLAPS 8 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY IN MSP. REMOVED AND REPLACED RIGHT SIDE NR 4 SKEW SENSOR. 2 L 7 2 4F RT A21EA 2008020700040 20080207 00040 EU 2008 2 7 2008UALA00310 1 20080117 A 3350 D9239003500060 EPSU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 419UA 487 EMERGENCY LIGHTS TEST FAILED, FAULTS AFT LEFT BATTERY. EPSU FAILURE. REPLACED AFT LEFT EPSU, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020700046 20080207 00046 NM 2008 2 7 2008UALA00419 1 20080124 A 5340 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 294 S8L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 BS 294.5 STRINGER 8L INTERCOSTAL TO FRAME ATTACH ANGLE CRACKED. MAJOR REPAIR: REPLACED INTERCOSTAL WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700047 20080207 00047 NM 2008 2 7 2008UALA00420 1 20080124 A 5340 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 294 S7L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 BS 294.5 AT STRINGER 7L INTERCOSTAL TO FRAME ATTACH ANGLE IS CRACKED. MAJOR REPAIR: REMOVED AND REPLACED CRACKED INTERC OSTAL WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700049 20080207 00049 NM 2008 2 7 2008UALA00423 1 20080124 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 794-797 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 AFT PIT COMPARTMENT BS 794 TO 797 AT STRINGER S-26R TO S-27R AND RBL 3-13 BEAR STRAP IS CORRODED. MAJOR REPAIR: REMOVED DAMAGED SECTION OF BEAR STRAP. FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700050 20080207 00050 NM 2008 2 7 2008UALA00425 1 20080124 A 5340 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FWD ENTRY DOOR CUTOUT 2ND STOP FITTING FROM BOTTOM ON AFT SIDE BS 344 INTERCOSTAL ATTACH ANGLE IS CRACKED AT STRINGER 15 L. MAJOR REPAIR: REPLACED ATTACH ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700053 20080207 00053 NM 2008 2 7 2008UALA00428 1 20080124 A 5330 BUTT JOINT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 360 S6L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 SCRIBE LINE DAMAGE AT BUTT JOINT STA 360 BELOW STR 6L. MAJOR REPAIR: REMOVED DAMAGE. REPLACED BUTT JOINT INTERNAL STRAP S FROM STR 3L-10L. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700054 20080207 00054 NM 2008 2 7 2008UALA00433 1 20080124 A 2560 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR DISENGAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 533UA 25073 SLIDE AT DOOR 1R IS DISENGAGED FROM DOOR. REINSTALLED SLIDE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020700059 20080207 00059 2008 2 7 2008UALA00442 4 20080127 A 2565 LANYARD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 472UA 1435 LANYARD FOR DOOR 2R IS NOT PACKED INTO SLIDEPACK AND EXTENDS ABOUT 2 FT. REINSTALLED LANYARD AND CHECKED SLIDE ARMING A ND DISARMING POSITIONS, ALL NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020700061 20080207 00061 EU 2008 2 7 2008UALA00444 1 20080128 A 2400 ELECTRICAL SYS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MALFUNCTIONED A UALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 WP 29 462UA 1272 RTFL DUE TO COMPLETE ELECTRICAL FAILURE WITH LOSS OF COMMUNICATION AND INSTRUMENTS. GEAR COMMANDED TO RETRACT AND DID N OT. F/O'S PFD POWERED, BUT NO AIRSPEED OR AIR DATA INDICATIONS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020700076 20080207 00076 EA 2008 2 7 COMA0860069 1 20080114 A 2751 8004404 SENSOR CNDAIR CL600 CL6002B19 1900309 EA RT T/E FLAP FAULTY A COMA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 916CA 549 7014 FLIGHT 5175 - FLAPS FAIL CAUTION MESSAGE WHEN SELECTING FLAPS TO 8 DEGREES. AIRCRAFT LANDED SAFELY IN MSP. REMOVED AND REPLACED RIGHT SIDE NR 3 SKEW SENSOR. 2 L 7 2 4F RT A21EA 2008021200053 20080212 00053 NM 2008 2 12 2008UALA00491 1 20080129 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT LIGHT INOP AT DOOR 2 RIGHT BUSTLE. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200054 20080212 00054 2008 2 12 2008UALA00490 4 20080128 A 2565 D31591478U1 GAUGE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EVAC SLIDE OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 303UA 23644 FORWARD GALLEY DOOR ESCAPE SLIDE BOTTLE GAUGE NOT CENTERED IN VIEW WINDOW. CENTERED PRESSURE GAUGE IN INSPECTION WINDOW. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200058 20080212 00058 NM 2008 2 12 2008UALA00483 1 20080128 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 296-356 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 CABIN FLOOR STR 17R CREASE BEAM UPPER SURFACE CORRODED AT FWD GALLEY DOOR AREA BS 296-356. REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200059 20080212 00059 NM 2008 2 12 2008UALA00482 1 20080128 A 2612 FIRE LOOP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 ENGINE FAILED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 214UA 30220 RTFL DUE TO NR 2 ENGINE FIRE DETECTION LOOP FAILURE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021200069 20080212 00069 NM 2008 2 12 2008UALA00469 1 20080128 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT ROW 44 RT INOP. RESECURED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200070 20080212 00070 NM 2008 2 12 2008UALA00468 1 20080128 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT ROW 43LT INOP. RESECURED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200076 20080212 00076 NM 2008 2 12 2008UALA00460 1 20080125 A 3350 1317 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 671UA 30026 EMERGENCY LIGHT ON SEAT 3B IS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021200078 20080212 00078 NM 2008 2 12 2008UALA00457 1 20080125 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 671UA 30026 LEFT AND RIGHT MID LAV EEL LIGHTS INOP. REMOVED AND REINSTALLED. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021200079 20080212 00079 NM 2008 2 12 2008UALA00456 1 20080126 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 663UA 27160 LEFT SIDE CABIN FLOOR LIGHTING INOP IN BUSS AND 1ST CLASS. REPLACED LIGHTS, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021200086 20080212 00086 NM 2008 2 12 2008UALA00412 1 20080122 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 671UA 30026 SEAT 38H EMERGENCY STRIP LIGHT BROKEN. REMOVED AND REPLACED LIGHT STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021200096 20080212 00096 NM 2008 2 12 2008UALA00385 1 20080120 A 5270 848401 PROXIMITY SENSOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FWD CARGO DOOR FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 855UA 1737 RTFL DUE TO FWD CARGO DOOR OPEN INDICATION. PROX SNSR 30WV TGT POS ECAM. PROX SENSOR FAILURE. REPLACED PROX SENSOR 30 WV. OPS CHECKED NORMAL. NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021200099 20080212 00099 NM 2008 2 12 2008UALA00370 1 20080121 A 3510 MF20010 OXYGEN MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 801UA 686 WHEN TESTING OBSERVERS O2 MASK, MASK DID NOT RESEAT AND CONTINUED TO PURGE O2. OBSERVER`S MASK LEAKING. REPLACED OBSER VERS MASK ASSY AND LEAK CHECKED. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021200100 20080212 00100 WP 2008 2 12 08FDEA00361 1 20080206 A 5347 4929148 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 388FE 46622 MCD SEAT TRACK AT BS 650-730 LBL 107 IS WORN. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1. 2 L 7 3 4F RT A22WE 2008021200104 20080212 00104 NM 2008 2 12 2008UALA00363 1 20080121 A 3350 CAP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN MISSING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 652UA 25390 EEL END CAP MISSING, BY 1E. REPLACED END CAP. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021200108 20080212 00108 NM 2008 2 12 2008UALA00359 1 20080122 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 RIGHT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP 4 EA LIGHT ASSY'S. RELAMPED EMERGENCY LIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200111 20080212 00111 NM 2008 2 12 2008UALA00358 1 20080122 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY EXIT LIGHT INOP AT DOOR 3 RIGHT FWD SILL. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200120 20080212 00120 NM 2008 2 12 2008UALA00348 1 20080120 A 3350 9F9948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 DOOR 5 LEFT EMERGENCY LIGHT EXIT SIGN INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200126 20080212 00126 NM 2008 2 12 2008UALA00345 1 20080120 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHTS AT ROW 6 TO 8 RT & ROW 55 TO 61 LT ARE INOP. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200127 20080212 00127 NM 2008 2 12 2008UALA00343 1 20080120 A 3350 1317 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 791UA 26933 EMERGENCY EXIT LIGHT OUTSIDE DOOR 3L INOPERATIVE. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021200133 20080212 00133 NM 2008 2 12 ASAA0842519 1 20080121 A 5750 TORQUE SHAFT BOEING 737 7374Q8 138447Q NM LT WING TE FLAPS BINDING A ASAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 NM 02 762AS 25099 FLAPS WOULD NOT EXTEND BEYOND 9 + 1. FLAPS WERE SYMMETRICAL BUT DID NOT AGREE WITH FLAP HANDLE COMMAND TO 15DEGS. FLAP WOULD NOT MOVE USING "ALT FLAPS". OPS FROM QRC EMERGENCY DECLARED. DIVERTED TO KTN. FOUND LT WING INBD FLAP MID FLAP TORQUE SHAFT DOOR BINDING AND RESTRICTING FLAP MOVEMENT. RELEASED PER CDL 57 53 1. LT INBD MID FLAP TORQUE SHAFT CLEA RANCE DOOR REMOVED. 2 L 7 2 4F RT A16WE 2008021200134 20080212 00134 NM 2008 2 12 2008UALA00336 1 20080117 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 528UA 25018 LEFT FWD EXT EMERGENCY SLIDE LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200137 20080212 00137 NM 2008 2 12 2008UALA00333 1 20080119 A 3397 58781 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 531UA 25042 EEL LIGHTS FROM ROWS 32-34 ARE INOPERATIVE. REPLACED FEEDER. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200138 20080212 00138 NM 2008 2 12 2008UALA00328 1 20080120 A 3350 FU305 FUSE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN BLOWN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 527UA 24995 L-1 AND R-1 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200142 20080212 00142 EU 2008 2 12 2008UALA00318 1 20080118 A 3350 321452 EPSU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 453UA 1001 EPSU BATTERY EMER R FAULT FOUND WHEN TESTING EMERGENCY LIGHTS. FAULTY EPSU. REPLACED EPSU, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020800288 20080208 00288 NM 2008 2 8 SWAA080627 1 20080203 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 805, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020800297 20080208 00297 WP 2008 2 8 AALA200800132 1 20080121 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9617R 53564 DFW - EMERGENCY EXIT MARKER AT LEFT TAIL COMPARTMENT SIDEWALL INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT MAR KER AT LEFT TAIL COMPARTMENT SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800307 20080208 00307 NM 2008 2 8 AALA200800110 1 20080119 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 197AN 32391 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020800377 20080208 00377 WP 2008 2 8 UPS08851544 1 20080122 A 5730 STRUCTURE DOUG DC8 DC873F 302199F WP LT WING MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 APPROX 3/8 BY 1 INCH PIECE OF SHEETMETAL MISSING ON T/E OF WING. LOCATED ON LT WING INBD OF NR 3 SPOILER PANEL. ACCOMP LISHED EO DC8-5730-28460A. 2 L 7 4 4F RT 4A25 2008020800401 20080208 00401 NM 2008 2 8 SWAA080669 1 20080204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020800407 20080208 00407 NM 2008 2 8 SWAA080678 1 20080205 A 5340 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 410, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020800408 20080208 00408 NM 2008 2 8 SWAA080679 1 20080205 A 5311 6546535 FRAME BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 13L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008021100011 20080211 00011 NM 2008 2 11 DLM90080153 1 20080201 A 5320 WEB DOUG MD90 MD9030 3023690 NM FS 210 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 L1 DOOR CUTOUT AFT SIDES FS 210 WEB FINGER CRACKED FWD FASTENER HOLE AT LONG 15. REPAIRED DAMAGE ON L1 DOOR CUTOUT AFT SIDE IAW MD-90 SRM 51-11-01 ON N/R 2000-0190 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008021100015 20080211 00015 EA 2008 2 11 SWIA200819197 1 20080205 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 440SW 7589 FLT 3822 - CAPTAINS SIDE WINDOW CRACKED. REPLACED WINDOW IAW 56-12-01, PN NP-139322-11, SN/OFF 03170H6806. 2 L 7 2 4F RT A21EA 2008021100024 20080211 00024 SW 2008 2 11 WGEA200800010 1 20080124 A 3150 WARNING MESSAGE ECLIPS EA500 ECLIPSEEA500 3350000 SW 7013348949 FALSE ACTIVATION E WGEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 146DJ 000058 CAS MESSAGE AIRSPEED DISAGREE ON TAKEOFF, 70 KTS LIGHT RAIN CALM WINDS (ABORTED T/O). PERFORMED FLIGHT ENVIRONMENT DATA ADJUSTMENT TEST IAW EA 500 M/M 34-10-00. SYSTEM TEST AND CHECKS GOOD, NO DEFECTS NOTED. 1 L 7 2 4J RT A00002AC 2008021100027 20080211 00027 EA 2008 2 11 SWIA200819177 1 20080129 A 3350 LENS CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 706SK 10149 FLT 6403 - EMERGENCY FLOOR LIGHT LENS IS MISSING. REPLACED LENS ASSEMBLY PER CRJ CMM 33-51-00. 2 L 7 2 4F RT A21EA 2008021100042 20080211 00042 EA 2008 2 11 SWIA200819169 1 20080202 A 2910 LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 07 492SW 7168 FLT 3776 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT. REPLACED LEAKING FLEX LINE TO ACTUATOR. NO LEAKS NOTED. 2 L 7 2 4F RT A21EA 2008021100067 20080211 00067 NM 2008 2 11 AALA200800152 1 20080123 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 767AJ 33539 DFW - EMERGENCY LIGHT AT SEAT 31C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021100084 20080211 00084 NM 2008 2 11 AALA200800194 1 20080128 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 946AN 30600 TUL - EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK AT STATION 727 RIGHT BUTT LINE 68 FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008021100086 20080211 00086 NM 2008 2 11 AALA200800155 1 20080123 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 767AJ 33539 DFW - EMERGENCY LIGHT AT SEAT 43G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 43G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021100088 20080211 00088 WP 2008 2 11 UPS08851561 1 20080107 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FS320 LBL55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK HAS LUG MISSING, LUG CRACKED AND TRACK GOUGED, STA 320 LBL55. REPAIRED MAIN CA BIN SEAT TRACK AT STA 320 AND LBL 55 REF SRM 53-02-03- 0 FIG 006D AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 2008021100091 20080211 00091 SO 2008 2 11 FDKA200801045 1 20080129 A 5411 FRAME EMB 145 EMB145LR 3260212 SO RT NACELLE CHAFED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 834MJ 145340 THE FOURTH RIB FROM THE FORWARD END OF THE RT LOWER COWLING IS CHAFED OUT OF LIMITS AT THE CENTER OF THE COWLING. THE D AMAGED FRAME HAS BEEN REPAIRED. 2 L 7 2 4T RT T00011AT 2008021100146 20080211 00146 WP 2008 2 11 UPS08851602 1 20080110 A 5541 RIB DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 16TH RIB FROM BOTTOM OF RUDDER ON LE CAVITY CRACKED. RUDDER REPLACED ON N/R 123801. 2 L 7 4 4F RT 4A25 2008021100166 20080211 00166 WP 2008 2 11 AALA200800187 1 20080127 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 408AA 49319 LGA - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008021100181 20080211 00181 2008 2 11 WGEA200800027 4 20080207 A 3414 INDICATOR ECLIPS EA500 ECLIPSEEA500 3350000 SW AIRSPEED MALFUNCTIONED E WGEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 158DJ 000074 ON TAKEOFF ROLL, NO AIRSPEED INDICATIONS ON LEFT PFD, MFD AND RIGHT PFD INDICATED UP TO 65KTS PRIOR TO ABORT. CONNECTED BARFIELD DPS 450 TO AIRCRAFT IAW AMM 34-10-00-070-701 TO SIMULATE AIRSPEED ON LEFT PFD. AIRSPEED CORRESPONDED WITH TES T BOX. SUSPECT MOISTURE WAS PRESENT EARLIER. 1 L 7 2 4J RT A00002AC 2008021100190 20080211 00190 WP 2008 2 11 DHL2007873540 1 20080113 A 5740 FITTING DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 NR 2 MAIN TANK FWD FITTING CRACKED BETWEEN STA XRS 74.000 AND S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1- 0 PG 1. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1 SRM 51-1-20D. CLEANED APPLIED POLYURETHANE TOP YELLOW COATING TO A REA IAW SRM 51-1-12 PG 7. INSTALLED NEW FITTING IAW SRM 51-1-12 SRM 51-3-0 SRM 51-1-23 (PLI-WASHER) SRM 51-1-20D SRM 51 -3-1 (TORQUE) REFER TO NR 107160 FOR LEAK CHECK. 2 L 7 4 4F RT 4A25 2008021200016 20080212 00016 EA 2008 2 12 A6WA200840036 1 20080112 A 7110 NOSE COWL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT ENGINE WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 LT ENGINE LOWER NOSE COWL (432AB) AFT CORNER WORN THIN.. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200041 20080212 00041 NM 2008 2 12 2008UALA00505 1 20080130 A 5311 FRAME SPLICE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 AFT PIT STA 1520 BETWEEN STR 24R AND 25R FRAME SPLICE HAS TOOL MARKS. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200049 20080212 00049 NM 2008 2 12 2008UALA00495 1 20080129 A 3350 9F199948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT LIGHT INOP AT DOOR 5 LEFT BUSTLE. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200056 20080212 00056 NM 2008 2 12 2008UALA00488 1 20080128 A 5347 SEAT TRACK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 AFT CABIN FLOOR SUPPORT BS 986 TO 1016 O/B SEAT TRACK H-CHANNEL UPPER SURFACE IS CORRODED RBL 37 TO 41. FABRICATED & IN STALLED SEAT TRACK. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200064 20080212 00064 EU 2008 2 12 08FDEA00342 1 20080201 A 5330 A53973276206 SKIN AIRBUS 300 A300B4605R 3930308 EU FUSELAGE GOUGED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 684FE 802 AFT CARGO PIT DOOR CUTOUT, FUSELAGE SKIN GOUGED FWD LOWER CORNER OF CUTOUT FR 59A, STR 40-41R. BLENDED GOUGE IAW SRM 5 1-73-10. FOUND OUT OF LIMITS IAW SRM 51-40-21. REWORKED AREA IAW SRM 53-17-12-101 C-2 FIG. 104. FOUND TO BE WITHIN LIM ITS. ALODINED, PRIMED & TOP COATED APPLIED IAW SRM 51-23-20, 51-21-10, 51-40-21. 2 L 7 2 4F RT A35EU 2008021200065 20080212 00065 WP 2008 2 12 DELA200800001 2 20080207 A 7261 OIL SYSTEM LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE7313A 01518 WP ENGINE LOW E DELA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 122LX 030 P85164 DURING CLIMB DETECTED LIGHT SMOKE ODOR IN A/C. OIL PRESSURE LIGHT CAME ON IN FLIGHT CLIMBING THROUGHFL300, REMAINED ON F OR APPROX 1 MIN. ANALOG GAUGE SHOWED 25 PSI. PULLED POWER TO IDLE TO START S/D PROCEDURE AND EVENTUALLY OIL PRESSURE BEC AME NORMAL. MONITORED CAREFULLY UNTIL LANDING AND REMAINED NORMAL. INSPECTED ENGINE AFTER LANDING AND FOUND NO OIL IN SI GHT GLASS. 2 L 7 2 4F 4 F A10CE E6WE 2008021200075 20080212 00075 NM 2008 2 12 2008UALA00461 1 20080128 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 796UA 26931 EMERGENCY PATH LIGHT IS OUT OF ITS TRACK 3F. RESECURED PATH LIGHTING. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021200077 20080212 00077 NM 2008 2 12 2008UALA00459 1 20080125 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 671UA 30026 EMERGENCY EXIT SEAT LIGHTS INOP RIGHT SIDE ROWS 26-36. RESECURED CONNECTOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021200102 20080212 00102 EU 2008 2 12 2008UALA00367 1 20080121 A 2740 3945128102 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELAC 2 FAULTY A UALA O OTHER W INADEQUATE Q C CL CLIMB 1 WP 29 491UA 1741 ON DEPARTURE FIRST OFFICERS PITCH TRIM DID NOT WORK. AIRCRAFT PITCHED UP UNTIL OVERRIDDEN WITH NOSE DOWN JOYSTICK COMMA ND. CAPT PITCH TRIM WORKS NORMAL WHEN COUPLED WITH EITHER AUTOPILOT. ELAC2 FAULT. REPLACED ELAC2, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021200131 20080212 00131 NM 2008 2 12 2008UALA00339 1 20080119 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INTERMITTENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 EMERGENCY STRIP LIGHTING BETWEEN ROWS 15 AND 25 CONTINOUSLY FLICKER ON AND OFF. COULD NOT DUPLICATE. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021200146 20080212 00146 EU 2008 2 12 2008UALA00316 1 20080118 A 2597 D31516113 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 428UA 523 CABIN EMERGENCY LIGHTS TEST FAILED EXT LOADS FWD L. WIRING SHORT IN SLIDE PACK. REPLACED SLIDE AT DOOR 1R. OPS CHECKE D NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021200147 20080212 00147 NM 2008 2 12 ASAA0842525 1 20080116 A 5280 65C2817829 SKIN BOEING 737 7374Q8 138447Q NM LT MLG DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 LT MLG INNER GEAR DOOR AFT EDGE CRACKED PREPARED DAMAGED AREA APPLIED SEVERAL LAYERS OF BMS 3 FIBERGLASS CLOTH AND BONDE D IN ACCORDANCE WITH B737 400 SRM 52 80 02 REPAIR 2 AND 52 40 02 PG 203. 2 L 7 2 4F RT A16WE 2008021200153 20080212 00153 NM 2008 2 12 ASAA0842524 1 20080110 A 5753 6546430189 SKIN BOEING 737 7374Q8 138447Q NM TE FLAPS DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 LT INBOARD AFT FORE FLAP LWR SURFACE CLUSTER OF DENTS BEHIND NR 2 TIRE. PREPARED DAMAGED AREA, FABRICATED EXTERAL DOUBL ER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008021200158 20080212 00158 NM 2008 2 12 ASAA0842526 1 20080110 A 5753 6546435281 SKIN BOEING 737 7374Q8 138447Q NM TE FLAPS DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 LT OUTBOARD AFT T/E FLAP DENTED ON UPPER SURFACE 68" FROM OUTBOARD B AND 1.5 INCH FROM T/E REMOVED DAMAGED AREA. FABRIC ATED REPAIR DOUBLER PREPARED AREA AND BONDED IAW B737 400 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008021200161 20080212 00161 NM 2008 2 12 ASAA0842527 1 20080110 A 5753 6546435281 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 LT OUTBOARD T/E FLAP LWR SURFACE CLUSTER OF DENTS 2 INCHES TO 22 INCHES FROM INBOARD END AND 1 2" TO 8" FROM T/E. REMOV ED DAMAGED AREA. FABRICATED REPAIR DOUBLER, PREPARED AREA AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008020700077 20080207 00077 EA 2008 2 7 COMA0860070 1 20080115 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 675BR 7635 FLIGHT 5492 - FLAPS FAIL CAUTION MESSAGE RECEIVED WHEN SELECTING FLAPS TO 8 DEGREES, FLAPS REMAINED AT 0 DEGREES. EMERG ENCY DECLARED AND AIRCRAFT LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTIO N. 2 L 7 2 4F RT A21EA 2008020700080 20080207 00080 EA 2008 2 7 COMA0860073 1 20080116 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA RT T/E FLAP FAULTY A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 675BR 9956 7635 FLIGHT 4940 - FLAPS FAILED AT 0 DEGREES ON APPROACH TO YUL. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND RE PLACED RIGHT I/B FLAP I/B ACTUATOR. 2 L 7 2 4F RT A21EA 2008020700083 20080207 00083 EA 2008 2 7 COMA0860076 1 20080117 A 2760 4916406 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 629BR 9389 7251 FLIGHT 5653 - RECEIVED CONFIG SPOILERS WARNING MESSAGE. ABORTED TAKEOFF, RETURNED TO GATE WITHOUT INCIDENT. REPLACED L EFT SECU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008020700086 20080207 00086 EA 2008 2 7 COMA0860078 1 20080118 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA LT T/E FLAP FAULTY A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 926CA 10541 7027 FLIGHT 5094 - FLAPS FAILED AT 0 DEGREES WHEN SELECTED TO 8 DEGREES ON APPROACH. EMERGENCY DECLARED. AIRCRAFT LANDED SA FELY. REMOVED AND REPLACED LEFT I/B FLAP O/B ACTUATOR. 2 L 7 2 4F RT A21EA 2008020700087 20080207 00087 EA 2008 2 7 COMA0860079 1 20080118 A 2752 852D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA LT T/E FLAP FAULTY A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 926CA 10541 7027 FLIGHT 5094 - FLAPS FAILED AT 0 DEGREES WHEN SELECTED TO 8 DEGREES ON APPROACH. EMERGENCY DECLARED. AIRCRAFT LANDED SA FELY. REMOVED AND REPLACED LEFT I/B FLAP I/B ACTUATOR. 2 L 7 2 4F RT A21EA 2008020700091 20080207 00091 EA 2008 2 7 COMA0860082 1 20080118 A 2752 854D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SO 01 685BR 9764 7712 FLIGHT 5696 - FLAPS FAILED ON TAKEOFF UPON RETRACTION, FAILED AT 18 DEGREES. AIRCRAFT RETURNED BACK TO DSM AND LANDED S AFELY. REMOVED AND REPLACED LEFT O/B FLAP O/B ACTUATOR. 2 L 7 2 4F RT A21EA 2008020700093 20080207 00093 EA 2008 2 7 COMA0860084 1 20080118 A 2613 6243843 OVERHEAT SENSOR CNDAIR CL600 CL6002B19 1900309 EA RT WING FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 920CA 354 7022 FLIGHT 5452 - RECEIVED WING OVERHEAT WARNING MESSAGE IN FLIGHT. COMPLETED QRH, OPERATED STANDBY MODE. MESSAGE PERSISTE D. AIRCRAFT RETURNED TO CVG AND LANDED SAFELY. REMOVED AND REPLACED RIGHT WING OVERHEAT/SUFFICIENT HEAT SENSOR. 2 L 7 2 4F RT A21EA 2008020700094 20080207 00094 EA 2008 2 7 COMA0860085 1 20080118 A 2613 6243843 OVERHEAT SENSOR CNDAIR CL600 CL6002B19 1900309 EA RT WING FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 920CA 18927 7022 FLIGHT 5452 - RECEIVED WING OVERHEAT WARNING MESSAGE IN FLIGHT. COMPLETED QRH, OPERATED STANDBY MODE. MESSAGE PERSISTE D. AIRCRAFT RETURNED TO CVG AND LANDED SAFELY. REMOVED AND REPLACED RIGHT WING CONTROL SENSOR. 2 L 7 2 4F RT A21EA 2008020700097 20080207 00097 EA 2008 2 7 COMA0870088 1 20080118 A 2752 854D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA LT T/E FLAP FAULTY A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 926CA 11953 7027 FLIGHT 5094 - FLAPS FAILED AT 0 DEGREES WHEN SELECTED TO 8 DEGREES ON APPROACH. EMERGENCY DECLARED. AIRCRAFT LANDED SA FELY. REMOVED AND REPLACED LEFT O/B FLAP O/B ACTUATOR. 2 L 7 2 4F RT A21EA 2008020700101 20080207 00101 NM 2008 2 7 2008UALA00326 1 20080118 A 3350 1619 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EXTERIOR INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 EXTERIOR EMERGENCY LIGHT DOOR 1L IS INOP. RELAMPED. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700102 20080207 00102 EA 2008 2 7 COMA0860092 1 20080121 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 709CA 7238 FLIGHT 5620 - FLAPS FAIL CAUTION MESSAGE, FLAPS FAILED AT 0 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. COMPL IED WITH TASK CARD SI-2-27I0001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 2008020600063 20080206 00063 EA 2008 2 6 COMA0860048 1 20080102 A 2750 1104SD100301 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA LT TE FLAPS WORN A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 806CA 7359 FLIGHT 5636 - FLAPS FAIL CAUTION MESSAGE ON APPROACH INTO BOS. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED LEFT SIDE NR 3 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2008020600064 20080206 00064 EA 2008 2 6 COMA0860049 1 20080102 A 2750 1104SD100401 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA LT TE FLAPS WORN A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 01 806CA 7359 FLIGHT 5636 - FLAPS FAIL CAUTION MESSAGE ON APPROACH INTO BOS. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED LEFT SIDE NR 4 FLEX DRIVE SHAFT. 2 L 7 2 4F RT A21EA 2008020600071 20080206 00071 NM 2008 2 6 HNAA0800035 1 20080118 A 3320 TERMINAL DHAV DHC8 DHC8102 2809003 NM BALLAST BURNED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 808EX 39745 39745 299 ELECTRICAL BURNING ODOR COMING FROM OVERHEAD BIN 5 D/F AREA. FOUND OVERHEAD BIN LIGHT AT 5DF WITH BURNED TERMINAL ENDS. REPLACED TERMINAL END AND BALLAST, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2008020600073 20080206 00073 WP 2008 2 6 MWEA080014 1 20080123 A 5330 59360213 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 810ME 48072 AFT LAVATORY SERVICE PANEL, BOX AND FUSELAGE SKIN SEPARATED AND CORROSION LEVEL 1 FOUND IN BETWEEN AT FORWARD LOWER CORN ER. CUT OUT DAMAGE AND FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2008021200169 20080212 00169 NM 2008 2 12 USAA920080318 1 20080122 A 5755 6546451 SKIN BOEING 737 7374B7 1384702 NM NR 6 SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 458UW 25022 PHL - MAJOR REPAIR - RON - RIGHT WING FLIGHT SPOILER PANEL NR 6 IS DELAMINATED. REPLACED RIGHT WING SPOILER PANEL NR 6 IAW B737 AMM 27-61-11. 2 L 7 2 4F RT A16WE 2008021200178 20080212 00178 EU 2008 2 12 BA08003 1 20080201 A 3350 32146210 BATTERY PACK AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHTS FAULTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AY 0370 PHL - MAINTENANCE REPORTED THE L1 AND R2 BATTERIES FAULTED ON EMERGENCY LIGHT BATTERY TEST. MAINTENANCE REMOVED AND REP LACED THE EPSU'S AT L1 AND R2. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A46NM 2008021200181 20080212 00181 NM 2008 2 12 USAA920080302 1 20080115 A 5320 654587552 SUPPORT ANGLE BOEING 737 7373Y0 1384671 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 C18 CHECK, CORROSION ON THE R1 DOOR CREASEBEAM SUPPORT ANGLE, BS 312 - BS 328, S17R. REPLACED THE R1 DOOR CREASE BEAM S UPPORT ANGLE, BS 312 - BS 328, S17R IAW BOEING DRAWING 65-45875. 2 L 7 2 4F RT A16WE 2008021200182 20080212 00182 NM 2008 2 12 USAA920080303 1 20080122 A 5320 652072613 ANGLE BOEING 737 7373Y0 1384671 NM BS 492 S25-26R CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - CORROSION ON FORWARD CARGO COMPARTMENT DOOR CUT OUT ANGLE, BS 492.4, S25R - S26R. REPL ACED FORWARD CARGO COMPARTMENT DOOR CUT OUT ANGLE, BS 492.4, S25R - S26R IAW BOEING DRAWING 65-20726. 2 L 7 2 4F RT A16WE 2008021200184 20080212 00184 NM 2008 2 12 USAA920080305 1 20080126 A 5753 SKIN BOEING 737 7373Y0 1384671 NM LWS 289-295 DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK, LEFT WING OUTBOARD FORE FLAP, UPPER SURFACE HAS AREA OF DISBOND, WS 289 - WS 295. REPAI RED LEFT WING OUTBOARD FORE FLAP, UPPER SURFACE, WS 289 - WS 295 IAW B737 SRM 51-70-10-2R3. 2 L 7 2 4F RT A16WE 2008021200185 20080212 00185 NM 2008 2 12 USAA920080314 1 20080125 A 5531 RIB BOEING 767 7672B7ER 1385107 NM VERTICAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 C4 CHECK, VERTICLE STABILIZER RIB CRACKED, BS1 1767.7. REPLACED VERTICLE STABILIZER RIB CRACKED, BS1 1767.7 IAW B767 SR M 55-30-09. 2 L 7 2 4F RT A1NM 2008021200186 20080212 00186 NM 2008 2 12 USAA920080315 1 20080109 A 5347 SEAT TRACK BOEING 767 7672B7ER 1385107 NM BS 1098-1208 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK - NR 6051673, LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 1098 - BS 1208, RBL 88. REPLACED CABIN SEAT TRACK, BS 1098 - BS 1208, RBL 88 I/A/W B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008021200187 20080212 00187 NM 2008 2 12 USAA920080320 1 20080111 A 5311 65465323 FRAME BOEING 737 7373Y0 1384671 NM BS 480 S9L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK , CRACKED FRAME, BS 480, S9L. REPAIRED FRAME, BS 480, S9L IAW USAIRWAYS EA 100190. 2 L 7 2 4F RT A16WE 2008021200188 20080212 00188 NM 2008 2 12 USAA920080321 1 20080111 A 5311 90526911 FRAME BOEING 737 7373Y0 1384671 NM BS 807 S9L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 807, S9L. REPAIRED FRAME, BS 807, S9L IAW USAIRWAYS EA 100190. 2 L 7 2 4F RT A16WE 2008021200190 20080212 00190 NM 2008 2 12 USAA920080323 1 20080111 A 5311 90526911 FRAME BOEING 737 7373Y0 1384671 NM BS 480 S9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 480, S9R. REPAIRED FRAME, BS 480, S9R IAW USAIRWAYS EA 100190. 2 L 7 2 4F RT A16WE 2008021200195 20080212 00195 NM 2008 2 12 USAA920080328 1 20080111 A 5311 654655211 FRAME BOEING 737 7373Y0 1384671 NM BS 827 S9R/L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 827, S9L AND S9R. REPAIRED FRAME, BS 827, S9L AND S9R IAW USAIRWAYS E A 100190. 2 L 7 2 4F RT A16WE 2008021200196 20080212 00196 NM 2008 2 12 USAA920080329 1 20080111 A 5311 65465292 FRAME BOEING 737 7373Y0 1384671 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 440, S9L & S9R. REPAIRED FRAME, BS 440, S9L & S9R IAW USAIRWAYS EA 10 0190. 2 L 7 2 4F RT A16WE 2008021200197 20080212 00197 NM 2008 2 12 SB08006 1 20080203 A 3350 036000570010 FUSE BOEING 737 7374B7 1384702 NM EMERGENCY LIGHTS BLOWN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 DFW - MAINTENANCE REPORTED THE EMERGENCY PATH LIGHTING AT SEATS 3, 4 AND 5 INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE FUSE IN THE POWER SUPPLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008021200198 20080212 00198 NM 2008 2 12 DLM90080152 1 20080202 A 2170 V1211 COALESCER BAG DOUG MD90 MD9030 3023690 NM AFT ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 901DA 53381 ON LANDING ROLLOUT, SIGNIFICANT SMOKE/ODOR NOTICED IN CABIN AND COCKPIT. PERFORMED DUCT BURNOUT PROCEDURE PER AMM AND I NSPECTED ACM TURBINES. NO CONTAMINATION FOUND. INSPECTED APU INLET. NO CONTAMINATION NOTED. REPLACED COALESCER BAGS. RAN PACKS WITH APU AND ENGS. NO SMOKE/ODOR NOTED. 2 L 7 2 4F RT A6WE 2008021200200 20080212 00200 2008 2 12 ASAA0852535 4 20080202 A 2310 RADIO BOEING 737 737890 1384527 NM NR 1 HF MALFUNCTIONED A ASAA O OTHER O OTHER CR CRUISE 1 NM 02 558AS 35177 NR 1 HF RADIO GARBLED. SELCAL CHIME AND LIGHT OK. FREQ 6673 & 3452 ATTEMPTED IN FLIGHT. HF NR 2 VOICE AND SELCAL OK. UNABLE TO VERIFY DISCREPANCY. REPLACED AND TESTED NR 1 HF ANTENNA COUPLER IAW 23 11 61 PGS 401 409. NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A16WE 2008021200204 20080212 00204 NM 2008 2 12 ASAA0852533 1 20080201 A 4990 38809381 OIL FILTER BOEING 737 737890 1384527 NM APU CLOGGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 570AS 35185 DURING TASKCARD 78349013, FOUND APU OIL FILTER DELTA P INDICATOR EXTENDED. REPLACED OIL FILTER. RESET INDICATOR. INSP ECTED FILTER AND MAG PLUG. OP AND LEAK CHECKS GOOD. 2 L 7 2 4F RT A16WE 2008021200205 20080212 00205 WP 2008 2 12 UPS08851604 1 20080111 A 5542 SKIN DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 EDGE CRACK ON RT UPPER RADIUS OF RUDDER TAB CUT OUT. RUDDER REPLACED ON N/R 123801. 2 L 7 4 4F RT 4A25 2008021200208 20080212 00208 EU 2008 2 12 BA08004 1 20080202 A 3350 32146210 EPSU AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHTS FAULTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 272AY 33519 2128 0333 PHL - THE DOOR R3 EMERGENCY POWER SUPPLY UNIT (EPSU), FIN 16WL, FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED EPSU, FIN 16WL, ABOVE DOOR R3. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A46NM 2008021200209 20080212 00209 NM 2008 2 12 USAA920080330 1 20080202 A 5754 65C26601174 SKIN BOEING 737 73733A 1384673 NM RT WING SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 PHX - MAJOR REPAIR - NR 4321748, RIGHT WING NR 6 SLAT LOWER SURFACE CRACKED. REPLACED RIGHT WING NR 6 SLAT IAW B737 AMM 27-81-00. 2 L 7 2 4F RT A16WE 2008021200210 20080212 00210 NM 2008 2 12 USAA920080331 1 20080131 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 CLT - MAJOR REPAIR - RON - NR 4262403, CRACK FOUND ON THE R2 DOOR UPPER HINGE CUTOUT AREA. REPAIRED THE R2 DOOR UPPER H INGE CUTOUT AREA IAW USAIRWAYS EA 110574. 2 L 7 2 4F RT A2NM 2008021200216 20080212 00216 EU 2008 2 12 USAA920080340 1 20080201 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320231 3930325 EU LOW A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 620AW 52 FLT NR 9205 - PIT-PHX - EMERGENCY LANDING, DURING DESCENT RECEIVED HYDRAULIC GREEN RESERVOIR LOW LEVEL ECAM. VERIFIED I NDICATION AT TOP OF AMBER BAND. COMPLIED WITH ECAM AND SHUT DOWN GREEN SYSTEM UNTIL GEAR EXTENSION REQUIRED. AFTER GEA R EXTENSION LEVEL INCREASED AND NORMAL GREEN SYSTEM OPERATION RESUMED. CREW DECLARED AN EMERGENCY, LANDED WITHOUT INCID ENT AND TAXIED TO THE GATE. MAINTENANCE SERVICED GREEN SYSTEM TO PROPER LEVEL. NO LEAKS WERE NOTED. 2 L 7 2 4F RT A28NM 2008021200221 20080212 00221 EU 2008 2 12 USAA920080341 1 20080203 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 622AW 15063 2248 54 FLT NR 570 - LAS-PHX - EEL - RIGHT EMERGENCY POWER SUPPLY UNIT WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED RIGHT EM ERGENCY POWER SUPPLY UNIT PER AIRBUS MAINTENANCE MANUAL. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008021200225 20080212 00225 EA 2008 2 12 SWIA200819174 1 20080201 A 3230 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 927SW 7693 FLT 5881 - AFTER RETRACTING LANDING GEAR, RECEIVED A NOSE DOOR OPEN AND GEAR DISAGREE WARNING MESSAGE. REPLACED NOSE LA NDING GEAR SELECTOR VALVE IAW CRJ 200 AMM 32-33-10, P/N 750006000, S/N OFF 2032. 2 L 7 2 4F RT A21EA 2008021200226 20080212 00226 EA 2008 2 12 SWIA200819175 1 20080131 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 970SW 7881 FLT 6331 - CREW REPORTED BURNING ODOR NEAR ROW 7. INSPECTED LIGHT FIXTURES AND OVERHEAD PANELS AS WELL AS AVIONICS BAY. NO DISCREPANCY NOTED. NO ODOR NOTED. 2 L 7 2 4F RT A21EA 2008021100021 20080211 00021 NM 2008 2 11 200800028 1 20080204 A 5753 SKIN BOEING 747 74747UF 1384812 NM TE FLAPS PUNCTURED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 493MC 29254 DURING A CHECK, FOUND LT WING T/E I/B MID FLAP WBL 443.83 LOWER SURFACE CRACKED AND BULLNOSE PUNCTURE, IN ADDITION LT IB AFT FLAP WBL 445 OUTBOARD EDGE WITH DELAMINATION. DISPOSITION WAS MADE TO PERFORM A WET LAY UP INTERIM REPAIR (REF BOE ING SRM 57-53-01, FIG 201, AND BOEING SRM 51-40-06). 2 L 7 4 4F RT A20WE 2008021100032 20080211 00032 EU 2008 2 11 SIMA200803901 1 20080206 A 3240 TRANSDUCER SAAB SF340 340B 7860101 EU WHEEL SPEED LOOSE A SIMA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SW 21 340RC 340B340 ON FLIGHT 3085, CREW REPORTED ON DESCENT INTO SAN AFTER LANDING GEAR EXTENSION, THE ANTI-SKID FAULT LIGHT ILLUMINATED. CREW TRIED TO CYCLE THE ANTI-SKID SYSTEM AS WELL AS CYCLING THE LANDING GEAR. ALL EFFORTS TO CLEAR THE FAULT WITH NO HE LP. CREW FOLLOWED AOM AND DETERMINED THAT THE RUNWAY IN SAN WAS NOT LONG ENOUGH FOR A NON ANTI-SKID LANDING. CREW ELEC TED TO RETURN TO LAX. AIRCRAFT DECLARED A EMERGENCY LANDING. THE AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND WHEEL SPEED TRANSDUCER LOOSE RECONNECTED WHEEL SPEED TRANSDUCE R AND NR 8194; NR 8194; AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2008021100045 20080211 00045 CE 2008 2 11 1356875020308 1 20080130 A 8011 642086A15R ADAPTER CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO STARTER FAILED E HYIA E ENGINE SHUTDOWN K R J FLUID LOSS PARTIAL RPM/PWR LOSS WARNING INDICATION LD LANDING 1 EA 61 6875D 703 402C0511 832058R ON SHORT FINAL OF APPROACH PILOT NOTICED RT PROP WANDERING, LOOKED AT GAGES AND SAW RT OIL PRESSURE AT 0. PILOT SHUTDOW N ENGINE AND FEATHERED PROP. AIRCRAFT LANDED WITHOUT INCIDENT. UPON INITIAL INVESTIGATION FOUND OIL ON RT MLG DOOR. M X INSPECTED ENGINE AND FOUND TEETH TO STARTER ADAPTER AND ENGINE LARGE CRANK SHAFT GEAR MISSING. UPON TALKING TO PILOT GROUP FOUND SEVERAL INSTANCES OF STARTER KICK BACK. THIS FAILURE HAS BEEN REFERRED TO CONTINENTAL MOTORS FOR FURTHER IN VESTIGATION OF CAUSE OF TEETH FAILURE. 1 L 7 2 3O 3 O A7CE E8CE 2008021100056 20080211 00056 NM 2008 2 11 UPS08451553 1 20080124 A 3350 7003122 LIGHT BOEING 747 747121 1384871 NM COCKPIT/SLIDE INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 683UP 20353 EMERGENCY LIGHT ABOVE SLIDE IN COCKPIT INOP. DEFERRED PER MEL 33-15 ON ITEM M367673. SLAVED IN NEW BATTERY PACK POWER SUPPLY, NO HELP. REMOVED AND REPLACED EMERG EXIT SIGN IAW AMM 33-1-51-04. EXIT LIGHT ASSY REPLACED PER MM 33-50-00. O PERATION NOW CHECKS NORMAL. 2 L 7 4 4F RT A20WE 2008021100072 20080211 00072 NM 2008 2 11 AALA200800142 1 20080123 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 608AA 27446 DFW - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2008021100074 20080211 00074 NM 2008 2 11 EIA2008010 1 20080119 A 3350 1317 BULB BOEING 747 747212B 1384886 NM EMERGENCY LIGHTS NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482EV 20713 R5 DOOR EMERGENCY EXIT AFT SILL LIGHT INOP. RELAMPED R5 EMERGENCY EXIT AFT SILL LIGHT PER 33-51-00. OPS CHECKED NORMAL . 2 L 7 4 4F RT A20WE 2008021100090 20080211 00090 NM 2008 2 11 AALA200800154 1 20080123 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 767AJ 33539 DFW - EMERGENCY LIGHT AT SEAT 38C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 38C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021100096 20080211 00096 WP 2008 2 11 UPS08851514 1 20080103 A 2750 5751152503 DRIVE ASSY DOUG DC8 DC871F 302199D WP TE FLAPS CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 ULTRASONIC INSPECTION, DETECTED A RADIAL CRACK ON THE INBD LUG OF THE LT WING FLAP DRIVE LINK AT STA XW 97 AT POINT "J". REMOVED AND REPLACED LT WING FLAP DRIVE LINK AT STA XW 97 IAW DC8- AMM 27-51-04-2. 2 L 7 4 4F RT 4A25 2008021100102 20080211 00102 NM 2008 2 11 DL777080147 1 20080201 A 5330 141W13254 SKIN BOEING 777 777232 1385232 NM STA 424-455 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 865DA 29737 FUSELAGE SKIN HAD LIGHTNING STRIKE DAMAGE AT STA 424 AND STA 455 AT S-10L. ALSO, THE S-10L STRINGER SUSTAINED TOOLING D AMAGE DURING ACCOMPLISHMENT OF THE SKIN REPAIRS. THE DAMAGED SKIN WAS CUT OUT AND REPAIR DOUBLERS WERE INSTALLED. THE DAMAGE IN THE STRINGER FLANGE WAS TRIMMED OUT AND A REPAIR ANGLE WAS INSTALLED. 2 L 7 2 4F RT T00001SE 2008021100107 20080211 00107 EA 2008 2 11 MASA200800062 1 20080124 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27191 7191 FLT 2982 - PHX-SLC - MAIN CABIN DOOR EMERGENCY LIGHT STRIP HAS 2 BULBS BURNED OUT AND EMERGENCY CEILING LIGHT AT ROW 14 INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008021100114 20080211 00114 2008 2 11 UPS08851613 4 20080204 A 2565 GAUGE DOUG DC8 DC873F 302199F WP SLIDE PRESSURE UNSERVICEABLE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 ESCAPE SLIDE PRESSURE GAUGE NOT VISIBLE. REPOSITIONED SLIDE IN CASE FOR PRESSURE GAUGE TO READABLE FROM WINDOW. 2 L 7 4 4F RT 4A25 2008021100138 20080211 00138 WP 2008 2 11 08FDEA00331 1 20080130 A 5320 AGA71703 BEAM DOUG DC10 DC1030F 3023504 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 CTR CARGO COMPT ON BEAM FOUND CRACK 0.70" LONG. REPAIRED BEAM IAW SRM 53-00-01 VOL I FIG 4 SHT 2. 2 L 7 3 4F RT A22WE 2008021100168 20080211 00168 WP 2008 2 11 UPS08851569 1 20080129 A 2910 AE2463532J0970 HOSE DOUG DC8 DC873F 302199F WP HYD SYSTEM CHAFED A IPXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 807UP 46007 THE CREW EXPERIENCED A HYDRAULIC LEAK. AFTER RUNNING THE CHECKLIST, DECLARED AN EMERGENCY AND CONTINUED TO PHL. AFTER APPROX 20 MIN IN CRUISE, LOST HYD QTY DOWN TO AUX AT THE "X" AND AIL CTRL MANUAL AND RUDDER CTRL MANUAL LTS ILLUM. RAN LOSS OF HYD FLUID/PRSR CK LIST. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PUMP PRESSURE HOSE ASSY. 2 L 7 4 4F RT 4A25 2008021100169 20080211 00169 WP 2008 2 11 UPS08851573 1 20080107 A 5522 SKIN DOUG DC8 DC871F 302199D WP RT ELEVATOR CANNING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 O/B UPPER SKIN IS OIL CANNED ON RT ELEVATOR. REPAIRED RT ELEVATOR O/B UPPER SKIN REF DWG 5654970 AND SRM 55-02-01 FIG 008. 2 L 7 4 4F RT 4A25 2008021100173 20080211 00173 WP 2008 2 11 AALA200800073 1 20080116 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9403W 53139 LGA - EMERGENCY EXIT SIGN LIGHTS AT OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHTS AT OVERW ING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008021100182 20080211 00182 SW 2008 2 11 WGEA200800022 1 20080205 A 3244 M16901 TIRE ECLIPS EA500 ECLIPSEEA500 3350000 SW ZONE 700 FAILED E WGEA O OTHER J WARNING INDICATION LD LANDING 1 EA 27 145DJ 48 000057 AFTER TOUCHDOWN, BOTH MAIN TIRES FAILED. REMOVED UNSERVICEABLE WHEEL AND BRAKE ASSEMBLIES ON BOTH LEFT AND RIGHT LANDIN G GEAR. INSPECTED LANDING GEAR, UNDER WINGS, FLAPS, AIRCRAFT, AND ENGINES BOTH LEFT AND RIGHT ON AIRCRAFT. NO DEFECTS N OTED. INSTALLED NEW SERVICEABLE BRAKE ASSEMBLIES AND INSTALL REPAIRED SERVICEABLE WHEEL ASSEMBLIES, BOTH LEFT AND RIGHT. SERVICED AND BLED BRAKES. WORK COMPLETED IAW EA500 AMM CHAPTER 32 PER 40, 41, 42. 1 L 7 2 4J RT A00002AC 2008021100189 20080211 00189 NM 2008 2 11 DLM90080150 1 20080201 A 5220 ESCAPE HATCH DOUG MD90 MD9030 3023690 NM FUSELAGE LOOSE A DALA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 SO 27 906DA 53386 FLIGHT DIVERTED TO DEN DUE TO FLAPS NOT DEPLOYING AND GEAR HANDLE WOULD NOT MOVE TO THE DOWN POSITION. AFTER ARRIVAL SY S CK FOUND FLAPS AND GEAR HANDLE OPS NML. FOUND WATER IN AREA OF FLOOR WHERE CABLES AND FAIRLEADS FOR FLAP AND GEAR ACT UATION PASS INTO THE GEAR WELL. FOUND ALL 4 OVERWING EXIT DOORS OUT OF RIG. THEY DID NOT HAVE THE MIN AMOUNT OF PRESS. REQUIRED TO LATCH THE DOOR. NO OTHER CAUSE OF WATER SOURCE FOUND. REMOVED WATER, ADJUSTED OVERWING DOORS PER M/M. S USPECT WATER MIGRATED FROM OVERWING DOOR AND INTO AREA AND FROZE FAIRLEADS. A/C BACK IN SERVICE 04:30 02/02/08. 2 L 7 2 4F RT A6WE 2008021100191 20080211 00191 WP 2008 2 11 DHL2007873518 1 20080112 A 5720 STIFFENER DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 NR 3 MAIN TANK STIFFENER CRACKED 4" AT STA XRS 69.500. REMOVED CRACKED STIFFENER IAW SRM 51-1-20D, SRM 51-1-21. CLEANE D AND APPLIED POLYURETHANE TOP YELLOW COATING TO AREA IAW SRM 51-1-12 PG 7. INSTALLED NEW STIFFENER IAW SRM 51-1-120D, SRM 51-3-1 (TORQUE), REFER TO JC EC-00717 (WO 2837) FOR STIFFENER FABRICATION. 2 L 7 4 4F RT 4A25 2008021100192 20080211 00192 WP 2008 2 11 DHL2007873519 1 20080120 A 5754 FRAME DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 LT WING L/E CONSTANT SECTION UPPER FORMER CRACKED 1 1/4" STA XCW 69.000. REMOVED CRACKED FORMER IAW SRM 51-1-20D, SRM 5 1-3-0. FABRICATED NEW FORMER (AL7075"0" 0.090") IAW SRM 57-3-3 FIG. 1, DOUGLAS DWG 5769646. HEAT TREATED FORMER FROM 7 075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED FORMER IAW SRM 51-3 -0, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2008021200002 20080212 00002 NM 2008 2 12 USAA920080339 1 20080204 A 5210 507945259 DOOR FRAME BOEING 737 7373Y0 1384671 NM ZONE 800 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - NR 6076267, CRACKED L2 DOOR AFT FRAME, BS 342 AT BEAM 12. REPAIRED THE L2 DOOR AFT FRA ME, BS 342, AT BEAM 12 IAW USAIRWAYS EA 100225. 2 L 7 2 4F RT A16WE 2008021200012 20080212 00012 EA 2008 2 12 A6WA200840039 1 20080115 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 PAX DOOR SURROUND STRUCTURE CAM FITTING GOUGE ON FS 349, STR 5L. REPLACED IWA SRM 51-42-21. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200028 20080212 00028 EA 2008 2 12 A6WA200840021 1 20080114 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 ANGLE CRACK ON IB SIDE OF FLOORBEAM AT FS 280, RBL 9. NEW ANGLE INSTALLED ON IB SIDE OF FLOORBEAM AT FS 280, RBL 9, SRM 51-42-20. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200067 20080212 00067 NM 2008 2 12 2008UALA00471 1 20080126 A 3350 SCREW BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LIGHT RECEPTACLE MISSING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 524UA 24977 EXTERIOR EMERGENCY EXIT LIGHT INOP AT DOOR 4R. REPLACED MISSING SCREWS. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200074 20080212 00074 EU 2008 2 12 2008UALA00462 1 20080127 A 3350 BR964422 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 404UA 450 SEAT MOUNTED FLOOR PROXIMITY EMERGENCY ESCAPE LIGHT OUT AT SEAT 24C. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021200098 20080212 00098 NM 2008 2 12 2008UALA00382 1 20080122 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY EXIT CEILING LIGHT INOP JUST INBOARD OF LAV 101. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200117 20080212 00117 2008 2 12 2008UALA00350 4 20080121 A 2565 STRAP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 402UA 439 PART OF SLIDE PACK IS HANGING FROM DOOR 1R WHILE THE DOOR IS CLOSED. D RING STRAP WAS OUTSIDE OF PACK ASSY, SECURED THE D RING STRAP, INSP SLIDE. ALL OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021200243 20080212 00243 2008 2 12 AMTA200800012 4 20080110 A 3160 4058650950 DISPLAY BOEING 757 75723N 1384973 NM RROYCE RB211 RB211* 54555 NE COCKPIT MALFUNCTIONED A AMTA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 11 514AT 27971 F/O MCDU BLANK. REMOVED AND REPLACED FO`S MCDU, IAW AMM 34-60-00, OPS CHECKS GOOD. (K) 2 L 7 2 4F 4 F RT A2NM A12EU 2008021200244 20080212 00244 NM 2008 2 12 AMTA200800014 1 20080111 A 4920 380029817 APU BOEING 757 75733N 1384931 NM RROYCE RB211 RB211* 54555 NE UNSERVICEABLE D AMTA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 11 550TZ 22108 22108 32584 APU ON START OIL QTY FLLUXUATION, CHIP DETECTOR HAS DEBRIS AND OIL DRAINS FROM CHECK VALVE TO ZERO QTY. REPLACED APU IA W M57-49-02. APU OPS AND LEAK CHECKED GOOD. (K) 2 L 7 2 4F 4 F RT A2NM A12EU 2008021200247 20080212 00247 EA 2008 2 12 A6WA200840004 1 20080101 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE WING FAILED A A6WA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 31 449AW 7818 FLAPS FAILED ON RETRACTION AFTER LANDING. RT FLAP INDICATES -0- DEGREES, LT FLAP INDICATES 22 DEGREES. C/W FLAP RESET, FLAP FAIL DID NOT CLEAR. FOUND FLAPS COVERED WITH ICE AND SNOW, PUT AC IN HANGAR TO THAW. PERFORMED RESET IAW AWAC SUP PLEMENT 98-018B AND PERFORMED OPS CK AND SYSTEM CHECK OF FLAPS IAW 27-50-00, OPS CHECK GOOD. NO FAULT CODES NOTED. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200250 20080212 00250 EA 2008 2 12 A6WA200840007 1 20080104 A 2740 70623 TRIM SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE STABILIZER MALFUNCTIONED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 31 441ZW 5048 7777 ON CLIMBOUT WITH FLAPS 8 DEGREES, STAB AND MACH TRIM WOULDN`T REMAIN ENGAGED. COMPLIED WITH QRH, RE-ENGAGED STAB AND MA CH TRIM, BOTH DISENGAGED AND WOULDN`T REENGAGE. SET FLAPS TO 2- DEGREES, RETURNED TO DEPARTURE. REMOVED AND REPLACED F O`S HORIZONTAL STAB TRIM SWITCH IAW AMM 27-14-05, NO FIX. REMOVED AND REPLACED HSTCU IAW AMM 27-41-01. OPS CHECK GOOD, I AW AMM 27-40-00. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200253 20080212 00253 NM 2008 2 12 AMTA200800017 1 20080117 A 3350 20131A BATTERY PACK BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 EMERGENCY PATH FLOOR LIGHTING INOPERATIVE, ROW 1-8. REPLACED BATTERY PACK. OPS CHECK GOOD REF MM 33-51-07. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008021200261 20080212 00261 NM 2008 2 12 2008UALA00508 1 20080130 A 3510 S475W0013 OXYGEN SYSTEM BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CREW O2 LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 221UA 30552 CREW OXYGEN IS LOW. SUSPECT LOW DUE TO PRE FLIGHT CHECKS. SERVICED CREW OXYGEN BOTTLE. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021200268 20080212 00268 NM 2008 2 12 2008UALA00519 1 20080130 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 DOOR 4R FWD EMERGENCY SILL LIGHT IS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200272 20080212 00272 NM 2008 2 12 2008UALA00523 1 20080129 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN ARCED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 655UA 25393 THE 9B READING LIGHT WIRES EXPOSED AND ARCING. REPLACED READING LIGHT OPS CHECK NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021200273 20080212 00273 NM 2008 2 12 2008UALA00524 1 20080129 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 665UA 29237 SEAT 17H EEL INOPERATIVE. REPLACED LIGHT STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020600075 20080206 00075 SO 2008 2 6 C2XA08SH018 1 20080202 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15973 145159 SHV - DURING C-CHECK LEFT OMEGA BEAM WEB AND FLANGE AT FR 20 HAS CORROSION. MX REPAIRED LEFT OMEGA BEAM BETWEEN FRM 19- 23 IAW EC5320-01229. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008020600118 20080206 00118 EA 2008 2 6 MASA200800093 1 20080121 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 570ML 7206 REPAIR TO PILOT'S BULKHEAD FS 280 LBL9. 2 L 7 2 4F RT A21EA 2008020600132 20080206 00132 NM 2008 2 6 UPS08M51548 1 20080114 A 5330 AGA74187383501 SKIN DOUG MD11 MD11 3023602 NM BS 1925 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 FUSELAGE SKIN REPAIR AT BS 1925 BETWEEN L45R AND L48L. INSTALLED TRIPLER REPAIR PER EO MD11-5330-28480 AND EA011-5330- 01-A1261. 2 L 7 3 4F RT A22WE 2008020600161 20080206 00161 NM 2008 2 6 2008UALA00324 1 20080119 A 5313 STRINGER SPLICE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 360 S4L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 LEFT UPPER FUSELAGE STA 360.5 STRINGER SPLICE CRACKED AT STR 4L. REPLACED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600171 20080206 00171 WP 2008 2 6 UPS08851502 1 20080102 A 5321 FLOORBOARD DOUG DC8 DC871F 302199D WP FS 1560 RBL 50 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 MAIN CABIN FLOORBOARD HEAVILY CORRODED STA 1560 RBL 50 REMOVED FLOORBOARD AT STA 1560 RBL 50. FA BRICATED AND INSTALLED REPAIR FLOORBOARD AT STA 1560 RBL 50 REF EO DC8-5320-9691C. 2 L 7 4 4F RT 4A25 2008020600192 20080206 00192 NM 2008 2 6 UPS08B51480 1 20080120 A 3350 LAMP BOEING 747 74744AF 13848B2 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 571UP 35668 L1 CEILING EMERGENCY LIGHT INOP. RELAMPED, OPS CHECKS GOOD. 2 L 7 4 4F RT A20WE 2008020600195 20080206 00195 NM 2008 2 6 2008UALA00344 1 20080120 A 2612 FIRE DETECTOR BOEING 777 777222 1385219 NM FIRE WARNING FALSE INDICATION A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 798UA 26928 PER FLIGHT ATTENDANT PANEL AT DOOR 1 LEFT FLASHED RED WITH FIRE DETECTED AND AT DOOR 3 RIGHT GOT A RED FIRE INDICATION. RESET PAX SERVICE ENTERTAINMENT UNIT (PSEU) AND ACCOMPLISHED PSEU ADJUSTMENT. TESTED & CHECKED FIRE DETECTION SYSTEM PER MM'S 26- 10-01, 26-14-12, & 32-08-00-501. SUSPECT FALSE ANNUNCIATOR INDICATION. NO FAULTS FOUND. 2 L 7 2 4F RT T0001SE 2008020600215 20080206 00215 NM 2008 2 6 ASAA0852489 1 20080117 A 4920 GTCP1319B APU BOEING 737 737890 1384527 NM STOPPED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 579AS 35187 APU STOPPED DURING DE-ICE ON GROUND. COULD NOT DUPLICATE. APU STARTED OK. CHECKED FOR GLYCOL IN INLET, NONE FOUND. 2 L 7 2 4F RT A16WE 2008020600243 20080206 00243 NM 2008 2 6 USAA920080205 1 20080112 A 5320 69489854 FITTING BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED L1 DOOR CUTOUT INTERCOSTAL CLIP, BS 360, S10L. REPLACED L1 DOOR CUTOUT INTERC OSTAL CLIP, BS 360, S10L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020600262 20080206 00262 EU 2008 2 6 USAA920080232 1 20080116 A 5347 F533114022001 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 270AY 315 BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON SEAT TRACK, BS 3727 / FR 50, -Y450. REPLACED SEAT TRACK, BS 3727 / FR 50, -Y450 IAW A330 SRM 53-31-15. 2 L 7 2 4F RT A46NM 2008020600263 20080206 00263 EU 2008 2 6 USAA920080233 1 20080116 A 5347 F5331295220000 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 270AY 315 BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON SEAT TRACK, BS 3674 / FR 49, -Y1959. REPLACED SEAT TRACK, BS 3674 / FR 49, -Y1959 IAW A330 SRM 53-31-15. 2 L 7 2 4F RT A46NM 2008020600280 20080206 00280 EA 2008 2 6 HNAA0800034 1 20080118 A 3320 BA080091 BALLAST DHAV DHC8 DHC8311 1386006 EA CABIN DEFECTIVE A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 328EN 28382 28382 281 SMELL COMING FROM SEAT 2AC OVERHEAD. DEACTIVATED SIDEWALL LIGHTING SYSTEM. REPLACED BALLAST, BULB AND LAMP HOLDER. 2 H 7 2 4T RT A13NM 2008020600281 20080206 00281 NM 2008 2 6 NOCA00508 1 20080121 A 3350 59192 POWER STRIP BOEING 767 767304 NM CABIN DEFECTIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 769NA 28039 E-PATH LIGHTS INOP ON LT SIDE FROM ROW 25-28. INSTALLED NEW CROSSOVER POWER STRIP PER MM 33-51-10, OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2008020600295 20080206 00295 NM 2008 2 6 2008UALA00303 1 20080117 A 2824 3004200000501 CONTROL UNIT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUEL SYSTEM FAILED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 823UA 952 FLIGHT DIVERTED UNDER AMBER ALERT DUE TO A FUEL IMBALANCE. FLSCU FAILURE. REPLACED NR 1 FLSCU, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600305 20080206 00305 NM 2008 2 6 2008UALA00371 1 20080123 A 2421 GENERATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE TRIPPED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 651UA 25389 RTFL DUE TO RIGHT GENERATOR TRIPPING AT 5,000 FT, FIELD OFF LIGHT ILLUMINATED. R GEN OFF EICAS DISPLAYED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020600312 20080206 00312 NM 2008 2 6 2008UALA00379 1 20080122 A 5321 FLOORBOARD BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 CABIN FLOORBOARD CF17S IS DAMAGED. REPLACED FLOORBOARD. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600322 20080206 00322 NM 2008 2 6 2008UALA00396 1 20080123 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 AFT PIT FRAME HAS 2 EACH DENTS ON INBOARD FLANGE BETWEEN STR 25L AND 26L AT STA 1400. ACCOMPLISHED MAJOR REPAIR AT GSO . 2 L 7 2 4F 4 F RT A2NM E17NE 2008020600334 20080206 00334 SO 2008 2 6 C2XA08IA031 1 20080123 A 2520 7281000501 CONTROL UNIT EMB 145 EMB145 3260210 SO CABIN SHORTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 27962 145110 IAH - FLIGHT 2380, DURING PREFLIGHT INSPECTION THE CREW REPORTED SMOKE AND A BURNING SMELL FROM THE PASSENGER SERVICE UN IT ABOVE SEAT 1A. MAINTENANCE REMOVED AND REPLACED THE CONTROL MODULE, INOPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008020600335 20080206 00335 SO 2008 2 6 C2XA08SH011 1 20080125 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18556 145595 SHV - DURING C-CHECK LEFT OMEGA BEAM HAS CORROSION ON FR 20. MX REPAIRED LEFT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 51-40 -02. THE AIRCRAFT WAS APRROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008020600344 20080206 00344 NM 2008 2 6 HNAA0800037 1 20080120 A 3350 1013079 MODULE DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 814EX 39307 131 318 SECOND RED EMERGENCY LIGHT FROM LAST IS INOPERATIVE. REPLACED SECOND RED EMERGENCY LIGHT FROM LAST MODULE AND SECURED, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2008020700012 20080207 00012 NM 2008 2 7 ZZDA2008051 1 20080107 A 5320 STIFFENER BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 A/C STRUCK BY BAG CART. STIFFENER AT 1178 FRAME AND LONGERON 22R DAMAGED. INSTALLED 2 EA NEW STIFFENER AT STA 1178 LON G 22R IAW B717 SRM 51-41-02. 2 L 7 2 4F TR A6WE 2008020700028 20080207 00028 NM 2008 2 7 HNAA0800043 1 20080119 A 3233 82970018013 DOOR ACTUATOR DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 838EX 16605 3138 220 AFTER TAKEOFF, THE LEFT MAIN GEAR DOOR CAUTION LIGHT ILLUMINATED AND THE GEAR DOOR WAS CONFIRMED TO BE IN THE OPEN POSIT ION. WHEN THE GEAR WAS CYCLED DOWN, ALL INDICATIONS WERE GREEN. THE CREW THEN CYCLED THE LANDING GEAR UP AND GOT THE S AME CAUTION INDICATION. THE CREW THEN ELECTED TO RETURN TO THE FIELD, BUT DID NOT DECLARE AN EMERGENCY. EMERGENCY EQUI PMENT WAS DISPATCHED BY THE TOWER AND FOLLOWED THE AIRCRAFT AFTER A NORMAL LANDING. MAINTENANCE CHANGED THE FORWARD GEA R DOOR ACTUATOR AND CHECKED RIGGING OF THE ACTUATOR AND DOOR SENSOR. OPS CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008020700062 20080207 00062 NM 2008 2 7 2008UALA00445 1 20080125 A 2913 PUMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 ENGINE FAILED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 309UA 23670 RTFL DUE TO NR 1 ENGINE HYDRAULIC PUMP FAILURE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700070 20080207 00070 NM 2008 2 7 2008UALA00476 1 20080126 A 5210 141N62031 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR ASSIST LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 575UA 26689 THE 1L DOOR ASSIST BOTTLE NOT IN GREEN BAND. REPLACED DOOR ASSIST BOTTLE 1L DUE TO CHRONIC LEAKING. 2 L 7 2 4F 4 F RT A2NM E17NE 2008020700071 20080207 00071 NM 2008 2 7 2008UALA00477 1 20080128 A 5230 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FWD CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 906UA 25006 FWD CARGO DOOR DAMAGED BY BELT LOADER. MAJOR REPAIR: REMOVED DAMAGED SKIN. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700105 20080207 00105 2008 2 7 COMA0860095 4 20080121 A 3160 DISPLAY CNDAIR CL600 CL6002B19 1900309 EA COCKPIT DIRTY A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 436CA 7482 FLIGHT 5485 - DISPLAY COOL CAUTION MESSAGE AT FL320. FOLLOWED QRH, MESSAGE PERSISTED. MESSAGE WENT AWAY AT 10K FT. A/ C DIVERTED TO AVL AND LANDED SAFELY. INSPECTED FOR LEAKS AT THE DISPLAY PLENUM NO LEAKS FOUND. REMOVED AND CLEANED F/O 'S NR 2 PFD FOR DUST BLOCKAGE. NO FAULTS FOUND ON GROUND. 2 L 7 2 4F RT A21EA 2008020700107 20080207 00107 NM 2008 2 7 ZZDA2008059 1 20080127 A 5310 DOOR FRAME BOEING 717 717200 1383700 NM RT MLG CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 604AT 55128 RIGHT MLG. WHEEL WELL CUTOUT FRAME CRACKED AT EDGE, 3 INCHES BELOW W/W DOOR SENSOR. INSTALLED FORMED CHANNEL REPAIR ON RIGHT HAND WHEEL WELL FRAME CUTOUT PER B717 SRM 51-70-11 FIG 201. 2 L 7 2 4F TR A6WE 2008020700110 20080207 00110 EA 2008 2 7 TRAX200800133 1 20080125 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 740EV 10151 RIGHT OVERWING EMERGENCY EXIT FORWARD LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS. 2 L 7 2 4F RT A21EA 2008020700112 20080207 00112 EA 2008 2 7 COMA0870005 1 20080123 A 3242 5013642 BRAKE CNDAIR CL600 CL6002C10 1390015 EA RT MLG LOCKED A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 374CA 5844 10090 FLIGHT 5007- RIGHT INBOARD TIRE BLEW DURING TAKEOFF ROLL. FOUND RIGHT INBOARD BRAKE LOCKED UP. REPLACED SAME BRAKE ASS EMBLY AND BOTH RIGHT MAIN TIRES. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008020700113 20080207 00113 EA 2008 2 7 COMA0860097 1 20080123 A 5315 601R350313 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 810CA 19882 19882 7370 CARGO FLOORBEAM CAP BETWEEN FS 569.0 AND FS 621 AND LBL 27 HAS CORROSION AROUND SEVERAL NUT PLATE HOLES. REMOVED DAMAGE D CARGO BEAM CAP AND INSTALLED SERVICEABLE CAP IAW COMAIR EA10-5360-02051. 2 L 7 2 4F RT A21EA 2008020700116 20080207 00116 EA 2008 2 7 COMA0860100 1 20080126 A 2752 852D10021 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA RT T/E FLAP FAULTY A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 940CA 465 7048 FLIGHT 5220 - RECEIVED FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. PERFORMED SI-2-2 7I0002, AND REPLACED RIGHT INBOARD FLAP ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008020700124 20080207 00124 SO 2008 2 7 C2XA08IA044 1 20080129 A 5730 14537011006 SKIN EMB 145 EMB145LR 3260212 SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14953 145071 IAH - DURING PREFLIGHT INSPECTION THE RIGHT WING SKIN WAS FOUND TO BE CRACKED AT THE CENTER HINGE POINT CUTOUT FOR THE G ROUND SPOILER. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE CRACK ON A 500FC DMI, WITH RE-INSPECTIONS TO BE MADE A T EVER 50FC, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 03/24/08 THE DAMAGED SECTRION OF SKIN WAS REMOVED , AND TRIPLERS INSTALLED AS A FINAL REPAIR, AND THE AIRCRAFT WAS APPROCVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008020700125 20080207 00125 GL 2008 2 7 C2XA08CL014 2 20080129 A 7321 00502710002 MODULE EMB 135 EMB135ER 3260203 SO ALLSN AE300 AE3007A GL FADEC DEFECTIVE A C2XA B A EMER. DESCENT UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 27 15509 145238 DAY FLIGHT 2382 - THE CREW REPORTED 10 MINUTES INFLIGHT IN CLIMB MODE THE NR 2 ENGINE POWERED BACK TO FLIGHT IDLE UNCOMM ANDED. THE AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE FA DEC 2A RESISTOR MODULE A0100 AND CONNECTOR J0584. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008020700126 20080207 00126 EA 2008 2 7 TRAX200800135 1 20080125 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 843AS 7310 AAR-2150 - FLOOR EMERGENCY FLOOR LIGHT ON WARDROBE IS BROKEN. 2 L 7 2 4F RT A21EA 2008020700130 20080207 00130 NM 2008 2 7 SWAA080504 1 20080129 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 25R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020700132 20080207 00132 NM 2008 2 7 SWAA080524 1 20080129 A 5310 6517685 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR FRAME CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008020700137 20080207 00137 NM 2008 2 7 SWAA080517 1 20080129 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020700145 20080207 00145 NM 2008 2 7 PIDA08007 1 20080130 A 3350 AD20131A BATTERY PACK BOEING 737 737228 13844AG NM CABIN DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 251TR 23792 EMERGENCY LIGHTS INOP AT RIGHT OVERWING AND NR 9 OVERHEAD BIN. REPLACED BATTERY PACK AT RIGHT OVERHEAD MID-CABIN. EMER GENCY LIGHTS OPS GOOD PER MM 33-51-31. 2 L 7 2 4F RT A16WE 2008020700149 20080207 00149 SO 2008 2 7 C2XA08TY018 1 20080130 A 3350 1317 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 21130 145704 LEFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED LEFT OVERWING LIGHT IAW EMB 145XR AMM 33-50-07 OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT 2008020700150 20080207 00150 SO 2008 2 7 C2XA08TY019 1 20080130 A 3350 744412 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16987 145261 EMERGENCY EXIT MARKER AT 3B INOP. REMOVED AND REPLACED EMERGENCY EXIT MARKER IAW EMB 145LR 33-50-14. OPS CHECK GOOD, A IRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008020700152 20080207 00152 SO 2008 2 7 C2XA08TY022 1 20080130 A 3350 1317 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14174 14500876 RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB IAW EMB 145 AMM 33-50-07, OPS CHECK GOOD. AIRCRAFT RELE ASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT 2008020700153 20080207 00153 SO 2008 2 7 C2XA08TY023 1 20080130 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13955 145075 SERVICE DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB IAW EMB 145 AMM 33-50-10. OPS CHECK GOOD. AIRCRAFT RELEA SED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008020700154 20080207 00154 NM 2008 2 7 HNAAA0800048 1 20080123 A 3350 AML91LA85 CIRCUIT BREAKER DHAV DHC8 DHC8102 2809003 NM CABIN FAULTY A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 914HA 53 GREEN LIGHT NOT ILLUMINATING ON EMERGENCY LIGHT SWITCH AT F/A'S PANEL. REPLACED SWITCH (P/N AML21GBA2CD), NO FIX, REPLA CED C/B, OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2008020700161 20080207 00161 NM 2008 2 7 WRLA2008014 1 20080123 A 2530 72067000 OVEN DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE GALLEY DEFECTIVE A WRLA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 277WA 48743 OKBK/EDDP. OVEN 509 MID GALLEY INOP BURNING SMELL WHEN USED. REMOVED AND REPLACED MID GALLEY OVEN 509 REF MM 25-33-00. DMI CLOSED. 2 L 7 3 4F 4 F RT A22WE E24NE 2008020700166 20080207 00166 NM 2008 2 7 SWAA080529 1 20080130 A 5311 6545805 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 278, STR 21R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008020700170 20080207 00170 NM 2008 2 7 SWAA080546 1 20080130 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2008020700173 20080207 00173 NM 2008 2 7 SWAA080548 1 20080130 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, LBL 2. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008020700174 20080207 00174 NM 2008 2 7 SWAA080550 1 20080130 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, STR 17R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008020700178 20080207 00178 SO 2008 2 7 C2XA08CL017 1 20080127 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO RT MLG OBSTRUCTED A C2XA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 27 11536 145520 MKE FLIGHT 2560 - THE CREW REPORTED A AIR/GROUND FAIL MESSAGE ON TAKEOFF. THE AIRCRAFT RETURNED TO MKE AND LANDED WITHO UT INCIDENT. MAINTENANCE INSPECTED AND CLEANED DEBRIS FROM RIGHT MAIN LANDING GEAR PROXIMITY SWITCH. OPERATIONAL CHECK S WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008020700185 20080207 00185 EU 2008 2 7 TRAX200800145 1 20080128 A 5720 ANGLE AEROSP ATR72 ATR72 EU LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 LT FAIRING WING BOX FR 28 ANGLE CRACKED. LT FAIRING WING BOX FR 28 ANGLE INSTALLED IAW SRM 51-25-01. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IAW S.P. 663 AND FAR 43 APPENDIX A. REPAIR ACCOMPLISHED IAW SRM 51-25-01 2 H 7 2 4T RT 2008020700192 20080207 00192 2008 2 7 TRAX200800152 4 20080128 A 2210 AUTOPILOT SYS CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A ASOA K NONE J WARNING INDICATION DE DESCENT 1 SO 27 830AS 7236 STAB TRIM / MACH TRIM / AP ND CAUT MSG ON ARRIVAL INTO COLUMBIA. EMERGENCY DECLARED & EMERGENCY EQUIPMENT ON STANDBY AS A PRECAUTION. AUTOPILOT SYSTEM. 2 L 7 2 4F RT A21EA 2008020700198 20080207 00198 SO 2008 2 7 C2XA08SH020 1 20080203 A 5751 145690094095D HOUSING EMB 145 EMB145LR 3260212 SO LT AILERON DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16559 145603 SHV - DURING C-CHECK LEFT AILERON O/B MOST FITTING (FOR PCA ATTACHMENT) FLANGER BUSHING HOUSING (ON BRACKET) IS ELONGATE D. MX REMOVED AND REPLACED LEFT AILERON O/B MOST FITTING FLANGER BUSHING HOUSING IAW EC5750-01177. THE AIRCRAFT WAS AP PROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008020800003 20080208 00003 EU 2008 2 8 USAA920080271 1 20080126 A 2597 PIN AIRBUS A321 A321211 3930370 EU EVAC SLIDE MISALIGNED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 182UW 1536 FLT 9172 - PIT-CLT - EMERGENCY LIGHTING - AFT EMERGENCY POWER SUPPLY UNIT SHOWS EXTERIOR LIGHTS FAULT. CIDS TEST SHOWS EPSU EXTERNAL LOAD LEFT AFT. MAINTENANCE ACCOMPLISHED TSM TASK 33-51-00. REALIGNED PIN IN RIGHT AFT ESCAPE SLIDE CONNE CTOR. OPERATIONAL CHECK WAS GOOD PER AIRBUS MAINTENANCE MANUAL 33-51-00-710-006. LEFT AND RIGHT AFT SLIDES ARE RESTORE D TO OPERATING CONDITION. 2 L 7 2 4F RT A28NM 2008020600260 20080206 00260 NM 2008 2 6 USAA920080229 1 20080108 A 5753 6546435340 FLAP BOEING 737 7373Y0 1384671 NM RT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C-18 CHECK - RIGHT WING OUTBOARD AFT FLAP HAS DELAMINATION, WBL 230 - WBL 232. REPAIRED RIGHT WING OUTBOARD AFT FLAP, WBL 230 - WBL 232 IAW B737 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2008020600293 20080206 00293 NM 2008 2 6 2008UALA00285 1 20080115 A 3397 CONNECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 824UA 965 EEL LIGHT AT 7C INOP. LOOSE CONNECTOR AT SEAT ROW 7. RESECURED LOOSE CONNECTOR, LIGHTS OPS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008020600310 20080206 00310 NM 2008 2 6 2008UALA00377 1 20080122 A 5712 RIB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 NR 1 MAIN FUEL TANK LOWER RIB WBL 135, ANGLE FWD UPPER RADIUS OF CUTOUT CRACKED. INSTALLED REPAIR TEE DOUBLER REPAIR A ND DRILL START FREEZE PLUG REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020600317 20080206 00317 NM 2008 2 6 2008UALA00391 1 20080123 A 2120 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN SMOKE A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 663UA 27160 CREW REPORTED SMOKE IN CABIN AND RETURN TO FIELD. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020600356 20080206 00356 EA 2008 2 6 COMA0860061 1 20080111 A 3244 0274380 TIRE CNDAIR CL600 CL6002B19 1900309 EA LT MLG BLOWN A COMA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 01 989CA 352 7215 FLIGHT 5030 - VIBRATION JUST BEFORE ROTATION SPEED. WOW INPUT CAUTION, AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. BOTH LEFT MLG TIRES BLOWN. REMOVED AND REPLACED LEFT MLG O/B WHEEL ASSY. 2 L 7 2 4F RT A21EA 2008020700005 20080207 00005 NM 2008 2 7 ZZDA2008041 1 20080107 A 5320 WEB BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 A/C STRUCK BY BAG CART. WEB AT FRAME AT STA 1161 DAMAGED BETWEEN BL 0 AND L24R. INSTALLED NEW WEB AT FRAME STA 1161 BE TWEEN BL 0 AND LONGERON 24R IAW B717 SRM 51-41-02 AND SRM 51-41-05. MATERIAL USED 7075 T6 .032. 2 L 7 2 4F TR A6WE 2008020700015 20080207 00015 NM 2008 2 7 WRLA2008015 1 20080124 A 5414 AUB75628 FAIRING DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 1 ENGINE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 279WA 48756 DURING C-CHECK INSPECTION, FOUND 2 INCH CRACK IN NR 1 ENGINE LOWER RIGHT AFT SECTION FAIRING. REPAIRED PER ENGINEERING INSTRUCTION NR W2008A57B-059 REV.00. REF EGAT NRC U05004. 2 L 7 3 4F 4 F RT A22WE E24NE 2008020700018 20080207 00018 NM 2008 2 7 ZZDA2008058 1 20080122 A 5311 FRAME BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 959AT 55021 SMALL CRACK NOTICED AT AFT INTERIOR FUSELAGE TAIL COMP. LEFT SIDE CANTED AREA STA 1178.225 BETWEEN LONG 13 AND 14 LEFT. INSTALLED FORMED ANGLE REPAIR ON LEFT FUSELAGE CANTED FRAME 1178 BETWEEN LONG 13 AND 14 LEFT PER B717 SRM 51-70-11 FIG 201. 2 L 7 2 4F TR A6WE 2008020700036 20080207 00036 EA 2008 2 7 COMA0860067 1 20080114 A 3231 601R3118515 BELLCRANK CNDAIR CL600 CL6002B19 1900309 EA LT MLG BENT A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 989CA 7215 FLIGHT 5535 - LEFT MAIN GEAR DISAGREE AFTER GEAR SELECTED UP. FOLLOWED QRH, THREE GREEN AFTER MANUAL GEAR EXTENSION. E MERGENCY DECLARED AND AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED LEFT MLG DOOR BELL CRANK. 2 L 7 2 4F RT A21EA 2008020700045 20080207 00045 NM 2008 2 7 2008UALA00418 1 20080124 A 5340 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU BS 294 S11L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 INTERCOSTAL ATTACH ANGLE IS CRACKED AT BS 294.5 AT STRINGER 11L. MAJOR REPAIR: REPLACED ATTACH ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700068 20080207 00068 NM 2008 2 7 2008UALA00464 1 20080128 A 2760 CONTROL CABLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU RT SPOILER SYS MISROUTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 905UA 25005 RIGHT WW SPOILER CABLES MISSED ROUTED FWD BLKH INSIDE PULLEY BRACKET. FOUND THAT THE SPOILER CABLES WERE MISROUTED. REP LACED WSB2-1 AND WSB1-2 CABLES. 2 L 7 2 4F 4 F RT A16WE E21EU 2008020700104 20080207 00104 EA 2008 2 7 COMA0860094 1 20080121 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 814CA 7387 FLIGHT 5154 - UPON SELECTION OF FLAPS TO 8 DEGREES, RECEIVED FLAPS FAIL CAUTION MESSAGE. EMERGENCY DECLARED, AIRCRAFT L ANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW UP MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 2008020700111 20080207 00111 SO 2008 2 7 C2XA08ON076 1 20080126 A 3350 1317 LIGHT EMB 145 EMB145XR 3260214 SO COCKPIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12167 10066 10066 14500834 FLT MX - ONT TO ONT - WHILE PERFORMING 2A CHECK PRELIMINATORY INSPECTION, INSPECTOR FOUND COCKPIT CEILING EMERGENCY LIGH T DOES NOT ILLUMINATE. MX PERSONNEL REMOVED AND REPLACED LIGHT BULB OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS R ELEASED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008020700143 20080207 00143 NM 2008 2 7 SWAA080522 1 20080129 A 5310 6546818 CREASE BEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM CHORD CORRODED BEWTEEN BS 950 AND BS 986.5, STR 17R. REMOVED AND REPLACE D CEASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2008020700176 20080207 00176 NM 2008 2 7 SWAA080547 1 20080130 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, RBL 2. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008020800006 20080208 00006 WP 2008 2 8 DHL2007873542 1 20080113 A 5740 FITTING DOUG DC8 DC873F 302199F WP NR 3 FUEL CELL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 NR 3 MAIN TANK INTERNAL FITTING CRACKED 2 INCHES AT STA XRS 74.000 S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D. CLEANED AND APPLIED POLYURETHANE TOP YELLOW CO ATING TO AREA IAW SRM 51-1-12 PG 7. INSTALLED NEW FITTING IAW SRM 51-1-12, SRM 51-3-0, SRM 51-1-23 (PLI WASHER) SRM 51- 1-20D, SRM 51-3-1 (TORQUE). REFER TO NR 107761 FOR LEAK CHECK. 2 L 7 4 4F RT 4A25 2008020800007 20080208 00007 WP 2008 2 8 DHL2007873520 1 20080118 A 5755 56551652 SKIN DOUG DC8 DC873F 302199F WP NR 1 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 NR 1 RT SPOILER UPPER SKIN DELAMINATED. REMOVED AND REPLACED NR 1 RT SPOILER IAW MM 27-61-1 PG 201-206. REFER TO NR 10 7757 FOR OPS CHECK. 2 L 7 4 4F RT 4A25 2008020800008 20080208 00008 WP 2008 2 8 AALA200800096 1 20080118 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 961TW 53611 DFW - EMERGENCY LIGHT AT RIGHT OVERHEAD SEAT ROW 23 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT OVERHEAD S EAT ROW 23. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800010 20080208 00010 WP 2008 2 8 AALA200800081 1 20080116 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9403W 53139 LGA - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800015 20080208 00015 SO 2008 2 8 RAIA00801027 1 20080125 A 3610 CLAMP EMB 145 EMB145LR 3260212 SO BLEED AIR SYS LOOSE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 845HK 14500842 FLT 7892 ORD - NR 1 BLEED LEAK ON EICAS WHEN CLIMBING THROUGH 10KFT IN ICING CONDITIONS. MAINTENANCE FOUND A LOOSE DUCT CLAMP IN THE LEFT PYLON. PERFORMED AN OPERATIONAL CHECK OF THE BLEED SYSTEM WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008020800017 20080208 00017 NM 2008 2 8 DLM88080133 1 20080129 A 5330 59364335 DOUBLER DOUG MD88 MD88 3023688 NM BS 1154 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 CORROSION AT FS 1154 BETWEEN L-29R AND L30R TO THE INTERNAL DOUBLER RESULTED IN A 2" BY .5" CUTOUT. THE OVERLYING SKIN WAS UNAFFECTED. MX INSTALLED A REPAIR DOUBLER WITH A STRUCTURAL SHIM EXTERNALLY PER 09-465651-14. REPAIR WAS APPROVED FOR STATIC STRENGTH WITH DTA TO FOLLOW AT A LATER DATE. 2 L 7 2 4F RT A6WE 2008020800022 20080208 00022 2008 2 8 DL76L080140 4 20080125 A 3444 341080163 IRU BOEING 767 767332 1382001 NM RT MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 192DN 28449 FMS POSITION WAS 10 MILES OFF AND COURSE NOT CORRECT. CENTER IRU DID NOT AGREE WITH LEFT AND RIGHT IRU`S. SWAPPED RIGH T IRS WITH CENTER IRS, REALIGNED ALL IRU`S. ALL INDICATIONS NORMAL NOW. RIGHT IRU INOP PER MEL 34-21-01C. 2 L 7 2 4F RT A1NM 2008020800024 20080208 00024 NM 2008 2 8 AALA200800114 1 20080120 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 355AA 24036 MIA - EXTERNAL EMERGENCY LIGHT AT LEFT AFT INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LEFT AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008020800032 20080208 00032 WP 2008 2 8 AALA200800134 1 20080122 A 3350 SHROUD DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 974TW 53624 DFW - EMERGENCY LIGHT AT SEAT 10D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800036 20080208 00036 NM 2008 2 8 BB08006 1 20080125 A 2722 8281081 GASKET BOEING 757 75723N 1384973 NM RUDDER ACTUATOR LEAKING A USAA K NONE K FLUID LOSS DE DESCENT 1 EA 19 204UW 30886 CUN FLT 803 PHL-CUN DURING LANDING GEAR EXTENSION, LEFT HYD SYSTEM QTY DROPPED TO .48 RF. MAINTENANCE FOUND RUDDER RAT IO ACTUATOR SOLENOID GASKET LEAKING. REPLACED GASKET. 2 L 7 2 4F RT A2NM 2008020800037 20080208 00037 2008 2 8 BB08007 4 20080127 A 2565 D30654122 LANYARD BOEING 757 7572B7 1384964 NM EVAC SLIDE FRAYED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 942UW 38649 1700 27807 LAS R4 DOOR ESCAPE SLIDE LANYARD HANGING AND FRAYED. MAINTENANCE REPLACED SLIDE, ALSO RIGGED DOOR SLIDE ARMED INDICATIO N. 2 L 7 2 4F RT A2NM 2008020800040 20080208 00040 NM 2008 2 8 ASAA082501 1 20080125 A 2161 3989083 MODULATING VALVE BOEING 737 737890 1384527 NM TEMP CONTROL MALFUNCTIONED A ASAA K NONE O OTHER CR CRUISE 1 NM 02 1935 1935 35681 AFT CABIN TEMPERATURE CONTROLLER WOULD NOT HOLD SET TEMPERATURE. REPLACED TRIM MOD VALVE. 2 L 7 2 4F RT A16WE 2008020800041 20080208 00041 WP 2008 2 8 DHL2007873543 1 20080115 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 680 DAMAGED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 89073 46091 MAIN CARGO COMPT FLOORBEAM MISDRILLED HOLE AT STA 680.000 LBL 15.187 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FOR M 8110-3 DATED 01-15-08, DWG AE85-53-101 REV IR DATED 12-28-07,EVA D85300030 REV IR DATED 01-02-08. CUT OUT DAMAGED SEC TION AND FABRICATED (2EA) REPAIR ANGLES AND FILLER IAW DWG AE85-53-101. HEAT TREATED REPAIR ANGLES IAW SRM 51-1-1 PG 1- 13-17. NDT INSPECTED REPAIR PARTS IAW DPS 4.707.1, NDT SPM PART 08. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG AE85-53-101, SRM 51-1-11, SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2008020800044 20080208 00044 NM 2008 2 8 ASAA082499 1 20080125 A 2421 761574B IDG BOEING 737 737890 1384527 NM LT ENGINE MALFUNCTIONED A ASAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 NM 02 5187 5187 35178 EN ROUTE SEA-HNL LEFTHAND IDG DRIVE ANNUNCIATED. ATB TO SEA. REPLACED IDG AND IDG OIL COOLER. 2 L 7 2 4F RT A16WE 2008020800045 20080208 00045 NM 2008 2 8 ASAA082502 1 20080125 A 4990 38762983 SENSOR BOEING 737 737890 1384527 NM APU DEFECTIVE A ASAA K NONE N FALSE WARNING AP APPROACH 1 NM 02 1479 1479 35683 APU MAINTENANCE ANNUNCIATION. REPLACED DEFECTIVE OIL LEVEL SENSOR. 2 L 7 2 4F RT A16WE 2008020800054 20080208 00054 NM 2008 2 8 ASAA0842503 1 20080126 A 5753 6570947296 DOOR BOEING 737 7374Q8 138447Q NM T/E FLAP BROKEN A ASAA K NONE F FLT CONT AFFECTED AP APPROACH 1 NM 02 764AS 25101 COULD NOT LOWER T/E FLAPS BEYOND 10 DEGS ON APPROACH INTO KTN. REMOVED DAMAGED RIGHTHAND INBOARD FLAP MID FLAP TORQUE D OOR WHICH WAS IMPEDING FLAP TRANSLATION. DOOR REPLACEMENT DEFERRED PER CDL. 2 L 7 2 4F RT A16WE 2008020800055 20080208 00055 NM 2008 2 8 ASAA082500 1 20080125 A 7910 M832481226 O-RING BOEING 737 737890 1384527 NM LT ENG OIL CAP SWOLLEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 35178 LEFTHAND ENGINE OIL TANK CAP O-RING SWELLED. REPLACED O-RING. 2 L 7 2 4F RT A16WE 2008020800056 20080208 00056 SW 2008 2 8 WGEA200800017 1 20080204 A 3244 M16901 TIRE ECLIPS EA500 ECLIPSEEA500 3350000 SW LT MLG FLAT E WGEA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 EA 27 146DJ 40 000058 DURING ROLLOUT, LEFT MAIN TIRE WENT FLAT. SUPPLEMENTAL INFORMATION, REMOVED AND REPLACED LEFT MAIN WHEEL ASSY, INSPECTE D FLAPS, ENGINE AND UNDERWING. NO DAMAGE FOUND IAW EA 500 M/M 32-42-00. 1 L 7 2 4J RT A00002AC 2008020800058 20080208 00058 NM 2008 2 8 USAA920080240 1 20080112 A 5310 DOOR FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FORWARD SERVICE DOOR CUTOUT STUB FRAME, BS 274.5, RBL 55. REPAIRED FORWARD SER VICE DOOR CUTOUT STUB FRAME, BS 274.5, RBL 55 IAW B737 SRM 51-70-11. 2 L 7 2 4F RT A16WE 2008020800059 20080208 00059 NM 2008 2 8 USAA920080241 1 20080117 A 5320 69355501 TIE CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED TIE CLIP, BS 747, RBL 15. REPLACED TIE CLIP, BS 747, RBL 15 IAW B737 SRM 51-10 -02. 2 L 7 2 4F RT A16WE 2008020800067 20080208 00067 NM 2008 2 8 USAA920080258 1 20080116 A 5320 6545834610 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q5 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 336, RBL 58 - RBL 60. REPLACED CABIN FLOOR SUPPORT, BS 336, RBL 58 - RBL 60 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008020800068 20080208 00068 NM 2008 2 8 USAA920080259 1 20080115 A 5210 DOOR FRAME BOEING 737 7374B7 1384702 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q5 CHECK - FORWARD SERVICE DOOR FRAME CRACKED AT THE 4TH STOP FITTING FROM THE TOP. REPAIRED THE F ORWARD SERVICE DOOR FRAME AT THE 4TH STOP FITTING FROM THE TOP IAW USAIRWAYS TYPICAL REPAIR 52-10-11. 2 L 7 2 4F RT A16WE 2008021200276 20080212 00276 NM 2008 2 12 2008UALA00527 1 20080130 A 5330 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU BS 947 S26-24L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 905UA 25005 SKIN CRACKED STA 947.5 BETWEEN STR 23L & STR 24L. REMOVED DAMAGE. FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200278 20080212 00278 NM 2008 2 12 2008UALA00530 1 20080130 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 947-996 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FUSELAGE STR 17R CREASE BEAM UPPER SURFACE CORRODED, BS 947-996. MAJOR REPAIR: REMOVED CORROSION DAMAGE. REPLACED AFT GALLEY DOOR CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200282 20080212 00282 NM 2008 2 12 2008UALA00535 1 20080130 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 956-993 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FUSELAGE STR 17L CREASE BEAM CORRODED ON THE UPPER SURFACE AND VERTICAL TRANSITION, BS 956-993. MAJOR REPAIR: REPLACED CREASE BEAM AT DOOR 2L. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200289 20080212 00289 NM 2008 2 12 2008UALA00544 1 20080130 A 5320 141T510410 ATTACH ANGLE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 664UA 29236 FWD E&E COMPT AT STA 246 AT RBL 11 ATTACH ANGLE IS CRACKED. REMOVED AND INSTALLED NEW ANGLE IAW SRM 51-40-02 AND DWG141 T5146. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021200292 20080212 00292 NM 2008 2 12 2008UALA00552 1 20080131 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EEL INOP SEAT 1J AFT SECTION. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021300005 20080213 00005 NM 2008 2 13 KCSA081056 1 20080201 A 5330 SKIN BOEING 747 747209B 138489B NM BS 346 S42-43R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FOUND SKIN DAMAGED AT STA-346 BETWEEN STR-42R AND STR-43R. 2 L 7 4 4F RT A20WE 2008021300006 20080213 00006 NM 2008 2 13 KCSA081057 1 20080201 A 5330 SKIN BOEING 747 747209B 138489B NM BS 354 S42-43R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FOUND STA-354 SKIN DAMAGED BETWEEN STR-42R AND STR-43R. 2 L 7 4 4F RT A20WE 2008021300007 20080213 00007 NM 2008 2 13 KCSA081058 1 20080201 A 5330 SKIN BOEING 747 747209B 138489B NM BS 362 S43-44R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FOUND STA-362 SKIN DAMAGED BETWEEN STR-43R AND STR-44R. 2 L 7 4 4F RT A20WE 2008021300008 20080213 00008 NM 2008 2 13 KCSA081059 1 20080201 A 5330 SKIN BOEING 747 747209B 138489B NM BS 364 S43-44R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FOUND STA 364 SKIN DAMAGED BETWEEN STR-43R AND STR-44R. 2 L 7 4 4F RT A20WE 2008021300017 20080213 00017 NM 2008 2 13 KCSA081065 1 20080202 A 5413 STRINGER BOEING 747 747209B 138489B NM NR 4 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 NR 4 PYLON INBOARD STRINGER IS CRACKED AT NAC STA 295 TO 300, BELOW MIDSPAR AREA. 2 L 7 4 4F RT A20WE 2008021300027 20080213 00027 WP 2008 2 13 ABXR080034 1 20080121 A 5730 591214426 SKIN DOUG DC9 DC915F 3022037 WP RT WING TE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 166DE 47152 RIGHT WING LOWER TRAILING EDGE SKIN AFT OF INBOARD BUTE DOOR WAS CRACKED. REPAIRED SKIN IAW DC9 SRM 57-01, FIGURE 3. 2 L 7 2 4F A6WE 2008021300029 20080213 00029 WP 2008 2 13 ABXA080035 1 20080202 A 5610 PIN DOUG DC9 DC941 302207N WP COCKPIT WINDOW DISLODGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT OPEN. FOUND UPPER GUIDE PIN OUT OF CAM SLOT. RE-ALIGNED CAM PIN WITH CAM SL OT. CLEARVIEW WINDOW TEST GOOD IAW DC9 AMM 56-10-03-5. 2 L 7 2 4F A6WE 2008021300030 20080213 00030 WP 2008 2 13 UPS08851623 1 20080111 A 5542 SKIN DOUG DC8 DC871F 302199D WP RUDDER DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 CREASED DENT ON LT UPPER SKIN OF RUDDER. RUDDER REPLACED ON N/R 123801. 2 L 7 4 4F RT 4A25 2008021300043 20080213 00043 NM 2008 2 13 ABXA080043 1 20080108 A 5753 STRUCTURE BOEING 767 767281 1385109 NM RT WING TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 787AX 23020 RIGHT WING OUTBOARD FLAP HAD CORROSION UNDERNEATH THE OUTBOARD SUPPORT BEAM. REMOVED AND REPLACED RIGHT OUTBOARD FLAP I AW B767 MM 27-51-20-4-10. 2 L 7 2 4F RT A1NM 2008021300044 20080213 00044 EU 2008 2 13 USAASA08004 1 20080202 A 2730 ROD END AIRBUS A319 A319112 3930323 EU ELEVATOR WORN A USAA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 19 767UW 1382 CLT FLT 1845 EN ROUTE PHL TO FPO - AIRFRAME VIBRATION WAS FELT AT FL 320 AND HIGHER SPEEDS. A DECISION WAS MADE TO DI VERT TO CLT. VIBRATION STOPPED BELOW 18,000 FEET AND SLOWER SPEEDS. FLIGHT LANDED IN CLT WITHOUT FURTHER INCIDENT. MA INTENANCE REPLACED 3 ELEVATOR SERVO ROD ENDS. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2008021300049 20080213 00049 EU 2008 2 13 USAA920080310 1 20080127 A 5320 D53112818200 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AW 543 SAL - MAJOR REPAIR - C8 CHECK - NR 6039301, CORROSION ON FLOOR SUPPORT, BS 709/FR 16 - BS 760/FR 18, +Y254. REPLACED FL OOR SUPPORT BS 709/FR 16 - BS 760/FR 18, +Y254 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008021300051 20080213 00051 NM 2008 2 13 USAA920080312 1 20080128 A 5310 CREASE BEAM BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 202UW 27811 BFM- MAJOR REPAIR - C4 CHECK - CORROSION ON CREASE BEAM, BS 324 - BS 377, RBL 62. REPLACED CABIN FLOOR SUPPORT, BS 324 - BS 377, RBL 62 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008021300052 20080213 00052 NM 2008 2 13 USAA920080313 1 20080125 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 202UW 27811 BFM - MAJOR REPAIR - C4 CHECK - NR 6040673, LEVEL 2 CORROSION ON INTERCOSTAL, BS 1640 - BS 1661, BL 0. REPLACED CABIN F LOOR SUPPORT, BS 324 - BS 377, RBL 62 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008021300053 20080213 00053 NM 2008 2 13 USAA920080332 1 20080129 A 5523 65G2638427 TAB BOEING 737 7374B7 1384702 NM LT ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 CLT - MAJOR REPAIR - C2 CHECK - NR 6005782/03-0555-8-0123/1, LEFT ELEVATOR TAB TRAILING EDGE IS DELAMINATED. REPLACED L EFT ELEVATOR TAB IAW JOB CARD 03C71127007. 2 L 7 2 4F RT A16WE 2008021300054 20080213 00054 NM 2008 2 13 USAA920080333 1 20080129 A 5523 65C2638428 TAB BOEING 737 7374B7 1384702 NM RT ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 CLT - MAJOR REPAIR - C2 CHECK - NR 6005690/03-0555-8-0126/1, RIGHT ELEVATOR TAB UPPER SURFACE NEAR NR 2 HINGE AREA IS DE LAMINATED. REPLACED RIGHT ELEVATOR TAB IAW JOB CARD 03C71127004A. 2 L 7 2 4F RT A16WE 2008021300056 20080213 00056 NM 2008 2 13 USAA920080346 1 20080202 A 5512 SKIN BOEING 737 7374B7 1384702 NM HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 453UW 24980 CLT - MAJOR REPAIR - C6 CHECK - NR JK-44-2500C/1, RIGHT HORIZONTAL STABILIZER LOWER SURFACE SKIN CRACKED, STABILIZER STA TION 120 - 129. REPAIRED RIGHT HORIZONTAL STABILIZER LOWER SURFACE SKIN, STABILIZER STATION 120 - 129 IAW USAIRWAYS TYP ICAL REPAIR 55-10-07 REV C. 2 L 7 2 4F RT A16WE 2008021300057 20080213 00057 NM 2008 2 13 USAA920080347 1 20080130 A 5754 SKIN BOEING 737 7374B7 1384702 NM NR 1 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 CLT - MAJOR REPAIR - C2 CHECK - NR JK-10-5725C-C1, LEFT WING NR 1 SLAT LOWER SURFACE SKIN CRACKED. REPAIRED LEFT WING N R 1 SLAT LOWER SURFACE SKIN IAW B737 SRM 57-43-01 REPAIR 6. 2 L 7 2 4F RT A16WE 2008021300059 20080213 00059 NM 2008 2 13 USAA920080349 1 20080114 A 5754 SKIN BOEING 737 7373S3 1384711 NM NR 4 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - NR 6033405, DISBOND ON THE LEFT WING NR 4 SLAT WEDGE LOWER SURFACE, SS 91. REPAIRED LE FT WING NR 4 SLAT WEDGE LOWER SURFACE, SS 91 IAW B737 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2008021300064 20080213 00064 NM 2008 2 13 AALA200800176 1 20080126 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 346AN 33085 ORD - EMERGENCY LIGHTS AT SEAT ROWS 35 TO 41 INOPERATIVE. REPLACED CONNECTOR AT SEAT ROW 36AB FOR EMERGENCY LIGHTS AT S EAT ROWS 35 TO 41. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008021300067 20080213 00067 NM 2008 2 13 AALA200800177 1 20080126 A 2910 6937317300 MODULE BOEING 737 737823 13844BZ NM HYD SYSTEM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SW 21 952AA 30088 AUS INFLIGHT T1622/26JAN - LEFT AND RIGHT HYDRAULIC LOW PRESSURE INDICATION DURING DESCENT. LANDED AUS WITHOUT INCIDEN T. REPLACED HYDRAULIC PUMP MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008021300073 20080213 00073 NM 2008 2 13 F3LA200800042 1 20080206 A 5315 D5347219021000 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 15440 5503 2019 REFERENCE NON ROUTINE 26654, DURING C3/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE MAIN DECK FLOORBEAM AT LBL 51 AND FRAME 66. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF A3 19 SRM 51-42-11. UPON COMPLETION OF THE INSTALLATION, THE NEW FLOORBEAM WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008031300192 20080313 00192 NM 2008 3 13 SWAA081176 1 20080303 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008021200010 20080212 00010 EA 2008 2 12 A6WA200840041 1 20080116 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 CRACK FOUND ON FLOOR STRUCTURE ON FS 280, LBL 9. DAMAGE ON FLOOR STRUCTURE AT FS 280, LBL 9 REPAIRED IAW REO 601R-53-11 -171. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200014 20080212 00014 NM 2008 2 12 MWEA080022 1 20080131 A 2820 LINE DOUG MD88 MD88 3023688 NM FUEL SYSTEM DISCONNECTED A MWEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 13 822ME 49759 THE AIRCRAFT IS NOT BURNING FUEL FROM THE RIGHT MAIN AND CENTER TANK FUEL. FOUND LEFT FUEL LINE IN CENTER TANK DISCONN ECTED. RECONNECTED LINE LEAK CHECKED GOOD. 2 L 7 2 4F RT A6WE 2008021200018 20080212 00018 EA 2008 2 12 A6WA200840034 1 20080112 A 7110 NOSE COWL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT ENGINE WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 LT ENGINE UPPER NOSE COWL (432AT) AFT CORNER WORN THIN. REPLACED ON LT ENG UPPER NOSE COWL (432AT) AFT CORNER IAW CMM 7 1-14-01-300-814-A01. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200025 20080212 00025 EA 2008 2 12 A6WA200840024 1 20080114 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 CRACK EXIST ON INTERCOSTAL LBL 27 AND LBL 36, FS 484. BRACKET REPLACED ON INTERCOSTAL LBL 27 AND LBL 36, FS 484. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200051 20080212 00051 NM 2008 2 12 2008UALA00493 1 20080128 A 2612 GE1317 LAMP BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE RT FIRE HANDLE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 671UA 30026 RIGHT FIRE HANDLE NEEDS RELAMPING. FOUND FAULTY BULB. REPLACED BULB.ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021200068 20080212 00068 NM 2008 2 12 2008UALA00470 1 20080126 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 524UA 24977 EXTERIOR EMERGENCY EXIT LIGHT INOP AT DOOR 2L. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200083 20080212 00083 NM 2008 2 12 2008UALA00440 1 20080126 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 812UA 850 CABIN EMERGENCY LIGHT TEST ITEM NR 2 ON 3SVC CK SHOWS RT EMERGENCY EPSU ON DISPLAY. REPLACED POWER SUPPLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021200091 20080212 00091 NM 2008 2 12 2008UALA00406 1 20080122 A 3350 M10770 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 531UA 25042 EMERGENCY AISLE LIGHTS AT SEAT'S 15A AND 18A INOP. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200092 20080212 00092 2008 2 12 2008UALA00405 4 20080123 A 2565 D31517317 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RIGHT SHORTED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 433UA 589 THE "EXT LOAD AFT LEFT" DISPLAYED DURING EMERGENCY LIGHT TEST. ELECTRICAL SHORT IN AFT SLIDE (RT). REPLACED AFT RT SLI DE. TESTED, PERFORMED NORMALLY. NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021200107 20080212 00107 EA 2008 2 12 MASA200800050 1 20080118 A 7120 601350061 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 591ML 7388 REPAIRED ENGINE SUPPORT BEAM, UPPER WEB WAS CRACKED. 2 L 7 2 4F RT A21EA 2008021200109 20080212 00109 EA 2008 2 12 MASA200800051 1 20080118 A 2750 865D1007 DRIVE UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A MASA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 07 651ML 7139 ASH FLT 7177 DSM-OVERNIGHT, FLAPS FAIL CAUTION. FLAPS FAILED AT 43 DEGREES ON THE GROUND DURING TAXI IN AND RETRACTION. REPLACED PDU, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008021200110 20080212 00110 EA 2008 2 12 MASA200800052 1 20080119 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17358 7358 ASH 2821 PHX - CENTER AISLE EMERGENCY FLOOD LIGHT INOP. MX RELAMPED THE LIGHT. 2 L 7 2 4F RT A21EA 2008021200129 20080212 00129 NM 2008 2 12 2008UALA00340 1 20080120 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 667UA 29239 EMERGENCY LIGHT AT SEAT 6H BROKEN. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021200156 20080212 00156 NM 2008 2 12 2008UALA00311 1 20080118 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY EXIT EEL LIGHTS ARE INOP AT SEATS 2J FWD & AFT, 4F FWD & AFT, FROM ROW 55 THRU 59 LEFT, AT ROW 61 LEFT AND AT DOOR 5 LEFT AFT LOWER WALL CROSS AISLE. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200157 20080212 00157 NM 2008 2 12 2008UALA00050 1 20080103 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EEL INOP ROW 32 LEFT INOPERATIVE. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200248 20080212 00248 EA 2008 2 12 A6WA200840005 1 20080101 A 3220 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NLG MALFUNCTIONED A A6WA K NONE O OTHER LD LANDING 1 GL 31 435AW 11795 7724 NOSE GEAR DOOR FLAPPING NOISE HEARD AFTER GEAR EXTENSION, TOOK LANDING GEAR CYCLE LONGER THAN NORMAL TO EXTEND. GEAR IN DICATOR SHOWED 3 GREEN SIMULTANEOUSLY. EMERGENCY LANDING DECLARED WITH UNEVENTFUL LANDING. (K) R&R NOSE LANDING GEAR S ELECT VALVE PER AMM 32-33-10. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200257 20080212 00257 NM 2008 2 12 AMTA200800021 1 20080116 A 4990 WARNING SYSTEM BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE APU ACTIVATED A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 522AT 29330 APU OIL QTY STATUS MSG DISPLAYED. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008021200262 20080212 00262 EU 2008 2 12 2008UALA00512 1 20080130 A 3350 BR964421 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 430UA 568 CABIN EMERGENCY AISLE LIGHT AT SEAT 14C IS INOP. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021200264 20080212 00264 NM 2008 2 12 2008UALA00515 1 20080130 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 UPPER DECK CEILING LIGHT NEAR 17AB IS INOP. RELAMPED CEILING LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200267 20080212 00267 NM 2008 2 12 2008UALA00518 1 20080130 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 SEAT 53ABC EMERGENCY LIGHT IS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200271 20080212 00271 2008 2 12 2008UALA00522 4 20080129 A 2330 VIDEO UNIT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ENTERTAIN SYS SHORTED A UALA K NONE W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 661UA 27158 SMOKE ODOR ROW 15-18. ENTERTAINMENT SYSTEM TURNED OFF. SMOKE DISSIPATED. SUSPECT INTERNAL SHORT VIDEO DISTRIBUTION BOX . REPLACED VDB UNDER ROW 17CDE,FOUND EVIDENCE OF BURNING INSIDE OF UNIT. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021200280 20080212 00280 NM 2008 2 12 2008UALA00532 1 20080130 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 360-380 S17R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FUSELAGE STR 17R CREASE BEAM WEB HAS ELONGATED HOLES FROM BS 360-380 RBL 58"-60". MAJOR REPAIR: REMOVED DAMAGE. FABRICA TED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200281 20080212 00281 NM 2008 2 12 2008UALA00534 1 20080130 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 DOOR 1R CREASE BEAM WEB AT BS 296, NUT PLATE HOLES ELONGATED. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED D OUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200290 20080212 00290 NM 2008 2 12 2008UALA00545 1 20080130 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 CREW REPORT: A CREASE ON THE LOWER FUSELAGE AFT OF THE AFT GALLEY DRAIN IS ABOUT A FOOT LONG. ACCOMPLISHED MAJOR REPA IR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021300013 20080213 00013 NM 2008 2 13 KCSA081064 1 20080202 A 5321 FLOOR SKIN BOEING 747 747209B 138489B NM BS 1860-1880 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 AFT BILGE FLOOR WEB IS CRACKED BETWEEN STA 1860 TO 1880, LBL 24. 2 L 7 4 4F RT A20WE 2008021300014 20080213 00014 NM 2008 2 13 KCSA081066 1 20080202 A 5311 FRAME BOEING 747 747209B 138489B NM BS 1780 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 AFT BILGE FUSELAGE FRAME UPPER CHORD IS DENTED AT STA 1780, RBL 51. 2 L 7 4 4F RT A20WE 2008021300015 20080213 00015 NM 2008 2 13 KCSA081067 1 20080202 A 5330 SKIN BOEING 747 747209B 138489B NM BS 590 S41L DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FOUND EXTERNAL FUSELAGE SKIN IS DAMAGED AT STA 590, STR 41L. 2 L 7 4 4F RT A20WE 2008021300025 20080213 00025 WP 2008 2 13 ABXR080032 1 20080109 A 5330 59114053 SKIN DOUG DC9 DC915F 3022037 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 166DE 47152 FOUND FUSELAGE SKIN CRACKED AT MAIN ENTRY DOOR UPPER AFT DOOR STOP HOLE. REPAIRED FUSELAGE SKIN AT MAIN ENTRY DOOR UPPE R AFT DOOR STOP IAW DC9 SRM 53-05. 2 L 7 2 4F A6WE 2008021300038 20080213 00038 NM 2008 2 13 ABXA080040 1 20080102 A 5330 145T86112 SKIN BOEING 767 767281 1385109 NM BS 780 S39R CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 787AX 23020 CORROSION UNDER SKIN CENTER WING FUSELAGE STRINGER 39 RIGHT, STA 780. REPAIRED AREA IAW REA 653-56928-MR. 2 L 7 2 4F RT A1NM 2008021300047 20080213 00047 NM 2008 2 13 USAA920080308 1 20080113 A 5320 6546579513 STIFFENER BOEING 737 7373S3 1384711 NM TORQUE BOX CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - NR 6028278, CORROSION ON APU CUT OUT TORQUE BOX STIFFENER, BS 1116, S18R. REPLACED APU CUT OUT TORQUE BOX STIFFENER, BS 1116, S18R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008021300063 20080213 00063 NM 2008 2 13 AALA200800175 1 20080126 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW - EMERGENCY LIGHTS AT OVERHEAD RIGHT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT O VERHEAD RIGHT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021300065 20080213 00065 WP 2008 2 13 AALA200800188 1 20080127 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 408AA 49319 LGA - EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020800079 20080208 00079 EA 2008 2 8 QXEA200800043 1 20080125 A 3320 BR9500106 BALLAST CNDAIR CL600 CL6002C10 1390015 EA CABIN LIGHTS ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 605QX 10022 PSP - FLIGHT 2610 - ELECTRICAL ODOR FROM ROW 4. MAINTENANCE COMPLIED WITH A INSPECTION OF THE SYSTEM AND WIRING AND FOU ND NO DEFECTS. REPLACE THE LAMPS AND THE PS50 BALLAST. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008020800081 20080208 00081 NM 2008 2 8 USAA920080276 1 20080115 A 5753 113N20033 FLAP BOEING 757 757225 1384959 NM LT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 MCN - MAJOR REPAIR - C11 CHECK - CORROSION ON LEFT WING INBOARD FLAP TRAILING EDGE, FLAP STATION 238 - FLAP STA 241. RE PAIRED LEFT WING INBOARD FLAP TRAILING EDGE, FLAP STATION 238 - FLAP STA 241 IAW B757 SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A2NM 2008020800084 20080208 00084 EU 2008 2 8 08FDEA00351 1 20080205 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 655FE 742 MCD FLOORBEAM HAS CRACK AT FR 30 LBL 67 FWD SIDE REWORKED AREA OF FLOORBEAM IAW SRM 51-10-15 FIG 212, RESTORED AREA IAW SRM 51-710. 2 L 7 2 4F RT A35EU 2008020800085 20080208 00085 NM 2008 2 8 USAA920080279 1 20080107 A 5511 182N1101 SPAR BOEING 757 757225 1384959 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 MCN - MAJOR REPAIR - C11 CHECK - CORROSION ON LEFT HORIZONTAL STABILIZER REAR SPAR, STABILZER STATION 236.25 - STABILIZE R STA 272.25. REPAIRED LEFT HORIZONTAL STABILIZER REAR SPAR, STABILZER STATION 236.25 - STABILIZER STA 272.25 IAW USAIR WAYS EA 100184. 2 L 7 2 4F RT A2NM 2008020800090 20080208 00090 NM 2008 2 8 USAA920080284 1 20080112 A 5347 SEAT TRACK BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 347 - BS 422, RBL 52, WL 200. REPLACED CABIN SEAT TRACK, BS 347 - BS 422, RBL 52, WL 200 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008020800091 20080208 00091 EU 2008 2 8 08FDEA00353 1 20080205 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 655FE 20414 742 MCD FLOORBEAM HAS CRACK AT FR25 RBL27 FWD SIDE REWORKED REPAIR AREA IAW 53-10-15, SRM 51-21-10 AND SRM 51-75-10, FINISHE D REPAIR IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008020800097 20080208 00097 SO 2008 2 8 CHQA200800019 1 20080201 A 7500 8166101 VALVE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RIGHT MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 574RP 9328 145845 CAE311908 CVG TO GSP - AFTER TAKEOFF, THE FLIGHT CREW RECEIVED A BLEED 2 OVER-TEMP MASTER WARNING. THE FLIGHT RETURNED TO FIELD A T CVG AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, THE FAULT TO THE NR 2 FAN AIR VALVE. THE NR 2 FAN AIR VALV E WAS REPLACED AND THE NR 2 BLEED SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008020800098 20080208 00098 NM 2008 2 8 NWAA080336746 1 20080127 A 3350 POWER SUPPLY BOEING 747 747222B 1384904 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 646NW 23737 DURING OVERNIGHT CHECK, FOUND EMERGENCY LIGHT LOCATED AT UPPER DECK CEILING NEAR GALLEY INOP. MAINTENANCE REMOVED AND R EPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008020800100 20080208 00100 NE 2008 2 8 HALA0800032 2 20080130 A 7420 106176651 IGNITION LEAD BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE LT ENGINE INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, NR 1 IGNITION ON LEFT ENG INOP. REPLACED NR 1 ENG FWD LEAD PER AMM 74-21-01. CHECKED LEAD, C OND SAME. REPLACED NR 1 ENG AFT LEAD, OPS CHECK GOOD PER AMM 74-21-01. 2 L 7 2 4F 4 F RT A1NM E13NE 2008020800101 20080208 00101 WP 2008 2 8 08FDEA00335 1 20080130 A 3260 UPLOCK SENSOR DOUG MD10 MD1010F 3022112 WP RT MLG OUT OF ADJUST A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 381FE 46615 UNSAFE RIGHT MAIN GEAR AFTER TAKEOFF WITH GEAR HANDLE IN "UP" POSITION, BOTH INDICATIONS. VISUAL INSPECTION INDICATED U P AND DOOR CLOSED. FOUND RT MAIN LANDING GEAR PROX UPLOCK SENSOR OUT OF ADJUSTMENT. SHIMMED IAW MM 32-61-15-4. PERFOR MED RTS IAW AMM 32-61-15-4. SYSTEM OP CK'D NORMAL. 2 L 7 3 4F RT A22WE 2008020800110 20080208 00110 WP 2008 2 8 AALA200800098 1 20080118 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 961TW 53611 DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 28 TO 30 AND AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY L IGHTS AT OVERHEAD SEAT ROWS 28 TO 30 AND AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800113 20080208 00113 EU 2008 2 8 SIMA200803102 1 20080128 A 5311 7253711164 FRAME SAAB SF340 340B 7860101 EU BS 225 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 320AE 21854 5000 340B320 DURING MBV INSPECTION, THE FLOOR SUPPORT FLANGE FRAME 225 WAS FOUND CORRODED. AIRCRAFT WAS OUT OF SERVICE. REMOVED AND REPLACED FRAME IAW SAAB 340 SRM 53-70-30. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2008020800114 20080208 00114 SO 2008 2 8 FDKA200801043 1 20080129 A 5411 14576631621 FRAME EMB 145 EMB145LR 3260212 SO LOWER COWLING CHAFED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 834MJ 145340 THE AFT FRAME OF THE LT AND RT LOWER COWLING IS CHAFED OUT OF LIMITS. THE DAMAGED FRAME HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008020800116 20080208 00116 WP 2008 2 8 AALA200800090 1 20080118 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 430AA 49342 LGA - EMERGENCY LIGHTS AT SEAT ROWS 14 TO 17 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 14 TO 17. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020800117 20080208 00117 NM 2008 2 8 AALA200800091 1 20080118 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 951AA 29538 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 7D HAS DAMAGED SHROUD. REPLACED AFT SHROUD FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008021300070 20080213 00070 EU 2008 2 13 08FDEA00362 1 20080206 A 5730 A57243210201 SKIN AIRBUS 310 A310222 3930315 EU RWS 1713 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 RIGHT WING SLAT NR 6 SCREWJACK CUT OUT, WING STATION 1713, CRACKED. REMOVED FASTENERS AT DAMAGED AREA IAW FEDEX A310-20 0 SRM 51-40-21 PAGE 22. CUT OUT SKIN DAMAGE AT LEADING EDGE WING STATION 1713 IAW FEDEX A310-200 SRM 57-41-12 PAGE 209 FIGURE 203. INSTALLED REPAIR PARTS IAW FEDEX A310-200 SRM 57-41-12 PAGE 209 FIGURE 203 AND A310-200 SRM 51-40-21 PAGE 2 2. 2 L 7 2 4F RT A35EU 2008021300079 20080213 00079 NM 2008 2 13 08FDEA00363 1 20080207 A 5415 311N5033 FITTING BOEING 757 7572B7 1384964 NM ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 AFTER INSP FOR FINAL REAM FOUND NR 2 PYLON MID BULKHEAD FWD AND AFT LUG HOLES FOR SLEEVE BOLTS ACTUALLY REAMED TO .772", FOUND CORROSION ON EO NR F-5450-7-5005 PE STEP 10. HFEC INSPECTION FWD AND AFT SLEEVE BOLT HOLES IN THE NR 2 PYLON MID BULKHEAD FITTING PER NTM 51-00-00 PT.6 WITH NO DEFECTS NOTED. BOTH HOLES WERE REAMED TO REMOVE CORROSION. THE FWD HOL E WAS FOUND TO HAVE A SLEEVE BOLT REPAIR. FWD HOLE DIA .7714", AFT HOLE DIA .7774" HAVING A BELL SHAPED CONDITION. FWD BOLT HOLE WAS REAMED TO .880-.887" AND A SLEEVE BUSHING INSTALLED PER EA F-5450-110819. BOTH FWD AND AFT BOLT HOLES WE RE REAMED TO .780 - .787" AND SB410YN10L34S SLEEVE BOLTS. INSTALLED PER EA NR F-5450-110819 DATED. 2 L 7 2 4F RT A2NM 2008021300088 20080213 00088 NM 2008 2 13 USAA920080358 1 20080205 A 5320 146N52468 INTERCOSTAL BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 202UW 27811 BFM - MAJOR REPAIR - C4 CHECK - NR 6040671, LEVEL 2 CORROSION ON CABIN FLOOR STRUCTURE INTERCOSTAL, BS 1641 - BS 1661, B L 56. REPLACED CABIN FLOOR STRUCTURE INTERCOSTAL, BS 1641 - BS 1661, BL 56 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008021300094 20080213 00094 NM 2008 2 13 USAA920080364 1 20080122 A 5311 FRAME BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q3 CHECK - NR JK-58-53507/3, CRACKED FRAME WEB, BS 500D, S9R. REPAIRED FRAME WEB, BS 500D, S9R IAW USAIRWAYS TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2008021300105 20080213 00105 NM 2008 2 13 DHLA200800014 1 20080208 A 2612 FIRE WARNING BOEING 727 727227 1384078 NM NR 3 NACELLE FALSE ACTIVATION A DHLA O OTHER N FALSE WARNING DE DESCENT 1 GL 05 782DH 21998 FLT 107, NR 3 ENG FIRE DETECTION AMBER LIGHT ILLUM INTERMITTENTLY ON DESCENT (P6-3). COULDNT DULPLICATE PROBLEM, OPS CH ECKS GOOD PER M/M 26-11-00. NO DEFECTES NOTED AT THIS TIME. ACFT GROUNDED. 2 L 7 3 4F A3WE 2008021300112 20080213 00112 WP 2008 2 13 UPS08851637 1 20080110 A 5311 FRAME DOUG DC8 DC871F 302199D WP FS 560 L21L CUT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 CUTOUT IN FRAME AT FS 560 BETWEEN L21+20L-MAIN CABIN FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 53-02-00,51-01-08, AND DWG DC8-53A-011. 2 L 7 4 4F RT 4A25 2008021300114 20080213 00114 NM 2008 2 13 UPS08M51638 1 20080121 A 5712 ARB2850506 FITTING DOUG MD11 MD11F 3023600 NM RT WING RIB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP 48768 INSPECTION TYPE:1C RT FIXED LE RIB FITTING IB OF NR 16 SLAT TRACK IS CRACKED. REMOVED AND REPLACED RT FIXED LE RIB FITT ING IB OF NR 16 SLAT TRACK PER MD-11 SRM 51-31-01 AND 51-35-01. 2 L 7 3 4F RT A22WE 2008021300123 20080213 00123 NM 2008 2 13 08FDEA00370 1 20080208 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 MAIN DECK, AFTER FLOOR PANEL REMOVAL TO FACILITATE SEAT TRACK REPAIR, FOUND SEAT TRACK UNDER FLOOR PANEL AT STA 635, X = 11 CRACKED. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSI FIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008021300129 20080213 00129 NM 2008 2 13 USAA920080385 1 20080103 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - NR 6006033 AND I2A53011/1, CRACKED BULKHEAD WEB, BS 178, RBL 1, WL 207. REPAIRED BULKH EAD WEB, BS 178, RBL 1, WL 207 IAW USAIRWAYS EA 100192. 2 L 7 2 4F RT A16WE 2008021300130 20080213 00130 NM 2008 2 13 USAA920080386 1 20080207 A 5310 6547952524 DOOR FRAME BOEING 737 7373G7 1384595 NM ZONE 100 - FUSEL CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - NR I2D52004/2, AFT CARGO DOOR FORWARD FRAME CRACKED. REPLACED AFT CARGO DOOR IAW B737 SRM 52-31-00. 2 L 7 2 4F RT A16WE 2008021300131 20080213 00131 NM 2008 2 13 USAA920080387 1 20080204 A 5512 SKIN BOEING 737 7374B7 1384702 NM ZONE 300 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 453UW 24980 CLT - MAJOR REPAIR - C1 CHECK - NR JK-44-2500C/1, RIGHT HORIZONTAL STABILIZER SKIN CRACKED. REPAIRED RIGHT HORIZONTAL S TABILIZER SKIN IAW USAIRWAYS TYPICAL REPAIR 55-10-07 REV C. 2 L 7 2 4F RT A16WE 2008021300138 20080213 00138 NM 2008 2 13 USAA920080394 1 20080205 A 5320 6948985 ANGLE BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 CLT - MAJOR REPAIR - C2 CHECK -NR 03-0553-8-0403/5, CRACKED ANGLE, BS 360, S8L. REPLACED ANGLE, BS 360, S8L IAW BOEING DRAWING 69-48985. 2 L 7 2 4F RT A16WE 2008021300147 20080213 00147 NM 2008 2 13 DHL2008782002 1 20080109 A 5412 FIREWALL BOEING 727 727227 1384078 NM NR 2 NACELLE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 UPON INSPECTING THE NR 2 ENGINE FIREWALL, FOUND AN APPROX 2 1/4 INCH CRACK IN AFT WEB AT 8 O'CLOCK POSITION APPROX 6" FR OM FLEX ADAPTER. REPAIR WILL BE MADE IAW SRM 54-10-01, 54-10-03 FIG 1 AND M/M 51-30-0. 2 L 7 3 4F A3WE 2008021300196 20080213 00196 NM 2008 2 13 USAA920080396 1 20080209 A 2611 100064904 SMOKE DETECTOR BOEING 737 737301 1384611 NM CARGO BAY FAILED A USAA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 19 577US 23742 CLT - EE - FLT NR 1524 - CREW REPORTED MX LIGHT ON CARGO FIRE PANEL ILLUMINATED. MX REPLACED SMOKE DETECTOR. OPERATION AL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2008021500022 20080215 00022 EA 2008 2 15 TRAX200800214 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 693-830 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 RT FLOOR SEAT RAIL FS 693.0 TO FS 830.40 AT LBL 9.0 HAS CORROSION DAMAGE ON RAIL AND HARDWARE. R & R RT FLOOR SEAT RAIL FS 693.0 TO FS 830.40 AT LBL 9.0 PER CRJ700 MM 53-00-49. 2 L 7 2 4F RT A21EA 2008021300200 20080213 00200 WP 2008 2 13 UPS08851642 1 20080107 A 5320 9755804 CUSP WEB DOUG DC8 DC871F 302199D WP FS 275 L21R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 MAIN CABIN, L21R HAS HEAVY INTERGRANULAR CORROSION AND A 4 INCH CRACK INSIDE TORQUE BOX STA 275. REP AIRED L21R CUSP CRACK AND CORROSION AT STA 210, 235 AND 275 IAW SRM 53-02-00 FIG 002, SRM 53-02-05 FIG 15 AND DWG 975580 8. 2 L 7 4 4F RT 4A25 2008021400002 20080214 00002 NM 2008 2 14 ZZDA2008063 1 20080129 A 5311 FRAME BOEING 717 717200 1383700 NM BS 1178 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 981AT 55040 TWO CRACKS FOUND AT INT TAIL COMP LT SIDE CANTED FRAME STA 1178.225 BETWEEN LONG 13L AND 14L. INSTALLED FORMED CHANNEL REPAIR ON CANTED FRAME LT STA 1178.225 PER B717 SRM 51-70-11 FIG 201. 2 L 7 2 4F TR A6WE 2008021400010 20080214 00010 EU 2008 2 14 TRAX200800161 1 20080128 A 5320 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 INTERCOSTAL CORRODED BTW FR 36-38 STRG 17R. REPLACED IAW SRM 51-25-01 AND SRM 51-25-04. 2 H 7 2 4T RT A53EU 2008021400013 20080214 00013 EU 2008 2 14 TRAX200800164 1 20080128 A 5313 STRINGER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 FR 37 CORRODED AT LEVEL STRG 17R. CORROSION 37 REMOVED AS PER SRM 51-21-42. OUT OF LIMITS AS PER SRM 53-61-00 FIG 301. REPAIRED AS PER SRI DO/TS-412/08-9790. NDT C/O ON FR CUT EDGE IAW NTM PART 1 CM 51-60-00 NO CRACKS DETECTED 2 H 7 2 4T RT A53EU 2008021400015 20080214 00015 EU 2008 2 14 TRAX200800166 1 20080130 A 5720 ANGLE AEROSP ATR72 ATR72212 8680945 EU LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 LT WING PRESSURE DECK ANGLE CRACKED IN Y AND X AXIS. E/C PERFORMED AMO 46-90 IAW NTM NED OF CRACK MARKED IN X AXIS CRA CK EXTENDS BEYOND FASTENER IN Y AXIS END OF CRACK MARKED. RIVET REMOVED FOR ROTOTEST INSPECTION IAW SRM 51-25-01. E/C H FEC & ROTO TEST PERFORMED AMO 46-90 IAW NTM NO CRACK IN FASTENER HOLE NO CRACKS ON ITEMS. RIVET INTALLED IAW SRM 51-25-0 1. PRC APPLY ON BOTH CRACKS IAW DO/TS-333/08-9783 COMPLIED WITH EC/TC DO/TS-333/08. 2 H 7 2 4T RT A53EU 2008021400018 20080214 00018 EU 2008 2 14 TRAX200800169 1 20080130 A 5720 BRACKET AEROSP ATR72 ATR72212 8680945 EU LT WING BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 LT RIB 8 FLAP BEAM (2) OMEGA BRACKET BROKEN. 2 H 7 2 4T RT A53EU 2008021400019 20080214 00019 EU 2008 2 14 TRAX200800170 1 20080130 A 5320 CHANNEL AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 CHANNEL AT LINE BEHIND L/E 325AL FOUND CRACKED. REPLACED IAW JIC 55-12-00. 2 H 7 2 4T RT A53EU 2008021400020 20080214 00020 EU 2008 2 14 TRAX200800171 1 20080130 A 5340 STRINGER CLIP AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 STRINGER CLIP 21 BIN AT FR 39 CORRODED. CORROSION REMOVED AS PER SRM 51-21-42. FABRICATED AS PER SRM 53-61-40 FIG 110. REMOVED AND INSTALLED AS PER SRM 51-25-01. OUT OF LIMITS AS PER SRM: 53-61-00 FIG 301. 2 H 7 2 4T RT A53EU 2008021400027 20080214 00027 EA 2008 2 14 TRAX200800178 1 20080201 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 680BR 7679 FS 280.00 LBL 9.00 OUTBD ATTACH ANGLE CRACKED. REMOVED CRACKED ATTACH ANGLE IAW SRM 51-42-06 AND SRM 51-42-21. COMPL IED WITH ASA EC/TC REO 601R-53-21-852. 2 L 7 2 4F RT A21EA 2008021400029 20080214 00029 EA 2008 2 14 TRAX200800180 1 20080201 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 680BR 7679 FS 280.00 RBL 9.00 INBD ATTACH ANGLE CRACKED. 2 L 7 2 4F RT A21EA 2008021400032 20080214 00032 EA 2008 2 14 TRAX200800183 1 20080202 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 RT STA 280 BULKHEAD WEB CORRODED AT CROSSBEAM. REPAIRED IAW IAE REO 670-53-11-052. 2 L 7 2 4F RT A21EA 2008021200174 20080212 00174 NM 2008 2 12 2008UALA00011 1 20080101 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 SEAT ROW 15 FWD & SEAT 40ABC EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED EMERGENCY LIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200249 20080212 00249 EA 2008 2 12 A6WA200840006 1 20080104 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NLG FAILED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 425AW 13091 7724 ON DEPARTURE, SELECTED GEAR LEVER UP. RECEIVED TRIPLE CHIME AND DISAGREE AURAL MESSAGE. GOT GEAR DISAGREE NOSE GEAR DO OR WARN MESSAGES AND WOW INPUT AND NWS INOPERATIVE CAUTION MESSAGES. EXECUTED QRH IN THAT ORDER, HAD 3 GEAR DOWN LOCKED INDICATIONS. REMOVED AND REPLACED NLG SELECTOR VALVE, SWING OF NLG CHECKS GOOD IAW AMM 32-33-10. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021300011 20080213 00011 NM 2008 2 13 KCSA081062 1 20080201 A 5330 SKIN BOEING 747 747209B 138489B NM BS 375 S41-42R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FOUND STA-375 SKIN DAMAGED BETWEEN STR-41R AND STR-42R. 2 L 7 4 4F RT A20WE 2008021300041 20080213 00041 NM 2008 2 13 ABXA080042 1 20080107 A 5330 SKIN BOEING 767 767281 1385109 NM BS 276 MISREPAIRED A ABXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 787AX 23020 COMPLY WITH REA B653-56867-MR FOR FORWARD FUSELAGE, STA 276, STRINGER 26 RIGHT SKIN REPAIR. REPAIRED FUSELAGE SKIN IAW B767 SRM 53-00-01, FIGURE 201, REPAIR 12 AND REA B653-56867-MR. 2 L 7 2 4F RT A1NM 2008021300069 20080213 00069 2008 2 13 AALA200800166 4 20080125 A 2565 100504205 SLIDE DOUG DC9 DC982 3022082 WP R1 DOOR FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 583AA 53160 SAN - EMERGENCY ESCAPE SLIDE AT R1 DOOR UNSUCCESSFULLY DEPLOYED. SLIDE WAS HANGING FROM GIRT BAR AT DOOR FRAME. REPLAC ED RIGHT NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008021300076 20080213 00076 NM 2008 2 13 F3LA200800045 1 20080206 A 5320 D5391379020002 PLATE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 15440 5503 2019 REFERENCE NON ROUTINE 26838, DURING C3/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE FRAME PLATE AT FRAME 2 8, ON THE RIGHT SIDE, NEAR THE CARGO DOOR OPENING. MAINTENANCE REMOVED AND REPLACED THE CORRODED FRAME PLATE IN ACCORDA NCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE INSTALLATION, THE NEW FRAME PLATE WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008021300089 20080213 00089 NM 2008 2 13 USAA920080359 1 20080206 A 5320 INTERCOSTAL BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 202UW 27811 BFM - MAJOR REPAIR - C4 CHECK - NR 6040672, LEVEL 2 CORROSION ON CABIN FLOOR STRUCTURE INTERCOSTAL, BS 1661 - BS 1682, R BL 56. REPLACED CABIN FLOOR STRUCTURE INTERCOSTAL, BS 1661 - BS 1682, RBL 56 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008021300096 20080213 00096 NM 2008 2 13 USAA920080366 1 20080124 A 5754 SKIN BOEING 737 7374B7 1384702 NM ZONE 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q3 CHECK - NR JK-11-57101/3, LEFT WING NR 3 SLAT LOWER SKIN CRACKED. REPAIRED LEFT WING NR 3 SLAT LOWER SKIN IAW B737 SRM 57-43-01. 2 L 7 2 4F RT A16WE 2008021300099 20080213 00099 NM 2008 2 13 USAA920080369 1 20080124 A 5313 STRINGER BOEING 737 7374B7 1384702 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q3 CHECK - NR JK-51-53500C/1, CRACKED STRINGER, BS 500, S24R. REPAIRED STRINGER, BS 500, S24R IAW B737 SRM 53-00-03 REPAIR 1. 2 L 7 2 4F RT A16WE 2008021300126 20080213 00126 EU 2008 2 13 08FDEA00373 1 20080208 A 7830 PANEL NA AIRBUS 310 A310222 3930315 EU THRUST REVERSER WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 0140 288 NR 2 ENGINE OUTBOARD T/R UPPER BIFURCATION DUCT INNER PANEL HAS WEAR COMPLIED WITH FED EX EA6-7830-7-113013. NR 2 ENGIN E OUTBOARD T/R UPPER BIFURCATION HEAT SHIELD REPAIR. 2 L 7 2 4F RT A35EU 2008021300139 20080213 00139 NM 2008 2 13 USAA920080395 1 20080113 A 5314 65621257 KEELBEAM BOEING 737 7373S3 1384711 NM BS 500D S28L CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 CLT - MAJOR REPAIR - C2 CHECK - NR 6033578, LEVEL 2 CORROSION ON KEEL BEAM LOWER CHORD, BS 500D, S28L. REPAIRED KEEL BE AM LOWER CHORD, BS 500D, S28L IAW B737 SRM 53-30-12. 2 L 7 2 4F RT A16WE 2008021300199 20080213 00199 NM 2008 2 13 UPS08551656 1 20080209 A 2560 SEAL BOEING 757 75724APF 1384969 NM PBE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 410UP 23732 SEAL ON PBE BROKEN AND VSI INDICATOR PROTRUDING. REMOVED AND REPLACED PBE ASSY AND VISUALLY CHECKED UNIT IAW MM 35-31-0 1-6. 2 L 7 2 4F RT A2NM 2008021400008 20080214 00008 EA 2008 2 14 TRAX200800159 1 20080201 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA EXTERNAL INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 750EV 10161 LT AFT MOST EXTERNAL EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008021400025 20080214 00025 EA 2008 2 14 TRAX200800176 1 20080201 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 680BR 7679 CABIN SUBFLOOR, 484.00 INTERCOSTAL CRACKED AT ATTACH POINT RBL 36. 2 L 7 2 4F RT A21EA 2008021400031 20080214 00031 EA 2008 2 14 TRAX200800182 1 20080202 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 LT STA 280 BULKHEAD WEB CORRODED AT CROSSBEAM. INSTALLED BULKHEAD WEB. ALL WORK IAW 670-53-11-052 BM 7024222. STARTED FABRICATING AND DRILLING NEW WEB. WEB FABRICATED IAW 670-53-11-052 BU 7024222. FINISH DRILLING OF WEB IAW 670-53-11-052 . OK TO INSTALL. INSTALLED WEB PER STEP/ITEM 2. PERFORMED FINAL CLEAN UP AS REQUIRED. 2 L 7 2 4F RT A21EA 2008021400036 20080214 00036 WP 2008 2 14 NWAA080389758 1 20080204 A 2910 O-RING DOUG DC9 DC941 302207N WP HYD SYSTEM FAILED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 758NW 47286 IN CRUISE FLT AT FL310, THE RT HYD SYS FAILED. QTY AND PRESSURE WERE BOTH LOST REQUIRING CREW TO SECURE SYSTEM. FLT CO NTINUED AS SCHEDULED AND THE EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED ON APPROACH. LANDING AT TPA INVOLVED THE GEAR DOORS MAKING CONTACT WITH THE RUNWAY. MAINTENANCE FOUND A HYD LEAK IN THE TAIL AREA AND REPLACED RUDDER LOW PRESS URE SWITCH DUE TO A FAILED O-RING. ALSO, BOTH GEAR DOORS WERE REPLACED DUE TO BEING SCRAPED UP DURING THE LANDING. OPE RATIONAL CHECK (GEAR SWING, DOOR SEQUENCE, AND PROPER INDICATIONS OF EACH) AND LEAK CHECK WERE GOOD AND THE AIRCRAFT RET URNED TO SERVICE. 2 L 7 2 4F A6WE 2008021400039 20080214 00039 NM 2008 2 14 ZZDA2008053 1 20080107 A 5311 FRAME BOEING 717 717200 1383700 NM BS 1178 S25R DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 FRAME DAMAGED AT STA 1178 BETWEEN LONG BL0 AND 25R. INSTALLED NEW LOWER CAP SECTION AND SPLICE AT STA 1178 BETWEEN LONG ERON BL0 AND 25R IAW SRM 51-70-11, AIRTRAN EA17-53-00939A AND MESSAGE 1-CEY7NA. 2 L 7 2 4F TR A6WE 2008021400060 20080214 00060 NM 2008 2 14 NWAA080406308 1 20080202 A 5315 FLOORBEAM BOEING 747 747451 1384940 NM BS 400 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 668US 24223 DURING "M" CHECK, FOUND DOUBLE DRILLED FASTENER HOLES IN UPPER DECK FLOORBEAM AT BS 400 LBL 20 AND LBL 40. REPAIRED PER EA 63-211701. 2 L 7 4 4F RT A20WE 2008021400062 20080214 00062 NM 2008 2 14 QXEA200800120 1 20080207 A 3231 MECHANISM BOMBDR DHC8 DHC8402 1390042 NM MLG DOOR FAILED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 403QX 4037 LAX - BOTH MAIN LANDING GEAR DOORS CYCLED DURING CLIMB AND THEN APPROXIMATELY EVERY 6 MINUTES, PLUS MLG RED CAUTION LIGH T ILLUMINATED. FERRIED AIRCRAFT TO PDX FOR MAINTENANCE. PDX MAINTENANCE REMOVED AND REPLACED LEFT MAIN LANDING GEAR AF T DOOR MECHANISM, EXTENSION AND RETRACTION OPS CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008021400063 20080214 00063 NM 2008 2 14 QXEA200800057 1 20080203 A 5210 8SC04421 SPRING DHAV DHC8 DHC8202 2809007 NM PAX DOOR MALFUNCTIONED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 PDX - MAIN CABIN DOOR DIFFICULT TO OPEN. PDX MAINTENANCE REMOVED AND REPLACED MAIN CABIN DOOR GAS SPRINGS WITH NEW SPRI NGS. OPS CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008021400064 20080214 00064 NM 2008 2 14 ZZDA2008066 1 20080206 A 5320 PAN BOEING 717 717200 1383700 NM CARGO DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 982AT 55041 AFT CARGO DOOR CUT OUT LOWER PAN HAS CORROSION. FOUND CORROSION OUT OF LIMITS TRIMED OUT DAMAGE SECTION AND INSTALLED N EW SECTION AND SPLICES IAW B717 SRM 53-20-15 FIG 201. 2 L 7 2 4F TR A6WE 2008021400066 20080214 00066 NM 2008 2 14 ZZDA2008068 1 20080205 A 5320 PAN BOEING 717 717200 1383700 NM CARGO DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 603AT 55127 AFT CARGO DOOR JAM CUT OUT LOWER PAN HAS CORROSION. CUT OUT LOWER JAM SECTION AND INSTALLED LOWER JAM SECTION AND SPLIC ES AT AFT CARGO COMP IAW B717 SRM 53-20-15 REP 7. 2 L 7 2 4F TR A6WE 2008020800118 20080208 00118 NM 2008 2 8 C1HA200893001 1 20080130 A 2750 FLAP SYSTEM BOEING 727 727212 138407G NM TE FLAPS MALFUNCTIONED A C1HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 293AS 21348 UPON FLAP RETRACTION, THE INBOARD TRAILING EDGE LEFT WING REMAINED AT 1 DEG OF EXTENSION. COMPLIED WITH COM 2.27.16. D UMPED FUEL COM 228.4. INSPECTED INBD T/E FLAPS PER WO 123219, N/R'S 1 AND 2. NO DEFECTS NOTED. INBD FLAP IND WAS 1 NEE DLE OFF. REMOVED AND REPLACED IND PER MM 27-52-21. SYSTEM OPS CK NORMAL. 2 L 7 3 4F A3WE 2008020800125 20080208 00125 NM 2008 2 8 AALA200800104 1 20080119 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 957AN 29541 DFW - EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A16WE 2008020800127 20080208 00127 2008 2 8 AALA200800106 4 20080119 A 2565 SLIDE BOEING 737 737823 13844BZ NM R1 DOOR FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 920AN 29521 SNA - EMERGENCY SLIDE AT RIGHT NUMBER ONE POSITION FELL FROM COVER AND DID NOT DEPLOY. REPLACED RIGHT NUMBER ONE DOOR S LIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008020800128 20080208 00128 NM 2008 2 8 AALA200800105 1 20080119 A 3350 SIGN BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 948AN 30086 MIA - EMERGENCY EXIT SIGN LIGHT AT RIGHT NUMBER ONE DOOR DAMAGED. REPAIRED EXIT SIGN FOR EMERGENCY LIGHT AT RIGHT NUMBE R ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008020800137 20080208 00137 WP 2008 2 8 AALA200800076 1 20080116 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9409F 53121 LGA - EMERGENCY EXIT SIGN LIGHT AT AFT CABIN DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY EXIT SIGN LIGHT AT AFT CABI N DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800139 20080208 00139 NM 2008 2 8 AALA200800088 1 20080118 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 360AA 24041 ORD - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008020800140 20080208 00140 WP 2008 2 8 AALA200800126 1 20080121 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9617R 53564 DFW - EMERGENCY LIGHT AT SEAT 16C HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 16C. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800141 20080208 00141 WP 2008 2 8 AALA200800127 1 20080121 A 3350 SHROUD DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9617R 53564 DFW - EMERGENCY LIGHT AT SEAT 13D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800143 20080208 00143 NM 2008 2 8 USAA920080287 1 20080110 A 5347 SEAT TRACK BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 1362 - BS 1479, RBL 55, WL 200. REPLACED CABI N SEAT TRACK, BS 1362 - BS 1479, RBL 55, WL 200 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008020800148 20080208 00148 NM 2008 2 8 USAA920080291 1 20080119 A 5330 SKIN BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON FUSELAGE SKIN INSIDE AFT CARGO COMPARTMENT, BS 1149, RBL 11. REPA IRED FUSELAGE SKIN INSIDE AFT CARGO COMPARTMENT, BS 1149, RBL 11 IAW USAIRWAYS EA 100146. 2 L 7 2 4F RT A1NM 2008020800153 20080208 00153 NM 2008 2 8 USAA920080296 1 20080127 A 5511 183N150127 RIB BOEING 757 757225 1384959 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 MCN - MAJOR REPAIR - C11 CHECK - CORROSION ON RIGHT HAND HORIZONTAL STABILIZER UPPER RIB CHORD, STABILIZER STATION 128.2 48. REPLACED RIGHT HAND HORIZONTAL STABILIZER UPPER RIB CHORD, STABILIZER STATION 128.248 IAW BOEING DRAWING 183N1501. 2 L 7 2 4F RT A2NM 2008020800156 20080208 00156 NM 2008 2 8 ASAA0842505 1 20080126 A 5210 632589 SNAP RING BOEING 737 7374Q8 138447Q NM L-1 DOOR MISSING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 THE L1 DOOR WAS HARD TO OPEN DUE TO A SNAP RING THAT HAD COME OFF OF A PIN THAT HOLDS THE TOP RADIUS LINK IN PLACE. THE LOSS OF THE SNAP RING CAUSED THE PIN TO MIGRATE UP CREATING A BINDING FEELING WHEN THE DOOR WAS OPENING. PUSHED PIN BA CK TO NORMAL POSITION AND INSTALLED HARDWARE PER MM 52 11 21. INSPECTED FOR DAMAGE, NONE NOTED OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2008020800157 20080208 00157 NM 2008 2 8 AALA200800115 1 20080120 A 2840 TRANSMITTER BOEING 767 767323 1385205 NM FUEL FLOW INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 370AA 25197 JFK INFLIGHT T0041/20JAN CDG TO ORD - CREW REPORTED FUEL DISAGREE MESSAGE IN FLIGHT. LANDED JFK WITHOUT INCIDENT. AIR CRAFT REMOVED FROM SERVICE. REPLACED LEFT FUEL FLOW TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008020800164 20080208 00164 2008 2 8 QXEA200800056 4 20080201 A 3170 8221310104 DCU CNDAIR CL600 CL6002C10 1390015 EA NR 2 SMOKE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 600QX 4290 10005 YEG- ON TAXI (APU POWER ON), THE CIRCUIT BREAKER FOR THE DCU 2 POPPED. SMOKE FROM THE H13 CIRCUIT BREAKER (EICAS). CIR CUIT BREAKER DID NOT POP. RECEIVED MULTIPLE FAULT STATUS MESSAGES FOR THE DCU 2 AND DCU AURAL 2 FAILURE. EVACUATED AIR CRAFT. MAINTENANCE REPLACED THE DCU NR 2 AND THE CIRCUIT BREAKERS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F RT A21EA 2008020800170 20080208 00170 WP 2008 2 8 AALA200800136 1 20080122 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 974TW 53624 DFW - EMERGENCY LIGHT AT SEAT 17D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020600361 20080206 00361 EA 2008 2 6 TRAX200800125 1 20080121 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 709EV 10068 LEFT AND RIGHT O/W EMERGENCY EXITS, LOWER LIGHTS HAVE SEVERAL BULBS INOP. 2 L 7 2 4F RT A21EA 2008020600368 20080206 00368 NM 2008 2 6 USAA920080250 1 20080115 A 5753 6546486 SKIN BOEING 737 7373Y0 1384671 NM T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - RIGHT WING INBOARD MID FLAP LOWER SURFACE HAS AREA OF DELAMINATION, WBL 73 - WBL 75. R EPAIRED RIGHT WING INBOARD MID FLAP LOWER SURFACE, WBL 73 - WBL 75 IAW B737 SRM 57-70-10-2R4. 2 L 7 2 4F RT A16WE 2008020600376 20080206 00376 NM 2008 2 6 USAA920080268 1 20080105 A 5347 SEAT TRACK BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 764 - BS 830, LBL 88.5. REPLACED CABIN SEAT TR ACK, BS 764 - BS 830, LBL 88.5 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008020700017 20080207 00017 NM 2008 2 7 ZZDA2008057 1 20080122 A 5320 PAN BOEING 717 717200 1383700 NM CARGO BAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 959AT 55021 FWD CARGO COMPARTMENT DOOR CUTOUT LOWER PAN HAS CORROSION BEYOND LIMITS. INSTALLED NEW PAN AND SPLICES AS PER B717 SRM 53-20-15 FIG 201. 2 L 7 2 4F TR A6WE 2008020700026 20080207 00026 EU 2008 2 7 08FDEA00334 1 20080130 A 5510 A55176100004 TIP CAP AIRBUS 310 A310 EU HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 LT HORIZONTAL STAB TIP, TRAILING EDGE, CRACKED. REMOVED DAMAGE & APPLIED FIBERGLASS WET LAY UP IAW 55-14-11 FIGURE 203, DWG A551- 76100 & EA 6-5510-113014. 2 L 7 2 4F RT A35EU 2008020700060 20080207 00060 NM 2008 2 7 2008UALA00443 1 20080125 A 2120 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE COCKPIT SMOKE A UALA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 221UA 30552 FLIGHT DIVERTED AFTER A PACK VALVE EICAS MESSAGE WAS DISPLAYED & SMOKE WAS DETECTED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008020700078 20080207 00078 NE 2008 2 7 COMA0860071 2 20080116 A 7200 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30068 NE LEFT FAILED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 01 964CA 19026 7129 807605 FLIGHT 5341 - EN ROUTE FROM MKE TO CVG SEVERE ENGINE NOISE AND SHUDDER ON LEFT ENGINE. PERFORMED IFSD. EMERGENCY DECLA RED AND AIRCRAFT DIVERTED TO ORD AND LANDED SAFELY. REMOVED AND REPLACED LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008020700117 20080207 00117 EA 2008 2 7 COMA0860101 1 20080127 A 5610 NP1393225 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 971CA 12220 7145 FLIGHT 5483 - LEFT COCKPIT SIDE WINDOW SHATTERED, FOLLOWED QRH, LANDED CVG WITHOUT INCIDENT. REPLACED LEFT COCKPIT SIDE WINDOW. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008020700135 20080207 00135 NM 2008 2 7 SWAA080514 1 20080129 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 453WN 29847 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2008020700136 20080207 00136 NM 2008 2 7 SWAA080516 1 20080129 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 483WN 32472 EEPLS LENS CRACKED AT ROW 19 DEF. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008020700158 20080207 00158 NM 2008 2 7 HNAA0800048 1 20080123 A 3350 AML91LA85 CIRCUIT BREAKER DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 53 GREEN LIGHT NOT ILLUMINATING ON EMERGENCY LIGHT SWITCH AT F/A'S PANEL. REPLACED SWITCH (P/N AML21GBA2CD) NO FIX, REPLAC ED C/B, OPS CK'D GOOD. 2 H 7 2 4T RT A13NM 2008020700184 20080207 00184 EA 2008 2 7 TRAX200800144 1 20080128 A 2560 MEGAPHONE CNDAIR CL600 CL6002C10 1390015 EA CABIN WEAK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 317CA 10055 AFT MEGAPHONE VOLUME WEAK. 2 L 7 2 4F RT A21EA 2008020700187 20080207 00187 EU 2008 2 7 TRAX200800147 1 20080128 A 5714 FAIRING AEROSP ATR72 ATR72 EU WING BOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 RIGHT SIDE WING BOX FAIRING FR 28A FACING CRACKED. REPAIR ACCOMPLISHED IAW SRM 51-25-01 2 H 7 2 4T RT 2008020800027 20080208 00027 NM 2008 2 8 HALA0800033 1 20080201 A 3241 42977 CONTROL UNIT BOEING 717 717200 1383700 NM ANTI SKID SYS FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 480HA 55125 ANTI-SKID FAIL IN FLT - ATB. REPLACED BCU PER AMM 32-45-01. RETURN TO SERVICE TEST PASSED. 2 L 7 2 4F TR A6WE 2008020800061 20080208 00061 NM 2008 2 8 USAA920080243 1 20080122 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - CRACKED WEB, BS 178, LBL 5.7, WL 207.5. REPAIRED WEB, BS 178, LBL 5.7, WL 207.5 IAW B7 37 SRM 51-70-13. 2 L 7 2 4F RT A16WE 2008020800070 20080208 00070 NM 2008 2 8 USAA920080261 1 20080115 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q5 CHECK - CRACKED FRAME, BS 480, S9L. REPAIRED FRAME, BS 480, S9L IAW USAIRWAYS TYPICAL REPAIR 53 -10-20E. 2 L 7 2 4F RT A16WE 2008020800095 20080208 00095 EU 2008 2 8 08FDEA00358 1 20080205 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 655FE 20411 742 MCD FLOORBEAM HAS CRACK AT FR 31 LBL67 FWD SIDE REWORKED CRACKED AREA IAW SRM 53-10-15 AND SRM 51-22-0, FINISHED REWORKE D AREA IAW 51-75-10. 2 L 7 2 4F RT A35EU 2008020800103 20080208 00103 NM 2008 2 8 08FDEA00337 1 20080131 A 2150 89812621 REGULATOR BOEING 727 727277 138408S NM A/C PACK FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 241FE 8148 8148 20979 DURING CLIMB-OUT WITH ENG ANTI ICE OPEN, WHEN RT PACK WAS TURNED ON, RIGHT PSI MAXED OUT TO 110 PSI. WHEN RT PACK WAS S WITCHED OFF, ENG 3 STRUT OVHT LIGHT ILLUM FOR APPROX 20 SEC. NR 3 PWR LEVER WAS REDUCED AND LIGHT WENT OUT. CYCLING TH E PACK BACK ON PSI REMAINED 20 PSI HIGHER THAN THE LEFT SIDE AT 50 PERCENT POWER SETTING. REMOVED AND REPLACED NR 3 HIG H PRESS REGULATOR PER AMM 36-12-051-4. RAN ENG PER JRH AND LEAK CK OF HIGH PRESSURE REGULATOR IS GOOD. NO LEAKS NOTED. PERFORMED HI-PRESS BLEED CONT SYS CK. CK OK PER 727 JRH 8-17. CK'D STRUT O/H LOOPS. NO DEFECTS NOTED. TEST SYS RUN OK. 2 L 7 3 4F RT A3WE 2008020800154 20080208 00154 NM 2008 2 8 USAA920080297 1 20080107 A 5511 18315045 RIB BOEING 757 757225 1384959 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 MCN - MAJOR REPAIR - C11 CHECK - CORROSION ON RIGHT HAND HORIZONTAL STABILIZER UPPER RIB CHORD, STABILIZER STATION 341.6 49. REPLACED RIGHT HAND HORIZONTAL STABILIZER UPPER RIB CHORD, STABILIZER STATION 341.649 IAW BOEING DRAWING 183N1504. 2 L 7 2 4F RT A2NM 2008020800176 20080208 00176 WP 2008 2 8 AALA200800128 1 20080121 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9617R 53564 DFW - EMERGENCY EXIT MARKER AT TAIL COMPARTMENT LEFT SIDEWALL INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT MAR KER AT TAIL COMPARTMENT LEFT SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800179 20080208 00179 NM 2008 2 8 QXEA200800049 1 20080127 A 5210 HANDLE BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR LACK OF LUBE A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 431QX 4164 PDX - FLIGHT 2250 (RNO-SEA) - IN CRUISE FLIGHT RECEIVED A FORWARD BAGGAGE DOOR WARNING. DIVERTED TO PDX AND ACCOMPLISHE D A UNEVENTFUL LANDING. MAINTENANCE CLEANED AND LUBRICATED THE DOOR HANDLE SHAFT. OPERATIONAL CHECKS GOOD. AIRCRAFT R ETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008020800180 20080208 00180 NM 2008 2 8 QXEA200800050 1 20080127 A 4920 APU BOMBDR DHC8 DHC8402 1390042 NM SMOKE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 401QX 4031 PDX - FLIGHT 2496 - AT THE GATE BEFORE PUSHBACK, THE APU WAS STARTED, AND UPON SELECTING APU BLEED AIR THE CABIN FILLED WITH BLUE SMOKE. MAINTENANCE PLACED THE APU ON MEL 49-50-1. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008020800181 20080208 00181 NM 2008 2 8 QXEA200800051 1 20080129 A 3230 483003 SEQUENCE VALVE BOMBDR DHC8 DHC8402 1390042 NM MLG MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 419QX 2844 4145 SEA - FLIGHT 2429 - AFTER GEAR RETRACTION, THE NOSE GEAR DOOR LIGHT ILLUMINATED. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. FERRIED THE AIRCRAFT TO PDX FOR REPAIRS. REPLACED THE NOSE GEAR SOLENOID SEQUENCE VALVE. OPERA TIONAL AND TEST FLIGHT CHECK TESTS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008020800185 20080208 00185 NM 2008 2 8 NWAA080326730 1 20080201 A 3350 POWER SUPPLY BOEING 747 7472J9F 1384806 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING OVERNIGHT CHECK, FOUND CREW REST OVERHEAD EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008020800186 20080208 00186 NM 2008 2 8 NWAA080346730 1 20080202 A 3350 CHARGER BOEING 747 7472J9F 1384806 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING OVERNIGHT CHECK, FOUND UPPER DECK EMERGENCY SIGN AT RT DOOR INOP. MAINTENANCE REMOVED AND REPLACED BATTERY CHARG ER. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008020800188 20080208 00188 NM 2008 2 8 AALA200800178 1 20080126 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 668AA 25333 DFW - EMERGENCY LIGHT AT LEFT BULLNOSE AT SEAT ROW 12 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT BULLNOSE A T SEAT ROW 12. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020800189 20080208 00189 NM 2008 2 8 AALA200800170 1 20080125 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 370AA 25197 JFK - EMERGENCY LIGHT AT RIGHT SIDE AFT OF FORWARD GALLEY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT SIDE AFT OF FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008020800192 20080208 00192 2008 2 8 BA08002 4 20080129 A 3441 46502003030316 ADIRU AIRBUS 330 A330323 3930335 EU NR 1 FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 272AY 25764 4750 333 PHL FLT 754 PHL-CDG EN ROUTE CREW THE NUMBER 1 ADIRU BECAME INOP. DUE TO PROCEDURAL ISSUES FLIGHT RETURNED TO PHL. MA INTENANCE REPLACED NUMBER 1 ADIRU. 2 L 7 2 4F RT A46NM 2008020800199 20080208 00199 NM 2008 2 8 SWAA080557 1 20080130 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 27L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008020800205 20080208 00205 NM 2008 2 8 SWAA080577 1 20080131 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800206 20080208 00206 NM 2008 2 8 SWAA080578 1 20080131 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER 17R CRACKED AT BS 638. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008020800208 20080208 00208 NM 2008 2 8 SWAA080588 1 20080131 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008020800212 20080208 00212 NM 2008 2 8 SWAA080558 1 20080130 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 424, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800214 20080208 00214 NM 2008 2 8 SWAA080559 1 20080130 A 5330 65C38192 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 512D, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800218 20080208 00218 NM 2008 2 8 SWAA080580 1 20080131 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BEAR STRAP BS 790, RBL 19. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008020800220 20080208 00220 NM 2008 2 8 SWAA080564 1 20080130 A 5313 6551698 STRINGER SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2008020800221 20080208 00221 NM 2008 2 8 SWAA080576 1 20080131 A 5311 6545629 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800223 20080208 00223 2008 2 8 SWAA080566 4 20080130 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008020800227 20080208 00227 NM 2008 2 8 SWAA080581 1 20080131 A 5753 6546429 FLAP TRACK BOEING 737 7373L9 1384470 NM T/E FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 7 T/E AFT FLAP TRACK WORN. REMOVED AND REPLACED FLAP TRACK PER MM. 2 L 7 2 4F RT A16WE 2008020800228 20080208 00228 NM 2008 2 8 SWAA080570 1 20080131 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 910, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008020800230 20080208 00230 NM 2008 2 8 SWAA080582 1 20080131 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008020800234 20080208 00234 NM 2008 2 8 SWAA080575 1 20080131 A 5311 6546564 FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 986.5, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008020800236 20080208 00236 NM 2008 2 8 HNAA0800052 1 20080127 A 6123 V319 SWITCH DHAV DHC8 DHC8102 2809003 NM AUTOFEATHER SYS FAILED A HNAA O OTHER O OTHER TO TAKEOFF 1 EA 07 906HA 59026 59026 9 AS THE POWER LEVERS WERE BEING ADVANCED TO START THE TAKEOFF ROLL, THE AUTOFEATHER SYSTEM DID NOT ACTIVATE AND THE NR 2 ENGINE TORQUE INDICATION WENT TO 105% FOR AT 3 SECONDS. MAINTENANCE PERFORMED THE BETA LOCKOUT GROUND LOGIC OPS CHECK W ORKCARD. MICRO SWITCH 6121-S10 AND WIRES 6121-16D22 & 6121-17A22 RUNNING FROM THE -S10 SWITCH TO CONNECTOR 9811-P38 WER E REPLACED. GROUND CHECKS WERE GOOD AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 2008020800239 20080208 00239 NM 2008 2 8 AALA200800171 1 20080125 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 361AA 24042 DFW - EMERGENCY LIGHT AT LEFT AFT OVERWING EXIT INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT LEFT AFT OVERWING EX IT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008020800240 20080208 00240 WP 2008 2 8 AALA200800163 1 20080124 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70401 49312 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROW 13 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROW 13. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020800242 20080208 00242 2008 2 8 SWAA080589 4 20080202 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 263WN 32520 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008020800246 20080208 00246 NM 2008 2 8 DL764080118 1 20080125 A 2822 PUMP BOEING 767 767432ER 1385134 NM FUEL SYSTEM MALFUNCTIONED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 828MH 29699 LT AFT FUEL PUMP LIGHT AND MSG ON AFTER PUSHBACK. PER DISPATCHER NEEDED MORE FUEL IN ORDER TO DISPATCH WITH MEL APPLIED . RETURNED TO BLOCK FOR FUEL. MX PLACED PUMP ON MCO PER MEL 28-22-01A. SECURED C/B. 2 L 7 2 4F RT A1NM 2008020800249 20080208 00249 NM 2008 2 8 DL76P080119 1 20080125 A 2161 6249584 CONTROLLER BOEING 767 767332 1382001 NM TEMP FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 140LL 48C0187 25988 ON TAXI OUT FLT DECK TEMP, AFT CABIN TEMP, MID CABIN TEMP, FWD CABIN TEMP CAUTION MSG ILLUMINATED. REPLACED ZONE TEMP CONTROLLER PER M/M. OPS CHK NORMAL. ACFT RTB. 2 L 7 2 4F RT A1NM 2008020800251 20080208 00251 2008 2 8 DL76L080120 4 20080126 A 3445 066500002120 PROCESSOR BOEING 767 767332 1382001 NM TCAS INOPERATIVE A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 175DN 3663 24803 TCAS INOP. REPLACED TCAS PROCESSOR. OPS CK GOOD. CK CB ALL OK. 2 L 7 2 4F RT A1NM 2008020800252 20080208 00252 NM 2008 2 8 SWAA080613 1 20080203 A 5310 6546956 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 400 AND BS 420, STR 17L. REMOVED AND REPLACED WE B PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800254 20080208 00254 NM 2008 2 8 SWAA080614 1 20080203 A 5310 6549921 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 360 AND BS 400, STR 17R. REMOVED AND REPLACED WE B PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800255 20080208 00255 NM 2008 2 8 SWAA080615 1 20080203 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 1006, STR 24L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020800256 20080208 00256 NM 2008 2 8 SWAA080594 1 20080203 A 5753 6546435277 FLAP BOEING 737 7373K2 13844BA NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED MV2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED AFT F LAP PER MM. 2 L 7 2 4F RT A16WE 2008020800257 20080208 00257 GL 2008 2 8 DL764080123 2 20080127 A 7310 FILTER BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 2 ENGINE DIRTY A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 845MH 29719 706181 RETURN TO GATE AFTER ENGINE START. EICAS MSG RT ENG FUEL FILTER. REPLACED RT ENG FUEL FILTER ELEMENT AS PER AMM 73-11- 02-004 AND AMM 73-11-02-404 CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E23EA 2008020800259 20080208 00259 NE 2008 2 8 DL76L080124 2 20080127 A 7250 TURBINE BLADES BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 194DN 68738 28451 724178 DURING NR 2 ENGINE OP 5067 BORO, FOUND 1 TURBINE BLADE MISSING. REPLACING ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020800266 20080208 00266 WP 2008 2 8 DHL2007873521 1 20080120 A 5751 BRACKET DOUG DC8 DC873F 302199F WP AILERONS BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 RT AIL BRACKET ASSY BROKEN (MAJOR REPAIR) INBD AIL. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED BROKEN FITTING IAW SRM 57-1-0 PG 1 SRM 51-1-21 SRM 51-1-20D. CLEANED, TREATED, PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IA W SRM 51-1-21 SRM 51-3-0 SRM 51-1-20D SRM 51-3-1 BALANCE IAW SRM 51-4-1 PG 1-5. REMOVED WEIGHTS AT STA 546.000, FOUND W ITHIN TOLERANCE. 2 L 7 4 4F RT 4A25 2008020800270 20080208 00270 WP 2008 2 8 DHL2007873523 1 20080115 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 RT OUTBD FLAP UPPER SKIN WORN AT STA XF 210.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-14- 08 EVA NR 0857-00032 REV IR DATED 01-05-08 SEMAN DWG ED-4680 DATED 01-02-08. REMOVED DAMAGE SKIN SEGMENT IAW SRM 51-1-2 1. FABRICATED NEW SKIN SEGMENT (AL2024-T30.040") AND SPLICE STRAP (AL 2024T30.050') IAW SMN DWG N ED-4680. PERFORMED N DT INSPECTED OF EXISTING CUT OUT AREA AND REPAIR PART NO CRACK NO CORROSION, FOUND IAW DPS 4.707-1 NDT SRM PART 08. CLE ANED, TREATED, PRIMED AREA AND INNER FACE OF NEW SKIN SEGMENT AND SPLICE STRAP IAW SRM 51-1-8B. INSTALLED NEW SKIN SEGM ENT IAW SRM51-1-11 SRM 51-1-21. 2 L 7 4 4F RT 4A25 2008020800274 20080208 00274 NM 2008 2 8 SWAA080621 1 20080203 A 5310 6545833 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 178, STR 17L. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2008020800275 20080208 00275 NM 2008 2 8 SWAA080622 1 20080203 A 5310 6545833 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 178, STR 17R. REMOVED AND REPLACED CREASE BEAM WEB PER SRM. 2 L 7 2 4F RT A16WE 2008020800280 20080208 00280 NM 2008 2 8 SWAA080603 1 20080201 A 5753 6546435 FLAP BOEING 737 7373A4 1384585 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2008020800281 20080208 00281 NM 2008 2 8 SWAA080604 1 20080202 A 3350 311500 LENS BOEING 737 7373Y0 1384671 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008020800282 20080208 00282 NM 2008 2 8 08FDEA00346 1 20080205 A 5313 ADA84291 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 MAIN DECK, LONGERON SPLICE FITTING AT STA 6-5, L24R FOUND CRACK NEAR FASTENER. REMOVED AS PER SRM 51-31-01 VOLUME II. N EW SPLICE FABRICATED AS PER DRAWING ADA8429 AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008020800285 20080208 00285 NM 2008 2 8 08FDEA00348 1 20080205 A 5740 ARC40092 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 HFEC OPEN HOLE INSPECTION CARRIED OUT AND FOUND 01 EACH HOLE WITH CRACK INDICATION AT RIGHT WING OUTBOARD FLAP, AFT SI DE OF FLAP HINGE SUPPORT FITTING. RT OUTBOARD FLAP ASSY REMOVED AND REPLACED AS PER AMM 27-50-30-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-830-805. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008020700121 20080207 00121 NM 2008 2 7 2008UALA00341 1 20080120 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 2F BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 EMERGENCY LIGHTING STRIP BROKEN ON SEAT 2F. REPLACED LIGHT STRIP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008020700144 20080207 00144 NM 2008 2 7 SWAA080523 1 20080129 A 5310 6545834 CREASE BEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM CHORD CORRODED BETWEEN BS 270 AND BS 360, STR 17R. REMOVED AND REPLACED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2008020700175 20080207 00175 NM 2008 2 7 SWAA080551 1 20080130 A 5311 6545808 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 291, STR 16R. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008020700194 20080207 00194 EA 2008 2 7 TRAX200800154 1 20080130 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 759EV 10211 OVERWING EMERGENCY EXIT SIGN "FORWARD FACING" NOT LIGHTING WHEN EMERGENCY LIGHTS TURNED ON. FLT 4302 CX. 2 L 7 2 4F RT A21EA 2008020800009 20080208 00009 NM 2008 2 8 08FDEA00333 1 20080130 A 5330 65175303 SKIN BOEING 727 727233 138408A NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 AFT LOWER EXTERIOR FUSELAGE, SKIN CREASED WITH SMALL GOUGE, STA 1183 5", 2" BELOW STR 20L. REMOVED DAMAGE AREA OF SKIN. HFEC CUTOUT, NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER AND FILLER, ALODINED AND PRIMED AND INSTALLED REPAIR, REF SR M 53-30-3 FIG 28 REF EA NR 7-5330-118238. THIS IS A CATEGORY "C" REPAIR AND INSPECTION THRESHOLD OF 3000 CYC REF TABLE 3 OF SRM 53-30-3 PG 175. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 2008020800019 20080208 00019 NM 2008 2 8 DL764080135 1 20080128 A 2530 250007390 OVEN BOEING 767 767432ER 1385134 NM GALLEY OVERHEATED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 842MH 29715 FIRST GLASS OVEN CB POPPED AND ELECTRICAL SMELL. REPLACED NR 2 OVEN. CKS GOOD. REMOVED MCO AND PLACARD. 2 L 7 2 4F RT A1NM 2008020800020 20080208 00020 NE 2008 2 8 DL76L080136 2 20080129 A 7250 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 194DN 68738 28451 724178 NR 2 ENGINE S/N 724178 FAILED BORO INSP OPN 5067. FOUND 2ND STAGE TURBINE BLADE MISSING AND DAMAGED AND OUT OF LIMITS. NR 2 ENGINE CHANGE REQUIRED. AP-10 BOROSCOPE PLUG NOT INSTALLED. REMOVED AND REPLACED NR 2 ENG PER TRANS 1T149. 2 L 7 2 4F 4 F RT A1NM E24NE 2008020800039 20080208 00039 NM 2008 2 8 DL76S080131 1 20080128 A 3246 162T1621 WASHER BOEING 767 767332 1382001 NM NLG WHEEL MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 131DN 24852 FOUND RT NLG WHEEL AXLE ASSY MISSING AXLE WASHER. REMOVED RT NLG WHEEL ASSY VISUALLY INSP AXLE AND WHEEL ASSY BEARING. NO DAMAGE NOTED. REINSTALLED WHEEL ASSY AND AXLE WASHER PER AMM. 2 L 7 2 4F RT A1NM 2008020800078 20080208 00078 SO 2008 2 8 FDKA200802050 1 20080204 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6088 MCO-RDU (0949 PHX LCL) - EMERGENCY EXIT ROW EXIT SIGN INOP. MX PERFORMED, OPS CHECKS. NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008020800121 20080208 00121 NM 2008 2 8 08FDEA00341 1 20080201 A 5210 SUPPORT BOEING 727 727232 1384082 NM PAX DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 FORWARD ENTRY DOOR LOWER AND UPPER AFT LATCH TORQUE TUBE SUPPORT CASTING HAS PARTIALLY DETACHED FROM DOOR FRAME AND FRAM E IS CRACKED ON BOTH UPPER AND LOWER ATTACH POINTS. REMOVED AND REPLACED L1 FORWARD ENTRY DOOR PER 727-200 MM 52-11-001 -4/ADJUSTMENT TEST GOOD PER 727-200MM 52-11-001-5. PREMATURE REMOVAL/INSTALLATION. 2 L 7 3 4F A3WE 2008020800122 20080208 00122 EU 2008 2 8 TRBA2008011 1 20080127 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 377AT 377 MULTIPLE EMERGENCY LIGHTS ON ERRONEOUSLY. REPLACED EMERGENCY LIGHTS POWER SUPPLY 61WL AS PER 33-51-21 AND FOUND WORKING PROPERLY. 2 H 7 2 4T RT A53EU 2008020800136 20080208 00136 WP 2008 2 8 AALA200800083 1 20080117 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 402A 49313 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 22 TO 24 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHE AD SEAT ROWS 22 TO 24. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020800142 20080208 00142 NM 2008 2 8 USAA920080286 1 20080113 A 5347 SEAT TRACK BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 1428 - BS 1479, RBL 88, WL 200. REPLACED CABI N SEAT TRACK, BS 1428 - BS 1479, RBL 88, WL 200 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008020800155 20080208 00155 NM 2008 2 8 ASAA0852506 1 20080128 A 2161 3989083 MODULATING VALVE BOEING 737 737890 1384527 NM CABIN TEMP FAULTY A ASAA K NONE J WARNING INDICATION NR NOT REPORTED 1 NM 02 570AS 35185 THE "ZONE TEMP" LIGHT ILLUMINATED ON RECALL EXTINGUISHED ON MASTER CAUTION RESET. REPLACED TRIM AIR MOD VALVE IAW 21 61 21. OPS NORMAL, NO LIGHTS ON RECALL. 2 L 7 2 4F RT A16WE 2008020800173 20080208 00173 NM 2008 2 8 USAA920080299 1 20080129 A 3260 189929 UPLOCK SENSOR BOEING 737 7373G7 1384595 NM RT MLG OUT OF ADJUST A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 302AW 24009 PHX - DEN - ATB - FLT 490 - DURING CLIMB CREW SELECTED GEAR UP. RED RIGHT MAIN LANDING GEAR LIGHT REMAINED ILLUMINATED. PER QRH CREW SELECTED GEAR DOWN. THREE GREEN GEAR DOWN LIGHTS ILLUMINATED. CREW DECLARED AN EMERGENCY AND CABIN WAS PREPPED. THE CREW RETURNED TO PHX. THE LANDING WAS UNEVENTFUL AND THE A/C TAXIED TO THE GATE. MX DISCOVERED THE RIGHT MLG UPLOCK SENSOR WAS OUT OF ADJUSTMENT. MX ADJUSTED SENSOR. OPERATIONAL CHECK WAS GOOD. THE A/C WAS RETURNED TO SER VICE. 2 L 7 2 4F RT A16WE 2008021400069 20080214 00069 WP 2008 2 14 UPS08851650 1 20080109 A 5312 5640918501 STIFFENER DOUG DC8 DC871F 302199D WP BS 980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 AREA OF CORROSION AND POSSIBLE CRACK ON AFT SIDE OF STA 980 BULKHEAD AT LT STIFFENER, BOTTOM C-PIT. REMOVED CORROSION AT 980 BULKHEAD LT VERTICAL STIFFENER. REMOVED STIFFENER AT 980 BULKHEAD. DRILLED UP REPLACEMENT STI FFENER AND INSTALLED AT 98 0 BULKHEAD IAW SRM 51-1-24,51-1-8,51-1-20D. 2 L 7 4 4F RT 4A25 2008021400070 20080214 00070 WP 2008 2 14 UPS08851651 1 20080129 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 980 L36 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 POSSIBLE CRACK ON STA 980 FRAME IN C-PIT AT L36. REMOVED CRACKED L ANGLE AT STA 980, DRILLED UP NEW L ANGLE AND INSTALLED AT STA 980 AT L36. 2 L 7 4 4F RT 4A25 2008021400086 20080214 00086 EU 2008 2 14 08FDEA00386 1 20080122 A 5347 A5327478621200 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 MDCC - SEAT TRACK Y-1970 BETWEEN FR60 AND FR61 FOUND CRACKED. THE ATA CHAPTER FOR THIS SDR IS IN FACT 5310, INSTEAD OF THE 5611 INSERTED ABOVE. THE SEAT TRACK WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2008021400090 20080214 00090 EA 2008 2 14 TRAX200800222 1 20080203 A 5242 HANDLE CNDAIR CL600 CL6002C10 1390015 EA E/E DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 AVIONICS COMPT DOOR HANDLE CRACKED. REMOVED AND REPLACED HANDLE ASSY IAW MM 52-42-02-000-801 AND SRM 51-42-20. 2 L 7 2 4F RT A21EA 2008021400091 20080214 00091 EA 2008 2 14 TRAX200800223 1 20080207 A 5220 DOOR CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 RT OVERWING EMERG EXIT DOOR FAILED FUNCTIONAL CK PER 52-840-100. 2 L 7 2 4F RT A21EA 2008021400093 20080214 00093 NM 2008 2 14 QXEA200800064 1 20080114 A 5320 SUPPORT ANGLE DHAV DHC8 DHC8202 2809007 NM THRESHOLD CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C CHECK - SUPPORT ANGLE AT APPROXIMATELY STA X553.00 AT DOOR THRESHOLD HAS CORROSSION ON NUTPLATES AND MOUNTING SU RFACE. REMOVED NUTPLATES AND REMOVED CORROSION, INSPECTED BLEND WITHIN LIMITS NO CRACKS FOUND. ALODINED PRIMED AND PAI NTED INSTALLED NUTPLATES. 2 H 7 2 4T RT A13NM 2008021400095 20080214 00095 NM 2008 2 14 QXEA200800066 1 20080114 A 5320 SUPPORT ANGLE DHAV DHC8 DHC8202 2809007 NM THRESHOLD CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C CHECK - SUPPORT ANGLE AT APPROX X586.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFACE. MAINTENANCE REMOVED NUTPLATES AND REMOVED CORROSION, INSPECTED BLEND, WITHIN LIMITS. ALODINED, PRIMED AND PAINTED. IN STALLED NEW NUTPLATES. 2 H 7 2 4T RT A13NM 2008021400098 20080214 00098 NM 2008 2 14 QXEA200800069 1 20080114 A 5340 NUT PLATE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - NUTPLATE AND MOUNTING SURFACE AT STA X599.00 Y21.00 LT IS CORRODED. MAINTENANCE REMOVED NUTPLATE AND R EMOVED CORROSION. INSPECTED BLENDED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE, PRIMER, AND PAINT. INS TALLED NEW NUTPLATE. 2 H 7 2 4T RT A13NM 2008021400102 20080214 00102 NM 2008 2 14 QXEA200800075 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS A SMALL AREA OF CORROSION AT APPROX X364. MAINTENANCE REMOVED CORR OSION, INSPECTED BLENDED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO BLENDED AREA. 2 H 7 2 4T RT A13NM 2008021400103 20080214 00103 NM 2008 2 14 QXEA200800076 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - TOP OF RIGHT OUTBOARD SEAT TRACK NR 10 IS CHAFED AT APPROX X362. MAINTENANCE BLENDED CHAFED AREA, WITH IN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMED AREA. 2 H 7 2 4T RT A13NM 2008021400109 20080214 00109 EU 2008 2 14 TRBA2008020 1 20080210 A 3350 GE44 LIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 548AT 548 THE EMERGENCY LIGHT ON THE AIRSTAIRS IS INTERMITTENT. RELAMPED AIRSTAIR LIGHT AND OPT CHECK IAW 33-50-00. 2 H 7 2 4T RT A53EU 2008021400113 20080214 00113 NM 2008 2 14 ABXA080045 1 20080107 A 5330 148T31212 SKIN BOEING 767 767232 1385132 NM BS 1654 S5-6R CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 740AX 22213 FUSELAGE SKIN CRACKED FS 1654.5 BETWEEN STRINGER 5 AND 6 RIGHT. REPAIRED CRACKED AREA IAW B767 SRM 53-80-01, FIGURE 201 . 2 L 7 2 4F RT A1NM 2008021400116 20080214 00116 NM 2008 2 14 ABXA080053 1 20080123 A 5730 114T13105 SKIN BOEING 767 767232 1385132 NM LEFT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 740AX 22213 LEFT WING LEADING EDGE STRUCTURE HAD A BROKEN FASTENER AND TWO CRACKED MEMBERS AT LEADING EDGE SLAT 160. INSTALLED NEW SKIN IAW B767 SRM 51-40-01. 2 L 7 2 4F RT A1NM 2008021400117 20080214 00117 NM 2008 2 14 ABXA080054 1 20080208 A 7933 BULB BOEING 767 767231 1385131 NM OIL TEMP MALFUNCTIONED A ABXA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 23 708AX 22571 708AX MADE A DIVERSION TO STA - PHX, NR 2 ENGINE SHUT DOWN DURING CRUISE DUE TO HIGH OIL TEMP, HIGHEST NOTED TEMP 173 DE GREES. ALL OTHER INDICATION APPEARED NORMAL. REPLACED RIGHT ENGINE OIL TEMP BULB IAW ABX B767 MM 79-34-00-4. TEMP SEPERA TION REMAINED CONSTANT THROUGHOUT RISE. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2008021400122 20080214 00122 NM 2008 2 14 QXEA200800080 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 IS CORRODED ON THE FRONT OUTBOARD CORNER AT APPROX X262. MAINTENANCE B LENDED OUT CORRODED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021400124 20080214 00124 NM 2008 2 14 QXEA200800091 1 20080114 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - X534 AND STRINGER 31R SUSPECT CORROSION AT SKIN CLIP. MAINTENANCE REMOVED RIVETS AND BLENDED OUT CORRO SION AT CLIP, REMAINED WITHIN LIMITS AND INSPECTED, NO CRACKS NOTED. INSTALLED NEW RIVETS AND RESTORED FINISH TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008020800187 20080208 00187 WP 2008 2 8 AALA200800168 1 20080125 A 3350 LAMP DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 963TW 53613 LGA - EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800204 20080208 00204 NM 2008 2 8 SWAA080556 1 20080130 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, LBL 7 TO LBL 13. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020800244 20080208 00244 NM 2008 2 8 SWAA080592 1 20080202 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EXTERIOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008020800263 20080208 00263 NM 2008 2 8 AALA200800146 1 20080123 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 630AA 24588 MIA - EMERGENCY LIGHT AT SEAT 9D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 2008020800265 20080208 00265 NM 2008 2 8 SWAA080616 1 20080201 A 2121 215201 GASPER FAN BOEING 737 7377H4 1384404 NM E&E BAY FAULTY A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 407WN 29817 DIVERSION - ACRID ODOR REPORTED IN CABIN WITH GASPER FAN ON. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2008020800283 20080208 00283 WP 2008 2 8 08FDEA00347 1 20080205 A 3210 862701 UPLOCK SENSOR DOUG MD10 MD1010F 3022112 WP LT MLG MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 566FE 46989 AFTER LEVEL OFF, THE LT MAIN GEAR LIGHT INDICATED RED. AS A PRECAUTIONARY MEASURE, SLOWED TO 230KTS FOR REMAINDER OF FL IGHT. DID ATTEMPT ONE RECYCLE OF GEAR HANDLE WHICH DID NOT CHANGE STATUS WITH GEAR HANDLE UP. STATUS PAGE SHOWED "PSE U FAULT". REMOVED LT MLG PROX UP AND LATCHED SENSOR B (D1-81) PER MD10 AMM 32-61-15-4. 2 L 7 3 4F RT A22WE 2008020800286 20080208 00286 NM 2008 2 8 SWAA080605 1 20080202 A 3350 1619 LIGHT BOEING 737 7373G7 1384595 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED MV2 CHECK, FOUND RIGHT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BUL B PER MM. 2 L 7 2 4F RT A16WE 2008020800287 20080208 00287 EU 2008 2 8 08FDEA00349 1 20080205 A 5340 A53773644 FITTING AIRBUS 330 A300* EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CORRODED CORNER FITTINGS AT C27 LT AND RT, CARGO FLOOR STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF CORNER FITTI NGS IAW SRM 51-72-10. 2 L 7 2 4F RT A26NM 2008020800290 20080208 00290 WP 2008 2 8 08FDEA00350 1 20080205 A 5753 ARC19591 SKIN DOUG DC10 DC1030F 3023504 WP TE FLAPS CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 LT WING INBOARD FLAP ON UPPER SKIN FOUND SCRATCH. 2 L 7 3 4F RT A22WE 2008020800293 20080208 00293 NM 2008 2 8 SWAA080623 1 20080203 A 5322 6546546 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020800296 20080208 00296 WP 2008 2 8 AALA200800131 1 20080121 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9617R 53564 DFW - EMERGENCY EXIT MARKER AT AFT DOOR NEAR FLOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT MARKER AT AFT DOOR NEAR FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800298 20080208 00298 WP 2008 2 8 AALA200800137 1 20080123 A 2150 A/C PACK DOUG DC9 DC982 3022082 WP SMOKE A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 490AA 49683 MSP INFLIGHT T1037/23JAN - VERY LIGHT SMOKE STARTED TO FLOW THROUGH CABIN. SHUT DOWN RIGHT AIR CONDITIONING PACK AND SM OKE DISSIPATED. CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL OP ERATION. 2 L 7 2 4F A6WE 2008020800304 20080208 00304 EA 2008 2 8 COMA0860102 1 20080129 A 5610 NP1393225 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 797CA 21398 7344 FLIGHT 5104 - COCKPIT LEFT SIDE WINDOW CRACKED AT CRUISE. RECEIVED WINDOW HEAT CAUTION MESSAGES. DECLARED EMERGENCY, D IVERTED TO ACY, LANDED WITHOUT INCIDENT. REPLACED COCKPIT LEFT SIDE WINDOW. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008020800305 20080208 00305 WP 2008 2 8 AALA200800139 1 20080123 A 8012 START VALVE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RT ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 9677W 53627 718537 SLC INFLIGHT T2036/23JAN - AT ROTATION RIGHT START VALVE OPEN LIGHT ILLUMINATED AND FIRE BELL SOUNDED FOR ABOUT 2 TO 3 S ECONDS THEN EXTINGUISHED. THE RIGHT START VALVE OPEN LIGHT ALSO EXTINGUISHED. RETURNED TO SLC AND LANDED WITHOUT INCID ENT. INSPECTED ENGINE AND FOUND START VALVE FAILED AND CAUSED DAMAGE TO BYPASS DUCT AND OTHER HARDWARE. REPLACED NUMBE R TWO ENGINE ON 25 JAN 2008 AT SLC. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A6WE E9NE 2008020800308 20080208 00308 NM 2008 2 8 AALA200800116 1 20080120 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AM 24487 DFW - EMERGENCY LIGHT AT SEAT 33D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 33D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008021400133 20080214 00133 NM 2008 2 14 QXEA200800101 1 20080114 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAPS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - RIGHT OUTBOARD FLAP NR 4 FLAP TRACK LOWER SIDE THERE ARE TWO AREAS OF ROLLER CHAFE DAMAGE WITH PITTING CORROSION IN BETWEEN. MAINTENANCE BLENDED OUT CHAFE AND PITTING CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRA CKS NOTED. 2 H 7 2 4T RT A13NM 2008021400134 20080214 00134 NM 2008 2 14 QXEA200800106 1 20080114 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM PAX DOORWAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - MAIN CABIN DOOR THRESHOLD HAS LIGHT CORROSION AT 5 EA NUTPLATES. MAINTENANCE REMOVED MCD THRESHOLD AND NUTPLATES. REMOVED LIGHT SURFACE CORROSION FROM LOWER SILL PLATE AND INSPECTED, BLENDED AREA REMAINED WITHIN LIMITS WI TH NO CRACKS NOTED. INSTALLED NEW NUTPLATES. 2 H 7 2 4T RT A13NM 2008021400147 20080214 00147 EU 2008 2 14 08FDEA00391 1 20080212 A 5313 A53611674202 STRINGER SPLICE AIRBUS 330 A300* EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 STRINGER COUPLING C 19, P46 AND 48 LT CORRODED REPAIR PERFORMED BY REPLACING OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A26NM 2008021400153 20080214 00153 EU 2008 2 14 08FDEA00398 1 20080212 A 5315 A53970197200 FLOORBEAM AIRBUS 330 A300* EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION ON TOP CAP BEAM C 57.2, Y 480 SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A26NM 2008021400154 20080214 00154 EU 2008 2 14 08FDEA00399 1 20080212 A 5313 A53974202408 STRINGER AIRBUS 330 A300* EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION ON STRINGER P 54 LT, C 61-64 REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A26NM 2008021400156 20080214 00156 EU 2008 2 14 08FDEA00401 1 20080212 A 5315 A53970197220 FLOORBEAM AIRBUS 330 A300* EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION AT TOP CAP BEAM, C57, Y-450. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A26NM 2008021400159 20080214 00159 EU 2008 2 14 08FDEA00404 1 20080212 A 5313 A53978149224 STRINGER AIRBUS 330 A300* EU ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND DEEP SCRATCH AT STRINGER 38 LT, C58-59. SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A26NM 2008021400161 20080214 00161 EU 2008 2 14 08FDEA00406 1 20080212 A 5320 A53970875201 PLATE AIRBUS 330 A300* EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 SCRUB MARKS AT RT EMERGENCY EXIT COVER PLATE. REPAIR PERFORMED BY REWORK OF DAMAGE, NDT FOR CRACK FREE CONDITION, FLAP PEENING IAW RAS/EFW/9000009/2007 ISS A, APPROVED BY EA 6-5316-114863. 2 L 7 2 4F RT A26NM 2008021400164 20080214 00164 NM 2008 2 14 08FDEA00409 1 20080212 A 5330 65545777 SKIN BOEING 727 727233 138408A NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 LWR FUSELAGE EXTERIOR SKIN SURFACE SHOWS CORROSION AT BOTTOM SIDE AT STA. 685, S27-28L. REMOVED INTERCOSTAL IAW SRM 51 -30-2. CUT OUT DAMAGED AREA IAW SRM 53-10-3 FIG 3A AND 53-30-3 FIG1. FABRICATED DOUBLER AND FILLER IAW SRM 53-10-3 FIG1 AND 53-10-3 FIG3A. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS AND INTERCOSTAL IAW SRM 51-30-2 2 L 7 3 4F RT A3WE 2008021400167 20080214 00167 EU 2008 2 14 TRAX200800225 1 20080129 A 5720 BRACKET AEROSP ATR72 ATR72212 8680945 EU RT WING BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 RT WING RIB 13 INBOARD AND OUTBOARD FLAP ARM OMEGA BRACKET BROKEN (X3). 2 H 7 2 4T RT A53EU 2008021400169 20080214 00169 EA 2008 2 14 TRAX200800227 1 20080201 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 680BR 7679 AAR - 8010 - PAX DOOR OUTER HANDLE IS CRACKED. 2 L 7 2 4F RT A21EA 2008021400173 20080214 00173 NM 2008 2 14 NWAA080446308 1 20080130 A 5311 FAILSAFE BOEING 747 747451 1384940 NM BS 1140 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 668US 24223 DURING "M" CHECK, FOUND FAIL/SAFE CHORD FASTENER HOLES CRACKED AND WITH SHORT EDGE MARGIN AT BS 1140 RT AND LT. REPAIRE D PER EA 63-211705. 2 L 7 4 4F RT A20WE 2008021400174 20080214 00174 NM 2008 2 14 KCSA081075 1 20080213 A 5310 DOOR FRAME BOEING 747 747209B 138489B NM BS 445 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 NR 1R MAIN ENTRY DOOR LOWER HORIZ FRAME CRACKED AT FWD CORNER. 2 L 7 4 4F RT A20WE 2008021400180 20080214 00180 EA 2008 2 14 MASA200800107 1 20080205 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 931LR 10349 15031 ASH FLT 2916 TUS-PHX 4 EMERGENCY EXIT SIGNS IN GALLEY INOP. REMOVED AND REPLACED NR 1 BATTERY PACK, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008021400182 20080214 00182 NM 2008 2 14 CALA0800094 1 20080129 A 5311 BAC15171470 FRAME BOEING 737 7373T0 1384582 NM BS 847 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FUSELAGE FRAME CRACKED AT STA 847 BETWEEN STRINGER 8L AND 9L. REPAIR PER ECRA 5310-04697. 2 L 7 2 4F RT A16WE 2008021400187 20080214 00187 EA 2008 2 14 MASA200800114 1 20080210 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 509MJ 10094 ASH FLT 7357 MCI - 3RD EMERGENCY CEILING FLOOD LIGHT INOP. RELAMPED, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008021400190 20080214 00190 WP 2008 2 14 G60A200800006 1 20080207 A 5320 PULLEY BRACKET DOUG DC10 DC1030F 3023504 WP BS 1381 CORRODED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 606GC 47929 FOUND CORROSION CENTER FUEL TANK AFT SIDE FUEL VALVE PULLEY BRACKET. 2 L 7 3 4F RT A22WE 2008021400191 20080214 00191 WP 2008 2 14 G60A200800015 1 20080207 A 5414 SKIN DOUG DC10 DC1030F 3023504 WP NR 2 PYLON CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 606GC 47929 NR 2 PYL PANEL 437HL HAS CRACKS. 2 L 7 3 4F RT A22WE 2008021500002 20080215 00002 NM 2008 2 15 2008UALA00588 1 20080131 A 3510 MXP147 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 511UA 24799 CREW REPORT: CAPT OXYGEN MASK MIC INOPERATIVE. FOUND ELECTRICAL SHORT IN WIRING IN CAPT O2 MASK MIC. REPLACED CAPT O 2 MASK AND MIC ASSY. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200229 20080212 00229 NM 2008 2 12 USAA920080338 1 20080203 A 5210 5079454 WEB BOEING 737 7373Y0 1384671 NM L2 DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - CRACKED L2 DOOR INNER WEB, BS 342 AT THE NR 6 AFT STOP. REPAIRED THE L2 DOOR INNER WEB , BS 342, AT THE NR 6 AFT STOP IAW USAIRWAYS EA 100225. 2 L 7 2 4F RT A16WE 2008021200233 20080212 00233 WP 2008 2 12 UPS08851619 1 20080111 A 5540 STIFFENER DOUG DC8 DC871F 302199D WP RUDDER BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 STIFFENER BROKEN ON RUDDER LOWER SIDE. RUDDER REPLACED ON N/R 123801. 2 L 7 4 4F RT 4A25 2008021200234 20080212 00234 WP 2008 2 12 UPS08851620 1 20080110 A 5542 SKIN DOUG DC8 DC871F 302199D WP RUDDER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 POPPED FASTENER HEADS AND HEAVY CORROSION ON LT RUDDER SKIN FWD OF TAB. RUDDER REPLACED ON N/R 12380 1. 2 L 7 4 4F RT 4A25 2008021200235 20080212 00235 WP 2008 2 12 UPS08851621 1 20080110 A 5540 WEB DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 LARGE CRACK ON LOWER WEB OF RUDDER. RUDDER REPLACED ON N/R 123737. 2 L 7 4 4F RT 4A25 2008021200274 20080212 00274 NM 2008 2 12 2008UALA00525 1 20080129 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 665UA 29237 SEAT 31B EEL INOP. REPLACED LIGHT STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021300058 20080213 00058 NM 2008 2 13 USAA920080348 1 20080125 A 5542 SKIN BOEING 737 7373S3 1384711 NM RUDDER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK NR 6038691, DELAMINATION ON THE RIGHT SIDE OF RUDDER, RS 220 - RS 232. REPAIRED RIGHT SI DE OF RUDDER, RS 220 - RS 232 IAW B737 SRM 51-70-07. 2 L 7 2 4F RT A16WE 2008021300060 20080213 00060 NM 2008 2 13 USAA920080350 1 20080111 A 5330 6545775594 SKIN BOEING 737 7373S3 1384711 NM BS 727E S25R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - NR 6040935, CRACKED FUSELAGE SKIN, BS 727E, S25R. REPAIRED FUSELAGE SKIN, BS 727E, S25 R IAW B737 SRM 53-00-01. 2 L 7 2 4F RT A16WE 2008021300061 20080213 00061 NM 2008 2 13 USAA920080351 1 20080203 A 5522 SKIN BOEING 737 7373S3 1384711 NM RT ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - NR 6033495, RIGHT ELEVATOR UPPER SURFACE HAS AREA OF DELAMINATION, ELEVATOR STATION 84. 9 - 93.9. REPAIRED RIGHT ELEVATOR UPPER SURFACE, ELEVATOR STATION 84.9 - 93.9 IAW B737 SRM 51-70-04. 2 L 7 2 4F RT A16WE 2008021300071 20080213 00071 2008 2 13 C8GA20080004 4 20080131 A 8300 HELICOIL BOEING 727 727225 1384077 NM GEARBOX MISSING A C8GA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 29 801EA 22432 FLT 716 FROM MEM TO HRL, ON DESCENT INTO HRL THE 1 ENGINE LOW OIL PSI LIGHT ILLUMINATED FOLLOWED BY A LOSS OF OIL QUALIT Y. THE NR 1 ENGINE WAS SHUT DOWN AND LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED A MISSING HELI COIL ON T HE GEARBOX. REMOVED AND REPLACED NR 1 ENGINE MAIN ACCY GEARBOX. OPS AND LEAK CHECK GOOD, NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2008021300078 20080213 00078 NE 2008 2 13 TRBA2008018 2 20080206 A 7200 ENGINE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE LEFT DAMAGED A TRBA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 29 417AT 417 127133 LT ENG ITT ROSE TO 800C DURING CLIMB, SMOKE IN THE COCKPIT AND PAX CABIN, CAPT SHUTDOWN ENGINE AS A PRECAUTIONARY PROCED URE. REMOVED AND REPLACED LT ENGINE AS PER WC 0500-CS-20000-001 R1. 2 H 7 2 4T 4 T RT A53EU E20NE 2008021300081 20080213 00081 EU 2008 2 13 08FDEA00365 1 20080207 A 5347 A53275018206 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 681FE 799 SEAT TRACK AT FR 57.1, 2 LT HAS 2 EA SCALLOPS WORN REMOVED DAMAGED SEAT TRACK SECTION AND INSTALLED SEAT TRACK REPAIR IA W A300-600 SRM 53-10-16, FIG 201. 2 L 7 2 4F RT A35EU 2008021300097 20080213 00097 NM 2008 2 13 USAA920080367 1 20080125 A 5754 SKIN BOEING 737 7374B7 1384702 NM ZONE 600 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q3 CHECK - NR JK-12-57102C/19, RIGHT WING NR 5 SLAT LOWER SKIN CRACKED. REPAIRED RIGHT WING NR 5 S LAT LOWER SKIN IAW B737 SRM 57-43-01. 2 L 7 2 4F RT A16WE 2008021300106 20080213 00106 EU 2008 2 13 USAA920080356 1 20080206 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS INTERMITTENT A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 644AW 23561 1077 317 FLT NR 322 - LAS-ORD - EEL - EMERGENCY LIGHTS AT DOORS L2, R2 AND ONE LOCATED IN CEILING BETWEEN AFT LAVS FLICKER ON AND OFF. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY UNIT. OPERATIONAL CHECK WAS NORMAL. 2 L 7 2 4F RT A28NM 2008021300107 20080213 00107 WP 2008 2 13 UPS08851631 1 20080111 A 5542 SKIN DOUG DC8 DC871F 302199D WP RUDDER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 CORROSION UNDER BONDED SKIN RT SIDE OF RUDDER ABOVE ISOLATION BELT. RUDDER REPLACED ON N/R 123801. 2 L 7 4 4F RT 4A25 2008021300121 20080213 00121 EU 2008 2 13 08FDEA00368 1 20080207 A 3240 C20104000 VALVE AIRBUS 300 A300F4605R 3930327 EU BRAKES INOPERATIVE A FDEA L A ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 25 691FE 877 IN PREPARATION FOR APPROACH INTO KBUR, WHEN AUTOBRAKES WERE SELECTED IN LOW OR MED THE AUTOBRAKE FAULT LIGHT ILLUMINATED (PREVIOUS WRITE UP). CONTACTED GOCC AND DIVERTED TO KLAX FOR MAINTENANCE. FOUND GROUND AT PIN B AT THE VALVES. REMOV ED AND REPLACED 89GG MASTER VALVE. CHECKED FILTER AT MASTER VALVE MANIFOLD FOUND NO DEFECTS. PERFORMED NORMAL BRAKING SYS, OPS CHECK NORMAL MM32-42-25, IPC 32-42-03, AWM 32-42-07 AND ASM 32-42-07. 2 L 7 2 4F RT A35EU 2008021300125 20080213 00125 EU 2008 2 13 08FDEA00372 1 20080208 A 5753 SKIN AIRBUS 330 A300* EU LT TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CRACKED HOLES FOUND DURING ACCOMPLISHMENT OF EO6-5750-7-5000 AT RIB 7, INNER FLAP LT AND DAMAGED NOSE SKIN JOINT STRIP. REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL AT HOLE ON RIB 7 AND REMOVAL OF CRACK AT NOSE SKIN JOINT STRIP IAW RAS/ FOK/015/2008 ISSUE A, APPROVED BY EA6-5752-114874. 2 L 7 2 4F RT A26NM 2008021300127 20080213 00127 NM 2008 2 13 08FDEA00374 1 20080208 A 7160 INLET DOUG MD11 MD11F 3023600 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 528FE 48623 NR 2 ENGINE INLET JUST FWD OF THE ENGINE FAN BLADES HAS NUMEROUS LOOSE FASTENERS AT THE 12:00, 9:00, AND 3:00 O'CLOCK PO SITION (REFERENCE MD 11 IPC 55-32-01-01, CIRCLED ITEM K). REMOVED AND REPLACED LOOSE FASTENERS INSIDE INLET PER AMM 20- 00-00. 2 L 7 3 4F 4 F RT A22WE E24NE 2008021300152 20080213 00152 NM 2008 2 13 DHL2008011702 1 20080117 A 5312 655851216 PRESSURE PANEL BOEING 727 727214 138407R NM MLG WW DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 15 BY 12 AREA DELAMINATED ON PANEL NR 3455 JUST FWD OF MLG WHEEL WELL AT STA 840. 2 L 7 3 4F A3WE 2008021300197 20080213 00197 NM 2008 2 13 USAA920080397 1 20080210 A 3350 BMS13311122 CHARGER BOEING 737 7373B7 1384580 NM EMERGENCY LIGHTS FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 533AU 24515 FLL - EEL - FLT NR 1249 - CREW REPORTED, LT SEAT EMERGENCY SEAT LIGHTS INOP, SEATS 5, 6, 7. MX REPLACED THE LT BATTERY CHARGER. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2008021400007 20080214 00007 EA 2008 2 14 TRAX200800158 1 20080201 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 750EV 10161 3RD FROM FORWARD CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008021400050 20080214 00050 EA 2008 2 14 TRAX200800204 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 581-693 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 LT FLOOR SEAT RAIL FS 581.0 TO FS 693.0 AT LBL 9.0 HAS CORROSION DAMAGE ON RAIL AND HARDWARE. 2 L 7 2 4F RT A21EA 2008021400052 20080214 00052 EA 2008 2 14 TRAX200800207 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 785-863 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 LT SIDEWALL SEAT RAIL FS 785.15 TO FS 863.0 HAS CORROSION DAMAGE. REMOVED AND REPLACED, LT SIDEWALL SEAT TRACK IAW AM M 53-00-49. 2 L 7 2 4F RT A21EA 2008021400056 20080214 00056 EA 2008 2 14 TRAX200800217 1 20080206 A 5310 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 871AS 7537 ENGINE SUPPORT BEAM UPPER WEB CRACKED AT AFT EDGE, FS 640, LBL8.0, WL119.12, MEASURES .80 INCHES LONG. ACCOMPLISHED RE PAIR TO ENG SUPPORT BEAM BY COMPLYING WITH REO 601R-53-61-345 IAW ASA EO 600-53-0072B CARD EO 600-53-72-0001. 2 L 7 2 4F RT A21EA 2008021400087 20080214 00087 NM 2008 2 14 08FDEA00387 1 20080211 A 5330 SKIN BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 LT LWR FUSELAGE EXTERIOR SKIN HAS CRACK AT STA 520, STR 23L. 22.500" FWD FROM STATIC PORT CENTER LINE. 2 L 7 3 4F RT A3WE 2008021400128 20080214 00128 NM 2008 2 14 QXEA200800087 1 20080114 A 5340 STRINGER CLIP DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - X468 AND STRINGER 31R SUSPECT CORROSION AT CLIP EDGE. MAINTENANCE BLENDED OUT CORROSION, REMAINED WITH IN LIMITS, INSPECTED AND NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021400130 20080214 00130 NM 2008 2 14 QXEA200800094 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 447-457 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - SEAT TRACK NR 5 X447 TO X457 IS GOUGED. MAINTENANCE BLENDED OUT GOUGE ON SEAT TRACK, INSPECTED AND REM AINED WITHIN LIMITS, NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021400143 20080214 00143 NM 2008 2 14 QXEA200800109 1 20080114 A 5320 SUPPORT ANGLE DHAV DHC8 DHC8202 2809007 NM BS 600 S28L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - CORROSION UNDER AFT CARGO DOOR THRESHOLD SUPPORT ANGLE APPROXIMATELY STA X600 STRINGER 28L. MAINTENANC E REMOVED RIVETS BLENDED CORROSION, INSPECTED, BLENDED AREA REMAINED WITHIN LIMITS WITH NO CRACKS NOTED. INSTALLED RIVE TS AND RESTORED FINISH TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021400151 20080214 00151 EU 2008 2 14 08FDEA00396 1 20080212 A 5315 A53978476200 FLOORBEAM AIRBUS 330 A300* EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION ON TOP CAP BEAM C61 REPAIR PERFORMED BY REPLACING OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A26NM 2008021400152 20080214 00152 EU 2008 2 14 08FDEA00397 1 20080212 A 5315 A53973611204 ATTACH FITTING AIRBUS 330 A300* EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION ON ATTACH FITTING TO TOP CAP BEAM, C 61 REPAIR PERFORMED BY REPLACING OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A26NM 2008021400162 20080214 00162 EU 2008 2 14 08FDEA00407 1 20080212 A 5320 A53981113 PLATE AIRBUS 330 A300* EU ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 741FD 611 FOUND 2 SHEAR PLATES AT C 79-80, P 26 LT/RT NOT CONFORM TO SRM 53-18-18 FIG 4. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A26NM 2008021400166 20080214 00166 EU 2008 2 14 TRAX200800224 1 20080128 A 5320 INTERCOSTAL AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 RT MLG W/W FR 25 INTERCOSTAL CRACKED. 2 H 7 2 4T RT A53EU 2008021500013 20080215 00013 2008 2 15 2008UALA00609 4 20080201 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR SLIDE MISRIGGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 546UA 25367 DOOR 4R, DOOR SLIDE WILL NOT FULLY DISARM. FOUND DOOR SLIDE LANYARD WRAPPED IN MECHANISM FOR SLIDE GIRT BAR. STOWED LAN YARD PROPERLY, DOOR SLIDE ARM/DISARM NOW WORKS FREELY. NO REPEATS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021500016 20080215 00016 NM 2008 2 15 08FDEA00411 1 20080212 A 5330 65561251 SKIN BOEING 727 727200 138407E NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 AFT CARGO COMPARTMENT FRAME SHEAR TIE HAS IMPROPER RIVET INSTALLATION ON FWD SIDE. RIVET INSTALLED THRU ANOTHER RIVET AT STA. 970, STR 25-26L. REMOVED RIVETS FROM SHEAR TIE AND FAIRING ATTACHMENT SUPPORT IAW SRM 51-30-2. CUT-OUT DAMAGED SK IN. FABRICATED REPAIR DOUBLER AND REPAIR FILLER IAW SRM 53-30-3 FIG1 AND 53-30-2 FIG 2.TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-30-3 FIG1 AND 51-30-2. 2 L 7 3 4F RT A3WE 2008021500018 20080215 00018 NM 2008 2 15 2008UALA00658 1 20080205 A 2910 V090497G7542 PRESSURE SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYD SYSTEM FAULTY A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 545UA 25323 RIGHT HYDRAULIC SYSTEM RESERVOIR LIGHT ILLUMINATED. FOUND PRESSURE SWITCH FAULTY. REPLACED PRESSURE SWITCH, NO REPEA TS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021500020 20080215 00020 EU 2008 2 15 2008UALA00662 1 20080205 A 3510 MXP401600U OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 461UA 1266 CREW REPORT: FO AND OBS1 OXYGEN MASKS WORK WELL BUT WILL NOT PRESS TO TEST WITHOUT PUSHING ON INNER O2 DOOR. REPLACED BOX ASSY, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021500025 20080215 00025 EA 2008 2 15 TRAX200800206 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 863-969 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 LT SIDEWALL SEAT RAIL FS 863.0 TO FS 969.0 HAS CORROSION DAMAGE. REMOVED CORRISION AND FOUND TO BE WITHIN LIMITS IAW CR J 700 SRM 53-51-49. APPLIED ALODINE IAW CRJ 700 ARM 51-21-16. 2 L 7 2 4F RT A21EA 2008021500033 20080215 00033 NM 2008 2 15 HALA0800067 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1093 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SEAT TRACK AT BS 1093 RBL 88.5, CORRODED BEYOND SRM LIMITS. SEAT TRACK REPLACED IAW SRM 53-00-52, FIG 201. 2 L 7 2 4F RT A1NM 2008021500038 20080215 00038 NM 2008 2 15 2008UALA00554 1 20080131 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY LIGHT INOP RIGHT CEILING ROW 32. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021500040 20080215 00040 NM 2008 2 15 HALA0800072 1 20080108 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 654 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SEAT TRACKS DAMAGED AT LOCATION RBL 54, STA. 654. DAMAGE REMOVED AT LOCATION RBL 54, STA. 654, IAW 767-300 SRM 53-00-52 , WITHIN SRM LIMITS. 2 L 7 2 4F RT A1NM 2008021500042 20080215 00042 NM 2008 2 15 HALA0800073 1 20080108 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 375 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SEAT TRACKS DAMAGED AT LOCATION LBL 88.5, STA. 375. DAMAGE REMOVED AT LOCATION LBL 88.5, STA 375, IAW SRM 53-00-52, WIT HIN LIMITS. 2 L 7 2 4F RT A1NM 2008021500044 20080215 00044 NM 2008 2 15 HALA0800074 1 20080108 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 785 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45, SEAT TRACK AT LBL 88.5, STA. 785. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW S RM 51-10-02, REV 75. BLENDED WITHIN LIMITS IAW SRM 53-00-52/101 REV 75. 2 L 7 2 4F RT A1NM 2008021500045 20080215 00045 NM 2008 2 15 HALA0800075 1 20080108 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 806 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION AT SECTION 45, SEAT TRACK AT LBL 88.5, STA 806. CORROSION REMOVED CONFIRMED BY 10X MAGNIFICANTION IAW SRM 51-10-02 REV 75, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101, REV 75. 2 L 7 2 4F RT A1NM 2008021500048 20080215 00048 NM 2008 2 15 HALA0800077 1 20080108 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 835 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION AT STATION 45, SEAT TRACK AT LBL 88.5, AT STA 835. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 51-10-02, REV 75. BLENDED WITHIN LIMITS, IAW SRM 53-00-52/101, REV 75. 2 L 7 2 4F RT A1NM 2008021500069 20080215 00069 NM 2008 2 15 2008UALA00038 1 20080102 A 5320 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FWD GALLEY DOOR CUTOUT INTERCOSTAL ANGLE CRACKED BETWEEN BS 277 & 294.5 AND BETWEEN STRINGERS 10R & 11R. MAJOR REPAIR: REPLACED ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500101 20080215 00101 SW 2008 2 15 497 1 20080121 A 6320 222375077105 TRANSDUCER BELL 430 430 1182150 SW OIL PRESSURE INOPERATIVE E AC2A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 31 430CT 49089 AIRCRAFT TRANSMISSION OIL PRESSURE ON INTEGRATED INSTRUMENT DISPLAY SYSTEM (IIDS) DECREASING. MADE TURN TO COME BACK TO INTRACOASTAL CITY. EMERGENCY CHECKLIST PULLED OUT AND FOLLOWED. INDICATED PRESSURE WENT DOWN INTO THE RED. LANDING A REA FOUND, AND LANDED THE AIRCRAFT IN MARSH AREA. ON SHORT FINAL, TRANSMISSION PRESSURE INDICATED 20 PSI, UPON LANDING, PRESSURE INDICATED 0 PSI. AIRCRAFT SHUTDOWN WITH NO DAMAGE TO AIRCRAFT, EXCEEDANCES, OR INJURY TO PASSENGERS. 1 G 7 2 3U RT H9SW 2008021500104 20080215 00104 2008 2 15 UPS08551667 4 20080213 A 3442 RADAR BOEING 757 75724APF 1384969 NM WX SYSTEM INOPERATIVE A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 467UP 25483 WX RADAR INOP. R&R WEATHER RADAR TRANSCEIVER AND WEATHER RADAR DRIVE ANTENNA PER AMM 34-43-05-4, AMM 34-43-04-4, AMM 34 -43-01-4, AND AMM 34-43-05-4. 2 L 7 2 4F RT A2NM 2008021500113 20080215 00113 NM 2008 2 15 2008UALA00561 1 20080130 A 2560 H2052K3833 LATCH BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EVAC SLIDE INADEQUATE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 664UA 29236 RT OVERWING SLIDE COMPARTMENT DOOR LATCHES NR 2 & 3 FAIL EDGE MARGIN MEASUREMENT. REMOVED AND REPLACED LATCHES. ACFT O K FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500118 20080215 00118 NM 2008 2 15 2008UALA00566 1 20080131 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 BS 293 INTERCOSTAL BETWEEN STRINGERS S-11R AND S-12R IS CRACKED. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500120 20080215 00120 NM 2008 2 15 2008UALA00569 1 20080131 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 BS 293 INTERCOSTAL BETWEEN STRINGERS S-10R AND S-11R IS CRACKED IN OUTBOARD ANGLE. MAJOR REPAIR ACCOMPLISHED: INSTALLE D NEW INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500124 20080215 00124 NM 2008 2 15 2008UALA00574 1 20080201 A 2120 1317 BALLAST BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN ODOR A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 173UA 24380 ODOR OF BURNING IN MAIN CABIN. UTILITY BUSSES TURNED OFF AND ODOR DISSIPATED. CREW HAVE LOCATED A LIGHT BALLAST THAT M AY HAVE BEEN THE PROBLEM. FOUND UD ROW 18 CEILING LIGHT SOCKET HAS ODOR. DISCONNECTED BALLAST FROM SIDE WALL. OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021500126 20080215 00126 NM 2008 2 15 2008UALA00576 1 20080201 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 DOOR 5 LEFT FWD SILL EMERGENCY LIGHT IS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021300075 20080213 00075 NM 2008 2 13 3LA200800044 1 20080206 A 5320 D5347217220400 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 15440 5503 2019 REFERENCE NON ROUTINE 26657, DURING C3/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE MAIN DECK FLOORBEAM AT LBL 48 BETWEEN FRAMES 67 AND 68. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM IN ACCORDANCE WITH THE REQUIR EMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE INSTALLATION, THE NEW FLOORBEAM WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008021300077 20080213 00077 EU 2008 2 13 TRBA2008017 1 20080204 A 3350 3013017 POWER SUPPLY AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHTS FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 538AT 538 EMERGENCY LIGHT POWER SUPPLY 62WL BATTERY PACK WILL NOT HOLD CHARGE. REPLACED POWER SUPPLY 62WL IAW JIC 33-51-21 RAI-10 00-007, OPS CK GOOD AT THIS TIME. 2 H 7 2 4T RT A53EU 2008021300101 20080213 00101 NM 2008 2 13 USAA920080371 1 20080123 A 5315 STIFFENER BOEING 737 7374B7 1384702 NM FLOORBEAM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q5 CHECK - NR JK-45-53500-C/10, CRACKED FLOORBEAM VERTICAL STIFFENER, BS 328, LBL 16. REPLACED FLO ORBEAM VERTICAL STIFFENER, BS 328, LBL 16 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008021300108 20080213 00108 WP 2008 2 13 UPS08851632 1 20080105 A 5347 36575011 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 CAPT'S FWD I/B SEAT TRACK IS WORN. REMOVED AND REPLACED CAPT'S FWD SEAT TRACKS REF, EO DC8-5340-1831 5 APPX B. 2 L 7 4 4F RT 4A25 2008021300115 20080213 00115 NM 2008 2 13 UPS08M51639 1 20080121 A 5712 ARB2850505 FITTING DOUG MD11 MD11F 3023600 NM LT WING RIB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 252UP 48768 INSPECTION TYPE:1C LT FIXED LE RIB FITTING IB OF NR 16 SLAT TRACK IS CRACKED. REMOVED AND REPLACED LT FIXED LE RIB FITT ING IB OF NR 16 SLAT TRACK PER MD-11 SRM 51-31-01 AND 51-35-01. 2 L 7 3 4F RT A22WE 2008021300148 20080213 00148 NM 2008 2 13 DHL2008782001 1 20080109 A 5754 651720927 ANGLE BOEING 727 727227 1384078 NM NR 4 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 782DH 21998 UPON INSPECTING THE LEADING EDGE, FOUND WHAT APPEARS TO BE A CRACK ON THE LEFT WING INBOARD MOUNT BRACKET FOR NR 4 LE SL AT ACTUATOR. THE CRACK TRAVELS FROM THE RADIUS TOWARDS THE BOLT AT APPROX WING STATION 393. ANGLE WILL BE REPLACED WIT H NEW PART. 2 L 7 3 4F A3WE 2008021400001 20080214 00001 NM 2008 2 14 ZZDA2008062 1 20080131 A 3397 WIRE BOEING 717 717200 1383700 NM EMERGENCY LIGHTS BROKEN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 921AT 55082 TEST OF EMERGENCY LIGHTS FOR SERVICE CHECK, TC601 STEP 34, REVEALED LIGHT INOPERATIVE AT SEAT 23D. REPAIRED BROKEN WIRE AT SEAT 23D IAW GMM 12-00-00, SYS CHECKS GOOD. 2 L 7 2 4F TR A6WE 2008021400005 20080214 00005 EU 2008 2 14 TRAX200800156 1 20080131 A 5311 FRAME AEROSP ATR72 ATR72212 8680945 EU LT MLG WW CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 642AS 395 LT WHEEL WELL FR 26 CRACKED. REPLACED IAW 51-25-04. 2 H 7 2 4T RT A53EU 2008021400016 20080214 00016 EU 2008 2 14 TRAX200800167 1 20080130 A 5330 SKIN AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 SKIN DOUBLER OF TAIL BUMPER BTW FR 38 TO 39 STR 21 RT TO 21 LT CORRODED. CORROSION REMOVED AS PER SRM 51-21-42. U/T PER FORMED IAW AMO 46-90. SKIN DOUBLER OF TAIL BUMPER REPAIRED AS PER SRM 53-00-00 FIG 410. OUT OF LIMITS AS PER SRM: 53-61- 00 FIG 301. 2 H 7 2 4T RT A53EU 2008021400017 20080214 00017 EU 2008 2 14 TRAX200800168 1 20080130 A 5720 BRACKET AEROSP ATR72 ATR72212 8680945 EU LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 LT WING RIB 13 I/B FLAP ARM (4) OMEGA BRACKET CRACKED. 2 H 7 2 4T RT A53EU 2008021400026 20080214 00026 EA 2008 2 14 TRAX200800177 1 20080201 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 680BR 7679 484.00 INTERCOSTAL CRACKED AT ATTACH POINT LBL 36, REPAIRED INTERCOSTAL, IAW REO'S 601R-53-41-059 AND 601R-53-41-662. 2 L 7 2 4F RT A21EA 2008021400028 20080214 00028 EA 2008 2 14 TRAX200800179 1 20080201 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 680BR 7679 FS 280.00 RBL 9.00 OUTBD ATTACH ANGLE CRACKED. REMOVED CRACKED ANGLE. REPAIRED FS 280.00 RBL 9.00 O/B ATTACH ANGLES P ER REO 601R-53-11-171. COMPLIED WITH EO 600-53-0090. 2 L 7 2 4F RT A21EA 2008021400041 20080214 00041 NM 2008 2 14 HALA0800036 1 20080207 A 4940 5198388 STARTER BOEING 767 76733A 1385209 NM APU FAILED A HALA K NONE O OTHER TX TAXI/GRND HDL 1 WP 13 587HA 33421 ETOPS SYSTEMS, APU FAULT, APU DOES NOT START. FOUND APU STARTER FAULT ON ECU. REPLACED APU STARTER PER AMM 49-41-01. OPS CHECK GOOD. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008021400051 20080214 00051 EA 2008 2 14 TRAX200800205 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 477-581 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 LT FLOOR SEAT RAIL FS 477.40 TO FS 581.0 HAS CORROSION DAMAGE ON RAIL AND HARDWARE. 2 L 7 2 4F RT A21EA 2008021400096 20080214 00096 NM 2008 2 14 QXEA200800067 1 20080114 A 5320 SUPPORT ANGLE DHAV DHC8 DHC8202 2809007 NM THRESHOLD CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C CHECK - SUPPORT ANGLE AT APPROXIMATELY STA X594.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTIN G SURFACE. MAINTENANCE REMOVED NUTPLATES AND REMOVED CORROSION. INSPECTED BLEND, WITHIN LIMITS. ALODINED, PRIMED AND PAINTED. INSTALLED NEW NUTPLATES. 2 H 7 2 4T RT A13NM 2008021400104 20080214 00104 NM 2008 2 14 QXEA200800077 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - RIGHT OUTBOARD SET TRACK NR 10 HAS SMALL AREA OF CORROSION AT APPROX X346. MAINTENANCE BLENDED CORRODE D AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021400107 20080214 00107 NM 2008 2 14 HALA0800037 1 20080209 A 2720 YAT06B BEARING BOEING 767 767332 1382001 NM RUDDER PEDAL FROZEN A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 598HA 23278 RUDDER PEDAL BINDING LEFT AND RIGHT ON BOTH CAPT'S AND FO'S RUDDER PEDALS. RIGHT RUDDER NOT RETURNING TO NEUTRAL. TROU BLESHOT PER FIM 27-21-00, FIG 107. FOUND BEARING FROZEN ON FEEL, CENTERING, AND TRIM MECHANISM (IPC 27-21-10-01, ITEM 4 08). REMOVED AND REPLACED BEARING PER AMM 27-21-10. SYSTEM OPS CHECKS GOOD. OK TO CONTINUE. 2 L 7 2 4F RT A1NM 2008021400115 20080214 00115 NM 2008 2 14 ABXA080052 1 20080123 A 5730 114T13312 SKIN BOEING 767 767232 1385132 NM LEFT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 740AX 22213 LEFT WING LEADING EDGE STRUCTURE HAD A BROKEN FASTENER AND TWO CRACKED MEMBERS AT LEADING EDGE SLAT 160. INSTALLED NEW SKIN IAW B767 SRM 51-40-1. 2 L 7 2 4F RT A1NM 2008021400120 20080214 00120 NM 2008 2 14 ABXA080048 1 20080108 A 5330 148T31213 SKIN BOEING 767 767232 1385132 NM BS 1767 S4R CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 740AX 22213 SKIN CRACKED STRINGER 4 RIGHT FS 1767. REPAIRED AREA RIGHT AFT FS 1767 IAW REA B653-56945. 2 L 7 2 4F RT A1NM 2008021400132 20080214 00132 NM 2008 2 14 QXEA200800111 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 312 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - NR 1 SEAT TRACK WEB TO FRAME ANGLE CLIP IS CRACKED FORWARD SIDE OF FRAME 312. MAINTENANCE REMOVED AND INSTALLED NEW CLIP. 2 H 7 2 4T RT A13NM 2008021400139 20080214 00139 NM 2008 2 14 QXEA200800099 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 496 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - SEAT TRACK NR 11 AT X496 HAS A CORROSION PIT ON TOP ANGLE. MAINTENANCE BLENDED OUT THE CORROSION, INSP ECTED, REMAINED WITHIN LIMITS WITH NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021500086 20080215 00086 NM 2008 2 15 2008UALA00429 1 20080124 A 3350 1619 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 350UA 24301 EES EXTERIOR LIGHT INOP JUST AFT OF DOOR 1R. RELAMPED EES EXTERIOR LIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500099 20080215 00099 NM 2008 2 15 2008UALA00511 1 20080129 A 3350 20121 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 326UA 23958 EMERGENCY EXIT FLOOR LIGHTS INOPERATIVE PAST ROW 15. REPLACED POWER SUPPLY, BATTERY AND LIGHT STRIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500128 20080215 00128 NM 2008 2 15 2008UALA00577 1 20080201 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 ZONE D LEFT SIDE CEILING EMERGENCY LIGHT IS INOP (2EA). RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021500138 20080215 00138 NM 2008 2 15 2008UALA00586 1 20080201 A 5753 113T1654179 PANEL BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE T/E FLAP PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 784UA 26951 OUTBOARD PANEL, ABOVE T/E FLAP PUNCTURED FROM FLAP GUIDE TRACK. SUSPECT FLAP TRACK SNAPPED. REMOVED PANEL AND ROUTED T O SHOP ON R & R NR R16520. REINSTALLED PANEL. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021500141 20080215 00141 NM 2008 2 15 2008UALA00596 1 20080201 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 616 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 MID CABIN STUB FRAME AT BS 616 LEFT SIDE BELOW WL 208 CRACKED. INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500143 20080215 00143 NM 2008 2 15 2008UALA00600 1 20080201 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 328 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 303UA 23644 FWD GALLEY DOOR CUTOUT CRACKED AT LOWER AFT CORNER NEAR BS 328. FABRICATED AND INSTALLED EXTERNAL FUSELAGE DOUBLER-TRIP LER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500144 20080215 00144 NM 2008 2 15 2008UALA00601 1 20080201 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 294-322 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 303UA 23644 RIGHT CREASE BEAM INNER CHORD CORRODED BS 294-322. REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500148 20080215 00148 NM 2008 2 15 2008UALA00606 1 20080201 A 5330 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU BS 280 S2-3L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 942UA 26679 FUSELAGE SKIN APPROX STA 280 BETWEEN STR 2L & 3L HAS BLEND MARKS. MAJOR REPAIR: MANUFACTURED AND INSTALLED REPAIR DOUBL ER WITH BLIND FASTENERS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500149 20080215 00149 NM 2008 2 15 2008UALA00607 1 20080203 A 2120 WIRE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COFFEEMAKER BURNED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 905UA 1039 25005 LANDED UNDER AN AMBER ALERT WITH SMOKE IN FORWARD GALLEY. FOUND FORWARD GALLEY COFFEEMAKER WITH SHORTED AND BURNED SENS OR WIRES. REPLACED COFFEEMAKER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500156 20080215 00156 NE 2008 2 15 2008UALA00619 2 20080203 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 DAMAGED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 793UA 26946 222085 SILENT SURGES DETECTED IN NR 1 ENGINE. ENGINE REPLACED AT SFO DUE TO HEAVY HP COMPRESSOR BLADE DAMAGE FOUND BY BORESC OPE INSPECTION. ONE BLADE WAS FOUND BROKEN IN THE AIRFOIL. SUSPECT DAMAGE TO BE THE RESULT OF VSV INNER TRUNNION BUTTO N LIBERATION. THIS IS A FIRST RUN HP COMPRESSOR. FINDINGS TO BE UPDATED FOLLOWING HP COMPRESSOR TEARDOWN. ESTIMATE 03/3 1/08. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021500158 20080215 00158 NM 2008 2 15 2008UALA00633 1 20080202 A 3350 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 WALL EXIT SIGN INOP DOOR 5R FWD SIDE. FOUND SHORTED AT FEEDER CABLE. REPAIRED SHORTED AT FEEDER CABLE. AC OK FOR SERVIC E. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021500160 20080215 00160 NM 2008 2 15 2008UALA00638 1 20080204 A 2120 UNKNOWN BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 677UA 30029 CREW REPORTS VISIBLE SMOKE IN CABIN, MOST NOTICEABLE AT ROW 12. UNABLE TO DUPLICATE REPORTED PROBLEM. MECHANICS AND FL T CREW NOTED NO SMOKE IN CABIN ON RETURN FLIGHT FROM MCI TO ORD. NOTED FIND IN ATA CODE 210000.ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500163 20080215 00163 NM 2008 2 15 2008UALA00643 1 20080204 A 3246 BEARING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT MLG FAILED A UALA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 WP 29 772UA 26930 RECEIVED A REPORT OF A FIRE IN VICINITY OF RT MAIN GEAR FROM CDG TOWER. ACFT DEPLANED IN TAXIWAY (ALL EIGHT SLIDES). N R 4 MLG (RT GEAR RT FRONT) OUTER WHEEL BEARING FAILED. NR 4 MLG (RT GEAR, RT FRONT) OUTER WHEEL BEARING FAILED. RT GE AR FWD AXLE IS HEAT DAMAGED AND CRACKED ON WHEEL NUT THREAD PORTION. REPLACED AXLE ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021500169 20080215 00169 NM 2008 2 15 SWAA080696 1 20080206 A 3397 W4142001520 WIRE BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 408WN 27895 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. FOUND LOOSE WIRE AT LIGHT ASSY. SECURED WIRE PER MM. 2 L 7 2 4F RT A16WE 2008021500174 20080215 00174 NM 2008 2 15 SWAA080701 1 20080206 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020800312 20080208 00312 NM 2008 2 8 AALA200800107 1 20080119 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 683A 25340 BOS - EMERGENCY LIGHT BATTERY PACK AT SEAT 1B INOPERATIVE. REPLACED BATTERY PACK AT SEAT 1B. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 2008020800314 20080208 00314 EA 2008 2 8 COMA0860103 1 20080130 A 2421 IDG CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE UNDERSERVICED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 804CA 7352 FLIGHT 5364 - ON TAKEOFF ROLL BELOW 40 KTS, LEFT IDG AND GEN MESSAGE ILLUMINATED. ABORTED TAKEOFF SAFELY. UPON INSPECT ION FOUND IDG UNDER SERVICED. RESERVICED IDG, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008020800315 20080208 00315 NM 2008 2 8 SWAA080628 1 20080204 A 3350 311500 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 259WN 35554 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008020800316 20080208 00316 NM 2008 2 8 SWAA080629 1 20080204 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 291WN 32539 DURING SCHEDULED MV2 CHECK, FOUND RT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 2008020800319 20080208 00319 NE 2008 2 8 SIMA200803501 2 20080130 A 7200 FAN BLADE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE ENGINE FAILED A SIMA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 21 503AE 10021 ON FLIGHT 4321 - AFTER TAKEOFF FLIGHT CREW NOTED ENGINE 2 VIBRATION. CREW REDUCED POWER AND NOTED VIBRATION AT 2.0 ON S CALE. CREW RETURNED TO ORD WITHOUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED ALL FAN BLADES AND REPA IRED FAN INLET. ALSO REPAIRED FAN CONTAINMENT RING PER IAW GE ENG MAN 72-00-23. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008020800322 20080208 00322 NM 2008 2 8 SWAA080632 1 20080204 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 8R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008020800324 20080208 00324 NM 2008 2 8 SWAA080647 1 20080204 A 5311 6545808 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 291, STR 14R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008020800325 20080208 00325 NM 2008 2 8 SWAA080633 1 20080204 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800332 20080208 00332 SO 2008 2 8 SIMA200803504 1 20080203 A 3230 SOLENOID VALVE EMB 135 EMB135LR 3260305 SO NLG MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 716AE 145264 ON FLIGHT4828 - CREW REPORT LOUD RUSHING NOISE COMING FROM THE NOSE GEAR WELL LIKE A GEAR DOOR WAS NOT FULLY CLOSED. AI RCRAFT REMOVED FROM SERVICE. TROUBLE SHOT SYSTEM. PERFORMED VISUAL INSPECTION OF NLG, AND DOORS. NO DEFECTS NOTED. P ERFORMED GEAR SWING IAW AMM 32-30-00. REMOVED AND REPLACED LGEU IAW 32-32-01 WITH GEAR UP FOUND NOSE LANDING GEAR DOOR SOLENOID VLV TO BE INTERMITTENT. REMOVED AND REPLACED NLG DOOR SOLENOID VALVE IAW AMM 32-33-02. OPERATIONAL CHECK GOOD AND LEAK CHECK GOOD. PERF GEAR SWINGS IAW AMM 32-30-00. OPERATIONAL CHECK GOOD, NO FURTHER DEFECTS. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4F RT T00011AT 2008020800333 20080208 00333 NM 2008 2 8 SWAA080639 1 20080203 A 5610 5716145 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 309SW 22948 FLIGHT DECK L1 WINDOW ARCED. REMOVED AND REPLACED WINDOW HEAT CONTROLLER AND WINDOW PER MM. 2 L 7 2 4F RT A16WE 2008020800336 20080208 00336 NM 2008 2 8 SWAA080640 1 20080204 A 5343 6546543 FITTING BOEING 737 7373H4 1384600 NM MLG W/W CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED MV2 CHECK, FOUND RT MLG SIDE SUPPORT FITTING LUG CORRODED AT BS 685. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800352 20080208 00352 NM 2008 2 8 SWAA080648 1 20080204 A 5311 6558280 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800355 20080208 00355 WP 2008 2 8 DHL2007873533 1 20080113 A 5720 FITTING DOUG DC8 DC873F 302199F WP NR 2 TANK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 NR 2 MAIN TANK AFT FITTING CRACKED BETWEEN STA XRS 74.000 AND S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1- 0 PG 1. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1 SRM 51-1-20D. CLEANED AND APPLIED POLYURETHANE TOP YELLOW COATING TO AREA IAW SRM 51-1-12 PG 7. INSTALLED NEW FITTING IAW SRM 51-1-12 SRM 51-3-0 SRM 51-1-23 (PLI -WASHER) SRM 51-1-20D S RM 51-3-1 (TORQUE) REFER TO NR 107760 FOR FUEL LEAK CHECK. 2 L 7 4 4F RT 4A25 2008020800357 20080208 00357 NM 2008 2 8 AALA200800148 1 20080123 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 767AJ 33539 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR LOWER CLOSET DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR LOWER CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008020800358 20080208 00358 NM 2008 2 8 AALA200800183 1 20080127 A 2530 OVEN BOEING 757 757223 1384957 NM CABIN SMOKE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 617AM 24525 VVI INFLIGHT 922/27JAN - CREW REPORTED SMOKE IN CABIN. TURNED OFF RIGHT AIR RECIRCULATION FAN AND SMOKE DISSIPATED. IN SPECTED AND CLEANED AFT GALLEY NUMBER TWO OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020800359 20080208 00359 NM 2008 2 8 SWAA080650 1 20080204 A 2560 6557463 FITTING BOEING 737 7375H4 138449D NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2008020800360 20080208 00360 NM 2008 2 8 AALA200800172 1 20080125 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 361AA 24042 DFW EXTERNAL EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMPS FOR EXTERNAL EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008020800366 20080208 00366 GL 2008 2 8 CHQA200800018 2 20080130 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 SMOKE A CHQA G A O2 MASK DEPLOYED UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 11 564RP 17548 2289 145524 CAE312502 JFK TO BUF - AT APPROXIMATELY 500FT AGL, THE FLIGHT CREW NOTICED SMOKE IN THE COCKPIT. OXYGEN MASKS WERE DONNED AND THE AIRCRAFT WAS PREPARED TO RETURN TO FIELD AT JFK. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RAN BOTH ENGINES A ND WAS ABLE TO DUPLICATE THE SMOKE WHEN RUNNING ON THE NR 1 ENGINE BLEED. MAINTENANCE DEFERRED THE NR 1 BLEED SYSTEM AN D THE AIRCRAFT WAS FERRIED TO CMH WHERE THE NR 1 ENGINE WAS REPLACED. AFTER REPLACING ENGINE 1, THERE WERE NO RE-OCCURR ENCES OF SMOKE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008020800368 20080208 00368 WP 2008 2 8 AALA200800089 1 20080118 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 430AA 49342 LGA - EMERGENCY LIGHTS AT SEAT ROWS 26 TO 29 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 26 TO 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020800370 20080208 00370 EA 2008 2 8 SIMA200803105 1 20080127 A 2910 SH670757921 LINE CNDAIR CL600 CL6002C10 1390015 EA HYD SYSTEM CRACKED A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 504AE 10044 ON FLIGHT 3626 CREW REPORTED DURING CRUISE THE NUMBER 3 HYDRAULIC SYSTEM DROPPED TO 5 PERCENT QUANTITY AND 0 PSI. CREW DECLARE AN EMERGENCY AND DIVERTING TO OKC DUE TO WEATHER IN DFW. AIRCRAFT REMOVED FROM SERVICE. FOUND NUMBER 3A HYDRAU LIC PUMP PRESS LINE CRACKED REPLACED LINE WITH TEMP FLEX LINE AND ISSUED TDMI FOR 450 FLIGHT HOURS. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F RT A21EA 2008020800372 20080208 00372 2008 2 8 UPS08151586 4 20080128 A 2565 SLIDE AIRBUS A300 A300F4622R 3930360 EU CREW DOOR DISLODGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 120UP 0805 DOOR WAS OPEN BEFORE SLIDE DISARMED, SLIDE DID NOT DEPLOY BUT FELL OUT ON STAIRS. DEFERRAL M367928. INSTALLED MAIN ENT RY DOOR ESCAPE SLIDE REF 25-61-21-04. PLACARD REMOVED. 2 L 7 2 4F RT A35EU 2008020800373 20080208 00373 NE 2008 2 8 UPS08451576 2 20080129 A 7230 FAN BLADE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 AFTER LANDING IN MEM, MX REPORTED DAMAGE TO MULTIPLE FAN BLADES AND INSIDE OF COWLING ON NR 2 ENGINE. THERE WERE NO IN FLIGHT INDICATIONS. REMOVED AND REPLACED 6 PAIRS OF FAN BLADES IAW MM 72-31-02. REMOVED AND REPLACED NR 2 ENG NOSE COW L IAW T C 5027. REPAIRED SOUND ABSORBING LINER 6 O'CLOCK POSITION. DEFERRED ABSORBING LINER REPAIR FOR REINSPECT WITHI N MAX OF 50 HRS. 2 L 7 4 4F 4 F RT A20WE E20EA 2008020800374 20080208 00374 NM 2008 2 8 UPS08551565 1 20080121 A 3350 BPS73 BATTERY PACK BOEING 757 75724APF 1384969 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 422UP 25324 EMERGENCY LIGHT INOP. ACCOMPLISHED FIM 33-51-00 FIG 103 SHEET 1 TO BLOCK 42. REPLACED BATTERY PACK IAW MM 33-51-07-2. SYSTEM OPS CK NORMAL. 2 L 7 2 4F RT A2NM 2008020800378 20080208 00378 WP 2008 2 8 UPS08851545 1 20080123 A 3350 LIGHT DOUG DC8 DC873F 302199F WP EMERGENCY EXIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 ON SHUTDOWN CHECKLIST, EMERGENCY EXIT LIGHTS DOES NOT ILLUMINATE. IN DISARM POSITION LIGHT WILL NOT PRESS TO TEST. REL AMPED EMERGENCY EXIT INDICATION LIGHT PER STD PRACTICES. OPS CHECKS NORMAL. 2 L 7 4 4F RT 4A25 2008020800380 20080208 00380 NE 2008 2 8 CHQA200800020 2 20080203 A 7260 5018T49P05 SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE ACCY GEARBOX LEAKING A CHQA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 467CA 7637 GEE873361 IAH TO SRQ - DURING CLIMB, THE CREW RECEIVED A WARNING FOR E1 OIL PRESSURE. E1 OIL PRESSURE WAS NOTED TO FLUCTUATE FROM BELOW 25PSI TO 40PSI. CREW FOLLOWED THE QRH AND REDUCED THRUST ON E1, AFTER WHICH IT WAS NOTED THAT THE OIL PRESSURE H AD STABILIZED AT THE LOWER POWER SETTING. THE FLIGHT RETURNED TO FIELD AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED E1 AND FOUND THE SEALS FOR THE ENGINE DRIVEN HYDRAULIC PUMP, INTEGRATED DRIVE GENERATOR, AND THE STARTER WERE LEAKING. THE AIRCRAFT WAS THEN FERRIED TO SDF WHERE THE EDP, IDG, AND STARTER SEALS WERE REPLACED. AFTER REPLACING THE SEALS AND SERVICING WITH OIL, THERE WERE NO FURTHER DEFECTS NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 2008020800382 20080208 00382 NM 2008 2 8 SWAA080646 1 20080204 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020800383 20080208 00383 NM 2008 2 8 WRLA2008017 1 20080201 A 5753 NRC6055508 SKIN DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE T/E FLAP CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 272WA 48437 DURING A CHECK INSPECTION 9 INCH CRACK FOUND RIGHT WING INBOARD FLAP UPPER SKIN INBOARD AFT SKIN PANEL AT XIFH231.2. RE PAIRED PER MD-11 SRM 57-20-00 VOL 1 REF ERA 466462-14. 2 L 7 3 4F 4 F RT A22WE E24NE 2008020800385 20080208 00385 NM 2008 2 8 WRLA2008020 1 20080203 A 2750 FLAP SYSTEM DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE WING FROZEN A WRLA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 11 274WA 48633 ON APPROACH FLAPS WOULD NOT EXTEND, NO FLAPS/SLATS EXTENDED CHECKLIST ACCOMPLISHED, EMERGENCY DECLARED. FOUND AREA ABOV E LT & RT MAIN GEAR BOX FLOODED WITH WATER & FROZEN. DRAINED & VENTILATED DRY. REPLACED INSULATION BLANKETS BS 1381-1521 MM 25-85-01. FLOOR PANELS INSTALLED AND SEALED. FLAPS/SLATS OPS CHECK REF MM 27-50-00. 2 L 7 3 4F 4 F RT A22WE E24NE 2008020800387 20080208 00387 2008 2 8 SWAA080656 4 20080204 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008020800388 20080208 00388 NM 2008 2 8 SWAA080657 1 20080205 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800389 20080208 00389 NM 2008 2 8 SWAA080658 1 20080205 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800392 20080208 00392 NM 2008 2 8 SWAA080681 1 20080204 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, 9 O'CLOCK POSITION. REPAIRED WEB PER S RM. 2 L 7 2 4F RT A16WE 2008020800396 20080208 00396 NM 2008 2 8 SWAA080664 1 20080204 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020800397 20080208 00397 NM 2008 2 8 SWAA080665 1 20080204 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020800403 20080208 00403 NM 2008 2 8 SWAA080674 1 20080205 A 5322 6546569 SHEAR TIE BOEING 737 7373TO 138447G NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 947, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020800404 20080208 00404 NM 2008 2 8 SWAA080675 1 20080205 A 5322 6546569 SHEAR TIE BOEING 737 7373TO 138447G NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020800409 20080208 00409 NM 2008 2 8 SWAA080680 1 20080205 A 5311 6567740 FRAME BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, BETWEEN STR 2R AND STR 3R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008021100001 20080211 00001 SW 2008 2 11 WGEA200800019 1 20080204 A 3411 10056418 PROBE ECLIPS EA500 ECLIPSEEA500 3350000 SW PITOT/STATIC MALFUNCTIONED E WGEA O OTHER N FALSE WARNING CL CLIMB 1 EA 27 160DJ 42 000077 CENTER AIRSPEED AND ALTIMETER READS 200 FEET LOW AND 20 KNOTS RESPECTIVELY UP TO CRUISE ALTITUDE OF 2200 FEET. REMOVED AND REPLACED STANDBY PITOT/STATIC PROBE WITH SERVICEABLE PROBE IAW EA500 AMM 34-10-12. PERFORMED STANDBY PITOT/STATIC VE RIFICATION TEST. OPS CHECK GOOD IAW EA500 AMM 34-10-00. 1 L 7 2 4J RT A00002AC 2008021100012 20080211 00012 WP 2008 2 11 IXXA080005O 1 20080203 A 2612 CONNECTOR DOUG DC8 DC872F 302199E WP FIRE WARNING DIRTY A IXXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 11 721CX 84622 2869 46013 DURING CRUISE FROM LPLA TO KBWI NR 1 ENGINE SHORT CIRCUIT LIGHT CAME ON, THE CREW ACCOMPLISHED EMERGENCY PROCEDURES AND SHUT DOWN NR 1 ENGINE AND LANDED WITHOUT INCIDENT AT KWRI. MAINTENANCE INSPECTED AND CLEANED NR 1 ENGINE FIRE SENSING E LEMENTS CONNECTORS, FOUND NO DEFECTS SYSTEM OPERATIONAL CHECK WAS GOOD IAW DACO DC8 MAINTENANCE MANUAL 26-10-1. AIRCRAF T WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2008021100016 20080211 00016 EA 2008 2 11 SWIA200819198 1 20080202 A 3520 OXYGEN MASK CNDAIR CL600 CL6002B19 1900309 EA ROW 5 UNWANTED DEPLOY A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 FLT 3798 - O2 MASKS INADVERTENTLY DEPLOYED AT ROW 5. RESTOWED O2 MASKS AS REQUIRED. 2 L 7 2 4F RT A21EA 2008020800012 20080208 00012 2008 2 8 USAA920080278 4 20080125 A 2565 D30664105 SLIDE RAFT AIRBUS 320 A320231 3930325 EU R1 DOOR DEFECTIVE A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 637AW 50314 9263 99 FLT 570 - LAS-PHX - EMERGENCY EQUIPMENT - R1 SLIDE WILL NOT ARM. HANDLE DOES NOT SNAP INTO POSITION. SLIDE WAS REMOVED FOR FERRY FLIGHT AND DOOR ASSIST BOTTLE DEACTIVATED. MAINTENANCE REMOVED AND REPLACED THE R1 DOOR SLIDE/RAFT IAW TASK CARD R1C25304. 2 L 7 2 4F RT A28NM 2008020800035 20080208 00035 NM 2008 2 8 BB08005 1 20080126 A 2750 FLAP SYSTEM BOEING 767 767201 1385125 NM MALFUNCTIONED A USAA K NONE J WARNING INDICATION DE DESCENT 1 EA 19 246AY 23898 MXP FLT 716 PHL-MXP - CREW RECEIVED EICAS MESSAGE T/E FLAP DISAGREE DISPLAYED. TRAILING EDGE LIGHT ILLUMINATED WHEN ANY T/E FLAP POSITION SELECTED. FLAPS FAIL TO MOVE TO SELECTED POSITION. MAINTENANCE PERFORMED TROUBLESHOOTING PER FIM - NO FAULT FOUND. INSPECTED T/E FLAPS ROTARY ACTUATOR OVERLOAD TRIP INDICATOR, NO FAULT FOUND. ALSO GROUNDED CIRCUIT FRO M PIN X2 ON PLUG D2268 TO A3 ON PLUG D1836A, NO FAULT FOUND. AIRCRAFT OK FOR DISPATCH. 2 L 7 2 4F RT A1NM 2008020800052 20080208 00052 WP 2008 2 8 DHL2007873509 1 20080108 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 1060 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 MAIN CARGO COMPT FITTING CORRODED STA 1060.000 L-21R. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS I AW SRM 53-2-0 PG 2P. REMOVED CORRODED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INS TALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2008020800112 20080208 00112 SO 2008 2 8 SIMA200803103 1 20080126 A 5320 14525480603 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AE 20224 5000 145111 DURING A MBV INSPECTION, THE CARGO DOOR CUT OUT LOWER SILL WAS FOUND TO BE CORRODED. AIRCRAFT WAS OUT OF SERVICE. REMO VED AND REPLACED SILL WITH NEW SILL IAW EMB SAR 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008020800151 20080208 00151 NM 2008 2 8 USAA920080294 1 20080127 A 5532 175T20014 PANEL BOEING 767 7672B7ER 1385107 NM VERTICAL STAB DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 24765 BFM - MAJOR REPAIR - C4 CHECK - DELAMINATION ON VERTICAL STABILIZER RIGHT HAND SIDE FIXED PANEL, FSS 118-75 - FSS 192.25 . REPLACED VERTICAL STABILIZER RIGHT HAND SIDE FIXED PANEL, FSS 118-75 - FSS 192.25 IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008020800174 20080208 00174 WP 2008 2 8 AALA200800121 1 20080121 A 3222 STRUT DOUG DC9 DC983 3022083 WP NLG FLAT A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 592AA 53255 PHL INFLIGHT T895/21JAN - NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED TO PHL AND LANDED WITHOUT INCIDENT. FOUND NOSE STRUT FLAT. REPACKED NOSE LANDING GEAR STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800177 20080208 00177 WP 2008 2 8 AALA200800129 1 20080121 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9617R 53564 DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 28 TO 30 AND AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY L IGHTS AT OVERHEAD SEAT ROWS 28 TO 30 AND AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800245 20080208 00245 NM 2008 2 8 SWAA080591 1 20080202 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 338 AND BS 350, STR 1. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008020800250 20080208 00250 NM 2008 2 8 SWAA080593 1 20080201 A 3350 6042221 CHARGER BOEING 737 7373H4 1384600 NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 FWD CABIN EMERGENCY EXIT LIGHTS ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2008020800277 20080208 00277 NM 2008 2 8 SWAA080599 1 20080202 A 3350 MS155721 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008020800291 20080208 00291 NM 2008 2 8 SWAA080624 1 20080203 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, BL 0 TO LBL 13. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020800342 20080208 00342 NM 2008 2 8 SWAA080651 1 20080204 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008020800347 20080208 00347 WP 2008 2 8 DHL2007873528 1 20080123 A 5523 BRACKET DOUG DC8 DC873F 302199F WP ELEVATOR TAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 LT ELEVATOR CONTROL TAB BRACKET CRACKED STA 75. REMOVED AND REPLACED LT ELEV CONTROL TAB BRACKET AT STA 75 IAW SRM 51-1 -21, SRM 51-1-20D. REFER TO NR 107757 FOR FLT CONTROL OPS CHECK, AND NR 107816 FOR WEIGHT AND BALANCE. 2 L 7 4 4F RT 4A25 2008020800348 20080208 00348 WP 2008 2 8 DHL2007873529 1 20080120 A 5410 ANGLE DOUG DC8 DC873F 302199F WP CFMINT CFM56 CFM562AFR 13802 EU NR 3 NACELLE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 NR 3 ENG ANGLE CRACKED 2" STA YN 163.535 AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 D ATED 01-08-08 BOEING MSG NR 1-746231818-2 DATED 01-09-08. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED NDT INSP TO VER IFY CRACK DO NOT EXTEND HOLE IAW NDT SPM PART 06-10-01-001. NO CRACK FOUND ENCLOSED SMN-FORM 242-2. FABRICATED REPAIR DOUBLER. 2 L 7 4 4F 4 F RT 4A25 E21EU 2008020800364 20080208 00364 NM 2008 2 8 DLM88080143 1 20080131 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 579 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 FUSELAGE SKIN INTERNAL DOUBLER AT FS 579 BETWEEN LONGERONS 28L AND 29L HAD A 0.45" CRACK. THE CRACK WAS TRIMMED OUT, AN D AN INTERNAL REPAIR DOUBLER WAS INSTALLED. 2 L 7 2 4F RT A6WE 2008020800375 20080208 00375 WP 2008 2 8 AALA200800077 1 20080116 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9403W 53139 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 27 TO 29 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHE AD SEAT ROWS 27 TO 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008020800410 20080208 00410 NM 2008 2 8 SWAA080667 1 20080204 A 5313 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008021100019 20080211 00019 EA 2008 2 11 SWIA200819201 1 20080205 A 5240 SEAL CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR OBSTRUCTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 449SW 7699 FLT 3987 - SERVICE DOOR IS DIFFICULT TO OPEN. INSPECTED AND REMOVED ICE FROM DOOR SEAL. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008021100020 20080211 00020 SO 2008 2 11 SWIA200819173 1 20080129 A 5210 HANDLE EMB 120 EMB120ER 3260203 SO PAX DOOR LACK OF LUBE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 579SW 120347 FLT 5753 - MAIN CABIN DOOR IS DIFFICULT TO OPEN. LUBED PAX DOOR HANDLE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008021100022 20080211 00022 SO 2008 2 11 SMIA200803701 1 20080202 A 2131 2225ONO30301 CONTROLLER EMB 135 EMB135KL 3260302 SO CABIN PRESSURE MALFUNCTIONED A SIMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 21 840AE 145656 ON FLT 4240, CREW REPORTED EN ROUTE AT FL360, THE CABIN ALTITUDE BEGAN A GRADUAL CLIMB IN TO THE AMBER RANGE. CREW SWIT CHED THE PRESSURIZATION MODE TO MANUAL MODE BUT WAS NOT INITIALLY ABLE TO CONTROL THE CABIN ALTITUDE. CREW INITIATED A D ESCENT WITH ATC AND ADVISED THAT THEY HAD A PROBLEM THE PRESSURIZATION. CREW DECLARED AN EMERGENCY AND REQUESTED 10,000 FEET. LANDED WITHOUT INCIDENT AIRCRAFT WAS NOT REMOVED FROM SERVICE. ISSUED MEL AIRCRAFT REMOVED FROM SERVICE. REMOV ED AND REPLACE DIGITAL CONTROLLER. FUNCTION TEST OF PRESSURIZATION CONTROL IN AUTO MODE CHECK GOOD, REF AMM 21-31-01 ME L 21-16. RESTORED AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008021100023 20080211 00023 2008 2 11 SMIA200803702 4 20080204 A 3140 7013348949 DAU EMB 135 EMB135KL 3260302 SO NR 1 MALFUNCTIONED A SIMA O OTHER N FALSE WARNING LD LANDING 1 SW 21 829AE 145609 ON FLIGHT 4548 CREW REPORTED AT GEAR EXTENSION. EICAS BREAK OUTBOARD INOP. CREW DECLARED AN EMERGENCY MESSAGE REMOVED AFTER LANDING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 DAU IAW EMB 140 AMM 32-41-02. CHECKS GOOD, NO DEFECTS NOTED. PERFORMED LANDING EXTENSION AND RETRACTION , AMM 32-34-00. NO DEFECTS NOTED, AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4F RT T00011AT 2008021100029 20080211 00029 SO 2008 2 11 SWIA200819179 1 20080129 A 5230 SEAL EMB 120 EMB120ER 3260203 SO CARGO DOOR LEAKING A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 582SW 120350 FLT 5758 - LOST CABIN PRESSURE AND OXYGEN MASKS DEPLOYED. REPAIRED UPPER CARGO DOOR SEAL. PRESSURIZATION CHECKS GOOD I N AUTO AND MANUAL MODES. 2 L 7 2 4T RT A31SO 2008021100030 20080211 00030 SW 2008 2 11 WGEA200800016 1 20080201 A 3240 BRAKE ECLIPS EA500 ECLIPSEEA500 3350000 SW MLG WEAK E WGEA O OTHER O OTHER LD LANDING 1 EA 27 141DJ 000055 MAX PEDAL DEFLECTION REQUIRED TO STOP, SPONGY FEEL ON BRAKES. SERVICED BRAKE RESERVOIR AND BLED BRAKES, NO DEFECTS NOTE D, IAW EA 500 MM 32-40-00. 1 L 7 2 4J RT A00002AC 2008021100031 20080211 00031 SO 2008 2 11 SIMA200803902 1 20080207 A 2820 VALVE EMB 145 EMB145LR 3260212 SO FUEL VENT MALFUNCTIONED A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 690AE 14500858 ON FLIGHT 4207, CREW REPORTED ON CLIMB-OUT THERE WAS SOME FUEL VENTING FROM THE RIGHT WING VENT VALVE. SERVICED TANKS T O 10600 LBS AND WAS UNABLE TO DUPLICATE LEAK. OK PER EMB AMM 28-12-00 OVERWEIGHT LANDING. AIRCRAFT REMOVED FROM SERVIC E. DESCENT WAS UNDER 300 FPM, NO MAINTENANCE ACTION REQUIRED FOR OVERWEIGHT LANDING. INSPECTED AIRCRAFT, NO ACTION REQ UIRED PER EMB AMM 28-12-00 AND NR 8194; AND NR 8194; AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008021100033 20080211 00033 NM 2008 2 11 DLM90080154 1 20080201 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 939 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 RT CUSP WEB FS 939 CORRODED AT LIGHTNING HOLE. REPAIRED CUSP WEB IAW EA 53-05D ON N/R 2700-0149 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008021100035 20080211 00035 NM 2008 2 11 DL76S080149 1 20080101 A 3397 WIRE BOEING 767 767332 1382001 NM EMERGENCY LIGHTS DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 137DL 25306 EMERGENCY LIGHT INOP AT SEAT 14F AND 10F. REPAIRED WIRES, OPS CK OK. 2 L 7 2 4F RT A1NM 2008021100043 20080211 00043 EA 2008 2 11 SWIA200819170 1 20080203 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY FAULTY A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 454SW 7749 AFT SMOKE DETECTOR GIVES ERRONEOUS SMOKE MESSAGE. REPLACED AFT CARGO SMOKE DETECTOR IAW MM 26-15-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008021100051 20080211 00051 EA 2008 2 11 MASA200800068 1 20080126 A 5270 SENSOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT DIRTY A MASA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 906FJ 15006 ASH 2726 PVR-LAS - CAPTAIN REPORTED A LT OVERWING EMERGENCY EXIT DOOR CAUTION MESSAGE DURING TAXI IN. MX CLEANED SENSOR , OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2008021100052 20080211 00052 EA 2008 2 11 MASA200800096 1 20080131 A 5270 PROXIMITY SWITCH CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT OUT OF ADJUST A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 904FJ 15004 ASH FLT 2627 CLT BHM - LT FORWARD EMERGENCY DOOR CAUTION WHEN AIRCRAFT IS DEPRESSURIZED. MX ADJUSTED PROX SWITCH. 2 L 7 2 4F RT A21EA 2008021100055 20080211 00055 EA 2008 2 11 CHQA200800023 1 20080204 A 4990 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE APU LOW A CHQA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 GL 11 473CA 7668 GEE873451 IAH TO MCI - DUE TO THE NR 2 IDG BEING ON MEL THE APU WAS REQUIRED TO BE RUN DURING THE FLIGHT. WHILE EN ROUTE TO MCI, THE CREW RECEIVED AN APU OIL TEMP CAUTION MESSAGE. THE CREW FOLLOWED THE QRH AND DIVERTED TO TUL. MAINTENANCE INSPECTE D THE APU AND FOUND THAT IT WAS LOW ON OIL. AFTER SERVICING THE OIL, THE APU OPERATED NORMALLY AND WAS RELEASED FOR SER VICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008021100062 20080211 00062 NM 2008 2 11 NWAA080376732 1 20080205 A 3244 TIRE BOEING 747 747251B 1384892 NM MLG WORN A NWAA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 01 632NW 23112 PERFORMED ABORTED TAKEOFF AT 120 KNOTS. EXPERIENCED HIGH VIBRATION DURING T/O ROLL THAT GOT WORSE AND A DRAGGING SENSAT ION FROM THE RIGHT SIDE OF AIRCRAFT. RETURNED TO GATE AND FOUND BOTH NOSE TIRES WORN ON LEFT EDGE. MAINTENANCE REMOVED AND REPLACED BOTH NOSE TIRES AND CHECKED ALL MAIN AND BODY TIRES FOR BRAKE FREE RUN. OPERATIONAL CHECKED GOOD AND AIRC RAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008021100064 20080211 00064 NM 2008 2 11 AALA200800149 1 20080123 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 767AJ 33539 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR LOWER GALLEY DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RIG HT NUMBER ONE DOOR LOWER GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021100065 20080211 00065 NM 2008 2 11 AALA200800150 1 20080123 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 767AJ 33539 DFW - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021100066 20080211 00066 NM 2008 2 11 AALA200800151 1 20080123 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 767AJ 33539 DFW - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021100069 20080211 00069 NM 2008 2 11 AALA200800141 1 20080123 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AA 27446 DFW - EMERGENCY LIGHT AT SEAT 17D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008021100070 20080211 00070 NM 2008 2 11 AALA200800143 1 20080123 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AA 27446 DFW - EMERGENCY LIGHT AT SEAT 22D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008021100076 20080211 00076 WP 2008 2 11 DHL2007873512 1 20080101 A 5512 SKIN DOUG DC8 DC873F 302199F WP HORIZONTAL STAB MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 89073 46091 LT HORIZ STAB ELEV HAS NON STANDARD REPAIR ON UPPER SKIN (STA XE 166.312 - 200.2379) MAJOR REPAIR. PERFORMED MAJOR REPA IR IAW SRM 55-4-1 FIG 1 SHEET 1, 2. REMOVED PANEL PLATING WITH NON-STANDARD REPAIR ON IT IAW SRM 55-1-0 PG 1, SRM 51-1- 21. FABRICATED PLATING AND FINGER DOUBLER BOTH FROM IAW SRM 55-4-1 FIG 1 SHEET 1-2 ITEM "E" "F". BONDED BOTH PARTS IAW SRM 51-1-9, SRM 51-1-9A, TR NR 51-142, TR NR 51-141. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF NEW PANEL PLAT ING IAW SRM 51-1-8B. INSTALLED NEW PANEL PLATING IAW SRM 51-1-21. PERFORMED WEIGHT AND BALANCE OF LT ELEV IAW SRM 51-4 -4 PG 1-4. FOUND WITHIN TOLERANCE. 2 L 7 4 4F RT 4A25 2008021100079 20080211 00079 NM 2008 2 11 AALA200800185 1 20080127 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 752AN 30260 DFW - EMERGENCY LIGHT AT SEAT ROW 25G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 25G. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021100089 20080211 00089 NM 2008 2 11 AALA200800157 1 20080123 A 3350 COVER BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 767AJ 33539 DFW - EMERGENCY LIGHT AT OVERHEAD AISLE LEFT NUMBER THREE DOOR HAS BROKEN COVER. REPLACED COVER FOR EMERGENCY LIGHT AT OVERHEAD AISLE LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021100093 20080211 00093 NM 2008 2 11 DLM88080130 1 20080128 A 3222 5920603509 STRUT DOUG MD88 MD88 3023688 NM NLG UNDERSERVICED A DALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 27 977DL 53258 NOSE GEAR UNSAFE LIGHT ON GEAR RETRACTION. NOISE INDICATED DOOR DID NOT SEQUENCE FULLY CLOSED. AUTOSPOILER INOP MESSAG E ALSO ILLUMINATED BUT EXTINGUISHED AFTER LANDING. QRH PROCEDURES COMPLETED TROUBLESHOT NOSE GEAR STRUT C/W OPN5006. F OUND NOSE STRUT UNDER SVCD. C/W OPN4703 NOSE STRUT SVC. MCC SET FOR RECHECK. CYCLED GEAR NUMEROUS TIMES TEST GOOD. 2 L 7 2 4F RT A6WE 2008021100113 20080211 00113 EA 2008 2 11 MASA200800070 1 20080127 A 5270 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR FALSE ACTIVATION A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 503MJ 10058 ASH 7144 ORD-ORF - PAX DOOR WARNING MSG. MX RAN ENGINES, RUNG WIRES IN THE DOOR HARNESS AND CHECKED ALL ASSOCIATED SWIT CHES AND COULD NOT DUPLICATE THE ISSUE. 2 L 7 2 4F RT A21EA 2008021100115 20080211 00115 NM 2008 2 11 UPS08B51611 1 20080201 A 2560 LATCH BOEING 747 74744AF 13848B2 NM SMOKE BARRIER OUT OF ADJUST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 571UP 35668 SMOKE BARRIER DOOR DOES NOT UNLATCH FROM OUTSIDE UPPER DECK. ADJUSTED DOOR LATCH PER EO B747-2520-28160B. OPS CHECK GO OD. 2 L 7 4 4F RT A20WE 2008021100120 20080211 00120 WP 2008 2 11 AALA200800079 1 20080116 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9403W 53139 LGA - EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD FIRS T CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008021100121 20080211 00121 WP 2008 2 11 AALA200800080 1 20080116 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9403W 53139 LGA - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008021100122 20080211 00122 NM 2008 2 11 AALA200800086 1 20080118 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 790AN 30251 JFK - EMERGENCY LIGHT AT SEAT 22C HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021100123 20080211 00123 NM 2008 2 11 070185 1 20080201 A 7430 5D04232 IGNITION SWITCH DOUG MD88 MD88 3023688 NM COCKPIT FAILED A WX0A O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 19 401NV 49761 DURING PREFLIGHT CHECK WITH EMERGENCY POWER SWITCH "ON", SMOKE EMITTED FROM THE OVERHEAD PANEL. ELECTRICAL POWER WAS DI SCONNECTED FROM THE AIRCRAFT AND THE SMOKE IN THE COCKPIT DISSIPATED. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE OV ERHEAD PANEL AND DETERMINED THE ROTARY IGNITION SWITCH TO BE MALFUNCTIONING. THE SWITCH WAS REPLACED, ELECTRICAL POWER RESTORED TO THE AIRCRAFT AND ALL EFFECTED SYSTEMS OPERATIONAL CHECKED NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008021100127 20080211 00127 EU 2008 2 11 UPS08151491 1 20080121 A 3350 LAMP AIRBUS A300 A300F4622R 3930360 EU EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 149UP 0832 EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP. OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 2008021100129 20080211 00129 WP 2008 2 11 UPS08851485 1 20080110 A 5320 BRACKET DOUG DC8 DC871F 302199D WP FS 1260 L33R MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 BRACKET MISSING BETWEEN STA 1260 FRAME AND INTERCOSTALS AT L33R. INSTALLED BRACKET AT FRAME 1260 L33 R IAW SRM 51-1-20D, AND SRM 51-03-02. 2 L 7 4 4F RT 4A25 2008021100132 20080211 00132 WP 2008 2 11 UPS08851536 1 20080109 A 5280 DOOR DOUG DC8 DC871F 302199D WP FS 960 LBL 60 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 L/MLG DOOR SWITCH MOUNT HOLES ARE ELONGATED. FABRICATED AND INSTALLED REPAIR DOUBLER ON LT MLG DOOR SWITCH MOUNT FRAME IAW EO DC8-3260-16914-A. 2 L 7 4 4F RT 4A25 2008021100143 20080211 00143 SO 2008 2 11 SWIA200819172 1 20080127 A 3397 TERMINAL EMB 120 EMB120ER 3260203 SO RCCB BURNED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 227SW 120304 FLT 5744 - CLICKING COULD BE HEARD FROM CAPTAINS SIDE PANEL ALONG WITH ELECTRICAL ODOR. REPLACED TERMINAL ON TAXI LIGHT RCCB. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008021100144 20080211 00144 WP 2008 2 11 UPS08851601 1 20080114 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 CABIN FLOOR PNL F212 CRACKED. REPAIRED CABIN FLOOR PNL. PER SRM 51-1-19. 2 L 7 4 4F RT 4A25 2008021500175 20080215 00175 NM 2008 2 15 SWAA080702 1 20080206 A 5311 6545805 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008021500176 20080215 00176 NM 2008 2 15 SWAA080703 1 20080206 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008021500177 20080215 00177 NM 2008 2 15 SWAA080704 1 20080206 A 5310 6516352 DOOR FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 2008021500186 20080215 00186 NM 2008 2 15 SWAA080712 1 20080207 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021500189 20080215 00189 NM 2008 2 15 SWAA080733 1 20080207 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008021500192 20080215 00192 NM 2008 2 15 SWAA080715 1 20080207 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 460, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008021500196 20080215 00196 2008 2 15 SWAA080719 4 20080207 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 455WN 32462 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008021500197 20080215 00197 2008 2 15 SWAA080720 4 20080207 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 498WN 32480 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008021500199 20080215 00199 NM 2008 2 15 SWAA080723 1 20080207 A 5311 6545805 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008021500201 20080215 00201 NM 2008 2 15 SWAA080722 1 20080207 A 5311 6545808 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294, STR 6R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008021500205 20080215 00205 NM 2008 2 15 SWAA080728 1 20080207 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008021500212 20080215 00212 EU 2008 2 15 2008UALA00484 1 20080128 A 3350 D9239003500060 EPSU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 496UA 1845 EMERGENCY LIGHTS FAIL TEST WITH EPSU FWD L EFG MSG. EPSU FAILURE. REPLACED EPSU. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021500217 20080215 00217 EU 2008 2 15 2008UALA00513 1 20080130 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 470UA 1427 CREW O2 NEEDS SERVICING 1420 PSI. SERVICED CREW O2 TO FULL, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021500220 20080215 00220 EU 2008 2 15 2008UALA00547 1 20080131 A 5210 CYLINDER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 446UA 834 DOOR ASSIST ACCUMULATOR AT 2L NEEDS SERVICING. SERVICED DOOR ASSIST CYLINDER AT DOOR 2L. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021900001 20080219 00001 NM 2008 2 19 BB08013 1 20080209 A 3350 BR9279109 LIGHT BOEING 757 7572B7 1384964 NM ZONE 200 FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 938UW 27246 FLL - EMERGENCY EXIT SIGN AT LEFT AFT DOOR INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F RT A2NM 2008021900002 20080219 00002 NM 2008 2 19 BB08014 1 20080209 A 2740 285T0015117 MODULE BOEING 757 757225 1384959 NM STAB TRIM LKOUT FAILED A USAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 EA 19 922UW 67533 27582 22202 FLT NR 1586 - ON FINAL JUST BELOW 1,000 FT AGL 27R, A/P OFF, A/T OFF, REF 138, WIND 280 AT 14 KTS THE A/C PITCHED UP ABO UT 8 FT ROLLED RT. CREW PUSHED A/C NOSE DOWN AND BANKED BACK LEFT. 15 SECONDS LATER DID THE SAME THING DID NOT FEEL AN Y WAKE TURBULENCE. CREW GOT STAB WARNING LIGHT ON EICAS AND OVERHEAD. MADE NORMAL LANDING. WAS NOT STAB NO CUTOUT NEE DED. MAINTENANCE REMOVED AND REPLACED MODULE ASSY STAB TRIM/AILERON LOCKOUT. 2 L 7 2 4F RT A2NM 2008021900005 20080219 00005 NM 2008 2 19 2008UALA00621 1 20080204 A 3350 276005 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP, 4 EACH. REPLACED FUSE & LAMP, OP CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021900009 20080219 00009 NM 2008 2 19 2008UALA00623 1 20080204 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 UPPER DECK CEILING EMERGENCY LIGHT INOP AT SEAT ROW 12-13. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021900020 20080219 00020 NM 2008 2 19 2008UALA00629 1 20080203 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY SILL LIGHT DOOR5 LT FWD INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021900021 20080219 00021 SO 2008 2 19 RAIA00801033 1 20080130 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 805HK 145096 PRE FLT NR 3538 - PIAT - EMERGENCY LIGHT ON AIRSTAIR HANDRAIL INOPERATIVE. MAINTENANCE DEFERRED THIS LIGHT IN ACCORDANC E WITH MEL. 2 L 7 2 4F RT T00011AT 2008021900022 20080219 00022 SO 2008 2 19 RAIA00802001 1 20080201 A 5210 NAS6204460 BOLT EMB 145 EMB145LR 3260212 SO PAX DOOR BROKEN A RAIA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 03 849HK 145002 POST FLT NR 7961 - IAD - MAIN CABIN DOOR ROCKER-ARM AND CAM ASSEMBLY HAS A BOLT THAT SHEARED OFF. MAINTENANCE REMOVED A ND REPLACED THE BOLT AND SPACER 2 L 7 2 4T RT T00011AT 2008021900024 20080219 00024 NM 2008 2 19 2008UALA00630 1 20080202 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 WALL EEL INOP LT SIDE MID LAVS WALL. REPLACED FEEDER WIRE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021900025 20080219 00025 NM 2008 2 19 2008UALA00631 1 20080202 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY LIGHTS INOP DOOR 1R SILL FWD AND AFT. RELAMPED EMERGENCY LIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021900027 20080219 00027 NM 2008 2 19 2008UALA00636 1 20080202 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 SEAT EEL INOP ROW 30L. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021900035 20080219 00035 EA 2008 2 19 TRAX200800216 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 477-581 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 RT FLOOR SEAT RAIL FS 477.40 TO FS 581.0 AT LBL 9.0 HAS CORROSION DAMAGE ON RAIL AND HARDWARE. THIS SDR WILL REMAIN OPE N PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. 2 L 7 2 4F RT A21EA 2008021900041 20080219 00041 2008 2 19 2008UALA00659 4 20080205 A 2565 5A29011 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA PA2722 25394 ASPIRATOR LEAKING. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021400034 20080214 00034 EA 2008 2 14 TRAX200800185 1 20080203 A 5220 HANDLE CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 CREW ESCAPE HANDLE CORRODED. 2 L 7 2 4F RT A21EA 2008021400084 20080214 00084 EU 2008 2 14 08FDEA00384 1 20080211 A 5320 A53612213216 FLOOR SUPPORT AIRBUS 330 A300* EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION ON FLOOR SUPPORT C 11-17, Y-1456 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A26NM 2008021400101 20080214 00101 NM 2008 2 14 QXEA200800074 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - RIGHT INBOARD SEAT TRACK NR 7 HAS APPROX .060 GOUGE ON THE OUTBOARD FLANGE AT APPROX X256. MAINTENANCE REMOVED TRACK AND INSTALL NEW TRACK. 2 H 7 2 4T RT A13NM 2008021400110 20080214 00110 EU 2008 2 14 TRBA2008021 1 20080209 A 5610 NP1588014 WINDSHIELD AEROSP ATR72 ATR72212 8680945 EU COCKPIT BROKEN A TRBA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 29 308AE 309 F/O WINDSHIELD CRACKED AT 17,000 FT, CRUISING ALTITUDE, NO WINDSHIELD HEATER FAULT INDICATION. REMOVED AND REPLACED WIN DSHIELD IAW JIC 56-11-00. PERFORMED OPT AND FUSELAGE PRESSURIZATION LEAK TEST IAW JIC 05-53-00. 2 H 7 2 4T RT A53EU 2008021400111 20080214 00111 NM 2008 2 14 KCSA081074 1 20080212 A 5320 WEB BOEING 747 747209B 138489B NM PAX DOORWAY CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 NR 3R MAIN ENTRY DOOR BOTTOM WEB TOP SURFACE CORRODED, BS 1280. 2 L 7 4 4F RT A20WE 2008021400131 20080214 00131 NM 2008 2 14 QXEA200800108 1 20080114 A 5320 INTERCOSTAL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - CORROSION ON AVIONICS RACK INTERCOSTAL AT FS X202 TO FS 198.300 OUTBOARD OF STRINGER 31L. MAINTENANCE REMOVED CORROSION, INSPECTED, BLENDED AREA REMAINED WITHIN LIMITS WITH NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021400142 20080214 00142 NM 2008 2 14 QXEA200800107 1 20080114 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - SPOT OF CORROSION ON THE INNER SKIN AROUND RIVET HOLE FORWARD OF FRAME STA 201 OUTBOARD OF STRINGER 31L . MAINTENANCE REMOVED MINOR CORROSION, INSPECTED, BLENDED AREA REMAINED WITHIN LIMITS WITH NO CRACKS NOTED. RESTORED F INISH TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021400145 20080214 00145 NM 2008 2 14 QXEA200800081 1 20080114 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 106 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - SCRATCH AND SMALL DENT AT APPROXIMATELY STA X106.00 AND APPROXIMATELY 4 INCHES ABOVE PANEL 112BR RIGHT EXTERNAL FUSELAGE. MAINTENANCE BLENDED AREA OF SCRATCH TO REMOVE DAMAGE, STILL WITHIN LIMITS AND INSPECTED NO CRACKS NO TED. RESTORED FINISH. 2 H 7 2 4T RT A13NM 2008021400165 20080214 00165 NM 2008 2 14 08FDEA00410 1 20080212 A 5330 65545777 SKIN BOEING 727 727233 138408A NM BS 720E-722E CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 LT WING TO BODY FUSELAGE SKIN SURFACE SHOWS CORROSION AND GOUGE AT LAP JOINT STA 720E, STR 19L. BURNISHED AFFECTED AREA AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG1,2. REMOVED FAIRING FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGE DIM 43/4 X 2 3/4. FABRICATED DOUBLER, FILLER IAW SRM 53-30-3 FIG6 AND 53-30-2 FIG2. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALL ED REPAIR PARTS IAW SRM 53-30--3 FIG6 AND 51-30-2. REINSTALLED BODY FAIRING IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2008021400183 20080214 00183 NM 2008 2 14 CALA0800104 1 20080130 A 5340 651768559 ATTACH FITTING BOEING 737 7373T0 1384582 NM BS 360 S11L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FORWARD ENTRY WEB AFT SUPPORT CLIP AT INTERCOSTAL 11L STA 360 IS CRACKED. REMOVED AND REPLACED CLIP PER ECRA 5311-01392 . 2 L 7 2 4F RT A16WE 2008021400185 20080214 00185 EA 2008 2 14 MASA200800112 1 20080210 A 3520 BOTTLE CNDAIR CL600 CL6002B19 1900309 EA OXYGEN SYSTEM LOW A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 97325 7325 ASH FLT 2777 PHX-BFL - PORTABLE O2 BOTTLE WAS LOW AT 1500 PSI. MX SERVICED THE BOTTLE TO 1850 PSI. 2 L 7 2 4F RT A21EA 2008021400188 20080214 00188 EA 2008 2 14 MASA200800115 1 20080210 A 5220 SEAL CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 930FJ 15030 ASH FLT 2824 PHX-TUS - LOUD SQUEAL AT EMERGENCY EXIT 16A. CLEANED AND LUBED SEAL, OPS GOOD. 2 L 7 2 4F RT A21EA 2008021500004 20080215 00004 EU 2008 2 15 2008UALA00589 1 20080201 A 2920 BLADES AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RAM AIR TURB BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 422UA 503 RAM AIR TURBINE BLADE BENT DURING RAT CHECK. ACCIDENTAL DAMAGE TO RAT BLADES. REPLACED THE RAT ASSY, ALL OPS CHECKS ACCOMLISHED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021500005 20080215 00005 NM 2008 2 15 2008UALA00591 1 20080201 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 846UA 1600 CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED CREW O2 TO 1740, HELD PRESSURE FOR 3 HOURS- NO L EAKS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021500006 20080215 00006 NM 2008 2 15 2008UALA00557 1 20080128 A 2560 O-RING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1R OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 DR 1R NO ARM AT DEPARTURE. FOUND O-RING IN THE WAY OF ARMING LEVER. REPOSITIONED O-RING, ARMS/DISARMS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021500007 20080215 00007 NM 2008 2 15 2008UALA00567 1 20080131 A 5320 WEB BOEING 737 737322 1384676 NM MID CABIN CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 MID CABIN PRESSURE DECK WEB CRACKED AT BS 663 AT LBL 32. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED REPAIR DOUB LER. 2 L 7 2 4F RT A16WE 2008021500021 20080215 00021 EU 2008 2 15 2008UALA00663 1 20080205 A 3510 MXP401600U OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 429UA 539 CAPTAIN'S OXYGEN MASK NO TEST. FOUND LEAK WITHIN THE STORAGE BOX ASSY. REPLACED FAULTY STOWAGE BOX ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021500052 20080215 00052 SO 2008 2 15 RAIA0802014 1 20080213 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 805HK 145096 PRE FLT NR 3562 - STL - SEVERAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RESEATED THE CONNECTOR AT THE NR 2 EMERGENCY POWER SUPPLY. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2008021500062 20080215 00062 NM 2008 2 15 2008UALA00033 1 20080102 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 UPPER EXTERNAL FUSELAGE SKIN IS WORN IN SEVERAL AREAS UNDERNEATH DORSAL FIN ON LT AND RT SIDE FROM STA 860-907. MAJOR R EPAIR: FABRICATED AND INSTALLED SINGLE DOUBLER AND SPLICE STRAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500070 20080215 00070 NM 2008 2 15 HALA0800115 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1040 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45 SEAT TRACK AT LBL 11, HAS DAMAGE TO SEAT TRACK CROWN AT STA1040. CORROSION REMOVED, CONFIR MED BY 10X MAGNIFICATION, IAW SRM 51-10-02 REV 76, BLENDED WITHIN LIMITS, IAW SRM 53-00-52/101 REV 75. 2 L 7 2 4F RT A1NM 2008021500075 20080215 00075 NM 2008 2 15 HALA0800107 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1061-1069 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45 SEAT TRACKS, AT RBL 11, STA.1061-1069. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION I AW SRM 51-10-02, REV 75, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101 REV 76. 2 L 7 2 4F RT A1NM 2008021500080 20080215 00080 SO 2008 2 15 C2XA08CL018 1 20080203 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13968 145138 DURING ROUTINE MAINTENANCE, THE EXIT MARKER LIGHT AT ROW 3 BC WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008021500082 20080215 00082 NM 2008 2 15 HNAA0800059 1 20080207 A 3220 XD4N RELAY DHAV DHC8 DHC8102 2809003 NM MLG FAILED A HNAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 07 908HA 57637 57637 015 WHEN LANDING GEAR WAS SELECTED DOWN, THE NOSE GEAR SHOWED AN UNSAFE INDICATION. THE ALTERNATE EXTENSION SYSTEM WAS USED FOR THE NOSE GEAR. THE MAIN GEAR OPERATED NORMALLY WITH NO OTHER CAUTION OR WARNING INDICATIONS. MAINTENANCE SWUNG TH E NOSE GEAR, NOTING NO DEFECTS IN THE SYSTEM. THE DRAG STRUT PROXIMITY SENSOR WAS CHECKED AND ADJUSTED, AND THE 3261-K7 RELAY WAS CHANGED. ENTIRE AIRCRAFT WAS THEN JACKED AND FULL GEAR SWINGS WERE DONE. NO DEFECTS WERE NOTED AT THAT TIME AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 2008021500083 20080215 00083 NM 2008 2 15 2008UALA00203 1 20080114 A 2842 HG1064AA07 PROCESSING UNIT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUEL SYSTEM FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 510UA 24780 FLIGHT DIVERTED DUE TO A FUEL QUANTITY PROBLEM. FUEL QTY PROCESSOR UNIT FAULTY. REPLACED THE FQPU, ALL SYSTEMS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021500084 20080215 00084 NM 2008 2 15 HNAA0800060 1 20080206 A 2612 6504 CONTROL MODULE DHAV DHC8 DHC8102 2809003 NM FIRE HANDLE FAILED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 906HA 31488 19742 9 WHEN TESTED, THE NR 1 ENGINE FIRE EXTINGUISHER 'T' HANDLE WOULD NOT ILLUMINATE. MAINTENANCE CLEANED THE ELECTRICAL CONN ECTOR BETWEEN THE 'T' HANDLE AND SHAFT, THEN REPLACED THE NR 1 FIRE DETECTION CONTROL MODULE. SYSTEM WAS CHECKED IAW MM PROCEDURES AND OPS CHECKED GOOD. AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 2008021500089 20080215 00089 NM 2008 2 15 SWAA080808 1 20080212 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 493WN 32477 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008021500091 20080215 00091 NM 2008 2 15 SWAA080810 1 20080212 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 867-887 S24R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 867 AND BS 887, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008021500093 20080215 00093 NM 2008 2 15 SWAA080809 1 20080212 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 747 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008021500094 20080215 00094 NM 2008 2 15 SWAA080811 1 20080212 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM BS 450 S24R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 450, STR 24R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008021500095 20080215 00095 SO 2008 2 15 C2XA08RI016 1 20080211 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16918 145397 FLIGHT 2301 - EWR - CREW REPORTED MAIN CABIN DOOR HARD TO OPEN. EWR MX LUBRICATED MAIN CABIN DOOR SEAL AND PERFORMED OP ERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008021500096 20080215 00096 NE 2008 2 15 495 2 20080120 A 7261 23060420 MAGNETIC SEAL BELL 430 430 1182150 SW ALLSN 250C 250C40B 03032 NE NR 2 ENGINE LEAKING E AC2A E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 31 430CT 49089 844192 NOTICED FLUCTUATING ENGINE OIL PRESSURE ON NR 2 ENGINE. PULLED OUT AIRCRAFT EMERGENCY PROCEDURE CHECKLIST. FOLLOWED EM ERGENCY PROCEDURE. OIL PRESSURE DECREASED BELOW 52.5± 2.5 PSI. SECURED NR 2 ENGINE. COMPLETED RUN ON LANDING ON THE G RASS STRIP AT INTRACOASTAL CITY. COMPLETED AIRCRAFT SHUTDOWN ACCORDING TO CHECKLIST. NO EXCEEDANCES ON AIRCRAFT. 1 G 7 2 3U 3 U RT H9SW E1GL 2008021500098 20080215 00098 NM 2008 2 15 2008UALA00448 1 20080127 A 3350 BATTERY BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FLASHLIGHT DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 307UA 23668 AFT F/A FLASHLIGHT INOPERATIVE. REPLACED BATTERY. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500116 20080215 00116 NM 2008 2 15 2008UALA00564 1 20080201 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 642UA 25092 FUSELAGE SKIN APPROX STA 280 BETWEEN STR 2L & 3L HAS BLEND MARKS. MAJOR REPAIR ACCOMPLISHED: MFG'D AND INSTALLED REPAI R DOUBLER WITH BLIND FASTENERS. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500132 20080215 00132 NM 2008 2 15 2008UALA00580 1 20080201 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 NEAR DOOR 3L LOWER SIDEWALL EMERGENCY LIGHT IS INOP. REPLACED FEEDER WIRE ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021500133 20080215 00133 NM 2008 2 15 2008UALA00581 1 20080201 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 653UA 25391 FWD RIGHT GALLEY EMERGENCY LIGHT STRIP (EEL) INOP. REMOVED AND REPLACED LIGHT STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500155 20080215 00155 NM 2008 2 15 2008UALA00617 1 20080203 A 3350 AD071701100 POWER SUPPLY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 774UA 26936 ALL EMERGENCY LIGHTS ON SEATS IN AFT SECTION OF COACH ARE INOP. REPLACED EMERGENCY POWER SUPPLY AT DOOR 3R. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021500168 20080215 00168 NM 2008 2 15 SWAA080695 1 20080206 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2008021500170 20080215 00170 NM 2008 2 15 SWAA080697 1 20080206 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 417WN 29822 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008021500187 20080215 00187 NM 2008 2 15 SWAA080713 1 20080207 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021500206 20080215 00206 NM 2008 2 15 SWAA080729 1 20080207 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008021500207 20080215 00207 NM 2008 2 15 SWAA080730 1 20080207 A 5313 6551698 STRINGER SPLICE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2008021500210 20080215 00210 NM 2008 2 15 2008UALA00264 1 20080114 A 4940 27044424 STARTER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE APU FAULTY A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 784UA 26951 APU APUC DETECTED FAULT THAT WOULD CAUSE AUTOMATIC SHUTDOWN OF APU IN UNATTENDED MODE OPERATION, OR COMPLETE LOSS OF APU C BUSS ACTIVITY (BOTH L AND R 629) FOR 3 SECONDS AFTER THE APU MASTER CONTROL SWITCH HAS BEEN IN THE ON POSITION FOR TEN APU CONTROLLER DETECTED FAULT THAT WOULD CAUSE AUTOMATIC SHUTDOWN OF APU IN UNATTENDED MODE OPERATION, OR COMPLETE LOSS OF APUC BUSS ACTIVITY. REPLACED FAILING ELECTRIC START MOTOR. APU STARTED. NO APUC MESSAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021500213 20080215 00213 NE 2008 2 15 2008UALA00485 2 20080128 A 7261 OIL SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 ENGINE LEAKING A UALA O OTHER W K B INADEQUATE Q C FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 803UA 748 V12177 CREW COMMENTS: OIL SMELL IN CABIN, WORSE ONCE AIRBORNE. OIL LEAKAGE DUE TO BEARING FAILURE. SMELL WAS NEVER TRACED TO A PARTICULAR COMPONENT, HOWEVER THE NR 1 ENG WAS REPLACED DUE TO AN OIL LEAK AROUND 4TH STAGE IGV AT 6 O'CLOCK POS AND LEASE RETURN AGREEMENTS. THE APU WAS ALSO REPLACED SHORTLY AFTERWARD WITH OIL LEAK ISSUES. AFTER ALL MTC, THE A/C HAS REMAINED CLEAR OF GRIPES FOR OIL SMELL IN CABIN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021900004 20080219 00004 NM 2008 2 19 2008UALA00620 1 20080204 A 3350 CONTACT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EEL INOP SEAT 51C. REPLACED CONTACT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021900040 20080219 00040 NM 2008 2 19 HALA0800047 1 20080110 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 425 S2L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LIGHTING STRIKE ON A/C CROWN AT LOACTION, STA 425, S2L. REPAIRED IAW 767-300, SRM 53-00-01, REPAIR 8. 2 L 7 2 4F RT A1NM 2008021900043 20080219 00043 NM 2008 2 19 HALA0800049 1 20080110 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 517 S2L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LIGHTING STRIKE ON A/C CROWN AT LOCATION, STA 517, BELOW S2L. REPAIRED IAW 767-300, SRM 53-00-01, REPAIR 8. 2 L 7 2 4F RT A1NM 2008021900054 20080219 00054 EU 2008 2 19 AALA200800200 1 20080129 A 2150 A/C PACK AIRBUS 300 A300B4605R 3930308 EU RIGHT DIRTY A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 21 80084 675 BOG INFLIGHT T913/29JAN - FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN WITH LAVATORY SMOKE DETECTOR ALARM SOUNDING. SMOKE INCREASED UNTIL LANDING THEN DISSIPATED. ISOLATED ODOR TO RIGHT PACK. PERFORMED PACK BURN. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A35EU 2008021900057 20080219 00057 EU 2008 2 19 AALA200800196 1 20080129 A 2910 LINE AIRBUS 300 A300B4605R 3930308 EU HYDRAULIC SYS LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 11060 470 SJU INFLIGHT T1692/29JAN - CREW REPORTED HYDRAULIC ODOR IN CABIN AROUND SEAT ROW 17AB. RETURNED TO SJU AND LANDED WITHO UT INCIDENT. FOUND HYDRAULIC LEAK AT SEAT ROW 16AB. REPAIRED HYDRAULIC LINE AT SEAT ROW 16AB AND CLEANED AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008021900058 20080219 00058 NM 2008 2 19 AALA200800197 1 20080129 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 776AN 29582 JFK - EMERGENCY LIGHT AT SEAT 39C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 36C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900071 20080219 00071 NM 2008 2 19 CALA0800123 1 20080212 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM BS 400 S8L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 PAX CABIN HAS FRAME CRACKED AT STA 400 BETWEEN STRINGER 8L AND 9L. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04714. 2 L 7 2 4F RT A16WE 2008021900072 20080219 00072 NM 2008 2 19 CALA0800124 1 20080212 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM BS 907 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 FRAME CRACKED AT STA 907 ABOVE STRINGER 9R. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04714. 2 L 7 2 4F RT A16WE 2008021900079 20080219 00079 NM 2008 2 19 HALA0800054 1 20080110 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 287 S3L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LIGHTING STRIKE ON A/C CROWN AT LOCATION, 287, ABOVE S3L. REPAIRED IAW 767-300, SRM 53-00-01, REPAIR 8. 2 L 7 2 4F RT A1NM 2008021900081 20080219 00081 NM 2008 2 19 HALA0800056 1 20080110 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 800 S2L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LIGHTING STRIKE ON A/C CROWN LOCATION, STA 800, S2L. REPAIRED IAW 767-300 SRM 53-00-01, REPAIR 8. 2 L 7 2 4F RT A1NM 2008021900082 20080219 00082 NM 2008 2 19 CALA0800087 1 20080201 A 5610 58935841 WINDSHIELD BOEING 737 737824 13844BZ NM COCKPIT DELAMINATED A CALA O OTHER O OTHER NR NOT REPORTED 1 SW 27 14250 28957 L5 WINDOW FAILED INTERNALLY AND THE OUTER LAMINATION BECAME SEPARATED FROM ITS ASSEMBLY. REMOVED AND REPLACED L5 WINDOW PER MM 56-11-31-000-801. 2 L 7 2 4F RT A16WE 2008021900083 20080219 00083 NM 2008 2 19 HALA0800057 1 20080110 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 836 S2L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LIGHTING STRIKE ON A/C CROWN AT LOCATION, STA 836, S2L. REPAIRED IAW 767-300, SRM 53-00-01, REPAIR 8. 2 L 7 2 4F RT A1NM 2008021900089 20080219 00089 SO 2008 2 19 RAIA00802007 1 20080205 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT SMOKE A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 846HK 14500855 FLT 7882 - CREW REPORTED SMOKE IN THE COCKPIT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE WINDSHIELD HEATING SYSTE M AND ASSOCIATED CONNECTORS. MAINTENANCE ALSO INSPECTED ALL COCKPIT LIGHTS AND CONNECTIONS. NO MALFUNCTION WERE NOTED. 2 L 7 2 4T RT T00011AT 2008021900091 20080219 00091 SO 2008 2 19 RAIA00802006 1 20080205 A 3260 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO NLG DEFECTIVE A RAIA O OTHER N FALSE WARNING LD LANDING 1 CE 03 823HK 145475 FLT NR 7903 - TUL - NOSE LANDING GEAR UNSAFE MESSAGE AND LANDING GEAR LEVER DISAGREE MESSAGES ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE RIGHT PROXIMITY SENSOR. OPERATIONALLY CHECKED GOOD AFTER CORRECTIVE ACTION. 2 L 7 2 4T RT T00011AT 2008021900093 20080219 00093 SO 2008 2 19 RAIA00802004 1 20080204 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 807HK 145119 PRE FLT NR 8006 -RIC-EMERGENCY FLOOR PROXIMITY LIGHT INOPERATIVE. MAINTENANCE RESEATED THE CONNECTOR TO THE AFFECTED LI GHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT T00011AT 2008021900097 20080219 00097 WP 2008 2 19 G60A200800021 1 20080208 A 5712 RIB DOUG DC10 DC1030F 3023504 WP RT WING CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 607GC 46978 RT WING REFUEL/DEFUEL BAY OUTBD RIB LWR AFT END CRACKED 1.5 INCH. 2 L 7 3 4F RT A22WE 2008021900108 20080219 00108 NM 2008 2 19 AALA200800218 1 20080130 A 3350 D71702100 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHTS AT LEFT AND RIGHT SEAT ROWS 1 TO 4 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LE FT AND RIGHT SEAT ROWS 1 TO 4. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900109 20080219 00109 NM 2008 2 19 AALA200800219 1 20080130 A 3350 D71702100 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHTS AT LEFT AND RIGHT SEAT ROWS 9 TO 13 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT L EFT AND RIGHT SEAT ROWS 9 TO 13. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900110 20080219 00110 WP 2008 2 19 AALA200800223 1 20080131 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 587AA 53250 LGA - EMERGENCY LIGHT BATTERY PACK AT SEAT ROW 8 WEAK. REPLACED BATTERY PACK AT SEAT ROW 8 CEILING FOR EMERGENCY LIGHTS . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008021900117 20080219 00117 EA 2008 2 19 MASA200800126 1 20080212 A 5210 WA670310381 STRUT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNKNOWN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 7337 FLT 2740, PSP-PHX - MAIN CABIN DOOR WILL NOT CLOSE. REPLACED DOOR ACTUATOR STRUT AND BRACKETS. 2 L 7 2 4F RT A21EA 2008021500064 20080215 00064 NM 2008 2 15 F3LA200800054 1 20080211 A 5320 D53476080206 PLATE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 902FR 5564 1515 DURING C7 C CHECK, WHILE PERFORMING AN INSPECTION FOR "OK TO INSTALL PARTS," INSPECTION REPORTED DAMAGE WAS FOUND TO THE CORNER PROFILE PLATE ON STRINGER 38 LT, BETWEEN FRAMES 59 AND 59. MAINTENANCE FABRICATED AND INSTALLED A DOUBLER ON TH E PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30027. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOU ND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008021500072 20080215 00072 NM 2008 2 15 2008UALA00040 1 20080102 A 5320 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FWD GALLEY DOOR CUTOUT INTERCOSTAL ATTACH ANGLE CRACKED AT BS 277-294.5 BETWEEN STRINGERS 11R & 12R. MAJOR REPAIR: REP LACED ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500106 20080215 00106 2008 2 15 2008UALA00555 4 20080129 A 2565 2A1459 DISK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EVAC SLIDE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 196UA 28715 LOW BOTTLE. BURST DISK LEAKING. REPLACED BURST DISK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021500142 20080215 00142 NM 2008 2 15 2008UALA00597 1 20080201 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 360 S14-15L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FWD ENTRY DOOR CUTOUT, BS 360 FRAME SHEAR TIE CRACKED BETWEEN STR 14L & 15L. INSTALLED NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500154 20080215 00154 NM 2008 2 15 2008UALA00616 1 20080203 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 672UA 30027 EEL STRIP AT SEAT 33A MISSING. REPLACED MISSING EEL LIGHT, OP CHECKS OK. RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500183 20080215 00183 2008 2 15 SWAA080709 4 20080206 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 250WN 34972 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008021500191 20080215 00191 NM 2008 2 15 SWAA080714 1 20080207 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, STR 28L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008021500219 20080215 00219 EU 2008 2 15 2008UALA00546 1 20080131 A 5210 CYLINDER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R1 DOOR LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 446UA 834 DOOR ASSIST ACCUMULATOR AT 1R NEEDS SERVICING. SERVICED DOOR ASSIST CYLINDER AT DOOR 1R. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021900014 20080219 00014 NM 2008 2 19 MASA200800104 1 20080206 A 5210 601R3862427 PRESSURE VALVE DHAV DHC8 DHC8202 2809007 NM DOOR SEAL MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 436YV 436 FLT 7075 - PASSENGER DOOR HARD TO OPEN. INFLATABLE DOOR SEAL NOT DEFLATING PROPLERLY. REPLACED PRESSURE VALVE, ELBOWS, AND TUBING. OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2008021900017 20080219 00017 NM 2008 2 19 2008UALA00628 1 20080203 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT ROW 5F AFT INOP. RESECURED LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021900051 20080219 00051 NM 2008 2 19 2008UALA00665 1 20080205 A 2432 425402 CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MASTER BATTERY FAULTY A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 187UA 26877 BATTERY CHARGER MAIN STATUS MSG DISPLAYED. SUSPECT FAULTY BATTERY CHARGER. REPLACED MAIN BATTERY CHARGER PER MM-24-31-0 2 MAIN BATTERY PER MM24-31-01. OPS CHECKED NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021900070 20080219 00070 NM 2008 2 19 CALA0800122 1 20080212 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM BS 440 S8L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 PAX CABIN HAS FRAME CRACKED AT STA 440 BETWEEN STRINGER 8L AND 9L. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04714. 2 L 7 2 4F RT A16WE 2008021900076 20080219 00076 NM 2008 2 19 CALA0800105 1 20080131 A 5313 656966412 STRINGER BOEING 737 7373T0 1384582 NM BS 357 S23R CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 CORROSION AT STA 357 STRINGER 23R REPAIRED PER ECRA 5311-01391. 2 L 7 2 4F RT A16WE 2008021900113 20080219 00113 NM 2008 2 19 AALA200800203 1 20080129 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 796AN 30796 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 22C . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900118 20080219 00118 EA 2008 2 19 MASA200800127 1 20080212 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PBE MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75991 7422 ASH FLT 7242 IAD-PHL - CAPTAIN'S PBE MISSING INSPECTION STICKER. MX INSPECTED THE PBE AND INSTALLED A NEW STICKER. 2 L 7 2 4F RT A21EA 2008021900126 20080219 00126 NM 2008 2 19 CALA0800092 1 20080129 A 5311 BAC15171470 FRAME BOEING 737 7373T0 1384582 NM BS 867 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FUSELAGE FRAME IS CRACKED AT STA 867 BETWEEN STRINGER 8L AND 9L. REPAIRED PER ECRA 5310-04697. 2 L 7 2 4F RT A16WE 2008021100145 20080211 00145 EA 2008 2 11 MASA200800067 1 20080125 A 5220 HANDLE CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 932LR 15032 ASH 2623 CLT-MCI - EMERGENCY EXIT PULL HANDLE COVER ROW 16A WILL NOT STAY CLOSED. MX RESECURED HANDLE. 2 L 7 2 4F RT A21EA 2008021100154 20080211 00154 WP 2008 2 11 AALA200800182 1 20080127 A 3232 ACTUATOR DOUG DC9 DC982 3022082 WP MLG DOOR BROKEN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 430AA 49342 STL INFLIGHT T1295/27JAN - AFTER LANDING GEAR RETRACTION CREW REPORT MODERATE VIBRATION. RETURNED TO STL AND LANDED WIT HOUT INCIDENT. FOUND RIGHT NOSE GEAR DOOR ACTUATOR ATTACH FORK BROKEN AND FOLLOW UP ROD END BRACKET. REPLACED RIGHT FO RWARD DOOR, DOOR LINK , DOOR LINK PIN, DOOR STOP LINK AND DOOR STOP PUSH ROD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008021100155 20080211 00155 2008 2 11 UPS08M51584 4 20080129 A 2565 COVER DOUG MD11 MD11F 3023600 NM L1 DOOR SLIDE UNSECURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP 48745 L1 ENTRY DOOR ESCAPE SLIDE COVER WILL NOT STAY SECURED TO MAG HOLDERS HANGS OPEN WHEN DOOR IS NOT CLOSED. SECURED L1 SL IDE COVER REF 25-61-15. 2 L 7 3 4F RT A22WE 2008021100157 20080211 00157 EU 2008 2 11 MALA080019 1 20080201 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 435XJ 340B435 RIGHT EXTERIOR EMERGENCY LIGHT 4LN FAILED TO ILLUMINATE. FOUND POWER SUPPLY 24LN TO BE BAD. REMOVED AND REPLACED AFT E MERGENCY PWR SUPPLY 24LN IAW SAAB AMM 33-50-10-04-01. 2 L 7 2 4T RT A52EU 2008021100162 20080211 00162 WP 2008 2 11 UPS08851567 1 20080110 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP FS 1190 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 C-PIT TORQUE BOX REPAIR DOUBLER GOUGED, STA 1190 L35R. REMOVED, FABRICATED AND INSTALLED REPAIR DOUB LER AT C-PIT TORQUE BOX FS 1190 AND L35R REF SRM 53-02-00 AND 51-1-8. 2 L 7 4 4F RT 4A25 2008021100174 20080211 00174 NM 2008 2 11 AALA200800193 1 20080128 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 946AN 30600 TUL - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT RIGHT BUTTLINE 7 FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008021100175 20080211 00175 NM 2008 2 11 AALA200800159 1 20080124 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AN 29605 MIA - EMERGENCY LIGHT AT SEAT 3B INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 3B. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008021100180 20080211 00180 WP 2008 2 11 AALA200800162 1 20080124 A 3222 SEAL DOUG DC9 DC982 3022082 WP NLG STRUT INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 405A 49316 TUS INFLIGHT T1418/24JAN - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO TUS AND LANDED WITHOUT INCIDENT. AC COMPLISHED NOSE GEAR SHOCK STRUT SEAL REPLACEMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008020800172 20080208 00172 NM 2008 2 8 BB08008 1 20080130 A 3350 20121 POWER SUPPLY BOEING 757 7572S7 1384962 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 906AW 23568 SNA - MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHTING IN THE AFT OF AIRCRAFT INOPERATIVE ALONG WITH THE L4 DOOR ESC APE SLIDE LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND POWER SUPPLY. OPERATIONAL CHECK OF LIGHTS GOOD. 2 L 7 2 4F RT A2NM 2008020800184 20080208 00184 EU 2008 2 8 TRBA2008014 1 20080203 A 3350 3013000 POWER SUPPLY AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHTS FAILED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 540AM 540 LAST 4 TO 5 INTERIOR EMERGENCY PATH EVACUATION LIGHTS CAME ON AND WILL NOT TURN OFF. REMOVED AND REPLACED EMERGENCY LIG HT POWER SUPPLIES 62WL AND 73WL IAW AMM/JIC 33-51-21. EMERGENCY LIGHTS OPERATE NORMAL IAW AMM/JIC 33-50-00. 2 H 7 2 4T RT A53EU 2008020800222 20080208 00222 NM 2008 2 8 SWAA080565 1 20080131 A 5311 6546525 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008020800224 20080208 00224 2008 2 8 SWAA080567 4 20080131 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008020800229 20080208 00229 NM 2008 2 8 SWAA080583 1 20080131 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008020800237 20080208 00237 NM 2008 2 8 HNAA0800053 1 20080127 A 3150 6500757 WARNING SWITCH DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A HNAA K NONE L NO TEST UK UNKNOWN 1 EA 07 826EX 30918 30918 389 WHEN THE COCKPIT WARNING AND CAUTION LIGHTS WERE CHECKED, IT WAS FOUND THAT THE MASTER WARNING SWITCH/LIGHT WAS INOPERAT IVE. THE SWITCH MODULE WAS REPLACED BY MAINTENANCE, OPS CHECKED GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 2008020800238 20080208 00238 NM 2008 2 8 NOCA01008 1 20080201 A 3350 S417N50915 LIGHT BOEING 767 76739H 1385311 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 760NA 26257 EMERGENCY FLOOR LIGHTS INOP BETWEEN 1AB AND 2AB. REPLACED LIGHT ASSY PER MM 33-51-10. 2 L 7 2 4F RT A1NM 2008020800279 20080208 00279 2008 2 8 SWAA080602 4 20080202 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008021900127 20080219 00127 NM 2008 2 19 CALA0800093 1 20080129 A 5311 BAC15171470 FRAME BOEING 737 7373T0 1384582 NM BS 887 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FUSELAGE FRAME IS CRACKED AT STA 887 BETWEEN STRINGER 8L AND 9L. REPAIRED PER ECRA 5310-04697. 2 L 7 2 4F RT A16WE 2008021900129 20080219 00129 EA 2008 2 19 MASA200800105 1 20080205 A 3350 BF10027002 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17231 7231 ASH 2796 PHX - REPORTED THE AFT CELING FLOOD LIGHT INOP. MX REPLACED THE FLOOD LIGHT. 2 L 7 2 4F RT A21EA 2008021900136 20080219 00136 NM 2008 2 19 AALA200800209 1 20080130 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT AT SEAT 26C INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900137 20080219 00137 NM 2008 2 19 AALA200800210 1 20080130 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT AT SEAT 35C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 35C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900138 20080219 00138 NM 2008 2 19 AALA200800211 1 20080130 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT AT SEAT 39C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 39C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900163 20080219 00163 NM 2008 2 19 AALA200800213 1 20080130 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900164 20080219 00164 WP 2008 2 19 AALA200800222 1 20080131 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 587AA 53250 LGA - EMERGENCY LIGHT BATTERY PACK AT OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERWING. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008021900166 20080219 00166 EU 2008 2 19 AALA200800220 1 20080131 A 2913 PUMP AIRBUS 300 A300B4605R 3930308 EU HYD SYSTEM INOPERATIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 59081 639 JFK INFLIGHT T1812/31JAN - GREEN SYSTEM HYDRAULIC FLUID LOSS IN FLIGHT. QUANTITY INDICATES ZERO. LANDING GEAR MANUALLY EXTENDED. LANDED JFK WITHOUT INCIDENT. REPLACED BOTH ENGINE GREEN HYDRAULIC PUMPS AND FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008021900168 20080219 00168 NE 2008 2 19 AALA200800231 2 20080201 A 7310 LINE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE FUEL SYSTEM LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 668AA 25333 31381 RDU INFLIGHT T1671/01FEB JFK TO CUN - FUEL DISAGREE LIGHT ILLUMINATED. SUSPECT FUEL LEAK IN LEFT ENGINE. LANDED RDU W ITHOUT INCIDENT. REPLACED LEFT ENGINE HIGH PRESSURE FUEL LINE AND O-RINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2008021900169 20080219 00169 NM 2008 2 19 AALA200800232 1 20080201 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 633AA 24591 DFW - EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008021900170 20080219 00170 NM 2008 2 19 AALA200800233 1 20080201 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 633AA 24591 DFW - EMERGENCY LIGHT FOR L1 SLIDE INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT L1 SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008021900184 20080219 00184 SO 2008 2 19 RAIA00802005 1 20080205 A 3297 CONNECTOR EMB 145 EMB145 3260210 SO DOWNLOCK SENSOR LOOSE A RAIA B EMER. DESCENT N FALSE WARNING DE DESCENT 1 CE 03 802HK 145066 FLT NR 3566-PIT-CREW REPORTED A LANDING GEAR LEVER DISAGREE ON THE EICAS DURING DESCENT. MAINTENANCE CLEANED AND TIGHTE NED A LOOSE DOWNLOCK PROXIMITY SENSOR. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2008021900185 20080219 00185 SO 2008 2 19 RAIA00802009 1 20080206 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN SMOKE A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 832HK 145771 FLT NR 7948 - LGA - CREW REPORTED SMOKE IN THE CABIN. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF ALL AIRCRAFT SYSTEMS WITH NO DEFECTS OR ODOR OF SMOKE. COULD NOT DUPLICATE THE CREW'S DISCREPANCY. 2 L 7 2 4T RT T00011AT 2008021900197 20080219 00197 WP 2008 2 19 G60A200800028 1 20080208 A 5350 TAIL CONE DOUG DC10 DC1030F 3023504 WP CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 607GC 46978 TAILCONE CRACKED APPROX 1 INCH AT UPPER RT SIDE IN WEB. 2 L 7 3 4F RT A22WE 2008021900198 20080219 00198 WP 2008 2 19 G60A200800029 1 20080208 A 5312 BULKHEAD DOUG DC10 DC1030F 3023504 WP FUSELAGE DENTED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 607GC 46978 AFT CARGO FWD BULKHEAD RT POST HAS DENT IN MID SECTION 3 CRACKS. 2 L 7 3 4F RT A22WE 2008020800306 20080208 00306 NM 2008 2 8 AALA200800140 1 20080123 A 3350 P2010031302 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 686AA 25343 TPA - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DO OR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020800326 20080208 00326 NM 2008 2 8 SWAA080634 1 20080204 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800337 20080208 00337 WP 2008 2 8 DHL2007873539 1 20080123 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 781 DAMAGED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 89073 46091 MAIN CARGO COMPT FLOORBEAM MISDRILLED HOLE AT STA 781.500 LBL.38.125 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FOR M 8110-3 DATED 01-11-08 EVA D853-00038 REV IR DATED 01-09-08, SEMAN DWG ED-4676 DATED 01-05-08. REMOVED FASTENERS IAW S RM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED FILLER AND REPAIR ANGLE IAW SEMAN DWG ED-4676. PERFORMED NDT INSP IAW DPS 4.707-1 NDT SPM PART 08, NO CRACK FOUND ENCLOSED SMN, FORM 242-4. CLEANED, TREATED, PRIMED AREA AND REPAIR PART IAW SRM 51-1-8B. INSTALLED REPAIR IAW SEMAN DWG ED-4676, SRM 51-1-11 SRM 51-1-20D SRM 51-3-1. 2 L 7 4 4F RT 4A25 2008020800346 20080208 00346 NM 2008 2 8 SWAA080655 1 20080204 A 5315 6545610 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 664, LBL 25. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2008020800354 20080208 00354 WP 2008 2 8 DHL2007873531 1 20080123 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 LT WING INBD L/E LWR SKIN HOLES ELONGATED AT STA XILD 42. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-11-08 EVA D857-00033 REV IR DATED 01-04-08 SEMAN DWG ED-4624 DATED 01-03-08. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION PLUS FABRICATED REPAIR DOUBLER AND REPAIR FILLER IAW SEMAN DWG ED-4674. PERFORMED NDT INSP IAW EVA-D857-00033 DPS 4.707-1 NDT SPM PART 08 NEITHER CRACK NOR CORROSION FOUND ENCLOSED SMN-FORM 242-4. CLEANED, TREATED, PRIMED AREA, R EPAIRED FILLER AND REPAIRED DOUBLER (INNER FACE) IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SEMAN DWG ED-4674 SRM 51-1 -11 SRM 51-1-21 SRM 51-3-0 SRM 51-1-20D SRM 51-3-1. 2 L 7 4 4F RT 4A25 2008020800379 20080208 00379 NM 2008 2 8 AALA200800074 1 20080116 A 2751 SENSOR BOEING 737 737823 13844BZ NM TE FLAPS INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SW 21 917AN 29518 DEN INFLIGHT T357/16JAN - TRAILING EDGE FLAPS SPLIT AT TWO DEGREES DURING APPROACH. LANDED DEN WITHOUT INCIDENT. REPLA CED NUMBER SIX SKEW SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008021100054 20080211 00054 SO 2008 2 11 CHQA200800022 1 20080204 A 3260 852701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RT MLG FAILED A CHQA O OTHER N FALSE WARNING AP APPROACH 1 GL 11 273SK 145331 CAE312347 CVG TO IND - WHILE ON APPROACH TO IND, CREW RECEIVED CAUTION MESSAGES "LG AIR/GROUND FAIL" AND "ENG 1/2 REV DISAGREE". THE QRH WAS FOLLOWED AND THE FLIGHT LANDED WITHOUT INCIDENT. UPON LANDING THE MESSAGES WENT AWAY. MAINTENANCE TROUBLES HOT THE AIR GROUND SYSTEM AND FOUND THAT THE RIGHT MAIN LANDING GEAR WEIGHT ON WHEELS PROX SWITCH WAS BAD, AS WELL AS TH E NOSE LANDING GEAR WEIGHT ON WHEELS HARNESS WAS BAD AS WELL. AFTER REPLACING THE PROX SWITCH AND NOSE LANDING GEAR WEI GHT ON WHEELS HARNESS THE AIR GROUND AND THRUST REVERSER SYSTEM FUNCTIONED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008021100059 20080211 00059 EA 2008 2 11 MASA200800098 1 20080201 A 2611 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY MALFUNCTIONED A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 649BR 7414 FLT 7245, IAD - SMOKE TOILET CAUTION IN FLIGHT. REMOVED AND REPLACED SMOKE DETECTOR. 2 L 7 2 4F RT A21EA 2008021100060 20080211 00060 NM 2008 2 11 MASA200800099 1 20080203 A 3350 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN NO TEST A MASA O OTHER L NO TEST NR NOT REPORTED 1 SW 07 434YV 434 ASH FLT 7351 DEN-RAP - EMERGENCY LIGHTS WILL NOT TEST FROM FA PANEL. MX PERFORMED, OPS CHECK OF SYSTEM. OPS CHECK GOOD . NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2008021100061 20080211 00061 EA 2008 2 11 MASA200800100 1 20080203 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 938LR 15038 ASH FLT 2920 PHX-COS - EMERGENCY CEILING FLOODLIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 2008021100109 20080211 00109 WP 2008 2 11 DHL2007873514 1 20080113 A 5740 FITTING DOUG DC8 DC873F 302199F WP WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 NR 2 MAIN TANK FWD FITTING CRACKED BETWEEN STA XRS 74.000 AND S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1- 0 PG 1. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D. CLEANED AND APPLIED POLYURETHANE TOP YELLOW COATING TO AREA IAW SRM 51-1-12 PG 7. INSTALLED NEW FITTING IAW SRM 51-1-12, SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1 (TORQUE). R EFER TO NR 107760 FOR FUEL LEAK CHECK. 2 L 7 4 4F RT 4A25 2008021100130 20080211 00130 WP 2008 2 11 UPS08851486 1 20080107 A 5523 57025792 TAB DOUG DC8 DC871F 302199D WP RT ELEVATOR DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 RT ELEVATOR GEAR TAB IS DELAMINATED. REMOVED AND REPLACED RT ELEVATOR GEAR TAB IAW DC8 AMM 27-30-03- 2. 2 L 7 4 4F RT 4A25 2008021100131 20080211 00131 WP 2008 2 11 UPS08851487 1 20080121 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 EMERGENCY EVAC LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-01. 2 L 7 4 4F RT 4A25 2008021100153 20080211 00153 WP 2008 2 11 DHL2007873538 1 20080123 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 LT OUTER WING OTBD L/E UPPER SKIN CRACKED 1" AT STA XW 761.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM DATE D 01-12-08 EVA D857-00037 REV IR DATED 01-08-08 REV IR SEMAN DWG NR ED-4670 DATED 12-12-07. REMOVED FASTENERS IAW SRM 5 1-1-21 SRM 51-1-20D. CUT OUT DAMAGE SECTION AND FABRICATED REPAIR DOUBLER (AL7075T6 0.063"), REPAIR FILLER (AL 7075 T6 0.050") IAW SEMAN DWG ED-4670. PERFORMED NDT INSP IAW EVA D857-00037 DPS 4.707 NEITHER CRACK NOR CORROSION FOUND, ENCLO SED SMN FORM 242-4. CLEANED, TREATED, PRIMED FILLER AND REPAIR DOUBLER INNER IAW SRM 51-1-8B. INSTALLED REPAIR PARTS I AW SEMAN DWG NR ED-4670 SRM 51-1-11 SRM 51-1-21 SRM 51-1-20D SRM 51-3-1. 2 L 7 4 4F RT 4A25 2008021100164 20080211 00164 NM 2008 2 11 AALA200800161 1 20080124 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 33G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 33G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021100194 20080211 00194 NM 2008 2 11 S2YA08002 1 20080205 A 2731 3280080 CONTROL PANEL DORNER DO32 DO328300 NM CENTER CONSOLE MALFUNCTIONED A S2YA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 GL 13 365SK 11874 3165 DURING APPROACH OF FLIGHT 2264 DAY-MKE THE CAPTAIN NOTICE THAT HIS PEN CAP WAS MELTING WHILE IT WAS SITTING ON THE CENTE R CONSOLE. THE CREW CALLED THE TOWER AND ASKED FOR PRIORITY. THE CAPTAIN DID NOT SEE ANY FIRE BUT THOUGHT HE MIGHT HAVE SEEN A LITTLE SMOKE WHEN HE PICKED UP HIS PEN CAP. THE CREW DID NOT DECLARE AN EMERGENCY NOR WHERE ANY OXYGEN MASKS DEPL OYED. THE CREW MADE A SAFE LANDING IN MKE AND THE PASSENGERS WHERE DEPLANED AT THE GATE AS NORMAL. MX REPLACED THE TRIM CONTROL PANEL P/N 328-0080 AND RETURNED THE AIRCRAFT TO SERVICE. MX INSPECTED THE TRIM CONTROL PANEL AND FOUND FACEPLATE P/N 328-0480 TO BE MELTED IN LOWER LEFT SIDE. 2 H 7 2 4T RT A55NM 2008021100196 20080211 00196 NM 2008 2 11 ASAA0852501 1 20080125 A 2160 3989083 VALVE BOEING 737 737890 1384527 NM TEMP MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 02 583AS 1935 1935 35681 AFT CABIN TEMPERATURE CONTROLLER WOULD NOT HOLD SET TEMPERATURE. REPLACED TRIM MOD VALVE. 2 L 7 2 4F RT A16WE 2008021200001 20080212 00001 NM 2008 2 12 USAA920080344 1 20080123 A 5311 65C35243 FRAME BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 CLT - MAJOR REPAIR - C20 CHECK - NR 03-0553-8-0315/4, AFT CARGO COMPARTMENT DOOR CUT OUT AFT FRAME CRACKED, BS 847. REP LACED AFT CARGO COMPARTMENT DOOR CUT OUT AFT FRAME, BS 847 IAW B737 SRM 51-40-00. 2 L 7 2 4F RT A16WE 2008021200006 20080212 00006 EA 2008 2 12 A6WA200840045 1 20080111 A 5242 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE E&E DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 HANDLE ASSY CRACKED ON AVIONIC BAY DOOR. HANDLE ASSY REPLACED ON AVIONIC BAY ACCESS DOOR IAW SRM 51-42-06 IAW AMM 52-41 -03-400-801. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200007 20080212 00007 EA 2008 2 12 A6WA200840044 1 20080115 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 PAX DOOR SURROUND STRUCTURE ROLLER BRACKET GOUGED ON FS 349, STR 6L. SURROUND STRUCTURE NEW ROLLER BRACKET INSTALLED ON PAX DOOR AT FS 349, STR 6 IAW SRM 51-41-04. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200009 20080212 00009 EA 2008 2 12 A6WA200840042 1 20080114 A 5420 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT PYLON CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 ONE ANGLE IS CRACKED ON LT PYLON ACCESS PANEL 412BT. ANGLE ON LT PYLON ACCESS PANEL 412BT, REPLACED IAW SRM 51-42-06. ( K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200017 20080212 00017 EA 2008 2 12 A6WA200840035 1 20080111 A 5320 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 MLG BAY LT HYDRAULIC SUPPORT BRACKET FOUND CRACKED. MLG BAY LT NEW HYDRAULIC SUPPORT BRACKET INSTALLED IAW SRM 51-42-06 . (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200022 20080212 00022 EA 2008 2 12 A6WA200840030 1 20080118 A 5420 SEPARATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT PYLON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 QTY 1 SEPARATOR HAS FRETTING ON LT PYLON ACCESS PANEL 421DB. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200026 20080212 00026 EA 2008 2 12 A6WA200840023 1 20080114 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 CRACK EXIST ON FLOOR SUPPORT STRUCTURE FS621, LBL 41. CRACK REMOVED ON FLOOR SUPPORT STRUCTURE FS 621, LBL 41 IAW REO 601R-53-61-117. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200030 20080212 00030 EA 2008 2 12 A6WA200840013 1 20080115 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS FAILED A A6WA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 31 438AW 7748 FLAPS FAIL AT ZERO ON APPROACH, DURING FLAP EXTENSION. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200033 20080212 00033 EU 2008 2 12 VQI2008F00000 1 20080111 A 5313 ASNA2215 STRINGER AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE FUSELAGE DAMAGED A VQIA O OTHER O OTHER AP APPROACH 1 WP 15 630VA MSN3101 ON APPROACH, AC SUSTAINED LIGHTING STRIKE, DAMAGING THE FUSELAGE SKIN FASTENER. LOCATION OF DAMAGE STRINGER 41, RT 4.40 INCHED AFTER FRAME 25. FASTENER REQUIRED REPLACEMENT AND STRINGER REPAIR. ADDITIONALLY, THE LT FWD NLG DOOR AND LT AF T NLG DOOR, RT WING TIP FENCE, TAT SENSOR, FWD DME ANTENNA, MARKER BEACON ANTENNA WERE REPLACED AS A RESULT OF LIGHTENIN G DAMAGE. (K) 2 L 7 2 4F 4 F RT A28NM E38NE 2008021200040 20080212 00040 NM 2008 2 12 2008UALA00506 1 20080130 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 AFT PIT FRAME DENTED AT STR 26L STA 1420 ON INBOARD FLANGE. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200045 20080212 00045 WP 2008 2 12 08FDEA00356 1 20080205 A 5230 AFA71321 FITTING DOUG DC10 DC1030F 3023504 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 ACCOMPLISHED AN INITIAL BHEC INSPECTION OF THE NR 6 MCD SPOOL BRACKET BOLT BORES IAW NTSPM 06-10-01.003 AND EA 8-5230-11 7632, STEP C. BORE HOLES B, C, AND D HAVE CRACK/CORROSION INDICATIONS. REAMED 4 EA. BOLT BORES, ACCOMPLISHED BHEC, FAB ERICATED AND INSTALLED 9 EA. REPAIR BUSHINGS IAW DC/MD-30 SRM 53-50-00 VOL I, FIG-17, PG-81 AND NTSPM 06-10-81.003. 2 L 7 3 4F RT A22WE 2008021200047 20080212 00047 NM 2008 2 12 2008UALA00497 1 20080129 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT LIGHT INOP AT UPPER DECK DOORS FWD CEILING LIGHT. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200050 20080212 00050 NM 2008 2 12 2008UALA00494 1 20080129 A 3520 418W10163 HINGE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE OXYGEN MASK BOX BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 224UA 30225 SEAT 26HJ OXYGEN MASK BOX DEPLOY PANEL HAS BOTH HINGES BROKEN. SUSPECT BROKEN BOX ASSEMBLY REPLACED 2 EACH HINGES AND SECURED PANEL. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021200057 20080212 00057 NM 2008 2 12 2008UALA00487 1 20080128 A 3350 LENS BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EXTERIOR MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 LEFT EXTERNAL FUSELAGE EMERGENCY EGRESS LIGHT LOCATED AFT OF DOOR 1L IS MISSING LENSE NUT PLATES. REPLACED EGRESS LIGHT ASSY REF SRM 51-40-02 PG 2. OPS CHECKED OKAY. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200066 20080212 00066 NM 2008 2 12 2008UALA00472 1 20080126 A 3397 58781 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 524UA 24977 EEL LIGHTING POWER FEED CABLE BURNT AND ARCHING AT ROW 18. EEL LIGHTS INTERMITTENT, 8 FOOT SECTION. REPLACED POWER FEE DER CABLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200073 20080212 00073 NM 2008 2 12 2008UALA00465 1 20080128 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT ROW 17B INOP. RESECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200080 20080212 00080 NM 2008 2 12 2008UALA00455 1 20080125 A 5330 DOUBLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 AFT CARGO COMP ANTENNA DOUBLER FWD LT FASTENER NUT PLATE HAS EXFOLIATION CORROSION. REMOVED CHANNEL ASSY. FABRICATED & INSTALLED NEW RADIUS FILLER. MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200081 20080212 00081 NM 2008 2 12 2008UALA00453 1 20080125 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 R-2 DOOR UPPER HINGE ARM CUTOUT IS DAMAGED. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200084 20080212 00084 NM 2008 2 12 2008UALA00435 1 20080124 A 3350 D71702001 BATTERY PACK BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 776UA 26937 EMERGENCY DOME LIGHT IN COCKPIT IS INOP. REPLACED BATTERY PACK. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021200085 20080212 00085 NM 2008 2 12 2008UALA00413 1 20080122 A 3350 8100133801 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 SEAT 3E IS MISSING AFT EEL LIGHT. REPLACED EEL LIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021200087 20080212 00087 NM 2008 2 12 2008UALA00411 1 20080122 A 3350 582233 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 EMERGENCY EEL LIGHT ASSY INOP AT RT MID LAV. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021200093 20080212 00093 NM 2008 2 12 2008UALA00403 1 20080123 A 3350 582240 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE O OTHER CR CRUISE 1 WP 29 199UA 28717 EMERGENCY LIGHTS 22A-B THROUGH 26A-B GOING ON AND OFF DURING FLIGHT. REPLACED POWER SUPPLY ABOVE DOOR 2L, OP CHECK GOOD . 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200094 20080212 00094 EU 2008 2 12 2008UALA00390 1 20080122 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 415UA 475 EMERGENCY LIGHT TEST FAILS BATTERY AFT L. LOOSE CONNECTOR AT AFT EMERGENCY POWER SUPPLY. RESET/RESEATED CONNECTOR, TES TED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021200095 20080212 00095 NM 2008 2 12 2008UALA00389 1 20080123 A 3070 11045968410354 DRAIN MAST AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE GALLEY SHORTED A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 810UA 843 AFTER T/O CABIN CREW IN AFT GALLEY SMELLED ELEC BURN SMELL. AFT GALLEY ODOR DISSIPATED IN A COUPLE MINUTES. NOTICED AF T GALLEY DRAIN C/B POPPED OVERHEAD PNL. GALLEY DRAIN MAST SHORTED. REPLACED GALLEY DRAIN MAST, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021200097 20080212 00097 NM 2008 2 12 2008UALA00383 1 20080122 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY EXIT CEILING LIGHT INOP AT ROW 5 LEFT. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200113 20080212 00113 NM 2008 2 12 2008UALA00356 1 20080122 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY EXIT EEL INOP AT SEAT ROW 58R. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200114 20080212 00114 NM 2008 2 12 2008UALA00355 1 20080122 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY EXIT CEILING LIGHT INOP ABOVE DOOR 3R. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200123 20080212 00123 NM 2008 2 12 2008UALA00347 1 20080120 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT AFT GALLEY WALL LT AND RT INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200125 20080212 00125 NM 2008 2 12 2008UALA00346 1 20080120 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT ROWS 42 ABC & 49 ABC ARE INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200130 20080212 00130 NM 2008 2 12 ASAA0852518 1 20080129 A 4990 38809381 OIL FILTER BOEING 737 737890 1384527 NM APU UNKNOWN A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 587AS 35684 APU OIL FILTER DELTA P INDICATOR EXTENDED, REF TASKCARD 78349013. REMOVED AND REPLACED APU OIL FILTER AND RESET DELTA P INDICATOR. 2 L 7 2 4F RT A16WE 2008021200132 20080212 00132 NM 2008 2 12 2008UALA00337 1 20080117 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 528UA 25018 EMERGENCY LIGHT AT SEAT 29 ABC ON BULLNOSE BIN PNL IS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200136 20080212 00136 NM 2008 2 12 2008UALA00334 1 20080119 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 531UA 25042 SEVERAL EEL AISLE LIGHTS ARE INOP THROUGHOUT THE CABIN. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200140 20080212 00140 2008 2 12 ASAA0852500 2 20080125 A 7261 M832481226 O-RING BOEING 737 737890 1384527 NM LT ENG OIL CAP SWOLLEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 559AS 35178 LEFT ENGINE OIL TANK CAP O-RING SWELLED. REPLACED O-RING. 2 L 7 2 4F RT A16WE 2008021200139 20080212 00139 NM 2008 2 12 2008UALA00327 1 20080119 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 515UA 24840 EMERGENCY FLOOR LIGHTING LOOSE NEAR 12C. RESECURED LIGHTING. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200141 20080212 00141 NE 2008 2 12 ASAA0852495 2 20080114 A 7200 CFM567B27 ENGINE BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE LEFT MALFUNCTIONED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 579AS 3448 3448 35187 894547 LEFT ENGINE GE REMOTE DIAGNOSTICS TREND DATA SHOWED GREATER THAN NORMAL EGT HDM LOSS WITH EGT AT THE ESTABLISHED THESHOL D. ACCOMPLISHED ENGINE COMPRESSOR WASH ON 25 JAN 08 PER MM SUPPLEMENT 72 00 00 PP 710 715. 2 L 7 2 4F 4 F RT A16WE E2GL 2008020800309 20080208 00309 NM 2008 2 8 AALA200800117 1 20080120 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 650AA 24608 MIA - EMERGENCY LIGHT AT SEAT 24D HAS DAMAGED LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008020800323 20080208 00323 SO 2008 2 8 SIMA200803506 1 20080131 A 5240 14521725003 SEAL EMB 145 EMB145LR 3260212 SO SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 626AE 145117 DURING MBV INSPECTION, FOUND FWD SERVICE DOOR SILL BETWEEN FRAME 22-23 IS CORRODED. REPLACED SILL IAW SRM 51-40-02. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008020800334 20080208 00334 WP 2008 2 8 ARWA20080104 1 20080129 A 7800 NSL6361507 TAIL CONE DOUG DC10 DC1030 3023501 WP NR 1 ENGINE DAMAGED A ARWA O OTHER O OTHER LD LANDING 1 SO 19 524MD 46999 ON POST FLIGHT, FOUND TAIL CONE COWLING DAMAGE ON NR 1 ENGINE. PERFORMED GENERAL AREA INSPECTION AND CHECK PNEU DUCTING FOR CONDITION, NO DAMAGE FOUND. REMOVED AND REPLACED NR 1 ENGINE O/B AFT CORE COWLING IN ACCORDANCE WITH DC-1030 M/M R EF 71-13-01. 2 L 7 3 4F A22WE 2008020800381 20080208 00381 NM 2008 2 8 SWAA080645 1 20080204 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, LBL 7 TO LBL 13. REMOVED AND REPLACED SHEAR TIE PER SR M. 2 L 7 2 4F RT A16WE 2008020800398 20080208 00398 NM 2008 2 8 SWAA080666 1 20080204 A 5320 6545819 WEB BOEING 737 7373A4 1384585 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND NOSE W/W RIGHT UPPER CEILING PANEL WEB CRACKED AT OUTBOARD END. REPAIRED WEB PER ER. 2 L 7 2 4F RT A16WE 2008020800405 20080208 00405 NM 2008 2 8 SWAA080676 1 20080205 A 5322 6546569 SHEAR TIE BOEING 737 7373TO 138447G NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 967, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008020800406 20080208 00406 NM 2008 2 8 SWAA080677 1 20080205 A 5322 6546529 SHEAR TIE BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500, STR 24R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008021100028 20080211 00028 SO 2008 2 11 SWIA200819178 1 20080128 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 586SW 120354 FLT 3730 - PILOTS FRONT WINDSHIELD IS CRACKED. REPLACED LEFT WINDSHIELD IAW 56-10-01, PN: NP-151311-1, SN OFF: 00213H44 17. 2 L 7 2 4T RT A31SO 2008021100058 20080211 00058 NM 2008 2 11 DLM90080146 1 20080131 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 1357 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 FOUND RT CUSP CRACKED RBL 57 STA 1357. REPAIRED CUSP WEB IAW MD-90 SRM 51-11-01 VOL 2 ON N/R 2000-0136 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008021100078 20080211 00078 WP 2008 2 11 DHL2007873513 1 20080103 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 660 DAMAGED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 89073 46091 MAIN CARGO COMPT FLOORBEAM MISDRILLED HOLE AT BS 660 LBL 15"125 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 51-2-1 F IG 1 SHEET 9-12, TR NR 51-130 DATED 01-26-04. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICAT ED REPAIR ANGLE AND FILLER IAW SRM 51-2-1 FIG 1 SHEET 9-12, TR NR 51-130. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 51-2-1 FIG 1 SHEET 9-12, TR NR 51-130, SRM 51-1-11, SRM 51-1-20D, SRM 51-3-1. 2 L 7 4 4F RT 4A25 2008021100083 20080211 00083 NM 2008 2 11 AALA200800192 1 20080128 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 946AN 30600 TUL - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT LEFT BUTT LINE 7 FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008021100085 20080211 00085 NM 2008 2 11 AALA200800195 1 20080128 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 946AN 30600 TUL - EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK AT STATION 565 FOR EMERGENCY LIGHTS AT MID CABIN . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008021100092 20080211 00092 NM 2008 2 11 F3LA200800038 1 20080127 A 3350 32145410 EPSU AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE EMERGENCY LIGHTS INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 921FR 570 2010 DURING REMAIN OVER NIGHT MAINTENANCE, THE EMERGENCY EXIT LIGHT EPSU, FOR THE OVERWING EXITS FOR THE LEFT SIDE OF THE CAB IN, FIN NR 11LN, FAILED ITS FUNCTIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE EPSU IN ACCORDANCE WITH THE REQUIREME NTS OF AMM 33-51-38 P 401. FOLLOWING COMPLETION OF THE INSTALLATION AND ITS INSPECTION, THE UNIT OPERATIONALLY CHECKED OKAY. 2 L 7 2 4F 4 F RT A28NM 2008021100100 20080211 00100 NM 2008 2 11 AALA200800158 1 20080123 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 767AJ 33539 DFW - EMERGENCY LIGHTS AT SEAT ROWS 20 TO 26 INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER THREE DOOR FOR EMERGENC Y LIGHTS AT SEAT ROWS 20 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021100106 20080211 00106 NM 2008 2 11 MASA200800056 1 20080121 A 2611 PU90461R2 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY FALSE ACTIVATION A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 454YV 15155 454 ASH FLT 7235 COD-DEN - LAV SMOKE DETECTOR ACTIVIATED IN FLIGHT WITH NO SMOKE. MX REMOVED AND REPLACED SMOKE DETECTOR. 2 H 7 2 4T RT A13NM 2008021100110 20080211 00110 SO 2008 2 11 SWIA200819171 1 20080131 A 2720 ACTUATOR EMB 120 EMB120ER 3260203 SO RUDDER MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 07 568SW 120343 FLT 3677 - AFTER DEPARTURE, THE RUDDER PEDALS FELT STIFF. REPLACED BLUE SYSTEM RUDDER ACTUATOR. OPS CHECKS GOOD IAW 27 -22-00, PN 388140-1003, SN/OFF 4995. 2 L 7 2 4T RT A31SO 2008021100151 20080211 00151 WP 2008 2 11 UPS08851537 1 20080109 A 5280 FITTING DOUG DC8 DC871F 302199D WP FS 960 RBL 60 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 RT MLG DOOR SWITCH MOUNT HOLES ARE ELONGATED. FABRICATED AND INSTALLED REPAIR DOUBLER ON RT MLG DOOR MOUNT SWITCH FITTING IAW EO DC8-3260-16914-A. 2 L 7 4 4F RT 4A25 2008021100159 20080211 00159 EU 2008 2 11 TRBA2008013 1 20080130 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS BURNED OUT A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 260AE 263 SERVICE DOOR'S BOTTOM EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT BULBS AND PERFORMED OP CK IAW JIC NR 33-50-00. 2 H 7 2 4T RT A53EU 2008021100160 20080211 00160 NM 2008 2 11 F3LA200800041 1 20080131 A 2910 6425658503 TUBE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE LT ENGINE LEAKING A F3LA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 03 924FR 30 2030 757638 DURING DESCENT & APPROACH, CREW REPORTED AN ECAM INDICATION OF LOW HYD PRESSURE & LOW HYD FLUID LEVEL FOR GREEN HYDC SYS . AN EMERGENCY DECLARED & CREW MANUALLY EXTENDED MLG. ACFT MADE AN UNEVENTFUL LANDING. MX FOUND A HYD TUBE ASSY LEAKI NG ON NR 1 ENGINE. TUBE ASSY R & R IAW AMM 20-25-11-911-001. MX INSPECTED NR 1 ENGINE CASE DRAIN FILTER & FOUND NO IND ICATIONS OF METAL. MX R & R CASE DRAIN FILTER IAW AMM 29-11-43 PB 401. MX SERVICED GREEN HYD SYS IAW AMM 12-12-29-611- 001 & RETURNED ACFT TO NORMAL CONFIGURATION IAW AMM 32-33-00 PB 501, SUB-TASK 32-33-00-860-064. MX LEAK CHECKED NR 1 E NGINE IAW AMM 71-00-00-710-006. NO LEAKS FOUND. ACFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM 2008021100161 20080211 00161 WP 2008 2 11 UPS08851566 1 20080109 A 5313 37502570503 LONGERON SPLICE DOUG DC8 DC871F 302199D WP FS 1050 L31L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 L31L SPLICE FITTING CRACKED AT STA 1050. REPLACED SPLICE FITTING AT FS 1050 AND L31L REF, SRM 51-1-2 0D AND SRM 51-1-24. 2 L 7 4 4F RT 4A25 2008021100188 20080211 00188 NM 2008 2 11 DL76S080132 1 20080128 A 2780 271703865 DRIVE ASSY BOEING 767 767332 1382001 NM LE FLAPS FAILED A DALA O OTHER F FLT CONT AFFECTED LD LANDING 1 SO 27 128DL 24078 DURING APPROACH LEADING EDGE DISAGREE FSEU FAULTS O/B SLAT PDU RVDT M548 AND FLAP LEVER RVDT MIS R M603. FLAPS SLATS RU N NML. RAN FLAPS SEVERAL MORE TIMES AND SLATS LOCKED UP WITH SAME FAULTS AS BEFORE. REPLACED SLAT PD RVDT NR 2 NEEDS R IG. REMOVED AND REPLACED FLAP HANDLE POSITION RVDT PER AMM. RIGGED PDU RVDT PER AMM. RAN FLAPS SEVERAL TIMES CK GOOD. 2 L 7 2 4F RT A1NM 2008021200013 20080212 00013 EA 2008 2 12 A6WA200840038 1 20080113 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 BTW FS 621.00 AT RT STR 14 STRINGER CLIP CRACKED. NEW STRINGER CLIP INSTALLED IAW SRM 51-42-20. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200048 20080212 00048 NM 2008 2 12 2008UALA00496 1 20080129 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT EEL LIGHT INOP ACROSS DOOR 3 LEFT LOWER AISLE WALL. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200060 20080212 00060 WP 2008 2 12 08FDEA00340 1 20080201 A 5320 AEA00246 INTERCOSTAL DOUG DC10 DC1030 3023501 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 RT MLG WW, MIDINTERCOSTAL INBD / OBRD SURFACES HAVE CORROSION JUST FWD OF AFT BULKHEAD. COROSION FOUND TO BE OUT OF LIMI TS, REMOVED INTERCOSTAL, FABERICATED NEW AND INSTALLED IAW SRM 51-21-01 PG-28, VOL. II, SRM 53-00-01, FIG A, VOL I, SRM 51-35-01 & SRM 51-33-01 VOL II, DAC DAW EAE 0024 REV. 5, SRM 51-21-01 PG. 21-24 & SRM 51-21-02 VOL II. 2 L 7 3 4F A22WE 2008021200062 20080212 00062 NM 2008 2 12 2008UALA00475 1 20080126 A 2612 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE WARNING SYS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 544UA 25322 CARGO FIRE (RED AFT) ARM SW LIGHT INOPERATIVE. REPLACED SWITCH ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200071 20080212 00071 NM 2008 2 12 2008UALA00467 1 20080128 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT ROW 24 AB INOPERATIVE. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200089 20080212 00089 NM 2008 2 12 2008UALA00409 1 20080122 A 3350 1317 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 MASTER CALL LIGHT ON EMERGENCY EXIT SIGN (ROW 15 RT SIDE) INOP. RELAMPED LIGHT ON EMERGENCY EXIT SIGN. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021200119 20080212 00119 NM 2008 2 12 2008UALA00349 1 20080121 A 3510 D9231026600060 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 834UA 1420 OXY REGUL LO PR 20 PSI. FOUND CAPT O2 BOX VALVE LEAKING. REPLACED CAPT O2 BOX AND MASK. SERVICED CREW O2 TO 1610 PSI. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021200143 20080212 00143 NM 2008 2 12 ASAA0852502 1 20080125 A 4990 38762983 SENSOR BOEING 737 737890 1384527 NM APU OIL LEVEL DEFECTIVE A ASAA O OTHER N FALSE WARNING AP APPROACH 1 NM 02 585AS 1479 1479 35683 APU MAINTENANCE ANNUNCIATION. REPLACED DEFECTIVE OIL LEVEL SENSOR. 2 L 7 2 4F RT A16WE 2008021200144 20080212 00144 WP 2008 2 12 UPS08851583 1 20080112 A 5230 SKIN DOUG DC8 DC871F 302199D WP CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 C-PIT DOOR EXTERIOR SKIN DAMAGED AT LOWER AFT CORNER. REPAIRED C-PIT DOOR EXTERIOR SKIN LOWER AFT CO RNER REF SRM 52-02-00-0 FIG 002 AND FIG 006. 2 L 7 4 4F RT 4A25 2008021200145 20080212 00145 WP 2008 2 12 UPS08851585 1 20080129 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 EMERGENCY LIGHT WOULD NOT TURN ON DURING PDC. EMERGENCY LIGHT BATTERY PACK REPLACED IAW AMM 33-50-01-2 AND CHECK SERVIC EABLE. 2 L 7 4 4F RT 4A25 2008021200148 20080212 00148 NM 2008 2 12 ASAA0842521 1 20080108 A 5754 65C26601389 SKIN BOEING 737 7374Q8 138447Q NM LT WING LE SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 LT WING NR 1 L E SLAT T/E WEDGE INBOARD FWD UPPER AND LOWER SURFACES DELAMINATED PREPARED AREA FOR REPAIR. REMOVED DAMA GED CORE, FABRICATED REPAIR CORE, REPAIR SKIN DOUBLER INSTALLED AND BONDED IAW B737 400 SRM 57 43 02 FIG 1 AND 51 70 10. 2 L 7 2 4F RT A16WE 2008021200149 20080212 00149 NM 2008 2 12 ASAA0842520 1 20080109 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 6 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 NR 6 SPOILER HAS MULTIPLE DENTS IN CENTER AREA OF LOWER SURFACE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLERS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008021200150 20080212 00150 NM 2008 2 12 2008UALA00315 1 20080120 A 5270 848401 PROXIMITY SWITCH AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FWD CARGO DOOR FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 855UA 1737 RTFL WITH A CARGO DOOR INDICATION PROBLEM. PROX SWITCH 30WV FAILED CAUSING FWD CARGO DOOR ECAM MESSAGE. REPLACED/ADJUS TED PROX SWITCH 30 WV. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021200151 20080212 00151 NM 2008 2 12 ASAA0842522 1 20080109 A 5753 654643528 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 RT OUTBOARD AFT FLAP HAS AN AREA OF MULTIPLE DENTS ON UPPER SURFACE. PREPARED DAMAGED AREA, FABRICATED EXTERNAL DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008021200152 20080212 00152 NM 2008 2 12 ASAA0842523 1 20080110 A 5753 6546430189 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 LT INBOARD AFT FORE FLAP DENTED 11" FROM O B AND 3" FROM T/E ON UPPER SURFACE PREPARED DAMAGED AREA. FABRICATED EXTERNA L DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008021200154 20080212 00154 EU 2008 2 12 2008UALA00314 1 20080120 A 3260 848401 PROXIMITY SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 438UA 678 RTFL DUE TO A GEAR UPLOCK INDICATION PROBLEM. FAILURE OF NOSE L-G EXT PROX SENSOR 25GA. REPLACED SENSOR 25GA, PERFORME D GEAR SWINGS, ALL NORMAL OPS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021200155 20080212 00155 NM 2008 2 12 2008UALA00312 1 20080117 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY EEL LIGHT INOP AT SEAT 1A FWD. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200163 20080212 00163 NM 2008 2 12 ASAA0842528 1 20080114 A 5751 65C2591128A SKIN BOEING 737 7374Q8 138447Q NM RT AILERON DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 RT AILERON LWR SURFACE SMALL AREA OF COMPOSITE SKIN DAMAGE AT O/B TAB ATTACH BEARING AREA PREPARED DAMAGED AREA WET LAY UP IAW 737 400 SRM 51 70 17 AND BONDED IAW B737 400 SRM 51 70 17 REPAIR 1 AND ASA EA 5760 01072 WEIGHT AND BALANCE ACCOM PLISHED ON MIG 5 NR 5085463. 2 L 7 2 4F RT A16WE 2008021200164 20080212 00164 NM 2008 2 12 2008UALA00046 1 20080103 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT INOP DOOR 2L AFT SILL. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200165 20080212 00165 NM 2008 2 12 ASAA0842529 1 20080110 A 5753 654C430189 SKIN BOEING 737 7374Q8 138447Q NM TE FLAPS DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 LT INBOARD AFT FORE FLAP LWR SURFACE CLUSTER OF DENTS BEHIND NR 1 TIRE PREPARED AREA OF DENT DAMAGE. FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008021200167 20080212 00167 NM 2008 2 12 ASAA0842530 1 20080122 A 5753 6546430130 SKIN BOEING 737 7374Q8 138447Q NM RT FORE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 RT WING INBOARD AFT FORE FLAP DENTED ON LOWER SURFACE IN 2 EACH PLACES 28" AND 29" FROM INBOARD END AND 6" FROM TRAILING EDGE. PREPARED AREA FOR REPAIR: FABRICATED REPAIR PARTS AND BONDED IAW B737 400 51 70 4 REPAIR 4. 2 L 7 2 4F RT A16WE 2008021200170 20080212 00170 NM 2008 2 12 USAA920080319 1 20080126 A 5230 WEB BOEING 737 7373B7 1384580 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT - MAJOR REPAIR - RON - AFT CARGO DOOR HAS CRACKED WEB INSIDE THE DOOR UNDER THE LINER. REPAIRED THE AFT CARGO DOOR WEB IAW USAIRWAYS EA 110557. 2 L 7 2 4F RT A16WE 2008021200171 20080212 00171 EU 2008 2 12 USAA920080316 1 20080130 A 3230 114079015 SELECTOR VALVE AIRBUS 320 A320231 3930325 EU NLG DEFECTIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 620AW 52 FLT NR 654 - ON CLIMB-OUT FROM DTW, NOSE GEAR DOORS WOULD NOT CLOSE. CREW ATTEMPTED TO RECYCLE GEAR FOUR TIMES UNSUCCES SFULLY. AIRCRAFT RETURNED TO DTW. AIRCRAFT WAS MAINTENANCE FERRIED TO PIT. MAINTENANCE ADJUSTED PROXIMITY SENSORS AND REPLACED THE LANDING GEAR SELECTOR VALVE. 2 L 7 2 4F RT A28NM 2008021200175 20080212 00175 EU 2008 2 12 USAA920080317 1 20080130 A 3231 VALVE AIRBUS 320 A320231 3930325 EU NLG DOOR INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 632AW 81 FLT NR 434, ON CLIMB-OUT OF MSP, GEAR RETRACTION TOOK PLACE BUT THE NOSE GEAR DOORS DID NOT CLOSE. CREW RECYCLED THE GE AR BUT THE NLG DOORS STILL DID NOT CLOSE. ACFT RETURNED TO MSP. MX REMOVED AND REPLACED SAFETY VALVE 2629GM PER MM, FA ULT CONTINUED. SWAPPED LGCIU'S, DOORS OPERATED NORMALLY. PLACED LGCIU NR 2 ON MEL 32-31-01A. MAINTENANCE ADJUSTED X D IMENSION FOR PROXIMITY SENSORS 18GA AND 19GA AND ADJUSTED NLG DOOR CONTROL RODS. OPERATIONAL CHECK OF LANDING GEAR DOOR S WAS GOOD. 2 L 7 2 4F RT A28NM 2008021200177 20080212 00177 NM 2008 2 12 ASAA0842531 1 20080129 A 2612 WARNING LIGHT BOEING 737 7374Q8 138447Q NM CARGO FIRE FALSE INDICATION A ASAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 02 763AS 25100 ON CLIMB-OUT, BOTH CARGO FIRE SUPPRESSION BOTTLE LIGHTS ILLUMINATED. REPLACED BOTH BOTTLES AND MODULE FOR CARGO FIRE SU PPRESSION SYSTEM. 2 L 7 2 4F RT A16WE 2008021200183 20080212 00183 NM 2008 2 12 USAA920080304 1 20080113 A 5310 654587545 CREASE BEAM BOEING 737 7373Y0 1384671 NM BS 289-298 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 C18 CHECK, CORROSION/CRACK ON THE R1 DOOR CREASEBEAM ANGLE, BS 289 - BS 298, S17R. REPLACED THE R1 DOOR CREASE BEAM ANG LE, BS 289 - BS 298, S17R IAW BOEING DRAWING 65-45875. 2 L 7 2 4F RT A16WE 2008021200189 20080212 00189 NM 2008 2 12 USAA920080322 1 20080111 A 5311 654655514 FRAME BOEING 737 7373Y0 1384671 NM BS 867 S9L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 867, S9L. REPAIRED FRAME, BS 867, S9L IAW USAIRWAYS EA 100190. 2 L 7 2 4F RT A16WE 2008021200191 20080212 00191 NM 2008 2 12 USAA920080324 1 20080111 A 5311 6520723U54 FRAME BOEING 737 7373Y0 1384671 NM BS 492 S25R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 492.4, S25R. REPAIRED FRAME, BS 492.4, S25R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008021200192 20080212 00192 NM 2008 2 12 USAA920080325 1 20080111 A 5311 90526911 FRAME BOEING 737 7373Y0 1384671 NM BS 747 S9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 747, S9R. REPAIRED FRAME, BS 747, S9R I/A/W USAIRWAYS EA 100190. 2 L 7 2 4F RT A16WE 2008021200193 20080212 00193 NM 2008 2 12 USAA920080326 1 20080111 A 5311 90526911 FRAME BOEING 737 7373Y0 1384671 NM BS 787 S9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 787, S9R. REPAIRED FRAME, BS 787, S9R IAW USAIRWAYS EA 100190. 2 L 7 2 4F RT A16WE 2008021900202 20080219 00202 WP 2008 2 19 G60A200800027 1 20080208 A 5415 ATTACH ANGLE DOUG DC10 DC1030F 3023504 WP LT NACELLE CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 607GC 46978 LT PYLON UPPER OUTBOARD SIDE STA YN214 ATTACH ANGLE CRACKED. 2 L 7 3 4F RT A22WE 2008021900204 20080219 00204 EA 2008 2 19 MASA200800117 1 20080210 A 3350 110049 CHARGER CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 931LR 15031 ASH FLT 2739 PHX-LGB, CAPTAIN REPORTED GALLEY EMERGENCY LIGHTS INOP. MX REPLACED CHARGER AND BATTERY PACK. 2 L 7 2 4F RT A21EA 2008021900212 20080219 00212 NM 2008 2 19 SWAA080780 1 20080211 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 232WN 32500 DURING SCHEDULED HC1 CHECK, FWD LT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008021900213 20080219 00213 NM 2008 2 19 SWAA080781 1 20080211 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 232WN 32500 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2008021900218 20080219 00218 NM 2008 2 19 SWAA080801 1 20080212 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008021900219 20080219 00219 NM 2008 2 19 SWAA080802 1 20080212 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008021900221 20080219 00221 NM 2008 2 19 SWAA080812 1 20080212 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CORRODED AT BS 947, STR 26R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008021900223 20080219 00223 EA 2008 2 19 QXEA200800175 1 20080207 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA MAIN PAX STICKING A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 601QX 10009 PDX- FLIGHT 2555 - MAIN CABIN DOOR COULD NOT BE OPENED BY PULLING THE HANDLE ON THE GROUND. HAD TO GET A LARGE LADDER T O OPEN THE DOOR. EVEN THEN IT WAS HARD TO OPEN. MAINTENANCE OPERATED THE DOOR THROUGH SEVERAL CYCLES WITH NO DEFECTS N OTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2008021900231 20080219 00231 NM 2008 2 19 SWAA080820 1 20080212 A 5551 6551524 FITTING BOEING 737 7373G7 1384595 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING P ER SRM. 2 L 7 2 4F RT A16WE 2008021900238 20080219 00238 NM 2008 2 19 SWAA080799 1 20080211 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008021900239 20080219 00239 NM 2008 2 19 SWAA080782 1 20080211 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 11 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008021900243 20080219 00243 NM 2008 2 19 CALA0800114 1 20080207 A 3210 69406883 LINK BOEING 737 7373T0 1384582 NM RT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14335 23573 RT MAIN GEAR STABILIZER LINK HAS CORROSION AT END. REMOVED AND REPLACED RT MAIN GEAR STABILIZER LINK PER MM 57-15-00. 2 L 7 2 4F RT A16WE 2008021900252 20080219 00252 NM 2008 2 19 SWAA080787 1 20080210 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008021900254 20080219 00254 NM 2008 2 19 SWAA080774 1 20080210 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 14R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008021900255 20080219 00255 NM 2008 2 19 QXEA200800178 1 20080211 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY NO TEST A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 365PH 17463 985 526 SEA - FLIGHT 2059 - BAGGAGE SMOKE DETECTOR WARNING WILL NOT TEST. MAINTENANCE PLACED ON MEL 26-8A. AIRCRAFT RETURNED T O SERVICE. ON 2/14/08, THE SMOKE DETECTOR WAS REPLACED. 2 H 7 2 4T RT A13NM 2008021900258 20080219 00258 WP 2008 2 19 G60A200800004 1 20080207 A 5311 FRAME DOUG DC10 DC1030F 3023504 WP BS 1902 S50L/R CORRODED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 606GC 47929 FOUND CORROSION ON FRAME. 2 L 7 3 4F RT A22WE 2008021900259 20080219 00259 WP 2008 2 19 G60A200800005 1 20080207 A 5320 FLOOR SUPPORT DOUG DC10 DC1030F 3023504 WP BS 1841-1967 CORRODED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 606GC 47929 FOUND CORROSION ON BULK CARGO FLOOR SUPPORT RAIL. 2 L 7 3 4F RT A22WE 2008021900263 20080219 00263 NM 2008 2 19 QXEA200800086 1 20080114 A 5340 STRINGER CLIP DHAV DHC8 DHC8202 2809007 NM BS 466 S31R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - X466 AND STRINGER 31R SUSPECT CORROSION AT CLIP RADIUS. MAINTENANCE BLENDED OUT CORROSION, REMAINED WI THIN LIMITS, INSPECTED AND NO CRACKS NOTED. ETCHED, ALODINED AND PRIMED REPAIR AREA. RESTORED FINISH. 2 H 7 2 4T RT A13NM 2008021900266 20080219 00266 NM 2008 2 19 QXEA200800096 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 476-486 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - SEAT TRACK NR 5 IS GOUGED X476 TO X 486. MAINTENANCE BLENDED OUT GOUGE. INSPECTED, REMAINED WITHIN LI MITS AND NO CRACK NOTED. RESTORED FINISH TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021900267 20080219 00267 NM 2008 2 19 QXEA200800097 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 520-522 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - SUSPECT CORROSION AROUND 2 SKIN RIVETS X520 TO X522 BELOW SEAT TRACK NR 2. MAINTENANCE REMOVED RIVETS, BLENDED OUT CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. INSTALLED RIVETS AND RESTORED FINISH TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021900272 20080219 00272 NM 2008 2 19 CALA0800130 1 20080212 A 5311 6546596 FRAME BOEING 737 737524 1384721 NM BS 727B S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 FRAME CRACKED AT STA 727B ABOVE STRINGER 9L. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04714. 2 L 7 2 4F RT A16WE 2008021900274 20080219 00274 NM 2008 2 19 CALA0800133 1 20080212 A 5340 6916970501 STRINGER CLIP BOEING 737 7373T0 1384582 NM BS 348 S15L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 STA 348.2 STRINGER 15L LOWER STRINGER CLIP IS CRACKED. INSTALLED NEW CLIP PER SRM 51-40-05. 2 L 7 2 4F RT A16WE 2008021900282 20080219 00282 WP 2008 2 19 G60A200800007 1 20080207 A 5330 SKIN DOUG DC10 DC1030F 3023504 WP BS 1942-2163 CORRODED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 606GC 47929 FOUND CORROSION ON FUSELAGE SKIN FS 1942-2163. 2 L 7 3 4F RT A22WE 2008021900285 20080219 00285 NM 2008 2 19 GTIA0800006 1 20080126 A 5210 D5211006820000 HOOK AIRBUS A319 A319132 3930340 NM R2 DOOR GALLED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 521NK 2797 R2 DOOR GEARBOX LOCK HOOK GALLED. REPLACED LOCK HOOK IAW AMM 52-11-21-400-001. 2 L 7 2 4F RT A28NM 2008021500129 20080215 00129 2008 2 15 BB08012 4 20080207 A 2565 D30656126 SLIDE BOEING 757 7572B7 1384964 NM ZONE 200 FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 201UU 668 668 27810 CLT - EMERGENCY DOOR SLIDE ON EXIT DOOR 4L HAS LOW BOTTLE PRESSURE. MAINTENANCE REMOVED AND REPLACED SLIDE ASSY. 2 L 7 2 4F RT A2NM 2008021500139 20080215 00139 2008 2 15 2008UALA00590 4 20080131 A 2565 5A29011 VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ASPIRATOR LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 655UA PF0121 25393 ASPIRATOR LEAKING. FAULTY VALVE. REPLACED SLIDE AND ASPIRATOR. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500161 20080215 00161 NM 2008 2 15 2008UALA00639 1 20080203 A 2560 131W18141104 FITTING BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GIRT BAR BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 782UA 26948 DOOR 4L AFT GIRT FITTING END BROKEN. REPLACED BRACKET. CHECKED DOOR GIRT BAR OPERATION PER 25-66-01 NORMAL. ACFT OK FO R SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021500198 20080215 00198 NM 2008 2 15 SWAA080721 1 20080207 A 5312 6545409 PRESSURE PANEL BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED HC1 CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 664, RBL 40. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008021500208 20080215 00208 2008 2 15 SWAA080731 4 20080207 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008021500216 20080215 00216 2008 2 15 2008UALA00510 4 20080128 A 2565 D31516121 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE SHORTED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 428UA 523 EMERGENCY LIGHT SYSTEM TEST FAILS WITH CFDS MESSAGE EXT LOAD FWD LEFT. ELECTRICAL SHORT WITHIN FWD LEFT SLIDE ASSY. RE PLACED SLIDE AT FWD LT DOOR. ALL CHECKS ARE NOW NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021900018 20080219 00018 EA 2008 2 19 CHQA200800024 1 20080206 A 3234 7455025 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE MLG MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 478CA 13160 13160 7671 GEE873457 AFTER TAKEOFF THE CREW SELECTED THE MLG LEVER TO THE UP AND THE MLG DID NOT RETRACT. WHILE THE LEVER WAS IN THE UP POSI TION, CREW RECEIVED MESSAGES FOR PARKING BRAKE SHUT-OFF VALVE AND ANTI-SKID INBOARD. EICAS INDICATING 3 GREEN AND DOWN WITH NO MLG DISAGREEMENT MESSAGES. AFTER RUNNING APPLICABLE CHECKLISTS, MLG SELECTED DOWN AND MESSAGES WENT AWAY. FLT THEN RETURNED TO FIELD AND LANDED UNEVENTFULLY AT KCLE. MX DUPLICATED FAULT WITH ACFT ON JACKS AND TROUBLESHOT PROBLEM TO MLG HANDLE. AFTER REPLACING HANDLE GEAR RETRACTED NORMALLY BUT THE ANTI-SKID MESSAGES REMAINED. PARKING BRAKE SWITC H WAS FOUND OUT OF ADJUSTMENT AND CAUSING THE ANTI-SKID MESSAGES, AND AFTER CLEANING AND ADJUSTING SWITCH, ANTI-SKID MES 2 L 7 2 4F 4 F RT A21EA E15NE 2008021900019 20080219 00019 SO 2008 2 19 CHQA200800025 1 20080206 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LT MLG FAULTY A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 292SK 145488 CAE311794 IAD TO GSO - AFTER TAKEOFF, WHEN THE CREW SELECTED THE LANDING GEAR UP, A LANDING GEAR AIR/GROUND FAIL MESSAGE WAS DISPL AYED ON EICAS AND THE LANDING GEAR WOULD NOT RETRACT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT AT IAD. M AINTENANCE TROUBLESHOT THE AIR/GROUND SYSTEM AND FOUND THE LEFT MAIN LANDING GEAR WEIGHT-ON-WHEELS PROX SWITCH FAULTY. AFTER REPLACING THE PROX SWITCH, THE MESSAGE CLEARED AND THE AIR/GROUND SYSTEM AND LANDING GEAR OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008021900031 20080219 00031 NM 2008 2 19 2008UALA00653 1 20080204 A 3040 ANTI-ICE SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 203UA 24718 FLIGHT DIVERTED DUE TO CAPTAIN'S WINDOW HEAT PROBLEM. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021900038 20080219 00038 NM 2008 2 19 CALA0800095 1 20080127 A 5310 65C251722 BEAM BOEING 737 7373T0 1384582 NM BS 1121 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76354 23592 FOUND CORROSION ON HORIZONTAL STAB CENTER SECTION RT PRIMARY BEAM LOWER CHORD VERTICAL LEG AT BODY STATION 1121. REPAIR ED PER ECRA 5510-01914. 2 L 7 2 4F RT A16WE 2008021900080 20080219 00080 NM 2008 2 19 HALA0800055 1 20080110 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 721 S2L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LIGHTING STRIKE ON A/C CROWN AT LOCATION, STA 721, S2L. REPAIRED IAW 767-300 SRM 53-00-01, REPAIR 8. 2 L 7 2 4F RT A1NM 2008021900107 20080219 00107 NM 2008 2 19 AALA200800208 1 20080130 A 3810 24E507040G04 WATER HEATER BOEING 757 757223 1384957 NM LAVATORY INOPERATIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 614AA 24490 GJT INFLIGHT T119/30JAN EWR TO LAX CREW REPORTED SMOKE IN CABIN. SMOKE DETECTORS IN LAVATORIES WENT OFF. LANDED GJT W ITHOUT INCIDENT. REPLACED MID LAVATORY WATER HEATER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008021900191 20080219 00191 NM 2008 2 19 CALA0800102 1 20080130 A 5320 69265553 BRACKET BOEING 737 7373T0 1384582 NM BS 348 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 BRACKET CRACKED AT STA 348.20 STRINGER 16L. REMOVED AND REPLACED PER ECRA 5311-01392. 2 L 7 2 4F RT A16WE 2008021900196 20080219 00196 NM 2008 2 19 SWAA080732 1 20080207 A 5320 111A5000 FITTING BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 764SW 27878 DURING SCHEDULED 8Y CHECK, FOUND CENTER WING BOX FUSELAGE FUEL SHEAR FITTING CRACKED AT BS 540, BETWEEN LBL 40.87 AND RB L 40.87. REPAIRED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2008021900207 20080219 00207 NM 2008 2 19 SWAA080738 1 20080209 A 5755 6567179 FITTING BOEING 737 7373H4 1384600 NM NR 4 SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 4 GROUND SPOILER INBOARD FITTING LUG CRACKED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900210 20080219 00210 NM 2008 2 19 SWAA080775 1 20080210 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 16R CORRODED AT BS 485. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008021900211 20080219 00211 NM 2008 2 19 SWAA080776 1 20080210 A 5311 6545808 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, STR 7L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008021900216 20080219 00216 NM 2008 2 19 SWAA080800 1 20080212 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 294WN 32540 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008021900230 20080219 00230 NM 2008 2 19 SWAA080819 1 20080212 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 19R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008021900244 20080219 00244 NM 2008 2 19 CALA0800115 1 20080208 A 5320 6517684Y642 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 294 S7L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14335 23573 BS 294.5 STRINGER 7L INTERCOSTAL WEB CRACKED AT IB FORWARD CORNER. REMOVED AND REPLACED PER ECRA 5310-04700. 2 L 7 2 4F RT A16WE 2008021900289 20080219 00289 NM 2008 2 19 GTIA0800001 1 20080128 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 521NK 2797 FLOORBEAM BETWEEN -Y254 AND -Y765 SHOWS SIGNS OF CORROSION. REMOVED AND REPLACED FLOORBEAM 2 L 7 2 4F RT A28NM 2008021900295 20080219 00295 NM 2008 2 19 SWAA080773 1 20080210 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008021900300 20080219 00300 WP 2008 2 19 G60A200800014 1 20080207 A 5414 PANEL DOUG DC10 DC1030F 3023504 WP NR 2 NACELLE CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 606GC 47929 NR 2 ENG PYLON PANEL 437DR HAS CRACK NEAR BASE OF FIN. 2 L 7 3 4F RT A22WE 2008021900303 20080219 00303 2008 2 19 SWAA080684 4 20080205 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 240WN 32503 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008021900304 20080219 00304 NM 2008 2 19 SWAA080685 1 20080204 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 259WN 35554 R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008021900305 20080219 00305 WP 2008 2 19 G60A200800017 1 20080207 A 5754 RIB DOUG DC10 DC1030F 3023504 WP SLAT CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 606GC 47929 FOUND LT L/E SLAT NR 1 RIB CRACKED AT STA XIS 201. 2 L 7 3 4F RT A22WE 2008021900306 20080219 00306 NM 2008 2 19 SWAA080687 1 20080206 A 5330 6545768 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 331, STR 17R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008021900316 20080219 00316 NM 2008 2 19 SWAA080694 1 20080206 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900317 20080219 00317 NM 2008 2 19 HALA0800044 1 20080110 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 325 S3L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LIGHTING STRIKE ON A/C CROWN AT LOCATION, STA 325 ABOVE S3L. REPAIRED IAW 767-300 SRM 53-00-01, REPAIR 8. 2 L 7 2 4F RT A1NM 2008021900327 20080219 00327 NM 2008 2 19 SWAA080744 1 20080208 A 5330 6547955 BEAR STRAP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT AFT CARGO DOOR LOWER FWD CUTOUT BS 798. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008021900329 20080219 00329 NM 2008 2 19 SWAA080745 1 20080210 A 5315 65C33950 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 46 TO RBL 46. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900335 20080219 00335 NM 2008 2 19 SWAA080747 1 20080210 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900336 20080219 00336 NM 2008 2 19 SWAA080750 1 20080210 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OUT. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008021900341 20080219 00341 NM 2008 2 19 SWAA080754 1 20080208 A 3350 20131A BATTERY PACK BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008021900342 20080219 00342 NM 2008 2 19 SWAA080764 1 20080210 A 5230 6549889 SKIN BOEING 737 7373G7 1384595 NM CARGO DOOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR OUTER SKIN CREASED. REMOVED AND REPLACED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008021900343 20080219 00343 NM 2008 2 19 SWAA080765 1 20080210 A 5330 65465768 SKIN BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 362 AND BS 364, STR 27L. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008021900348 20080219 00348 NM 2008 2 19 SWAA080757 1 20080210 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED MV3 CHECK, FOUND RT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER M M. 2 L 7 2 4F RT A16WE 2008021900354 20080219 00354 NM 2008 2 19 SWAA080791 1 20080211 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND STRINGER 28R CORRODED AT BS 360. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008021900355 20080219 00355 NM 2008 2 19 SWAA080798 1 20080211 A 3097 722SW WIRE HARNESS BOEING 737 7377H4 1384404 NM COCKPIT ARCED A SWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 735SA 27867 AIR TURNBACK, FLIGHT DECK L1 WINDOW ELECTRICAL CORD ARCED. REMOVED AND REPLACED ELECTRICAL HARNESS PER MM. 2 L 7 2 4F RT A16WE 2008021900360 20080219 00360 NM 2008 2 19 SWAA080827 1 20080213 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008021900361 20080219 00361 NM 2008 2 19 SWAA080828 1 20080213 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930 AND BS 920, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008022000035 20080220 00035 NM 2008 2 20 ASMF200801004 1 20080123 A 3340 LIGHT BOEING 777 777* UTILUSE NM GE GE90 GE9092B 30036 NE DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 774AM 28689 THE LT SLAT NR 1 OF THE AC REGISTRATION N746AM HIT AC LT WING TIP. DETAILED INSPECTION WAS PERFORMED ON LT WING TIP DETE CTING CRACKED THE LENS OF THE LT REAR POSITION LIGHT AND MISSING THE AFT STATIC TIP WING DISCHARGE, SO LENS WAS REPLACED AND STATIC TIP WING DISCHARGE WAS INSTALLED IAW MM 33-43-02 AND 23-61-01, TESTED CORRECT. 2 L 7 2 4F 4 F RT T00001SE E00049EN 2008021900053 20080219 00053 WP 2008 2 19 AALA200800199 1 20080129 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 255AA 49287 LGA - EMERGENCY LIGHT AT OVERHEAD SEAT 16D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008021900056 20080219 00056 NM 2008 2 19 AALA200800201 1 20080129 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 796AN 30796 DFW - EMERGENCY LIGHT AT AFT GALLEY LEFT SIDE MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT AFT GALLEY LEFT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900073 20080219 00073 NM 2008 2 19 CALA0800125 1 20080212 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM BS 867 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 FRAME CRACKED AT STA 867 ABOVE STRINGER 9R. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04714. 2 L 7 2 4F RT A16WE 2008021900078 20080219 00078 NM 2008 2 19 CALA0800107 1 20080130 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373T0 1384582 NM CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14335 23573 FOUND RBL 18 HAS SIGNS OF SURFACE CORROSION. REMOVED FLOORBOARDS FOR FOM IAW SRM 51-40-02. REMOVED AND REPLACED CORROD ED SEAT TRACK SECTION IAW SRM 53-00-52 FIG 201 AND SRM 51-40-02. REINSTALLED FLOORBOARDS IAW SRM 51-40-02 SEALED FLOORB OARDS PER AMM 51-30-00. 2 L 7 2 4F RT A16WE 2008021900086 20080219 00086 EU 2008 2 19 MALA080022 1 20080207 A 3350 66362 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 415XJ 340B415 EMERGENCY FLOOR LIGHT P/N 6636-2 INOP. REMOVED AND REPLACED LIGHT IAW SAAB AMM 33-50-20-04. 2 L 7 2 4T RT A52EU 2008021900098 20080219 00098 WP 2008 2 19 G60A200800016 1 20080207 A 5754 RIB DOUG DC10 DC1030F 3023504 WP SLAT CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 606GC 47929 FOUND LT L/E SLAT NR 1 RIB CRACKED AT STA XIS 189. 2 L 7 3 4F RT A22WE 2008021900103 20080219 00103 NM 2008 2 19 AALA200800216 1 20080130 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 55C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900112 20080219 00112 NM 2008 2 19 AALA200800225 1 20080131 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 772AN 29580 DFW - EMERGENCY LIGHT AT SEAT 40G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 40G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900115 20080219 00115 SW 2008 2 19 WGEA200800025 1 20080205 A 2721 271127521004 ACTUATOR ECLIPS EA500 ECLIPSEEA500 3350000 SW RUDDER TRIM DEFECTIVE E WGEA O OTHER O OTHER CR CRUISE 1 EA 27 139DJ 91 000054 UNCOMMANDED TRIM IN FLIGHT, ON GROUND. ELEVATOR TRIM GOING UP AND DOWN AND SPLIT. REFERENCE DAYJET WORK ORDER 1299, NR I 1 AND 3. REFERENCE TSR 22-020608G AND NRI 1 FOR RUDDER TRIM ACTUATOR REPLACEMENT. REMOVED AND REPLACED RUDDER TRIM A CTUATOR WITH NEW ACTUATOR IAW EA500 AMM 27-23-16. PERFORMED OPERATIONAL CHECK OF RUDDER TRIM ACTUATOR IAW EA500 27-00-0 1. OPS CHECK GOOD. 1 L 7 2 4J RT A00002AC 2008021900134 20080219 00134 NM 2008 2 19 AALA200800228 1 20080131 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 970AN 30096 DFW - EMERGENCY LIGHT AT SEAT 28D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008021900135 20080219 00135 NM 2008 2 19 AALA200800230 1 20080201 A 2150 A/C PACK BOEING 757 757223 1384957 NM CONTAMINATED A AALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 660AM 25294 DTW INFLIGHT T398/01FEB ORD TO LGA - CREW REPORTED SMOKE IN CABIN WITH LEFT HYDRAULIC PRESSURE INDICATION AND RUDDER RA TIO LIGHT ILLUMINATED. LANDED DTW WITHOUT INCIDENT. FOUND GLYCOL INGESTED INTO AIR CONDITIONING. PERFORMED PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008021900172 20080219 00172 2008 2 19 MALA080021 4 20080126 A 3497 CONNECTOR CNDAIR CL600 CL6002D24 1390016 EA AOA SENSOR FAULTY A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 906XJ 1806 15138 ACFT STALL WARNING & STICK SHAKER OCCURRED AT FL390. CREW TOOK EVASIVE ACTION INITIATING A DESCENT. STICK SHAKER CONTI NUED FOR SOME TIME BEFORE STOPPING. CREW REPORTED THAT THE STALL WARNING OCCURRED AT FL390 & AGAIN AT FL340. CAPTAIN E XPRESSED CONCERN THAT SINCE THE AFT CARGO DOOR INDICATOR WAS DEFERRED THEY THOUGHT MAYBE THE DOOR HAD OPENED IN FLIGHT. DECLARED AN EMERGENCY. PRESSURIZATION HAD NOT BEEN LOST. FLT DIVERTED & LANDED WITHOUT FURTHER INCIDENT.. FOUND NR 1 LT AOA SENSOR CONNECTOR TO BE AT FAULT. REPLACED CONNECTOR IAW STANDARD PRACTICE M/M. 2 L 7 2 4F RT A21EA 2008021900232 20080219 00232 NM 2008 2 19 SWAA080821 1 20080212 A 5551 6551524 FITTING BOEING 737 7373TO 138447G NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING P ER SRM. 2 L 7 2 4F RT A16WE 2008021900236 20080219 00236 NM 2008 2 19 SWAA080792 1 20080211 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 680, STR 10L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008021900292 20080219 00292 EA 2008 2 19 CHQA200800026 1 20080207 A 4990 MS280343 BULB CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE APU OIL TEMP MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 473CA 7668 GEE873451 CLT TO IAH - APPROXIMATELY 40 MINUTES INTO THE FLIGHT THE CREW RECEIVED AN APU OIL TEMP MESSAGE ON EICAS. THE AIRCRAFT DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE APU WITH OIL AND IT OPERATED NORMALLY, AND T HE AIRCRAFT WAS RETURNED TO SERVICE. THE APU OIL TEMP BULB WAS LATER REPLACED ON 2/8 AND THE APU, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2008021900330 20080219 00330 NM 2008 2 19 SWAA080746 1 20080210 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900347 20080219 00347 NM 2008 2 19 SWAA080756 1 20080209 A 5743 115A5211 FITTING BOEING 737 7377H4 1384404 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 720WN 27854 DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900350 20080219 00350 NM 2008 2 19 SWAA080788 1 20080211 A 3397 65C27093 CONNECTOR BOEING 737 737317 138447P NM CABIN DIRTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INTERMITTENT. FOUND LIGHT ASSY CONNECTOR DIRTY. CLEANED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2008021900353 20080219 00353 NM 2008 2 19 SWAA080797 1 20080211 A 2560 6557463 FITTING BOEING 737 7373G7 1384595 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2008021900359 20080219 00359 NM 2008 2 19 SWAA080826 1 20080213 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 791, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900362 20080219 00362 NM 2008 2 19 SWAA080856 1 20080213 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900363 20080219 00363 NM 2008 2 19 SWAA080855 1 20080213 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022000002 20080220 00002 WP 2008 2 20 NWAA080529881 1 20080214 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 676MC 47652 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT LIGHTS FOR THE TAIL COMPARTMENT WERE INOPERATIVE. BOTH LEF T AND RIGHT LAMPS WERE CHANGED BUT DID NOT CORRECT THE FAULT. MAINTENANCE THEN REPLACED THE BATTERIES AND THE SYSTEM OP ERATIONALLY CHECKED FUNCTIONAL. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008022000084 20080220 00084 SO 2008 2 20 C2XA08TY026 1 20080205 A 5730 14537011003 SKIN EMB 145 EMB145LR 3260212 SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15986 145254 TYS - DURING AN A-CHECK INSPECTION A CRACK IN THE UPPER LT WING SKIN FWD OF THE I/B SPOILER CENTER HINGE POINT. THE SKI N WAS INSPECTED AND PLACED ON DMI FOR 500FC WITH A REINSPECT EVERY 50FC IAW IC2008-145/00965. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022000086 20080220 00086 SO 2008 2 20 C2XA08IA052 1 20080207 A 3230 355022002 ELECTRONIC UNIT EMB 145 EMB145XR 3260214 SO LANDING GEAR INOPERATIVE A C2XA O OTHER J WARNING INDICATION DE DESCENT 1 SW 27 11106 12632 12632 145650 IAH - FLIGHT 2271 - THE CREW REPORTED, RECEIVED A LANDING GEAR AIR GROUND FAILED EICAS MESSAGE WHEN THE GEAR WAS SELECTE D DOWN, AND CLEARED WHEN GEAR EXTENDS. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED T HE LANDING GEAR ELECTRONIC UNIT (LGEU), OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008022000092 20080220 00092 NM 2008 2 20 SWAA080853 1 20080213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008022000093 20080220 00093 NM 2008 2 20 SWAA080854 1 20080213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022000095 20080220 00095 NM 2008 2 20 SWAA080829 1 20080213 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 410WN 27897 AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008022000109 20080220 00109 NM 2008 2 20 HALA0800145 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 2 CORROSION ON SEAT TRACKS, SECTION 46, RBL 11, STA 1197+32. REWORKED IAW SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022000110 20080220 00110 NM 2008 2 20 HALA00800146 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 2 CORROSION ON SEAT TRACKS AT SECTION 45,RBL 11, STA 1197+75. REWORKED AREA IAW SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022000112 20080220 00112 NM 2008 2 20 SWAA080830 1 20080213 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 422WN 29826 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 157. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008022000113 20080220 00113 NM 2008 2 20 SWAA080831 1 20080213 A 3350 100031 SIGN BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND AFT CABIN EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EXIT SIGN ASSY PER MM. 2 L 7 2 4F RT A16WE 2008022000114 20080220 00114 NM 2008 2 20 SWAA080832 1 20080213 A 5311 6547959 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CORRODED AT BS 794, STR 27R. REMOVED AND REPLACED FRA ME PER ACO. 2 L 7 2 4F RT A16WE 2008022000127 20080220 00127 NM 2008 2 20 TSAA0853006 1 20080214 A 5330 6545768 SKIN BOEING 737 737290C 138448V NM BS 486 S14R DENTED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 842AL 23136 DENT IN SKIN AT STR 14 + 6 BS 486. REPAIRED BY ECO 3720 FINAL REPAIR SIZE APPROX 13IN X 19IN. 2 L 7 2 4F A16WE 2008022000128 20080220 00128 NM 2008 2 20 TSAA0853007 1 20080214 A 5330 6545768 SKIN BOEING 737 737290C 138448V NM BS 444 S14R DENTED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 842AL 23136 DENT IN SKIN AT STR 14 +6 BS 444. REPAIRED BY ECO 3720 FINAL REPAIR SIZE APPROX 12IN X 16IN. 2 L 7 2 4F A16WE 2008022000138 20080220 00138 2008 2 20 SWAA080842 4 20080213 A 2565 6949956 CABLE BOEING 737 7373TO 138447G NM EVAC SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2008022000141 20080220 00141 NM 2008 2 20 SWAA080845 1 20080213 A 5311 65C22909 FRAME BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008022000146 20080220 00146 NM 2008 2 20 SWAA080839 1 20080213 A 5512 6573782 SKIN BOEING 737 7373TO 138447G NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 125. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008022000147 20080220 00147 NM 2008 2 20 SWAA080837 1 20080213 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 750SA 29802 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008022000148 20080220 00148 NM 2008 2 20 SWAA080838 1 20080213 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 750SA 29802 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2008022000153 20080220 00153 SO 2008 2 20 C2XA08SH027 1 20080219 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11544 145557 SHV - DURING C-CHECK LT OMEGA BEAM REPAIR AT FR 20 IS CORRODED. MX REMOVED AND REPLACED PREVIOUS REPAIR AT FR 20 IAW EM B 145 SRM 51-40-02 & 5300-10 FIG 201 DET A. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008022000155 20080220 00155 SO 2008 2 20 C2XA08SH029 1 20080216 A 5320 14522459001 ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11544 145557 SHV - DURING C-CHECK LT OMEGA BEAM RAMP ANGLE FR 19-20 IS CORRODED. MX REMOVED AND REPLACED CORRODED LT OMEGA BEAM RAMP ANGLE FR 19-20 IAW EMB 145 SRM 51-30-01 AND 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008022000170 20080220 00170 NM 2008 2 20 HALA0800062 1 20080130 A 5320 RAMP BOEING 767 7673G5 1385126 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SEVERE CORROSION AT AWR52, INT-MID GALLEY CART RAMP, ADJACENT TO TRASH CONTAINER. MID GALLEY REMOVED IAW GMM 25-01-49, RAMP INSPECTED AND REQUIRES REPLACEMENT. NEW RAMP INSTALLED AND GALLEY LOWER HALF INSTALLED ON A/C IAW 25-02-49. 2 L 7 2 4F RT A1NM 2008022000172 20080220 00172 NM 2008 2 20 HALA0800064 1 20080114 A 5753 SKIN BOEING 767 7673G5 1385126 NM TE FLAP CHAFED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LT INBOARD AFT FLAP HAS LEADING EDGE CHAFED ALONG IT LENGTH ASSESS DAMAGE PER SRM 57-53-02. AFT FLAP INCORRECTLY ADJUST ED, PULLING IN TIGHTLY AGAINST MID FLAP SEAL. BLENDED IAW SRM 57-53-01, FIG 101. RIG CHECK OF FLAPS OK. 2 L 7 2 4F RT A1NM 2008022000182 20080220 00182 SO 2008 2 20 SIMA200804302 1 20080116 A 3230 SWITCH EMB 145 EMB145 3260210 SO MLG MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION DE DESCENT 1 SW 21 612AE 145079 ON FLIGHT 4025, CREW REPORTED AFTER THEY SELECTED GEAR DOWN. A LANDING GEAR/LEVER DISAGREE MESSAGE APPEARED. THE MESSA GE REMAINED DURING TRANSIT AND AFTER LOCKED INDICATION. MESSAGE EXTINGUISHED APPROXIMATELY 1-2 SECONDS AFTER IN TRANSIT LIGHTS WENT OUT AND 3 GREEN INDICATIONS WERE ILLUMINATED. INITIATED GO-AROUND, PROCEEDED TO INITIATE THE EMERGENCY/ABN ORMAL PROCEDURE. DECLARED AN EMERGENCY AND DID NOT HAVE FUEL TO DO FLY BY AFTER FOLLOWING ALL PROCEDURES. LANDED SAFEL Y WITH NO FURTHER INCIDENTS. AIRCRAFT REMOVED FROM SERVICE. DURING OPS CHECK FOUND DOWN OVERRIDE SWITCH TO BE POSITION ED IN THE WRONG POSITION. AFTER PUTTING SWITCH TO NORMAL, OPERATION CHECK WAS GOOD IAW 32-30-00. AIRCRAFT RETURNED TO 2 L 7 2 4F RT T00011AT 2008022000183 20080220 00183 SO 2008 2 20 C2XA08ON084 1 20080203 A 3350 14532843401 CONTROL SWITCH EMB 145 EMB145XR 3260214 SO COCKPIT FAULTY A C2XA K NONE O OTHER UK UNKNOWN 1 SW 27 11181 8436 8436 14500904 FLT 7694 - LAX TO LAX - FLIGHT CREW REPORTED EMERGENCY LIGHTS STAYING ON, WHEN SWITCH ON AND OVERHEAD IS IN THE OFF POSI TION. MX PERSONNEL REMOVED AND REPLACED SWITCH MODULE OPERATIONALLY CHECKED SATISFACTORY. A/C WAS RELEASED TO RETURN F OR SERVICE. 2 L 7 2 4F RT 2008022000185 20080220 00185 SO 2008 2 20 SIMA200805004 1 20080215 A 2740 3621001013 CONTROL UNIT EMB 135 EMB135KL 3260302 SO PITCH TRIM MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 839AE 145653 ON FLIGHT 4393, CREW REPORTED AFTER TAKEOFF THAT MAIN PITCH TRIM INOP EICAS MESSAGE APPEARED ON EICAS. EMERGENCY WAS DE CLARED AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED HSCU PER EMB AMM 27-40-01 AND NR 8194; AIRCRAFT RETURNED TO SERVICE AND NR 8194; AND NR 8194; AND NR 8194; AND 8194. 2 L 7 2 4F RT T00011AT 2008022000186 20080220 00186 SO 2008 2 20 C2XA08ON085 1 20080206 A 2810 27700138101 FLAPPER VALVE EMB 145 EMB145XR 3260214 SO LT WING MISSING A C2XA K NONE K FLUID LOSS UK UNKNOWN 1 SW 27 11187 6979 6979 14500927 FLT 54 - MCI TO MCI - FLIGHT CREW REPORTED LEFT WING LEAKING FUEL. MX PERSONNEL REMOVED AND REPLACED LEFT WING FLAPPER VALVE OPERATIONALLY AND LEAK CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008022000192 20080220 00192 SO 2008 2 20 C2XA08ON087 1 20080208 A 5210 14540853407 DOOR EMB 145 EMB145XR 3260214 SO PAX DOOR OUT OF ADJUST A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 12166 10408 10408 14500831 FLT 2 - ONT TO ONT - FLIGHT CREW REPORTED MAIN DOOR HARD TO OPEN. MX PERSONNEL TIGHTENED BOLTS ON HANDLE POT, CLEANED/L UBE ROLLERS, OPERATIONALLY CHECKED SATISFACTORY. A/C WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008022000200 20080220 00200 WP 2008 2 20 NWAA080489870 1 20080211 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 779NC 48101 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINT ENANCE REPLACED THE EMERGENCY BATTERY PACK AND OPERATIONALLY CHECKED THE SYSTEM. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008022000205 20080220 00205 EU 2008 2 20 SIMA200805005 1 20080216 A 2120 ENGINE SAAB SF340 340B 7860101 EU LEFT ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 902AE 340B269 ON FLIGHT 3343, CREW REPORTED STRANGE ODOR IN CABIN. NO SMOKE OR FUMES OBSERVED. ALSO PASSENGER AND FLIGHT ATTENDANT O BSERVED BLUE BLACK SMOKE COMING OUT JUST AFT OF PROP. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENGINE IAW WC 72-49-03. LEAK AND OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4T RT A52EU 2008021900200 20080219 00200 WP 2008 2 19 G60A200800026 1 20080208 A 5330 SKIN DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 607GC 46978 FWD CARGO DOOR CUTOUT AFT EDGE FUSELAGE SKIN CRACKED APPROX 1/4". 2 L 7 3 4F RT A22WE 2008021900203 20080219 00203 2008 2 19 CALA0800113 4 20080206 A 2330 RDAV980301 MONITOR BOEING 757 757224 1384958 NM ROW 20 BURNED A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 33132 29281 REPORT OF ELECTRICAL SMOKE IN THE AREA OF ROW 20 OVERHEAD. REMOVED POWER TO THE RIGHT UTILITY BUS AND TURNED OFF THE L+ R RECIRC FANS, SMELL DISSIPATED. CONTINUED TO EWR WITH NO FURTHER ACTION. FOUND OVERHEAD MONITOR ATE ROW 20 BURNED. 2 L 7 2 4F RT A2NM 2008021900208 20080219 00208 2008 2 19 SWAA080739 4 20080208 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008021900220 20080219 00220 NM 2008 2 19 SWAA080803 1 20080212 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008021900222 20080219 00222 NM 2008 2 19 SWAA080813 1 20080212 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN DETERIORATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT LENS DETERIORATED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008021900229 20080219 00229 NM 2008 2 19 SWAA080818 1 20080212 A 5314 6562125 KEELBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 505D AND BS 525. REPAIRED BEAM PER ER. 2 L 7 2 4F RT A16WE 2008021900245 20080219 00245 NM 2008 2 19 SWAA080786 1 20080211 A 5755 654458114 ACTUATOR BOEING 737 7375H4 138449D NM NR 5 SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SPOILER OUTBOARD ACTUATOR FWD MOUNT CRACKED. REMOVED AND REPLACED SPOILE R ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2008021200194 20080212 00194 NM 2008 2 12 USAA920080327 1 20080111 A 5311 654655714 FRAME BOEING 737 7373Y0 1384671 NM BS 887 S9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 887, S9R. REPAIRED FRAME, BS 887, S9R IAW USAIRWAYS EA 100190. 2 L 7 2 4F RT A16WE 2008021200199 20080212 00199 WP 2008 2 12 DHL2007873541 1 20080114 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1040 DAMAGED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 873SJ 89073 46091 AFT CARGO COMPT FLOORBEAM 1/4" MISDRILLED HOLE AT STA 1040.000 RBL 56" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA F ORM 8110-3 DATED 01-15-08 EVA D85300031 REV IR DATED 01-04-08 DWG AE85-53-102 REV IR DATED 01-03-08. REMOVED FASTENERS IAW SRM 51-1-20D. FABRICATED REPAIR ANGLE AND STRAP IAW DWG AE85-53-102 REV IR HEAT TREATED REPAIR ANGLE IAW SRM 51-1-1 PG 1-13.17 NDT INSPECTED REPAIR AND STRAP NO CRACK ANGLE NO CRACK FOUND IAW DPS 4.707-1. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG NR AE85-53-102 REV IR SRM 51-1-20D SRM 51-3-1, SRM 5 1-3-0. 2 L 7 4 4F RT 4A25 2008021200201 20080212 00201 2008 2 12 ASAA0852534 4 20080201 A 3460 1762000101 COMPUTER BOEING 737 737890 1384527 NM FLT MANAGE MALFUNCTIONED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 579AS 35187 FMC FAIL ON BOTH CAPT'S AND F O'S. RESTORED BOTH AND CONTINUED. PERFORMED FMC OPERATIONAL TEST PER 34 61 00. NO DEFEC TS NOTED. FMC'S CHECK NORMAL. 2 L 7 2 4F RT A16WE 2008021200202 20080212 00202 NM 2008 2 12 ASAA0852536 1 20080203 A 7500 1074847 REGULATOR BOEING 737 737890 1384527 NM BLEED AIR SYSTEM FAULTY A ASAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 02 579AS 35187 ON DEPARTURE, BLEED AIR DUCT PRESSURE OSCILLATED BETWEEN 20 AND 40PSI. LT NEEDLE APPEARED TO BE CHASING RT WITH NEVER M ORE THAN 10 PSI SEP. REPLACED HIGH STAGE REGULATOR. BLEED AIR SYSTEM, OP CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2008021200203 20080212 00203 NM 2008 2 12 ASAA0852537 1 20080203 A 7500 1074926 REGULATOR BOEING 737 737890 1384527 NM BLEED AIR FAULTY A ASAA O OTHER O OTHER CL CLIMB 1 NM 02 579AS 35187 ON DEPARTURE BLEED AIR DUCT PRESSURE OSCILLATED BETWEEN 20 AND 40PSI. LT NEEDLE APPEARED TO BE CHASING RT WITH NEVER MO RE THAN 10 PSI SEP. REPLACED NR 2 ENGINE BLEED AIR REGULATOR. BLEED AIR SYSYTEM, OP CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2008021200206 20080212 00206 WP 2008 2 12 UPS08851605 1 20080111 A 5542 SKIN DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 1" CRACK BELOW RUDDER TAB ON RT SIDE OF RUDDER. RUDDER REPLACED ON N/R 123801. 2 L 7 4 4F RT 4A25 2008021200207 20080212 00207 WP 2008 2 12 UPS08851606 1 20080111 A 5541 RIB DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 9TH RIB FROM BOTTOM OF RUDDER IS CRACKED ON LT SIDE AT FRONT SPAR. RUDDER REPLACED ON N/R 123801. 2 L 7 4 4F RT 4A25 2008021200211 20080212 00211 NM 2008 2 12 USAA920080335 1 20080130 A 5311 652072328 FRAME BOEING 737 7374B7 1384702 NM BS 492 S24R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 454UW 24996 CLT - MAJOR REPAIR - FPBH INSP - NR 6005985 AND 03-0553-8-0385-1, FORWARD CARGO DOOR CUT OUT AFT FRAME CRACKED, BS 492. 4, S24R. REPAIRED FORWARD CARGO DOOR CUT OUT AFT FRAME, BS 492.4, S24R IAW USAIRWAYS EA 100205. 2 L 7 2 4F RT A16WE 2008021200218 20080212 00218 NM 2008 2 12 ASAA0842538 1 20080129 A 5210 6552873 SKIN BOEING 737 7374Q8 138447Q NM PAX DOO DEFORMED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 L1 DOOR UPPER AFT CORNER DEFORMED. INSTALLED REPAIR DOUBLER IAW SRM 52 00 01 REPAIR 2. PAINTED PER MM 51 20 99. 2 L 7 2 4F RT A16WE 2008021200220 20080212 00220 2008 2 12 FFKA020108124 4 20080201 A 6122 9696001115 TUBE WOODWARD BEECH 58 58 1152740 CE CONT O520 IO520CB 17032 SO PROP GOVERNOR BROKEN B FFKA E B A ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING K F J FLUID LOSS FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 05 11HW 1438180 TH271 244309R AFTER TAKEOFF PILOT REPORTED AN UN-COMMANDED FEATHERING OF THE LEFT ENGINE. AFTER LANDING MAINTENANCE FOUND OIL RESIDUE ON THE OUTSIDE OF ENGINE NACELLE, AND THE TUBE ASSEMBLY FOR THE PROPELLER ACCUMULATOR CRACKED AT THE FLARE ON THE PROPE LLER GOVERNOR FITTING. IT IS BELIEVED THAT THE B-NUT HAD BEEN OVER TIGHTENED ONE OR MORE TIMES, CUTTING THE FLARE OFF O F THE LINE ALLOWING OIL TO FLOW OUT. 1 L 7 2 3O 3 O 3A16 E5CE 2008021200227 20080212 00227 NM 2008 2 12 USAA920080336 1 20080115 A 5210 6516487 GATE BOEING 737 7373Y0 1384671 NM L1 DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - NR 6071109, L1 DOOR BOTTOM GATE PUSH ROD CENTER LUG CRACKED. REPLACED L1 DOOR LOWER GA TE IAW B737 SRM 52-11-51. 2 L 7 2 4F RT A16WE 2008021100034 20080211 00034 NM 2008 2 11 DLM90080155 1 20080201 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 772 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 RT CUSP WEB CORROSION STA 772 RBL 58. REPAIRED CUSP WEB IAW ERA 413196-14MA DATE 5/15/03 ON N/R 2000-0140 AT HMV-2 IN O KC. 2 L 7 2 4F RT A6WE 2008021100040 20080211 00040 NM 2008 2 11 Q2SA748003 1 20080205 A 7722 8DJ200LWW1 INDICATOR BOEING 747 747206B 1384856 NM EGT ERRATIC A Q2SA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 63 748SA 21110 EGT'S ALL READING ERRATIC DURING CLIMB-OUT FROM KMIA. OFF FLAGS FOR NR 2 COMES ON ERRATICALLY, NO LIGHTS COME ON. OPER ATIONAL NORMAL AT ENGINE START AND CRUISE FLIGHT. RETURNED TO KMIA. NO FUEL DUMPED. REMOVED AND REPLACED VERTICAL SCA LE EGT INDICATOR IN ACCORDANCE WITH AMM 77-21-03. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 2008021100075 20080211 00075 NM 2008 2 11 AALA200800184 1 20080127 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 752AN 30260 DFW - EMERGENCY LIGHT AT SEAT ROW 25G INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT ROW 25G. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021100081 20080211 00081 WP 2008 2 11 UPS08851610 1 20080131 A 3350 BULB DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 EMERGENCY EXIT LIGHTS DISARM CHECK BULB BURNED OUT. RELAMPED DISARM EMERGENCY LIGHT. OPS CHECKED GOOD PER MM 25-60-00. 2 L 7 4 4F RT 4A25 2008021100087 20080211 00087 NM 2008 2 11 AALA200800156 1 20080123 A 3350 COVER BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 767AJ 33539 DFW - EMERGENCY LIGHT AT OVERHEAD AISLE RIGHT NUMBER THREE DOOR HAS BROKEN COVER. REPLACED COVER FOR EMERGENCY LIGHT AT OVERHEAD AISLE RIGHT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021100103 20080211 00103 NM 2008 2 11 AALA200800190 1 20080127 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 694AN 26974 DFW - EMERGENCY LIGHT AT SEAT 22D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008021100112 20080211 00112 EA 2008 2 11 SWIA200819182 1 20080204 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 915EV 7754 FLT 3986 - LEFT WINDSHIELD OUTER PLY IS CRACKED. REPLACED PILOT'S WINDSHIELD IAW 56-11-01, P/N: NP-139321-B, S/N OFF: 0 2298H8774. 2 L 7 2 4F RT A21EA 2008021100118 20080211 00118 WP 2008 2 11 AALA200800097 1 20080118 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 961TW 53611 DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 8 TO 13 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEA D SEAT ROWS 8 TO 13. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008021100147 20080211 00147 WP 2008 2 11 DHL2007873515 1 20080113 A 5740 FITTING DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 873SJ 89073 46091 NR 3 MAIN TANK EXTERNAL FITTING CRACKED 2" AT STA XRS 74.000 S-51 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-20D. CLEANED AND APPLIED POLYURETHANE TOP YELLOW COATING TO AREA IAW SRM 51-1-12 PG 7. INSTALLED NEW FITTING IAW SRM 51-1-12, SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1 (TORQUE). RE FER TO NR 107761 FOR LEAK CHECK. 2 L 7 4 4F RT 4A25 2008021100156 20080211 00156 SO 2008 2 11 CHQA200800017 1 20080129 A 3310 12030182001 RHEOSTAT EMB EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL FO GLARESHIELD MELTED A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 843RP 145665 145599 CAE312124 TRI TO CVG - IMMEDIATELY AFTER THE CLIMB CHECKLIST WAS COMPLETED THE FIRST OFFICER NOTICED SMOKE. THE CAPTAIN VERIFIED THE SMOKE WAS COMING FROM THE FIRST OFFICER'S RHEOSTAT/GLARESHIELD AREA. O2 MASKS WERE DONNED AND THE MEMORY ITEMS FOR COCKPIT SMOKE WERE ACCOMPLISHED. THE AIRCRAFT RETURNED TO FIELD AT TRI AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPEC TED THE AIRCRAFT AND FOUND THE FIRST OFFICER'S GLARE SHIELD MOUNTED CHART HOLDER DIMMER SWITCH HAD MELTED. THE COCKPIT READING LIGHTS WERE DEFERRED AND THE CIRCUIT BREAKER COLLARED. THE FIRST OFFICER'S LIGHT CONTROL MODULE WAS LATER REPLA CED AND THE CIRCUIT BREAKER RESET. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008021100158 20080211 00158 NM 2008 2 11 AALA200800160 1 20080124 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 33G INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 33G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021100167 20080211 00167 WP 2008 2 11 AALA200800099 1 20080118 A 3350 SHROUD DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 961TW 53611 DFW - EMERGENCY LIGHT AT SEAT 17D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008021100170 20080211 00170 WP 2008 2 11 UPS08851575 1 20080124 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 LOWER SKIN HAS CRACK RUNNING OFF RIVET NR 1 PYLON STUB WING. REPAIRED LT OUTBD STUB WING LOWER SKIN REF SRM 57-02-01A-0 FIG 002. 2 L 7 4 4F RT 4A25 2008021100183 20080211 00183 EU 2008 2 11 08FDEA00359 1 20080205 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 655FE 20414 742 MCD FLOORBEAM HAS CRACK AT FR 32 LBL 67 FWD SIDE, REWORKED CRACKED FLOORBEAM IAW 53-10-15 FIG 212 SHEET 2. 2 L 7 2 4F RT A35EU 2008021200027 20080212 00027 EA 2008 2 12 A6WA200840022 1 20080114 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 CRACK EXIST ON INTERCOSTAL RBL 27, FS 484. BRACKET ON INTERCOSTAL RBL 27, FS 484, REPLACED IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200044 20080212 00044 NM 2008 2 12 2008UALA00499 1 20080128 A 2822 568129117003 PUMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUEL SYSTEM MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 216UA 30549 R CENTER BOOST PUMP UNABLE TO OPERATE. SUSPECT FAULTY FUEL PUMP. REPLACED CENTER RT ELECTRIC OVERRIDE FUEL PUMP. OPS C HECKS NORMAL. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021200055 20080212 00055 NM 2008 2 12 2008UALA00489 1 20080128 A 5320 FLOOR SUPPORT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 AFT CABIN LT LAV FLOOR SUPPORT I CHANNEL BETWEEN STA 1008 AND 1016 LBL 5 TO LBL 10 IS CORRODED AROUND FASTENER HOLE AND UPPER SURFACE. REPLACED FLOOR SUPPORT I CHANNEL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200063 20080212 00063 NM 2008 2 12 2008UALA00474 1 20080126 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 L1 DOOR LOWER GATE HAS HOLE IN INSIDE LIP. INSTALLED FILL WELD REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200072 20080212 00072 NM 2008 2 12 2008UALA00466 1 20080128 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT UPPER DECK ALONG STAIRS WALL INOP. RESECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200082 20080212 00082 NM 2008 2 12 2008UALA00452 1 20080125 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 FWD PIT AT STA 600, STR 24L FRAME IS DENTED ON INBOARD FLANGE. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021200088 20080212 00088 NM 2008 2 12 2008UALA00410 1 20080122 A 3350 582233 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 EMERGENCY EEL LIGHT INOP AT RT MID CLOSET. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021200090 20080212 00090 NM 2008 2 12 2008UALA00408 1 20080122 A 3350 582233 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 EMERGENCY EEL LIGHT INOP FROM SEAT 6EF TO 10EF. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021200106 20080212 00106 NM 2008 2 12 2008UALA00360 1 20080122 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY EXIT SIGN INOP ABOVE DOOR 3 RIGHT. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200159 20080212 00159 NM 2008 2 12 2008UALA00049 1 20080103 A 3350 276005 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHTS INOP LT OVERWING FWD 2 ASSY'S. REPLACED FUSE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200254 20080212 00254 NM 2008 2 12 AMTA200800018 1 20080117 A 3350 20131A BATTERY PACK BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 EMERGENCY EXIT SIGN AND FLOOR PATH LIGHTING AT L2 DOOR INOPERATIVE. REPLACED BATTERY PACK, OPS CHECK GOOD REF MM 33-51- 07. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008021200255 20080212 00255 NM 2008 2 12 AMTA200800019 1 20080116 A 3350 20131A BATTERY PACK BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 520AT 27976 EMERGENCY FLOOR LIGHTING INOPERATIVE AT ROWS 6 DEF - 9 DEF. REMOVED AND REPLACED FWD BATTERY PACK. OPS CHECK GOOD. (K ) 2 L 7 2 4F 4 F RT A2NM E12EU 2008021200258 20080212 00258 EA 2008 2 12 A6WA200840011 1 20080114 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE SERVICE DOOR LACK OF LUBE A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 A6WA 7899 SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. CLEANED AND LUBED OUTER HANDLE AND OPS CK NORMAL IAW 52-41-00. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200260 20080212 00260 SO 2008 2 12 MLJ2008F00000 2 20080114 A 8530 AEC648029 PISTON CESSNA 310 310Q 2074242 CE CONT O470 IO470VO 17026 SO NR 2 CYLINDER FAILED E MLJA O OTHER O OTHER NR NOT REPORTED 1 GL 11 790DM 933 310Q0828 900983 THE LT ENGINE WAS EXHIBITING LOW OIL PRESSURE. THE OIL FILTER WAS PULLED, CUT OPEN, AND INSPECTED. A SIGNIFICANT AMOUN T OF METAL WAS FOUND. THE ENGINE WAS THEN TORN DOWN FOR FURTHER INSPECTION. CHUNKS OF PISTON SKIRTING WAS FOUND IN THE OIL PAN, NR 2 PISTON HAD COME APART AT THE SKIRTING AROUND THE BOTTOM RING-LAND BELOW THE PISTON PIN, AND THE NR 1 PIST ON WAS FOUND THE BE CRACKED IN THE SAME AREA THAT THE NR 2 PISTON WAS BROKEN. NR 2 PISTON TAKEN FOR METALLURGICAL TESTI NG. A POSSIBLE CONTRIBUTING FACTOR MAY HAVE BEEN THE START OF THE ENGINE AT A TEMPERATURE NEAR 0 DEGREES (F). (K) 1 L 7 2 3O 3 O 3A10 3E1 2008021200265 20080212 00265 NM 2008 2 12 2008UALA00516 1 20080130 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 DOOR 1R AFT SILL EMERGENCY LIGHT IS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200269 20080212 00269 NM 2008 2 12 2008UALA00520 1 20080130 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 UPPER DECK SEAT 15 LEFT EMERGENCY LIGHT IS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200275 20080212 00275 NM 2008 2 12 2008UALA00526 1 20080130 A 5753 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU TE FLAP DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 302UA 23643 LEFT INBOARD MID FLAP DELAMINATED OUT OF LIMITS. REPAIRED DELAMINATION. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200277 20080212 00277 NM 2008 2 12 2008UALA00529 1 20080126 A 2497 LUG BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 GENERATOR CORRODED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 783UA 26950 FOUND NR 2 ENGINE GENERATOR FEEDER LUGS DISCOLORED, PITTED AND PROTECTIVE COATING FLAKED OFF. SUSPECT PITTING AND CORRO SION. REPLACED TERMINAL LUGS PER SWPM 20-15-21. PAGE 5.ACCOMPLISHED ENGINE RUN AND OPS GOOD PER MM-24-11-19 P410. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021200279 20080212 00279 NM 2008 2 12 2008UALA00531 1 20080130 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 AFT CABIN FLOORBEAM TEE CAP UPPER SURFACE CORRODED AT BS 986. FROM RBL 20 TO RBL 37. MAJOR REPAIR: CORROSION DAMAGE REMOVED. FABRICATED AND INSTALLED NEW TEE SECTION SPLICE ANGLES. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200283 20080212 00283 NM 2008 2 12 2008UALA00536 1 20080130 A 5743 ATTACH FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT MLG CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 RIGHT MLG SUPPORT BEAM OUTBOARD ATTACH FITTING IS CRACKED AT NR 2 HOLE IN TWO PLACES. THE CRACKS ARE AT 3 AND 6 O'CLOCK POSITIONS. MAJOR REPAIR: REPLACED RT MLG SUPPORT BEAM OUTBOARD FITTING. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200284 20080212 00284 NM 2008 2 12 2008UALA00537 1 20080130 A 5320 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FUSELAGE STR 17R CREASE BEAM LOWER ATTACH ANGLE IS CORRODED BS 325. MAJOR REPAIR: REMOVED AND REPLACED CORRODED ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200285 20080212 00285 NM 2008 2 12 2008UALA00538 1 20080130 A 5320 BRACKET BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 727D CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 AFT PIT BS 727D FORWARD RT ANTENNA MOUNT REINFORCING BRACKET CRACKED AT UPPER FORWARD HOLE. MAJOR REPAIR: REMOVED AND REPLACED REINFORCING BRACKET. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200287 20080212 00287 NM 2008 2 12 2008UALA00540 1 20080130 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 AFT ENTRY DOOR CUTOUT CREASE BEAM CORRODED AT AFT THRESHOLD NUT PLATE. MAJOR REPAIR: REPAIRED "Z" ANGLE WITH A TYPICAL FORMED SINGLE REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200288 20080212 00288 NM 2008 2 12 2008UALA00541 1 20080130 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 STR 17R CREASE BEAM CORRODED AT APPROX FWD EDGE OF DOOR 1R CUTOUT. MAJOR REPAIR: REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021200291 20080212 00291 NM 2008 2 12 2008UALA00548 1 20080130 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 EEL LIGHT ADJACENT TO DOOR 1R INOP. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021200293 20080212 00293 NM 2008 2 12 2008UALA00553 1 20080131 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY LIGHT INOP RIGHT CEILING AFT ROW 8. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021300002 20080213 00002 NM 2008 2 13 KCSA081053 1 20080201 A 5311 FRAME BOEING 747 747209B 138489B NM BS 1680 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FOUND FUSELAGE FRAME WEB IS CORRODED AT STA-1680 AT LBL-50. 2 L 7 4 4F RT A20WE 2008021300012 20080213 00012 NM 2008 2 13 KCSA081063 1 20080201 A 5330 SKIN BOEING 747 747209B 138489B NM BS 362 S42-43R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FOUND STA-362 SKIN DAMAGED BETWEEN STR-42R AND STR-43R. 2 L 7 4 4F RT A20WE 2008021300016 20080213 00016 NM 2008 2 13 KCSA081068 1 20080202 A 5730 SKIN BOEING 747 747209B 138489B NM RWS 679 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FOUND CORROSION ON RT WING LOWER SKIN INBOARD BOOST PUMP ACCESS PANEL CUTOUT FLANGE AT WS 679.50. 2 L 7 4 4F RT A20WE 2008021300018 20080213 00018 NM 2008 2 13 KCSA081071 1 20080204 A 5511 STRINGER BOEING 747 747209B 138489B NM HORIZONTAL STAB CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 HORIZ STAB CENTER SECTION LOWER STR-14 CORRODED AT RBL-14. 2 L 7 4 4F RT A20WE 2008021300020 20080213 00020 NM 2008 2 13 KCSA081070 1 20080203 A 5511 STRINGER BOEING 747 747209B 138489B NM HORIZONTAL STAB CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 HORIZ STAB LOWER STR-8 CORRODED AT RBL-14. 2 L 7 4 4F RT A20WE 2008021300021 20080213 00021 NM 2008 2 13 KCSA081072 1 20080204 A 5340 STRINGER CLIP BOEING 747 747209B 138489B NM BS 1680 S44L CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 STRINGER CLIP S44L IS CORRODED AT STA-1680. 2 L 7 4 4F RT A20WE 2008021300022 20080213 00022 NM 2008 2 13 KCSA081073 1 20080204 A 5340 BRACKET BOEING 747 747209B 138489B NM BS 1780 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FOUND STA-1780 LBL-69 FRAME TO SIDE RAIL BRACKET IS CRACKED .25 INCH. 2 L 7 4 4F RT A20WE 2008021300023 20080213 00023 WP 2008 2 13 ABXA080030 1 20080123 A 5310 99115057 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING WINDOW FRAME MODIFICATION, FOUND COCKPIT WINDOW ENCLOSURE CENTER FRAME HAD MULTIPLE CRACKS AT BOTH ENDS EXCEEDING LIMITS. REPLACED FRAME IAW DC9 SRM 53-03, FIGURE 34 AND DC9 SRM 51-10-4, (3 CRACKS: 1.5 INCH, 1.25 INCH, AND 1INCH). 2 L 7 2 4F A6WE 2008021300024 20080213 00024 WP 2008 2 13 ABXA080031 1 20080128 A 5310 591235020 DOUBLER DOUG DC9 DC941 302207N WP STRUCTURE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING WINDOW FRAME MOD, FOUND WINDSHIELD WIPER DOUBLER CRACKED, 3 INCHES LONG LOCATED 10.5" FROM THE RIGHT OUTBOARD EDG E. REMOVED AND REPLACED DOUBLER IAW EA 53300036-010. 2 L 7 2 4F A6WE 2008021300028 20080213 00028 NM 2008 2 13 ABXA080028 1 20080203 A 3350 20131 BATTERY PACK BOEING 767 767232 1385132 NM EMERGENCY LIGHTS DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 743AX 22218 EMERGENCY LIGHT NR 9023 IN SUPERNUMERARY INOPERATIVE, SECOND LIGHT INBOARD OF MAIN ENTRY DOOR. REMOVED AND REPLACED M73 6 BATTERY PACK WITH SPARE BATTERY PACK M734 IAW B767 MM 33-51-07. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2008021300031 20080213 00031 WP 2008 2 13 UPS08851624 1 20080111 A 5542 SKIN DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 EDGE CRACK ON RT SIDE OF RUDDER TAB CUT OUT. RUDDER REPLACED ON N/R 123801. 2 L 7 4 4F RT 4A25 2008021300032 20080213 00032 WP 2008 2 13 UPS08851625 1 20080102 A 5320 564989334 CHANNEL DOUG DC8 DC871F 302199D WP BS 732 RBL 65 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:C2 RT BELLY PANEL LANDING FRAME CRACKED AT STA 732 RBL65. REMOVED, FABRICATED AND INSTALLED RT BELLY PA NEL LANDING CHANNEL AT STA 732 AND RBL 65 PER DWG 5649893, SRM 51-1-21, SRM 51-1-20D AND SRM 51-01-24. 2 L 7 4 4F RT 4A25 2008021300034 20080213 00034 NM 2008 2 13 UPS08M51616 1 20080116 A 5414 AVB752579 PANEL DOUG MD11 MD11F 3023600 NM NR 2 NACELLE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE:C NR 2 PYLON PANEL 457GR HAS A DENT ON ITS SKIN. REPAIR ACCOMPLISHED PER EA 11-5400-27-A1772 AND UPS EO NO MD11-5480-28541-A. 2 L 7 3 4F RT A22WE 2008021300040 20080213 00040 NM 2008 2 13 ABXA080041 1 20080102 A 5330 141T333074 SKIN BOEING 767 767281 1385109 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 787AX 23020 R1 DOOR AFT LOWER CORNER SKIN HAD OUTER SKIN CRACKED. REPAIRED R1 DOOR AT AFT LOWER CORNER IAW B767 SRM. 2 L 7 2 4F RT A1NM 2008021300045 20080213 00045 NM 2008 2 13 USAA920080306 1 20080114 A 5753 654643099 SKIN BOEING 737 7373S3 1384711 NM TE FLAPS DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - NR 6033450, LEFT WING INBOARD FORE FLAP, UPPER SURFACE HAS AREA OF DEBOND, WBL 117.5 - WBL 119.5. REPAIRED LEFT WING INBOARD FORE FLAP, UPPER SURFACE IAW B737 SRM 51-70-10-2R REPAIR 3. 2 L 7 2 4F RT A16WE 2008021300048 20080213 00048 NM 2008 2 13 USAA920080309 1 20080113 A 5313 654657959 STRINGER BOEING 737 7373S3 1384711 NM BS 1120-1126 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - NR 6034177, CORROSION ON APU CUT OUT TORQUE BOX STRINGER, BS 1120 - BS 1126, S18R. REP LACED APU CUT OUT TORQUE BOX STRINGER, BS 1120 - BS 1126, S18R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008021300050 20080213 00050 NM 2008 2 13 USAA920080311 1 20080128 A 5320 141N5160U3 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 202UW 27811 BFM - MAJOR REPAIR - C4 CHECK - NR 6039997, CORROSION ON CABIN FLOOR SUPPORT, BS 343 - BS 365, RBL 45, WL 208. REPLACED CABIN FLOOR SUPPORT, IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008021300062 20080213 00062 NM 2008 2 13 USAA920080352 1 20080203 A 5755 SKIN BOEING 737 7373S3 1384711 NM NR 7 SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - NR 6033563, RIGHT WING NR 7 SPOILER HAS 2 AREAS OF DELAMINATION, WBL 356 - WBL 358 AND WBL 378 - WBL 387. REPAIRED RIGHT WING NR 7 SPOILER IAW B737 SRM 51-70-10-2R3. 2 L 7 2 4F RT A16WE 2008021200019 20080212 00019 EA 2008 2 12 A6WA200840033 1 20080112 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CARGO BAY GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 BRACKET ASSY FWD AND AFT OF CARGO STEP PLATE FOUND GOUGED. BRACKET ASSY FWD AND AFT ON CARGO STEP PLATE REPLACED IAW SR M 51-42-21. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200020 20080212 00020 EA 2008 2 12 A6WA200840032 1 20080117 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 700 S22-23L DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 DENT EXIST ON SKIN FS 700 STR L 22 TO L 23. REMOVED FRAME IAW REO 601R-53-61-2482. NEW FRAME INSTALLED IAW SRM 51-42-06 . (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200039 20080212 00039 NM 2008 2 12 2008UALA00507 1 20080130 A 5753 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RT WING TE FLAP NICKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 227UA 30555 RIGHT I/B MAIN FLAP UPPER PANEL HAS A NICK AROUND A FASTENER HOLE, APPROX 1.8 INCHES FROM O/B END AND 36.10 FROM AFT END . SUSPECT FOREIGN OBJECT DAMAGEREPAIRED PER SRM 51-00-04, OK TO CF PER EVA-71089. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021200042 20080212 00042 NM 2008 2 12 2008UALA00504 1 20080129 A 2120 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN & COCKPIT SMOKE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 221UA 30552 FLIGHT DIVERTED DUE TO SMOKE AND ODOR REPORTED IN CABIN AND COCKPIT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021200061 20080212 00061 NM 2008 2 12 2008UALA00481 1 20080127 A 3350 321431 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 840UA 1522 EPSU BATTERY FWD L DISPLAYED ON EMERGENCY LIGHT TEST. REPLACED BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021200103 20080212 00103 EA 2008 2 12 MASA200800049 1 20080120 A 5297 WIRE CNDAIR CL600 CL6002B19 1900309 EA LAV DOOR DAMAGED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 75993 7372 ASH FLT 7306 IAD - SMOKE IN LAV. REMOVED AND REPLACED LAV DOOR SWITCH AND REPAIRED DAMAGED WIRING. 2 L 7 2 4F RT A21EA 2008021200105 20080212 00105 NM 2008 2 12 2008UALA00361 1 20080122 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EEL INOP SEAT 54C. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200112 20080212 00112 NM 2008 2 12 2008UALA00357 1 20080122 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY LIGHT INOP AT DOOR 3 RIGHT BUSSLE LIGHT. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200251 20080212 00251 EA 2008 2 12 A6WA200840008 1 20080104 A 3241 428853 ANTI-ICE SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE MLG MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 410AW 15763 7490 GROUND LIFT DUMP UNSAFE CAUTION MESSAGE IN FLIGHT. QRH PROCEDURE CLEARED MESSAGE. COMPLIED WITH OPS CHECK OF SPOILER F LIGHT SYSTEM. IAW SYS IAW AMM 27-60-00 PARA 11. THIS MESSAGE IS CAUSED BY ANIT-SKID PROBLEM. REMOVED AND REPLACED IAW 32 -44-06. OPS CHECK GOOD AT THIS TIME/ REF LP 198609/4 FOR ANTI-SKID WRITE UP. REMOVED AND REPLACED ANTI-SKID CONTROL UN IT IAW 32-44-06. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200256 20080212 00256 2008 2 12 AMTA200800020 4 20080117 A 3140 WARNING SYSTEM BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT ACTIVATED A AMTA K NONE J WARNING INDICATION LD LANDING 1 GL 11 522AT 29330 (LT IRS FAULT) EICAS MSG COMES ON DURING ROLL OUT AFTER LANDING. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008021200266 20080212 00266 NM 2008 2 12 2008UALA00517 1 20080130 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 SEAT 57ABC EMERGENCY LIGHT IS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021300001 20080213 00001 NM 2008 2 13 ABXA080029 1 20080126 A 3350 335010401266 LIGHT BOEING 767 767205 1385121 NM CABIN DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 713AX 23058 EMERGENCY LIGHT ASSEMBLY AT MAIN ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY IAW B767 AMM CHAPTER 33. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2008021300003 20080213 00003 NM 2008 2 13 KCSA081054 1 20080201 A 5347 SEAT TRACK BOEING 747 747209B 138489B NM BS 1908 WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 AFT BILGE SEATRACK IS WORN UNDERNEATH AFT STOP AT RBL-25 AT STA-1908. 2 L 7 4 4F RT A20WE 2008021300026 20080213 00026 WP 2008 2 13 ABXR080033 1 20080109 A 5312 991016463 BULKHEAD DOUG DC9 DC915F 3022037 WP RT WHEEL WELL CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 166DE 47152 INBOARD KEEL BULKHEAD AT BUTT LINE '0', FS 604.00 VERTICAL ATTACH ANGLE ON AFT SIDE CRACKED. REPAIRED VERTICAL ATTACH A NGLE ON KEEL BULKHEAD STA 604 RIGHT IAW DC9 SSRM DWG K05159. 2 L 7 2 4F A6WE 2008021300055 20080213 00055 NM 2008 2 13 USAA920080334 1 20080128 A 5753 SKIN BOEING 737 7374B7 1384702 NM LT WING TE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 CLT - MAJOR REPAIR - C2 CHECK - NR 6005796/JK-15-2725C/1, LEFT WING OUTBOARD TRAILING EDGE FLAP HAS AREA OF DELAMINATION . REPLACED LEFT WING OUTBOARD TRAILING EDGE FLAP IAW B737 AMM 27-51-39. 2 L 7 2 4F RT A16WE 2008021300074 20080213 00074 NM 2008 2 13 F3LA200800043 1 20080206 A 5315 D5347218820400 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 15440 5503 2019 REFERENCE NON ROUTINE 26658, DURING C3/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE MAIN DECK FLOORBEAM AT LBL 47 AND FRAME 68. MAINTENANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF A3 19 SRM 51-42-11. UPON COMPLETION OF THE INSTALLATION, THE NEW FLOORBEAM WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008021300082 20080213 00082 EU 2008 2 13 08FDEA00366 1 20080207 A 5347 R5327049020000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 681FE 799 MDCC SEAT TRACK NR 1 BETWEEN FR 57 AND FR 57.1 HAS 2 SCALLOPS BROKEN. REMOVED DAMAGED SECTION OF TRACK AND INSTALLED SE AT TRACK REPAIR IAW A300-600 SRM 53-10-16, FIG 201. 2 L 7 2 4F RT A35EU 2008021300083 20080213 00083 EU 2008 2 13 08FDEA00367 1 20080207 A 5347 A5383202020400 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 681FE 799 MAIN CARGO DECK NR 1 SEAT TRACK BETWEEN FR 41 AND FR 45N HAS SEVERAL SCALLOPS WORN REMOVED AND REPLACED SEAT TRACK IAW A 300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008021300085 20080213 00085 NM 2008 2 13 USAA920080354 1 20080204 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 202UW 27811 BFM - MAJOR REPAIR - C4 CHECK - NR 6039970, LEVEL 2 CORROSION ON CABIN FLOORBEAM PREVIOUS REPAIR, BS 377.7, LBL 1 - LBL 20. REPLACED CABIN FLOORBEAM, BS 377.7, LBL 1 - LBL 20 IAW B757 SRM 53-15-01. 2 L 7 2 4F RT A2NM 2008021300086 20080213 00086 NM 2008 2 13 USAA920080355 1 20080204 A 5320 141N5160 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 202UW 27811 BFM - MAJOR REPAIR - C4 CHECK - NR 6039999, CORROSION ON CABIN FLOOR SUPPORT, BS 343- BS 365, RBL 62, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 343- BS 365, RBL 62, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008021300087 20080213 00087 NM 2008 2 13 USAA920080357 1 20080131 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 1520-1640 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 202UW 27811 BFM - MAJOR REPAIR - C4 CHECK, LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 1520 - BS 1640, BL 24.75. REPLACED CABIN SEAT TRACK, BS 1520 - BS 1640, BL 24.75 IAW B757 SRM 53-00-52. 2 L 7 2 4F RT A2NM 2008021300090 20080213 00090 NM 2008 2 13 USAA920080360 1 20080206 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 202UW 27811 BFM - MAJOR REPAIR - C4 CHECK - NR 6040676, LEVEL 2 CORROSION ON FLOOR SUPPORT, BS 1681, RBL 56. REPLACED FLOOR SUPPOR T, BS 1681, RBL 56 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008021300092 20080213 00092 NM 2008 2 13 USAA920080362 1 20080125 A 5311 FRAME BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q3 CHECK - NR JK -58-53507/7, CRACKED FRAME WEB, BS 380, S9L. REPAIRED FRAME WEB, BS 380, S9L IAW USAIRWAYS TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2008021300093 20080213 00093 NM 2008 2 13 USAA920080363 1 20080121 A 5311 FRAME BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q3 CHECK - NR JK-58-53507/4, CRACKED FRAME WEB, BS 727D, S9L. REPAIRED FRAME WEB, BS 727D, S9L IAW USAIRWAYS TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 2008021300100 20080213 00100 NM 2008 2 13 USAA920080370 1 20080122 A 5712 65C34815 RIB BOEING 737 7374B7 1384702 NM ZONE 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q3 CHECK - NR 03-0529-8-0083/1, LEFT WING FUEL TANK RIB CRACKED, WBL 135.50. REPAIRED LEFT WING F UEL TANK RIB, WBL 135.50 IAW BOEING DRAWING 65C34815. 2 L 7 2 4F RT A16WE 2008021300109 20080213 00109 WP 2008 2 13 UPS08851634 1 20080109 A 5220 STRUCTURE DOUG DC8 DC871F 302199D WP OVERWING DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 POSSIBLE CRACK LOWER AFT CORNER OF LT OVERWING EXIT DOOR. STOP DRILLED CRACK, FABRICATED AND INSTALL ED REPAIR DOUBLER IAW SRM 52-02-00 FIG 02, 51-1-24, 51-1-20D AND DWG 5758037. 2 L 7 4 4F RT 4A25 2008021300110 20080213 00110 WP 2008 2 13 UPS08851635 1 20080104 A 5753 SKIN DOUG DC8 DC871F 302199D WP LT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 2 DENTS ON LOWER SKIN LT I/B FLAP POSSIBLE CRACKS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-02-01. 2 L 7 4 4F RT 4A25 2008021300111 20080213 00111 WP 2008 2 13 UPS08851636 1 20080105 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS -38 WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 COCKPIT STA -38 SEAT TRACK IS WORN AND LOCK PIN HOLES ARE WORN. REMOVED AND REPLACED F/E AFT SEAT TR ACK IAW SRM 51-03-00, 51-01-24. 2 L 7 4 4F RT 4A25 2008021300113 20080213 00113 NM 2008 2 13 UPS08M51626 1 20080206 A 2810 FUEL TANK DOUG MD11 MD11F 3023600 NM LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 277UP 48578 ATB - PASSING 15000, RECEIVED A FUEL QUANTITY/USED CHECK LEVEL 2 ALERT. POSSIBLE FUEL LEAK. RAN CHECKLIST AND DETERMIN ED THERE WAS A LOSS OF FUEL. A/C BLOCKED IN WITH 89,600 LBS REMAINING FUEL. FUEL USED WAS 22,440 LBS TOTAL FUEL = 112, 040 LBS. A/C INITIALLY FUELED TO 122,988 LBS. COMPLIED WITH FIM 28-14-00 FIG 102 SHEETS 9810. NO FAULTS FOUND. NO AL ERTS PRESENT AT BLOCK IN. 2 L 7 3 4F RT A22WE 2008021300116 20080213 00116 2008 2 13 ASAA0852539 4 20080207 A 2310 8220990004 TRANSCEIVER BOEING 737 737890 1384527 NM HF SYSTEM MALFUNCTIONED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 558AS 35177 BOTH HF2 RADIOS WILL NOT GO INTO DATA MODE. UNABLE TO DUPLICATE. NR 2HF DATA MODE OPS NORMAL (REF MM23 27 00) HF OPS N ORMAL. (REF MM23 11 00) 2 L 7 2 4F RT A16WE 2008021300117 20080213 00117 NM 2008 2 13 SB08007 1 20080208 A 3350 20121 CHARGER BOEING 737 737401 1384701 NM EMERGENCY LIGHTS FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 417US 23984 PVD - MAINTENANCE REPORTED THE RIGHT AFT SERVICE DOOR AND CENTER AFT GALLEY EMERGENCY EXIT LIGHTS WERE ILLUMINATED. MAI NTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008021300118 20080213 00118 NM 2008 2 13 BB08010 1 20080208 A 3350 CHARGER BOEING 767 7672B7 1385107 NM EMERGENCY LIGHTS FAULTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 BRU - PART OF THE FLOOR LIGHTING FROM 6FG TO THE OVERWING EXIT WAS NOT WORKING. MAINTENANCE REPAIRED WIRING AND REPLACE D A BATTERY CHARGER. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A1NM 2008021300120 20080213 00120 NM 2008 2 13 08FDEA00255 1 20080124 A 5753 ARC2128501 HINGE DOUG MD11 MD11F 3023600 NM TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 617FE 48748 LEFT WING, OUTBOARD FLAP OUTBOARD HINGE AFT FAIRING STRUT AFT FASTENER HOLE FOUND CORRODED. CORROSION AT LEFT WING OUTB OARD FLAP OUTBOARD HINGE AFT STRUT AFT HOLE REPAIRED AS PER FEDEX EA NR 1-5750-117303, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008021300122 20080213 00122 NM 2008 2 13 08FDEA00369 1 20080208 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 MAIN DECK, AFTER FLOOR PANEL REMOVAL TO FACILITATE SEAT TRACK REPAIR, FOUND SEAT TRACK UNDER FLOOR PANEL AT STA 635, X = 33 CRACKED. SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 625 TO STA 665, X = 33" PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008021300128 20080213 00128 NM 2008 2 13 USAA920080381 1 20080112 A 5313 654988630 STRINGER BOEING 737 7373Y0 1384671 NM BS 500C CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - NR 6060939, CRACKED STRINGER, BS 500C S16R. REPAIRED STRINGER, BS 500C, S16R IAW USAIR WAYS ER 03-5312-01094-DD1. 2 L 7 2 4F RT A16WE 2008021300133 20080213 00133 NM 2008 2 13 USAA920080389 1 20080206 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 CLT - MAJOR REPAIR - C2 CHECK - NR 03-0553-8-0399/1, CRACKED BULKHEAD, BS 178, LBL 9, WL 234. REPAIRED BULKHEAD, BS 178 , LBL 9, WL 234 IAW B737 SRM 51-10-08 REPAIR 9. 2 L 7 2 4F RT A16WE 2008021300137 20080213 00137 NM 2008 2 13 USAA920080393 1 20080205 A 5320 WEB BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 CLT - MAJOR REPAIR - C2 CHECK - NR 03-0553-8-0105/3, CRACKED WEB, BS 184, LBL 17, WL 231. REPAIRED WEB, BS 184, LBL 17, WL 231 IAW B737 SRM 53-10-08. 2 L 7 2 4F RT A16WE 2008021300140 20080213 00140 2008 2 13 ASAA0842540 4 20080204 A 2565 1061323469 SLIDE BOEING 737 737490 1384715 NM R2 DOOR CONTAMINATED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 02 713AS 12322 225 30161 RIGHT FORWARD (R 2) SERVICE DOOR EMERGENCY SLIDE FAILED TO DEPLOY DURING DURING TEST. DETERMINE THAT SLIDE WAS TIED WIT H A CHORD WHICH PREVENTED IT FROM DEPLOYING. REMOVED SLIDE AND SHIPPED WITH A VIDEO OF THE FAILED DEPLOYMENT TEST. DET ERMINED NO SYSTEM FAULT. NON SYSTEM STRAP LEFT IN SLIDE DURING REPACKING AT THE AIR CRUISER FACILITY CAUSED FAILURE TO D EPLOY. 2 L 7 2 4F RT A16WE 2008021400003 20080214 00003 NM 2008 2 14 ZZDA2008064 1 20080129 A 5311 FRAME BOEING 717 717200 1383700 NM BS 1178 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 981AT 55040 CRACK AT TAIL COMPARTMENT, RIGHT CANTED FRAME 1178.225 BETWEEN LONG 13 AND 14 R. INSTALLED FORMED CHANNEL REPAIR ON RIG HT CANTED 1178.225 PER SRM 41-70-11 F 201. 2 L 7 2 4F TR A6WE 2008021400004 20080214 00004 EA 2008 2 14 TRAX200800155 1 20080130 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA ROW 4-9 INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 921EV 7819 FOUND EMERGENCY FLOOR TRACK LIGHTING INOP FROM ROW 4 TO 9. 2 L 7 2 4F RT A21EA 2008021400009 20080214 00009 EA 2008 2 14 TRAX200800160 1 20080201 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 836AS 7263 FLOOR LEVEL LIGHT BY PAX DOOR BROKEN. 2 L 7 2 4F RT A21EA 2008021400012 20080214 00012 EU 2008 2 14 TRAX200800163 1 20080128 A 5313 STRINGER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 FOUND STRG 17R CORRODED BTW FR 36-38. OUT OF LIMITS AS PER SRM: 53-61-00 FIG 301. REPAIRED IAW SRM 53-00-00 FIG 428 2 H 7 2 4T RT A53EU 2008021400014 20080214 00014 EU 2008 2 14 TRAX200800165 1 20080129 A 5220 ANGLE AEROSP ATR72 ATR72212 8680945 EU EMERGENCY EXIT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 ANGLE CRACKED ON EMERGENCY EXIT 843. 2 H 7 2 4T RT A53EU 2008021400022 20080214 00022 EU 2008 2 14 TRAX200800173 1 20080131 A 5753 BRACKET AEROSP ATR72 ATR72212 8680945 EU TE FLAP CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 642AS 395 TWO OMEGA BRACKET FOUND CRACKED ON INBOARD FLAP ARM OF LT INBOARD FLAP. 2 H 7 2 4T RT A53EU 2008021400024 20080214 00024 EA 2008 2 14 TRAX200800175 1 20080131 A 5300 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 680BR 7679 FWD PRESSURE BULKHEAD CRACKED WHERE PARKING BRAKE CABLE PASSES THROUGH. COMPLIED WITH REO 601R-53-11-563 AND EO 600-53- 217 C/W TO REPAIR THE FWD PRESSURE BULKHEAD. 2 L 7 2 4F RT A21EA 2008021200160 20080212 00160 NM 2008 2 12 2008UALA00048 1 20080103 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EEL INOP SEAT 4A AFT SECTION. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200162 20080212 00162 NM 2008 2 12 2008UALA00047 1 20080103 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHTS INOP COCKPIT CEILING, CEILING ROW 12, ROW 46 RT CEILING & ROW 46 LT CEILING. RELAMPED EMERGENCY LIGHT S. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200270 20080212 00270 NM 2008 2 12 2008UALA00521 1 20080129 A 3350 3020423 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 597UA 28750 LEFT AFT OVERWING EMERGENCY LIGHT INOP AND LENS CRACKED RIGHT AFT OVERWING EMERGENCY LIGHT INOP ALSO. REPLACED BOTH BUL BS AND REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021300004 20080213 00004 NM 2008 2 13 KCSA081055 1 20080201 A 5412 FIREWALL BOEING 747 747209B 138489B NM NR 4 NACELLE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 NR 4 PYLON FIREWALL CHAFED FROM FROM NAC-STA-180 TO NAC-STA-240 INBOARD SIDE. 2 L 7 4 4F RT A20WE 2008021300009 20080213 00009 NM 2008 2 13 KCSA081060 1 20080201 A 5330 SKIN BOEING 747 747209B 138489B NM BS 370 S43-44R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FOUND STA 370 SKIN DAMAGED BETWEEN STR-43R AND STR-44R. 2 L 7 4 4F RT A20WE 2008021300010 20080213 00010 NM 2008 2 13 KCSA081061 1 20080201 A 5330 SKIN BOEING 747 747209B 138489B NM BS 372 S41R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 FOUND STA-372 SKIN DAMAGED AT STR-41R. 2 L 7 4 4F RT A20WE 2008021300019 20080213 00019 NM 2008 2 13 KCSA081069 1 20080203 A 5511 STRINGER BOEING 747 747209B 138489B NM HORIZONTAL STAB CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 HORIZ STAB CENTER SECTION LOWER STR-7 CORRODED AT RBL-15. 2 L 7 4 4F RT A20WE 2008021300066 20080213 00066 WP 2008 2 13 AALA200800173 1 20080126 A 3230 SCHRADER VALVE DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 411AA 49322 RSW INFLIGHT T1093/26JAN - CREW REPORTED NOSE GEAR RED LIGHT AFTER RETRACTION. RETURNED TO RSW AND LANDED WITHOUT INCID ENT. ACCOMPLISHED NOSE LANDING GEAR STRUT REPACK AND REPLACED SCHRADER VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008021300068 20080213 00068 NM 2008 2 13 AALA200800179 1 20080126 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 668AA 25333 DFW - EXTERNAL EMERGENCY LIGHT AT LOWER AFT DOOR INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LOWER AFT D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008021300084 20080213 00084 NM 2008 2 13 USAA920080353 1 20080201 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 202UW 27811 BFM - MAJOR REPAIR - C4 CHECK - NR 6040679, LEVEL 2 CORROSION ON CABIN FLOORBEAM, BS 1640, BL 0. REPLACED CABIN FLOORBE AM, BS 1640, BL 0 IAW B757 SRM 53-15-01. 2 L 7 2 4F RT A2NM 2008021300095 20080213 00095 NM 2008 2 13 USAA920080365 1 20080124 A 5754 SKIN BOEING 737 7374B7 1384702 NM ZONE 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q3 CHECK - NR JK-11-27300/1, LEFT WING NR 2 SLAT LOWER SKIN CRACKED. REPAIRED LEFT WING NR2 SLAT L OWER SKIN IAW B737 SRM 57-43-01 REPAIR 6. 2 L 7 2 4F RT A16WE 2008021300102 20080213 00102 NM 2008 2 13 USAA920080372 1 20080125 A 5313 FRAME BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q5 CHECK - NR JK-46-53502/4, CRACKED FRAME, BS 312, RBL 72. REPLACED FRAME, BS 312, RBL 72 IAW B73 7 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008021300119 20080213 00119 2008 2 13 BB08011 4 20080208 A 2565 101651303 SLIDE BOEING 767 7672B7 1385107 NM ZONE 200 DISCONNECTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AY 47538 2898 26847 MIA - A LOWER DEPLOYMENT STRAP WAS FOUND RELEASED ON THE FORWARD SERVICE DOOR SLIDE ASSEMBLY. MAINTENANCE REPLACED THE FORWARD SERVICE DOOR ESCAPE SLIDE. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008021300124 20080213 00124 NM 2008 2 13 08FDEA00371 1 20080208 A 5347 ACA7104521 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 MAIN DECK, AFTER FLOOR PANEL REMOVAL TO FACILITATE SEAT TRACK REPAIR, FOUND SEAT TRACK UNDER FLOOR PANEL AT STA 635, X = -11 CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008021300136 20080213 00136 NM 2008 2 13 USAA920080392 1 20080206 A 5320 WEB BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 CLT - MAJOR REPAIR - C2 CHECK -NR 03-0553-8-0105/5, CRACKED VERTICAL WEB, BS 183, RBL 17, WL 225. REPAIRED VERTICAL WEB , BS 183, RBL 17, WL 225 IAW B737 SRM 53-10-08. 2 L 7 2 4F RT A16WE 2008021300201 20080213 00201 WP 2008 2 13 UPS08851643 1 20080109 A 5340 3755822511 FITTING DOUG DC8 DC871F 302199D WP FS 340 L35R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 A-PIT, CORROSION AND BARE METAL ON BATHTUB FITTING STA 340 AND L35R. REPLACED CORRODED BATHTUB FITTI NG AT STA 340 AND L35R IAW SRM 53-02 -00 FIG 002 AND DWG 3755822. 2 L 7 4 4F RT 4A25 2008021400023 20080214 00023 EU 2008 2 14 TRAX200800174 1 20080131 A 5753 BRACKET AEROSP ATR72 ATR72212 8680945 EU TE FLAP CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 642AS 395 OUTBOARD FLAP ARM OF RT INBOARD FLAP FOUND WITH 4 OMEGA BRACKET CRACKED. 2 H 7 2 4T RT A53EU 2008021400030 20080214 00030 EA 2008 2 14 TRAX200800181 1 20080201 A 5320 FLANGE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 680BR 7679 FS 280.00 OUTBD OF RBL 9.00, LOWER FLANGE CRACKED. REPAIRED IAW REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2008021400033 20080214 00033 EA 2008 2 14 TRAX200800184 1 20080202 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 STA 280 CROSSBEAM CORRODED. 2 L 7 2 4F RT A21EA 2008021400038 20080214 00038 NM 2008 2 14 ZZDA2008050 1 20080107 A 5311 FRAME BOEING 717 717200 1383700 NM BS 1178 S25R DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 A/C STRUCK BY BAGGAGE CART, STA 1178 FRAME DAMAGED BETWEEN LONGERON BL0 AND 25R. INSTALLED COMPLETE REPAIR PART AT STA 1178 BETWEEN LONG BL0 AND 25R IAW B717 SRM 51-41-05 AND MESSAGE 1-CEY7GK AND AIRTRAN EA17-53-009392. 2 L 7 2 4F TR A6WE 2008021400042 20080214 00042 2008 2 14 HALA0800035 4 20080206 A 3460 8221261101 COMPUTER BOEING 767 76733A 1385209 NM FLT CONTROL FAULTY A HALA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 WP 13 587HA 33421 DURING TAKEOFF LNAV AND VNAV WOULD ENGAGE BUT WOULD NOT CAPTURE GREEN LIGHTS ON FMA AND WHITE LIGHTS ON ANNUNCIATOR (ADI ) UNDER ATT-ROLL MODES ANNUNCIATOR SHOWED ALT AND HDG HOLD (MODES) AP WAS NOT FUNCTIONAL (CTR). ALSO ON CLIMB-OUT WHEN VNAV ENGAGED, AT DISENGAGED 3404134 046138 07F631 LT. MCDP LAST LEG FAULTS IND FMC L-TMC, FMC L-R CH AND FD BAR MODES E RROR. REMOVED AND REPLACED LEFT FMC PER AMM 34-61-01 AND DATA CROSSLOAD PER AMM 34-61-00. LEFT FMC NORMAL. ACCOMPLISH MCDP TEST NR 40 AND TEST NR 59 NO FAULTS NOTED. BOTH TEST PASSED PER AMM 22-00-02. AIRCRAFT LMP STATUS RETAINED LAND 3. ACCOMPLISHED TSI NR 22-00/0004771, REPLACED NR 1 FCC. GROUND OPS CHECK OK, 22-11-01. ACCOMP MCDP TEST 30. NO FAUL 2 L 7 2 4F RT A1NM 2008021400047 20080214 00047 EA 2008 2 14 TRAX200800200 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 379-477 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 LT SIDEWALL SEAT RAIL FS 379.0 TO FS 477.40 AT HAS CORROSION DAMAGE. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IA W SRM 53-21-49. APPLIED ALODINE IAW CRJ 700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2008021900269 20080219 00269 NM 2008 2 19 CALA0800132 1 20080212 A 5551 6550581 FITTING BOEING 737 737524 1384721 NM HORIZONTAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 RT HORIZONTAL STAB FORWARD UPPER LUG HAS CORROSION. REMOVED SLEEVE AND BUSHINGS. REMOVED CORROSION AND PERFORMED REQUI RED INSPECTIONS PER ECRA 5510-01915. FABRICATED AND INSTALLED REPAIR SLEEVE AND FLANGE BUSHINGS PER SRM 55-10-10. 2 L 7 2 4F RT A16WE 2008021900279 20080219 00279 NM 2008 2 19 CALA0800135 1 20080206 A 5322 65465592 SHEAR TIE BOEING 737 7373T0 1384582 NM BS 927 S26-27R CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 STA 927 FRAME TO SKIN ATTACH LEG CORRODED BETWEEN STRINGER 26R AND 27R. REMOVED AND REPLACED DAMAGED FRAME SECTION PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2008021900308 20080219 00308 NM 2008 2 19 SWAA080686 1 20080206 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER 25L CORRODED AT BS 927. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008021900346 20080219 00346 NM 2008 2 19 SWAA080755 1 20080209 A 5743 115A5211 FITTING BOEING 737 7377H4 1384404 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 720WN 27854 DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUG CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900351 20080219 00351 NM 2008 2 19 SWAA080790 1 20080211 A 5330 6545768 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 312, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008022000058 20080220 00058 NM 2008 2 20 CALS097004 1 20080126 A 5610 65B270462 WINDSHIELD BOEING 747 747409 13848AU NM COCKPIT CRACKED W SAJF K NONE O OTHER IN INSP/MAINT 1 WP 03 18251 58930 27965 B-18251, FLIGHT CI-003 ENROUTE, GROUND VISUAL INSPECTION FOUND 1 CM CRACK AT (2R) WINDSHIELD EDGE. 2 L 7 4 4F RT A20WE 2008022000121 20080220 00121 NM 2008 2 20 HALA0800134 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1030 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 LIGHT SURFACE CORROSION TO TRACK BASE, AT LBL 54.75 CROWN DAMAGE AT BS 1030. REWORK CORROSION IAW SRM 51-10-02 REV 76. ALODINE REWORK AREA IAW SRM 51-20-01, REV 76. PRIME IAW AMM 51-21-00 REV 67. REWORK WITHIN LIMITS PER SRM 53- 00-52/101 REV 75. 2 L 7 2 4F RT A1NM 2008022000123 20080220 00123 NM 2008 2 20 HALA0800142 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1030-1046 GOUGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SECTION 45 SEAT TRACK CROWN GOUGED AT LBL 54.75, BS 1030-1046. REMOVED DAMAGE PER SRM 51-10-02, REV 75. REWORK WITHIN LIMITS PER SRM 53-00-52/101, REV 75. ALODINED PER SRM 51-20-01 REV 75. PRIMED PER AMM 51-21-00, REV 67. 2 L 7 2 4F RT A1NM 2008022000152 20080220 00152 SO 2008 2 20 C2XAO8SH026 1 20080219 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11544 145557 SHV - DURING C-CHECK LOWER CUTOUT BETWEEN FR 65-68 STR 16L HAS CORROSION. MX REMOVED AND REPLACED LOWER CUTOUT BETWEEN FRM 65-68 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008022000156 20080220 00156 SO 2008 2 20 C2XASH08030 1 20080219 A 5330 14533826001 DOUBLER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11544 145557 SHV - DURING C-CHECK SKIN DOUBLER AROUND HEATED WATER NIPPLES FR 57-58 HAS CORROSION. MX REPAIRED SKIN DOUBLER AROUND H EATED WATER NIPPLES AT FR 57-58 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008022000206 20080220 00206 SO 2008 2 20 SIMA200805006 1 20080210 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSLEAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 678AE 9450 5000 14500813 DURING IMBV, THE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. PERFORMED CUT OUT OF CORROSION, USED PART NUMBER EPNEM53EP54701 FOR A DOUBLER, USED PART NUMBER EPNEM53EP54703 FOR A FILLER AND AL2024T3 FOR SHIMS. DONE IAW SRM (SRM E MB145/1142 REV 39) CHAPTER 53-00-10 FIG 202 SHEET 2. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022000217 20080220 00217 NM 2008 2 20 HALA0800038 1 20080114 A 5753 STRUCTURE BOEING 767 7673G5 1385126 NM TE FLAP CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 2 CORROSION, LT WING INBD T/E AFT FLAP HAS LOOSE SEALANT AND EXFOLIATION CORROSION, ASSESS PER SRM 57-53-02. ACCO MPLISHED CORROSION REPAIR PER AIR NEW ZEALAND TECHNICAL INSTRUCTION 190111707-0001 AND HAL M105 586069. 2 L 7 2 4F RT A1NM 2008022000218 20080220 00218 NM 2008 2 20 HALA0800039 1 20080114 A 5753 STRUCTURE BOEING 767 7673G5 1385126 NM TE FLAP CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 2 CORROSION, RT WING INBD T/E AFT FLAP HAS LOOSE SEALANT, BULGING OF LWR SKIN AND EXFOLIATION CORROSION ADJACENT T O OUTER HINGE POINT, ASSESS PER SRM 57-53-02. ACCOMPLISHED CORROSION REPAIR PER AIR NEW ZEALAND TECHNICAL INSTRUCTION 1 9011691-0001 AND HAL M105 586070. 2 L 7 2 4F RT A1NM 2008022000225 20080220 00225 NM 2008 2 20 HALA0800117 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 827-830 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45,SEAT TRACK AT LBL 11 HAS LIGHT CORROSION IN TRACK AT STA 872-830. CORROSION REMOVED, CONFI RMED BY 10X MAGNIFICATION IAW SRM 51-10-02, REV 75, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101, REV 75. 2 L 7 2 4F RT A1NM 2008022000231 20080220 00231 NM 2008 2 20 HALA0800083 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 818 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION ON SEAT TRACK AT BS 818. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 51-10-02 REV 76, B LENDED WITHIN LIMITS IAW SRM 53-00-52/101 REV 76. 2 L 7 2 4F RT A1NM 2008022000232 20080220 00232 SO 2008 2 20 C2XA08TY027 1 20080205 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15986 145254 TYS - DURING ROUTINE MX THE EMERGENCY LIGHTS AT ROW 7 AND 12 INOP. MX REMOVED AND REPLACED LIGHT BULBS IAW EMB 145 AMM 33-50-08, OPS CHECK GOOD. A/C WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022000239 20080220 00239 SO 2008 2 20 C2XA08IA048 1 20080130 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 14116 145672 IAH - FLT 2593, THE CREW REPORTED STRONG FUEL SMELL AFTER T/O APU POWERING, PACKS SMELL GOES AWAY AFTER SWITCHING PACKS TO ENG BLEED. A/C RELEASED IAW MEL 49-00-00 CAT "C" CONT #138323, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. IN EWR ON 01/31/08, MAINTENANCE OPERATIONALLY CHECKED THE PACKS USING THE APU WITH NO DEFECTS NOTED. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008022000240 20080220 00240 EU 2008 2 20 SIMA200804403 1 20080211 A 3230 HP848430621 VALVE SAAB SF340 340B 7860101 EU MLG WORN A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 238AE 340B238 ON FLIGHT 3220 CREW REPORTED AFTER TAKEOFF LANDING GEAR SELECTED UP IN TRANSIT LIGHT CAME ON ALL THREE GREENS STAYED ON COMPLIED WITH AOM PROCEDURES DID NOT HAVE THE FUEL TO CONTINUE TO DFW RETURNED TO TYR. AIRCRAFT REMOVED FROM SERVICE. ISSUED MEL, REMOVED AND REPLACED LANDING GEAR EXTENSION/RETRACTION CONTROL VALVE IAW AMM 32-31-15. OPERATIONAL CHECK GO OD. NO DEFECTS NOTED, MEL RESTORED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2008022000246 20080220 00246 NM 2008 2 20 HALA0800092 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1007 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION AT SEAT TRACKS, BS 1007. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 51-10-02 REV.76, B LENDED WITHIN LIMITS, IAW SRM 53-00-52/101, REV.76 2 L 7 2 4F RT A1NM 2008022000248 20080220 00248 NM 2008 2 20 HALA0800093 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION ON SEAT TRACKS AT RBL 88.5. CORROSION REMOVED, CONFIRMED BY 1-X MAGNIFICATION IAW SRM 51-10-02, REV 7 6, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101 REV 76. 2 L 7 2 4F RT A1NM 2008022000253 20080220 00253 WP 2008 2 20 NWAA080459858 1 20080127 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 767NC 47724 DURING A LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD F AILED. MAINTENANCE REPLACED BATTERY PACK AA AND ASSOCIATED FUSE. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008022000255 20080220 00255 NM 2008 2 20 HALA0800127 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 756 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 43, SEAT TRACK AT RBL 88.5, STA 756. CORROSION BLENDED OUT WITHIN SRM LIMITS, SRM 51-10-02. 2 L 7 2 4F RT A1NM 2008022000259 20080220 00259 NM 2008 2 20 HALA0800114 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1011 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45, SEAT TRACK AT LBL 11, HAS DAMAGE TO SEAT TRACK CROWN AT STA 1011. CORROSION REMOVED, CONF IRMED BY 10X MAGNIFICATION IAW SRM 51-10-02, REV 76,BLENDED WITHIN LIMITS, IAW SRM 53-00-52/101, REV.75. 2 L 7 2 4F RT A1NM 2008022000261 20080220 00261 SO 2008 2 20 C2XA08IA050 1 20080204 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 14116 145672 IAH - FLIGHT 2428, THE CREW REPORTED STRONG FUEL SMELL ON TAKEOFF WITH APU POWERING PACKS. MAINTENANCE OPERATIONALLY CH ECKED THE PACKS WITH APU BLEED AIR WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008022000267 20080220 00267 NM 2008 2 20 HALA0800143 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1065-1080 GOUGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SECTION 45 SEAT TRACK CROWN GOUGED AT LBL 54.75, BS 1065-1080. REMOVED DAMAGE PER SRM 51-10-02, REV 75. REWORK WITHIN LIMITS PER SRM 53-00-52/101 REV 75. ALODINED PER SRM 51-20-01, REV 75. PRIMED PER AMM 51-21-00, REV 67. 2 L 7 2 4F RT A1NM 2008022000273 20080220 00273 NM 2008 2 20 HALA0800135 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 870 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SECTION 45 SEAT TRACK CROWN DAMAGED AT LBL 54.75, STA.870. REWORK IAW SRM 51-10-02 REV 76 WITHIN LIMITS PER SRM 53-00-5 2 REV 76. ALODINE PER SRM 51-20-01 REV 76. PRIME PER AMM 51-21-00, REV 67. 2 L 7 2 4F RT A1NM 2008022000276 20080220 00276 NM 2008 2 20 HALA0800153 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1339 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 2 CORROSION SECTION 46, SEAT TRACKS AT RBL 11, STA 1339. REWORKED IAW SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022000289 20080220 00289 SO 2008 2 20 C2XA08RI017 1 20080211 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG INTERMITTENT A C2XA K NONE N FALSE WARNING TO TAKEOFF 1 SW 27 12567 145623 FLIGHT 2761 - EWR - CREW REPORTED THAT AFTER ROTATION, LDG/AIR GRD FAIL MESSAGE AND REV DISAGREE MESSAGE APPEARED ON EIC AS. MESSAGES CLEARED UPON GEAR EXTENSION NEAR EWR. EWR MX REMOVED AND REPLACED NLG AIR/GRD PROXIMITY SWITCH AND PERFOR MED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022000291 20080220 00291 SO 2008 2 20 C2XA08SH021 1 20080213 A 5751 14569009410SD BUSHING EMB 145 EMB145LR 3260212 SO RT AILERON MIGRATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11544 145557 SHV - DURING C-CHECK RT WING AILERON ATTACHMENT BRACKET TO PCA HAS MIGRATING HAT BUSHING. MX REMOVED AND REPLACED RT WI NG AILERON ATTACHMENT BRACKET IAW EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008022000293 20080220 00293 SO 2008 2 20 C2XA08IA058 1 20080206 A 3411 CS500060D4A RELAY EMB 145 EMB145LR 3260212 SO PITOT/STATIC SYS INOPERATIVE A C2XA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SW 27 14902 145496 MCI - FLIGHT 2212, THE CREW REPORTED A PITOT2 INOP MESSAGE APPEARED DURING APPROACH WITH A BURNING SMELL. THE AIRCRAFT LANDED AT MCI WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE CURRENT SENSING RELAY FOR PITOT TWO, OPERATION ALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022000295 20080220 00295 NM 2008 2 20 MWEA080029 1 20080213 A 2620 B-NUT BOEING 717 717200 1383700 NM FIRE SUPPRESSION DISCONNECTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 928ME 55194 LEFT ENGINE FIRE SUPPRESSION LINE AFT "B" NUT DISCONNECTED. RECONNECTED "B" NUT. SURPRESSION 2 L 7 2 4F TR A6WE 2008022000304 20080220 00304 NM 2008 2 20 HNAA080054 1 20080128 A 7712 SEL0C2N INDICATOR DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A HNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 07 935HA 142 ON TAKEOFF ROLL NR 2 ENG TQ IND WENT TO ZERO, SPEED LESS THAN 40KTS, CYCLED CB'S J5 & K5, ENG GROUND RUN GOOD, INDICATIO N NORMAL. REPLACED TQ IND, INSPECTED & CLEANED ELECTRICAL CONNECTORS ON NR 2 ENG, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2008022000305 20080220 00305 EU 2008 2 20 YENA2008006 1 20080114 A 2730 31075440 PCU AIRBUS 320 A320232 3930326 EU ELEVATOR OUT OF LIMITS A YENA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 15 558JB 27924 9624 1915 FLT 562, FLL-SWF, AIR RETURN TO FLL, AIRFRAME VIBRATION AT 300-320 KIAS CLIMBING THROUGH FL230. VIBRATION FADED AS AIRC RAFT SLOWED BELOW 230 KTS. ENG AND FLIGHT CONTROLS INDICATED NORMAL. PERFORMED TSM TASK 05-50-00-810-801. PER CREW IN PUT VIBRATION REPORTING SHEET DECISION TABLE FOLLOWING TASK PERFORMED. PERFORMED ELEVATOR PCU CHECK PER MM 27-34-00-200 -001, MEASUREMENTS. LT INBD-5.5MM, LT OTBD 6MM, RT INBD, 2MM, RT OTBD 4MM. PERFORMED RUDDER PCU CHECK PER AMM 27-24-00 -200-001, BLUE- 6MM, YELLOW- 6.5MM, GREEN 7MM, REPLACED LT OTBD BLUE SYSTEM ELEVATOR PCU 34CE3 DUE ROD END OUT OF LIMITS PER AMM 27-34-51-04, OPS AND LEAK CHECK OK. 2 L 7 2 4F RT A28NM 2008022000306 20080220 00306 EU 2008 2 20 YENA2008017 1 20080211 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 15 570JB 2099 FLT 383, LGA-FLL, APPROXIMATELY 3 MINUTES PRIOR TO LANDING NR 1 F/A CALLED TO REPORT "BURNING SMELL" IN CABIN. NR 1 F/A TURNED OFF TV'S AND DID NOT SMELL IT AGAIN. BOTH PILOTS COULD SMELL THE SAME THING IN THE COCKPIT. ACCOMPLISHED AND P ERFORMED CHECK AS PER TSM 23-39-00-810-801, ALL OPS CHECK OK, SYSTEM WORKING NORMAL. 2 L 7 2 4F RT A28NM 2008022000311 20080220 00311 NM 2008 2 20 MWEA080030 1 20080214 A 7830 7150922REVC FRAME BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 920ME 55182 RIGHT ENGINE THRUST REVERSER UPPER DEFLECTOR DOOR ZEE FRAME HAS TWO CRACKS AT THE RIGHT SIDE 1 EACH IN THE RADIUS AT THE END AND 1 EACH BETWEEN 2 FASTENERS, ALSO EXTENDING FROM 1 OF THE RIVETS LOCATED APPROXIMATLEY 4 INCHES INBOARD 26.666. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2008022000315 20080220 00315 WP 2008 2 20 MWEA080032 1 20080215 A 3350 100865 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 814ME 48010 UPPER EMERGENCY LIGHTS INOPERATIVE AT AFT GALLEY. REMOVED AND REPLACED BATTERY. 2 L 7 2 4F A6WE 2008022000317 20080220 00317 SO 2008 2 20 C2XA08ON073 1 20080121 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN SMOKE A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 11181 1450904 FLT 7676 - SLC TO SLC - FLIGHT CREW REPORTED SMOKE IN THE CABIN AFTER T/O AND OVER WEIGHT LANDING. CONTRACT MX INSPECTE D AIRCRAFT, RAN ENGINES, APU, BLEED SYSTEM AND COULD NOT DUPLICATE; HARD LANDING WAS FOUND WITHIN LIMITS. AIRCRAFT RETU RNED TO THE GATE TO REMOVED ICE FROM ENGINE, OPERATIONALLY CHECKED ALL SYSTEM SATISFACTORY. AIRCRAFT WAS RELEASED TO RE TURN FOR SERVICE. 2 L 7 2 4F RT 2008021900298 20080219 00298 EA 2008 2 19 CHQA200800027 1 20080209 A 3097 CONTACTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE WINDSHIELD HEAT LOOSE A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 653BR 7438 GEE872823 IAH TO HRL - DURING CRUISE, THE CREW NOTICED SPARKS AND SMOKE FROM AROUND THE LOWER RIGHT CORNER OF THE FO'S WINDSHIELD. THE CREW RAN THE MEMORY ITEMS FOR COCKPIT SMOKE, TURNED OFF THE WINDSHIELD HEAT, AND PULLED THE CIRCUIT BREAKER FOR TH E RIGHT WINDSHIELD HEATING ELEMENT. THE FLIGHT LANDED IN CRP WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND LOOSE L UGS ON THE HEAT CONTACTOR FOR THE FO'S WINDSHIELD. AFTER CLEANING AND RESECURING THE TERMINALS, THE WINDSHIELD HEAT SYS TEM OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2008021900322 20080219 00322 NM 2008 2 19 HALA0800046 1 20080110 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 386 S2L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LIGHTING STRIKE ON A/C CROWN AT LOCATION, STA 386 BELOW S2L. REPAIRED IAW 767-300 SRM 53-00-01, REPAIR 8. 2 L 7 2 4F RT A1NM 2008021900340 20080219 00340 NM 2008 2 19 SWAA080763 1 20080207 A 5330 6550570 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008021900349 20080219 00349 NM 2008 2 19 SWAA080789 1 20080211 A 3397 65C27093 CONNECTOR BOEING 737 737317 138447P NM CABIN DIRTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INTERMITTENT. FOUND LIGHT ASSY CONNECTOR DIRTY. CLEANED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2008022000091 20080220 00091 SO 2008 2 20 C2XA08SH024 1 20080214 A 5512 14532235402 SKIN EMB 135 EMB135LR 3260305 SO HORIZ STAB CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28529 145512 SHV - DURING C-CHECK RT HORIZONTAL STAB L/E HAS CORROSION ON SKINS AROUND RIVETS AND SCREW HEADS. MX REPAIRED RT HORIZO NTAL STAB L/E ON SKINS AROUND RIVETS AND SCREW HEADS IAW EC5510-01178. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2008022000108 20080220 00108 NM 2008 2 20 HALA0800144 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1180 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 2 CORROSION SEAT TRACK SECTION 46, RBL 11, STA 1180. REWORKED IAW SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022000129 20080220 00129 WP 2008 2 20 ARWA20080203 1 20080213 A 7722 8DJ175LXP2 INDICATOR DOUG DC10 DC1030 3023501 WP EGT MALFUNCTIONED A ARWA D E RETURN TO BLOCK ENGINE SHUTDOWN N FALSE WARNING TX TAXI/GRND HDL 1 SO 19 524MD 46999 NR 2 ENGINE NO EGT INDICATOR FOUND ON POINTER OR DIGITAL READ OUT ON ENGINE START, ALL OTHER PARAMETERS NORMAL START. S HUTDOWN ENGINE. REMOVED AND REPLACED EGT INDICATOR CHECKED GOOD IN ACCORDANCE WITH M/M 77-20-00 AND M/M 71-00-00. 2 L 7 3 4F A22WE 2008022000139 20080220 00139 NM 2008 2 20 SWAA080843 1 20080213 A 5311 6558280 FRAME BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 19R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008022000140 20080220 00140 NM 2008 2 20 SWAA080844 1 20080213 A 5311 65C22908 FRAME BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008022000157 20080220 00157 SO 2008 2 20 C2XA08SH031 1 20080219 A 5320 14529150001 ATTACH ANGLE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11544 145557 SHV DURING C-CHECK FR 23 CROSSBEAM LOWER ATTACHMENT ANGLE HAS VARIOUS AREAS OF CORROSION, MX REMOVED AND REPLACED LOWER ATTACHMENT ANGLE AT FR 23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008021400049 20080214 00049 EA 2008 2 14 TRAX200800203 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 693-830 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 LT FLOOR SEAT RAIL FS 693.0 TO FS 830.40 AT LBL 9.0 HAS CORROSION DAMAGE ON RAIL AND HARDWARE. 2 L 7 2 4F RT A21EA 2008021400057 20080214 00057 EA 2008 2 14 TRAX200800218 1 20080206 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 EMERGENCY LIGHT IN CABIN INOP, SECOND LIGHT FROM FRONT. 2 L 7 2 4F RT A21EA 2008021400058 20080214 00058 SW 2008 2 14 WGEA200800021 1 20080205 A 2133 5411001 OUTFLOW VALVE ECLIPS EA500 ECLIPSEEA500 3350000 SW ZONE 100 DEFECTIVE E WGEA K NONE O OTHER CR CRUISE 1 EA 27 139DJ 91 000054 PRESSURIZATION OVER PRESSURIZING AT 18,000 FEET. CABIN ALTITUDE READS +250 FEET AND 8.4 DIFFERENTIAL. ON DECK WITH DOO R OPEN CABIN PRESSURE READS 600 FEET. REFERENCE DAYJET WORK ORDER 1299, NRI 2. REMOVED AND REPLACED PRIMARY OUTFLOW VA LVE IAW EA500 AMM 21-30-12. PERFORMED CPCS OUTFLOW VALVE ADJUSTMENT/TEST IAW EA500 AMM 21-30-01. OPS CHECK GOOD. PERF ORMED PRIMARY AND SECONDARY OUTFLOW VALVE DELTA-P LIMITER TEST IAW EA500 AMM 21-30-03. OPS CHECK GOOD. 1 L 7 2 4J RT A00002AC 2008021400065 20080214 00065 NM 2008 2 14 ZZDA2008067 1 20080207 A 5330 SKIN BOEING 717 717200 1383700 NM FS 215-244 GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 603AT 55127 GOUGES IN FUSELAGE SKIN FS 215-244 LONGERON 16L. BLENDED DAMAGE, FABRICATED AND INSTALLED INTERNAL DOUBLER IAW B717 SRM 53-00-01 REPAIR 2. 2 L 7 2 4F TR A6WE 2008021400071 20080214 00071 2008 2 14 UPS08851653 4 20080211 A 2565 BRACKET DOUG DC8 DC871F 302199D WP ESCAPE SLIDE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 EVAC SLIDE PSI AND EXPIRATION ILLEGIBLE FROM INSPECTION WINDOW. EVAC SLIDE COVER LATCH BRACKET IS BROKEN. SLIDE COVER REMOVED AND ROUTED FOR REPAIR INSTALLED LATCH AS REQUIRED PER SRM 51-01-21A. REINSTALLED SLIDE INSIDE COVER AND ON TO A IRCRAFT, REF MM 25-60-01-2. 2 L 7 4 4F RT 4A25 2008021400073 20080214 00073 WP 2008 2 14 UPS08851655 1 20080207 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 FOUND EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2008021400077 20080214 00077 EU 2008 2 14 08FDEA00272 1 20080122 A 5315 A5397422122451 FLOORBEAM AIRBUS 310 A310222 3930315 EU BS 3514 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 447FE 251 N00529 LOWER FUSELAGE, PREVIOUS REPAIR FOUND LOCATED ON AFT CARGO FLOORBEAM OF FR 65, Y-950. REPAIR REQUIRES EVALUAT ION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NO T TO CONFORM TO AN SRM REPAIR. NEW BEAM P/N A5397422122451. INSTALLED IN ACCORDANCE WITH SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008021400078 20080214 00078 NM 2008 2 14 08FDEA00376 1 20080210 A 5347 ACA7104521 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 MAIN DECK, AFTER FLOOR PANEL REMOVAL FOR WIRING MOD, FOUND SEAT TRACK UNDER FLOOR PANEL AT STA 635, X = 55 CRACKED. SE AT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR P ER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008021400079 20080214 00079 EU 2008 2 14 08FDEA00377 1 20080211 A 7830 2210501531 SKIN AIRBUS 310 A310221 3930310 EU ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 NR 1 ENGINE INBOARD THRUST REVERSER INTERIOR SKIN CHAFED JUST BELOW DEOILER EXHAUST PORT, NAC STATION 385 ,4:00 POSITION . REPAIRED PER EA NR 6-7800-113019 , EXHAUST, NR 1 ENGINE INBOARD T/R AFT BARREL SKIN DOUBLER, REPAIR. 2 L 7 2 4F RT A35EU 2008021400080 20080214 00080 EU 2008 2 14 08FDEA00380 1 20080211 A 5320 A53832100208 WEB AIRBUS 330 A300* EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CRACKS AT C 47 IN WEBS BETWEEN TRACK 1-2 LT/RT. CRACK LENGTH TRACK 1-2 LH: 10MM, TRACK 1-2 RT: 13MM REPAIR PERFOR MED BY CRACK STOP HOLE AND INSTALLING AN EXTERNAL DOUBLER IAW RAS/AS/003/2008 ISS A, APPROVED BY EA 6-5315-114876. 2 L 7 2 4F RT A26NM 2008021400081 20080214 00081 EU 2008 2 14 08FDEA00381 1 20080211 A 5320 A53832103206 WEB AIRBUS 330 A300* EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CRACKS AT C 47 IN WEBS BETWEEN TRACK 3-4 LT/RT. CRACK LENGTH TRACK 3-4 LT: 6 MM, TRACK 3-4 RH: 13MM. REPAIR PERF ORMED BY CRACK STOP HOLE AND INSTALLING AN EXTERNAL DOUBLER IAW RAS/AS/003/2008 ISS A, APPROVED BY EA 6-5315-114876. 2 L 7 2 4F RT A26NM 2008021400083 20080214 00083 EU 2008 2 14 08FDEA00383 1 20080211 A 5320 A53612214200 FLOOR SUPPORT AIRBUS 330 A300* EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION FOUND ON FLOOR STRUCTURE C 11-14, Y730. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A26NM 2008021400088 20080214 00088 EA 2008 2 14 TRAX200800220 1 20080122 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 916EV 7757 ASD EXTERNAL HANDLE FLAPPER DOOR CRACKED. 2 L 7 2 4F RT A21EA 2008021400089 20080214 00089 EA 2008 2 14 TRAX200800221 1 20080122 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 916EV 7757 ASD EXTERNAL HANDLE CRACKED. 2 L 7 2 4F RT A21EA 2008021400092 20080214 00092 WP 2008 2 14 NWAA080419926 1 20080207 A 2497 TERMINAL DOUG DC9 DC932 3022066 WP TRANSFORM REC BURNED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 01 926NW 47425 DURING THE DESCENT THROUGH 10,000 FEET INTO MSP, THE CAPTAIN NOTICED FUMES LIKE BURNED INSULATION IN THE COCKPIT. FUMES WENT AWAY SLIGHTLY AND THEN WERE STRONGER AGAIN AROUND 6000 FT. 1ST OFFICER CONFIRMED HE DETECTED IT ALSO. CAPTAIN DO NNED O2 MASK FOR REMAINDER OF APPROACH. AFTER AN UNEVENTFUL LANDING WHEN O2 MASK WAS REMOVED, THE ODOR WAS MUCH MORE NO TICEABLE. ALL ELECTRICAL INDICATORS IN USE WERE SHOWING NORMAL AND THERE WAS NO OTHER ODORS, SMOKE, OR ABNORMAL NOISE. MX TROUBLESHOT AND FOUND THE NR 2 TRANSFORMER RECTIFIER OVERHEATING. ALSO, FOUND A 50 AMP CIRCUIT BREAKER AND WIRE/TER MINAL (09-2493-3-1790) BEHIND THE CAPTAINS' SEAT BURNED. AFFECTED PARTS WERE REPLACED, FUNCTIONAL CHECKS WERE GOOD, PAC 2 L 7 2 4F A6WE 2008021400094 20080214 00094 NM 2008 2 14 QXEA200800065 1 20080114 A 5320 SUPPORT ANGLE DHAV DHC8 DHC8202 2809007 NM THRESHOLD CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C CHECK - SUPPORT ANGLE AT APPROX STA X569.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURFA CE. MAINTENANCE REMOVED NUTPLATES AND REMOVED CORROSION, INSPECTED BLEND, WITHIN LIMITS NO CRACKS NOTED. ALODINED, PRI MED AND PAINTED. INSTALLED NUTPLATES. 2 H 7 2 4T RT A13NM 2008022000164 20080220 00164 NM 2008 2 20 NWAA080503168 1 20080213 A 2120 1303A000003 VALVE AIRBUS A319 A319114 3930350 NM FLOW CONTROL MALFUNCTIONED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 368NB 12048 4362 2039 AFTER DEPARTURE IN CLIMB, NOTICED STRONG ODOR LIKE ELECTRICAL WIRES HEATING UP, AFT CABIN F/A ALSO DETECTED SAME THING, F/A SAYS IT WAS VERY STRONG ELECTRICAL ODOR. AIRCRAFT RETURNED TO MSP LANDING UNEVENTFULLY, PASSENGERS THROUGHOUT CABIN DETECTED SIMILAR ODOR. REPLACED SEALS AND GROUND STRAP ADJACENT TO NR 1 PACK FLOW CONTROL VALVE. REPLACED NR 1 PACK F LOW CONTROL VALVE. REPLACED SLEEVE, ELBOW AND SEALS ADJACENT TO HEAT EXCHANGER. REPLACED L/R OZONE CONVERTERS. REPLAC ED RECIRCULATION FILTERS. CHECKS OK. 2 L 7 2 4F RT A28NM 2008022000226 20080220 00226 NM 2008 2 20 HALA0800082 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 805 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION ON SEAT TRACKS AT BS 805. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION, IAW SRM 51-10-02, REV 76 , BLENDED WITHIN LIMITS IAW SRM 53-00-52/101, REV 76. 2 L 7 2 4F RT A1NM 2008022000241 20080220 00241 NE 2008 2 20 SIMA200804402 2 20080211 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE NR 2 ENGINE FLAMED OUT A SIMA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 SW 21 307AE 340B307 ON FLIGHT 3230 CREW REPORTED ON FINAL APPROACH INTO DFW FOLLOWING THE APPROACH CHECKLIST THEY SELECTED AUTO COARSEN ON. AS THE SWITCH WAS SELECTED ON THE N 2 ENGINE FLAMED OUT WITH NO RELIGHT. CREW FOLLOWED AOM PROCEDURES AND DECLARED AN EMERGENCY. AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. 2 L 7 2 4T 4 T RT A52EU E8NE 2008022000244 20080220 00244 NM 2008 2 20 HALA0800090 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 967 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION ON SEAT TRACKS AT BS 967. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION, IAW SRM 51-10-02, REV 76 , BLENDED WITHIN LIMITS, IAW SRM 53-00-02/101 REV.76 2 L 7 2 4F RT A1NM 2008022000262 20080220 00262 NM 2008 2 20 HALA0800122 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1012 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 2 CORROSION SECTION 45, SEAT TRACK AT LBL 88.5, STA 1012. SEAT TRACK REPLACED. 2 L 7 2 4F RT A1NM 2008022100074 20080221 00074 NM 2008 2 21 08FDEA00470 1 20080217 A 5347 53FX139821 SEAT TRACK BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 MAIN CABIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION FROM STA 870 TO STA 890, BL 0. REMOVED SEAT TRACK WITH OUT OF LI MIT COROSION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK IAW SRM (ER 01-049) 53-10-5 AND 53-10-2 FIG7. LOCATED AND DRLLE D NEW SEAT TRACK IAW SRM 51-30-5. TREATED AND PRIMED SEAT TRACK IAW SRM 51-10-2. INSTALLED NEW SEAT TRACK IAW ER 01-049 AND SRM 53-10-5 AND 53-102 FIG7. 2 L 7 3 4F RT A3WE 2008022100075 20080221 00075 NM 2008 2 21 08FDEA00471 1 20080217 A 5347 BAC1520792 SEAT TRACK BOEING 727 727233 138408A NM BS 950-950E CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 MAIN CABIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION FROM STA 950 TO STA 950E, BL 0. REMOVED DAMAGED SEAT TRACK SECTI ON IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION IAW SRM ER 01-049, SRM 53-10-5 FIG 7A. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED SEAT TRACK SECTION IAW SRM ER 01-049. 2 L 7 3 4F RT A3WE 2008022100079 20080221 00079 EU 2008 2 21 08FDEA00492 1 20080121 A 5350 A5398862420000 STRUT AIRBUS 310 A310222 3930315 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 TAIL CONE, SMALL SPOTS OF CORROSION AT LT AFT TRACK ATTACHMENT FITTING AT FRAME 87. STRUT-CROSS WAS REPLACED IN ACCORDA NCE WITH SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2008022100081 20080221 00081 WP 2008 2 21 08FDEA00494 1 20080218 A 5347 AEA7325503 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MAIN CABIN SEAT TRACK SCALLOPS ARE GOUGED FROM STA 1461 TO 1521 BL 48L. REMOVED AND REPLACED DAMAGED SEAT TRACK IAW FED EX DWG NR NEA 6022 REV AM. INSTALLED SPLICE HAT AND 2 SPLICE PLATES IAW MD-10 / DC-10 SRM 53-70-00, VOL I. ALODINED/PR IMED AND TOP COAT IAW MD-10/DC-10 SRM 51-21-02, VOL II. 2 L 7 3 4F RT A22WE 2008022100083 20080221 00083 WP 2008 2 21 08FDEA00497 1 20080218 A 5230 ANB73283587 RETAINER DOUG DC10 DC1030F 3023504 WP ZONE 100 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 CTR CARGO DOOR FWD LOWER L/E SEAL RETAINER IS BROKEN (INTERIOR). REMOVED AND INSTALLED RETAINER IAW DC-10 SRM 51-35-01, VOL II. MAT ID .032 7075-T6 PO NR 547197.3 AND FABBED IAW DAC DWG ANB 7328. ALODINE AND PRIME IAW DC-10 SRM 51-21-01, VOL II. PART MARKED IAW FEDEX GMM 7-0-1001. 2 L 7 3 4F RT A22WE 2008022100088 20080221 00088 EU 2008 2 21 08FDEA00502 1 20080218 A 5321 B5327060401300 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 MAIN CABIN FLOOR BOARD 242UJ IS CRACKED. FABRICATED NEW FLOOR BOARD PNL NR 242UJ IAW FEDEX DWG SRZ 25-005 REV F. FOR I NSTALLATION SEE W/C 62C0702. 2 L 7 2 4F RT A35EU 2008022100093 20080221 00093 WP 2008 2 21 08FDEA00448 1 20080215 A 5310 AFA00395 BEAM DOUG DC10 DC1030F 3023504 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 FWD CARGO COMPT PERFORMED REWORKING IAW EO 8-2550-7-2354 P1 ON BEAM FOUND CRACK. REPAIRED BEAM IAW SRM 53-60-01 FIG 3 V OL I. 2 L 7 3 4F RT A22WE 2008022100097 20080221 00097 WP 2008 2 21 08FDEA00453 1 20080215 A 5321 ACA3205559 FLOOR PANEL DOUG DC10 DC1030F 3023504 WP BS 555 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 CABIN FLOOR PANEL AT STA 555 RBL 8.5 TO 27.5 HAS EDGE DAMAGE AND HOLES. FABRICATED NEW FLOOR PANEL STA 555, POTTED ED GES, COMPETED CURE AND SANDED EDGE POTTING, INSTALLED INSERTS AND APPLIED ANTI-SKID IAW FEDEX DWG SRZ 25-005 REV F. THIS IS A MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008022100099 20080221 00099 EU 2008 2 21 08FDEA00416 1 20080213 A 5230 A5237402220400 BUSHING AIRBUS 300 A300F4605R 3930327 EU CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 AFT CARGO DOOR NR 6 ECCENTRIC BUSHING SUPPORT INNER BORE IS CORRODED. REMOVED AND REPLACED AFT CARGO DOOR NR 6 ECCENTRI C BUSHING REF FEDEX ROUTINE CARD 61X5030ALI AND A300-600 AMM 52-32-11-5. T/W TWS8330A. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008022100100 20080221 00100 NM 2008 2 21 08FDEA00417 1 20080213 A 5315 BAC15061108 FLOORBEAM BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 MAIN CABIN, FLOORBEAM UPPER SURFACE HAS CORROSION AT STA 846, LBL 48. REMOVED SEAT TRACK AND REMOVED SUPPORT TEE IAW SR M 51-30-2. FABRICATED, LOCATED AND DRILLED NEW TEE BEAM IAW SRM 53-10-2 FIG7 AND 51-30-5.TREATED AND PRIMED AFFECTED ARE A IAW SRM 51-10-2. INSTALLED IAW SRM 51-30-2 AND 53-10-2 FIG7. 2 L 7 3 4F RT A3WE 2008022100102 20080221 00102 EU 2008 2 21 08FDEA00419 1 20080213 A 5230 A5237408120400 BUSHING AIRBUS 300 A300F4605R 3930327 EU CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 AFT CARGO DOOR NR 5 ECCENTRIC BUSHING SUPPORT INNER BORE IS CORRECTED. REMOVED AND REPLACED AFT CARGO DOOR NR 5 ECCENTR IC BUSHING REF FEDEX ROUTINE CARD 61X5030ALI AND A300-600 AMM 52-32-11-5. T/W TWS8330A. 2 L 7 2 4F RT A35EU 2008022100105 20080221 00105 NM 2008 2 21 08FDEA00461 1 20080216 A 5311 AFA00203 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 MAIN DECK, FRAME DOUBLER AT RIGHT STA 1701 LONGERON 12 FOUND WITH DENT. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES AS PER S RM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008022100111 20080221 00111 NM 2008 2 21 08FDEA00469 1 20080217 A 5347 53FX139820 SEAT TRACK BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 MAIN CABIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION FROM STA 1070 TO STA 1130, BL 0. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED SEAT TRACK IAW SRM 53-10-5, 53-10-2 FIG 7A (ER 01-049) LOCATED AND DRILL NEW SEAT TRACK IAW SRM 51-30-5. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED SEAT TRACK SECTION IAW ER 01-049 SRM 53-10-5 AND 53-10-2 FIG 7. 2 L 7 3 4F RT A3WE 2008022100118 20080221 00118 NM 2008 2 21 08FDEA00512 1 20080219 A 5420 651950839 STIFFENER BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE NR 1 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 NR 1 ENG UPPER COWL STIFFENER CRACKED BETWEEN 2ND AN 3RD LOWER LATCH CUTOUTS. REMOVED SEAL AND SEAL RETAINER, REMOVED C RACKED COWL STIFFENER, VERIFIED MATERIAL ID. FABRICATED NEW COWL STIFFENER, TREATED AND PRIMED, INSTALLED NEW COWL STIF FENER. REINSTALLED RETAINER AND SEAL, AND WROTE PART NUMBER ON NEW COWL STIFFENER. REF DWG 65-19508-39, REF SRM 51-30- 2 PG 1, REF SRM 51-20-1 PG 13 FIG 2, REF SRM 51-30-2 PG 7, REF GMM 7-0-1001 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F 4 F A3WE E2EA 2008022100126 20080221 00126 NM 2008 2 21 HALA0800155 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1387 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 2 CORROSION, SECTION 46, SEAT TRACKS AT RBL 11, STA 1387. REWORKED IAW SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022100130 20080221 00130 NM 2008 2 21 F3LA200800066 1 20080202 A 5744 D5757420200100 ATTACH FITTING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 5503 2019 DURING C3/S1 C CHECK, INSPECTION REPORTED THE RIGHT, OUTBOARD NUMBER 3 FLAP DRIVE LEVER EXTENSION ARM FITTING WAS FOUND GOUGED WHERE IT CONNECTS TO BOTTOM OF THE DRIVE ARM. MAINTENANCE BLENDED THE DAMAGED AREA IN ACCORDANCE WITH THE REQUIR EMENTS OF A319 SRM 51-73-00. PERFORMED HFEC (EDDY CURRENT) INSPECTION AND FOUND NO DEFECTS. AREA WAS PRIMED AND PAINTE D IN ACCORDANCE WITH EA A9-53R-30009. UPON COMPLETION OF THE REPAIRS, THE UNIT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008022100136 20080221 00136 WP 2008 2 21 08FDEA00455 1 20080215 A 5321 ADA3201509 FLOORBOARD DOUG DC10 DC1030F 3023504 WP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MAIN CABIN FLOORBOARD AT APPROX RBL-90, BETWEEN STA 800 TO 850 IS DELAMINATED. REMOVED FLOORBOARD IAW AMM 53-21-01-2. FABBED FLOORBOARD IAW SRZ-25-005 REV F. LOCATED HOLES FOR INSERTS IAW DWG SRZ 25-005 REV F. POTTED EDGES AND STARTED C URE IAW DWG SRZ 25-005 REV F. CURE COMPLETED, SANDED EDGES IAW DWG SRZ 25-005 REV F. POTTED INSERTS IAW DWG SRZ 25-005 R EV F. INSTALLED ANTI-SKID IAW DWG SRZ 25-005 REV F. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008022100145 20080221 00145 EA 2008 2 21 SWIA200819208 1 20080204 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE ACTIVATION A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 910EV 7727 RECEIVED A SMOKE TOILET MESSAGE AFTER TAKE OFF, FLIGHT NR 3942. INSPECTED AREA AND OPERATIONALLY CHECKED LAVATORY SMOKE DETECTOR. NO DISCREPENCIES NOTED. 2 L 7 2 4F RT A21EA 2008022100149 20080221 00149 NM 2008 2 21 HALA0800158 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1432 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 2 CORROSION SECTION 46, SEAT TRACKS AT RBL 11, STA 1432. REWORKED IAW SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022100151 20080221 00151 NM 2008 2 21 HALA0800160 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1437 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 46, SEAT TRACKS AT RBL 88.5, STA 1437. REWORKED IAW SRM 53-00-52/101, AND REPLACED SEAT TRACK IAW SRM WHERE DAMAGE WAS OUT OF LIMITS. 2 L 7 2 4F RT A1NM 2008022100152 20080221 00152 NM 2008 2 21 HALA0800161 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1433 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 46, SEAT TRACKS AT RBL 46, STA 1433. REWORKED IAW SRM 53-00-52/101. REPLACED SEAT TRACK IAW SRM WHERE OUT OF LIMITS. 2 L 7 2 4F RT A1NM 2008022100153 20080221 00153 NM 2008 2 21 HALA0800162 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1414 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24259 LEVEL 1 CORROSION SECTION 46, SEAT TRACKS, AT RBL 88.5, STA 1414. REWORKED IAW SRM 53-00-52/101 AND REPLACED SEAT TRACK IAW SRM WHERE DAMAGE WAS OUTSIDE LIMITS. 2 L 7 2 4F RT A1NM 2008022100158 20080221 00158 NM 2008 2 21 F3LA200800055 1 20080216 A 2432 350L5100508 LIMITER AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE BATTERY CHARGER INOPERATIVE A F3LA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 928FR 126 2236 DURING TAKEOFF, THE FLIGHT CREW REPORTED AN ELAC BCL2 FAULT ON THE ECAM. THE FLIGHT CREW PERFORMED AN AIR TURN BACK AND AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 BATTERY CHARGE LIMITER IN ACCORD ANCE WITH THE REQUIREMENTS OF AMM 24-38-34-41. FOLLOWING COMPLETION OF THE INSTALLATION, THE UNIT WAS OPERATIONALLY TES TED AND FOUND OKAY. CORRECTED PART SERIAL NUMBER TO READ 2081/END. 2 L 7 2 4F 4 F RT A28NM 2008022100160 20080221 00160 NM 2008 2 21 08FDEA00514 1 20080219 A 5311 53FX1350 FRAME BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 FWD CARGO PIT, FRAME EXTENSION AT BS 600 IS CRACKED IN UPPER RADIUS, ABOVE STR 22L ON FWD SIDE OF FRAME. MARKED END OF CRACK WITH BLACK DOT CIRCLE. GENERATED FROM W/C 53F0020. FABRICATED FRAME EXTENSION REF DWG 53FX1350. HEAT TREATED TO T-6 CONDITION ON 8130 NR 2008-02-083, TREATED AND PRIMED. INSTALLED FRAME EXTENSION. REF SRM 51-30-2/51-10-2. THIS I S CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008022100166 20080221 00166 NM 2008 2 21 08FDEA00425 1 20080214 A 5320 65575703 FLOOR SUPPORT BOEING 727 727227 1384078 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 LT EDGE SUPPORT CHANNEL FLOOR IS CRACKED AT CTR HOLE, STA 1030 TO 1070 FABRICATED NEW EDGE SUPPORT P/N 65-57570-1 AND SP LICE P/N 65-57570-3. TREATED AND PRIMED AND INSTALLED NEW EDGE SUPPORT AND SPLICE. REF BOEING DWG 65-57570/SRM 51-10-1 PG 12/SRM 51-10-2 PG 1/2, SRM 51-30-2 PG 5 AND 6. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008022100168 20080221 00168 NM 2008 2 21 HALA0800168 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1313 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 46, SEAT TRACKS AT RBL 88.5, STA 1313. REWORKED IAW SRM 53-00-52/101 AND REPLACED SEAT TRACKS WHERE OUT OF LIMITS. 2 L 7 2 4F RT A1NM 2008022100171 20080221 00171 NM 2008 2 21 HALA0800171 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1275 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24259 LEVEL 1 CORROSION SECTION 46, SEAT TRACKS AT RBL 88.5, STA 1275. REWORKED IAW SRM 53-00-52/101, AND REPLACED SEAT TRACK S WHERE OUT OF LIMITS. 2 L 7 2 4F RT A1NM 2008022000173 20080220 00173 NM 2008 2 20 HALA0800065 1 20080118 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 891-1098 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SEAT TRACK CORRODED 2 STA 889-1098, LBL 88.5, BEYOND SRM LIMITS. SEAT TRACK REPLACED IAW SRM 53-00-52 FIG 201, REPAIR 3 , BETWEEN STA 891 AND 1098. 2 L 7 2 4F RT A1NM 2008022000190 20080220 00190 SO 2008 2 20 C2XA08ON086 1 20080207 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO LAVATORY MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 14177 8707 8707 14500888 FLT 7681 - LAX TO LAX - FLIGHT CREW REPORTED LAV SMOKE DETECTOR INDICATION IN FLIGHT. FLIGHT CREW DID NOT REPORT EMERGE NCY AND RETURNED TO BLOCK WITHOUT INCIDENT. MX PERSONNEL REMOVED AND REPLACED LAV SMOKE DETECTOR OPERATIONALLY CHECKED SATISFACTORY. A/C WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008022000207 20080220 00207 NM 2008 2 20 PIDA08009 1 20080205 A 5330 SKIN BOEING 737 737291 138448W NM FUSELAGE CANNING A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 583CC 21069 DURING MAINTENANCE, NOTED FUSELAGE SKIN OIL CANNED AT BS 200 APPROX 14 INCHES BELOW STR 19RT. REPAIRED DAMAGE PER SRM 5 3-30-03 FIG 49. 2 L 7 2 4F A16WE 2008022000211 20080220 00211 NM 2008 2 20 MWEA080023 1 20080204 A 5311 7150922507 FRAME BOEING 717 717200 1383700 NM FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 906ME 55170 UPPER BUCKET Z-FRAME LEFT END AT STATION 26.666 IS CRACKED. FABRICATED AND INSTALLED Z-FRAME. 2 L 7 2 4F TR A6WE 2008022000228 20080220 00228 NM 2008 2 20 HALA0800098 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 866-871 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION AT SECTION 45, SEAT TRACK AT RBL 11, AT STA866-871. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 51-10-02, REV 75, BLENDED WITHIN LIMITS, IAW SRM 53-00-02/101, REV 76. 2 L 7 2 4F RT A1NM 2008022000272 20080220 00272 NM 2008 2 20 HALA0800132 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 836 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1, LIGHT SURFACE CORROSION TO TRACK BASE, SECTION 45 SEAT TRACK LBL 54.75 STA.836. REWORKED CORROSION IAW SRM 51- 10-02 REV 76. ALODINE REWORKED AREA IAW SRM 51-20-01 REV 76. PRIMED IAW AMM 51-21-00 REV 67. REWORK WITHIN LIMITS PER SRM 53-00-52/101, REV 75. 2 L 7 2 4F RT A1NM 2008022000284 20080220 00284 SO 2008 2 20 C2XA08IA055 1 20080210 A 2510 12315660401 HOLDER EMB 145 EMB145LR 3260212 SO COCKPIT SHORTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14543 14756 14756 145553 IAH - FLIGHT 2292 - THE CREW REPORTED THAT THE COCKPIT READING LIGHT CIRCUIT BREAKER POPPED ON CLIMBOUT WHEN THE CHART H OLDER WAS OPENED FOLLOWED BY A LITE SMELL OF SMOKE. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT AND MAINTENANCE REMOVED AND REPLACED THE CAPTAINS CHART HOLDER, RESET THE CIRCUIT BREAKER, OPERATIONALLY CHECKED WITH NO DEF ECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022000316 20080220 00316 NM 2008 2 20 BB08004 1 20080119 A 3397 WIRE BOEING 767 767201 1385125 NM CABIN BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 250AY 23902 MAD - MAINTENANCE REPORTED THE FLOOR PATH EMERGENCY LIGHTING AT SEAT 12F INOPERATIVE. MAINTENANCE SPLICED BROKEN WIRE. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A1NM 2008022100095 20080221 00095 WP 2008 2 21 08FDEA00451 1 20080215 A 5730 ARC02634 SKIN DOUG MD10 MD1010F 3022112 WP RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 RIGHT WING UPPER TRAILING EDGE PANEL HAS CORROSION ON THE UPPER SURFACE, APPROXIMATELY XORS 345. REMOVED CORROSION; OUT OF LIMITS IAW 10 SRM 51-21-01, VOL II & 57-31-01 FIG A, VOL III & 57-00-01 FIG A, VOL I. REMOVED PANEL IAW SRM 51-3 3-01, VOL II, 51-35-01, VOL II & 51-31-01, VOL III. REPAIRED PANEL BY REBUILDING PER DWG ARC 0263 REV AA & TPS 1001 R EV E, IAW EA 8-5720-113029. INSTALLED PANEL IAW SRM 51-31-01, VOL II. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008022100124 20080221 00124 NM 2008 2 21 HALA0800152 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1280 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 2 CORROSION SECTION 46, SEAT TRACKS AT RBL 11, STA 1280. REWORKED IAW SRM 53-0052/101. 2 L 7 2 4F RT A1NM 2008022100129 20080221 00129 NM 2008 2 21 08FDEA00466 1 20080216 A 5347 ACA7399501 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 635 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 MAIN DECK COMPARTMENT, AFTER REMOVAL OF DAMAGED LOWER CARGO CEILING PANELS FOUND SEAT TRACK AT STA 635, X = 47.50" CRACK ED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PE R GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008022100131 20080221 00131 NM 2008 2 21 F3LA200800067 1 20080131 A 5320 D5337062220400 HINGE FITTING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 5503 2019 DURING THE C3/S1 C CHECK, INSPECTION REPORTED THE RIGHT, FORWARD, MAIN LANDING GEAR DOOR, KEEL MOUNTED HINGE FITTING, AT THE AFT LUG, HAD A NICK IN ITS BOTTOM EDGE. MAINTENANCE BLENDED THE DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-73-00. PERFORMED HFEC (EDDY CURRENT) TESTING AND FOUND NO DEFECTS. THE PART WAS TREATED, PRIMED AND PAINTED IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30004. UPON COMPLETION OF THE REPAIR, THE PART WAS INSPECTED AND FOUND A CCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008022100132 20080221 00132 NM 2008 2 21 F3LA200800061 1 20080207 A 5321 D5367204701000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 5503 2019 DURING C3/S1 C CHECK, INSPECTION REPORTED THE AFT CARGO PIT FLOOR PANEL 161BF HAD DENTS AND GOUGES OUT OF LIMITS. MAINT ENANCE REPAIRED THE DENTS AND GOUGES IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, TREATED, PRIMED AND PAINT ED THE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-21-11. UPON COMPLETION OF THE REPAIRS, THE PANEL WAS IN SPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008022100140 20080221 00140 EA 2008 2 21 SWIA200819202 1 20080206 A 5320 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CHAFED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 609SK 10020 CO-PILOT CONTROL COLUMN IS DIFFICULT TO MOVE. FOUND CROSS BEAM AT FS 295.0 CHAFED BY ELEVATOR CABLE. REPAIRED AREA IAW CRJ 700 REO 670-53-21-330. 2 L 7 2 4F RT A21EA 2008022100154 20080221 00154 NM 2008 2 21 HALA0800163 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1403 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 46, SEAT TRACKS AT RBL 88.5, STA 1403. REWORKED IAW SRM 53-00-52/101. REPLACED SEAT TRACKS I AW SRM WHERE DAMAGE WAS OUT OF LIMITS. 2 L 7 2 4F RT A1NM 2008022100170 20080221 00170 NM 2008 2 21 HALA0800170 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1288 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 46, SEAT TRACKS AT RBL 88.5, STA 1288. REWORKED IAW SRM 53-00-52/101, AND REPLACED SEAT TRACK S IAW SRM WHERE OUT OF LIMITS. 2 L 7 2 4F RT A1NM 2008022100177 20080221 00177 NM 2008 2 21 HALA0800178 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1156 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION AT RBL 54.75, SEAT TRACK, STA 1156, AT THE BASE OF TRACKS. CORROSION REMOVED PER SRM 51-10-02, REV 76 AND SRM 53-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008022100185 20080221 00185 EA 2008 2 21 SWIA200819215 1 20080211 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 947SW 7786 CAPTAINS WINDSHIELD CRACKED AFTER TAKEOFF, FLIGHT NR 5978. REPLACED CAPTAINS WINDSHIELD IAW CRJ 200 MM 56-11-01, PN: N P-139321-13, SN OFF: 03003H3702. 2 L 7 2 4F RT A21EA 2008022100189 20080221 00189 NM 2008 2 21 08FDEA00427 1 20080214 A 5320 655756911 SUPPORT BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 468FE 21452 LOWER AFT CARGO PIT, LT SIDE EDGE SUPPORT FROM FS 950F TO FS 1030 HAS AREAS OF SURFACE CORROSION AS MARKED REMOVED CORRO SION. ORIGINAL THICKNESS .056", .017 INCH REMAINING, .036 INCH MAT REMOVED. OUT OF LIMITS. REPAIR DOUBLER FABRICATED, TREATED AND PRIMED AND INSTALLED AT BS 991 REF SRM 51-10-1 FIG 7, 53-10-2 PG 45-46, 51-40-2, FIG 1 PG 1, 2, 3, 6, AMM 5 1-20-021-7 PG 1-7, 51-20-031-7 PG 1-7 THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008022100193 20080221 00193 NM 2008 2 21 HALA0800179 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1170 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION AT RBL 54.75, SEAT TRACKS, STA 1170, AT THE BASE OF TRACKS. CORROSION REMOVED PER SRM 51-10-02, REV 7 6 AND SRM 53-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008022100199 20080221 00199 EU 2008 2 21 08FDEA00443 1 20080214 A 5321 B5327028100200 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 MAIN DECK CARGO COMPARTMENT FLOOR BOARD 251 XF IS TORN. FABRICATED NEW PANEL NR 251 XF IAW FEDEX SRZ-005 REV F. MAJOR R EPAIR. 2 L 7 2 4F RT A35EU 2008022100203 20080221 00203 NM 2008 2 21 F3LA200800069 1 20080211 A 5320 D5347028200200 STRUCTURE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 902FR 5546 1515 DURING C5 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND AT THE CUT OUT OF THE AFT CARGO DOOR SELECTOR BOX. MAINTENAN CE REMOVED AND REPLACED THE CORRODED SELECTOR BOX IN ACCORDANCE WITH THE A319 SRM 51-42-11, A319 SRM 52-36-15-400-001 AN D EA A9-53R-30029. FOLLOWING COMPLETION OF THE INSTALLATION, THE BOX WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008022200004 20080222 00004 NM 2008 2 22 HALA0800262 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1385 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1385, AREA HAS BEEN REWORKED BEFORE. SEAT TRACK REPLACED PE R SRM. 2 L 7 2 4F RT A1NM 2008022200008 20080222 00008 WP 2008 2 22 08FDEA00495 1 20080218 A 5414 AUB703635 PANEL DOUG DC10 DC1030F 3023504 WP RT PYLON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 NR 3 PYLON AFT "V" PANEL NR 488 GL, ATTACHMENT HOLES CHAFFED. BLENDED DAMAGED AREAS, MAXIMUM DEPTH .055 IAW SRM 54-00-0 1, FIG 1A VOL I. FABRICATION PER EA NR 8-5480-118437. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II, PG 21-24. INSTAL LED DOUBLER AND FILLERS PER SRM 51-35-01 AND 51-33-01, VOL II. 2 L 7 3 4F RT A22WE 2008022200010 20080222 00010 EU 2008 2 22 08FDEA00504 1 20080218 A 5321 B5327062002900 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 MAIN CABIN FLOOR PANEL NR 242 RG IS CRACKED. FABRICATED NEW FLOORBOARD PNL NR 242RG IAW FEDEX DWG SRZ 25-005 REV F FOR INSTALLATION SEE W/C 62C0702. 2 L 7 2 4F RT A35EU 2008022200011 20080222 00011 EU 2008 2 22 08FDEA00505 1 20080218 A 5321 B5327061400500 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 MAIN CABIN FLOOR PANEL NR 242EK IS CRACKED. FABRICATED NEW FLOOR PNL NR 242EK IAW FEDEX DWG SRZ 25-005 REV F FOR INSTAL LATION, SEE W/C 62C0702. MAJOR REPAIR. 2 L 7 2 4F RT A35EU 2008022200014 20080222 00014 NM 2008 2 22 HAL0800245 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SEAT TRACK CROWN/BASE AT 1197+21. REWORKED PER SRM 51-10-02 AND SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022200017 20080222 00017 NM 2008 2 22 2008UALA00684 1 20080206 A 5241 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FWD GALLEY DOOR SN 1245, STOP PIN FITTING CUTOUT CRACKED, AFT SIDE, 2ND STOP FROM LOWER END. MAJOR REPAIR: BLENDED OUT DAMAGE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200018 20080222 00018 NM 2008 2 22 2008UALA00685 1 20080206 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 847 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 AFT CARGO DOOR CUTOUT AFT SIDE AT BS 847 HAD DAMAGE. MAJOR REPAIR: REINSTALLED SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200019 20080222 00019 NM 2008 2 22 2008UALA00687 1 20080206 A 5210 TORQUE TUBE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 R-1 DOOR UNDER UPPER HINGE TORQUE TUBE, WEB AND SKIN GOUGED BEYOND SRM LIMITS. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022200024 20080222 00024 NM 2008 2 22 HALA0800227 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1005 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT RBL 11, STA 1005. MAX DEPTH OF BLENDOUT WAS 0.012". BLENDED IAW SRM 51-10 -02. ALL BLENDOUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200025 20080222 00025 NM 2008 2 22 HALA0800206 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 867 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT RBL 54.75, STA 867, MAX DEPTH OF BLEND OUT WAS 0.003". BLENDED IAW SRM 51- 10-02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200026 20080222 00026 NM 2008 2 22 HALA0800199 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 848 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45,SEAT TRACK AT RBL 88.5, STA 848, MAX DEPTH BLENDOUT WAS 0.020". BLENDED IAW SRM 51-10-02. ALL BLENDOUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200029 20080222 00029 NM 2008 2 22 HALA0800207 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 787 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45,SEAT TRACKS AT LBL 88.5, STA 787, MAX DEPTH OF BLEND WAS 0.016". BLEND IAW SRM 51-10-02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200031 20080222 00031 NM 2008 2 22 HALA0800268 1 20080218 A 2150 A/C PACK BOEING 767 7673CB 1385187 NM LEFT MALFUNCTIONED A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM, L PACK INOP LIGHT ILLUM. EICAS MESSAGE L PACK TEMP DISPLAYED. OPERATED NORM AFTER STBY SELEC TED. TRIED AGAIN OK NO LIGHTS. INFO NOTED. CYCLED L PACK OPS CK NORMAL, NO FAULTS NOTED. REF AMM 21-00-00. OK FOR S ERVICE. 2 L 7 2 4F RT A1NM 2008022200035 20080222 00035 NM 2008 2 22 2008UALA00692 1 20080206 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 665UA 29237 FOUND EMERGENCY LIGHT AT SEAT 17HJ IS INOP. RESECURED LOOSE CONNECTION. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022200040 20080222 00040 NM 2008 2 22 HALA0800252 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1224 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1224 AREA HAS BEEN REWORKED BEFORE. SEAT TRACK REPLACED PER SRM. 2 L 7 2 4F RT A1NM 2008022200041 20080222 00041 NM 2008 2 22 HALA0800226 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 972 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT RBL 11, STA 972, MAX DEPTH OF BLEND OUT WAS 0.003". BLENDED IAW SRM 51-10- 02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200043 20080222 00043 NM 2008 2 22 HALA0800244 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1197+3. REWORKED PER SRM 51-10-02 AND SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022200046 20080222 00046 NM 2008 2 22 HALA0800254 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1256 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1256, AREA HAS BEEN REWORKED BEFORE. SEAT TRACK REPLACED PER S RM. 2 L 7 2 4F RT A1NM 2008022200047 20080222 00047 NM 2008 2 22 HALA0800198 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 837 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION AT RBL 88.5, SEAT TRACKS, STA.837 MAX BLEND OUT WAS 0.020".//BLENDED IAW SRM 51-10-02. BLENDOUTS WITHI N SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200048 20080222 00048 NM 2008 2 22 HALA0800201 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 948 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45 SEAT TRACKS AT RBL 88.5, STA 948, MAX BLEND OUT WAS 0.024". BLENDED IAW SRM 51-10-02. ALL BLENDS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200051 20080222 00051 NM 2008 2 22 2008UALA00702 1 20080207 A 5320 255T124128 SUPPORT BRACKET BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE BS 246 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 665UA 29237 BS 246, RBL 13.96 PULLEY SUPPORT BRACKET IS CRACKED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021400100 20080214 00100 NM 2008 2 14 QXEA200800073 1 20080114 A 5720 BRACKET DHAV DHC8 DHC8202 2809007 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - LT WING INBOARD LEADING EDGE LOWER OUTBOARD BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACE LEADING E DGE BRACKET. 2 H 7 2 4T RT A13NM 2008021400106 20080214 00106 NM 2008 2 14 QXEA200800058 1 20080204 A 2840 INDICATION SYS BOMBDR DHC8 DHC8402 1390042 NM FUEL MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 429QX 4161 GEG- FLIGHT 2328 (BZN-SEA) - FUEL IMBALANCE THAT COULD NOT BE CORRECTED BY FUEL TRANSFER. PANEL SHOWED GREEN AND WORKIN G, BUT AFTER ONE HOUR, NO FUEL TRANSFERRED. ON DESCENT IT WORKED PROPERLY. DIVERTED TO GEG AND ACCOMPLISHED A UNEVENTF UL LANDING. MAINTENANCE PERFORMED A OPERATIONAL CHECK OF THE FUEL SYSTEM WITH NO DEFECTS NOTED. COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008021400121 20080214 00121 NM 2008 2 14 QXEA200800103 1 20080114 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAPS DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - RIGHT OUTBOARD FLAP AREA NR 5 FLAP TRACK. THERE ARE TWO ROLLER CHAFE AREAS ON THE UPPER SURFACE. MAIN TENANCE BLENDED AREA, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2008021400123 20080214 00123 NM 2008 2 14 QXEA200800084 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX -C1 CHECK - SEAT TRACK NR 3 HAS A CORROSION PIT IN THE CHANNEL AT X544. MAINTENANCE BLENDED THE AREA, REMAINED WITH IN LIMITS AND INSPECTED, NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021400125 20080214 00125 NM 2008 2 14 QXEA200800102 1 20080114 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAPS CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - RIGHT OUTBOARD FLAP NR 4 FLAP TRACK INBOARD SIDE LOWER SURFACE OF UPPER FLANGE. THERE IS PITTING CORRO SION AT ROLLER CONTACT AREA. MAINTENANCE BLENDED OUT THE PITTING CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CR ACKS NOTED. 2 H 7 2 4T RT A13NM 2008021400126 20080214 00126 NM 2008 2 14 QXEA200800083 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - NR 2 SEAT TRACK HAS VERY LIGHT PITTING IN THE CHANNEL AT APPROXIMATELY X488. MAINTENANCE BLENDED THE P ITTED AREA, REMAINED WITHIN LIMITS AND INSPECTED, NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021400127 20080214 00127 NM 2008 2 14 QXEA200800079 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS 2 SMALL AREAS OF CORROSION AT APPROX X310. MAINTENANCE BLENDED OUT CORROSION, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021400129 20080214 00129 NM 2008 2 14 QXEA200800093 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 545 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - SEAT TRACK 36 AT X545 HAS PIT OF CORROSION THAT IS OUT OF LIMITS AT .028 DEEP. MAINTENANCE REMOVED SEA T TRACK AND INSTALLED NEW SEAT TRACK. 2 H 7 2 4T RT A13NM 2008021400135 20080214 00135 NM 2008 2 14 QXEA200800110 1 20080114 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSLEAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - LAV SERVICE DOOR APERATURE AFT LOWER CORNER CORRODED AROUND FASTENER. MAINTENANCE REMOVED LAV SERVICE DOOR CUT OUT DAMAGED AREA, FABRICATED REPAIR PACKER AND BACKING PLATE AND INSTALLED PACKER AND BACKING PLATE. 2 H 7 2 4T RT A13NM 2008021400140 20080214 00140 NM 2008 2 14 QXEA200800100 1 20080114 A 5542 SKIN DHAV DHC8 DHC8202 2809007 NM RUDDER DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - FORE RUDDER HAS A 1/4 BY 1/2 DENT ON RIGHT SIDE 13 INCHES FROM TOP EDGE 4 INCHES FROM TRAILING EDGE. M AINTENANCE CUT OUT SKIN DAMAGE, INSPECTED FOR CRACKS, NO CRACKS NOTED. REPAIRED IAW RD 8-55-1905 AND DHC8 200 SRM. 2 H 7 2 4T RT A13NM 2008021400146 20080214 00146 EU 2008 2 14 08FDEA00388 1 20080130 A 5753 BUSHING AIRBUS 310 A310222 3930315 EU LT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 LT WING OUTB FLAP, FITTING WITH UPPER BUSHING ATTACHMENT TO NR 3 TRUNNION WITH SPOTS OF CORROSION. REPAIRED IN ACCORDAN CE WITH FEDEX EA 6-5710-117224. 2 L 7 2 4F RT A35EU 2008021400149 20080214 00149 EU 2008 2 14 08FDEA00394 1 20080212 A 5315 A53974322202 FLOORBEAM AIRBUS 330 A300* EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION FOUND ON TOP CAP BEAM C 62 LT, Y450. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 208. 2 L 7 2 4F RT A26NM 2008021400150 20080214 00150 EU 2008 2 14 08FDEA00395 1 20080212 A 5340 A53773644202 FITTING AIRBUS 330 A300* EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION ON CORNER FITTING C 35 LT REPAIR PERFORMED BY REPLACING OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A26NM 2008021400155 20080214 00155 EU 2008 2 14 08FDEA00400 1 20080212 A 5315 A53974219220 FLOORBEAM AIRBUS 330 A300* EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION AT TOP CAP BEAM, C63, Y1470 REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A26NM 2008021400160 20080214 00160 EU 2008 2 14 08FDEA00405 1 20080212 A 5315 A53778807202 FLOORBEAM AIRBUS 330 A300* EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION AT TOP CAP BEAM C30 RT, C35 RT SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A26NM 2008021400163 20080214 00163 WP 2008 2 14 08FDEA00408 1 20080212 A 5310 CAP DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 388FE 46622 LT END CAP OF CAC DOMED PRESSURE BULKHEAD CRACKED. REMOVED AND REPLACED END CAP IAW SRM 51-31-01. END CAP FABRICATED O N MAE TRAVELER T8/725202. REMOVED AND REINSTALLED DOUBLER IAW SRM 51-31-01 FOR ACCESS. CLEANED AND RESEALED AREA IAW M M 20-60-08-2. 2 L 7 3 4F RT A22WE 2008021400168 20080214 00168 EA 2008 2 14 TRAX200800226 1 20080131 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 680BR 7679 AAR - 2031 - EMERGENCY EXIT INSTRUCTION PLACARD ON CREW ESCAPE HATCH UN READABLE. 2 L 7 2 4F RT A21EA 2008021400172 20080214 00172 NM 2008 2 14 NWAA080436314 1 20080211 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN DISCONNECTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 674US 30269 DURING OVERNIGHT CHECK, FOUND EMERGENCY LIGHTS LT AISLE IN A ZONE INOP. MAINTENANCE RECONNECTED LIGHT ASSEMBLY. OPERAT IONAL CHECKED OK AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008021400175 20080214 00175 EA 2008 2 14 MASA200800103 1 20080205 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75991 7422 ASH 7439 IAD AFT CELING FLOOD LIGHT INOP. RELAMPED 2 L 7 2 4F RT A21EA 2008021400177 20080214 00177 EA 2008 2 14 MASA200800109 1 20080207 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 931LR 3728 15031 ASH FLT 2885 PHX-IAH - CREW REPORTED 4 FWD GALLEY EMERGENCY LIGHTS INOPERATIVE. REMOVE AND REPLACED BATTERY PACKS. 2 L 7 2 4F RT A21EA 2008021400179 20080214 00179 EA 2008 2 14 MASA200800111 1 20080210 A 2560 PBE CNDAIR CL600 CL6002B19 1900309 EA NONE NONE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 77302 7302 ASH FLT 7202 ORD-MBS - AFT FA PBE WAS MISSING AN INSPECTION STICKER AND FWD FA PBE WAS MISSING AN INSPECTION STICKER AND TAMPER SEAL. MX INSPECTED THE EQUIPMENT AND INSTALLED INSPECTION STICKERS AND SEALS AS REQUIRED. 2 L 7 2 4F RT A21EA 2008021400184 20080214 00184 WP 2008 2 14 G60A200800010 1 20080207 A 5310 DOOR FRAME DOUG DC10 DC1030F 3023504 WP NLG WW CORRODED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 606GC 47929 FOUND CORROSION NOSE WHEEL WELL DOOR JAM STRUCTURE, SHELF. 2 L 7 3 4F RT A22WE 2008021400186 20080214 00186 EA 2008 2 14 MASA200800113 1 20080210 A 2560 PBE CNDAIR CL600 CL6002B19 1900309 EA NONE NONE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 77331 7331 ASH FLT 7368 ORD-MBS - CAPTAIN’S PBE WAS MISSING THE INSPECTION STICKER. MX INSPECTED THE PBE AND INSTALLED A NEW STICK ER. 2 L 7 2 4F RT A21EA 2008021500001 20080215 00001 EU 2008 2 15 2008UALA00556 1 20080130 A 3510 FILLER AIRBUS 320 A320232 3930326 EU OXYGEN SYSTEM LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 463UA 1282 AIRCRAFT O2 LOW. SUPPLEMENTAL DATA UPDATE CAUSE: LEAKING FILL PORT ON CREW O2 SERVICING PANEL. REPLACED FILL PORT AN D SERVICED CREW O2 TO FULL, NO LEAKS NOTED. 2 L 7 2 4F RT A28NM 2008021500023 20080215 00023 EA 2008 2 15 TRAX200800202 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 830-985 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 LT FLOOR SEAT RAIL FS 830.40 TO FS 985.0 AT LBL 9.0 HAS CORROSION DAMAGE ON RAIL AND HARDWARE. REMOVED CORROSION AND FO UND TO BE WITHIN LIMITS IAW CRJ 700 SRM 53-51-49. APPLIED ALODINE IAW CRJ 700 SRM 51-31-16. 2 L 7 2 4F RT A21EA 2008021200228 20080212 00228 NM 2008 2 12 USAA920080337 1 20080111 A 5311 654655514 FRAME BOEING 737 7373Y0 1384671 NM BS 867 S9L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 334AW 23748 MCN - MAJOR REPAIR - C18 CHECK - NR 6076586, CRACKED FRAME, BS 867, S9L. REPAIRED FRAME, BS 867, S9L IAW USAIRWAYS EA 1 00190. 2 L 7 2 4F RT A16WE 2008021200230 20080212 00230 NM 2008 2 12 USAA920080342 1 20080204 A 5330 6552988 SKIN BOEING 737 7373G7 1384595 NM BS 967 S21L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 PHX - MAJOR REPAIR - DAILY CHECK - NR 7884884, CRACKED FUSELAGE SKIN, BS 967, S21L. REPAIRED FUSELAGE SKIN, BS 967, S21 L IAW USAIRWAYS EA 120566. 2 L 7 2 4F RT A16WE 2008021200231 20080212 00231 EU 2008 2 12 USAA920080343 1 20080129 A 5280 D5281003400102 HINGE FITTING AIRBUS 320 A320232 3930326 EU NLG DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 675AW 2405 SAL - MAJOR REPAIR - BC2 CHECK - NR 6038208, NOSE LANDING GEAR RIGHT DOOR CENTER HINGE FITTING CRACKED. REPLACED THE NO SE LANDING GEAR RIGHT DOOR CENTER HINGE FITTING IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008021200232 20080212 00232 NM 2008 2 12 UPS08551615 1 20080203 A 3350 BULB BOEING 757 75724APF 1384969 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 407UP 23729 FOUND EMERGENCY LIGHT INOP. REPLACED LIGHT BULB PER MM 33-10-00. OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2008021200252 20080212 00252 EA 2008 2 12 A6WA200840009 1 20080105 A 3240 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BRAKES OUT OF ADJUST A A6WA O OTHER J WARNING INDICATION CL CLIMB 1 GL 31 435AW 7724 ANTI-SKID IB CAUTION MESSAGE AFTER TAKEOFF FOLLOWED BY PARKING BRAKE SHUTOFF VALVE CAUTION MESSAGE. LANDING GEAR HESITA TED TO RETRACT THEN RETRACTED SLOWLY, CAUTION MESSAGES WENT AWAY. HYD SYS NR3 QUANTITY AND PRESS NORMAL, ON GROUND SYST EM 3 HYD QTY 60 PERCENT. ADJUSTED PARKING BRAKE SWITCH IAW AMM 32-45-16. OPS CHECK GOOD. PERFORMED GEAR SWING AND TIMED GEAR SWINGS W/ 3A AND3B ALONE 7 TOGETHER . NO DEFECTS NOTED DUE TO DISCREPANCY INSPECTED HARNESSES PROX SWITCHES INTERG RATED PSCU NO FAULTS IN MEMORY. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008021200263 20080212 00263 2008 2 12 2008UALA00514 4 20080130 A 2565 BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EVAC SLIDE LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 117UA 28810 LEFT UPPER DECK DOOR SLIDE, AFT BOTTLE NEEDLE IS OUT OF THE GREEN BAND. SUSPECT FAULTY O-RING. REPLACED AFT BOTTLE PER AMM 25-68-02. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021200286 20080212 00286 NM 2008 2 12 2008UALA00539 1 20080130 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 616 S17R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 MID CABIN CREASE BEAM WEB AT STRINGER S-17R CRACKED ON LOWER SURFACE AT AFT SIDE OF BS 616 STUB FRAME. MAJOR REPAIR: RE MOVED AND INSTALLED NEW CREASE BEAM WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021300042 20080213 00042 NM 2008 2 13 ABXA080044 1 20080102 A 5330 141T83208 SKIN BOEING 767 767281 1385109 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 787AX 23020 R1 DOOR AFT LOWER CORNER INNER SKIN CRACKED. REPAIRED R1 DOOR AT AFT LOWER CORNER IAW B767 SRM. 2 L 7 2 4F RT A1NM 2008021300046 20080213 00046 NM 2008 2 13 USAA920080307 1 20080119 A 5753 RIB BOEING 737 7373S3 1384711 NM RT WING TE FLAP CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - NR 6060828, RIGHT WING OUTBOARD MIDFLAP RIB CRACKED, WBL 387.06. REPLACED RIGHT WING O UTBOARD MIDFLAP RIB IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008021300072 20080213 00072 EU 2008 2 13 USAA920080345 1 20080204 A 4900 APU AIRBUS 320 A320232 3930326 EU APU BAY ODOR A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 657AW 1083 LOG PAGE 7869922 - FLT NR 430 - CLT-PHX - ODOR - "DIRTY SOCKS" ODOR IS VERY STRONG IN CABIN CAUSING SEVERAL ALLERGIC REA CTIONS FROM CREW MEMBERS AND PASSENGERS. MAINTENANCE CLEANED THE APU INLET IAW TASK CARD Z6D49302. RAN PACKS AND OPERA TIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008021300091 20080213 00091 NM 2008 2 13 USAA920080361 1 20080122 A 5311 FRAME BOEING 737 7374B7 1384702 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q3 CHECK - NR E1A53032/4, CRACKED FRAME WEB, BS 178, RBL 5.7, WL 184. REPAIRED FRAME WEB, BS 178, RBL 5.7, WL 184 IAW B737 SRM 51-70-13. 2 L 7 2 4F RT A16WE 2008021300098 20080213 00098 NM 2008 2 13 USAA920080368 1 20080201 A 5754 SKIN BOEING 737 7374B7 1384702 NM ZONE 600 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q3 CHECK - NR JK-12-57502C/20, RIGHT WING NR 4 SLAT TRAILING EDGE DELAMINATED. REPAIRED RIGHT WING NR 4 SLAT TRAILING EDGE IAW USAIRWAYS TYPICAL REPAIR 57-42-03. 2 L 7 2 4F RT A16WE 2008021300103 20080213 00103 NM 2008 2 13 USAA920080373 1 20080125 A 5315 6545833212 FLOORBEAM BOEING 737 7374B7 1384702 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q5 CHECK - NR JK-46-53500-C/3, LEVEL 2 CORROSION ON FLOOR STRUCTURE "Z" ANGLE, BS 270, LBL 2 - RBL 2. REPAIRED FLOOR STRUCTURE "Z" ANGLE, BS 270, LBL 2 - RBL 2 IAW USAIRWAYS TYPICAL REPAIR 53-20-08. 2 L 7 2 4F RT A16WE 2008021300134 20080213 00134 NM 2008 2 13 USAA920080390 1 20080205 A 5322 6948985 SHEAR TIE BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 CLT - MAJOR REPAIR - C2 CHECK -NR 03-0553-8-0403/3, CRACKED SHEAR TIE, BS 360, S13L - S14L. REPLACED SHEAR TIE, BS 360, S13L - S14L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008021400006 20080214 00006 EA 2008 2 14 TRAX200800157 1 20080201 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 878AS 7590 DEPARTING ATL, FLAPS FAILED AT 8. COMPLIED WITH QRH RETURNED TO ATL, EMERGENCY DELCARED. 2 L 7 2 4F RT A21EA 2008021400011 20080214 00011 EU 2008 2 14 TRAX200800162 1 20080129 A 5210 SKIN AEROSP ATR72 ATR72212 8680945 EU PAX DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 ON PAX DOOR LWR FWD INNER SKIN HAS FASTENERS CORRODED. 2 H 7 2 4T RT A53EU 2008021400021 20080214 00021 EU 2008 2 14 TRAX200800172 1 20080131 A 5753 BRACKET AEROSP ATR72 ATR72212 8680945 EU TE FLAP CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 642AS 395 TWO OMEGA BRACKETS FOUND CRACKED ON FLAP ARM OUTB FLAP ARM OF LT INBOARD FLAP. 2 H 7 2 4T RT A53EU 2008021400035 20080214 00035 EA 2008 2 14 TRAX200800186 1 20080203 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA BS 645 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 LIGHT SURFACE CORROSION ON FRAME AT FS 645.00 BETWEEN BL 27L AND 27R AND BELLY SKIN JUST AFT OF FRAME INSIDE FWD CARGO B AY. CLEAN IMMEDIATE SURROUNDING AREA AND INSPECT FOR FURTHER CORROSION DAMAGE. 2 L 7 2 4F RT A21EA 2008021400045 20080214 00045 EU 2008 2 14 TRAX200800188 1 20080204 A 5720 ANGLE AEROSP ATR72 ATR72212 8680945 EU RT WINGBOX CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 642AS 395 RT WINGBOX FR 28 ANGLE CRACKED. 2 H 7 2 4T RT A53EU 2008021400048 20080214 00048 EA 2008 2 14 TRAX200800201 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 347-477 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 LT FLOOR SEAT RAIL FS 347.0 TO FS 477.0 AT LBL 9.0 HAS CORROSION DAMAGE ON TRACK AND HARDWARE. 2 L 7 2 4F RT A21EA 2008021400054 20080214 00054 EA 2008 2 14 TRAX200800212 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 785-863 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 RT SIDEWALL SEAT TRACK FS 785.15 TO FS 863.0 HAS CORROSION DAMAGE. REMOVED AND REPLACED RT SIDEWALL SEAT TRACKIAW AMM 53-00-49. 2 L 7 2 4F RT A21EA 2008021400055 20080214 00055 EA 2008 2 14 TRAX200800215 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 581-693 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 RT FLOOR SEAT RAIL FS 581.0 TO FS 693.0 AT LBL 9.0 HAS CORROSION DAMAGE ON RAIL AND HARDWARE. 2 L 7 2 4F RT A21EA 2008021400061 20080214 00061 NM 2008 2 14 NWAA080396308 1 20080202 A 5315 FLOORBEAM BOEING 747 747451 1384940 NM BS 380 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 668US 24223 DURING "M" CHECK, FOUND DOUBLE DRILLED FASTENER HOLES IN UPPER DECK FLOORBEAM AT BS 380 LBL 20 AND LBL 40. REPAIRED PER EA 63-211700. 2 L 7 4 4F RT A20WE 2008021400067 20080214 00067 WP 2008 2 14 UPS08851644 1 20080112 A 5230 SEAL DOUG DC8 DC871F 302199D WP CARGO DOOR BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 APPROX 3 INCHES OF SEAL BACK-UP STRUCTURE MISSING AT LOWER AFT CORNER OF C-PIT DOOR. REPAIRED C-PIT DOOR LOWER AFT CORNER IAW DWG. 5754260 AND SRM 52-02 -00 FIG 002. 2 L 7 4 4F RT 4A25 2008021400075 20080214 00075 EU 2008 2 14 08FDEA00270 1 20080121 A 5313 A30302525 STRINGER AIRBUS 310 A310222 3930315 EU BS 3143-3196 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 AFT CARGO COMPARTMENT, SUPERFICIAL CORROSION AT FR 58/59, STGR 56 LT. CORROSION WAS REMOVED IN ACCORDANCE WITH SRM 51-7 4-10 WITH A MAXIMUM DEPTH OF 0.008". REWORK AUTHORIZED PER FEDEX EA 6-5310-115316. 2 L 7 2 4F RT A35EU 2008021400097 20080214 00097 NM 2008 2 14 QXEA200800068 1 20080114 A 5320 SUPPORT ANGLE DHAV DHC8 DHC8202 2809007 NM THRESHOLD CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - SUPPORT ANGLE AT APPROX STA X600.00 AT DOOR THRESHOLD AREA HAS CORROSION ON NUTPLATES AND MOUNTING SURF ACE. MAINTENANCE REMOVED SUPPORT ANGLE AND INSTALLED NEW SUPPORT ANGLE. 2 H 7 2 4T RT A13NM 2008021400105 20080214 00105 NM 2008 2 14 QXEA200800078 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS A SMALL AREA OF CORROSION AT APPROX X330. MAINTENANCE BLENDED CORR ODED AREA, WITHIN LIMITS AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021400112 20080214 00112 NM 2008 2 14 ABXA080049 1 20080108 A 5300 141T300110 STRINGER BOEING 767 767232 1385132 NM BS 566-588 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 740AX 22213 STRINGER 36 RIGHT CRACKED BELOW SPLICE REPAIR, BETWEEN FS 566 AND 588. REPAIRED LONGERON 36 RIGHT IAW B767 SRM 53-00-03 , FIGURE 201 AND SRM 51-40-1. 2 L 7 2 4F RT A1NM 2008021400119 20080214 00119 NM 2008 2 14 ABXA080047 1 20080107 A 5330 141T8320 SKIN BOEING 767 767232 1385132 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 740AX 22213 SKIN CRACKED AT SERVICE DOOR ENTRY AFT LOWER CORNER INNER SKIN. REPAIRED SERVICE DOOR AFT LOWER CORNER. 2 L 7 2 4F RT A1NM 2008021400136 20080214 00136 NM 2008 2 14 QXEA200800085 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 468 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - SEAT TRACK NR 5 AT X468 HAS 2 CORROSION PITS ON INNER FLOORBOARD FLANGE. MAINTENANCE BLENDED OUT CORRO SION, REMAINED WITHIN LIMITS, INSPECTED AND NO CRACKS NOTED. APPLIED ALODINE AND PRIMER TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021400137 20080214 00137 NM 2008 2 14 QXEA200800082 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - NR 4 SEAT TRACK HAS CORROSION AT CAMLOCK RECEPTACLE UNDER DRIP TRAY AT STA X240. MAINTENANCE REMOVED C ORRODED SEAT TRACK AND INSTALLED NEW SEAT TRACK. 2 H 7 2 4T RT A13NM 2008021400138 20080214 00138 NM 2008 2 14 QXEA200800098 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - SUSPECT LIGHT CORROSION FORMING ON WEB TIE RIVET HEADS BELOW FLOOR AND SEAT TRACK. MAINTENANCE REMOVED RIVETS AND BLENDED OUT CORROSION, INSPECTED, REMAINED WITHIN LIMITS AND NO CRACKS NOTED. INSTALLED RIVETS AND RESTORED FINISH TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021400144 20080214 00144 NM 2008 2 14 QXEA200800092 1 20080114 A 5322 SHEAR TIE DHAV DHC8 DHC8202 2809007 NM BS 545 S31R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - X545 STRINGER 31R SUSPECT CORROSION AT SKIN CLIP. MAINTENANCE REMOVED RIVETS AND BLENDED OUT CORROSION FROM CLIP, BLEND REMAINED WITHIN LIMITS, INSPECTED AND NO CRACKS NOTED. INSTALLED RIVETS AND RESTORED FINISH TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021400148 20080214 00148 EU 2008 2 14 08FDEA00392 1 20080212 A 5313 A53974228200 STRINGER CLIP AIRBUS 330 A300* EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 STRINGER COUPLING C 65, P52 LT CORRODED. REPAIR PERFORMED BY REPLACING OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A26NM 2008021400158 20080214 00158 EU 2008 2 14 08FDEA00403 1 20080212 A 5313 A53778561207 STRINGER AIRBUS 330 A300* EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CORROSION AT STRINGER 53 RT, C28-29. SPLICE REPAIR PERFORMED IAW. SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A26NM 2008021500010 20080215 00010 2008 2 15 2008UALA00592 4 20080201 A 2565 D30654122U1 ASPIRATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 597UA 28750 FLAPPER VALVES ON ASPIRATOR LEAKING. FOUND SLIDE WAS DEPLOYED AND COULD BE THE CAUSE OF DAMAGED ASPIRATOR. REPLACED ASP IRATOR, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021500011 20080215 00011 EU 2008 2 15 2008UALA00593 1 20080202 A 3350 LAMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 421UA 500 LEFT OVERWING EMERGENCY LT. TEST FAILED EXTERNAL LOADS. SUPPLEMENTAL DATA UPDATE CAUSE: SEVERAL LAMPS FAILED IN LIGHT A SSY.CORRECTIVE ACTION: RELAMPED ASSY, OPS CHECK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021500012 20080215 00012 EU 2008 2 15 2008UALA00594 1 20080203 A 3350 D9239003500060 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 451UA 865 L MID CABIN EPSU FAILED TEST. FOUND EPSU FAILED. REPLACED EPSU, ALL TESTS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021500014 20080215 00014 NM 2008 2 15 2008UALA00610 1 20080202 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SEAT 17C INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 555UA 26647 SEAT 17C EEL LIGHT OUT. FOUND LAMP BURNED OUT. RELAMPED LIGHT, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021500015 20080215 00015 2008 2 15 2008UALA00644 4 20080204 A 2565 MECHANISM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ESCAPE SLIDE OUT OF ADJUST A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 437UA 655 DOOR 1L DOES NOT SHOW "SLIDE" ON ECAM OR "SLIDE ARMED" ON DOOR WHEN DOOR ARMING HANDLE IS PLACED IN THE ARM POSITION. F OUND DOOR ARMING MECHANISM OUT OF ADJUSTMENT. ADJUSTED DOOR, ARM LIGHTS OPERATE NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021500017 20080215 00017 NM 2008 2 15 08FDEA00412 1 20080212 A 5347 BAC1520729 SEAT TRACK BOEING 727 727200 138407E NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 MAIN CARGO COMPARTMENT, SEAT TRACK CORRODED IN NUMEROUS PLACES FROM BS 360-400, LBL 24. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-2 FIG7 AND 53-10-1 FIG3, SRM PAGE 23. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRI CATED NEW SEAT TRACK SECTION IAW SRM ER 01-040, 53-10-2 FIG7A, REV D 51-30-5 AND 51-10-1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2008021500019 20080215 00019 NM 2008 2 15 2008UALA00661 1 20080205 A 3350 2514303 LENS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 829UA 1211 DOOR 2 LEFT EXIT LT BROKEN. REPLACED LENS COVER. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021500026 20080215 00026 NM 2008 2 15 2008UALA00549 1 20080130 A 2611 GE1317 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SMOKE DETECTOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 EQUIPMENT COOLING SYSTEM TEST FAILED. SMOKE ANNUNCIATOR LIGHT INOP. EQUIPMENT COOLING SYS TEST FAILED. SMOKE ANNUNCIAT OR LIGHT INOP. RELAMPED DETECTOR. OPS CHECK OK. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500027 20080215 00027 EA 2008 2 15 TRAX200800209 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 570-708 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 LT SIDEWALL SEAT RAIL FS 570.0 TO FS 708.0 HAS CORROSION DAMAGE. REMOVED AND REPLACED SEAT RAIL IAW CRJ 700 AMM 53-00-49 . 2 L 7 2 4F RT A21EA 2008021500028 20080215 00028 EA 2008 2 15 TRAX200800210 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 477-570 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 LT SIDEWALL SEAT RAIL FS 477.40 TO FS 570.0 HAS CORROSION DAMAGE. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 53-31-49. APPLIED ALODINE IAW CRJ 700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2008021500029 20080215 00029 NM 2008 2 15 NOCA01308 1 20080208 A 3350 8100022608 LIGHT BOEING 757 75728A 1384976 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 752NA 28174 E-PATH LIGHT INOP ROW 16-19 ABC ACTION REPLACED LIGHT ASSY. 2 L 7 2 4F RT A2NM 2008021500030 20080215 00030 NM 2008 2 15 SWAA080804 1 20080212 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 504 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504C, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008021500031 20080215 00031 NM 2008 2 15 2008UALA00325 1 20080119 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 794 S26-27R CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 AFT PIT BILGE FRAME SHEAR TIE AND BEAR STRAP CORRODED BS 794 STR 26R TO 27R. FABRICATED AND INSTALLED SHEAR TIE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008021500032 20080215 00032 NM 2008 2 15 HALA0800066 1 20080118 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 730-110 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SEAT TRACK CORRODED BEYOND LIMITS AT STA 730 TO 110. REPLACED CORRODED SEAT TRACK IAW SRM 53-00-52 FIG 201, REPAIR 1. 2 L 7 2 4F RT A1NM 2008021500034 20080215 00034 NM 2008 2 15 HALA0800068 1 20080108 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 568 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SEAT TRACKS DAMAGED AT LOCATION LBL 11, STA.568. DAMAGE REMOVED IAW B767-300 SRM 53-00-52. WITHIN SRM LIMITS. 2 L 7 2 4F RT A1NM 2008021500035 20080215 00035 NM 2008 2 15 HALA0800069 1 20080108 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 534 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SEAT TRACKS DAMAGED AT LOCATION LBL 11 STA 534. DAMAGE REMOVED AT LOCATION LBL 11, STA 534 IAW B767-300 SRM 53-00-52, W ITH IN LIMITS. 2 L 7 2 4F RT A1NM 2008021500036 20080215 00036 NM 2008 2 15 HALA0800070 1 20080108 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 520 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SEAT TRACKS DAMAGED AT LOCATION RLB 11, STA 520. DAMAGE REMOVED AT LOCATION RBL 11, STA 520, IAW B767-300 SRM 53-00-52, WITHIN SRM LIMITS. 2 L 7 2 4F RT A1NM 2008021500037 20080215 00037 CE 2008 2 15 DXTA200802802 1 20080127 A 5210 SEAL CESSNA 750 750 2076810 CE PAX DOOR CONTAMINATED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 956QS 7500156 MAIN ENTRANCE DOOR HANDLE WILL NOT OPEN THE MAIN ENTRANCE DOOR FROM THE INSIDE, PASSENGERS AND CREW EXITED AIRCRAFT THRO UGH EMERGENCY EXIT (M2B). FOUND WATER IN DOOR SEAL PLUMBING, PURGED WATER FROM PLUMBING. OPERATIONALLY CHECKS GOOD IAW : CE750 M/M 52-10-04. 2 L 7 2 4J RT T00007WI 2008021500039 20080215 00039 NM 2008 2 15 HALA0800071 1 20080108 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 598 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SEAT TRACKS DAMAGED AT LOCATION RBL 11, STA 598. DAMAGE REMOVED AT LOCATION RBL 11, STA 598, IAW 767-300 SRM 53-00-52, WITHIN SRM LIMITS. 2 L 7 2 4F RT A1NM 2008021500047 20080215 00047 NM 2008 2 15 HALA0800076 1 20080108 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 820 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION AT SECTION 45, SEAT TRACK AT LBL 88.5, STA 820. CORROSION REMOVED CONFIRMED BY 10X MAGNIFICATION IAW SRM 51-10-02, BLENDED WITHIN LIMITES IAW SRM 53-00-52/101 REV 75. 2 L 7 2 4F RT A1NM 2008021500049 20080215 00049 CE 2008 2 15 DXTA200802807 1 20080129 A 3260 99147282 LOGIC CARD CESSNA 750 750 2076810 CE MLG INOPERATIVE E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 900QS 6315 6315 7500123 ON SHORT FINAL, THE RED UNLOCK LIGHT ILLUMINATED AND THE GEAR WARNING HORN BEGAN TO SOUND. R&R NLG ACTUATOR DOWNLOCK SW ITCH OPS CHECK GOOD. SERVICED EMERGENCY GEAR BLOW DOWN ACCUMULATOR . CHECKED HYD LEVELS NO SERVICING REQUIRED. WORK DONE IAW MM 12-10-15, 32-00-01, 33-30-03, 32-60-00, 12-10-35, IPC 3260-00 R&R MLG LOGIC MODULE IAW MM 24-53-00, OPS GOOD. 2 L 7 2 4J RT T00007WI 2008021500050 20080215 00050 NM 2008 2 15 BB08017 1 20080212 A 7334 21SN04158C PRESSURE SWITCH BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 205UW 23103 2733 30887 31743 ORF PHL-MCO FLT NR 1727 20 MINUTES AFTER TAKEOFF CREW RECEIVED A FUEL FILTER STATUS MESSAGE FOR NR 2 ENGINE. FLIGHT DIV ERTED TO ORF PER QRH. MAINTENANCE REPLACED THE LOW PRESSURE FUEL FILTER ON NR 2 ENGINE. NO FAULT FOUND. REPLACED NR 2 ENGINE DIF PRESSURE SWITCH. LEAK AND OPS CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E12EU 2008021500051 20080215 00051 NM 2008 2 15 ANCF200800004 1 20080208 A 3610 312N53217 AIR DUCT BOEING 757 7572T7 1384914 NM RROYCE RB211 RB211535E4 54555 NE LEAKING W ANCF E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 23 513NA 23895 31728 EICAS MESSAGE "L ENG OVHT" DISPLAYED, WITH "ENG OVHT" LIGHT ILLUM. LIGHT REMAINED ILLUM AFTER THRUST REDUCTION, ENGINE WAS SHUTDOWN , (LIGHT EXTINGUISHED INITIALLY AFTER THRUST REDUCTION BUT AFTER FEW SECONDS IT ILLUMINATED AGAIN). PERFOR M FIM 26-11-00 AND FIM 71-05-00 FIG 121, FOUND EGT EXCEEDANCE 865°C FOR 33 SECONDS ON ZONE "A", AS PER FIG 121, IT IS WI THIN LIMITS. ALSO PERFORMED FIM 26-11-00, ALL ENGINE OVERHEAT DETECTION TEST OK. DUE ENGINE SHUTDOWN IN FLIGHT MM 71- 99-00 PAGE 604 PARAGRAPH FOR -2B, WAS PERFORMED. DURING INSPECTION FOUND HP2 AND HP6 DUCTS EVIDENCE OF PLAY ON JUNCTIO N, CAUSING AIR LEAK. REF IPC, 75-00-51-01 FIG 1 PROCEDURE TO REPLACE, HP2 AND HP6 DUCTS PER AMM 36-11-01-401. 2 L 7 2 4F 4 F RT A2NM E12EU 2008021500063 20080215 00063 NM 2008 2 15 2008UALA00034 1 20080102 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FUSELAGE SKIN CRACKED AT FASTENER HOLE AFT OF E&E COOLING EXHAUST DUCT CUTOUT LBL 2 STA 378. MAJOR REPAIR: FABRICATED AND INSTALLED LARGE AREA EXTERNAL FUSELAGE DOUBLER AT E&E COOLING EXHAUST AND PREVENTATIVE MOD EXTERNAL DOUBLERS AT LOWE R RA ANTENNA. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500065 20080215 00065 NM 2008 2 15 2008UALA00035 1 20080102 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 DOOR 1L CUTOUT - UPPER DOOR HINGE CUTOUT CRACKED AT AFT EDGE OF FUSELAGE SKIN BEARSTRAP. MAJOR REPAIR: FABRICATED AND INSTALLED EXTERNAL FUSELAGE SKIN REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500066 20080215 00066 NM 2008 2 15 2008UALA00036 1 20080102 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 FUSELAGE EXTERIOR SKIN CRACKED AT BS 520 STR 12R. MAJOR REPAIR: FABRICATED AND INSTALLED EXTERNAL FUSELAGE SKIN DOUBLE R-TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500067 20080215 00067 NM 2008 2 15 2008UALA00037 1 20080102 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 AFT FUSELAGE SKIN CRACKED AT CHEM MILL STEP BS 727E + 3" STR 18L. MAJOR REPAIR: FABRICATED AND INSTALLED EXTERNAL FUSE LAGE SKIN DOUBLER-TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500088 20080215 00088 NM 2008 2 15 2008UALA00430 1 20080124 A 3350 1619 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 350UA 24301 EES LIGHT EXTERIOR LIGHT INOP JUST AFT OF DOOR 1L. RELAMPED EES EXTERIOR LIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500097 20080215 00097 NM 2008 2 15 2008UALA00438 1 20080126 A 2560 FITTING AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE GIRT BAR OUT OF ADJUST A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 805UA 783 TRYING TO INSTALL NEW SLIDE DOOR 2R. GIRT BAR WILL NOT ALIGN WITH PINS. SUSPECT GIRT GAR FITTINGS OR EMERGENCY CONTROL HANDLE OUT OF RIG. *S/D* GIRT BAR FITTING OUT OF ADJUSTMENT. ADJUSTED GIRT BAR FITTING, SYSTEM OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021500102 20080215 00102 NM 2008 2 15 UPS08551662 1 20080212 A 5610 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT STICKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 433UP 25464 CAPTAIN'S SLIDING WINDOW HARD TO OPEN AND CLOSE. DEFEREED PER MM 56-11-02-5, PG. 7. MAXIMUM 10 DAYS. CAPTAIN'S L2 WIND OW REMOVED AND REPLACED. THIS CLEARS D369021. 2 L 7 2 4F RT A2NM 2008021500103 20080215 00103 NM 2008 2 15 2008UALA00551 1 20080131 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY LIGHTS INOP LEFT OVERWING 2ND ASSY AFT FROM FWD MOST. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021500105 20080215 00105 NM 2008 2 15 UPS08551668 1 20080214 A 3260 LANDING GEAR BOEING 757 75724APF 1384969 NM MAIN WARNING MESSAGE A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 421UP 25281 AIR/GROUND DISAGREE MESSAGE. ACCOMPLISH FIM 32-09 FIG 106 NO FAULTS AND FIM 32-09-03 FIG 103 PSEU BITE CHECK, NO FAULTS NOTED. PSEU SYSTEM IS OK. STATUS MESSAGE CLEARED. 2 L 7 2 4F RT A2NM 2008021500107 20080215 00107 NM 2008 2 15 UPS08551669 1 20080210 A 2560 SEAL BOEING 757 75724APF 1384969 NM COCKPIT MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 441UP 27386 COCKPIT EMERGENCY DESCENT DEVICES NR 1, NR 2 AND NR 5 TAMPER RESISTANT SEALS ARE MISSING. REMOVED AND INSTALLED SERVICE ABLE DESCENT DEVICES AT POSITIONS 1, 2 AND 5. REF B757 MM 25-61-02-2. 2 L 7 2 4F RT A2NM 2008021500110 20080215 00110 2008 2 15 YENA2008015 4 20080201 A 2565 L32A319160001 CONTROL CABLE AIRBUS 320 A320232 3930326 EU LT OVERWING STIFF A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 613JB 11360 11360 2449 ON C2-01 CHECK, LEFT OVERWING SLIDE FLEXIBLE CONTROL CABLE STIFF AND FAILS TO RETRACT FOR OPS TEST. REMOVED AND REPLACE D LT FLEXIBLE CONTROL CABLE ASSY PER AMM 25-62-43-04, OPS CHECK OK. 2 L 7 2 4F RT A28NM 2008021500111 20080215 00111 2008 2 15 UPS08551671 4 20080211 A 3442 RADAR BOEING 757 75724APF 1384969 NM WX SYSTEM INOPERATIVE A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 467UP 25483 WX RADAR INOP THUNDERSTORMS IN AREA. R&R WEATHER RADAR TRANSCEIVER PER 757 AMM 34-43-01-4. OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 2008021500112 20080215 00112 NM 2008 2 15 2008UALA00560 1 20080130 A 2560 H2052K3833 LATCH BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EVAV SLIDE WORN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 664UA 29236 LEFT OVERWING ESCAPE SLIDE DOOR LATCHES 2, 3 AND 4 HAVE GROOVES (WEAR) ON SLIDER PLATES. REMOVED AND REPLACED LATCHES. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500114 20080215 00114 NM 2008 2 15 2008UALA00562 1 20080130 A 3350 LENS BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN CRACKED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 664UA 29236 SEVERAL LOWER EMERGENCY EXIT IDENTIFIER LENSES ARE CRACKED OR EXCESSIVELY DIRTY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500122 20080215 00122 2008 2 15 2008UALA00572 4 20080131 A 2350 MICROPHONE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT INOPERATIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 305UA 23666 FIRST OFFICER`S O2 MASK MICROPHONE INOP. REPLACED OXYGEN MASK. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500123 20080215 00123 2008 2 15 2008UALA00573 4 20080131 A 2350 MICROPHONE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 305UA 23666 OBSERVER`S O2 MASK MICROPHONE INOP. SWAPPED TO FIRST OFFICERS POSITION PER MEL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021300080 20080213 00080 EU 2008 2 13 08FDEA00364 1 20080207 A 5753 SKIN AIRBUS 300 A300B4605R 3930308 EU RT TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 DENT AND CRACK FINDING ON RT CENTER FLAP TRAILING EDGE LOWER SKIN. REPAIR PERFORMED BY INSTALLING A EXTERNAL PATCH IAW RAS/FOK/011/2008, APPROVED BY EA 6-5753-114875. 2 L 7 2 4F RT A35EU 2008021300104 20080213 00104 NM 2008 2 13 USAA920080374 1 20080203 A 5414 SKIN BOEING 737 7374B7 1384702 NM ZONE 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q5 CHECK - NR JK-81-54500/8, NR 1 PYLON LEFT SKIN CRACKED AT ACCESS PANEL 5924L. REPAIRED NR 1 PYL ON LEFT SKIN IAW USAIRWAYS TYPICAL REPAIR 54-50-07. 2 L 7 2 4F RT A16WE 2008021300132 20080213 00132 NM 2008 2 13 USAA920080388 1 20080203 A 5330 SKIN BOEING 737 7374B7 1384702 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 CLT - MAJOR REPAIR - C2 CHECK - NR 03-0553-8-0399/1, CRACKED FUSELAGE SKIN, BS 410, RBL 3. REPAIRED FUSELAGE SKIN, BS 4 10, RBL 3 IAW USAIRWAYS EA 110571 AND TYPICAL REPAIR 53-30-19A. 2 L 7 2 4F RT A16WE 2008021300135 20080213 00135 NM 2008 2 13 USAA920080391 1 20080205 A 5320 6926555 ANGLE BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 CLT - MAJOR REPAIR - C2 CHECK -NR 03-0553-8-0403/4, CRACKED ANGLE, BS 348 - B 351, S16L. REPLACED ANGLE, BS 348 - B 351, S16L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008021400040 20080214 00040 NM 2008 2 14 ZZDA2008054 1 20080107 A 5311 FRAME BOEING 717 717200 1383700 NM BS 1161 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 HOLES ELONGATED ON FRAME STA 1161 LBL0 TO LBL14. INSTALLED NEW LOWER CAP SECTION AND SPLICE FROM LBL0 TO LBL14, STA 116 1 IAW AIRTRAN EA17-53-00939A. 2 L 7 2 4F TR A6WE 2008021400044 20080214 00044 EA 2008 2 14 TRAX200800187 1 20080204 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 909EV 7658 EMERGENCY LIGHTS INOP. 2 L 7 2 4F RT A21EA 2008021400053 20080214 00053 EA 2008 2 14 TRAX200800208 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 708-761 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 LT SIDEWALL SEAT TRACK FS 708.0 TO FS 761.85 HAS CORROSION DAMAGE. REMOVED AND REPLACED LT SIDEWALL SEAT TRACK IAW AMM 53-00-49. 2 L 7 2 4F RT A21EA 2008021400082 20080214 00082 EU 2008 2 14 08FDEA00382 1 20080211 A 5320 A53612214201 FLOOR SUPPORT AIRBUS 330 A300* EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION FOUND ON FLOOR STRUCTURE C 11-14, Y-730, REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A26NM 2008022200053 20080222 00053 NM 2008 2 22 2008UALA00704 1 20080208 A 3350 5660568 LENS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 772UA 26930 FOUND DOOR 4R AFT EMERGENCY EXIT LIGHT LENS COVER MISSING. REPLACED LENS 2 L 7 2 4F 4 F RT T0001SE E46NE 2008022200054 20080222 00054 NM 2008 2 22 2008UALA00705 1 20080207 A 3350 767 LAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 791UA 26933 3L EXTERIOR MED EMERGENCY LIGHT INOP. SUSPECT FAULTY BULB. RELAMPED. OPS CHECKED OK. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008022200055 20080222 00055 NM 2008 2 22 2008UALA00706 1 20080207 A 3350 LAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE MID GALLEY RH INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 791UA 26933 EEL LIGHTS INOPERATIVE MID GALLEY RT SIDE. RELAMPED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008022200058 20080222 00058 NM 2008 2 22 AALA200800254 1 20080205 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39356 24037 JFK - EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RIG HT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008022200069 20080222 00069 WP 2008 2 22 AALA200800274 1 20080208 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 410AA 49321 DFW - EMERGENCY LIGHTS AT OVERHEAD TAIL COMPARTMENT AND TAIL CONE HANDLE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGEN CY LIGHTS AT OVERHEAD TAIL COMPARTMENT AND TAIL CONE HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022200071 20080222 00071 NM 2008 2 22 AALA200800264 1 20080207 A 3350 767 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 669AA 25334 SFO - EXTERIOR EMERGENCY EXIT LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY EXIT LIGH T AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008022200075 20080222 00075 NM 2008 2 22 2008UALA00707 1 20080206 A 2497 CONNECTOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE GALLEY FEEDER LOOSE A UALA O OTHER O OTHER CL CLIMB 1 WP 29 670UA 29240 LOST GALLEY POWER ON RIGHT SIDE ON CLIMB. REPLACED AFT GALLEY ELECTRICAL LOAD CONTROL UNIT M 226 AND RELAY K2 AT OVERHE AD PANEL, CHECKED K101,K102,K103 FOR SEC AND OVERHEAT. NO FAULTS NOTED. SEC AFT GALLEY MAIN FEEDER CONNECTOR 2 & HALF TU RN 138164ACP. OPS CHECK WITH ENG NR 2 RUNNING NO FAULTS NOTED. NO POWER TRIP OR GALLEY POWER SHED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022200078 20080222 00078 NM 2008 2 22 08FDEA00520 1 20080220 A 5710 69333281 FRAME BOEING 727 727227 1384078 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 LEFT WING OUTBOARD T/E NR 1 TRACK CENTER FAIRING INTERNAL AFT FORMER FRAME IS CRACKED IN CENTER. REMOVED AFT FORMER FRA ME, LOCATED AND DRILLED NEW AFT FORMER FRAME AND INSTALLED REF SRM 51-30-2 PG 1, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008022200080 20080222 00080 NM 2008 2 22 AALA200800239 1 20080203 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 766AN 32880 ORD - EMERGENCY LIGHT AT SEAT 23C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022000266 20080220 00266 NM 2008 2 20 F3LA200800064 1 20080212 A 5321 D5367403600000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 5503 2019 DURING THE C3/S1 C CHECK, INSPECTION REPORTED THE AFT CARGO PIT FLOOR PANEL 161CF HAD TWO AREAS OF OUT OF LIMITS DAMAGE ON ITS TOP FACE. MAINTENANCE REPAIRED THE AFFECTED AREAS IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, PRIM ED AND PAINTED THE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 25-00-00 801. UPON COMPLETION OF THE REPAIR AN D PAINTING, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008022000268 20080220 00268 NM 2008 2 20 HALA0800133 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 870 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 LIGHT SURFACE CORROSION TO TRACK BASE, SEAT TRACK AT LBL 54.75 STA 870. REWORKED CORROSION IAW SRM 51-10-02 REV 76. ALODINED REWORK AREA IAW SRM 51-20-01, REV 76. PRIMED IAW AMM 51-21-00 REV 67. REWORK WITHIN LIMITS PER SRM 53-0 0-52/101 REV 75. 2 L 7 2 4F RT A1NM 2008022000269 20080220 00269 NM 2008 2 20 HALA0800084 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 849 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION ON SEAT TRACK AT BS 849. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 51-10-02 REV 76, B LENDED WITHIN LIMITS IAW SRM 53-00-52/101, REV 76. 2 L 7 2 4F RT A1NM 2008022000270 20080220 00270 NM 2008 2 20 HALA0800085 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 867 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION ON SEAT TRACK AT BS 867. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 51-10-02 REV 76, B LENDED WITHIN LIMITS, IAW SRM 53-00-52/101, REV 76. 2 L 7 2 4F RT A1NM 2008022000278 20080220 00278 SO 2008 2 20 C2XA08IA049 1 20080206 A 3350 365271 SIGN EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 10156 145786 IAH - DURING A-CK INSPECTION THE LOWER EXIT SIGN ON THE LEFT HAND OVERWING EMERGENCY EXIT SURROUND WAS FOUND TO BE INOPE RATIVE. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APP ROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008022000294 20080220 00294 WP 2008 2 20 MWEA080028 1 20080213 A 2560 LATCH DOUG DC9 DC982 3022082 WP GIRT BAR INCORRECT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 808ME 48070 FLIGHT ATTENDANT ADVISED THAT THE GIRT BAR WAS THE INCORRECT SIZE & WOULD NOT FIT INTO FLOOR FITTINGS. REMOVED SEALANT FROM AFT GIRT BAR LATCH. REMOVED AND REPLACED FORWARD GALLEY GIRT BAR LATCH. 2 L 7 2 4F A6WE 2008021400108 20080214 00108 NM 2008 2 14 NWAA080426308 1 20080202 A 5347 SEAT TRACK BOEING 747 747451 1384940 NM BS 1080-1210 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 668US 24223 DURING "M" CHECK, FOUND CORROSION ON SEAT TRACK AT BS 1080 AND BS 1210 RBL 33.99. REPAIRED PER EA 63-211709. 2 L 7 4 4F RT A20WE 2008021400114 20080214 00114 NM 2008 2 14 ABXA080046 1 20080107 A 5330 141T3330 SKIN BOEING 767 767232 1385132 NM BS 1654 S4-8L CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 740AX 22213 SEVERAL FUSELAGE SKIN CRACKS FS 1654.5, STRINGER 4 LEFT, STRINGER 8 LEFT. REPAIRED AREA IAW B767 SRM 53-80-01. 2 L 7 2 4F RT A1NM 2008021400118 20080214 00118 NM 2008 2 14 ABXA080051 1 20080123 A 5410 313T1380243 STRUT BOEING 767 767232 1385132 NM LT ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 740AX 22213 NR 1 ENGINE STRUT INBOARD AFT BEAM INSIDE HYDRAULIC BAY CRACKED AT FORWARD END OF BEAM. INSTALLED NEW BEAM IAW B767 SRM 51-40-2. 2 L 7 2 4F RT A1NM 2008021400170 20080214 00170 EA 2008 2 14 TRAX200800228 1 20080201 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 680BR 7679 FS 280.00 RBL 9.00 INBD ATTACH ANGLE CRACKED. 2 L 7 2 4F RT A21EA 2008021400181 20080214 00181 WP 2008 2 14 G60A200800002 1 20080207 A 5347 SEAT TRACK DOUG DC10 DC1030F 3023504 WP BS 1927-1957 CORRODED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 606GC 47929 FOUND CORROSION ON SEAT TRACK IN FRONT OF AFT CARGO DOOR. 2 L 7 3 4F RT A22WE 2008021500009 20080215 00009 NM 2008 2 15 2008UALA00587 1 20080131 A 3510 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 1ST OFFICER'S MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 511UA 24799 F-O OXYGEN MASK AND SPEAKER ARE INSTALLED IN REVERSE POSITIONS. FOUND TO BE INSTALLATION ERROR (QA). REINSTALLED OXYG EM BOX AND SPEAKER BOX IN CORRECT POSITIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021500108 20080215 00108 NM 2008 2 15 2008UALA00558 1 20080130 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 UPPER DECK RT DOOR GROUND BATTERY TEST FAILS TO LIGHT. REPLACED BATTERY ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021500119 20080215 00119 NM 2008 2 15 2008UALA00568 1 20080131 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 BS 292 INTERCOSTAL BETWEEN STRINGER S-13R AND S-14R IS CRACKED AT THE OUTBOARD ANGLE. MAJOR REPAIR ACCOMPLISHED: INSTA LLED NEW INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500121 20080215 00121 NM 2008 2 15 2008UALA00570 1 20080131 A 5340 MOUNT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD ENTRY CORRODED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 382UA 24657 FORWARD ENTRY DOOR ESCAPE SLIDE AFT FLOOR MOUNT FOR SLIDE BRACKET CORRODED. MAJOR REPAIR: BLENDED CORROSION TO WITHIN L IMITS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500125 20080215 00125 NM 2008 2 15 2008UALA00575 1 20080201 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 SEAT 3A FWD EMERGENCY LIGHT IS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021500130 20080215 00130 NM 2008 2 15 2008UALA00578 1 20080201 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 UPPER DECK CEILING EMERGENCY LIGHT NEAR CEILING 16AB IS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021500131 20080215 00131 NM 2008 2 15 2008UALA00579 1 20080201 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 DOOR 2L CLOSET EMERGENCY LIGHT IS INOP. REPLACED ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021500135 20080215 00135 NM 2008 2 15 2008UALA00583 1 20080131 A 2560 HOUSING BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EVAC SLIDE BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 664UA 29236 LEFT OVERWING SLIDE DOOR DISCONNECT HOUSING IS BROKEN AND NEEDS TO BE REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500136 20080215 00136 NM 2008 2 15 2008UALA00584 1 20080131 A 5320 ATTACH ANGLE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 664UA 29236 FWD E&E COMPT AT STA 246 AT LBL 40 ATTACH ANGLE AFT SIDE OF FLOORBEAM IS CRACKED. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW ATTACH ANGLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500140 20080215 00140 NM 2008 2 15 2008UALA00595 1 20080201 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FUSELAGE STR 17R CREASE BEAM CORRODED AT APPROX AFT EDGE OF DOOR 2R CUTOUT. MAJOR REPAIR: INSTALLED NEW CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022000296 20080220 00296 NM 2008 2 20 PIDA08010 1 20080207 A 5313 STRINGER BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 DURING MAINTENANCE CHECK, NOTED CORROSION BETWEEN STRINGER 22LT AND FUSELAGE ATTACH ANGLE AT BS 727A. REPLACED DAMAGED SECTION OF STRINGER AND INSTALLED NEW STRINGER ATTACH CLIP PER EA 53-017. 2 L 7 2 4F RT A16WE 2008022000314 20080220 00314 NM 2008 2 20 MWEA080033 1 20080215 A 3310 UI3029 DIMMER BOEING 717 717200 1383700 NM COCKPIT FAULTY A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 917ME 55179 CIRCUIT BREAKER K-14 POPPED DURING COCKPIT PREP CHECK. REMOVED AND REPLACED DIMMER. 2 L 7 2 4F TR A6WE 2008022100103 20080221 00103 WP 2008 2 21 08FDEA00458 1 20080215 A 5321 AFA32043 FLOOR PANEL DOUG DC10 DC1030F 3023504 WP CARGO BAY DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 UPPER CARGO COMPARTMENT, AFT SECTION, LT SIDE AT STA 1741, THE O/B PANEL NR 281 FE (ORANGE) (MARKED AS "14L") IS DELAMIN ATED AND HAS TWO SMALL PUNCTURES. FABRICATED NEW FLOOR PANEL 281FE, POTTED EDGE, COMPLETED CURE AND SANDED EDGE POTTING . INSTALLED INSERTS, APPLIED NON-SKID AND PART MARKED PANEL IAW SRZ - 005 REV F. INSTALLED FLOOR PANEL IAW DC-10-30 S RM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2008022100122 20080221 00122 NM 2008 2 21 HALA0800150 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 2 CORROSION SECTION 46, SEAT TRACKS AT RBL 11, STA1197+137. REWORKED IAW SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022100128 20080221 00128 NM 2008 2 21 08FDEA00460 1 20080216 A 5753 ARC27364 SKIN DOUG MD11 MD11F 3023600 NM TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 RIGHT WING, INBOARD FLAP INBOARD LOWER SEGMENT LOWER SURFACE FOUND WITH DENT. DENT AREA FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I AND REPAIR CARRIED OUT AT RT WING INBOARD FLAP INBOARD LOWER SEGMENT LOWER SURFACE AS PER S RM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008022100161 20080221 00161 WP 2008 2 21 08FDEA00515 1 20080219 A 5330 NYB60085 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 CENTER WHEEL WELL LOWER SKIN HAS CORROSION FROM FS 1501 TO 1521 BETWEEN STR 50L TO51R. REMOVED, FABRICATED AND INSTALLE D REPAIR PER E8-5330-113024" FUSELAGE-SKIN AT STA 1519 AND L-52-REPAIR. 2 L 7 3 4F RT A22WE 2008022100165 20080221 00165 EU 2008 2 21 08FDEA00424 1 20080122 A 5753 SKIN AIRBUS 310 A310222 3930315 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 PREVIOUS REPAIR FOUND LOCATED ON LT (FLAP INBD UPPER SKIN) RIB 2/4 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINAT ION AND IF WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUS REPAIR WAS FOUND DAMAGED AND IT WAS REMOVED. NEW REPAIR WAS DONE PER SRM 57-52-12. 2 L 7 2 4F RT A35EU 2008022100172 20080221 00172 NM 2008 2 21 HALA0800172 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1243 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 46 SEAT TRACKS, AT RBL 88.5, STA 1243. REWORKED IAW SRM 53-00-52/101, AND REPLACED SEAT TRACK S WERE OUT OF LIMITS. 2 L 7 2 4F RT A1NM 2008022100180 20080221 00180 2008 2 21 SWIA200819210 3 20080209 A 6111 BLADE EMB 120 EMB120ER 3260203 SO LT PROPELLER CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 561SW 120335 LEFT PROP NR 1 BLADE APPEARS TO BE CRACKED. REPLACED NR 1 BLADE ASSY WITH SERVICEABLE UNIT. NO LEAKS NOTED, PN RFC11M1 R6AD4E2, SN OFF 880331. 2 L 7 2 4T RT A31SO 2008022100197 20080221 00197 EU 2008 2 21 08FDEA00440 1 20080214 A 3230 A252801 SEQUENCE VALVE AIRBUS 300 A300B4605R 3930308 EU MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 733FD 715 AFTER TAKEOFF FROM KIAD, THE RIGHT MAIN LANDING GEAR FAILED TO RETRACT AND REMAINED FULLY DOWN AND LOCKED ON BOTH FORWAR D AND OVERHEAD PANEL INDICATIONS. FOLLOWED ECAM AND QRH PROCEDURES, GOT DOWN AND LOCKED INDICATIONS ON ALL 3 GEAR. TH EN RETURNED TO LAND T/S RT GEAR HAS NO PRESS WITH GEAR PINNED. ACN RELEASED FOR SERVICE PER MEL/CDL: 32-30-01 CATEGORY: C EXPIRATION: 24FEB08 "MEL 32-30-01: LANDING GEAR RETRACTION SYSTEM - INOP TO MEM BASE FOR REPAIR. REMOVED AND REPLACE D RT MLG SEQUENCE VALVE IAW AIRBUS A300-600 AMM REF 32-31-37-4. OPS CK GOOD OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2008022100198 20080221 00198 NM 2008 2 21 08FDEA00442 1 20080214 A 5320 BAC1590100146 FLOOR SUPPORT BOEING 727 727227 1384078 NM BS 1164-1166 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 AFT LWR CARGO BAY BS 1164 - 1166 FLOOR SUPPORT ANGLE AT LBL 16 HAS CORROSION ON UNDERSIDE REPLACED FLOOR SUPPORT ANGLE A T BS 1164 - 1166 LBL 16, SRM 53-10-5 FIG 4 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2008022200006 20080222 00006 NM 2008 2 22 HALA0800265 1 20080218 A 2612 FIRE WARNING BOEING 767 7673G5 1385126 NM MALFUNCTIONED A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM, ARRIVED AT ACFT TO COMPLETE ETOPS-1 ASTERISKS ITEMS AND FOUND EICAS MSG "L ENG FIRE LP-1" ON E ICAS SCREEN STATUS AND MAINTENANCE PAGE. PERFORMED FIM 26-11-00 FIG 105 AND FIG 104, CYCLED C/B'S AS INDICATED IN PRERE QUISITES AND SWAPPED AFO LTS CARDS AS INDICATED IN FIM. CLEARED EICAS MSG AND PERFORMED FIRE WARNING TEST. NOW OPS GOO D. 2 L 7 2 4F RT A1NM 2008022200009 20080222 00009 EU 2008 2 22 08FDEA00503 1 20080218 A 5321 B5327060901500 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 MAIN CABIN FLOOR PANEL 242 ZJ IS CRACKED. FABRICATED NEW FLOOR BOARD PNL NR 242ZJ IAW FEDEX DWG SRZ 25-005 REV F FOR IN STALLATION SEE W/C 62C0702. 2 L 7 2 4F RT A35EU 2008022200023 20080222 00023 NM 2008 2 22 HALA0800217 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1062 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS LBL AT 88.5, STA 1062. MAX DEPTH BLENDED WAS 0.012". BLENDED IAW SRM 51-10-0 2. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200037 20080222 00037 NM 2008 2 22 2008UALA00694 1 20080206 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 665UA 29237 AFT ENTRY DOOR LEFT AND RIGHT EMERGENCY EXIT LIGHT IS INOP. INSTALLED NEW BATTERY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022200059 20080222 00059 NM 2008 2 22 AALA200800255 1 20080206 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 MIA - EMERGENCY LIGHT AT SEAT 31C HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 31C. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022800116 20080228 00116 NM 2008 2 28 AALA200800299 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022800117 20080228 00117 NM 2008 2 28 SWAA080953 1 20080219 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, LBL 3. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008021500145 20080215 00145 NM 2008 2 15 2008UALA00602 1 20080201 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 227 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 303UA 23644 FUSELAGE SKIN LOWER LOBE, LIGHTNING STRIKE AT BS 227, RBL 2. MAJOR REPAIR: FABRICATED AND INSTALLED EXTERNAL FUSELAG E SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500146 20080215 00146 NM 2008 2 15 2008UALA00603 1 20080202 A 5753 ATTACH FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FOREFLAP BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 RIGHT WING OUTBOARD FORE FLAP OUTBOARD ATTACH FITTING BROKEN AT FLAP CONNECTION POINT. REPLACED THE RT WING OUTBOARD FO RE FLAP ASSEMBLY. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500147 20080215 00147 NM 2008 2 15 2008UALA00605 1 20080202 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 EXTERNAL FUSELAGE SKIN HAS 2 EA CRACKS AT FASTENER HOLES AT FWD GALLEY DOOR UPPER HINGE CUTOUT. MAJOR REPAIR: INSTALLED NEW INTERCOSTAL WEB ASSEMBLY. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500151 20080215 00151 NM 2008 2 15 2008UALA00613 1 20080201 A 3350 BATTERY BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 EMERGENCY EXIT SIGNS AT BOTH AFT ENTRY DOORS ARE INOP. REMOVED AND REPLACED BATTERY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500153 20080215 00153 NM 2008 2 15 2008UALA00615 1 20080202 A 3350 582233 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 672UA 30027 FIVE EACH EXIT SIGN INOP L322, L297, L699, L700 AND L1050 WING HATCH EXIT SIGN. REPLACED BATTERY PACK. AT LOCATION M120 9. OP CHECKS OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500162 20080215 00162 2008 2 15 2008UALA00641 4 20080204 A 2330 RDFW785451 MONITOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN MALFUNCTIONED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 647UA 25284 ELECTRICAL ODOR COMING FROM VIDEO MONITOR LOCATED AT SEAT 8J. UNIT THEN SHUT DOWN. THE UNIT WAS CONFIRMED TO BE INOPER ABLE BY PACTECHNICIAN. AFTER INSPECTING ALL RELATED WIRING ASSOCIATED WITH THIS CIRCUIT, THE UNIT WAS REPLACED WITH A S ERVICABLE UNIT AND OPS CHECKED SATISFACTORY. THE SERVICABLE UNIT HAS BEEN ROUTED TO PAC REPAIR STATION FOR FURTHER INVE STIGATION ON FEB 1. GOOD-IN INSPECTION CONFIRMED THAT THE UNIT HAS A SLIGHT ELECTRICAL ODOR. TEAR DOWN REPORT TO FOLLO W. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500164 20080215 00164 NM 2008 2 15 SWAA080692 1 20080206 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021500165 20080215 00165 NM 2008 2 15 SWAA080706 1 20080206 A 5320 6545833 ANGLE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND ZEE CHORD CORRODED AT BS 270, LBL 11 TO RBL 11. REMOVED AND REPLACED ZEE CHORD PER S RM. 2 L 7 2 4F RT A16WE 2008021500167 20080215 00167 NM 2008 2 15 SWAA080708 1 20080206 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 23L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008021500173 20080215 00173 NM 2008 2 15 SWAA080700 1 20080206 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008021500178 20080215 00178 2008 2 15 SWAA080705 4 20080206 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008021500180 20080215 00180 WP 2008 2 15 G60A200800022 1 20080208 A 5320 FLOOR SUPPORT DOUG DC10 DC1030F 3023504 WP BS 1009 CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 607GC 46978 FWD CARGO COMPT STA 1009 LWR SIDEWALL FLOOR SUPPORT LWR END CRACKED 1 1/2". 2 L 7 3 4F RT A22WE 2008021500181 20080215 00181 WP 2008 2 15 G60A200800024 1 20080208 A 5312 STRUCTURE DOUG DC10 DC1030F 3023504 WP BULKHEAD CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 607GC 46978 AFT CARGO FWD BULKHEAD INBD POST HAS 2 CRACKS AT TOP CORNER. 2 L 7 3 4F RT A22WE 2008021500185 20080215 00185 NM 2008 2 15 SWAA080711 1 20080207 A 5330 6545768 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED BETWEEN BS 301 AND BS 331, STR 17R. REPAIRED SKIN PE R ER. 2 L 7 2 4F RT A16WE 2008021500188 20080215 00188 NM 2008 2 15 SWAA080734 1 20080207 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008021500190 20080215 00190 NM 2008 2 15 SWAA080735 1 20080207 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259.5, BETWEEN STR 21L AND STR 23L. REPAIRED SKIN PER AC O. 2 L 7 2 4F RT A16WE 2008021500193 20080215 00193 NM 2008 2 15 SWAA080716 1 20080207 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008021500203 20080215 00203 NM 2008 2 15 SWAA080726 1 20080207 A 5512 182A4001 SKIN BOEING 737 73776Q 13845AA NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 551WN 30280 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008021500209 20080215 00209 NM 2008 2 15 2008UALA00263 1 20080115 A 8012 8088846 START VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT ENGINE FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 776UA 26937 ENGINE WILL NOT TURN WITH STICK START. RIGHT ENGINE STARTER AIR VALVE POSITION DISAGREES WITH COMMANDED POSITION. REPL ACED STARTER VALVE PER MM 80-11-02. RAN ENGINE STARTED NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008021500214 20080215 00214 EU 2008 2 15 2008UALA00486 1 20080128 A 3510 OXYGEN BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 486UA 1620 O2 BOTTLE LOW AT SEAT ROW 26ABC. REMOVED AND REPLACED O2 BOTTLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021500215 20080215 00215 EU 2008 2 15 2008UALA00509 1 20080129 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 457UA 1146 CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED CREW O2, NO LEAKS WERE NOTED AT THIS TIME. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021900003 20080219 00003 NM 2008 2 19 2008UALA00571 1 20080131 A 3350 LENS BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 303UA 23644 EMERGENCY EXIT LIGHT ABOVE FORWARD GALLEY DOOR LENS IS LOOSE IN FRAME. REPLACED DAMAGED LENS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021900007 20080219 00007 NM 2008 2 19 HALA0800108 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 790-793 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45 SEAT TRACK AT LBL 11, HAS DAMAGE TO SEAT TRACK CROWN AT STA 790-793. CORROSION REMOVED, CO NFIRMED BY 10X MAGNIFICATION IAW SRM 51-10-02, REV 76, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101, REV 75. 2 L 7 2 4F RT A1NM 2008021900008 20080219 00008 NM 2008 2 19 HALA0800111 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 920 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45 SEAT TRACKS, AT LBL 11, HAS DAMAGE TO SEAT TRACK CROWN AT STA 920. CORROSION REMOVED, CONF IRMED BY 10X MAGNIFICATION IAW SRM 51-10-02, REV 76, BLENDED WITHIN LIMITS, IAW SRM 53-00-52/101, REV 75. 2 L 7 2 4F RT A1NM 2008021900010 20080219 00010 NM 2008 2 19 2008UALA00624 1 20080204 A 3397 UNKNOWN CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 118UA 28811 EEL PLUG BROKEN AT DOOR 5R. REPLACED PLUG. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021900011 20080219 00011 NM 2008 2 19 2008UALA00625 1 20080203 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT UPPER DECK ALONG STAIRS WALL INOP. REPLACED LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021900013 20080219 00013 WP 2008 2 19 G60A200800003 1 20080207 A 5320 FLOOR SUPPORT DOUG DC10 DC1030F 3023504 WP BS 1960-1968 CORRODED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 606GC 47929 FOUND CORROSION AFT CARGO FLOOR ANGLE. 2 L 7 3 4F RT A22WE 2008021900023 20080219 00023 SO 2008 2 19 RAIA00802002 1 20080202 A 2730 UNKNOWN EMB 145 EMB145LR 3260212 SO UNKNOWN A RAIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CE 03 838HK 145321 FLT 7961 - RUDDER PEDALS WILL NOT MOVE. HYDRAULIC PRESSURE INDICATED GOOD. FOLLOWED BY A YAW DAMPER FAIL MESSAGE ON T HE EICAS. MAINTENANCE DISENGAGED THE AUTOPILOT/YAW DAMPER AND PERFORMED A SUCCESSFUL OPERATIONAL CHECK OF THE RUDDER. MAINTENANCE PLACED THE YAW DAMPER FUNCTION ON MEL. 2 L 7 2 4T RT T00011AT 2008022200064 20080222 00064 WP 2008 2 22 AALA200800281 1 20080210 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 409AA 49320 LGA - EMERGENCY LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD GALLEY. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022200083 20080222 00083 NM 2008 2 22 AALA200800242 1 20080203 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 172AJ 32400 MIA - EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008022200088 20080222 00088 NM 2008 2 22 2008UALA00712 1 20080207 A 2612 LAMP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FIRE HANDLE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 935UA 26663 NR 1 AND NR 2 ENGINE FIRE HANDLES EACH HAVE ONE BULB BURNED OUT. REPLACED FIRE HANDLE BULBS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200092 20080222 00092 NM 2008 2 22 HALA0800243 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1187 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1187. REWORKED PER SRM 51-10-02 AND SRM 53-00-52. 2 L 7 2 4F RT A1NM 2008022200096 20080222 00096 NM 2008 2 22 AALA200800244 1 20080203 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 978AN 30100 MIA - EMERGENCY LIGHT AT SEAT 5E MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A16WE 2008022200097 20080222 00097 2008 2 22 2008UALA00714 4 20080208 A 2565 5A29011 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE ESCAPE SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 669UA 30025 SLIDE ASPIRATOR BARREL LEAKING. NO APPARENT DAMAGE TO ASPIRATOR. SUSPECT SEAL LEAKAGE. REPLACED ASPIRATOR & SLIDE ASS Y. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022200098 20080222 00098 2008 2 22 2008UALA00715 4 20080208 A 2565 O-RING BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SLIDE ASPIRATOR LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 673UA N5967 29241 SLIDE ASPIRATOR LEAKING. ASPIRATOR HAD BAD O-RING. REPLACED ASPIRATOR. SUSPECT O-RING PINCHED OR OVERLY COMPRESSED DU RING INSTALLATION. SLIDE REPLACED AND A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022200111 20080222 00111 NM 2008 2 22 2008UALA00724 1 20080208 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 480 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FUSELAGE DENTED AT STA 480 JUST BELOW FWD CARGO DOOR. MAJOR REPAIR: REMOVED DAMAGE. INSTALLED REPAIR DOUBLER AND FILLER S. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200113 20080222 00113 NM 2008 2 22 HALA0800253 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1241 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON SEAT TRACK/BASE AT LBL 88.5, STA 1241, AREA WAS REWORKED PREVIOUSLY. SEAT TRACK REPLACED PER SRM. 2 L 7 2 4F RT A1NM 2008022200116 20080222 00116 NM 2008 2 22 HALA0800237 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1073 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1073. REWORKED PER SRM 51-10-02 AND SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022200119 20080222 00119 NM 2008 2 22 HALA0800247 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1197+50. REWORKED PER SRM 51-10-02 AND SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022200121 20080222 00121 NM 2008 2 22 2008UALA00726 1 20080209 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 EXTERNAL FUSELAGE SKIN WORN .002" IN AN "L" PATTERN UNDER DORSAL FIN LANDING, JUST FWD OF DORSAL FIN AFT LT MOUNT. MAJO R REPAIR: REPAIRED FUSELAGE SKIN BY BLENDING OUT DAMAGE AND INSTALLED WEAR STRIPS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200124 20080222 00124 NM 2008 2 22 2008UALA00729 1 20080210 A 5340 ATTACH ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 300 S10L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FUSELAGE STR 10L INTERCOSTAL ATTACH ANGLE IS CRACKED BS 300. MAJOR REPAIR: REPLACED INTERCOSTAL, ATTACH ANGLE AND H-STR AP. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200132 20080222 00132 NM 2008 2 22 2008UALA00736 1 20080210 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FUSELAGE JUST FWD OF STA 360 AT DR 1L OPENING HAS WEB CRACKED AT STR 11L . MAJOR REPAIR: REPLACED INTERCOSTAL WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200133 20080222 00133 NM 2008 2 22 2008UALA00737 1 20080208 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 727B BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FOUND STRINGER CLIP BROKEN AT BS 727B AND STR S-20R. MAJOR REPAIR: REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2008021900029 20080219 00029 NM 2008 2 19 2008UALA00647 1 20080204 A 5210 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD ENTRY DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FWD ENTRY DOOR SN 251 UPPER BODY T-FITTING AREA GOUGED AT LOWER SIDE. MAJOR REPAIR: REMOVED DAMAGE. DRILLED UP AND INS TALLED NEW REPLACEMENT INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021900039 20080219 00039 NM 2008 2 19 2008UALA00657 1 20080204 A 2611 SMOKE DETECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU MALFUNCTIONED A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 305UA 23666 CARGO DETECTION SUPPRESSION PANEL FWD PIT FAIL LIGHTS ILLUMINATED. MODULE INDICATING BOTH B AND ONE A LOOP INOPERATIVE. REPLACED 1A AND 2B SMOKE DETECTORS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021400043 20080214 00043 SW 2008 2 14 WGEA200800020 1 20080204 A 2133 5412003 OUTFLOW VALVE ECLIPS EA500 ECLIPSEEA500 3350000 SW ZONE 100 DEFECTIVE E WGEA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 27 153DJ 42 000072 AT ALTITUDE THE DOOR LIGHT CAME ON, FOLLOWED BY CABIN DP HIGH LIGHT DP NOTED AS 8.6 PSI W/CABIN ALTITUDE INDICATING MUCH LOWER THAN NORMAL. TURNED OFF THE AIR SOURCE SELECTOR AND DESCENDED. CABIN ALTITUDE INDICATED, 500 FEET, EVEN AFTER D UMPING THE CABIN ON FINAL APPROACH, AND ON THE GROUND W/THE CABIN DOOR OPEN. REFERENCE WORK ORDER 1296, NRI 1. REPLACE D SECONDARY OUTFLOW VALVE PER EA500 AMM 21-30-13. ADJUSTED DOOR SENSOR PER EA500 AMM 52-00-00. PERFORMED PRESSURIZATION TEST PER EA500 AMM 21-30-03. OPS CHECK GOOD, NO FAULTS OR DEFECTS FOUND. 1 L 7 2 4J RT A00002AC 2008021400046 20080214 00046 EA 2008 2 14 TRAX200800191 1 20080204 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 902EV 7620 FS 280 AFT ANGLE CRACKED JUST O/B OF LBL 9.0. COMPLIED WITH EO 600-53-0091 PER REO 601R-53-11-136 & 601R53-11-1311. 2 L 7 2 4F RT A21EA 2008021400072 20080214 00072 WP 2008 2 14 UPS08851654 1 20080210 A 5753 SKIN DOUG DC8 DC871F 302199D WP RT TE FLAPS GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 RIGHT INBOARD T/E FLAP LOWER SURFACE DENT AT INBOARD LOCATION. MEASURE DENT AT 1 1/4 BY 1 3/4 .063 DEEP. FOUND .015 GO UGE IN DENT AND BLENDED TO .019 DEEP. REMOVED DAMAGE PER SRM 57-02-05. VERIFIED DAMAGED REMOVED. OK TO INSTALL DOUBLE R. INSTALLED DOUBLER AND COMPLETED REPAIR PER SRM 57-02. 2 L 7 4 4F RT 4A25 2008021400074 20080214 00074 EU 2008 2 14 08FDEA00269 1 20080121 A 5313 A30302525 STRINGER AIRBUS 310 A310222 3930315 EU BS 3090-3143 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 AFT CARGO COMPARTMENT, SUPERFICIAL CORROSION BETWEEN FR 54.3 AND 55, STGR 52LH. CORROSION WAS REWORKED IN ACCORDANCE WI TH SRM 51-74-10 WITH A MAXIMUM DEPTH OF 0.013". REWORK AUTHORIZED PER FEDEX EA 6-5310-115316. 2 L 7 2 4F RT A35EU 2008021400076 20080214 00076 EU 2008 2 14 08FDEA00271 1 20080121 A 5313 A30302525 STRINGER AIRBUS 310 A310222 3930315 EU BS 3249-3408 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 AT CARGO COMPARTMENT, SUPERFICIAL CORROSION AT FR 60/63, STGR 47 RT. CORROSION WAS REMOVED IN ACCORDANCE WITH SRM 51-74 -10, WITH A MAXIMUM DEPTH OF 0.008". REWORK AUTHORIZED PER FEDEX EA 6-5310-115316. 2 L 7 2 4F RT A35EU 2008021400085 20080214 00085 EU 2008 2 14 08FDEA00385 1 20080116 A 5347 A5381310920000 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 MDCC - SEAT-TRACK AT Y-2456 BETWEEN FR 38.2 AND FR40 WITH CRACK. SEAT-TRACK WAS REPLACED IN ACCORDANCE WITH SRM 51-72-1 0. 2 L 7 2 4F RT A35EU 2008021400099 20080214 00099 NM 2008 2 14 QXEA200800072 1 20080114 A 5315 FLOORBEAM DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - FLOORBOARD SUPPORT ANGLE CORRODED AT APPROX STA X599.00, Y26.00 RT TO Y31.00 RT, Y 0.00 TO Y 8.00 RT, Y 0.00 TO Y 6.00 LT. MAINTENANCE REMOVED CORROSION INSPECTED BLENDED AREA, WITHIN LIMITS AND NO CRACKED NOTED. ALODINED, PRIMED AND PAINTED. 2 H 7 2 4T RT A13NM 2008021400141 20080214 00141 NM 2008 2 14 QXEA200800105 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 370 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - SUSPECT CORROSION AROUND RIVET ON VERTICAL FRAME SUPPORT FOR NR 4 SEAT TRACK AT STA X370.00 INBOARD OF STRINGER 31L BOTTOM MOST INBOARD RIVET. MAINTENANCE REMOVED RIVET BLENDED OUT CORROSION, INSPECTED, REMAINED WITHIN LIM ITS AND NO CRACKS NOTED. INSTALLED RIVET AND RESTORED FINISH TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021400157 20080214 00157 EU 2008 2 14 08FDEA00402 1 20080212 A 5313 A53971007220 STRINGER AIRBUS 330 A300* EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION AT STRINGER 51 LT, C57.2-57.3 SPLICE REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A26NM 2008021400171 20080214 00171 EA 2008 2 14 TRAX200800230 1 20080206 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 902EV 7620 LOWER FS 280 FLOORBEAM WEB CRACKED OUTBOARD OF RBL9 (MARKED). REPAIRED DAMAGE IAW EO 600-53-90. 2 L 7 2 4F RT A21EA 2008021400178 20080214 00178 EA 2008 2 14 MASA200800110 1 20080209 A 5270 SENSOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT OUT OF ADJUST A MASA O OTHER N FALSE WARNING LD LANDING 1 SW 07 906FJ 15006 ASH FLT 2877 PHX-ELP - LT FWD EMERGENCY DOOR CAUTION MESSAGE AFTER LANDING. ADJUSTED SENSOR, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008021400189 20080214 00189 EA 2008 2 14 MASA200800116 1 20080210 A 4930 SOLENOID CNDAIR CL600 CL6002C10 1390015 EA APU LEAKING A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 521LR 10261 ASH FLT RON IN IAD - CAPTAIN REPORTED STRONG FUEL ODOR WHEN STARTING AND RUNNING APU ON GROUND. MX CND, CHECKED FUEL SO LENOID, RAN APU. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2008021500003 20080215 00003 EA 2008 2 15 FFKA020108125 2 20080201 A 8500 LW10442 DRIVE SHAFT PIPER PA32 PA32260 7103206 SO LYC O540 O540E4C5 41532 EA PROP GOVERNOR SHEARED B FFKA B A EMER. DESCENT UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 05 4817S 724 321277 L1199540C PILOT REPORTED A LOSS OF ENGINE RPM CONTROL (RUNAWAY PROP). AFTER REPLACING THE PROPELLER GOVERNOR AND THE PROPELLER TH ERE WAS STILL NO PROP CONTROL. MAINTENANCE FURTHER INVESTIGATED THE PROBLEM AND FOUND THE PROPELLER GOVERNOR DRIVE SHAF T GEAR SHEARED. AFTER ENGINE TEAR DOWN, IT WAS FOUND THAT A “BODY, HYDRAULIC TAPPET P/N 72877 WAS ALSO BROKEN. IT US U NKNOWN WHETHER THIS IS THE CAUSE OF THE ENGINE OVER SPEED OR THE PROPELLER GOVERNOR DRIVE SHAFT. 1 L 7 1 3O 3 O A3SO E295 2008022200137 20080222 00137 NM 2008 2 22 2008UALA00741 1 20080209 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 500B-500C CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FWD CARGO COMPARTMENT INTERCOSTAL CRACKED AT RT Z-ANGLE BETWEEN STA 500B AND 500C. MAJOR REPAIR: REPLACED CRACKED INTER COSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200142 20080222 00142 NM 2008 2 22 2008UALA00746 1 20080210 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 FOUND SEAT 5F FWD EMERGENCY LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022200143 20080222 00143 EU 2008 2 22 CPCP20080009 1 20080124 A 5320 BRACKET AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 399AT 399 LT BETWEEN FRAME 36 TO 39 FOLDING STEP BRACKETS CORRODED. CORROSION REMOVED ON FOLDING STEP BRACKETS IAW SRM 51-21-42. BRACKET FOUND OUT OF LIMITS 51-10-10. LT THRESHOLD FOLDING STEP BRACKET FABRICATED IAW SRM 53-67-70, FIG 128 AND INSTA LLED IAW SRM 51-25-00. 2 H 7 2 4T RT A53EU 2008022200145 20080222 00145 EU 2008 2 22 CPCP20080004 1 20080123 A 5310 DOOR FRAME AEROSP ATR72 ATR72212 8680945 EU PAX DOORWAY CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 399AT 399 PAX DOOR STAIRCASE THREADS UPPER & LOWER SURFACE CORRODED IN NUT PLATES AREA. PAX DOOR STAIRCASE TREADS SUPPORT CORROSI ON REMOVED IAW SRM 51-21-42 ON TREADS SUPPORT NR 1-2,4 AND 5 AND FOUND WITHIN LIMITS AS PER SRM 52-11-00 FIG 301. TREAD SUPPORT NR 3 HAVE BEEN REPLACED IAW SRM 52-25-01. 2 H 7 2 4T RT A53EU 2008022200148 20080222 00148 NM 2008 2 22 2008UALA00747 1 20080210 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 7AB FWD INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 FOUND SEAT 7AB FWD EMERGENCY LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022200158 20080222 00158 NM 2008 2 22 HALA0800209 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 884 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT LBL 88.5, STA 884, MAX DEPTH BLENDED WAS 0.026". BLEND IAW SRM 51-10-02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022500029 20080225 00029 NM 2008 2 25 HNAA0800058 1 20080203 A 3350 82520089101 LENS DHAV DHC8 DHC8102 2809003 NM CABIN DEFECTIVE A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 42387 42387 227 DURING SCHEDULED INSPECTION, THE CABIN EMERGENCY EXIT ILLUMINATED 'EXIT' SIGNS WERE FOUND TO BE DIM. MAINTENANCE CHANGE D THE LENSES OVER THE GLOW PANELS TO A CLEAR POST-MOD STYLE. DISCREPANCIES WERE SIGNED OFF AND AIRCRAFT RELEASED FOR SE RVICE. 2 H 7 2 4T RT A13NM 2008022500030 20080225 00030 NM 2008 2 25 HNAA0800057 1 20080202 A 3242 214665 BRAKE ASSY DHAV DHC8 DHC8102 2809003 NM MLG MALFUNCTIONED A HNAA C ABORTED TAKEOFF G MULTIPLE FAILURE TO TAKEOFF 1 EA 07 805EX 228 AFTER SETTING PARKING BRAKE AND RELEASING IT FOR TURN ONTO RUNWAY, BRAKES WERE GRABBING AND JERKY. WHILE TAXIING BACK T O GATE NR 1 AND NR 2 MAIN TIRES WENT FLAT. REPLACED BOTH NR 1 AND NR 2 BRAKES AND WHEEL ASSY'S. 2 H 7 2 4T RT A13NM 2008022500032 20080225 00032 NM 2008 2 25 HNAA0800061 1 20080208 A 2910 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYSTEM LEAKING A HNAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 07 814EX 318 NR 2 HYD QTY DROPPED TO .5 QTS AFTER T/O ASSOCIATED W/ISO LIGHT ILLUMINATED. RETURNED TO FIELD. INSTALLED TFL BEHIND N OSE GEAR GRAVEL GUARD, PLACED ON 70HR DMT, REMOVED FLEX LINE AND INSTALLED RIGID LINE. 2 H 7 2 4T RT A13NM 2008022500033 20080225 00033 NM 2008 2 25 2008UALA00670 1 20080205 A 2560 GIRT BAR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU R1 DOOR DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 914UA 25381 GIRT BAR AT 1R CATCHES ON AFT DOOR FRAME. MOVED GIRT BAR STOWAGE CLIPS TO PROPER LOCATION. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500045 20080225 00045 NM 2008 2 25 2008UALA00761 1 20080209 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 197UA 26901 EMERGENCY EXIT LIGHTS NEAR DOORS 1L AND 1R AND 1ST CLASS SEAT EMERGENCY LIGHTS ILLUMINATE DURING FLT. RECONNECTED BATTE RY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022100082 20080221 00082 WP 2008 2 21 08FDEA00496 1 20080218 A 2497 WIRE DOUG DC10 DC1030F 3023504 WP R1 DOOR BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 BY R-1 DOOR AIR BOTTLE TERMINAL BLOCK 53-901 HAS BROKEN WIRES AND TERMINAL BLOCK. REPLACED TERMINAL STRIP 53-901 IAW WD M 33-52-01. OP'S CHECKED EMERGENCY EXIT LIGHTS IAW 33-51-01-2, OPS CHECK GOOD. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008022100094 20080221 00094 WP 2008 2 21 08FDEA00449 1 20080215 A 5330 AYB60085 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 CENTER WHEEL WELL LOWER INTERIOR SKIN HAS CORROSION BETWEEN STR 47 R AND STR 48 R FROM FS 1501 TO FS 1520. REMOVED, FA BRICATED AND INSTALLED REPAIR PER E8-5330-113023 "FUSELAGE-SKIN AT STA 1507 AND 1519 AND L-48 RT-REPAIR. 2 L 7 3 4F RT A22WE 2008022100096 20080221 00096 WP 2008 2 21 08FDEA00452 1 20080215 A 5321 AFA3163509 FLOORBOARD DOUG DC10 DC1030F 3023504 WP BS 899-979 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MAIN CABIN FLOORBOARD AT APPROX RBL-20, AT APPROX BETWEEN STA 899 TO 979 IS DELAMINATED. FABBED NEW FLOORBOARD STA 89 9 TO 979, POTTED EDGES, COMPLETED CURE AND SANDED. INSTALLED INSERT , APPLIED ANTI-SKID, MARKED PNL IAW FEDEX DWG SRZ 25-005 REV F. THIS IS A MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008022100101 20080221 00101 NM 2008 2 21 08FDEA00418 1 20080213 A 5311 65561261 FRAME BOEING 727 727233 138408A NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 AFT CARGO COMPARTMENT INTERIOR, FRAME SURFACE HAS DENT AT STA 950F, STR 25L. REMOVED PREVIOUS REPAIR ANGLE IAW SRM 51-3 0-2. FABRICATED NEW REPAIR ANGLE IAW SRM 51-20-151-40-3 FIG 1 AND 53-10-2 FIG 5. HEAT TREATED ANGLE. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTALLED REPAIR ANGLE AT AFT CARGO COMP. FRAME BS 950F ABOVE S25L IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2008022100110 20080221 00110 NM 2008 2 21 08FDEA00468 1 20080217 A 5347 53FX139821 SEAT TRACK BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 MAIN CABIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION FROM STA 890 TO STA 950, BL 0. REMOVED AND REPLACED SEAT TRACK I AW SRM ER 01-049 AND SRM 53-10-5 AND 53-10-2 FIG 7A 2 L 7 3 4F RT A3WE 2008022100135 20080221 00135 NM 2008 2 21 F3LA00800046 1 20080206 A 3350 321430 BATTERY PACK AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE EMERGENCY LIGHTS FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 902FR 2147 1515 DURING C5 C CHECK, INSPECTION REPORTED FOUR EPSU BATTERY PACKS FAILED THEIR FUNCTIONAL TEST. PART NUMBERS WERE 3214-30 AND 3214-31 AND SERIAL NUMBERS 26993, 24287, 25994, AND 45007, RESPECTIVELY. MAINTENANCE REMOVED AND REPLACED ALL FOUR BATTERY PACKS IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-38-00-002 AND AMM 33-51-38-400-002. FOLLOWING COMPLETION OF THE INSTALLATION AND THEIR INSPECTION, THE UNITS TESTED GOOD. 2 L 7 2 4F 4 F RT A28NM 2008022100159 20080221 00159 NM 2008 2 21 F3LA200800057 1 20080217 A 5320 D5397496800400 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 903FR 5893 1560 DURING C5 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ALONG THE ATTACHMENT HOLES OF THE AFT CARGO PIT PROFILE AT FR AME 58, FROM THE RIGHT TO THE LEFT SIDE. MAINTENANCE REMOVED AND REPLACED THE PROFILE, COMMON TO FRAME 58, IN ACCORDANC E WITH THE A319 AMM 51-42-11, PARAGRAPH 6. FOLLOWING COMPLETION OF THE INSTALLATION, IT WAS INSPECTED AND FOUND ACCEPTA BLE. 2 L 7 2 4F 4 F RT A28NM 2008022100194 20080221 00194 NM 2008 2 21 08FDEA00437 1 20080214 A 5330 6554575 SKIN BOEING 727 727227 1384078 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 LOWER LEFT SIDE EXTERIOR FUSELAGE SKIN HAS DENT WITH SCRAPE STA 680 3 AND 7" BELOW STR 17L DENT WITHIN 10" OF PRODUCTION SEAM, REPAIR REQUIRED REF SRM 53-30-1 FIG 1. REMOVED DAMAGE IN REF TO SRM 53-30-1 HFEC FOR CRACKS AT CUT OUT . NONE F OUND. VERIFIED MATERIAL FOR REPAIR PLATE AS 2024 T3, .063 REF SRM 53-30-3 FIG 3A. FABRICATE DOUBLER IN REF TO 53-030-3 FIG 3A. INSTALLED DOUBLER IN REF TO 53-30-3 FIG 3A. THIS IS A CATEGORY "B" REPAIR, REFER TO SRM 51-00-6 GENERAL DATA REFER TO TABLE 3 FOR INSP INTERVALS THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008022200007 20080222 00007 EU 2008 2 22 08FDEA00487 1 20080215 A 5270 ABS030901 SWITCH AIRBUS 300 A300F4605R 3930327 EU CARGO DOOR FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 656FE 745 MAIN DECK CARGO DOOR OPEN (ECAM) IN FLT PASSING FL230 IN CLIMB. WARNING WENT OUT PASSING 10,000 MSL IN DESENT. RETURNE D TO KMEM "MEL 52-71-01: (IDENTIFY) MCD DOOR CLOSED AND LOCKED INDICATION ON ECAM DOOR PAGE INOP. MTSI OPENED DUE TO PR EV HISTORY. REPLACED MCD WARNING SWITCHES 48WS AND 49WS PER MM 52-71-11-5. CHECKED PER MM 52-71-11-5. OPS CHECK IS GO OD. 2 L 7 2 4F RT A35EU 2008022200013 20080222 00013 NM 2008 2 22 2008UALA00682 1 20080206 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 907 GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 EXTERNAL FUSELAGE SKIN IS GOUGED UNDER DORSAL FIN LANDING, 44" FWD OF BS 907 AT CENTERLINE. MAJOR REPAIR: BLENDED OUT D AMAGE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200057 20080222 00057 NM 2008 2 22 AALA200800253 1 20080205 A 2560 P2070003001 FLASHLIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 363AA 24044 SFO - EMERGENCY FLASHLIGHT AT AFT RIGHT FLIGHT ATTENDANT STATION INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT AT AFT RIGH T FLIGHT ATTENDANT STATION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008022200072 20080222 00072 WP 2008 2 22 AALA200800266 1 20080208 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISLODGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7536A 49990 LGA - EMERGENCY LIGHTS AT OVERHEAD FORWARD OF AFT ENTRY DOOR INOPERATIVE. SECURED LOOSE BATTERIES IN POWER PACK FOR EME RGENCY LIGHTS AT OVERHEAD FORWARD OF AFT ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022200108 20080222 00108 WP 2008 2 22 AALA200800250 1 20080205 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 251AA 49270 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 5 AND 6 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEA D SEAT ROWS 5 AND 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022200114 20080222 00114 NM 2008 2 22 HALA0800225 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 950 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION, SECTION 45 SEAT TRACKS AT RBL 11, STA 950, MAX DEPTH BLENDED WAS 0.009". BLENDED IAW SRM 51-10-02. ALL BLEND OUT WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200122 20080222 00122 NM 2008 2 22 2008UALA00727 1 20080209 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 DURING AFT LOWER LT FUSELAGE SKIN REPLACEMENT PER SB 737-53-1168, AN EXISTING .315" DIA HOLE AND AN EXISTING .156" DIA H OLE WERE FOUND AT LAP JOINT S-20L AT BS 727+9.9. MAJOR REPAIR: REMOVED DAMAGE. INSTALLED REPAIR DOUBLER AND TRIPLER WI TH FILLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200146 20080222 00146 EU 2008 2 22 CPCP20080006 1 20080124 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 399AT 399 LT SEAT TRACK BETWEEN FRAME 36-39 CORRODED. NEW SEAT TRACK LT BETWEEN FRAME 36-39. INSTALLED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2008022200151 20080222 00151 WP 2008 2 22 08FDEA00522 1 20080220 A 5320 AFA387019 INTERCOSTAL DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 LOWER AFT CARGO COMPARTMENT CORROSION ON INTERCOSTAL BETWEEN STRINGERS 44 AND 45 LT AT FS 1781. FABRICATED NEW INTERCOS TAL PER DAC DAW AFA 3870 REV F AND INSTALLED PER DC/MD10 SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2008022500003 20080225 00003 NM 2008 2 25 HNAA0800056 1 20080204 A 3260 864202 PROXIMITY SENSOR DHAV DHC8 DHC8102 2809003 NM LT MLG INTERMITTENT A HNAA K NONE N FALSE WARNING DE DESCENT 1 EA 07 934HA 139 GEAR SELECTED DOWN, LEFT MAIN GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED, ALT GEAR IND HAD THREE GREEN. CREW VERIFIED G EAR WAS DOWN. 2 H 7 2 4T RT A13NM 2008022500036 20080225 00036 NM 2008 2 25 2008UALA00672 1 20080205 A 2440 655379911 RECEPTACLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EXTERNAL POWER FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 347UA 24251 EXTERNAL POWER WAS ARCHING WHEN IN USE. SIGN OF CHARRING ON PANEL. REPLACED EXTERNAL POWER RECEPTACAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500008 20080215 00008 NM 2008 2 15 2008UALA00604 1 20080201 A 3234 GA65925 LEVER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NLG FAULTY A UALA O OTHER O OTHER CL CLIMB 1 WP 29 809UA 825 LDG GEAR DOORS SEQUENCED IMPROPERLY WHEN GEAR HANDLE RAISED. RED GEAR UNLK LTS EXTINGUISHED. INDICATIONS CYCLING OUT OF SEQUENCE AFTER HANDLE RAISED. ALL IND NORMAL AT THIS TIME, HOWEVER THERE IS A SLIGHT VIBRATION NOTED ON THE FLT DECK FLO OR. COULD NOT DUPLICATE CONDITION. PERFORMED ALL BYTE CHECKS- NORMAL, CFDS TESTS ARE NORMAL, INTERROGATED PFR REPORT - NO FAILURE OR FAULTS NOTED. PERFORMED A VISUAL CHECK ON NLG- NO DEFECTS NOTED. PERFORMED GEAR SWINGS AND NOTED SOME SEQUENCE ISSUES-REPLACED NOSE GEAR TARGET LEVER...ALL SEQUENCE ISSUES NOW RESOLVED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021500053 20080215 00053 SO 2008 2 15 RAIA00802013 1 20080212 A 3097 WIRE EMB 145 EMB145LR 3260212 SO ANTI ICE SYS BROKEN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 817HK 145058 FLT NR 5589 - STL - WING ANTI-ICE FAIL MESSAGE ON THE EICAS. MAINTENANCE REPAIRED A WIRE AT THE NR 1 BURST PRESSURE SWI TCH. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008021500054 20080215 00054 NM 2008 2 15 F3LA200800049 1 20080213 A 5411 D54630334206 FRAME AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE RT PYLON CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 902FR 5546 1515 DURING C7 C CHECK AND LEAK CHECKING THE RIGHT PYLON, INSPECTION REPORTED A CRACKED FRAME ON THE TOP, RIGHT SIDE OF THE P YLON, JUST AFT OF THE PRE-COOLER. MAINTENANCE REPAIRED THE CRACK IN ACCORDANCE WITH THE REQUIREMENTS OF DRAWING D546304 62, A319 SRM 54-52-12, PARAGRAPH 5E, SRM 51-42-11, PARAGRAPH 6B AND EA A9-54R-30020. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008021500068 20080215 00068 NM 2008 2 15 HALA0800113 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 987 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45 SEAT TRACK AT LBL 11, HAS DAMAGE TO SEAT TRACK CROWN AT STA 987M. CORROSION REMOVED, CONFI RMED BY 10X MAGNIFICATION, IAW SRM 51-10-02,REV 76, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101 REV 75. 2 L 7 2 4F RT A1NM 2008021500071 20080215 00071 NM 2008 2 15 HALA0800118 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 973 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45 AT LBL 11, HAS LIGHT CORROSION IN TRACK, AROUND HYLOX AT STA 973. CORROSION REMOVED, CONFI RMED BY 10X MAGNIFICATION IAW SRM 51-10-02, REV 75, BLENDED WITHIN LIMITS, IAW SRM 53-00-52/101, REV 75. 2 L 7 2 4F RT A1NM 2008021500073 20080215 00073 NM 2008 2 15 HALA0800119 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 950 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 2 CORROSION SECTION 45 SEAT TRACK AT LBL 88.5, AT STA 950. SEAT TRACK SECTION 950 REPLACED. 2 L 7 2 4F RT A1NM 2008021500074 20080215 00074 NM 2008 2 15 HALA0800103 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1003-1006 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45 SEAT TRACK, AT RBL 11, STA 1003-1006. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION, I AW SRM 51-10-02, REV 75, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101 REV 76. 2 L 7 2 4F RT A1NM 2008021500076 20080215 00076 EA 2008 2 15 COMA0860112 1 20080205 A 3010 53990001 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA RT NACELLE FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 409CA 6371 7441 FLIGHT 5003 - RECEIVED RIGHT COWL ANTI-ICE CAUTION ON CLIMB, ANTI-ICE SELECTED OFF. RETURNED TO CVG, LANDED WITHOUT INC IDENT. REPLACED RT COWL PRSOV. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008021500078 20080215 00078 2008 2 15 HNAA0800055 4 20080127 A 2340 53831 CRADLE DHAV DHC8 DHC8102 2809003 NM HANDSET INOPERATIVE A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 837EX 217 INTERPHONE BETWEEN FA'S STATION AND FLIGHT COMPARTMENT INOP, REPLACED HANDSET CRADLE, OPS CK'D GOOD. 2 H 7 2 4T RT A13NM 2008021500079 20080215 00079 NM 2008 2 15 SWAA080805 1 20080212 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 436WN 32456 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008021500081 20080215 00081 EU 2008 2 15 YENA2008013 1 20080202 A 3240 398912 CONTROL VALVE EMB ERJ190 ERJ190100IGW 3260408 EU BREAKS FAULTED A YENA O OTHER S AFFECT SYSTEMS AP APPROACH 1 EA 15 266JB 338 338 19000054 FLT NR 611, PWM-JFK, MESSAGES AT GEAR EXTENSION- BRK LH FAULT, BRK RT FAULT, REDUCED BRAKE EFFECTIVENESS ON ROLL OUT AND TAXI IN NOTED. DE/RE-ENERGIZE A/C PER FIM 32-41-00. REPLACED NR 4 BRAKE CONTROL VALVE PER AMM 32-41-00. OPS OK, LEAK CHECKED OK. 2 L 7 2 4F RT A57NM 2008021500085 20080215 00085 2008 2 15 SWAA080806 4 20080212 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 451WN 32495 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008021500087 20080215 00087 2008 2 15 SWAA080807 4 20080212 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 493WN 32477 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008021500090 20080215 00090 NM 2008 2 15 2008UALA00431 1 20080124 A 3350 1619 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 350UA 24301 EES EXTERIOR LIGHT INOP JUST AFT OF LT AFT WING TO BODY FAIRING. CLEANED, SOCKED AND RELAMPED. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500115 20080215 00115 NM 2008 2 15 2008UALA00563 1 20080131 A 5330 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU BS 941-944 S24L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 905UA 25005 EXTERNAL FUSELAGE SKIN CRACK STA 941- 944 STR 24L. MAJOR REPAIR: ACCOMPLISHED REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500040 20080225 00040 NM 2008 2 25 2008UALA00675 1 20080205 A 2421 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 589UA 28707 THE L BUSS TIE WILL NOT COME ON-LINE. LT (NR 1 ENG) IDG IS FAILING. REPLACED IDG, ALL TESTS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500048 20080225 00048 NM 2008 2 25 2008UALA00770 1 20080208 A 3350 1317 LAMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 665UA 29237 RIGHT AFT DOOR UPPER EMERGENCY EXIT LIGHT, DOOR HANDLE ILLUMINATION PORTION IS INOP. RELAMPED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500049 20080225 00049 NM 2008 2 25 2008UALA00771 1 20080208 A 2560 HOUSING BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EVAC SLIDE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 665UA 29237 LEFT OVERWING EMERGENCY SLIDE DISCONNECT HOUSING IS CRACKED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500054 20080225 00054 NM 2008 2 25 2008UALA00776 1 20080208 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 665UA 29237 L-1 DOOR EMERGENCY EXIT LIGHT IS INOP. RESEATED CONNECTOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500132 20080225 00132 EU 2008 2 25 2008UALA00695 1 20080208 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 401UA 435 EXTERNAL FUSELAGE SKIN IS DAMAGED AT FR 69+4 14" BELOW FLOOR. ACCOMPLISHED MAJOR REPAIR AT SFO. 2 L 7 2 4F 4 F RT A28NM E40NE 2008022500135 20080225 00135 EU 2008 2 25 2008UALA00697 1 20080207 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 442UA 780 CORROSION ON R2 DOOR SILL STRUCTURE FWD OF FR 68. ACCOMPLISHED MAJOR REPAIR AT LCQ. 2 L 7 2 4F 4 F RT A28NM E40NE 2008022500148 20080225 00148 NM 2008 2 25 2008UALA00713 1 20080207 A 2750 211C223212 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE T/E FLAP FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 595UA 28748 STATUS MESSAGE: FLAP ISLN VAL. PTU PRESSURE SWITCH FAULTY. REPLACED PTU PRESSURE SWITCH, OPS AND LEAK CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500158 20080225 00158 NM 2008 2 25 2008UALA00751 1 20080208 A 2612 M10427 CIRCUIT CARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE DETECTION FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 554UA 26644 FLIGHT DIVERTED DUE TO AFT CARGO FIRE INDICATION. INDICATION ISSUE WITH CONTROL CARD. REPLACED FIRE DET CIRCUIT CARD M 10427 FOR FWD AND AFT CARGO SMOKE DETECTION. ALL OPS CHECKS PERFORMED WERE SATISFACTORY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500178 20080225 00178 NM 2008 2 25 2008UALA00781 1 20080209 A 3350 582233 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 665UA 29237 LEFT EMERGENCY LIGHTS L1 AND L3 OVERWING LIGHTS ARE INOP. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500179 20080225 00179 NM 2008 2 25 2008UALA00783 1 20080211 A 2910 O-RING BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE HYDRAULIC SYS LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 676UA 30028 LANDED UNDER AMBER ALERT DUE TO CENTER HYDRAULIC SYSTEM INDICATION. CONDUCTED TROUBLESHOOTING. FOUND NR 3 SPOILER ACTU ATOR PLUG FOR FINGER FILTER O'RING BAD. REPLACE O'RING. OPERATES NORMALLY WITH NO LEAKS NOTED. SERVICED CENTER HYD SYS TEM FLUID TO FULL. A/C OK FOR RETURN TO SERVICE 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500199 20080225 00199 NM 2008 2 25 2008UALA00791 1 20080208 A 5230 146T6335 STRUCTURE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 665UA 29237 AFT MANUAL CARGO DOOR HAS DENT APPROX 3 INCHES FROM AFT EDGE AND THREE FEET FROM BOTTOM. REMOVED DAMAGED AREA. FABRICAT ED AND INSTALLED DOUBLER REPAIR. A/C OK FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500207 20080225 00207 NM 2008 2 25 2008UALA00800 1 20080211 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 673UA 29241 EEL LIGHT NEAR FWD GALLEY, ADJACENT TO DOOR 1L INOP. REPLACED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500210 20080225 00210 NM 2008 2 25 2008UALA00803 1 20080212 A 3350 1317 LAMP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 SEAT 49A SEAT EEL LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022500215 20080225 00215 NM 2008 2 25 2008UALA00808 1 20080211 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 WALL EEL INOP: BETWEEN MID LAVS. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021500117 20080215 00117 NM 2008 2 15 2008UALA00565 1 20080131 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 BS 293 INTERCOSTAL BETWEEN STRINGERS S-12R AND S-13R IS CRACKED IN OUTBOARD ANGLE. MAJOR REPAIR ACCOMPLISHED: INSTALLE D NEW INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500134 20080215 00134 NM 2008 2 15 2008UALA00582 1 20080131 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 EXIT PATH LIGHT STRIP AT 1F DISCONNECTED. SECURED CONNECTOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500137 20080215 00137 NM 2008 2 15 2008UALA00585 1 20080131 A 5753 HINGE FITTING BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE T/E FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 664UA 29236 RIGHT I/B AFT FLAP CENTER HINGE FITTING CRACKED ON I/B AND O/B SIDES. ACCOMPLISHED INSPECTION OF THE OUTBOARD HINGE FIT TINGS ON LEFT AND RIGHT WING INBOARD TRAILING EDGE MAIN FLAPS. MANDATED BY AD 2003-13-01 AND NOT EXTENDABLE. REMOVED, RE PLACED AND INSTALLED DAMAGED FLANGES. ACFT OK FOR SERVICE 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500157 20080215 00157 NM 2008 2 15 2008UALA00632 1 20080202 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 SEAT EEL INOP ROWS 55 THRU 61 RT. FOUND FEEDER SHORTED. REPAIRED SHORT AT FEEDER. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021500159 20080215 00159 NM 2008 2 15 2008UALA00634 1 20080202 A 3350 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 WALL EEL INOP DOOR 5R CROSS AISLE. FOUND SHORTED AT FEEDER WIRE. REPAIRED SHORT CIRCUIT AT FEEDER. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021500172 20080215 00172 NM 2008 2 15 SWAA080699 1 20080206 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 455WN 32462 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS MISSING AT ROW 11 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008021500184 20080215 00184 NM 2008 2 15 SWAA080710 1 20080207 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008021500194 20080215 00194 NM 2008 2 15 SWAA080717 1 20080207 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 414WN 29820 DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS MISSING AT LT OVERWING EXIT. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008021500218 20080215 00218 EU 2008 2 15 2008UALA00542 1 20080130 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 418UA 485 EMERGENCY LIGHT SYSTEM TEST FAILS FWD LEFT POWER SUPPLY UNIT. BATTERY FAILURE. REPLACED BATTERY ON 10WL UNIT AT DOOR 1 LEFT. EMERGENCY LIGHTS TEST OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008021900012 20080219 00012 EU 2008 2 19 MALA080023 1 20080210 A 3240 BRAKE ASSY SAAB SF340 340B 7860101 EU MLG FROZEN A MALA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 15 421XJ 340B421 LANDED WITH A FROZEN BRAKE ASSEMBLY, RESULTING IN FLAT RT MAIN GEAR TIRES. COMPLETE RT BRAKE CHANGE AND THAW OF LANDING GEAR. 2 L 7 2 4T RT A52EU 2008021900015 20080219 00015 NM 2008 2 19 2008UALA00626 1 20080203 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT ROW 58 LT INOPERATIVE. REPLACED LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021900016 20080219 00016 NM 2008 2 19 2008UALA00627 1 20080203 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT ROW 3J FWD INOPERATIVE. REPLACED LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030300038 20080303 00038 NM 2008 3 3 08FDEA00646 1 20080226 A 2497 MC27212212 WIRE HARNESS BOEING 727 7272S2F 1384O81 NM ZONE 100 BURNED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 213FE 22935 WHILE WORKING WRI 31-30/9464, TECH FOUND A SHORTED WIRE HARNESS IN AVIONICS COMPT. THE 3 PHASE WIRE HARNESS FROM THE EX TERNAL POWER RELAY HAS MADE CONTACT WITH GND BUS STRIP T268 (LOCATED DIRECTLY ABOVE APU GCU). INITIAL VISUAL INSPECTION SHOWS SEVERAL GND STUDS ARE BURNED/DAMAGED, ONE OR MORE WIRES FROM EPR ARE DAMAGED AND A SECOND HARNESS LOCATED IN THE SAME AREA APPEARS TO BE DAMAGED. INSTALLED T00268 PER WDM 91-21-41 PG 37, EXT POWER FEEDER CABLES PER WDM 91-21-11 PG 1 , UP LIST 91-21-11 PG1 AND AS PER MM 20-20-00, BOEING SWPM CHAPT 20. REF EA 7-2440-119592 USE OF ORIGINAL TERMINAL STRI P IN REVERSE POSITION. 2 L 7 3 4F A3WE 2008021900030 20080219 00030 NM 2008 2 19 2008UALA00649 1 20080204 A 5210 5A26443 RESERVOIR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 195UA 26899 UPPER DECK, RIGHT HAND EXIT DOOR EMERGENCY RESERVIOR PRESSURE IN THE YELLOW BAND. SUSPECT FAULTY O-RING. REPLACED DOOR EMERGENCY POWER RESERVOIR PER 52-23-13 . OPS CHECKS OK . 2 L 7 4 4F 4 F RT A20WE E24NE 2008021900032 20080219 00032 NM 2008 2 19 2008UALA00654 1 20080203 A 5753 FLAP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT WING CRUSHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 661UA 27158 LEFT WING,OUTBOARD FLAP LEADING EDGE IS CRUSHED AND HAS 1 INCH LONG PUNCTURE LOCATED FROM APPROX 24 INCHES FROM OUTBOARD END TO APPROX 48 INCHES FROM OUTBOARD END. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500223 20080225 00223 NM 2008 2 25 2008UALA00820 1 20080212 A 3350 1317 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 644UA 25094 RIGHT OVERWING EEL AND ROWS 16 THRU 26 EEL INOP. CLEANED, DRIED AND REINSTALLED LAMPS. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022100179 20080221 00179 NM 2008 2 21 08FDEA00426 1 20080214 A 5753 SKIN BOEING 727 727227 1384078 NM TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 RT WING OUTBOARD AFT FLAP, LWR SURFACE 1 INCH FROM OUTBOARD END, SKIN DISBONDED. REPAIRED RT OUTBOARD AFT FLAP LOWER SU RFACE 1 INCH FROM OUTBOARD END. REF 51-40-20 PAR 7, 8, 14, 15, 18, 20-22. THIS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008022200028 20080222 00028 NM 2008 2 22 HALA0800242 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1168 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1168. REWORKED PER SRM 51-10-02 AND SRM 53-00-52. 2 L 7 2 4F RT A1NM 2008022200056 20080222 00056 CE 2008 2 22 JX6A200800001 1 20080116 A 3230 45A38672031 CABLE ASSY MTSBSI MTSBSI MU300 MU300 5780602 CE MLG DOOR KINKED E JX6A O OTHER P NO WARNING INDICATION LD LANDING 1 CE 09 4569 A029SA DURING LANDING IN FAY THE LT MLG DOOR CONTACTED THE RUNWAY. 3 DOWN & LOCKED LIGHTS WERE ILLUMINATED IN THE COCKPIT. MAI NTENANCE DISCOVERED THE LT MLG EMERGENCY RELEASE CABLE HAD BECOME LODGED & WOULD NOT ALLOW THE DOOR UP-LOCK TO FULLY OP EN. THE UPLOCK DID ALLOW THE DOOR TO OPEN BUT WOULD NOT ALLOW THE DOOR TO RETURN TO THE FULL UP & LOCKED POSITION DURING GEAR EXTENSION. THE DOOR UPLOCK DID HOWEVER, LATCH IN THE CLOSED POSITION ILLUMINATING THE GREEN DOWN & LOCKED LIGHT LE ADING THE CREW TO BELIEVE THAT THE GEAR WAS SAFE FOR LANDING. WITH THE LANDING GEAR EXTENDED & ALL SWITCHES IN THEIR PR OPER LANDING POSITION, THE HYDRAULIC SYSTEM PRESSURE WAS RELIEVED & NO LONGER APPLIED TO THE MLG SYSTEM THUS ALLOWING TH 2 H 7 2 4F RT A14SW 2008022200067 20080222 00067 EU 2008 2 22 CPCP20080007 1 20080124 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 399AT 399 RT SEAT TRACK BETWEEN FRAME 36 TO 39 CORRODED. NEW SEAT TRACK RT BETWEEN FRAME 36 TO 39, INSTALLED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2008022200070 20080222 00070 NM 2008 2 22 AALA200800265 1 20080208 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 787AL 30010 ORD - EMERGENCY WALL MOUNTED LIGHT AT RIGHT AFT GALLEY WALL MISSING LENS. REPLACED LIGHT ASSEMBLY AND REPAIRED BROKEN W IRE FOR EMERGENCY WALL MOUNTED LIGHT AT RIGHT AFT GALLEY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022200074 20080222 00074 NM 2008 2 22 AALA200800238 1 20080203 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 766AN 32880 ORD - EMERGENCY LIGHT AT SEAT 19C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 19C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022200131 20080222 00131 NM 2008 2 22 HALA0800219 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 875 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT LBL 54.75, STA 87, MAX DEPTH OF BLEND OUT WAS 0.009". BLENDED IAW SRM 51-1 0-02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200136 20080222 00136 NM 2008 2 22 2008UALA00740 1 20080208 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 867 S20R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 AFT CARGO COMPARTMENT STA 867 STR 20R STRINGER CLIP IS DAMAGED. MAJOR REPAIR: REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200149 20080222 00149 NM 2008 2 22 2008UALA00748 1 20080210 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 ZONE D CEILING EMERGENCY LIGHTS BOTH SIDES IS INOP. BATTERY PACK INOPERATIVE. REPLACED BATTERY 2 L 7 4 4F 4 F RT A20WE E24NE 2008022200150 20080222 00150 NM 2008 2 22 2008UALA00749 1 20080209 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 WALL EEL INOP:LT SIDE AFT GALLEY. REPLACED LAMP 2 L 7 4 4F 4 F RT A20WE E24NE 2008022200153 20080222 00153 NM 2008 2 22 AALA200800267 1 20080208 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 195AN 32389 DFW - EMERGENCY LIGHT AT SEAT 19D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008022500125 20080225 00125 NM 2008 2 25 2008UALA00686 1 20080206 A 2597 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GIRT BAR OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 529UA 25019 DOOR 4L DOOR SLIDE ARM LIGHT DOES NOT COME ON WHEN ARMED, POPS C-B. FOUND WIRES AT GIRT BAR SWITCH CONTACTING GROUND. REPOSITIONED WIRES CORRECTLY, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500168 20080225 00168 NM 2008 2 25 2008UALA00768 1 20080211 A 2560 SIGN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 590UA 28708 AFT SIDE OF OVERWING EXIT SIGN IS LOOSE ON THE RIGHT SIDE OF AIRCRAFT. RESECURED EXIT SIGN. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500200 20080225 00200 2008 2 25 2008UALA00792 4 20080211 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AFT RT DOOR OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 546UA 25367 AFT RIGHT DOOR WON'T ARM. LANYARD INTERFERENCE. REPOSITIONED LANYARD, DOOR ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021900037 20080219 00037 NM 2008 2 19 CALA0800110 1 20080203 A 5310 6520722U98 DOOR FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 FORWARD CARGO DOOR CUTOUT FORWARD FRAME HAS A CRACK AT THE NR 5 DOOR STOP. REPLACED FORWARD CARGO DOOR CUT-OUT FORWARD FRAME PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008021900042 20080219 00042 NM 2008 2 19 HALA0800048 1 20080110 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 471 S2L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LIGHTING STRIKE ON A/C CROWN AT LOCATION, STA 471,S2L. REPAIRED IAW 767-300, SRM 53-00-01 REPAIR 8. 2 L 7 2 4F RT A1NM 2008021900044 20080219 00044 NM 2008 2 19 CALA0800096 1 20080127 A 5310 65C251721 BEAM BOEING 737 7373T0 1384582 NM BS 1121 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76354 23592 CORROSION ON HORIZONTAL STAB CENTER SECTION LT PRIMARY BEAM LOWER CHORD VERTICAL LEG AT BODY STATION 1121. REPAIR PER E CRA 5510-01914. 2 L 7 2 4F RT A16WE 2008021900047 20080219 00047 NM 2008 2 19 HALA0800051 1 20080110 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 594 S2L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LIGHTING STRIKE ON A/C CROWN AT LOCATION,STA. 594, BELOW S2L. REPAIRED IAW 767-300, SRM 53-00-01, REPAIR 8. 2 L 7 2 4F RT A1NM 2008021900048 20080219 00048 NM 2008 2 19 HALA0800052 1 20080110 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 641 S2L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LIGHTING STRIKE ON A/C CROWN AT LOCATION, STA 641,S2L. REPAIRED IAW 767-300, SRM 53-00-01, REPAIR 8. 2 L 7 2 4F RT A1NM 2008030300039 20080303 00039 EU 2008 3 3 08FDEA00647 1 20080228 A 2560 A2562002800160Y ESCAPE ROPE AIRBUS 300 A300F4605R 3930327 EU ZONE 200 NONE A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 684FE 802 F/O ESCAPE ROPE IS STILL IN THE PLASTIC PACKAGING. REMOVED PLASTIC PACKAGING AS REQUIRED. REF FEDEX STANDARD MAINTENAN CE PRACTICES. 2 L 7 2 4F RT A35EU 2008021900049 20080219 00049 NM 2008 2 19 HALA0800053 1 20080110 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 654 S2L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LIGHTING STRIKE ON A/C CROWN AT LOCATION, STA 654 +56, S2L. REPAIED IAW 767-300, SRM 53-00-01, REPAIR 8. 2 L 7 2 4F RT A1NM 2008021900050 20080219 00050 NM 2008 2 19 CALA0800097 1 20080130 A 5313 65617777 STRINGER BOEING 737 7373T0 1384582 NM BS 360 S15L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FORWARD ENTRY STRINGER 15L AT STA 360 IS CRACKED AT FASTENER HOLES. REMOVED AND REPLACED PER ECRA 5311-01392. 2 L 7 2 4F RT A16WE 2008021900052 20080219 00052 NM 2008 2 19 AALA200800198 1 20080129 A 5101 SKIN BOEING 767 767223 1385123 NM NONE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 324AA 22325 AFW - FUSELAGE SKIN AT STATION 1582 HAD A TEMPORARY REPAIR. AREA OF DISCREPANCY IS 3.8 INCH BY 2.7 INCH. ACCOMPLISHED PERMANENT REPAIR FOR FUSELAGE SKIN AT STATION 1582 STRINGER 25L. 2 L 7 2 4F RT A1NM 2008021900060 20080219 00060 NM 2008 2 19 AALA200800217 1 20080130 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EXTERIOR EMERGENCY LIGHT AT R3 DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EXTERIOR EMERGENCY LIGHT AT R3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900062 20080219 00062 NM 2008 2 19 CALA0800116 1 20080212 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM BS 827 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 FRAME CRACKED AT STA 827 ABOVE STRINGER 9R. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04710. 2 L 7 2 4F RT A16WE 2008021900064 20080219 00064 NM 2008 2 19 CALA0800118 1 20080212 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM BS 907 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 FRAME CRACKED AT STA 907 ABOVE STRINGER 9L. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04714. 2 L 7 2 4F RT A16WE 2008021900069 20080219 00069 NM 2008 2 19 CALA0800121 1 20080212 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM BS 747 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 FRAME CRACKED AT STA 747 ABOVE STRINGER 9L. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04714. 2 L 7 2 4F RT A16WE 2008021900074 20080219 00074 NM 2008 2 19 CALA0800126 1 20080212 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 787 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 FRAME CRACKED AT STA 787 ABOVE STRINGER 9R. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04714. 2 L 7 2 4F RT A16WE 2008021900077 20080219 00077 NM 2008 2 19 CALA0800106 1 20080131 A 5340 6916970501 ATTACH ANGLE BOEING 737 7373T0 1384582 NM BS 350 S15L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14335 23573 ATTACH ANGLE CRACKED AT STA350 STRINGER 15L AFT SIDE OF L-1 DOOR. REMOVED AND REPLACED ANGLE PER SRM 51-40-02 AND EA 35 4-53-002 CAL REV 2. 2 L 7 2 4F RT A16WE 2008021900084 20080219 00084 NM 2008 2 19 HALA0800058 1 20080110 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 873 S2L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LIGHTING STRIKE ON A/C CROWN AT LOCATION, STA 873, S2L. REPAIRED IAW 767-300, SRM 53-00-01, REPAIR 8. 2 L 7 2 4F RT A1NM 2008021900085 20080219 00085 NM 2008 2 19 HALA0800059 1 20080110 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 955 S2L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LIGHTING STRIKE ON A/C CROWN AT LOCATION, STA 955, S2L. REPAIRED IAW 767-300, SRM 53-00-01, REPAIR 8. 2 L 7 2 4F RT A1NM 2008021900092 20080219 00092 SO 2008 2 19 RAIA00802010 1 20080207 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BROKEN A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 816HK 145055 PRE FLT NR 5511 - STL - EMERGENCY LIGHT AT FLOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CONNECTOR TO THE SUB JECT LIGHT. OPERATIONAL CHECKED GOOD WITH NO OTHER DEFECTS. 2 L 7 2 4T RT T00011AT 2008021900094 20080219 00094 WP 2008 2 19 IXXA08SMN068S 1 20080208 A 5753 DRIVE LINK DOUG DC8 DC873F 302199F WP TE FLAPS BENT B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LINK AT FLAP DRIVE LINK BENT AT STATION 3.000. REMOVED AND REPLACED LEFT WING FLAP DRIVE LINK IAW DC8 MAINTENANCE MANUAL 20-16-0 PAGE 202. PERFORMED OPS CHECK TO ALL FLIGHT CONTROLS. OPE RATIONAL CHECK GOOD IAW DC8 MAINTENANCE MANUAL 27-11-0 PAGE 10-14, DC8 27-21-0 PAGE 5-9. DC8 27-30-0 PAGE 4-7, DC8 27-40 -0 PAGE 1-2. DC8 27-41-0 PAGE 10-13, DC8 27-51-0 PAGE 11-12, DC8 27-61-0 PAGE 5-7, DC8 27-70-0 PAGE 1-2 DC8 27-80-0 PAGE 4. 2 L 7 4 4F RT 4A25 2008021900096 20080219 00096 WP 2008 2 19 G60A200800020 1 20080208 A 5730 SKIN DOUG DC10 DC1030F 3023504 WP LT WING CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 607GC 46978 LT WING TIP TOP SIDE OUTBD AFT END SKIN CRACKED APPROX 5". 2 L 7 3 4F RT A22WE 2008021900106 20080219 00106 NM 2008 2 19 AALA200800207 1 20080130 A 3097 CWC011210 CONNECTOR BOEING 757 757223 1384957 NM WINDSHIELD HEAT FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 624AA 24582 PBI INFLIGHT T1738/30JAN SJU TO PHL - CREW REPORTED SMOKE IN COCKPIT AND SMOKE ODOR IN CABIN. FIRST OFFICERS WINDSHIE LD SHATTERED. LANDED PBI WITHOUT INCIDENT. REPLACED FIRST OFFICERS WINDSHIELD AND WINDSHIELD HEAT CONNECTOR. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008021900111 20080219 00111 NM 2008 2 19 AALA200800224 1 20080131 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 772AN 29580 DFW - EMERGENCY LIGHT AT SEAT 40G MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 40G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900116 20080219 00116 SW 2008 2 19 WGEA200800026 1 20080206 A 3246 M16901 TIRE ECLIPS EA500 ECLIPSEEA500 3350000 SW MLG FAILED E WGEA O OTHER O OTHER LD LANDING 1 EA 27 162DJ 50 000079 NUMBER 1 TIRE FLAT ON LANDING. REMOVED NR 1 WHEEL ASSEMBLY AND INSTALLED A SERVICEABLE WHEEL ASSEMBLY IAW EA500 AMM 32- 42-00. 1 L 7 2 4J RT A00002AC 2008021900119 20080219 00119 EA 2008 2 19 MASA200800130 1 20080212 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 502MJ 10050 ASH FLT 7287 CLT-ORD - ROW 12 EMERGENCY STRIP NOT SECURED. MX RE-SECURED. 2 L 7 2 4F RT A21EA 2008021500024 20080215 00024 EA 2008 2 15 TRAX200800199 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 379-477 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 RT SIDEWALL SEAT RAIL FS 379.0 TO FS 477.40 HAS CORROSION DAMAGE. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW C RJ 700 SRM 53-21-49. APPLIED ALODINE IAW CRJ 700 SRM 51-21-16. 2 L 7 2 4F RT A21EA 2008021500092 20080215 00092 NM 2008 2 15 2008UALA00432 1 20080124 A 3350 1619 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 350UA 24301 EES EXTERIOR LIGHT INOP, JUST AFT OF RT AFT WING TO BODY FAIRING. CLEANED SOCKET AND RELAMPED. 2 L 7 2 4F 4 F RT A16WE E21EU 2008021500100 20080215 00100 NM 2008 2 15 2008UALA00550 1 20080131 A 3350 276005 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE POWER SUPPLY FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY LIGHTS INOP RIGHT OVERWING 2 FWD MOST ASSY' S. REPLACED FUSE AT POWER SUPPLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021500109 20080215 00109 NM 2008 2 15 2008UALA00559 1 20080130 A 3350 1317 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 657UA 27112 FWD LEFT OVERWING EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500150 20080215 00150 NM 2008 2 15 2008UALA00612 1 20080203 A 2560 SMOKE GOGGLES BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT CRACKED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 659UA 27114 CAPTAIN'S SMOKE GOGGLES BROKEN AND CRACKED. REPLACED GOGGLES. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500152 20080215 00152 NM 2008 2 15 2008UALA00614 1 20080202 A 2761 154260015 ACTUATOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE SPOILER SYS FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 671UA 30026 EICAS MSG SPOILERS DISPLAYED. SPOILERS LIGHT ILLUM WITH SPOILERS SELECTED UP. FAULTY POWER CONTROL ACTUATOR. REPLACE D NR 9 PCA PER MM 27-61-02. OPS CHECK GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021500195 20080215 00195 NM 2008 2 15 SWAA080718 1 20080207 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 434WN 32454 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008022500208 20080225 00208 NM 2008 2 25 2008UALA00801 1 20080212 A 3350 1317 LAMP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EEL CEILING LIGHT NEAR SEAT 23A INOPERATIVE. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022500216 20080225 00216 NM 2008 2 25 2008UALA00809 1 20080211 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 WALL EEL INOP: LEFT AFT SIDE NEAR DOOR 1L. RESECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022500234 20080225 00234 NM 2008 2 25 2008UALA00823 1 20080213 A 5753 PANEL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE T/E FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 644UA 25094 RIGHT OUTBOARD FLAP OUTBOARD WRAP AROUND PANEL AT OUTBOARD SIDE UNDER AUX TRACK HAS CRACK. DURING A CHECK FOUND RH OUTB OARD FLAP OUTBOARD FLAP GUIDE BROKEN AND MISSING. SENT LEADING EDGE PANEL 666FT TO SHOP 273 FOR REPAIR. REPLACED RT OU TBOARD FLAP DEFLECTION TRACK REF 27-51-24. REINSTALLED REPAIRED PANEL 666FT. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500244 20080225 00244 NE 2008 2 25 2008UALA00833 2 20080214 A 7200 NUT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 IGV BROKEN A UALA C ABORTED TAKEOFF W INADEQUATE Q C TO TAKEOFF 1 WP 29 668UA 30024 727875 NR 2 ENGINE SLOW TO SPOOL AT TAKEOFF. THIS ENGINE HAD AN N2 OVERSPEED OF 105.6%. THE ENGINE WAS REPLACED AT SFO PRIOR T O FURTHER FLIGHT. THE IGV UNISON RING ADJUSTER ROD END CLEVIS CONNECTOR ON THE BELLCRANK WAS DISCONNECTED DUE TO A BROKE N SLEEVE NUT. (IPC 72-35-00-025-040)BECAUSE THE OVERSPEED EXCEEDED 105.0% FOR 9 SECONDS, ALL STAGE-5, -6, AND-7 BLADE S WILL BE SCRAPPED DUE TO CONCERN OF HIGH CYCLE FATIGUE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500248 20080225 00248 NM 2008 2 25 HNAA0800084 1 20080213 A 2611 3023143 SMOKE WARNING DHAV DHC8 DHC8102 2809003 NM CARGO BAY FALSE ACTIVATION A HNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 07 807EX 292 SMOKE WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL, ABORTED T/O & RETURNED TO GATE. LIGHT EXTINGUISHED. BOTH BAG BAY SMOKE DETECTORS TEST NORM, INSP BOTH BAG BAY SMOKE DET AND WIRING, NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2008022500270 20080225 00270 NM 2008 2 25 2008UALA00219 1 20080113 A 2420 GEAR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE IDG FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 677UA 30029 FOUND NR 1 ENG IDG DELTA P SWITCH POPPED WITH METAL IN FILTER. SUSPECT BEARING OR GEAR FAILURE DUE TO METAL FOUND IN FI LTER. REPLACED NR 1 ENG IDG PER MM 24-11-01, LEAK AND OPS CHECK OK. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500277 20080225 00277 NM 2008 2 25 2008UALA00269 1 20080115 A 7930 21SN04414 SWITCH BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE OIL FILTER MALFUNCTIONED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 664UA 29236 NR 2 ENG OIL FILTER STATUS MSG DISPLAYED AFTER START. THE MAIN OIL FILTER & MAGNETIC CHIP DETECTORS CHECKED OK. REPLACE D THE OIL FILTER DELTA-P SWITCH.PROBLEM DID NOT RECUR. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500279 20080225 00279 NM 2008 2 25 DL757080226 1 20080218 A 5347 SEAT TRACK BOEING 757 757232 1384965 NM COCKPIT CRACKED A DALA O OTHER O OTHER CR CRUISE 1 SO 27 680DA 26956 CAPT SEAT LOOSE DURING FLIGHT. FOUND AFT LEFT SEAT TRACK STOP FITTING CRACKED REPLACED SEAT TRACK. 2 L 7 2 4F RT A2NM 2008022500280 20080225 00280 2008 2 25 2008UALA00372 4 20080123 A 2300 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SATCOM UNKNOWN A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 646UA 25283 RTFL DUE TO SATCOM FAILURE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500282 20080225 00282 NM 2008 2 25 DL764080246 1 20080219 A 2720 RUDDER PEDAL BOEING 767 767432ER 1385134 NM COCKPIT OUT OF ADJUST A DALA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 27 832MH 29704 DURING FLT CONTROL CHECK, F/O RT RUDDER PEDAL HITS THE AFT STOP COVER. RTB ADJ RUDDER PEDALS TO NML CONFIG. RAN PEDALS FULL LT AND RT PEDAL DOES NOT HIT THE SHROUD. PEDALS ARE EVEN ALL POS AND IND NML. 2 L 7 2 4F RT A1NM 2008011400073 20080114 00073 EA 2008 1 14 N6WA0080101 1 20080103 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE EMERGENCY LIGHTS BURNED OUT A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 155GJ 10225 EMERGENCY LIGHT INOP AT LOWER AFT INSIDE OF SERVICE DOOR. REPLACED BULB OPS OK. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008011400080 20080114 00080 CE 2008 1 14 DXTA200802745 1 20080103 A 3297 CONNECTOR CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE MLG DIRTY E DXTA O OTHER N FALSE WARNING LD LANDING 1 GL 07 644QS 5605582 SELECTED GEAR DOWN AND RECEIVED A DOWN INDICATION FOR RT MAIN AND NOSE ONLY. RED UNLOCK LIGHT ILLUMINATED ACCOMPANIED WI TH NO LT MAIN INDICATION. SERVICED GEAR BLOW DOWN BOTTLE AND SAFETIED AS REQUIRED. BLEED MLG HYD SYSTEM. T/S LANDING GE AR SYSTEM. CLEANED LT MLG DOWNLOCK SWITCH CONNECTOR. SWUNG GEAR OVER 16 CYCLES WITH NO ISSUES. FROZE DOWNLOCK SWITCH MUL TIPLE TIMES WITH FREEZE SPRAY, SWUNG GEAR WITH NO FAILURES OF LANDING GEAR SYSTEM/ OPS CHECK GOOD. IAW CE 560 XLS M/M 12 -13-01 AND 32-30-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008011400081 20080114 00081 CE 2008 1 14 DXTA200802744 1 20080103 A 3231 SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG DOOR MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 896QS 258640 AFTER T/O AND GEAR RETRACTION THE RT MAIN GEAR (RED) LIGHT REMAINED ILLUMINATED. REPLACED RT MLG DOOR UP SWITCH WITH NE W P/N 1EN1-14N119, PERFORMED SATISFACTORY OPS CHECK. IAW MM 32-40-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2008011400091 20080114 00091 SW 2008 1 14 DUFA20080002 1 20080103 A 2613 434422122 OVERHEAT SENSOR SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT NACELLE DEFECTIVE E DUFA O OTHER N FALSE WARNING CL CLIMB 1 GL 27 3116N AC596 WHILE ON CLIMB OUT, THE PILOT NOTICED THAT THE RT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWING PROCEDURE, THE LT GENERATOR WAS SHUTDOWN, BLEED AIR TURNED OFF AND THE LANDING GEAR EXTENDED. AFTER APPROXIMATELY ONE MINUTE THE LIGHT EXTINGUISHED . THE FLIGHT CONTINUED WITHOUT ANY PROBLEMS. UPON INVESTIGATION, NO EVIDENCE OF FIRE OR OVERHEATING COULD FOUND IN THE W ING AND GEAR WELL AREAS. IT IS SUSPECTED THAT DUE TO HIGH WINDS DURING THE PILOT’S BACK TAXI TO THE ACTIVE RUNWAY, HE MA Y HAVE HAD TO APPLY CONSTANT BRAKE PRESSURE TO KEEP HIS TAXI SPEED LOW. THIS WOULD HAVE CAUSED EXCESSIVE HEATING OF THE BRAKE ASSEMBLY AND ONCE THE GEAR WAS RETRACTED, CAUSED THE WING OVERHEAT LIGHT TO COME ON. IT WAS ALSO REPORTED THAT THE 2 L 7 2 4T 4 T RT A8SW E4WE 2008021500202 20080215 00202 NM 2008 2 15 SWAA080725 1 20080207 A 5512 182A4001 SKIN BOEING 737 73776Q 13845AA NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 551WN 30280 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147.90. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008021500204 20080215 00204 NM 2008 2 15 SWAA080727 1 20080207 A 5512 182A4001 SKIN BOEING 737 73776Q 13845AA NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 551WN 30280 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 147.90 AND STA 157.10. REPAIR ED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008021500211 20080215 00211 NM 2008 2 15 2008UALA00332 1 20080118 A 2560 233N31011 PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT SHORTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 528UA 25018 EVACUATION COMMAND - SIGNAL IN COCKPIT OVERHEAD PNL HAS DARK AREAS. ELECTRICAL SHORTING ON PANEL ITSELF. REPLACED COCK PIT EVAC PANEL, NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021900026 20080219 00026 NM 2008 2 19 2008UALA00635 1 20080202 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 SEAT EEL INOP ROW 38L. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021900028 20080219 00028 NM 2008 2 19 2008UALA00637 1 20080202 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY EXIT LIGHT INOP DOOR3L SLIDE ILLUM. REPLACED LAMP ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021900034 20080219 00034 NM 2008 2 19 2008UALA00655 1 20080205 A 8011 35054367 STARTER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 1 ENGINE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 675UA 29243 NR 1 ENGINE STARTER FAILED. REPLACED STARTER AND STARTER START VALVE PER MM 80-11-01 & MM 80-11-02. ACP ENG RUN CHECKS OK. NO LEAKS FOUND. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021900045 20080219 00045 NM 2008 2 19 HALA0800050 1 20080110 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 553 S2L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LIGHTING STRIKE ON A/C CROWN AT LOCATION, STA 553, S2L. REPAIRED IAW 767-300, SRM 53-00-01, REPAIR 8. 2 L 7 2 4F RT A1NM 2008021900059 20080219 00059 NM 2008 2 19 AALA200800202 1 20080129 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 796AN 30796 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900061 20080219 00061 NM 2008 2 19 AALA200800221 1 20080131 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 JFK - EMERGENCY LIGHT AT SEAT 37C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 37C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900063 20080219 00063 NM 2008 2 19 CALA0800117 1 20080212 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM BS 827 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 FRAME CRACKED AT STA 827 ABOVE STRINGER 9L. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04710. 2 L 7 2 4F RT A16WE 2008021900066 20080219 00066 NM 2008 2 19 2008UALA00668 1 20080205 A 5320 STIFFENER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 665UA 29237 BS 246 AT LBL 26.39 STIFFENER IS CRACKED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021900075 20080219 00075 NM 2008 2 19 CALA0800127 1 20080212 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM BS 747 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 FRAME CRACKED AT STA 747 ABOVE 9R. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04714. 2 L 7 2 4F RT A16WE 2008021900095 20080219 00095 WP 2008 2 19 IXXA08SMN069S 1 20080208 A 5753 LINK DOUG DC8 DC873F 302199F WP TE FLAPS CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 604BX 87931 2957 46046 DURING ROUTINE C CHECK INSPECTION, FOUND FLAP MECHANISM OF INNER WING FORWARD LINK CRACKED AT STATION 3.000 RIGHT. REMO VED REPLACED INNER WING FORWARD LINK OF FLAP MECHANISM IAW OHM 27-27-1 PAGE 4. PERFORMED OPS CHECK TO ALL FLIGHT CONTRO LS. GOOD IAW DC8 MAINTENANCE MANUAL 27-11-0 PAGE 10-14, DC8 27-21-0 PAGE 5-9. DC8 27-30-0 PAGE 4-7, DC8 27-40-0 PAGE 1- 2 DC8 27-41-0 PAGE 10-13, DC8 27-51-0 PAGE 11-12, DC8 27-61-0 PAGE 5-7, DC8 27-70-0 PAGE 1-2 DC8 27-80-0 PAGE 4. 2 L 7 4 4F RT 4A25 2008021900104 20080219 00104 NM 2008 2 19 AALA200800226 1 20080131 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 772AN 29580 DFW - EMERGENCY LIGHT AT SEAT 26G MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900105 20080219 00105 NM 2008 2 19 AALA200800206 1 20080130 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 696AN 26976 MIA - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT NUMBER O NE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008011400095 20080114 00095 EU 2008 1 14 QMLA010208001 1 20080102 A 2120 UNKNOWN BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101* NE ODOR E QMLA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 138HH 7060 SHORTLY AFTER TAKEOFF, MED CREW SAID THEY COULD DETECT A FUEL TYPE ODOR THAT WAS FAIRLY STRONG. THE PILOT ABORTED THE F LIGHT AND LANDED AT DEPARTURE. AIRCRAFT WAS SHUTDOWN. THE PILOT CHECKED ENGINE COMPARTMENTS FOR FUEL AND CHECKED UNDER DRAIN LINES FOR FUEL. NONE WAS FOUND AND NO ODOR OF FUEL WAS DETECTED IN THE AIRCRAFT. AIRCRAFT WAS REFUELED AND THE MISSION WAS COMPLETED WITHOUT FURTHER INCIDENT. MAINTENANCE ALSO CHECKED AIRCRAFT FOR CAUSE OF ODOR, AND FOUND NONE, BE LIEVED THAT IT WAS THE LAST FUELING OF AIRCRAFT. 1 G 7 2 3U 3 U H13EU E5NE 2008011400118 20080114 00118 WP 2008 1 14 08FDEA00030 1 20080104 A 3230 ARG70255527 RETRACT CYLINDER DOUG MD10 MD1010F 3022112 WP ZONE 700 LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 363FE 48263 HYD SYS QTY SLOW LEAK 0.1 GAL. PER 3 MIN GOT HYD 3 ELEV OFF AND HYD SYS 3 LOW LANDED DEN WITHOUT INCIDENT. RT MAIN GEA R RETRACT CYL LEAKING, SPARES NOT IN PLACE, NEEDS NEW ACTUATOR, OR GEAR DOWN FLT, ACT NIS DEN. REMOVED RETRACT CYLINDER PER MM 32-33-01-4. REPLACED MLG RETRACT CYLINDER PER AMM-32-33-01-4. LEAK CK, OPS CHECK SAME. OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2008011100064 20080111 00064 NM 2008 1 11 2008UALA0023 1 20080101 A 2612 FIRE LOOP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 3 ENGINE FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 195UA 26899 THE 'ENG 3 FIRE LP B' EICAS STATUS MSG DISPLAYED. ENG 3 FIRE LOOP-B FIRE OR FAULT OUTPUT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011100112 20080111 00112 NM 2008 1 11 SWAA080116 1 20080103 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 415 TO BS 429, STR 1. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011100160 20080111 00160 NM 2008 1 11 SWAA080151 1 20080106 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008011100173 20080111 00173 NM 2008 1 11 SWAA080152 1 20080106 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011100180 20080111 00180 NM 2008 1 11 SWAA080158 1 20080106 A 3397 D3790 CONNECTOR BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED BRDG CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT CONNECTOR BROKEN. REPAIRED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 2008011100195 20080111 00195 NM 2008 1 11 SWAA080149 1 20080103 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740E, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011100212 20080111 00212 EA 2008 1 11 COMA0860008 1 20080101 A 2752 854D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 924CA 564 7026 FLIGHT 5682 - RECEIVED FLAP FAIL CAUTION AND STALL FAIL CAUTION MESSAGES. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED RIGHT NR 4 FLAP ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011100245 20080111 00245 EA 2008 1 11 COMA0860023 1 20080102 A 2752 1104SD100501 FLEX DRIVE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 675BR 7635 FLIGHT 5391- RECEIVED FLAP FAIL MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LEFT SIDE NR 5 FLAP FLE X DRIVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011400048 20080114 00048 NM 2008 1 14 DXTA200802747 1 20080104 A 3260 SQUAT SWITCH GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 GL 07 749QS 165 GROUND AIR BRAKES DEPLOYED ON FINAL APPROACH WHEN THE SWITCH WAS ARMED. R & R LT MLG WOW SWITCH AND HARNESS IAW AMM 32- 60-05. OPERATIONAL & FUNCTIONAL CHECK GOOD WITH NO FURTHER DEFECTS NOTED. 2 L 7 2 4F 4 F RT A53NM E35NE 2008011400083 20080114 00083 CE 2008 1 14 DXTA200802742 1 20080103 A 3260 UPLOCK BEECH MU300 400A 1155402 CE MLG OUT OF ADJUST E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 138QS RK492 LANDING GEAR IN TRANSIT / UNSAFE LIGHT WOULD NOT EXTINGUISH AFTER LANDING GEAR RETREACTION. ACCESSED CONNECTORS P271 A ND P272. OHMED OUT DOOR CLOSED SWITCH & UPLOCK SWITCH PER WDM 32-61-01-02 NO DEFECTS NOTED. JACKED ACFT & INSTALLED HYDR AULIC MULE. ACCOMPLISHED MLG FUNCTIONAL TEST/PREOPS CHECKS. ON PERFORMING PREOPS CHECKS AT 950 PSI & 2.0 GPM EXPERIENCED AN UNSAFE HANDLE INDICATION WITH BOTH MLG DOORS OPEN. DROPPED HYDRAULIC PRESSURE TO ZERO & NOTED NLG AND RT MLG GEAR DR OP OUT OF WELL. CHECKED & ADJUSTED NLG UPLOCK & RT MLG UPLOCK PER MM 32-20-00 & 32-30-00. REPEATED PREOPS CHECKS AT 950 PSI & 2.0 GPM SEVERAL TIMES, NO FAULTS INDICATED. ACCOMPLISHED OPS CHECKS. SERVICED RESERVOIR. 2 H 7 2 4F RT A16SW 2008011500186 20080115 00186 SO 2008 1 15 C2XA08ON059 1 20080104 A 2750 FLAP EMB 145 EMB145LR 3260212 SO WING MALFUNCTIONED A C2XA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 27 14907 14500468 FLT 0431 - SAN TO SAN - FLIGHT CREW AIR RETURN DUE TO SEVERE TURBULENCE ENCOUNTERED IN FLIGHT AND FLAP OVERSPEED AT 9 DE GREES, SPEED 252KIAS. A/C RETURN TO BLOCK SAFELY WITHOUT INCIDENT. SAN MX PERSONNEL INSPECTED THE A/C FOR SEVERE TURBU LENCE AND FLAP OVERSPEED AND FOUND NO ISSUES WITH THE AIRCRAFT, OPERATIONALLY CHECKED GOOD AND A/C WAS RELEASED TO RETUR N FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008011500196 20080115 00196 NM 2008 1 15 CALA0800003 1 20080104 A 5340 6935352U14 STRINGER CLIP BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 CLIP CRACKED AT STA 597, S8L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008011500215 20080115 00215 NM 2008 1 15 CALA0800008 1 20080107 A 5311 6546539 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FUSELAGE FRAME IS CRACKED AT STA 616 BETWEEN S7L AND S8L. REPAIRED PER SRM 53-00-07 FIG 201. 2 L 7 2 4F RT A16WE 2008011500229 20080115 00229 NM 2008 1 15 CALA0800010 1 20080108 A 5347 6546816 SEAT TRACK BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 RIGHT O/B SEAT TRACK CORRODED STA 887 TO 927. FABRICATED AND INSTALLED NEW SEAT TRACK SECTION PER SRM 53-00-02 REPAIR 3 . 2 L 7 2 4F RT A16WE 2008011500281 20080115 00281 2008 1 15 R61A200800001 4 20080101 A 2565 4A40304 SLIDE EMB ERJ170 ERJ170100SU 3260403 NM L1 DOOR DEFLATED A R61A K NONE O OTHER IN INSP/MAINT 1 GL 11 829MD 1345 17000049 DURING A SCHEDULE MAINTENANCE CHECK, MAINTENANCE DEPLOYED L1 DOOR SLIDE. SLIDE DEPLOYED CORRECTLY THEN DEFLATED AFTER D EPLOYMENT. MAINTENANCE REMOVED AND REPLACED L1 DOOR SLIDE. 2 L 7 2 4F RT A56NM 2008011500283 20080115 00283 NM 2008 1 15 UPS08451380 1 20080105 A 3350 SIGN BOEING 747 747200 1384847 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:N/A EXIT SIGN, LT & FWD OF UPPER DECK RT DOOR INOP. PREVIOUSLY DEACTIVITED, APPLIED DEACTIVATED PLACARD PER EO B747-3350-15296-B. 2 L 7 4 4F RT A20WE 2008011500292 20080115 00292 NM 2008 1 15 ASAA0852455 1 20080106 A 4970 WARNING SYSTEM BOEING 737 737890 1384527 NM APU MALFUNCTIONED A ASAA K NONE N FALSE WARNING UK UNKNOWN 1 NM 02 585AS 35683 APU "MAINT" LIGHT ILLUMINATED. PERFORMED FIM 49 60 TASK 801. OP CHECKS GOOD FAULT CLEARED. NO HISTORY. OIL QTY FULL. 2 L 7 2 4F RT A16WE 2008011500299 20080115 00299 NM 2008 1 15 ASAA0872459 1 20080108 A 5347 453A261121 SCUFF PLATE BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 649AS 30663 AFT CARGO COMPARTMENT FWD TIE DOWN CORRODED. REMOVED CORROSION IAW B737 SRM 53-00-53 FIG 103 PG 110. CORROSION FOUND T O BE OUT OF LIMITS IAW B737 SRM 53-00-53 FIG 103 PG 110. FABRICATED NEW SCUFF PLATE IAW B737 SRM 51-30-01 PG 22, 23 & 2 4. 2 L 7 2 4F RT A16WE 2008011500310 20080115 00310 2008 1 15 SWAA080167 4 20080107 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008011500314 20080115 00314 NE 2008 1 15 ABXA080004 2 20080104 A 7200 JT8D11 ENGINE DOUG DC9 DC941 302207N WP PWA JT8 JT8D11 52044 NE LEFT MALFUNCTIONED A ABXA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 GL 23 974AX 42609 47623 667094 LOST LEFT ENGINE OIL QUANTITY AND PRESSURE. SECURED ENGINE IN FLIGHT. REPLACED LEFT ENGINE IAW DC9 ENGINE CHANGE CARD 9090010. 2 L 7 2 4F 4 F A6WE E2EA 2008011500315 20080115 00315 WP 2008 1 15 ABXA080005 1 20080105 A 3260 DOWNLOCK SWITCH DOUG DC9 DC941 302207N WP NLG FAULTY A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 979AX 47492 ON 1ST LANDING GEAR EXTENSION, NOSE GEAR LIGHT DID NOT ILLUMINATE, RED LIGHT WENT OUT. RECYCLED LANDING GEAR, NOSE LIGH T ILLUMINATED ON 2ND EXTENSION. REPLACED NOSE GEAR DOWNLOCK SWITCH IAW DC9 AMM 32-60-01-2. 2 L 7 2 4F A6WE 2008011500320 20080115 00320 SO 2008 1 15 C2XA08ON062 1 20080105 A 2612 902081 CONTROL MODULE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL FIRE DETECTION MALFUNCTIONED A C2XA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 27 13161 12626 12626 14500805 CAE312760 FLT 22 - ONT - FLIGHT CREW REPORTED ENG 2 FIRE DETECTION FAIL MSG ON EICAS. AIRCRAFT RETURNED TO BLOCK WHERE IT LANDED SAFELY AND NO EMERGENCY WAS DECLARED. MX REMOVED AND REPLACED RT FIRE DETECTION CONTROL MODULE, OPERATIONALLY CHECK SAT ISFACTORY AND AIRCRAFT WAS RETURNED FOR SERVICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4F 4 F RT TE6CH 2008011500321 20080115 00321 SO 2008 1 15 C2XA08ON063 1 20080107 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13908 14500465 ONT OVERNIGHT MX - WHILE PERFORMING OPERATIONAL CHECK ON EMERGENCY LIGHTING SYSTEM MX FOUND EMERGENCY EXIT LIGHTS WILL N OT ILLUMINATE FROM 8ABC TO 14ABC INCLUDING EXIT HATCH LIGHTING. MX PERSONNEL FOUND CONNECTOR LOOSE AND RE-TIGHTEN CONNE CTOR AT SEAT 12A BATTERY SUPPLY, PERFORMED OPS CHECKS ON EMERGENCY LIGHTING IAW EMB 145 AMM 33-50-00, OP'S CHECKS SATISF ACTORY. A/C WAS RETURNED FOR SERVICE IN AIRWORTHY CONDITIONS. 2 L 7 2 4T RT T00011AT 2008011500324 20080115 00324 SO 2008 1 15 C2XA08IA010 1 20080105 A 2611 SMOKE WARNING EMB 145 EMB145XR 3260214 SO CARGO BAY MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 11119 145677 IAH - FLIGHT 2208, THE CREW REPORTED A BAGGAGE SMOKE INDICATION AFTER THE RECIRC FAN CIRCUIT BREAKER POPPED. THE AIRCRA FT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND PLACED THE RECIRC FAN ON M EL 21-22-06 CAT CCTL 136433, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 01/07/07, THE AIRCRAFT RON'D IN SH V WHERE MAINTENANCE OPERATIONALLY CHECKED THE BAGGAGE COMPARTMENT VENTILATION SYSTEM WITH NO DEFECTS, REMOVED THE MEL, A ND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008011500325 20080115 00325 SO 2008 1 15 C2XA08IA009 1 20080107 A 2611 SMOKE WARNING EMB 145 EMB145XR 3260214 SO CARGO BAY ACTIVATED A C2XA O OTHER N FALSE WARNING UK UNKNOWN 1 SW 27 13123 145688 CME - FLIGHT 2021 THE CREW REPORTED A BAGGAGE SMOKE INDICATION ON EICAS AND THE BAGGAGE EXTINGUISHER BUTTON WAS ILLUMINA TED. THE AIRCRAFT WAS PLACED ON MEL 21-22-06 CTL 136538 CAT C, AND RELEASED FOR SERVICE. THE AIRCRAFT CAME TO IAH ON F LIGHT 2021 WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE BAGGAGE SMOKE DETECTORS SYSTEM WITH NO DE FECTS NOTED, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008011500330 20080115 00330 SO 2008 1 15 C2XA08IA015 1 20080107 A 3350 M835366022M RELAY EMB 145 EMB145XR 3260214 SO COCKPIT INOPERATIVE A C2XA K NONE J WARNING INDICATION UK UNKNOWN 1 SW 27 12160 145799 IAH - FLIGHT 2785, THE CREW REPORTED RECEIVING AN "EMERGENCY LIGHTS NOT ARMED" MESSAGE IN FLIGHT. THE AIRCRAFT LANDED A T IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED RELAY K0097, OPERATIONALLY CHECKED WITH NO DEFECTS, AND TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008011100192 20080111 00192 NM 2008 1 11 SWAA080146 1 20080106 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011100216 20080111 00216 EA 2008 1 11 COMA0860012 1 20080101 A 5315 601R311135758 ATTACH BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 447CA 7552 DURING HMV3 INSPECTION FOUND LONGITUDINAL FLOORBEAM ATTACH BRACKETS CRACKED AT AFT SIDE. REMOVED AND REPLACED DAMAGED B RACKETS. 2 L 7 2 4F RT A21EA 2008011100277 20080111 00277 NM 2008 1 11 HALA0800003 1 20080103 A 2612 CIRCUIT CARD BOEING 767 7673G5 1385126 NM FIRE DETECTION NOT SEATED A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, APU FIRE LOOP 2 EICAS MESSAGE. TROUBLESHOT PER FIM 26-15-00 FIGURE 103. RESEATED NR 2 FIRE D ETECTOR CARD. SYSTEM NOW TESTS OK. OK PER FIM. 2 L 7 2 4F RT A1NM 2008011100281 20080111 00281 NM 2008 1 11 08FDEA00028 1 20080103 A 3221 ACA7017501 TRUNNION DOUG MD11 MD11F 3023600 NM NLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 583FE 48421 NOSE LANDING GEAR LEFT TRUNNION FITTING SUSPECT CRACKED. REPAIR CARRIED OUT AS PER SRM 53-40-00 FIGURE 23 VOLUME I AND FEDEX EA 1-5340-117249. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008011400014 20080114 00014 2008 1 14 COEA0801816 4 20080107 A 3440 959960714562 TRANSCEIVER AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE ALTIMETER FAILED A COEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 13 816FX 347 AIR TURN BACK. FLT NR 8663, CREW RECEIVED A LEVEL 3 CAP ALERT LANDING GEAR NOT DOWN FOLLOWED BY A STICK PUSHER/ STICK S HAKER FAULT, TERRAIN ALERT WARNING SYS (TAWS) WARNING, RADIO ALTIMETER WENT TO 0. CREW ELECTED TO RETURN TO DEPARTURE, AIRCRAFT LANDED NORMALY AND SAFELY. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008011400017 20080114 00017 WP 2008 1 14 AMTA200800005 1 20080102 A 3350 D71701100 BATTERY LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE EMERGENCY LIGHTS UNSERVICEABLE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 163AT 1229 L1 DOOR INT AND EXT EGRESS LIGHTS FAIL TO ILLUM. REMOVED AND REPLACED L1 DOOR INT AND EXT EGRESS LIGHT BATT PACK. CKS G OOD IAW AMM 33-51-06. 2 L 7 3 4F 4 F A23WE E12EU 2008011500019 20080115 00019 NM 2008 1 15 2008UALA0038 1 20080102 A 5320 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FWD GALLEY DOOR CUTOUT INTERCOSTAL ANGLE CRACKED BETWEEN BS 277 & 294.5 AND BETWEEN STRINGERS 10R & 11R. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011500023 20080115 00023 2008 1 15 2008UALA0042 4 20080102 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR INOPERATIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 526UA 24994 SLIDE LEFT DOOR 2R INOPERATIVE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008011500028 20080115 00028 NM 2008 1 15 2008UALA0047 1 20080103 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHTS INOP: COCKPIT CEILING, CEILING ROW 12, ROW 46 RT CEILING & ROW 46 LT CEILING. 2 L 7 4 4F 4 F RT A20WE E24NE 2008011500033 20080115 00033 EU 2008 1 15 YENA2008001 1 20080101 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 608JB 5271 5147 2415 REAR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED AFT CABIN EPSU POWER SUPPLY (13WL) PER AMM 33-51-38-04. OPS CHECKS OK . 2 L 7 2 4F RT A28NM 2008011500178 20080115 00178 SO 2008 1 15 C2XA08IA008 1 20080102 A 3350 7287580503 LIGHT EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15941 145035 IAH - DURING MAINTENANCE INSPECTION EMERGENCY FLOOR LIGHT STRIP NR 6 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008011500181 20080115 00181 GL 2008 1 15 C2XA08IA003 2 20080102 A 7200 AE3007A1E ENGINE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL RIGHT LEAKING A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 11121 14243 14243 145683 CAE312326 DFW - FLIGHT 3130, THE CREW REPORTED A LOSS OF OIL PRESSURE AND QTY ON THE NUMBER TWO ENGINE DURING CRUISE. THE NUMBER TWO ENGINE WAS SHUT DOWN AS A PRECAUTION, AND THE AIRCRAFT DIVERTED TO DFW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANC E REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2008011500204 20080115 00204 EU 2008 1 15 08FDEA00039 1 20080105 A 5347 A5381206720100 SEAT TRACK AIRBUS 300 A300B4622 3930401 EU ZONE 200 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 LT TRACK Y1456 FR50, AFTER REMOVAL OF WEB, FOUND 1 LINK TRACK WITH BENT TAB ON I/B SIDE. REMOVED AND REPLACED SUPPORT L INK BRACKET, LT TRACK Y1456 FR50 IAW A300-600 SRM 51-41-21. 2 L 7 2 4F RT A35EU 2008011500241 20080115 00241 NM 2008 1 15 CALA0800013 1 20080109 A 3350 8100037901 LIGHT BOEING 737 737924 13848A1 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 30401 30118 LEFT FORWARD OVERWING EMERGENCY LIGHT WOULD NOT TEST ON. REPLACED LAMP, TEST OK. 2 L 7 2 4F RT A16WE 2008011500290 20080115 00290 NM 2008 1 15 UPS08M51379 1 20080105 A 2560 SIGN DOUG MD11 MD11F 3023600 NM COCKPIT BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:N/A EMERGENCY EXIT SIGN BROKEN. REINSTALLED EMERGENCY EXIT SIGN. 2 L 7 3 4F RT A22WE 2008011500352 20080115 00352 NM 2008 1 15 SWAA080159 1 20080107 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011500358 20080115 00358 NM 2008 1 15 SWAA080164 1 20080107 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 13R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008011600005 20080116 00005 NM 2008 1 16 SWAA080175 1 20080107 A 5311 6546555 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600035 20080116 00035 NM 2008 1 16 SWAA080229 1 20080110 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER 9L CRACKED AT BS 727B. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008011600055 20080116 00055 NM 2008 1 16 SWAA080233 1 20080110 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731E, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008011600056 20080116 00056 NM 2008 1 16 SWAA080234 1 20080110 A 5751 SM45E1501 BEARING BOEING 737 7373H4 1384600 NM RT AILERON WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED 14Y CHECK, RT WING AILERON FAILED FREE PLAY CHECK. REMOVED AND REPLACED CONTROL ROD BEARING PER MM. 2 L 7 2 4F RT A16WE 2008011600057 20080116 00057 NM 2008 1 16 SWAA080235 1 20080110 A 5752 6546455 SKIN BOEING 737 7373H4 1384600 NM AILERON TAB DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED 14Y CHECK, FOUND RT WING AILERON TAB DELAMINATED AT UPPER SURFACE T/E. REMOVED AND REPLACED TAB PER MM . 2 L 7 2 4F RT A16WE 2008011500016 20080115 00016 NM 2008 1 15 2008UALA0035 1 20080102 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 383UA 24658 DOOR 1L CUTOUT - UPPER DOOR HINGE CUTOUT CRACKED AT AFT EDGE OF FUSELAGE SKIN BEAR STRAP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011500035 20080115 00035 NM 2008 1 15 WRLA2008001 1 20080102 A 5245 SKIN DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE A/C BAY DOOR CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 277WA 48743 DURING C-CHECK INSPECTION FOUND CRACK ON RIGHT FWD AIR CONDITION COMPARTMENT DOOR OUTER SKIN UPPER EDGE APPROX 4.5 INCHE S. REPAIRED PER MD-11 SRM 52-10-00 VOL.I REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2008011500187 20080115 00187 SO 2008 1 15 C2XA08ON060 1 20080105 A 2840 INDICATION SYS EMB 145 EMB145LR 3260212 SO FUEL SYSTEM MALFUNCTIONED A C2XA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 27 14570 14500632 FLT 7823 - GEG TO LAX - FLIGHT CREW REPORTED ATO NR 2 FUEL QTY INDICATION CHANGED VALUE AND GAVE FUEL IMBALANCE MSG WHEN THRUST LEVERS ADVANCED. AFTER RETURNING TO BLOCK FLIGHT CREW PERFORMED A SYSTEM REST AND RAN UP THE ENGINES AND FOUND NO PROBLEMS. NO W/U AND NO MX ACTION. A/C WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008011500194 20080115 00194 NM 2008 1 15 CALA0800002 1 20080104 A 5340 6935352U14 STRINGER CLIP BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 CLIP CRACKED AT STA 578, S8L. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008011500225 20080115 00225 NM 2008 1 15 WRLA2008008 1 20080107 A 5320 S393210712400 FLOOR SUPPORT DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 277WA 48743 DURING C-CHECK INSPECTION FOUND AFT FUSELAGE FLOOR SUPPORT CORROSION AT STA Y=2007, X= 56.65. REPLACED AFT FLOOR SUPPO RT PER MD11 SRM VOL.II 51-35-01 FIG.1 REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2008011500245 20080115 00245 NM 2008 1 15 WRLA2008009 1 20080110 A 5347 AEA73255 SEAT TRACK DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 277WA 48743 DURING C-CHECK INSPECTION FOUND SEAT TRACK CORROSION AT STA Y=840 TO 859 X=14. BLENDED CORROSION, WITHIN ALLOWABLE LIM ITS PER MD11 SRM VOL.1 53-00-01 FIG.3 REV.40. REF EGAT NRCU 05022. 2 L 7 3 4F 4 F RT A22WE E24NE 2008011500249 20080115 00249 NM 2008 1 15 CALA0800018 1 20080111 A 5313 65516982 STRINGER SPLICE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 STRINGER SPLICE IS CRACKED AT STA 907 STR 4R. REMOVED AND REPLACED STRINGER SPLICER PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008011500291 20080115 00291 NM 2008 1 15 ASAA0852454 1 20080105 A 2131 71231997303 CONTROLLER BOEING 737 737890 1384527 NM CABIN PRESSURE MALFUNCTIONED A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 587AS 35684 THE "AUTO FAIL" LIGHT ILLUMINATED WITH PRESS MODE SELECTED IN AUTOMODE. CHECKED PER AMM 21-31-00 CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2008011500312 20080115 00312 SO 2008 1 15 C2XA08CL002 1 20080108 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13992 145284 DURING ROUTINE MAINTENANCE THE EMERGENCY AILSE PATH LIGHTING AND THE EXIT DOOR LIGHT WERE INOPERATIVE. MAINTENANCE INSP ECTED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008011500323 20080115 00323 SO 2008 1 15 C2XA08IA012 1 20080104 A 5730 14537011003 SKIN EMB 145 EMB145EP 3260221 SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14925 145004 IAH, FLIGHT 2472, DURING PREFLIGHT INSPECTION THE CREW REPORTED A CRACK IN THE LEFT WING UPPER SKIN ADJACENT TO THE LEFT SPOILER INBOARD HINGE POINT. THE SKIN WAS INSPECTED AND PLACED ON DMI FO 500FC, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. ON 02/01/08 MAINTENANCE PREFORMED A TRIPLER REPAIR IAW ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5740-0 1133, REMOVED FROM DMI, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008011600007 20080116 00007 NM 2008 1 16 SWAA080177 1 20080107 A 5311 6545805 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600008 20080116 00008 NM 2008 1 16 SWAA080181 1 20080108 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 249WN 34951 EEPLS LENS BROKEN AT ROW 1ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008011600019 20080116 00019 2008 1 16 SWAA080191 4 20080108 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 489WN 33855 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008011600020 20080116 00020 NM 2008 1 16 SWAA080192 1 20080108 A 2730 6545187 TORQUE TUBE BOEING 737 7373H4 1384600 NM EELVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED BRDG CHECK, RT HORIZONTAL STABILIZER FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2008011600021 20080116 00021 NM 2008 1 16 SWAA080193 1 20080108 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 18L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011600028 20080116 00028 NM 2008 1 16 SWAA080199 1 20080108 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2008011600054 20080116 00054 NM 2008 1 16 SWAA080232 1 20080110 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 911, STR 22R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008011600062 20080116 00062 NM 2008 1 16 SWAA080240 1 20080110 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 803, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008011600068 20080116 00068 NM 2008 1 16 SWAA080250 1 20080110 A 5712 6545445 RIB BOEING 737 7373G7 1384595 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND RT WING LOWER RIB CHORD CRACKED AT STA 135.5, STR 2. REPAIRED CHORD PER ACO. 2 L 7 2 4F RT A16WE 2008011600069 20080116 00069 NM 2008 1 16 SWAA080251 1 20080110 A 5712 6545445 RIB BOEING 737 7373G7 1384595 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND LT WING LOWER RIB CHORD CRACKED AT STA 135.5, STR 2. REPAIRED CHORD PER ACO. 2 L 7 2 4F RT A16WE 2008011600072 20080116 00072 NM 2008 1 16 SWAA080245 1 20080110 A 2560 6557463 FITTING BOEING 737 7373TO 138447G NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2008011600074 20080116 00074 NM 2008 1 16 SWAA080247 1 20080110 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600077 20080116 00077 NM 2008 1 16 SWAA080256 1 20080111 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 242WN 32505 EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 2008011600082 20080116 00082 NM 2008 1 16 SWAA080258 1 20080113 A 5520 6545166 ROD BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED BRDG CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED INPUT ROD PER MM. 2 L 7 2 4F RT A16WE 2008011600090 20080116 00090 NM 2008 1 16 SWAA080264 1 20080111 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 411WN 29821 EEPLS COVER LOOSE AT ROW 3 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008011600092 20080116 00092 2008 1 16 SWAA080265 4 20080113 A 2565 63562101 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 427WN 29831 R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008021900130 20080219 00130 EA 2008 2 19 MASA200800106 1 20080205 A 5240 HANDLE CNDAIR CL600 CL6002D24 1390016 EA SERVICE DOOR INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 910FJ 15010 ASH FLT 2709 PHX-FAT - SERVICE DOOR RELEASE HANDLE INOP. MX SECURED SET SCREW DOOR, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008021900131 20080219 00131 NM 2008 2 19 AALA200800205 1 20080130 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 657AM 24615 DFW - EMERGENCY LIGHTS AT SEAT ROW 20 TO AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT R OW 20 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008021900132 20080219 00132 NM 2008 2 19 AALA200800204 1 20080129 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 796AN 30796 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 22C . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900133 20080219 00133 NM 2008 2 19 AALA200800227 1 20080131 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 772AN 29580 DFW - EMERGENCY LIGHT AT SEAT 26G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900162 20080219 00162 NM 2008 2 19 AALA200800212 1 20080130 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT AT L1 DOOR DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT L1 DOOR. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900165 20080219 00165 NM 2008 2 19 AALA200800229 1 20080131 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 970AN 30096 DFW - EMERGENCY LIGHT AT SEAT 28D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008021900177 20080219 00177 SO 2008 2 19 RAIA00801032 1 20080128 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHTS LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 809HK 145187 PRE FLT NR 7982 - IAD - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE SECURED THE CONNECTOR AT THE LIGHT ASSEMBLY. OPERATIO NAL CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2008021900179 20080219 00179 NM 2008 2 19 CALA0800098 1 20080130 A 5313 6561777505 STRINGER BOEING 737 7373T0 1384582 NM BS 360 S14L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FORWARD ENTRY AT AFT SIDE OF L-1 DOOR CUT OUT STRINGER 14L CRACKED AT STA 360. REMOVED AND REPLACED PER ECRA 5311-01392 . 2 L 7 2 4F RT A16WE 2008021900182 20080219 00182 NM 2008 2 19 CALA0800109 1 20080127 A 5313 BAC1498159 STRINGER BOEING 737 7373T0 1384582 NM BS 849 S23R CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 STA 849 STRINGER 23R CORRODED. REMOVED AND REPLACED PER SRM 53-00-03. 2 L 7 2 4F RT A16WE 2008021900186 20080219 00186 SO 2008 2 19 RAIA00802011 1 20080207 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DEFECTIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 818HK 145059 PRE FLT NR 5518 - STL - EMERGENCY LIGHT INOPERATIVE AT THE COCKPIT STEP AND GALLEY. MAINTENANCE REMOVED AND REPLACED TH E INVERTER. 2 L 7 2 4T RT T00011AT 2008021900193 20080219 00193 NM 2008 2 19 CALA0800089 1 20080128 A 5311 654655434 FRAME BOEING 737 7373T0 1384582 NM BS 847 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 ABB BELTFRAME STA847 RBL8 TO LBL4 HAS CORROSION. INSTALLED NEW FRAME SECTION PER ECRA 5311-01394. 2 L 7 2 4F RT A16WE 2008021900199 20080219 00199 WP 2008 2 19 G60A200800025 1 20080208 A 5312 BULKHEAD DOUG DC10 DC1030F 3023504 WP FUSELAGE CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 607GC 46978 FWD CARGO COMPT AFT BULKHEAD HAS 2 CRACKS APPROX 1". 2 L 7 3 4F RT A22WE 2008021900209 20080219 00209 NM 2008 2 19 SWAA080778 1 20080210 A 5711 6946466 SUPPORT ANGLE BOEING 737 7373H4 1384600 NM CENTER WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND WING CENTER SECTION FRONT SPAR STIFFENER SUPPORT ANGLE CRACKED AT BS 540, LBL 57. RE MOVED AND REPLACED SUPPORT ANGLE PER SRM. 2 L 7 2 4F RT A16WE 2008021900217 20080219 00217 NM 2008 2 19 SWAA080817 1 20080212 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900224 20080219 00224 NM 2008 2 19 QXEA200800061 1 20080205 A 6123 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM PROPELLER MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 422QX 4150 BLI- FLIGHT 2489 - AUTOFEATHER FAILS TO ILLUMINATE WITH THE BUTTON PUSHED IN. THE FLIGHT CREW RESELECTED THE TEST IN AC CORDANCE WITH THE INSTRUCTIONS FROM MAINTENANCE CONTROL. TESTED OK. NO FURTHER DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2008021900226 20080219 00226 NM 2008 2 19 SWAA080822 1 20080207 A 5210 6545871 ROLLER BOEING 737 7373A4 1384585 NM R1 DOOR JAMMED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 R1 DOOR JAMMED. FREED UPPER ROLLERS, INSPECTED DOOR PER MM. 2 L 7 2 4F RT A16WE 2008021900228 20080219 00228 NM 2008 2 19 SWAA080814 1 20080212 A 5310 6546956 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 420 AND BS 440, LBL 65. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008021900233 20080219 00233 NM 2008 2 19 SWAA080815 1 20080212 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 750SA 29802 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008021900237 20080219 00237 SO 2008 2 19 RAIA00802012 1 20080208 A 3297 355022002 ELECTRONIC UNIT EMB 145 EMB145LR 3260212 SO MLG MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 818HK 13045 183 145059 FLT NR5481 - STL - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF WITH LANDING GEAR DISAGREE MESSAGE ON THE EICAS. MAINTE NANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECK OF THE GEAR EXTENSION AND RETRACTION CHE CKED GOOD. 2 L 7 2 4T RT T00011AT 2008021900240 20080219 00240 NM 2008 2 19 QXEA200800060 1 20080203 A 2612 47387202 AMPLIFIER BOMBDR DHC8 DHC8402 1390042 NM FIRE DETECTION MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 406QX 4048 SEA - FLIGHT 2397 - IN CRUISE FLIGHT, MOMENTARY FIRE DETECTION MASTER CAUTION FOLLOWED BY A FAULT "B" ON NR 1 ENGINE. B OTH WENT BACK OUT IN LESS THEN 2 SECONDS. MAINTENANCE FOUND NO FIRE EVIDENCE. CLEANED PINS TO CONNECTOR AND REPLACED T HE FIRE CONTROL AMP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008021900242 20080219 00242 NM 2008 2 19 SWAA080784 1 20080211 A 5310 6559659 DOOR FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT STR 25R. REPAIRED FRAME PER SRM AND BOEING DRAWING. 2 L 7 2 4F RT A16WE 2008021900248 20080219 00248 NM 2008 2 19 QXEA200800177 1 20080211 A 2430 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM GENERATOR ILLUMINATED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 418QX 4143 BOI- FLIGHT 2391 - ON TAKEOFF ROLL AT ABOUT 45 KNOTS, THE NR 1 DC GENERATOR CAUTION LIGHT ILLUMINATED. ABORTED TAKEOFF. LIGHT WENT OUT AS ENGINES MOVED BACK TO DISC. RETURNED TO THE GATE. MAINTENANCE PLACED THE SYSTEM ON MEL 24-30-6. A IRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008021900249 20080219 00249 NM 2008 2 19 SWAA080795 1 20080211 A 5311 6546554 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900257 20080219 00257 NM 2008 2 19 CALA0800100 1 20080130 A 5320 69165096 ANGLE BOEING 737 7373T0 1384582 NM BS 384-351 S16L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 ANGLE CRACKED BETWEEN STA 384.20 AND STA 351.20 STRINGER 16L. REMOVED AND REPLACED ANGLE PER ECRA 5311-01392. 2 L 7 2 4F RT A16WE 2008021900260 20080219 00260 NM 2008 2 19 CALA0800101 1 20080130 A 5320 69265552 BRACKET BOEING 737 7373T0 1384582 NM BS 351 S16L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 BRACKET CRACKED AT STA 351 STRINGER 16L. REMOVED AND REPLACED BRACKET PER ECRA 5311-01392. 2 L 7 2 4F RT A16WE 2008021900262 20080219 00262 NM 2008 2 19 CALA0800128 1 20080212 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM BS 440 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 PAX CABIN HAS FRAME CRACKED AT STA 440 BETWEEN STRINGER 8R AND 9R. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04714. 2 L 7 2 4F RT A16WE 2008021900271 20080219 00271 NM 2008 2 19 CALA0800129 1 20080212 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM BS 400 S8R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 PAX CABIN HAS FRAME CRACKED AT STA 400 BETWEEN STRINGER 8R AND 9R. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04714. 2 L 7 2 4F RT A16WE 2008021900273 20080219 00273 NM 2008 2 19 CALA0800131 1 20080212 A 5551 6550582 FITTING BOEING 737 737524 1384721 NM HORIZONTAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 RT HORIZONTAL STAB FORWARD LOWER LUG HAS CORROSION. REMOVED SLEEVE AND BUSHINGS, REMOVED CORROSION AND PERFORMED REQUIR ED INSPECTIONS PER ECRA 5510-01915. FABRICATED AND INSTALLED REPAIR SLEEVE AND FLANGE BUSINGS PER SRM 55-10-10. 2 L 7 2 4F RT A16WE 2008021900275 20080219 00275 NM 2008 2 19 CALA0800134 1 20080213 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM BS 360 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 PAX CABIN HAS FRAME CRACKED AT STA 360 BETWEEN STRINGER 8L AND 9L. TRIMMED OUT CRACKED AREA INSTALLED REPAIR DOUBLERS A ND REPLACED CLIP PER ECRA 5310-04706. 2 L 7 2 4F RT A16WE 2008021900276 20080219 00276 NM 2008 2 19 SWAA080777 1 20080210 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 2 L/E SLAT LOWER SURFACE CRACKED. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 2008021900278 20080219 00278 NM 2008 2 19 SWAA080771 1 20080210 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 10L CRACKED AT BS 296. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008021900283 20080219 00283 WP 2008 2 19 G60A200800009 1 20080207 A 5320 SUPPORT DOUG DC10 DC1030F 3023504 WP BS 541-547 CORRODED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 606GC 47929 FOUND CORROSION NOSE WHEEL WELL JAM SUPPORT AT STATION 541 AND 547. 2 L 7 3 4F RT A22WE 2008021900284 20080219 00284 WP 2008 2 19 G60A200800013 1 20080207 A 5753 ANGLE DOUG DC10 DC1030F 3023504 WP TE FLAP CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 606GC 47929 RT INBOARD FLAP INBOARD LWR CLOSE OUT PANEL HAS CRACKED ANGLE. 2 L 7 3 4F RT A22WE 2008021500127 20080215 00127 NM 2008 2 15 UPS08651670 1 20080214 A 2720 YAW DAMPER BOEING 767 76734AF 1385212 NM FLIGHT CONTROL INOPERATIVE A IPXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 315UP 27743 A/C YAWED CONTINUOUSLY LT AND RT AT HIGH SPEEDS. T/S FOUND M509 RT UPR YAW DAMPER SERVO LVDT RESISTANCE VALUE ABNORMAL AND M317 O/B SPOILER NR 12 PCA LVDT PIN 8 SHROTED TO CASING. BOTH M509 RT UPPER YAW DAMPER SERVO AND M317 O/B SPOILER N R 12 PCA REPLACED. YAW DAMPER SERVO INSTALLATION TEST O/B SPOILER NR 12 PCA INSTALLATION TEST NORMAL. 2 L 7 2 4F RT A1NM 2008021500166 20080215 00166 NM 2008 2 15 SWAA080707 1 20080206 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP WEB CRACKED AT BS 1016, 12 O'CLOCK POSITION. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008021500171 20080215 00171 NM 2008 2 15 SWAA080698 1 20080206 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 432WN 33715 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 18 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008021500200 20080215 00200 NM 2008 2 15 SWAA080724 1 20080207 A 5322 6546546 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 827, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008021900006 20080219 00006 NM 2008 2 19 2008UALA00622 1 20080204 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 LEFT OVERWING EMERGENCY EXIT LIGHTS INOP 1ST, 2ND, & 3RD FROM FWD. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008021900046 20080219 00046 NM 2008 2 19 2008UALA00660 1 20080206 A 2810 FUEL CELL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUEL SYSTEM CONTAMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 562UA 26664 RTFL DUE TO L ENGINE FUEL FILTER MSG. FOUND POSSIBLE MICROBIAL CONTAMINATION ON FILTER. ACCOMPLISHED FUEL CONTAMINATION TEST PER MM28-10-00 ON LT AND RT FUEL TANKS. RT TANK TESTED NEGATIVE -- LT TANK TESTED LOW POSITIVE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008021900055 20080219 00055 NM 2008 2 19 2008UALA00666 1 20080205 A 2497 WIRE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE IDG MISINSTALLED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 670UA 29240 R GEN DRIVE EICAS AND DRIVE LIGHT ILLUMINATED. WIRE IMPROPERLY INSTALLED AND FAULTY IDG. REPAIRED WIRE HARNESS REPLACE D FAULTY IDG OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021900065 20080219 00065 NM 2008 2 19 2008UALA00667 1 20080205 A 3510 OXYGEN BOTTLE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CREW O2 LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 677UA 30029 CREW O2 NEEDS SERVICING. NOW AT 940 PSI. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021900090 20080219 00090 SO 2008 2 19 RAIA00802008 1 20080206 A 3350 BULB EMB 145 EMB145ER 3260211 SO EMERGENCY LIGHTS INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 808HK 145157 PRE FLT NR 7963 - CVG - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE AFFECTED LIGHT AS SEMBLY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT T00011AT 2008021900099 20080219 00099 WP 2008 2 19 G60A200800019 1 20080207 A 5754 RIB DOUG DC10 DC1030F 3023504 WP SLAT CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 606GC 47929 FOUND LT L/E SLAT NR 1 RIB CRACKED AT STA XIS 183. 2 L 7 3 4F RT A22WE 2008021900181 20080219 00181 NM 2008 2 19 CALA0800108 1 20080202 A 5210 6545875U70 ANGLE BOEING 737 7373T0 1384582 NM R1 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 R-1 DOOR Z ANGLE HAS CORROSION STA 296. INSTALLED NEW Z ANGLE PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008021900205 20080219 00205 2008 2 19 QXEA200800174 4 20080206 A 6122 697073002 GOVERNOR BOMBDR DHC8 DHC8402 1390042 NM OVERSPEED MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 402QX 4032 PDX - NR 1 ENGINE TOOK ABOUT 1 MINUTE LONGER THE NR 2 ENGINE TO COME OUT OF FEATHER DURING ENGINE START. MAINTENANCE RE PLACED THE OVERSPEED GOVERNOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008021900235 20080219 00235 NM 2008 2 19 QXEA200800063 1 20080206 A 5230 HANDLE BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR UNSECURE A QXEA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 NM 09 408QX 4050 BOI- FLIGHT 2342. FORWARD CARGO DOOR WARNING AFTER TAKEOFF FROM SUN. NO LOSS OF PRESSURE. DIVERTED TO BOI AND ACCOMPLI SHED A UNEVENTFUL LANDING. MAINTENANCE FOUND HANDLE OUT 1/4 INCH. SECURED DOOR. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE AND FLIGHT CONTINUED TO LAX. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008021900246 20080219 00246 NM 2008 2 19 QXEA200800180 1 20080212 A 3097 697071272 LEAD BOMBDR DHC8 DHC8402 1390042 NM PROP DE-ICE BROKEN A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 425QX 4039 SEA - FLIGHT 2275 - RECEIVED A PROP DE-ICE CAUTION LIGHT FOR THE RIGHT SIDE. DIVERTED TO PDX AND ACCOMPLISHED A UNEVENT FUL LANDING. MAINTENANCE FOUND A BROKEN LEAD AT THE NR 2 BLADE ON THE RIGHT PROP. REPLACED LEAD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008021900251 20080219 00251 NM 2008 2 19 SWAA080794 1 20080211 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900265 20080219 00265 NM 2008 2 19 QXEA200800095 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 510-520 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - SEAT TRACK NR 5 IS GOUGED X510 TO 520. MAINTENANCE BLENDED OUT GOUGE ON TRACK, INSPECTED REMAINED WITH IN LIMITS AND NO CRACKS NOTED. RESTORED FINISH TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021900277 20080219 00277 NM 2008 2 19 CALA08119 1 20080212 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM BS 867 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 FRAME CRACKED AT STA 867 ABOVE STRINGER 9L. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04714. 2 L 7 2 4F RT A16WE 2008021900281 20080219 00281 WP 2008 2 19 G60A200800023 1 20080208 A 5411 RIB DOUG DC10 DC1030F 3023504 WP LT NACELLE CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 607GC 46978 FOUND LT PYLON PNL 437FL RIB CRACKED. 2 L 7 3 4F RT A22WE 2008021900290 20080219 00290 NM 2008 2 19 GTIA0800002 1 20080128 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 521NK 2797 FLOORBEAM AT STA Y765 BETWEEN FRAME 66 AND 68 SHOWS SIGN OF CORROSION. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2008021900291 20080219 00291 NM 2008 2 19 GTIA0800005 1 20080126 A 5210 D5211006820000 HOOK AIRBUS A319 A319132 3930340 NM R1 DOOR GALLED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 521NK 2797 R1 DOOR GEARBOX LOCK HOOK GALLED. REPLACED LOCK HOOK IAW 52-11-21-400-001. 2 L 7 2 4F RT A28NM 2008021900293 20080219 00293 NM 2008 2 19 SWAA080770 1 20080210 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900294 20080219 00294 NM 2008 2 19 SWAA080772 1 20080210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008021900296 20080219 00296 NM 2008 2 19 SWAA080768 1 20080210 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900297 20080219 00297 NM 2008 2 19 SWAA080769 1 20080210 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900299 20080219 00299 NM 2008 2 19 SWAA080740 1 20080209 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730D, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008021900302 20080219 00302 NM 2008 2 19 SWAA080683 1 20080205 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 225WN 34333 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 4 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008021900310 20080219 00310 NM 2008 2 19 SWAA080690 1 20080206 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 346, STR 2L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008021900312 20080219 00312 NM 2008 2 19 SWAA080688 1 20080206 A 5753 65C30462 SKIN BOEING 737 7373H4 1384600 NM FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD FOREFLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FLAP PER M M. 2 L 7 2 4F RT A16WE 2008021900313 20080219 00313 NM 2008 2 19 HALA0800042 1 20080114 A 7830 SUPPORT BRACKET BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE THRUST REVERSER CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 ENGINE NR 2 INBD T/R HAS CRACKED SUPPORT BRACKET (FWD FACE, 8 O'CLOCK POSITION). FABRICATED AND INSTALLED BRACKET P/N 3 15T3633-37 IAW 767-300, SRM 51-60-02. 2 L 7 2 4F 4 F RT A1NM E24NE 2008021900314 20080219 00314 NM 2008 2 19 HALA0800043 1 20080110 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 260 S3L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LIGHTING STRIKE ON A/C CROWN AT STA 260 S3L. REPAIRED IAW 767-300 SRM 53-00-01, REPAIR 6. 2 L 7 2 4F RT A1NM 2008021900318 20080219 00318 NM 2008 2 19 SWAA080693 1 20080206 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900319 20080219 00319 NM 2008 2 19 SWAA080691 1 20080206 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900320 20080219 00320 NM 2008 2 19 HALA0800045 1 20080110 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 400 S2L DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LIGHTING STRIKE ON A/C CROWN AT LOCATION, STA 400 S2L. REPAIRED IAW 767-300, SRM 53-00-01, REPAIR 8. 2 L 7 2 4F RT A1NM 2008021900325 20080219 00325 NM 2008 2 19 SWAA080759 1 20080210 A 3350 311500 LENS BOEING 737 7377H4 1384404 NM EXTERIOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 413WN 29819 DURING SCHEDULED 6Y CHECK, FOUND LT OVERWING EMERGENCY EXIT EXTERIOR LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008021900326 20080219 00326 NM 2008 2 19 SWAA080743 1 20080208 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 484WN 33841 DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 2008021900332 20080219 00332 NM 2008 2 19 SWAA080761 1 20080210 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900333 20080219 00333 NM 2008 2 19 SWAA080749 1 20080210 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900334 20080219 00334 NM 2008 2 19 SWAA080748 1 20080210 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900344 20080219 00344 NM 2008 2 19 SWAA080766 1 20080210 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND STRINGER 28R CRACKED AT BS 440. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008021900358 20080219 00358 NM 2008 2 19 SWAA080825 1 20080213 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008021900364 20080219 00364 NM 2008 2 19 SWAA080857 1 20080213 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900365 20080219 00365 NM 2008 2 19 SWAA080851 1 20080213 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 8R CRACKED AT BS 500A. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008022000001 20080220 00001 EU 2008 2 20 NSVA2008004 1 20080217 A 3231 55028REVK PUSHROD SAAB SF340 340B 7860101 EU MLG DOOR DAMAGED A NSVA O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 27 198CJ 340B198 LT INBD MAIN LANDING GEAR DOOR OPENED IN FLIGHT. REMOVED AND REPLACED LT GEAR DOOR RELEASE PUSH ROD. 2 L 7 2 4T RT A52EU 2008022000025 20080220 00025 WP 2008 2 20 ASMF200802005 1 20080213 A 5100 UNKNOWN DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE UNKNOWN W ASMF D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 23 583MD 49659 725575 AC RETURNED TO PLATFORM DUE TO IGNITION FAILURE IN LT ENGINE. MAINT REPLACED IGNITION BOX IAW MM 74-10-01, TESTED CORREC T. AC WAS DISPATCHED AND RETURNED TO PLATFORM AGAIN DUE TO THE SAME FAILURE. LT ENGINE WAS STARTED WITH EMERGENCY INVERT ER, AND BREAKERS R2-91 AND R2-92 WERE CHECKED BUT FAILURE CONTINUED, SO FAILURE WAS DEFERRED BY MEL 74-2. AT MEX THE BRE AKER B1-424 WAS REPLACED AND TESTED IAW MM 74-00-00 AND 71-00-00, ALL CORRECT. THE DEFERRED REPORT WAS CLOSED. 2 L 7 2 4F 4 F RT A6WE E9NE 2008022000071 20080220 00071 2008 2 20 ASMF200802004 4 20080211 A 3452 BXS700724 WIRE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE TRANSPONDER DAMAGED W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 838AM 49397 AC RETURNED, DUE TO TRANSPONDERS FAILED AND NO RADAR CONTACT WAS REPORTED BY CONTROL TOWER. MAINT PERFORMED AUTO TEST IN THE TRANSPONDER 1 AND 2 IAW MM 34-54-00, ALL CORRECT. AC WAS SENT TO THE HANGAR AND SYSTEMS WERE TESTED WITH TESTER MOD EL TR-220 AND (C) AND (S) MODE WERE DETECTED OUT OF SERVICE. THE TRANSPONDER/TCAS CONTROL PANEL WAS REPLACED FOR THE (S) MODE IAW MM 34-54-03, TESTED CORRECT. IN THE (C) MODE THE WIRING WAS DETECTED DAMAGED, THEREFORE WIRING WAS REPAIRED IA W EO983490, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2008021900068 20080219 00068 NM 2008 2 19 CALA0800120 1 20080212 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 787 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 FRAME CRACKED AT STA 787 ABOVE STRINGER 9L. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04714. 2 L 7 2 4F RT A16WE 2008021900087 20080219 00087 EA 2008 2 19 MASA200800108 1 20080206 A 3250 STEERING SYS CNDAIR CL600 CL6002D24 1390016 EA MALFUNCTIONED A MASA O OTHER O OTHER LD LANDING 1 SW 07 923FJ 15023 ASH 2885 RNO-PHX - UNCOMMANDED LT TURN WHEN BRAKES APPLIED. MX TROUBLESHOT AND COULD NOT FIND ANY DEFECTS. 2 L 7 2 4F RT A21EA 2008021900088 20080219 00088 SO 2008 2 19 RAIA00802003 1 20080203 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 838HK 145321 PRE FLT NR 7982 - ALB - CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB TO THE AFFECT LI GHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008021900100 20080219 00100 NM 2008 2 19 AALA200800214 1 20080130 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900101 20080219 00101 NM 2008 2 19 AALA200800215 1 20080130 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT AT SEAT 44C INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 44C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008021900178 20080219 00178 NM 2008 2 19 CALA0800088 1 20080202 A 3040 5893543139 HEATER BOEING 737 7373T0 1384582 NM L1 WINDOW SPARKS A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 16339 23577 L-1 WINDOW HEAT CAUSED SPARKING AND SMOKE IN THE COCKPIT TO COME FROM THE L-1 WINDOW CONNECTION. 2 L 7 2 4F RT A16WE 2008021900180 20080219 00180 NM 2008 2 19 CALA0800099 1 20080130 A 5340 65617777 BRACKET BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FORWARD ENTRY INTERCOSTAL STRINGER 15L WEB FWD SUPPORT CLIP CRACKED. REMOVED AND REPLACED PER ECRA 5311-01392. 2 L 7 2 4F RT A16WE 2008021900183 20080219 00183 SW 2008 2 19 WGEA200800028 1 20080207 A 2820 6225765 PROBE ECLIPS EA500 ECLIPSEEA500 3350000 SW ZONE 600 DEFECTIVE E WGEA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 132DJ 208 000034 FUEL VENTING OVERBOARD ON RIGHT WING AFTER ENGINE START. TOTALIZER READ 1,470 LBS, RIGHT WING INDICATED 680 LBS, LEFT W ING 750 LBS. VISUALLY JET WAS TOPPED OFF. AFTER START JET AUTO TRANSFER FUEL FROM LEFT TO RIGHT. DEFUELED AND SUMPED PER EA500 AMM 12-10-01. PERFORMED FUEL PROBE CALIBRATION AND FUEL GAUGING TEST IAW EA500 AMM 28-40-00. RIGHT SIDE FAIL ED TEST. FOUND BAD PROBE IN BAY 9 AND 12. REMOVED AND REPLACED BAD PROBE IAW EA500 AMM 57-10-11. PERFORMED ATP DATA EN TRY FOR NEW PROBES, DRY CALIBRATION AND WET CALIBRATION TEST PER EA500 AMM 28-40-00. CHECKED GOOD. 1 L 7 2 4J RT A00002AC 2008021900192 20080219 00192 NM 2008 2 19 CALA0800103 1 20080130 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FORWARD ENTRY L-1 DOOR STRINGER 11L AT STA 360 CRACKED AT UPPER FLANGE. REMOVED AND REPLACED CLIP PER ECRA 5311-01392. 2 L 7 2 4F RT A16WE 2008021900195 20080219 00195 WP 2008 2 19 G60A200800001 1 20080207 A 5315 FLOORBEAM DOUG DC10 DC1030F 3023504 WP BS 1781 S5-25L CORRODED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 606GC 47929 FOUND CORROSION ON FLOORBEAM LBL 5 STATION 1781. 2 L 7 3 4F RT A22WE 2008021900206 20080219 00206 NM 2008 2 19 SWAA080737 1 20080210 A 3260 6555797 PIN BOEING 737 7373H4 1384600 NM UPLOCK SENSOR NOT SEATED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 29 316SW 23338 AIR TURNBACK, RT MLG RED LIGHT DID NOT EXTINGUISH AFTER RAISING LANDING GEAR. RESEATED PIN 3 ON RT MLG UPLOCK SENSOR PE R MM. 2 L 7 2 4F RT A16WE 2008021900214 20080219 00214 NM 2008 2 19 SWAA080779 1 20080211 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 232WN 32500 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008021900215 20080219 00215 NM 2008 2 19 SWAA080793 1 20080211 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER 25L CORRODED AT BS 889. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008021900241 20080219 00241 NM 2008 2 19 SWAA080783 1 20080211 A 3350 3071BPEGL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 404WN 27892 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008021900247 20080219 00247 NM 2008 2 19 SWAA080785 1 20080211 A 5330 6545774 BEAR STRAP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 847, STR 26R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008021900253 20080219 00253 NM 2008 2 19 CALA0800091 1 20080129 A 5311 BAC15171470 FRAME BOEING 737 7373T0 1384582 NM BS 767 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 FUSELAGE FRAME IS CRACKED AT BS 767 BETWEEN STRINGER 8R AND 9R. REPAIR DONE PER ECRA 5310-04697. 2 L 7 2 4F RT A16WE 2008021900268 20080219 00268 NM 2008 2 19 QXEA2008OOO70 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 310 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - RIGHT OUTBOARD SEAT TRACK NR 10 HAS 2 SMALL AREAS OF CORROSION AT APPROX X310. MAINTENANCE REMOVED COR ROSION, INSPECTED BLENDED AREA AND NO CRACKS NOTED. APPLIED ALODINE, PRIMER TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008021900280 20080219 00280 NM 2008 2 19 CALA0800136 1 20080206 A 5322 65465592 SHEAR TIE BOEING 737 7373T0 1384582 NM BS 927 S26-27L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 STA 927 FRAME TO SKIN ATTACH LEG CORRODED BETWEEN STRINGER 26L AND 27L. REMOVED AND REPLACED DAMAGED FRAME SECTION PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2008021900301 20080219 00301 NM 2008 2 19 SWAA080682 1 20080205 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 225WN 34333 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008021900307 20080219 00307 WP 2008 2 19 G60A200800018 1 20080207 A 5754 RIB DOUG DC10 DC1030F 3023504 WP SLAT CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 606GC 47929 FOUND LT L/E SLAT NR 1 RIB CRACKED AT STA XIS 177. 2 L 7 3 4F RT A22WE 2008021900324 20080219 00324 NM 2008 2 19 SWAA080742 1 20080210 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 404WN 27892 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 3 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008021900328 20080219 00328 NM 2008 2 19 SWAA080760 1 20080210 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CREASED AT BS 370, STR 4L. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008021900339 20080219 00339 NM 2008 2 19 SWAA080753 1 20080210 A 3350 1619 LIGHT BOEING 737 7373Q8 1384670 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 2008021900345 20080219 00345 NM 2008 2 19 SWAA080767 1 20080210 A 5754 65C26602 SKIN BOEING 737 737317 138447P NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD LOWER SURFACE. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900352 20080219 00352 NM 2008 2 19 SWAA080796 1 20080211 A 2560 6557463 FITTING BOEING 737 7373G7 1384595 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2008022000085 20080220 00085 NM 2008 2 20 HALA0800130 1 20080108 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1433 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 LIGHT CORROSION FOUND IN SEAT TRACK, SECT 46, LBL 88.5 AT STA 1433. CORROSION BLENDED OUT AND DEPTH ASSESSED IA W SRM 53-00-52, ALLOWABLE DAMAGE 1, AND FOUND TO BE WITHIN LIMITS. RE-WORKED AREAS ALODINED AND PAINTED IAW SRM 53-00-5 2 AND SOPM 20-41-04. LPS3 APPLIED TO SEAT TRACK. 2 L 7 2 4F RT A1NM 2008022000088 20080220 00088 NM 2008 2 20 HALA0800131 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 785 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1, LIGHT SURFACE CORROSION TO TRACK BASE, SECTION 45 SEAT TRACK LBL 54.75, STA 785. REWORK CORROSION IAW SRM 51-1 0-02, REV 76, ALODINED REWORK AREA IAW SPM 51-20-01 REV 76. PRIMED IAW AMM 51-21-00 REV 67. REWORK WITHIN LIMITS PER S RM 53-00-52/101 REV 75. 2 L 7 2 4F RT A1NM 2008022000111 20080220 00111 NM 2008 2 20 HALA0800141 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 905-915 GOUGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SECTION 45 SEAT TRACK CROWN GOUGED, AT LBL 54.75, BS 905-915. REMOVED DAMAGE PER SRM 51-10-02, REV 75. REWORK WITHIN L IMITS PER SRM 53-00-52/101 REV 75. ALODINED PER SRM 51-20-01, REV 75. PRIMED PER AMM 51-21-00, REV 67. 2 L 7 2 4F RT A1NM 2008022000116 20080220 00116 2008 2 20 SWAA080834 4 20080213 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008022000117 20080220 00117 NM 2008 2 20 SWAA080835 1 20080213 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED SPV CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED AT OUTBOARD T/E. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008011600102 20080116 00102 GL 2008 1 16 CHQA200800004 2 20080104 A 7397 23062387 WIRE HARNESS EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL FADEC CHAFED A CHQA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 11 373SK 145543 CAE311999 AUS TO STL - DURING CLIMB AT FL320, THE CREW NOTICED A THUMPING SOUND. THE NOISE WAS TRACED TO THE NR 1 ENGINE WHICH CO MPRESSOR STALLED WITH EACH DECREASE IN THRUST. THE CAPTAIN PULLED BACK POWER ON E1 AS THE QRH WAS BEING REFERENCED FOR THE PROPER CHECKLISTS, AND E1 SPOOLED DOWN RAPIDLY. WHILE THE ENGINE WAS SPOOLING DOWN IT ATTEMPTED AN AUTO RELIGHT UNS UCCESSFULLY THEN SHUT DOWN WITH AN ENG 1 OUT CAUTION MESSAGE ON EICAS. THE FLIGHT CREW FOLLOWED THE QRH AND SECURED THE ENGINE OFF AND BEGAN TO DESCEND. DURING THE DESCENT, FOLLOWING THE QRH, THE FLIGHT CREW PERFORMED AN INFLIGHT RESTART OF E1 WHICH WAS SUCCESSFUL. THE AIRCRAFT LANDED WITHOUT INCIDENT IN DFW. MAINTENANCE PERFORMED A VISUAL INSPECTION OF 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008011600104 20080116 00104 EU 2008 1 16 08FDEA00044 1 20080105 A 5320 A5383210420600 WEB AIRBUS 300 A300B4622 3930401 EU ZONE 200 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 FUS FR 48,BETWEEN SEAT TRACKS 3L AND 4L, STIFFENER WEB 12" TO 24" BELOW FLOOR IS BENT. REMOVED AND REPLACED WEB IAW A30 0-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008011600113 20080116 00113 NM 2008 1 16 08FDEA00054 1 20080106 A 5730 65507481 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 RIGHT WING FUEL TANK ACCESS PANEL 641MB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 641MB IAW SRM 57-20- 01. AFTER REWORK AMOUNT REMAINING NOT WITHIN LIMITS IAW SRM 57-20-01, FIG 201, DETAIL II, III WITHIN 0.10" OF SEAL. RE PLACED ACCESS PANEL 641MB IAW AMM 28-11-01. 2 L 7 2 4F RT A2NM 2008011600114 20080116 00114 NM 2008 1 16 08FDEA00055 1 20080106 A 5730 112N60081 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 RIGHT WING FUEL TANK ACCESS PANEL 642AB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 642AB IAW SRM 57-20-0 1, FOUND TO BE OUT OF LIMITS PER SRM 57-20-01, FIG 201, DETAIL I, SECTION AA, NOTE B. REPLACED ACCESS PANEL IAW AMM 28- 11-01. 2 L 7 2 4F RT A2NM 2008011600115 20080116 00115 WP 2008 1 16 08FDEA00056 1 20080107 A 5522 ALC7386504 SKIN DOUG DC10 DC1030 3023501 WP RT ELEVATOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 RT INBD ELEVATOR LWR SURFACE FOUND DENT ON SKIN. 2 L 7 3 4F A22WE 2008011600116 20080116 00116 WP 2008 1 16 08FDEA00057 1 20080107 A 5522 NLC6041503 SKIN DOUG DC10 DC1010F 3022111 WP LT ELEVATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 369FE 46607 OUTBD ELEVATOR LT T/E TIP WITH CRACK DUE ACCIDENTAL CONTACT AGAINST CRADLE. 2 L 7 3 4F A22WE 2008011600151 20080116 00151 2008 1 16 SWAA080166 4 20080107 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED BRDG CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008011600152 20080116 00152 NM 2008 1 16 SWAA080178 1 20080107 A 5753 65C30462 SKIN BOEING 737 7373Y0 1384671 NM FORE FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED SPV CHECK, FOUND LT WING INBOARD FORE FLAP UPPER SURFACE DISBONDED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2008011600154 20080116 00154 NM 2008 1 16 SWAA080204 1 20080109 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER 8R CRACKED AT BS 727E. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008011500313 20080115 00313 SO 2008 1 15 C2XA08CL003 1 20080108 A 3297 CONNECTOR EMB 145 EMB145LR 3260212 SO NLG LOOSE A C2XA K NONE N FALSE WARNING DE DESCENT 1 SW 27 12957 145080 CLE FLIGHT 2039 - THE CREW REPORTED A LANDING GEAR DISAGREE ON EXTENSION. MAINTENANCE INSPECTED AND RESECURED THE NOSE GEAR UPLOCK BOX CONNECTOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008011500328 20080115 00328 SO 2008 1 15 C2XA08IA013 1 20080107 A 3030 CS500060D4A SENSOR EMB 145 EMB145EP 3260221 SO COCKPIT BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 14930 145011 IAH - FLIGHT 2137, WHILE "SITTING AT THE GATE" THE CREW REPORTED A BURNT SMELL IN THE COCKPIT. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND PITOT NUMBER ONE CURRENT SENSOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPR OVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008011500354 20080115 00354 2008 1 15 SWAA080160 4 20080107 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 320SW 23341 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008011500359 20080115 00359 NM 2008 1 15 SWAA080165 1 20080107 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 312, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011600009 20080116 00009 NM 2008 1 16 SWAA080182 1 20080108 A 5311 6546595 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022500283 20080225 00283 NM 2008 2 25 2008UALA00386 1 20080121 A 2697 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FIRE DETECTION DAMAGED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 772UA 26930 BLEED LOOP 2 BODY FAILURE OF BODY DUCT LEAK DETECTION LOOP OR RIGHT DUCT LEAK OVERHEAT DETECTION SYSTEM (DLODS) CARD. S USPECT POSSIBLE HIGH RESISTANCE. CONNECTOR DP8402 PINS 45 AND 46 HAVE A RESISTANCE OF 136.9 OHMS. SHOULD BE 128.7 (+-12 .9) . RE-TORQUED CONNECTORS TO CARD. MEASURES WITHIN LIMIT. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008022500284 20080225 00284 2008 2 25 DLM88080176 4 20080207 A 3418 349001016 STALL WARNING DOUG MD88 MD88 3023688 NM FALSE ACTIVATION A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 944DL 49817 DURING CLIMB-OUT AS SLATS RETRACTED BOTH STALL IND FAIL AND WINDSHEAR INOP LIGHTS ILLUMINATED. REPLACED NR 2 STALL WARN ING COMPUTER AND RT AOA TRANSDUCER CHECKS NORMAL. PERFORMED STALL WARNING TROUBLESHOOTING CHEC PER AMM 34-19-00 PAGE B LOCK 101 AND ADJUSTMENT TEST PER AMM 34-19-00-201 WINDSHEAR CHECKS GOOD 2 L 7 2 4F RT A6WE 2008022500287 20080225 00287 NM 2008 2 25 DL764080180 1 20080209 A 3240 321002519 VALVE BOEING 767 767432ER 1385134 NM MLG BRAKE FAILED A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 830MH 29701 RTB - RT HYD SYSTEM QTY WENT TO ZERO. REPLACED B BRAKE RT SIDE FUSE AND ANTI-SKID VLV ON RT SIDE BRAKE ANTI-SKID MODULE PER AMM. LK CK OK. OPS CKS GOOD PER MM. SERVICED HYD SYSTEM RT SIDE PER MM. 2 L 7 2 4F RT A1NM 2008022500291 20080225 00291 NM 2008 2 25 AALA200800296 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 36C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 36C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022500293 20080225 00293 NM 2008 2 25 AALA200800304 1 20080211 A 3397 WIRE BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 353AA 24034 SFO - EMERGENCY LIGHT AT FORWARD SEAT 17AB INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT FORWARD SEAT 17AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008022500295 20080225 00295 NM 2008 2 25 2008UALA00446 1 20080126 A 2700 TRIM SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU UNKNOWN A UALA O OTHER W F INADEQUATE Q C FLT CONT AFFECTED CR CRUISE 1 WP 29 338UA 24242 LANDED UNDER AMBER ALERT DUE TO A TRIM PROBLEM. RESUBMITTED. UNKNOWN PART INFO. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500296 20080225 00296 NM 2008 2 25 AALA200800295 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 32C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 32C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022500303 20080225 00303 NM 2008 2 25 AALA200800324 1 20080215 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 ORD - EMERGENCY LIGHT AT SEAT 40C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 40C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022500308 20080225 00308 NE 2008 2 25 AALA200800325 2 20080215 A 7230 BLADE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535* NE COMPRESSOR FAILED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 683A 3564 25340 31079 MIA INFLIGHT T15FEB - NUMBER ONE ENGINE SURGING AFTER TAKEOFF AT 800 TO 900 FEET. CREW DECREASED THROTTLE AND SURGING S TOPPED. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND COMPRESSOR BLADE FAILURE. REPLACED NUMBER ONE ENGINE ON 16 FEB AT MIA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2008022500309 20080225 00309 NM 2008 2 25 AALA200800326 1 20080215 A 2560 L20191009 FLASHLIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 918AN 29519 LGA - EMERGENCY FLASHLIGHT AT AFT RIGHT FLIGHT ATTENDANT JUMPSEAT INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT AT AFT RIG HT FLIGHT ATTENDANT JUMPSEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008022500310 20080225 00310 NE 2008 2 25 DLM88080184 2 20080210 A 7200 JT8D219 TURBINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED A DALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 27 931DL 42977 49718 725736 IN FLT RETURN RT ENG FAILURE DURING CLIMB-OUT NORMAL PWR T/O WITH ENG A/I ON. ALL INDICATIONS NORMAL. AT 1300' AGL BUM P NOISE LIKE A COMP STALL. PERFORM INITIAL ACTION ITEMS AND STARTED RETURN TO AIRPORT. PLANNED TO RUN ENG AT IDLE BUT APPROX 2-3 MIN ENG STARTED TO VIBRATE. CONT ENG FAILURE CKLIST AND SECURED RT ENG NORMAL LANDING. REMOVED AND REPLACED RT ENG PER TRANSMITTAL 9T102. 2 L 7 2 4F 4 F RT A6WE E9NE 2008022500312 20080225 00312 NE 2008 2 25 DL76G080190 2 20080212 A 7230 FAN BLADE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 ENGINE DAMAGED A DALA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 27 1605 26251 704696 30198 704696 LEFT ENGINE INGESTED BIRDS AFTER TAKEOFF. CREW REPORTED LEFT ENG HIGH VIBRATION ENGINE NOT SHUTDOWN. RETURNED TO ACC. 6 FAN BLADES BEYOND LIMITS. HAVE NOT BORO CORE AT THIS TIME SENDING AMTS, BORO EQUIP AND FAN BLADES. REPLACED DAMAGE D FAN SETS NR 1 ENG BORESCOPED MPC FOUND NO BIRD STRIKE DAMAGE AFTER REMOVING BLADES VISUALLY INSPECTED CORE INTAKE FOU ND NO DEBRIS. CORE OK. PBS RUN FAILED FOR DATA LO CHECKED AND RAN SECOND AND THIRD VIBE RUN. RESET ALL WEIGHT PER BAL ANCE RUN FAN VIBS NOW 1.1 AT 98 PERCENT N1 OK FOR ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS. 2 L 7 2 4F 4 F RT A1NM E13NE 2008022500314 20080225 00314 NM 2008 2 25 DL76L080192 1 20080213 A 2150 A/C PACK BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE RIGHT ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 185DN 27961 704696 F/A IN AFT GALLEY REPORTED POSSIBLE ELEC ODOR. ODOR DISSIPATED ONLY TO RECUR 10 MIN LATER EMERGENCY DECLARED DIV TO FRA . INSP GALLEY C/MAKERS OVENS LIGHTS/BALLASTS. INSP CHILLERS AND WATER COMP INSP C/P AND E/E AND CARGO AREA CKS CONDUCT ED W/ENGS OFF AND ENG RUNNING AND CABIN PRESSURIZED. FOUND RT PACK BITE LAST FAULT TCV REST OPS NORM, ON ENG RUN PRECAU TIONARY REMOVED AND REPLACED RT PACK TCV OPS AND LK CHK. 2 L 7 2 4F 4 F RT A1NM E13NE 2008022500319 20080225 00319 NM 2008 2 25 DLM90080199 1 20080213 A 5530 LUG DOUG MD90 MD9030 3023690 NM GE CF6 CF680C2B6F 30025 NE VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 704696 LT O/B VERTICAL STABILIZER LUG CORRODED. REPAIRED LEFT OUTBOARD VERTICAL LUG (STAB), IAW MD90 SRM 55-30-05. 2 L 7 2 4F 4 F RT A6WE E13NE 2008022500320 20080225 00320 NM 2008 2 25 DLM90080200 1 20080206 A 5347 5930545 SEAT TRACK DOUG MD90 MD9030 3023690 NM GE CF6 CF680C2B6F 30025 NE BS 486-551 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 704696 CABIN SEAT TRACK GOUGED AND CORRODED OUT OF LIMITS FS 486-551 RBL.22, .058" REMAINING MATERIAL. REMOVED AND REPLACED SE AT TRACK FS 486-551 RBL 22, IAW MD90 SRM 51-30-01 AND SRM 53-40-01 FIG 6. 2 L 7 2 4F 4 F RT A6WE E13NE 2008022500326 20080225 00326 GL 2008 2 25 FDKA200802051 2 20080204 A 7200 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A FDKA O OTHER O OTHER CR CRUISE 1 SW 07 835MJ 14001 145353 CAE311938 FDM 6206 FLL (1042 PHX LCL). ENGINE NR 1 OUT IN FLIGHT. MX REMOVED AND REPLACED NR 1 ENGINE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008022500328 20080225 00328 EU 2008 2 25 USAA920080400 1 20080210 A 3397 WIRE AIRBUS 320 A320232 3930326 EU CABIN DISCONNECTED A USAA K NONE O OTHER UK UNKNOWN 1 EA 19 640AW 448 FLT 710 - FLL-PHX - EEL - R1 SERVICE / EMERGENCY DOOR EXIT ESCAPE PATH LIGHT ABOVE DOOR IS INOP. MAINTENANCE REMOVED PA NEL AND RECONNECTED WIRING TO LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008022500335 20080225 00335 2008 2 25 BB08015 4 20080210 A 2310 6226827002 TRANSCEIVER BOEING 757 7572S7 1384962 NM HF COMM FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 906AW 5859 1306 23568 PHX PHX-OGG FLT 432 - CREW STATED A/C HAD LOST ITS NUMBER 2 HF RADIO. RADIO WOULD NOT TRANSMIT AT ALL. TRIED TO RESET CB AND RADIO WOULD STILL NOT TRANSMIT. CAPT AND CONTROLLING DISPATCHER AGREE TO RETURN TO PHX. MAINTENANCE REPLACED NR 2 HF COMM TRANSCEIVER & PERFORMED SATISFACTORY OPS CHECK. 2 L 7 2 4F RT A2NM 2008022500337 20080225 00337 NM 2008 2 25 USAA920080403 1 20080112 A 5330 6545768227 BEAR STRAP BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FORWARD CARGO DOOR SURROUND LOWER AFT CORNER BEAR STRAP, BS 492, S25R. REPAIRE D FORWARD CARGO DOOR SURROUND LOWER AFT CORNER BEAR STRAP, BS 492, S25R IAW B737 SRM 53-00-01-2R32. 2 L 7 2 4F RT A16WE 2008022500342 20080225 00342 NM 2008 2 25 USAA920080408 1 20080204 A 5210 5079454 WEB BOEING 737 7373S3 1384711 NM L1 DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - CRACKED L1 DOOR INNER WEB SKIN PREVIOUS REPAIR, BS 319, S9L - S10L. REPAIRED L1 DOOR I NNER WEB SKIN, BS 319, S9L - S10L IAW B737 SRM 51-70-13. 2 L 7 2 4F RT A16WE 2008022500343 20080225 00343 NM 2008 2 25 USAA920080409 1 20080112 A 5330 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - CRACKED SKIN, BS 454, BL 0 - LBL 2, WL 148. REPAIRED SKIN, BS 454, BL 0 - LBL 2, WL 14 8 IAW USAIRWAYS TASK CARD M2A53002. 2 L 7 2 4F RT A16WE 2008022500344 20080225 00344 NM 2008 2 25 USAA920080410 1 20080110 A 5330 6547766 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - CRACKED SKIN, BS 500D - BS 520, S12R. REPAIRED SKIN, BS 500D - BS 520, S12R IAW USAIRW AYS EO 100228. 2 L 7 2 4F RT A16WE 2008022500345 20080225 00345 NM 2008 2 25 USAA920080411 1 20080108 A 5414 313A1200 SKIN BOEING 737 7373S3 1384711 NM NR 2 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - CRACKED NR 2 PYLON SKIN PANEL, PYLON STATION 261. REPAIRED NR 2 PYLON SKIN PANEL, PYLO N STATION 261 IAW USAIRWAYS EA 100219. 2 L 7 2 4F RT A16WE 2008022200085 20080222 00085 NM 2008 2 22 AALA200800243 1 20080203 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 978AN 30100 MIA EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A16WE 2008022200103 20080222 00103 NM 2008 2 22 AALA200800245 1 20080204 A 3397 WIRE BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 385AM 27059 CDG - EMERGENCY LIGHT ASSEMBLY AT SEAT 5B BROKEN OFF. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT ASSEMBLY AT SEAT 5B. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008022200110 20080222 00110 WP 2008 2 22 AALA200800252 1 20080205 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 495AA 49733 DFW - EMERGENCY LIGHT AT OVERHEAD COCKPIT INOPERATIVE. REPLACED BATTERY PACK AT FORWARD OVERHEAD AISLE PANEL FOR EMERGE NCY LIGHT AT OVERHEAD COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022200118 20080222 00118 NM 2008 2 22 HALA0800232 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 947 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT LBL 11, STA 974, MAX DEPTH OF BLEND OUT WAS 0.011". BLENDED IAW SRM 51-10- 02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200129 20080222 00129 NM 2008 2 22 2008UALA00734 1 20080210 A 5320 CHANNEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FUSELAGE STRINGERS 14L AND 15L U-CHANNELS ARE CRACKED AT BS 360 ON LWR FLANGE. MAJOR REPAIR: REPLACED CHANNELS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200130 20080222 00130 NM 2008 2 22 2008UALA00735 1 20080210 A 5340 ATTACH ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FUSELAGE STRINGERS 8L AND 11L INTERCOSTAL ATTACH ANGLES ARE CRACKED AT BS 360. MAJOR REPAIR: REPLACED ATTACH ANGLES. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022500002 20080225 00002 NM 2008 2 25 NOCA01208 1 20080207 A 3350 BPS73 POWER SUPPLY BOEING 767 76739H 1385311 NM CABIN DISCHARGED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 760NA 26257 EMERGENCY EXIT LIGHTS AFT OF DOOR L2 ON THE FLOOR ARE VERY DIM. REMOVED AND REPLACED POWER SUPPLY (M373) PER MM 33-51-0 7. 2 L 7 2 4F RT A1NM 2008022500038 20080225 00038 2008 2 25 2008UALA00673 4 20080205 A 2565 COVER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R4 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 116UA 26908 THE 4R SLIDE PACK COVER FELL OFF. MAINT TEXT: SLIDE PACK CAME LOOSE FROM TOP ATTACH POINT. SUSPECT SLIDE IMPROPERLY I NSTALLED. REINSTALLED SLIDE. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022500056 20080225 00056 NM 2008 2 25 2008UALA00778 1 20080208 A 5320 SUPPORT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 665UA 29237 BS 246 AT BL 0, PULLEY SUPPORT CRACKED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500057 20080225 00057 NM 2008 2 25 2008UALA00779 1 20080208 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 665UA 29237 IN SEAT EMERGENCY LIGHTS AT SEATS 3HJ, 24HJ AND 35HJ ARE INOP. REMOVED AND REPLACED LIGHTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500173 20080225 00173 NM 2008 2 25 2008UALA00780 1 20080207 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 527UA 24995 EMERGENCY LIGHT AT DOOR 4 RT INOP (EXT). LIGHT BULB VIBRATED LOOSE. SECURED LIGHT BULB AND OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500205 20080225 00205 NM 2008 2 25 2008UALA00798 1 20080211 A 5210 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD ENTRY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FWD ENTRY DOOR AFT FRAME INNER SKIN CRACKED BETWEEN THE 5TH AND 7TH STOP PIN CUTOUT. MAJOR REPAIR: REMOVED DAMAGE. INSTA LLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500218 20080225 00218 2008 2 25 2008UALA00813 4 20080212 A 2565 PIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EVAC SLIDE IMPROPER PART A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 376UA 24641 AFT GALLEY DOOR EVACUATION SLIDE HAS THE WRONG SAFETY PIN INSTALLED. THE INSTALLED PIN CANNOT DISARM THE BOTTLE. INSTA LLED NEW LOCK PIN. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500246 20080225 00246 EA 2008 2 25 HNAA0800082 1 20080210 A 3320 BALLAST DHAV DHC8 DHC8311 1386006 EA CABIN MALFUNCTIONED A HNAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 EA 07 328 281 ELECTRICAL SMELL NOTICED BY F/A AT ROW 2DF, DEACTIVATED CABIN NORN LIGHT SYS, FOUND BALLAST CONN AT 2DF BURNT, MEL'D IAW 33-2. 2 H 7 2 4T RT A13NM 2008022500301 20080225 00301 NM 2008 2 25 DLM90080254 1 20080221 A 3240 50121934 BRAKE DOUG MD90 MD9030 3023690 NM LEFT MLG LEAKING A DALA D RETURN TO BLOCK K A FLUID LOSS FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 904DA 53384 A/C ARRIVED AND HAD A HOT BRAKE NR 2, BRAKE WAS LEAKING HYD FLUID AND STARTED BURNING. FIRE WENT OUT ON ITS OWN. REPLA CED NR 1 AND NR 2 BRAKE ASSYS PER M/M. 2 L 7 2 4F RT A6WE 2008022500302 20080225 00302 NM 2008 2 25 DL76G080250 1 20080215 A 4920 491003096 APU BOEING 767 7673P6 1385105 NM APU BAY ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 153DL 23357 24985 STRONG OIL ODOR ENTIRE A/C W/PACKS RUNNING. INSP APU AND APU BLEED DUCT NO OIL FND. INSP PACKS BAYS NOTHING ABNORMAL. RAN PACKS INDEPENDENTLY TRYING TO DETERMINE WHICH HAD MORE SMELL. PERFORMED DUCT BURNOUT UP TO STEP 10 PER M/M 250083. REPLACED APU PER AMM. FINISHED DUCT BURNOUT PER AMM 21-00-2. 2 L 7 2 4F RT A1NM 2008022500316 20080225 00316 NM 2008 2 25 DLM90080196 1 20080211 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM GE CF6 CF680C2B6F 30025 NE BS 439-519 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 704696 CABIN SEAT TRACK GOUGED OUT OF LIMITS, FS 439-519 RBL 54. FABBED NEW SEAT TRACK AND INSTALLED, IAW MD90 SRM 53-40-01 VO L I. 2 L 7 2 4F 4 F RT A6WE E13NE 2008022500347 20080225 00347 SO 2008 2 25 FDKA200802054 1 20080211 A 2120 71346311 DUCT EMB 145 EMB145LR 3260212 SO NR 2 PACK DEFECTIVE A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 860MJ 145773 FDM 6210 ATL. SMOKE IN CABIN AND COCKPIT. MX REMOVED AND REPLACED NR 2 PACK DUCT, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008022500349 20080225 00349 2008 2 25 USAA920080415 4 20080210 A 2565 D30665105 SLIDE RAFT AIRBUS 320 A320232 3930326 EU R2 DOOR DEFECTIVE A USAA K NONE J WARNING INDICATION CL CLIMB 1 EA 19 619AW 36000 132 527 FLT 560 - PDX-LAS - EMERG EQUIP - R2 DOOR SLIDE ARMING LEVER POPPED OUT AFTER TAKEOFF. DOOR SHOWS DISARMED IN FLIGHT. ARMING LEVER STAYS OUT. MAINTENANCE REMOVED AND REPLACED THE AFT SLIDE RAFT ASSEMBLY IAW TASK CARD R1C25304. 2 L 7 2 4F RT A28NM 2008022500355 20080225 00355 EU 2008 2 25 USAA920080379 1 20080129 A 5315 D5347219020490 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AW 543 SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON CABIN SEAT RAIL BEAM, BS 3043 / FR 64 - BS 3158 / FR 66, +Y1242. REPLACED CABIN SEAT RAIL BEAM, BS 3043 / FR 64 - BS 3158 / FR 66, +Y1242 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022500359 20080225 00359 NM 2008 2 25 USAA920080384 1 20080207 A 5320 PLATE BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 202UW 27811 BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR PRESS PLATE, BS 1681 - BS 1720, LBL 56 - RBL 56. REPAI RED CABIN FLOOR PRESS PLATE, BS 1681 - BS 1720, LBL 56 - RBL 56 IAW B757 SRM 53-60-51. 2 L 7 2 4F RT A2NM 2008022500360 20080225 00360 NM 2008 2 25 USAA920080413 1 20080211 A 5330 6545778 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 PHX - MAJOR REPAIR - CRACKED FUSELAGE SKIN CRACKED, BS 930, S25R. REPAIRED FUSELAGE SKIN, BS 930, S25R IAW B737 SRM 53- 00-01-2R. 2 L 7 2 4F RT A16WE 2008022000118 20080220 00118 NM 2008 2 20 SWAA080841 1 20080213 A 2560 6557463 FITTING BOEING 737 7373TO 138447G NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2008022000119 20080220 00119 NM 2008 2 20 SWAA080836 1 20080213 A 5753 6546481 CARRIAGE BOEING 737 7373TO 138447G NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP NR 2 CARRIAGE LOWER SPINDLE CORRODED. REMOVED AND REPLA CED CARRIAGE PER MM. 2 L 7 2 4F RT A16WE 2008022000120 20080220 00120 NM 2008 2 20 HALA0800121 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 981 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 2 CORROSION SECTION 45, SEAT TRACK AT LBL 88.5, STA 981. SEAT TRACK REPLACED. 2 L 7 2 4F RT A1NM 2008022000122 20080220 00122 NM 2008 2 20 HALA0800138 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 999 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SECTION 45 SEAT TRACK CROWN DAMAGED (SCRATCHED/GOUGES) AT LBL 54.75, STA 999. REWORKED IAW SRM 51-10-02, REV 76. WITHI N LIMITS PER SRM 53-00-52, REV 76. ALODINED PER SRM 51-20-01 REV 76. PRIMED PER AMM 51-21-00, REV 67. 2 L 7 2 4F RT A1NM 2008022000125 20080220 00125 SO 2008 2 20 CHQA200800030 1 20080214 A 3610 DUCT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BLEED AIR DAMAGED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 269SK 145293 CAE311698 IAD TO YOW - AFTER GEAR RETRACTION ON CLIMB THE CREW RECEIVED A LAV SMOKE EICAS MESSAGE. WHILE PREPARING TO RETURN TO I AD, THE FLIGHT ATTENDANT VERIFIED THAT THERE WAS NO VISIBLE SMOKE OR ODOR IN THE LAVATORY. SHORTLY AFTER, THE EICAS MES SAGE WENT AWAY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE WAS ABLE TO DUPLICATE THE MESSAGE AND FOUND THAT I T OCCURRED ONLY WHILE RUNNING OFF OF THE NR 1 BLEED. THE NR 1 BLEED WAS DEFERRED AND THE AIRCRAFT WAS FERRIED TO A MAIN TENANCE BASE FOR FURTHER TROUBSHOOTING. ONCE THE AIRCRAFT ARRIVED THE E1 PRSOV WAS RE-ACTIVATED AND THE BLEED SYSTEM WA S OPS CHECKED FOR 20 MINUTES AT TAKEOFF POWER. WHILE RUNNING E1 A LOUD NOISE WAS HEARD BELOW THE FLOOR AND AFTER FURTHE 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008022000137 20080220 00137 NM 2008 2 20 SWAA080840 1 20080213 A 2560 6557463 FITTING BOEING 737 7373TO 138447G NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2008022000142 20080220 00142 NM 2008 2 20 SWAA080846 1 20080213 A 5322 6546546 SHEAR TIE BOEING 737 7373TO 138447G NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008022000144 20080220 00144 NM 2008 2 20 SWAA080848 1 20080213 A 5322 6546529 SHEAR TIE BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500, STR 18L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008022000150 20080220 00150 SO 2008 2 20 C2XA08SH025 1 20080216 A 5320 14527150001 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11565 145621 SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION BETWEEN FR 18-23. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FR1 8-23 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008022000151 20080220 00151 SO 2008 2 20 C2XA08TY030 1 20080217 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15980 145202 EMERGENCY LIGHT AT SEAT 12BC INOP. REMOVED AND REPLACED LAMP IAW EMB 145 AMM 33-50-06. OPS CHECK GOOD. AIRCRAFT RELEA SED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022000166 20080220 00166 GL 2008 2 20 3257 1 20080208 A 7930 12635002 SENSOR CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL OIL PRESSURE SYS ERRATIC E J4PA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 13 398SR 866 2102 689888 FP4964B IN TAKEOFF CLIMB AND THE OIL PRESSURE WAS FLUCTUATING BETWEEN 25 PSI AND 60 PSI. AIRCRAFT RETURNED TO HOME STATION WITH OUT INCIDENT. ONE PASSENGER ONBOARD, NO INJURIES OR DAMAGE TO AIRCRAFT. TROUBLESHOT SYSTEM, FOUND THE OIL PRESSURE SEN SOR WAS READING ERRATIC AT ALL PRESSURE SETTING. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2008022000167 20080220 00167 WP 2008 2 20 NWAA080549858 1 20080215 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 767NC 47724 THE EMERGENCY PATHWAY LIGHTING AT EACH SEAT IN THE FIRST CLASS SECTION WAS FOUND TO BE INOPERATIVE. THE BATTERY PACKS F OR THOSE ROWS WERE REPLACED AND THE LIGHTS FUNCTIONALLY CHECKED GOOD. 2 L 7 2 4F RT A6WE 2008022000169 20080220 00169 NM 2008 2 20 HALA0800061 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 654 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION ON SEAT TRACKS AT STA 654 + 58, LBL 11. CORROSION REMOVED, REPROTECTED, STOP PLATE INSTALLATION, IAW SRM 51-10-02. C.P.C. APPLICATION AND ALUMINIZED PRIMER. 2 L 7 2 4F RT A1NM 2008022000171 20080220 00171 NM 2008 2 20 HALA0800063 1 20080125 A 5340 ATTACH FITTING BOEING 767 7673G5 1385126 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 AFT GALLEY COMPARTMENT NR 405 AND NR 411, CORRODED ATTACHMENT BLOCKS. REMOVED AND FABRICATED ATTACHMENT BLOCKS IAW BOEI NG SOPM D6-51702 REV 104. INSTALLED BLOCKS, IAW CMM-25-28-73. 2 L 7 2 4F RT A1NM 2008022000175 20080220 00175 SO 2008 2 20 C2XA08ON081 1 20080203 A 2612 MS3726316002 RELAY EMB 145 EMB145LR 3260212 SO COCKPIT FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14907 15628 15628 14500479 FLT 0097 - ONT TO ONT - FLIGHT CREW REPORTED BAGGAGE FIRE TEST INOP. MX REMOVED AND REPLACED RELAY FROM RT RELAY SUPPOR T (H16) OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022000177 20080220 00177 SO 2008 2 20 C2XA08IA045 1 20080202 A 2150 14553103001 NOZZLE EMB 145 EMB145EP 3260221 SO A/C PACK DIRTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 14945 145049 IAH - FLIGHT 2818, THE CREW REPORTED FOG DENSE IN COCKPIT DURING TAKEOFF ROLL, NO BURNING SMELL JUST FOGGED ALL WINDOWS. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE CLEANED WATER SPRAY NOZZLE ON NR 1 PACK IA W EMB145 AMM 21-51-13, OPERATIONALLY CHECKED WITH NO DEFECTS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008022000180 20080220 00180 SO 2008 2 20 C2XA08IA051 1 20080207 A 2130 2014AB MODULE EMB 145 EMB145XR 3260214 SO CABIN PRESSURE INOPERATIVE A C2XA B G EMER. DESCENT O2 MASK DEPLOYED O OTHER CR CRUISE 1 SW 27 13123 14277 14277 145688 IAH - FLIGHT 2926, THE CREW REPORTED CABIN DECOMPRESSED AT FL340, CABIN PRESSURE FLUCTUATED BETWEEN 7200' & 14,200' CABI N ALT, OXYGEN MASKS DEPLOYED AUTOMATICALLY. THE CREW PERFORMED AN EMERGENCY DESCENT AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE CABIN PRESSURE ACQUISITION MODULE (CPAM), OPERATIONAL LY CHECKED WITH NO DEFECTS, THE AIRCRAFT WAS TEST FLOWN SATISFACTORILY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. 2 L 7 2 4F RT 2008022000184 20080220 00184 SO 2008 2 20 SIMA200805002 1 20080215 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT FUMES A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 21 693AE 14500868 ON FLIGHT 4064, CREW REPORTED THAT ON APPROACH TO ORD ELECTRICAL FUMES IN COCKPIT. EMERGENCY DECLARED. AIRCRAFT LANDED WITH OUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. COULD NOT ISOLATE PROBLEM AT THIS TIME. A/C DID 2510 CHECK FLIGHT AND PASSED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022000187 20080220 00187 NM 2008 2 20 HALA0800078 1 20080108 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 850 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45, SEAT TRACK AT LBL 88.5, STA 850. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION, IAW S RM 51-10-02, REV 75, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101 REV 75. 2 L 7 2 4F RT A1NM 2008022000195 20080220 00195 SO 2008 2 20 C2XA08ON088 1 20080208 A 2150 8152915 PRESSURE SWITCH EMB 145 EMB145XR 3260214 SO NR 1 PACK BLOWN A C2XA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SW 27 14168 1753 1753 14500840 FLT 7775 - SEA TO SEA - FLIGHT CREW REPORTED PACK 1 OVERLOAD - ICE DET FAIL. FLIGHT CREW RETURNED TO BLOCK WITHOUT INCI DENTS. MX PERSONNEL REMOVED AND REPLACED PRESSURE SWITCH OPERATIONALLY CHECKED SATISFACTORY. A/C WAS RELEASED TO RETUR N FOR SERVICE. 2 L 7 2 4F RT 2008022000196 20080220 00196 WP 2008 2 20 NWAA080559857 1 20080214 A 2120 UNKNOWN DOUG DC9 DC951 3022051 WP CABIN ODOR A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 766NC 47739 A STRONG SMELL OF JET FUEL CIRCULATED ABOUT THE CABIN AND COCKPIT. CREW SWITCHED FROM APU SUPPLIED AIR TO ENGINE AIR AN D FUMES REMAINED/REOCCURRED. COCKPIT CREW DONNED OXYGEN MASKS FOR DURATION OF FLIGHT. CREW NOTED THAT THE FUMES WERE S TRONG ENOUGH TO CAUSE THEM HEADACHES. LANDING IN DTW WAS NORMAL AND PASSENGERS DEPLANED NORMALLY. NO EVIDENCE OF ANY F UEL LEAKING FROM EITHER POWERPLANT, APU, FUEL TANKS, OR FUEL LINES. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008022000199 20080220 00199 WP 2008 2 20 NWAA080479866 1 20080108 A 3397 CONNECTOR DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 775NC 47785 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE TAILCONE CATWALK WAS INOPERATIVE. MAINT ENANCE FOUND THE COMPARTMENT FLOODLIGHTS CONNECTORS WERE CORRODED AND REPLACED THEM. THE LIGHTS WERE OPERATIONALLY CHEC KED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008021900173 20080219 00173 EA 2008 2 19 MASA200800101 1 20080203 A 3610 GG670800053 SENSOR CNDAIR CL600 CL6002D24 1390016 EA BLEED TEMP MALFUNCTIONED A MASA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 07 909FJ 3447 15009 FLT 2816 - SMOKE IN FLIGHT DECK AFTER APU START. MX CHANGED BLEED TEMP SENSOR. 2 L 7 2 4F RT A21EA 2008021900190 20080219 00190 EA 2008 2 19 MASA200800119 1 20080211 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA COCKPIT ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 512MJ 10109 ASH FLT 7401 CLE - NOISE AT ROW 12 RT SIDE ALONG WITH ODOR IN CABIN AND COCKPIT. MX INSPECTED AREA, NO NOISE NOTED AND NO DAMAGE. 2 L 7 2 4F RT A21EA 2008021900201 20080219 00201 NM 2008 2 19 SWAA080736 1 20080209 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 208WN 29856 DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008021900225 20080219 00225 2008 2 19 QXEA200800179 4 20080211 A 2210 7002260723 SERVO DHAV DHC8 DHC8202 2809007 NM AILERONS JAMMED A QXEA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED AP APPROACH 1 NM 09 355PH 18138 1734 500 PDX - FLIGHT 2193 (OTH-PDX) ON APPROACH WITH THE AUTOPILOT ON, EXPERIENCED A UNCOMMANDED ROLL TO THE LEFT. AUTOPILOT WA S TURNED OFF AND THE WHEEL APPEARED TO BE JAMMED (NO MOVEMENT POSSIBLE). CONTROL THEN BECAME UN-JAMMED AND OPERATED NOR MALLY AFTER A FEW SECONDS. LANDED WITH SPOILER CONTROL ONLY. EMERGENCY DECLARED WITH ATC. LANDING UNEVENTFUL. MAINTEN ANCE REPLACED THE AUTOPILOT AILERON SERVO. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008021900227 20080219 00227 EA 2008 2 19 QXEA200800062 1 20080206 A 5210 LC063F6MW SPRING CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR HANDLE BROKEN A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 600QX 10005 ONT - FLIGHT 2624.; AFTER TAKEOFF, THE REAR SERVICE DOOR WARNING LIGHT ILLUMINATED, THEN RECEIVED A PROX SENSOR INDICATI ON. HANDLE ON THE DOOR STARTED TO MOVE UP. THE REAR FLIGHT ATTENDANT WAS UNABLE TO KEEP THE HANDLE DOWN. DIVERTED TO ONT AND ACCOMPLISHED A UNEVENTFUL LANDING. NO EMERGENCY OR CFR CALLED. MAINTENANCE FOUND A BROKEN SPRING ON THE INNER HANDLE DETENT. REPLACED THE SPRING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008021900234 20080219 00234 NM 2008 2 19 SWAA080816 1 20080212 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 750SA 29802 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2008021900250 20080219 00250 NM 2008 2 19 CALA0800090 1 20080129 A 5311 BAC15171470 FRAME BOEING 737 7373T0 1384582 NM BS 380 S8R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12322 23373 CABIN FRAME IS CRACKED AT STA 380 RIGHT ABOVE STRINGER 8R AT SUPPORT BRACKET. REPAIRED PER ECRA 5310-04697. 2 L 7 2 4F RT A16WE 2008021900264 20080219 00264 NM 2008 2 19 QXEA200800090 1 20080114 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 349PH 486 PDX - C1 CHECK - RIVET HEADS ABOVE INNER SKIN ON WEB X528 TO X534 ON THE RIGHT SIDE BELOW SEAT TRACK 8/9 SUSPECT LIGHT C ORROSION. MAINTENANCE REMOVED RIVETS AND BLENDED CORROSION FROM WEB, REMAINED WITHIN LIMITS AND INSPECTED NO CRACKS NOT ED. INSTALLED NEW RIVETS AND RESTORED FINISH TO REPAIR AREA. 2 H 7 2 4T RT A13NM 2008022500365 20080225 00365 NM 2008 2 25 USAA920080420 1 20080208 A 5311 6547959 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q5 CHECK - AFT CARGO COMPARTMENT DOOR CUTOUT FORWARD FRAME CRACKED, BS 800. REPLACED AFT CARGO COM PARTMENT DOOR CUTOUT FORWARD FRAME, BS 800 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008022500366 20080225 00366 EU 2008 2 25 USAA920080421 1 20080210 A 5347 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 271AY 323 BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 4523 / FR 56, +Y450. REPLACED CABIN SEAT TRACK, BS 45 23 / FR 56, +Y450 IAW A330 SRM 51-42-00. 2 L 7 2 4F RT A46NM 2008022500373 20080225 00373 NM 2008 2 25 USAA920080429 1 20080210 A 5330 DOUBLER BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 CLT - MAJOR REPAIR - C2 CHECK - FUSELAGE SKIN INTERNAL DOUBLER CRACKED, BS 328, LBL 3.5 AT THE EQUIPMENT COOLING PORT. REPAIRED FUSELAGE SKIN INTERNAL DOUBLER, BS 328, LBL 3.5 AT THE EQUIPMENT COOLING PORT IAW B737 SRM 53-30-01. 2 L 7 2 4F RT A16WE 2008022500374 20080225 00374 NM 2008 2 25 USAA920080430 1 20080211 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CANNING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 24781 CLT - MAJOR REPAIR - C6 CHECK - FUSELAGE SKIN OIL CANNING, BS 727D - BS 727E, S23R - S24R. REPAIRED FUSELAGE SKIN, BS 7 27D - BS 727E, S23R - S24R IAW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008022500375 20080225 00375 NM 2008 2 25 USAA920080431 1 20080213 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 23886 CLT - MAJOR REPAIR - C4 CHECK - CRACKED FUSELAGE, BS 747, S25R. REPAIRED FUSELAGE SKIN, BS 747, S25R IAW B737 SRM 53-00 -01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008022500377 20080225 00377 2008 2 25 2008UALA00502 4 20080127 A 8300 GEARBOX BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE MAKING METAL A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 549UA 25397 726580 L ENG PRI CONT EICAS MSG DISPLAYED AND NO IND SEC TOOK OVER. INTERNAL GEARBOX FAILURE INDICATED BY LARGE CHUNKS OF META L ON CHIP DETECTORS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500378 20080225 00378 NM 2008 2 25 NOCA 1 20080214 A 3350 276005 FUSE BOEING 757 75728A 1384976 NM CABIN BLOWN A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 752NA 28174 EMERGENCY LIGHTS AT ROW 1 ABC AND 4 ABC OVERHEAD BIN LOCATIONS INOP. REPLACED POWER SUPPLY FUSE AT BOTH LOCATIONS PER M M 33-51-07, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2008022500380 20080225 00380 SO 2008 2 25 FDKA200802056 1 20080213 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FDM 6002 MCO (0640 PHX LCL). EMERGENCY EXIT LIGHT GALLEY EXIT INOP. MX RESECURED/RESET LIGHT ASSY. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008022500383 20080225 00383 SO 2008 2 25 FDKA200802059 1 20080213 A 5320 14522459003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 THE FLOOR SUPPORT AT BL 0 AND FRAME 20 IS CORRODED OUT OF LIMITS. THE DAMAGED SUPPORT HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008022500387 20080225 00387 EU 2008 2 25 USAA920080433 1 20080215 A 2611 RAI2800M0706 CONTROL UNIT AIRBUS 320 A320232 3930326 EU SMOKE DETECTION FAILED A USAA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 19 660AW 11710 7925 1234 PHX - EE - FLT 320 - MX REPORTED SMOKE CARGO LAV FAULT MESSAGE ILLUMINATED. MX REPLACED THE SMOKE DETECTOR CONTROL UNIT (SDCU) 10WQ. OPERATIONAL TEST WAS GOOD. 2 L 7 2 4F RT A28NM 2008022500390 20080225 00390 NM 2008 2 25 NOCA01408 1 20080214 A 3350 276005 FUSE BOEING 757 75728A 1384976 NM CABIN BLOWN A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 752NA 28174 EMERGENCY LIGHTS AT ROW 1 ABC AND 4 ABC OVERHEAD BIN LOCATIONS INOP. REPLACED POWER SUPPLY FUSE AT BOTH LOCATIONS PER M M 33-51-07, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2008022600020 20080226 00020 NM 2008 2 26 ASAA0852543 1 20080210 A 3040 8300005604 CIRCUIT BREAKER BOEING 737 737890 1384527 NM COCKPIT POPPED A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 559AS 35178 RIGHT FWD WINDOW OVERHEAT LIGHT ILLUMINATES ON THE GROUND. FOUND RIGHT FWD WINDOW HEAT POWER C/B ON P6 12 OUT. ACCOMPL ISHED C/B RESET PROCEDURE (REF MM20 60 01), OP CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2008022600026 20080226 00026 NM 2008 2 26 ASAA0852542 1 20080209 A 4950 32912142 BLEED VALVE BOEING 737 737890 1384527 NM APU FAULTY A ASAA K NONE J WARNING INDICATION DE DESCENT 1 NM 02 577AS 35186 THE "DUAL BLEED" LIGHT ILLUMINATED OUT OF 13000'. FLICKERED ON & OFF. ON FINAL APPROACH REMAINED ILLUMINATED UNTIL REA CHING THE GATE. MASTER CAUTION FLICKERED BUT RT SIX PACK DID NOT ILLUMINATE. FOLLOWED FIM 49 51 TASK 801. REPLACED BL EED AIR VALVE. ACCOMPLISHED BITE OF CDU CONFIRMED CURRENT STATUS "NO MAINT MSGS FAULTS". 2 L 7 2 4F RT A16WE 2008022600028 20080226 00028 NE 2008 2 26 MALA080027 2 20080222 A 7310 LINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUEL SYSTEM LEAKING A MALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 15 438XJ 340B438 UPON POWER REDUCTION FOR DESCENT, SUDDEN FUEL AND/OR BURNING ODOR. FOUND SMALL FUEL LEAK AT LINE CONNECTION TO THE FUEL /OIL HEATER, REPLACED O-RING AT FITTING. REMOVED AND REPLACED RT HMU. 2 L 7 2 4T 4 T RT A52EU E8NE 2008022600045 20080226 00045 NM 2008 2 26 DLM88080228 1 20080217 A 5620 5951584505 WINDOW DOUG MD88 MD88 3023688 NM CABIN MISINSTALLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 933DL 49720 CABIN WINDOWS IMPROPERLY INSTALLED RESULTED IN FATIGUE CHIPPING OF 2 OUTER PANES. REPLACED DAMAGED PANES. 2 L 7 2 4F RT A6WE 2008022600059 20080226 00059 SO 2008 2 26 FDKA200802066 1 20080217 A 2621 WARNING MESSAGE EMB 145 EMB145LR 3260212 SO CARGO BAY ACTIVATED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 841MJ 145448 FDM 6177 PNS. BAG EXTINGUISH BOTTLE MESSAGE IN FLIGHT. MX INSPECTED AND OPS GOOD. 2 L 7 2 4T RT T00011AT 2008022600066 20080226 00066 NM 2008 2 26 USAA920080451 1 20080217 A 5310 652072270 DOOR FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 455UW 24997 PIT - MAJOR REPAIR - FPBH INSPECTION - FORWARD CARGO COMPARTMENT DOOR CUT OUT FORWARD FRAME CRACKED, BS 44, S24R. REPAI RED FORWARD CARGO COMPARTMENT DOOR CUTOUT FORWARD FRAME, BS 440, S24R IAW USAIRWAYS EA 110651. 2 L 7 2 4F RT A16WE 2008022500171 20080225 00171 NM 2008 2 25 2008UALA00769 1 20080208 A 2560 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 588UA 26717 DOOR 1R WILL NOT ARM. LANYARD INTERFERENCE. SECURED LANYARD, DOOR ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500192 20080225 00192 2008 2 25 2008UALA00785 4 20080209 A 2330 RECEPTACLE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN MALFUNCTIONED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 793UA 26946 THE 12B LAPTOP POWER OUTLET SMOKED WHEN PLUGGED IN, PER F/A PASSENGER STOPPED USING IT. TESTED PLUG. NO SIGN OF BURNED PINS OR SMOKE DAMAGE. UNABLE TO DUPLICATE PROBLEM. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008022500198 20080225 00198 NM 2008 2 25 2008UALA00790 1 20080209 A 2612 M10427 CIRCUIT CARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE DETECTION FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 554UA 26644 AFT CARGO FIRE WARNING SYSTEM INOPERATIVE. INDICATION ISSUE WITH FIRE DET CIRCUIT CARD. REPLACED BOTH FWD AND AFT FIRE DET CIRCUIT CARDS, ACCOMPLISHED ALL CHECKS FOR SYSTEM OPS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500206 20080225 00206 NM 2008 2 25 2008UALA00799 1 20080212 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 FUSELAGE FRAME AT BS 1600 STR 26L AND BS 1320 STR 28L IS DAMAGED. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500221 20080225 00221 NM 2008 2 25 2008UALA00816 1 20080212 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 Z-ANGLE UPPER SURFACE FROM BS 962 TO 976 IS CORRODED AT AFT GALLEY SERVICE DOOR CUTOUT. MAJOR REPAIR ACCOMPLISHED: REM OVED & REPLACED STR 17R FLOOR CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500231 20080225 00231 NM 2008 2 25 2008UALA00822 1 20080213 A 3213 161N12204 CYLINDER BOEING 161N0001133 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT MLG CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 RIGHT OUTER CYLINDER HAS CORROSION. REMOVED GEAR, SENT TO SHOP FOR REWORK AND REINSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500243 20080225 00243 NM 2008 2 25 2008UALA00831 1 20080214 A 2916 RESERVOIR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYDRAULIC SYS MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 545UA 25323 R HYD RESERVOIR PRESSURE EICAS AND ASSOCIATED OVERHEAD AMBER ILLUMINATED. REPLACED RESERVOIR AND ALL SWITCHES AND SENSO RS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500289 20080225 00289 NE 2008 2 25 DL757080183 2 20080210 A 7261 FILTER BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE UNKNOWN A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 6716C 65333 30838 716330 AFTER TAKEOFF, THE LEFT ENGINE OIL PRESS FLUX TO YELLOW BAND, THEN OIL QTY WENT TO ZERO. OIL PRESS THEN WENT TO RED. C REW THEN SHUT ENGINE DOWN. FOUND SCAVENGE LINE CHIP DETECTOR LAYING IN COWL. INSP CHIP DET POP OUT CHK VLV. FOUND SM ALL PIECE OF SAFETY WIRE HOLDING CHK VLV OPEN. REPLACED CHIP DET AND POP OUT CHK VLV. RAN ENG AND NO LEAKS. REPLACED AND INSP MAIN ENG OIL FILTER. NO CONTAMINATION FOUND. RAN ENG NO LEAKS. ENG OIL SERVICED TO FULL. REPLACED ENGINE PE R TRAN 6T103 NR 1 ENGINE CHANGE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500297 20080225 00297 NM 2008 2 25 AALA200800287 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 24G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022500311 20080225 00311 WP 2008 2 25 VGCA20080212 1 20080212 A 2612 356080765 FIRE DETECTOR CVAC 440 440 2422902 WP MALFUNCTIONED A VGCA F E B A ACTIVATE FIRE EXT. ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 361FL 790 790 343 RT ZONE 1 FIRE ALARM CAME ON JUST BEFORE LEVELING AT 12000', CREW FOLLOWED EMERGENCY PROCEDURES TO SHUTDOWN AND SECURE E NGINE. 2 L 7 2 4R 6A6 2008022500334 20080225 00334 NE 2008 2 25 DL76G080247 2 20080219 A 7200 CF680C2B6F ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 POWER LOSS A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1613B 46022 32776 704234 NR 2 ENGINE REPLACED DECLINING PERFORMANCE. 2 L 7 2 4F 4 F RT A1NM E13NE 2008022500346 20080225 00346 NM 2008 2 25 USAA920080412 1 20080130 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 CLT - MAJOR REPAIR - C2 CHECK - CRACKED FORWARD PRESSURE BULKHEAD, BS 178, LBL 115, WL 218. REPAIRED FORWARD PRESSURE B ULKHEAD, BS 178, LBL 115, WL 218 IAW USAIRWEAYS EA 100230. 2 L 7 2 4F RT A16WE 2008022500381 20080225 00381 SO 2008 2 25 FDKA200802057 1 20080214 A 5210 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6083 MCO (1010 PHX LCL). MAIN CABIN DOOR DIFFICULT TO OPEN. MX LUBED SEAL, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008022500384 20080225 00384 SO 2008 2 25 FDKA200802060 1 20080214 A 5420 ANGLE EMB 145 EMB145LR 3260212 SO LT COWLING CHAFED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 THE O/B FRAME ANGLE, JUST AFT OF THE AFT HINGE, ON THE LT LOWER ENGINE COWLING IS CHAFED. THE DAMAGE HAS BEEN REPAIRED. 2 L 7 2 4T RT T00011AT 2008022500393 20080225 00393 EU 2008 2 25 BA08006 1 20080217 A 3040 A5398117400200 ATTACH FITTING AIRBUS 330 A330323 3930335 EU EVAC SLIDE INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AY 0375 CWF - THE FORWARD, MAIN ENTRY DOOR EMERGENCY ESCAPE SLIDE ATTACH FITTING ICE PROTECTION WAS FOUND INOPERATIVE. MAINTENA NCE REPLACED HEATED ATTACH FITTING. OPS CHECKED OK. 2 L 7 2 4F RT A46NM 2008022500394 20080225 00394 NM 2008 2 25 USAA920080449 1 20080113 A 5755 6546451605P SKIN BOEING 737 7373S3 1384711 NM NR 7 SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - RIGHT WING NR 7 SPOILER UPPER SURFACE HAS DELAMINATION. REPAIRED RIGHT WING NR 7 SPOIL ER UPPER SURFACE IAW B737 SRM 51-70-10-2R REPAIR 4. 2 L 7 2 4F RT A16WE 2008022600050 20080226 00050 NM 2008 2 26 AALA200800332 1 20080207 A 5330 SKIN BOEING 767 767323 1385205 NM BS 1518-1554 SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 358AA 24039 AFW - FUSELAGE SKIN AT STATION 1518 TO 1554 HAS 48 INCH LONG SCRATCH THAT CROSSES THE LAP SPLICE BETWEEN STATION 1518, S KIN PANEL 146T3230, AND STATION 1554, SKIN PANEL 146T3240, AND EXTENDS FROM STRINGER S34L TO S39R, AREA IS 48 INCHES BY 1 INCH WITH AT DEPTH OF .057 AND .056 INCH. BLENDED AND SMOOTHED GOUGE. REMOVED FASTENERS WITHIN 1.5 DIAMETER OF BLEND ED REGION. ALL FASTENER LOCATIONS HAVE A 2 DIAMETER FLAT AREA. MAINTAINED A BLEND RATIO OF 20 TO 1. ACCOMPLISHED A HI GH FREQUENCY EDDY CURRENT TO INSPECT FOR CRACKS. REINSTALLED FASTENERS AND APPLIED ALODINE 1000 TO BLENDED AREAS. 2 L 7 2 4F RT A1NM 2008022600055 20080226 00055 NM 2008 2 26 ASAA0842565 1 20080112 A 5313 654657959 STRINGER BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 CORROSION FOUND ON LOWER TEE STRINGER AT APU INLET TORQUE BOY RT SIDE. CORROSION ON LOWER TEE STRINGER WAS BLENDED OUT AND FOUND BEYOND ALLOWABLE IAW B737 400 SRM 53 80 13. REMOVED TEE STRINGER AND INSTALLED NEW PART IAW B737 400 SRM 51 4 0 02. 2 L 7 2 4F RT A16WE 2008022600068 20080226 00068 EU 2008 2 26 USAA920080450 1 20080219 A 2611 RAI2800M0706 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU CARGO BAY DEFECTIVE A USAA K NONE N FALSE WARNING UK UNKNOWN 1 EA 19 659AW 22277 22277 1166 FLT 920 - PHX-PDX - EE - CARGO SMOKE DETECTOR FAULT. MAINTENANCE REMOVED AND REPLACED THE SMOKE DETECTOR CONTROL UNIT A ND CARGO SMOKE DETECTOR. OPERATIONAL CHECK WAS GOOD. CARGO SMOKE DETECTOR, MFR SIEMENS, MPN PPA1102-00, MSN 2199, TOTA L TIME 21393, TOTAL CYCLES 8207, TIME SINCE REPAIR 406. 2 L 7 2 4F RT A28NM 2008022600073 20080226 00073 WP 2008 2 26 AALA200800327 1 20080215 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 232AA 49179 LGA - EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. SECURED WIRE FOR EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F A6WE 2008022600075 20080226 00075 NM 2008 2 26 G8GA20080006 1 20080215 A 2782 269002916 ACTUATOR BOEING 727 727227 1384078 NM NR 2 SLAT MALFUNCTIONED A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 308AS 22002 FLT 715 FROM HRL TO MEM. DURING CLIMB OPERATION ON FLAP RETRACTION THE NR 2 LEADING EDGE SLAT WOULD NOT RETRACT. CREW P ERFORM REQUIRED PROCEDURES AND RETURNED TO HRL WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 SLAT ACTUATOR WAS REMOVED AND REPLACED, OPS AND LEAK CHECKED GOOD. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2008022600078 20080226 00078 NM 2008 2 26 ASAA0842612 1 20080117 A 5311 65C323511 FRAME BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 BS 500 E FUSELAGE FRAME CRACKED AT FASTENER HOLE BETWEEN STR 13L 14L BS 500 E. FRAME BETWEEN STA 13L AND 14L REPAIRED I AW ASA EO 5310 02642 AND ASA DRAWING A 53100264248. 2 L 7 2 4F RT A16WE 2008022600081 20080226 00081 NM 2008 2 26 AALA200800305 1 20080212 A 3350 P4010051112 CONTROL MODULE BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 695AN 26975 MCO - EMERGENCY LIGHTS AT SEAT ROWS 26 TO 32 AND EXIT IDENTIFIERS AT LEFT AND RIGHT NUMBER FOUR DOORS INOPERATIVE. REPL ACED CONTROL MODULE AT STATION 1480 FOR EMERGENCY LIGHTS AT SEAT ROWS 26 TO 32 AND EXIT IDENTIFIERS AT LEFT AND RIGHT NU MBER FOUR DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008022600083 20080226 00083 NM 2008 2 26 ASAA0842613 1 20080130 A 5320 69265553 ANGLE BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 BS 348.5 STR I5L & 16L 8 HOLES CRACKED. FRAME FOUND NOT TO BE CRACKED. ANGLE AT BS 348 STR 16 LT FOUND CRACKED AT FAST ENER HOLES AND REPLACED WITH NEW PART IAW B737 400 SRM 51 40 02. 2 L 7 2 4F RT A16WE 2008022600084 20080226 00084 NM 2008 2 26 DL764080251 1 20080217 A 4990 LINE BOEING 767 767432ER 1385134 NM APU OIL SYSTEM LEAKING A DALA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 27 843MH P1043 29716 APU LEAKING OIL AT SCAVENGE LINE FITTING TURBINE BEARING. REMOVED AND REPLACED APU PER TRANSMITTAL 14T102 OP AND LK CK OK. 2 L 7 2 4F RT A1NM 2008022600085 20080226 00085 NM 2008 2 26 P5CA0801544 1 20080218 A 5510 STRUCTURE BOEING 747 74746NF 13848BT NM HORIZONTAL STAB DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 451PA 30809 DURING GROUND HANDLING AND PREFLIGHT WALK AROUND FLIGHT CREW FOUND 3 DENTS TO THE LEFT LEADING EDGE OF THE HORIZONTAL ST ABILIZER. AN INTERIM REPAIR WAS COMPLETED WITH A DVI EVERY 5 FLIGHT CYCLES AS PER MA A45510-01:01 AND SRM 55-10-01 FIG 201. 2 L 7 4 4F RT A20WE 2008022600086 20080226 00086 NM 2008 2 26 ASAA0842614 1 20080105 A 5310 655484221 SKATE ANGLE BOEING 737 7374S3 1384711 NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 CHAFING DAMAGE FOUND ON VERTICAL STAB TO FUSELAGE LT SKATE ANGLE. CHAFING DAMAGE FOUND ON VERTICAL STAB TO FUSELAGE AT LT SKATE ANGLE REPAIRED IAW ALASKA EA 5310 02769. 2 L 7 2 4F RT A16WE 2008022600087 20080226 00087 NM 2008 2 26 ASAA0842630 1 20080117 A 5311 6545816501 FRAME BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 CORROSION ON BS 328 FRAME AT STR 28R. CORROSION ON FRAME AT BS 328 STR 28R BLENDED BEYOND LIMITS IAW B737 400 SRM 53 10 07 FIG 1. REPAIR PART MADE FROM 0.0407 7075TG PDH 10978S AND 0.052" 7075TG PDH 11425 IAW B737 400 SRM 53 00 07. REPAIR 5 FIG 201. REPAIR PART INSTALLED IAW B737 400 SRM 51 40 02. 2 L 7 2 4F RT A16WE 2008022600089 20080226 00089 NM 2008 2 26 ASAA0842632 1 20080117 A 5311 654653161 FRAME BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 BS 520 FUSELAGE FRAME CRACKED AT FASTENER HOLE BETWEEN STR 13L 14L. REPAIRED WITH MADE REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600090 20080226 00090 NM 2008 2 26 ASAA0842633 1 20080117 A 5311 65C323962 FRAME BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 BS 727 G FUSELAGE FRAME CRACKED AT FASTENER HOLE BETWEEN STR 13L 14L. REPAIRED WITH MADE REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600091 20080226 00091 NE 2008 2 26 P5CA0801545 2 20080220 A 7261 1163M64P07 CARBON SEAL BOEING 747 74746NF 13848BT NM GE CF6 CF680C2B2 30025 NE NR 4 ENGINE LEAKING A P5CA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 453PA 30811 "ENG 4 OIL PRESSURE" ENG 4 SHUT DOWN DUE TO ZERO OIL QUANTITY/LOW PRESS AFTER SHUT DOWN OIL PRESS REMAINED 7PSI. SERVED ENG OIL WITH 25 QTS ACCOMPLISHED ENG MOTORING AND FOUND LEAK ON IDG DRAIN PORT. REPLACED NR 4 ENG IDG CARBON SEAL. AC COMPLISHED ENG RUN AND NO LEAK FOUND AMM 24-11-01. 2 L 7 4 4F 4 F RT A20WE E13NE 2008022600103 20080226 00103 NM 2008 2 26 2008UALA00756 1 20080209 A 3350 81781 BALLAST BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 MAIN STAIRS EMERGENCY LIGHTS INOP. REPLACED BALLAST. LIGHTS OP CHECK GOOD. A/C OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022600104 20080226 00104 NM 2008 2 26 2008UALA00757 1 20080208 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 1J MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 127UA 28813 FOUND SEAT 1J EMERGENCY LIGHT MISSING. REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022600108 20080226 00108 NM 2008 2 26 2008UALA00760 1 20080210 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FLUCTUATES A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY FLOOR PATH LIGHTS FLICKER ON AND OFF AT ROWS 5, 6 AND 7. COULD NOT DUPLICATE FAULT. AS PRECAUTION, REPLACED M 7925 BATTERY AND M6003 POWER SUPPLY PER MM 33-51-04. SHOOK HARNESSES LOCALLY -- NO FLICKERING NOTED. OBSERVED SYSTEM FOR EXTENDED PERIOD WITH NO FAULTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022600121 20080226 00121 NM 2008 2 26 ASAA0842598 1 20080124 A 5320 694147328 INTERCOSTAL BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO RBL 21 INTERCOSTAL CRACKED AT BS 500 D TO 500 E. CASCADE RESPONSIBILITY INTERCOSTAL REPLACED. 2 L 7 2 4F RT A16WE 2008022600123 20080226 00123 NM 2008 2 26 ASAA0842602 1 20080115 A 5347 65C314838 SEAT TRACK BOEING 737 7374S3 1384711 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 SEAT TRACK GOUGED STA 727 B+ (4" 7") LBL 25. REPAIRED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008022600124 20080226 00124 NM 2008 2 26 ASAA0842604 1 20080115 A 5347 6546813U109 SEAT TRACK BOEING 737 7374S3 1384711 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 SEAT TRACK AT STA 536 RBL 45 GOUGED. REPAIRED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008022600125 20080226 00125 NM 2008 2 26 ASAA0842605 1 20080116 A 5320 654659247 CHANNEL BOEING 737 7374S3 1384711 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 TRANSFERRED FROM NR 5116889 BEYOND LIMITS DAMAGE TO FLOOR CHANNEL BS 767+4 LBL 8 AFT CARGO PIT. REPAIRED WITH REPAIR PA RT. 2 L 7 2 4F RT A16WE 2008022600142 20080226 00142 NM 2008 2 26 2008UALA00819 1 20080212 A 3250 AS1582T08 METERING VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG STEERING FAULTY A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 556UA 26650 ON TAXI-OUT TO RUNWAY, ON RH TURN AN AUDIBLE POP WAS HEARD AND NWS TILLER IS STUCK TO THE RIGHT. AFTER EXTENSIVE TROUBL E SHOOTING, THE METERING VALVE WAS REPLACED AND ISSUE WENT AWAY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022600151 20080226 00151 EU 2008 2 26 USAA920080457 1 20080214 A 5320 D53471124201 SHEAR PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON RIGHT HAND CABIN LATERAL SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70. R EPLACED RIGHT HAND CABIN LATERAL SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022600152 20080226 00152 EU 2008 2 26 USAA920080458 1 20080214 A 5320 D53471124200 SHEAR PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON LEFT HAND CABIN LATERAL SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70. RE PLACED LEFT HAND CABIN LATERAL SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022600160 20080226 00160 SO 2008 2 26 FDKA200802071 1 20080219 A 5210 DOOR EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FDM 6183 MCO-RDU (1102 PHX LCL). MAIN CABIN DOOR DIFFICULT TO OPEN. MX LUBED DOOR, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008021900286 20080219 00286 NM 2008 2 19 GTIA0800004 1 20080129 A 5210 D5211006820000 HOOK AIRBUS A319 A319132 3930340 NM L1 DOOR GALLED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 521NK 2797 L1 DOOR GEARBOX LOCK HOOK GALLED. REPLACED DOOR GEARBOX LOCK HOOK OAW AMM 52-11-21-400-001. 2 L 7 2 4F RT A28NM 2008021900288 20080219 00288 NM 2008 2 19 GTIA0800003 1 20080128 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 521NK 2729 FLOORBEAM AT STA -765 BETWEEN FRAMES 66 AND 68 SHOWS SIGNS OF CORROSION. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2008021900315 20080219 00315 NM 2008 2 19 SWAA080689 1 20080206 A 5753 6546434369 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED C2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED FLAP P ER MM. 2 L 7 2 4F RT A16WE 2008021900321 20080219 00321 NM 2008 2 19 SWAA080758 1 20080210 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT E&E EQUIPMENT COOLING EXHAUST DUCT. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008021900337 20080219 00337 NM 2008 2 19 SWAA080752 1 20080210 A 5313 BAC1498 STRINGER BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED SPV CHECK, FOUND STRINGER 27L CORRODED AT BS 503 TO BS 512B. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008021900356 20080219 00356 NM 2008 2 19 SWAA080823 1 20080213 A 5330 6545778 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STR 13R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008021900357 20080219 00357 NM 2008 2 19 SWAA080824 1 20080213 A 5311 6547955 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR AFT FRAME CRACKED AT BS 847, STR 25R. REMOVED AND REPLACED FRAME PER A CO. 2 L 7 2 4F RT A16WE 2008021900366 20080219 00366 NM 2008 2 19 SWAA080850 1 20080213 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 14R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008022000063 20080220 00063 NE 2008 2 20 ASMF200801002 2 20080124 A 7230 BLADES DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE ENGINE DAMAGED W ASMF K NONE C F.O.D. IN INSP/MAINT 1 SW 23 803ML 49726 725965 DURING OVERNIGHT CHECK, 10 FAN BLADES OF THE RT ENG WERE DETECTED WITH DENTS AND LOSS OF MATERIAL DUE TO AN FOD. MAINTEN ANCE PERFORMED A BOROSCOPIC INSP IAW MM 72-00-00 AND NO ADDITIONAL DAMAGES WERE FOUND; THE 10 DAMAGED BLADES WERE REPAI RED IAW MM 72-33-21, AFTER REPAIRS, 2 BLADES WERE RESTRICTED TO ONLY 24 HOURS CONTINUE-IN-SERVICE CONDITION, SO DURING T HE NEXT OVERNIGHT CHECK AT MEX, THE C1 DISK WAS REPLACED AND TESTED IAW MM 72-33-02 AND 71-00-00, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2008022000082 20080220 00082 SO 2008 2 20 C2XA08IA047 1 20080119 A 2797 W502003324GR WIRE EMB 145 EMB145XR 3260214 SO LT WING BROKEN A C2XA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SW 27 17108 145655 IAH - FLIGHT 2392, THE CREW REPORTED A SPOILER FAIL WITH A SPOILER OPEN INDICATION WITH THE SPOILERS CLOSED. THE CREW P ERFORMED AN EMERGENCY DESCENT, AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED A BR OKEN WIRE ON THE LEFT HAND INBOARD SPOILER PROXIMITY SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008022000087 20080220 00087 NM 2008 2 20 HALA0800129 1 20080108 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1099 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 LIGHT CORROSION FOUND IN SEAT TRACK, SECTION 46, LBL 88.5, STA 1099. CORROSION BLENDED OUT AND DEPTH ASSESSED, IAW SRM 53-00-52, ALLOWABLE DAMAGE 1, AND FOUND TO BE WITHIN LIMITS. RE-WORKED AREAS ALODINED AND PAINTED IAW SRM 53-00 -52 AND SOPM 20-41-04. LPS3 APPLIED TO SEAT TRACK. 2 L 7 2 4F RT A1NM 2008022000090 20080220 00090 WP 2008 2 20 070187 1 20080214 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 895GA 49667 IT HAS BEEN REPORTED BY THE FLIGHT CREW THE EMERGENCY EVACUATION LIGHTING SYSTEM HAS BEEN FOUND TO BE DEFECTIVE. MAINTE NANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS. AN OP ERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2008022000143 20080220 00143 NM 2008 2 20 SWAA080847 1 20080213 A 5340 65C27314 STRINGER CLIP BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022000176 20080220 00176 SO 2008 2 20 C2XA08IA046 1 20080201 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 17138 145727 ORF - FLIGHT 2113, THE CREW REPORTED A STRONG ODOR POSSIBLY ELEC IN FLIGHT. THE AIRCRAFT LANDED AT ORF WITHOUT INCIDENT . MAINTENANCE INSPECTED THE AIRCRAFT, VERIFIED NO EICAS MESSAGES OR OTHER DISCREPANCIES. OPERATIONALLY CHECK ELECTRICA L SYSTEMS WITH NO DEFECTS NOTED, AND THE AIRCTRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2008022000179 20080220 00179 SO 2008 2 20 C2XA08TY028 1 20080205 A 5311 12010732001 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13949 145057 TYS MOD - DURING ROUTINE MX FOUND FRAME 81 CRACKED AT THE 6 O'CLOCK POSITION. THE FRAME WAS REMOVED AND REPLACED IAW SR M 51-40-02 AND A/C WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008022000181 20080220 00181 SO 2008 2 20 SIMA200804301 1 20080110 A 2900 UNKNOWN EMB 145 EMB145LR 3260212 SO UNKNOWN A SIMA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 928AE 14500911 ON FLIGHT 3686 - CREW REPORTED AUTOPILOT DISENGAGED WITH RUDDER 1-2 INOP EICAS MESSAGE.AFTER A FEW SECONDS, THE MESSAGE DISAPPEARED. THE CREW RE-ENGAGED THE AUTOPILOT AND THE MESSAGE RETURNED. THE CREW FOLLOWED THE PROCEDURE IN THE AOM AN D THE RUDDER SYSTEM 2 WAS TURNED OFF. THE DECISION WAS MADE TO DECLARE AN EMERGENCY. THE FLIGHT CONTINUED WITHOUT FURT HER INCIDENT AND LANDED SAFELY. AIRCRAFT REMOVED FROM SERVICE. PRESSURIZE HYDRAULIC SYSTEM IAW EMB-145 AMM 29-10-00. NO RUDDER SYS EICAS MSG SHOWN, FOLLOWED FIM 27-23-00-810-802 A, CONNECTED PITO/STATIC SYS TEST TO SIMULATE AIR SPEED TO 140 KNOTS IAW EMB-145 AMM 34-13-00 RUDDER SYS 2 INOP EICAS MESSAGE NOT SHOWN ON EICAS, CAN NOT DUPLICATE AT THIS TIME, A 2 L 7 2 4T RT T00011AT 2008022000197 20080220 00197 WP 2008 2 20 NWAA080469860 1 20080212 A 3350 LIGHT DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 769NC 47757 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE VENTRAL STAIRWAY WAS INOPERATIVE. MAINT ENANCE REPLACED THE LIGHTS AND OPERATIONAL CHECKED THE SYSTEM. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008022000204 20080220 00204 SO 2008 2 20 SIMA200805003 1 20080213 A 5540 NAS65947 ROD END EMB 135 EMB135LR 3260305 SO RUDDER CORRODED A SIMA O OTHER E VIBRATION/BUFFET DE DESCENT 1 SW 21 736DT 145388 ON FLIGHT 4632, CREW REPORTED STABILIZER VIBRATION DURING CLIMB. AIRCRAFT REMOVED FROM SERVICE. PERFORMED W/C 12-20-01 VIBRATION AND FOUND RUDDER ROD END BEARING GREASE COVER AND CORRODED. REPLACED ROD END IAW EO EM-55AD-201R6. ALL CHEC KS GOOD AND NR 8194; AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008022000209 20080220 00209 SO 2008 2 20 C2XA08TY025 1 20080205 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT SMOKE A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 13978 145180 GSP - DURING CLIMB THE CREW HAD A LAV SMOKE INDICATION ON EICAS WITH VISIBLE SMOKE AND SMOKE SMELL. CREW AIR RETURNED T O GSP, MX PERFORMED HIGH POWER ENG RUNS FOR APPROXIMATELY 3 MINUTES AND COULD NOT DUPLICATE DISCREPANCY. A/C WAS RETURN ED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022000212 20080220 00212 WP 2008 2 20 070186 1 20080207 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 877GA 53467 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008022000216 20080220 00216 NM 2008 2 20 QXEA200800204 1 20080216 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM UNKNOWN A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 425QX 4039 PSC - AFT PASSENGER DOOR WILL NOT CLOSE. PSC MAINTENANCE COMPLIED WITH DH8-400 SL 52-003A. OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008022000221 20080220 00221 NM 2008 2 20 HALA0800120 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 970 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 2 CORROSION SECTION 45 SEAT TRACK AT LBL 88.5, STA 970, SEAT TRACK REPLACED. 2 L 7 2 4F RT A1NM 2008022000223 20080220 00223 NM 2008 2 20 HALA0800139 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1012 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SECTION 45 SEAT TRACK CROWN DAMAGED (SCRATCHES/GOUGES) AT LBL 54.75, BS 1012. REWORKED IAW SRM 51-10-02 REV 76 WITHIN L IMITS. ALODINED PER SRM 51-20-01 REV 76. PRIMED PER AMM 51-21-00, REV 67. 2 L 7 2 4F RT A1NM 2008022000227 20080220 00227 NM 2008 2 20 HALA0800087 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 882 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION ON SEAT TRACKS AT BS 882. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 51-10-02, REV 76, BLENDED WITHIN LIMITS, IAW SRM 53-00-52/101, REV 76. 2 L 7 2 4F RT A1NM 2008022000230 20080220 00230 NM 2008 2 20 HALA0800140 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 808-820 GOUGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SECTION 54 SEAT TRACK DAMAGED, CROWN GOUGED, AT LBL 54.75, BS 808-820. REMOVED DAMAGE PER SRM 51-10-02 REV 75. REWORK WITHIN LIMITS PER SRM 53-00-52/101 REV 75. ALODINED PER SRM 51-20-01, REV 75. PRIMED PER AMM 51-21-00, REV 67. 2 L 7 2 4F RT A1NM 2008022000242 20080220 00242 NM 2008 2 20 HALA0800101 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 955 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45 SEAT TRACK AT RBL 11, STA 955. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 5 1-10-02, REV 75, BLENDED WITHIN LIMITS, IAW SRM 53-00-52/101 REV 76. 2 L 7 2 4F RT A1NM 2008022000247 20080220 00247 NM 2008 2 20 HALA0800099 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 884-893 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45 SEAT TRACKS AT RBL 11, STA 884-893. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 51-10-02, REV 75, BLENDED WITHIN LIMITS, IAW 53-00-52/101 REV 76. 2 L 7 2 4F RT A1NM 2008022000250 20080220 00250 NM 2008 2 20 HALA0800096 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 808 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45, SEAT TRACK AT RBL 11, STA 808. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 51-10-02, REV 75, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101 REV 76. 2 L 7 2 4F RT A1NM 2008022000254 20080220 00254 NM 2008 2 20 HALA0800110 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 809 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45 SEAT TRACKS AT LBL 11, STA 809. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 51-10-02, REV 76, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101 REV 75. 2 L 7 2 4F RT A1NM 2008022000256 20080220 00256 NM 2008 2 20 HALA0800136 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 878 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SECTION 45 SEAT TRACK CROWN DAMAGED (SCRATCHED/GOUGED) AT LBL 54.75, BS 878. REWORK IAW SRM 51-10-02 REV 76, WITHIN LIM ITS, PER SRM 53-00-52 REV 76. ALODINED PER SRM 51-20-01 REV 76. PRIME PER AMM 51-21-00 REV 67. 2 L 7 2 4F RT A1NM 2008022000257 20080220 00257 NM 2008 2 20 HALA0800137 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 952 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SECTION 45 SEAT TRACK CROWN DAMAGED (SCRATCHES/GOUGES) AT LBL 54.75, STA 952. REWORKED IAW SRM 51-10-02, REV 76. WITHIN LIMITS PER SRM 53-00-52, REV 76. ALODINED PER SRM 51-20-01 REV 76. PRIME PER AMM 51-21-00, REV 67. 2 L 7 2 4F RT A1NM 2008022000264 20080220 00264 NM 2008 2 20 HALA0800094 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 791-797 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION AT SECTION 45 SEAT TRACKS AT RBL 11, STA 791-797. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION I AW SRM 51-10-02,REV 75, BLENDED WITHIN LIMITS, IAW SRM 53-00-52 REV 76. 2 L 7 2 4F RT A1NM 2008022000274 20080220 00274 NM 2008 2 20 F3LA200800058 1 20080130 A 5321 D5367200000061 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 5503 2019 DURING C3/S1 C CHECK, INSPECTION REPORTED A PUNCTURE WAS FOUND IN THE FORWARD CARGO COMPARTMENT FLOOR PANEL, 131VG. MAI NTENANCE REPAIRED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, PAGES 14 AND 15, STEPS A-M. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008022000282 20080220 00282 SO 2008 2 20 C2XA08IA054 1 20080206 A 2130 12039715001 FLAPPER VALVE EMB 145 EMB145LR 3260212 SO CABIN PRESSURE INOPERATIVE A C2XA O OTHER O OTHER CL CLIMB 1 SW 27 16571 145633 IAH - FLIGHT 2582 - THE CREW REPORTED THAT THE PRESSURIZTION FAILED IN AUTO AND MANUAL AFTER TAKEOFF. THE AIRCRAFT RETU RNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE GROUND AIR CONDITIONING FLAPPER VALV E, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022000285 20080220 00285 SO 2008 2 20 C2XA08IA056 1 20080209 A 3350 3104404 FUSE EMB 145 EMB145EP 3260221 SO CABIN BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14925 145004 IAH - DURING MAINTENANCE INSPECTION THE BOTH LT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE FUSE FOR THE EMERGENCY LIGHTS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008022000286 20080220 00286 SO 2008 2 20 C2XA08IA057 1 20080207 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11192 14500936 AUS - DURING MAINTENANCE INSPECTION, THE LOWER RIGHT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008022000288 20080220 00288 SO 2008 2 20 C2XA08ON090 1 20080212 A 3350 20131A BATTERY EMB 145 EMB145XR 3260214 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14180 4996 4996 14500900 FLT MX - ONT - WHILE PERFORMING INTERVALS 2A CHECK AT ONT AND PERFORMING AN OPERATIONAL CHECK FOR THE EMERGENCY LIGHTING SYSTEM, THE MX TECHNICIAN FOUND THAT THE EMERGENCY LIGHT IN GALLEY AREA WAS INOP. MX PERSONNEL REMOVED AND REPLACED TH E EMERGENCY LIGHT BATTERY NR 2 LOCATED ABOVE THE SERVICE DOOR, OPERATIONALLY CHECKED SATISFACTORY. A/C WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008022000290 20080220 00290 SO 2008 2 20 C2XA08RI018 1 20080204 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN & COCKPIT ODOR A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 13997 145298 FLIGHT 2491 - EWR - CREW REPORTED STRONG SMELL IN CABIN AND FLIGHT DECK. CREW PERFORMED AN AIR RETURN AND LANDED UNEVEN TFULLY. EWR MX PERFORMED VISUAL INSPECTION OF BOTH ENGINE INLET ZERO BEARING AND NO OIL LEAK WAS FOUND. MX ALSO RUN AP U, AND BOTH ENGINES AND BOTH PACKS, BUT COULD NOT DUPLICATE THE SMELL. PERFORMED ICE TEST, BUT COULD NOT DUPLICATE THE SMELL. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022000301 20080220 00301 2008 2 20 C2XA08IA061 4 20080214 A 2300 7013270965 RMU EMB 135 EMB135LR 3260305 SO COCKPIT INOPERATIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 17513 13229 11824 145292 IAH - FLIGHT 2671, THE CREW REPORTED SMOKE FROM THE NUMBER TWO RADIO MANAGEMENT UNIT. THE AIRCRAFT LANDED AT IAH WITHOU T INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO RADIO MANAGEMENT UNIT, OPERATIONALLY CHECKED WITH NO DE FECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008022000302 20080220 00302 2008 2 20 YENA2008014 4 20080201 A 2565 L32A319160001 CONTROL CABLE AIRBUS 320 A320232 3930326 EU EVAC SLIDE STIFF A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 613JB 11360 11360 2449 ON C2-01 CHECK, RIGHT HAND OVERWING SLIDE FLEXIBLE CONTROL CABLE STIFF AND FAILS TO RETRACT FOR OPS TEST. REMOVED AND R EPLACED RT FLEXIBLE CONTROL CABLE ASSY PER AMM 25-62-43-04, OPS CHECK OK. 2 L 7 2 4F RT A28NM 2008022000312 20080220 00312 NM 2008 2 20 MWEA080031 1 20080214 A 2422 R25124 RELAY BOEING 717 717200 1383700 NM ELECTRICAL SYS FAILED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 908ME 55172 BUSS AC "EMERGENCY OFF" LIGHT ILLUMINATED. REMOVED AND REPLACED RELAY. 2 L 7 2 4F TR A6WE 2008022000318 20080220 00318 NM 2008 2 20 MWEA080012 1 20080121 A 3350 6011779 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 920ME 55182 AFT OVERWING EVACUATION LIGHT STAY ON WHEN EMERGENCY LIGHT IS SWITCHED OFF. REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F TR A6WE 2008021900287 20080219 00287 NM 2008 2 19 GTIA0800007 1 20080126 A 5210 D5211006820000 HOOK AIRBUS A319 A319132 3930340 NM L2 DOOR GALLED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 521NK 2797 L2 DOOR GEARBOX LOCK HOOK GALLED. REPLACED LOCK HOOK IAW AMM 52-11-21-400-001. 2 L 7 2 4F RT A28NM 2008021900309 20080219 00309 NM 2008 2 19 HALA0800040 1 20080111 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION ON SEAT TRACK,SECTION 45,RBL 54.75 AT SEVERAL LOCATIONS. CORROSION BLENDED OUT AND DEPTH ASSESSED IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 AND FOUND TO BE WITHIN LIMITS. REWORKED AREAS ALODINED AND PAINTED IAW SRM 53-00-52 AN D SOPM 20-41-04. LPS-3 APPLIED TO SEAT TRACK. 2 L 7 2 4F RT A1NM 2008021900311 20080219 00311 NM 2008 2 19 HALA0800041 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1186 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 SEAT TRACK AT BS 1186 RBL 88.5, CORROSION BEYOND SRM LIMITS. REPLACED SEAT TRACK IAW 767-300 SRM 53-00-52, FIG 201 REPA IR 3. 2 L 7 2 4F RT A1NM 2008021900323 20080219 00323 NM 2008 2 19 SWAA080741 1 20080208 A 5755 654645258 HINGE FITTING BOEING 737 7373H4 1384600 NM NR 4 SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED SPV CHECK, FOUND LT WING NR 4 GROUND SPOILER NR 3 HINGE FITTING CRACKED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2008021900331 20080219 00331 NM 2008 2 19 SWAA080762 1 20080210 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008021900338 20080219 00338 NM 2008 2 19 SWAA080751 1 20080210 A 5330 6545767 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, BL 0. REPAIRED SKIN P ER EA. 2 L 7 2 4F RT A16WE 2008022000168 20080220 00168 NM 2008 2 20 HALA0800060 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 654 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION ON SEAT TRACK ST. 654 + 44/ + 66, RBL 11. REWORKED AREA, REPAINTED WITH ALUMINIZED PRIMER, C.P.C. APP LIED. 2 L 7 2 4F RT A1NM 2008022000178 20080220 00178 GL 2008 2 20 C2XA08ON082 2 20080203 A 7532 32158861 BLEED VALVE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL NR 1 ENGINE FAILED A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 16183 7824 7824 14500914 FLT 7771 - RNO TO RNO - DURING TAKEOFF FLIGHT CREW REPORTED BLD 1 VALVE FAIL ON EICAS AT 60 KNOTS. MX PERSONNEL REMOVED AND REPLACED E1 BLD VALVE OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2008022000198 20080220 00198 WP 2008 2 20 NWAA080499872 1 20080117 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 781NC 48121 DURING LINE CHECK, MAINTENANCE FOUND THEY HAD NO CONTROL OF THE EMERGENCY PATHWAY LIGHTING IN THE CABIN, THEY WOULD NOT TURN OFF. MAINTENANCE REPLACED BATTERY PACK AND OPERATIONALLY CHECKED THE SYSTEM. ALL CHECKS WERE GOOD AND THE AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008022000214 20080220 00214 NM 2008 2 20 QXEA200800203 1 20080215 A 5210 SEAL BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 407QX 4049 PDX - FLIGHT 2427 - FLIGHT ATTENDENT REPORTS REAR PASSENGER DOOR DIFFICULT TO OPEN/CLOSE. PDX MAINTENANCE INSPECTED AND FOUND DOOR SEAL CATCHING ON DOOR FRAME. INSPECTED FOR DAMAGE NONE NOTED, CLEANED DOOR SEAL AS REQUIRED OPERATED DOOR S EVERAL TIMES. NO FURTHER DEFECTS. OPS CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE. NO PARTS REQUIRED. 2 H 7 2 4T RT A13NM 2008022000229 20080220 00229 NM 2008 2 20 HALA0800100 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 924-926 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45 SEAT TRACK AT RBL 11, STA 924-926. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW S RM 51-10-02,REV 75, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101 REV 76. 2 L 7 2 4F RT A1NM 2008022000236 20080220 00236 NM 2008 2 20 HALA0800097 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 854 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION, SECTION 45, SEAT TRACK AT RBL 11, STA 854. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 51-10-02, REV 75, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101 REV 76. 2 L 7 2 4F RT A1NM 2008022000237 20080220 00237 SO 2008 2 20 SIMA200804404 1 20080211 A 2750 3631001011 CONTROL UNIT EMB 145 EMB145LR 3260212 SO TE FLAPS WORN A SIMA O OTHER G MULTIPLE FAILURE LD LANDING 1 SW 21 925AE 14500908 ON FLIGHT 4473 CREW REPORTED FLAP FAIL IN LANDING WHEN FLAPS SELECTED TO 9. CREW DECLARED EMERGENCY AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLAP ELECTRONIC UNIT IAW EMB 145 AMM 27-53-02 AND REMOVED AND REPLACED LEFT WING FLAP TRANSITIONS BREAK IAW AMM 27-51-01 AND 8194; OPERATIO NAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022000238 20080220 00238 SO 2008 2 20 SIMA200804401 1 20080211 A 3260 852701 SQUAT SWITCH EMB 135 EMB135KL 3260302 SO MLG WORN A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 805AE 145489 ON FLIGHT 4915, CREW REPORTED JUST AFTER TAKEOFF WHEN SELECTING GEAR UP, GOT A LANDING LEVER DISAGREE ON EICAS. CYCLED GEAR AS PER AOM PROCEDURES. SAME MESSAGE. CYCLED LEVER DOWN GOT 3 GREEN AND NO LEVER DISAGREE MESSAGE. RETURNED TO CV G. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED HARNESS AND NOSE WOW SWITCH PER EMB AMM 32-63-05. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008022000243 20080220 00243 NM 2008 2 20 HALA0800089 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 950 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION ON SEAT TRACKS BS 950. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 51-10-02, REV 76, BL ENDED WITHIN LIMITS IAW SRM 53-00-52/101, REV 76. 2 L 7 2 4F RT A1NM 2008022000245 20080220 00245 NM 2008 2 20 HALA0800091 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 981 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION ON SEAT TRACKS AT BS 981. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION, IAW SRM 51-10-02, REV 76 , BLENDED WITHIN LIMITS IAW SRM 53-00-52/101 REV 76. 2 L 7 2 4F RT A1NM 2008022000275 20080220 00275 NM 2008 2 20 F3LA200800048 1 20080212 A 3350 32145410 EPSU AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE EMERGENCY LIGHTS INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 928FR 97 2236 DURING PERFORMANCE OF EO A9-25EO-02752, REV G, INSPECTION REPORTED EMERGENCY PATHWAY LIGHTS AT ROWS 1, 2, 5 AND 6 WERE I NOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EPSU IN ACCORDANCE WITH THE REQUIREMENTS OF AMMM 33-51-38 PB 401. FOL LOWING COMPLETION OF THE MAINTENANCE ACTION, THE WORK WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008022000287 20080220 00287 SO 2008 2 20 C2XA08ON089 1 20080212 A 2913 971808MODA PUMP EMB 145 EMB145XR 3260214 SO NR 1 ENGINE FAILED A C2XA K NONE O OTHER AP APPROACH 1 SW 27 16170 9789 9789 14500850 FLT 7759 - TUS - FLIGHT CREW REPORTED NR 1 EDHP FAILURE ON GEAR EXTENSION. AIRCRAFT LANDED WITHOUT DECLARING EMERGENCY AND WITH NO INCIDENTS. MX PERSONNEL REMOVED AND REPLACED NR 1 EDHP OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RE LEASED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2008022000297 20080220 00297 SO 2008 2 20 C2XA08CL020 1 20080210 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG FAULTY A C2XA K NONE E VIBRATION/BUFFET CL CLIMB 1 SW 27 11536 145520 CLE FLIGHT 2592 - THE CREW REPORTED A UNUSUAL LOAD SOUND FROM UNDER THE COCKPIT FLOOR ONLY IN CLIMB AND CRUISE. ALSO RE PORTED A SLIGHT VIBRATION OF YOLK AND RUDDER PEDALS. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR UPLOCK BO X "B"PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008022000303 20080220 00303 2008 2 20 YENA2008016 4 20080205 A 2565 L32A320160 CONTROL CABLE AIRBUS 320 A320232 3930326 EU EVAC SLIDE STIFF A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 645JB 5712 5712 2900 ON C1 CHECK, LT EMERGENCY EXIT FAILS OPS TEST FLEX CABLE STIFF AND WILL NOT RETRACT. REMOVED AND REPLACED LT FLEXIBLE C ABLE ASSY PER AMM 25-62-43-04. 2 L 7 2 4F RT A28NM 2008022100076 20080221 00076 EU 2008 2 21 08FDEA00489 1 20080117 A 5350 A539867512 RIB AIRBUS 310 A310222 3930315 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 TAIL CONE, RIBS BETWEEN FR 84 AND 86, AND STRINGER 32 LT DAMAGED, RIBS (SECTION-L) WERE REPLACED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2008022100078 20080221 00078 EU 2008 2 21 08FDEA00491 1 20080117 A 5350 A5398862420400 STRUT AIRBUS 310 A310222 3930315 EU TAIL CONE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 TAIL CONE, SMALL SPOTS OF CORROSION AT TRACK LT, ATTACHMENT FITTING TO FR 86. STRUT-CROSS WAS REPLACED IN ACCORDANCE WI TH SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2008022100084 20080221 00084 WP 2008 2 21 08FDEA00498 1 20080218 A 5321 ACA3206509 FLOORBOARD DOUG DC10 DC1030F 3023504 WP BS 595-675 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MAIN CABIN FLOORBOARD AT APPROX LBL - 90, BETWEEN STA 595 TO 675 IS DELAMINATED. FABRICATED NEW FLOORBOARD STA NR 595 - 675. POTTED EDGES, COMPLETED CURE AND SANDED, INSTALLED INSERTS, APPLIED NON-SKID MARKED MANUAL IAW SRZ 25-005 REV F. INSTALLED IAW SRM 51-31-01, VOL II. 2 L 7 3 4F RT A22WE 2008022100086 20080221 00086 WP 2008 2 21 08FDEA00500 1 20080218 A 5321 ACA7373507 FLOORBOARD DOUG DC10 DC1030 3023501 WP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 CABIN FLOORBOARD BS 675 LBL 27.50 DELAMINATED AND CRACKED. FABBED FLOORBOARD IAW DWG SRZ 25-005 REV F. LOCATED AND POT TED INSERTS IAW DWG SRZ 25-005 REV F. INSTALLED NON-SKID, POTTED AND SANDED EDGES IAW DWG SRZ 25-005 REV F. INSTALLED NEW FLOORBOARD IAW SRM 51-31-01 VOL II. MINOR REPAIR. 2 L 7 3 4F A22WE 2008022100087 20080221 00087 EU 2008 2 21 08FDEA00501 1 20080218 A 5730 SKIN AIRBUS 300 A300F4605R 3930327 EU RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 RT WING LOWER O/B PANEL 590 BB HAS SCRATCHES ON THE SKIN AROUND THE CUTOUT, AND ON THE ANGLES INSIDE THE CUTOUT. 2 L 7 2 4F RT A35EU 2008022100091 20080221 00091 NM 2008 2 21 08FDEA00414 1 20080213 A 5210 6556297102 SKIN BOEING 727 727233 138408A NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 AFT FUSELAGE EXTERIOR, NR 3 CARGO DOOR SKIN HAS SEVERAL DENTS AT FWD LWR EDGE BS 1090, S26-27R. EVALUATED DENTS AND FOU ND OUT OF LIMITS. CUT OUT DAMAGED SKIN IAW SRM 53-00-03 FIG4. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 52-30-1 FIG 6. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 52-00-3 FIG 4 AND 52-30-1 FIG 6. 2 L 7 3 4F RT A3WE 2008022100092 20080221 00092 NM 2008 2 21 HALA0800088 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 919 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION ON SEAT TRACKS AT BS 919. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 51-10-02, REV 76, BLENDED WITHIN LIMITS, IAW SRM 53-00-52/101, REV 76. 2 L 7 2 4F RT A1NM 2008022100104 20080221 00104 WP 2008 2 21 08FDEA00459 1 20080215 A 5321 AGA5207517 FLOORBOARD DOUG DC10 DC1030F 3023504 WP BS 1761-1821 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MAIN CABIN FLOORBOARD AT APPROX RBL-20, BETWEEN STA 1821 TO 1761 IS SPONGY. FABBED FLOORBOARD, LOCATED AND POTTED INSER TS, POTTED AND SANDED THE EDGES AND APPLIED THE ANTI-SKID IAW DWG SRZ-005 REV F. INSTALLED FLOORBOARD IAW SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2008022100106 20080221 00106 NM 2008 2 21 08FDEA00462 1 20080216 A 5320 AGA7551503 FLOOR SUPPORT DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 MAIN DECK COMPARTMENT, STA 1989, X= 55 FLOOR SUPPORT FOUND CRACKED. SUPPORT REMOVED AS PER SRM 51-31-01 VOLUME II. NE W FLOOR SUPPORT MACHINED AS PER DRAWING AGA7551 AND INSTALLED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008022100107 20080221 00107 NM 2008 2 21 08FDEA00463 1 20080216 A 5347 ACA7104511 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 MAIN DECK COMPARTMENT, AFTER REMOVAL OF LOWER CARGO CEILING PANEL FOUND SEAT TRACK AT STA 635, X = 8.50 INCH CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008022100109 20080221 00109 NM 2008 2 21 08FDEA00467 1 20080216 A 5414 313N50027 PANEL BOEING 757 7572B7 1384964 NM NR 2 NACELLE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 NR 2 PYLON PANEL 444BL IS GOUGED IN 2 PLACES AND HAS SURFACE CORROSION. REMOVED CORROSION IAW SRM 54-50-71. ORIGINAL M ATERIAL THICKNESS .063. L=1.0", W=.50", D=.011". FOUND TO BE OUT OF SRM 54-50-71, FIG 101 LIMITS, 10 PERCENT MATERIAL LOSS. FABRICATED NEW CHANNEL ON MAE TRAVELER NR T7/715551, FROM 7075-0, 0.063C, HEAT TREATED TO T6. REMOVED AND REPLAC ED CHANNEL IAW SRM 51-40-01. PAINTED CHANNEL IAW AMM 51-21-00-7. 2 L 7 2 4F RT A2NM 2008022100113 20080221 00113 EU 2008 2 21 08FDEA00507 1 20080218 A 5420 FAIRING AIRBUS 300 A300F4605R 3930327 EU NR 1 NACELLE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 NR 1 PYLON LOWER FAIRING FWD LT ATTACH HOLES ARE ELONGATED. REMOVED SKIN PER SRM 51-40-21 PARA 6 & 7 DUE TO FASTENER HOLES ELONGATED BEYOND LIMITS PER SRM 54-55-51. FABRICATED UPPER LONGERON REPAIR SECTION & SPLICE PER SRM 54-55-51, FIG 207. ALODINED AND PRIMED UPPER LONGERON REPAIR SECTION & REPAIR SPLICE PER SRM 51-21-10 & 51-23-10. FABRICATED NEW SKIN PER SAMPLE & PER GMM 7-0-1001. ALODINED & PRIMED NEW SKIN PER SRM 51-21-10 & 51-23-10. REMOVED UPPER LONGERON SE CTION PER SRM 54-55-51, FIG 207. INSTALLED UPPER LONGERON SECTION; SPLICE & NEW SKIN PER SRM 51-40-21 PARA 6 & 7. MI NOR PEPAIR 2 L 7 2 4F RT A35EU 2008022100114 20080221 00114 EU 2008 2 21 08FDEA00508 1 20080219 A 5210 A52175325300 BEAM AIRBUS 330 A300* EU ZONE 800 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND AT AFT PAX DOOR LT UNDER BEAM 8 FRAME SEGMENT DAMAGED. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A26NM 2008022100115 20080221 00115 NM 2008 2 21 08FDEA00509 1 20080219 A 5320 655931821 STIFFENER BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 A/C EQUIP BAY, FAIRING SUPPORT INTERCOSTAL HAS CORROSION, STA 780, 3 INCHES, BL 0, JUST BELOW DELTA BEAM (STIFFENER). R EMOVED CORRODED STIFFENER AND STRAP AT STA 780 + 3". REMOVED CORROSION AND MATERIAL WAS OUT OF LIMITS, BEYOND 10 PERCEN T ALLOWABLE DAMAGE. FABRICATED NEW STRAP (PN 65-59318) AND STIFFENER (65-59318-21). STIFFENER WAS HEAT TREATED TO T-6 CONDITION ON NR N00507. TREATED AND PRIMED AND INSTALLED NEW STRAP AND STIFFENER. REF BOEING DWG 65-59318/SRM 51-30-02 PG 2 AND 13 SRM 53-10-1 PG 2 SRM 51-10-1 PG 12. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008022600163 20080226 00163 EU 2008 2 26 SA08005 1 20080221 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 712US 18332 843 1038 DCA - THE EMERGENCY LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT, FIN 10WL, AND BATTERY. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2008022600166 20080226 00166 NM 2008 2 26 ASAA0842658 1 20080110 A 5315 6545808198 FLOORBEAM BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 CORROSION FOUND ON FLOORBEAM AT BS 294 RBL 10 TO RBL 20. CORROSION BLENDED OUT FOUND TO BE BEYOND LIMITS. REPAIR & PAR T INSTALLED IAW B737 400 SRM CH 53 10 51 FIG 201. 2 L 7 2 4F RT A16WE 2008022600167 20080226 00167 NM 2008 2 26 ASAA0842552 1 20080117 A 5320 69417579 INTERCOSTAL BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO PIT FLOOR SUPPORT INTERCOSTAL FOUND CORRODED AT BS 500F TO 500G LBL 24. INTERCOSTAL REPLACED. 2 L 7 2 4F RT A16WE 2008022600171 20080226 00171 NM 2008 2 26 ASAA0842615 1 20080117 A 5311 90526911 FRAME BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 BS 500F FUSELAGE FRAME CRACKED AT FASTENER HOLE BETWEEN STR 13R AND 14R BS 500 F. FUSELAGE FRAME BETWEEN STR 13R AND ST R 14R REPAIR IAW JA DRAWING A53100264248 AND EO 5310 02642. 2 L 7 2 4F RT A16WE 2008022600174 20080226 00174 NM 2008 2 26 ASAA0842620 1 20080117 A 5311 65C27308106 ANGLE BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO COMP FRAME REINFORCEMENT AT STA 500D RBL 28 IS CORRODED. REPAIRED WITH REPAIR PARTS. 2 L 7 2 4F RT A16WE 2008022600176 20080226 00176 NM 2008 2 26 ASAA0842570 1 20080105 A 5320 6546592503 CHANNEL BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT FLOOR CHANNEL FOUND CORRODED AT BS 767+6 TO BS 847+14 RBL 3. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600178 20080226 00178 NM 2008 2 26 ASAA0842573 1 20080105 A 5320 654659247 CHANNEL BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT FLOOR CHANNEL AT BS 847+14 TO 867 LBL 8 FOUND CORRODED. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600179 20080226 00179 NM 2008 2 26 ASAA0842578 1 20080106 A 5347 655384410 CARGO TRACK BOEING 737 7374S3 1384711 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT TIE DOWN TRACK LUG FOUND CORRODED AT BS 727 D LBL 17. TIE DOWN LUG REPLACED. 2 L 7 2 4F RT A16WE 2008011600010 20080116 00010 NM 2008 1 16 SWAA080183 1 20080108 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600011 20080116 00011 NM 2008 1 16 SWAA080184 1 20080108 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600023 20080116 00023 NM 2008 1 16 SWAA080194 1 20080108 A 5312 6549892 CAP BOEING 737 7373G7 1384595 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED DAL CHECK, FOUND AFT PRESSURE BULKHEAD DOME CAP CRACKED AT BS 1016, BETWEEN 12 O'CLOCK AND 6 O'CLOCK PO SITION. REPAIRED DOME CAP PER SRM. 2 L 7 2 4F RT A16WE 2008011600095 20080116 00095 EU 2008 1 16 MALA080001 1 20080105 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 433XJ 340B433 EMERGENCY LIGHTING SUPPLY 21LN FAULTED DURING FUNCTIONAL TEST OF EMERGENCY BATTERY CAPACITY. REMOVED AND REPLACED EMERG ENCY LIGHT POWER SUPPLY 21LN IAW AMM 33-50-10-04-1. OPS CHECK GOOD, PN: 3301-51; SN ON: 2062; SN OFF: 2119. 2 L 7 2 4T RT A52EU 2008011600096 20080116 00096 NM 2008 1 16 SWAA080267 1 20080111 A 3350 B21506 FUSE BOEING 737 7377H4 1384404 NM CABIN BLOWN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 436WN 32456 DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP BETWEEN ROW 1 ABC AND ROW 4 ABC. REMOVED AND REPL ACED FUSE PER MM. 2 L 7 2 4F RT A16WE 2008011600105 20080116 00105 EU 2008 1 16 08FDEA00045 1 20080105 A 5330 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS EXTERNAL LAPSEAM REPAIR LOCATED AT LOWER RT SIDE FUS SKIN FR 39, BTWN STR 47 TO 51 RT, REPAIR FILLER MEASURES 8 .8" BY 6.4", REPAIR DOUBLER MEASURES 8.5" BY 16.9" REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUSLY INSTALLED REPAI R AND INSTALLED CORRECT REPAIR IAW A310 SRM 53-15-12, FIG 201, SHEETS 1 AND 2. THIS AN AIRBUS REPAIR WITH NO ASSIGNED P ART NUMBER THIS IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008011600111 20080116 00111 NM 2008 1 16 08FDEA00052 1 20080106 A 5730 112N60101 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 RIGHT WING TANK ACCESS PANEL 643CB HAS SURFACE CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 643CB IAW SRM 57- 20-01, FOUND TO BE OUT OF LIMITS PER SRM 57-20-01, FIG 201, DETAIL I, SECTION AA, NOTE B. REPLACED ACCESS PANEL 643CB I AW AMM 28-11-01. 2 L 7 2 4F RT A2NM 2008022100117 20080221 00117 NM 2008 2 21 08FDEA00511 1 20080219 A 5320 652938952 THRESHOLD BOEING 727 727227 1384078 NM BS 312-340 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 MAIN ENTRY DOOR CUTOUT LWR AFT SS THRESHOLD CORNER PLATE HAS 2 CRACKS RECEIVED SERVICEABLE THRESHOLD PLATE REF A TAG FEX 3650, AND 8130-3 5517-0000, PLATE WILL BE INSTALLED ON EO CARD NR 7-5310-7-3362 P3 CARD 3 STEP C-2, THIS IS CLASSIFIED A S A MINOR REPAIR. 2 L 7 3 4F A3WE 2008022100121 20080221 00121 NM 2008 2 21 HALA0800149 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 2 CORROSION SECTION 46, SEAT TRACKS AT RBL 11, STA 1197+122. REWORKED IAW SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022100123 20080221 00123 NM 2008 2 21 HALA0800151 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1235 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 2 CORROSION SECTION 46, SEAT TRACKS AT RBL 11, STA 1235. REWORKED IAW SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022100125 20080221 00125 NM 2008 2 21 HALA0800154 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1373 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 2 CORROSION SECTION 46, SEAT TRACKS AT RBL 11, STA 1373. REWORKED IAW SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022100134 20080221 00134 NM 2008 2 21 F3LA200800062 1 20080210 A 5321 D5367302000000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 5503 2019 DURING C3/S1 C CHECK, INSPECTION REPORTED THE AFT CARGO PIT FLOOR PANEL 151BE HAD A PUNCTURE ON ITS UPPER SURFACE. MAIN TENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00. FOLLOWING COMPLETION OF THE REPAI R, THE FLOOR PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008022100143 20080221 00143 2008 2 21 SWIA200819206 3 20080203 A 6110 SIGNAL COND UNIT EMB 120 EMB120ER 3260203 SO LT PROPELLER MALFUNCTIONED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 217SW 120286 LEFT PROP AUTO FEATHERED UNCOMMANDED WHILE EXITING THE RUNWAY, FLIGHT NR 3715. REPLACED TORQUE SIGNAL CONDITIONER IAW EMB MM 77-12-00, PN 30005-0000-52, SN OFF 2229. 2 L 7 2 4T RT A31SO 2008022100144 20080221 00144 EA 2008 2 21 SWIA200819207 1 20080208 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 448SW 7678 CAPTAINS SIDE WINDOW CRACKED WHILE TAXIING, FLIGHT NR 3963. REPLACED PILOT WINDOW IAW MM 56-12-01, PN NP-139322-5, SN OFF, 02114H4742. 2 L 7 2 4F RT A21EA 2008022100146 20080221 00146 NM 2008 2 21 F3LA200800056 1 20080217 A 5320 D5397496700000 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 903FR 5893 1560 DURING A C5 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ALONG THE ATTACHMENT HOLES OF THE AFT CARGO PIT PROFILE AT FRAME 59, FROM THE RIGHT TO THE LEFT SIDE. MAINTENANCE REMOVED AND REPLACED THE PROFILE, COMMON TO FRAME 59, IN ACCORDA NCE WITH THE A319 SRM 51-42-11, PARAGRAPH 6. FOLLOWING COMPLETION OF THE INSTALLATION, IT WAS INSPECTED AND FOUND ACCEP TABLE. 2 L 7 2 4F 4 F RT A28NM 2008022100148 20080221 00148 NM 2008 2 21 HALA0800157 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1417 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 2 CORROSION SECTION 46, SEAT TRACKS AT RBL 11, STA 1417. REWORKED IAW SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022100150 20080221 00150 NM 2008 2 21 HALA0800159 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1447 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 2 CORROSION SECTION 46, SEAT TRACKS AT RBL 11, STA 1447. REWORKED IAW SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022100156 20080221 00156 NM 2008 2 21 HALA0800165 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1370 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 46, SEAT TRACKS AT RBL 88.5, STA 1370. REWORKED IAW SRM 53-00-52/101, AND REPLACED SEAT TRACK S IAW SRM WHERE DAMAGE WAS OUT OF LIMITS. 2 L 7 2 4F RT A1NM 2008022100157 20080221 00157 NM 2008 2 21 HALA0800166 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1339 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 46 SEAT TRACKS AT RBL 88.5, STA 1339. REWORKED IAW SRM 53-00-52/101, AND REPLACED SEAT TRACKS IAW SRM WHERE DAMAGE WAS OUT OF LIMITS. 2 L 7 2 4F RT A1NM 2008022100163 20080221 00163 EU 2008 2 21 08FDEA00420 1 20080213 A 5230 A5237405220400 BUSHING AIRBUS 300 A300F4605R 3930327 EU CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 AFT CARGO DOOR NR 4 ECCENTRIC BUSHING SUPPORT INNER BORE IS CORRODED. REMOVED AND REPLACED AFT CARGO DOOR NR 4 ECCENTRI C BUSHING REF FEDEX ROUTINE CARD 61X5030ALI AND A300-600AMM 52-32-11-5. T/W, TWS8330A. 2 L 7 2 4F RT A35EU 2008022100164 20080221 00164 WP 2008 2 21 08FDEA00423 1 20080214 A 5244 AKC7332503 ACCESS DOOR DOUG MD10 MD1010F 3022112 WP ZONE 100 MISSING A FDEA L ABORTED APPROACH O OTHER AP APPROACH 1 SO 25 563FE 46948 DURING WALKAROUND, FOUND AFT ACCESSORY COMPARTMENT DOOR MISSING. NEED IPC 53-52-01-01 ITEM 440 MPN AKC7332-1 LOWER TAIL CONE DOOR. REMOVED TAIL CONE IAW MD-10-10 AMM 53-52-00-2. COMPLETED INSTALLATION OF TAIL CONE ASSY. SAFTIED AND LUBED HINGE BOLTS. INSTALLED HINGE FAIRINGS PR MD10-10 M/M 53-52-00-1. 2 L 7 3 4F RT A22WE 2008022100173 20080221 00173 NM 2008 2 21 HALA0800174 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 46, SEAT TRACKS AT RBL 88.5, STA 1197+2. REWORKED IAW SRM 53-00-52/101, AND REPLACED SEAT TRA CKS WHERE DAMAGE WAS OUT OF LIMITS. 2 L 7 2 4F RT A1NM 2008011600155 20080116 00155 NM 2008 1 16 SWAA080203 1 20080109 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER 21R CRACKED AT BS 355. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008011600156 20080116 00156 NM 2008 1 16 SWAA080205 1 20080109 A 5755 654645262A SPOILER BOEING 737 7373H4 1384600 NM RT WING DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED MV2 CHECK, FOUND RT WING NR 5 GROUND SPOILER ATTACH LUG BROKEN. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2008011600175 20080116 00175 NM 2008 1 16 SWAA080270 1 20080110 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 438WN 29833 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 129. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600179 20080116 00179 NM 2008 1 16 SWAA080292 1 20080113 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008011600180 20080116 00180 NM 2008 1 16 SWAA080291 1 20080113 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011600185 20080116 00185 2008 1 16 SWAA080276 4 20080113 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008011600192 20080116 00192 NM 2008 1 16 SWAA080293 1 20080114 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 254WN 32512 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008011600197 20080116 00197 EU 2008 1 16 SWAA080224 2 20080107 A 7200 332A1000 ENGINE BOEING 737 7373K2 13844BA NM CFMINT CFM56 CFM563B2 13802 EU LEFT MALFUNCTIONED A SWAA A UNSCHED LANDING B Y SMOKE/FUMES/ODORS/SPARKS ENGINE STOPPAGE CL CLIMB 1 SW 29 340LV 23738 85614 AIR TURNBACK / DECLARED EMERGENCY / INFLIGHT SHUTDOWN. NR 1 ENGINE FAILURE ON CLIMBOUT OF SMF, NOTICED BURNING BIRD RES IDUE SMELL. POSSIBLY AS A RESULT OF BIRD STRIKE OR FROM PREVIOUS FLIGHT. APPROX 4500' MSL NR 1 ENGINE MADE LOUD BANGIN G NOISE. REMOVED AND REPLACED NR 1 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E21EU 2008011600198 20080116 00198 NM 2008 1 16 SWAA080223 1 20080109 A 3350 101331 LENS BOEING 737 7373K2 13844BA NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 LEFT OVERWING EMERGENCY EXIT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008011600204 20080116 00204 NM 2008 1 16 SWAA080299 1 20080114 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011600205 20080116 00205 NM 2008 1 16 SWAA080300 1 20080114 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2008011600207 20080116 00207 NM 2008 1 16 SWAA080316 1 20080111 A 3397 W3142011520 WIRE BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 408WN 27895 EEPLS INOP AT ROW 2 ABC. FOUND LOOSE WIRE. SECURED WIRE PER WDM. 2 L 7 2 4F RT A16WE 2008011600208 20080116 00208 NM 2008 1 16 SWAA080317 1 20080110 A 2910 NAS16128 O-RING BOEING 737 7377H4 1384404 NM HYDRAULIC SYS LEAKING A SWAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 29 410WN 27897 DIVERSION - ON CLIMB TO CRUISE "B" HYDRAULIC SYSTEM SLOWLY DECREASED TO "0" QUANTITY. DID NOT LOOSE "B" SYSTEM PRESSURE UNTIL FLAPS LOWERED ON APPROACH. REMOVED AND REPLACED "O" RING LEAKING ON PRESSURE SWITCH AT "B" SYSTEM HYDRAULIC MODU LE PER MM. 2 L 7 2 4F RT A16WE 2008011600216 20080116 00216 NM 2008 1 16 SWAA080307 1 20080114 A 5743 6559886 BAR BOEING 737 7373T5 1384608 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED MV2 CHECK, FOUND RT WING MLG STABILIZER BAR CORRODED. REMOVED AND REPLACED STABILIZER BAR PER MM. 2 L 7 2 4F RT A16WE 2008011600219 20080116 00219 NM 2008 1 16 SWAA080310 1 20080114 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 DURING SCHEDULED HC1 CHECK, RT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008011600274 20080116 00274 NM 2008 1 16 SWAA080170 1 20080107 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 884, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600275 20080116 00275 NM 2008 1 16 SWAA080214 1 20080109 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT LT BS 520 TO LT BS 540. REMOVED AND REPLA CED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008011600276 20080116 00276 NM 2008 1 16 SWAA080213 1 20080109 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT LT BS 344 TO LT BS 440. REMOVED AND REPLA CED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008011600277 20080116 00277 NM 2008 1 16 SWAA080215 1 20080109 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT LT BS 639 TO LT BS 706. REMOVED AND REPLA CED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008011600278 20080116 00278 NM 2008 1 16 SWAA080216 1 20080109 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT RT BS 400 TO RT BS 440. REMOVED AND REPLA CED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008011600333 20080116 00333 EA 2008 1 16 MASA200800008 1 20080105 A 3260 SWITCH CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR OPEN A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 7305V 7305 ASH FLT 2721 DRO-PHX - DIVERTED TO ABQ DUE TO GEAR DISAGREE/NOSE DOOR OPEN MESSAGE. MX FOUND THE NOSE DOOR RELEASE SWIT CH IN THE DOOR OPEN POSITION. NO DAMAGE NOTED. SWUNG GEAR WITH OPS NORMAL. 2 L 7 2 4F RT A21EA 2008011600338 20080116 00338 NM 2008 1 16 MASA200800016 1 20080106 A 5230 85230461107 TRACK DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CHAFED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 454YV 454 CHAFING WAS FOUND ON AFT CARGO DOOR TRACK. REMOVED AND REPLACED AFT CARGO DOOR TRACK. 2 H 7 2 4T RT A13NM 2008011600339 20080116 00339 EA 2008 1 16 MASA200800006 1 20080102 A 2560 LS6006182 GLOWSTRIP CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 916FJ 15016 ASH FLT 2834 (INBOUND) TUS - EXIT PATH STRIP PHOTO ILLUM IN EXIT ROW INOP. REMOVED AND REPLACED LIGHT STRIP. 2 L 7 2 4F RT A21EA 2008011600344 20080116 00344 EU 2008 1 16 08FDEA00060 1 20080107 A 5311 A5711211720100 FRAME AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 HOLES NR 25 AND NR 27 FRAME 46 RT HAS CRACK INDICATIONS IN FRAME FEET. REAMED HOLES 26 AND 27 TO ELIMINATE CRACK INDICAT IONS IAW EA 6-5310-113006. REMOVED FOOT FITTING AND BUSHED HOLE 27 IAW EA 6-5310-113006. INSTALLED FOOT FITTING IAW SR M 51-40-21 OAR 7, EA 6-5310-113006 AND W/C E 6-5310-7-5020 PT 2. 2 L 7 2 4F RT A35EU 2008011600347 20080116 00347 NM 2008 1 16 08FDEA00063 1 20080107 A 5730 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 583FE 48421 02 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT WING LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. COMPLIED WITH FEDEX E.A. 1-5710-117257, CLASSIFIED AS A MAJOR REPAIR AS PER FEDE X GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008011600006 20080116 00006 NM 2008 1 16 SWAA080176 1 20080107 A 5311 6546549 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600015 20080116 00015 NM 2008 1 16 SWAA080188 1 20080108 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 421LV 32452 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 133. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600016 20080116 00016 NM 2008 1 16 SWAA080189 1 20080108 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 421LV 32452 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 133. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600093 20080116 00093 NM 2008 1 16 SWAA080266 1 20080113 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 429WN 33658 DURING SCHEDULED MV1 CHECK, FOUND EEPLS COVER BROKEN AT ROW 4 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 2008011600182 20080116 00182 NM 2008 1 16 SWAA080289 1 20080113 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011600184 20080116 00184 2008 1 16 SWAA080275 4 20080113 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008011600186 20080116 00186 NM 2008 1 16 SWAA080277 1 20080112 A 5753 6546435335 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED MV1 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2008011600191 20080116 00191 NM 2008 1 16 SWAA080283 1 20080111 A 3211 115A5211 FITTING BOEING 737 7377H4 1384404 NM LT MLG TRUNNION CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 718SW 27852 DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600194 20080116 00194 NM 2008 1 16 SWAA080298 1 20080114 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600199 20080116 00199 NM 2008 1 16 SWAA080222 1 20080109 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 732E AND BS 727E, STR 21L AND STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008011600200 20080116 00200 NM 2008 1 16 SWAA080282 1 20080111 A 3211 115A5211 FITTING BOEING 737 7377H4 1384404 NM RT MLG TRUNNION CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 718SW 27852 DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600346 20080116 00346 NM 2008 1 16 08FDEA00062 1 20080107 A 5714 APB74471 SKIN DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 583FE 48421 MAIN DECK CARGO COMPT, FOUND UNDER FLOOR STRUCTURE WITH CORROSION AT STA 1230, LBL 105". REPAIR CARRIED OUT AS PER FEDE X EA 1-5330-117256, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008011600349 20080116 00349 NM 2008 1 16 08FDEA00065 1 20080107 A 5320 NCA604641 SUPPORT DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 583FE 48421 LT AIRCON COMPT FOUND SUPPORT ON STA Y=575.00 CORROSION. REPAIR CARRIED OUT AS PER SRM 53-00-01 FIGURE 8 VOLUME I. RE PAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008011600352 20080116 00352 EU 2008 1 16 08FDEA00068 1 20080108 A 5315 SKIN AIRBUS 310 A310203 3930313 EU ZONE 200 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT UPPER LT SIDE FUSELAGE SKIN AT FRAME 64 BETWEEN STRINGER 21 TO 22A LT ON LAP SEAM REPAIR DOUBLER MEASURE 6.9" BY 5.6" REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUSLY INSTALLED REPAIR AND INST ALLED CORRECT FUSELAGE SKIN LAPSEAM REPAIR IAW A310 SRM 53-10-12, FIG 216,SHEET 1 AND 2. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008011600360 20080116 00360 EU 2008 1 16 MALA080005 1 20080106 A 5320 WEB SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 WEB AT STA 294 HAS CHAFE MARK FROM AIRSTAIRS SLIDER CHANNEL COVER. INSTALLED DOUBLER. COMPLETED REPAIR IAW MAL EO NR S 53362. 2 L 7 2 4T RT A52EU 2008011600383 20080116 00383 SO 2008 1 16 CHQA200800007 1 20080107 A 2910 A91391 LINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL HYD SYSTEM LEAKING A CHQA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 382SK 145624 CAE312609 STL TO EWR - DURING CLIMB, THE CREW RECEIVED A HYDRAULIC SYSTEM 2 FAIL MESSAGE WITH THE SYSTEM 2 HYDRAULIC PRESSURE AT Z ERO AND QUANTITY IN THE AMBER RANGE. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE PRESSURE LINE FROM THE ENGINE DRIVEN HYDRAULIC PUMP LEAKING. AFTER REPLACING THE PRESSURE L INE AND ENGINE DRIVEN PUMP, THE NR 2 HYDRAULIC SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008011600386 20080116 00386 NM 2008 1 16 08FDEA00075 1 20080109 A 5343 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 616FE 48747 NOSE LANDING GEAR LEFT TRUNNION SUPPORT FITTING FOUND CRACK. CARRIED OUT REPAIR AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2 -100. 2 L 7 3 4F RT A22WE 2008011700002 20080117 00002 EA 2008 1 17 SWIA200819024 1 20080107 A 3222 O-RING CNDAIR CL600 CL6002B19 1900309 EA NLG STRUT LEAKING A SWIA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 07 405SW 7029 FLT 3920 - RECEIVED "GEAR DISAGREE" MESSAGE AFTER GEAR RETRACTION. REPLACED O-RINGS AND SEALS ON NOSE STRUT IAW AMM 32- 21-30. 2 L 7 2 4F RT A21EA 2008011700004 20080117 00004 EA 2008 1 17 SWIA200819026 1 20080105 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 865AS 7507 FLT 3886 - FO'S WINDSHIELD DELAMINATED IN FLIGHT. REPLACED WINDSHIELD PER MM 56-11-01. OPS AND LEAK CHECKS GOOD, PN: N P-139321-14, SN OFF: 01025H8368. 2 L 7 2 4F RT A21EA 2008011700007 20080117 00007 SO 2008 1 17 SWIA200819029 1 20080103 A 5210 LINKAGE EMB 120 EMB120ER 3260203 SO PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 224SW 120294 FLT 5714 - FLIGHT ATTENDANT REPORTS CABIN DOOR IS DIFFICULT TO OPERATE. LUBRICATED CABIN DOOR LINKAGE AND ROLLERS. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2008011700016 20080117 00016 CE 2008 1 17 DXTA200702733 1 20080101 A 3297 WIRE HARNESS CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG DAMAGED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 926QS 7500026 AFTER TAKEOFF UNABLE TO RETRACT THE LANDING GEAR. REMOVED GEAR HANDLE ASY P/N 9914551-4 S/N 0222. INSTALLED HANDLE P/N 9914551-4 S/N 0162. REMOVED LOGIC MODULE P/N 9914728-2 S/N 151 AND INSTALLED LOGIC MODULE P/N 9914728-2 S/N 350. OPS CHE CKS FAILED. TROUBLESHOT TO BROKEN WIRES AT NOSE GEAR UPPER TORQUE LINK GLIDE. FABRICATED NEW WIRE HARNESS WITH NEW CONNE CTOR AND OPERATIONAL CHECK GOOD. ALL WORK IAW CH'S 24-53-00 AND 32-60-00 OF THE CE750 MM 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008011700085 20080117 00085 NM 2008 1 17 UIEA200800010 1 20080110 A 5730 PANEL BOEING 747 74747UF 1384812 NM RT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 412 30559 RT WING L/E FIXED UPPER PANEL WS426 CRACKED FROM THE L/E OF THE PANEL THROUGH TO THE FIRST RIVET HOLE. LOCATION IS 29" OUTBD OF INBD EDGE OF FIXED PANEL AT WS 426, 0.500" LONG. OUT OF LIMITS AS PER SRM 51-70-02. 2 L 7 4 4F RT A20WE 2008011700088 20080117 00088 WP 2008 1 17 08FDEA00081 1 20080110 A 5311 NJC6374511 FRAME DOUG DC10 DC1030F 3023504 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 AFT FUSE WASTE TANK COMPT ON FRAME FOUND CRACK. REPAIRED FRAME IAW SRM 53-30-00 FIG 4 VOL I. 2 L 7 3 4F RT A22WE 2008011700093 20080117 00093 EU 2008 1 17 08FDEA00086 1 20080110 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 53 LT BETWEEN FRAMES 62 TO 64 HAS 1 REPAIR SECTION MEASURING 1 7.1" LONG AND 2 REPAIR SPLICES MEASURING 7.9" LONG REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALL ED CORRECT STRINGER REPAIR IAW A310 SRM 53-10-14, FIG 201. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008011700094 20080117 00094 EU 2008 1 17 08FDEA00087 1 20080110 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 55 LT BETWEEN FRAMES 61 TO 64 HAS 1 REPAIR SECTION MEASURING 4 2" LONG AND 2 REPAIR SPLICES MEASURING 7.8" LONG. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTA LLED CORRECT STRINGER REPAIR IAW A310 SRM 53-10-14, FIG 201. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008011700095 20080117 00095 EU 2008 1 17 08FDEA00088 1 20080110 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 55 LT BETWEEN FRAMES 55/58 TO 60 HAS 1 REPAIR SECTION MEASURIN G 29.1" LONG AND 1 REPAIR SPLICE MEASURING 7.7" LONG. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INS TALLED CORRECT STRINGER REPAIR IAW A310 SRM 53-10-14, FIG 201. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AN D IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008011700096 20080117 00096 NM 2008 1 17 08FDEA00089 1 20080110 A 5311 53FX1350 FRAME BOEING 727 727277 138408S NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 246FE 22068 LOWER FWD CARGO, SPLICE FRAME AT ST 580, STR 22L IS CRACKED. VERIFIED BY HFEC. REMOVED 53FX1350 SPLICE FRAME, FABRICAT ED AND INSTALLED NEW SPLICE FRAME IAW FEDEX DRWG 53FX1350 REV A AND 727-200 SRM 51-30-2. 2 L 7 3 4F RT A3WE 2008011700106 20080117 00106 NM 2008 1 17 HALA0800013 1 20080108 A 7603 THROTTLE BOEING 767 767332 1382001 NM LACK OF LUBE A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 ETOPS SIGNIFICANT SYSTEM, BOTH THROTTLES AREA BINDING. LUBE AND CLEANED THROTTLE QUADRANT. 2 L 7 2 4F RT A1NM 2008011700107 20080117 00107 NM 2008 1 17 HALA0800011 1 20080109 A 3150 WARNING MESSAGE BOEING 767 76733A 1385209 NM FALSE ACTIVATION A HALA O OTHER N FALSE WARNING DE DESCENT 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, AILERON LOCKOUT EICAS MSG ON DESCENT FROM 20,000-10,000'. MSG DISAPPEARED DURING APPROACH. B ITE CHECKED SAM, CHECKED GOOD PER FIM 27-11-00 FIG 104. 2 L 7 2 4F RT A1NM 2008011700109 20080117 00109 EU 2008 1 17 08FDEA00047 1 20080106 A 5610 NP1752013 WINDOW AIRBUS 310 A310324 3930206 EU COCKPIT CRACKED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 802FD 542 CAPT FRONT COCKPIT WINDOW CRACKED REMOVED AND REPLACED WINDOW HEAT PROTECTION NR 1 IAW MM 30-42-11-4. PERFORMED OPS CHE CK AS PER MM 30-42-00-5. ALL TEST PASSED. 2 L 7 2 4F RT A35EU 2008011700110 20080117 00110 EU 2008 1 17 08FDEA00090 1 20080110 A 5320 A53870037201 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 CRACK INDICATION IN FR 43A RT SIDE LOWER HOLE EXTENDING FWD AND DOWNWARD APPROX 45 DEGREE, 2 CRACK INDICATIONS IN UPPE R CRUCIFORM FITTING AT FR 43A LOWER HOLE RT SIDE BOTH EXTENDING UPWARD APPROX 30 DEGREE, ONE FWD AND ONE AFT, CRUCIFORM CRACKS BEGIN AT INBD FACE OF CRUCIFORM AND EXTEND OUTWARD INTO CRUCIFORM 1/8 INCH LOCATIONS MARKED. REAMED HOLE (BOTTOM HOLE) IN FITTING TO .401 BHEC ACCOMPLISHED BY NDT CRACK IS STILL PRESENT, REAMED HOLE TO .433 CRACK STILL PRESENT. REMO VED FITTING FROM AIRCRAFT FOUND FITTING TO BE CRACKED. FABBED NEW FITTING ON FEDEX NONROUTINE NO1367, LOCATED DRILLED UP AND INSTALLED FITTING IAW A310 SRM 51-40-23 PARAGRAPH 7. RESTORED CIC IAW A310 AMM 51-22-00-0. 2 L 7 2 4F RT A35EU 2008011700111 20080117 00111 EU 2008 1 17 08FDEA00091 1 20080110 A 5310 A53611513201007 FAILSAFE AIRBUS 310 A310203 3930313 EU R1 DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 RT FWD PASSENGER/CREW DOOR CUT OUT FASTENER HOLE ON FAIL-SAFE RING RTA 1285/FR16A 2ND HOLE FROM FIGURE 10 G1 (KIR AO1) CRACK INDICATION FOUND USING BOLT HOLE INSPECTION NTM 53-30-53 PT6 ALL MAINTENANCE ACCOMPLISHED IAW FEDEX EA 6-5330-113 003 EA TITLE; FUSELAGE AD2007-11-12 SKIN UNDER R1 DOOR SCUFF PLATE AT FRAME 16A REPAIR. 2 L 7 2 4F RT A35EU 2008011700116 20080117 00116 NM 2008 1 17 08FDEA00097 1 20080110 A 5412 311N50434 BULKHEAD BOEING 757 7572B7 1384964 NM ZONE 400 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 WHILE ACCOMPLISHING EO NR F-5450-7-5005 PT2, THE NR 2 PYLON MID BULKHEAD FWD LT BOLT HOLE WAS FOUND AT MAXIMUM DIAMETER OF 0.3918". MAXIMUM DIAMETER PER EO IS 0.3901-0.3911". THE FWD RT BOLT HOLE WAS FOUND TO BE 0.3934", OUT OF LIMITS PER EO. HFEC INSPECTED MID BULKHEAD FWD LT AND RT BOLT HOLES PER NDT MANUAL PART 6, SECTION 51-00-00. REAMED AND INSTALLE D LOCK FASTENERS AT BOTH LOCATIONS AND VISUALLY INSPECTED FOR PROPER INSTALLATION PER EA F-5450-110813. 2 L 7 2 4F RT A2NM 2008011700117 20080117 00117 NM 2008 1 17 08FDEA00098 1 20080110 A 5315 BAC15123345 FLOORBEAM BOEING 757 757200 1384950 NM BS 377 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 CORROSION ON FLOORBEAM AT STA 377.7, LBL3, LBL6, LBL10 AND LBL12. FOUND EXCEED LIMITS IN SRM 53-00-51. REPAIR CARRIED O UT IAW SRM 53-00-51 FIG 201 REPAIR 1 REV. 93. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008011700118 20080117 00118 NM 2008 1 17 08FDEA00099 1 20080110 A 5310 146N559058 STRUCTURE BOEING 757 757200 1384950 NM BS 1280 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 CORROSION ON INBOARD STRUCTURE AT STA 1280, S17L. REPLACED IAW DWG NR 146N5590. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008011700119 20080117 00119 NM 2008 1 17 08FDEA00101 1 20080110 A 5315 BAC15123345 FLOORBEAM BOEING 757 757200 1384950 NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 CORROSION ON FLOORBEAM AT STA 344, LBL4, LBL2, BL0, RBL 2 AND RBL 4. REPAIR CARRIED OUT IAW SRM 53-00-51 FIG.201 REPAIR 1. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008011800006 20080118 00006 WP 2008 1 18 NWAA080079926 1 20080108 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 408 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 926NW 47425 DURING "H" CHECK, FOUND CORROSION ON INNER SURFACE OF FUSELAGE SKIN AT LOWER EDGE OF CARGO DOOR CUTOUT AT BS 408. REPAI RED PER EA 99-211057. 2 L 7 2 4F A6WE 2008011800007 20080118 00007 WP 2008 1 18 NWAA080089918 1 20080107 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1132 S14L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 940N 47572 DURING LINE CHECK, FOUND CRACKS IN FUSELAGE SKIN AT CANTED FRAME BS 1132 S14L. REPLACED SKIN SECTION PER 51-30-02. 2 L 7 2 4F A6WE 2008011800008 20080118 00008 EU 2008 1 18 DHLA200800004 1 20080110 A 3231 UPLOCK SWITCH AIRBUS 300 A300B4203 3930306 EU RT MLG MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION AP APPROACH 1 GL 05 364DH 141 FLT 165, RIGHT MAIN GEAR DOOR DID NOT RETRACT AFTER GEAR EXTENDED. ABNORMAL PROCEDURE ACCOMPLISHED. CLEANED AND RESEC URED RT MLG INBD DOOR UPLOCK SWITCHES, OPERATED GEAR DOORS. NO DEFECTS NOTED, REF M/M 32-30-00. OPS NORMAL AT THIS TIM E. ACFT GROUNDED. 2 L 7 2 4F RT A35EU 2008011600073 20080116 00073 NM 2008 1 16 SWAA080246 1 20080110 A 2560 6557463 FITTING BOEING 737 7373TO 138447G NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2008011600075 20080116 00075 NM 2008 1 16 SWAA080248 1 20080110 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 756SA 27872 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 4 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008011600078 20080116 00078 NM 2008 1 16 SWAA080257 1 20080112 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 266WN 32523 DURING SCHEDULED MV3 CHECK, FOUND EEPLS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 2008011600083 20080116 00083 NM 2008 1 16 SWAA080259 1 20080113 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 11R CRACKED AT BS 947. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008011600190 20080116 00190 NM 2008 1 16 SWAA080281 1 20080113 A 5311 6546539 FRAME BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, LBL 65. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008011600220 20080116 00220 NM 2008 1 16 SWAA080311 1 20080114 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008011600281 20080116 00281 NM 2008 1 16 SWAA080221 1 20080109 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER 5L CRACKED AT BS 1010. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008011600334 20080116 00334 EA 2008 1 16 MASA200800009 1 20080105 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 591ML 7388 ASH 7171 ORD SERVICE DOOR OUTER HANDLE HARD TO CLOSE. MX CLEANED AND LUBED OUTER HANDLE. 2 L 7 2 4F RT A21EA 2008011600385 20080116 00385 EU 2008 1 16 08FDEA00073 1 20080108 A 5311 SR531299A00301 FAILSAFE AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 RT FWD PASSENGER/CREW DOOR CUT OUT AREA AROUND FAIL SAFE RING AND ADJACENT SKIN (SCUFF PLATE AREA) HAS 9 EACH AREAS OF S URFACE CORROSION AND TOOL MARKS. REMOVED CORROSION FROM 9 EACH NOTED AREAS IAW FEDEX A310-200 SRM 51-74-10. 7 OF THE 9 AREAS WERE IN CLOSE PROXIMITY OF EACH OTHER ON THE LOWER PORTION OF THE FAIL SAFE RING AND WERE FOUND TO BE OUT OF LIMI TS IAW FEDEX A310-200 SRM 53-12-81 FIG 101. REMOVED AND REPLACED THE LOWER FAIL SAFE RING IAW FEDEX A310-200 SRM 53-12- 81 PARA 5C AND AIRBUS DWG 12R53610174 REV F. 2 AREAS OF CORROSION ON SKIN FOUND TO BE WITHIN LIMITS IAW FEDEX A310-200 FRM 53-12-12 DIAG 103 AND FIG 108. RE PROTECTED AREAS IAW FEDEX A310-200 AND 51-23-10 AND 51-21-10. 2 L 7 2 4F RT A35EU 2008011700005 20080117 00005 EA 2008 1 17 SWIA200819027 1 20080107 A 3234 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG SELECTOR MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 435SW 7555 FLT 3760 - NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. REPLACED NOSE GEAR SELECTOR VALVE. OPS AND LEAK CHECK GOOD, PN OFF 250006000, SN OFF 1644. 2 L 7 2 4F RT A21EA 2008011700122 20080117 00122 NM 2008 1 17 HALA0800009 1 20080107 A 2697 WIRE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE FIRE LOOP BROKEN A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, LEFT ENG FIRE LOOP 1 EICAS MESSAGE DISPLAYED. FOUND BROKEN WIRE AT AFT TOP FIRE LOOP LUG. IN STALLED NEW LUG. OPS SECURITY CK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2008011700126 20080117 00126 EA 2008 1 17 SWIA200819035 1 20080107 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 426SW 7468 FLT 3811 - LEFT WINDSHIELD IS CRACKED. REPLACED LEFT WINDSHIELD IAW CRJ 200 MM 56-11-01, PN/OFF NP-139321-9, SN/OFF 021 92H9830. 2 L 7 2 4F RT A21EA 2008011800010 20080118 00010 SO 2008 1 18 SIMA200801102 1 20080109 A 5270 SWITCH EMB 145 EMB145LR 3260212 SO SERVICE DOOR OUT OF ADJUST A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 698CB 14500877 ON FLIGHT 3484 DURING CLIMB AT 280, CREW REPORTED SERVICE DOOR WARNING INDICATION ILLUMINATED. PRESSURIZATION HELD. CR EW DECLARED EMERGENCY. AIRCRAFT REMOVED FROM SERVICE. MAINTENANCE MEASURED GAPS AROUND SERVICE DOOR AND OPERATIONAL CH ECKED THE DOOR, ISSUED MEL 52-04. ADJUSTED MICROSWITCH S7246 IAW EMB 145 AMM 52-74-01. OPERATIONAL TEST GOOD. THIS RE STORES MEL 52-04. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008011800015 20080118 00015 2008 1 18 UIEA200800002 4 20080101 A 3441 46300181300413 INU BOEING 747 7472D7B 1384803 NM NR 1 FAILED A UIEA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 526MC 22337 AIR TURN BACK, AFTER TAKEOFF THE CAPT'S ADI AND THE NR 1 INS FAILED. PLACING THE PLATFORM SWITCH TO POSITION 3 MADE NO DIFFERENCE. SWAPPED NR 1 AND NR 3 INU DUE TO NR 1 FAILED. OPS CHECKED GOOD ON NR 1 PLACED NR 3 ON DMI. 2 L 7 4 4F RT A20WE 2008011800018 20080118 00018 GL 2008 1 18 SIMA200800902 2 20080108 A 7200 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 FIRE A SIMA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN A FLAME/FIRE TX TAXI/GRND HDL 1 SW 21 628AE 15587 145124 CAE311449 ON FLIGHT 4221 CREW REPORTED NR 2 ENGINE ON FIRE. REPORTED FROM TRAILING SINGLE ENGINE A/C ON TAXIWAY. WHILE STARTING NR 2 ENGINE A HUNG START WAS NOTED. TAILWIND 130 DEGRESS 23 GUSTING TO 29. HUNG START PROCEDURE APPLIED BUT TRAILING A /C REPORTED FLAMES AND SMOKE COMING OUT OF BOTH INTAKE AND EXHAUST AND TORCHING FUSELAGE. NO COCKPIT INDICATIONS EXCEPT SMOKE ODOR. ENGINE FIRE PROCEDURE APPLIED. CABIN AND COCKPIT FIRE SMOKE FUMES CHECKLIST APPLIED. ENGINE CHECKED AND SECURED BY CFR. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT ENGINE IAW WORK CARD 72-00-00. OPERATION CH ECK GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008011800020 20080118 00020 SO 2008 1 18 SIMA200801406 1 20080108 A 4920 M4504113A APU EMB 135 EMB135LR 3260305 SO SMOKE A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 716AE 10013 145264 ON FLIGHT 4610, CREW REPORTED BURNING ODOR/FUMES IN COCKPIT AND CABIN. AFTER LANDING, AIRCRAFT REMOVED FROM SERVICE. F OUND APU BLEED TO BE THE SOURCE OF BURNING ODOR, APU PLACED ON MEL 4901. REMOVED AND REPLACED APU IAW WC 49-800-05. O PS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008011800028 20080118 00028 SO 2008 1 18 SIMA200801401 1 20080112 A 4950 4505113A APU EMB 145 EMB145LR 3260212 SO SMOKE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 669MB 145788 ON FLIGHT 4362 - AFTER SHUTDOWN AT THE GATE AND WITH THE APU AND NUMBER 2 PACK RUNNING, A/C CABIN AND COCKPIT FILLED WIT H SMOKE. APU AUTO SHUTDOWN. AIRCRAFT REMOVED FROM SERVICE ISSUED MEL 49-1. REMOVED AND REPLACED APU AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008011800064 20080118 00064 EA 2008 1 18 SWIA200819040 1 20080107 A 3350 AD20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 937SW 974 974 7735 FLT 6799 - CEILING EMERGENCY EXIT SIGNS AT OVERWING EXIT ARE INOP. REPLACED NR 3 EMERGENCY LIGHT BATTERY PACK WITH A SE RVICEABLE UNIT. OPS CHECKS GOOD IAW 33-51-01. 2 L 7 2 4F RT A21EA 2008011800065 20080118 00065 EA 2008 1 18 SWIA200819041 1 20080108 A 3397 FEEDER CABLE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 461SW 7811 FLT 3937 - LAST SECTION OF EMERGENCY LIGHTING IS INOP. REPLACED EMERGENCY LIGHT CONNECTOR CABLE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008011800070 20080118 00070 EA 2008 1 18 SWIA200819046 1 20080110 A 3350 COVER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS MISSING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 724SK 10189 FLT 6508 - SERVICE DOOR EMERGENCY EXIT LIGHT COVER MISSING. REPLACED MISSING SERVICE DOOR LIGHT COVER. 2 L 7 2 4F RT A21EA 2008011800071 20080118 00071 EA 2008 1 18 SWIA200819047 1 20080107 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 407SW 12980 12980 7034 FLT 3942 - NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. REPLACED NOSE GEAR SELECTOR VALVE IAW MM 32-33-10. OPS CHECK GOO D. 2 L 7 2 4F RT A21EA 2008011800081 20080118 00081 EA 2008 1 18 SWIA200819057 1 20080113 A 3250 MODULE CNDAIR CL600 CL6002B19 1900309 EA STEERING TILLER MALFUNCTIONED A SWIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 976SW 7952 FLT 6747 - ON TAKEOFF ROLL, AIRCRAFT PULLED TO THE RIGHT. ADJUSTED RIGHT FEEDBACK RVDT IAW CRJ MM 32-51-20 AND REPLACED STEERING TILLER IAW CRJ MM 32-51-01, P/N: 16650-101, S/N OFF: DCH05/04. 2 L 7 2 4F RT A21EA 2008011800116 20080118 00116 NM 2008 1 18 UIEA200800012 1 20080110 A 5753 SKIN BOEING 747 74747UF 1384812 NM RT WING TE FLAP DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 497MC 29258 RIGHT INBOARD TRAILING EDGE MID FLAP (UPPER SURFACE) HAS EVIDENCE OF DISBONDING AROUND AN AREA OF 4 INCHES DIAMETER AT A PPROX WBL 235 AND 29 INCHES FWD OF MID FLAP TRAILING EDGE. REPAIRED AREA IAW SRM 51-70-10 AND EO NUMBER 4457A116. 2 L 7 4 4F RT A20WE 2008011800118 20080118 00118 EU 2008 1 18 NSVA20070255 1 20080115 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU COCKPIT ODOR A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 EA 27 193CJ 340B193 DCP FLAGS ON CA SIDE EFIS TUBES WITH ELECTRICAL ODOR IN FLIGHT DECK DURING LANDING. INSPECTED CAPS SIDE EFIS AND SURROU NDING EQUIPMENT COULD NOT GET EFIS TO FAULT RAN FOR 6 HOURS, NO DEFECTS NOTED. OK FOR SERVICE PER AMM 34-20-00. 2 L 7 2 4T RT A52EU 2008011800124 20080118 00124 NM 2008 1 18 HALA0800018 1 20080113 A 2150 A/C PACK BOEING 767 76733A 1385209 NM LEFT INTERMITTENT A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, LEFT AIR CONDITIONING PACK SHUTS DOWN INTERMITTENTLY ON GROUND. FOLLOWED INSTRUCTION ON TEMP CONTROL AND BIT ALL ZONES. NO FAULTS NOTED. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008011800132 20080118 00132 NM 2008 1 18 QXEA200800032 1 20080115 A 5210 8SC0442002 STRUT BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR MALFUNCTIONED A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 402QX 4032 PDX - CREW REPORTS THAT THE MAIN CABIN DOOR IS VERY HEAVY AND HARD TO PULL CLOSED AND SLAMS OPEN. MAINTENANCE REPLACED BOTH GAS SPRING STRUTS FOR THE MAIN CABIN DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008011800135 20080118 00135 EA 2008 1 18 QXEA200800033 1 20080114 A 3240 BRAKE CNDAIR CL600 CL6002C10 1390015 EA MLG DRAGGING A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 09 606QX 10023 PDX - FLIGHT 2578 - AIRCRAFT PULLS TO THE LEFT DURING LANDING ROLL AND TAXI. BASED ON THE BRAKE TEMP INDICATIONS, SUSPE CT THE LEFT OUTBOARD BRAKE IS DRAGGING. MAINTENANCE JACKED THE LT WHEELS AND CHECKED ROTATION WITH NO DEFECTS NOTED. C OMPLIED WITH RIGGING CHECK OF THE RDVT AND RAN AUTO RIG WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2008011800137 20080118 00137 WP 2008 1 18 NWAA080149855 1 20080110 A 2750 FLAP SYSTEM DOUG DC9 DC951 3022051 WP SPLIT A NWAA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 01 764NC 47717 THE AIRCRAFT ROLLED SLIGHTLY WHEN THE FLAPS DEPLOYED AT DIFFERENT RATES. CREW CORRECTED THE ROLL AND WAS ABLE TO NOTICE THAT THE LEFT FLAP TRAILED THE RIGHT FLAP DOWN TO THE 5 DEGREE EXTENDED POSITION. CREW ALSO STATED THAT THE SPLIT FLAP CONFIGURATION WAS NOT AS PRONOUNCED IN THE 5 TO 15 DEGREE OR THE 25 DEGREE AND BEYOND RANGES. THE FLIGHT LANDED IN MEM WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED FOUR FLAP BUSS CONTROL CABLES AND TWO PULLEYS. RIG, TENSION ADJUSTMENT , AND CHECK COMPLETED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008022000083 20080220 00083 SO 2008 2 20 C2XA08ON083 1 20080204 A 3350 LIGHT EMB 145 EMB145XR 3260214 SO CABIN OUT OF POSITION A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 12195 14500943 FLT 501 - SAT TO RDU - FLIGHT CREW REPORTED EMERGENCY FLOOR PROXIMITY STRIP MISSING ROW 9. CONTRACT MX WAS DISPATCHED T O RECOVER. CONTRACT MX FOUND MISSING LIGHT STRIP WAS UNDER ANOTHER ONE AND RESECURED STRIP ON ITS ORIGINAL POSITION OPE RATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008022000089 20080220 00089 SO 2008 2 20 C2XA08SH023 1 20080214 A 5512 14532235401 SKIN EMB 135 EMB135LR 3260305 SO HORIZ STAB CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28529 145512 SHV - DURING C-CHECK LT HORIZONTAL STAB L/E HAS CORROSION ON SKINS AROUND RIVETS AND SCREW HEADS. MX REPAIRED LT HORIZO NTAL STAB L/E ON SKINS AROUND RIVETS AND SCREW HEADS IAW EC5510-01178. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2008022000094 20080220 00094 NM 2008 2 20 SWAA080852 1 20080213 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 8R CRACKED AT BS 500B. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008022000115 20080220 00115 NM 2008 2 20 SWAA080833 1 20080213 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 414, BL 0. REPAIRED SKIN P ER SRM. 2 L 7 2 4F RT A16WE 2008022000124 20080220 00124 SO 2008 2 20 CHQA200800028 1 20080212 A 3260 8005701 PROXIMITY SENSOR EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NLG MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 376SK 145578 CAE311852 STL TO MSP, ON INITIAL CLIMB, THE CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS WHEN THEY ATTEMPTED TO M OVE THE LANDING GEAR LEVER TO THE UP POSITION WITHOUT SUCCESS. WHILE PREPARING TO RETURN TO FIELD AT STL THE CREW RAN T HROUGH THE QRH CHECKLIST BUT THE MESSAGE DID NOT DISAPPEAR. THERE WERE THREE DOWN AND GREEN INDICATIONS FOR THE LANDING GEAR DURING THE FLIGHT. THE AIRCRAFT THEN LANDED WITHOUT INCIDENT, AND DURING TAXI BACK THE AIR/GROUND MESSAGE CLEARED ITSELF. MAINTENANCE INTERROGATED THE CMC FOR FAULT CODES AND FOUND SEVERAL FOR THE NOSE LANDING GEAR PROX SWITCH. AFT ER CHANGING THE NOSE LANDING GEAR PROX SWITCH AND SWINGING THE GEAR THE PROX SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008022000126 20080220 00126 SO 2008 2 20 CHQA200800029 1 20080212 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LAVATORY FALSE ACTIVATION A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 257JQ 145812 CAE311677 PHL TO SDF - DURING INITIAL CLIMB AT ABOUT 500 FT, THE CREW NOTICED A LAV SMOKE MESSAGE DISPLAYED ON EICAS. THE FLIGHT ATTENDANT CHECKED INSIDE THE LAVATORY FOR SMOKE OR ODOR AND REPORTED THAT THERE WAS NO VISIBLE SMOKE OR ODOR. WHILE PRE PARING TO RETURN TO PHL, THE EICAS MESSAGE CLEARED AND DID NOT RETURN. THE APPROPRIATE CHECKLISTS WERE RUN IN THE QRH A ND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINES AND RAN BOTH AT HIGH POWER AND COULD NOT GET THE LAV SMOKE MESSAGE TO RETURN, AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE AIRCRAFT WAS DE-ICED TWICE BEFORE TAKEO FF, THE SECOND TIME APPROXIMATELY TEN MINUTES PRIOR TO TAKEOFF. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008022000145 20080220 00145 NM 2008 2 20 SWAA080849 1 20080213 A 5322 6546529 SHEAR TIE BOEING 737 7373TO 138447G NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500, STR 20L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008022000149 20080220 00149 SO 2008 2 20 C2XA08CL019 1 20080213 A 3320 BR900022 BALLAST EMB 145 EMB145 3260210 SO CABIN FAULTY A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 13989 145271 BDL FLIGHT 2303 - CREW REPORTED SMOKE ODOR IN CABIN AND DIVERTED FLIGHT TO SYR AND LANDED WITHOUT INCIDENT. SYR MAINTEN ANCE FOUND STRONG ODOR AT THIRD AFT LIGHTING BALLAST IN CABIN AND DISCONNECTED IT. PLACED ON MEL. FLIGHT CONTINUED ON T O CLE FROM SYR. CLE MAINTENANCE REMOVED AND REPLACED THE THIRD AFT LIGHTING BALLAST. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2008022000154 20080220 00154 SO 2008 2 20 C2XA08SH028 1 20080219 A 5320 14522461011 DOUBLER EMB 145 EMB145LR 3260212 SO OMEGA BEAM CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11544 145557 SHV - DURING C-CHECK RT OMEGA BEAM DOUBLER AT FR 22 HAS CORROSION AROUND NUT PLATE HOLES. MX REMOVED AND REPLACED RT OM EGA BEAM DOUBLER AT FR 22 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008022000174 20080220 00174 2008 2 20 C2XA08ON080 4 20080203 A 3431 ILS SYSTEM EMB 145 EMB145XR 3260214 SO COCKPIT FLUCTUATES A C2XA A UNSCHED LANDING O OTHER AP APPROACH 1 SW 27 12166 14500831 FLT 0025 - TUS TO ICT - FLIGHT CREW REPORTED ILS FLUX ON CAT II WHILE ON APPROACH INTO MCI. AIRCRAFT DIVERTED TO ICT, W HERE FLIGHT CREW RESET BOTH NAV SYSTEMS AND OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED FOR RETURN TO SER VICE. 2 L 7 2 4F RT 2008022000188 20080220 00188 NM 2008 2 20 HALA0800079 1 20080108 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 865 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION, AT SECTION 45, SEAT TRACKS AT LBL 88.5, STA 865. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION, IAW SRM 51-10-02, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101, REV 75. 2 L 7 2 4F RT A1NM 2008022000189 20080220 00189 NM 2008 2 20 HALA0800080 1 20080108 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 880 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION, SECTION 45 SEAT TRACK, AT LBL 88.5, STA 880. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW S RM 51-10-02, REV 75, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101, REV 75. 2 L 7 2 4F RT A1NM 2008022000213 20080220 00213 NM 2008 2 20 MWEA080024 1 20080204 A 5311 7150922507 FRAME BOEING 717 717200 1383700 NM FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 906ME 55170 UPPER BUCKET Z-FRAME LEFT END AT STATION 35.669 IS CRACKED. FABRICATED AND INSTALLED Z-FRAME. 2 L 7 2 4F TR A6WE 2008022000215 20080220 00215 NM 2008 2 20 MWEA080025 1 20080205 A 5310 7150922507 DOOR FRAME BOEING 717 717200 1383700 NM FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 906ME 55170 LOWER DEFLECTOR DOOR Z-FRAME IS CRACKED AT STATION 26.666 (LEFT). FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2008022000222 20080220 00222 NM 2008 2 20 MWEA080026 1 20080205 A 5310 7150922507 DOOR FRAME BOEING 717 717200 1383700 NM FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 906ME 55170 LOWER DEFLECTOR DOOR Z-FRAME CRACKED AT STATION 35.669 (LEFT). FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 2008022000224 20080220 00224 NM 2008 2 20 MWEA080027 1 20080205 A 5310 7150922507 DOOR FRAME BOEING 717 717200 1383700 NM FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 906ME 55170 LOWER DEFLECTOR DOOR Z-FRAME IS CRACKED AT STATION 35.669 (RIGHT). FABRICATED AND INSTALLED Z-FRAME. 2 L 7 2 4F TR A6WE 2008022000263 20080220 00263 NM 2008 2 20 HALA0800123 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1030-1034 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 2 CORROSION SECTION 45, SEAT TRACK AT LBL 88.5, STA 1030-1034. SEAT TRACK REPLACED. 2 L 7 2 4F RT A1NM 2008022000271 20080220 00271 NM 2008 2 20 HALA0800086 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 880 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION ON SEAT TRACKS AT BS 880. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICANTION IAW SRM 51-10-02 REV 76, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101, REV 76. 2 L 7 2 4F RT A1NM 2008022000283 20080220 00283 SO 2008 2 20 C2XA08TY029 1 20080212 A 3350 1317 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17108 145655 TYS - DURING ROUTINE MX THE FWD CEILING EMERGENCY LIGHT WAS FOUND INOP. MX REMOVED AND REPLACED THE LAMPS IAW 145XR AMM 33-50-06 AND OPS CHECKED GOOD. A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT 2008022000292 20080220 00292 SO 2008 2 20 C2XA08SH022 1 20080213 A 5320 14521713005 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 28529 145512 SHV - DURING C-CHECK CENTER OMEGA BEAM HAS PITTING ON OUTSIDE RADIOUS AT FR 20. MX REMOVED AND REPLACED CENTER OMEGA BE AM AT FR 20 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2008022100073 20080221 00073 NM 2008 2 21 08FDEA00464 1 20080216 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 MAIN DECK COMPARTMENT, AFTER REMOVAL OF DAMAGED LOWER CARGO CEILING PANELS FOUND SEAT TRACK AT STA 635, X = -8.50" CRACK ED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR P ER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008022100077 20080221 00077 EU 2008 2 21 08FDEA00488 1 20080117 A 5350 A539867512 RIB AIRBUS 310 A310222 3930315 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 TAIL CONE, RIBS BETWEEN FRAME 85 TO 87 AND STRINGER 33 RT DAMAGED. THE RIBS (SECTION-L) WERE REPLACED IN ACCORDANCE WIT H SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2008022100080 20080221 00080 WP 2008 2 21 08FDEA00493 1 20080218 A 5210 ADA00061 BEAM DOUG DC10 DC1030F 3023504 WP ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 CABIN OVERWING DOOR LT SIDE AFT UPPER STOP FITTING IS CRACKED. REMOVED AND REPLACED BEAM IAW FEDEX DWG NR ADA 3462 REV AE AND MD-10/DC-10 SRM 51-31-01, VOL II. 2 L 7 3 4F RT A22WE 2008022100116 20080221 00116 NM 2008 2 21 08FDEA00510 1 20080219 A 3020 39270811 CONTROL VALVE BOEING 727 727233 138408A NM NR 2 ENGINE FAILED A FDEA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 274FE 5463 5463 22039 AT ROTATION NR 2 DUCT ANTI-ICE OVERHEAT LIGHT ILLUMINATED TEMP OFF SCALE HIGH . AN QRH FOR ANTI-ICE DUCT OVERHEAT LIGHT. NR 2 ENGINE COULD NOT BE OPERATED ABOVE 1.25 EPR NR 2 DUCT OVERHEAT LIGHT ON MEL 30-11-A NR 2 ENGINE 13TH STAGE VALVE OPEN GOC ADVISED AIR TURN BACK TO MEM. REMOVED AND REPLACED NR 2 COWL ANTI-ICE THERMOSTATIC CONTROL VALVE IAW 727 MM-30 -21-021-4. A/C OK FOR RETURN TO SERVICE. 2 L 7 3 4F RT A3WE 2008022100133 20080221 00133 NM 2008 2 21 F3LA200800065 1 20080130 A 5321 D5367200000061 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 5503 2019 DURING THE C3/S1 C CHECK, INSPECTION REPORTED THE FORWARD CARGO PIT FLOOR PANEL 131QC HAD A PUNCTURE HOLE IN ITS UPPER S URFACE. MAINTENANCE REPAIRED THE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, PAGES 14 AND 15, STEPS A THROUGH M. UPON COMPLETION OF THE REPAIR, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008022100155 20080221 00155 NM 2008 2 21 HALA0800164 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1384 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 46, SEAT TRACKS AT RBL 88.5, STA 1384. REWORKED IAW SRM 53-00-52/101, AND REPLACED SEAT TRACK S IAW SRM WHERE DAMAGE WAS OUT OF LIMITS. 2 L 7 2 4F RT A1NM 2008022100167 20080221 00167 NM 2008 2 21 HALA0800167 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1320 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 46 SEAT TRACKS, AT RBL 88.5, STA 1320. REWORKED IAW SRM 53-00-52/101, REPLACED SEAT TRACKS IA W SRM WHERE DAMAGE WAS OUT OF LIMITS. 2 L 7 2 4F RT A1NM 2008022100174 20080221 00174 NM 2008 2 21 HALA0800175 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1186 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 46, SEAT TRACKS, AT RBL 88.5, STA 1186. REWORKED IAW SRM 53-00-52/101, AND REPLACED SEAT TRAC KS WHERE OUT OF LIMITS. 2 L 7 2 4F RT A1NM 2008022100175 20080221 00175 NM 2008 2 21 HALA0800176 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1094 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 46, SEAT TRACKS AT RBL 88.5, STA 1094. REWORKED IAW SRM 53-00-52/101, AND REPLACED SEAT TRACK S WHERE DAMAGE WAS OUT OF LIMITS. 2 L 7 2 4F RT A1NM 2008022100176 20080221 00176 NM 2008 2 21 HALA0800177 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 2008 24257 LEVEL 1 CORROSION SECTION 46, SEAT TRACKS AT RBL 88.5, STA 1197+20. REWORKED IAW SRM 53-00-52/101, AND REPLACED IAW SRM SEAT TRACKS WHERE DAMAGE WAS OUT OF LIMITS. 2 L 7 2 4F RT A1NM 2008022100178 20080221 00178 SO 2008 2 21 SWIA200819209 1 20080201 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 295UX 120295 EMERGENCY LIGHT AT ROW 6A IS DAMAGED, FLIGHT NR 5723. REPLACED EXIT SIGN PER MM 33-51-02. OPS CHECK OK. 2 L 7 2 4T RT A31SO 2008022100186 20080221 00186 EA 2008 2 21 SWIA200819216 1 20080210 A 2913 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K FLUID LOSS AP APPROACH 1 NM 07 710BR 7852 LOST SYSTEM NR 2 HYDRAULIC FLUID ON SHORT FINAL, FLIGHT NR 2591. REPLACED NR 2 HYDRAULIC SYSTEM ENGINE DRIVEN PUMP IAW AMM 29-11-01, PN: 887055, SN OFF: MX-642339. 2 L 7 2 4F RT A21EA 2008022100187 20080221 00187 EA 2008 2 21 SWIA200819217 1 20080206 A 7830 SWITCH CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER FAULTY A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 866AS 7517 RECEIVED A "LEFT THRUST REVERSER UNLOCK" CAUTION MESSAGE AFTER TAKEOFF, FLIGHT NR 3843. REPLACED THROTTLE LOCKOUT MICRO SWITCH IAW AMM 78-37-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008022100190 20080221 00190 NM 2008 2 21 08FDEA00428 1 20080214 A 5420 6519507223 INTERCOSTAL BOEING 727 727227 1384078 NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 NR 1 ENG LOWER COWL FWD END INTERCOSTAL CRACKED AND WORN MANUFACTURED AND INSTALLED NEW INTERCOSTAL FWD END OF NR 1 ENG COWL REF 65-19507 AND SRM 51-30-2. 2 L 7 3 4F A3WE 2008022100195 20080221 00195 NM 2008 2 21 08FDEA00438 1 20080214 A 5320 651986220 STRUCTURE BOEING 727 727227 1384078 NM BS 301-305 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 NOSE W/W AIRCRAFT INTERIOR SURFACE AT BS 301 TO 305 RBL 14", WL 169 TO 171 LONGITUDINAL CHORD ABOVE HORIZONTAL WALKWAY IS CORRODED REMOVED FASTENERS, BLENDED CORROSION, FOUND TO BE WITHIN LIMITS, ORIGINAL MATERIAL .350", MATERIAL REMAININ G .330' LOSS IS AT 5.7 PERCENT MAXIMUM LOSS IS 15 PERCENT, REF SRM 53-10-1 FIG 4 SHEET 2, ITEM E, NDT MAPPED BLENDED ARE A REF D6-48875 PART 4 51-00-00 FIG 2. FLAP PEENED, TREATED, PRIMED AND CIC APPLIED. REF EA 7-5310-113970 PART 1 STEPS 7, 8, 9, 12. FASTENERS INSTALLED REF ESR 7-5310-113970 PART 1 STEP 11, SRM 51-30-4 FIG 1. REPLACED WIRE CHANNEL REF EA 7-5310-113970 PART 1 STEP 13. THIS IS CLASSIFIED AS MINOR REPAIR LEVEL 1 CORROSION. 2 L 7 3 4F A3WE 2008022100201 20080221 00201 WP 2008 2 21 08FDEA00445 1 20080214 A 5320 NWJ600625 SUPPORT DOUG DC10 DC1030F 3023504 WP ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 AFT PIT, AFT BULKHEAD STRAP 187EA (NWJ6006-35) (NWJ6006-25NC) (MARKED AS "A2-A4) STRAP IS CRACKED ON THE (A2 END), HAS C ORROSION, IS DENTED AND ALL 4 FASTENER HOLES ARE GOUGED. FORMED SUPPORT PER DAC DWG NWJ6006 REV C AND FEDEX GMM 7-0-100 1, PG 2. FABRICATED SUPPORT PER FEDEX GMM 7-0-1001 AND DAC DWG NWS6006 REV B. ALODINED PER DC-10 SRM 51-21-01PARA 31, VOL II. PRIMED PER DC-10 SRM 51-21-01 PARA 24, VOL II. PAINTED PER DC-0 SRM 51-21-02, VOL II, PART MARKED PER FEDEX GM M 7-0-1001. 2 L 7 3 4F RT A22WE 2008022100202 20080221 00202 WP 2008 2 21 08FDEA00446 1 20080214 A 5320 NWJ600619 STRAP DOUG DC10 DC1030F 3023504 WP ZONE 100 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 AFT PIT, AFT BULKHEAD STRAP 187 CA (NWJ 6006-19)(MARKED AS B4/C4) IS DAMAGED, BENT, HAS 4 ELONGATED FASTENER HOLES AND IS CORRODED. MINOR REPAIR. FORMED HAT SECTION PER DAC DWG NWJ 6006 REV C AND FEDEX GMM 7-0-1001, PG 2. FABBED HAT SE CTION PER FEDEX GMM 7-0-1001 AND DAC DWG NWJ 6006 REV B. ALODINED PER DC-10 SRM 51-21-01 PARA 31, VOL II. PRIMED PER D C-10 SRM 51-21-01 PARA 24, VOL II. PAINTED PER DC-10 SRM 51-21-02, VOL II. PART MARKED PER FEDEX GMM 7-0-1001. 2 L 7 3 4F RT A22WE 2008022200001 20080222 00001 NM 2008 2 22 HALA0800205 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 850 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, AT RBL 54.75, SEAT TRACKS, STA 850, MAX BLEND OUT WAS 0.005". BLENDED IAW SRM 51-00-52. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200002 20080222 00002 NM 2008 2 22 HALA0800210 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 957 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS, AT LBL 88.5, STA 957, MAX DEPTH BLENDED WAS 0.029". BLEND IAW SRM 51-10-02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200003 20080222 00003 WP 2008 2 22 08FDEA00518 1 20080219 A 5320 ACA721613 BRACKET DOUG DC10 DC1030F 3023504 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MAIN CABIN WEB STA 590 TO STA 695 BRACKET HAS NUMEROUS NICKS. FABRICATED NEW - 13 CLIP IAW DWG ACA 7216 REV L. ALODINE D CLIP IAW MD/DC-10-30 SRM 51-21-01 PG 25, VOL II. PRIMED CLIP IAW MD/DC-10-30 SRM 51-21-01 PG 21, VOL II. PAINTED CLI P IAW MD/DC-10-30 SRM 51-21-02 PG 8, VOL II. INSTALLED CLIP IAW DAC DWG NR ACA 7216 REV L AND MD/DC-10-30 SRM 51-33-0 1 PG 25, VOL II. 2 L 7 3 4F RT A22WE 2008022200005 20080222 00005 NM 2008 2 22 HALA0800266 1 20080218 A 2612 89873202 CIRCUIT CARD BOEING 767 7673G5 1385126 NM FIRE DETECTION MALFUNCTIONED A HALA O OTHER N FALSE WARNING CR CRUISE 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM, EICAS STATUS MSG ENG FIRE LP1 DISPLAYED. PERFORMED FIM 26-11-00. REPLACED NR 1 ENG LOOP 1 FI RE DETECTION CARD (M681) PER 767 AMM 26-10-01. GROUND RUN CHECK OK. 2 L 7 2 4F RT A1NM 2008022200015 20080222 00015 NM 2008 2 22 HALA0800269 1 20080218 A 2841 INDICATION SYS BOEING 767 7673CB 1385187 NM FUEL QTY MALFUNCTIONED A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 590HA 23278 ETOPS SIGNIFICANT SYSTEM, AFTER FUELING, FUEL SLIP INDICATES AN ACTUAL DIFFERENCES OF 331GALLONS (325 ALLOWED) REQUEST T ANKS TO BE MEASURED. VERIFIED FUEL QTY USING MEASURING STICKS AS REQUESTED BY FLIGHT CREW, NO DEFECTS NOTED, FUELER VER IFIED FUEL LOAD. 2 L 7 2 4F RT A1NM 2008022200016 20080222 00016 NM 2008 2 22 2008UALA00683 1 20080206 A 5241 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FWD GALLEY DOOR, FWD FRAME IS CRACKED AT LWR STOP FITTING. MAJOR REPAIR: REMOVED DAMAGE. INSTALLED FRAME REPAIR SPLICE KIT. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200021 20080222 00021 NM 2008 2 22 HALA0800218 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 807 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS, AT LBL 54.75, STA 807. MAX DEPTH OF BLENDOUT WAS 0.007". BLENDED IAW SRM 51 -10-02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200022 20080222 00022 NM 2008 2 22 HALA0800213 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1002 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT LBL 88.5, STA 1002 MAX DEPTH BLENDED WAS 0.027". BLENDED IAW SRM 51-10-02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200027 20080222 00027 NM 2008 2 22 HALA0800241 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1153 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION, SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1153. REWORKED PER SRM 51-10-02 AND SRM 53-00-52. 2 L 7 2 4F RT A1NM 2008022200033 20080222 00033 NM 2008 2 22 2008UALA00690 1 20080206 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CENTER GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 653UA 25391 CENTER GALLEY LT EMERGENCY LIGHT STRIP INOP. REPLACED LT CENTER GALLEY EEL STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022200034 20080222 00034 NM 2008 2 22 2008UALA00691 1 20080206 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CENTER GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 653UA 25391 CENTER GALLEY RT EMERGENCY LIGHT (EEL) STRIP INOP. REPLACED EEL STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022200036 20080222 00036 NM 2008 2 22 2008UALA00693 1 20080206 A 5320 SUPPORT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE BS 246 RBL 15 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 665UA 29237 BS 246 AT RBL 15.78 PULLEY SUPPORT CRACKED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022200038 20080222 00038 NM 2008 2 22 2008UALA00698 1 20080207 A 5340 ATTACH FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FLOOR PANEL ADJACENT TO FORWARD GALLEY DOOR ATTACH INSERTS FOR AFT GIRT BAR ATTACH FITTING CORRODED. REPLACED FLOORBOAR D AFT NUT PLATE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200039 20080222 00039 NM 2008 2 22 HALA0800211 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 970 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION, SECTION 45 SEAT TRACKS, AT LBL 88.5, STA 970 MAX DEPTH BLENDED WAS 0.028". BLEND IAW SRM 51-10-02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200050 20080222 00050 NM 2008 2 22 2008UALA00701 1 20080207 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 4R DOOR LOWER CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 R4 DOOR LOWER GATE SKIN HAS CORROSION. REPLACED LOWER GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022200052 20080222 00052 NM 2008 2 22 2008UALA00703 1 20080207 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE L1 DOOR UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 665UA 29237 EMERGENCY EXIT LIGHT AT L-1 DOOR-UPPER SIGN IS NOT PROPERLY SECURED, CAUSES LENSE TO BE LOOSE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022200063 20080222 00063 WP 2008 2 22 AALA200800237 1 20080202 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 411AA 49322 ORD INFLIGHT T2481/02FEB - NOSE GEAR UNSAFE LIGHT ILLUMINATED AFTER NOSE GEAR RETRACTION. RETURNED TO ORD AND LANDED WI THOUT INCIDENT. ACCOMPLISHED NOSE GEAR SHOCK STRUT SEAL REPLACEMENT AND REPLACED TURNING TUBE CYLINDER AND LOWER BEARIN G ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022200065 20080222 00065 NM 2008 2 22 AALA200800280 1 20080210 A 2751 90004213 SENSOR BOEING 737 737823 13844BZ NM TE FLAPS INOPERATIVE A AALA O OTHER N FALSE WARNING DE DESCENT 1 SW 21 913AN 29514 DEN INFLIGHT T2281/10FEB - DURING APPROACH FLAP ASYMMETRY OCCURRED AT APPROXIMATELY TWO DEGREES. LANDED DEN WITHOUT IN CIDENT. REPLACED NUMBER SIX FLAP SKEW SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008022200079 20080222 00079 NM 2008 2 22 08FDEA00521 1 20080220 A 5330 6518380 SKIN BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 FWD PIT BILGE ( STA 720 ), BL 0 LWR SKIN CORRODED UNDER LEVELING COMPOUND. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMAINING THICKNESS OF .028 INCH. FABRICATED DOUBLER AND INSTALLED DOUBLER TO SKIN REF 53-30-3 PG 3-5. 2 L 7 3 4F A3WE 2008022200081 20080222 00081 NM 2008 2 22 AALA200800256 1 20080206 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 392AN 29429 SFO - EXTERNAL EMERGENCY LIGHT AT LEFT OVERWING EXIT INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LEFT OV ERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008022000208 20080220 00208 NE 2008 2 20 SIMA200805001 2 20080211 A 7320 HMU SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE NR 2 ENGINE MALFUNCTIONED A SIMA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 SW 21 307AE 340B307 785300 ON FLIGHT 3230 ON FINAL APPROACH INTO DFW, THE CREW WAS FOLLOWING APPROACH CHECKLIST, SELECTED AUTO COARSEN ON. AS THE SWITCH WAS SELECTED ON THE NUMBER TWO ENGINE FLAMED OUT WITH NO RELIGHT. CREW FOLLOWED AOM PROCEDURES AND DECLARED AN E MERGENCY. AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE. NOTED RIGHT ENGINE HMU INTERNAL FAILURE WITH DAMAGE TO ENGINE ACCESSORY GEAR BOX. REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY IAW E AGLE WORK CARD NR 72-4930. ALL OPERATIONAL CHECKS GOOD IAW SAAB 340AMM 71-00-00 AND 61-00-00 AND NR 8194; AIRCRAFT RETU RNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 2008022000258 20080220 00258 NM 2008 2 20 HALA0800112 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 973 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45 SEAT TRACK, AT LBL 11, STA 973. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 51-10-02,REV 76, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101, REV 75. 2 L 7 2 4F RT A1NM 2008022000265 20080220 00265 NM 2008 2 20 F3LA200800063 1 20080206 A 5321 D536720800000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 5503 2019 DURING C3/S1 C CHECK, INSPECTION REPORTED AFT CARGO PIT FLOOR PANEL 161FF HAD DENTS OUT OF LIMITS. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-01-00, TREATED, PRIMED AND PAINTED THE PANEL IN ACCORDANC E WITH THE REQUIREMENTS OF A319 SRM 51-21-11. UPON COMPLETION OF THE REPAIRS, THE PANEL WAS INSPECTED AND FOUND ACCEPTA BLE. 2 L 7 2 4F 4 F RT A28NM 2008022000277 20080220 00277 NM 2008 2 20 F3LA200800068 1 20080202 A 5753 D5755100601602 ARM AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE TE FLAP DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 5503 2019 DURING C3/S1 C CHECK, INSPECTION REPORTED THE LEFT WING, NUMBER 2 FLAP DRIVE LEVER EXTENSION ARM (STRUT) FITTING, ON THE FLAP, IS CHAFING INTO THE FITTING AT THE ATTACH POINT (BOTTOM AND TOP) ON THE FLAP. MAINTENANCE BLENDED AND CHAMFERED THE EDGE OF THE FITTING, TREATED, PRIMED AND PAINTED THE FITTING IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-57R-30041. UPON COMPLETION OF THE REPAIR, THE FITTING WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008022000279 20080220 00279 NM 2008 2 20 F3LA200800059 1 20080206 A 5321 D53672223700000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE CARGO BAY] DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 5503 2019 DURING C3/S1 C CHECK, INSPECTION REPORTED UNACCEPTABLE DENTS AND GOUGES IN THE AFT CARGO COMPARTMENT FLOOR PANEL 162BF. MAINTENANCE REPAIRED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 AND PRIMED AND REPAINTED THE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-21-11. UPON COMPLETION OF THE REPAIRS, THE FLOOR PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008022000280 20080220 00280 NM 2008 2 20 HALA0800156 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1400 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 2 CORROSION SECTION 46, SEAT TRACKS AT RBL 11, STA1400. REWORKED IAW SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022000298 20080220 00298 SO 2008 2 20 C2XA08SH032 1 20080219 A 5330 14533825001 DOUBLER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11544 145557 SHV - DURING C-CHECK SKIN DOUBLER AROUND FUSELAGE DRAIN AT FR 53 IS CORRODED. MX REMOVED AND REPLACED SKIN DOUBLER AROU ND FUSELAGE DRAIN AT FR53 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008022000299 20080220 00299 SO 2008 2 20 C2XA08IA059 1 20080216 A 3350 78241 BALLAST EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14940 145033 IAH - DURING MAINTENANCE INSPECTION THE INTERIOR LT OVERWING EMERGENCY HATCH EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MA INTENANCE REMOVED AND REPLACED THE NUMBER FOUR BALLAST, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPR OVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008022000300 20080220 00300 SO 2008 2 20 C2XA08IA060 1 20080212 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13553 1802 1802 145585 ONT - FLIGHT 125, DURING POST FLIGHT INSPECTION THE LT EMERGENCY EXIT LIGHT FWD OF WING WAS FOUND TO BE INOPERATIVE. MA INTENANCE REMOVED AND REPLACED THE NUMBER ONE BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022000313 20080220 00313 NM 2008 2 20 HNAA0800086 1 20080214 A 3350 6013211X BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 943HA 12873 489 167 DURING ROUTINE POST FLIGHT, THE RIGHT HAND AFT EMERGENCY EGRESS LIGHT AND ONE OF THE CENTER CEILING EMERGENCY LIGHTS WER E FOUND TO BE INOPERATIVE. MAINTENANCE CHANGED THE ROW 7DF EMERGENCY LIGHT BATTERY PACK (3351-PS4). SYSTEM OPS CHECKS WERE GOOD. 2 H 7 2 4T RT A13NM 2008022100098 20080221 00098 WP 2008 2 21 08FDEA00454 1 20080215 A 5321 ACA7373507 FLOORBOARD DOUG DC10 DC1030F 3023504 WP BS 595-675 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MAIN CABIN FLOORBOARD AT APPROX LBL 38, BETWEEN STA 595 TO 675 IS WARPED. FABBED FLOORBOARD PANEL AT STA 595-675 IAW DW G SRZ 25-005 REV F. LOCATED HOLES, COUNTERBORED HOLES, POTTED INSERTS, POTTED EDGES, CURED EDGES, SANDED EDGES, AP PLIED ANTI-SKID IAW DWG SRZ 25-005 REV F. MINOR REPAIR 2 L 7 3 4F RT A22WE 2008022100108 20080221 00108 NM 2008 2 21 08FDEA00465 1 20080216 A 5347 ACA7102519 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 621FE 48792 MAIN DECK COMPARTMENT, AFTER REMOVAL OF DAMAGED LOWER CARGO CEILING PANELS FOUND SEAT TRACK AT STA 635, X = -27.50 INCH CRACKED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJ OR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008022100120 20080221 00120 NM 2008 2 21 HALA0800148 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 2 CORROSION SECTION 46 SEAT TRACK AT RBL 11, STA 1197+108. REWORK IAW SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022100137 20080221 00137 WP 2008 2 21 08FDEA00456 1 20080215 A 5321 ACA3207515 FLOORBOARD DOUG DC10 DC1030F 3023504 WP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MAIN CABIN FLOORBOARD AT LBL - 20, BETWEEN STA 1821 TO 1881 IS SPONGY. FABBED FLOORBOARD IAW SRZ-25-005 REF F. INSTALL ED FLOORBOARD IAW SRM 51-31-01 VOL II. LOCATED, DIRLLED HOLES. INSTALLED INSERTS, INSTALLED ANTISKID IAW DWG SRZ 25 -005 REV F. INSTALLED FLOORBOARD IAW SRM 51-31-01, VOL II. MINOR REPAIR 2 L 7 3 4F RT A22WE 2008022100139 20080221 00139 NM 2008 2 21 F3LA200800060 1 20080206 A 5321 D5367406600000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 5503 2019 DURING C3/S1 C CHECK, INSPECTION REPORTED THE FORWARD CARGO PIT FLOOR PANEL 132DG WAS DELAMINATED AND HAD OUT OF LIMIT D ENTS. MAINTENANCE REPAIRED THE DELAMINATED AREA AND FILLED THE DENTS IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53 -02-00, PRIMED AND PAINTED THE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-21-11. UPON COMPLETION OF THE R EPAIR, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008022100147 20080221 00147 EU 2008 2 21 08FDEA00490 1 20080117 A 5350 A5398862420400 STRUT AIRBUS 310 A310222 3930315 EU TAILCONE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 TAIL CONE, SMALL SPOTS OF CORROSION AT TRACK LT, ATTACHMENT FITTING TO FR 86, STRUT-CROSS WAS REPLACED IN ACCORDANCE WIT H SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2008022100169 20080221 00169 NM 2008 2 21 HALA0800169 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1307 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 46, SEAT TRACKS AT RBL 88.5, STA 1307. REWORKED IAW SRM 53-00-52/101, AND REPLACED SEAT TRACK S WERE DAMAGE WAS OUT OF LIMITS. 2 L 7 2 4F RT A1NM 2008022100191 20080221 00191 NM 2008 2 21 08FDEA00429 1 20080214 A 5753 6521795405A FAIRING BOEING 727 727227 1384078 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 LT WING, I/B FLAP, I/B TRACK AFT FAIRING SKIN CRACKED OUT ON TOP SIDE I/B OF AFT ATTACH BOLT, BOLT MOUNT CUTOUT. REPLAC ED FAIRING WITH SERVICEABLE UNIT. NR 4 TRACK POSITION. INSTALLATION ACCOMPLISHED ON WORK CARD NR 75C001-01. THIS IS CL ASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008022100196 20080221 00196 NM 2008 2 21 08FDEA00439 1 20080214 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 727 727227 1384078 NM BS 1164-1166 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 AFT LWR CARGO BAY BS 1164-1166 FLOOR SUPPORT ANGLE AT RBL 4, HAS CORROSION ON UNDERSIDE. REMOVED CORROSION ON AFT LWR C ARGO BAY STA 1164 - 1166 FLOOR SUPPORT ANGLE AT RBL 4, REF SRM 51-10-6, MATERIAL LOSS OF 50 PERCENT, FOUND TO BE OUT OF LIMITS. REF SRM 53 10-1. FABRICATED REPAIR, REPAIR CHANNEL AND SPLICES REF SRM 53-10-5 FIG 4. TREATED AND PRIMED REP AIR PARTS REF SRM 51-10-2. INSTALLED REPAIR CHANNEL AND SPLICES, REF SRM 53-10-5 FIG 4 AND 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008022100200 20080221 00200 WP 2008 2 21 08FDEA00444 1 20080214 A 2810 ARB0872545 PANEL DOUG DC10 DC1030F 3023504 WP FUEL TANK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 RT WING TANK PLATE PANEL NR 634 AT IS CORRODED. MACHINED NEW FUEL PANEL (545) IAW DAC DWG ARB 0872 REV AV AND ALODINED AND PRIMED, 545 FUEL PANEL IAW DPS 4.50 -127 AND MIL-C-5541 AFTER FINDING ORIGINAL PANEL WAS UNDER LIMITS AFTER CORROSIO N REMOVAL. 2 L 7 3 4F RT A22WE 2008022200030 20080222 00030 NM 2008 2 22 HALA0800267 1 20080217 A 2150 CONTROLLER BOEING 767 7673CB 1385187 NM LT AC PACK MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM, LEFT PACK TEMP EICAS MESSAGES AND PACK INOP LIGHT ILLUMINATED OPERATED NORMAL MASTER STBY SELE CTED. TS PER FIM 21 51 00 FIG 103 BIT OF LEFT PACK TEMP CONTROLLER FAULTS L RAM INLET DOOR. DOOR ON BIT AND PREVIOUS F LIGHT VERIFY CHECKS OK SUBSEQUENT BITE HAS NO FAULTS OPERATED PACK FAULT DID NOT RETURN. 2 L 7 2 4F RT A1NM 2008022200032 20080222 00032 NM 2008 2 22 HALA0800248 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1197+64. REWORKED PER SRM 51-10-02 AND SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022200042 20080222 00042 NM 2008 2 22 HAL0800240 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1137 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1137. REWORKED PER SRM 51-10-02 AND SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022200049 20080222 00049 NM 2008 2 22 2008UALA00700 1 20080207 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR UPPER CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 R-1 DOOR UPPER GATE CRACKED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022200060 20080222 00060 NM 2008 2 22 AALA200800234 1 20080130 A 3350 D71702100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 948AN 30086 TUL - EMERGENCY LIGHT BATTERY PACK FOR MID TO AFT CABIN RIGHT SIDE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIG HTS AT MID TO AFT CABIN RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008022200076 20080222 00076 NM 2008 2 22 HALA0800246 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1197.30. REWORKED IAW SRM 51-01-02 AND SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022200082 20080222 00082 EU 2008 2 22 AALA200800241 1 20080203 A 3350 321441 POWER SUPPLY AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 JFK - EMERGENCY LIGHT TEST BUTTON AT LEFT NUMBER ONE DOOR DOES NOT ILLUMINATE DURING TEST. REPLACED POWER SUPPLY UNIT A T 29WL6 FOR EMERGENCY LIGHT TEST BUTTON AT LEFT NUMBER ONE DOOR. 2 L 7 2 4F RT A35EU 2008022200084 20080222 00084 NM 2008 2 22 AALA200800240 1 20080203 A 2100 A/C PACK BOEING 757 757223 1384957 NM LEFT CONTAMINATED A AALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 660AM 25294 BWI INFLIGHT T775/03FEB LGA TO MIA AT FLIGHT LEVEL 400 FLIGHT ATTENDANT REPORTED AFT AND MID LAVATORY SMOKE DETECTORS AC TIVATED FOLLOWED BY VISIBLE SMOKE AND SMELL IN CABIN AND COCKPIT. SMOKE BECAME MODERATE IN AFT CABIN AND SMOKE BEGAN TO DISSIPATE ON DESCENT AND AFTER LEFT AIR CONDITIONER PACK TURNED OFF. LANDED BWI WITHOUT INCIDENT. FOUND LEFT AIR COND ITIONING PACK AND MIX MANIFOLD CONTAMINATED WITH OIL. REPLACED LEFT AIR CYCLE MACHINE AND REHEATER AND CLEANED LEFT AND RIGHT AIR CONDITIONING PACK PNEUMATIC DUCTS AND MIX MANIFOLDS. ACCOMPLISHED PACK BURN. SYSTEM GROUND CHECKED NORMAL O PERATION. 2 L 7 2 4F RT A2NM 2008022200086 20080222 00086 NE 2008 2 22 2008UALA00710 2 20080208 A 7261 OIL SYSTEM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 ENGINE LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 213UA 30219 777034 RTFL DUE TO NR 1 OIL QUANTITY LOSS INDICATION. THE ENGINE'S ANGLE GEARBOX (AGB) WAS REPLACED AT HNL, AND THE AIRCRAFT R ETURNED TO SERVICE. PROBLEM DID NOT RECUR. SHOP INVESTIGATION FOUND THAT THE AGB SNOUT PACKING (IPC 72-62-00-001-001) W AS WORN FLUSH WITH THE GLAND. PACKING SHAVINGS WERE PRESENT, AND THE PACKING ALSO HAD TEARS. THIS IS A NEW FAILURE MOD E. THE PACKING DID NOT EXHIBIT ANY CHEMICAL DETERIORATION; ONLY MECHANICAL DAMAGE WAS EVIDENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008022200091 20080222 00091 NM 2008 2 22 HALA0800239 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1124 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION AT SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1124. REWORKED PER SRM 51-10-02, AND SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022200099 20080222 00099 NM 2008 2 22 2008UALA00720 1 20080209 A 5320 ANGLE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE BS 300 S10L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 902UA 25002 CABIN INTERCOSTAL CRACKED AT STA 300 STR 10 LT. REPAIRED ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200100 20080222 00100 NM 2008 2 22 2008UALA00721 1 20080210 A 5712 RIB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 LEFT WING WBL 135.5 AFT RIB LOWER FITTING CRACKED. REMOVED DAMAGE AND ACCOMPLISHED REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200101 20080222 00101 NM 2008 2 22 2008UALA00722 1 20080208 A 5320 FLOOR SUPPORT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 942-946 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 AFT CARGO COMPARTMENT STA 942 TO 946 RT FLOOR SUPPORT FITTING IS CORRODED. REPLACED RT FLOOR SUPPORT FROM BS 897 TO 94 7. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022500353 20080225 00353 EU 2008 2 25 USAA920080376 1 20080124 A 5320 D53471124200 SHEAR PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AW 543 SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON CABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, +Y1250. REPLACED CA BIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, +Y1250 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022500389 20080225 00389 NM 2008 2 25 USAA920080446 1 20080215 A 5330 6545776 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 PHX - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 747, S25R. REPAIRED FUSELAGE SKIN, BS 747, S25R IAW B737 SRM 53-00-01 RE PAIR 237. 2 L 7 2 4F RT A16WE 2008022500396 20080225 00396 NM 2008 2 25 DLM90080237 1 20080215 A 5530 LUG DOUG MD90 MD9030 3023690 NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 RT INBOARD VERTICAL STAB LUG CORRODED. REPAIRED RT INBOARD VERTICAL STAB LUG, IAW DAL ER/A 466168-14 DATED 02/15/08 REV A. 2 L 7 2 4F RT A6WE 2008022600043 20080226 00043 NM 2008 2 26 ASAA0852545 1 20080210 A 4940 2118966222 CONTROL UNIT BOEING 737 737890 1384527 NM APU UNKNOWN A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 587AS 35684 APU START ATTEMPT AFTER LANDING. BOTH STARTS UNSUCCESSFUL WITH FAULT LIGHT. TROUBLESHOT PER FIM 49 60 TASK 801. NO CU RRENT FAULTS. 2 L 7 2 4F RT A16WE 2008022600063 20080226 00063 EU 2008 2 26 USAA920080441 1 20080131 A 5347 D53730464200 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AW 543 SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON SEAT TRACK, BS 1377 / FR 32, -Y765. REPAIRED SEAT TRACK, BS 1377 / FR 32, -Y765 IAW A320 SRM 53-00-15. 2 L 7 2 4F RT A28NM 2008022600064 20080226 00064 NM 2008 2 26 USAA920080447 1 20080218 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 PHX - MAJOR REPAIR - OVERNIGHT CHECK - CRACKED FUSELAGE SKIN, BS 847, S23L - S24L. REPAIRED FUSELAGE SKIN, BS 847, S23L - S24L IAW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008022600069 20080226 00069 NM 2008 2 26 ASAA0852590 1 20080216 A 2160 3989083 MODULATING VALVE BOEING 737 737890 1384527 NM A/C BAY FAULTY A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 558AS 35177 AFTER ENGINE START DURING RECALL GOT A "CNTL CAB ZONE TEMP" LIGHT. FOUND CNTL CAB ZONE TRIM MOD VALVE FAULT LOGGED ON N R 1 TEMP CONTROLLER. REPLACED CONTROL CABIN TRIM MOD VALVE. GROUND BITE TEST OK. 2 L 7 2 4F RT A16WE 2008022600099 20080226 00099 NE 2008 2 26 DLM88080252 2 20080220 A 7510 DUCT DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 932DL 49719 725514 AFTER SELECTION CLIMB POWER GOT A FIRE LIGHT ON NR 1 ENGINE FOLLOWED BY A BELL, RETARDED ENG TO IDLE AND LIGHT WENT OUT. INSP AREA FOUND WIRING AROUND NOSE ANTI-ICE VALVE DAMAGED. FOUND DUCT BLOWN APART. REPLACED DUCT. AFT CLAMP SECURED , FWD LOOSE NEEDS MID CLAMP, CW 426246. INSTALLED MID CLAMP AND TIGHTENED FWD NUT. UPON FURTHER INSP FOUND LEFT IGV AN TI-ICE TUBE DAMAGED 417998. REPAIRED SEVEN DAMAGED WIRES GOING TO P1-808 AND P1-809 COWL ANTI-ICE VALVE AND LEFT ANTI-I CE VALVE. CHK GOOD PER M/M 943755. REPLACED ANTI-ICE DUCT. A/C RAN TAKEOFF POWER PER M/M. NO TROUBLE NOTED. 2 L 7 2 4F 4 F RT A6WE E9NE 2008022600122 20080226 00122 NM 2008 2 26 ASAA0842599 1 20080124 A 5320 694175710 INTERCOSTAL BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO RBL 21 INTERCOSTAL CRACKED BS 500 F TO 500 G. INTERCOSTAL REPLACED. 2 L 7 2 4F RT A16WE 2008022600181 20080226 00181 NM 2008 2 26 ASAA0842581 1 20080109 A 5320 69353654 INTERCOSTAL BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 CABIN FLOOR INTERCOSTAL STA 350 400 AT BL 0 IS CRACKED AT SCREW HOLES. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600184 20080226 00184 NM 2008 2 26 ASAA0842589 1 20080124 A 5320 694147327 INTERCOSTAL BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO LBL 21 FLOOR INTERCOSTAL CRACKED AT BS 500D TO 500E. CASCADE RESPONSIBILITY INTERCOSTAL REPLACED. 2 L 7 2 4F RT A16WE 2008022600195 20080226 00195 NM 2008 2 26 ASAA0842625 1 20080110 A 5320 693535214 TIE CLIP BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 TIE CLIP FOUND CRACKED AT STA 500G STR 7L. REPLACED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008022600199 20080226 00199 2008 2 26 ASAA0852639 4 20080220 A 2210 4082499903 AUTOLAND SYS BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA K NONE O OTHER LD LANDING 1 NM 02 577AS 35186 AUTOLAND EVAL TOUCHDOWN WELL LEFT OF CENTERLINE APPROXIMATELY 37'. ACCOMPLISHED LAND VERIFY TEST BITE GROUP 49. ALL TE STS PASS (REF AMM 22 11 00 201). AIRCRAFT REMAINS CATIIIA HGS ONLY. 2 L 7 2 4F RT A16WE 2008022600212 20080226 00212 NM 2008 2 26 ASAA0842656 1 20080117 A 5315 6545812206 FLOORBEAM BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FLOORBEAM AT FS 328 BL 0 CORROSION AT SCREW HOLE. FLOORBEAM AT FS 328 BL 0 REPAIRED IAW B737 400 SRM 53 10 51 FIG 201. 2 L 7 2 4F RT A16WE 2008022600217 20080226 00217 EA 2008 2 26 A6WA200840015 1 20080216 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE COCKPIT ACTIVATED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 441ZW 7777 NOSE GEAR DISAGREE WHEN GEAR RETRACTED. NOSE GEAR SHOWED RED, ALSO HEARD CLICKING NOISE BELOW FEET. AIR RETURN TO BTV, UPON GEAR EXTENSION GEAR SHOWED 3 GREEN DOWN AND LOCKED. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022600219 20080226 00219 EA 2008 2 26 A6WA200840017 1 20080119 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE WING FAILED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 GL 31 438AW 7748 ON APPROACH, WHEN FLAPS SELECTED, THE FLAPS FAILED TO MOVE AND (FLAPS FAIL) EICAS MESSAGE APPEARED, DIVERTED TO PIT, LAN DED WITHOUT INCIDENT. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022600223 20080226 00223 EA 2008 2 26 A6WA200840051 1 20080123 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RIGHT MALFUNCTIONED A A6WA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 413AW 7585 RT PACK PRESSURE UNCONTROLLABLE, FOLLOWS ENGINE POWER SETTINGS, FALLS OFF LINE AT HIGH POWER SETTINGS. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022600227 20080226 00227 EA 2008 2 26 A6WA200840056 1 20080130 A 2425 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE COCKPIT ACTIVATED A A6WA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 448AW 7814 IDG NR 1 CAUTION MESSAGE ON TAKEOFF, TAKEOFF ABORTED AT LESS THAN 80 KNOTS. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022600228 20080226 00228 EA 2008 2 26 A6WA200840058 1 20080201 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE WING FAILED A A6WA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 31 441ZW 7777 FLAPS FAIL CAUTION IN FLIGHT. FLAPS FAILED AT 40 DEGREES. EMERGENCY LANDING DECLARED. LANDING UNEVENTFUL. COMPLIED W ITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-108B STEPS 1.3 AND 1.4, FLAPS SYSTEM RESET OK. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022600229 20080226 00229 EA 2008 2 26 A6WA200840059 1 20080131 A 2751 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE T/E FLAP FAULTY A A6WA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 31 441ZW 8326 7777 FLAPS FAIL CAS MESSAGE, BOTH FLAPS INDICATE 42 DEGREES. PERFORMED FLAPS RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STE PS 1.3 AND 1.4 FLAPS RESET OK. (FERRIED TO ORF DUE TO HISTORY) LT BPSU WON`T STAY IN RIG. REMOVED AND REPLACED LT PBSU IAW AMM 27-51-10-. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022600230 20080226 00230 2008 2 26 2008UALA00828 4 20080214 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 581UA 26701 WIRE HANGING BELOW SLIDE ON DOOR 2L. RESTOWED D-RING STRING BEHIND BUSTLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022600232 20080226 00232 EA 2008 2 26 A6WA200840061 1 20080203 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE COCKPIT ACTIVATED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 460AW 7867 ON NORMAL TAKEOFF, SELECTED GEAR UP AND RECEIVED NLG DOOR OPEN AND GEAR DISAGREE WARNINGS AND WOW INPUT AND NWS INOP CAS MESSAGES. COMPLIED WITH QRH FOR ALL MESSAGES, ALL CLEARED, ALL 3 GEARDOWN AND LOCKED. RETURNED TO DEPARTURE FOR NORMA L LANDING. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022500242 20080225 00242 2008 2 25 2008UALA00825 4 20080213 A 2565 31104200 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 651UA PK0118 25389 ASPIRATOR LEAKS. CAUSE UNKNOWN. REPLACED ASPIRATOR AND BARREL ASSEMBLY. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500281 20080225 00281 NM 2008 2 25 DLM90080236 1 20080216 A 5310 BEAM DOUG MD90 MD9030 3023690 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 AFT CARGO BAY BRACKET AT AFT END OF LWR BEAM (DOOR CUT-OUT) CORRODED. REMOVED AND REPLACED BRACKET IN AFT OF LWR BEAM, IAW MD90 SRM 51-30-05. 2 L 7 2 4F RT A6WE 2008022500317 20080225 00317 NM 2008 2 25 DLM90080197 1 20080212 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM GE CF6 CF680C2B6F 30025 NE BS 588-759 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 704696 CABIN SEAT TRACK GOUGED AND CORRODED OUT OF LIMITS FS 588-759 RBL 54. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01. 2 L 7 2 4F 4 F RT A6WE E13NE 2008022500321 20080225 00321 NM 2008 2 25 DLM90080201 1 20080201 A 5320 9940443 CUSP WEB DOUG MD90 MD9030 3023690 NM GE CF6 CF680C2B6F 30025 NE BS 770 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 704696 LEFT CUSP WEB FS 770 EXFOLIATED AT LIGHTENING HOLE. REPAIRED CUSP WEB, IAW DELATA REPAIR DOC NR 53-05D SHT 1 FIG 827D. 2 L 7 2 4F 4 F RT A6WE E13NE 2008022500332 20080225 00332 NM 2008 2 25 USAA920080401 1 20080211 A 5330 6552988108 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 24781 CLT - MAJOR REPAIR - C6 CHECK - CRACKED FUSELAGE SKIN, BS 944, S24L. REPAIRED FUSELAGE SKIN, BS 944 S24L IAW USAIRWAYS EA 100236. 2 L 7 2 4F RT A16WE 2008022500333 20080225 00333 NM 2008 2 25 USAA920080402 1 20080206 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CANNING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 24781 CLT - MAJOR REPAIR - C6 CHECK - FUSELAGE SKIN HAS 6" BY 7" AREA THAT IS OIL CANNING, BS 727E, S22L - S24L. REPAIRED FUS ELAGE SKIN, BS 727E, S22L - S24L IAW USAIRWAYS TYPICAL REPAIR 53-27. 2 L 7 2 4F RT A16WE 2008022500354 20080225 00354 EU 2008 2 25 USAA920080377 1 20080124 A 5315 D53472194202 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AW 543 SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3043 / FR 64 - BS 3366 / FR 70, +Y515. REPLACED CABIN FLOORBEAM, BS 3043 / FR 64 - BS 3366 / FR 70, +Y515 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022500357 20080225 00357 EU 2008 2 25 USAA920080382 1 20080202 A 5315 D53472172202 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AW 543 SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3158 / FR 66 - BS 3207 / FR 67, +Y1280. REPLACED CABIN FLOORBEAM, BS 3158 / FR 66 - BS 3207 / FR 67, +Y1280 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022500363 20080225 00363 NM 2008 2 25 USAA920080418 1 20080206 A 5754 65C26603101 WEDGE BOEING 737 7374B7 1384702 NM L/E SLAT DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q5 CHECK - LEFT WING NR 3 SLAT TRAILING EDGE WEDGE HAS AREA OF DISBOND. REPAIRED LEFT WING NR 3 SL AT TRAILING EDGE WEDGE IAW USAIRWAYS TYPICAL REPAIR 57-42-03. 2 L 7 2 4F RT A16WE 2008022500371 20080225 00371 NM 2008 2 25 USAA920080426 1 20080211 A 5330 6545774 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT - MAJOR REPAIR - DAILY CHECK - CRACKED FUSELAGE SKIN, BS 762, S 19R. REPAIRED FUSELAGE SKIN, BS 762, S19R IAW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008022500385 20080225 00385 SO 2008 2 25 FDKA200802061 1 20080214 A 5320 14527016001 STRIKER EMB 145 EMB145LR 3260212 SO DOOR FRAME DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 THE CARGO DOOR STRIKER PLATES ON THE FORWARD AND AFT FRAMES ARE DAMAGED. THE DAMAGED PARTS HAVE BEEN REMOVED AND REPLAC ED. 2 L 7 2 4T RT T00011AT 2008022600093 20080226 00093 NM 2008 2 26 HALA0800235 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1017 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT LBL 11, STA 1017, MAX DEPTH OF BLENDOUT WAS 0.010. BLENDED IAW SRM 51-10-0 2. ALL BLENDOUT WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022600096 20080226 00096 NM 2008 2 26 AALA200800284 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 20G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 20G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022600100 20080226 00100 NM 2008 2 26 ASAA0842568 1 20080105 A 5320 654659247 CHANNEL BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT FLOOR CHANNEL FOUND CORRODED AT BS 767+6 LBL 13. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600115 20080226 00115 NM 2008 2 26 AALA200800303 1 20080211 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 348AN 33087 SFO - EMERGENCY EXIT SIGN LIGHT AT OVERHEAD LEFT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN L IGHT AT OVERHEAD LEFT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008022600158 20080226 00158 EU 2008 2 26 USAA920080439 1 20080214 A 5347 D53112815200 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SEAT TRACK, BS 605 / FR 12 TO BS 950 / FR 24, +Y1292. REPLACED CORRO SION ON CABIN SEAT TRACK, BS 605 / FR 12 TO BS 950 / FR 24, +Y1292, IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022600164 20080226 00164 NM 2008 2 26 ASAA0842659 1 20080111 A 5320 654655831 ANGLE BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT FAILSAFE ANGLE AT BS 907 STR 26R TO STR 27R FOUND CORRODED. REPAIRED WITH MADE REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600165 20080226 00165 NM 2008 2 26 ASAA0842648 1 20080106 A 5320 652072519 WEB BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO PIT ZEE WEB BETWEEN BS 440 AND BS 420 STR 26 RT SIDE HAS DENT WITH CRACK. FWD CARGO PIT ZEE WEB REPLACED WITH MADE REPAIR PART IAW B737 400 SRM DWG 65 20725. 2 L 7 2 4F RT A16WE 2008022600193 20080226 00193 NM 2008 2 26 ASAA0842623 1 20080108 A 5320 650163312 TIE CLIP BOEING 737 7374S3 1384711 NM FUSELAGE BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 TIE CLIP BROKEN AT BS 294.5 S13L. REPAIRED IAW ASA EA 5310 02758. 2 L 7 2 4F RT A16WE 2008022600200 20080226 00200 NM 2008 2 26 ASAA0852638 1 20080215 A 2421 761574B IDG BOEING 737 737890 1384527 NM NR 2 ENGINE DEFECTIVE A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 577AS 35186 FOLLOW UP TO FREQUENT SERVICING OF NR 2 IDG. ACCOMPLISH IDG STATIC LEAK CHECK. REPEAT LEAK TEST TO ELIMINATE INTERNAL AIR OIL OR FUEL OIL COOLER LEAKS. IF NO EXTERNAL LEAKS TO IDG FOUND REPLACE IDG. PERFORMED IDG STATIC LEAK CHECK. IDG SHOWS NO SIGN OF INTERNAL LEAKAGE. REPLACED NR 2 IDG, REPLACED NR 2 IDG OIL SEAL. OP AND LEAK CHECKS GOOD. GROUND VE RIFICATION COMPLETE ON NR 2 IDG. 2 L 7 2 4F RT A16WE 2008022600213 20080226 00213 NM 2008 2 26 ASAA0842660 1 20080122 A 5754 65C26601197 WEDGE BOEING 737 7374S3 1384711 NM L/E SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 NR 1 SLAT HAS DELAM AT O/B AFT END. REPLACED NR 1 SLAT DELAMINATED AT O/B AFT END IAW B737 400 SRM CH 51 70 10 REPAIR 4 . 2 L 7 2 4F RT A16WE 2008022600221 20080226 00221 EA 2008 2 26 A6WA200840048 1 20080202 A 3411 PITOT SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PITOT/STATIC SYS CONTAMINATED A A6WA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 GL 31 462AW 7875 ON TAKEOFF ROLL STANDBY IAS READS -0- KNOTS, REJECTED TAKEOFF AT ABOUT 85 KNOTS, MAX BTMS = 8,7,6,6. NOTE: NO HES/RTO I NSPECTION REQUIRED. FOUND WATER IN THE STANDBY PITOT/STATIC SYSTEM. PERFORMED CONTAMINATION REMOVAL OF THE STANDBY PIT OT/ STATIC SYSTEM. PERFORMED LEAK CHECK OF P3 SYSTEM IAW AMM 34-11-00. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022600247 20080226 00247 NM 2008 2 26 AMTA200800036 1 20080125 A 4920 APU BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE OIL CONSUMPTION A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 522AT 29330 DUE TO HISTORY OF APU USING EXCESSIVE OIL, APU IS CONSIDERED INOPERATIVE. APU OIL CONSUMPTION RATE 0.274 QTS PER HOUR, WITHIN THE ETOPS LIMIT IAW GMM CHAPTER 15, PAGE 18, OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008022600250 20080226 00250 NM 2008 2 26 AMTA200800039 1 20080129 A 2822 21C1321 SWITCH BOEING 757 75723N 1384973 NM FUEL SYSTEM UNSERVICEABLE A AMTA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 GL 11 519AT 27975 AFT BOOST PUMP LOW PRESS LIGHT FAILED TO ILLUM, AND EICAS FAILED TO DISPLAY WITH SW OFF. REMOVED AND REPLACED RT AFT BO OST PUMP SWITCH OPS CKD GOOD IAW AMM 28-22-00. (K) 2 L 7 2 4F RT A2NM 2008022600251 20080226 00251 NM 2008 2 26 AMTA200800040 1 20080129 A 3350 LENS BOEING 757 75723N 1384973 NM CABIN MISSING A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 522AT 29330 SEATS 17DEF, 20DEF, 28DEF, AND 7DEF EGRESS LENSES MISSING. REPLACED MISSING EGRESS LENS ROWS 17, 20, 28 AND 7DEF, OK FO R SERVICE. (K) 2 L 7 2 4F RT A2NM 2008022600256 20080226 00256 2008 2 26 AMTA200800046 4 20080201 A 2310 9640452012 TRANSCEIVER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE HF COMM MALFUNCTIONED A AMTA K NONE L NO TEST CR CRUISE 1 GL 11 560TZ 33525 LT HF TRANSMISSION INOPERATIVE AT ALL STATIONS. REMOVED AND REPLACED LT HF R/T GROUND CHECKS, OK. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008022600258 20080226 00258 NM 2008 2 26 AMTA200800048 1 20080202 A 2560 BATTERY BOEING 737 73783N 13844HI NM FLASHLIGHT DISCHARGED A AMTA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 11 308TZ 28244 FLASHLIGHT UNDER REAR FLIGHT ATTENDANT JUMPSEAT AIRCRAFT LT RED LIGHT DOES NOT BLINK. REMOVED AND REPLACED FLASHLIGHT B ATTERY IAW MM 25-64-00. OPS CHECKED GOOD. (K) 2 L 7 2 4F RT A16WE 2008022600260 20080226 00260 EA 2008 2 26 A6WA200840095 1 20080213 A 2530 3510003903 COFFEEMAKER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE GALLEY MALFUNCTIONED A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 31 464AW 6587 7890 IN FLIGHT WHEN FLIGHT ATTENDANT TURNED ON COFFEE MAKER IT STARTED TO SMOKE. STOPPED SMOKING WHEN IT WAS TURNED OFF. RE MOVED AND REPLACED COFFEE MAKER. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022600266 20080226 00266 EA 2008 2 26 A6WA200840062 1 20080210 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE WING FAILED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 455AW 7848 FLAP FAIL CAS MESSAGE IN FLIGHT, FLAP FAILED AT ZERO DEGREES. LDNG WT= 44,300. APPROX 150 KNTS. MAT BTMS = 5,4,2,2 AN D VERTICAL DESCENT RATE LESS THAN 10 FT PM. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B. STEPS 13 AND 1.4, FLA P SYS OK. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022600273 20080226 00273 WP 2008 2 26 AMTA200800101 1 20080219 A 5347 CARGO TRACK LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE CARGO BAY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 164AT 1238 CORROSION AT NUTPLATE AFT LT CORNER OF C-1 CARGO PIT, FWD SIDE OF MESC BULKHEAD ON BOTTOM SIDE OF CARGO RAIL. REPAIRED DAMAGED AREA IAW L1011, SRM 51-50-02, FIG 2 SHEET 2, PAGE 4. (K) 2 L 7 3 4F 4 F A23WE E12EU 2008022600274 20080226 00274 2008 2 26 AMAT200800050 2 20080202 A 7321 EEC BOEING 737 73783N 13844HI NM NR 2 ENGINE MALFUNCTIONED A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 318TZ 28247 AFTER ENG NR2 WAS STARTED WE GOT AN ENGINE CONTROL LIGHT CAME ON. NR 2 EEC BITE SHOWED FAULT CODE 75-20582 TBV DEMAND A ND SIGNAL DISAGREE. NO FAULTS ON CDS BITE. PERFORMED TEST 12 IAW MM 71-00-00-700-807. BOTH CHANNELS PASSED. NO FAULT S ON EEC. VERIFIED ELECT CONNECTORS AND FLUID LINE. (K) 2 L 7 2 4F RT A16WE 2008022600279 20080226 00279 NM 2008 2 26 AMTA200800056 1 20080114 A 5315 FLOORBEAM BOEING 737 73783N 13844HI NM BS 986 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 317TZ 28246 FLOORBEAM CORRODED NUTPLATE HOLES FROM BL34L TO BL45L, STA 986.5. ORIGINAL MATERIAL THICKNESS WAS .105, REMOVED MATERIA L .065 FOUND OUT OF LIMITS AND REPAIRED IAW SRM 53-70-51, EA 737-5370-08-A0003. ALODINED PRIMED AND PAINTED AREA IAW SRM 51-20-01. (K) 2 L 7 2 4F RT A16WE 2008022600280 20080226 00280 NM 2008 2 26 AMTA200800058 1 20080111 A 5320 CHANNEL BOEING 737 73783N 13844HI NM BS 767-847 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 317TZ 28246 ZEE CHANNEL FROM STA 847 TO STA 767 WITH EXFOLIATION CORROSION. ORIGINAL THICKNESS .040, MATERIAL LOSS .028 FOUND OUT O F LIMITS IAW SRM 53-00-53. REPAIRED ZEE CHANNEL IAW SRM 53-00-53-2R-5. ALODINE, PRIMED AND PAINTED IAW SRM 51-20-10. (K) 2 L 7 2 4F RT A16WE 2008022600281 20080226 00281 NM 2008 2 26 AMTA200800059 1 20080119 A 5320 FLOOR SUPPORT BOEING 737 73783N 13844HI NM BS 990 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 317TZ 28246 FLOOR SUPPPORT STRUCTURE WEB CORRODED AT STA 990, BL 335L, WL 208.1. REMOVED FLOOR SUPPORT WEB AT FS 990, BL35L, WL 208 .1 IAW SRM 51-40-02, FABRICATED AND INSTALLED WEB AT STA 990, BL 35L, WL 208.1 IAW EA 737-5300-08-A0011. ALODINED, PRIM ED AND PAINTED AFFECTED AREA IAW SRM 51-20-01. (K) 2 L 7 2 4F RT A16WE 2008022600285 20080226 00285 NM 2008 2 26 AMTA200800063 1 20080209 A 3350 D71701100 BATTERY PACK BOEING 737 73783N 13844HI NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 314TZ 30640 L1 DOOR EMERGENCY LIGHTING INOPERATIVE AT EXTERIOR AND INTERIOR POSITIONS. REMOVED AND REPLACED BATTERY PACK AS REQUIRE D. OPS CHECK GOOD. OF FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2008022700001 20080227 00001 NM 2008 2 27 WRLA2008021 1 20080211 A 5320 ADA33527 STANCHION DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 48632 DURING C-CHECK INSPECTION, CORROSION FOUND FWD CARGO COMPARTMENT AND DEFORM ON LT SIDE AFT BULKHEAD PANEL SUPPORT STANCH ION AT STA Y=1129. 2 L 7 3 4F 4 F RT A22WE E24NE 2008022700004 20080227 00004 EA 2008 2 27 COMA0860104 1 20080202 A 3234 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 720SW 21430 7297 FLIGHT 4957 - AFTER SELECTING GEAR DISAGREE AND DOOR DISAGREE MESSAGES WITH MAIN GEAR UP, NOSE DOWN. REPLACED NOSE GEAR SELECTOR VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008022700007 20080227 00007 EA 2008 2 27 COMA0860107 1 20080203 A 2120 32156222 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA RT A/C PACK FAULTY A COMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 01 786CA 9113 7333 FLIGHT 4964 - RECEIVED SMOKE TOILET AND RT PACK HIGH TEMP MESSAGES. DECLARED EMERGENCY, RETURNED TO CVG, LANDED WITHOUT INCIDENT. REPLACED RIGHT PACK PRSOV. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008022700011 20080227 00011 EA 2008 2 27 COMA0860111 1 20080205 A 3010 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYSTEM MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 912CA 7011 FLIGHT 5267 - RECEIVED RT WING ANTI-ICE CAUTION ON TAKEOFF ROLL, WINGS AND COWL "ON". ABORTED TAKEOFF, RETURNED TO GATE WITHOUT INCIDENT. PERFORMED OPERATION CHECK OF WING ANTI-ICE SYSTEM. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2008022700014 20080227 00014 WP 2008 2 27 WRLA2008024 1 20080211 A 5330 DOUBLER DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 136WA 47844 DURING MAINTENANCE INSPECTION AT SAA, CORROSION FOUND BETWEEN SKIN PANEL DOUBLER AND DOOR JAMB DOUBLER NEAR STA 1704 BET WEEN LONGERONS 45R-46R. REPAIRED PER SAA EA 010-5330-11-A1230 REV NC. 2 L 7 3 4F 4 F A22WE E23EA 2008022700017 20080227 00017 EA 2008 2 27 COMA0870006 1 20080211 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT ACTIVATED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 371CA 10082 FLIGHT 5543 - AVIONICS BAY DOOR CAUTION MESSAGE ON TAKEOFF. ABORTED TAKEOFF SAFELY. DEFERRED PER MEL 52-70-02. 2 L 7 2 4F RT A21EA 2008022700018 20080227 00018 EA 2008 2 27 COMA0860114 1 20080208 A 3350 59257 INVERTER CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 934CA 7042 FLIGHT 5141 - FLOOR EMERGENCY LIGHTS INOP. REPLACED NR 3 EMERGENCY LIGHT INVERTER. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008022700019 20080227 00019 NE 2008 2 27 COMA0860115 2 20080208 A 7200 CF343A1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30068 NE RIGHT VIBRATION A COMA E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 SO 01 427CA 3957 7460 807584 FLIGHT 5024 - DURING CRUISE, RIGHT ENGINE N1 VIBE SHOWED AMBER DASHES AT IDLE AND RIGHT ENGINE VIBE INDICATION SHOWED 3. 0. DECLARED EMERGENCY, DIVERTED TO STL, LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE. NO FURTHER DEFECTS. 2 L 7 2 4F 4 F RT A21EA E15NE 2008022700025 20080227 00025 NM 2008 2 27 UIEA200800046 1 20080215 A 5711 SPAR BOEING 747 7472D7B 1384803 NM RT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 WS 410 - WS 470 FRONT SPAR CORROSION EVIDENT ON RIGHT WING. BLENDED OUT CORROSION IAW SRM 51-10-01. REPROTECTED PER 51 -10-02. 2 L 7 4 4F RT A20WE 2008022700030 20080227 00030 WP 2008 2 27 IXXA08SMN006S 1 20080114 A 5753 SKIN DOUG DC8 DC862F 3021972 WP TE FLAP DELAMINATED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING JOINT FLAP DELAMINATED SKIN. REMOVED DAMAGED JOINT FLAP. INSTALLED NEW JOINT FLAP IAW DC8 SRM 51-3-0, 51-3-1. 2 L 7 4 4F 4A25 2008022700035 20080227 00035 NM 2008 2 27 UIEA200800018 1 20080126 A 5730 SKIN PANEL BOEING 747 7472D3B 1384805 NM ZONE 600 DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 RT WING LOWER FIXED LEADING EDGE HAS A 12.0 INCH LONG BY 10.0 INCH WIDE AREA OF DELAMINATION. PERMANENT REPAIR ACCOMPLI SHED AS PER SRM 51-40-09 FIG 18, SHEET 1, 2, AND 5, PREPREG 250 DEGREES F CURE. ALSO REFERENCE EO NR 4757A412. 2 L 7 4 4F RT A20WE 2008022700036 20080227 00036 EA 2008 2 27 COMA0860116 1 20080209 A 5297 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR LOOSE A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 918CA 7018 FLIGHT 5311 - RECEIVED PAX DOOR OUTER HANDLE CAUTION MESSAGE. DIVERTED TO GSP, LANDED WITHOUT INCIDENT. FOUND CARGO DO OR HARNESS CONNECTOR LOOSE. REMOVED, CLEANED AND REINSTALLED HARNESS. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008022700037 20080227 00037 EA 2008 2 27 COMA0860117 1 20080209 A 2421 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA NR 1 IDG LOW A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 804CA 7352 FLIGHT 5186 - DURING TAKEOFF, RECEIVED IDG 1 CAUTION, CONFIG SPOILERS WARNING, AND GENERATOR 1 OFF CAUTION MESSAGES. AB ORTED TAKEOFF, RETURNED TO GATE. FOUND IDG 1 OIL LEVEL LOW. SERVICED TO PROPER LEVEL. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008022700042 20080227 00042 NM 2008 2 27 UIEA200800019 1 20080126 A 5755 PANEL BOEING 747 7472D3B 1384805 NM NR 10 SPOILER DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 RT WING NR 10 SPOILER PANEL HAS A 5.0 INCH BY 5.0 INCH AREA OF DELAMINATION AT UPPER SIDE, OUTBOARD, TRAILING EDGE. PER MANENT REPAIR ACCOMPLISHED AS PER SRM 51-40-06 FIG. 1 AND 4 AND SRM 51-40-20, PREPREG 250 DEGREES F CURE. ALSO REFERENC E EO NR 4757A413. 2 L 7 4 4F RT A20WE 2008022700043 20080227 00043 2008 2 27 COMA0860122 4 20080211 A 3418 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING MALFUNCTIONED A COMA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 924CA 7026 FLIGHT 5362 - STALL FAIL CAUTION MESSAGE "ON" IN FLIGHT. EMERGENCY DECLARED, A/C LANDED SAFELY. RESET STALL COMPUTER, MESSAGE CLEARED, NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008022700062 20080227 00062 EA 2008 2 27 COMA0860134 1 20080214 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 SO 01 932CA 18 7038 FLIGHT 5361 - RECEIVED FLAP FAIL MESSAGE, DECLARED EMERGENCY, DIVERTED TO GRB, LANDED WITHOUT INCIDENT. REPLACED RIGHT WING BPSU. PERFORMED SI-2-27I0002. RE-SHIMMED RIGHT OUTBOARD FLAP AND RIGGED LEFT BPSU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008022700063 20080227 00063 EA 2008 2 27 COMA0860135 1 20080215 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 920CA 7022 FLIGHT 5403 - FLOOR EMERGENCY LIGHTING AT ROW 8 IS INOP. REPLACED EMERGENCY LIGHTING FLOOR STRIP. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008022700071 20080227 00071 NM 2008 2 27 ASAA0842554 1 20080117 A 5320 654587545 SILL BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD GALLEY SERVICE DOOR SILL CHORD FROM STA 291.5 TO 330 IS CORRODED. SILL CHORD REPLACED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008022700072 20080227 00072 NM 2008 2 27 ASAA0842555 1 20080117 A 5315 6545808198 FLOORBEAM BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FLOORBEAM AT FS 294 BL L CORROSION AROUND SCREW HOLE. CORROSION BLENDED OUT AND FOUND TO BE BEYOND LIMITS. MATERIAL RE MOVED 0.030" OUT OF 0.100" THE ORIGINAL THICKNESS. REPAIRED IAW B737 400 SRM CH 53 10 51 FIG 201. 2 L 7 2 4F RT A16WE 2008022700085 20080227 00085 NM 2008 2 27 SWAA080890 1 20080218 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 246LV 32507 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 5 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008022700086 20080227 00086 NM 2008 2 27 SWAA080891 1 20080218 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 252WN 34973 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008022700088 20080227 00088 NM 2008 2 27 SWAA080872 1 20080217 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 406 AND BS 414, LBL 2 AND LBL 4. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008022700089 20080227 00089 NM 2008 2 27 SWAA080873 1 20080218 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700090 20080227 00090 NM 2008 2 27 SWAA080874 1 20080218 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700091 20080227 00091 NM 2008 2 27 SWAA080887 1 20080218 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, BL 0. REPAIRED SKIN P ER SRM. 2 L 7 2 4F RT A16WE 2008022700093 20080227 00093 NM 2008 2 27 SWAA080898 1 20080218 A 2560 P2070001 FLASHLIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 423WN 29827 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2008031300015 20080313 00015 NM 2008 3 13 ASAA0842686 1 20080227 A 5210 6552873158 HINGE BOEING 737 7374Q8 138447Q NM L2 DOOR LACK OF LUBE A ASAA K NONE O OTHER NR NOT REPORTED 1 NM 02 765AS 25102 L2 DOOR GRINDING STIFF & DIFFICULT TO CLOSE & OPEN. LUBRICATED UPPER HINGE, L2 DOOR OP CHECKS GOOD. 2 L 7 2 4F RT A16WE 2008031300036 20080313 00036 NM 2008 3 13 2008UALA01119 1 20080301 A 2560 BRACKET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GIRT BAR MISALIGNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 DOOR 3R NO DOOR ARMED LIGHT. FOUND GIRT BAR BRACKET MISALIGNED. REINSTALLED GIRT BAR BRACKET, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031300057 20080313 00057 EU 2008 3 13 YENA2008018 1 20080220 A 3240 389575001 SHUTOFF VALVE EMB ERJ190 ERJ190100IGW 3260408 EU BRAKE SYS FAILED A YENA O OTHER J WARNING INDICATION AP APPROACH 1 EA 15 283JB 852 852 19000125 FLT 1003, BOS-JFK, BRAKE LT FAULT ON EICAS UPON GEAR EXTENSION. REMOVED AND REPLACED O/B MAIN BRAKE SOV PER AMM 32-41-0 3, OPS CHECK GOOD. A/C OK FOR SERVICE. 2 L 7 2 4F RT A57NM 2008031300078 20080313 00078 NM 2008 3 13 2008UALA01151 1 20080229 A 3397 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 533UA 25073 COACH CLASS EEL FWD AND AFT SECTIONS INOP. REPLACED FEEDER CABLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031300080 20080313 00080 NM 2008 3 13 2008UALA01153 1 20080301 A 3397 POWER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 657UA 27112 EEL ADJACENT TO DR 1R INOP. REPAIRED POWER CABLE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031300083 20080313 00083 NM 2008 3 13 ASAA0852692 1 20080304 A 2750 285A12001 FSEU BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 02 546AS 30022 FLAPS WOULD NOT EXTEND NORMALLY. ATTEMPTED TO EXTEND FLAPS VIA ALT EXTENSION BUT TRAILING EDGE FLAPS LOCKED OUT. LEADI NG EDGE DEVICES EXTENDED NORMALLY VIA ALT EXTENSION. MADE TRAILING EDGE FLAP UP LANDING. LANDING WEIGHT = 130 000 LBS B RAKES ON SPEED = 170 KTS. DUE TO HISTORY REPLACED FLAP POSITION INDICATOR. REPLACED FLAP SLAT ELECTRONICS UNIT. OP CH ECK & BITE SHOW NO ACTIVE FAULTS. CHECKED SKEW SENSORS ALL WITHIN RANGE. INSPECTED WIRING AT EACH SENSOR & FLAP TRANSM ITTER NO FAULTS FOUND. OLD FSEU SHOWED NO EXISTING FAULTS WHEN TESTED. 2 L 7 2 4F RT A16WE 2008031300102 20080313 00102 NM 2008 3 13 2008UALA01171 1 20080229 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 793UA 26946 2E SIDE PANEL EMERGENCY ESCAPE LIGHT ASSY DAMAGED. REPLACED 2E EMERGENCY LIGHT ASSY. OPS OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008031300107 20080313 00107 EA 2008 3 13 HNAA0800095 1 20080220 A 2424 51608003 GCU DHAV DHC8 DHC8311 1386006 EA NR 2 INTERMITTENT A HNAA K NONE J WARNING INDICATION CR CRUISE 1 EA 07 337EN 30151 3428 284 AFTER TAKEOFF EMERGENCY LIGHTS IN CABIN, ENGINE INTAKE HEAT (BOTH LEFT AND RIGHT OPEN AND HEATER) AND PROP SYNC ADVISORY LIGHTS FLICKERED INTERMITTENTLY UNTIL EMERGENCY LIGHTS WERE SELECTED OFF. REPLACED NR 2 GCU, ADVISORY LIGHTS DIM AND T EST BOX AND F/A'S EMERGENCY LIGHT SWITCH. 2 H 7 2 4T RT A13NM 2008031300143 20080313 00143 WP 2008 3 13 08FDEA00735 1 20080305 A 5730 ARC0357 SKIN DOUG MD10 MD1010F 3022112 WP RT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 RT WING PANEL 641LB INTERIOR SKIN IS GOUGED (2 PLACES). REPAIRED THE TWO GOUGED AREAS BY REMOVING THE DAMAGE. FABRICATI NG A NEW CORE PLUG, FILLER & DOUBLERS USING BONDING REPAIRS IAW SRM 51-71-00; VOL II. ALODINED, PRIMED, SEALED AND PAIN TED IAW SRM 51-21-02; VOL II. MINOR REPAIR 2 L 7 3 4F RT A22WE 2008031300159 20080313 00159 EU 2008 3 13 08FDEA00750 1 20080306 A 5420 A5461111250100 SUPPORT BRACKET AIRBUS 310 A310203 3930313 EU NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 PYLON FIRE EXTINGUISHER NR 2 SUPPORT BRACKET IS CRACKED. CLEANED MARKED AREA PER AMM 12-21-11-0. ACCOMPLISHED HF EC IAW NTM 51-10-01 PT 6 USING T8257A. NO CRACKS NOTED. PRIMED CLEANED AREA PER SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008031300162 20080313 00162 NM 2008 3 13 SWAA081188 1 20080303 A 5322 69363656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 16R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008031300190 20080313 00190 NM 2008 3 13 SWAA081158 1 20080302 A 5754 65C26601 SLAT BOEING 737 7375H4 138449D NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT OUTBOARD T/E. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008031300223 20080313 00223 NM 2008 3 13 SWAA081163 1 20080229 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 224WN 32493 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008031300243 20080313 00243 NM 2008 3 13 SWAA081155 1 20080229 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR LOWER HINGE CUTOUT SKIN CRACKED AT LOWER CORNER. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300245 20080313 00245 NM 2008 3 13 SWAA081193 1 20080303 A 3350 65C27093 LIGHT BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008031300247 20080313 00247 NM 2008 3 13 SWAA081202 1 20080303 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031300249 20080313 00249 NM 2008 3 13 SWAA081204 1 20080303 A 5311 6546550 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300269 20080313 00269 NM 2008 3 13 SWAA081228 1 20080304 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031300278 20080313 00278 2008 3 13 SWAA081238 4 20080304 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031300287 20080313 00287 EA 2008 3 13 SWIA200819317 1 20080301 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR WORN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 410SW 7066 FLT 3858 - PASSENGER DOOR HANDLE WILL NOT STOW. REPLACED PAX DOOR OUTER HANDLE ASSEMBLY IAW AMM 52-11-03. OPS CHECK GO OD. 2 L 7 2 4F RT A21EA 2008031300288 20080313 00288 EA 2008 3 13 SWIA200819318 1 20080301 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX DIRTY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 498CA 7792 FLT 2511 - MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. CLEANED, LUBED AND CYCLED DOOR SEVERAL TIMES IAW CRJ AMM 52-70-00 . OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008022200102 20080222 00102 NM 2008 2 22 2008UALA00723 1 20080208 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FWD GALLEY DOOR SN 1245 FRAME CRACKED AT UPPER AFT CORNER NEXT TO THE STOP FITTING. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200106 20080222 00106 NM 2008 2 22 AALA200800249 1 20080204 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 625AA 24583 DFW - EMERGENCY LIGHT AT SEAT 1E HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 1E. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008022200107 20080222 00107 NM 2008 2 22 AALA200800248 1 20080204 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 625AA 24583 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 14D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008022200109 20080222 00109 NM 2008 2 22 AALA200800251 1 20080205 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 951AA 29538 DFW - EMERGENCY LIGHT AT AFT RIGHT DOOR EXIT INDICATOR LIGHT BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT AFT RIGHT DOOR EXIT INDICATOR LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008022200115 20080222 00115 NM 2008 2 22 HALA0800221 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 958 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT LBL 54.75 STA 958, MAX DEPTH OF BLEND OUT WAS 0.005". BLENDED IAW SRM 51-1 0-02. ALL BLENDOUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200117 20080222 00117 NM 2008 2 22 HALA0800238 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1105 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1105. REWORK PER SRM 51-10-02 AND SRM 53-00-02. 2 L 7 2 4F RT A1NM 2008022200120 20080222 00120 NM 2008 2 22 2008UALA00725 1 20080208 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FUSELAGE DOOR 2L LOWER HINGE CUTOUT IS CRACKED AT LOWER FWD CORNER. MAJOR REPAIR: INSTALLED DOUBLER AND TRIPLER WITH A FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200123 20080222 00123 NM 2008 2 22 2008UALA00728 1 20080209 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 EXTERNAL FUSELAGE SKIN HAS CRACKED FASTENER HOLE AT FWD GALLEY DOOR LOWER HINGE CUTOUT. MAJOR REPAIR: REMOVED DAMAGE. INSTALLED REPAIR DOUBLER WITH FILLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200125 20080222 00125 NM 2008 2 22 2008UALA00730 1 20080210 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 303 S13L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 EXTERNAL FUSELAGE SKIN FASTENER HOLE CRACKED FWD ENTRY DOOR LOWER HINGE CUTOUT, BS 303 STR 13L. MAJOR REPAIR: REMOVED D AMAGE. INSTALLED REPAIR DOUBLER AND FILLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200126 20080222 00126 NM 2008 2 22 2008UALA00731 1 20080210 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 303 S10L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 EXTERNAL FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR UPPER HINGE CUTOUT 2 EA FASTENER HOLES BS 303 STR 10L. MAJOR REPAIR: I NSTALLED REPAIR DOUBLER WITH FILLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200127 20080222 00127 NM 2008 2 22 2008UALA00732 1 20080210 A 5340 ATTACH ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 348 S15L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FUSELAGE STR 15L INTERCOSTAL LOWER ATTACH ANGLE CRACKED BS 348. MAJOR REPAIR: REPLACED INTERCOSTAL ATTACH ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200135 20080222 00135 NM 2008 2 22 2008UALA00739 1 20080208 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 767 S25R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 LOWER FUSELAGE BS 767 STR 25R STRINGER CLIP CRACKED. MAJOR REPAIR: REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200138 20080222 00138 NM 2008 2 22 2008UALA00742 1 20080210 A 5310 STOP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR FRAME CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 302UA 23643 FWD CARGO DR CUTOUT, FWD FRAME AT LWR STOP PAD FITTING CRACKED ON FWD SIDE OF FRAME IN UPPER RADIUS. MAJOR REPAIR: ACCO MPLISHED REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200139 20080222 00139 NM 2008 2 22 2008UALA00743 1 20080208 A 5753 WEDGE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE TE FLAP DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 302UA 23643 DURING RIGGING OF LEFT WING INBOARD SPOILER FOUND MID FLAP TRAILING EDGE LOWER SKIN DELAMINATED AND SEPARATED FROM MIDFL AP. ACCOMPLISHED REPAIR OF DELAMINATED SKIN. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200141 20080222 00141 NM 2008 2 22 2008UALA00745 1 20080210 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 DOOR 4R AFT SILL EMERGENCY LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031300289 20080313 00289 EA 2008 3 13 SWIA200819319 1 20080301 A 3520 OXYGEN SYSTEM CNDAIR CL600 CL6002B19 1900309 EA FAILED A SWIA G B O2 MASK DEPLOYED EMER. DESCENT J WARNING INDICATION NR NOT REPORTED 1 NM 07 926SW 7687 FLT 5949 - RECEIVED "CABIN ALT" WARNING MESSAGE AND O2 MASKS DEPLOYED. REPLACED RIGHT PRSOV, REPLACED O2 GENERATORS AND REPACKED O2 MASKS IAW CRJ MM 35-12-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008031300295 20080313 00295 NM 2008 3 13 DL76L080307 1 20080302 A 3150 WARNING MESSAGE BOEING 767 767332 1382001 NM FALSE ACTIVATION A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 184DN 27111 CENTER ADP PRESS LIGHT AND EICAS MSG. PERFORMED RESET PER FIM. CENTER ADP OPS CKS OK. 2 L 7 2 4F RT A1NM 2008031300305 20080313 00305 NM 2008 3 13 DL757080316 1 20080304 A 2121 731376 FAN BOEING 757 757232 1384965 NM EQUIP COOLING FUMES A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 631DL 0341 23612 AT CRUISE, CREW HAD FUMES IN COCKPIT ELEC FUMES. CREW DIVERTED INTO NAS, DECLARED EMERGENCY. EICAS MSG EQUIP COOLING F AN AND ECS MSG FWD EQUIP SUP FAN 1. REPLACED SUPPLY FAN NR 1, OPS CHECKED OK PER MM. REMOVED MCO A PLAC. 2 L 7 2 4F RT A2NM 2008031300315 20080313 00315 EA 2008 3 13 MASA200800185 1 20080305 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDS A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27172 7172 FLT 7167, IAD-CAE. PAX DOOR WILL NOT CLOSE FROM INSIDE. MX PERFORMED OP CHECKS, OP CHECKS GOOD. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2008031300346 20080313 00346 EU 2008 3 13 08FDEA00753 1 20080306 A 5411 FRAME AIRBUS 310 A310203 3930313 EU NR 2 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 PYLON A-FRAME IS CRACKED AT STA 1115/RIB 21. REMOVED A5451675001 FLODED SHEET METAL SECTION & CRACKED A54521550100 TEE PER SRM 51-40-21 PARA 5. ORDERED & RECEIVED NEW A54521550100 TEE. LOCATED, DRILLED & DEBURRED FASTENER HOLES ON NEW TEE IAW SRM 51-40-40. INSTALLED NEW TEE & FOLDED SHEET METAL SECTION PER SRM 51-40-21; PARA 5. MINOR REPAIR 2 L 7 2 4F RT A35EU 2008031300351 20080313 00351 EU 2008 3 13 08FDEA00758 1 20080306 A 7830 LATCH AIRBUS 310 A310203 3930313 EU THRUST REVERSER CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 1 ENGINE INBD T/R, LOWER FWD LATCH DOOR IS CHAFED TO A KNIFE EDGE AND CRACKED OUT IN THE UPPER CORNER. REMOVED DAM AGED DOOR AND INSTALLED NEW DOOR P/N 9071M77G11; PO 610928.2. IAW SRM 51-40-21; PARA 5. MINOR REPAIR 2 L 7 2 4F RT A35EU 2008031300353 20080313 00353 NM 2008 3 13 SWAA081175 1 20080303 A 5311 6545812 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 303, STR 4L. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008031300357 20080313 00357 NM 2008 3 13 ASAA0842696 1 20080118 A 5330 654576666 SKIN BOEING 737 7374S3 1384711 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FUSELAGE GOUGE AT BS 500 G+1" 2" BELOW STR 13R (CASCADE RESPONSIBILITY HUMAN FACTORS). REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008031300358 20080313 00358 NM 2008 3 13 ASAA0842697 1 20080130 A 5330 654576666 SKIN BOEING 737 7374S3 1384711 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FUSELAGE SKIN DAMAGE AT 500 E 3" BELOW STR 13R (CASCADE RESPONSIBILITY HUMAN FACTORS). REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008031300364 20080313 00364 NM 2008 3 13 SWAA081244 1 20080305 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008031300365 20080313 00365 NM 2008 3 13 SWAA081246 1 20080305 A 5311 65C35356 FRAME BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 413WN 29819 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300366 20080313 00366 NM 2008 3 13 SWAA081245 1 20080305 A 5311 6546596 FRAME BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 413WN 29819 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300367 20080313 00367 NM 2008 3 13 SWAA081263 1 20080303 A 2121 215201 GASPER FAN BOEING 737 7375H4 138449D NM E&E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 515SW 25154 CREW REPORTS ODOR FROM RT PACK, TURNED PACK OFF. FOUND ODOR COMING FROM GASPER FAN. REMOVED AND REPLACED GASPER FAN PE R MM. 2 L 7 2 4F RT A16WE 2008031300377 20080313 00377 NM 2008 3 13 SWAA081264 1 20080306 A 5512 65C25727 SKIN BOEING 737 7373G7 1384595 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 66 AND STA 94. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008031300378 20080313 00378 NM 2008 3 13 SWAA081265 1 20080306 A 5311 6546539 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME INNER CHORD CRACKED AT RT BS 616. REPAIRED FRAME CHORD PER SRM. 2 L 7 2 4F RT A16WE 2008031300379 20080313 00379 NM 2008 3 13 SWAA081254 1 20080305 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008022200154 20080222 00154 NM 2008 2 22 2008UALA00750 1 20080209 A 3350 276005 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT LIGHTS INOP: LT OVERWING 2 AFT ASSY. REPLACED FUSE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022200155 20080222 00155 NM 2008 2 22 2008UALA00752 1 20080209 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY LIGHT INOPERATIVE, R5 DOOR SLIDE ILLUMINATED. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022200156 20080222 00156 NM 2008 2 22 2008UALA00753 1 20080209 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 WALL EEL INOP, DR5R CROSS AISLE. REPLACED FEEDER CABLE. EEL SYSTEM OP CHECKS OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022200157 20080222 00157 NM 2008 2 22 HALA0800220 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 885 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT LBL 54.75, STA 885, MAX DEPTH OF BLEND OUT WAS 0.005". BLENDED IAW SRM 51- 10-02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022500001 20080225 00001 NM 2008 2 25 HNAA080058 1 20080203 A 3350 82520089101 LENS DHAV DHC8 DHC8102 2809003 NM CABIN INADEQUATE A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 804EX 42387 42387 227 DURING SCHEDULED INSPECTION, THE CABIN EMERGENCY EXIT ILLUMINATED 'EXIT' SIGNS WERE FOUND TO BE DIM. MAINTENANCE CHANGE D THE LENSES OVER THE GLOW PANELS TO A CLEAR POST-MOD STYLE. DISCREPANCIES WERE SIGNED OFF AND AIRCRAFT RELEASED FOR SE RVICE. 2 H 7 2 4T RT A13NM 2008022500034 20080225 00034 NM 2008 2 25 2008UALA00671 1 20080205 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 333UA 24228 ROW 9 TO 15 EMERGENCY LIGHT STRIP ON FLOOR INOP. COULD NOT DUPLICATE FAULT. OPS CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500042 20080225 00042 NM 2008 2 25 2008UALA00676 1 20080205 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 659UA 27114 EMERGENCY EEL LIGHT INOPERATIVE AT SEAT 5AB. SECURED CONNECTOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500043 20080225 00043 NM 2008 2 25 2008UALA00677 1 20080205 A 3350 LENS BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN CRACKED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 665UA 29237 SEVERAL LOWER EMERGENCY EXIT LIGHT IDENTIFIER LENSES ARE CRACKED OR EXCESSIVELY DIRTY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500044 20080225 00044 NM 2008 2 25 2008UALA00678 1 20080205 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 665UA 29237 WITH FLIGHT DECK EMERGENCY LIGHT SWITCH IN ARM, INTERIOR EMERGENCY EXIT LIGHTS TURN ON. AFTER FURTHER TROUBLESHOOTING F OUND EMERGENCY C/B TO BE COLLARED. RESET C/B`S AND CHECKED GOOD IAW MM 33-51-00. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022100072 20080221 00072 WP 2008 2 21 08FDEA00457 1 20080215 A 5321 AEA7317501 FLOOR PANEL DOUG DC10 DC1030F 3023504 WP ZONE 200 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MAIN CABIN FLOOR PNL AT STA 1481 TO 1561, LBL 40 FWD CORNER DELAMINATED. FABRICATED NEW FLOOR PANEL STA 1481 TO 1561, P OTTED EDGES, COMPLETED CURE AND SANDED EDGE POTTING. INSTALLED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX SRZ 25-005 REV F. 2 L 7 3 4F RT A22WE 2008022100085 20080221 00085 WP 2008 2 21 08FDEA00499 1 20080218 A 5321 ACA3205547 FLOORBOARD DOUG DC10 DC1030F 3023504 WP BS 495-615 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 MAIN CABIN FLOORBOARD AT APPROX BL-0 BETWEEN STA 495 TO 615 IN DELAMINATED. FABRICATED NEW FLOOR BOARD PANEL STA 495 TO 615, POTTED EDGES, COMPLETED CURE AND SANDED EDGE POTTING. INSTALLED INSERTS, APPLIED NON-SKID AND PART MARKED IAW SRZ 25-005 REV F. INSTALLED FLOORBOARD IAW SRM 51-31-01, VOL II. 2 L 7 3 4F RT A22WE 2008022100089 20080221 00089 WP 2008 2 21 08FDEA00447 1 20080214 A 5320 NWJ600619 STRAP DOUG DC10 DC1030F 3023504 WP ZONE 100 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 AFT PIT, AFT BULKHEAD STRAP 187 CA (NWJ 6006-19)(MARKED AS B2/C2) IS DAMAGED, BENT, HAS ELONGATED FASTENER HOLES AND IS CORRODED. FORMED HAT SECTION PER DAC DWG NWJ 6006 REV C AND FEDEX GMM 7-0-1001 PG 2. FABBED HAT SECTION PER FEDEX GMM 7-0-1001 AND DAC DWG NWJ 6006 REV B. ALODINED PER DC-10 SRM 51-21-01 PARA 31,VOL II. PRIMED PER DC-10 SRM 51-21-01 PAR A 24,VOL II. PAINTED PER DC-10 SRM 51-21-20 VOL II. PART MARKED PER FEDEX GMM 7-0-1001. 2 L 7 3 4F RT A22WE 2008022100090 20080221 00090 NM 2008 2 21 08FDEA00413 1 20080213 A 5347 BAC1520792 SEAT TRACK BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 MAIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION IN SEVERAL PLACES FROM STA 360 TO STA 380, LBL 48. REMOVED CORROSION I AW SRM 51-10-6 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-2 FIG 7 AND 53-10-1 FIG3 SRM PAG23. REMOVED SEAT TRACK SECT ION IAW 51-30-2. FABRICATED NEW SEAT TRACK IAW SRM ER 01-049, 53-10-2 FIG 7A REV D, 51-30-5, 51-10-1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 2008022100112 20080221 00112 EU 2008 2 21 08FDEA00506 1 20080218 A 5321 B5327080600000 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 MAIN CABIN FLOOR PNL 232 YG IS CRUSHED. FABRICATED NEW FLOOR BOARD PNL NR 232 YG IAW FEDEX DWG SRZ 25-005 REV F. FOR I NSTALLATION SEE W/C 62C0701. 2 L 7 2 4F RT A35EU 2008022100119 20080221 00119 NM 2008 2 21 HALA0800128 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 743 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 43, SEAT TRACKS AT RBL 88.5, STA 743. CORROSION BLENDED OUT WITHIN SRM LIMITS, SRM 51-10-02. 2 L 7 2 4F RT A1NM 2008022100127 20080221 00127 NM 2008 2 21 08FDEA00513 1 20080219 A 5322 6515937 SHEAR TIE BOEING 727 727227 1384078 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 MAIN CARGO BAY BS 680 FRAME SHEAR TIE HAS HAS TOOLING DAMAGE IN THE RADIUS BETWEEN STR S 14L AND S 15L, GENERATED BY 5 30045 CHECK DAMAGE LIMITS, ORIG MAT'L .045", MAT'L LOSS .007' WITH .038 REMAINING. DAMAGE IS OUT OF LIMITS REF SRM 53-1 0-2 PG 12A FIG 3. CUT OUT DAMAGE AREA REF, REF 53-10-04 PG 43. FABRICATED REPAIR ANGLE REF SRM 53-10-7 PG 44, HEATED T REATED ANGLE, TREATED AND PRIMED ANGLE, REF SRM 51-10-2 PG 7. INSTALLED ANGLE REF 51-30-2 PG 2. 2 L 7 3 4F A3WE 2008022200093 20080222 00093 NM 2008 2 22 HALA0800212 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 982 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT LBL 88.5 STA 982, MAX DEPTH BLENDED WAS 0.025". BLENDED IAW SRM 51-10-02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200112 20080222 00112 NM 2008 2 22 HALA0800250 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON SEAT TRACK CROWN/BASE AT LBL 88.5, STA 197+126, AREA HAS BEEN REWORKED BEFORE. SEAT TRACK WAS REPL ACED PER SRM. 2 L 7 2 4F RT A1NM 2008022200134 20080222 00134 NM 2008 2 22 2008UALA00738 1 20080208 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 887 STR 20R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FUSELAGE STRINGER CLIP IS CRACKED, BS 887 STR 20R. MAJOR REPAIR: REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200152 20080222 00152 WP 2008 2 22 AALA200800271 1 20080208 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 410AA 49321 DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 3 TO 6 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 3 TO 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022500047 20080225 00047 NM 2008 2 25 2008UALA00766 1 20080209 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 R-1 DOOR LOWER GATE CORRODED AND DAMAGED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED: REPLACED DOOR 1R GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500050 20080225 00050 NM 2008 2 25 2008UALA00772 1 20080209 A 2421 FILTER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE IDG UNKNOWN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 781UA 26945 FOUND RIGHT HAND ENG IDG FILTER BYPASS D, P, I POPPED OUT. REPLACED IDG PER MM 24-11-01. OPS. CHECK NORMALLY. SUSPECT IDG BEARING & SEAL DETERIORATION. COMPLETED VERIFICATION FLT & RT ENGINE IDG CHECKD GOOD FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008022500053 20080225 00053 NM 2008 2 25 2008UALA00775 1 20080208 A 3397 582233 CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 665UA 29237 EXTERIOR LIGHTS, OVERWING EMERGENCY SLIDE AND DOOR LIGHTS ARE INOP (LEFT SIDE). RESEATED CONNECTOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500117 20080225 00117 NM 2008 2 25 2008UALA00284 1 20080113 A 2421 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 598UA 28751 RIGHT GEN DRIVE LIGHT IS OUT WITH ENGINE SHUTDOWN. POSSIBLY A LOW OIL CONDITION (OVERHEAT). SERVICED IDG AND ACCOMPLIS HED TEST RUN OF RIGHT IDG, NO LEAKS NOTED AND IDG WAS INDICATING NORMAL. NO REPEATS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500120 20080225 00120 NM 2008 2 25 2008UALA00679 1 20080207 A 3350 BR964422 LENS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN MISSING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 807UA 798 EEL RED LENS MISSING AT FORWARD CLOSET. REPLACED EEL LENS COVER. 2 L 7 2 4F 4 F RT A28NM E40NE 2008022500134 20080225 00134 EU 2008 2 25 2008UALA00696 1 20080206 A 3520 21214001 ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE PAX O2 WEAK A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 406UA 454 OXYGEN MASK 6ABC FELL OUT. WEAK ACTUATOR. REPLACED DOOR ACTUATOR AND TESTED O2 SYSTEM, SYSTEM OPS CHECKS NORMAL AND DO OR REMAINS IN PLACE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008022500146 20080225 00146 NM 2008 2 25 2008UALA00709 1 20080206 A 2530 3510003201 COFFEEMAKER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE AFT GALLEY FAULTY A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 839UA 1507 ELECTRICAL SMELL EMANATING FROM THE AFT GALLEY. UNKNOWN (POSSIBLE SHORT WITHIN COFFEE MAKER). REPLACED COFFEEMAKER AND OPS CHECKED OK, NO SMELL, NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008022500163 20080225 00163 NM 2008 2 25 2008UALA00764 1 20080208 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 L-2 DOOR UPPER HINGE ARM CUTOUT REQUIRES DOUBLER INSTALLATION. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500166 20080225 00166 NM 2008 2 25 2008UALA00767 1 20080208 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 550UA 25398 LEFT LAMP INOP IN FLT DECK DOOR (LOCK FAIL) INDICATOR. BULB OUT (BURNED OUT). REPLACED BULB, OPS CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500180 20080225 00180 NM 2008 2 25 2008UALA00784 1 20080210 A 2497 WIRE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GALLEY SPARKS A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 228UA 30556 FAINT BURNING ODOR DETECTED FROM OVEN R31. NO ODOR WITH POWER OFF. INSIDE OF THE R31 OVEN WAS CLEAN. NO BURNING ODOR F ROM OVEN. ONE ELECTRICAL TERMINAL IN THE CHILLER FOOD CART DOCK (COMPARTMENT 300) WAS BROKEN LOOSE. DAMAGE CAUSED SPAR K AND BURNING ODOR. TRACED PROBLEM TO LOOSE TERMINAL BLOCK. SECURED TERMINAL BLOCK AND TESTED CART. NO FURTHER SPARK S OR ODOR. SUSPECT DAMAGE DUE TO ITEMS IMPACTING TERMINAL BOARD DURING USAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008022500202 20080225 00202 NM 2008 2 25 2008UALA00795 1 20080208 A 3350 8100133801 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 780UA 26944 EMERGENCY EXIT LIGHTS ARE INOP AT SEATS 1F, 24C, 32G AND 39C. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008022500204 20080225 00204 NM 2008 2 25 2008UALA00797 1 20080211 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FWD GALLEY DOOR LOWER DOOR, LOWER FRAME IS CRACKED UNDER AFT STOP FITTING. MAJOR REPAIR: REPLACED LOWER FRAME WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500212 20080225 00212 NM 2008 2 25 2008UALA00805 1 20080211 A 3397 784480 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 ALL SEAT EEL INOP: RIGHT SIDE A-ZONE. FOUND SHORT AT CONNECTOR IN SEAT 3J. REPAIRED CONNECTOR AND SECURED. EEL SYSTE M OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022500214 20080225 00214 NM 2008 2 25 2008UALA00807 1 20080211 A 3397 80603 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 WALL EEL INOP: LEFT SIDE AFT GALLEY. REPLACED FEEDER WIRE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022500217 20080225 00217 NM 2008 2 25 2008UALA00812 1 20080212 A 5320 STRAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 UPPER FUSELAGE HAS SCRIBELINE DAMAGE AT THE BS 907 BUTT JOINT BETWEEN STRINGERS 6R & 8R. MAJOR REPAIR ACCOMPLISHED: FA BRICATED & INSTALLED NEW BUTT SPLICE INTERNAL STRAP SECTION FROM STRINGERS 4R-10R & REINSTALLED STRINGER SPLICES. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500224 20080225 00224 NM 2008 2 25 2008UALA00821 1 20080213 A 3510 MC1019101 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 571UA 26681 CAPTAIN'S O2 MASK WILL NOT DEFLATE & MIC IS INOP. REPLACED CAPT O2 MASK, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022100192 20080221 00192 NM 2008 2 21 08FDEA00435 1 20080214 A 5753 SKIN BOEING 727 727227 1384078 NM TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 RT WING OUTBD T/E FLAP, LWR SURFACE OUTBD END, LIGHT SURFACE CORROSION REPAIRED RT OUTBOARD T/E FLAP LOWER SURFACE REF SRM 51-40-20 PAR 7, 8, 14, 15, 18, 20-22 AND APPLIED EXTERIOR PROTECTIVE PAINT FINISH REF MM 51-20-151-7, THIS IS CLASS IFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008022200012 20080222 00012 NM 2008 2 22 2008UALA00681 1 20080206 A 5340 ATTACH ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 300 S13L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FUSELAGE INTERCOSTAL ATTACH ANGLE AT BS 300 STR 13L IS CRACKED. MAJOR REPAIR: REPLACED INTERCOSTAL ATTACH ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022200020 20080222 00020 NM 2008 2 22 2008UALA00688 1 20080206 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 R-1 DOOR HANDLE BOX CRACKED AT CAM BASKET HOLES. STRESS CRACK TO HANDLE BOX. REMOVED AND REPLACED HANDLE BOX AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022200044 20080222 00044 NM 2008 2 22 HALA0800264 1 20080215 A 2150 BOOT BOEING 717 717200 1383700 NM ACM LOOSE A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 478HA 55123 WHEN ENTERING COCKPIT ON CREW CHANGE, FOUND TAIL TEMP HIGH LIGHT ON. A/C PACKS SHUTOFF. FOUND RT ACM EXHAUST DUCT BOOT LOOSE AND LEAKING. RESECURED RT PACK EXHAUST BOOT. OPS CK LEAK CK GOOD. 2 L 7 2 4F TR A6WE 2008022200061 20080222 00061 WP 2008 2 22 AALA200800235 1 20080202 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 575AM 53152 ORD INFLIGHT T1145/02FEB - NOSE GEAR UNSAFE LIGHT ILLUMINATED AFTER NOSE GEAR RETRACTION. RETURNED TO ORD AND LANDED WI THOUT INCIDENT. REPACKED NOSE STRUT ASSEMBLY AND REPLACED METERING PIN SEALS AND LOWER TURNING TUBE BEARING. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022200062 20080222 00062 WP 2008 2 22 AALA200800236 1 20080202 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 492AA 49730 ORD INFLIGHT T1545/02FEB - NOSE GEAR UNSAFE LIGHT ILLUMINATED AFTER NOSE GEAR RETRACTION. RETURNED TO ORD AND LANDED W ITHOUT INCIDENT. REPACKED NOSE STRUT ASSEMBLY AND REPLACED LOWER TURNING TUBE BEARING ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022200066 20080222 00066 EU 2008 2 22 TRBA2008023 1 20080218 A 3350 3011210 BULB AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 420AT 420 EMERGENCY LIGHT FOR ENTRANCE DOOR INOP. REPLACED EMERGENCY LIGHT ENTRANCE BULB AS PER JIC 33-50-00. 2 H 7 2 4T RT A53EU 2008022200068 20080222 00068 EU 2008 2 22 CPCP20080005 1 20080123 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 399AT 399 LT INBOARD SEAT TRACK, BETWEEN FRAME 29-35 CORRODED. LT INBOARD SEAT TRACK BETWEEN FRAME 20 TO 35. REPLACED AS PER SRM 51-25-04. 2 H 7 2 4T RT A53EU 2008022200073 20080222 00073 WP 2008 2 22 AALA200800258 1 20080207 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG LEAKING A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 400AA 49311 JFK INFLIGHT T321/07FEB LGA TO ORD - UNABLE TO RETRACT NOSE GEAR AFTER TAKEOFF. LANDED JFK WITHOUT INCIDENT. REPACKED NOSE GEAR SHOCK STRUT IN ACCORDANCE WITH SPECIAL ITEM CARD 32 92 12. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022200077 20080222 00077 WP 2008 2 22 08FDEA00519 1 20080220 A 7603 2606270001 THROTTLE CABLE DOUG DC10 DC1030F 3023504 WP GE CF6 CF66D 30020 GL NR 2 ENGINE FAILED A FDEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 25 560FE 3000 46938 451374 NR 2 THROTTLE STUCK AT HIGH POWER SETTING AT CRUISE ALTITUDE. ALL ATTEMPTS TO THAW LINKAGES WERE UNSUCCESSFUL. NR 2 EN GINE WAS SHUT DOWN ON APPROACH TO KMEM. AFTER LANDING THROTTLE OPERATED NORMALLY. REMOVED AND REPLACE NR 2 ENGINE THRO TTLE CABLE AND THROTTLE DRUM BEARING PER MM 76-11-01-2. PERFORMED RIGGING OF NR 2 THROTTLE CABLE, REF. MM 76-11-01-2. O PS CHECK GOOD. OK FOR SERVICE 2 L 7 3 4F 4 F RT A22WE E23EA 2008022200089 20080222 00089 NM 2008 2 22 HALA0800230 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 846 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45,SEAT TRACKS AT LBL 11, STA 846, MAX DEPTH OF BLEND OUT WAS 0.011". BLENDED IAW SRM 51-10-0 2. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200090 20080222 00090 NM 2008 2 22 HALA0800233 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 985 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT LBL 11, STA 985, MAX DEPTH OF BLEND OUT WAS 0.012". BLENDED IAW SRM 51-10- 02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200095 20080222 00095 NM 2008 2 22 HALA0800236 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1035 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT LBL 11, STA 1035, MAX DEPTH OF BLEND WAS 0.015". BLENDED IAW SRM 51-10-02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200104 20080222 00104 NM 2008 2 22 AALA200800246 1 20080204 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 771AN 29579 NRT - EMERGENCY LIGHT FRAME AT FIRST CLASS CLOSET DOOR IS BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FIRST CLASS CLOSET DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022200105 20080222 00105 WP 2008 2 22 AALA200800247 1 20080204 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 449AA 49475 LGA - EMERGENCY LIGHTS AT FORWARD CABIN AND LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD CABIN AND LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022200128 20080222 00128 NM 2008 2 22 2008UALA00733 1 20080210 A 5340 ATTACH ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 348 S16L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 FUSELAGE STR 16L INTERCOSTAL ATTACH ANGLE CRACKED BS 348, ALSO ATTACH CLIP AT BS 348 STR 16 INTERCOSTAL. MAJOR REPAIR: REPLACED INTERCOSTAL ATTACH ANGLE. AND CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2008022500046 20080225 00046 NM 2008 2 25 2008UALA00762 1 20080210 A 3350 AML76C10T01P003 SWITCH BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS MALFUNCTIONED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 197UA 26901 MISC EMERGENCY LIGHTING ON IN CABIN. RESET EMERGENCY SWITCH GUARD AND LIGHT OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022500121 20080225 00121 EU 2008 2 25 2008UALA00680 1 20080207 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 447UA 836 CREW O2 SHOWS LOW 1460 PSI. SERVICED CREW O2 TO FULL, NO LEAKS NOTED AT THIS TIME. 2 L 7 2 4F 4 F RT A28NM E40NE 2008022500139 20080225 00139 NM 2008 2 25 2008UALA00699 1 20080207 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 525UA 24978 EMERGENCY LIGHT AT DOOR 4 RT INOP (EXT). LIGHT BULB VIBRATED LOOSE. SECURED LIGHT BULB AND OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500144 20080225 00144 NM 2008 2 25 2008UALA00708 1 20080204 A 2612 BCREFA0526 CONTROL PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE WARNING SYS SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 544UA 25322 AFT CARGO FIRE SYS SWITCH LT DOES NOT ILLUMINATE DURING TEST. ASSOC EICAS MSG DOES DISPLAY. CARGO FIRE TEST PANEL SHOR T. REPLACED CARGO FIRE TEST PANEL. ALL OPS CHECKS ARE GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500150 20080225 00150 NM 2008 2 25 2008UALA00716 1 20080208 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW O2 LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 803UA 748 OXYGEN NEEDS TO BE SERVICED. SERVICED O2 TO FULL, NO LEAKS WERE NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008022500154 20080225 00154 2008 2 25 2008UALA00718 4 20080207 A 2350 MF20010 MICROPHONE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE OXYGEN MASK SHORTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 830UA 1243 F/O'S OXYGEN MASK MICROPHONE IS INOPERATIVE. SHORT IN MIC WIRING IN MASK (F/O). REPLACED F/O O2 MASK ASSY. ALL OPS CH ECKS WERE GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008022500165 20080225 00165 NM 2008 2 25 2008UALA00765 1 20080208 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 R-2 DOOR UPPER HINGE ARM CUTOUT REQUIRES DOUBLER. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022500196 20080225 00196 EU 2008 2 25 2008UALA00787 1 20080211 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 438UA 678 THE L2 DOOR SILL PLATE HAS CORROSION AT FR 68. MAJOR REPAIR ACCOMPLISHED AT LCQ. 2 L 7 2 4F 4 F RT A28NM E40NE 2008022500236 20080225 00236 NM 2008 2 25 2008UALA00824 1 20080213 A 5340 ATTACH ANGLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 902UA 25002 MED 1 LT INTERCOSTAL ANGLE CRACKED AT STR 13L. MAJOR REPAIR: STRINGER 13 INTERCOSTAL ANGLE REPLACED. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500255 20080225 00255 NM 2008 2 25 2008UALA00108 1 20080107 A 3810 1G390 PRESSURE SWITCH BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE POTABLE WATER FAILED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 104UA 26902 LOST POTABLE WATER SYSTEM PRESSURE. REPLACED S251 PRESSURE SWITCH AND RPL INLINE FILTER. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022500260 20080225 00260 NE 2008 2 25 2008UALA00122 2 20080106 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 MAKING METAL A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 667UA 29239 727817 NR 2 ENG MAIN OIL FILTER HAS METAL IN IT, AND OIL IS BLACK. REPLACED THE MAIN OIL FILTER PER AMM 79-21-05. ALL CHIP DE TECTORS WERE CLEAN, AND THERE WAS NO EVIDENCE OF HYDRAULIC FLUID OR FUEL CONTAMINATION. THE MAIN OIL FILTER WAS CHECKED 25 FLIGHT HOURS LATER, AND FOUND TO HAVE NO CONTAMINATION. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500267 20080225 00267 2008 2 25 2008UALA00123 4 20080104 A 3431 8220298001 RECEIVER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE ILS FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 782UA 26948 RIGHT ILS LOC SIGNAL BAD, MAT SHOWED RT ILS RECEIVER LOC SIGNAL INVALID NO OTHER FAULTS INDICATED CTR AND LT OK. SUSPEC T FAULTY ILS. REPLACED RIGHT INSTRUMENT LANDING SYSTEM RECEIVER PER MM 34-31-01. PERFORMED MAT TEST, CK'S GOOD. ACFT O K FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008022500285 20080225 00285 NM 2008 2 25 2008UALA00388 1 20080122 A 2710 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE AILERON UNKNOWN A UALA O OTHER J W WARNING INDICATION INADEQUATE Q C NR NOT REPORTED 1 WP 29 661UA 27158 AILERON LOCKOUT SLOWING THRU 250 KNOTS. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500286 20080225 00286 NM 2008 2 25 DL76L080178 1 20080209 A 3240 26124121A BRAKE BOEING 767 767332 1382001 NM MLG DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 171DN 24759 ON EPDC, FOUND 2 TIE BOLTS BROKEN ON THE NR 1 BRAKE UNIT, NR 1 MLG BRAKE ASSY REPLACED IAW MM 32-41-08. 2 L 7 2 4F RT A1NM 2008022500292 20080225 00292 NM 2008 2 25 C8GA20080007 1 20080221 A 3230 656021123 ACCESSORY UNIT BOEING 727 7272A1 138407F NM MLG MALFUNCTIONED A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 286SC 21601 FLT 706 FROM TOL TO MSP, AFTER TAKEOFF FROM TOL ,THE LANDING GEAR HANDLE WOULD NOT RAISE TO THE UP POSITION. THE AIRCRA FT RETURNED TO TOL WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE LANDING GEAR ACCESSORY UN IT WAS AT FAULT. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT AND OPERATIONALLY CHECKED GOOD. AIRCRAFT WAS RETURNE D TO SERVICE. 2 L 7 3 4F A3WE 2008022500304 20080225 00304 NM 2008 2 25 AALA200800330 1 20080129 A 5330 SKIN BOEING 767 767223 1385123 NM BS 1081-1087 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 324AA 22325 AFW - FUSELAGE SKIN AT STATION 1081 TO 1087 BETWEEN S39R AND S39L HAD CORROSION BLENDED ON INNER SURFACE BEYOND SRM LIMI TS. BLENDED CORROSION FROM PARENT THICKNESS OF 0.316 INCH WITH REMAINING THICKNESS NO LESS THAN 0.252 INCH AND 0.233 IN CH. INSPECTED BLENDED AREA TO CONFIRM COMPLETE REMOVAL OF DAMAGE PER 767 200 SRM 51 10 02 06. ACCOMPLISHED EDDY CURREN T INSPECTION TO ENSURE NO CRACKING AT BLENDED AREAS. 2 L 7 2 4F RT A1NM 2008022500305 20080225 00305 WP 2008 2 25 AALA200800322 1 20080215 A 2913 PUMP DOUG DC9 DC982 3022082 WP HYD SYSTEM FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7544A 53026 DFW INFLIGHT T1695/15FEB - NUMBER ONE ENGINE DRIVEN HYDRAULIC PUMP FAILED IN FLIGHT. RETURNED TO DFW AND LANDED WITHOU T INCIDENT. REPLACED NUMBER ONE ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022500315 20080225 00315 NE 2008 2 25 DL76G080193 2 20080212 A 7230 FAN BLADE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 ENGINE DAMAGED A DALA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 27 1605 26251 704696 30198 704696 ON T/O BIRD STRIKE LEFT ENG VIBS HIGH RETURNED FOR LNDG. NO SMELL IN CABIN ASSOC W/BIRD STRIKE NOTED. REPLACED DAMAGED FAN SETS NR 1 ENG. BOROSCOPED HPC FOUND NO BIRD STRIKE DAMAGE AFTER REMOVING BLADES VISUALLY INSPECTED CORE INTAKE FOU ND NO DEBRIS. CORE OK. PBS RUN FAILED FOR DATA LOSS. CHECKED AND RAN SECONDS AND THIRD VIBE RUN. RESET ALL WEIGHTS P ER BALANCE RUN FAN VIBS NOW 1.1 AT 98 PERCENT N1 OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E13NE 2008022500318 20080225 00318 NM 2008 2 25 DLM90080198 1 20080213 A 5530 LUG DOUG MD90 MD9030 3023690 NM GE CF6 CF680C2B6F 30025 NE VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 704696 LT INBOARD VERTICAL STABILIZER LUG CORRODED. REPAIRED LT INBOARD VERTICAL STAB LUG, IAW MD90 SRM 55-30-05. 2 L 7 2 4F 4 F RT A6WE E13NE 2008022500323 20080225 00323 NM 2008 2 25 DLM90080203 1 20080207 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM GE CF6 CF680C2B6F 30025 NE BS 731-750 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 704696 RT CUSP WEB 731-750 CORRODED AROUND FASTENERS. REPAIRED DAMAGED CUSP WEB, IAW MD90 SRM 51-30-08, ERA 398191-14MA DATE 0 9-18-02. 2 L 7 2 4F 4 F RT A6WE E13NE 2008022500324 20080225 00324 NM 2008 2 25 DLM90080204 1 20080212 A 5550 PLATE DOUG MD90 MD9030 3023690 NM STABILIZER CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 DURING HMV THE RT VERTICAL-TO-HORIZONTAL STABILIZER INBOARD AND OUTBOARD HINGE PLATES WERE FOUND WITH CORROSION IN THE B ORES. A REPAIR WAS MADE AND APPROVED VIA FAA FORM 8100-9. 2 L 7 2 4F RT A6WE 2008022500325 20080225 00325 NM 2008 2 25 DL757080205 1 20080214 A 3350 767 BULB BOEING 757 757232 1384965 NM EXTERIOR INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 638DL 23761 DURING A SVC CK AD 5 FOUND EXTERIOR EMERGENCY LIGHTS INOP AT R-2 DOOR - 4L DOOR - 4R DOOR, AND LT FUSELAGE BEHIND WING A REA INOP. RELAMPED 2 L 7 2 4F RT A2NM 2008022500327 20080225 00327 EU 2008 2 25 USAA920080399 1 20080209 A 3350 CONTROL PANEL AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHTS MALFUNCTIONED A USAA K NONE O OTHER UK UNKNOWN 1 EA 19 656AW 1079 FLT 291 - SEA-LAS - EEL - EMERGENCY EXIT LIGHTS COME ON WHEN EMERGENCY EXIT LIGHTS ARE TURNED OFF. MAINTENANCE REPLACED LIGHTING CONTROL PANEL 25VU. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008022500329 20080225 00329 EA 2008 2 25 FDKA200802052 1 20080206 A 4920 APU CNDAIR CL600 CL6002D24 1390016 EA CONTAMINATED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 601LR 15145 FDM 6017 ORD-CVG (1226 PHX LCL). RETURNED TO GATE DUE TO SMOKE IN CABIN AND FLIGHT DECK. PILOT REPORTS THAT DE-ICE WAS STARTED WITHOUT HIS KNOWLEDGE AND WAS NOT ABLE TO SHUT APU OR PACKS OFF IN TIME TO PREVENT INGESTION. MX PERFORMED OP CHECKS OF PACK SYSTEM, NO SMOKE NOTED. SYSTEM OP NORMAL. 2 L 7 2 4F RT A21EA 2008022500336 20080225 00336 NM 2008 2 25 BB08016 1 20080210 A 3397 WIRE HARNESS BOEING 757 757225 1384959 NM CABIN DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 915AW 22209 PHX ROW 16 LEFT EMERGENCY LIGHT INOP. MAINTENANCE REMOVED & REPLACED SEAT EMERGENCY LIGHT HARNESS. 2 L 7 2 4F RT A2NM 2008022500338 20080225 00338 NM 2008 2 25 USAA920080404 1 20080211 A 5330 6518420 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FUSELAGE SKIN, BS 312, S10L - S11L. REPAIRED FUSELAGE SKIN, BS 312, S10L - S11 L CRACKED FUSELAGE SKIN, BS 312, S10L - S11L. 2 L 7 2 4F RT A16WE 2008022500339 20080225 00339 NM 2008 2 25 USAA920080405 1 20080211 A 5531 65474585 RIB BOEING 737 7373S3 1384711 NM VERTICAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - VERTICAL STABILIZER LEADING EDGE RIB IS CRACKED, STABILIZER STATION 86.12. REPAIRED VE RTICAL STABILIZER LEADING EDGE RIB, STABILIZER STATION 86.12 IAW USAIRWAYS EA 100232. 2 L 7 2 4F RT A16WE 2008022500341 20080225 00341 NM 2008 2 25 USAA920080407 1 20080202 A 5754 65C26602218 WEDGE BOEING 737 7373S3 1384711 NM L/E SLAT DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - RIGHT WING NR 5 SLAT TRAILING EDGE WEDGE HAS AREA OF DISBOND, SS 126.9. REPAIRED RIGHT WING NR 5 SLAT TRAILING EDGE WEDGE, SS 124.90 - SS 128.40 IAW B737 SRM 51-70-10-2R. 2 L 7 2 4F RT A16WE 2008022200087 20080222 00087 NM 2008 2 22 2008UALA00711 1 20080207 A 2150 21FA319 FILTER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EQUIP COOLING CLOGGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 223UA 30224 EQUIP COOLING EQUIPMENT COOLING FUNCTION IS INOPERATIVE (LOW FLOW), OR COOLING SUPPLY AIR TEMPERATURE IS EXCESSIVE ON TH E GROUND, OR BOTH EQUIPMENT COOLING OVERRIDE VALVE ACTUATORS (NR 1 AND NR 2) HAVE FAILED BITE TEST OR HAVE FAILED TO REA CH COMMANDED POSITION. INLET FILTER. REPLACED EQUIPMENT COOLING INLET FILTER. REF MM21-27-02, ACP GND PASSED. ACFT OK F OR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008022200094 20080222 00094 NM 2008 2 22 HALA0800222 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 965 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT LBL 54.75, STA 965, MAX DEPTH OF BLEND OUT WAS 0.007". BLENDED IAW SRM 51- 10-02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022200140 20080222 00140 2008 2 22 2008UALA00744 4 20080211 A 2565 BOTTLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L2 DOOR SLIDE READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 DOOR SLIDE PRESSURE OUT OF LIMITS AT 2L. REPLACED DOOR 2L SLIDE ASSEMBLY . SUSPECT LEAKING PRESS BOTTLE. A/C OK FOR S ERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022200144 20080222 00144 EU 2008 2 22 TRBA2008019 1 20080213 A 2497 E0261CF202224 WIRE AEROSP ATR72 ATR72212 8680945 EU COCKPIT BURNED A TRBA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 29 417AT 417 EMERGENCY BATTERY FAULT IN FLIGHT AND ELECTRICAL BURNED ODOR IN COCKPIT. AFTER A RESET IT CAME BACK ON. ALSO A FAULT ON THE AVIONICS VENT CAME ON SHORTLY AFTER. REPAIRED VARIOUS WIRES OF THE EMERGENCY BATTERY CHARGE SYSTEM IAW JIC 20-27- 17 AND PERFORMED OPT CK IAW JIC 24-31-85. PERFORMED OPT CK OF AVIONICS VENT VALVE IAW JIC 21-23-00. 2 H 7 2 4T RT A53EU 2008022200147 20080222 00147 EU 2008 2 22 CPCP20080008 1 20080124 A 5320 FITTING AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 399AT 399 LT BETWEEN FRAME 36 TO 39 FORWARD THRESHOLD FITTING CORRODED. CORROSION REMOVED ON LT FORWARD THRESHOLD FITTING AS PER SRM 51-21-42. FITTING FOUND OUT OF LIMITS 51-10-10 LT THRESHOLD FITTING FABRICATED AS PER SRM 53-67-70. FIG.128 AND INS TALLED IAW SRM 51-25-17. 2 H 7 2 4T RT A53EU 2008022500055 20080225 00055 NM 2008 2 25 2008UALA00777 1 20080208 A 3350 1317 LAMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 665UA 29237 EMERGENCY AISLE LIGHT ABOVE SEAT 12HJ IS DIM. REMOVED AND REPLACED LAMP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500197 20080225 00197 2008 2 25 2008UALA00789 4 20080211 A 2565 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU R2 DOOR DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 918UA 25385 DOOR 2R SLIDE PACK HAS CORDS EXPOSED IN AREA AROUND GIRT BAR. REINSERTED CORDS IN GIRT BAR FOLD ATTACHMENT. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500201 20080225 00201 NM 2008 2 25 2008UALA00794 1 20080212 A 2750 FLAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WING MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 337UA 24241 FLIGHT DIVERTED DUE TO A FLAP ASYMMETRY PROBLEM. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500209 20080225 00209 NM 2008 2 25 2008UALA00802 1 20080212 A 3350 1317 LAMP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 SEAT 3A AFT EEL LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022500219 20080225 00219 NM 2008 2 25 2008UALA00814 1 20080212 A 5320 ATTACH ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 INTERCOSTAL ATTACH ANGLE CRACKED STR 10R AT STA 294. MAJOR REPAIR: REMOVED AND REPLACED STRINGER 10R ATTACH ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008031300382 20080313 00382 NM 2008 3 13 SWAA081256 1 20080305 A 5754 65C26601 SLAT BOEING 737 7377H4 1384404 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 766SW 29806 DURING SCHEDULED 8Y CHECK, FOUND RT WING NR 7 L/E SLAT CRACKED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 2008031300385 20080313 00385 SO 2008 3 13 RAIA00803004 1 20080305 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN SMOKE A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CE 03 812HK 145373 FLT 5526 - ATL - CREW REPORTED SMOKE SMELL ALONG WITH VISIBLE SMOKE IN THE CABIN. MAINTENANCE INSPECTED THE AIRCRAFT'S AIR DISTRIBUTION SYSTEM AND IT'S PNEUMATIC BLEED SYSTEM. NO DEFECTS AND NO DUPLICATION OF DISCREPANCY COULD BE FOUND. 2 L 7 2 4T RT T00011AT 2008031300386 20080313 00386 SO 2008 3 13 RAIA00803005 1 20080305 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 841HK 145382 PRE FLT 7908 - IAD - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE AFFECTED LIGHT. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008031300392 20080313 00392 NM 2008 3 13 ASAA0872704 1 20080131 A 5754 114A80211 SKIN BOEING 737 737790 13844CN NM L/E SLAT CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 612AS 30162 NR 2 LEADING EDGE SLAT HAS 1, 4 INCH CRACK ADJACENT TO ACTUATOR MOUNT FASTENER. SLAT SKIN REPAIR COMPLETED. 2 L 7 2 4F RT A16WE 2008031300393 20080313 00393 2008 3 13 ASAA0852700 2 20080308 A 7261 CFM567B27 ENGINE BOEING 737 737890 1384527 NM LEFT OVERSERVICED A ASAA O OTHER W K INADEQUATE Q C FLUID LOSS IN INSP/MAINT 1 NM 02 585AS 35683 NR 1 ENGINE HAS OIL STREAK AND APPEARS TO HAVE A PUDDLE ON GROUND. OPENED COWL & INSPECTED AREA. FOUND OIL ABOVE OVERS ERVICE DRAIN. ENGINE RUN BY FLIGHT CREW, NO LEAKS NOTED. SERVICED BOTH ENGINES TO FULL. LT=4QTS RT=3.5QTS. 2 L 7 2 4F RT A16WE 2008031300398 20080313 00398 EU 2008 3 13 08FDEA00759 1 20080306 A 5210 RUB STRIP AIRBUS 310 A310203 3930313 EU R1 DOOR CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 R-1 UPPER FWD CORNER IS CHAFED. REMOVED CHAFED RUB STRIP IAW SRM 51-40-21; PARA 6. ALODINED AND PRIMED AREA SRM 51 -21-10. INSTALLED NEW RUB STRIP REF A310-200 SRM 51-40-21 PARA 6. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008031300405 20080313 00405 EU 2008 3 13 08FDEA00768 1 20080306 A 5540 A5547029500000 STRAP AIRBUS 310 A310203 3930313 EU RUDDER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RUDDER L/E PANEL NR 326 JL BRIDGING STRAP IS CORRODED UNDER THE NUTPLATES. REMOVED AND REPLACED STRAPS IAW SRM 51-40-21 PARA 5. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008031300412 20080313 00412 WP 2008 3 13 08FDEA00778 1 20080307 A 5730 PANEL DOUG MD10 MD1010F 3022112 WP RT WING PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 RT WING, INBD UPPER T/E FIXED PANEL P/N ARC0269-502 HAS A PUNCTURE ON THE LOWER SIDE. REMOVED DAMAGE FROM THE AREA; PR EPPED AREA FOR BONDING; FABRICATED REPAIR CORE PLUG & DOUBLERS; LAYED UP AND BONDED IAW SRM 51-31-01 VOL III FIG 4 & S RM 51-71-00 VOL II PG 1. SEALED, PRIMED & PAINTED IAW SRM 51-70-00; VOL II CH 17C. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008031300413 20080313 00413 NM 2008 3 13 08FDEA00783 1 20080307 A 5350 655850248 FRAME BOEING 727 727227 1384078 NM WG TO BDY PANEL CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 BODY TO WING FAIRING PANEL, NR 3218 BETWEEN PRIMARY HEAT EXCHANGER RT O/B FRAME WEB HAS CORROSION ON MATING SURFACE AT F S 825, RBL WL 138. RT O/B FRAME WEB FOUND TO HAVE 50 PERCENT MATERIAL LOSS, OUT OF LIMITS REF SRM 51-10-01. REMOVED AN D REPLACED FRAME WEB REF SRM 51-30-2, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008031300421 20080313 00421 NM 2008 3 13 QXEA200800253 1 20080227 A 5315 FLOORBEAM BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - ON THE AFT BAG BAY FLOOR, UNDER PANEL 144JZ THERE ARE TWO AREA OF CORROSION AROUND NUTPLATE HOLES. REPAIRED IAW DASH 8 Q400 SRM 51-21-00, 51-14-00, 51-42-05 AND 51-42-45, DASH 8 Q400 NDTM PART 6 51-00-01 AND NDTM PART 51-00-04. 2 H 7 2 4T RT A13NM 2008031300425 20080313 00425 NM 2008 3 13 SWAA081274 1 20080309 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2008031400003 20080314 00003 NE 2008 3 14 Q2SA740007 2 20080303 A 7261 9176M20G01 TUBE BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE ENGINE OIL CRACKED A Q2SA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 63 740SA 21380 517139 INFLIGHT ENGINE SHUTDOWN OF NR 2 ENGINE DUE TO LOSS OF ENGINE OIL QUANTITY AND PRESSURE DURING THE CLIMB-OUT OF RKSI. F OLLOWED QRH PROCEDURES BY SHUTTING ENGINE DOWN. MAINTAINED A POSITIVE OIL PRESSURE AND OIL QUANTITY INFLIGHT. IN ADDIT ION TO WINDMILLING AFTER ENGINE WAS SHUTDOWN. DUMPED APPROXIMATELY 200,000 LBS OF FUEL AND AIR TURN BACK TO RKSI. FOUN D OIL TUBE CRACKED AND LEAKING BETWEEN OIL PUMP AND TRANSFER GEAR BOX. REPLACED TUBE ASSEMBLY IN ACCORDANCE WITH AMM 79 -21-02. SERVICED ENGINE OIL AND RAN ENGINE. LEAK CHECK GOOD. 2 L 7 4 4F 4 F RT A20WE E23EA 2008031400009 20080314 00009 NM 2008 3 14 USAA920080560 1 20080305 A 5412 311N50335 FITTING BOEING 757 7572S7 1384962 NM ZONE 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 901AW 23321 MCN - MAJOR REPAIR - C12 CHECK - LT PYLON MID BULKHEAD FITTING CRACKED, PYLON STATION 174. REPLACED LEFT PYLON MID BULK HEAD FITTING, PYLON STATION 174 I/A/W USAIRWAYS EA 100260. 2 L 7 2 4F RT A2NM 2008031400012 20080314 00012 NM 2008 3 14 QXEA200800258 1 20080227 A 5280 BUSHING BOMBDR DHC8 DHC8402 1390042 NM MLG DOOR MIGRATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - LEFT NACELLE, FORWARD INBOARD DOOR, AFT HINGE, FORWARD BUSHING HAS MIGRATED OUT OF NACELLE HINGE FITTING. RE MOVED ATTACH HINGE AND INSTALLED NEW HINGE IAW DASH 8 Q400 SRM 51-42-05, 51-40-15, 51-42-15, 51-42-45. 2 H 7 2 4T RT A13NM 2008031400018 20080314 00018 NM 2008 3 14 2008UALA01114 1 20080301 A 2611 350F51000 CIRCUIT CARD AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FIRE CONTROL FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 808UA 804 RTFL WITH AN ENGINE FIRE WARNING INDICATION. INTERFACE CIRCUIT BOARD FAILED (5LP). AFTER TROUBLESHOOTING, REPLACED THE 5LP INTERFACE BOARD AND ALSO FOUND LOOSE CONNECTION AT FIREX BOTTLE. REPLACED FIREX BOTTLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031400020 20080314 00020 NE 2008 3 14 2008UALA01116 2 20080303 A 7200 144171000031600U TRANSDUCER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 ENGINE FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 801UA 686 V11158 DIVERTED DUE TO LEFT ENGINE VIBRATION. REPLACED EVM (TRANSDUCER). ENGINE RUNS WERE NORMAL AFTERWARD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031400021 20080314 00021 EU 2008 3 14 2008UALA01121 1 20080301 A 3211 BRACKET AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MLG SENSOR BINDING A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 438UA 678 ON TAKEOFF GOT L/G GEAR NOT UPLOCKED AND CYCLED GEAR HANDLE. GEAR RETRACT 2ND TIME. FOUND 25GA SENSOR TARGET BRACKET A SSY BINDING, CAUSING TARGET TO NOT COME INTO ALIGNMENT WITH SENSOR. FOUND TARGET BRACKET SWIVEL BUSHING AND 9366BOLT BI NDING. REMOVED BOLT, CLEANED AND DRESSED BUSHING AND BOLT FOR BOTH 24GA AND 25GA. LUBED AND INSTALLED. FREEDOM OF M OVEMENT NOW MAKES SENSORS COME INTO ALIGNMENT AND GAP GOOD WITH NLG STRUT EXTENDED. ACCOMPLISHED COMPLETE LANDING GEAR RETRACTION AND EXTENSION TEST. LGCIU1 AND LGCIU2 BITE TEST NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031400025 20080314 00025 NM 2008 3 14 2008UALA01138 1 20080229 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1440 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 AFT PIT FRAME DENTED STA 1440 AT STR 25L. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031400029 20080314 00029 NM 2008 3 14 2008UALA01187 1 20080303 A 5322 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1300 S20-21L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 AFT CARGO PIT SHEAR TIE AT STA 1300 BETWEEN STR 20L AND 21L CRACKED. MAJOR REPAIR ACCOMPLISHED AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031400035 20080314 00035 NM 2008 3 14 2008UALA01202 1 20080304 A 3040 ELEMENT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE WINDOW HEAT ARCED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 304UA 23665 CPT L SIDE WINDOW HEATING ELEMENT NEAR CPT FWD WINDOW IS ARCING JUST AFTER T/O. REPLACED LEFT NR 2 SLIDING WINDOW PER M M 56-12-11. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031400037 20080314 00037 NM 2008 3 14 2008UALA01212 1 20080304 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE SEAT 21A OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 670UA 29240 FOUND EXIT LIGHT IS HANGING LOOSE OVER SEAT 21A. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031400046 20080314 00046 NM 2008 3 14 CALA0800199 1 20080306 A 5311 65033511 FRAME BOEING 737 737524 1384721 NM BS 440 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 FRAME CRACKED STA 440 BETWEEN S8R AND S9R. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A. 2 L 7 2 4F RT A16WE 2008031400047 20080314 00047 NM 2008 3 14 CALA0800200 1 20080306 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM BS 747 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 FRAME CRACKED STA 747 ABOVE S9R. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A. 2 L 7 2 4F RT A16WE 2008031400048 20080314 00048 NM 2008 3 14 CALA0800201 1 20080306 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 787 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 FRAME CRACKED STA 787 ABOVE S9R. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A. 2 L 7 2 4F RT A16WE 2008031400056 20080314 00056 NM 2008 3 14 CALA0800209 1 20080303 A 5315 141T5146 STIFFENER BOEING 767 767424ER 1385270 NM FLOORBEAM CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59053 29448 FX FLOORBEAM STIFFENER FOUND CRACKED AT BS 246 LBL 40 FWD SIDE. FX FLOORBEAM BS 246 LBL 40 FWD SIDE STIFFENER REPAIRED AS PER ECRA5310-04723 AND HFEC , NO CRACK FOUND. 2 L 7 2 4F RT A1NM 2008031400057 20080314 00057 CE 2008 3 14 QXEA200800265 1 20080307 A 5210 85217079101 SHAFT CESSNA 402 402CESSNA 207590K CE PAX DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 4009Q 4020109 SEA - FLIGHT ATTENDANT REPORTS MAIN CABIN DOOR DIFFICULT TO CLOSE. SEA MAINTENANCE INSPECTED AND FOUND HOLE ON SHAFT OB LONG. REMOVED AND REPLACED SHAFT FOR HANDRAIL MECHANISM ASSEMBLY ON FORWARD SIDE OF MAIN CABIN DOOR. DOOR OPS CHECKS G OOD. AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3O A7CE 2008031400060 20080314 00060 NM 2008 3 14 QXEA200800252 1 20080227 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 406 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - LEFT INBOARD SEAT TRACK NR 7 HAS CORROSION ON THE INBOARD FLANGE OF TRACK AT STATION X406. REPAIRED IAW DASH 8 Q400 RD8/4-53-884 AND NDTM PART 6 51-00-01. 2 H 7 2 4T RT A13NM 2008031400065 20080314 00065 NM 2008 3 14 AALA200800442 1 20080228 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 775AN 29584 DFW - EMERGENCY LIGHT AT SEAT 32G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031400073 20080314 00073 NM 2008 3 14 AALA200800452 1 20080229 A 3350 SHROUD BOEING 767 767223 1385123 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 336AA 22334 LAX - EMERGENCY LIGHT AT SEAT 27B HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 27B. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008031400075 20080314 00075 NM 2008 3 14 AALA200800454 1 20080229 A 3350 0201804001 LENS BOEING 767 767223 1385123 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 336AA 22334 LAX - EMERGENCY LIGHT AT SEAT 27B HAS LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 27B. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008031400077 20080314 00077 NM 2008 3 14 AALA200800447 1 20080228 A 3350 HOUSING BOEING 777 777223 1385213 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 775AN 29584 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR GALLEY AREA DAMAGED. REPLACED HOUSING FOR EMERGENCY LIGHT AT RIGHT NUMBE R ONE DOOR GALLEY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031300122 20080313 00122 EU 2008 3 13 08FDEA00711 1 20080305 A 5753 A5796507100200 FAIRING AIRBUS 310 A310203 3930313 EU LT WING TE FLAP ERODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LEFT WING FLAP FAIRING 533CB L/E IS ERODED BY THE TEFLON SEAL. REPAIRED LEFT WING FLAP FAIRING L/E BY REMOVING THE TEFL ON SEAL TO AND REMOVED THE DAMAGE. CLEANED & PREPPED FOR A WET LAY UP. APPLIED, CURED & SANDED THE WET LAY UP. CLEANE D & PREPPED FOR REFINISH. APPLIED REFINISH & REINSTALLED SEAL IAW SRM 57-20-35, SRM 51-40-13, SRM 51-40-00, SRM 51-23-1 0 & 51-40-10. 2 L 7 2 4F RT A35EU 2008031300146 20080313 00146 EU 2008 3 13 08FDEA00737 1 20080305 A 5315 A5361073220600 FLOORBEAM AIRBUS 310 A310324 3930206 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 THE FLOORBEAM IS CORRODED AT THE CONNECTION TO FRAME 14 RT SIDE, Y - 1958. REMOVED DAMAGED SECTION OF THE FLOORBEAM IAW SRM 53-12-15. REMOVED FLOORBEAM END CONNECTORS, ATTACH ANGLES AND THE DUCT ATTACH BRACKET IAW SRM 53-12-15. RECEIVED MACHINED SECTION OF FLOORBEAM & NR 1 SPLICE ANGLES. FABRICATED DOUBLER, DOUBLER, SHIM & FILLER IAW SRM 53-12-15 FIG 203 . ALODINED IAW SRM 51-21-10. PRIMED & APPLIED GRAY TOP COAT IAW SRM 51-23-10. INSTALLED NEW FLOORBEAM SECTION, ATTACH ANGLES, DUCT ATTACH BRACKET AND & REPAIR PARTS IAW SRM 53-12-15 FIG 203. 2 L 7 2 4F RT A35EU 2008031300149 20080313 00149 NM 2008 3 13 08FDEA00740 1 20080306 A 5313 ADA84131 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 CRACK FOUND DURING X-RAY INSPECTION AT STATION 6-0, LONGERON NR 6R STRINGER SPLICE. CRACK LENGTH APPROXIMATELY 1 INCH. CRACKED SPLICE AT STATION 6-0 LONGERON 6R REMOVED AS PER SRM 51-31-01, VOL 2. NEW SPLICE FABRICATED AS PER DRAWING AD A 8413 AND INSTALLED AS PER SRM 51-31- 01,VOL.2. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008031300160 20080313 00160 EU 2008 3 13 08FDEA00751 1 20080306 A 5414 2110081512 FAIRING AIRBUS 310 A310203 3930313 EU NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 PYLON SKIN ABOVE THE INBD T/R IS CRACKED AT APPROX STA 704 RIB 7. CLEANED AREA & REMOVED SCRATCHES IAW SRM 51-73-1 0 PG 203. NO CRACKS NOTED. REPLACED SEAL SECTION IAW SRM 51-40-21. ORIGINAL MATERIAL THICKNESS 0.024. MATERIAL REMAINING 0.021. WITHIN LIMITS IAW SRM 54-50-00. 2 L 7 2 4F RT A35EU 2008031300191 20080313 00191 NM 2008 3 13 SWAA081157 1 20080302 A 5754 65C26602 SLAT BOEING 737 7375H4 138449D NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED AT OUTBOARD T/E. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008031300216 20080313 00216 NM 2008 3 13 SWAA081215 1 20080303 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 790SW 30604 DURING SCHEDULED HC2 CHECK, LT OVERWING EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008031300217 20080313 00217 NM 2008 3 13 SWAA081150 1 20080228 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 EEPLS LENS CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008031300297 20080313 00297 NM 2008 3 13 DLM88080310 1 20080220 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 833 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 961DL 49980 EXCESSIVE EXFOLIATION CORROSION ON LT CUSP WEB AT STA 833. REPAIRED PER ERA 398191-14MA ON N/R T0083662 AT HMV-3 AT GDL . 2 L 7 2 4F RT A6WE 2008031300321 20080313 00321 NM 2008 3 13 UPS08551761 1 20080305 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM BS 1075 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 456UP 25477 INSPECTION TYPE:C-2 CORROSION ON SEAT TRACK AT NUTPLATE BS 1075, RBL 24, WL 208. REPAIRED SEAT TRACK IAW ATS EO NR 08-1 354 AND UPS EO NR B757-5310-28743-A. 2 L 7 2 4F RT A2NM 2008031300322 20080313 00322 NM 2008 3 13 UPS08551762 1 20080305 A 5730 SKIN BOEING 757 75724APF 1384969 NM LT WING CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 456UP 25477 INSPECTION TYPE:C-2 LW LWR SKIN T/E CHAFED IB AND OB OF NR 1 FLAP TRACK. REPAIRED LT WING LWR SKIN IAW ATS ER 08-1340. 2 L 7 2 4F RT A2NM 2008031300406 20080313 00406 EU 2008 3 13 08FDEA00771 1 20080306 A 5540 STRAP AIRBUS 310 A310203 3930313 EU RUDDER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RUDDER L/E PANEL NR 326 CL BRIDGING STRAPS ARE CORRODED UNDER THE NUT PLATES. 2 L 7 2 4F RT A35EU 2008031400010 20080314 00010 NM 2008 3 14 USAA920080561 1 20080301 A 5240 SKIN BOEING 737 737401 1384701 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 CLT - MAJOR REPAIR - C1 CHECK - FORWARD SERVICE DOOR OUTER SKIN CRACKED, FORWARD LOWER CORNER. REPAIRED FORWARD SERVICE DOOR OUTER SKIN, FORWARD LOWER CORNER IAW B737 SRM 52-10-01. 2 L 7 2 4F RT A16WE 2008031400036 20080314 00036 NM 2008 3 14 2008UALA01210 1 20080304 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 196UA 28715 FOUND SEVERAL SEAT EEL LIGHTS LOOSE FIRST CLASS SECTION. RESECURED ALL LOOSE CONNECTIONS. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031400038 20080314 00038 2008 3 14 2008UALA01214 4 20080304 A 2565 1A25092 O-RING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SLIDE BOTTLE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 117UA 28810 LOW BOTTLE PRESSURE. O-RING LEAKING UNDER ACTUATOR ASSEMBLY. REPLACED O-RING. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031400054 20080314 00054 NM 2008 3 14 CALA0800207 1 20080306 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 787 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 FRAME CRACKED STA 787 ABOVE S9L. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A. 2 L 7 2 4F RT A16WE 2008031400074 20080314 00074 NM 2008 3 14 AALA200800453 1 20080229 A 3350 LAMP BOEING 767 767223 1385123 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 336AA 22334 LAX - EMERGENCY LIGHT AT SEAT 27B HAS LAMP MISSING. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 27B. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008031400083 20080314 00083 NM 2008 3 14 AALA200800445 1 20080228 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 775AN 29584 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031400088 20080314 00088 NM 2008 3 14 F3LA200800080 1 20080229 A 5320 D5347112420100 SUPPORT ANGLE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED THE RIGHT SHEAR PLATE SUPPORT ANGLE, LOCATED BETWEEN FRAMES 69 AND 70, SHOWED SIGNS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE SHEAR PLATE SUPPORT ANGLE, LOCATED BETWEEN FRAMES 69 AND 70, I N ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPHS 6, 7 AND 14. FOLLOWING COMPLETION OF THE INSTALLATI ON, THE SUPPORT ANGLE WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008031400091 20080314 00091 NM 2008 3 14 TSAA0827013 1 20080306 A 2751 2061141 INDICATOR BOEING 737 737236 1384476 NM TE FLAPS FAILED A TSAA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 WP 13 843AL 23172 FLIGHT 209 KOA-OGG - ON APPROACH, THE CREW SELECTED FLAPS 5 AND THE FLAP INDICATOR SHOWED FLAPS 2. THE CREW EXECUTED A MISSED APPROACH AND COMPLIED WITH THE EMERGENCY CHECKLIST. THE CREW RETURNED TO KOA WITHOUT FURTHER INCIDENT. MAINTENA NCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR PER AMM 27-58-41 WITH ALL OPERATIONAL CHECKS SATISFACTORY. THE AIR CRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2008031400099 20080314 00099 NM 2008 3 14 2008UALA01232 1 20080306 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 291.5 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 INTERCOSTAL IS CRACKED AT BS 291.5 JUST BELOW STR 11R. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED CRACKED INTERCOSTA L. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031400101 20080314 00101 NM 2008 3 14 2008UALA01234 1 20080306 A 5310 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 616 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 BS 616 LT STUB FRAME CRACKED FROM LOWEST FASTENER HOLE ABOVE LOWER STUB FRAME BELOW FLOOR LINE. MAJOR REPAIR ACCOMPLISH ED: FABRICATED & INSTALLED FRAME STIFFENING ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031400102 20080314 00102 NM 2008 3 14 2008UALA01235 1 20080306 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FWD GALLEY DOOR SURROUND BS 277 STR 14R WEB IS CRACKED INBD FWD CORNER. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED W EB. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031700005 20080317 00005 NM 2008 3 17 2008UALA01241 1 20080307 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 ALL A AND B ZONE EMERGENCY LTS INOP, CEILING. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031700010 20080317 00010 NM 2008 3 17 2008UALA01244 1 20080307 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY LIGHTS INOP:CEILING DOOR1L. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031700015 20080317 00015 SO 2008 3 17 C2XA08IA073 1 20080301 A 2150 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16571 145633 IAH - FLIGHT 3102, THE CREW REPORTED A BURNING SMELL WITH PACK 2 ON THE GROUND. MAINTENANCE PLACED THE NUMBER 2 PACK ON MEL 21-51-00/2 CAT C, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. EWR MAINTENANCE OPERATIONALLY CHECKED THE N UMBER TWO PACK WITH NO DEFECTS NOTED, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE ON 03/03/08. 2 L 7 2 4T RT T00011AT 2008031700018 20080317 00018 NM 2008 3 17 2008UALA01266 1 20080307 A 2751 ACTUATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FLAPERON LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 76UA 26937 RT FLAPERON ACTUATOR LEAKING 36 DROPS A MINUTE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008031700026 20080317 00026 SO 2008 3 17 C2XA08RI029 1 20080228 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 13969 17 145141 FLIGHT 2076 CREW REPORTED BOTH LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. EWR MX REMOVED AND REPLACED REAR E MERGENCY LIGHT BATTERY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008031700029 20080317 00029 SO 2008 3 17 C2XA08CL025 1 20080304 A 4910 INLET EMB 145 EMB145LR 3260212 SO APU OBSTRUCTED A C2XA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 27 13964 145123 CLE FLIGHT 2423 - THE CREW REPORTED AN APU FIRE WARNING DURING TAXI WITH APU AUTOSHUT DOWN. THE AIRCRAFT RETURNED TO TH E GATE. MAINTENANCE INSPECTED AND REMOVED EXCESSIVE BUILD UP OF ICE AND SNOW FROM THE APU INLET. OPERATIONAL CHECKS OF APU WAS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008031700035 20080317 00035 WP 2008 3 17 UPS08851765 1 20080220 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 FLT DECK PANEL 682A HAS DOUBLE DRILLED HOLES WITH NO ED AND ALL HAT CHANNELS CHAFED. FABRICATED AND INSTALLED 1 WEB AND 6 HAT CHANNELS IAW DWG 56935 7 AND S275589. 2 L 7 4 4F RT 4A25 2008022500220 20080225 00220 NM 2008 2 25 2008UALA00815 1 20080212 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 376UA 24641 RIGHT OVERWING EEL AND ROWS 16 THRU 26 EEL INOPERATIVE. MAJOR REPAIR: FABRICATED AND INSTALLED NEW BUTT SPLICE INTERNAL STRAP SECTION FROM STRINGERS 4R-10R AND REINSTALLED STRINGER SPLICES. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500222 20080225 00222 NM 2008 2 25 2008UALA00817 1 20080213 A 7930 PRESSURE SWITCH BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 ENG OIL SYS MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 340UA 24244 FLIGHT DIVERTED UNDER AMBER ALERT DUE TO ILLUMINATION OF THE NR 1 ENGINE OIL FILTER BYPASS LIGHT. REPLACED OIL DIFFEREN TIAL PRESSURE SWITCH. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500251 20080225 00251 2008 2 25 2008UALA00068 4 20080105 A 3400 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NAVIGATION UNKNOWN A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 417UA 483 CAPT LOST PARTIAL NAV DISPLAY FROM 80 MILE RANGE TO 10 RANGE. F/O LOST PARTIAL NAV DISPLAY. RMP FAILURE. SHOP COULD F IND NO IMMEDIATE FINDINGS -CHRONIC UNIT- UNIT WAS REPROGRAMMED BUT NOT YET REINSTALLED ON ANY A/C. 2 L 7 2 4F 4 F RT A28NM E40NE 2008022500288 20080225 00288 NE 2008 2 25 2008UALA00402 2 20080123 A 7397 WIRE HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 EEC SHORTED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 177UA 24384 NR 2 "EEC GRD TEST ENG" CIRCUIT BREAKER ON PANEL P414, GRID D22 POPS WHEN NR 2 EEC TEST SWITCH IS SELECTED TO TEST ON TH E COCKPIT OVERHEAD PANEL. ENGINE REPLACED. FOUND W1 & W2 HARNESS SHORTED AND CAUSING CIRCUIT BREAKERS TO POP. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022500299 20080225 00299 NM 2008 2 25 AALA200800288 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 38G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 38G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022500306 20080225 00306 NM 2008 2 25 AALA200800323 1 20080215 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 ORD - EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022500307 20080225 00307 WP 2008 2 25 AALA200800321 1 20080215 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 207AA 49158 DFW - EMERGENCY LIGHT AT SEAT 21D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022500322 20080225 00322 NM 2008 2 25 DLM90080202 1 20080207 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM GE CF6 CF680C2B6F 30025 NE BS 674-798 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 704696 CABIN SEAT TRACK GOUGED AND CORRODED OUT OF LIMITS FS 674-798 RBL 22. REMOVED AND REPLACED DAMAGED SEAT TRACK, IAW MD90 SRM 53-40-01FIG 6 VOL I. 2 L 7 2 4F 4 F RT A6WE E13NE 2008022500330 20080225 00330 SO 2008 2 25 FDKA200802053 1 20080210 A 5210 DOOR EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FDM 5978 MCO (1436 PHX LCL). MAIN CABIN DOOR HARD TO OPEN FROM THE INSIDE. MX CLEANED AND LUBED DOOR. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008022500340 20080225 00340 NM 2008 2 25 USAA920080406 1 20080118 A 5330 6545769 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FUSELAGE SKIN, BS 390, BL 0, WL 390. REPAIRED FUSELAGE SKIN, BS 390, BL 0, WL 390 IAW USAIRWAYS EA 100191. 2 L 7 2 4F RT A16WE 2008011600034 20080116 00034 NM 2008 1 16 SWAA080228 1 20080110 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011600059 20080116 00059 NM 2008 1 16 SWAA080237 1 20080110 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 780 AND BS 790, STR 18L AND STR 17L. REPAIRED SKIN P ER SWA EA. 2 L 7 2 4F RT A16WE 2008011600064 20080116 00064 NM 2008 1 16 SWAA080242 1 20080110 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011600065 20080116 00065 NM 2008 1 16 SWAA080243 1 20080110 A 5322 6546546 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 827, STR 26L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008011600070 20080116 00070 NM 2008 1 16 SWAA080252 1 20080110 A 5553 6546872 ATTACH FITTING BOEING 737 7373G7 1384595 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND RT VERTICAL STABILIZER PRIMARY FITTING ATTACH LUGS CORRODED. REPAIRED FITTING PER SW A EA. 2 L 7 2 4F RT A16WE 2008031700039 20080317 00039 EU 2008 3 17 TRBA2008026 1 20080308 A 3350 3013047 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHTS FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 529AM 529 EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE WHEN TURNED ON WITH NO BATTERY SWITCH ACTIVATION. REPLACED EMERGENCY LIGHTS POWER SUPPLY PACK 63WL AND 62WL PER MM 33-51-21 AND FOUND WORKING PROPERLY. 2 H 7 2 4T RT A53EU 2008031700047 20080317 00047 SO 2008 3 17 C2XA08IA075 1 20080306 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13956 145078 IAH - FLIGHT 3019, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN EMERGENCY EXIT LIGHT INOP. MAINTENANCE INSPECTED TH E AIRCRAFT, RESET THE EMERGENCY LIGHTS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008031700054 20080317 00054 NM 2008 3 17 SWAA081276 1 20080309 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008031700056 20080317 00056 NM 2008 3 17 SWAA081305 1 20080306 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008031700059 20080317 00059 NM 2008 3 17 SWAA081307 1 20080306 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIPS WORN BETWEEN ROW 6 ABC AND ROW 8 ABC. REMOVED AND REPLAC ED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008031700062 20080317 00062 NM 2008 3 17 SWAA081310 1 20080306 A 3350 MS155721 LIGHT BOEING 737 7373K2 13844BA NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008031700064 20080317 00064 NM 2008 3 17 SWAA081280 1 20080307 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 460, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008031700068 20080317 00068 NM 2008 3 17 SWAA081335 1 20080310 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008031700069 20080317 00069 WP 2008 3 17 08FDEA00802 1 20080310 A 5310 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOORWAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 MCD LOWER JAMB AT SPOOL FITTING LOCATION NUMBER 7 SHOWED EVIDENCE OF CRACKS IN HOLES A, B, C, D. 2 L 7 3 4F RT A22WE 2008031700070 20080317 00070 WP 2008 3 17 08FDEA00803 1 20080310 A 5310 SUPPORT FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOORWAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 MAIN CARGO DOOR LOWER JAMB AND SUPPORT FITTING HAD CORROSION IN HOLES B, C, D AT FITTING LOCATION NR 6. 2 L 7 3 4F RT A22WE 2008031700079 20080317 00079 NM 2008 3 17 SWAA081287 1 20080309 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 457WN 33856 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008031700084 20080317 00084 EU 2008 3 17 08FDEA00812 1 20080310 A 5320 A53973637212 PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND TORSION BOX PANEL C 63-64, P44-46RH DAMAGED. REPAIR PERFORMED BY SPLICE PLATE REPAIR IAW SRM 53-17-18, FIG 206. 2 L 7 2 4F RT A35EU 2008031700086 20080317 00086 NM 2008 3 17 SWAA081292 1 20080307 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS CRACKED AT ROW 7 DEF. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008031700087 20080317 00087 NM 2008 3 17 SWAA081288 1 20080307 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 DURING SCHEDULED HC2 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008031700089 20080317 00089 EU 2008 3 17 08FDEA00814 1 20080310 A 5330 A53772018202 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND DENT AT SKIN PANEL C21-22, P 36-37 LT. REPAIR PERFORMED BY CUT OUT DAMAGED AREA AND INSTALLING AN EXTERNAL DOUBLE R IAW RAS/DABRE/7008975/2008 ISS A, APPROVED BY EA 6-5313-115243. 2 L 7 2 4F RT A35EU 2008031700106 20080317 00106 EU 2008 3 17 08FDEA00828 1 20080310 A 5730 A5735000420000 PANEL AIRBUS 310 A310203 3930313 EU RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT WING LOWER SKIN IS CRACKED IN THE TRAILING EDGE AREA AT WING STA 653, JUST INBD OF RIB 11. COMPLIED WITH EA 6-5730- 118457 REV A. 2 L 7 2 4F RT A35EU 2008031700109 20080317 00109 EU 2008 3 17 08FDEA00831 1 20080310 A 5330 A5397070320000 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT LOWER SKIN HAS CORROSION AT STR 57; FRAMES 54 THRU 54.1. REMOVED FASTENERS IAW SRM 51-40-21. REMOVED CORROSION I AW SRM 51-74-10. CHECKED LIMITS IAW SRM 53-16-12. ORIG. MAT THICKNESS IS .177 REMAINING MAT. THICKNESS .174. REMOVED .003. FOUND TO BE WITHIN LIMITS IAW SRM 53-10-12 PG. 139. ALODINED IAW SRM 51-21-10. PRIMED AND PAINTED IAW SRM 51-23- 10. INSTALLED RIVETS IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008031700110 20080317 00110 EU 2008 3 17 08FDEA00832 1 20080310 A 5313 A53970701215 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT STRINGER 45R IS CORRODED WHERE IT PASSES UNDER FRAME 54.2. REMOVED CORROSION IAW SRM 51-74-10. ORIGINAL THICKN ESS WAS 0.110. REMAINING MATERIAL 0.105. WITHIN LIMITS IAW SRM 53-10-00. ALODINED IAW SRM 51-21-10. PRIMED & PAINTED AR EA IAE SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008031700111 20080317 00111 WP 2008 3 17 08FDEA00833 1 20080310 A 5320 707576 SUPPORT FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 363FE 48263 MCD JAMB SUPPORT FITTING NR 7 HOLES A, B, C AND D ARE CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-31-01. REMOVED SEAT TRACK, ATTACH ANGLE, INTERCOSTAL AND WEB (BY CUTTING) FOR ACCESS IAW SRM 51-31-01. REINSTALLED SEAT TRACK, ATTA CH ANGLE, INTERCOSTAL IAW SRM 51-31-01. REINSTALLED AND REPAIRED WEB IAW SRM 51-33-01 AND 51-35-01. INSTALLED NEW FITT ING IAW SRM 51-31-01 AND RIGGED ON EA 8-5230-117634 WRI 52-30/5344 2 L 7 3 4F RT A22WE 2008031700119 20080317 00119 NM 2008 3 17 SWAA081299 1 20080306 A 3350 417A5701 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 EEPLS LENS CRACKED AT ROW 6 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008031700120 20080317 00120 EU 2008 3 17 08FDEA00842 1 20080310 A 5311 A53973176200 FRAME AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT FUSELAGE FRAME HAS CORROSION ON THE WEB BETWEEN STR 49L AND STR 50L, FRAME 65. REMOVED CORROSION IAW SRM 51-74- 10. CHECKED LIMITS IAW SRM 53-17-13 & FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. FORMED IAW SRM 51-26-00. REPAIR PART S HEAT TREATED. REPAIR PARTS LOCATED & DRILLED IAW SRM 51-40-44. ALODINED IAW SRM 51-21-10. PRIMED & TOPCOAT PAINT IAW SRM 51-23-10. INSTALLED IAW SRM 53-10-13 PAGE 205. MAJOR REPAIR. 2 L 7 2 4F RT A35EU 2008031700124 20080317 00124 NM 2008 3 17 SWAA081336 1 20080310 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300198 20080313 00198 NM 2008 3 13 SWAA081212 1 20080303 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300213 20080313 00213 NM 2008 3 13 SWAA081214 1 20080229 A 5320 6545819 WEB BOEING 737 7373G7 1384595 NM NLG W/W CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND NLG W/W CHORD CORRODED AT BS 247, RBL 16. REMOVED AND REPLACED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2008031300235 20080313 00235 NM 2008 3 13 SWAA081139 1 20080229 A 5523 65C2579810 FITTING BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED CV CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REPAIRED NR 1 TAB HINGE FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300262 20080313 00262 NM 2008 3 13 SWAA081222 1 20080304 A 5754 65C26601 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED HC2 CHECK, FOUND LT WING NR1 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008031300271 20080313 00271 NM 2008 3 13 SWAA081231 1 20080304 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031300275 20080313 00275 NM 2008 3 13 SWAA081230 1 20080304 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031300283 20080313 00283 2008 3 13 SWAA081239 4 20080304 A 2565 D31354433 SLIDE BOEING 737 7373A4 1384585 NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031300294 20080313 00294 NM 2008 3 13 DL76L080306 1 20080302 A 4900 APU BOEING 767 767332 1382001 NM MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 1201P 28458 NO APU AIR FROM APU AFTER PUSH BACK. APU S/W OFF AND RESTARTED ALL NOW, OPS OK AIR SYSTEM ALL OK. 2 L 7 2 4F RT A1NM 2008031300320 20080313 00320 NM 2008 3 13 ASAA0852694 1 20080305 A 2160 233A3101 CONTROLLER BOEING 737 737890 1384527 NM CABIN TEMP MALFUNCTIONED A ASAA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 02 587AS 35684 MASTER CAUTION ON RECALL. CNTL CABIN ZONE TEMP ILLUMINATED. RESET WITH MASTER CAUTION. RESET FAULT ON NR 2 ZONE TEMP CNTLR. GROUND VERIFICATION TEST PASSED. 2 L 7 2 4F RT A16WE 2008031300329 20080313 00329 NM 2008 3 13 SWAA081201 1 20080303 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011600076 20080116 00076 NM 2008 1 16 SWAA080255 1 20080109 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 237WN 34632 L1 DOOR EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008011600084 20080116 00084 NM 2008 1 16 SWAA080260 1 20080111 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2008011600085 20080116 00085 NM 2008 1 16 SWAA080261 1 20080112 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED A1 CHECK, FOUND RT AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008011600088 20080116 00088 NM 2008 1 16 SWAA080262 1 20080113 A 5751 65C25911 AILERON BOEING 737 7373H4 1384600 NM LT WING DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED 14Y CHECK, FOUND LT WING AILERON OUTBOARD T/E DISBONDED. REPAIRED AILERON PER SRM. 2 L 7 2 4F RT A16WE 2008011600089 20080116 00089 NM 2008 1 16 SWAA080263 1 20080112 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 408WN 27895 EEPLS INOP AT 2 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008011600103 20080116 00103 EU 2008 1 16 08FDEA00043 1 20080105 A 5320 A5383210420600 WEB AIRBUS 300 A300B4622 3930401 EU ZONE 200 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 718FD 365 FUS FR 52,BETWEEN SEAT TRACKS 3L AND 4L,STIFFENER WEB 12" TO 24" BELOW FLOOR IS BENT, TOP I/B EDGE. REMOVED AND REPLACE D WEB IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008011600107 20080116 00107 EU 2008 1 16 08FDEA00048 1 20080106 A 5340 ATTACH FITTING AIRBUS 310 A310222 3930315 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 ONE HALF INCH CRACK IN UPPER FLANGE RADIUS OF AFT CARGO DOOR ACTUATOR ATTACH FITTING. CRACK MARKED AND IN APPROX CENTER OF RADIUS BETWEEN FORE AND AFT EDGE OF FITTING. COMPLIED WITH EA 6-5230-113011--AFT CARGO DOOR FRAME 61A EXISTING REPAI R. 2 L 7 2 4F RT A35EU 2008011600109 20080116 00109 EU 2008 1 16 08FDEA00050 1 20080106 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 56 RT BETWEEN FRAMES 55/58 TO 60, HAS 1 EA REPAIR SECTION MEAS URING 28.7" LONG, 1 EA REPAIR SPLICE MEASURING 13.8" LONG AND 1 EA REPAIR FILLER 16.1" LONG REPAIR NOT IAW SRM REQUIREME NTS. REMOVED PREVIOUSLY INSTALLED REPAIR AND INSTALLED CORRECT STRINGER REPAIR IAW A310 SRM 53-10-14, FIG 201A. THIS I S AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008011600110 20080116 00110 NM 2008 1 16 08FDEA00051 1 20080106 A 5730 112N60091 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 RIGHT WING FUEL TANK ACCESS PANEL 641EB HAS CORROSION ON LOWER SURFACE REMOVED CORROSION ON PANEL 641EB PER SRM 57-20-01 , FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 201, DETAIL I, SECTION A-A, NOTE B. REPLACED PANEL IAW AMM 28-11-01. 2 L 7 2 4F RT A2NM 2008011600117 20080116 00117 NM 2008 1 16 C8GA20080001 1 20080103 A 3231 69678896 ROD BOEING 727 727225 1384077 NM NLG DOOR BROKEN A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 808EA 22439 FLT 1723 FROM ROC TO TOL, DURING GEAR RETRACTION AT POSITIVE CLIMB RATE CREW HEARD A LOAD "POP" FROM THE NOSE GEAR FOLLO WED BY THE ILLUMINATION OF THE RED DOOR INDICATOR LIGHT ON THE FRONT PANEL. THE AIRCRAFT RETURNED TO ROC WHERE IT LANDE D WITHOUT INCIDENT. POST FIGHT INSPECTION REVEALED THAT THE NOSE LANDING GEAR DOOR SYNCHRONIZATION ROD WAS BROKEN. REM OVED AND REPLACED NLG DOOR SYNCHRONIZING ROD, RIGGED DOOR AND PERFORMED GEAR SWING, OPERATIONAL CHECK GOOD. NO OTHER DE FECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2008011600157 20080116 00157 NM 2008 1 16 SWAA080272 1 20080110 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 438WN 29833 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 120. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600158 20080116 00158 NM 2008 1 16 SWAA080268 1 20080110 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 438WN 29833 DURING SCHEDULED HC1 CHECK, RT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008011500318 20080115 00318 GL 2008 1 15 C2XA08CL004 2 20080108 A 7532 8166011 BLEED VALVE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL NR 2 ENGINE FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 16151 12245 12245 145758 CLE FLIGHT 2034 - THE CREW REPORTED A HIGH STAGE VALVE 2 FAIL MESSAGE IN FLIGHT. THE AIRCRAFT RETURNED TO CLE AND LANDE D WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE HIGH STAGE BLEED VALVE AND SWITCH. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT TE6CH 2008011500327 20080115 00327 SO 2008 1 15 C2XA08IA017 1 20080103 A 3350 7287580507 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18557 145596 MCI - DURING MAINTENANCE INSPECTION, THE AISLE PATH LIGHT STRIP BETWEEN 8A-9A WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERTIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008011500351 20080115 00351 NM 2008 1 15 SWAA080220 1 20080109 A 5310 6546956 CREASE BEAM BOEING 737 7373TO 138447G NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 417, LBL 70. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008011600002 20080116 00002 NM 2008 1 16 SWAA080168 1 20080107 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 740, STR 22R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600003 20080116 00003 NM 2008 1 16 SWAA080173 1 20080107 A 5311 6546532 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600066 20080116 00066 NM 2008 1 16 SWAA080244 1 20080110 A 2560 P4010021 BATTERY BOEING 737 7373A4 1384585 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 676SW 23288 AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008011600067 20080116 00067 NM 2008 1 16 SWAA080254 1 20080110 A 5322 6546546 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008011600079 20080116 00079 NM 2008 1 16 SWAA080287 1 20080113 A 5311 6546595 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600112 20080116 00112 NM 2008 1 16 08FDEA00053 1 20080106 A 5713 112N60111 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 RIGHT WING FUEL TANK ACCESS PANEL 642BB HAS CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 642BB IAW SRM 57-20- 01, FOUND TO BE OUT OF LIMITS PER SRM 57-20-01, FIG 201, DETAIL I, SECTION AA, NOTE B. REPLACED ACCESS PANEL 642BB IAW AMM 28-11-01. 2 L 7 2 4F RT A2NM 2008011600153 20080116 00153 NM 2008 1 16 SWAA080179 1 20080107 A 5330 6552988 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 23L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600174 20080116 00174 2008 1 16 SWAA080269 4 20080110 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 438WN 29833 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008011600177 20080116 00177 NM 2008 1 16 SWAA080273 1 20080111 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 487WN 33854 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008011600181 20080116 00181 NM 2008 1 16 SWAA080290 1 20080113 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011600187 20080116 00187 NM 2008 1 16 SWAA080278 1 20080110 A 5610 5893543130 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 654SW 28399 FLIGHT DECK L1 WINDOW ARCING DURING FLIGHT. REMOVED AND REPLACED L1 WINDOW PER MM. 2 L 7 2 4F RT A16WE 2008011600196 20080116 00196 NM 2008 1 16 SWAA080296 1 20080114 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008011600206 20080116 00206 NM 2008 1 16 SWAA080301 1 20080114 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 405WN 27893 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008011600209 20080116 00209 NM 2008 1 16 SWAA080314 1 20080114 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM R1 DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 454WN 29851 R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK BROKEN. REMOVED AND REPLACED HOOK PER MM. 2 L 7 2 4F RT A16WE 2008011600211 20080116 00211 NM 2008 1 16 SWAA080315 1 20080114 A 5313 6551698 STRINGER SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2008011600212 20080116 00212 NM 2008 1 16 SWAA080303 1 20080114 A 3350 MS25237 LIGHT BOEING 737 7373H4 1384600 NM COCKPIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED HC1 CHECK, FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008031300338 20080313 00338 NM 2008 3 13 QXEA200800243 1 20080227 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 698-670 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - RIGHT INBOARD SEAT TRACK NR 16 HAS SEVERAL CORRODED AREAS ON UPPER TRACK SURFACE AT APPROXIMATELY STATION 698 .0 TO 670.0. REMOVED AND INSTALLED NEW SEAT TRACK IAW DASH 8 Q400 SRM 51-40-07, 51-42-00, 51-42-05, AND 51-40-15. 2 H 7 2 4T RT A13NM 2008031300370 20080313 00370 NM 2008 3 13 SWAA081247 1 20080305 A 5311 6546543 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300389 20080313 00389 2008 3 13 ASAA0852701 4 20080309 A 2211 4082499903 COMPUTER BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA O OTHER F FLT CONT AFFECTED LD LANDING 1 NM 02 558AS 35177 CAT IIIA AUTOLAND AIRCRAFT TRACKED AND TOUCHED DOWN APPROX 35' LEFT OF CENTERLINE. NO FLIGHT FAUTLS LOGGED. CURRENT ST ATUS CHECKED NORMAL. PERFORMED "LAND VERIFY" TEST PG 201. TEST PASSED. PERFORMED HGS SENSOR TEST, ALL NO DEFECTS. 2 L 7 2 4F RT A16WE 2008031300410 20080313 00410 EU 2008 3 13 08FDEA00776 1 20080307 A 5414 A5461081160000 PANEL AIRBUS 310 A310324 3930206 EU NR 1 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 PYLON NR 1 LEFT SIDE LOWER SHIRT CLOSE OUT AT RIB 9 AND JUST FWD OF RIB 8, SHIRT IS CRACKED. REMOVED RUB STRIP, COVER PLATE, SHIRT PANEL AND ATTACH ANGLE IAW FEDEX A310-300 SRM 51-40-21, PG 6. LOCATED, DRILLED AND DEBURRED CLOSE OUT PA NEL P/N A5461081160000, PO 558144.5; IAW A310-300 SRM 51-40-44. INSTALLED RUBSTRIP, COVER PLATE, SHIRT PANEL, CLOSE OU T PANEL AND ANGLE IAW A310-300 SRM 51-40-21, PG 7 AND PG 133. 2 L 7 2 4F RT A35EU 2008031300420 20080313 00420 NM 2008 3 13 QXEA200800250 1 20080227 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - POSSIBLE CORROSION ON TRACK NR 9 FROM FWD END TO 24 INCHES AFT OF FWD END ZONE 141/144. REMOVED SEAT TRACK A ND INSTALL NEW TRACK IAW DASH 8 Q400 SRM 51-42-05 AND 51-40-15. 2 H 7 2 4T RT A13NM 2008031300424 20080313 00424 NM 2008 3 13 SWAA081273 1 20080309 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 204, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031400024 20080314 00024 NM 2008 3 14 2008UALA01136 1 20080229 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1480 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 AFT PIT FRAME DENTED AT INBOARD FLANGE AT BS 1480 BETWEEN STR 25L AND STR 26L. MAJOR REPAIR ACCOMPLISHED AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031400026 20080314 00026 NM 2008 3 14 2008UALA01139 1 20080302 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 FOUND DENT AND WEAR MARKS ON FUSELAGE. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031400033 20080314 00033 EU 2008 3 14 2008UALA01194 1 20080304 A 5754 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 4 SLAT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 495UA 1842 LT NR 4 LEADING EDGE SLAT DAMAGED ON ARRIVAL. REMOVED AND REPLACED NR 4 LT SLAT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031400053 20080314 00053 NM 2008 3 14 CALA0800206 1 20080306 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM BS 747 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 FRAME CRACKED STA 747 ABOVE S9L. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A. 2 L 7 2 4F RT A16WE 2008031400059 20080314 00059 NM 2008 3 14 QXEA200800251 1 20080227 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 242-245 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - LEFT INBOARD SEAT TRACK NR 7 HAS CORROSION ON THE INBOARD FLANGE OF TRACK FROM STATION 242 TO 245. REPAIRED IAW DASH 8 Q400 RD8/4-53-884 AND NDTM PART 6 51-00-01. 2 H 7 2 4T RT A13NM 2008031700001 20080317 00001 SO 2008 3 17 C2XA08ON097 1 20080303 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO LAVATORY MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 11189 6978 6978 14500931 FLT 0001 - ONT - FLIGHT CREW REPORTED LAV SMOKE INDICATION DURING CLIMB. NO VISIBLE SMOKE. AIRCRAFT RETURNED TO BLOCK WITHOUT INCIDENT, EMERGENCY WAS NOT DECLARED. MX PERSONNEL INSPECTED AND FOUND NO DEFECTS. OPERATIONALLY CHECKED SATIS FACTORY. AIRCRAFT WAS RELEASED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2008031700008 20080317 00008 2008 3 17 C2XA08CL023 4 20080304 A 3160 7014300901 DISPLAY EMB 145 EMB145LR 3260212 SO COCKPIT SHORTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14905 145476 DURING ROUTINE MAINTENANCE SMOKE WAS OBSERVED COMING FROM THE EICAS ON POWER UP. MAINTENANCE INSPECTED AND REPLACED THE EICAS DISPLAY UNIT NR 3. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008031700017 20080317 00017 SO 2008 3 17 C2XA08IA074 1 20080301 A 2150 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 14116 145672 IAH - FLIGHT 2084, THE CREW REPORTED A STRONG FUEL ODOR AFTER TAKEOFF THAT WENT AWAY WHEN ENGINE BLEEDS WERE SELECTED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE APU FOR FUEL LEAKS AND, OPERATIONALLY CHECKE D THE PACKS WITH APU BLEED AIR ALL WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008031700021 20080317 00021 NM 2008 3 17 2008UALA01269 1 20080307 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 910UA 25254 DOOR 2R HAS TWO INCH CRACK IN FUSELAGE SKIN AT LOWER FWD CORNER. MAJOR REPAIR ACCOMPLISHED: MANUFACTURED & INSTALLED FI LLER, DOUBLER NR 1, DOUBLER NR 2 AND TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031700032 20080317 00032 SO 2008 3 17 SIMA200807002 1 20080303 A 3222 STRUT EMB 145 EMB145LR 3260212 SO NOSE DISCHARGED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 933JN 14500918 ON FLIGHT 3459, CREW REPORTED AFTER TAKEOFF EICAS LANDING GEAR AIR/GND MESSAGES. SHORTLY AFTER RECEIVING EICAS MESSAGE RETURNED TO DFW AND MESSAGE EXTINGUISHED WITH GEAR DOWN ON APPROACH. AIRCRAFT REMOVED FROM SERVICE. FOUND NOSE STRUT D EPLETED OF NITROGEN NOT EXTENDING SERVICED NOSE GEAR WITH NITROGEN IAW 32-20-01 AND VERIFIED FULL EXTENSION OF NOSE STRU T. WEIGHT WHEEL PROX SWITCH GAP AND WIRING WAS VERIFIED IN GOOD WORKING CONDITION IAW FIM 32-63-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008031700060 20080317 00060 NM 2008 3 17 SWAA081306 1 20080306 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C1 CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008031700073 20080317 00073 NM 2008 3 17 SWAA081282 1 20080307 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 400WN 27891 EEPLS LENS MISSING AT ROW 10 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008031700085 20080317 00085 EU 2008 3 17 08FDEA00813 1 20080310 A 5320 A53973637212 PANEL AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND DOUBLE HOLES IN TORSION BOX SHEET C 59-60, P 44-46 RT. REPAIR PERFORMED BY CUT OUT THE TORSION BOX AND INSTALLING A SPLICE IAW. SRM 53-17-18 FIG.206. 2 L 7 2 4F RT A35EU 2008031700088 20080317 00088 NM 2008 3 17 SWAA081289 1 20080307 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS CRACKED AT ROW 5 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008031700091 20080317 00091 NM 2008 3 17 SWAA081291 1 20080307 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS CRACKED AT ROW 3 DEF. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008031700108 20080317 00108 EU 2008 3 17 08FDEA00830 1 20080310 A 5347 R5327049020000 SEAT TRACK AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 806FD 458 MAIN DECK CARGO FLOOR SEAT TRACK NR 1 RT SIDE, FR 61 HAS DAMAGE ON LOWER SURFACE, .545 IN ROUND BY .045 IN DEEP. REMO VED DAMAGED SEAT TRACK SECTION FROM FR 60.5 TO FR 61.5 AND REPAIRED IAW A310 SRM 53-10-16,FIG 208 2 L 7 2 4F RT A35EU 2008043000020 20080430 00020 EA 2008 4 30 TRAX200800565 1 20080420 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA ASD BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 ASD HARD TO OPEN. 2 L 7 2 4F RT A21EA 2008031700125 20080317 00125 EU 2008 3 17 08FDEA00844 1 20080310 A 5311 A5397317827600 FRAME AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT FUSELAGE FRAME HAS CORROSION ON THE WEB AT FRAME 64 BETWEEN STR 49L AND 50L. REMOVED CORROSION IAW SRM 51-74-10 . ORIGINAL MATERIAL 0.045; MATERIAL REMOVED 0.017, MATERIAL REMAINING 0.028. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00 . FORMED ANGLE, HEAT TREATED ANGLE IAW TPS 1003; REV A. DRILLED UP PARTS, ALODINED, PRIMED & TOP COATED PARTS IAW SR M 51-40-44, 51-21-10, & 51-23-10. INSTALLED PARTS IAW SRM 53-10-13. ALSO APPLIED TOP COAT ON PARTS IAW SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008031700127 20080317 00127 EU 2008 3 17 08FDEA00846 1 20080310 A 5311 A53973179270 FRAME AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT FUSELAGE FRAME WEB HAD CORROSION AT FRAME 66 BETWEEN STR 49L AND STR 50L. REPAIRED FUSELAGE FRAME 66 BETWEEN ST RINGER 49L & STRINGER 50L IAW SRM 53-10-10; PARA 4. 2 L 7 2 4F RT A35EU 2008031700129 20080317 00129 EU 2008 3 17 08FDEA00847 1 20080310 A 5321 A2901115300000 FLOOR PANEL AIRBUS 310 A310203 3930313 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FLOOR PANEL 147BF UPPER LAYERS ARE DETERIORATED IN NUMEROUS PLACES. FABRICATED NEW FLOOR PANEL 147 BF; POTTED EDGES; COMPLETED CURE & SANDED EDGE POTTING. INSTALLED INSERTS & APPLIED NON-SKID IAW SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 2008031700131 20080317 00131 NM 2008 3 17 SWAA081323 1 20080310 A 5531 6546872 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED 12Y CHECK, FOUND VERTICAL STABILIZER SPAR RT AND LT AFT OUTBOARD LUG FITTINGS CORRODED. REPAIRED FITTI NGS PER MM. 2 L 7 2 4F RT A16WE 2008031700137 20080317 00137 NM 2008 3 17 SWAA081316 1 20080310 A 5310 6978062 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 2008031700139 20080317 00139 NM 2008 3 17 SWAA081315 1 20080310 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED SPV CHECK, FOUND STRINGER 16R CRACKED AT BS 487. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008031700141 20080317 00141 NM 2008 3 17 SWAA081317 1 20080310 A 5310 6516352 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 2008031700142 20080317 00142 NM 2008 3 17 AALA200800469 1 20080302 A 2761 PLUG BOEING 767 767323 1385205 NM SPOILER ACTUATOR CRACKED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 387AM 27184 LAX INFLIGHT T88/02MAR - AFTER TAKEOFF, LEFT HYDRAULIC QUANTITY DECREASED TO .15. RETURNED TO LAX AND LANDED WITHOUT I NCIDENT. FOUND NUMBER SIX SPOILER ACTUATOR FILTER PLUG CRACKED AND LEAKING. REPLACED NUMBER SIX SPOILER ACTUATOR FILTE R PLUG AND O-RING. REPLACED ALL FOUR LEFT BRAKES DUE TO HYDRAULIC CONTAMINATION. SERVICED LEFT HYDRAULIC SYSTEM. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008011600218 20080116 00218 NM 2008 1 16 SWAA080309 1 20080114 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 DURING SCHEDULED HC1 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008011600221 20080116 00221 NM 2008 1 16 SWAA080312 1 20080114 A 5315 141A5504 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 760SW 27874 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 45 TO RBL 60. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2008011600279 20080116 00279 NM 2008 1 16 SWAA080217 1 20080109 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT RT BS 520 TO RT BS 540. REMOVED AND REPLA CED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008011600282 20080116 00282 2008 1 16 SWAA080219 4 20080109 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008011600283 20080116 00283 NM 2008 1 16 SWAA080211 1 20080109 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2008011600284 20080116 00284 NM 2008 1 16 SWAA080210 1 20080109 A 5311 6558280 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600285 20080116 00285 NM 2008 1 16 SWAA080209 1 20080109 A 5311 6546548 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600286 20080116 00286 NM 2008 1 16 SWAA080208 1 20080109 A 5311 65C22909 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600330 20080116 00330 WP 2008 1 16 NWAA070029941 1 20080104 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 465 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3224L 47103 DURING GROUND OPERATIONS AIRCRAFT WAS STRUCK BY A SERVICE TRUCK. FUSELAGE SKIN AT BS 465 L22L AND L23L AND SHEAR TIE AT BS 465 WERE DAMAGED. REPAIRED ACCOMPLISHED PER EA 99-211512. 2 L 7 2 4F A6WE 2008011600332 20080116 00332 EA 2008 1 16 MASA200800004 1 20080102 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE INDICATION A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 37342 7342 ASH FLT 7350 CAE-ORD - LAV SMOKE CAUTION MESSAGE. CREW REPORTED THE MESSAGE OCCURRED WHILE TRYING TO COOL DOWN THE PACK S IN MANUAL MODE. CREW REPORTED NO ODOR OR SIGN OF ACTUAL SMOKE. MX OP CHECKS THE LAV SMOKE DETECTION SYSTEM AND PACK SYSTEM WITH NO FAULTS FOUND. 2 L 7 2 4F RT A21EA 2008011600342 20080116 00342 EU 2008 1 16 08FDEA00058 1 20080107 A 5313 A53974202471 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 AFT PIT STR 49R, FRAME 59 HAS CORROSION. REPAIRED STR 49R AT FR 59 IAW A310 SRM 53-10-14 FIG 201, REPLACED STR 49R FROM FR 58 TO FR 60. 2 L 7 2 4F RT A35EU 2008011600343 20080116 00343 EU 2008 1 16 08FDEA00059 1 20080107 A 5311 A5711211720101 FRAME AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FRAME 46 LT HOLE NR 24 CRACK INDICATION IN FITTING ATTACH ANGLE, HOLE NR 25 CRACK INDICATION IN FRAME FOOT AND ATTACH AN GLE, HOLE NR 27 INDICATION IN FRAME FOOT AND HOLE NR 29 INDICATION IN FRAME FOOT. REAMED HOLES 25 AND 29 IAW EA 6-5310- 113006, INSTALLED BUSHINGS IAW EA 6-5310-113006. REAMED HOLES TO .250 IAW EA 6-5310-113006. INSTALLED FASTENERS NSA-53 51-4-9 IAW EA 6-5310-113006. LOCATED AND DRILLED NEW FRAME STRAP (HOLES 24 AND 27 IN FRAME STRAP) AND INSTALLED IAW A31 0-200 SRM 51-40-21 PAR 7. 2 L 7 2 4F RT A35EU 2008011600345 20080116 00345 EU 2008 1 16 08FDEA00061 1 20080107 A 5311 A5711211720100 FRAME AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 HOLE NR 21 FRAME 45 RT HAS CRACK INDICATION IN FRAME FOOT. REAMED HOLE 21 FR 45R TO .314 IAW EA 6-5310-113006. COLD WO RKED HOLE IAW EA 6-5310-113006 AND SRM 51-40-41 PF 5/6 TABLE 1. FINAL REAMED HOLE TO .339 IAW EA 6-5310-11306. INSTALL ED FASTENER IAW EA 6-5310-113006. 2 L 7 2 4F RT A35EU 2008011600001 20080116 00001 NM 2008 1 16 SWAA080171 1 20080107 A 2560 6557463 FITTING BOEING 737 7373Q8 1384670 NM GIRT BAR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CRACKED. REMOVED AND REPLACED FITTI NG PER MM. 2 L 7 2 4F RT A16WE 2008011600014 20080116 00014 NM 2008 1 16 SWAA080187 1 20080108 A 3230 BACC2C4A556 CONTROL CABLE BOEING 737 7373H4 1384600 NM MLG WW OUT OF ADJUST A SWAA K NONE J WARNING INDICATION AP APPROACH 1 SW 29 313SW 23335 ON APPROACH HAD THREE GREEN LIGHTS AND THREE RED LIGHTS, CYCLED GEAR LEVER HAD THREE GREEN LIGHTS NO RED. ADJUSTED LAND ING GEAR CONTROL CABLE PER MM. 2 L 7 2 4F RT A16WE 2008011600026 20080116 00026 NM 2008 1 16 SWAA080197 1 20080108 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008011600027 20080116 00027 NM 2008 1 16 SWAA080198 1 20080108 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 14L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2008011600060 20080116 00060 NM 2008 1 16 SWAA080239 1 20080110 A 5312 6546568 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REMOVED AND REPLACED WEB PER SR M. 2 L 7 2 4F RT A16WE 2008011600063 20080116 00063 NM 2008 1 16 SWAA080241 1 20080110 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED SERVICE CHECK, FOUND AFT LT FUSELAGE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008011600081 20080116 00081 NM 2008 1 16 SWAA080285 1 20080113 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600106 20080116 00106 NM 2008 1 16 08FDEA00046 1 20080105 A 5730 112N60032 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 901FD 27122 RT WING TANK ACCESS PANEL 643BB HAS SURFACE CORROSION ON LOWER SURFACE. REMOVED CORROSION ON PANEL 643BB IAW SRM 57-20- 01, FOUND TO BE OUT OF LIMITS PER DETAIL I, SEC AA, NOTE B, NOT ALLOWED DAMAGE PER FIG 201. ORDERED AND REPLACED WITH N EW PANEL. 2 L 7 2 4F RT A2NM 2008011600108 20080116 00108 EU 2008 1 16 08FDEA00049 1 20080106 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 400 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 55 RT BETWEEN FR 55/58 TO 60 HAS 1 EA REPAIR SECTION MEASURING 29" LONG AND 1 EA REPAIR SPLICE MEASURING 7.9" LONG REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUSLY INSTALLED REPA IR AND INSTALLED CORRECT STRINGER REPAIR IAW A310 SRM 53-10-14, FIG 201. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008011600176 20080116 00176 NM 2008 1 16 SWAA080271 1 20080110 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 438WN 29833 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 129. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600201 20080116 00201 NM 2008 1 16 SWAA080284 1 20080113 A 5315 147A5504 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 760SW 27874 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947, LBL 5. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2008011600213 20080116 00213 NM 2008 1 16 SWAA080304 1 20080114 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED MV1 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 2008011600239 20080116 00239 EA 2008 1 16 MASA200800003 1 20080101 A 2611 SMOKE WARNING CNDAIR CL600 CL6002D24 1390016 EA LAVATORY ILLUMINATED A MASA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 909FJ 15009 ASH FLT 2708 PHX - AFT LAV SMOKE WARNING ON TAXI. RESET SYSTEM, OPS GOOD. 2 L 7 2 4F RT A21EA 2008011600329 20080116 00329 2008 1 16 TSAA0834001 4 20080104 A 3425 4033169902 INDICATOR BOEING 737 737236 1384476 NM NR 1 HSI FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 153FV 23172 NON-ETOPS FLIGHT 205 HNL-LIH - DURING CLIMB, THE CREW NOTED THE NR 1 HSI DISPLAYED THE HEADING FAULT FLAG. THE CREW LAN DED IN HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 HSI WITH ALL OPERATIONAL CHECKS SATISFAC TORY PER AMM 34-26-21. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2008011600340 20080116 00340 SO 2008 1 16 SIMA200800801 1 20080106 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO CARGO DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 671AE 9733 5000 145793 DURING IMBV INSPECTION THE CARGO DOOR SILL WAS FOUND TO BE CORRODED BEYOND MANUAL LIMITS. REPLACED CARGO DOOR SILL IN A CCORDANCE WITH EMBRAER SRM (SRM-145/1142 REV. 38) CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008011600350 20080116 00350 EU 2008 1 16 08FDEA00066 1 20080108 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS CROSSBEAM REPAIR LOCATED IN FWD CARGO UNDERFLOOR AT FRAME 38.2 BETWEEN ROLLER TRACKS LT NR 2 Y805 AND RT NR 2 -Y805 HAS 1 REPAIR SECTION MEASURING 27.4" LONG AND 2 REPAIR ANGLES MEASURING 11" LONG LT SIDE AND 8.5" LONG RT SID E REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUSLY INSTALLED REPAIR AND INSTALLED CORRECT CROSSBEAM REPAIR IAW A310 SRM 53-10-15, FIG 207. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTI ON. 2 L 7 2 4F RT A35EU 2008011600351 20080116 00351 EU 2008 1 16 08FDEA00067 1 20080108 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 200 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS REPAIR LOCATED ON MAIN CABIN FLOORBEAM FR 37 LT SIDE BETWEEN SEAT TRACKS NR 4 LT Y1456 AND NR 5 LT Y1959 HAS 1 REPAIR ANGLE MEASURING 8.5" LONG BY 2.5" WIDE ON THE UPPER FORWARD FLANGE WITH 2 STOP DRILLED HOLES ON FLOORBEAM REPAIR NOT IAW EA REQUIREMENTS. REMOVED PREVIOUSLY INSTALLED REPAIR AND INSTALLED CORRECT FLOORBEAM REPAIR IAW FED EX EA 6-512 2-50302, DATED MAY 3, 2000. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INS PECTION. 2 L 7 2 4F RT A35EU 2008011600354 20080116 00354 EU 2008 1 16 08FDEA00070 1 20080108 A 5320 FLOOR SUPPORT AIRBUS 310 A310203 3930313 EU ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS REPAIR LOCATED ON MAIN CABIN COURIER AREA FLOOR SUPPORT "T" CAP RT SIDE BETWEEN FR 14 TO 15A , NR 4 LONGERON FR OM CENTER -Y1956 HAS 2EA REPAIR ANGLES MEASURING 7.2" LONG AND 1 REPAIR SECTION MEASURING 17.2" LONG. REPAIR NOT IAW SR M REQUIREMENTS. REMOVED PREVIOUSLY INSTALLED REPAIR AND INSTALLED CORRECT REPAIR IAW A310 SRM 53-12-15,FIG 207. THIS I S AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008011600355 20080116 00355 WP 2008 1 16 NWAA080039751 1 20080105 A 2150 ACM DOUG DC9 DC941 302207N WP LEFT ODOR A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 01 751NW 47115 ON FINAL APPROACH INTO MSP, ODOR OF SMOKE FILLED THE AFT CABIN SECTION. THE AFT LAVATORY SMOKE DETECTOR WENT INTO ALARM AND ILLUMINATED THE WARNING INDICATOR IN THE COCKPIT. ALL OTHER INDICATIONS WERE NORMAL INCLUDING ALL THE PACKS. FLIG HT CREW REQUESTED THAT EMERGENCY VEHICLES MEET THE AIRCRAFT AFTER LANDING. FLIGHT LANDED WITHOUT INCIDENT AND THE SMOKE DISSIPATED AFTER TOUCHDOWN. MAINTENANCE FOUND EVIDENCE OF OIL IN THE LEFT COALESCER BAG AND DETERMINED THE SOURCE TO B E THE LEFT AIR CYCLE MACHINE. THE ACM WAS REPLACED; PACK BURNOUT PROCEDURES COMPLIED WITH, AND A FINAL WATER SOCK REPLAC EMENT PRIOR TO THE AIRCRAFT RETURNING TO SERVICE. 2 L 7 2 4F A6WE 2008011600362 20080116 00362 EU 2008 1 16 MALA080002 1 20080106 A 5512 SKIN SAAB SF340 340B 7860101 EU HORIZONTAL STAB DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 DENT IN LOWER SKIN OF RT HORIZONTAL STABILIZER. PERFORMED PERMANENT REPAIR TO DENT ON LOWER SKIN OF RT HORIZONTAL STABI LIZER IAW MAL EO NR S55017. 2 L 7 2 4T RT A52EU 2008011600363 20080116 00363 EU 2008 1 16 MALA080003 1 20080106 A 5320 PANEL SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 PANEL 193AL HAS SEVERAL DENTS. REPAIRED DENTS ON PANEL 193AL WITH A COLD BOND WET LAYUP IAW MAL EO NR S51031. 2 L 7 2 4T RT A52EU 2008011600365 20080116 00365 EU 2008 1 16 121834010808 1 20080107 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A HYIA K NONE L NO TEST IN INSP/MAINT 1 EA 61 14834 193 FLOOD LIGHT FOR EMERGENCY LIGHT AT PASSENGER/CREW DOOR IN OPERATIVE. REMOVED AND INSTALLED SERVICEABLE EMERGENCY FLOOD LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. 2 H 7 2 4T RT A53EU 2008011600384 20080116 00384 NM 2008 1 16 NWAA080045647 1 20080103 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 547US 26494 DURING OVERNIGHT LINE CHECK, EMERGENCY LIGHT AT DOOR 1L AND F/C AISLE LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POW ER SUPPLY AND BATTERY PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2008011600394 20080116 00394 WP 2008 1 16 08FDEA00079 1 20080109 A 5311 ABA71125 FRAME DOUG DC10 DC1030F 3023504 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 308FE 48297 UPPER FUSELAGE ENTRY WAY CRACK ON FITTING SUPPORT (P/N AWE8001-503 ). REPAIRED FRAME IAW SRM 53-30-00 FIG 5 SHT 1 VOL I . 2 L 7 3 4F RT A22WE 2008011700003 20080117 00003 EA 2008 1 17 SWIA200819025 1 20080106 A 5240 SEAL CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 433SW 7550 FLT 3906 - GALLEY SERVICE DOOR IS EXTREMELY HARD TO OPEN. REPLACED GALLEY SERVICE DOOR SEAL IAW MM 52-41-02. 2 L 7 2 4F RT A21EA 2008011700009 20080117 00009 SO 2008 1 17 SWIA200819031 1 20080102 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 393SW 120330 RIGHT WING FUEL PANEL ACCESS HAS A CRACK ON STRINGER 10 BETWEEN FRAMES 8 AND 9. REPAIRED CRACKED AFT STRINGER IAW SRM 5 7-20-03. 2 L 7 2 4T RT A31SO 2008011700086 20080117 00086 EU 2008 1 17 NSVA20070253 1 20080107 A 3350 SIGN SAAB SF340 SF340A 7850100 EU EMERGENCY LIGHTS INOPERATIVE A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 121CQ 121 EMERGENCY EXIT SIGN FORWARD CABIN RIGHT SIDE DOES NOT ILLUMINATE. TESTED EMERGENCY EXIT LIGHT IAW AMM 33-50-10. OPS CH ECK GOOD. 2 L 7 2 4T RT A52EU 2008011700087 20080117 00087 EU 2008 1 17 08FDEA00080 1 20080109 A 5320 A5387006420100 BRACKET AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN CABIN CORNER BRACKET CRACKED BELOW EMERGENCY EXIT DOOR AT FR 43R. REMOVED CRACKED BRACKET IAW A310-200 SRM 51-40-2 1 PARA 7. FABED BRACKET IAW AIRBUS DWG A53870064. ALODINED IAW A310-200 SRM 51-21-10, PRIMED AND PAINTED IAW A310-200 SRM 51-23-10 AND INSTALLED BRACKET IAW A310-200 SRM 51-40-21 PARA 7 PART MARKED BRACKET IAW FEDEX GMM 7-0-1000. 2 L 7 2 4F RT A35EU 2008011700089 20080117 00089 EU 2008 1 17 08FDEA00082 1 20080110 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 57 BETWEEN FRAMES 68 TO 70 HAS 1 REPAIR SECTION MEASURING 18. 8" LONG AND 2 REPAIR SPLICES MEASURING 7.6" LONG REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED . CORRECT REPAIR IAW FED-EX EA NR 6-5310-113429, DATED 16 DECEMBER 2007. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PAR T NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008011700090 20080117 00090 EU 2008 1 17 08FDEA00083 1 20080110 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 53 RT BETWEEN FRAMES 61 TO 63 HAS 2 REPAIR SECTION MEASURING 1 6" LONG FOR THE FORWARD REPAIR SECTION AND 19.7" LONG ON THE AFT SECTION WITH 2 REPAIR SPLICES MEASURING 8" LONG. REPAI R NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT STRINGER REPAIR IAW A310 SRM 53-10-14, FIG 20 1. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008011700091 20080117 00091 EU 2008 1 17 08FDEA00084 1 20080110 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 52 RT BETWEEN FRAMES 60 TO 62 HAS 1 REPAIR SECTION MEASURING 1 6.3" LONG AND 2 REPAIR SPLICES MEASURING 7.4" LONG. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTA LLED CORRECT STRINGER REPAIR IAW A310 SRM 53-10-14, FIG 201. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008011700092 20080117 00092 EU 2008 1 17 08FDEA00085 1 20080110 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN AFT CARGO ON STRINGER 54 RT BETWEEN FRAMES 55/58 TO 60 HAS 1 REPAIR SECTION MEASURIN G 29" LONG AND 1 REPAIR SPLICE MEASURING 7.9" LONG. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTA LLED CORRECT STRINGER REPAIR IAW A310 SRM 53-10-14, FIG 201. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008011700108 20080117 00108 NM 2008 1 17 HALA0800012 1 20080109 A 2841 INDICATOR BOEING 767 76733A 1385209 NM FUEL QTY INOPERATIVE A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, CENTER FUEL TANK AND TOTAL FUEL QUANTITY INDICATOR BLANK. EICAS MSG FUEL QTY IND DISPLAYED. FUEL QTY TEST NOT CHECKED. PERFORMED BITE CHECK OF FQIS COMPUTER PER FIM 28-41-00 FIG 104. NO CURRENT OR PREVIOUS FLT FAULTS INDICATED. QUANTITY INDICATION NOW NORMAL ON BOTH GAUGES. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008011700112 20080117 00112 EU 2008 1 17 08FDEA00092 1 20080110 A 5311 A53778807202 FRAME AIRBUS 310 A310203 3930313 EU BS 1870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FWD LOWER CARGO PIT FRAME 34 RBL 56 "T" CAP CORRODED REMOVED CORROSION IAW A310 SRM 51-74-10 ORIGINAL THICKNESS .125 REM AINING THICKNESS .094. REMOVED .031 FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-00 TABLE 102 MATERIAL ID T-CAP LN9497. 420. REPAIR PROFILE LN 9496.310 IAW A310 SRM 53-14-15 AND 53-10-15, TREATED IAW A310 SRM 51-21-10 AND 51-23-10. INSTAL LED IAW A310 SRM 51-10-30. 2 L 7 2 4F RT A35EU 2008011700113 20080117 00113 EU 2008 1 17 08FDEA00093 1 20080110 A 5311 A53778807202 FRAME AIRBUS 310 A310203 3930313 EU BS 2029 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FWD LOWER CARGO PIT FR37 LBL 56 "T" CAP CORRODED UNDER NUT PLATES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW A310 SRM 53-10-00 ORIGINAL .126 REMAINING .092 REMOVED .034. REMOVED T-CAP IAW A310 51-40-21 MATERIAL ID LN9497A420 FOR T -CAP FRAME LN9496B310 IAW A310 SRM 53-10-15. ALODINED IAW A310 SRM 51-21-10. PRIMED AND PAINTED IAW A310 SRM 51-23-10. INSTALLED T-CAP IAW A310 SRM 53-10-15. 2 L 7 2 4F RT A35EU 2008011700114 20080117 00114 EU 2008 1 17 08FDEA00094 1 20080110 A 5311 A53778807202 FRAME AIRBUS 310 A310203 3930313 EU BS 1923 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 FWD LOWER CARGO OIT FR35 LBL56 T-CAP CORRODED REMOVED CORROSION IAW A310 SRM 51-71-10, FOUND TO BE OUT OF LIMITS IAW A31 0 SRM 53-10-00 ORIGINAL .126 REMAINING .090 REMOVAL OF .036 REMOVED T-CAP IAW SRM 51-40-21 MATERIAL ID LN 9497A420 IAW A 310SRM 53-10-15. FABBRICATED IAW A310 SRM 53-10-15. ALODINED IAW A310 SRM 51-21-10. PRIMED AND PAINTED IAW A310 SRM 5 1-23-10 INSTALLED IAW A310 SRM 53-10-15 2 L 7 2 4F RT A35EU 2008011700115 20080117 00115 EU 2008 1 17 08FDEA00095 1 20080110 A 5711 NA57150824 SPAR AIRBUS 310 A310222 3930315 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 416FE 288 CORROSION ON RIGHT WING REAR SPAR DOUBLER AROUND SPOILER NR 7 ACTUATOR REMOVED CORROSION IAW A310-200 SRM 51-74-10 ITEM 3. ORIGINAL THICKNESS .206 IAW AIRBUS DRAWING N : A 571-50824. REMOVED .002, REMAINING THICKNESS .204. WITHIN LIMITS IAW A310-200 SRM 57-51-11 PAGE 102. ALODINED IAW A310-200 SRM 51-21-10 PAGE 3, PRIMED IAW A310-200 SRM 51-23-10 PAGE 2 4, PAINTED IAW A310-200 SRM 51-23-10 PAGE 24. 2 L 7 2 4F RT A35EU 2008011700120 20080117 00120 NM 2008 1 17 08FDEA00102 1 20080110 A 5315 BAC15123345 FLOORBEAM BOEING 757 757200 1384950 NM BS 1640 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 CORROSION ON FLOORBEAM AT STA 1640, LBL9 AND RBL14. REPAIR CARRIED OUT IAW SRM 53-00-51 FIG 201 REPAIR 1 AS PER EAR P33 7-24137-C0017. 2 L 7 2 4F RT A2NM 2008011800003 20080118 00003 EU 2008 1 18 SIMA200801001 1 20080109 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 219AE 340B219 ON FLIGHT 3270, EMERGENCY EXIT LIGHTS IN CABIN DOOR AND FLOOR INOP AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY 21LN. PERFORMED OPERATIONAL CHECK OF LIGHTS. OPERATIONAL CHECK GOOD IAW SAAB 340 AMM 33-5 0-10. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2008011800004 20080118 00004 SO 2008 1 18 SIMA200800901 1 20080107 A 4990 4504113 APU EMB 135 EMB135LR 3260305 SO LEAKING A SIMA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 723AE 145288 ON FLIGHT 4883, ON THE GROUND AT GATE CREW GOT THE LAV SMOKE ON EICAS. CREW REPORTED THAT THERE WAS SMOKE AND POSSIBLE FIRE IN LAV. EVACUATED AIRCRAFT BY STAIRS. FIRE DEPT INSPECTED AIRCRAFT AND FOUND NO EVIDENCE OF FIRE. AIRCRAFT REMOV ED FROM SERVICE. SMOKE IN CABIN CAUSED BY INTERNAL LEAKING INSIDE APU. REMOVED AND REPLACED APU IAW W/C 49-800-05. NO LEAKS NOTED. NO FURTHER DEFECTS NOTED AT THIS TIME. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008011800005 20080118 00005 EA 2008 1 18 SIMA200801002 1 20080108 A 3150 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA FALSE INDICATION A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 521AE 10142 ON FLIGHT 3895, CREW REPORTED T/O ABORT DUE TO A EMERGENCY LIGHT WARNING THAT WENT AWAY BEFORE HE COULD EVEN LOOK DOWN A ND SEE WHAT IT WAS. CHECKED MDC FOR CURRENT FAULTS CHECKED FAULT HISTORY NO FAULTS NOTED HIGH SPEED TAXI PERFORMED BY F LIGHT CREW (TWICE), NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2008011600061 20080116 00061 NM 2008 1 16 SWAA080238 1 20080110 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 887, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008011600071 20080116 00071 NM 2008 1 16 SWAA080253 1 20080110 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008011600080 20080116 00080 NM 2008 1 16 SWAA080286 1 20080113 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008011600188 20080116 00188 NM 2008 1 16 SWAA080279 1 20080113 A 3350 20131A BATTERY PACK BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008011600210 20080116 00210 NM 2008 1 16 SWAA080302 1 20080114 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 EEPLS LENS CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008011600280 20080116 00280 NM 2008 1 16 SWAA080218 1 20080109 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED 14Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT RT BS 747 TO RT BS 827. REMOVED AND REPLA CED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008011600335 20080116 00335 EA 2008 1 16 MASA200800010 1 20080105 A 3350 9324131501 COVER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BROKEN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 7264V 7264 ASH 2864 PHX - ONE FWD FLOOR PATH LIGHTING COVER BROKEN. REPLACED COVER. 2 L 7 2 4F RT A21EA 2008011600337 20080116 00337 NM 2008 1 16 MASA200800015 1 20080106 A 5230 SKIN DHAV DHC8 DHC8202 2809007 NM CARGO DOOR DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 454YV 454 CARGO DOOR OUTER SKIN HAS SCRATCHES. REPAIRED CARGO DOOR. 2 H 7 2 4T RT A13NM 2008011600387 20080116 00387 EU 2008 1 16 08FDEA00076 1 20080109 A 5313 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 404FE 233 PREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 56 LT BETWEEN FRAMES 66 TO 69 HAS 1 REPAIR SECTION MEASURIN G 47.1" LONG AND 2 REPAIR SPLICES MEASURING 8" LONG. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INST ALLED CORRECT STRINGER SPLICE REPAIR IAW A310 SRM 53-10-14, FIG 201. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUM BER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008011700028 20080117 00028 NM 2008 1 17 F3LA200800001 1 20080107 A 2750 FLAP SYSTEM AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE TE FLAPS OUT OF ALIGNMENT A F3LA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 03 935FR 2318 DURING THE APPROACH, THE FLIGHT CREW RECEIVED AN ECAM MESSAGE THAT THE FLIGHT CONTROLS - FLAPS - WERE LOCKED DUE TO AN A LIGNMENT FAULT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE RESET THE WING TIP BREAK I N ACCORDANCE WITH AMM 27-50-00-869-006 AND PERFORMED EXTENSION AND RETRACTION TESTS IN ACCORDANCE WITH AMM 27-50-00-866- 008. MAINTENANCE ALSO PERFORMED BITE TEST OF SFCC 1 AND 2 IN ACCORDANCE WITH AMM 27-51-00-740-002 AND NO FAULTS WERE FO UND. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM 2008011700030 20080117 00030 NM 2008 1 17 08FDEA00100 1 20080110 A 5270 JE5 SWITCH BOEING 727 727277 138408S NM DAMAGED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 241FE 20979 AFT AIRSTAIR AMBER WARNING LIGHT ILLUMINATED IN FLIGHT WHILE CRUISING AT FL 350. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 21JAN08 "MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT - INOP." REMOVED AND RE PLACED AFT AIRSTAIRS UPPER HANDLE SWITCH S395 USING S/M/P REF AMM CHAPTER 20. PERFORMED ADJ/TEST REF AMM 52-70-001-5. OPS CHECKS NORMAL. 2 L 7 3 4F RT A3WE 2008011700121 20080117 00121 NE 2008 1 17 UIEA200800007 2 20080108 A 7300 UNKNOWN BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE UNKNOWN A UIEA O OTHER O OTHER CL CLIMB 1 EA 15 355MC 23395 530272 DURING CLIMB WITH AUTOTHROTTLES ENGAGED AND CLIMB THRUST SET AT APPROX FL10.5 NR 4 ENGINE ROLLED BACK TO IDLE THRUST AFT ER ABOUT 10 SECONDS NR 4 ENGINE RETURNED TO CLIMB THRUST. THE THRUST LEVER NEVER MOVED. THE ENGINE OPERATED NORMAL FOR THE REMAINDER OF THE FLIGHT. INSPECTED INLET AND EXHAUST PER AMM 71-00-00, NO DEFECTS NOTED. FOLLOW TROUBLESHOOTING C HART ON AMM 71-00-42, BLEW OUT THE CDP LINE AND CHECKED FOR LEAKS. NO LEAKS OR DEFECTS NOTED. CHECKED AND FOUND FUEL F ILTER CLEAN. REPLACED FILTER AS A PRECAUTION. PERFORMED ENGINE RUN TEST 3, THE ENGINE OPS CHECKED OKAY. INSPECTED VSV FEEDBACK CABLE. 2 L 7 4 4F 4 F RT A20WE E23EA 2008011700123 20080117 00123 NM 2008 1 17 HALA0800015 1 20080111 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 CORROSION FOUND IN SEAT TRACK, SECT 46, RBL 88.5 AT SEVERAL LOCATIONS. SEAT TRACK FROM STA 977-1186 AND STA 1208 - STA 1428 CORROSION REMOVED. REWORKED AREA OUT OF SRM 53-00-52 ALLOWABLE DAMAGE LIMITS 1. STATION 1186 - 1208 AND STA 1428 - 1444, CORROSION REMOVED AND FOUND TO BE WITHIN SRM 53-00-52 ALLOWABLE DAMAGE LIMITS. REWORKED AREAS ALODINED AND PAINT ED IAW SRM 53-00-52 AMD SPM 20-41-04. LPS -3 APPLIED TO SEAT TRACKS. 2 L 7 2 4F RT A1NM 2008011700124 20080117 00124 NM 2008 1 17 HALA0800014 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 791-797 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 CORROSION ON SECTION 45 SEAT TRACK AT RBL 11, STA 791-797. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 51 -10-02 REV 75. BLENDED WITHIN LIMITS, IAW SRM 53-00-52/101 REV76. 2 L 7 2 4F RT A1NM 2008011800002 20080118 00002 NM 2008 1 18 NWAA080065515 1 20080108 A 2540 LAVATORY BOEING 757 757251 1384970 NM FIRE A NWAA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 GL 01 515US 23203 AIRCRAFT WAS AT GATE PRIOR TO BOARDING, THERE WAS AN ONBOARD FIRE IN LAV 3L. PILOT AND FIRST OFFICER HAD ALL OTHER CREW MEMBERS EVACUATE AIRCRAFT. 2 HALON FIRE BOTTLES WERE USED TO EXTINGUISH FIRE. FIRE AND RESCUE WAS CALLED WHEN SMOKE/F IRE WAS FIRST NOTICED. MAINTENANCE REMOVED AND REPLACED FILL SENSOR AND 2 CIRCUIT BREAKERS. OPERATION AND LEAK CHECK G OOD, OK FOR SERVICE JOB COMPLETE. 2 L 7 2 4F RT A2NM 2008011800019 20080118 00019 SO 2008 1 18 SIMA200801402 1 20080112 A 2120 14522285401 DUCT EMB 145 EMB145LR 3260212 SO CABIN DIST ODOR A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 622AE 145108 ON FLIGHT 3786 CREW DIVERTED TO MSY, FLIGHT ATTENDANT REPORTING PLASTIC BURNING ODOR AND GREY HAZE IN CABIN. NO WARNING MESSAGES OF ANY KIND. AIRCRAFT REMOVED FROM SERVICE. FOUND DUCT UNDER SEAT 7-8BC MELTED FROM NR 2 PACK. REMOVED AND R EPLACED SERVICEABLE NR 2 PACK INTAKE DUCT IAW AMM 21-20-05 UNDER SEAT 7-8BC.& 8194; AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022500348 20080225 00348 SO 2008 2 25 FDKA200802055 1 20080212 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FDM 6002 MCO (1115 PHX LCL). EMERGENCY EXIT LIGHT GALLEY EXIT INOP. MX OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008022500350 20080225 00350 EU 2008 2 25 USAA920080416 1 20080212 A 3350 321454 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 619AW 31428 4911 527 FLT 274 - PHX-IAH - EEL - EMERGENCY LIGHT TEST FAILS - EMERGENCY POWER SUPPLY UNIT ARMED/ON LEFT AFT. MAINTENANCE REMOV ED AND REPLACED THE LT AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008022500351 20080225 00351 NM 2008 2 25 BB08018 1 20080213 A 2782 5006397R ROTARY ACTUATOR BOEING 757 7572S7 1384962 NM L/E SLAT MALFUNCTIONED A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 905AW 41059 20718 23567 PHX FLT 432 EN ROUTE CLT TO PHX. DURING APPROACH, CREW RECEIVED "LE FLAP DISAGREE" MESSAGE ON EICAS, WHEN FLAPS WERE POSITIONED TO ONE. THE FLIGHT DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMB ER 2 SLAT ROTARY ACTUATOR. OPS CHECKED OK. 2 L 7 2 4F RT A2NM 2008022500352 20080225 00352 EU 2008 2 25 USAA920080375 1 20080124 A 5315 D53472193200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AW 543 SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3158 / FR 66 - BS 3366 / FR 70, -Y765. REPLACED CABIN FLOORBEAM, BS 3158 / FR 66 - BS 3366 / FR 70, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022500358 20080225 00358 EU 2008 2 25 USAA920080383 1 20080123 A 5321 D5367180500200 FLOOR PANEL AIRBUS 320 A320232 3930326 EU CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AW 543 SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON CABIN FLOOR PANEL 261 FF, BS 3158 / FR 66 - BS 3257 / FR 68, +Y1160. REPLA CED CABIN FLOOR PANEL 261 FF, BS 3158 / FR 66 - BS 3257 / FR 68, +Y1160 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022500361 20080225 00361 NM 2008 2 25 USAA920080414 1 20080203 A 5511 6547533513 RIB BOEING 737 7373S3 1384711 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - LEFT HORIZONTAL STABILIZER LEADING EDGE RIB WEB CRACKED, STABILIZER STATION 83. REPAIR ED LEFT HORIZONTAL STABILIZER LEADING EDGE RIB WEB, STABILIZER STATION 83 - 86.66 IAW USAIRWAYS EA 100234. 2 L 7 2 4F RT A16WE 2008022500364 20080225 00364 NM 2008 2 25 USAA920080419 1 20080206 A 5751 SKIN BOEING 737 7374B7 1384702 NM RT AILERON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q5 CHECK - RIGHT WING AILERON UPPER SKIN CRACKED. REPAIRED RIGHT WING AILERON UPPER SKIN IAW B737 SRM 57-70-17. 2 L 7 2 4F RT A16WE 2008022500368 20080225 00368 NM 2008 2 25 USAA920080423 1 20080209 A 5320 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 202UW 27811 BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT WEB ANGLE, BS 1661 - BS 1682, RBL 12. REPLACED CABIN FLOOR SUPPORT WEB ANGLE, BS 1661 - BS 1682, RBL 12 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008022500369 20080225 00369 NM 2008 2 25 USAA920080424 1 20080209 A 5320 FITTING BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 202UW 27811 BFM - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT PRESSURE PLATE TIE DOWN FITTING, BS 1681. REPL ACED CABIN FLOOR SUPPORT PRESSURE PLATE TIE DOWN FITTING, BS 1681 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008022500372 20080225 00372 NM 2008 2 25 USAA920080427 1 20080213 A 5347 SEAT TRACK BOEING 767 7672B7ER 1385107 NM BS 347-522 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AY 26847 MIA - MAJOR REPAIR - C4 CHECK - CORROSION ON CABIN SEAT TRACK, BS 347, RBL 86. REPLACED SEAT TRACK BS, 347 - BS 522, RB L 86. 2 L 7 2 4F RT A1NM 2008022500376 20080225 00376 NM 2008 2 25 USAA920080432 1 20080112 A 5743 65C365451 FITTING BOEING 737 7373S3 1384711 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 MCN - MAJOR REPAIR - C20 CHECK - LEFT WING LANDING GEAR SUPPORT FITTING CRACKED, RSS 224.14. REPLACED LEFT WING LANDING GEAR FITTING, RSS 224.14 IAW USAIRWAYS EA 100196. 2 L 7 2 4F RT A16WE 2008022500391 20080225 00391 NM 2008 2 25 BB08019 1 20080217 A 2782 5006397R ROTARY ACTUATOR BOEING 757 7572S7 1384962 NM L/E SLAT BINDING A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 906AW 80358 19438 23568 PHX - FLT 653 - EN ROUTE SNA TO PHX. DURING APPROACH, RECEIVED SLAT DISAGREE MESSAGE WHEN THE FLAPS WERE SELECTED TO 1 DEGREE. COMPLIED WITH APPROPRIATE PROCEDURES. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT WING, NR 3 LEADING EDGE SLAT ROTARY ACTUATOR. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 2008022500392 20080225 00392 EU 2008 2 25 BA08007 1 20080218 A 3040 A5398117400200 ATTACH FITTING AIRBUS 330 A330323 3930335 EU EVAC SLIDE DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 276AY 0375 CWF - FOUND AFT HEATER, FIN 4DH, INOPERATIVE. MAINTENANCE REPLACED 4DH AFT HEATED SLIDE ATTACHMENT FITTINGS. OPERATION ALLY CHECKS OK. 2 L 7 2 4F RT A46NM 2008022500395 20080225 00395 EU 2008 2 25 BA08008 1 20080219 A 3040 A5398117400200 ATTACH FITTING AIRBUS 330 A330323 3930335 EU L3 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 276AY 0375 CWF - MAINTENANCE FOUND THE FORWARD HEATER, FIN 15DH, FOR THE L3 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE 15DH FORWARD HEATER GIRT BAR ATTACH FITTING PER MM 30-46-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A46NM 2008022600001 20080226 00001 2008 2 26 ASAA0852541 4 20080207 A 2310 8220990004 HF COMM BOEING 737 737890 1384527 NM NR 2 MALFUNCTIONED A ASAA K NONE O OTHER NR NOT REPORTED 1 NM 02 558AS 35177 BOTH HF2 RADIOS WILL NOT GO INTO DATA MODE. UNABLE TO DUPLICATE. NR 2 HF DATA MODE OPS NORMAL (REF 23 27 00), NR 2 HF OPS NORMAL (REF 23 11 00). 2 L 7 2 4F RT A16WE 2008022600016 20080226 00016 NM 2008 2 26 ASAA0852544 1 20080210 A 2611 4735975 SMOKE DETECTOR BOEING 737 737890 1384527 NM CARGO BAY FALSE ACTIVATION A ASAA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 NM 02 587AS 35684 ON GROUND AT GATE WITH FWD CARGO PIT EMPTY THE FWD CARGO FIRE LIGHT & BELL ILLUMINATED SOUNDED. CONDITION RECURS AFTER SILENCING BELL LIGHT. BOTH A&B LOOPS TEST OK. UNABLE TO DUPLICATE DISCREPANCY. CLEANED ALL FWD CARGO PIT SMOKE DETECT ORS PRECAUTIONARY. OP CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2008022600036 20080226 00036 WP 2008 2 26 DHLA200800009 1 20080125 A 2612 8989880250 FIRE DETECTOR DOUG DC8 DC873F 302199F WP NR 1 NACELLE MALFUNCTIONED A DHLA O OTHER N FALSE WARNING DE DESCENT 1 GL 05 806DH 5 5 46002 FLT 160, DURING START OF DESCENT, NR 1 ENG FIRE WARNING LIGHT ILLUMINATED AND WARNING BELL ACTIVATED INTERMITTENTLY FOR 5 SECS IN DESENT "A LOOP' PER MEL 26-2-3 CAT C MDDR NR 31535 PLACARD INSTALLED, S/P COMPLIED WITH M/M 26-10-0. R7R FIRE DETECTOR CONTROL BOX UNIT IAW 26-10-4 TESTING SYSTEM OK DMI 31535 CLEARED. AIRCRAFT WAS GROUNDED. 2 L 7 4 4F RT 4A25 2008022600044 20080226 00044 NM 2008 2 26 DLM90080239 1 20080218 A 5313 593666711 LONGERON DOUG MD90 MD9030 3023690 NM BS 1344-1364 L29 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 AFT CARGO BAY LONGERON 29R BETWEEN STA 1344 AND 1364 CORRODED. REMOVED AND REPLACED CORRODED LONGERON SECTION, IAW MD90 SRM 51-30-01, 51-30-05 AND 53-10-01 FIG 7. 2 L 7 2 4F RT A6WE 2008022600046 20080226 00046 NM 2008 2 26 DLM90080229 1 20080218 A 5311 5930584121 FRAME DOUG MD90 MD9030 3023690 NM BS 1003 CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 LEFT MAIN LANDING GEAR BAY FORWARD FRAME CHAFED FS 1003 LBL36. REMOVED AND REPLACED INBOARD FORWARD FRAME, IAW MD90 SRM 51-30-02 AND 51-30-05. 2 L 7 2 4F RT A6WE 2008022600047 20080226 00047 NM 2008 2 26 AALA200800320 1 20080215 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 633AA 24591 MIA - EMERGENCY LIGHT AT SEAT 15D INOPERATIVE. RESECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008022600051 20080226 00051 NM 2008 2 26 ASAA0852547 1 20080212 A 3610 32145525 SHUTOFF VALVE BOEING 737 737890 1384527 NM BEED AIR SYS MALFUNCTIONED A ASAA K NONE O OTHER CL CLIMB 1 NM 02 579AS 35187 LEFT DUCT PRESSURE INDICATOR FLUCTUATED DURING CLIMBOUT AT 3 SECOND INTERVALS. INITIALLY 35 PSI TO 55 PSI, ABOVE 10 000 ' 35 PSI TO 50 PSI. FLUCTUATION QUIT APPROACHING FL190. BOTH INDICATORS FLUCTUATED TOGETHER THEN SETTLED OUT. PERFORM ED NR 1 ENGINE BLEED AIR REGULATOR AND PRSOV HEALTH CHECK. PRSOV FAILS HEALTH CHECK. REPLACED PRSOV & BLEED AIR REGULA TOR. OP CHECKED BLEED AIR CONTROL SYSTEM. OP CHECKS OK NO FLUCTUATIONS OR ABNORMAL INDICATIONS. 2 L 7 2 4F RT A16WE 2008022600052 20080226 00052 NM 2008 2 26 AALA200800328 1 20080215 A 2120 UNKNOWN BOEING 757 757223 1384957 NM LAVATORY SMOKE A AALA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 660AM 25294 EWR INFLIGHT T164/15FEB - CREW REPORTS MID LAVATORY SMOKE DETECTORS ACTIVATED FOLLOWED BY SMOKE AND ODOR IN CABIN. LAND ED EWR WITHOUT INCIDENT. REPLACED SMOKE DETECTOR IN MID LAVATORY. AIRCRAFT FERRIED TO TUL FOR FURTHER EVALUATION AND R EPAIRS. 2 L 7 2 4F RT A2NM 2008022600054 20080226 00054 NM 2008 2 26 ASAA0842557 1 20080117 A 5311 654795928 FRAME BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT CORROSION ON BS 794 FRAME BETWEEN STR 25R AND 26R. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008031700147 20080317 00147 EU 2008 3 17 AALA200800475 1 20080302 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 MIA - EMERGENCY LIGHTS AT SEAT ROWS 7C TO 18C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 7C T O 18C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008031700149 20080317 00149 NM 2008 3 17 AALA200800476 1 20080302 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW - EMERGENCY LIGHT BATTERY PACK FOR LEFT NUMBER DOOR EMERGENCY EXIT LIGHT FAILED FUNCTIONAL TEST. REPLACED BATTERY P ACK M33400 FOR EMERGENCY LIGHTS AT LEFT NUMBER THREE DOOR EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031700152 20080317 00152 NM 2008 3 17 AALA200800464 1 20080302 A 3350 SIGN BOEING 767 767323 1385205 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 381AN 25450 MIA - BI DIRECTIONAL EMERGENCY EXIT IDENTIFIER FORWARD OF SEAT 20G IS BROKEN. REPLACED BI DIRECTIONAL EMERGENCY EXIT SI GN ASSEMBLY FORWARD OF SEAT 20G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008031700153 20080317 00153 EU 2008 3 17 AALA200800465 1 20080302 A 3350 LENS AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70072 515 JFK - EMERGENCY LIGHT AT SEAT 19G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 19G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008031700154 20080317 00154 EU 2008 3 17 AALA200800467 1 20080302 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70072 515 JFK EMERGENCY LIGHT AT SEAT 29G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 29G. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A35EU 2008031700158 20080317 00158 EU 2008 3 17 F3LA200800086 1 20080229 A 5320 WEB AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED SHEARED RIVETS WERE FOUND IN THE RIGHT SUPPORT WEB, LOCATED BETWEEN FRAMES 68 AND 69, WHERE IT CONNECTS TO STRINGER Y1292. MAINTENANCE INSTALLED NEW LOCK FASTENER IN ACCORDANCE WITH THE REQUIREMENT S OF A319 SRM 51-42-11, PARAGRAPH 7 AND EA A9-53R-30090. FOLLOWING COMPLETION OF THE INSTALLATION, THE LOCK FASTENER WE RE INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008031700162 20080317 00162 NM 2008 3 17 HALA0800369 1 20080308 A 2430 SM135B2 RELAY BOEING 717 717200 1383700 NM EMERGENCY POWER FAILED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 475HA 55121 EMERGENCY POWER TEST FAILED. REMOVED AND REPLACED EMERGENCY POWER RELAY, OPS CHECK OK IAW BOEING AMM 24-24-00. 2 L 7 2 4F TR A6WE 2008031700165 20080317 00165 NM 2008 3 17 SWAA081340 1 20080310 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031700170 20080317 00170 2008 3 17 SWAA081326 4 20080310 A 2565 D31354 SLIDE BOEING 737 7373TO 138447G NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031700181 20080317 00181 NM 2008 3 17 HALA0800377 1 20080305 A 5320 SUPPORT BEAM BOEING 767 767332 1382001 NM BS 654 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 FWD CARGO BAY RT SIDE REAR OF CARGO DOOR AT ST 654 SIDE PANEL, ATTACHMENT BEAM CRACKED AT UPPER ANGLE BY HOLE. CARRIED OUT REPAIRS TO SUPPORT BEAM IAW 767-300 SRM 51-70-11, FIG 1. FABRICATED REPAIR PARTS IAW 767-300 SRM 51-20-11,FIG 1. A PPLIED ALODINE 1200 TO REPAIR PARTS AND PRIMED WITH BMS 10-11 TYPE 1, PRIMED IAW 767-300 SRM 51-20-01. INSTALLED REPAIR PARTS IAW 767-300 SRM 51-70-11, FIG 1. 2 L 7 2 4F RT A1NM 2008031700182 20080317 00182 NM 2008 3 17 HALA0800378 1 20080305 A 5320 SUPPORT BEAM BOEING 767 767332 1382001 NM BS 500 CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 FWD CARGO BAY RH SIDE FWD OF CARGO BAY DOOR AT ST 500 SIDE PANEL ATTACHMENT BEAM CRACKED AT UPPER ANGLE, BRACKET THROUGH HOLE. CARRIED OUT REPAIRS TO SUPPORT ANGLE IAW 767-300 SRM 51-70-11, FIG 1. FABRICATED REPAIR PARTS IAW 767-33 SRM 51 -70-11, FIG 1. APPLIED ALODINE 1200 TO REPAIR PARTS AND PRIME WITH BMS 10-11,TYPE 1, IAW 767300 SRM 51-20-01. INSTALLE D REPAIR PARTS IAW 767-300 SRM 51-70-11, FIG 1. 2 L 7 2 4F RT A1NM 2008031700186 20080317 00186 NM 2008 3 17 HALA0800371 1 20080309 A 5420 ACOUSTIC LINER BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 478HA 55123 ACOUSTIC LINER DAMAGE OK TO CONTINUE PER M105 FILE NR 478112. REPAIR PER AMM 72-34-01, NO LATER THAN 3/31/08. OK TO CO NTINUE PER GMM4-3.1 2 L 7 2 4F 4 F TR A6WE E00061EN 2008031700188 20080317 00188 NM 2008 3 17 HALA0800376 1 20080306 A 5754 SKIN BOEING 767 767332 1382001 NM NR 1 SLAT DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 NR 1 SLAT HAS MINOR DAMAGE TO UPPER LEADING EDGE. BLENDED MINOR DAMAGE, MAX DEPTH OF REWORK AREA IS 0.0065", WITHIN LIM ITS AS PER SRM 57-43-01, FIG 10, NOTE B, DETAIL 1V. SURFACE FINISH RESTORED IAW AMM 51-21-06. 2 L 7 2 4F RT A1NM 2008031700189 20080317 00189 SO 2008 3 17 C2XA08ON100 1 20080310 A 2611 14534156401 BUTTON EMB 145 EMB145LR 3260212 SO COCKPIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14907 15730 15730 145468 FLT 0429 - SAN - BAGGAGE SMOKE DID NOT TEST WHILE PERFORMING OPS CHECKS. MX PERSONNEL REMOVED AND REPLACED TEST PUSH BU TTON FROM THE FIRE EXTINGUISHER APU/BAG MODULE IN THE OVERHEAD PANEL. OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008031700196 20080317 00196 NM 2008 3 17 SWAA081353 1 20080311 A 2761 65671795 LUG BOEING 737 7375H4 138449D NM NR 5 SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED C4 CHECK, FOUND RT WING NR 5 GROUND SPOILER ACTUATOR LUG CRACKED. REPAIRED ACTUATOR PER SWA EA. 2 L 7 2 4F RT A16WE 2008022600058 20080226 00058 SO 2008 2 26 FDKA200802065 1 20080217 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6195 ATL. FWD CABIN EMERGENCY LIGHT OUT. MX OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008022600060 20080226 00060 SO 2008 2 26 FDKA200802067 1 20080217 A 2611 SMOKE WARNING EMB 145 EMB145LR 3260212 SO CARGO BAY MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 838MJ 145384 FDM 6192 BOS-JFK. BAG SMOKE WARNING IN FLIGHT. MX PERFORMED OPS CHECK AND NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008022600061 20080226 00061 NM 2008 2 26 USAA920080435 1 20080217 A 5330 6552988 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q5 CHECK - CRACKED FUSELAGE SKIN, BS 947.5, S24L. REPAIRED FUSELAGE SKIN, BS 947.5, S24L IAW USAIR WAYS EA 100250. 2 L 7 2 4F RT A16WE 2008022500051 20080225 00051 NM 2008 2 25 2008UALA00773 1 20080207 A 3350 3071BPEGPL LAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 791UA 26933 EEL LIGHTS INOP MID GALLEY RT SIDE. RELAMPED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008022500052 20080225 00052 2008 2 25 2008UALA00774 4 20080208 A 2565 CYLINDER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EVAC SLIDE DEFECTIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 665UA 29237 LEFT OVERWING SLIDE CABLE BALL IS BELOW RETAINER SPRING ON INFLATION CYLINDER. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022500203 20080225 00203 NM 2008 2 25 2008UALA00796 1 20080211 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FWD GALLEY DOOR, AFT FRAME STOP PIN FITTING CUTOUT CRACKED, 4TH FROM TOP. MAJOR REPAIR: INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022500211 20080225 00211 NM 2008 2 25 2008UALA00804 1 20080212 A 3350 582233 BATTERY BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 SEVERAL EEL LAMPS INOP NEAR DOOR 4L. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022500213 20080225 00213 NM 2008 2 25 2008UALA00806 1 20080211 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EEL INOP: SEAT 54H. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022500247 20080225 00247 NM 2008 2 25 HNAA0800083 1 20080212 A 2150 ACM DHAV DHC8 DHC8102 2809003 NM A/C BAY MALFUNCTIONED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 941HA 161 ACM MAKING LOUD NOISES AND EMITTING BURNT OIL SMELL IN CABIN & FLIGHT DECK. 2 H 7 2 4T RT A13NM 2008022500290 20080225 00290 NM 2008 2 25 AALA200800306 1 20080212 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 696AN 26976 MIA - EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RIGH T NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008022500294 20080225 00294 NM 2008 2 25 AALA200800292 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 39C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 39C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022500331 20080225 00331 NM 2008 2 25 USAA920080398 1 20080209 A 5330 6545774 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 23634 PHX - MAJOR REPAIR - RON - CRACKED FUSELAGE SKIN, BS 770, S23L. REPAIRED FUSELAGE SKIN, BS 770, S23L IAW B737 SRM 53-00 -01-2R-31. 2 L 7 2 4F RT A16WE 2008022500356 20080225 00356 EU 2008 2 25 USAA920080380 1 20080129 A 5320 D53480048202 FITTING AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AW 543 SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON THE L2 DOOR CUTOUT LOWER CENTER SHAPE SILL FITTING, BS 3257 /FR 68, S23L. REPLACED THE L2 DOOR CUTOUT LOWER CENTER SHAPE SILL FITTING, BS 3257 / FR 68, S23L IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022500362 20080225 00362 NM 2008 2 25 USAA920080417 1 20080206 A 5754 65C26601107 WEDGE BOEING 737 7374B7 1384702 NM L/E SLAT DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - Q5 CHECK - LEFT WING NR 1 SLAT TRAILING EDGE WEDGE HAS AREA OF DISBOND. REPAIRED LEFT WING NR 1 SL AT TRAILING EDGE WEDGE IAW B737 SRM 57-70-10. 2 L 7 2 4F RT A16WE 2008022500386 20080225 00386 SO 2008 2 25 FDKA200802062 1 20080214 A 5350 ATTACH ANGLE EMB 145 EMB145LR 3260212 SO FAIRING CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 THE ATTACH ANGLE FOR THE LT WING TO FUSELAGE FAIRING IS CRACKED, JUST AFT OF THE CENTER WING. THE DAMAGE HAS BEEN REPAI RED. 2 L 7 2 4T RT T00011AT 2008031700198 20080317 00198 NM 2008 3 17 SWAA081351 1 20080311 A 5753 6546430190 FLAP BOEING 737 7375H4 138449D NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2008031700199 20080317 00199 NM 2008 3 17 SWAA081350 1 20080311 A 5230 6549889 SKIN BOEING 737 7375H4 138449D NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008031700201 20080317 00201 SO 2008 3 17 C2XA08SH047 1 20080313 A 5320 14530642401 FLOOR SUPPORT EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12528 145504 SHV - DURING C-CHECK LT OMEGA BEAM HAS VARIOUS AREAS OF CORROSION AT FR24-28. MX REPAIRED FR 24-28 IAW EMB145 53-00-10 FIG 202. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2008031700203 20080317 00203 EA 2008 3 17 VNAA0802015 1 20080223 A 5244 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE COMM OPEN A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 05 247JS 7922 CREW REPORTED A NOISE FROM THE FRONT THE AIRCRAFT AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCID ENT. MAINTENANCE INSPECTED AND FOUND THE COMM DOOR OPEN. MAINTENANCE SECURED DOOR CLOSED AND FOUND NO DEFECTS OR DAMAG E. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008031700208 20080317 00208 WP 2008 3 17 ABXR080080 1 20080214 A 5531 9911824501 RIB DOUG DC9 DC933F 302207A WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 RIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERTICAL STAB LEADING EDGE ZFS 74. REPAIRED LEFT AND RIGHT RIBS IAW DC 9 SSRM K05159. 2 L 7 2 4F A6WE 2008031700213 20080317 00213 WP 2008 3 17 ABXR080068 1 20080205 A 5320 9957913501 STRUCTURE DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 STRUCTURE UNDER FORWARD LOWER CARGO DOOR AFT ATTACH POINT AS SEEN THROUGH LIGHTENING HOLE WAS CRACKED. REPAIRED IAW REA D953-57015-MR. 2 L 7 2 4F A6WE 2008031700215 20080317 00215 WP 2008 3 17 ABXR080070 1 20080205 A 5280 5910161116 DOOR DOUG DC9 DC933F 302207A WP RT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 RIGHT MAIN LANDING GEAR INBOARD DOOR CRACKED, UPPER AFT CORNER. REPAIRED CRACKED AREA IAW DC9 REA D952-57026. 2 L 7 2 4F A6WE 2008031700216 20080317 00216 WP 2008 3 17 ABXR080071 1 20080206 A 5230 59101575 REPAIR DOUG DC9 DC933F 302207A WP AFT CARGO DOOR DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 AFT LOWER CARGO DOOR INNER PAN REPAIR AT THE AFT LOCK REQUIRED EVAL IAW AD 2006-10-14. REMOVED AND REPAIRED AREA IAW DC 9 SRM 52-05, FIG 26B, 51-30-5, 51-30-2, AND ST-6244-03. 2 L 7 2 4F A6WE 2008031700220 20080317 00220 WP 2008 3 17 ABXR080075 1 20080214 A 5531 991188512 RIB DOUG DC9 DC933F 302207A WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 RIB CRACKED AT FASTENER RIGHT SIDE OF VERTICAL STAB LEADING EDGE ZFS 23. REPAIRED IAW DC9 SSRM DWG K05159. 2 L 7 2 4F A6WE 2008031700223 20080317 00223 WP 2008 3 17 ABXR080078 1 20080214 A 5531 991188111 RIB DOUG DC9 DC933F 302207A WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 RIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERTICAL STAB LEADING EDGE ZFS 50. REPAIRED IAW DC9 SSRM DWG K05159. 2 L 7 2 4F A6WE 2008031700224 20080317 00224 WP 2008 3 17 ABXR080081 1 20080214 A 5531 99118315 RIB DOUG DC9 DC933F 302207A WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 RIB CRACKED AT FASTENER LEFT SIDE OF VERTICAL STAB LEADING EDGE XFS 148. REPAIRED IAW DC9 SSRM DWG K05159. 2 L 7 2 4F A6WE 2008031700226 20080317 00226 SO 2008 3 17 C2XA08ON096 1 20080228 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16559 5585 5585 145603 FLT 0024 - ONT - WHILE PERFORMING EMERGENCY LIGHT OPERATIONAL CHECK, MX PERSONNEL FOUND BATTERY NR 4 (AFT) INOP. MX PER SONNEL REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO R ETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008031700230 20080317 00230 SO 2008 3 17 C2XA08CL024 1 20080303 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145EP 3260221 SO NLG FAULTY A C2XA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 27 14945 145049 YQB FLIGHT 3072 - THE CREW REPORTED AFTER TAKEOFF A LOUD CLUNK ALONG WITH VIBRATION FELT IN FLIGHT CONTROLS. MAINTENANC E INSPECTED AND FOUND THE NOSE GEAR UPLOCK PROXIMITY SWITCH "A" OPEN. THE PROXIMITY SWITCH WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2008031700232 20080317 00232 SO 2008 3 17 C2XA08RI027 1 20080228 A 3260 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A C2XA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SW 27 13979 145181 FLIGHT 2142 - MKE - CREW REPORTED LANDING GEAR AIR/GRND FAIL MESSAGE ON EICAS. AIR/GRND C/B WAS RESET AND MESSAGE WAS C LEARED ON EICAS. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008031700234 20080317 00234 WP 2008 3 17 ABXR080086 1 20080214 A 5531 991188612 RIB DOUG DC9 DC933F 302207A WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 RIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERT STAB LEADING EDGE ZFS 18. REPAIRED IAW DC9 SSRM DWG K05159. 2 L 7 2 4F A6WE 2008031700235 20080317 00235 WP 2008 3 17 ABXA080088 1 20080303 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 949AX 47325 EMERGENCY LIGHTS WILL NOT ILLUMINATE WITH SWITCH IN THE 'ON' POSITION. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00-8. 2 L 7 2 4F A6WE 2008031700238 20080317 00238 NM 2008 3 17 ZZDA2008078 1 20080209 A 5311 FRAME BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 920AT 55083 CRACK NOTICED AFT FUSELAGE INT LEFT CANTED FRAME AREA STA 1178.225 BELOW L16L AFT OF HYD S/O VALVE. INSTALLED ANGLE REP AIR AT LEFT CANTED FRAME STA 1178.225 BELOW L161L, AFT OF HYD S/O VALVE IAW B717 SRM 51-70-11 FIG 201 REPAIR 1. MATERIA L USED 7075-0 .080 SIZE 11" X 21.2". HEAT TREATED FROM 0 TO T6 IAW AVBORNE HEAVY MAINTENANCE, GENERAL PROCESS SPEC 98PM S.24PS-01. 2 L 7 2 4F TR A6WE 2008031700240 20080317 00240 SO 2008 3 17 C2XA08SH045 1 20080313 A 5751 145690009610 ATTACH FITTING EMB 135 EMB135LR 3260305 SO RT AILERON DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12528 145504 SHV - DURING C-CHECK RIGHT AILERON TO PCA BRACKET HAS AN ELONGATED BUSHING HOUSING. MX REMOVED AND REPLACED RIGHT AILER ON TO PCA FITTING IAW EC5750-01177. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2008031300352 20080313 00352 NM 2008 3 13 SWAA081203 1 20080303 A 5311 6546548 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300369 20080313 00369 NM 2008 3 13 SWAA081257 1 20080305 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300373 20080313 00373 2008 3 13 SWAA081250 4 20080305 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031300381 20080313 00381 NM 2008 3 13 SWAA081255 1 20080305 A 5315 6546811 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, LBL 7 TO RBL 15. REPAIRED CHORD PER ER. 2 L 7 2 4F RT A16WE 2008031300391 20080313 00391 NM 2008 3 13 ASAA0872703 1 20080131 A 5754 114A80212 SKIN BOEING 737 737790 13844CN NM L/E SLAT CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 612AS 30162 NR 7 LEADING EDGE SLAT HAS 1, 4 INCH CRACK ADJACENT TO ACTUATOR MOUNT FASTENER. SLAT SKIN REPAIR COMPLETED. 2 L 7 2 4F RT A16WE 2008031300400 20080313 00400 EU 2008 3 13 08FDEA00761 1 20080306 A 5420 2210081511 FAIRING AIRBUS 310 A310324 3930206 EU NR 1 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 NR 1 ENGINE AFT PYLON FAIRING; AFT WELDED SKIN IS CRACKED. STOP DRILLED THE CRACK IAW SRM 54-55-51 FIG 201.FABRICATED R EPAIR IAW SRM 54-55-51 FIG 201 & EA 06-5480-118441. INSTALLED REPAIR IAW SRM 54-55-51 FIG 201 & EA 06-5480-118441. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008031300404 20080313 00404 EU 2008 3 13 08FDEA00767 1 20080306 A 5312 BULKHEAD AIRBUS 310 A310203 3930313 EU MLG WW DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 MAIN WHEEL WELL FWD BULKHEAD PANEL NR 147 CZ HAS SEVERAL RETAINER BRACKETS THAT HAVE WORN PIP PIN HOLES. 2 L 7 2 4F RT A35EU 2008031300418 20080313 00418 EU 2008 3 13 08FDEA00792 1 20080307 A 5347 A5327400500053 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 MAIN CABIN SEAT TRACK IS BROKEN BETWEEN STA 60 AND 61, RBL 77. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 101. REM OVED SEAT TRACK SECTION IAW SRM 51-40-21 PARA 7. FABRICATED NEW SEAT TRACK SECTION REF SRM 53-51-16 FIG 203. LOCATED & DRILLED NEW SEAT TRACK SECTION IAW SRM 51-40-44 PARA 2. ALODINED SEAT TRACK IAW SRM 51-21-10 PARA 2. PRIMED & PAINTED SEAT TRACK IAW SRM 51-23-10 PARA 1. INSTALLED SEAT TRACK SECTION IAW SRM 51-40-21 PARA 7. MAJOR REPAIR. 2 L 7 2 4F RT A35EU 2008031400002 20080314 00002 NM 2008 3 14 TSAA0827010 1 20080301 A 2750 18173810 TRANSMITTER BOEING 737 73776N 13844CH NM TE FLAPS INTERMITTENT A TSAA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 WP 13 746AL 29905 FLIGHT 486 LIH-SNA - DURING APPROACH, WHEN THE CREW ATTEMPTED TO EXTEND THE FLAPS, THE LEADING EDGE TRANSIT WARNING LIGH T ILLUMINATED AND THE TRAILING EDGE FLAPS LOCKED-OUT BEFORE FLAPS 1 WITH A SPLIT INDICATION ON THE FLAP GAUGE. THE CREW ELECTED TO DIVERT TO ONT DUE TO SNA AIRPORT RESTRICTIONS. THE CREW SELECTED ALTERNATE EXTENSION FOR THE FLAPS BUT THEY REMAINED LOCKED-OUT BEFORE FLAPS 1. THE CREW LANDED IN ONT WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED A BITE CHE CK OF THE FLAP SLAT ELECTRONICS UNIT PER AIRCRAFT FIM 27-51-00-810-801 AND FOUND INTERMITTENT FAULT 27-52260. THE RIGHT TRAILING EDGE FLAP POSITION TRANSMITTER DISAGREED WITH THE LEFT TRAILING EDGE FLAP POSITION TRANSMITTER. AS A PRECAUTI 2 L 7 2 4F RT A16WE 2008031400014 20080314 00014 NM 2008 3 14 QXEA200800262 1 20080227 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - MCD THRESHOLD FLOOR SUPPORT STRUCTURE FRAME CASTELLATION IS CORRODED (STATION X27.4.0, Z95.0, Y38). REMOVED FRAME AND INSTALLED NEW FRAME IAW DASH 8 Q400 SRM 51-40-07, 51-42-05 AND 51-25-15. 2 H 7 2 4T RT A13NM 2008031400055 20080314 00055 NM 2008 3 14 CALA0800208 1 20080306 A 5311 6546549 FRAME BOEING 737 737524 1384721 NM BS 867 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 FRAME CRACKED STA 867 ABOVE S9L. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A. 2 L 7 2 4F RT A16WE 2008031400067 20080314 00067 WP 2008 3 14 AALA200800455 1 20080229 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 494AA 49732 LGA - EMERGENCY LIGHTS AT SEAT ROW 20 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROW 20. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031700020 20080317 00020 NM 2008 3 17 2008UALA01268 1 20080306 A 2612 FIRE LOOP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CARGO BAY NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 651UA 25389 FOUND CARGO FIRE TEST FAILED CARGO FWD HEAT INHIBIT. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031700050 20080317 00050 NE 2008 3 17 08FDEA00800 2 20080309 A 7200 ENGINE AIRBUS 310 A310203 3930313 EU GE CF6 CF680A3 30025 NE NR 1 VIBRATION A FDEA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 25 423FE 35330 35330 281 CLIMBING THROUGH FL 320 TO FL 350 WITH ALL CONDITION NORMAL, ACFT SHUDDERED AND SWERVED SLIGHTLY, THEN BEGAN CONTINUOUS THUMPS, BOTH AUDIBLE AND CLEARLY FELT THROUGH AIRFRAME. THERE WERE NO ECAM ADVISORIES, BUT NR 1 ENGINE N1 DECREASED TO APPROX 60 PERCENT. BROUGHT NR 1 THROTTLE TO IDLE AND THUMPS STOPPED. STILL NO OBVIOUS INSTRUMENT INDICATIONS AND NO VI BRATION INDICATION ON ECAM ENGINE PAGE. ADVANCED THROTTLE SLIGHTLY AND GOT IMMEDIATE RETURN OF VIBRATIONS. SHUT DOWN E NGINE, DECLARED EMERGENCY, AND DIVERTED. R&R NR 1 ENGINE IAW WORK CARD 44T0701-1, OPS CHECK NORMAL IAW WORK CARD 44T 0701-1. 2 L 7 2 4F 4 F RT A35EU E13NE 2008031700053 20080317 00053 NM 2008 3 17 SWAA081334 1 20080310 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 5 TO RBL 46. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2008031700067 20080317 00067 NM 2008 3 17 SWAA081281 1 20080307 A 5610 5717623122 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 349SW 24408 FLIGHT DECK R2 WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2008031700092 20080317 00092 NM 2008 3 17 SWAA081290 1 20080307 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008031700107 20080317 00107 EU 2008 3 17 08FDEA00829 1 20080310 A 5330 A53879301200000 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT SIDE FUSELAGE SKIN HAS CORROSION AROUND THE WING TO BODY FAIRING MOUNT AREA BETWEEN FRAME 45 AND FRAME 46. REMOVED CO RROSION IAW SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM 53-10-12; PAGE 139. ALODINED AREA IAW SRM 51-21-10. PRIMED & TOP COAT PAINTED BOTH IAW SRM 51-23-10. MINOR REPAIR 2 L 7 2 4F RT A35EU 2008031700117 20080317 00117 NM 2008 3 17 SWAA081297 1 20080309 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER 4R CRACKED AT BS 910. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008031700118 20080317 00118 NM 2008 3 17 SWAA081298 1 20080308 A 5755 654645258 SPOILER BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED MV1 CHECK, FOUND RT WING NR 5 SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2008031700157 20080317 00157 EU 2008 3 17 AALA200800466 1 20080302 A 3350 LENS AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70072 515 JFK - EMERGENCY LIGHT AT SEAT 23G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008031700166 20080317 00166 NM 2008 3 17 SWAA081341 1 20080310 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031700167 20080317 00167 NM 2008 3 17 SWAA081324 1 20080310 A 5312 6546568 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6R. REPAIRED WEB PER ER. 2 L 7 2 4F RT A16WE 2008031700169 20080317 00169 2008 3 17 SWAA081325 4 20080310 A 2565 D31354 SLIDE BOEING 737 7373TO 138447G NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPL ACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031700179 20080317 00179 NM 2008 3 17 SWAA081304 1 20080308 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 768SW 30587 L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008031700190 20080317 00190 NM 2008 3 17 SWAA081347 1 20080311 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 216WR 32488 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 12 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008031700191 20080317 00191 NM 2008 3 17 SWAA081357 1 20080311 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2008031700194 20080317 00194 2008 3 17 SWAA081348 4 20080311 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008022600048 20080226 00048 NM 2008 2 26 AALA200800331 1 20080131 A 5330 SKIN BOEING 767 767223 1385123 NM BS 412-434 S37L CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 324AA 22325 AFW - FUSELAGE SKIN HAS CORROSION ON INNER SURFACE AT STATION 412 TO 434 UNDER S37L. BLENDED OUT CORROSION USING A MINI MUM TAPER RATIO OF 20 TO 1. VISUALLY CONFIRMED NO FURTHER CORROSION. PERFORMED HIGH FREQUENCY EDDY CURRENT ON BLENDED AREAS AND HOLES SURROUNDING BLENDS. TREATED BLENDED AREAS WITH ALODINE AND TWO COATS PRIMER AND FILLED WITH BMS595 SEAL ANT. 2 L 7 2 4F RT A1NM 2008022600049 20080226 00049 NM 2008 2 26 ASAA0852546 1 20080205 A 5320 111A73022 STIFFENER BOEING 737 737890 1384527 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 564AS 35103 DRILL START MARK ON STIFFENER ANGLE IN AIR CON BAY AT BS 663 RBL 40. REPLACED IAW EA5310 02768. 2 L 7 2 4F RT A16WE 2008022600057 20080226 00057 SO 2008 2 26 FDKA200802064 1 20080217 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 FDM 6198 JFK. GALLEY/SERVICE DOOR EMERGENCY EXIT LIGHT OUT. MX RESECURED LOOSE CONNECTOR, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008022600065 20080226 00065 EU 2008 2 26 USAA920080448 1 20080218 A 5330 D53480022213 SKIN AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AW 543 SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON FUSELAGE EXTERNAL SKIN, BS 3310 / FR 69 - BS 3366 / FR 70, S31R - S32R AROU ND THE OVERBOARD VENT. REPAIRED FUSELAGE EXTERNAL SKIN, BS 3310 / FR 69 - BS 3366 / FR 70, S31R - S32R AROUND THE OVERB OARD VENT IAW A320 SRM 53-41-11. 2 L 7 2 4F RT A28NM 2008022600070 20080226 00070 2008 2 26 ASAA0852593 4 20080215 A 2210 4082260939ASA CONTROL PANEL BOEING 737 737890 1384527 NM COCKPIT FAULTY A ASAA K NONE N FALSE WARNING UK UNKNOWN 1 NM 02 577AS 35186 N1 INDICATOR LIGHTS ON BOTTOM OF MCP ARE INOP. RELAMPED MCP GROUP 70 & INTERACTIVE TESTS PASSED. REPLACED DFC MODE CNT L PNL. PERFORMED "LAND VERIFY" AND HGS SYSTEM TESTS. NO DEFECTS. 2 L 7 2 4F RT A16WE 2008022600076 20080226 00076 NM 2008 2 26 ASAA0842601 1 20080117 A 5311 6545812172 FRAME BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 CORROSION ON BS 344 FRAME AT STR 28R CORROSION ON FRAME AT BS 344 STR L8R BLENDED OUT AND FOUND TO BE BEYOND LIMITS. RE PAIR PARTS MADE FROM 0.040" 707ST6 PDH 109 785 AND 0.050" 7075T6 PDH109785 AND 0.050" 7075 T6 PDH 11425 IAW B737 400 SRM 53 00 07 REPAIRS FIG 201 AND INSTALLED IAW B737 400 SRM 53 00 07 REPAIR 5 FIG 201. 2 L 7 2 4F RT A16WE 2008022600082 20080226 00082 NM 2008 2 26 AALA200800298 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022600094 20080226 00094 NM 2008 2 26 HALA0800249 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1197.95. REWORKED PER SRM 51-10-02 AND SRM 53-00-52/101. 2 L 7 2 4F RT A1NM 2008022600101 20080226 00101 NM 2008 2 26 2008UALA00755 1 20080209 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 38R INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY LIGHT LAMP INOP, SEAT 38R. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022600105 20080226 00105 NM 2008 2 26 ASAA0842575 1 20080106 A 5320 69412285 SUPPORT FITTING BOEING 737 7374S3 1384711 NM FUSELAGE CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 R2 DOOR CUTOUT CHAFING DAMAGE ON DOOR SILL SUPPORT FITTING AT BS 966 STR 17R. REPAIRED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008022600106 20080226 00106 NM 2008 2 26 2008UALA00758 1 20080211 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY LIGHT INOP, RT OVERWING FWD MOST ASSY FWD LAMP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022600109 20080226 00109 NM 2008 2 26 HALA0800231 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 855 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT LBL 11, STA 855, MAX DEPTH OF BLEND OUTS WAS 0.008". BLENDED IAW SRM 51-10 -02. ALL BLENDOUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022600111 20080226 00111 NM 2008 2 26 ASAA0842577 1 20080106 A 5320 654652848 ANGLE BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO PIT 'Z' ANGLE FOUND CORRODED AT BS 500 A TO 500 G RBL 24. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600113 20080226 00113 NM 2008 2 26 AALA200800293 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 40G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 40G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022600117 20080226 00117 NM 2008 2 26 ASAA0842584 1 20080115 A 5347 65C314838 SEAT TRACK BOEING 737 7374S3 1384711 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 SEAT TRACK GOUGED STA 727 B+4 "7" LBL 25. SEAT TRACK REPLACED. 2 L 7 2 4F RT A16WE 2008031700217 20080317 00217 WP 2008 3 17 ABXR080072 1 20080206 A 5311 591359577 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 FRAME CRACKED STA 1076, LONGERON 14 RIGHT. REPAIRED FRAME IAW DC9 SRM 53-03, FIG 32, SHEET 4. 2 L 7 2 4F A6WE 2008031700231 20080317 00231 SO 2008 3 17 C2XA08RI026 1 20080228 A 3230 355022002 CONTROL UNIT EMB 145 EMB145XR 3260214 SO E&E BAY DEFECTIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 25134 6263 145714 RIC - DURING A-CHECK, AIRCRAFT FAILED LANDING GEAR AIR-GROUND CHECK. RIC MX PERFORMED TROUBLESHOOTING AND FOUND LGEU NO T WORKING PROPERLY. MX REMOVED AND REPLACED LGEU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED T O RETURN TO SERVICE. 2 L 7 2 4F RT 2008031700241 20080317 00241 SO 2008 3 17 C2XA08SH046 1 20080313 A 5320 14521700007 REPAIR EMB 135 EMB135LR 3260305 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12528 145504 SHV - DURING C-CHECK LEFT OMEGA BEAM PREVIOUS REPAIRED AT FR 20 HAS CORROSION. MX REPAIRED LEFT OMEGA BEAM PREVIOUS REP AIRED IAW SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2008031700247 20080317 00247 CE 2008 3 17 JDWA2008SAF01 1 20080218 A 2400 RC20GF100J RESISTOR BEECH 99 99 1154002 CE PWA PT6 PT6A20 52043 EA HARTZL HCB3T HCB3TN3 GL COCKPIT BLOWN E JDWA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 09 118SF U32 20687 BUA27574 ON MONDAY THE 18TH OF FEBRUARY 2008, BEECH 99, N118SF, S/N U-32, SUBURBAN AIR FREIGHT POSITIONING FLIGHT, ROUTE NUMBER S UBAIR 13 OPERATING UNDER PART 91, DEPARTED OMAHA, NE EN ROUTE TO MOLINE, IL. AT APPROXIMATELY 20:30 HOURS JUST NORTH OF MUSCATINE, IA CENTER CLEARED THE FLIGHT FOR DESCENT OUT OF 9000 FT. PASSING THRU 8000 FT, THE PILOT SMELLED SMOKE AND AT THAT TIME THE PILOT NOTICED A GLOW COMING FROM INSIDE OF THE CENTER CONTROL COLUMN AND NOTICED A REFLECTION ON THE TO E OF HIS RIGHT SHOE. THE PILOT SHUT DOWN THE ELECTRICAL SYSTEMS AND PROCEEDED TO GET THE FIRE EXTINGUISHER OUT. FIRE E XTINGUISHER WAS NOT USED, AS THE GLOW AND THE SMOKE STOPPED. DECLARED AN EMERGENCY AND CONTINUED TO MOLINE, LANDED WITH 1 L 7 2 3T 3 T A14CE E4EA 6 C P15EA 2008031700248 20080317 00248 NM 2008 3 17 JJBA200857030 1 20080223 A 5320 PLATE DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 360PH 515 MECH WAS TRYING TO EASY-OUT A SCREW FROM LEFT LADDER PLATE (STATION 5711069, BETWEEN YW74.4 AND YW90.6 ON STRINGER 6) DR ILLED A HOLE INTO THE LADDER PLATE. PERMANENT REPAIR (RD 8-57-93) WAS COMPLIED WITH ON 23 FEB 2008, BY DOING A BUSHING REPAIR FOR THE DAMAGED HOLE. TO BE REINSPECTED BY STANDARD HIGH FREQUENCY EDDY CURRENT AT INTERVALS OF 8160 FLIGHTS. 2 H 7 2 4T RT A13NM 2008031700251 20080317 00251 EU 2008 3 17 BAQA20080002 1 20080124 A 6210 L621M1010222 BOLT UROCOP EC135 EC135P2 5620027 EU MAIN ROTOR BLADE MISINSTALLED E BAQA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 03 62UP 822 822 0475 WHILE PERFORMING AN 800 HOUR INSP OF THE MAIN ROTOR BLADES, FOUND 2 BLADES THAT THE BEARING PIN, EXPANSION BOLT, AND NUT WERE NOT INSTALLED PROPERLY BY THE MFG. BOTH EXPANSION BOLTS WERE BROKEN DURING REMOVAL FOR THE FIRST 800 INSPECTION I NTERVAL ON THESE BLADES. THE BEARING PIN HAD SLOTS IN IT AND THE NUT HAS TABS ON AND THEY LOCK TOGETHER. WHEN THEY ARE PROPERLY LOCKED 1 TO 2MM OF THREAD MUST PROTRUDE THROUGH THE NUT. WE HAVE ISSUED A QAN TO INSPECT THE BOLTS FOR PROPER SEATING AND HAVE CONTACTED THE MFG. 1 G 7 2 3U H88EU 2008031700254 20080317 00254 CE 2008 3 17 GUUA01230801 1 20080123 A 3230 CIRCUIT BREAKER BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA COCKPIT POPPED A GUUA K NONE O OTHER AP APPROACH 1 SO 29 16540 UE172 FLIGHT: 9167, DURING APPROACH WHEN SELECTING THE LANDING GEAR DOWN THE LANDING GEAR CB FOR THE MOTOR POPPED. INSPECTED THE LANDING GEAR SYS, PERFORMED LANDING GEAR EXTENSION AND RETRACTION, OPS CHECK NORMAL. 2 L 7 2 4T 3 T RT A24CE E2NE 2008031700263 20080317 00263 CE 2008 3 17 DXTA200802787 1 20080122 A 2731 444303739 TRIM MOTOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ELEVATOR STICKS E DXTA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 07 628QS 5176 5605305 CLIMBING FROM FL 380 TO FL 410 AT 18,600 LBS AND 180 KTS WHEN WE RAN OUT OF FWD NOSE DOWN TRIM. REPLACED ELECTRIC TRIM MOTOR FOR TROUBLESHOOTING PURPOSES AND FOR POSSIBLE COLD SOAK OF OLD TRIM MOTOR CAUSING OVER TORQUE CONDITION. OPS. CHE CKED OKAY. LOWERING TRIM CABLE TENSIONS NOT REQUIRED. CHECKED ELEVATOR TRIM MOTOR AND ELEVATOR TRIM CABLE TENSIONS, TH EY FALL WITHIN SPECS AT THIS TIME. CHECKED ELEVATOR TRIM TAB TRAVELS OKAY AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008031700265 20080317 00265 2008 3 17 DXTA200802791 4 20080123 A 3160 10644D02M03 DISPLAY CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT MALFUNCTIONED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 659QS 3395 5605359 AT FL340, LT ENGINE INSTRUMENT LCD WENT BLANK, SHORTLY AFTER WE DETECTED AN ELECTRICAL BURNING ODOR AND RETURNED TO AIRP ORT. REMOVED AMLCD AND INSTALLED MODIFIED AMLCD IAW MM 77-40-00. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008031700270 20080317 00270 NM 2008 3 17 XXUA200800002 1 20080226 A 3350 767 LIGHT BOEING 757 7572Q8 1384972 NM PWA PW2037 PW2037M 52117 NE EXTERIOR INOPERATIVE A XXUA K NONE L NO TEST IN INSP/MAINT 1 EA 15 403JS 27351 EMERGENCY EXTERIOR LIGHT AT L4 DOOR WILL NOT ILLUMINATE WHEN LIGHT SWITCH SELECTED. FOUND LAMP FAILED AND REPLACED. OP ERATION NORMAL 2 L 7 2 4F 4 F RT A2NM E17NE 2008031700272 20080317 00272 EA 2008 3 17 MASA200800190 1 20080306 A 5210 SWITCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 570ML 7206 ASH FLT 7350 - ORD - PAX DOOR OUTER HANDLE HARD TO STOW. ADJUSTED OUTER HANDLE STOW SWITCH, OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2008031700273 20080317 00273 EA 2008 3 17 MASA200800191 1 20080306 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17275 7275 ASH 2728 PHX-LGB - PAX DOOR WILL NOT CLOSE. MX LUBED THE PAX DOOR AND OPS CHECK NORMAL. 2 L 7 2 4F RT A21EA 2008031700274 20080317 00274 EA 2008 3 17 MASA200800192 1 20080306 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA FA PBE MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 571ML 7209 ASH FLT 7252 ORD-AVP - FWD FA PBE INSPECTION STICKER WAS MISSING. MX INSPECTED THE PBE AND INSTALLED A NEW STICKER. 2 L 7 2 4F RT A21EA 2008031700283 20080317 00283 NM 2008 3 17 MASA200800208 1 20080301 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 448YV 448 REPAIR OF THE RT NR 5 FLAP TRACK. 2 H 7 2 4T RT A13NM 2008031700285 20080317 00285 NM 2008 3 17 MASA200800210 1 20080301 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 448YV 448 REPAIR FOR WEAR AND CORROSION ON THE LT NR 1 FLAP TRACK. 2 H 7 2 4T RT A13NM 2008022600120 20080226 00120 NM 2008 2 26 ASAA0842597 1 20080124 A 5320 694147328 INTERCOSTAL BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO RBL 21 BS 500 E TO 500 F INTERCOSTAL CRACKED. CASCADE RESPONSIBILITY INTERCOSTAL REPLACED. 2 L 7 2 4F RT A16WE 2008022600126 20080226 00126 NM 2008 2 26 ASAA0842606 1 20080117 A 5320 6545829502 WEB BOEING 737 7374S3 1384711 NM FUSELAGE SCRATCHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 E AND E COMPT DOOR CMT RT WEB SCRATCHES FOUND ABOUT LATCH FITTING. WEB REPLACED. 2 L 7 2 4F RT A16WE 2008022600127 20080226 00127 NM 2008 2 26 ASAA0842607 1 20080119 A 5320 69374024 ATTACH ANGLE BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD GALLEY SERVICE DOOR WAY FLOOR ATTACH ANGLE FWD OF FWD STUB FRAME CRACKED AT AFT FASTENER HOLE ATTACHMENT TO LOWER SI LL CHORD. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600128 20080226 00128 NM 2008 2 26 ASAA0842610 1 20080214 A 5347 654681349 SEAT TRACK BOEING 737 7374S3 1384711 NM FUSELAGE DEFECTIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 BS 500B RBL 24 SEAT TRACK INERFERES WITH SEAT INSTALLATION BS 500B TO BS 500D RBL 24. SEAT TRACK REPLACED IAW B737 400 SRM 53 00 52 REPAIR 1 FIG 201. 2 L 7 2 4F RT A16WE 2008022600129 20080226 00129 NM 2008 2 26 ASAA0842611 1 20080106 A 5347 655548410 CARGO TRACK BOEING 737 7374S3 1384711 NM CARGO BAY GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO PIT RT TIE DOWN TRACK HAS GOUGED AT BS 460 + 2 RBL 14. FWD CARGO PIT RT TIE DOWN TRACK AT BS 460 REPAIRED IAW B737 400 SRM 53 00 53. 2 L 7 2 4F RT A16WE 2008022600130 20080226 00130 NM 2008 2 26 ASAA0842617 1 20080120 A 5320 69165096 ANGLE BOEING 737 7374S3 1384711 NM FUSELAGE BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CABIN BS 345 LBL 64 WL 216 ANGLE BROKEN. BROKEN ANGLE AT BS 345 LBL 216 REPLACED WITH MADE REPAIR PART IAW B737 400 SRM 51 40 02. 2 L 7 2 4F RT A16WE 2008022600131 20080226 00131 NM 2008 2 26 ASAA0842619 1 20080117 A 5315 6545810 FLOORBEAM BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FLOORBEAM AT FS 312 BL 2L TO BL 11R HAS CORROSION AROUND SCREW HOLES. FLOORBEAM REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600132 20080226 00132 NM 2008 2 26 ASAA0842621 1 20080105 A 5320 654659247 CHANNEL BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT FLOOR CHANNEL FOUND CORRODED AT BS 727F+8 LBL 11. REPAIRED WITH MADE REPAIR PARTS. 2 L 7 2 4F RT A16WE 2008022600134 20080226 00134 NM 2008 2 26 ASAA0842627 1 20080114 A 5320 6941773674 INTERCOSTAL BOEING 737 7374S3 1384711 NM FUSELAGE BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO COMP INTERCOSTAL IS BENT AT BS 440 460 LBL 25. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600136 20080226 00136 NM 2008 2 26 ASAA0842634 1 20080128 A 5754 65C26602224 WEDGE BOEING 737 7374S3 1384711 NM L/E SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 NR 5 SLAT HAS DELAM AT I/B AFT CORNER. REPAIRED NR 5 SLAT AT I/B END IAW B737 400 SRM CH 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 2008022600137 20080226 00137 NM 2008 2 26 ASAA0842635 1 20080122 A 5754 65C26602224 WEDGE BOEING 737 7374S3 1384711 NM L/E SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 NR 5 SLAT HAS DELAM AT O/B AFT END. REPAIRED NR 5 SLAT AT O/B AFT END IAW B737 400 SRM CH 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 2008022600139 20080226 00139 EU 2008 2 26 08FDEA00432 1 20080214 A 5320 A53610270221 INTERCOSTAL AIRBUS 300 A300B4605R 3930308 EU BS 972 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 AVIONICS COMPARTMENT, INTERCOSTAL UNDER THE FLIGHT DECK FLOOR IS CRACKED ON THE AFT END; LOCATED AT BS 972 (FR 10), LBL 39. REMOVED INTERCOSTAL IAW SRM 51-40-21. FABBED NEW WEB IAW DWG 45-A53611975 ISSUE A, TPS 1003 REV A & SRM 51-4 0-44. ALODINED, PRIMED IAW SRM 51-21-10 & 51-23-10. PART MARKED IAW GMM 7-0-1000. INSTALLED INTERCOSTAL IAW SRM 51-40-21. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008022600140 20080226 00140 NM 2008 2 26 SB08008 1 20080220 A 3897 WIRE BOEING 737 737401 1384701 NM LAVATORY SPARKS A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 418US 23985 MCO FLT 1458 DURING CRUISE, EN ROUTE FROM FLL TO PHL, CREW REPORTED TO DISPATCH VIA ACAR'S THAT A PASSENGER AND A FLIGHT ATTENDANT SAW SPARKS COMING FROM BENEATH THE PAPER TOWEL RACK IN THE AFT LEFT LAVATORY. THE FIRST OFFICER ALSO CONFIRM ED SPARKS FROM THAT AREA. CREW DECLARED AN EMERGENCY AND DIVERTED TO MCO. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND T AXIED TO THE GATE. MAINTENANCE DISABLED AFFECTED WIRE BUNDLE, BLOCKED THE LAV AND PLACED IT ON MEL. MAINTENANCE REPAIRE D BROKEN WIRE BEHIND TOWEL RACK AND RECONNECTED HARNESS. REMOVED MEL. 2 L 7 2 4F RT A16WE 2008022600148 20080226 00148 EU 2008 2 26 USAA920080454 1 20080218 A 5315 D53472284008 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3101 / FR 65, -Y464.8. REPLACED CABIN FLOORBEAM, BS 30 43 / FR 64 - BS 3207 / FR 67, -Y464.8 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022600154 20080226 00154 EU 2008 2 26 USAA920080460 1 20080212 A 5347 D53371110008 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SEAT TRACK, BS 1810 / FR 41 - BS 2136 / FR 47, +Y765. REPLACED CABIN SEAT TRACK, BS 1810 / FR 41 - BS 2136 / FR 47, +Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031700286 20080317 00286 NM 2008 3 17 MASA200800211 1 20080301 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 448YV 448 REPAIR OF THE LT NR 4 FLAP TRACK. 2 H 7 2 4T RT A13NM 2008031700287 20080317 00287 NM 2008 3 17 MASA200800212 1 20080301 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 448YV 448 REPAIR OF THE LT NR 5 FLAP TRACK. 2 H 7 2 4T RT A13NM 2008031700291 20080317 00291 NE 2008 3 17 DHLA200800026 2 20080223 A 7321 LINE DOUG DC8 DC873 302199C WP GE CFM56 CFM562C 13802 NE NR 4 ENGINE LOOSE A DHLA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 05 807DH 45990 692389 FLT NR 9994, NR 4 ENGINE ROLLBACK AT FL280 DESCENDED TO FL 200 ENGINE RESTARED NORMAL AND RAN NORMAL THE REST OF THE TRI P WITH NORMAL INDICATIONS. INSPECTED NR 4 ENGINE INTAKE AND EXHAUST NO DEFECTS NOTED. FOUND CDP LINE LOOSE RESECURED L INE IAW CFM 56 MM 71-00-00, 73-21-10. PERFORMED MPA RUN NR 4 ENGINE. OP CHECKED NORMAL IAW JRH 13.3. AIRCRAFT WAS GRO UNDED. 2 L 7 4 4F 4 F RT 4A25 E2GL 2008031700292 20080317 00292 EU 2008 3 17 MALA080036 1 20080307 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446XJ 340B446 11 DENTS AND 9 GOUGES FOUND RT FUSELAGE SKIN BENEATH NR 7 ICE SHIELD. INSTALLED DOUBLER/TRIPLER IAW EO NR S53536. 2 L 7 2 4T RT A52EU 2008031800003 20080318 00003 EU 2008 3 18 MALA080037 1 20080304 A 5522 SKIN SAAB SF340 340B 7860101 EU LT ELEVATOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 446XJ 340B446 3 DENTS FOUND LT ELEVATOR LEADING EDGE UPPER SKIN. REPAIRED IAW EO NR S55137. 2 L 7 2 4T RT A52EU 2008031800004 20080318 00004 NE 2008 3 18 DHLA200800017 2 20080226 A 7321 FCU BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE OUT OF ADJUST A DHLA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 05 743DH 22438 FLT NR 385, 1 ENG WOULD NOT PRODUCE TAKEOFF EPR RTO WT 174.9 24 DEGED C PA-70 BRAKE ENERGY ZONE NORMAL IAS LESS THAN 60 NTS SWAPPED NR 1 AND 2 EPR GAUGES FOR TROUBLESHOOTING RAN ENGINE, ALL ENGINE PARAMETER LOW ON NR 1 ENG. RETURN NR 1 AND 2 EPR GAUGES TO ORIGINAL POSITIONS PERFORMED NR 1 ENGINE RUN AND TRIM RECORD IAW B727 JRH 7.7. ADJUSTED MIL 25 CLICKS INCREASE IDLE TRIM DOWN 18 CLICKS. ALL PARAMETERS CHECK GOOD. AIRCRAFT WAS GROUNDED. 2 L 7 3 4F 4 F A3WE E2EA 2008031800012 20080318 00012 EU 2008 3 18 08FDEA00854 1 20080310 A 5320 A21510415000400 PANEL AIRBUS 310 A310203 3930313 EU FUSELAGE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FOUND DELAMINATION ON PANEL NR 143FL, INTERIOR SKIN. REPAIRED BY REMOVING DAMAGE. APPLIED, CURED & SANDED WET LAY UP. APPLIED REFINISH IAW SRM 51-77-10 & SRM 51-75-10. 2 L 7 2 4F RT A35EU 2008031800014 20080318 00014 EU 2008 3 18 08FDEA00856 1 20080310 A 5320 A2557561200600 PANEL AIRBUS 310 A310203 3930313 EU AFT CARGO BAY PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT CARGO PIT PANEL NR 162 OW IS PUNCTURED. REPAIRED AFT CARGO PIT PANEL AND TOP COATED ( WHITE ) IAW DRAWING SRZ -75-0 13. 2 L 7 2 4F RT A35EU 2008031800015 20080318 00015 EU 2008 3 18 08FDEA00857 1 20080310 A 2550 A25575538014510 PANEL AIRBUS 310 A310203 3930313 EU AFT CARGO BAY DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT CARGO PIT CEILING PANEL NR 152 DC IS DELAMINATED AND DENTED. RECEIVED NEW PANEL. TO BE INSTALLED ON CARD 41C0071. 2 L 7 2 4F RT A35EU 2008031800021 20080318 00021 NM 2008 3 18 08FDEA00863 1 20080310 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 521FE 48478 FOUND MAIN DECK SEAT TRACK AT STA 1521, X = -75.25, FOUND EXFOLIATION CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPL ACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008031800022 20080318 00022 NM 2008 3 18 08FDEA00864 1 20080310 A 5712 ARB292225 RIB DOUG MD11 MD11F 3023600 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 521FE 48478 LEFT WING, LEADING EDGE RIB FOUND CRACKED AT XOS 795. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. NEW RIB FABRI CATED AS PER DRAWING ARB2922. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008031800028 20080318 00028 WP 2008 3 18 08FDEA00872 1 20080311 A 5311 AGA00143 FRAME DOUG DC10 DC1010F 3022111 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MODIFICATION DC10 CARGO TO MD10 ACF, AT REMOVAL BRACKET IS NOTED CRACK 1.5 INCH LONG ON FRAME STA 1851 RT SIDE LO NGERON 10 TO 11. PERFORMED REPAIR FOR EA FEDEX 8-5310-111515. 2 L 7 3 4F A22WE 2008031800029 20080318 00029 EU 2008 3 18 08FDEA00877 1 20080311 A 2710 A2717097000200 GUIDE AIRBUS 310 A310324 3930206 EU AILERON CABLES WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 IN LT MLG AREA; ALL CABLE GUIDES INBD OF THE LT TRUNNION FOR THE AILERON CABLES ARE WORN. REMOVED AND INSTALLED 3 NEW C ABLE GUIDES ON THE INBD SIDE OF THE LT MLG TRUNNION FOR THE AILERON CABLES IAW A310-300 AMM 20-21-12 AND AMM 27-10-00-6. 2 L 7 2 4F RT A35EU 2008031800035 20080318 00035 EU 2008 3 18 08FDEA00886 1 20080311 A 5321 A5327279800800 FLOOR PANEL AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FLOOR PANEL 152YF HAS EDGE DAMAGE AND IS DENTED. FABRICATED NEW FLOOR PANEL. POTTED EDGES, COMPLETED CURE & SANDED E DGE POTTING. INSTALLED INSERTS & APPLIED NON-SKID IAW DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 2008031800037 20080318 00037 EU 2008 3 18 08FDEA00888 1 20080311 A 5321 35039003 FLOOR PANEL AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FOUND FLOOR PANEL P/N 35039003 HAS EDGE DAMAGE. REPAIRED FLOOR PANEL 132 YF I.A.W. FEDEX DWG. SRZ-25-00 REV. E. 2 L 7 2 4F RT A35EU 2008031800039 20080318 00039 NM 2008 3 18 QXEA200800267 1 20080228 A 5210 HINGE FITTING BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - FORWARD PAX DOOR SHAFT HINGE ASSY IS CORRODED ON DOOR ATTACH LUGS WHERE GOOSE NECK ATTACHES. REMOVED HINGE S HAFT IAW Q400 AMM 52-11-26-000-801. REMOVED FWD AND AFT HINGE LUGS AND INSTALLED NEW HINGE LUGS IAW DHC8 Q400 SRM 51-42 -60. INSTALLED THE MCD HINGE SHAFT IAW Q400 AMM 52-11-26-400-801. 2 H 7 2 4T RT A13NM 2008031800042 20080318 00042 NE 2008 3 18 HALA0800384 2 20080310 A 7230 BLADE BOEING 767 7673CB 1385187 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE NICKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM, SMALL NICK FOUND ON LEADING EDGE OF NR 2 ENG, BLADE NR 23 APPROX 6 INCHES FROM ROOT. REPAIRED BY BLENDING PER AMM 72-31-02-308-003-N00. PERFORMED DYE PEN INSP ON REPAIRED AREA, NO TROUBLE FOUND. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800046 20080318 00046 GL 2008 3 18 HALA0800386 2 20080308 A 7230 BLADE BOEING 767 767332 1382001 NM GE CF6 CF680C GL NR 2 ENGINE DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 ETOPS SIGNIFICANT SYSTEM, ON WALKAROUND ON NR 2 ENGINE FOUND 1 DING ON BLADE 1, 9 APPROX 5 INCHES FROM BLADE ROOT AREA C PER MM 72-31-02-3-08-003. BLENDED BLADE PER MM TASK 72-31-02 AREA C LEADING EDGE. NEEDS DYE PENETRANT INSPECTION PER AMM 70-11-06/201. REMOVED APPROX 015. EDDY CURRENT CHECKED OK PER AMM 72-31-02, NO FAULTS NOTED. 2 L 7 2 4F 4 F RT A1NM E23EA 2008031800049 20080318 00049 NM 2008 3 18 QXEA200800274 1 20080306 A 5321 FLOORBOARD DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - C5 - CORROSION ON FLOORBOARD FLANGE UPPER SURFACE AT STATION 599.5 OUTBOARD OF STRINGER 28R TO END OF FLANGE. REM OVED NUT PLATE, BLENDED OUT CORROSION IAW DASH 8 200 CPM CHAPTER 4, BLENDED AREA WITHIN LIMITS IAW DASH 8 200 SRM 51-20- 11. ALODINED AND PRIMED BLENDED AREA IAW DASH 8 200 SRM 51-20-16 AND 51-20-36. INSTALLED NUT PLATES IAW DASH 8 200 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2008031800052 20080318 00052 EA 2008 3 18 MASA200800213 1 20080310 A 5210 SEAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DIRTY A MASA O OTHER O OTHER DE DESCENT 1 SW 07 7291Z 7291 FLT 2741, PHX-PSP - MAIN CABIN DOOR MAKES A HISSING NOISE PASSING THROUGH FL 200 AND BELOW, PLANE DID NOT LOSE PRESSURE. MX FOUND DOOR SEAL DIRTY, CLEANED AND RELUBED SEAL. 2 L 7 2 4F RT A21EA 2008031800054 20080318 00054 NM 2008 3 18 QXEA200800275 1 20080306 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - C5 - CORROSION ON FLOOR BOARD NUT PLATE FLANGE UNDER PANEL 144BZ AT STATION 199.5 INBOARD OF SEAT TRACK. REMOVED NUTPLATE, BLENDED OUT CORROSION IAW DASH 8 200 CPM CHAPTER 4, FOUND TO BE WITHIN LIMITS IAW DASH 8 200 SRM 51-20-11. ALO DINED AND PRIMED BLENDED AREA IAW DASH 8 200 SRM 51-20-16 AND 51-20-36. INSTALLED NUTPLATE IAW DASH 8 200 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2008031800055 20080318 00055 EU 2008 3 18 TRBA2008028 1 20080311 A 3230 1206P0121 PRESSURE SWITCH AEROSP ATR72 ATR72212 8680945 EU LANDING GEAR FAILED A TRBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 270AT 270 RT MAIN GEAR FAILED TO RETRACT AFTER TAKEOFF. UPON TROUBLE SHOOTING FOUND GREEN LOW PRESSURE INDICATION, RAI SWITCH 12G NA, LEAK CHECKED. PERFORMED LG EXTENSION RETRACTION IAW JIC 32-31-00. NO FAULTS NOTED AT THIS TIME. 2 H 7 2 4T RT A53EU 2008031800066 20080318 00066 NM 2008 3 18 QXEA200800272 1 20080306 A 5320 BRACKET DHAV DHC8 DHC8202 2809007 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - C5 - ANGLE BRACKET FORWARD OF STATION 600 AND INBOARD OF STRINGER 31R WEB UNDER FLOOR PANEL 441CZ IS CRACKED IN UP PER RADIUS. DRILLED OUT RIVETS IN THE ANGLE BRACKET. REMOVED IAW D8 200 SRM 51-10-21 PG 2 FIG 1. HFEC INSPECTED CUT A WAY FOR REMOVAL OF CRACK IAW D8 200 NDTM PART 6 51-00-01. INSTALL BRACKET IAW D8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008031800070 20080318 00070 NM 2008 3 18 MASA200800223 1 20080310 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 448YV 448 LH Y-9.25 FLOOR SUPPORT CORRODED. MX CW REPAIR. 2 H 7 2 4T RT A13NM 2008031800071 20080318 00071 EU 2008 3 18 08FDEA00889 1 20080311 A 5413 2210081328 LONGERON AIRBUS 310 A310203 3930313 EU NR 2 PYLON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 ENGINE PYLON AFT FAIRING; OUTBD UPPER LONGERON IS CHAFFED AT SEVERAL SCREW HOLES. REMOVED DAMAGED LONGERON IAW A31 0-300 SRM 61-40-21; PG 7, RECEIVED LONGERON P/N 221-0081-328, PO 610555.3 AND LOCATED HOLES IAW A310-300 SRM 51-40-40. INSTALLED LONGERON IAW A310-300 SRM 51-40-21; PARAGRAPH 6. 2 L 7 2 4F RT A35EU 2008031800072 20080318 00072 EU 2008 3 18 08FDEA00890 1 20080311 A 5413 2210081328 LONGERON AIRBUS 310 A310203 3930313 EU NR 2 PYLON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 ENGINE PYLON AFT FAIRING; OUTBD UPPER LONGERON IS CHAFED AT SEVERAL SCREW HOLES. REMOVED DAMAGED LONGERON IAW A310 -300 SRM 61-40-21; PG 7. RECEIVED LONGERON P/N 221-0081-328, PO 610555.3 AND LOCATED HOLES IAW A310-300 SRM 51-40-40. INSTALLED LONGERON IAW A310-300 SRM 51-40-21; PARAGRAPH 6. 2 L 7 2 4F RT A35EU 2008031800078 20080318 00078 EU 2008 3 18 08FDEA00899 1 20080312 A 5347 A5381310620000 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 CENTER ARTICULATING SEAT TRACK BETWEEN FRAME 38.2 AND FRAME 40. REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-21 PARA. 6. I NSTALLED NEW SEAT TRACK IAW EO E-6-5310-7-3322 PT 2. 2 L 7 2 4F RT A35EU 2008031400078 20080314 00078 NM 2008 3 14 AALA200800444 1 20080228 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 775AN 29584 DFW - EMERGENCY LIGHT AT SEAT 26G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031400089 20080314 00089 NM 2008 3 14 F3LA200800081 1 20080229 A 5320 D5347112420100 SHEAR PLATE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B6P 13018 NE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED THE RIGHT SHEAR PLATE, LOCATED BETWEEN FRAMES 69 AND 70, SHOWED SIGNS OF CORRO SION. MAINTENANCE REMOVED AND REPLACED THE SHEAR PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGR APHS 6, 7 AND 14. FOLLOWING CONPLETION OF THE INSTALLATION, THE SHEAR PLATE WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032800092 20080328 00092 2008 3 28 SWAA081561 4 20080321 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031700002 20080317 00002 GL 2008 3 17 CHQA200800047 2 20080306 A 7261 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 LEAKING A CHQA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 575RP 17605 145847 CAE311280 CMH TO BOS - WHILE CLIMBING THROUGH FL190, THE CREW RECEIVED AN E1 IMPENDING OIL BYPASS MESSAGE. THE FIRST OFFICER PERF ORMED THE QRH CHECKLISTS, WHILE THE CAPTAIN CHECKED THE ENGINE STATUS ON THE MFD. THE CAPTAIN NOTICED THAT THE OIL QUAN TITY WAS DOWN TO 3 QUARTS FOR E1 AND THE OIL TEMPERATURE CLIMBED QUICKLY TO 141 DEGREES CELSIUS. AT THAT POINT THE FLIG HT CREW SHUT DOWN E1 AS A PRECAUTION AND RETURNED TO CMH, WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUB LESHOT THE FAULT AND FOUND THAT THE ENGINE WAS LEAKING OIL INTERNALLY. THE NUMBER 1 ENGINE WAS THEN REPLACED AND THE AI RCRAFT RETURNED TO SERVICE 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008031700003 20080317 00003 SO 2008 3 17 CHQA200800046 1 20080303 A 3620 7276045 FILTER ELEMENT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 BLEED SYS DIRTY A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 573RP 145837 CAE312348 SBN TO CVG - DURING CLIMB-OUT, CREW RECEIVED A BLEED 1 OVERTEMP MESSAGE AT AROUND 4,000 FEET. THE FLIGHT RETURNED TO FI ELD AND LANDED WITHOUT INCIDENT AT SBN. MAINTENANCE TROUBLESHOT THE BLEED SYSTEM PER THE FIM, REMOVED THE FAN AIR VALVE FILTER AND CLEANED IT. THE FILTER WAS THEN REINSTALLED AND THE BLEED SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008031700012 20080317 00012 NM 2008 3 17 2008UALA01246 1 20080307 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY EXIT SIGN INOP, ACROSS AISLE FWD GALLEY. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031700024 20080317 00024 SO 2008 3 17 C2XA08IA072 1 20080303 A 3230 852701 PROXIMITY SWITCH EMB 145 EMB145EP 3260221 SO RT MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13935 145022 IAH - FLIGHT 2742, THE CREW REPORTED A LOUD BANGING SOUND AFTER GEAR RETRACTION COMING FROM THE NOSE GEAR AREA, AND AFTE R DEPARTURE THE RIGHT MAIN GEAR INDICATION SWITCHED FROM UP TO AMBER, BACK TO UP. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE RIGHT HAND MAIN LANDING GEAR UPLOCK BOX AND PROXIMITY SWITCHES, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. 2 L 7 2 4F RT T00011AT 2008031700027 20080317 00027 SO 2008 3 17 C2XA08SH030 1 20080219 A 5330 14533826001 DOUBLER EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11544 145557 SHV - DURING C-CHECK, SKIN DOUBLER AROUND HEATED WATER NIPPLES FR 57-58 HAS CORROSION. MX REPAIRED SKIN DOUBLER AROUND HEATED WATER NIPPLES AT FR 57-58 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008031700040 20080317 00040 NM 2008 3 17 08FDEA00795 1 20080308 A 5311 6516349Y130 FRAME BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 MAIN BODY FRAME ASSY CORRODED, BS 1166, STR 17L, WL 208. REMOVED CORROSION FROM BS 1166, S17L FRAME AND FOUND TO BE OUT OF LIMITS, REMOVED FRAME AND INSTALLED. REFERENCE SRM 51-30-2. CLASSIFIED AS MAJOR REAIR 2 L 7 3 4F A3WE 2008031700043 20080317 00043 NM 2008 3 17 08FDEA00797 1 20080309 A 5730 ARB2886503 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 521FE 48478 LEFT WING, NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUTOUT INBOARD CORNER FOUND CRACK. REPAIRED AS PER SRM 57-10-00 FIG URE 43 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008031700051 20080317 00051 NM 2008 3 17 SWAA081275 1 20080309 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2008031700072 20080317 00072 WP 2008 3 17 08FDEA00805 1 20080310 A 5310 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOORWAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 MCD LOWER JAMB AT SPOOL FITTING LOCATION NUMBER 4 SHOWED EVIDENCE OF CRACKS IN HOLES A, B, C, D. 2 L 7 3 4F RT A22WE 2008031700080 20080317 00080 WP 2008 3 17 08FDEA00808 1 20080310 A 5310 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOORWAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 MCD LOWER JAMB AT SPOOL FITTING LOCATION NUMBER 2 SHOWED EVIDENCE OF CRACK IN HOLES A, B, C, D. 2 L 7 3 4F RT A22WE 2008031700100 20080317 00100 WP 2008 3 17 08FDEA00821 1 20080310 A 5414 AUB7120501 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 NR 3 PYLON PANEL 488CL IS CRACKED AT THE CUTOUT. WELD REPAIRED CRACKS IAW DWG AUB 7120 & DPS 4.801 & DPS 10.225. 2 L 7 3 4F RT A22WE 2008031700140 20080317 00140 NM 2008 3 17 AALA200800474 1 20080302 A 3397 WIRE BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 376AN 25445 SFO - EMERGENCY LIGHTS AT SEATS 17EH INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHTS AT SEATS 17EH. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008031700178 20080317 00178 NM 2008 3 17 SWAA081342 1 20080310 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 766SW 29806 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 32 TO RBL 50. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2008031700183 20080317 00183 NM 2008 3 17 HALA0800379 1 20080305 A 5730 SKIN BOEING 767 767332 1382001 NM RT WING CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 CORROSION ON RT WING LOWER SURFACE, RIB 8 FWD OF STRINGER L10, CORROSION FOUND SURROUNDING RIVET HEADS. REPAIR IN WORK. 2 L 7 2 4F RT A1NM 2008031700195 20080317 00195 NM 2008 3 17 SWAA081349 1 20080311 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 481WN 29853 R2 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008022600157 20080226 00157 EU 2008 2 26 USAA920080463 1 20080210 A 5320 D53480043205 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON THE R2 DOOR CUTOUT LOWER SILL, BS 3158 / FR 66, -Y1732. REPAIRED THE R2 DO OR CUTOUT LOWER SILL, BS 3158 / FR 66, -Y1732 IAW A320 SRM 53-41-11. 2 L 7 2 4F RT A28NM 2008022600162 20080226 00162 SO 2008 2 26 FDKA200802073 1 20080220 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO CARGO BAY MALFUNCTIONED A FDKA O OTHER O OTHER CR CRUISE 1 SW 07 825MJ 145179 FDM 6152 MCO-GSO (1558 PHX LCL) EN ROUTE TO GSO AIRCRAFT DIVERTED TO SAV DUE TO BAG SMOKE WARNING ON EICAS IN FLIGHT. N O EVIDENCE OF FIRE WAS FOUND AND MX REMOVED AND REPLACED SMOKE DETECTOR AND BOTTLES. 2 L 7 2 4T RT T00011AT 2008022600180 20080226 00180 NM 2008 2 26 ASAA0842579 1 20080107 A 5320 654659247 CHANNEL BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT FLOOR CHANNEL FOUND CORRODED AT BS 767+6 LBL 8. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600188 20080226 00188 NM 2008 2 26 ASAA0842600 1 20080201 A 5320 694147317 INTERCOSTAL BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO PIT BS 400 TO 420 LBL 24 INTERCOSTAL CRACKED. CASCADE RESPONSIBILITY REPAIRED WITH REPAIR PARTS. 2 L 7 2 4F RT A16WE 2008022600189 20080226 00189 NM 2008 2 26 ASAA0842603 1 20080115 A 5347 0071230073 SEAT TRACK BOEING 737 7374S3 1384711 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 SEAT TRACK AT STA 500 F+10" RBL 45 GOUGED. SEAT TRACK REPLACED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600196 20080226 00196 NM 2008 2 26 ASAA0842629 1 20080116 A 5347 654681349 SEAT TRACK BOEING 737 7374S3 1384711 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 SEAT TRACK GOUGED BS 500 B+8 TO 500 L+12 RBL 25. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600198 20080226 00198 EA 2008 2 26 TRAX200800211 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 863-969 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 RT SIDEWALL SEAT RAIL FS 863.0 TO FS 969.0 HAS CORROSION DAMAGE. REMOVED CORRISION AND FOUND TO BE WITHIN LIMITS IAW CR J 700 SRM 53-51-49. APPLIED ALODINE IAW SRM 51-21-16. 2 L 7 2 4F RT A21EA 2008022600201 20080226 00201 2008 2 26 ASAA0852642 4 20080218 A 2210 ZR2A SENSOR BOEING 737 737890 1384527 NM TAIL COMPARTMENT FAULTY A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 557AS 35176 AUTOLAND "LAND VERIFY" TEST FAILS 49.35 BITE. FCC "B" FAULTS ELEV POS SEN 2 MSG 22 11126. REPLACED ELEVATOR POSITION S ENSOR 2. RIG AND SENSOR TESTS ALL CHECK GOOD. LAND VERIFY PASSES 49.35 BUT NOW FAILS 49.32 WITH SAME FAULT (ELEV POS S EN 2). REPLACED NSS. LAND VERIFY OP CHECKS PASS. 2 L 7 2 4F RT A16WE 2008022600203 20080226 00203 2008 2 26 ASAA0852644 4 20080224 A 3460 1762000101 COMPUTER BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA K NONE O OTHER CL CLIMB 1 NM 02 577AS 35186 DEPARTING SEA WHEN V NAV WAS REQUESTED THE SINGLE ENGINE CLIMB PAGE WAS ENGAGED. SELECTED BOTH ENGINES PAGE AND DEPARTE D NORMALLY. BITE CHECK OF FMC'S SHOWS NO FAULTS, HAS NO RELATED HISTORY. REQUEST FLIGHT CREWS MONITOR FMS IN V NAV MOD E. 2 L 7 2 4F RT A16WE 2008022600206 20080226 00206 NM 2008 2 26 ASAA0842654 1 20080206 A 5313 654988656 STRINGER BOEING 737 7374S3 1384711 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FUSELAGE STR 14R HAS DRILL BIT DAMAGES AT 3 LOCATIONS BETWEEN STA 500F+16 & 500 G + 4. REPAIRED WITH MADE REPAIR PARTS. 2 L 7 2 4F RT A16WE 2008022600207 20080226 00207 NM 2008 2 26 ASAA0842657 1 20080128 A 5311 654655211 FRAME BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FUSELAGE FRAME CRACKED AT BS 827 RT BETWEEN STR 13R AND 14R. FUSELAGE FRAME AT BS 827 RT BETWEEN STR 13R AND 14R REPAIR ED IAW ASA DRAWING A 53100264247. 2 L 7 2 4F RT A16WE 2008022600216 20080226 00216 NM 2008 2 26 ASAA0842646 1 20080126 A 5310 6545785521 WINDOW FRAME BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 THREE CRACKS FOUND ON WINDOW FRAME AT BS 500G 500F RT. NEW WINDOW FRAME WAS TRIMMED AND INSTALLED IAW ASA EO 5330 02294 . 2 L 7 2 4F RT A16WE 2008022600224 20080226 00224 EA 2008 2 26 A6WA200840054 1 20080127 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE SERVICE DOOR LOOSE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 460AW 7867 SERVICE DOOR HOLD OPEN LATCH HANDLE LOOSE. (K) REMOVED AND REPLACED HOLD OPEN LATCH HANDLE ROLL PINS (2). OPS CHECK G OOD IAW AMM 52-41-00. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022500245 20080225 00245 EA 2008 2 25 HNAA0800081 1 20080208 A 2120 UNKNOWN DHAV DHC8 DHC8311 1386006 EA CABIN ODOR A HNAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 326EN 234 BURNING SMELL DETECTED IN ACFT WITH BLEEDS ON, GND RAN ENG WITH BLEEDS SEL ON FULL HOT 20 MIN, CND. 2 H 7 2 4T RT A13NM 2008022500298 20080225 00298 NM 2008 2 25 AALA200800285 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 23G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022500300 20080225 00300 NM 2008 2 25 AALA200800290 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 37G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 37G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022500313 20080225 00313 NM 2008 2 25 DL76G080191 1 20080212 A 3240 BRAKE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE RT MLG OVERHEATED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 173DZ 29692 704696 ON ARRIVAL, RT MAIN GEAR BRAKES REPORTED SMOKING BY TOWER ON TAXI IN. WHEN ARRIVED AT GATE RIGHT BRAKES INSPECTED WITH NO HYDRAULIC LEAKS EVIDENT. BRAKE CYCLED SEVERAL TIMES WITH NO FAULT. SUSPECT DE-ICE FLUID CONTAMINATION. 2 L 7 2 4F 4 F RT A1NM E13NE 2008022500370 20080225 00370 2008 2 25 USAA920080425 4 20080208 A 2565 101651303 SLIDE BOEING 767 7672B7ER 1385107 NM SERVICE DOOR DEFECTIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AY 2898 2898 26847 MIA - EES - C4 CHCEK - FORWARD SERVICE DOOR SLIDE DEPLOYMENT STRAP IS RELEASED. REPLACED FORWARD SERVICE DOOR SLIDE ASS EMBLY IAW USAIRWAYS JOB CARD J8-90-90202. 2 L 7 2 4F RT A1NM 2008022600040 20080226 00040 EU 2008 2 26 MALA080024 1 20080210 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 629 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 417XJ 340B417 2 DENTS LOCATED IN LOWER FUSELAGE SKIN AT STA 629, ONE AT EACH FUSELAGE DRAIN. INSTALLED DOUBLER IAW EO NR S53526. 2 L 7 2 4T RT A52EU 2008022600042 20080226 00042 NM 2008 2 26 DLM90080238 1 20080215 A 5530 LUG DOUG MD90 MD9030 3023690 NM VERT STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 RT O/B VERT STAB LUG CORRODED. RT O/B VERT STAB LUG REPAIRED, IAW DAL ER/A 466168-14 DATE 02/15/08 REV A. 2 L 7 2 4F RT A6WE 2008022600067 20080226 00067 EU 2008 2 26 USAA920080452 1 20080123 A 5522 D5528000100151 SKIN AIRBUS 320 A320232 3930326 EU RT ELEVATOR SATURATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AW 543 SAL - MAJOR REPAIR - C8 CHECK - RIGHT ELEVATOR UPPER SURFACE HAS 12 AREAS THAT HAVE INDICATION OF WATER ENTRAPMENT. REP AIRED RIGHT ELEVATOR UPPER SURFACE IAW A320 SRM 51-77-13. 2 L 7 2 4F RT A28NM 2008022600071 20080226 00071 NM 2008 2 26 ASAA0842585 1 20080117 A 5320 69412608 STIFFENER BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 CORROSION ON VERTICAL STIFFENER AT BS 328 AND STR 28 RT. VERTICAL STIFFENER REPLACED. 2 L 7 2 4F RT A16WE 2008022600112 20080226 00112 EA 2008 2 26 REXA200800004 1 20080222 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA CONTAMINATED A REXA C ABORTED TAKEOFF B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SO 25 8505Q 7505 SMOKE TOILET MESSAGE ON TAKEOFF. INVESTIGATED DETERMINE TO BE RESIDUAL DE-ICE FLUID IN ACS SYSTEM. MAINTENANCE COMPLIE D WITH PROJECT AUTHORIZATION PA 21-009 BLOCKING OFF LAVATORY VENT TO PREVENT REPEATS DUE TO DE-ICE FLUID INGESTION CAUSI NG VAPORS IN LAVATORY AREA. 2 L 7 2 4F RT A21EA 2008022600116 20080226 00116 NM 2008 2 26 AALA200800309 1 20080213 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 JFK - EMERGENCY LIGHT AT FLOOR LEVEL FIRST CLASS GALLEY INOPERATIVE. REPLACED BATTERY PACK AT LEFT NUMBER ONE DOOR FOR EMERGENCY LIGHT AT FLOOR LEVEL FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022600138 20080226 00138 EU 2008 2 26 BA08009 1 20080220 A 2910 HYDRAULIC LINE AIRBUS 330 A330323 3930335 EU GREEN SYSTEM LEAKING A USAA K NONE K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 19 273AY 0337 PHL FRA-PHL FLT 701 - CREW REPORTED ON DESCENT ECAM MESSAGE STATING "HYD SYS G LEAKING". PRESSURE WAS REPORTED AT 2950 LBS, NO QUANTITY EVER GIVEN. NO EQUIPMENT WAS CALLED FOR LANDING. AFTER LANDING WHILE ON TAXIING TO THE GATE, THE AIRC RAFT HAD A COMPLETE HYDRAULIC FAILURE. THE AIRCRAFT WAS THEN TOWED FROM TAXIWAY TO GATE. MAINTENANCE FOUND LEFT ENGINE GREEN HYD PUMP PRESS LINE LEAKING. REMOVED AND REPLACED GREEN PUMP LINE. 2 L 7 2 4F RT A46NM 2008022600145 20080226 00145 EU 2008 2 26 USAA920080437 1 20080214 A 5347 D5323174200 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SEAT TRACK, BS 1323 / FR 31 , -Y1292. REPAIRED CABIN SEAT TRACK, BS 1323 / FR 31, -Y1292 IAW A320 SRM 53-00-15. 2 L 7 2 4F RT A28NM 2008022600147 20080226 00147 EU 2008 2 26 USAA920080453 1 20080220 A 5315 D53472188204 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3207 / FR 67 - BS 3310 / FR 69, +Y1162.5. REPLACED CAB IN FLOORBEAM, BS 3207 / FR 67 - BS 3310 / FR 69, +Y1162.5 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022600168 20080226 00168 NM 2008 2 26 ASAA0842558 1 20080117 A 5322 65465324 SHEAR TIE BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO BILGE T/E FRAME AT FS 480 BL 2" L CORRODED SHEAR TIE. SHEER TIE REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600170 20080226 00170 NM 2008 2 26 ASAA0842564 1 20080105 A 5320 654659244 CHANNEL BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT FLOOR CHANNEL AT BS 790 TO 867 RBL 8 FOUND CORRODED. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600175 20080226 00175 NM 2008 2 26 ASAA0842569 1 20080105 A 5320 654659249 CHANNEL BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT FLOOR CHANNEL FOUND CORRODED AT BS 767+6 LBL 3. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600187 20080226 00187 EU 2008 2 26 08FDEA00433 1 20080214 A 5321 B5327036800000 FLOOR PANEL AIRBUS 300 A300B4605R 3930308 EU MAIN CARGO FLOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 MAIN CARGO COMPARTMENT FLOOR PANEL 262NF IS CRACKED. FABRICATED NEW PANEL 262 NF IAW SRZ 25-005 REV F. 2 L 7 2 4F RT A35EU 2008022600197 20080226 00197 NM 2008 2 26 ASAA0842636 1 20080126 A 5315 654581890 FLOORBEAM BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 CORROSION FOUND ON FLOORBEAM AROUND SCREW HOLD AT BS 360 RBL 2. REPAIRED WITH MADE REPAIR PARTS. 2 L 7 2 4F RT A16WE 2008022600209 20080226 00209 NM 2008 2 26 ASAA0842652 1 20080105 A 5320 69429455 INTERCOSTAL BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT ATTACHED ANGLE INTERCOSTAL TO FRAME AT BS 847 RBL 19 FOUND CORRODED. INTERCOSTAL REPLACED DUE TO CRACK (C ORROSION WITHIN SRM LIMITS). 2 L 7 2 4F RT A16WE 2008022600211 20080226 00211 NM 2008 2 26 ASAA0842655 1 20080116 A 5347 6546813518 SEAT TRACK BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 SEAT TRACK CORRODED BS 480 TO 500 RBL 45. SEAT TRACK REPLACED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600215 20080226 00215 NM 2008 2 26 ASAA0842645 1 20080117 A 5320 65458159 SUPPORT ANGLE BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 E+E COMP CORROSION FOUND ON FRAME SUPPORT ANGLE BS 344 AT STR 28R CORROSION ON FRAME ANGLE AT BS 344 STR 28R FOUND TO BE BEYOND LIMITS IAW B737 400 SRM 53 00 07 FIG 101. MADE REPAIR PART AND INSTALLED REPAIR PART IAW B737 400 SRM 51 30 01 51 40 05 AND 51 40 02. 2 L 7 2 4F RT A16WE 2008022600218 20080226 00218 EA 2008 2 26 A6WA200840016 1 20080116 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE T/E FLAP FAILED A A6WA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 31 458AW 7861 REF 183967/2 DUE TO RECENT FLAP HISTORY AND CRJ AMM TEMP REVISION 05-035, AIRCRAFT REQUIRES FURTHER FLAP TROUBLESHOOTING AND RECTIFICATION CW CRJ AMM TR 05-035. REMOVED AND REPLACED LT BPSU, OPS TEST GOOD IAW AMM 27-51-10. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022600220 20080226 00220 EA 2008 2 26 A6WA200840018 1 20080114 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 GOUGE FOUND ON AFT OF FLIGHT COMPARTMENT BULKHEAD RBL9, WL 97.50 (.250 X 300). (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022600233 20080226 00233 2008 2 26 AMTA200800023 4 20080119 A 2565 BATTERY DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL EVAC SLIDE DISCHARGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 702TZ 46912 L3 DOOR REMOTE SLIDE PACK PRESSURE INDICATOR TEST WEAK. REMOVED AND REPLACED BATTERY IAW AMM 25-61-03. 2 L 7 3 4F 4 F A22WE A23EA 2008022600234 20080226 00234 2008 2 26 AMTA200800024 4 20080119 A 2565 BATTERY DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL EVAC SLIDE DISCHARGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 702TZ 46912 R4 DOOR REMOTE SLIDE PACK PRESSURE INDICATOR TEST WEAK. REMOVED AND REPLACED BATTERY IAW AMM 25-61-03. (K) 2 L 7 3 4F 4 F A22WE A23EA 2008022600240 20080226 00240 NM 2008 2 26 AMTA200800030 1 20080122 A 2421 727810C GENERATOR BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE APU MALFUNCTIONED A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 561TZ 33526 EICAS MSGAPU GEN OFF DISPLAYED AND APU GEN OFF LGT ILLUM W/APU GENERATOR IAW MM CH24-21-01-024-001, APU OPS CHECKS NORMA L. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008022600242 20080226 00242 NM 2008 2 26 AMTA200800032 1 20080123 A 2421 727792M IDG BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE MALFUNCTIONED A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 550TZ 8272 32584 L ENG GENERATOR DRIVE LIGHT DOES NOT ILLUMINATED AT SHUTDOWN. REMOVED AND REPLACED LT ENGINE IDG IAW M57-24-01, OPS CK GOOD, NO LEAKS NOTED. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008022600245 20080226 00245 2008 2 26 AMTA200800035 4 20080127 A 3441 IRU BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE MALFUNCTIONED A AMTA K NONE J WARNING INDICATION CR CRUISE 1 GL 11 520AT 27976 C. IRS FAULT ON EICAS. SWAPPED RT WITH CENTER IRU, CENTER IRU SN 98052824. RT IRU SN NOW 6456. OPS CK GOOD, OK FOR SE RVICE. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008022600246 20080226 00246 WP 2008 2 26 08FDEA00527 1 20080220 A 3350 EMBS1392 POWER SUPPLY DOUG DC10 DC1030F 3023504 WP EMERGENCY LIGHT INOPERATIVE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 EMERGENCY LIGHTS DO NOT OPERATE CORRECTLY AND FAILED TEST. REMOVED AND REPLACED EMERGANCY LIGHTS BATTERY POWER SUPPLY IAW AMM 33-51-01-2. OPS CHECK GOOD IAW AMM 33-51-01-2. LOCATED BEHIND PANEL 231 AC, CEILING PANEL AFT OF LEFT FWD P ASSENGER DOOR. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008022600249 20080226 00249 2008 2 26 AMTA200800038 4 20080125 A 3442 066500080406 TRANSCEIVER BOEING 737 73783N 13844HI NM WEATHER RADAR FAULTY A AMTA K NONE O OTHER CL CLIMB 1 GL 11 310TZ 28243 WXR FAIL MESSAGE SHOWED ON TRACK OFF ROLL AND CLIMB, WENT OUT AT 26,000 FT. T/S IAW FIM 34-43-410400-801.NO FAULT NOTED . REMOVED AND REPLACED WEATHER RADAR RECEIVER/TRANSCEIVER IAW AMM 34-43-410400-801. OPS CHECK NORMAL ON GROUND. (K) 2 L 7 2 4F RT A16WE 2008022600255 20080226 00255 NM 2008 2 26 AMTA200800044 1 20080128 A 2560 CONTACT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE GIRT BAT DIRTY A AMTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 11 514AT 27971 L2 ENTRY DOOR ARM LIGHT INTERMITTENT WITH DOOR ARMED. CLEANED GIRT BAR CONTACTS ARM LIGHT, OPS NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008022600263 20080226 00263 WP 2008 2 26 AMTA200600116 1 20080220 A 3350 LIGHT LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE CABIN INOPERATIVE A AMTA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 11 163AT 1229 FLOOR EGRESS TRACK LIGHT AT ROW 3 HJK, 1 SEGMENT INOPERATIVE. REPLACED INOPERATIVE SEGMENT OF EGRESS TRACK LIGHTING. O PS CHECK GOOD. (K) 2 L 7 3 4F 4 F A23WE E12EU 2008022600268 20080226 00268 2008 2 26 AMTA200800066 4 20080210 A 3160 6227999003 DISPLAY BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT FAULTY A AMTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 552TZ 20977 20977 32586 EICAS MSG EICAS DISPLAY IN VIEW. REMOVED AND REPLACED LOWER EICAS DISPLAY IAW AMM 24-41-01. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008022600275 20080226 00275 2008 2 26 AMTA200800052 4 20080203 A 3160 S242T404602 DISPLAY BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT INTERMITTENT A AMTA K NONE J WARNING INDICATION CR CRUISE 1 GL 11 522AT 19478 19478 29330 CENTER LWR CDU (EICAS) GOES DIM AND BLANKS OUT COMPLETELY. INTERMITTENT OPERATION. REPLACED LWR CDU, OPS CHECK NORMAL IAW MM. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008022600276 20080226 00276 NM 2008 2 26 AMTA200800053 1 20080204 A 3397 WIRE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE CABIN DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 522AT 29330 EMERGENCY ESCAPE PATH LIGHT AT ROW 16, 17, AND 20, INOPERATIVE. FOUND WIRE DISCONNECTED AT ROW 20, RECONNECTED WIRE IN PLACE, OPS CHECK NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008022600286 20080226 00286 2008 2 26 AMTA200800064 4 20080209 A 3442 20414440401 ANTENNA BOEING 737 73783N 13844HI NM WEATHER RADAR UNSERVICEABLE A AMTA K NONE J WARNING INDICATION CR CRUISE 1 GL 11 317TZ 28246 WXR FAIL FLAG DISPLAYED. REMOVED AND REPLACED WEATHER RADAR ANTENNA IAW AMM 34-43-11-4, OPS TEST NORMAL. (K) 2 L 7 2 4F RT A16WE 2008022700002 20080227 00002 NM 2008 2 27 WRLA2008022 1 20080211 A 2781 SENSOR DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE L/E SLAT MALFUNCTIONED A WRLA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 11 272WA 48437 DURING APPROACH RECEIVED SLAT DISAGREE ALERT, FOLLOWED BY STICK SHAKER. PERFORMED SLAT DISAGREE CHECKLIST, DIVERTED TO KPSM DUE TO RUNWAY CONDITIONS. EMERGENCY DECLARED. REPLACED SLAT POS. SENSORS D1-17 AND D1-18 PER MM 27-84-02. PERFORM ED THE SLAT RANGE OF MOTION, MOVEMENT TEST LT & RT WING PER AMM 27-80-00, CHECK GOOD 2-13-08 REPLACED PROX SENSORS D1-13 & D1-14. 2 L 7 3 4F 4 F RT A22WE E24NE 2008022700008 20080227 00008 EA 2008 2 27 COMA0860108 1 20080203 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA A/C BAY MALFUNCTIONED A COMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 01 786CA 24185 7333 FLIGHT 4964 - RECEIVED SMOKE TOILET AND RT PACK HIGH TEMP MESSAGES. DECLARED EMERGENCY, RETURNED TO CVG, LANDED WITHOUT INCIDENT. REPLACED RIGHT ACM. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008011800026 20080118 00026 NM 2008 1 18 XXUA200700042 1 20080103 A 5270 841602 PSEU BOEING 757 7572Q8 1384972 NM PWA 2037 PW2040 NE E/E BAY INOPERATIVE A XXUA O OTHER N FALSE WARNING CR CRUISE 1 EA 15 763MX 29443 "EMERGENCY DOOR" LIGHT ON OVERHEAD PANEL AND " L EMERGENCY EXIT " STATUS MESSAGE INDICATED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008011800029 20080118 00029 EU 2008 1 18 SMIA200801101 1 20080109 A 6120 7901998 PCU SAAB SF340 340B 7860101 EU RIGHT FAILED A SIMA C ABORTED TAKEOFF G J MULTIPLE FAILURE WARNING INDICATION TO TAKEOFF 1 SW 21 394AE 17563 340B394 ON FLIGHT 3050 - CREW REPORTED DURING LOW SPEED TAKEOFF ROLL, RIGHT ENGINE PROP FEATHERED. UPON FURTHER TROUBLESHOOTING , RT TORQUE INDICATION WAS ZERO. WHEN SELECTING AUTOCOARSEN SWITCH TO OFF, PROPELLER UN-FEATHERED BUT TORQUE INDICATION WAS STILL ZERO. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE . REMOVED AND REPLACED RIGHT ENGINE PCU, RIGHT ENGINE OIL TRANSFER TUBE, RIGHT ENGINE PROP ACTUATOR, AND AUTOCOARSEN CO MPUTER SWITCH. 2 L 7 2 4T RT A52EU 2008011800066 20080118 00066 SO 2008 1 18 SWIA200819042 1 20080103 A 3350 SIGN EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 297SW 120327 LEFT LOWER PAX DOOR INTERIOR EXIT SIGN IS BROKEN. REPLACED LEFT EMERGENCY EXIT DOOR LIGHT AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008011800068 20080118 00068 SO 2008 1 18 SWIA200819044 1 20080106 A 2121 AE1711AA0 COOLING FAN EMB 120 EMB120ER 3260203 SO CABIN FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 226SW 13391 9668 120296 FLT 5700 - CABIN FILLS WITH THE ODOR OF SMOKE. REPLACED RIGHT GROUND COOLING FAN IAW MM 21-51-03. OPS CHECKS OK. 2 L 7 2 4T RT A31SO 2008011800069 20080118 00069 SO 2008 1 18 SWIA200819045 1 20080112 A 5210 BUSHING EMB 120 EMB120ER 3260203 SO PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 236SW 120312 FLT 3726 - PAX DOOR IS HARD TO OPEN AND CLOSE FROM INSIDE AIRCRAFT. REPLACED INTERMEDIATE TORQUE TUBE BUSHINGS IN PAX D OOR IAW 52-11-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008011800114 20080118 00114 NM 2008 1 18 UIEA200800015 1 20080110 A 5230 BRACKET BOEING 747 74747UF 1384812 NM CARGO DOOR CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 497MC 29258 MAIN DECK SIDE CARGO DOOR HAS BRACKET FOR DOOR CLOSED SWITCH STATION 1850 WITH SIGNS OF MINOR CORROSION. CLEANED UP COR ROSION IAW SRM 57-10-02. 2 L 7 4 4F RT A20WE 2008011800115 20080118 00115 NM 2008 1 18 UIEA200800014 1 20080110 A 5751 SKIN BOEING 747 74747UF 1384812 NM RT AILERON CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 497MC 29258 RT OUTBOARD AILERON HAS EVIDENCE OF LIGHT SURFACE CORROSION UNDER THE ALUMINUM FOIL STRIPS AT THE 4TH STATIC WICK. REMO VED LIGHT SURFACE CORROSION IAW SRM 57-70-14, AND 57-21-03. 2 L 7 4 4F RT A20WE 2008011800117 20080118 00117 NM 2008 1 18 UIEA200800016 1 20080110 A 5230 BEAM BOEING 747 74747UF 1384812 NM CARGO DOOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 497MC 29258 MAIN DECK SIDE CARGO DOOR HAS 1/2 INCH CRACK AT FWD HOOK ACTUATOR ARM LOWER BEAM AT STA 1800. CRACK REPAIRED IAW SRM 51 -70-13 AND EO NUMBER 4452A030. 2 L 7 4 4F RT A20WE 2008031700197 20080317 00197 NM 2008 3 17 SWAA081352 1 20080311 A 5753 GUIDE BOEING 737 7375H4 138449D NM T/E FLAP LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD FORE FLAP GUIDE LOOSE. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2008031700206 20080317 00206 NM 2008 3 17 ZZDA2008079 1 20080304 A 3350 8039251 BATTERY BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 929AT 55075 EPL LIGHTS OUT ON SEATS 25-31. REMOVED AND REPLACED BATTERY ASSY B5-119. 2 L 7 2 4F TR A6WE 2008031700218 20080317 00218 WP 2008 3 17 ABXR080073 1 20080207 A 5330 591022813 DOUBLER DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 DOUBLER SKIN BETWEEN STA 1132 AND 1143 WAS CRACKED AT BOTH CORNERS TO FASTENER HOLES. INSTALLED TWO DOUBLERS AT EACH CR ACK LOCATION IAW DC9 SRM 53-01 FIG 2, SHEET 3. 2 L 7 2 4F A6WE 2008031700239 20080317 00239 SO 2008 3 17 C2XA008SH0440 1 20080313 A 3350 30251031217 LIGHT EMB 135 EMB135LR 3260305 SO INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12528 145504 SHV - DURING C-CHECK EMERGENCY LIGHT ON RIGHT FWD PNL 191 INOP. MX REMOVED AND REPLACED RIGHT FWD EMERGENCY LIGHT ASSY ON 191 PNL IAW EMB 135 AMM 33-50-10, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2008031700250 20080317 00250 CE 2008 3 17 4516201192008 1 20080119 A 2923 6629201000015 PUMP LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312 01518 WP HYDRAULIC SYS OUT OF ADJUST E J7SA O OTHER J WARNING INDICATION LD LANDING 1 SW 05 426FX 162 LT AND RT OB BRAKES FAIL LIGHT ILLUMINATED AFTER GEAR EXTENSION (AMBER CAS). CREW DECLARED AN IFE. LANDING AND ROLLOUT WITHOUT INCIDENT 1/20/08. MX FERRY FLIGHT. 1/23/08. MX FOUND THE PRESSURE FROM THE AUX PUMP TOO HIGH AND WOULD NOT ADJ UST. INSTALLED NEW AUX PUMP, BRAKE CONTROL VALVE AND PRESSURE SWITCH. PRESSURE ADJUSTED AND SEVERAL GEAR SWINGS PERFORME D. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT T00008WI E6WE 2008031700269 20080317 00269 NM 2008 3 17 XXUA200800001 1 20080226 A 2897 BACR13CD2 WIRE BOEING 757 7572Q8 1384972 NM PWA PW2037 PW2037M 52117 NE FUEL SYSTEM DAMAGED A XXUA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 926JS 24964 "APU FAULT" WITH "FUEL VALVE" EICAS CAUTION CAME ON DURING CLIMB TO CRUISE LEVEL. FOUND WIRING DAMAGED AND REPAIRED. W IRE NUMBER W2658-0001/0003/0004. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031800063 20080318 00063 EA 2008 3 18 MASA200800219 1 20080311 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA LIFE VEST MISSING A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 77302 7302 ASH FLT 7351 ORD-ATW - CAPTAIN'S LIFE VEST INSPECTION STICKER WAS MISSING AND THE F/O LIFE VEST INSPECTION STICKER WAS E XPIRED. MX INSPECTED BOTH LIFE VESTS AND APPLIED NEW STICKERS ON THEM. 2 L 7 2 4F RT A21EA 2008031800076 20080318 00076 EU 2008 3 18 08FDEA00896 1 20080311 A 5414 2210081168 SKIN AIRBUS 310 A310324 3930206 EU NR 2 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 NR 2 ENGINE AFT PYLON FAIRING; INBD MID SKIN IS CRACKED AT THREE PLACES. REMOVED DAMAGED SKIN AND DOUBLER. FABRICATED DOUBLER FROM .063 2024-0, PO 597274.1 IAW A310-300 SRM 51-26-10 AND 51-26-20; LOCATED HOLES IAW A310-300 SRM 51-40-40. ALODINED AND PRIMED IAW A310-300 SRM 51-21-10 AND 51-23-10. INSTALLED NEW SKIN AND DOUBLER IAW A310-300 SRM 51-40-21; P ARAGRAPH 6. 2 L 7 2 4F RT A35EU 2008031800084 20080318 00084 WP 2008 3 18 UPS08851772 1 20080302 A 5720 DOUBLER DOUG DC8 DC873F 302199F WP WING BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 BROKEN REPAIR DOUBLER AT END OF RIB IN LT CENTER LE NEAR STA XFS341. REMOVED AND REPLACED REPAIR DOU BLER END OF RIB IN LT CENTER L/E AT XFS341 IAW SRM 51-1-20D, 57-3-3 FIG 5, 51-2-00 FIG 2, 51-1-8. 2 L 7 4 4F RT 4A25 2008031800087 20080318 00087 WP 2008 3 18 UPS08851783 1 20080301 A 5720 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 LT WING OB LE INTERNAL DOUBLER CRACKED, CHAFED AT IB END OF IB SECTION. REMOVED CRACKED DOUBLER, FAB BED AND INSTALLED REPLACEMENT DOUBLER IAW SRM51-1-21, 51-1-15, 51-1-8, 51-3-2. 2 L 7 4 4F RT 4A25 2008031800092 20080318 00092 WP 2008 3 18 UPS08851789 1 20080229 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 RT WING OB LE UPPER SCREW HOLE GOUGED AND DAMAGED,IB OF ACCESS PANEL51 7B. CUT OUT DAMAGE, FABBED RE PAIR AND INSTALLED IAW SRM 57-2-1,51-3-1, 51- 1-8 2 L 7 4 4F RT 4A25 2008031800093 20080318 00093 WP 2008 3 18 UPS08851790 1 20080229 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 RT WING OB LE UPPER ATTACH SCREW HOLE GOUGED AND DAMAGED ABOVE PNL 518 C. CUT OUT DAMAGE, FABBED AN D INSTALLED REPAIR DOUBLER,IAW SRM 57-2-1 FIG 38, 51-1-8, 57-2-0, 57-3-1. 2 L 7 4 4F RT 4A25 2008031800094 20080318 00094 WP 2008 3 18 UPS08851792 1 20080220 A 5311 56141605 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 A/C COMPARTMENT STA 55 L24L FRAME IS CRACKED AT DUCT ATTACH ROD CLIP. REPAIRED A/C COMPARTMENT FRAME AND SHEAR TIE AT STA 55 AND L24L IAW SRM 53-02-00 FIG 002, SRM 53-02-00 FIG 2B, SRM 51-9-0 FIG 068A. 2 L 7 4 4F RT 4A25 2008031800104 20080318 00104 WP 2008 3 18 IXXA08SMN056S 1 20080207 A 5320 FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FITTING CRACKED AT STATION 960.000 LONGERON19 LEFT. REMOVED CRACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AR EA AND FITTING. INSTALLED FITTING IAW DC8 SRM 51-1-20D, 51-3-1, DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATION NUMBER 2003- 05, DRAWING DOUGLAS 3779874, NDT SPM PART 08-00-02 TO 07, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008031800106 20080318 00106 WP 2008 3 18 IXXA08SMN060S 1 20080207 A 5323 37796631 FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 680.000 LONGERON 1. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008031800108 20080318 00108 WP 2008 3 18 IXXA08SMN066S 1 20080208 A 5320 4750521U1 FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 690.000 LONGERON 1. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008031800111 20080318 00111 2008 3 18 2008UALA01213 4 20080305 A 2565 D31516113 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 417UA 483 ON PTP PANEL TEST GOT EXT LOADS AFT L MESSAGE. INTERNAL SHORT IN 2L SLIDE. REPLACED DOOR 2L SLIDE. OPS CHECKED NORMAL . 2 L 7 2 4F 4 F RT A28NM E40NE 2008031800112 20080318 00112 NM 2008 3 18 2008UALA01215 1 20080305 A 5320 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 807UA 798 DOOR SILL CASTING 2R CORRODED ON FWD SECTION BEYOND REPAIR. ACCOMPLISHED MAJOR REPAIR AT DEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031800121 20080318 00121 NM 2008 3 18 2008UALA01260 1 20080307 A 5320 SHEAR PLATE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 807UA 798 FOUND SHEAR PLATE DAMAGED BEYOND LIMITS. ACCOMPLISHED MAJOR REPAIR AT DEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031800122 20080318 00122 NM 2008 3 18 2008UALA01270 1 20080308 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 ENGINE FAILED A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 204UA 28713 EN ROUTE LOST RIGHT GENERATOR. APU WAS STARTED PER CFM CHECKLIST. FLIGHT CONTINUED TO PLANNED DESTINATION. SUSPECT FA ULTY BEARING. REPLACED RT IDG ACCOMPLISHED ENGINE RUN IAW MM 24-11-01 PG 401 OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008031800128 20080318 00128 NM 2008 3 18 2008UALA01276 1 20080308 A 5320 SUPPORT ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FWD GALLEY DOOR SURROUND OTBD WEB SUPPORT ANGLE CRACKED AT BS 277 TO 294.5 BETWEEN STR 13R AND 14R. MAJOR REPAIR ACCOMP LISHED: REPLACED ANGLE BTWN STRINGERS 10R & 11R. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800130 20080318 00130 NM 2008 3 18 2008UALA01278 1 20080308 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 CABIN FLOOR CREASE BEAM "Z" ANGLE IS CORRODED BS 260-347 RBL 63". MAJOR REPAIR ACCOMPLISHED: REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800132 20080318 00132 NM 2008 3 18 2008UALA01281 1 20080308 A 2761 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SPOILER LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 660UA 27115 CENTER HYD QTY DROPPING AFTER START. FOUND SPOILER ACTUATOR NR 9 LEAKING FROM PISTON'S BODY. LEAKAGE BEYOND DISPATCH L IMITS. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800137 20080318 00137 NM 2008 3 18 2008UALA01288 1 20080309 A 5210 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD ENTRY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FORWARD ENTRY DOOR AFT FRAME CRACKED AT 6TH FROM BOTTOM STOP PIN FITTING. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTA LLED EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800138 20080318 00138 NM 2008 3 18 2008UALA01289 1 20080309 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 BS 727C SHEAR TIE HAS MISDRILLED HOLE BETWEEN STRINGERS S-21R AND S-22R. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SEC TION OF SHEAR TIE & FABRICATED & INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800139 20080318 00139 NM 2008 3 18 2008UALA01290 1 20080309 A 5320 SUPPORT ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FWD GALLEY DOOR SURROUND OTBD WEB SUPPORT ANGLE CRACKED AT BS 277 TO 294.5 BETWEEN STR 12R AND 13R. MAJOR REPAIR ACCOMP LISHED: REMOVED & REPLACED ANGLE BETWEEN STRINGERS S-12R & S-13R. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800140 20080318 00140 NM 2008 3 18 2008UALA01291 1 20080309 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FOUND BS 727C BETWEEN STRINGERS S-21R AND S-22R SHEAR TIE HAS A MISDRILLED HOLE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAM AGED SECTION OF SHEAR TIE. FABRICATED & INSTALLED SHEAR TIE REPAIR SECTION. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800142 20080318 00142 EU 2008 3 18 2008UALA01293 1 20080309 A 2700 3945128102 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ELAC FAILED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 481UA 1559 ELEVATOR-AILERON COMPUTER (ELAC) 1 INOP. FCDC1 FAULTY: SHOP FINDINGS NFF. REPLACED FCDC1, ALL OPS CHECKS WERE NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031800147 20080318 00147 NM 2008 3 18 2008UALA01298 1 20080309 A 5753 BUSHING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 7 FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 NR 7 FLAP SUPPORT UNDERWING LINK, IB JOINT 7V BUSHING. WORN IS BEYOND LIMIT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008031800149 20080318 00149 NM 2008 3 18 2008UALA01301 1 20080308 A 2621 FIRE BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 ENGINE BLOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 851UA 1664 NR 1 ENG NR 1 BOTTLE INADVERTENTLY BLOWN DURING HMV VISIT. ACCIDENTAL DEPLOYMENT OF FIRE BOTTLE. REPLACED BOTTLE AND C LEANED AREA. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031800159 20080318 00159 NM 2008 3 18 2008UALA01313 1 20080308 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 EEL FEEDER AT STA 1000L IS BROKEN. REPLACED EEL FEEDER OPS CK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800162 20080318 00162 NM 2008 3 18 2008UALA01316 1 20080308 A 2613 285N002836 CIRCUIT CARD BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE COCKPIT OVERHEATED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 666UA 29238 L ENG OH LP 1 STATUS MESSAGE WILL NOT ERASE. FOUND OVERHEAT DETECTION CARD. RESEATED OVERHEAT CARD FOR NR 1 ENGINE MES SAGE CLEARED, FIRE-TEST CHECKS GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800164 20080318 00164 NM 2008 3 18 2008UALA01318 1 20080307 A 5753 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE T/E FLAP DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 308UA 23669 LT INBD MID FLAP T/E LWR SKIN DELAM 18" FROM OUTBOARD EDGE. MAJOR REPAIR: REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800165 20080318 00165 NM 2008 3 18 2008UALA01319 1 20080309 A 3350 BATTERY PACK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 313UA 23674 FOUND CENTER EEL LIGHT INOPERATIVE. FOUND FAULTY BATTERY PACK. REPLACED FEEDER AND STRIP AND BATTERY OPS CHECK GOOD PER MM 33-51-92 MM 33-51-91 MM 33-51 -90. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800167 20080318 00167 NM 2008 3 18 2008UALA01325 1 20080309 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 EMERGENCY EXIT PATH LIGHTING IN FIRST CLASS IS LOOSE. SECURED LIGHT OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800169 20080318 00169 2008 3 18 2008UALA01328 4 20080310 A 3445 WARNING SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE TCAS INOPERATIVE A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 351UA 24319 FLIGHT DIVERTED TO DUE TO INOP TCAS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800170 20080318 00170 2008 3 18 2008UALA01331 4 20080310 A 2565 BOTTLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 LOW BOTTLE PRESSURE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800171 20080318 00171 EU 2008 3 18 2008UALA01332 1 20080310 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 489UA 1702 DENT BETWEEN STR 20L AND 21L 4 INCHES FWD OF FRAME 12. MAJOR REPAIR ACCOMPLISHED AT LCQ. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031800172 20080318 00172 EU 2008 3 18 2008UALA01339 1 20080311 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 457UA 1146 CREW O2 IS LOW AND NEEDS SERVICING. SERVICED CREW O2 TO FULL. NO LEAKS WERE NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031800176 20080318 00176 NM 2008 3 18 2008UALA01343 1 20080311 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 CABIN U-D ZN SEAT ROW 15AB,16AB EEL LIGHT NOT ON. REPLACED LAMP. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031800180 20080318 00180 NM 2008 3 18 2008UALA01350 1 20080310 A 3350 4877873 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 EMERGENCY LIGHT BAR AT MID RIGHT LAV IS DAMAGED. REPAIRED LIGHT STRIP OPS CHECK GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800182 20080318 00182 NM 2008 3 18 2008UALA01352 1 20080311 A 2560 WIRE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE GIRT BAR BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 769UA 26921 WHILE REMOVING SLIDE FOUND BREAK AWAY WIRE ON GIRT BAR LANYARD BROKEN. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008031800185 20080318 00185 2008 3 18 MASA200800224 4 20080312 A 2561 P01074201 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 693BR 3384 7761 ASH FLT 1040 HNL-ITO. SEAT 10A LIFE VEST WAS MISSING. MX INSTALLED A NEW LIFE VEST. 2 L 7 2 4F RT A21EA 2008031800190 20080318 00190 EU 2008 3 18 TRBA2008030 1 20080311 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU CABIN DISCHARGED A TRBA K NONE O OTHER UK UNKNOWN 1 SO 29 270AT 270 SEVERAL FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY 4 3WL IAW AMM JIC 33-51-21. OPS CHECKED OK IAW MM 33-50-00. 2 H 7 2 4T RT A53EU 2008031800197 20080318 00197 SO 2008 3 18 LR7A08029 1 20080128 A 5311 34004327 FRAME LKHEED 382 382G 526414U SO FUSELAGE BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 560 4606 DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5302, FOUND OVERHEAD RING SEGMENT BROKEN AT FS 477, WL260, LBL45. REPAIR ACC OMPLISHED BY REPLACING RING CHANNEL IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008031800201 20080318 00201 EA 2008 3 18 A6WA200840093 1 20080205 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 CRACK EXIST ON BRACKET FS 280, LBL 9, ABD RBL 9 CRACK LENGTH .200. (K) REPAIR PERFORMED IAW REO 601R-53-11-171, FABRIC ATED NEW ANGLE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031900002 20080319 00002 SO 2008 3 19 N93A22022008 1 20080222 A 3230 1159SCH23135 CONTROL VALVE GULSTM GVSP GVSPG550 3980203 SO MLG FAILED E N93A O OTHER J WARNING INDICATION LD LANDING 1 SO 13 518QS 5075 DURING GEAR EXTENSION FOR LANDING, NOSE LANDING GEAR FAILED TO EXTEND DURING FIRST ATTEMPT. SECOND ATTEMPT WAS SUCCESSF UL. DOOR CONTROL VALVE WAS ADJUSTED TO CORRECT PROBLEM. 2 L 7 2 4F RT A12EA 2008031700161 20080317 00161 NM 2008 3 17 HALA0800368 1 20080308 A 2841 FG1006AA15 METERING UNIT BOEING 767 76733A 1385209 NM FUEL SYS MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 904 904 25531 ETOPS SIGNIFICANT SYSTEM, LT FUEL QUANTITY INDICATION BLANK INTERMITTENTLY. ACCOMPLISHED FQUIS BITE PER FIM 28-41-00. SHOWED FAULT CODE 63. ACCOMPLISHED FIM 28-41-00 TABLE 127. E/E WET CAPACITANCE CHECKED GOOD. FQIS INSULATION RESISTAN CE TEST CHECKED GOOD. REMOVED AND REPLACED LEFT WING MAIN TANK UNIT NR 13 PER AMM 28-41-00. ACCOMPLISHED FQIS BITE AND NO FAULTS NOTED. LEAK CHECK OK. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008031700214 20080317 00214 WP 2008 3 17 ABXR080069 1 20080205 A 5511 9918419509 RIB DOUG DC9 DC933F 302207A WP LT HORIZ STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 LEFT HORIZONTAL STAB LEADING EDGE NR 3 FROM INBOARD RIB CRACKED. INSTALLED SINGLE STACK REPAIR IAW DC9 ABX DWG K05159. 2 L 7 2 4F A6WE 2008031700260 20080317 00260 CE 2008 3 17 DXTA200802797 1 20080125 A 3260 WARNING LIGHT BEECH MU300 400A 1155402 CE COCKPIT ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 138QS RK492 ON GEAR RETRACTION, RED LIGHT IN LANDING GEAR HANDLE REMAINED ILLUMINATED AND ALL GREEN LIGHTS EXTINGUISHED. CYCLED LAND ING GEAR DOWN AND ALL GREEN AND RED LIGHTS FUNCTIONED PROPERLY. RETRACTED GEAR AGAIN + RED GEAR HANDLE LIGHT REMAINED IL LUMINATED. 2 H 7 2 4F RT A16SW 2008031700271 20080317 00271 NM 2008 3 17 XXUA200800003 1 20080226 A 3397 WIRE BOEING 757 7572Q8 1384972 NM PWA PW2037 PW2037M 52117 NE CABIN LOOSE A XXUA K NONE L NO TEST IN INSP/MAINT 1 EA 15 403JS 27351 EMERGENCY EXTERIOR LIGHT AT DOOR R2 WILL NOT ILLUMINATE WHEN LIGHT SWITCH IS SELECTED. FOUND LOOSE WIRE AT ASSEMBLY TER MINAL, RESECURED WIRE. OPERATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031700275 20080317 00275 EA 2008 3 17 MASA200800193 1 20080308 A 5270 864202 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FAULTY A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 17175 9645 7175 ASH 7226 ORD-LAN - PAX DOOR MASTER WARNING MESSAGE IN FLIGHT. REMOVED AND REPLACED SWITCH S102MB AND REPAIRED WIRING, O PS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008031700289 20080317 00289 EU 2008 3 17 TRBA2008027 1 20080308 A 3350 3013000 POWER SUPPLY AEROSP ATR72 ATR72212A 8680902 EU CABIN FAILED A TRBA K NONE O OTHER TX TAXI/GRND HDL 1 SO 29 541AT 541 EMERGENCY LIGHTS (FLOOR) AND EMERGENCY EXIT LIGHTS OVERHEAD DOORS CABIN TO COCKPIT AND MAIN ENTRY CONTINUOUSLY ON WONT R ESET. REPLACED EMERGENCY LIGHTS POWER SUPPLY 62WL PER JIC 33-51-21 AND FOUND WORKING PROPERLY. 2 H 7 2 4T RT A53EU 2008031800013 20080318 00013 EU 2008 3 18 08FDEA00855 1 20080310 A 2550 A2557387100200 PANEL AIRBUS 310 A310203 3930313 EU AFT CARGO BAY DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT CARGO PIT PANEL NR 151PW IS DISBONDED. REPAIRED PANEL & APPLIED TOP COAT WHITE IAW DRAWING SRZ 25-013. 2 L 7 2 4F RT A35EU 2008031800023 20080318 00023 EU 2008 3 18 08FDEA00865 1 20080311 A 5320 SEAL DEPRESSOR AIRBUS 310 A310324 3930206 EU CARGO BAY DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FWD LWR CARGO PIT SEAL DEPRESSOR SCRATCHED AND WORN FWD AND AFT SIDES UPPER PORTION IN WORK. 2 L 7 2 4F RT A35EU 2008031800047 20080318 00047 NM 2008 3 18 HALA0800381 1 20080306 A 5730 SKIN BOEING 767 767332 1382001 NM RT WING CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 LEVEL 1 CORROSION ON RT WING LOWER SURFACE, STRINGER L15, BETWEEN RIBS 5 AND 7, CORROSION ON FASTENER HEADS. AREA PAINT STRIPPED IAW SOPM 20-30-02, REV 104. LIGHT CORROSION REMOVED FROM FASTENER HEADS BY GLASS BEADING IAW SRM 51-10-02, RE V 76, NEGLIGIBLE MATERIAL REMOVED. SURFACE PROTECTION APPLIED IAW AMM 51-20-10, REV 95. 2 L 7 2 4F RT A1NM 2008031800062 20080318 00062 EA 2008 3 18 MASA200800218 1 20080311 A 3530 E2818010 PBE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT OPEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75992 7401 ASH FLT 7149 IAD-BNA - CAPTAIN’S PBE WAS OPENED. MX REPLACED THE PBE. 2 L 7 2 4F RT A21EA 2008031800077 20080318 00077 EU 2008 3 18 08FDEA00898 1 20080312 A 5330 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT IF THE BULK PIT FROM FRAME 78 TO FRAME 79; STRINGER 50R TO STRINGER 51R INTERIOR SURFACE HAS CORROSION. R&R DOUBL ER LAV SERVICE DOOR; S50R & DRAIN MAST IAW 51-40-21 & AMM 30-71-11-4. REMOVED & REINSTALLED S45R; 47R; 48R FROM FRAMES 75-82& PAN IAW SRM 51-40-21. REMOVED CORROSION FROM DOUBLER & FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. ORIG MAT 0. 098; REMAINING MAT 0.054; REMAINING MAT 0.044. REMOVED CORROSION FROM S50R & FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00 . ORIG MAT .039; REMAINING MAT 0.000; REMOVED MAT 0.039. FABBED DOUBLER S50R IAW DWG A5398067 & A53980908. TREATED IA W SRM 51-21-10 & 51-23-10. 2 L 7 2 4F RT A35EU 2008011800119 20080118 00119 NM 2008 1 18 NWAA080105527 1 20080115 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 527US 23842 PILOT REPORTED EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED FORWARD BATTERY PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2008011800128 20080118 00128 NM 2008 1 18 QXEA200800027 1 20080110 A 3010 85520259005 HEATER DHAV DHC8 DHC8202 2809007 NM ELEVATOR HORN INOPERATIVE A QXEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 09 352PH 12688 494 BOI - FLIGHT 2192 (BOI-LWS), RIGHT ELEVATOR HORN HEAT INOP. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING . MAINTENANCE REPLACED THE ELEVATOR HORN HEAT UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008011800131 20080118 00131 EA 2008 1 18 QXEA200800029 1 20080113 A 5240 ROLL PIN CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 615QX 10065 SEA - FLIGHT 2536 - SERVICE DOOR WILL NOT CLOSE. MAINTENANCE REPLACED THE ROLL PIN FOR THE DOOR. OPERATIONAL CHECKS GO OD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008011800133 20080118 00133 NM 2008 1 18 QXEA200800026 1 20080109 A 3234 483003 SELECTOR BOMBDR DHC8 DHC8402 1390042 NM LT MLG MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 409QX 4076 4051 RNO - FLIGHT 2256 (RNO-SEA), CLIMBING FROM RENO (40 NM) THE LEFT MAIN GEAR DOOR CYCLED. RETURNED TO THE FIELD AND ACCOM PLISHED A UNEVENTFUL LANDING. FERRIED THE AIRCRAFT TO PDX FOR REPAIRS. IN PDX, REPLACED THE LANDING GEAR SELECTOR. OP ERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008011800134 20080118 00134 NM 2008 1 18 QXEA200800028 1 20080111 A 3010 4100S005003 VALVE BOMBDR DHC8 DHC8402 1390042 NM DEICE DISTRIB MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 09 406QX 6394 1010 4048 BZN - FLIGHT 2311 (BZN TO SEA), RECEIVED A DE-ICE PRESSURE CAUTION FOR THE H-STAB BOOT. DIVERTED TO PASCO AND ACCOMPLIS HED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE NR 5 DISTRIBUTOR VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008012200002 20080122 00002 SW 2008 1 22 EAC0705 1 20080103 A 2613 434422122 OVERHEAT SENSOR SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT WING DEFECTIVE E DUFA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 27 159MC AC728B WHILE ON CLIMB OUT, THE PILOT NOTICED THAT THE LT WING OVERHEAT LIGHT ILLUMINATED. FOLLOWING PROCEDURE, THE LT GENERATOR WAS SHUTDOWN, BLEED AIR TURNED OFF AND THE LANDING GEAR EXTENDED. AFTER 3 MINUTES THE LIGHT WAS STILL ILLUMINATED AND P ROCEDURES CALL OUT FOR ENGINE SHUTDOWN. SHORTLY AFTER ENGINE SHUTDOWN THE LIGHT EXTINGUISHED. THE PILOT INFORMED THE TOW ER OF HIS SITUATION AND WAS CLEARED TO RETURN TO DEPARTURE, WHERE HE MADE AN UNEVENTFUL LANDING. UPON INVESTIGATION, NO EVIDENCE OF FIRE OR OVERHEATING COULD BE FOUND IN THE WING AND GEAR WELL AREAS. IT IS SUSPECTED THAT DUE TO HIGH WINDS D URING THE PILOT’S BACK TAXI TO THE ACTIVE RUNWAY, HE MAY HAVE HAD TO APPLY CONSTANT BRAKE PRESSURE TO KEEP HIS TAXI SPEE 2 L 7 2 4T 4 T RT A8SW E4WE 2008022500367 20080225 00367 EU 2008 2 25 USAA920080422 1 20080210 A 5347 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 271AY 323 BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 5478 / FR 70, +Y450. REPLACED CABIN SEAT TRACK, BS 54 78 / FR 70, +Y450 IAW A330 SRM 51-42-00. 2 L 7 2 4F RT A46NM 2008022500379 20080225 00379 EU 2008 2 25 USAA920080378 1 20080125 A 5320 D53471124201 SHEAR PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AW 543 SAL - MAJOR REPAIR - C8 CHECK - CORROSION ON CABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, -Y1250. REPLACED CA BIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, -Y1250 IAW A320 SRM 51-72-11. *SUPPLEMENT* CORRECTED REGISTRATION NUMBER FROM 334AW TO 605AW. 2 L 7 2 4F RT A28NM 2008022500382 20080225 00382 SO 2008 2 25 FDKA200802058 1 20080214 A 5210 DOOR EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF RIG A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6083 MCO (6075 PHX LCL). MAIN CABIN DOOR DIFFICULT TO OPEN. MX RIGGED DOOR, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008022500388 20080225 00388 NM 2008 2 25 USAA920080434 1 20080217 A 2560 284N1420 PROXIMITY SWITCH BOEING 757 7572B7 1384964 NM L1 GIRT BAR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 202UW 27811 BFM - EES - C4 CHECK - SLIDE LIGHT INOPERATIVE ON ALL DOORS. REPLACED AND OPERATIONAL CHECKED THE L1 DOOR GIRT BAR PROX IMITY SWITCH IAW B757 AMM 25-66-11. 2 L 7 2 4F RT A2NM 2008022600053 20080226 00053 NM 2008 2 26 AALA200800329 1 20080125 A 5313 STRINGER BOEING 767 767223 1385123 NM BS 1300 S37L CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 324AA 22325 AFW - STRINGER 37L AT STATION NUMBER 1300 WAS CORRODED JUST FORWARD OF A PRODUCTION SPLICE. FABRICATED AND INSTALLED EX TENDED SPLICE. 2 L 7 2 4F RT A1NM 2008022600056 20080226 00056 NM 2008 2 26 BB08020 1 20080216 A 2782 5006397R ROTARY ACTUATOR BOEING 757 7572S7 1384962 NM L/E SLAT BINDING A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 905AW 28946 20759 23567 HNL - FLT20 - DURING APPROACH TO HNL FROM PHX, CREW RECEIVED A "LE SLAT DISAGREE" LIGHT AT FIRST SELECTION OF FLAPS FOR ARRIVAL. CREW ACCOMPLISHED QRH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED FIM 27-81-00 THRU ITEM 1B . SYSTEM CHECKED OK. NO FAULTS OR MESSAGES. ADDITIONAL FOLLOW-UP REVEALED 5 SLAT ROTARY ACTUATORS WITH TRIPPED TORQUE LIMITER INDICATORS AT POSITIONS 4, 8, 9, 11 AND 20. MAINTENANCE REMOVED AND REPLACED POSITIONS 4, 8, 9, 11 AND 20 SLAT ROTARY ACTUATORS. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 2008022600062 20080226 00062 EU 2008 2 26 USAA920080440 1 20080131 A 5320 D53480020697 SHEAR PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AW 543 SAL - MAJOR REPAIR - C8 CHECK - CRACKED CABIN TRAY / SHEAR PLATE, BS 3257 / FR 68, -Y1732. REPLACED CABIN TRAY / SHEAR PLATE, BS 3257 / FR 68, -Y1732 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022600072 20080226 00072 NM 2008 2 26 ASAA0842586 1 20080117 A 5320 69412609 STIFFENER BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 CORROSION ON VERTICAL STIFFENER AT BS 344 AND STR 28 RT. VERTICAL STIFFENER REPLACED. 2 L 7 2 4F RT A16WE 2008022600092 20080226 00092 NM 2008 2 26 ASAA0842566 1 20080114 A 5311 654655055 FRAME BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT BS 787 BODY FRAME SKIN ATTACHMENT CRACKED AT STR 27R DUET. CORROSION REPAIR BODY FRAME TO SKIN ATTACHMENT ON AFT CARGO PIT. BS 787 STR 27R IAW B737 400 SRM 53 00 07 FIG 201. 2 L 7 2 4F RT A16WE 2008031800110 20080318 00110 NM 2008 3 18 2008UALA00030 1 20080102 A 3830 DUMP VALVE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LAVATORY OBSTRUCTED A UALA A UNSCHED LANDING W K INADEQUATE Q C FLUID LOSS CR CRUISE 1 WP 29 341UA 24245 FLIGHT DIVERTED DUE TO FORWARD LAVATORY OVERFLOW. FOUND FOREIGN OBJECT IN DUMP VALVE ALLOWING FLUID TO BYPASS VALVE. R EMOVED OBJECT. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800120 20080318 00120 EU 2008 3 18 2008UALA01257 1 20080307 A 3397 WIRE HARNESS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 418UA 485 ROWS 14 ABC AND 21 ABC EMERGENCY PATHWAY LIGHT ON SEATS ARE INOP. UNKNOWN DAMAGE TO HARNESS. REPLACE HARNESSES AT SEVE RAL POINTS. ALL OPS CHECKS PERFORMED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031800129 20080318 00129 NM 2008 3 18 2008UALA01277 1 20080308 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FWD GALLEY DOOR SURROUND BS 277 STR 15R HAS STRINGER CLIP CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED & INSTALLED NEW C LIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800131 20080318 00131 NM 2008 3 18 2008UALA01279 1 20080308 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 CABIN FLOORBEAM BS 864 UPPER CAP CORRODED AT FASTENER HOLE FOR EVAC SLIDE HOLD DOWN FITTING RBL 44 INCH. MAJOR REPAIR AC COMPLISHED: FABRICATED & INSTALLED UPPER CAP FLOORBEAM REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800133 20080318 00133 NM 2008 3 18 2008UALA01282 1 20080308 A 4940 STARTER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE APU FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 APU WILL NOT START, FAULTS STARTER. REPLACED APU BATTERY PER MM24- 31-04 AND REPLACED STARTER MOTOR PER MM49-41-01. OPS CHECK OK. VERIFICATION FLIGHT CONFIRMS NORMAL OPERATION OF THE SUBJECT SYSTEM. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800151 20080318 00151 EU 2008 3 18 2008UALA01303 1 20080309 A 5210 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 460UA 1248 DOOR 2R EMERGENCY DOOR ASSIST BOTTLE PRESS LOW. SERVICED BOTTLE TO FULL, NO LEAKS NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031800177 20080318 00177 NM 2008 3 18 2008UALA01344 1 20080311 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 CABIN 'E' ZONE RT AFT COLUMN EEL LIGHT NOT. REPLACED LAMP. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031800199 20080318 00199 SO 2008 3 18 LR7A08031 1 20080227 A 5312 34258224R CAP LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2299 5025 DURING SCHEDULED C-7 CHECK, PER JOB CARD HC5315, FOUND RT BHD INBD CAP CRACKED AT FS 880, WL192, RBL 65. REPAIR ACCOMPL ISHED IAW SMP583 FIG 53-50-17. 2 H 7 4 4T A1SO 2008031800200 20080318 00200 EA 2008 3 18 A6WA200840092 1 20080205 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 CRACK EXIST ON FLOOR STRUCTURE FS 280, RBL 9 CRACK LENGTH .150. (K) CUT OUT DAMAGE IAW REO 601R-53-11-171. REPAIR PER FORMED IAW REO 601R-53-11-171. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031900010 20080319 00010 SO 2008 3 19 SWIA200819328 1 20080305 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 215SW 120281 FLT 5747 - EMERGENCY EXIT SIGN OVER SEAT 9B INOP. REPAIRED WIRING AT LIGHT ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008031900011 20080319 00011 EA 2008 3 19 SWIA200819329 1 20080305 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 935SW 7725 FLT 6753 - A SECTION OF EMERGENCY FLOOR LIGHTS ARE INOP. RESECURED CONNECTOR ON FLOOR STRIP. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008031900012 20080319 00012 SO 2008 3 19 SWIA200819330 1 20080309 A 2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203 SO LAVATORY FAULTY A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 237SW 120314 FLT 5778 - LAV FIRE ALARM IS ACTIVATING INTERMITTENTLY. REPLACED LAV SMOKE DETECTOR. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008031900014 20080319 00014 CE 2008 3 19 GUUA01310801 1 20080131 A 5260 CAM BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE AIRSTAIR DOOR OUT OF ADJUST A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87554 UE227 AT SCHEDULED INSPECTION, DISCOVERED AIRSTAIR DOOR WILL NOT LATCH WHEN CLOSED. ADJUSTED CAM ON DOOR. 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900017 20080319 00017 CE 2008 3 19 GUUA02070801 1 20080207 A 5220 1294300451 DOOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE EMERGENCY EXIT DELAMINATED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 29 53545 UE185 FLIGHT: 5402, PILOT REPORTED LT EMERGENCY EXIT IS DELAMINATED. REPLACED LT EMERGENCY EXIT. 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900018 20080319 00018 CE 2008 3 19 GUUA02060801 1 20080206 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT MLG BYPASSING A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 29 53545 UE185 FLIGHT: 9149, DURING FLIGHT DC LOAD METERS BOTH SPIKE 20 PERCENT EVERY 20 SECONDS. REPLACED THE RT MLG ACTUATOR. 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900019 20080319 00019 SO 2008 3 19 GUUA02120801 1 20080212 A 3350 AGC1 FUSE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHTS BLOWN A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 285AS 120265 FLIGHT:5454, PILOT REPORTED BOTTOM EXTERNAL EMERGENCY LIGHT DOES NOT WORK ON BOTH SIDES OF AC. REPLACED EMERGENCY LIGHT FUSES. 2 L 7 2 4T 4 T RT A31SO E20NE 2008031900021 20080319 00021 CE 2008 3 19 GUUA02090801 1 20080209 A 5220 1295140351 LATCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE EMERGENCY EXIT BROKEN A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 38537 UE158 DURING SCHEDULED ROUTINE MAINT, DISCOVERED RT AFT EMERGENCY EXIT DOOR TOP CAM BROKEN. REPLACED EMERGENCY EXIT ARM LATCH ASSY. 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900026 20080319 00026 CE 2008 3 19 GUUA03010801 1 20080301 A 5520 1016200131 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 38537 26008 UE158 DURING SCHEDULED ROUTINE MAINT DISCOVERED LT CTR ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR CENTER HINGE B RACKET. 2 L 7 2 4T 3 T RT A24CE E2NE 2008031900027 20080319 00027 CE 2008 3 19 GUUA03010802 1 20080301 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 38537 7008 UE158 DURING SCHEDULED ROUTINE MAINT, DISCOVERED LT ELEVATOR OB HINGE BRACKET EXFOLIATED. REPLACED LT ELEVATOR OB HINGE BRACK ET. 2 L 7 2 4T 3 T RT A24CE E2NE 2008031900035 20080319 00035 CE 2008 3 19 GUUA03090802 1 20080309 A 3260 1003810061 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NLG SHORTED A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 81533 UE137 FLIGHT: 9201, DURING FLIGHT, LANDING GEAR HANDLE LIGHT ILLUMINATED WITH LANDING GEAR RETRACTED. INSTALLED UPLOCK SWITCH AND RIGGED UP AND DOWNLOCK SWITCHES FOR THE NOSE LANDING GEAR. 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900041 20080319 00041 NM 2008 3 19 TAMF20080006S 1 20080225 A 5751 WEB BOEING 767 767200 1385120 NM LT AILERON CHAFED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 769QT 23801 DURING C CHECK INSPECTION, FOUND CLOSURE RIB WEB WITH CHAFING OUT OF LIMITS AT LT WING INBOARD AILERON. DAMAGED AREA WA S REPAIRED IAW EWO 767-57-033 AND BOEING SERVICE REQUEST 1-773827820. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F RT A1NM 2008031900043 20080319 00043 NM 2008 3 19 TAMF20080007S 1 20080218 A 5330 SKIN BOEING 767 767200 1385120 NM FUSELAGE CHAFED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 769QT 23801 DURING C CHECK INSPECTION, FOUND SKIN WEAR ON RUB STRIPS, STA 1725.5 STRINGER 22RH. DAMAGED AREA WAS REPAIRED IAW EWO 7 67-53-070 AND BOEING SERVICE REQUEST 1-773844480. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F RT A1NM 2008031900044 20080319 00044 NM 2008 3 19 TAMF20080008S 1 20080227 A 7830 FITTING BOEING 767 767200 1385120 NM THRUST REVERSER CRACKED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 769QT 23801 DURING C CHECK INSPECTION, FOUND THRUST REVERSER FITTING POS 4 O'CLOCK CRACKED. DAMAGED AREA WAS REPAIRED IAW EWO 767-5 4-032 AND IAAC TAC-080227. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F RT A1NM 2008031900047 20080319 00047 CE 2008 3 19 DXTA200802801 1 20080127 A 3297 TERMINAL RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP LOOSE E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 845QS 258545 AFTER T/O, AFTER RETRACTING GEAR, THE STALL IDENT,SQUAT,R GEAR LIGHTS CAME ON. TIGHTENED TERMINAL KKR7 ON PANEL TBKK IAW RAC DWG. 25-8NAS-2584. OPS CHECK GOOD. REF WO: 07-19-1635-1.2 2 L 7 2 4F 4 F RT A3EU E6WE 2008031900048 20080319 00048 NM 2008 3 19 TAMF20080009S 1 20080226 A 7830 491B1330014003 FRAME BOEING 767 767200 1385120 NM THRUST REVERSER CRACKED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 769QT 23801 DURING C CHECK INSPECTION, FOUND CRACK DAMAGE AT FRAME P/N 491B1330014-003 AT 5 O’CLOCK POSITION OF THRUST REVERSER P/N 681L272G07 (RT). DAMAGED AREA WAS REPAIRED IAW EWO 767-54-031 AND IAAC TAC-080226. FAA FORM 8110-3 WAS ISSUED APPROVIN G THIS REPAIR. THIS REPAIR IS A TEMPORARY REPAIR AND THE AFFECTED FRAME SHOULD BE CHANGED AT NEXT MAJOR INSPECTION (C C HECK). 2 L 7 2 4F RT A1NM 2008031900049 20080319 00049 NM 2008 3 19 TAMF20080010S 1 20080301 A 5754 SLAT BOEING 767 767200 1385120 NM WING DAMAGED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 769QT 23801 DURING CHECK INSPECTION WAS FOUND A BIRD STRIKE ON SLAT 12. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-037 AND IAAC TAC-0 80225 REPAIR ORDER. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F RT A1NM 2008031900050 20080319 00050 CE 2008 3 19 DXTA200802803 1 20080128 A 3260 WARNING LIGHT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 665QS 5605165 HYD PRESS LIGHT REMAINED ILLUMINATED FOLLOWED BY THE STAB MISCOMPARE. (2)-POSITION TAIL SYS, OPS CHECK GOOD. STAB LIGHT DUE TO EXTENDED TRAVEL TIME FROM FLAPS, UP TO FLAPS DOWN DURING EMERGENCY GEAR INDICATION DURING TAKEOFF IAW MM CHAP. 2 7-40-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008031900053 20080319 00053 CE 2008 3 19 DXTA200802806 1 20080128 A 2612 FIRE LOOP CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LT NACELLE OUT OF POSITION E DXTA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 613QS 5605599 AT 34.0 FT IB TO MSP LT ENGINE, ENGINE FIRE LIGHT BLINKED ON AND OFF ABOUT 10 TIMES A MIN FOR 10 MIN INSPECTED LT ENGINE FIRE LOOP CONNECTIONS. INSPECTED FIRE LOOP AND FOUND CONTACTING LINE FROM FUEL/OIL HEAT EXCHANGER. REPOSITIONED FIRE LO OP TO MAINTAIN CLEARANCE IAW AMM 26-11-01. PERFORMED SYS TEST IAW AMM 26-11-00. SYSTEM CHECK IAW PROCEDURE. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008031900056 20080319 00056 NM 2008 3 19 MWEA080038 1 20080304 A 2530 OVEN BOEING 717 717200 1383700 NM GALLEY DIRTY A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 13 920ME 55182 SMOKE STARTED COMING OUT OF THE NR 2 OVEN. FOUND FOOD IN BACK OF OVEN CAUSING THE SMOKE. CLEANED FOOD OFF OVEN AND SWA PPED OVEN CONTROL MODULES FROM NR 1 TO NR 2 OVEN TIMER KNOB, NOW CHECKED GOOD. 2 L 7 2 4F TR A6WE 2008022600110 20080226 00110 NM 2008 2 26 ASAA0842576 1 20080106 A 5347 655384110 CARGO TRACK BOEING 737 7374S3 1384711 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT LEFT TIE DOWN TRACK FOUND CORRODED ON LUG AT BS 847 LBL 17. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600118 20080226 00118 NM 2008 2 26 ASAA0842587 1 20080125 A 5320 65C335335 SUPPORT BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 SURFACE CORROSION UNDER FLOORBOARD 24794 ATTACH HOLES CORRODED. SUPPORT TEE UNDER FLOORBOARD REPLACED. 2 L 7 2 4F RT A16WE 2008022600133 20080226 00133 NM 2008 2 26 ASAA0842626 1 20080114 A 5320 694147317 INTERCOSTAL BOEING 737 7374S3 1384711 NM FUSELAGE BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO PIT INTERCOSTAL IS BENT BS 440 460 LBL 25. REPLACED WITH MADE REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600135 20080226 00135 NM 2008 2 26 ASAA0842618 1 20080125 A 5754 65C26602282 PANEL BOEING 737 7374S3 1384711 NM L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 NR 5 SLAT INBOARD END COVE PANEL INNER SURFACE AT END CAP LOCATION CHAFING DAMAGE. ON NR 5 SLAT INBOARD END COVE PANEL INNER SURFACE AT END CAP REPAIR IAW B737 400 SRM 57 43 01 FIG 201. 2 L 7 2 4F RT A16WE 2008022600144 20080226 00144 EU 2008 2 26 USAA920080436 1 20080213 A 5347 D53472190202 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN RAIL SEAT BEAM, BS 3101 / FR 65, +Y765. REPLACED CABIN RAIL SEAT BE AM, BS 3043 / FR 64 - BS 3158 / FR 66, +Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022600183 20080226 00183 NM 2008 2 26 2008UALA00827 1 20080213 A 3350 OL3071BPEGPL BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMEGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 570UA 26678 DOOR 2 LEFT EXTERIOR EMERGENCY LIGHT IS INOP. FOUND BULB OUT. RELAMPED BULB, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022600214 20080226 00214 NM 2008 2 26 ASAA0842647 1 20080110 A 5311 65C329621 FRAME BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT MAIN FRAME AT BS 727 G STR 24R 25R FOUND CORRODED. AFT CARGO PIT MAIN FRAME AT BS 727G REPAIRED IAW B737 400 SRM 51 70 11. 2 L 7 2 4F RT A16WE 2008022600235 20080226 00235 WP 2008 2 26 AMTA200800025 1 20080119 A 3397 WIRE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL CABIN BROKEN A AMTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 11 702TZ 46912 AFTER LANDING, FOUND EMERGENCY LIGHTS OVERHEAD CIRCUIT BREAKER (D-4) POPPED. WILL NOT RESET. FOUND BROKEN WIRE LEADING TO OVERWING EMERGENCY LIGHTS BATTERY POWER SUPPLY. REPAIRED IAW SWP EMERGENCY LIGHT. OPS CHECKS NORMAL. (K) 2 L 7 3 4F 4 F A22WE A23EA 2008022600257 20080226 00257 NM 2008 2 26 AMTA200800047 1 20080202 A 2560 GLOWSTRIP BOEING 737 73783N 13844HI NM CABIN PEELING A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 305TZ 30706 AT ROW 16 AND 17 ABC PHOTOLUMINESCENT STRIP PEELING UP. REMOVED AND REPLACED PHOTO LUMINESCENT STRIP AT ROW 16 AND 17 A BC IAW 35-51-15-2. (K) 2 L 7 2 4F RT A16WE 2008022600277 20080226 00277 NM 2008 2 26 AMTA200800054 1 20080205 A 4997 WIRE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE CARGO BAY BROKEN A AMTA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 518AT 27974 APU FAULT LIGHT ILLUMINATED AND EICAS APU FUEL VALVE MESSAGE DISPLAYED. FOUND WIRE W2658-001-20 UNDER AFT CARGO PIT FLO OR BROKEN. REPAIRED BROKEN WIRE WITH SPLICES IAW SWP 20-30-12. OPS CHECK GOOD. NO FAULT NOTED. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008022600278 20080226 00278 NM 2008 2 26 AMTA200800055 1 20080205 A 4930 VALVE BOEING 757 75723N 1384973 NM APU MALFUNCTIONED A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 514AT 27971 EICAS MSG, APU FUEL VALVE. FAULT LIGHT ILLUMINATED. UNABLE TO START APU. CYCLED APU FUEL VALVE IAW FIM 49-11-00, FIG 104 APU. OPS NORMAL. (K) 2 L 7 2 4F RT A2NM 2008022700026 20080227 00026 WP 2008 2 27 IXXA08SMN015S 1 20080115 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND LT WING UPPER SKIN CORRODED AROUND FASTENERS AT STATION XRS 358.000 -371.000, S TRINGER 5 TO STRINGER 8. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMO VED DAMAGE AREA. FABRICATED REPAIR DOUBLER AND FILLER PLUG. TAPERED BOTH SIDES OF REPAIR DOUBLER. PERFORMED NDT INSPE CTION. NO CRACK, OR CORROSION FOUND. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 57-2-1 FIGURE 29, SRM 51-1-20D, SRM 51-1-8 PAGES 17-18, SRM 57-2-0 PAGE 16, NDT SPM PART 06-10-01-0 01, SRM 51-1-12 PAGE 7, AND SRM 51-3-1. 2 L 7 4 4F 4A25 2008022700039 20080227 00039 EA 2008 2 27 COMA0870119 1 20080210 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 969CA 7141 FLIGHT 4963 - RECEIVED FLAP FAIL CAUTION MESSAGE. ABORTED APPROACH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPL IED WITH SI-2-27I0001 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, FLAP SYSTEM WAS RESET WITH NO FURTHER MESSA GES. 2 L 7 2 4F RT A21EA 2008022700040 20080227 00040 EA 2008 2 27 COMA0860120 1 20080210 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 814CA 7387 FLIGHT 5441 - RECEIVED FLAP FAIL CAUTION MESSAGE ON APPROACH. EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. COMPLIED WI TH SI-2-2710001 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2008022700041 20080227 00041 EA 2008 2 27 COMA0860121 1 20080210 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 821CA 7420 FLIGHT 5275 - RECEIVED FLAP FAIL CAUTION MESSAGE ON APPROACH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WIT H SI-2-2710001 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2008031900062 20080319 00062 EU 2008 3 19 TRAX200800368 1 20080303 A 3350 LIGHT AEROSP ATR72 ATR72 EU PAX DOOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 641AS 387 PAX DOOR LIGHT DOES NOT WORK. 2 H 7 2 4T RT 2008031900065 20080319 00065 EA 2008 3 19 TRAX200800371 1 20080304 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 972EV 7534 RIGHT OBLIQUE ANGLE BRACKET IN WEB IS CRACKED. REMOVED RT OBLIQUE ANGLE, DISCARDED. DUPLICATED NEW ANGLE, LOCATED HO LES, DEBURRED, ALODINED, PRIMED/TOPCOAT AND INSTALLED WET WITH LOCK FASTENER PINS, TOPCOAT APPLIED, REWORK ACCAMPLISHED IAW SRM 53-61-17, 51-21-11, 51-42-21, 51-25-06, 51-25-16, AND 51-23-00. NEW ANGLE P/N S6144A33 2 L 7 2 4F RT A21EA 2008031900070 20080319 00070 EA 2008 3 19 TRAX200800378 1 20080305 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 916EV 7757 RIGHT EMERGENCY EXIT DOOR LOWER FWD EXIT SIGN LIGHT BURNT OUT. 2 L 7 2 4F RT A21EA 2008031900071 20080319 00071 EA 2008 3 19 TRAX200800379 1 20080306 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 823AS 7196 FLAP FAIL, EMERGENCY TRUCKS ON STANDBY. 2 L 7 2 4F RT A21EA 2008031900076 20080319 00076 NM 2008 3 19 KCSA081148 1 20080307 A 5313 STRINGER BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 STA 1240 TO STA 1260 STR 4L HAS CORROSION AROUND FASTENERS. 2 L 7 4 4F RT A20WE 2008031900077 20080319 00077 NM 2008 3 19 KCSA081150 1 20080307 A 5313 STRINGER BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 STA 1180 STR 4L HAS CORROSION AROUND FASTENERS. 2 L 7 4 4F RT A20WE 2008031900078 20080319 00078 NE 2008 3 19 DXTA200802794 2 20080124 A 7200 3051700 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15* 52060 NE NR 1 VIBRATION E DXTA A UNSCHED LANDING B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CL CLIMB 1 GL 07 303QS 6214 5600343 PCE500027 WHEN INCREASING POWER TO INITIATE CLIMB FROM 17000FT WE ENCOUNTERED LOUD NOISE FOLLOWED BY STRONG ODOR. REMOVED AND REP LACED NR1 ENGINE WITH REPAIRED UNIT IAW MM 71-01-02. OPS AND LEAK CHECKS GOOD. (FOR DETAILS REFER TO WO NR 030453) 2 L 7 2 4F 4 T RT A22CE E1NE 2008031900079 20080319 00079 NM 2008 3 19 KCSA081151 1 20080307 A 5313 STRINGER BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 STA 1005 STR 4L HAS CORROSION AROUND FASTENERS. 2 L 7 4 4F RT A20WE 2008031900081 20080319 00081 NM 2008 3 19 KCSA081152 1 20080307 A 5524 ATTACH FITTING BOEING 747 747209B 138489B NM RT ELEVATOR CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 RIGHT I/B ELEV POWER PACK ATTACH UPPER FITTINGS HAS CORROSION. 2 L 7 4 4F RT A20WE 2008031900083 20080319 00083 NM 2008 3 19 KCSA081153 1 20080307 A 5313 STRINGER BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 STA 1480 STR 4L HAS CORROSION. 2 L 7 4 4F RT A20WE 2008031900087 20080319 00087 NM 2008 3 19 KCSA081155 1 20080307 A 5320 STRAP BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 LEFT STABILIZATION STRAP CRACKED 1 INCH BETWEEN STA 1720 TO STA 1740. 2 L 7 4 4F RT A20WE 2008031900089 20080319 00089 NM 2008 3 19 KCSA081149 1 20080307 A 5313 STRINGER BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 STA 1470 STR 4L HAS CORROSION AROUND FASTENERS. 2 L 7 4 4F RT A20WE 2008031900091 20080319 00091 NM 2008 3 19 KCSA081158 1 20080308 A 5320 STIFFENER BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 LOWER BILGE FUSELAGE FRAME VERTICAL STIFFENER IS CORRODED AT STA 2220, LBL 40. 2 L 7 4 4F RT A20WE 2008031900092 20080319 00092 NM 2008 3 19 KCSA081159 1 20080309 A 5522 SKIN BOEING 747 747209B 138489B NM LT ELEVATOR CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 LEFT O/B ELEVATOR L/E UPPER SURFACE CHAFING AT ELEV STA 231. 2 L 7 4 4F RT A20WE 2008031900094 20080319 00094 NM 2008 3 19 KCSA081161 1 20080309 A 5313 LONGERON BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 LEFT BODY MLG W/W LONGERON CRACKED AT BS 1480 BELOW THE OVERWING LONGERON EXTENSION FITTING. 2 L 7 4 4F RT A20WE 2008022700061 20080227 00061 NM 2008 2 27 UIEA200800050 1 20080215 A 5313 BAC14981327075 STRINGER BOEING 747 7472D7B 1384803 NM BS 2240 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 AFT AND BULK CARGO COMPARTMENTS STA 2240 LEFT SIDE STRINGER 50 FOUND CRACKED. STRINGER REPAIRED PER 53-10-03. 2 L 7 4 4F RT A20WE 2008022700068 20080227 00068 NM 2008 2 27 UIEA200800026 1 20080202 A 5330 SKIN BOEING 747 747243B 1384830 NM PAX DOORWAY CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 MAIN ENTRY DOOR L-1, EXTERIOR LOWER HINGE CUT-OUT, PREVIOUS DOUBLER REPAIR, LOWER CORNER IS CRACKED AT STA 452.5 L. REM OVED CRACKED DOUBLER, FABRICATED NEW DOUBLER AS PER SB 747-52-2144 REV 2. VERIFIED STOP DRILLED ENDED CRACK USING HFEC INSP. AS PER 747 NDT MANUAL PART 6, 51-00-00 FIG 23. INSTALLED NEW DOUBLER AS PER SB 747-52-2144 REV 2 REF EO 4752A130. 2 L 7 4 4F RT A20WE 2008022700099 20080227 00099 NM 2008 2 27 SWAA080908 1 20080218 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700100 20080227 00100 NM 2008 2 27 SWAA080909 1 20080215 A 5754 65C26602224 SLAT BOEING 737 7375H4 138449D NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED NR 5 SLAT PER MM. 2 L 7 2 4F RT A16WE 2008022700101 20080227 00101 NM 2008 2 27 SWAA080902 1 20080218 A 5754 65C26601 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED A1 CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT INBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008022700103 20080227 00103 2008 2 27 SWAA080884 4 20080214 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 725SW 27857 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008022700104 20080227 00104 NM 2008 2 27 SWAA080917 1 20080217 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 246LV 32507 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008022700107 20080227 00107 NM 2008 2 27 SWAA080931 1 20080219 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022700108 20080227 00108 NM 2008 2 27 SWAA080930 1 20080219 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022700112 20080227 00112 NM 2008 2 27 SWAA080949 1 20080219 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700116 20080227 00116 NM 2008 2 27 SWAA080938 1 20080219 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2008022700117 20080227 00117 NM 2008 2 27 SWAA080939 1 20080218 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN DEFECTIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 485WN 32473 L1 DOOR EMERGENCY EXIT LIGHT COVER FELL OFF. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008022700118 20080227 00118 NM 2008 2 27 TSAA0832009 1 20080218 A 2910 65447314 VALVE BOEING 737 7372T4 1384492 NM HYD SYSTEM LEAKING A TSAA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 WP 13 808AL 23445 NON-ETOPS FLIGHT 88 HNL-KOA, DURING TAKEOFF, THE CREW NOTED THE HYDRAULIC QUANTITY DROP FROM 3 GALLONS TO LESS THAN 1 GA LLON. THE CREW ELECTED TO ABORT THE TAKEOFF AT LESS THAN 80 KNOTS INDICATED AIRSPEED. MAINTENANCE FIRST REPLACED A LEA KING O-RING SEAL ON THE A SYSTEM BRAKE AUGMENTATION VALVE AND SERVICED THE HYDRAULIC RESERVOIR. MAINTENANCE THEN DECIDE D TO REMOVE AND REPLACE THE BRAKE FEEL AUGMENTATION VALVE PER AMM 32-41-00 WITH ALL OPERATIONAL AND LEAK CHECKS SATISFAC TORY. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A16WE 2008022700120 20080227 00120 NM 2008 2 27 SWAA080944 1 20080219 A 5753 65464291 ATTACH FITTING BOEING 737 7373TO 138447G NM FLAP TRACK CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND LT WING OUTBOARD FORE FLAP TRACK ATTACH FITTING CORRODED. 2 L 7 2 4F RT A16WE 2008022700124 20080227 00124 NM 2008 2 27 ASAA0842594 1 20080106 A 5320 69417579 INTERCOSTAL BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO PIT FLOOR SUPPORT INTERCOSTAL CORRODED BS 500F TO 500G LBL 24. INTERCOSTAL REPLACED. 2 L 7 2 4F RT A16WE 2008022700127 20080227 00127 NM 2008 2 27 ASAA0842637 1 20080116 A 5347 654681350 SEAT TRACK BOEING 737 7374S3 1384711 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 SEAT TRACK GOUGED BS 500D TO 500E RBL 45. REPLACED WITH MADE REPAIR PART. 2 L 7 2 4F RT A16WE 2008022700132 20080227 00132 NM 2008 2 27 TSAA0829008 1 20080215 A 2910 AE2460010H0180 HOSE BOEING 737 737282C 13844AU NM HYD SYS FAILED A TSAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 13 826AL 23051 NON-ETOPS FLIGHT 215 HNL-LIH, DURING CRUISE FLIGHT, THE CREW NOTED THE HYDRAULIC QUANTITY GAUGE DROPPED TO ZERO. CREW C OMPLETED THE HYDRAULIC SYSTEM A FAILURE CHECKLIST AND DECLARED AN EMERGENCY. THE CREW RETURNED TO HNL WITHOUT FURTHER I NCIDENT. MAINTENANCE TOWED THE AIRCRAFT FROM RUNWAY 8L AFTER ARRIVAL. THE A SYSTEM LT REAR SPAR HYDRAULIC HOSE ASSEMBL Y WAS REPLACED. ALL OPERATIONAL AND LEAK CHECKS SATISFACTORY PER AMM 29-11-0 PG 201. THE AIRCRAFT WAS RETURNED TO SERV ICE. 2 L 7 2 4F RT A16WE 2008022700138 20080227 00138 NM 2008 2 27 UIEA200800037 1 20080208 A 5753 SKIN BOEING 747 747271C 1384869 NM TE FLAP DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 LEFT OUTBOARD MIDFLAP LE CHIPPED AND HAS EVIDENCE OF DELAMINATION APPROX 6 INCHES LOCATED 18 INCHES OUT BOARD OF NR 1 FL AP TRACK. REPAIRED PER SRM 51-40-12 AND EO4757A418. 2 L 7 4 4F RT A20WE 2008022700141 20080227 00141 NM 2008 2 27 UIEA200800038 1 20080207 A 5320 SUPPORT BOEING 747 747271C 1384869 NM BS 1915 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 LOWER AFT CARGO COMP HAS PALLET STOP SUPPORT WEB SPLIT AT STATION 1915 FROM LBL 22-LBL 28. REPAIRED DAMAGE IAW SRM 51-4 0-03 FIG 2 AND EO 4753A110. 2 L 7 4 4F RT A20WE 2008022700142 20080227 00142 NM 2008 2 27 UIEA200800039 1 20080208 A 5711 SPAR BOEING 747 747271C 1384869 NM RT WING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 EVIDENCE OF DELAMINATION AND CRACKING ON LEADING EDGE TO FRONT SPAR UPPER SURFACE PANEL APPROX WS 380. REPAIRED IAW SRM 51-40-12. 2 L 7 4 4F RT A20WE 2008022700144 20080227 00144 NM 2008 2 27 UIEA200800043 1 20080215 A 5711 SPAR BOEING 747 7472D7B 1384803 NM RT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 W/S 780 UPPER SKIN MIDSPAR CORROSION EVIDENT. LEVEL 1 RIGHT WING, BLENDED OUT CORROSION IAW SRM 51-10-01. REPROTECTED PER 51-10-02. 2 L 7 4 4F RT A20WE 2008022700147 20080227 00147 NM 2008 2 27 NWAA080595635 1 20080217 A 2530 OVEN BOEING 757 757251 1384970 NM GALLEY ODOR A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 535US 26482 JUST PRIOR TO DESCENT FLIGHT ATTENDANT ADVISED A HOT/SMOKY ODOR FROM THE FRONT GALLEY, ALL COMPONENTS TURNED OFF AND CIR CUIT BREAKERS PULLED AS A PRECAUTION, AND ODOR DID DISSIPATE. FLIGHT CONTINUED ON AND LANDING WAS UNEVENTFUL. MAINTENA NCE FOUND ODOR AND A BEARING SOUND FROM RIGHT OVEN. REMOVED AND REPLACED OVEN. OPERATIONAL CHECKED GOOD, AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2008022700149 20080227 00149 2008 2 27 IXXA080007O 4 20080221 A 2200 75130 TRANSFER VALVE DOUG DC8 DC871F 302199D WP FUEL SYSTEM DEFECTIVE A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 820BX 90232 1153 46065 AFTER ROTATION FROM KLRD AIRCRAFT DID A UNCOMMANDED YAW TO THE LEFT AND RIGHT, THE CREW TURNED YAW DAMPER OFF AND OSCILL ATION DAMPENED OUT. THE CREW RETURNED TO KLRD AND LANDED WITH OUT INCIDENT. MAINTENANCE DEFERRED THE AUTO PILOT SYSTEM IAW ATI MEL 22-01-00 TO KTOL. MAINTENANCE IN KTOL INSPECTED THE AUTO PILOT SYSTEM AND REPLACED YAW DAMPER TRANSFER VAL VE, OPERATIONAL CHECK GOOD IAW UAL DC8 MAINTENANCE MANUAL 22-10-37. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2008022700152 20080227 00152 WP 2008 2 27 IXXA08SMN027S 1 20080119 A 5330 SKIN DOUG DC8 DC862F 3021972 WP BS 485 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE SKIN HAS IMPROPER REPAIR AT STATION 485.000 LONGERON 25 RIGHT. REMOVE D EXISTING REPAIR. REMOVED DAMAGE AREA. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION AFTER INSPECTION. FABRICATE D REPAIR DOUBLER, AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SRM 51 -1-20D, 51-3-1, FAA FORM 8110-3 NUMBER 08033 DATED 01-23-08, SEMAN DRAWING NUMBER ED-4691 DATED 01-17-08, DC8 SRM 51-1-2 1, 51-3-0, DC8 NDT SPM PART 06.10.001, AND DC8 SRM 51-1-8B. 2 L 7 4 4F 4A25 2008022700153 20080227 00153 WP 2008 2 27 IXXA080009S 1 20080119 A 5330 SKIN DOUG DC8 DC862F 3021972 WP ZONE 100 MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE SKIN HAS IMPROPER REPAIR AT STATION 485.000 LONGERON 26 RIGHT. REMOVE D EXISTING REPAIR. REMOVED DAMAGE AREA. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION AFTER INSPECTION. FABRICATE D REPAIR DOUBLER, AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SRM 51 -1-20D, 51-3-1, FAA FORM 8110-3 NUMBER 08033 DATED 01-23-08, SEMAN DRAWING NUMBER ED-4691 DATED 01-17-08, DC8 SRM 51-1-2 1, 51-3-0, DC8 NDT SPM PART 06.10.001, DC8 SRM 51-1-8B. 2 L 7 4 4F 4A25 2008022700159 20080227 00159 NM 2008 2 27 JJBA200825011 1 20080205 A 3350 61049811 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN NOT SEATED A JJBA K NONE L NO TEST IN INSP/MAINT 1 EA 01 368PH 512 PRIOR TO FLIGHT EMERGENCY OVERHEAD LIGHT FOUND TO BE INOP. RESEATED BATTERY, OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2008022700161 20080227 00161 CE 2008 2 27 BSAASDR0801 1 20080102 A 5270 SWITCH BEECH 1900 1900D 1154162 CE CRAGO DOOR OUT OF ADJUST A BSAA K NONE N FALSE WARNING CR CRUISE 1 NM 05 856CA UE405 CARGO DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT, NO LOSS OF PRESSURIZATION. INITIALLY DEFERRED. ADJUSTED CARGO DOOR SWITC H, OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A24CE 2008022700168 20080227 00168 NM 2008 2 27 08FDEA00542 1 20080221 A 5712 ARB71284 RIB DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 RIGHT WING, UPON REMOVAL OF NR 1 SLAT INBOARD CRUISE PERFORMANCE FILLET FOR NR 1 SLAT INBOARD LEADING EDGE METAL SEAL RE PLACEMENT, FOUND OUTBOARD RIB NEAR ALIGNMENT AREA CRACKED. REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 5 VOLUME I. R EPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008022700169 20080227 00169 EU 2008 2 27 08FDEA00550 1 20080123 A 5743 A2757036000400 TRUNNION AIRBUS 310 A310222 3930315 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 RT WING NR 3 FLAP OUTBOARD TRUNNION WITH WEAR. TRUNNION NR 3 RT WAS REMOVED, REPAIRED PER CMM 57-53-12 AND INSTALLED PE R AMM 27-54-37. 2 L 7 2 4F RT A35EU 2008022700172 20080227 00172 EU 2008 2 27 08FDEA00543 1 20080116 A 5410 A5461092600040 BEAM AIRBUS 310 A310222 3930315 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 NR 2 PYLON, AFT ATTACHMENT BEAM ASSEMBLY WITH CORROSION ON MATING FACE. CORROSION OUT OF LIMITS, REPLACED BEAM ASSEMBLY IAW SRM 54-51-81 AND AMM 54-51-85. 2 L 7 2 4F RT A35EU 2008022700178 20080227 00178 NM 2008 2 27 08FDEA00586 1 20080223 A 5313 6558352207 STRINGER BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 FWD PIT FLOORBOARD SUPPORT STRG AT (STA 645) RBL 12 IS CORRODED (MARKED ) REMOVED DAMAGED AT STA 645 AND FABED A REPAIR . APPLIED ALODINE, PRIMER AND PAINT. REINSTALLED FLOOR SUPPORT AND INSTALLED SPLICE AT STA 670. APPLIED ALODINE, PRIM E AND PAINT, REF SRM 53-10-1 FIG 1. CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008031900106 20080319 00106 CE 2008 3 19 ACE020508 1 20080205 A 3245 G195X6758 TUBE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA NLG TIRE SPLIT E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 113AX 61 UC41 NOSE TIRE LOOSING AIR AFTER LANDING (BET) REPLACED NOSE TIRE ASSY (FOUND INNER TUBE SPLIT ON SEAM 1/8). THIS IS THE LA TEST IN A STRING OF INNER TUBE FAILURES FOR UNDETERMINED REASONS. THIS WAS A CANADIAN MANUFACTURED TUBE AND THE FAILUR E SEEMS TO BE AT A DEFECT IN A JOINING SEAM. 2 L 7 2 4T 4 T RT A24CE E4EA 2008031900107 20080319 00107 CE 2008 3 19 ACE011108 1 20080111 A 3245 G195X6758 TUBE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA NLG TIRE BLOWN E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 111AX 95 UC81 PILOT REPORTED NOSE TIRE FLAT ON LANDING. REPLACED TIRE ASSY DUE FAILED INNER TUBE. WE ARE EXPERIENCING MULTIPLE FAILU RES / BURST TUBES FROM THIS MFG. MFG PREVIOUSLY NOTIFIED. 2 L 7 2 4T 4 T RT A24CE E4EA 2008031900109 20080319 00109 NM 2008 3 19 15528 1 20080206 A 2782 ACTUATOR EMB ERJ170 ERJ170200LR 3260121 NM GE CF34 CF348E5 30061 NE SLAT DEFECTIVE A C77A A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 27 606CZ 557 17000188 SLAT FAIL MESSAGE ON EICAS AFTER TAKEOFF. PILOTS PERFORMED QRH MESSAGE DID NOT CLEAR. PEFORMING TROUBLESHOOTING. 2 L 7 2 4F 4 F RT A56NM E00063EN 2008031900113 20080319 00113 CE 2008 3 19 DJFA2008007 1 20080124 A 2163 11509761 SENSOR BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE CABIN TEMP INOPERATIVE E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 454LX 5262 RK327 DURING CRUISE CREW REPORTED BURNING ODOR NEAR THE LAV AREA. CREW CONTINUED TO DESTINATION. MAINTENANCE FOUND THE CABIN TEMP SENSOR FAILED. THE TEMP SENSOR WAS REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2008031900117 20080319 00117 EA 2008 3 19 S9BA200800001 1 20080211 A 5730 SKIN DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA LT WING CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 20206 1310 573 CPCP INSPECTION, LT FWD SKIN ON LT WING IS CORRODED AT WS 63.5. REPLACED LOWER SKIN FROM RIB 1 (STA 35.15) TO RIB 10 (S TA 147.5) SPLICED SKIN AT RIB 2 (STA 47.5) AIRCRAFT GROUNDED? YES 1 H 7 2 3T 4 T RT A9EA E4EA 2008031900118 20080319 00118 EA 2008 3 19 S9BA200800002 1 20080211 A 5711 C6W105662 SPAR DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA ZONE 500 CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 20206 1310 573 CPCP INSPECTION, FWD LT WING SPAR HAS CORROSION BETWEEN STATIONS 72.5 AND WS 135. REPLACED AND SPLICED FWD SPAR WS 72. 5 TO 135 IAW RD6-57-191. AIRCRAFT GROUNDED, YES. 1 H 7 2 3T 4 T RT A9EA E4EA 2008031900122 20080319 00122 EA 2008 3 19 S9BA20080012 1 20080211 A 5730 C6W1001 SKIN DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA ZONE 600 CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 20206 1310 573 CPCP INSPECTION, RT WING IB FWD SKIN CORRODED WS STA. 35.15 TO 185. REPLACED SKIN IAW SRM CH 57-30-00 FIG 1AND RD 6-57- 164. EMERGENCY MEASURES EXECUTED? NO. AIRCRAFT GROUNDED? YES. 1 H 7 2 3T 4 T RT A9EA E4EA 2008031900124 20080319 00124 EA 2008 3 19 S9BA20080003 1 20080211 A 5730 C6W1024 SKIN DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA ZONE 500 CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 20206 1310 573 CPCP INSPECTION, LT WING CORRUGATION AT WS 65 TO 125 CORRODED. REPAIRED CORRUGATION BETWEEN WS 65 AND 125 IAW SRM 57-30 -00 FIG 4 AND RD6-57-077. EMERGENCY MEASURES EXECUTED? NO. AIRCRAFT GROUNDED? YES. 1 H 7 2 3T 4 T RT A9EA E4EA 2008031900126 20080319 00126 CE 2008 3 19 20061066 1 20080211 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 163 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 257GL UE257 FRAME AT FS 163.97 AND STR 9R CRACKED APPROX .40 INCH IN LENGTH - RII REQUIRED TC 8.2.1. OPEN 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900130 20080319 00130 WP 2008 3 19 UG8A08P021401 2 20080211 A 7250 RETAINER RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP LT TURBINE ASSY LOOSE E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 715PH 1168 258715 P107984 NR 1 ENGINE FAN WOULD NOT ROTATE FREELY ON POSTFLIGHT INSP. BINDING STILL PRESENT AFTER SEVERAL HOURS OF COOL DOWN TIME . OUTSIDE VENDOR CALLED IN TO DISASSEMBLE ENGINE ENOUGH TO DETERMINE CAUSE OF BINDING. IT WAS FOUND THAT MANY OF THE F IRST STAGE TURBINE BLADE RETAINING CLIPS WERE MISSING ALLOWING BLADE SHIFT. TURBINE SECTION IS BEING REBUILT. AC WILL BE RETURNED TO SERVICE AFTER RECEIVING AND INSTALLING REBUILT TURBINE SECTION OF ENGINE ASSY. 2 L 7 2 4F 4 F RT A3EU E6WE 2008031900150 20080319 00150 NM 2008 3 19 KCSA081166 1 20080311 A 5347 STOP FITTING BOEING 747 747209B 138489B NM FWD CARGO BAY CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FWD PIT FLOOR CARGO PALLET STOP FITTING CRACKED AT BS 962, RBL 44. 2 L 7 4 4F RT A20WE 2008031900155 20080319 00155 NM 2008 3 19 KCSA081169 1 20080311 A 5210 DOOR FRAME BOEING 747 747SR46 1384816 NM L2 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 MAIN ENTRY DOOR 2L FWD LOWER CORNER FRAME CRACKED BS 808. 2 L 7 4 4F RT A20WE 2008031900157 20080319 00157 WP 2008 3 19 MWEA080041 1 20080308 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 809ME 48071 FORWARD SECTION OF EMERGENCY LIGHTING BY GALLEY TWO IS INOPERATIVE. REPAIRED BROKEN WIRE. 2 L 7 2 4F A6WE 2008031900159 20080319 00159 2008 3 19 MWEA080040 4 20080307 A 2565 100502119 SLIDE DOUG DC9 DC981 3022081 WP CABIN DEPLOYED A MWEA O OTHER O OTHER CR CRUISE 1 GL 13 803ME 48029 AFT GALLEY SLIDE DEPLOYED IN FLIGHT WEDGING ITSELF BETWEEN THE BULKHEAD AND GALLEY CART. REMOVED AND REPLACED AFT SLIDE . 2 L 7 2 4F A6WE 2008031900163 20080319 00163 EA 2008 3 19 TRAX200800330 1 20080226 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 THE 280 BEAM CORRODED BEYOND LIMITS. REFER TO E/C FOR REPLACEMENT REFER TO M-234 FORM ATTACHED TO N/R FOR WORK ACCOMPLI SHED SM7017032. REPAIR MADE IAW ASA EO700-53-0061. SUPPLEMENTAL SDR CLOSED 3/7/08. 2 L 7 2 4F RT A21EA 2008031700258 20080317 00258 NM 2008 3 17 C77A200800005 1 20080127 A 5754 17036006401 SLAT TRACK EMB ERJ170 ERJ170200LR 3260121 NM GE CF34 CF348E5 30061 NE L/E SLAT OBSTRUCTED A C77A K NONE F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 EA 27 606CZ 483 265 17000188 DURING FLIGHT INBOUND, PILOT SENT ACARS MESSAGE OF SLAT FAIL. A/C PERFORMED A ZERO FLAP LANDING, AND THE PILOT AS NOTED THE BRAKES HAVING A HIGH TEMP. AC PROCEEDED TO GATE UNDER ITS OWN POWER. MAINT THEN PERFORMED THE SLAT-ACE 1 AND 2 TESTS . ALL TESTS COMPLETED AND PASSED, IAW EMB175 FIM 27-81-00-810-803-A. MECHANIC DID NOTE WET SNOW IN THE SLAT TRACKS UPON PLACING THE SLATS TO THE FULL DOWN POSITION. THE WET SNOW WAS THEN REMOVED FROM THE TRACK. MAINT ALSO PERFORMED A GVI O F MAIN LANDING GEAR BRAKES IAW EMB175 AMM 32-41-00. THE MECHANIC DID NOT NOTICE ANY MECHANICAL DEFECTS ON LANDING GEAR B RAKES AND TIRES. 2 L 7 2 4F 4 F RT A56NM E00063EN 2008031700261 20080317 00261 CE 2008 3 17 DJFA2008008 1 20080124 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE COCKPIT ODOR E DJFA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 464LX RK453 IN FLIGHT, CREW REPORTED BURNING RUBBER SMELL WHEN AIR IS HOT. MAINT RAN BOTH ENGINES AND BLEED AIR SYSTEM WITH CABIN T EMP TO FULL HOT BUT COULD NOT DUPLICATE THE DISCREPANCY. 2 H 7 2 4F 4 F RT A16SW E25EA 2008031800005 20080318 00005 NM 2008 3 18 F3LA200800087 1 20080310 A 3240 201042418 LINE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE BRAKE SYSTEM DAMAGED A F3LA O OTHER K FLUID LOSS AP APPROACH 1 NM 03 923FR 61 2019 DURING THE APPROACH, THE FLIGHT CREW REPORTED SEVERAL BIRD STRIKES (CANADIAN GEESE). ON LANDING, THE FLIGHT CREW REPORT ED THE LOSS OF NORMAL BRAKING DURING THE ROLL OUT. MAINTENANCE INSPECTED THE LANDING GEAR AND FOUND BRAKE LINE 27 ON TH E RIGHT MAIN LANDING GEAR TO BE DAMAGED. MAINTENANCE REPLACED BRAKE LINE 27 IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 32-11-12-400-001, STEPS 4B (2) (R) AND (W). FOLLOWING INSTALLATION OF THE BRAKE LINE, THE BRAKE AND STEERING SYSTEM WAS BITE TESTED IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 32-46-00-740-001 AND TESTED OKAY. THE AIRCRAFT WAS RETURNED TO SERVICE FOLLOWING OTHER MINOR REPAIRS. 2 L 7 2 4F 4 F RT A28NM 2008031800020 20080318 00020 EU 2008 3 18 08FDEA00862 1 20080310 A 5712 A5726007320200 RIB AIRBUS 310 A310203 3930313 EU LT WINGLET CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 LT WINGLET RIB CRACKED REPLACE, REPAIR RIB. 2 L 7 2 4F RT A35EU 2008031800036 20080318 00036 EU 2008 3 18 08FDEA00887 1 20080311 A 5321 A2577283500300 FLOOR PANEL AIRBUS 310 A310203 3930313 EU AFT CARGO BAY DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT CARGO PIT FLOOR PANEL 151FF HAS CORNER DAMAGE. FABRICATED NEW FLOOR PANEL. POTTED EDGES. COMPLETED CURE & SANDED E DGE POTTING. INSTALLED INSERTS & APPLIED NON-SKID IAW DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 2008031800068 20080318 00068 EA 2008 3 18 MASA200800222 1 20080311 A 1100 PLACARD CNDAIR CL600 CL6002D24 1390016 EA LAVATORY MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 920FJ 15020 ASH FLT 2682 CLT-IAD - OXYGEN INSTRUCTIONAL PLACARD IN AFT LAV MISSING. INSTALLED PLACARD 2 L 7 2 4F RT A21EA 2008031800069 20080318 00069 EU 2008 3 18 TRBA2008029 1 20080310 A 3350 7012210 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN INOPERATIVE A TRBA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 29 426AT 426 RIGHT SIDE EMERGENCY FORWARD FLOOD LIGHT INOP. REMOVED AND INSTALLED RIGHT SIDE FORWARD EMERGENCY LAMP AS PER MM 33-51- 00. OPS CHECK OK. 2 H 7 2 4T RT A53EU 2008031800086 20080318 00086 WP 2008 3 18 UPS08851781 1 20080109 A 5220 DOOR FRAME DOUG DC8 DC871F 302199D WP OVERWING EXIT GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 OUTER FRAME GOUGED IN 3 PLACES LT SIDE OF LT OVERWING EXIT DOOR, BLENDED OUT GOUGES, WENT OUT OF LIMI TS. FABRICATED REPAIR DOUBLER AND INSTALLED IAW 52-2-0, 51-1-20D, 51-1-8,52-2-0 FIG 6. 2 L 7 4 4F RT 4A25 2008031800103 20080318 00103 NM 2008 3 18 UPS08M51798 1 20080226 A 5512 SKIN DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 6 LEFT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944. 2 L 7 3 4F RT A22WE 2008031800105 20080318 00105 WP 2008 3 18 IXXA08SMN057S 1 20080207 A 5320 4705419U502 FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STATION 759 LONGERON 11 RIGHT. REMOVED CRAC KED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALL NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, AND DC8 SRM 5 1-1-8B. 2 L 7 4 4F RT 4A25 2008031800117 20080318 00117 NM 2008 3 18 2008UALA01249 1 20080307 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 SEAT EEL INOP:4F AFT SECTION, RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031800123 20080318 00123 NM 2008 3 18 2008UALA01271 1 20080307 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 INTERCOSTAL IS CRACKED AT STA 291.5 JUST BELOW STR 12R. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800157 20080318 00157 NM 2008 3 18 2008UALA01311 1 20080308 A 2497 TERMINAL BLOCK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 IDG DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 651UA 25389 NR 1 ENG IDG FEEDERS SHOW SIGNS OF HEAT DAMAGE AT TERMINALS. FOUND DAMAGED TERMINALS AT IDG TERMINAL BLOCK. REPLACED T ERMINALS. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800175 20080318 00175 NM 2008 3 18 2008UALA01342 1 20080311 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 FOUND SEAT EEL LIGHT NOT ON AT 5E AFT. REPLACED LAMP ASSEMBLY. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022700180 20080227 00180 NM 2008 2 27 08FDEA00587 1 20080223 A 5720 652678930 FAIRING BOEING 727 727227 1384078 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 RT WING O/B JACKSCREW TOP WING PANEL BRACKET CRACKED AT AFT I/B SIDE OF FAIRING. REMOVED FAIRING, REMOVED AND REPLACED DOUBLER ON FAIRING REF SRM 51-30-. REINSTALLED FAIRING REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008022700193 20080227 00193 WP 2008 2 27 08FDEA00596 1 20080225 A 5347 601096418 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 363FE 48263 SEAT TRACK AT STA 755 LBL 48 HAS WORN LUGS REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1. REPAIR PARTS FABRICATED ON TRAVE LER T8/725392. 2 L 7 3 4F RT A22WE 2008022700198 20080227 00198 EA 2008 2 27 TRAX200800197 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 RIGHT SIDEWALL SEAT RAIL FS 570.0 TO FS 708.0 HAS CORROSION DAMAGE. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 53-31-49. APPLIED ALODINE IAW CRJ 700 SRM 51-21-16. SUPPLEMENTAL SDR CLOSED 2/12/08. 2 L 7 2 4F RT A21EA 2008022700215 20080227 00215 2008 2 27 UPS08851661 4 20080212 A 2565 SLIDE DOUG DC8 DC871F 302199D WP MAIN ENTRY DOOR OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:N/A CREW REPORTED THAT THE MAIN ENTRY DOOR SLIDE GIRT BAR WILL NOT LOCK IN TO FLOOR WITH DOOR CLOSED. R EPACKED MAIN ENTRY DOOR SLIDE IAW MM 25-60, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2008022600074 20080226 00074 NE 2008 2 26 DL76L080216 2 20080216 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 OIL CONSUMPTION A DALA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SO 27 191DN 61639 28448 723844 DUE TO CONTINUED INCREASE IN OIL USAGE, REPLACE ENG. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008022600077 20080226 00077 NM 2008 2 26 DLM90080230 1 20080218 A 5311 5930584123 FRAME DOUG MD90 MD9030 3023690 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 AFT OF LEFT HYDRAULIC SERVICE BOX SUPPORT IS CRACKED. REMOVED AND REPLACED OUTBOARD FRAME, IAW MD90 SRM 51-30-02 AND 51 -30-05. 2 L 7 2 4F RT A6WE 2008022600080 20080226 00080 WP 2008 2 26 AALA200800318 1 20080214 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 463AA 49593 LGA - EMERGENCY LIGHT AT SEAT 26D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022600088 20080226 00088 NM 2008 2 26 ASAA0842631 1 20080117 A 5311 6546530502 FRAME BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 BS 460 FUSELAGE FRAME CRACKED AT FASTENER HOLE BETWEEN STR 13L 14L. REPAIRED WITH MADE REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600095 20080226 00095 NM 2008 2 26 HALA0800229 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 838 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT LBL 11, STA 838, MAX DEPTH OF BLEND OUT WAS 0.010". BLENDED IAW SRM 51-10- 02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022600098 20080226 00098 NM 2008 2 26 ASAA0842567 1 20080105 A 5320 654659249 CHANNEL BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT FLOOR CHANNEL FOUND CORRODED AT BS 727 F +8 LBL 3. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600102 20080226 00102 NM 2008 2 26 ASAA0842574 1 20080105 A 5320 654659249 CHANNEL BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT FLOOR CHANNEL AT BS 847+14 867+14 LBL 3 FOUND CORRODED. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600149 20080226 00149 EU 2008 2 26 USAA920080455 1 20080217 A 5321 D5367180500400 FLOORBOARD AIRBUS 320 A320232 3930326 EU CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBOARD 261FF, BS 3158 / FR 66 - BS 3257 / FR 68, +Y1292. REPLACE D CABIN FLOORBOARD 261FF, BS 3158 / FR 66 - BS 3257 / FR 68, +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022600155 20080226 00155 EU 2008 2 26 USAA920080461 1 20080213 A 5315 D53472094008 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3043 / FR 64 - BS 3207 / FR 67, +Y512. REPLACED CABIN FLOORBEAM, BS 3043 / FR 64 - BS 3207 / FR 67, +Y512 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022600156 20080226 00156 EU 2008 2 26 USAA920080462 1 20080213 A 5347 D53112815200 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SEAT TRACK, BS 709 / FR 16 - BS 808 / FR 20, +Y765. REPLACED CABIN S EAT TRACK, BS 605 / FR 12 - BS 808 / FR 20, +Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022600159 20080226 00159 NM 2008 2 26 USAA920080444 1 20080208 A 5340 69468314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER TIE CLIP, BS 360 AND S5L. REPLACED STRINGER TIE CLIP, BS 360 AND S5L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008022600173 20080226 00173 NM 2008 2 26 ASAA0842616 1 20080208 A 5313 654988665 STRINGER BOEING 737 7374S3 1384711 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 STR 19L DENTED ON FREE FLANGE AT ST 477 STR 19L. FREE FLANGE AT STA 477 FOUND TO BE BEYOND ALLOWABLE LIMITS AND REPAIRE D IAW B737 400 SRM 53 00 03 FIG 101 & FIG 201. 2 L 7 2 4F RT A16WE 2008022600190 20080226 00190 NM 2008 2 26 ASAA0842608 1 20080116 A 5347 654681350 SEAT TRACK BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 SEAT TRACK CORRODED BS 500 + 18 LBL 45. REPAIR WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600191 20080226 00191 NM 2008 2 26 ASAA0842609 1 20080117 A 5320 69434452 ATTACH BRACKET BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT STRINGER TO INTERCOSTAL ATTACH BRACKET EXFOLIATED AT BS 767+6 RBL 20. AFT CARGO PIT ATTACHED STRINGER TO INTERCOSTAL AT BS 767+6 RBL 20 REPLACED WITH MADE REPAIR PART IAW B737 400 SRM 51 30 01 AND 51 40 02. 2 L 7 2 4F RT A16WE 2008022600194 20080226 00194 NM 2008 2 26 ASAA0842624 1 20080109 A 5320 654578315 SUPPORT CHANNEL BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO COMP BILGE VHF NR 2 ANTENNA SUPPORT CHANNEL AND MOUNT PLATE AT STA 515 BL 0 HAS CORROSION. FWD CARGO VHF NR 2 ANTENNA SUPPORT REPLACED WITH MADE REPAIR PART IAW B737 400 SRM. 2 L 7 2 4F RT A16WE 2008022600204 20080226 00204 NM 2008 2 26 ASAA0852643 1 20080224 A 4990 38809381 FILTER BOEING 737 737890 1384527 NM APU CLOGGED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 558AS 35177 WHILE PERFORMING TASKCARD 78349013 (APU OIL FLITER DELTA P INDICATOR) FOUND THE INDICATOR EXTENDED. ACCOMPLISHED OIL FI LTER INDICATOR SERVICING. LEAK CHECK OK. 2 L 7 2 4F RT A16WE 2008022600226 20080226 00226 EA 2008 2 26 A6WA200840055 1 20080127 A 5230 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CARGO DOOR UNSECURE A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 452AW 7835 ON CLIMBOUT AFTER TAKEOFF, APROX 600 MSL, CARGO DOOR MESSAGE ED1 AND CAUTION LIGHT ILLUMINATED. CABIN CLIMBING APPROX 1 400 FT PER MIN. C/W QRH. AFTER LANDING NOTED CARGO DOOR HANDLE POPPED. FOUND CARGO DOOR HANDLE EXTENDED UPON ARRIVAL AT GATE. STOWED CARGO DOOR HANDLE, PRESSURIZED AIRCRAFT, NO DEFECTS NOTED W/ CARGO DOOR WARNING SYS, OPS CHECK OF CARGO DOOR HANDLE GOOD IAW AMM 52-31-03. OK FOR CONTINUED SERVICE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022600264 20080226 00264 EA 2008 2 26 A6WA200840047 1 20080122 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE WING FAILED A A6WA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 31 438AW 7748 FLAPS FAILED AT ZERO DEGREES, COMPLIED WITH QRH. FAILED ON APPROACH, OAT -1C. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022600265 20080226 00265 EA 2008 2 26 A6WA200840052 1 20080124 A 2910 HYDRAULIC SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 2 LEAKING A A6WA O OTHER K FLUID LOSS DE DESCENT 1 GL 31 426AW 7669 IB CREW REPORTED HYD NR 2 LEAK ON SHORT FINAL. HYD NR 2 CAUTION MESSAGE RECEIVED. HYD QUANTITY NO READS 25 PERCENT. ( K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022600270 20080226 00270 NM 2008 2 26 AMTA200800113 1 20080219 A 3397 WIRE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE CABIN DISCONNECTED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 522AT 29330 EMER FLOOR LIGHTING ROWS 15 THRU 21 INOPERATIVE. T/S FOUND WIRING DISCONNECTED AT ROW 21. RECONNECTED WIRES, OPS CHECK S GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008022600271 20080226 00271 EA 2008 2 26 A6WA200840096 1 20080217 A 2750 DETECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE T/E FLAP MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 441ZW 7777 ON SHORT FINAL FLAPS FAILED AT 45 DEGREES. RAN QRH. NO FURTHER PROBLEMS. REMOVED AND REPLACED SKEW DETECTION UNIT IAW AMM 27-51-15. OPS CHECK GOOD IAW AMM 27-54-00. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022700003 20080227 00003 EA 2008 2 27 COMA0880002 1 20080201 A 3010 WARNING SYSTEM CNDAIR CL600 CL6002D24 1390016 EA ANTI-ICE SYSTEM MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 693CA 15096 FLIGHT 4985 - RECEIVED ANTI-ICE DUCT WARNING CAUTION MESSAGE. RETURNED TO PHL, LANDED WITHOUT INCIDENT. PERFORMED TEST S OF ANTI-ICE AND LEAK DETECTION CONTROLLER, AND THE WING ANTI-ICE CONTROL INDICATION SYSTEM. NO DEFECTS NOTED. AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008022700024 20080227 00024 EA 2008 2 27 SWIA200819229 1 20080215 A 3210 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 959SW 7840 FLT NR 6670. RECEIVED A GEAR DISAGREE WARNING ON NOSE GEAR AFTER TAKEOFF, PERFORMED FUNCTIONAL TEST OF THE LANDING GE AR SYSTEM SEVERAL TIMES. COULD NOT DUPLICATE PROBLEM. OPS CHECKED NORMAL IAW AMM 32-30-00. 2 L 7 2 4F RT A21EA 2008022700044 20080227 00044 EA 2008 2 27 COMA0860123 1 20080211 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 932CA 7038 FLIGHT 5360 - ON FINAL APPROACH TO JFK, SELECTED FLAPS TO 8 DEG, RECEIVED FLAP FAIL MESSAGE AT 2 DEG. EMERGENCY DECLARE D, A/C LANDED SAFELY. COMPLIED WITH SI-2-2710002 FLAP CAUTION MESSAGE FOLLOW UP MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 2008022700054 20080227 00054 EA 2008 2 27 COMA0860129 1 20080212 A 3010 6420002 PRESSURE SWITCH CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYSTEM FAILED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 969CA 7141 FLIGHT 5516 - RIGHT WING A/I CAUTION MESSAGE ON T/O ROLL, JUST BEFORE 100 KTS. ABORTED TAKEOFF SAFELY. REMOVED AND REP LACED RIGHT PRESSURE SWITCH. 2 L 7 2 4F RT A21EA 2008022700056 20080227 00056 EA 2008 2 27 COMA0860131 1 20080213 A 2910 HYDRAULIC SYSTEM CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 818CA 7408 FLIGHT 5381- EN ROUTE FROM JFK TO RIC, 31 HYDRAULICS READING 30% DURING HOLDING. EMERGENCY DECLARED AND AIRCRAFT DIVERT ED TO ORF AND LANDED SAFELY. PERFORMED LEAK CHECK AND DIRECT READING GAUGE CHECK. ALL CHECKS GOOD. DEFERRED PER MEL 2 9-32-01. 2 L 7 2 4F RT A21EA 2008022700073 20080227 00073 NM 2008 2 27 ASAA0842556 1 20080117 A 5315 654581283 FLOORBEAM BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 CORROSION ON FLOORBEAM MULTIPLE AREAS AT BS 324 RBL 10 TO RBL 30. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022700077 20080227 00077 NM 2008 2 27 ASAA0842561 1 20080115 A 5347 65468136 SEAT TRACK BOEING 737 7374S3 1384711 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 SEAT TRACK GOUGED AT STA 536 LBL 25. SEAT TRACK REPLACED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008022700082 20080227 00082 NM 2008 2 27 UIEA200800028 1 20080205 A 5730 65B149622 PANEL BOEING 747 7472D7B 1384803 NM RT WING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 RT WING FIXED UPPER L/E PANEL DIRECTLY ABOVE NR 3 GROUP L/E PDU HAS AREA OF 23.5 BY 19.0 INCHES OF DELAMINATION. INTERI M REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-16 FIG 1, SRM 51-70-06, SRM 51-30-02, ATLAS AIR EO NR 4757A417 AND F AA FORM 8110-3. REQUIRES DETAILED VISUAL INSPECTION AT EVERY A-CHECK UNTIL PERMANENT REPAIR IS ACCOMPLISHED AT C-CHECK. 2 L 7 4 4F RT A20WE 2008022700098 20080227 00098 NM 2008 2 27 SWAA080901 1 20080218 A 5313 6551698 STRINGER SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2008022700134 20080227 00134 WP 2008 2 27 IXXA08SMN008S 1 20080115 A 5755 SKIN DOUG DC8 DC862 3021970 WP NR 4 SPOILER DELAMINATED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 SPOILER DELAMINATED. REMOVED DAMAGED SPOILER. INSTALLED N EW RIGHT SPOILER IAW DC8 MAINTENANCE MANUAL 27-60-1 PAGES 201-207. PERFORMED OPERATIONAL CHECK TO ALL FLIGHT CONTROLS, GOOD IAW DC8 MAINTENANCE MANUAL 27-11-0 PAGES 10-14, DC8 27-21-0 PAGES 5-9, 27-30-0 PAGES 4-7, 27-40-0 PAGES 1-2, 27-40- 1 PAGES 10-13, 27-51-0 PAGES 10-12, 27-61-0 PAGES 5-7, 27-70-0 PAGES 1-2, AND 27-80-0 PAGES 4. 2 L 7 4 4F 4A25 2008022700139 20080227 00139 NM 2008 2 27 DHL2008752604 1 20080208 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1130 S26L DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 AFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4" BY 1/2" IAW B727 SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR MATERIAL USED 7075-O .071 PO NR 9006377 DIMENSION 9" B Y 4" IAW B727 SRM 51-40-3 FIG1 AND IAW B727 SRM 53-10-2 FIG 5. HEAT TREAT PART 7075-O TO 7075T6 IAW B727 FLIGHTSTAR AIR CRAFT SERVICES ENGINEERING REPORT NR 2-37153-801 REVA TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008022700140 20080227 00140 NM 2008 2 27 DHL2008752602 1 20080204 A 5320 WEB BOEING 727 727223 1384074 NM BS 1223-1225 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 LT SIDE OF AIRSTAIR WEB CRACKED AT LIGHTING HOLE BS 1223. CUTOUT DAMAGED AREA AT LT SIDE OF AIRSTAIR WEB STA 1223 IAW S RM 51-40-2 FIG1. FABRICATED DOUBLER IAW SRM 51-40-2 FIG1 AND SRM 53-10-2 FIG 6. TREATED AND PRIMED AREA IAW SRM 51-10- 2. INSTALLED DOUBLER REPAIR AT LT SIDE OF AIRSTAIR WEB BS 1223 IAW SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2008022700150 20080227 00150 WP 2008 2 27 IXXA08SMN009S 1 20080115 A 5730 SKIN DOUG DC8 DC862 3021970 WP ZONE 600 DELAMINATED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING (MLG/FUSELAGE) MIDDLE DOOR, DELAMINATED SKIN. REMOVED DAMAGED SKIN. INSTALLED NEW SKIN CENTER DOOR ON RIGHT MAIN LANDING GEAR FUSELAGE. PERFORMED OPERATIONAL CHECK FOR HYD SYSTEM LEAKS, GOOD IAW DC8 MINATENANCE MANUAL 27-10-0, 27-20-0, 27-40-0, 27-50-0, 27-60-0, 27-80-0, 27-00, 32-30-0, 32-42-0, 32-50-0, 52-36-1 AND 78-30-0, AND DC8 32-12-1 PAGES 401-404. 2 L 7 4 4F 4A25 2008022700175 20080227 00175 WP 2008 2 27 08FDEA00584 1 20080223 A 3200 UNKNOWN DOUG MD10 MD1010F 3022112 WP MLG UNKNOWN A FDEA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 25 68049 47803 PDIS ON APPROACH INTO LAX, GEAR HANDLE CAME DOWN BUT NO GREEN LIGHTS, THEY REMAINED RED. GEAR HANDLE WAS IN DETENT. C OULD HEAR THE ADDITIONAL AIRFLOW OVER THE GEAR DOORS OR GEAR. ON GO AROUND, CYCLED THE GEAR AND THEY CAME DOWN NORMALL Y. HAD NO HYDRAULIC MALFUNCTIONS MADE A NORMAL LANDING. COULD NOT DUPLICATE PROBLEM. PSEU LOGGED NO FAULTS. SENSORS ALL NORMAL. INSPECTED ALL GEAR WELLS, CABLES, SENSORS, TARGETS AND HYDRO UNITS. FOUND NO DISCREPANCIES. PINNED ALL GE AR AND CYCLED HANDLE. DOORS WORK AND POSITIVE HYDRO PRESSURE GOOD TO EACH DOWN ACTUATOR. REMOVED PINS AND RETURNED TO NORMAL. INDICATION NORMAL. OK FOR FLIGHT PER MM. 2 L 7 3 4F RT A22WE 2008022700218 20080227 00218 EA 2008 2 27 TRAX200800239 1 20080210 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA WING DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 873AS 7549 APPEARS TO BE SKIN CRACKING OR DELAMINATION ON UPPER WING TO WINGLET MATING AREA. FLT 4330 DEL 35 MINS. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. 2 L 7 2 4F RT A21EA 2008022700221 20080227 00221 2008 2 27 2008UALA00078 4 20080105 A 3451 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE UNKNOWN A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 432UA 587 AFTER TAKEOFF BOTH DME'S VARIABLE +/- 20NM, EN ROUTE CONDITION WORSENED TO 100NM AT TIMES. PATCH WITH SAMC & C/B RESET DIDN'T RESOLVE CONDITION. CHECKED DME INTEROGATORS, BITE CHECK OK AND DME DISTANCE TO STATIONS ARE NORMAL. CHECKED AND RESET FMGC COMPUTERS, ALL TEST NORMAL. ACP PHC 1, 2 & 3 TEST. HAD CLASS 3 FAULTS FOR ALL PROBES, TAT, AOA ON BOTH PHC 1& 2. CYCLED PH C CB'S AND RETESTED, ALL OK NOW. LGCUI 1& 2 TESTED NORMAL. ILS TESTED OK. COULD NOT DUPLICATE ANY N AV FAULTS. A/C HAS NOT REPEATED SINCE THIS INCIDENT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008022700223 20080227 00223 NM 2008 2 27 CALA0800137 1 20080204 A 5320 654576834 FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 FOUND CORROSION AT FORWARD CARGO DOOR CUTOUT AT STRINGER 22R. REMOVED, FABRICATED AND INSTALLED NEW CLIP PER SRM 51-10- 02. 2 L 7 2 4F RT A16WE 2008022700239 20080227 00239 EU 2008 2 27 MAC020803 1 20080214 A 3243 10025111Y00 MASTER CYLINDER AEROSP ATR72 ATR72202 8680940 EU BRAKE SYSTEM DEFECTIVE A MTNA K NONE O OTHER TX TAXI/GRND HDL 1 EA 68 810FX 220 AFTER ARRIVAL, THE PILOT REPORTED THE CAPT SIDE RIGHT BRAKE INOPERATIVE. THE MASTER CYLINDER WAS REPLACED AND THE BRAKE LOW PRESSURE SIDE WAS BLED. 2 H 7 2 4T RT A53EU 2008022700241 20080227 00241 NM 2008 2 27 KCSA081080 1 20080216 A 5730 SKIN BOEING 747 747209B 138489B NM CENTER WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 AIR CONDITIONING BAY CENTER WING LOWER SKIN MATERIAL LOSS FOUND OUT OF LIMITS AT STA 1067, CENTER WING LBL 116 BETWEEN W ING STRINGERS 17 AND 18 AREA MAPPED. 2 L 7 4 4F RT A20WE 2008022700244 20080227 00244 NM 2008 2 27 KCSA081081 1 20080216 A 5311 FRAME BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE FRAME IS CRACKED (.25") AT STA 1800 BETWEEN STR 10R & 11R. 2 L 7 4 4F RT A20WE 2008022700253 20080227 00253 NM 2008 2 27 CALA0800144 1 20080216 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 68061 29456 WHILE REPLACING EMERGENCY LIGHT BATTERY CHARGER WOULD NOT TEST. REPLACED BATTERY CHARGER PER AMM 33-51-01. 2 L 7 2 4F RT A1NM 2008031800186 20080318 00186 EA 2008 3 18 MASA200800225 1 20080312 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75995 7361 ASH FLT 7073 IAD-LGA - EMERGENCY LIGHT STRIP AT ROWS 1 AND 2 WAS LOOSE. MX RESECURED THE LIGHT STRIP AND IT OP CHECKED GOOD. 2 L 7 2 4F RT A21EA 2008031800198 20080318 00198 SO 2008 3 18 LR7A08030 1 20080128 A 5343 388482 BEAM LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 560 4606 DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5301, FOUND LT UPPER MAIN WHEEL WELL LANDING GEAR BEAM FRAME CRACKED AT FS 57 7, WL236, LBL65. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-08-006. 2 H 7 4 4T A1SO 2008031900003 20080319 00003 SO 2008 3 19 N93A29022008 1 20080229 A 3220 1159LM306223 PAD GULSTM G1159 GIV 3980115 SO NLG OVERTORQUED E N93A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 13 424QS 9894 1324 AFTER TAKEOFF, RETRACTED GEAR AND NOSE GEAR FAILED TO FULLY RETRACT, EXTENDED GEAR AGAIN AND RIGHT MAIN FAILED TO INDICA TE DOWN AND LOCKED UNTIL EMERGENCY BLOWDOWN WAS ACTIVATED. MAINTENANCE FOUND NOSE GEAR JACK PAD OVER TORQUED AND EXCESS IVE PAINT, REMOVED PAINT AND LOOSENED NUT. RIGHT GEAR ISSUE WAS DUE TO CONFIGURATION ISSUE. 2 L 7 2 4F RT A12EA 2008031900029 20080319 00029 CE 2008 3 19 GUUA03010803 1 20080301 A 5520 1016200131 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 38537 26008 UE158 DURING SCHEDULED ROUTINE MAINT, DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR CTR HINGE BRA CKET. 2 L 7 2 4T 3 T RT A24CE E2NE 2008031900036 20080319 00036 CE 2008 3 19 GUUA02070802 1 20080207 A 5220 1295140351 ARM BEECH 1900 1900D 1154162 CE EMERGENCY EXIT BROKEN A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81546 UE187 DURING SCHEDULED ROUTINE MAINT, DISCOVERED THE LT EMERGENCY EXIT ARM ASSY BROKEN. REPLACED LT EMERGENCY EXIT ARM ASSY. 2 L 7 2 4T RT A24CE 2008031900066 20080319 00066 EU 2008 3 19 TRAX200800372 1 20080304 A 5720 ANGLE AEROSP ATR72 ATR72 EU WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 ETNRC - ANGLE CRACKED AT WING BOX SUPPORT UNDER PANEL 291 AL FR 23 C STR 1R, NEED TO BE FABRICATED. 2 H 7 2 4T RT 2008031900067 20080319 00067 EU 2008 3 19 TRAX200800373 1 20080304 A 5720 ANGLE AEROSP ATR72 ATR72 EU WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 ETNRC - ANGLES CRACKED AT WING BOX SUPPORT UNDER PANEL 295 DL AT FR 28D STR 1L AND 1R, NEED TO BE FABRICATED. 2 H 7 2 4T RT 2008031900075 20080319 00075 NM 2008 3 19 DXTA200802776 1 20080121 A 3297 D3899924WB98SN CONNECTOR GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE RT MLG DEFECTIVE E DXTA O OTHER N FALSE WARNING CL CLIMB 1 GL 07 752QS 596 152 AFTER TAKEOFF AT MLG AMBER AND RED HASHES FLASHED ON AND OFF THRU ENTIRE FLIGHT. REPLACED RT MLG CONNECTOR 44G1 USING CO NNECTOR P/N D38999/24WB98SN. BACKSHELL P/N TX1240AB90-1006A1 AND BOOT 202S132-25S. WORK IAW ENG ORDER DOC 4AS8104002 A0 13REV. PERFORMED RT MLG FWD AND AFT PROX UPLOCK SWITCH ADJUSTMENT AND FUNCTIONAL CHECK. OPS CHECK GOOD MM 32-10-41. 2 L 7 2 4F 4 F RT A53NM E35NE 2008031900100 20080319 00100 NM 2008 3 19 14779 1 20080201 A 2420 1701321D GCU EMB ERJ170 ERJ170200LR 3260121 NM MALFUNCTIONED A C77A K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 27 614CZ 12 17000205 WHILE ON MAINTENANCE, THE APU AGCU FAILED P/N 1701321D S/N 1324 INSPECTED MAU3 AND SPDA 2 NO DAMAGE, NOTED REPLACING AGC U. 2 L 7 2 4F RT A56NM 2008031900153 20080319 00153 NM 2008 3 19 KCSA081168 1 20080311 A 5210 DOOR FRAME BOEING 747 747SR46 1384816 NM PAX DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 MAIN ENTRY DOOR 4R LOWER AFT CORNER FRAME CRACKED AT PREVIOUS STOP DRILL. 2 L 7 4 4F RT A20WE 2008031900184 20080319 00184 EU 2008 3 19 TRAX200800384 1 20080307 A 3060 DEICE SYSTEM AEROSP ATR72 ATR72 EU NR 2 PROPELLER INTERMITTENT A ASOA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 634AS 370 NR 2 PROP DE-ICE INTERMITTENT IN FLIGHT. FLT 4206 DEL 300 MINS. NC FLT 4343 X2 CX & ON 3/7/08 FLTS 4343X2. CAPT DECLA RED EMERGENCY. 2 H 7 2 4T RT 2008031900187 20080319 00187 EA 2008 3 19 TRAX200800385 1 20080307 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 917EV 7769 ENGINE SUPPORT BEAM UPPER WEB CRACKED AT FS 640 LBL 9.5 WL 19.12. ALL REPAIRS PERFORMED IN ACCORDANCE WITH REO 601R-53- 61-345 AND REO 601R-58-61-348. 2 L 7 2 4F RT A21EA 2008031900189 20080319 00189 EA 2008 3 19 TRAX200800386 1 20080307 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 917EV 7769 FS 280 RBL 9 OUTBOARD CLIP CRACKED. 2 L 7 2 4F RT A21EA 2008031900193 20080319 00193 EU 2008 3 19 USAA920080605 1 20080310 A 5210 FE240221001 DIAPHRAGM RATIER AIRBUS 320 A320214 3930316 EU R2 DOOR DEFECTIVE A USAA K NONE O OTHER UK UNKNOWN 1 EA 19 122US 2629 1298 FLT 9225 - MBJ-CLT - R2 DOOR WOULD NOT MOVE WITH NORMAL PRESSURE. MAINTENANCE REPLACED THE DIAPHRAGM IN THE PERCUSSION MECHANISM OF THE RIGHT AFT DOOR DAMPER AND EMERGENCY OPERATION CYLINDER. DOOR OPERATION NORMAL. 2 L 7 2 4F RT A28NM 2008031900218 20080319 00218 EU 2008 3 19 USAA920080570 1 20080226 A 5315 D53472192200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651AW 866 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3257 /FR 68, +Y765. REPLACED CABIN FLOORBEAM, BS 3257 /FR 68, +Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900220 20080319 00220 EU 2008 3 19 USAA920080571 1 20080223 A 5347 D57130147202 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651AW 866 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SEAT TRACK BS 1590 /FR 36 - BS 1810 /FR 36, -Y1292. REPLACED CABIN S EAT TRACK BS 1590 /FR 36 - BS 1810 /FR 36, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900224 20080319 00224 EU 2008 3 19 USAA920080573 1 20080224 A 5315 D5347219020590 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651AW 866 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3043 /FR 64 - BS 3158 /FR 66, -Y1292. REPLACED CABIN FLOORBEAM, BS 3043 /FR 64 - BS 3158 /FR 66, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900238 20080319 00238 EU 2008 3 19 USAA920080587 1 20080224 A 5315 D5347218920200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651AW 866 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3257 /FR 68 - BS 3310 /FR 69, -Y1162. REPLACED CABIN F LOORBEAM, BS 3257 /FR 68 - BS 3310 /FR 69, -Y1162 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900239 20080319 00239 EU 2008 3 19 USAA920080588 1 20080224 A 5315 D53472172203 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651AW 866 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3158 /FR 66 - BS 3257 /FR 68, -Y1292. REPLACED CABIN F LOORBEAM, BS 3158 /FR 66 - BS 3257 /FR 68, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900243 20080319 00243 EU 2008 3 19 USAA920080596 1 20080308 A 3350 321454 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 651AW 866 SAL - EEL - C7 CHECK - RIGHT HAND EMERGENCY EXIT POWER SUPPLY INOPERATIVE. REPLACED AND FUNCTIONAL CHECKED THE RIGHT HA ND EMERGENCY EXIT POWER SUPPLY IAW A320 AMM 33-51-38. 2 L 7 2 4F RT A28NM 2008031900244 20080319 00244 EU 2008 3 19 USAA920080598 1 20080308 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 651AW 35846 35846 866 SAL - EEL - C7 CHECK - LEFT HAND SIDE EMERGENCY POWER SUPPLY UNIT INOPERATIVE. REPLACED LEFT HAND SIDE EMERGENCY POWER SUPPLY UNIT IAW A320 AMM 31-51-58. 2 L 7 2 4F RT A28NM 2008031900245 20080319 00245 NM 2008 3 19 USAA920080599 1 20080305 A 5320 D53471124200 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801AW 889 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SHEAR PLATE, BS 2936, FR 69 - BS 2992, +Y1292. REPLACED CABIN SHEAR PLATE, BS 2936, FR 69 - BS 2992, +Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900247 20080319 00247 NM 2008 3 19 KCSA081171 1 20080312 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE SKIN INTERNAL SURFACE CORRODED AT BS 1239, STR 2L. 2 L 7 4 4F RT A20WE 2008031900251 20080319 00251 CE 2008 3 19 DXTA200802808 1 20080129 A 3260 622EN2266 SQUAT SWITCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ZONE 700 INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 939QS 5968 7500193 AFTER TAKEOFF, GEAR WOULD NOT RETRACT. REMOVED AND REPLACED NLG SQUAT SWITCH WITH A NEW UNIT ALL WORK PERFORMED IAW MM C H 32-60-00. ALSO REPACKED NLG WHEEL BEARINGS IAW MM CH 32-40-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008031900255 20080319 00255 CE 2008 3 19 GLBA20061065 1 20080211 A 5330 SKIN BEECH 1900 1900D 1154162 CE BS 213-228 CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 257GL UE257 BELLY CORROSION FS 213.25 AND FS 228.25 AT STRINGERS 15R, 16R, 14L/13L AT FS 213.25 AND 15L/14L AT FS 228.25. MAINT REPA IRED DEBONDED STR 15R,15L,14L, FOR FS 213.25 TO FS 228.25 IAW SRM 53-90. STR REPAIR DIMENSIONS APPROX 10.5 INCHES. 2024 T-3. RII C/W IAW TASKCARD 8.2.1. 2 L 7 2 4T RT A24CE 2008031900258 20080319 00258 CE 2008 3 19 GLBA20061068 1 20080211 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 213-228 CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 257GL UE257 BELLY SKIN REPAIR DUE TO CORROSION REPAIR. SKIN REPAIR AREA APPROX 31.5 INCHES X 23 INCHES FROM FS 213.25/228.25 AND ST RINGERS 13L TO 15R. MAINT REPAIRED BELLY SKIN 15R TO 13L AT/FROM FS 213.25 TO FS 228.25 IAW SRM 51-70. REPAIR DIMENSION 26.250 INCHES X 33.5 INCHES 2024 T3 .025. RII C/W IAW T.C. 8.2.1 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900259 20080319 00259 EU 2008 3 19 45302172008 1 20080217 A 2422 RX060 CONVERTER UROCOP EC135 EC135P2 5620027 EU BURNED E QMLA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 NM 03 534LN 0453 DURING A HEMS FLIGHT WITH PATIENT ON BOARD, THE CREW SMELLED AN ELECTRICAL BURNING ODOR. THE AC WAS LANDED SAFELY. OTH ER TRANSPORT WAS ARRANGED AND MAINT CALLED. THE ONLY FAILURE THE MECHANIC FOUND WAS A 110 VAC TO 28 VDC CONVERTER, THAT WAS USED WITH THE IV WARMER, THAT HAD FAILED AND WAS SUSPECTED TO BE THE CAUSE OF THE ODOR. THE EXTERIOR OF THE CONVER TER WAS NOT SHOWING SIGNS OF OVERHEATING. THE CONVERTER WAS REPLACED AND THE AC WAS RELEASED FOR SERVICE. 1 G 7 2 3U H88EU 2008031900268 20080319 00268 EA 2008 3 19 S9BA200800013 1 20080222 A 2750 C6CF108511 CONTROL ROD DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA TE FLAPS CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 888PV 855 620 125 HR INSPECTION, EMERGENCY MEASURES EXECUTED, NO, AC GROUNDED. NO CORROSION FOUND ON RT FLAP INTERCONNECT ROD UNDER FLEXIBLE BOOT. ON IB END. REMOVED AND REPLACED CONTROL ROD. 1 H 7 2 3T 4 T RT A9EA E4EA 2008031900269 20080319 00269 CE 2008 3 19 GLBA20061060 1 20080218 A 5320 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 288 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 184UX UE184 RT WING TO FUSELAGE HEAVY ANGLE CRACKED APPROX 2.125 INCH AT FWD BEND RADIUS AT FS 288.0. MAINT REPAIRED THE LT TO FUSEL AGE HEAVY ANGLE IAW SRM 53-90. REPAIR APPROX 13.5 INCH. RII INSP COMPLIED WITH IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900271 20080319 00271 CE 2008 3 19 GLBA20061059 1 20080218 A 5320 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 288 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 184UX UE184 LT WING TO FUSELAGE HEAVY ANGLE CRACKED APPROX 1.750 AT FWD BEND RADIUS AT FS 288.0. MAINT REPAIRED THE LT TO FUSELAGE H EAVY ANGLE IAW. SRM 53-90. REPAIR APPROX 13.5 INCH. RII INSP COMPLIED IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900275 20080319 00275 NM 2008 3 19 USAA920080617 1 20080209 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER TIE CLIP, BS 616, S8R. REPLACED STRINGER TIE CLIP, BS 616, S8R IAW B7 37 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008031900278 20080319 00278 NM 2008 3 19 SB08013 1 20080309 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 439US 24781 MIA - MAINTENANCE REPORTED THE EMERGENCY EXIT SLIDE LIGHTS AT RIGHT-HAND SIDE (FORWARD, AFT AND OVERWING LIGHTS-EXTERIOR ) ALONG WITH THE LEFT AND RIGHT OVERWING ESCAPE HATCH AND SEAT MOUNTED EXIT IDENTIFIERS INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE BATTERY PACKS. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008031900287 20080319 00287 CE 2008 3 19 GLBA20061072 1 20080219 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 248 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 184UX UE184 FUSELAGE SKIN CRACK IN/AT PREVIOUS REPAIR CRACK APPROX 1 INCH LENGTH AT FS 248.0 ABOVE STR 9L. MAINT REPAIRED FUSELAGE S KIN AT FS 248.0 IAW SRM 51-70. REPAIR DIMENSIONS APPROXIMATELY 14 FT BY 12.5 FT, 2024 T3 .040. RII INSP C/W IAW TASKCA RD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900289 20080319 00289 NE 2008 3 19 SA08011 2 20080307 A 7530 5860017139 ACTUATOR AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE NR 1 ENGINE FAILED A USAA A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 19 808AW 21937 1088 V11027 ORD FLT 269 - LAS TO YYZ. WHILE AT FL 370, EXPERIENCED AN ENGINE ONE COMPRESSOR STALL. ABOUT 30 MINUTES LATER, THE NUM BER ONE ENGINE STALLED AGAIN. FLIGHT DIVERTED INTO ORD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ENGIN E ONE ACC ACTUATOR. OPERATIONALLY CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031900290 20080319 00290 EU 2008 3 19 USAA920080563 1 20080229 A 5320 D5311224200 FITTING AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651AW 866 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOOR CORNER FITTING, BS 783 /FR 19A - BS 808 / FR 20, S19L. REPLACE D CABIN FLOOR CORNER FITTING, BS 783 /FR 19A - BS 808 / FR 20, S19L IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900294 20080319 00294 EU 2008 3 19 USAA920080566 1 20080301 A 5315 D53472188202 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651AW 866 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3257 /FR 68, +Y1292. REPLACED CABIN FLOORBEAM, BS 3257 /FR 68, +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900296 20080319 00296 NM 2008 3 19 USAA920080604 1 20080225 A 5321 D5367180500300 FLOORBOARD AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801AW 889 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBOARD 262FF. REPLACED CABIN FLOORBOARD 262 FF IAW A319 AMM 53-4 2-12. 2 L 7 2 4F RT A28NM 2008031900298 20080319 00298 SW 2008 3 19 AC2A021408001 1 20080214 A 6320 GEARBOX AGUSTA AB139 AB139 0260110 SW PWA PT6 PT6* 52043 EA MAKING METAL E AC2A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 31 139JP 31039 IN CRUISE FLIGHT, AT 3500 MSL, THE MGB CHIP SUMP CAS MESSAGE CAME ON. FOLLOWED THE EMERGENCY PROCEDURE. THE CHIP BURNER WOULD NOT CLEAR THE CHIP. LANDED AT AIRPORT WITHOUT INCIDENT. FOUND 3 SMALL FLAKES ON RT LOWER CHIP PLUG. PERFORMED SERV ICEABILITY CHECK AND FOUND SERVICEABLE. 2 G 7 2 4U 3 T R00002RD E2NE 2008031900310 20080319 00310 NM 2008 3 19 BB08033 1 20080311 A 7334 21SN04158C PRESSURE SWITCH BOEING 757 7572G7 1384963 NM RROYCE RB211 RB211535E4 54555 NE FUEL SYSTEM FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 910AW 24523 30560 HNL - FLT 9030 OGG TO PHX. DURING CLIMB, RECEIVED EICAS MESSAGE "L ENG LP PUMP", WITH A FUEL TEMP OF +35. FLIGHT DIVE RTED TO HNL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED, INSPECTED, THEN REPLACED THE LEFT ENGINE LOW PRES SURE FUEL FILTER. AFTERWARDS, MAINTENANCE REPLACED THE FUEL PRESSURE SWITCH. OPERATIONALLY AND LEAK CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E12EU 2008031900311 20080319 00311 2008 3 19 BB08034 4 20080311 A 2565 D30654122 SLIDE RAFT BOEING 757 757225 1384959 NM R1 DOOR OUT OF POSITION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 919UW 1470 22198 CLT - THE R1 DOOR ESCAPE SLIDE FELL OUT OF CONTAINER. MAINTENANCE REPLACED THE R1 DOOR ESCAPE SLIDE. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2008031800099 20080318 00099 NM 2008 3 18 UPS08M51793 1 20080226 A 5512 SKIN DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 2 LEFT BARREL NUT BORE HOLE, (UPPER). REMOVED CORROSION, FABRICATED, AND INSTA LLED REPAIR BUSHING PER EO MD11-5510-19409-M, BUSHING OD 1.069 BORE I.D. 1.035. 2 L 7 3 4F RT A22WE 2008031800116 20080318 00116 NM 2008 3 18 2008UALA01247 1 20080307 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 FOUND SEAT EEL INOP:22L FWD SECTION. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031800148 20080318 00148 NM 2008 3 18 2008UALA01299 1 20080309 A 5753 SUPPORT FITTING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 7 FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 NR 7 FLAP UNDER WING SUPPORT FITTING IS WORN ON OUTBD SIDE, IB END, NR 7V JOINT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008031800155 20080318 00155 NM 2008 3 18 2008UALA01308 1 20080308 A 3510 OXYGEN SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CREW O2 LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 305UA 23666 CREW O2 LOW. SERVICED OXYGEN SYSTEM. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800156 20080318 00156 NM 2008 3 18 2008UALA01310 1 20080307 A 3350 BRACKET BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EXIT LIGHT DEBONDED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 AFT OVERWING EMERGENCY LIGHT BRACKET DISBONDED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800184 20080318 00184 EU 2008 3 18 F3LA200800088 1 20080303 A 2560 MS21060L3 STRAP AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE NUT PLATE STRAP, UNDER THE FORWARD GIRT BAR FITTING , BELOW THE BLANKING PLATE, AT THE R-1 DOOR. MAINTENANCE INSTALLED A NEW NUT PLATE STRAP IN ACCORDANCE WITH THE REQUIRE MENTS OF A319 SRM 51-72-11. UPON INSTALLATION OF THE NEW STRAP, IT WS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008031800196 20080318 00196 SO 2008 3 18 LR7A08028 1 20080128 A 5320 3622571 STIFFENER LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 560 4606 DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5302, FOUND OVERHEAD STIFFENER CRACKED AT FS940, WL284, LBL22. REPAIR ACCOMP LISHED IAW SMP583 FIG 51-140-19. 2 H 7 4 4T A1SO 2008031900005 20080319 00005 NM 2008 3 19 ANCF200800005 1 20080103 A 3150 UNKNOWN BOEING 757 757236 1384971 NM UNKNOWN UNKNOWN W ANCF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 522NA 25133 DURING CLIMB, 8 MINUTES AFTER TAKEOFF, AT 20.500 FEET, EICAS MESSAGE "LEFT ENGINE OVERHEAT" IS SHOWED. CHECK LIST WAS P ERFORMED. VISUAL INSPECTION AND CHECK OF CONDITION OF ALL PNEUMATIC DUCTS, VALVES AND ALSO LINES. BITE PROCEDURE WAS A CCOMPLISHED IN ACCORDANCE WITH FIM 26-11-00 PAGE 106-108. TEST WAS PERFORMED WITH ENGINE RUN UP WITH TAKEOFF POWER SET, NO EICAS MESSAGE WAS PRESENTED. AIRCRAFT IS OK. 2 L 7 2 4F RT A2NM 2008031900024 20080319 00024 CE 2008 3 19 GUUA02240801 1 20080224 A 5260 12951405913 CABLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA AIRSTAIR DOOR FAILED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 53545 UE185 PILOT REPORTED AIRSTAIR DOOR WILL NOT OPEN. REPLACED UPPER AIRSTAIR DOOR CABLES. 2 L 7 2 4T 3 T RT A24CE E2NE 2008031900057 20080319 00057 WP 2008 3 19 MWEA080039 1 20080305 A 5330 5920323555 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 813ME 48007 DENT IN FUSELAGE AT STATION 273 BETWEEN LONGERON 22 & 21 RIGHT. PERFORMED INSPECTION AT DENTED AREA, NO CRACKS FOUND. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2008031900084 20080319 00084 SO 2008 3 19 GLBA20061058 1 20080129 A 5712 RIB EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT WING CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 108UX 120108 RT RIB NR 18 CRACKED APPROX .375 INCH IN LENGTH AT STRINGER NR1 AT WS YA-5405. MAINTENANCE REMOVED DAMAGED AREA AND INS TALLED REPAIR PIECE CUT FROM NEW RIB. IAW SRM 57-20-07. 2 L 7 2 4T 4 T RT A31SO E20NE 2008031900093 20080319 00093 NM 2008 3 19 KCSA081160 1 20080309 A 5524 WEB BOEING 747 747209B 138489B NM LT ELEVATOR GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 LEFT O/B ELEVATOR I/B END CLOSURE WEB GOUGED, ELEV STA 194. 2 L 7 4 4F RT A20WE 2008031900105 20080319 00105 WP 2008 3 19 ASMF200802001 1 20080204 A 3231 PROXIMITY SWITCH DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE MLG DOOR MALFUNCTIONED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 838AM 49397 DURING TRANSIT CHECK WAS DETECTED GEAR DOOR OPEN LIGHT TURNED ON. TECH VERIFIED TARGET SENSORS AND PERFORMED AUTO TEST T O THE PROXIMITY SWITCH, BUT LIGHT CONTINUED; SO PROXIMITY SWITCH WAS REPLACED IAW MM 36-60-04, REMAINING SAME CONDITION. AC WAS SENT TO THE HANGAR AND MAIN LANDING GEAR DOORS TARGET SENSOR WAS ADJUSTED IAW MM 32-60-05, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2008031900108 20080319 00108 CE 2008 3 19 020108N547CS1 1 20080130 A 3233 99125374 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG FAILED E Z5FA O OTHER J WARNING INDICATION AP APPROACH 1 EA 63 547CS 3047 5605542 RT MAIN GEAR DOWN INDICATION FAILED TO ILLUMINATE AFTER GEAR EXTENSION. CREW RAN AFM CHECK LIST PROCEDURES WITH NO CHANG E. GEAR BLOWN DOWN, EMERGENCY DECLARED AND AC LANDED WITHOUT INCIDENT. AC CURRENTLY IN MAINT 02/01/2008. ON SITE MAINT REPLACED RT MAIN GEAR ACTUATOR, OPS CHECKED GOOD, AC RETURNED TO SERVICE 02/02/2008. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008031900111 20080319 00111 CE 2008 3 19 DJFA2008015 1 20080205 A 2170 18084928 COALESCER BAG BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE ODOR E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 441LX RK292 DURING CRUISE, CREW REPORTED BURNING ODOR WITH HEAT IN AUTO OR MANUAL. AIRCRAFT LANDED SAFELY AT INTENDED DESTINATION. MAINTENANCE RAN THE ENGINES AND NOTED A MOLDY SMELL BUT NOT A BURNING SMELL. THE COALESCER BAG WAS REPLACED AND ALL SM ELLS WENT AWAY. 2 H 7 2 4F 4 F RT A16SW E25EA 2008031900144 20080319 00144 EU 2008 3 19 USAA920080597 1 20080307 A 2782 830A000004 ACTUATOR AIRBUS 320 A320214 3930316 EU L/E SLAT MALFUNCTIONED A USAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 19 121UW 24870 1205 1294 FLT 1643 - CLT-PHX - EMERGENCY LANDING - DURING APPROACH, SLATS FAILED TO DEPLOY. CREW MADE A CONFIG 3 LANDING AND LAND ED AT APPROXIMATELY 158 KTS. NO BRAKING ISSUES. EMERGENCY EQUIPMENT HAD RESPONDED BUT AIRCRAFT TAXIED TO THE GATE WITH OUT INCIDENT. MAINTENANCE FOUND ACTUATOR 6029CM INDICATOR POPPED. REMOVED AND REPLACED B-SLAT ACTUATOR 6029CM. OPERAT IONAL CHECK WAS NORMAL. 2 L 7 2 4F RT A28NM 2008031900156 20080319 00156 NM 2008 3 19 KCSA081170 1 20080311 A 5210 FITTING BOEING 747 747SR46 1384816 NM R1 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 MAIN ENTRY DOOR 1R UPPER AFT CORNER FITTING CRACKED BS 485. 2 L 7 4 4F RT A20WE 2008031900190 20080319 00190 EA 2008 3 19 TRAX200800387 1 20080307 A 2560 GLOWSTRIP CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 730EV 10141 FLOOR EMERGENCY LIGHTING PHOTOLUMINESCENT STRIP MISSING IN FRONT OF GALLEY CARTS. 2 L 7 2 4F RT A21EA 2008031900236 20080319 00236 EU 2008 3 19 USAA920080586 1 20080226 A 5315 D53472094008 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651AW 866 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3158 /FR 66, +Y519.5. REPLACED CABIN FLOORBEAM, BS 315 8 /FR 66, +Y519.5 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900280 20080319 00280 NM 2008 3 19 CALA0800211 1 20080306 A 5311 BAC1517705 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16703 28764 FUSELAGE FRAME CRACKED AT BRACKET MOUNT BETWEEN STR 8 AND 9 LT AT STA 747. INTERIM REPAIRED PER ECRA5310-04729. DIP CO NTROL NUMBER 86938. 2 L 7 2 4F RT A16WE 2008031900283 20080319 00283 2008 3 19 SA08008 4 20080307 A 2565 D30665105 SLIDE RAFT AIRBUS A319 A319112 3930323 EU R2 DOOR BULGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 708UW 19992 1871 0972 PIT - THE R2 DOOR ESCAPE SLIDE COVER WAS FOUND TO CONTACT THE FUSELAGE WHEN THE DOOR WAS FULLY OPENED. MAINTENANCE REPL ACED THE R2 DOOR ESCAPE SLIDE. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2008031900285 20080319 00285 NE 2008 3 19 SA08010 2 20080307 A 7532 AC69924 BLEED VALVE AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE NR 1 ENGINE FAULTY A USAA A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 19 808AW 21943 15769 1088 V11027 ORD FLT 269 - LAS TO YYZ. WHILE AT FL 370, EXPERIENCED AN ENGINE ONE COMPRESSOR STALL. ABOUT 30 MINUTES LATER, THE NUM BER ONE ENGINE STALLED AGAIN. FLIGHT DIVERTED INTO ORD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ENGIN E ONE SEVENTH STAGE, LOWER RIGHT (7B), BLEED VALVE. OPERATIONALLY CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031900305 20080319 00305 NM 2008 3 19 USAA920080612 1 20080227 A 5312 6517582 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 CLT - MAJOR REPAIR - C17 CHECK - CRACKED BULKHEAD WEB, BS 178, RBL 17, WL 230. REPLACED BULKHEAD WEB, BS 178, RBL 17, W L 230 IAW B737 SRM 53-10-08. 2 L 7 2 4F RT A16WE 2008031900307 20080319 00307 NM 2008 3 19 USAA920080614 1 20080225 A 5310 652072328 DOOR FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 456UW 25020 PIT - MAJOR REPAIR - FPBH INSPECTION - FORWARD CARGO DOOR CUTOUT AFT FRAME CRACKED, BS 492.4, S24R. REPAIRED FORWARD CA RGO DOOR CUTOUT AFT FRAME, BS 492.4, S24R IAW USAIRWAYS EA 110728. 2 L 7 2 4F RT A16WE 2008031900308 20080319 00308 NM 2008 3 19 USAA920080615 1 20080310 A 5330 6545776 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT - MAJOR REPAIR - RON - CRACKED FUSELAGE SKIN, BS 727F, S25R. REPAIRED FUSELAGE SKIN, BS 727F, S25R IAW USAIRWAYS EA 100306. 2 L 7 2 4F RT A16WE 2008031900309 20080319 00309 NM 2008 3 19 CALA0800214 1 20080311 A 5610 58935733 WINDOW BOEING 737 737524 1384721 NM COCKPIT CRACKED A CALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 27 14655 26863 28916 CAPTAINS R4 WINDOW CRACKED ON INNER PANEL EN ROUTE, NO WINDOW HEAT WAS ON EFFECTED WINDOW (COLD) CONTROLLER WAS ON. REM OVED AND REPLACED LEFT HAND NUMBER 4 WINDOW IAW MM 56-11-31 PAGE 401-414. 2 L 7 2 4F RT A16WE 2008031900316 20080319 00316 2008 3 19 712902242008 4 20080224 A 2297 WIRE BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE COCKPIT CHAFED E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 485UM 7129 IMMEDIATELY AFTER TAKEOFF, AN ELECTRICAL BURNING ODOR WAS NOTED IN THE COCKPIT. SPAS (STICK POSITION AUGMENTATION SYSTE M) LIGHT ILLUMINATED AND SPAS CIRCUIT BREAKER POPPED. AC LANDED BACK AT HOME BASE WITH OUT INCIDENT AFTER 6 MINUTES OF FLIGHT. THE COMPUTER DAMAGED DUE TO CHAFED WIRES IN THE SPAS HARNESS. 1 G 7 2 3U 3 U H13EU E5NE 2008031900317 20080319 00317 CE 2008 3 19 DXTA200802813 1 20080130 A 5270 LATCH CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE LT MLG DOOR OUT OF ADJUST E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 357QS 6800155 AFTER T/O AND AFTER GEAR RETRACTION, AMBER NOSE DOOR L CAS MESSAGE APPEARED. ADJUSTED L DOOR LATCHES IAW MM CHAP 52-40- 20. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RC T00012WI E35NE 2008031900319 20080319 00319 EA 2008 3 19 TRAX200800395 1 20080309 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 718EV 10095 PAX DOOR HANDLE VERY DIFFICULT TO OPEN. 2 L 7 2 4F RT A21EA 2008031900327 20080319 00327 NM 2008 3 19 USAA920080603 1 20080302 A 5320 D53471124201 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801AW 889 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SHEAR PLATE, BS 2936 / FR 69 - BS 2992 / FR 70, -Y1292. REPLACED CAB IN SHEAR PLATE, BS 2936 / FR 69 - BS 2992 / FR 70, -Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900330 20080319 00330 NM 2008 3 19 USAA920080620 1 20080312 A 5340 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 CLT - MAJOR REPAIR - C17 CHECK - CRACKED STRINGER CLIP, BS 937, S25R. REPLACED STRINGER CLIP, BS 937, S25R IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008031900331 20080319 00331 NM 2008 3 19 USAA920080621 1 20080229 A 5322 6546573 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 CLT - MAJOR REPAIR - C17 CHECK - CRACKED SHEAR TIE, BS 1088, S2R. REPLACED SHEAR TIE, BS 1088, S2R IAW B737 SRM 51-10-0 2. 2 L 7 2 4F RT A16WE 2008031900337 20080319 00337 CE 2008 3 19 DXTA200802818 1 20080131 A 2750 RESOLVER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS OUT OF ADJUST E DXTA O OTHER F FLT CONT AFFECTED LD LANDING 1 GL 07 919QS 7500224 FLAPS FAILED AT 15 DEGREES, PUSHED RESET BUTTON AND FLAPS REMAINED FAILED. FOUND BITES 1, 2 AND 9 ILLUMINATED. RESET CO NTROLLER, FLAPS WORKED NORMALLY. TROUBLESHOT FEEDBACK SYS RT FLAP RESOLVER OUT OF ADJUSTMENT. RIGGED RT RESOLVER TO MATC H LT RESOLVER FOR ZERO VOLTAGE DIFFERENCE. ELECTRICAL RIG CHECK OF RESOLVERS FOUND NORMAL. OPS CHECK OF FLAPS, NORMAL. W ORK DONE IAW MM CH 27-50-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008031900338 20080319 00338 CE 2008 3 19 DXTA200802819 1 20080131 A 2741 701730031444 COMPUTER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL STAB TRIM INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 913QS 5374 7500113 AT FL410 GOT AMBER PRI STAB TRIM FAIL. TROUBLESHOT TO NR1 (LT) IAC, REMOVED REPLACED AND OPS CHECK GOOD, NR1(LT) IAC IAW MM 34-25-01 NO OTHER DEFECTS NOTED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008031900339 20080319 00339 NM 2008 3 19 USAA920080625 1 20080228 A 5540 D5537131800200 HINGE FITTING AIRBUS A319 A319132 3930340 NM RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801AW 889 SAL - MAJOR REPAIR - C7 CHECK - RUDDER HINGE FITTING NR 3 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 2279 / RIB 5. REPLACED RUDDER HINGE FITTING NR 3, VERTICAL STABILIZER STATION 2279 / RIB 5 IAW A319 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2008022700257 20080227 00257 2008 2 27 NWAA080633141 4 20080222 A 2565 60592101 CABLE AIRBUS A319 A319114 3930350 NM ESCAPE SLIDE BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 341NB 16317 16317 1738 LT EMERGENCY EXIT RESERVOIR FLEX CABLE END FOUND BROKEN DURING PREDOCK CHECK. REPLACED LT OFFWING ESCAPE SLIDE INFLATIO N RESERVOIR. OPS TEST GOOD. 2 L 7 2 4F RT A28NM 2008022700258 20080227 00258 NM 2008 2 27 UIEA200800021 1 20080126 A 5730 SKIN BOEING 747 7472D3B 1384805 NM LT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 LT WING LEADING EDGE LOWER SURFACE, OUTBOARD FUELING DOOR FRAME CUT-OUT HAS A COMPOSITE CRACK AT OUTBOARD SIDE, FORWARD EDGE. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18 SHEETS 3 AND 5 AND SRM 51-40-12, PREPREG 250 DE GREES F CURE. ALSO, REFERENCE ATLAS AIR EO 4757A414. 2 L 7 4 4F RT A20WE 2008022700259 20080227 00259 EU 2008 2 27 CALA0800146 2 20080214 A 7200 03720090001 ENGINE BOEING 737 737524 1384721 NM CFMINT CFM56 CFM563C1 13802 EU LEFT FAILED A CALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 37615 27328 AFTER LIFT OFF THICK SMOKE IN COCKPIT VISIBILITY IMPAIRED WHICH SLOWLY CLEARED. SMELL AND VISIBLE SMOKE THROUGHOUT THE AIRCRAFT. NR 1 ENGINE WAS BORESCOPED AND OIL FOUND IN ALL STAGES. ENGINE REPLACED PER W/C 03-7100-1-9400. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022700260 20080227 00260 2008 2 27 UIEA200800029 4 20080206 A 8300 GEARBOX BOEING 747 7472D7B 1384803 NM GE CF6 CF680 30025 NE ZONE 400 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 NR 4 ENGINE GEAR BOX WAS FOUND WITH A 3.0 INCH CRACK ON INBOARD SIDE OF FUEL PUMP DRIVE PAD AREA. ENGINE CHANGE IS CURR ENTLY IN PROGRESS. 2 L 7 4 4F 4 F RT A20WE E13NE 2008022700263 20080227 00263 NM 2008 2 27 UIEA200800040 1 20080212 A 5420 321U2731102 BRACE BOEING 747 7472D7B 1384803 NM WORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 NR 4 DIAGONAL BRACE FORWARD PORTION LOWER SURFACE PRIMER DISCOLORED. REPLACED DIAGONAL BRACE PER MM 54-10-03. 2 L 7 4 4F RT A20WE 2008022700009 20080227 00009 EA 2008 2 27 COMA0860109 1 20080204 A 2752 853D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 814CA 13800 7387 FLIGHT 5620 - RECEIVED FLAP FAIL CAUTION MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED INBOARD ACTUAT OR ON LEFT OUTBOARD FLAP. PERFORMED CARD SI-2-2710001. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008022700010 20080227 00010 EA 2008 2 27 COMA0860110 1 20080204 A 2752 854D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 814CA 13800 7387 FLIGHT 5620 - RECEIVED FLAP FAIL CAUTION MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED OUTBOARD ACTUA TOR ON LEFT OUTBOARD FLAP. PERFORMED SI-2-270001. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008022700016 20080227 00016 NM 2008 2 27 WRLA2008025 1 20080214 A 5753 SKIN DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE FLAP VANE DEBONDED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 48632 DURING C-CHECK INSPECTION FOUND LEFT INBOARD FLAP VANE LOWER SKIN DISBONDED TWO PLACES (20" X 23.5", 18" X 22"). REPAIR ED LH FLAP VANE REF JOB CARD 038236 ITEM 1. 2 L 7 3 4F 4 F RT A22WE E24NE 2008022700027 20080227 00027 WP 2008 2 27 IXXA08SMN016S 1 20080115 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND LT WING UPPER SKIN CORRODED AROUND FASTENERS AT STATION XRS 278.000 STRINGER10. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. FILLED WITH SEALANT REWORKED AREA. PERFORMED NDT NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER. TAPERED REPAIR DOUBLER CLEANED, TREATED , AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTNERS AND REPAIR PARTS IAW FAA FORM 8110-3 NR 08042 DATED 01-29-08 DRAWING ED-4688 DATED 01-17-08, SRM 51-1-21, 51-3-0, SRM 51-1-8 PAGES 17-18, SRM 57-2-0 PAGE 16, SRM 51-1-11, NDT SPM P ART 06-10-01-001, SRM 51-1-12 PAGE 7, SRM 51-1-20D, AND 51-3-1. 2 L 7 4 4F 4A25 2008022700038 20080227 00038 EA 2008 2 27 COMA0860118 1 20080210 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 932CA 7038 FLIGHT 5232 - RECEIVED FLAP FAIL MESSAGE ON APPROACH. ABORTED APPROACH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. C OMPLIED WITH SI-2-27I0001 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, FLAP SYSTEM WAS RESET WITH NO FURTHER M ESSAGES. 2 L 7 2 4F RT A21EA 2008022700051 20080227 00051 EA 2008 2 27 COMA0860126 1 20080211 A 2750 860D10018ABCD ECU CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 821CA 14940 7420 FLIGHT 5366 - FLAPS FAIL CAUTION MESSAGE AT 0 DEGREES ON APPROACH WHEN SELECTING FLAPS TO 8 DEGREES. EMERGENCY DECLARED , AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED FECU. 2 L 7 2 4F RT A21EA 2008022700052 20080227 00052 EA 2008 2 27 COMA0860127 1 20080211 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 821CA 15229 7420 FLIGHT 5366 - FLAPS FAIL CAUTION MESSAGE AT 0 DEGREES ON APPROACH WHEN SELECTING FLAPS 8 DEGREES. EMERGENCY DECLARED, A IRCRAFT LANDED SAFELY. REMOVED AND REPLACED PDU. 2 L 7 2 4F RT A21EA 2008022700053 20080227 00053 EA 2008 2 27 COMA0860128 1 20080211 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 721CA 7259 FLIGHT 5190 - FLAPS FAIL CAUTION MESSAGE ON APPROACH. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. COMPLIED WITH SI-2-2 710001 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2008022700055 20080227 00055 EA 2008 2 27 COMA0860130 1 20080213 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 591SW 7079 FLIGHT 5200 - FLAPS FAIL CAUTION MESSAGE, LEFT FLAP AT 2 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY. COMPLIED WITH SI- 2-2710001 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2008022700057 20080227 00057 EA 2008 2 27 COMA0870007 1 20080216 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA E&E BAY DOOR MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 371CA 10082 FLIGHT 5579 - AVIONICS BAY DOOR CAUTION MESSAGE DURING TAKEOFF ROLL. ABORTED TAKEOFF SAFELY. INSPECTED AVIONICS BAY DO OR AND HANDLE, NO DEFECTS FOUND. OPS CHECK OF DOOR INDICATION NORMAL. 2 L 7 2 4F RT A21EA 2008022700059 20080227 00059 EA 2008 2 27 COMA0860133 1 20080204 A 5730 6001038058 SKIN PANEL CNDAIR CL600 CL6002B19 1900309 EA RT WING CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA * 7012 SKIN PANEL ON RIGHT LOWER WINGTIP FOUND CHAFED THRU AT WS 407. REPLACED DAMAGED SKIN PANEL. 2 L 7 2 4F RT A21EA 2008022700060 20080227 00060 NM 2008 2 27 UIEA200800048 1 20080215 A 5753 SKIN BOEING 747 7472D7B 1384803 NM TE FLAP CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 LEFT OUTBOARD AFT FLAP UPPER SKIN HAS MINOR SURFACE CORROSION FOUND AFT OF OUTBOARD OF NR 2 SPINDLE. BLENDED OUT CORROS ION IAW SRM 51-10-01. REPROTECTED PER 51-10-02. 2 L 7 4 4F RT A20WE 2008022700064 20080227 00064 EA 2008 2 27 COMA0860136 1 20080217 A 3234 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAILED A COMA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 SO 01 797CA 21536 7344 FLIGHT 5386 - LANDING GEAR DISAGREE MESSAGE WHEN SELECTING GEAR DOWN. NOSE GEAR DOWN AND LOCKED MAINS REMAINED UP AND L OCKED. FOLLOWED QRH, PERFORMED MANUAL EXTENSION. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED MAI N LANDING GEAR SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2008022700067 20080227 00067 NM 2008 2 27 ASAA0842550 1 20080217 A 5210 69242491 LINK BOEING 737 7374Q8 138447Q NM L1 DOOR BROKEN A ASAA K NONE O OTHER NR NOT REPORTED 1 NM 02 762AS 25099 L1 DOOR IS DIFFICULT TO CLOSE. NOT A SMOOTH ACTION, FEELS LIKE IT CATCHES ON SOMETHING. FOUND RADIUS LINK BROKEN. REP LACED LINK ASSY & SNUBBER. NO HELP, DOOR STILL HARD TO CLOSE. ADJUSTED L1 GUIDE ARM. DOOR OPERATES NORMALLY. 2 L 7 2 4F RT A16WE 2008022700070 20080227 00070 NM 2008 2 27 UIEA200800027 1 20080202 A 5312 BULKHEAD BOEING 747 7472D7B 1384803 NM BS 2397 DAMAGED A UIEA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 527MC 22471 PRELIMINARY REPORT, ON TAKEOFF ROTATION, FREIGHT CAME LOOSE ON MAIN DECK SLID AFT AND PENETRATED THE AFT PRESSURE BULKHE AD. CREW PERFORMED AN ATB AND LANDED WITHOUT INCIDENT INTO LFW. AIRCRAFT SUSTAINED APPROX 12 INCH HOLE. AIRCRAFT DAMA GE BEING EVALUATED BY MANUFACTURE TEAM. 2 L 7 4 4F RT A20WE 2008022700074 20080227 00074 NM 2008 2 27 ASAA0842551 1 20080117 A 5320 65479575 INTERCOSTAL BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT INTERCOSTAL AT BS 787 792 RBL 19 FOUND CORRODED. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022700075 20080227 00075 NM 2008 2 27 ASAA0842559 1 20080115 A 5347 65468136 SEAT TRACK BOEING 737 7374S3 1384711 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 SEAT TRACK AT BS 536 RBL 25 GOUGED. SEAT TRACK REPAIRED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008022700076 20080227 00076 NM 2008 2 27 ASAA0842560 1 20080115 A 5347 65468136 SEAT TRACK BOEING 737 7374S3 1384711 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 SEAT TRACK AT BS 536 RBL 45 GOUGED. SEAT TRACK REPLACED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008022700080 20080227 00080 2008 2 27 SWAA080889 4 20080218 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 216WR 32488 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008022700081 20080227 00081 NM 2008 2 27 SWAA080882 1 20080215 A 2824 405744 ACTUATOR BOEING 737 7377H4 1384404 NM FUEL CROSSFEED FAULTY A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 29 226WN 32494 DIVERSION/DECLARED EMERGENCY. AT CRUISE FUEL IMBALANCE REPORTED, NR 2 TANK CONTINUED DECREASING WITH PUMPS OFF. REMOVE D AND REPLACED CROSSFEED VALVE ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2008022700092 20080227 00092 2008 2 27 SWAA080907 4 20080218 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 413WN 29819 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031300008 20080313 00008 EU 2008 3 13 UPS08151744 1 20080302 A 2420 GCU AIRBUS A300 A300F4622R 3930360 EU COCKPIT FAILED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 124UP 0808 ATB - PRIMARY FLT AND NAV DISPLAYS BLANKING. C/W TSM 24-00-00 FAULT ISOLATION CH GPCU BITE. GCU FAILED. REMOVED AND REPLACED NR 2 ENGINE GCU REF A300 MM 24-22-12-00. PERFORMED OPERATIONAL TEST REF AMM 24-41-00-05. TESTS OK, OK TO CONT INUE SERVICE. 2 L 7 2 4F RT A35EU 2008031300025 20080313 00025 WP 2008 3 13 UPS08851750 1 20080221 A 5313 DC853B00939 LONGERON DOUG DC8 DC873F 302199F WP BS 1750 L15L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 AFT CABIN L15L CRACKED AT CANTED FRAME STA 1750. REPAIRED LONG 15L AND SPICE AT CANTED FRAME STA 175 0 IAW SRM 53-02-02 FIG 10, SRM 51-1-24 AND SRM 51-1-8. 2 L 7 4 4F RT 4A25 2008031300026 20080313 00026 WP 2008 3 13 UPS08851751 1 20080219 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP COCKPIT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 COCKPIT FLOORPANEL 680 HAS LARGE FIELD REPAIR, DAMAGE CHANNELS AND SKIN. FABRICATED COCKPIT FLOORPAN EL 680 IAW DWG 3619352 AND S2755898, SRM 51 -1-8 AND SRM 51-01-21. 2 L 7 4 4F RT 4A25 2008031300055 20080313 00055 NM 2008 3 13 ASAA0852688 1 20080229 A 4990 38809381 FILTER BOEING 737 737890 1384527 NM APU CLOGGED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 557AS 35176 OIL FILTER INDICATING SERVICING DUE. FOUND DURING TASKCARD 78349013. REPLACED OIL FILTER. OP & LEAK CHECK GOOD. DPI RESET. 2 L 7 2 4F RT A16WE 2008031300094 20080313 00094 NM 2008 3 13 HNAA0800093 1 20080220 A 3230 841005 PSEU DHAV DHC8 DHC8102 2809003 NM NLG MALFUNCTIONED A HNAA K NONE J WARNING INDICATION CR CRUISE 1 EA 07 912HA 38462 486 040 AT 10,000 FT AND 210 KNOTS NOSE GEAR EXTENDED UNCOMMANDED FOR APPROXIMATELY 5 SECONDS THEN RETRACTED. THEN NOSE GEAR CY CLED DOWN AND UP BRIEFLY WITH MAIN GEAR DOORS OPENING THEN CLOSING. GEAR EXTENDED NORMALLY ON APPROACH. REPLACED PSEU. 2 H 7 2 4T RT A13NM 2008031900346 20080319 00346 NM 2008 3 19 CALA0800216 1 20080312 A 5320 141A541016 INTERCOSTAL BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24715 28786 INTERCOSTAL FRAME CRACKED AT SCREW HOLES BETWEEN STA 320-344 AT LBL 42. REMOVED AND REPLACED INTERCOSTAL IN REF TO SRM 51-40-02 AND BOEING DRAWING 141A5410. 2 L 7 2 4F RT A16WE 2008031900348 20080319 00348 NM 2008 3 19 CALA0800217 1 20080313 A 5320 141A541023 INTERCOSTAL BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24715 28786 INTERCOSTAL FRAME CRACKED BESIDE SCREW HOLE BETWEEN STA 344-360 AT BL 0. REMOVED DAMAGED INTERCOSTAL, DRILLED UP AND IN STALLED NEW INTERCOSTAL, REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008031900350 20080319 00350 NM 2008 3 19 CALA0800219 1 20080313 A 3350 11583211 HOUSING BOEING 757 757224 1384958 NM EVAC LIGHT SHORTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26123 28966 EMERGENCY LAMPS AT OVERWING THAT SHINE DOWN ON HANDLES OF OVERWING EMERGENCY DOORS, LOCATED AT FWD POST - LEFT OVERWING BOTH DOORS AND AFT RIGHT OVERWING FWD LAMP ARE OUT, REPLACED BULBS, NO HELP. FOUND LIGHT ASSY AFT LEFT OVERWING SHORTIN G OUT AND BLOWING FUSE AT M10568 W/D 33-51-13 PG 2. REPLACED LIGHT HOUSING ASSY P/N 11- 5832-11 IPC 33-51-51-50 ITEM 45 . REPLACED FUSE AT BATTERY CHARGER, OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 2008031900352 20080319 00352 EA 2008 3 19 TRAX200800397 1 20080310 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 AAR - EMERGENCY ESCAPE HATCH PLACARDS CREW INSTRUCTION, OPEN, ARROW AND CLOSE ARE DAMAGED OR MISSING. 2 L 7 2 4F RT A21EA 2008031900356 20080319 00356 EA 2008 3 19 TRAX200800401 1 20080310 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 972EV 7534 AAR - FS 280 CLIP CRACKED I/B OF LBL 9. 2 L 7 2 4F RT A21EA 2008031900362 20080319 00362 EA 2008 3 19 TRAX200800407 1 20080310 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 INTERCOSTAL CLIP CRACKED AT FS 484 LBL 36. REMOVED CRACKED LIGHTED FLOOR LEVEL EXIT SIGN P/N BR9279-106 IAW AMM 33-51- 10. INSTALLED SERVICEABLE LIGHTED FLOOR-LEVEL EXIT SIGN P/N BR9279-106 IAW AMM 33-51-10. OPS CHECK REQUIRED. PERFORME D OPS CHECK IAW AMM 33-51-00. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2008031900363 20080319 00363 EA 2008 3 19 TRAX200800408 1 20080310 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 972EV 7534 PAX DOOR AFT EDGE MEMBER CRACKED UNDER STEP 832ET. REMOVED DAMAGED AREA OF PAX DOOR AFT EDGE MEMBER PER: REO 601R-52-11 -279. C/W HFEC INSP OF PAX DOOR AFT MEMBER, IAW NDTM 51-20-06 AND REO 601R-52-11-279. NO DEFECTS NOTED. COMPLIED WITH R EPAIR OF PAX DOOR AFT EDGE MEMBER AS REQUIRED, IN ACCORDANCE WITH REO 601R-52-11-279. COMPLIED WITH EC/TC EO 600-52-43. 2 L 7 2 4F RT A21EA 2008031900364 20080319 00364 CE 2008 3 19 DXTA200802820 1 20080131 A 3150 WARNING SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ACTIVATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 905QS 7500105 DURING TAKEOFF RED NO TAKEOFF CAS MESSAGE AND DOUBLE CHIME ABORTED TAKE OFF. APPLIED POWER TO AC. RAN BOTH ENGINES. PER FORMED THE FLIGHT CONTROL INDICATIONS MAINT PRACTICES. NO TAKEOFF WARNING DESCRIPTION AND OPERATION. EXCERISED FLIGHT CO NTROLS SEVERAL TIMES IN AND OUT OF (NO TAKE OFF) MONITORING TO T/O PROBE SYS IS OPERATING NORMAL AT THIS TIME IAW CH 31- 52-00 OF MM. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008031900367 20080319 00367 2008 3 19 E0X2008F00001 4 20080207 A 2200 UNKNOWN BRAERO 1000 BAE1251000A 1500104 EU PWA 305 PW305 NE UNKNOWN E E0XA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 39 542LR 258 ON APPROACH, AT 3000 FT, EXPERIENCED A PARTIAL PANEL FAILURE ON THE CAPT EADI, EHSI, MFG. TRANSFERRED CONTROL OF AC TO THE F/O. SELECTED THE NR 2 AFSC AND 30 SECONDS THE AC DEPARTED LEVEL FLIGHT AND STARTED AN UNCOMMANDED DESCENT. AT 270 0 FT BOTH FLIGHT CRE COULD NOT STOP DESCENT AND THE AUTOPILOT WOULD NOT DISCONNECT ON THE CAPTAINS YOKE. THE A/P AND SF SC C/B WERE PULLED AND CONTROL OF AC WAS REGAINED. AT THIS POINT AN EMERGENCY WAS DECLARED AND AC WAS DIVERTED. THE LA NDING WAS UNEVENTFUL, WITH NO INJURIES TO THE 8 PASSENGERS OR CREW. AT THIS TIME THE AC IS BEING INSPECTED, IT IS NOT K NOW WHAT UNITS FAILED AT THIS TIME. (K) 2 L 7 2 4F 4 F RT A3EU E35NE 2008031900369 20080319 00369 CE 2008 3 19 DXTA200802822 1 20080203 A 3233 99125373 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LT MLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 623QS 5295 5605299 WHILE ON DOWNWIND GEAR WAS SELECTED DOWN, WE DID NOT HAVE A GREEN LIGHT FOR LT MAIN. WE HAD PROPER INDICATION FOR RT MAI N AND NOSE (GREEN) AND RED UNSAFE. GEAR WAS CYCLED AND 3 GREEN LIGHTS WERE OBSERVED, NO FURTHER ISSUES AROSE. REPLACED LT MAIN GEAR ACTUATOR WITH INSPECTED UNIT IAW MM CH 32-30-04 AND SEVERAL GEAR RETRACTIONS IAW MM CH 32-30-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008031900375 20080319 00375 EA 2008 3 19 TRAX200800410 1 20080310 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 972EV 7534 AAR - FS 280 CLIP CRACKED I/B OF RBL 36. 2 L 7 2 4F RT A21EA 2008031900379 20080319 00379 EA 2008 3 19 TRAX200800416 1 20080313 A 2612 FIRE WARNING CNDAIR CL600 CL6002C10 1390015 EA COCKPIT MALFUNCTIONED A ASOA K NONE N FALSE WARNING CR CRUISE 1 SO 27 718EV 10095 FIRE SYS FAULT STATUS MSG CAME ON IN FLIGHT THEN EXTINGUISHED. DISCREPANCY NO LONGER EXIST. 2 L 7 2 4F RT A21EA 2008031900383 20080319 00383 NM 2008 3 19 KCSA081178 1 20080315 A 5320 INTERCOSTAL BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 FUSELAGE FRAME INTERCOSTAL IS CRACKED BETWEEN STA 2220 & 2240, RBL 46 STR 43R. 2 L 7 4 4F RT A20WE 2008031900384 20080319 00384 NM 2008 3 19 KCSA081179 1 20080315 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE SKIN IS CORRODED AT STA 1239 BETWEEN STR 7L & 8L. 2 L 7 4 4F RT A20WE 2008031900395 20080319 00395 NM 2008 3 19 CALA0800226 1 20080316 A 3397 S479W2203 WIRE BOEING 757 75733N 1384931 NM L3 DOOR DISCONNECTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 77867 32592 EMERGENCY LIGHT TEST FOUND EXIT LIGHTING ON L3 DOOR INOP. FOUND WIRES DISCONNECTED. DEACTIVATED L3 DOOR SLIDE TO GAIN ACCESS TO WIRES PER MM 25-66-03. OPENED AND CLOSED L3 DOOR REF MM 52-21-01 TO GAIN ACCESS TO WIRES. RECONNECTED WIRES AND ACTIVATED L3 DOOR SLIDE. 2 L 7 2 4F RT A2NM 2008031300136 20080313 00136 WP 2008 3 13 08FDEA00726 1 20080305 A 5230 LINER DOUG MD10 MD1010F 3022112 WP CARGO DOOR DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 THE AFT CARGO DOOR LINER REPAIR PATCH IS DISBONDED. REPAIRED THE AFT CARGO DOOR LINER BY REMOVING THE DAMAGE; CLEANED & PREPARED FOR WET LAY-UP TO THE INTERIOR AND EXTERIOR SURFACES. APPLIED, CURED, AND SANDED WET LAY-UP ON THE INTERIOR A ND EXTERIOR SURFACES IAW SRM 51-43-01. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008031300144 20080313 00144 NM 2008 3 13 SWAA081185 1 20080302 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008031300161 20080313 00161 NM 2008 3 13 SWAA081136 1 20080302 A 5311 65C22910 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008031300166 20080313 00166 NM 2008 3 13 SWAA081154 1 20080229 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 375, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300202 20080313 00202 NM 2008 3 13 SWAA081183 1 20080303 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300206 20080313 00206 NM 2008 3 13 SWAA081179 1 20080303 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300250 20080313 00250 NM 2008 3 13 SWAA081194 1 20080303 A 5311 6546526 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300266 20080313 00266 NM 2008 3 13 SWAA081225 1 20080304 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031300334 20080313 00334 SW 2008 3 13 WGEA200800042 1 20080229 A 5270 PROXIMITY SENSOR ECLIPS EA500 ECLIPSEEA500 3350000 SW DOOR OUT OF ADJUST E WGEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 161DJ 000078 CLIMBING THROUGH FL 230, GOT DOOR WARNING CAS. VISUALLY INSPECTED THE DOOR LOCKS (5 GREEN). CAS CLEARED BELOW 10,000 F T, LANDING IN GNV. INSPECTED DOOR PROX SENSOR. FOUND SENSOR TO BE OUT OF ADJUSTMENT. ADJUSTED SENSOR AND PERFORMED SE NSOR TEST. NO UNSAFE DOOR CAS MESSAGES NOTED. TEST CHECKED GOOD IAW EA500 AMM 52-00-00. 1 L 7 2 4J RT A00002AC 2008031300335 20080313 00335 NM 2008 3 13 P5CA0801547 1 20080304 A 7160 INLET BOEING 747 74747UF 1384812 NM GE CF6 CF680C2* GL NR 3 NACELLE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 416MC 32838 706451 DURING THE OIL SERVICING OF THE NR 3 ENGINE DAMAGE OCCURRED TO THE RIGHT SIDE OF THE INLET COWLING AT THE 3 O'CLOCK POSI TION. ACCOMPLISHED INTERIM REPAIR PER EO NR 4471A012 PART 1 PER SRM 54-15-01. 2 L 7 4 4F 4 F RT A20WE E23EA 2008031300345 20080313 00345 SW 2008 3 13 WGEA200800043 1 20080227 A 2750 571043851007 FLAP ECLIPS EA500 ECLIPSEEA500 3350000 SW RIGHT OUT OF ADJUST E WGEA O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 27 142DJ 77 000056 FOUND RIGHT FLAP, OUTBOARD END TO BE .5 DEGREE HIGHER THAN THE INBOARD END AND THE WHOLE LEFT FLAP. THIS IS WITHIN LIMI TS, ADJUSTED TO MATCH THE INBOARD END AND THE LEFT FLAP IAW EA500 AMM 27-50-00. RIG CHECKED BOTH AILERONS AND FOUND THE M TO BE THE SAME AND WITHIN AMM LIMITATIONS. RIG CHECKED THE ELEVATOR AND ELEVATOR TRIM TABS AND FOUND THEM TO BE THE S AME AND TO BE WITHIN AMM LIMITS, PERFORMED ALL RIG CHECKS AND ADJUSTMENTS IAW EA500 AMM 27-00-00. REFERENCE LOGBOOK PAG E 0897, ITEM 3. EVALUATION FLIGHT UNSATISFACTORY. IN CRUISE, FLAPS UP, 220 KNOTS, AILERON TRIM REQUIRED 41 PERCENT LWD . WITH FLAPS LDG, 105 KTS, REQUIRED 37 PERCENT LWD. PITCH TRIM NORMAL. REFERENCE LOGBOOK PAGE 0898, ITEM 1, AND DAYJE 1 L 7 2 4J RT A00002AC 2008031300347 20080313 00347 EU 2008 3 13 08FDEA00754 1 20080306 A 5411 SPAR AIRBUS 310 A310203 3930313 EU NR 2 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 PYLON AFT LOWER SPAR ANGLE IS CRACKED AT STA 999/RIB 19. REMOVED A54515241500 STAMPING TO ACCESS THE CRACKED ANGLE PER SRM 51-40- 21 PARA 5. REMOVED CRACKED A54515063204 ANGLE PER SRM 51-40-21; PARA 5 & 6. ORDERED AND RECEIVED NEW A 54515063204 NAGLE. LOCATED, DRILLED AND DEBURRED FASTENER HOLES ON THE NEW ANGLE PER SRM 51-40-40. INSTALLED THE NEW ANG LE & REINSTALLED STAMPING PER SRM 51-40-21; PARA 5, 6 AND 7. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008031300350 20080313 00350 EU 2008 3 13 08FDEA00757 1 20080306 A 5414 A5461135700100 PANEL AIRBUS 310 A310203 3930313 EU NR 2 PYLON DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 PYLON PANEL NR 423 DL IS DENTED. DRESSED OUT DENT REF SRM 51-73-10 PAGE 214. ACCOMPLISHED HFEC INSPECTION IF THE D ENT AREA IAW NTM 51-10-20. NO DEFECTS NOTED. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008031300355 20080313 00355 NM 2008 3 13 SWAA081143 1 20080302 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008031300356 20080313 00356 NM 2008 3 13 SWAA081159 1 20080302 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031900396 20080319 00396 NM 2008 3 19 CALA0800227 1 20080314 A 2560 P4010021 BATTERY BOEING 767 767424ER 1385270 NM FLASHLIGHT DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 76065 29460 R4 ATTENDANT STATION FLASHLIGHT BATTERY DEAD. REPLACED BATTERY PER AMM 25-60-00. 2 L 7 2 4F RT A1NM 2008031900397 20080319 00397 EA 2008 3 19 TRAX200800417 1 20080304 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 917EV 7769 ASD AFT ANCHOR FITTING CRACKED. 2 L 7 2 4F RT A21EA 2008031900398 20080319 00398 EA 2008 3 19 TRAX200800418 1 20080311 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 27 823AS 7196 FLAPS FAIL AT ZERO DEGREES UPON DEPARTURE. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2008031900399 20080319 00399 NM 2008 3 19 USAA920080630 1 20080312 A 3350 32145410 EPSU AIRBUS A319 A319132 3930340 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 801AW 1553 1553 889 SAL - EEL - C7 CHECK - AFT GALLEY EPSU INOPERATIVE. REPLACED AFT GALLEY EPSU IAW A319 AMM 33-51-38. 2 L 7 2 4F RT A28NM 2008031900402 20080319 00402 NM 2008 3 19 CALA0800229 1 20080317 A 5340 6935352U14 STRINGER CLIP BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 STRINGER CLIP AT STRINGER 4L STA 380 CRACKED. REMOVED AND REPLACED STRINGER CLIP REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008032000015 20080320 00015 CE 2008 3 20 DXTA200802830 1 20080202 A 5270 SWITCH CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE PAX DOOR DAMAGED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 379QS 5600479 MAIN ENTRY DOOR UNLOCK LIGHT ILLUMINATED AFTER DEPARTURE AT ABOUT 200FT AGL. FOUND DOOR LOCK SWITCH PLUNGER NOT TO HAVE ENOUGH TRAVEL. ADJUSTED PLUNGER TRAVEL IAW MM 52-10-02. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2008032000017 20080320 00017 CE 2008 3 20 DXTA200802832 1 20080201 A 3222 STRUT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG DISCHARGED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 975QS 7500175 NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. THE NOSE GEAR LIGHT AND THE GEAR UNSAFE LIGHT REMAINED ON WITH THE GEAR HANDLE IN THE UP POSITION. JACKED AC AND SERVICED NLG STRUT IAW MM CH 12-10-38. PERFORMED SEVERAL GEAR EXTENSION AND RETRACTIO NS. NO DEFECTS NOTED. GEAR SWINGS DONE IAW MM 32-30-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032000018 20080320 00018 CE 2008 3 20 DXTA200802833 1 20080201 A 5610 99143795 WINDOW CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT BROKEN E DXTA O OTHER O OTHER CR CRUISE 1 GL 07 986QS 6519 7500086 PILOT FWD SIDE WINDOW SHATTERED IN FLIGHT. REMOVED PILOT FWD SIDE WINDOW P/N 9914379-5, S/N 99048H 9608 AND INSTALLED A NEW SERVICEABLE WINDOW P/N 9914379-7, S/N 07024H3614. PERFORMED CABIN PRESSURIZATION CHECK AND WINDSHIELD HEAT CHECK. OPS CHECKED GOOD WITH NO DEFECTS NOTED AT THIS TIME. WORK DONE IAW AMM 56-12-00, 21-30-00 AND 30-41-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032000029 20080320 00029 CE 2008 3 20 DXTA200802839 1 20080205 A 2120 UNKNOWN RAYTHN 900 HAWKER900XP 4220011 CE GARRTT TFE731 TFE7315R 01518 WP COCKPIT ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 848QS HA0031 BURNING ELECTRICAL AND RUBBER ODOR FROM BEHIND CO-PILOTS SEAT. ON ENTERING CABIN THE ONLY ODOR NOTED WAS THAT OF NEW INT ERIOR. ACCESSED THE DA PANEL AND OPENED SUB PANELS DA/A (CB PANEL BEHIND CO-PILOT) DA/B (RELAY PANEL BEHIND CO-PILOT), D A/J (A/C ELECTRICAL POWER PANEL INSIDE DA PANEL), DA/D (MAIN CIRCUIT BREAKER PANEL) MWS CARDS PANEL L AN DINSPECTED FOR SIGNS OF OVERHEATING/ BURNING, NONE NOTED. POWERED UP AC SYS USING THE APU AND BOTH ENGINES. ENGINE MAIN AIR VALVES OPEN AND APU BLEED ON, SELECTED FULL HOT ON TEMP SELECTOR. RADIO MASTER SWITCHES ON, ENGINE , ALTERNATOR SWITCHES ON, WINDSC REEN HEAT ON, ALL COCKPIT AND CABIN LIGHTING ON. ALLOWED TO OPERATE FOR 1 HOUR 30 MINUES WITH NO UNUSUAL ODORS DETECTED. 1 L 7 2 4F 4 F RT A3EU E6WE 2008032000032 20080320 00032 CE 2008 3 20 DXTA200802842 1 20080205 A 2612 37702838 CONTROL UNIT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE FIRE DETECTOR INOPERATIVE E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 613QS 2343 5605599 AT HIGH POWER SETTING, LT ENGINE FIRE WARNING LIGHT FLICKERED ON AND OFF (VERY DIM) NEVER CAME ON FULL BRIGHT. FOUND FI RE DETECTOR CONTROL UNIT BAD. INSTALLED NEW CONTROL UNIT IAW THE MM 26-11-02. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032000033 20080320 00033 CE 2008 3 20 DXTA200802843 1 20080206 A 2120 UNKNOWN RAYTHN 900 HAWKER900XP 4220011 CE GARRTT TFE731 TFE7315R 01518 WP COCKPIT ODOR E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 848QS HA0031 ELECTRICAL BURNING ODOR FROM BEHIND OR UNDER COPILOTS SEAT. POWERED UP AC SYS USING THE APU AND BOTH ENGS, SELECTED FULL HOT ON TEMP SELECTOR, RADIO MASTER ON, ENG ALTERNATOR'S ON WINDSCREEN HEAT ON AND COCKPIT AND CABIN LIGHTS ON OPERATED ALL SYS FOR 1 HR WITH NO UNUSUAL ODORS DETECTED. NO DISCREPANCY WAS NOTED IAW MM, CH 24-10-00 AND 71-00-00. 1 L 7 2 4F 4 F RT A3EU E6WE 2008031900015 20080319 00015 CE 2008 3 19 GUUA02020801 1 20080202 A 5220 DOOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE EMERGENCY EXIT UNSECURE A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 29 81533 UE137 FLIGHT: 9179, PILOT REPORTED: DISCOVERED LT EMERGENCY EXIT DOOR APPEARS UNSECURE. RIGGED LT EMERGENCY EXIT DOOR. 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900023 20080319 00023 SO 2008 3 19 GUUA02190801 1 20080219 A 3350 AGC1 FUSE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHTS INOPERATIVE A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 283AS 120236 FLIGHT: 9208, PILOT REPORTED OUTSIDE EMERGENCY LIGHTS BY RT PACK INOPERATIVE. REPLACED EMERGENCY LIGHT FUSE. 2 L 7 2 4T 4 T RT A31SO E20NE 2008031900033 20080319 00033 CE 2008 3 19 GUUA03080801 1 20080308 A 3260 H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA LT MLG SHORTED A GUUA O OTHER N FALSE WARNING CL CLIMB 1 SO 29 81556 UE239 FLIGHT: 5407, AFTER TAKEOFF, LANDING GEAR UNSAFE LIGHT ILLUMINATED IN THE GEAR UP POSITION. REPLACED LT MLG UPLOCK SWIT CH. 2 L 7 2 4T 3 T RT A24CE E2NE 2008031900042 20080319 00042 CE 2008 3 19 GUUA03130801 1 20080313 A 3260 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT MLG OUT OF ADJUST A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 29 190YV UE190 FLIGHT: 9310, DURING FLIGHT LANDING GEAR RED UNSAFE TRANSIT LIGHT FLICKERING CONSTANTLY. ADJUSTED LT MLG UPLOCK SWITCH. 2 L 7 2 4T 4 T RT A24CE E26NE 2008031300359 20080313 00359 EA 2008 3 13 MASA200800189 1 20080303 A 2740 3094334 TRIM SWITCH CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A MASA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SW 07 17231 7231 FLT 2889, BFL-PHX. STAB TRIM RUNAWAY 1000 FT OFF GROUND. NOSE OF AC PITCHED DOWN. DECLARED AN EMERGENCY AND RTF. MX REPLACED THE F/O'S STAB TRIM SWITCH. 2 L 7 2 4F RT A21EA 2008031300361 20080313 00361 NM 2008 3 13 SWAA081243 1 20080305 A 5610 6531914102 MECHANISM BOEING 737 7373H4 1384600 NM R2 WINDOW OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND FLIGHT DECK R2 WINDOW EXTERNAL RELEASE HANDLE WILL NOT UNLOCK WINDOW. ADJUSTED RELEAS E HANDLE MECHANISM PER MM. 2 L 7 2 4F RT A16WE 2008031300363 20080313 00363 NM 2008 3 13 SWAA081261 1 20080306 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 271, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008031300371 20080313 00371 NM 2008 3 13 SWAA081248 1 20080305 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008031300380 20080313 00380 2008 3 13 SWAA081253 4 20080305 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031300383 20080313 00383 SO 2008 3 13 RAIA00803002 1 20080303 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 841HK 145382 PRE FLT 7959 - ROC - OVERHEAD EMERGENCY LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR TO THE AFFECTE D LIGHT ASSEMBLY. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008031300388 20080313 00388 NM 2008 3 13 ASAA0852702 1 20080309 A 2150 3989083 CONTROL VALVE BOEING 737 737890 1384527 NM LT A/C PACK FAILED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 559AS 35178 LEFT PACK LIGHT ILLUMINATES ON RECALL. PACK CONTROL BIT SHOWS LEFT PACK TCV FAILED. REPLACED TCV. BITE CHECK & LEAK C HECK OK. 2 L 7 2 4F RT A16WE 2008031300390 20080313 00390 NM 2008 3 13 ASAA0852699 1 20080308 A 4990 38809381 FILTER BOEING 737 737890 1384527 NM APU CLOGGED A ASAA O OTHER J WARNING INDICATION IN INSP/MAINT 1 NM 02 577AS 35186 APU LUBE FILTER INDICATOR POPPED. REPLACED APU LUBE FILTER ELEMENT. LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 2008031300395 20080313 00395 NM 2008 3 13 SWAA081267 1 20080307 A 2133 2079801 OUTFLOW VALVE BOEING 737 7377H4 1384404 NM CABIN PRESSURE STUCK A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 239WN 34714 DIVERSION - ON CLIMBOUT PASSING FL 300, CABIN ALTITUDE WARNING HORN CAME ON. FOUND FWD OUTFLOW VALVE STUCK. REMOVED AN D REPLACED OUTFLOW VALVE PER MM. 2 L 7 2 4F RT A16WE 2008031300396 20080313 00396 NM 2008 3 13 SWAA081268 1 20080309 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 246LV 32507 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 3 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008031300397 20080313 00397 NM 2008 3 13 SWAA081269 1 20080307 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 247WN 32508 EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008031300399 20080313 00399 EU 2008 3 13 08FDEA00760 1 20080306 A 5210 RUB STRIP AIRBUS 310 A310203 3930313 EU R1 DOOR CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 R-1 DOOR UPPER AFT CORNER IS CHAFED. REMOVED CHAFED RUB STRIP REF SRM 51-40-21 PARA 6. ALODINED AND PRIMED AREA REF SRM 51-21-10. INSTALLED NEW RUB STRIP REF SRM 51-40-21 PARA 6. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008031300403 20080313 00403 WP 2008 3 13 08FDEA00764 1 20080306 A 5512 ALC7426502 PANEL DOUG MD10 MD1010F 3022112 WP HORIZONTAL STAB CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 RT HORIZONTAL STABILIZER REAR SPAR HINGE PANEL BELOW THE INBD DAMPER IS CHAFED ON THE INTERIOR SKIN, OUTBD ELEVATOR. RE MOVED PANEL TO FOM. IAW SRM 51-31-01 VOL II. REMOVED DAMAGE AND PREPARED SURFACES FOR BONDNG IAW SRM 51-71-00 VOL II. FABRICATED REPAIR FILLER, DOUBLER, BONDED & CURED IAW SRM 51-71-00 VOL II. APPLIED SEALANT IAW SRM 51-71-00 VOL II. PAINTED AREA IAW SRM 51-21-01 VOL II. RE-INSTALLED PANEL IAW SRM 51-31-01 VOL II PG 1. 2 L 7 3 4F RT A22WE 2008031300407 20080313 00407 WP 2008 3 13 08FDEA00772 1 20080307 A 5347 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 685-768 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 FOUND CABIN FLOOR DECK SEAT TRACK HAS SEVERAL WEAR MARKS FROM STA 685 - STA 768 RBL 9 IN WORK. 2 L 7 3 4F RT A22WE 2008031300408 20080313 00408 WP 2008 3 13 08FDEA00774 1 20080307 A 5420 AUB70273 BRACKET DOUG DC10 DC1010F 3022111 WP NR 3 NACELLE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 FOUND ON PYLON NR 3 ON STA YN=240 THE BRACKET WITH DAMAGED AND DO NOT INSTALLED FOR DWG REPLACE WEB FOR SRM 51-33-01 VOL II AND DWG AUB7027. 2 L 7 3 4F A22WE 2008031300411 20080313 00411 WP 2008 3 13 08FDEA00777 1 20080307 A 5730 ARC0267502 PANEL DOUG MD10 MD1010F 3022112 WP RT WING DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 RT MLG AREA PANEL ABOVE THE MLG ACTUATOR IS DENTED. REMOVED DAMAGED AREA, PREPPED AREA FOR BONDING, FABRICARED REPAIR C ORE PLUG & DOUBLERS. LAYED UP & BONDED IAW SRM 51-31-01 VOL III FIG 1 & 51-71-00 VOL II PG 1. SEALED, PRIMED & PAINTED I AW SRM 51-31-01 VOL II. PANEL 152 ET INSTALLED ON W/C 53P10.048B. 2 L 7 3 4F RT A22WE 2008031900045 20080319 00045 CE 2008 3 19 DXTA200802799 1 20080125 A 3150 WARNING LIGHT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 642QS 5605561 (EMERGENCY DECLARED) PASSING THRU 10,000 FT, RT WING OVERHEAT LIGHT ILLUMINATED WITH ANTI-ICE SWITCH IN (OFF) POSITION. REDUCED POWER ON RT ENGINE TO IDLE AND LIGHT DIDN’T EXTINGUISH. APPROX 5 MIN LATER WHILE ENROUTE TO LANDING, LIGHT DID EXTINGUISH. LANDED UNEVENTFULLY; AC DID NOT EXCEED MAX LANDING WEIGHT. CHECKED VOLTAGE AND OPERATION OF RT ANTI-ICE V ALVE IN ALL POSITIONS. OPS CHECKS GOOD. CHECKED RT ENG PCB, NO DEFECTS NOTED. COMPLIED WITH OPERATIONAL CHECK OF ANTI-IC E SYS. OPS CHECKS GOOD IAW MM CHP 30-11-00 2 L 7 2 4F 4 F RT A22CE E00059EN 2008031900046 20080319 00046 NM 2008 3 19 DXTA200802800 1 20080126 A 2780 CONTROL UNIT GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE SLATS MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 712QS 073 SLATS FAILED TO RETRACT, CAS MSG: SLAT UNBALANCED, SLAT FLAP MAINTAIN. FLAPS/SLATS FUNCTIONAL TEST GOOD. PERFORMED FSECU BITE CHECK. NO FAULTS FOUND. 2 L 7 2 4F 4 F RT A53NM E35NE 2008031900055 20080319 00055 CE 2008 3 19 DXTA200802809 1 20080130 A 3620 1103P0912 PRESSURE SWITCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL HP DUCT INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 950QS 1118 7500050 ON THE TAKEOFF ROLL THE HP DUCT (O) PRESSURE RT ILLUMINATED. REPLACED FAILED RT HP DUCT OVER-PRESSURE SWITCH WITH NEW IA W CHAPTER 30-10-00 OF THE MM. OPERATONAL CHECK OK. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008031900063 20080319 00063 EA 2008 3 19 TRAX200800369 1 20080304 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR STICKS A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 719EV 10099 AIRSTAIR DOOR HANDLE (INSIDE) STICKS IN LOCKED POSITION (DOOR CLOSED). CANNOT OPEN DOOR FROM OUTSIDE. 2 L 7 2 4F RT A21EA 2008031900064 20080319 00064 EA 2008 3 19 TRAX200800370 1 20080304 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 972EV 7534 LT OBLIQUE ANGLE BRACKET IN WEB IS CRACKED. REMOVED LT OBLIQUE ANGLE, DISCARDED. DUPLICATED NEW ANGLE, LOCATED HOLES, DEBURRED, ALODINED, PRIMED/TOPCOAT AND INSTALLED NEW ANGLE WET WITH LOCK FASTENER PINS, TOPCOAT APPLIED, ALL REWORK ACC OMPLISHED IAW SRM 53-61-17, 51-12-11, 51-42-21, 51-25-06, 51-25-16, 51-23-00. NEW ANGLE P/N S6144A33. 2 L 7 2 4F RT A21EA 2008031900101 20080319 00101 EA 2008 3 19 N6WA0080201 1 20080201 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE EMERGENCY LIGHTS BURNED OUT A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 153GJ 10219 CEILING LEVEL EMERGENCY LIGHT OUT AT ROW 7. REPLACED BULB. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008031900114 20080319 00114 SO 2008 3 19 DJFA2008017 1 20080207 A 2120 UNKNOWN EMB 135 EMB135BJ 3260306 SO ALLSN AE300 AE3007A GL CABIN ODOR E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 910LX 14500952 DURING CRUISE CREW REPORTED A BURNING ODOR FROM GALLEY AREA WHEN OPERATING THE MICROWAVE. MAINT OPERATED THE SYS BUT WA S UNABLE TO DUPLICATE THE DISCREPANCY. 2 L 7 2 4F 4 F RT TE6CH 2008031900115 20080319 00115 2008 3 19 DJFA2008016 4 20080207 A 3420 HSI RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP MALFUNCTIONED E DJFA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 EA 23 815TA 258534 DURING CLIMBOUT CREW REPORTED DUAL HSI FAILURE WITH BOTH SIDES OFF BY 30 DEGREES. CREW RETURNED TO THE FIELD. AFTER LA NDING CREW REPORTED A BURNING ODOR. MAINT OPERATED THE AVIONICS SYSTEMS BUT WAS UNABLE TO DUPLICATE THE DISCREPANCIES. 2 L 7 2 4F 4 F RT A3EU E6WE 2008031900120 20080319 00120 EA 2008 3 19 S9BA20080008 1 20080211 A 7120 C6WM151728 MOUNT DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA ZONE 400 CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 20206 1310 573 CPCP INSP, LT NACELLE OB MOTOR MOUNT CORRODED. REMOVED AND REPLACED ENG MOUNT IAW RD 6-54-006. EMERGENCY MEASURES EXEC UTED? NO AIRCRAFT GROUNDED? YES 1 H 7 2 3T 4 T RT A9EA E4EA 2008031900211 20080319 00211 EU 2008 3 19 USAA920080568 1 20080226 A 5320 D5311283020200 DUMMY RAIL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651AW 866 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN DUMMY RAIL, BS 605 /FR 12 - BS 709 /FR 16, -Y81. REPLACED CABIN DUMM Y RAIL, BS 605 /FR 12 - BS 709 /FR 16, -Y81 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900252 20080319 00252 CE 2008 3 19 DXTA200802810 1 20080130 A 3240 AE3663218E0117 HOSE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D1 52060 NE BRAKE SYSTEM LEAKING E DXTA O OTHER K FLUID LOSS LD LANDING 1 GL 07 375QS 11051 5600375 DURING TOUCHDOWN AT PDK, COPILOT'S LT BRAKE PEDAL WENT COMPLETELY TO THE FLOOR. REMOVED AND REPLACED BOTH CO-PILOTS UPP ER MASTER CYLINDER HOSES. IAW MM CHAP 32-42-02. ALSO COMPLETED APPROVED BLEEDING PROCEDURES CHAP 32-42-00. 2 L 7 2 4F 4 F RT A22CE E1NE 2008031900263 20080319 00263 GL 2008 3 19 3002012821608 1 20080216 A 3230 302270402 PSEU BOMBDR BD100 BD1001A10 1390044 GL HNYWL AS907 AS90711A 33908 WP MLG FAILED E J7SA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 529FX 1190 20128 PILOT REPORTS THAT THE GEARS WOULD NOT RETRACT AFTER SEVERAL ATTEMPTS WITH A CYAN PSEU FAULT FOLLOWED BY AN AMBER GEAR D ISAGREE CAS MESSAGE. TECHS PUT AC ON JACKS AND ATTEMPTED TO SWING GEAR. UPON GEAR UP SELECTION, THE PROX SYS FAULT CYA N CAS POSTED AND THE GEAR DID NOT COME UP. MDC CURRENT FAULTS SHOWED THE PSEU SYSTEM FAILURE. ADVANCED DIAGNOSTICS SAID PSEU INTERNAL FAILURE. INSTALLED NEW PSEU AND OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT T00005NY E00010LA 2008031900288 20080319 00288 CE 2008 3 19 GLBA20061073 1 20080219 A 5313 STRINGER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 243 S9L DEBONDED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 184UX UE184 STRINGER 9L DISBONDED AT FS 243.25 TO FS 258.25. MAINT REPAIRED DISBONDED STRINGER 9L AT FS 243.25 TO FS 258.25 IAW SRM 53-90. REPAIR APPROX 10.5 INCH. 2024 T3. RII INSP C/W IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900334 20080319 00334 NM 2008 3 19 USAA920080623 1 20080308 A 5330 6545776 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT - MAJOR REPAIR - RON - CRACKED FUSELAGE SKIN, BS 727F, S25R. REPAIRED FUSELAGE SKIN, BS 727F, S25R IAW USAIRWAYS 10 036 LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 794 - BS 947, RBL 13.80. 2 L 7 2 4F RT A16WE 2008031300414 20080313 00414 EU 2008 3 13 08FDEA00786 1 20080307 A 7830 SEALANT AIRBUS 310 A310203 3930313 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 ENGINE OUTBD THRUST REVERSER TRANSLATOR SLEEVE LOWER CORNER IS CRACKED. EVALUATED DAMAGE AND FOUND CRACKED SEALAN T ONLY, REMOVED DAMAGED SEALANT AND RESEALED IAW SRM 51-24-00 AND 51-76-10. PERFORMED PAINT TOUCH-UP OF REPAIR AREA IAW SRM 51-75-10 2 L 7 2 4F RT A35EU 2008031300416 20080313 00416 EU 2008 3 13 08FDEA00790 1 20080307 A 5347 A5381192220300 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 MAIN CABIN SEAT TRACK AT Y 450 IS GOUGED FROM FRAMES 50 TO 51. REMOVED GOUGE IAW SRM 51-73-10. ORIGINAL DIAMETER OF THE SCALLOPS IS .790 IAW DWG A5381922. MATERAL REMOVED IS .020. DIAMETER DIAMETER REMAINING FOR SCALLOP IS .810. FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16. ALODINED, PRIMED, AND PAINTED AREA IAW AND AMM 51-23-10-0. 2 L 7 2 4F RT A35EU 2008031300419 20080313 00419 NM 2008 3 13 QXEA200800249 1 20080227 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - THE INBOARD FLANGE ON SEAT TRACK NR 12 FROM X102.5 TO X 114.5 HAS BEEN PITTING AND GOUGED FROM THE FLOORBOARD . REMOVED SEAT TRACK AND INSTALLED NEW TRACK IAW DASH 8 Q400 SRM 51-42-05, 51-40-15 AND 51-42-45 2 H 7 2 4T RT A13NM 2008031300422 20080313 00422 NE 2008 3 13 SWAA081314 2 20080306 A 7320 442369 HMU BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE NR 2 ENGINE FAULTY A SWAA O OTHER E Y VIBRATION/BUFFET ENGINE STOPPAGE NR NOT REPORTED 1 SW 29 268WN 32524 894489 NR 2 ENGINE SHUTDOWN IN FLIGHT ACCOMPANIED BY A VIBRATION. TROUBLESHOT ENGINE, REMOVED AND REPLACED HMU AND ENGINE DRIV E FUEL PUMP PER MM. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008031300426 20080313 00426 NM 2008 3 13 SWAA081272 1 20080309 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031400006 20080314 00006 WP 2008 3 14 NWAA080849984 1 20080305 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 984US 47383 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE AFT SECTION HAD FAILED. MAINTENANCE REP LACED THE EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2008031400011 20080314 00011 NM 2008 3 14 USAA920080562 1 20080301 A 5752 654645521C TAB BOEING 737 737401 1384701 NM ZONE 500 DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 CLT - MAJOR REPAIR - C1 CHECK - LEFT WING AILERON TAB HAS AREA OF DISBOND. REPLACED LEFT WING AILERON TAB IAW TASK CARD O3L30627002. 2 L 7 2 4F RT A16WE 2008031400013 20080314 00013 NM 2008 3 14 QXEA200800261 1 20080227 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - MCD THRESHOLD FLOOR SUPPORT STRUCTURE FRAME CASTELLATION IS CORRODED (STATION X6.0, Z95.0, Y38). REMOVED FRA ME AND INSTALLED NEW FRAME IAW DASH 8 Q400 SRM 51-40-07, 51-42-05 AND 51-25-15. 2 H 7 2 4T RT A13NM 2008031400015 20080314 00015 EU 2008 3 14 2008UALA01110 1 20080228 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 429UA 539 LT FUSE HAD PREVIOUSLY ARCHIVED DENTS IN ADJACENT FRAME BAYS BETWEEN FR 18 - 20 AND STR 32L AND 33L. DENTS ARE BEYOND L IMITS. ACCOMPLISHED MAJOR REPAIR IN DEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031400017 20080314 00017 2008 3 14 2008UALA01112 4 20080228 A 2565 LANYARD AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LT OWING SLIDE DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 817UA 873 LT OFFWING EVAC SLIDE INFLATION CYLINDER WIRE CONTROL ASSY WAS NOT ENGAGED WITH FLEX CONTROL ASSY PER AMM 25-62-46-400-0 01 AND AIRBUS DIAGRAM D4-0140 PAGE 2. BOTTLE IS LOCATED IN AFT PIT. RE-CONNECTED WIRE CONTROL ASSY CORRECTLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031400023 20080314 00023 NM 2008 3 14 2008UALA01135 1 20080229 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1540 S36 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 AFT PIT FRAME DENTED ON INBOARD FLANGE AT BS 1540 AND STR 26. MAJOR REPAIR ACCOMPLISHED AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031400030 20080314 00030 NM 2008 3 14 2008UALA01188 1 20080303 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1520 S23-25R GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 AFT PIT FRAME GOUGED 4 EA PLACES AT BS 1520 BETWEEN STR 23R AND 25R. MAJOR REPAIR ACCOMPLISHED AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031400031 20080314 00031 NM 2008 3 14 2008UALA01189 1 20080303 A 5340 ATTACH ANGLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1380-1440 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 AFT CARGO DOOR LOWER SILL ATTACH ANGLE HAS CORROSION ON UPPER SURFACE FROM BS 1380 TO 1440. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031400032 20080314 00032 NM 2008 3 14 2008UALA01190 1 20080303 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 L2 DOOR UPPER HINGE ARM CUT OUT REQUIRES DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031400040 20080314 00040 NM 2008 3 14 2008UALA01217 1 20080305 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE STA 300 S19R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 STATION 300 STRINGER 19R SKIN LAP MIDDLE ROW OF FASTENERS LIGHTNING STRIKE, HOLE BURNED THRU EXTERNAL SKIN TO FRAME. MA JOR REPAIR ACCOMPLISHED: INSTALLED SOLID RIVET AND INTERNAL SHEAR TIE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031400042 20080314 00042 NM 2008 3 14 2008UALA01219 1 20080305 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S13-14L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FRAME SHEAR TIE CRACKED AT BS 360 BETWEEN STR 13L AND 14L. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031400044 20080314 00044 NM 2008 3 14 2008UALA01221 1 20080305 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 986.5 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 BS 986.5 FLOORBEAM CORRODED FROM RBL5 TO BL0. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED FLANGE ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031400045 20080314 00045 NM 2008 3 14 CALA0800198 1 20080306 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM BS 400 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 FRAME CRACKED STA 400 BETWEEN S8L AND S9L. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A. 2 L 7 2 4F RT A16WE 2008031400049 20080314 00049 NM 2008 3 14 CALA0800202 1 20080306 A 5313 6546549 FRAME BOEING 737 737524 1384721 NM BS 767 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 FRAME CRACKED STA 767 ABOVE S9R. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A. 2 L 7 2 4F RT A16WE 2008031400050 20080314 00050 NM 2008 3 14 CALA0800203 1 20080306 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM BS 400 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 FRAME CRACKED STA 400 BETWEEN S8R AND S9R. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A. 2 L 7 2 4F RT A16WE 2008031400058 20080314 00058 NM 2008 3 14 QXEA200800247 1 20080227 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 449-469 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - SEAT TRACK NR 13 AT STATION 449 TO 469 GOUGED. REPAIRED IAW Q400 RD8/4-53-884 AND NDTM PART 6-51-00-01. 2 H 7 2 4T RT A13NM 2008031400061 20080314 00061 NM 2008 3 14 QXEA200800254 1 20080227 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM BS 234 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - RIGHT SIDE FRAME CASTELLATION (SKIN LEG), AT STATION X234.4 AND BETWEEN STRINGER 24S AND 25S HAS CORROSION AR OUND RIVET. REPAIRED IAW DASH 8 Q400 SRM 51-42-05, 51-21-00, 51-21-10, 51-25-15, AND Q400 NDTM PART 1 51-00-04 AND PART 6 51-00-01. 2 H 7 2 4T RT A13NM 2008031400062 20080314 00062 NM 2008 3 14 QXEA200800257 1 20080227 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - THERE IS EVIDENCE OF LIGHTING STRIKE, APPROXIMATELY FIVE BURNED RIVETS IN THE DOUBLER LOCATED APPROXIMATELY 4 .5 INCHES AFT OF RED ANTI-COLLISION LAMP ASSY BETWEEN STR 2P AND 2S AT Z182.00 AND FWD OF JOINT X234.475. POLISHED LIGH T BURN PITS WITH SCOTCH BRITE PAD, FINISHED REPAIR IAW Q400 NDTM PART 1 51-00-04 AND PART 6 51-00-01 AND DASH 8 Q400 SRM 51-21-10 AND 51-25-05. 2 H 7 2 4T RT A13NM 2008031400063 20080314 00063 NM 2008 3 14 QXEA200800259 1 20080227 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM BS 449 S24R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - RIGHT FRAME CASTELLATION AT STATION 449.5 AND STRINGER 24S HAS CORROSION AROUND RIVET. REMOVED RIVET AT LOCA TION AND CORROSION. INSTALLED RIVET IAW DASH 8 Q400 SRM 51-21-00, 51-42-05 AND 51-25-25. 2 H 7 2 4T RT A13NM 2008031400064 20080314 00064 NM 2008 3 14 QXEA200800260 1 20080227 A 5320 FLOOR SUPPORT BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - SUPPORT FOR FLOORBOARD 141FZ OUTBOARD SIDE (PART OF AFT STAIR STRACK ASSY) HAS CORROSION IN SEVERAL PLACES AR OUND ATTACHING SCREW HOLES. BLENDED CORROSION ON SUPPORT IAW DASH 8 Q400 SRM 51-21-00, FINISHED REPAIR IAW Q400 SRM 51- 21-10, NDTM PART 6 51-00-01 AND SRM 51-42-35, 51-25-10. 2 H 7 2 4T RT A13NM 2008031400069 20080314 00069 WP 2008 3 14 AALA200800457 1 20080229 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 487AA 49680 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 7 TO 16 INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEA D SEAT ROWS 7 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031400070 20080314 00070 NM 2008 3 14 AALA200800449 1 20080228 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 775AN 29584 DFW - EMERGENCY LIGHT AT SEAT 35G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 35G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031400072 20080314 00072 NM 2008 3 14 AALA200800451 1 20080229 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 789AN 30252 DFW - EMERGENCY LIGHT AT SEAT 38G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 38G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031400076 20080314 00076 NM 2008 3 14 AALA200800446 1 20080228 A 3350 HOUSING BOEING 777 777223 1385213 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 775AN 29584 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET AREA DAMAGED. REPLACED HOUSING FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031300124 20080313 00124 EU 2008 3 13 08FDEA00713 1 20080305 A 5510 FAIRING AIRBUS 310 A310203 3930313 EU HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT HORIZONTAL STABILIZER FWD APRON FAIRING BLADES ARE CRACKED. REMOVED THE DAMAGED SECTION IAW SRM 15-15-11 PGS 219 & 2 20. FABRICATED DOUBLER PLATE IAW SRM 15-15-11 PG 225. INSTALLED DOUBLER IAW SRM 15-15-11 PARA 5-B (4). 2 L 7 2 4F RT A35EU 2008031300140 20080313 00140 WP 2008 3 13 08FDEA00730 1 20080305 A 5730 ARC2008507N SKIN DOUG DC10 DC1010F 3022111 WP WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 GOUGED INTERNAL SKIN ON PANEL 535GL, ON THE PARTS RACK. REPAIRED INTERNAL SKIN PANEL 535 GL BY REMOVING THE DAMAGE & BL ENDING & REMOVING BURRS. FABRICATED REPAIR DOUBLER & BONDED DOUBLER TO THE PANEL. VACUUMED COMPLETING CURE OF BOND & R EMOVING EXCESS ADHESIVE FLASH. APPLYING SEALANT TO THE DOUBLER EDGES AND CURING. REAPPLIED FR PRIMER FINISH TO REPAIR AR EA AND CURING IAW SRM 51-21-01. MINOR REPAIR. 2 L 7 3 4F A22WE 2008031300147 20080313 00147 WP 2008 3 13 08FDEA00738 1 20080305 A 2910 S4928944T108 REDUCER DOUG MD10 MD1010F 3022112 WP HYD SYSTEM LEAKING A FDEA O OTHER K FLUID LOSS LD LANDING 1 SO 25 374FE 46612 HYD 3 ELEV OFF AND HYD 3 QTY LOW ALERT ANNUNCIATED. HYDRAULIC QUANTITY STABILIZED AT 3.9 GALLON. TIGHTENED "B" NUT UNI ON (REDUCER) ON RT MAIN LANDING GEAR SWIVEL GLAND, SERVICED HYDRAULICS'S AND LEAK CHECKED CHECKED GOOD IAW MD10-10 AMM 20-50-01-2 AND MD10-10 AMM 29-00-00-2, MD10-10 AMM 12-00-00. 2 L 7 3 4F RT A22WE 2008031300151 20080313 00151 NM 2008 3 13 08FDEA00742 1 20080306 A 5320 146N541614 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD STRINGER L10.45, STA 1280-1300, TO EVALUATE EXISTING REPAIR. EXISTING REP AIR FOUND NOT IAW B757-200 SRM 51-70-11, FIG 1 DETAIL I, II. AFT CARGO FLOORBOARD STRINGER L10.45 REPLACED IAW B757-200 SRM 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-02-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008031300179 20080313 00179 NM 2008 3 13 SWAA081173 1 20080302 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 469WN 33859 EEPLS LENS LOOSE AT ROW 23 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008031300209 20080313 00209 NM 2008 3 13 SWAA081217 1 20080303 A 5315 65C33944 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 360, RBL 1. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2008031300210 20080313 00210 NM 2008 3 13 SWAA081216 1 20080303 A 5310 6546956 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 400 AND BS 440, RBL 70. REMOVED AND REPLACED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300214 20080313 00214 NM 2008 3 13 SWAA081149 1 20080302 A 5330 6545767 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 410 AND BS 430, BL 0. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008031300215 20080313 00215 2008 3 13 SWAA081184 4 20080301 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 731SA 27863 DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031300222 20080313 00222 NM 2008 3 13 SWAA081162 1 20080229 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 208WN 29856 EEPLS LENS MISSING AT ROW 3 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008031300259 20080313 00259 NM 2008 3 13 SWAA081218 1 20080303 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008031300265 20080313 00265 NM 2008 3 13 SWAA081224 1 20080304 A 5311 65C34356 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300277 20080313 00277 2008 3 13 SWAA081237 4 20080304 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031300304 20080313 00304 2008 3 13 DL76G080315 4 20080303 A 2565 101651303 SLIDE BOEING 767 767332 1382001 NM L1 DOOR UNSECURE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1604R 30180 L1 DOOR SLIDE HAS BACK BOARD CABLE NOT ATTACHED. FOUND SLIDE PACK NOT SECURED ALONG ONE SIDE AND LOOSE ON THE OTHER SID E. FOUND DUCT TAPE COVERING RETAINING CABLE HOLE AT TOP OF SLIDE. SLIDE REPLACED ON NR 00175 AND DL JIC 7809 SLIDE PAR T NBR 251004926 (DL) 101651-303 (MFG). 2 L 7 2 4F RT A1NM 2008031300331 20080313 00331 2008 3 13 HALA0800365 4 20080305 A 3442 20414440402 ANTENNA BOEING 767 7673G5 1385126 NM WX RADAR SYS FAILED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, WX FAIL ON BOTH L/R ON HSI SCREEN. WIND SHEAR AHEAD FAIL ON F/O INST PANEL ILLUM. DURING TES T OF RADAR HSI SCREEN DISPLAYS WX FAIL W/BLUE "RT" BELOW WX FAIL. REPLACED WXR ANTENNA. GND OPS CHK OK AMM 34-43-00. 2 L 7 2 4F RT A1NM 2008031300349 20080313 00349 EU 2008 3 13 08FDEA00756 1 20080306 A 7160 2241101503 NOSE COWL AIRBUS 310 A310203 3930313 EU NR 1 ENGINE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 1 ENGINE NOSE SECTION HAS CORROSION ON THE INNER SKIN OF THE INTAKE AT THE 4:00 O'CLOCK POSITION; ACCESS 434BR. REMO VED AND REPLACED NR 1 ENGINE NOSE COWL IAW MM 71-11-00-4. 2 L 7 2 4F RT A35EU 2008031300354 20080313 00354 NM 2008 3 13 SWAA081142 1 20080302 A 5311 6545808 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 295, STR 8L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008031300362 20080313 00362 NM 2008 3 13 SWAA081262 1 20080306 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER 26R CORRODED AT BS 510A. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008031300368 20080313 00368 NM 2008 3 13 SWAA081258 1 20080305 A 5311 6546558 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300387 20080313 00387 SO 2008 3 13 RAIA00803006 1 20080305 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 846HK 14500855 PRE FLT 7923 - PHL - AISLE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE AFFECTED LIGHT . 2 L 7 2 4T RT T00011AT 2008031300394 20080313 00394 NM 2008 3 13 SWAA081266 1 20080307 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 235WN 34630 DURING SCHEDULED HC1 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008031300401 20080313 00401 WP 2008 3 13 08FDEA00762 1 20080306 A 5414 AJC70722 ACCESS PANEL DOUG MD10 MD1010F 3022112 WP NR 2 NACELLE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 NR 2 ENGINE PYLON ACCESS PANEL NR 362 DR HAS A DENT. REPAIRED PANEL BY FABRICATING SKINS, CORE, LAYED UP & BONDED IAW T PS 1001 REV E & EA 8-5530-116967 "RT VERTICAL STABILIZER PICKLE BARREL PANEL". PANEL REMOVED & REINSTALLED TO FACILITA TE MAINTENANCE IAW SRM 51-31-01 VOL II PG 1. 2 L 7 3 4F RT A22WE 2008031300415 20080313 00415 EU 2008 3 13 08FDEA00789 1 20080307 A 5347 A5327400500053 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 MAIN CABIN SEAT TRACK AT Y 953 SCALLOPS ARE GOUGED AND CRACKED AT FRAMES 42 TO 43. FOUND TO BE OUT OF LIMITS IAW SRM 53 -10-16. REMOVED ORIGINAL SEAT TRACK IAW SRM 51-40-21. IAW SRM 53-15-16. LOCATED & DRILLED NEW SEAT TRACK SECTION IAW D WG A53874204. ALODINED & PRIMED IAW 51-75-10. INSTALLED IAW SRM 51-40-21. CIC AREA IAW AMM 51-20-00-0. MAJOR REPAIR. 2 L 7 2 4F RT A35EU 2008031300423 20080313 00423 NM 2008 3 13 SWAA081332 1 20080310 A 3397 W4142001220 WIRE BOEING 737 7377H4 1384404 NM CABIN CHAFED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 297WN 32542 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT RT FWD CABIN. FOUND CHAFED WIRE. REPAIRED WIRE PER WDM. 2 L 7 2 4F RT A16WE 2008031400004 20080314 00004 NE 2008 3 14 Q2SA740008 2 20080304 A 7261 CF650E2 ENGINE BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 2 LEAKING A Q2SA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 63 740SA * 21380 517139 NUMBER 2 ENGINE SHUTDOWN DUE TO LOSS OF ENGINE OIL QUANTITY IN FLIGHT OUT OF RKSI. OIL QUANTITY DRAMATICALLY DECREASED FROM ABOVE 3 GALLONS TO BELOW 1 GALLON IN LESS THAN 5 MINUTES. OIL PRESSURE WAS STEADY, OIL TEMPERATURE WAS NORMAL. AF TER ENGINE WAS SHUTDOWN IN ACCORDANCE WITH QRH PROCEDURES, THE OIL QUANTITY AND PRESSURE DECREASED TO ZERO WITH THE ENGI NE WINDMILLING. ALL OTHER ENGINE INDICATIONS WERE NORMAL PRIOR TO ENGINE SHUTDOWN. DUMPED APPROXIMATELY 200,000 POUNDS OF FUEL AND RETURNED TO RKSI. METAL PARTICLES FOUND AT CHIP DETECTOR. REPLACING NR 2 ENGINE. 2 L 7 4 4F 4 F RT A20WE E23EA 2008031400007 20080314 00007 NM 2008 3 14 QXEA200800255 1 20080227 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - RIGHT SIDE FRAME CASTELLATION (SKIN LEG) AT STATION X136 AND STRINGER 24S HAS AREA OF CORROSION AROUND RIVET. REPAIRED IAW DASH 8 Q400 SRM 51-42-05, 51-21-00, Q400 NDTM PART 6 51-00-01 AND PART 1 51-00-04, Q400 SRM 51-21-10, 51- 25-10, 51-21-00, 51-42-00, AND 51-25-10 AND 51-25-15. 2 H 7 2 4T RT A13NM 2008031400008 20080314 00008 NM 2008 3 14 QXEA200800256 1 20080227 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - CORROSION ON FRAME CLIP AFT CARGO PIT STATION X819/Z111.5/STRINGER 21R UNDER CARGO TIE DOWN COVER 251VZ. REM OVED CLIP AND REPAIRED IAW DASH 8 Q400 SRM 51-21-00 QND 51-14-00, ALSO Q400 NDTM PART 6 51-00-01. REINSTALLED CLIP IAW D ASH 8 Q400 SRM 51-42-05, 51-21-10, 51-25-45 AND 51-25-20. 2 H 7 2 4T RT A13NM 2008031400022 20080314 00022 NM 2008 3 14 2008UALA01134 1 20080229 A 5210 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 R1 DOOR WEB BY UPPER HINGE INTERCOSTAL GOUGED. ACCOMPLISHED AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031400028 20080314 00028 NM 2008 3 14 2008UALA01186 1 20080303 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 620 S16L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 CRACK FOUND IN STRINGER 16L AT BS 620, OUT OF FASTENER HOLE. CRACK VERIFIED ON LT EXTERNAL SKIN REPAIR. MAJOR REPAIR A CCOMPLISHED AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031400034 20080314 00034 EU 2008 3 14 2008UALA01196 1 20080305 A 2421 IDG AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 467UA 1359 NR 2 ENGINE IDG POWER FEEDER CONNECTION FAILURE CAUSED DIVERSION. FOUND NR 2 ENG IDG FAILURE. NO IDG FEEDER CABLE ISSUE . REPLACED NR 2 IDG, PERFORMED INSPECTION OF IDG FEEDER CONNECTION AT PYLON AND CKECKED FOR PIN BURNING OR ARCING. ARE A OK, NO ISSUES NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031400041 20080314 00041 NM 2008 3 14 2008UALA01218 1 20080305 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FWD PIT DOOR CUTOUT, AFT FRAME IS CRACKED ABOVE LOWER STOP FITTING. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED N ESTED ANGLE FRAME REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031900342 20080319 00342 NM 2008 3 19 USAA920080628 1 20080301 A 5330 144N33108402 SKIN BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 917UW 22193 PIT - MAJOR REPAIR - C1 CHECK - CORROSION ON INTERNAL FUSELAGE SKIN BUTT SPLICE, BS 900, S15R - S17R. REPLACED INTERNAL FUSELAGE SKIN BUTT SPLICE, BS 900, S15R - S17R IAW USAIRWAYS EA 110650 AND 97847. 2 L 7 2 4F RT A2NM 2008031900361 20080319 00361 EA 2008 3 19 TRAX200800406 1 20080310 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 AAR - INTERCOSTAL CLIP CRACKED AT FS 484 LBL 36. 2 L 7 2 4F RT A21EA 2008031900381 20080319 00381 NM 2008 3 19 KCSA081176 1 20080315 A 5311 STRAP BOEING 747 747SR46 1384816 NM FUSELAGE MISSING A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 AFT BILGE FUSELAGE FRAME STABILIZATION STRAP IS MISSING A SECTION AT STA 2160, LBL 6. 2 L 7 4 4F RT A20WE 2008031900393 20080319 00393 NM 2008 3 19 CALA0800224 1 20080307 A 5320 6517688132 SUPPORT ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 LEFT SUPPORT ANGLE FOR Z-ANGEL AT L1 DOOR JUST FWD OF FS 324 IS CORRODED. REMOVED AND INSTALLED NEW SUPPORT L-1 DOOR SU PPORT ANGLE IAW SRM 53-10-15. 2 L 7 2 4F RT A16WE 2008032000016 20080320 00016 CE 2008 3 20 DXTA200802831 1 20080201 A 3510 OXYGEN MASK CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE COCKPIT MALFUNCTIONED E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 324QS 5600423 BOTH PILOT AND COPILOT OXYGEN MASK HAVE REDUCED OXYGEN FLOW, AS IF AN OBSTRUCTION OF VALVE FAILURE OCCURED. RESEATED OXY GEN MASKS OPS CHECKED SATISFACTORY IAW MM 35-00-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2008032000034 20080320 00034 NM 2008 3 20 DXTA200802844 1 20080207 A 2120 4AS7811103507 AIR DUCT GULSTM 200 200 4500308 NM PWA PW206 PW206A NE CONTAMINATED E DXTA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 07 707QS 4216 066 WITH THE APU ON THE COCKPIT FILLED WITH JET FUEL FUMES STRONG ENOUGH TO BURN YOUR EYES. FOUND AIR COND. DUCTS UNDER CABI N FLOOR TO BE FUEL SOAKED. REMOVED FUEL SOAKED DUCTS AND INSTALLED INSPECTED DUCTS, LEAK AND OPS CHECKED OK. IAW G200 M M 25-00-00. NO ODOR DETECTED. 2 L 7 2 4F 3 U RT A53NM E42NE 2008032000042 20080320 00042 CE 2008 3 20 DXTA200802850 1 20080207 A 2750 FLAP SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS CONTAMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 953QS 7500153 (FLAPS FAIL) CAS MESSAGE AFTER TAKEOFF WHEN FLAP LEVER SELECTED UP. CLEANED SAND AND OTHER DEBRIS FROM FLAP WELL. OPS C HECK GOOD AD NO BITE APPEARED AFTER SEVERAL OPERATIONS. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032000044 20080320 00044 CE 2008 3 20 DXTA200802852 1 20080207 A 3260 S31771 UPLOCK SWITCH CESSNA 750 750 2076810 CE NLG INOPERATIVE E DXTA O OTHER N FALSE WARNING DE DESCENT 1 GL 07 945QS 9234 7500029 RED GEAR (UNLOCKED) LIGHT REMAINED ON AFTER GEAR RETRACTED. REMOVED AND REPLACED NLG UPLOCK SWITCH IAW MM 32-30-05. OPS CHECK GOOD. 2 L 7 2 4J RT T00007WI 2008032000046 20080320 00046 CE 2008 3 20 DXTA200802853 1 20080208 A 3620 99141492 THERMAL SWITCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE RT BLEED SYS MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 605QS 4977 5605321 RT BLEED AIR OVERHEAT ANNUNCIATOR ILLUMINATED ON DEPARTURE, RT THROTTLE RETARDED TO BELOW 80 PERCENT N1 AND LIGHT WENT O UT. TROUBLESHOT SQUAWK DOWN TO RT BLEED AIR OVERTEMP SWITCH. REMOVED AND REPLACED RT BLEED AIR OVERTEMP SWITCH AND OPS AND LEAK CHECKED GOOD IAW MM 36-11-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032000057 20080320 00057 NE 2008 3 20 DXTA200802864 2 20080210 A 7200 31J190001 ENGINE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LEFT SHUTDOWN E DXTA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 GL 07 677QS 3568 5605367 PCEDB0761 LT ENGINE QUIT SHORTLY AFTER TAKEOFF. FIRST NOTICED EEC MANUAL ANNUNCIATOR, FOLLOWED BY (DASHES) ON LT FUEL FLOW INDICAT OR (NEW GAUGES). ENG WAS ROTATING FREELY AND LT BOOST PUMP CAME ON AUTOMATICALLY. REMOVED AND REPLACED NR1 ENG WITH REPA IRED UNIT IAW MM 71-00-03. OPERATIONAL AND LEAK CHECKS GOOD. FOR DETAILS REFER TO WO NR 030705. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032000058 20080320 00058 CE 2008 3 20 DXTA200802865 1 20080210 A 2150 73838433 ACM CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL AFT SERVICE BAY LEAKING E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 903QS 3056 3056 7500162 SMOKE IN CABIN ON START OF TAXI, MAINLY LT SIDE VENTS NEAR TABLE. REMOVED AND REPLACED FWD ACM ASSY IAW MM CH 21-51-00. OPERATIONAL AND LEAK CHECKS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032000059 20080320 00059 CE 2008 3 20 DXTA200802866 1 20080210 A 3230 BUMPER BLOCK BEECH MU300 400A 1155402 CE NLG DAMAGED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 153QS RK490 UPON LANDING GEAR RETRACTION, THE 3 GREEN LIGHTS EXTINGUISHED BUT THE RED GEAR HANDLE UNSAFE LIGHTS REMAINED ILLUMINATED . REMOVED EXCESS MATERIAL FROM RUBBER NOSE GEAR BUMPERS IN NOSE WHEEL WELL. OPERATIONAL CHECK NOW SATISFACTORY. CYCLED G EAR & CHECKED NOSE GEAR UPLOCK SWITCH ADJUSTMENT. CHECKS GOOD IAW MM CH 32-30-00. SERVICED HYD RESERVOIR. 2 H 7 2 4F RT A16SW 2008032000061 20080320 00061 CE 2008 3 20 DXTA20082868 1 20080210 A 2150 73838433 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AFT SERVICE BAY LEAKING E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 926QS 273 7500026 FWD ACM HAS OIL DRIPPING FROM IT, CABIN AS OILY SMELL COMING FROM VENTS. REMOVED AND REPLACED CABIN ACM. REMOVED AND C LEANED COALESCER SOCK, INSTALLED SOCK. OPERATIONAL CHECK GOOD ON ACM. NO LEAKS NOTED. PERFORMED ASPIRATOR LINE FUNCTION AL CHECK. FUNCTIONAL CHECK GOOD. WORK PERFORMED IAW MM 12-10-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032000062 20080320 00062 CE 2008 3 20 DXTA20082869 1 20080212 A 5610 991438011 WINDSHIELD CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL COCKPIT FRACTURED E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 956QS 6835 7500156 PILOTS WINDOW STARTED ARCING THEN SHATTERED IN FLIGHT THROUGH FL400. REMOVED AND REPLACED PILOTS WINDSHIELD, OPERATIONAL LY AND LEAK CHECKS GOOD IAW MM 56-11-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032000064 20080320 00064 CE 2008 3 20 DXTA20082871 1 20080213 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MALFUNCTIONED E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 312QS 5600312 CO-PILOT'S LT BRAKE DEPRESSES TO FLOOR WITH NO RESULT. COMPLETED BRAKE BLEED PROCEDURE. BRAKES OPS CHK GOOD. AMM 32-42-0 0. 2 L 7 2 4F 4 F RT A22CE E25EA 2008032000071 20080320 00071 NM 2008 3 20 EVAS097002 1 20080223 A 2497 FEEDER CABLE BOEING 747 747400 13848AT NM GE CF6 CF680C2* GL NR 1 GENERATOR ARCED W QOCF H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 03 16410 29061 AFTER A/C ON BLOCK, FOUND THE DADO PANEL ON SIDE WALL PANEL 64A, 65A HAS SMOKE. MAINTENANCE USED ONE FIRE BOTTLE TO EXTI NGUISH THE SMOKE, TROUBLESHOOTING FIND: THERE WAS ARCING ON THE APU NR1 GENERATOR FEEDER CABLE, ALSO FOUND THE RIVETS ON THE STAND-OFF FOR SUPPORTING THE CABLE WAS SHEARED, THE UNSUPPORTED CABLE WAS DROPPED AND CONTACTED THE LOWER SIDE BOLT CAUSED THE ARCING DURING APU LANDING START. 2 L 7 4 4F 4 F RT A20WE E23EA 2008032000072 20080320 00072 NM 2008 3 20 EVAS097003 1 20080219 A 2822 20C1445 VALVE BOEING 747 747400 13848AT NM GE CF6 CF680C2* GL FUEL DISCHARGE FRACTURED W QOCF A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 03 16405 70448 27142 DURING CRUISE, AFTER TAKEOFF 2 HRS, PILOT FOUND THE FUEL QTY INDICATION DROP 7000 KG/HR ABNORMAL, CHECKED, FND FUEL DUMP FROM L WING TIP, PILOT CLOSE ALL 4EA CROSSFEED VALVE, THEN NO MORE FUEL OVERBOARD. AC DIVERTED FOR CHECKING AND REFUELI NG, AFTER, BACK TO HOME BASE, MAINT FOUND THE NR 2 FUEL BOOST PUMP DISCHARGE CHECK VALVE HOUSING HAD FRACTURED. 2 L 7 4 4F 4 F RT A20WE E23EA 2008032000075 20080320 00075 CE 2008 3 20 DXTA20082876 1 20080214 A 3230 99124913 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE NLG FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 675QS 5241 5605275 AFTER TAKEOFF, DURING GEAR RETRACTION, NOSE GEAR STAYED DOWN AND LOCKED (GREEN ) MAIN GEARS OPERATED NORMALLY. REMOVED N OSE GEAR ACTUATOR DUE TO INTERNAL FAILURE. INSTALLED RENTAL ACTUATOR IAW MM CH 32-30-03. PERFORMED GEAR FUNCTIONAL TES T IAW MM CH 32-01-00. OPS CHECK AND LEAK CHECK, GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032000077 20080320 00077 CE 2008 3 20 DXTA20082878 1 20080214 A 2797 WIRE BEECH MU300 400A 1155402 CE STAB FAIL IND BROKEN E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 106QS RK381 (H) STAB FAIL) LIGHT ILLUMINATED IN FLIGHT. INSPECTED AND FOUND BROKEN WIRE AT P540 CONNECTOR PLUG. REPAIRED WIRE IAW MM 20-20-04. PERFORMED PITOT TEST, SYSTEM PASSED. PERFORMED GROUND CHECK, OPS CHECK GOOD. DONE IAW AMM 30-12-00. 2 H 7 2 4F RT A16SW 2008032000078 20080320 00078 CE 2008 3 20 DXTA20082879 1 20080217 A 3260 1223820381 CONTROL SWITCH BEECH MU300 400A 1155402 CE MLG INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 138QS 687 RK492 RED LANDING GEAR UNSAFE LIGHT REMAINS ON AFTER GEAR RETRACTION. REPLACED LANDING GEAR CONTROL SWITCH ASSY WITH NEW UNIT. PERFORMED LANDING GEAR FUNCTIONAL CHECK - SWUNG GEAR 5 TIMES WITH NO DEFECTS. OPS CHECKS GOOD. MX IAW MM CH 32-30-00. 2 H 7 2 4F RT A16SW 2008032000084 20080320 00084 SO 2008 3 20 FDKA200803093 1 20080307 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6071 MCO-PNS (0443 PHX LCL) - ROW 12 EMERGENCY LIGHTS INOP. MX RESECURED LIGHT CONNECTORS, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008032000085 20080320 00085 SO 2008 3 20 FDKA200803095 1 20080307 A 3411 PITOT HEAD EMB 145 EMB145LR 3260212 SO INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FDM 6201 FLL (0629 PHX LCL) - DECLARED EMERGENCY CAPTAIN AIRSPEED AND ALTITUDE INDICATION INACCURATE AND SUSPECT PITOT H EAT SYSTEM INOP. MX DRAINED WATER FROM PITOT STATIC SYSTEM AND RESET PITOT HEAT SYSTEM, SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008032000091 20080320 00091 SO 2008 3 20 FDKA200803102 1 20080307 A 5414 PANEL EMB 145 EMB145LR 3260212 SO NACELLE DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 835MJ 145353 PANEL 412CL HAS ONE FASTENER HOLE ELONGATED. THE DAMAGE HAS BEEN REPAIRED AND A DIMPLED WASHER INSTALLED. 2 L 7 2 4T RT T00011AT 2008032000092 20080320 00092 EA 2008 3 20 SWIA200819331 1 20080307 A 5610 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 744SK 10200 FLT 6229 - CAPTAINS WINDSHIELD SHATTERED DURING FLIGHT. REPLACED CAPTAIN'S WINDSHIELD WITH SERVICEABLE UNIT IAW MM 56-1 1-01, P/N OFF: 601R33033-17, S/N OFF: 04206H1831. 2 L 7 2 4F RT A21EA 2008032000107 20080320 00107 WP 2008 3 20 NWAA080919995 1 20080311 A 2612 FIRE DETECTOR DOUG DC9 DC931 3022065 WP APU BAY MALFUNCTIONED A NWAA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 GL 01 8978E 47327 THE AIRCRAFT DISPATCHED WITH LOOP A OF THE FIRE DETECTION SYSTEM ON MEL. WHEN PASSING THROUGH FL300 THE APU FIRE WARNIN G INDICATIONS ILLUMINATED. THE AMBER "LOOP B" LIGHT, THE RED "APU FIRE" LIGHT, AND BOTH THE RED "MASTER WARNING" AND TH E YELLOW "MASTER CAUTION" LIGHTS ILLUMINATED. THE APU WAS SECURED PRIOR TO FIRE INDICATIONS. FLIGHT CREW COMPLIED WITH COM AND DISCHARGED THE NR 1 FIRE AGENT BOTTLE. THE NR 1 "AGENT LOW" INDICATION DID NOT COME ON SO THE CREW ACTIVATED T HE NR 2 AGENT BOTTLE. THE "APU FIRE" INDICATION REMAINED EVEN AFTER BOTH BOTTLES WERE DISCHARGED. AN EMERGENCY WAS DEC LARED WITH ATC AND THE AIRCRAFT IMMEDIATELY RETURNED TO BOS. THE LANDING WAS UNEVENTFUL AND NO EVIDENCE OF FIRE HAS BEEN 2 L 7 2 4F A6WE 2008032000111 20080320 00111 SO 2008 3 20 SIMA200807304 1 20080311 A 2150 A/C PACK EMB 145 EMB145LR 3260212 SO ODOR A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 642AE 145193 ON FLIGHT 3653, CREW REPORTED DURING TAXI OUT WITH APU BLEED SUPPLYING THE PACKS A "HAZE" IN THE COCKPIT AND CABIN. ALS O DETECTED A BURNING SULFUR ODOR. 2 L 7 2 4T RT T00011AT 2008032000117 20080320 00117 NM 2008 3 20 DL76G080323 1 20080308 A 2420 IDG BOEING 767 767332 1382001 NM INOPERATIVE A DALA H DEACTIVATE SYST/CIRCUITS H J ELECT. POWER LOSS-50 PC WARNING INDICATION DE DESCENT 1 SO 27 1613B C0871 32776 90 MIN OUT OF MAN, THE CREW GOT A LT ENG IDG DRIVE LIGHT. AFTER FOLLOWING QRH 50 MIN LATER, THE APU FAILED AND WOULD NO T RESTART. LGCU SWAPPED WITH APU GCU. LEFT S/N 1195 AND APU NOW S/N 6111. IDG REPLACED. ENGINE RUN CARRIED OUT. IDG OPS NML. LEAK OK. DISCONNECT FUNCTION, OPS NML. 2 L 7 2 4F RT A1NM 2008032000123 20080320 00123 NM 2008 3 20 DL777080330 1 20080310 A 4920 498040000 ENGINE BOEING 777 777232 1385232 NM APU MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 862DA 13591 29734 APU AUTO SHUTDOWN REPLACED APU PER TRANSMITTAL 11T007. 2 L 7 2 4F RT T00001SE 2008032000127 20080320 00127 NM 2008 3 20 DL757080334 1 20080203 A 5321 FLOOR PANEL BOEING 757 757232 1384965 NM CARGO BAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 FWD CARGO FLOOR PANEL 121BF CORRODED UPPER AND LOWER SURFACES AND CRACKED IN CUTOUT. REPAIRED IAW SRM 53-30-53 FIG/SHT 7 AND SRM 51-20-01. 2 L 7 2 4F RT A2NM 2008032000128 20080320 00128 NM 2008 3 20 DL757080335 1 20080217 A 5210 GATE BOEING 757 757232 1384965 NM L2 DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 FOUND CORROSION ON LOWER GATE OF L2 DOOR. REPLACED GATE IAW MM 52-11-38. 2 L 7 2 4F RT A2NM 2008031400051 20080314 00051 NM 2008 3 14 CALA0800204 1 20080306 A 5311 65C34355 FRAME BOEING 737 737524 1384721 NM BS 482 S9L/R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 FRAME CRACKED STA 482 BETWEEN S9L AND S9L. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A. 2 L 7 2 4F RT A16WE 2008031400068 20080314 00068 WP 2008 3 14 AALA200800456 1 20080229 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 494AA 49732 LGA - EMERGENCY LIGHTS AT FIRST CLASS GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS GAL LEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031400071 20080314 00071 NM 2008 3 14 AALA200800450 1 20080228 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 775AN 29584 DFW - EMERGENCY LIGHT AT SEAT 36G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 36G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031400081 20080314 00081 WP 2008 3 14 AALA200800458 1 20080229 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 487AA 49680 LGA - EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031400082 20080314 00082 WP 2008 3 14 AALA200800459 1 20080229 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 258AA 49288 DFW - EMERGENCY LIGHT AT SEAT 12D HAS SHROUD MISSING. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031400084 20080314 00084 NM 2008 3 14 AALA200800448 1 20080228 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 775AN 29584 DFW - EMERGENCY LIGHT AT SEAT 31C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031400085 20080314 00085 EU 2008 3 14 F3LA200800083 1 20080229 A 5320 D5347112420000 SHEAR PLATE AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE LEFT CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED THE LEFT SHEAR PLATE BETWEEN FRAMES 69 AND 70 SHOWED SIGNS OF CORROSION. MAIN TENANCE REMOVED AND REPLACED THE SHEAR PLATE AT FRAMES 69 AND 70, IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42- 11 PARAGRAPHS 6 AND 7 AND AIRBUS DRAWING D53474180. FOLLOWING COMPLETION OF THE INSTALLATION THE SHEAR PLATE WAS INSPEC TED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008031400086 20080314 00086 NM 2008 3 14 F3LA200800078 1 20080301 A 5320 D5391635520000 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED THE RIGHT, FORWARD CARGO PIT FLOORBOARD ATTACH POINT AT STRINGER 38 HAD EVIDEN CE OF CORROSION AT THE NUT PLATE HOLE LOCATIONS BETWEEN FRAME 28 AND 35. MAINTENANCE REMOVED AND REPLACED THE PROFILE P LATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPH 6. FOLLOWING COMPLETION OF THE REPLACEMENT, TH E PROFILE WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008031400087 20080314 00087 NM 2008 3 14 F3LA200800079 1 20080301 A 5320 D5348004320601 SILL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED THE L-2 DOOR SILL, AFT GIRT BAR FITTING CUT OUT, SHOWED SIGNS OF CORROSION ON THE AFT, OUTBOARD SCREW HOLE. MAINTENANCE REMOVED AND REPLACED THE L-2 DOOR SILL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PAGE 7. FOLLOWING COMPLETION OF THE INSTALLATION, THE DOOR SILL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008031400092 20080314 00092 NM 2008 3 14 DHL2008753500 1 20080308 A 5320 STIFFENER BOEING 727 727223 1384074 NM BS 930 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 C CHECK REF N/R 096608, LT WHEEL WELL STA 930 LBL 8, VERTICAL STIFFENER HAS CORROSION AT LOWER END AROUND NUT PLATE, ANC HOR NUT AND SURFACE. REMOVED CORROSION ON LT WHEEL WELL STA 930 LBL 8, VERTICAL STIFFENER IAW B727 SRM 51-10-6, PER SRM 53-10-2 FIG4 ORIGINAL THICKNESS IS .150 MATERIAL REMOVED IS .039, MATERIAL REMAINING .111 FOUND TO BE OUT OF LIMITS PER 53-10-01 FIG 1. FABRICATED NEW VERTICAL STIFFENER FROM BAC1520-1247 7178-T6 3' IN LENGTH PO NR 7232230, PER DIG NR 65- 18636 REV F AND PL 65-18636 REV G. INSTALLED STIFFENER IAW SRM 51-30-2 AND BACK DIG NR 65-18636 REV F. 2 L 7 3 4F A3WE 2008031400093 20080314 00093 2008 3 14 IXXA080010O 4 20080306 A 2300 G515B SPEAKER DOUG DC8 DC862F 3021972 WP COCKPIT ODOR A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 71CX 71698 1695 45961 DURING CRUISE FROM PKWA, THE CREW NOTICE A ELECTRICAL ODOR COMING FROM THE RIGHT RECIRC FAN. THE CREW TURNED OFF THE R IGHT RECIRC FAN AND LANDED WITHOUT INCIDENT IN PHIK. MAINTENANCE INSPECTED AND FOUND THAT THE ELECTRICAL ODOR WAS COMIN G FROM THE FIRST OFFICER'S OVERHEAD PANEL SPEAKER. MAINTENANCE DEFERRED FIRST OFFICERS SPEAKER IAW ATI MEL 23-1 TO KMCC . MAINTENANCE IN KMCC REPLACED FIRST OFFICER'S OVERHEAD SPEAKER OPERATIONAL CHECK GOOD IAW DACO DC8 23-50-0. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 2008031400097 20080314 00097 NM 2008 3 14 2008UALA01229 1 20080306 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 500 S21R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 STATION 500A 2" BELOW STRINGER 21R LIGHTNING STRIKE METAL EXPOSED. MAJOR REPAIR ACCOMPLISHED: INSTALLED SOLID RIVET AND INSTALLED SHEAR TIE REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031700004 20080317 00004 NM 2008 3 17 NWAA080856309 1 20080307 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT LIGHTS ON RIGHT SIDE AFT WING TO BODY FAIRING INOP. MAINTENANCE REMOVED AN D REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008031700006 20080317 00006 NM 2008 3 17 2008UALA01242 1 20080307 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY LT INOP, DR1L BOTH SILLS. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031700007 20080317 00007 SO 2008 3 17 C2XA08ON098 1 20080225 A 3010 4800104 SWITCH EMB 145 EMB145XR 3260214 SO COCKPIT INOPERATIVE A C2XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 11193 7015 7015 14500938 FLT 0030 - MCI - FLIGHT CREW REPORTED NR 1 WING ANTI-ICE FAIL ON EICAS. FLIGHT DIVERTED FROM OMA TO MCI. MX PERSONNEL REMOVED AND REPLACED NR 1 WING ANTI-ICE PUSH BUTTON, OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETUR N TO SERVICE. 2 L 7 2 4F RT 2008031700009 20080317 00009 NM 2008 3 17 2008UALA01243 1 20080307 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 FOUND DOOR 1L UPPER EMERGENCY EXIT SIGN INOP. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031700023 20080317 00023 SO 2008 3 17 C2XA08IA071 1 20080303 A 3230 23092900001B UPLOCK EMB 145 EMB145EP 3260221 SO RT MLG DEFECTIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13935 22321 22321 145022 IAH - FLIGHT 2742, THE CREW REPORTED A LOUD BANGING SOUND AFTER GEAR RETRACTION COMING FROM THE NOSE GEAR AREA, AND AFTE R DEPARTURE THE RIGHT MAIN GEAR INDICATION SWITCHED FROM UP TO AMBER, BACK TO UP. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE RIGHT HAND MAIN LANDING GEAR UPLOCK BOX AND PROXIMITY SWITCHES, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. 2 L 7 2 4F RT T00011AT 2008031700025 20080317 00025 SO 2008 3 17 C2XA08RI028 1 20080228 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 13969 7385 3245 145141 FLIGHT 2076 CREW REPORTED BOTH LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. EWR MX REMOVED AND REPLACED FWD EM ERGENCY LIGHT BATTERY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008031700033 20080317 00033 NM 2008 3 17 UPS08551768 1 20080307 A 3350 LAMP BOEING 757 75724APF 1384969 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 450UP 25472 EMERGENCY EXIT LIGHTS "UNARMED" LIGHT MODULE ONE LAMP INOP. RELAMPED PER AMM 33-13-00-2. 2 L 7 2 4F RT A2NM 2008031700037 20080317 00037 SO 2008 3 17 C2XA08IA076 1 20080308 A 3213 23092005007 SHOCK ABSORBER EMB 145 EMB145LR 3260212 SO RT MLG STICKING A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 12564 14948 14948 145618 IAH - FLIGHT 2192, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE AND THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND MAIN LANDIN G GEAR SHOCK ABSORBER, OPERATIONALLY CHECKED THE EXTENSION / RETRACTION SYSTEM WITH NO DEFECTS, AND THE AIRCRAFT WAS APP ROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008031700041 20080317 00041 SO 2008 3 17 C2XA08IA078 1 20080307 A 3320 BR90002 BALLAST EMB 145 EMB145LR 3260212 SO LAVATORY DEFECTIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 13955 145075 BNA - FLIGHT 3025M THE CREW REPORTED A SMOKE SMELL COMING FROM THE LAV WHEN FLUSHED. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE LAV ON MEL 38-30-00 CAT C CONTROL NUMBER 140961, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. T HE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE LAVATORY LIGHT BALLAST ABOVE THE SINK, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. 2 L 7 2 4T RT T00011AT 2008031700044 20080317 00044 SO 2008 3 17 C2XA08IA077 1 20080303 A 2611 WARNING SYSTEM EMB 145 EMB145XR 3260214 SO LAVATORY MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 SW 27 11189 14500931 AUS - FLIGHT 1, THE CREW REPORTED A LAV SMOKE WARNING IN FLIGHT. THE AIRCRAFT RETURNED TO AUS WHERE IT LANDED WITHOUT I NCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE LAV SMOKE DETECTOR WITH NO DEFECTS NOTED, AND TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008031700045 20080317 00045 NM 2008 3 17 08FDEA00798 1 20080309 A 5730 ARB23122 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 521FE 48478 RT WING, DROOP LEADING EDGE SURFACE FOUND CRACKED AT FASTENER HOLE. REPAIRED AS PER SRM 57-10-00 FIGURE 30 VOLUME I. RE PAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008031700046 20080317 00046 NM 2008 3 17 08FDEA00799 1 20080309 A 5710 ARB2886504 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 521FE 48478 RING WING, LEADING EDGE TELESCOPIC DUCT CUTOUT DOOR OUTBOARD CORNER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 43 VOLUME I AND EA 1-5710-115329. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008031700048 20080317 00048 NM 2008 3 17 SWAA081270 1 20080309 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031700049 20080317 00049 NM 2008 3 17 SWAA081333 1 20080310 A 5310 6546818 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 952 AND BS 990, STR 17R. REMOVED AND REPLACED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2008031700055 20080317 00055 NM 2008 3 17 SWAA081277 1 20080309 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 520, STR 23R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008031700058 20080317 00058 NM 2008 3 17 SWAA081308 1 20080306 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIPS WORN BETWEEN ROW 6 DEF AND ROW 8 DEF. REMOVED AND REPLAC ED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008031700065 20080317 00065 NM 2008 3 17 SWAA081329 1 20080310 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA BS 390, STR 28R. REPAIRED SKIN PER E A. 2 L 7 2 4F RT A16WE 2008031700066 20080317 00066 NM 2008 3 17 SWAA081278 1 20080307 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 410, BL 0. REPAIRED SKIN PER EA AND SB. 2 L 7 2 4F RT A16WE 2008032000137 20080320 00137 NM 2008 3 20 DL757080344 1 20080204 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 1640 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 CORROSION ON MAIN CABIN FLOORBEAM STA 1640 RBL 2. REMOVED DAMAGE IAW SRM 53-00-51. FABRICATED AND INSTALLED BEAM IAW S RM 53-00-51. 2 L 7 2 4F RT A2NM 2008032000139 20080320 00139 NM 2008 3 20 DL757080346 1 20080201 A 5347 SEAT TRACK BOEING 757 757232 1384965 NM BS 365-440 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 MAIN CABIN STA 365-440; SEAT TRACK AT RBL 24 HAS SECTION OF SEVERE COROSION. FABRICATED AND REPLACED SEAT TRACK SECTION IAW SRM 53-10-52. 2 L 7 2 4F RT A2NM 2008032000140 20080320 00140 NM 2008 3 20 DL757080347 1 20080205 A 5320 FLOOR SUPPORT BOEING 757 757232 1384965 NM BS 1650-1670 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 CORROSION ON FLOOR SUPPORT AFT CABIN STA 1650-1670 RBL 60. REMOVED AND REPLACED SUPPORT IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008032000143 20080320 00143 NM 2008 3 20 DL757080350 1 20080205 A 5321 FLOOR PANEL BOEING 757 757232 1384965 NM CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 FWD CARGO FLOOR PANEL 121BF HAS CORROSION ON UPPER AND LOWER SURFACE. FABRICATED FLOOR PANEL IAW SRM 51-20-01 AND INSTA LLED IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008032000150 20080320 00150 NM 2008 3 20 NWAA080936309 1 20080221 A 5313 STRINGER BOEING 747 747451 1384940 NM BS 480 S10L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING M" CHECK FOUND CRACKS IN STRINGER 10L AT BS 480. REPAIRED PER EA 63-212201. 2 L 7 4 4F RT A20WE 2008032000151 20080320 00151 NM 2008 3 20 NWAA080776309 1 20080221 A 5313 STRINGER BOEING 747 747451 1384940 NM BS 500 S10L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING "M" CHECK, FOUND CRACKS IN STRINGER 10L AT BS 500. REPAIRED PER EA 63-212202. 2 L 7 4 4F RT A20WE 2008032000163 20080320 00163 WP 2008 3 20 08FDEA00906 1 20080312 A 5730 ARC0389U13 RETAINER DOUG MD10 MD1010F 3022112 WP LT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LEFT WING INBD T/E PANEL 541 GB SEAL HOLDER IS GOUGED. REMOVED GOUGED SEAL RETAINER AND REPLACED IAW SRM 51-35-01 VOL I I. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008032000164 20080320 00164 WP 2008 3 20 08FDEA00907 1 20080312 A 5754 ARC2012506 PANEL DOUG MD10 MD1010F 3022112 WP RT WING TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RT WING OUTBD FLAP HINGE PANEL NR 636GL IS DELAMINATED ON THE INNER SURFACE. REPAIRED PANEL & FABRICATED & BONDED NEW I NNER & OUTER SKINS IAW DWG ARC2012, TPS 1001 REV E & EA 8-5750-116964. 2 L 7 3 4F RT A22WE 2008031900213 20080319 00213 EU 2008 3 19 USAA920080569 1 20080226 A 5315 D53472173200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651AW 866 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3158 /FR 66 - BS 3366 /FR 70, -Y765. REPLACED CABIN FL OORBEAM, BS 3158 /FR 66 - BS 3366 /FR 70, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900232 20080319 00232 NM 2008 3 19 USAA920080578 1 20080302 A 5315 D5347209000200 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801AW 889 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 2728 / FR 65, +Y765. REPLACED CABIN FLOORBEAM, BS 2728 / FR 65, +Y765 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900233 20080319 00233 NM 2008 3 19 USAA920080579 1 20080302 A 5320 D5311283320000 DUMMY RAIL AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801AW 889 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN DUMMY RAIL BEAM, BS 683 / FR 15 - BS 709 / FR 16, -Y1380. REPLACED C ABIN DUMMY RAIL BEAM, BS 683 / FR 15 - BS 709 / FR 16, -Y1380 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900254 20080319 00254 2008 3 19 DXTA200802811 4 20080130 A 2210 6229814632 PCB AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE AUTOPILOT INOPERATIVE E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 226QS 5409 126 INTERCEPTED ILS LOCALIZER WITH AUTOPILOT ENGAGED ABOUT 3 MILES BEFORE GLIDESLOPE INTERCEPT AUTOPILOT ABRUPTLY PITCHED DO WN 4 TO 5 DEGREES THEN UP A FEW DEGREES WITH A SMALL AMOUNT OF BANK. REPLACED 2B10C CARD AND CHECKED IAW A/C SYS MANUAL, COMPLETED IAW MM 22-100, COMPLETED BRIEF AND DETAILED CHECK ON FLIGHT CONTROLS IAW MM 27-014 AND 27-016. ALL CHECK GOO D AT THIS TIME. 2 L 7 2 4F 4 F RT A50NM E44NE 2008031900264 20080319 00264 CE 2008 3 19 021708N339CS1 1 20080217 A 3260 BULB CESSNA 500 550 2076604 CE PWA 530 PW530A NE MLG INDICATOR INOPERATIVE E Z5FA A UNSCHED LANDING P NO WARNING INDICATION AP APPROACH 1 EA 63 339CS 5501085 ON APPROACH, THE RT MAIN GEAR INDICATOR LIGHT WOULD NOT ILLUMINATE. CREW FOLLOWED AFM CHECKLIST PROCEDURE. THE LANDING G EAR EMERGENCY BLOW DOWN BOTTLE WAS USED. AC DIVERTED, LANDING WAS UNEVENTFUL, EMERGENCY VEHICLES WERE STANDING BY. MAIN T TROUBLESHOT THE DISCREPANCY TO A LOOSE RT LANDING GEAR INDICATOR SWITCH. THE SWITCH WAS RESEATED AND THE BULBS WERE RE PLACED. MAINT RESET, PURGED, AND SERVICED THE EMERGENCY GEAR AND BRAKE SYSTEM. SEVERAL GEAR SWINGS WERE PERFORMED. SYSTE M OPERATION CHECKED GOOD. 1 L 7 2 4F 4 F A22CE E00053EN 2008031900267 20080319 00267 SO 2008 3 19 2008F00001 1 20080220 A 6210 L621M1010056 BLADE PIPER PA44 PA44180 7104402 SO LYC O360 O360A1D 41514 EA MAIN ROTOR CRACKED G K NONE O OTHER IN INSP/MAINT 1 GL 13 135U 375 4496015 COMPOSITE MAIN ROTOR BLADE CRACKED FROM STA 4855 TO 4880, (45 DEGREE CRACK) FROM TRAILING EDGE FWD TO EDGE OF SPAR. MFG TECHNICAL INFORMATION LETTER NR EC135 014-2005 ADDRESSES 45 DEGREE CRACKS IN EARLIER S/N BLADES. OPERATOR GROUNDED AIR CRAFT AND CONTACTED MFG. 1 L 7 2 3O 3 O A19S0 E286 2008031900322 20080319 00322 NM 2008 3 19 KCSA081173 1 20080313 A 3350 3010274 LIGHT BOEING 747 747246F 1384850 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 707CK 21681 UPPER DECK EMERGENCY SLIDE LIGHT IS INOP. 2 L 7 4 4F RT A20WE 2008031900332 20080319 00332 CE 2008 3 19 DXTA200802816 1 20080131 A 2741 55657563 TRIMMER CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ELEVATOR WORN E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 639QS 6729 5605139 THE TRIM (PITCH) INDICATOR WHILE IN CRUISE IS AT THE MOST FWD PART OF THE TRIM INDICATOR. REMOVED AND REPLACED THE ELEV ATOR TRIM TABA CONTROL WHEEL P/N 5565756-3. ALSO REPLACED POINTER ARM ASSY. P/N 5565756. ALSO REPLACED POINTER ARM ASSY P/N 6661053-15, POINTER P/N 666042-12 AND ADDED (2) SHIMS P/N 6661042-16. I.AW SB REF: FIG 1 DETAIL C AND THE MM CHAP 27-32-01. ALL RIGGING CHECKS AND OPERATIONAL CHECKS SATISFACTORY AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008031900333 20080319 00333 NM 2008 3 19 USAA920080622 1 20080305 A 5347 SEAT TRACK BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 CLT - MAJOR REPAIR - C17 CHECK - LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 794 - BS 947, RBL 13.80. REPAIRED CABIN SEAT TRACK, BS 794 - BS 947, RBL 13.80 IAW USAIRWAYS EA 100289. 2 L 7 2 4F RT A16WE 2008031900351 20080319 00351 EA 2008 3 19 TRAX200800396 1 20080310 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 861AS 7445 BURNING PLASTIC SMELL COMING FROM APU BLEED. FLT 4566 DEL 21 MINS. 2 L 7 2 4F RT A21EA 2008031900359 20080319 00359 EA 2008 3 19 TRAX200800404 1 20080310 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 972EV 7534 FS 280 SUPPORT ANGLE FOR FLOORBOARD 221ALF (FLIGHT DECK FLOORBOARD) CRACKED AT RBL 9. REMOVED ANGLE IAW SRM 51-42-06. LOCATED HOLES IN NEW SERVICEABLE SUPPORT ANGLE IAW SRM 51-42-06. OK TO INSTALL. INSTALLED NEW SERVICEABLE ANGLE IAW SR M 51-42-06. FILLET SEALED AND TOPCOATED SUPPORT ANGLE IAW SRM 51-25-16 AND 51-23-00. OPS CHECK GOOD IAW MM 32-34-00. 2 L 7 2 4F RT A21EA 2008031900370 20080319 00370 CE 2008 3 19 DXTA200802823 1 20080203 A 3260 UPLOCK SWITCH BEECH MU300 400A 1155402 CE MLG OUT OF ADJUST E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 138QS RK492 RED LANDING GEAR UNSAFE REMAINS ON AFTER GEAR RETRACTION. (M2B) PERFORMED GEAR SWINGS WITH NO ADVERSE INDICATIONS CHECKE D CLEARANCES OF GEAR DOOR UPLOCK ROLLERS. NO DEFECTS FOUND, CHECKED MLG DOOR UPLOCK SW FOR PLUNGER OVERTRAVEL. FOUND RH SW. OUT OF ADJUSTMENT. ADJUSTED RH MLG DOOR UPLOCK SW. TO WITHIN LIMITS. CHECKED GEAR UPLOCK SWITCHES & FOUND RH SW OUT OF ADJ. FOR PLUNGER OVER TRAVEL. ADJUSTED GEAR UPLOCK SW. LUBED RH UPLOCK MECHANISM. PERFORMED SEVERAL MORE GEAR SWINGS WITH NO FURTHER DEFECTS NOTED IAW H400XP MM 32-00-00, 32-10-00 & 12-20-00. 2 H 7 2 4F RT A16SW 2008031900372 20080319 00372 CE 2008 3 19 DXTA200802825 1 20080203 A 3510 MC1016150 OXYGEN MASK CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT LEAKING E DXTA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 690QS 1442 1442 5605090 CAPT'S 02 MASK HOSE DEVELOPED A LEAK WHERE IT ATTACHES TO MASK AND COULD NOT STOP LEAK. INSTALLED NEW O2 MASK. OPS CHECK GOOD IAW MM CH 35-10-01. (K) 2 L 7 2 4F 4 F RT A22CE E00059EN 2008031900374 20080319 00374 EA 2008 3 19 TRAX200800409 1 20080310 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 972EV 7534 AAR - CRACK ON FS 280.0 UPPER ANGLE AT APPROX LBL 13.0 AT RIVET 13333. 2 L 7 2 4F RT A21EA 2008031900376 20080319 00376 EA 2008 3 19 TRAX200800411 1 20080312 A 5720 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 RT DRAG ANGLE I/B OF RIGHT BATTERY RIB IS CRACKED. REMOVED FASTENERS FROM R/H DRAG ANGLE & REMOVED ANGLE AFT OF DRAG ANG LE 15021. REMOVED DRAG ANGLE, LOCATED FASTENER LOCATION ON SERVICEABLE DRAG ANGLE. OK TO INSTALL. INSTALLED NEW SERVICEA BLE DRAG ANGLE IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 2008031900385 20080319 00385 SO 2008 3 19 C2XA08TY034 1 20080316 A 5730 14566208408 SKIN PANEL EMB 145 EMB145EP 3260221 SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14939 145030 TYS - DURING A CURRENT 5A INSPECTION THE RT WING UPPER SKIN I/B GROUND SPOILER WAS FOUND CRACKED. MAINTENANCE REMOVED T HE DAMAGED SKIN, FABRICATED A FILLER, THE DOUBLER TRIPLED DRILL AND COUNTERSUNK. ALODINED, PRIMED AND INSTALLED IAW EC5 740-01141. RESTORED TO THE ORIGINAL FINISH. A/C WILL BE RELEASED AT THE END OF THE CHECK. 2 L 7 2 4F RT T00011AT 2008031900405 20080319 00405 NM 2008 3 19 BB08035 1 20080314 A 3397 WIRE BOEING 767 767201 1385125 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 245AY 23897 PHL - THE FLOOR LEVEL EMERGENCY EXIT STRIP WAS FOUND INOPERATIVE ON THE LEFT AISLE, FROM ROW 12 TO 18. MAINTENANCE REPA IRED THE WIRING AS REQUIRED. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A1NM 2008032000025 20080320 00025 EA 2008 3 20 N6WA0080206 1 20080225 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE EMERGENCY LIGHTS BURNED OUT A N6WA K NONE L NO TEST IN INSP/MAINT 1 CE 03 165GJ 10257 LT WING EMERGENCY EXIT LIGHT INOP. REPLACE BULB. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008032000028 20080320 00028 2008 3 20 DXTA200802838 2 20080204 A 7321 211800262 EEC RAYTHN DH125 HAWKER800XP 7150012 CE LT ENGINE MALFUNCTIONED E DXTA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 867QS 4285 258576 WHEN APPLYING TAKEOFF POWER LT ENGINE LAGS BEHIND R BY APPROX 15-20 PERCENT. REMOVED AND REPLACED LT DEEC WITH AN INSPEC TED DEEC AND OPERATIONAL CHECKED OK IAW LMM CH 76-10-02 AND 72-00-00. 2 L 7 2 4F RT A3EU 2008032000055 20080320 00055 NE 2008 3 20 DXTA200802862 2 20080210 A 7200 3041960 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE RIGHT OVERTEMP E DXTA E C ENGINE SHUTDOWN ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 807QS 4255 5600617 PCEDC0158 RT ENG WOULD NOT ATTAIN POWER WITHOUT EXCEEDING ITT AND N2 LIMITS. TAKE OFF ABORTED. REPLACED RT ENGINE WITH REPAIRED UN IT AND REPLACED RT BDV CONTROLLER WITH REPAIRED UNIT. PERFORMED IAW MM CHAP 75-30-01 AND MM CHAP 71-01-05. PERFORMED ALL ENGINE ADJUSTMENTS AND CHECKS IAW MM CHAP 71-00-00 AND MM CHAP 71-01-05. ALL OPS CHECKS AND LEAK CHECKS GOOD AT THIS TI ME. 2 L 7 2 4F 4 F RT A22CE E00053EN 2008032000068 20080320 00068 CE 2008 3 20 GLBA20061075 1 20080225 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 163 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 122UX UE122 FUSELAGE FRAME CRACKED .5 NR AT FS 163.9 AND STR 9R MAINT REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE FS 163.9 STRINGER 9R IAW SRM REF. 51-70. REPAIR APPROX 5.5 X 2.5 2024-T3 .071. RII INSP COMPLIED IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2008032000080 20080320 00080 NM 2008 3 20 DXTA20082881 1 20080215 A 3260 7049 BULB AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE MLG INDICATOR BURNED OUT E DXTA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 210QS 4560 211 WHEN PUTTING THE LANDING GEAR CONTROL HANDLE DOWN, THE LT MAIN (2) GREEN DOWN INDICATORS FAIL TO BOTH LIGHT. THE BOTTOM LT WILL NOT LIGHT CONSISTENTLY AT GEAR EXTENSION UNLESS YOU WIGGLE THE LIGHT. REMOVED AND REPLACED BOTH BULBS OPS CHECK ED GOOD. REF: MM SEC 32-30-00. 2 L 7 2 4F 4 F RT A50NM E44NE 2008031700071 20080317 00071 WP 2008 3 17 08FDEA00804 1 20080310 A 5310 DOOR FRAME DOUG MD10 MD1010F 3022112 WP CARGO DOORWAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 MCD LOWER JAMB AT SPOOL LOCATION NUMBER 5 SHOWED EVIDENCE OF CRACK IN HOLES A,B,C,D IN WORK 2 L 7 3 4F RT A22WE 2008031700076 20080317 00076 NM 2008 3 17 SWAA081285 1 20080307 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 435WN 32455 DURING SCHEDULED HC2 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008031700078 20080317 00078 WP 2008 3 17 08FDEA00807 1 20080310 A 5310 SUPPORT FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOORWAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 MCD LWR JAMB, NR 1 LATCH SPOOL LWR JAMB SUPPORT FITTING (THRU LIGHTENING HOLE) FWD I/B LEG, CRACKED AND MK'D. 2 L 7 3 4F RT A22WE 2008031700082 20080317 00082 WP 2008 3 17 08FDEA00809 1 20080310 A 5311 707500063 FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 363FE 48263 CENTER CARGO COMPARTMENT DOOR LOWER TORQ BOX AFT LIGHTENING HOLE FWD INBOARD FRAME IS CORRODED REMOVED AND REPLACED FR AME IAW SRM 53-30-00 FIG 2. CUT AND REMOVED FLOORBEAM AND FRAME FOR ACCESS AND REINSTALLED AND REPAIRED IAW SRM 51-33-0 1 AND 53-30-00. 2 L 7 3 4F RT A22WE 2008031700083 20080317 00083 EU 2008 3 17 08FDEA00811 1 20080310 A 5230 A52374160208 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 800 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 DENT WITH CRACK FOUND AT AFT CARGO DOOR SKIN PLATE REPAIR PERFORMED BY CUT OUT THE DAMAGED SKIN AND INSTALLING A DOUBLER IAW/RAS/DAHAM/4024234/2008 ISS A, APPROVED BY EA 6-5230-115241. 2 L 7 2 4F RT A35EU 2008031700094 20080317 00094 WP 2008 3 17 08FDEA00816 1 20080310 A 5330 AFA30311 SKIN DOUG MD10 MD1010F 3022112 WP BS 1789-1796 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 DENTED EXTERNAL FUSELAGE SKIN FROM STA 1789 TO 1796.5; BETWEEN LONGERON 29R AND 30R. BLENDED GOUGED AREA. FOUND TO BE O UT OF LIMITS IAW SRM 53-20-00 VOL I PG 116 FIG 6. GENERATED RFTS N384FE-7-23178. REMOVED DAMAGED AREA IAW SRM 53-20-00 V OL I PG 73 FIG 6. LOCATED, DRILLED & TRIMED IAW SRM 53-20-00 VOL I FIG 6. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. INS TALLED REPAIR IAW SRM 51- 33-01 VOL II. HFEC OF DENT IAW NDT 60-10-001. 2 L 7 3 4F RT A22WE 2008031700096 20080317 00096 WP 2008 3 17 08FDEA00817 1 20080310 A 5330 AFA30311 SKIN DOUG MD10 MD1010F 3022112 WP BS 1801-1802 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 DENTED EXTERNAL FUSELAGE SKIN FROM STA 1801 TO STA 1802.5; BETWEEN LONGERON 29R TO 30R. BLENDED GOUGED AREA. FOUND TO BE OUT OF LIMITS IAW SRM 53-20-11 VOL I PG 116. REMOVED DAMAGE IAW SRM 53-20-00 VOL I. GENERATED RFTS N384FE-6-23179. FABRICATED REPAIR IAW SRM 53-20-00 VOL I FIG 6. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. INSTALLED REPAIR IAW SRM 5 1-33-01 VOL II. HFEC IAW NDT 06-10-001. 2 L 7 3 4F RT A22WE 2008031700099 20080317 00099 EU 2008 3 17 08FDEA00819 1 20080310 A 5510 ALC705220 ATTACH ANGLE AIRBUS 300 A300F4605R 3930327 EU HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 2ND INBD LEADING EDGE SECTION ON THE RT HORIZONTAL STABILIZER; "UPPER OUTBD ATTACH ANGLE" IS CRACKED. REMOVED CRACKED A NGLE IAW SRM 51-31-01 VOL II PG 1. FORMED NEW ANGEL IAW DWG ALC 07052 REV G. LOCATED; DRILLED & DEBURRED NEW ANGLE IAW S RM 51-31-01 VOL II PG 1. ALODINED & PRIMED NEW ANGLE IAW SRM 51-21-01 VOL II PGS - 18. INSTALLED ANGLE IAW SRM 51-33-01 PG 1 & 51-35-01 VOL II PG 1. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008031700101 20080317 00101 WP 2008 3 17 08FDEA00822 1 20080310 A 5414 AUB7120501 PANEL DOUG MD10 MD1010F 3022112 WP NR 3 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 NR 3 PYLON PANEL 488CL IS CRACKED AT THE CUTOUT. WELD REPAIRED CRACKS IAW DWG AUB 7120 AND DPS 4.801 AND DPS 10.225. 2 L 7 3 4F RT A22WE 2008031700102 20080317 00102 EU 2008 3 17 08FDEA00824 1 20080310 A 5315 FLOORBEAM AIRBUS 310 A310203 3930313 EU CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 CORROSION IS ON THE BOTTOM OF THE FLOORBEAM AT FRAME 47; LBL 103CM IN FWD PIT. FOUND TO BE OUT OF LIMITS IAW SRM 52-30 -00. REMOVED EDGE MEMBER IAW SRM 51-40-21. REMOVED SEAL RETAINER IAW SRM 51-40-21. RECEIVED NEW EDGE MEMBER IAW SRM 52-31-00. FABBED DOUBLER AND FILLER IAW SRM 52-30-00. INSTALLED DOUBLER & FILLER IAW SRM 51-40-21. INSTALLED EDGE MEMB ER & SEAL RETAINER IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008031700105 20080317 00105 EU 2008 3 17 08FDEA00827 1 20080310 A 5340 A5341076720000 ATTACH ANGLE AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT CARGO PIT; FWD BULKHEAD AT FRAME 54; THE CEILING PANEL ATTACH ANGLE IS CORRODED AT RBL 166 CM 65. REMOVED CORROS ION IAW SRM 51-74-10. ORIGINAL MATERIAL THICKNESS .098. REMAINING MATERIAL .043. REMOVED .055, OUT OF LIMITS IAW SRM 53- 10-00. REMOVED ANGLE IAW SRM 51-40-21. FABBED NEW ANGLE IAW DWG A53410767. ALODINED IAW SRM 51-21-10. PRIMED AND PAINTE D IAW SRM 51-23-10. PART MARKED IAW GMM 7-0-1001. INSTALLED ANGLE IAW SRM 51-40-21. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008031700112 20080317 00112 EU 2008 3 17 08FDEA00834 1 20080310 A 5313 A53970701215 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT STRINGER 45R IS CORRODED BETWEEN FRAMES 54.2 AND 54.3. REMOVED CORROSION IAW SRM 51-74-10. ORIGINAL THICKNESS WAS 0.110. REMAINING MATERIAL 0.105. WITHIN LIMITS IAW SRM 53-10-00. ALODINED IAW SRM 51-21-00. PRIMED & PAINTED IAW SR M 51-23-00. 2 L 7 2 4F RT A35EU 2008031700113 20080317 00113 EU 2008 3 17 08FDEA00835 1 20080310 A 5330 A5397070320000 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT LOWER FUSELAGE SKIN IS CORRODED AROUND THE DRAIN HOLE AREA AT STR 57 BETWEEN FRAMES 54.1 AND 54.2. REMOVED CORR OSION IAW SRM 51-74-10. ORIG. MAT. THICKNESS IS .196 IAW DWG. A53970182. REMOVED .023. REMAINING MAT. OF .173 IS WITHIN LIMITS IAW SRM 53-10-00. ALODINED IAW SRM 51-21-10. PRIMED & PAINTED IAW SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008031700114 20080317 00114 EU 2008 3 17 08FDEA00837 1 20080310 A 5313 A5397452723800 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT LOWER FUSELAGE STRINGER 51R HAS CORROSION IN THE AREA ON THE STRINGER BETWEEN FRAMES 60 AND 61. REMOVED CORROSI ON FROM STRINGER IAW SRM 51-74-10. ORIGINAL MATERIAL THICKNESS 0.110. MATERIAL REMOVED 0.013. REMAINING MATERIAL 0.09 7. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. REMOVED STRINGER IAW SRM 53-10-10. FABBED REPAIR STRINGER & COUPLINGS I AW SRM 51-21-10. ALODINED REPAIR STRINGER & COUPLINGS IAW SRM 51-21-10. PRIMED & PAINTED REPAIR STRINGER & COUPLINGS I AW SRM 53-23-10. INSTALLED REPAIR STRINGER & COUPLINGS IAW SRM 53-10-14. 2 L 7 2 4F RT A35EU 2008031700116 20080317 00116 EU 2008 3 17 08FDEA00840 1 20080310 A 5313 A5397814622600 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT STR 56R HAS CORROSION ON THE LOWER ANGLE AT FRAME 69. REMOVED FASTENERS IAW SRM 51-40-21. REMOVED CORROSION IA W SRM 51-74-10. ORIGINAL THICKNESS 0.079. REMAININGMATERIAL 0.073. WITHIN LIMITS IAW SRM 53-10-00. ALODINED IAW SRM 51-21-00. PRIMED IAW SRM 51-23-00. INSTALLED FASTENERS IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008032000156 20080320 00156 SO 2008 3 20 LR7A08037 1 20080227 A 5310 3390108R RIB LKHEED 382 382G 526414U SO BS 132 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2299 5025 DURING SCHEDULED C-7 CHECK, PER JOB CARD HC5311, FOUND COCKPIT RT RIB WITH CRACKS AT FS 132, WL 210-220, RBL61. REPAIR ACCOMPLISHED BY REPLACING RIB IAW SMP583 CHAP 51-60 AND 51-70 WITH REFERENCE TO DWG 339010. 2 H 7 4 4T A1SO 2008032000157 20080320 00157 SO 2008 3 20 LR7A08038 1 20080227 A 5320 33911826L27L INTERCOSTAL LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2299 5025 DURING SCHEDULED C-7 CHECK, PER JOB CARD HC5211, FOUND RAMP DOOR INTERCOSTAL CRACKED AT RS6-8, BL0-LBL4. REPAIR ACCOMPL ISHED BY FABRICATION AND REPLACING THE BULKHEAD WEB/SUPPORT ANGLE IAW SMP583 CHAP 51-70 WITH REFEERENCE TO DWGS 339118 A ND 375137. 2 H 7 4 4T A1SO 2008032000165 20080320 00165 NM 2008 3 20 08FDEA00908 1 20080312 A 5753 ARC27361 SKIN DOUG MD11 MD11F 3023600 NM LT WING TE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 521FE 48478 LEFT WING, INBOARD FLAP LOWER SURFACE FOUND GOUGE AT XIFH 191. REPAIRED AS PER SRM 57-10-00 FIG.2 VOL.I. REPAIR CLASSIF IED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032000166 20080320 00166 NM 2008 3 20 08FDEA00909 1 20080312 A 5311 AFA00273 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 521FE 48478 MAIN DECK FRAME AT RT STA 1661 L12 FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIG. 1 VOL.I. INITIAL INSPECTION AT 145 00 CYCLES AND REPETITIVE INSPECTION AT 9500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG. 1 VOL. I. REPAIR CLASSIFIE D AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032000167 20080320 00167 NM 2008 3 20 08FDEA00910 1 20080312 A 5311 AFA00283 FRAME DOUG MD11 MD11F 3023600 NM BS 1681 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 521FE 48478 MAIN DECK FRAME AT RT STA 1681 L12 FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIG. 1 VOL.I. INITIAL INSPECTION AT 145 00 CYCLES AND REPETITIVE INSPECTION AT 9500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032000175 20080320 00175 SO 2008 3 20 LR7A08042 1 20080311 A 5311 LS4325 FRAME LKHEED 382 382G 526414U SO FS 814 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 652 4763 DURING SCHEDULED B-1 CHECK, PER JOB CARD HB5302, FOUND CABIN BULKHEAD INBD FRAME CRACKED AT FS 814, WL176, RBL 67. REPA IR ACCOMPLISHED IAW SMP583 FIG 53-50-14. 2 H 7 4 4T A1SO 2008032000176 20080320 00176 EU 2008 3 20 F3LA200800091 1 20080306 A 5320 D536700920030 THRESHOLD AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON BOTH ENDS OF THE R-2 DOOR THRESHOLD STRIP. MAINTENANCE REMOVED AND REPLACED THE THRESHOLD STRIP IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-42-12 PB 401. UPON COMPLETION O F THE REPLACEMENT, THE NEW THRESHOLD STRIP WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032000178 20080320 00178 NE 2008 3 20 MASA200800159 2 20080219 A 7320 4128T48G09 ROD CNDAIR CL600 CL6002D24 1390016 EA GE CF34 CF348C5 30050 NE NR 1 ENGINE DEFECTIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 933LR 142 15033 NR 1 ENGINE, S/N 194271, EXPERIENCED ITT EXCEEDANCE OF 1031C FOR 2.7 SECONDS DURING START. BORESCOPE C/W WITH NO DEFECT S. MX REPLACED MASTER AND SLAVE VG TORQUE RODS. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008032000181 20080320 00181 WP 2008 3 20 UPS08851822 1 20080301 A 5730 SKIN DOUG DC8 DC873F 302199F WP LWS 598 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 POSSIBLE CRACK AT DRAIN HOLE, LT WING OB LE IB SECTION LOWER SURFACE NEAR STA XFS 598. STOP DRILLED CRACK, FAB AND INSTALLED REPAIR DOUBLER IAW SRM 57-3-1, E O DC85720-4087-B, 51-1-8. 2 L 7 4 4F RT 4A25 2008032000182 20080320 00182 WP 2008 3 20 UPS08851824 1 20080301 A 5340 2649946N FITTING DOUG DC8 DC873F 302199F WP BS 200 L21R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 MAIN CABIN STA 200 LONG 21R, CUSP FITTING IS CRACKED. REMOVED AND REPLACED CUSP FITTING. 2 L 7 4 4F RT 4A25 2008032000184 20080320 00184 WP 2008 3 20 UPS08851840 1 20080221 A 5511 SPAR DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 LT HORIZ STAB REAR SPAR WEB CRACKED AT FASTENER HOLE INBD OF INBD HINGE. REPAIRED HORIZ STAB REAR SP AR WEB CRACK AT FASTENER HOLE, INBD OF INBD HINGE IAW SRM 55-02-00 FIG 004, SRM 55-02-00 FIG 002 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2008032000190 20080320 00190 NM 2008 3 20 UPS08M51803 1 20080226 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 12 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M, BUSHING O.D. .946 BORE I.D. .944. 2 L 7 3 4F RT A22WE 2008032000192 20080320 00192 NM 2008 3 20 2008UALA01172 1 20080229 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 FOUND CEILING EMERGENCY LIGHT ABOVE LAV 100 INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032000194 20080320 00194 NM 2008 3 20 2008UALA01178 1 20080304 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 FOUND EMERGENCY LIGHT INOP, UPPER DECK AFT LT. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032000198 20080320 00198 NM 2008 3 20 2008UALA01182 1 20080304 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 FOUND WALL EEL INOP, BETWEEN MID LAVS. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032000200 20080320 00200 NM 2008 3 20 2008UALA01184 1 20080304 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 FOUND EMERGENCY LIGHT INOP, RT OVERWING 3RD AFT ASSY. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032000201 20080320 00201 NM 2008 3 20 2008UALA01185 1 20080303 A 3350 D31865107 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 829UA 1211 EPSU EXT LOAD EMER R. FOUND INTERNAL SHORT WITHIIN SLIDE PACK. REPLACE RT OVERWING SLIDE AND PSU 12WL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032000203 20080320 00203 EU 2008 3 20 08FDEA00769 1 20080306 A 5544 A5547020000000 STRAP AIRBUS 310 A310203 3930313 EU RUDDER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RUDDER L/E PANEL NR 326 EL BRIDGING STRAPS ARE CORRODED UNDER THE NUT PLATES. REMOVED AND REPLACED THE BRIDGING STRAPS REFERENCE A310-200 SRM 51-40-21; PARA 5. 2 L 7 2 4F RT A35EU 2008032100005 20080321 00005 EU 2008 3 21 08FDEA00784 1 20080307 A 5510 A5517610000300 TIP CAP AIRBUS 310 A310203 3930313 EU HORIZONTAL STAB ERODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT HORIZONTAL STABILIZER TIP IS ERODED AT THE LOWER L/E. REPAIRED LT HORIZONTAL STAB TIP BY REMOVING PREVIOUS REPAIR AN D APPLING A WET LAY-UP FIBERGLASS REPAIR AND REFINISHING AREA IAW SRM 55-14-11. 2 L 7 2 4F RT A35EU 2008032100006 20080321 00006 EU 2008 3 21 08FDEA00785 1 20080307 A 5532 A5537247000000 PANEL AIRBUS 310 A310203 3930313 EU VERTICAL STAB BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 VERTICAL STABILIZER PANEL NR 325 CR IS BROKEN. REMOVED DAMAGE, VERIFIED MAT I.D. APPLIED REPAIR PLYS, CURED. RESTORED F INISH IAW SRM 55-33-13 & 51-77-00. 2 L 7 2 4F RT A35EU 2008032100009 20080321 00009 EU 2008 3 21 08FDEA00793 1 20080307 A 5280 SKIN AIRBUS 310 A310203 3930313 EU RT MLG DOOR DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT MAIN LANDING GEAR DOOR EXTERNAL SKIN HAS DELAMINATION 34" FROM THE FWD END. REMOVED DAMAGE AT THE TWO EACH AREAS. P ERPARED AREA FOR REPAIR PLY LAY UP. LAYED UP, BAGGED & CURED REPAIR PLYS. APPLIED & CURED ROSIN COAT, RESTORED FINISH I AW SRM 52-81-10 & 51-77-10 PG 209; WET LAY UP REPAIR. 2 L 7 2 4F RT A35EU 2008032100010 20080321 00010 EU 2008 3 21 08FDEA00794 1 20080307 A 5280 SKIN AIRBUS 310 A310203 3930313 EU LT MLG DOOR DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT MAIN LANDING GEAR DOOR EXTERNAL SKIN HAS DELAMINATION 36" FROM THE FWD END. REMOVED THE DAMAGE. CLEANED & PREPPED FO R THE REPAIR. POTTED AREA; CURED; SANDED & APPLIED REPAIR PLYS & VAC BAGGED. CURED, SANDED PERFORMED A RESIN SWEEP. CURE D & SANDED SMOOTH IAW SRM 51-77-12 FIG 202. RESTORED FINISH IAW SRM 51-75-10. 2 L 7 2 4F RT A35EU 2008032100016 20080321 00016 NM 2008 3 21 2008UALA01203 1 20080304 A 2560 GIRT BAR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R1 DOOR DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 855UA 1737 DOOR 1R AFT GIRT BAR FITTING STOP LEVER MECHANISM STUCK IN DOWN POSITION. FOUND DIRTY FITTING. CLEANED AND LUBED FITTI NG. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032100017 20080321 00017 NM 2008 3 21 2008UALA01204 1 20080304 A 3350 5650033 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 855UA 1737 BATTERY FAULT LIGHT ILLUMINATED ON AFT CABIN EMERGENCY LIGHT POWER SUPPLY UNIT. FOUND THE BATTERY FAILED. REPLACED BAT TERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032100018 20080321 00018 NM 2008 3 21 2008UALA01205 1 20080304 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE RT OVERWING EEL NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 855UA 1737 RT OVERWING EXIT EMERGENCY LIGHT POWER SUPPLY UNIT WILL NOT TEST. REPLACED POWER SUPPLY UNIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032100026 20080321 00026 2008 3 21 2008UALA01225 4 20080305 A 2565 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR SLIDE MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 503UA 24624 DOOR NR 4 EMERGENCY ESCAPE SLIDE LAMP NOT ILLUMINATING, CHANGE LAMP, NO HELP. PERFORMED OPS TESTS OF EMER DOOR 4L AND S LIDE, ALL OPS CHECKS WERE NORMAL.. NO REPEATS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100027 20080321 00027 NM 2008 3 21 2008UALA01226 1 20080304 A 3597 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OXYGEN MASK SHORTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 CAPT O2 MASK MIC INOP. FOUND SHORTED WIRING INSIDE O2 MASK. REPLACED CAPT O2 MASK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100028 20080321 00028 NM 2008 3 21 2008UALA01227 1 20080305 A 2710 251N10022 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AILERON PCA LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 545UA 25323 RT OTBD AILERON INBD PCA ACTIVE LEAK 50 DROPS PER MINUTE. FOUND LEAKING ROD SEAL ON PCA. REPLACED RT OUTBOARD AILERON I NBOARD PCA. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100034 20080321 00034 NM 2008 3 21 2008UALA01254 1 20080306 A 5210 LIFTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 4R WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 577UA 26693 DOOR 4R IS HARD TO ARM. FOUND AFT LIFTER ASSY WORN. FOUND METAL BURRS ON SLIDER. FILED OFF BURRS AND CLEANED SLIDERS, D OOR ARMS AND DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100041 20080321 00041 NM 2008 3 21 08FDEA00810 1 20080310 A 5320 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 MAIN DECK CARGO DOOR LOWER JAMB BACKUP FITTING FOUND CRACKED. REMOVED AND REPLACED WITH A FABRICATED FITTING AS PER SR M 51-33-01 VOLUME II. FITTING FABRICATED AS PER EA 1-5300-112586, REPAIR CLASSIFIED AS MINOR PER GM 6-2-100. 2 L 7 3 4F RT A22WE 2008031700121 20080317 00121 NM 2008 3 17 SWAA081300 1 20080309 A 5330 6545779 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN WORN UNDER DORSAL FIN BETWEEN BS 857 TO BS 887. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008031700122 20080317 00122 EU 2008 3 17 08FDEA00843 1 20080310 A 5311 A53973178276 FRAME AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT FUSELAGE FRAME HAS CORROSION ON THE WEB AT FRAME 64 BETWEEN STR 49L AND 50L. REMOVED CORROSION IAW SRM 51-74-10 . FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. FORMED ANGLE, HEAT TREATED ANGLE IAW TPS 1003; REV A. DRILLED UP PARTS ; ALODINED, PRIMED & TOP CAOTED PARTS IAW SRM 51-40-44; 51-21-10 & 51-23-10. INSTALLED PARTS IAW SRM 53-10-13. ALSO APPLIED TOP COAT PN PARTS IAW SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008031700123 20080317 00123 NM 2008 3 17 SWAA081337 1 20080310 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300232 20080313 00232 NM 2008 3 13 SWAA081219 1 20080303 A 2611 100064901 SMOKE DETECTOR BOEING 737 7373H4 1384600 NM AFT CARGO BAY INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, AFT CARGO COMPARTMENT RT FWD SMOKE DETECTOR INOP. REMOVED AND REPLACED SMOKE DETECTOR PER MM. 2 L 7 2 4F RT A16WE 2008031300268 20080313 00268 NM 2008 3 13 SWAA081227 1 20080304 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031300276 20080313 00276 NM 2008 3 13 SWAA081236 1 20080304 A 5311 6545808 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294, STR 12L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008031300280 20080313 00280 NM 2008 3 13 SWAA081241 1 20080304 A 5322 6546529 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 500, RBL 4. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008031300299 20080313 00299 NE 2008 3 13 MASA200800181 2 20080302 A 7261 6087T04P09 SCAVENGE PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT ENGINE MALFUNCTIONED A MASA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SW 07 75995 7361 ASH 7423 MDT-ORD. EN ROUTE TO ORD AIRCRAFT DIVERTED TO PIT DUE TO LT ENG SHUTDOWN IN FLIGHT. MX CHANGED LUBE/SCAV PUMP , MASTER CHIP SEALS, OP AND LEAD CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2008031300303 20080313 00303 NM 2008 3 13 DLM88080314 1 20080216 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 1048-1053 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 961DL 49980 EXFOLIATION CORROSION ON RT CUSP WEB BETWEEN STA 1048 TO 1053, TASK CARD 58-53313. REPAIRED PER ERA 398191-14MA REV ORG ON N/R T0083346 AT HMV-3 IN GDL. 2 L 7 2 4F RT A6WE 2008031300307 20080313 00307 NM 2008 3 13 DL757080320 1 20080306 A 3397 CONNECTOR BOEING 757 757232 1384965 NM EMERGENCY LIGHTS DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 618DL 22908 TWO RED EMERGENCY LIGHT AT 26FED INOP. REPLACED CONNECTOR UNDER SEAT 26F, OP OK. 2 L 7 2 4F RT A2NM 2008031300360 20080313 00360 NM 2008 3 13 SWAA081260 1 20080305 A 2530 41600019 COFFEEMAKER BOEING 737 7377H4 1384404 NM AFT GALLEY LEAKING A SWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 217JC 34232 AIR TURNBACK. AFT GALLEY SMOKE, STEAM, DRAINING WATER. FOUND AFT NR 2 COFFEEMAKER LEAKING. REMOVED AND REPLACED COFFE EMAKER PER MM. 2 L 7 2 4F RT A16WE 2008031300376 20080313 00376 NM 2008 3 13 SWAA081251 1 20080305 A 5523 65C35943 BEARING BOEING 737 7373H4 1384600 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED HC1 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING AND BEA RING PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300384 20080313 00384 SO 2008 3 13 RAIA00803003 1 20080304 A 3610 FILTER EMB 145 EMB145LR 3260212 SO BLEED AIR SYS DIRTY A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 835HK 145670 FLT 7887 - ORD - BLEED NR 2 EICAS MESSAGE DURING CLIMBOUT. MAINTENANCE CLEANED THE FAN AIR VALVE FILTER. SYSTEM OPS CH ECKED GOOD. 2 L 7 2 4T RT T00011AT 2008031300402 20080313 00402 WP 2008 3 13 08FDEA00763 1 20080306 A 5512 ALC7065541 SKIN DOUG MD10 MD1010F 3022112 WP HORIZONTAL STAB CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 LEFT HORIZONTAL SATBILIZER REAR SPAR PANEL 334 SB IS CHAFED ON THE INTERIOR SKIN FAYING SURFACE XE 306. REMOVED FINISH AT INTERIOR OF PANEL IAW SRM 51-21-01, VOL I. CHAFED AREA FOUND TO BE WITHIN LIMITS OF FIGURE 1-A. SRM 55-00-01 VOL I. APPLIED SURFACE PROTECTOR IAW SRM 51-21-01 VOL II. APPLIED SURFACE FINISH IAW SRM 51-21-01 VOL II. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008031300417 20080313 00417 EU 2008 3 13 08FDEA00791 1 20080307 A 5347 CARGO TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 MAIN CARGO COMPARTMENT AT FRAME 46 BETWEEN SEAT TRACK -Y 450 AND -Y 953 TIE DOWN TRACK IS CRACKED. REMOVED AND REPLACED TIE DOWN TRACK IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008032100042 20080321 00042 WP 2008 3 21 08FDEA00815 1 20080310 A 5330 AGA31025 SKIN DOUG MD10 MD1010F 3022112 WP BS 1909 BULGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 BULGING AT EXTERNAL FUSELAGE SKIN; RT STA 1909; LONGERON 41R TO 42 R. FOUND TO BE OUT OF LIMITS IAW SRM 53-20-00; VOL I; PG 116. DRILLED OUT BULGED AREA AT .250 & REPAIRED IAW SRM 53-20-00; FIG 13; SHEET 1; VOL I. 2 L 7 3 4F RT A22WE 2008032100043 20080321 00043 WP 2008 3 21 08FDEA00820 1 20080310 A 5414 AUB7120501 FAIRING DOUG MD10 MD1010F 3022112 WP NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 NR 1 PYLON PANEL 438CL IS CRACKED. REPAIRED CRACKS IAW DRAWING AIB7120-501. 2 L 7 3 4F RT A22WE 2008032100044 20080321 00044 WP 2008 3 21 08FDEA00823 1 20080310 A 5420 AUL7000515 DRAIN DOUG MD10 MD1010F 3022112 WP NR 1 NACELLE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 NR 1 ENGINE PYLON AFT FAIRING LOWER PANEL 438EL HAS A CHAFED DRAIN TUBE. WELDED CHAFED AREA IAW DPS 10.225. MINOR REP AIR. 2 L 7 3 4F RT A22WE 2008032100045 20080321 00045 EU 2008 3 21 08FDEA00838 1 20080310 A 5330 SKIN AIRBUS 310 A310203 3930313 EU BS 3355 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT LOWER FUSELAGE SKIN IS CORRODED AT FRAME 62; S56R. REMOVED CORROSION IAW SRM 51-74-10; CHECKED LIMITS IAW SRM 53-17-12. FOUND TO BE WITHIN LIMITS IAW SRM 53-10-12. ALODINED IAW A310 SRM 51-21-10. PRIMED AND PAINTED BOTH IAW A3 10 SRM 51-23-10. MINOR REPAIR 2 L 7 2 4F RT A35EU 2008032100046 20080321 00046 EU 2008 3 21 08FDEA00839 1 20080310 A 5313 A53974527242 STRINGER AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT STR 49R HAS CORROSION ON THE LOWER RADIUS 6" AFT OF FRAME 65. REMOVED CORROSION IAW SRM 51-74-10. REMOVED FA STENERS TO F.O.M. ORIGINAL MATERIAL THICKNESS 0.092. MATERIAL REMOVED 0.004. MATERIAL REMAINING 0.088. FOUND TO BE WI THIN LIMITS IAW SRM 53-10-00. ALODINED IAW SRM 51-21-10. PRIMED & PAINTED IAW SRM 51-23-10. INSTALLED FASTENERS IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008032100053 20080321 00053 WP 2008 3 21 08FDEA00874 1 20080311 A 5310 ADA0010 SHEAR TIE DOUG MD10 MD1010F 3022112 WP BS 824 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 FWD LOWER CARGO PIT BILGE SHEAR TIE IS CORRODED AT BS 824 BETWEEN STR 51L AND STR 52L. REMOVED CORROSION IAW SRM 51-21- 01; VOL II; PG 28. ORIGINAL THICKNESS .071 IAW SRM 53-13-01; VOL III; FIG 8A AND SRM 51-10-02; VOL II. REMAINING THICK NESS .068; FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01; FIG 1; PG 4B. UT GAUGE NR 78224Q. ALODINED AND PRIMED IAW SRM 51-21-01; VOL II; PGS 21 AND 24. APPLIED TOP COAT IAW SRM 51-21-02; VOL II; PG 1. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008032100054 20080321 00054 WP 2008 3 21 08FDEA00875 1 20080311 A 5320 ADA0010 CHANNEL DOUG MD10 MD1010F 3022112 WP BS 824 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 FWD LOWER CARGO PIT BILGE FRAME J-CHANNEL IS CORRODED AT BS 824 S51R. REMOVED CORROSION IAW SRM 51-21-01; VOL II; PG 28 . ORIGINAL THICKNESS .071 IAW SRM 53-13-01; VOL III; FIG 8A AND SRM 51-10-02; VOL II. REMAINING THICKNESS .069; FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01; VOL II; FIG 1A; PG 4B. UT GAUGE NR T8224Q. ALODINED AND PRIMED IN REF TO SRM 51 -21-01; VOL II; PGS 21 AND 24. APPLIED TOP COAT IN REF TO SRM 51-21-02; VOL II; PG 1. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008032100057 20080321 00057 WP 2008 3 21 08FDEA00880 1 20080311 A 5320 ADA0145 SUPPORT DOUG MD10 MD1010F 3022112 WP BS 959 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 FWD CARGO PIT BILGE AREA; DRAIN PAN SUPPORT ANGLE LOWER SURFACE AND NUT PLATES HAVE CORROSION ABOVE FRAME AT FS 959, S49 -51L. REMOVED CORROSION IAW SRM 51-21-01; VOL II; PG 28. THE ORIGINAL THICKNESS IS .040 IAW DWG ADA0145 REV J; THE MAT ERIAL REMOVED IS .002; MATERIAL REMAINING IS .038. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01; VOL II; FIG 1B. TREAT AND PRIMED IAW SRM 53-21-01; VOL II; PGS 21 AND 24; THEN INSTALLED NUT PLATES IAW SRM 51-33-01; VOL II; PG 2. 2 L 7 3 4F RT A22WE 2008032100058 20080321 00058 WP 2008 3 21 08FDEA00881 1 20080311 A 5320 ADA0145 SUPPORT DOUG MD10 MD1010F 3022112 WP BS 939 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 FWD CARGO PIT BILGE AREA FOUND CORROSION ON THE DRAIN PAN SUPPORT ANGLE AROUND THE NUT PLATES ABOVE THE FRAME AT FS 939; STR 49L/R. REMOVED CORROSION IAW SRM 51 21-01; VOL II; PG 28. THE ORIGINAL THICKNESS IS .040 IAW DWG ADA 0145 REV J. THE MATERIAL REMOVED IS .003. THE MATERIAL REMAINING IS .037. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01; VOL II; FI G 1B. TREAT AND PRIMED IAW SRM 53-21-01; VOL II; PGS 21 AND 24; THEN INSTALLED THE NUT PLATES IAW SRM 51-35-01; VOL II; PG 2. 2 L 7 3 4F RT A22WE 2008032100059 20080321 00059 EU 2008 3 21 08FDEA00891 1 20080311 A 5411 2210081181 FRAME AIRBUS 310 A310203 3930313 EU NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 STRINGER PANEL 485AL HAS A CRACKED FRAME ON THE LT SIDE AT FWD MID SKIN. REMOVED CRACKED FRAME; RECEIVED NEW FRAME P/N 221-0081-181; PO 611742.3. LOCATED HOLES IAW SRM 51-40-40 AND INSTALLED IAW SRM 51-40-31 PARA 6. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008032100061 20080321 00061 WP 2008 3 21 08FDEA00900 1 20080312 A 5313 ADA3064 STRINGER DOUG MD10 MD1010F 3022112 WP BS 809 S52L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 FWD CARGO PIT BILGE; STRINGER 52 IS CORRODED AT BS 809. REMOVED CORROSION IAW SRM 51-21-01; VOL II; PG 26. WITHIN L IMITS IAW SRM 53-00-01; VOL I; FIG 1A. ORIGINAL THICKNESS IS .071. MATERIAL LOSS IS .006. REMAINING THICKNESS IS .06 5. ALODINED; PRIMED AND TOP COATED IAW SRM 51-21-01; VOL II; PGS 19; 21 AND 24. MINOR REPAIR 2 L 7 3 4F RT A22WE 2008032100062 20080321 00062 EU 2008 3 21 08FDEA00901 1 20080312 A 5330 NOA6014 DOUBLER AIRBUS 310 A310203 3930313 EU CORRODED A FDEA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 25 425FE 264 FWD LOWER CARGO PIT BILGE DOUBLER IS CORRODED BETWEEN STR 51L AND STR 52 L. 2 L 7 2 4F RT A35EU 2008032100063 20080321 00063 NM 2008 3 21 2008UALA01280 1 20080308 A 5753 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT TE FLAP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 LEFT INBOARD MAIN FLAP UPPER SURFACE CONTACTING NR 5 SPOILER, PREVIOUS REPAIR GOUGED. ACCOMPLISHED MAJOR REPAIR 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100071 20080321 00071 NM 2008 3 21 2008UALA01333 1 20080310 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 DOOR 1R INTERIOR STRUCTURE IS GOUGED AT UPPER HINGE ARM AREA. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031900326 20080319 00326 NM 2008 3 19 USAA920080602 1 20080302 A 5320 D5361018300200 SUPPORT ANGLE AIRBUS A319 A319132 3930340 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801AW 889 SAL - MAJOR REPAIR - C7 CHECK - CRACKED CABIN SUPPORT ANGLE, BS 605 / FR 12, -Y940. REPLACED CABIN SUPPORT ANGLE, BS 60 5 / FR 12, -Y254 TO -Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008032000013 20080320 00013 CE 2008 3 20 DXTA200802828 1 20080202 A 3222 STRUT CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE NLG UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 346QS 6800013 AFTER TAKEOFF UNABLE TO MOVE GEAR HANDLE TO UP POSITION. SHORTLY AFTER TAKE OFF WOW MISCOMPARE CAS ILLUMINATED, 5 MINUT ES LATER EXTINGUISHED THEN UNABLE TO MOVE HANDLE UP BUT LT MAIN REMAINED DOWN W/RED UNLOCK. CHECKED NITROGEN PRESSURE IN NLG STRUT AND FOUND NONE. DISASSEMBLED, CLEANED, INSPECTED NR REPACKED NLG STRUT WITH NEW SEALS AND GASKETS IAW CHAPTER 32-20-00 OF THE CE-680 MM. SERVICED; OPS CHECK, LEAK CHECK SATISFACTORY. 2 L 7 2 4F 4 F RC T00012WI E35NE 2008032000037 20080320 00037 2008 3 20 U0GA118933 4 20080218 A 3442 40008330208 DISPLAY BELL 212 212 1181420 SW WX RADAR ODOR E U0GA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 03 508EH 30908 WX RADAR DISPLAY STARTED FLICKERING AND GOING BLACK. RADAR TURNED OFF. CIRCUIT BREAKER PULLED AFTER ODOR OF ELECTRICAL BURN WAS NOTICED. 1 G 7 1 4U H4SW 2008032000045 20080320 00045 WP 2008 3 20 ASMF200802008 1 20080226 A 3250 4916688AS04126 CONTROL CABLE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE NLG BROKEN W ASMF D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 23 754RA 49641 DURING TAXING, CAPTAIN REPORTED STEERING FAILURE. MAINT CHECKED THE STEERING BY-PASS, FINDING ALL CORRECT; THEN, THE STE ERING VALVE WAS CHECKED, DETECTING THE STEERING CONTROL CABLE BROKEN, AC WAS SENT TO THE HANGAR AND THE CONTROL CABLE WA S REPLACED AND ADJUSTED IAW MM 32-50-00 AND 32-50-01, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 2008032000048 20080320 00048 CE 2008 3 20 DXTA200802855 1 20080209 A 3230 SPRING CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE UPLOCK ACTUATOR WEAK E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 671QS 5605071 AFTER TAKEOFF, THE GEAR UNSAFE LIGHT ILLUMINATES AFTER THE GEAR HANDLE IS PLACED IN THE UP POSITION. THE HYD PRESS AND S TAB MISCOMPARE ANNUNCIATOR ALSO ILLUMINATE. PULLING THE HYD CONT CB, DOES NOT DROP ANY LANDING GEAR ASSEMBLIES OR EXTING UISH THE UNLOCK LIGHT. TROUBLESHOT TO THE RT UPLOCK ACTUATOR, SPRING TOO WEAK TO ENGAGE HOOK FULLY. REMOVED AND REPLAC ED SPRING. OPS CHECK GOOD IAW MM CH 32-30-05 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032000060 20080320 00060 CE 2008 3 20 DXTA200802867 1 20080210 A 2130 99100956 PRESSURE SWITCH CESSNA 560 560XL 2076702 CE CABIN PRESSURE MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 651QS 5478 5605251 CAB ALT 10, 000 CAME ON AT 10,500 FEET WITH MASTER WARNING. REMOVED CABIN ALTITUDE PRESSURE SWITCH. REPLACED WITH NEW SW ITCH. OPERATIONAL CHECK GOOD. WORK IAW MM 21-30-00. 2 L 7 2 4F RT A22CE 2008032000066 20080320 00066 CE 2008 3 20 DXTA20082873 1 20080213 A 3240 215297 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT MLG WEAK E DXTA O OTHER O OTHER LD LANDING 1 GL 07 322QS 452 452 5600421 BOTH LT BRAKES REQUIRE MORE PRESSURE THAN THE RT. REMOVED AND REPLACED LT AND RT BRAKE ASSY'S IAW MM CH. 32-42-00. BLED BRAKES IAW MM CH 32-42-00. TAXI CHECK GOOD. LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2008032000101 20080320 00101 EU 2008 3 20 08FDEA00893 1 20080311 A 5751 WEDGE AIRBUS 310 A310203 3930313 EU RT AILERON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT OUTBD AILERON T/E WEDGE IS CRACKED AND THE AFT EDGE IS SEPARATED. THIS SDR WAS OPENED FOR AIRCRAFT N425FE INSTEAD OF AIRCRAFT N365FE IN ERROR. SDR 08-0895 HAS BEEN INITIATED TO ADDRESS THE DISCREPANCY DOCUMENTED ON NON-ROUTINE N00026 T HAT WAS WRITTEN AGAINST AIRCRAFT N365FE. 2 L 7 2 4F RT A35EU 2008032000106 20080320 00106 WP 2008 3 20 NWAA080889954 1 20080306 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 921RW 47164 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROWS 14 THROUGH 17 WERE INOPERATIVE. THE RI GHT AFT OVERWING HATCH EXIT SIGN POWER PACK WAS REPLACED. FUNCTIONAL CHECKS WERE GOOD AND THE AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F A6WE 2008032000113 20080320 00113 SW 2008 3 20 WGEA200800045 1 20080307 A 2710 AILERON ECLIPS EA500 ECLIPSEEA500 3350000 SW OUT OF RIG E WGEA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 142DJ 000056 COMPLIED WITH ECLIPSE TSR 27-030508G REV C. NO DEFECTS NOTED. PERFORMED AILERON FRICTION TEST, AILERON TENSION TEST AS PRESENTED IN SEC 12.3, PAGE 35 OF FLT CONTROL RIGGING SPEC. 27-109846 REV. 5, PERFORMED MEASUREMENT OF AILERON SKIN CON TOUR EAC AERO 07-500 015 SDR REV C. REFERENCE LOGBOOK PAGE 0901 ITEM 1. EVAL FLIGHT UNSATISFACTORY, AIRCRAFT STILL REQ UIRES EXCESSIVE AILERON TRIM. 1 L 7 2 4J RT A00002AC 2008032000138 20080320 00138 2008 3 20 DL757080345 4 20080205 A 2565 SLIDE BOEING 757 757232 1384965 NM LT OFF WING NO TEST A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 643DL 23997 LEFT OFF WING SLIDE FAILED AMNUAL BACK-UP SYSTEM TEST. REPLACED BOTTLE BACK-UP CABLE IAW MM 25-65-06. 2 L 7 2 4F RT A2NM 2008032000158 20080320 00158 SO 2008 3 20 LR7A08039 1 20080227 A 5312 3700323944 BULKHEAD LKHEED 382 382G 526414U SO FS 180 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2299 5025 DURING SCHEDULED C-7 CHECK, PER SB A382-53-51 R1, FOUND UNDERDECK BULKHEAD CRACKED AT FS 180.5, WL172, LBL10-RBL28.8. R EPAIR ACCOMPLISHED IAW SB A382-53-51-R1WITH REFERENCE TO DWG SK382-53-187. 2 H 7 4 4T A1SO 2008032000168 20080320 00168 NM 2008 3 20 08FDEA00911 1 20080312 A 5311 AFA00203 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 521FE 48478 MAIN DECK FRAME AT RT STA 1701 L12 FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIG. 1 VOL.I. INITIAL INSPECTION AT 14500 CYCLES AND REPETITIVE INSPECTION AT 9500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032000185 20080320 00185 2008 3 20 UPS08851851 4 20080312 A 2565 SLIDE DOUG DC8 DC871F 302199D WP DISLODGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 GROUND PERSONNEL OPENED DOOR WITH GIRT BAR IN PLACE. SLIDE FELL OUT OF CONTAINER. REINSTALLED ESCAPE SLIDE PER MM 25-6 0-01-2. 2 L 7 4 4F RT 4A25 2008032100002 20080321 00002 EU 2008 3 21 08FDEA00779 1 20080307 A 5530 A5537016500000 TIP CAP AIRBUS 310 A310203 3930313 EU VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 VERTICAL STABILIZER TIP IS CRACKED AND DELAMINATED AT THE FWD HOIST POINT HOLE. REPAIRED VERTICAL STAB TIP ERROSION DAM AGE BY REMOVING DAMAGE SKIN PLYS, APPLING A WET LAYUP FIBERGLASS REPAIR AND REFINISHING IAW SRM 55-34-11. 2 L 7 2 4F RT A35EU 2008032400008 20080324 00008 EA 2008 3 24 COMA0870010 1 20080308 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA NLG OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 642CA 10125 FLIGHT 5219 - RECEIVED NOSE DOOR OPEN WARNING AND PROX SYSTEM 1 FAULT MESSAGES. DECLARED EMERGENCY, RETURNED TO SDF, LA NDED WITHOUT INCIDENT. ADJUSTED PX31 GAP TO AMM LIMITS, REMOVED SNOW AND ICE FROM AREA. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008031400001 20080314 00001 NM 2008 3 14 TSAA0829011 1 20080301 A 2910 651782117 VALVE BOEING 737 737230 1384401 NM A HYD SYSTEM LEAKING A TSAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 13 823AL 23154 FLIGHT 266 LIH-HNL - DURING APPROACH TO HNL, THE CREW NOTED THE A SYSTEM HYDRAULIC QUANTITY INDICATED ZERO GALLONS AND T HE A SYSTEM HYDRAULIC LOW PRESSURE INDICATOR ILLUMINATED. THE CREW DECLARED AN EMERGENCY, COMPLETED THE EMERGENCY CHECK LIST AND LANDED IN HNL WITHOUT FURTHER INCIDENT. MAINTENANCE TOWED THE AIRCRAFT FROM RUNWAY 8R TO THE GATE. MAINTENANC E REPLACED A FAILED PLUG AND O-RING SEAL ON THE A SYSTEM HYDRAULIC PRESSURE MODULAR ASSEMBLY. THE NR 2 ENGINE DRIVEN HY DRAULIC PUMP WAS ALSO REPLACED IN ACCORDANCE WITH AMM 29-11-32 2 L 7 2 4F RT A16WE 2008031400039 20080314 00039 NM 2008 3 14 2008UALA01216 1 20080305 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294-344 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 RT FWD GALLEY DOOR CREASE BEAM FROM STA 294 TO 344 IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REPLACE THE RT FWD GALLEY DO OR CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031400052 20080314 00052 NM 2008 3 14 CALA0800205 1 20080306 A 5311 6546596 FRAME BOEING 737 737524 1384721 NM BS 727B S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 FRAME CRACKED STA 727B ABOVE S9L. FABRICATED AND INSTALLED REPAIR ANGLES PER ECRA 5310-04727 REV A. 2 L 7 2 4F RT A16WE 2008031400066 20080314 00066 NM 2008 3 14 AALA200800443 1 20080228 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 775AN 29584 DFW - EMERGENCY LIGHT AT SEAT 25G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031400100 20080314 00100 NM 2008 3 14 2008UALA01233 1 20080306 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 727D S22-23R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 RT AFT LOWER FUSELAGE STA 727D BETWEEN STR 22R AND 23R FRAME LOWER FLANGE OTBD SURFACE HAS TOOLING DAMAGE. MAJOR REPAIR ACCOMPLISHED: CUT OFF LWR FLANGE. FABRICATED & INSTALLED REPAIR ANGLE & FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031400103 20080314 00103 NM 2008 3 14 2008UALA01236 1 20080308 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 CABIN FLOORBEAM FRAME UPPER SURFACE IS CORRODED, BS 294.5, RBL 15"-25". MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALL ED BS 294 FLOORBEAM UPPER CAP SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031700019 20080317 00019 NM 2008 3 17 2008UALA01267 1 20080306 A 2997 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEFT HYD SUPPLY DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 LEFT HYDRAULIC SUPPLY SHUTOFF VALVE DOES NOT CYCLE (MOVE) WHEN ENGINE FIRE HANDLE IS PULLED. FOUND CONNECTOR D44045 DAMA GED SUSPECT IMPROPERLY INSTALLED. REPLACED CONNECTOR OPS CHECKED GOOD IAW MM 29-11-06. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031700028 20080317 00028 EA 2008 3 17 SIMA200807001 1 20080306 A 3260 895303 PSEU CNDAIR CL600 CL6002C10 1390015 EA MLG MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 504AE 10044 ON FLIGHT 3847, CREW REPORTED GEAR DISAGREE WARNING WITH LANDING GEAR HANDLE UP NOSE INDICATED SAFE, BOTH MAINS DID NOT. AIRCRAFT REMOVED FROM SERVICE. REPLACED MPSEU PER MM 37-61-01. OPERATION CHECK GOOD SEE. AIRCRAFT RETURNED TO SERVI CE. 2 L 7 2 4F RT A21EA 2008031700031 20080317 00031 SO 2008 3 17 C2XA08TY033 1 20080307 A 5730 SKIN EMB 145 EMB145EP 3260221 SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14930 145011 A 1.26 LONG CRACK WAS DISCOVERED ON THE LT WING UPPER TRAILING EDGE SKIN ADJACENT TO THE CENTER SPOILER HINGE CUTOUT. R EPAIRED CRACK IAW EC5740-01140. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008031700036 20080317 00036 WP 2008 3 17 UPS08851766 1 20080309 A 3350 6012235 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 ON PREFLT, FOUND EMERGENCY EXIT LTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK PER UPS AMM 33-50. 2 L 7 4 4F RT 4A25 2008031700057 20080317 00057 NM 2008 3 17 SWAA081309 1 20080306 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIPS WORN BETWEEN ROW 9 DEF AND ROW 10 DEF. REMOVED AND REPLA CED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008031700075 20080317 00075 NM 2008 3 17 SWAA081284 1 20080307 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 435WN 32455 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2008031700077 20080317 00077 2008 3 17 SWAA081283 4 20080307 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 435WN 32455 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031700093 20080317 00093 2008 3 17 SWAA081293 4 20080307 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 470WN 33860 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031700097 20080317 00097 WP 2008 3 17 08FDEA00818 1 20080310 A 5510 ALC705220 TEE FITTING DOUG MD10 MD1010F 3022112 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 2ND FROM INBD LEADING EDGE SECTION AT THE RT HORIZONTAL STABILIZER; "UPPER OUTBD ATTACH ANGLE" IS CRACKED. REMOVED RACK ED TEE ANGLE IAW SRM 51-31-01 VOL II PG 1. FORMED NEW TEE CAP IAW DWG ALC 07052 REV G. LOCATED, DRILLED & DEBURRED NEW TEE CAP IAW SRM 51-31-01 VOL II PG 1. ALODINED & PRIMED NEW TEE CAP IAW SRM 51-21-01 VOL II PG 18. PART MARKED TEE C AP IAW GMM 7-0-100 PGS 1-2. INSTALLED TEE CAP IAW SRM 51-33-01 PG 1 & 51-35-01 VOL II PG 1. 2 L 7 3 4F RT A22WE 2008031700098 20080317 00098 2008 3 17 SWAA081295 4 20080308 A 2565 D313591478 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031700126 20080317 00126 NM 2008 3 17 SWAA081338 1 20080310 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031700132 20080317 00132 NM 2008 3 17 SWAA081322 1 20080310 A 5311 65C25230 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727D, STR 27L AND STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008031700133 20080317 00133 NM 2008 3 17 SWAA081320 1 20080310 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, STR 26L AND STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008031700135 20080317 00135 NM 2008 3 17 SWAA081321 1 20080310 A 5311 65C25230 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727E, STR 26L AND STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008031700136 20080317 00136 EU 2008 3 17 F3LA200800084 1 20080228 A 5321 31953000112 COVER AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FLOOR PANEL CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE COVER SHEET OF AFT CARGO PIT FLOOR PANEL 151VG. MA INTENANCE REMOVED THE CORRODED COVER SHEET FROM THE FLOOR PANEL. A REPLACEMENT COVER SHEET WAS FABRICATED IN ACCORDANCE WITH THE REQUIREMENTS OF EO A9-53E0-20231. THE NEW COVER SHEET WAS INSTALLED AND INSPECTED. UPON COMPLETION OF THE IN SPECTION, THE COVERSHEET AND FLOOR PANEL WERE FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008031700143 20080317 00143 NM 2008 3 17 AALA200800473 1 20080302 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 376AN 25445 SFO - EMERGENCY LIGHT AT OVERHEAD FORWARD GALLEY RIGHT SIDE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD FORWARD GALLEY RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008031700145 20080317 00145 NM 2008 3 17 AALA200800471 1 20080302 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 910AN 29512 MIA - EMERGENCY LIGHT AT SEAT 24D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008031700150 20080317 00150 NM 2008 3 17 SWAA081318 1 20080310 A 5315 6545834 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 29 TO RBL 42. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2008031700151 20080317 00151 NM 2008 3 17 AALA200800463 1 20080302 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7375A 25202 DFW - EMERGENCY LIGHT AT SEAT 12B MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 12B. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A1NM 2008031700155 20080317 00155 2008 3 17 SWAA081302 4 20080307 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031700156 20080317 00156 WP 2008 3 17 AALA200800468 1 20080302 A 2822 3980001 PUMP DOUG DC9 DC982 3022082 WP FUEL BOOST INOPERATIVE A AALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SW 21 251AA 49270 LGA INFLIGHT T333/02MAR - AFT CENTER FUEL BOOST PUMPS POPPED CIRCUIT BREAKERS. RETURNED TO LGA AND LANDED WITHOUT INCID ENT. REPLACED AFT CENTER FUEL TANK BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031700160 20080317 00160 NM 2008 3 17 HALA0800362 1 20080229 A 5330 PANEL BOEING 767 7673G5 1385126 NM BS 786-787 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION AT PANEL ATTACHMENT HOLE AT STA 786 TO 787 LBL 9.5. REPAIRED PER TI 190112993-0001. 2 L 7 2 4F RT A1NM 2008031700168 20080317 00168 NM 2008 3 17 SWAA081331 1 20080310 A 5711 112A1302 STIFFENER BOEING 737 7373G7 1384595 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND LT WING AFT SPAR UPPER CHORD INBOARD STIFFENER CRACKED. REPAIRED STIFFENER PER ER. 2 L 7 2 4F RT A16WE 2008031700171 20080317 00171 2008 3 17 SWAA081312 4 20080306 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 709SW 27843 L1 DOOR EMERGENCY EVAC SLIDED FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031700173 20080317 00173 NM 2008 3 17 SWAA081345 1 20080310 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 740SW 29276 DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION FITTING LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 2008031700175 20080317 00175 NM 2008 3 17 SWAA081328 1 20080310 A 5315 147A5504 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 766SW 29806 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 951, RBL 5. REPAIRED FLOORBEAM PER EA. 2 L 7 2 4F RT A16WE 2008031700176 20080317 00176 NM 2008 3 17 SWAA081327 1 20080310 A 5310 146A5925 CREASE BEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 766SW 29806 DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 807 AND BS 847, RBL 70. REMOVED AND REPLACED CREASE BE AM PER SRM. 2 L 7 2 4F RT A16WE 2008031700187 20080317 00187 SO 2008 3 17 C2XA08SH043 1 20080312 A 5230 14525480603 BEAM EMB 145 EMB145LR 3260212 SO CARGO DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13566 145622 SHV - DURING C-CHECK CARGO DOOR LOWER BEAM HAS VARIOUS AREAS OF CORROSION. MX REMOVED AND REPLACED CARGO DOOR LOWER BEA M IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008031700200 20080317 00200 NM 2008 3 17 SWAA081354 1 20080311 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008031700202 20080317 00202 EA 2008 3 17 VNAA0802016 1 20080223 A 3244 H29X9015 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT MLG SEPARATED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 253PS 22 7934 CREW REPORTED THE RIGHT INBOARD TIRE SEPARATED. MAINTENANCE INSPECTED AND FOUND THE TREAD SEPARATION AND DAMAGE TO THE RIGHT INBOARD FLAP. MAINTENANCE REMOVED AND REPLACED THE NR 3 AND NR 4 MAIN TIRES. MAINTENANCE REPAIRED FLAP DAMAGE PE R REO 601R57-52-716 AND TEMP REPAIR 11000. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008031700204 20080317 00204 SO 2008 3 17 C2XA08IA069 1 20080211 A 3231 22250100003 SOLENOID VALVE EMB 145 EMB145XR 3260214 SO NLG DEFECTIVE A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 12157 16714 7696 145787 IAH - FLIGHT 2388, THE CREW REPORTED THAT THE NOSE LANDING GEAR DOORS OPENED BY THEMSELVES IN FLIGHT AT FL370. THE AIRC RAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOOR SOLENOID VALVE, OPERAT IONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008031700205 20080317 00205 SO 2008 3 17 C2XA08IA070 1 20080226 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 11565 145621 IAH - FLIGHT 2656, DURING PREFLIGHT INSPECTION THE CREW REPORTED A FUEL SMELL IN THE COCKPIT. MAINTENANCE INSPECTED THE AIRCRAFT WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008031700207 20080317 00207 WP 2008 3 17 ABXR080079 1 20080214 A 5531 99118241 RIB DOUG DC9 DC933F 302207A WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 RIB CRACKED AT FASTENER RIGHT SIDE OF VERTICAL STAB LEADING EDGE ZFS 80. REPAIRED RIB IAW DC9 SSRM K05159. 2 L 7 2 4F A6WE 2008031700210 20080317 00210 WP 2008 3 17 ABXR080065 1 20080202 A 5730 5912156131 SKIN DOUG DC9 DC933F 302207A WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 LEFT WING UPPER TRAILING EDGE SKIN BULGED, RIVETS CUPPED FORWARD OF SPOILER BOARDS (CENTER). CUT OUT DAMAGE. INSTALLED NEW SECTION OF SKIN AND -9 DOUBLER IAW DC9 SRM 57-30-3, 57-01, FIG 3, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2008031700227 20080317 00227 SO 2008 3 17 C2X08ON098 1 20080225 A 3010 4800104 BUTTON EMB 145 EMB145XR 3260214 SO COCKPIT DEFECTIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 11193 7015 7015 14500938 FLT 0030 - MCI - FLIGHT CREW REPORTED NR 1 WING ANTI-ICE FAIL ON EICAS. FLIGHT DIVERTED FROM OMA TO MCI. MX PERSONNEL REMOVED AND REPLACED NR 1 WING ANTI-ICE PUSH BUTTON, OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETUR N TO SERVICE. 2 L 7 2 4F RT 2008031700229 20080317 00229 SO 2008 3 17 C2XA08TY032 1 20080303 A 3350 276005 FUSE EMB 135 EMB135LR 3260305 SO CABIN BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27506 145206 TYS - DURING AN OVERNIGHT INSPECTION MX FOUND THE RT AND LT EMERGENCY LIGHTS INOP. THE EMERGENCY LIGHT BATTERY FUSE WAS REMOVED AND REPLACED IAW EMB 135 AMM 24-30-02, OPS CHECKED GOOD AND THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008031700233 20080317 00233 WP 2008 3 17 ABXA080087 1 20080229 A 3232 39208025503 ACTUATOR DOUG DC9 DC941 302207N WP RT MLG DAMAGED A ABXA K NONE O OTHER DE DESCENT 1 GL 23 966AX 7568 47510 UPON PUTTING GEAR HANDLE DOWN, HEARD LOUD BANG AND SHUTTER IN AIRCRAFT. NORMAL GEAR INDICATION. FOUND RIGHT MAIN LANDI NG GEAR ACTUATOR EYE BOLT PULLED OUT OF THE ACTUATOR. REPLACED THE RIGHT MAIN LANDING GEAR ACTUATOR IAW DC9 AMM 32-32-0 2. 2 L 7 2 4F A6WE 2008031700236 20080317 00236 SO 2008 3 17 C2XA08CL026 1 20080306 A 2761 3605401007 ACTUATOR EMB 145 EMB145LR 3260212 SO RT SPEED BRAKE MALFUNCTIONED A C2XA K NONE F FLT CONT AFFECTED CR CRUISE 1 SW 27 12564 11676 145618 IAH FLIGHT 3013 - THE CREW REPORTED THE LEFT SPEED BRAKE EXTENDED FASTER THAN THE RIGHT INFLIGHT CAUSING THE AIRCRAFT TO ROLL ABOUT 4 DEGRESS PER SECOND WITH AND WITHOUT AUTOPILOT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT OUTBOARD SPEE D BRAKE ACTUATOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008031700237 20080317 00237 SO 2008 3 17 C2XA08CL027 1 20080309 A 3397 CONNECTOR EMB 145 EMB145XR 3260214 SO CABIN DIRTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13124 145689 DURING ROUTINE MAINTENANCE THE AFT EMERGENCY EXIT LIGHT SIGN WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND CLEANED E LECTRICAL CONNECTORS OF THE AFT EMERGENCY EXIT SIGN. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2008031700243 20080317 00243 EA 2008 3 17 VNAA0802018 1 20080224 A 2810 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE FUEL SYSTEM OPEN A VNAA A UNSCHED LANDING W INADEQUATE Q C TO TAKEOFF 1 GL 05 723PS 10181 CREW REPORTED A LOUD BANGING NOISE IN FLIGHT. CREW ELECTED TO RETURN TO BHM AND LANDED WITHOUT INCIDENT. MAINTENANCE I NSPECTED AND FOUND REFUEL DOOR OPEN AND CAP MISSING. MAINTENANCE FOUND NO EVIDENCE OF ENGINE INGESTION OR OTHER STRUCTU RAL DAMAGE. MAINTENANCE SECURED THE DOOR CLOSED AND REPLACED THE MISSING FUEL CAP IN ACCORDANCE WITH THE AIRCRAFT MAINT ENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008031700244 20080317 00244 EA 2008 3 17 VNAA0802019 1 20080225 A 3244 H29X9015 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE MLG SEPARATED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 207PS 121 7873 CREW REPORTED THE LEFT HAND OUTBOARD MAIN TIRE'S TREAD SEPARATED. MAINTENANCE INSPECTED AND CONFIRMED THE TREAD LOSS IN ADDITION TO DAMAGE TO THE LEFT HAND INBOARD FLAP ASSEMBLY AND LEFT GEAR DOOR. MAINTENANCE REMOVED AND REPLACED THE MAI N TIRE, FLAP ASSEMBLY AND GEAR DOOR IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE PERFORM ED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008031300348 20080313 00348 EU 2008 3 13 08FDEA00755 1 20080306 A 5510 A55178101200000 BRIDGE AIRBUS 310 A310203 3930313 EU HORIZONTAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT HORZIONTAL STABILIZER TIP BRIDGING STRIP CORRODED UNDER THE NUTPLATES. REMOVED THE CORROSION REF SRM 51-74-10; PA RA 5. FOUND TO BE WITHIN LIMITS IAW SRM 55-10-00 TABLE 101. ALODINED REF SRM 51-21-10, PARA 5. PRIMED REF SRM 51-23-10 ; PG 1. INSTALLED NUTPLATES REF SRM 51-40-21 PARA 6. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008031300372 20080313 00372 NM 2008 3 13 SWAA081259 1 20080305 A 5311 6546533 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, STR 28L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008031300374 20080313 00374 2008 3 13 SWAA081249 4 20080305 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031300375 20080313 00375 NM 2008 3 13 SWAA081252 1 20080305 A 5523 65C35943 BEARING BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED HC1 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING AND BEA RING PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300409 20080313 00409 EU 2008 3 13 08FDEA00775 1 20080307 A 7830 SLEEVE AIRBUS 310 A310203 3930313 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 ENGINE OUTBD T/R TRANSLATOR SLEEVE, UPPER CORNER PANELS ARE CRACKED. CLEANED FWD TRANSLATOR SLEEVE PANEL REF AMM 1 2-21-11. HFEC PANEL EF NDT MANUAL 51-10-08. NO CRACKS FOUND. REMOVED AFT TRANSLATOR SLEEVE PANEL REF SRM 51-40-21 PARA 1 3. CLEANED AFT PANEL REF AMM 12-21-11. HFEC PANEL REF NDT MANUAL 51-10-08. NO CRACKS NOTED. ALODINED FWD & AFT PANEL R EF SRM 51-21-10. PRIMED REF SRM 51-23-10. REINSTALLED AFT PANEL REF SRM 51-40-10 PARA 13. PAINTED REF SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008031300427 20080313 00427 NM 2008 3 13 SWAA081271 1 20080309 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031400005 20080314 00005 NM 2008 3 14 TSAA0877012 1 20080304 A 7722 SEL0C19G INDICATOR BOEING 737 737282C 13844AU NM NR 1 FAILED A TSAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 826AL 23051 FLIGHT 269 HNL-LIH - AT TAKEOFF, THE CREW NOTED THE NR 1 EGT READ LOW AT APPROXIMATELY 250 DEGREES AND ELECTED TO ABORT THE TAKEOFF AT 90 KTS AIRSPEED. THE AIRCRAFT WAS TAXIED BACK TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE EGT INDICATOR AND COMPLETED A HIGH POWER ENGINE RUN WITH ALL CHECKS SATISFACTORY. THE AIR CRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2008031400016 20080314 00016 EU 2008 3 14 2008UALA01111 1 20080228 A 2810 FUEL TANK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT WING LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 447UA 836 FUEL LEAKING, INBD PORTION OF THE RT TANK, COMING FROM FASTENERS AND SEALANT, BY THE RT MLG GEAR DOOR. UNKNOWN FUEL LEA K. IDENTIFIED LEAKS IN TANK USING BLOW BACK METHOD. FUEL LEAKING FROM RT WING TANK AT REAR SPAR TO RIB CASTING SEPARAT ING WING AND CTR TANK. REMOVED SEALANT IN LEAK AREAS AND APPLIED NEW SEALANT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031400019 20080314 00019 NM 2008 3 14 2008UALA01115 1 20080302 A 2133 OUTFLOW VALVE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN PRESSURE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 817UA 873 RTFL WITH A CABIN PRESSURE ISSUE. VALVE 22HQ IN OFF POSITION CAUSING SKIN FAULT ECAM. TURNED ON VALVE 22HQ AND REPLACE D THE AVEC AS PRECAUTIONARY. BITE TEST WAS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031400027 20080314 00027 2008 3 14 2008UALA01145 4 20080228 A 2565 D31865111 SLIDE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE MISINSTALLED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 848UA 1647 THE BLOW OUT DOOR LOCKING PIN WAS NOT COMPLETELY LATCHED. SLIDE WAS PACKED TOO HIGH. REBAND AND OVEN BAKE 12 HOURS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031400043 20080314 00043 NM 2008 3 14 2008UALA01220 1 20080305 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FWD GALLEY DOOR SURROUND OTBD WEB SUPPORT ANGLE CRACKED AT BS 277 TO 294.5 BETWEEN STR 11R AND 12R. MAJOR REPAIR ACCOMP LISHED: INSTALLED NEW SUPPORT ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031400096 20080314 00096 NM 2008 3 14 2008UALA01228 1 20080306 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 500 S27-28R CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FWD CARGO COMPARTMENT FRONT SIDE OF THE FLOORBEAM AT BS 500 BETWEEN STRINGER 28R AND 27R IS CORRODED. MAJOR REPAIR ACCO MPLISHED: FABRICATED & INSTALLED SHEAR TIE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031700014 20080317 00014 NM 2008 3 17 2008UALA01258 1 20080306 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 456 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 FWD PIT FRAME WEB CRACKED AT BS 456 LBL 28. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031700016 20080317 00016 NM 2008 3 17 2008UALA01265 1 20080306 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 651UA 25389 DOOR 2 LEFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RESECURED CONNECTOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031700034 20080317 00034 NM 2008 3 17 UPS08551776 1 20080228 A 8011 STARTER BOEING 757 75724APF 1384969 NM LEFT ENGINE FIRE A IPXA K NONE A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 457UP 25478 WHILE STARTING LEFT ENGINE, MECHANIC REPORTED SPARKS AND FLAMES COMING FROM SIDES OF ENGINE COWLING. FOUND PNEUMATIC ST ARTER BROKEN. REMOVED AND REPLACED PNEUMATIC STARTER PER MM 80-11-01-4. PERFORMED DRY MOTOR PROCEDURES IAW AMM 71-00-0 0/201. FOUND NORMAL. NO LEAKS NOTED. A/C OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2008031700038 20080317 00038 NM 2008 3 17 UPS08M51770 1 20080309 A 3350 LAMP DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 EMERGENCY POWER "OFF" LIGHT INOP. RELAMPED PER MM 33-00-00. OPS CHECK GOOD. 2 L 7 3 4F RT A22WE 2008031700081 20080317 00081 2008 3 17 SWAA081286 4 20080309 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 457WN 33856 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031700095 20080317 00095 NM 2008 3 17 SWAA081294 1 20080307 A 3350 1619 LIGHT BOEING 737 7375H4 138449D NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008031700115 20080317 00115 NM 2008 3 17 SWAA081296 1 20080308 A 3232 654482517 ACTUATOR BOEING 737 7375H4 138449D NM RT MLG FAULTY A SWAA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 29 510SW 24187 RETRACTED LANDING GEAR, RT MLG UNSAFE LIGHT ILLUMINATED. CYCLED GEAR, SAME INDICATION, LIGHT WENT OUT ABOVE 10000 FT. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2008031700148 20080317 00148 NM 2008 3 17 AALA200800472 1 20080302 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 181AN 29591 MIA - EMERGENCY LIGHT AT SEAT 35D INOPERATIVE. RESET CONNECTOR FOR EMERGENCY LIGHT AT SEAT 35D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008031700159 20080317 00159 NM 2008 3 17 HALA0800373 1 20080306 A 5420 ATTACH BRACKET BOEING 767 767332 1382001 NM NR 2 INLET GOUGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 NR 2 ENGINE NOSE INLET COWL TO FAN CASE ATTACHMENT BRACKET AT 3 O'CLOCK POSITION GOUGED. DAMAGE AT 3 O'CLOCK ON NOSE CO WL AFT BULKHEAD INNER RING BLENDED IAW SRM 54-11-02/1A01, FIG 101, DETAIL 111, WITHIN SRM LIMITS. 2 L 7 2 4F RT A1NM 2008031700180 20080317 00180 NM 2008 3 17 HALA0800375 1 20080306 A 5415 ATTACH BRACKET BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 INLET GOUGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 AT 2 ENG NOSE INLET COWL TO FAN CASE ATTACHMENT BRACKETS AT 7 O'CLOCK POSITION GOUGED. DAMAGE ON NOSE COWL AFT BULKHEAD INNER RING, 7 O'CLOCK POSITION BLENDED IAW SRM 54-11-02/1A01, FIG 101, DETAIL 111, WITHIN SRM LIMITS. 2 L 7 2 4F 4 F RT A1NM E13NE 2008031700209 20080317 00209 WP 2008 3 17 ABXR080083 1 20080214 A 5531 991188612 RIB DOUG DC9 DC933F 302207A WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 RIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERT STAB LEADING EDGE ZFS 18. REPAIRED IAW DC9 SSRM DWG K05159. 2 L 7 2 4F A6WE 2008031700219 20080317 00219 WP 2008 3 17 ABXR080074 1 20080207 A 5311 99118431 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 FRAME AT STA 1168 AT APPROX 3 O'CLOCK POSITION WAS CRACKED. REPAIRED AREA IAW DC9 SRM 53-01, FIG 2. 2 L 7 2 4F A6WE 2008031700242 20080317 00242 EA 2008 3 17 VNAA0802017 1 20080224 A 5242 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE GROUND POWER OPEN A VNAA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 05 716PS 10171 CREW REPORTED THE GROUND POWER DOOR LEFT OPEN FOR FLIGHT. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. M AINTENANCE INSPECTED AND SECURED THE DOOR CLOSED. MAINTENANCE FOUND NO DEFECTS OR DAMAGE. AIRCRAFT WAS RELEASED FOR SE RVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008031700245 20080317 00245 EA 2008 3 17 VNAA0802021 1 20080226 A 5730 FAIRING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT WING DAMAGED A VNAA O OTHER O OTHER LD LANDING 1 GL 05 250PS 7929 CREW REPORTED THE RIGHT WING STRUCK THE GROUND UPON LANDING. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE RIGHT HAND W INGTIP LOWER SKIN PANEL. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND WINGTIP FAIRING IN ACCORDANCE WITH THE AIRCRA FT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008031700246 20080317 00246 EA 2008 3 17 VNAA0802023 1 20080227 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF348C1 30049 NE FUSELAGE DENTED A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 05 712PS 10168 CREW REPORTED A DENT IN THE AIRCRAFT SKIN TO THE LEFT FRONT BY THE WINDSHIELD. DAMAGE CAUSED BY A PART OF THE JETWAY FE LL ON THE AIRCRAFT. MAINTENANCE INSPECTED AND FOUND A DENT ABOVE THE CAPTAINS WINDOW FRAME. AIRCRAFT APPROVED FOR RETU RN TO SERVICE PER REO 670-53-11-277. MAINTENANCE ISSUED DAMAGE AUTHORIZATION 20074. AIRCRAFT WAS RELEASED FOR SERVICE . 2 L 7 2 4F 4 F RT A21EA E00063EN 2008031700249 20080317 00249 CE 2008 3 17 022708 1 20080221 A 2710 ATTACH FITTING CESSNA 208 208B 2073701 CE AILERON CONTROL ROTATED E AWHA K NONE O OTHER CR CRUISE 1 WP 00 763FE 7803 38 208B0256 PILOT REPORTED BINDING AND NOISE IN THE OVERHEAD IN AILERON CONTROL SYSTEM. FLIGHT CONTINUED NORMAL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE ATTACH BLOCK OF THE AILERON CONTROL CABLE LOOP SYSTEM ROTATED AND WAS STR IKING THE LOWER BELL CRANK QUAD ASSEMBLY. THE BLOCK WAS REPOSITIONED TO ACHIEVE CLEARANCE AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 H 7 1 3T A37CE 2008031700255 20080317 00255 CE 2008 3 17 GUUA01200801 1 20080120 A 5210 DOOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA LACK OF LUBE A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 81535 UE147 FLIGHT: 9257, PILOT REPORTED THE CABIN DOOR WILL NOT SHUT. LUBED CABIN DOOR. 2 L 7 2 4T 3 T RT A24CE E2NE 2008031700257 20080317 00257 EU 2008 3 17 01282008 1 20080125 A 5302 DOUBLER BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE TAILBOOM CRACKED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 171MU 7138 DURING DAILY INSPECTION, A 3 INCH LONG CRACK WAS FOUND ON THE LT SIDE TAILBOOM DOUBLER. 1 G 7 2 3U 3 U H13EU E5NE 2008031700268 20080317 00268 SO 2008 3 17 GUUA01300801 1 20080130 A 3350 D36604001 BATTERY EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN DISCHARGED A GUUA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 29 285AS 120265 DURING PREFLIGHT DISCOVERED EMERGENCY LIGHTS ON SIDE OF THE GALLEY INOPERATIVE. REPLACED EMERGENCY LIGHTS FRONT BATTERY . 2 L 7 2 4T 4 T RT A31SO E20NE 2008031700276 20080317 00276 EA 2008 3 17 MASA200800194 1 20080309 A 2611 SMOKE WARNING CNDAIR CL600 CL6002B19 1900309 EA LAVATORY MALFUNCTIONED A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 649BR 7414 ASH FLT 7158 CLE-IAD - LAV SMOKE CAUTION MESSAGE AND SMELL IN FLIGHT. INSPECTED LAV DETECTOR, PERFORMED ENGINE RUNS, NO EVIDENCE OF SMOKE NOTED, DETECTOR OPS NORMAL. 2 L 7 2 4F RT A21EA 2008031700277 20080317 00277 EA 2008 3 17 MASA200800195 1 20080306 A 5514 FITTING CNDAIR CL600 CL6002D24 1390016 EA HORIZ STAB GOUGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 917FJ 15017 REPAIR TO GOUGE DAMAGE TO H-STAB PIVOT FITTING. 2 L 7 2 4F RT A21EA 2008031700278 20080317 00278 EA 2008 3 17 MASA200800196 1 20080306 A 5210 WEB CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 917FJ 15017 REPAIR TO PAX DOOR AFT WEB CRACKS. 2 L 7 2 4F RT A21EA 2008031700284 20080317 00284 NM 2008 3 17 MASA200800209 1 20080301 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 448YV 448 REPAIR ON THE RT NR 4 FLAP TRACK. 2 H 7 2 4T RT A13NM 2008031700288 20080317 00288 NM 2008 3 17 HALA0800372 1 20080306 A 7110 ATTACH BRACKET BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE COWL GOUGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 NR 2 ENGINE NOSE INLET COWL TO FAN CASE ATTACHMENT BRACKET AT 2 O'CLOCK POSITION GOUGED. DAMAGE ON NOSE COWL AFT BULKHE AD INNER RING BLENDED IAW SRM 54-11-02/1A01, FIG. 101, DETAIL 111, WITHIN SRM LIMITS. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031700290 20080317 00290 NM 2008 3 17 DHLA200800022 1 20080305 A 3350 38931002 BATTERY PACK BOEING 727 727223 1384074 NM COCKPIT DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 GL 05 749DH 22013 COCKPIT EMERGENCY EXIT LIGHT INOP. REPLACED COCKPIT EMERGENCY EXIT LIGHT BATTERIES MODEL NR-106PER MM 33-50-71. OPS CK SERVICEABLE. AIRCRAFT WAS GROUNDED. 2 L 7 3 4F A3WE 2008031800002 20080318 00002 NM 2008 3 18 C8GA20080009 1 20080306 A 7920 STRAINER BOEING 727 727223 1384074 NM NR 3 ENGINE UNKNOWN A C8GA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 29 898AA 22014 FLT 724 FROM TOL TO ROC - DURING CLIMB OPERATION, THE NR 3 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. THE NR 3 ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO TOL WHERE IT LANDED WITHOUT INCIDENT. ON POST FLIGHT, REMOVED AND INSPECTED THE MAIN OIL STRAINER, NO CONTAMINATION WAS NOTED. THE MAIN OIL STRAINER AND MAIN OIL BY-PASS SWITCH WAS REMOVED AND RE PLACED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2008031800007 20080318 00007 EU 2008 3 18 08FDEA00849 1 20080310 A 5753 SKIN AIRBUS 310 A310203 3930313 EU T/E FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT OUTBD FLAP AFT EDGE OF THE FLAP IS DELAMINATED ON THE UPPER SURFACE. PREPARED & RESEALED IAW SRM 57-53-12 FIG 209. 2 L 7 2 4F RT A35EU 2008031800008 20080318 00008 EU 2008 3 18 08FDEA00850 1 20080310 A 5753 A5797149820400 RUB STRIP AIRBUS 310 A310203 3930313 EU T/E FLAP DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT OUTBD FLAP UPPER EXTERNAL SKIN HAS THE METAL CHAFE STRIP DISBONDED. REMOVED & REPLACED CHAFE STRIP IAW SRM 57-53-12 F IG 201. 2 L 7 2 4F RT A35EU 2008031800010 20080318 00010 EU 2008 3 18 08FDEA00852 1 20080310 A 5320 A2551020400000 FLOOR PANEL AIRBUS 310 A310203 3930313 EU ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FLOOR PANEL PANEL 147 AF IS DELAMINATED AND OIL SATURATED. FABRICATED NEW FLOOR PANEL. LOCATED HOLES, POTTED EDGES. CURED EDGE POTTING. INSTALLED INSERTS AND APPLIED NON-SKID IAW SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 2008031800011 20080318 00011 EU 2008 3 18 08FDEA00853 1 20080310 A 5320 A21510415000400 PANEL AIRBUS 310 A310203 3930313 EU FUSELAGE PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 PUNCTURE ON THE INTERIOR SURFACE OF PANEL NR 144FR. REPAIRED INTERIOR SURFACE BY REMOVING THE DAMAGE. APPLIED, CURED & SANDED THE WET LAY UP. APPLIED REFINISH IAW SRM 51-77-10 & SRM 51-75-10. 2 L 7 2 4F RT A35EU 2008031800016 20080318 00016 EU 2008 3 18 08FDEA00858 1 20080310 A 2550 A2557222900200 PANEL AIRBUS 310 A310203 3930313 EU AFT CARGO BAY DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT CARGO PIT PANEL NR 161MW IS DELAMINATED AND PUNCTURED. REPAIRED PANEL & APPLIED TOP COAT (WHITE) ON AFT CARGO PIT I AW DWG SRZ 25-013. 2 L 7 2 4F RT A35EU 2008032400010 20080324 00010 SO 2008 3 24 FDKA200803092 1 20080306 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 FDM 6119 MCO-FLL (0714 PHX LCL). LEFT SIDE EMERGENCY LIGHT INOP OVERWING. MX RESET LIGHTING SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008032400015 20080324 00015 EA 2008 3 24 COMA0860159 1 20080305 A 3260 BRACKET CNDAIR CL600 CL6002B19 1900309 EA NLG BENT A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 960CA 7117 FLIGHT 5458 - RECEIVED GEAR DISAGREE MESSAGE AND NOSE DOOR WARNING. NOSE GEAR DID NOT INDICATE UP. COMPLIED WITH QRH. RETURNED TO ATL, LANDED WITHOUT INCIDENT. FOUND NLG OLEO SENSOR BRACKET BENT, INCREASING SENSOR GAP BEYOND LIMIT. REW ORKED BRACKET. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008032400018 20080324 00018 WP 2008 3 24 UPS08851861 1 20080314 A 2133 OUTFLOW VALVE DOUG DC8 DC873F 302199F WP CABIN PRESSURE MALFUNCTIONED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 808UP 46008 CLIMBING THRU FL250 CABIN PRSR/ALT WARNING HORN SOUNDED. CABIN ATL WAS 13000 FT AND CLIMBING AT 4000 FPM. LOCKED OUTFL OW VLV CLOSED AND TURNED BOTH PACKS TO MAX. NO OTHER LIGHTS OR INDICATIONS. WENT BACK TO AUTO AND WORKED OK. BOTH PAC KS WERE AT MINIMUM AT TIME OF PROBLEM. PRESSURIZED A/C, FOUND (L) OVER-PRESS. RELIEF VALVE OPENING PREMATURELY. DEFER RED PER MEL 21-10-2, MEL NR 371331. PRESSURIZED A/C, FOUND (L) OVER-PRESS. RELIEF VALVE OPENING PREMATUREL Y. REF AMM 2 1-31-05-2. ADJUSTED LEFT CABIN PRESSURE SAFETY VALVE TO 1/4 TURN COUNTER CLOCKWISE TO INCREASE CRACK PRESS DIFFERENTIAL CRACK POINT. OPS CHECKS GOOD ON GROUND. M371331 CLOSED. 2 L 7 4 4F RT 4A25 2008032400027 20080324 00027 NM 2008 3 24 PIDA08012 1 20080207 A 5313 STRINGER BOEING 737 7372K5 138448X NM FUSELAGE CORRODED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 249TR 22598 DURING MAINTENANCE CHECK, NOTED CORROSION AT STRINGER 22LT BETWEEN ATTACH ANGLE AND STRINGER AT BS 727A. REPAIRED DAMAG ED AREA PER SRM AND EA 53-017A. 2 L 7 2 4F RT A16WE 2008032400030 20080324 00030 NM 2008 3 24 UPS08M51815 1 20080302 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 25 LEFT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALL ED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.069 BORE I.D. 1.067 2 L 7 3 4F RT A22WE 2008032400036 20080324 00036 NM 2008 3 24 UPS08M51821 1 20080221 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 35 LT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.180 BORE I.D. 1.178. 2 L 7 3 4F RT A22WE 2008032400037 20080324 00037 WP 2008 3 24 08FDEA01023 1 20080318 A 5712 RIB DOUG MD10 MD1010F 3022112 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LT WING L/E INTERNAL RIB UPPER AFT EDGE IS CRACKED INBD OF THE NR 15 SLAT TRACK. REMOVED AND REPLACED RIB ARB-4352-35, PO 612712.1 IAW SRM 57-20-00 FIG 1 VOL I & 51-33-01 VOL II. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008032400038 20080324 00038 EA 2008 3 24 SWIA200819342 1 20080310 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS UNSECURE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 926SW 7687 FLT 6728 - FORWARD SECTION OF FLOOR EMERGENCY LIGHTS DO NOT ILLUMINATE. RESECURED CONNECTION AT LIGHT STRIP. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008032400043 20080324 00043 WP 2008 3 24 08FDEA00955 1 20080314 A 5730 ARC0740507 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 CHAFED INTERIOR SKIN REPAIR DOUBLER ON PANEL NR 535 DL. REMOVED DAMAGED DOUBLER. CLEANED & PREPPED AREA. FABRICATED NE W DOUBLER & FILLER. APPLIED A HOT BOND, SEALED EDGES WITH SEALANT. PRIMED & PAINTED IAW SRM 51-71-00 VOL II. 2 L 7 3 4F RT A22WE 2008032400044 20080324 00044 EU 2008 3 24 08FDEA00968 1 20080314 A 5740 ATTACH FITTING AIRBUS 310 A310203 3930313 EU RT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT WING SKIN ABOVE THE PYLON OUTBD ATTACH FITTING IS GOUGED. REPAIRED AREA IAW EA 6-5730-118443. 2 L 7 2 4F RT A35EU 2008032400053 20080324 00053 NM 2008 3 24 UPS08M51804 1 20080218 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION ON NR 14 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND IN STALLED REPAIR BUSHING PER EO MD11-5510-19409-M, BUSHING O.D. .9755 BORE I.D. .974. 2 L 7 3 4F RT A22WE 2008032400054 20080324 00054 NM 2008 3 24 UPS08M51805 1 20080226 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 15 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M, BUSHING O.D. 1.037 BORE I.D. 1.035. 2 L 7 3 4F RT A22WE 2008032400059 20080324 00059 NM 2008 3 24 UPS08M51812 1 20080226 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 21 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035. 2 L 7 3 4F RT A22WE 2008032400060 20080324 00060 NM 2008 3 24 UPS08M51813 1 20080302 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 22 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 1.069 BORE I.D. 1.067 2 L 7 3 4F RT A22WE 2008032400061 20080324 00061 NM 2008 3 24 UPS08M51823 1 20080228 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 36 LT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 2.243 BORE I.D. 2.442. 2 L 7 3 4F RT A22WE 2008032400065 20080324 00065 NM 2008 3 24 UPS08M51829 1 20080218 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 2 RT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.077 BORE I.D. 1.075. 2 L 7 3 4F RT A22WE 2008032400067 20080324 00067 NM 2008 3 24 UPS08M51831 1 20080305 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 4 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944. 2 L 7 3 4F RT A22WE 2008032400068 20080324 00068 NM 2008 3 24 UPS08M51832 1 20080218 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 5 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M, BUSHING O.D .946 BORE I.D. .944. 2 L 7 3 4F RT A22WE 2008032400069 20080324 00069 NM 2008 3 24 UPS08M51833 1 20080226 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 6 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944. 2 L 7 3 4F RT A22WE 2008032400074 20080324 00074 NM 2008 3 24 UPS08M51838 1 20080226 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 12 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944. 2 L 7 3 4F RT A22WE 2008032400075 20080324 00075 NM 2008 3 24 UPS08M51839 1 20080218 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND IN NR 14 RT (UPPER) BARREL NUT BORE HOLE AND ON BOTTOM SURFACE OF RADIUS. REMOVED CO RROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5110-19409-M, BUSHING O.D. .976 BORE I.D. .974. 2 L 7 3 4F RT A22WE 2008032400076 20080324 00076 NM 2008 3 24 UPS08M51841 1 20080226 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 15 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035. 2 L 7 3 4F RT A22WE 2008032400077 20080324 00077 NM 2008 3 24 UPS08M51842 1 20080218 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 17 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.069 BORE I.D. 1.067. 2 L 7 3 4F RT A22WE 2008032400078 20080324 00078 NM 2008 3 24 UPS08M51843 1 20080226 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 18 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035. 2 L 7 3 4F RT A22WE 2008032400083 20080324 00083 NM 2008 3 24 UPS08M51849 1 20080226 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 24 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035. 2 L 7 3 4F RT A22WE 2008032400084 20080324 00084 NM 2008 3 24 UPS08M51852 1 20080219 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 26 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035. 2 L 7 3 4F RT A22WE 2008032400085 20080324 00085 NM 2008 3 24 UPS08M51853 1 20080226 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 27 RT (UPPER) BARREL NUT BORE HOLE AND BOTTOM SURFACE CORRODED THRU. REMOVED C ORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 1.164 BORE I.D. 1.162. 2 L 7 3 4F RT A22WE 2008032400089 20080324 00089 NM 2008 3 24 UPS08M51857 1 20080304 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 31 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.180 BORE I.D. 1.178. 2 L 7 3 4F RT A22WE 2008032400091 20080324 00091 EU 2008 3 24 YENA2008021 1 20080308 A 3230 17071000407 UPLOCK EMB ERJ190 ERJ190100IGW 3260408 EU RT MLG MALFUNCTIONED A YENA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 15 192JB 6044 3919 19000014 FLT 610, JAX-JFK, ON FINAL APPROACH, LANDING GEAR LIGHT DISAGREE RIGHT MAIN DID NOT INDICATE DN/LOCKED. "LG LEVER DISAG ". QRH CHECK LIST AND LDG ABNORMAL EXTENSION CHECK LIST COMPLIED WITH. RT MAIN GEAR DID THEN SHOW GREEN DOWN/LOCKED. MANUAL RELEASE LEVER DEPLOYED GEAR. NOT OVERRIDE. REPLACED RT MAIN LANDING GEAR UPLOCK BOX PER AMM 32-31-03 AND PERFO RMED AN OPERATIONAL TEST OF THE LANDING GEAR SYSTEM PER AMM 32-33-00-710-801A/500. OPS CHECK OK. 2 L 7 2 4F RT A57NM 2008032400120 20080324 00120 EA 2008 3 24 COMA0860167 1 20080310 A 5350 SEALANT CNDAIR CL600 CL6002B19 1900309 EA FAIRING MISSING A COMA L ABORTED APPROACH E VIBRATION/BUFFET AP APPROACH 1 SO 01 933CA 7040 FLIGHT 5451 - UPON FLAP SELECTION TO 8 DEGREES A THUMPING WAS FELT. ABORTED APPROACH, DECLARED EMERGENCY, TOWER VERIFIE D GEAR DOWN UPON SELECTION. LANDED WITHOUT INCIDENT. REPLACED MISSING SEALANT TO BELLY AND WING ROOT FAIRINGS. NO FUR THER DEFECTS. 2 L 7 2 4F RT A21EA 2008032400125 20080324 00125 EU 2008 3 24 YENA2008023 1 20080310 A 3350 321431 BATTERY AIRBUS 320 A320232 3930326 EU CABIN FAULTY A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 561JB 21698 21698 1927 ON MX INSPECTION, FWD EPSU FAULTS EMERGENCY LIGHT BATTERY. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT FWD EPSU PER 33-51-38-04, OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2008032400129 20080324 00129 EA 2008 3 24 COMA0860170 1 20080310 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA O OTHER O OTHER IN INSP/MAINT 1 SO 01 798CA 21224 7348 CRACK ON THE CAP ANGLE AT RBL 18.00 AT FS 559. REPAIRED CRACK ON CAP ANGLE AT RBL 18.00 IAW REO 601R-53-41-260. 2 L 7 2 4F RT A21EA 2008032400131 20080324 00131 EU 2008 3 24 F3LA200800104 1 20080302 A 2571 D5391215720000 FITTING AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE BATTERY TRAY WORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 888 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED THE FORWARD AND AFT ATTACH POINTS OF THE NUMBER 1 BATTERY TRAY SHOWED EVIDENCE OF FRETTING. MAINTENANCE REMOVED AND REPLACED THE FORWARD BATTERY TRAY FITTING IN ACCORDANCE WITH THE REQUIREMENTS OF EA A0-53T-12210 AND SRM 51-42-11, PARAGRAPH 7. FOLLOWING THE INSTALLATION OF THE FITTING, IT WAS INSPECTED AND FOUND AC CEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400135 20080324 00135 NM 2008 3 24 08FDEA00924 1 20080313 A 5320 146N54165 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 AFT CARGO FLOOR SUPPORT AT BETWEEN STA 1320-1340, RBL 12, HAS CORROSION AROUND NUT PLATE HOLES. REMOVED CORROSION IAW S RM 51-10-02, L= 2", W= 1", D= .013", ORIGINAL MATERIAL THICKNESS .063". FOUND TO BE OUT OF SRM 53-00-53, FIG 101, SHEET 2 LIMITS. FABRICATED NEW FLOOR SUPPORT ON TRAVELER NR T7/718075 FROM BAC1517-2226. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 53-00-53 AND 51-40-02. THIS IS A MINOR REPAIR WITH NO FOLLOW UP ACTION REQUIRED. 2 L 7 2 4F RT A2NM 2008032400137 20080324 00137 NM 2008 3 24 ASAA0892706 1 20080221 A 5320 143A52409 FLOOR SUPPORT BOEING 737 737990 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 315AS 30019 CABIN FLOORBOARD SUPPORT ANGLE CRACKED AT STA 540 LBL 1. CUT OUT DAMAGED AREA. FABRICATED REPAIR PARTS. INSPECTED JOGGL E AREA FOR CRACKS, NO DEFECTS NOTED. LOCATED DRILLED AND INSTALLED REPAIR ANGLE AND REPAIR PARTS IAW ASA EA5320 01831. 2 L 7 4 4F RT A16WE 2008032400139 20080324 00139 EU 2008 3 24 08FDEA00926 1 20080314 A 5320 A53810771200 FLANGE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CHAFING MARKS ON C 50, P50LH ON AFT FLANGE. REPAIR PERFORMED BY REPLACEMENT OF FLANGE IAW SRM 53-15-87. 2 L 7 2 4F RT A35EU 2008032400140 20080324 00140 EU 2008 3 24 08FDEA00927 1 20080314 A 5753 A57942552 FLAP TRACK AIRBUS A300 A300F4622R 3930360 EU ZONE 500 CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CRACKS FOUND IN HOLE 15 FLAP TRACK BEAM 2 LT. REPAIR PERFORMED BY INSTALLING SB 57-6006 (OVERSIZING AND COLD WORKING OF HOLES), APPROVED BY EO 6-5750-7-3000 PT 1. 2 L 7 2 4F RT A35EU 2008032400141 20080324 00141 NM 2008 3 24 ASAA0892707 1 20080221 A 5320 143A524010 FLOOR SUPPORT BOEING 737 737990 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 315AS 30019 CABIN FLOORBOARD SUPPORT ANGLE CRACKED AT STA 540 RBL 1. CUT OUT DAMAGED AREA. FABRICATED REPAIR PART. NDT INSPECTED JOGGLES FOR CRACKS, NO DEFECTS NOTED. LOCATED DRILLED AND INSTALLED REPAIR ANGLE AND REPAIR PART IAW ASA EA5320 01831. 2 L 7 4 4F RT A16WE 2008032400145 20080324 00145 NM 2008 3 24 SWAA081368 1 20080312 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 20L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032400146 20080324 00146 EU 2008 3 24 08FDEA00929 1 20080314 A 5315 A53970091 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND A DOUBLE HOLE AT CROSSBEAM C 62, Y-405. SPLICE REPAIR PERFORMED IAW. SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2008032400147 20080324 00147 NM 2008 3 24 SWAA081370 1 20080312 A 5322 65446529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 25L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008032000035 20080320 00035 CE 2008 3 20 DXTA200802845 1 20080207 A 2612 FIRE DETECTOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP CARGO BAY FALSE ACTIVATION E DXTA O OTHER N FALSE WARNING DE DESCENT 1 GL 07 893QS 258393 CARGO FIRE WARNING LIGHT COME ON DURING APPROACH. VISUALLY CHECKED THE FWD, UNDERSINK AND AFT SMOKE DETECTORS MOUNTING AREAS FOR SIGN OF BURNED/HEATING PARTS OF THE AC, CHECKED WIRES AND CONNECTORS OF THE SMOKE DETECTORS, NO FAULTS FOUND. CHECKED VISUALLY THE SMOKE DETECTOR AMPLIFIER AND SLIGHTLY TAPPED THE AMPLIFIER, NO FAULT FOUND. CHECKED THE SWITCHES TERMINALS, NO FAULT NOTED. PERFORMED SMOKE DETECTION SYS FUNCTIONAL TEST, CHECKED GOOD, IAW MM ADDENDA ATA 26-11-00. W ORK DONE IAW DWG NR A8-8R-100. REFER TO WO SC1823 ITEM 1.9 FOR DETAILS. 2 L 7 2 4F 4 F RT A3EU E6WE 2008032000063 20080320 00063 CE 2008 3 20 DXTA20082870 1 20080212 A 3230 LANDING GEAR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D1 52060 NE MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 375QS 5600375 UPON RETRACTION OF LANDING GEAR, GEAR UNSAFE LIGHT ILLUMINATED. JACKED AND SWUNG GEAR TEN TIMES WITH NO FAULTS. LUBED A LL UP LOCK ROLLERS AND GEAR. OPS CHECKED GOOD IAW MM CH32-01-00. 2 L 7 2 4F 4 F RT A22CE E1NE 2008032000089 20080320 00089 SO 2008 3 20 FDKA200803100 1 20080307 A 5320 THRESHOLD EMB 145 EMB145LR 3260212 SO DOOR CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 835MJ 145353 SERVICE DOOR THRESHOLD IS CORRODED. THE DAMAGE HAS BEEN REPAIRED. 2 L 7 2 4T RT T00011AT 2008032000100 20080320 00100 CE 2008 3 20 NSVA2008009 1 20080310 A 3230 11438800013 POWERPACK BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 172MJ UE72 AIRCRAFT DECLARED EMERGENCY LANDING GEAR DID NOT EXTEND, CREW PERFORMED CHECKLIST AND MANUALLY EXTENDED GEAR, AIRCRAFT L ANDED SAFELY AND TAXIED TO THE GATE. REPLACED LANDING GEAR POWER PACK IAW MM 32-30-02, OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 2008032000120 20080320 00120 NM 2008 3 20 DL76S080326 1 20080309 A 5297 WIRE BOEING 767 767332 1382001 NM C1 DOOR SHORTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 134DL 25123 ON ARRV, FOUND C1 DOOR WILL NOT OPEN ELECTRICALLY. FOUND C/B TRIPPED ON P34 PANEL. FOUND WIRE IN BUNDLE JUST BELOW P34 HAD RUBBED ON FRAME AND SHORTED. REPAIRED WIRE PER PS DOOR OPS NORMAL. 2 L 7 2 4F RT A1NM 2008031800017 20080318 00017 EU 2008 3 18 08FDEA00859 1 20080310 A 2550 A2557222800600 PANEL AIRBUS 310 A310203 3930313 EU CARGO BAY DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 BULK CARGO PIT PANEL NR 161JW IS PUNCTURED AND DELAMINATED. REPAIRED BULK CARGO PIT IAW DWG SRZ 25-013. PAINTED PANEL IAW DWG SRZ 25-013. 2 L 7 2 4F RT A35EU 2008031800018 20080318 00018 EU 2008 3 18 08FDEA00860 1 20080310 A 2550 A2557386800090 PANEL AIRBUS 310 A310203 3930313 EU AFT CARGO BAY PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT CARGO PIT PANEL NR 152LW IS PUNCTURED. REPAIRED AFT PIT PANEL & TOP COATED (WHITE) IAW DWG SRZ 25-031. 2 L 7 2 4F RT A35EU 2008031800019 20080318 00019 EU 2008 3 18 08FDEA00861 1 20080310 A 5320 A2557238700400 PANEL AIRBUS 310 A310203 3930313 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT CEILING PANEL 162AB OUTER SURFACE IS DELAMINATED AND CRACKED; THE INNER SURFACE HAS PUNCTURED AREAS. REPAIRED I AW DWG SRZ 25-013 & PAINTED. 2 L 7 2 4F RT A35EU 2008031800024 20080318 00024 WP 2008 3 18 08FDEA00866 1 20080311 A 5720 WEDGE DOUG MD10 MD1010F 3022112 WP NR 2 FAIRING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 NR 2 ENGINE AFT FAIRING T/E WEDGE IS CRACKED AT LOWER END IN WORK. 2 L 7 3 4F RT A22WE 2008031800030 20080318 00030 WP 2008 3 18 08FDEA00879 1 20080311 A 3830 111909555 WASTE TANK DOUG DC10 DC1030 3023501 WP LAVATORY LEAKING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 FWD ELECTRONIC COMPARTMENT RIGHT SIDE HAS EVIDENCE OF LEAK; BLUE WATER THROUGHOUT THE E/E COMPARTMENT. REMOVED AND RE PLACED THE LAV TANK ASSY P/N 1-119095-55; S/N 10-52-05 IAW DC-10-30 AMM 38-31-05-02. COMPLIED WITH EA 8-3831-116953 PT 1; " WATER AND WASTE, WASTE DISPOSAL, TOILET TANK VENT LINE, INTERIM REPAIR" DATED 03-10-08. OPS CHECK GOOD IAW DC-10- 30 AMM 38-31-05-2. 2 L 7 3 4F A22WE 2008031800031 20080318 00031 EU 2008 3 18 08FDEA00882 1 20080311 A 5512 FAIRING AIRBUS 310 A310203 3930313 EU HORIZ STAB DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT HORIZONTAL STABILIZER LOWER APRON FAIRING IS DELAMINATED. REAPPLIED ADHESIVE PER SRM 55-15-11; PARAGRAPHS (H) & (I) TO DISBONDED SILICONE MATERIAL. 2 L 7 2 4F RT A35EU 2008031800032 20080318 00032 EU 2008 3 18 08FDEA00883 1 20080311 A 2550 A2557421600500 PANEL AIRBUS 310 A310203 3930313 EU FWD CARGO BAY DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FWD CARGO PIT CEILING PANEL 132GC HAS EXPOSED CORE ON BOTH SIDES OF THE PANEL. REPAIRED PANEL & APPLIED PAINT (WHITE) O N FWD PIT CEILING IAW DRAWING SRZ 25-013. 2 L 7 2 4F RT A35EU 2008031800033 20080318 00033 EU 2008 3 18 08FDEA00884 1 20080311 A 5321 A5327256100000 FLOOR PANEL AIRBUS 310 A310203 3930313 EU FWD CARGO BAY DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FWD CARGO PIT FLOOR PANEL 131RF IS DELAMINATED IN 5 AREAS. FABBED NEW FLOOR PANEL. LOCATED HOLES, POTTED EDGES, CURED EDGE POTTING; INSTALLED INSERTS & APPLIED NON-SKID IAW DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 2008031800034 20080318 00034 EU 2008 3 18 08FDEA00885 1 20080311 A 5321 A5327279000400 FLOOR PANEL AIRBUS 310 A310203 3930313 EU FWD CARGO BAY DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FWD CARGO PIT FLOOR PANEL 132GF HAS EDGE DAMAGE AND IS DELAMINATED. FABRICATED NEW FLOOR PANEL. LOCATED HOLES, POTTED EDGES, CURED EDGE POTTING. INSTALLED INSERTS & APPLIED NON-SKID IAW DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 2008031800041 20080318 00041 NM 2008 3 18 QXEA200800269 1 20080306 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM CARGO BAY CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - C5 - CARGO BAY ENTRYWAY THRESHOLD HAS SEVERAL AREAS OF LIGHT CHAFING. REPAIRED CHAFE BY BLENDING, MAX MATERIAL RE MOVED WAS .005" WITHIN LIMITS REFERENCE TO D-8 200 SRM 51-20-11 . 2 H 7 2 4T RT A13NM 2008031800043 20080318 00043 NM 2008 3 18 HALA0800382 1 20080306 A 5730 SKIN BOEING 767 767332 1382001 NM RT WING CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 LEVEL 1 CORROSION ON RT WING LOWER SURFACE, RIB 8 AFT OF STRINGER L-6, CORROSION ON FASTENER HEADS. AREA PAINT STRIPPED IAW SOPM 20-302, REV 104. LIGHT CORROSION REMOVED FROM FASTENER HEADS BY GLASS BEADING, IAW SRM 51-10-02, REV 76. NEG LIGIBLE MATERIAL REMOVED. SURFACE PROTECTION APPLIED IAW AMM 51-20-10 REV 95. 2 L 7 2 4F RT A1NM 2008031800044 20080318 00044 NM 2008 3 18 HALA0800383 1 20080310 A 3350 LIGHT BOEING 767 7673CB 1385187 NM CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 590HA 33467 FIRST CLASS CROSS AISLE-TRACK LIGHT INOP. REPLACED CROSS AISLE TRACK LIGHT ASSY, LIGHT OPS NORMAL. 2 L 7 2 4F RT A1NM 2008031800050 20080318 00050 WP 2008 3 18 DHLA200800031 1 20080123 A 2612 482449 FIRE DETECTOR DOUG DC8 DC873F 302199F WP NR 1 ENG MALFUNCTIONED A DHLA O OTHER N FALSE WARNING AP APPROACH 1 GL 05 806DH 1811 1811 46002 FLT NR 403, NR 1 ENGINE FIRE WARNING FLASHED A COUPLE OF TIMES DURING FINAL APPROACH LOOP A HANDLE AND MASTER LIGHTS. D EFERRED PER MEL 26-2-3 A-LOOP DMI NR 31485 PLACARD INSTALLED CAT C B-LOOP OPS CK GOOD SP C/W 26-2. T/S SYS IAW MMS 26-1 0-0. REMOVED AND REPLACED 1 DETECTOR NR 1 ENG IAW MMS 26-10-1 RAN NR 1 ENG PER JRH. SYS TESTS GOOD. THIS ACTION CL EARS MDDR NR 31485 PLACARDS, REMOVED AIRCRAFT WAS GROUNDED. SEE PART 1-5 SDR NUMBER DHLA200800008 AND 0030-0034. 2 L 7 4 4F RT 4A25 2008031800051 20080318 00051 WP 2008 3 18 DHLA200800032 1 20080122 A 2612 472450 FIRE DETECTOR DOUG DC8 DC873F 302199F WP NR 1 ENGINE MALFUNCTIONED A DHLA O OTHER N FALSE WARNING AP APPROACH 1 GL 05 806DH 1811 1811 46002 FLT NR 403, NR 1 ENGINE FIRE WARNING FLASHED A COUPLE OF TIMES DURING FINAL APPROACH LOOP A HANDLE AND MASTER LIGHTS. D EFERRED PER MEL 26-2-3 A-LOOP DMI NR 31485, PLACARD INSTALLED CAT C B-LOOP. OPS CK GOOD SP C/W 26-2. T/S SYS IAW MMS 2 6-10-0. REMOVED AND REPLACED 1 DETECTOR NR 1 ENG IAW MMS 26-10-1 RAN NR 1 ENG PER JRH. SYS TESTS GOOD. THIS ACTION CLEARS MDDR NR 31485 PLACARDS REMOVED AIRCRAFT WAS GROUNDED. SEE PART 1-5 SDR NUMBER DHLA200800008 AND 0030-0034. 2 L 7 4 4F RT 4A25 2008031800053 20080318 00053 NM 2008 3 18 MASA200800214 1 20080310 A 5220 SEAL DHAV DHC8 DHC8202 2809007 NM EMERGENCY EXIT DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 445YV 445 ASH 7147 EGE-DEN - CAPTAIN REPORTED LOUD NOISE FROM EMERGENCY EXIT AT ROW 4D. MX CLEANED AND LUBED EXIT DOOR SEAL, OPS GOOD. 2 H 7 2 4T RT A13NM 2008032000129 20080320 00129 NM 2008 3 20 DL757080336 1 20080205 A 5321 FLOOR PANEL BOEING 757 757232 1384965 NM CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 AFT CARGO PANEL 153CF CORRODED, PUNCTURED. FABRICATED PANEL IAW SRM 53-60-53. 2 L 7 2 4F RT A2NM 2008032000177 20080320 00177 EA 2008 3 20 MASA200800168 1 20080226 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 928LR 15028 ASH FLT 2831 PHX-TUS - CAPTAIN REPORTED OVERHEAD EMERGENCY FLOOD LIGHT INOP AT ROW 7. RELAMPED, OPS GOOD. 2 L 7 2 4F RT A21EA 2008032000204 20080320 00204 EU 2008 3 20 08FDEA00770 1 20080306 A 5540 A5547025000000 STRAP AIRBUS 310 A310203 3930313 EU RUDDER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RUDDER L/E PANEL NR 326GL BRIDGING STRAPS ARE CORRODED UNDER THE NUT PLATES. REMOVED AND REPLACED THE BRIDGING STRAPS R EFERENCE FEDEX A310-200 SRM 51-40- 21. 2 L 7 2 4F RT A35EU 2008032100036 20080321 00036 NM 2008 3 21 2008UALA01256 1 20080307 A 3510 MXA1040 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OXYGEN MASK FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 508UA 24744 1ST OBSV O2 MASK EMERGENGY BUTTON STUCK ON. REPLACED SWITCH, OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100048 20080321 00048 EU 2008 3 21 08FDEA00845 1 20080310 A 5311 A53973178274 FRAME AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT FUSELAGE FRAME HAS CORROSION ON THE WEB AT FRAME 65 BETWEEN STR 49L AND 50L. REMOVED CORROSION IAW SRM 51-74-10 . CHECKED LIMITS IAW SRM 53-17-12. FOUND TO BE WITHIN LIMITS. ALODINED IAW SRM 51-21-10. PRIMED AND PAINTED BOTH IAW SRM 51-23-10. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008032100049 20080321 00049 NM 2008 3 21 DHLA200800029 1 20080311 A 3350 1000647 LIGHT BOEING 727 727214 138407R NM L1 DOOR DEFECTIVE A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 786AT 21692 FWD ENTRY L1 DOOR EMERGENCY LIGHT ASSY "ON" IN ARM POSITION, WOULD NOT TURN OFF. REMOVED AND REPLACED FWD ENTRY DOOR EM ERGENCY LIGHT ASSY IAW MM 33-50-101. OPS CKS NORMAL PER MM 33-50-01. AIRCRAFT WAS GROUNDED. 2 L 7 3 4F A3WE 2008032100065 20080321 00065 2008 3 21 2008UALA01309 4 20080307 A 2310 4998220330001 TRANSCEIVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT HF INTERMITTENT A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 548UA 25396 LEFT HF INTERMITTENT, PER CHIDD. PER IB CREW: TX AND RX VERY GARBLED. REPLACED LT HF TRANSCEIVER, OPS & SELCAL CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100066 20080321 00066 NM 2008 3 21 2008UALA01320 1 20080310 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 5F INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 SEAT EEL INOP, 5F AFT SECTION. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032100067 20080321 00067 NM 2008 3 21 2008UALA01322 1 20080310 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 58L INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 SEAT EEL INOP: 58L. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032100068 20080321 00068 NM 2008 3 21 2008UALA01323 1 20080308 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 504UA 24625 EEL LIGHT STRIP INOP IN FRONT OF MID AFT LAV. FOUND EEL STRIP DAMAGED BY PASSENGER. REPAIRED EEL STRIP, OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032400006 20080324 00006 NM 2008 3 24 WRLA2008027 1 20080311 A 7110 NOSE COWL DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE NR 3 ENGINE DEBONDED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 48407 DURING C-CHECK INSPECTION NR 3 ENGINE NOSE COWL INNER BARREL COMPOSITE DISBONDED. REF EGAT NR U02006. REPAIRED NR 3 E NGINE INLET COWL DISBONDED AREA IAW ERA 087123. 2 L 7 3 4F 4 F RT A22WE E24NE 2008032400026 20080324 00026 NM 2008 3 24 PIDA08011 1 20080307 A 3350 900542 BATTERY PACK BOEING 737 7372K5 138448X NM CABIN DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 249TR 22598 AT THE COMPLETION OF MAINTENANCE CHECK, NOTED SEAT MOUNTED EMERGENCY EXIT LIGHTING AND OVERHEAD "BULL NOSE" EMERGENCY LI GHT INOP. REPLACED BATTERY PACKS AND OPS CHECKED LIGHTING PER MM 33-51-81. 2 L 7 2 4F RT A16WE 2008032400047 20080324 00047 WP 2008 3 24 08FDEA00978 1 20080317 A 5730 ARC06231 PANEL DOUG MD10 MD1010F 3022112 WP LT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LT WING LOWER SURFACE HINGED PANEL 551 DB UPPER SURFACE IS GOUGED AND BENT ON THE AFT MID SECTION. REPAIRED IAW SRM 51-7 1-00 VOL II. ALODINED & PRIMED REPAIR AREA IAW SRM 51-21-01 VOL II. SEALED REPAIR IAW SRM 51-71-00 & 51-71-01 VOL II . PAINTED REPAIR IAW SRM 51-21-01 VOL II. REMOVED & INSTALLED THE SEAL RETAINER & PANEL 551 DB IN REF TO SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2008032400099 20080324 00099 SW 2008 3 24 WGEA200800044 1 20080302 A 2711 271096691005 SPRING ECLIPS EA500 ECLIPSEEA500 3350000 SW AILERON TRIM DAMAGED E WGEA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 EA 27 142DJ 78 000056 REPLACED AILERON TRIM SPRING WITH NEW TRIM SPRING IAW AMM 27-11-20. PERFORMED AILERON TRIM SYSTEM ADJUSTMENT/TES IAW AM M 27-00-01. SYSTEM TEST AND CHECKS GOOD, NO DEFECTS NOTED. ITEM 1. FLIGHT WAS UNSATISFACTORY. AT 220KTS 82 PERCENT OF TRIM WAS REQUIRED TO MAINTAIN STRAIGHT AND LEVEL FLIGHT. AT 160 KTS 30 PERCENT TRIM (AILERON TRIM) WAS REQUIRED. P ERFORMED FLAP RIGGING IAW AMM 27-50-00 AND EA TSR 27-030408G. RIG CHECKED GOOD. VERIFIED FLAPS ARE AT 0 PERCENT. EVAL UATION FLIGHT UNSATISFACTORY. AT 250 KTS REQUIRES AILERON TRIM IN EXCESS OF 101 PERCENT LWD. AT 220 KTS, 37 PERCENT L WD. AT 160 KTS, 23 PERCENT LWD. FOUND RT FLAP TO HAVE EXCESSIVE PLAY, ADJUSTED FLAP IAW AMM 27-50-00. FLAPS OPERATE 1 L 7 2 4J RT A00002AC 2008032400102 20080324 00102 WP 2008 3 24 IXXA08SMN044S 1 20080201 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING RIGHT INBOARD FLAP UPPER SKIN HAS DENTS BETWEEN STATION XW 3.000 AND XW 91.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE PANEL PLATING. FABRICATED NEW SKIN, AND DOU BLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS A ND REPAIR PARTS IAW DC8 SRM 51-1-11, DC8 SRM 57-7-1 FIGURE 1, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, SRM 57-7-1 FIGURE 1 ITEM "A" AND "L", DC8 SRM 51-1-9 T/R 51-142, DC8 SRM 51-1-9A T/R 51-141, DC8 SRM 51-1-8B, 2 L 7 4 4F RT 4A25 2008032400103 20080324 00103 EU 2008 3 24 F3LA200800097 1 20080302 A 5315 D53974967000 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE AFT CARGO COMPARTMENT FLOOR FRAME PLATE AT FRAME 59 . MAINTENANCE REMOVED AND REPLACED THE PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11, PARAGRAPHS 5 AND 6. FOLLOWING COMPLETION OF THE PLATE REPLACEMENT, THE NEW PLATE WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400104 20080324 00104 EU 2008 3 24 F3LA200800098 1 20080302 A 5315 D5391215720000 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE AFT CARGO COMPARTMENT FLOOR FRAME PLATE AT FRAME 56 . MAINTENANCE REMOVED AND REPLACED THE PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. FOLLOWING COMPL ETION OF THE PLATE REPLACEMENT, THE NEW PLATE WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400105 20080324 00105 EA 2008 3 24 CHQA200800049 1 20080312 A 2133 VP1257C00 OUTFLOW VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CABIN AIR MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 639BR 13696 7313 GEE872507 IAH TO CMH - AFTER TAKEOFF, THE AIRCRAFT WOULD NOT PRESSURIZE AND AN OVERBOARD COOL MESSAGE WAS DISPLAYED ON EICAS. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAULT TO THE OVERBOARD EXHAUST SHUTOFF VALVE. THE VALVE WAS PLACED ON MEL AND THE PRESSURIZATION SYSTEM, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2008032400106 20080324 00106 WP 2008 3 24 IXXA08SMN051S 1 20080207 A 5522 SKIN DOUG DC8 DC871F 302199D WP RT ELEVATOR MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR UPPER SKIN SHOWS IMPROPER REPAIR AT STATION XE 50.000 TO XE 132. 000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. BALANCED RIGHT ELEVATOR. FOUND MOMENT WITHIN TOLERANCE 1449.3 INCH POUND. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, DC8 SRM 51-1-2 1, DC8 SRM 55-4-1 FIGURE 1 SHEET 1 AND 2 ITEMS "E" AND "F", DC8 SRM 55-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 51-1-9 T/R 5 1-142, DC8 SRM 51-1-9A T/R 51-141, DC8 SRM 51-1-8B, DC8 SRM 51-4-4 PAGE 2 AND 3, AND T/R 51-116 DATED 11/03/00. 2 L 7 4 4F RT 4A25 2008032400108 20080324 00108 EA 2008 3 24 SWIA200819343 1 20080312 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA GALLEY LOOSE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 755SK 10220 FLOOR LEVEL EMERGENCY LIGHT IN GALLEY IS LOOSE. REPLACED FLOOR LEVEL EMERGENCY LIGHT IAW CRJ MM 33-51-04. 2 L 7 2 4F RT A21EA 2008032400110 20080324 00110 EA 2008 3 24 SWIA200819345 1 20080310 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 427SW 7497 FLT 3830 - LEFT FORWARD CABIN DOOR EMERGENCY EXIT SIGN LENS IS CRACKED. REPLACED FIXTURE BASE AND LENS COVER ASSEMBLY P ER MM 33-51-19. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008032400115 20080324 00115 WP 2008 3 24 IXXA08SMN061S 1 20080208 A 5340 3640887U FITTING DOUG DC8 DC871F 302199D WP BS 960-980 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CORRODED AT STATION 960.000 TO STATION 980.000 L EFT BUTTOCKS LINE 45. REMOVED CORRODED FITING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51 -1-20D, DC8 SRM 51-3-1, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008032400116 20080324 00116 EA 2008 3 24 COMA0860164 1 20080310 A 5320 60034017351 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 957CA 7109 DURING HMV NR 6 INSPECTION, VISUAL INSPECTION FOUND FLOOR DECK SUPPORT ANGLE CRACKED AT FS 280. REMOVED AND REPLACED SU PPORT ANGLE PER CRJ SRM 51-42-21 AND SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008032400152 20080324 00152 2008 3 24 SWAA081358 4 20080312 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED C1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032400154 20080324 00154 NM 2008 3 24 SWAA081376 1 20080312 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 417WN 29822 DURING SCHEDULED 6Y CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 77 AND STA 79. REPAIRED SKIN P ER SRM. 2 L 7 2 4F RT A16WE 2008032400155 20080324 00155 EU 2008 3 24 08FDEA00934 1 20080314 A 5730 A5351063200000 PANEL AIRBUS 310 A310203 3930313 EU LT WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LEFT WING PANEL 577 BT IS DELAMINATED IN NUMEROUS PLACES. REMOVED DAMAGED; PREPED FOR BOND, LAYED UP, VAC BAGGED & CUR ED REPAIR IAW SRM 51-77-12 & 51-77-10. RESTORED PROTECTIVE FINISH IAW SRM 51-75-10. 2 L 7 2 4F RT A35EU 2008032400158 20080324 00158 NM 2008 3 24 SWAA081360 1 20080312 A 3350 417A5600201 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 430WN 33659 DURING SCHEDULED CV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008032400159 20080324 00159 EU 2008 3 24 08FDEA00937 1 20080314 A 5320 A2557238700400 PANEL AIRBUS 310 A310203 3930313 EU INTERIOR DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT CEILING PANEL 162 AB OUTER SURFACE IS DELAMINATED AND CRACKED; THE INNER SURFACE HAS PUNCTURED AREAS. REPAIRED CEILING PANEL 162 AB FOR THE AFT PIT IAW DWG SRZ 25-013 AND PAINTED (WHITE). 2 L 7 2 4F RT A35EU 2008032400161 20080324 00161 EU 2008 3 24 08FDEA00939 1 20080314 A 5540 NSA1500006C BEARING AIRBUS 310 A310203 3930313 EU RUDDER HINGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RUDDER HINGE ARM NR 6; RUDDER BEARINGS ARE CORRODED. REMOVED 3 BEARING ASSEMBLIES. CLEANED AND INSPECTED HINGE ARM. R EPLACED BEARING ASSEMBLIES IAW A310 200 AMM 53-36-11-08, P/N OF THE BEARING ASSEMBLIES ARE AS FOLLOWS, NSA5100-006C; NSA 8130-08 AND A5537014020000. 2 L 7 2 4F RT A35EU 2008032400162 20080324 00162 EU 2008 3 24 08FDEA00940 1 20080314 A 5755 STRUCTURE AIRBUS 310 A310203 3930313 EU NR 4 SPOILER CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT WING NR 4 SPOILER; OUTBD EDGE IS CHAFED AND WORN. NO DAMAGE NOTED TO INDER LYING CFRP STRUCTURE AT THE OUTBOARD END OF THE RT WING NR 4 SPOILER IAW SRM 57-70-00 & 51-10-10. APPLIED SURFACE PROTECTION IAW SRM 51-75-10. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008032400164 20080324 00164 EU 2008 3 24 08FDEA00942 1 20080314 A 5753 A5796512000751 FAIRING AIRBUS 310 A310203 3930313 EU TE FLAP ERODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 5 RT WING FLAP FAIRING HAS NUMEROUS SPOTS OF EROSION AND CHIPPED PAINT. PAINTED IAW AMM 51-75-10-8. 2 L 7 2 4F RT A35EU 2008032400165 20080324 00165 EU 2008 3 24 08FDEA00943 1 20080314 A 5320 A2557238100000 PANEL AIRBUS 310 A310203 3930313 EU INTERIOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT CEILING PANEL 162 DC HAS EXPOSED COMPOSITE CORE AND IS CRUSHED. REPAIRED AFT PIT CEILING BY APPLYING A FIBERGLA SS OVERALL IAW SRZ 25-013 & RESTORED THE FINISH IAW SRZ 25-013. 2 L 7 2 4F RT A35EU 2008032400170 20080324 00170 WP 2008 3 24 08FDEA00948 1 20080314 A 5330 ABA75181 SKIN DOUG MD10 MD1010F 3022112 WP BS 278-323 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 EXTERNAL FUSELAGE SKIN JUST BELOW THE WINDSHIELD AND SLIDING WINDOW HAS A DENT BETWEEN STA 278 AND 323; RT SIDE. COMPLI ED WITH EA 8-5330-118447. 2 L 7 3 4F RT A22WE 2008032400173 20080324 00173 EU 2008 3 24 08FDEA00950 1 20080314 A 5730 A57151559 SKIN AIRBUS 310 A310324 3930206 EU RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 RIGHT WING UPPER SURFACE SKIN HAS AREAS OF CORROSION ALONG FRONT SPAR ATTACH ROW STA 556-565. REMOVED CORROSION IAW SRM 51-74-10 & WAS FOUND TO BE OUT OF LIMITS. ACCOMPLISHED HFEC OF HOLES IAW NTM 51-10-01. FLAT PEENED AREA IAW SRM 51-25-0 0. ALODINED IAW SRM 51-21-10. PRIMED IAW SRM 51-21-00. PAINTED IAW 51-21-00. REPLACED FASTENERS IAW SRM 51-40-21. MIN OR REPAIR. 2 L 7 2 4F RT A35EU 2008032400177 20080324 00177 NM 2008 3 24 QXEA200800284 1 20080306 A 5340 BRACKET DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - C5 - MCD SURROUND FWD END OF SILL PLATE BRACKET FOR SILL PLATE CORRODED AGAINST FUSELAGE. REMOVED THE MCD THRESHO LD BY DRILLING OUT THE RIVETS HOLDING THE THRESHOLD TO LOWER SILL PLATE, REMOVED NUTPLATES FROM THE LOWER SILL PLATE. B LENDED OUT CORROSION FROM AFFECTED AREA OF SILL PLATE. NEGLIGIBLE MATERIAL REMOVED, WITHIN LIMITS PER SRM 51-20-11. HFE C INSPECTED BLENDED AREA FOR CRACKS IAW -8/200 NDTM PART 6, 51-00-01. REINSTALLED MCD THRESHOLD TO SILL PLATE AND INSTA LLED NEW (5EA) NUTPLATES PER Q-200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008032400179 20080324 00179 WP 2008 3 24 IXXA08SMN078S 1 20080215 A 5751 SKIN DOUG DC8 DC871F 302199D WP RT AILERON DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD AILERON UPPER SKIN HAS DENT AND NO STANDARD REPAIR AT STATION XA 580.000 TO XA 610.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, AND D OUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIRED PARTS. BALANCED AND FOUND MO MENT WITHIN LIMITS MOMENT: 3331.3 INCH POUND. INSTALLED NEW FASTENERS AND REPAIRED PARTS IAW DC8 SRM 51-1-11, DC8 SRM 5 7-8-1 FIGURE 1, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 57-8-1 FIGURE 4 ITEM "B" AND "K", DC8 SRM 51-1-9 T/R 51- 142, DC8 SRM 51-1-9A T/R 51-141, DC8 SRM 51-1-8B, AND DC8 SRM 51-4-1 PAGE 1 AND 2, 2 L 7 4 4F RT 4A25 2008032400180 20080324 00180 NM 2008 3 24 SWAA081371 1 20080312 A 5315 65C34059 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 31 TO LBL 45. REPAIRED FLOORBEAM PER ER. 2 L 7 2 4F RT A16WE 2008032400181 20080324 00181 NM 2008 3 24 QXEA200800285 1 20080306 A 5340 ATTACH FITTING DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - C5 - MCD LAY SHAFT FWD AND AFT GOOSE NECK ATTACH FITTINGS ARE PITTING AND CORRODED. REMOVED MCD LAY SHAFT REF -8/ 200 AMM 52-10-00FIG 501 SHEETS (3&4). REMOVED BOTH FWD AND AFT HINGE FITTINGS FROM FWD AND AFT TUBE ASSEMBLIES REF -8/2 00 SRM 51-40-11. INSTALLED NEW HINGE FITTINGS ON FWD AND AFT END OF TUBE ASSEMBLY REF -8/200 SRM 51-40-00. INSTALLED M CD LAY SHAFT. 2 H 7 2 4T RT A13NM 2008032400182 20080324 00182 EU 2008 3 24 F3LA200800105 1 20080302 A 5311 D53974966000 FRAME AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE ZONE 100 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE AFT CARGO COMPARTMENT FRAME PLATE AT FRAME 61. MAI NTENANCE REMOVED AND REPLACED THE FRAME PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPHS 5 AND 6. FOLLOWING COMPLETION OF THE PLATE REPLACEMENT, THE NEW PLATE WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400183 20080324 00183 EU 2008 3 24 AALA200800480 1 20080303 A 3350 BR9662103 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70054 461 JFK - EMERGENCY LIGHT JUST FORWARD OF LEFT NUMBER TWO DOOR DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT JUST FO RWARD OF LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008032400184 20080324 00184 NM 2008 3 24 SWAA081366 1 20080312 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400188 20080324 00188 NM 2008 3 24 SWAA081367 1 20080312 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 790SW 30604 EEPLS LENS MISSING AT ROW 15 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008032400192 20080324 00192 NM 2008 3 24 AALA200800481 1 20080303 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 771AN 29579 DFW - EMERGENCY LIGHT AT SEAT 21C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032400198 20080324 00198 WP 2008 3 24 AALA200800477 1 20080303 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 289AA 49301 JFK - EMERGENCY LIGHTS AT SEAT ROWS 20DEF TO 32DEF INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD 20DEF FOR EMERGENCY L IGHTS AT SEAT ROWS 20DEF TO 32DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008032400199 20080324 00199 EU 2008 3 24 2008UALA01354 1 20080312 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 451UA 865 THE O2 NEEDS SERVICING SHOWS 1420. SERVICED CREW O2 TO FULL, NO LEAKS NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031800056 20080318 00056 WP 2008 3 18 DHLA200800033 1 20080122 A 2612 472451 FIRE DETECTOR DOUG DC8 DC873F 302199F WP NR 1 ENGINE MALFUNCTIONED A DHLA O OTHER N FALSE WARNING AP APPROACH 1 GL 05 806DH 3651 3651 46002 FLT NR 403, NR 1 ENGINE FIRE WARNING FLASHED A COUPLE OF TIMES DURING FINAL APPROACH LOOP A HANDLE AND MASTER LIGHTS. D EFERRED PER MEL 26-2-3 A-LOOP DMI NR 31485 PLACARD INSTALLED CAT C B-LOOP. OPS CK GOOD SP C/W 26-2. T/S SYS IAW MMS 26 -10-0. REMOVED AND REPLACED 1 DETECTOR NR 1 ENG IAW MMS 26-10-1 RAN NR 1 ENG PER JRH. SYS TESTS GOOD. THIS ACTION CLEARS MDDR NR 31485 PLACARDS REMOVED AIRCRAFT WAS GROUNDED. SEE PART 1-5 SDR NUMBER DHLA200800008 AND 0030-0034. 2 L 7 4 4F RT 4A25 2008031800059 20080318 00059 EA 2008 3 18 MASA200800217 1 20080310 A 3350 BATTERY CNDAIR CL600 CL6002D24 1390016 EA CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 908FJ 15008 ASH FLT 2785 OKC-PHX - EMERGENCY LIGHTS INOP. MX CHARGED BATTERIES, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008031800060 20080318 00060 NM 2008 3 18 QXEA200800276 1 20080306 A 5320 CHANNEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - C5 - LOWER FORWARD EMERGENCY EXIT THRESHOLD CHANNEL PN 85320693 REQUIRES REPLACEMENT IN ACCORDANCE WITH EA 2-53-73 3 PERMANENT REPAIR FOR DENT IN CHANNEL. REMOVED FLOORBOARD SUPPORT CHANNEL ASSEMBLY AFT OF EMERGENCY EXIT AND EXIT THRE SHOLD COVER PLATE. VERIFIED DEPTH OF DENT TO BE .055" DEEP. HFEC IAW -8 200 NDTM PART 6 51-00-01, NO CRACK NOTED. INS TALL THRESHOLD COVER PLATE IAW Q400 SRM 51-40-00. REINSTALLED FLOORBOARD SUPPORT CHANNEL IAW -8 200 SRM 51-40-00, 51-40 -11. 2 H 7 2 4T RT A13NM 2008031800074 20080318 00074 WP 2008 3 18 08FDEA00894 1 20080311 A 5751 SKIN DOUG MD10 MD1010F 3022112 WP RT AILERON DEPARTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RT OUTBD AILERON UPPER SKIN HAS NUMEROUS DENTS. MEASURED DEPTH IS .056. FOUND TO BE WITHIN LIMITS IAW SRM 51-80-01; PROCEDURE "F" PG 1 VOL II. MINOR REPAIR 2 L 7 3 4F RT A22WE 2008031800080 20080318 00080 WP 2008 3 18 IXXA08SMN055S 1 20080207 A 5320 4750419U501 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FORWARD FITTING CRACKED AT STATION 759.000 LONGERON 11 R IGHT. REMOVED (CRACKED) FITTING. CLEANED, TREATED AND PRIMED AREA INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008031800081 20080318 00081 EU 2008 3 18 UPS08151791 1 20080311 A 5200 LINER AIRBUS A300 A300F4622R 3930360 EU DOOR LOOSE A IPXA K NONE J WARNING INDICATION NR NOT REPORTED 1 SO 01 138UP 0821 CREW ENTRY DOOR SLIDE WARNING SOUNDING IN FLIGHT. FOUND GUIDE ARM LINING LOOSE AND MISSING HARDWARE. LINING WAS INTERF ERING WITH DOOR CLOSING. INSTALLED HARDWARE AND LINING IAW 52-10-13-04. PRESS A/C IAW 21-31-00-5. NO DEFECTS NOTED. PERF ORMED TEST OF MAIN ENTRY DOOR WARNING HORN IAW 52-43-12-04. NO DEFECTS NOTED. 2 L 7 2 4F RT A35EU 2008031800082 20080318 00082 WP 2008 3 18 UPS08851767 1 20080301 A 5720 DOUBLER DOUG DC8 DC873F 302199F WP LT WING BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 PIECE OF INTERNAL DOUBLER BROKEN, MISSING AT OB END OF LT WING OUTER L L/E. REMOVED BROKEN DOUBLER, FABBED AND INSTALLED REPLACEMENT INTERNAL DOUBLER AT OB END OF LW OUTER LE IAW SRM 51-1-21, 51-1-8, 51-3-2. 2 L 7 4 4F RT 4A25 2008031800083 20080318 00083 WP 2008 3 18 UPS08851769 1 20080301 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 AFT END OF INNER RIB CRACKED IN LT WING OB L/E IB SECTION NEAR STA X FS 609, UPPER STOP DRILLED CRACK , FABBED AND INSTALLED REPAIR DOUBLERS ON L/W OB LEADING EDGE UPPER RIB AT XFS609 IAW SRM 57-3-3 FIG 6, SRM 57-2-0 FIG 2 , 51-1-8 2 L 7 4 4F RT 4A25 2008031400079 20080314 00079 WP 2008 3 14 AALA200800461 1 20080301 A 2161 SYLZ52876 CONTROLLER DOUG DC9 DC982 3022082 WP LT A/C PACK INOPERATIVE A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 232AA 49179 DFW INFLIGHT T2459/01MAR - LEFT AIR CONDITIONING PACK TEMPERATURE HIGH INDICATION AND PNEUMATIC PRESSURE MAXED OUT. RET URNED TO DFW AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE FOR EVALUATION. REPLACED TEMPERATURE SENSOR AN D CONTROLLER. FOUND WIRE PULLED OUT OF CONNECTOR ON PRESSURE REGULATOR. REPAIRED CONNECTOR WIRE ON PRESSURE REGULATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031400080 20080314 00080 NM 2008 3 14 AALA200800462 1 20080301 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 629AA 24587 DFW EMERGENCY SPOT LIGHT AT SEAT 18F INOPERATIVE. REPLACED LAMP FOR EMERGENCY SPOT LIGHT AT SEAT 18F. SYSTEM GROUND C HECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A2NM 2008031400090 20080314 00090 NM 2008 3 14 F3LA200800082 1 20080229 A 5320 D5347112320200 SUPPORT ANGLE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B6P 13018 NE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED THE LEFT, SHEAR PLATE SUPPORT ANGLE, LOCATED BETWEEN FRAMES 69 AND 70, SHOWED SIGNS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE SHEAR PLATE SUPPORT ANGLE, LOCATED BETWEEN FRAMES 69 AND 70, I N ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPH 6. FOLLOWING COMPLETION OF THE INSTALLATION, THE ANG LE WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008031400098 20080314 00098 NM 2008 3 14 2008UALA01230 1 20080306 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 POSSIBLE FUSELAGE CRACK LT SIDE AFT OF WING BODY FARING, BELOW OVERWING ESCAPE LIGHT. MAJOR REPAIR ACCOMPLISHED: REPLAC ED THE LT AFT SKIN. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031700011 20080317 00011 NM 2008 3 17 2008UALA01245 1 20080307 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY EXIT SIGN INOP:LT SIDE FWD GALLEY. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031700013 20080317 00013 NM 2008 3 17 2008UALA01248 1 20080307 A 3397 80603 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 WALL EEL INOP, LT SIDE LAV 111. REPLACED FEEDER CABLE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031700022 20080317 00022 NM 2008 3 17 GTIA0800038 1 20080305 A 2560 A3061402 MEGAPHONE AIRBUS A319 A319132 3930340 NM CABIN INOPERATIVE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 528NK 2983 AFT MEGAPHONE INOP. SIREN WILL NOT GO OFF. 2 L 7 2 4F RT A28NM 2008032400200 20080324 00200 NM 2008 3 24 2008UALA01355 1 20080311 A 5230 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 AFT CARGO DOOR FWD FRAME LOWER CORNER IS CRACKED AT FASTENER HOLE NEXT TO LOWER STOP FITTING. MAJOR REPAIR ACCOMPLISHED : REPLACED FRAME. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032400202 20080324 00202 2008 3 24 ASAA0852708 4 20080313 A 2310 8220990004 TRANSCEIVER BOEING 737 737890 1384527 NM HF COMM FAULTY A ASAA K NONE O OTHER NR NOT REPORTED 1 NM 02 570AS 35185 HF 2 DOES NOT TRANSMIT. NR 2 HF DOES NOT TRANSMIT ON 10 MEGS BUT VOICE HEARD ON 13 MEGS. REPLACED NR 2 HF TRANSCEIVER. OP CHECKS GOOD. 2 L 7 2 4F RT A16WE 2008032400207 20080324 00207 NM 2008 3 24 SWAA081382 1 20080313 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 DURING SCHEDULED HC2 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008032400208 20080324 00208 NM 2008 3 24 SWAA081383 1 20080313 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008032400209 20080324 00209 WP 2008 3 24 IXXA08SMN079S 1 20080215 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD AFT LOWER FLAP SKIN SHOWS DENTS AT STATION XE 2.000 TO STA XE 91.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDE D PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIRED PARTS. INSTALLED NEW FASTENERS AND REPAIRE D PARTS IAW SRM 51-1-11, SRM 57-1-0 PAGE 1, SRM 51-1-21, SRM 57-7-1 FIG 1 ITEMS "B" AND "L", SRM 51-1-9 T/R 51-142, SRM 51-1-9A T/R 51-141, AND SRM 51-1 8B. 2 L 7 4 4F RT 4A25 2008032400210 20080324 00210 NM 2008 3 24 SWAA081384 1 20080313 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 DURING SCHEDULED HC2 CHECK, LT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008032400213 20080324 00213 EU 2008 3 24 F3LA200800106 1 20080229 A 5315 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED SHEARED FASTENERS WERE FOUND WHERE THE LEFT SUPPORT BEAM, BETWEEN FRAMES 68 AN D 69, CONNECTS TO FLOORBEAM Y1292. MAINTENANCE REMOVED THE SHEARED FASTENERS. NEW FASTENERS WERE INSTALLED IN ACCORDAN CE WITH THE REQUIREMENTS OF EA A9-53R-30090, REVISION ORIGINAL, AND A319 SRM 51-42-11, PARAGRAPH 7. WHEN COMPLETED, THE INSTALLATION WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400220 20080324 00220 NM 2008 3 24 SWAA081389 1 20080313 A 5330 65C381921 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400249 20080324 00249 NM 2008 3 24 SWAA081393 1 20080313 A 3350 3071BPEGPL LIGHT BOEING 737 73776Q 13845AA NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 551WN 30280 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 20 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008032400251 20080324 00251 NM 2008 3 24 SWAA081406 1 20080313 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032400253 20080324 00253 NM 2008 3 24 SWAA081394 1 20080313 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400269 20080324 00269 NM 2008 3 24 SWAA081413 1 20080316 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032400277 20080324 00277 NM 2008 3 24 2008UALA01366 1 20080311 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 AFT PIT STA 1088 BETWEEN STR 39L AND STR 39R, SKIN IS CORRODED. MAJOR REPAIR ACCOMPLISHED @ GSO: REMOVED DAMAGED AREA FA BRICATED REPAIR AND INSTALLED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032400278 20080324 00278 NM 2008 3 24 2008UALA01367 1 20080311 A 3350 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN EXPOSED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 EMERGENCY LIGHT STRIP ON FLOOR ROW 14B IS PULLED UP W-WIRES SHOWING. REPAIRED LIGHT BAR OPS CHECKED GOOD. AC OK FOR SERV ICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032400279 20080324 00279 NM 2008 3 24 HALA0800389 1 20080310 A 5314 KEELBEAM BOEING 767 767332 1382001 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 CORROSION ON KEELBEAM TEE PIECES AT AFT EDGE OF PANEL 139AL,139BL, AND 139CL CORRODED AROUND NUTS QTY 3. CORROSION NOTE D EXCESSIVE. TEE SECTIONS (3) INSTALLED ON KEEL BEAM IAW 51-40-02 SRM. 2 L 7 2 4F RT A1NM 2008032400281 20080324 00281 NM 2008 3 24 HALA0800397 1 20080313 A 5512 SKIN BOEING 767 767332 1382001 NM HORIZONTAL STAB DENTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 SUP - RT HORIZONTAL STAB HAS 3X L/E DENTS, NOT IN A/C DAMAGE REGISTER. PERMANENT SRM REPAIR CARRIED OUT IAW SRM 51-70-1 0, REPAIR 2 REF TI 190113615-0001 AND HAL FILE NR 594051. 2 L 7 2 4F RT A1NM 2008032000173 20080320 00173 WP 2008 3 20 08FDEA00918 1 20080313 A 5710 ARB1180 TEE FITTING DOUG DC10 DC1030F 3023504 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 307FE 48291 RT WING L/E INT ZONE FOUND CRACK ON FIXED TEE CAP. REPAIRED TEE CAP IAW SRM 57-10-00 VOL I FIG 49. 2 L 7 3 4F RT A22WE 2008032000174 20080320 00174 SO 2008 3 20 LR7A08041 1 20080311 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FS 846 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 652 4763 DURING SCHEDULED B-1 CHECK, PER JOB CARD HB5302, FOUND CABIN BHD CRACKED AT FS 846, WL170, RBL73. REPAIR ACCOMPLISHED I AW SMP583 FIG 53-50-10. 2 H 7 4 4T A1SO 2008032000186 20080320 00186 NM 2008 3 20 UPS08M51799 1 20080302 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 7 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED A ND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944 2 L 7 3 4F RT A22WE 2008032100020 20080321 00020 NM 2008 3 21 2008UALA01207 1 20080305 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 SEAT 8GH FWD EMERGENCY LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032100025 20080321 00025 NM 2008 3 21 2008UALA01224 1 20080305 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 580UA 26698 CREW REPORT: DOOR 4R WILL NOT ARM. FOUND DEBRIS UNDER GIRT BAR AREA. CLEANED AND LUBED GIRT BAR, SLIDER AND OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100040 20080321 00040 2008 3 21 YENA2008020 4 20080307 A 3444 066500070212 TRANSCEIVER AIRBUS 320 A320232 3930326 EU RADIO ALTIMETER FAILED A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 629JB 21508 9586 2580 FLT 369, LGA-PBI, ON CLIMBOUT OF 1000', ECAM "LDG GEAR NOT DOWN", AURAL WARNING "RETARD", CAPTS RA INDICATED -3, NO RA F AULT ON ECAM, 10 MINS LATER F/O'S RA IND -3, PROBLEM CLEARED 15 MINS LATER. DIVERTED TO JFK. PER PFR RAI SYST FAILED. ALL CHECKS ON RA1 NORMAL. PRECAUTION T/S REMOVED AND REPLACED NR 1 RADIO ALTM R/T PER AMM 34-42-33-04, CHECKS OK. REM OVED AND REPLACED R/A XTMIT AND REC ANTENNAS 5SA1 & 52A2 PER AMM 34-42-11-04, CHECK SECURITY OF R/A ANT CONNECTORS. ALL CHECKS OK. 2 L 7 2 4F RT A28NM 2008032400001 20080324 00001 EU 2008 3 24 08FDEA00916 1 20080313 A 5414 A5461128900000 PANEL AIRBUS 310 A310203 3930313 EU NR 1 NACELLE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 1 PYLON PANEL NR 414 GR IS CORRODED AROUND THE SCREW HOLES. REMOVED THE CORROSION IAW SRM 51-74-10. ORIGINAL MAT TH ICKNESS .079 IAW SRM 54-52-51; PG 12. REMOVED .059; .020 MAT REMAINING. OUT OF LIMITS IAW SRM 54-52-51; FIG 101. FABBE D FILLER/DOUBLER AND REMOVED DAMAGE IAW SRM 54-52-51; FIG 203. ALODINED FILLER/DOUBLER IAW SRM 51-21-10. PRIMED FILLER /DOUBLER IAW SRM 51-23-10. PAINTED FILLER/DOUBLER IAW SRM 51-23-10. INSTALLED FILLER/DOUBLER IAW SRM 54-52-51;FIG 203. 2 L 7 2 4F RT A35EU 2008032400003 20080324 00003 EU 2008 3 24 08FDEA00919 1 20080313 A 5414 A5461143200000 ACCESS PANEL AIRBUS 310 A310324 3930206 EU NR 1 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 NR 1 PYLON, LEFT SIDE THRU ACCESS PANEL 413EL THE INTERNAL WEBBING IS CRACKED AT A PREVIOUS WELD. REMOVED INTERNAL DOUB LER IAW SRM 51-40-21; PG 7. PART MARKED IAW GMM 7-0-1001. INSTALLED IAW SRM 51-40-21; PG 7. MINOR REPAIR 2 L 7 2 4F RT A35EU 2008032400004 20080324 00004 EU 2008 3 24 F3LA200800089 1 20080303 A 5320 D53112191203 SILL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND AT THE R-1 DOOR SILL FITTING AT THE AFT 2 NUT PLACE HOLES AT THE GIRT BAR FITTING ATTACH POINT. REMOVED CORROSION FROM THE R-1 DOOR SILL FITTING IN ACCORDANCE WITH THE REQUIREME NTS OF A319 SRM 51-47-00 AND EA A9-53R-30097. UPON COMPLETION OF THE REPAIR, THE SILL WAS INSPECTED AND FOUND ACCEPTABL E. 2 L 7 2 4F 4 F RT A28NM 2008032400020 20080324 00020 NM 2008 3 24 UPS08M51814 1 20080226 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 24 LEFT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALL ED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035. 2 L 7 3 4F RT A22WE 2008032400021 20080324 00021 WP 2008 3 24 IXXA08SMN046S 1 20080201 A 5340 4641324U501 FITTING DOUG DC8 DC871F 302199D WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND AFT ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 1690.000 LONGERON 28 LEFT. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-3-1 PAGE 2A, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008032400022 20080324 00022 EU 2008 3 24 F3LA200800099 1 20080302 A 5315 D5397496800400 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE AFT CARGO COMPARTMENT FLOOR FRAME PLATE AT FRAME 68 . MAINTENANCE REMOVED AND REPLACED THE PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPHS 5 AND 6. FOLLOWING COMPLETION OF THE PLATE REPLACEMENT, THE NEW PLATE WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400023 20080324 00023 EA 2008 3 24 SWIA200819339 1 20080309 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 495CA 7774 RECEIVED "FLAPS FAIL" CAUTION MESSAGE. DIVERTED TO GRR. RESET CIRCUIT BREAKERS CB1-F4 & CB2-F4 AND PERFORMED FECU TEST IAW MM 27-51-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008032400024 20080324 00024 SO 2008 3 24 SWIA200819340 1 20080309 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 569SW 120344 RIGHT WING FUEL PANEL INBOARD OF NACELLE IS LEAKING FUEL. FOUND STRINGER NR 10 BETWEEN RIB 8 AND 9 ON RIGHT WING TO BE CRACKED. COMPLIED WITH STRINGER REPAIR PER EMB SRM 57-20-03. 2 L 7 2 4T RT A31SO 2008031700030 20080317 00030 SO 2008 3 17 C2XA08ON099 1 20080304 A 2710 35353701001 MANIFOLD EMB 145 EMB145LR 3260212 SO NR 2 AILERON INOPERATIVE A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 10575 13060 13060 145640 FLT 7822 - LAX - DURING PREFLIGHT CHECK CREW REPORTED NOT GETTING AILERON 2 INOP MSG ON EICAS WHILE AIRCRAFT WAS POWER U P WITH HYD SYSTEM OFF. MX PERSONNEL REMOVED AND REPLACED NR 2 AILERON HYD MANIFOLD OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008031700042 20080317 00042 NM 2008 3 17 08FDEA00796 1 20080308 A 5315 652083835 FLOORBEAM BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 MAIN DECK FLOORBEAM UPPER CAP LOWER SURFACE IS CORRODED NUTPLATE BS 1130, LBL 28-38. COMPLIED WITH EA 7-5310-113971 PAR T 1. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008031700052 20080317 00052 NM 2008 3 17 SWAA081343 1 20080310 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 270, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008031700061 20080317 00061 NM 2008 3 17 SWAA081311 1 20080306 A 5330 6545800 SKIN BOEING 737 7373K2 13844BA NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008031700063 20080317 00063 NM 2008 3 17 SWAA081279 1 20080307 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED SPV CHECK, FOUND STRINGER 16L CRACKED BETWEEN BS 348 AND BS 360. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008031700074 20080317 00074 WP 2008 3 17 08FDEA00806 1 20080310 A 5310 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOORWAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 MCD LOWER JAMB AT SPOOL FITTING LOCATION NUMBER 3 SHOWED EVIDENCE OF CRACKS IN HOLES A, B, C, D. 2 L 7 3 4F RT A22WE 2008031700090 20080317 00090 NM 2008 3 17 SWAA081346 1 20080307 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008031700103 20080317 00103 EU 2008 3 17 08FDEA00825 1 20080310 A 5340 A5341076720000 ATTACH ANGLE AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT CARGO PIT; FWD BULKHEAD AT FRAME 54; THE CEILING PANEL ATTACH ANGLE IS CORRODED FROM RBL 37 TO 48 CM (14" TO 18.5 "). REMOVED CORROSION IAW SRM 51-74-10. ORIGINAL MATERIAL THICKNESS .098. REMAINING MATERIAL .043. MATERIAL REMOVED .0 55. OUT OF LIMITS IAW SRM 53-10-00. REMOVED ANGLE IAW SRM 51-40-21. FABBED NEW ANGLE IAW DWG A53410767. ALODINED IAW SRM 51-21-10. PRIMED AND PAINTED IAW SRM 51-23-10. PART MARKED ANGLE IAW GMM 7-0-1001. INSTALLED ANGLE IAW SRM 51-40-2 1. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008031700104 20080317 00104 EU 2008 3 17 08FDEA00826 1 20080310 A 5340 A5341076720000 ATTACH ANGLE AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT CARGO PIT; FWD BULKHEAD AT FRAME 54; THE CEILING ATTACH ANGLE IS CORRODED FROM 131 TO 139 CM (51.5" TO 54.5 "). RE MOVED CORROSION IAW SRM 51-74-10. ORIGINAL MATERIAL THICKNESS .098. REMAINING LATERIAL .050. MATERIAL REMOVED .048. OU T OF LIMITS IAW SRM 53-10-00. REMOVED ANGLE IAW SRM 51-40-21. FABBED NEW ANGLE IAW DWG A53410767. ALODINED IAW SRM 51 -21-10. PRIMED AND PAINTED IAW SRM 51-23-10. PART MARKED IAW GMM 7-0-1001. INSTALLED ANGLE IAW SRM 51-40-21. MINOR REPAI R. 2 L 7 2 4F RT A35EU 2008031700128 20080317 00128 NM 2008 3 17 SWAA081319 1 20080310 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, STR 26L AND STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008031700130 20080317 00130 NM 2008 3 17 SWAA081330 1 20080310 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807 BETWEEN STR 26L AND STR 27R. REPAIRED FRAME PER SRM . 2 L 7 2 4F RT A16WE 2008031700134 20080317 00134 NE 2008 3 17 KNNA20080003 2 20080308 A 7200 ENGINE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 1 FAILED A KNNA E B A ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING R E J PARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 WP 25 326DL 23098 P687596B ACCORDING TO THE PILOT IN COMMAND’S REPORT, THEY HAD TO DEICE THE PLANE BEFORE TAKEOFF. THEN, ON TAKEOFF ROLL, DURING R OTATION, THERE WAS A LOUD BANG AND VIBRATION. THE CAPTAIN’S FIRST THOUGHT WAS THAT A TIRE HAD BLOWN. ONCE AIRBORNE, TH E VIBRATION CONTINUED ACCOMPANIED BY LOUD BANGING. THE NR 1 ENGINE WAS NOT DEVELOPING POWER AND SEEMED TO BE HAVING COM PRESSOR STALLS. THE FIRST OFFICER ADVISED THE TOWER OF OUR EMERGENCY AND REQUESTED AN IMMEDIATE RETURN TO THE AIRPORT. PILOTS ACCOMPLISHED THE ENGINE FAILURE AND SHUTDOWN CHECKLIST FOLLOWED BY THE ONE ENGINE INOPERATIVE LANDING CHECKLIST AND THEN USED AN ILS APPROACH TO LAND AT THE AIRPORT ORIGINALLY DEPARTED FROM. 2 L 7 2 4F 4 F RT A16WE E2EA 2008031700163 20080317 00163 NM 2008 3 17 SWAA081303 1 20080307 A 3350 20131A BATTERY PACK BOEING 737 7373Y0 1384671 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008031700185 20080317 00185 NE 2008 3 17 HALA0800370 2 20080309 A 7230 BRH20390 BLADE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NR 1 ENGINE NICKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 478HA 55123 FOUND TWO NICKS ON NR 1 ENGINE FAN BLADES, ONE ON EACH BLADE, BLADES NR 7 AND NR 8. REMOVED AND REPLACED NR 7, NR 8 BLA DE PER AMM72-38-15. VIBRATION CK PEND. VIBRATION CK GOOD PER AMM71-00-03. 2 L 7 2 4F 4 F TR A6WE E00061EN 2008031700192 20080317 00192 NM 2008 3 17 SWAA081356 1 20080311 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2008031700193 20080317 00193 NM 2008 3 17 SWAA081355 1 20080311 A 5310 6546956 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 328 AND BS 344, STR 17R. REMOVED AND REPLACED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 2008031700211 20080317 00211 WP 2008 3 17 ABXR080066 1 20080204 A 5755 3923254502 SUPPORT DOUG DC9 DC933F 302207A WP RT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 RIGHT INBOARD SPOILER TORQUE TUBE INBOARD VERTICAL SUPPORT CRACKED AT UPPER END. REMOVED AND REPLACED SUPPORT IAW DC9 S RM 51-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 2008031700212 20080317 00212 WP 2008 3 17 ABXR080067 1 20080205 A 5311 59114481 FRAME DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 FRAME CORRODED ON AFT SIDE AT STA 350, LONGERON 30. REPAIRED CRACKED FRAME IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 2008031700225 20080317 00225 WP 2008 3 17 ABXR080084 1 20080214 A 5531 991188212 RIB DOUG DC9 DC933F 302207A WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 RIB CRACKED AT FASTENERS LEFT AND RIGHT VERT STAB LEADING EDGE ZFS 43. REPAIRED IAW DC9 SSRM DWG K05159. 2 L 7 2 4F A6WE 2008031700282 20080317 00282 NM 2008 3 17 MASA200800207 1 20080301 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 448YV 448 REPAIR OF THE LT NR 3 FLAP TRACK. 2 H 7 2 4T RT A13NM 2008031800006 20080318 00006 EU 2008 3 18 08FDEA00848 1 20080310 A 5321 A2901115300100 FLOOR PANEL AIRBUS 310 A310203 3930313 EU FUSELAGE PEELING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 MLG WHEEL WELL FLOOR PANEL 148BF UPPER LAYER IS PEELING. FABRICATED NEW FLOOR PANEL. LOCATED HOLES, POTTED EDGES. CURED EDGE POTTING. INSTALLED INSERTS AND APPLIED NON-SKID IAW SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 2008031800025 20080318 00025 WP 2008 3 18 08FDEA00867 1 20080311 A 5420 FAIRING DOUG MD10 MD1010F 3022112 WP NR 2 ENGINE BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 NR 2 ENGINE AFT FAIRING (BEAVER TAIL), LOWER AFT CORNER, (INNER PAN) IS BROKEN OUT. 2 L 7 3 4F RT A22WE 2008031800057 20080318 00057 NM 2008 3 18 MASA200800215 1 20080310 A 5210 MS24586C140 CABLE DHAV DHC8 DHC8202 2809007 NM PAX DOOR DEFECTIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 989HA 427 ASH 2859 PHX-MRY - CAPTAIN REPORTED THE MAIN PAX DOOR IS DIFFICULT TO OPEN AND CLOSE, LOCK/UNLOCK. REMOVED AND REPLACED THRESHOLD RETRACT CABLE. 2 H 7 2 4T RT A13NM 2008031800058 20080318 00058 EA 2008 3 18 MASA200800216 1 20080310 A 3530 E28095 BRACKET CNDAIR CL600 CL6002D24 1390016 EA OXYGEN BOTTLE BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 916FJ 15016 ASH FLT 2632 CLT-ORF - FWD POB HOLD DOWN CLIP BROKEN. MX CHANGED HOLD DOWN CLIP. 2 L 7 2 4F RT A21EA 2008031800061 20080318 00061 NM 2008 3 18 QXEA200800277 1 20080306 A 5753 SKIN DHAV DHC8 DHC8202 2809007 NM L/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - C5 - UPPER SURFACE OF LEFT INBOARD FLAP 5" AFT OF THE LEADING EDGE AT STATION YW139.00 IS CHAFED APPROXIMATELY .30 " BY .35". BLENDED OUT CHAFE IAW -8 200 SRM 57-50-16 PG 2 TABLE 1. HFEC INSPECTED BLEND IAW-8 200 NDTM PART 6 51-00-01 . NO CRACKS NOTED, UT THICKNESS CHECK IAW -8 200 NDTM PART 1 51-00-04 HIGH .052 LOW .050. FOUND TO BE WITHIN LIMITS IA W -8 200 SRM 57-50-16 PG 2 TABLE 1. ALODINED, PRIMED AND TOP COAT TO THE BLENDED AREA IAW -8 200 SRM 51-20-16, 51-20-36 AND 51-20-51. 2 H 7 2 4T RT A13NM 2008031800073 20080318 00073 WP 2008 3 18 08FDEA00892 1 20080311 A 5754 NRB60371 SLAT DOUG DC10 DC1010 3022110 WP ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 THE NR 8 SLAT HAS NUMEROUS L/E DENTS ALONG THE ENTIRE SPAN. REMOVED & REPLACED NR 8 SLAT. EXTEND & RETRACTED SLATS SE VERAL TIMES. NO BINDING & GAP CHECK GOOD PER AMM 27-80-01-4. 2 L 7 3 4F A22WE 2008031800079 20080318 00079 EU 2008 3 18 08FDEA00902 1 20080312 A 5347 A53612518200 SEAT TRACK AIRBUS 300 A300B4622 3930401 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 720FD 417 MAIN DECK ZONE 221.FORWARD CABIN SEAT TRACK LBL 18 (Y450) BETWEEN FR 14 THRU FR19 HAS STRUCTURAL DAMAGES (HEAVY CORROSIO N, EXFOLIATION). REMOVED SEAT TRACK IAW SRM 51-40-21 LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-44. INSTALLED SEAT TRACK IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008031800085 20080318 00085 WP 2008 3 18 UPS08851779 1 20080308 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED EMERGENCY LT BATTERY PACK PER MM 33-50-01-2. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2008031800089 20080318 00089 WP 2008 3 18 UPS08851786 1 20080302 A 5713 FRAME DOUG DC8 DC873F 302199F WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 LT CENTER LE FRAME CRACKED AT AFT END BETWEEN PANELS 522A, 520B. STOP DRILLED CRACK. FABBED REPAIR ANGLE AND INSTALLED IAW SRM 51-1-857 -2-0 FIG 2, 51-1-20D, 51-3-1. 2 L 7 4 4F RT 4A25 2008031800095 20080318 00095 WP 2008 3 18 UPS08851794 1 20080301 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 INNER RIB CRACKED AT AFT END IN LT WING OB LE IB SECTION NEAR STA XFS6 03. STOP DRILLED CRACK, FABBE D AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-2 1, 51-1-21D, 51-1-8, 57-2-00. 2 L 7 4 4F RT 4A25 2008031800098 20080318 00098 2008 3 18 UPS08M51780 4 20080310 A 2565 INDICATOR DOUG MD11 MD11F 3023600 NM EVAC SLIDE DEFECTIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 251UP 48744 L1 DOOR RAFT/ESCAPE SLIDE PRESSURE INDICATOR WILL NOT ILLUMINATE. DEFERRED IAW UPS MEL 25-61-2 DMP PROC C/W. PRESSURE CHECKS GOOD, M371018 ASSIGNED. INSTALLED NEW SLIDE AND CONTAINER ON DOOR PER AMM 25-61-01-4. THIS CLEARS M371018. 2 L 7 3 4F RT A22WE 2008031800100 20080318 00100 NM 2008 3 18 UPS08M51795 1 20080302 A 5512 SKIN DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 3 LEFT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED, AND INSTALL ED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING OD .946 BORE ID .944. 2 L 7 3 4F RT A22WE 2008031800101 20080318 00101 NM 2008 3 18 UPS08M51796 1 20080305 A 5512 SKIN DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 4 LT BARREL NUT BORE HOLE, (UPPER). REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944. 2 L 7 3 4F RT A22WE 2008031800102 20080318 00102 NM 2008 3 18 UPS08M51797 1 20080218 A 5512 SKIN DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND IN NR 5 LEFT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. .990 BORE I.D. .988. 2 L 7 3 4F RT A22WE 2008031800107 20080318 00107 SO 2008 3 18 CHQA200800048 1 20080309 A 7830 TY203914A ACTUATOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL THRUST REVERSER OUT OF ADJUST A CHQA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 272SK 19658 19658 145306 CAE311940 CMH TO CMH - DURING CLIMB-OUT FROM CMH, THE CREW RECEIVED AN E1 REVERSER DISAGREE MESSAGE ON EICAS. THE CREW LEVELED OF F, FOLLOWED THE APPROPRIATE QRH CHECKLISTS, AND E1 WAS SHUTDOWN. THE AIRCRAFT THEN LANDED AT CMH WITHOUT INCIDENT. MAI NTENANCE TROUBLESHOT THE E1 REVERSER AND FOUND THAT THE UPPER AND LOWER PIVOT DOOR ACTUATORS WERE OUT OF ADJUSTMENT. AF TER ADJUSTING THE ACTUATORS, THE THRUST REVERSER OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008031800114 20080318 00114 EU 2008 3 18 2008UALA01239 1 20080306 A 2560 GIRT BAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR OBSTRUCTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 416UA 479 CREW REPORT: 2R DOOR ARMED BUT THEN DISARMED AND WOULD NOT ARM AGAIN. DEBRIS UNDER GIRT BAR. CLEANED DEBRIS, DOOR ARMS AND DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031800115 20080318 00115 EU 2008 3 18 2008UALA01240 1 20080306 A 3350 D9239003500060 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 493UA 1821 ON EMERGENCY LIGHT TEST ON PTP PANEL GOT EPSU BATT FWD LEFT MESSAGE. EPSU FAILURE. REPLACED POWER SUPPLY AND BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031800124 20080318 00124 NM 2008 3 18 2008UALA01272 1 20080307 A 5320 PAN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LAV SERVICE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 AFT EQUIP BAY, AFT LAV SERVICE PANEL PAN, SURFACE CORRODED AROUND DUMP HOSE FLANGE CONNECTION. MAJOR REPAIR ACCOMPLISHE D: REMOVED & INSTALLED NEW INNER PAN DOUBLER & BRACKETS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800126 20080318 00126 NM 2008 3 18 2008UALA01274 1 20080308 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 CABIN CREASE BEAM INNER CHORD ANGLE CRACKED BS 520 STR 17R RBL 64". MAJOR REPAIR ACCOMPLISHED: REPLACED CREASE BEAM ANG LE WITH NESTED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800127 20080318 00127 NM 2008 3 18 2008UALA01275 1 20080308 A 5230 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FWD CARGO DOOR FWD FRAME LOWER CORNER IS CRACKED IN RADIUS JUST ABOVE LOWER STOP FITTING. MAJOR REPAIR ACCOMPLISHED: RE PLACED LOWER FWD FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800136 20080318 00136 NM 2008 3 18 2008UALA01287 1 20080309 A 5210 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD ENTRY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FWD ENTRY DOOR INNER SKIN AFT EDGE HAS A CRACK BETWEEN THE 5TH AND 6TH STOP PIN FITTING FROM BOTTOM. MAJOR REPAIR ACCOM PLISHED: REMOVED CRACK FROM SKIN AT 5TH FROM BOTTOM STOP PIN. FABRICATED & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800141 20080318 00141 NM 2008 3 18 2008UALA01292 1 20080309 A 2497 285W0020101 CIRCUIT CARD BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE POWER SUPPLY MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 787UA 26939 AIRCRAFT HAS NUMEROUS STATUS MESSAGES ALL RELATED TO LOSS OF POWER DURING FLIGHT. AFTER EXTENSIVE TROUBLE SHOOTING FOUN D POWER SUPPLY CARD FAULTY. REPLACED A18 POWER SUPPLY CARD MSG CLEARED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008031800143 20080318 00143 NM 2008 3 18 2008UALA01294 1 20080309 A 2560 GIRT BAR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE L1 DOOR LOOSE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 371UA 24540 ESCAPE SLIDE AT 1L HAS SLACK. REPACKED SLIDE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800144 20080318 00144 NM 2008 3 18 2008UALA01295 1 20080309 A 2150 3964622 CONTROL VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE A/C PACK FOD A UALA O OTHER C B F.O.D. SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 652UA 25390 LEFT PACK FAILED ON TAKEOFF WITH PACK INOP AND PACK OFF DISPLAYED RESET NORMAL BUT HAD PLASTIC BURNING SMELL AND ALSO A RATTLING SOUND IN DUCTING AREA ABOVE SEAT 9C. CREW SELECTED PACK OFF AGAIN AND BURNING SMELL AND RATTLE STOPPED. FOUND LEFT PACK CONTROL VALVE NOT OPENING FULLY FOUND PLASTIC IN BUSINESS CLASS WARMING OVEN, REMOVED PLASTIC. REPLACED VALVE PER MM 21-51-01. PACK OPS CHECKS NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800145 20080318 00145 EU 2008 3 18 2008UALA01296 1 20080308 A 3510 SEAL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 489UA 1702 INBD FLIGHT CREW, CHECK FOR SLOW 02 LEAK, LOST 200 PSI IN 2 HRS. FO FWD O2 MASK BOX LEAKING AT SEAL. REPLACED SEAL ON FO O2 STOWAGE BOX. LEAK CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031800150 20080318 00150 2008 3 18 2008UALA01302 4 20080308 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR FAULTY A UALA O OTHER W L INADEQUATE Q C NO TEST LD LANDING 1 WP 29 442UA 780 DOOR 1L SLIDE DEPLOYED FOR EVAC AND DID NOT INFLATE AUTOMATICALLY OR BY PULLING MANUAL HANDLE. SLIDE IS REMOVED FROM AI RCRAFT. WAITING ON SHOP FINDINGS FROM SLIDE IN QUESTION. THIS INCIDENT IS UNDER INVESTIGATION FROM NTSB AND FLIGHT SAF ETY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031800152 20080318 00152 EU 2008 3 18 2008UALA01304 1 20080308 A 5220 FITTING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY EXIT LOOSE A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 477UA 1514 R AFT EMERG EXIT DISPLAYED ON UPPER ECAM SCREEN DOOR. CREW COMMENTS: HAD INTERMITTENT ECAM FOR BOTH RT SIDE OVERWING EX ITS. CLEARED BY ITSELF OR BY RESEATING COVERS. LOOSE CLIPS HOLDING ASSY. TAPPED SIDE PANEL, FOUND LIGHT INTERMITTENT. REPOSITION AND TIGHTEN ACCESS PANEL CLIP. OPS TEST, NO LIGHT FAULT OR ECAM. DID NOT REMOVE DOOR OR TOUCHED ARMING ME CHANISM. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031800158 20080318 00158 NM 2008 3 18 2008UALA01312 1 20080308 A 2497 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 IDG MISINSTALLED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 651UA 25389 NR 2 ENGINE IDG WIRE LUGS ARE IMPROPERLY CRIMPED, MULTIPLE WIRE STRANDS BROKEN AT CRIMP POINT. REMOVED AND REPLACED IDG FEEDERS FROM PRODUCTION SPLICE AND REPLACED TERMINALS. OPS CHECK PERFORMED & INSPECTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800160 20080318 00160 NM 2008 3 18 2008UALA01314 1 20080308 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 658UA 27113 EEL LIGHTING INOP BY SEAT 14B. ACP PERMANENT REPAIR TO EEL LIGHT STRIP OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800161 20080318 00161 NM 2008 3 18 2008UALA01315 1 20080310 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 666UA 29238 RT FWD OVERWING CABIN EEL LIGHT INOP. TROUBLESHOOT FOUND UNDER SEAT CONNECTOR LOOSE. SECURED THE CONNECTION OPS CKECKED OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800163 20080318 00163 NM 2008 3 18 2008UALA01317 1 20080307 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 782UA 26948 INSEAT EMERGENCY LIGHTS AT SEAT 1E 2E AND 3E NEED RESECURING. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008031800166 20080318 00166 NM 2008 3 18 2008UALA01321 1 20080310 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT INOP: 32L CEILING, RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031800173 20080318 00173 NM 2008 3 18 2008UALA01340 1 20080311 A 3397 362624 PIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BROKEN A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 LAV 110 SIDE EEL ASSEMBLY PIN BROKEN. FOUND BROKEN PIN CONNECTION. REPLACED PIN OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031800174 20080318 00174 NM 2008 3 18 2008UALA01341 1 20080311 A 3350 OL307115 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 ATTENDANT SEAT L1 EMERGENCY PUSH BUTTON SWITCH LAMP INOP. REPLACED LAMP. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031800179 20080318 00179 NM 2008 3 18 2008UALA01349 1 20080310 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 EMERGENCY LIGHT BARS AT FWD AND MID CROSSAISLE ARE DAMAGED. REPAIRED AND REPLACED LIGHT BARS OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800181 20080318 00181 NM 2008 3 18 2008UALA01351 1 20080310 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 EMERGENCY LIGHT BARS AT FWD RIGHT LAV, MID LEFT LAV, AND BOTH AFT LAVS ARE DAMAGED. REPAIRED AND REPLACED LIGHT BARS OPS CHECKED GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800183 20080318 00183 EU 2008 3 18 F3LA200800090 1 20080308 A 2560 D5348015900700 PLATE AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE R-2 DOOR, FORWARD GIRT BAR PLATE. MAINTENANCE REMO VED AND REPLACED THE GIRT BAR PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-42-12-991-003B. UPON COMPLETION OF TH E INSTALLTION, THE NEW PLATE WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008031800189 20080318 00189 EA 2008 3 18 MASA200800228 1 20080313 A 5280 RIVET CNDAIR CL600 CL6002C10 1390015 EA LT MLG DOOR LOOSE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 507MJ 10077 REMOVED AND REPLACED LOOSE RIVET ON LT MLG IB DOOR LOWER SKIN. 2 L 7 2 4F RT A21EA 2008031800191 20080318 00191 EU 2008 3 18 CPCP20080011 1 20080221 A 5347 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 494AE 494 LT SEAT TRACK BETWEEN FRAME 36-39 CORRODED. LT SEAT TRACK BETWEEN FRAME 36-39, REPLACED AND INSTALLED AS PER SRM 51-25 -04. 2 H 7 2 4T RT A53EU 2008031800193 20080318 00193 SO 2008 3 18 LR7A08025 1 20080128 A 5312 LS603451 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 560 4606 DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5301, FOUND LT UPPER MAIN WHEEL WELL BHD WEB CRACKED AT FS 617, WL 215, LBL 7 3. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-40-10. 2 H 7 4 4T A1SO 2008031800195 20080318 00195 SO 2008 3 18 LR7A08027 1 20080128 A 5312 LS4325 CAP LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 560 4606 DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5302, FOUND INTERIOR FUSELAGE BHD INBD CAP CRACKED AT FS 814, WL 165, RBL 69. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-50-14. 2 H 7 4 4T A1SO 2008031800202 20080318 00202 EA 2008 3 18 A6WA200840094 1 20080212 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 CRACK FOUND ON REAR PRESSURE BULKHEAD WEB FS 621.00, WL 106.17, LBL 36.00 (LINTEL ATTACHMENT FITTING). (K) REPAIRED RE AR PRESSURE BULKHEAD IAW REO 601R-53-61-1230 REV D. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031900006 20080319 00006 EA 2008 3 19 SWIA200819324 1 20080305 A 2701 BEARING CNDAIR CL600 CL6002C10 1390015 EA YOKE ROUGH A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 710SK 10170 FLT 5951 - BOTH CONTROL YOKES FEEL ROUGH WHEN MOVED TO THE RIGHT. REPLACED CAPTAINS CONTROL WHEEL SHAFT BEARINGS IAW CR J 700 MM 27-31-01 AND 27-11-01. 2 L 7 2 4F RT A21EA 2008031700138 20080317 00138 EU 2008 3 17 F3LA200800085 1 20080302 A 5321 D5367175604800 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE GALLEY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED SEVERAL POTTED INSERTS WERE MISSING FROM AFT GALLEY FLOOR PANEL 261PF. MAINTE NANCE REMOVED AND REPLACED THE DAMAGED PANEL IN ACCORDANCE WITH AMM 53-42-12 PB 401. FOLLOWING THE REPLACEMENT OF THE D AMAGED PANEL, THE NEW ONE WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008031700144 20080317 00144 NM 2008 3 17 AALA200800470 1 20080302 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 910AN 29512 MIA - EMERGENCY LIGHT AT SEAT 21D HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008031700146 20080317 00146 NM 2008 3 17 SWAA081301 1 20080307 A 3230 65446915 VALVE BOEING 737 7373H4 1384600 NM MLG WW FAULTY A SWAA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 29 653SW 28398 LEFT MLG WOULD NOT EXTEND NORMALLY. LOWERED GEAR WITH MANUAL GEAR EXTENSION. REMOVED AND REPLACED LEFT MLG MODULAR VAL VE PER MM. 2 L 7 2 4F RT A16WE 2008031700164 20080317 00164 NM 2008 3 17 SWAA081339 1 20080310 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031700172 20080317 00172 2008 3 17 SWAA081313 4 20080305 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 713SW 27847 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031700174 20080317 00174 NM 2008 3 17 SWAA081344 1 20080310 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 740SW 29276 DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION FITTING LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 2008031700177 20080317 00177 NM 2008 3 17 HALA0800374 1 20080306 A 5415 ATTACH BRACKET BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 INLET GOUGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 NR 2 ENGINE NOSE INLET COWL TO FAN CASE ATTACHMENT BRACKETS AT 5 O'CLOCK POSITION GOUGED. DAMAGE AT 5 O'CLOCK POSITION ON NOSE COWL AFT BULKHEAD INNER RING BLENDED IAW SRM 54-11-02/1A01, FIGURE 101, DETAIL 111, WITHIN SRM LIMITS. 2 L 7 2 4F 4 F RT A1NM E13NE 2008031700184 20080317 00184 NM 2008 3 17 HALA0800380 1 20080305 A 5730 SKIN BOEING 767 767332 1382001 NM RT WING CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 CORROSION ON RT WING LOWER SURFACE, RIB 7 AFT OF STRINGER L6, SURROUNDING RIVET HEADS. REPAIR IN WORK. 2 L 7 2 4F RT A1NM 2008031700221 20080317 00221 WP 2008 3 17 ABXR080076 1 20080214 A 5531 991188611 RIB DOUG DC9 DC933F 302207A WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 RIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERTICAL STAB LEADING EDGE ZFS 18. REPAIRED IAW DC9 SSRM DWG K05159. 2 L 7 2 4F A6WE 2008031700222 20080317 00222 WP 2008 3 17 ABXR080077 1 20080214 A 5531 991188211 RIB DOUG DC9 DC933F 302207A WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 RIB CRACKED AT FASTENERS LEFT AND RIGHT SIDE OF VERTICAL STAB LEADING EDGE ZFS 43. REPAIRED IAW DC9 SSRM DWG K05159. 2 L 7 2 4F A6WE 2008031700228 20080317 00228 SO 2008 3 17 C2XA08RI025 1 20080214 A 3320 BR90002 BALLAST EMB 145 EMB145LR 3260212 SO CABIN DEFECTIVE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 13989 145271 FLIGHT - 2303 - SYR - CREW REPORTED SMOKE ODOR IN CABIN COMING FROM OVERHEAD PANEL ABOVE SEAT 1A. CREW PERFORMED AIR RE TURN AND LANDED ACFT UNEVENTFULLY. MX FOUND ODOR AT THIRD BALLAST AFT MX REMOVED AND REPLACED BALLAST IAW EMB145 AMM 33 -21-03 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008031700279 20080317 00279 NM 2008 3 17 MASA200800204 1 20080301 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 448YV 448 REPAIR FOR WEAR AND CORROSION ON THE LT NR2 FLAP TRACK. 2 H 7 2 4T RT A13NM 2008031700280 20080317 00280 NM 2008 3 17 MASA200800205 1 20080301 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 448YV 448 REPAIR TO WEAR AND CORROSION ON RT NR 1 FLAP TRACK. 2 H 7 2 4T RT A13NM 2008031700281 20080317 00281 NM 2008 3 17 MASA200800206 1 20080301 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM T/E FLAP CORRODED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 448YV 448 REPAIR OF WEAR AND CORROSION ON THE NR 2 FLAP TRACK. 2 H 7 2 4T RT A13NM 2008031800038 20080318 00038 NM 2008 3 18 QXEA200800266 1 20080228 A 5320 THRESHOLD BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - MCD THRESHOLD HAS CORROSION AROUND THE SCREW HOLES. REMOVED THRESHOLD AND INSTALLED NEW THRESHOLD IAW DHC8 Q 400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 2008031800048 20080318 00048 WP 2008 3 18 DHLA200800030 1 20080122 A 2612 4172448 FIRE DETECTOR DOUG DC8 DC873F 302199F WP NR 1 NACELLE MALFUNCTIONED A DHLA O OTHER N FALSE WARNING AP APPROACH 1 GL 05 806DH 1802 1802 46002 FLT NR 403, NR 1 ENGINE FIRE WARNING FLASHED A COUPLE OF TIMES DURING FINAL APPROACH LOOP A HANDLE AND MASTER LIGHTS. D EFERRED PER MEL 26-2-3 A-LOOP DMI NR 31485 PLACARD INSTALLED CAT C B-LOOP OPS CK GOOD SP C/W 26-2. T/S SYS IAW MMS 26-1 0-0. REMOVED AND REPLACED 1 DETECTOR NR 1 ENG IAW MMS 26-10-1 RAN NR 1 ENG PER JRH. SYS TESTS GOOD. THIS ACTION CL EARS MDDR NR 31485 PLACARDS. REMOVED AIRCRAFT WAS GROUNDED, SEE PART 1-5 SDR NUMBER DHLA200800008 AND 0030-0034. 2 L 7 4 4F RT 4A25 2008031800064 20080318 00064 NM 2008 3 18 QXEA200800270 1 20080306 A 5320 ATTACH ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - C5 - CARGO BAY ENTRYWAY THRESHOLD ATTACHMENT ANGLE AT APPROXIMATELY STA 580.5 HAS CORROSION AROUND NUT PLATES. RE MOVED CARGO BAY THRESHOLD PLATE BY REMOVING BOLTS AND SCREWS. REMOVED ANGLE BRACKET AND NUT PLATES BY REMOVING SOLID RI VETS. BLENDED CORROSION ON ANGLE BRACKET. MAX MATERIAL REMOVED .002". REPAIR IS WITHIN LIMITS PER SRM 51-20-11. ALOD INED AND PRIMED BRACKETS. INSTALLED BRACKET WITH SOLID RIVETS, RIVETS THROUGH EXTERIOR SKIN WERE INSTALLED WET WITH SEA LANT. INSTALLED NUT PLATES TO BRACKET WITH BLIND RIVETS. REFERENCE SRM 51-40-11, 51-40-00. REINSTALLED CARGO BAY THRE SHOLD PLATE BY REPLACING BOLTS, AND SCREWS. BOLTS INSTALLED WITH SEALANT, APPLIED SEALANT TO ENDS OF BOLTS AND FILET SE 2 H 7 2 4T RT A13NM 2008031800090 20080318 00090 WP 2008 3 18 UPS08851787 1 20080304 A 5720 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 RT WING CENTER LE, STALL WARNING SENSOR DOUBLER IS CORRODED. REMOVED CORRODED DOUBLER, FABBED AND IN STALLED NEW DOUBLER IAW SRM 51 -1-15, 51-1-21, 51-1-8, 51-3-2. 2 L 7 4 4F RT 4A25 2008031800091 20080318 00091 WP 2008 3 18 UPS08851788 1 20080302 A 5720 DOUBLER DOUG DC8 DC873F 302199F WP RT WING WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 RT WING CENTER LE HAS FRETTING WEAR AT OB MATING SURFACE. REMOVED INTERNAL DOUBLER, FABBED NEW DOUBL ER AND INSTALLED IAW SRM 51- 3-0, 51-1-21, 57-3-3 FIG 5, 57-3-3 FIG 5, 51-1-8. 2 L 7 4 4F RT 4A25 2008031800119 20080318 00119 NM 2008 3 18 2008UALA01251 1 20080307 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY LIGHT INOP, DR5L SLIDE ILLUM, RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031800153 20080318 00153 NM 2008 3 18 2008UALA01306 1 20080307 A 5340 BRACKET BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GIRT BAR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FWD ENTRY DOOR WAY, FWD GIRT BAR ATTACH ANGLE DAMAGED AT AFT END OF RADIUS. REPLACED GIRT BAR BRACKET. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800178 20080318 00178 NM 2008 3 18 2008UALA01348 1 20080310 A 3350 60243 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 EMERGENCY LIGHT BAR AT AFT GALLEY AREA LEFT SIDE IS DAMAGED. REPLACED EEL STRIP OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800192 20080318 00192 EU 2008 3 18 CPCP20080010 1 20080221 A 5347 SEAT TRACK AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 494AE 494 RT SEAT TRACK BETWEEN FRAME 39-40 CORRODED. RT SEAT TRACK BETWEEN FRAME 39-40, REMOVED IAW SRM 51-21-42. 2 H 7 2 4T RT A53EU 2008031800194 20080318 00194 SO 2008 3 18 LR7A08026 1 20080128 A 5312 LS306191 ANGLE LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 560 4606 DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5302, FOUND LT BHD REPAIR ANGLE CRACKED AT FS 497, WL260, LBL63. REPAIR ACCO MPLISHED BY REPLACING ANGLE IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008031900004 20080319 00004 SW 2008 3 19 P4YA22808 1 20080225 A 3260 LIGHT FRCHLD SA227 SA227DC 3377521 SW COCKPIT BURNED OUT E P4YA O OTHER O OTHER AP APPROACH 1 EA 39 955BW DC821B ON APPROACH, LANDING GEAR WAS SELECTED DOWN WITH NO NOSE LANDING GEAR INDICATION TO INDICATE "DOWN & LOCKED". AIRCRAFT DECLARED AN EMERGENCY AND LANDED SAFELY. NOSE LANDING GEAR INDICATOR LAMP WAS FOUND TO BE "BURNED OUT" AND WAS REPLACED . LANDING GEAR SYSTEM RETRACTION TEST PERFORMED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A18SW 2008031900007 20080319 00007 EA 2008 3 19 SWIA200819325 1 20080305 A 5240 SEAL CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR ICED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 917SW 7641 FLT 6602 - SERVICE DOOR IS DIFFICULT TO OPEN. INSPECTED, CLEANED AND REMOVED ICE FROM DOOR SEAL. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008032400040 20080324 00040 EU 2008 3 24 08FDEA00936 1 20080314 A 5350 A21510415000400 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 DELAMINATION ON PANEL NR 143 FL; INTERIOR SKIN. REPAIRED IAW SRM 51-77-10 & 51-75-10. 2 L 7 2 4F RT A35EU 2008032400041 20080324 00041 EU 2008 3 24 08FDEA00945 1 20080314 A 5730 A5724852600100 SKIN AIRBUS 310 A310203 3930313 EU RT WING DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT WING UPPER L/E SKIN PANEL AT STA WQFS 66-151 LINER FOIL IS DISBONDED AND TORN. REMOVED & REPLACED DAMAGED FOIL IAW S RM 57-41-12. 2 L 7 2 4F RT A35EU 2008032400123 20080324 00123 EU 2008 3 24 YENA2008022 1 20080310 A 3350 321431 BATTERY AIRBUS 320 A320232 3930326 EU CABIN FAULTY A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 561JB 21698 21698 1927 ON MX INSPECTION, RT EMERGENCY EXIT EPSU FAULTS BATTERY. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT RT EMERGENCY E XIT ESPU PER AMM 33-51-38-04, OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2008032400127 20080324 00127 EA 2008 3 24 COMA0860169 1 20080310 A 5320 601R53410562 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 957CA 30563 7109 CRACK FOUND ON RBL 27 AT FS 409+128 ON INBOARD SIDE OF VERTICAL BEAM LOWER. REPAIRED CRACK IAW REO 601R-53-41-056. 2 L 7 2 4F RT A21EA 2008032400130 20080324 00130 EA 2008 3 24 COMA0860171 1 20080310 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 798CA 21224 7348 CRACK ON THE CAP ANGLE AT LBL 18.00 AT FS 559. REPAIRED CRACK ON CAP ANGLE AT LBL 18.00 IAW REO 601R-53-41-260. 2 L 7 2 4F RT A21EA 2008032400156 20080324 00156 NM 2008 3 24 SWAA081377 1 20080312 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 417WN 29822 DURING SCHEDULED 6Y CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 90. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032400203 20080324 00203 NM 2008 3 24 SWAA081379 1 20080313 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 221WN 34259 R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008032400247 20080324 00247 NM 2008 3 24 SWAA081392 1 20080313 A 5311 6546526 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 24L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032400250 20080324 00250 NM 2008 3 24 SWAA081403 1 20080313 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500B, STR 28R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032400254 20080324 00254 NM 2008 3 24 SWAA081405 1 20080313 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032400282 20080324 00282 NM 2008 3 24 HALA0800396 1 20080313 A 5512 SKIN BOEING 767 767332 1382001 NM HORIZONTAL STAB DENTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 SUP - LT HORIZONTAL STAB HAS L/E DAMAGE IN 5 PLACES INBD, AND 1 PLACE OUTBOARD. NOT ON A/C DAMAGE REGISTER. PERMANENT SRM REPAIR CARRIED OUT IAW SRM 51-70-10, REPAIR 2, REFERENCE ANZ TI 190113615-0001 AND HAL FILE NR 594051. 2 L 7 2 4F RT A1NM 2008032400283 20080324 00283 NM 2008 3 24 HALA0800394 1 20080309 A 5520 BALANCE WEIGHT BOEING 767 767332 1382001 NM RT ELEVATOR CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 SURRFACE CORROSION FOUND LT AND RT ELEVATOR QUADRANT BALANCE WEIGHT X2. SURFACE CORROSION REMOVED PER SRM 51-10-02, REV . 76. SURFACE FINISH RESTORED PER SOFM 20-41-02 REV 104. 2 L 7 2 4F RT A1NM 2008032400286 20080324 00286 NM 2008 3 24 DHL2008763508 1 20080313 A 5753 69166441 RIB BOEING 727 727264 138408M NM LT WING TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 PREVIOUS REPAIR ON L/WING O/B FORE FLAP UPPER SURFACE CHAFED, LWBL 400. REMOVED EXISTING REPAIR AND ASSOCIATED INTERNAL RIB. FABRICATED AND INSTALLED NEW REPAIR SKIN SECTION, 2024-T3 .050 INCH BY 14.125 INCH BY 5.875 INCH, PO NR 9005554; AND SPLICE, 2024-T3 .063" BY 12" BY 5", PO NR 9005551 PER B727 SRM 57-50-4 FIG 4, 57-50-2 FIG 3. INSTALLED NEW RIB ASSY PER B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008032400288 20080324 00288 NM 2008 3 24 DHL2008763510 1 20080312 A 5740 ATTACH ANGLE BOEING 727 727264 138408M NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 R/WING L/E INTERIOR, CRACKED RIB ATTACH ANGLE AT RWS 125 (FRONT SPAR). FABRICATED AND INSTALLED REPAIR DOUBLER, 7075-T6 .050 INCH BY 10.5 INCH BY 2.5 INCH, PO NR 9006153, AND FILLER, 7075-T6 .040 INCH BY 3 INCH BY 2.5 INCH, PO NR 9006639, PER B727 SRM 51-40-3 FIG 1 AND 57-20-2 FIG 1. 2 L 7 3 4F A3WE 2008032400289 20080324 00289 EU 2008 3 24 F3LA200800117 1 20080228 A 5320 D5367226300000 SILL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND AT VARIOUS THROUGH HOLES ON THE UNDERSIDE OF SILL PLATE 15 2YG. MAINTENANCE REPAIRED THE SILL PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-21-11, A319 SRM 51-23-11 AN D EA A9 53R-30123. UPON COMPLETION OF THE REPAIR, THE SILL PLATE WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008031900008 20080319 00008 EA 2008 3 19 SWIA200819326 1 20080303 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STUCK A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 939SW 7742 FLT 5824 - MAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. LUBED AND CLEANED PAX DOOR SYSTEM IAW AMM 52-00. OPS CHECKS GOO D. 2 L 7 2 4F RT A21EA 2008031900013 20080319 00013 CE 2008 3 19 GUUA01290801 1 20080129 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 318 S15L CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87554 UE227 AT SCHEDULED INSP, DISCOVERED EXFOLIATED SECTION OF SKIN AT FS 318.250 STR 15L. REMOVED EXFOLIATED SECTION OF SKIN FABR ICATED AND INSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW SRM 51-70-06. 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900016 20080319 00016 SO 2008 3 19 GUUA02040801 1 20080204 A 3260 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO LT MLG DIRTY A GUUA O OTHER N FALSE WARNING CL CLIMB 1 SO 29 268AS 120202 FLIGHT: 9273, AFTER TAKEOFF, LT LANDING GEAR (A) AND (B) RED LIGHTS ILLUMINATED WITH THE GEAR COMMANDED UP. LIGHTS EXTIN GUISH AFTER RECYCLING GEAR. CLEANED LT LANDING GEAR PROXIMITY SWITCHES. 2 L 7 2 4T RT A31SO 2008031900020 20080319 00020 SO 2008 3 19 GUUA02160801 1 20080216 A 3350 AGC1 FUSE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHTS BLOWN A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 283AS 120236 FLIGHT: 8148, DURING PREFLIGHT, PILOT REPORTED RT SIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED AFT LAMP FUSE. 2 L 7 2 4T 4 T RT A31SO E20NE 2008031900037 20080319 00037 2008 3 19 GUUA03140801 4 20080314 A 3452 6226523208 CONTROL HEAD BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE TRANSPONDER SHORTED A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 29 87550 UE205 FLIGHT: 9208, AFTER TAKEOFF SMOKE IN COCKPIT TURNED OFF TRANSPONDER SMOKE STOPPED.RETURNED TO PNS. LANDED WITHOUT INCIDE NT. REPLACED ATC TRANSPONDER CONTROL. 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900038 20080319 00038 NM 2008 3 19 TAMF20080001S 1 20080301 A 5730 ACCESS DOOR BOEING 767 767200 1385120 NM LT WING CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 769QT 23801 DURING INSPECTION CHECK, FOUND LT WING 541AB MAIN FUEL TANK ACCESS DOOR OUTER SKIN WITH A SCRATCH AND CORROSION. DAMAGE D AREA WAS REPAIRED IAW EWO 767-57-038 AND BOEING SERVICE REQUEST 1-771920168. THIS REPAIR IS CLASSIFIED AS MAJOR REPAI R. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F RT A1NM 2008031900039 20080319 00039 NM 2008 3 19 TAMF20080002S 1 20080225 A 5751 RIB BOEING 767 767200 1385120 NM AILERON CHAFED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 769QT 23801 DURING INSPECTION CHECK, FOUND A WEAR OUT OF LIMITS ON INBOARD AILERON RT OUTBOARD CLOSURE RIB WEB. DAMAGED AREA WAS RE PAIRED IAW EWO 767-57-034 AND BOEING SERVICE REQUEST 1-773827820. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F RT A1NM 2008031900040 20080319 00040 NM 2008 3 19 TAMF20080003S 1 20080229 A 5330 SKIN BOEING 767 767200 1385120 NM FUSELAGE NICKED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 769QT 23801 DURING C CHECK INSPECTION, FOUND SKIN CORROSION AND NICK ON STA 478.6 STRINGER 31RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-071 AND BOEING SERVICE REQUEST 1-775312353. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F RT A1NM 2008031900051 20080319 00051 NM 2008 3 19 DTHA2008001 1 20080211 A 2133 OUTFLOW VALVE DORNER DO32 DO328300 NM CABIN PRESSURE DIRTY E DTHA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 25 407FJ 3157 EN ROUTE DTW TO CLT AT FL310 UNCOMMANDED CABIN ALTITUDE CLIMB TO 9100'. MAINTENANCE DETERMINED PNEUMATIC OUTFLOW VALVE/ FILTER ASSY CONTAMINATED. VALVE AND FILTERS CLEANED, FUNCTION RESTORED. 2 H 7 2 4T RT A55NM 2008031900060 20080319 00060 NM 2008 3 19 TAMF20080004S 1 20080226 A 5720 SPLICE PLATE BOEING 767 767200 1385120 NM LT WING CRACKED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 769QT 23801 DURING C CHECK INSPECTION WAS FOUND A CRACK ON LEFT WING LEADING EDGE LOWER SPLICE PLATE - ISS 257-. DAMAGED AREA WAS R EPAIRED IAW EWO 767-57-035 AND BOEING SERVICE REQUEST 1-773976194. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F RT A1NM 2008031900068 20080319 00068 EA 2008 3 19 TRAX200800375 1 20080304 A 5230 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 972EV 7534 CARGO DOOR FWD TRACK, LOWER U-CHANNEL CRACKED. DRILLED OUT CRACKED LOWER U-CHANNEL LOCATED IN THE CARGO BAY. IDENTIFIE D MATERIAL IAW SRM 53-61-23 AND MADE A SERVICEABLE PART (DUPLICATE) IAW SRM 51-24-21. ALODINED AND PRIMED DUPLICATED PA RT IAW SRM 51-25-06. APPLIED TOPCOAT IAW 51-25-16. INSTALLED SERVICEABLE DUPLICATED PART IAW SRM 51-42-060. 2 L 7 2 4F RT A21EA 2008031900073 20080319 00073 NM 2008 3 19 KCSA081146 1 20080307 A 5730 SKIN BOEING 747 747209B 138489B NM CENTER WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 CORROSION AT CENTER WING TANK UPPER SKIN SEAM AT STA 1050 RBL 92. 2 L 7 4 4F RT A20WE 2008031900080 20080319 00080 SO 2008 3 19 GLBA20061056 1 20080129 A 5712 RIB EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT WING CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 108UX 120108 LT RIB NR19 AT WS, YA-5825 AND STRINGER NR 1 CRACKED IN (2) PLACES. CRACKS APPROX .250 AND .375 RESPECTIVELY. MAINTENA NCE REMOVED DAMAGED AREA AND INSTALLED REPAIR PIECE IAW SRM 57-20-07. REPAIR PIECE CUT FROM NEW RIB. 2 L 7 2 4T 4 T RT A31SO E20NE 2008031900082 20080319 00082 SO 2008 3 19 GLBA20061057 1 20080128 A 5712 RIB EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT WING CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 108UX 120108 RT WING RIB NR 21 AT WS, YA-6750. CRACKED APPROX .375 INCH IN LENGTH AT STRINGER NR 1. MAINTENANCE REMOVED DAMAGED AR EA AND INSTALLED REPAIR PIECE IAW SRM 57-20-07. REPAIR PIECE CUT FROM NEW RIB SECTION. 2 L 7 2 4T 4 T RT A31SO E20NE 2008031900088 20080319 00088 NM 2008 3 19 KCSA081156 1 20080307 A 5313 STRINGER BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 STA 1790-1830 STR 23R HAS CORROSION AROUND FASTENERS ON UPPER ROW OF LAP SEAM. 2 L 7 4 4F RT A20WE 2008032400290 20080324 00290 NM 2008 3 24 DHL2008763511 1 20080316 A 5344 HINGE BOEING 727 727264 138408M NM CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 MCD AFT HINGE SEGMENT AFT LOBE CRACKED. REMOVED AND REPLACED HINGE SEGMENT WITH MS 20001-16-7200 MATERIAL PO NR 9002527 PER AEI B727-200 FREIGHTER MM CH 52 FIG 5201A AND SRM 51-30-5. 2 L 7 3 4F A3WE 2008032400295 20080324 00295 NM 2008 3 24 TSAA0827015 1 20080312 A 2750 FLAP SYSTEM BOEING 737 73776N 13844CH NM TE FLAPS MALFUNCTIONED A TSAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 WP 13 748AL 30050 ETOPS FLIGHT 442 HNL-OAK - ON APPROACH THE CREW SELECTED FLAPS 15 AND THE FLAPS ONLY MOVED TO FLAPS 1. THE CREW USED TH E ALTERNATE SYSTEM TO DEPLOY TO FLAPS 15. THE CREW LANDED IN OAK WITHOUT FURTHER INCIDENT. MAINTENANCE BITE CHECKED TH E FLAP SLAT ACCESSORY UNIT AND OPERATIONAL CHECKED THE FLAPS WITH NO FAULTS FOUND PER AIRCRAFT FIM 27-51-00-810-836. TH E AIRCRAFT WAS RETURNED TO SERVICE AND COMPLETED A FLIGHT VERIFICATION ON THE NEXT FLIGHT LEG. 2 L 7 2 4F RT A16WE 2008032400300 20080324 00300 WP 2008 3 24 NWAA080989760 1 20080316 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NW 47288 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY OVERWING EXIT SIGNS ON BOTH THE LEFT AND RIGHT SIDES WERE INOPER ATIVE. AFTER INSTALLATION OF A NEW BATTERY PACK, MAINTENANCE OPERATIONALLY CHECKED SYSTEM AND AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F A6WE 2008032400303 20080324 00303 SO 2008 3 24 FDKA200803098 1 20080310 A 5230 DOOR EMB 145 EMB145LR 3260212 SO CARGO VENT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 842MJ 145457 FDM 6152- PFN-MCO (0800 PHX LCL) - BAGGAGE VENT DOOR WILL NOT CLOSE PROPERLY. MX ADJUSTED VENT DOOR. DOOR AND INDICATI ON OPS GOOD. 2 L 7 2 4T RT T00011AT 2008032400305 20080324 00305 SO 2008 3 24 FDKA200803104 1 20080312 A 2560 HOLDER EMB 145 EMB145LR 3260212 SO FLASHLIGHT INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 829MJ 145228 FDM 6090 BWI-JFK - AFT EMERGENCY FLASHLIGHT INOP. MX REMOVED AND REPLACED FLASHLIGHT HOLDER. 2 L 7 2 4T RT T00011AT 2008032400306 20080324 00306 SO 2008 3 24 FDKA200803105 1 20080312 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM 6152 MCO-GSO (0922 PHX LCL) - EMERGENCY EXIT SIGN ROW 12 LT SIDE INOP. MX PERFORMED OPS CHECK. NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008032400311 20080324 00311 WP 2008 3 24 08FDEA00953 1 20080314 A 5230 ADA019343 LINER DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 FWD CARGO DOOR LINER LOWER EDGE CRACKED OUT AT THE FASTENER HOLES; PREVIOUS REPAIR IS DELAMINATING WITH WASHERS PULLING THROUGH. APPLIED FIBERGLASS OVERLAY REPAIR IAW SRM 51-43-01; VOL II. 2 L 7 3 4F RT A22WE 2008032400315 20080324 00315 WP 2008 3 24 08FDEA00958 1 20080314 A 5753 ARC0740507 SKIN DOUG MD10 MD1010F 3022112 WP TE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT WING OUTBD FLAP INBD HINGE FAIRING PANEL NR 635 BR INNER SKIN IS GOUGED. REPAIRED IAW SRM 51-71-00, VOL II, PARA 1 7. ALODINDE, PRIMED & PAINTED IAW SRM 51-71-00, VOL II. 2 L 7 3 4F RT A22WE 2008032400318 20080324 00318 WP 2008 3 24 08FDEA00960 1 20080314 A 5730 ARC0257503 PANEL DOUG MD10 MD1010F 3022112 WP LT WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LEFT WING LOWER T/E PANEL NR 541 NB IS DELAMINATED. REPAIRED IAW SRM 51-71-00; VOL II. 2 L 7 3 4F RT A22WE 2008032400320 20080324 00320 NM 2008 3 24 2008UALA01372 1 20080312 A 5753 SUPPORT FITTING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE T/E FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 NR 1 FLAP SUPPORT FITTING, JOINT 1V INBOARD BUSHING BORE IS WORN. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032400322 20080324 00322 WP 2008 3 24 08FDEA00961 1 20080314 A 5753 ARC2231503 PANEL DOUG MD10 MD1010F 3022112 WP LT WING TE FLAP DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LEFT WING INBD FLAP FAIRING NR 535HL HAS AREAS OF DISBOND. REPAIRED BY FABRICATING & BONDING THE INNER & OUTER SKINS; INNER & OUTER DOUBLERS & CORE IAW TPS 1001, REV E & EA 8-5720-118479, 2 L 7 3 4F RT A22WE 2008032400325 20080324 00325 NM 2008 3 24 2008UALA01375 1 20080311 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 226UA 30226 EIGHT EMERGENCY LIGHTS NOT WORKING LOCATED ON THE OUTSIDE OF THE TWO LEFT LAVATORY MODULES AFT OF ROW 25 AND FWD OF ROW 31. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032400326 20080324 00326 WP 2008 3 24 08FDEA00963 1 20080314 A 5753 ARC22322 PANEL DOUG MD10 MD1010F 3022112 WP RT WING TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT WING OUTBD FLAP INBD FAIRING PANEL NR 636 DR IS DELAMINATED. REPAIRED IAW DWG ARC 2232, TPS 1001 REV E & EA 8-5750 -116970. RESTORED FINISH SRM 51-21-02; VOL II. 2 L 7 3 4F RT A22WE 2008032400331 20080324 00331 NM 2008 3 24 2008UALA01377 1 20080312 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 UPPER EXTERNAL FUSELAGE SKIN HAS AREAS OF WEAR UNDER DORSAL FIN LANDING FROM SEAL CONTACT FROM BS 860-907. MAJOR REPAIR ACCOMPLISHED: BLENDED WORN AREA. FABRICATED & INSTALELD EXTERNAL DOUBLER & TRIPLER REPAIR (INCLUDING BONDED WEAR STRIPS) . REPLACED SEATS & SEAL RETAINERS ON DORSAL FIN. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032400343 20080324 00343 NM 2008 3 24 2008UALA01384 1 20080312 A 5610 WINDOW BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT CRACKED A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 29 941UA 26676 CREW REPORT: L2 WINDOW CRACKED AND ARCED ON APPROACH INTO YYZ AT 2000 MSL. TURNED OFF WINDOW HEAT. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032400352 20080324 00352 NM 2008 3 24 2008UALA01389 1 20080313 A 3350 90085 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 LEFT NR 2 AND RIGHT NR 2 EXIT SIGN LIGHT NOT ON. REPLACED BATTERY PACK OPS CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032400363 20080324 00363 NM 2008 3 24 SWAA081414 1 20080316 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 R1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008032400364 20080324 00364 NM 2008 3 24 SWAA081421 1 20080316 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008032400367 20080324 00367 NM 2008 3 24 SWAA081416 1 20080316 A 2560 P2070001 FLASHLIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 747SA 29799 DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2008032400372 20080324 00372 NM 2008 3 24 Y2LA200800016 1 20080316 A 5610 NP1653117 WINDSHIELD AIRBUS A319 A319111 3930336 NM COCKPIT CRACKED A Y2LA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 572SX 1963 WHILE ON DESCENT INTO CMH THE CAPTAIN NOTICED SPARKS SHOOTING ACROSS CA WINDSHIELD. F/O DECLARED AN EMERGENCY. SHORTLY AFTER THE WINDSHIELD HAD SPIDER WEBBED CRACKED. THE AIRCRAFT LANDED SAFELY WITHOUT ANY FURTHER ISSUES. CAPTAINS WINDS HIELD CRACKED. REMOVED AND REPLACED CAPTAINS WINDSHIELD PER AMM 56-11-11-400-001 AND WINDSHIELD HEAT CONTROLLER NR 1 RE PLACED FOR PREVENTATIVE MEASURE AND OPERATIONAL TEST OF THE WINDSHIELD ANTI-ICING AND DEFOGGING PER AMM 30-42-00-710-001 WAS COMPLETED. 2 L 7 2 4F RT A28NM 2008032400374 20080324 00374 NM 2008 3 24 SWAA081422 1 20080315 A 3397 W4142001220 WIRE BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 231WN 32499 DURING SCHEDULED MV3 CHECK, FOUND EEPLS INOP AT ROW 12 ABC. FOUND LOOSE WIRE. SECURED WIRE PER MM. 2 L 7 2 4F RT A16WE 2008032400375 20080324 00375 NM 2008 3 24 SWAA081423 1 20080315 A 3350 8200048901 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 237WN 34632 L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008032400376 20080324 00376 NM 2008 3 24 SWAA081424 1 20080314 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 246LV 32507 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008032400385 20080324 00385 NM 2008 3 24 SWAA081458 1 20080313 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 867, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032400388 20080324 00388 NM 2008 3 24 SWAA081432 1 20080314 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 883, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032400390 20080324 00390 NM 2008 3 24 SWAA081434 1 20080317 A 5743 6537877 FITTING BOEING 737 7373H4 1384600 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED MV2 CHECK, FOUND LT MLG WALKING BEAM FWD OUTBOARD FITTING CORRODED. REMOVED AND REPLACED FITTING PER S WA EA. 2 L 7 2 4F RT A16WE 2008032400406 20080324 00406 2008 3 24 SWAA081445 4 20080314 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032400407 20080324 00407 NM 2008 3 24 SWAA081464 1 20080313 A 5330 6545766 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515D, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400408 20080324 00408 NM 2008 3 24 SWAA081447 1 20080314 A 5330 6545767 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 405, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400411 20080324 00411 NM 2008 3 24 SWAA081465 1 20080313 A 5312 6546568 BULKHEAD BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED C4 CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008032400414 20080324 00414 NM 2008 3 24 SWAA081448 1 20080314 A 5330 65C381921 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505D, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400415 20080324 00415 NM 2008 3 24 SWAA081467 1 20080314 A 5330 6545766 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 438, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400420 20080324 00420 NM 2008 3 24 SWAA081450 1 20080317 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032400424 20080324 00424 NM 2008 3 24 SWAA081470 1 20080313 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 731SA 27863 L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2008032100076 20080321 00076 2008 3 21 2008UALA01338 4 20080310 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 DOOR ONE RIGHT SLIDE LIGHT WILL NOT ILLUMINATE AND UNABLE TO DISARM DOOR. FOUND DOOR SLIDE HARDWARE OUT OF ADJUSTMENT. ADJUSTED DOOR SLIDE HARDWARE, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100077 20080321 00077 NM 2008 3 21 2008UALA01345 1 20080310 A 3397 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 531UA 25042 EEL FEEDER AT STA 1060 DAMAGED. REPLACED EEL FEEDER, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100079 20080321 00079 NM 2008 3 21 2008UALA01347 1 20080310 A 3397 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 531UA 25042 ONE COACH EMERGENCY ESCAPE LIGHT FEEDER BROKEN. REPLACED FEEDER ASSY, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100080 20080321 00080 NM 2008 3 21 2008UALA01353 1 20080309 A 3510 OXYGEN SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CREW LOW A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 543UA 25698 OXYGEN QUANTITY READS 1660 PSI. SERVICED CREW O2 TO FULL, NO LEAKS NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032400014 20080324 00014 NE 2008 3 24 COMA0860158 2 20080305 A 7597 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30068 NE BLEED AIR VALVE LOOSE A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 927CA 7031 FLIGHT 5451 - WITH BLEED AIR SOURCE FOR PACKS ON, APU LT 10TH STAGE BLEED VALVES CLOSED RT 10TH OPEN AND LOAD CONTROL VA LVE CLOSED. OPENED ISO SWITCH AND LOAD CONTROL OPENED, SAME, REPEATED SEVERAL TIMES. FOUND CONNECTORS LOOSE ON THE ISO LATION AND 10TH STAGE BLEED VALVES. SECURED CONNECTORS. NO FURTHER DEFECTS. 2 L 7 2 4F 4 F RT A21EA E15NE 2008032400017 20080324 00017 EA 2008 3 24 COMA0860161 1 20080307 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 CORROSION FOUND AT FLOOR SILL AFT OF MAIN DOOR AS MARKED BETWEEN FS 349.00 AND 364.00. CUT OUT CORRODED SILL AND INSTAL LED A REPAIR DOUBLER AND SERVICEABLE SILL IAW EA 10-5320-02121 DATED 3/4/08. 2 L 7 2 4F RT A21EA 2008032400093 20080324 00093 NM 2008 3 24 UPS08M51858 1 20080228 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 35 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.132 BORE I.D. 1.130 2 L 7 3 4F RT A22WE 2008032400094 20080324 00094 NM 2008 3 24 UPS08M51859 1 20080218 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 36 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 2.5735 BORE I.D. 2.572. 2 L 7 3 4F RT A22WE 2008032400095 20080324 00095 NM 2008 3 24 UPS08M51860 1 20080212 A 5751 SKIN DOUG MD11 MD11F 3023600 NM RT IB AILERON GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C RT WING IB AILERON UPPER SURFACE AT OB VERY LE HAS 5 INCH LONG DEEP GOUGE RUNNING THRU REPAIR DOUBLER . REMOVED PREVIOUS REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER PER MD-11 SRM 57-00-01 AND 51-35-01. 2 L 7 3 4F RT A22WE 2008032400097 20080324 00097 EU 2008 3 24 F3LA200800096 1 20080303 A 5340 D53915503200 ATTACH ANGLE AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE BULKHEAD CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND IN MULTIPLE NUT PLATE HOLES ON THE FORWARD CARGO PIT, AFT BULKHEAD, FLOOR PLATE, LOCATED AT FRAME 35, BETWEEN STRINGERS L38 AND R38. MAINTENANCE REMOVED AND REPLACED THE PLATE I N ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. FOLLOWING COMPLETION OF THE INSTALLATION, THE NEW PLATE WAS IN SPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400098 20080324 00098 NM 2008 3 24 TSAA0852014 1 20080311 A 5230 SEAL BOEING 737 7372X6C 1384552 NM CARGO DOOR OUT OF ADJUST A TSAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 840AL 23124 CARGO FLIGHT 940 HNL-KOA - DURING CLIMB, THE CREW NOTED A LOUD AIR NOISE COMING FROM THE MAIN CARGO DOOR INDICATING AN I NCOMPLETE SEAL ON THE DOOR. THE CREW RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE MAIN CARGO DOO R PRESSURE SEAL AND PRESSURE CHECKED THE AIRCRAFT PER AMM 21-00-05. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2008032400134 20080324 00134 NM 2008 3 24 WRLA2008029 1 20080313 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 48407 DURING C-CHECK INSPECTION, MAIN DECK FLOOR PANEL SUPPORT CRACKED STA Y=635 X=8.5 X=27.5. PERFORM MAIN DECK FLOOR SUPPOR T SEAT TRACK REPAIR PER MD11 SRM VOL.III 53-70-00 FIG.1 REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2008032400150 20080324 00150 NM 2008 3 24 SWAA081359 1 20080312 A 5753 6546435281 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PE R MM. 2 L 7 2 4F RT A16WE 2008032400233 20080324 00233 NM 2008 3 24 DHL2008753504 1 20080225 A 5320 INTERCOSTAL BOEING 727 727223 1384074 NM BS 227 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 DURING "C" CHECK FWD E/E COMPT BS 227.8 CORROSION ON WEB AND ANGLE BBL "0". REMOVED INTERCOSTAL DAMAGE, STIFFENER AND A NGLE FOR ACCESS IAW SRM 51-30-2. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. CUTOUT DAMAGED AREA APP ROX 11 INCHES. FAB FILLER, 2 SPLICES IAW SRM 51-40-4 FIG 1. HEAT TREATED PARTS IAW FAS ENG REPORT 2-37153-801 REV A. TREATED, PRIMED AND INSTALLED PARTS REPAIR IAW SRM 51-10-2 AND 51-40-4 FIG 1. FAB NEW INTERCOSTAL IAW SRM 51-10-2 AND 51-30-2. MAJOR REPAIR, PERMANENT REPAIR 2 L 7 3 4F A3WE 2008032400234 20080324 00234 NM 2008 3 24 DHL2008753505 1 20080228 A 5753 SKIN BOEING 727 727223 1384074 NM RT WING TE FLAP CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 "C' CHECK, RT O/B FORE FLAP UPPER L/E 400 (WBL) HAS DEEP CHAFE MARK. BLENDED OUT AREA AT RT OB FORE FLAP UPPER L/E WBL4 00 IAW SRM 51-10-6. MAT LOSS 50 PERCENT. FOUND OUT OF LIMITS IAW SRM 57-50-1. CUTOUT DAMAGED AREA APPROX 1 1/8 INCH B Y 1 7/8 INCH AND FAB DOUBLER REPAIR IAW SRM 57-50-4 FIG 1. TREATED AND PRIMED AREA AND DOUBLER IAW SRM 51-10-2. INSTAL LED DOUBLER REPAIR IAW SRM 57-50-4 FIG 1. 2 L 7 3 4F A3WE 2008032400235 20080324 00235 NM 2008 3 24 DHL2008753506 1 20080226 A 5730 SKIN BOEING 727 727223 1384074 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 "C" CHECK LT WING L/E CRACKED AT NR 4 SLAT O/B TRACK CUTOUT. REMOVED PAINT LT WING L/E NR 4 SLAT O/B TRACK IAW MM 51-20 -1. STOP DRILLED WITH .250 AT THE END OF THE CRACK IAW SRM 51-10-1. FAB DOUBLER REPAIR IAW SRM 57-30-4 FIG 11 AND SRM 51-20-1 FIG 7. TREATED AND PRIMED AREA AND DOUBLER REPAIR IAW SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW SRM 57-30-4 FI G 11. C/W HFEC IAW NDTM PT6 51-00-00 FIG 23. CRACK TERMINATES IN STOP DRILL HOLE. 2 L 7 3 4F A3WE 2008032400236 20080324 00236 NM 2008 3 24 DHL2008753507 1 20080301 A 5522 PANEL BOEING 727 727223 1384074 NM LT ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 "C" CHECK, CRACK INDICATION INSIDE LT ELEVATOR PANEL 9305 ON LWR RIB ELEV STA 20. REMOVED CRACKED ANGLE LT ELEVATOR AT LOWER RIB AT PANEL NR 9305 STA 20 IAW SRM 51-30-2. FORMED NEW ANGLE PER DRAWING 65-25634, REV G AND 51-10-3 AND 51-20-1 OF THE SRM. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED ANGLE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032400238 20080324 00238 SW 2008 3 24 WGEA200800046 1 20080313 A 2730 8000883017 SELECTOR SWITCH ECLIPS EA500 ECLIPSEEA500 3350000 SW ELEVATOR TRIM DEFECTIVE E WGEA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 163DJ 26 000081 ELEVATOR TRIM SPLIT - LEFT TAB FROZEN AT 7 PERCENT. REMOVED AND REPLACED CENTER SWITCH PANEL WITH NEW UNIT. PERFORMED TEST IAW EA500 AMM 31-10-00. CSP TEST GOOD. 1 L 7 2 4J RT A00002AC 2008032400239 20080324 00239 SW 2008 3 24 WGEA200800047 1 20080313 A 2720 RUDDER ECLIPS EA500 ECLIPSEEA500 3350000 SW OUT OF ADJUST E WGEA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 EA 27 163DJ 000081 AIRCRAFT REQUIRES 100 PERCENT RWD AT 252 KTS, WITH 16 PERCENT LEFT RUDDER. REFERENCE WORK ORDER 1602, NR-00001. PER TS R 27-030508G, REV C. AIRCRAFT IS WITHIN SPECIFICATION AND NO FURTHER MAINTENANCE ACTION IS REQUIRED AT THIS TIME ON STA TED CONDITION. 1 L 7 2 4J RT A00002AC 2008032400241 20080324 00241 EU 2008 3 24 TRBA2008031 1 20080314 A 3350 AQS1000 BATTERY PACK AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 431AT 431 EMERGENCY LIGHTS CAME ON AND OFF AFTER ENGINE START. REPLACED EMERGENCY LIGHT BATTERY PACK 61WL AND 43WL AND PERFORMED OPT TEST PER JIC 33-51-21. FOUND SYSTEM WORKING OK. 2 H 7 2 4T RT A53EU 2008032400242 20080324 00242 EU 2008 3 24 TRBA2008032 1 20080315 A 3350 HD3013017 POWER SUPPLY AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHTS FAILED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 541AT 541 HALF OF AISLE PATH EVACUATION LIGHTS NOT WORKING ON BATTERY POWER. REPLACED AND TESTED EMERGENCY LIGHTS POWER SUPPLY 61 WL BATTERY PACK AS PER MM 33-51-21 AND FOUND WORKING PROPERLY. 2 H 7 2 4T RT A53EU 2008032400243 20080324 00243 EU 2008 3 24 F3LA200800115 1 20080303 A 5320 D53112191203 SILL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE R-1 DOOR SILL PLATE AT 2 NUT PLATE LOCATIONS ON THE FORWARD GIRT BAR FITTING ATTACH POINT. MAINTENANCE REMOVED THE CORROSION, TREATED THE BLENDED AREAS WITH ALODINE, PAIN TED WITH PRIMER, FILLED THE BLENDED AREA WITH HYSOL 9394 AND PERFORMED THESE ACTIONS IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30097, STEPS 6 AND 7. UPON COMPLETION OF THE WORK, THE SILL PLATE WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400245 20080324 00245 NM 2008 3 24 HALA0800387 1 20080306 A 5314 KEELBEAM BOEING 767 767332 1382001 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 CORROSION ON FUSE-KEEL BEAMS AT BL62, SEVERAL ANCHOR NUTS INSTALLED WITH STEEL RIVETS WHICH ARE CORRODING. REPLACED COR RODED STEEL RIVETS WITH CORRECT SOLID RIVETS IAW SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008032400252 20080324 00252 NM 2008 3 24 SWAA081404 1 20080313 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032400255 20080324 00255 NM 2008 3 24 SWAA081395 1 20080313 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 632SW 27707 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008032400267 20080324 00267 NM 2008 3 24 ASAA0852709 1 20080314 A 4990 38809381 FILTER BOEING 737 737890 1384527 NM APU DIRTY A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 570AS 35185 WHILE CHECKING APU OIL FOR PRE DEPARTURE CHECK FOUND RED OIL FILTER CLOGGING INDICATOR PROTRUDING FROM FILTER BOWL. PER FORMED BITE CHECK OF CDU NO CURRENT FAULTS. REPLACED APU LUBE OIL FILTER. FILTER CHECK GOOD. OIL FILTER INDICATOR CHE CK GOOD. MAG DRAIN PLUG CHECK GOOD. OPERATED APU, NO LEAKS NOTED. 2 L 7 2 4F RT A16WE 2008032400276 20080324 00276 NM 2008 3 24 2008UALA01365 1 20080312 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 LEFT WING EXTERIOR EMERGENCY EXIT LIGHTS INOP TWO AFT LIGHT ASSY'S. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032400336 20080324 00336 EU 2008 3 24 08FDEA00969 1 20080314 A 5414 A54611357200 PANEL AIRBUS 310 A310203 3930313 EU NR 2 NACELLE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 PYLON PANEL NR 423 BL IS CHAFED ON THE MATING SURFACES. BLENDED CHAFED AREAS IAW SRM 54-52-51; ITEM 4; PG 102. O RIGINAL MATERIAL THICKNESS IS .079 IAW SRM 54-52-51; FIG 4; SHEET 2. REMOVED .031; REMAINING MATERIAL THICKNESS IS .04 8. FOUND TO BE OUT OF LIMITS IAW SRM 54-52-51; DIAGRAM 101. FABBED DOUBLER IAW SRM 54-52-51; FIG 202. ALODINED IAW SRM 51-21-10. PRIMED IAW SRM 51-23-10. INSTALLED DOUBLER IAW SRM 54-52-51; FIG 202. TOP COATED IAW SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008032400337 20080324 00337 EU 2008 3 24 08FDEA00970 1 20080314 A 5730 A5724351200200 PANEL AIRBUS 310 A310203 3930313 EU RT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT WING PANEL NR 672 CB UPPER SKIN IS CHAFED. REPAIRED IAW SRM 51-77-10 & BONDED IT IAW SRM 51-77-12. REFINISHED ARE A IAW SRM 51-75-10. 2 L 7 2 4F RT A35EU 2008032400338 20080324 00338 EU 2008 3 24 08FDEA00971 1 20080314 A 5730 A5724349623239 PANEL AIRBUS 310 A310203 3930313 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT WING L/E PANEL UPPER SURFACE; APPROX RIB 14 HAS THE PROTECTIVE METAL TAPE LOOSE AND PAINT PEELING. REMOVED DAMAGE D FOIL IAW SRM 57-41-12. APPLIED NEW FOIL IAW SRM 57-41-12. APPLIED PROTECTIVE FINISH IAW A310 SRM 51-75-10. PRIMED IA W SRM 57-41-12. 2 L 7 2 4F RT A35EU 2008032400340 20080324 00340 EU 2008 3 24 08FDEA00972 1 20080314 A 5730 A57245318200 SKIN AIRBUS 310 A310203 3930313 EU RT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT WING INBD SLAT; INBD OF NR 1 TRACK; INNER SURFACE FASTENERS ARE CHAFING ON THE WING L/E SKIN. BLENDED AREA SMOOTH & REMOVED DAMAGE IAW SRM 51-73-10. FOUND TO BE OUT OF LMITS IAW SRM 57-40-00. DAMAGED SECTION OF THE L/E SKIN IAW SRM 57-41-12. HEAT TREATED NEW FORMED L/E SKIN. FABBED, LOCATED & DRILLED NEW SKIN & 1 REPAIR BUTT STRAP IAW SRM 57-41-12 FIG 203 & 51-40-44. ALODINED REPAIR PARTS IAW SRM 51-21-10. PRIMED & TOP COAT PAINTED IAW SRM 5-23-10. INSTALLED NEW S KIN SECTION & REPAIR BUTT STRAP IAW SRM 51-41-12. 2 L 7 2 4F RT A35EU 2008032400342 20080324 00342 EU 2008 3 24 08FDEA00973 1 20080314 A 5755 STRUCTURE AIRBUS 310 A310203 3930313 EU NR 1 SPOILER DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 1092 264 LT WING NR 1 SPOILER INBD FWD CORNER IS DISBONDED. REPAIRED NR 1 SPOILER AT THE INBD FWD CORNER BY APPLYING REPAIR PLIES IAW SRM 51-77-11 PARA 3E; FIGURE 208. 2 L 7 2 4F RT A35EU 2008032400349 20080324 00349 WP 2008 3 24 08FDEA00979 1 20080317 A 5740 ARC087313 BRACKET DOUG MD10 MD1010F 3022112 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LT WING OUTBD FLAP FWD HINGE; POSITION TRANSMITTER SUPPORT BRACKET IS CRACKED. REMOVED CRACKED BRACKET IAW SRM 51-33-01 & 51-35-01; VOL II. FABRICATED IAW DWG ARC0873 REV 6. ALODINED & PRIMED IAW SRM 51-21-01 PGS 24 THRU 24 VOL II. INS TALLED IAW SRM 51-33-01 & 51-31-01 VOL III. 2 L 7 3 4F RT A22WE 2008032400360 20080324 00360 WP 2008 3 24 08FDEA00994 1 20080317 A 5320 ADA39415 FRAME DOUG MD10 MD1010F 3022112 WP BS 791 S49-50R BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 FWD LOWER CARGO BILGE J-CHANNEL HAS BENT EDGE AT BS 791 BETWEEN STR 49R AND STR 50R. REPAIRED THE FRAME J-CHANNEL IN RE FERENCE WITH SRM 53-30-00 VOL I FIGURE 5. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008032400382 20080324 00382 NM 2008 3 24 SWAA081429 1 20080314 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008032400391 20080324 00391 2008 3 24 SWAA081435 4 20080315 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032400396 20080324 00396 NM 2008 3 24 SWAA081459 1 20080317 A 5753 6546434 FLAP BOEING 737 7375H4 138449D NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2008032400413 20080324 00413 NM 2008 3 24 SWAA081466 1 20080313 A 5330 6545766 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400437 20080324 00437 EU 2008 3 24 COEA0801908 1 20080220 A 5230 0513872 RELEASE CABLE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE FWD CARGO DOOR LACK OF LUBE A COEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 13 908FX 023 AIR TURNBACK, FLT NR 7304. UPON ROTATION, THE CARGO DOOR UNLOCK LIGHT ILLUMINATED. CREW ELECTED TO RETURNED. AIR CRAF T MADE A SAFE AND NORMAL LANDING. DOOR LOCK RELEASE CABLE WAS LUBRICATED AND AC RETURNED TO SERVICE. AS A PRECAUTION F WD CARGO DOOR LOCK RELEASE CABLE TO BE REPLACED AT NEXT SCHEDULED MAINTENANCE EVENT. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008032500004 20080325 00004 NE 2008 3 25 DXTA20082884 2 20080216 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE RIGHT POWER LOSS E DXTA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 807QS 5600617 ATTEMPTED A STATIC T/O AND THE RT ENG DIDN'T MAKE THE COMPUTED T/O PWR WITH FULL THROTTLE TRAVEL. IT WAS 2 PERCENT SHOR T OF THE REQUIRED 92.2 PERCENT AT 0 DEG C. PERFORMED TAXI/ POWER OF THE DAY CHECKS WITH CREW AT 5 DEGREES C. POWER NEED ED WAS 91.5 PERCENT N1 AND POWER ACHIEVED WAS 93 PERCENT N1. POWER CHECKS GOOD AT THIS TIME IAW AFM. 2 L 7 2 4F 4 F RT A22CE E00053EN 2008032500005 20080325 00005 CE 2008 3 25 DXTA20082885 1 20080216 A 3243 9536717 MASTER CYLINDER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT BRAKE ASSY BYPASSING E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 312QS 601 5600312 CO PILOTS LT BRAKE DEPRESSES ALL THE WAY TO THE FLOOR. PUMPING PEDAL TEMPORARILY RESTORES EFFECTIVNESS FOR A FEW SECOND S ONLY. REMOVED COMPLETE LT WHEEL BRAKE MASTER CYL PN 95367-17 SN 0921. INSTALLED OVERHAULED CO-PILOT LT WHEEL BRAKE MA STER CYL PN 95367-17 SN 1246 IAW MM 32-42-02. BRAKE BLEEDING ACCOMPLISHED IAW MM 32-41-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2008031900090 20080319 00090 NM 2008 3 19 KCSA081157 1 20080308 A 5320 FITTING BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE STRINGER END FITTING BOLT HOLE HAS PITTING AT THE FORWARD SIDE OF THE STA 2360 PRESSURE BULKHEAD STR 36R. 2 L 7 4 4F RT A20WE 2008031900095 20080319 00095 NM 2008 3 19 KCSA081162 1 20080210 A 5311 FRAME BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 BS 2220 FUSELAGE FRAME LOWER CHORD CORRODED ABOVE STR 42L, LBL 33. 2 L 7 4 4F RT A20WE 2008031900097 20080319 00097 NM 2008 3 19 KCSA081164 1 20080310 A 5322 SHEAR TIE BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 BS 2220 FUSELAGE FRAME SHEAR TIE CORRODED BETWEEN STR 38L AND 40L. 2 L 7 4 4F RT A20WE 2008031900099 20080319 00099 NM 2008 3 19 SB08012 1 20080309 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 439US 24781 MIA - MAINTENANCE REPORTED THE FORWARD ENTRANCE AND AFT ENTRANCE CENTER EMERGENCY EXIT SIGN AT L1, R1, L2 AND R2 DOORS A LONG WITH THE EXIT IDENTIFIERS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS. OPERATIONAL CHECK GOOD . 2 L 7 2 4F RT A16WE 2008031900110 20080319 00110 CE 2008 3 19 DJFA2008014 1 20080204 A 5511 1286200210001 RIB BEECH MU300 400A 1155402 CE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 434LX 1244 351 RK274 DURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB BRACKET WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COM MUNIQUE' NR 70. BOTH INBOARD RIBS WERE REPLACED WITH THE NEW STYLE RIBS. 2 H 7 2 4F RT A16SW 2008031900112 20080319 00112 CE 2008 3 19 DJFA2008004 1 20080116 A 5511 45A21085004 RIB BEECH MU300 400A 1155402 CE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 446CW 1064 RK346 DURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE BOTH IB RIBS WERE FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COM MUNIQUE' NR 70. MAINT REPLACED BOTH RIBS WITH THE IMPROVED PARTS. 2 H 7 2 4F RT A16SW 2008031900116 20080319 00116 EA 2008 3 19 S9BA200800007 1 20080211 A 5711 C6W105664 SPAR DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA RT WING CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 20206 1310 573 CPCP INSPECTION, RT WING NOSE SPAR CORRODED WS 35.15 TO WS 135. REPLACED NOSE SPAR WITH FACTORY NEW PART IAW AC43.13-1B CHAP 4 PARA 4-57. EMERGENCY MEASURES EXECUTED. NO AIRCRAFT GROUNDED. 1 H 7 2 3T 4 T RT A9EA E4EA 2008031900121 20080319 00121 EA 2008 3 19 S9BA20080011 1 20080211 A 5730 C6W1024 SKIN DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA ZONE 600 CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 20206 1310 573 CPCP INSPECTION; RT WING FWD CORRUGATION AT WS 58 CORRODED. REPAIRED CORRUGATION AT WS 58 WITH FACTORY NEW PART IAW SRM 57-30-00 PAGE 4. EMERGENCY MEASURES EXECUTED? NO AIRCRAFT GROUNDED? YES. 1 H 7 2 3T 4 T RT A9EA E4EA 2008031900123 20080319 00123 EA 2008 3 19 S9BA20080004 1 20080211 A 5414 C6W15002728 SKIN DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA RT NACELLE CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 573 CPCP INSPECTION, LT WING, LT AND RT NACELLE SKINS CORRODED. REMOVED AND REPLACED NACELLE SKINS AND SPLICED SKINS IAW RD 6-54-004 AND AC 43-13, PARA 4-57. 1 H 7 2 3T 4 T RT A9EA E4EA 2008031900127 20080319 00127 CE 2008 3 19 20061067 1 20080211 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 177 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 257GL UE257 FRAME AT FS 177.35 AND STRINGER 9R CRACKED APPROX .500 INCH IN LENGTH. OPEN 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900129 20080319 00129 CE 2008 3 19 GLBA20061069 1 20080213 A 2612 24412886 FIRE LOOP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 2 NACELLE FAULTY A GLBA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 NM 03 122UX UE122 ENG SHUTDOWN- FLIGHT NR 5067 ENROUTE, THE PILOTS SHUTDOWN AND SECURED THE NR 2 ENGINE IN FLIGHT, DUE TO A NR 2 FIREWALL FUEL VALVE HANDLE THAT ILLUMINATED DURING FLIGHT. MAINT REMOVED AND REPLACED THE NR 2 ENG FW FIRELOOP IAW MM 26-10-01. O PS CHECK OF THE SYS WAS GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900148 20080319 00148 NM 2008 3 19 KCSA081165 1 20080311 A 5412 BULKHEAD BOEING 747 7472B4B 138481B NM NR 1 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NR 1 PYLON AFT ENG MOUNT BULKHEAD FWD FRAME WEB CRACKED AT I/B LOWER SIDE NAC STA 221.9. 2 L 7 4 4F RT A20WE 2008031900151 20080319 00151 NM 2008 3 19 KCSA081167 1 20080311 A 5210 DOOR FRAME BOEING 747 747SR46 1384816 NM PAX DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 MAIN ENTRY DOOR 4R TOP AFT CORNER FRAME CRACKED BS 1700. 2 L 7 4 4F RT A20WE 2008031700253 20080317 00253 CE 2008 3 17 GUUA01210801 1 20080121 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA FUSELAGE CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81538 UE199 AT SCHEDULED INSPECTION, DISCOVERED A 1.0 INCH CRACK BETWEEN FS 230.75 AND 310.75 AT BL 30.62. STOP DRILLED CRACK AND I NSTALLED EXTERNAL REINFORCEMENT DOUBLER IAW SRM 53-90-18. 2 L 7 2 4T 3 T RT A24CE E2NE 2008031700259 20080317 00259 NM 2008 3 17 ASMF200801003 1 20080123 A 5754 114W411029 SLAT BOEING 777 777* UTILUSE NM WING DAMAGED W ASMF K NONE O OTHER TX TAXI/GRND HDL 1 SW 23 746AM 8217 32719 DURING TAXING, AC HIT WITH LT SLAT NR 1 ON THE LT WING OF THE AIRCRAFT REGISTRATION N774AM. DETAILED INSPECTION WAS PERF ORMED ON LT WING TIP DETECTING A STRUCTURAL DAMAGE ON SLAT NR 1 OF 17 INCHES LENGTH AND 11 INCHES WIDTH, OUT OF LIMITS, LOCATED BETWEEN STATIONS WS1375 AND WS1408; ADDITIONALLY, THE AERODYNAMIC SEAL OF LT SLAT NR 1 LEADING EDGE WAS FOUND CR ACKED. MAINT REPLACED THE OB LEADING EDGE SLAT NR 1 AND SEAL-END IAW MM 27-81-15. RII INSPECTION WAS PERFORMED, ALL CORR ECT. 2 L 7 2 4F RT T00001SE 2008032500006 20080325 00006 CE 2008 3 25 DXTA20082886 1 20080215 A 2150 73838433 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AFT SERVICE BAY LEAKING E DXTA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 931QS 749 7500064 DURING TAXI CABIN FILLED WITH SMOKE. FWD ACM SUSPECTED. REMOVED AND REPLACED CABIN (FWD) ACM. OPS AND LEAK CHECKS GOOD IAW MM 21-11-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032500009 20080325 00009 CE 2008 3 25 DXTA20082889 1 20080219 A 2720 7022090901 COMPUTER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FWD AVIONICS BAY FAULTY E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 946QS 59 7500195 YD FAIL UPPER B CAS MESSAGE DISPLAYED WHILE CLIMBING THROUGH APPROX FL240. COULD NOT VERIFY DISCREPANCY AT THIS TIME. DUE TO PRIOR HISTORY, REMOVED SUSPECTED FAULTY YSAC COMPUTER. PERFORMED OPS CHECKS WITH NO DISCREPANCIES NOTED AT THIS TIME. ALL WORK PERFORMED IAW (X) MM 27-24-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032500010 20080325 00010 CE 2008 3 25 DXTA20082890 1 20080219 A 3230 LANDING GEAR CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE LEFT MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 806QS 5600614 DURING NORMAL GEAR EXTENISON ON FINAL APPROACH, LT MAIN GEAR WOULD NOT INDICATE DOWN AND LOCKED BY THE GEAR INDICATOR LI GHT. CLEAN AND LUBRICATED LT AND RT MLG UPLOCKS. COMPLETED LANDING GEAR HYD SYS FUNCTIONAL TEST IAW MM CHAPTER 32-01 W ITH NO DEFECTS AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E00053EN 2008032500011 20080325 00011 CE 2008 3 25 DXTA20082891 1 20080220 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 352QS 5600352 COPILOTS SIDE BRAKES REQUIRE MORE THAN NORMAL PRESSURE TO GET ANY BRAKING. RAN AC WITH ANTI-SKID ON AND OFF CONDUCTING HIGH SPEED STOPS AND MANY MANUVERING TURNS WITH NO DISCREPANCIES NOTED FROM EITHER PILOT OR COPILOT SIDE. ANTI-SKID BIT INDICATORS WERE CHECKED BEFORE AND AFTER RUN WITH NONE TRIPPED EITHER TIME. FORCE REQUIRED TO ACTUATE BRAKING IS EQUAL BETWEEN LT AND RT, BRAKE AND EQUAL BETWEEN PILOT AND COPILOT SIDE. 2 L 7 2 4F 4 F RT A22CE E25EA 2008032500014 20080325 00014 CE 2008 3 25 DXTA20082894 1 20080222 A 3220 62422171 ELASTOMER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG WORN E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 942QS 8321 7500024 AC BEGAN SHAKING AT 40 KTS ON TAKEOFF. YAW DAMPER CAME OFF LINE AND TAKE OFF ABORTED AT 70 KNOTS. GAINED ACCESS TO NOSE LANDING GEAR ELASTOMER (ACTUATOR AREA). REMOVED OLD ELASTOMERS AND INSTALLED NEW ELASTOMERS AND HARDWARE. PLACED AC ON JACKS, CYCLED LANDING GEARS SEVERAL TIMES. OPS CHECKED GOOD. DOWNJACK AC. WORK DONE IAW CH 32-30-03 OF THE MM. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032500026 20080325 00026 NM 2008 3 25 2008UALA01362 1 20080312 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY EXIT LIGHT INOP AT DOOR 3 RIGHT CEILING ENTRY. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032500043 20080325 00043 2008 3 25 AMWA89978 4 20080206 A 3454 6226521016 CONTROL HEAD BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA NR 1 VOR SMOKE A AMWA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CE 07 167YV 21282 2284 UE167 DURING SHORT FINAL APPROACH, SMOKE WAS DETECTED COMING OUT OF THE NR1 NAV CONTROL HEAD. THE NR1 NAV CB'S WERE PULLED, TH E SMOKE STOPPED AND AC LANDED WITHOUT FURTHER INCIDENT. MAINT REMOVED AND REPLACED CONTROL HEAD AND CLEARED DISCREPANCY. SUBSEQUENT TEARDOWN AT REPAIR VENDOR SHOWED BURNED COMPONENTS ON POWER SUPPLY CARD. NO PRIOR HISTORY OF THIS PROBLEM ON COMPANY FLEET. 2 L 7 2 4T 3 T RT A24CE E2NE 2008032500048 20080325 00048 NM 2008 3 25 USAA920080589 1 20080217 A 5330 654577678 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - CORROSION ON FUSELAGE SKIN, BS 757, BL 0 UNDER AIR PHONE ANTENNA. REPAIRED FUSELAGE SK IN, BS 757, BL 0 UNDER AIR PHONE ANTENNA IAW USAIRWAYS EA 100280. 2 L 7 2 4F RT A16WE 2008032500050 20080325 00050 NM 2008 3 25 USAA920080590 1 20080219 A 5754 65C26799 SKIN BOEING 737 7373S3 1384711 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - LEFT WING NR 1 SLAT LOWER SURFACE CRACKED, SS 298. REPAIRED LEFT WING NR 1 SLAT LOWER SURFACE, SS 298 IAW B737 SRM 51-70-10-2R. 2 L 7 2 4F RT A16WE 2008032500055 20080325 00055 WP 2008 3 25 ASMF200802009 1 20080229 A 2721 INDICATOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE RUDDER TRIM OUT OF ADJUST W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 501AM 49188 CAPTAIN REPORTED THAT THE RUDDER WAS TRIMMED 3 DEGREES TO THE LT DURING ALL FLIGHT. MAINTENANCE PERSONNEL REPLACED AND A DJUSTED THE RUDDER TRIM CONTROL POSITION INDICATOR IAW MM 27-20-00, TESTED CORRECT. 2 L 7 2 4F 4 F A6WE E2EA 2008032500056 20080325 00056 NM 2008 3 25 USAA920080632 1 20080317 A 5330 6545877 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 23879 CLT - MAJOR REPAIR - CRACKED FUSELAGE SKIN BS 328, S17R. REPAIRED FUSELAGE SKIN, BS 328, S17R IAW USAIRWAYS EA 100320. 2 L 7 2 4F RT A16WE 2008032500057 20080325 00057 NM 2008 3 25 USAA920080633 1 20080313 A 5330 6545775594 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FUSELAGE SKIN, BS727D, S23R. REPAIRED FUSELAGE SKIN, BS 727D, S23R IAW B737 SR M 53-00-01-1A1. 2 L 7 2 4F RT A16WE 2008032500058 20080325 00058 GL 2008 3 25 I5HA0858001 2 20080306 A 7322 AN17412C BOLT CVAC 580 580 2422806 WP ALLSN 501D 501D13A 03004 GL THROTTLE LINKAGE BROKEN A I5HA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 25 588X 52 DURING CLIMBOUT, THE CREW LOST THROTTLE CONTROL ON THE NR 2 ENGINE. THEY PREFORMED THE EMERGENCY PROCEDURES AND SHUTDOWN THE ENGINE. UPON ARRIVAL MAINT INSPECTED THE NR 2 ENGINE AND FOUND THAT THE THROTTLE LINKAGE BOLT HOLDING THE LINKAGE O N TO THE FUEL CONTOL WAS BROKEN ALLOWING THE BELLCRANK TO SLIDE OFF THE FUEL CONTROL. MAINT REPLACED THE BOLT AND PREFO RMED AND RIG CHECK AND OPS CHECK OF THE ENGINE CONTROLS. ALL WERE FOUND SATISFACTORY. THE AC WAS RETURNED TO SERVICE AND WAS RELAUNCHED. 2 L 7 2 4T 4 T RT E282 2008032500059 20080325 00059 NM 2008 3 25 USAA920080634 1 20080222 A 5312 651728349 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - CRACKED BULKHEAD VERTICAL BEAM WEB, BS 178, LBL 5.71, WL 178. REPAIRED BULKHEAD VERTIC AL BEAM WEB, BS 178, LBL 5.71, WL 178 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008032500063 20080325 00063 NM 2008 3 25 ASMF200803001 1 20080306 A 2913 66087 PUMP BOEING 737 73776Q 13845AA NM CFMINT CFM567 CFM567B22 13802 NE HYD SYSTEM LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 853AM 10999 10999 33791 890954 DURING TRANSIT CHECK WAS DETECTED A LEAK IN RT ENGINE. TECHNICAL PERSONNEL VERIFIED THE ENGINE AND FOUND A LEAK IN THE H YD PUMP. THE PUMP WAS REPLACED IAW MM 29-11-11 AND HYD TANKS WERE CHECKED IAW TASK 12-12-00-610-801, TESTED CORRECT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008032500074 20080325 00074 CE 2008 3 25 DXTA20082935 1 20080312 A 3260 65430087 UPLOCK SENSOR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RTMLG MALFUNCTIONED E DXTA O OTHER N FALSE WARNING CL CLIMB 1 GL 07 382QS 5600382 UPON GEAR RETRACTION, OUT OF DEPARTURE, RT GEAR WOULD NOT RETRACT. REMOVED AND REPLACED RT UPLOCK SWITCH WITH NEW. C/W FULL GEAR FUNCTIONAL CHECK. ALL OPS CHECK GOOD AT THIS TIME. IAW MM 32-61-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2008032500076 20080325 00076 NM 2008 3 25 HNAA0800103 1 20080316 A 2910 82950010143 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM NR 1 NACELLE LEAKING A HNAA A UNSCHED LANDING K J A FLUID LOSS WARNING INDICATION FLAME/FIRE CL CLIMB 1 EA 07 815EX 39913 39913 321 AFTER DEPARTURE FROM ABE, AT APPROX 200 FT THE CREW NOTICED THE ILLUMINATION CAUTION LIGHTS ASSOCIATED WITH THE NR 1 HYD RAULIC SYSTEM AT APPROX 400 FT. THE CREW WAS ABLE TO VERIFY THAT THE NR 1 HYDRAULIC SYSTEM QUANTITY WAS AT ZERO. THE C REW RETURNED TO THE FIELD AND SHUT THE ENGINES DOWN ON THE RUNWAY AND AWAITED THE GROUND CREW TO TOW THE AIRCRAFT BACK T O THE GATE. ALL PAX ARE OK. AFTER INVESTIGATION OF LEAK MX DISCOVERED EVIDENCE OF A FLASH FIRE UNDER PANEL 419AT, WITH WIRE COATINGS BURNED OFF. LEAK ORIGINATED 8 INCHES OUTBOARD OF NACELLE UNDER PANEL 532AB. PINHOLE FOUND IN HYDRAULIC LINE. LINE WAS REPLACED WITH A TEMP FLEX LINE AND WIRING REPAIRED AFTER BEING FERRIED TO MDT. 2 H 7 2 4T RT A13NM 2008032500080 20080325 00080 2008 3 25 DXTA20082937 4 20080314 A 3460 43606 CONTROLLER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FLT DIRECTOR FAILED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 934QS 4360 4360 7500034 ON CLIMBOUT AT 2000 FEET, PRIMARY STAB TRIM FAIL. FOUND DEFECTIVE FLIGHT DIRECTOR CONTROLLER. REMOVED & REPLACED DEFECT IVE FLIGHT GUIDANCE CONTROLLER WITH REPAIRED EXCHANGE UNIT. PERFORMED OPS CHECKS OPS CHECKS GOOD IAW CE750 MM 22-10-03. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032500081 20080325 00081 EA 2008 3 25 COMA0860166 1 20080310 A 5720 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 957CA 7109 DURING HMV NR 6 INSPECTION, NDT INSPECTION FOUND A CRACK ON THE 540 DB FUEL TANK CUTOUT, BETWEEN WS 85.5 AND 106.4. DAM AGE WAS BLENDED OUT PER REO 601R-57-21-030. 2 L 7 2 4F RT A21EA 2008032500088 20080325 00088 CE 2008 3 25 DXTA20082942 1 20080315 A 3260 WARNING LIGHT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG ILLUMINATED E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 601QS 5605301 WHEN THE LANDING GEAR WAS LOWERED THE RT DOWN AND LOCKED LIGHT DID NOT ILLUMINATE, RES (UNLOCK) LIGHT REMAINED ON, BLED HYDRAULICS SYSTEMS ON AIRCRAFT IAW MM 32-30-00, 27-50-00, 27-40-00, AND 27-60-00. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500090 20080325 00090 2008 3 25 DXTA20082944 4 20080316 A 2210 AUTOPILOT SYS GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE PITCH FAILED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 719QS 162 AUTO PILOT PITCH FAILED. PERFORMED HORIZONTAL STABILIZER TRIM SYSTEM INTERFERENCE TEST, TRAVEL TEST, AND FUNCTIONAL TES T I.A.W. G200 M.M. 27-40-00. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A53NM E35NE 2008032500092 20080325 00092 2008 3 25 DXTA20082945 4 20080314 A 3410 DISPLAY CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT FAILED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 628QS 5605305 DURING CLIMBOUT PFD NR2 SCREEN WENT DARK, PFD FAILURE WAS ACCOMPANIED BY A BURNING ODOR. REMOVED AND REPLACED PFD NR 2 WITH A REPAIRED UNIT AND SECURED. OPS CHECKED SATISFACTORY IAW MM CHAPTER 34-25-01. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500113 20080325 00113 NE 2008 3 25 DJFA2008027 2 20080317 A 7397 CONNECTOR BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE ENGINE DIRTY E DJFA D RETURN TO BLOCK Y ENGINE STOPPAGE TX TAXI/GRND HDL 1 EA 23 708TA RK178 PCEJA0125 ON TAXI TO TAKEOFF, DURING EFC TEST, CREW EXPERIENCED AN UNCOMMANDED SHUTDOWN OF THE NR 2 ENGINE. MAINTENANCE CLEANED T HE EFC CONNECTOR AND PERFORMED SEVERAL GROUND RUNS, EFC TESTS, AND A T/R CHECK WITHOUT FAILURE. 2 H 7 2 4F 4 F RT A16SW E25EA 2008032500121 20080325 00121 NM 2008 3 25 SWAA081499 1 20080318 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 8L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008032500123 20080325 00123 NM 2008 3 25 SWAA081474 1 20080318 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 263, STR 9L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400175 20080324 00175 NM 2008 3 24 SWAA081365 1 20080312 A 5330 65C381921 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 857, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400204 20080324 00204 NM 2008 3 24 SWAA081378 1 20080313 A 3350 8200037710 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 221WN 34259 RIGHT AFT CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008032400215 20080324 00215 WP 2008 3 24 IXXA08SMN080S 1 20080215 A 5340 37508651 SUPPORT FITTING DOUG DC8 DC871F 302199D WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TAIL SKID SUPPORT FITTING CRACKED AT STATION 1734.000 LONGERON36. REM OVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-3-1, DC8 SRM 51-1-20D, DC 8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008032400216 20080324 00216 EU 2008 3 24 F3LA200800107 1 20080302 A 5321 D5367175604800 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE GALLEY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED POTTED INSERTS WERE FOUND MISSING ON THE AFT GALLEY 261PF FLOOR PANEL. MAINTE NANCE REMOVED AND REPLACED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-42-12 PB 401. FOLLOWING THE IN STALLATION OF THE NEW FLOOR PANEL, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008031700262 20080317 00262 CE 2008 3 17 DJFA2008010 1 20080125 A 2120 DUCT BEECH MU300 400A 1155402 CE CABIN OBSTRUCTED E DJFA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 439LX RK284 IN FLIGHT, CREW REPORTED CABIN HEAT INOP AND BURNING SMELL IN REAR OF CABIN. MAINT FOUND THE CARPET IMPROPERLY TUCKED B EHIND THE SIDEWALLS AND BLOCKING THE HEAT DUCT HOLES. THE CARPET WAS ADJUSTED AND THE SYS CHECKED SATISFACTORILY. 2 H 7 2 4F RT A16SW 2008031700266 20080317 00266 CE 2008 3 17 DXTA200802792 1 20080124 A 2760 602EN166 SWITCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LT SPEEDBRAKE INOPERATIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 645QS 7091 5605145 HAD A (NO TAKEOFF) ANNUN AFTER ADDING TO THRUST AND REACHING APPROX 30 KTS, THE LIGHT CAME ON ALONG WITH HORN. ABORTED T AKEOFF. REMOVED LT SPEEDBRAKE SWITCH P/N 602EN16-6. INSTALLED NEW LT SPEED BRAKE SWITCH P/N 602EN16-6 IAW 27-61-06 OF MM . OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008031700267 20080317 00267 CE 2008 3 17 DXTA200802798 1 20080125 A 7603 BELLCRANK BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE NR 2 ENGINE OUT OF ADJUST E DXTA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 07 149QS RK473 PCEJA0739 NR2 ENGINE WOULD NOT MAINTAIN TAKEOFF TARGET N1 OF 96.9. INITIALLY NR2 N1 INDICATED 96.9 WITH POWER LEVER AT FULL FWD BU T IMMEDIATELY DROPPED TO AND MAINTAINED 94.4. NR1 ENGINE MAINTAINED 96.9 WITH FULL POWER APPLIED. ADJUSTED NR2 ENGINE BE LL CRANK ASSY IN REAR BAY. ENGINE OPS CHECK GOOD AT THIS TIME. ALL WORK DONE IAW MM CH 76-10-00 AND 71-00-00. 2 H 7 2 4F 4 F RT A16SW E25EA 2008031800001 20080318 00001 NM 2008 3 18 C8GA20080008 1 20080306 A 7920 OIL FILTER BOEING 727 727223 1384074 NM NR 3 ENGINE DIRTY A C8GA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 29 898AA 22014 FLT 719 FROM ALT TO TOL - DURING CRUISE OPERATION, THE NR 3 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT IN TOL. THE NR 3 ENGINE OIL FILTER WAS REMOVED AND INSPECTED, CARBON CONTAMINATION WAS NOTED AND THE OIL FILTER WAS REPLACED. PERFORMED ENGINE RUN, OPS AND LEAK CHECKS. AFTER RUN THE FILT ER WAS REMOVED AND INSPECTED FOR FURTHER CONTAMINANTS. NO CONTAMINANTS NOTED. INSTALLED NEW OIL FILTER, RAN ENGINE AND PERFORMED LEAK AND OPS CHECK, NO LEAKS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2008031800009 20080318 00009 EU 2008 3 18 08FDEA00851 1 20080310 A 5753 A5797149820400 RUB STRIP AIRBUS 310 A310203 3930313 EU T/E FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT OUTBD FLAP UPPER SURFACE CENTER CHAFE STRIP IS WRINKLED AND BULGING. REMOVED & REPLACED THE CHAFE STRIP IAW SRM 57-53 -12; FIG 201. 2 L 7 2 4F RT A35EU 2008031800026 20080318 00026 EU 2008 3 18 08FDEA00868 1 20080311 A 5320 A53832103206 WEB AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CRACKS ON WEBS BETWEEN TRACK 3-4 LT/RT, 3-4 LT: 16MM 3-4RH:15MM. REPAIR PERFORMED BY CRACK STOP HOLE AND INSTALLI NG A DOUBLER IAW RAS 70503745/2008 ISS A, APPROVED BY EA 6-5315-115282. 2 L 7 2 4F RT A35EU 2008031800027 20080318 00027 EU 2008 3 18 08FDEA00869 1 20080311 A 5320 A538321000208 WEB AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CRACKS ON WEBS BETWEEN TRACK 1-2 LT. REPAIR PERFORMED BY CRACK STOP HOLE AND INSTALLING A DOUBLER IAW RAS 7050374 5/2008 ISS A, APPROVED BY EA 6-5315-115282. 2 L 7 2 4F RT A35EU 2008031800040 20080318 00040 NM 2008 3 18 QXEA200800268 1 20080228 A 5420 PANEL BOMBDR DHC8 DHC8402 1390042 NM PYLON CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - PANEL 414AR UPPER AFT SECTION IS CHAFED. REPAIRED CHAFED AREA IAW RD8/4-54-012, Q400 NDTM PART 6 51-00-01. 2 H 7 2 4T RT A13NM 2008031800045 20080318 00045 NM 2008 3 18 HALA0800385 1 20080309 A 2842 TOTALIZER BOEING 767 76733A 1385209 NM FUEL SYSTEM INTERMITTENT A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, FUEL TOTALIZER INTERMITTENT INOP. PERFORMED FUEL QTY BITE CK, NO FAULTS NOTED. OK FOR SERVIC E. 2 L 7 2 4F RT A1NM 2008031800065 20080318 00065 NM 2008 3 18 MASA200800220 1 20080311 A 2620 FIRE BOTTLE DHAV DHC8 DHC8202 2809007 NM LT AND RT MALFUNCTIONED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 989HA 427 ASH FLT 2950 PHX-ASE - LT FWD AND RT AFT FIRE BOTTLE WILL NOT ILLUMINATE DURING TEST. RESET, OPS GOOD. 2 H 7 2 4T RT A13NM 2008031800067 20080318 00067 EA 2008 3 18 MASA200800221 1 20080311 A 2560 SWITCH CNDAIR CL600 CL6002C10 1390015 EA MEGAPHONE OUT OF ADJUST A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 507MJ 10077 ASH FLT 7277 IAD-PWM. MEGA PHONE INOP. MX ADJUSTED TRANSMIT SWITCH. 2 L 7 2 4F RT A21EA 2008031800075 20080318 00075 WP 2008 3 18 08FDEA00895 1 20080311 A 5751 ARC10582 WEDGE DOUG MD10 MD1010F 3022112 WP RT AILERON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 THE RT OUTBD AILERON T/E WEDGE IS CRACKED AND THE AFT EDGE IS SEPARATED. CUT OUT DAMAGED SECTION OF THE WEDGE IAW SRM 5 7-20-00 FIG 10 VOL I. FABRICATED A NEW WEDGE SECTION & ZEE ANGLE IAW SRM 57-20-00 FIG 10 VOL I. ALODINED & PRIMED I AW SRM 51-21-01 VOL II. REMOVED 3 STATIC DISCHARGE WICK BASES IAW AMM 23-00-00-2. INSTALLED WEDGE SECTION; ZEE ANGLE & 3 STATIC DISCHARGE WICK BASES IAW SRM 51-35-01 VOL II 57-20-00 FIG 10 VOL I & AMM 23-60-00-2. 2 L 7 3 4F RT A22WE 2008031800088 20080318 00088 WP 2008 3 18 UPS08851785 1 20080301 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 AFT END OF INNER RIB CRACKED IN LT WING OB LE IB SECTION NEAR STA XFS6 27, UPPER STOPPED DRILLED CRAC K. FABBED AND INSTALLED REPAIR DOUBLER. 2 L 7 4 4F RT 4A25 2008031800096 20080318 00096 WP 2008 3 18 UPS08851810 1 20080305 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 840UP 46140 EMERGENCY EXIT LIGHTS DO NOT TEST. REPLACED EMERGENCY BATTERY PACK AND RELAY ASSY. OPS CHECK GOOD, REF MM 33-50-01. 2 L 7 4 4F RT 4A25 2008031800109 20080318 00109 WP 2008 3 18 NWAA080899954 1 20080306 A 3397 CONNECTOR DOUG DC9 DC931 3022065 WP CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 921RW 47164 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTS AT ROWS 5, 6, AND 7 ON THE RIGHT SIDE WERE INOPER ATIVE. THEY REPLACED THE EMERGENCY BATTERY POWER SUPPLY AT ALL FOUR OVERWING EXIT SIGNS BUT THAT DID NOT CORRECT THE PR OBLEM. MAINTENANCE THEN FOUND A CONNECTOR IN THE IMMEDIATE AREA DISCONNECTED. AFTER THE PLUG WAS RECONNECTED THE SYSTE M OPERATED AS DESIGNED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2008031800113 20080318 00113 NM 2008 3 18 2008UALA01222 1 20080306 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 FOUND SEAT EEL LIGHT NOT ON AT SEAT 3A FWD. REPLACED LAMP AND FUSE AND LIGHT CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031800135 20080318 00135 NM 2008 3 18 2008UALA01285 1 20080310 A 3320 81781 BALLAST BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LIGHTS FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 128UA 30023 SLIGHT BURNING SMELL APPARENT IN CABIN DURING CLIMB BUT DISSIPATED AFTER A WHILE. ELECTRICAL SMELL APPEARED IN AREA OF 3L A WHILE LATER AND SLOWLY INCREASED IN INTENSITY. UNABLE TO LOCATE SOURCE AND POWER TO GALLEYS AND ENTERTAINMENT SYSTE M REMOVED AS PRECAUTION. REPLACED FAILED BALLAST ABOVE SEATS 41 HJK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031800168 20080318 00168 NM 2008 3 18 2008UALA01326 1 20080310 A 2560 MASK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT CRACKED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 652UA 25390 SMOKE MASK ON CAPTAIN'S SIDE IS CRACKED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031800188 20080318 00188 NM 2008 3 18 MASA200800227 1 20080312 A 5540 HINGE DHAV DHC8 DHC8202 2809007 NM RUDDER DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 448YV 448 REPAIR OF AFT RUDDER CENTER UPPER HINGE 2 H 7 2 4T RT A13NM 2008031900022 20080319 00022 CE 2008 3 19 GUUA02100801 1 20080210 A 3610 BLEED AIR SYS BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA CONTAMINATED A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 231YV UE231 FLIGHT: 5401, DURING FLIGHT, FUNKY SMOKE ODOR IN THE COCKPIT WITH BLEED OPEN. CLEANED RESIDUAL OIL, FROM OIL SERVICING. 2 L 7 2 4T 3 T RT A24CE E2NE 2008031900028 20080319 00028 CE 2008 3 19 ZESA2008002 1 20080228 A 3213 65414204 STRUT CESSNA CESSNA 500 550 2076604 CE RT MLG DEFECTIVE E ZESA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 03 824CB 3664 3664 24 5500824 PILOT NOTICED AFTER LANDING GEAR WAS SELECTED UP, GEAR WARNING LIGHT AND HYDRAULIC ON LIGHT WERE ON. SELECTED GEAR DOWN , HAD THREE GREEN DOWN AND LOCKED INDICATION. WENT BACK TO ORIGINAL AIRPORT AND LANDED UNEVENTFULLY. JACKED AIRCRAFT S WUNG GEAR AND FOUND THAT RIGHT MAIN LANDING GEAR OLIO STRUT WAS NOT FULLY EXTENDED, MISALIGNING THE UPLOCK ROLLER TO SWI TCH. REPLACED OLIO STRUT WITH A SERVICEABLE UNIT. 1 L 7 2 4F A22CE 2008031900030 20080319 00030 WP 2008 3 19 ABXR080082 1 20080214 A 5531 99118275 RIB DOUG DC9 DC933F 302207A WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 RIB CRACKED AT FASTENER LEFT SIDE VERT STABILIZER LEADING EDGE ZFS 93. REPAIRED RIB IAW DC9 SRM D05159. 2 L 7 2 4F A6WE 2008031900032 20080319 00032 SO 2008 3 19 GUUA03030801 1 20080303 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN SMOKE A GUUA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 29 282AS 120226 FLIGHT:9264, DURING CLIMB THROUGH 3000 FT, THERE WAS A STRONG ODOR OF ELECTRICAL SMOKE. RETURNED TO DEPARTURE, LANDED W ITHOUT INCIDENT. INSPECTED BUSS BARS PERFORMED ENGINE RUN TURNED ON ALL SYS, NO SMOKE NOTED. TEST FLIGHT SATISFACTORY. 2 L 7 2 4T 4 T RT A31SO E20NE 2008031900059 20080319 00059 EA 2008 3 19 TRAX200800365 1 20080302 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 906EV 7642 RIGHT NR 2 EXTERIOR FUSE EMERGENCY EXIT LIGHT INOP. 2 L 7 2 4F RT A21EA 2008031900061 20080319 00061 EA 2008 3 19 TRAX200800366 1 20080303 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 SERVICE DOOR MISSING EMERGENCY EXIT INSTRUCTION PLACARD. 2 L 7 2 4F RT A21EA 2008031900069 20080319 00069 EA 2008 3 19 TRAX200800377 1 20080305 A 5320 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 CORROSION DAMAGE IN MAIN AVIONICS BAY JUST FWD OF DOOR CUTOUT FS 364.00 AT STR 27 (MARKED). C/W REPAIR ON CORROSION DA MAGE IN MAIN AVIONICS BAY FWD OF DOOR CUT OUT. 2 L 7 2 4F RT A21EA 2008031900125 20080319 00125 CE 2008 3 19 0211 1 20080213 A 2910 592712010 LINE CESSNA 425 425 2076018 CE PWA PT6 PT6* 52043 EA HYDRAULIC SYS CHAFED E CX0A K NONE O OTHER IN INSP/MAINT 1 SO 19 425AL 4787 4250100 FOUND BOTH LT AND RT MLG UPLOCK HYD LINES P/N 5927120-10 AND 5927120-11 WITH TOOLING MARKS. THESE MARKS EXCEEDED THE MIN WALL THICKNESS AND HAD DENTED THE LINE. THE TOOLING MARKS ARE CAUSED BY YEARS OF REMOVING AN INSPECTION PANEL DIRECTLY BEHIND THE LINE. MORE CAUTION SHOULD BE TAKEN DURING PANEL REMOVAL. MFG COULD NOT GIVE A LEAD TIME OR PRICE FOR PURCHASI NG NEW REPLACEMENT PARTS BUT WILL CHARGE YOU $600 FOR SPEC'S OF THE ASSEMBLY. 1 L 7 2 3T 3 T RT A7CE E2NE 2008031900145 20080319 00145 EA 2008 3 19 TRAX200800383 1 20080227 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 RT FLOOR SILL AT FS 280 CORRODED. REPAIRED IAW W/O 84336 EC/TC 670-53-21-139. 2 L 7 2 4F RT A21EA 2008031900181 20080319 00181 EA 2008 3 19 TRAX200800381 1 20080306 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 917EV 7769 FS 280 WEB IS CRACKED AT RBL 9. FS 280 WEB AT RBL 9 CLEANED OF CORROSION PREVENTATIVE COMPOUND PER CRJ200 AMM 51-26-00, INSPECTED DISCREPANT AREA NO DEFECTS NOTED, RE-APPLIED CORROSION PREVENTATIVE COMPOUND PER CRJ200 SRM 51-21-11. REFER TO ATTACHED M234 ITEMS 2 THRU 4 FOR WORK PERFORMED. CLEANED STA 280 PILOTS BULKHEAD WEB AT RBL 9 PER CRJ 200 AMM 51-26- 00. VISUALLY INSPECTED BULKHEAD WEB, NO DEFECTS NOTED. PERFORMED EDDY CURRENT INSPECTION OF SUSPECT AREA AT RBL 9 FS 2 80 IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. RE-APPLIED CORROSION - PREVENTIVE COMPOUND AS PER CRJ 200 SRM 51-21-11 TO 280 BULKHEAD WEB AT RBL 9. JOB COMPLETED. SUPPLEMENTAL SDR CLOSED3/11/08. 2 L 7 2 4F RT A21EA 2008031900191 20080319 00191 EA 2008 3 19 TRAX200800388 1 20080307 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 856AS 7404 FWD FACING OVERWING EMERGENCY EXIT LIGHTS IN CEILING INOP. RESET SYS C/B. 2 L 7 2 4F RT A21EA 2008031900195 20080319 00195 EU 2008 3 19 USAA920080606 1 20080310 A 2700 3945123506 COMPUTER AIRBUS 320 A320231 3930325 EU NR 2 MALFUNCTIONED A USAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION UK UNKNOWN 1 EA 19 644AW 27361 68 317 FLT 363 - PHX-SMF - UNSCHEDULED LANDING - CREW REPORTED AN ELECTRICAL BURNING SMELL IN THE COCKPIT JUST AFTER AN ELAC-2 FAULT. CREW WERE UNABLE TO RESET AND SUSPECTED THE BURNING SMELL WAS FROM THE ELAC (ELEVATOR AILERON COMPUTER). THE AI RCRAFT WAS DIVERTED TO LAS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ELEVATOR AILE RON COMPUTER. SYSTEM TEST PASSED AND NO ELECTRICAL SMELL NOTED. 2 L 7 2 4F RT A28NM 2008031900230 20080319 00230 NM 2008 3 19 USAA920080577 1 20080301 A 5320 D53480019216 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801AW 889 SAL - MAJOR REPAIR - C7 CHECK - CRACKED CABIN SHEAR PLATE, BS 2884 / FR 68 - BS 2936 / FR 69, +Y1292. REPLACED CABIN SH EAR PLATE, BS 2884 / FR 68 - BS 2936 / FR 69, +Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900235 20080319 00235 EU 2008 3 19 USAA920080585 1 20080224 A 5315 D53472098006 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651AW 866 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3101 /FR 65 - BS 3207 /FR 67, +Y919. REPLACED CABIN FL OORBEAM, BS 3101 /FR 65 - BS 3207 /FR 67, +Y919 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900240 20080319 00240 EU 2008 3 19 USAA920080592 1 20080306 A 3350 3214 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AW 57548 13273 661 PIT - EEL - C8 CHECK - EMERGENCY POWER SUPPLY UNIT 13WL FAILS EXTERNAL LOAD TEST. REPLACED AN OPERATIONAL CHECKED EMER GENCY POWER SUPPLY UNIT 13WL. 2 L 7 2 4F RT A28NM 2008031900246 20080319 00246 2008 3 19 TAMF20080011O 4 20080307 A 3160 CDU BOEING 767 767200 1385120 NM COCKPIT MALFUNCTIONED W TAMF K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 23 769QT 23801 PILOT REPORT, DURING TAXIING RIGHT CDU WENT BLANK ALONG WITH ELECTRICAL SMOKE. INITIALLY ITEM WAS TRANSFERRED TO DMI 09 052 MEL 34-61-1-1 CAT C, AND MAP 34-61-1-1 WAS PERFORMED. RIGHT CDU WAS REMOVED AND REPLACED IAW AMM 34-61-02 PG 201-20 6. 2 L 7 2 4F RT A1NM 2008031900248 20080319 00248 NM 2008 3 19 KCSA081172 1 20080312 A 5311 STRAP BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 AFT CARGO PIT FUSELAGE FRAME STABILIZATION STRAP CRACKED BETWEEN BS 7150 AND 1770, LBL 83, WL 135. 2 L 7 4 4F RT A20WE 2008031900249 20080319 00249 NM 2008 3 19 DXTA200802795 1 20080125 A 3297 CIRCUIT BOARD AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE MLG DAMAGED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 284QS 185 BRAKES DO NOT WORK PROGRESSIVELY. THEY GRAB OR RELEASE SUDDENLY WHEN PRESSED OR RELEASED. INSPECTED ALL GEAR UPLOCK SWI TCHES WIRING, NO DEFECTS NOTED. CHECKED UPLOCK SWITCHES ADJUSTMENTS AND GEAR UPLOCK LINKAGE, NO DEFECTS NOTED. REPLACED LANDING GEAR CONTROL PCB (A162) WITH NEW PCB (A162). CYCLED LANDING GEAR NUMEROUS TIMES, OPS CHECK GOOD. VERIFIED THAT R ED TRANSIT LIGHT EXTINGUISHES AFTER CYCLE. ALL WORK IAW 400XP WDM 32-31-01 AND 400XP MM 32-20-00, 32-30-00. 2 L 7 2 4F 4 F RT A50NM E44NE 2008031900253 20080319 00253 NM 2008 3 19 SPAA0800096 1 20080215 A 3350 110049 POWER SUPPLY BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15A 52051 NE EMERGENCY LIGHTS INOPERATIVE A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 07 712S 23038 AFT SECTION OF FLOOR PATH ESCAPE LIGHTING INOPERATIVE. REPLACED FLOOR TRACK POWER SUPPLY IAW MM 33-21-27. OPS CHECK SATI SFACTORY. 2 L 7 2 4U 4 F RT A16WE E2EA 2008031900265 20080319 00265 CE 2008 3 19 021708N554CS1 1 20080217 A 2910 AE6209H0300130 LINE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE HYD SYSTEM DEFECTIVE E Z5FA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 EA 63 554CS 2359 5605572 DURING APPROACH THE (LOW HYD LEVEL) AND (LT/RT LOW HYD FLOW) INDICATION ILLUMINATED. CREW FOLLOWED THE ABNORMAL CHECKLIS T, MANUALLY EXTENDED THE LANDING GEARS, AND DECLARED AN EMERGENCY LANDING. LANDING WAS UNEVENTFUL. MAINT FOUND A DEFECTI VE LT HYDRAULIC PUMP PRESSURE LINE. THE PRESSURE LINE WAS REPLACED, HYD SYS WAS SERVICED, GEAR SWINGS WERE PERFORMED AND SYS WAS LEAKED CHECKED WITH ENGINES RUNNING. OPS AND LEAK CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008031900270 20080319 00270 EA 2008 3 19 TRAX200800389 1 20080304 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 917EV 7769 CARGO COMPT DOOR CUTOUT COAMING HAS PITTING AND CORROSION ALONG BOTTOM (MARKED). 2 L 7 2 4F RT A21EA 2008031900272 20080319 00272 EA 2008 3 19 TRAX200800382 1 20080306 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 917EV 7769 FS 280 AFT FLOOR SUPPORT ANGLE IS CRACKED AT LBL 9. JOB COMPLETE. REFER TO M-234 FORM STEPS 2 THRU 9 FOR CORRECTIVE AC TION. CUT AWAY DAMAGED SECTION OF 280 AFT FLOOR SUPPORT ANGLE IAW REO 601R-53-11-138. PERFORMED NDT ON CUTLINE PER REO 601R-53-11-138 NO DEFECTS NOTED AT THIS TIME PER NDTM 51-20-08. FABRICATED -3 AND -5 REPAIR ANGLES IAW REO 601R-53-11- 138. HEAT TREAT REQUIRED. HEAT TREATED FABRICATED -3 & -5 ANGLES TO T62 CONDITION AS PER CRJ 200 SRM 51-24-06. HARDNE SS TEST GOOD. DRILLED AND FIT -3 & -5 REPAIR ANGLES IAW REO 601R-53-11-138 READY TO INSTALL. FABRICATED -1 FILLER ANGL E FROM NEW 600-3407-595 ANGLE IAW REO 601R-53-11-138. READY TO INSTALL. INSTALLED -1 FILLER ANGLE AND -3 & 5 REPAIR AN 2 L 7 2 4F RT A21EA 2008031900277 20080319 00277 EA 2008 3 19 VNAA0803002 1 20080306 A 4920 APU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE MALFUNCTIONED A VNAA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 05 202PS 7858 CREW REPORTED THE APU FLAMED OUT AFTER ENGINE SHUTDOWN. GROUND CREW STATED SMOKE WAS COMING FROM THE RIGHT SIDE OF THE AIRCRAFT. MAINTENANCE INSPECTED AND FOUND SMOKE COMING FROM THE APU INTAKE DOOR, FUEL LEAKING FROM DRAIN ON TO THE AFT EQUIPMENT BAY. MAINTENANCE PERFORMED A GENERAL VISUAL CHECK OF THE APU, PERFORMED A GENERAL VISUAL INSPECTION OF THE AP U FUEL SYSTEM COMPONENTS AND PERFORMED A START/STOP SEQUENCE OF THE APU IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANU AL. OPERATIONAL CHECKS WERE PERFORMED. NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008031900279 20080319 00279 NM 2008 3 19 CALA0800210 1 20080306 A 5311 BAC1517705 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16703 28764 FUSELAGE FRAME CRACKED BETWEEN STR 8 AND 9 LT AT STA 787. INTERIM REPAIRED PER ECRA5310-04729. DIP CONTROL NUMBER 8693 8. 2 L 7 2 4F RT A16WE 2008031900281 20080319 00281 NM 2008 3 19 CALA0800212 1 20080306 A 5311 BAC1517705 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16703 28764 FRAME CRACKED STA 400 AT S-9R. INTERIM REPAIR PER ECRA5310-04729. DIP CONTROL NUMBER 86938. 2 L 7 2 4F RT A16WE 2008031900292 20080319 00292 NE 2008 3 19 GLBA20061054 2 20080130 A 7200 PT6A67D ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE NR 1 DETERIORATED A GLBA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 NM 03 154GL 24839 12853 UE154 ENGINE SHUTDOWN, FLT 5041 ENROUTE 10 MILES OUT ON FINAL THE NR1 ENGINE FEATHERED INFLIGHT AND THE PILOTS PERFORMED THE E NG SECURE PROCEDURES AND SHUTDOWN THE ENG MAINT REMOVED AND REPLACED THE NR1 ENG ASSY IAW TASKCARD NR 1900-7100.00. RII INSP COMPLIED WITH. 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900293 20080319 00293 EU 2008 3 19 USAA920080565 1 20080301 A 5315 D5347217220290 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651AW 866 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3158 /FR 66 - BS 3257 /FR 68, +Y1292. REPLACED CABIN F LOORBEAM, BS 3158 /FR 66 - BS 3257 /FR 68, +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900299 20080319 00299 CE 2008 3 19 DXTA200802793 1 20080124 A 3233 AIR484843 ACTUATOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP RT MLG DOOR MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 896QS 3672 258640 RT21, MLG RED LIGHT ILLUMINATES WHEN AC IS ACCELERATED ABOVE ABOUT 280KIAS. REMOVED MALFUNCTIONING RT MLG DOOR ACTUATOR AND INSTALLED OVERHAULED ACTUATOR IAW MAINT CONTROL. VERIFIED ALL RT MLG INDICATION WIRING CONDITION AND SECURITY WITH SATISFACTORY RESULTS. VERIFIED AND ADJUSTED RT MLG DOOR RIGGING WITH SATISFACTORY RESULTS. ALL WORK PERFORMED IAW AMM CH 32-10-41 AND CH 32-60-00. RT MLG DOOR ACTUATOR AND INDICATION OPERATIONAL AND LEAK CHECKED SATISFACTORY. 2 L 7 2 4F 4 F RT A3EU E6WE 2008031900302 20080319 00302 CE 2008 3 19 DXTA200802812 1 20080130 A 2720 991455811 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RUDDER MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 986QS 2533 2533 7500086 ON CLIMB OUT, PASSING THROUGH 10,000 FT AND 250 KIAS , RUDDER LIMIT FAIL-B CAS MESSAGE LIMIT WAS FAILED AT 26 PERCENT. TROUBLESHOT: REPLACED ACTUATOR A IAW MM CHAP 27-23-00 OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008031900303 20080319 00303 NM 2008 3 19 USAA920080610 1 20080225 A 5312 6517582 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 CLT - MAJOR REPAIR - C17 CHECK - CRACKED BULKHEAD VERTICAL BEAM WEB, BS 178, RBL 17, WL 228. REPLACED BULKHEAD VERTICAL BEAM WEB, BS 178, RBL 17, WL 228 IAW B737 SRM 51-20-01. 2 L 7 2 4F RT A16WE 2008031900306 20080319 00306 NM 2008 3 19 USAA920080613 1 20080304 A 5311 6547959 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 CLT - MAJOR REPAIR - C17 CHECK - LEVEL 2 CORROSION ON FRAME, BS 794.5, RBL 13.80. REPAIRED FRAME, BS 794.5, RBL 13.80 I AW B737 SRM 51-70-11. 2 L 7 2 4F RT A16WE 2008031900312 20080319 00312 EA 2008 3 19 TRAX200800391 1 20080308 A 2751 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA K NONE J WARNING INDICATION CL CLIMB 1 SO 27 929EV 8007 FLAPS FAIL MSG WHEN RETRACTING FROM 8 TO 0 AFTER TAKEOFF. F/CTL PAGE SHOWED ZERO DEGREES ON BOTH SIDES BUT RECEIVED FLA P OVERSPEED AURAL WARNING ABOVE 230 KTS ZERO FLAP LANDING IN ATL, VERTICAL SPEED AT TOUCHDOWN 100 FPM. EMERGENCY DECLAR ED. 2 L 7 2 4F RT A21EA 2008031900314 20080319 00314 EA 2008 3 19 TRAX200800393 1 20080309 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 760EV 10212 THE 2 MOST AFT CEILING EMERGENCY LIGHTS INOP. 2 L 7 2 4F RT A21EA 2008031800118 20080318 00118 NM 2008 3 18 2008UALA01250 1 20080307 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY LIGHT INOP, DR 4R CEILING, RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031800125 20080318 00125 NM 2008 3 18 2008UALA01273 1 20080308 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 INTERCOSTAL IS CRACKED AT BS 291.5 JUST ABOVE STR 11R. MAJOR REPAIR ACCOMPLISHED: REPLACED INTERCOSTAL JUST ABOVE STRI NGER 11R. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800134 20080318 00134 NM 2008 3 18 2008UALA01284 1 20080308 A 3510 RCF6705 SOLENOID VALVE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW O2 SYSTEM FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 815UA 867 CREW O2 SYSTEM, OP CHECK OF LP SOLENOID FAILED. LP VALVE FAULTY. REPLACED LP SOLENOID VLV. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031800146 20080318 00146 EU 2008 3 18 2008UALA01297 1 20080310 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 489UA 1702 DENT BETWEEN STR 20L AND 21L 4" FWD OF FRAME 12. ACCOMPLISHED MAJOR REPAIR IN LCQ. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031800154 20080318 00154 NM 2008 3 18 2008UALA01307 1 20080308 A 3350 101331101 LENS BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 RT OVERWING EMERGENCY EXIT SIGN DAMAGED. REPLACED BROKEN LENS IAW 33-51-11. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031800187 20080318 00187 EA 2008 3 18 MASA200800226 1 20080312 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 919FJ 15019 ASH FLT 2824 PHX-TUS - GALLEY FLOOR LEVEL EMERGENCY LIGHTS INOP. MX RE-LAMPED, OPS GOOD. 2 L 7 2 4F RT A21EA 2008031900001 20080319 00001 SO 2008 3 19 N93A26012008 1 20080126 A 3297 CONNECTOR GULSTM G1159 GIV 3980115 SO DOWNLOCK SWITCH DISCONNECTED E N93A A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 SO 13 460QS 1360 AFTER GEAR EXTENSION LT MAIN LANDING GEAR DOWN LOCK LIGHT DID NOT ILLUMINATE. MAINTENANCE FOUND LT DOWNLOCK SWITCH CONN ECTOR DISCONNECTED. RECONNECTED AND OPS CHECKED GOOD. 2 L 7 2 4F RT A12EA 2008031900034 20080319 00034 CE 2008 3 19 GUUA03090801 1 20080309 A 3260 H111541 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT MLG SHORTED A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 190YV UE190 FLIGHT: 9193, DURING FLIGHT, GEAR HANDLE LIGHTS ILLUMINATED INTERMITTENTLY. RETURNED TO DEPARTURE. LANDED WITHOUT INCID ENT. REPLACED RT MAIN GEAR UPLOCK SWITCH. 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900052 20080319 00052 CE 2008 3 19 DXTA200802804 1 20080128 A 3080 HEATER CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE PITOT LINE MALFUNCTIONED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 381QS 6800097 AMBER PITOT STATIC COLD R CAME ON DURING T/O ROLL. CYCLED SEVERAL TIMES, INTERMITTENT THEREAFTER. TROUBLESHOT PITOT STA TIC SYS AND FOUND SYS TO WORK NORMAL SEVERAL TIMES. COMPLIED WITH PITOT STATIC AND STANDBY HEATER CHECK IAW MM CH 34-11- 00. INSPECTED RT PITOT HEATER WIRING CONNECTOR, FOUND TO BE GOOD. 2 L 7 2 4F 4 F RC T00012WI E35NE 2008031900054 20080319 00054 NE 2008 3 19 20080306 2 20080302 A 7250 SHROUD EMB ERJ170 ERJ170100SE 3260406 NM GE CF34 CF348E5 30061 NE NR 1 ENGINE DAMAGED A UHLA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 GL 11 861RW 17000094 GEE193262 FLIGHT 6451 ATL TO MSY ON DESCENT NR 1 ENGINE N1 WAS AT APPROX 25-28%, THE ITT WENT TO AMBER THEN RETURNED TO NORMAL FOR A MOMENT ONLY TO RETURN TO AMBER AND THEN RED. CREW SHUT DOWN NR 1 ENGINE AND LANDED WITHOUT INCIDENT. ENGINE BORESCO PE REVEALED 3RD STAGE TURBINE SHROUD HAS DAMAGE RESULTING IN LOSS OF MATERIAL. NOT SURE AT THIS TIME IF THE T3 SHROUD D AMAGE WAS THE CAUSE OF THE EVENT OR A RESULT. ENGINE WAS REMOVED AND REPLACED. SPECIFIC PART OR STRUCTURE CAUSING THE DIFFICULTY UNKNOWN AT THIS TIME. 2 L 7 2 4F 4 F RT A56NM E00063EN 2008031900058 20080319 00058 EA 2008 3 19 TRAX200800364 1 20080302 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SO 27 878AS 7590 FLAPS FAIL MSG IN FLT FAILED AT FLAPS INDICATION OF 8 WHEN SELECTED TO 20. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGEN CY DECLARED. 2 L 7 2 4F RT A21EA 2008031900072 20080319 00072 EA 2008 3 19 TRAX200800380 1 20080306 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 917EV 7769 FLOORBEAM AT LBL 36 AND FS 621 HAS POSSIBLE CRACK ON OUTBOARD UNDERSIDE IN RADIUS. 2 L 7 2 4F RT A21EA 2008031900074 20080319 00074 NM 2008 3 19 KCSA081147 1 20080307 A 5320 STRAP BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 STABILIZATION STRAP BROKEN AT STA 2160 TO 2200 RBL 13. 2 L 7 4 4F RT A20WE 2008031900085 20080319 00085 NM 2008 3 19 KCSA081154 1 20080307 A 5311 FRAME BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 UPPER CHORD AT STA 2200 FRAME CORRODED LBL 4 TO LBL 50. 2 L 7 4 4F RT A20WE 2008031900086 20080319 00086 SO 2008 3 19 GLBA20061055 1 20080129 A 5712 RIB EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT WING CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 108UX 120108 LT RIB NR 21 AT WS YA-6750 BETWEEN WING FRONT SPAR AND THE WING AUXILLARY SPAR, CRACKED FWD AND AFT OF STRINGER NR 1. CR ACKS APPROX .375 INCH IN LENGTH. MAINTENANCE REMOVED DAMAGED AREA AND INSTALLED REPAIR PIECE IAW SRM 57-20-07 REPAIR PI ECE CUT FROM NEW RIB. 2 L 7 2 4T 4 T RT A31SO E20NE 2008031900096 20080319 00096 NM 2008 3 19 KCSA081163 1 20080310 A 5311 FRAME BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 BS 2200 FUSELAGE FRAME LOWER CHORD CORRODED ABOVE STR 42L, LBL 33. 2 L 7 4 4F RT A20WE 2008031900102 20080319 00102 CE 2008 3 19 AMWA89766BC 1 20080124 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CL CLIMB 1 CE 07 135YV 11541 74 UE135 AFTER TAKEOFF, BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINT REPLACED BATTERY AND CLEARED DISCREPANCY. 2 L 7 2 4T 3 T RT A24CE E4EA 2008031900119 20080319 00119 EA 2008 3 19 S9BA20080005 1 20080211 A 5411 C6W1708275 FRAME DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA LT NACELLE CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 20206 1310 573 CPCP INSPECTION, LT NACELLE HOOPFRAME CORRODED. REMOVED AND REPLACED HOOP FRAME IAW SRM 57-30-00 PAGE 1 AND AC 43-13, P ARA 4-57. AC GROUNDED, YES. 1 H 7 2 3T 4 T RT A9EA E4EA 2008031900209 20080319 00209 EU 2008 3 19 USAA920080567 1 20080228 A 5320 D53471123203 SUPPORT FITTING AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651AW 866 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SUPPORT FITTING, BS 3310 /FR 69 - BS 3366 /FR 70, -Y1170. REPLACED C ABIN SUPPORT FITTING , BS 3310 /FR 69 - BS 3366 /FR 70, -Y1170 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900241 20080319 00241 NM 2008 3 19 USAA920080593 1 20080303 A 5347 D57130142202 SEAT TRACK AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801AW 889 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SEAT TRACK, BS 1430 / FR 36 - BS 1650 / FR 41, +Y1292. REPLACED CABI N SEAT TRACK, BS 1430 / FR 36 - BS 1650 / FR 41, +Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900257 20080319 00257 CE 2008 3 19 GLBA20061067 1 20080211 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 177 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 257GL UE257 FRAME AT FS 177.35 AND STR 9R CRACKED APPROX .500 INCHES IN LENGTH. **SUPPLEMENTAL INFORMATION WILL BE PROVIDED UPON COM PLETION OF THE REPAIR** 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900261 20080319 00261 CE 2008 3 19 021408N329CS1 1 20080214 A 2731 5534200161 TRIM TAB CESSNA 500 550 2076604 CE PWA 530 PW530A NE ELEVATORS LACK OF LUBE E Z5FA A UNSCHED LANDING W F J INADEQUATE Q C FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 EA 63 329CS 3921 5501077 DURING DESCENT FROM FL36, AUTO PILOT MIS TRIM LIGHT ILLUMINATED. ELEVATOR TRIM WOULD NOT TRIM PAST 1 INCH FROM FULL DOWN POSITION. THE AC DIVERTED AND AN EMERGENCY WAS DECLARED. AC LANDING WAS UNEVENTFUL. MAINT LUBRICATED THE ELEVATOR TRIM TABS AND PERFORMED AN AUTOPILOT FUNCTIONAL CHECK. AN OPERATIONAL CHECK FLIGHT (OCF) WAS PERFORMED FOLLOWING MAINT. THE O CF WAS SUCCESSFUL. 1 L 7 2 4F 4 F A22CE E00053EN 2008031900274 20080319 00274 NM 2008 3 19 USAA920080616 1 20080209 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER TIE CLIP, BS 727C, S4R. REPLACED STRINGER TIE CLIP, BS 727C, S4R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008031900276 20080319 00276 NM 2008 3 19 USAA920080618 1 20080208 A 5320 6517684 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED INTERCOSTAL, BS 294.5, S7L. REPLACED INTERCOSTAL, BS 294.5, S7L IAW B737 SRM 5 1-40-02. 2 L 7 2 4F RT A16WE 2008031900282 20080319 00282 NM 2008 3 19 CALA0800213 1 20080309 A 5320 149N713073 SUPPORT BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14115 27557 WING TO BODY FAIRING STRUCTURE AT BL 0 FWD ECS DOOR SUPPORT ATTACH ANGLE HAS CORROSION. PERFORMED REPAIR TO P/N 149N713 0-73 OUTBOARD CHORD, BS 900 LBL 11.5 TO RBL 11.5 REF ECRA 5352-01034. 2 L 7 2 4F RT A2NM 2008031900321 20080319 00321 NM 2008 3 19 SA08013 1 20080312 A 3350 32145410 EPSU AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 832AW 22985 1643 PHX - AIRCRAFT FAILED THE OPERATIONAL TEST OF THE EMERGENCY LIGHTS SYSTEM. MAINTENANCE REPLACED THE EMERGENCY POWER SUP PLY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2008031900323 20080319 00323 NM 2008 3 19 KCSA081174 1 20080313 A 5330 SKIN BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 L3 WINDOW, AFT LOWER CORNER EXTERIOR FUSELAGE SKIN HAS A CRACK EXTENDING FROM FASTENER HOLE .250 INCH LONG AT STA 338, S TR 8L. 2 L 7 4 4F RT A20WE 2008031900329 20080319 00329 CE 2008 3 19 DXTA200802815 1 20080131 A 2797 CONNECTOR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE SPEED BRAKE LOOSE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 393QS 5600393 DURING T/O POWER APPLICATION HYD PRESS LIGHT CAME ON AT APPX 80 PERCENT N1. ABORTED T/O. GAINED ACCESS TO SPEED BRAKE S WITCHES. FOUND CONNECTOR FOR SWITCH WIRING IN LT SPEED BRAKE COVE NOT FULLY SEATED. C/W SPEEDBRAKE SWITCH RIG. SECURE D CONNECTORS. C/W SATISFACTORY GROUND RUNS AT T/O POWER. ALL INDICATORS NORMAL. ALL WORK IAW MM 27-60-00 2 L 7 2 4F 4 F RT A22CE E25EA 2008031900340 20080319 00340 NM 2008 3 19 USAA920080626 1 20080304 A 5310 146N871333 DOOR FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 917UW 22193 PIT - MAJOR REPAIR - C1 CHECK - L4 DOOR CUTOUT FORWARD FRAME DOOR JAMB WEB CRACKED, BS 1640, S12L. REPAIRED THE L4 DOOR CUTOUT FORWARD FRAME DOOR JAMB WEB, BS 1640, S12L IAW B757 SRM 51-70-13. 2 L 7 2 4F RT A2NM 2008031900341 20080319 00341 NM 2008 3 19 USAA920080627 1 20080304 A 5310 146N871332 DOOR FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 917UW 22193 PIT - MAJOR REPAIR - C1 CHECK - R4 DOOR CUTOUT FORWARD FRAME DOOR JAMB WEB CRACKED, BS 1640, S12R. REPAIRED THE R4 DOOR CUTOUT FORWARD FRAME DOOR JAMB WEB, BS 1640, S12R IAW B757 SRM 51-70-13. 2 L 7 2 4F RT A2NM 2008031900343 20080319 00343 SO 2008 3 19 C2XA08TY035 1 20080313 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16919 145393 TYS - DURING A OVERNIGHT A-CHECK THE AFT CEILING EMERGENCY LIGHT WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE E MERGENCY LAMP IAW AMM 33-50-08. OPS CHECKS GOOD. 2 L 7 2 4T RT T00011AT 2008031900347 20080319 00347 SO 2008 3 19 C2XA08CL029 1 20080313 A 3350 1317 LIGHT EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12946 145052 DURING ROUTINE MAINTENANCE THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LIGHT BULB. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2008031900349 20080319 00349 NM 2008 3 19 CALA0800218 1 20080313 A 5320 141A541012 INTERCOSTAL BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24715 28786 INTERCOSTAL FRAME CRACKED AT SCREW HOLES BETWEEN STA 312-328 AND RBL 30. REMOVED AND REPLACED INTERCOSTAL BETWEEN STA 3 12-328 AT RBL 30. REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008031900353 20080319 00353 EA 2008 3 19 TRAX200800398 1 20080310 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 AAR - LEFT OVERWING EMERGENCY EXIT PUSH PLACARD DAMAGED. 2 L 7 2 4F RT A21EA 2008031900354 20080319 00354 EA 2008 3 19 TRAX200800399 1 20080310 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 972EV 7534 AAR - CLIP CRACKED O/B SIDE OF LBL 27 AT FS 484. 2 L 7 2 4F RT A21EA 2008031900355 20080319 00355 EA 2008 3 19 TRAX200800400 1 20080310 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 972EV 7534 AAR - CLIP CRACKED O/B SIDE OF LBL 27 AT FS 484. 2 L 7 2 4F RT A21EA 2008031900357 20080319 00357 EA 2008 3 19 TRAX200800402 1 20080310 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 972EV 7534 AAR - FS 280 CLIP CRACKED O/B OF LBL 9. 2 L 7 2 4F RT A21EA 2008031900358 20080319 00358 EA 2008 3 19 TRAX200800403 1 20080310 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 972EV 7534 AAR - FS 280 CLIP CRACKED O/B OF RBL 9. 2 L 7 2 4F RT A21EA 2008032400227 20080324 00227 EU 2008 3 24 F3LA200800112 1 20080302 A 5321 D5367175201800 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED DELAMINATION WAS FOUND ON THE EDGE OF FLOOR PANEL 251WF. MAINTENANCE REPAIRED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 212. FOLLOWING COMPLETON OF THE REPAI R, THE FLOOR PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400229 20080324 00229 EU 2008 3 24 F3LA200800114 1 20080302 A 5321 D5361067500000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTING FINDING DELAMINATION ON THE EDGE OF FLOOR PANEL 222EF. MAINTENANCE REPAIRED THE DAMAGED PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 PB 201, PARAGRAPH 8.J, FIGURE 212. FOLLOWING COMPLETION OF THE REPAIR, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400266 20080324 00266 NM 2008 3 24 HNAA0800102 1 20080314 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INTERMITTENT A HNAA O OTHER O OTHER CR CRUISE 1 EA 07 810EX 39478 39478 308 CABIN EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY IN FLIGHT. FOUND POWER SUPPLY 3352 PS2 WOULD INTERMITTENTLY TURN ON F LOOR LIGHTS. REMOVED AND REPLACED 3352-PS2 POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2008032400354 20080324 00354 2008 3 24 2008UALA01394 4 20080313 A 2565 62773318 SLIDE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE R3 DOOR UNWANTED DEPLOY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 785UA 26954 DOOR 3R SLIDE DISCHARGED. SLIDE DEPLOYED ACCIDENTALLY. REPLACED DOOR SLIDE PER AMM 25-66-00 P.201, 25-66-01 P.401, REP LACED 'EPAS' RESERVOIR PER AMM 52-11-22 P.401. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032400361 20080324 00361 NM 2008 3 24 2008UALA00028 1 20080101 A 2421 757183F GENERATOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 ENGINE MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 795UA 26927 ELEC BACKUP GEN R RIGHT BACKUP GENERATOR OFF DUE TO A PROTECTIVE TRIP. SUSPECT SHAFT SHEARED. REPLACED LT BACK UP GENE RATOR. OPS CHECKS GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032400383 20080324 00383 NM 2008 3 24 SWAA081456 1 20080317 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032400384 20080324 00384 NM 2008 3 24 SWAA081457 1 20080313 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503, BETWEEN STR 20R AND STR 21R. REPAIRED SKIN PER SWA E A. 2 L 7 2 4F RT A16WE 2008032500007 20080325 00007 NM 2008 3 25 DXTA20082887 1 20080218 A 2780 1250A000002 CONTROL UNIT GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE KRUEGER FLAPS INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 706QS 870 131 ON DEPARTURE, RECEIVED (KRUEGER IMBALANCE) CAS MESSAGE. REMOVED AND REPLACED FLAP/SLAT ELECTRIC CONTROL UNIT. PERFORMED FUNCTIONAL TEST WITH NO DEFECTS NOTED. ALL WORK DONE IAW MM CHAPTER 27-51-45 AND CHAPTER 27-52-00. (SQK NR 1.4) 2 L 7 2 4F 4 F RT A53NM E35NE 2008032500016 20080325 00016 CE 2008 3 25 DXTA20082896 1 20080224 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE WEAK E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 337QS 5600437 RT BRAKE PEDAL ON RT SEAT SIDE GOES TO THE FLOOR WHEN BRAKES ARE PRESSED. COMPLIED WITH BRAKE BLEED IAW MM 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2008032500019 20080325 00019 CE 2008 3 25 DXTA20082897 1 20080224 A 3241 ANTI-SKID SYS CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE MLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 814QS 5600776 ON TAXI OUT LOW BRAKE PRESS AND ANTI-SKID INOP LIGHT ILLUMINATED. NORMAL BRAKING WAS INEFFECTIVE. EMERGENCY BRAKE WAS US ED TO STOP THE AC. GAINED ACCESS TO ANTI-SKID CONTROLLER AND FOUND NO FAULTS. EMERGENCY PNEUMATIC BOTTLE IS SERVICED TO TOP OF GREEN ARC. BLED ANTI-SKID BRAKE SYS IAW CHECKLIST AND MM CHAPTER 32-42-01. SERVICED BRAKE RESERVOIR IAW MM CHA PTER 12-12-02. ANTI-SKID SYSTEM OPS CHECK GOOD. TAXI CHECK GOOD. AFTER RESETTING CIRCUIT BREAKER IT NEVER TRIPPED DURI NG SERVICING OR OPS CHECKS. 2 L 7 2 4F 4 F RT A22CE E00053EN 2008032500030 20080325 00030 NM 2008 3 25 2008UALA01364 1 20080312 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY EXIT LIGHT INOP AT DOOR 3 RIGHT SILL. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032500052 20080325 00052 NM 2008 3 25 USAA920080591 1 20080306 A 5313 654657959 STRINGER BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - CORROSION ON STRINGER, BS 1125, RBL 24, WL 230. REPLACED STRINGER, BS 1125, RBL 24, WL 230 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008022600141 20080226 00141 SO 2008 2 26 FDKA200802068 1 20080217 A 5420 14576631621 STIFFENER EMB 145 EMB145LR 3260212 SO LT COWLING DAMAGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 LEFT LOWER ENGINE COWLING HAS FRETTING DAMAGE TO THE AFT STIFFENER. THE DAMAGED STIFFENER HAS BEEN REMOVED AND REPLACED . 2 L 7 2 4T RT T00011AT 2008022600169 20080226 00169 NM 2008 2 26 ASAA0842563 1 20080115 A 5347 654681513 SEAT TRACK BOEING 737 7374S3 1384711 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 SEAT TRACK AT STA 661 LBL 25 GOUGED SEAT TRACK AT STA 661 LBL 25. REPAIRED IAW B737 400 SRM 53 00 52 REPAIR 6. 2 L 7 2 4F RT A16WE 2008022600172 20080226 00172 WP 2008 2 26 08FDEA00450 1 20080215 A 5320 AFA01545 WEB DOUG MD10 MD1010F 3022112 WP BS 1781 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 CENTER CARGO COMP AT STA 1781 BELOW THE FLOOR AREA FROM L 52 - L 44 L WEB P/N AFA0154-5 1S CRACKED. FABRICATED NEW WEB PER REF. DAC DWG AFA 0154 REV. AT. INSTALLED IAW MD/DC 10 SRM 51-33-01 VOL. II. PART MARKED PER GMM7-0-1000. MINOR R EPAIR. 2 L 7 3 4F RT A22WE 2008022600177 20080226 00177 NM 2008 2 26 ASAA0842572 1 20080105 A 5347 655384410 CARGO TRACK BOEING 737 7374S3 1384711 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT RT TIE DOWN TRACK AT BS 767 TO 827 RBL 13 FOUND CORRODED. TIE DOWN TRACK REPLACED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008022600182 20080226 00182 NM 2008 2 26 ASAA0842582 1 20080115 A 5347 65C314838 SEAT TRACK BOEING 737 7374S3 1384711 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 SEAT TRACK GOUGED AT STA 727 B+4 LBL 45. SEAT TRACK REPAIR WITH NEW PART. 2 L 7 2 4F RT A16WE 2008022600185 20080226 00185 NM 2008 2 26 ASAA0842591 1 20080124 A 5320 694147327 INTERCOSTAL BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO LBL 21 INTERCOSTAL CRACKED AT BS 500A TO 500B. CASCADE RESPONSIBILITY INTERCOSTAL REPLACED. 2 L 7 2 4F RT A16WE 2008022600186 20080226 00186 NM 2008 2 26 ASAA0842592 1 20080124 A 5320 694147335 INTERCOSTAL BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO LBL 21 FLOOR INTERCOSTAL CRACKED BS 500 L TO 500 D. CASCADE RESPONSIBILITY INTERCOSTAL REPLACED. 2 L 7 2 4F RT A16WE 2008022600202 20080226 00202 2008 2 26 ASAA0852641 4 20080222 A 2310 5145164 AUDIO PANEL BOEING 737 737890 1384527 NM COCKPIT FAULTY A ASAA K NONE O OTHER NR NOT REPORTED 1 NM 02 579AS 35187 FIRST OFFICER'S HF 2 MIC SELECTOR. REPLACED F/O'S AUDIO CONTROL PANEL PER AMM 23 51 02. 2 L 7 2 4F RT A16WE 2008022600205 20080226 00205 NM 2008 2 26 ASAA0842649 1 20080117 A 5311 90526911 FRAME BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 BS 727G FUSELAGE FRAME CRACKED AT FASTENER HOLD BETWEEN STR 13L 14L. CRACKED FRAME REPAIRED. 2 L 7 2 4F RT A16WE 2008022600208 20080226 00208 NM 2008 2 26 ASAA0842650 1 20080105 A 5320 6546952503 CHANNEL BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT FLOOR CHANNEL FOUND CORRODED AT BS 727 F + 8 RBL 3. AFT CARGO PIT FLOOR CHANNEL AT BS 727+8 RBL 3 REPAIRE D IAW ASA EA 5310 02764. 2 L 7 2 4F RT A16WE 2008022600210 20080226 00210 NM 2008 2 26 ASAA0842653 1 20080117 A 5320 654581229 SUPPORT ANGLE BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 E & E COMP CORROSION FOUND ON FRAME SUPPORT ANGLE BS 328 AT STR 28R. E & E COMP FRAME SUPPORT ANGLE REPLACED WITH MADE REPAIR PART IAW B737 400 SRM 53 10 07 FIG 1. 2 L 7 2 4F RT A16WE 2008022600231 20080226 00231 EA 2008 2 26 A6WA200840060 1 20080201 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE WING STUCK A A6WA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 31 441ZW 7777 INFLIGHT, FLAPS STUCK AT 42 DEGREES WHEN SELECTED 45 DEGREES. AFTER 10 MINUTES, FLAPS WENT TO 45 DEGREES, NO FAULT MESS AGES ILLUMINATED. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022600236 20080226 00236 WP 2008 2 26 AMTA200800026 1 20080119 A 5210 BOTTLE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL L1 DOOR BLOWN A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 705TZ 46915 L1 DOOR EMERGENCY BOTTLE BLOWN. RESERVICED L1 DOOR EMERGENCY BOTTLE IAW MM 52-11-07, OK FOR SERVICE. (K) 2 L 7 3 4F 4 F A22WE A23EA 2008022600241 20080226 00241 WP 2008 2 26 AMTA200800031 1 20080123 A 3350 516574 CHARGER LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 162AT 1220 EMERGENCY POWERPACK AT R2 DOOR, INOPERATIVE. REPLACED EMERGENCY POWERPACK WITH SERVICEABLE UNIT. OPS CHECKS GOOD REF A MM 33-51-03. (K) 2 L 7 3 4F 4 F A23WE E12EU 2008022600267 20080226 00267 EA 2008 2 26 A6WA200840063 1 20080210 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE WING FAILED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 GL 31 438AW 7748 FLAPS FAILED AT ZERO IN FLIGHT. RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4. FLAP SYSTEM RESET OK. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022600282 20080226 00282 2008 2 26 AMTA200800060 4 20080205 A 2565 BATTERY PACK DOUG DC10 DC1030 3023501 WP EVAC SLIDE DISCHARGED A AMTA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 11 706TZ 46582 L2 DOOR ESCAPE SLIDE LIGHT NOT TESTING. REPLACED LOW PRESSURE INDICATOR, BATTERY PACK, JACK ASSY, INDICATOR OPS CKS, NOR MAL IAW AMM 25-61-03. (K) 2 L 7 3 4F A22WE 2008022600283 20080226 00283 2008 2 26 AMTA200800061 4 20080206 A 2565 BATTERY DOUG DC10 DC1030 3023501 WP EVAC SLIDE DISCHARGED A AMTA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 11 705TZ 46915 R2 DOOR ESCAPE SLIDE LIGHT DOES NOT TEST. REPLACED BATTERYS IN LOW PRESSURE INDICATOR SYSTEM, OPS CKS NORMAL. (K) 2 L 7 3 4F A22WE 2008022700015 20080227 00015 2008 2 27 WRLA2008026 4 20080213 A 2565 AWD9830507 VENTURI DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE EVAC SLIDE OBSTRUCTED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 48632 DURING C-CHECK INSPECTION L1 SLIDE FAILED TO DEPLOY TEST PER WOA J/C WA1095, SLIDE FAILED TO FULLY INFLATE DUE TO PLASTI C COVERING AIRCRAFT OBSTRUCTED VENTURI. REPLACED SLIDE/RAFT IAW WOA CARD NBR 0048. 2 L 7 3 4F 4 F RT A22WE E24NE 2008022700028 20080227 00028 WP 2008 2 27 IXXA08SMN019S 1 20080119 A 5330 SKIN DOUG DC8 DC862F 3021972 WP ZONE 100 WORN B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND OUTER FUSELAGE WORN AT STATION FS 443.000 L21L. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTENT REPAIR. REMOVED DAMAGE AREA. PERFORMED NDT INSPECTION. NO CRACK NO CORROSION DETEC TED AFTER INSPECTION. FABRICATED REPAIR DOUBLERS, REPAIR TRIPLERS, FILLERS, AND FINGER DOUBLERS. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-9 DATED 02-01-08, MANUFACTURE R MESSAGES 1-760836333-2 DATED 02-01-08 AND 1-752082423-7 DATED 01-22-08, AD-2006-03-04, SB 53-079 REVISION 2, DRAWING S R08530027, ROD SKETCH 200801150024, DRAWING ED-4684-1, SRM 51-1-20D, NDT SPM PART 06-10-01-001. 2 L 7 4 4F 4A25 2008022700066 20080227 00066 NM 2008 2 27 UIEA200800025 1 20080202 A 5753 65B019709 SKIN BOEING 747 747243B 1384830 NM TE FLAP CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 LT WING O/B FLAP, AFT FLAP UPPER SKIN ON PANEL, AN AREA OF 5.0 INCH BY 2.0 INCH IS CORRODED AT WBL 625 LT. PERMANENT RE PAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 5, SHEETS 7 AND 9, PREPREG LAYUP 250 DEGREES F CURE PER SRM 51-40-12 . REF: ATLAS AIR EO 4757A416. 2 L 7 4 4F RT A20WE 2008022700102 20080227 00102 NM 2008 2 27 SWAA080905 1 20080218 A 3350 20121 CHARGER BOEING 737 7373G7 1384595 NM CABIN FAULTY A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 683SW 24008 EMERGENCY EXIT LIGHTS C/B OPENED INFLIGHT, C/B WOULD RESET. REMOVED AND REPLACED FWD CABIN BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2008022700105 20080227 00105 NM 2008 2 27 SWAA080924 1 20080219 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022700109 20080227 00109 NM 2008 2 27 SWAA080934 1 20080219 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 13L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008022700113 20080227 00113 NM 2008 2 27 SWAA080948 1 20080219 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700115 20080227 00115 NM 2008 2 27 SWAA080947 1 20080219 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700121 20080227 00121 NM 2008 2 27 ASAA0842628 1 20080114 A 5320 65617777 CHANNEL BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 STRINGER SPLICE CHANNEL CRACKED AT STR 15L AND BS 360. REPAIRED IAW ASA RA 5310 02 758. 2 L 7 2 4F RT A16WE 2008022700126 20080227 00126 NM 2008 2 27 ASAA0842596 1 20080124 A 5320 694147328 INTERCOSTAL BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO RBL 21 FLOOR INTERCOSTAL CRACKED BS 500 C TO 500 D. CASCADE RESPONSIBILITY INTERCOSTAL REPLACED. 2 L 7 2 4F RT A16WE 2008022700129 20080227 00129 NM 2008 2 27 JJBA200871007 1 20080126 A 7921 28E997 OIL COOLER DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 1 ENGINE LEAKING A JJBA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 01 375PH 18768 2405 529 PCEAG0110 FLT 8713 CLE-AVP PIC REPORTED, HAD MASTER CAUTION WARNING FOR LOW OIL PRESSURE NR 1 ENGINE. SHUT DOWN NR 1 ENGINE, LAN DED IN PIT. SENT MAINTENANCE CREW TO PIT FOUND NR 1 OIL COOLER LEAKING. REPLACED NR 1 OIL COOLER, RESERVICED NR 1 ENGI NE AND OTHER CHECKS FOR ENGINE SHUT DOWN IAW PWC MAINTENANCE MANUAL. NO OTHER DEFECTS NOTED. 2 H 7 2 4T 4 T RT A13NM E20NE 2008022700136 20080227 00136 NM 2008 2 27 UIEA200800033 1 20080209 A 5330 SKIN BOEING 747 74747UF 1384812 NM BS 1790 S38-39L SCRATCHED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 415MC 32837 SCRATCH ON FUSELAGE SKIN AT STATION 1790 BETWEEN STRINGER 38L-39L. INSPECTED AS PER SRM 51-10-02. REPAIRED AS PER SRM 53-00-01 REPAIR 1 FIGURE 201. 2 L 7 4 4F RT A20WE 2008022700143 20080227 00143 NM 2008 2 27 UIEA200800030 1 20080212 A 5415 LUG BOEING 747 74747UF 1384812 NM NR 1 PYLON CHAFED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 415MC 32837 DURING SCHEDULED MAINTENANCE FOUND NR 1 PYLON WEAR DAMAGE ON THE LUG FACE OF THE UNDERWING MIDSPAR FITTINGS. THE DAMAGE WAS REMOVED FROM THE LUG SURFACES BY BLENDING SMOOTH. THE FITTINGS WERE CONFIRMED FREE OF CRACKS AND OTHER DAMAGE BY D ETAIL VISUAL AND NDT INSPECTION. AS PER BOEING MESSAGE 1-760110158-5 AND FAA 8100-9. 2 L 7 4 4F RT A20WE 2008022700145 20080227 00145 NM 2008 2 27 UIEA200800044 1 20080215 A 5754 RIB BOEING 747 7472D7B 1384803 NM NR 11 K FLAP CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 NR 11 KRUGER FLAP INNER FACE UPPER BACKUP STIFFENER I/B END CRACKED. REPAIRED PER BOEING MESSAGE NR 1-748489952-4. 2 L 7 4 4F RT A20WE 2008022700155 20080227 00155 WP 2008 2 27 IXXA08SMN007S 1 20080114 A 5753 SKIN DOUG DC8 DC862F 3021972 WP TE FLAP DELAMINATED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING JOINT FLAP DELAMINATED. REMOVED FASTENERS AS NEEDED TO PERFORM REPA IR. REMOVED DAMAGE AREA. FABRICATED NEW SKIN. REMOVED CORE AND CLEANED AREA. INSTALLED CORE AND NEW FASTENERS AND RE PAIRED PARTS IAW DC8 SRM 57-7-1 PAGE 2, SRM 51-1-9 T/R 51-142, AND DC8 SRM 51-1-9 PAGE 1. 2 L 7 4 4F 4A25 2008022700167 20080227 00167 NM 2008 2 27 08FDEA00534 1 20080220 A 5730 1060031117 PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 WING FUEL PANEL 642DB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 642DB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-117. 2 L 7 2 4F RT A2NM 2008022700170 20080227 00170 NM 2008 2 27 08FDEA00535 1 20080220 A 5730 1060031117 PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 WING FUEL PANEL 642CB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 642CB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-117. 2 L 7 2 4F RT A2NM 2008022700171 20080227 00171 NM 2008 2 27 200802131 1 20080209 A 2797 17106275401 WIRE HARNESS EMB ERJ170 ERJ170100SE 3260406 NM SLAT/FLAP SYS FAULTY A UHLA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 634RW 17000055 FLIGHT 7722 ORD TO IND DURING APPROACH CREW SELECTED 5 FLAPS AND RECEIVED A "SLAT FAIL" CAUTION AND ASSOC AMBER BOX ON S LAT/FLAP INDICATION. CREW DECLARED AN EMERGENCY AND THEN LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LT OUTBOARD SKEW SENSOR HARNESS. 2 L 7 2 4F RT A56NM 2008022700173 20080227 00173 EU 2008 2 27 08FDEA00544 1 20080221 A 2197 WIRE AIRBUS 310 A310324 3930206 EU DAMAGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 808FD 439 AFTER START GOT OVERBOARD VALVE FAULT COMPLIED WITH ECAM QRH AND CHECKED MEL. DURING CLIMB-OUT, AIRCRAFT WOULD NOT PRES SURIZE. REMOVED AVIONICS EXTRACT VALVE TO FOM AV LINE C/B'S 60HR, 61HR PULLED AND COLLARED. FOUND WIRE BUNDLE CUT, FOR AV EXTRACT VALVE. PERFORMED WIRE SPLICE REPAIRS IN ZONE 133 STA 1715 TO WIRES 2123-5000-24, 5001-22, 5002-24, 5003-24, 5004-24, 5005-22, 5006-20, AND 5023-20 PER AIRBUS ELECTRICAL STD PRACTICES MANUAL, REINSTALLED VALVE, 2 GOOD LEGS. EXT RACT VLV PLACED ON MEL-GSO/23 , VALVE REMOVED AND REPLACED RSW/23. AFTER RECHECKING PREV SPLICE REPAIRS. 2 L 7 2 4F RT A35EU 2008022700179 20080227 00179 NM 2008 2 27 ZZDA2008069 1 20080210 A 5311 FRAME BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 950AT 55012 SMALL CRACK AFT FUSELAGE INTERNAL LT CANTED FRAME STA 1200.019. INSTALLED REPAIR 15" X 2" AS REQ 51-70-11 MATERIAL USED 7075.0 .063 HEAT TREATMENT TO 7075 T6 .063 AS PER SRM 51-32.01. 2 L 7 2 4F TR A6WE 2008022700181 20080227 00181 NM 2008 2 27 08FDEA00588 1 20080223 A 5315 BAC1518338 FLOORBEAM BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 MAIN DECK FLOORBEAM, UPPER FLANGE IS CORRODED, BS 1070, LBL 47-60, WL 208. REMOVED CORROSION ON MAIN DECK FLOORBEAM UPP ER FLANGE, STA 1070, LBL 47"-60". FOUND TO BE OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR, REF SRM 53-10-08 FIG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008022700182 20080227 00182 EA 2008 2 27 TRAX200800234 1 20080201 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 680BR 7679 AAR - CRACK ON PAX DOOR LOWER FWD CORNER UNDER HINGE STEP. 2 L 7 2 4F RT A21EA 2008022700184 20080227 00184 EU 2008 2 27 08FDEA00551 1 20080123 A 5743 A2757038000400 TRUNNION AIRBUS 310 A310222 3930315 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 RT WING NR 4 TRUNNION OF OUTBD FLAP WITH WEAR. TRUNNION NR 4 RT WAS REMOVED, REPAIRED PER CMM 57-53-12 AND INSTALLED PE R AMM 27-54-37. 2 L 7 2 4F RT A35EU 2008022700186 20080227 00186 NM 2008 2 27 08FDEA00590 1 20080225 A 5320 146N5300U79 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 CORROSION FOUND ON FLOORBOARD U-CHANNEL FROM STA 1700 TO STA 1718, BL 0. SUPPORT REPLACED IAW SRM 51-10-02 REV.93 AS PE R EAR P337-24137-C0013. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 2 4F RT A2NM 2008022700189 20080227 00189 NM 2008 2 27 08FDEA00592 1 20080225 A 5320 146N5281U6 INTERCOSTAL BOEING 757 75727B 1384921 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 FOUND CORROSION ON INTERCOSTAL FROM STA 1300 TO STA 1320, RBL 21. REPLACED IAW SRM 51-10-02 REV.93 PER EAR P337-24137-C 0045. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 2 4F RT A2NM 2008022700190 20080227 00190 EA 2008 2 27 TRAX200800237 1 20080208 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 748EV 10158 RIGHT AFT MOST EXTERNAL EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008022700195 20080227 00195 WP 2008 2 27 08FDEA00598 1 20080225 A 5347 601096418 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 363FE 48263 SEAT TRACK LUG IS CHIPPED AT F/S 635 TRACK RBL 8. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1. REPAIR PARTS FABRICATED ON TRAVELERS T8/725394 AND T8/725350. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008022700196 20080227 00196 WP 2008 2 27 08FDEA00599 1 20080225 A 5347 601096418 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 363FE 48263 SEAT TRACK LUG WORN AT FS 750 TRACK LBL 28. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1. REPAIR PART FABRICATED ON TRAV ELER, T8/725094. 2 L 7 3 4F RT A22WE 2008022700199 20080227 00199 WP 2008 2 27 NWAA080569941 1 20080218 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING LINE CHECK, MAINTENANCE FOUND THE OVERWING EMERGENCY EXIT SIGN LIGHTS ON THE LEFT SIDE WERE INOPERATIVE. THE EME RGENCY PATH LIGHTING AT ROWS 5, 6, AND 7 WERE ALSO NOT FUNCTIONING. MAINTENANCE REPLACED THE OVERWING EXIT SIGN BATTERY PACK AND OPERATIONALLY CHECKED THE SYSTEM. ALL CHECKS WERE GOOD AND THE AIRCRAFT RETURNED TO REVENUE SERVICE. 2 L 7 2 4F A6WE 2008022700212 20080227 00212 NM 2008 2 27 DHL2008749001 1 20080110 A 5313 STRINGER BOEING 727 7272J0 138407E NM BS 680 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 FORWARD CARGO COMPARTMENT CORROSION ON STRINGER SPLICE, STRINGER 28R BETWEEN BS 680 FRAME. FOUND CORROSION OUT OF LIMIT S IAW B-727 SRM 53-10-1 FIGURE 1 ON UPPER FLANGE ON SPLICE. REMOVED SPLICE IAW B-727 SRM 51-30-2. FABRICATED NEW SPLIC E USING BAC 1498-132 7075-T6 PO NR 7308420 DIMENSION 13" IAW B-727 SRM 51-20-1, 51-30-5 AND 53-10-2 FIGURE 9. ALODINED AND PRIMED AREA IAW B-727 SRM 51-10-2. INSTALLED SPLICE IAW B-727 SRM 53-10-3 FIGURE 1. 2 L 7 3 4F RT A3WE 2008022700213 20080227 00213 NM 2008 2 27 KCSA081077 1 20080213 A 5210 DOOR FRAME BOEING 747 747209B 138489B NM L3 DOOR CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 L-3 DOOR HAS CORROSION ON VERTICAL CHORD FWD CORNER INSIDE DOOR 4 INCHES FROM BOTTOM. 2 L 7 4 4F RT A20WE 2008022600079 20080226 00079 NM 2008 2 26 DLM90080240 1 20080219 A 5311 5930584124 FRAME DOUG MD90 MD9030 3023690 NM BS 1019 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 RIGHT MLG BAY FORWARD FRAME CRACKED APPROXIMATELY FS 1019 RBL 56.5. REMOVED AND REPLACED RIGHT MLG BAY FORWARD FRAME, I AW MD90 SRM 51-30-02, 51-30-05 AND 51-10-03. 2 L 7 2 4F RT A6WE 2008031900365 20080319 00365 NE 2008 3 19 DXTA200802821 2 20080203 A 7321 30J265802 FUEL CONTROL CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE NR 1 ENGINE MALFUNCTIONED E DXTA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 647QS 3012 5605547 PCEDD0101 DURING TAKEOFF ROLL THE NR 1 ENG DID NOT DEVELOPE T/O POWER. TARGET N1 WAS 88.6 PERCENT BUT ONLY DEVELOPED 81 PERCENT N1 . DOWNLOADED NR1 ENG. DCU AND SENT INFO TO MFG, SWAPPED EEC'S AND RAN FOR PWR OF DAY. DOWNLOADED DCU NR SENT TO MFG. P ERFORMED OPS CHECK OF LT AND RT RVDT. OPS CHECK NORMAL. REMOVED AND REPLACED NR1 ENG FUEL CONTROL. RIGGED AND LEAK CHECK ED. RAN NR1 ENG PWR OF THE DAY WAS NOT MET. DOWNLOADED DCU AND SENT TO MFG PERFORMED WIRING CHECKS ON CONNECTORS P1,P3, J1 AND PT009. WIRING CHECKS GOOD AT THIS TIME. RAN NR1 ENG FOR PWR OF DAY. PWR OF THE DAY WAS ACHIEVED. NR1 ENG PWR OF D AY OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008031900368 20080319 00368 NM 2008 3 19 CALS097007 1 20080226 A 2497 FEEDER CABLE BOEING 747 747409 13848AU NM APU GEN CHAFED W SAJF K NONE O OTHER IN INSP/MAINT 1 WP 03 18203 28711 APU GENERATOR FEEDER CABLES AND CLAMP STANDOFF FOR CHAFING AGAINST THE WASTE TANK DUCT, AND FOUND THAT B-18203 LT BULK C ARGO COMPARTMENT STA 2060 APU GENERATOR FEEDER CABLE CLAMP STANDOFF RIVET SHEARED. 2 L 7 4 4F RT A20WE 2008031900373 20080319 00373 CE 2008 3 19 DXTA200802826 1 20080203 A 2720 EM407011 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL RUDDER INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 903QS 1766 1766 7500162 RUDDER LIMIT FAIL B 89 PERCENT. REPLACED LOWER LIMIT (B) ACTUATOR IAW CH 27-23-00. OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008031900377 20080319 00377 EA 2008 3 19 TRAX200800414 1 20080312 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT LACK OF LUBE A ASOA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 857AS 7411 RIGHT OVERWING EMERGENCY EXIT FAIL THE PULL TEST ON EXIT HANDLE. LUBRICATED & RETESTED, NO DEFECTS NOTED AT THIS TIME IAW MM 112-20-52 & 52-21-00. 2 L 7 2 4F RT A21EA 2008031900380 20080319 00380 NM 2008 3 19 KCSA081175 1 20080315 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 EXTERNAL FUSELAGE HAS CORROSION ON SKIN JUST BENEATH LAP SEAM AT STA 1060 TO 1080, STR 4R. 2 L 7 4 4F RT A20WE 2008031900382 20080319 00382 NM 2008 3 19 KCSA081177 1 20080315 A 5311 STRAP BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 AFT BILGE FUSELAGE FRAME STABILIZATION STRAP IS CRACKED AT STA 2160, LBL 28. 2 L 7 4 4F RT A20WE 2008031900387 20080319 00387 NM 2008 3 19 KCSA081180 1 20080317 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE SKIN IS CORRODED AT STA 1239, STR 11L. 2 L 7 4 4F RT A20WE 2008031900389 20080319 00389 NM 2008 3 19 CALA0800220 1 20080317 A 5320 143N5366126 ANGLE BOEING 757 75733N 1384931 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 57868 32590 WHILE PERFORMING WC 53-5330-1-2801, FOUND CORROSION AT FWD CARGO DOOR SILL PLATE AREA AT LOWER AFT END 18 INCH LENGTH AR EA, AND FWD END AT NUT PLATE HOLES FOR SILL PLATE ATTACH POINTS. REMOVED AND REPLACED FWD CARGO ENTRANCE Z-ANGLE AS PER SRM 51-4-0-02. 2 L 7 2 4F RT A2NM 2008031900390 20080319 00390 NM 2008 3 19 CALA0800221 1 20080316 A 5230 6547952162 SKIN BOEING 737 7373T0 1384582 NM AFT CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 C2 AFT CARGO DOOR, DENT FOUND ON OUTER SKIN, CUT OUT DAMAGE APPROX 2 INCH SQ AT 22 INCH FROM TOP, 31 INCH FROM FWD. INC ORPORATED PREVIOUS REPAIR TO FORM ON DOUBLER PER SRM 52-00-01 FIG 201 REPAIR 3. DIP ISSUED TO INSPECT REPAIR PER SRM 52 -00-01 REPAIR 3 WITHIN EVERY 4000 FLIGHT CYCLES. 2 L 7 2 4F RT A16WE 2008031900401 20080319 00401 NM 2008 3 19 CALA0800228 1 20080317 A 5313 BAC1498150 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 STRINGER 4-L DAMAGED AT STA 380. REMOVED DAMAGED SECTION OF STRINGER FROM A/C AND SPLICED IN NEW. REF SRM 53-00-03 REP AIR 3. 2 L 7 2 4F RT A16WE 2008031900403 20080319 00403 NM 2008 3 19 CALA0800230 1 20080317 A 5315 141T5108 FLOORBEAM BOEING 767 767424ER 1385270 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 67052 29447 CABIN - BS 325 RBL 3" - LBL 56" FLOOR SUPPORT FOUND CORRODED AFTER FLOOR PANEL REMOVED. CABIN BS 325 RB 10" TO LBL 45" F LOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND HFEC NO CRACK FOUND AND LBL 45" TO LBL 56" CORROS ION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01. DEPTH 0.007" WITHIN SRM 53-00-51 ALLOWABLE DAMAGE 1 LIMIT. 2 L 7 2 4F RT A1NM 2008031900404 20080319 00404 NM 2008 3 19 CALA0800231 1 20080317 A 5330 6545800 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 R-1 DOOR CUTOUT LWR AFT CORNER CRACKED APPROX 1.5 INCH LONG. INSTALLED REPAIR REF SRM 53-10-01 REPAIR 2. 2 L 7 2 4F RT A16WE 2008032000019 20080320 00019 CE 2008 3 20 DXTA200802834 1 20080201 A 2133 3212921 OUTFLOW VALVE RAYTHN 900 HAWKER900XP 4220011 CE GARRTT TFE731 TFE7315R 01518 WP AFT SERVICE BAY INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 848QS 32 HA0031 AFTER T/O LT MAIN AIR VALVE LIGHT CAME ON AND CHECKLIST CALLS TO RECYCLE CLOSED/OPEN. LIGHT CAME BACK ON. REPLACED LT MA IN AIR VALVE WITH O/H UNIT. OPS AND LEAK CHECKED GOOD IAW MM 21-16-25. 1 L 7 2 4F 4 F RT A3EU E6WE 2008032000020 20080320 00020 CE 2008 3 20 DXTA200802835 1 20080204 A 7933 45AS86825009 INDICATOR BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LT OIL TEMP INOPERATIVE E DXTA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 GL 07 131QS 1531 RK431 ON TAKEOFF LT OIL TEMP WENT TO 0, ABORTED TAKEOFF. SWAPPED GAUGES FROM RT TO LT, STARTED ENGINES, DID FIND OIL TEMP NEE DLE DID NOT RISE TAPPED ON GAUGE AND IT CAME UP. SWAPPED GAUGES TO THE ORIGINAL POSITION, RAN ENGINES AGAIN PROBLEM STIL L FOLLOWED. REPLACED LT OIL TEMP PRESSURE GAUGE WITH AN OVERHAULED UNIT IAW MM CHAP 31-10-00. 2 H 7 2 4F 4 F RT A16SW E25EA 2008032000026 20080320 00026 CE 2008 3 20 DXTA200802836 1 20080204 A 2910 AE366323E0117 LINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE HYDRAULIC SYS WORN E DXTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 394QS 9902 5600394 ON FO SIDE, RT BRAKE FEELS SLUGGISH COMPARED TO THE LT BRAKE. REMOVED AND REPLACED CO-PILOTS LT AND RT BRAKE MASTER CYLI NDER PRESSURE AND RETURN LINES (4EA) AND BLED HYD SYS ALL WORK PERFORMED IAW MM, CH 32-42-02 AND 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2008022600097 20080226 00097 NM 2008 2 26 2008UALA00754 1 20080209 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 22R INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY LIGHT LAMP INOP, SEAT 22R. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2008022600107 20080226 00107 NM 2008 2 26 2008UALA00759 1 20080211 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY LIGHT INOP:LT OVERWING 2ND AFT ASSY, AFT LAMP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008022600114 20080226 00114 NM 2008 2 26 ASAA0842583 1 20080115 A 5347 654681349 SEAT TRACK BOEING 737 7374S3 1384711 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 SEAT TRACK GOUGED AT STA 520 LBL 25. REPAIRED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008022600119 20080226 00119 NM 2008 2 26 ASAA0842588 1 20080124 A 5320 694147327 INTERCOSTAL BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO LBL 21 FLOOR INTERCOSTAL CRACKED AT BS 500E TO 500F. CASCADE RESPONSIBILITY INTERCOSTAL REPLACED. 2 L 7 2 4F RT A16WE 2008022600143 20080226 00143 SO 2008 2 26 FDKA200802069 1 20080218 A 5270 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO CARGO DOOR MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 856MJ 145626 FDM 6046 CVG (1404 PHX LCL). BAGGAGE DOOR WARNING WITH DOOR VERIFIED CLOSED AND LOCKED. MX OPS CHECKED AND NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008022600146 20080226 00146 EU 2008 2 26 USAA920080438 1 20080214 A 5315 D53472172204 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3158 / FR 66 - BS 3207 / FR 67 , +Y1292. REPLACED CABI N FLOORBEAM, BS 3158 / FR 66 - BS 3207 / FR 67 , +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022600150 20080226 00150 EU 2008 2 26 USAA920080456 1 20080215 A 5347 D53472190211 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SEAT RAIL BEAM, BS 3043 / FR 64 - BS 3101 / FR 66 , -Y1292. REPLACED CABIN SEAT RAIL BEAM, BS 3043 / FR 64 - BS 3101 / FR 66 , -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022600153 20080226 00153 EU 2008 2 26 USAA920080459 1 20080214 A 5315 D53472189204 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3257 / FR 68, -Y1162.5. REPLACED CABIN FLOORBEAM, BS 3 207 / FR 67 - BS 3310 / FR 69 , -Y1162.5 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008022600161 20080226 00161 SO 2008 2 26 FDKA200802070 1 20080219 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO CARGO BAY MALFUNCTIONED A FDKA K NONE L NO TEST NR NOT REPORTED 1 SW 07 849MJ 145534 FDM 6150 TYS (0350 PHX LCL). BAG SMOKE DETECTOR WILL NOT TEST. MX RESET, NO FURTHER ACTION REQUIRED. 2 L 7 2 4T RT T00011AT 2008022600192 20080226 00192 NM 2008 2 26 ASAA0842622 1 20080105 A 5347 65538449 CARGO TRACK BOEING 737 7374S3 1384711 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT LT TIE DOWN TRACK AT BS 947 LBL 17 FOUND CORRODED. REPAIRED WITH MADE REPAIR PART. 2 L 7 2 4F RT A16WE 2008022600225 20080226 00225 EU 2008 2 26 08FDEA00434 1 20080214 A 5321 B5327027300000 FLOOR PANEL AIRBUS 300 A300B4605R 3930308 EU MAIN CARGO BAY TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 MAIN DECK CARGO COMPARTMENT FLOOR PANEL 252 GF IS TORN. FABRICATED NEW PANEL 252 GF IAW FEDEX SRZ 25-005 REV F. 2 L 7 2 4F RT A35EU 2008022600237 20080226 00237 2008 2 26 AMTA200800027 4 20080118 A 2310 9641453011 COUPLER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE HF COMM DEFECTIVE A AMTA K NONE O OTHER CR CRUISE 1 GL 11 520AT 27976 LT HF WILL NOT TRANSMITT AT ALL STATIONS. REMOVED AND REPLACED HF COUPLER LT SIDE. RADIO CHECK, OPS GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008022600238 20080226 00238 NM 2008 2 26 AMTA200800028 1 20080118 A 3350 BATTERY PACK BOEING 737 73783N 13844HI NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 314TZ 30640 RT AFT SERVICE DOOR INT AND EXT EMERGENCY LIGHTS FAIL TO ILLUM. CHARGE THE BATTERY PACKS IAW AMM 24-22-00-860-811, EMER GENCY LIGHTS . OPS CK OK IAW AMM 33-51-00-720-801. (K) 2 L 7 2 4F RT A16WE 2008022600239 20080226 00239 2008 2 26 AMTA200800029 4 20080120 A 3442 RADAR BOEING 737 73783N 13844HI NM WEATHER RADAR MALFUNCTIONED A AMTA K NONE O OTHER CR CRUISE 1 GL 11 318TZ 28247 RADAR TILT INOPERATIVE CONTOUR LINES STAY AT 7 MILES. PERFORMED WEATHER RADAR RECEIVER/TRANSMITTER BITE TEST IAW FIM 34 -43-00-81-801, NO DEFECT NOTED, OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2008022600248 20080226 00248 NM 2008 2 26 AMTA200800037 1 20080128 A 4930 RELAY BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE APU DEFECTIVE A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 518AT 27974 APU FAULT LIGHT ILLUMINATED AND EICAS, APU VAV MESSAGE DISPLAYED. COULD NOT DUPLICATE FAULT, FOR COMPANY CONVENIENCE. REMOVED AND REPLACED APU SHUTOFF VALVE DISAGRE RELAY K10160, AND SHUTOFF VALVE DISAGREE ENABLE RELAY, IAW WDM 28-25-21, OPS NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008032000027 20080320 00027 CE 2008 3 20 DXTA200802837 1 20080204 A 2710 991444011 PCU CESSNA 750 750 2076810 CE PWA JT15 JT15D5 52112 NE AILERONS MALFUNCTIONED E DXTA O OTHER F FLT CONT AFFECTED LD LANDING 1 GL 07 936QS 9414 7500036 ROLL CONTROL FEELS ABNORMAL. CONTROLS ARE BINDING, THEN RELEASING. ESPECIALLY NOTICEABLE DURING SLOW FLIGHT. REMOVED A ND REPLACED LT AND RT AILERON PCU'S IAW MM 27-11-05. OPS AND RIGGING CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI E25EA 2008032000031 20080320 00031 CE 2008 3 20 DXTA200802841 1 20080205 A 2150 73838433 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AFT SERVICE BAY LEAKING E DXTA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 982QS 1422 1422 7500182 SMOKE IN COCKPIT, SMELLED AND SEEN AS A LIGHT MIST, IMMEDIATELY AFTER TAKE OFF. RETURNED (M-2B) T/S AND REMOVED AND R EPLACED COCKPIT ACM WITH A NEW UNIT. PERFORMED OPERATIONAL AND LEAK CHECKS. IAW MM 21-51-00. REMOVED AND REPLACED CAB IN AND COCKPIT WATER SOCKS. NO DEFECTS NOTED AT THIS TIME.OLD P/N 738-384-33.OLD S/N 200-301-014. NEW P/N 738-384-33. NEW S/N200-7101-360. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008031900009 20080319 00009 EA 2008 3 19 SWIA200819327 1 20080307 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 411SW 7067 FLT 3774 - LEFT WINDSHIELD SHATTERED INFLIGHT. REPLACED LEFT WINDSHIELD IAW AMM 56-11-01. OPS CHECK GOOD, P/N OFF: NP- 139321-9, S/N OFF: 01200H3576. 2 L 7 2 4F RT A21EA 2008031900025 20080319 00025 SO 2008 3 19 GUUA02260801 1 20080226 A 3350 AGC1 FUSE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHTS BLOWN A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 285AS 120265 FLIGHT: 9265, PILOT REPORTED AFT LT AND RT EXTERIOR EMERGENCY LIGHTS ARE NOT WORKING. REPLACED EMERGENCY LIGHT FUSE. 2 L 7 2 4T 4 T RT A31SO E20NE 2008031900031 20080319 00031 WP 2008 3 19 ABXR080085 1 20080214 A 5531 991188112 RIB DOUG DC9 DC933F 302207A WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 208US 47220 RIB CRACKED AT FASTENERS LEFT AND RIGHT SIDES OF VERT STAB LEADING EDGE ZFS 50. REPAIRED IAW DC9 SSRM DWG K05159. 2 L 7 2 4F A6WE 2008031900098 20080319 00098 NM 2008 3 19 SB08011 1 20080309 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 439US 24781 MAINTENANCE REPORTED THE OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 3, 9, 11, 14, 18, 20, 22 AND 24 ALONG WITH THE SEAT MOUN TED EMERGENCY AISLE LIGHTS AT SEAT ROWS 3, 4, 5, 10, 13 THRU 19, 24 AND 25 INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE BATTERY PACKS. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008031900128 20080319 00128 CE 2008 3 19 20061068 1 20080211 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 213-228 CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 257GL UE257 BELLY SKIN REPAIR DUE TO CORROSION REPAIR. SKIN REPAIR AREA APPROX 31.5 INCHES X 23 INCHES FROM FS 213.25/228.25 AND ST RINGERS 13L TO 15R. OPEN 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900131 20080319 00131 EA 2008 3 19 N6WA0080202 1 20080214 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE CABIN INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 157GJ 10230 CABIN LEVEL CEILING EMERGENCY LIGHT INOP AT ROW 14 AND 15. DEFERRED IAW MEL 33-51-01-2A. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008031900132 20080319 00132 EA 2008 3 19 N6WA0080203 1 20080214 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE CABIN INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 153GJ 10219 5332-PWM-AFT CEILING LEVEL EMERGENCY LIGHT INOP. DEFERRED IAW MEL 33-51-01-2A 2 L 7 2 4F 4 F RT A21EA E00063EN 2008031900177 20080319 00177 EA 2008 3 19 TRAX200800376 1 20080305 A 3350 LENS CNDAIR CL600 CL6002C10 1390015 EA CABIN CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 RIGHT EMERGENCY WING LIGHT LENS CRACKED. REMOVED AND REPLACED LENS IAW CRJ 700 AMM 33-51-21. SUPPLEMENTAL SDR CLOSED 3 /11/08. 2 L 7 2 4F RT A21EA 2008031900222 20080319 00222 EU 2008 3 19 USAA920080572 1 20080224 A 5320 D5347219020200 DUMMY RAIL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651AW 866 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN DUMMY RAIL, BS 3043 /FR 64, +Y765. REPLACED CABIN DUMMY RAIL, BS 304 3 /FR 64, +Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900225 20080319 00225 NM 2008 3 19 USAA920080574 1 20080226 A 5315 D53472172202 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801AW 889 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 2835 / FR 67, +Y1292. REPLACED CABIN FLOORBEAM, BS 283 5 / FR 67, +Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900250 20080319 00250 CE 2008 3 19 DXTA200802805 1 20080128 A 3240 AE366323FE0117 HOSE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE HYD SYSTEM LEAKING E DXTA O OTHER O OTHER LD LANDING 1 GL 07 386QS 8372 5600486 F/O'S BRAKE PEDALS ARE SOFT. INSPECTED SYS AND FOUND UPPER (SUPPLY) HOSE OF CO-PILOTS RT MASTER CYLINDER BRAIDING BROKEN AND FRAYED. ALSO FOUND SWIVEL FITTING FOR BRAKES ON TOP OF LT MLG LEAKING. CLEANED AND TIGHTENED FITTING AND REPLACED FRAYED LINE. BLEED BRAKES 3 TIMES WITH .5 HOURS BREAK IN BETWEEN. ALL WORK DONE IAW MM CHAP 32-42-00. SYS OPS CHECKS AND LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2008031900256 20080319 00256 CE 2008 3 19 GLBA20061066 1 20080211 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 163 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 257GL UE257 FRAME AT FS 163.97 AND STR 9L CRACKED APPROX .40 INCH IN LENGTH. RII REQUIRED TC 8.2.1. MAINT REPAIRED FRAME CRACK AT S TRINGER RELIEF HOLE F.S. 163.97 AND STRINGER 9L IAW SRM 51-70. REPAIR APPROX 5 INCHES X 2.7 INCHES. 2024-T3 .071. RII C/ W IAW TC 8.2.1 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900273 20080319 00273 NM 2008 3 19 USAA920080607 1 20080207 A 5330 6545775 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FUSELAGE SKIN, BS 727E, S24R. REPAIRED FUSELAGE SKIN, BS 727E, S24R IAW B737 S RM 53-00-01-2R31. 2 L 7 2 4F RT A16WE 2008022600252 20080226 00252 NM 2008 2 26 AMTA200800041 1 20080128 A 5210 SEAL BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE L1 DOOR DAMAGED A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 552TZ 32586 LOUD SQUEAL AT DOOR 1L DURING FLIGHT. FOUND LEAK AT FWD AND AFT BOTTOM OF DOOR CUTOUT THRESHOLD. RESEALED PRESSURIZED AC, NO LEAKS NOTED. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008022600254 20080226 00254 2008 2 26 AMTA200800043 4 20080130 A 2310 TRANSCEIVER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE HF COMM MALFUNCTIONED A AMTA K NONE O OTHER CR CRUISE 1 GL 11 560TZ 33525 RT HF TRANSMISSION INOP AT ALL CREW STATIONS. SWAPPED HF RT`S PN 964-0452-012. LT HF SN 1427 RT HF RT SN 1412, BOTH HF `S OPS CHECK NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008022600259 20080226 00259 2008 2 26 AMTA200800051 2 20080203 A 7320 1853M56908 HMU BOEING 737 73783N 13844HI NM NR 2 ENGINE ACTIVATED A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 318TZ 19186 19186 28247 ON PUSH BACK AND START OF NR 2 ENGINE, ENGINE CONTROL LIGHT ON. REPLACED NR 2 HMU IAW MM 73-21-10-4. OPS CHECKS NORMAL . (K) 2 L 7 2 4F RT A16WE 2008022600262 20080226 00262 NM 2008 2 26 AMTA200800073 1 20080212 A 5320 FITTING BOEING 737 73783N 13844HI NM BS 727D CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 317TZ 28246 AFT CARGO COMPARTMENT (TEE) ON STA 727D, FOUND WITH SURFACE CORROSION (BOTH SIDES) INCLUDED ALL RAIL ASSY ON THIS STA AN D CHANNELS. REMOVED CORROSION FROM RBL 13.84, LBL 3.0 TO LBL 8.1 IAW SRM 53-00-53-1A2 AND FOUND OUT OF LIMITS. REPAIR A CCOMPLISHED IAW EA 737-5300-08-A0007 AND SRM 53-00-53 REPAIR 2 WITHOUT FILLER INSTALLED. ALODINE, PRIMED PAINTED IAW SR M 51-20-01. (K) 2 L 7 2 4F RT A16WE 2008022600284 20080226 00284 NM 2008 2 26 AMTA200800062 1 20080209 A 2560 BATTERY BOEING 737 73783N 13844HI NM FLASHLIGHT DISCHARGED A AMTA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 11 301TZ 28239 FLASHLIGHT AT L2 DOOR, LED DOES NOT TURN ON. REPLACED FLASHLIGHT BATTERY. OPS CHECK, OK. (K) 2 L 7 2 4F RT A16WE 2008022700005 20080227 00005 EA 2008 2 27 COMA0860105 1 20080202 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 720SW 21430 7297 FLIGHT 4957 - AFTER SELECTING GEAR UP, RECEIVED GEAR DISAGREE AND DOOR DISAGREE MESSAGES WITH MAIN GEAR UP, NOSE DOWN. REPLACED NOSE GEAR PRIORITY VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008022700006 20080227 00006 EA 2008 2 27 COMA0860106 1 20080202 A 2130 21197646 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 01 436CA 12421 7482 FLIGHT 9757 - RECEIVED CABIN ALTITUDE MESSAGE AT 24000 FT MANUAL CONTROL WOULD NOT WORK. INITIATED EMERGENCY DESCENT. LANDED WITHOUT INCIDENT. REPLACED CABIN PRESSURE SELECTOR PANEL. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008022700050 20080227 00050 EA 2008 2 27 COMA0860125 1 20080211 A 2752 854D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 721CA 2346 7259 FLIGHT 5532 - FLAPS FAIL CAUTION MESSAGE AT 0 DEGREES WHEN SELECTING 8 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED SAF ELY. REMOVED AND REPLACED RIGHT O/B FLAP O/B ACTUATOR. 2 L 7 2 4F RT A21EA 2008022700079 20080227 00079 NM 2008 2 27 SWAA080888 1 20080218 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 204WN 29855 EEPLS END CAP LOOSE AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 2008022700111 20080227 00111 NM 2008 2 27 SWAA080923 1 20080219 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022700148 20080227 00148 NM 2008 2 27 DHL2008752600 1 20080204 A 5730 SLAT BOEING 727 727223 1384074 NM ZONE 600 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 RT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/ B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL USED 2024T3 .063 PO NR 9006288 DIMENSION 7" BY 8.5" IAW SRM 57-30-4 FIG 11 AND SRM 57-30-2 FIG 3. TREATED AND PRIMED DOUBLER REPAIR AND AREA IAW SRM 51-10-2. INSTALLED NEW DOUBLER REPAIR AND REINSTALLED FASTENERS IAW SRM 51-30-2 . 2 L 7 3 4F A3WE 2008022700165 20080227 00165 NM 2008 2 27 08FDEA00583 1 20080223 A 5410 B277101801 FRAME BOEING 727 727227 1384078 NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 NR 1 ENG UPPER COWL FWD I/B END FRAME CRACKED REMOVED INB END FRAME. FABRICATED INSTALLED DOUBLER IAW SRM 51-40-2. TRE ATED PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED STRIKER PLATE IAW SRM 51-30-1. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008022700225 20080227 00225 NM 2008 2 27 DHL2008749013 1 20080204 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950 - 1010 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 AFT PIT STRINGER 29R CRACKED AT SPLICE AFT OF BS 950. REMOVED AFT PIT STRINGER 29R, LOCATED AND DRILLED NEW STRINGER 29 L P/N 65-52441-8 PO NR 7370104. INSTALLED NEW STRINGER 29L FROM BS 950 TO BS 1010 IAW B-727 SB 727-53-0179. 2 L 7 3 4F A3WE 2008022700230 20080227 00230 WP 2008 2 27 08FDEA00600 1 20080225 A 5347 601096418 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 363FE 48263 SEAT TRACK AT FS 755 LBL 8 HAS WORN LUGS. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1. REPAIR PARTS FABRICATED ON TRAVE LERS, T8/725391 AND T8/725395. 2 L 7 3 4F RT A22WE 2008022700231 20080227 00231 NE 2008 2 27 MAC020801 2 20080213 A 7200 PW124B ENGINE AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE NR 1 MALFUNCTIONED A MTNA B E A EMER. DESCENT ENGINE SHUTDOWN UNSCHED LANDING R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CR CRUISE 1 EA 68 809FX 22336 10016 217 PCE124437 THE PIC NOTICED TORQUE FLUCTUATIONS AND LOSS OF TORQUE. A VIBRATION WAS NOTICED. THE PIC SHUT DOWN THE NR 1 ENGINE IN FLIGHT, DECLARED AN EMERGENCY AND DIVERTED TO MBJ AND LANDED. THE A/C WAS DETERMINED TO BE DOWN FOR AN ENGINE CHANGE. 2 H 7 2 4T 4 T RT A53EU E2ONE 2008031900286 20080319 00286 CE 2008 3 19 GLBA20061070 1 20080219 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 177 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 184UX UE184 02/18/08, FRAME CRACKED AT STR 9R CUTOUT. CRACK APPROX .500 IN LENGTH AT FS 177.35. MAINT REPAIRED FRAME CRACK AT STR RE LIEF HOLE AT FS 177.35 AND STR 9R IAW SRM 51-70. REPAIR APPROX 5 INCH X 2.5 INCH 2024 T-3 .071. RII INSP C/W IAW TASKCAR D 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2008031900297 20080319 00297 NM 2008 3 19 USAA920080608 1 20080303 A 5230 6547952337 SKIN BOEING 737 7373G7 1384595 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 CLT - MAJOR REPAIR - C17 CHECK - AFT CARGO DOOR SKIN CRACKED AT THE DOOR HANDLE CUTOUT. REPAIRED THE AFT CARGO DOOR SKI N IAW B737 SRM 52-00-01-2R2. 2 L 7 2 4F RT A16WE 2008031900300 20080319 00300 WP 2008 3 19 ASMF200802006 1 20080224 A 3320 BV04005N0184 SOCKET DOUG DC9 DC987 3022087 WP CABIN LIGHT BURNED W ASMF K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 23 205AM 49405 DURING TRANSIT CHECK, A BURNED ODOR WAS DETECTED IN PASSENGERS CABIN. MAINTENANCE PERSONNEL CHECKED AFFECTED AREA AND A LAMP IN RAW 3 WAS DETECTED OVERHEATED. THE LAMP WAS REPLACED IAW MM 33-21-03 BUT FAILURE CONTINUED. AIRCRAFT WAS SENT TO THE HANGAR AND DURING CHECK, THE LOWER SIDE WALL LIGHT SOCKET WAS DETECTED BURNED, SO IT WAS REPLACED IAW MM 33-22-18, TESTED CORRECT. 2 L 7 2 4F RT A6WE 2008031900301 20080319 00301 NM 2008 3 19 USAA920080609 1 20080225 A 5312 6517582 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 CLT - MAJOR REPAIR - C17 CHECK - CRACKED BULKHEAD VERTICAL BEAM WEB, BS 178, RBL 17, WL 232. REPLACED BULKHEAD VERTICAL BEAM WEB, BS 178, RBL 17, WL 232 IAW B737 SRM 51-20-01. 2 L 7 2 4F RT A16WE 2008031900304 20080319 00304 NM 2008 3 19 USAA920080611 1 20080223 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 CLT - MAJOR REPAIR - C17 CHECK - CRACKED BULKHEAD WEB, BS 178, RBL 5.7, WL 180. REPAIRED BULKHEAD WEB, BS 178, RBL 5.7, WL 180 IAW B737 SRM 51-70-13 FIGURE 1. 2 L 7 2 4F RT A16WE 2008031900328 20080319 00328 NM 2008 3 19 USAA920080619 1 20080311 A 5330 6545776 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 24479 CLT - MAJOR REPAIR - OVERNIGHT - CRACKED FUSELAGE SKIN, BS 727E, S21R - S25R. REPAIRED FUSELAGE SKIN, BS 727E, S21R - S 25R IAW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008031900344 20080319 00344 SO 2008 3 19 C2XA08CL028 1 20080312 A 2822 2C74 PUMP EMB 145 EMB145LR 3260212 SO LT WING FAULTY A C2XA K NONE J WARNING INDICATION CR CRUISE 1 SW 27 15912 13950 145439 CLE FLIGHT 2469 - THE CREW REPORTED A E1 FUEL IMPENDING BYPASS MESSAGE IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED FU EL PUMP 1A AND ENGINE 1 FUEL FILTER. DEBRIS WAS ALSO REMOVED FROM THE PUMP 1A INLET. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008031900360 20080319 00360 EA 2008 3 19 TRAX200800405 1 20080310 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 INTERCOSTAL CLIP CRACKED AT FS 484 LBL 28. REPAIRED, IAW REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2008031900378 20080319 00378 EA 2008 3 19 TRAX200800415 1 20080313 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 TOP THRESHOLD STEP BROKEN. 2 L 7 2 4F RT A21EA 2008031900391 20080319 00391 NM 2008 3 19 CALA0800222 1 20080315 A 5310 6520723U54 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 AFT FRAME WEB IS CRACKED ABOVE UPPER I/B BOLT OF LOWER STOP PAD, FWD CARGO DOOR, AFT FRAME WEB. REPLACED C-1 AFT FRAME PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008032000036 20080320 00036 CE 2008 3 20 DXTA200802846 1 20080207 A 3222 STRUT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG UNDERSERVICED E DXTA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 07 931QS 7500064 1) RIGHT AFTER TAKEOFF, A LOUD NOISE WAS HEARD COMING FROM THE NOSE WHEEL. TROUBLESHOT TO NOSE STRUT SERVICE LOW, SERVI CED. PERFORMED OPS CHECK AND CHECKS GOOD. IAW MM CH 12-10-38 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032000038 20080320 00038 SW 2008 3 20 AC2A118969 1 20080223 A 5302 SKIN BELL 427 427 1182207 SW PWC PW207 PW207D NE TAILBOOM CHAFED E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 31 427CU 56047 AIRCRAFT WAS BROUGHT IN FROM OFFSHORE. DURING A DAILY INSPECTION SOME WORKING AND MISSING RIVETS WERE FOUND ON THE TAIL BOOM. A THROUGH INSPECTION WAS PERFORMED ON THE TAIL BOOM ATTACHMENT FITTING. TAIL ROTOR DRIVE TRAIN, TAIL ROTOR GEAR BO X CASTING, TAIL ROTOR GEAR BOX HOUSING, INCLUDING A COMPLETE TAIL BOOM STRUCTURE INSPECTION AND TAIL ROTOR BALANCE CHEC K. FOUND A CHAFE ON THE TAIL BOOM SKIN THAT MEASURED .275 IN LENGH AND A DEPTH OF .020. THE TAIL ROTOR BALANCE VIBRATION WAS ALSO FOUND TO BE HIGH 5.31 IPS, AND THE TAIL ROTOR WAS CHANGED. 1 G 7 1 3U 3 U R00001RC E42NE 2008032000040 20080320 00040 CE 2008 3 20 DXTA200802848 1 20080207 A 3260 UPLOCK SWITCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE NLG LOOSE E DXTA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 07 668QS 5605268 WHEN THE GEAR IS SELECTED UP AND IT'S UP AND STOWED, A LOUD CLUNK OCCURS FROM THE NOSE AREA. FOUND NOSE GEAR UPLOCK AFT JAM NUT LOOSE AND NOT MAKING ADEQUATE CONTACT WITH UPLOCK ROLLER. RIGGED AND SAFETIED NOSE GEAR UPLOCK SWITCH IAW MM 32- 61-00. COMPLIED WITH GEAR SWINGS AND PERTAINING PORTIONS OF GEAR FUNCTIONAL CHECK IAW MM 32-01-00. OPERATIONAL CHECKS GO OD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032000049 20080320 00049 CE 2008 3 20 DXTA200802856 1 20080209 A 3240 BRAKE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG CONTAMINATED E DXTA O OTHER E VIBRATION/BUFFET LD LANDING 1 GL 07 958QS 7500158 LANDING, INITIAL BRAKING WAS FIRM AND COULD NOT BE MAINTAINED BECAUSE OF BRAKE CHATTER. RELEASED AND REAPPLIED BRAKES A ND THERE WAS STILL CHATTER. BLED AIR FROM BRAKE SYS. PERFORMED OPERATIONAL CHECK OPS CHECK GOOD. WORK DONE IAW CHAPTE R 32-42-00 OF THE MM. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032000050 20080320 00050 CE 2008 3 20 DXTA200802857 1 20080209 A 2131 52770114 CONTROLLER CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE CABIN PRESSURE MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 697QS 2750 2750 5605197 AFTER LIFTOFF CABIN WOULD NOT PRESSURIZE. CABIN WAS CLIMBING AT SAME RATE AS AC. M2B- COMPLIED WITH KOLLSMAN DYNAMIC TE ST, TEST FAILED. REMOVED AND REPLACED CONTROLLER IAW MM 21-30-00. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008022700232 20080227 00232 NM 2008 2 27 08FDEA00601 1 20080225 A 3231 LINK DOUG MD11 MD11F 3023600 NM MLG DOOR OUT OF TOLERANCE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 618FE 48754 RIGHT MLG TO 90 SEC TO 2 MIN TO COMPLETE RETRACTION CYCLE. RED IN TRANSIT LIGHT ON BOTH PRIMARY AND SECONDARY SYSTEMS. FOUND RIGHT GEAR DOOR LINK ASSY CLEARANCE TO BE OUT OF TOLERANCE. INSTALLED SHIM AND ADJUSTED IAW MD11 MM 32-34-05-5. COMPLIED WITH GEAR SWING TO VERIFY GOOD INDICATION. OPS CHECKS GOOD, REF MD11 MM 32-31-00-5 STEP 10. 2 L 7 3 4F RT A22WE 2008022700235 20080227 00235 SO 2008 2 27 Z4TA20080001 1 20080214 A 3610 101469002 TUBE PIPER PA46 PA46500TP 7104622 SO PWA PT6 PT6A42 52043 NE BLEED AIR SYS CONTAMINATED E Z4TA H B A DEACTIVATE SYST/CIRCUITS EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 39 91KM 1 1 4697120 PCERM0132 MAINTENANCE REPLACED RT BLEED AIR TUBE ASSY (P/N 101469-002) DUE TO TIME CHANGE. THE ASSY WAS INSPECTED FOR CONDITION A ND RECEIVING DOCUMENTS FOR TRACEABILITY OF THE PART. NO DEFECTS WERE NOTED DURING RECEIVING INSPECTION. GROUND RUNUP O K AFTER REPLACEMENT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT PREPOSITIONED TO KINT FOR PASSENGER PICK-UP . UPON DEPARTURE AND CLIMBOUT, PILOT NOTICED ODOR AND SMOKE IN COCKPIT. AFTER LANDING, MAINTENANCE INSPECTED BLEED AIR SYSTEM. THE TUBE ASSY PREVIOUSLY REPLACED (P/N 101469-002), WAS REMOVED FOR INSPECTION. THE TUBE ASSY WAS CLEAR EXCEP T FOR SOME TYPE OF CONTAMINATION WHICH WAS FOUND IN THE FOLDS OF THE FLEXIBLE PORTION OF THE TUBE ASSY. THE UNIT WAS SU 1 L 7 1 3O 4 T RT A25SO E4EA 2008022700236 20080227 00236 GL 2008 2 27 CHQA200800032 2 20080217 A 7261 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL OVERSERVICED A CHQA A UNSCHED LANDING W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 294SK 145497 CAE311855 CMH TO IAD - ON INITIAL CLIMB CREW RECEIVED A LAVATORY SMOKE INDICATION ON EICAS ACCOMPANIED BY VISIBLE SMOKE/SMOKE SMEL L IN THE COCKPIT AND CABIN. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. DURING APPROACH THE SMOKE INDI CATION WENT AWAY, BUT THERE WAS STILL SOME VISIBLE SMOKE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND BOTH ENGINES OVE R-SERVICED WITH OIL. AFTER REMOVING EXCESS OIL AND RESERVICING TO THE CORRECT OIL LEVEL, BOTH ENGINES WERE RUN AND NO F URTHER SMOKE OR SMOKE INDICATIONS WERE NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008022700242 20080227 00242 SO 2008 2 27 SIMA200805303 1 20080220 A 3230 8271043 CONTROL PANEL EMB 135 EMB135KL 3260302 SO MLG MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 805AE 145489 ON FLIGHT 4820, CREW REPORTED UPON GEAR RETRACTION GOT 'LANDING GEAR HANDLE DISAGREE WITH GEAR DOWN AND UNSAFE INDICATIO N. CYCLED GEAR AND GEAR CAME UP. AIRCRAFT REMOVED FROM SERVICE. AFTER TROUBLESHOOTING DETERMINE LANDING GEAR HANDLE F OUND TO BE DEFECTIVE. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW AMM 32-32-02. PERFORMED SEVERAL OPERATIONAL SYSTEM CHECK IAW EMB AMM 32-30-00. OPERATIONAL CHECK GOOD, NO FURTHER DEFECTS NOTED AND NR 8194; AIRCRAFT RETURNED TO S ERVICE. 2 L 7 2 4F RT T00011AT 2008022700243 20080227 00243 SO 2008 2 27 SIMA200805301 1 20080219 A 5315 14530627001 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AE 20212 145101 DURING HEAVY CHECK, FLOORBEAM BETWEEN FRAME 24 AND FRAME 29, AT FRAME 25, WAS FOUND TO HAVE CORROSION. FLOORBEAM WAS RE PAIRED IAW SRM 53-22-10. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022700248 20080227 00248 NM 2008 2 27 KCSA081083 1 20080218 A 5313 STRINGER BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 STR 12R CRACKED AT BS 1780. 2 L 7 4 4F RT A20WE 2008022700251 20080227 00251 NM 2008 2 27 CALA0800141 1 20080216 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 68061 29456 WHILE REPLACING EMERGENCY LIGHT BATTERY AT STA 1340 FOUND BATTERY CHARGER WOULD NOT TEST. REPLACED BATTERY CHARGER PER AMM 33-51-07. 2 L 7 2 4F RT A1NM 2008022700252 20080227 00252 NM 2008 2 27 CALA0800142 1 20080216 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 68061 29456 WHILE REPLACING EMERGENCY LIGHT BATTERY AT STA 1362 FOUND BATTERY CHARGER WOULD NOT TEST. REPLACED BATTERY CHARGER PER AMM 33-51-07. 2 L 7 2 4F RT A1NM 2008022700256 20080227 00256 WP 2008 2 27 IXXA08SMN003S 1 20080114 A 5752 TAB DOUG DC8 DC862F 3021972 WP AILERON DELAMINATED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CONTROL TAB AILERON DELAMINATED. REMOVED REPLACE AILERON CONTROL TAB IAW DC8 MM 27-11-4 PAGES 201-205, PERFORMED OPS CHECK TO ALL FLIGHT CONTROLS GOOD IAW DC8 MM 27-11-0 PAGES 10-14, DC8 M M 27-21-0 PAGES 5-9, MM 27-30-0 PAGES 4-7, MM 27-40-0 PAGES 1-2, MM 27-40-1 PAGES 10-13, MM 27-51-0 PAGES 10-12, MM 27-6 1-0 PAGES 5-7, MM 27-70-0 PAGES 1-2, MM 27-80-0 PAGES 4. 2 L 7 4 4F 4A25 2008022700262 20080227 00262 NM 2008 2 27 UIEA200800032 1 20080209 A 5320 FLOOR SUPPORT BOEING 747 74747UF 1384812 NM BS 531-688 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 415MC 32837 MAIN DECK CARGO COMPARTMENT FLOOR PANEL SUPPORT CRACKED AT STATION 531 AND 688 RBL 116. REPAIRED FLOOR PANEL SUPPORT AS PER BOEING DOCUMENT RDR 0691225-1 TO 5. 2 L 7 4 4F RT A20WE 2008022700264 20080227 00264 NM 2008 2 27 CALA0800148 1 20080215 A 5315 141T5147 FLOORBEAM BOEING 767 767424ER 1385270 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 66051 29446 BODY STA 246 FLOORBEAM LBL 40 MID CHORD CRACKED. FLOORBEAM MID CHORD REPAIRED PER ECRA 5310-04718. 2 L 7 2 4F RT A1NM 2008022700268 20080227 00268 NM 2008 2 27 CALA0800149 1 20080215 A 5315 141T5107 FLOORBEAM BOEING 767 767424ER 1385270 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 66051 29446 CABIN STA 303 LBL 15 TO 32 FLOOR SUPORT UPPER CHORD FOUND CORRODED. FLOORBEAM REPAIRED PER SRM 53-0051. 2 L 7 2 4F RT A1NM 2008022700270 20080227 00270 NM 2008 2 27 CALA0800150 1 20080215 A 5320 141T5014 STIFFENER BOEING 767 767424ER 1385270 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 66051 29446 BS 246 FLOORBEAM LBL 40 FORWARD SIDE STIFFENER FOUND CRACKED. STIFFENER REPLACED AND INSTALLED PER SRM 53-10-51 REPAIR 4 FIG 201. 2 L 7 2 4F RT A1NM 2008022700272 20080227 00272 NE 2008 2 27 UIEA200800023 2 20080130 A 7230 COMPRESSOR BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE ENGINE STALLED A UIEA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 EA 15 523MC 21782 517547 COMPRESSOR STALL ON ENGINE 1. N1 DECREASED FROM 105 PERCENT TO 100 PERCENT REDUCED THRUST TO 33 PERCENT N1 STABILIZED F L 390, TAT -21 DEGREES. ON LANDING ROLLOUT, NR 1 N1 DECREASED AND EGT INCREASED TO 900 DEGREES. REPLACED ENGINE. 2 L 7 4 4F 4 F RT A20WE E23EA 2008022700273 20080227 00273 NM 2008 2 27 CALA0800152 1 20080215 A 5311 143A1110 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16709 28779 FRAME CRACKED STA 380 BETWEEN STRINGER 8R AND 9R. REPAIRED PER ECRA 5310-04717. 2 L 7 2 4F RT A16WE 2008022700274 20080227 00274 NM 2008 2 27 UIEA200800024 1 20080202 A 5730 PANEL BOEING 747 747243B 1384830 NM LT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 LT WING UPPER FIXED T/E PANELS AT STA WBL 445, 11.0 INCHES FROM TRAILING EDGE AND WBL 515, 6.0 INCHES FROM TRAILING EDGE HAVE A 1.0 INCH CRACK. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 2 SHEETS 3 AND 5, PREPREG LAYUP 250 DEGREES F CURE PER SRM 51-40-12. REF: ATLAS AIR EO 4757A415. 2 L 7 4 4F RT A20WE 2008022700276 20080227 00276 NM 2008 2 27 CALA0800153 1 20080215 A 5311 146A1102 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16709 28779 FRAME CRACKED AT STA 727B BETWEEN 9 & 9R. REPAIRED PER ECRA 5310-04717. 2 L 7 2 4F RT A16WE 2008022700283 20080227 00283 NM 2008 2 27 08FDEA00532 1 20080220 A 5730 1060031118 PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 WING FUEL PANEL 642BB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 642BB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-118. 2 L 7 2 4F RT A2NM 2008022700284 20080227 00284 NM 2008 2 27 08FDEA00533 1 20080220 A 5730 1060031116 PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 WING FUEL PANEL 641DB HAS SURFACE CORROSION. WING FUEL PANEL 641DB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01 , SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-116. 2 L 7 2 4F RT A2NM 2008022700287 20080227 00287 NM 2008 2 27 08FDEA00541 1 20080221 A 5730 1060031116 PANEL BOEING 757 7572B7 1384964 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 WING FUEL PANEL 541LB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 541LB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-116, ALTERNATE PN: 112N6101-1. 2 L 7 2 4F RT A2NM 2008022700289 20080227 00289 NM 2008 2 27 UIEA200800035 1 20080214 A 5330 SKIN BOEING 747 74747UF 1384812 NM BS 166 S46R DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 415MC 33837 FOUND LIGHTNING STRIKE AT STATION 166 STRINGER 46R. REPAIRED AS PER SRM 53-00-01 FIGURE 201 REPAIR 1 AND AS PER BOEING MESSAGE 1-764547003-7 AND FAA FORM 8100-9. 2 L 7 4 4F RT A20WE 2008022700290 20080227 00290 NM 2008 2 27 CALA0800158 1 20080216 A 5315 141T5108 FLOORBEAM BOEING 767 767424ER 1385270 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 66051 29446 BS 325 LBL 22-44 FLOOR SUPPORT FOUND CORRODED. FLOORBEAM REPAIRED PER SRM 53-00-51. 2 L 7 2 4F RT A1NM 2008022700291 20080227 00291 WP 2008 2 27 NWAA080589935 1 20080219 A 3397 WIRE DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1332U 47404 DURING LINE CHECK, MAINTENANCE FOUND THAT TWO OF THE THREE CATWALK EMERGENCY PATHWAY LIGHTING IN THE TAIL COMPARTMENT WE RE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE. THE SYSTEM OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4F A6WE 2008022700292 20080227 00292 WP 2008 2 27 NWAA080579927 1 20080212 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8920E 45835 DURING LINE CHECK, MAINTENANCE FOUND THAT THE CATWALK EMERGENCY PATHWAY LIGHTING IN THE TAIL COMPARTMENT WERE INOPERATIV E. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK AND ALSO REPLACED A DAMAGED WIRE HARNESS FROM THE FLOODLIGHTS TO THE CATWALK LIGHTS. OPERATIONALLY CHECKED THE SYSTEM AND RETURNED THE AIRCRAFT TO REVENUE SERVICE. 2 L 7 2 4F A6WE 2008022700295 20080227 00295 WP 2008 2 27 IXXA08SMN013S 1 20080115 A 5311 25311160071 FRAME DOUG DC8 DC862 3021970 WP ZONE 100 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT CRACK ON FRAME FLANGE AT STATION 240.000 LONGERON 21RIGH T. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED FRAME. FABRICATED FRAME AND SPLICE AND ANGLE PERFOR MED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC 8 SRM 53-2-0 FIGURE 2 SHEETS 2, AND 6, DC8 SRM 51-1-20D, DC8 SRM 53-4-1 FIGURE 41 SHEETS 7 AND 8, DC8 SRM 53-2-0 FIGURE 2 SHEET 1, DC8 SRM 51-2-0 FIGURE 50 SHEET 49A, DC8 SRM 57-2-0 FIGURE 2 SHEET 7 AND 8 TR NUMBER 53-110 DATED 11-10-00, DC 8 SRM 51-1-1 PAGES 1, 13 AND 17, DC8 SRM 51-1-8B, AND 51-3-1. 2 L 7 4 4F 4A25 2008022700297 20080227 00297 NM 2008 2 27 CALA0800159 1 20080218 A 5720 114T2300 BEAM BOEING 767 767424ER 1385270 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 66051 29446 LEFT-HAND WING LEADING EDGE BEAM FOUND CRACKED AT LEADING EDGE STATION 679. REPAIRED PER SRM 57-41-13. 2 L 7 2 4F RT A1NM 2008022700302 20080227 00302 WP 2008 2 27 IXXA08SMN023S 1 20080119 A 5730 SKIN DOUG DC8 DC862F 3021972 WP BS 186 DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING OUTER FLAP LOWER PANEL SKIN DENTED AT STATION 164.000 TO STATION XF 1 86.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PAR TS IAW DC8 SRM 57-7-1 FIGURE 4 TR NUMBER 57-94, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 4 TR NUMBE R 57-94 DATED 10-01-02 ITEM "P" AND "Q", DC8 SRM 51-1-9 TR NUMBER 51-1-42, DC8 SRM 51-1-9A AND TR 51-1-41, DC8 51-1-8B, DC8 SRM 51-1-11 AND 51-1-21. 2 L 7 4 4F 4A25 2008022700305 20080227 00305 NM 2008 2 27 UIEA200800064 1 20080221 A 5340 65B38170 FITTING BOEING 747 7472D3B 1384805 NM BS 1823 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 AFT CARGO DOOR FAILED TO CLOSE DURING NORMAL OPERATION. AFTER DISASSEMBLY (REFERENCE SDR UIEA200800063) FOUND FORWARD P OSITION ROTARY LIFT ACTUATOR FRAME REINFORCEMENT FITTING WITH ELONGATED ACTUATOR MOUNT BOLT HOLES. REPLACED FITTING 65B 38170-3 PER STANDARD PRACTICES IAW SRM 51-30-02 AND LIFT ACTUATOR 60B00305-1 PER AMM 52-34-03. OPS CHECK NORMAL. 2 L 7 4 4F RT A20WE 2008022700306 20080227 00306 NM 2008 2 27 KCSA081084 1 20080219 A 5412 BULKHEAD BOEING 747 747209B 138489B NM NR 3 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 NR 3 PYLON NAC STA 221.9 BULKHEAD WEB CHAFED AT HYD RETURN LINE. 2 L 7 4 4F RT A20WE 2008022700307 20080227 00307 NM 2008 2 27 KCSA081085 1 20080219 A 5315 FLOORBEAM BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 UPPER DECK FLOORBEAM LOWER CHORD CORRODED AT BS 780, RBL 20. 2 L 7 4 4F RT A20WE 2008022700308 20080227 00308 SO 2008 2 27 SIMA200805703 1 20080221 A 3010 10006491 ANTI-ICE VALVE EMB 145 EMB145LR 3260212 SO WING INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 630AE 145132 ON FLIGHT 3422, CREW REPORTED RETURN TO FIELD FOR ANTI-ICE CONDITION INOP MESSAGES WITH WING AND STAB MESSAGES. THE CRE W DID DECLARE AN EMERGENCY. LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT WING A NTI-ICING VALVE. OPERATIONAL CHECK GOOD AND NR 8194; AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032000051 20080320 00051 NM 2008 3 20 DXTA200802858 1 20080210 A 2612 312062 FUSE GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE FIRE DETECTION FAILED E DXTA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 07 729QS 2184 118 APU FIRE CAS MESSAGE ILLUMINATED ALONG WITH FIRE BELL ENROUTE AT FL380. RT FIRE BOTTLE WAS DISCHARGED INTO APU. FIRE IND ICATION REMAINED ON, DIVERTED. AFTER SHUTTING DOWN AND EXITING AC, NO SMOKE, FLAMES OR SOOT WERE VISIBLE IN THE AREA OF THE APU BUT THE APU FIRE CAS MESSAGE PERSISTED. REPLACED FUSE P/N 312-062 IN APU FIRE WARNING SYS. CONDUCTED FIRE WARNI NG TEST. OPERATIONAL CHECKS GOOD. IAW MM CH 26-10-25. REPLACED FIRE EXTINGUISHER WITH A NEW UNIT. INSTALLED 3 NEW SQ UIBS. OPS TEST GOOD. MX IAW MM 26-20-05, 26-20-10, 26-10-25. 2 L 7 2 4F 4 F RT A53NM E35NE 2008032000052 20080320 00052 CE 2008 3 20 DXTA200802859 1 20080210 A 3260 65430087 UPLOCK SWITCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG INOPERATIVE E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 650QS 6823 5605150 AFTER TAKEOFF, THE GEAR UNLOCK LIGHT, STAB MISCOMPARE AND HYD PRESS ANNUNCIATORS ILLUMINATED CONTINUOUSLY AFTER THE GEAR HANDLE WAS RAISED TO THE (UP) POSITION. THE HYD PRESS LIGHT NEVER FLASHED. REPLACED UPLOCK SWITCH IAW CH 32-60-01 WHILE ADJUSTING SWITCH, NOTICED UPLOCK ROLLER BRACKET ASSY BENT. REPLACED BRACKET ASSY IAW MM CHPT 32-20-01. ADJUSTED SWITCH IAW MM CHAPT 32-61-00. OPS CHECK GOOD DURING LANDING GEAR FUNCTIONAL. C/W UPLOCK SWITCH SAFTIES. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032000065 20080320 00065 NM 2008 3 20 DXTA20082872 1 20080213 A 3244 5009029 TIRE GULSTM 200 200 4500308 NM PWC PW306 PW306C 52169 NE RT MLG FAILED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 723QS 352 352 099 UPON LANDING, THE RT MAIN TIRES BLEW AND DISINTEGRATED AND DAMAGED THE RIMS AND GEAR DOOR. REPLACED ALL 4 MLG WHEEL ASSE MBLIES IAW THE G200 CMP'S NR`S 324201, 324202, 324203 AND 324204. 2 L 7 2 4F 4 F RT A53NM E35NE 2008032000069 20080320 00069 CE 2008 3 20 DJFA2008018 1 20080227 A 3297 CONNECTOR BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE UPLOCK SWITCH DAMAGED E DJFA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 23 429LX RK265 CREW REPORTED AFTER TAKEOFF UPON GEAR RETRACTION THE RED UNSAFE LANDING GEAR LIGHT REMAINED ILLUMINATED. EMERGENCY GEAR EXTENSION WAS PERFORMED WITH NORMAL INDICATION AFTERWARD. THE AC DIVERTED, MAINT FOUND PIN M OF THE RT DOOR UPLOCK SWI TCH PUSHED BACK. THE PIN WAS REPAIRED, OPS CHECKS WERE GOOD AND THE AC WAS RETURNED TO SERVICE 2 H 7 2 4F 4 F RT A16SW E25EA 2008032000070 20080320 00070 CE 2008 3 20 DJFA2008019 1 20080225 A 3260 UPLOCK SWITCH BEECH MU300 400A 1155402 CE MLG OUT OF ADJUST E DJFA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 EA 23 429LX RK265 CREW REPORTED AFTER TAKE OFF DURING GEAR RETRACTION THE UNSAFE GEAR LIGHT ILLUMINATED. THE GEAR WAS EXTENDED WITH NO DO WN AND LOCKED INDICATION. EMERGENCY PROCEDURES WERE TAKEN AND LANDING WAS NORMAL. MAINT FOUND LT AND RT LANDING GEAR D OOR UPLOCK SWITCHES IN NEED OF ADJUSTMENT. ADJUSTMENTS WERE MADE PER THE MM. SEVERAL GEAR SWINGS WERE PERFORMED WITH N O DEFECTS NOTED AND THE AC WAS RETURNED TO SERVICE. 2 H 7 2 4F RT A16SW 2008032000074 20080320 00074 CE 2008 3 20 DXTA20082875 1 20080214 A 2435 99121253 STARTER GEN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT ENGINE VIBRATION E DXTA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 07 373QS 789 789 5600373 BUFFETING/GRINDING NOISE INTERMITTENT AT ALL ALTITUDES AND SPEEDS. FOUND STARTER/GENERATOR ON LT ENGINE VIBRATING EXCESS IVELY. REMOVED AND REPLACED GENERATOR IAW ULTRA MM 80-11-01. GROUND RUN OPERATIONAL CHECKS SATISFACTORY. EXTERIOR INSPEC TION OF AC REVEALED NO FAULTS. 2 L 7 2 4F 4 F RT A22CE E25EA 2008032000076 20080320 00076 CE 2008 3 20 DXTA20082877 1 20080214 A 3260 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG WARNING LIGHT E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 367QS 5600367 AFTER GEAR RETRACTION WAS SELECTED RED INTRANSIT LIGHT REMAINED ON. JACKED AC, INSPECTED W/W AND WIRING CK'D SWITCHES IA W WDM 32-30-01-02 AND 32-60-01-04 ALL NORM. HOOKS APPEAR NORMAL. NO ABNORMAL INDICATION AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E25EA 2008032000082 20080320 00082 CE 2008 3 20 DXTA20082883 1 20080215 A 2731 TRIM SYSTEM RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP ELEVATORS OUT OF RIG E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 838QS 258338 DURING CLIMB (APPROXIMATELY 16,000-18,000) TRIM SYS REACHED FWD NOSE DOWN POSITION AND PILOT WAS HOLDING FWD PRESSURE O N YOKE. RIGGED ELEVATOR TRIM JACKS AND ELEVATORS IAW AMM 27-30-00, 27-30-51 AND 27-30-22. 2 L 7 2 4F 4 F RT A3EU E6WE 2008032000088 20080320 00088 SO 2008 3 20 FDKA200803099 1 20080307 A 5340 14536830001 MOUNT EMB 145 EMB145LR 3260212 SO ANTENNA CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 835MJ 145353 RAD LL ANTENNA MOUNT IS CORRODED ON THE LOWER FUSELAGE. THE MOUNT HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008032000090 20080320 00090 SO 2008 3 20 FDKA200803101 1 20080307 A 7830 DOOR EMB 145 EMB145LR 3260212 SO THRUST REVERSER BENT A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 835MJ 145353 LEADING EDGE OF NR 1 THRUST REVERSER LOWER DOOR IS BENT. STRAIGHTENED DAMAGED AREA AND NDT SHOWS NO CRACKS. 2 L 7 2 4T RT T00011AT 2008032000093 20080320 00093 EA 2008 3 20 SWIA200819332 1 20080304 A 3350 LENS CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 727SK 10191 FLT 6392 - LENS OF EMERGENCY LIGHT IS MISSING. INSTALLED SERVICEABLE LENS ON EMERGENCY LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008032000103 20080320 00103 WP 2008 3 20 NWAA080909929 1 20080310 A 2740 ACTUATOR DOUG DC9 DC931 3022065 WP STAB TRIM MALFUNCTIONED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 8923E 45838 AIRCRAFT RETURNED TO A SAFE LANDING AFTER PILOT EXPERIENCED HORIZONTAL STABILIZER PROBLEMS DURING CLIMB-OUT. FIRST OFFI CER HAD SELECTED STABILIZER TRIM AND WAS UNABLE TO STOP THE STABILIZER FROM CONTINUOUSLY MOVING, OSCILLATING UP AND DOWN PAST THE DESIRED POINT. COM WAS COMPLIED WITH AND AFTER STABILIZER TRIM CUTOUT WAS SELECTED TO STOP, THE HUNTING OF THE STAB STOPPED BUT THE WARNING HORN CONTINUED. FLIGHT RETURNED TO AN UNEVENTFUL LANDING UNDER A DECLARED YELLOW EMERGENCY . MAINTENANCE REPLACED THE PRIMARY TRIM ACTUATOR MOTOR, PRIMARY TRIM UPPER RELAY R20-16 & LOWER RELAY R20-15, THE F/O’S PRIMARY TRIM YOKE SWITCH, AND CIRCUIT BREAKER B10-92. STOP ADJUSTMENTS WERE MADE, HARDWARE TORQUED, AND THE AIRCRAFT RE 2 L 7 2 4F A6WE 2008032000104 20080320 00104 NM 2008 3 20 NWAA080866306 1 20080309 A 3397 CONNECTOR BOEING 747 747451 1384940 NM EMERGENCY LIGHTS DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 666UD 23821 DURING OVERNIGHT CHECK, ZONE D LEFT SIDE EMERGENCY LIGHTS WON'T ILLUMINATE. MAINTENANCE RECONNECTED ELECTRICAL CONNECTO RS. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008032000105 20080320 00105 NM 2008 3 20 NWAA080876306 1 20080309 A 3397 CONNECTOR BOEING 747 747451 1384940 NM EMERGENCY LIGHTS DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 666US 23821 DURING OVERNIGHT CHECK, FOUND ZONE B LEFT SIDE EMERGENCY LIGHTS WON'T ILLUMINATE. MAINTENANCE RECONNECTED ELECTRICAL CO NNECTORS. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008032000108 20080320 00108 SO 2008 3 20 SIMA200807301 1 20080311 A 2150 ACM EMB 145 EMB145LR 3260212 SO ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 664MS 145779 ON FLIGHT 4101, CREW REPORTED A STRONG FUEL ODOR WHEN APU IS POWERING PACKS AND OIL ODOR WHEN ENGINES POWERING PACKS. 2 L 7 2 4T RT T00011AT 2008032000109 20080320 00109 SO 2008 3 20 SMIA200807302 1 20080309 A 3222 EM14532078KIT PACKING EMB EMB 145 EMB145LR 3260212 SO NLG DAMAGED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 933JN EM14532078 14500918 ON FLIGHT 3788, CREW REPORTED AFTER TAKEOFF DURING GEAR RETRACTION RECEIVED LANDING AIR/GND FAIL MESSAGE AND E1(2) REVE RSE DISAGREE EICAS MESSAGE. AIRCRAFT REMOVED FROM SURVIVE. REMOVED AND REPLACED NLG STRUT SEAL. LEFT AND RIGHT TR OPE RATIONAL CHECK GOOD IAW EMB AMM 78-31-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032000110 20080320 00110 EA 2008 3 20 SIMA200807303 1 20080310 A 3260 895302 PSEU CNDAIR CL600 CL6002C10 1390015 EA MLG MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 504AE 10044 ON FLIGHT 3757 CREW REPORTED DURING CLIMB-OUT AFTER COMMANDING LANDING GEAR RETRACTION VIA THE LANDING GEAR CONTROL HAND LE. THE EICAS WARNING MESSAGE GEAR DISAGREE WARNING MSG ILLUMINATED ALONG WITH A NOISE FROM THE NOSE GEAR AREA. CREW F OLLOWED AOM PROCEDURES AND ELECTED TO RETURN TO DFW. AFTER 2 TOWER FLYBYS TO CONFIRM THE SAFETY OF THE LANDING GEAR. TO WER CHECK GOOD. AIRCRAFT LANDED SAFELY AND WAS TOWED TO THE GATE WITHOUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVI CE. REMOVED AND REPLACED PSEU IAW CRJ 700 AMM 32-61-01OPS CHECK PERFORMED GEAR SWING IAW CRJ 700 AMM 32-30-00 GEAR SWIN G CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008032000118 20080320 00118 NM 2008 3 20 DL75E080324 1 20080307 A 3297 WIRE BOEING 757 757231 1384950 NM ANTI SKID SYS DAMAGED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 721TW 29954 AFTER PUSHBACK, EICAS ANNUN ANTI-SKID AND STATUS ANTI-SKID AND ALTN ANTI-SKID MSG WAS INTERMITTENT. BITE CK NR 1 TDCR. REPLACED TDCR AND CHECKED RES OF PINS 1 TO 3. CHECKED WIRING FROM E5 TO TDCR CKS OK SUSPECT CONTROL UNIT. RETERMINATE D FERRULE AT REAR LANDING GEAR JUNCTION BOX, CHECKS OK. 2 L 7 2 4F RT A2NM 2008032000121 20080320 00121 NE 2008 3 20 DL75E080327 2 20080309 A 7200 PW2037RTC ENGINE BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE NR 2 UNKNOWN A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 713TW 23727 28173 728772 IN CRUISE GOT RT ENG PRI CONT AND A RT ENG SEC CONT MESSAGE. THE EPCS MESSAGES WERE: P SVA OR FCU/EEC AND S SVA OR FCU/ EEC. DUE TO HISTORY AND UNABLE LOCATE DEFINITIVE PROBLEM. REPLACING NR 2 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032000122 20080320 00122 NE 2008 3 20 DL738080329 2 20080310 A 7310 3400162510 LINE BOEING 737 737832 13844CF NM GE CFM56 CFM56* 13802 NE NR 2 FUEL RUPTURED A DALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 379DA 30349 874871 CREW FOUND FUEL IMBALANCE DETERMINED TO BE COMING FROM NR 2 ENG, FOLLOWED QRH PROCEDURE FOR ENGINE FUEL LEAK AND SHUT EN GINE DOWN. FUEL LEAK FOUND TO BE CAUSED BY RUPTURED FLEX LINE COMING FROM IDG OIL COOLER, P/N 340-016-251-0 REF IPC 73- 11-00-02 ITEM 245J. 2 L 7 2 4F 4 F RT A16WE E2GL 2008032000125 20080320 00125 NM 2008 3 20 DL757080332 1 20080211 A 5330 DOUBLER BOEING 757 757232 1384965 NM BS 1530 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 CORROSION ON TRANSITION PANEL SPLICE DOUBLER STATION 1530 LT SIDE IS OUT OF LIMITS. REPAIRED DOUBLER IAW SRM 51-40-05 A ND SRM 51-20-01. 2 L 7 2 4F RT A2NM 2008032000126 20080320 00126 NM 2008 3 20 DL757080333 1 20080203 A 5320 SPLICE BOEING 757 757232 1384965 NM BS 1500 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 AFT CARGO PIT-STA 1500, LBL 28 HAS SEVERE CORROSION. REPAIRED IAW SRM 53-00-03 FIG 201 AND DRAWING NR 146N3110. 2 L 7 2 4F RT A2NM 2008032000130 20080320 00130 NM 2008 3 20 DL757080337 1 20080209 A 5313 STRINGER BOEING 757 757232 1384965 NM BS 1644-1654 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 STRINGER 520R REPAIR SPLICE AT STA 1644-1654 IS CORRODED SEVERAL PLACES WITH A MISDRILLED HOLE. FABRICATED SPLICE IAW S RM 51-10-02. 2 L 7 2 4F RT A2NM 2008032000131 20080320 00131 NM 2008 3 20 DL757080338 1 20080203 A 5311 FRAME BOEING 757 757232 1384965 NM BS 690 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 SURFACE CORROSION ON FRAME AT FS 690 RBL 13. FABRICATED "U" CHANNEL IAW B757 DRAWING 453N1853 AND SRM 51-70-11. INSTAL LED IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008032000132 20080320 00132 NM 2008 3 20 DL757080339 1 20080203 A 5320 STRUCTURE BOEING 757 757232 1384965 NM AFT CARGO CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 AFT CARGO PIT BS 1480, LBL 29; AREA CORRODED. REMOVED CORROSION IAW SRM 51-40-02, MEASURED AREA IAW NDTM PT 4, 51-00-00 . CHECKED GOOD. TREATED AND PRIMED AREA IAW SRM 51-00-01. 2 L 7 2 4F RT A2NM 2008032000133 20080320 00133 NM 2008 3 20 DL757080340 1 20080206 A 5320 PANEL BOEING 757 757232 1384965 NM BS 620 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 CORROSION EXIST ON FWD CARGO RT CATWALK PANEL STA 620 RBL 29. REPLACED WITH FABRICATED PANEL IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008032000134 20080320 00134 NM 2008 3 20 DL757080341 1 20080205 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 329 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 MAIN CABIN FLOOR SUPPORT STA 329 RBL 23 HAS ELONGATED FASTENER HOLE. REFABRICATED FLOOR SUPPORT IAW DWGJ141N5150. 2 L 7 2 4F RT A2NM 2008032000135 20080320 00135 NM 2008 3 20 DL757080342 1 20080205 A 5321 FLOOR PANEL BOEING 757 757232 1384965 NM CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 AFT CARGO FLOOR PANEL 153AF HAS CORROSION. FABRICATED FLOOR PANEL IAW SRM 53-60-53 FIG 1 AND INSTALLED. 2 L 7 2 4F RT A2NM 2008032000141 20080320 00141 NM 2008 3 20 DL757080348 1 20080201 A 5320 FLOOR SUPPORT BOEING 757 757232 1384965 NM BS 1650-1670 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 CORROSION ON FLOOR SUPPORT AFT CABIN STA 1650-1670 RBL 60. FABRICATED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008032000145 20080320 00145 NM 2008 3 20 DL757080352 1 20080311 A 5330 146N37805 SKIN BOEING 757 757232 1384965 NM BS 1621-1661 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 DURING HMV, SEVERAL DENTS AND TWO EXISTING SKIN REPAIRS WERE FOUND BETWEEN STA 1621 AND STA 1661, S19R TO S23R. THE DEN TS AND EXISTING REPAIR DOUBLERS WERE REMOVED AND A SINGLE REPAIR WAS INSTALLED AND APPROVED BY BOEING VIA FAA FORM 8100- 9 FOR STATIC STRENGTH. A DTA IS DUE WITHIN 12 MONTHS. 2 L 7 2 4F RT A2NM 2008032000146 20080320 00146 NM 2008 3 20 DLM90080356 1 20080218 A 5320 STRAP DOUG MD90 MD9030 3023690 NM BS 1364 S29LR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 88739 53391 AFT CARGO BAY TIE STRAP ATTACHED TO TOP SIDE OF LONG 29R, 30, AND 29L STA 1364 CORRODED. REMOVED AND REPLACED AFT CARGO TIE STRAP, IAW MD90 SRM 51-30-02. 2 L 7 2 4F RT A6WE 2008032000147 20080320 00147 NM 2008 3 20 DLM90080357 1 20080219 A 5322 9957739 SHEAR TIE DOUG MD90 MD9030 3023690 NM BS 1344 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 AFT CARGO BAY SHEAR TIE AFT SIDE OF STA 1344 BETWEEN LONGERON 27L AND 26R CORRODED. REMOVED AND REPLACED DAMAGED SHEAR TIE WITH FABRICATED PARTS IAW DAC DWG 9957739 AND MD90 SRM 51-30-02. 2 L 7 2 4F RT A6WE 2008032000149 20080320 00149 NM 2008 3 20 NWAA080926309 1 20080221 A 5313 STRINGER BOEING 747 747451 1384940 NM BS 500 S10R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING "M" CHECK, FOUND CRACKS IN STRINGER 10R AT BS 500. REPAIRED PER EA 63-212202. 2 L 7 4 4F RT A20WE 2008032000155 20080320 00155 SO 2008 3 20 LR7A08036 1 20080227 A 7120 36001725 MOUNT LKHEED 382 382G 526414U SO ENGINE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2299 5025 DURING SCHEDULED C-7 CHECK, PER AD96-12-20, FOUND ENGINE NR 4 INBD TRUSS LUG DIAGONAL TUBE ATTACHMENT CRACKED AND BUSHIN G HOLE TO BE BEYOND LIMITS AT FS 488.5, WL269.75, RT OWS 162.75. REPAIR ACCOMPLISHED BY REPLACING INBD TRUSS MOUNT IAW SMP583 CHAP 54-30 AND FIG 54-30-06. 2 H 7 4 4T A1SO 2008032000159 20080320 00159 SO 2008 3 20 LR7A08040 1 20080227 A 5320 3700326465 SUPPORT LKHEED 382 382G 526414U SO FS180 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2299 5025 DURING SCHEDULED C-7 CHECK, PER SB A382-53-51 R1, FOUND UNDERDECK CROSS BEAM EXTRUSION CRACKED AT FS 180.5, WL172, LBL10 -RBL10. REPAIR ACCOMPLISHED IAW SMP583 CHAP 51-60 AND 51-70 AND SB A382-53-51 R1 REFERENCING DWG 382-53-187. 2 H 7 4 4T A1SO 2008031900176 20080319 00176 EA 2008 3 19 TRAX200800349 1 20080227 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 CORROSION DAMAGE IN MAIN AVIONICS BAY BETWEEN FS 295.00 AND 310.00 FRAMES (MARKED). BLENDED CORROSION ON FS 295 FRAME I N LIMITS, .047 MATERIAL REMAINING IAW CRJ 700 SRM 53-21-06. SUPPLEMENTAL SDR CLOSED 3/7/08. 2 L 7 2 4F RT A21EA 2008031900226 20080319 00226 NM 2008 3 19 USAA920080575 1 20080226 A 5315 D5347218820200 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801AW 889 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 2884 / FR 68, +Y1292. REPLACED CABIN FLOORBEAM, BS 288 4 / FR 68, +Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900228 20080319 00228 NM 2008 3 19 USAA920080576 1 20080301 A 5320 D53480019217 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801AW 889 SAL - MAJOR REPAIR - C7 CHECK - CRACKED CABIN SHEAR PLATE, BS 2884 / FR 68 - BS 2936 / FR 69, -Y1292. REPLACED CABIN SH EAR PLATE, BS 2884 / FR 68 - BS 2936 / FR 69, -Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900260 20080319 00260 EA 2008 3 19 N6WA0080204 1 20080218 A 3350 BC50393103 LENS CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE EMERGENCY LIGHTS MISSING A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 151GJ 10216 EXIT LENS MISSING IN LOWER CORNER BY SERVICE DOOR. REPLACED LENS. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008031900284 20080319 00284 NE 2008 3 19 SA08009 2 20080307 A 7530 AC69572 SOLENOID AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE NR 1 ENGINE FAULTY A USAA A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 19 808AW 1088 V11027 ORD FLT 269 - LAS TO YYZ. WHILE AT FL 370, EXPERIENCED AN ENGINE ONE COMPRESSOR STALL. ABOUT 30 MINUTES LATER, THE NUM BER ONE ENGINE STALLED AGAIN. FLIGHT DIVERTED INTO ORD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ENGIN E ONE SOLENOID 7B. OPERATIONALLY CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031900291 20080319 00291 EU 2008 3 19 USAA920080564 1 20080301 A 5320 D5347219020490 DUMMY RAIL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651AW 866 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOOR DUMMY RAIL, BS 3043 /FR 64 - BS 3158 /FR 66, +Y1292. REPLACED CABIN FLOOR DUMMY RAIL, BS 3043 /FR 64 - BS 3158 /FR 66, +Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900313 20080319 00313 EA 2008 3 19 TRAX200800392 1 20080309 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 835AS 7258 EMERGENCY LIGHT ON RIGHT FUSELAGE AFT IS INOP. 2 L 7 2 4F RT A21EA 2008031900315 20080319 00315 NM 2008 3 19 ASMF200802007 1 20080224 A 5730 SKIN BOEING 777 777* UTILUSE NM GE GE90 GE9092B 30036 NE LT WING DEFORMED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 774AM 28689 DURING TAXING, THE AC LT SLATS NR 2 AND 3 STRUCK AGAINST A LAMPPOST OF TAXIWAY. DETAILED INSP WAS PERFORMED ON LT WING D ETECTING STRUCTURAL DAMAGE ON SLATS NR 2 AND 3 OF 70 INCHES LENGTH AND 25 INCHES WIDTH, OUT OF LIMITS, LOCATED BETWEEN S TATIONS WS1110 AND WS1162, WHICH INCLUDES CRACKS IN LEADING EDGE AND STRUCTURE OF 53 INCHES LENGTH AND 22 INCHES WIDTH. ADDITIONALLY, THE LT WING UPPER SKIN FROM STA WS1125 TO WS1147 WAS FOUND DEFORMED AND WITH A CRACK NEAR TO THE FWD BEAM AND THE LT WING LOWER SKIN FROM STA WS1125 TO WS1174 WAS FOUND DEFORMED AND CRACKED NEAR TO THE FWD BEAM. DETAILED REPA IR INFORMATION WILL BE SENT AS A SUPPLEMENT. 2 L 7 2 4F 4 F RT T00001SE E00049EN 2008031900318 20080319 00318 CE 2008 3 19 DXTA200802814 1 20080130 A 2150 73838431 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AFT SERVICE BAY LEAKING E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 949QS 9075 7500049 AFTER APU START CABIN FILLED UP WITH ENVIROMENTAL SMOKE. REMOVED AND REPLACED FWD (CABIN) ACM WITH REPAIRED UNIT AND SE RVICED WITH OIL. IAW MM 21-51-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008031900335 20080319 00335 NM 2008 3 19 USAA920080624 1 20080311 A 5330 65C3262 SKIN BOEING 737 737401 1384701 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 423US 23990 CLT - MAJOR REPAIR - C1 CHECK - LEVEL 2 CORROSION ON FUSELAGE SKIN, BS 727, S3R. REPAIRED FUSELAGE SKIN, BS 727, S3R IA W USAIRWAYS EA 100285. 2 L 7 2 4F RT A16WE 2008031900345 20080319 00345 2008 3 19 CALA0800215 4 20080312 A 2564 64356101 LIFE RAFT BOEING 737 737824 13844BZ NM DOOR DISCHARGED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 27 27239 28951 FWD AND AFT LIFE RAFT ASSY'S INOP. BOTTLES HAVE ZERO PSI. PLACED RAFTS ON PLACARD A/C OVERWATER RESTRICTED. 2 L 7 2 4F RT A16WE 2008031900371 20080319 00371 NE 2008 3 19 DXTA200802824 2 20080203 A 7200 305257101 GASKET CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE RT ENGINE LEAKING E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 807QS 4255 5600617 DURING TAKEOFF ROLL, RT ENGINE ITT CLIMBED TO 700 DEG WHERE AS LT ENGINE STABILILZED AT 650 DEG ABORTED TO ROLL. CONFIR MED RT ENGINE TO GO UP TO 700 DEGREES AND T/O POWER. PERFORMED ALL ELECTRICAL CHECKS TO DETERMINE NR2 ITT INDICATION SY STEM IS READING TRUE ITT. INSTALLED ALL NEW BLEED AIR LINE GASKETS, SEALS, AND BELLOWS. PERFORMED ENGINE RUNS AT T/O P OWER, NO BLEED AIR LEAKS NOTICED. PERFORMED 5 POINT PWR RUNS, UNCAPPED N1 91.5 PERCENT, 700 ITT, 99.2 PERCENT N2. ALL PARAMETERS WITHIN LIMITS AT THIS TIME IAW MM CHAP 5-10-00, 77-20-00, 77-20-00, 75-30-01, 75-00-00 AND MM CHAP 36-12-01. 2 L 7 2 4F 4 F RT A22CE E00053EN 2008031900388 20080319 00388 EU 2008 3 19 USAA920080631 1 20080316 A 5610 NP1653115 WINDSHIELD AIRBUS 320 A320232 3930326 EU COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 647AW 38383 38383 762 FLT 531 - FLL-LAS - DIVERSION - RECEIVED ACARS MESSAGE THAT CAPTAIN'S WINDOW PANE CRACKED, DESCENDED TO FL 230. AIRCRAF T DIVERTED TO IAH DUE TO MAINTENANCE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN' S WINDSHIELD. 2 L 7 2 4F RT A28NM 2008031900392 20080319 00392 NM 2008 3 19 CALA0800223 1 20080309 A 5320 65C10592155 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INTERCOSTAL BETWEEN 967 + 986.5 FLOORBEAMS RBL 18 IS CRACKED 986.5 SIDE. REMOVED AND REPLACED FLOOR SUPPORT LOCATED AT RBL 18 AND BETWEEN BS 967 TO BS 986.5, REF 737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008031900394 20080319 00394 NM 2008 3 19 CALA0800225 1 20080317 A 5330 6545800 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 R-1 DOOR CUTOUT LWR AFT CORNER CRACKED APPROX 1.5 INCHES LONG. INSTALLED REPAIR REF SRM 53-10-01 REPAIR 2. 2 L 7 2 4F RT A16WE 2008032000014 20080320 00014 CE 2008 3 20 DXTA200802829 1 20080202 A 2497 D50000Y0 CONNECTOR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE ELECTRICAL BROKEN E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 390QS 8178 5600490 WHILE AT CRUISE ALT 32000 WITH 28 MIN INTO THE FLIGHT, ACFT FAIL LIGHT CAME ON WITH MASTER WARNING. ACFT FAIL LIGHT STAY ED ON UNTIL WE RESET MASTER WARNING AFTER 5 MIN. DURING THIS TIME VOLTS SHOWED 28 AND GENS SHOW 50 AMPS EACH AND WERE ST EADY. INVERTERS SHOWED GOOD. M2B- FOUND CONNECTOR PN 383 OF NOSE AVIONICS J-BOX WITH BROKEN THUMBSCREEN CAUSING LOOSE CO NNECTION REPLACED THUMBSCREEN WITH NEW, OPS CHECK NORMAL IAW MM 20-21-03 AND 560 WDM 24-20-01 2 L 7 2 4F 4 F RT A22CE E25EA 2008032000024 20080320 00024 EA 2008 3 20 N6WA0080104 1 20080130 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE EMERGENCY LIGHTS BURNED OUT A N6WA K NONE L NO TEST IN INSP/MAINT 1 CE 03 165GJ 10257 EXIT ROW 12 LT LOWER EMERGENCY EXIT SIGN HAS INOP BULB. REPLACED BULB. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008032000030 20080320 00030 NM 2008 3 20 DXTA200802840 1 20080205 A 2120 6411801 SWITCH GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE BLEED OVERTEMP INOPERATIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 728QS 2288 116 DURING T/O ROLL WITH THROTTLES AT T/O DETENT THE BLEED PRESS/TEMP HIGH MSG ILLUMINATED. THE T/O WAS ABORTED. M2B- REMOVE D FWD OVERTEMP SWITCH P/N 641180-1 S/N 0245 AND INSTALLED NEW FWD OVERTEMP SWITCH P/N 641180-1 S/N 0368. REMOVED AFT OVE RTEMP SWITCH P/N 641180-1 S/N 9247 AND INSTALLED NEW AFT OVERTEMP SWITCH P/N 641180-1 S/N 0375. REMOVED OVERPRESSURE SWI TCH P/N 642021-1 S/N 0102 AND INSTALLED NEW OVER PRESSURE SWITCH P/N 642021-1 S/N 0183. PERFORMED FUNCTIONAL AND OPERATI ONAL CHECK, FUNCTIONAL AND OP'S CHECK GOOD. NO DEFECTS NOTED. ALL WORK PERFORMED IAW MM 21-11-00. 2 L 7 2 4F 4 F RT A53NM E35NE 2008032000039 20080320 00039 CE 2008 3 20 DXTA200802847 1 20080207 A 3233 278882 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 919QS 4623 7500224 FOLLOWING GEAR RETRACTION AFTER TAKEOFF, THE GREEN NOSE GEAR DOWN LIGHT REMAINED ILLUMINATED. REPLACED NLG ACTUATOR IAW MM CH 32-30-03 OPS AND LEAK CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032000054 20080320 00054 CE 2008 3 20 DXTA200802861 1 20080210 A 2130 CABIN PRESSURE CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 381QS 6800097 ON CLIMBOUT, AC PRESSURIZED UNTIL 9.3 PSI SWITCHED TO MANUAL AND WAS ABLE TO CONTROL PRESSURIZATION, SWITCHED BACK TO AU TO FOR THE DESCENT AND APPEARED TO OPERATE NORMALLY IN DESCENT. OPERATIONALLY CHECKED PRESSURIZATION SYS IAW MM CH 21-3 0-00, NO DISCREPANCIES NOTED. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RC T00012WI E35NE 2008032000056 20080320 00056 CE 2008 3 20 DXTA200802863 1 20080210 A 3244 AHA1814 TIRE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP MLG FAILED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 885QS 242 258743 BOTH LT MAIN TIRES BLEW UPON LANDING AND DAMAGED LT RIMS. M2B- REMOVED AND REPLACED NR 1 AND NR 2 MLG WHEEL/TIRE ASSEMBL IES AND NR 1 AND NR 2 MLG BRAKE ASSEMBLIES REF AMM 32-40-12 AND 32-40-114. REMOVED AND REPLACED NR 3 AND NR 4 MLG WHEEL/ TIRE ASSEMBLIES AS A PRECAUTION. 2 L 7 2 4F 4 F RT A3EU E6WE 2008032000067 20080320 00067 CE 2008 3 20 GLBA20061076 1 20080225 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BS 183 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 122UX UE122 FUSELAGE FRAME CRACKED .5 INCH AT FS 183 AT STRINGER 9R. MAINT REPAIRED FRAME CRACK AT STR RELIEF HOLE FS 183, STRINGER 9R IAW SRM REF 51-70. REPAIR APPROXIMATELY 5.5 INCH X 2.5 2024-T3 .071. RII INSPCOMPLIED WITH IAW TASKCARD 8.2.1. 2 L 7 2 4T 3 T RT A24CE E2NE 2008032000087 20080320 00087 SO 2008 3 20 FDKA200803097 1 20080309 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6154 RDU-BOS (1333 PHX LCL) - SERVICE DOOR EMERGENCY EXIT SIGN INOP. MX RESECURED CONNECTORS. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008032000114 20080320 00114 SW 2008 3 20 WGEA200800040 1 20080304 A 2711 TRIM SYSTEM ECLIPS EA500 ECLIPSEEA500 3350000 SW AILERONS MALFUNCTIONED E WGEA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 EA 27 163DJ 000081 WHILE HAND FLYING, AILERON TRIM DOES NOT SEEM TO WORK TO THE RIGHT EVEN WITH FULL DEFLECTION. OK TO THE LEFT. TRIM IND ICATION MOVES OK. SUPPLEMENTAL INFORMATION, PERFORMED AILERON TRIM FUNCTIONAL TEST IAW EA500 AMM 27-00-00 SUB TASK 27-0 0-00-071. ALL CHECKS GOOD. PERFORMED AILERON FRICTION CHECK IAW ECLIPSE TSR NR 27-030308G REV A DATED 03-03-08 ALL CHE CKS GOOD. SUPPLEMENTAL INFORMATION, REFERENCE LOGBOOK PAGE 1762, ITEM 2. EVALUATION FLIGHT UNSATISFACTORY, LOGBOOK PAG E 1762, ITEM 3. REQUIRES RWD AILERON TRIM AT HIGH AIRSPEEDS 250 KTS - 101 PERCENT RWD, 220 KTS - 84 PERCENT RWD, 200 KT S - 47 PERCENT RWD, 180 KTS AND BELOW, NO AILERON TRIM REQUIRED. REFERENCE DAYJET WORK ORDER 1540, NR-00001,2,3. COMPL 1 L 7 2 4J RT A00002AC 2008032000124 20080320 00124 NM 2008 3 20 DL757080331 1 20080205 A 5320 SILL BOEING 757 757232 1384965 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 CORROSION AROUND SEVERAL FASTENER HOLES AT AFT CARGO ENTRY DOOR LOWER SILL UPPER SURFACE. REMOVED CORR IAW SRM 51-10-02 AT AFT CARGO ENTRY DOOR LOWER SILL "T" CHORD. INSTALLED "T" CHORD IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008032000161 20080320 00161 EU 2008 3 20 08FDEA00904 1 20080312 A 5330 A53879301200 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT SIDE FUSELAGE SKIN IS CORRODED AROUND THE WING TO FUSELAGE FAIRING NUT PLATES AT 3 PLACES BETWEEN FRAMES 45 AND 46. REMOVED DOME NUTS AND REPLACED DOME NUTS PER FEDEX A310-200 SRM 51-40-21; PARAGRAPH 6. REMOVED CORROSION PER FEDEX A3 10-200 SRM 51-73-12. CHECKED LIMITS AND FOUND TO BE IN LIMITS PER FEDEX A310-200 SRM 53-15-12; FIG 1; SHEET 4 AND DIAGR AM 101. ORIGINAL MATERIAL .236, MATERIAL REMAINING .205 AT THE FWD SPOT; CENTER SPOT .224 AND THE AFT SPOT .217. MATE RIAL LOSS AT THE FWD SPOT .031; THE CENTER SPOT .012 AND THE AFT SPOT .019. UT GAUGE USED T8225Q. ALODINED; PRIMED AND PAINTED PER FEDEX A310-200 AMM 51-23-10. 2 L 7 2 4F RT A35EU 2008032000170 20080320 00170 NM 2008 3 20 08FDEA00913 1 20080312 A 5311 ACA73511 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 521FE 48478 MAIN DECK LT FRAME AT STA 535 L20 FOUND DENTED. DENTED AREA REPAIRED AS PER DWG SRZ-53- 503. REPAIR CLASSIFIED AS MINO R AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032000171 20080320 00171 NM 2008 3 20 08FDEA00914 1 20080313 A 5330 SKIN BOEING 757 75727B 1384921 NM ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR, SKIN EXTERNAL DOUBLER, STA 1681, STRINGER S-15L TO EVALUATE EXISTING REPAIR. EXISTING REPAIR FOUND N OT IAW SRM APPLICABILITY. SKIN EXTERNAL DOUBLER REPLACED. R & R DOUBLER IAW EA F-5330-117347. REPAIR A CATEGORY B RE PAIR AS DEFINED IN SRM 51-00-06, REQUIRING SUPPLEMENTAL INSPECTION IN ADDITION TO THOSE ALREADY SPECIFIED IN THE MPD. SUPPLEMENTAL INSPECTION ARE TO BEGIN WHEN THE AIRFRAME ACCUMULATES 34,500 FLIGHT CYCLES WITH REPEAT INSPECTIONS EVERY 3,000 FLT CYCLES. THE SKIN PANEL IS TO BE INSPECTED USING LFEC (PER B757 NDT 53-00-06, PART 6) ALONG THE PERIPHERAL FAST ENER ROWS THROUGH THE EXTERNAL DOUBLER. REPAIR IS CLASSIFIED MAJOR AS PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008032000179 20080320 00179 EU 2008 3 20 F3LA200800092 1 20080305 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED FLOOR PANEL 262FF WAS DAMAGED AT ITS AFT, INBOARD CORNER. MAINTENANCE REMOVED AND REPLACED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-42-12-991-003B. FOLLOWING INSTALLATION OF T HE NEW FLOOR PANEL, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032000183 20080320 00183 WP 2008 3 20 UPS08851825 1 20080302 A 5714 STRUCTURE DOUG DC8 DC873F 302199F WP CENTER WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 FH WING CENTER LE HAS LWR ATTACH SCREW HOLE DAMAGED AFT OF SLOT DOOR. REMOVED DAMAGED, FAB AND INSTA LL REPAIR DOUBLER IAW SRM 57-3-1 FIG4, EO DC8-5720-4087 APPD C, 51-1-8. 2 L 7 4 4F RT 4A25 2008032000189 20080320 00189 NM 2008 3 20 UPS08M51802 1 20080218 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 11 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M, BUSHING O.D. .946 BORE I.D. .944 2 L 7 3 4F RT A22WE 2008032000191 20080320 00191 NM 2008 3 20 2008UALA01113 1 20080228 A 2612 355932255 FIRE LOOP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 NACELLE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 NR 1 ENG PYLON DUCT LEAK LOOP TS5260 IS BROKEN. REPLACED LOOP TS5260, REF MM26-18-01. OPS CHECKS NORMAL PER MM 26-18-0 1. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032000193 20080320 00193 NM 2008 3 20 2008UALA01177 1 20080304 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 23 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 FOUND EMERGENCY LT INOP, CEILING ROW 23. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032000195 20080320 00195 NM 2008 3 20 2008UALA01179 1 20080304 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R4 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 FOUND EMERGENCY LT INOP, DR 4R SLIDE ILLUMINATED. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032000196 20080320 00196 NM 2008 3 20 2008UALA01180 1 20080304 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 FOUND WALL EEL INOP, DR5L CROSS AISLE. SECURED LOOSE CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032000197 20080320 00197 NM 2008 3 20 2008UALA01181 1 20080304 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 FOUND WALL EEL INOP, RT SIDE AFT GALLEY. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032000199 20080320 00199 NM 2008 3 20 2008UALA01183 1 20080304 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 37ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 FOUND SEAT EEL INOP, ROW 37ABC. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2008032000202 20080320 00202 NM 2008 3 20 2008UALA01084 1 20080227 A 5210 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 588UA 26717 FOUND DOOR 1R HARD TO ARM. FOUND LANYARD INTERFERENCE. SECURED LANYARD, DOOR OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100007 20080321 00007 EU 2008 3 21 08FDEA00787 1 20080307 A 5720 A57971362000 RUB STRIP AIRBUS 310 A310203 3930313 EU LT WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT WING PANEL NR 587FT IS DELAMINATING. REPAIRED LEFT WING PANEL 587FT BY REMOVING RUB STRIP, FABRICATING A NEW RUB STRI P & BONDING THE NEW ONE ON IAW SRM 57-52-12. 2 L 7 2 4F RT A35EU 2008032100008 20080321 00008 EU 2008 3 21 08FDEA00788 1 20080307 A 5280 A52860010000 PANEL AIRBUS 310 A310203 3930313 EU RT MLG DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT MLG ZONE 742 STRUT DOOR LOWER AFT SECTION HAS A DEEP NICK AND THE EDGE IS CHIPPED AWAY. REMOVED DAMAGE AND REPAIRED IAW SRM 52-81-11 PB 201 & 51-77-11 CHAP 4D. 2 L 7 2 4F RT A35EU 2008022700311 20080227 00311 EA 2008 2 27 SIMA200805704 1 20080223 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA CABIN SMOKE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 520DC 10140 ON FLIGHT 3559, CREW REPORTED WHILE DURING PASSENGER BOARDING, PASSENGERS REPORTED SMOKE IN THE AFT PART OF THE CABIN. CREW DETERMINED THAT THE SMOKE WAS POSSIBLY ELECTRICAL IN NATURE. CREW AND PASSENGERS DEBOARDED SAFELY. AIRCRAFT REMOV ED FROM SERVICE. PERFORMED EXTENSIVE RUNS, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008022700315 20080227 00315 NM 2008 2 27 SWAA080914 1 20080218 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700322 20080227 00322 SO 2008 2 27 SIMA200805702 1 20080225 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 643AE 145200 ON FLIGHT 3801, CREW REPORTED WHILE AT THE GATE APU RUNNING AVIONICS ON A STRONG ELECTRICAL BURNING SMELL OCCURRED FOLLO WED BY EICAS 115 V AC BUS DISCONNECTED. THE AC POWER BUTTON AND STARTED CHECKLIST. SMELL (FUMES) DISAPPEARED SHORTLY T HEREAFTER. AIRCRAFT REMOVED FROM SERVICE. INSPECTED INVERTER AND ELECTRICAL COMPARTMENTS, NO FAULTS OR SMOKE NOTED AND NR 8194; AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022700325 20080227 00325 EA 2008 2 27 MASA200800129 1 20080212 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 514MJ 10116 ASH FLT 7326 IAD-BDL. EMERGENCY CEILING FLOOD LIGHT ROW 16 INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2008022600244 20080226 00244 NM 2008 2 26 AMTA200800034 1 20080125 A 4970 WARNING SYSTEM BOEING 757 75723N 1384973 NM COCKPIT FALSE ACTIVATION A AMTA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 518AT 27974 APU FAULT LIGHT ILLUMINATED AND EICAS APU FUEL VA MESSAGE DISPLAYED. CYCLED APU FUEL VALVE SEVERAL TIMES, STARTED APU, VALVE OPS CHECK NORMAL IAW AMM 28-25-02, NO FAULT LIGHT. (K) 2 L 7 2 4F RT A2NM 2008022600261 20080226 00261 NM 2008 2 26 AMTA200800071 1 20080212 A 5340 FITTING BOEING 737 73783N 13844HI NM BS 727 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 317TZ 28246 AFT CARGO COMPARTMENT (TEE) ON STA 727, FOUND WIGH EXFOLUATION ON CORROSION (BOTH SIDES) INCLUDED ALL RAIL ASSY SUPPORTS ON THIS STA. REPAIRED IAW EA 737530008A0007 AND INSTALLED IAW SRM 51-40-02. ALODINED PRIMED AND PAINTED AREA IAW SRM 5 1-20-01. 2 L 7 2 4F RT A16WE 2008022600272 20080226 00272 EA 2008 2 26 A6WA200840098 1 20080218 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CABIN INOPERATIVE A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 407AW 7424 FLOOR LEVEL EMERGENCY LIGHTING ADJACENT TO ROW 1, ORANGE SEGMENT FWD INOPERATIVE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008022700046 20080227 00046 EA 2008 2 27 COMA0860124 1 20080211 A 2752 853D10020 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 721CA 2346 7259 FLIGHT 5532 - FLAPS FAIL CAUTION MESSAGE AT 0 DEGREES WHEN SELECTING TO 8 DEGREES. EMERGENCY DECLARED, A/C LANDED SAFEL Y. REMOVED AND REPLACED RIGHT O/B FLAP I/B ACTUATOR. 2 L 7 2 4F RT A21EA 2008022700058 20080227 00058 EA 2008 2 27 COMA0860132 1 20080204 A 5730 600103851008 FAIRING CNDAIR CL600 CL6002B19 1900309 EA RT WING CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 34270 7012 RIGHT WING TIP FORWARD FAIRING CHAFED THRU ON BOTTOM AT WS 407. REPLACED RIGHT WINGTIP FORWARD. 2 L 7 2 4F RT A21EA 2008022700065 20080227 00065 WP 2008 2 27 IXXA08SMN029S 1 20080122 A 5320 SPLICE DOUG DC8 DC862F 3021972 WP ZONE 700 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR WHEEL WELL SPLICE CRACKED AT STATION 879.375. REMOVED FASTENERS AS TO PERFORM REPAIR. REMOVED CRACKED SPLICE. FABRICATED NEW SPLICE. CLEANED, TREATED AND PRIMED AREA AND R EPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 53-2-0 FIGURE 8 SHEET 1, 3, 6, SRM 53-1-0 PAGE 1, 51-1-2 0D, SRM 51-1-8B, AND 51-3-1. 2 L 7 4 4F 4A25 2008032500061 20080325 00061 NM 2008 3 25 USAA920080635 1 20080222 A 5312 6516300512 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - CRACKED BULKHEAD WEB, BS 178, RBL 12, WL 234. REPAIRED BULKHEAD WEB, BS 178, RBL 12, W L 234 IAW B737 SRM 53-10-08-2R9. 2 L 7 2 4F RT A16WE 2008032500073 20080325 00073 NM 2008 3 25 DXTA20082934 1 20080312 A 3240 BRAKE GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE MLG WEAK E DXTA O OTHER O OTHER LD LANDING 1 GL 07 703QS 060 BRAKES ARE VERY SOFT AND WONT GRAB ON LANDING ROLLOUT UNTIL ABOUT 30 KNOTS (BOTH CAPTAIN AND PILOT SIDES). BLED BRAKES AFTER INSPECTION FOUND BRAKES WERE WITHIN TOLERANCE. NO AIR NOTED AT THIS TIME. WORK DONE IAW MM 32-40-20. 2 L 7 2 4F 4 F RT A53NM E35NE 2008032500075 20080325 00075 CE 2008 3 25 GLBA20061082 1 20080313 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 303 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 208GL UE208 CRACK ON BELLY SKIN AT FS 303.25 AT BL 29.06. CRACK APPROX 2.250 INCH. MAINT STOP DRILLED AND PATCHED AFFECTED AREA IAW SRM 51-70. DAMAGED AREA APPROX 6.3 BY 4.5. RII INSPCOMPLIED WITH IAW TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2008032500078 20080325 00078 CE 2008 3 25 DXTA20082936 1 20080313 A 2797 CONNECTOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL PITCH FEEL UNSECURE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 960QS 7500160 ON CLIMBOUT, PASSING 4000 FT, RECEIVED PITCH FEEL FAIL AMBER CAS MSG. FOUND PIN *14 & 1 CONNECTOR PQ016 UNLOCKED AND RE CESSED. LOCKED PIN CONNECTOR SYSTEM OPS CHECKS GOOD IN REF FT CES-750-071. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032500100 20080325 00100 EA 2008 3 25 COMA0860178 1 20080316 A 7830 THRUST REVERSER CNDAIR CL600 CL6002B19 1900309 EA RIGHT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 427CA 7460 FLIGHT 5015 - ON CLIMBOUT FROM YYZ PASSING THROUGH 8000 FT, RECEIVED RIGHT REV UNLOCK CAUTION MESSAGE. AIRCRAFT DIVERTE D TO BUF AND LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL 78-30-01. 2 L 7 2 4F RT A21EA 2008032500109 20080325 00109 NM 2008 3 25 HNAA0800105 1 20080318 A 2910 82970009209 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM NR 1 NACELLE CRACKED A HNAA O OTHER K FLUID LOSS CR CRUISE 1 EA 07 941HA 48422 48422 161 EN ROUTE HYDRAULIC QUANTITY DROPPED, QTY REMAINED AT .7 QT. UPON LANDING FOUND LEAK FROM NUMBER ONE NACELLE. CREW DID NOT DECLARE AN EMERGENCY, TRUCKS DID RESPOND. INSTALLED TEMP FLEX LINE FROM NUMBER ONE MLG DOOR SEQUENCE SOLENOID, PORT C2, TO UNION. GROUND RAN, OPS AND LEAK CHECKS GOOD. 2 H 7 2 4T RT A13NM 2008032500117 20080325 00117 CE 2008 3 25 DJFA2008028 1 20080318 A 3020 INLET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE NR 2 ENGINE CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 438LX RK202 DURING A SCHEDULED INSPECTION, MAINT DISCOVERED THE NR 2 ENGINE HEATED INLET CRACKED. MAINTENANCE REPLACED THE INLET. 2 H 7 2 4F 4 F RT A16SW E25EA 2008032500122 20080325 00122 NM 2008 3 25 SWAA081500 1 20080318 A 5311 6546595 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 25L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032500126 20080325 00126 NM 2008 3 25 SWAA081476 1 20080318 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008032500131 20080325 00131 NM 2008 3 25 SWAA081481 1 20080318 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008032500133 20080325 00133 2008 3 25 SWAA081483 4 20080318 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 403WN 29815 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032500135 20080325 00135 CE 2008 3 25 DXTA20082914 1 20080305 A 3260 65430087 UPLOCK SWITCH CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE MLG DAMAGED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 657QS 1882 5605636 AFTER TAKEOFF WHEN GEAR HANDLE PLACED IN UP NOSE WHEEL UNLOCK. RED LIGHT STARTED FLASHING AND THUMPING NOISE CAME FROM N OSE AREA. DURING ARRIVAL INSPECTION. RH MAIN UPLOCK SWITCH WAS FOUND DAMAGED PUT AIRCRAFT ON JACKS. REMOVED AND REPLA CED DAMAGED UPLOCK SWITCH IN ACCORDANCE WITH CE-560XL-MM CHAPTER 32-30-05. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500140 20080325 00140 NM 2008 3 25 SWAA081489 1 20080318 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 881, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032500141 20080325 00141 NM 2008 3 25 SWAA081491 1 20080318 A 5311 6546541 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3L. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2008032500143 20080325 00143 CE 2008 3 25 DXTA20082917 1 20080305 A 3233 99125373 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LT MLG INTERMITTENT E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 606QS 4484 5605338 DURING INITIAL LANDING ATTEMPT, LT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED. PERFORMED GEAR SWING MANY TIMES AND COULD NOT DUPLICATE PROBLEM. REMOVED LT MLG ACTUATOR WHICH INCORPORATES THE DOWN AND LOCK SWITCH AND INSTALLED INSPECTED ACTU ATOR IAW MM 32-30-04. FUNCTIONAL CHECKS AND CLEARANCES PERFORMED GOOD AND NO LEAKS NOTED. RESECURED SAFETY ON BLOWDOWN B OTTLE AS WELL. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500144 20080325 00144 NM 2008 3 25 DXTA20082919 1 20080306 A 2121 031048 COOLING FAN AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE COCKPIT MALFUNCTIONED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 07 277QS 5752 177 UPON LANDING, RED TEMP FOR CAPTIANS MFD DISPLAYED. IN ADDITION A SLIGHT SMELL OF ELECTRICAL SMOKE WAS EVIDENT UPON SHUTD OWN OF AVIONICS. T/S FOUND PILOTS MFD COOLING FAN INOP. REMOVED INOP FAM AND INSTALLED A NEW FAN. OPS CHECK GOOD I/A/ W DA2000 MM 34-001. 2 L 7 2 4F 4 F RT A50NM E44NE 2008032500150 20080325 00150 NM 2008 3 25 SWAA081494 1 20080318 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008032500157 20080325 00157 NM 2008 3 25 SWAA081508 1 20080318 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 632SW 27707 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, STR 26R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008032500162 20080325 00162 NM 2008 3 25 SWAA081517 1 20080318 A 2560 33500003 GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 763SW 27877 DURING SCHEDULED 8Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008032500165 20080325 00165 NM 2008 3 25 SWAA081516 1 20080318 A 2560 33500003 GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 763SW 27877 DURING SCHEDULED 8Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008032500170 20080325 00170 CE 2008 3 25 DXTA20082924 1 20080308 A 2750 CONTROLLER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS FAILED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 978QS 7500187 UPON SELECTING FLAPS FOR 15 DEGREES FROM35 DEGREES FLAPS FAILED AT APPROX 17 DEGREES. T/S. FOUND FLAPS AT FULL UP UPON ARRIVAL AT AIRCRAFT. FOUND BITE 2 ON FLAP CONTROLLER. RAN FLAPS THROUGH NO DEFECTS. RESET FLAPS AND RAN SOME MORE. NO BI TE CODES PRESENT. PERFORMED BITE 2 TROUBLESHOOTING OER MX MANUAL NO DEFECTS NOTED. SYSTEM OPS CHECKS GOOD PER CE750 M/M 27-50-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032500172 20080325 00172 SO 2008 3 25 FDKA200803110 1 20080315 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM 6173 BNA-MCO (0503 PHX LCL), ROW 12 EMERGENCY SIDEWALL LIGHT INOP. MX RESECURED CONNECTORS, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008032500175 20080325 00175 SO 2008 3 25 FDKA200803113 1 20080316 A 3350 20131ASMI BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 8899 145217 FDM 5970 JFK (1556 PHX LCL), LEFT EMERGENCY LIGHT INOP AT ROW 12. MX REMOVED AND REPLACED BATTERY PACK, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008032500179 20080325 00179 2008 3 25 VNAA0803004 4 20080307 A 3417 8220372445 ADC CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 2 FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 248PS 9171 7925 CREW REPORTED 20 KNOT INDICATED AIRSPEED SPLIT BETWEEN CAPTAINS AND FIRST OFFICERS. CREW ABORTED TAKEOFF AND RETURNED T O THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE CAPTAINS AND STANDBY TO AGREE BUT THE FIRST OFFICERS T O BE 20 KNOTS SLOW. MAINTENANCE REMOVED AND REPLACED THE NR 2 AIR DATA COMPUTER IN ACCORDANCE WITH THE AIRCRAFT MAINTEN ANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008032500180 20080325 00180 EA 2008 3 25 VNAA0803005 1 20080310 A 2740 TRIM SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE MALFUNCTIONED A VNAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 05 206PS 7860 CREW REPORTED THE STAB TRIM & MACH TRIM WILL NOT ENGAGE ON CLIMBOUT. CREW ELECTED TO RETURN TO LEX AND LANDED WITHOUT I NCIDENT. MAINTENANCE CYCLED THE HSTCU CIRCUIT BREAKERS, PERFORMED A MEMORY RESET AND PERFORMED AN OPS CHECK IN ACCORDAN CE WITH THE AIRCRAFT MAINTENANCE MANUAL. BITE AND OPS CHECKS BOTH WERE GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SE RVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008032500183 20080325 00183 CE 2008 3 25 DXTA20082927 1 20080309 A 4900 99124841 APU CESSNA 560 560XL 2076702 CE APU BAY SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 611QS 1949 5605548 APU RUNNING, WITH BLEED ON AND ENGINES RUNNING, SMOKE ENTERED THE CABIN. REMOVED AND REPLACED APU. SERVICED OIL TO FULL . OPERATIONAL AND LEAK CHECK GOOD. WORK PERFORMED IAW MM 49-10-00. 2 L 7 2 4F RT A22CE 2008032500188 20080325 00188 CE 2008 3 25 DXTA20082931 1 20080312 A 2841 99124987 SIGNAL COND UNIT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE FUEL QTY IND INACCURATE E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 676QS 422 422 5605176 DURING TAKEOFF ROLL BELOW 70 KNOTS, (LT FUEL GAGE) AND MASTER CAUTION LIGHTS CAME ON. REPLACED FUEL QUANTITY SIGNAL CON DITIONER IAW MM CHAPTER 28-41-00. PERFORMED FUEL SYSTEM ADJUSTMENT AND TEST IAW MM CHAPTER 28-41-00. TEST GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500195 20080325 00195 NM 2008 3 25 2008UALA01396 1 20080312 A 4930 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU APU ODOR A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 313UA 23674 FUEL SMELL W-APU IN USE SMOKE ALSO NOTED AT TAIL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500202 20080325 00202 2008 3 25 2008UALA01437 4 20080313 A 2565 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 537UA 25157 LOW BOTTLE PRESSURE. *S/D* UNDER FILL AT TIME OF INSTALLATION. TECHNICIAN RETRAINED AND BOTTLE SERVICED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500212 20080325 00212 NM 2008 3 25 2008UALA01448 1 20080315 A 5320 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 808UA 804 BEAM 175 IS CORRODED. CORROSION REMOVED WITH LIGHT BURNISHING. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500213 20080325 00213 NM 2008 3 25 2008UALA01449 1 20080315 A 5320 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 808UA 804 BEAM 185 FRD HAS 1 CLIP NUT HOLE WITH CORROSION. CORROSION REMOVED WITH LIGHT BURNISHING. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500221 20080325 00221 NM 2008 3 25 2008UALA01458 1 20080314 A 2612 TEST UNIT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE WARNING INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 302UA 23643 FIRE TEST INOPERATIVE. REPLACED MODULE ASSEMBLY FIRE TEST OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500222 20080325 00222 EU 2008 3 25 2008UALA01459 1 20080316 A 2121 VD390003 FAN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MALFUNCTIONED A UALA A UNSCHED LANDING W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 428UA 523 DIVERTED DUE TO BURNING-ACRID SMELL IN AFT CABIN. BURNT BEARING IN LT RECIRC FAN. REPLACED LT RECIRC FAN, ALL TESTS WE RE NORMAL, NO SMELL NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500225 20080325 00225 EU 2008 3 25 2008UALA01462 1 20080316 A 2611 RAI2800M0706 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SMOKE DETECTION FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 473UA 1469 LAVATORY AND CARGO DETECTOR FAULT DISPLAYED ON UPPER ECAM SCREEN - SMOKE. SDCU FAILURE. REPLACED THE SDCU, ALL OPS CHE CKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500226 20080325 00226 NM 2008 3 25 2008UALA01507 1 20080318 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT EEL INOP AT SEAT 7GH. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032500231 20080325 00231 NM 2008 3 25 2008UALA01512 1 20080317 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 AFT PIT FS 1520 STR 26L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED & INSTALLED FRAME REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500233 20080325 00233 NM 2008 3 25 2008UALA01514 1 20080317 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 AFT PIT FS 1420 FRAME DENTED STR 26L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED & INSTALLED FRAME REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500235 20080325 00235 NM 2008 3 25 2008UALA01534 1 20080317 A 2421 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT IDG DRIVE INOPERATIVE A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 661UA 27158 RIGHT IDG DRIVE LIGHT INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032500236 20080325 00236 NM 2008 3 25 2008UALA01588 1 20080319 A 3350 582233 BATTERY BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 671UA 30026 EMERGENCY EXIT PATH LIGHTING FLASHING ON & OFF INTERMITTENTLY. FOUND BATTERY DEAD IN FIRST CLASS. REPLACED BATTERY, OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032500246 20080325 00246 NM 2008 3 25 2008UALA01596 1 20080321 A 5312 STRUCTURE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BULKHEAD CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 180UA 25224 BS 2598 BULKHEAD RT AFT INNER CHORD 30MM CRACK. REPAIRED PER SRM 53-80-08 REPAIR 11. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032500248 20080325 00248 NM 2008 3 25 2008UALA01598 1 20080320 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 BS 747 STR 25L, STRINGER CLIP CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500249 20080325 00249 NM 2008 3 25 2008UALA01599 1 20080320 A 5230 TEE FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 AFT CARGO DOOR S/N 1664 LOWER T-CHORD CRACKED AT AFT CORNER. MAJOR REPAIR ACCOMPLISHED: REPLACED T-CHORD. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500250 20080325 00250 NM 2008 3 25 2008UALA01600 1 20080320 A 5230 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 AFT CARGO DOOR S/N 1664 EXTERNAL SKIN DENTED 10 INCHES FROM TOP AND 11 INCHES FROM FWD SIDE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE & INSTALLED A DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500251 20080325 00251 NM 2008 3 25 2008UALA01601 1 20080320 A 5230 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 AFT CARGO DOOR LWR AFT FRAME WEB CRACKED AT INBOARD FASTENER HOLE ABOVE LWR STOP PIN FITTING. MAJOR REPAIR ACCOMPLISHED : REMOVED DAMAGE & INSTALLED A DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500259 20080325 00259 EU 2008 3 25 2008UALA01608 1 20080320 A 3350 BR964421 LAMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 416UA 479 SEAT MOUNTED AISLE EMERGENCY FLOOD LIGHT AT SEAT 22C INOP. LAMP INOP. RELAMPED, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500261 20080325 00261 NM 2008 3 25 2008UALA01610 1 20080320 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 SEAT 5E AFT EMERGENCY EVACUATION LIGHT INOP. REPLACED LIGHT ASSY, OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032500262 20080325 00262 NM 2008 3 25 2008UALA01611 1 20080320 A 2560 KNOB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 EMERGENCY EVACUATION PANEL HAS MISSING HORN SHUTOFF KNOB MISSING IN FLIGHT DECK COMPARTMENT. REPLACED EES PANEL, OPS CH ECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032400296 20080324 00296 WP 2008 3 24 NWAA080969606 1 20080314 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 606NW 47225 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WERE IN OPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK IN THE AFT ACCESSORY COMPARTMENT. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2008032100011 20080321 00011 NM 2008 3 21 2008UALA01197 1 20080305 A 2916 RESERVOIR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYD SYSTEM LOW A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 545UA 25323 'CTR SYST RSVR' EICAS MSG DISPLAYED, QTY RDG .38. DEPARTED WITH CTR QTY AT .95. SELECTED PUMPS AND QTY CAME BACK UP A LITTLE TO .53. SERVICED CENTER HYD RES TO FULL. RAN ALL COMPONENTS ON CENTER SYSTEM FOR MORE THAN 1 HOUR NO FLUID LOSS N OTED. NO HISTORY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100012 20080321 00012 NM 2008 3 21 2008UALA01198 1 20080304 A 5310 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1600 S27-28L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 FOUND DENT AT STATION 1600 BETWEEN STR 27 AND 28 LEFT. FOUND DENT TO HAVE A CRACK. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100013 20080321 00013 NM 2008 3 21 2008UALA01199 1 20080304 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 R2 DOOR UPPER HINGE ARM CUTOUT IS DAMAGED. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100014 20080321 00014 NM 2008 3 21 2008UALA01200 1 20080304 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1648-1681 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 MAIN CABIN FLOOR SUPPORT AT STA 1648 TO 1681, RBL 54 HAS CORROSION. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100015 20080321 00015 NM 2008 3 21 2008UALA01201 1 20080304 A 5340 FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1720 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 MAIN CABIN RT SIDE BS 1720 BULKHEAD FITTING CORRODED AT RBL 47. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100029 20080321 00029 CE 2008 3 21 DXTA20082920 1 20080308 A 3240 BRAKE CESSNA 560 560XL 2076702 CE PWC PW306 PW306C 52169 NE RIGHT CONTAMINATED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 670QS 5605170 PILOT'S RT BRAKE PEDAL VERY SOFT GOES ALMOST TO STOP. FOUND AIR IN SYSTEM, BLED BRAKES AS REQUIRED PER CESSNA 560XL M/M 32-42-00 FUNCTION CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E35NE 2008032100030 20080321 00030 2008 3 21 DXTA20082921 4 20080308 A 2210 54019760 POTENTIOMETER RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP TE FLAPS OUT OF TOLERANCE E DXTA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 07 836QS 6684 258436 WHILE ENROUTE FD WAS PITCHING UP AND DOWN CAUSING PLANE TO PORPISE. ALTITUDE VARIED BY AS MUCH AS +-150 FEET. TROUBLESHO T PROBLEM TO FLAP/FLIGHT DIRECTOR BIASING POTENTIOMETER. REMOVED RT. WING ACCESS PANEL TO REMOVE POTENTIOMETER. REMOVED OLD UNIT AND INSTALLED NEW UNIT. INSTALLED AND ADJUSTED IAW HAWKER 800XP MAINTENANCE MANUAL CHAPTER 34-22-60-501. FLIGHT DIRECTOR COMMAND BARS OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A3EU E6WE 2008032100031 20080321 00031 CE 2008 3 21 DXTA20082922 1 20080307 A 3240 BRAKE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE RT MLG CONTAMINATED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 670QS 5605170 PILOTS RT BRAKE PEDAL GOES TO THE STOP WITH LITTLE OR NO RESISTANCE. FOUND AIR IN SYSTEM, BLED BRAKES AS REQUIRED PER MM 32-42-00 FUNCTION CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032100032 20080321 00032 NM 2008 3 21 2008UALA01252 1 20080306 A 2611 332N35002 FIRE LOOP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 NACELLE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 IN BULLNOSE AREA OF PYLON NR 1, FIRE LOOP 'B ' CONNECTOR D1950 IS BROKEN AND NEEDS TO BE REPLACED. FOUND DAMAGED FIRE LO OP (BROKEN) -UNKNOWN REASONS. REMOVED AND REPLACED FIRE LOOP A, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100033 20080321 00033 NM 2008 3 21 2008UALA01253 1 20080306 A 2611 332N35002 FIRE LOOP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 NACELLE BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 531UA 25042 IN BULL NOSE AREA OF PYLON NR 1, FIRE LOOP ' A' ON BULL NOSE PANEL BROKEN. FOUND FIRE LOOP BROKEN. REMOVED AND REPLAC ED FIRE LOOP A, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100035 20080321 00035 NM 2008 3 21 2008UALA01255 1 20080307 A 3350 3016691 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 583UA 26705 NR 1 DOOR OUTSIDE EEL LIGHT INOP. FOUND LAMP BURNT OUT. RELAMPED BULB, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100037 20080321 00037 NM 2008 3 21 2008UALA01263 1 20080306 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 588UA 26717 R3 DOOR WILL NOT ARM. FOUND DEBRIS UNDER GIRT BAR AREA. CLEANED DEBRIS FROM UNDER DOOR R3 AND MOVED LANYARD (POSSIBLE INTERFERENCE), ALL DOORS ARM/DISARM NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100038 20080321 00038 NM 2008 3 21 2008UALA01264 1 20080307 A 3350 362624 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 583UA 26705 NR 1 RIGHT OUTSIDE EEL LIGHT INOP. FOUND BULB BURNED OUT. RELAMPED EEL LIGHT, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100039 20080321 00039 CE 2008 3 21 GLBA20061081 1 20080306 A 5711 SPAR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT WING CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 153GL UE153 DURING STRUCTURAL INSP MAINT FOUND CORROSION ON THE RT WING SPAR AT APPROX WS 126.5. MAINTENANCE REMOVED CORROSION AND INSTALLED REINFORCEMENT STRAP PER E.O. 08-UE153-02. REAPAIR APPROXIMATELY 14" . .190 7075-T73. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2008032400297 20080324 00297 EU 2008 3 24 NWAA080993308 1 20080314 A 3240 BRAKE ASSY AIRBUS 330 A330323 3930335 EU MLG FIRE A NWAA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 GL 01 808NW 0591 DURING AIRCRAFT ARRIVAL AT GATE, SMALL FLAMES WERE COMING FROM BRAKE POSITION NR 8. NO "ECAM" WARNING OR MESSAGES, NO E XCESSIVE BRAKE TEMPERATURE "(415 DEG C.)", FLIGHT CREW DID NOT REPORT ANY DISCREPANCIES. CARGO LOADERS CALLED CFR, FLAM ES EXTINGUISHED BY ITSELF. WHEEL AND BRAKE INSPECTED AND FOUND FREE ROTATION AND NO HYDRAULIC LEAKS, CHECKED AXLE SLEEV E TO HAVE NO DAMAGE. FOUND A LOT OF GREASE ON THE OUTSIDE OF INNER WHEEL BEARING AND INNER WHEEL RIM HALF. CLEANED AND REMOVED EXCESSIVE GREASE AND CHECKED BEARINGS AND REINSTALLED WHEEL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A46NM 2008032400298 20080324 00298 WP 2008 3 24 NWAA080979921 1 20080314 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 943N 47647 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INO PERATIVE. MAINTENANCE REPLACED THE BATTERIES AT B27 POWER UNIT AND AT THE TAIL COMPARTMENT POWER SUPPLY. OPERATIONAL C HECK WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2008032400299 20080324 00299 EU 2008 3 24 NWAA081003226 1 20080316 A 2910 MANIFOLD AIRBUS 320 A320211 3930320 EU HYD SYSTEM LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 326US 282 SHORTLY AFTER TAKEOFF THE HYD G RSVR LO LVL FAULT ANNUNCIATED. AIRCRAFT RETURNED TO MEM, LANDING GEAR GRAVITY EXTENDED. AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWED TO GATE. REPLACED GREEN GROUND LEAK MEASUREMENT MANIFOLD AND NR 1 ENGINE D RIVEN GREEN PUMP. 2 L 7 2 4F RT A28NM 2008032400323 20080324 00323 NM 2008 3 24 2008UALA01374 1 20080312 A 5753 SUPPORT FITTING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE T/E FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 NR 2 FLAP SUPPORT FITTING 2V JOINT OUTBOARD END BUSHING BORE IS WORN. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032400348 20080324 00348 NM 2008 3 24 2008UALA01387 1 20080313 A 3350 209 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 RIGHT NR 4 DOOR EMERGENCY LIGHT INOP (DOOR MOUNT LIGHT). REPLACED LAMP OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032400366 20080324 00366 2008 3 24 SWAA081415 4 20080316 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032400389 20080324 00389 NM 2008 3 24 SWAA081433 1 20080317 A 5743 6537877 FITTING BOEING 737 7373H4 1384600 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED MV2 CHECK, FOUND RIGHT MLG WALKING BEAM FWD OUTBOARD FITTING CORRODED. REMOVED AND REPLACED FITTING PE R MM. 2 L 7 2 4F RT A16WE 2008032400397 20080324 00397 NM 2008 3 24 SWAA081440 1 20080316 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008032400409 20080324 00409 NM 2008 3 24 SWAA081446 1 20080314 A 5330 6545767 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED PM CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 427, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032400423 20080324 00423 NM 2008 3 24 SWAA081451 1 20080317 A 5330 6545766 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 512D, STR 26R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032500021 20080325 00021 CE 2008 3 25 DXTA20082899 1 20080225 A 2711 4214002111N CONTROL MODULE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TRIM SYSTEM MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 975QS 6138 7500175 AFTER 15 MINS OF CRUISE FLT AT FL400 (MACH TRIM OFF) AND (PRI STAB TRIM FAIL) MESSAGE KEPT DISPLAYING AND RESETTING. RE MOVED DEFECTIVE ECM P/N 4214-0021-11N S/N 3125, INSTALLED UNIT MODIFIED BY MFG SERVICE, IAW MM CHAP 72-40-00. OPERATIONA L CHECKS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032500024 20080325 00024 CE 2008 3 25 DXTA20082901 1 20080226 A 3233 99125373 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LT MLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 644QS 2563 5605582 SELECTED GEAR DOWN LT MAIN NO GREEN ANNUNCIATOR AND RED UNLOCK ANNUNCIATOR ON. REMOVED ACTUATOR P/N 9912537-3 S/N 0760. CLEANED AND INSPECTED GEAR ASSY. INSTALLED REPAIRED ACTUATOR P/N 9912537-3 S/N 0441. RESERVICED N2. CHECKED CAMBER, OPS CK OF GEAR GOOD. ALL IAW MM 32-30-04, 32-10-00. 12-13-01. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500040 20080325 00040 NM 2008 3 25 USAA920080581 1 20080218 A 5320 69353652 INTERCOSTAL BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - CRACKED INTERCOSTAL WEB, BS 380, BL 0, WL 208. REPLACED INTERCOSTAL WEB, BS 380, BL 0, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008032500069 20080325 00069 NM 2008 3 25 USAA920080640 1 20080309 A 5320 6545834525 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED INTERCOSTAL, BS 344, BL 0, WL 208. REPLACED INTERCOSTAL, BS 344, BL 0, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008032500071 20080325 00071 NM 2008 3 25 USAA920080641 1 20080314 A 5315 654583469 STRAP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FLOORBEAM STABILIZATION STRAP, BS 344, RBL 33. REPAIRED FLOORBEAM STABILIZATIO N STRAP, BS 344, RBL 33 IAW B737 SRM 53-10-51-2R4. 2 L 7 2 4F RT A16WE 2008032500095 20080325 00095 EA 2008 3 25 COMA0860176 1 20080314 A 3230 UPLOCK CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF RIG A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 710CA 7241 FLIGHT 5653 - GEAR DISAGREE MESSAGE ON APPROACH INTO MCI. AIRCRAFT LANDED SAFELY. FOUND NLG UPLOCK PIN OUT OF RIG. PE RFORMED RIGGING OF NLG UPLOCK PIN, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008032500098 20080325 00098 EA 2008 3 25 COMA0860177 1 20080314 A 2613 356124310 SENSING ELEMENT CNDAIR CL600 CL6002B19 1900309 EA OVERHEAT WARNING FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 477CA 7670 FLIGHT 5664 - RECEIVED LEFT ANTI-ICE DUCT WARNING MESSAGE ON CLIMBOUT FROM CVG. AIRCRAFT RETURNED TO CVG AND LANDED SAF ELY. REMOVED AND REPLACED AFT BAY HEAT SENSING ELEMENT (A47WK). 2 L 7 2 4F RT A21EA 2008032500119 20080325 00119 CE 2008 3 25 DJFA2008029 1 20080319 A 3020 45A35042003 INLET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE NR2 ENGINE CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 745TA RK145 DURING A SCHEDULED INSP, MAINT DISCOVERED THE NR 2 ENGINE HEATED INLET CRACKED AT THE 4 O'CLOCK POSITION. MAINT REMOVED AND REPLACED THE INLET. 2 H 7 2 4F 4 F RT A16SW E25EA 2008032500136 20080325 00136 NM 2008 3 25 SWAA081488 1 20080318 A 5330 6545800 BEAR STRAP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032500142 20080325 00142 NM 2008 3 25 SWAA081501 1 20080318 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482A, STR 27L TO STR 28L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008032500153 20080325 00153 NM 2008 3 25 SWAA081505 1 20080318 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008032500154 20080325 00154 NM 2008 3 25 SWAA081506 1 20080318 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008032500160 20080325 00160 NM 2008 3 25 SWAA081511 1 20080318 A 5743 115A5211 FITTING BOEING 737 7377H4 1384404 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 741SA 29277 DURING SCHEDULED MV2 CHECK, FOUND LEFT MLG FWD TRUNNION FITTING LUG FACE CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008032500161 20080325 00161 NM 2008 3 25 SWAA081510 1 20080318 A 5743 115A5211 FITTING BOEING 737 7377H4 1384404 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 741SA 29277 DURING SCHEDULED MV2 CHECK, FOUND RIGHT MLG FWD TRUNNION FITTING LUG FACE CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008032500174 20080325 00174 SO 2008 3 25 FDKA200803112 1 20080316 A 5610 WINDOW EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 829MJ 145228 FDM 6157 NAS-MCO (0916 PHX LCL), CAPTAIN WINDOW WILL NOT CLOSE. MX RE-INSTALLED WINDOW, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008032500182 20080325 00182 EA 2008 3 25 VNAA0803007 1 20080315 A 5350 RADOME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE DAMAGED A VNAA O OTHER O OTHER AP APPROACH 1 GL 05 206PS 7860 CREW REPORTED ON APPROACH A LIGHTNING STRIKE TO THE NOSE AREA. MAINTENANCE PERFORMED A VISUAL EN ROUTE AND A DETAILED L IGHTNING STRIKE INSPECTION. MAINTENANCE FOUND DAMAGE TO THE RADOME AND OTHER AREAS. MAINTENANCE REPAIRED ALL DAMAGE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE . 2 L 7 2 4F 4 F RT A21EA E15NE 2008032500193 20080325 00193 NM 2008 3 25 2008UALA01000 1 20080222 A 2700 4885501002 CONTROL BOX BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FLIGHT CONTROL FAULTY A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 792UA 26934 FLIGHT CONTROL SYSTEM MESSAGE OCCURRED IN FLIGHT. PERFORMED EXTENSIVE TROUBLESHOOTING, & CHRONIC SYSTEM REVIEW. MANY U NITS PREVIOUSLY REPLACED BUT PROB NOT ENTIRELY CORRECTED. REPLACED POWER SUPPLY ASSY & ACE L-1 A SECOND TIME. ALL TEST S PERFORMED WITH GOOD RESULTS, A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500206 20080325 00206 NM 2008 3 25 2008UALA01442 1 20080315 A 5320 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 808UA 804 BEAM 195 HAS SEVERAL CLIP NUT AND NUT PLATE HOLES WITH CORROSION. MAJOR REPAIR ACCOMPLISHED AT DEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500232 20080325 00232 NM 2008 3 25 2008UALA01513 1 20080317 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 AFT PIT FS 1500 STR 26L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED FRAME REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500239 20080325 00239 NM 2008 3 25 2008UALA01589 1 20080319 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 780UA 26944 SEAT 1F AFT EEL LIGHT IS MISSING. REPLACED MISSING EEL LIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500240 20080325 00240 NM 2008 3 25 2008UALA01590 1 20080319 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 768UA 26919 EEL LIGHT INOP 2F AFT POSITION. REPLACED EEL LIGHT IN SEAT 2F AFT POSITION. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500241 20080325 00241 NM 2008 3 25 2008UALA01591 1 20080320 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 788UA 26942 DOOR 3L THRESHOLD LIGHT IS INOP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500260 20080325 00260 EU 2008 3 25 2008UALA01609 1 20080320 A 7830 THRUST REVERSER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 449UA 851 NR 1 ENGINE LT REVERSER DAMAGED. UNKNOWN A/C DAMAGE. PERFORMED PERMANENT REPAIR ON REVERSER HALF (COMPOSITE). 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500264 20080325 00264 NM 2008 3 25 2008UALA01613 1 20080320 A 2560 BUTTON BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 OVERHEAD PANEL EVAC HORN SHUTOFF BUTTON MISSING. REPLACED EMER EVAC PANEL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500269 20080325 00269 NM 2008 3 25 2008UALA01618 1 20080321 A 2560 284N10079 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 537UA 25157 GIRT-BAR ARM LT C/B TRIPPING, UNABLE TO ISOLATE FAULT. FOUND PROX SWITCH SW10216 FAILED. REPLACED PROX SWITCH SW10216. GIRT BAR LIGHT WORKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500270 20080325 00270 NM 2008 3 25 2008UALA01537 1 20080316 A 2421 GENERATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RIGHT FAILED A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 771UA 26932 RIGHT GENERATOR FAILED DURING CRUISE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500272 20080325 00272 2008 3 25 2008UALA01535 4 20080314 A 2565 SLIDE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RT WING FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 672UA 30027 CABIN RT WING SLIDE ASSY IMPROPERLY PACKED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032500273 20080325 00273 NM 2008 3 25 2008UALA01526 1 20080318 A 5320 CHANNEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 SPLICE CHANNEL IS CRACKED ON FWD SIDE OF THE FRAME BS 360 AT STR 14L. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500275 20080325 00275 NM 2008 3 25 2008UALA01524 1 20080318 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 310 S13L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FORWARD ENTRY DOOR LOWER HINGE CUTOUT HAS 2 EA CRACKS IN FASTENER HOLES AT BS 310 AND STRINGER S-13L. MAJOR REPAIR ACCO MPLISHED BY REMOVING DAMAGE AND INSTALLING STRUCTURAL FILLER AND REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500283 20080325 00283 NM 2008 3 25 2008UALA01515 1 20080317 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 AFT PIT FS 1460 STR 26L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED & INSTALLED FRAME REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500286 20080325 00286 NM 2008 3 25 2008UALA01472 1 20080315 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 CABIN FLOORBEAM UPPER SURFACE CORRODED AT BS 947, RBL 29"-48". MAJOR REPAIR ACCOMPLISHED: INSTALLED MAIN DECK FLOORBEA M UPPER CAP REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500288 20080325 00288 2008 3 25 2008UALA01470 4 20080315 A 2564 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LIFE RAFT OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 597UA 28750 DOOR 1R WILL NOT ARM. INTERFERENCE FROM RAFT LANYARD. CLEARED AND STOWED PROPERLY, DOOR ARMS/DISARMS PROPERLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500290 20080325 00290 2008 3 25 2008UALA01468 4 20080316 A 2397 WIRE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU O2 MASK FRAYED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 930UA 26655 F/O O2 MASK MIC INOP. WIRE IS VISIBLY FRAYED. REPLACED MASK OPS CK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500293 20080325 00293 NM 2008 3 25 2008UALA01465 1 20080316 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 BS 294.5 STRINGER CLIP CRACKED AT STRINGER S-7L. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED CRACKED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032100051 20080321 00051 NM 2008 3 21 08FDEA00870 1 20080311 A 2131 CONTROLLER BOEING 727 727233 138408A NM CABIN PRESSURE UNKNOWN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 276FE 22041 CLIMBING OUT OF LAX, PRESSURE CONTROLLER INDICATED -100 FPM (DESCENT) UNTIL 8000'MSL. F/O COMPLAINED OF PAIN IN EARS/TEE TH ALMOST IMMEDIATELY. CAPTS EARS ALSO PAINFUL. AT 8000' CABIN BEGAN TO CLIMB PASSING 12000, F/O STILL UNCOMFORTABLE. DI RECTED S/O TO SWITCH TO "STANDBY" A/C CONTINUED AS BEFORE. F/O CONTINUE TO HAVE PROBLEMS, SO WE WENT ON O2. DECLARED AN D EMERGENCY AND LANDED AT PHX. AMM PRESSURE CONTROLLER AND INDICATOR CHECKED NORMAL. RECOMMEND REPLACING RATE OF CLIMB, CABIN ALT INDICATOR, PRESSURE CONTROLLER AS A PRECAUTION. R & R CABIN PRESSURE CONTROLLER PER MM. R & R CABIN PRESSUR E CONTROL PANEL AND ALTITUDE DIFFERENTIAL PRESSURE INDICATOR PER MM. PANEL CHECKS OK NEED TO CHECK INDICATOR WHEN A/C 2 L 7 3 4F RT A3WE 2008032100052 20080321 00052 WP 2008 3 21 08FDEA00873 1 20080311 A 5322 ADA0010 SHEAR TIE DOUG MD10 MD1010F 3022112 WP FUELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 FWD LOWER CARGO PIT BILGE SHEAR TIE IS CORRODED AT BS 824 BETWEEN STR 51R AND STR 52R. REMOVED CORROSION IAW SRM 51-21- 01; VOL II; PG 28. ORIGINAL THICKNESS .071 IAW SRM 53-13-01; VOL III; FIG 8A AND SRM 51-10-02; VOL II. REMAINING THICK NESS .068; FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01; FIG 1A; PG 4B. UT GAUGE NR T8224Q. ALODINED AND PRIMED IN REF T O SRM 51-21-01; VOL II; PG'S 21 AND 24. APPLIED TOPCOAT IAW SRM 51-21-02; VOL II; PG 1. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008032100055 20080321 00055 WP 2008 3 21 08FDEA00876 1 20080311 A 5320 ACA72281 SILL DOUG MD10 MD1010F 3022112 WP BS 715 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 CARGO DOOR CUT-OUT LOWER JAMB INBOARD ANGLE AT NR 5 LATCH SPOOL AREA HAS 2 GOUGES; .065 AND .085. CLEANED UP GOUGES ARE A IN REF TO SRM 53-00-01; VOL I; FIG 1A WITHIN LIMITS; MAINTAINED 2D EDGE DISTANCE IN REF TO SRM 53-00-01;VOL I; FIG 1A . ALODINED AND PRIMED AREA IN REF TO SRM 51-21-01; VOL II; PGS 21 AND 25. 2 L 7 3 4F RT A22WE 2008032100056 20080321 00056 WP 2008 3 21 08FDEA00878 1 20080311 A 5320 ADA0145 SUPPORT DOUG MD10 MD1010F 3022112 WP BS 959 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 FWD CARGO PIT BILGE AREA; DRAIN PAN SUPPORT LOWER SURFACE AND NUT PLATES HAVE CORROSION ABOVE FRAME FS 959 FROM S49-51R. REMOVED CORROSION IAW SRM 51-21-01; VOL II; PG 28. THE ORIGINAL THICKNESS IS .040 IAW DWG ADA0145 REV J. THE MATERI AL REMOVED IS .002; MATERIAL REMAINING IS .038. FOUND TO BE IN LIMITS IAW SRM 53-00-01; VOL II; FIG 1B. TREAT AND PR IMED IAW SRM 51-21-01; VOL II; PGS 21 AND 24; THEN INSTALLED NUT PLATES IAW SRM 51-35-01; VOL II PG 2. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008032100060 20080321 00060 NM 2008 3 21 08FDEA00897 1 20080311 A 5320 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 MAIN DECK, CARGO DOOR LOWER JAMB WHILE CARRYING OUT HFEC ON NR 3 SPOOL BRACKET BOLT BORE, FOUND ON 1 CRACK ON SUPPORT FI TTING BORE HOLE "A". REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032100064 20080321 00064 NM 2008 3 21 2008UALA01286 1 20080310 A 2750 FLAP SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAPS MALFUNCTIONED A UALA L ABORTED APPROACH O OTHER AP APPROACH 1 WP 29 564UA 26666 TRAILING EDGE FLAP DISAGREE BETWEEN 25 AND 30. PERFORMED SEVERAL FLAP DEPLOYMENTS, NO DISAGREE NOTED AT ANY SETTING OR B ETWEEN SETTINGS, UNABLE TO DUPLICATE ON GROUND, NO HISTORY OR REPEATS SINCE ORIGINAL WRITE UP. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100070 20080321 00070 NM 2008 3 21 2008UALA01329 1 20080310 A 3230 LANDING GEAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MALFUNCTIONED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 589UA 28707 UPON T/O, GEAR DISAGREE AND GEAR DOOR DISPLAYED FOR A SHORT PERIOD TIME DURING GEAR RETRACTION. AFTER A SHORT PERIOD TI ME ALL MSG'S CLEARED. JACKED A/C AND SWUNG GEAR, ALL CHECKED NORMALLY. LUBED NOSE GEAR ASSY, SWUNG GEAR SEVERAL TIMES WITH NORMAL SWING TIMES. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100072 20080321 00072 NM 2008 3 21 2008UALA01334 1 20080310 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 DOOR 2R UPPER HINGE CUTOUT REQUIRES DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031900320 20080319 00320 NM 2008 3 19 SA08012 1 20080312 A 3397 WIRE AIRBUS A319 A319132 3930340 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 829AW 1563 LAS - THE ROW ONE LEFT SEAT MOUNTED EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE CRIMPED AND SECURED WIRE A BROKE N WIRE AT THE EMERGENCY LIGHT CONNECTOR. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2008031900324 20080319 00324 NM 2008 3 19 USAA920080600 1 20080305 A 5315 D53472190203 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801AW 889 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 2670 / FR 64 - BS 2786 / FR 66, -Y765. REPLACED CABIN FLOORBEAM, BS 2670 / FR 64 - BS 2786 / FR 66, -Y765 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900325 20080319 00325 NM 2008 3 19 USAA920080601 1 20080305 A 5315 D53472190205 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801AW 889 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 2786 / FR 66, -Y1292. REPLACED CABIN FLOORBEAM, BS 267 0 / FR 64 - BS 2786 / FR 66, -Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008031900386 20080319 00386 GL 2008 3 19 C2XA08IA079 2 20080310 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 LEAKING A C2XA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 13978 16398 16398 145180 CAE311743 IAH - FLIGHT 2156 - AFTER TAKEOFF THE LAVATORY SMOKE INDICATOR WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. UPON INSPECTION THE NR 2 ENGINE WAS FOUND TO BE THE SOURCE OF THE SMOKE. MAINTENANCE REMO VED AND REPLACED THE NR 2 ENGINE, PERFORMED GROUND RUNS AND CLEARED THE DISCREPANCY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008031900400 20080319 00400 NM 2008 3 19 USAA920080629 1 20080315 A 3397 WIRE BOEING 737 7373G7 1384595 NM CABIN SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 157AW 23779 FLT 391 - LAS - MX REPORTED EMERGENCY LIGHTS ROW 5-10 INOP. MX DISCOVERED LAMP PINS AT ROW 10 GROUNDED OUT. MX REPAIRE D WIRES AND RE-LAMPED. OPERATIONAL TEST WAS GOOD. 2 L 7 2 4F RT A16WE 2008032000012 20080320 00012 NM 2008 3 20 DXTA200802827 1 20080202 A 3240 7G1042 PRESSURE SWITCH AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE BRAKE ASSY MALFUNCTIONED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 245QS 6156 145 WHEN MAIN BRAKES ARE RELEASED BRAKE PRESSURE ANNUNICATOR ILLUMINATES, CHECKED LT AND RT SIDE, ONLY ILLUMINATES FOR LT SI DE. LT BRAKE MINELCO RED + RT AILERON MINELCO RED. (M-2B) REMOVED PRESSURE SWITCH ON THE LT SIDE P/N 7G1042 S/N 723. INSTALLED A NEW SWITCH SAME P/N S/N 1337. OPS CHECK GOOD. REPOSITIONED THE NR 1 NR 2 BSCU'S. NR1 P/N C203470060700 S /N 047 AND INSTALLED IN THE NR 2 POSITION. REPOSITION NR2 P/N C203470060700 S/N 183 AND PLACED IN THE NR2 POSITION. OP S CHECK GOOD IAW MM 32-42-00 NR 32-446. REF FAS 08-299. 2 L 7 2 4F 4 F RT A50NM E44NE 2008032000022 20080320 00022 EA 2008 3 20 N6WA0080205 1 20080222 A 2560 FLASHLIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE CABIN INOPERATIVE A N6WA K NONE L NO TEST IN INSP/MAINT 1 CE 03 153GJ 10219 AFT FLIGHT ATTENDANT FLASHLIGHT INOP. DEFERRED IAW MEL 25-61-04-2. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008032000023 20080320 00023 EA 2008 3 20 N6SA0080206 1 20080225 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE EMERGENCY LIGHT INOPERATIVE A N6WA K NONE L NO TEST IN INSP/MAINT 1 CE 03 165GJ 10257 LT WING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACE BULB. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008032000043 20080320 00043 CE 2008 3 20 DXTA200802851 1 20080207 A 3243 991205018 MASTER CYLINDER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT BRAKE LEAKING E DXTA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 GL 07 394QS 36 5600394 LT BRAKE PEDAL ON FO'S SIDE SPONGY, SQK 2. REMOVED AND REPLACED CHECK VALVE FOR CABIN PRESSURE TO BRAKE RESERVOIR. REMO VED AND REPLACED PRESSURE RELIEF VALVE FOR BRAKE RESERVOIR. ALL WORK DONE IAW MM 20-10-01 REMOVED AND REPLACED MASTER CYLINDER IN-LINE FILTER REF SB560-32-35 CLEANED ALL FOUR MASTER CYLINDERS AND RAN ALL BRAKE PEDALS. FOUND PILOT IB MAS TER CYLINDER LEAKING AT PISTON SEALS REMOVED AND REPLACED PILOT IB MASTER CYLINDER IAW CH 32-42-02 REV. 12 BLEED BRA KES IAW MM 32-42-00 REV 23. 2 L 7 2 4F 4 F RT A22CE E25EA 2008032000053 20080320 00053 CE 2008 3 20 DXTA200802860 1 20080210 A 2750 FLAP SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 07 962QS 7500126 ON APPROACH, SELECTED FLAPS TO 35 AND THE FLAPS WENT TO ABOUT 20 AND GOT A FLAPS FAIL EICAS MESSAGE. DOWNLOADED FAULTS B ITE CODES 2 AND 8, RESET BITE. OPERATED FLAP SYS SATISFACTORY. ALL FLAP TRAVEL IS GOOD. REPLACED FLAP RELAY KZ089 WITH N EW, IAW MM 27-51-00. OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032000073 20080320 00073 CE 2008 3 20 DXTA20082874 1 20080213 A 2840 PROBE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE FUEL SYSTEM READS LOW E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 627QS 5605227 ON TAKEOFF ROLL, MASTER CAUTION CAME ON, REJECTED TAKEOFF, LT FUEL GAUGE ANNUNCIATOR LIGHT ON. CONNECTED TEST SET, FOUN D PROBE NR 6 READING LOW. REMOVED NR6 PROBE, CLEANED AND REINSTALLED, PROBE NOW READING IN SAME RANGE AS OTHER PROBES, C /W WET CAL IAW MM CH 28-41-00. OPS CHECKED GOOD. LEAK CHECKED GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032000079 20080320 00079 CE 2008 3 20 DXTA20082880 1 20080217 A 3230 LANDING GEAR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 382QS 5600382 MANUAL GEAR EXTENSION WITH BLOW DOWN DUE TO NOSE GEAR NOT EXTENDED DURING LANDING. RESET BLOWDOWN BOTTLE AND SERVICED S WING GEAR MULTIPLE TIMES. UNABLE TO DUPLICATE PROBLEM. REF: MM SEC 32-30-00 2 L 7 2 4F 4 F RT A22CE E25EA 2008032000086 20080320 00086 SO 2008 3 20 FDKA200803096 1 20080307 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 828MJ 145218 FDM 6077 IAD (1435 PHX LCL) - EMERGENCY LIGHT UNDER FA JUMPSEAT INOP. MX RESET LIGHTING SYSTEM, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008032000115 20080320 00115 NM 2008 3 20 P5CA0801548 1 20080311 A 5280 SKIN BOEING 747 74746NF 13848BT NM MLG DOOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 453PA 30811 RT WING LANDING GEAR STRUT DOOR SKIN DELAMINATED. ACCOMPLISHED INTERIM REPAIR PER MA NR A4 5280-03:00 PART 1. 2 L 7 4 4F RT A20WE 2008032000119 20080320 00119 NM 2008 3 20 DL76G080325 1 20080309 A 2530 828450407 OVEN BOEING 767 767332 1382001 NM AFT GALLEY SPARKS A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1613B 32776 AFT GALLEY OVEN NR 3 HAD SPARKS ON TOP WHEN TURNED ON, PULLED C/B. PULLED OVEN AND INSPECTED OVEN AND AREA FOR EVIDENCE OF ELECTRICAL OR MECHANICAL DEFECT. NO TROUBLE FOUND. REACTIVATED OVER AND PERFORMED OP CK, NO DEFECT NOTED. AS PREC AUTION REPLACED OVEN, S/N670. 2 L 7 2 4F RT A1NM 2008032000148 20080320 00148 NM 2008 3 20 DLM90080358 1 20080228 A 5514 LUG DOUG MD90 MD9030 3023690 NM VERTICAL STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 HORZ STAB PIVOT BEARING LUGS (4 EA) AND BARE SLEEVES (2 EA) CORRODED AND PITTED. INSTALLED REPAIRED HORZ STAB LUGS, IAW DELTA ER/A 466670-14 REV. DATE 19FEB08 I/R. 2 L 7 2 4F RT A6WE 2008032000153 20080320 00153 SO 2008 3 20 LR7A08034 1 20080227 A 5230 33983728L STIFFENER LKHEED 382 382G 526414U SO FS 1020 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2299 5025 DURING SCHEDULED C-7 CHECK, PER JOB CARD HC5212, FOUND CARGO DOOR REAR BULKHEAD STIFFENER CRACKED AT FS 1020, WL270, LBL 20. REPAIR ACCOMPLISHED BY REPLACING STIFFENER IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008032000154 20080320 00154 SO 2008 3 20 LR7A08035 1 20080227 A 7120 36001425 BUSHING LKHEED 382 382G 526414U SO ENGINE MOUNT MISSING A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2299 5025 DURING SCHEDULED C-7 CHECK, PER AD96-12-20, FOUND ENGINE NR 1 INBD TRUSS LUG AT DIAGONAL TUBE ATTACHMENT BUSHING MISSING AND HOLE ELONGATED AT FS 515, WL 277.25, LT OWS 162.75. REPAIR ACCOMPLISHED BY PERFORMING NDT, REAMING HOLE AND INSTAL LING NEW BUSHING IAW SMP583 FIG 54-30-17, SB382-71-23 R1 AND SP-76 APPENDIX A PARA 1B. 2 H 7 4 4T A1SO 2008032000160 20080320 00160 EU 2008 3 20 08FDEA00903 1 20080312 A 5414 A5461135720000 PANEL AIRBUS 310 A310203 3930313 EU NR 1 NACELLE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 1 PYLON PANEL NR 414BR HAS 2 CORNERS CHAFED. BLENDED CHAFED AREA IAW SRM 54-52-51; FIG 101. FOUND TO BE OUT OF LIMIT S IAW SRM 54-52-51; FIG 101. FABBED DOUBLER IAW SRM 54-52-51; FIG 202. ALODINED IAW SRM 51-21-10 AND PRIMED IAW 54-52-51 ; FIG 51-23-10. INSTALLED DOUBLER IAW SRM 54-52-51; FIG 202. TOP COATED AREA IAW SRM. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008032000162 20080320 00162 WP 2008 3 20 08FDEA00905 1 20080312 A 5730 ARB128213 PANEL DOUG MD10 MD1010F 3022112 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LEFT WING OUTBD L/E PANEL 527 AB OUTBD END ACCESS DOOR HINGE MOUNT IS CRACKED. REMOVED & REPLACED THE HINGE IAW SRM 51- 35-01 VOL II. 2 L 7 3 4F RT A22WE 2008032000169 20080320 00169 NM 2008 3 20 08FDEA00912 1 20080312 A 5311 ACA73511 FRAME DOUG MD11 MD11F 3023600 NM BS 535 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 521FE 48478 MAIN DECK LT FRAME AT STA 535 L24 FOUND DENTED. DENTED AREA REPAIRED AS PER DWG SRZ-53-503. REPAIR CLASSIFIED AS MINO R AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032000180 20080320 00180 EU 2008 3 20 F3LA200800093 1 20080302 A 5321 D5367150100000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED FLOOR PANEL 231MF WAS PUNCTURED ON ITS TOP SURFACE. MAINTENANCE REPAIRED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 201, ZONE A. UPON COMPLETION OF THE REPAIR , THE FLOOR PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032500295 20080325 00295 2008 3 25 2008UALA01463 4 20080315 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU R1 DOOR MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 372UA 24637 THE 1R SLIDE PARTIALLY DEPLOYED FROM SLIDE PACK. GIRT BAR WAS NOT STOWED PROPERLY. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032600003 20080326 00003 NM 2008 3 26 HALA0800402 1 20080311 A 3080 DETECTION SYS BOEING 717 717200 1383700 NM ICE DETECTION MALFUNCTIONED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 485HA 55130 LT AND RT WING ICE DETECT FAIL FAULT. ACCOMPLISHED FIM TASK 30-81-00-810-802. NO FAULT NOTED. OK FOR SERVICE. 2 L 7 2 4F TR A6WE 2008032600005 20080326 00005 2008 3 26 HALA0800403 4 20080313 A 3425 ACARS BOEING 767 7673G5 1385126 NM COCKPIT MALFUNCTIONED A HALA K NONE N FALSE WARNING CR CRUISE 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM - EICAS "FMC" MSG ILLUMINATED AND STAYED ON ENTIRE FLIGHT WITH NO UPLINK MESSAGES PENDING. CLE ARED ACARS BUFFER. GRD CHK OK. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008032600013 20080326 00013 NM 2008 3 26 QXEA200800287 1 20080313 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM NR 11 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - C4- RIGHT INBOARD SEAT TRACK NR 11 HAS CORROSION (STAX10 SEVERAL SPOTS), STAX64, STAX94 CORROSION AND SCRATCHES. BLENDED OUT CORROSION IAW DASH 8 Q400 RD8/4-53-884, OUT OF LIMITS. REMOVED SEAT TRACK NR 11 REF Q400 SRM 51-40-07 AND I NSTALLED NEW SEAT TRACK NR 11 IAW Q400 SRM 51-42-05 AND 51-40-15. 2 H 7 2 4T RT A13NM 2008032600015 20080326 00015 SO 2008 3 26 LR7A08043 1 20080227 A 3010 3517863 DIFFUSER LKHEED 382 382G 526414U SO RT WING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2299 5025 DURING SCHEDULED C-7 CHECK, PER JOB CARD HC5702, FOUND RT OUTER WING LEADING EDGE ANTI-ICING DIFFUSER ASSY CRACKED AT OW S349. REPAIR ACCOMPLISHED IAW LAC MEA 382-30-08-008. 2 H 7 4 4T A1SO 20081010 NM 2008 10 10 UPS08653430 1 20080924 A 5320 140T013039 BRACKET BOEING 767 76734AF 1385212 NM CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 330UP 27756 INSPECTION TYPE:C AFT CARGO COMPT STA 1087 RBL 25 UNDER FLOOR BRACKET FOUND CRACK (CRACK LENGTH 1 INCH). BRACKET REPLAC ED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008032600023 20080326 00023 EU 2008 3 26 08FDEA00995 1 20080317 A 5311 FRAME AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT FRAME 69 HAS CORROSION ON THE UP RIGHT DAM ABOVE STR 55 LEFT. REMOVED CORROSION IAW SRM 51-74-10; CHECKED LIMIT S IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. REMOVED DAMAGED PARTS IAW SRM 51-40-21. RECIEVED NEW PA RT (WEB). LOCATED AND DRILLED NEW PART IAW SRM 51-40-44; INSTALLED IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008032600026 20080326 00026 NM 2008 3 26 DHL2008752505 1 20080208 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 AFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4 INCH BY 1/2 INCH IAW B727SRM 51-40-3 FIG1. FABRICATED FRAME REPAIR MATERIAL USED 7075-O .071 PO NR 9006377 DIMENSIO N 9 INCH BY 4 INCH IAW B727 SRM 51-40-3 FIG 1 AND IAW B727 SRM 53-10-2 FIG 5. HEAT TREAT PART 7075-O TO 7075T6 IAW B727 FLIGHTSTAR AIRCRAFT SERVICES ENGINEERING REPORT NR 2-37153-801 REV A TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-1 0-2. INSTALLED REPAIR IAW B727SRM 51-30-2. 2 L 7 3 4F A3WE 2008032600027 20080326 00027 NM 2008 3 26 DHL2008752507 1 20080206 A 5720 STRUCTURE BOEING 727 727223 1384074 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 LT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IS CRACKED FWD. REMOVED FASTENERS AT LT WING UPPER T /E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IAW B727SRM 51-30-2. STOP DRILLED 0.250" DIA AT END OF CRACK IAW B7 27 SRM 57-30-4 FIG 10. FABRICATED DOUBLER MATERIAL USED 7075T6 0.071 PO NR 9005482 DIMENSION 4 INCH BY 5 5/8 INCH IAW B 727SRM 57-30-4 FIG10. TREATED AND PRIMED DOUBLER AND AREA IAW B727SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727SRM 51 -30-2 AND 57-30-4 FIG 10. 2 L 7 3 4F A3WE 2008032600029 20080326 00029 NM 2008 3 26 DHL2008752510 1 20080206 A 5752 SKIN BOEING 727 727223 1384074 NM AILERON TAB DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 LT OB AILERON TAB UPPER SURFACE HAS DELAMINATED AREA. CUTOUT DELAMINATED AREA 2 INCHES DIA ON LT O/B AIL TAB UPPER SURF ACE. FABRICATED FILLER AND DOUBLER IAW B727SRM 57-50-2, BONDED FILLER AND DOUBLER IAW B727SRM 51-40-20. 2 L 7 3 4F A3WE 2008032600035 20080326 00035 NM 2008 3 26 EIA2008011 1 20080204 A 3350 1317 LIGHT BOEING 747 747230F 1384829 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490EV 24138 CEILING EMERGENCY LIGHT AT UPPER DECK CREW EXIT DOOR INOP. RELAMPED CEILING EMERGENCY EXIT LIGHT IAW B747 MM 33-51-00, OPS CHECK NORMAL. 2 L 7 4 4F RT A20WE 2008032600041 20080326 00041 WP 2008 3 26 08FDEA01000 1 20080317 A 5280 ARC2859511 DOOR DOUG MD10 MD1010F 3022112 WP LT MLG DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LT MLG STRUT DOOR EXTERNAL DOUBLER IS DISBONDING. LEFT MLG STRUT DOOR WAS FOUND TO REQUIRE REPLACEMENT. REMOVED & REPL ACED LT MLG STRUT DOOR & ADJUSTED THE DOOR FOR PROPER FIT & FAIR LIMITS ON GEAR RETRACTION IAW AMM 32-14-01-2. PERFORM ED THE FUNCTIONAL CHECK LISTED ON THE JPF STEP 8. 2 L 7 3 4F RT A22WE 2008041500151 20080415 00151 EA 2008 4 15 TRAX200800525 1 20080410 A 5313 STRINGER CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 723EV 10132 STR 26RT CORRODED BETWEEN STA 333 AND 349. REMOVED AND REPLACED STRINGER PER SRM 51-42-06 AND 51-42-21. 2 L 7 2 4F RT A21EA 2008032600043 20080326 00043 EU 2008 3 26 08FDEA01003 1 20080317 A 5544 A554715000061 FITTING AIRBUS 310 A310203 3930313 EU RUDDER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RUDDER; LEFT SIDE LEADING EDGE; BR 4 UPPER HINGE BLOCK REPAIR AREA HAS 1 EACH MISSED DRILLED HOLE. COMPLIED WITH EA 655 40-118461. 2 L 7 2 4F RT A35EU 2008032600059 20080326 00059 WP 2008 3 26 08FDEA01012 1 20080318 A 5320 NCA604641 STIFFENER DOUG DC10 DC1030F 3023504 WP FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 307FE 48291 DURING ACF MODIFICATION AS REQUIRE ON ACF J/C SP10240305-7003-5J, FOUND SEVERE WEARS ON VERTICAL STIFFENERS LT AIR COND COMPT. REPAIRED STIFFENER IAW SRM 53-00-01 FIG 9 SHT 7 VOL I. 2 L 7 3 4F RT A22WE 2008032600060 20080326 00060 EU 2008 3 26 08FDEA01013 1 20080318 A 5330 A53980911202 DOUBLER AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CORROSION AT VENTURI OUTLET DOUBLER C72-73, P41-44LT, REPAIR PERFORMED BY REPLACEMENT OF DOUBLER IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008032000187 20080320 00187 NM 2008 3 20 UPS08M51800 1 20080218 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 8 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED A ND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M, BUSHING O.D. .946 BORE I.D. .944. 2 L 7 3 4F RT A22WE 2008032000188 20080320 00188 NM 2008 3 20 UPS08M51801 1 20080226 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 9 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED A ND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. .945 I.D. .944 2 L 7 3 4F RT A22WE 2008032100001 20080321 00001 NM 2008 3 21 08FDEA00773 1 20080307 A 5340 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 MAIN DECK CARGO DOOR, LOWER JAMB SUPPORT FITTING AT NR 7 A POS HFEC CHECK FOUND FASTENER HOLE CRACKED. REPAIR CARRIED O UT AS PER FEDEX EA1-5310-112585, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032100003 20080321 00003 EU 2008 3 21 08FDEA00780 1 20080307 A 5510 A5517610000500 TIP CAP AIRBUS 310 A310203 3930313 EU HORIZONTAL STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT HORIZONTAL STABILIZER TIP LOWER L/E IS ERODING BEHIND THE ANTI-EROSION STRIP. REMOVED DAMAGE, VERIFIED MAT I.D. APPL IED LAYUP & CURED, RESTORED FINISH IAW 55-14-11. 2 L 7 2 4F RT A35EU 2008032100004 20080321 00004 EU 2008 3 21 08FDEA00781 1 20080307 A 5532 A5537246500000 PANEL AIRBUS 310 A310203 3930313 EU VERTICAL STAB PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 VERTICAL STABILIZER PANEL NR 325 FL IS PUNCTURED. REPAIRED DAMAGED AREA BY APPLYING FIBERGLASS OVERLAYS IAW SRM 53-33-1 3 FIG 201 SECTION C-C. PAINTED REPAIR AREA ON THE PANEL IAW 51-75-10-08. 2 L 7 2 4F RT A35EU 2008032400005 20080324 00005 NM 2008 3 24 08022601 1 20080226 A 2421 729825J IDG BOEING 757 757200 1384950 NM RT ENGINE DEFECTIVE A BEFA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 19 741PA 412 412 24737 ABORTED T/O FOR R GEN OFF CAUTION, QRH COMPLETED, LIGHT (CAUTION) RESET. ACP BPCU BITE TEST IAW B757 FIM 24-20-00, OP C HECK OK. TAKEOFF ROLL AT 105 KTS RT GEN OFF CAUTION APPEARED CONTINUED T/O. QRH COMPLETE NO FURTHER ACTION INFLT REQUI RED. ACP BITE CHECK OP BPCU RESET ACP BITE CHECK AFTER RESET FOUND SYS OK IAW B757 MM 24-20-00 OP CHECK OK. ON T/O RT ENGINE GEN LIGHT ON EICAS. QRH PROCEDURE FOLLOWED & GEN RESTORED - UPON DESCENT MESSAGE RETURNED. MEL 24-00-01A AUTH MX 41-176 PER MEL DISC PER MEL PLACARD INSTALLED. REF MEL 24-00-01A AUTHORIZATION NR 41-176 RT ENGINE GEN LIGHT OFF MSG O N EICAS LOG PAGE 3677. REMOVED AND REPLACED RT ENGINE IDG IAW B757 AMM 24-11-01. OPS CHECK GOOD IAW AMM 7100-00. THIS 2 L 7 2 4F RT A2NM 2008032400009 20080324 00009 NM 2008 3 24 ASAA0852705 1 20080310 A 3040 1016755 WARNING SYSTEM BOEING 737 737890 1384527 NM L1 WINDOW MALFUNCTIONED A ASAA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 01 558AS 35177 LEFT SIDE WINDOW OVERHEAT LIGHT ANNUNCIATED. QRH FOLLOWED. OPS NORMAL. REPEAT WRITE UP. WINDOW HEAT CONTROLLER LOGS WINDOW SENSOR FAILURE. ACCOMPLISHED VISUAL INSPECTION OF L1 WINDOW NO CRAZING NOTED. NO VISUAL DISTORTION OR DEFECTS N OTED. CHANGED TO SPARE TEMP SENSOR. OP CHECKS GOOD. 2 L 7 2 4F RT A16WE 2008032400011 20080324 00011 SO 2008 3 24 FDKA200803091 1 20080306 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6104 MCO (0925 PHX LCL) GALLEY DOOR EMERGENCY EXIT LIGHT INOP. MX RESET LIGHTING SYSTEM. 2 L 7 2 4T RT T00011AT 2008032400012 20080324 00012 SO 2008 3 24 FDKA200803094 1 20080307 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6069 TYS-MCO (0437 PHX LCL). EMERGENCY EXIT ROW 12 RT DOES NOT ILLUMINATE. MX RESECURED CONNECTOR ON LIGHT ASSY, O PS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008032400013 20080324 00013 EA 2008 3 24 COMA0860157 1 20080304 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 965CA 17746 7131 FLIGHT 5479 - FLOOR MOUNTED EMERGENCY STRIP BEHIND ROW 8A IS INOP. REPLACED BATTERY PACK NR 4. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008032400028 20080324 00028 NM 2008 3 24 HNAA0800098 1 20080308 A 3350 85 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 804EX 42519 42519 227 FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH BACK LIGHTING IS INOP. RELAMPED FLIGHT ATTENDANT EMERGENCY LIGHT OPERATIONAL CH ECK GOOD. 2 H 7 2 4T RT A13NM 2008032400031 20080324 00031 NM 2008 3 24 UPS08M51816 1 20080303 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 28 LT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.164 BORE I.D. 1.162. 2 L 7 3 4F RT A22WE 2008032400032 20080324 00032 NM 2008 3 24 UPS08M51817 1 20080226 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 30 LT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.132 BORE I.D. 1.130. 2 L 7 3 4F RT A22WE 2008032400033 20080324 00033 NM 2008 3 24 UPS08M51818 1 20080305 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 31 LT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.132 BORE I.D. 1.130. 2 L 7 3 4F RT A22WE 2008032400034 20080324 00034 NM 2008 3 24 UPS08M51819 1 20080219 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 32 LT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.132 BORE I.D. 1.130. 2 L 7 3 4F RT A22WE 2008032400035 20080324 00035 NM 2008 3 24 UPS08M51820 1 20080307 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 33 LT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.164 BORE I.D. 1.162. 2 L 7 3 4F RT A22WE 2008032400042 20080324 00042 NM 2008 3 24 QXEA200800278 1 20080309 A 2120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM AFT CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 424QX 4006 FLT 2258 - FLIGHT ATTENDANT AND NON-REV PILOT REPORTED DETECTING A FAINT ODOR OF SMOKE IN THE REAR OF THE AIRCRAFT. FRO NT FLT ATTENDANT AND COCKPIT CREW DETECTED NOTHING. LASTED FOR ABOUT 1 MINUTE. MAINTENANCE GROUND RAN AIRCRAFT FOR 30 MINUTES WHILE ALTERNATING THE PACKS AND TEMPERATURE SETTINGS. NO DEFECTS OR ODORS NOTED. OPERATIONAL TEST OF ECS CONTR OL SYSTEM CHECKS GOOD. COULD NOT DUPLICATE. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008032400045 20080324 00045 NM 2008 3 24 QXEA200800280 1 20080309 A 2612 82410910957 CONTROL PANEL BOMBDR DHC8 DHC8402 1390042 NM FIRE DETECTION MALFUNCTIONED A QXEA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 406QX 4048 YKA- FLIGHT 2210 - DURING APPROACH, THE FIRE DETECT LIGHT ILLUMINATED INTERMITTENTLY. ALSO, THE NR 2 FAULT "A" LIGHT IL LUMINATED AS WELL. AIRCRAFT FERRIED TO PDX FOR REPAIRS. IN PDX, THE WIRING WAS CHECKED WITH NO DEFECTS. THE FIRE DETE CTION PANEL WAS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008032400050 20080324 00050 NM 2008 3 24 HALA0800388 1 20080306 A 5312 BULKHEAD BOEING 767 767332 1382001 NM FUSELAGE DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 SCRATCH FOUND ON AFT PRESS BULKHEAD ABOUT 16" TO RIGHT OF CENTER. BLENDED IAW SRM 53-80-05/101. ALODINED REWORKED AREA IAW SRM 51-20-01. REWORK VARIFIED WITHIN SRM LIMITS IAW SRM 53-80-08/101. MAX BLEND .003". REWORKED AREA PRIMED AND TOP COAT APPLIED IAW BMM 51-21-10. 2 L 7 2 4F RT A1NM 2008032400051 20080324 00051 NM 2008 3 24 HALA0800391 1 20080310 A 5532 ACCESS PANEL BOEING 767 767332 1382001 NM VERTICAL STAB DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 VERTICAL FIN ACCESS PANEL 324 CLX HAS BUBBLE ON PANEL. PERMANENT REPAIR CARRIED OUT IAW HAL B767-300 SRM 55-30-01/201 A ND 51-70-17, 200F WET LAY UP HOT BOND REPAIR. 2 L 7 2 4F RT A1NM 2008032400052 20080324 00052 NM 2008 3 24 HALA0800392 1 20080311 A 5540 STRUCTURE BOEING 767 767332 1382001 NM RUDDER DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 DENT FOUND ON LT SIDE, ABOUT 3M FROM TOP OF RUDDER. REPAIR IN WORK. 2 L 7 2 4F RT A1NM 2008032400055 20080324 00055 NM 2008 3 24 UPS08M51806 1 20080302 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 16 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M, BUSHING O.D. 1.069 BORE I.D. 1.067 2 L 7 3 4F RT A22WE 2008032400056 20080324 00056 NM 2008 3 24 UPS08M51807 1 20080226 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 18 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M, BUSHING O.D. 1.037 BORE I.D. 1.035. 2 L 7 3 4F RT A22WE 2008032400057 20080324 00057 NM 2008 3 24 UPS08M51809 1 20080302 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 19 LEFT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.069 BORE I.D. 1.067 2 L 7 3 4F RT A22WE 2008032400058 20080324 00058 NM 2008 3 24 UPS08M51811 1 20080219 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 20 LT BARREL NUT BORE HOLE, UPPER HORIZ STAB. REMOVED CORROSION, FABRICATED AN D INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035. 2 L 7 3 4F RT A22WE 2008032400062 20080324 00062 NM 2008 3 24 UPS08M51826 1 20080104 A 5753 SKIN DOUG MD11 MD11 3023602 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C LT WING I/B FLAP LOWER SURFACE I/B AND O/B SEGMENT FOUND SURFACE CORROSION AS MARKED. LHW I/B FLAP I/ B AND O/B SEGMENT LOWER SURFACE SKIN REMOVED PER SRM 51-3 1-01 V.II R35. NEW LHW INBOARD FLAP I/B AND O/B SEGMENT LOWER SURFACE SKIN FAB PER DWG ARC2736. NEW FAB 02 EA SKIN FOR LHW INBOARD FLAP I/B AND O/B SEGMENT INSTALLED PER SRM 51-35- 01 V.II REV35. 2 L 7 3 4F RT A22WE 2008032400063 20080324 00063 NM 2008 3 24 UPS08M51827 1 20080103 A 5754 SKIN DOUG MD11 MD11 3023602 NM TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C LHW LE FIXED WING APPROX STA XORS 577 INNER SKIN FOUND CRACKED. FASTENERS AT CRACKED AREA AT LHW LE F IXED WING STA XORS 577 INNER SKIN AREA REMOVED PER SRM51-35-01 V.II R35 AND CRACKED AREA AT XORS 577 TRIMMED OUT PER SRM 57-10-00 V.I FIG R40. NEW REPAIR DOUBLER 01EA, REPAIR FILLER 01EA AND 04 EA REPAIR ANGLES FAB AND INSTALLED PER SRM 57 -10-00 FIG 27 VOL I REV 40. 2 L 7 3 4F RT A22WE 2008032400064 20080324 00064 NM 2008 3 24 UPS08M51828 1 20080227 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48473 INSPECTION TYPE:3C FOUND CORROSION ON NR 1 RT BARREL NUT BORE HOLE, UPPER. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.505 BORE I.D. 1.503. 2 L 7 3 4F RT A22WE 2008032400066 20080324 00066 NM 2008 3 24 UPS08M51830 1 20080302 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 3 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. .976 BORE I.D. .974. 2 L 7 3 4F RT A22WE 2008032400070 20080324 00070 NM 2008 3 24 UPS08M51834 1 20080303 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 7 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER EO MD11-5510-19409-M, BUSHING O.D. .976 BORE I.D. .974. 2 L 7 3 4F RT A22WE 2008032400071 20080324 00071 NM 2008 3 24 UPS08M51835 1 20080218 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 8 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944. 2 L 7 3 4F RT A22WE 2008032400072 20080324 00072 NM 2008 3 24 UPS08M51836 1 20080226 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 9 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944. 2 L 7 3 4F RT A22WE 2008032400073 20080324 00073 NM 2008 3 24 UPS08M51837 1 20080218 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 11 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. .946 BORE I.D. .944. 2 L 7 3 4F RT A22WE 2008032400079 20080324 00079 NM 2008 3 24 UPS08M51844 1 20080218 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 20 RT (UPPER) BARREL NUT HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING PER E.O. MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035. 2 L 7 3 4F RT A22WE 2008032400080 20080324 00080 NM 2008 3 24 UPS08M51845 1 20080226 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 21 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035. 2 L 7 3 4F RT A22WE 2008032400081 20080324 00081 NM 2008 3 24 UPS08M51846 1 20080302 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 22 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 1.037 BORE I.D. 1.035. 2 L 7 3 4F RT A22WE 2008032400082 20080324 00082 NM 2008 3 24 UPS08M51847 1 20080219 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 23 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER E.O. MD11-5510-19409-M BUSHING O.D. 1.037 BORE I.D. 1.035 2 L 7 3 4F RT A22WE 2008032400086 20080324 00086 NM 2008 3 24 UPS08M51854 1 20080304 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 28 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 1.132 BORE I.D. 1.130. 2 L 7 3 4F RT A22WE 2008032400087 20080324 00087 NM 2008 3 24 UPS08M51855 1 20080218 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 29 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 1.164 BORE I.D. 1.162. 2 L 7 3 4F RT A22WE 2008032400088 20080324 00088 NM 2008 3 24 UPS08M51856 1 20080226 A 5512 PANEL DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C CORROSION FOUND ON NR 30 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 1.132 BORE I.D. 1.130. 2 L 7 3 4F RT A22WE 2008032400090 20080324 00090 NM 2008 3 24 HNAA0800099 1 20080310 A 3230 841005 PSEU DHAV DHC8 DHC8102 2809003 NM LANDING GEAR DEFECTIVE A HNAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 07 837EX 34963 33306 217 RIGHT FWD GEAR DOOR REMAINED OPEN AFTER GEAR RETRACTION. CREW CYCLED GEAR PER EMERGENCY CHECK LIST, GEAR RETRACTED NORM ALLY. CHECKED DOOR RIGGING, CHECK GOOD. CHECK SENSOR RIGGING, CHECK GOOD. C/W SEVERAL GEAR SWINGS, CHECK GOOD. REMOV ED AND REPLACED PSEU, SELF TEST GOOD. 2 H 7 2 4T RT A13NM 2008032400092 20080324 00092 NM 2008 3 24 HNAA0800101 1 20080308 A 2913 LD4 HYDRAULIC SYSTEM DHAV DHC8 DHC8102 2809003 NM NR 1 LOW A HNAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 07 911HA 034 ON APPROACH NR 1 HYDRAULIC SYSTEM QTY WAS AT 1.5 QTS, AFTER LANDING COCKPIT GAUGE SHOWED 1.3 QTS. LOSS OF NORMAL BRAKES AND ISO LIGHT ILLUMINATED ON TAXI. NR 1 GAUGE ON NACELLE READS .5 QTS, SERVICED NR 1 HYDRAULIC SYSTEM, RAN AIRCRAFT TW ICE AND CYCLED TOE BRAKES, OPS NORMAL AT THIS TIME. NO LEAKS NOTED, ISO LIGHT IS OUT. NOTE: NR 2 SYSTEM FOUND OVERSER VICED FROM FLUID TRANSFER, CORRECTED TO PROPER LEVEL. LEAK CHECK OF COMPLETE NR 1 HYDRAULIC SYSTEM, NO LEAKS FOUND. 2 H 7 2 4T RT A13NM 2008032400113 20080324 00113 2008 3 24 COMA0860162 4 20080307 A 3425 6229336400 AHRS CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 446CA 3188 7546 FLIGHT 5675 - RECEIVED EFIS COMP MON CAUTION MESSAGE. ATTEMPTED TO CORRECT, BOTH HSI'S SHOWED RED HEADING FLAG. ATC AD VISED30 DEGREES OFF COURSE. RETURNED TO BOS, LANDED WITHOUT INCIDENT. REPLACED NR 2 AHRS. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008032400121 20080324 00121 WP 2008 3 24 IXXA08SMN047S 1 20080214 A 5340 FITTING DOUG DC8 DC871F 302199D WP BS 1690 L28R CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND AFT ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 1690.000 LONGERON 28 RIGHT . REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-3-1, SRM 5 1-1-20D, AND SRM 51-1 8B. 2 L 7 4 4F RT 4A25 2008032400124 20080324 00124 EU 2008 3 24 F3LA200800103 1 20080229 A 5315 D5347218820200 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSLEAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND AT THE NUT PLATE HOLE, AT THE FORWARD SPLICE, ON THE Y1292 FLOORBEAM, BETWEEN FRAMES 68 AND 69. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM AND SPLICE ANGLES IN ACCORDANCE WI TH SRM 51-42-11, PARAGRAPH 7 AND DRAWING D53472780. UPON COMPLETION OF THE INSTALLATION THE WORK WAS INSPECTED AND FOUN D ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400126 20080324 00126 NM 2008 3 24 QXEA200800282 1 20080306 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX- C5 - CORROSION ON LOWER SURFACE OF MCD SILL PLATE STATION X250 AT AFT NUT PLATE. BLENDED TO REMOVE CORROSION IAW R D8-53-8921. HFEC INSPECTION OF BLENDED AREA IAW -8/200 NDTM PART 6 51-00-01, NO CRACKS NOTED. AREA IS WITHIN LIMITS, E TCH, ALODINE AND PRIMED REF RD8-53-8921. 2 H 7 2 4T RT A13NM 2008032400128 20080324 00128 NM 2008 3 24 QXEA200800283 1 20080306 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 354PH 498 PDX - C5 - MCD SURROUND FWD SIDE OF SILL PLATE AREA, CORROSION AT SEAL INFLATION FEED THROUGH, IPC 52-05-00 FIG 5 ITEM 4 90. REMOVED MCD SEAL INFLATION TUBE AND REMOVED CORROSION AROUND HOLE REF RD8-53-8921. HFEC INSPECTION IAW -8/200 NDTM PART 6 51-00-01 AND THICKNESS CHECK IAW PART 1 51-00-04. AREA IS WITHIN LIMITS. ETCH, ALODINE AND PRIMED REF RD8-53-8 921. 2 H 7 2 4T RT A13NM 2008032400132 20080324 00132 EU 2008 3 24 YENA2008024 1 20080306 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 597JB 2307 FLT 319, FLL-IAD, BURNING RUBBER SMELL IN CABIN AROUND ROWS 11 & 12. SMELL WAS FIRST DISCOVERED BY PAX AND CONFIRMED BY ALL THREE F/A'S. NO OTHER ABNORMALS NOTED AND SMELL WAS CONSTANT DURING FLIGHT. ACCOMPLISHED TSM PROCEDURES 24-00-00- 810-823 AND 23-39-00-810-801. OPERATED LVTV ALL VDU'S OPERATING. CHECKED A/C EXTERIOR NO EVIDENCE OF FLUID LEAKS. OPER ATED LT & RT AIR COND SYS WHILE ISOLATING LT ENGINE RT ENGINE. NO EVIDENCE OF BURNING SMELL IN CABIN, A/C OK FOR SERVIC E. 2 L 7 2 4F RT A28NM 2008032400133 20080324 00133 WP 2008 3 24 08FDEA00921 1 20080313 A 5311 TAS793359514 FRAME DOUG MD10 MD1010F 3022112 WP BS 899 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 FWD CARGO COMPARTMENT BILGE AREA; FS 899 FRAME LOWER FLANGE UPPER SURFACE HAS LIGHT CORROSION; STR 51R - 51L. REMOVED C ORROSION IAW SRM 51-21-01; VOL II; PG 28 AT STA 899 STR 51R - 51L FRAME FLANGE. FOUND TO BE WITHIN LIMITS IAW SRM 53-00 -01;FIG 1A. ORIGINAL THICKNESS IS .080. MATERIAL LOSS OS .010. REMAINING THICKNESS IS .070. ALODINED, PRIMED, AND T OP COATED IAW SRM 51-21-01; VOL II; PGS 19; 21 AND 24. INSTALLED FASTENERS 6 IAW SRM 51-33-01; VOL II; PG 1. MINOR RE PAIR. 2 L 7 3 4F RT A22WE 2008032400138 20080324 00138 NM 2008 3 24 08FDEA00925 1 20080313 A 5310 146N38101 SPLICE BOEING 757 7572B7 1384964 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 UPON REMOVAL OF INTERCOSTAL AT STA 1400, LBL 2, FOUND CORROSION ON BUTT SPLICE STRAP. REMOVED CORROSION IAW SRM 51-10-0 2, L= 1.5", W= 1.1", D=.030" SRM DOES NOT PROVIDE ALLOWABLE DAMAGE LIMITS FOR THIS PART, CONTACTED ENGINEERING. PER EA F-5330-110824: TRIMMED OUT DAMAGED AREA ON SPLICE STRAP, HFEC INSPECTED AREA, VERIFIED FRAME SHEAR TIE BETWEEN S29L AND 30 NOT DAMAGED. FABRICATED REPAIR DOUBLER AND FILLER, INSTALLED REPAIR PARTS. THIS IS A MAJOR REPAIR WITH NO FOLLOW UP ACTIONS IMPOSED BY SAID EA. 2 L 7 2 4F RT A2NM 2008032400143 20080324 00143 EU 2008 3 24 08FDEA00928 1 20080314 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 2 SLAT MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 741FD FH1459 611 EXISTING REPAIR ON LT SLAT NR 2, LEADING EDGE AREA INBOARD END, WITH MIS-DRESSED HOLES FOUND. REPAIR PERFORMED BY INSTA LLING A DOUBLER IAW RAS /FOK/320/2008 ISS A, APPROVED BY EA 6-5743-114857. 2 L 7 2 4F RT A35EU 2008032400144 20080324 00144 EA 2008 3 24 COMA0860173 1 20080312 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 957CA 7109 DURING HMV-6 INSPECTION, NDT (HK) FOUND CRACK AT LOWER END OF VERTICAL STIFFENER, FS 409+128, LBL 27. CUT OUT DAMAGE AN D INSTALLED DOUBLER IAW BOMBARDIER REO 601R-53-41-056. 2 L 7 2 4F RT A21EA 2008032400148 20080324 00148 EU 2008 3 24 08FDEA00930 1 20080314 A 5320 A53973300202 FLANGE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND DAMAGED BEARING SUPPORT FLANGE AT C 68-69, P34 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008032000041 20080320 00041 CE 2008 3 20 DXTA200802849 1 20080207 A 3260 UPLOCK SWITCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG OUT OF ADJUST E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 650QS 5605150 AFTER TAKEOFF , THE GEAR UNLOCK LIGHT ANNUNCIATOR ILLUIMINATED CONTINUOSLY AFTER THE GEAR HANDLE WAS RAISED TO THE UP PO SITION. ADJUSTED L/R MAIN UPLOCK SWITCHES IAW MM CHPT 32-30-05. OPS CHECK GOOD IAW MM CHPT 32-01-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032000047 20080320 00047 CE 2008 3 20 DXTA200802854 1 20080208 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG WEAK E DXTA O OTHER O OTHER LD LANDING 1 GL 07 386QS 5600486 CO PILOTS RT BRAKE PEDAL SOFT, PRESSURE DROPS DURING BRAKING. PERFORMED ANTI-SKID BRAKE SYS BLEED PROCEDURE. BRAKES CH ECK GOOD AT THIS TIME. NO PRESSURE DROP NOTED, IAW MM 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2008032000081 20080320 00081 CE 2008 3 20 DXTA20082882 1 20080215 A 3230 LANDING GEAR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP NLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 840QS 258340 NOSE GEAR LIGHT FAILED TO ILLUMINATE ON GEAR EXTENSION. LANDED SUCCESSFULLY. RED GEAR UNSAFE WARNING DURING LANDING. PER FORMED MANUAL EXTENSION IAW NJA EMERGENCY CHECKLIST PROCEDURES. LIGHT ILLUMINATED DURING TOW TO THE RAMP. PERFORMED LAN DING GEAR OPERATIONAL CHECK, ALL INDICATIONS NORMAL. WORK PERFORMED IAW MM CHAP 29-10-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2008032000112 20080320 00112 EU 2008 3 20 SMIA200807305 1 20080310 A 2613 173436245 OVERHEAT SENSOR SAAB SF340 340B 7860101 EU LT ENGINE MALFUNCTIONED A SIMA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SW 21 266AE 340B266 ON FLIGHT 3306, CREW REPORTED ON THE GROUND THEY GOT A LEFT ENGINE TAIL PIPE HOT LIGHT DURING CLIMB-OUT FOLLOWED AOM. L IGHT DID NOT GO OUT THEY THEN SHUT DOWN ENGINE 1 AS A PRECAUTIONARY PROCEDURE AND RETURNED TO ACT. AIRCRAFT REMOVED FRO M SERVICE. REMOVED AND REPLACED LEFT ENGINE OVERHEAT DETECTOR NR 2 IAW SAAB 340 AMM 26-12-05. OPERATIONAL CHECK GOOD C /W EO G1-26AD-017-R1 PART E REPORTING REQUIREMENTS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2008032000116 20080320 00116 NM 2008 3 20 DL757080322 1 20080306 A 5330 146N37505 SKIN BOEING 757 757232 1384965 NM BS 1690 S14R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 DURING HMV, THE FUSELAGE SKIN AT STA 1690 BETWEEN S-14R AND S-15R WAS FOUND DENTED. THE DENT WAS CUT OUT AND REPAIRED P ER BOEING INSTRUCTIONS. 2 L 7 2 4F RT A2NM 2008032000136 20080320 00136 NM 2008 3 20 DL757080343 1 20080205 A 5321 FLOOR PANEL BOEING 757 757232 1384965 NM CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 AFT CARGO FLOOR PANEL 161AF HAS CORROSION AND REPAIR DOUBLER BUCKLED. FABRICATED AND INSTALLED FLOOR PANEL IAW 53-60-53 . 2 L 7 2 4F RT A2NM 2008032000142 20080320 00142 NM 2008 3 20 DL757080349 1 20080203 A 5320 INTERCOSTAL BOEING 757 757232 1384965 NM BS 1480-1500 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 AFT CARGO PIT WEB INTERCOSTAL BETWEEN STA 1480-1500 LBL 27 CORRODED. FABRICATED NEW INTERCOSTAL IAW SRM 53-60-04 AND IN STALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008032000144 20080320 00144 2008 3 20 DL757080351 4 20080205 A 2565 SLIDE BOEING 757 757232 1384965 NM RT OFF WING NO TEST A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 643DL 23997 RIGHT OFF WING SLIDE FAILED OPS TEST FOR MANUAL DEPLOYMENT OF CARRIER. READJUSTED CARRIER HOOK LOCK AND PERFORMED OPS T EST FOR MANUAL DEPLOYMENT OF CARRIER IAW MM 25-65-08. 2 L 7 2 4F RT A2NM 2008032000152 20080320 00152 SO 2008 3 20 LR7A08033 1 20080227 A 5320 35969711 WEB LKHEED 382 382G 526414U SO FS 902 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2299 5025 DURING SCHEDULED C-7 CHECK, PER JOB CARD HC5315, FOUND CABIN BHD LT SIDE WEB CRACKED AT FS 902, WL 202, LBL 63. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-17. 2 H 7 4 4T A1SO 2008032000172 20080320 00172 NM 2008 3 20 08FDEA00915 1 20080313 A 2120 UNKNOWN BOEING 727 727277 138408S NM COCKPIT ODOR A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 25 243FE 21480 ODOR SMOKE IN COCKPIT WITH APU AND LEFT PACK RUNNING. 2 L 7 3 4F RT A3WE 2008032100047 20080321 00047 EU 2008 3 21 08FDEA00841 1 20080310 A 5311 A53973180272 FRAME AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT FUSELAGE FRAME HAS CORROSION ON THE WEB AT FRAME 67 ABOVE S49L. REMOVED CORROSION IAW SRM 51-74-10. CHECKED LI MITS IAW SRM 53-17-13. FOUND TO BE WITHIN LIMITS; ALODINED IAW SRM 51-21-10. PRIMED AND PAINTED BOTH IAW SRM 51-23-1 0. MINOR REPAIR 2 L 7 2 4F RT A35EU 2008032100050 20080321 00050 NM 2008 3 21 WRLA2008028 1 20080311 A 5320 AEA0218U53 INTERCOSTAL DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE LT MLG WW CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 48407 DURING C-CHECK INSPECTION CRACK FOUND LT WHEEL WELL UNDER WING BARREL KEEL STRUCTURE INTERCOSTAL. REF EGAT NR U05001. REPLADCED LT WHEELWELL UNDERWING BARREL KEEL STRUCTURE INTERCOSTAL PER MD11 SRM 51-35-01 VOL.II REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2008032100069 20080321 00069 NM 2008 3 21 2008UALA01324 1 20080308 A 3350 0L3071BPEGPL LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS WEAK A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 504UA 24625 EEL LIGHT ABOVE DOOR DIM, DOORS 1R AND 2R. FOUND WEAK BULBS (LAMPS) IN LIGHT ASSY. RELAMPED EEL LIGHTS ABOVE DOOR 1R, 2 R..LIGHTS ARE FUNCTIONING NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032400016 20080324 00016 EA 2008 3 24 COMA0860160 1 20080306 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 933CA 14113 7040 FLIGHT 5236 - RECEIVED GEAR DISAGREE WARNING. RAN QRH, LOWERED GEAR MANUALLY, DECLARED EMERGENCY, LANDED WITHOUT INCIDE NT. REPLACED NLG PRIORITY VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008032400046 20080324 00046 NM 2008 3 24 QXEA200800281 1 20080308 A 5210 85210240007 ROD DHAV DHC8 DHC8202 2809007 NM PAX DOOR BROKEN A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 353PH 496 ALW - UPON TRYING TO OPEN THE MAIN CABIN DOOR, THE GROUND CREW REPORTED THAT THE WERE UNABLE TO DO SO. MAINTENANCE ENTE RED AIRCRAFT THROUGH THE CARGO DOOR AND FOUND THAT THE SUPPORTING ROD WAS BROKEN AT THE BASE. AIRCRAFT FERRIED TO PDX F OR REPAIRS. IN PDX, REPLACED THE FORWARD AND AFT UPPER STAY STRUTS AND HANDRAIL SUPPORTS. OPERATIONAL CHECKS GOOD. AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008032400048 20080324 00048 WP 2008 3 24 08FDEA00991 1 20080317 A 5730 ARB11066 PANEL DOUG MD10 MD1010F 3022112 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT WING UPPER L/E PANEL NR 617 CT IS CRACKED IN 2 PLACES. PERFORMED HFEC PER NDT SPM 06-10-09-09. MARKED CRACKS. STO P DRILLED CRACKS. FABBED DOUBLERS REF SRM 57-10-00 VOL I. ALODINED & PRIMED REF SRM 51-21-01 VOL II. INSTALLED DOUBLERS REF SRM 51-35-01 VOL II. PAINTED REF SRM 51-21-01 VOL II. 2 L 7 3 4F RT A22WE 2008032400049 20080324 00049 NM 2008 3 24 HALA0800393 1 20080309 A 5512 ACCESS PANEL BOEING 767 767332 1382001 NM HORIZONTAL STAB DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 RT HORIZONTAL STABILIZER CR PCA ACCESS PANEL ANCHOR NUT MISSING AND ANCHOR NUT RAIL CRACKED. CRACK BLENDED OUT IAW 7673 00 SRM 55-10-90 FIG 201. DAMAGE WITHIN LIMITS. INSTALLED NEW ANCHOR NUT IAW 767-300 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008032400100 20080324 00100 EU 2008 3 24 NWAA080943251 1 20080312 A 3350 32145410 BATTERY AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 351NW 21959 20089 766 FAILED EMERGENCY LIGHT TEST ON CIDS. REPLACED EPSU 10WL/BATTERY, CHECKS OK. 2 L 7 2 4F RT A28NM 2008032400101 20080324 00101 WP 2008 3 24 IXXA08SMN043S 1 20080201 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD FLAP LOWER SKIN HAS DENTS AT STATION XW 3.000 - 91.000. REM OVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE PANEL PLATING. FABRICATED NEW SKIN AND DOUBLER. BONDED PAR TS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIRED PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, DC8 SRM 57-7-1 FIGURE 1, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 1 ITEM "B" AND "L", DC8 SRM 51-1-9 T/R 51-142, DC8 SRM 51-1-9A T/R 51-141, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008032400107 20080324 00107 EU 2008 3 24 F3LA200800100 1 20080302 A 5315 D5397470900000 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 REFERENCE NON ROUTINE C039954. DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE AFT CARGO COMPARTME NT FLOOR FRAME PLATE AT FRAME 63. MAINTENANCE REMOVED AND REPLACED THE PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A31 9 SRM 51-42-11, PARAGRAPHS 5 AND 6. FOLLOWING COMPLETION OF THE PLATE REPLACEMENT, THE NEW PLATE WAS INSPECTED AND FOUN D ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400109 20080324 00109 SO 2008 3 24 SWIA200819344 1 20080311 A 2611 47359713 SMOKE DETECTOR EMB 120 EMB120ER 3260203 SO CARGO BAY NO TEST A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 585SW 1905 1905 120353 FLT 5416 - BAGGAGE FIRE DETECTION DOES NOT TEST CORRECTLY. REPLACED FORWARD SMOKE DETECTOR IN CARGO BAY. OPS CHECK GOO D. 2 L 7 2 4T RT A31SO 2008032400111 20080324 00111 WP 2008 3 24 IXXA08SMN058S 1 20080207 A 5542 SKIN DOUG DC8 DC871F 302199D WP RUDDER DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND RUDDER RIGHT SKIN SIDE DENTED AT STATION ZR 276.531 TO ZR 267.218. REMOVED FAS TENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE PANEL PLATING. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NE EDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. BALANCED RUDDER MOMENT WITHIN TOLERANCE. MOMENT: 25 03.25 INCH POUND. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-1-11, SRM 55-1-0 PAGE 1, SRM 51-1-21, SRM 55-6-1 FIGURE 1 ITEM "A", SRM 51-1-9 T/R 51-142, SRM 51-1-9A T/R 51-141, SRM 51-1-8B, AND SRM 51-4-6 PAGES 1 AND 2. 2 L 7 4 4F RT 4A25 2008032400112 20080324 00112 EU 2008 3 24 F3LA200800101 1 20080301 A 5320 D5391635420000 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND AROUND THE NUT PLATES OF THE FORWARD CARGO COMPARTMENT, FL OOR PANEL ATTACH POINTS, BETWEEN FRAMES 24 AND 35, AT STRINGER 38L. MAINTENANCE REMOVED AND REPLACED TWO FRAME PLATES ( PN D5391635420000 AND D5392059220000) IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11, PARAGRAPHS 5 AND 6. UPON COM PLETION OF THE INSTALLATION, IT WAS INSPECTED AND FOUND OKAY. 2 L 7 2 4F 4 F RT A28NM 2008032400114 20080324 00114 EA 2008 3 24 COMA0860163 1 20080308 A 3620 355862255 LOOP CNDAIR CL600 CL6002B19 1900309 EA RT FUSELAGE FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 455CA 7592 FLIGHT 5563 - RECEIVED ANTI-ICE DUCT WARNING MESSAGE. RIGHT FUSELAGE DUCT WAS RED IN EICAS. DIVERTED TO GRR, LANDED WI THOUT INCIDENT. REPLACED FUSELAGE DETECTION LOOP A18. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008032400117 20080324 00117 EU 2008 3 24 F3LA200800102 1 20080301 A 5315 D5391379020002 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, CORROSION WAS FOUND ON THE FORWARD CARGO COMPARTMENT NUT PLATES ON THE FRAME PLATE AT FRAME 28. M AINTENANCE REMOVED AND REPLACED THE PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PAGE 6. FOLLOWING C OMPLETION OF THE INSTALLATION, THE PLATE WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400118 20080324 00118 WP 2008 3 24 IXXA08SMN062S 1 20080208 A 5340 5750540U501 FITTING DOUG DC8 DC871F 302199D WP BS 680 L11L CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FITTING CRACKED AT STATION 680.000 LONGERON 11 RIGHT. REMOVED CRACK ED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-0, DC8 SRM 51-1 -21, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008032400149 20080324 00149 NM 2008 3 24 SWAA081369 1 20080312 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032400151 20080324 00151 EU 2008 3 24 08FDEA00932 1 20080314 A 5315 A53773651212 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND TOP CAP BEAM C 35 LT CORRODED. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2008032400153 20080324 00153 EU 2008 3 24 08FDEA00933 1 20080314 A 5315 A53779635200 FLOORBEAM AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FWD PIT HAS CORROSION ON THE BOTTOM OF THE FLOORBEAM AT FRAME 37; LBL 103CM (40.5). REMOVED CORROSION FROM THE BOTTOM O F FLOORBEAM 37; Y 1000 TO 1030 IAW SRM 51-74-10; PG 210. ORIGINAL THICKNESS .126 IAW SRM 53-14-15; PG 9 AND DRAWING A53 779635. MATERIAL REMOVED .054. OUT OF LIMITS IAW SRM 53-10-15. INSTALLED REQUIRED REPAIR IAW SRM 53-10-15; FIG 206. 2 L 7 2 4F RT A35EU 2008032400157 20080324 00157 EU 2008 3 24 08FDEA00935 1 20080314 A 5350 21510415000400 FAIRING AIRBUS 310 A310203 3930313 EU ZONE 100 PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 PUNCTURE ON THE INTERIOR SURFACE OF PANEL NR 144FR. REPAIRED INTEROR SURFACE OF PANEL 144 FR BY REMOVING THE DAMAGE. CL EANED & PREPPED FOR APPLICATION OF THE WET LAY UP. APPLIED, CURED & SANDED THE WET LAY UP. CLEANED & PREPPED FOR THE A PPLICATION OF THE REFINISH. APPLIED THE REFINISH IAW SRM 51-77-10 & SRM 51-75-10. 2 L 7 2 4F RT A35EU 2008032400160 20080324 00160 EU 2008 3 24 08FDEA00938 1 20080314 A 5540 NAS5100006C BEARING AIRBUS 310 A310203 3930313 EU RUDDER HINGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RUDDER HINGE ARM; NR 5 BEARINGS ARE CORRODED. REMOVED 2 BEARING ASSEMBLIES. CLEANED AND INSPECTED HINGE ARM. REPLACE D BEARING ASSEMBLIES IAW FEDEX A310-200 AM 53-36-11-08 P/N FOR ALL OF THE BEARING THAT WERE REPLACED ARE AS FOLLOWS; NS A 5100-006C; NSA 8130-08. 2 L 7 2 4F RT A35EU 2008032400163 20080324 00163 NM 2008 3 24 SWAA081361 1 20080312 A 2731 251A24207 CONTROL VALVE BOEING 737 7377H4 1384404 NM ELEVATOR TAB FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 DURING SCHEDULED HC2 CHECK, ELEVATOR TAB CONTROL SYSTEM FAILED CHECK. REMOVED AND REPLACED TAB CONTROL VALVE PER MM. 2 L 7 2 4F RT A16WE 2008040300110 20080403 00110 NM 2008 4 3 ASAA0872799 1 20080326 A 5753 113A210042 SKIN BOEING 737 737790 13844CN NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 607AS 29751 RT INBOARD MAIN FLAP O/B UPPER PANEL (653ET) HAS NUMEROUS DENTS AT UPPER SURFACE RT INBD MAIN FLAP OUTBD UPPER PNL. REP AIRED IAW B737 700 SRM CH 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008032400166 20080324 00166 NM 2008 3 24 SWAA081362 1 20080312 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 DURING SCHEDULED HC2 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008032400167 20080324 00167 EU 2008 3 24 08FDEA00944 1 20080314 A 5700 A5795617300300 FAIRING AIRBUS 310 A310 EU RT WING DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT WING FAIRING 634 AT IS DENTED AND DELAMINATED. REPAIRED IAW SRM 57-20-35. 2 L 7 2 4F RT A35EU 2008032400168 20080324 00168 EU 2008 3 24 08FDEA00946 1 20080314 A 5753 A5796505000100 FAIRING AIRBUS 310 A310203 3930313 EU TE FLAP ERODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FWD FLAP FAIRING 634 AB/BB; FWD END IS ERODED. REPAIRED ERROSION BY REMOVING THE DAMAGE AND APPLIED A WET LAY UP IAW A3 10 SRM 57-20-35. 2 L 7 2 4F RT A35EU 2008032400169 20080324 00169 EU 2008 3 24 08FDEA00947 1 20080314 A 5753 A5796505000100 FAIRING AIRBUS 310 A310203 3930313 EU TE FLAPS DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FWD FLAP FAIRING 634 AB/BB LOWER AFT END IS DENTED. REPAIRED DENT BY REMOVING THE DAMAGE AND APPLYING A WET LAY UP. 2 L 7 2 4F RT A35EU 2008032400171 20080324 00171 WP 2008 3 24 08FDEA00949 1 20080314 A 5320 15F5255501 INTERCOSTAL DOUG MD10 MD1010F 3022112 WP BS 806 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 FWD LOWER CARGO BILGE INTERCOSTAL STRUCTURE IS CRACKED AT BS 806; RBL 40.0 REMOVED INTERCOSTAL AND PLUGGED HOLES IAW DC/ MD-10 SRM 51-31-01; VOL II; PGS 1 - 10 AND EA NR 8-5320-118449 "FUSELAGE MID LAV WASTE LINT SUPPORT BRACKET - REMOVAL". 2 L 7 3 4F RT A22WE 2008032600062 20080326 00062 EU 2008 3 26 08FDEA01015 1 20080318 A 5420 A54612546 FITTING AIRBUS 300 A300B4622R 3930312 EU NR 1 PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND ON PYLON NR 1 SPIGOT FITTING WITH CORROSION AROUND BEARING SEAT. REPAIR PERFORMED BY REPLACEMENT OF SPIGOT FITTIN G IAW SB 54-6017, APPROVED BY EA 6-5451-114936. 2 L 7 2 4F RT A35EU 2008032600074 20080326 00074 NM 2008 3 26 HA0800412 1 20080314 A 5754 114T4101 DOUBLER BOEING 767 767332 1382001 NM L/E SLAT DEBONDED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 LE SLAT POSITION NR 5 TE WEDGE INBOARD TOP END. PREVIOUS REPAIR DOUBLER HAS DISBONDED. REPAIRED PER SRM 57-43-01 AND S RM 51-70-10 (REV 76). 2 L 7 2 4F RT A1NM 2008032600076 20080326 00076 NM 2008 3 26 HA0800414 1 20080314 A 5512 184T10061 PANEL BOEING 767 767332 1382001 NM HORIZ STAB DENTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 DENT ON LT HORIZONTAL STABILIZER LE PANEL 332BL. PERMANENT SRM REPAIR CARRIED OUT PER SRM 51-70-10, REF ANZ T1 19011361 5-0001 AND HAL FILE NR 594051. 2 L 7 2 4F RT A1NM 2008032600077 20080326 00077 NM 2008 3 26 HA0800415 1 20080314 A 5512 184T10061 PANEL BOEING 767 767332 1382001 NM HORIZ STAB DENTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 DENT ON LT HORIZONTAL STABILIZER LE PANEL 332BL. PERMANENT SRM REPAIR CARRIED OUT PER SRM 51-70-10, REF ANZ T1 19011361 5-0001 AND HAL FILE NR 594051. 2 L 7 2 4F RT A1NM 2008032600078 20080326 00078 NM 2008 3 26 DL76S080359 1 20080313 A 5343 ATTACH FITTING BOEING 767 767332 1382001 NM NLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 NLG W/W LT AND RT NLG TRUNNION ATTACH FITTINGS. CORROSION IN FITTING BORES AND TOOLING DAMAGED FASTENER HOLES. OVERSIZ ED BORES AND INSTALLED NEW ENLARGED BUSHINGS. 2 L 7 2 4F RT A1NM 2008032600079 20080326 00079 2008 3 26 DL76G080360 4 20080313 A 2565 PIN BOEING 767 767332 1382001 NM EVAC SLIDE LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1612T 30575 L2 SLIDE LOCK BALL PINS ARE LOOSE. REMOVED AND REPLACED L2 DOOR SLIDE/RAFT. 2 L 7 2 4F RT A1NM 2008032600081 20080326 00081 NM 2008 3 26 DL764080363 1 20080313 A 3350 SWITCH BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL COCKPIT INTERMITTENT A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 834MH 29707 P1828 EMERGENCY LIGHTS ILLUM WITH ALL EMERG SWITCHES IN OFF DISARMED POSITION WHEN EXTERNAL PWR TURNED OFF. FOUND EMERGENCY L IGHTS ARMING SWITCH INTERMITTENT. REPLACED PANEL, CHKS GOOD PER AMM. 2 L 7 2 4F 4 F RT A1NM E23EA 2008032600082 20080326 00082 NM 2008 3 26 DL764080364 1 20080313 A 3597 PIN BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL COCKPIT BACKED OUT A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 834MH 29707 P1828 DURING CHK OF EMERGENCY LIGHTS/OXY PANEL FOUND MANUAL DEPLOYMENT FAIL. FOUND K466 ON P19 BAD ALSO PIN 3 OF RELAY SOCKET PUSHED BACK. RESECURED PIN 3 AND REPLACED RELAY K466 CHKS GOOD PER AMM. 2 L 7 2 4F 4 F RT A1NM E23EA 2008032600084 20080326 00084 NM 2008 3 26 DLM88080366 1 20080313 A 5330 593805085 DOUBLER DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 939DL 49812 THE FWD LAV SERVICE CUTOUT SURROUND DOUBLER WAS CORRODED NEAR THE LOWER FWD CORNER. THE FUSELAGE SKIN AND DOUBLER WAS C UT TO REMOVE THE DAMAGE AND A REPAIR WAS INSTALLED. 2 L 7 2 4F RT A6WE 2008032600087 20080326 00087 NM 2008 3 26 DL76G080371 1 20080313 A 3350 LIGHT BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1612T 30575 SEAT EMERGENCY LIGHTS AT 1A, 2A, 4A, 3G, 17G ARE INOP. RELAMPED SEAT EMERGENCY LIGHTS AT SEATS 1A, 2A, 4A, 3G, AND 17G, NO FAULTS NOTED ON OPS CHECK IAW B767-300 AMM 33-51-10. 2 L 7 2 4F RT A1NM 2008032600089 20080326 00089 NM 2008 3 26 DL76G080372 1 20080313 A 3350 LENS BOEING 767 767332 1382001 NM EMERGENCY SIGN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1612T 30575 RT OVERHEAD AISLE EMERGENCY EXIT SIGN MISSING LENS. REMOVED AND REPLACED EMERGENCY EXIT SIGN LENS IAW DAL B767-300 AMM 33-51-01,TIMCO HMV CARD 41147 2 L 7 2 4F RT A1NM 2008032600092 20080326 00092 NM 2008 3 26 DL76G080373 1 20080313 A 3597 WIRE BOEING 767 767332 1382001 NM DOOR ACTUATOR DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1612T 30575 OXYGEN MASK AT FWD MID LAV AND 28AB DID NOT DEPLOY. RECONNECTED CONNECTOR FOR FWD MID LAV DOOR ACTUATOR IAW B767-300 AM M 35-21-16. REPAIRED WIRES FOR 28AB DOOR ACTUATOR IAW SWPM 20-10-13. MANUAL DEPLOY GOOD IAW B767-300 AMM 35-21-00. 2 L 7 2 4F RT A1NM 2008032600102 20080326 00102 NE 2008 3 26 DLM88080376 2 20080315 A 7250 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 DAMAGED A DALA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 27 904DL 47813 49535 718233 NR 1 ENGINE FAILURE ON T/O ROLL, HIGH VIBE ENGINE SHUT DOWN HOT SECTION MISSING BLADES ETC. REMOVED AND REPLACED NR 1 E NGINE PER TRANS 9T102. 2 L 7 2 4F 4 F RT A6WE E9NE 2008032600109 20080326 00109 NM 2008 3 26 DL76L080377 1 20080315 A 2910 271002252 ACTUATOR BOEING 767 767332 1382001 NM HYDRAULIC SYS DAMAGED A DALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 27 188DN 2016 27583 LOST CENTER SYS HYD QTY DURING CLIMB. C/W QRH PROCEDURE FOR C SYS HYD FAILURE. FOUND LCCA IN RIGHT W/W WITH BLOWN FILTE R CAP. WAITING ON LCCA FROM LAX. REMOVED AND REPLACED CTR LCCA PER AMM. LEAK CHECKS OK. PERFORMED RII INSP PER TOPPS 40-30-05. LCCA INSTALLATION CKS OK. 2 L 7 2 4F RT A1NM 2008032600110 20080326 00110 2008 3 26 2008UALA01554 4 20080318 A 2565 416N20021060 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 577UA 26693 DOOR 1L MOUNTED ESCAPE SLIDE BOTTLE PRESSURE AT THE LOW END OF THE GREEN BAND AFTER 2 HOURS. FOUND SLOW LEAK ON SLIDE B OTTLE. REPLACED ESCAPE SLIDE ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022700069 20080227 00069 NM 2008 2 27 ASAA0842553 1 20080117 A 5320 SILL BOEING 737 7374S3 1384711 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CABIN R2 DOOR SILL CHORD FOUND CORRODED AT BS 947+10 TO BS 988. SILL CHORD REPLACED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008022700078 20080227 00078 NM 2008 2 27 ASAA0842562 1 20080115 A 5347 65468136 SEAT TRACK BOEING 737 7374S3 1384711 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 SEAT TRACK GOUGED (2 PLACES) AT BS 536 LBL 45. REPLACED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008022700094 20080227 00094 NM 2008 2 27 SWAA080899 1 20080218 A 3397 W41420113 WIRE BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 440LV 29835 EEPLS INOP AT ROW 4 ABC. FOUND LOOSE WIRES AT EEPLS CONNECTOR. SECURED CONNECTOR PER WDM. 2 L 7 2 4F RT A16WE 2008022700097 20080227 00097 2008 2 27 SWAA080879 4 20080214 A 2565 D313591478 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008022700106 20080227 00106 NM 2008 2 27 SWAA080932 1 20080219 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022700114 20080227 00114 WP 2008 2 27 IXXA08SMN021S 1 20080119 A 5330 SKIN DOUG DC8 DC862F 3021972 WP ZONE 100 WORN B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CABIN COMPARTMENT SKIN WORN AT STATION FS 340 L21L. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTENT REPAIR. REMOVED DAMAGE AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORRO SION DETECTED AFTER INSPECTION. FABRICATED REPAIR DOUBLERS, REPAIR TRIPLERS, FILLERS, AND FINGER DOUBLERS. CLEANED, TR EATED, PRIMED AREA, AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-9 DATED 02-01-08, MESS AGES 1-760836333-2 DATED 02-01-08 AND 1-752082423-7 DATED 01-22-08, AD-2006-03-04 S/B 53-079 REVISION 2, DRAWING SR08530 027, ROD SKETCH 200801150024, DRAWING ED-4684-1, SRM 51-1-20D, NDT SPM PART 06-10-01-001, 2 L 7 4 4F 4A25 2008022700119 20080227 00119 NM 2008 2 27 SWAA080940 1 20080219 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700123 20080227 00123 NM 2008 2 27 ASAA0842580 1 20080109 A 5320 6941473628 INTERCOSTAL BOEING 737 7374S3 1384711 NM FSUELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO COMP INTERCOSTAL AT STA 500A RBL 27 IS CRACKED. INTERCOSTAL REPLACED. 2 L 7 2 4F RT A16WE 2008022700133 20080227 00133 CE 2008 2 27 195WA020508 1 20080205 A 5610 WINDOW BEECH 99 99 1154002 CE COCKPIT LEAKING E AXSA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 65 195WA U38 AIRCRAFT 195WA DEPART MPV-MHT FLIGHT 1057. 15NM FROM MPV THE PILOT NOTED SPARKS AND SMOKE COMING FROM THE CB PANEL WITH INSTRUMENT PANEL LIGHTS FLICKERING AND ATTITUDE INDICATOR CB POPPED. THE PILOT ADVISED ATC OF THE SITUATION AND RETURN ED TO MPV AND LANDED WITHOUT FURTHER INCIDENT. INSPECTION REVEALED WATER HAD LEAKED FROM THE WINDSHIELD INTO THE CB PAN EL CAUSING A SHORT CIRCUIT THAT RESULTED IN SMOKE AND SPARKS. THE AIRCRAFT WAS INSPECTED BY MAINTENANCE AND RELATED PAR TS WERE DRIED AND OPERATIONALLY CHECKED. INOPERATIVE SYSTEMS WERE DEFERRED IN ACCORDANCE WITH MEL PROCEDURES. THE LEAK ING AREAS WERE IDENTIFIED AND TEMPORARILY REPAIRED IN ORDER TO FERRY THE AIRCRAFT TO A MAINTENANCE FACILITY (MHT) FOR PE 1 L 7 2 3T A14CE 2008022700146 20080227 00146 NM 2008 2 27 UIEA200800045 1 20080215 A 5754 RIB BOEING 747 7472D7B 1384803 NM NR 12 K FLAP CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 NR 12 KRUGER FLAP INNER FACE UPPER BACKUP STIFFENER O/B END CRACKED. REPAIRED PER BOEING MESSAGE NR 1-748489952-4. 2 L 7 4 4F RT A20WE 2008022700174 20080227 00174 CE 2008 2 27 135763022008 1 20080217 A 8120 4066109028 TURBOCHARGER CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO ENGINE FAILED E HYIA E ENGINE SHUTDOWN R K J PARTIAL RPM/PWR LOSS FLUID LOSS WARNING INDICATION LD LANDING 1 EA 61 763EA 2401 2401 402C0497 832030R THE MANIFOLD PRESSURE DROPPED TO AMBIENT AND OIL PRESSURE DECREASED SHORTLY THERE AFTER. PILOT PERFORMED PRECAUTIONARY ENGINE SHUT DOWN. MAINTENANCE INSPECTED ENGINE AND FOUND BAD TURBOCHARGER AND REPLACED. MAINTENANCE PERFORMED PRECAUTI ONARY OIL FILTER, AND PROPELLER GOVERNOR SCREEN INSPECTION, AND INSTALLED MEB-009 FOR POSSIBLE ICE BUILD UP IN OIL SCAVE NGE LINES. 1 L 7 2 3O 3 O A7CE E8CE 2008022700188 20080227 00188 NM 2008 2 27 08FDEA00591 1 20080225 A 5315 FLOORBEAM BOEING 757 75727B 1384921 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 CORROSION ON FLOORBEAM AT STA 1280, RBL6, RBL10, RBL14. CORROSION FOUND EXCEED LIMITS IN SRM 53-00-51 FIG 101. REPAIR C ARRIED OUT IAW SRM 53-00-51, REPAIR 3, FIG. 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 2 4F RT A2NM 2008022700202 20080227 00202 EU 2008 2 27 Y2LA200800008 1 20080207 A 3411 STATIC PORT AIRBUS A319 A319112 3930323 EU PITOT/STATIC SYS SCRATCHED A Y2LA K NONE O OTHER UK UNKNOWN 1 GL 07 572SX 1963 CAPTAINS STATIC PORT ON RIGHT HAND SIDE HAS SCRATCH IN RVSM CRITICAL AREA. REPAIRED SCRATCH ON CAPTAINS STATIC PORT ON RIGHT HAND SIDE OF AIRCRAFT PER SRM 53-11-11. FOUND SCRATCH TO BE IN LIMITS PER SRM 53-00-11. RVSM NOT AUTHORIZED MAIN TENANCE CONTROL NOTIFIED. COMPLIED WITH A319 RVSM CRITICAL WAVINESS CHECK IAW 53-00-11. 2 L 7 2 4F RT A28NM 2008022700269 20080227 00269 NM 2008 2 27 UIEA200800022 1 20080127 A 3244 314799 TIRE BOEING 747 74747UF 1384812 NM MLG FAILED A UIEA O OTHER E C VIBRATION/BUFFET F.O.D. TO TAKEOFF 1 EA 15 498MC 29259 ON TAKEOFF OUT OF PVG NR 9 AND 10 WHEELS RUPTURED. THIS CAUSED DAMAGE TO STRUT DOORS WHEEL WELL DOORS AND PNEUMATIC DUC TING. BOTH TIRES RIMS AND BRAKES DAMAGED. REPLACED BRAKES WHEELS AND DOOR STRUT. PERFORMED REPAIR TO DUCT. MAINTENAN CE FERRY FLIGHT TO HKG FOR PERMANENT REPAIRS. 2 L 7 4 4F RT A20WE 2008022700329 20080227 00329 NM 2008 2 27 SWAA080880 1 20080216 A 2150 20405011 ACM BOEING 737 7373H4 1384600 NM A/C BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 346SW 24153 FLIGHT ATTENDANT REPORTED STRONG EXHAUST TYPE SMELL DURING CLIMB AND DESCENT. REMOVED AND REPLACED RT ACM PER MM. 2 L 7 2 4F RT A16WE 2008032400172 20080324 00172 NM 2008 3 24 SWAA081364 1 20080312 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2008032400174 20080324 00174 NM 2008 3 24 SWAA081363 1 20080312 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008032400176 20080324 00176 EU 2008 3 24 08FDEA00951 1 20080314 A 5340 A5361155629804 FITTING AIRBUS 310 A310324 3930206 EU L1 DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 L-1 LOWER AFT SEALING SECTION CORNER HAS A DOUBLE DRILLED HOLE. REMOVED AND REPLACED WITH NEW FITTING PART NR A53611556 29804; PO 611014.1 IAW A310 SRM 51-40-21; PG 7. 2 L 7 2 4F RT A35EU 2008032400178 20080324 00178 NM 2008 3 24 SWAA081372 1 20080312 A 5712 6545445 RIB BOEING 737 7375H4 138449D NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND LT WING LOWER RIB CHORD CRACKED AT STA 135, STR 2. REPAIRED CHORD PER ACO. 2 L 7 2 4F RT A16WE 2008032400186 20080324 00186 NM 2008 3 24 SWAA081374 1 20080312 A 5315 6545810 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 1. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2008032400187 20080324 00187 NM 2008 3 24 SWAA081375 1 20080312 A 5315 6545815 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 1 TO LBL 9. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2008032400189 20080324 00189 NM 2008 3 24 PIDA08013 1 20080308 A 2150 20405011 ACM BOEING 737 737291 138448W NM A/C BAY FAULTY A PIDA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 05 583CC 21069 APU MISTING OIL IN CABIN ON PACS 1 OR 2. FERRIED AT AIRCRAFT TO INT FOR MAINTENANCE. TROUBLESHOT APU AND OIL SYSTEM, N O FAULT FOUND. RT ACM BY PASSING OIL CAUSING SMOKE IN CABIN. REMOVED AND REPLACED RT ACM, OP'S CHECKS GOOD IAW B737 MM 21-51-11. 2 L 7 2 4F A16WE 2008032400190 20080324 00190 NE 2008 3 24 AALA200800484 2 20080303 A 7310 PRESSURE SWITCH AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE ENGINE FUEL INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 70073 516 BWI INFLIGHT T613/03MAR JFK TO MIA - NUMBER TWO ENGINE FUEL FILTER CLOG LIGHT ILLUMINATED. LANDED BWI WITHOUT INCIDENT . REPLACED THE NUMBER TWO ENGINE FUEL FILTER AND FUEL FILTER DIFFERENTIAL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F 4 F RT A35EU E13NE 2008032400191 20080324 00191 NM 2008 3 24 AALA200800485 1 20080303 A 2612 SMOKE DETECTOR BOEING 777 777223 1385213 NM CARGO BAY FALSE INDICATION A AALA F J A ACTIVATE FIRE EXT. DUMP FUEL UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 780AN 29956 GLA INFLIGHT T137/03MAR LHR TO LAX - CREW REPORTED CARGO FIRE AFT EICAS AND FIRE WARNING LIGHT. FIRE BOTTLES WERE DISCH ARGED AND FLIGHT DIVERTED TO GLA AND LANDED WITHOUT INCIDENT. NO EVIDENCE OF FIRE OR SMOKE FOUND. REPLACED AFT CARGO S MOKE DETECTOR AND REPLACED FIRE EXTINGUISHER BOTTLES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032400193 20080324 00193 NM 2008 3 24 AALA200800482 1 20080303 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032400194 20080324 00194 NM 2008 3 24 AALA200800483 1 20080303 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW - EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032400195 20080324 00195 WP 2008 3 24 AALA200800478 1 20080303 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 289AA 49301 JFK - EMERGENCY LIGHTS AT SEAT ROWS 8DEF TO 19DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 8DEF TO 19DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008032400196 20080324 00196 NM 2008 3 24 AALA200800479 1 20080303 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 681AA 25338 MIA - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 12AB INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 12AB. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008032400197 20080324 00197 NM 2008 3 24 2008UALA01144 1 20080302 A 2421 520854 CONTROL PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HMG SHORTED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 598UA 28751 HMG FAILED OP CHECK. HMG CONTROL PANEL SHORTING. REPLACED HMG CONTROL PANEL, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032400201 20080324 00201 NM 2008 3 24 2008UALA01356 1 20080311 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FWD PIT DOOR CUTOUT, FWD FRAME, AT LOWER STOP FITTING HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED: REPLACED FWD PIT DOOR CUTO UT FWD FRAME. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022700331 20080227 00331 NM 2008 2 27 UIEA200800055 1 20080215 A 5340 STRINGER CLIP BOEING 747 7472D7B 1384803 NM ZONE 100 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 AFT CARGO COMPARTMENT STRINGER 44 LEFT CLIP CORROSION AT STATION 1680, LEVEL 1 CORROSION. REPLACED CLIP PER SRM 51-10-0 1. 2 L 7 4 4F RT A20WE 2008022700332 20080227 00332 NM 2008 2 27 SWAA080896 1 20080215 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008022700333 20080227 00333 NM 2008 2 27 SWAA080897 1 20080215 A 5330 65C33756 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700335 20080227 00335 NM 2008 2 27 UIEA200800057 1 20080215 A 5313 STRINGER BOEING 747 7472D7B 1384803 NM ZONE 100 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 AFT CARGO COMPARTMENT STA 1890 STRINGER 46 CORRODED. REMOVED CORROSION PER SRM 51-10-01. REPROTECTED PER 51-10-02. 2 L 7 4 4F RT A20WE 2008022700345 20080227 00345 NM 2008 2 27 SWAA080861 1 20080217 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022700346 20080227 00346 NM 2008 2 27 SWAA080862 1 20080217 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022700347 20080227 00347 NM 2008 2 27 SWAA080863 1 20080217 A 5311 6545808 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, STR 7R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700354 20080227 00354 NM 2008 2 27 SWAA080885 1 20080213 A 2740 AR7077M3 MOTOR BOEING 737 7373H4 1384600 NM HORIZ STAB FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED HC1 CHECK, FOUND JACKSCREW GIMBAL HITS STABILIZER JACKSCREW NOSE DOWN STOP WITH FLAPS DOWN. REMOVED AN D REPLACED MAIN ELECTRIC STABILIZER MOTOR PER MM. 2 L 7 2 4F RT A16WE 2008022700355 20080227 00355 2008 2 27 SWAA080903 4 20080218 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008022700357 20080227 00357 NM 2008 2 27 SWAA080875 1 20080218 A 5310 6547959 DOOR FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME UPPER CRACKED. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008022800002 20080228 00002 NM 2008 2 28 UPS08551676 1 20080214 A 5610 HANDLE BOEING 757 75724APF 1384969 NM COCKPIT OUT OF ADJUST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 471UP 28842 INSPECTION TYPE:N/AQ CAPTAIN'S SIDE WINDOW UNLATCH HANDLE REQUIRES TREMENDOUS FORCE TO UNLATCH. PERFORMED ADJ/TEST REF AMM 56-11-02-5 PG 5 TASK S825-014. ADJUSTED WINDOW OPERATION CRANK TO FWD POSITION BELOW HORIZONTAL LINE. WINDOW NOW O PERATES PROPERLY PER B757 AMM. OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A2NM 2008022800009 20080228 00009 EU 2008 2 28 08FDEA00613 1 20080226 A 5520 STRUCTURE AIRBUS 310 A310324 3930206 EU LT ELEVATOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 LEFT ELEVATOR LEADING EDGE INTERIOR; FWD OF THE OUTBOARD ACTUATOR IS CORRODED. REMOVED AND REPLACED IAW AMM 27-31-24. PERFORMED A FUNCTIONAL TEST OF THE ELEVATOR REF AMM 27-31-00; TEST GOOD. REMOVED AND REINSTALLED ACCESS PANELS 335 AB; 335BB; 335CB; 335DB AND 3356EB REF A310-300 AMM 55-22-13. 2 L 7 2 4F RT A35EU 2008022800027 20080228 00027 WP 2008 2 28 UPS08851677 1 20080102 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT NOT SEATED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WILL NOT ARM. RESEATED BATTERY PACK. OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 2008022800030 20080228 00030 EU 2008 2 28 UPS08151682 1 20080217 A 2120 UNKNOWN AIRBUS A300 A300F4622R 3930360 EU COCKPIT SMOKE A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 135UP 0818 INSPECTION TYPE:N/A SMOKE IN COCKPIT ORIGINATING FROM CENTER CONSOLE APU ELEC & AIR W/PACKS ON IR'S WHEN IN AUGMENT ACCO MPLISHED SHUTDOWN. SECURE CHECK LIST AND EVACUATED AIRCRAFT. INPS LOWER E/E FOR OVERHEATED UNITS AND TRIPPED C/B'S. N OTHING FOUND IN LWR ELEC COMPT. REMOVED ALL CENTER CONSOLE UNITS & EXAMINED WIRING IN AFFECTED AREA. NO DAMAGE OR HEAT EVIDENCE SHOWN. POWERED UP A/C W/ELEC, PNEU & HYD AND OPERATED NORMAL CONFIGURATION. 2 L 7 2 4F RT A35EU 2008022800032 20080228 00032 NM 2008 2 28 HALA0800278 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 478 S37-38R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE STA 478 LONG 37R AND 38R, FASTENER CLEANED/PRIMED/PAINTED. FASTENER TO BE REPAIRED PER SRM 53-00-01 AND SRM 53-00-01. REPAIR NR 8 AT OR BEFORE 50 FLT CYCLES. 2 L 7 2 4F RT A1NM 2008022800035 20080228 00035 NM 2008 2 28 HALA0800270 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 132 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 132.5 AT 6 O'CLOCK POSITION, MARKED NR 6, AREA INSPECTED. FASTENER DAMAGE W/I ALLOW ABLE LIMITS AS PER SRM 53-00-01/101. FASTENER CLEANED, PRIMED, AND PAINTED. FASTENER REQ'D TO BE REPAIRED AS PER SRM 5 3-00-01 REPAIR 8. 2 L 7 2 4F RT A1NM 2008032400206 20080324 00206 NM 2008 3 24 SWAA081381 1 20080313 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739D, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032400211 20080324 00211 2008 3 24 SWAA081401 4 20080313 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032400212 20080324 00212 NM 2008 3 24 SWAA081385 1 20080313 A 5330 65C381921 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400217 20080324 00217 NM 2008 3 24 SWAA081387 1 20080313 A 5330 65C381921 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 482, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400218 20080324 00218 NM 2008 3 24 SWAA081388 1 20080313 A 5330 6545766 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400221 20080324 00221 NM 2008 3 24 SWAA081390 1 20080313 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032400257 20080324 00257 NM 2008 3 24 SWAA081409 1 20080313 A 5315 6546813 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 512A, RBL 14. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 2008032400258 20080324 00258 NM 2008 3 24 SWAA081410 1 20080313 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008032400259 20080324 00259 NM 2008 3 24 SWAA081396 1 20080313 A 5330 6545765 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506D, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400261 20080324 00261 2008 3 24 SWAA081408 4 20080313 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032400262 20080324 00262 2008 3 24 SWAA081397 4 20080313 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032400264 20080324 00264 NM 2008 3 24 SWAA081399 1 20080313 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 748SW 29800 DURING SCHEDULED HC1 CHECK, RIGHT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008032400265 20080324 00265 NM 2008 3 24 SWAA081400 1 20080313 A 3350 417A5600201 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 754SW 29849 RIGHT AFT CABIN EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008032400268 20080324 00268 NM 2008 3 24 SWAA081412 1 20080316 A 5330 65C381921 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400273 20080324 00273 NM 2008 3 24 2008UALA01359 1 20080311 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN IMPROPER PART A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 SEAT EEL LIGHT WORN INSTALL (NOT ARROW MARK TYPE). INSTALLED EEL LIGHT, 2 L 7 4 4F 4 F RT A20WE E24NE 2008022800039 20080228 00039 NM 2008 2 28 HALA0800302 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 375 S37-38R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 375 BETWEEN LONGERONS S37R AND S38R. CLEANED, TREATED AND PRIMED PER SRM 53-00-01 P AINT PEND, AREA PAINTED AS PER SRM 51-22-01. 2 L 7 2 4F RT A1NM 2008022800048 20080228 00048 GL 2008 2 28 UPS08651683 2 20080216 A 7311 1601425 HEAT EXCHANGER BOEING 767 76734AF 1385212 NM GE CF6 CF680C2* GL LT ENGINE LEAKING A IPXA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 327UP 27753 INSPECTION TYPE:ETOP DIVERSION - FUEL LEAK ON LT ENG, LT ENG SHUT DOWN AS PER CHECKLIST. REPLACED FUEL/OIL HEAT EXCHANG ER PER MM 79-21-01-4. PERFORMED ENG RUN CHECK 40 MIN INCLUDE HI PWR PER MM 71-00-00 AND NO FUEL LEAK NOTED. ACCOMPLISH ED WINDMILLING INSP PER MM 72-00-00-6. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E23EA 2008022800054 20080228 00054 NM 2008 2 28 HALA0800332 1 20080218 A 5510 TRACK BOEING 717 717200 1383700 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION ON VERTICAL STAB RT EXTERIOR SURFACE AFT OF HORIZ STAB ROLLER TRACK. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800062 20080228 00062 EU 2008 2 28 08FDEA00608 1 20080226 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION FOUND ON RT WING BOTTOM SKIN RIB 1-2 AND REAR SPAR AND AFT OF REAR SPAR. REPAIR PERFORMED BY REWORK OF CORROS ION AND OVERSIZING THE HOLES IAW RAS/BAE/1006320/2008 ISS A, APPROVED BY EA 6-5720-114867. 2 L 7 2 4F RT A35EU 2008022800064 20080228 00064 NM 2008 2 28 HALA0800296 1 20080217 A 5280 STRUCTURE BOEING 717 717200 1383700 NM LT MLG DOOR CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 SURFACE CORROSION AND PAINT PEELING ON LT MLG DOOR ON LEADING EDGE, REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800075 20080228 00075 NM 2008 2 28 KCSA081092 1 20080220 A 5210 DOOR FRAME BOEING 747 747209B 138489B NM R1 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 R1 MAIN ENTRY DOOR FWD VERT FRAME CRACKED AT LOWER END. 2 L 7 4 4F RT A20WE 2008022800084 20080228 00084 NM 2008 2 28 SWAA080933 1 20080219 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800086 20080228 00086 NM 2008 2 28 HALA0800341 1 20080219 A 5280 CHANNEL BOEING 717 717200 1383700 NM RT MLG DOOR CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 CRACK ON RT MLG I/B DOOR, FWD "Z" CHANNEL. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800091 20080228 00091 NM 2008 2 28 SWAA080922 1 20080219 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800102 20080228 00102 NM 2008 2 28 HALA0800304 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 447 S37-38R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 447 BETWEEN LONGERONS S37R AND S38R. CLEANED, TREATED AND PRIMED PER SRM 53-00-01. PAINT PEND, AREA PAINTED AS PER SRM 51-22-01. 2 L 7 2 4F RT A1NM 2008022800103 20080228 00103 NM 2008 2 28 SWAA080945 1 20080219 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM CORRODED BETWEEN BS 520 AND BS 540, LBL 11. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2008022800105 20080228 00105 WP 2008 2 28 AALA200800272 1 20080208 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 410AA 49321 DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 18 TO 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHE AD SEAT ROWS 18 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022800108 20080228 00108 NM 2008 2 28 SWAA080951 1 20080219 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800112 20080228 00112 NM 2008 2 28 SWAA080950 1 20080219 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800114 20080228 00114 NM 2008 2 28 SWAA080946 1 20080219 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800115 20080228 00115 NM 2008 2 28 08FDEA00517 1 20080219 A 5320 STIFFENER DOUG MD11 MD11F 3023600 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 AFT FUSELAGE COMPT: AFT PRESSURE BULKHEAD VERTICAL STIFFENER AT STA 2007, X=-10 UPPER END FOUND CRACKED. REPAIR CARRIED OUT AS PER EA 1-5310-117418, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008022700110 20080227 00110 WP 2008 2 27 DHLA200800015 1 20080221 A 2530 3115HC RECEPTACLE DOUG DC8 DC873F 302199F WP GALLEY BURNED A DHLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 05 873SJ 46091 FLT 445 - SMOKE IN ENTRY WAY AND OR MAIN CABIN IN FLT. RAN ALL ENGINES PER JRH 11.8, NO SMOKE IN ENTRY OR MAIN CABIN. FOUND ELECTRICAL ODOR AT HOT CUP RECEPTICAL. TRANSFERRED "HOT CUP" TO DMI NR 31815, MEL REF 25-13. DMI EXPIRES JUNE 22 , 2008, CAT "D". GALLEY HOT CUP. C/B REMOVED AND REPLACED HOT CUP PN:3-115HC PER MM 25-30-1. OPS CK GOOD DMI 31815 CO NTINUES. AIRCRAFT WAS GROUNDED. 2 L 7 4 4F RT 4A25 2008022700128 20080227 00128 EU 2008 2 27 080048 1 20080118 A 2435 23080005 STARTER GEN BRAERO DH125 HS125700A 4230170 EU GARRTT TFE731 TFE731* 01518 WP LT ENGINE MALFUNCTIONED E DGCA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 9999V 921 NA0308 P84355 LEFT STARTER GENERATOR DROPPED OFF LINE. 2 L 7 2 4F 4 F A3EU E6WE 2008022700183 20080227 00183 NM 2008 2 27 08FDEA00589 1 20080223 A 5320 655756730 CHANNEL BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 AFT LWR CARGO BAY CENTER LINE FLOOR ANGLE AT BS 1035-1037 HAS CORROSION ON THE UNDERSIDE VERFIED MATERIAL FOR REPAIR PAR TS. FABRICATED REPAIR PARTS REF SRM 53-10-5, DWG SR27-53-039. REMOVED CORROSION, FOUND TO WITHIN LIMITS REF SRM 53-10- 1 FIG 4. TREATED PRIMED REPAIR PARTS REF SRM 51-10-2 MM 51-20-151-7. INSTALLED REPAIR SPLICE ANGLES REF SRM 53-10-5 FI G 4 DWG SRM 27-53-039. ORIGINAL MAT .063 REMOVED .008 REMAIN .055, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008022700185 20080227 00185 EU 2008 2 27 TRAX200800235 1 20080208 A 2560 COVER AEROSP ATR72 ATR72 EU EXIT SIGN CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 F/A REPORTS FLOOR LEVEL EXIT SIGN AT ROW 1 A/B HAS CRACKED COVER AND NOT LEGIBLE. 2 H 7 2 4T RT 2008022700191 20080227 00191 WP 2008 2 27 08FDEA00595 1 20080225 A 5347 60715817075T65 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 363FE 48263 SEAT TRACK LUGS WORN AT FS 900, 906 AND 935. TRACK 48L REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1. REPAIR PARTS FABRIC ATED ON TRAVILERS T8/725338 AND T8/725336. 2 L 7 3 4F RT A22WE 2008022700197 20080227 00197 NM 2008 2 27 WRNA200800005 1 20080205 A 5320 RIB BOEING 747 747230B 1384889 NM FUSELAGE BROKEN A WRNA K NONE O OTHER TX TAXI/GRND HDL 1 SO 05 508MC 21644 DURING CARGO LOADING, LOADED PALLET CONTACTED AND BROKE RIB, RIGHT HAND SIDE AT STA 1760, 8 FEET ABOVE WATER LINE. ACCO MPLISHED UNPRESSURIZED FERRY FLIGHT TO OSCODA MICHIGAN FOR REPAIRS. REPAIR ACCOMPLISHED IAW B747 SRM 51-40-03 FIGURE 2. AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008022700214 20080227 00214 NM 2008 2 27 200802141 1 20080211 A 2750 FLAP EMB ERJ170 ERJ170100SE 3260406 NM WING MALFUNCTIONED A UHLA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 11 869RW 17000133 FLIGHT 6457 ALT TO MSP FLAPS STOP AT FLAPS 1 AND WITH ZERO SLATS. NO FLAPS LANDING, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. MAINTENANCE CLEARED SF-ACE INHIBITS, AND RELEASED ELECTRONIC BRAKE. HAS NOT REPEATED THIS DATE 02/14/2008. 2 L 7 2 4F RT A56NM 2008022700228 20080227 00228 WP 2008 2 27 IXXA08SMN012S 1 20080115 A 5280 DOOR DOUG DC8 DC862 3021970 WP MLG DELAMINATED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING (MLG/FUSELAGE) UPPER DOOR DELAMINATED SKIN. REMOVED DAMAGED DOOR. I NSTALLED NEW DOOR. PERFORMED OPS CHECK FOR HYD SYSTEM LEAKS GOOD IAW DC8 MAINTENANCE MANUAL 32-12-1 PAGE 401, DC8 27-10 -0, 27-20-0, 27-40-0, 27-50-0, 27-60-0, 27-80-0, 27-00, 32-30-0, 32-42-0, 32-50-0, 52-36-1 AND 78-30-0. 2 L 7 4 4F 4A25 2008022700246 20080227 00246 NM 2008 2 27 KCSA081082 1 20080218 A 5340 STRINGER CLIP BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 STR 7R CLIP IS CORRODED AT BS 1540. 2 L 7 4 4F RT A20WE 2008022700249 20080227 00249 NM 2008 2 27 CAL08001433 1 20080216 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 68061 29456 WHILE REPLACING EMERGENCY LIGHT BATTERY AT STA 654 FOUND CHARGER WOULD NOT TEST. REPLACED BATTERY CHARGER PER AMM 33-51 -07. 2 L 7 2 4F RT A1NM 2008022700250 20080227 00250 NM 2008 2 27 CALA0800140 1 20080216 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 68061 29456 WHILE REPLACING EMERGENCY LIGHT BATTERY PACK AT STA 841 FOUND BATTERY CHARGER WOULD NOT TEST. REPLACED CHARGER PER AMM 33-51-07. 2 L 7 2 4F RT A1NM 2008022700271 20080227 00271 NM 2008 2 27 CALA0800151 1 20080215 A 5311 143A1111 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16709 28779 FRAME CRACKED AT STA 400 BETWEEN STRINGER 8R AND 9R. REPAIRED PER ECRA 5310-04717. 2 L 7 2 4F RT A16WE 2008022700288 20080227 00288 NM 2008 2 27 UIEA200800034 1 20080210 A 5330 SKIN BOEING 747 74747UF 1384812 NM BS 2200 S22-23L SCRATCHED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 415MC 32837 FOUND NICK ON FUSELAGE SKIN STATION 2200 STRINGER 22L-23L. REPAIRED AS PER SRM 53-00-01 REPAIR 1 DETAIL 3 FIGURE 201 AN D 53-60-01 FIGURE 1 AND SRM 51-40-06 FIGURE 3 2 L 7 4 4F RT A20WE 2008022700353 20080227 00353 NM 2008 2 27 SWAA080886 1 20080213 A 2740 654997025 JACKSCREW BOEING 737 7373H4 1384600 NM HORIZ STAB MALFUNCTIONED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED HC1 CHECK, FOUND HORIZONTAL STABILIZER MOTOR CONTINUES TO FREE WHEEL AFTER RELEASING SWITCH IN FLIGHT D ECK. REMOVED AND REPLACED STABILIZER JACKSCREWER MM. 2 L 7 2 4F RT A16WE 2008032400280 20080324 00280 NM 2008 3 24 HALA0800390 1 20080309 A 3230 SEQUENCE VALVE BOEING 767 767332 1382001 NM MLG CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 CORROSION ON MAIN L/G OPERATING SEQUENCE VLV ROD IN RT WHEEL WELL. REMOVED CORROSION AND CPC APPLIED AS PER SRM 51-10-0 2. 2 L 7 2 4F RT A1NM 2008032100019 20080321 00019 NM 2008 3 21 2008UALA01206 1 20080305 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 FOUND SEAT 1A FWD EMERGENCY LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032100021 20080321 00021 NM 2008 3 21 2008UALA01208 1 20080305 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 FOUND SEAT 42 ABC EMERGENCY LIGHT IS INOP. RESECURED LOOSE CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032100022 20080321 00022 NM 2008 3 21 2008UALA01209 1 20080305 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 FOUND SEAT 56 HJK EMERGENCY LIGHT IS INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032100023 20080321 00023 NM 2008 3 21 2008UALA01211 1 20080304 A 5270 PROXIMITY SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 525UA 24978 DOOR 1R SLIDE LT DOES NOT ILLUMINATE W/ DOOR CLOSED. FOUND DIRT AND DEBRIS CAUSING JAMMING, PROX SWITCH ALSO DIRTY. CLE ANED AREA AND PROX SWITCHES, SYSTEM OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100024 20080321 00024 NM 2008 3 21 2008UALA01223 1 20080305 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 365 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 FOUND MAIN CABIN FLOORBEAM AND PREVIOUS REPAIR CORRODED STA 365, RBL12. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032400002 20080324 00002 WP 2008 3 24 08FDEA00917 1 20080313 A 5710 ARB1180 TEE FITTING DOUG DC10 DC1030F 3023504 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 307FE 48291 RT WING INT ZONE L/E FOUND CRACK ON FIXED TEE CAP. REPAIRED TEE CAP IAW SRM 57-10-00 VOL I FIG 49. 2 L 7 3 4F RT A22WE 2008032400007 20080324 00007 EA 2008 3 24 COMA0880003 1 20080307 A 3250 WARNING SYSTEM CNDAIR CL600 CL6002D24 1390016 EA NLG STEERING MALFUNCTIONED A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 549CA 15164 FLIGHT 4685 - RECEIVED STEERING INOP CAUTION MESSAGE WHEN GEAR SELECTED DOWN. ABORTED APPROACH, PERFORMED QRH, DID NOT CLEAR. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED MWS OPS CHECK IAW AMM 32-51-00. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 2008032400019 20080324 00019 EU 2008 3 24 08FDEA01006 1 20080317 A 5522 A55276950 PANEL AIRBUS 310 A310203 3930313 EU LT ELEVATOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT ELEVATOR PANEL NR 335 CT IS CORRODED. REMOVED CORROSION IAW A310 SRM 51-74-10. ORIGINAL MATERIAL THICKNESS 0.080 IA W AIRBUS DWG 38; A55276950. REMOVED 0.001; REMAINING MATERIAL 0.079. FOUND TO BE WITHIN LIMITS IAW A310 SRM 55-22-00 ; TABLE 101. UT GAUGE NR T8225Q; CAL DATE 21/20/07. ALODINED IAW A310 SRM 51-21-10. PRIMED AND TOP COATED IAW A310 SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008032400025 20080324 00025 EA 2008 3 24 SWIA200819341 1 20080307 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 440SW 7589 FLT 3934 - EMERGENCY EXIT SIGN AT CENTER CABIN IS INOP. RELAMPED AS REQUIRED. 2 L 7 2 4F RT A21EA 2008032400029 20080324 00029 EA 2008 3 24 HNAA0800100 1 20080307 A 5350 4426X210 RADOME DHAV DHC8 DHC8311 1386006 EA FUSELAGE DAMAGED A HNAA O OTHER O OTHER CR CRUISE 1 EA 07 327EN 43206 848 261 ENCOUNTERED LIGHTNING STRIKE, INFLIGHT SYSTEM CHECK GOOD. INSPECTED AIRCRAFT, EVIDENCE OF BURN MARKS ON RIGHT HAND SIDE OF RADOME, WILL FERRY AIRCRAFT TO ROA. REMOVED AND REPLACED RADOME. 2 H 7 2 4T RT A13NM 2008032400039 20080324 00039 WP 2008 3 24 08FDEA00923 1 20080313 A 5313 ADA3064 STRINGER DOUG MD10 MD1010F 3022112 WP BS 1019-1039 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 FWD CARGO COMPARTMENT BILGE AREA; FOUND CORROSION ON STRINGER 52 OUTBD FACE; FROM FS 1019-1039. REMOVED CORROSION IN RE FERENCE WITH SRM 51-21-01; VOL II; PG 28. ORIGINAL THICKNESS IS .090 IAW SRM 53-13-01; VOL III; ITEM 39. MATERIAL REM OVED IS .002. MATERIAL REMAINING IS .088. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01; VOL I; FIG 1B. ALODINED AND PRI MED IN REFERENCE WITH SRM 51-21-01; VOL II; PGS 21 AND 25. 2 L 7 3 4F RT A22WE 2008032400185 20080324 00185 NM 2008 3 24 SWAA081373 1 20080312 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400214 20080324 00214 NM 2008 3 24 SWAA081386 1 20080313 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 513, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032400231 20080324 00231 NM 2008 3 24 DHL2008753501 1 20080227 A 5753 STRUCTURE BOEING 727 727223 1384074 NM TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 DURING "C" RT I/B MID FLAP LOWER T/E CHORD AT CUTOUT WBL 102 IS CRACKED. OPENED SECTION OF LOWER PANEL RT I/B MID FLAP T/E IAW SRM 51-30-2. REMOVED SEAL AND SEL RETAINER FOR ACCESS IAW SRM 51-30-2. CUTOUT DAMAGE AREA AT CHORD APPROX 70 I NCH. FAB NEW CHORD AND ONE SPLICE IAW SRM 57-50-2 FIG 5 AND 51-40-4 FIG 1. TREATED, PRIMED AND SEAL INSTALLED PARTS RE PAIR IAW SRM 51-10-2, 51-40-4 FIG 1. INSTALLED SEAL AND SEAL RETAINER IAW SRM 51-30-2. CLOSED LOWER PANEL RT I/B MID F LAP IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008022800003 20080228 00003 NM 2008 2 28 HALA0800303 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 378 S37-38R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 378 BETWEEN LONGERONS S37R AND S38R. CLEANED, TREATED AND PRIMED PER SRM 53-00-01. PAINT PEND AREA PAINTED AS EPR SRM 51-22-01. 2 L 7 2 4F RT A1NM 2008022800021 20080228 00021 NM 2008 2 28 HALA0800280 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 560 S37R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 560 AT LONGERON S-37R, MARKED NR 3, AREA INSPECTED. FASTENER DAMAGE W/I LIMITS AS P ER SRM 53-00-01/101. FASTENER CLEANED/PRIMED/PAINTED. FASTENER REQ'D TO BE REPAIRED AS PER SRM 53-00-01. REPAIR AT OR BEFORE 50 FLT CYCLES. OK TO CONTINUE PER SRM 53-00-01/101. 2 L 7 2 4F RT A1NM 2008022800036 20080228 00036 NM 2008 2 28 HALA0800271 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 133 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 133.5 AT 6 O'CLOCK POSITION, MARKED NR 7, AREA INSPECTED. FASTENER DAMAGE W/I LIMIT S AS PER SRM 53-00-01/101 FASTENER. FASTENER CLEANED/PRIMED/PAINTED. FASTENER REQ'D TO BE REPAIRED AS PER SRM 53-00-01 REPAIR 8 AT OR BEFORE 50 FLT CYCLES. 2 L 7 2 4F RT A1NM 2008022800037 20080228 00037 NM 2008 2 28 HALA0800272 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 164 DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 164.75 AT 6 O'CLOCK POSITION, MARKED NR 9, AREA INSPECTED. FASTENER DAMAGE W/I ALLO WABLE LIMITS AS PER SRM 53-00-01/101. FASTENER CLEANED/PRIMED/PAINTED. FASTENER REQ'D TO BE REPAIRED AS PER SRM 53-00- 0 1. REPAIR 8 AT OR BEFORE 50 FLT CYCLES. 2 L 7 2 4F RT A1NM 2008022800040 20080228 00040 NM 2008 2 28 HALA0800293 1 20080217 A 5280 INTERCOSTAL BOEING 717 717200 1383700 NM RT MLG DOOR CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 RT MLG DOOR INTERCOSTAL CRACKED SEEN INSIDE FWD MID ACCESS PANEL. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800049 20080228 00049 NM 2008 2 28 HALA0800343 1 20080219 A 5347 SEAT TRACK BOEING 717 717200 1383700 NM BS 737 CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 CRACK ON RT SIDE OUTBOARD SEAT TRACK SUPPORT BRACKET EAR, UNDER FLOOR BOARD AT FUSELAGE STA 737.00. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800067 20080228 00067 EU 2008 2 28 08FDEA00609 1 20080226 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION FOUND ON RT WING BOTTOM SKIN IN RIB 8 AND STRINGER 18 AREA. REPAIR PERFORMED BY BLEND OUT OF CORROSION, NDT F OR CRACK FREE AND OVERSIZING OF FASTENER IAW RAS/BAE/1006317/2008 ISS A, APPROVE DBY EA 6-5720-114868. 2 L 7 2 4F RT A35EU 2008022800069 20080228 00069 NM 2008 2 28 UPS08M51686 1 20080218 A 5754 SLAT DOUG MD11 MD11F 3023600 NM LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:N/A LT WING INBOARD SLAT AND LEADING EDGE DAMAGED APPROX 4 FT INBOARD OF PYLON. CUT OUT DAMAGE REF PREL IMINARY EO MD11-5730-28618A 6A(2). PERFORMED HFEC PER MD11 NDT SPM 06-10-01 001 IN REF W/EO MD11-5730-28618A. NO CRACK S NOTED AT THIS TIME. OK TO INSTALL PER QC. FAB'D AND INSTALLED REPAIR. 2 L 7 3 4F RT A22WE 2008022800077 20080228 00077 NM 2008 2 28 SWAA080929 1 20080219 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800094 20080228 00094 NM 2008 2 28 AALA200800277 1 20080209 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 360AA 24041 JFK - EMERGENCY LIGHT AT SEAT 6H INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 6H. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008022800095 20080228 00095 NM 2008 2 28 08FDEA00525 1 20080220 A 5711 6483331 SPAR BOEING 727 727233 138408A NM ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 LT WING LEADING EDGE FRONT SPAR FASTENER HOLE HAS NO EDGE DISTANCE AT WS 167, LE STA 90. REPAIRED IAW EA 7-5710-11695 7. 2 L 7 3 4F RT A3WE 2008022800101 20080228 00101 NM 2008 2 28 AALA200800286 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 22G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022800118 20080228 00118 SO 2008 2 28 CHQA200800037 1 20080222 A 2120 8166248 THERMOSTAT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FAN AIR FAULTED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 574RP 9450 9450 145845 CAE311908 CMH TO BOS - ON INITIAL CLIMB, THE CREW RECEIVED A MASTER WARNING AND EICAS MESSAGE FOR BLEED 2 OVERTEMP. AFTER RUNNING THE QRH, IT WAS DECIDED TO RETURN TO CMH, WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAUL T TO THE FAN AIR CONTROL THERMOSTAT, AND AFTER REPLACING IT, THE NUMBER 2 BLEED SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008022800120 20080228 00120 NM 2008 2 28 SWAA080935 1 20080217 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 346SW 24153 AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK AND BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 2008022800132 20080228 00132 WP 2008 2 28 AALA200800275 1 20080209 A 2810 TANK DOUG DC9 DC982 3022082 WP RT WING LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 408AA 49319 STL INFLIGHT T368/09FEB AUS TO ORD - RIGHT WING FUEL TANK LEAK AT BOOST PUMP COVER. RIGHT TANK QUANTITY SHOWED LOSS OF 100 POUNDS EVERY 3 TO 4 MINUTES. LANDED STL WITHOUT INCIDENT. FOUND SCREWS HOLDING FUEL PLATE BOTTOMED OUT. INSTALLED CORRECT LENGTH SCREWS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022800138 20080228 00138 NM 2008 2 28 SWAA080916 1 20080219 A 5312 6545409 PRESSURE PANEL BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE BEADED PRESSURE WEB CRACKED AT BS 664, LBL 40. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008022800140 20080228 00140 EA 2008 2 28 COMA0870008 1 20080218 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 371CA 10082 FLIGHT 5644 - ON TAKEOFF ROLL RECEIVED AVIONICS BAY DOOR CAUTION MESSAGE, ABORTED TAKEOFF AT LOW SPEED. INSPECTED AVION ICS BAY DOOR AND PROX SENSOR, NO DEFECTS NOTED. INDICATION IS WORKING PROPERLY. 2 L 7 2 4F RT A21EA 2008022800144 20080228 00144 EA 2008 2 28 COMA0860140 1 20080220 A 2497 601R5790015 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE FAULTY A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 932CA 7038 FLIGHT 5279 - RECEIVED IDG CAUTION MESSAGE. ABORTED APPROACH, PERFORMED QRH, LANDED WITHOUT INCIDENT. REPLACED NR 2 EN GINE VIOLET HARNESS. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008022800148 20080228 00148 NM 2008 2 28 KCSA081076 1 20080213 A 5230 SKIN BOEING 747 747209B 138489B NM CARGO DOOR DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 STA 2000 BULKPIT DOOR LOWER FWD EDGE HAS SKIN DAMAGE. 2 L 7 4 4F RT A20WE 2008022800155 20080228 00155 NM 2008 2 28 KCSA081100 1 20080221 A 5311 FRAME BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE FRAME UPPER CHORD CORRODED AT BS 2220, RBL 58, ABOVE STR-40R. 2 L 7 4 4F RT A20WE 2008022800156 20080228 00156 NM 2008 2 28 HALA0800214 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1014 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT LBL 88.5, STA 1014, MAX DEPTH BLENDED WAS 0.026". BLENDED IAW SRM 51-10-02 . ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022800158 20080228 00158 NM 2008 2 28 HALA0800224 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 927 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT RBL 54.75, STA 927, MAX DEPTH BLENDED WAS 0.008". BLENDED IAW SRM 51-10-02 . ALL BLEND OUT WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022800161 20080228 00161 NM 2008 2 28 DL76G080206 1 20080215 A 3697 CONNECTOR BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE PRSOV DIRTY A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 1609 30574 704749 INBOUND RT ENG HPSOV EICAS MSG, MTC PLACED HPSOV ON MEL-THENON TAXI OUT NO PNEUMATIC AIR FROM RT ENGINE, RTB-MTC THEN CL EANED PRSOV CONNECTOR. 2 L 7 2 4F 4 F RT A1NM E13NE 2008022800163 20080228 00163 NM 2008 2 28 DL76L080208 1 20080215 A 3000 VALVE BOEING 767 767332 1382001 NM OVERHEATED A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 175DN 24803 AFTER T/O AT JFK, AFT AND MID SMOKE DET WENT OFF, SMELL ALL OVER CABIN WAS NOTICED STRONG ENOUGH TO RETURN TO JFK. SMOK E AND FUMES REMOVAL AND ELEC SMOKE CKLIST RUN TO NO AVAIL. ELECTRICAL SYS TURNED OFF, NO EFFECT TAXIED TO GATE. INSP G ALLEYS/CHILLERS-COFFEE MAKERS-OVENS-LAVS. REMOVED AFT AND FWD CARGO AFT BULKHEADS. INSP EXHAUST FANS, LAV WASTE VENT FANS-RECIRC FANS-GASPER FAN, NO PROBLEM FOUND. INSPECTED A/C BAYS, FOUND LEFT BAY MID ZONE TRIM VLV OVERHEATED. REMOV ED AND REPLACED MID ZONE TRIM VLV. OPS CK OK. TAXIED A/C NO FAULT FOUND. PERF IFSDCK 1/2 ENGS. NO FAULT FOUND. 2 L 7 2 4F RT A1NM 2008022800164 20080228 00164 NE 2008 2 28 DLM88080212 2 20080216 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RIGHT DAMAGED A DALA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 27 944DL 49073 49817 718134 ON DEPARTURE, A LOUD BANG WAS HEARD FOLLOWED BY RIGHT ENGINE ROLLBACK. IDLE OIL PRESS OK. QRH FOLLOWED WITH NO OTHER SI GNIFICANT ISSUES NOTED. REPLACED RT ENGINE PER TRANSMITTAL 9T102. 2 L 7 2 4F 4 F RT A6WE E9NE 2008022800177 20080228 00177 NM 2008 2 28 KCSA081103 1 20080221 A 5320 STRAP BOEING 747 747209B 138489B NM FUSELAGE BROKEN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 AFT PIT STABILIZATION STRAP BROKEN AT BS 2220, RBL 25. 2 L 7 4 4F RT A20WE 2008022800187 20080228 00187 NM 2008 2 28 SWAA080967 1 20080220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800190 20080228 00190 NM 2008 2 28 DLM90080158 1 20080204 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM STA 588 LBL 58 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 LT CUSP WEB HAS CORROSION STA 588 LBL 58. REPAIRED CUSP WEB IAW MD-80 SRM 53-05D FIG 827D ON N/R 2700-0226 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008022800191 20080228 00191 NM 2008 2 28 DLM90080161 1 20080204 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM FS 585 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 CABIN SEAT TRACK GOUGED OUT OF LIMITS FS 585 LBL 22. REMOVED AND REPLACED DAMAGED PORTION OF SEAT TRACK IAW SRM 53-40-0 1 VOL 1 ON N/R 2700-0129 AT HMV-2 IN OKC. 2 L 7 2 4F RT A6WE 2008022800192 20080228 00192 NM 2008 2 28 SWAA080964 1 20080220 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 414WN 29820 DURING SCHEDULED 6Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767, LBL 13 TO LBL 17. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400232 20080324 00232 NM 2008 3 24 DHL2008753503 1 20080228 A 5753 STRUCTURE BOEING 727 727223 1384074 NM TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 DURING "C" CHECK LT I/B MIDFLAP T/E CHORD CRACKED WBL 124. OPENED SECTION OF LOWER PANEL I/B MID FLAP T/E IAW SRM 51-30 -2. REMOVED FASTENERS AND CUTOUT DAMAGED AREA AT CHORD APPROX 46 1/4 INCH. FAB NEW PART AND ONE SPLICE IAW SRM 57-50-2 FIG 5 AND 51-40-4 FIG 1. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED PARTS REPAIR IAW SRM 51-40-4. IN STALLED SEAL AND SEAL RETAINER AND CLOSED LOWER PANEL AT LT I/B MID FLAP IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032400248 20080324 00248 NM 2008 3 24 SWAA081402 1 20080313 A 5754 65C26602 SLAT BOEING 737 7375H4 138449D NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED. REPAIRED SLAT PER BOEING DRAWING AND SRM. 2 L 7 2 4F RT A16WE 2008032400272 20080324 00272 NM 2008 3 24 2008UALA01358 1 20080311 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 RIGHT OVERWING EMERGENCY LIGHT NOT ON 3RD AND 4TH. REPLACED LAMP. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032400275 20080324 00275 NM 2008 3 24 2008UALA01361 1 20080312 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY EXIT EEL LIGHT INOP AT DOOR 4 LEFT LOWER WALL CROSS AISLE IN GALLEY. SECURED CONNECTOR 2 L 7 4 4F 4 F RT A20WE E24NE 2008032400284 20080324 00284 NM 2008 3 24 HALA0800407 1 20080313 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE GOUGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 485HA 55130 GOUGE IN FUSELAGE NEAR REAR CARGO DOOR. EDDY CURRENT AREA, NO CRACK INDICATION. BLENDED AREA AND TREATED PER SRM 53-00 -01. OK AS IS PER SRM 53-00-01. 2 L 7 2 4F TR A6WE 2008032400285 20080324 00285 NM 2008 3 24 HALA0800410 1 20080313 A 5320 CHANNEL BOEING 767 767332 1382001 NM FUSELAGE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23275 LT STRUT AFT FAIRING CHANNEL OTBD, CRACKED AT FWD END. O/B AFT FAIRING CHANNEL PT NR 313T1380-241, REPLACED IAW SRM 51- 40-02, REV 76. 2 L 7 2 4F RT A1NM 2008032400287 20080324 00287 NM 2008 3 24 DHL2008763509 1 20080316 A 5753 SKIN BOEING 727 727264 138408M NM RT FORE FLAP CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 RT I/B FORE FLAP I/B L/E CHAFED AT RWBL 73. DAMAGE BEYOND SERVICE LIMITS. REMOVED, FABRICATED, AND INSTALLED SKIN PANE L, 2024-T3 .050 INCH BY 14 INCH BY 14.5 INCH, PONR 9006586, PER B727 SRM 57-50-2 FIG 3, 51-20-1, AND 51-30-2. 2 L 7 3 4F A3WE 2008032400291 20080324 00291 NM 2008 3 24 DHL2008763512 1 20080309 A 5280 SUPPORT ANGLE BOEING 727 727264 138408M NM MLG DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 RMLG BODY DOOR ACTUATOR HANGER SUPPORT ANGLE CRACKED AT BS 870. REMOVED, FABRICATED, AND INSTALLED SUPPORT ANGLE, 7075- T6 .100 INCH BY 3.75 INCH BY 3.375 INCH, PO NR 9005773, PER B727 SRM 53-10-2 51-20-1 AND 51-30-5. 2 L 7 3 4F A3WE 2008032400292 20080324 00292 NM 2008 3 24 DHL2008763513 1 20080307 A 5347 BAC1520841 SEAT TRACK BOEING 727 727264 138408M NM BS 760-850 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 SEAT TRACK CORRODED BS 760 TO 850, RBL 45. REMOVED AND REPLACED SEAT TRACK SECTION WITH BAC1520-841 EXTRUSION, PO NR 81 0987, 95 INCHES LONG, PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 2. 2 L 7 3 4F A3WE 2008032400293 20080324 00293 NM 2008 3 24 DHL2008763514 1 20080308 A 5347 BAC1520841 SEAT TRACK BOEING 727 727264 138408M NM BS 760-850 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 SEAT TRACK CORRODED BS 760 TO 850, RBL 25. REMOVED AND REPLACED SEAT TRACK SECTION WITH BAC1520-841 EXTRUSION, PO NR 81 0987, 95 INCH LONG, PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 2. 2 L 7 3 4F A3WE 2008032400294 20080324 00294 NM 2008 3 24 DHL2008763515 1 20080314 A 5347 652363753 SEAT TRACK BOEING 727 727264 138408M NM BS 500-720 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 SEAT TRACK DAMAGED BS 520 TO 540, LBL 45. REMOVED AND REPLACED SEAT TRACK SECTION WITH P/N 65-23637-53, PO NR 658565, 2 20 INCH LONG, PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 2. 2 L 7 3 4F A3WE 2008032400301 20080324 00301 NM 2008 3 24 DHL2008753509 1 20080227 A 5415 ATTACH ANGLE BOEING 727 727223 1384074 NM NR 1 NACELLE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 "C" CHECK 1 ENG PYLON OB UPPER ATTACH ANGLE CRACKED AT SECOND HOLE, VERIFIED BY NDT. REMOVED DAMAGED ANGLE AT NR 1 ENGI NE (PYLON) OB UPPER IAW B727 SRM 51-30-2. LOCATED HOLE, DRILLED AND DEBURRED ANGLE WITH P/N 69-16977-1 PO NR 738094 IAW B727 SRM 51-30-5 AND 54-10-2 FIG 3. INSTALLED ANGLE AT NR 1 ENGINE PYLON OB UPPER SIDE IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008032400304 20080324 00304 NM 2008 3 24 2008UALA01369 1 20080312 A 2560 SPRING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EVAC SLIDE WEAK A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 768UA 26919 DOOR 3L SLIDE PACK LATCH LEVER SPRING IS WEAK, LATCH LEVER HAS NO OVERCENTER FORCE ENGAGEMENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032400307 20080324 00307 SO 2008 3 24 FDKA200803106 1 20080312 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO GALLEY INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6184 MCO-BNA (0915 PHX LCL) - GALLEY EMERGENCY EXIT SIGN OUT. MX PERFORMED OPS CHECK AC EMERGENCY LIGHTING SYSTEM A ND FOUND NO DEFECTS. OPS GOOD 2 L 7 2 4T RT T00011AT 2008032400308 20080324 00308 SO 2008 3 24 FDKA200803107 1 20080312 A 5610 SEAL EMB 145 EMB145LR 3260212 SO COCKPIT WINDOW LEAKING A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 FDM 6031 - JFK- IAD (1638 PHX LCL) - LOUD NOISE FROM F/O'S SIDE WINDOW DURING DESCEND. MX RESECURED THE WINDOW SEAL AND LEAK CHECKED. 2 L 7 2 4T RT T00011AT 2008022800196 20080228 00196 NM 2008 2 28 SWAA080966 1 20080220 A 2560 6557463 FITTING BOEING 737 7373TO 138447G NM GIRT BAR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CRACKED. REMOVED AND REPLACED FITTI NG PER SRM. 2 L 7 2 4F RT A16WE 2008022800198 20080228 00198 NM 2008 2 28 SWAA080965 1 20080220 A 2730 6545166 ROD END BOEING 737 7373TO 138447G NM LT ELEVATOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 697SW 23838 DURING SCHEDULED 20Y CHECK, FOUND LT ELEVATOR TAB CONTROL ROD ENDS CORRODED. REMOVED AND REPLACED ROD ENDS PER MM. 2 L 7 2 4F RT A16WE 2008022800199 20080228 00199 NM 2008 2 28 DLM88080165 1 20080205 A 3244 329001470 TIRE DOUG MD88 MD88 3023688 NM NR 2 FAILED A DALA O OTHER O OTHER LD LANDING 1 SO 27 927DA 49714 DL784 NR 2 TIRE BLOWN IN LANDING LGA (MCC/1600Z), MED AUTOBRAKES IN USE AT TIME. REMOVED AND REPLACED NR 1 AND NR 2 MAIN TIRE S INSPECTED A/C AND INLET OF NR 1 AND NR 2 ENG NO DAMAGE FOUND, PERFORMED ANTI-SKID TEST AND INSPECTED TRANSDUCERS ON NR 1 AND NR 2 AXLES ALL NORMAL. ITEM NR 2 REMOVED AND REPLACED ANTI-SKID CONTROL PER M/M 32-43-04-201 WORKING NML. 2 L 7 2 4F RT A6WE 2008022800209 20080228 00209 EU 2008 2 28 2008UALA00608 1 20080201 A 2700 3945128102 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELAC 2 FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 409UA 462 ELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. ELAC 2 FAILURE, CIRCUIT BOARD FAILURE. BOTH ELAC 1 AND ELAC 2 WERE REPLAC ED ON THE A/C FOR PRECAUTION. ALL SYSTEM TEST ACCOMPLISHED AND NO FAULTS NOTED. THE ELAC UNIT WAS SENT TO THALES AND S EVERAL COMPONENTS (INTERNAL) WERE REPLACED, MN61, MN13, ,M73, MN173, MN71, MN121 ONBOARD MDG. 2 L 7 2 4F 4 F RT A28NM E40NE 2008022800211 20080228 00211 WP 2008 2 28 AALA200800315 1 20080213 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 244AA 49256 JFK - EMERGENCY LIGHT AT AFT CABIN INOPERATIVE. REPLACED SHORTED WIRE IN TAIL SECTION FOR EMERGENCY LIGHTS AT AFT CABIN . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022800212 20080228 00212 NM 2008 2 28 2008UALA00611 1 20080202 A 3231 SOLENOID BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CONTROL VALVE FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 555UA 26647 LEFT MAIN LANDING DOOR WILL NOT CLOSE. LT MLG DOOR CONTROL VALVE SOLENOID FAILED. REPLACED LT MLG DOOR CONTROL VALVE, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022800213 20080228 00213 NM 2008 2 28 CALA0800163 1 20080220 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM CABIN FAILED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 69063 29458 EMERGENCY LIGHT BATTERY FAILED TEST AFTER REPLACEMENT PER WORKCARD 64-3350-1-3800. REMOVED AND REPLACED BATTERY CHARGER . 2 L 7 2 4F RT A1NM 2008022800216 20080228 00216 WP 2008 2 28 AALA200800313 1 20080213 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7520A 49897 LGA - EMERGENCY LIGHTS AT SEAT ROWS 20 TO 22 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 20 TO 22. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022800219 20080228 00219 NM 2008 2 28 AALA200800312 1 20080213 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 909AN 29511 MIA - EMERGENCY LIGHT AT SEAT 3E INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 3E. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A16WE 2008022800221 20080228 00221 NM 2008 2 28 CALA0800166 1 20080205 A 5330 65C22910 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 FOUND CORROSION IN FORWARD PIT ON SKIN AND AROUND DOME NUT AT BS 500D LBL 17-21. REPAIRED PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2008022800223 20080228 00223 NM 2008 2 28 CALA0800168 1 20080204 A 5320 65176856 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 STA 348.2 STRINGER 16 LT SIDE STRAP CRACKED. REPLACED PER JOB 24-0553-8-0114 SEQ 482. 2 L 7 2 4F RT A16WE 2008022800225 20080228 00225 NM 2008 2 28 SWAA080970 1 20080221 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 256WN 32514 EEPLS LENS LOOSE AT ROW 5 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008022800233 20080228 00233 NM 2008 2 28 SWAA080991 1 20080221 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008022800235 20080228 00235 NM 2008 2 28 SWAA080981 1 20080221 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 184. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008022800236 20080228 00236 NM 2008 2 28 SWAA080980 1 20080221 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM 'HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 157. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008022800244 20080228 00244 NM 2008 2 28 SWAA080988 1 20080221 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800245 20080228 00245 NM 2008 2 28 SWAA080989 1 20080221 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED MV4 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008022800247 20080228 00247 CE 2008 2 28 191WA021908 1 20080219 A 2910 1240084CR0140 FITTING BEECH 99 99 1154002 CE HYDRAULIC SYS LOOSE E AXSA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION AP APPROACH 1 EA 65 191WA 27417 U136 FLIGHT 1064 MHT-BTV DURING APPROACH SELECTED GEAR DOWN. THE GEAR INTRANSIT LIGHT REMAINED ILLUM AND THE LANDING GEAR C/ B POPPED. THE GEAR DID NOT EXTEND. RESET THE C/B AND REATTEMPTED GEAR EXTENSION. THE LOW HYDRAULIC LIGHT ILLUM AND TH E C/B POPPED AGAIN. ELECTED TO RETURN TO MHT AFTER DISCUSSION WITH FLT OPS. WITHIN 40NM OF MHT DECLARED AN EMERGENCY A ND USED EMERGENCY GEAR EXTENSION PROCEDURES. THE GEAR EXTENDED NORMALLY AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDEN T. EXAMINATION OF THE AIRCRAFT REVEALED A LEAKING HYD LINE FITTING. THE LINE WAS TIGHTENED AND THE HYD SYSTEM WAS SERV ICED. OPERATIONAL CHECKS OF THE GEAR DID NOT REVEAL ANY OTHER MALFUNCTIONS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 3T A14CE 2008022800252 20080228 00252 NM 2008 2 28 KCSA081108 1 20080223 A 5230 SKIN BOEING 747 747209B 138489B NM CARGO DOOR DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 C-2 CARGO DOOR EXTERNAL SKIN HAS DAMAGE AT AFT LOWER CORNER STA 1914. 2 L 7 4 4F RT A20WE 2008022800253 20080228 00253 NM 2008 2 28 KCSA081109 1 20080223 A 5230 SKIN BOEING 747 747209B 138489B NM CARGO DOOR CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 C-2 CARGO DOOR FORWARD LOWER CORNER HAS SKIN PILLOWING BETWEEN FASTENERS AT STA 1830, STR 39R. 2 L 7 4 4F RT A20WE 2008022800256 20080228 00256 NM 2008 2 28 KCSA081112 1 20080223 A 5210 DOOR FRAME BOEING 747 747209B 138489B NM R1 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 R1 MAIN ENTRY DOOR HAS A 2 INCH LONG CRACK IN THE LOWER FORWARD VERTICAL CHORD RADIUS AT STA 446 BETWEEN WL 200 & 208. 2 L 7 4 4F RT A20WE 2008022800261 20080228 00261 EU 2008 2 28 Y2LA200811 1 20080215 A 2120 UNKNOWN AIRBUS A319 A319112 3930323 EU CABIN ODOR A Y2LA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 07 553SX 3171 CABIN FILLED WITH STRONG SMELL AND HAZE JUST BEFORE LANDING. ENGINE IDLE CHECK, OIL ADDED. NO LEAKS NOTED. NO POST FL IGHT REPORT MESSAGES. AIRCRAFT DEPARTED NORMALLY. 2 L 7 2 4F RT A28NM 2008022800265 20080228 00265 EA 2008 2 28 TRAX200800245 1 20080212 A 5210 SEAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 901EV 7616 SMALL CRACK IN FUSELAGE WHERE BOARDING DOOR SEALS. LOWER RIGHT CORNER OF FUSELAGE. REMOVED AND REPLACED PAX DOOR SEAL REF AMM 52-11-10. 2 L 7 2 4F RT A21EA 2008022800268 20080228 00268 EA 2008 2 28 TRAX200800246 1 20080212 A 2913 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 824AS 7203 HYD PUMP 2B FAILED ON SHORT FINAL INTO ATL. SWITCH WAS CYCLED AND 2B PUMP STARTED WORKING. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2008022800269 20080228 00269 EA 2008 2 28 TRAX200800247 1 20080212 A 2560 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 858AS 7417 SIGN MISSING ON LEFT OF PAX DOOR. 2 L 7 2 4F RT A21EA 2008022800270 20080228 00270 NM 2008 2 28 2008UALA00642 1 20080203 A 2697 WIRE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FIRE SQUIB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 808UA 804 NR 1 ENGINE, NR 1 SQUIB DOES NOT TEST. FIRE PNL NO HELP. BROKEN WIRES AT SQUIB. REPLACED TWO WIRES AT SQUIB LOCATION, SYSTEM TESTS NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030300034 20080303 00034 2008 3 3 2008UALA00788 4 20080211 A 2565 60592101 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT OWING SLIDE READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 442UA 780 RT OVERWING SLIDE BOTTLE PRESS LOW. BOTTLE LEAKING AT FITTING. REPLACED BOTTLE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030300035 20080303 00035 NM 2008 3 3 08FDEA00642 1 20080228 A 5347 AEA732515 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1524 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 CABIN NEAR STATION 1524, X = -75.25, SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER S RM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008030300036 20080303 00036 NM 2008 3 3 08FDEA00643 1 20080228 A 5730 ARB74023 SKIN DOUG MD11 MD11F 3023600 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 HFEC OPEN HOLE INSPECTION CARRIED OUT AND FOUND 7 HOLES WITH CRACK INDICATION AT LT WING ACCESS DOOR 536AB CUT OUT. R EPAIR CARRIED OUT AS PER EA 1-5710-109925, PART 1. REPAIR CLASSIFIED AS MAJOR AS PER PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008030300037 20080303 00037 NM 2008 3 3 08FDEA00644 1 20080228 A 5710 ARB74024 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 HFEC OPEN HOLE INSPECTION CARRIED OUT AND FOUND 10 HOLES WITH CRACK INDICATION AT RIGHT WING ACCESS DOOR 636AB CUT OUT . (BETWEEN STATION XORS 683.4 AND XORS 713.6). REPAIR CARRIED OUT AS PER EA 1-5710-109926, PART 1 REPAIR CLASSIFIED AS MAJOR AS PER PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032400309 20080324 00309 WP 2008 3 24 08FDEA00920 1 20080313 A 5315 ADA0030 FLOORBEAM DOUG MD10 MD1010F 3022112 WP BS 879 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 FWD CARGO COMPARTMENT BILGE AREA; FLOORBEAM WEB AFT FACE HAS TOOL MARKINGS ABOVE STR 47R; FS 879. BLENDED AREA IAW SRM 53-00-01; VOL I; FIG 8. ORIGINAL THICKNESS .062 IAW SRM 53-13-01; VOL III; FIG 6; PG 24B AND SRM 51-10-01; FIG 32. RE MAINING THICKNESS .062; FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01; VOL I; PG 8. ALODINED AND PRIMED IN REF TO SRM 51- 21-01; VOL II; PGS 31 AND 24. APPLIED TOP COAT IN REF SRM 51-21-01; VOL II; PGI. REMOVED AND REPLACED FASTENERS IAW 5 1-31-01; VOL II; PG 1 - 10. 2 L 7 3 4F RT A22WE 2008032400310 20080324 00310 WP 2008 3 24 08FDEA00922 1 20080313 A 5320 NDA6014 SUPPORT ANGLE DOUG MD10 MD1010F 3022112 WP BS 1019-1039 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 FWD CARGO COMPARTMENT BILGE AREA; FOUND CORROSION ON THE FUSELAGE SKIN DOME NUT SUPPORT ANGLE JUST OUTBD OF STR 52 FROM FS 1019 - 1039. REMOVED CORROSION IN REFERENCE WITH SRM 51-21-01; VOL II; PG 28. ORIGINAL THICKNESS IS .063 IAW DWG NDA 6014; REV A B. MATERIAL REMOVED IS .004; MATERIAL REMAINING IS .059. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01; VOL I; FIG 1B. ALODINED AND PRIMED TN REFERENCE WITH SRM 51-21-01; VOL II; PGS 21 AND 25. REMOVED AND REINSTALLED A NGLE IN REFERENCE WITH SRM 51-35-01; VOL II; PG 1. 2 L 7 3 4F RT A22WE 2008032400312 20080324 00312 WP 2008 3 24 08FDEA00954 1 20080314 A 5730 ARC29061 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 PANEL NR 541 CR EXTERNAL SKIN IS DENTED AND GOUGED. REPAIRED DENT & GOUGED PANEL BY REMOVING THE DAMAGE AT THE OUTER SK IN SECTION. FABRICATING & BONDING A REPAIR SKIN SECTION & DOUBLER IAW SRM 51-71-00 VOL II. ALODINED & PRIMED REPAIR A REA IAW IAW 51-21-01 VOL II. SEALED REPAIR IAW SRM 51-71-00 VOL II. RESTORED THE FINISH TO THE REPAIR AREA IAW SRM 51- 21-01 VOL II. 2 L 7 3 4F RT A22WE 2008032400313 20080324 00313 WP 2008 3 24 08FDEA00956 1 20080314 A 5230 ADA019343 LINER DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 FWD CARGO DOOR LINER IS CRACKED AT THE LOWER CORNER OF THE ACTUATOR ARM CUTOUT. APPLIED FIBERGLASS OVERLAY REPAIR IAW S RM 51-43-01; VOL II. 2 L 7 3 4F RT A22WE 2008032400314 20080324 00314 WP 2008 3 24 08FDEA00957 1 20080314 A 5230 ADA019343 LINER DOUG MD10 MD1010F 3022112 WP CARGO DOOR DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 THE FWD CARGO DOOR LINER HAS A PREVIOUS REPAIR THAT IS DELAMINATING ON THE AFT EDGE. APPLIED FIBERGLASS OVERLAY REPAIR IAW SRM 51-43-01 VOL II. 2 L 7 3 4F RT A22WE 2008032400316 20080324 00316 WP 2008 3 24 08FDEA00959 1 20080314 A 5730 ARC02642 PANEL DOUG MD10 MD1010F 3022112 WP RT WING DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT WING PANEL NR 641 EB; CORNER IS DISBONDED. RESTORED TO ORIGINAL IAW SRM 51-71-00, 51-21-01 & 51-21-02 VOL II. 2 L 7 3 4F RT A22WE 2008032400317 20080324 00317 EU 2008 3 24 2008UALA01370 1 20080311 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 498UA 1865 CREW O2 APPEARS TO HAVE A LEAK. SERVICED CREW O2 TO 2000 PSI, FOUND AT 1475, NO LEAKS WERE PRESENT AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032400324 20080324 00324 WP 2008 3 24 08FDEA00962 1 20080314 A 5753 ARC05422 PANEL DOUG MD10 MD1010F 3022112 WP RT WING TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT WING OUTBD FLAP; INBD PANEL NR 635 DL IS DELAMINATED. FABRICATED & BONDED PANEL IAW EA 8-5720-118478. 2 L 7 3 4F RT A22WE 2008032400327 20080324 00327 WP 2008 3 24 08FDEA00964 1 20080314 A 5730 ARB1100B402A PANEL DOUG MD10 MD1010F 3022112 WP ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT WING UPPER L/E PANEL NR 618 BT IS DELAMINATED. REPAIRED PANEL IAW DWG ARB1100, TPS 1001 REV E & EA. 8-5710-116969 . 2 L 7 3 4F RT A22WE 2008032400328 20080324 00328 WP 2008 3 24 08FDEA00965 1 20080314 A 5730 ARC0357502 PANEL DOUG MD10 MD1010F 3022112 WP RT WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT WING LOWER T/E PANEL NR 641LB IS DELAMINATED. REPAIRED PANEL BY FABRICATING & BONDING SKINS, CORE, DOUBLERS AND P HENOLIC FILLER IAW EA 8-5720-118473; DWG ARC0357 & TPS 1001, REV E. 2 L 7 3 4F RT A22WE 2008032400329 20080324 00329 NM 2008 3 24 2008UALA01376 1 20080311 A 3260 WARNING SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 302UA 23643 FIVE MILE FINAL UNSAFE GEAR INDICATION RED UNSAFE GEAR LIGHTS ILLUMINATED DURING GO-AROUND ACHIEVED. NO FAULT FOUND. L UBED GEAR HANDLE SLIDE MECHANISM. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032400330 20080324 00330 WP 2008 3 24 08FDEA00966 1 20080314 A 7160 INTAKE DOUG MD10 MD1010F 3022112 WP LT ENGINE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 NR 1 ENGINE INTAKE AT THE 8:30 POSITION; ABLATIVE COATING IS MISSING. REMOVED DAMAGE, APPLIED SEALANT TO REPAIR & CURED IAW ENGINE MANUAL 72-22-01 REPAIR 10. 2 L 7 3 4F RT A22WE 2008032400334 20080324 00334 WP 2008 3 24 08FDEA00967 1 20080314 A 7110 1539M25G01 ACOUSTIC PANEL DOUG MD10 MD1010F 3022112 WP NR 1 ENGINE BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 NR 1 ENGINE INTAKE BLACK SOUND SUPPRESSION FWD LIP IS BROKE AT THE 10:30 POSITION. REMOVED PANEL IAW MM 72-23-01. REPA IRED IAW MM 72-23-01. RESTORED FINISH IAW SRM 51-21-02 VOL II. REINSTALLED SUPPRESSION PANEL IAW AMM 72-23-00. 2 L 7 3 4F RT A22WE 2008032400335 20080324 00335 NM 2008 3 24 2008UALA01380 1 20080312 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 LEFT SIDE FUSELAGE SKIN, PREVIOUS DOUBLER REPAIR HAS A DENT AT BS 598 TO 625, BETWEEN STR 15L-17L. ACCOMPLISHED AT MAJO R REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032400341 20080324 00341 NM 2008 3 24 2008UALA01383 1 20080313 A 5520 ELEVATOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU LEFT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 FOUND A CRACK ON THE LT ELEV FWD OF TRIM TAB (DMG) APPROX 8" TO 10" LONG. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032400350 20080324 00350 NM 2008 3 24 2008UALA01388 1 20080313 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 LEFT NR 1 DOOR EMERGENCY LIGHT INOP (DOOR MOUNT LIGHT). REPLACED LAMP OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032400355 20080324 00355 NM 2008 3 24 2008UALA00015 1 20080102 A 2750 15441007 PCU BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE T/E FLAP FAULTY A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 212UA 30218 DURING GRND TEST OF RIGHT FLAPERON MSG 27-16039 OCCURS. ACCOMPLISHED TEST SEVERAL TIMES WITH SAME RESULT. SUSPECT POWE R CONTROL UNIT. REPLACED INBOARD FLAPERON PCA FOR RIGHT FLAPERON PER MM 27-11-12, OPS AND LEAK CK GOOD. PASSES ALL MAT TESTS. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032400359 20080324 00359 NM 2008 3 24 2008UALA00027 1 20080101 A 2710 251W12001 PCU BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE AILERON FAULTY A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 779UA 26941 THE "FLIGHT CONTROLS" EICAS APPEARED AFTER ENGINE START. SUSPECT AILERON POWER CONTROL UNIT. REPLACED LT INBOARD AILER ON PCU PER MM 27-11-11. ACP'D MAT CKS AND ADJUSTMENTS. RAN ENGINES, NO MSG'S DISPLAYED OR ACTIVE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032400365 20080324 00365 NM 2008 3 24 SWAA081420 1 20080316 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008032400368 20080324 00368 NM 2008 3 24 SWAA081419 1 20080316 A 5311 147A57446 FRAME BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 763SW 27877 DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 990, RBL 38. REPAIRED WEB PER SRM AND BOEING DRAWING. 2 L 7 2 4F RT A16WE 2008032400369 20080324 00369 NM 2008 3 24 SWAA081418 1 20080316 A 5311 141A1120 FRAME BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 763SW 27877 DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294, STR 47R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032400370 20080324 00370 NM 2008 3 24 SWAA081417 1 20080316 A 5311 6546529 BELTFRAME BOEING 737 7377H4 1384404 NM FUSELAGE WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 763SW 27877 DURING SCHEDULED 8Y CHECK, FOUND BELTFRAME WORN AT BS 335, STR 5R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032400371 20080324 00371 SO 2008 3 24 FDKA200803108 1 20080313 A 3350 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM FLT 6097 MCO-CHS (1134 PHX LCL) ROW 12 OVERHEAD EXIT SIGN INOP. MX REMOVED AND REPLACED INVERTER AND SIGN. 2 L 7 2 4T RT T00011AT 2008032400377 20080324 00377 2008 3 24 SWAA081425 4 20080314 A 2565 63550 SLIDE BOEING 737 737705 13844SC NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 271LV 29090 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032400378 20080324 00378 NM 2008 3 24 SWAA081426 1 20080314 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 283WN 36610 EEPLS LENS MISSING AT ROW 5 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008032400380 20080324 00380 NM 2008 3 24 SWAA081455 1 20080317 A 5230 6546921 SKIN BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND FWD CARGO DOOR FWD UPPER SKIN CRACKED. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400381 20080324 00381 NM 2008 3 24 SWAA081428 1 20080314 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND RT WING 36 L/E SLAT UPPER SURFACE DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008032400386 20080324 00386 NM 2008 3 24 SWAA081430 1 20080314 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 FUSELAGE SKIN CRACKED AT BS 797, STR 17L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032400392 20080324 00392 2008 3 24 SWAA081436 4 20080315 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 450WN 32470 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032400393 20080324 00393 2008 3 24 SWAA081437 4 20080314 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 494WN 33868 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032400394 20080324 00394 2008 3 24 SWAA081438 4 20080314 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 494WN 33868 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032400398 20080324 00398 2008 3 24 SWAA081441 4 20080314 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032400400 20080324 00400 NM 2008 3 24 SWAA081461 1 20080317 A 5311 65C22910 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500D, STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032400402 20080324 00402 NM 2008 3 24 SWAA081442 1 20080317 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 867, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008032400403 20080324 00403 NM 2008 3 24 SWAA081463 1 20080317 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 29L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032400404 20080324 00404 NM 2008 3 24 SWAA081443 1 20080317 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 632SW 27707 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008032400405 20080324 00405 NM 2008 3 24 SWAA081444 1 20080315 A 2121 215201 GASPER FAN BOEING 737 7373H4 1384600 NM E&E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 634SW 27937 DECLARED EMERGENCY. ELECTRICAL FUMES IN CABIN AND FLIGHT DECK. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2008032400410 20080324 00410 NM 2008 3 24 SWAA081471 1 20080317 A 5311 6554892 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 335, STR 17L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032400417 20080324 00417 NM 2008 3 24 SWAA081468 1 20080313 A 5330 65C381921 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506D, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400419 20080324 00419 NM 2008 3 24 SWAA081449 1 20080317 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032400426 20080324 00426 NM 2008 3 24 SWAA081453 1 20080314 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 30544 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032100073 20080321 00073 NM 2008 3 21 2008UALA01335 1 20080310 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 DOOR 2L UPPER HINGE CUT-OUT REQUIRES DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100074 20080321 00074 NM 2008 3 21 2008UALA01336 1 20080309 A 3510 OXYGEN SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CREW LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 CREW OXYGEN BELOW ETOPS MIN AT 1480 PSI. SERVICED CREW O2 TO FULL FOR ETOPS FLIGHT. NO LEAKS WERE NOTED AT TIME OF SER VICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100075 20080321 00075 NM 2008 3 21 2008UALA01337 1 20080310 A 3510 OXYGEN SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CREW LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 CREW O2 NEEDS SERVICE 1400 PSI. SERVICED CREW O2 TO FULL, NO LEAKS NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032100078 20080321 00078 NM 2008 3 21 2008UALA01346 1 20080310 A 3397 CONTACT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 531UA 25042 COACH EEL HAS A LIGHT STRIP WITH BROKEN CONTACTS. REPLACED LIGHT STRIP, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030300120 20080303 00120 NM 2008 3 3 HALA0800350 1 20080222 A 5753 FAIRING BOEING 717 717200 1383700 NM TE FLAP CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION ON RT I/B FLAP ACTUATOR AFT FAIRING. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008030300122 20080303 00122 NE 2008 3 3 HALA0800351 2 20080226 A 7300 UNKNOWN BOEING 767 767300 1385204 NM PWA 4060 PW4060 52119 NE UNKNOWN A HALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, ON DESCENT THROTTLES 1 INCH DIFFERENCE WITH SAME EPR. PERFORMED MCDP GRD TEST 02-10 ALSO COMP ARED THROTTLES POSITION ON THE EPCS PAGE. THE TRA AND EPR POS CHECKED OK, NO FAULTS WITH THROTTLES POS, ACCOMPLISHED PI MU BITE CHK. ALSO NO FAULTS. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030300123 20080303 00123 NM 2008 3 3 AALA200800359 1 20080220 A 3350 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 335AA 22333 JFK - EMERGENCY LIGHT AT OVERHEAD FIRST CLASS GALLEY INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 2HJ FOR EMERGENCY L IGHT AT OVERHEAD FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008032600111 20080326 00111 NM 2008 3 26 DL76P080378 1 20080316 A 2910 HYDRAULIC LINE BOEING 767 767332 1382001 NM THRUST REVERSER LEAKING A DALA K NONE K FLUID LOSS LD LANDING 1 SO 27 144DA 27584 ON LANDING ROLLOUT, AFTER ACTUATING THRUST REVERSERS LOST RT HYDRAULIC QTY. FOUND REVERSER HYDRAULIC LINE WITH HOLE IN IT. PERFORMED TEMP REPAIR PER MM 20-10-09-358-151. CYCLED REVERSER AND ALL HYDRAULIC SYSTEMS SEVERAL TIMES. OPS NORMA L. OLD BAD HYDRAULIC LINE LOCATED IN MCO POUCH. 2 L 7 2 4F RT A1NM 2008032600113 20080326 00113 2008 3 26 DL75E080379 4 20080316 A 2565 SLIDE BOEING 757 7572Q8 1384972 NM L2 DOOR OUT OF POSITION A DALA K NONE O OTHER TO TAKEOFF 1 SO 27 712TW 27624 L2 DOOR SLIDE AND COVER FELL OFF DOOR. SEA MX, REINSTALLED SLIDE PER AMM. 2 L 7 2 4F RT A2NM 2008032500034 20080325 00034 CE 2008 3 25 DJFA2008021 1 20080301 A 5510 SUPPORT BRACKET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 449LX RK257 DURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. THE LT AND RT RIB ASSEMBLIES WERE REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2008032500035 20080325 00035 NM 2008 3 25 2008UALA01386 1 20080313 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN MISSING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 178UA 24385 SEAT 4HJK EMERGENCY LIGHT IS MISSING. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032500083 20080325 00083 NM 2008 3 25 HNAA0800104 1 20080318 A 2120 UNKNOWN DHAV DHC8 DHC8102 2809003 NM CABIN ODOR A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 931HA 132 SMOKEY LIKE SMELL IN REAR CABIN DURING CRUISE. RAN AIRCRAFT ON GROUND WITH APU OFF, ENGINE BLEEDS ON, ONE AT A TIME AND BOTH TOGETHER AND OFF, NO SMELL NOTICED INSIDE AIRCRAFT. OK FOR SERVICE. 2 H 7 2 4T RT A13NM 2008032500099 20080325 00099 SW 2008 3 25 AC2A119193 1 20080314 A 6200 SHEARRESTRAINT PIN BELL 430 430 1182150 SW MAIN ROTOR DEBONDED E AC2A O OTHER O OTHER NR NOT REPORTED 1 SW 31 430CM 49090 PIN DEBONDED. 1 G 7 2 3U RT H9SW 2008032500102 20080325 00102 NM 2008 3 25 AMTA200800200 1 20080301 A 5347 CARGO TRACK BOEING 737 73783N 13844HI NM CARGO BAY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 RAIL ASSY RBL 8.1 STA, 767 HAVE A UNIFORM CORROSION AFT CARGO COMPARTMENT. REMOVED CORROSION ON RAIL ASSY, ORG MAT .071 , MAT LOSS .030, REM MAT .041, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A DETAIL D, FABRICATED REPAIR PART FROM BAC 1 510-1355 IAW EA 737-5300-08-A0036. (K) 2 L 7 2 4F RT A16WE 2008032500104 20080325 00104 EA 2008 3 25 COMA0860179 1 20080317 A 3260 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 912CA 23448 7011 FLIGHT 5480 - NOSE LANDING GEAR AND GEAR DOOR INDICATION REMAINED "RED" ON RETRACTION. DECLARED EMERGENCY, LANDED CVG W ITHOUT INCIDENT. INSPECTED AND GREASED NLG AND DOORS. ADJUSTED STRUT PROX SENSOR, SWUNG GEAR 15 TIMES INCLUDING PRIORI TY TEST. REPLACED PSEU DUE TO NO CODES DISPLAYED FOR EVENT. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008032500120 20080325 00120 NM 2008 3 25 SWAA081498 1 20080318 A 5754 65C26601 SLAT BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND LT WING L/E NR 3 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008032500124 20080325 00124 NE 2008 3 25 DJFA2008030 2 20080321 A 7200 79015510 HMU BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE NR 2 ENGINE FAILED E DJFA D RETURN TO BLOCK Y J ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 EA 23 708TA RK178 PCEJA0125 ON TAXI FOR TAKE-OFF, WHILE PERFORMING THE EFC TEST, THE NR 2 ENGINE SHUT DOWN UNCOMMANDED. MAINTENANCE CHECKED RIGGI NG AND PERFORMED SEVERAL OPERATIONAL CHECKS. MAINTENANCE DETERMINED THAT THE HMU REQUIRED REPLACEMENT. THE HMU AND FLO W DIVIDER WERE REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2008032500130 20080325 00130 NM 2008 3 25 SWAA081480 1 20080318 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008032500132 20080325 00132 NM 2008 3 25 SWAA081482 1 20080318 A 5753 6546435278 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2008032500151 20080325 00151 NM 2008 3 25 SWAA081493 1 20080318 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 747, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008032500203 20080325 00203 NM 2008 3 25 2008UALA01439 1 20080315 A 5753 113W30033 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE T/E FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 51719 26919 LEFT O/B FLAP I/B END, 12 FROM FRONT END, SKIN IS WORN. REPAIR PER EN-27- 51-21-028--21 AND EVA-71266. THE REPAIR IS AP PROVED BY BAC, 8 100-9. THE REPAIR IS 12 MONTH LIMITED REPAIR, AND A NEW 8100-9 MUST BE ISSUED TO COMPLY WITH 1 4 CFR 2 5.571 AND 26.43 (D). OK TO CF PER EVA 71266. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500214 20080325 00214 NM 2008 3 25 2008UALA01450 1 20080315 A 5320 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 808UA 804 BEAM 190 HAS 1 CLIP NUT HOLE WITH CORROSION. MAJOR REPAIR ACCOMPLISHED AT DEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500217 20080325 00217 NM 2008 3 25 2008UALA01453 1 20080315 A 5320 SHEAR PLATE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 808UA 804 RIGHT SIDE SHEAR PLATE, FRAME SUPPORT HAS CORROSION ON BOTTOM SIDE OF SUPPORT. ACCOMPLISHED A MAJOR REPAIR IN DEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500223 20080325 00223 NM 2008 3 25 2008UALA01460 1 20080315 A 5754 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L/E SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 NR 9 SLAT O/B EDGE DELAM ON UPPER AND LOWER SURFACE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500243 20080325 00243 2008 3 25 2008UALA01593 4 20080319 A 2565 PROXIMITY SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR SLIDE FAILED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 568UA 26674 NO SLIDE ARMED LIGHT 2L. FOUND PROXIMITY SWITCH FAILED. REPLACED PROX SWITCH "A" S10218, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500253 20080325 00253 NM 2008 3 25 2008UALA01603 1 20080320 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 UPPER FUSELAGE CROWN SKIN HAS WEAR FROM DORSAL FIN CONTACT, BS 900-913 STR 2R. MAJOR REPAIR ACCOMPLISHED: INSTALLED WEA R STRIP REPAIR PER SRM 53-60-01. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500274 20080325 00274 NM 2008 3 25 2008UALA01525 1 20080318 A 5313 STRINGER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 BS 360 STRINGER S-15L CRACKED AT CLIP FASTENER HOLES JUST AFT OF DOOR 1L CUTOUT. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500285 20080325 00285 NM 2008 3 25 2008UALA01473 1 20080315 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FRAME WEB CRACKED AT UPPER SHEAR TIE FASTENER BELOW STR 13R AT BS 360. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALL ED NESTED ANGLE FRAME SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500287 20080325 00287 NM 2008 3 25 2008UALA01471 1 20080315 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE MISREPAIRED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 386UA 24661 FUSELAGE EXTERNAL SKIN REPAIR DOUBLER AT DOOR 2R UPPER HINGE CUTOUT IS INSTALLED WITH BLIND FASTENERS. REMOVED BLIND FA STENERS & INSTALLED SOLID FASTENERS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500296 20080325 00296 EU 2008 3 25 08FDEA00996 1 20080317 A 7120 A54612406600 MOUNT AIRBUS 310 A310203 3930313 EU NR 2 ENGINE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 ENGINE UPPER INBD FWD MOUNT BEAM IS GOUGED IN AREAS. BLENDED DAMAGED AREA REF A310 SRM 51-72-10. ORIGINAL THICKNE SS WAS .320. REMOVED .010; REMAINING THICKNESS .310. WITHIN LIMITS REF A310 SRM 54-51-81. CAD PLATED REF A310 SRM 5 1-21-10. PRIMED REF A310 SRM 54-51-81. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008032500297 20080325 00297 EU 2008 3 25 08FDEA00997 1 20080317 A 7120 A54612406600 MOUNT AIRBUS 310 A310203 3930313 EU NR 2 ENGINE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 PYLON FWD ENGINE MOUNT HOLES HAVE CORROSION. REMOVED CORROSION REF SRM 51-74-10. AFT INBD HOLE SIZE IS 0.825. AL L REMAINING HOLES ARE 0.809. WITHIN LIMITS REF SRM 54-51-81; CADMIUM PLATED REF A310 SRM 51-21-10. PRIMED AREA REF SRM 54-51-81. MINOR REPAIR 2 L 7 2 4F RT A35EU 2008032600010 20080326 00010 NM 2008 3 26 HALA0800405 1 20080312 A 2612 644501 CIRCUIT CARD BOEING 767 767332 1382001 NM GE CF6 CF680C2* GL OVERHEAT SYS FAULTY A HALA K NONE N FALSE WARNING CR CRUISE 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, INTERMITTENT LOWER EICAS STATUS MESSAGE "R ENG OH LP2". PERFORMED FIM 26-11-00 FIG 104. CLEA NED NR 2 ENG O/H LP2 CONNECTORS AND REPLACED M960 LP2 O/H DETECTOR CARD PER AMM 26-10-01. OVERHEAT TEST CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E23EA 2008032600011 20080326 00011 NM 2008 3 26 HALA0800395 1 20080309 A 5420 BRACKET BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE RT NACELLE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 APPROX 1/2" CRACK TO LIGHT STRUCTURE BRACKET RT ENGINE STRUT NAC STA 298.93 - 297, INBD SIDE ATOP AND FWD OF PANEL 447 E LX. BRACKET MEASURES APPROX 3 INCHES BY 1 INCH AND ATTACHES STRUT AFT TORQUE BOX TO SIDE PANELS, FWD AND ABOVE HYDRAULI C SHUTOFF VALVE. REPLACED BRACKET. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032600044 20080326 00044 EU 2008 3 26 08FDEA01004 1 20080317 A 5414 2241202505 SKIN AIRBUS 310 A310203 3930313 EU NR 2 COWLING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 ENGINE OUTBD FAN COWL IS DELAMINATED AT THE EXTERIOR CENTER SECTION, 18 INCHES FROM THE T/E. ABRADED SURFACE & RE PAIRED IAW SRM 54-10-00 FIG 1 & RDN 54-20-00 REPAIR 1 & 2. 2 L 7 2 4F RT A35EU 2008032600061 20080326 00061 EU 2008 3 26 08FDEA01014 1 20080318 A 5420 A54612546 FITTING AIRBUS 300 A300B4622R 3930312 EU NR 2 PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND ON PYLON NR 2 SPIGOT FITTING WITH CORROSION AROUND BEARING SEAT. REPAIR PERFORMED BY REPLACEMENT OF SPIGOT FITTIN G IAW SB 54-6017, APPROVED BY EA 6-5451-114936. 2 L 7 2 4F RT A35EU 2008032600068 20080326 00068 WP 2008 3 26 08FDEA01021 1 20080318 A 5753 RUB STRIP DOUG MD10 MD1010F 3022112 WP T/E FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LT WING FLAP FWD SIDE L/E RUB STRIP IS WORN IN AREAS. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IN REF TO SRM 57-00-01 VOL I. REMOVED RUB STRIPS IN REF TO SRM 51-35-01 VOL II. DRILLED, DEBURRED, & COUNTERSUNK NEW RUB STRIP IN REF TO SR M 51-31-01 VOL II. INSTALLED RUB STRIP IN REF TO SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2008032600069 20080326 00069 WP 2008 3 26 08FDEA01022 1 20080318 A 5712 RIB DOUG MD10 MD1010F 3022112 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LT WING L/E INTERNAL RIB UPPER AFT EDGE REPAIR DOUBLER IS CRACKED INBD OF THE NR 16 SLAT TRACK. REPAIRED RIB & INSTALL ED CUP ARB 1292-39, PO 612641.1; IAW SRM 57-20-00 FIG 1 VOL I & 51-33-01 VOL II. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008032600114 20080326 00114 NM 2008 3 26 2008UALA01556 1 20080319 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INTERMITTENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 EMERGENCY PATH LIGHTS IN COACH ON THE RIGHT SIDE COMES ON INTERMITTENTLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032600115 20080326 00115 NM 2008 3 26 DL76G080380 1 20080316 A 2910 PACKING BOEING 767 767332 1382001 NM HYD MANIFOLD DAMAGED A DALA O OTHER K FLUID LOSS CR CRUISE 1 SO 27 169DZ 29689 LEFT HYD QTY CAUTION HYD LEAK PRESSURE LIGHT DID NOT COME ON AS QTY WENT TO .03RF. FOUND HYD LEAK AT VERT STAB HYD MANI FOLD. REMOVED AND REPLACED PACKING FROM HYD LINE TO MANIFOLD. OPERATED LEFT HYD SEVERAL TIMES. OPS NORMAL. SERVICE D QTY TO FULL. 2 L 7 2 4F RT A1NM 2008032600116 20080326 00116 EU 2008 3 26 2008UALA01557 1 20080318 A 3350 D9239003500060 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 454UA 1104 EPSU EXT LOAD EMERGENCY L DISPLAYED AFTER EMERGENCY LIGHT TEST. BATTERY FAILURE. REPLACED EMERGENCY BATTERY FOR OVERWI NG CHARGER. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032600119 20080326 00119 2008 3 26 2008UALA01560 4 20080317 A 2565 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR SLIDE UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 403UA 442 THE 2R SLIDE COVER FELL OFF AGAIN. PREVIOUS DAMAGE TO COVER. REPAIRED SLIDE COVER. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032600121 20080326 00121 NM 2008 3 26 2008UALA01561 1 20080317 A 3350 9027323626247487 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE MID GALLEY BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 EEL STRIP BROKEN BY MID GALLEY. REPLACED SPLICES, CRIMPER AND PLASTIC COVER. CHECKED EMERGENCY LIGHT OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032600130 20080326 00130 NM 2008 3 26 2008UALA01566 1 20080318 A 2612 FIRE LOOP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 NACELLE SHORTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 824UA 965 ENG NR 2 LOOP A FIRE DETECTOR. HUNG NEW LOOP, NO HELP. SUSPECT FDU BENCH PLUG, SHAKING FDU CLEARS FAULT. FOUND WIRING SHORT IN FAN LOOP HARNESS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032600136 20080326 00136 NM 2008 3 26 2008UALA01568 1 20080320 A 5320 STRUCTURE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE OXYGEN BOX BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 792UA 26934 OXYGEN BOX LID BROKE AND MASKS FELL AT LOCATION 23J. NEEDS NEW PLASTIC LID HINGE OR BOX ASSY, BOTTLE DID NOT DISCHARGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032600138 20080326 00138 NM 2008 3 26 2008UALA01569 1 20080320 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 2E BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 792UA 26934 SEAT 2E EEL LIGHT BROKEN. REPLACED LIGHT SEGMENT. OP CHECKED OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032600140 20080326 00140 EA 2008 3 26 SWIA200819351 1 20080311 A 3350 AD20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 751SK 4566 4566 10208 SOME EMERGENCY LIGHTS ARE WEAK. REPLACED ELBP NR 2. OPS CHECK GOOD PER AMM 33-51-17. 2 L 7 2 4F RT A21EA 2008032600141 20080326 00141 EU 2008 3 26 2008UALA01570 1 20080319 A 3350 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 427UA 512 SEAT 15C IS MISSING EMERGENCY LIGHT COVER. REPLACED MISSING COVER. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032600142 20080326 00142 EU 2008 3 26 2008UALA01571 1 20080319 A 3350 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SEAT 23C MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 427UA 512 SEAT 23C IS MISSING EMERGENCY LIGHT COVER. REPLACED MISSING LIGHT COVER. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032600147 20080326 00147 NM 2008 3 26 2008UALA01576 1 20080319 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 540 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 FWD PIT FRAME DENTED STA 540, STR 25L. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032600148 20080326 00148 NM 2008 3 26 2008UALA01577 1 20080319 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 740 S28L/R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 FWD PIT FRAME REPAIR AT STA 740 STR 28L TO STR 28R. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032600149 20080326 00149 SO 2008 3 26 SWIA200819353 1 20080311 A 3397 WIRE EMB 120 EMB120ER 3260203 SO CABIN DAMAGED A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 227SW 120304 FLT 5724 - FIRST RED EMERGENCY FLOOR LIGHT IS INOP. REPAIRED WIRING AT FLOOR EMERGENCY LIGHT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008032600155 20080326 00155 SO 2008 3 26 SWIA200819358 1 20080314 A 6120 PCU EMB 120 EMB120ER 3260203 SO RIGHT OUT OF ADJUST A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 236SW 120312 FLT 5504 - ON CLIMB-OUT, RIGHT NP INCREASED TO 104 PERCENT. ADJUSTED PROPELLER PCU IAW HAMILTON STANDARD 61-22-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008032600162 20080326 00162 NM 2008 3 26 2008UALA01583 1 20080320 A 2613 P4100822 SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CARGO OVERHEAT FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 643UA 25093 LEFT ENGINE FIRE HANDLE AND L ENGINE FUEL CONTROL FIRE LIGHTS CAME ON, ENG NOT RUNNING AND IN. SUSPECT APU CARGO OVERHE AT SWITCH. REPLACED ENGINE APU CARGO OVERHEAT TEST SWITCH. GROUND CHECK NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032600176 20080326 00176 SO 2008 3 26 SIMA200807908 1 20080313 A 3230 M8353616022M RELAY EMB 145 EMB145LR 3260212 SO FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 644AE 145204 ON FLIGHT 3957, CREW REPORTED DURING TAKEOFF AFTER ROTATION RECEIVED L/G AIR GRND FAIL AMBER EICAS MESSAGE. GEAR HANDLE WOULD NOT MOVE ONCE TRIM WENT OUT OF TAKEOFF RANGE. BEGAN RECEIVING TAKEOFF TRIM AND TAKEOFF FLAPS AURAL WARNING AFTER APPROX 4 MINUTES THE LG AIR GRND FAIL WENT AWAY ALONG WITH AURAL WARNING LEFT GEAR DOWN AND RETURNED TO ORD WITHOUT INC IDENT. CMC MSG LGEU FAIL. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RELAY. PERFORMED RETRACTION TEST OF LA NDING GEAR. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032600177 20080326 00177 EA 2008 3 26 SIMA200807906 1 20080317 A 3250 530003 MANIFOLD CNDAIR CL600 CL6002C10 1390015 EA NLG STEERING FAULTY A SIMA O OTHER J WARNING INDICATION CL CLIMB 1 SW 21 523AE 10152 ON FLIGHT 4168, CREW REPORTED AFTER GEAR RETRACTION, GOT A STEERING INOP MESSAGE. CREW FOLLOW THE AOM AND DECLARE AN EM ERGENCY IN ORD. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NOSE WHEEL STEERING MANIFOLD. OPERATIONAL CHECK G OOD IAW CRJ AMM 32-51-50. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008032600179 20080326 00179 SO 2008 3 26 SIMA200807901 1 20080317 A 3230 355022002 ELECTRONIC UNIT EMB 135 EMB135LR 3260305 SO LANDING GEAR MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 715AE 145262 ON FLIGHT 4557, CREW REPORTED THAT AFTER TAKEOFF LANDING GEAR AIR/GND FAIL CAUTION MESSAGE ILLUMINATED. RETURNED FOR NO RMAL LANDING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LGEU IAW EMB 135 32-32-01. PERFORMED OPERATIONAL CH ECK NO DEFECTS OR MESSAGES NOTED. PERFORMED FCF, NO DEFECTS OR MESSAGES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008032600184 20080326 00184 NM 2008 3 26 QXEA200800294 1 20080313 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - C4 - SUSPECT CORROSION AT STA 176 ON FRAME, INBOARD OF STRINGER 31L. REMOVED RIVETS (4) AND BLENDED OUT CORROSION IAW Q400 SRM 51-42-05 AND 51-21-00. HFEC INSPECTED BLENDED AREA FOR CRACKS, IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECK IAW Q400 NDTM PART 1, 51-00-04, ALL WITHIN LIMITS IAW Q400 SRM 51-14-00. INSTALLED RIVETS (4 ) IAW Q400 SRM 51-42-05. ALODINED, PRIME, AND PAINTED AREA IAW Q400 SRM 51-21-10, 51-21-15. 2 H 7 2 4T RT A13NM 2008032600199 20080326 00199 EU 2008 3 26 F3LA200800126 1 20080227 A 3350 321430 BATTERY AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE CABIN FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 608 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED FOUR EPSU FAILURES DURING CAPACITY TESTING. MAINTENANCE REMOVED AND REPLACED THE EPSU BATTERIES (PN 3214-30, SN 27195, 27186, 25851, AND 27185) IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-38-0 00-002, AMM 33-51-38-400-002, AMM 33-51-28-020-053 AND AMM 33-51-38-420-052. UPON COMPLETION OF THE REPLACEMENTS, THE U NITS WERE TESTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032600206 20080326 00206 EU 2008 3 26 08FDEA01028 1 20080318 A 5730 A5724351300100 PANEL AIRBUS 310 A310203 3930313 EU LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT WING T/E PANEL NR 572 DB IS CHAFED AND CORRODED WITH PAINT PEELING ON THE MATING SURFACES. REPAIRED PANEL BY REMOVING DAMAGE, FABRICATING FILLER PLATE AND DOUBLER, LAYING UP REPAIR DOUBLER AND FILLER PLATE & COMPLETING CURE & REMOVING EX CESS ADHESIVE FLASH, APPLING SEALANT TO REPAIR DOUBLER EDGES & CURING, APPLING FE PRIMER AND APPLING FINISH COAT IAW SRM 51-77-12, 51-77-10, 51- 35-00, AND 51-75-10. 2 L 7 2 4F RT A35EU 2008032600207 20080326 00207 EU 2008 3 26 08FDEA01029 1 20080318 A 5330 A53610567235 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AVIONICS COMPARTMENT FUSELAGE INTERIOR SKIN IS CORRODED FWD OF FRAME 17; OUTBD OF STRINGER 44L. REMOVED CORROSION IAW SRM 51-74-10. MEASURED MATERIAL THICKNESS. REMAINING MATERIAL THICKNESS 0.197. SHOWED TO BE 0.1968 / - 1MM IAW DWG A 53610567. FOUND TO BE WITHIN LIMITS. RFTS GENERATED; NO. N425FE-26-32-569. ALODINED AREA IAW SRM 51-21-10. PRIMED & P AINTED AREA IAW SRM 51-23-10. RESTORED CIC COATING IAW AMM 51-23-20-0. 2 L 7 2 4F RT A35EU 2008032600208 20080326 00208 EU 2008 3 26 08FDEA01030 1 20080318 A 5313 A5361060720200 FITTING AIRBUS 310 A310 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AVIONICS COMPARTMENT STRINGER 44L END FITTING IS CORRODED FWD OF FR 17. FITTING REMOVED IAW SRM 51-40-21. REMOVED CORR OSION IAW SRM 51-74-10. ORIGINAL MAT 0.067. MAT REMOVED 0.014. MAT REMAINING 0.053. OUT OF LIMITS IAW SRM 53-10-00 & DWG A53610607. REMOVED FITTING, RECEIVED NEW FITTING, LOCATED, DRILLED & INSTALLED NEW FITTING IAW SRM 51-40-21, 51-40 -44 & TORQUED BOLTS TO 150 IN LBS IAW SRM 51-49-00. INSTALLED EDGING IAW SRM 51-40-21. APPLIED CIC IAW AMM 51-22-00-0. 2 L 7 2 4F RT A35EU 2008032600209 20080326 00209 EU 2008 3 26 08FDEA01031 1 20080318 A 5730 A5724855600000 PANEL AIRBUS 310 A310203 3930313 EU LT WING ERODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LEFT WING LOWER SURFACE L/E DROP PANEL (RIB 28) EXTERNAL SURFACE HAS AN ERODED AREA. REPAIRED LT WING LOWER SURFACE L/E DROP PANEL BY REMOVING DAMAGE, APPLING FOIL REPAIR, ALODINING FOIL REPAIR, APPLING FR PRIMER, AND APPLING FINISH COAT I AW SRM 57-41-12,51-21-00, & 51-75-10. 2 L 7 2 4F RT A35EU 2008032600211 20080326 00211 EU 2008 3 26 08FDEA01033 1 20080318 A 5730 A5724609100300 PANEL AIRBUS 310 A310203 3930313 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT WING L/E LOWER SURFACE ACCESS PANEL 623 JB UPPER SURFACE SPEED TAPE IS PEELING OFF AND TORN. REMOVED DAMAGED IAW S RM 57-41-12. APPLIED NEW FOIL IAW SRM 57-41-12. APPLIED SURFACE FINISH IAW SRM 57-41-12 PG 227. 2 L 7 2 4F RT A35EU 2008032600213 20080326 00213 EU 2008 3 26 08FDEA01035 1 20080318 A 5730 A5724854600100 PANEL AIRBUS 310 A310203 3930313 EU ZONE 600 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT WING L/E LOWER SURFACE PANEL 623 MB SPEED TAPE IS PEELING OFF AND TORN. REMOVED DAMAGED FOIL IAW SRM 57-41-12. APPLI ED NEW FOIL IAW SRM 57-41-12. APPLIED SURFACE FINISH IAW SRM 51-75-10. 2 L 7 2 4F RT A35EU 2008032600221 20080326 00221 WP 2008 3 26 08FDEA01044 1 20080318 A 5751 SKIN DOUG MD10 MD1010F 3022112 WP LLT AILERON DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LT WING; FOUND 2 DENTS ON THE INBD AILERON LOWER SURFACE SKIN IN THE FWD OUTBD EDGE AREA. CHECKED DENT, FOUND TO BE OUT OF LIMITS IAW SRM 51-80-01 VOL II AT STA XIA 350. FABRICATED IAW SRM 57-10-00 FIG 85 VOL I. ALODINED & PRIMED I AW SRM 51-21-01 PGS 21-24 VOL II. INSTALLED IAW SRM 51-21-01 VOL II. 2 L 7 3 4F RT A22WE 2008032600222 20080326 00222 WP 2008 3 26 08FDEA01045 1 20080318 A 5751 ARC12501 PANEL DOUG MD10 MD1010F 3022112 WP LT AILERON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LT WING INBD AILERON L/E INBD SURFACE CLOSE OUT PANEL HAS CHAFING WEAR. LT WING INBD AILERON L/E INBOARD SURFACE CLOSE OUT PANEL WAS WORN BEYOND ALLOWABLE LIMITS IAW SRM 57-00-01 VOL I. FABRICATED, TREATED & PRIMED IAW THE FOLLOWING SRM`S 57-00-01 VOL I & 51-21-01 VOL II. INSTALLED REPAIR DOUBLER IAW SRM 51-31-01 VOL II. REINSTALLED PANEL IAW SRM 51-31 -01 VOL II. 2 L 7 3 4F RT A22WE 2008032600223 20080326 00223 WP 2008 3 26 08FDEA01047 1 20080319 A 5344 ACA0012539 HINGE DOUG MD10 MD1010F 3022112 WP CARGO DOOR WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 LOWER FWD CARGO DOOR FWD HINGE SEGMENT LOBES ARE WORN BEYOND LIMITS PER FEDEX WORK CARD 52X3502. MACHINED 3 EACH REPAIR BUSHINGS IAW SRM 52-10-00 PG 23 VOL I. INSTALLED BUSHINGS IAW SRM 51-39-01 VOL II PG 3. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008032600230 20080326 00230 WP 2008 3 26 08FDEA01056 1 20080319 A 5320 INTERCOSTAL DOUG MD10 MD1010F 3022112 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 FWD LOWER CARGO BILGE INTERCOSTAL IS CORRODED BETWEEN BS 1059 AND 1079; LBL 57. FOUND CRACK, REMOVED ANGLE & FITTING I AW SRM 51-35-01 VOL II. FABRICATED ANGLE & FITTING ON N/R N00806 & N00807 IAW DWG AFA 3866. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. FABRICATED INTERCOSTAL WEB IAW DWG AFA 3866. TREATED & PRIMED IAW SRM 51-21-01 VOL II. INSTALL ED INTERCOSTAL, ANGLE & FITTING IAW DWG AFA 3866 & SRM 51-33-01; VOL II. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008032600235 20080326 00235 WP 2008 3 26 08FDEA01059 1 20080319 A 7830 9059M71G04 FAIRING DOUG MD10 MD1010F 3022112 WP THRUST REVERSER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 NR 3 ENGINE OUTBD T/R LOWER OUTBD FAIRING IS DAMAGED, (MISSING FWD EDGE). REMOVED FAIRING IAW MANUAL 70-13-01. DRILLE D NEW PANEL IAW MANUAL 70-13-01. INSTALLED NEW FAIRING IAW MANUAL 70-13-01. 2 L 7 3 4F RT A22WE 2008032600245 20080326 00245 WP 2008 3 26 08FDEA01064 1 20080319 A 5420 CHANNEL DOUG MD10 MD1010F 3022112 WP NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 NR 1 PYLON PANEL NR 437 DR HAS A CRACKED CHANNEL. REMOVED CHANNEL IAW AMM 51-31-01 VOL II. FABRICATED CHANNEL IAW SRM 51-10-00 FIG 2 VOL II & DWG 7054, REV J. HEAT TREATED CHANNEL IAW TPS 1003. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. PART MARKED CHANNEL IAW DWG FX AUB 7054-5; REV J & GMM 7-0-1000. INSTALLED CHANNEL IAW SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2008032600247 20080326 00247 EU 2008 3 26 08FDEA01065 1 20080319 A 5730 A5714361420600 PANEL AIRBUS 310 A310203 3930313 EU LT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT WING T/E NR 572 BB HAS CHAFING; BARE METAL AND PEELING PAINT ON THE INNER SURFACE. REMOVED DAMAGED AREA, FABRICATE D FILLER PLATE & DOUBLER. LAID UP REPAIR,CURED, PLACED A BEAD OF SEALANT AROUND DOUBLER. INSTALLED NEW GROMMET, PRIMED P ANEL & APPLIED FINISH COAT. IAW SRM 51-77-12,51-77-10, 51-35-00, & 51-75-10. 2 L 7 2 4F RT A35EU 2008032600263 20080326 00263 NM 2008 3 26 DHL2008765024 1 20080127 A 5754 SKIN BOEING 727 727264 138408M NM NR 4 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, NR 4 SLAT UPPER SKIN CRACKED AT INBOARD HOOK MOUNT SCREW WS 390. STRIPPED AREA IAW B727 MM 51-20-1, C/S HFEC IAW B727 NDTM PT6 51-00-00 FIG 23. CRACKS TERMINATE IN STOP DRILL HOLES. FABRICATED REPAIR PLATE MATERIAL USED 7 075-T6 0.125" PO NR 9005685 DIMENSION 3.5" BY 4" IAW B727 SRM 57-50-3 FIG 10. TREATED AND PRIMED AREA AND PART REPAIR I AW B727 SRM 51-10-2. INSTALLED REPAIR PLATE IAW B727 SRM 57-50-3 FIG 3. 2 L 7 3 4F A3WE 2008032500125 20080325 00125 NM 2008 3 25 SWAA081475 1 20080318 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 LEFT OVERWING EMERGENCY EXIT LIGHT ASSY LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008032500127 20080325 00127 NM 2008 3 25 SWAA081477 1 20080318 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008032500155 20080325 00155 NM 2008 3 25 SWAA081507 1 20080318 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032500156 20080325 00156 NM 2008 3 25 SWAA081492 1 20080318 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, STR 26L TO BS 27R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032500171 20080325 00171 NM 2008 3 25 DXTA20082925 1 20080308 A 3220 ADAPTER GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE NLG TOW DIRTY E DXTA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 07 752QS 152 ON APPROACH TO ASE, SELECTED GEAR DOWN AND GOT RED HASH MARKS ON NOSE GEAR. TROUBLESHOT SYSTEM FOUND ON VISUAL INSPECT ION OF NOSE GEAR TOW ADAPTOR WOULD NOT SPIN TO THE DOWN POSITION. REMOVED TOW ADAPTOR, CLEANED DEBRIS, LUBED, INSTALLED , OPS CHECK GOOD. CHECKED FOR GROUND THROUGH DCU TO GEAR BOTH GROUND CHECKS GOOD. DCU OPS CHECK AND LAND GEAR EXTENSIO N WARNING SYSTEM OPS CHECKS GOOD. DCU OPS CHECK AND LAND GEAR EXTENSION WARNING SYSTEM OPS CHECKS GOOD. VISUAL INSPECT ION GOOD REF. G200 MM 31-50-05 AND 32-60-00. 2 L 7 2 4F 4 F RT A53NM E35NE 2008032500196 20080325 00196 NM 2008 3 25 2008UALA01397 1 20080313 A 7830 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE THRUST REVERSER TORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 NR 1 ENG LEFT REVERSER HALF HAS A 10 INCH TEAR IN SKIN AT AFT COWL LATCH PANEL ACCESS DOOR. REPLACED NR 1 ENGINE THRUST REVERSER HALF. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500204 20080325 00204 NM 2008 3 25 2008UALA01440 1 20080315 A 5753 PANEL BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE T/E FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 RIGHT O/B FLAP, UPPER SKIN PANEL IS WORN AT OUTBOARD END. REPAIR PER EN-57- 0028-01 AND EVA-71269. THE REPAIR IS APPROV ED BY MANUFACTURER. THE REPAIR IS 12 MONTH LIMITED REPAIR AND A NEW 8100-9 MUST BE ISSUED TO COMPLY WITH 14 CFR 25.5 71 AND 26.43(D). OK TO CF PER EVA 71269. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500205 20080325 00205 NM 2008 3 25 2008UALA01441 1 20080314 A 5320 PLATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 MAIN CABIN DECK PLATE STA 1681 HAS CORROSION TOP SURFACE, RBL 20. ACCOMPLISHED MAJOR REPAIR IN GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500207 20080325 00207 NM 2008 3 25 2008UALA01443 1 20080315 A 5320 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 808UA 804 BEAM 90 IS CORRODED. MAJOR REPAIR ACCOMPLISHED AT DEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500215 20080325 00215 NM 2008 3 25 2008UALA01451 1 20080315 A 5320 SHEAR PLATE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 808UA 804 LEFT SHEAR PLATE CLIP NUT HOLES HAVE CORROSION. CORROSION REMOVED WITHOUT BLENDING ANY METAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500229 20080325 00229 NM 2008 3 25 2008UALA01510 1 20080318 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 LEFT OVERWING EMERGENCY LIGHT LAMP OUT 3RD FROM FWD 1 EA. REPLACED WITH NEW LAMP. OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032600019 20080326 00019 EU 2008 3 26 F3LA200800121 1 20080302 A 2560 D53112191202 FITTING AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE FORWARD, INBOARD, GIRT BAR FITTING NUT PLATE HOLE, BELOW THE BLANKING PLATE, AT THE L-1 DOOR. MAINTENANCE BLENDED OUT THE CORROSION, TREATED AND PAINTED THE AFFECTED AREA IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30106 AND A319 SRM 51-74-00, PARAGRAPH 6. UPON COMPLETION OF THE REPA IR, THE AFFECTED AREA WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032600028 20080326 00028 NM 2008 3 26 DHL2008752508 1 20080223 A 5754 6517327U3 RIB BOEING 727 727223 1384074 NM L/E SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 NR 1 SLAT ACTUATOR INBD ATTACHING RIB (AT SLAT) CRACKED. REMOVED RIB AND "U" CHANNEL FOUND CRACK IAW B727SRM 51-30-2 LO CATED, DRILLEDAND DEBURRED RIB P/N 65-17327U3 PO 7375239 IAW B727 SRM 51-30-5. FABRICATED CHANNEL USING 2024-T3 .071 P O 9005922 DIM 6.5 INCH BY 3.5 INCH IAW BDW NR 65-17327 AND B727SRM51-20-01,51-20-2,51-30-5. INSTALLED RIB AND CHANNEL I AW B727SRM 51-30-2 AT NR 1 SLAT ACTUATOR. 2 L 7 3 4F A3WE 2008032600030 20080326 00030 NM 2008 3 26 DHL2008752511 1 20080226 A 7110 SKIN BOEING 727 727223 1384074 NM NR 3 COWLING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 NR 3 NOSE COWL O/B T/E SKIN CRACKED ABOVE COWL LATCH. INSTALLED REPAIR IAW B727 SRM 54-30-2 FIG 1. 2 L 7 3 4F A3WE 2008032600037 20080326 00037 EU 2008 3 26 08FDEA00952 1 20080314 A 5420 A54610805504 DRAIN LINE AIRBUS 310 A310203 3930313 EU NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 NR 1 PYLON HYD/FUEL DRAIN PAN HAS A 3/4 INCH CRACK ON THE DRAIN TUBE AT 837. REMOVED DRAIN PAN REF A310-300 SRM 51-40-2 1; PG 7. WELD REPAIRED REF AEROSPATIALE DWG IA-546-10805 AND INSTALLED DRAIN PAN REF A310-300 SRM 51-40-21; PG 7. 2 L 7 2 4F RT A35EU 2008032600042 20080326 00042 WP 2008 3 26 08FDEA01002 1 20080317 A 5420 AUB7120501 PANEL DOUG MD10 MD1010F 3022112 WP NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 NR 1 ENGINE PYLON PANEL NR 438CR IS CRACKED. WELD REPAIRED CRACKS IAW DAC DRWG AUB 7120; DPS 4.801 AND DPS 10.225. 2 L 7 3 4F RT A22WE 2008032600052 20080326 00052 NM 2008 3 26 2008UALA01502 1 20080318 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 4A AFT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 4A AFT LIGHT ASSY. SECURED CONNECTOR 2 L 7 4 4F 4 F RT A20WE E24NE 2008032600053 20080326 00053 NM 2008 3 26 2008UALA01503 1 20080318 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 2J AFT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 2J AFT LIGHT ASSY. SECURED CONNECTOR. OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032600054 20080326 00054 NM 2008 3 26 2008UALA01504 1 20080318 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT EEL LIGHT INOP LOWER WALL ACROSS LAV 101. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032600056 20080326 00056 NM 2008 3 26 2008UALA01505 1 20080318 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT EEL LIGHT INOP LOWER WALL AFT OF DOOR 1R. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032600085 20080326 00085 NM 2008 3 26 DL76G080370 1 20080313 A 3397 WIRE BOEING 767 767332 1382001 NM CABIN BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1612T 30575 OVERHEAD LT AISLE EMERGENCY LIGHTS HAS BROKEN WIRE AT STA 1197+132. SPLICED REPAIRED BROKEN WIRE AT LT AISLE EMERGENCY LIGHT STA 1197+132 IAW B767-300 SWPM 20-30-12. NO FAULTS NOTED ON OPS CHECK IAW B767-300 AMM 33-57-05. 2 L 7 2 4F RT A1NM 2008032600167 20080326 00167 EA 2008 3 26 SWIA200819362 1 20080314 A 7830 PDU CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 506CA 7793 FLT 2655 - RECEIVED A "R REV UNLOCK" MESSAGE IN FLIGHT. REPLACED RIGHT THRUST REVERSER PNEUMATIC DRIVE UNIT IAW AMM 78- 32-03. OPS CHECK GOOD, P/N: 126758-7, S/N OFF: 2991. 2 L 7 2 4F RT A21EA 2008032600172 20080326 00172 NM 2008 3 26 NSVA2008010 1 20080317 A 5230 HANDLE BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR UNSECURE A NSVA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 191WQ 4191 AFTER PASSING 14000 FT FUSELAGE DOOR ANNUNCIATOR LIGHT ILLUMINATED, FOUND CARGO DOOR TO SHOW OPEN ON MFD, LOST PRESSURI ZATION AND FA REPORTED LOUD NOISE COMING FROM THE BACK LEFT SIDE. RETURNED TO FIELD. FOUND AFT BAGGAGE DOOR "T" HANDLE POPPED OUT. RESECURED HANDLE, WARNING LIGHTS EXTINGUISHED. PERFORMED OPS CHECK IAW AMM 52-31-01. CHECKS GOOD. 2 H 7 2 4T RT A13NM 2008032600174 20080326 00174 NM 2008 3 26 QXEA200800292 1 20080313 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - C4- RIGHT INBOARD SEAT TRACK NR 15 HAS MINOR SCRATCHES AT STA X609 TO X 620. BLENDED SCRATCHES ON RIGHT INBOARD SEAT TRACK NR 15 AT STA X609 TO X620 REF RD8/4-53-884. HFEC INSPECTION BLENDED AREA FOR CRACKS IAW Q400 NDTM PART 6, 51 -00-01, NO CRACKS NOTED. APPLIED ALODINE TO BLENDED AREAS OF SEAT TRACK IAW D8 Q400 SRM 51-21-10. 2 H 7 2 4T RT A13NM 2008032600185 20080326 00185 NM 2008 3 26 QXEA200800295 1 20080313 A 5230 SUPPORT BOMBDR DHC8 DHC8402 1390042 NM MID CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - C4- MCD LAYSHAFT AFT SUPPORT IS CORRODED. REMOVED 3 BOLTS, NUTS, WASHERS, REMOVED AFT LAYSHAFT SUPPORT AND INSTAL LED SERVICEABLE SUPPORT FROM STOCK. SECURED WITH 3 BOLTS NUTS AND WASHERS. 2 H 7 2 4T RT A13NM 2008032600189 20080326 00189 CE 2008 3 26 DJFA2008031 1 20080323 A 2170 DUCT RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP WATER SEPARATOR LOOSE E DJFA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 23 828CW 258428 WHILE IN CRUISE, FL 390 THE PILOTS STARTED TO SENSE A CHANGE IN CABIN PRESSURE BASED ON HOW THEIR EARS FELT. THEY THEN L OOKED AT THE PRESSURIZATION INSTRUMENTATION AND CONFIRMED THERE WAS CABIN PRESSURIZATION PROBLEM. PUT ON OXYGEN MASKS A ND INITIATED AN EMERGENCY DESCENT TO 10000 FT. CABIN PRESSURE CLIMBED AT A RATE OF 6000 FT PER MINUTE. DECLARED AN EMERG ENCY AND UPON REACHING A 10000 FT DECIDED TO CONTINUE ON TO DESTINATION. MX FOUND THE WATER SEPERATOR DUCT COUPLINGS LOOSE. MX RESECURED DUCTS AND PERFORMED AND GOOD OPS AND LEAK CHECK. 2 L 7 2 4F 4 F RT A3EU E6WE 2008032600191 20080326 00191 CE 2008 3 26 DXTA20082952 1 20080320 A 5240 LATCH CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE TAIL DOOR OBSTRUCTED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 686QS 5605661 AC DOOR LIGHT (TAIL) ILLUMINATED ON TAKEOFF. FOUND BAGGAGE AFT UPPER LATCH STIFF. CLEANED SLIDE (BAYONET) AND HINGE PO INTS AND LUBED. REMOVED UNIT FROM BAYONET RECEPTACLE. ADJUSTED SPRING TENSION. FOUND TAILCONE FWD ACCESS DOOR AFT UPP ER LATCH STIFF AND RUBBING STROBE. CLEANED, ADJUSTED AND LUBED LATCH. ADJUSTED TAILCONE FWD ACCESS DOOR SWITCH 1 FLAT. OVERTRAVEL PART ACTUATION NOW .080". IAW MM 52-30-01 & 52-40-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032600193 20080326 00193 NE 2008 3 26 DXTA20082954 2 20080320 A 7320 ENGINE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LEFT POWER LOSS E DXTA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 07 693QS 5605657 LT ENGINE WILL NOT MAKE TAKEOFF POWER IN THE TAKEOFF DETENT AND WITH EECS IN AUTO AND FAILED TO MANUAL. RAN ENGINES AT 88.4 PERCENT N1 WITH SEVERAL ACCELERATIONS AND DECELERATIONS WITH NO FAULTS FOUND I/A/W FAULT ISOLATION SECTION OF MM 72 -00-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032600194 20080326 00194 NM 2008 3 26 DXTA20082955 1 20080321 A 2612 FUSE GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE FIRE DETECTION FAILED E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 755QS 168 AFTER ENGINE START (BOTH ENGINES STARTED) WITH ECS SELECTOR STILL IN (RAM), APU FIRE WARNING MESSAGE ILLUMINATED. T/S F OUND BLOWN FUSE 405. REPLACED FUSE WITH NEW PART. OPS CHECK GOOD. IAW MM 26-10-25. 2 L 7 2 4F 4 F RT A53NM E35NE 2008032600198 20080326 00198 CE 2008 3 26 DXTA20082957 1 20080321 A 3260 SQUAT SWITCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG OUT OF ADJUST E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 975QS 7500175 DURING TAKEOFF, NOSE GEAR DID NOT RETRACT. REMOVED AND REPLACED NLG SQUAT SWITCH CAM AND SPACER IAW MM 32-20-00. ADJUST ED SWITCH IAW MM 32-60-00. OPERATIONAL CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032600203 20080326 00203 CE 2008 3 26 DXTA20082960 1 20080323 A 2701 SPROCKET CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE CONTROL COLLUMN OBSTRUCTED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 374QS 5600475 JAMMED ELEVATOR TRIM TAB ON DEPARTURE. FOUND FOD WEDGED IN CHAIN SPROCKET AREA OF PEDESTAL. REMOVED FOD, NO DAMAGE NOTE D, CLEANED AND LUBED TRIM COMPONENTS, OPS CHECK AND TRAVEL CHECKS GOOD AT THIS TIME. REF. CE560 M/M 27-31-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2008032600210 20080326 00210 EU 2008 3 26 08FDEA01032 1 20080318 A 5730 A5724398500100 ACCESS PANEL AIRBUS 310 A310203 3930313 EU RT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT WING L/E LOWER SURFACE ACCESS PANEL 623 GB EDGES IS CHAFED AND HAS 3 WEAK SPOTS. BLENDED CHAFED AREA IAW SRM 51-73-1 0. ORIGINAL THICKNESS 0.056. REMAINING THICKNESS 0.054 IAW A57243224 DWG. FOUND TO BE WITHIN LIMITS. ALODINED IAW SRM 51-21-01. PRIMED IAW SRM 51-23-01. RESTORED CIC IAW AMM 51-22-00. 2 L 7 2 4F RT A35EU 2008032600240 20080326 00240 WP 2008 3 26 08FDEA01062 1 20080319 A 5753 S391318172 WEDGE DOUG MD10 MD1010F 3022112 WP T/E FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RT OUTBD FLAP T/E WEDGE IS DELAMINATED. REMOVED T/E SECTION IAW SRM 51-35-01 VOL II. LOCATED, DRILLED & DEBURRED NEW T/ E SECTION IAW SRM 57-20-00 FIG 10 VOL I. INSTALLED T/E SECTION IAW SRM 57-20-00 FIG 10 VOL I. 2 L 7 3 4F RT A22WE 2008032600265 20080326 00265 EU 2008 3 26 08FDEA01093 1 20080321 A 5542 PANEL AIRBUS 310 A310324 3930206 EU RUDDER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 LEFT RUDDER PANEL, 4TH FASTENER FROM THE TOP OF THE RUDDER HAS WATER IN 5 CONNECTED CELLS; 2 INDIVIDUAL CELLS AND DELAMI NATION 1.8" BY 1.7", MARKED IN WHITE MARKER. REPAIRED LT RUDDER PANEL SKIN 4TH FASTENER FROM TOP BY REMOVING DELAMINATE D AREA & APPLIED REPAIR PLIES IAW EA 6-5540-118453. 2 L 7 2 4F RT A35EU 2008032600268 20080326 00268 CE 2008 3 26 EPUA031608 1 20080308 A 5531 RIB BEECH 1900 1900C 1154161 CE VERTICAL STAB CRACKED E EPUA K NONE O OTHER IN INSP/MAINT 1 AL 03 404GV UC154 CRACK DISCOVERED DURING ROUTINE INSP ON VERT STAB RIB FLANGE AT RIB STRINGER INTERSECTION 39.5 AND RIB 54.026 CANT STAB STA, RT SIDE. REPAIRED CRACK IAW WITH APPROVED DATA, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2008032600269 20080326 00269 EU 2008 3 26 08FDEA01129 1 20080324 A 5320 603408*18 FLOOR SUPPORT AIRBUS 300 A300B4622 3930401 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 720FD 417 MAIN CARGO COMPARTMENT FLOOR SUPPORT BETWEEN FR 14 AND FR 16 RBL 40 HAS CORROSION IN SEVERAL PLACES ON LOWER SURFACE ARO UND FASTENER HOLES REMOVED FLOOR SUPPORT BEAM IAW SRM 51-40-21. FABRICATED NEW FLOOR SUPPORT BEAM IAW SRM 53-12-15 AND SPLICES, LOCATED AND DRILLED IAW SRM 51-12-15. ALODINE AND PRIMED IAW SRM 51-21-10. INSTALLED NEW FLOOR SUPPORT AND SP LICES IAW SRM 53-15-15. 2 L 7 2 4F RT A35EU 2008032400096 20080324 00096 EU 2008 3 24 F3LA200800094 1 20080308 A 2560 D5348015800600 PLATE AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE FORWARD, LOWER GIRT BAR PLATE AT THE L-2 DOOR. MAI NTENANCE REMOVED AND REPLACED THE GIRT BAR PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 5-42-12-991-003B. UPON COMP LETION OF THE REPLACEMENT, THE NEW PLATE WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400119 20080324 00119 EA 2008 3 24 COMA0860165 1 20080310 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 957CA 7109 DURING HMV INSPECTION, VISUAL INSPECTION FOUND UPPER EDGE OF FLOOR DECK SUPPORT WEB CORRODED AT FS 280. CUT OUT CORRODE D EDGE AND INSTALLED FILLER AND DOUBLER PER EA 10-5310-02124. 2 L 7 2 4F RT A21EA 2008032400122 20080324 00122 EA 2008 3 24 COMA0860168 1 20080310 A 5320 601R53410566 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 957CA 30563 7109 CRACK FOUND ON RBL 18 AT FS 409+128 ON OUTBOARD SIDE OF VERTICAL BEAM LOWER. REPAIRED IAW REO 601R-53-41-056. 2 L 7 2 4F RT A21EA 2008032400136 20080324 00136 NM 2008 3 24 WRLA2008030 1 20080313 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 48407 DURING C-CHECK INSPECTION FOUND MAIN DECK FLOOR PANEL SUPPORT SEAT TRACK CRACKED STA Y=755 X=+75.25. REPAIRED PER SRM VOL.III 53-70-00 FIGURE 1 REV.40. 2 L 7 3 4F 4 F RT A22WE E24NE 2008032400142 20080324 00142 EA 2008 3 24 COMA0860172 1 20080312 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 957CA 7109 DURING HMV-6 INSPECTION, NDT (HK) FOUND CRACK AT LOWER END OF VERTICAL STIFFENER, FS 409+128, LBL 18. CUT OUT DAMAGE AN D INSTALLED DOUBLER IAW BOMBARDIER REO 601R-53-41-056. 2 L 7 2 4F RT A21EA 2008032400237 20080324 00237 NM 2008 3 24 DHL2008753508 1 20080227 A 5720 BEAM BOEING 727 727223 1384074 NM LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 "C" CHECK, LT WING UPPER T/E PANEL SUPPORT "J" BEAM WBL 124 HAS DOUBLER REPAIR. REMOVED "J" BEAM IAW B727 SRM 51-30-2. FABRICATED NEW "J" BEAM PER DRAWING 65-21655 REV J AND EC-00829-001 FROM BAC1506-860 7075T6 DIM.81" PO NR 738052. TREA TED AND PRIMED IAW B727 SRM 51-10-2. LOCATION OF BEAM IS LT WING WBL 124 IDENTIFIED PART AS 65-21655 440 PER EC-00829-0 01. INSTALLED "J" BEAM IAW B727 SRM 51-30-2 AND DRAWING 65-21655. 2 L 7 3 4F A3WE 2008032400240 20080324 00240 NM 2008 3 24 NWAA080955808 1 20080315 A 3350 POWER SUPPLY BOEING 757 757351 1384991 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 588NW 32988 DURING OVERNIGHT CHECK, FOUND EMERGENCY LIGHTS FROM ROWS 14 TO 27 INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY, AND OPERATIONAL CHECKED GOOD, AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2008032400244 20080324 00244 EU 2008 3 24 F3LA200800116 1 20080305 A 5321 D5361087600100 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE LOWER SURFACE OF FLOOR PANEL 222FF. MAINTENANCE RE MOVED AND REPLACED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-12-12-400-001. FOLLOWING COMPLETION OF THE REPLACEMENT, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400246 20080324 00246 NM 2008 3 24 SWAA081391 1 20080313 A 5330 65C381921 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 857, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032400260 20080324 00260 NM 2008 3 24 SWAA081407 1 20080313 A 5315 6545834 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 294, LBL 12 TO RBL 4. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2008032400263 20080324 00263 NM 2008 3 24 SWAA081398 1 20080313 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 747SA 29799 L1 DOOR EMERGENCY EXIT LIGHT LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008032400274 20080324 00274 NM 2008 3 24 2008UALA01360 1 20080312 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 37 ABC. REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032400344 20080324 00344 EU 2008 3 24 08FDEA00974 1 20080314 A 5347 RAIL AIRBUS 310 A310203 3930313 EU CARGO TRAY BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FWD CARGO COMPARTMENT; ROLLER TRAY SIDE RAIL IS BENT; BY CARGO DOOR OPENING JUST ABOVE DOOR SPOOL NR 3. ROLLER TRAY FOU ND TO BE OUT OF LIMITS IAW SRM 53-10-00 REMOVED AND REPLACED IAW AMM 25-52-21-4 PARA 2B & 2D. FABBED IAW DWG. A25771256. ALODINED IAW SRM 51-21-10. PRIMED & PAINTED IAW SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008032400345 20080324 00345 EU 2008 3 24 08FDEA00975 1 20080314 A 5730 A5724852600000 PANEL AIRBUS 310 A310203 3930313 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LEFT WING PANEL (WS 66-151) FOIL ON THE BACK OF THE PANEL IS PEELING OFF AND THE PANEL IS PUNCTURED. REPAIRED LT WING PA NEL WS 66-151, BY APPLYING REPAIR PLIES IAW SRM 51-77-10 & 51-77-12. REMOVED DAMAGED FOIL IAW SRM 57-42-12. APPLIED NEW FOIL IAW SRM 57-41-12. APPLIED SURFACE FINISH IAW SRM 51-75-10, PRIMED IAW SRM 57-41-12. 2 L 7 2 4F RT A35EU 2008032400347 20080324 00347 WP 2008 3 24 08FDEA00977 1 20080317 A 5730 ARC0619506 PANEL DOUG MD10 MD1010F 3022112 WP RT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RT WING LOWER T/E PANEL NR 651 BB AT THE OUTBD FLAP IS CHAFED ON THE INBD INNER SKIN. REPAIRED IAW SRM 51-71-00 VOL II & DWG ARC 0781. REMOVED & INSTALLED PANEL & SEAL IN REF TO SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2008032400351 20080324 00351 WP 2008 3 24 08FDEA00980 1 20080317 A 5744 ARC06221 HINGE DOUG MD10 MD1010F 3022112 WP LT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 FRAGMENTS ARE MISSING FROM THE INBD PIANO HINGE ON PANEL 551 CB LT WING T/E LOWER SURFACE. REMOVED PANEL IAW SRM 51-3 1-01; VOL II. REMOVED HINGED PANEL IAW SRM 51-33-01 VOL II. LOCATED & DRILLED HOLES IAW SRM 51-33-01 VOL II. ALOD INED & PRIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II. INSTALLED PANEL & HINGE IAW SRM 51-31-01 & 51-33-01 VOL II. PAINTED IAW SRM 51-21-01 PG 8 VOL II. 2 L 7 3 4F RT A22WE 2008032400353 20080324 00353 NM 2008 3 24 2008UALA01392 1 20080312 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 DENT IN EXTERNAL FUSELAGE SKIN AT BS 369 JUST ABOVE STR 19R. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032400357 20080324 00357 WP 2008 3 24 08FDEA00992 1 20080317 A 5321 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 CENTER PIT FLOOR PANEL 183 KF HAS CRACKED SKIN AND THE EDGES ARE DELAMINATED. FABRICATED A NEW CTR PIT FLOOR BOARD IAW DWG SRZ 25-005; REV E. PART MARKED NEW PANEL IAW GMM 7-0-1000. 2 L 7 3 4F RT A22WE 2008032400358 20080324 00358 WP 2008 3 24 08FDEA00993 1 20080317 A 5330 ADA31391 SKIN DOUG MD10 MD1010F 3022112 WP BS 820 S37L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 DENTED; EXTERNAL SKIN AT STA 820; BELOW LONGERON 37L. REPAIRED AREA OF SKIN AT STA 820; BELOW LONGERON 37L IN REFEREN CE WITH SRM 53-20-00 VOL I FIGURE 13. EXTERNAL DOUBLER HAS A EDGE DISTANCE TO HEIGHT RATIO OF 211 THAT IS WITHIN LIMITS IAW SRM 53-00-02 VOL II FIGURE 1 SHEET 2. MINOR REPAIR 2 L 7 3 4F RT A22WE 2008032400362 20080324 00362 2008 3 24 2008UALA00051 4 20080103 A 2211 8220006103 COMPUTER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE AUTOPILOT SYS SHORTED A UALA O OTHER W INADEQUATE Q C DE DESCENT 1 WP 29 799UA 26926 NO LAND 3 DEGRADATION IN AUTOLAND SYSTEM PRIOR TO APPROACH (BEFORE LAND 3 AUTOLAND STATUS ANNUNCIATION). AUTOPILOT FLIG HT DIRECTOR COMPUTER (RIGHT) A LIVE CIRCUIT IS OPEN OR SHORTED. REPLACED AFDC RT. RT LRU TEST PASSED. RETURNED TO CAT 3 STATUS. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032400395 20080324 00395 2008 3 24 SWAA081439 4 20080314 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 498WN 32480 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032400399 20080324 00399 NM 2008 3 24 SWAA081460 1 20080317 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500C, STR 28L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032400422 20080324 00422 NM 2008 3 24 SWAA081469 1 20080317 A 5315 6545834 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 312, LBL 12 TO RBL 12. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2008032400433 20080324 00433 EA 2008 3 24 A6WA200840091 1 20080213 A 2520 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CABIN CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 REPAIR CRACK ON PAX DOOR AFT SIDEWALL LOWER SIDE FWD OF DOOR ASSIST MOTOR PULLEY ASSY. (K) CRACK ON PAX DOOR REPAIRED IAW REO 601-52-11-513 REV A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008032400436 20080324 00436 EU 2008 3 24 COEA0803819 1 20080115 A 5714 S53573201 ANGLE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE WING BOX CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 819FX * 359 FOUND DURING HEAVY CHECK, LT AND RT AFT UPPER WING PRESSURE DECK INTERNAL SPLICE ANGLES CRACKED. AFT OF FRAME 27 AT STR INGERS 4L AND 4R. LT ANGLE PN IS S53573201210, RT S53573201211. SRAS, SHEET REF: SO/TS-232/08/4462. DAMAGES LEFT, AS IS AFTER INSPECTION PERFORMED IAW ATR REF DO/TS-232/08-9756 AND DO/TS-254/08-9756. WO 73513, NR 200018. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008032500012 20080325 00012 CE 2008 3 25 DXTA20082892 1 20080221 A 3260 9006EN42 DOWNLOCK SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP MLG INOPERATIVE E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 811QS 3437 258614 AFTER TAKEOFF, GOT RED NOSE GEAR RT GEAR AND LT GEAR INDICATIONS ALSO GREEN LT GEAR INDICATION. REPLACED LT GEAR DOWN LO CK SWITCH IAW MM 32-60-00. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A3EU E6WE 2008032500013 20080325 00013 CE 2008 3 25 DXTA20082893 1 20080221 A 3233 99125373 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 697QS 6277 5605197 WHILE RESETTING HYD CONTROL CIRCUIT BREAKER , L T MAIN GEAR EXTENDED AND GREEN DOWN AND LOCKED LIGHT ILLUMINATED. REMOVE D AND REPLACED LT MAIN GEAR ACTUATOR WITH RENTAL UNIT IAW MM 32-30-04. OPS AND LEAK CHECK GOOD. INSTALLED UNIT HAS 208 9 CYCLES. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500023 20080325 00023 CE 2008 3 25 DXTA20082900 1 20080226 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE LAVATORY ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 131QS RK431 ELECTRICAL ODOR IN LAVATORY. REMOVED ALL PANELS IN LAV AREA. COULD NOT DUPLICATE ODOR. INSPECTED ALL WIRES, PC BOARDS TERMINALS ETC. FOR SIGNS OF DAMAGE. NO DEFECTS NOTED. SUPPLIED GROUND POWER TO AIRCRAFT THROUGHOUT ENTIRE INSPECTION P ROCESS. SUPPLIED GROUND POWER FOR ONE HOUR ETC. NO DISCREPANCIES. 2 H 7 2 4F RT A16SW 2008032500029 20080325 00029 CE 2008 3 25 DXTA20082905 1 20080228 A 3233 99125373 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 603QS 496 5605203 UPON LOWERING THE LANDING GEAR THE RED (UNSAFE) LIGHT REMAINED ILLUMINATED AND THE LT MAIN GEAR GREEN LIGHT REMAINED OFF . LT GEAR ACTUATOR REPLACED WITH RENTAL UNIT. SYS TESTED IAW MM 32-30-04. ACTUATOR REPLACED DUE TO SUSPECTED INDICATI ON FAILURE. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500036 20080325 00036 CE 2008 3 25 DJFA2008022 1 20080302 A 5510 SUPPORT BRACKET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 751TA RK225 DURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED I N COMMUNIQUE' NR 70. THE LT AND RT RIB ASSEMBLIES WERE REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2008032600272 20080326 00272 NM 2008 3 26 AALA200800504 1 20080304 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 921AN 29522 MIA - EMERGENCY LIGHT AT SEAT ROW 22 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 22. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008032600275 20080326 00275 NM 2008 3 26 NSVA2008011 1 20080319 A 2120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM CABIN ODOR A NSVA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 188WQ 4188 ELECTRICAL BURNING TYPE SMELL IN AFT GALLEY SECTION OF AIRCRAFT. ATTEMPTED TO LOCATE SMELL IN CABIN, GAINED ACCESS TO T HE GALLEY LIGHT CONTROL PANEL, VISUALLY INSPECTED SWITCHES AND BALLAST, FOUND NO OBVIOUS DAMAGE TO BALLAST OR ELECTRICAL CONNECTOR. OPENED REAR SERVICE DOORS, A/C CLEARED OF SMELL SELECTED CABIN LIGHTING ON WHILE APU WAS RUNNING AND SMELL RETURNED THEN SHUT DOWN APU, INSPECTED APU COMPARTMENT FOUND OIL SERVICE LEVEL NORMAL, BUT FOUND CARBON LIKE FILM ON GEN ERATOR, WITH A/C NOW ON GPU POWER AND APU SHUT OFF SELECTED ALL CABIN INTERIOR LIGHTING ON FOR APPROX 45 MIN. CABIN AND GALLEY REMAINED FREE OF ELECTRICAL FUMES, THEN ALONG WITH MXCO DETERMINED POSSIBLE CAUSE OF FUMES TO COME FROM APU WHIL 2 H 7 2 4T RT A13NM 2008032600279 20080326 00279 NM 2008 3 26 08FDEA01051 1 20080319 A 3232 651783013 ACTUATOR BOEING 727 727233 138408A NM RT MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 274FE 2069 2069 22039 RED GEAR DOORS LIGHT AND RIGHT GEAR RED UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. AMBER RIGHT GEAR DOOR LIGHT ON S/O PANEL ALSO ILLUMINATED. REPLACED RT MAIN GEAR ACTUATOR IAW AMM 32-32-002-4, AND RT MAIN GEAR CYCLES UP AND DOWN NOR MAL WITH NO LEAKS NOTED. PREMATURE REMOVAL/INSTALLATION OFF MFG 65-17830-13. 2 L 7 3 4F RT A3WE 2008032600280 20080326 00280 EU 2008 3 26 08FDEA01067 1 20080319 A 2611 CG7G011 SMOKE DETECTOR AIRBUS 310 A310324 3930206 EU E&E BAY FAILED A FDEA K NONE N FALSE WARNING UK UNKNOWN 1 SO 25 814FD 1307 1307 534 MIN EQUIPMENT BAY SMOKE INDICATION CAME ON INTERMITTENTLY, THEN STAYED ON CONSTANT. RAN ECAM ITEMS AND CHECKLIST (QRH ). NO VISIBLE INDICATIONS OF SMOKE. PROBLEM CLEARED ITSELF AFTER ABOUT 2 MINS. REMOVED AND REPLACED MIN EQPT BAY SMO KE DET (12WA) PER M/M 26-15-12-4. OPS CHECK GOOD. ALSO, CLEANED UP EXCESSIVE WATER UNDER ACCESS PANEL 134AR AND SURROU NDING AREA BY DET 12WA. 2 L 7 2 4F RT A35EU 2008032600284 20080326 00284 EU 2008 3 26 08FDEA01072 1 20080320 A 5730 A57260300007 SKIN AIRBUS 300 A300B4622R 3930312 EU RT WING TIP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CORROSION AROUND STATIC DISCHARGER OUTBOARD, WING TIP RT. REPAIR PERFORMED BY BLEND OUT OF CORRODED AREA AND INST ALLING A REPAIR PATCH IAW RAS/FOK/319/2007 ISS A, APPROVED EA 6-5730-114859. 2 L 7 2 4F RT A35EU 2008032600286 20080326 00286 EU 2008 3 26 08FDEA01074 1 20080320 A 5730 A57260300006 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING TIP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND OLD CORROSION REPAIR UNDER STATIC DISCHARGER, LT WING TIP WITHOUT DOCUMENTATION REPAIR PERFORMED BY BLEND OUT CO RROSION AND INSTALLING A REPAIR PATCH IAW RAS/FOK/016/2008 ISS A, APPROVED BY EA 6-5730-114884. 2 L 7 2 4F RT A35EU 2008032600287 20080326 00287 EU 2008 3 26 08FDEA01075 1 20080320 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CORROSION ON BOTTOM SKIN AT RIB 4 REAR SPAR AREA. REPAIR PERFORMED BY REWORK OF CORRODED AREA IAW RAS/BAE/1006318 /2008, APPROVED BY EA 6-5720-114866. 2 L 7 2 4F RT A35EU 2008032600292 20080326 00292 NM 2008 3 26 08FDEA01080 1 20080320 A 5347 BAC1520792 SEAT TRACK BOEING 727 727227 1384078 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 MAIN DECK FLOOR SEAT TRACK, BS 1124 - 1125, LBL 45 - 46, HAS CORROSION AROUND FASTENER HOLE, UPPER AND LOWER SURFACE. REMOVED AND REPLACED SEAT TRACK, IAW SRM 53-10-5. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008032600295 20080326 00295 NM 2008 3 26 DL757080385 1 20080317 A 3244 TIRE BOEING 757 757232 1384965 NM LANDING GEAR BLOWN A DALA O OTHER O OTHER TO TAKEOFF 1 SO 27 689DL 27172 BLOWN TIRE NR 7, REPLACED NR 7 WHEEL ASSY PER MM. 2 L 7 2 4F RT A2NM 2008032600296 20080326 00296 NM 2008 3 26 DL76G080387 1 20080318 A 5420 112T700540 SHIM BOEING 767 767332 1382001 NM NR 2 PYLON MIGRATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1603 29695 MIGRATED SHIM BETWEEN NR 2 PYLON AFT PITCH LOAD FITTING AND WING SKIN. PITCH LOAD FITTING AND DAMAGED SHIM WAS REMOVED, SHIM WAS REPLACED AND PITCH LOAD FITTING WAS REINSTALLED. 2 L 7 2 4F RT A1NM 2008032600297 20080326 00297 GL 2008 3 26 DL764080388 2 20080317 A 7200 CF680C2B8F ENGINE BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 1 MAKING METAL A DALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 839MH 22163 29712 706382 RTO DUE TO NR 1 ENG STALLED. REPLACED NR 1 ENG. FOUND METAL IN TAILPIPE. 2 L 7 2 4F 4 F RT A1NM E23EA 2008032600298 20080326 00298 NE 2008 3 26 DL76L080389 2 20080317 A 7200 BEARING BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE LEAKING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 61567 723843 27583 723843 DUE TO HOC INSPECTED FOR LEAK FOUND NR 3 BEARING LEAKING. REPLACING ENGINE NR 2 ENG. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032600300 20080326 00300 EU 2008 3 26 MALA080039 1 20080317 A 5753 SKIN SAAB SF340 340B 7860101 EU T/E FLAP DEBONDED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 444XJ 340B444 LT FLAP TRAILING EDGE UPPER SKIN HAS 6 DISBONDED DENTS. REPAIRED IAW EO S57179. 2 L 7 2 4T RT A52EU 2008032600301 20080326 00301 EU 2008 3 26 MALA080040 1 20080317 A 5230 SKIN SAAB SF340 340B 7860101 EU CARGO DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 444XJ 340B444 CARGO DOOR EXTERIOR SKIN HAS 2 DENTS. REPAIRED IAW EO NR S52107. 2 L 7 2 4T RT A52EU 2008032700001 20080327 00001 NM 2008 3 27 DL764080304 1 20080302 A 7500 2780539104 ISOLATION VALVE BOEING 767 767432ER 1385134 NM RT BLEED INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 828MH 29699 REPEAT EICAS MSG R BLEED ISOLATION VALVE DISPLAYED WITH R ISLN LIGHT ILLUM WITH SWITCH UNLATCHED. BOTH ENGINES RUNNING AND APU SHUTDOWN. REMOVED AND REPLACED RT BLEED ISOLATION VALVE. RAN RT ENG, OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A1NM 2008032500037 20080325 00037 NM 2008 3 25 SWAA081454 1 20080314 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 765SW 29805 R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008032500038 20080325 00038 CE 2008 3 25 DJFA2008023 1 20080302 A 5511 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 479LX RK397 DURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT AND RT IB RIBS WERE FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED I N COMMUNIQUE' NR 70. THE LEFT AND RIGHT RIB ASSEMBLIES WERE REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2008032500039 20080325 00039 NM 2008 3 25 USAA920080580 1 20080222 A 5312 6516300511 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - CRACKED BULKHEAD WEB, BS 178, LBL 12, WL 234. REPAIRED BULKHEAD WEB, BS 178, LBL 12, W L 234 IAW B737 SRM 53-10-08-2R9. 2 L 7 2 4F RT A16WE 2008032500042 20080325 00042 NM 2008 3 25 USAA920080582 1 20080218 A 5754 65C26601180SP SKIN BOEING 737 7373S3 1384711 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - RIGHT WING NR 6 SLAT LOWER SKIN CRACKED, SS 327. REPAIRED RIGHT WING NR 6 SLAT LOWER S KIN IAW B737 SRM 57-43-01-2R6. 2 L 7 2 4F RT A16WE 2008032500044 20080325 00044 NM 2008 3 25 USAA920080583 1 20080220 A 5755 654645165 SKIN BOEING 737 7373S3 1384711 NM LT SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - LEFT WING NR 1 SPOILER UPPER SURFACE HAS DELAMINATION, WS 430.97 - 439.47. REPAIRED LE FT WING NR 1 SPOILER UPPER SURFACE, WS 430.97 - 439.47 IAW B737 SRM 51-70-10-2R. 2 L 7 2 4F RT A16WE 2008032500046 20080325 00046 NM 2008 3 25 USAA920080584 1 20080222 A 5312 651758243 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - CRACKED BULKHEAD VERTICAL BEAM WEB, BS 178, LBL 17.1, WL 228. REPAIRED BULKHEAD VERTIC AL BEAM WEB, BS 178, LBL 17.1, WL 228 IAW B737 SRM 53-10-08-2R12. 2 L 7 2 4F RT A16WE 2008032500047 20080325 00047 EA 2008 3 25 S9BA20080006 1 20080211 A 5413 C6W1512S141S142 LONGERON DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA LT NACELLE CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 573 CPCP INSPECTION, LT NACELLE LONGERONS CORRODED. REMOVED AND REPLACED LT AND RT LONGERON IAW SRM 57-30-00 AND AC43-14, C HAPTER 4 PARA 4-57. 1 H 7 2 3T 4 T RT A9EA E4EA 2008032500049 20080325 00049 EA 2008 3 25 S9BA20080009 1 20080211 A 5712 C6W115628 RIB DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA RT WING CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 573 CPCP INSPECTION, RT WING FWD RIB AT STA 72.5 CORRODED. REMOVED AND REPLACED RIB WITH NEW PART IAW AC43-14, CHAPTER 4 PA RA 4-57. 1 H 7 2 3T 4 T RT A9EA E4EA 2008032500051 20080325 00051 EA 2008 3 25 S9BA20080010 1 20080211 A 5712 C6W115032 RIB DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6A27 52043 EA RT WING CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 573 CPCP INSP, RT WING FWD RIB AT STA.85 CORRODED. REMOVED AND REPLACED RIB WITH NEW PART IAW AC43-14, CHAPTER 4 PARA 4-57. 1 H 7 2 3T 4 T RT A9EA E4EA 2008032500053 20080325 00053 NM 2008 3 25 USAA920080594 1 20080222 A 5312 651758243 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - CRACKED BULKHEAD VERTICAL BEAM WEB, BS 178, RBL 17.1, WL 228. REPAIRED BULKHEAD VERTIC AL BEAM WEB, BS 178, RBL 17.1, WL 228 IAW B737 SRM 53-10-08-2R12. 2 L 7 2 4F RT A16WE 2008032500054 20080325 00054 NM 2008 3 25 USAA920080595 1 20080229 A 5312 651758245 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - CRACKED BULKHEAD VERTICAL BEAM WEB, BS 178, RBL 17.1, WL 183. REPAIRED BULKHEAD VERTIC AL BEAM WEB, BS 178, RBL 17.1, WL 183 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008032500064 20080325 00064 NM 2008 3 25 USAA920080636 1 20080217 A 5753 6546486129 FLAP BOEING 737 7373S3 1384711 NM LT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - LEFT WING INBOARD MIDFLAP HAS DELAMINATION, WBL 73 - WBL 82. REPAIRED LEFT WING INBOAR D MIDFLAP, WBL 73 - WBL 82 IAW B737 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2008032500066 20080325 00066 NM 2008 3 25 USAA920080638 1 20080312 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER CLIP, BS 616, S4L. REPLACED STRINGER CLIP, BS 616, S4L IAW B737 SRM 5 1-40-02. 2 L 7 2 4F RT A16WE 2008032500070 20080325 00070 SW 2008 3 25 AC2A119028 1 20080223 A 5302 427034851101 SUPPORT FITTING BELL 427 427 1182207 SW PWC PW207 PW207D NE TAILBOOM DAMAGED E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 31 427CU 56047 DURING A DAILY INSP SOME WORKING RIVETS WERE FOUND ALONG WITH SHEARED RIVET HEADS AT THE TAILBOOM WHERE THE TAIL ROTOR G EARBOX SUPPORT FITTING ATTACHES. 1 G 7 1 3U 3 U R00001RC E42NE 2008032500079 20080325 00079 NE 2008 3 25 030108N577CS1 2 20080301 A 7532 30J295401 BLEED VALVE CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE NR 2 ENGINE DEFECTIVE E Z5FA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 EA 63 577CS 444 5605726 DD0468 ENROUTE, CREW EXPERIENCED NR 2 ENGINE EEC ANNUNCIATION FOLLOWED BY ENGINE VIBRATION. CREW FOLLOWED CHECKLIST AND FOR PR ECAUTIONS, SHUTDOWN RT ENGINE, DIVERTED AND DECLARED AN EMERGENCY. AC LANDED WITHOUT INCIDENT. CURRENTLY CAUSE IS YET T O BE DETERMINED AND AC IS IN MAINT FOR TROUBLESHOOTING AND REPAIRS. MAINT PERSONNEL INSPECTED AND FOUND FOREIGN DEBRIS IN ENGINE FUEL FILTER. WINGS SUMPED AND NO DEBRIS FOUND. UPON RECOMMENDATION, FUEL CONTROL UNIT AND BOTH ENGINE FUEL FI LTERS WERE REPLACED. WHEN GROUND RUN OF AC WAS PERFORMED, COMPRESSOR SURGING WAS EVIDENT. TROUBLESHOT TO DEFECTIVE COMP RESSOR BLEED VALVE. COMPRESSOR BLEED VALVE AND ASSOCIATED BLEED VALVE SERVO AND TRANSFORMER WERE REPLACED. GROUND RUN P 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500082 20080325 00082 CE 2008 3 25 DXTA20082938 1 20080314 A 2740 SENSOR BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE TEMP FAILED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 119QS RK394 HORIZONTAL STAB FAILED IN FLIGHT. TROUBLESHOT IAW MM 30-12-00 FOUND LEFT STAB TEMP SENSOR TO HAVE SPLIT READINGS FROM P 473 AT THE CONTROLLER, AT 238.3 OHMS AND ONE AT 203.2 OHMS. CLEANED TERMINAL STRIP 061. RECHECKED RESISTANCE FOUND GOOD AT 202 EACH. PERFORMED OPERATIONAL CHECK NO DISCREPANCIES NOTED AT THIS TIME. 2 H 7 2 4F 4 F RT A16SW E25EA 2008032500089 20080325 00089 NM 2008 3 25 DXTA20082943 1 20080316 A 3150 WARNING LIGHT GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 702QS 070 ON TAKEOFF ROLL AT APPROX 60 KIAS, WE GOT A L. BLEED PRESS/TEMP HI CAS. PERFORMED APU & ENGINE RUNS WITH BLEEDAIR SELEC TED ON BOTH ENGINES WITH NO DEFECTS NOTED. THEN PERFORMED BLEED AIR SELECTED ON APU WITH NO DEFECTS NOTED AT THIS TIME W ITH ENGINES & APU RUNNING FOR 45 MIN. NO LT BLEED PRESS/TEMP HIGH MESSAGE. NO DEFECTS NOTED AT THIS TIME IAW MM 21-00-00 & AFM 2 L 7 2 4F 4 F RT A53NM E35NE 2008032500093 20080325 00093 EA 2008 3 25 COMA0860175 1 20080312 A 3010 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYSTEM MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 477CA 7670 FLIGHT 5606 - ON CLIMBOUT FROM BOS RECEIVED ANTI-ICE DUCT WARNING MESSAGE (LEFT FUSELAGE). FOLLOWED QRH, AIRCRAFT DIVER TED TO JFK AND LANDED SAFELY. INSPECTED ANTI-ICE AND BLEED LEAK SYSTEMS. PERFORMED OPS CHECKS, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2008032500096 20080325 00096 CE 2008 3 25 DJFA2008026 1 20080313 A 5511 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 493CW RK93 DURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNI QUE' NR 70. 2 H 7 2 4F 4 F RT A16SW E25EA 2008032500097 20080325 00097 CE 2008 3 25 DXTA20082946 1 20080317 A 2740 99145584 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL PITCH FEEL INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 970QS 8719 7500070 PITCH FEEL FAIL EICAS MESSAGE ILLUMINATED IN FLIGHT. REMOVED AND REPLACED THE PITCH FEEL LINEAR ACTUATOR FOR THE LT AND RT SIDE ELEVATORS. OPS CHECKS GOOD IAW 27-30-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032500103 20080325 00103 NM 2008 3 25 ASMF200803002 1 20080314 A 5610 5893543150 WINDSHIELD BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE RT SIDE SCRATCHED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 851AM 10279 10279 29363 CAPTAIN REPORTED SEVERAL SCRATCHES ON RT WINDSHIELD NR 1. RT WINDSHIELD NR 1 WAS REPLACED IAW MM 56-11-11, TESTED CORRE CT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008032500107 20080325 00107 CE 2008 3 25 DXTA20082947 1 20080318 A 2740 991455812 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL RUDDER LIMIT INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 951QS 6 7500151 RUD LIMIT FAIL A CAS MSG CAME ON IN FLIGHT. RUDDER LIMIT 20 PERCENT. REMOVED ACTUATOR P/N 9914558-12 S/N 072 AND INSTAL LED OVERHAULED ACTUATOR P/N 9914558-12 S/N 086. OPS CHECK IS GOOD. WORK PERFORMED IAW 27-23-00 AND 27-20-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032500110 20080325 00110 CE 2008 3 25 DXTA20082950 1 20080319 A 3411 PITOT SYSTEM CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE AIRSPEED CONTAMINATED E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 834QS 5600669 ON TAKEOFF ROLL F/O AIRSPEED MISCOMPAIRED WITH CAPT A/S, TAKEOFF WAS ABORTED. DRAINED OUT EXCESS WATER FROM THE PITOT PR OBES AND STATIC PROBES, AND PERFORMED AN AIR DATA SYSTEMS - INSPECTION/ CHECK. SYSTEMS CHECKED NORMAL IAW MM REV. 23, 3 4-11-10 & 34-11-26. 2 L 7 2 4F 4 F RT A22CE E00053EN 2008032500111 20080325 00111 NM 2008 3 25 HNAA0800106 1 20080316 A 3320 BVO330211150 LAMP SOCKET DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 EA 07 806EX 41648 41648 263 STRONG SMELL OF BURNING PLASTIC/ELECTRICAL IN GALLEY AREA. AIRCRAFT WAS PARKED AT GATE HAD JUST BEEN DEPLANED. MAINTEN ANCE FOUND A BURNED LAMP SOCKET AT OVERHEAD LIGHT LOCATED AT SEAT 1DF. BULB WAS REMOVED AND MEL PROCEDURES WERE USED. MECHANICS REPLACED BOTH LAMP HOLDERS AND REACTIVATED OVERHEAD LIGHT SYSTEM. 2 H 7 2 4T RT A13NM 2008032500112 20080325 00112 2008 3 25 DXTA20082951 4 20080319 A 2310 7012100825 RMU CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE NR 1 ODOR E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 697QS 5605197 NR 1 RMU SWITCHED ON AND OFF TWICE IN FLIGHT. EACH TIME THIS HAPPENED A STRONG ELECTRICAL ODOR WAS NOTICED. NR 1 COMM CB WAS PULLED. REMOVED RMU AND INSTALLED SERVICEABLE UNIT IAW MM 23-80-01. SYSTEM OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500114 20080325 00114 NM 2008 3 25 ASAA0852710 1 20080318 A 3020 32156184 ANTI-ICE VALVE BOEING 737 737890 1384527 NM NR 2 COWLING MALFUNCTIONED A ASAA K NONE J WARNING INDICATION NR NOT REPORTED 1 NM 02 585AS 35683 ENGINE NR 2 COWL ANTI ICE VALVE LIGHT STAYS BRIGHT BLUE WHEN IN "ON" POSITION. PERFORMED FIM 30 21 TASKS 804 805 STEPS A E3. COULD NOT DUPLICATE PROBLEM. REPLACED NR 2 ENGINE COWL ANTI ICE VALVE. 2 L 7 2 4F RT A16WE 2008032500115 20080325 00115 NM 2008 3 25 SWAA081472 1 20080318 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 225WN 34333 EEPLS LENS LOOSE AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008032500116 20080325 00116 NM 2008 3 25 SWAA081497 1 20080318 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 246LV 32507 EEPLS LENS LOOSE AT ROW 4 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008032400205 20080324 00205 NM 2008 3 24 SWAA081380 1 20080313 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 743, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032400219 20080324 00219 WP 2008 3 24 IXXA08SMN086S 1 20080215 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 200 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT FUSELAGE TAIL SECTION PLATING CRACKED AT STATION FS 1766.000 TO STATION 17 81.000 LONGERON10 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, AND INTERNAL FINGER DOUBLER, AND FILLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-1-11, SRM 51-1-20D, SRM 51-3-1, SRM 53-2-1 FIGURE 7 SHEETS 1, 4, 5, SRM 51-1-21, SRM 53-2-1 FIGURE 7 SHEETS 1, 4, 5, 53-5-1 FIGURE 1 ITEM "A", AND SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008032400222 20080324 00222 NM 2008 3 24 QXEA200800279 1 20080309 A 2611 PU904615 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY FALSE ACTIVATION A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 355PH 500 YKM - FLIGHT 2002 - LAVATORY SMOKE DETECTOR WENT OFF WITH NO SMOKE DETECTED. MAINTENANCE PLACED THE SYSTEM ON MEL 26-4. AIRCRAFT RETURNED TO SERVICE. CLEARED BY REPLACING THE SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 2008032400223 20080324 00223 EU 2008 3 24 F3LA200800108 1 20080305 A 5321 D536715000000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED DELAMINATION WAS FOUND ON THE TOP SURFACE OF FLOOR PANEL 231NF. MAINTENANCE R EPAIRED THE DELAMINATED AREA IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 212. FOLLOWING COMPLETION OF THE REPAIR, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400224 20080324 00224 EU 2008 3 24 F3LA200800109 1 20080302 A 5321 D5367151700000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED DELAMINATION WAS FOUND ON THE UPPER SURFACE OF FLOOR PANEL 252GG. MAINTENANCE REPAIRED THE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 212. FOLLOWING COMPLETION OF THE R EPAIR, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400225 20080324 00225 EU 2008 3 24 F3LA200800110 1 20080302 A 5321 D5367150100000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED DELAMINATION WAS FOUND ON FLOOR PANEL 251NF. MAINTENANCE REPAIRED THE FLOOR P ANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 212. FOLLOWING COMPLETION OF THE REPAIR, THE FLOO R PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400226 20080324 00226 NM 2008 3 24 F3LA200800111 1 20080302 A 5321 D5367150100000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 813FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED DELAMINATION WAS FOUND ON THE TOP SURFACE OF FLOOR PANEL 252NF. MAINTENANCE R EPAIRED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 212. FOLLOWING COMPLETION OF T HE REPAIR, THE FLOOR PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400228 20080324 00228 EU 2008 3 24 F3LA200800113 1 20080302 A 3222 D64433 HINGE PIN AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE NLG CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 530 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED, DURING THE PERFORMANCE OF DYE PENETRANT INSPECTION OF THE NOSE LANDING GEAR H INGE PIN, A CRACK WAS FOUND IN THE CENTER TORQUE PIN. MAINTENANCE REMOVED AND REPLACED THE CENTER TORQUE PIN IN ACCORDA NCE WITH THE REQUIREMENTS OF AMM 32-21-13-400-001, STEP 4B (17) TO (23). ON COMPLETION OF THE REPLACEMENT, THE INSTALLA TION WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032400230 20080324 00230 NM 2008 3 24 DHL2008753502 1 20080227 A 5720 SUPPORT BOEING 727 727223 1384074 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 DURING "C" RT WING UPPER T/E WBL 124 "J" BEAM PANEL SUPPORT IS CRACKED FWD OF SPOILER ACTUATOR. REMOVED "J" BEAM IAW B7 27 SRM 51-30-2. FABRICATED NEW "J" BEAM PER DRAWING 65-21655 REV J AND EC-00829-001 FROM BAC1506-860 7075T6 DIM.81" PO NR 738738052. TREAT AND PRIMED IAW SRM 51-10-2. INSTALLED "J" BEAM IAW SRM 51-30-2. LOCATION OF BEAM IS RT WING WBL 1 24. IDENTIFIED PART AS 65-21655-4405P PER EC-00829-001 STEP 6. MAJOR REPAIR/PERMANENT REPAIR. 2 L 7 3 4F A3WE 2008032400256 20080324 00256 NM 2008 3 24 SWAA081411 1 20080313 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008032400270 20080324 00270 NM 2008 3 24 Y2LA200800015 1 20080313 A 5610 NP1653133 WINDOW AIRBUS A319 A319111 3930336 NM COCKPIT CRACKED A Y2LA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 554SX 3309 AT CRUISE LEFT AFT COCKPIT WINDOW OUTER PANE CRACKED WITH NUMEROUS CRACKS. APPROX 25 MIN LATER ECAM MESSAGE APPEARED L WINDOW HEAT INOP. REMOVED LEFT FIXED WINDOW PER AMM 56-11-12 PB 401 AP 2661665. INSTALLED LT FIXED WINDOW AND TORQUED PER AMM 56-11-12 PB 401. 2 L 7 2 4F RT A28NM 2008032400271 20080324 00271 NM 2008 3 24 2008UALA01357 1 20080311 A 5313 STRINGER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 STRINGER 23R AT STA 288 DAMAGED. MAJOR REPAIR: ACCOMPLISHED REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032400319 20080324 00319 NM 2008 3 24 2008UALA01371 1 20080312 A 3350 1317 BULB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 651UA 25389 DOOR 2 LEFT EXTERIOR EMERGENCY EXIT LIGHT INOP. SUSPECT BURNED OUT BULB. REPLACED LAMP OPS CHECKED GOOD. AC OK FOR SERV ICE 2 L 7 2 4F 4 F RT A1NM E24NE 2008032400332 20080324 00332 NM 2008 3 24 2008UALA01378 1 20080312 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 UPPER FUSELAGE EXTERIOR SKIN HAS AREAS OF WEAR UNDER LT & RT SIDES OF DORSAL FIN LANDING FROM BS 908-1006. BLENDED WORN AREA & ACP NDT FOR MATERIAL LOSS. FABRICATED & INSTALLED BONDED WEAR STRIPS REF EA 080202. THIS REPAIR IS APPROVED AS A N AMOC TO AD 2004-22-05 AND REQUIRES REINSPECTION AT 60,000 CYCLES AFTER REPAIR INSTALLED.THIS REPAIR THRESHOLD IS COVE RED BY CARRIER REPAIR ASSESSMENT PROGRAM EC 95-5330-095SA-A. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032400346 20080324 00346 NM 2008 3 24 2008UALA01385 1 20080312 A 2560 65451433 WINDOW BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EVAC SLIDE COVER CRACKED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 381UA 24656 FWD GALLEY DOOR ESCAPE SLIDE COVER, PRESSURE GAUGE WINDOW IS CRACKED. REPLACED VIEWING WINDOW OF SLIDE COVER ASSY REF G PM 6-0-0-008 PG 6. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032400387 20080324 00387 NM 2008 3 24 SWAA081431 1 20080315 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032400401 20080324 00401 NM 2008 3 24 SWAA081462 1 20080317 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 27R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032500020 20080325 00020 2008 3 25 DXTA20082898 4 20080224 A 2310 7012100825 RMU CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE NR 1 ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 616QS 2927 5605345 10 MINUTES AFTER TAKEOFF CREW SMELLED A BURNING PLASTIC LIKE ODOR. REMOVED NR 1 RMU PN 7012100-825 SN 98112277 AND INST ALLED REPAIRED UNIT PN 7012100-825 SN: 00102968. OPERATIONAL TEST IS GOOD REF EXCEL AMM 23-80-01 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500022 20080325 00022 NM 2008 3 25 2008UALA00893 1 20080214 A 3242 429074 CONTROL UNIT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE BRAKE SYSTEM FAULTY A UALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 772UA 26930 ANTISKID EICAS MSG ON TAXI. SUSPECT BRAKE SYSTEM CONTROL UNIT. REPLACED BRAKE SYSTEM CONTROL UNIT AS PER MM 32 -42-01, PASSED MAT TEST. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500025 20080325 00025 CE 2008 3 25 DXTA20082902 1 20080227 A 2750 FLAP SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 950QS 7500050 FLAPS AND SLATS FAILED IN UP POSITION. COMPLIED WITH MECHANICAL AND ELECTRIC RIG CHECKS OF FLAPS. COMPLIED WITH TORQUE C HECK OF PDU, CHECKED GOOD. INSPECTED IB FLAP CABLES LT AND RT. NO DEFECTS FOUND. QUICK FROZE BOTH RESOLVERS, RAN FLAPS NO DEFECTS. APPLIED DRY ICE TO RESOLVER CONVERTERS DMC PDU OPERATED FLAPS. NO DEFECTS NOTED. WORK PERFORMED IAW MM CH AP 27-50-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032500085 20080325 00085 NM 2008 3 25 DXTA20082940 1 20080315 A 2400 CIRCUIT BREAKER GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE TRIPPED E DXTA A UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 GL 07 708QS 069 CLIMBING THROUGH FL 3111 I HEARD A CB POP, FOLLOWED BY NUMEROUS EICAS CAUTION AND WARNING MESSAGES. TROUBLESHOT SYSTEM, FOUND CB135P EMERGENCY BUSS BATTERY CB (60 AMP) TO BE DEFECTIVE. REPLACED CB135P AND PERFORMED GCU OPERATIONAL TEST AND DC LOAD SHEDDING OPERATIONAL TEST PER GAC G200 M.M. 24-30-00. OPS TESTED GOOD. 2 L 7 2 4F 4 F RT A53NM E35NE 2008032500087 20080325 00087 EA 2008 3 25 COMA0860174 1 20080311 A 2130 21197646 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A COMA L ABORTED APPROACH O OTHER AP APPROACH 1 SO 01 969CA 11791 7141 FLT 4993 - ON APPROACH INTO JFK A/C BECAME UPRESSURIZED AT 4,000 FT. A/C LANDED SAFELY. REMOVED AND REPLACED CABIN PRE SSURE SELECTOR PANEL. 2 L 7 2 4F RT A21EA 2008032500094 20080325 00094 CE 2008 3 25 DJFA2008025 1 20080310 A 5511 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 790TA RK252 DURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN C OMMUNIQUE' NR 70. MAINTENANCE REPLACED BOTH RIBS WITH NEW STYLE RIB ASSEMBLIES. 2 H 7 2 4F 4 F RT A16SW E25EA 2008032500101 20080325 00101 NE 2008 3 25 AC2A119194 1 20080314 A 6200 NAS195842D BOLT SKRSKY S76 S76A 8143006 NE MAIN ROTOR CORRODED E AC2A O OTHER O OTHER NR NOT REPORTED 1 SW 31 5447C 760180 NEW BOLTS HAVE A PIT IN THE SHANK OFF THE BOLT. 1 G 7 2 3U H1NE 2008032500118 20080325 00118 NM 2008 3 25 SWAA081473 1 20080318 A 2560 33500001 GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 7 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008032500128 20080325 00128 NM 2008 3 25 SWAA081478 1 20080318 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008032500137 20080325 00137 NM 2008 3 25 SWAA081487 1 20080318 A 5330 6545800 BEAR STRAP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032500138 20080325 00138 NM 2008 3 25 SWAA081485 1 20080318 A 5330 6545800 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032500139 20080325 00139 NM 2008 3 25 SWAA081486 1 20080318 A 5330 6545800 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032500145 20080325 00145 NM 2008 3 25 SWAA081490 1 20080318 A 5315 6545410 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CHORD CRACKED AT BS 667, LBL 24. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2008032500146 20080325 00146 NM 2008 3 25 SWAA081503 1 20080318 A 5310 6978062 DOOR FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032500147 20080325 00147 NM 2008 3 25 SWAA081502 1 20080318 A 5310 6516352 DOOR FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 2 DOOR STOP. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032500148 20080325 00148 CE 2008 3 25 DXTA20082923 1 20080308 A 3240 BRAKE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG CONTAMINATED E DXTA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 679QS 5605279 UPON SHUTDOWN , SUFFICENT SMOKE FROM RT MAIN GEAR. SMOKE PERSISTED FOR 15 MIN. REMOVED RT MAIN WHEEL AND INSP WHEEL AND BRAKE ASSY FOUND EXCESSIVE GREASE ON INSIDE OF WHEEL, CLEANED GREASE AND FOUND SMALL SUPERFICIAL BURN MARKS. REINSTALLE D RT MAIN WHEEL IAW MM 32-41-02. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500149 20080325 00149 NM 2008 3 25 SWAA081495 1 20080318 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 907, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008032500158 20080325 00158 NM 2008 3 25 SWAA081509 1 20080318 A 5311 6545875 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE STUB FRAME CORRODED AT BS 312, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032500164 20080325 00164 NM 2008 3 25 SWAA081515 1 20080318 A 3350 8200048901 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 763SW 27877 DURING SCHEDULED 8Y CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. R7R LENS PER MM. 2 L 7 2 4F RT A16WE 2008032500166 20080325 00166 NM 2008 3 25 SWAA081512 1 20080318 A 5312 148A2280 BULKHEAD BOEING 737 7377H4 1384404 NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 786SW 29811 DURING SCHEDULED CV CHECK, FOUND AFT PRESSURE BULKHEAD OIL CANNED AT BS 1016, STR 3L TO STR 4L. REPAIRED BULKHEAD PER S WA EA. 2 L 7 2 4F RT A16WE 2008032500167 20080325 00167 NM 2008 3 25 SWAA081513 1 20080318 A 5312 148A2280 BULKHEAD BOEING 737 7377H4 1384404 NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 786SW 29811 DURING SCHEDULED CV CHECK, FOUND AFT PRESSURE BULKHEAD OIL CANNED AT BS 1016, STR 2R TO STR 3R. REPAIRED BULKHEAD PER S WA EA. 2 L 7 2 4F RT A16WE 2008032500168 20080325 00168 SO 2008 3 25 FDKA200803109 1 20080314 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6145 MCO-HSV (1353 PHX LCL), ROW 12 EMERGENCY LIGHT INOP. MX RESECURED CONNECTORS. 2 L 7 2 4T RT T00011AT 2008032500169 20080325 00169 SO 2008 3 25 SIMA200708404 1 20080228 A 2422 PC2511237 STATIC INVERTER EMB 135 EMB135KL 3260302 SO FAILED A SIMA O OTHER B P SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION CR CRUISE 1 SW 21 855AE 145747 ON FLIGHT 3833 CREW REPORTED IN FLIGHT THAT THE PFD1-2, FMS ONE, TCAS, GPWS, AND TRANSPONDER FAILED. CREW REPORTED DETEC TED SMOKE. AIRCRAFT REMOVED FROM SERVICE. C/A- REMOVED AND REPLACED STATIC INVERTER IAW EMB AMM 24-20-01. AIRCRAFT RETU RNED TO SERVICE 2 L 7 2 4F RT T00011AT 2008032500173 20080325 00173 SO 2008 3 25 FDKA200803111 1 20080311 A 2612 3601135470 FIRE LOOP EMB 145 EMB145LR 3260212 SO APU FAILED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 831MJ 12083 145273 FDM 6121 PWM-JFK (1303 PHX LCL), APU FIRE DET FAIL MSG ON EICAS. MX REMOVED AND REPLACED APU FIRE DETECTION LOOP. 2 L 7 2 4T RT T00011AT 2008032500176 20080325 00176 SO 2008 3 25 FDKA200803114 1 20080317 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 FDM 6085 MCO (0822 PHX LCL), THE12A OVERHEAD EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED EMERGENCY LIGHT. 2 L 7 2 4T RT T00011AT 2008032500178 20080325 00178 EU 2008 3 25 YENA2008025 1 20080319 A 2121 EVT3454HC FAN AIRBUS 320 A320232 3930326 EU E&E BAY SEIZED A YENA A UNSCHED LANDING E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 552JB 22256 22256 1861 FLT 501, EWR-FLL, DIVERTED TO JAX, AT CRUISE PILOTS/FLT ATTENDANTS NOTICED A VIBRATION FOLLOWED BY ELECTRICAL FUMES MAIN LY IN THE COCKPIT & FORWARD CABIN. STARTED SMOKE/FUME REMOVAL CHECKLIST, SHUT OFF COMMERCIAL/LIVE TVS BLOWER/EXTRACT OV ERRIDE ALSO HAD A EXTRACT FAULT ECAM. ONCE QRC COMPLETE & AT 10,000 FUMES BECAME LESS INTENSE LANDING SAFELY IN JAX. R EMOVED AND REPLACED AVIONICS EXTRACT FAN (18HQ) IAW AMM 21-26-51, OPS CHECK NORMAL, A/C OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2008032500181 20080325 00181 EA 2008 3 25 VNAA0803006 1 20080311 A 2913 6619005 PUMP CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE NR 1 ENGINE LEAKING A VNAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 05 705PS 8272 10144 CREW REPORTED A NR 1 HYDRAULIC LOW PRESSURE MESSAGE ON CLIMBOUT. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCID ENT. MAINTENANCE INSPECTED AND FOUND THE NR 1 ENGINE DRIVEN PUMP LEAKING FROM THE CASE. MAINTENANCE REMOVED AND REPLAC ED THE NR 1 ENGINE DRIVEN PUMP (EDP) IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERV ICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008032500184 20080325 00184 EA 2008 3 25 VNAA0803009 1 20080316 A 5244 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE COMM SERVICE OPEN A VNAA A UNSCHED LANDING O OTHER TO TAKEOFF 1 GL 05 207PS 7873 CREW REPORTED A NOISE COMING FROM THE NOSE AREA ON TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE COMMUNICATION SERVICE DOOR OPEN. MAINTENANCE SECURED THE DOOR CLOSED AND FOUND NO DEFECTS OR DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008032500185 20080325 00185 2008 3 25 DXTA20082928 4 20080310 A 2210 7022090901 YAW DAMPER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 958QS 7500158 UPPER YAW DAMPENER CHANNEL (A) FAILED. REMOVED CHANNEL A YSAC DUE TO INTERNAL FAILURE. INSTALLED REPAIRED YSAC IAW CE75 0 M/M CH 27-24-01, OPS CHECKED GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032500186 20080325 00186 CE 2008 3 25 DXTA20082929 1 20080310 A 3233 99125373 ACTUATOR CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE LT MLG FALSE INDICATION E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 595QS 703 5605712 DURING DESCENT, WE NOTICED THE LT MAIN DOWN AND LOCK GREEN ANNUNC ON, WITH NO OTHER ABNORMAL INDICATIONS. T/S TO BAD AC TUATOR. REPLACED L/H MAIN LANDING GEAR ACTUATOR IAW 560XL MM CH 32-30-04. ADJUSTED CAMBER IAW 560XL MM CH 32-10-00. O P'S & LK CK GOOD 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500187 20080325 00187 CE 2008 3 25 DXTA20082930 1 20080311 A 3243 MASTER CYLINDER CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LT MLG FAILED E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 604QS 5605204 DURING TAXI, NO BRAKE FUNCTION UNTIL MAXIMUM PRESSURE IS APPLIED AND THEN LT BRAKE LOCKS. REPLACED CAPTAINS LEFT BRAKE MASTER CYL WITH NEW UNIT AND BLEED SYSTEM IAW MMCH 32-42-02, NO LEAKS, OPS CHECK GOOD. TAXIED AIRCRAFT MADE SEVERAL LEFT AND RIGHT TURNS. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500189 20080325 00189 CE 2008 3 25 DXTA20082932 1 20080312 A 2913 PUMP CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE HYD SYSTEM INOPERATIVE E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 679QS 120 5605279 WHILE TAXING, ANTI SKID INOP LIGHT CAME ON , FOLLOWED BY LOW BRAKE PRESS LIGHT AND SUBSEQUENT LOSS OF NORMAL BRAKING. R EPLACED POWER BRAKE HYDRAULIC PUMP WITH NEW CUSTOMER SUPPLIED. REPLACED ANTI-SKID RELAY WITH NEW P/N: MS2416602, REMOVED RELAY P/N: MS2416602. BLED ANTISKID BRAKE SYSTEM AND SERVICED BRAKE SYSTEM TO FULL. BRAKES OPS CHECK AND LEAK CHECK GOO D. ALL WORK IAW MM 32-42-00, 32-44-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500190 20080325 00190 CE 2008 3 25 DXTA20082933 1 20080312 A 3234 049801001 CONTROL HANDLE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG INOPERATIVE E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 671QS 1551 5605071 DURING GEAR RETRACTION RED UNLOCK LIGHT STAYED ILLUMINATED. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE IAW MM 32- 30-01 ALSO REMOVED AND REPLACED LANDING GEAR PCB IAW MM 24-51-02. C/W LANDING GEAR FUNCTIONAL CHECKS IAW MM 32-01-00. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500191 20080325 00191 2008 3 25 UPS08851863 4 20080313 A 2565 SLIDE DOUG DC8 DC873F 302199F WP COCKPIT LOW PRESSURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 CREW ESCAPE SLIDE SHOWS LOW PRESSURE. DEFERRED CREW EMERGENCY ESCAPE SLIDE PER MEL 52-7-4. PLACARD INSTALLED. R&R EME RGENCY EVAC SLIDE PER MM 25-60-01-2. THIS CLEARS M371295 PLACARD REMOVED. 2 L 7 4 4F RT 4A25 2008032500192 20080325 00192 EU 2008 3 25 F3LA200800095 1 20080305 A 5321 D5361087600000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE L0WER SURFACE OF FLOOR PANEL 221FF. MAINTENANCE RE MOVED AND REPLACED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-12-12-000-001. FOLLOWING COMPLETION OF THE INSTALLATION OF THE NEW FLOOR PANEL, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032500198 20080325 00198 NM 2008 3 25 2008UALA01390 1 20080312 A 5220 SHAFT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY EXIT OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 531UA 25042 THE 4L EMERGENCY POWER ACTUATOR CABLE FAILS TRAVEL CHECK. FOUND SPLINE SHAFT AND LOWER HINGE LINK WERE CLOCKED WRONG. CLOCKED ASSY WITH NEW PARTS AND PASTED CABLE TRAVEL CHECK. ALL OPS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500200 20080325 00200 NM 2008 3 25 2008UALA01037 1 20080226 A 2421 757183F GENERATOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LEFT FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 786UA 26938 LEFT BUG HAS TRIPPED DELTA PRESSURE INDICATOR SWITCH. SUSPECT BLOCKED FILTER. REPLACED BACKUP GENERATOR IN ACCORDANCE WITH AMM. OPS & LEAK CHECK OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500201 20080325 00201 NM 2008 3 25 2008UALA01191 1 20080303 A 5420 STRUCTURE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 NR 2 PYLON RIGHT SIDE IS CHAFED IN 5 SPOTS AT NAC 195. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA, FABRICATED & I NSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032500211 20080325 00211 NM 2008 3 25 2008UALA01447 1 20080315 A 5320 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 808UA 804 BEAM 165 FRD HAS 1 CLIP NUT HOLE WITH CORROSION. CORROSION REMOVED WITH LIGHT BURNISHING. 2 L 7 2 4F 4 F RT A28NM E40NE 2008022700265 20080227 00265 NM 2008 2 27 UIEA200800041 1 20080212 A 5420 321U2731102 BRACE BOEING 747 7472D7B 1384803 NM ZONE 400 WORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 NR 1 DIAGONAL BRACE FORWARD PORTION LOWER SURFACE PRIMER DISCOLORED. REPLACED DIAGONAL BRACE PER MM 54-10-03. 2 L 7 4 4F RT A20WE 2008022700266 20080227 00266 NM 2008 2 27 UIEA200800042 1 20080213 A 5350 RADOME BOEING 747 7472D7B 1384803 NM ZONE 400 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 AIRCRAFT WAS HIT BY LIGHTNING STRIKE. ENTRANCE AT THE RADOME. NO COMMUNICATIONS OR NAV FAILURES REPORTED BY CREW. FOU ND RADOME DAMAGED BY LIGHTNING STRIKE. FOUND RIGHT HF ANTENNA DAMAGED BY LIGHTNING STRIKE. LIGHTNING STRIKE INSPECTION ACCOMPLISHED PER 5-51-13 FOUND SATISFACTORY. DUE TO NO AVAILABLE RADOME AT THE STATION EO 4753B117 ISSUED. PERFORM PA RT 1 TIME LIMITED REPAIR. PART 2 VISUAL INSPECTIONS BEFORE EACH FLIGHT. PART 3 IS TO PERFORM REPAIR WITHIN 15 FLIGHT C YCLES. PARTS 1 AND 2 ACCOMPLISHED. REWORKED HF ANT PER 23-11-02 FOUND DAMAGE WITHIN LIMITS. 2 L 7 4 4F RT A20WE 2008022700277 20080227 00277 EU 2008 2 27 08FDEA00545 1 20080130 A 5311 R53610898001 FAILSAFE AIRBUS 310 A310222 3930315 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 447FE 251 FUSELAGE, CORROSION FOUND ON TOP SURFACE OF RT FWD PAX DOOR FAIL/SAFE RING, BETWEEN FR 14 AND 14B. FAIL/SAFE RING REPAI RED IN ACCORDANCE WITH FEDEX EA 6-5310-117229 AND RAS/AS/023/2008 ISSUE A. 2 L 7 2 4F RT A35EU 2008022700278 20080227 00278 NM 2008 2 27 CALA0800154 1 20080215 A 5311 143A1114 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16709 28779 FRAME CRACKED AT STA 480 BETWEEN STRINGER 8 & 9R. REPAIRED PER ECRA 5310-04717. 2 L 7 2 4F RT A16WE 2008022700280 20080227 00280 NM 2008 2 27 CALA0800155 1 20080215 A 5311 143A1113 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16709 28779 FRAME CRACKED AT STA 440 BETWEEN 8 & 9R. REPAIRED PER SRM 5210-04717. 2 L 7 2 4F RT A16WE 2008022700281 20080227 00281 2008 2 27 SWIA200819228 2 20080210 A 7261 COVER CNDAIR CL600 CL6002B19 1900309 EA ENGINE LEAKING A SWIA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 NM 07 920SW 7660 RECEIVED A RIGHT ENGINE OIL PRESS WARNING MESSAGE ON DESCENT. PERFORMED PRECAUTIONARY SHUT DOWN, FLIGHT NR 5873. SECUR ED CRANK PAD COVER AND VERIFIED INSTALLATION IAW CRJ 200 AMM 72-00-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008032700006 20080327 00006 NM 2008 3 27 DHL2008765027 1 20080111 A 5755 SKIN BOEING 727 727264 138408M NM NR 3 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, NR 3 SPOILER NR 3 HINGE CUT OUT ON LT WING TRAILING EDGE IS CRACKED. STOP DRILLED CRACK 0.250 IAW SRM 5 1-10-1. FABRICATED DOUBLER REPAIR IAW SRM 51-20-1, 51-30-5 AND 57-30-4 FIG 10. ALODINED AND PRIMED DOUBLER AND AREA IA W SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW SRM 57-30-4 FIG 10 AT NR 3 SPOILER NR 3 HINGE CUT OUT. 2 L 7 3 4F A3WE 2008032700010 20080327 00010 NM 2008 3 27 DHL2008765007 1 20080115 A 5754 SKIN BOEING 727 727264 138408M NM NR 8 SLAT DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, RT WING WS 760 NR 8 SLAT UPPER SURFACE HAS A DENT AROUND FASTENER. EVALUATED AND FOUND DENT OUT OF LIMI TS IAW SRM 57-50-1 FIG 2 DUE TO DENT BEING ON FASTENER. CUT OUT DAMAGED AREA DIMENSION 1.75" BY 1.125" IAW SRM 57-50-3 FIG 1. FABRICATED DOUBLER REPAIR AND FILLER, IAW SRM 57-50-3 FIG 1. LOCATED AND DRILLED HOLES IAW SRM 51-30-5. TREAT ED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED DOUBLER REPAIR AT NR 8 SLAT WS 760 IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032700011 20080327 00011 NM 2008 3 27 DHL2008749018 1 20080115 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 919 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 DURING C CHECK, EXFOLIATION AT FASTENER ON "L" ANGLE ON UPPER SURFACE OF LONGITUDINAL FRAME, BS 919 RWBL 70.5. FABRICAT ED NEW "L" ANGLE IAW SRM 51-30-5, 51-10-3 AND 53-10-2 FIG 4. INSTALLED IAW SRM 51-30-2. NR 033718 2 L 7 3 4F A3WE 2008032700012 20080327 00012 NM 2008 3 27 DHL2008765017 1 20080116 A 5754 SKIN BOEING 727 727264 138408M NM NR 4 LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, RT WING NR 4 LEADING EDGE FLAP INNER SKIN CRACKED 3 PLACES AROUND RIVETS AT INBOARD IND WS 150. STOP DR ILLED 3 EACH CRACKED PLACES AROUND RIVETS AT INBOARD END WS 150 (DIAMETER 0.190") IAW SRM 51-10-1 AND 57-50-3 FIGURE 12. HFEC C/W AROUND STOP DRILL HOLES, NO CRACKS NOTED PER NDT PART 6 51-00-00 FIG 23. FABRICATED REPAIR DOUBLER IAW SRM 5 7-50-3 FIGURE 12. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR DOUBLERS IAW SRM 51-30-2 AND 57-50-3 FIGU RE 12. 2 L 7 3 4F A3WE 2008032700017 20080327 00017 NM 2008 3 27 NOCA01708 1 20080309 A 2610 033638 BLOWER BOEING 757 75728A 1384976 NM SMOKE DETECTOR MALFUNCTIONED A NOCA K NONE N FALSE WARNING UK UNKNOWN 1 EA 15 755NA 30043 EICAS MESSAGE AFT DET FAN. T/S PER FIM 26-16-00 AND FOUND NR 3 BLOWER AT FAULT. REMOVED AND REPLACED NR 3 BLOWER PER A MM 26-16-02, OPS CHECKS OK. 2 L 7 2 4F RT A2NM 2008032700023 20080327 00023 NM 2008 3 27 DHL2008765025 1 20080119 A 5754 SKIN BOEING 727 727264 138408M NM NR 3 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, CRACKED ON NR 3 SLAT UPPER SURFACE AT INBOARD SLAT HOOK MOUNT SCREW WS 520. REMOVED HOOK FROM AREA IAW SRM 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 57-50-3 FIG 10. TREATED AND PRIMED PART IAW SRM 51-10-2. INSTALLED DOU BLER REPAIR AT NR 3 SLAT UPPER SURFACE WS 520 IAW SRM 51-30-2. REINSTALLED HOOK (SLAT HOOK IAW SRM 51-30-2). 2 L 7 3 4F A3WE 2008032700024 20080327 00024 SO 2008 3 27 RAIA00803007 1 20080310 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 818HK 145059 PRE FLT 5488 - STL - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RE-SECURED THE WIRING TO THE AFFECTED LIGHT ASSEMBLY. 2 L 7 2 4T RT T00011AT 2008032700025 20080327 00025 NM 2008 3 27 DHL2008765005 1 20080119 A 5310 TORQUE BOX BOEING 727 727264 138408M NM BS 1240 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, AFT STAIRWELL LIGHTENING HOLE CRACKED 6 O'CLOCK POSITION RIGHT SIDE BS 1240 (TORQUE BOX). CUT OUT DAMAG ED AREA AT AFT STAIRWELL LIGHTENING HOLES 6 O'CLOCK POSITION BS 1240 RT IAW SRM 51-40-2 FIG 1, DIMENSION 1.25" BY .5". FABRICATED DOUBLER REPAIR AT AFT STAIRWELL LIGHTENING HOLE 6 O'CLOCK POSITION BS 1240 IAW SRM 53-10-2 FIG 6 AND 51-40-1 FIG 1. TREATED AND PRIMED PART AND AREA IAW SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032700034 20080327 00034 2008 3 27 2008UALA01421 4 20080313 A 2350 MICROPHONE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE O2 MASK SHORTED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 803UA 748 CREW REPORT: F/O O2 MASK IS INTERMITTENT. NO SOUND THROUGH SPEAKER. INTERMITTENT SHORT IN MIC. REPLACED MASK ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032700039 20080327 00039 NM 2008 3 27 2008UALA01430 1 20080313 A 3350 767 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 597UA 28750 NR 2 LEFT MAIN ENTRY DOOR OUTSIDE EMERGENCY LIGHT IS INOPERATIVE. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032700040 20080327 00040 NM 2008 3 27 2008UALA01431 1 20080313 A 3350 387 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 597UA 28750 AFT RIGHT HAND OVERWING EMERGENCY EXIT INSIDE AFT EMERGENCY LIGHT IS INOPERATIVE. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032700045 20080327 00045 NM 2008 3 27 DHL2008749021 1 20080121 A 5313 STRINGER BOEING 727 7272J0 138407E NM BS 560-573 S27R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 DURING C CHECK, CORROSION NOTED ON STRINGER 27R REPAIR CHANNEL, BS 560 TO BS 573. REMOVED FASTENERS IAW SRM 51-30-2. R EMOVED CHANNEL IAW SRM 51-30-2. FABRICATED NEW REPAIR IAW SRM 51-20-1, 51-20-2, 51-30-2, 53-10-2 FIG 9 AND 53-10-3 FIG 1. CLEANED STRINGER AREA IAW MM 12-40-00, NO CORROSION NOTED IAW SRM 51-10-6. ALODINE AND PRIMED REPAIR IAW SRM 51-10- 2. INSTALLED CHANNEL IAW SRM 53-10-3 FIG 2. 2 L 7 3 4F RT A3WE 2008032700048 20080327 00048 NM 2008 3 27 DHL2008765011 1 20080121 A 5320 SUPPORT BOEING 727 727264 138408M NM BS 880 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, RIGHT WHEEL WELL SUPPORT STRUCTURE HAS CRACK AT BS 880 RBL 26. REMOVED SUPPORT STRUCTURE AT RIGHT WHEEL WELL BS 880 RBL 26 IAW SRM 51-30-2. FABRICATED NEW SUPPORT STRUCTURE AT RIGHT WHEEL WELL BS 880 RBL 26 IAW SRM 53-10-2 FIG 4 AND 51-10-3. DRILLED HOLES ON NEW SUPPORT STRUCTURE IAW SRM 51-305. TREATED AND PRIMED PART AND AREA IAW SRM 51 -10-2. INSTALLED NEW SUPPORT STRUCTURE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032700060 20080327 00060 NM 2008 3 27 DHL2008765010 1 20080129 A 5311 FRAME BOEING 727 727264 138408M NM BS 480 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, FUSELAGE FRAME GOUGED AT BS 480 BELOW STRINGER 17L. BLENDED AREA AT BS 480 BELOW STRINGER 17L, ORIGINAL MATERIAL 0.150", MATERIAL REMAINING WAS APPROXIMATE 40% OF THICKNESS LEAVING 60% FOUND TO BE WITHIN LIMITS IAW EO NR OE -N765AT-1-25-08. TREATED AND PRIMED AREA IAW SRM 51-10-2 AND EVA B253-00043. 2 L 7 3 4F A3WE 2008032700061 20080327 00061 2008 3 27 MASA200800230 3 20080314 A 6197 CONNECTOR DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE LOOSE A MASA O OTHER O OTHER CR CRUISE 1 SW 07 446YV 446 ASH FLT 7177 RAP-DEN, NR 2 ENGINE UNSCHEDULED AUTO FEATHER CONDITION IN FLIGHT AT AROUND 1000 FT. CREW DECLARED AN EMER GENCY AND RTF. RE-SECURED CONNECTOR ON TORQUE SENSOR, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2008032700063 20080327 00063 EA 2008 3 27 MASA200800232 1 20080316 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002D24 1390016 EA FWD LAVATORY FALSE ACTIVATION A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 909FJ 15009 ASH FLT 2685 CLT-SRQ, FWD LAV SMOKE DETECTOR GOING OFF. MX RESET SYSTEM, NO FAULTS NOTED AND NO SMOKE NOTED. 2 L 7 2 4F RT A21EA 2008032700065 20080327 00065 EA 2008 3 27 MASA200800233 1 20080316 A 5220 SEAL CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY ESCAPE DIRTY A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 909FJ 15009 ASH 2664 SRQ-CLT, FLIGHT DECK EMERGENCY ESCAPE HATCH LEAKING WATER. MX INSPECTED, CLEANED & LUBED SEAL, OPS GOOD. 2 L 7 2 4F RT A21EA 2008032700067 20080327 00067 EA 2008 3 27 MASA200800235 1 20080315 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 591ML 7388 PERMANENT REPAIR TO FUSELAGE SKIN FS 349.00 TO 364.00 STR 13 TO 15 RIGHT HAND SIDE. 2 L 7 2 4F RT A21EA 2008032700069 20080327 00069 SO 2008 3 27 C2XA08IA080 1 20080311 A 3350 110049 POWER SUPPLY EMB 145 EMB145XR 3260214 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11107 145654 EWR, DURING POST FLIGHT INSPECTION THE LEFT HAND AND RIGHT HAND EXTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008032700072 20080327 00072 SO 2008 3 27 C2XA08ON105 1 20080317 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO LAVATORY INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 14174 9471 9471 14500876 FLT 0001 - AUS - FLIGHT CREW REPORTED LAV SMOKE DETECTION NO TEST. MX PERSONNEL REMOVED AND REPLACED LAV SMOKE DETECTOR . OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008032700073 20080327 00073 NM 2008 3 27 NOCA01908 1 20080315 A 5320 143N536677 PANEL BOEING 757 75728A 1384976 NM FUSELAGE CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 756NA 32448 RIGHT HAND TRANSITION PANEL HAS CORROSION ALONG TAPE LINE FROM STA 800-850. REMOVED AND REPLACED TRANSITION PANEL AS PE R SRM 51-10-02. 2 L 7 2 4F RT A2NM 2008032700074 20080327 00074 SO 2008 3 27 RAIA0803014 1 20080317 A 3610 BLEED AIR SYS EMB 145 EMB145LR 3260212 SO NR 1 & NR 2 MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 844HK 14500838 FLT 7910 - CVG - BLEED NR 1 AND NR 2 OVERTEMP MESSAGE ON THE EICAS. MAINTENANCE PERFORMED A BLEED SYSTEM OPERATIONAL CH ECK OF BOTH THE BLEED SYSTEM AND THE ANTI-ICING SYSTEM WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008032700075 20080327 00075 NM 2008 3 27 DHL2008763519 1 20080301 A 5311 FRAME BOEING 727 727264 138408M NM BS 580 S16-17R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 FRAME DENTED IN CARGO COMPT AT BS 580, ABOVE STR 17R. CUT OUT DAMAGE, FABRICATED FRAME REPAIR, AND INSTALLED PER B727 S RM 51-40-3 FIG 1, 53-10-2 FIG 3, AND 51-30-2. 2 L 7 3 4F A3WE 2008032500267 20080325 00267 NM 2008 3 25 2008UALA01616 1 20080321 A 5210 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE R4 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 778UA 26940 DOOR 4R HAS A DENT 12 INCHES UP FROM LOWER PORTION OF DOOR IN BETWEEN PAINT COLORS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500294 20080325 00294 NM 2008 3 25 2008UALA01464 1 20080315 A 5210 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR DISLODGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 588UA 26717 F/A'S UNABLE TO ARM DOOR 1R. UPPER AFT SECTION OF DOOR SEAL WAS DISLODGED FROM RETAINER. RE-INSTALLED RETAINER, DOOR O PS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032600004 20080326 00004 NM 2008 3 26 QXEA200800286 1 20080313 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM NR 5 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - C4- LEFT INBOARD SEAT TRACK NR 5 HAS CORROSION AT STA X-19, X-7, X1, X10, 26,(X32 TO X60) (OUTBOARD FLANGE X75 TO X99). REMOVED NR 5 SEAT TRACK AND INSTALLED NEW SEAT TRACK REF DASH 8 Q400 SRM 51-42-05, 51-40-15. 2 H 7 2 4T RT A13NM 2008032600006 20080326 00006 NM 2008 3 26 HALA0800404 1 20080313 A 5410 FAIRING BOEING 767 767332 1382001 NM RT ENGINE DELAMINATED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 RT ENGINE FAIRING 411AT DELAMINATION AT PREVIOUS REPAIR LOCATION. INJECTED EC9394 INTO AREA TO STABILIZE CORE, 4 CYCLE LIMIT, START AT 30164. 2 L 7 2 4F RT A1NM 2008032600016 20080326 00016 SO 2008 3 26 LR7A08044 1 20080227 A 2140 3710141 DUCT LKHEED 382 382G 526414U SO CARGO BAY CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2299 5025 DURING SCHEDULED C-7 CHECK, PER JOB CARD HC5314, FOUND CARGO FLOOR HEATING DUCT ASSY P/N 371014-1 CRACKED AT FS 537-577. REPAIR ACCOMPLISHED IAW LAC MEA 382-21-08-009. 2 H 7 4 4T A1SO 2008032600025 20080326 00025 NM 2008 3 26 F3LA200800127 1 20080314 A 5210 D5211200300000 SKIN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE L1 DOOR DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 13563 611 2258 FOLLOWING CONTACT OF THE JET BRIDGE WITH THE L-1 DOOR, INSPECTION, DURING THE DAILY CHECK, REPORTED DAMAGE WAS FOUND TO THE LOWER, FORWARD CORNER OF THE DOOR SKIN. MAINTENANCE REPAIRED THE FORWARD LOWER CORNER OF THE L-1 DOOR IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-52R-30107 AND SRM 51-42-11. FOLLOWING COMPLETION OF THE REPAIR, THE DOOR WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032600033 20080326 00033 EA 2008 3 26 REXA200800005 1 20080317 A 3310 LIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT SHORTED A REXA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 25 8918B 7918 CAPTAIN SIDE FLOOD LIGHT RHEOSTAT SMOKED WHEN ADJUSTED. REPLACED SHORTED LIGHT ASSEMBLY. OPERATION NORMAL IAW AIRCRAFT MAINTENANCE MANUAL 33-11-00. 2 L 7 2 4F RT A21EA 2008032600045 20080326 00045 EU 2008 3 26 08FDEA01005 1 20080317 A 7830 0748291894516035 ACOUSTIC PANEL AIRBUS 310 A310203 3930313 EU THRUST REVERSER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 DELAMINATION ON THE NR 2 ENGINE LEFT LOWER ACOUSTIC PANEL. REMOVED DAMAGE, APPLIED & CURED REPAIR. RESTORED FINISH IA W ENGINE MANUAL 78-32-02. 2 L 7 2 4F RT A35EU 2008032600067 20080326 00067 WP 2008 3 26 08FDEA01020 1 20080318 A 5753 ARC0566502 PANEL DOUG MD10 MD1010F 3022112 WP T/E FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RT WING OUTBD FLAP; INBD PANEL NR 636 BR IS DENTED IN SEVERAL PLACES. REPAIRED RT WING OUTBD FLAP INBD PANEL 636 BR BY C HECKING LIMITS ON THE DENTS IAW SRM 51-80-01 VOL II. REMOVED DAMAGED AREAS FOUND TO BE OUT OF LIMITS. PERFORMED DOUBLE R REPAIR AT THE OUTER SKIN BY METAL BONDING IAW SRM 51-71-00 VOL II. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. SEALE D IAW SRM 51-41-01 VOL II & RESTORED FINISH IAW SRM 51-21-02 VOL II. 2 L 7 3 4F RT A22WE 2008032600073 20080326 00073 NM 2008 3 26 HA0800413 1 20080314 A 5512 184T10062 PANEL BOEING 767 767332 1382001 NM HORIZ STAB DENTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 DENT ON RT HORIZONTAL STABILIZER LE PANEL 342BR. PERMANENT SRM REPAIR CARRIED OUT PER SRM 51-70-10, REF ANZ T1 19011361 5-0001 AND HAL FILE NR 594051. 2 L 7 2 4F RT A1NM 2008032600093 20080326 00093 EU 2008 3 26 2008UALA01541 1 20080318 A 3350 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 492UA 1755 THREE SVC EMERGENCY LIGHT TEST FAULTED EPSU BATTERY AFT LEFT. PERFORM RESET OF EPSU (LEFT AFT BATTERY) AND SYSTEM NOW C HECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032600098 20080326 00098 NM 2008 3 26 2008UALA01544 1 20080318 A 5210 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU PAX DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FWD ENTRY DOOR, AFT SIDE INNER SKIN CRACKED AT MID STOP PIN LOCATION. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLE D SKIN DOUBLER REPAIR TO INNER DOOR SKIN. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032600100 20080326 00100 NM 2008 3 26 2008UALA01546 1 20080319 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT OVERWING INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 RIGHT OVERWING EMERGENCY LIGHT, SECOND AFT IS INOP. REPLACED LIGHT FIXTURE RIGHT OVERWING EXIT. OP CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032600101 20080326 00101 NM 2008 3 26 2008UALA01547 1 20080319 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT OVERWING INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 199UA 28717 RIGHT OVERWING EMERGENCY FWD LIGHT INOP. RELAMPED RIGHT OVERWING EMERGENCY FWD LIGHT. OPS CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032600104 20080326 00104 NM 2008 3 26 2008UALA01549 1 20080318 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 R4 DOOR HANDLE BOX CORRODED BEYOND LIMITS. REPLACED HANDLE BOX. REPLACED HANDLE BOX. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032600135 20080326 00135 SO 2008 3 26 SWIA200819348 1 20080115 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 250YV 120250 LEFT FORWARD CABIN SEAT TRACK ALONG WALL IS CORRODED, FOUND AT C-CHECK. REPLACED SEAT TRACK IAW MM 55-12-345-12. 2 L 7 2 4T RT A31SO 2008032600139 20080326 00139 EA 2008 3 26 SWIA200819350 1 20080313 A 3350 INVERTER CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 492SW 7168 FLT 3905 - RIGHT SIDE EXIT ROW EMERGENCY EXIT LIGHT IS INOP. REPLACED RIGHT EMERGENCY LIGHT SIDEWALL INVERTER. OPS CHE CK GOOD. 2 L 7 2 4F RT A21EA 2008032600151 20080326 00151 NM 2008 3 26 2008UALA01579 1 20080319 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 760 S28L/R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 FWD PIT FRAME AT STA 760 STR 28L TO STR 28R HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032600158 20080326 00158 NM 2008 3 26 2008UALA01580 1 20080319 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 780 S28L/R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 FWD PIT REPAIR ON FRAME STA 780 STR 28L AND STR 28R HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032600159 20080326 00159 NM 2008 3 26 2008UALA01581 1 20080319 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 800 S28L/R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 FWD PIT FRAME REPAIR AT STA 800, STR 28L TO STR 28R HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032600161 20080326 00161 NM 2008 3 26 2008UALA01582 1 20080319 A 3350 767 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 575UA 26689 EXTERIOR EMERGENCY LIGHTS INOP AT DOOR 4L AND 4R. FOUND LAMP INOPERATIVE. REPLACED LAMP, CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032600197 20080326 00197 EU 2008 3 26 F3LA200800124 1 20080227 A 5270 2LA00546900 PROXIMITY SWITCH AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE R1 DOOR INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 608 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED THE R-1 DOOR SLIDE ARM LIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE R-1 DOOR PROXIMITY SWITCH (13WV2) IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 52-71-11-020-051, AMM 25-23-400-001 A ND AMM 52-71-00-710-505. UPON COMPLETION OF THE INSTALLATION, THE NEW SWITCH WAS TESTED, INSPECTED AND FOUND ACCEPTABLE . 2 L 7 2 4F 4 F RT A28NM 2008032600216 20080326 00216 EU 2008 3 26 08FDEA01038 1 20080318 A 5320 A53981113200201 SHEAR PLATE AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 MAIN CABIN INTERCOSTAL WEB IS CRACKED AT FRAME 79 AND STRINGER 26R. REMOVED FLOOR PANEL 262 AH IAW SRM 51-40-21 PARA 5. REMOVED SHEAR PLATE IAW SRM 51-40-21 PARA 7. LOCATED & DRILL NEW SHEAR PLATE IAW SRM 51-40-40. INSTALLED SHEAR PLAT E REF SRM 51-40-21 PARA 7. INSTALLED FLOOR PANEL 262 AH REF SRM 51-40-21 PARA 5. RESTORED CIC TO NEW SHEAR PLATE REF AM M 51-22-00-0. 2 L 7 2 4F RT A35EU 2008032600233 20080326 00233 CE 2008 3 26 DXTA20082926 1 20080309 A 2120 UNKNOWN CESSNA 500 560CESSNA 2076750 CE CABIN SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 373QS 5600373 AFTER TAKE OFF SMOKE SMELL - (NO SIGN OF VISUAL SMOKE) APPEARED. 2 L 7 2 4F RT A22CE 2008032600244 20080326 00244 CE 2008 3 26 DXTA20082962 1 20080324 A 7603 THROTTLE CABLE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT FROZEN E DXTA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 322QS 5600421 LT (NR1) THROTTLE CABLE FROZE IN POSITION AT FL400 AT -40 DEG C RAM. REPLACED THE LT AFT THROTTLE CABLE. CONDUCTED ENG INE RUN AND VERIFIED PROPER RIGGING IAW MM CH 76-11-02. 2 L 7 2 4F 4 F RT A22CE E25EA 2008032600246 20080326 00246 CE 2008 3 26 DXTA20082963 1 20080324 A 4920 APU CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 923QS 7500023 STRONG ODOR COMING FROM AIR CONDITION AND IN CABIN OF AIRCRAFT. REMOVED DEFECTIVE APU AND INSTALLED A REPAIRED APU. PE RFORMED AN OPERATIONAL AND LEAK CHECK. ALL CHECKS PASSED. ALL WORK ACCOMPLISHED IAW MM CHAPTER 49-10-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032600249 20080326 00249 CE 2008 3 26 GUUA03080802 1 20080308 A 5260 CABLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE AIRSTAIR FAILED A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 47542 UE198 FLIGHT: 9302, PILOT REPORTED CABIN DOOR EXTREMELY HARD TO OPEN FROM OUTSIDE. REPOSITIONED AIRSTAIR DOOR FWD UPPER HANDR AIL CABLE. 2 L 7 2 4T 4 T RT A24CE E26NE 2008032600250 20080326 00250 CE 2008 3 26 GUUA03080803 1 20080308 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT MLG CRACKED A GUUA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 29 81556 21345 UE239 FLIGHT: 9258, PILOT REPORTED, FOUND LT MLG LEAKING HYD FLUID. REPLACED LT MLG ACTUATOR. 2 L 7 2 4T 4 T RT A24CE E26NE 2008032600252 20080326 00252 SO 2008 3 26 GUUA03220801 1 20080322 A 3397 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHTS INOPERATIVE A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 285AS 120265 FLIGHT: 5402, DURING PREFLIGHT, DISCOVERED EXTERNAL EMERGENCY LIGHTS INOPERATIVE. REPOSITIONED CONNECTORS ON LIGHT ASSE MBLY. 2 L 7 2 4T 4 T RT A31SO E20NE 2008032600254 20080326 00254 EA 2008 3 26 MALA080038 1 20080317 A 2120 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA COCKPIT ODOR A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 15 919XJ 15163 HOT PLASTIC SMELL NOTED IN FLIGHTDECK DURING DESCENT, LANDING ,TAXI IN DTW. ARRIVED AT A/C COULD NOT SMELL ANYTHING. R AN PACK'S FULL NOT COULD NOT SMELL ANYTHING JUST THE NEWNESS OF THE A/C COULD NOT DUPLICATE THE SMELL. INSPECTED THE VE NT'S COULD NOT SEE ANYTHING. 2 L 7 2 4F RT A21EA 2008032600256 20080326 00256 NM 2008 3 26 DHL2008752506 1 20080208 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 AFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4 INCH BY 1/2 INCH IAW B727SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR MATERIAL USED 7075-O .071 PO NR 9006377 DIMENSI ON 9" BY 4" IAW B727 SRM 51-40-3 FIG1 AND IAW B727SRM 53-10-2 FIG 5. HEAT TREAT PART 7075-O TO 7075T6 IAW B727 FLIGHTST AR AIRCRAFT SERVICES ENGINEERING REPORT NR 2-37153-801 REV A. TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. I NSTALLED REPAIR IAW B727SRM 51-30-2. 2 L 7 3 4F A3WE 2008032600257 20080326 00257 CE 2008 3 26 DXTA20082965 1 20080325 A 2731 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL PITCH FEEL MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 933QS 7500133 AFTER TAKEOFF, WHILE ACCELERATING THROUGH 240 KIAS AT5000 FT, PITCH FEEL FAIL CAS MESSAGE ILLUMINATED. REMOVED RT PITCH FEEL ACTUATOR AND REPLACED IAW MM 27-33-00. ALL OPS CHECKS IAW MM 27-30-00. ALL CHECKS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032600261 20080326 00261 EA 2008 3 26 SWIA200819372 1 20080317 A 2130 21197646 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 710BR 2239 2239 7852 AIRCRAFT WAS NOT PRESSURIZING ON CLIMB-OUT, FLIGHT NR 2914. REPLACED CABIN PRESSURE SELECTOR PANEL IAW AMM 21-31-10. O PS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008032600305 20080326 00305 NM 2008 3 26 QXEA200800297 1 20080315 A 4920 4503067A APU BOMBDR DHC8 DHC8402 1390042 NM APU BAY LEAKING A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 427QX 8612 2532 4156 YYJ - FLIGHT 7400 - AFTER LANDING, THE FLIGHT ATTENDANT NOTICED A RAW FUEL SMELL IN THE AIRCRAFT. DURING TAXI AND SHUTD OWN THE SMELL INCREASED. MAINTENANCE RAN BOTH ENGINES FOR 10 MINUTES WITH THE BLEEDS ON AND NOTICED NO FUEL SMELLS. NO TICED LARGE AIR LEAK AT APU JOINT. PLACED APU ON MEL 49-00-1. RETURNED TO SERVICE. REPLACED THE APU. OPERATIONAL CHE CKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008032700004 20080327 00004 NM 2008 3 27 DHL2008765019 1 20080109 A 5531 STRINGER BOEING 727 727264 138408M NM VERTICAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, VERTICAL STABILIZER NR 8 STRINGER CRACKED FIN STATION 133. REMOVED PREVIOUS REPAIR FROM AREA IAW SRM 51 -30-2. FABRICATED 2 EACH REPAIR ANGLES IAW SRM 55-30-5 FIGURE 1 AND 55-30-2 FIGURE 2. HFEC VERIFIED CRACK TERMINATES I N FASTENER HOLE IAW NDT PT 6 CH 51-00-00. TREATED AND PRIMED PARTS IAW SRM 51-10-2 AND INSTALLED REPAIR ANGLES (2 EACH) AT VERTICAL STABILIZER NR 8 STRINGER FIN STATION 133 IAW SRM 55-30-5 FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 2008032700019 20080327 00019 NM 2008 3 27 DHL2008765006 1 20080118 A 5751 COVER BOEING 727 727264 138408M NM RT AILERON GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, RT INBOARD AILERON UPPER INBOARD HINGE COVER HAS DEEP GOUGE. REMOVED COVER IAW SRM 51-30-2. FABRICATED NEW COVER IAW SRM 57-50-2 FIGURE 7 AND 51-20-1. TREATED AND PRIMED NEW COVER IAW SRM 51-10-2. INSTALLED NEW COVER AT RT WING INBOARD AILERON UPPER INBOARD IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032700021 20080327 00021 NM 2008 3 27 DHL2008765030 1 20080119 A 5754 RIB BOEING 727 727264 138408M NM NR 4 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, CRACK INDICATION ON NR 4 SLAT OUTBOARD ACTUATOR SUPPORT RIB. REMOVED ACCESS PANEL AT NR 4 SLAT IAW SRM 51-30-2. LOCATED AND DRILLED HOLES ON NEW RIB IAW SRM 51-30-5. INSTALLED NEW RIB AT NR 4 SLAT OUTBOARD ACTUATOR IAW SR M 51-30-2. INSTALLED ACCESS PANEL AT NR 4 SLAT IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008022700282 20080227 00282 NM 2008 2 27 CALA0800156 1 20080215 A 5311 143A1113 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16709 28779 FRAME CRACKED AT STA 440 BETWEEN STRINGER 8 AND 9L. REPAIRED PER ECRA 5310-04717. 2 L 7 2 4F RT A16WE 2008022700293 20080227 00293 CE 2008 2 27 191WA21408 1 20080214 A 2140 E10D40 HEATER BEECH 99 99 1154002 CE COCKPIT FAULTY E AXSA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 65 191WA 753 U136 FLIGHT 1043 (PWM-MHT) JUST AFTER DEPARTURE THE PILOT NOTED A BURNING SMELL AND SMOKE IN THE COCKPIT COMING FROM UNDER TH E INSTRUMENT PANEL FOLLOWED SHORTLY BY THE SOUND OF A POPPING CIRCUIT BREAKER. THE PILOT IDENTIFIED THE CIRCUIT BREAKER AS THE COMBUSTION HEATER CB AND ALMOST IMMEDIATELY THE SMOKE BEGAN TO CLEAR. THE FLIGHT CONTINUED TO THE DESTINATION W ITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL DETERMINED THE SMOKE WAS CAUSED BY A FAULTY COMBUSTION HEATER. THE HEAT ER WAS DEFERRED UNDER MEL 21-1 AND RETURNED TO SERVICE. 1 L 7 2 3T A14CE 2008022700299 20080227 00299 WP 2008 2 27 IXXA08SMN030S 1 20080122 A 5310 BEAM DOUG DC8 DC862F 3021972 WP BS 902 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO LOWER FLANGE BEAM CRACKED AND CORROSION AT STATION 902.000 LEFT BOTT OM LINE 51". REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AR EA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION AFTER INSPECTION. FABRICATED INTERNAL AND EXTERNAL DOUBLER. PER FORMED HEAT TREATMENT TO REPAIR PARTS AS NEEDED. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FAST ENERS AND REPAIR PARTS IAW FAA FORM FAA 8100-9 DATED 02-19-08, MESSAGE BOEING 1-766871200-5 DATED 02-19-08, MESSAGE BOEI NG NUMBER 1-752696686-5 DATED 01-30-08, ROD SKETCH 200801240024, SEMAN DRAWING ED-4692, DC8 SRM 51-1-8, PAGES 17-18, DC8 2 L 7 4 4F 4A25 2008022700301 20080227 00301 WP 2008 2 27 IXXA08SMN024S 1 20080119 A 5340 FITTING DOUG DC8 DC862F 3021972 WP BS 759 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 759.000 LEFT BOTTOM LINE 24" (CENTER WING AREA). REMOVED CRACK FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-0 AND SRM 51-3-1. 2 L 7 4 4F 4A25 2008022700310 20080227 00310 NM 2008 2 27 KCSA081087 1 20080219 A 5420 STIFFENER BOEING 747 747221F 1384868 NM NR 3 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 NR 3 PYLON RT UPPER STIFFENER CRACKED AT ATTACH ANGLE OF THE FWD ENG MOUNT BULKHEAD INTERNAL ANGLE. 2 L 7 4 4F RT A20WE 2008022700312 20080227 00312 NM 2008 2 27 KCSA081088 1 20080219 A 5420 STIFFENER BOEING 747 747221F 1384868 NM NR 3 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 NR 3 PYLON LT UPPER STIFFENER CRACKED AT ATTACH POINT OF THE FWD ENG MOUNT BULKHEAD INTERNAL ANGLE. 2 L 7 4 4F RT A20WE 2008022700314 20080227 00314 NM 2008 2 27 SWAA080892 1 20080218 A 5311 6546554 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, STR 27L. REPAIRED FRAME PER FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008022700316 20080227 00316 EA 2008 2 27 SIMA200805706 1 20080223 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 503AE 10021 ON FLIGHT 4074, CREW REPORTED 3 EMERGENCY LIGHTS INOP IN CABIN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED EM ERGENCY EXIT BATTERY AND CHARGER AT SEAT 12 IAW W/C 33-002. OPERATIONAL CHECK GOOD AND NR 8194; AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4F RT A21EA 2008022700317 20080227 00317 NM 2008 2 27 SWAA080894 1 20080215 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, RBL 3. REPAIRED S KIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700319 20080227 00319 NM 2008 2 27 SWAA080893 1 20080215 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SK IN PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700324 20080227 00324 WP 2008 2 27 AALA200800319 1 20080214 A 2150 A/C PACK DOUG DC9 DC982 3022082 WP DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 445AA 49471 STL INFLIGHT T1419/14FEB - AFTER TAKEOFF CREW REPORTED SMOKE AND FUMES IN CABIN. RETURNED TO STL AND LANDED WITHOUT IN CIDENT. ACCOMPLISHED AIR CONDITIONING PACK BURN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022700326 20080227 00326 WP 2008 2 27 IXXA08SMN025S 1 20080119 A 5340 37552222 FITTING DOUG DC8 DC862F 3021972 WP BS 822 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 822.500 LEFT BOTTOM LINE 24" (CENTER WING AREA). REMOVED CRACKED FITTING. CLEANED TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-3- 0, 51-1-20D, 51-3-1, DC8 SRM 51-3-0, AND DC8 SRM 51-1-8B. 2 L 7 4 4F 4A25 2008022600243 20080226 00243 NM 2008 2 26 AMTA200800033 1 20080126 A 3350 D71701100 BATTERY PACK BOEING 737 73783N 13844HI NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 314TZ 30640 FWD GALLEY RT EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY, BATTERY PACK IAW AMM 33-51-06-960-8-0 5, OPS CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 2008022600253 20080226 00253 NM 2008 2 26 AMTA200800042 1 20080130 A 4930 RELAY BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE APU DEFECTIVE A AMTA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 518AT 27974 APU FAULT LIGHT ON AT ALL TIMES WITH SWITCH OFF AND APU VALVE MESSAGE ON. NO FAULTS FOUND IN THE WIRING, FOUND RELAY K1 0162 BAD, REMOVED AND REPLACED K10162 RELAY. REMOVED AND REPLACED APU SURGE FILTER, APU. OPS CHECKS NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008022600269 20080226 00269 NM 2008 2 26 AMTA200800081 1 20080212 A 5340 ATTACH FITTING BOEING 737 73783N 13844HI NM LAVATORY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 317TZ 28246 AFT OB ATTACHMENT BLOCK CORRODED IN LAV E. REMOVED AND REPLACED ATTACHEMENT BLOCK IAW 25-46-99. (K) 2 L 7 2 4F RT A16WE 2008022700013 20080227 00013 WP 2008 2 27 WRLA2008023 1 20080211 A 5730 APB7132 SKIN DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CENTER WING CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 136WA 47844 DURING MAINTENANCE INSPECTION AT SAA, CORROSION FOUND ON CENTER WING UPPER SKIN LT SIDE, APPROX STA XCW101. REPAIRED PE R SAA EA 010-5710-11-A0232 REV A. 2 L 7 3 4F 4 F A22WE E23EA 2008022700029 20080227 00029 WP 2008 2 27 NWAA080629956 1 20080221 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 923RW 47183 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE R EPLACED THE EMERGENCY BATTERY PACK AND OPERATIONALLY CHECKED THE SYSTEM. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2008022700045 20080227 00045 NM 2008 2 27 UIEA200800020 1 20080126 A 5280 STRUCTURE BOEING 747 7472D3B 1384805 NM LT MLG DOOR DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 LT MAIN LANDING GEAR OUTBOARD STRUT DOOR HAS AN 18.0 INCH LONG SECTION AT LEADING EDGE OF MATERIAL SEPARATING. PERMANEN T REPAIR ACCOMPLISHED AS PER SRM 51-40-09 FIG 12 SHEET 1 AND 4 AND SRM 51-40-12, PREPREG 250 DEGREES F CURE. ALSO REFER ENCE EO NR 4752A129. 2 L 7 4 4F RT A20WE 2008022700095 20080227 00095 NM 2008 2 27 SWAA080900 1 20080216 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 443WN 29838 DURING SCHEDULED HC1 CHECK, FOUND EEPLS LENS CRACKED AT ROW 17 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008022700096 20080227 00096 2008 2 27 SWAA080881 4 20080217 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008022700122 20080227 00122 NM 2008 2 27 ASAA0842571 1 20080105 A 5320 65465926 CHANNEL BOEING 737 7374S3 1384711 NM FSUELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 AFT CARGO PIT FLOOR CHANNEL FOUND CORRODED AT BS 767+6 RBL 8. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008022700125 20080227 00125 NM 2008 2 27 ASAA0842595 1 20080124 A 5320 694147327 INTERCOSTAL BOEING 737 7374S3 1384711 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 786AS 24795 FWD CARGO PIT LBL 21 FLOOR INTERCOSTAL CRACKED BS 500 B TO 500 C. CASCADE RESPONSIBILITY INTERCOSTAL REPLACED. 2 L 7 2 4F RT A16WE 2008022700130 20080227 00130 NM 2008 2 27 LYNX00007 1 20080201 A 5270 401010101 PROXIMITY SENSOR BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY EXIT LACK OF LUBE A 3LYA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 21 503LX 4170 AIR TURNBACK - MASTER WARNING W/ "FUSELAGE DOOR" LIGHT CAME ON CLIMBING THROUGH 20000 FEET ACCOMPANIED BY RED "EMERGENCY EXIT" ON "RIGHT FRONT" ILLUMINATED ON SYSTEM DOORS PAGE. PRESSURIZATION NORMAL. RETURNED TO DEN PER QRH. MAINTENANC E LUBRICATED FORWARD EMERGENCY EXIT DOOR PROXIMITY SENSOR PER Q400 AMM TASK 52-71-01-830-805. OPS CHECK GOOD. NO DEFEC TS NOTED AT THIS TIME. 2 H 7 2 4T RT A13NM 2008022700176 20080227 00176 NM 2008 2 27 08FDEA00585 1 20080223 A 5311 6914871 FRAME BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 FWD LOWER CARGO COMPT FRAME TIE AT STA 580 LBL 20 CORRODED AT END VERIFIED MATERIAL FOR REPLACEMENT FRAME TIE REF DWG 69 -14871 .050 7075 T-6. FABRICATED NEW FRAME TIE REF DWG 69-14871. TREATED PRIMED REF SRM 51-10-2. INSTALLED NEW FRAME TIE REF SRM 51-30-2, CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008022700177 20080227 00177 EU 2008 2 27 TRAX200800233 1 20080128 A 5320 FITTING AEROSP ATR72 ATR72 EU FUSELAGE BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 FWD WING BOX BETWEEN FR 23 STR LT 1 - RT 1 CLIP BROKEN. 2 H 7 2 4T RT 2008022700187 20080227 00187 EU 2008 2 27 TRAX200800236 1 20080208 A 3350 COVER AEROSP ATR72 ATR72 EU CABIN CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 643AS 413 F/A REPORTS SERVICE DOOR EXIT LIGHT COVER IS CRACKED AND NOT LEGIBLE. 2 H 7 2 4T RT 2008022700194 20080227 00194 WP 2008 2 27 08FDEA00597 1 20080225 A 5347 60715817075T65 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 363FE 48263 SEAT TRACK HAS 2 WORN LUGS AT FS 1631 AND 1636, TRACK LBL 8. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1. REPAIR PARTS FABRICATED ON TRAVELERS T8/725335 AND T8/725337 MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008022700200 20080227 00200 EA 2008 2 27 TRAX200800198 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 RIGHT SIDEWALL SEAT RAIL FS 477.40 TO FS 570.0 HAS CORROSION DAMAGE. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IA W CRJ 700 SRM 53-31-49. APPLIED ALODINE IAW CRJ 700 SRM 51-21-16. SUPPLEMENTAL SDR CLOSED 2/12/08. 2 L 7 2 4F RT A21EA 2008022700227 20080227 00227 WP 2008 2 27 IXXA08SMN010S 1 20080115 A 5280 DOOR DOUG DC8 DC862 3021970 WP MLG DELAMINATED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING (MLG/FUSELAGE) UPPER DOOR DELAMINATED SKIN. REMOVED RIGHT MAIN LAND ING GEAR OUTBOARD DOOR. INSTALLED NEW DOOR. PERFORMED OPS CHECK FOR HYD SYSTEM LEAKS GOOD IAW DC8 MM 32-12-1 PAGE 404, DC8 MAINTENANCE MANUAL 32-12-1 PAGE 401 01-07-08, DC8 MM 27-10-0, 27-20-0, 27-40-0, 27-50-0, 27-60-0, 27-80-0, 27-00, 3 2-30-0, 32-42-0, 32-50-0, 52-36-1 AND 78-30-0. 2 L 7 4 4F 4A25 2008022700234 20080227 00234 SO 2008 2 27 CHQA200800031 1 20080215 A 5610 SEAL EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL WINDSHIELD LOOSE A CHQA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 11 845RP 145551 CAE312428 CVG TO AZO - ON INITIAL CLIMB, THE FLIGHT CREW NOTICED A RUMBLING SOUND COMING FROM THE FIRST OFFICER'S WINDSHIELD. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE HUMP SEAL ON TH E FIRST OFFICER'S WINDSHIELD WAS COMING LOOSE. MAINTENANCE APPLIED A TEMPORARY REPAIR FOR THE SEAL AND OPENED A RESCHED ULE FOR A FINAL REPAIR. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008032700028 20080327 00028 EA 2008 3 27 426PE03A 1 20080312 A 3260 824034 PROXIMITY SWITCH CNDAIR CL600 CL6002B16 1900305 EA NLG FAILED E DBCA A UNSCHED LANDING E P VIBRATION/BUFFET NO WARNING INDICATION CL CLIMB 1 GL 13 426PE 7862 5046 ON DEPARTURE FROM MKE CREW REPORTED A BUFFETING NOISE FROM THE NOSE OF THE AIRCRAFT, SOUNDED LIKE THE NOSE GEAR DOOR WAS OPEN, BUT WERE NOT GETTING A "NOSE GEAR DOOR OPEN" ANNUNCIATOR. CREW PERFORMED A PASS DOWN THE RUNWAY AND MAINTENANCE WAS ABLE TO VERIFY ONE NOSE GEAR DOOR WAS OPEN. CREW CIRCLED AIRPORT TO BURN OFF FUEL TO GET BELOW MAX LANDING WEIGHT, THEN LANDED AT MKE WITHOUT INCIDENT. AIRCRAFT WAS PLACED ON JACKS AND NOSE GEAR LINKAGE WAS INSPECTED. FOUND LEFT GEA R DOOR ACTUATOR LINK ASSY WAS UNLATCHED. LATCHED LINK ASSY AND ALL OPERATION WAS NORMAL. SUSPECT LEFT LINK ASSY WASN'T LATCHED AFTER MANUAL RELEASE FOR PREFLIGHT. INSPECTED "NOSE GEAR DOOR OPEN" ANNUNCIATOR SYSTEM AND FOUND LEFT NOSE GEA 2 L 7 2 4F RT A21EA 2008032700054 20080327 00054 SO 2008 3 27 SWIA200819365 1 20080126 A 5540 BEARING EMB 120 EMB120ER 3260203 SO RUDDER HINGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 289YV 120289 LOWER RUDDER HINGE NR 1 BEARING IS CORRODED, FOUND AT C-CHECK. REPLACED HINGE BEARING IAW EMB 120 MM 55-30-01. 2 L 7 2 4T RT A31SO 2008032700077 20080327 00077 SO 2008 3 27 RAIA00803015 1 20080319 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 834HK 145269 PRE FLT 7932 - IAD - BLUE PORTION OF EMERGENCY LIGHT STRIP AT SEAT 2A INOP. MAINTENANCE DEFERRED THIS SECTION OF THE FL OOR STRIP IAW MEL. 2 L 7 2 4T RT T00011AT 2008032700080 20080327 00080 NM 2008 3 27 TSAA0821016 1 20080313 A 2121 215201 FAN BOEING 737 737282 13844AT NM GASPERS FAILED A TSAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 824AL 23045 FLIGHT 93 OGG - HNL - THE CREW NOTED AN UNPLEASANT BURNING ODOR IN THE CABIN DURING FLIGHT WITH NO SMOKE PRESENT. THE O DOR DECREASED WITH ENGINES AT LOWER THROTTLE SETTINGS. THE AIRCRAFT LANDED IN HNL WITHOUT FURTHER INCIDENT. MAINTENANC E REMOVED AND REPLACED THE AIR CONDITIONING GASPER FAN PER AMM 21-24-21 WITH ALL OPERATIONAL CHECKS SATISFACTORY. 2 L 7 2 4F RT A16WE 2008032700081 20080327 00081 NE 2008 3 27 F3LA200800129 2 20080317 A 7230 BEARING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE NR 1 ENGINE FAILED A F3LA E B A ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 NM 03 928FR 13927 121 2236 575824 DURING CRUISE, FLIGHT CREW REPORTED VIBRATION FOLLOWED BY ECAM WARNING OF NUMBER 1 ENGINE OIL FILTER CLOG, LOSS OF OIL P RESSURE, INCREASE IN OIL TEMPERATURE AND LOSS OF OIL LEVEL. THE ENGINE WAS SHUT DOWN, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY AT THE DIVERSION AIRPORT. PRELIMINARY ENGINEERING EVALUATION INDICATES POSSIBLE FAILURE OF THE NUMBER 3 BEARING IN THE COMPRESSOR SECTION OF THE ENGINE. ENGINE CHANGE WILL BE ACCOMPLISHED. DAMAGED ENGINE WILL BE S ENT FOR TEARDOWN. WHEN TEAR DOWN REPORT IS AVAILABLE, THIS SDR WILL BE UPDATED. ENGINE CHANGE COMPLETED AND AIRCRAFT R ETURNED TO SERVICE. DAMAGED ENGINE EN ROUTE TO GE (STROTHER FACILITY) FOR TEAR DOWN. 2 L 7 2 4F 4 F RT A28NM 2008032700085 20080327 00085 EA 2008 3 27 MASA200800238 1 20080318 A 3350 M610624001 RELAY CNDAIR CL600 CL6002D24 1390016 EA CABIN FAULTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 926LR 15026 ASH FLT 2946 PHX-MEM, PILOT REPORTED THAT THE EMERGENCY LIGHTS WERE CYCLING ON AND OFF. MX CHANGED THE CONTROL PANEL AN D RELAY, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2008032700095 20080327 00095 NM 2008 3 27 08FDEA01088 1 20080320 A 5320 146N53993 INTERCOSTAL BOEING 757 7572B7 1384964 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 AFT PIT, LOWER FLANGE OF INTERCOSTAL AT STA 1402, RBL 2.90 IS CORRODED. REMOVED CORROSION, L=3.9", W= .75", D= .012", O RIGINAL MATERIAL THICKNESS WAS .040". INTERCOSTAL FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04, FIG 101, DETAIL II LIMITS . REMOVED INTERCOSTAL IAW SRM 51-40-02. FABRICATED REPLACEMENT INTERCOSTAL ON TRAVELER NR T8/72622 HEAT TREATED TO T6 IAW SRM 51-10-02. INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-40-02. TREATED AND PRIMED AREA IAW SRM 51-20-01. TOP C OATED AREA IAW AMM 51-21-00-7. 2 L 7 2 4F RT A2NM 2008032700096 20080327 00096 WP 2008 3 27 08FDEA01089 1 20080321 A 5730 ARB30272 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 307FE 48291 RT WING L/E DROPPED (REMOVED PART) FOUND WEAR ON SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 39 SHT 2 VOL I. 2 L 7 3 4F RT A22WE 2008032700098 20080327 00098 EU 2008 3 27 08FDEA01091 1 20080321 A 5542 PANEL AIRBUS 310 A310324 3930206 EU RUDDER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 LEFT RUDDER PANEL, 2ND FASTENER FROM THE TOP HAS WATER IN 7 CONNECTED CELLS; 5 CONNECTED CELLS AND 5 INDIVIDUAL CELLS, (MARKED IN WHITE MARKER) AND DELAMINATION 3.3 INCH BY 1.9 INCH. REPAIRED LT RUDDER PANEL 2ND FASTENER FROM TOP BY REMOV ING THE DAMAGED AREA & BONDING NEW CORE & PAY UP REPAIR PLIES IAW EA 6-5540-118453. 2 L 7 2 4F RT A35EU 2008032700106 20080327 00106 SO 2008 3 27 SIMA200808111 1 20080313 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 19976 5000 145130 DURING MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED AND REPLACED WITH NEW PART IAW SRM 51-4 0-02 AND 51-20-03. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032700107 20080327 00107 SO 2008 3 27 SIMA200808101 1 20080317 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 623AE 145109 DURING MBV INSPECTION, FOUND LEFT OMEGA BEAM CORRODED ON INBOARD SIDE AT CARBON CROSS MEMBER AT FRAME 20. REPAIRED OMEG A BEAM AT FRAME 20 IAW SRM 53-00-10 FIGURE 201. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032700111 20080327 00111 SO 2008 3 27 SIMA200808114 1 20080312 A 5320 14529610003 PROFILE EMB 145 EMB145LR 3260212 SO CARGO DOORWAY CRACKED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 683AE 9364 5000 14500833 DURING A IMBV INSPECTION, THE CARGO FWD EDGE PROFILE LOWER CORNER WAS FOUND CRACKED. REMOVED PROFILE REPLACED WITH NEW PART IAW SRM 51-40-02, 51-40-04. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032700112 20080327 00112 SO 2008 3 27 SIMA200808117 1 20080319 A 3411 PITOT LINE EMB 145 EMB145LR 3260212 SO CONTAMINATED A SIMA O OTHER C F.O.D. AP APPROACH 1 SW 21 909AE 14500899 ON FLIGHT 4125, CREW REPORTED DURING APPROACH THAT THEY COULD NOT TELL WHAT ATTITUDE THEY WERE AT. ALL THREE ALTIMETERS SHOWING DIFFERENT READINGS. CREW DECLARED EMERGENCY, FMS MESSAGE UNRELIABLE ALTIMETER DO NOT USE FOR NAV. AFTER LANDI NG CREW NOTICED THE STANDBY ALTIMETER WAS OFF 800 TO 900 FT. AFTER CREW SAT AT THE GATE FOR A WHILE ALL THREE INDICATIO NS CAME BACK TO NORMAL. FOUND A LOT OF WATER IN THE RIGHT PITOT LINE. MINOR AMOUNT IN THE RIGHT LINE. AIRCRAFT RETURN ED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032700113 20080327 00113 SO 2008 3 27 SIMA200808108 1 20080312 A 5320 14522178 SILL EMB 145 EMB145LR 3260212 SO SERVICE DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AE 19993 5000 145148 DURING MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REPAIRED SERVICE DOOR SILL IAW EMB SRM 53-21-02 FIG 201 AND 51-40-02. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4T RT T00011AT 2008032700117 20080327 00117 SO 2008 3 27 SIMA200808116 1 20080313 A 5320 145217000007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 683AE 9364 5000 14500833 DURING A IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED CORRODED AREA REPAIR IAW SRM 53-0 0-10 FIG 201. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022700275 20080227 00275 NM 2008 2 27 08FDEA00536 1 20080220 A 5730 1060031116 PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 WING FUEL PANEL 642AB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 642AB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-116. 2 L 7 2 4F RT A2NM 2008022700285 20080227 00285 NM 2008 2 27 08FDEA00540 1 20080220 A 5730 1060031119 PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 WING FUEL PANEL 641JB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 641JB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-119. 2 L 7 2 4F RT A2NM 2008022700286 20080227 00286 NM 2008 2 27 CALA0800157 1 20080207 A 5320 69366564 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 INTERCOSTAL WEB AT STA 927 TO 947 CORRODED. REMOVED DAMAGED 4 ANGLES AND INSTALLED NEW ANGLES PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008022700309 20080227 00309 NM 2008 2 27 KCSA081086 1 20080219 A 5315 FLOORBEAM BOEING 747 747209B 138489B NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 UPPER DECK FLOORBEAM WEB DENTED AT BS 780, RBL 20. 2 L 7 4 4F RT A20WE 2008022700318 20080227 00318 NM 2008 2 27 SWAA080895 1 20080215 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, LBL 2. REPAIRED S KIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700328 20080227 00328 NM 2008 2 27 UIEA200800053 1 20080215 A 5313 STRINGER BOEING 747 7472D7B 1384803 NM ZONE 100 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 AFT CARGO COMPARTMENT STRINGER 49 CORROSION AT STATION 1600, LEVEL 1 CORROSION. AFT CARGO STRINGER CORROSION REPAIRED I AW SRM 51-10-01. APPLIED FINISH IAW 51-21-00. 2 L 7 4 4F RT A20WE 2008022700334 20080227 00334 NM 2008 2 27 UIEA200800056 1 20080215 A 5313 STRINGER BOEING 747 7472D7B 1384803 NM ZONE 100 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 AFT CARGO COMPARTMENT STA 1500 STRINGER 43 CORRODED. REMOVED CORROSION PER SRM 51-10-01. REPROTECTED PER 51-10-02. 2 L 7 4 4F RT A20WE 2008022700336 20080227 00336 NM 2008 2 27 SWAA080858 1 20080214 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 410WN 27897 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008022700337 20080227 00337 NM 2008 2 27 UIEA200800058 1 20080215 A 5330 SKIN BOEING 747 7472D7B 1384803 NM ZONE 100 SCRATCHED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 PERFORMED EO 4753B107 FOUND SCRIBE LINE DISCREPANCY. REPAIRED LAP JOINT PAR ATLAS EO 4753B107 AND 4753B108. 2 L 7 4 4F RT A20WE 2008022700340 20080227 00340 NM 2008 2 27 SWAA080859 1 20080217 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482A, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022700341 20080227 00341 NM 2008 2 27 SWAA080868 1 20080217 A 5311 6546555 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700342 20080227 00342 NM 2008 2 27 SWAA080865 1 20080217 A 5311 65C34356 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700344 20080227 00344 NM 2008 2 27 SWAA080860 1 20080217 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022700350 20080227 00350 NM 2008 2 27 SWAA080912 1 20080218 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST DUCT BS 380. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008022700351 20080227 00351 NM 2008 2 27 SWAA080910 1 20080216 A 3397 W146001520 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND EEPLS INOP AT ROW 1 DEF. FOUND LOOSE WIRE. SECURED WIRE PER MM. 2 L 7 2 4F RT A16WE 2008022700358 20080227 00358 NM 2008 2 27 SWAA080876 1 20080218 A 5310 6546817 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 360 AND BS 380, RBL 65. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008022700359 20080227 00359 NM 2008 2 27 SWAA080877 1 20080218 A 5310 6546956 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 400 AND BS 420, RBL 65. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008022700360 20080227 00360 NM 2008 2 27 SWAA080878 1 20080218 A 5743 657172 SUPPORT FITTING BOEING 737 7373G7 1384595 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND LT MLG WALKING BEAM SUPPORT FITTING LUG CORRODED. REMOVED AND REPLACED FITTING PER MM . 2 L 7 2 4F RT A16WE 2008022700362 20080227 00362 2008 2 27 SWAA080883 4 20080214 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 725SW 27857 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008022800004 20080228 00004 NM 2008 2 28 F3LA200800073 1 20080225 A 3350 32146210 EPSU AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE EMERGENCY LIGHTS INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 949FR 10 2857 DURING C1 C CHECK, INSPECTION REPORTED THE OPERATIONAL TEST OF THE EMERGENCY LIGHTS FAILED WITH A FAULT MESSAGE OF "EPSU (13WL) AFT L/DEU B." MAINTENANCE REMOVED AND REPLACED THE EPSU IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-38-000 -001 AND AMM 33-51-38-400-001. UPON COMPLETION OF THE INSTALLATION, THE EPSU OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM 2008022800010 20080228 00010 NM 2008 2 28 HALA0800335 1 20080219 A 5312 BULKHEAD BOEING 717 717200 1383700 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION AT STATION 37 PRESSURE BULKHEAD, HORIZONTAL SKIN (SHELF). REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800014 20080228 00014 NM 2008 2 28 HALA0800306 1 20080222 A 2432 2404087 BATTERY BOEING 767 7673CB 1385187 NM MASTER HOT A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM, STATUS MSG "MAIN BATT CHGR" BATT VOLTAGE 26VDC, BATTERY HOT, CHARGER GREEN LT ON, FOUND DURING ETOPS 1 CHECK. T/S PER FIM 24-31-00 FIG 103A, REMOVED AND REPLACED MAIN A/C BATTERY PER AMM 24-31-01-004-001/404-006. VOLTAGE CHECK AND CHARGER OPS NORMAL. TIME BASES AND CLOCKS RESET PER AMM 31-25-00/501. 2 L 7 2 4F RT A1NM 2008022800018 20080228 00018 NM 2008 2 28 HALA0800284 1 20080220 A 5330 SKIN BOEING 767 7673G5 1385126 NM BS 1540 S38R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 1540 AT LONGERON S-38R, MARKED NR 40, AREA INSPECTED. FASTENER DAMAGE W/I LIMITS AS PER SRM 53-00-01/101. FASTENER CLEANED/PRIMED/PAINTED. FASTENER REQ'D TO BE REPAIRED AS PER SRM 53-00-01 REPAIR 8 AT OR BEFORE 50 FLT CYCLES. 2 L 7 2 4F RT A1NM 2008022800023 20080228 00023 2008 2 28 HALA0800307 4 20080221 A 3442 RADAR BOEING 767 7673CB 1385187 NM WX SYSTEM MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM, WXR SYS ON STATUS PAGE. CYCLED CAPT AND FO WXR SWITCHES. MSG CLEARED. PERFORMED OP TEST PER AMM 34-43-00, TESTS GOOD. 2 L 7 2 4F RT A1NM 2008040200102 20080402 00102 NM 2008 4 2 USAA920080705 1 20080324 A 5523 65C2638427 TAB BOEING 737 7373B7 1384580 NM LT ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 23380 CLT - MAJOR REPAIR - C4 CHECK - LEFT ELEVATOR TRIM TAB HINGE CUT OUT CRACKED AND DELAMINATED. REPLACED LEFT ELEVATOR TR IM TAB IAW B737 AMM 27-31-00. 2 L 7 2 4F RT A16WE 2008022800025 20080228 00025 EU 2008 2 28 F3LA200800072 1 20080223 A 2761 31077111 ACTUATOR AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE SPOILER LEAKING A F3LA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 03 812FR 2340 1222 3163 DURING CLIMB, THROUGH 15000 FEET, THE FLIGHT CREW RECEIVED AN ECAM WARNING INDICATING THE GREEN SYSTEM HYDRAULIC QUANTIT Y WAS LOST. THE FLIGHT CREW PERFORMED AN AIR TURNBACK AND AFFECTED AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AI RCRAFT AND FOUND THE NR 5 RT SPOILER ACTUATOR LEAKING. MAINTENANCE REPLACED THE ACTUATOR IN ACCORDANCE WITH THE REQUIRE MENTS OF AMM 27-64-51-PB-401. FOLLOWING INSTALLATION, THE NEW UNIT OPERATIONALLY CHECKED OKAY. MAINTENANCE ALSO REMOVE D AND REPLACED THE HYDRAULIC CASE DRAIN FILTER IN ACCORDANCE WITH AMM 29-11-43-PB-401. NO METAL WAS FOUND AND THE REPLA CEMENT FILTER LEAK CHECKED OKAY. MAINTENANCE SERVICED THE GREEN HYDRAULIC SYSTEM IN ACCORDANCE WITH AMM 12-62-29-611-00 2 L 7 2 4F 4 F RT 2008022800026 20080228 00026 NM 2008 2 28 HALA0800334 1 20080219 A 5312 BULKHEAD BOEING 717 717200 1383700 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 2 CORROSION, ON RADOME PRESSURE BULKHEAD RT SIDE O/B INTERCOSTAL, (STIFFENER). REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800029 20080228 00029 NM 2008 2 28 HALA0800285 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 733 S36R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 733 AT LONGERONS S-36R, MARKED NR 37. REPAIRED PER SRM 53-00-01-ZR-8 CAT C REPAIR ( TEMP). REPETITIVE INSPECTIONS EVERY 1500 CYCLES. PERMANENT REPAIR AT 6000 CYCLES. 2 L 7 2 4F RT A1NM 2008022800031 20080228 00031 NM 2008 2 28 HALA0800292 1 20080217 A 5280 DOOR BOEING 717 717200 1383700 NM RT MLG CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 RT MLG DOOR RAMP CRACKED AT INBD MOUNT BRACKET. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800034 20080228 00034 NM 2008 2 28 HALA0800274 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 357 S38-39R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 357 BETWEEN LONGERONS S-38R AND S-39R. REPAIRED PER SRM 53-00-01-ZR-8 CAT C REPAIR (TEMP). REPETITIVE INSPECTIONS EVERY 1500 CYCLES. PERMANENT REPAIR AT 6000 CYCLES. 2 L 7 2 4F RT A1NM 2008022800041 20080228 00041 NM 2008 2 28 HALA0800301 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 364 S37-38R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 364 BETWEEN LONGERONS S37R AND S38R. CLEANED, TREATED AND PRIMED PER SRM 53-00-01 P AINT PEND. AREA PAINTED AS PER SRM 51-22-01. 2 L 7 2 4F RT A1NM 2008032700118 20080327 00118 SO 2008 3 27 SIMA200808107 1 20080316 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO CARGO DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 19976 5000 145130 DURING A MBV INSPECTION, THE BAGGAGE DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. REMOVED THE DAMAGED SILL AND REPLACED WITH NEW SILL IAW EMB 145 SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032700119 20080327 00119 NM 2008 3 27 NWAA081026307 1 20080320 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 667US 24222 DURING OVERNIGHT CHECK, FOUND UPPER DECK FORWARD EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY M 335 AND BATTERY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008032700120 20080327 00120 EA 2008 3 27 MASA200800244 1 20080319 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 938LR 15038 ASH FLT 2774 PHX-OAK, EMERGENCY CEILING FLOODLIGHT AT ROW 23 INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2008032700123 20080327 00123 SO 2008 3 27 CHQA200800055 1 20080318 A 3350 100865 POWER SUPPLY EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHTS INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 567RP 6422 500 145698 CAE312049 DURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE NON FUNCTIONAL. THE NR 4 EMERGENCY LIGHT POWER SUPPLY WAS REPLACED AND THE OVERWING EMERGENCY LIGHT SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008032700127 20080327 00127 EA 2008 3 27 MASA200800247 1 20080320 A 3350 LS6006182 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75995 7361 ASH FLT 7078 IAD-OVERNIGHT, FWD EMERGENCY FLOOR LIGHT STRIP INOP AND POSSIBLY DAMAGED. MX REPLACED THE LIGHT STRIP ASSE MBLY. 2 L 7 2 4F RT A21EA 2008032700136 20080327 00136 EA 2008 3 27 MASA200800254 1 20080321 A 2750 766389N ECU CNDAIR CL600 CL6002D24 1390016 EA NR 1 MALFUNCTIONED A MASA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 07 912FJ 11027 15012 ASH FLT 2934 PHX- MEM, FLAP HALF SPEED MESSAGE, SPOILER STAB FAULT MESSAGE, FLAP AURAL WARNING WITH FLAP AT ZERO DEGREES , AND ALT 100-200 FT HIGH AT FL 330. REMOVED AND REPLACED NR 1 SFECU. 2 L 7 2 4F RT A21EA 2008032700144 20080327 00144 NM 2008 3 27 DL777080397 1 20080320 A 5330 146W63501 SKIN BOEING 777 777232 1385232 NM BS 1640- 1650 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 864DA 29736 FUSELAGE SKIN HAS TWO DENTS/GOUGES LOCATED BETWEEN STA 1630 AND 1650 AT S-32R. CUTOUT DAMAGED SKIN AND INSTALLED REPAIR . 2 L 7 2 4F RT T00001SE 2008032700145 20080327 00145 NE 2008 3 27 DL76G080398 2 20080320 A 7261 LINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 ENGINE OIL CRACKED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 1602 40302 29694 704809 RT ENG OIL QTY LOSS, FOUND OIL QTY XMITTER LINE MPN 1978M64G01 CRACKED. REPLACED SAME, LEAK CKS OK SERVICED ENG W/MOBIL JET. 2 L 7 2 4F 4 F RT A1NM E13NE 2008032700146 20080327 00146 NE 2008 3 27 DLM90080399 2 20080321 A 7200 ACTUATOR DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE LT ENG STATER MALFUNCTIONED A DALA O OTHER Y ENGINE STOPPAGE DE DESCENT 1 SO 27 906DA 21691 020105 53386 020105 LEFT ENGINE SHUT ITSELF DOWN ON APPROACH INTO SEA. LEFT ENG RESTARTED. REPLACED L ENG STATOR VANE ACTUATOR PER AMM, ST ILL NEEDS L CHECK AND ENG TEST NR 3 AND 11, DC 690463. LEAK CHECKS E AND C/W TEST NR 3 AND NR 11. 2 L 7 2 4F 4 F RT A6WE E40NE 2008032700149 20080327 00149 NM 2008 3 27 DL764080402 1 20080322 A 3231 TDH80505001 RELAY BOEING 767 767432ER 1385134 NM MLG DOORS MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 831MH NA 29702 GEAR DISAGREE PLUS GEAR DOORS ADVISORY MSG AFTER T/O. CYCLED BUT NO HELP, WITH GEAR DOWN, GEAR DOORS ADVISORY MESSAGE R EMAINS. CLOSED DOORS WITH DOOR CLOSE SWITCH. CYCLED GEAR HANDLE, DOORS OPEN AND WILL NOT CLOSE UNLESS WITH MTC SWITCH. NO HYD TO DOOR ACTUATOR EXTEND SIDE. NO POWER AT SAFETY VALVE. FOUND RELAY K10365 BAD. REPLACED RELAY. GOOD POWER AT VALVE BUT DOORS STILL INOP WITH GEAR HANDLE. JACKED ACFT AND PERFORMED GEAR SWING PER AMM. CHECKS GOOD SEVERAL TIME S. 2 L 7 2 4F RT A1NM 2008032700151 20080327 00151 NM 2008 3 27 DL757080403 1 20080322 A 2120 UNKNOWN BOEING 757 757232 1384965 NM CABIN SMOKE A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 693DL 29725 AFTER STARTING RT ENGINE AND PUTTING ON PACKS, COCKPIT FILLED WITH SMOKE. RAN LT AND RT PACKS OFF APU AIR. NO SMOKE OR ODOR. STARTED ENG OFF APU AIR CROSSBLEED STARTED LT ENG. RAN PACKS FULL H TO FULL COLD 3 TIMES. NO SMOKE OR ODOR. R AN ENG TO TAKEOFF PWR FOR 3 MIN. NO SMOKE OR ODOR. OK FOR SVC. 2 L 7 2 4F RT A2NM 2008032600120 20080326 00120 NE 2008 3 26 DL757080384 2 20080317 A 7261 1A821101 MANIFOLD BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE BROKEN A DALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 27 641DL 23995 726689 RT ENG OIL QTY AT ZERO AND OIL PRESSURE DROPPING WITH OIL PRESS LIGHT FLICKERING AT CRUISE. MX FOUND THE MAIN BEARING B REATHER MANIFOLD BROKEN. REPLACED SAME, RAN ENGINE LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032600183 20080326 00183 GL 2008 3 26 SIMA200807907 2 20080313 A 7200 AE3007A13 ENGINE EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL NR 2 MALFUNCTIONED A SIMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SW 21 728AE 145328 CAE312770 ON FLIGHT 4564, CREW REPORTED STRONG SMOKE SMELL AND LAV SMOKE DETECTOR GOING OFF. AIRCRAFT LANDED WITHOUT INCIDENT. A IRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER 2 ENGINE IAW W/C 71-000-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008032600228 20080326 00228 WP 2008 3 26 08FDEA01054 1 20080319 A 5712 ARB1161 RIB DOUG DC10 DC1030F 3023504 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 307FE 48291 RT WING L/E INT ZONE FOUND CRACK ON RIB AND MISSING GANG CHANNEL ON RIB. REPAIRED AREA IAW SRM 57-00-01 FIG 10 VOL I. 2 L 7 3 4F RT A22WE 2008032600302 20080326 00302 EU 2008 3 26 MALA080041 1 20080317 A 5522 SKIN SAAB SF340 340B 7860101 EU RT ELEVATOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 444XJ 340B444 RT ELEVATOR UPPER SKIN LEADING EDGES HAVE 6 DENTS. REPAIRED IAW EO NR S55139. 2 L 7 2 4T RT A52EU 2008032700007 20080327 00007 NM 2008 3 27 DHL2008765008 1 20080112 A 5320 INTERCOSTAL BOEING 727 727264 138408M NM BS 950A CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, AFT CARGO COMPARTMENT BS 950A + 19" INTERCOSTAL LBL 5" HAS FASTENERS POPPED AND METAL CRACKED. REMOVED INTERCOSTAL AT AFT CARGO PIT IAW SRM 51-30-2. FABRICATED NEW INTERCOSTAL IAW SRM 53-10-2 FIG 5 AND 51-20-1. LOCATED AN D DRILLED NEW INTERCOSTAL IAW SRM 51-30-5. TREATED AND PRIMED AREA AND PART IAW SRM 51-10-2. INSTALLED NEW INTERCOSTAL IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032700009 20080327 00009 NM 2008 3 27 DHL2008765026 1 20080115 A 5755 SKIN BOEING 727 727264 138408M NM NR 2 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, NR 2 SPOILER NR 2 HINGE CUT OUT ON LT WING TRAILING EDGE CRACKED. REMOVED ON LT WING TRAILING EDGE SKIN SECTION AT NR 2 SPOILER DIMENSION 36" BY 2.5" IAW SRM 51-30-2. FABRICATED NEW SKIN SECTION IAW SRM 57-30-2 FIG 4 AND 5 1-20-1. TREATED AND PRIMED PART AND AREA IAW SRM 51-10-2. INSTALLED NEW SKIN SECTION AT NR 2 SPOILER NR 2 HINGE CUT O UT IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032700018 20080327 00018 NM 2008 3 27 DHL2008749020 1 20080118 A 5322 SHEAR TIE BOEING 727 7272J0 138407E NM BS 720C CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 DURING C CHECK, FRAME SHEAR TIE CORRODED AT BS 720C BETWEEN STRINGERS 28L AND 28R. FOUND CORROSION ON SHEAR TIE OUT OF LIMITS IAW SRM 53-10-1 FIG 1. FABRICATED NEW SHEAR TIE IAW SRM 51-20-1, 51-20-2, 51-30-5 AND 53-10-2 FIG 3. ALODINE AN D PRIMED ANGLE IAW SRM 51-10-2. INSTALLED NEW SHEAR TIE IAW SRM 51-30-2, 51-40-3 FIG. 1 AND 53-10-4 FIG 15. 2 L 7 3 4F RT A3WE 2008032700032 20080327 00032 EU 2008 3 27 2008UALA01420 1 20080314 A 2600 DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LAVATORY MALFUNCTIONED A UALA K NONE N FALSE WARNING AP APPROACH 1 WP 29 481UA 1559 LAVATORY DETECTOR ECAM ON SHORT FINAL. SWAPPED FWD LAV FOR AFT AND SYSTEM OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032700064 20080327 00064 NM 2008 3 27 DHL2008765001 1 20080129 A 5330 SKIN BOEING 727 727264 138408M NM BS 1185 MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, EXISTING REPAIR HAS BLIND RIVETS INSTALLED IN DOUBLER SHOULD BE SOLID FASTENERS PER SRM AT BS 1185 STRIN GER 17L. REMOVED EXISTING REPAIR IAW SRM 51-30-2. FABRICATED NEW REPAIR DOUBLER IAW SRM 53-30-3 FIG 26 AND 53-30-2 FIG 3. ZERO TIMING OF EXISTING FASTENERS HOLES IN THE CRITICAL ROWS OF THE REPAIR, HFEC INSPECTED THE CRITICAL ROWS IAW ND TM PT6-51-00-00 FIG 16 AND FIG 23 AND IAW SRM 51-10-1 FIG. 12. NO CRACK INDICATIONS WERE NOTED. REAMED THE EXISTING FA STENER HOLES IN THE CRITICAL ROWS OF THE REPAIR TO 1/16 INCH OVERSIZE IAW SRM 51-10-1. TREAT AND PRIME DOUBLER IAW SRM 51-10-2. INSTALLED NEW REPAIR DOUBLER IAW SRM 53-30-3 FIG 26 AND 53-30-2. 2 L 7 3 4F A3WE 2008032700071 20080327 00071 NM 2008 3 27 DHL2008749019 1 20080206 A 5310 ANGLE BOEING 727 727223 1384074 NM BS 990 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 DURING C CHECK, EXFOLIATION NOTED AT C2 DOOR CUT OUT, BS 990 (FRAME) BETWEEN STRINGERS 26R AND 27R. REMOVED CORROSION A T C2 DOOR CUT OUT BS 990 IAW SRM 51-10-6, ORIGINAL THICKNESS 0.100, MATERIAL LOSS 0.35, MATERIAL REMAINING 0.65, FOUND O UT OF LIMITS IAW SRM 53-10-2 FIG 5 AND 53-10-1 FIG 1. FABRICATED ANGLE REPAIR & FABRICATED REPAIR STRAP IAW COTNEY AER OSPACE DRAWING NR AE95-53-101 REV IR. TREATED AND PRIMED PARTS AND AREA IAW SRM 51-10-2. INSTALLED ANGLE REPAIR AT BS 990 BETWEEN STRINGERS 26R AND 27R IAW SRM 51-30-2 AND DRAWING NR AE95-53-101 WITH 8110-3 DATED 02/06/2008. 2 L 7 3 4F A3WE 2008032700088 20080327 00088 WP 2008 3 27 08FDEA01083 1 20080320 A 5321 ACA3205505 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 MAIN CABIN FLOORBOARD AT LBL 48 TO 76 FROM BS 506 TO 590 HAS A PUNCTURED UPPER SKIN. REPAIRED MAIN CABIN FLOOR PANEL AT LBL 48 TO 76; BS 506 TO 590 WITH FILLER AS REQUIRED IAW FEDEX DC/MD-10 DWG SRZ 25-005, REV F. 2 L 7 3 4F RT A22WE 2008032700103 20080327 00103 SO 2008 3 27 SIMA200808104 1 20080309 A 5320 14525382004 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 617AE 145093 DURING MBV INSPECTION, FOUND FLOOR SILL AT FRAME 71 ABOVE STR 17R WITH CORROSION. REMOVED AND REPLACED RT FLOOR SILL AT FRAME 71 IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032700121 20080327 00121 SO 2008 3 27 CHQA200800054 1 20080317 A 2131 22250N030301 CONTROLLER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN PRESSURE MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 260SK 18269 18269 145128 CAE311802 CLE TO ATL - DURING FLIGHT, THE AIRCRAFT CABIN WOULD NOT PRESSURIZE FULLY. THE CREW DROPPED BELOW 10,000 FT AND USED TH E PRESSURE DUMP TO RELEASE REMAINING PRESSURE AND RETURNED TO CLE. MAINTENANCE TROUBLESHOT THE PRESSURIZATION SYSTEM AN D FOUND THE DIGITAL PRESSURE CONTROLLER MALFUNCTIONING AND REPLACED IT. AFTER REPLACING THE DIGITAL PRESSURE CONTROLLER , THE PRESSURIZATION SYSTEM OPERATED NORMALLY 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008032700147 20080327 00147 EA 2008 3 27 MASA200800255 1 20080321 A 5210 CABLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF POSITION A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651MJ 7139 ASH FLT IAD-CAE, PAX DOOR WOULD NOT OPEN AND CABLE STICKING OUT OF THE DOOR AND WAS UNABLE TO OPEN IT FROM OUTSIDE. MX OPENED THE DOOR AND REPOSITIONED CABLE AND OP CHECKED THE DOOR GOOD. 2 L 7 2 4F RT A21EA 2008032700152 20080327 00152 EA 2008 3 27 MASA200800257 1 20080322 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF ADJUST A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 715SF 7115 ASH 7291 SPI - IAD, NOSE GEAR DOOR OPEN WARNING. ADJUSTED PROX SENSOR, SWUNG GEAR, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008032700170 20080327 00170 NM 2008 3 27 2008UALA01406 1 20080313 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FWD ENTRY DOOR UPPER HINGE CUTOUT HAS CRACK IN FASTENER HOLE ON LWR SIDE. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INST ALLED EXTERNAL FUSELAGE SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700173 20080327 00173 EU 2008 3 27 CPCP20080014 1 20080304 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 377AT 377 FOUND LT O/B SEAT TRACK BETWEEN FRAME 29 TO FRAME 35 CORRODED. LEFT O/B SEAT TRACK BETWEEN FRAME 29 TO FRAME 35. REPLA CED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2008032700182 20080327 00182 WP 2008 3 27 08FDEA01046 1 20080319 A 5230 ADA37741 SKIN DOUG MD10 MD1010F 3022112 WP CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 GOUGED/DENTED FORWARD LOWER CARGO DOOR SKIN AT THE FORWARD CORNER. COMPLIED WITH CARGO DOOR SKIN/PAN REPAIR IAW DC/MD-1 0 SRM 52-10-00; VOL I; FIG 17. 2 L 7 3 4F RT A22WE 2008032700184 20080327 00184 NM 2008 3 27 2008UALA01414 1 20080313 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 MED (FORWARD ENTRY DOOR) CUTOUT LOWER HINGE 1 EA FASTENER ABOVE & 1 EA FASTENER BELOW HINGE CUTOUT HAS CRACK INDICATIONS . MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008022800042 20080228 00042 NM 2008 2 28 HALA0800294 1 20080217 A 5280 SKIN BOEING 717 717200 1383700 NM RT MLG DOOR CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 RT MLG DOOR HAS SURFACE CORROSION ON OUTER SKIN. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800045 20080228 00045 NM 2008 2 28 HALA0800286 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 698 S36R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 698 AT LONGERON S-36R, MARKED NR 36. REPAIRED PER SRM 53-00-01-ZR-8 CAT C REPAIR (T EMP). REPETITIVE INSPECTIONS EVERY 1500 CYCLES. PERMANENT REPAIR AT 6000 CYCLES. 2 L 7 2 4F RT A1NM 2008022800047 20080228 00047 NM 2008 2 28 HALA0800275 1 20080220 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 370 S37-38R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 LIGHTNING STRIKE ON FUSELAGE AT STA 370 BETWEEN LONGERONS S-37R AND S-38R, MARKED NR 18. AREA INSPECTED. FASTENER DAMA GE W/I ALLOWABLE LIMITS AS PER SRM 53-00-01/101. FASTENER CLEANED/PRIMED/PAINTED. FASTENER REQ'D TO BE REPAIRED AS PER SRM 53-00-01. REPAIR 8 AT OR BEFORE 50 FLT CYCLES. 2 L 7 2 4F RT A1NM 2008022800050 20080228 00050 NM 2008 2 28 HALA0800345 1 20080219 A 5311 FRAME BOEING 717 717200 1383700 NM BS 465 L29R CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION, FWD CARGO PIT STA 465, ON FRAME AROUND FASTENERS, L 29R. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800051 20080228 00051 2008 2 28 UPS08851672 4 20080214 A 2565 LATCH DOUG DC8 DC873F 302199F WP EVAC SLIDE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:N/A EMERGENCY ESCAPE SLIDE HAS BROKEN LATCH. SLIDE INOP FOR CREW ENTRY DOOR. DEFERRED CREW ENTRY DOOR SLIDE PER MEL 52-7-4. SLIDE IS SECURED IN SUITCASE. REMOVED SLIDE COVER AND ROUTED TO SHEET METAL. REMOVED AND REPLAC ED LATCH REF DCI SRM 51-01-21. REINSTALLED ORIGINAL SLIDE INTO CONTAINER AND INSTALLED ON DOOR REF MM 25-60-01-2. M369 243 CLEARED. 2 L 7 4 4F RT 4A25 2008022800060 20080228 00060 EU 2008 2 28 08FDEA00606 1 20080226 A 5730 A57340096 SKIN AIRBUS 300 A300B4622R 3930312 EU RT WING CHAFED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 745FD 668 CHAFING MARKS FOUND ON LT OUTER WING BOTTOM SKIN REINFORCING PLATE AT RIB 7. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS AND NDT FOR CRACK FREE IAW RAS/BAE/1006409/2008 ISS A, APPROVED BY EA 6-5720-114930. 2 L 7 2 4F RT A35EU 2008022800061 20080228 00061 EU 2008 2 28 08FDEA00607 1 20080226 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 CORROSION ON LT WING BOTTOM SKIN UPPER SURFACE AT RIB 5 AFT OF REAR SPAR. REPAIR PERFORMED BY BLEND OUT THE CORROSION A ND NDT FOR CRACK FREE CONDITION, FLAP PEENING IAW RAS/BAE/1006416/2008 ISS A, APPROVED BY EA 6-5720-114931. 2 L 7 2 4F RT A35EU 2008022800065 20080228 00065 NM 2008 2 28 UPS08M51681 1 20080110 A 5720 DOUBLER DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C LEFT WING FIXED L/E COMPT AT STA XORS 500 APPROX FOUND UPPER DOUBLER SUSPECTED CRACK AS MARKED. HFEC INSP C/O PER NDTSPM 06-10-01.001 R13 ON SUSPECTED CRACK AREAS & FOUND APPROX 1/4 CRACK AS MARKED. INBOARD & OUTBOARD RI B AT LEFT FIXED L/E COMPT AT STA XORS 500 AREA REMOVED FOR ACCESS PER SRM 51-31-01 V.II R35. NEW REPAIR DOUBLER 01EA, R EPAIR FILLER 01EA & 04EA REPAIR ANGLES FAB & INSTALLED PER SRM 57-10-00 V.I FIG 27 REV 40. 2 L 7 3 4F RT A22WE 2008022800066 20080228 00066 EU 2008 2 28 08FDEA00616 1 20080226 A 5311 A5361119220500 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 COCKPIT WINDSHIELD CENTER FRAME EXTERIOR, 2ND BOLT HOLE FROM THE BOTTOM IS ELONGATED. COMPLIED WITH EA NR 6-5310-113036 PART 1. 2 L 7 2 4F RT A35EU 2008022800068 20080228 00068 WP 2008 2 28 IXXA08SMN026S 1 20080119 A 5340 FITTING DOUG DC8 DC862F 3021972 WP BS 702 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 702.000 LEFT BOTTOM LINE 24" (CENTER WING AREA). REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-0 AND SRM 51-3-1. 2 L 7 4 4F 4A25 2008022800070 20080228 00070 2008 2 28 SWAA080906 4 20080218 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 749SW 29801 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008022800071 20080228 00071 NM 2008 2 28 SWAA080871 1 20080217 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 762SW 27876 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008022800072 20080228 00072 NM 2008 2 28 KCSA081089 1 20080220 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE SKIN DAMAGED AT BS 580, NEAR STR 46R. 2 L 7 4 4F RT A20WE 2008022800076 20080228 00076 EA 2008 2 28 CHQA200800039 1 20080223 A 7830 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE THRUST REVERSER ILLUMINATED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 469SM 7650 GEE873397 SDF TO IAH - AFTER TAKEOFF, THE CREW RECEIVED A REV NR 1 UNLOCK MESSAGE ON EICAS, THE QRH WAS FOLLOWED AND THE AIRCRAFT RETURNED TO FIELD AND LANDED UNEVENTFULLY AT SDF. MAINTENANCE LOCKED OUT THE REVERSER AND PLACED IT ON MEL. 2 L 7 2 4F 4 F RT A21EA E15NE 2008022800078 20080228 00078 NM 2008 2 28 AALA200800300 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700186 20080327 00186 WP 2008 3 27 08FDEA01057 1 20080319 A 5313 AGA31851 STRINGER SPLICE DOUG MD10 MD1010F 3022112 WP BS 1056 S45L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 FWD LOWER CARGO BILGE STR 45L U-CHANNEL HAD CORROSION AT BS 1056. REMOVED CORROSION; ORIGINAL MATERIAL .070; MATERIAL R EMAINING .050 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01; VOL I. REMOVED AND REPLACED SPLICE CLIP IAW SRM 51-33-01; VOL II, P/N AGA 3185-1, PO 612787.1. 2 L 7 3 4F RT A22WE 2008032700188 20080327 00188 NM 2008 3 27 2008UALA01417 1 20080313 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 STRINGER CLIP 13L IS CRACKED ON FWD SIDE OF A FRAME AT BS 294.5. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED CLIP. FAB RICATED & INSTALLED NEW CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700193 20080327 00193 NM 2008 3 27 2008UALA01428 1 20080313 A 5313 FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FUSELAGE STRINGER END FITTING IS CRACKED BS 360 STR 15L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED CHANNEL. INSTALLE D REPLACEMENT CHANNEL. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700197 20080327 00197 WP 2008 3 27 08FDEA01099 1 20080321 A 5321 ACA3205505 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 200 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 MAIN CABIN FLOORBOARD AT RBL 48 TO 76; BS 615 TO 675 IS SOFT AND SPONGY. EVALUATED FLOOR PANEL INSTALLED INSERTS. FO UND PANEL TO BE SOLID PER FEDEX SRZ 25-005 REV F. SDR SUBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 3 4F RT A22WE 2008032700202 20080327 00202 2008 3 27 2008UALA01436 4 20080313 A 2565 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 525UA 24978 SLIDE WILL NOT ARM LEFT AFT DOOR. LAMPS BURNT OUT. RELAMPED 2 EACH LIGHT BULBS IN SLIDE INDICATOR. OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032700206 20080327 00206 NM 2008 3 27 08FDEA01108 1 20080322 A 5720 65162101 SUPPORT BEAM BOEING 727 727225 1384077 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 MIGRATING SHIMS AND LOOSE HARDWARES AT LWR SIDE OF NR 7 SPOILER SUPPORT BEAM FITTING WS 198. REPAIRED NR 7 SPOILER ACTU ATOR SUPPORT BEAM FITTING IAW DRAWING SR27-57-038 REV "C". 2 L 7 3 4F A3WE 2008032700209 20080327 00209 NM 2008 3 27 08FDEA01110 1 20080322 A 5720 SR2757025 BEAM BOEING 727 727225 1384077 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 RT WING I/B T/E "J " BEAM AT WING STATION 92 CRACKED, WING T/E SUPPORT BEAM FOR NR 7 SPOILER. TRIMMED OUT CRACKED AREA LENGTH 0.75" IAW SRM 51-10-1. TREATED AND PRIMED AREA "J" BEAM IAW SRM 51-10-2 DRAWING SR27-57-025. 2 L 7 3 4F A3WE 2008032700213 20080327 00213 NM 2008 3 27 2008UALA01478 1 20080316 A 2621 BOTTLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FIRE BOTTLE FAULTY A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION IN INSP/MAINT 1 WP 29 942UA 26679 APU BOTTLE DISCHARGE LIGHT ILLUMINATED. AFTER TROUBLE SHOOTING SYSTEM FOUND FIRE EXTINGUISHING BOTTLE FAULTY. REPLACED A PU FIRE EXTINGUISHING BOTTLE IAW MM 26-22-11. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700220 20080327 00220 NM 2008 3 27 2008UALA01482 1 20080316 A 3350 90085 CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 OVERWING EMERGENCY LIGHT 2FWD RT INOP. REPLACED BATTERY CHARGER. OP CHECKED NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032700223 20080327 00223 NM 2008 3 27 2008UALA01484 1 20080317 A 3510 89151114 BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW O2 LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 104UA 26902 CREW O2 1550 PSI. SERVICED CREW O2 TO 1800 PSI. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032700225 20080327 00225 NM 2008 3 27 08FDEA01118 1 20080323 A 5311 AFA00193 FRAME DOUG MD11 MD11F 3023600 NM BS 1721 S12L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 522FE 48476 MAIN DECK LEFT FRAME AT BS 1721 S12L FOUND DENTED. REPAIRED AS PER SRM 53-30-00, FIG.1, VOL.1. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00, FIG.1, VOL.1. REPAIR C LASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032700227 20080327 00227 NM 2008 3 27 2008UALA01485 1 20080317 A 3510 MC1019151 OXYGEN MASK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 104UA 26902 CAPT O2 MASK SQUEEZE TO INFLATE MECH STICKY. REPLACED OXYGEN MASK. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032700234 20080327 00234 WP 2008 3 27 08FDEA01124 1 20080324 A 5322 ADA011223 SHEAR TIE DOUG MD10 MD1010F 3022112 WP BS 899 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 FWD PIT; FS 899 SHEAR TIE AT L49L TO L51R HAS DOUBLE DRILLED HOLES. FABRICATED NEW SECTION OF THE SHEAR TIE & SHEAR TIE SPLICE SPLICE IAW DWG ADA 0112; REV P & SRM 53-30-00 VOL I FIG 10. ALODINED, PRIMED & PAINTED IAW SRM VOL II PG 8. PART MARKED IAW GMM 7-0-1000. 2 L 7 3 4F RT A22WE 2008032700240 20080327 00240 WP 2008 3 27 08FDEA01127 1 20080324 A 5420 AVB702733 SEAL DOUG MD10 MD1010F 3022112 WP NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 NR 2 ENGINE LEFT CORE COWL SKIRT FAIRING SPRING SEALS ARE CRACKED. REMOVED & REPLACED THE SPRING SEAL IAW SRM 51-35-01; VOL II. 2 L 7 3 4F RT A22WE 2008032700244 20080327 00244 EU 2008 3 27 08FDEA01131 1 20080324 A 5320 A5377832900000 WEB AIRBUS 310 A310203 3930313 EU CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FWD LOWER CARGO COMPARTMENT/CORROSION ON WEB BETWEEN FRAMES 34 AND 35 RT UNDER ROLLER TRACK AT RBL 56 ABOVE STRINGER 44. REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008022800080 20080228 00080 NM 2008 2 28 SWAA080928 1 20080219 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800083 20080228 00083 NM 2008 2 28 HALA0800329 1 20080218 A 5280 DOOR BOEING 717 717200 1383700 NM RT MLG CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION ON THE EXTERIOR SURFACE OF THE RT MLG OTBD DOOR. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800085 20080228 00085 NM 2008 2 28 HALA0800344 1 20080219 A 5312 BULKHEAD BOEING 717 717200 1383700 NM BS 686 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION IN FWD CARGO PIT (AFT BULKHEAD), STA 686 FRAME. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800088 20080228 00088 NM 2008 2 28 DHL2008752605 1 20080206 A 5730 SKIN BOEING 727 727223 1384074 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 LT WING UPPER T/E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IS CRACKED FWD. REMOVED FASTENERS AT LT WING UPPER T /E WBL 320 NR 4 SPOILER INBOARD CENTER HINGE CUTOUT IAW B727 SRM 51-30-2. STOP DRILLED 0.250" DIA AT END OF CRACK IAW B 727 SRM 57-30-4 FIG 10. FABRICATED DOUBLER MATERIAL USED 7075T6 0.071 PO NR 9005482 DIMENSION 4" BY 55/8" IAW B727 SRM 57-30-4 FIG 10. TREATED AND PRIMED DOUBLER AND AREA IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW B727SRM 51-30-2 AND 57-30-4 FIG 10. 2 L 7 3 4F A3WE 2008022800090 20080228 00090 NM 2008 2 28 SWAA080925 1 20080219 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800089 20080228 00089 WP 2008 2 28 AALA200800270 1 20080208 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 410AA 49321 DFW - EMERGENCY LIGHT AT TAIL COMPARTMENT SIDEWALL MISSING LENS. REPLACED BROKEN LIGHT ASSEMBLY AND LENS FOR EMERGENCY LIGHT AT TAIL COMPARTMENT SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022800097 20080228 00097 NM 2008 2 28 HALA0800342 1 20080219 A 5347 SEAT TRACK BOEING 717 717200 1383700 NM BS 437 CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 CRACK ON LT SIDE OTBD SEAT TRACK SUPPORT EAR, UNDER FLOORBOARD AT FUSELAGE STA 437.00. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800098 20080228 00098 NM 2008 2 28 SWAA080918 1 20080219 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800100 20080228 00100 NM 2008 2 28 HLA0800340 1 20080219 A 5414 SKIN BOEING 717 717200 1383700 NM LT NACELLE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION ON LT ENG, LOWER COWLING FWD NR 1RIB, I/B REPAIR DOUBLER. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800106 20080228 00106 NM 2008 2 28 SWAA080952 1 20080219 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800107 20080228 00107 WP 2008 2 28 AALA200800273 1 20080208 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 410AA 49321 DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 28 TO 30 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHE AD SEAT ROWS 28 TO 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022800109 20080228 00109 NM 2008 2 28 AALA200800257 1 20080207 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 767AJ 33539 DFW - EMERGENCY LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD GALLEY. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022800110 20080228 00110 NM 2008 2 28 AALA200800262 1 20080207 A 3350 8039001 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9630A 53561 LGA - EMERGENCY LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHTS AT FORWARD GALLEY . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2008022800111 20080228 00111 WP 2008 2 28 AALA200800269 1 20080208 A 3350 SHROUD DOUG DC9 DC982 3022082 WP CABINEMERGENCY L DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AA 49321 DFW - EMERGENCY LIGHT AT SEAT 10D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022800113 20080228 00113 WP 2008 2 28 08FDEA00516 1 20080219 A 5340 ACA721831 BRACKET DOUG DC10 DC1030F 3023504 WP BS 365-363 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 WEB SUPPORT BRACKET ACA 7218-31 HAS TOOLING MARKS. BLENDED TOOLING MARKS ON WEB SUPPORT BRACKET IAW SRM 51-21-02, VOL I I. ORIGINAL MATERIAL THICKNESS .090 IAW DWG ACA 7218 REV E MATERIAL LOSS .068, OUT OF LIMITS IAW SRM 53-00-01, VOL I. FABRICATED NEW ACA 7218-31 BRACKET BY FORMING AND DRILLING IAW DWG ACA 7218 REV E. ALODINED, PRIMED IAW SRM 51-21-02 PG 8, VOL II. PART MARKED PER FEDEX GMM 7-0-1000. BRACKET INSTALLED ON CARD NR 52305547. 2 L 7 3 4F RT A22WE 2008022700135 20080227 00135 NM 2008 2 27 UIEA200800031 1 20080212 A 5415 FITTING BOEING 747 74747UF 1384812 NM NR 4 PYLON CHAFED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 415MC 32837 DURING SCHEDULED MAINTENANCE, FOUND NR 4 PYLON WEAR DAMAGE ON THE LUG FACE OF THE UNDERWING MIDSPAR FITTINGS. THE DAMAG E WAS REMOVED FROM THE LUG SURFACES BY BLENDING SMOOTH. THE FITTINGS WERE CONFIRMED FREE OF CRACKS AND OTHER DAMAGE BY DETAIL VISUAL AND NDT INSPECTION. AS PER BOEING MESSAGE 1-760110158-5 AND FAA 8100-9. 2 L 7 4 4F RT A20WE 2008022700137 20080227 00137 NM 2008 2 27 UIEA200800036 1 20080207 A 5753 SKIN BOEING 747 747271C 1384869 NM TE FLAP ERODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 537MC 22403 LEFT OUTBOARD FOREFLAP HAS EVIDENCE OF EROSION AT 2 PLACES ON IT'S LEADING EDGE AT APPROX 12 AND 18 INCHES OUTBOARD OF N R 1 FLAP TRACK, EVIDENCE OF CONTACT BETWEEN FOREFLAP AND T/E PANEL. LT OUTBOARD FOREFLAP LEADING EDGE EROSION REPAIRED IAW SRM 51-40-12 AND EO 4757A418. 2 L 7 4 4F RT A20WE 2008022700166 20080227 00166 EU 2008 2 27 MJN1 1 20080204 A 3610 SEAL AMD FALC10 FALCON10 2730101 EU GARRTT TFE731 TFE73121C NE BLEED AIR SYS WORN E 9MJA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CR CRUISE 1 GL 09 769B 60 CREW REPORTED SMOKE IN CABIN, FOLLOWED PROCEDURES TO CLEAR SMOKE AND ISOLATED POWER TO MEDICAL EUIPMENT BELIEVING THAT W AS THE SOURCE. NO ADDITIONAL SMOKE OR SMELL WAS OBSERVED. WHILE EN ROUTE TO MAINTENANCE FACILITY THE CREW REPORTED HEA RING AND FEELING A LOUD VIBRATION IN THE AIRFRAME, BELIEVING IT TO BE FROM AN ENGINE. INSPECTION REVEALED NO EVIDENCE O F FIRE IN AIRCRAFT. THE NR 2 ENGINE OIL WAS OBSERVED TO BE HIGHER THAN NORMAL, POSSIBLY CAUSING A MINOR LEAK RESULTING IN THE SMOKE IN CABIN. TWO BLEED AIR LINE CONNECTIONS WERE FOUND WITH WORN SEALS AT THE HEAT EXCHANGER CAUSING THE META L LINE TO VIBRATE AND LEAK CAUSING THE VIBRATION. 2 L 7 2 4F 4 F A33EU E6WE 2008022700192 20080227 00192 EA 2008 2 27 TRAX200800238 1 20080208 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 852AS 7369 PAX DOOR TOP STEP B/W BROKEN. 2 L 7 2 4F RT A21EA 2008022700220 20080227 00220 EA 2008 2 27 TRAX200800241 1 20080210 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 825AS 7207 ON APPROACH, FLAPS FAIL AT ZERO. EMERGENCY DECLARED. FLT 4892 CX. 2 L 7 2 4F RT A21EA 2008022700226 20080227 00226 NM 2008 2 27 CALA0800139 1 20080214 A 5330 6545774 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16301 23352 STA 747 ABOVE STRINGER 24 FOUND 1.8" LONG CRACK WHILE PERFORMING C-SCAN INSPECTION. REPAIRED FUSELAGE PER SRM 53-00-01 REPAIR 31 DETAIL X. 2 L 7 2 4F RT A16WE 2008022700237 20080227 00237 SO 2008 2 27 SIMA200805304 1 20080218 A 3233 21180100401 ACTUATOR EMB 145 EMB145LR 3260212 SO MLG WORN A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 691AE 14500860 ON FLIGHT 3973, CREW REPORTED LANDING GEAR CLUNKING NOISE. DURING LANDING GEAR RETRACTION CLUNKING LOUD BANG AT RETRACT ION. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NOSE LANDING GEAR DOOR ACTUATOR IAW EMB 145 AMM 32-33-03. OP ERATIONAL CHECK GOOD. NO DEFECTS NOTED AND NR 8194; AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008022700238 20080227 00238 EU 2008 2 27 MAC020802 1 20080203 A 3240 20125112Y00 METERING VALVE AEROSP ATR72 ATR72202 8680940 EU BRAKE SYSTEM MALFUNCTIONED A MTNA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 68 810FX 220 DURING TAXI ON INITIAL BRAKE CHECK, LOW RIGHT BRAKE PRESSURE WAS DISCOVERED ON BOTH THE PIC AND SIC SIDES. THE A/C RETU RNED TO THE GATE. THE BRAKE METERING VALVE WAS REPLACED. 2 H 7 2 4T RT A53EU 2008022700245 20080227 00245 WP 2008 2 27 IXXA08SMN014S 1 20080115 A 5330 SKIN PANEL DOUG DC8 DC862F 3021972 WP ZONE 100 CRACKED B IXXA O OTHER O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO PANELS SUPPORT CRACK AT STATION 460 LONGERON 30 LEFT. REMOVED FA STENERS AS NEEDED TO PERFORM REPAIR. FABRICATED ANGLE DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INS TALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-20D, 51-1-21, DC8 SRM 53-2-0 PAGE 2E AND 2F, DC8 SRM 51-1-8B, AND 51-3-1. 2 L 7 4 4F 4A25 2008022700294 20080227 00294 WP 2008 2 27 IXXA08SMN011S 1 20080115 A 5280 SKIN DOUG DC8 DC862 3021970 WP MLG DELAMINATED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING (MLG/FUSELAGE) MIDDLE DOOR DELAMINATED SKIN. REMOVED DELAMINATED DOO R. INSTALLED NEW MID DOOR. PERFORMED OPS CHECK FOR HYD SYSTEM LEAKS GOOD IAW DC8 MM 32-12-1 PAGE 404, DC8 MM 27-10-0, 27-20-0, 27-40-0, 27-50-0, 27-60-0, 27-80-0, 27-00, 32-30-0, 32-42-0, 32-50-0, 52-36-1 AND 78-30-0. 2 L 7 4 4F 4A25 2008022700320 20080227 00320 SO 2008 2 27 SIMA200805701 1 20080223 A 5100 NONE EMB 135 EMB135KL 3260302 SO NONE NONE A SIMA O OTHER O OTHER CR CRUISE 1 SW 21 804AE 145487 ON FLIGHT 4188, CREW REPORTED WHILE EN ROUTE "LO FUEL NR 2" WARNING WITH NR 1 TANK ON EICAS SHOWING BLANK. CLEARED IT S ELF THEN REAPPEARED. FUEL QUANTITY ON FMS SYSTEM ALL NORMAL. APPROACHING ORD, ANOTHER WARNING AND NR 2 FUEL ON EICAS S HOWED BLANK. DECLARED EMERGENCY/PRIORITY APPROACH AND LANDED SHORTLY AFTER. AIRCRAFT REMOVED FROM SERVICE. FOUND REFU EL PANEL POWER SWITCH IN "BATTERY" POSITION. RESET POWER SWITCH TO "POWER" POSITION. OPERATIONAL CHECK GOOD AND NR 819 4; AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008022700321 20080227 00321 NM 2008 2 27 SWAA080866 1 20080217 A 5311 6546536 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022700339 20080227 00339 NM 2008 2 27 UIEA200800059 1 20080215 A 5330 SKIN BOEING 747 7472D7B 1384803 NM ZONE 100 SCRATCHED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 PERFORMED EO 4753B107 FOUND SCRIBE LINE DISCREPANCY. REPAIRED LAP JOINT PER ATLAS EO 4753B107 AND 4753B108. 2 L 7 4 4F RT A20WE 2008022700361 20080227 00361 NM 2008 2 27 SWAA080911 1 20080218 A 5330 6545776 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008022800001 20080228 00001 EU 2008 2 28 08FDEA00614 1 20080226 A 5347 A5327400500053 SEAT TRACK AIRBUS 310 A310324 3930206 EU BS 2984-3090 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 MAIN CABIN FLOOR BETWEEN FS 54.2 AND FS 54.3; 37 INCHES RIGHT OF CENTER LINE SEAT TRACK IS GOUGED/WORN. REPAIRED SEAT T RACK IAW A310-300 SRM 53-10-16; FIG 101. 2 L 7 2 4F RT A35EU 2008022800005 20080228 00005 NM 2008 2 28 HALA0800295 1 20080217 A 5280 SKIN BOEING 717 717200 1383700 NM LT MLG DOOR CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LT MLG DOOR HAS SURFACE CORROSION ON OUTER SKIN. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800019 20080228 00019 NM 2008 2 28 F3LA200800071 1 20080218 A 5751 D5764004000060 SEAL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE RT AILERON CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 903FR 5893 1560 DURING C5 C CHECK, MAINTENANCE REPORTED CORROSION FOUND ON RIGHT WING AILERON HINGE SEAL NEAR OUTBOARD HINGE LOCATION. MAINTENANCE REMOVED AND REPLACED AILERON SEAL IN ACCORDANCE WITH REQUIREMENTS OF A319 SRM 51-72-11 AND EA A9-57R-30062. TOUCH PAINTING PERFORMED IN ACCORDANCE WITH A319 SRM 57-61-21-K-FIGURE 211. FOLLOWING COMPLETION OF INSTALLATION AND P AINT, SEAL AND AILERON WERE INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008022800052 20080228 00052 NM 2008 2 28 HALA0800319 1 20080218 A 5510 STRUCTURE BOEING 717 717200 1383700 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 1 CORROSION ON RT HORIZ 2. RUSTED NUTS AFT SIDE OF HORIZ INTERNAL STRUCTURE AT STA XHS 103. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008022800093 20080228 00093 NM 2008 2 28 SWAA080920 1 20080219 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800099 20080228 00099 NM 2008 2 28 SWAA080926 1 20080219 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800122 20080228 00122 NM 2008 2 28 SWAA080936 1 20080218 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 FUSELAGE SKIN CRACKED BETWEEN BS 462 AND BS 466, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008022800128 20080228 00128 NM 2008 2 28 SWAA080941 1 20080219 A 5310 6516352 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 602SW 27953 DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT NR 4 DOOR STOP. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008022800131 20080228 00131 2008 2 28 SWAA080942 4 20080218 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED BRDG CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008022800133 20080228 00133 NM 2008 2 28 AALA200800260 1 20080207 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 771AN 29579 JFK - EMERGENCY LIGHT AT SEAT 34C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 34C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022800134 20080228 00134 NM 2008 2 28 UIEA200800051 1 20080215 A 5315 FLOORBEAM BOEING 747 7472D7B 1384803 NM ZONE 100 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 AFT CARGO COMPARTMENT STA 1700 RBL 55 FLOORBEAM CHORD ANCHOR NUT AREA FOUND MINOR CORROSION. LEVEL 1, BLENDED OUT CORRO SION IAW SRM 51-10-01 0.049" 1" WIDE 2" LONG. REPROTECTED PER 51-10-02. APPLIED CORROSION INHIBITOR COMPOUND. 2 L 7 4 4F RT A20WE 2008022800139 20080228 00139 NM 2008 2 28 SWAA080943 1 20080218 A 5330 6545857 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800142 20080228 00142 EA 2008 2 28 COMA0860138 1 20080216 A 5311 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 811CA 7380 RIGHT FS 640.00 FRAME DOUBLER IS CRACKED BETWEEN STR 9 AND STR 12. REMOVED FRAME DOUBLER P/N 601-36001-30 AND INSTALLED SERVICEABLE FRAME DOUBLER P/N 601-36001-30S IAW CRJ SRM 51-00-00 AND SR99-5140-0001. 2 L 7 2 4F RT A21EA 2008032500219 20080325 00219 NE 2008 3 25 2008UALA01456 2 20080314 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LEFT VIBRATION A UALA O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 29 228UA 30556 222050 LEFT ENGINE HAS PRONOUNCED VIBRATION AT 76 PERCENT N2 ABOVE 2.0. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500220 20080325 00220 NM 2008 3 25 2008UALA01457 1 20080314 A 3350 58674 INVERTER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 306UA 23667 EMERGENCY EXIT LIGHTS INOP ROW 15 REARWARD. REPLACED EEL LIGHT INVERTER AT ROW 20. ALL GND CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500227 20080325 00227 NM 2008 3 25 2008UALA01508 1 20080318 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT LIGHT INOP AT DOOR 5L AFT SILL. RELAMPED EMERGENCY LIGHT, OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032500228 20080325 00228 NM 2008 3 25 2008UALA01509 1 20080318 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 SEAT EEL LIGHT INOP ROW 3A 2ND FROM FWD. REPLACED EEL LIGHT. OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032700245 20080327 00245 NM 2008 3 27 2008UALA01495 1 20080316 A 2120 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN ODOR A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 829UA 1211 MOMENTARY ELECTRICAL SMELL IN AFT CABIN, SMELL DISSIPATED. COULD NOT DUPLICATE. CHECKED INDIVIDUAL SEATS AND WALL DISC ONNECT BOX 50MK6A, CHECKED BEHIND FLOOR SIDEWALL PANELS, POWERED PES, RAN PACKS, CHECKED GALLEY UNITS, COULD NOT DUPLICA TE SMELL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032700248 20080327 00248 NM 2008 3 27 2008UALA01527 1 20080318 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 INTERCOSTAL IS CRACKED AT FWD I/B CORNER BS 294.5 STR 12L. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700253 20080327 00253 NM 2008 3 27 AALA200800486 1 20080304 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 JFK - EMERGENCY LIGHT AT SEAT 23C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700255 20080327 00255 NM 2008 3 27 AALA200800488 1 20080304 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 JFK - EMERGENCY LIGHT AT SEAT 24C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700259 20080327 00259 NM 2008 3 27 AALA200800491 1 20080304 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 966AN 30094 MIA - EMERGENCY LIGHT AT SEAT ROW 27 HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 27. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008032700261 20080327 00261 NM 2008 3 27 2008UALA01532 1 20080317 A 3510 OXYGEN SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW O2 LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 378UA 24653 CREW O2 NEEDS REPLENISHING. SERVICED CREW O2. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700265 20080327 00265 NM 2008 3 27 AALA200800496 1 20080304 A 3350 FUSE BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 JFK - EMERGENCY LIGHTS AT FIRST CLASS GALLEY INOPERATIVE. REPLACED FUSE IN BATTERY PACK ABOVE LEFT NUMBER ONE DOOR FOR EMERGENCY LIGHTS AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700269 20080327 00269 NM 2008 3 27 AALA200800502 1 20080304 A 3350 LAMP DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 951TW 53470 LGA - EMERGENCY LIGHT AT OVERHEAD SEAT 26D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2008032700278 20080327 00278 NM 2008 3 27 AALA200800499 1 20080304 A 2560 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 951TW 53470 LGA - AISLE FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT GALLEY INOPERATIVE. REPLACED BATTERIES FOR EMERGENCY FLASHLIGHT AT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2008032700290 20080327 00290 SO 2008 3 27 C2XA08RI030 1 20080317 A 3233 21180100401 ACTUATOR EMB 145 EMB145LR 3260212 SO NLG DOOR DEFECTIVE A C2XA K NONE J WARNING INDICATION LD LANDING 1 SW 27 15986 19249 145254 FLIGHT 3053 - EWR - CREW REPORTED LANDING GEAR AIR/GRND WARNING MESSAGE DURING GEAR TRANSITION TO EXTEND. EWR MX REMOVE D AND REPLACED NOSE LANDING GEAR DOOR ACTUATORS IAW EMB 145 AMM 32-30-03 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. THIS SDR WAS FILED FOR THE LEFT HAND ACTUATOR. SDR C2XA08RI031 WAS FILED F OR THE RIGHT HAND ACTUATOR. 2 L 7 2 4T RT T00011AT 2008032700295 20080327 00295 2008 3 27 ARWA20080304 4 20080323 A 3422 COMPASS DOUG DC8 DC863F 302198F WP COCKPIT INOPERATIVE A ARWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 29 661AV 45969 FIRST OFFICER'S COMPASS INOPERATIVE. REMOVED AND REPLACED DIRECTIONAL GYRO NR 2 (DG-2) IN ACCORDANCE WITH M/M 34-21-1 A ND RADIO DIRECTION INDICATOR NR 2 (RDI NR 2) IN ACCORDANCE WITH 31-00. COMPASS GROUND TEST NORMAL IN ACCORDANCE WITH M/ M 34-21-0; 34-54-0 AND 34-51-0; 34-52-0. 2 L 7 4 4F 4A25 2008032700296 20080327 00296 NM 2008 3 27 DHL2008763516 1 20080308 A 5347 BAC1520792 SEAT TRACK BOEING 727 727264 138408M NM BS 560-600 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 SEAT TRACK CORRODED AT BS 560-600, LBL 25. REMOVED, FABRICATED FROM BAC1520-792, PO NR 9006020, 209" LONG, AND REPLACED SEAT TRACK SECTION PER B727 SRM 53-10-1 FIG 7 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 2008032700299 20080327 00299 NM 2008 3 27 DHL2008763518 1 20080314 A 5347 BAC1520792 SEAT TRACK BOEING 727 727264 138408M NM BS 480-600 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 FOUND SEAT TRACK CORRODED AT BS 480-600, RBL 24. REMOVED, FABRICATED FROM BAC 1520-792, PO NR 9006020, 209" LONG, AND I NSTALLED PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 2008032700301 20080327 00301 SO 2008 3 27 C2XA08IA087 1 20080321 A 3230 MS277891A SWITCH EMB 135 EMB135LR 3260305 SO COCKPIT MALFUNCTIONED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 27523 145389 IAH - FLIGHT 2220, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LAN DED WITHOUT INCIDENT. MAINTENANCE RESET THE EMERGENCY GEAR DOOR EXTENSION SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS , AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008032700305 20080327 00305 2008 3 27 ARWA20080305 4 20080324 A 3417 HG280D80 ADC DOUG DC10 DC1030F 3023504 WP NR 1 INTERMITTENT A ARWA O OTHER O OTHER DE DESCENT 1 SO 29 478CT 47819 CAPTAIN'S AIR DATA COMPUTER (ADC) CONTINUOUSLY FAILS IN FLIGHT. REMOVED AND REPLACED NR 1 CAPTAIN'S AIR DATA COMPUTER ( CADC) IN ACCORDANCE WITH M/M 34-16-00. NO LEAKS NOTICED AT THIS TIME IN ACCORDANCE WITH M/M 34-11-00. 2 L 7 3 4F RT A22WE 2008032700308 20080327 00308 WP 2008 3 27 NWAA081059995 1 20080318 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8978E 47327 DURING LINE CHECK, MAINTENANCE FOUND THAT THE CENTER EMERGENCY EXIT LIGHT IN THE TAIL COMPARTMENT WALKWAY WAS INOPERATIV E. MAINTENANCE REPLACED THE LIGHT ASSEMBLY, FUNCTIONALLY CHECKED IT, AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4F A6WE 2008032700309 20080327 00309 WP 2008 3 27 NWAA081089941 1 20080318 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3324L 47103 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY OVERWING EXIT SIGN ON THE RIGHT SIDE AT ROW 12 AND THE EMERGENCY PATHWAY LIGHTS AT ROWS 14, 15, 16, AND 17 WERE ALL FOUND TO BE INOPERATIVE. THE BATTERY PACK (09-3300-4-0122) AND POWE R SUPPLY (09-3300-4-0123) WERE BOTH REPLACED. ALSO MAINTENANCE FOUND AND REPAIRED A DAMAGED WIRE AT ROW 14. OPERATIONA L CHECKS WERE GOOD AND THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2008032700310 20080327 00310 WP 2008 3 27 NWAA081139851 1 20080324 A 3350 CHARGER DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NC 47708 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY FLOOD LIGHT FOR THE AFT EVACUATION SLIDE WAS NOT FUNCTIONAL. THE BATTERIES IN THE CHARGER PACK B5-28 WERE REPLACED AND THE LAMP WAS REPLACED. FUNCTIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A6WE 2008032700321 20080327 00321 SO 2008 3 27 C2XA08CL037 1 20080322 A 4950 4952375 BLEED VALVE EMB 145 EMB145LR 3260212 SO APU FAULTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16999 145307 CLE FLIGHT 2890 - THE CREW REPORTED A FUEL SMELL WHEN THE PACKS WERE OPERATING FROM THE APU. MAINTENANCE INSPECTED AND REPLACED THE APU BLEED VALVE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008032700324 20080327 00324 SO 2008 3 27 C2XA08RI036 1 20080303 A 3230 23092900001 UPLOCK EMB 145 EMB145EP 3260221 SO LT MLG DEFECTIVE A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 14933 20306 7594 145018 FLIGHT 2400 - EWR - CREW REPORTED NOSE LANDING GEAR MADE CONTINUOUS BANGING SOUND AFTER RETRACTION. CREW DIVERTED FLIGH T TO EWR AND LANDED AIRCRAFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED LEFT MAIN GEAR UPLOCK BOX AND PERFORMED OPERATIO NAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008032700327 20080327 00327 EU 2008 3 27 08FDEA01101 1 20080321 A 5230 A000702300285 LINER AIRBUS 310 A310324 3930206 EU CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 EXFOLIATED CORROSION AROUND THE AFT CARGO DOOR LINER FASTENER INSERT BETWEEN FRAME 59 AND FRAME 60 ON THE DOOR; FRONT AN D BACK SIDE OF THE FRAME. MATERIAL ID 2024-T3 0.050 PO 602303.2 IAW A310-300 SRM 52-32-00; PG 35 AND 51-31-00; PG 21- 22. CUT OUT DAMAGE AND FABBED REPAIR IAW A310-300 SRM 51-70-10. ALODINED IAW A310-300 SRM 51-21-00. PRIMED IAW A310-3 00 SRM 51-21-10. PAINTED IAW A310-300 SRM 51-23-10. INSTALLED DOUBLER IAW A310-300 SRM 51-70-10. 2 L 7 2 4F RT A35EU 2008032700331 20080327 00331 WP 2008 3 27 08FDEA01136 1 20080325 A 5753 ARC0503501 HINGE BRACKET DOUG DC10 DC1010F 3022111 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION, FOUND LT OUTBOARD FLAP OUTBOARD HINGE WITH ATTACH POINTS WITH OXIDE. REPLACED BRACKET ASS Y P/N ARC0503-501 FOR DWG ARC0505. 2 L 7 3 4F A22WE 2008032700333 20080327 00333 EU 2008 3 27 08FDEA01138 1 20080325 A 5730 A5735003200000 PANEL AIRBUS 310 A310203 3930313 EU RT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT WING FUEL PANEL 650KB HAS GOUGING ON THE UNDERSIDE. PANEL FOUND TO BE OUT OF LIMITS REF A310-200 SRM 57-20-16. F OR THE INSTALLATION OF THE PANEL SEE FEDEX WIC 46X5042ALI. 2 L 7 2 4F RT A35EU 2008032700335 20080327 00335 EU 2008 3 27 08FDEA01140 1 20080325 A 5730 A5735003200000 PANEL AIRBUS 310 A310203 3930313 EU RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT WING FUEL PANEL 650 HB HAS FRETTING CORROSION AROUND THE ATTACHMENT HOLES. PANEL FOUND TO BE OUT OF LIMITS REF A3 10-200 SRM 57-50-16. FOR INSTALLATION SEE FEDEX WIC 46X5042 ALI. 2 L 7 2 4F RT A35EU 2008032700338 20080327 00338 2008 3 27 NWAA081173210 4 20080323 A 2565 D30665105 SLIDE AIRBUS 320 A320211 3930320 EU L2 DOOR FAULTY A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 310NW 30420 94 121 WHILE PERFORMING EMERGENCY LIGHT SYSTEM CHECK PER LINE CHECK "EXT LOADS AFT L" MESSAGE, REF L/P 4273412. REMOVED AND RE PLACED 2L EVACUATION SLIDE. CHECKS GOOD. 2 L 7 2 4F RT A28NM 2008032700344 20080327 00344 NM 2008 3 27 HALA0800428 1 20080324 A 3620 WARNING SYSTEM BOEING 767 7673CB 1385187 NM BLEED AIR SYS MALFUNCTIONED A HALA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 592HA 33468 ETOPS SIGNIFICANT SYSTEM, AFTER R ENGINE STARTED. R ENGINE BLEED OFF AND ENG PRV DISPLAYED. R ENG BLEED OFF AND BLEED LT ILLUMINATED. NOTE RESET ITSELF UPON L ENG START PWR XFER. ACCOMPLISHED AMM 71-00-00 TEST 3. GND IDLE TEST. OPS CH ECK NORMAL. 2 L 7 2 4F RT A1NM 2008032700346 20080327 00346 NM 2008 3 27 HALA0800420 1 20080318 A 2613 710101950600 OVERHEAT LOOP BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 ENGINE MALFUNCTIONED A HALA K NONE N FALSE WARNING CR CRUISE 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, INTERMITTENT EICAS STATUS MSG, R ENG OH LP2 DISPLAYED. REPLACED NR 2 ENG FWD UPPER LOOP PER A MM 26-11-02. OPS CHK PER AMM 26-11-00. ENGINE HIGH PWR RUN, NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A1NM E13NE 2008032700349 20080327 00349 2008 3 27 HALA0800423 4 20080323 A 3416 ALTIMETER BOEING 767 76733A 1385209 NM COCKPIT MALFUNCTIONED A HALA K NONE O OTHER CR CRUISE 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, AFTER APPROX 3HR OF FLIGHT F/OS ALTIMETER CLIMBED BETWEEN 160' TO 180' SHOWED 37180 SWITCHED T O ALT AIR DATA ALTIMETER INDICATED GOOD AT 37020. TROUBLESHOT F/O ALTIMETER PER FIM 34-12-0. NO FAULTS ON EITHER ADC, CHECK PITOT STATIC SYSTEM PER FIM 34-11-00/101. ALL CHECKS OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008032700352 20080327 00352 NM 2008 3 27 HALA0800425 1 20080322 A 2613 644501 CIRCUIT CARD BOEING 767 767332 1382001 NM GE CF6 CF680A 30025 NE OVERHEAT SYSTEM FAULTY A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, EICAS STATUS MSG, R ENG OH LPW DISPLAYED. REPLACED RT OVERHEAT DETECTION CARD PER AMM 26-11-0 2. OPS CK OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2008032700358 20080327 00358 NM 2008 3 27 AALA200800534 1 20080309 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 972AN 30097 MSP - EMERGENCY LIGHT FORWARD OF RIGHT FORWARD OVERWING EXIT DOOR. REPLACED LIGHT ASSEMBLY AND LENS FOR EMERGENCY LIGHT FORWARD OF RIGHT FORWARD OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008032600274 20080326 00274 EU 2008 3 26 DHLA200800035 1 20080318 A 4990 TSCP7004B APU AIRBUS 300 A300B4203 3930306 EU APU BAY LEAKING A DHLA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION IN INSP/MAINT 1 GL 05 362DH 48874 88 084 BEFORE FLIGHT 102 ON GROUND IN SFO, 3 CABIN SMOKE DETECTORS ILLUMINATED ON THE GROUND. ON INSP FOUND APU TO BE LEAKING OIL. INGESTED INTAKE, SMOKE DET OK IAW AMM 26-10-0 DEFERRRED IAW MEL 49-11-01 DMI NR 32097. AIRCRAFT WAS GROUNDED. 2 L 7 2 4F RT A35EU 2008032600288 20080326 00288 EU 2008 3 26 08FDEA01076 1 20080320 A 5754 A53510561200 FITTING AIRBUS 300 A300B4622R 3930312 EU KRUEGER FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CORROSION ON FITTING AT KRUEGER FLAP AREA LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008032600289 20080326 00289 EU 2008 3 26 08FDEA01077 1 20080320 A 5754 A53510217201 FITTING AIRBUS 300 A300B4622R 3930312 EU KRUEGER FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CORROSION ON FITTING AT KRUEGER FLAP AREA RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008032600294 20080326 00294 NM 2008 3 26 DL76P080368 1 20080309 A 3397 WIRE BOEING 767 767332 1382001 NM COCKPIT OUT OF POSITION A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1402A 25989 WHEN BASE OF GRIMES LT TOUCHES FOOT SHOULDER HEATER SWITCH SPARKS ARE EMITTED. BOTH CAPT AND F/O SIDE. PULLED CB P-32 TO DEACTIVATE ALL GRIMES LTS FWD TO MCO AND PLACARD PER MEL 33-11-01. DISCONNECTED F/O LIGHT ASSY FRM TERMINAL STRIP FO R CIRCUIT ISOLATION. RECONNECTED F/O LIGHT ASSY TO TERMINAL STRIP. FO WIRES AT TB5100 5102 5104 SWAPPED. REWIRED PER W/D CKS GOOD PER MM. MCO/PLACARD REMOVED. 2 L 7 2 4F RT A1NM 2008032700014 20080327 00014 NM 2008 3 27 DHL2008765018 1 20080116 A 5754 STRUCTURE BOEING 727 727264 138408M NM NR 6 SLAT GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, RIGHT WING NR 6 SLAT TRAILING EDGE GOUGED AT HOOK FITTINGS WS 150 APPROXIMATE. REMOVED HOOK FITTING FRO M ACCESS IAW SRM 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 57-50-3 FIGURE 10. TREATED AND PRIMED DOUBLER AND AREA IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND 57-50-3 FIGURE 10. REINSTALLED HOOK FITTING AT RT WING NR 6 SLAT TRAILING EDGE WS 520 IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032700052 20080327 00052 NM 2008 3 27 DHL2008765016 1 20080125 A 5710 BEAM BOEING 727 727264 138408M NM LWS 124 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, LT WING UPPER TRAILING EDGE PANEL SUPPORT 'J' BEAM WBL 124 IS CRACKED IN CUT OUT FORWARD OF NR 7 SPOILER ACTUATOR. REMOVED TRAILING EDGE UPPER PANEL FROM LT WING FOR ACCESS IAW SRM 51-30-2. REMOVED CRACKED 'J' BEAM IAW SRM 51-30-2. FABRICATED NEW 'J' BEAM FROM IAW EC-00726-001 AND DRAWING NR 65-21655. INSTALLED NEW 'J' BEAM IAW SRM 51-30-2 . REINSTALLED TRAILING EDGE UPPER PANEL AT LT WING WBL 124 FORWARD OF NR 7 SPOILER ACTUATOR IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032700086 20080327 00086 WP 2008 3 27 08FDEA01081 1 20080320 A 5321 ACA3205505 FLOORBOARD DOUG MD10 MD1010F 3022112 WP BS 755 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 MAIN CABIN FLOOR PANEL AT STA 755; LBL 5 IS CRACKED. REPAIRED CRACK IAW FEDEX SRZ 25-005 REV F. 2 L 7 3 4F RT A22WE 2008032700097 20080327 00097 WP 2008 3 27 08FDEA01090 1 20080321 A 5730 ARB30272 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 307FE 48291 RT WING L/E DROPPED (REMOVED PART) FOUND WEAR ON LWR SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 39 SHT 2 VOL I. 2 L 7 3 4F RT A22WE 2008032700116 20080327 00116 SO 2008 3 27 SIMA200808106 1 20080317 A 5320 14521413605 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 683AE 9364 5000 14500833 DURING A IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 29 WAS FOUND CORRODED. REPAIRED CORRODED AREA REPAIR IAW SRM 53- 00-10 FIG 202. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032700133 20080327 00133 NM 2008 3 27 NOCA02008 1 20080320 A 2610 2156604 DETECTOR BOEING 767 76739H 1385311 NM AFT CARGO BAY MALFUNCTIONED A NOCA O OTHER N FALSE WARNING UK UNKNOWN 1 EA 15 760NA 26257 AFT CARGO DETECTOR NR 1 EICAS STATUS MSG DISPLAYED (M) REMAINING DETECTOR IS VERIFIED TO OPERATE NORMAL BEFORE EACH DEPA RTURE WITH A LOGBOOK ENTRY. EICAS MESSAGE AFT DET FAN. REMOVED AND REPLACED AFT CARGO DETECTOR PER MM 26-16-00. OPS C HECKS OK. 2 L 7 2 4F RT A1NM 2008032700157 20080327 00157 GL 2008 3 27 SIMA200808402 2 20080322 A 7261 4252070 CARBON SEAL EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 1 ENGINE WORN A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 833AE 16216 145629 CAE311137 ON FLIGHT 3900 - CREW REPORTED NUMBER 1 ENGINE OIL QUANTITY WENT FROM 11 TO 4 QTS IN LESS THAN 15 MINUTES. PERFORMED PR ECAUTIONARY SHUTDOWN. OVERWEIGHT LANDING PERFORMED 43700 LBS TOUCHDOWN OF LESS THAN 100 FPM. AIRCRAFT LANDED UNEVENTFU LLY. AIRCRAFT REMOVED FROM SERVICE. REMOVED NR 1 ANGLE GEARBOX BREATHER MAGNETIC CARBON SEAL IAW ROLLS ROYCE FIM TASK 72-00-00-810-815, REF ETN EM 79-007 R1. RESERVICED OIL WITH 14 PTS IAW AMM 79-11-01. NO DEFECTS NOTED. PASSED FCF AN D COMPLETED TRIAD EVENT AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008032700165 20080327 00165 NM 2008 3 27 2008UALA01401 1 20080313 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FORWARD ENTRY DOOR CUTOUT FORWARD SIDE INTERCOSTAL BELOW STRINGER S-13L GOUGED NEAR AFT INBOARD CORNER. MAJOR REPAIR AC COMPLISHED: REMOVED & INSTALLED INTERCOSTAL WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700171 20080327 00171 NM 2008 3 27 2008UALA01407 1 20080313 A 5320 6517684642 WEB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 BS 294.5 WEB WAS FOUND CRACKED AT STRINGER S-7L. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED WEB. INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700191 20080327 00191 NM 2008 3 27 2008UALA01426 1 20080313 A 5313 FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FUSELAGE STRINGER 10L END CLIP IS CRACKED BS 360. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED ANGLE. INSTALLED NEW REP LACEMENT ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700199 20080327 00199 WP 2008 3 27 08FDEA01100 1 20080321 A 5321 ACA3205505 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 200 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 MAIN CABIN FLOORBOARD AT RBL 48 TO 76; BS 615 TO 675 IS SOFT AND SPONGY. EVALUATED FLOOR PANEL INSTALLED INSERTS. FOU ND PANEL TO BE SOLID PER FEDEX SRZ 25-005 REV F. SDR SUBMITTED IN ERROR- ADMINISTRATOR. 2 L 7 3 4F RT A22WE 2008032700208 20080327 00208 NM 2008 3 27 08FDEA01109 1 20080322 A 5720 SHIM BOEING 727 727225 1384077 NM ZONE 100 MIGRATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 MIGRATING SHIMS AND LOOSE HARDWARE AT LWR SIDE OF NR 8 SPOILER ACTUATOR SUPPORT BEAM FITTING, WS 198. REPAIRED SUPPORT BEAM FITTING IAW DRAWING SR27-57-038 REV "C". 2 L 7 3 4F A3WE 2008032700243 20080327 00243 EU 2008 3 27 08FDEA01130 1 20080324 A 5315 A53974322224 FLOORBEAM AIRBUS 300 A300B4622 3930401 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 720FD 417 AFT CARGO FR 67 FLOOR PANEL HAS SEVERAL SPOTS OF CORROSION LBL 60 TO RBL 60, CROSS BEAM. REMOVED CROSS BEAM IAW SRM 51- 73-10 LOCATED AND DRILLED NEW CROSS BEAM IAW SRM 51-40-44. INSTALLED CROSS BEAM IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008032700256 20080327 00256 NM 2008 3 27 AALA200800489 1 20080304 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 JFK - EMERGENCY LIGHT AT SEAT 24C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700274 20080327 00274 NM 2008 3 27 AALA200800507 1 20080305 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT AT SEAT 20C HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700285 20080327 00285 NM 2008 3 27 AALA200800512 1 20080305 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT AT SEAT 31G HAS MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700286 20080327 00286 NM 2008 3 27 AALA200800513 1 20080305 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 788AN 30011 DFW - EMERGENCY LIGHT AT OVERHEAD LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700287 20080327 00287 NM 2008 3 27 AALA200800514 1 20080305 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 MIA - EMERGENCY LIGHT AT SEAT 39G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 39G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700288 20080327 00288 WP 2008 3 27 AALA200800517 1 20080305 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 289AA 49301 MSP - EMERGENCY LIGHT AT SEAT 12D HAS MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008032700292 20080327 00292 SO 2008 3 27 C2XA08RI031 1 20080317 A 3233 21180100401 ACTUATOR EMB 145 EMB145LR 3260212 SO NLG DOOR DEFECTIVE A C2XA K NONE J WARNING INDICATION LD LANDING 1 SW 27 15986 19249 145254 FLIGHT 3053 - EWR - CREW REPORTED LANDING GEAR AIR/GRND WARNING MESSAGE DURING GEAR TRANSITION TO EXTEND. EWR MX REMOVE D AND REPLACED NOSE LANDING GEAR DOOR ACTUATORS IAW EMB 145 AMM 32-30-03 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. THIS SDR WAS FILED FOR THE RIGHT HAND ACTUATOR. SDR C2XA08RI030 WAS FILED FOR THE LEFT HAND ACTUATOR. 2 L 7 2 4T RT T00011AT 2008032700306 20080327 00306 WP 2008 3 27 NWAA081149875 1 20080322 A 5420 WEB DOUG DC9 DC951 3022051 WP LT NACELLE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 784NC 48109 DURING ENGINE CHANGE, FOUND CRACKS IN LT PYLON CLOSURE WEB AT STA YN 135. REPAIRED PER EA 98-211617. 2 L 7 2 4F RT A6WE 2008032700307 20080327 00307 WP 2008 3 27 NWAA081069973 1 20080318 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9337 47346 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN LIGHT FOR THE AFT OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY EXIT SIGNS BATTERY PACK (B5-25) AND OPERATIONALLY CHECKED THE SYSTEM. THE AIRCRAFT W AS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2008032700316 20080327 00316 SO 2008 3 27 C2XA08IA081 1 20080317 A 3350 66369 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16520 145372 IAH - FLIGHT 2725, DURING MAINTENANCE INSPECTION THE 2ND AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE AFFECTED AISLE PATH LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008032700339 20080327 00339 EU 2008 3 27 NWAA081163302 1 20080323 A 3350 POWER SUPPLY AIRBUS 330 A330300 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 802NW 0533 ESCAPE SLIDE LIGHT EMERGENCY POWER SUPPLY UNIT FAILED TEST, REPLACED EPSU AND TESTED OK. 2 L 7 2 4F RT 2008032700362 20080327 00362 EU 2008 3 27 AALA200800548 1 20080310 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 MIA - EMERGENCY LIGHTS AT SEAT ROWS 1G TO 5G INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 1G TO 5G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008032700364 20080327 00364 NM 2008 3 27 AALA200800547 1 20080310 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 185AN 32379 JFK - EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 16 FOR EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008032700366 20080327 00366 NM 2008 3 27 AALA200800566 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT SEAT 41G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 41G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700368 20080327 00368 NM 2008 3 27 AALA200800568 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT SEAT 32G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700369 20080327 00369 NM 2008 3 27 AALA200800569 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT SEAT 31G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700378 20080327 00378 NM 2008 3 27 AALA200800560 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700379 20080327 00379 NM 2008 3 27 AALA200800561 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700381 20080327 00381 NM 2008 3 27 AALA200800556 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700382 20080327 00382 NM 2008 3 27 AALA200800527 1 20080308 A 3350 SHROUD BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AA 27057 DFW - EMERGENCY LIGHT AT SEAT 29D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 29D. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008032700384 20080327 00384 NM 2008 3 27 AALA200800551 1 20080310 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 929AN 30078 MIA - EMERGENCY LIGHT AT OVERHEAD SEAT 25C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT 25C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008032700387 20080327 00387 NM 2008 3 27 AALA200800535 1 20080310 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 395AN 29432 EZE - EMERGENCY LIGHTS AT SEAT ROWS 32H TO 41H INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 32H TO 41H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008032700389 20080327 00389 NM 2008 3 27 AALA200800546 1 20080310 A 3397 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 185AN 32379 JFK - EMERGENCY LIGHT AT FIRST CLASS CABIN INOPERATIVE. SECURED CONNECTOR AT BATTERY PACK FOR EMERGENCY LIGHT AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008032700390 20080327 00390 NM 2008 3 27 AALA200800537 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 MIA - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700394 20080327 00394 NM 2008 3 27 AALA200800536 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 MIA - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700395 20080327 00395 NM 2008 3 27 AALA200800554 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LEFT NUMBER ONE D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700396 20080327 00396 NM 2008 3 27 AALA200800570 1 20080310 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT SEAT 21G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700397 20080327 00397 NM 2008 3 27 AALA200800571 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT SEAT 21G MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800001 20080328 00001 NM 2008 3 28 AALA200800578 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 32C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 32C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800003 20080328 00003 NM 2008 3 28 AALA200800580 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 39C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 39C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032500230 20080325 00230 NM 2008 3 25 2008UALA01511 1 20080317 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 AFT PIT FS 1440 FRAME DENTED AT STR 25L AND 26L. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED FRAME REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500234 20080325 00234 NM 2008 3 25 2008UALA01531 1 20080318 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 119UA 28812 AFT EMERGENCY LIGHT IS BROKEN OFF FROM THE SEAT AT SEAT 3J. REPLACED LIGHT ASSY, OPS CHECK IS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032500237 20080325 00237 EU 2008 3 25 F3LA200800118 1 20080301 A 5320 D53230585200 SILL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED SURFACE CORROSION WAS FOUND ON NUT PLATE HOLES ON THE END OF THE FORWARD CARGO DOOR SILL PLATE. MAINTENANCE REMOVED THE FASTENERS, REPAIRED THE CORRODED SURFACES, BY BLENDING, IN ACCORDANCE WITH TH E REQUIREMENTS OF A319 SRM 51-74-00, PARAGRAPH 6 AND EA A9-53R-30109. FASTENERS WERE RE-INSTALLED IN ACCORDANCE WITH TH E REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE REPAIR, THE AREA WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032500238 20080325 00238 2008 3 25 F3LA200800119 4 20080229 A 2565 LANYARD AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE SLIDE BROKEN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 93FR 608 A9518 1863 REFERENCE NON ROUTINE C039690. DURING C4/S1 C CHECK, INSPECTION REPORTED THE R-2 DOOR SLIDE/RAFT ASSEMBLY BALL LANYARD BROKE LOOSE. MAINTENANCE REMOVED AND REPLACED THE SLIDE ASSEMBLY WITH A NEW UNIT IN ACCORDANCE WITH THE REQUIREMENTS OF THE WORK CARD C528001-8. UPON COMPLETION OF THE REPLACEMENT, THE UNIT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032500242 20080325 00242 2008 3 25 2008UALA01592 4 20080319 A 3460 K217ABM11 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT FAILED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 403UA 442 FLIGHT DIVERTED WITH AUTOPILOT PROBLEMS. POSSIBLE FMGC/FCU FAILURE. REPLACED FMGC/FCU COMBO. SYSTEM CHECKS NORMALLY, RESTORED TO CAT III STATUS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500245 20080325 00245 EU 2008 3 25 2008UALA01595 1 20080321 A 5297 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO DOOR DIRTY A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 441UA 751 FLIGHT DIVERTED DUE TO AFT CARGO DOOR INDICATION PROBLEM. POSSIBLE DIRTY CONNECTOR. CLEANED AND SECURED AFT CARGO INDI CATION CONNECTOR, ALL FAULTS CLEARED AND NO FURTHER DEFECTS NOTED, OPENED & CLOSED DOOR SEVERAL TIMES WITH NO DEFECTS, A FT CARGO DOOR WARNING CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500252 20080325 00252 NM 2008 3 25 2008UALA01602 1 20080320 A 5230 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 AFT CARGO DOOR 22" AFT OF RT LOWER CORNER AND 16" UP FROM BOTTOM EDGE AN INNER SHEAR TIE HAS MISDRILLED HOLE. MAJOR REP AIR ACCOMPLISHED: REPLACED T-ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500256 20080325 00256 NM 2008 3 25 2008UALA01606 1 20080320 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 853UA 1688 FUSELAGE DENTED 1" AFT OF FRAME 23, 1" BELOW STR 22L. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500263 20080325 00263 NM 2008 3 25 2008UALA01612 1 20080320 A 3350 767 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXT EMER LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 581UA 26701 DOOR 4R OUTSIDE EMERGENCY LIGHT INOP. RELAMPED EMER LIGHT AT 4R, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032400302 20080324 00302 NM 2008 3 24 2008UALA01368 1 20080312 A 2560 SPRING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EVAC SLIDE WEAK A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 NR 2L DOOR SLIDE LATCH HOOK SPRING IS WEAK AND LATCH LEVER HINGE IS WORN. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032400321 20080324 00321 NM 2008 3 24 2008UALA01373 1 20080312 A 5753 SUPPORT FITTING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE T/E FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 NR 8 FLAP SUPPORT FITTING JOINT 8V, BOTH INBOARD AND OUTBOARD END BUSHING BORE HOLE IS WORN. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032400333 20080324 00333 NM 2008 3 24 2008UALA01379 1 20080312 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 LOWER FUSELAGE SKIN HAS SCRIBE MARK AT FWD CARGO DOOR CUTOUT LOWER AFT CORNER BS 484 BETWEEN STR 25R - 25R, 3 INCH LONG MARK, .001" DEEP. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED EXTERNAL DOUBLER & FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032400339 20080324 00339 EU 2008 3 24 2008UALA01382 1 20080313 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 488UA 1680 LEFT HAND EMERGENCY LIGHTING AT OVERWING EXIT INOP. LOOSE WIRE. SECURED LOOSE WIRE, ALL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032400373 20080324 00373 NM 2008 3 24 SA08014 1 20080317 A 3350 32145410 EPSU AIRBUS A319 A319132 3930340 NM CABIN FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 832AW 54180 51 1643 LAX - EMERGENCY POWER SUPPLY UNIT, FIN 12WL, FAILED THE BITE CHECK. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT, F IN 13WL. 2 L 7 2 4F RT A28NM 2008032800006 20080328 00006 NM 2008 3 28 AALA200800583 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 41G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 41G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800008 20080328 00008 NM 2008 3 28 AALA200800585 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 31G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800011 20080328 00011 NM 2008 3 28 AALA200800588 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 44C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 44C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800013 20080328 00013 NM 2008 3 28 AALA200800590 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 22G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800017 20080328 00017 NM 2008 3 28 AALA200800524 1 20080307 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 787AL 30010 DFW - EMERGENCY LIGHT AT SEAT 22G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800018 20080328 00018 NM 2008 3 28 AALA200800559 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800020 20080328 00020 NM 2008 3 28 AALA200800540 1 20080310 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 784AN 29588 MIA - EMERGENCY LIGHT AT SEAT 39G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 39G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800022 20080328 00022 NM 2008 3 28 DHLA200800036 1 20080325 A 3097 WIRE BOEING 727 727224 1384076 NM COCKPIT DAMAGED A DHLA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 05 747DH 22253 ON GROUND BURNING ELECTRICAL SMELL IN COCKPIT AFT OF CAPTS SEAT (L-2 WINDOW WIRING) L-2 HEAT INOP. TRANSFERRED TO DEFER LOG NR 32178 IAW MEL 30-15-1 CAT C PLACARD INSTALLED DMI. REPAIRED WIRING AS PER SWPM 20-10-13 AND 727-200 WIRING DIA G 30-41-12 PG 5. SYSTEM RESTORED TO NORMAL CONFIG, AND OP'S CHKS GOOD AT THIS TIME PER MM30-41-02, THIS CLEARS DMI 3217 6 PLACARDS REMOVED, AIRCRAFT WAS GROUNDED. 2 L 7 3 4F A3WE 2008032800028 20080328 00028 EA 2008 3 28 A6WA200840110 1 20080214 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 430AW 7719 PILOTS BULKHEAD FS 280 RBL 9 FOUND CRACKED. BULKHEAD REPAIRED IAW REO 601R-53-11-171 REV D. (M) 2 L 7 2 4F RT A21EA 2008032800029 20080328 00029 EA 2008 3 28 A6WA200840111 1 20080217 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 430AW 7719 AT FS 574 TO FS 621 WL 73.50 SILL PLATE CORRODED. BLENDED SILL PLATE IAW 51-21-06 SRM. (M) 2 L 7 2 4F RT A21EA 2008032800031 20080328 00031 WP 2008 3 28 IXXA08SMN039S 1 20080201 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT EXTERNAL DOUBLER LEFT AFT FUSELAGE SIDE FORWARD OF AFT PRESS URE BULKHEAD AT STATION FS 1742, LONGERON 16.5 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING R EPAIR DOUBLER. REMOVED DAMAGE AREA. FABRICATE REPAIR DOUBLER, INTERNAL FINGER DOUBLER, FILLER CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 51-1-11, SRM 51-3-1, DC8 SRM 53-2-1 FIGURE 7 S HEETS 1, 3, 5, DC8 SRM 53-5-1 FIGURE 1 ITEM "E", DC8 SRM 51-1-21, DC8 SRM 51-1-20D, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008032800032 20080328 00032 EA 2008 3 28 A6WA200840112 1 20080217 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 430AW 7719 AT FS 574 TO FS 621 WL 73.50 LBL 30.00 PLATE CORRODED. BLENDED PLATE IAW (51-21-06) SRM. (M) 2 L 7 2 4F RT A21EA 2008032800033 20080328 00033 EA 2008 3 28 A6WA200840113 1 20080216 A 5320 SUPPORT FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 430AW 7719 SUPPORT FITTING (MACHINED PLATE) RBL 9 FS 460 CRACK. SUPPORT FITTING REPLACED IAW CRJ 200 SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2008032800037 20080328 00037 SO 2008 3 28 C2XA08CL032 1 20080317 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14905 145476 DURING ROUTINE MAINTENANCE THE AFT EMERGENCY FLOOR AISLE PATH LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008032800038 20080328 00038 SO 2008 3 28 C2XA08TY036 1 20080318 A 3350 375911 LIGHT EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14947 145054 EMERGENCY EXIT ROW OVERHEAD AFT EXIT LIGHT INOP. REPLACED EXIT LIGHT ASSY IAW EMB 145AMM 33-50-13. OPS CHECK GOOD AIRC RAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008032800048 20080328 00048 NM 2008 3 28 SWAA081527 1 20080319 A 3350 20131A BATTERY PACK BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008032800050 20080328 00050 SO 2008 3 28 C2XA08SH044 1 20080313 A 3350 30251031217 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12528 145504 SHV - DURING C-CHECK EMERGENCY LIGHT ON RIGHT FWD PNL 191 INOP. MX REMOVED AND REPLACED RIGHT FWD EMERGENCY LIGHT ASSY ON 191 PNL IAW EMB 135 AMM 33-50-10, OPS CHECK GOOD. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT T00011AT 2008032800051 20080328 00051 SO 2008 3 28 C2XA08IA084 1 20080314 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO LT MLG INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13995 145295 BTR - FLIGHT 2078, THE CREW REPORTED A BANGING NOISE FROM THE NLG AREA. MAINTENANCE INSPECTED THE AIRCRAFT AND IT WAS F ERRIED TO IAH ON 03/15/08 WHERE IT LANDED WITHOUT INCIDENT. IAH MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK PROXIMITY SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . 2 L 7 2 4T RT T00011AT 2008032800052 20080328 00052 SO 2008 3 28 C2XA08RI033 1 20080313 A 2611 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT FALSE ACTIVATION A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 22971 145149 FLIGHT 2794 - EWR - CREW REPORTED LAVATORY SMOKE MASTER WARNING. CREW PERFORMED SYSTEM RESET SUCCESSFULLY. NO MAINTENA NCE ACTION WAS NECESSARY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032800053 20080328 00053 SO 2008 3 28 C2XA08CL034 1 20080322 A 3030 CS500060D4A RELAY EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 12921 145354 CLE FLIGHT 2210 - THE CREW REPORTED SHORTLY AFTER TAKEOFF A STRONG SMELL OF ELECTRICAL BURNING IN THE COCKPIT. THE AIRC RAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE CURRENT SENSOR RELAY KOO57. O PERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008032800055 20080328 00055 SO 2008 3 28 C2XA08TY037 1 20080323 A 3230 23092900401 UPLOCK EMB 145 EMB145LR 3260212 SO RT MLG FAILED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 13964 145123 TYS FLT 2926 - AIR RETURN BACK TO TYS FOR LANDING GEAR AIR GROUND FAIL AND LANDING GEAR LEVER DISAGREE ON EICAS. THE RT MLG UPLOCK BOX WAS REMOVED AND REPLACED AND OPS CHECKED GOOD IAW EMB AMM 32-33-10. A/C WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032800056 20080328 00056 NM 2008 3 28 SWAA081530 1 20080323 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 219WN 32490 DURING SCHEDULED MV3 CHECK, FOUND EEPLS LENS MISSING AT ROW 5 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008032800059 20080328 00059 NM 2008 3 28 SWAA081569 1 20080320 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED C2 CHECK, FOUND RT WING NR 4 L/E SLAT CRACKED AT OUTBOARD T/E. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008032800061 20080328 00061 NM 2008 3 28 SWAA081567 1 20080320 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT UPPER AFT CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032800065 20080328 00065 NM 2008 3 28 SWAA081538 1 20080320 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 R2 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008032800067 20080328 00067 NM 2008 3 28 SWAA081541 1 20080323 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032800075 20080328 00075 NM 2008 3 28 SWAA081548 1 20080320 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 444WN 29839 DURING SCHEDULED MV1 CHECK, FOUND EEPLS ASSY BROKEN AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008032800076 20080328 00076 NM 2008 3 28 SWAA081549 1 20080320 A 2560 801881 LATCH BOEING 737 7375H4 138449D NM COCKPIT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 FLIGHT DECK RIGHT EMERGENCY ESCAPE ROPE DOOR LATCH INOP. REMOVED AND REPLACED LATCH PER MM. 2 L 7 2 4F RT A16WE 2008032800078 20080328 00078 NM 2008 3 28 SWAA081551 1 20080323 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 972, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032800084 20080328 00084 NM 2008 3 28 SWAA081572 1 20080323 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008032800085 20080328 00085 NM 2008 3 28 SWAA081554 1 20080322 A 3350 100031 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2008032700076 20080327 00076 SO 2008 3 27 RAIA00803012 1 20080316 A 3610 O-RING EMB 145 EMB145LR 3260212 SO BLEED AIR SYS WORN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 817HK 145058 FLT 5571 - STL - BLEED NR 2 LEAK INDICATION ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE BLEED DUCT O-RINGS AND A DJUSTED THE CLAMP ON THE DUCT. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008032700091 20080327 00091 WP 2008 3 27 08FDEA01086 1 20080320 A 5754 NRB60372 SKIN DOUG DC10 DC1010 3022110 WP NR 8 SLAT DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RT WING NR 8 SLAT LOWER EXTERIOR SKIN IS DENTED. CUT OUT DAMAGED SKIN IAW SRM 57-10-00 FIG 11 VOL I. DENT FOUND TO BE OUT OF LIMITS IAW SRM 57-10-00 FIG 41 VOL I. FABRICATED DOUBLERS, 2 SEALS, SPLICE PLATE, FILLER & 4 EACH SUPPORTS IAW SRM 57-10-00 FIG II VOL I. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. INSTALLED REPAIR IAW SRM 51-35-02 VOL II. 2 L 7 3 4F A22WE 2008032700094 20080327 00094 EA 2008 3 27 MASA200800242 1 20080319 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA LIFE VEST MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27318 7318 ASH FLT 7063 ORD-SBN, CAPTAIN'S LIFE VEST INSPECTION STICKER WAS MISSING. MX INSPECTED THE LIFE VEST AND INSTALLED A NE W INSPECTION STICKER. 2 L 7 2 4F RT A21EA 2008032700124 20080327 00124 EA 2008 3 27 MASA200800245 1 20080319 A 5220 SEAL CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT DIRTY A MASA O OTHER O OTHER CL CLIMB 1 SW 07 930LR 15030 ASH FLT 2734 PHX, LOUD SQUEAL FROM EMERGENCY EXIT 16A DURING CLIMBOUT. CLEANED AND INSPECTED EMERGENCY EXIT SEAL, NO DE FECTS NOTED. 2 L 7 2 4F RT A21EA 2008032700143 20080327 00143 NM 2008 3 27 DL76P080396 1 20080320 A 2131 CONTROLLER BOEING 767 767332 1382001 NM CABIN PRESSURE MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 143DA 25991 ON TAXI OUT STATUS CABIN ALT AUTO 2 AFTER SWITCHING TO AUTO 1 ALT AUTO 1 ANNUNCIATED. RESET AND RERACK AUTO CONTROLLERS PERFORMED BITE ON BOTH PRESS CONTROLLERS CHECKS OK NO FAULTS. 2 L 7 2 4F RT A1NM 2008032700177 20080327 00177 NM 2008 3 27 2008UALA01409 1 20080313 A 5320 SUPPORT FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FUSELAGE STRINGER 13L SUPPORT CLIP FOR INTERCOSTAL IS CRACKED BS 303.5. MAJOR REPAIR ACCOMPLISHED: REPAIR CONSISTS OF NEW H-STRAP, .063" FRAME DOUBLER, 2 FABRICATED CLIPS & 1 FABRICATED ANGLE & 2 ANGLES REPLACED. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700203 20080327 00203 NM 2008 3 27 08FDEA01106 1 20080322 A 5315 BAC1505100617 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 MAIN CARGO COMPARTMENT, FLOORBEAM CORRODED BETWEEN BL 0 BL 25L, BS 950D. CUT OUT DAMAGE IAW SRM 53-10-3 FIG 3 & SRM ER- 01-049 REV E. FABRICATED SECTION, SUPPORT ANGLES AND REINFORCEMENT STRAPS IAW SRM 53-10-3 FIG 3 TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032700205 20080327 00205 NM 2008 3 27 2008UALA01475 1 20080315 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FWD PIT, LEFT SIDE STA 660 BETWEEN STR 25 AND 26L, MAIN FRAME HAS DENT INTO RADIUS UPPER BEND. ACCOMPLISHED A MAJOR REP AIR AT ORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032700242 20080327 00242 NM 2008 3 27 2008UALA01494 1 20080317 A 5753 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT FOREFLAP PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 FOUND PUNCTURE IN RT INBOARD TRAILING EDGE FORE FLAP UPPER SURFACE. PREVIOUS REPAIR DISBONDED AND TORN. HOLE IS .5 IN X .25 IN, LOCATION IS 4.5 FEET O/B 7.5 IN FROM TRAILING EDGE. FOUND PUNCTURE IN RT INBOARD TRAILING EDGE FORE FLAP UPPE R SURFACE. REMOVED RT INBD FOREFLAP. RECEIVED & INSTALLED NEW FOREFLAP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700266 20080327 00266 NM 2008 3 27 AALA200800497 1 20080304 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 395AN 29432 MIA - EMERGENCY LIGHTS AT SEAT 20B TO 24B INOPERATIVE. REPLACED BATTERY PACK AT M737 FOR EMERGENCY LIGHTS AT SEAT 20B T O 24B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008032700281 20080327 00281 NM 2008 3 27 AALA200800515 1 20080305 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 MIA - EMERGENCY LIGHT AT SEAT 21G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700319 20080327 00319 SO 2008 3 27 C2XA08CL035 1 20080323 A 3350 744412 SIGN EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18982 145223 DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT SIGN IN FRONT OF ROW 3 BC WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPL ACED THE EMERGENCY EXIT SIGN. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008032700332 20080327 00332 WP 2008 3 27 08FDEA01137 1 20080325 A 5753 ARC0503502 HINGE BRACKET DOUG DC10 DC1010 3022110 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION FOUND RT OUTBOARD FLAP, OUTBOARD HINGE WITH RUT AND CORROSION. REPLACED BRACKET ASSY OUT F LAP FOR DWG ARC0503-502 2 L 7 3 4F A22WE 2008032700348 20080327 00348 NM 2008 3 27 HALA0800422 1 20080322 A 4990 O-RING BOEING 767 7673G5 1385126 NM APU PINCHED A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, EVIDENCE OF OIL LEAK BELOW APU. FOUND APU CAP O-RING PINCHED. REMOVED AND REPLACED O-RING. LEAK CK OK. SERVICED 1 PINT OF OIL. 2 L 7 2 4F RT A1NM 2008032700388 20080327 00388 NM 2008 3 27 AALA200800549 1 20080310 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 929AN 30078 MIA - EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHTS AT SEAT 24D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008032800002 20080328 00002 NM 2008 3 28 AALA200800579 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 35C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 35C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032400379 20080324 00379 NM 2008 3 24 SWAA081427 1 20080316 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 285WN 32536 EEPLS ASSY LOOSE AT ROW 1 ABC. SECURED EEPLS ASSY PER MM. 2 L 7 2 4F RT A16WE 2008032400425 20080324 00425 NM 2008 3 24 SWAA081452 1 20080316 A 3350 65C27028 LIGHT BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 BULLNOSE EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 22 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008032500008 20080325 00008 2008 3 25 DXTA20082888 4 20080218 A 2210 TRIM SYSTEM BEECH MU300 400A 1155402 CE AUTOPILOT PITCH MALFUNCTIONED E DXTA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 07 122QS RK467 LT AND RT AP TRIM PITCH TRIM FAIL LIGHTS ON TRIM INDICATIONS WERE FINE, BUT NOSE DOWN PITCH WHEN AP DISENGAGED. INSPECT ED PITCH TRIM SERVO, VERIFIED NO DEFECTS. PERFORMED PITCH TRIM SERVO SPIN UP TEST WITH NO DEFECTS NOTED. SYSTEM OPERATES NORMAL IAW SRM PUB NR 523-0775807. 2 H 7 2 4F RT A16SW 2008032500032 20080325 00032 SW 2008 3 25 AC2A118979 1 20080302 A 6200 430010122101 STOP BELL 430 430 1182150 SW ALLSN 250C 250C40B 03032 NE CRACKED E AC2A K NONE O OTHER IN INSP/MAINT 1 SW 31 430CT 49089 STOP CRACKED IN RADIUS. 1 G 7 2 3U 3 U RT H9SW E1GL 2008032500062 20080325 00062 CE 2008 3 25 DJFA2008024 1 20080303 A 5511 45A21104642 RIB BEECH MU300 400A 1155402 CE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 459LX 3268 745 RK365 DURING A SCHEDULED MAINT VISIT, WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB RIB WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED INCOMMUNI QUE' NR 70. MAINT INSTALLED NEW BRACKET ASSEMBLIES ON BOTH SIDES. 2 H 7 2 4F RT A16SW 2008032500067 20080325 00067 NM 2008 3 25 USAA920080639 1 20080312 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER CLIP, BS 639, S4L. REPLACED STRINGER CLIP, BS 639, S4L IAW B737 SRM 5 1-40-02. 2 L 7 2 4F RT A16WE 2008032500072 20080325 00072 NM 2008 3 25 USAA920080642 1 20080308 A 5320 143N51528200 FITTING BOEING 757 7572G7 1384963 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 908AW 24233 MCN - MAJOR REPAIR - C3 CHECK , CRACKED CLIP, BS 860 - BS 880, BL 0. REPLACED CLIP, BS 860 - BS 880, BL 0 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008032500077 20080325 00077 WP 2008 3 25 AMTA200800188 1 20080228 A 3397 WIRE DOUG DC10 DC1030 3023501 WP EMERGENCY LIGHTS BROKEN A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 701TZ 46583 BOTH RED FLOOR PROX LIGHT AT 37R ARE INOPERATIVE. RELAMPED AND REPAIRED BROKEN WIRES IAW WIRING PRACTICE MANUAL AND AMM CHAP 33-50-00. CHECKS GOOD. OK FOR SERVICE. (K) 2 L 7 3 4F A22WE 2008032500108 20080325 00108 CE 2008 3 25 DXTA20082948 1 20080318 A 3241 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG WEAK E DXTA O OTHER O OTHER LD LANDING 1 GL 07 391QS 5600493 RT PILOT BRAKES ARE SOFT (NOTE APPROX 75 PERCENT TRAVEL BEFORE BRAKING IS FELT. PERFORMED THE ANTI-SKID BRAKE SYSTEM BL EEDING PROCEDURE IAW THE CESSNA MM CHAPTER 32-42-00. OPERATIONAL CHECK OF AIRCRAFT BRAKING SYSTEM SATISFACTORY. 2 L 7 2 4F 4 F RT A22CE E25EA 2008032500134 20080325 00134 NM 2008 3 25 SWAA081484 1 20080318 A 3350 311500 LENS BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 BULLNOSE EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008032500152 20080325 00152 NM 2008 3 25 SWAA081504 1 20080318 A 5311 65C25230 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727E, STR 27L TO 27R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032500163 20080325 00163 NM 2008 3 25 SWAA081514 1 20080318 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 763SW 27877 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 41 TO RBL 39. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2008032500177 20080325 00177 NM 2008 3 25 HNAA0800107 1 20080319 A 3350 1013073 PIN DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 827EX 32690 32690 390 FIRST 4 RED FLOOR EMERGENCY LIGHTS BURNED OUT AT ROW 1. RE-SECURED PIN FOR THE FEMALE PART OF THE CONNECTOR UNDER FLOOR FOR THE FIRST 4 RED FLOOR EMERGENCY LIGHTS, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2008032500197 20080325 00197 NM 2008 3 25 2008UALA01398 1 20080311 A 2781 851801 SENSOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 1 SLAT ACTIVATED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 676UA 30028 A/C EXPERIENCING L/E FLAP ASSYM FAULT MESSAGES. REPLACED NR 1 SLAT INBD SENSOR RAN FLAPS THROUGH FULL CYCLE SEVERAL TIM ES, NO FAULTS OPS CK NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032500209 20080325 00209 NM 2008 3 25 2008UALA01445 1 20080315 A 5320 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 808UA 804 BEAM #145 IS CORRODED. MAJOR REPAIR ACCOMPLISHED AT DEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500218 20080325 00218 NM 2008 3 25 2008UALA01454 1 20080315 A 5320 PLATE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 808UA 804 DOOR 2R SILL PLATE AT GIRT BAR FITTING HAS CORROSION. ACCOMPLISHED MAJOR REPAIR AT DEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500258 20080325 00258 NM 2008 3 25 2008UALA01607 1 20080320 A 5411 PIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 NR 1 PYLON, LT MIDSPAR FUSE PIN HAS CRACK INDICATIONS IN INSIDE DIAMETER. MAJOR REPAIR ACCOMPLISHED: MIDSPAR FUSE PIN IS REPLACED WITH NEW PIN (P/N 311N5500-1). 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500268 20080325 00268 2008 3 25 2008UALA01617 4 20080321 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 417UA 483 WHILE ACCOMPLISHING TEST OF EMERGENCY LIGHTING SYSTEM, HAVING FAULT MESSAGE EPSU EXT LOAD AFT LEFT. INTERNAL ELECTRICAL FAILURE IN SLIDE 2L. REPLACED SLIDE 2L WITH BORROWED PART. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500271 20080325 00271 NM 2008 3 25 2008UALA01536 1 20080316 A 3510 OXYGEN SYSTEM BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CREW O2 LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 225UA 30554 CREW OXYGEN LOW CREW PRESSURE IS LOW. CREW COMMENTS: CONTINUOUS SLOW LEAK. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500276 20080325 00276 NM 2008 3 25 2008UALA01523 1 20080318 A 5210 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FORWARD ENTRY DOOR UPPER HINGE CUTOUT HAS 2 EA CRACKS IN FASTENER HOLES AT BS 310 AND STRINGER S-10L. MAJOR REPAIR ACCO MPLISHED BY REMOVING DAMAGE AND INSTALLING STRUCTURAL FILLER AND REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500279 20080325 00279 NM 2008 3 25 2008UALA01519 1 20080318 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 UPPER FUSELAGE EXTERNAL SKIN HAS NUMEROUS DENTS IN THE AREA FROM BS 727B +6" TO 727D +12" AND FROM LBL 13 - RBL 23. MA JOR REPAIR ACCOMPLISHED: REMOVED DAMAGE WHICH INCLUDED PREVIOUS SCRIBES ADJACENT TO STRINGER S4R & ACP NDT. FABRICATED & INSTALLED DOUBLER,TRIPLER,FILLERS AND INTERNAL TEAR STRAPS REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500280 20080325 00280 NM 2008 3 25 2008UALA01518 1 20080317 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 797UA 26924 SEAT 1E ONE EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSY & CHECK OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500281 20080325 00281 NM 2008 3 25 2008UALA01517 1 20080317 A 4920 APU BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE UNKNOWN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 666UA 29238 APU WILL NOT START. AFTER EXTENSIVE TEST, REPLACED APU PER MM 49-11- 01 PG401.PERFORMED APU TEST PER JRH 2-6-15 AND PER UNIMATIC DISPLAY 2450 PERFORMANCE CHECK GOOD. VERIFICATION FLIGHT ACCOMPLISHED. APU STARTED NORMALLY. AC OK FOR SERVICE . 2 L 7 2 4F 4 F RT A1NM E24NE 2008032500282 20080325 00282 NM 2008 3 25 2008UALA01516 1 20080317 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 562UA 26664 EXTERIOR EMERGENCY LIGHT AT DOOR 1L INOP. LAMP IS OUT. RELAMPED DOOR 1L, OPS CHECKED OK. FOUND LAMP OUT. RELAMPED DO OR 1L, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500289 20080325 00289 NM 2008 3 25 2008UALA01469 1 20080316 A 4920 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU DIRTY A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION IN INSP/MAINT 1 WP 29 597UA 28750 APU FAILED TO START. FAULT LIGHT ILLUM AND EICAS MSG. APU FAULT DISPLAYED. ADDITIONAL START ATTEMPTS UNSUCCESSFUL. C LEANED LOW PRESSURE SWITCH, CHECKED OIL LEVEL, OK, APU STARTED 1ST ATTEMPT, NO REPEAT ISSUES. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500292 20080325 00292 NM 2008 3 25 2008UALA01466 1 20080316 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FWD GALLEY DOOR FWD FRAME LOWER CORNER 2 EACH O/B FASTENER HOLES CRACKED. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED L OWER FWD FRAME SECTION & INSTALLED NEW FRAME REPAIR KIT. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032600002 20080326 00002 2008 3 26 HALA0800401 4 20080312 A 3442 066500080406 DRIVE UNIT BOEING 717 717200 1383700 NM WEATHER RADAR MALFUNCTIONED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 478HA 16876 16876 55123 WRX FAIL TEST. REMOVED AND REPLACED WXR ANT DRIVE UNIT PER 34-41-07 AND REMOVED AND REPLACED WXR T/R PER MM 34-41-01, O PS CK OKAY FOR SERVICE. 2 L 7 2 4F TR A6WE 2008032600008 20080326 00008 NM 2008 3 26 HALA0800408 1 20080314 A 5754 WEDGE BOEING 767 767332 1382001 NM L/E SLAT DELAMINATED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 DELAMINATION ON SLAT POSITION 12 T/E WEDGE, 3 AREAS ON LOWER CLOSURE PANEL INBD END SLAT. REPAIRED PER SRM 57-43-02 AND 51-70-10. 2 L 7 2 4F RT A1NM 2008032600009 20080326 00009 NM 2008 3 26 HALA0800409 1 20080313 A 5420 CHANNEL BOEING 767 767332 1382001 NM LT FAIRING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 LT STRUT AFT FAIRING CHANNEL, INBD CRACKED AT FWD END. I/B AFT FAIRING CHANNEL PT NR 313T1380-243. REPLACED IAW SRM 51 -40-02, REV 76. 2 L 7 2 4F RT A1NM 2008032600014 20080326 00014 NE 2008 3 26 HALA0800399 2 20080312 A 7230 BLADE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE NICKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, SMALL NICK FOUND ON NR 1 ENG ON NR 7 FAN BLADE APPROX 5 INCHES FROM BLADE ROOT AREA C. REPAIR ED FAN BLADE BY BLENDING AND PERFORMING FPI PER MM 72-31-02-308-003-N00. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032600017 20080326 00017 SO 2008 3 26 LR7A08045 1 20080227 A 2140 3710142 DUCT LKHEED 382 382G 526414U SO CARGO BAY CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 2299 5025 DURING SCHEDULED C-7 CHECK, PER JOB CARD HC5314, FOUND CARGO FLOOR HEATING DUCT ASSY P/N 371014-2 CRACKED AT FS 497-517. REPAIR ACCOMPLISHED IAW LAC MEA 382-21-08-010. 2 H 7 4 4T A1SO 2008032600020 20080326 00020 EU 2008 3 26 F3LA200800123 1 20080302 A 5320 D53112199203000 SCUFF PLATE AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE R-1 DOOR FITTING (PN D531219820105) AND SCUFF PLATE (PN D53112199203000). MAINTENANCE REMOVED AND REPLACED THE SCUFF PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53 R-30133 AND AMM 52-15-15. THE DOOR FITTING WAS REWORKED IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-74-00, PARAG RAPH 6. FOLLOWING COMPLETION OF THE MAINTENANCE ACTION, THE AREA WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008032600022 20080326 00022 EU 2008 3 26 F3LA200800125 1 20080315 A 5321 D5367161500000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED A PUNCTURE WAS FOUND IN FLOOR PANEL 241EF. MAINTENANCE REPAIRED THE DAMAGED P ANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, PAGE 205, A319 SRM 52-02-00, PAGE 206, PARAGRAPH 201 AND A319 SRM 53-02-00. FOLLOWING COMPLETION OF THE REPAIR, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032600024 20080326 00024 NM 2008 3 26 F3LA20080017 1 20080314 A 5210 D5211200300000 SKIN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE L1 DOOR DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 923FR 13563 611 2258 FOLLOWING CONTACT OF THE JET BRIDGE WITH THE L-1 DOOR, INSPECTION, DURING THE DAILY CHECK, REPORTED DAMAGE WAS FOUND TO THE LOWER, FORWARD CORNER OF THE DOOR SKIN. MAINTENANCE REPAIRED THE FORWARD LOWER CORNER OF THE L-1 DOOR IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-52R-30107 AND SRM 51-42-11. FOLLOWING COMPLETION OF THE REPAIR, THE DOOR WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032600031 20080326 00031 NM 2008 3 26 DHL2008752512 1 20080208 A 5720 ANGLE BOEING 727 727223 1384074 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 RT WING I/B L/E AREA AT FSS 107.2 FWD WING SPAR TERMINAL JOINT ANGLE CRACK AT BOTTOM. STOP DRILLED CRACK DIM .250 IAW B 727 SRM 51-10-1 HFEC VERIFIED THAT CRACK END ON STOP DRILL HOLE IAW B727 NDTM PT6 51-00-00 FIG 23. FABRICATED NEW ANGLE USING 7075-T6 .063 PO NR 9006027 DIM 11" BY 21/4" IAW B727 SRM 51-20-1, 51-30-5 AND 57-10-2 FIG 3. INSTALLED NEW ANGLE IAW B727 SRM 51-30-2 AND 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2008032600032 20080326 00032 NM 2008 3 26 DHL2008752513 1 20080203 A 5320 6518636378 ANGLE BOEING 727 727223 1384074 NM RT MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 CRACK AT RT MLG WHEEL WELL STATION 870 FWD INBD LWR BULKHEAD 18: LEFT OF LOAD CONTROL VALVE 8 INCHES RIGHT OF CENTER. R EMOVED AND REPLACED ANGLE AT RT MLG W/W STA 870 FWD I/B LOWER BULKHEAD IAWB727SRM 51-30-2. 2 L 7 3 4F A3WE 2008032600040 20080326 00040 WP 2008 3 26 08FDEA00999 1 20080317 A 5280 ARC2859511 DOOR DOUG MD10 MD1010F 3022112 WP LT MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LT MLG STRUT DOOR LOWER CORNER HAS CORROSION. DOOR WAS REPLACED & ALL WORK WAS ACCOMPLISHED ON W/C N00122. 2 L 7 3 4F RT A22WE 2008032600046 20080326 00046 EU 2008 3 26 08FDEA01007 1 20080317 A 5730 PAINT AIRBUS 310 A310203 3930313 EU RT WING PEELING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 PANEL 613 JR RT WING LEADING EDGE HAS PEELING PAINT. REMOVED DAMAGE; MATERIAL ID; CLEANED & PREPPED FOR REPAIR. FILLE D DAMAGED AREAS; CURED; SANDED & APPLIED FOIL REPAIR. ALODINED, PRIMED & RESTORED FINISH IAW SRM 57-41-12 & SRM 51- 75-10 PARA 5-A (5) & 5-C. INSTALLED IAW SRM 51-40-21; PG 7. MINOR REPAIR 2 L 7 2 4F RT A35EU 2008032600047 20080326 00047 NM 2008 3 26 08FDEA01008 1 20080318 A 5312 AJC705070 STIFFENER DOUG MD11 MD11F 3023600 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 580FE 48471 AFT PRESSURE BULKHEAD BS 2007 AFT SIDE VERTICAL STIFFENER AT X = -10, FOUND 1/4 INCH CRACKED AT TOP CORNER AREA. COMPLIE D WITH EA 1-5310-112588 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032600048 20080326 00048 NM 2008 3 26 08FDEA01009 1 20080318 A 5753 ARC2512504 HINGE FITTING DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 521FE 48478 RIGHT WING, INBOARD FLAP AFT HINGE AFT INBOARD FASTENER HOLE FOUND CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750 -116428. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032600063 20080326 00063 EU 2008 3 26 08FDEA01016 1 20080318 A 5347 A5383202020400 SEAT TRACK AIRBUS 300 A300B4622 3930401 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 720FD 39140 417 MAIN DECK ZONE 221, FORWARD CABIN SEAT TRACK 37.5 LBL HAS STRUCTURAL DAMAGE (HEAVY CORROSION EXFOLIATED) BETWEEN FR 15A THRU FR 19. REMOVED SEAT TRACK IAW SRM 51-40-21, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-44. INSTALLED NEW SEAT TRACK IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008032600064 20080326 00064 EU 2008 3 26 08FDEA01017 1 20080318 A 5330 A53778180202 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND AN OLD FLUSH REPAIR AT C35, P34-35RH, WHICH IS NOT COMPATIBLE WITH P TO F CONVERSION REPAIR RENEWED (EXTERNAL DO UBLER INSTALLED) IAW. SRM 53-10-12 FIG.225 AND 53-10-14 FIG.201A, APPROVED BY RAS/EFW/9000022/2008 AND EA 6-5314-11713 7 2 L 7 2 4F RT A35EU 2008032600065 20080326 00065 EU 2008 3 26 08FDEA01018 1 20080318 A 5320 A53974219220 CROSSBEAM AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CORROSION AT CROSS BEAM C 63 SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 2008032600070 20080326 00070 WP 2008 3 26 08FDEA01024 1 20080318 A 5712 RIB DOUG MD10 MD1010F 3022112 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LT WING L/E INTERNAL RIB UPPER AFT EDGE IS CRACKED OUTBD OF NR 12 SLAT TRACK. INSTALLED REPAIR ARB-4352-35, PO 612903. 1 IAW SRM 57-20-00 FIG 1 VOL I & 53-33-01 VOL II. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008032600071 20080326 00071 WP 2008 3 26 08FDEA01025 1 20080318 A 5730 ARC0822501 PANEL DOUG MD10 MD1010F 3022112 WP LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LT WING T/E UPPER SURFACED FIXED PANEL LOWER SURFACE SKIN HAS CORROSION AND DELAMINATION JUST ABOVE THE OUTBD FLAP TRACK . REPAIRED IAW DWG ARC0822, TPS 1001 REV E & EA 8-5710-7-116966. 2 L 7 3 4F RT A22WE 2008032600072 20080326 00072 WP 2008 3 26 08FDEA01026 1 20080318 A 5340 ATTACH BRACKET DOUG MD10 MD1010F 3022112 WP NLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 NOSE LANDING GEAR RT LANDING LIGHT SUPPORT/ATTACH BRACKET IS CRACKED AT THE LOWER EDGE. REMOVED CRACKED BRACKET LOCATIO N AND DRILLED THE NEW BRACKET. INSTALLED NEW BRACKET REF SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 2008032600080 20080326 00080 NM 2008 3 26 DL76S080362 1 20080313 A 4920 331200 APU BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE MALFUNCTIONED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 136DL 25136 23146 P1828 SMOKE DETECTORS AT STATIONS 214-215-219 SOUNDED DUE TO LIGHT OIL MIST IN THE CABIN, ALL 3 MID LAVS. THIS HAPPENS ONLY O N THE GROUND WITH APU AIR AND NO ENGS RUNNING. FWD APU TO MCO AND PLACARD PER MEL 49-11-01A. REPLACED APU PER M/M. LE AK CKS GOOD. GENERATOR CKS GOOD. 2 L 7 2 4F 4 F RT A1NM E13NE 2008032600096 20080326 00096 2008 3 26 DL76G080375 4 20080313 A 2565 CHARGER BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1612T 30575 LT AND RT EMERGENCY EXIT SQUIB TEST DOES NOT WORK ON TEST 1 OR TEST 2. DISARMED OFFWING ZSCOPE SYSTEM IAW B767-300 AMM 25-65-00. REMOVED AND REPLACED M961 BATTERY CHARGER IAW B767-300 AMM 25-65-17. RE-ARMED OFFWING ESCAPE SYSTEM IAW B767 -300 AMM 25-65-00. OFFWING ESCAPE SYSTEM SQUIB TEST OK IAW B767-300 AMM 25-65-00-442-010-001 SUB TASK 732-017-001. 2 L 7 2 4F RT A1NM 2008032600112 20080326 00112 NM 2008 3 26 2008UALA01555 1 20080318 A 3350 1012701 SIGN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY EXIT SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 577UA 26693 LAST EXIT SIGN IN FIRST CLASS INOP. FOUND SHORT IN SIGN. REPLACED EMER EXIT SIGN, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500015 20080325 00015 CE 2008 3 25 DXTA20082895 1 20080222 A 3260 DOWNLOCK SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP MLG LOOSE E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 840QS 258340 1ST APPCH, NOSE GEAR LIGHT DID NOT COME ON BUT TESTED GOOD, CYCLED (3) TIMES AND NO POSTIVE DOOR LIGHT. JACKED AC AND CY CLED (5) TIMES WITH NO DEFECTS NOTED. INSPECTED WIRING, SWITCHES AND RESECURED A LOOSE BACK SHELL ON DOOR DOWNLOCK SWIT CH WITH SAFETY WIRE. FROZE SWITCHES AND PERFORMED GEAR SWINGS, NO DEFECTS NOTED. CLEANED SWITCHES AND LUBED STAY. AL L WORK DONE IAW MM 32-60-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2008032500027 20080325 00027 NM 2008 3 25 2008UALA01363 1 20080312 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY EXIT LIGHT INOP AT DOOR 3 RIGHT BUSSLE. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032500028 20080325 00028 CE 2008 3 25 DXTA20082903 1 20080228 A 4900 APU CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL APU BAY OVERSERVICED E DXTA A UNSCHED LANDING W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 982QS 7500182 ON TAKEOFF, COCKPIT AND CABIN BEGAN FILLING WITH SMOKE. AN IMMEDIATE RETURN FOR LANDING WAS ACCOMPLISHED. FOUND APU OVE R SERVICED AND REMOVED EXCESS OIL. INSPECTED ENGINE AND AIRFRAME. INSPECTED BOTH WATER SEPARATOR AND CLEANED. OPERATI ONAL AND LEAK CHECKED GOOD. WORK DONE IAW AMM 21-11-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032500031 20080325 00031 CE 2008 3 25 020108N509CS1 1 20080130 A 3297 664810410 WIRE HARNESS CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG DAMAGED E Z5FA O OTHER J WARNING INDICATION CL CLIMB 1 EA 63 509CS 5356 5605310 DURING TAKEOFF ROLL, CREW NOTICED ANTI-SKID INOP ANNUNCIATION. CREW CONTINUED TAKEOFF AND RETURNED TO AIRPORT. AFTER LA NDING CREW REPORTED DAMAGE TO TIRE, WHEEL, WHEEL WELL AREA AND FLAP. AC CURRENTLY IN MAINT. MAINT FOUND ANTI SKID DISCR EPANCY TO BE CAUSED BY DAMAGED LANDING GEAR WIRE BUNDLE ASSY. WIRE BUNDLE WAS REPLACED AND DAMAGED FLAP WAS REPLACED AND RT MAIN TIRE WAS REPLACED. A PORTION OF OB LOWER WING SKIN WAS REPAIRED AND IB LOWER WING SKIN WAS REPLACED. AC RETURN ED TO SERVICE. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500041 20080325 00041 CE 2008 3 25 GLBA20061079 1 20080304 A 3097 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE WINDSHIELD DEICE DETACHED A GLBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 211GL UE211 SMOKE/FUMES, FLIGHT 5061 AIR RETURN, PILOTS REPORTED THAT WHILE CLIMBING THROUGH 21.5 FOR 240 THEY NOTICED AN ELECTRICAL FUME ODOR. PILOTS PERFORMED WINDSHILED FAULT EMERGENCY CHECKLIST. TURNING OFF WINSHIELD ANTI-ICE GOT RID OF THE FUMES. MAINT SECURED A LOOSE POWER WIRE AT THE CONNECTOR FOR THE CAPTAINS WINDSHIELD DE-ICE SYS. OPS TEST WAS GOOD MM 56-10. 2 L 7 2 4T 4 T RT A24CE E26NE 2008032500065 20080325 00065 NM 2008 3 25 USAA920080637 1 20080312 A 5340 69414372 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER CLIP, BS 663.75, S10L AND S10R. REPLACED STRINGER CLIP, BS 663.75, S1 0L AND S10R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008032500084 20080325 00084 CE 2008 3 25 DXTA20082939 1 20080314 A 3230 66187161 PCB CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE INOPERATIVE E DXTA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 GL 07 814QS 191 5600776 LANDING GEAR DID NOT EXTEND WHEN GEAR HANDLE WAS PUT DOWN. REPLACED PCB NZ014 PER CE560 ENCORE & MM 24-51-01, REPLACED LANDING GEAR CONTROL HANDLE ASSY. PER CE560 ENCORE & MM 32-31-01. FUNCTIONAL CHECKED GOOD PER 560 ENCORE & MM 32-01-00. 2 L 7 2 4F 4 F RT A22CE E00053EN 2008032500086 20080325 00086 CE 2008 3 25 DXTA20082941 1 20080315 A 3233 99125373 ACTUATOR CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE MLG FALSE INDICATION E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 643QS 1908 5605588 LANDING GEAR IND UNSAFE (LEFTSIDE- NOGREEN- RED UNLOCK ON). INSTALLED REPAIRED LT MAIN LANDING GEAR ACTUATOR, PERFORMED CAMBER CHECK, SLOW CYCLE GEAR AND PURGED AIR FROM SYSTEM, SERVICED EMERGENCY AIR BOTTLE, CYCLED GEAR NUMEROUR TIMES, OP S CHECK GOOD. REF FESSNA MM 32-30-04, 32-10-00, & 32-01-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032500091 20080325 00091 CE 2008 3 25 031308N338CS1 1 20080313 A 3233 15478006 ACTUATOR CESSNA 500 550 2076604 CE PWA 530 PW530A NE MLG INTERMITTENT E Z5FA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 63 338CS 822 5501084 ON APPROACH, CREW REPORTED RT MAIN GEAR DOWN INDICATOR LIGHT FAILED TO ILLUMINATE. CREW FOLLOWED CHECKLIST AND WAS UNABL E TO RESOLVE PROBLEM. CREW ELECTED TO DIVERT. APPROACH WAS ABORTED; ON APPROACH INTO CREW BLEW GEAR DOWN AND DECLARED AN EMERGENCY. PRIOR TO LANDING, GEAR DOWN LIGHT CAME ON, AC LANDED AND SHORTLY AFTERWARDS, LIGHT WENT OUT AGAIN. CREW PULL ED OFF RUNWAY, STOPPED AND SHUTDOWN AND HAD AC TOWED TO FBO WITHOUT INCIDENT. MAINT STAFF FOUND RT MAIN INTERNAL GEAR DO WN SWITCH DEFECTIVE. GEAR ACTUATOR REPLACED AND OPS CHECKED SATISFACTORY. AC RETURNED TO SERVICE. 1 L 7 2 4F 4 F A22CE E00053EN 2008032500129 20080325 00129 NM 2008 3 25 SWAA081479 1 20080318 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008032500194 20080325 00194 NM 2008 3 25 2008UALA01395 1 20080312 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 775UA 26947 AFT EMERGENCY LIGHT INOP AT SEAT 2F. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500199 20080325 00199 NM 2008 3 25 2008UALA01391 1 20080312 A 3350 58731 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 531UA 25042 EEL LIGHT AT SEAT 5AB INOP. UNKNOWN DAMAGE. REMOVED AND REPLACED A SECTION OF EEL AT 5ABC, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500210 20080325 00210 NM 2008 3 25 2008UALA01446 1 20080315 A 5320 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 808UA 804 BEAM 150 IS CORRODED. MAJOR REPAIR ACCOMPLISHED AT DEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500284 20080325 00284 NM 2008 3 25 2008UALA01474 1 20080315 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 FORWARD PIT, LT SIDE, STA 580 BETWEEN STR 24L AND 25L, MAIN FRAME IS DENTED 3 PLACES, WITH ONE INTO FRAME UPPER RADIUS B END. ACCOMPLISHED MAJOR REPAIR AT ORD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500291 20080325 00291 2008 3 25 2008UALA01467 4 20080316 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 585UA 26709 THE 1R SLIDE HAS LANYARD HANGING DOWN. STOWED LANYARD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500298 20080325 00298 NM 2008 3 25 DHL2008752501 1 20080204 A 5754 STRUCTURE BOEING 727 727223 1384074 NM NR 5 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 RT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/ B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL USED 2024T3 .063 PO NR 9006288 DIMENSION 7 INCH BY 8.5 INCH IAW SRM 57-30-4 FIG 11 AND SRM 57-30-2 FIG3. TREA TED AND PRIMED DOUBLER REPAIR AND AREA IAW SRM 51-10-2. INSTALLED NEW DOUBLER REPAIR AND REINSTALLED FASTENERS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032500299 20080325 00299 NM 2008 3 25 DHL2008752502 1 20080204 A 5754 STRUCTURE BOEING 727 727223 1384074 NM NR 5 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 RT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/ B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT L/E SLAT MATERIAL USED 2024T3 .063 PO NR 9006288 DIMENSION 7 INCH BY 8.5 INCH IAW SRM 57-30-4 FIG 11 AND SRM 57-30-2 FIG 3. TRE ATED AND PRIMED DOUBLER REPAIR AND AREA IAW SRM 51-10-2. INSTALLED NEW DOUBLER REPAIR AND REINSTALLED FASTENERS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032500300 20080325 00300 NM 2008 3 25 DHL2008752503 1 20080204 A 5754 STRUCTURE BOEING 727 727223 1384074 NM NR 5 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 RT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/ B BULK SEAL IAW SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AT NR 5 L/E SLAT MATERIAL USED 2024T3 .063 PO NR 9006288 DIMENSION 7 INCH BY 8.5 INCH IAW SRM 57-30-4 FIG 11 AND SRM 57-30-2 FIG3. TREATED AND PRIMED DOUBLER REPAIR AND AREA IAW SRM 51-10-2. INSTALLED NEW DOUBLER REPAIR AND REINSTALLED FASTENERS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032500301 20080325 00301 NM 2008 3 25 DHL2008752504 1 20080204 A 5260 WEB BOEING 727 727223 1384074 NM AIRSTAIR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 LT SIDE OF AIRSTAIR WEB CRACKED AT LIGHTING HOLE BS 1223. CUTOUT DAMAGED AREA AT LT SIDE OF AIRSTAIR WEB SAT 1223 IAW S RM 51-40-2 FIG 1. FABRICATED DOUBLER MAT USED 7075T6 0.032 DIMENSION 2.5 INCH BY 2.5 INCH PO NR 9006457 IAW SRM 51-40-2 FIG 1 AND SRM 53-10-2 FIG 6. TREATED AND PRIMED AREA IAW SRM 51-10-2. INSTALLED DOUBLER REPAIR AT LT SIDE OF AIRSTAIR WEB STA 1223 IAW SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2008032600001 20080326 00001 WP 2008 3 26 08FDEA01010 1 20080318 A 5510 363GL ACCESS PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 EMPENNAGE, LT INLET DUCT ACCESS PANEL 363 GL IS DENTED REPAIRED DENT DAMAGES ON LT LOWER VERT STAB FAIRING PNL 363 GL BY REMOVING DAMAGED AREAS, HOT BONDING SKIN PLUGS, DOUBLERS, AND FILL AND FAIR, AND REFINISHING IAW DC/MD-10 SRMS 55-33-01 VOL III, 51-71- 00 VOL II AND DAC DWG AJC 7074 PANEL REMOVED AND REINSTALLED IAW MD/DC10 SRM 51-31-01 VOL II PAGE 1. 2 L 7 3 4F RT A22WE 2008032600018 20080326 00018 NM 2008 3 26 Q2SA752007 1 20080314 A 2797 WIRE BOEING 747 747228F 1384895 NM L/E FLAP BROKEN A Q2SA A J UNSCHED LANDING DUMP FUEL F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 63 752SA 21255 NR 4 LEADING EDGE FLAP DID NOT RETRACT AFTER TAKEOFF. AMBER LEADING EDGE FLAP LIGHT ON FORWARD PANEL AND FLIGHT ENGINEE R PANEL ILLUMINATED. REPAIRED WIRE NR W840-C345-20R PER WDM 20-30-12. 2 L 7 4 4F RT A20WE 2008032600036 20080326 00036 NM 2008 3 26 EIA2008012 1 20080301 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 20712 BS 340 LEFT BELOW STRINGER 5 CRACK FROM FASTENER HOLE. STOP DRILLED CRACK INSTALLED PREFABBED DOUBLERS PER ECRA 485-53- 188-2. 2 L 7 4 4F RT A20WE 2008032600055 20080326 00055 WP 2008 3 26 08FDEA01011 1 20080318 A 5753 ARC2735 SKIN DOUG DC10 DC1030F 3023504 WP T/E FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 307FE 48291 LT WING INBD FLAP UPPER SURFACE FOUND 1 EA DENT ON SKIN. REPAIRED SKIN IAW SRM 51-10-00 PAR 2 VOL II. 2 L 7 3 4F RT A22WE 2008032600117 20080326 00117 EU 2008 3 26 2008UALA01558 1 20080318 A 2560 D5211210100060 GIRT BAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 433UA 589 DOOR 2R ARMED INDICATOR BAR MISSING. REPLACED GIRT BAR. REPLACED GIRT BAR. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032600118 20080326 00118 2008 3 26 2008UALA01559 4 20080319 A 2565 CYLINDER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R1 DOOR SLIDE LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 807UA 798 DOOR 1R EMERGENCY CYLINDER PRESSURE WAS LOW. SERVICED EMERGENCY CYLINDER. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032600122 20080326 00122 EA 2008 3 26 CHQA200800052 1 20080315 A 7897 M8372395R10054 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE THRUST REVERSER LOOSE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 638BR 7311 GEE872506 MAF TO IAH - WHILE CLIMBING THROUGH 17,000 FT, THE CREW RECEIVED AT L REV UNLOCKED MESSAGE ON EICAS WITH A REV ICON ON T HE N1 GAUGE. THERE WAS NO DEGRADATION OF AIRCRAFT PERFORMANCE NOTED. THE CREW PERFORMED THE APPROPRIATE CHECKLISTS AND RETURNED TO MAF. MAINTENANCE STOWED THE THRUST REVERSER AND DEFERRED IT. WHILE WORKING TO CLEAR THE DEFERRAL ON THE T RUST REVERSER, THE CONNECTOR ON THE REVERSER POWER DRIVE UNIT WAS DISCOVERED TO BE LOOSE. AFTER RECONNECTING THE CONNEC TOR, THE REVERSER OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2008032600123 20080326 00123 NM 2008 3 26 2008UALA01562 1 20080317 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 DOOR 2L WOULD NOT ARM ON PUSHBACK. FOUND GIRT BAR NOT IN NORMAL POSITION. REPOSITIONED GIRT BAR, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032600125 20080326 00125 NM 2008 3 26 2008UALA01563 1 20080317 A 2560 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 1R DOOR SLIDE OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 DOOR 1R WILL NOT ARM. FOUND LANYARD WRAPPED AROUND GIRT BAR. REPOSITIONED LANYARD, DOOR OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032600127 20080326 00127 NM 2008 3 26 2008UALA01564 1 20080319 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INTERMITTENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 671UA 30026 EMERGENCY EXIT PATH LIGHTING FLASHING ON & OFF INTERMITTENTLY. REPLACED BATTERY. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032600128 20080326 00128 NM 2008 3 26 QXEA200800288 1 20080313 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - C4- RIGHT INBOARD SEAT TRACK NR 13 HAS MINOR SCRATCHES AT (STA X236 TO X258), (STAX268 TO X290), (STAX301 TO X373) , STAX410 TO X434), (STAX475 TO 495), (STAX509 TO X529), (STAX 547 TO X558). REMOVED SCRATCHES IAW DASH 8 Q400 RD 8/4-5 3-884. MEASURED ALL REMAINING AREA MAX MATERIAL REMOVED IS .024" WITHIN LIMITS PER RD 8/4-53-884. HFEC INSPECTED BLEND ED AREAS FOR CRACK IAW Q400 NDTM PART 6, 51-00-01. NO CRACK NOTED. APPLIED ALODINE TO BLENDED AREAS OF SEAT TRACK IAW D8 Q400 SRM 51-21-10. 2 H 7 2 4T RT A13NM 2008032600129 20080326 00129 NM 2008 3 26 2008UALA01565 1 20080319 A 2420 GENERATOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE APU FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 671UA 30026 WITH APU RUNNING, GEN OFF LIGHT ILLUM AFT NR 1 ENG START WITH PWR TRANSFER. CYCLED APU GEN GCU, NO HELP. BOTH ENG GENS ON LINE AND RESET. NO HELP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032600131 20080326 00131 NM 2008 3 26 QXEA200800289 1 20080313 A 5220 SILL BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY EXIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - C4- FROM STA X71.0 TO X94.0 ON THE RIGHT EMERGENCY DOOR LOWER AUX SILL HAS CORROSION AROUND NUT PLATES. REMOVED U PPER THRESHOLD SILL, REMOVED LOWER THRESHOLD BEAM EDGE (PN 85329514-101) BY DRILLING REF Q400 SRM 51-40-07. INSTALLED N EW FROM STOCK LOWER THRESHOLD PIECE BY INSTALLING SOLID RIVETS IAW DASH 8 400 SRM 51-42-05 AND CHERRYMAY RIVETS IAW DASH 8 400 SRM 51-42-15. REINSTALLED UPPER THRESHOLD SILL USING NEW FROM STOCK HARDWARE AS REQUIRED. 2 H 7 2 4T RT A13NM 2008032600132 20080326 00132 NM 2008 3 26 2008UALA01567 1 20080320 A 2897 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE BOOST PUMP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 213UA 30219 THE L FWD FUEL BOOST PUMP PRESSURE SWITCH SIGNAL IS LOW WITH L FWD FUEL BOOST PUMP ON. FOUND FAULTY FUEL PUMP AND CONNE CTOR DAMAGED. REPLACED CONNECTOR AND PUMP. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032600134 20080326 00134 SO 2008 3 26 SWIA200819347 1 20080115 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 250YV 120250 FOUND AT C-CHECK, LEFT FORWARD CABIN SEAT TRACK IS CORRODED. REPLACED LEFT FORWARD SEAT TRACK IAW EMB-120 MM 53-01-05. 2 L 7 2 4T RT A31SO 2008032600143 20080326 00143 NM 2008 3 26 2008UALA01572 1 20080320 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 344 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 FWD ENTRY DOOR CUTOUT CREASE BEAM CORRODED AROUND FASTENER HOLES AT BS 344 LBL 56 - 59 AT WL 208. MAJOR REPAIR ACCOMPLI SHED: REMOVED & REPLACED FWD ENTRY DOOR CUTOUT CREASE BEAM. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED FWD ENTRY DOO R CUTOUT CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032600144 20080326 00144 NM 2008 3 26 2008UALA01573 1 20080319 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 847 S25L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 BS 847 STR 25L, STRINGER CLIP CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032600145 20080326 00145 NM 2008 3 26 2008UALA01574 1 20080319 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1520 S22-23R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 AFT PIT STA 1520 BETWEEN S22-23R HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF INBOARD FLANGE. FA BRICATED & INSTALLED J-ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032600146 20080326 00146 NM 2008 3 26 2008UALA01575 1 20080319 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 800-1420 S25L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 FRAME AT BS 800-1420 LBL 5 - RBL 5 S25L REQUIRED REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032600150 20080326 00150 EA 2008 3 26 SWIA200819354 1 20080313 A 3350 INVERTER CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 935SW 7725 FLT 5983 - FORWARD EMERGENCY LIGHT STRIP ON FLOOR AND ALSO AT EMERGENCY EXIT DOOR IS INOP. REPLACED INVERTER ON NR 2 EL BP IAW CRJ 200 AMM 33-51-07. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008032600153 20080326 00153 SO 2008 3 26 SWIA200819356 1 20080305 A 2121 RCCB EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 07 292SW 120319 FLT 5742 - SMOKE IN COCKPIT WHILE AT THE GATE. REPLACED RCCB FOR LEFT GROUND COOLING FAN. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008032600154 20080326 00154 EA 2008 3 26 SWIA200819357 1 20080314 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 916SW 7634 FLOOR LEVEL EMERGENCY LIGHT AT PAX DOOR IS BROKEN. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F RT A21EA 2008032600157 20080326 00157 SO 2008 3 26 SWIA200819360 1 20080312 A 5210 FORK EMB 120 EMB120ER 3260203 SO PAX DOOR DEFECTIVE A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 293SW 120320 FLT 5727 - MAIN CABIN DOOR WILL NOT OPEN. REPLACED FORK ASSEMBLY ON AFT OVER CENTER CAM LINKAGE FOR CABIN DOOR. OP CHE CKS GOOD. 2 L 7 2 4T RT A31SO 2008032600160 20080326 00160 SO 2008 3 26 SWIA200819361 1 20080317 A 2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203 SO LAVATORY FAULTY A SWIA O OTHER N FALSE WARNING UK UNKNOWN 1 NM 07 290SW 120317 THE LAV SOME DETECTOR GOES OFF INTERMITTENTLY. REPLACED LAV SMOKE DETECTOR WITH A SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008032600163 20080326 00163 NM 2008 3 26 2008UALA01584 1 20080319 A 3150 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ILLUMINATED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 644UA 25094 NR 2 ENG 'ENG CONTROL' MESSAGE APPEARED ON EICAS WITH EEC IN NORMAL MODE. RECURRED ON SUBSEQUENT FLIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032600164 20080326 00164 NM 2008 3 26 2008UALA01585 1 20080319 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 EMERGENCY LIGHT ON FLOOR 1E PLASTIC IS MISSING. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032600165 20080326 00165 NM 2008 3 26 2008UALA01586 1 20080319 A 3320 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LAVATORY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 661UA 27158 LIGHT OUT IN FWD LAV. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032600166 20080326 00166 NM 2008 3 26 2008UALA01587 1 20080319 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE SEAT 6B UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 666UA 29238 SEAT 6B EMERGENCY LIGHT ON SIDE NEEDS GLUE, IT'S DANGLING ON WIRE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032600170 20080326 00170 SW 2008 3 26 WGEA200800050 1 20080317 A 2710 271058221002A BELLCRANK ECLIPS EA500 ECLIPSEEA500 3350000 SW AILERON SYS BINDING E WGEA O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 27 162DJ 99 000079 IN FLIGHT AILERON FLIGHT CONTROL SIDE STICK FEELS VERY NOTCHY WHEN ROLLING LEFT OR RIGHT. SUPPLEMENTAL INFORMATION-GAIN ED ACCESS TO RT AILERON JOINT, FOUND IT TO BE BINDING. REPLACED JOINT AND BELLCRANK WITH NEW. CHECKED LT AILERON JOINT AND FOUND IT TO BE FREE MOVING. ALL WORK DONE IAW EA500 MM TR 27-1, 27-11-18 AND 27-11-17. LT AND RT AILERON POS 4 PU SH RODS ARE BOTH SECURED AND SAFETIES IAW EA500 MM 27-11-16. NO ROD ADJUSTMENTS WERE DONE. ACCESS PANELS REINSTALLED I AW EA500 MM 06-50-00. REMOVAL AND INSTALLATION OF RT AILERON DONE IAW EA500 MM 27-11-21. PERFORMED FUNCTIONAL TEST (TR AVEL CHECKS) IAW EA500 MM 27-00-00-071-8-701-001. NO DEFECTS NOTED. 1 L 7 2 4J RT A00002AC 2008032600171 20080326 00171 SW 2008 3 26 WGEA200800051 1 20080318 A 2710 271058201002 BELLCRANK ECLIPS EA500 ECLIPSEEA500 3350000 SW AILERON SYS BINDING E WGEA O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 27 148DJ 156 000061 FOUND LT AILERON JOINT AND BELLCRANK BINDING. REMOVED LT AILERON, REPLACED LT BELLCRANK AND JOINT ASSY WITH NEW. REINS TALLED LT AILERON. VERIFIED RT AILERON DOES NOT HAVE ANY BINDING. COMPLIED WITH SATISFACTORY OP'S CHECK OF LT BELLCRAN K AND JOINT. COMPLIED WITH TRAVEL CHECKS OF LT AND RT AILERONS. NO DEFECTS NOTED. ALL WORK DONE IAW EA500 MM 27-11-21 , 27-11-17, TR 27-3, 27-11-18, AND 27-00-00. 1 L 7 2 4J RT A00002AC 2008032600173 20080326 00173 NM 2008 3 26 QXEA200800291 1 20080313 A 5313 STRINGER BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX-C4- SUSPECT CORROSION ON STR 31P AROUND RIVET TAILS FROM X176 TO X182. REMOVED RIVETS (7) AFT OF STA 176 AT STR 31L , REF. -8 Q400 SRM 51-42-05. REMOVED CORROSION ON STR 31P IAW Q400 SRM 51-21-00. HFEC INSPECTED AFFECTED AREA FOR CRAC KS IAW D8 Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. INSTALLED 7 RIVETS PREVIOUSLY REMOVED IAW SRM 51-42-05. ALODINE D BLENDED AREA IAW Q400 SRM 51-21-10, PRIMED AREA IAW Q400 SRM 51-25-10 AND PAINT AREA IAW Q400 51-25-15. 2 H 7 2 4T RT A13NM 2008032600180 20080326 00180 SO 2008 3 26 SIMA200807902 1 20080318 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A SIMA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 696AE 14500874 ON FLIGHT 3731, CREW REPORTED UPON REACHING TAKEOFF SPEED NOTED SMOKE SMELL IN THE COCKPIT. CREW ABORTED TAKEOFF AND R ETURNED TO GATE. 2 L 7 2 4T RT T00011AT 2008032600181 20080326 00181 SO 2008 3 26 SIMA200807903 1 20080311 A 4930 4504616A FUEL CONTROL EMB 145 EMB145LR 3260212 SO APU FAULTY A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 664MS 145779 ON FLIGHT 4101, CREW REPORTED STRONG FUEL SMELL WHEN APU POWERING PACKS AND OIL SMELL WHEN ENGINES POWERING PACKS. AIRC RAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED APU FUEL CONTROL IAW EMB 145 AMM 49 -32-01-000-801-A 49-32-01-400-801-A LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032600182 20080326 00182 SO 2008 3 26 SIMA200807904 1 20080311 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO A/C BAY MALFUNCTIONED A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 642AE 145193 ON FLIGHT 3653, CREW REPORTED DURING TAXI OUT WITH APU BLEED SUPPLYING THE PACKS A HAZE IN THE COCKPIT AND CABIN WAS NOT ED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LT HEAT EXCHANGER AND LEFT ACM IAW EMB AMM 21-51-02 AND 21-51- 03. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032600202 20080326 00202 NM 2008 3 26 Z6WR200800001 1 20080318 A 7830 315W52176 BLADE BOEING 777 BOEING 777 777 UTILUSE NM THRUST REVERSER MISLOCATED B DALA K NONE O OTHER IN INSP/MAINT 1 CE 07 000061 THE 315W5217-6 OUTER V-BLADE IS MISLOCATED TOO FAR FORWARD AS NOTED BELOW, .018" AT 18.5" FROM LOWER EDGE OF THE 315W521 7-6 OUTER V-BLADE, .030" AT 65.5" FROM LOWER EDGE OF THE 315W5217-6 OUTER V-BLADE, .047" AT 92.75 FROM LOWER EDGE OF THE 315W5217-6 OUTER V-BLADE, .044" AT 116.25" FROM LOWER EDGE OF THE 315W5217-6 OUTER V-BLADE. THE 315W5217-6 OUTER V-BLA DE HAS A 12.5" LONG CRACK LOCATED 146.75" FROM LOWER EDGE. UNABLE TO DETERMINE IF V-BLADE WAS MISLOCATED AT THIS LOCATI ON DUE TO CRACK CONDITION. MISLOCATED/CRACKED 315W5217-6 OUTER V-BLADE IS BEING REPLACED PER SERVICE BULLETIN 777-78-00 61. 2 L 7 2 4F RT T00001SE 2008022800143 20080228 00143 EA 2008 2 28 COMA0860139 1 20080220 A 2420 63E791 HEAT EXCHANGER CNDAIR CL600 CL6002B19 1900309 EA RT PYLON FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 932CA 1916 7038 FLIGHT 5279 - RECEIVED IDG NR 2 CAUTION MESSAGE. ABORTED APPROACH, PERFORMED QRH, LANDED WITHOUT INCIDENT. REPLACED NR 2 IDG HEAT EXCHANGER. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008022800154 20080228 00154 NM 2008 2 28 KCSA081099 1 20080221 A 5313 STRINGER BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE STR 34L CRACKED AT BS 1780. 2 L 7 4 4F RT A20WE 2008022800157 20080228 00157 NM 2008 2 28 HALA0800203 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 805 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION, SECTION 45,SEAT TRACK AT RBL 54.75, STA 805, MAX DEPTH OF BLEND OUT WAS 0.002". BLENDED IAW SRM 51-1 0-02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022800160 20080228 00160 NM 2008 2 28 HALA0800202 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1030 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS AT RBL 88.5, STA 1030, MAX BLEND OUT 0.015". BLENDED IAW SRM 51-00-02. ALL B LEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008022800165 20080228 00165 2008 2 28 DL76G080213 4 20080216 A 3417 4040800911 ADC BOEING 767 7673P6 1385105 NM FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 154DL 25241 F/O'S ALTIMETER OFF FLAG DISPLAYED REPLACED RT ADC PER M/M. ALL TESTS PASS, FLAG CLEARED, P/N 4040800-911. 2 L 7 2 4F RT A1NM 2008022800167 20080228 00167 NM 2008 2 28 AALA200800263 1 20080207 A 3350 1000679 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 338AA 22335 LAX - EMERGENCY EXIT LIGHT IN COCPIT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT LIGHT IN COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008022800168 20080228 00168 NM 2008 2 28 2008UALA00265 1 20080115 A 5240 CONTROL ROD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 DOOR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 581UA 26701 MAIN CABIN DOOR 3L VERY DIFFICULT TO DISARM. DOOR CONTROL ROD OUT OF ADJUSTMENT. ADJUSTED RETRACTABLE DOOR MECH CONTRO L ROD. ACCOMPLISHED DOOR OPS CHECK, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008022800169 20080228 00169 WP 2008 2 28 AALA200800310 1 20080213 A 4990 MAGNETIC PLUG DOUG DC9 DC982 3022082 WP APU LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 412AA 49323 EWR INFLIGHT T1883/13FEB - CREW REPORTED SMOKE IN CABIN AFTER TAKEOFF. RETURNED TO EWR AND LANDED WITHOUT INCIDENT. FO UND AUXILLIARY POWER UNIT (APU) LEAKING OIL AT OIL TANK MAGNETIC PLUG. REPLACED O-RINGS ON MAGNETIC PLUG. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008022800170 20080228 00170 WP 2008 2 28 IXXA08SMN033S 1 20080122 A 5522 SKIN DOUG DC8 DC862F 3021972 WP LT ELEVATOR CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND CORROSION AND DENTS ON LEFT ELEVATOR LOWER SKIN AT STATION XE 28.800 TO STATION XE 127.900. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PART AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AR EA AND REPAIR PARTS. PERFORMED BALANCE LEFT ELEVATOR FOUND AT THE MOMENT WITH IN TOLERANCE MOMENT=1509.5 INCH POUND. I NSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 55-4-1 FIGURE 1 SHEET 1 AND 2, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 5 5-2-0 PAGE 12, DC8 SRM 55-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 55-4-1 FIGURE 1 SHEET 1AND 2 PAGE 2AND3 ITEM "E" AND "F", DRA 2 L 7 4 4F 4A25 2008022800176 20080228 00176 NM 2008 2 28 KCSA081102 1 20080221 A 5320 STRAP BOEING 747 747209B 138489B NM FUSELAGE BROKEN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 BULK PIT STABILIZATION STRAP BROKEN AT BS 1950, LBL 71. 2 L 7 4 4F RT A20WE 2008022800178 20080228 00178 NM 2008 2 28 SWAA080955 1 20080220 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 266WN 32523 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 19 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008022800180 20080228 00180 NM 2008 2 28 SWAA080960 1 20080220 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800181 20080228 00181 NM 2008 2 28 SWAA080963 1 20080220 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, STR 27L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008022800183 20080228 00183 NM 2008 2 28 SWAA080962 1 20080220 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, STR 26L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032800005 20080328 00005 NM 2008 3 28 AALA200800582 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 41C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 41C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800021 20080328 00021 NM 2008 3 28 AALA200800541 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 796AN 30796 DFW - EMERGENCY LIGHT AT SEAT 29G MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 29G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800060 20080328 00060 2008 3 28 SWAA081568 4 20080320 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032800068 20080328 00068 NM 2008 3 28 SWAA081542 1 20080323 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032800090 20080328 00090 NM 2008 3 28 SWAA081559 1 20080323 A 3350 20131A BATTERY PACK BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED C4 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008032800091 20080328 00091 NM 2008 3 28 SWAA081560 1 20080323 A 3350 20131A BATTERY PACK BOEING 737 7373Q8 1384670 NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED PM CHECK, FWD CABIN EMERGENCY EXIT LIGHTS REMAIN ON. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008032800097 20080328 00097 2008 3 28 SWAA081578 4 20080324 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 252WN 34973 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032800103 20080328 00103 WP 2008 3 28 YYFA200800002 1 20080307 A 2910 7912641966 HYDRAULIC LINE DOUG DC9 DC982 3022082 WP HYDRAULIC SYS LEAKING A YYFA K NONE K FLUID LOSS CR CRUISE 1 SO 29 905TA 49905 DURING CRUISE RIGHT HYDRAULIC PRESSURE LOW AND RUDDER CONTROL MANUAL DUE TO RIGHT HAND HYDRAULIC SYSTEM LEAK. 2 L 7 2 4F A6WE 2008032800107 20080328 00107 NM 2008 3 28 SWAA081524 1 20080319 A 5512 65C25727 SKIN BOEING 737 7375H4 138449D NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032800111 20080328 00111 WP 2008 3 28 UPS08851867 1 20080305 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 5 SPOTS OF CORROSION ON TOP OF LAV AREA FLOOR PANEL, STA 62-75 RBL 30-37. REMOVED CORROSION WENT OUT OF LIMITS. FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-3 FIG 10, 51-1-8. 2 L 7 4 4F RT 4A25 2008032800112 20080328 00112 WP 2008 3 28 UPS08851868 1 20080228 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 SKIN AROUND LT CENTER L/E INBOARD HOIST ATTACH POINT IS BULGING AND CRACKED. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR DOUBLERS IAW SRM 51-1-21, 57-2-00 FIG 2A, 51-1-8 , 51-1-26. 2 L 7 4 4F RT 4A25 2008032800113 20080328 00113 WP 2008 3 28 UPS08851869 1 20080302 A 5720 STRUCTURE DOUG DC8 DC873F 302199F WP LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 3 DRILL STARTS IN COUNTERSINK ON TOP OF LEFT L/E AUX TANK, OUTBOARD END. OVERSIZED FASTENER HOLE, IN STALLED CONICAL WASHERS, FABBED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-1 FIG 37, 51-1-8, 51-3-4, 51-1-26. 2 L 7 4 4F RT 4A25 2008030300124 20080303 00124 NM 2008 3 3 AALA200800354 1 20080219 A 3397 1703663 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 646AA 24604 SFO - EMERGENCY LIGHTS AT SEAT ROWS 26 AND AFT INOPERATIVE. REPLACED CONNECTOR AT SEAT ROW 29 FOR EMERGENCY LIGHTS AT S EAT ROWS 26 AND AFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008030300125 20080303 00125 WP 2008 3 3 AALA200800356 1 20080220 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 488AA 49681 LGA - EMERGENCY LIGHTS AT OVERHEAD FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD FO RWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030300127 20080303 00127 NE 2008 3 3 AALA200800349 2 20080218 A 7261 OIL SYSTEM DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RIGHT ENGINE LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 405A 49316 728235 ORD INFLIGHT T1462/18FEB - DURING CLIMB CREW REPORTED NUMBER TWO ENGINE LOW OIL PRESSURE INDICATION. OIL QUANTITY, PRES SURE AND TEMPERATURE INDICATIONS GRADUALLY WENT TO ZERO. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TI ME APPROXIMATELY 10 MINUTES. REPLACED NUMBER TWO ENGINE AND ISOLATORS ON 19 FEB AT ORD DUE TO OIL PRESSURE AND QUANTITY OUT OF LIMITS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2008030300129 20080303 00129 SW 2008 3 3 WGEA200800033 1 20080222 A 7930 UNKNOWN ECLIPS EA500 ECLIPSEEA500 3350000 SW NR 1 ENGINE UNKNOWN E WGEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 163DJ 000081 DURING T/O ROLL, NR 1 ENGINE OIL PRESSURE 8.2 PSI, AMBER, DISCONTINUED T/O. PERFORMED ENGINE RUN OIL PRESSURE GOOD AT I DLE AND MAX POWER. AT MAX POWER READ 5.2 ON LEFT ENGINE AND 4.9 ON RIGHT ENGINE. OPS CHECK GOOD IAW EA500 AMM 71-00-00 . 1 L 7 2 4J RT A00002AC 2008030300131 20080303 00131 SO 2008 3 3 SWIA200819255 1 20080222 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 580SW 14346 3508 120348 FLT 5485 - SEVERAL EMERGENCY FLOOR LIGHTS AND BOTH OVERWING EXIT LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK. OPS CH ECK GOOD. 2 L 7 2 4T RT A31SO 2008030300132 20080303 00132 NM 2008 3 3 2008UALA00896 1 20080215 A 3350 SIGN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 337UA 24241 FOUND DOOR 2R FWD EXIT SIGN FELL OFF. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030400001 20080304 00001 NM 2008 3 4 2008UALA00897 1 20080215 A 2730 251N601818 PULLEY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ELEVATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 CABIN CEILING AREA ELEVATOR CONTROL CABLE PULLEY CRACKED OB SIDE BETWEEN BS 333 AND BS 350 L4L. STRESS FRACTURE. REPLA CED ELEVATOR CONTROL CABLE PULLEY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030400038 20080304 00038 NM 2008 3 4 DHL2008749008 1 20080122 A 5754 ATTACH FITTING BOEING 727 727223 1384074 NM NR 5 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 RT WING NR 5 SLAT ACTUATOR ATTACH FITTING CRACKED AT INBOARD SIDE, INSIDE LEADING EDGE STRUCTURE. FABRICATED NEW RIBS ( 2 EACH) IAW SRM 57-50-2 FIGURE 2, 51-20-1 FIGURE 1 AND SRM 51-20-1 FIGURE 2. IAW ER 2-37163-801 REV A. INSTALLED NEW RIBS AT NR 5 SLAT IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008030400039 20080304 00039 NM 2008 3 4 DHL2008749009 1 20080123 A 5524 ANGLE BOEING 727 727223 1384074 NM RT ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 RIGHT ELEVATOR LOWER SKIN INTERIOR SUPPORT ANGLE IS CRACKED ELEVATOR STATION 20 VIEW THROUGH ACCESS 9405. REMOVED ANGLE IAW SRM 51-30-2. FABRICATED NEW ANGLE IAW SRM 51-20-1, 51-20-2, 51-30-5, 55-20-2 FIGURE 7. ALODINE AND PRIMED ANGLE I AW SRM 51-10-2. INSTALLED ANGLE IAW SRM 51-30-2 AND 51-40-3 FIGURE 1. OPEN AND CLOSED AFTER INSTALLED ANGLE, SIDE SKIN IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008030400047 20080304 00047 WP 2008 3 4 08FDEA00547 1 20080221 A 3260 RELAY DOUG MD10 MD1010F 3022112 WP MLG MALFUNCTIONED A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 565FE 46996 ON ARRIVAL AFTER GEAR DOWN GOT LVL 2 LT ANTI-SKID FAIL. IT DID NOT REAPPEAR AFTER DROPPING GEAR ON SECOND APPROACH. RE PLACED RELAY R2-105 PER SMP. OP CHECKED SYSTEM PER MD10-10 MM 32-45-00-5. OP CHECK OK. OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2008030400062 20080304 00062 NM 2008 3 4 08FDEA00530 1 20080220 A 5246 112N61015 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 WING FUEL PANEL 641EB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 641EB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 112N6101-5. 2 L 7 2 4F RT A2NM 2008030400085 20080304 00085 SO 2008 3 4 SWIA200819225 1 20080208 A 2121 EVAC523C2 FAN EMB 120 EMB120ER 3260203 SO RECIRCULATION SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 565SW 13488 13352 120340 SMELL OF SMOKE WHILE IN FLIGHT AT LOW POWER SETTINGS, FLIGHT NR 5499. REPLACED THE LEFT RECIRCULATION FAN WITH A SERVIC EABLE UNIT IAW EMB 120 MM 21-24-03. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2008030400100 20080304 00100 NM 2008 3 4 DL75E080245 1 20080215 A 3150 WARNING LIGHT BOEING 757 7572Q8 1384972 NM ILLUMINATED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 702TW 28162 AFTER PUSHBACK AND ENGINE START. RECEIVED A AUTOSPEED BRAKE MSG. FWD TO MCO PER MEL 27-62-01B. MCO AND PLAC INSTALLED . 2 L 7 2 4F RT A2NM 2008030400107 20080304 00107 NM 2008 3 4 2008UALA00652 1 20080204 A 5753 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAP GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 RT INBOARD FLAP VANE UPPER EXTERNAL SURFACE IS GOUGED AT OUTBOARD END OF VANE. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030400116 20080304 00116 NM 2008 3 4 HALA0800186 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION AT RBL 54.75, SEAT TRACKS, STA 1197+88, BASE OF TRACKS. CORROSION REMOVED PER SRM 51-10-02 REV 76 AND SRM 53-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030400119 20080304 00119 EU 2008 3 4 2008UALA00862 1 20080218 A 3510 OXYGEN BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 431UA 571 COCKPIT OXYGEN BOTTLE, LOW CREW COMMENTS: CREW O2 NEEDS SERVICING. SERVICED CREW O2 TO FULL, NO LEAKS WERE NOTED AT THI S TIME. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030400122 20080304 00122 EU 2008 3 4 2008UALA00865 1 20080216 A 3350 D9239003500060 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 497UA 1847 RT EMERGENCY EXIT LIGHT BATTERY FAILS TEST, BATTERY FAILURE. REPLACED BATTERY. ALL OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030400130 20080304 00130 NM 2008 3 4 HALA0800188 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION RBL 54.75, SEAT TRACKS, STA 1197+120, BASE OF TRACK. CORROSION REMOVED PER SRM 51-10-02 REV 76 AND SR M 53-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030400133 20080304 00133 2008 3 4 2008UALA00866 4 20080218 A 2565 LANYARD AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L1 DOOR SLIDE OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 847UA 1627 LANYARD HANGING OUT OF SLIDE PACK AT 1L. REPACKED LANYARD AND SLIDE ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030400134 20080304 00134 EU 2008 3 4 2008UALA00867 1 20080217 A 2612 700TS06Y12 CONTROL PANEL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FIRE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 463UA 1282 APU FIRE BOTTLE DISCHARGE LIGHT IS ILLUMINATED BLOW OUT DISK IS INTACT LOW PRESSURE. FOUND APU FIRE TEST SWITCH INTERMI TTENT STUCK, CAUSED APU BOTTLE DISCHARGE LIGHT PROBLEM. REPLACED ENG, APU FIRE PANEL (1WD) THEN OP-TEST NO FAULT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030400149 20080304 00149 NM 2008 3 4 DLM88080262 1 20080213 A 5330 59360665 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 DURING HMV, CORROSION WAS FOUND AT STA Y=730 ON SKIN P/N 5936 066-5 BETWEEN LONGERON 30 AND 29 RT. A PERMANENT REPAIR W AS PERFORMED IAW ER/A 465648-14. 2 L 7 2 4F RT A6WE 2008030400157 20080304 00157 SO 2008 3 4 SIMA200805103 1 20080219 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 619AE 145101 DURING MBV INSPECTION, FOUND SERVICE DOOR CENTER SILL CORRODED. REPLACED SERVICE DOOR SILL IAW EMB SRM 51-40-02. A/C R ETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008030400160 20080304 00160 SO 2008 3 4 SIMA200805105 1 20080218 A 3260 23092900H01 UPLOCK EMB 145 EMB145LR 3260212 SO RT MLG INOPERATIVE A SIMA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 641AE 145191 ON FLIGHT 4122, CREW REPORTED RIGHT MAIN GEAR DID NOT INDICATE DOWN. CREW DECLARED EMERGENCY AND FOLLOWED AOM PROCEDURE S ALL THREE GEAR IN THE GREEN. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR UPLOCK BOX IAW EMB 145 AMM 32-33-10. ALL SUBSEQUENT OPERATIONAL CHECKS SATISFACTORY AND NR 8194; AIRCRAFT RETURNED TO SERVICE AND NR 8194; AND NR 8194;AND NR 8194; 2 L 7 2 4T RT T00011AT 2008030400181 20080304 00181 NM 2008 3 4 08FDEA00576 1 20080222 A 5730 1060031116 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 WING FUEL PANEL 541DB HAS SURFACE/FRETTING CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF SRM 57-20-01, SECTION A-A, DETAIL I LIMITS. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-116. 2 L 7 2 4F RT A2NM 2008030400188 20080304 00188 NM 2008 3 4 F3LA200800047 1 20080213 A 3412 102EH2EB TAT PROBE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE INOPERATIVE A F3LA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 938FR 10791 178 2406 ON CLIMB-OUT, THE FLIGHT CREW REPORTED AN ECAM MESSAGE (15052) INDICATING THE CAPTAIN'S TAT SENSOR WAS INOPERATIVE. DES TINATION AIRPORT REQUIRED TAT INFORMATION FOR ANTI-ICING OPERATIONS. THE FLIGHT CREW RETURNED TO THE DEPARTURE AIRPORT AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS TAT SENSOR IN ACCORDANCE WITH THE REQUIRE MENTS OF AMM 34-11-18 PB 401. OPERATIONS TEST WAS ACCOMPLISHED IN ACCORDANCE WITH AMM 30-31-00-710-001 AND TESTED GOOD. 2 L 7 2 4F 4 F RT A28NM 2008030400190 20080304 00190 EU 2008 3 4 08FDEA00619 1 20080226 A 5320 A5398675120590 ANGLE AIRBUS 310 A310324 3930206 EU INTERCOSTAL BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 EMPENNAGE FR 87 TO FR 88 APPROX AT STRINGER 26, THE INTERCOSTAL IS BENT. REMOVED INTERCOSTAL FOR FOM IAW SRM 51-40-21. REMOVED DANAGED ANGLE FROM THE INTERCOSTAL IAW SRM 51-40-21. RECEIVED NEW ANGLE. INSTALLED NEW ANGLE & INTERCOSTAL I AW SRM 51-40-21. MINOR REPAIR 2 L 7 2 4F RT A35EU 2008030400198 20080304 00198 NM 2008 3 4 08FDEA00577 1 20080222 A 5730 1060031118 ACCESS PANEL BOEING 757 7572B7 1384964 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 WING FUEL PANEL 542BB HAS SURFACE/FRETTING CORROSION. REMOVED CORROSION FROM PANEL 542BB, FOUND TO BE OUT OF SRM 57-20- 01, SECTION A-A, DETAIL I LIMITS. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-118. 2 L 7 2 4F RT A2NM 2008030500017 20080305 00017 NM 2008 3 5 QXEA200800158 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 547-549 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - AT APPROXIMATELY STATION X547 TO X549 ON LEFT INBOARD SEAT TRACK NR 6 THERE IS CORROSION IN THE CENTER OF THE TRACK. REPAIRED IAW DHC8 200 RD8-53-3644, NDTM PT-6 51-00-01, AND DHC8 200 SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2008030500022 20080305 00022 NM 2008 3 5 QXEA200802076 1 20080101 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM BS 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - FLANGE THAT ATTACHES TO STATION 600.0 HAS CORROSION ON UNDER SIDE, ALSO NUT PLATE ATTACHMENT HAS NO COA TING FOR PROTECTION FROM RIGHT SIDE TO CENTER. REPAIRED IAW -8 200 CPC CHAPTER 4 STEP 8, AND -8 200 SRM 51-20-11, 51-40 -11. 2 H 7 2 4T RT A13NM 2008030500048 20080305 00048 NM 2008 3 5 QXEA200800119 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - SEAT TRACK NR 1 HAS SEVERAL SPOTS OF MILD SURFACE CORROSION AT STATIONS X60.0, X94.8, X130.0, X196.0 AN D 224.0. REMOVED AND INSTALL NEW TRACK IAW Q400 SRM 51-40-07, 51-40-15, 51-42-05. 2 H 7 2 4T RT A13NM 2008030500066 20080305 00066 NM 2008 3 5 QXEA200800152 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 455 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - AT APPROXIMATELY STATION X455 LEFT OUTBOARD SEAT TRACK NR 2 HAS CORROSION ON TOP OF TRACK. REPAIRED IA W DHC8 200 RD8-53-1342, NDTM PT-6 51-00-01, AND DHC8 200 SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2008030500087 20080305 00087 NM 2008 3 5 QXEA200802073 1 20080101 A 5313 STRINGER DHAV DHC8 DHC8202 2809007 NM BS 467 S31R CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - CORROSION ON STATION X467.000 ON RIGHT SIDE OF STRINGER 31R. REPAIRED IAW -8 200 CPC CHAPTER 4 PG 4-16 8B AND -8 200 SRM 51-20-16, 51-20-36, 51-20-11, 51-20-51. 2 H 7 2 4T RT A13NM 2008030500097 20080305 00097 NM 2008 3 5 QXEA200800187 1 20080130 A 5740 MOUNT DHAV DHC8 DHC8202 2809007 NM AILERON TRIM ACT LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - THE BOTTOM RIVETS ON THE AILERON TRIM ACTUATOR HINGE ARM MOUNTING PLATE ARE LOOSE AND WORKING. REMOVED AND REPLACED RIVET AT AILERON TRIM ACTUATOR AS PER DHC 8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008022800185 20080228 00185 NM 2008 2 28 AALA200800283 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 21G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022800189 20080228 00189 NM 2008 2 28 SWAA080968 1 20080220 A 5330 652072417 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT FWD CARGO DOOR CUTOUT LOWER CORNER BS 451. REPAI RED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800200 20080228 00200 WP 2008 2 28 IXXA08SMN031S 1 20080122 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND CORROSION ON LEFT WING ON LEADING EDGE OUTER UPPER PART AT STATION XFS 822.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGE AREA. PERFOR MED NDT INSPECTION. NO CRACK, NO CORROSION NOTED AFTER INSPECTION. FABRICATED REPAIR DOUBLER, AND FILLER CLEANED, TREA TED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08030 DATED 0 1-22-08, SEMAN DRAWING NUMBER ED-4690 DATED 01-16-08, DC8 SRM 51-1-21, 51-1-20D, 51-3-0, DC8 SRM 51-1-8 PAGES 17AND18, D C8 SRM 57-2-1 FIGURE 2G, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, 51-3-0, 51-1-21A, AND 51-3-1. 2 L 7 4 4F 4A25 2008022800201 20080228 00201 WP 2008 2 28 IXXA08SMN032S 1 20080122 A 5522 SKIN DOUG DC8 DC862F 3021972 WP LT ELEVATOR CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR CORRODED ON LOWER SKIN AT STATION XE 104.310 TO STATION XE 108.8 43. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABR ICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA A ND REPAIR PARTS. PERFORMED BALANCE RIGHT ELEVATOR FOUND AT THE MOMENT WITH IN TOLERANCE MOMENT 1506-5 INCH POUND INSTAL LED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 55-4-1 FIGURE 1 SHEET 1 AND 2, DC8 SRM 51-1-8 PAGES 17 AND 18, DC8 SRM 55 -2-0 PAGE 12, DC8 SRM 55-1-0 PAGE 1, SRM DC8 51-1-21, DC8 SRM 55-4-1 FIGURE 1 SHEET 1AND 2 PAGES 2 AND 3 ITEM "E" AND "F 2 L 7 4 4F 4A25 2008022800202 20080228 00202 NM 2008 2 28 AALA200800291 1 20080210 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 35G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 35G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008022800214 20080228 00214 NM 2008 2 28 AALA200800316 1 20080213 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 978AN 30100 DFW - EMERGENCY LIGHT AT SEAT 20D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008022800215 20080228 00215 NM 2008 2 28 AALA200800308 1 20080213 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 932AN 29530 MIA - EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RIG HT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008022800217 20080228 00217 NM 2008 2 28 AALA200800307 1 20080212 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 696AN 26976 MIA - EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2008022800227 20080228 00227 NM 2008 2 28 SWAA080972 1 20080221 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND LT KEEL BEAM CORRODED BETWEEN BS 721 AND BS 727, LBL 8. REMOVED AND REPLACED KEEL BEA M PER ER. 2 L 7 2 4F RT A16WE 2008022800241 20080228 00241 NM 2008 2 28 SWAA080985 1 20080221 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800242 20080228 00242 NM 2008 2 28 SWAA080986 1 20080221 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008022800243 20080228 00243 NM 2008 2 28 SWAA080987 1 20080221 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008022800246 20080228 00246 NM 2008 2 28 SWAA080990 1 20080221 A 5610 141A48103 WINDOW BOEING 737 7377H4 1384404 NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 783SW 29809 FLIGHT DECK L2 WINDOW ARCED AND CRACKED PASSING FL 230. REMOVED AND REPLACED WINDOW AND WINDOW HEAT CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2008022800248 20080228 00248 NM 2008 2 28 KCSA081104 1 20080222 A 5311 FRAME BOEING 747 747209B 138489B NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE FRAME IS DENTED AT STA 1860, STR 11R. 2 L 7 4 4F RT A20WE 2008022800249 20080228 00249 NM 2008 2 28 KCSA081105 1 20080222 A 5313 STRINGER BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE STRINGER IS CRACKED (1") AT STA 1500, STR 6L. 2 L 7 4 4F RT A20WE 2008022800251 20080228 00251 NM 2008 2 28 KCSA081107 1 20080223 A 5320 FITTING BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE UPPER SPLICE FITTING IS CORRODED AT STA 970 TO 1000, STR 38L. 2 L 7 4 4F RT A20WE 2008022800260 20080228 00260 NM 2008 2 28 KCSA081116 1 20080224 A 5711 STIFFENER BOEING 747 747209B 138489B NM RT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 RIGHT WING FRONT SPAR STIFFENER CORRODED AT L/E/ STA 1310. 2 L 7 4 4F RT A20WE 2008022800263 20080228 00263 EA 2008 2 28 TRAX200800243 1 20080211 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 845AS 7324 EXIT EMERGENCY LIGHT FACING FWD ON CEILING AT OVERWING HATCHES IS OUT. 2 L 7 2 4F RT A21EA 2008022800266 20080228 00266 SW 2008 2 28 WGEA200800029 1 20080211 A 2621 FX002002 FIRE BOTTLE ECLIPS EA500 ECLIPSEEA500 3350000 SW NR 2 NACELLE LEAKING E WGEA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 27 115DJ 152 000020 NR 2 ENGINE FIRE BOTTLE IS LEAKING, IT WAS LEAKING WHEN DISCONNECTED FOR 300 HOUR, NO EXTERNAL LEAK ON ENGINE. REMOVED AND REPLACED WITH NEW RIGHT PHOSTREX BOTTLE IAW EA500 AMM 26-20-10. INSPECTED ENGINE AND UPPER AND LOWER COWL FOR ANY P HOSTREX RESIDUE AND CLEANED AS REQUIRED. FOLLOWING CLEANUP PROCEDURES IAW EA500 AMM 26-20-00. SUPPRESSION AGENT CLEANU P PROCEDURES AND EMM 05-50-00-210-811, 05-50-16-021-801, AND 71-00-00. 1 L 7 2 4J RT A00002AC 2008022800267 20080228 00267 NM 2008 2 28 08FDEA00537 1 20080220 A 5730 1060031119 PANEL BOEING 757 7572B7 1384964 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 WING FUEL PANEL 541EB HAS SURFACE FRETTING CORROSION. WING FUEL PANEL 541EB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-119. 2 L 7 2 4F RT A2NM 2008030300031 20080303 00031 NM 2008 3 3 2008UALA00424 1 20080124 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 344 S16L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FWD ENTRY DOOR CUTOUT BS 344 STR 16L INTERCOSTAL WEB AND ATTACH ANGLES CRACKED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR: REPLACED ANGLE AND A TIE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030300032 20080303 00032 NM 2008 3 3 2008UALA00786 1 20080211 A 2560 GIRT BAR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE DOOR 2R OBSTRUCTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 823UA 952 DOOR 2R DOES NOT REMAIN ARMED AFTER INITIAL ARMING OF DOOR MUST REARM SEVERAL TIME. DEBRIS UNDER GIRT BAR FITTING. REM OVED AND CLEANED DEBRIS FROM AREA AROUND FLOOR FITTINGS. DOOR ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030300033 20080303 00033 NM 2008 3 3 08FDEA00641 1 20080228 A 5347 AFA77951 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1841-1861 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 CABIN BETWEEN STATION 1841 TO 1861, X = -8.5, SEAT TRACK FOUND CORROSION. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008030300121 20080303 00121 NM 2008 3 3 HALA0800346 1 20080221 A 5530 SCOOP BOEING 717 717200 1383700 NM VERTICAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 479HA 55124 LEVEL 2 CORROSION VERTICAL STAB RAM AIR INLET SCOOP 2 REPAIR DOUBLERS LEFT AND RIGHT SIDE. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 2008030300126 20080303 00126 NM 2008 3 3 AALA200800350 1 20080218 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 786AN 30250 DFW - EMERGENCY LIGHT AT SEAT 20C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008030300128 20080303 00128 WP 2008 3 3 AALA200800351 1 20080218 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 590AA 53253 LGA - EMERGENCY EXIT SIGN LIGHT AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHT AT AFT CA BIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008030300130 20080303 00130 NM 2008 3 3 2008UALA00848 1 20080214 A 5220 520007351 SQUIB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMER ESCAP DOOR NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 529UA 25019 EMERGENCY ESCAPE TEST 2 GREEN LIGHT DOES NOT TEST. RT MASTER CONTROL VALVE SQUIB FOR RT OFF WING ESCAPE DOOR INOP. REP LACED RT MASTER CONTROL VALVE SQUIB FOR RT OFF WING ESCAPE DOOR. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030400003 20080304 00003 NM 2008 3 4 2008UALA00899 1 20080216 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 576UA 26690 CREW REPORTS FUSELAGE HAS A DENT AND SCRATCH BELOW AND FORWARD OF DOOR 2LH. BURNISHED AREA AND CHECKED FOR CRACKS, NONE FOUND. ACCOMPLISHED HFEC, NO CRACKS NOTED. ALODINE AND PAINT, PERMANENT REPAIR TO BE PERFORMED BY NEXT "C" CHK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030400036 20080304 00036 NM 2008 3 4 DHL2008749005 1 20080114 A 5230 ANGLE BOEING 727 727223 1384074 NM BS 500 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 C-1 DOOR FORWARD FRAME REINFORCEMENT 3RD ANGLE CRACKED BS 500. REMOVED ANGLE IAW SRM 51-30-2. FABRICATED NEW ANGLE IAW SRM 51-20-2, 51-30-5 AND 52-30-1 FIGURE 4. ALODINE AND PRIMED ANGLE IAW SRM 51-10-2. INSTALLED ANGLE IAW SRM 51-30-2 AND 51-40-3 FIGURE 1. 2 L 7 3 4F A3WE 2008030400037 20080304 00037 NM 2008 3 4 DHL2008749006 1 20080115 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 480 - 620 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 SEAT TRACK CORRODED IN MAIN CARGO COMPARTMENT BS 480 - 620 LBL 45. FABRICATED NEW SEAT TRACK IAW SRM 53-10-2 FIGURE 7 AND SRM 53-10-5 FIGURE 1. INSTALLED NEW SEAT TRACK IAW SRM 53-10-5 FIGURE 1 USING PREVIOUS GOOD CONDITION SPLICE PARTS. 2 L 7 3 4F A3WE 2008030400043 20080304 00043 NM 2008 3 4 DL76S080182 1 20080209 A 3397 WIRE BOEING 767 767332 1382001 NM EMERGENCY LIGHTS BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 136DL 23146 FOUND EMERGENCY LIGHT AT SEAT 26F INOP. REPAIRED BROKEN WIRE AND RELAMPED. 2 L 7 2 4F RT A1NM 2008030500098 20080305 00098 NM 2008 3 5 QXEA200800139 1 20080119 A 5230 SKIN BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - FORWARD CARGO DOOR HAS GOUGE IN SKIN FORWARD LOWER CORNER. REPAIRED IAW Q400 RD8/4-52-381. 2 H 7 2 4T RT A13NM 2008030500101 20080305 00101 NM 2008 3 5 QXEA200800142 1 20080119 A 5312 PANEL BOMBDR DHC8 DHC8402 1390042 NM NLG WW CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - AFT NLG WHEEL WELL WALL IS CHAFED ON THE FORWARD FACE JUST LEFT OF CENTER. REPAIRED IAW RD8/4-53-1224, Q400 NDTM PT-6 51-00-01,PT-1 51-00-04 AND Q400 SRM 51-21-10, 51-25-05. 2 H 7 2 4T RT A13NM 2008030500112 20080305 00112 NM 2008 3 5 QXEA200802078 1 20080101 A 5320 SUPPORT DHAV DHC8 DHC8202 2809007 NM BS 234 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - FRAME SUPPORT CLIP CRACKED AT APPROXIMATELY STATION X234.5 (CENTER OF THRESHOLD OF MAIN PASSENGER DOOR) . REMOVED CLIP AND INSTALL NEW CLIP IAW -8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008030500114 20080305 00114 NM 2008 3 5 UIEA200800047 1 20080215 A 5310 DOOR FRAME BOEING 747 7472D7B 1384803 NM BS 1686-1687 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 MAIN DECK NR 4R DOOR AFT SIDE EDGE FRAME LOWER POSITION FOUND CRACKED. REPAIRED CRACK PER SRM 52-10-02. 2 L 7 4 4F RT A20WE 2008030500116 20080305 00116 NM 2008 3 5 QXEA200800141 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 236-289 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - (CORRECTION FROM N/R-00405) LEFT INBOARD SEAT TRACK NR 7 HAS NUMEROUS AREAS OF MINOR SURFACE CORROSION STATION X236 TO X289. REPAIRED IAW RD8/4-53-884, Q400 NDTM PT-6 51-00-01. 2 H 7 2 4T RT A13NM 2008030500119 20080305 00119 NM 2008 3 5 QXEA200800137 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - RIGHT SEAT TRACK NR 11, FORWARD END FLANGE AT SPLICE, OUTBOARD SIDE HAS SURFACE CORROSION. REMOVED AND INSTALLED NEW TRACK IAW Q400 SRM 51-42-05 AND 51-40-15. 2 H 7 2 4T RT A13NM 2008030500127 20080305 00127 NM 2008 3 5 QXEA200800148 1 20080119 A 5320 SUPPORT CHANNEL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - MCD THRESHOLD SUPPORT CHANNEL HAS CORROSION AROUND SCREW HOLES. REMOVED THRESHOLD SUPPORT CHANNEL AND INSTALLED NEW CHANNEL FROM STOCK IAW -8 Q400 SRM 51-42-05, 51-25-00, AND 51-42-45. 2 H 7 2 4T RT A13NM 2008030500129 20080305 00129 NM 2008 3 5 QXEA200800131 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 624-644 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - LEFT SEAT TRACK 15 BETWEEN FRAME 624.5 TO 644.5 HAS MULTIPLE CHAFES/GOUGES. REPAIRED IAW RD8/4-53-884, Q400 NDTM PT-6 51-00-01, AND Q400 SRM 51-21-10. 2 H 7 2 4T RT A13NM 2008030500132 20080305 00132 NM 2008 3 5 QXEA200800150 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 265 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - AT APPROXIMATELY STA X265 THE LEFT OUTBOARD SEAT TRACK NR 1 HAS CORROSION ON TOP OF TRACK. REPAIRED IA W DHC 8 200 RD8-53-1342, NDTM PT-6 51-00-01, AND DHC8 200 SRM 51-20-10, 51-20-36. 2 H 7 2 4T RT A13NM 2008030500160 20080305 00160 NM 2008 3 5 QXEA200802068 1 20080101 A 5711 SPAR DHAV DHC8 DHC8202 2809007 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - LEFT WING FORWARD SPAR APPROXIMATELY YW 42.0, Z ANGLE CRACKED AT UPPER END. REMOVED Z ANGLE BRACKET AN D FABRICATED NEW ANGLE IAW T/C 2-57-205. INSTALLED FABRICATED Z ANGLE IAW -8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008030500170 20080305 00170 NM 2008 3 5 QXEA200800211 1 20080208 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - SEAT TRACK 5, STATION 21.5 HAS BUBBLED PAINT AND SIGNS OF CORROSION. REPAIRED IAW Q400 RD8/4-53-884, R D 8/4-53-2260, AND NDTM PT-6 51-00-01 2 H 7 2 4T RT A13NM 2008030500185 20080305 00185 NM 2008 3 5 QXEA200802071 1 20080101 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 387 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - THERE IS A CHAFED SPOT AT APPROXIMATELY 12" FORWARD OF STATION X387.350 ON THE LEFT OUTBOARD SEAT TRACK . REPAIRED IAW RD8-53-1342 AND -8 200 SRM 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2008030500197 20080305 00197 NM 2008 3 5 QXEA200800184 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 582 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - NR 6 SEAT TRACK FLOORBOARD MOUNT FLANGE (INBOARD) SIDE OF FLANGE APPROXIMATELY STATION X582.00 IS CORRO DED. REPAIRED IAW DHC 8 200 RD 8-53-784, NDTM PT-6 51-00-01, RD 8-53-9998, AND DHC 8 200 SRM 51-40-11, 51-20-96. 2 H 7 2 4T RT A13NM 2008030500199 20080305 00199 NM 2008 3 5 QXEA200800193 1 20080208 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - NR 10 SEAT TRACK AT STATION X1.500 HAS AN AREA OF CORROSION AROUND NUTPLATE HOLE. REMOVED SEAT TRACK A ND INSTALLED NEW SEAT TRACK IAW Q400 SRM 51-40-15 AND 51-42-05. 2 H 7 2 4T RT A13NM 2008030600014 20080306 00014 SO 2008 3 6 RAIA00802015 1 20080214 A 3230 23092900001 UPLOCK EMB 145 EMB145LR 3260212 SO LT MLG MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 818HK 145059 FLT 5558 - ATL - LEFT GEAR DID NOT INDICATE UP ON THE EICAS AFTER RETRACTION. MAINTENANCE REMOVED AND REPLACED THE LT M LG UPLOCK BOX. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008030600015 20080306 00015 SO 2008 3 6 RAIA00802016 1 20080217 A 2740 3621001013 CONTROL UNIT EMB 145 EMB145LR 3260212 SO HORIZ STAB MALFUNCTIONED A RAIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 03 844HK 14500838 FLT 7971 - IAD - MAIN PITCH TRIM INOP DURING CLIMB. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008030400044 20080304 00044 EA 2008 3 4 SWIA200819226 1 20080213 A 2710 PULLEY CNDAIR CL600 CL6002C10 1390015 EA AILERON CONTROL DIRTY A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 710SK 10170 FLT NR 5848. CONTROL YOKE HAS A NOTCHY SPOT WHEN MOVING AILERONS, REMOVED A PEBBLE FROM THE RT AILERON CONTROL PULLEY AT WING ROOT AT INBOARD FLAP. NO DAMAGE NOTED. 2 L 7 2 4F RT A21EA 2008030400060 20080304 00060 NM 2008 3 4 GTIA0800012 1 20080201 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 501NK 2424 FLOORBEAM BETWEEN Y254 AND Y765 BETWEEN FRAME 66 AND 70 SHOWS SIGNS OF CORROSION. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2008030400068 20080304 00068 NM 2008 3 4 DLM88080221 1 20080217 A 3260 833704 SENSOR DOUG MD88 MD88 3023688 NM LT MLG WEAK A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 928DL 49715 GEAR DOOR OPEN LIGHT ILLUM IN CRUISE. LIGHT EXTINGUISHED ONCE ON DESCENT STARTED. FOUND LT MAIN GEAR DOOR SENSOR OUT O F LIMITS NDS SENSOR P/N 279202670. REPLACED D1-30 PER MM DOOR INDICATIONS NORMAL SWU GEAR INDICATIONS NORMAL. 2 L 7 2 4F RT A6WE 2008030400070 20080304 00070 EU 2008 3 4 2008UALA00851 1 20080215 A 2611 FIRE LOOP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 469UA 1409 FIRE LOOP A FAULT DISPLAYED ON UPPER ECAM SCREEN, ENG 2. FOUND WIRE 2612-276 SHORT TO GRD FROM PIN A OF 450VT2 TO JSIDE OF POSITION 1 OF 458VC2 ON JUNCTION BOX. REPAIRED SHORT, OPS CHECKS ARE GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030400076 20080304 00076 NM 2008 3 4 2008UALA00857 1 20080216 A 5320 D5311219920100 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOORWAY CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 806UA 788 DOOR 2R DOOR SILL FWD SIDE HAS CORROSION IN AREA OF PREVIOUS REPAIR. REPLACED DOOR SILL ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030400099 20080304 00099 EU 2008 3 4 2008UALA00860 1 20080217 A 5210 ACCUMULATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DOOR ASSIST UNDERSERVICED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 429UA 539 NR 2 LEFT MAIN ENTRY DOOR EMERGENCY CYLINDER ACCUMULATOR NEEDS SERVICING. SERVICED MED ACCUMULATOR, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030400101 20080304 00101 NM 2008 3 4 AALA200800276 1 20080209 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 ORD - EMERGENCY LIGHT AT RIGHT CORNER OF FORWARD GALLEY CABINET INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGH T AT RIGHT CORNER OF FORWARD GALLEY CABINET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008030400102 20080304 00102 NM 2008 3 4 AALA200800259 1 20080207 A 3350 OL3071BPEGPL LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 771AN 29579 JFK - EMERGENCY LIGHT AT SEAT 34C MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 34C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008030400103 20080304 00103 NM 2008 3 4 AALA200800261 1 20080207 A 3350 6011779 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9630A 53561 LGA - EMERGENCY LIGHT AT AFT OVERWING EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2008030400104 20080304 00104 NM 2008 3 4 AALA200800279 1 20080210 A 3350 FUSE BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 EZE - EMERGENCY LIGHTS AT AFT COACH CLASS INOPERATIVE. FOUND SEAT 34C LIGHT SHORTED AND POWER SUPPLY 3R FUSE OPENED. I NSTALLED NEW FUSE AND REPLACED LAMP AT SEAT 34C FOR EMERGENCY LIGHTS AT AFT COACH CLASS. SYSTEM GROUND CHECKED NORMAL O PERATION. 2 L 7 2 4F RT T00001SE 2008030400112 20080304 00112 NM 2008 3 4 HALA0800184 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION AT RBL 54.75, SEAT TRACKS, STA 1197+81, BASE OF TRACK. CORROSION REMOVED PER SRM 51-10-02, REV 76 AND SRM 53-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030400120 20080304 00120 EU 2008 3 4 2008UALA00863 1 20080216 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 438UA 678 FWD PIT STRINGER 41L HAS CORROSION BETWEEN FRAME 34 AND 35. MAJOR REPAIR ACCOMPLISHED AT LCQ. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030400123 20080304 00123 NM 2008 3 4 HALA0800187 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION RBL 54.75, SEAT TRACKS AT STA 1197+113, BASE OF TRACK. CORROSION REMOVED PER SRM 51-10-02 REV 76 AND SRM 53-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030400139 20080304 00139 NM 2008 3 4 2008UALA00669 1 20080205 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1681 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 AIRCRAFT RECEIVED DAMAGE TO THE BS 1681 FRAME AT WL 210, NEAR THE THRESHOLD AT DOOR 4R. ACCOMPLISHED MAJOR REPAIR AT GS O. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030400151 20080304 00151 EU 2008 3 4 08FDEA00572 1 20080222 A 5413 STRINGER AIRBUS 310 A310324 3930206 EU NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 NR 2 ENG AFT PYLON FAIRING (STRINGER), OUTBD SIDE, AFT CORNER IS CRACKED. REMOVED EXISTING DOUBLER FROM THE ADJACENT AR EA TO FOM IAW SRM 51-40- 10. FABRICATED NEW REPAIR IAW SRM 54-55-51; FIG 201 & EA 06-5480-118441. STOP DRILLED THE C RACK & REMOVED THE DAMAGE IAW SRM 54-55-51; FIG 201. INSTALLED BOTH REPAIRS, EXISTING AND NEW IAW SRM 54-55-51; FIG 20 1 & EA 06-5480-118446. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008030600018 20080306 00018 EA 2008 3 6 MASA200800157 1 20080219 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXIT SIGN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37178 7178 ASH 2841 PHX-YUM, 3 OF 5 LAMPS IN THE OVERWING EXIT SIGN INOP. MX RELAMPED THE LIGHT BULBS. 2 L 7 2 4F RT A21EA 2008030600021 20080306 00021 SO 2008 3 6 C2XA08ON091 1 20080215 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12569 14500630 FLT 7782 - SJC TO LAX - WHILE PERFORMING SERVICE CHECK MX PERSONNEL FOUND LT OVERWING EMERGENCY LIGHT INOP. MX PERSONNE L REMOVED AND REPLACED LT OVERWING EMERGENCY LIGHT BULBS OPERATIONALLY CHECK SATISFACTORY. A/C WAS RELEASED TO RETURN F OR SERVICE. 2 L 7 2 4T RT T00011AT 2008030400046 20080304 00046 NM 2008 3 4 2008UALA00850 1 20080214 A 5210 CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 L-4 DOOR POWER ACTUATOR CABLE OUT OF ADJUSTMENT. L-4 DOOR POWER ACTUATOR CABLE OUT OF ADJUSTMENT. ADJUSTED STUD ON THE TRIGGER TO GET CORRECT CABLE TRAVEL (0.9375") REQUIRED RANGE 0.95 + O R - 0.05". INSTALLED SPRING CLIP TO LOCK THE STU D IN POSITION. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030400051 20080304 00051 NM 2008 3 4 HALA0800215 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1031 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45 AT LBL 88.5, SEAT TRACKS, STA 1031, MAX DEPTH BLENDED WAS 0.010". BLENDED IAW SRM 51-10-02 . ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008030400066 20080304 00066 NM 2008 3 4 C8GA20080005 1 20080208 A 2782 269002914 ACTUATOR BOEING 727 727227 1384078 NM NR 2 SLAT LEAKING A C8GA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 SO 29 308AS 22002 FLT 707 FROM PHX TO MCI - AFTER LANDING AND DURING TAXI, A NOTICEABLE STIFFENING IN THE NOSE STEERING, FOLLOWED BY THE I LLUMINATION OF THE "A" SYSTEM HYDRAULIC LIGHT AND LOW HYDRAULIC FLUID QUANTITY OCCURRED. POST FLIGHT INSPECTION REVEALE D THAT THE NR 2 SLAT ACTUATOR WAS LEAKING. REMOVED AND REPLACED THE NR 2 SLAT ACTUATOR, OP'S AND LEAKS CHECKS GOOD. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2008030400073 20080304 00073 EU 2008 3 4 2008UALA00854 1 20080217 A 3230 114087005 CONTROL VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MLG UPLOCK LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 440UA 702 RTFL DUE TO A GREEN HYDRAULIC LOW PRESSURE WARNING INDICATION. MLG UPLOCK VALVE LEAKING, UNKNOWN DAMAGE, BOLT HEADS WEA R SHEARED OFF. REPLACED MLG UPLOCK VALVE, SERVICED GREEN SYSTEM HYDRO, PERFORMED GEAR SWINGS AND PLACED SYSTEM BACK TO NORMAL AFTER FREEFALL TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030400086 20080304 00086 NM 2008 3 4 DL757080285 1 20080225 A 5742 112N700323 FITTING BOEING 757 757232 1384965 NM LT WING DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 DURING HMV AT SAA, TWO OF THE NR 1 ENGINE PYLON SIDE LOAD FITTING FASTENER HOLES WERE OVERSIZED TO CLEAN UP TOOLING DAMA GE. THE HOLES WERE REAMED UP TO TRANSITION FIT HOLE SIZES FOR OVERSIZE FASTENERS APPROVED BY BOEING. 2 L 7 2 4F RT A2NM 2008030400096 20080304 00096 NM 2008 3 4 HALA0800255 1 20080215 A 5347 SEAT TRACK BOEING 767 767* NM BS 1273 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1273, AREA WAS HAS BEEN REWORKED BEFORE. SEAT TRACK REPLACE D PER SRM. 2 L 7 2 4F RT A1NM 2008030400121 20080304 00121 NM 2008 3 4 2008UALA00864 1 20080218 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 RAMP REPORTS DENTS AFT OF DOOR 2L, THERE IS A TOTAL OF 4 DENTS. SKIN REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030400132 20080304 00132 NM 2008 3 4 HALA0800190 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1241 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION RBL 54.75, SEAT TRACKS AT STA 1241, BASE OF TRACKS. CORROSION REMOVED PER SRM 51-10-02, REV 76 AND SR M 53-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030400146 20080304 00146 EU 2008 3 4 2008UALA00907 1 20080218 A 2700 3945128102 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ELAC FAULTY A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 419UA 487 ELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. DISCREET OUTPUTS OUT OF CALIBRATION. REPLACED ELAC NR 1, ALL OPS CHECKS P ERFORMED SATIFACTORY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030400150 20080304 00150 NM 2008 3 4 DLM88080263 1 20080213 A 5753 99359426 SKIN DOUG MD88 MD88 3023688 NM RT TE FLAP NICKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 DURING HMV, SEVERAL NICKS WERE FOUND ON THE RT INBOARD FLAP LOWER SKIN P/N 9935942-6. A REPAIR WAS PERFORMED IAW ER/A 4 66344-14. 2 L 7 2 4F RT A6WE 2008030400154 20080304 00154 EU 2008 3 4 08FDEA00575 1 20080222 A 5420 SUPPORT ANGLE AIRBUS 310 A310324 3930206 EU NR 2 NACELLE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 NR 2 PYLON, ACCESS PANEL 484 BR CUTOUT, 2 AFT VERTICAL SUPPORT ANGLES HAVE CORROSION AROUND THE NUTPLATES AND FASTENER HOLES. REMOVED AND REPLACED GUSSET IN REF TO SRM 51-40-21; PG 7. 2 L 7 2 4F RT A35EU 2008030400172 20080304 00172 NM 2008 3 4 HALA0800095 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 804 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45, SEAT TRACK AT STA 804. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 51-10-02 , REV 75, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101, REV 76. 2 L 7 2 4F RT A1NM 2008030400177 20080304 00177 NM 2008 3 4 HALA0800124 1 20080109 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1060 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 2 CORROSION SECTION 45, AT LBL 88.5, STA 1060. SEAT TRACK REPLACED. 2 L 7 2 4F RT A1NM 2008030400152 20080304 00152 EU 2008 3 4 08FDEA00573 1 20080222 A 5413 A54515214500 STRINGER AIRBUS 310 A310324 3930206 EU NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 NR 2 ENG AFT PYLON FAIRING (STRINGER), INBD INTERNAL, AFT SIDE AT NUTPLATES HAS 5 CRACKS. RECEIVED FROM STOCK P/N A5451 52411500 PO 569792.1. NEW MEMBER TO BE INSTALLED ON CARD 44T0512-2. 2 L 7 2 4F RT A35EU 2008030400153 20080304 00153 NM 2008 3 4 2008UALA00908 1 20080216 A 3510 CONNECTOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE O2 MASK FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 CAPTAIN'S OXYGEN MASK DOES NOT TEST. YELLOW CROSS APPEARS BUT DOES NOT DISAPPEAR. RESET CONNECTOR. CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030400165 20080304 00165 NM 2008 3 4 HALA0800193 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1338 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION RBL 54.75, SEAT TRACKS, STA 1338, BASE OF TRACK. CORROSION REMOVED PER SRM 51-10-02 REV 76 AND SRM 53 -00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030400194 20080304 00194 NM 2008 3 4 2008UALA00876 1 20080215 A 5330 6545776 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 908-968 WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 51315 24657 FUSELAGE SKIN UNDER DORSAL FIN WORN AT BS 908 TO 968 RBL 8 TO 12. BLENDED AREA WITH MATERIAL LOSS BETWEEN .001" AND .00 3". THIS DATE BOEING WILL ISSUE A NEW FAA FORM 8100-9 TO SHOW COMPLIANCE WITH 14 CFR PART 26.43D AIRCRAFT IS NOT AIRWORT HY AFTER 14 FEB 2009 WITHOUT NEW FAA FORM. AT THAT TIME NEW MF ITEM WILL BE CREATED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030400199 20080304 00199 NM 2008 3 4 08FDEA00578 1 20080222 A 5347 143N50903 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 440-640 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 SEAT TRACK DAMAGED AT STA 640, LBL 45.50, WL 208. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK FROM MATERIAL: BAC 1520 -792/24, LOCATED AND DRILLED, TREATED, PRIMED AND INSTALLED SEAT TRACK IAW SRM'S: 51-40-02, 53-30-52, 51-40-05 AND 51- 20-01. 2 L 7 2 4F RT A2NM 2008030500016 20080305 00016 NM 2008 3 5 QXEA200800156 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 532 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - AT APPROXIMATELY STATION X532 ON LEFT OUTBOARD SEAT TRACK NR 3 HAS CORROSION ON THE TOP OF THE TRACK. REPAIRED IAW DHC8 200 RD8-53-3644, NDTM PT-6 51-00-01, AND DHC8 200 SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2008030500067 20080305 00067 NM 2008 3 5 QXEA200800154 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 488 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C4 CHECK - AT APPROXIMATELY STATION X488 THE LEFT OUTBOARD SEAT TRACK NR 2 HAS CORROSION ON TOP OF TRACK. REPAIRE D IAW DHC8 200 RD8-53-1342, NDTM PT-6 51-00-01, AND DHC8 200 SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2008030500068 20080305 00068 NM 2008 3 5 QXEA200800155 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 504 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - AT APPROXIMATELY STATION X504 ON THE LEFT INBOARD SEAT TRACK NR 5 THERE IS CORROSION IN THE CENTER OF T HE TRACK. REPAIRED IAW DHC8 200 RD8-53-3644, NDTM PT-6 51-00-01, AND DHC8 200 SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2008030500074 20080305 00074 NM 2008 3 5 QXEA200802094 1 20080101 A 5310 STRUCTURE DHAV DHC8 DHC8202 2809007 NM BS 580 S30 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - UNDER FLOOR CARGO PIT STATION 580.500 HAS CORROSION AT STRINGER 30. REPAIRED IAW -8 200 CPC CHAPTER 4 STEP 8, -8 200 NDTM PART 6, 51-00-01, PART 1, 51-00-04, AND -8 200 SRM 51-20-16, 51-20-36, 51-20-51, 51-20-11, 51-40-11. 2 H 7 2 4T RT A13NM 2008030500076 20080305 00076 NM 2008 3 5 QXEA200802084 1 20080101 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 208-222 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - CORROSION ON LEFT CENTER SEAT TRACK AROUND RIVETS AT APPROXIMATELY STATION X205 - X222. REMOVED SEAT T RACK AND INSTALLED NEW TRACK FROM STOCK IAW -8 200 SRM 51-40-11, RD8-53-4473 AND RD8-53-1102. 2 H 7 2 4T RT A13NM 2008030500080 20080305 00080 NM 2008 3 5 QXEA200800132 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 644 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - LEFT SEAT TRACK NR 15 BETWEEN FRAME 644.5 TO END OF TRACK HAS MULTIPLE CHAFES/GOUGES. REPAIRED IAW RD8 /4-53-884, Q400 NDTM PT-6 51-00-01, AND Q400 SRM 51-21-10. 2 H 7 2 4T RT A13NM 2008030500092 20080305 00092 NM 2008 3 5 QXEA200800133 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 725 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - SEAT TRACK IN CARGO PIT TRACK NR 9 HAS GOUGES IN CLEAT AT APPROXIMATELY STATION 725. REMOVED AND INSTA LLED NEW TRACK IAW Q400 SRM 51-40-15 AND 51-42-05. 2 H 7 2 4T RT A13NM 2008030500125 20080305 00125 NM 2008 3 5 QXEA200800145 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - NR 5 SEAT TRACK OUTBOARD FLANGE HAS CORROSION PITS BETWEEN STATION 1.0 AND 19.4 UNDERNEATH TRIANGULAR S UPPORT BRACKET. REMOVED AND INSTALLED NEW TRACK IAW Q400 SRM 51-42-05 AND 51-40-15. 2 H 7 2 4T RT A13NM 2008030500130 20080305 00130 CE 2008 3 5 0805301 1 20080222 A 2612 24405215 FIRE LOOP LEAR 35 31A 5170531 CE RT NACELLE MISALIGNED E CVGA O OTHER N FALSE WARNING AP APPROACH 1 GL 05 431DA 163 AT LOW POWER SETTING RIGHT ENGINE FIRE FLASHED INTERMITTENTLY. MAINTENANCE FINDING, FOUND FIREWALL SENSING ELEMENT PINC HED AGAINST RT UPPER ENGINE MOUNT. REPOSITIONED LOOP. PERFORMED ENGINE GROUND RUNS AND TAXI CHECKS. ACCOMPLISHED SEVE RAL ENGINE STARTS/SHUTDOWNS WITH NO FAULTS NOTED. FLIGHT TEST PERFORMED SATISFACTORILY. 2 L 7 2 4F RT A10CE 2008030500134 20080305 00134 NM 2008 3 5 QXEA200800160 1 20080130 A 5340 FITTING DHAV DHC8 DHC8202 2809007 NM MLG ACTUATOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - RIGHT MLG RETRACTION ACTUATOR FITTING HAS CORROSION ON FRAME JUST ABOVE TOP BOLT HOLE IN CENTER. REPAI RED IAW DHC8 200 RD8-54-1178, NDTM PT-6 51-00-01, PT-1 51-00-04. 2 H 7 2 4T RT A13NM 2008030500137 20080305 00137 NM 2008 3 5 QXEA200800118 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 584 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - FOUND MINOR CORROSION ON LEFT INBOARD SEAT TRACK, FORWARD OF FRAME 584.5. REPAIRED IAW RD8/4-53-884, Q 400 NDTM PT-6 51-00-01. 2 H 7 2 4T RT A13NM 2008030500147 20080305 00147 NM 2008 3 5 QXEA200800181 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 264 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - AT APPROXIMATELY STATION X264 THE LEFT INBOARD SEAT TRACK NR 4 HAS CORROSION ON TOP OF TRACK. REMOVED SEAT TRACK AND INSTALLED NEW TRACK IAW DHC 8 200 SRM 51-40-11, 51-40-00, RD 8-53-1102, AND RD 8-53-4473. 2 H 7 2 4T RT A13NM 2008030500171 20080305 00171 NM 2008 3 5 QXEA200800213 1 20080208 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 682 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - SUSPECT CORROSION ON RIGHT INBOARD SEAT TRACK, TOP OUTBOARD SIDE AT APPROXIMATELY STATION X682. REMOVE D SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW Q400 RD 8/4-53-884, AND Q400 SRM 51-42-05, 51-40-15. 2 H 7 2 4T RT A13NM 2008030500186 20080305 00186 NM 2008 3 5 QXEA200802075 1 20080101 A 5310 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - CORROSION ON NUT PLATE UNDER SIDE AT STATION 580.50 LEFT SIDE LOOKING THROUGH ACCESS PANEL 144FZ. REPA IRED IAW -8 CPC CHAPTER 4 STEP 8 AND -8 200 SRM 51-20-11, 51-40-11, 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2008030500193 20080305 00193 NM 2008 3 5 QXEA200800186 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 565 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - NR 9 SEAT TRACK INBOARD AND OUTBOARD FLOORBOARD SUPPORT MOUNT FLANGE SUSPECTED CORROSION AT STATION X56 5.00. REPAIRED IAW DHC 8 200 RD8-53-784, NDTM PT-6 51-00-01, AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008030500194 20080305 00194 NM 2008 3 5 QXEA200802096 1 20080101 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM RT WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - RIGHT WING LOWER SKIN DOUBLER HAS NUMBEROUS SMALL GOUGES IN AN AREA APPROXIMATELY 8" BY 1" LOCATED AT Y W225 AND 10" AFT OF MAGNA STICK. REPAIRED IAW RD8-57-2996, 1-82-7A PT 6 51-00-02, 1-82-7A PT 1 51-00-05 AND RD8-57-382 1, AND -8 200 SRM 51-20-16. 2 H 7 2 4T RT A13NM 2008030500196 20080305 00196 NM 2008 3 5 QXEA200800183 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - SEAT TRACK NR 7 HAS CORROSION ON THE TOP BETWEEN STA Y213 TO Y240. REMOVED SEAT TRACK AND INSTALLED NE W TRACK IAW DHC 8 200 SRM 51-40-11, AND RD 8-53-1102. 2 H 7 2 4T RT A13NM 2008030600012 20080306 00012 CE 2008 3 6 021408458F 1 20080214 A 3260 99124655 DOWNLOCK SWITCH CESSNA 500 550 2076604 CE LT MLG MALFUNCTIONED E T6FA L ABORTED APPROACH N FALSE WARNING DE DESCENT 1 GL 09 458F 2721 2139 5500986 DURING THE APPROACH INTO PALWAUKEE (PWK), THE GEAR HANDLE WAS SELECTED TO THE DOWN POSITION TO EXTEND THE GEAR. AFTER T HE GEAR EXTENDED IT WAS NOTED THAT THE LEFT MAIN GEAR GREEN DOWN AND LOCK LIGHT WAS NOT ILLUMINATED. THE GEAR WAS CYCLE D UP AND DOWN TWICE, AND AFTER THE SECOND EXTENSION THE EMERGENCY GEAR EXTENSION SYSTEM WAS DEPLOYED TO ENSURE THAT THE GEAR WAS DOWN AND LOCKED. THE GREEN LIGHT DID NOT COME ON. THE PILOTS DIVERTED TO O’HARE (ORD), AND AS THE LEFT GEAR C ONTACTED THE RUNWAY THE LIGHT ILLUMINATED. THE AIRCRAFT WAS INSPECTED AND ISSUED A SPECIAL FLIGHT PERMIT AND REPOSITION ED TO GRAND RAPIDS (GRR) WITH THE GEAR DOWN. 1 L 7 2 4F A22CE 2008030600016 20080306 00016 SO 2008 3 6 RAIA00802018 1 20080217 A 3350 RPS1B BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 833HK 145240 PRE FLT 7987 - RIC - SEVERAL EMERGENCY LIGHTS IN CABIN WILL NOT SHUT OFF. MAINTENANCE REMOVED AND REPLACED THE NR 2 EME RGENCY LIGHT BATTERY. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008030400058 20080304 00058 NM 2008 3 4 DL757080195 1 20080213 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM BS 620 S16L PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 619DL 22909 FUSELAGE SKIN PUNCTURED AFT OF STA 620 ABOVE STER 16L. ADJACENT SKIN REPAIR REMOVED AND BOTH CUTOUTS REPAIR WITH A DOUB LER. 2 L 7 2 4F RT A2NM 2008030400078 20080304 00078 2008 3 4 2008UALA00859 4 20080215 A 2565 SLIDE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LT OVERWING FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 852UA 1671 LT OFFWING SLIDE HAS DELAMINATION FOUR INCHES LONG AT AFT EDGE IN AREA. REPLACED LT OVERWING SLIDE 2 L 7 2 4F 4 F RT A28NM E40NE 2008030400079 20080304 00079 2008 3 4 SWIA200819219 2 20080211 A 7230 COMPRESSOR CNDAIR CL600 CL6002B19 1900309 EA ENGINE SMOKE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 932SW 7714 FLT NR 5833. SHORTLY AFTER TAKEOFF, RECEIVED SMOKE TOILET CAUTION MESSAGE, PERFORMED COMPRESSOR WASH ON BOTH ENGINES TO REMOVE DEICE FLUID FROM ENGINES IAW AMM 72-00-00. 2 L 7 2 4F RT A21EA 2008030400090 20080304 00090 NM 2008 3 4 HALA0800258 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1319 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON SEAT TRACK CROWN/BASE AT 88.5, STA 1319, AREA HAS BEEN REWORKED BEFORE. REPLACED SEAT TRACK PER SR M. 2 L 7 2 4F RT A1NM 2008030400091 20080304 00091 NM 2008 3 4 HALA0800251 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON SEAT TRACK CROWN/BASE AT LBL 88.5, STA 1197+144, AREA HAS BEEN REWORKED BEFORE. SEAT TRACK WAS REP LACED PER SRM. 2 L 7 2 4F RT A1NM 2008030400097 20080304 00097 NM 2008 3 4 HALA0800208 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 818 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS, AT LBL 88.5, STA 818, MAX DEPTH OF BLEND WAS 0.012". BLEND IAW SRM 51-10-02. ALL BLEND OUTS WITHIN SRM 53-00-52 LIMITS. 2 L 7 2 4F RT A1NM 2008030400115 20080304 00115 NM 2008 3 4 HALA0800185 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION AT RBL 54.75, SEAT TRACKS AT STA 1197+85, BASE OF TRACK. CORROSION REMOVED PER SRM 51-10-02, REV 76 A ND SRM 53-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030400186 20080304 00186 NM 2008 3 4 HALA0800104 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1015 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45, SEAT TRACKS, AT RBL 11, STA 1015. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW S RM 51-10-02,REV 75, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101 REV 76. 2 L 7 2 4F RT A1NM 2008030400195 20080304 00195 NM 2008 3 4 2008UALA00877 1 20080215 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 344 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 51315 24657 FUSELAGE STRINGER END FITTING, STRAP ACROSS TOP IS CRACKED, BS 344.5 STR 16L. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW STRAP. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030500040 20080305 00040 NM 2008 3 5 QXEA200802091 1 20080101 A 5320 PLATE DHAV DHC8 DHC8202 2809007 NM BS 182 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - CORROSION AT LOWER AFT LIP OF CENTER AISLE KICK PLATE AT STATION 182.00. REMOVED KICK PLATE AND FABRIC ATED NEW KICK PLATE AND INSTALLED FABRICATED KICK PLATE IAW T/C 2-53-829 AND -8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008030500049 20080305 00049 NM 2008 3 5 QXEA200800121 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 624 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - FOUND MINOR CORROSION ON LEFT INBOARD SEAT TRACK 4" FORWARD OF FRAME 624.5. REPAIRED IAW RD8/4-53-884, Q400 NDTM PT-6 51-00-01. 2 H 7 2 4T RT A13NM 2008030500060 20080305 00060 NM 2008 3 5 QXEA200800128 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 547 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - LEFT SEAT TRACK NR 7 BETWEEN FRAME 547.0 TO END OF TRACK HAS MULTIPLE CHAFES/GOUGES. REPAIRED IAW RD8/ 4-53-884, Q400 NDTM PT-6 51-00-01, AND Q400 SRM 51-21-10. 2 H 7 2 4T RT A13NM 2008030500091 20080305 00091 NM 2008 3 5 QXEA200800149 1 20080119 A 5411 FRAME BOMBDR DHC8 DHC8402 1390042 NM RT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - THE OUTBOARD LOWER COWL ATTACH LUG ON THE RIGHT NACELLE FORWARD FRAME IS CHAFED. REPAIRED IAW -8 Q400 RD8/4-54-232 AND Q400 NDTM PT-6 51-00-01. 2 H 7 2 4T RT A13NM 2008030500115 20080305 00115 NM 2008 3 5 QXEA200800138 1 20080119 A 5220 SKIN BOMBDR DHC8 DHC8402 1390042 NM ESCAPE HATCH DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - SMALL DENT ON EXTERNAL SKIN OF COCKPIT ESCAPE HATCH. FOUND DIMENSION AND LOCATION OF DENT ARE WITHIN L IMITS IAW Q400 SRM 53-00-00 REPAIR 02, PG 201 PARA 2A. INSPECTED IAW Q400 NDTM PT-6 51-00-01, NO CRACKS NOTED. PAINTED IAW Q400 SRM 51-25-05. 2 H 7 2 4T RT A13NM 2008030500133 20080305 00133 NM 2008 3 5 QXEA200800151 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 350-356 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - AT APPROXIMATELY STA X350 TO X356 LEFT OUTBOARD SEAT TRACK NR 1 HAS GOUGES ON THE TOP AT THE INBOARD ED GE. REPAIRED IAW DHC8 200 RD8-53-1342, NDTM PT-6 51-00-01, AND DHC8 200 SRM 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2008030500148 20080305 00148 NM 2008 3 5 QXEA200800192 1 20080130 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAPS DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - THERE IS ONE DIVOT ON THE UPPER SIDE OF THE OUTBOARD LOWER FLANGE OF THE RIGHT NR 4 FLAP TRACK. REPAIR ED IAW DHC8 200 RD8-57-988, NDTM PT-6 51-00-01. 2 H 7 2 4T RT A13NM 2008030500161 20080305 00161 NM 2008 3 5 QXEA200800165 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 582 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - NR 9 SEAT TRACK INBOARD AND OUTBOARD FLOORBOARD SUPPORT MOUNT FLANGES SUSPECTED CORROSION AT STATION X5 82.00. REPAIRED IAW DHC8 200 RD8-53-784, NDTM PT-6 51-00-01 AND DHC8 200 SRM 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 2008030500174 20080305 00174 NM 2008 3 5 QXEA200800163 1 20080130 A 5410 BRACKET DHAV DHC8 DHC8202 2809007 NM NR 2 NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - NR 2 ENGINE COWLING NR 3 BRACKET ON INBOARD SIDE IS CHAFED. REMOVED FIRE SEAL BRACKET FROM LOWER COWL AND INSTALLED NEW FIRE SEAL BRACKET IAW DHC8 200 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2008030500181 20080305 00181 NM 2008 3 5 QXEA200802092 1 20080101 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 405 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - RIGHT OUTBOARD SEAT TRACK HAS LIGHT SURFACE PITTING AT APPROXIMATELY X405.737. REMOVED SEAT TRACK AND INSTALLED NEW TRACK FROM STOCK IAW -8 200 SRM 51-40-00, 51-40-11. 2 H 7 2 4T RT A13NM 2008030500198 20080305 00198 NM 2008 3 5 QXEA200800185 1 20080130 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 545 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - NR 6 SEAT TRACK INBOARD FLOORBOARD MOUNT FLANGE, SUSPECTED CORROSION FROM STA X545.00 - X600.00. REPAI RED IAW DHC 8 200 RD8-53-784, NDTM PT-6 51-00-01 AND SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008030600025 20080306 00025 SO 2008 3 6 C2XA08RI019 1 20080221 A 3350 78211 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16963 145116 RIC - DURING ROUTINE MAINTENANCE, MX FOUND EXIT ROW LIGHT AT SEAT 12C INOPERATIVE. MX REMOVED AND REPLACED NR 5 INVERTE R IAW EMB145 AMM 33-50-11 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008030600026 20080306 00026 SO 2008 3 6 C2XA08RI020 1 20080214 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO NR 2 MALFUNCTIONED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 13978 20143 145180 FLIGHT 2985 - EWR - CREW REPORTED LAV SMOKE AND SMOKE IN THE CABIN DURING TAKEOFF. CREW PERFORMED AIR RETURN AND LANDED AIRCRAFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED NR 2 ACM IAW EMB 145 AMM 21-51-03 AND PERFORMED OPERATIONAL CHECK S UCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008030600027 20080306 00027 SO 2008 3 6 C2XA08RI021 1 20080218 A 3234 8271013 CONTROL LEVER EMB 145 EMB145EP 3260221 SO COCKPIT FAULTY A C2XA K NONE O OTHER TO TAKEOFF 1 SW 27 14947 20620 145054 FLIGHT 2823 - EWR - CREW REPORTED LANDING GEAR DID NOT RETRACTED AT FIRST ATTEMPT AFTER TAKEOFF. LANDING GEAR RETRACTED ON THE THIRD ATTEMPT. EWR MX REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW EMB145 AMM 32-32-02 AND PERFORMED OPE RATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. NOTE: MX ALSO REMOVED AND REPLACED LGEU, SEE SDR C2XA08RI022. 2 L 7 2 4F RT T00011AT 2008030600031 20080306 00031 EU 2008 3 6 FX7A200800001 1 20080128 A 3350 LIGHT SCHLER ASW20 ASW20 3801506 EU CABIN INOPERATIVE A FX7A K NONE L NO TEST IN INSP/MAINT 1 SO 19 905 20494 FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE FROM ROW 6 FORWARD. 1 K 0 0 EXPA1K00 2008030600038 20080306 00038 EU 2008 3 6 UPS08151692 1 20080220 A 2560 POWER SUPPLY AIRBUS A300 A300F4622R 3930360 EU COCKPIT DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 173UP 0005 INSPECTION TYPE:N/A EVACUATION SLIDE WARNING SYSTEM LIGHT ON CABIN DOOR INOP. BUZZER DOES NOT WORK. DEFERRED EVACUATIO N SLIDE WARNING SYSTEM LIGHT IAW MEL 52-73-001-1. REMOVED AND REPLACED AUTONOMOUS PWR SUPPLY UNIT IAW MM 52-73-18-04. OPS CHECK GOOD IAW 52-73-00-05. THIS CLEARS M369580. 2 L 7 2 4F RT A35EU 2008030600040 20080306 00040 WP 2008 3 6 UPS08851696 1 20080221 A 2913 PUMP DOUG DC8 DC873F 302199F WP NR 2 ENGINE FAILED A IPXA O OTHER K FLUID LOSS DE DESCENT 1 SO 01 803UP 46073 INSPECTION TYPE:N/A HYDRAULIC FAILURE. ON DESCENT HYD QTY WAS NOTED TO HAVE DROPPED TO THE AUX LEVEL. APPROPRIATE CHEC K LIST ACCOMPLISHED. REMOVED AND REPLACED NR 2 ENG DRIVEN HYD PUMP ASSY PER MM 29-10-12-2. 2 L 7 4 4F RT 4A25 2008030600045 20080306 00045 WP 2008 3 6 UPS08851702 1 20080109 A 5720 56139123 WEB DOUG DC8 DC871F 302199D WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 NR 1 MAIN WEB CRACK BETWEEN XRS 255 AND XRS 250. REPAIRED NR 1 MAIN WEB CRACK BETWEEN XRS 255 AND XR S 250 IAW EO DC8-5710 -28478-B AND EA 008-5710-01-A1261. 2 L 7 4 4F RT 4A25 2008030600054 20080306 00054 NM 2008 3 6 ZZDA2008070 1 20080218 A 5230 PAN BOEING 717 717200 1383700 NM AFT CARGO DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 987AT 55088 WHILE PREPARING TO TAXI A/C FOUND AFT PIT DOOR FWD PAN CRACKED. FABRICATED .063" 2024-T42 REPAIR ANGLE AND .050" 301 1/ 2 HARD DOUBLER. INSTALLED REPAIR PARTS WITH HLT 434-6 AND HLT 334-6 REFERENCE EA 17-52-01010IR AND SRM CHAPTER 51. 2 L 7 2 4F TR A6WE 2008030600055 20080306 00055 SO 2008 3 6 C2XA08ON094 1 20080220 A 5532 14551187401 SKIN EMB 145 EMB145XR 3260214 SO VERTICAL STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 22909 15774 15774 145459 FLT 7754 - LAX - WHILE PERFORMING ROUTING CHECK INSPECTION MX PERSONNEL FOUND A TEAR ON VERTICAL STAB SKIN 35MM FROM END OF SKIN AT ZV935.00MM TO RIVET ON LOWER PROFILE CHANNEL. ENGINEERING INFORMS A FLY BY FOR NEXT 500FC IS ACCEPTABLE PRO VIDED: - THERE IS NO BENT PARTS ON TORN REGION AND THE EDGE OF VERTICAL STABILIZER IS FOUND SMOOTH (FREE OF BENT/LIFTED EDGE). DETAILED VISUAL INSPECTION IS MADE EVERY 200FC (TWO HUNDRED FLIGHT CYCLES) TO CERTIFY THE DAMAGE HAS NOT GROWN; IN ORDER TO PROVIDE THE FINAL REPAIR STATEMENT EMBRAER REQUESTS A MAP OF AFFECTED REGION SHOWING. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE ON DMI CONTROL #723563 CLASS A REINSPECT AND CONTROL #723560. 2 L 7 2 4F RT 2008030600056 20080306 00056 GL 2008 3 6 C2XA08ON095 2 20080219 A 7530 2305591728 DUCT CLAMP EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL ENGINE DEFECTIVE A C2XA D RETURN TO BLOCK M OVER TEMP CL CLIMB 1 SW 27 11189 6867 6867 14500931 CAE312842 FLT 22 ONT - FLIGHT CREW REPORTED ON CLIMB FROM ONT-E2 HIGH ITT - CANNOT MAINTAIN POWER. FLIGHT CREW RETURNED TO BLOCK AND DID NOT DECLARE AN EMERGENCY AND LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED 14TH STAGE COMPRESSOR DISCHARGE TUBE V-BAND CLAMP OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2008030600059 20080306 00059 NM 2008 3 6 2008UALA00921 1 20080219 A 3397 59191 CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 339UA 24243 EEL LIGHTS INOP ROWS 12-14. REPLACED CABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030600067 20080306 00067 NM 2008 3 6 2008UALA00961 1 20080220 A 2560 GIRT BAR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L2 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 904UA 25004 THE 2L GIRT BAR WON`T STAY IN HOLDER DE-ARM POSITION. REPACKED SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030600068 20080306 00068 NM 2008 3 6 2008UALA00962 1 20080220 A 5510 TEE FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZONTAL STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 RT HORIZONTAL STAB L/E FWD SPAR UPPER TEE IS CRACKED IN RADIUS, FROM 41"-48" FROM OUTBOARD END. MAJOR REPAIR: FABRICATE D AND INSTALLED NESTED ANGLE REPAIR DOUBLERS ON EACH SIDE OF UPPER TEE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030600069 20080306 00069 NM 2008 3 6 2008UALA00968 1 20080220 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 671UA 30026 FUSELAGE DAMAGE AT APPROX STR 32LT STA 610 DENT APPROX .097 DEEP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030600072 20080306 00072 SO 2008 3 6 C2XA08SH037 1 20080224 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18557 145596 SHV - DURING C-CHECK EMERGENCY LIGHT (PROXIMITY) INOP AFT OF WING BOX. MAINTENANCE REMOVED AND REPLACED AFT EMERGENCY L IGHT BATTERY OF WING BOX IAW EMB 145 AMM 33-50-04, OP'S CHECK GOOD. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008030600075 20080306 00075 SO 2008 3 6 C2XA08SH039 1 20080224 A 5512 14532235602 SKIN EMB 145 EMB145LR 3260212 SO HORIZ STAB CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18557 145596 SHV - DURING C-CHECK RT HORIZONTAL STAB L/E HAS CORROSION ON SKIN AND AROUND RIVET & SCREW HOLE. MX REPAIRED RT HORIZON TAL STAB L/E ON SKIN AND AROUND RIVET & SCREW HOLE IAW EC 5510-01179 AND EC 5530-01116. THE AIRCRAFT WAS APPROVED TO RE TURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008030600077 20080306 00077 NM 2008 3 6 UPS08551705 1 20080201 A 5311 146N1004 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 459UP 25480 INSPECTION TYPE:C2 FRAME DENTED AT BS 1260, STR 26-27R. REPAIRED PER SRM 53-00-07, SRM 51-70-11-0G. 2 L 7 2 4F RT A2NM 2008030600078 20080306 00078 NM 2008 3 6 UPS08651703 1 20080219 A 3350 SWITCH BOEING 767 76734AF 1385212 NM COCKPIT DEFECTIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 323UP 27749 INSPECTION TYPE:N/A EMERGENCY LIGHTS SWITCH ON OVERHEAD PANEL DOES NOT WORK PROPERLY. OPS CHECK EMERGENCY LIGHT SWITCH IAW MM 33-51-00, OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2008030400148 20080304 00148 NM 2008 3 4 DLM88080261 1 20080213 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 959DL 49978 DURING MC THREE CRACKS WITH .031", .031" AND .046" LENGTH WERE FOUND ON FUSELAGE SKIN AT STA Y=191 AND Y=197 NEXT TO LON GERON 22LH. A PERMANENT REPAIR WAS PERFORMED IAW EA 09-069085-12AD REV DME-02 IN COMPLIANCE WITH AD 98-17-06. 2 L 7 2 4F RT A6WE 2008030400155 20080304 00155 NM 2008 3 4 DLM90080232 1 20080218 A 5313 5936667 LONGERON DOUG MD90 MD9030 3023690 NM BS 1344-1364 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 AFT CARGO BAY LONGERON 29L BETWEEN STA.1344 AND 1364 CORRODED. REMOVED AND REPLACED CORRODED LONGERON SECTION, IAW MD90 SRM 51-30-02, 51-30-05 AND 53-10-01 FIG 7. 2 L 7 2 4F RT A6WE 2008030400164 20080304 00164 NM 2008 3 4 HALA0800192 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1307 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION RBL 54.75, SEAT TRACKS AT STA 1307, BASE OF TRACK. CORROSION REMOVED PER SRM 51-10-02, REV 76 AND SRM 53-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030400171 20080304 00171 NM 2008 3 4 F3LA200800051 1 20080210 A 5320 D53974968004 COVER AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 902FR 5546 1515 DURING C7 C CHECK, INSPECTION REPORTED SURFACE CORROSION WAS FOUND AROUND THE RIGHT CARGO NET HOLD DOWN BRACKET ON THE C OVER PROFILE, UNDER THE FLOORBOARDS OF THE AFT CARGO PIT, AT FRAME 58. MAINTENANCE REMEDIATED THE SURFACE CORROSION ON THE COVER PROFILE, FABRICATED AND INSTALLED A NEW DOUBLER IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30026. UPON COMPLETION OF THE MAINTENANCE ACTION, THE REPAIR WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008030400176 20080304 00176 NM 2008 3 4 HALA0800102 1 20080110 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 978-987 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 LEVEL 1 CORROSION SECTION 45 SEAT TRACK, AT STA 978-987. CORROSION REMOVED, CONFIRMED BY 10X MAGNIFICATION IAW SRM 51-1 0-02, REV 76, BLENDED WITHIN LIMITS IAW SRM 53-00-52/101 REV 76. 2 L 7 2 4F RT A1NM 2008030400179 20080304 00179 NM 2008 3 4 2008UALA00873 1 20080217 A 5340 ATTACH ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 50863 24641 STRINGER 12R INTERCOSTAL ATTACH ANGLE CRACKED BS 294. REMOVED & REPLACED CRACKED ATTACH ANGLE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030400180 20080304 00180 NM 2008 3 4 2008UALA00912 1 20080218 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 AT 1 + 30 AFTER TAKEOFF EMERGENCY LIGHTS IN ZONE A RIGHT SIDE CAME ON, INCLUDING DOOR 1R. REPLACED EMER LT BATTERY PACK . TESTS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030400197 20080304 00197 NM 2008 3 4 2008UALA00879 1 20080215 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FUSELAGE SKIN CRACKED AT 1 FASTENER HOLE ABOVE AND 2 FASTENER HOLES BELOW FORWARD ENTRY DOOR LOWER HINGE CUT-OUT. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED EXTERNAL DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030400200 20080304 00200 WP 2008 3 4 08FDEA00579 1 20080222 A 5753 ATTACH FITTING DOUG DC10 DC1030F 3023504 WP TE FLAPS DAMAGED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 317FE 46835 DURING DEPARTURE, PRIOR TO FLAPS RETRACTION RIGHT FLAP TAPES MOVED FROM 20 PERCENT TO 28 PERCENT. AIRCRAFT REQUIRED SIG NIFICANT RT AILERON TO KEEP WINGS LEVEL. ON ARRIVAL AT KMEM, A CONTROLLABILITY CHECK WAS PERFORMED WHEN FLAPS WERE EXTE NDED TO 22' RIGHT FLAP TAPE INDICATED 30 AND 3/4 RIGHT LATERAL CONTROL WAS REQUIRED TO MAINTAIN WINGS LEVEL. FLAPS WER E RETRACTED AND A O EXT APPROACH AND LANDING WAS ACCOMPLISHED WITHOUT INCIDENT. REMOVED AND REPLACED ATTACH FITTING F ROM RT O/B FLAP O/B HINGE BRACKET ASSY IN REF TO SRM 51-31-01 VOL2 51-33-01 VOL2 AND 51-35-01 VOL2. 2 L 7 3 4F RT A22WE 2008030500075 20080305 00075 NM 2008 3 5 QXEA200802072 1 20080101 A 5730 SKIN DHAV DHC8 DHC8202 2809007 NM WING BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - APERTURE FOR PANEL 522AT HAS A BROKEN NUT PLATE LEFT HAND CORNER. REMOVED BROKEN NUTPLATE FOR PANEL 52 2AT AND REPLACED WITH NEW NUTPLATE FROM STOCK. 2 H 7 2 4T RT A13NM 2008030500100 20080305 00100 NM 2008 3 5 QXEA200800146 1 20080119 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM BS 281-301 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - AFT OF RIGHT ICE SHIELD BETWEEN STR 16P AND 19P AND APPROXIMATELY BETWEEN X281 AND X301 ARE NUMEROUS DE NTS NOT IDENTIFIED ON AIRCRAFT DAMAGE YELLOW DOTS. REPAIRED IAW Q400 NDTM PT-6 51-00-01, AND RD8/4-53-2237. 2 H 7 2 4T RT A13NM 2008030500141 20080305 00141 NM 2008 3 5 QXEA200800197 1 20080208 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 200 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - NR 18 SEAT TRACK HAS AN AREA OF CORROSION INSIDE TRACK AT STATION X200.000. REMOVED SEAT TRACK AND INS TALLED NEW SEAT TRACK IAW Q400 SRM 51-40-15, 51-40-07, 51-42-05, AND 51-42-45. 2 H 7 2 4T RT A13NM 2008030500159 20080305 00159 NM 2008 3 5 UIEA200800049 1 20080215 A 5754 STRUCTURE BOEING 747 7472D7B 1384803 NM KRUEGER FLAP CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 NR 15 KRUEGER FLAP UPPER BACKUP STIFFENER REPAIRED DOUBLER CRACKED AT OUTBOARD HINGE SUPPORT AREA. REPLACED EXISTING RE PAIR DOUBLER IAW SRM 51-10-01. 2 L 7 4 4F RT A20WE 2008030500165 20080305 00165 NM 2008 3 5 UIEA200800060 1 20080215 A 5330 SKIN BOEING 747 7472D7B 1384803 NM ZONE 100 SCRATCHED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 PERFORMED EO 4753B100 FOUND SCRIBE LINE DISCREPANCY. REPAIRED LAP JOINT PER ATLAS EO 4753B106. 2 L 7 4 4F RT A20WE 2008030500183 20080305 00183 NM 2008 3 5 QXEA200802095 1 20080101 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM RT TE FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX- C5 CHECK - RIGHT FLAP TRACK HAS 4 WORN SPOTS ON THE LOWER INBOARD TRACK, BOTTOM OF THE TRACK. REPAIRED TRACK IAW R D8-57-988. 2 H 7 2 4T RT A13NM 2008030600080 20080306 00080 WP 2008 3 6 UPS08851687 1 20080216 A 5320 BEAM DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:N/A AFT PRESS BULKHEAD J BEAM CRACKED. REMOVED FASTENERS 6" L & R OF BL 0 FOR ACCESS FOR FOM. REPAIRED PER EO DC8-5310-6598-C. MATCH DRILLED 3 REPAIR ANGLES AND CLIPS. ACCOMPLISHED APPENDIX B STEPS 7 - 12. 2 L 7 4 4F RT 4A25 2008030600090 20080306 00090 SO 2008 3 6 RAIA00802020 1 20080218 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 829HK 145281 PRE FLT 7979 - MLI - EMERGENCY LIGHTS INOP IN AFT CABIN. MAINTENANCE RESECURED THE CONNECTOR AND PERFORMED AN OPERATION AL CHECK OF THE LIGHTS WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008030600093 20080306 00093 SO 2008 3 6 C2XA08TY031 1 20080225 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14960 145100 THE AFT FACING PORTION OF THE CEILING EMERGENCY EXIT SIGN AT SEAT 12 IS INOP. RESECURED THE CONNECTOR, OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008030600094 20080306 00094 SO 2008 3 6 C2XA08CL022 1 20080220 A 3310 2LA00626500 LIGHT EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 16918 145397 CLE FLIGHT 2080 - THE CREW REPORTD COCKPIT READING LIGHT CIRCUIT BREAKER H-11 POPPED IN FLIGHT. ALSO REPORTED A BURNING SMELL. MAINTENANCE INSPECTED AND RELEASED AIRCRAFT IAW MEL 25-12-02. SUPPLEMENT TO FOLLOW. MAINTENANCE REPLACED THE CAPTAIN`S READING LIGHT ASSEMBLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008030600102 20080306 00102 NM 2008 3 6 SWAA081049 1 20080225 A 3350 1619 LIGHT BOEING 737 7375H4 138449D NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008030600107 20080306 00107 NM 2008 3 6 SWAA081053 1 20080225 A 3350 147A5701 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008030600108 20080306 00108 2008 3 6 SWAA081052 4 20080225 A 2565 61620468 HANDLE BOEING 737 7373H4 1384600 NM EVAC SLIDE MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE MANUAL INFLATION HANDLE MISSING. REMOVED AND REPLACED EV AC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008030600109 20080306 00109 2008 3 6 SWAA081054 4 20080225 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008030600110 20080306 00110 2008 3 6 SWAA081055 4 20080225 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 763SW 27877 R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008030600112 20080306 00112 NM 2008 3 6 2008UALA00928 1 20080218 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 530UA 25043 LIGHT BAR (EEL) AT K-LAV IS INOP. INTERNAL SHORTING. REPLACED LIGHT BAR (EEL) AT K LAV LOCATION. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030600115 20080306 00115 NM 2008 3 6 2008UALA00940 1 20080219 A 3350 20131 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 530UA 25043 EMERGENCY LIGHT BATTERY PACK M10567 IS INOP. DATA UPDATE CAUSE: BATTERY FAILURE. REMOVED AND REPLACED BATTERY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030600116 20080306 00116 NM 2008 3 6 2008UALA00941 1 20080219 A 3350 M10699 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 530UA 25043 EMERGENCY LIGHT BATTERY PACK M10699 IS INOP. BATTERY FAILURE. REMOVED AND REPLACED BATTERY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030600118 20080306 00118 NM 2008 3 6 2008UALA00956 1 20080220 A 2612 FIRE LOOP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 ENGINE OUT OF POSITION A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 824UA 965 FIRE LOOP A FAULT DISPLAYED ON UPPER ECAM SCREEN ENG 2. FOUND LOOP TOUCHING METAL FRAME IN ENGINE. REPOSITIONED LOOP T O CORRECT POSITION, OPS TESTED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030600120 20080306 00120 EU 2008 3 6 2008UALA00958 1 20080220 A 3350 D9239003500060 EPSU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MALFUNCTIONED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 473UA 1469 WHILE PERFORMING EMERGENCY LIGHTING CHECK RECEIVED CODE (EPSU BATT FAULT-R). EPSU FAILURE. REPLACED EPSU. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030600121 20080306 00121 EU 2008 3 6 2008UALA00959 1 20080221 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE O2 SYSTEM LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 441UA 751 THE O2 NEEDS SERVICING. SHOWS 1420 PSI. SERVICED CREW O2 LEVEL TO FULL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030500187 20080305 00187 NM 2008 3 5 QXEA200802077 1 20080101 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - LAST NUT PLATE ON RIGHT CENTER SEAT TRACK AT STATION 600.0 HAS CORROSION ON THE UNDER SIDE. REMOVED AN D INSTALL NEW NUTPLATE IAW -8 200 SRM 51-40-00. 2 H 7 2 4T RT A13NM 2008030600020 20080306 00020 SO 2008 3 6 C2XA08CL021 1 20080218 A 2400 860CC01KOO80 RELAY EMB 145 EMB145LR 3260212 SO ELECTRICAL SYS FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 12924 145311 CLE FLIGHT 2793 - THE CREW REPORTED MULTIPLE WARNINGS DURING CLIMB E1 FUEL LO LEVEL, AMBER DASHES ON FUEL TOTAL + TANK 2 FUEL LEVELS, RMU NR 2 BLANK, APU SHUTOFF VALVE CLOSED, AURAL WARNING FLAP FAIL, AUTO PILOT FAIL. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. ON GROUND, RECEIVED ESS BUS 2 FAIL, STICK SHAKER, AND GUSTLOCK FAIL. MAINTENANCE INSPECTED AND REPLACED CONTACTOR RELAYS KOO80 AND K0016. OPERATIONAL CHECKS OF THE DC DISTRIBUTION WERE GOOD. KO016 P/ N 464CC01. 2 L 7 2 4T RT T00011AT 2008030600024 20080306 00024 NM 2008 3 6 MWEA080034 1 20080220 A 3350 6011779 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 910ME 55174 LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS ARE NOT ILLUMINATING. REMOVED AND REPLACED EMERGENCY BATTERY PACK. 2 L 7 2 4F TR A6WE 2008030600028 20080306 00028 SO 2008 3 6 C2XA08RI022 1 20080218 A 3230 355022002MOD3 ELECTRONIC UNIT EMB 145 EMB145EP 3260221 SO E&E BAY MALFUNCTIONED A C2XA K NONE O OTHER TO TAKEOFF 1 SW 27 14947 13334 8943 145054 FLIGHT 2823 - EWR - CREW REPORTED LANDING GEAR DID NOT RETRACTED AT FIRST ATTEMPT AFTER TAKEOFF. LANDING GEAR RETRACTED ON THE THIRD ATTEMPT. EWR MX REMOVED AND REPLACED LANDING GEAR ELECTRONIC CONTROL (LGEU) IAW EMB145 AMM 32-32-01 AND P ERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. NOTE: MX ALSO REMOVED AND REPLACE D L/G CONTROL LEVER. SEE SDR C2XA08RI021. 2 L 7 2 4F RT T00011AT 2008030600029 20080306 00029 SO 2008 3 6 C2XA08RI023 1 20080118 A 3350 1317 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13118 145675 EWR - DURING ROUTINE MAINTENANCE, MX FOUND EMERGENCY LIGHT AT 12C SEAT INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY L IGHT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2008030600034 20080306 00034 SO 2008 3 6 C2XA08SH035 1 20080221 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18557 145596 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MAINTENANCE REMOVED AND REPLACED THE A FFECTED OMEGA BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008030600053 20080306 00053 SW 2008 3 6 PNSA080202 1 20080219 A 3220 UNKNOWN SWRNGN SA227 SA227AC 8780603 SW NLG DIRTY A PNSA K NONE J WARNING INDICATION CL CLIMB 1 AL 03 640PA AC759B DURING A CHECK FLIGHT FOR A RT ENGINE CHANGE THE NOSE GEAR WOULD NOT STAY IN THE UPLOCK POSITION. AFTER THE CHECK FLIGH T THE MX DEPARTMENT CLEANED AND LUBED THE NOSE GEAR AND PERFORMED AN OP CHECK, NORMAL. 2 L 7 2 4T RT A8SW 2008030600064 20080306 00064 EU 2008 3 6 2008UALA00935 1 20080218 A 3510 RCF6705 REGULATOR VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 427UA 512 COCKPIT OXYGEN BOTTLE - LOW CREW COMMENTS: COCKPIT OXYGEN PRESSURE SLOW LEAK LOSING 100 PSI - HOUR IN FLT. LEAK AT PRE SSURE REGULATOR. REPLACED PRESSURE REGULATOR, SERVICED CREW O2, LEAK CHECKED SYSTEM, ALL OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030600065 20080306 00065 NM 2008 3 6 2008UALA00938 1 20080219 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 SEAT 4E AFT EEL INOP. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030600079 20080306 00079 NM 2008 3 6 UPS08651708 1 20080221 A 2761 ACTUATOR BOEING 767 76734AF 1385212 NM NR 6 SPOILER LEAKING A IPXA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 SO 01 326UP 27752 INSPECTION TYPE:N/A DIVERSION - LEFT HYD QTY DECREASED TO ZERO AND SYSTEM PRESSURE AND QTY LIGHTS ILLUM, EICAS MSG LEFT HYD SYSTEM PRESS AND LEFT HYD QTY DISPLAYED. COMPLIED WITH QRH PROCEDURES. SERVICED LEFT HYD AND FOUND NR 6 SPOILER AC TUATOR LEAKING. REMOVED AND REPLACED ACTUATOR, OPS AND LEAK CK GOOD PER MM B767 27-61-02-4. 2 L 7 2 4F RT A1NM 2008030600081 20080306 00081 WP 2008 3 6 UPS08851704 1 20080110 A 5350 570466334 FRAME DOUG DC8 DC871F 302199D WP TAILCONE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 TAIL CONE FRAME FWD OF LOWER NAV LIGHT CUTOUT HAS CORROSION. REPAIRED TAIL CONE FRAME FWD OF NAV LIG HT IAW RAA DC8-53-20678 AND EA 008-5710-01-A1261. 2 L 7 4 4F RT 4A25 2008032600205 20080326 00205 WP 2008 3 26 08FDEA01027 1 20080318 A 5730 ARB24123 PANEL DOUG MD10 MD1010F 3022112 WP LT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LT WING L/E PANEL 517 AB OUTER SKIN EDGE IS CHAFED AND CRACKED. BLENDED AREA IAW SRM 57-00-01. FOUND TO BE OUT OF LIMIT S IAW SRM 57-00-01 VOL I. CUT OUT DAMAGED AREA IAW SRM 57-00-01 VOL I. FABRICATED DOUBLER & FILLER IAW 57-00-01 VOL I. ALODINED, PRIMED & PAINTED IAW SRM 51-21-01 & 51-21-02 VOL II. INSTALLED DOUBLER & FILLER IAW SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2008032600214 20080326 00214 EU 2008 3 26 08FDEA01036 1 20080318 A 5730 A5724611300000 PANEL AIRBUS 310 A310203 3930313 EU ZONE 600 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT WING L/E LOWER SURFACE PANEL 623 FB SPEED TAPE IS PEELING OFF AND TORN. REMOVED DAMAGED FOIL IAW SRM 51-75-10. APPLI ED NEW FOIL IAW SRM 57-41-12. PRIMED IAW SRM 57-41-12. 2 L 7 2 4F RT A35EU 2008032600217 20080326 00217 WP 2008 3 26 08FDEA01040 1 20080318 A 5753 ARC223319 PANEL DOUG MD10 MD1010F 3022112 WP T/E FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LT WING OUTBD FLAP PANEL 536 HL; CORNER IS DELAMINATED. REPAIRED BY REMOVING THE DAMAGED SKIN FABRICATING A SKIN, PLUG & DOUBLE. HOT BONDED REPAIR & REFINISHED IAW SRM 51-71-00. 2 L 7 3 4F RT A22WE 2008032600218 20080326 00218 WP 2008 3 26 08FDEA01041 1 20080318 A 5753 SKIN DOUG MD10 MD1010F 3022112 WP T/E FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LT WING INBD FLAP FWD SURFACE HAS MANY DENTS. REMOVED & INSTALLED 2 FLAP WEDGES IN REF TO SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2008032600219 20080326 00219 WP 2008 3 26 08FDEA01042 1 20080318 A 5753 ARC315223 PANEL DOUG MD10 MD1010F 3022112 WP T/E FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LT WING INBD FLAP FWD L/E PANEL IS CHAFED AT THE OUTBD HINGE AREA. BLENDED CHAFFED AREA & FOUND OUT OF LIMITS IAW SRM 5 7-00-01 VOL I, ORIGINAL THICKNESS 0.080. REMAINING MATERIAL 0.020. MATERIAL REMOVED 0.060. FABRICATED SKIN & INNER DOU BLER IAW DWG ARC 3152, REV M. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. REMOVED & REPLACED SKIN PANEL IAW SRM 51-31-01 VOL II. PAINTED SKIN PANEL IAW SRM 51-21-01 VOL II. 2 L 7 3 4F RT A22WE 2008032600224 20080326 00224 EU 2008 3 26 08FDEA01048 1 20080319 A 5720 A5724609520001 PANEL AIRBUS 310 A310203 3930313 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT WING PANEL 524 AB IS CRACKED. REMOVED PANEL. REPAIRED BY REMOVING THE PREVIOUS REPAIR. APPLYING A FIBERGLASS WET LAY UP APPLYING NEW ALUMINUM FOIL & REFINISHING IAW SRM 51-40-21 PARA 5. 2 L 7 2 4F RT A35EU 2008032600226 20080326 00226 WP 2008 3 26 08FDEA01052 1 20080319 A 5730 ARB1066 SKIN DOUG DC10 DC1030F 3023504 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 307FE 48291 RT WING L/E EXT ZONE FOUND CRACKS ON UPPER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 68 VOL I. 2 L 7 3 4F RT A22WE 2008032600227 20080326 00227 WP 2008 3 26 08FDEA01053 1 20080319 A 5720 ARB1066 DOUBLER DOUG DC10 DC1030F 3023504 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 307FE 48291 RT WING L/E INT ZONE FOUND CRACK ON UPPER DOUBLER. REPAIRED IAW SRM 57-10-00 FIG 71 VOL I. 2 L 7 3 4F RT A22WE 2008032600231 20080326 00231 WP 2008 3 26 08FDEA01058 1 20080319 A 5730 ARC0288501 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LT WING T/E UPPER SURFACE OF THE MOST INBD FIXED PANEL AFT EDGE HAS CHAFING WEAR ABOVE THE INBD FLAP VANE INBD EDGE. TR IMMED WORN EDGE IAW SRM 57-00-01. REPAIRED PUNCTURED AREA BY BONDING A FILLER & DOUBLER IAW SRM 51-71-00 VOL II. REMOVED CORROSION, ALODINED & PRIMED IAW 57-00-01 VOL I. CHECKED DENTS ON THE UPPER & LOWER SURFACES AND FOUND THEM TO BE WITHI N LIMITS IAW SRM 51-71-00 VOL II. 2 L 7 3 4F RT A22WE 2008032600236 20080326 00236 WP 2008 3 26 08FDEA01060 1 20080319 A 5751 ARC110944 SKIN DOUG MD10 MD1010F 3022112 WP RT AILERON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RT OUTBD AILERON LOWER SKIN FWD EDGE IS CRACKED. REMOVED SKIN PANEL IAW SRM 51-31-01; VOL II. FABRICATED IAW SRM 57-0 0-01 FIG 4 PARA 12 VOL I. HEAT TREAT IAW TPS 1003 REV A. LOCATED & DRILLED HOLES IAW SRM 51-35-01 VOL II. ALODINED & P RIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II. INSTALLED DOUBLER REPAIR & SKIN PANEL IAW SRM 51-25-01 VOL II. INSTALLED COVERS IAW SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2008032600238 20080326 00238 WP 2008 3 26 08FDEA01061 1 20080319 A 5753 NRC60532 SKIN DOUG MD10 MD1010F 3022112 WP T/E FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RT OUTBD FLAP LOWER SKIN HAS HAIL DAMAGE; SEVERAL DENTS. RECORDED & REPAIRED AS REQUIRED. REMOVED & INSTALLED RT WING OUTBD FLAP INBD HINGE FAIRING TO WEDGE BRACKETS IN REF TO SRM 51-31-01 VOL II. REMOVED & INSTALLED 3 EA T/E WEDGES IN RE F TO SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2008032600242 20080326 00242 WP 2008 3 26 08FDEA01063 1 20080319 A 5753 NRC6055506 SKIN DOUG MD10 MD1010F 3022112 WP T/E FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RT INBD FLAP HAS HAIL DAMAGE; SEVERAL DENTS ON THE LOWER SURFACE. RECORDED & REPAIRED AS REQUIRED. REMOVED & INSTALLED RIGHT WING INBD FLAP T/E WEDGE IN REF TO SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2008032600258 20080326 00258 NM 2008 3 26 DHL2008752509 1 20080223 A 5753 6517327U3 FLAP BOEING 727 727223 1384074 NM RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 RT INBD MIDFLAP HAS DELAM AT LOWER OUTBD TRAILING EDGE (AT WBL 238.0). CUT OUT DELAMINATED AREA ON RT I/B MIDFLAP APPRO X 1.5 INCH DIAMETER APPLIED POTTING COMPOUND AND CURED AND SANDED SMOOTH. FABRICATED DOUBLER APPROX 3.5 DIAMETER FROM 7 075T6 .020 PO NR 7281324. CLEANED, PREPPED, PRIMED, BONDED, CLEANED, TREATED, PRIMED AND SEALED EDGES IAW B727 SRM 57-5 0-2 FIG 3 AND 51-40-22 FIG 3 (AT WBL 238.0). 2 L 7 3 4F A3WE 2008032600262 20080326 00262 NM 2008 3 26 DHL2008765020 1 20080201 A 5512 SKIN BOEING 727 727264 138408M NM HORIZONTAL STAB DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, 2 EACH PROTRUDING DENTS ON RIGHT HORIZONTAL STABILIZER UPPER SURFACE 3" INBOARD OF PCU PANEL. REWORKED TO ORIGINAL CONTOUR IAW SRM 51-40-1, 2 EACH DENTS. C/W HFEC IAW NDTM PT 6 51-00-00 FIG 23, CRACK INDICATION. REMOVED D AMAGED DRILLED HOLE SIZE .309 DIAMETER IAW SRM 51-10-1. C/W HFEC ON .309 DRILLED HOLE AND ADJACENT EDGE. REMOVED FASTE NER HOLE IAW SRM 51-30-2 AND NDTM PT6 51-00-00 FIG 23. NO CRACKS INDICATED. FABRICATED REPAIR DOUBLER IAW SRM 55-20-3 FIG 5 AND 55-10-2 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED COUNTERSINK WASHER IAW SRM 51-30-8. INSTALLED DOUBLER REPAIR IAW SRM 55-2-3 FIG 5 ON RIGHT HORIZONTAL STABILIZER UPPER SURFACE. 2 L 7 3 4F A3WE 2008032600264 20080326 00264 NM 2008 3 26 DHL2008752515 1 20080203 A 5720 BEAM BOEING 727 727223 1384074 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 RT WING T/E UPPER "J" BEAM IS CRACKED AT WBL 118. ACCOMPLISHED REPAIR TO CRACKED RT WING T/E UPPER "J" BEAM WBL 118. R EPLACED MATERIAL USED J BEAM P/N BAC1506-860 7075T6 DIM 80.625" IAW EC-00795-001, DWG NR 65-21655 REV J DATED 12/4/78, B 727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008032500159 20080325 00159 NM 2008 3 25 SWAA081496 1 20080318 A 5230 6549889 SKIN BOEING 737 7373T5 1384608 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED HC2 CHECK, FOUND FWD CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032500216 20080325 00216 NM 2008 3 25 2008UALA01452 1 20080315 A 5320 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 808UA 804 DOOR 2L SILL PLATE HAS 1 NUT PLATE HOLE WITH CORROSION. NOT CONSIDERED A MAJOR REPAIR. CORROSION WAS CLEANED, INSPECTE D, AND RETREATED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032500224 20080325 00224 NM 2008 3 25 2008UALA01461 1 20080315 A 5754 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L/E SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 NR 11 SLAT OUTBOARD EDGE UPPER AND LOWER SURFACES DELAMINATED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032500244 20080325 00244 2008 3 25 2008UALA01594 4 20080319 A 2215 31073052 SERVO AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT AILERON LEAKING A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 401UA 435 AILERON SERVO FAULT DISPLAYED. LEFT AILERON SERVO FAILURE, INTERNAL HYDRO LEAKAGE. REPLACED LEFT AILERON GREEN SERVO C ONTROLLER, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030600140 20080306 00140 NM 2008 3 6 2008UALA00985 1 20080221 A 3040 ANTI-ICE SYSTEM BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE WINDSHIELD FAILED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 216UA 30549 WINDOW HEAT LT SIDE FAILURE OF LT NR 2 SIDE WINDSHIELD HEATING CIRCUIT (LOSS OF WINDOW COATING, WIRING OR THE INDIVIDUAL WHCU CIRCUIT FOR THAT WINDOW). TESTED SYSTEM OPS NORMAL. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008030500021 20080305 00021 NM 2008 3 5 QXEA200802069 1 20080101 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - THERE IS A GOUGE 12" FROM THE FORWARD EDGE OF THE LEFT OUTBOARD SEAT TRACK. REPAIRED IAW RD8-53-1342 A ND -8 200 SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2008030500037 20080305 00037 NM 2008 3 5 QXEA200800159 1 20080130 A 5343 FRAME DHAV DHC8 DHC8202 2809007 NM LT MLG WW CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - LEFT MLG RETRACTION ACTUATOR FITTING HAS CORROSION ON ATTACHMENT FRAME ON LOWER OUTBOARD BOLT HOLE. RE PAIRED IAW DHC8 200 RD8-54-1178, NDTM PT-6 51-00-01, PT-1 51-00-04. 2 H 7 2 4T RT A13NM 2008030500058 20080305 00058 NM 2008 3 5 QXEA200800126 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 509-529 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - LEFT SEAT TRACK NR 7 BETWEEN FRAME 509.5 TO 529.5 HAS MULTIPLE CHAFES/GOUGES. REPAIRED IAW RD8/4-53-88 4, Q400 NDTM PT-6 51-00-01, AND Q400 SRM 51-21-10. 2 H 7 2 4T RT A13NM 2008030500070 20080305 00070 NM 2008 3 5 QXEA200800117 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 243-256 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - SEAT TRACK NR 19 HAS SEVERAL SPOTS OF MILD SURFACE CORROSION STATION X243.0, X256.0 AND X310.0. REPAIR ED IAW RD8/4-53-884, Q400 NDTM PT-6 51-00-01, AND Q400 SRM 51-21-10. 2 H 7 2 4T RT A13NM 2008030500077 20080305 00077 NM 2008 3 5 QXEA200802082 1 20080101 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 600 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - JUST FORWARD OF FS X600 W/L Z99 B/L Y34 THERE IS CORROSION ON THE INSIDE OF THE OUTSIDE SKIN. REPAIRED IAW -8 200 CPC CHAPTER 4 STEP 8 AND -8 200 SRM 51-20-16, 51-20-36, 51-20-11, 51-20-51, 51-20-26. 2 H 7 2 4T RT A13NM 2008030500099 20080305 00099 NM 2008 3 5 QXEA200800140 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 301-413 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - LEFT INBOARD SEAT TRACK NR 7 HAS SEVERAL SCRATCHS AND NUMEROUS AREAS OF MINOR SURFACE CORROSION STA X30 1 TO X 413. REPAIRED IAW RD8/4-53-884, Q400 NDTM PT-6 51-00-01, AND Q400 SRM 51-21-10. 2 H 7 2 4T RT A13NM 2008030500113 20080305 00113 NM 2008 3 5 QXEA200802080 1 20080101 A 5210 STRUCTURE DHAV DHC8 DHC8202 2809007 NM PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - FORWARD CABIN DOOR HAS CORROSION AROUND NUTPLATE HOLES AND RIVETS. REPAIRED IAW -8 200 SRM 51-40-11 AN D -8 CPCM CHAPTER 4. 2 H 7 2 4T RT A13NM 2008030500146 20080305 00146 NM 2008 3 5 QXEA200800136 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - NR 10 SEAT TRACK , AFT END FLANGE AT SPLICE OUTBOARD SIDE HAS SURFACE CORROSION. REMOVED TRACK AND INS TALLED NEW TRACK IAW -8 Q400 SRM 51-40-15 AND 51-42-05. 2 H 7 2 4T RT A13NM 2008030500155 20080305 00155 NM 2008 3 5 QXEA200800230 1 20080226 A 6120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM PROPELLER UNKNOWN A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 406QX 4048 PDX- NR 2 ENGINE DID NOT COME OUT OF FEATHER. MAINTENANCE PERFORMED A TIME CHECK IAW TASK 61-20-00-720-80. CHECKS GOOD WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008030500173 20080305 00173 NM 2008 3 5 QXEA200800231 1 20080227 A 5250 DOOR DHAV DHC8 DHC8202 2809007 NM COCKPIT STIFF A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 347PH 480 PSC- COCKPIT DOOR VERY HARD TO OPEN. MAINTENANCE FILED THE STRIKER PLATE AND LUBRICATED THE DOOR. OPERATIONAL CHECKS G OOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008032800114 20080328 00114 WP 2008 3 28 UPS08851870 1 20080301 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 LEFT WING O/B LEADING EDGE EXTERIOR SKIN CRACKED AROUND SCREW HOLE AT I/B END. CUT OUT DAMAGE, FABBE D AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-1 FIG H. 2 L 7 4 4F RT 4A25 2008032800115 20080328 00115 WP 2008 3 28 UPS08851871 1 20080302 A 5720 STRUCTURE DOUG DC8 DC873F 302199F WP RT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 RIGHT CENTER L/E HAS LWR ATTACH SCREW HOLE DAMAGED O/B OF FUELING PORT. REMOVED DAMAGE, FABBED AND I NSTALLED REPAIR DOUBLER IAW SRM EO DC8-5720 -4087, 51-1-8, 51-1-26. 2 L 7 4 4F RT 4A25 2008032800122 20080328 00122 EU 2008 3 28 UPS08151906 1 20080320 A 2560 SLIDE AIRBUS A300 A300F4622R 3930360 EU GIRT BAR LACK OF LUBE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 133UP 0816 INSPECTION TYPE:N/A SLIDE ARMING LEVER VERY DIFFICULT TO DISARM. LEVER MOVEMENT STOPS 3/4 ON TRAVEL, IT TAKES SEVERAL A TTEMPTS FOR LEVER TO FULLY DISARM SLIDE. LUBRICATED SLIDERS ON GIRT BAR AND LEVER. FUNCTIONAL TEST OK IAW MM 25-61-15- 5. 2 L 7 2 4F RT A35EU 2008032800124 20080328 00124 WP 2008 3 28 UPS08851890 1 20080311 A 3260 SWITCHMOUNT MOUNT DOUG DC8 DC873F 302199F WP RT MLG W/W DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 RIGHT MLG DOOR SWITCH MOUNT HOLES ELONGATED. REPAIRED RIGHT MLG DOOR SWITCH HOLES IAW DWG 5653490, D C8-3260-16914 AND SRM 51-1-8. 2 L 7 4 4F RT 4A25 2008032800129 20080328 00129 WP 2008 3 28 UPS08851901 1 20080320 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01. 2 L 7 4 4F RT 4A25 2008032800134 20080328 00134 WP 2008 3 28 UPS08851908 1 20080317 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 LOWER FLANGE OF SEAT TRACK EXTRUSION EXFOLIATED IN MAIN CABIN, STA 1455-1462 LBL 60. REPAIRED CABIN SEAT TRACK AT STA 1455-1462 LBL 60 IAW SRM 53-02-03-0, AND SRM 53-02-03-0 FIG 008A. 2 L 7 4 4F RT 4A25 2008032800135 20080328 00135 WP 2008 3 28 UPS08851909 1 20080316 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 CORROSION ON SEAT TRACK AT STA 1470 LBL 45. FABRICATED AND REPLACED CABIN SEAT TRACK SECTION AT STA 1470 AND LBL 45 IAW SRM 51-03-00, SRM 51-03-02, SRM 51-03-01 AND SRM 51-1-8. 2 L 7 4 4F RT 4A25 2008032800145 20080328 00145 NM 2008 3 28 SWAA081584 1 20080322 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 407WN 29817 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008032800146 20080328 00146 NM 2008 3 28 SWAA081586 1 20080324 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008032800155 20080328 00155 SO 2008 3 28 C2XA08SH051 1 20080326 A 5751 14569009410 BRACKET EMB 145 EMB145XR 3260214 SO RT AILERON WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 21129 145703 SHV - DURING C-CHECK IT WAS FOUND THAT THE RT AILERON PCA BRACKET WAS WORN AND WOULD NOT CONTAIN THE HAT BUSHINGS. MAIN TENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW CONTINENTAL EXPRESS EC5750-01177. THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. 2 L 7 2 4F RT 2008032800159 20080328 00159 WP 2008 3 28 UPS08851918 1 20080221 A 5313 SAA78828903 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 AFT CABIN L14R CRACKED AT CANTED FRAME STA 1755. REPAIRED L14R AT STA 1755 CANTED FRAME IAW SRM 51-3 -0, 53-2-2 FIG 10, 51-1-8, EO DC8-5320-28843A AND EA 008-5320-01-A1314. 2 L 7 4 4F RT 4A25 2008032800160 20080328 00160 WP 2008 3 28 UPS08851919 1 20080221 A 5313 SAA78828913 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 AFT CABIN L15R CRACKED AT CANTED FRAME STA 1750. REPAIRED L15R AT STA 1750 CANTED FRAME IAW SRM 51-1 -21, SRM 51-3-0, SRM 53-2-2 FIG 10, EO DC8-5320-28843-A AND EA 008-5320--01-A1314. 2 L 7 4 4F RT 4A25 2008032800161 20080328 00161 WP 2008 3 28 UPS08851920 1 20080222 A 5347 36575031 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 STOP HOLES WORN IN F/E'S FOWARD SEAT TRACK. REMOVED AND REPLACED FWD SEAT TRACK IAW SRM 51-3-0, 51-1 -8, 51-1-24. 2 L 7 4 4F RT 4A25 2008032800162 20080328 00162 WP 2008 3 28 UPS08851921 1 20080304 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 COCKPIT FLOOR PANEL 678 CRACKED AT NOTED LOCATIONS, LOOSE CHAFE STRIP DISBONDED BOOK SHELF BRACKET. STOP DRILLED CRACK, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-8, 51-1-21, 53-2-00 FIG 1B, 51-3-1. 2 L 7 4 4F RT 4A25 2008032800169 20080328 00169 NM 2008 3 28 SWAA081606 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032800170 20080328 00170 NM 2008 3 28 SWAA081607 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032800174 20080328 00174 NM 2008 3 28 SWAA081611 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032800177 20080328 00177 NM 2008 3 28 SWAA081595 1 20080325 A 5311 65C25228 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 14R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032800180 20080328 00180 NM 2008 3 28 SWAA081637 1 20080325 A 5313 6552988 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER 8L CRACKED AT BS 1010. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008032800183 20080328 00183 NM 2008 3 28 SWAA081642 1 20080325 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 390 AND BS 410, RBL 1.5 TO RBL 3. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008032800184 20080328 00184 NM 2008 3 28 SWAA081641 1 20080325 A 5753 65C30462 SKIN BOEING 737 7375H4 138449D NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SKIN DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER S RM. 2 L 7 2 4F RT A16WE 2008032500247 20080325 00247 NM 2008 3 25 2008UALA01597 1 20080320 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 BS 867 STR 25L, STRINGER CLIP CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500254 20080325 00254 NM 2008 3 25 2008UALA01604 1 20080320 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 RT FUSELAGE EXTERNAL SKIN HAS SCRIBE LINES AT APPROX BS 727A + 10" - 727B + 10" BETWEEN STR 17R-18R, MAJOR REPAIR ACCO MPLISHED: INSTALLED SINGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500255 20080325 00255 NM 2008 3 25 2008UALA01605 1 20080320 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 537UA 25157 LEFT EXTERNAL FUSELAGE STA 600-640, STR 15L - 17L, 3 EA DENTS, 2 EA OF WHICH ARE ON EXISTING DOUBLER. MAJOR REPAIR ACCO MPLISHED: REMOVED DAMAGED SKIN & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032500266 20080325 00266 NM 2008 3 25 2008UALA01615 1 20080320 A 2120 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU REAR GALLEY SMOKE A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 398UA 24673 SMOKE FROM COFFEEMAKER IN REAR GALLEY. UNABLE TO DUPLICATE SMOKE. REMOVED BOTH AFT GALLEY C-MS AND INSPECTED BOTH AS WE LL AS ALL ELECTRICAL COMPTS. NO FAULTS NOTED. NO EVIDENCE OF BURNING. BOTH C-M,S OPS NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032600007 20080326 00007 NM 2008 3 26 HALA0800398 1 20080312 A 2840 PROCESSOR BOEING 767 76733A 1385209 NM FUEL QUANTITY MALFUNCTIONED A HALA K NONE O OTHER NR NOT REPORTED 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, CENTER FUEL TANK AND TOTAL FUEL QTY INDICATORS INTERMITT. NO EICAS MSG. T/S PER FIM 28-41-00 SYST CKD OK. RE-RACKED FUEL QTY PROCESSOR SELF TEST OK. NO EICAS MSG. 2 L 7 2 4F RT A1NM 2008032600039 20080326 00039 WP 2008 3 26 08FDEA00998 1 20080317 A 5280 STRUCTURE DOUG DC10 DC1010F 3022111 WP LT MLG DOOR DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LT MLG STRUT DOOR; LOWER AFT END HAS THE METAL EDGE PROTECTOR DISBONDING. LT MLG STRUT DOOR WAS REPLACED. ALL WORK WAS ACCOMPLISHED ON N00122. 2 L 7 3 4F A22WE 2008032600049 20080326 00049 NM 2008 3 26 2008UALA01499 1 20080317 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 683 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 EXTERNAL KEEL BEAM LOWER SKIN PANEL BETWEEN MLG WHEEL WELLS IS CRACKED AT BS 683 APPROX AT LBL 4. MAJOR REPAIR ACCOMPLI SHED: STOP DRILLED ENDS OF CRACK. FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR. REMOVED CRACKED KEELBEAM LOWER PANEL & REPLACED IT WITH NEW PANEL P-N 65-45866U205. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032600050 20080326 00050 NM 2008 3 26 2008UALA01500 1 20080317 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 303 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FWD ENTRY DOOR CUTOUT AT BS 303.9 FRAME WEB DOUBLER AT STRINGER S-16L IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED STO P FITTING DOUBLER & WEB. INSTALLED NEW WEB & DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032600051 20080326 00051 NM 2008 3 26 2008UALA01501 1 20080317 A 3350 20131A BATTERY PACK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 312UA 23673 EEL LIGHTS AND LT OVERWING HATCH EXIT EMERGENCY LIGHTS INOP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032600057 20080326 00057 NM 2008 3 26 2008UALA01506 1 20080318 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 6GH. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032600058 20080326 00058 NM 2008 3 26 2008UALA01533 1 20080317 A 3150 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE AILERON LOCKOUT ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 646UA 25283 AILERON LOCKOUT EICAS SLOWING THRU 270 AT 11000. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032600075 20080326 00075 NM 2008 3 26 HA0800416 1 20080314 A 5512 184T10061 PANEL BOEING 767 767332 1382001 NM HORIZ STAB DENTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 DENT ON LT HORIZONTAL STABILIZER LE PANEL 332BL. PERMANENT SRM REPAIR CARRIED OUT PER SRM 51-70-10, REF ANZ T1 19011361 5-0001 AND HAL FILE NR 594051. 2 L 7 2 4F RT A1NM 2008032600094 20080326 00094 NM 2008 3 26 DL76G080374 1 20080313 A 3350 FUSE BOEING 767 767332 1382001 NM CABIN BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1612T 30575 EMERGENCY LIGHTS L979, L9700, L975, L9699, L308, L333 ARE INOP. TROUBLESHOT SYSTEM AND DETERMINED PICO FUSE BLOWN. REM OVED AND REPLACED FUSE IAW DAL B767-300 MM 33-51-07. OPS CHECK GOOD IAW B767-300 AMM 33-51-07. 2 L 7 2 4F RT A1NM 2008032600108 20080326 00108 NM 2008 3 26 2008UALA01553 1 20080318 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 577UA 26693 EXTERIOR EMERGENCY LIGHT AT DOOR 4R INOP. RELAMPED ASSY, OPS CHECKED NORMAL. FOUND AMP INOPERATIVE. RELAMPED ASSY, OP S CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032600133 20080326 00133 SO 2008 3 26 SWIA200819346 1 20080115 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 250YV 120250 FOUND AT C-CHECK, LEFT WING INBOARD UNDERWING NR 2 FUEL PANEL HAS LEAKING RIVETS. REPLACED RIVETS AND REPAIRED CRACKED STRINGER IAW SRM 57-20-03. 2 L 7 2 4T RT A31SO 2008032600178 20080326 00178 SO 2008 3 26 SIMA200807905 1 20080315 A 7110 COWLING EMB 145 EMB145LR 3260212 SO NR 1 ENGINE OPEN A SIMA K NONE E VIBRATION/BUFFET CR CRUISE 1 SW 21 616AE 145092 ON FLIGHT 4154, CREW REPORTED ENGINE VIBRATION IN CRUISE FLIGHT. PASSENGER REPORTED HEARING A LOUD BOOM NOISE FROM THE ENGINE IN FLIGHT. UPON LANDING IN ORD, THE TOWER REPORTED THAT EAGLE SHOULD CHECK THE NR 1 ENGINE DUE TO OBVIOUS DAMAGE AS SEEN DURING TAXI IN TO ORD. UPON POST-FLT INSPECTION, IT WAS DISCOVERED THAT THE NR 1 ENGINE COWL HAD OPENED IN FLI GHT AND PARTS HAD SEPARATED THE AIRCRAFT AND DAMAGE TO THE ENGINE HAD OCCURRED. 2 L 7 2 4T RT T00011AT 2008032600187 20080326 00187 EA 2008 3 26 N6WA0080301 1 20080319 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE EMERGENCY LIGHTS INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 155GJ 10225 PILOT NOTICED ON POST FLIGHT INSPECTION EMERGENCY LIGHTS WON'T GO OFF. REPLACED BATTERY PACK AND CHARGER IN NR 3 POSITI ON. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008032600190 20080326 00190 SO 2008 3 26 HSYA20080317 1 20080317 A 2797 W602000522WH WIRE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE TE FLAPS BROKEN E HSYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 05 223AS 120021 AFTER TAKEOFF AND ROTATION THE CREW REPORTED A CONTROL FAULT INDICATION AND ASYMMETRY FAULT INDICATION ON THE IB T/E FLA PS. THE CREW RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX PERFROMED TROUBLESHOOTING AND FOUND A BROKEN WIRE ON THE RT IB FLAP ACTUATOR CONNECTOR. MX REPAIRED THE BROKEN WIRE AND THE ACFT APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 2008032600192 20080326 00192 CE 2008 3 26 DXTA20082953 1 20080320 A 3260 UPLOCK SWITCH CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG OUT OF ADJUST E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 671QS 5605071 WHILE FLYING AT FL400 A LOUD (THUNK) WAS HEARD COMING FROM THE BACK. THE GEAR UNSAFE LIGHT ILLUMINATED WITH HYD PRESS ST EADY. ADJUSTED NOSE GEAR UPLOCK HOOK AND UP LOCK SWITCH IAW MM 32-30-05 GEAR SWING OPERATIONAL CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008032600195 20080326 00195 2008 3 26 F3LA200800122 4 20080228 A 2565 MRR171700LH CABLE ASSY AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE EVAC SLIDE BINDING A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED THE LEFT, OVERWING EMERGENCY EXIT SLIDE CABLE FAILED ITS OPERATIONAL TEST. MA INTENANCE APPLIED LUBRICATING COMPOUND 05-027 TO THE CABLE IN ACCORDANCE WITH THE REQUIREMENTS OF EA A0-52T-30102. FOLL OWING THIS MAINTENANCE ACTION, THE CABLE WAS TESTED, INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032600196 20080326 00196 CE 2008 3 26 DXTA20082956 1 20080321 A 3150 WARNING LIGHT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 930QS 7500130 CYAN (YD FAIL UPPER B) CAS MESSAGE ILLUMINATED INFLIGHT. ACCOMPLISHED UPPER RUDDER STABILITY AUGMENTATION TEST IAW MM 2 7-24-01. OPS CHECK GOOD. SWAPPED A & B YSAC FOR FURTHER MONITORING. OPS CHECK GOOD IAW MM 27-24-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032600200 20080326 00200 CE 2008 3 26 DXTA20082958 1 20080321 A 2400 DIODE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL BURNED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 999QS 7500203 REMOTE CB TRIPPED CYAN CAS MESSAGE. ILLUMINATED DURING DESCENT. MESSAGE WAS ACCOMPANIED BY ODOR OF ELECTRICAL SMOKE. O PENED AFT "J" BOX & FOUND CB HK005 TRIPPED. RESET BREAKER, POWERED AIRCRAFT. POWERED PASSENGER SAFETY SYSTEM. AFTER APPR OX 10 MIN. CB HK005 TRIPPED. INSPECTED WIRING & FOUND DIODE BURNED ON RELAY BEHIND SWITCH PANEL FOR PASSENGER SAFETY SWI TCH. REMOVED & REPLACED BAD DIODE. C/W SATISFACTORY OPERATIONAL CHECK OF THE PASSENGER WARNING SYSTEM. ALL EICAS INDICAT IONS NORMAL. IAE MM 33-20-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032600201 20080326 00201 CE 2008 3 26 DXTA20082959 1 20080322 A 2750 FLAP SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS FAILED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED DE DESCENT 1 GL 07 907QS 7500201 (FLAPS FAIL) AT APPROX 3 DEGREES WITH SLATS EXTENDED. PERFORMED FLAP SYSTEM OPERATION TEST IAW MM 27-50-00 4 A, B, C, D & F. RAN FLAPS THROUGH 10 TIMES. OPS CHECK GOOD AT THIS TIME 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008032600204 20080326 00204 NM 2008 3 26 NWAA081015802 1 20080318 A 3397 PIN BOEING 757 757351 1384991 NM CABIN BACKED OUT A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 582NW 32981 DURING OVERNIGHT CHECK, FOUND DOOR 2 CENTER AISLE EMERGENCY EXIT SIGN INOP. MAINTENANCE FOUND PIN 18 NOT INSERTED IN D4 2722P, AND REINSERTED PIN. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2008032600215 20080326 00215 EU 2008 3 26 08FDEA01037 1 20080318 A 5730 A5724608900100 PANEL AIRBUS 310 A310203 3930313 EU ZONE 600 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT WING L/E LOWER SURFACE PANEL 623 EB SPEED TAPE IS PEELING OFF AND TORN. REMOVED DAMAGED FOIL IAW SRM 57-41-12. APPLI ED NEW FOIL IAW SRM 57-41-12. PRIMED IAW SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008032600266 20080326 00266 EU 2008 3 26 08FDEA01094 1 20080321 A 5542 PANEL AIRBUS 310 A310324 3930206 EU RUDDER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 LEFT RUDDER PANEL, 3RD FASTENER FROM THE TOP OF THE RUDDER HAS WATER IN 7 CONNECTED CELLS; 4 CONNECTED CELLS; 2 CONNEC TED CELLS AND 5 INDIVIDUAL CELLS, DELAMINATION 3.4 INCH BY 2.8 INCH. REPAIRED REMOVING DELAMINATED AREA & BONDING A NEW CORE & LAY UP REPAIR PLIES IAW EA 6-5540-118453. 2 L 7 2 4F RT A35EU 2008032600267 20080326 00267 NM 2008 3 26 08FDEA01095 1 20080321 A 2910 CHECK VALVE BOEING 727 727233 138408A NM HYD SYSTEM LEAKING A FDEA A UNSCHED LANDING K S FLUID LOSS AFFECT SYSTEMS CL CLIMB 1 SO 25 221FE 20932 INSTANTANOUS LOSS OF HYD SYS A PRESSURE AND QUANTITY. ALL QRH PROCEDURES COMPLETED. NO RESTORATION. FOUND SYS "A" HYD RAULIC MODULAR PACKAGE WITH BLOWNOUT CHECK VALVE. REMOVAL/INSTALLATION OFF MFG 65-17821-14. 2 L 7 3 4F RT A3WE 2008032600270 20080326 00270 EA 2008 3 26 QXEA200800296 1 20080314 A 2720 PS644 POWER SUPPLY CNDAIR CL600 CL6002C10 1390015 EA RUDDER TRIM INTERMITTENT A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 602QX 10010 PDX- FLIGHT 2594 (PDX-BIL). ON TAKEOFF ROLL RECEIVED A "CONFIG RUDDER" WARNING. RUDDER TRIM WAS SHOWING CENTERED AND IN THE GREEN. "TAKEOFF CONFIG OK" WAS DISPLAYED AT THE START OF THE TAKEOFF ROLL. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE DETERMINED IT TO BE A INDICATION PROBLEM. REPLACED THE AILERON/RUDDER TRIM POWER SU PPLY. OPERATIONAL AND CHECKS FLIGHT ARE GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008032600271 20080326 00271 NM 2008 3 26 P5CA0801549 1 20080315 A 5347 CARGO TRACK BOEING 747 74746NF 13848BT NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 450PA 30808 MAIN DECK CARGO TRACK HAS A CRACK AT BS 1800 LBL 98.5 MEASURING 10.0 INCHES. TIME LIMITED REPAIR WAS ACCOMPLISHED PER E O NR 4453A138 PART 1. 2 L 7 4 4F RT A20WE 2008032600276 20080326 00276 WP 2008 3 26 IXXA080001O 1 20080107 A 3610 32143242 REGULATOR VALVE DOUG DC8 DC872F 302199E WP PNEUMATIC SYS DEFECTIVE A IXXA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 11 721CX 84550 2797 46013 DURING CRUISE FROM KMLB, THE CREW NOTICE THE LEFT PNEUMATIC MANIFOLD READ'S 17 PSI LOWER THAN THE RIGHT SIDE, THE LEFT S IDE READ'S 20 PSI AND THE RIGHT SIDE READ'S 37 PSI. THE LEFT SIDE MANIFOLD COULD NOT REACH 35 PSI TO DO PRESSURE DECAY CHECK, THE LEFT SIDE ONLY WENT TO 28 PSI AT POWER. THE CREW RETURNED TO KMLB, AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 AND NR 2 PNEUMATIC REGULATOR VALVE IAW DACO DC-8 MAINTENANCE MANUAL 36-12-1. OPERATIONAL CHE CK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2008032800185 20080328 00185 NM 2008 3 28 SWAA081643 1 20080325 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, RBL 1.5. REPAIRED SK IN PER ER. 2 L 7 2 4F RT A16WE 2008032800190 20080328 00190 NM 2008 3 28 SWAA081635 1 20080325 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008032800202 20080328 00202 NM 2008 3 28 SWAA081650 1 20080326 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND STRINGER 11R CRACKED AT BS 540. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008032800203 20080328 00203 WP 2008 3 28 IXXA08SMN045S 1 20080201 A 5753 SKIN DOUG DC8 DC871F 302199D WP TE FLAP DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND LT WING FLAP INBOARD UPPER SKIN SHOWS DENTS BETWEEN STATION XW 3.000 - XW 91.00 0. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, DOUBLER. CLEANED, TREAT ED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-1-11, DC8 SRM 51-1-21, SRM 57-7 -1 FIGURE 1 ITEM "A" AND "L", 57-1-0 PAGE 1, SRM 51-1-21, AND SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008032800206 20080328 00206 EA 2008 3 28 A6WA200840118 1 20080218 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 430AW 7719 AT FS 621, WL 114, LBL 27, BELOW BEAM ANGLE CRACKED. BEAM ANGLE REPLACED IAW SRM 51-24-21. (M) 2 L 7 2 4F RT A21EA 2008032800212 20080328 00212 EA 2008 3 28 A6WA200840123 1 20080220 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 605 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 FOUND LOWER SILL CRACK ON FS 605 LBL 45 OF CARGO DOOR. REPAIRED IAW REO 601R-53-61-433. (M) 2 L 7 2 4F RT A21EA 2008032800213 20080328 00213 EA 2008 3 28 A6WA200840124 1 20080226 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 CRACK FOUND ON RT INTERCOSTAL FS 484 RBL 36 AND RBL 27, CRACK LENGTH .100. INTERCOSTAL CLIPS AT FS 484 RBL 36 AND 27 RE PAIRED IAW REO 601R53-41-059 EDDY CURRENT PERFORM ON INTERCOSTAL CUT LINE AND FABRICATED PARTS. (M) 2 L 7 2 4F RT A21EA 2008032800214 20080328 00214 WP 2008 3 28 IXXA08SMN052S 1 20080207 A 5340 FITTING DOUG DC8 DC871F 302199D WP BS 680 L20L CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FITTING CRACKED AT STATION 680.000 LONGERON 20 RT. REMOVE CRACKED F ITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW SRM 51-3-1, SRM 51-1-20D, AND SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008032800215 20080328 00215 NM 2008 3 28 SWAA081651 1 20080326 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 981, STR 22L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008033100002 20080331 00002 EU 2008 3 31 UPS08151914 1 20080321 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 142UP 0825 INSPECTION TYPE:N/A GLARESHIELD EMERGENCY LIGHTS INOP. RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD PER MC 050000-01-1-000. 2 L 7 2 4F RT A35EU 2008033100004 20080331 00004 NM 2008 3 31 UPS08651915 1 20080322 A 5610 SEAL BOEING 767 76734AF 1385212 NM COCKPIT WINDOW LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 303UP 27241 INSPECTION TYPE:N/A CAPTAIN'S SIDE WINDOW BINDS WHEN OPENING OR CLOSING. FOUND CAPTAIN'S WINDOW SEAL LOOSE ON TOP OF WI NDOW FRAME AND INTERFERING WITH WINDOW OPERATION, SECURED SEAL PER B767 MM 56-11-11-4.3, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008033100007 20080331 00007 NM 2008 3 31 QXEA200800304 1 20080313 A 5320 ANGLE BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX -C4- ANGLE CORRODED ON AFT SIDE OF WEB AND ATTACHED TO SKIN SURFACE AT STA X26.7 STR 24P (UNDER LAYSHAFT). REMOVED THE ANGLE BY DRILLING OUT RIVETS HOLDING ANGLE TO AIRCRAFT. DRILLED AND INSTALLED NEW BRACKET IAW DHC-8 400 SRM 51-42-0 5. 2 H 7 2 4T RT A13NM 2008033100008 20080331 00008 NM 2008 3 31 QXEA200800305 1 20080313 A 5340 COLLAR BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX -C4- THE LOCK FASTENER COLLARS ON STR 25S/L BETWEEN FRAMES X26.700 TO X32.300 ARE CORRODED. REMOVED AFFECTED LOCK F ASTENERS AND COLLARS BETWEEN STA X25.00 AND X32.400. INSTALLED NEW LOCK FASTENERS IAW D-8 Q400 SRM 51-40-15. 2 H 7 2 4T RT A13NM 2008033100026 20080331 00026 WP 2008 3 31 08FDEA00987 1 20080317 A 5321 AGA38644 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 AFT PIT FLOOR PANEL NR 187 HF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL NR 187 HF. LOCATED HOLES ; POTTED EDGES; COMPLETED CURE; SANDED EDGES AND INSTALLED INSERTS. FABRICATED TOP SHEET; LAYED UP UNDER A VAC BAG; CO MPLETED CURE; COUNTER SUNK HOLES AND APPLIED NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008033100031 20080331 00031 NM 2008 3 31 SWAA081666 1 20080326 A 5311 6546532 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008033100033 20080331 00033 NM 2008 3 31 SWAA081667 1 20080326 A 5311 65C22909 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008032700187 20080327 00187 NM 2008 3 27 2008UALA01416 1 20080313 A 5320 ANGLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FUSELAGE BODY FRAME INTERCOSTAL AT BS 310 OUTBOARD CHORD ANGLE CRACKED AT STRINGER S-13L. MAJOR REPAIR ACCOMPLISHED: R EMOVED & REPLACED CRACKED CHORD ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700196 20080327 00196 WP 2008 3 27 08FDEA01098 1 20080321 A 5321 ACA3205505 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 200 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 MAIN CABIN FLOORBOARD AT RBL 9 TO 28; BS 615 TO 735 IS SOFT AND SPONGY. EVALUATED THE FLOOR PANEL AND FOUND IT TO BE SO LID IAW FEDEX SRZ 25-005; REV F. SDR SUMITTED IN ERROR- ADMINISTRATOR. 2 L 7 3 4F RT A22WE 2008032700210 20080327 00210 NM 2008 3 27 08FDEA01111 1 20080323 A 5330 65184207 SKIN BOEING 727 727225 1384077 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 LT FUSELAGE SKIN WORN AT BS 310 BTW S10L AND S11L, WORN BY FWD ENTRY DOOR MECHANISM LONG BOLT INSTALLED. REPAIRED FWD ENTRY DOOR MECHANISM IAW SRM 51-30-2 AND EA 7-5330-116972. 2 L 7 3 4F A3WE 2008032700214 20080327 00214 NM 2008 3 27 08FDEA01113 1 20080323 A 5311 AFA00283 FRAME DOUG MD11 MD11F 3023600 NM BS 1681 S12R DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 522FE 48476 MAIN DECK RIGHT FRAME AT STATION 1681, STRINGER 12 RIGHT FOUND DENTED. REPAIRED AS PER SRM 53-30-00, FIG.1, VOL.1. INI TIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00, FIG.1, VOL.1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032700226 20080327 00226 WP 2008 3 27 08FDEA01119 1 20080324 A 5414 PANEL DOUG MD10 MD1010F 3022112 WP NR 1 NACELLE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 NR 1 PYLON PANEL NR 439 AL IS CHAFED. REMOVED WEB IAW SRM 51-31-01 VOL II. LOCATED, DRILLED & DEBURRED NEW WEB IAW SRM 51-35-01 VOL II. INSTALLED WEB IAW DWG AUG 7107; REV P. 2 L 7 3 4F RT A22WE 2008032700230 20080327 00230 NM 2008 3 27 2008UALA01487 1 20080316 A 3350 SIGN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 642UA 25092 EMERGENCY EXIT LIGHT IN COCKPIT IS ON WHEN SWITCH IS IN ARMED POSITION WHILE ON GROUND. REPLACED PORTABLE EMERGENCY EXI T SIGN ABOVE FLIGHT DECK DOOR PER MM 33-51-01. OPS CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032700238 20080327 00238 WP 2008 3 27 08FDEA01126 1 20080324 A 5730 ARB25104 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT WING LOWER L/E PANEL 616 HB IS CHAFED ALONG THE EDGE. CLEANED RIGHT WING LOWER L/E PANEL 616 HB TO EVALUATE DAMAG E AND PANEL WAS FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01; VOL I. PANEL REQUIRED A SRM REPAIR. FABRICATED REPAIR DOU BLER IAW DC/MD-10 SRM 57-00-01; VOL I. TREATED; PRIMED AND TOPCOATED DOUBLER IAW 51-21-01; VOL II. INSTALLED REPAIR D OUBLER IAW SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 2008032700239 20080327 00239 NM 2008 3 27 2008UALA01492 1 20080315 A 2120 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GALLEY ODOR A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 785UA 26954 LIGHT CHEMICAL-PLASTIC SMELL IN AFT GALLEY. COULD NOT LOCATE SOURCE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032700254 20080327 00254 NM 2008 3 27 AALA200800487 1 20080304 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 JFK - EMERGENCY LIGHT AT SEAT 23C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700263 20080327 00263 NM 2008 3 27 AALA200800494 1 20080304 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 966AN 30094 MIA - EMERGENCY LIGHT AT SEAT ROW 28 HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 28. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008032700271 20080327 00271 SO 2008 3 27 C2XA08RI037 1 20080319 A 3243 429515 CONTROL UNIT EMB 135 EMB135LR 3260305 SO BRAKE SYSTEM DEFECTIVE A C2XA K NONE O OTHER LD LANDING 1 SW 27 14508 14650 3218 145220 FLIGHT 2424 - EWR - CREW REPORTED BRAKES INEFFECTIVE AT HIGH SPEED AFTER LANDING. BRAKE DEGRADE MESSAGE ON EICAS APPEAR ED MOMENTARILY, AND THEN DISAPPEARED, BUT BRAKE OPERATED NORMAL AT LOW SPEED. EWR MX REMOVED AND REPLACED BRAKE CONTROL UNIT AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008032700272 20080327 00272 NM 2008 3 27 AALA200800505 1 20080304 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 921AN 29522 MIA - EMERGENCY LIGHT AT SEAT ROW 27 HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008032700297 20080327 00297 NM 2008 3 27 DHL2008763517 1 20080312 A 5347 BAC1520792 SEAT TRACK BOEING 727 727264 138408M NM BS 958-1139 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 SEAT TRACK CORRODED AT BS 1110-1130, LBL 24. REMOVED, FABRICATED FROM BAC 1520-792, PO NR 9006020, 297" LONG, AND INSTA LLED PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 1 AT BS 958.5" TO BS 1139. 2 L 7 3 4F A3WE 2008032700334 20080327 00334 EU 2008 3 27 08FDEA01139 1 20080325 A 5730 A5735003200000 PANEL AIRBUS 310 A310203 3930313 EU LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LEFT WING FUEL PANEL 550 HB HAS FRETTING CORROSION AROUND THE ATTACHMENT HOLES. PANEL FOUND TO BE OUT OF LIMITS REF A31 0-200 SRM 57-20-16, FOR INSTALLATION OF THE NEW PANEL SEE FEDEX WIC 45X5052ALI. 2 L 7 2 4F RT A35EU 2008032700345 20080327 00345 NM 2008 3 27 HALA0800430 1 20080323 A 7700 WARNING SYSTEM BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE LT ENGINE MALFUNCTIONED A HALA K NONE N FALSE WARNING NR NOT REPORTED 1 WP 13 476HA 55118 ENGINE LEFT SYSTEM FAULT LIGHT CAME ON. PER FIM TASK 71-00 ELECTRONIC ENGINE CONTROLLER BITE CK, NO FAULTS FOUND. RAN NR 1 ENG, NO FAULTS. OK FOR SERVICE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2008032600283 20080326 00283 EU 2008 3 26 08FDEA01071 1 20080320 A 5311 A53981311 FRAME AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND DENT AT C74, P26-27 LT/RT REPAIR PERFORMED BY REWORK OF FRAME OUTER FLANGE AT P26 LT/RT, NDT FOR CRACK FREE IAW RA S/EFW/9000010/2008 ISS A, APPROVED BY EA 6-5318-114865 2 L 7 2 4F RT A35EU 2008032600285 20080326 00285 EU 2008 3 26 08FDEA01073 1 20080320 A 5312 A53810770200 DOUBLER AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND OLD REPAIR ON PRESSURE BULKHEAD C 39, P55 WITH NEW DEFECTS (CHAFING MARKS AND POSSIBLE CRACK IDENTIFICATION IN H OLE). REPAIR PERFORMED BY OVERSIZING THE HOLE, CUT THE STRINGER P55 AND INSTALLING A SPECIAL REPAIR COUPLING IAW DRAWIN G R538-10691, APPROVED BY RAS 052653/080/2007 ISS A AND EA 6-5314-115239. 2 L 7 2 4F RT A35EU 2008032600290 20080326 00290 EU 2008 3 26 08FDEA01078 1 20080320 A 5754 A53510561200 FITTING AIRBUS 300 A300B4622R 3930312 EU KRUEGER FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CORROSION ON FITTING AT KRUEGER FLAP AREA LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008032600291 20080326 00291 EU 2008 3 26 08FDEA01079 1 20080320 A 5330 A53776533200 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 DURING REMOVAL OF STRINGER 26 LT DRILLING MARK EXISTS BETWEEN C38.2-39. REPAIR PERFORMED BY BUSH INSTALLATION IAW SRM 5 3-10-12 FIG 221. 2 L 7 2 4F RT A35EU 2008032600299 20080326 00299 NM 2008 3 26 DL757080391 1 20080318 A 5330 141N33131 SKIN BOEING 757 757232 1384965 NM FUSELAGE SCRATCHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 633DL 23614 SCRATCH IN FUSELAGE SKIN, FS440, STR6L TO 7L. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER AND TRIPLER. 2 L 7 2 4F RT A2NM 2008032600303 20080326 00303 EU 2008 3 26 MALA080042 1 20080317 A 5522 SKIN SAAB SF340 340B 7860101 EU LT ELEVATOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 444XJ 340B444 LT ELEVATOR UPPER SKIN LEADING EDGES HAVE 13 DENTS. REPAIRED IAW EO NR S55138. 2 L 7 2 4T RT A52EU 2008032600304 20080326 00304 EU 2008 3 26 MALA080043 1 20080317 A 5210 SKIN SAAB SF340 340B 7860101 EU PAX DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 444XJ 340B444 PASSENGER ENTRANCE DOOR HAS 1 DENT THAT IS DISBONDED. REPAIRED IAW EO NR S5202.8. 2 L 7 2 4T RT A52EU 2008032600306 20080326 00306 NM 2008 3 26 QXEA200800298 1 20080316 A 2150 78279018 ACM DHAV DHC8 DHC8202 2809007 NM A/C BAY MALFUNCTIONED A QXEA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 NM 09 355PH 43075 5717 500 PDX - FLIGHT 2193, ON APPROACH THE LAVATORY SMOKE DETECTOR WENT OFF TWICE. BOTH TIMES THE FLIGHT ATTENDANT REPORTED NO INDICATIONS OF SMOKE. AIR WAS SMOOTH AND THE BLEEDS WERE ON MAX. MAINTENANCE REPLACED THE AIR CYCLE MACHINE, CONDENSER /MIXER AND HEAT EXCHANGER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008032700003 20080327 00003 NM 2008 3 27 DHL2008765029 1 20080109 A 5755 SKIN BOEING 727 727264 138408M NM NR 4 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, NR 4 SPOILER NR 2 HINGE CUT OUT ON LT WING TRAILING EDGE CRACKED. STOP DRILLED CRACK DIAMETER 0.250 INC H AND FABRICATED REPAIR DOUBLER IAW SRM 51-10-1 AND 57-30-4 FIG 10, NDT CONFIRMED STOP DRILL END STOP CRACK IAW NDT MM C H 51-00-00 PART 6 FIG 25. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER AT NR 4 SPOILER NR 2 HING E CUT OUT ON LT WING TRAILING EDGE IAE SRM 57-30-4 FIG 10 AND 51-30-2. 2 L 7 3 4F A3WE 2008032700013 20080327 00013 CE 2008 3 27 725FX031008 1 20080310 A 2120 UNKNOWN CESSNA 208 208B 2073701 CE COCKPIT SMOKE E AXSA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 65 725FX 208B0460 FLT 7307 DEPARTED ISP-EWR AND AS THE PILOT LEVELED OFF AT 6000 FT AND TURNED ON THE HEAT THE COCKPIT APPEARED TO FILL WI TH SMOKE. THE PILOT TURNED OFF ALL UNNECESSARY EQUIPMENT AND DIVERTED TO BDR AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS INSPECTED BY MAINTENANCE TO INCLUDE SERVICING THE ENGINE WITH 2 QUARTS OF OIL, RUNNING THE ENGINE FOR AN EXTENDED P ERIOD WITH THE HEAT ON AND CHECKING THE ENGINE COMPARTMENT FOR ANY EVIDENCE OF LEAKING. NO DEFECTS OF ANY KIND WERE NOT ED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 H 7 1 3T A37CE 2008032700016 20080327 00016 NM 2008 3 27 DHL2008765031 1 20080117 A 5754 RIB BOEING 727 727264 138408M NM NR 3 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, CRACK INDICATION ON PREVIOUS REPAIR OF NR 3 SLAT OUTBOARD ACTUATOR SUPPORT RIB. REMOVED NR 3 SLAT ACCES S PANEL IAW SRM 51-30-2. REMOVED CRACKED RIB IAW SRM 51-30-2. LOCATED AND DRILLED NEW RIB IAW SRM 51-30-5. INSTALLED NEW RIB IAW SRM 51-30-2. REINSTALLED ACCESS PANELS AT NR 3 SLAT IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032700020 20080327 00020 NM 2008 3 27 DHL2008765004 1 20080119 A 5310 TORQUE BOX BOEING 727 727264 138408M NM BS 1243 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, AFT STAIRWELL LIGHTENING HOLE CRACKED 12 O'CLOCK POSITION RIGHT SIDE OF STAIRWELL BS 1243 (TORQUE BOX). CUT OUT DAMAGED AREA AT AFT STAIRWELL LIGHTENING HOLE BS 1243 RIGHT DIMENSION 1.5" BY .5" IAW SRM 51-40-2 FIG 1. FABRI CATED REPAIR AT AFT STAIRWELL LIGHTENING HOLE BS 1243 RIGHT IAW SRM 53-10-2 FIG 6A AND 51-40-2 FIG 1. TREATED AND PRIMED PART AND AREA IAW SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032700026 20080327 00026 SO 2008 3 27 RAIA00803010 1 20080311 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 818HK 145059 PRE FLT 5564 - OKC - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RESECURED THE WIRING TO THE EMERGENCY LIGHT. OPERATIONAL LY CHECKED GOOD. NO FURTHER DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008032700029 20080327 00029 NM 2008 3 27 2008UALA01399 1 20080314 A 3230 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LANDING GEAR MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 807UA 798 RETURN TO FIELD DUE TO INABILITY TO RETRACT LANDING GEAR. STILL WORKING. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032700030 20080327 00030 NM 2008 3 27 2008UALA01400 1 20080314 A 5753 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE T/E FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 LEFT O/B FLAP, NEAR MID POINT, 30" FROM AFT END, SKIN IS WORN. REPAIR PER EN57-0 028-03 AND EVA-71266. THE REPAIR IS AP PROVED BY BAC, 8100-9. THE REPAIR IS 12 MONTH LIMITED REPAIR, NEW 8100-9 MUST BE ISSUED TO COMPLY WITH 14 CFR25.571 AND 26.43(D). OK TO CF PER EVA 71266. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032700375 20080327 00375 2008 3 27 AALA200800529 2 20080309 A 7532 32143044 BLEED VALVE BOEING 757 757223 1384957 NM RT ENGINE LEAKING A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 690AA 25696 MIA INFLIGHT T725/09MAR - DURING CLIMB CREW RECEIVED RIGHT ENGINE OVERHEAT INDICATION. RETURNED TO MIA AND LANDED WITHO UT INCIDENT. REPLACED HIGH STAGE PNEUMATIC VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008032800023 20080328 00023 EA 2008 3 28 A6WA200840105 1 20080214 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 430AW 7719 ANGLE AT FS 280 LBL 9 AND RBL 9 INBOARD AND OUTBOARD FOUND CRACK. ANGLES REPLACED IAW REO 601R-53-11-171 REV D. OUTBOAR D ANGLE REPLACED IAW REO 601R-53-11-171 REV D, INBOARD ANGLE REPLACED IAW SRM 51-42-05 AND SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2008032800041 20080328 00041 SO 2008 3 28 C2XA08ON102 1 20080315 A 2611 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO SMOKE DETECTION MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 12569 145630 FLT 7822 - SMF - THIS FLIGHT DIVERTED TO SMF ON A ROUTE FROM LAX TO BOI, DUE TO A BAGGAGE SMOKE LIGHT ILLUMINATED INFLIG HT. NO EMERGENCY WAS DECLARED AND AIRCRAFT LANDED SAFELY. FLIGHT CREW REPORTED CLIMBING OUT OF LAX WENT THROUGH MOD TU RB SET OFF BAGGAGE LIGHT, NO MASTER WARNING. JUST LIGHT; DIVERTED TO SMF. MX INSPECTED CARGO DETECTORS, NO DEFECTS NOT ED AT THE TIME. AIRCRAFT PWR RESET NORMAL. FIRE AND SMOKE TEST OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEA SED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008032800042 20080328 00042 SO 2008 3 28 C2XA08ON103 1 20080313 A 7920 432278 OIL FILTER EMB 145 EMB145LR 3260212 SO NR 2 ENGINE CLOGGED A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 12569 13516 13516 145630 FLT 7823 - GEG - FLIGHT CREW REPORTED E2 OIL IMPENDING BYPASS MSG ON TAKEOFF ROLL. FLIGHT CREW DID NOT DECLARED EMERGEN CY AND AIRCRAFT LANDED SAFELY. CONTRACT MX REMOVED AND REPLACED OIL FILTER AND CREW OPERATIONALLY AND LEAK CHECKED SATI SFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008032800062 20080328 00062 NM 2008 3 28 SWAA081535 1 20080321 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 523, STR 13R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032800069 20080328 00069 NM 2008 3 28 SWAA081543 1 20080323 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032800079 20080328 00079 NM 2008 3 28 SWAA081552 1 20080323 A 3397 W4142001220 WIRE BOEING 737 73776Q 13845AA NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 551WN 30280 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT MID CABIN. FOUND LOOSE WIRE. SECURED LOOSE WIRE PER MM. 2 L 7 2 4F RT A16WE 2008032800080 20080328 00080 2008 3 28 SWAA081553 4 20080321 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032800083 20080328 00083 NM 2008 3 28 SWAA081573 1 20080323 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008032800095 20080328 00095 SO 2008 3 28 C2XA08IA086 1 20080321 A 2611 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO SMOKE DETECTION FALSE ACTIVATION A C2XA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING NR NOT REPORTED 1 SW 27 22971 145149 IAH - FLIGHT 4917, THE CREW REPORTED A LAV SMOKE WARNING IN FLIGHT WITH NO EVIDENCE OF SMOKE. CIRCUIT BREAKERS E11 AND E12 WERE PULLED IAW EMERGENCY / ABNORMAL PROCEDURES AND THE WARNING WENT AWAY. THE AIRCRAFT LANDED AT IAH WITHOUT INCID ENT WHERE MAINTENANCE REMOVED AND RESET THE CIRCUIT BREAKERS, INSPECTED THE AIRCRAFT, AND OPERATIONALLY CHECKED THE SMOK E DETECTION SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032800106 20080328 00106 NM 2008 3 28 SWAA081525 1 20080319 A 5523 DAS4141A BEARING BOEING 737 7375H4 138449D NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING AND BEAR ING PER SWA EA. 2 L 7 2 4F RT A16WE 2008032800128 20080328 00128 2008 3 28 UPS08851894 4 20080319 A 2565 SLIDE DOUG DC8 DC873F 302199F WP CABIN DEPLOYED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:N/A ESCAPE SLIDE PARTIALLY DEPLOYED. ESCAPE SLIDE PACK REMOVED FOR REPACKING. REPACKED AND REINSTALLED ESCAPE SLIDE. OK FOR SERVICE. REF MM 25-60-01-2. 2 L 7 4 4F RT 4A25 2008032800176 20080328 00176 NM 2008 3 28 SWAA081596 1 20080325 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 908, STR 15L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008032800182 20080328 00182 NM 2008 3 28 SWAA081640 1 20080325 A 5523 65C26384 TAB BOEING 737 7375H4 138449D NM LT ELEVATOR DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND LT ELEVATOR TAB DISBONDED AT NR 2 UPPER HINGE CUTOUT. REPAIRED TAB PER ER. 2 L 7 2 4F RT A16WE 2008032800186 20080328 00186 NM 2008 3 28 SWAA081636 1 20080325 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008032700033 20080327 00033 NM 2008 3 27 DHL2008765032 1 20080119 A 5754 RIB BOEING 727 727264 138408M NM NR 2 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, NR 2 SLAT OUTBOARD ACTUATOR SUPPORT RIB CRACKED. REMOVED ACCESS PANEL AT NR 2 SLAT IAW SRM 51-30-2. LO CATED AND DRILLED HOLES ON NEW RIB IAW SRM 51-30-5. INSTALLED NEW RIB AT NR 2 SLAT OUTBOARD ACTUATOR IAW SRM 51-30-2. INSTALLED ACCESS PANEL AT NR 2 SLAT IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032700036 20080327 00036 NM 2008 3 27 2008UALA01423 1 20080313 A 2611 CGAB140001 SMOKE DETECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO BAY FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 366UA 24535 AFT CARGO COMPT LOOP-A SMOKE DETECTOR INOP, DOES NOT TEST FAIL LIGHT ON. FOUND FAULTY SMOKE DETECTOR. REPLACED SMOKE DE TECTOR AFT A2 REFERENCE AMM 26-16-01. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700041 20080327 00041 2008 3 27 2008UALA01434 4 20080313 A 2562 ELT201 ELT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE AFT CABIN FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 120UA 29166 AIRPORT OPS REPORTED ELT TRANSMISSION FROM AIRCRAFT. FOUND AFT CABIN CLOSET ELT FAILS BIT. REPLACED ELT. AC OK FOR SERV ICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032700043 20080327 00043 NM 2008 3 27 DHL2008765021 1 20080120 A 5344 HINGE BOEING 727 727264 138408M NM BS 612 S4L CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, MCD AFT HINGE SECTION IS CRACKED AT BS 612 STRINGER 4L. REMOVED AFT HINGE SECTION AT MAIN CARGO DOOR BS 612 STRINGER 4L IAW MM FIG 5201B REV E. FABRICATED HINGE SECTION IAW MM FIG 5201B REV E. TREATED AND PRIMED PARTS AN D AREA IAW SRM 51-10-2. INSTALLED HINGE SECTION AT MCD BS 612 STINGER 4L IAW MM FIG 5201B REV E. 2 L 7 3 4F A3WE 2008032700044 20080327 00044 NM 2008 3 27 DHL2008765012 1 20080121 A 5313 STRINGER BOEING 727 727264 138408M NM BS 880 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK: DISCREPANCY - RT WHEEL WELL STRINGER 18A IS CORRODED AT WBL 70 ON FORWARD SIDE OF BS 880. REMOVED STRIN GER 18A IAW SRM 51-30-2. FABRICATED STRINGER 18A IAW SRM 53-10-2 FIG 4, 51-10-3 AND 51-30-5. TREATED AND PRIMED PART A ND AREA IAW SRM 51-10-2. INSTALLED REPAIR IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032700047 20080327 00047 EA 2008 3 27 MASA200800229 1 20080313 A 2150 78279015 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA RIGHT MALFUNCTIONED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 17337 18057 7337 ASH FLT 2818 PHX-DSM. STRONG SMOKE ODOR AT THE GALLEY AREA AND THE AFT CABIN AREA. REMOVED AND REPLACED RT PACK, OPS C HECK GOOD. 2 L 7 2 4F RT A21EA 2008032700049 20080327 00049 SO 2008 3 27 C2XA08CL031 1 20080316 A 2770 14542420401 SOLENOID EMB 145 EMB145LR 3260212 SO GUST LOCK DEFECTIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16987 145261 CLE FLIGHT 3040, THE CREW REPORTED THE GUST LOCK LEVER DID NOT STAY IN LOCKED POSITION. MAINTENANCE INSPECTED AND REPLA CED THE GUST LOCK SOLENOID. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008032700051 20080327 00051 NM 2008 3 27 DHL2008765034 1 20080123 A 5312 BULKHEAD BOEING 727 727264 138408M NM BS 227.8 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, BS 227.8 BULKHEAD FORWARD LOWER WEB AND STIFFENER IS CORRODED. REMOVED STIFFENERS AND ATTACHED PARTS IN AREA FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGED SECTION IAW SRM 51-40-4 FIG 1 AND 53-10-2 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-40-4 FIG 1 AND 51-30-2. LOCATED DRILLED AND INSTALLED NEW STI FFENERS (3 EACH) AND VERTICAL SECTION (1 EACH) IAW SRM 51-30-5 AND 51-30-2. REINSTALLED PREVIOUSLY REMOVED PARTS AT BS 227.8 BULKHEAD AREA IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032700053 20080327 00053 NM 2008 3 27 DHL2008749016 1 20080125 A 7110 NOSE COWL BOEING 727 7272J0 138407E NM NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 DURING C CHECK, NR 1 ENGINE NOSE COWL EXTERIOR SURFACE AT 9 O'CLOCK AFT TRAILING EDGE IS BENT OUT AND 1" CRACK. CUT OUT DAMAGE AREA DIMENSION 2" BY .75" IAW SRM 51-10-1. FABRICATED NEW DOUBLER REPAIR IAW SRM 51-30-5 AND 54-30-2 FIG 1. AL ODINED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 54-30-3 FIG 8 AND 51-30-2 ON NR 1 ENGINE NOSE COWL EXTERIOR SKIN TRAILING EDGE 9 O'CLOCK POSITION. 2 L 7 3 4F RT A3WE 2008032700056 20080327 00056 SO 2008 3 27 SWIA200819367 1 20080126 A 5210 BRACE EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 289YV 120289 PAX DOOR HAS CRACKED BRACE IN BAY NR 18, FOUND AT C-CHECK. REPLACED CRACKED BRACE IAW SRM 51-10-02. 2 L 7 2 4T RT A31SO 2008032700058 20080327 00058 NM 2008 3 27 DHL2008749015 1 20080128 A 7110 NOSE COWL BOEING 727 727200 138407E NM NR 1 ENGINE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 DURING C CHECK, NR 1 ENGINE NOSE COWL EXTERIOR SURFACE AT 9 O'CLOCK AFT TRAILING EDGE COWL TO COWL LIP FLANGE IS BENT, D ENTED, AND METAL PIECE BROKEN OFF. CUT OUT DAMAGE AREA ON NR 1 ENGINE NOSE COWL AFT TRAILING EDGE DIMENSION CUT OUT 1.7 5 INCH BY .5 INCH IAW B727 SRM 151-40-3 FIG 1. FABRICATED ANGLE REPAIR IAW SRM 54-10-2 FIG 1 AND 51-40-3 FIG 1. ALODIN E AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 2008032700062 20080327 00062 EA 2008 3 27 MASA200800231 1 20080316 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27318 7318 ASH FLT 7547 ORD-SPI, PASSENGER DOOR WILL NOT OPEN FROM THE OUTSIDE. LUBED OUTER HANDLE, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008032700066 20080327 00066 NM 2008 3 27 DHL2008765033 1 20080201 A 5754 RIB BOEING 727 727264 138408M NM NR 2 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, NR 2 SLAT INBOARD ACTUATOR SUPPORT RIB CRACKED. REMOVED INNER SKIN PANEL FOR ACCESS IAW SRM 51-30-2. R EMOVED DAMAGE INBOARD RIB IAW SRM 51-30-2. LOCATED AND DRILLED NEW RIB IAW SRM 51-30-5 AND 51-40-1. TREATED AND PRIME D HOLES AND AREA IAW SRM 51-10-2. INSTALLED NEW RIB IAW SRM 51-30-2. REINSTALLED INNER SKIN ACCESS PANEL IAW SRM 51-30 -2. 2 L 7 3 4F A3WE 2008032700070 20080327 00070 EA 2008 3 27 MASA200800236 1 20080316 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 505MJ 10070 ASH FLT 7389 BDL-ORD, FWD MOST CEILING FLOODLIGHT WAS INOP. RELAMPED FLOODLIGHT, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008032500277 20080325 00277 NM 2008 3 25 2008UALA01521 1 20080318 A 5712 RIB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 LEFT WING TANK LOWER RIB CRACKED WS 135.5 APPROX 12" FWD OF AFT SPAR. MAJOR REPAIR ACCOMPLISHED BY REMOVING DAMAGE AND VERIFYING DAMAGE REMOVAL WITH HFEC. REPAIRED RIB. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032500278 20080325 00278 NM 2008 3 25 2008UALA01520 1 20080318 A 5712 RIB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 RIGHT WING TANK RIB CRACKED AT WS 135.5 APPROX 12" FWD OF AFT SPAR. MAJOR REPAIR ACCOMPLISHED BY REMOVING DAMAGE AND VE RIFYING DAMAGE REMOVAL WITH HFEC. REPAIRED RIB. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032600012 20080326 00012 NM 2008 3 26 HALA0800400 1 20080312 A 2697 WIRE BOEING 767 767332 1382001 NM SMOKE DETECTOR EXPOSED A HALA K NONE N FALSE WARNING CR CRUISE 1 WP 13 596HA 23276 LEFT AFT LAV SMOKE DETECTOR WENT OFF DURING FLIGHT. FLIGHT ATTENDANT SAID WIRE WAS EXPOSED ON SMOKE DETECTOR, POSSIBLE TAMPERING WITH. INSPECTED LEFT AFT LAV SMOKE DETECTOR. NO FAULTS NOTED. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008032600034 20080326 00034 NM 2008 3 26 FLA200800128 1 20080317 A 3350 BR964424 LIGHT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE CABIN INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 906FR 450 1684 DURING THE CABIN CHECK, THE INSPECTION DISCLOSED EMERGENCY LIGHTS WERE NOT FUNCTIONING ON TWO ROWS (ROWS 8 AND 15). MAI NTENANCE REPLACED THE EMERGENCY LIGHTS ON THE TWO MALFUNCTIONING ROWS IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-1 9 PB 401. UPON COOMPLETION OF THE INSTALLATION THE LIGHTS WERE TESTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032600038 20080326 00038 WP 2008 3 26 08FDEA00976 1 20080317 A 5753 ARC2735 SKIN DOUG DC10 DC1030F 3023504 WP T/E FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 306FE 48287 DURING INSPECTION ON LT WING INBD FLAP UPPER SKIN FOUND 2 EA DENTS: 1) UPPER 1 INCH BY 1 INCH DEEP .074 INCH 2) LWR 2 I NCH BY 1.50 INCH DEEP .050 INCH. REPAIRED SKIN IAW SRM 57-10-00 VOL I FIG 65. 2 L 7 3 4F RT A22WE 2008032600066 20080326 00066 EU 2008 3 26 08FDEA01019 1 20080318 A 5330 A53777227200 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 OLD REPAIR C 36-37, P 13-14 RT IS NOT PERFORMED IAW RAS/DABRE/7002005/2002. DOUBLER REPAIR RENEWED IAW RAS/DABRE/700901 6/20008 ISS B AND DRAWING R5370627, APPROVED BY EA 6-5314-115238. 2 L 7 2 4F RT A35EU 2008032600083 20080326 00083 NM 2008 3 26 DL76G080365 1 20080313 A 3350 BATTERY PACK BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1612T 30575 RIGHT SIDE AFT 3 EXTERIOR EMERGENCY LIGHTS INOP. CHARGED BATTERY PACKS, OPS CHECK GOOD IAW B767-300 MM 33-51-07 WDM 33- 51-00. 2 L 7 2 4F RT A1NM 2008032600086 20080326 00086 EU 2008 3 26 2008UALA01498 1 20080316 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 432UA 587 CREW OXY SYSTEM NEEDS SERVICE. SERVICED CREW O2 SYSTEM, NO LEAKS WERE NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032600088 20080326 00088 NM 2008 3 26 2008UALA01538 1 20080318 A 2120 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN ODOR A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 313UA 23674 STRONG FUEL ODOR DETECTED IN CABIN. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032600090 20080326 00090 NM 2008 3 26 2008UALA01539 1 20080319 A 5720 STRIP BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU RT WING LOOSE A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 904UA 25004 RTFL DUE TO A SMALL STRIP OF METAL HANGING FROM RIGHT WING. RE-BONDED METAL STRIP TO WING. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032600091 20080326 00091 NM 2008 3 26 2008UALA01540 1 20080318 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 853UA 1688 GOUGE ON EXTERNAL SKIN FRAME 13 STR 5L. ACCOMPLISHED MAJOR REPAIR IN LCQ. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032600095 20080326 00095 NM 2008 3 26 2008UALA01542 1 20080318 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 294-360 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 CABIN FLOOR CREASE BEAM ADJACENT TO FWD GALLEY DOOR CUTOUT CORRODED IN SEVERAL AREAS BS 294-360 STR 17R. MAJOR REPAIR A CCOMPLISHED: REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032600097 20080326 00097 NM 2008 3 26 2008UALA01543 1 20080318 A 2612 6937307149 MODULE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FIRE DETECTION FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 932UA 26658 CREW REPORTS 1 ENG B FIRE LOOP WILL NOT TEST, A FIRE LOOP TESTS GOOD. SUSPECT FIRE TEST MODULE. REPLACED ENGINE AND AP U FIRE CONTROL MODULE REFERENCE AMM 26-21-51. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032600099 20080326 00099 2008 3 26 2008UALA01545 4 20080318 A 2565 O-RING BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE L2 SLIDE BOTTLE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 OVERWATER CHECK FOUND DOOR 2L SLIDE BOTTLE PRESSURE OUT OF GREEN BAND. FOUND FAULTY O-RING. REPLACED SLIDE RAFT ASSEMBL Y. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032600103 20080326 00103 NM 2008 3 26 2008UALA01548 1 20080319 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 32 HJK MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 199UA 28717 SEAT 32 HJK EMERGENCY LIGHT STRIP MISSING. REPLACED LIGHT STRIP SEAT 32 HJK. OPS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032600105 20080326 00105 NM 2008 3 26 2008UALA01550 1 20080318 A 5210 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR OUT OF TOLERANCE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 R2 DOOR UPPER HINGE ARM CUTOUT HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032800200 20080328 00200 NM 2008 3 28 SWAA081649 1 20080326 A 2560 63550 GIRT BAR BOEING 737 7377H4 1384404 NM EVAC SLIDE STUCK A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 241WN 32504 R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STUCK. FREED GIRT BAR PER MM. 2 L 7 2 4F RT A16WE 2008033100001 20080331 00001 EA 2008 3 31 A6WA200840125 1 20080225 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 BULKHEAD WEB CRACK AT FS 280 LBL 9. REMOVED IAW REO 53-11-171 REV D SHEET 2 EDDY CURRENT PERFORMED ON CUTOUT FPI PERFOR MED ON FABRICATED PARTS. REPAIR PERFORMED IAW REO 601R-53-11-171 REV D SCHEM B. (M) 2 L 7 2 4F RT A21EA 2008033100010 20080331 00010 NM 2008 3 31 SWAA081652 1 20080326 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED C2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 1 ABC. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008033100021 20080331 00021 WP 2008 3 31 08FDEA00984 1 20080317 A 5321 AGA38643 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 AFT PIT FLOOR PANEL NR 187 BF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL 187 BF; POTTED EDGES; COM PLETED CURE AND SANDED EDGE POTTING. INSTALLED INSERTS; FABRICATED TOP SHEET LAYED UP UNDER VAC BAG; COMPLETED CURE; C OUNTER SUNK HOLES AND APPLIED NON-SKID IAW SRZ 25-005 REV F AND 25-011 REV C. 2 L 7 3 4F RT A22WE 2008033100024 20080331 00024 WP 2008 3 31 08FDEA00986 1 20080317 A 5321 AGA38763 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 25 365FE 46601 AFT PIT FLOOR PANEL NR 187 EF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL 3 187 EF. LOCATED HOLES; POTTED EDGES; COMPLETED CURE; SANDED EDGES AND INSTALLED INSERTS. FABRICATED TOP SHEET AND LAYED UP UNDER A VAC BAG; COMPLETED CURE; COUNTER SUNK HOLES AND APPLIED NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008033100034 20080331 00034 NM 2008 3 31 SWAA081668 1 20080326 A 5311 6546534 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008033100042 20080331 00042 WP 2008 3 31 UPS08851936 1 20080305 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 MAIN CABIN INTERGRANULAR CORROSION ON FLOORBEAM STA 70 BETWEEN RBL 20 AND 48. REMOVED CORROSION, FA BBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-7, 51-1-8, 51-2-0, 53-7-3. 2 L 7 4 4F RT 4A25 2008033100051 20080331 00051 EU 2008 3 31 B4V2008F00000 2 20080119 A 7297 057150E000901AT CONNECTOR DIAMON DA42 DA42 2990004 EU THIELT TAE125 TAE12501 59300 EU ENGINE ARCED A B4VS K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 28 4130M 294 42AC069 020201618 CONNECTOR IS NOT MAKING GOOD CONTACT AND CAUSING ARCING AND ENGINE TO QUIT. PROBABLE CAUSE IS AUTOMOTIVE QUALITY AND NO T OF THE THREADED TYPE. TO PREVENT RECURRENCE RECOMEND USING AVIATION THREADED TYPE PLUG. (K) 1 L 7 2 3I 3 B RT A57CE E00069EN 2008033100060 20080331 00060 NM 2008 3 31 NWAA081185508 1 20080320 A 3040 CAP BOEING 757 757251 1384970 NM WINDOW HEAT DAMAGED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 508US 23197 DURING FLIGHT HAD ODD ELECTRICAL SMELL IN FLIGHT DECK. SMELL CAME FROM ABOVE COCKPIT WINDSHIELD VENT. FLIGHT CONTINUED ON AND LANDING WAS UNEVENTFUL. MAINTENANCE REPAIRED WINDOW HEAT TERMINAL CAP J-8. OPERATIONAL CHECKED GOOD AND AIRCRA FT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2008033100064 20080331 00064 NM 2008 3 31 AMTA200800120 1 20080224 A 5347 RAIL BOEING 737 73783N 13844HI NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 RAIL ASSY LBL 3.0, STAT 727I (T) UNION AREA HAVE A LIGHT CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS REPAIRED IAW EA 737-53-00-08-A0037. 2 L 7 2 4F RT A16WE 2008033100065 20080331 00065 NM 2008 3 31 AMTA200800123 1 20080224 A 5320 FLOOR SUPPORT BOEING 737 73783N 13844HI NM BS 767-787 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 AFT CARGO COMPARTMENT RT DECK SUPPORT SECTION 46 BETWEEN STA 787 AND 767, FOUND WITH EXFOLIATION CORROSION. (K) 2 L 7 2 4F RT A16WE 2008033100072 20080331 00072 WP 2008 3 31 08FDEA01143 1 20080325 A 7110 9020M10P008A WEB DOUG MD10 MD1010F 3022112 WP NR 1 COWLING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 NR 1 ENGINE WEB APPEARS TO HAVE CORROSION JUST FWD OF THE HYD FILTER BOWLS. REPAIRED WEB IN REF TO EA 8-7220-118465 . 2 L 7 3 4F RT A22WE 2008033100075 20080331 00075 NM 2008 3 31 AMTA200800158 1 20080228 A 5320 CHANNEL BOEING 737 73783N 13844HI NM BS 727-847 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 AFT CARGO COMP ZEE CHANNEL LT BETWEEN STA 727I TO STA 847 FOUND WITH EXFOLIATION CORROSION. REMOVED CORROSION ON ZEE CH ANNEL, LBL 19 FROM STA 727I TO STA 848, ORG MAT .032, MAT LOSS .007 REMAINING MAT .025, FOUND TO BE OUT OF LIMITS IAW SR M 53-00-53, FABRICATED ZEE CHANNEL AND SPLICE FROM BAC 1496-377 IAW SRM 53-00-53-2R. (K) 2 L 7 2 4F RT A16WE 2008033100078 20080331 00078 WP 2008 3 31 08FDEA01145 1 20080325 A 7830 9095M49P002C FAIRING DOUG MD10 MD1010F 3022112 WP THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 NR 3 ENGINE OUTBD T/R UPPER INNER FAIRING IS CRACKED. VERIFIED CRACK PER NTSPM 06-10-11-001. REMOVED DAMAGE IAW ESPM 7 8-32-01. LOCATED & DRILLED HOLES IAW ESPM 78-32-03. FABBED DOUBLER IAW ESPM 78-32-03. ALODINED & PRIMED DOUBLER IAW DC/ MD- 10 SRM 51-21-01; VOL II. INSTALLED NEW FAIRING IAW ESPM 78-32-03. 2 L 7 3 4F RT A22WE 2008033100083 20080331 00083 NM 2008 3 31 AMTA200800164 1 20080228 A 5730 SKIN PANEL BOEING 737 73783N 13844HI NM LT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LT WING FUEL TANK ACCESS 532RB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROS ION ON LT FUEL TANK ACCESS LANDING 532RB IAW B737-800, SRM 51-01-02-0G ORG MAT .176, MAT LOSS .004, REM MAT .172, FOUND WITHIN LIMITS IAW SRM 57-20-01-1A, IAW FORMED FLAP PEENING IAW SRM 51-20-06 AND SOPM 20-10-03. 2 L 7 2 4F RT A16WE 2008033100084 20080331 00084 NM 2008 3 31 AMTA200800165 1 20080228 A 5730 SKIN PANEL BOEING 737 73783N 13844HI NM LT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LT WING FUEL TANK ACCESS 532QB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROS ION ON LT FUEL TANK ACCESS LANDING 532QB, IAW B737-800, SRM 51-01-02-0G, ORG MAT .176, MAT LOSS .006, REM MAT .170, FOUN D WITHIN LIMITS IAW 57-20-01-1A, PERFORMED FLAP PEENING 51-20-06 AND SOPM 20-10-03. 2 L 7 2 4F RT A16WE 2008033100090 20080331 00090 NM 2008 3 31 AMTA200800172 1 20080228 A 5730 SKIN PANEL BOEING 737 73783N 13844HI NM LT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LT WING FUEL TANK ACCESS 532HB HAS PITTING CORROSION ON LWR SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROSIO N ON LWR FUEL TANK ACCESS LANDING 532HB IAW B737-800, SRM 51-01-02=0G, ORG MAT .206, MAT LOSS .004, REM MAT .202, FOUND TO BE WITHIN LIMITS IAW SRM 57-20-01-A1-1, PERFORMED FLAP PEENING IAW SRM 51-20-06 AND SOPM 20-10-A1-1, PERFORMED FLAP P EENING IAW SRM 51-20-06 AND SOPM 20-10. (K) 2 L 7 2 4F RT A16WE 2008033100102 20080331 00102 EU 2008 3 31 08FDEA01153 1 20080326 A 5210 A5217542101363 WEB AIRBUS 310 A310324 3930206 EU ENTRY DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 LEFT AFT ENTRY DOOR HAS CORROSION ON THE VERTICAL WEB AROUND A GROMMET HOLE. REMOVED AND REPLACED LT VERTICAL WEB ON TH E AFT ENTRY DOOR IAW SRM 51-40-21 PG 7. 2 L 7 2 4F RT A35EU 2008033100104 20080331 00104 SO 2008 3 31 SWIA200819373 1 20080307 A 5420 NACELLE EMB 120 EMB120ER 3260203 SO LT ENGINE DAMAGED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 581SW 120349 LEFT LOWER NACELLE AT OIL COOLER AREA DAMAGED FROM BIRD STRIKE. REPAIRED THE LOWER NACELLE BIRD STRIKE DAMAGE AREA IAW EMB SRM 51-40-22, 51-40-06, 51-22-00 AND 51-25-00. 2 L 7 2 4T RT A31SO 2008033100111 20080331 00111 NM 2008 3 31 AMTA200800187 1 20080228 A 5730 SKIN PANEL BOEING 737 73783N 13844HI NM RT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 RT WING FUEL TANK ACCESS 631BB HAS PITTING CORROSION ON LOWER SKIN PANEL AND CLAMP RING. REMOVED PITTING CORROSION ON R T WING FUEL TANK ACCESS LANDING IAW B737-800, SRM 51-10-02-1A-1, ORG MAT .200, MAT LOSS .002, REM MAT .198, FOUND TO BE WITHIN LIMITS IAW SRM 57-20-01-1A-1, PERFORMED FLAP PEENING IAW SRM 51-20-06 AND SOPM 20-10-03. (K) 2 L 7 2 4F RT A16WE 2008033100112 20080331 00112 NM 2008 3 31 AMTA200800189 1 20080229 A 5315 FLOORBEAM BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 1485 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 520AT 27976 AFT CARGO, FOUND CORROSION ON FLOOR STRINGER STA 1485, RBL (EXFOLIATION). REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED IAW 51-70-06. TREATED AND PRIMED AREA IAW SRM 51-20-01. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008033100115 20080331 00115 NM 2008 3 31 AMTA200800194 1 20080301 A 5347 RAIL BOEING 737 73783N 13844HI NM BS 727 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 RAIL ASSY LBL 8.1, STA 727I (T-UNION) AREA HAS LIGHT CORROSION. REMOVED CORROSION ON RAIL, OR MAT .071, MAT LOSS .012, REM MAT .059, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A, FIG 103, DETAIL D, FABRICATED REPAIR IAW SRM 53-00-53-2R2, TABLE 201 AND EA 737-5300-08-A0037. (K) 2 L 7 2 4F RT A16WE 2008033100117 20080331 00117 NM 2008 3 31 AMTA200800196 1 20080301 A 5347 RAIL BOEING 737 73783N 13844HI NM BS 767 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 RAIL ASSY LBL 12.5, STA 767 HAVE A UNIFORM CORROSION, AFT CARGO COMPARTMENT. REMOVED CORROSION ON RAIL, ORG MAT .071, M AT LOSS .014, REM MAT .057, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A DETAIL D, FABRICATED REPAIR PART FROM BAC 1510 -1355 IAW EA 737-5300-08-A0036. (K) 2 L 7 2 4F RT A16WE 2008033100121 20080331 00121 NM 2008 3 31 AMTA200800201 1 20080229 A 2432 893003 CHARGER BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE BATTERY UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 550TZ 32584 EICAS MESSAGE MAIN BATTERY CHARGER. REMOVED AND REPLACED MAIN BATTERY CHARGER IAW MM 24-31-02-4. TESTED GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008033100122 20080331 00122 SO 2008 3 31 SWIA200819374 1 20080307 A 5711 SPAR EMB 120 EMB120ER 3260203 SO LT WING DAMAGED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 581SW 120349 LEFT WING ROOT AUXILIARY SPAR DAMAGED FROM BIRD STRIKE. REPAIRED THE LEFT WING ROOT SPAR IAW EMB REF IC2008-120/01998-A . 2 L 7 2 4T RT A31SO 2008033100123 20080331 00123 EA 2008 3 31 SWIA200819375 1 20080321 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCONNECTED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 452SW 7716 FLT 3898 - EMERGENCY LIGHTS FROM 9C TO 12C ARE NOT WORKING. RESECURED LIGHT STRIP CONNECTION. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008033100129 20080331 00129 2008 3 31 AMTA200800206 4 20080305 A 3460 DISPLAY BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE FMC UNSERVICEABLE A AMTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 11 550TZ 32584 IAW CREW DEBRIEF F/O, SFMC CDU INTERMITTENTLY BLANKS OUT, SELECT SW. TO ALTERNATE, NO HELP. REMOVED AND REPLACED FMC CD U IAW AMM 344-62-02. OPS CHECKED GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008033100133 20080331 00133 SO 2008 3 31 XGN2008F00003 2 20080227 A 8530 ECITISN712BCA CYLINDER CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO ENGINE CRACKED A XGNA K NONE O OTHER IN INSP/MAINT 1 SW 05 5421M 402B0021 CYLINDER CRACKED BETWEEN FIN NR1-3 BEHIND INJECTOR, DEFECTIVE PRODUCT. (K) 1 L 7 2 3O 3 O A7CE E8CE 2008033100134 20080331 00134 SO 2008 3 31 XGN2008F00004 2 20080227 A 8530 ECITISN712BCA CYLINDER CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO ENGINE CRACKED A XGNA K NONE O OTHER IN INSP/MAINT 1 SW 05 5421M 544 402B0021 815088 CYLINDER CRACKED BEHIND NR 1-3 FIN BY FUEL INJECTOR, DEFECTIVE PRODUCT. (K) 1 L 7 2 3O 3 O A7CE E8CE 2008032700372 20080327 00372 NM 2008 3 27 AALA200800563 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT SEAT 38C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 38C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700376 20080327 00376 NM 2008 3 27 AALA200800557 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700393 20080327 00393 NM 2008 3 27 AALA200800526 1 20080307 A 3350 LENS BOEING 777 777223 1385213 NM DOOR MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 787AL 30010 DFW - EMERGENCY LIGHT EXTERIOR LEFT NUMBER ONE DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT EXTERIOR LEFT NU MBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700399 20080327 00399 NM 2008 3 27 AALA200800573 1 20080311 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 21C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700402 20080327 00402 NM 2008 3 27 AALA200800576 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 26C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800004 20080328 00004 NM 2008 3 28 AALA200800581 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 40C INOPERATIVE. REPLACED SOCKET AND LAMP FOR EMERGENCY LIGHT AT SEAT 40C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800044 20080328 00044 NM 2008 3 28 SWAA081519 1 20080319 A 5754 65C26601 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED C1 CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT INBOARD T/E. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008032800063 20080328 00063 NM 2008 3 28 SWAA081571 1 20080323 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032800064 20080328 00064 NM 2008 3 28 SWAA081570 1 20080323 A 5523 6959227 BUSHING BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED C1 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BUSHING PER SWA EA. 2 L 7 2 4F RT A16WE 2008032800073 20080328 00073 NM 2008 3 28 SWAA081540 1 20080323 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032800093 20080328 00093 NM 2008 3 28 SWAA081562 1 20080321 A 5755 656717910 LUG BOEING 737 737317 138447P NM NR 5 SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SPOILER INBOARD ATTACH LUG CRACKED. REMOVED AND REPLACED ATTACH LUG PER SWA EA. 2 L 7 2 4F RT A16WE 2008032800098 20080328 00098 NM 2008 3 28 SWAA081579 1 20080324 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 279WN 32532 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008032800144 20080328 00144 NM 2008 3 28 SWAA081583 1 20080324 A 5310 6948062 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REMOVED AND REPLACED FRAME PER ACO. 2 L 7 2 4F RT A16WE 2008032800158 20080328 00158 WP 2008 3 28 UPS08851917 1 20080320 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 BROKEN FITTING IN FWD ACC COMPT STA 640 L35R-L36. FABRICATED AND REPLACED FITTING AT STA 640 AND L35 R-L36 IAW DWG 3750 834, SRM 51-1-8, SRM 51-01-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 2008032800168 20080328 00168 NM 2008 3 28 SWAA081605 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032800189 20080328 00189 NM 2008 3 28 SWAA081634 1 20080325 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500C, STR 27L TO STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032800192 20080328 00192 NM 2008 3 28 SWAA081617 1 20080325 A 5330 6545767 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 433 AND BS 448, LB L 3 AND RBL 2. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032600106 20080326 00106 NM 2008 3 26 2008UALA01551 1 20080318 A 5210 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 L2 DOOR HINGE ARM CUTOUT HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032600107 20080326 00107 NM 2008 3 26 2008UALA01552 1 20080318 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 577UA 26693 EXTERIOR EMERGENCY LIGHT AT DOOR 2L INOP. REPLAMPED ASSY, OPS CHECKED NORMALLY. FOUND LAMP INOPERATIVE. REPLAMPED ASSY , OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032600124 20080326 00124 SO 2008 3 26 CHQA200800051 1 20080315 A 2131 92185A010200 CONTROLLER EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN PRESSURE FAULTY A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 579RP 8785 145871 CAE311509 MSN TO CVG - WHILE CLIMBING THROUGH 13,000 FT, THE CREW RECEIVED A CABIN ALTITUDE RED MESSAGE CABIN ALTITUDE 10,000 ALON G WITH A WARNING MESSAGE. THE CREW LEVELED OFF AT 15,000 FT THEN STARTED TO DESCEND. WHILE DESCENDING THE CABIN PRESSU RE BECAME AMBER THEN GREEN AGAIN. THE AIRCRAFT LANDED BACK AT MSN UNEVENTFULLY. MAINTENANCE DEFERRED BOTH OUTFLOW VALV ES AND THE AIRCRAFT WAS FERRIED UNPRESSURIZED TO CVG. ONCE IN CVG MAINTENANCE TROUBLESHOT THE FAULT DOWN TO THE PRESSUR E CONTROLLER, AND AFTER REPLACING IT, THE PRESSURIZATION SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008032600137 20080326 00137 SO 2008 3 26 SWIA200819349 1 20080115 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 250YV 120250 LEFT SIDE FLOOR SEAT TRACK FRONT SECTION IS CORRODED, FOUND AT C-CHECK. REPLACED LEFT SEAT TRACK IAW APPROVED REPAIR 55 -12-345-1235. 2 L 7 2 4T RT A31SO 2008032600152 20080326 00152 EA 2008 3 26 SWIA200819355 1 20080312 A 3350 AD20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 935SW 3050 3050 7725 FORWARD EMERGENCY LIGHT STRIP ON FLOOR AND ALSO AT LEFT EMERGENCY EXIT DOOR IS INOP. REPLACED NR 2 EMERGENCY LIGHT BATT ERY. OPS CHECKS GOOD IAW AMM 33-51-04. 2 L 7 2 4F RT A21EA 2008032600156 20080326 00156 SO 2008 3 26 SWIA200819359 1 20080315 A 3397 WIRE EMB 120 EMB120ER 3260203 SO FUSELAGE DAMAGED A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 288SW 120316 FLT 5561 - RED EMERGENCY LIGHTS ARE NOT WORKING. REPAIRED WIRING AT ENVIRONMENTAL SPLICE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008032600229 20080326 00229 WP 2008 3 26 08FDEA01055 1 20080319 A 5712 ARB29188 RIB DOUG DC10 DC1030F 3023504 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 307FE 48291 RT WING L/E INT ZONE FOUND CRACK ON RIB. REPAIRED FORMER IAW SRM 57-00-01 FIG 10 SHT 1 VOL I. 2 L 7 3 4F RT A22WE 2008032600232 20080326 00232 NM 2008 3 26 22967 1 20080324 A 2540 CONTAINER EMB ERJ170 ERJ170200LR 3260121 NM LAV WASTE SMOKE A C77A A UNSCHED LANDING A FLAME/FIRE CR CRUISE 1 EA 27 614CZ 17000205 DURING FLIGHT, IN THE AFT GALLEY WHEN ONE FLIGHT ATTENDANT DETECTED AN ODOR OF SMOKE, INVESTIGATED AFT LAV AND FOUND SM OKE COMING FROM THE AFT LAV WASTE BIN. FLIGHT ATTENDANT EXTINGUISHED THE FIRE USING A PORTABLE HALON EXTINGUISHER. IT W AS REPORTED THAT THERE WAS WATER IN THE LAV WASTE BIN. THE AIRCRAFT THEN DIVERTED. 2 L 7 2 4F RT A56NM 2008032600234 20080326 00234 EA 2008 3 26 N6WA0080302 1 20080322 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE CABIN INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 163GJ 10255 ONE CEILING EMERGENCY LIGHT INOP. OPS CHECKED GOOD ON GROUND IAW AMM 33-51-09. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008032600237 20080326 00237 CE 2008 3 26 938012108A 1 20080121 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUSELAGE CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 81538 UE199 AT SCHEDULED INSPECTION, DISCOVERED ONE INCH LATERAL CRACK IN FUSELAGE BELLY SKIN IN SPAR AREA AT BL 30.62. STOP DRILLE D CRACK AND INSTALLED REINFORCEMENT DOUBLER REF SRM 53-90-18, (FUSELAGE SKIN CRACK REPAIR IN SPAR AREA). 2 L 7 2 4T 4 T RT A24CE E26NE 2008032600239 20080326 00239 CE 2008 3 26 933011308A 1 20080113 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 281 CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 81533 UE137 AT SCHEDULED INSPECTION, DISCOVERED (2) CRACKS IN FUSELAGE BELLY SKIN AT FS 281, ONE WAS A (2) INCH LATERAL CRACK, AND T HE OTHER A ONE INCH LONGITUDINAL CRACK, STOP DRILLED CRACKS AND INSTALLED ONE EXTERNAL DOUBLER OVER BOTH CRACKED AREA. REFERENCE SRM 53-90-18. 2 L 7 2 4T 4 T RT A24CE E26NE 2008032600243 20080326 00243 2008 3 26 DXTA20082961 4 20080324 A 2210 AUTOPILOT SYS CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE INOPERATIVE E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 391QS 5600493 AT FL430 ACCIDENTLY HIT TURN KNOB, AUTO PILOT WOULD NOT WORK CORRECTLY. IN HEADING MODE IT WOULD ALWAYS STOP 10 DEG SHO RT OF THE HEADING BUG. NO FAULT CODES REPORTED. DISCREPANCY RELATED TO INVERTER FAULT. INVERTER SELECT SWITCH REPLACE D. OPERATIONAL CHECK GOOD. IAW 560 M.M. CH. 24-20-04. 2 L 7 2 4F 4 F RT A22CE E25EA 2008032600248 20080326 00248 CE 2008 3 26 DJFA8032 1 20080325 A 2612 SMOKE DETECTOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP CARGO BAY LOOSE E DJFA O OTHER J WARNING INDICATION CL CLIMB 1 EA 23 809LX 258432 AFTER TAKEOFF, THE CREW REPORTED THE BAGGAGE FIRE LIGHT ILLUMINATED. A FLASHING SEQUENCE WAS NOTED AND THE BAGGAGE LIGHT WAS INTERMITENT DURING THE FLIGHT. THE AC DIVERTED AND LANDED WITHOUT INCIDENT. MAINT PERFORMED VISUAL INSPECTION OF F WD / AFT / LAV SMOKE DETECTORS. FOUND FWD SMOKE DETECTOR PHOTO CELL HOUSING WITH BACKED OFF NUTS AND ALSO FOUND DETECTOR CAGE CONTACTING SOLDER JOINTS INTERNAL OF DETECTOR. SECURED LOOSE CONNECTION AND REPOSITIONED CAGE. PERFORMED SMOKE DE TECTOR TEST ON GROUND AND CKS GOOD. 2 L 7 2 4F 4 F RT A3EU E6WE 2008032600253 20080326 00253 SW 2008 3 26 AC2A119271 1 20080317 A 7100 WARNING LIGHT BELL 430 430 1182150 SW ALLSN 250C 250C40B 03032 NE ILLUMINATED B AC2A O OTHER J WARNING INDICATION CR CRUISE 1 SW 31 430CT 49089 CAE844078 NR 2 ENGINE CHIP SUMP LIGHT ILLUMINATED IN FLIGHT. FOLLOWED EMERGENCY CHECKLIST AND LANDED. REMOVED CHIP PLUGS, CLEANED AND PERFORMED PENALTY RUN. FOUND SERVICEABLE. 1 G 7 2 3U 3 U RT H9SW E1GL 2008032600255 20080326 00255 CE 2008 3 26 DXTA20082964 1 20080325 A 3260 INDICATOR BEECH MU300 400A 1155402 CE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 138QS RK492 UPON GEAR RETRACTION, ALL GREEN DOWN AND LOCKED LIGHTS EXTINGUISHED. HOWEVER, RED IN TRANSIT LIGHT REMAINED ILLUMINATED . REPLACED GROUND SAFE PCB A161. OPS CHECK GOOD. IAW MM CH 32-60-00. 2 H 7 2 4F RT A16SW 2008032600259 20080326 00259 EU 2008 3 26 08FDEA01092 1 20080321 A 5542 PANEL AIRBUS 310 A310324 3930206 EU RUDDER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 LEFT RUDDER PANEL, 25TH FASTENER FROM THE TOP OF THE RUDDER HAS 1 CELL OF WATER, MARKED IN WHITE MARKER. REPAIRED LT RUDDER PANEL 25TH FASTENER FROM TOP BY REMOVING DAMAGE & BONDING A NEW CORE & LAY-UP REPAIR PLIES IAW EA 6-5540-118453. 2 L 7 2 4F RT A35EU 2008032600260 20080326 00260 NM 2008 3 26 NWAA081036623 1 20080320 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 523US 23617 DURING OVERNIGHT CHECK, FOUND EMERGENCY PATH LIGHTS BOTH SIDES FROM ROW 35 TO 45 INOP. MAINTENANCE REMOVED AND REPLACED BATTERY AND POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2008032600281 20080326 00281 NM 2008 3 26 08FDEA01069 1 20080320 A 5320 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 580FE 48471 MAIN DECK CARGO DOOR, LOWER JAMB FITTING FOUND NR 1 MOUNT HOLE POSITION "A", "B", AND "D" CRACKED. COMPLIED WITH EA 1 -5310-112601 PART 1. FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6 -2-100. 2 L 7 3 4F RT A22WE 2008032600293 20080326 00293 EU 2008 3 26 MALA080026 1 20080220 A 5753 SKIN SAAB SF340 340B 7860101 EU T/E FLAP DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 340B453 DURING 4K CHECK, PERMANENT REPAIR WAS MADE TO LT FLAP LOWER SURFACE IAW EO NR S57060. COMPLETE PERMANENT REPAIR TO RT F LAP LOWER SURFACE LOCATED AT WS 85 PROTRUDING HEAD BLIND RIVET. 2 L 7 2 4T RT A52EU 2008032700002 20080327 00002 NM 2008 3 27 DHL2008765028 1 20080109 A 5755 SKIN BOEING 727 727264 138408M NM NR 4 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, NR 4 SPOILER NR 3 HINGE CUT OUT ON LEFT WING TRAILING EDGE CRACKED. STOP DRILLED CRACK DIAMETER 0.250" IAW SRM 51-10-1 AND 57-30-4 FIG 10, NDT STOP DRILL CONFIRMED END OF CRACK IAW NDT MM CH 51-00-00 PART 6. FABRICATED REP AIR DOUBLER IAW SRM 57-30-4 FIG 10. TREATED AND PRIMED AREA AND PARTS IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER AT NR 4 SPOILER NR 3 HINGE CUT OUT AT LEFT WING TRAILING EDGE IAW SRM 57-30-4 FIG 10 AND 51-30-2. 2 L 7 3 4F A3WE 2008032700008 20080327 00008 NM 2008 3 27 DHL2008765013 1 20080115 A 5753 SKIN BOEING 727 727264 138408M NM FORE FLAP GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, LT OUTBOARD FORE FLAP OUTBOARD LEADING EDGE REPAIR IS GOUGED 2 PLACES. REMOVED OLD DOUBLER REPAIR IAW S RM 51-30-2. FABRICATED NEW DOUBLER REPAIR IAW SRM 57-50-2 FIG 4. TREATED AND PRIMED NEW DOUBLER IAW SRM 51-10-2. INST ALLED NEW DOUBLER IAW SRM 51-30-2. REPAIR SRM 57-50-4 FIG 1. 2 L 7 3 4F A3WE 2008032700031 20080327 00031 EU 2008 3 27 2008UALA01410 1 20080313 A 2611 PPA120100 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FWD LAVATORY FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 487UA 1669 ECAM SMOKE LAVATORY DETECTOR FAULT. REPLACED FWD LAV DETECTOR. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032700037 20080327 00037 NM 2008 3 27 2008UALA01424 1 20080313 A 2611 SMOKE DETECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD CARGO BAY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 366UA 24535 FWD CARGO COMPT LOOP-B SMOKE DETECTOR INOP, DOES NOT TEST FAIL LIGHT ON. REPLACED SMOKE DETECTOR B2 FWD REFERENCE AMM 2 6-16-01. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700038 20080327 00038 NM 2008 3 27 DHL2008749014 1 20080120 A 5752 TAB BOEING 727 7272J0 138407E NM AILERON DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 DURING C CHECK, LT WING OUTBOARD AILERON CONTROL TAB HAS A DENT WBL 592 TOP SURFACE. DENTED AREA FOUND OUT OF LIMITS IA W SRM 57-50-1 FIG 4, CUT OUT DENTED AREA APPROXIMATE 2" DIAMETER. FABRICATED FILLER APPROXIMATE 2 INCHES DIAMETER AND D OUBLER APPROXIMATE 5" BY 5", CLEANED, PREPPED, PRIMED, BONDED, TREATED, AND SEALED EDGES IAW SRM 57-50-2 FIG 8, 51-40-2, AND 51-40-20 FIG 3. TAB WEIGHT BEFORE REPAIR 3.59 LBS. TAB WEIGHT AFTER REPAIR 3.65 LBS. WITHIN LIMITS IAW SRM 51-80 FIG 2. 2 L 7 3 4F RT A3WE 2008032700055 20080327 00055 SO 2008 3 27 SWIA200819366 1 20080126 A 5210 BRACE EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 289YV 120289 PAX DOOR FORWARD SIDE INTERNAL BRACE IS CRACKED IN BAY NR 15, FOUND AT C-CHECK. REPLACED FRAME IAW SRM 51-10-02. 2 L 7 2 4T RT A31SO 2008032700057 20080327 00057 NM 2008 3 27 DHL2008765022 1 20080127 A 5710 BEAM BOEING 727 727264 138408M NM RT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, REJECTED NR 105146 BECAUSE ORIGINAL FABRICATED 'J' BEAM WAS DAMAGED UPON INSTALLATION. RT WING TRAILING EDGE UPPER 'J' BEAM IS CRACKED AT WBL 118. REMOVED TRAILING EDGE PANEL FOR ACCESS AT RT WING IAW SRM 51-30-2. REMOVED 'J' BEAM AT RT SIDE IAW SRM 51-30-2. FABRICATED 'J' BEAM STIFFENER AS PER EC-00728-001 DRAWING NR 65-21625 REV J. LOC ATED AND DRILLED HOLES IAW SRM 51-30-5. TREATED AND PRIMED NEW 'J' BEAM IAW SRM 51-10-2. INSTALLED NEW 'J' BEAM IAW DR AWING NR 65-21655 REV J, AS PER EC-00724-001. INSTALLED TRAILING EDGE PANEL UPPER WING IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032700068 20080327 00068 NM 2008 3 27 DHL2008765015 1 20080201 A 5753 STRUCTURE BOEING 727 727264 138408M NM LT WING TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, LEFT INBOARD MID FLAP LOWER TRAILING EDGE WBL 102 AT PUSH-ROD IS CRACKED, INBOARD. REMOVED INBOARD MID FLAP LOWER SKIN AND NR 3 TEAR DROP FOR ACCESS IAW SRM 51-30-2. FABRICATED NEW SECTION DIMENSION 57.5" LONG IAW SRM 53-3 0-5 AND 57-50-2 FIG 5. TREATED AND PRIMED PART AND AREA IAW SRM 51-10-2. INSTALLED NEW PART IAW SRM 51-30-2. INSTALLE D LT INBOARD MID FLAP LOWER SKIN AND NR 3 TEAR DROP IAW SRM 51-30-2. OPS CHECK GOOD IAW MM 27-51-00. 2 L 7 3 4F A3WE 2008032700079 20080327 00079 EU 2008 3 27 F3LA200800120 1 20080302 A 5320 D53112191202 SILL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE NUT PLATE HOLES BELOW THE FORWARD AND AFT GIRT BAR FITTINGS ON THE L-1 DOOR SILL. MAINTENANCE BLENDED THE CORROSION, TREATED AND PAINTED THE AFFECTED AREAS IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30106 AND SRM 51-74-00, PARAGRAPH 6. UPON COMPLETION OF THE REPAIRS, THE AREAS WERE INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032700082 20080327 00082 SO 2008 3 27 RAIA0803011 1 20080314 A 3230 23092400401 UPLOCK EMB 145 EMB145 3260210 SO LT MLG MALFUNCTIONED A RAIA B EMER. DESCENT J WARNING INDICATION LD LANDING 1 CE 03 809HK 19473 19473 145187 FLT 5502 - STL - YAW DURING LANDING GEAR EXTENSION. LEFT MAIN INDICATED IN TRANSIT FOLLOWED BY A LANDING GEAR DISAGREE MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE LT MLG UPLOCK BOX. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2008032700083 20080327 00083 2008 3 27 TRBA2008033 4 20080319 A 3497 NSA93412101C DIODE AEROSP ATR72 ATR72212A 8680902 EU COCKPIT 22VU FAILED A TRBA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 29 533AT 533 AVIONICS VENT C/B POPPED AND COULD NOT BE RESET. WHEN TESTING ANNUNCIATOR LIGHTS ELECTRICAL SMOKE ODOR AND "ANNUNCIATOR LIGHT TEST" C/B POPPED OUT. RESET OK. REMOVED AND REPLACED DIODE BOX 22VD IAW JIC NR 20-45-10 AND OPT CK OK. RELOCAT E WIRE TERMINAL PLU A/B AT CONNECTOR 22VT IAW AWM STANDARD PRACTICES NR 20-45-11, AWM NR 33-14-01 AND NR 21-51-05. OPT CK OK. 2 H 7 2 4T RT A53EU 2008032800201 20080328 00201 NM 2008 3 28 SWAA081661 1 20080326 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND KEEL BEAM CHORD CORRODED BETWEEN BS 510D TO BS 540, RBL 6. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2008032800210 20080328 00210 EA 2008 3 28 A6WA200840122 1 20080219 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 529-523 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 CRACK FOUND ON HYDRAULIC BRACKET ON MLG BAY FS 529 AND 523 RBL 27. REPLACED IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2008033100003 20080331 00003 WP 2008 3 31 IXXA08SMN053S 1 20080207 A 5340 SUPPORT ANGLE DOUG DC8 DC871F 302199D WP ZONE 200 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO FORMER CRACKED AT STATION 1766.000 LONGERON1. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP HOLE ON END CRACK. FABRICATED ANGLE DOUBLER. PERFORMED HEAT TREATMENT CLEANE D, TREATED AND PRIMED AREA AND ANGLE DOUBLER. INSTALLED NEW FASTENERS AND ANGLE DOUBLER IAW SRM 51-1-20D, 51-3-1, SRM 5 3-2-0 PAGE 2P, SRM 51-1-1 PAGES 1 13 AND 17, AND SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008033100011 20080331 00011 NM 2008 3 31 QXEA200800306 1 20080313 A 5320 STRUCTURE BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX -C4- CORROSION AROUND DRAIN HOLE ON FLAT BEAM UNDER MCD LAYSHAFT, APPROXIMATELY STA X27, Z98 STR 25P. REMOVED BEAM AND ATTACHING ANGLES, MID BEAMS IAW D-8 Q400 SRM 51-42-05 AND 51-40-15. INSTALLED FLAT BEAM, INSTALLED FWD AND AFT SUPP ORT FRAME IAW DHC-8 Q400 SRM 51-42-05 AND 51-40-15. 2 H 7 2 4T RT A13NM 2008033100012 20080331 00012 NM 2008 3 31 SWAA081653 1 20080326 A 5523 65C25798 HINGE BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED C2 CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE ASSY PER SWA EA. 2 L 7 2 4F RT A16WE 2008033100018 20080331 00018 WP 2008 3 31 08FDEA00982 1 20080317 A 5321 AGA38753 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 AFT PIT FLOOR PANEL NR 187 DF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL 187 DF; POTTED EDGES; COM PLETED CURE AND SANDED EDGE POTTING. INSTALLED INSERTS AND FABRICATED TOP SHEET. LAYED UP TOP SHEET UNDER THE VAC BAG; COMPLETED CURE; COUNTER SUNK HOLES AND APPLIED NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C. 2 L 7 3 4F RT A22WE 2008033100029 20080331 00029 NM 2008 3 31 SWAA081669 1 20080326 A 5311 65C25230 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008033100035 20080331 00035 NM 2008 3 31 SWAA081660 1 20080326 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 761RR 27875 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, LBL 5 TO RBL 40. REPAIRED CHORD PER SWA EA. 2 L 7 2 4F RT A16WE 2008033100036 20080331 00036 NM 2008 3 31 UPS08551938 1 20080326 A 3350 LIGHT BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 418UP 23905 INSPECTION TYPE:N/A EMERGENCY LIGHTS "UNARMED" ANNUC INOP. RELAMPED, OPS NORMAL. 2 L 7 2 4F RT A2NM 2008030500180 20080305 00180 NM 2008 3 5 UIEA200800067 1 20080229 A 5347 BAC15201566 SEAT TRACK BOEING 747 7472D7B 1384803 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 FOUND MAIN DECK CARGO SEAT TRACK AT BS 1920, LBL99 IS CRACKED. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 53-10- 05, FIG 1A, REFERENCE ATLAS AIR EO NR 4753B118. 2 L 7 4 4F RT A20WE 2008030600001 20080306 00001 NM 2008 3 6 08FDEA00473 1 20080218 A 5320 146N544419 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD STRINGER L2.90 STA 1540-1560, TO EVALUATE EXISTING REPAIR. EXISTING REPAI R FOUND NOT CARRIED OUT IAW B757 SRM 51-70-11 FIG 1 DETAIL I, II. STRINGER L2.90 FROM STA 1540-1560 REPLACED IAW B757-2 00 SRM 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008030600002 20080306 00002 NM 2008 3 6 08FDEA00668 1 20080229 A 5753 65727311 SKIN BOEING 727 727233 138408A NM ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 LT WING I/B AFT FLAP DENTED AND DELAMINATED AT WBL 124 CUT OUT DAMAGED AREA ON LT WING I/B AFT FLAP LWR SURFACE WBL 124 AND REMOVED DAMAGED CORE. FABRICATED DOUBLER AND CORE PLUG IAW SRM 57-50-2. BONDED CORE AND DOUBLER, AND PRIMED AND SE ALED IAW SRM 51-40-24. 2 L 7 3 4F RT A3WE 2008030600004 20080306 00004 CE 2008 3 6 020108A 1 20080215 A 3000 66083171 SENSOR LEAR 35 36LEAR 5170601 CE COCKPIT BURNED E ESPA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 71PG 635 635 013 ON THE CLIMB 4' CREW SMELL OF BURNING WIRES, AND SMOKE RISING FROM CAPTAIN BREAKER PANEL. CREW ELECTED TO COME BACK AND LAND AT ATL. THE EL LIGHT CIRCUIT CB WAS PULLED, & MEL DUE TO FAULTY CB. SEEMED TO FIX THE PROBLEM. DEPARTED AGAIN, ABOUT 10 MINUTES INTO THE FLIGHT CREW NOTICE THE SMELL, AND SMOKE COMING FROM THE CAPTAIN SIDE CB PANEL AREA. AIRCRAFT WAS DIVERTED TO HOME BASE VPC, AND LANDED UNEVENTFULLY. NO EMERGENCY WAS DECLARED ON EITHER INFLIGHT ABORTS. 2 L 7 2 4F A10CE 2008030600007 20080306 00007 NM 2008 3 6 08FDEA00691 1 20080304 A 2450 B1174 RCCB DOUG MD11 MD11F 3023600 NM FAILED A FDEA J A DUMP FUEL UNSCHED LANDING G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SO 25 620FE 48791 T/O ROLL NR 4 DU BLANKED, NR 1 FMS DISP "TIMEOUT RESELECT" NR 3 MCDU BLANKED, OCCURRED PRIOR TO V, CONTINUED T/O. AT 18 0 NM FROM HNL RECEIVED MANY LVL 1 AND LVL 2. ALERTS MOST SIGNIFICANT LVL 1 "BUS AC 1 OFF" AND LVL2 FUEL QTY FAULT", LVL 2 SELECT FADEC ALTN". AUX IRU WENT TO "BATT" AND FAILED 20 MINUTES LATER. NR 1 FMS WENT TO STBY. DUMPED 120K FUEL. RETURNED TO HNL. NR 1 AC BUS REPOWERED ITSELF PRIOR TO APPROACH AND ALL DU CONTINUED TO FLICKER OFF/ON DURING APPROACH. AVIONICS RACK FAN C/B POPPED AND CAC FAN C/B. REMOVED AND REPLACED SENSE RELAY R2-5071, NO JOY. REMOVED AND REPLACED NR 1 GCU. OPS CHECK GOOD. REMOVED AND REPLACED NR 1 APR AND RAN ENGINES. EPCU CURRENT FAULTS SENSE RELAY STILL THERE 2 L 7 3 4F RT A22WE 2008030600017 20080306 00017 EA 2008 3 6 MASA200800156 1 20080219 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A MASA O OTHER O OTHER AP APPROACH 1 SW 07 37208 7208 ASH FLT 7309 BNA - ORD, FLAPS FAIL AT 20 DEGREES DURING APPROACH. MX COMPLIED WITH PART A. 2 L 7 2 4F RT A21EA 2008030600066 20080306 00066 NM 2008 3 6 2008UALA00943 1 20080219 A 5330 DOUBLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 LEFT EXT SKIN DOUBLER AT BS 596 AND 598 HAS TWO SMALL DENTS BETWEEN STRINGER 15 AND 16. ACCOMPLISHED MAJOR REPAIR AT GS O. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030600070 20080306 00070 NM 2008 3 6 2008UALA00971 1 20080221 A 2622 FIRE BOTTLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CARGO BAY MALFUNCTIONED A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION IN INSP/MAINT 1 WP 29 912UA 25290 DURING 3SVC CHECK FOUND CARGO FIRE SYSTEM 1ST BOTTLE DISCHARGE LIGHT ON. REPLACED NR 1 CARGO FIRE BOTTLE PER MM 26-23-0 1 AND GROUND CHECKED OK. REPLACED DUCT ASSY AND LEAK CHECKED GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030600113 20080306 00113 NM 2008 3 6 2008UALA00929 1 20080218 A 2560 1158291 SIGN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 571UA 26681 RIGHT OVERWING EXITS EMERGENCY EXIT SIGN MISSING. LATCHING MECHANISM NOT WORKING PROPERLY CAUSING THE SIGN TO FALL OUT/ OFF. MADE AN INTERIM REPAIR AND INSTALLED A NEW EMERGENCY EXIT SIGN. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030600130 20080306 00130 NM 2008 3 6 2008UALA00979 1 20080221 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 DOOR DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 546UA 25367 DOOR 3L WILL NOT DISARM. GIRT BAR STUCK, DIRTY. CLEANED AND LUBED GIRT BAR ASSY. ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030600135 20080306 00135 NM 2008 3 6 2008UALA00983 1 20080220 A 5730 SD69771351 SEAL BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE WING ACESS PANEL LEAKING A UALA D RETURN TO BLOCK K FLUID LOSS NR NOT REPORTED 1 WP 29 779UA 26941 FUEL LEAK RT WING UNDERSIDE OUTBOARD OF RT ENGINE PYLON. SUSPECT SEAL ON FUEL TANK ACCESS PLATE. REPLACED SEAL. ACFT O K FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008030600184 20080306 00184 NM 2008 3 6 2008UALA00993 1 20080222 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 450 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 EXISTING REPAIR DOUBLER AT LOWER LOBE SKIN BL 0 BS 450 RADIO ALTIMETER ANTENNA CUTOUT REQUIRES EG DISPOSITION. MAJOR RE PAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED LARGE AREA DOUBLER FROM E&E TO THE RA ANTENNAE CUTOUTS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030600185 20080306 00185 NM 2008 3 6 2008UALA00994 1 20080222 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 360 S14L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 STRINGER 14L SHEAR TIE CRACKED AT BS 360. MAJOR REPAIR: FABRICATED AND INSTALLED NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030600188 20080306 00188 NM 2008 3 6 2008UALA01001 1 20080223 A 2910 HOSE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE HYD SYSTEM FAILED A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 788UA 26942 FLIGHT LANDED UNDER AMBER ALERT DUE TO A FAILED CENTER HYDRAULIC SYSTEM. NORMAL LANDING, BUT FLIGHT HAD TO BE TOWED TO GATE. FOUND FLEX HOSE TORN BY NOSE STEERING ACTUATOR. REPLACED HOSE. SERVICED HYD SYS. OP CHECKED OK. NO LEAK. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008030600191 20080306 00191 NM 2008 3 6 2008UALA01022 1 20080224 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 671UA 30026 FUSELAGE DAMAGE AT STA 650 STR 31L TO 35L HAS GOUGE APPROX .060 DEEP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030600193 20080306 00193 NM 2008 3 6 2008UALA01024 1 20080223 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT DOOR FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 641UA 25091 EMERGENCY EXIT LIGHT AT FLIGHT DECK DOOR IS ON WITH STANDBY SWITCH IN OFF POSITION. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030600196 20080306 00196 NM 2008 3 6 ZZDA2008071 1 20080225 A 2120 UNKNOWN BOEING 737 73776N 13844CH NM COCKPIT SMOKE A ZZDA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 37 174AT 32667 LEFT PACK SHUT DOWN ON ACPR AFTER NOTICING AC SMOKE IN COCKPIT RAN QRH. SMOKE WENT AWAY AFTER SHUTTING DOWN LEFT PACK. T/S IAW FIM 21-00-802, RAN L-PACK W/ APU & NR 1 ENG BLEED AIR, NO SMOKE OR FUMES NOTED. INSPECTED L-PACK SYST W/NO FOU NDS, SYS IS WORKING GOOD, INTERMITTENT FAULT IAW STEP D-5D, L-PACK BACK TO NORMAL CONFIG & OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2008030600197 20080306 00197 NM 2008 3 6 ZZDA2008072 1 20080208 A 5311 FRAME BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 982AT 55041 CRACK NOTICED AT AFT FUSELAGE INT LEFT CANTED BLKD STA 1178.225 L16L AFT OF HYD S/O VALVE. INSTALLED DOUBLE REPAIR AT A FT FUSELAGE INTERNAL LT CANTED BLKD STA 1178.225 L16L IAW B717 SRM 51-70-11 FIG 201 REPAIR 1, MEASURE 12" X 3". 2 L 7 2 4F TR A6WE 2008030600246 20080306 00246 NM 2008 3 6 CALS097003 1 20080124 A 5312 65B025394 FITTING BOEING 747 747409 13848AU NM BS 2598 CRACKED W SAJF K NONE O OTHER IN INSP/MAINT 1 WP 03 18201 28709 WHEN PERFORMING FAA AD 2006-05-06 ON AC B-18201, DSGN FOUND GRH SIDE AFTER SPLICE FITTING CRACKED APPROXIMATELY 1.25 INC H IN LENGTH. 2 L 7 4 4F RT A20WE 2008030600248 20080306 00248 2008 3 6 ASMF200802003 4 20080209 A 3416 6223890015 ALTIMETER DOUG DC9 DC983 3022083 WP PWA JT8 JT8D* NE COCKPIT FAILED W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 838AM 12246 12246 49397 AC RETURNED OF FLIGHT DUE TO GPWS FAULT AND TAWS AUDIBLE WARNINGS WERE ACTIVATED DURING CLIMB. THE GPWS WAS TESTED IAW M M 34-45-00, ALL CORRECT. AS A PRECAUTIONARY ACTION, THE RADIO ALTIMETER WAS REPLACED AND TESTED IAW MM 34-42-03 AND 34-4 3-20, ALL CORRECT. THE OVERWEIGHT INSPECTION WAS NOT NECESSARY DUE TO THE LANDING WEIGHT WAS 109,700 POUNDS AND THE MAXI MUM IS 139,500 POUNDS. 2 L 7 2 4F 4 F RT A6WE E2EA 2008030600256 20080306 00256 EA 2008 3 6 VNAA0802012 1 20080217 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE EXTERNAL POWER OPEN A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 05 719PS 10177 CREW REPORTED A LOUD SQUEAL AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSP ECTED AND FOUND THE EXTERNAL GROUND POWER DOOR OPEN. MAINTENANCE SECURED DOOR CLOSED AND FOUND NO DEFECTS OR DAMAGE. A IRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008030600260 20080306 00260 NM 2008 3 6 SWAA081063 1 20080226 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 204WN 29855 DURING SCHEDULED MV2 CHECK, FOUND EEPLS END CAP MISSING AT ROW 1 ABC. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 2008030600266 20080306 00266 NM 2008 3 6 SWAA081069 1 20080226 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 408WN 27895 EEPLS INOP AT ROW 2 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008030600268 20080306 00268 2008 3 6 SWAA081071 4 20080226 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 454WN 29851 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008030600269 20080306 00269 NM 2008 3 6 SWAA081072 1 20080226 A 2560 417A56014 SIGN BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 468WN 33858 RIGHT AFT CABIN EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2008030600276 20080306 00276 2008 3 6 SWAA081074 4 20080226 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 603SW 27954 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008030600283 20080306 00283 2008 3 6 Q2SA746003 4 20080212 A 2565 SLIDE BOEING 747 747206B 1384856 NM LEFT UNWANTED DEPLOY A Q2SA O OTHER O OTHER NR NOT REPORTED 1 EA 63 746SA 21111 INADVERTENTLY DEPLOYED LEFT UPPER DECK SLIDE WHILE AIRCRAFT WAS ON GROUND AT KMIA. REMOVED SLIDE IN ACCORDANCE WITH AMM 25-68-02. TRANSFERRED TO DI NR 14742 PER MEL 25-11. PLACARD INSTALLED. SLIDE DEPLOYED WITHOUT ANY PROBLEMS. 2 L 7 4 4F RT A20WE 2008030600286 20080306 00286 NM 2008 3 6 HALA0800196 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1401 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION RBL 54.75, SEAT TRACKS AT STA 1401, BASE OF TRACKS. CORROSION REMOVED PER SRM 51-10-02, REV 76 AND SR M 53-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030600288 20080306 00288 NM 2008 3 6 HALA0800197 1 20080215 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1436 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION RBL 54.75, SEAT TRACKS AT STA 1436, BASE OF TRACKS. CORROSION REMOVED PER SRM 51-10-02, REV 76 AND SR M 53-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030600289 20080306 00289 NM 2008 3 6 HALA0800173 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1288 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION SECTION 46, SEAT TRACKS AT RBL 88.5, STA 1288. REWORK IAW SRM 53-00-52/101 AND REPLACED SEAT TRACK IA W SRM WHERE DAMAGE WAS OUT OF LIMITS. 2 L 7 2 4F RT A1NM 2008030600290 20080306 00290 EA 2008 3 6 MASA200800163 1 20080223 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 931LR 15031 ASH FLT 2934 PHX-MEM, ROW 1 CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008030600294 20080306 00294 NM 2008 3 6 DLM90080234 1 20080216 A 5320 BRACKET DOUG MD90 MD9030 3023690 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 AFT CARGO BAY BRACKET AT LWR END OF CARGO DOOR AFT CUT-OUT CORRODED. REMOVED AND REPLACED AFT CARGO BAY BRACKET AFT LWR END OF CARGO DOOR CUT-OUT, IAW MD90 SRM 51-30-05. 2 L 7 2 4F RT A6WE 2008030600296 20080306 00296 NM 2008 3 6 DLM90080235 1 20080216 A 5320 BRACKET DOUG MD90 MD9030 3023690 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 AFT CARGO BAY BRACKET AT FWD END OF LWR BEAM (DOOR CUT OUT) CORRODED. REMOVED AND REPLACED BRACKET IN AFT CARGO BAY AT FWD END OF LWR BEAM, IAW MD90 SRM 51-30-05. 2 L 7 2 4F RT A6WE 2008030600298 20080306 00298 NM 2008 3 6 KNNA200700069 1 20080121 A 4900 380428114 APU BOEING 737 7372L9 1384497 NM UNKNOWN A KNNA H B F A DEACTIVATE SYST/CIRCUITS EMER. DESCENT ACTIVATE FIRE EXT. UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 WP 25 737Q 21279 THERE WAS AN APU FIRE INDICATION IN FLIGHT AFTER PILOTS FOLLOWED ABNORMAL CHECK LIST FOR CSD LOW OIL PRESSURE LIGHT ILLU MINATION. ACCORDING TO PILOT'S REPORT, THEY WERE AT FLIGHT LEVEL 34,000 FEET WHEN THEY ATTEMPTED TO START, AS PER CHECK LIST, THE APU WHEN THE APU FIRE WARNING BELL RANG AND LIGHT ILLUMINATED. THE PILOTS PERFORMED MEMORY ITEMS FROM APU FI RE CHECKLIST AND THEN FIRED APU FIRE BOTTLE. THE APU WAS REMOVED AND THOROUGHLY INSPECTED IAW MM 49-00-00 AND FOUND SEV ICEABLE THEN REINSTALLED. 2 L 7 2 4F RT A16WE 2008030600104 20080306 00104 NM 2008 3 6 SWAA081061 1 20080225 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008030600122 20080306 00122 EU 2008 3 6 2008UALA00960 1 20080221 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 457UA 1146 SEAT 16D EEL LIGHT IS BROKEN. REPLACED EEL LIGHT ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030600124 20080306 00124 EU 2008 3 6 2008UALA00972 1 20080221 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 438UA 678 STR 39R HAS CORROSION BETWEEN FR 65 AND 66. MAJOR REPAIR ACCOMPLISHED AT LCQ. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030600129 20080306 00129 NM 2008 3 6 2008UALA00978 1 20080222 A 2621 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE BOTTLE LOOSE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 564UA 26666 NR 2 CARGO FIRE BOTTLE DISCHARGE LIGHT INOP. INDICATOR LIGHT LOOSE. SECURED LIGHT ASSY, GROUND CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030600198 20080306 00198 NM 2008 3 6 ZZDA2008073 1 20080226 A 3020 32157341 SHUTOFF VALVE BOEING 717 717200 1383700 NM ANTI-ICE SYS INOPERATIVE A ZZDA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 SO 37 923AT 55051 ON APPROACH 'WING ANTI-ICE OFF' ALERT ILLUMINATED. ACCOMPLISHED CHECK LIST AFTER LANDING "WING HEAT FAIL" ALERT ILLUMIN ATED. REMOVED AND REPLACED PODS CONTROLLER AND WING ANTI-ICE PROSV, AND CONNECTOR LEAK CHECKED WING TEE AREA FOUND NO D EFECTIVE WIRING TIGHTEN FITTING ON RT A/I SENSE LINE REF: B 717 36-30-11, OPS CHECK GOOD. 2 L 7 2 4F TR A6WE 2008030600258 20080306 00258 EA 2008 3 6 VNAA0802003 1 20080205 A 3040 601R515187 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE COCKPIT FAULTY A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 05 221PS 9612 7889 CREW REPORTED THE CAPTAINS AND FIRST OFFICERS WIPER BLADES CAME ON DURING FLIGHT MULTIPLE TIMES. THE FIRST OFFICERS SID E CAME ON AND WOULD NOT SHUT OFF. CREW ELECTED TO RETURN TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND R EPLACED THE FIRST OFFICERS WIPER STALL CONTROL PANEL IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS R ELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008030600275 20080306 00275 NM 2008 3 6 SWAA081079 1 20080226 A 2560 6557463 FITTING BOEING 737 7375H4 138449D NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2008030600285 20080306 00285 EA 2008 3 6 MASA200800161 1 20080226 A 2910 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS INACTIVE A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 17156 7156 ASH FLT 7348 IAD-DTW, CREW REPORTED GETTING A GEAR DISAGREE WARNING MESSAGE IN FLIGHT AND DECLARED AN EMERGENCY. MX FO UND THE NR 3 HYDRAULIC SYSTEM PUMPS WERE NOT ALL ON. PERFORMED GEAR SWINGS AND OP CHECK WERE GOOD. 2 L 7 2 4F RT A21EA 2008030600304 20080306 00304 NM 2008 3 6 08FDEA00581 1 20080223 A 5311 651693220 FRAME BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 FWD CARGO COMPT CORROSION ON STA 580 TO SKIN, LBL 3" TO LBL 10". REPAIRED SHEAR TIE AT STA 580, LBL 3" TO 10". REF SRM 53-10-4 FIG 15. THIS IS CLASSIFID AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008030600307 20080306 00307 EU 2008 3 6 USAA920080464 1 20080210 A 5320 D53480043205 SILL AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON R2 DOOR CUTOUT LOWER SILL, BS 3207/FR 67, -Y1732. REPAIRED R2 DOOR CUTOUT LOWER SILL, BS 3207/FR 67, -Y1732 IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2008030600308 20080306 00308 EU 2008 3 6 USAA920080465 1 20080210 A 5320 D53480020437 SHEAR WEB AIRBUS 320 A320232 3930326 EU ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CRACKED SHEAR WEB/TRAY, BS 3257/FR 68 - BS 3310/FR 69, -Y1732. REPLACED SHEAR WEB/TRAY, BS 3257/FR 68 - BS 3310/FR 69, -Y1732 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008030600309 20080306 00309 EU 2008 3 6 USAA920080466 1 20080210 A 5347 D53472190203 SEAT TRACK AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN RAIL SEAT BEAM, BS 3043/FR 64 - BS 3158 FR 66, -Y765. REPLACED CABIN RAIL SEAT BEAM, BS 3043/FR 64 - BS 3158/FR 66, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008030600311 20080306 00311 EU 2008 3 6 USAA920080467 1 20080210 A 5320 D53480020436 SHEAR WEB AIRBUS 320 A320232 3930326 EU ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CRACKED SHEAR WEB TRAY, BS 3257/FR 68 - BS 3310/FR 69, +Y1732. REPLACED SHEAR WEB TRAY, BS 3257/FR 68 - BS 3310/FR 69, +Y1732 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008030600314 20080306 00314 NM 2008 3 6 USAA920080485 1 20080201 A 5754 ANGLE BOEING 767 7672B7ER 1385107 NM NR 7 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AY 26847 MIA - MAJOR REPAIR - C4 CHECK - RIGHT WING LEADING EDGE NR 7 SLAT LOWER FORWARD SUPPORT BRACKET ANGLES CRACKED, LES 227 - LES 321. REPLACED RIGHT WING LEADING EDGE NR 7 SLAT LOWER FORWARD SUPPORT BRACKET ANGLES, LES 227 - LES 32 IAW BOEING DRAWING 114T3100 AND B767 SRM 51-10-02. 2 L 7 2 4F RT A1NM 2008030600316 20080306 00316 NM 2008 3 6 ABXA080061 1 20080128 A 5230 140T26033 BEAM BOEING 767 767281 1385109 NM AFT CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 796AX 23146 I-BEAM DIRECTLY BELOW DEPRESSURIZATION VENTS ON AFT LOWER CARGO DOOR HEAVILY CORRODED. REMOVED AND REPLACED BEAM IAW B7 67 SRM 51-40-2. 2 L 7 2 4F RT A1NM 2008030600317 20080306 00317 NM 2008 3 6 USAA920080487 1 20080209 A 5315 FLOORBEAM BOEING 767 7672B7ER 1385107 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AY 26847 MIA - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOORBEAM, BS 847 - BS 899, LBL 56. REPAIRED CABIN FLOORBEAM , BS 847 - BS 899, LBL 56 IAW B767 SRM 53-00-51 REPAIR 3. 2 L 7 2 4F RT A1NM 2008030600323 20080306 00323 NM 2008 3 6 ABXA080062 1 20080129 A 5230 140T2603Y3 DOOR FRAME BOEING 767 767281 1385109 NM FWD CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 796AX 23146 FORWARD LOWER CARGO DOOR FRAME UNDER VENT DOORS CORRODED IN SEVERAL PLACES. REMOVED AND REPLACED FORWARD LOWER CARGO DO OR FRAME IAW B767 SRM. 2 L 7 2 4F RT A1NM 2008030600324 20080306 00324 NM 2008 3 6 USAA920080502 1 20080221 A 5340 692655 ATTACH FITTING BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 23934 CLT - MAJOR REPAIR - C1 CHECK - CRACKED FORWARD ENTRY DOOR CUT OUT INTERCOSTAL UPPER AND LOWER ATTACH CLIPS, BS 348.20. REPLACED FORWARD ENTRY DOOR CUT OUT INTERCOSTAL UPPER AND LOWER ATTACH CLIP, BS 348.20 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008030600329 20080306 00329 WP 2008 3 6 ABXA080060 1 20080206 A 5310 99115057 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DURING WINDOW FRAME MOD TO COCKPIT STRUCTURE, FOUND CENTER FRAME WITH MULTIPLE CRACKS. REPLACED CENTER FRAME SEGMENT IA W DC9 SRM 51-30-2 PER WO 600283624. 2 L 7 2 4F A6WE 2008030700007 20080307 00007 NM 2008 3 7 USAA920080507 1 20080222 A 5340 6916970 STRINGER CLIP BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 23934 CLT - MAJOR REPAIR - C1 CHECK - CRACKED STRINGER TIE CLIP, BS 348, S15R. REPLACED STRINGER TIE CLIP, BS 348, S15R IAW B 737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008030700013 20080307 00013 NM 2008 3 7 BB08022 1 20080224 A 3350 20121 CHARGER BOEING 767 7672B7 1385107 NM EMERGENCY LIGHTS FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 251AY 24764 BRU - DURING DAILY CHECK, FOUND GROUP OF FLOOR EMERGENCY LIGHTS ON RIGHT SIDE WALK WAY INOP. MAINTENANCE REPLACED BATTE RY CHARGER. 2 L 7 2 4F RT A1NM 2008030700015 20080307 00015 NM 2008 3 7 BB08023 1 20080224 A 2840 INDICATOR BOEING 757 7572G7 1384963 NM FUEL QTY ERRATIC A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 910AW 24523 PHX FLT NR 22 PHX - HNL WHILE IN CRUISE FLIGHT, THE CENTER TANK FUEL QTY READINGS BECAME ERRATIC. FLIGHT RETURNED TO PH X WITHOUT FURTHER INCIDENT. 2 L 7 2 4F RT A2NM 2008030700016 20080307 00016 NM 2008 3 7 BB08024 1 20080225 A 2782 5006397R ROTARY ACTUATOR BOEING 757 7572G7 1384963 NM LE FLAPS BINDING A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 908AW 21362 21362 24233 PHX FLT NR 144 KOA-PHX, DURING APPROACH, AFTER SELECTING FLAP LEVER TO 1, CREW RECEIVED EICAS MESSAGE "LE SLAT DISAGREE" FLAPS INDICATED BETWEEN 0 AND 1. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACE D LEADING EDGE SLAT ROTARY ACTUATOR. OPS CHECKED OK. 2 L 7 2 4F RT A2NM 2008030700018 20080307 00018 2008 3 7 SA08006 4 20080225 A 2565 BOTTLE AIRBUS A319 A319132 3930340 NM ESCAPE SLIDE READS LOW A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 825AW 21923 3948 1527 PHX - THE L2 DOOR ESCAPE SLIDE BOTTLE PRESSURE WAS NOT IN THE GREEN. MAINTENANCE REPLACED THE L2 DOOR ESCAPE SLIDE. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2008030700019 20080307 00019 NE 2008 3 7 2008UALA00951 2 20080220 A 7310 FUEL BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 773UA 26929 FUEL LEAK DETECTED FROM DRAIN MAST BETWEEN MLG DOORS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008030700023 20080307 00023 CE 2008 3 7 35741 1 20080220 A 2612 302158 FIRE DETECTOR BEECH 200 B200 1152922 CE PWC PT6 PT6A42A 52043 NE RT ENGINE FALSE ACTIVATION E GSPA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 05 32WC BB1285 PCE94076 DEPARTING TUCSON, DURING CLIMBOUT, NW BOUND, COPILOT ANNOUNCED "MASTER WARN - RT ENG FIRE". NO OBVIOUS INDICATION OF A FIRE. REQUESTED A CHANGE OF COURSE DUE TO THE FIRE DETECTION SYS DESIGN - PHOTO-SENSITIVE. AFTER FLYING THE NEW HEADIN G FOR APPROX 3 MIN, THE ANNUNCIATORS REMAINED ON, DIVERT TO TUCSON, TO HAVE A MECHANIC INVESTIGATE. DECLARED AN EMERGEN CY, LIGHT HAD BEEN ON FOR 3 MINUTES, AND FLYING A NEW HEADING. DURING THE DESCENT AND VECTOR TO 29R, THE R ENG FIRE LIG HT FLICKERED, THEN EXTINGUISHED, APPROX 5 MIN PRIOR TO LANDING. AN UNEVENTFUL LANDING WAS MADE. TECHNICIAN WAS DISPATC H TO LOCATION TO INVESTIGATE. THE ‘ENGINE FIRE` INDICATION WAS A FAULTY INDICATION AND THE AC WAS CLEARED AND RETURNED 1 L 7 2 4T 4 T A24CE E4EA 2008030700026 20080307 00026 NM 2008 3 7 BB08025 1 20080226 A 3350 BPS73 BATTERY PACK BOEING 757 7572B7 1384964 NM EMERGENCY LIGHTS FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 929UW 27144 TPA - MAINTENANCE FOUND AFT LEFT EMERGENCY BATTERY CHARGER INOP. MAINTENANCE REPLACED AFT LEFT EMERGENCY LIGHT BATTERY PACK. OPS CHECKS OK. 2 L 7 2 4F RT A2NM 2008030700030 20080307 00030 2008 3 7 2008UALA01009 4 20080222 A 2565 INSERT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 RIGHT OVERWING SLIDE INFLATION HOSE CLAMP INSERT PULLED OUT. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030700037 20080307 00037 NM 2008 3 7 ASAA0842661 1 20080127 A 5753 6546435237SP SKIN BOEING 737 7374Q8 138447Q NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 LEFT WING O/B AFT FLAP LOWER SURFACE HAS MULTIPLE DENTS AT MID SECTION. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLE R AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008030700039 20080307 00039 NM 2008 3 7 ASAA0842663 1 20080127 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 1 SPOILER DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 LEFT WING NR 1 SPOILER LOWER SURFACE HAS SHARP DENT 12" FRM I/B AND 4" FRM L/E. PREPARED DAMAGED AREA, FABRICATED REPAI R DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 PGS 212 214 223 241 AND 254 257 REPAIR 2. 2 L 7 2 4F RT A16WE 2008030700042 20080307 00042 NM 2008 3 7 ASAA0842666 1 20080127 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 3 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 LEFT WING NR 3 SPOILER UPPER SUFACE HAS AN AREA OF 3 EA DENTS. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BON DED IAW B737 400 SRM 51 70 10 PGS 212 214 223 241 AND 254 257 REPAIR 2. 2 L 7 2 4F RT A16WE 2008030700043 20080307 00043 NM 2008 3 7 ASAA0842667 1 20080127 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 9 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 RIGHT WING NR 9 SPOILER HAS AREA OF DELAMINATION ON UPPER I/B SURFACE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 PGS 212 276 241 AND PG 255 PAR B. 2 L 7 2 4F RT A16WE 2008030700044 20080307 00044 NM 2008 3 7 ASAA0842668 1 20080127 A 5755 654645268A SKIN BOEING 737 7374Q8 138447Q NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 RIGHT WING NR 5 SPOILER LOWER SURFACE HAS MULTIPLE DENTS ON I/B EDGE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 PGS 212 214 223 241 AND 254 257 REPAIR 2. 2 L 7 2 4F RT A16WE 2008030700049 20080307 00049 NM 2008 3 7 BB08026 1 20080227 A 3260 841602 PROXIMITY SWITCH BOEING 757 7572S7 1384962 NM MLG FAILED A USAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 19 902AW 25335 2204 23322 PHX FLL-PHX FLT NR 181 AT FL320, CREW RECEIVED RED FLAPS AND 3 GREEN GEAR DOWN LANDING LIGHTS ALONG WITH OTHER CAUTIONS. THE CREW PUT THE LANDING LEVER FROM THE NORMAL POSITION TO THE UP POSITION AND LIGHTS AND TAKEOFF CONFIG HORN WENT OUT . FLIGHT CONTINUED TO PHX WITH MACH/SPEED TRIM, AIR/GROUND DISAGREE WARNING, WARNING ELECTRIC LANDING GEAR MONITOR, AND NOSE AIR/GROUND DISAGREE. CREW DECLARED AN EMERGENCY AND REQUESTED CFR. ON ARRIVAL, LANDING GEAR EXTENDED PROPERLY WI TH NORMAL INDICATIONS, LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED PROX SWITCH ELECTRONICS UNIT. OPS CHECKED OK. 2 L 7 2 4F RT A2NM 2008030700056 20080307 00056 NM 2008 3 7 ASAA0842678 1 20080127 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 2 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 LEFT WING NR 2 SPOILER UPPER SURFACE HAS AREA OF MULTIPLE DENTS. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLERS AND BONDED IAW B737 400 SRM 51 70 10 PGS 212 214 223 241 AND 254 257 REPAIR 2 (5 EA. REPAIR DOUBLERS). 2 L 7 2 4F RT A16WE 2008030700062 20080307 00062 EA 2008 3 7 COMA0860143 1 20080221 A 2130 VALVE CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 7017 FLIGHT 5158 - AFTER TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE. RECEIVED OTBD COOL CAUTION AND INBD COOL FAIL MESSAGES. DEC LARED EMERGENCY, RETURNED TO BOS, LANDED WITHOUT INCIDENT. FOUND O/B COOL VALVE OPEN. PERFORMED MEL PROCEDURES TO ENSU RE VALVE RESET TO CORRECT POSITION. REMOVED CONNECTORS. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008030700065 20080307 00065 NM 2008 3 7 KNNA20080001 1 20080121 A 4900 380428114 APU BOEING 737 7372L9 1384497 NM MALFUNCTIONED A KNNA H B A F DEACTIVATE SYST/CIRCUITS EMER. DESCENT UNSCHED LANDING ACTIVATE FIRE EXT. H N ELECT. POWER LOSS-50 PC FALSE WARNING CR CRUISE 1 WP 25 737Q 21279 THERE WAS AN APU FIRE INDICATION IN FLIGHT AFTER PILOTS FOLLOWED ABNORMAL CHECK LIST FOR CSD LOW OIL PRESSURE LIGHT ILLU MINATION. ACCORDING TO PILOT'S REPORT, THEY WERE AT FLIGHT LEVEL 34,000 FEET WHEN THEY ATTEMPTED TO START, AS PER CHECK LIST, THE APU WHEN THE APU FIRE WARNING BELL RANG AND LIGHT ILLUMINATED. THE PILOTS PERFORMED MEMORY ITEMS FROM APU FI RE CHECKLIST AND THEN FIRED APU FIRE BOTTLE. AT MERCED, THE APU WAS REMOVED AND THOROUGHLY INSPECTED IAW MM 49-00-00 AN D FOUND SERVICEABLE THEN REINSTALLED. 2 L 7 2 4F RT A16WE 2008030700068 20080307 00068 NM 2008 3 7 USAA920080428 1 20080212 A 5210 507945264 FRAME BOEING 737 7374B7 1384702 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - C3 CHECK - FORWARD PASSENGER DOOR INNER FRAME CRACKED AT NR 7 DOOR STOP. REPAIRED THE FORWARD PASS ENGER DOOR INNER FRAME AT NR 7 DOOR STOP IAW USAIRWAYS EA 100186. CORRECTED DISCREPANCY AND CORRECTIVE ACTION TO REFLEC T ONLY THE DOOR FRAME. THE DOOR SKIN WAS REPORTED USAA920080512. 2 L 7 2 4F RT A16WE 2008030700072 20080307 00072 EA 2008 3 7 TRAX200800313 1 20080224 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA NR 3 FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 867AS 7463 NR 3 FLAP FAIL, EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2008030700073 20080307 00073 EA 2008 3 7 TRAX200800314 1 20080213 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 889AS 7538 CREW ESCAPE HATCH EXTERIOR PLACARDS WORN AND MISSING. 2 L 7 2 4F RT A21EA 2008030700074 20080307 00074 EA 2008 3 7 COMA0860146 1 20080225 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 811CA 7380 FLIGHT 5382 - RECEIVED FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH SI-2- 27I0001 FLAP CAUTION MESSAGE FIRST EVENT MAINTENANCE ACTION. FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. 2 L 7 2 4F RT A21EA 2008030700086 20080307 00086 NM 2008 3 7 HALA0800361 1 20080226 A 5711 SPAR BOEING 767 7673G5 1385126 NM LWS 1070 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION AROUND FASTENER AT LT WING STA 1070, ON TOP SURFACE, ON FRONT SPAR. REPAIRED PER SRM 57-20-01. 2 L 7 2 4F RT A1NM 2008030700087 20080307 00087 NM 2008 3 7 HALA0800359 1 20080128 A 5711 SPAR BOEING 767 7673G5 1385126 NM LWS 775 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION AROUND FASTENER AT LT WING STA 775, ON TOP SURFACE ON FRONT SPAR. REPAIRED PER SRM 57-20-01. 2 L 7 2 4F RT A1NM 2008030700088 20080307 00088 NM 2008 3 7 HALA0800358 1 20080228 A 5711 SPAR BOEING 767 7673G5 1385126 NM LWS 860 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ARROUND FASTENER AT LT WING STA 860, ON TOP SURFACE, 6 INCHES AFT OF FRONT SPAR. REPAIRED PER SRM 57- 20-01. 2 L 7 2 4F RT A1NM 2008030700093 20080307 00093 NM 2008 3 7 NWAA080716304 1 20080227 A 2530 OVEN BOEING 747 747451 1384940 NM GALLEY FIRE A NWAA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 664US 23819 FLIGHT ATTENDANT REPORTED A SMALL PIECE OF TAPE WAS STUCK IN THE OVEN AT DOOR 4 OVEN BELOW UNIT 3-57, AND HALON BOTTLE A T 4L WAS USED, BECAUSE OF A SMALL FIRE DID ERUPT. MAINTENANCE CONFIRMED SOURCE OF SMOKE WAS CATERING TAG/TAPE. REMOVED AND REPLACED OVEN, OVEN CONTROLLER, AND HALON FIRE BOTTLE. OPERATIONAL CHECKED GOOD, AND AIRCRAFT WAS RETURNED TO SERV ICE. 2 L 7 4 4F RT A20WE 2008030700094 20080307 00094 WP 2008 3 7 UPS08851719 1 20080225 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT CHECK FAILED. REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD PER MM 33 -50-01-2. 2 L 7 4 4F RT 4A25 2008030700095 20080307 00095 WP 2008 3 7 NWAA080689756 1 20080227 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 756NW 47180 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAI LED. THE BATTERY PACK AT THE FORWARD CABIN RIGHT DOOR WAS REPLACED. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RE TURNED TO SERVICE. 2 L 7 2 4F A6WE 2008030700097 20080307 00097 NM 2008 3 7 UPS08M51710 1 20080212 A 5720 SUPPORT ANGLE DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:1C RIGHT L/E ACCESS PNL MATING SURFACE AFT OF NR 9 SLAT TRACK CRACKED. REMOVED CRACKED SUPPORT ANGLE, F ABRICATED AND INSTALLED REPLACEMENT SUPPORT ANGLE IAW MD-11 SRM 51-10-00, 51-21-01, 51-35-01 AND DPS 1.05-3. 2 L 7 3 4F RT A22WE 2008030700098 20080307 00098 NM 2008 3 7 UPS08M51711 1 20080212 A 5754 DOUBLER DOUG MD11 MD11F 3023600 NM L/E SLAT CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:1C RIGHT WING L/E NR 1 SLAT TRACK CUTOUT HAS DOUBLER CHAFED. REMOVED REPAIR DOUBLER, FABRICATED AND INS TALLED REPLACEMENT REPAIR DOUBLER IAW MD-11 SRM 57-10-00, 51-21-01, 51-33-01 AND 51-35-01. 2 L 7 3 4F RT A22WE 2008030700102 20080307 00102 NM 2008 3 7 UPS08M51720 1 20080110 A 5720 DOUBLER DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:C LEFT WING FIXED L/E COMPT AT STA XORS 558 APPROX FOUND UPPER DOUBLER CRACK AS MARKED. I/B & O/B RIB A T LEFT WING FIXED L/E COMPT AT XORS 558 AREA REMOVED FOR ACCESS AS PER SRM 51-31-01 V.II R35. FASTENERS AT CRACKED AREA AT LEFT WING L/E FIXED COMPT STA XORS 558 UPPER DOUBLER AREA REMOVED PER SRM 51-35-01 V.II. R35 & CRACKED AREA TRIM OUT . REPAIR DOUBLER 01EA, REPAIR FILLER 01EA FAB AND INSTALLED PER SRM 57-10-00 FIG 27 VOL I REV 40. 2 L 7 3 4F RT A22WE 2008030700107 20080307 00107 SO 2008 3 7 FDKA200802076 1 20080221 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO CARGO BAY MALFUNCTIONED A FDKA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 825MJ 17418 145179 FDM 6185 MCO-PNS (1545 PHX LCL) EN ROUTE TO PNS AIRCRAFT DIVERTED TO TLH DUE TO BAG SMOKE WARNING IN EICAS IN FLIGHT. M X REMOVED AND REPLACED SMOKE DETECTOR, SMOKE DETECTOR RELAY, AND FAN RELAY. 2 L 7 2 4T RT T00011AT 2008030700109 20080307 00109 SO 2008 3 7 BSYR20080002 1 20080115 A 2421 ALU8521RS ALTERNATOR PIPER PA31 PA31350 7103110 SO ENGINE FAILED E BSYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 35871 318052123 AFTER TAKEOFF OUT OF LCK THE RIGHT ALTERNATOR CIRCUIT BREAKER POPPED. AIRCRAFT RETURNED TO LCK WHERE MAINTENANCE CHANGE D ALTERNATOR, OPS CHECKS GOOD. 1 L 7 2 3O A20SO 2008030700111 20080307 00111 SO 2008 3 7 BSYA20080004 2 20080124 A 7322 653377A2 SERVO BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO RT ENGINE DEFECTIVE E BSYA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 GL 07 62500 TH1347 830956R BEFORE TAKEOFF OUT OF HFD THE RIGHT ENGINE WOULD NOT RUN AT LOW POWER WITHOUT THE BOOST PUMP BEING ON. MAINTENANCE CHAN GED ENGINE DRIVEN FUEL PUMP, FLOW DIVIDER, FUEL SERVO, OPS CHECKS GOOD. FLOW DIVIDER P/N 631427-24A3. 1 L 7 2 3O 3 O 3A16 E5CE 2008030700112 20080307 00112 SO 2008 3 7 C2XA08IA063 1 20080222 A 3297 14550707403 WIRE HARNESS EMB 145 EMB145XR 3260214 SO NLG DEFECTIVE A C2XA O OTHER O OTHER AP APPROACH 1 SW 27 13123 145688 IAH - FLIGHT 2945. THE CREW REPORTED A DISTINCT THUMPING SOUND ON APPROACH WITH THE GEAR UP AND DOWN ON FINAL. THE AIRC RAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NLG DOWNLOCK HARNESS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008030700113 20080307 00113 SO 2008 3 7 C2XA08IA065 1 20080225 A 2611 SMOKE WARNING EMB 145 EMB145LR 3260212 SO CARGO BAY FALSE ACTIVATION A C2XA O OTHER N FALSE WARNING AP APPROACH 1 SW 27 16976 145171 IAH - ON SHORT FINAL THE CREW REPORTED A BAG SMOKE WARNING WHEN THE APU SWITCH WAS TURNED TO THE ON POSITION AND EXTG BA GS LIGHT AS WELL WITHOUT DISCHARGING THE FIRE BOTTLES. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE IN SPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE APU, BAGGAGE FIRE DETECTION SYSTEM, ALL WITH NO DEFECTS NOTED, AND THE A IRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008030700115 20080307 00115 NM 2008 3 7 2008UALA00045 1 20080102 A 3350 8100833801 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 780UA 26944 EEL LIGHTS AT SEATS 12D AND 15D ARE BROKEN. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008030700119 20080307 00119 NM 2008 3 7 2008UALA00847 1 20080214 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 119UA 28812 SEAT 35C HAS EXIT LIGHT OFF OF SIDE OF SEAT. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700130 20080307 00130 NM 2008 3 7 2008UALA00904 1 20080216 A 7920 FILTER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT ENGINE CLOGGED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 670UA 29240 EICAS 'L ENG OIL FILTER` MESSAGE DISPLAYED AFTER ENGINE START, MESSAGE REMAINED WITH OIL TEMP READING 92 DEGREES. REPLA CED THE MAIN OIL FILTER. MOTORED ENGINE WITH NO LEAKS. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030700132 20080307 00132 NM 2008 3 7 2008UALA00909 1 20080217 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHT INOP: CEILING ROW 7R. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030600114 20080306 00114 NM 2008 3 6 2008UALA00939 1 20080219 A 5210 DOOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 OUT OF ADJUST A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 511UA 24799 DOOR 3R HAS ARMING PROBLEMS. DOOR OUT OF ADJUSTMENT. ADJUSTED DOOR. ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030600192 20080306 00192 NM 2008 3 6 2008UALA01023 1 20080225 A 5330 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE BS 667 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 A DENT WAS FOUND ON FUSELAGE SKIN AT STA 667, BETWEEN STR 26L AND 27L. DENT IS 4" X 5". CUT OUT DENT AND ACP HEFC INSP FOR DAMAGE FREE. ACP OPEN HOLE HFEC INSP FOR FASTENER HOLES. INSTALLED DOUBLER REPAIR. THE REPAIR IS CAT B REQUIRES FU TURE REINSPECTION AFTER NEXT 30000 FLT CYL. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032700084 20080327 00084 EU 2008 3 27 08FDEA01068 1 20080319 A 3233 C23131102 ACTUATOR AIRBUS 310 A310222 3930315 EU NLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 455FE 7599 7599 331 AFTER TAKEOFF HAD NOSE LDG GEAR DOOR NOT CLOSED ANNUNCIATION ON ECAM. BOTH FWD LDG GEAR INDICATOR AND OVERHEAD INDICATO R SHOWED AMBER NOSE DOOR ANNUNCIATION, BOTH SYSTEM 1 AND 2. R AND I LT NLG DOOR ACTUATOR PER MM 32-31-16-4 AND DOOR OP S CHK PER MM 32-31-00 AND LEAK CHK OK. A/C OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2008032700087 20080327 00087 WP 2008 3 27 08FDEA01082 1 20080320 A 5321 ACA3205505 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP BS 630 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 MAIN CABIN FLOOR PANEL AT STA 630; LBL 95 IS PUNCTURED. REMOVED LEFT OVER DAMAGED MATERIAL; CLEANED THE AREA AND FILLED IAW FEDEX SRZ 25-005 REV F. 2 L 7 3 4F RT A22WE 2008032700090 20080327 00090 WP 2008 3 27 08FDEA01085 1 20080320 A 5321 ACA3205505 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 200 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 MAIN CABIN FLOORBOARD AT LBL 76 TO 108; BS 506 TO 590; PREVIOUS REPAIR AT THE FWD END IS DISBONDED. REPAIRED MAIN CABIN FLOORBOARD WITH FILLER AT LBL 76 TO 108; BS 506 TO 590 AS REQUIRED IAW FEDEX DC/MD-10 DWG SRZ 25-005; REV F. REPAIRED THE DELAMINATION OF THE FWD END PREVIOUS REPAIR IAW FEDEX DC/MD-10 SRM 51-62-01. 2 L 7 3 4F RT A22WE 2008032700093 20080327 00093 EA 2008 3 27 MASA200800239 1 20080318 A 5220 SJ3518 HOOK AND LOOP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT MISSING A MASA O OTHER O OTHER CR CRUISE 1 SW 07 930LR 15030 ASH 2831 SNA-PHX, CAPTAIN REPORTED AFTER LANDING THE LT AFT OVERWING EMERGENCY EXIT HATCH HANDLE COVER VELCRO AS MISSING AND THE HATCH WHISTLED IN FLIGHT. MX REPLACED THE VELCRO AND CLEANED THE HATCH SEAL. 2 L 7 2 4F RT A21EA 2008032700099 20080327 00099 NM 2008 3 27 QXEA200800299 1 20080320 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX -C4 - CORROSION ABOVE STR-25L FWD OF FRAME STA-X240.5 ON SKIN DOUBLER. REMOVED RIVET FROM SKIN IN AREA OF CORROSION AND BLENDED AREA OF DAMAGE TO REMOVE CORROSION IAW CPM CHAP 4, FOUND AREA OF BLEND TO BE WITHIN LIMITS IAW SRM 51-20-11 WITH .005" REMOVED FROM ORIGINAL .050". HFEC IAW NDTM PART 6, 51-00-01, NO CRACKS NOTED. RE-INSTALLED RIVET IAW SRM 5 1-40-11 AND RE ALODINED AND PRIMED BARE AREA IAW SRM 51-20-36. 2 H 7 2 4T RT A13NM 2008032700101 20080327 00101 NM 2008 3 27 QXEA200800301 1 20080313 A 5340 ATTACH ANGLE BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - C4 - THE ANGLE ATTACHED TO FRAME X6.00 AT STR 25S/L IS CORRODED (BELOW DOOR SILL). DRILLED OUT RIVETS SECURING FW D SCUPPER AND REMOVED SCUPPER. DRILLED OUT RIVETS SECURING ANGLE TO AIRFRAME AND REMOVED ANGLE REF SRM 53-20-23 FIG 1, SHEET 3, ITEM 34. FABRICATED NEW ATTACH ANGLE, ALODINED, PRIMED, PAINTED AND INSTALLED WITH RIVETS PER SRM 51-42-05. I NSTALLED REMAINING LOCK FASTENER, REF Q-400 SRM 51-40-15. 2 H 7 2 4T RT A13NM 2008032700104 20080327 00104 SO 2008 3 27 SIMA200808105 1 20080318 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 683AE 9364 5000 14500833 DURING A IMBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 29 WAS FOUND CORRODED. REPAIRED CORRODED AREA, REPAIR IAW SRM 53 -00-10 FIG 202. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032700105 20080327 00105 SO 2008 3 27 SIMA200808110 1 20080314 A 5320 14521413605 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 19976 5000 145130 DURING MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 23 WAS FOUND CORRODED. REWORKED AREA IAW SRM 53-21-10, FIG 206. AI RCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032700115 20080327 00115 SO 2008 3 27 SIMA200808103 1 20080319 A 5330 14564090001 SKIN EMB 145 EMB145LR 3260212 SO ZONE 100 DEFORMED A SIMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 21 672AE 9755 145794 ON FLIGHT 4177 - DURING PUSHBACK CREW PUSHED AIRCRAFT BACK OVER BAGGAGE CART DAMAGING AIRCRAFT SKIN AT FRAMES 74-75 AND BETWEEN STRINGERS 19R-19L. AIRCRAFT REMOVED FROM SERVICE. REPAIRED BY REMOVING AND REPLACING DAMAGED MATERIALS, SKIN, FRAMES, STRINGERS IN THE EFFECTIVE AREA IAW EO NR EM53MR-1033R1 AND EMB SRM 53-00-03. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032700122 20080327 00122 SO 2008 3 27 CHQA200800053 1 20080317 A 2760 14533022407 CONTROL UNIT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL SPOILERS MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 567RP 114 114 145698 CAE312049 CVG TO GSP - DURING CLIMB-OUT, THE CREW RECEIVED AN AMBER EICAS SPOILER FAIL MESSAGE. THE APPROPRIATE CHECKLISTS WERE F OLLOWED IN THE QRH AND THE AIRCRAFT RETURNED TO CVG WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAULT TO THE SPOILER ELECTRONIC CONTROL UNIT, AND AFTER REPLACING IT, THE SPOILER SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008032700125 20080327 00125 EA 2008 3 27 MASA200800237 1 20080317 A 2121 GG670950227 FAN CNDAIR CL600 CL6002C10 1390015 EA CABIN MALFUNCTIONED A MASA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 07 503MJ 11356 10058 ASH FLT 7387 CHS-ORD, RECIRCULATION FAN FAULT STATUS MESSAGE AND LAST ROW ELECTRICAL SMELL. REPLACED RECIRCULATION FAN. 2 L 7 2 4F RT A21EA 2008032700126 20080327 00126 EA 2008 3 27 MASA200800246 1 20080320 A 3510 80343622 DOOR CNDAIR CL600 CL6002B19 1900309 EA MASK BOX BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17231 7231 ASH FLT 2737 PHX-PSP, F/O'S O2 MASK DOOR BROKEN. MX REPLACED THE MASK BOX ASSEMBLY. 2 L 7 2 4F RT A21EA 2008032700128 20080327 00128 EU 2008 3 27 F3LA200800130 1 20080319 A 2120 UNKNOWN AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE COCKPIT/CABIN SMOKE A F3LA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 NM 03 808FR 3038 DURING LANDING ROLL OUT, THE FLIGHT CREW REPORTED WHITE/GRAY SMOKE AND ACRID ODOR IN THE COCKPIT AND PASSENGER CABIN. M AINTENANCE PERFORMED IDLE LEAK CHECK OF BOTH ENGINES IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 71-00-00-710-006 AND PER FORMED A CHECK OF THE PACK SYSTEM OPERATION IAW AMM 21-26-00-710-001-01. A FOD INSPECTION WAS CONDUCTED OF BOTH ENGINES IAW MP 72400-01. ALL SYSTEMS CHECK NORMAL AND THE ACFT RETURNED TO SERVICE. ENGINEERING NOTED THIS SITUATION HAS OCC URRED IN THE PAST AND HAS BEEN LINKED TO DE-ICING FLUID ON THE RUNWAY BEING INGESTED INTO THE AIR HANDLING SYSTEM ON LAN DING. 2 L 7 2 4F 4 F RT 2008032700130 20080327 00130 NM 2008 3 27 XXUA200800004 1 20080319 A 3350 20121 POWER SUPPLY BOEING 757 7572Q8 1384972 NM PWA PW2037 PW2037M 52117 NE EMERGENCY LIGHTS INOPERATIVE A XXUA K NONE L NO TEST IN INSP/MAINT 1 EA 15 406JS 29443 EMERGENCY LIGHT AT 11F (BULLNOSE) IS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY OPS CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032700132 20080327 00132 NM 2008 3 27 XXUA200800005 1 20080319 A 2560 TARGET BOEING 757 7572Q8 1384972 NM PWA PW2037 PW2037M 52117 NE GIRT BAR SENSOR DIRTY A XXUA K NONE L NO TEST IN INSP/MAINT 1 EA 15 401JS 26332 R-2 DOOR SLIDE LIGHT INDICATION OF DOOR INOP. CLEANED GIRT BAR TARGETS REF MM 25-66-00. OPERATION OF PAX DOOR ESCAPE S YSTEM NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030600247 20080306 00247 WP 2008 3 6 ASMF200802002 1 20080208 A 3220 39567851 LINK DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE NLG LOOSE W ASMF C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SW 23 754RA 49641 AC RETURNED TO DEPARTURE DURING TAKEOFF, NOISE AND VIBRATION IN THE NOSE LANDING GEAR WERE DETECTED AND CONTINUED WITH F LAPS AT 40 DEGREES. ABNORMAL PROCEDURE SECTION 5-10 WAS PERFORMED. AT PLATFORM, MAINT DETECTED THE NOSE LANDING GEAR D OOR OPEN AND UNLOCKED, AC WAS SENT TO THE HANGAR AND A LINK WAS DETECTED LOOSE. THE LINK WAS REPLACED IAW MM 32-22-01, T ESTED CORRECT. THE OVERWEIGHT INSP WAS NOT NECESSARY DUE TO THE LANDING WEIGHT WAS 110,500 POUNDS AND THE MAXIMUM IS 128 ,000 POUNDS. 2 L 7 2 4F 4 F RT A6WE E9NE 2008030600250 20080306 00250 EA 2008 3 6 TRAX200800194 1 20080204 A 5534 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 VERTICAL STAB TO FUSELAGE LT DRAG ANGLE CRACKED. REPAIRED LT DRAG ANGLE IAW REO 670-55-31-018 REFER TO ATTACHED M-234 I TEMS 2- 5 FOR COMPLIANCE. CUT OUT, DAMAGE FABRICATED AND DRILLED FILLER AND DOUBLER ALL WORK IAW REO 670-55-31-018 FILL ER AND DOUBLER MADE OUT OF 2024T3 .090 0030031186. PERFORMED ET INSP OF CUTLINES IAW CRJ 700NDTM 51-20-006, NO DEFECTS NOTED. SEALED AND STARTED INSTALLING LT DRAG ANGLE REPAIR FILLER AND DOUBLER ALL RIVETS SHOT ALL BUT (5) HI-LOKS INSTAL LED IAW REO 670-55-31-018. FINISHED INSTALLING FILLER AND DOUBLER FILLET SEALED EDGES AND PAINTED ALL WORK IAW REO 670- 55-31-019. SUPPLEMENTAL SDR CLOSED 2/15/08. 2 L 7 2 4F RT A21EA 2008030600251 20080306 00251 EA 2008 3 6 TRAX200800195 1 20080204 A 5534 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 VERTICAL STAB TO FUSELAGE RT DRAG ANGLE CRACKED. REPAIRED RT VERT STAB DRAG ANGLE IAW REO 670-55-31-018 REFER TO ATTACH ED M-234 ITEMS 2-5 FOR COMPLIANCE. CUT OUT DAMAGE, FABRICATED AND DRILLED FILLER AND DOUBLER ALL WORK IAW REO 670-55-3 1-31-018, FILLER AND DOUBLER MADE OUT OF 2024T3 .090 P030031186. PERFORMED ET INSP OF CUTLINES PER NDTM CRJ 700 51-20-0 06, NO DEFECTS NOTED. SEALED AND STARTED INSTALLING RT REPAIR FILLER AND DOUBLER ON RT DRAG ANGLE, ALL RIVETS SHOT NEED S HI-LOKS INSTALLED IAW REO670-55-31-018. FINISHED INSTALLING FILLER AND DOUBLER FILLET SEALED EDGES AND PAINTED ALL WO RK IAW REO 670-55-31-018. SUPPLEMENTAL SDR CLOSED 2/15/08. 2 L 7 2 4F RT A21EA 2008030600257 20080306 00257 EA 2008 3 6 VNAA0801009 1 20080131 A 2421 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 2 FAILED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 218PS 8990 7885 CREW ABORTED THE TAKEOFF DUE TO A GEN 2 OFF CAS MESSAGE. CREW RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PER FORMED A REJECTED TAKEOFF INSPECTION AND DEFERRED THE NR 2 IDG PER MEL 24-11-01-3. MAINTENANCE REMOVED AND REPLACED THE NR 2 IDG. MEL WAS CLEARED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008030600265 20080306 00265 NM 2008 3 6 SWAA081068 1 20080226 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 405WN 27893 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008030600306 20080306 00306 EA 2008 3 6 MASA200800171 1 20080226 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 592ML 7410 PERMANENT REPAIR OF INTERCOSTALS. 2 L 7 2 4F RT A21EA 2008030600325 20080306 00325 NM 2008 3 6 ABXA080063 1 20080129 A 5230 140T260313 DOOR FRAME BOEING 767 767231 1385131 NM AFT CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 707AX 22570 AFT LOWER CARGO DOOR FRAME BELOW VENT DOORS CORRODED IN SEVERAL PLACES. REMOVED AND REPLACED CHORD DOOR BEAM IAW B767 S RM 51-40-02. 2 L 7 2 4F RT A1NM 2008030700004 20080307 00004 NM 2008 3 7 USAA920080505 1 20080222 A 5230 FRAME BOEING 737 7374B7 1384702 NM ZONE 800 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 445US 1826 24863 CLT - MAJOR REPAIR - C1 CHECK - AFT CARGO COMPARTMENT DOOR FORWARD FRAME CRACKED. REPLACED AFT CARGO COMPARTMENT DOOR I AW USAIRWAYS TASK CARDS 03C21952004 AND 03C21952008. 2 L 7 2 4F RT A16WE 2008030700014 20080307 00014 NM 2008 3 7 2008UALA00950 1 20080218 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 336UA 24240 RAMP REPORTS DENTS AFT OF DOOR 2L, THERE IS A TOTAL OF 4 DENTS. SKIN REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700036 20080307 00036 NM 2008 3 7 ASAA0842679 1 20080130 A 5754 65C26601389 WEDGE BOEING 737 7374Q8 138447Q NM L/E SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 LEFT WING NR 1 SLAT T/E WEDGE AREA OF DELAMINATION ON O/B UPPER SUFACE. REMOVED DAMAGED AREA OF DELAMINATION, FABRICATE D CORE AND REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 PGS 201 PAR 9G 217 218 PAR 8 214 PAR 15 20 PGS 241 242 25 4 257. 2 L 7 2 4F RT A16WE 2008030700046 20080307 00046 NM 2008 3 7 ASAA0842670 1 20080127 A 5755 SKIN BOEING 737 7374Q8 138447Q NM NR 6 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 RIGHT WING NR 6 SPOILER DENTED ON UPPER SURFACE 15" FRM I/B END. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND B ONDED IAW B737 400 SRM 51 70 10 PGS 212 214 223 241 AND 254 257 REPAIR 2. 2 L 7 2 4F RT A16WE 2008030700051 20080307 00051 EU 2008 3 7 USAA920080516 1 20080226 A 3350 LIGHT AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 634AW 91 FLT NR 617 PHX - EEL - PASSENGER SEAT EMERGENCY ESCAPE PATH LIGHT AT 5 LT INOP. REPLACED SPLICES IN RUN ON SEAT 5 LT EM ERGENCY ESCAPE PATH LIGHT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008030700069 20080307 00069 NM 2008 3 7 USAA920080512 1 20080212 A 5230 507945264 SKIN BOEING 737 7374B7 1384702 NM ZONE 800 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT - MAJOR REPAIR - C3 CHECK - FORWARD PASSENGER DOOR INNER SKIN CRACKED AT NR 7 DOOR STOP. REPAIRED THE FORWARD PASSE NGER DOOR INNER SKIN AT NR 7 DOOR STOP IAW USAIRWAYS EA 100186. 2 L 7 2 4F RT A16WE 2008030700085 20080307 00085 NM 2008 3 7 HALA0800360 1 20080228 A 5730 SKIN BOEING 767 7673G5 1385126 NM LWS 802 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION ON LEFT WING TOP SURFACE, AT REAR SPAR, LEFT WING STATION 802. REPAIRED PER SRM 57-20-01. 2 L 7 2 4F RT A1NM 2008030700092 20080307 00092 WP 2008 3 7 UPS08851716 1 20080225 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-01-2. 2 L 7 4 4F RT 4A25 2008032700134 20080327 00134 NE 2008 3 27 MASA200800240 2 20080319 A 7200 CF343B1 ENGINE CNDAIR CL600 CL6002D24 1390016 EA GE CF34 CF343B1 30070 NE NR 2 MALFUNCTIONED A MASA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 07 27185 24251 7185 872093 ASH FLT 7347 ORD-BHM, CAPT REPORTS HEARING A LOUD POPPING NOISE FROM NR 2 ENGINE FOLLOWED BY HIGH ITT (RED-LINE) AND ENG INE VIB. CAPT SHUTDOWN NR 2 ENGINE, DECLARED AN EMERGENCY AND DIVERTED TO SPI. REMOVED AND REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008032700135 20080327 00135 SO 2008 3 27 LR7A08046 1 20080319 A 5330 SKIN LKHEED 382 382G 526414U SO FS 142 DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 480 4590 DURING MAINTENANCE REVIEW A 4 INCH LONG DENT WAS NOTED IN NOSE WHEEL WELL SKIN AT FS 142, WL156, RBL66, REQUIRING MAJOR REPAIR. AIRCRAFT FERRIED TO ANC, REPAIR ACCOMPLISHED IAW LAC MEA 382-53-08-016. 2 H 7 4 4T A1SO 2008032700138 20080327 00138 SO 2008 3 27 SWIA200819369 1 20080318 A 5753 STRUCTURE EMB 120 EMB120ER 3260203 SO NACELLE FLAP CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 291SW 120318 RIGHT NACELLE FLAP IS CRACKED. REPLACED RIGHT NACELLE FLAP IAW EMB 120 MM 27-50-03. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008032700139 20080327 00139 EA 2008 3 27 SWIA200819370 1 20080316 A 3260 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 983CA 111 111 7169 RECEIVED "GEAR DISAGREE" AND "NOSE DOOR OPEN" WARNING MESSAGES, FLIGHT NR 2702. REPLACED PSEU IAW AMM 32-61-00. ALL CH ECKS OK. 2 L 7 2 4F RT A21EA 2008032700142 20080327 00142 NM 2008 3 27 DL738080395 1 20080319 A 2120 UNKNOWN BOEING 737 737832 13844CF NM CABIN ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 3752 29670 DURING CRUISE, FLIGHT ATTENDANT AND PASSENGERS REPORT SMELLING FUEL IN FIRST CLASS. INSPECTED A/C IAW MM. RAN ENGINES TO T/O AND CRUISE SETTINGS FOR 20 MINUTES. NO EVIDENCE OF ANY ODOR IN CABIN. ENGINE ANTI-ICE, WING, PACKS FULL HOT AND FULL COLD, RECIRC FANS ON AND OFF, APU ON AND OFF. FOUND PAX BAG WITH OPEN CONTAINER OF FLUID. A/C OK FOR SERVICE IAW M M. 2 L 7 2 4F RT A16WE 2008032700148 20080327 00148 NE 2008 3 27 DL76L080400 2 20080321 A 7230 CASE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 FAN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 197DN 41606 28454 727775 NR 1 ENG CHANGE DUE TO FAN CASE CRACK. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032700158 20080327 00158 EA 2008 3 27 SIMA200808403 1 20080322 A 2781 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA SLATS ILLUMINATED A SIMA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 521AE 10142 ON FLIGHT 3645 CREW REPORTED ON APPROACH INTO PIT THE SLAT FAIL CAUTION MSG. CREW ELECTED TO DECLARE AN EMERGENCY. AIR CRAFT LANDED AND TAXIED SAFELY TO THE GATE WITHOUT FURTHER INCIDENT. 2 L 7 2 4F RT A21EA 2008032700159 20080327 00159 EA 2008 3 27 MASA200800250 1 20080320 A 5210 HANDLE CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR OBSTRUCTED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 925FJ 15025 ASH FLT 2643 CLT-IND, PAX DOOR OUTER HANDLE STOW CAUTION IN FLIGHT. MX CLEANED DEBRIS, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008032700162 20080327 00162 NM 2008 3 27 P5CA0801550 1 20080320 A 7830 GIMBAL JOINT BOEING 747 74747UF 1384812 NM THRUST REVERSER BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 416MC 32838 DURING ROUTINE INSPECTION OF NR 3 THRUST REVERSER FOUND LT LOWER ACTUATOR MOUNTING BRACKET GIMBAL BROKEN. REMOVED THE N R 3 ENGING LOWER LT ANGLE GEARBOX HOUSING AND BALLSCREW ACTUATOR AS PER AMM 78-31-22, PERFORM DVI INSPECTIONS PER EO NR 4478A065 PRIOR TO EACH CYCLE. 2 L 7 4 4F RT A20WE 2008032700163 20080327 00163 EU 2008 3 27 CPCP20080012 1 20080304 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 377AT 377 RT I/B SEAT TRACK BETWEEN FRAME 29 TO FRAME 35 CORRODED. RT I/B SEAT TRACK BETWEEN FRAME 29 TO FRAME 35. REPLACED IAW SRM 51-40-22. 2 H 7 2 4T RT A53EU 2008032700167 20080327 00167 NM 2008 3 27 2008UALA01403 1 20080313 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 LOWER FUSELAGE AFT RT SIDE OUTFLOW VALVE CUTOUT HAS GOUGES AT BS 976 NEAR STRINGER S-22R. MAJOR REPAIR ACCOMPLISHED: F ABRICATED & INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER AT OUTFLOW CUTOUT. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032600126 20080326 00126 SO 2008 3 26 CHQA200800050 1 20080314 A 2520 7277120501 PRINTED CKT BOAR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN BURNED A CHQA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 11 579RP 145871 CAE311509 RIC TO CVG - ON APPROACH TO CVG, THE FLIGHT ATTENDANT NOTIFIED THE FLIGHT CREW THAT THERE WAS SMOKE COMING FROM THE OVER HEAD AROUND ROW 8 ACCOMPANIED BY THE SMELL OF BURNING ELECTRONICS. THE FLIGHT CREW HAD NO INDICATIONS ON EICAS AND THE AIRCRAFT CONTINUED APPROACH AND LANDED AT CVG WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE C IRCUIT BOARD FOR THE PSU ABOVE SEAT 7A WAS BURNT. THE CIRCUIT BOARD WAS REPLACED AND THERE WERE NO FURTHER DEFECTS NOTE D. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008032600175 20080326 00175 NM 2008 3 26 QXEA200800293 1 20080313 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - C4- AFT CARGO BAY SEAT TRACK NR 9 HAS NUMEROUS AREAS OF CORROSION INSIDE TRACK AND AROUND RIVETS. REMOVED SEAT TR ACK REF Q400 SRM 51-42-05. INSTALLED NEW SEAT TRACK NR 9 REF Q400 SRM 51-42-05 AND 51-40-15. 2 H 7 2 4T RT A13NM 2008032600212 20080326 00212 EU 2008 3 26 08FDEA01034 1 20080318 A 5730 A5724854500100 PANEL AIRBUS 310 A310203 3930313 EU ZONE 600 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT WING L/E LOWER SURFACE PANEL 623 LB SPEED TAPE IS PEELING OFF AND TORN. REMOVED DAMAGED FOIL IAW SRM 57-41-12. APPLI ED NEW FOIL IAW SRM 51-75-12. PRIMED IAW SRM 57-41-12. 2 L 7 2 4F RT A35EU 2008032600220 20080326 00220 WP 2008 3 26 08FDEA01043 1 20080318 A 5753 S391318154 PANEL DOUG MD10 MD1010F 3022112 WP RT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RT INBD FLAP AFT INBD EDGE IS CRACKED. REMOVED, LOCATED, DRILLED & INSTALLED T/E TIP IAW SRM 51-35-02, VOL II. REMOVED, INSTALLED & CHECKED PER AMM 27-50-01-4. 2 L 7 3 4F RT A22WE 2008032600225 20080326 00225 EU 2008 3 26 08FDEA01049 1 20080319 A 5420 A546114002000 PANEL AIRBUS 310 A310203 3930313 EU NR 2 PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 PYLON PANEL NR 423 EL IS CORRODED ON THE MATING SURFACES. RECEIVED NEW PANEL. INSTALLED NEW EDGE STRIPS TO THE PA NEL REF SRM 51-40-21 PARA 6. 2 L 7 2 4F RT A35EU 2008032600251 20080326 00251 EU 2008 3 26 08FDEA01066 1 20080319 A 5320 A5361068856702 FITTING AIRBUS 310 A310324 3930206 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 EDDIE CURRENT AND VISUAL INSPECTIONS INDICATE SURFACE CORROSION AT APPROX 45 PLACES ON THE SCUFF PLATE RETAINER BETWEEN FR 14B AND FR 16A; LT FWD DOOR CUTOUT. SEE ATTACHED FOR LOCATIONS. MARKED IN BLUE ON THE RETAINER. REMOVED CORROSION IAW A310-SRM 53-10-18; FIG 101. ORIGINAL MATERIAL .500. MATERIAL LOSS .010. MATERIAL REMAINING .490. CENTER SECTION F OUND TO BE OUT OF LIMITS DUE TO A CRACK IAW A310 SRM 53-10-18; FIG 101. REMOVED AND REPLACED WITH NEW CENTER SECTION P/ N A5361068856702; PO 611668.1 IAW A310 SRM 53-12-18; FIG 1 SHEET 2; 51-40-40; 51-40-21, PG 7; 51-21-10 AND 51-23-10. 2 L 7 2 4F RT A35EU 2008032600273 20080326 00273 NM 2008 3 26 C8GA20080011 1 20080314 A 5270 1SE16 SWITCH BOEING 727 727225 1384077 NM AFT AIRSTAIRS FAULTY A C8GA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 29 755DH 21857 FLT 738 FROM TOL TO SLW - DURING CLIMB-OUT, THE AFT AIRSTAIR LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT RETURNED TO TOL WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE AFT AIRSTAIR CONTROL HANDLE MICROSWITCH WAS AT FAULT. THE AFT AIRSTAIR CONTROL HANDLE MICROSWITCH WAS REMOVED AND REPLACED, ADJUSTED AND PERFORMED, OPS CHECK ALL C HECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2008032600278 20080326 00278 EA 2008 3 26 REXA200800006 1 20080319 A 2611 PU90421R3 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY MALFUNCTIONED A REXA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 25 8495B 7495 FALSE TOILET SMOKE MESSAGE ON TAKEOFF, QRH FOLLOWED RETURNED TO AIRPORT NO SMOKE OR HEAT NOTICED. SYSTEM DEFERRED PER M EL 26-16-01 (DETECTOR NEEDS CHANGED). 2 L 7 2 4F RT A21EA 2008032700015 20080327 00015 NM 2008 3 27 NOCA01808 1 20080313 A 2560 P4010021 BATTERY BOEING 757 75728A 1384976 NM FLASHLIGHT DISCHARGED A NOCA K NONE O OTHER UK UNKNOWN 1 EA 15 754NA 29381 R3 JUMPSEAT FLIGHT ATTENDANT FLASHLIGHT INOP. REMOVED AND REPLACED R3 FLASHLIGHT BATTERY, SECURED AS REQUIRED, OK FOR S ERVICE. 2 L 7 2 4F RT A2NM 2008032700027 20080327 00027 SO 2008 3 27 RAIA00803008 1 20080311 A 3297 CONNECTOR EMB 145 EMB145 3260210 SO NLG DEFECTIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 805HK 145096 FLT 3539 - PIT - LANDING GEAR WOULD NOT RAISE AFTER TAKEOFF. ASSOCIATED AIR/GROUND FAIL MESSAGE ON THE EICAS. MAINTENA NCE REMOVED AND REPLACED THE NOSE DOWNLOCK CONNECTOR. SYSTEM CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2008032700042 20080327 00042 NM 2008 3 27 2008UALA01435 1 20080314 A 2612 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO FIRE PANEL INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 312UA 23673 NR 1 CARGO FIRE BOTTLE LIGHT INOP ON CARGO FIRE PANEL. REPLACED FIRE DETECTION CONTROL PANEL LIGHT TESTS OK. AC OK FOR S ERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700046 20080327 00046 NM 2008 3 27 DHL2008765003 1 20080121 A 5310 TORQUE BOX BOEING 727 727264 138408M NM BS 1265 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, AFT STAIRWELL LIGHTENING HOLE CRACKED 5 O'CLOCK POSITION RIGHT SIDE BS 1265 (TORQUE BOX). CUT OUT DAMAG ED AREA AT AFT STAIRWELL LIGHTENING HOLE DIMENSION 1" BY .75" IAW SRM 51-40-2 FIG 1. FABRICATED DOUBLER REPAIR IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. DRILLED HOLES AT NEW DOUBLER IAW SRM 51-30-5. TREATED AND PRIMED PART AND AREA IAW SR M 51-10-2. INSTALLED DOUBLER REPAIR IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032700078 20080327 00078 SO 2008 3 27 RAIA00803013 1 20080317 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 840HK 145341 PRE FLT 8005 - IAD - EMERGENCY LIGHT INOPERATIVE IN THE CABIN. MAINTENANCE RE-SECURED A LOOSE WIRE ON THE LIGHT ASSEMBL Y. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008032700100 20080327 00100 NM 2008 3 27 QXEA200800300 1 20080313 A 5340 ATTACH ANGLE BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - C4 - THE ANGLE ATTACHED TO FRAME X26.700 AT STR 25S/L IS CORRODED (BELOW DOOR SILL). REMOVED THE ATTACH ANGLE FRO M FRAME X26.700 AND STR 25S/L BY REMOVING THE RIVETS FROM THE AIRCRAFT. FABRICATED A NEW ANGLE OUT OF 7075 T6 .050 USIN G OLD PART AS A TEMPLATE. HFEC INSPECTED BLEND RADIUS ON FABRICATED ANGLE FOR CRACKS IAW NDTM PART 6, 51-00-01. NO CRA CKS NOTED. INSTALLED ATTACH ANGLE WITH RIVETS PER SRM 51-42-05. ALODINED AND PRIMED ANGLE PRIOR TO INSTALLATION, INSTA LLED REMAINING HI LIGHT FASTENER, REF SRM 51-40-15. 2 H 7 2 4T RT A13NM 2008032700102 20080327 00102 SO 2008 3 27 SIMA200808115 1 20080310 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO CARGO DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 683AE 9364 5000 14500833 DURING A IMBV INSPECTION, THE CARGO DOOR CENTER SILL WAS FOUND CORRODED. REMOVED SILL REPLACED WITH NEW PART IAW SRM 51 -40-02, 51-40-04, AND 51-40-06. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032700129 20080327 00129 EA 2008 3 27 MASA200800248 1 20080320 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17231 7231 ASH FLT 2824 PHX-TUS, RT OVERWING EMERGENCY EXIT FLOOR LEVEL SIGN LIGHTS INOP. MX RESET THE SYSTEM AND THE LIGHT OP CHE CKED GOOD. 2 L 7 2 4F RT A21EA 2008032700131 20080327 00131 EA 2008 3 27 MASA200800249 1 20080320 A 5270 SWITCH CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT DIRTY A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 926LR 15026 ASH FLT 2878 PHX-ELP, RIGHT AFT EMERGENCY EXIT DOOR CAUTION MESSAGE INTERMITTENT. MX CLEANED SWITCH. 2 L 7 2 4F RT A21EA 2008032700140 20080327 00140 SO 2008 3 27 SWIA200819371 1 20080319 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO CABIN SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 07 578SW 120346 AIRPLANE FILLED WITH HAZE ON DESCENT, FLIGHT NR 5478. INSPECTED PACKS AND RAN ENGINES WITH NO DEFECTS NOTED. OPS CHECK GOOD IAW EMB MM 21-10-00. 2 L 7 2 4T RT A31SO 2008032700141 20080327 00141 NM 2008 3 27 DL76S080394 1 20080319 A 3610 212T311917X DUCT BOEING 767 767332 1382001 NM APU SUPPLY SPLIT A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 127DL 24077 CREW REPORTED HEARING LOUD POP AND FELT EARS POP THEN GOT BODY DUCT LEAK LIGHT. AFT CABIN FILLED WITH SMOKE AND CABIN G OT VERY HOT. PASSENGER SEATED AT 42A GOT A BURN TO HER LEG. PBE AND HALON BOTTLES USED, FLT DIVERTED TO GSP. MTC FOUN D PNEU DUCT LOCATED LT SIDE OF AFT B/B BLOWN/SPLIT, MPN 212T3119-17X. ALSO, HAD DAMAGE TO INSULATING BLANKETS AND SIDEW ALL PANELS. DELTA MTC PERFORMING REPAIRS. VOICE RECORDER AND FLT REC PULLED AT REQUEST OF FLT SAFETY. 2 L 7 2 4F RT A1NM 2008032700154 20080327 00154 GL 2008 3 27 SIMA200808118 2 20080320 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 SMOKE A SIMA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 696AE 15656 14500874 CAE311718 ON FLIGHT 3799, CREW REPORTED SMOKE IN CABIN AND COCKPIT WHEN POWER WAS APPLIED FOR TAKEOFF. ABORTED TAKEOFF AND EMERGE NCY WAS DECLARED. AIRCRAFT RETURNED TO GATE UNEVENTFULLY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 EN GINE ASSEMBLY IAW WORK CARD 71-000-00. OPERATIONAL CHECKS GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008032700156 20080327 00156 2008 3 27 MASA200800241 4 20080319 A 2561 P0640101 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA CABIN OPEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 654BR 644 7454 ASH FLT 1002 HNL-ITO, INFANT LIFE VEST PACKAGE WAS OPENED. MX REPLACED THE LIFE VEST. 2 L 7 2 4F RT A21EA 2008032700168 20080327 00168 NM 2008 3 27 2008UALA01404 1 20080313 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 STRINGER CLIP CRACKED ON STR 25R AT BS 747. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700174 20080327 00174 EU 2008 3 27 CPCP20080015 1 20080304 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 377AT 377 RT INBOARD SEAT TRACK FRAME 23- FRAME 29 CORRODED. RT INBOARD SEAT TRACK FRAME 23 TO FRAME 29. REPAIRED AS PER SRM 53- 00-00. 2 H 7 2 4T RT A53EU 2008032700176 20080327 00176 NM 2008 3 27 2008UALA01408 1 20080313 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FWD GALLEY DOOR LOWER HINGE CUTOUT HAS 5 EA FASTENER HOLES CRACKED. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT CRACK COMMO N TO BEAR STRAP. FABRICATED & INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER REPAIR & FREEZE PLUG REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700180 20080327 00180 NM 2008 3 27 2008UALA01413 1 20080313 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 CABIN FRAME BS 303.9 IS CRACKED ON AFT SIDE DOUBLER AT FEED THROUGH FOR STR 16L. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED FRAME REPAIR ANGLE REPAIR. REPAIR OF INTERCOSTAL - FABRICATED AND INSTALLED 2 CLIPS & 2 ANGLES, 1 H-STRAP & 1 FRAME DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700181 20080327 00181 2008 3 27 HALA0800411 4 20080313 A 3461 FMC BOEING 767 76733A 1385209 NM MALFUNCTIONED A HALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 580HA 28140 SUB - ATB - RETURNED TO HNL DUE TO UNRELIABLE NAV, LANDING WEIGHT 312,000, UNDER WEIGHT. ACCOMPLISHED FIM 34-61-00, NO FAULTS FOUND. RELOADED LEFT FMC SOFTWARE AS PRECAUTIONARY. BOTH LEFT AND RIGHT FMC OPS CHECK OK PER AMM 34-61-10. 2 L 7 2 4F RT A1NM 2008032700183 20080327 00183 WP 2008 3 27 08FDEA01050 1 20080319 A 5350 AKC707411 SKIN DOUG MD10 MD1010F 3022112 WP TAILCONE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 TAIL CONE UPPER AFT SKIN HAS 3 HOLES (LT AFT EDGE). REPAIRED HOLES PER SRM 53-00-01; VOL I. DOUBLER PER SRM 53-00-01; VOL I AND SRM 53-52-01; VOL III; PO 483358.1. ALODINED AND PRIMED PER SRM 51-21-01; VOL II. INSTALLED PER SRM 53-00-0 1; VOL I AND SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 2008032700189 20080327 00189 NM 2008 3 27 2008UALA01418 1 20080313 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 CATERERS NOTIFIED MAINTENANCE OF 3 DENTS AFT OF DOOR 2L. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED DOUBLER/TRI PLER/FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700190 20080327 00190 NM 2008 3 27 2008UALA01425 1 20080313 A 5320 SUPPORT FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FUSELAGE STR 8L SUPPORT CLIP FOR INTERCOSTAL IS CRACKED BS 360. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED REPL ACEMENT CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700194 20080327 00194 WP 2008 3 27 08FDEA01096 1 20080321 A 5344 29993257200 HINGE DOUG MD10 MD1010F 3022112 WP ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 FWD CARGO DOOR CONTROL PANEL DOOR HINGE HAS EXCESSIVE PLAY. REMOVED FWD CARGO DOOR CONTROL PANEL DOOR TO FOM PER DC/MD- 10 SRM 53-31-01; VOL II. RECEIVED NEW HINGE P/N 2999325N, AND P/N ADA 3469-7, PO 544680.1. ALODINED HINGE PER SRM 51-2 1-01; PARA 31; VOL II. INSTALLED CONTROL PANEL DOOR PER SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 2008032700198 20080327 00198 NM 2008 3 27 2008UALA01432 1 20080314 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 ROW 55 LT EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032700200 20080327 00200 NM 2008 3 27 2008UALA01433 1 20080314 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 ROW 5A AFT EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032700201 20080327 00201 WP 2008 3 27 08FDEA01105 1 20080321 A 5410 AUB7054501 PANEL DOUG MD10 MD1010F 3022112 WP NR 3 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 NR 3 ENGINE PYLON PER-COOLER PANEL NR 487 DR HAS 2 CRACKS AT THE LOUVER OPENING. INSTALLED REPAIR DOUBLER IAW SRM 54-00 -01 VOL I FIG 2-B SHEET 2. TOPCOATED IAW SRM 51-23-01 VOL II. 2 L 7 3 4F RT A22WE 2008032700204 20080327 00204 NM 2008 3 27 08FDEA01107 1 20080322 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 MAIN CARGO COMPARTMENT, FLOORBEAM CORRODED BETWEEN BL 0 BL 25L , B.S. 950D 2 L 7 3 4F A3WE 2008032700211 20080327 00211 NM 2008 3 27 2008UALA01477 1 20080315 A 2560 65659733 ANCHOR FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU GIRT BAR CORRODED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 202UA 24717 DOOR 1L ESCAPE SLIDE GIRT BAR FLOOR LATCH ANCHOR FITTINGS ARE CORRODED BS 312 & 344 APPROX LBL 54". REPLACED GIRT BAR FL OOR FITTINGS. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700215 20080327 00215 NM 2008 3 27 2008UALA01479 1 20080316 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 315UA 23947 EMERGENCY PATH LIGHTS LOOSE ON FLOOR NEAR 7C. SECURED PLASTIC COVER FOR EEL PATH LIGHTING AT ROW 7ABC,OPS NORMAL. AC O K FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700216 20080327 00216 NM 2008 3 27 2008UALA01480 1 20080316 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT DOOR 4LT AFT SILL INOP. REPLACED LAMP, OP CK'D NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032700217 20080327 00217 NM 2008 3 27 08FDEA01114 1 20080323 A 5311 AFA00193 FRAME DOUG MD11 MD11F 3023600 NM BS 1721 S12R DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 522FE 48476 MAIN DECK RIGHT FRAME AT BS 1721 S12R FOUND DENTED. REPAIRED AS PER SRM 53-30-00, FIG.1, VOL.1. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00, FIG.1, VOL.1. REPAIR CLAS SIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032700219 20080327 00219 NM 2008 3 27 08FDEA01115 1 20080323 A 5311 AFA00273 FRAME DOUG MD11 MD11F 3023600 NM BS 1661 S12L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 522FE 48476 MAIN DECK LEFT FRAME AT STATION 1661, STRINGER 12 LEFT FOUND DENTED. REPAIRED AS PER SRM 53-30-00, FIG.1, VOL.1. INITI AL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00, FIG.1, V OL.1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032700228 20080327 00228 WP 2008 3 27 08FDEA01120 1 20080324 A 7830 9059M71G03 FAIRING DOUG MD10 MD1010F 3022112 WP THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 NR 2 ENGINE LT T/R TRANSLATING SLEEVE AFT LOWER FAIRING IS CRACKED AT THE FWD CORNER. THE CRACK WAS PREVIOUSLY STOP DRI LLED BUT HAS PROGRESSED BEYOND THE STOP DRILL. REMOVED FAIRING IAW SRM 51-35-01; VOL II. LOCATED & DRILLED HOLES IN TH E SUBSTRUCTURE IAW SRM 51-31-01; VOL II. INSTALLED SUBSTRUCTURE IAW SRM 51-35-01 VOL II. INSTALLED FAIRING IAW SRM 51-3 5-01 VOL II. 2 L 7 3 4F RT A22WE 2008032700229 20080327 00229 NM 2008 3 27 2008UALA01486 1 20080316 A 3350 3004071 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 CABIN L1 DOOR MOUNT SLIDER EMERGENCY LIGHT NOT ON. REPLACED LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032700233 20080327 00233 WP 2008 3 27 08FDEA01123 1 20080324 A 5311 ADA007311 FRAME DOUG MD10 MD1010F 3022112 WP BS 899 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 FWD PIT; FS 899, L51L FRAME HAD DOUBLE DRILLED HOLES. REPAIRED IAW SRM 53-00-01 VOL. I FIG. 10. 2 L 7 3 4F RT A22WE 2008032700251 20080327 00251 EU 2008 3 27 08FDEA01134 1 20080324 A 5730 A5735005700000 PANEL AIRBUS 310 A310203 3930313 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT FUEL TANK PANEL 640 FB HAS FRETTING CORROSION ON OUTER PANEL MATING SURFACES. FUEL PANEL IS OUT OF LIMITS REF A 310-200 SRM 57-20-16; FIG 103; SHEET 4. REPLACED FUEL PANEL TO BE INSTALLED ON FEDEX WIC 46X5052ALI. 2 L 7 2 4F RT A35EU 2008032700252 20080327 00252 NM 2008 3 27 2008UALA01529 1 20080318 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 CABIN FLOOR CREASE BEAM CORRODED BS 500 - 520 RBL 63"-69". 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700257 20080327 00257 NM 2008 3 27 2008UALA01530 1 20080318 A 5320 TEAR STRAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 787-794 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 AFT CARGO COMPARTMENT LOWER FWD CORNER TEAR STRAP HAS SURFACE CORROSION BS 787 TO 794 AND STRINGERS 26R 27R. MAJOR REPA IR ACCOMPLISHED: FABRICATED AND INST'D EXTERNAL FUSELAGE SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700258 20080327 00258 NM 2008 3 27 AALA200800490 1 20080304 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 966AN 30094 MIA - EMERGENCY LIGHT AT SEAT ROW 27 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 27. SYSTEM GROUND CHEC KED NORMAL OPERATION 2 L 7 2 4F RT A16WE 2008032700267 20080327 00267 NM 2008 3 27 AALA200800498 1 20080304 A 3350 BPS73 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 322AA 22323 LAX - EMERGENCY EXIT SIGN LIGHTS AT LEFT AND RIGHT OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHTS AT LEFT AND RIGHT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008032700268 20080327 00268 NM 2008 3 27 AALA200800501 1 20080304 A 3397 WIRE DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 951TW 53470 LGA - EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT 2008032700277 20080327 00277 NM 2008 3 27 AALA200800509 1 20080304 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT AT SEAT 26C HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700279 20080327 00279 SO 2008 3 27 C2XA08ON106 1 20080308 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 22909 15997 15997 145459 FLT 7780 - LAX TO SFO - WHILE PERFORMING EMERGENCY LIGHT TESTING, CREW REPORTED AISLE EMERGENCY EXIT PROXIMITY STRIP LIG HT INOP. MX ROBBED EMERGENCY LIGHT BATTERY FROM A/C 569, OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032700280 20080327 00280 NM 2008 3 27 AALA200800500 1 20080304 A 3350 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT OUT OF ADJUST A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 951TW 53470 LGA - EMERGENCY LIGHTS AT FIRST CLASS ENTRY INOPERATIVE. ADJUSTED CONTACTS IN BATTERY PACK FOR EMERGENCY LIGHTS AT FIRS T CLASS ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2008032700282 20080327 00282 NM 2008 3 27 AALA200800516 1 20080305 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 750AN 30259 MIA - EMERGENCY LIGHT AT SEAT 39G HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 39G. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700283 20080327 00283 NM 2008 3 27 AALA200800510 1 20080305 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT AT SEAT 26C HAS MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700294 20080327 00294 NM 2008 3 27 AALA200800520 1 20080305 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 944AN 29535 MIA - EMERGENCY LIGHT AT SEAT 21D INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008032700300 20080327 00300 NM 2008 3 27 DHL2008763520 1 20080302 A 5311 FRAME BOEING 727 727264 138408M NM BS 600 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 FRAME GOUGED IN CARGO COMPT AT BS 600, ABOVE STR 17R. CUT OUT DAMAGE, FABRICATED FRAME REPAIR, AND INSTALLED PER B727 S RM 51-40-3 FIG 1, 53-10-2 FIG 3, AND 51-30-2. 2 L 7 3 4F A3WE 2008032700302 20080327 00302 NM 2008 3 27 DHL2008763521 1 20080302 A 5311 FRAME BOEING 727 727264 138408M NM BS 640 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 FRAME DENTED AND GOUGED IN CARGO COMPT AT BS 640, ABOVE STR 17R. CUT OUT DAMAGE, FABRICATED FRAME REPAIR, AND INSTALLED PER B727 SRM 51-40-3 FIG 1, 53-10-2 FIG 3, AND 51-30-2. 2 L 7 3 4F A3WE 2008032700311 20080327 00311 WP 2008 3 27 NWAA081119606 1 20080321 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 606NW 47225 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WERE IN OPERATIVE. MAINTENANCE REPLACED THE TAIL COMPARTMENT EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2008032700312 20080327 00312 WP 2008 3 27 NWAA081079753 1 20080318 A 3397 WIRE DOUG DC9 DC941 302207N WP EMERGENCY LIGHT DAMAGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 753NW 47117 DURING LINE CHECK, MAINTENANCE FOUND THAT TWO OF THE EMERGENCY PATHWAY LIGHTS FOR THE CATWALK IN THE TAIL COMPARTMENT WE RE INOPERATIVE. MAINTENANCE FOUND OPEN WIRES IN THREE LOCATIONS AND REPAIRED THEM AND THEN RETURNED THE AIRCRAFT TO SER VICE. 2 L 7 2 4F A6WE 2008032700314 20080327 00314 WP 2008 3 27 NWAA081109613 1 20080320 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 613NW 47438 DURING LINE CHECK, MAINTENANCE FOUND THAT THE AFT EMERGENCY OVERWING EXIT SIGNS ON BOTH THE LEFT AND RIGHT SIDES WERE IN OPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY (B5-25) AND OPERATIONALLY CHECKED THE SYSTEM. THE AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F A6WE 2008032700315 20080327 00315 SO 2008 3 27 C2XA08IA088 1 20080321 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 12157 145787 YYT - FLIGHT 2507, THE CREW REPORTED A BURNING SMELL THROUGH THE PACKS WITH THE APU RUNNING. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL 49-00-00 CAT C CONTROL NUMBER 141634, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. ON 03/20/08 FLIGHT 2017 THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE OPERATIONALLY CHECKED THE PACK SYSTEM USING THE APU WITH NO DEFECTS NOTED. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008032700317 20080327 00317 SO 2008 3 27 C2XA08TY038 1 20080322 A 2797 WIRE EMB 145 EMB145XR 3260214 SO SPOILER SYSTEM BROKEN A C2XA K NONE O OTHER CR CRUISE 1 SW 27 17108 145655 EWR/CLT- FLT 3068 - UNCOMMANDED SPOILER INDICATION IN FLIGHT. CLT MX REPAIRED A BROKEN WIRE AT C/P P1167 PIN A. OPS CH ECKS WERE GOOD IAW EMB 145 AMM 27-63-01. A/C WAS RELEASED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008032700318 20080327 00318 SO 2008 3 27 C2XA08CL036 1 20080322 A 5210 14524355001 BELLCRANK EMB 145 EMB145XR 3260214 SO PAX DOOR WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 34110 145658 CLE FLIGHT 2867 - THE CREW REPORTED THE MAIN CABIN DOOR WAS HARD TO OPEN. MAINTENANCE INSPECTED AND REPLACED THE ACTUAT ING CAM BELLCRANK TO CAM ROLLER BUSHING AND ADJUSTED THE MAIN CABIN DOOR RIGGING. OPERATIONAL CHECKS WERE GOOD. THE DO OR SEAL AND FUSELAGE SEALS WERE ALSO REPLACED. 2 L 7 2 4F RT 2008032700322 20080327 00322 SO 2008 3 27 C2XA08ON101 1 20080312 A 3080 AE717539 CONDUIT EMB 145 EMB145XR 3260214 SO ICE DETECTOR CRACKED A C2XA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 27 17196 6655 6655 14500945 FLT 0216 - ONT - ON 03/12/2008 FLIGHT CREW REPORTED WHAT APPEARED TO BE FUEL LEAKING FROM LT WING, MX PERSONNEL INSPECTE D THE AIRCRAFT AND NO FUEL LEAKS WERE FOUND. ON 03/14/2008 FLT 0010 - ONT - FLIGHT CREW REPORTED AGAIN LT WHEEL WELL FU EL LEAK. MX PERSONNEL CLEANED AND INSPECTED LT SIDE BELLY ACCESS PANEL AND NO DRIPS WERE NOTED AT THAT TIME. ON 0316/2 008 FLT 0107 - ONT - FLIGHT CREW REPORTED A FUEL LEAK COMING FROM THE LT WHEEL WELL. MX PERSONNEL RE-INSPECTED AND FOUN D ICE DETECTOR CONDUIT CRACKED, MX PERSONNEL REMOVED AND REPLACED ICE DETECTOR CONDUIT OPERATIONALLY AND LEAK CHECKED SA TISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008032700323 20080327 00323 SO 2008 3 27 C2XA08RI034 1 20080312 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO CARGO BAY DEFECTIVE A C2XA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 27 16976 12754 1270 145171 FLIGHT 2566 - EWR - CREW REPORTED BAG SMOKE INDICATION ON EICAS DURING TAXI. CREW RETURNED TO GATE WITHOUT ANY INCIDENT . EWR MX REMOVED AND REPLACED BAG SMOKE DETECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED T O RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032700328 20080327 00328 EU 2008 3 27 08FDEA01102 1 20080321 A 5230 A000702300258 DOOR FRAME AIRBUS 310 A310324 3930206 EU CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION AROUND THE AFT CARGO DOOR LINER FASTENER RECEPTICAL; LOWER PART OF FRAME 60 ON THE DOOR FRONT AND BACK SIDE OF THE DOOR. REMOVED CORROSION IAW A310-300 SRM 51-22-00 AND FOUND TO BE OUT OF LIMITS IAW A310-300 SRM 51-21-00. MATERI AL ID 2024-T3 0.050 PO 602303.2 IAW A310-300 SRM 52-32-00; PG 35 AND 51-31-00; PGS 21 AND 22. CUT OUT DAMAGE AND FABB ED REPAIR IAW A310-300 SRM 51-70-10. ALODINED IAW A310-300 SRM 51-21-00. PRIMED IAW A310-300 SRM 51-21-10. PAINTED IA W A310-300 SRM 51-23-10. INSTALLED DOUBLER IAW A310-300 SRM 51-70-10. 2 L 7 2 4F RT A35EU 2008032700329 20080327 00329 EU 2008 3 27 08FDEA01103 1 20080321 A 5230 A000702300258 LINER AIRBUS 310 A310324 3930206 EU CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 CORROSION AROUND THE AFT CARGO DOOR LINER FASTENER RECEPTACLE BETWEEN FRAME 62 AND FRAME 63 ON THE DOOR FRONT AND BACK S IDE OF THE DOOR. REMOVED CORROSION IAW A310-300SRM 51-22-00 AND FOUND TO BE OUT OF LIMITS IAW A310-300 SRM 52-30-00. M ATERIAL ID 2024-T3 PO 602303.2 IAW A310-300 SRM 52-30-00; PG 35 AND 51-31-00; PGS 21 AND 22. CUT OUT DAMAGE AND FABBE D DOUBLER IAW A310-300 SRM 51-70-10. ALODINED IAW A310-300 SRM 51-21-00. PRIMED IAW A310-300 SRM 51-21-10. PAINTED IA W A310-300 SRM 51-23-10. INSTALLED DOUBLER IAW A310-300 SRM 51-70-10. 2 L 7 2 4F RT A35EU 2008032700336 20080327 00336 SW 2008 3 27 WGEA200800049 1 20080314 A 3250 M04007H101013 STEERING SYS ECLIPS EA500 ECLIPSEEA500 3350000 SW NLG MALFUNCTIONED E WGEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 146DJ 139 000058 TAKING THE RUNWAY AT A SLOW SPEED, AND STEERING DISPLACEMENT AT 10 PERCENT TO 15 PERCENT RATE OF TURN. AIRCRAFT LOST ST EERING CAPABILITY (CASTERED), TRY TO REENGAGE 2 TIMES, RETURN TO GATE. REMOVED NOSE GEAR ASSEMBLY AND INSTALLED NEW ASS EMBLY IAW EA500 AMM 32-20-10 AND TSR 32-031708G. PERFORMED NOSE GEAR AND DOORS ADJUSTMENT/TEST IAW EA500 AMM 32-20-00. PERFORMED STEERING ADJUSTMENT/TEST IAW EA500 AMM 32-50-00. ALL CHECKS GOOD. 1 L 7 2 4J RT A00002AC 2008032700337 20080327 00337 NE 2008 3 27 NWAA081159974 2 20080321 A 7200 JT8D9A ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE NR 1 MALFUNCTIONED A NWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 9338 63910 3884 47347 65700 ON TAKEOFF FLIGHT, CREW NOTICED FORWARD CARGO SMOKE WARNING FOLLOWED BY FIRST CLASS LAV SMOKE DETECTOR SOUNDING. PILOT AND FIRST OFFICER BOTH SMELLED EXHAUST/OIL. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT. NO EVIDENCE OF FIRE FO UND. CARGO SMOKE CONTROL PANEL REPLACED, FIRST CLASS LAV SMOKE DETECTOR AND WATER SEPARATORS REPLACED. ENGINE NR 1 REM OVED AND REPLACED ON THE FOLLOWING DAY SEE LOGS 4345641 AND 4345644. 2 L 7 2 4F 4 F A6WE E2EA 2008032700341 20080327 00341 NM 2008 3 27 HALA0800429 1 20080324 A 2425 WARNING SYSTEM BOEING 767 7673CB 1385187 NM PWA 4060 PW4060 52119 NE COCKPIT MALFUNCTIONED A HALA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 592HA 33468 ETOPS SIGNIFICANT SYSTEM, IMMEDIATELY AFTER ENGINE START. EICAS MSG "L GEN OFF" DISPLAYED. L GEN OFF LT ILLUMINATED. CONDITION RETURNED TO NORMAL AFTER GEN SW RESET. ACCOMPLISHED FIM 24-20-00 FIG 101. NO DEFECTS NOTED. RAN NR 1 ENGINE ON GND, LT GENERATOR CAME ON LINE. PUT LOAD ON LT GENERATOR, OPS CHECK OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032700343 20080327 00343 NM 2008 3 27 HALA0800418 1 20080322 A 7603 ROD END BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE THRUST LEVER DAMAGED A HALA K NONE O OTHER CR CRUISE 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, ENG THRUST LEVERS MISALIGNED IN NORM MODE IN LEVEL FLT AT FL 390 WITH EPR'S MATCHED AT 1.37 AN D N1 AT 86.3, THRUST LEVERS SPLIT ONE FULL KNOB APART, R THRUST LEVER LAGS. CHECKED THRUST LEVERS AND RESOLVER ANGLES A LL OK. FOUND RT INPUT LEVER LOWER ROD END DAMAGED. AWAITING PARTS, MM 73-21-11 MM 76-11-00. REMOVED ROD END. INSTALL ED NEW ROD END. OPS CK GOOD PER AMM 76-11-00. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032700350 20080327 00350 2008 3 27 HALA0800424 4 20080322 A 3442 RADAR BOEING 767 76733A 1385209 NM WEATHER RADAR MALFUNCTIONED A HALA K NONE J WARNING INDICATION CR CRUISE 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM, WX FAIL DISPLAYED ON HSI WITH L/R SELECTED. TEST ATTEMPTED WITH NO RESULTS. REALIGNED IRUS. TESTED NR 1 AND NR 2 WXR PER M/M 34-43-00. BOTH SYSTEMS CHECK OK. 2 L 7 2 4F RT A1NM 2008032700353 20080327 00353 NM 2008 3 27 HALA0800427 1 20080317 A 5420 STRUCTURE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 1 NACELLE DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 NR 1 ENGINE I/B CORE COWL HAS VARIOUS DEFECTS ALONG THE BOTTOM STRUCTURE. BLENDED THE DAMAGE AREA IAW SRM 54-41-02, FIG 101. 2 L 7 2 4F 4 F RT A1NM E13NE 2008032700359 20080327 00359 NM 2008 3 27 AALA200800543 1 20080310 A 2742 6355B000103 ACTUATOR BOEING 737 737823 13844BZ NM HORIZ STAB INOPERATIVE A AALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 966AN 30094 MIA INFLIGHT T592/10MAR - BOTH CAPTAIN AND FIRST OFFICERS STABILIZER TRIM INOPERATIVE. RETURNED MIA AND LANDED WITHOUT INCIDENT. REPLACED HORIZONTAL STABILIZER TRIM ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008032700360 20080327 00360 NM 2008 3 27 AALA200800545 1 20080310 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 346AN 33085 JFK - EMERGENCY LIGHT AT RIGHT FORWARD OVERWING EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK M1209 FOR EMERGENCY LIGHT AT RIGHT FORWARD OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008032600277 20080326 00277 WP 2008 3 26 070188 1 20080317 A 2150 A/C PACK DOUG DC9 DC983 3022083 WP A/C BAY MALFUNCTIONED A WX0A K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 19 868GA 49554 DURING FLIGHT 582 BLI TO LAS, IT WAS REPORTED THAT SMOKE AND ODOR WAS ENTERING THE CABIN. THE FLIGHT CREW DETERMINED TH AT THE RIGHT AIR CONDITIONING PACK WAS CAUSING THE SMOKE AND ODOR. IT WAS TURN OFF AND THE CABIN CLEARED. UPON ARRIVAL IN LAS VEGAS, THE MAINTENANCE DEPARTMENT PERSONNEL PERFORMED BURNOUT PROCEDURE OF THE RIGHT AIR CONDITIONING SYSTEM IAW THE AMM 21-20-02. NO ABNORMAL ODORS OR SMOKE DETECTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008032600282 20080326 00282 NM 2008 3 26 08FDEA01070 1 20080320 A 5320 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 580FE 48471 MAIN DECK CARGO DOOR, LOWER JAMB FITTING FOUND NR 7 HOLE POSITION "C" "A", "B", ":D" CORRODED. COMPLIED WITH EA 1-5310 -112602 PART 1. FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 . 2 L 7 3 4F RT A22WE 2008032700005 20080327 00005 NM 2008 3 27 DHL2008746017 1 20080110 A 5322 SHEAR TIE BOEING 727 727223 1384074 NM BS 970 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 749DH 22013 DURING C CHECK, AFT PIT BS 970 SHEAR TIE CORROSION BETWEEN STRINGER 29L AND 28L. FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1 FIG 1, CUT OUT DAMAGE AREA DIMENSION 6.5" BY 1" IAW SRM 51-10-1, 53-10-1 FIG 1 AND 53-10-4 FIG 11. FABRICATED S HEAR TIE REPAIR IAW SRM 51-20-2 FIG 5 AND 51-30-5, 53-10-4 FIG 11. ALODINE AND PRIMER REPAIR PART IAW SRM 51-10-2. INS TALLED NEW SHEAR TIE IAW SRM 53-10-4 FIG 11 ON SHEAR TIE. 2 L 7 3 4F A3WE 2008032700022 20080327 00022 NM 2008 3 27 DHL2008765002 1 20080119 A 5320 WEB BOEING 727 727264 138408M NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, CUT OUT DAMAGED AREA AFT STAIRWELL LIGHTENING HOLE 10 O'CLOCK POSITION DIMENSION CUT OUT 1.5" BY .75" IA W SRM 51-40-2 FIG 1. FABRICATED DOUBLER REPAIR AT AFT STAIRWELL LIGHTNING HOLES 10 O'CLOCK POSITION IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. TREATED AND PRIMED PARTS AND AREA IAW SRM 51-10-2. INSTALLED DOUBLER REPAIR IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008032700035 20080327 00035 NM 2008 3 27 2008UALA01422 1 20080313 A 3510 MF20010 OXYGEN MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 829UA 1211 F/O O2 MASK INOP. REPLACED F/O O2 MASK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032700050 20080327 00050 NM 2008 3 27 DHL2008765014 1 20080121 A 5753 STRUCTURE BOEING 727 727264 138408M NM RT WING TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK: DISCREPANCY - RIGHT WING INBOARD FLAP, MID FLAP AFT IS CRACKED ON BOTH INBOARD AND OUTBOARD SIDE WBL 90. 69 AND WBL 104.0. REMOVED NR 5 AND 6 TEAR DROP FAIRINGS AND RIGHT INBOARD MID FLAP LOWER SKIN TO GAIN ACCESS IAW SRM 51 -30-2. REMOVED CRACKED SECTION IAW SRM 51-30-2. FABRICATED NEW SECTION IAW SRM 51-30-5 AND 57-50-2 FIG 5. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW SECTION IAW SRM 51-30-2. INSTALLED RT INBOARD MID FLAP LOWER SKIN AND NR 5 AND 6 TEAR DROP IAW SRM 51-30-2. OPS CHECK GOOD IAW MM 27-51-00. 2 L 7 3 4F A3WE 2008032700059 20080327 00059 NM 2008 3 27 DHL2008765009 1 20080129 A 5311 FRAME BOEING 727 727264 138408M NM BS 480 DAMAGED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 765AT 23014 DURING C CHECK, 2 MISDRILLED HOLES IN FUSELAGE FRAME STRINGER 18L BS 480. REMOVED AND REINSTALLED HINGE ASSEMBLY AT FRA ME, STRINGER 18 BS 480 IAW STC DRAWING 727021025-1, DRILLED THROUGH THE TWO HOLES AND INSTALLED MS20426AD6-6 RIVET FLUSH IAW DRAWING NR 727021028 REV F, IAW DE-N765AT 1-25-08 AND ASTAR EVA B253-00043. 2 L 7 3 4F A3WE 2008032700089 20080327 00089 WP 2008 3 27 08FDEA01084 1 20080320 A 5311 ADA007313 FRAME DOUG MD10 MD1010F 3022112 WP BS 899 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 FWD LOWER CARGO BILGE J-CHANNEL IS CORRODED AT BS 899 BETWEEN STR 51L AND STR 51R. REMOVED CORROSION FROM THE LOWER FRA ME CAP (J CHANNEL) IAW SRM 51-21-01 VOL II PG 28 & FOUND MATERIAL LOSS EXCEEDED ALLOWABLE LIMITS. ORIGINAL THICKNESS 0. 071, MATERIAL REMAINING 0.054 IAW SRM 53-00-01 VOL I FIG 1A. REPAIRED LOWER FRAME CAP IAW SRM 53-30-00 VOL I FIG 5 & DAM AGED SHEAR TIE SECTION IAW SRM 53-30-00 VOL I FIG 10. 2 L 7 3 4F RT A22WE 2008032700108 20080327 00108 SO 2008 3 27 SIMA200808112 1 20080313 A 5320 14521718007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 629AE 19976 5000 145130 DURING MBV INSPECTION, THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED AND REPLACED WITH NEW PART IAW SRM 5 3-00-10, 53-20-03, 51-21-04 AND 51-21-05. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032700109 20080327 00109 EA 2008 3 27 MASA200800243 1 20080319 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A MASA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 07 17358 7358 ASH FLT MFR-LAS, CREW REPORTED FLAPS FAIL CAUTION OCCURRED ON APPROACH AT ZERO DEGREES WHEN SELECTED TO 8 DEGREES. MX C OMPLIED WITH THE FLAPS FAIL PART A PROCEDURE AND FECU INTERROGATION. 2 L 7 2 4F RT A21EA 2008032700110 20080327 00110 SO 2008 3 27 SIMA200808113 1 20080316 A 5320 14522178005 SILL EMB 145 EMB145LR 3260212 SO SERVICE DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 683AE 9364 5000 14500833 DURING A IMBV INSPECTION, THE SERVICE DOOR CUT OUT LOWER CENTER SILL WAS FOUND CORRODED. BLENDED CORRODED AREAS TREATED AND NDT. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032700150 20080327 00150 EA 2008 3 27 MASA200800256 1 20080322 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 77331 16374 7331 ASH 7392 ORD-MDT, NOSE GEAR DISAGREE ON TAKEOFF AND GEAR WAS SLOW TO EXTEND. REMOVED AND REPLACED NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2008032700161 20080327 00161 SW 2008 3 27 WGEA200800048 1 20080313 A 2750 FLAP SYSTEM ECLIPS EA500 ECLIPSEEA500 3350000 SW TE FLAPS OUT OF ADJUST E WGEA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 EA 27 142DJ 000056 AIRCRAFT REQUIRES 12 PERCENT LWD WITH 7 PERCENT RUDDER AT 160 KTS, 88 PERCENT LWD WITH 0 PERCENT RUDDER AT 160 KTS. REF ERENCE DAYJET WORK ORDER 1600, NR-00001. TEMPORARILY INSTALLED 2 EACH GURNEY TABS ON THE RT WING FLAP IAW SEM 500-0096 REVISION B DATED 3/20/2008. UPON COMPLETION OF TEST FLIGHT, IF PROBLEM IS CORRECTED, RETURN AIRCRAFT TO GNV SERVICE CEN TER FOR PERMANENT ATTACHMENT OF GURNEY TABS IAW SEM 500-0096 REVISION B DATED MARCH 20, 2008. REFERENCE LOGBOOK PAGE 09 02, ITEM 1. EVALUATION FLT COMPLETED, DATA FORWARDED TO MAINTENANCE ENGINEERING FOR REVIEW. REFERENCE WORK ORDER 1676, NR-00001. INSTALLED 2 GURNEY TABS ON RIGHT OUTBOARD FLAP TRAILING EDGE IAW SEM 500-0096 REVISION B. 1 L 7 2 4J RT A00002AC 2008032700175 20080327 00175 NM 2008 3 27 F3LA200800131 1 20080319 A 5321 D5367424200000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 937FR 5516 2400 DURING C2 C CHECK, INSPECTION REPORTED A HOLE WAS PUNCTURED INTO THE UPPER SKIN OF AFT CARGO PIT FLOOR PANEL 151VG, NEAR THE FORWARD EDGE, IN THE CENTER. MAINTENANCE REMOVED AND REPLACED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-42-14 PB 401. UPON COMPLETION OF THE INSTALLATION OF THE NEW PANEL, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008032700178 20080327 00178 NM 2008 3 27 2008UALA01411 1 20080313 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FUSELAGE STRINGER 10L AUXILARY INTERCOSTAL IS CRACKED BS 303.5. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED 2 CL IPS, 2 ANGLES, 1 H-STRAP & 1 FRAME DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700224 20080327 00224 NM 2008 3 27 08FDEA01117 1 20080323 A 5311 ACA73511 FRAME DOUG MD11 MD11F 3023600 NM BS 535 S23-24L CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 522FE 48476 MAIN DECK LT FRAME AT STATION 535 , BETWEEN L23-24L, 1 CHAFED MARK FOUND. REPAIRED AS PER DRAWING SRZ-53-503. REPAIR C LASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032700232 20080327 00232 NM 2008 3 27 2008UALA01489 1 20080316 A 3350 78941 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 664UA 29236 SEAT 1H EEL LIGHT BROKEN. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032700246 20080327 00246 EU 2008 3 27 08FDEA01132 1 20080324 A 5320 A5377832900000 WEB AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FWD LOWER CARGO COMPARTMENT/CORROSION ON WEB BETWEEN FRAMES 34 AND 35 RT UNDER ROLLER TRACK AT RBL 56 ABOVE STRINGER 44. WEB AT FRAME 34-35 RT REPLACED IAW SRM 51-72-10. DWG. 14A53778329 ISSUE N & SRM 53-14-18. 2 L 7 2 4F RT A35EU 2008032700247 20080327 00247 2008 3 27 2008UALA01496 4 20080317 A 2565 3A2704 FITTING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SLIDE BOTTLE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 122UA 29168 LOW BOTTLE. FOUND LEAKING AT TUBE ASSEMBLY FLARE FITTING. TIGHTENED FITTING AND SERVICED BOTTLE TO FULL. AC OK FOR SERVI CE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032700270 20080327 00270 NM 2008 3 27 AALA200800503 1 20080304 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 675AN 29425 DFW - EMERGENCY LIGHT AT RIGHT AFT LAVATORY DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008032700275 20080327 00275 NM 2008 3 27 AALA200800508 1 20080305 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT AT SEAT 20C HAS MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008030700110 20080307 00110 CE 2008 3 7 BSYA20080003 1 20080115 A 3710 442CW12 PUMP BEECH 58 58 1152740 CE RT ENGINE FAILED E BSYA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 3695V TH1183 AFTER TAKEOFF OUT OF BDL LOST RIGHT VAC PUMP, RETURNED TO BDL. MAINTENANCE CHANGED RIGHT VAC PUMP, OPS CHECKS GOOD. 1 L 7 2 3O 3A16 2008030700114 20080307 00114 SO 2008 3 7 C2XA08IA064 1 20080222 A 3230 8005701 PROXIMITY SWITCH EMB 145 EMB145XR 3260214 SO NLG FAULTY A C2XA O OTHER O OTHER AP APPROACH 1 SW 27 13123 145688 IAH - FLIGHT 2945 - THE CREW REPORTED A DISTINCT THUMPING SOUND ON APPROACH WITH THE GEAR UP AND DOWN ON FINAL. THE AIR CRAFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NLG DOWNLOCK PROX SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008030700117 20080307 00117 NM 2008 3 7 NWAA080726311 1 20080226 A 2530 OVEN BOEING 747 747451 1384940 NM GALLEY SMOKE A NWAA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 671US 26477 DURING FLIGHT, FLIGHT ATTENDANT REPORTED THAT OVEN NR 1, IN GALLEY NR 2 HAD SMOKE COMING FROM UPPER RT OF SEAL. FIRE EX TINGUISHER WAS USED (REFERENCE LOG PAGE 2810194). FLIGHT CONTINUED ON, AND LANDING WAS UNEVENTFUL. MAINTENANCE FOUND O VEN CONTROL C/B POPPED. REMOVED AND REPLACED OVEN, OVEN CONTROLLER, RELAY, AND CHECKED WIRING. OPERATIONAL CHECKED GOO D, AND A/C WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008030700118 20080307 00118 NM 2008 3 7 2008UALA00843 1 20080215 A 3350 AML76C10T01P003 COVER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LIGHT SWITCH OUT OF ADJUST A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHTS COME ON INTERMITTENTLY. ADJUSTED COVER ON SWITCH. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700139 20080307 00139 SO 2008 3 7 SIMA200806002 1 20080219 A 5320 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 679AE 9357 5000 14500814 DURING A IMBV INSP, THE LT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. REPAIR, PERFORMED A CUTOUT OF BEAM, PREPARED A DO UBLER, FILLER AND TWO SHIMS. CLEANED AND TREATED REPAIR PARTS AND INSTALLED. REPAIR DONE IAW EMBRAER 145 SRM (SRM EMB 145/1142 REV. 39) CHAPTER 53-00-10. 2 L 7 2 4T RT T00011AT 2008030700147 20080307 00147 NM 2008 3 7 2008UALA00926 1 20080219 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY LIGHT ROW 1J INOP. RESECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008033100047 20080331 00047 WP 2008 3 31 UPS08851939 1 20080228 A 5711 FITTING DOUG DC8 DC873F 302199F WP SPAR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 NR 4 ALT THRU 560A BETWEEN XRS 428 AND XRS 463 STRINGER TO FRONT SPAR FITTING CRACKED. FABRICATED AN D INSTALLED FRONT SPAR FITTING IN NR 4 ALT XRS 428 TO XRS 463 IAW DWG 3644046 AND SRM 51-1-8 AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 2008033100050 20080331 00050 WP 2008 3 31 UPS08851877 1 20080316 A 5350 SKIN DOUG DC8 DC873F 302199F WP TAILCONE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 INSPECTION TYPE:N/A CRACK AND CORROSION ON TAIL CONE UPPER SURFACE. C/O DAMAGE AND RADIUSED 4 EA CORNERS. DAMAGE REMOV ED. FABRICATED PARTS FILLER & DOUBLER, OK TO INSTALL PER QC. INSTALLED REPAIR. ITEM 371453 ASSIGNED FOR 6000 CYCLES PER DC8 SRM 53-02-01-0. 2 L 7 4 4F RT 4A25 2008033100058 20080331 00058 NM 2008 3 31 KNNA20080004 1 20080324 A 5230 HANDLE BOEING 737 7372L9 1384497 NM CARGO DOOR UNSECURE A KNNA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 25 737Q 21528 ACCORDING TO CAPTAIN'S REPORT, THEY DEPARTED ON RUNWAY 10 WITH FLAPS 5 DEGREES FOR IMPROVED PERFORMANCE AND UNPRESSURIZE D DUE TO DEFERRED APU. AT 2,000 FT AND 210 KM/H, ENGINE BLEEDS UTILIZED FOR PRESSURIZATION. PERFORMED CLIMBING RIGHT T URN TO CROSS VALENCIA VOR WHILE CLIMBING TO 10,000 FT. DURING CLIMB OUT AT 7,000 FT, RECEIVED MASTER/CAUTION WITH ASSOC IATED AFT CARGO DOOR INDICATION. CABIN PRESSURIZATION LOST. PERFORMED DOOR ANNUNCIATOR ILLUMINATED CHECKLIST. RETURNE D TO LANDING RUNWAY 10, SMOOTH LANDING. POST FLIGHT INSPECTION REVEALED IMPROPERLY SECURED AFT CARGO DOOR HANDLE. MAIN TENANCE FOUND PROXIMITY SENSOR AND ALSO HOLD CLOSE SPRING OUT OF ADJUSTMENT. 2 L 7 2 4F RT A16WE 2008033100091 20080331 00091 NM 2008 3 31 AMTA200800173 1 20080228 A 5730 SKIN PANEL BOEING 737 73783N 13844HI NM LT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LT WING FUEL TANK ACCESS 532GB HAS PITTING CORROSION ON LWR SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORRIOSI ON ON LWR FUEL TANK ACCESS LANDING 532GB IAW SRM 51-10-02-0G, ROG MAT .202, MAT LOSS .002, REM MAT .200, FOUND TO BE WIT NIN LIMITS IAW SRM 57-20-01-1A-1, PERFORMED FLAP PEENING IAW SRM 51-20-06 AND SOPM. (K) 2 L 7 2 4F RT A16WE 2008033100101 20080331 00101 NM 2008 3 31 08FDEA01152 1 20080326 A 5330 65561251 SKIN BOEING 727 727225 1384077 NM BS 1050-1054 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 DENT RT AFT FUSELAGE STA 1050 STR 23R (DENT FOUND OUT OF LIMITS). CUT OUT DAMAGED AREA IAW SRM 53-30-1 FIG1. FABRICATED REPAIR DOUBLER TREATED AND PRIMED REPAIR PART AND AREA IAW SRM 51-10-2. INSTALLED DOUBLER IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008033100103 20080331 00103 WP 2008 3 31 08FDEA01154 1 20080326 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 STABILIZER JACKSCREW COMPARTMENT DOOR CUTOUT FOR PANEL 311 AB BETWEEN STA 2007 AND 2033 INNER SURFACE OF THE SKIN IS WOR N FROM FRETTING ON THE DOOR LATCHES (4) PLACES LEFT AND RIGHT SIDES. COMPLIED WITH EA 8-5330-116971. 2 L 7 3 4F RT A22WE 2008033100147 20080331 00147 NM 2008 3 31 AMTA200800211 1 20080306 A 4920 RELAY BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE APU INOPERATIVE A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 518AT 27974 APU WILL NOT START. T/S AND FOUND BAD RELAY K10163, REMOVED AND REPLACED IAW SWPM 20-81-82, APU START AND OPS CHECK GOO D IAW MM 49-11-00. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008033100153 20080331 00153 WP 2008 3 31 AMTA200800217 1 20080310 A 5520 TRUSS LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE ELEVATOR DAMAGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 164AT 1238 ELEVATOR ASSY-INSPECTION/ REPAIR OF TRUSS RUB STRUCTURE. COMPLY WITH EO L10-55AD-1793. REPAIRED TRUSS RIB IAW EO L10-5 5AD-1793. REPAIRED TRUSS RIB IAW EO L10-55AD-1793, SECTION III. (K) 2 L 7 3 4F 4 F A23WE E12EU 2008033100155 20080331 00155 NM 2008 3 31 AMTA200800218 1 20080311 A 5320 FLOOR SUPPORT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 330-365 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 520AT 27976 UPPER SURFACE CORROSION ON CHANNEL UNDER FLOORBOARD 221DF AND 222CF AT BL0 BS 330 TO BS 365. (82567). REMOVED CORROSION AT BS 330 TO BS 365 ON THE UPPER SURFACE OF CHANNEL IAW SRM 51-10-02. FOUND STA AT BS 345 OUT OF LIMITS. ALL OTHER AR EAS WITHIN LIMITS. OTHER MATER THK .063 MATL LOSS AT .015. REPAIRED IAW SAA EA 757-5311-09-A1303. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008033100156 20080331 00156 WP 2008 3 31 AMTA200800221 1 20080312 A 3350 FUSE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2B 30018 NE EMERGENCY LIGHTS BLOWN A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 701TZ 46583 EMERGENCY EGRESS LIGHTING INOPERATIVE, ROWS 21-29, BOTH SIDES. T/S IAW TAFI 33-50-00. CMM 33-21-70. FOUND FUSE BLOWN, EMERGENCY LIGHT PACK. REPLACED FUSE IAW CMM 33-21-70. EMERGENCY LIGHTS OPS CK GOOD IAW 33-51-01. 2 L 7 3 4F 4 F A22WE E23EA 2008033100157 20080331 00157 NM 2008 3 31 AMTA200800222 1 20080313 A 3350 LENS BOEING 737 73783N 13844HI NM EMERGENCY LIGHTS DISTORTED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 305TZ 30706 LT AFT ENTRY DOOR EGRESS LENS UNREADABLE. REMOVED AND REPLACED LENS ASSY. REQ`D OPS CK NORMAL. (K) 2 L 7 2 4F RT A16WE 2008033100158 20080331 00158 NM 2008 3 31 AMTA200800223 1 20080312 A 3350 D71701100 BATTERY BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHTS UNSERVICEABLE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 550TZ 32584 EGRESS LIGHTS INOPERATIVE AT LT EMERGENCY EXIT JUST AFT OF WING-LIGHTS INOP ARE SIDEWALL AFT, SLIDE LIGHT ON FUSELAGE BE LLY, WHITE LIGHT BETWEEN LAVS, JUST FWD OF DOOR AND CROWN EXIT NEXT TO DOOR. REMOVED AND REPLACED BATTERY PACK GROUND C KD NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008033100163 20080331 00163 EA 2008 3 31 SWIA200819385 1 20080319 A 2842 SENSOR CNDAIR CL600 CL6002B19 1900309 EA LT FUEL TANK FAULTY A SWIA O OTHER K FLUID LOSS UK UNKNOWN 1 NM 07 471CA 7655 FUEL LEAKING FROM LEFT MAIN TANK RELIEF VALVE. REPLACED LEFT HIGH-LEVEL SENSOR IAW AMM 28-25-13. OPS AND LEAK CHECK GO OD. 2 L 7 2 4F RT A21EA 2008033100165 20080331 00165 EA 2008 3 31 SWIA200819386 1 20080320 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA CABIN FAULTY A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 984CA 7171 FLT 2871 - EMERGENCY LIGHTS CYCLE ON AND OFF DURING FLIGHT. REPLACED NR 4 BATTERY PACK AND CHARGER IAW AMM 33-51-04. O PS CHECK GOOD, PN AD-2013-1A SN/OFF 66453. 2 L 7 2 4F RT A21EA 2008033100166 20080331 00166 2008 3 31 AMTA200800228 4 20080316 A 3422 BATTERY BOEING 737 73783N 13844HI NM ISFD UNSECURE A AMTA O OTHER O OTHER LD LANDING 1 GL 11 310TZ 28243 ISFD WENT BLACK WITH NOSE WHEEL TOUCHDOWN. FOUND ISFD BATTERY NOT SEATED IN RACK. SECURED ISFD BATTERY. OPS TEST IAW FIM 34-24-00-810-804. OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2008033100168 20080331 00168 2008 3 31 AMTA200800230 4 20080316 A 3422 CHARGER BOEING 737 73783N 13844HI NM ISFD FAULTY A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 310TZ 28243 ISFD BATTERY FAULT LIGHT ON. REMOVED AND REPLACED ISFD BATTERY CHARGER OPS CHECK GOOD NO FAULT LIGHT. (K) 2 L 7 2 4F RT A16WE 2008033100183 20080331 00183 EA 2008 3 31 SWIA200819392 1 20080318 A 3260 BRACKET CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 978SW 7953 FLT 6384 - RECEIVED A "GEAR DISAGREE" WARNING MESSAGE AND NOSE GEAR DID NOT RETRACT. ADJUSTED THE NOSE WHEEL WEIGHT OFF WHEELS SENSOR BRACKET. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008033100188 20080331 00188 EA 2008 3 31 SWIA200819395 1 20080325 A 2621 8990741 EXTINGUISHER CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE DISCHARGED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 909SW 16954 4660 7558 RIGHT ENGINE FIRE BOTTLE DISCHARGED. REPLACED FIRE BOTTLE IAW CRJ 200 MM 26-21-07. 2 L 7 2 4F RT A21EA 2008033100190 20080331 00190 SO 2008 3 31 SWIA200819397 1 20080324 A 2611 BATTERY EMB 120 EMB120ER 3260203 SO SMOKE DETECTOR FAULTY A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 218SW 120287 FLT 5474 - LAV SMOKE DETECTOR ACTIVATED INFLIGHT. REPLACED LAV SMOKE DETECTOR BATTERY. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008033100191 20080331 00191 NM 2008 3 31 AALA200800593 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LEFT NUMBER ONE D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008033100197 20080331 00197 WP 2008 3 31 AALA200800599 1 20080311 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70524 49916 LGA - EMERGENCY LIGHT AT RIGHT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT OVERWING E XIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008033100199 20080331 00199 NM 2008 3 31 AALA200800592 1 20080311 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 MIA - EMERGENCY LIGHTS AT RIGHT SEAT ROWS 37 TO 45 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT SEA T ROWS 37 TO 45. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008033100200 20080331 00200 NM 2008 3 31 AALA200800591 1 20080311 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 MIA - EMERGENCY LIGHTS AT LEFT SEAT ROWS 37 TO 45 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT SEAT ROWS 37 TO 45. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008033100204 20080331 00204 NM 2008 3 31 DHL2008763525 1 20080304 A 5313 STRINGER SPLICE BOEING 727 727264 138408M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 AFT CARGO COMP AT BS 1010, STR 29R SPLICE CORRODED O/B SIDE. REMOVED, FABRICATED NEW SPLICE FROM BAC1498-131, 15" LONG, PO NR 9005686, AND INSTALLED PER B727 SRM 53-10-2 FIG 9, 53-10-3 FIG 1, AND 51-30-2. 2 L 7 3 4F A3WE 2008032700289 20080327 00289 WP 2008 3 27 AALA200800518 1 20080305 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 289AA 49301 MSP EMERGENCY LIGHT AT SEAT 12D HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008032700293 20080327 00293 WP 2008 3 27 AALA200800521 1 20080305 A 2731 79237991 MOTOR DOUG DC9 DC983 3022083 WP STAB TRIM INOPERATIVE A AALA O OTHER O OTHER AP APPROACH 1 SW 21 9616G 53563 DFW INFLIGHT T1360 - ON FINAL APPROACH CREW REPORTED NO RESPONSE FROM STABILIZER IN PRIMARY OR ALTERNATE. LANDED DFW WI THOUT INCIDENT. REPLACED PRIMARY AND ALTERNATE STABILIZER TRIM MOTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008032700313 20080327 00313 WP 2008 3 27 NWAA081099759 1 20080319 A 3350 FUSE DOUG DC9 DC941 302207N WP EMERGENCY LIGHT FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 759NW 47287 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAI LED. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY FUSE. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4F A6WE 2008032700320 20080327 00320 SO 2008 3 27 C2XA08ON104 1 20080313 A 7334 M832482912 O-RING EMB 145 EMB145LR 3260212 SO FUEL SYSTEM WORN A C2XA K NONE K FLUID LOSS UK UNKNOWN 1 SW 27 18556 13971 13971 145595 FLT 0060 - TUS - FLIGHT CREW REPORTED E2 FUEL IMPENDING BYPASS MSG ON EICAS/ E2 FUEL LEAK. MX PERSONNEL FROM IAH REMOVE D AND REPLACED O-RINGS FOR THE ELECTRICAL IMPENDING BYPASS SWITCH OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELE ASED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008032700326 20080327 00326 WP 2008 3 27 NWAA081129865 1 20080323 A 3350 LIGHT DOUG DC9 DC951 3022051 WP EXTERIOR MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 774NC 47776 DURING LINE CHECK, MAINTENANCE FOUND THAT THE RIGHT SIDE EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. THE POWER SUPP LY WAS INITIALLY REPLACED BUT THAT DID NOT CORRECT THE DISCREPANCY. SYSTEM WAS PLACED ON MEL 33-20. LATER, MAINTENANCE WAS UNABLE TO DUPLICATE ORIGINAL FAULT AND FOUND RIGHT HAND EXTERIOR FLOOD LIGHT OPERATED NORMALLY. MEL WAS REMOVED AN D THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008032700340 20080327 00340 2008 3 27 HALA0800419 4 20080321 A 3460 COMPUTER BOEING 767 7673CB 1385187 NM COCKPIT MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 588HA 33466 ETOPS SIGNIFICANT SYSTEM, CO PILOTS FMS COMPUTER INOP. PULLED C/B ON FMS COMPUTER RESET C/B FMS COMPUTER SYNC WITH OTHE R COMPUTER. CHECKS OK PER MM 34-61-01-424-05. 2 L 7 2 4F RT A1NM 2008032700347 20080327 00347 NM 2008 3 27 HALA0800421 1 20080323 A 2710 WARNING SYSTEM BOEING 767 76733A 1385209 NM AILERON SYSTEM MALFUNCTIONED A HALA K NONE N FALSE WARNING CR CRUISE 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, AILERON LOCKOUT LIGHT ILLUM. AT LOW SPEED EICAS "AILERON LOCKOUT" DISPLAYED. TEMPORARY CONDI TION LIGHT ON AT 13,000' AND 250KT. STAYED ON 30SEC TO 1 MIN. PERFORMED FIM 27-11-00, NO FAULTS NOTED, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008032700357 20080327 00357 WP 2008 3 27 AALA200800533 1 20080309 A 3350 SHROUD DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 DFW EMERGENCY LIGHT AT SEAT 28D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008032700363 20080327 00363 NM 2008 3 27 AALA20800544 1 20080310 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 346AN 33085 JFK - EMERGENCY LIGHT AT LEFT FORWARD OVERWING EXIT DOOR INOPERATIVE. REPLACED BATTERY PACK M732 FOR EMERGENCY LIGHT AT LEFT FORWARD OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008032700367 20080327 00367 NM 2008 3 27 AALA200800567 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT SEAT 40G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 40G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700371 20080327 00371 NM 2008 3 27 AALA200800555 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700373 20080327 00373 NM 2008 3 27 AALA200800564 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT SEAT 39C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 39C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700377 20080327 00377 NM 2008 3 27 AALA200800558 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700380 20080327 00380 NM 2008 3 27 AALA200800562 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT SEAT 30C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 30C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700383 20080327 00383 NM 2008 3 27 AALA200800550 1 20080310 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 929AN 30078 MIA - EMERGENCY LIGHT AT OVERHEAD SEAT 5E INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008032700385 20080327 00385 NM 2008 3 27 AALA200800542 1 20080310 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 796AN 30796 MIA - EMERGENCY LIGHT AT SEAT 29G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 29G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700400 20080327 00400 NM 2008 3 27 AALA200800574 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700403 20080327 00403 NM 2008 3 27 AALA200800577 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 31C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800009 20080328 00009 NM 2008 3 28 AALA200800586 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 38G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 38G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800010 20080328 00010 NM 2008 3 28 AALA200800587 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 34G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 34G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800012 20080328 00012 NM 2008 3 28 AALA200800589 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 26G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800015 20080328 00015 NM 2008 3 28 AALA200800539 1 20080310 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 784AN 29588 MIA - EMERGENCY LIGHT AT SEAT 34G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 34G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800016 20080328 00016 NM 2008 3 28 AALA200800552 1 20080310 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 929AN 30078 MIA - EMERGENCY LIGHT AT OVERHEAD SEAT 26D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008032800019 20080328 00019 NM 2008 3 28 AALA200800538 1 20080310 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 784AN 29588 MIA - EMERGENCY LIGHT AT SEAT 33C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 33C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800024 20080328 00024 EA 2008 3 28 A6WA200840106 1 20080217 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 430AW 7719 AT FS 589 WL 73.5 CARGO SILL BESIDE RIVET CRACKED. REPAIRED CARGO SILL IAW REO 601R-53-61-43. (M) 2 L 7 2 4F RT A21EA 2008032800026 20080328 00026 EA 2008 3 28 A6WA200840109 1 20080214 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 430AW 7719 PILOTS BULKHEAD FS 280 LBL 9 FOUND CRACKED. BULKHEAD REPAIR CARRIED OUT IAW REO 601R-53-11-171 REV D. (M) 2 L 7 2 4F RT A21EA 2008032800030 20080328 00030 WP 2008 3 28 IXXA08SMN038S 1 20080201 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND EXTERNAL DOUBLER RIGHT FORWARD FUSELAGE FORWARD OF B-PIT DOOR HAS IMPROPER REPA IR AT STATION FS 466, LONGERON 25.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. RE MOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND AFTER INSPECTION. FABRICATED REPAIR DOUBLE R, TRIPLER, FILLER SKIN, INTERNAL FINGER DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FAST ENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08086 DATED 02-27-08, SEMAN DRAWING ED-4701 DATED 02-05-08, DC8 SRM 51 -1-21, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND 51-3-1. 2 L 7 4 4F RT 4A25 2008032800034 20080328 00034 EA 2008 3 28 A6WA200840114 1 20080214 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 430AW 7719 CARGO DOOR PLATE FOUND CRACKED. REPLACED CARGO DOOR PLATE IAW SRM 51-41-02. (M) 2 L 7 2 4F RT A21EA 2008032800035 20080328 00035 EA 2008 3 28 A6WA200840115 1 20080216 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 430AW 7719 AT INTERCOSTAL FS 484 RBL 27 AND 36, OUTBOARD AND INBOARD ANGLE CRACK. INTERCOSTAL REPAIRED IAW SRM 51-42-21 AND REO 60 1R-53-41-059 REV A. (M) 2 L 7 2 4F RT A21EA 2008032800036 20080328 00036 SO 2008 3 28 C2XA08SH048 1 20080318 A 5320 14525480003 THRESHOLD EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14173 14500872 SHV - DURING C-CHECK IT WAS FOUND THAT THE CARGO DOOR THRESHOLD WAS CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED THRESHOLD IAW EMB 145XR SRM 51-40-02 AND CONTINENTAL EXPRESS EC 5320-01137. THE AIRCRAFT WAS APP ROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008032800040 20080328 00040 SO 2008 3 28 C2XA08IA083 1 20080310 A 3350 7287577505 SIGN EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12175 14500878 MCI - DURING MAINTENANCE INSPECTION THE EMERGENCY SIGN FORWARD OF SEAT 3BC WAS FOUND TO BE INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008032800047 20080328 00047 NM 2008 3 28 SWAA081521 1 20080319 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 942, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008033100206 20080331 00206 WP 2008 3 31 08FDEA01144 1 20080325 A 5512 ALC739282 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 300 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT HORIZONTAL STABILIZER PANEL NR 346 BB IS GOUGED AND HAS CORROSION. REMOVED AND REPLACED RUB STRIP SKIN IAW SRM 51- 31-01 VOL II PG 1. 2 L 7 3 4F RT A22WE 2008033100211 20080331 00211 NM 2008 3 31 DHL2008763530 1 20080324 A 5315 65175882 FLOORBEAM BOEING 727 727264 138408M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 EXFOLIATION FOUND ON FLT DECK FLOORBEAM UPPER CAP AT BS 266, BL 0. REMOVED AND REPLACED UPPER CHORD SECTION WITH P/N 65 -17588-2, PO NR 8109233, PER B727 SRM 51-30-5, 51-30-2, AND BAC DWG 65-17588 REV D. 2 L 7 3 4F A3WE 2008033100212 20080331 00212 NM 2008 3 31 QXEA200800307 1 20080313 A 5315 FLOORBEAM BOMBDR DHC8 DHC8402 1390042 NM BS 545 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - C4- CORROSION FOUND ON RT FLOOR SUPPORT FRAME CASTELLATION AT STA 545. REMOVED 5 RIVETS FROM CASTELLATION AND BLE NDED OUT CORROSION. REF CPM CHAPTER 4. HFEC INSPECTED BLEND AREA FOR CRACK IAW D-8 200 NDTM PART 6, 51-00-01, NO CRACK S NOTED. UT THICKNESS CHECK OF BLENDED AREA IAW NDTM PART 1, 51-00-04 HIGH .050 LOW .047. AREA OF BLEND WITHIN LIMITS AS PER SRM 51-20-11. APPLIED ETCH, ALODINE, AND PRIMER IAW SRM 51-20-16 AND 51-20-36. REINSTALLED RIVETS IN CASTELLATI ON REF SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008033100219 20080331 00219 WP 2008 3 31 DHL2008805530 1 20080303 A 5330 REPAIR DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 INSPECT PREVIOUS REPAIR AT STA 1690 - 1700 LONGERON 17L - 18L. ASSURE REPAIR WAS ACCOMPLISHED WITH APPROVED DATA. INDI CATE CATEGORY OF REPAIR AND REINSPECTION INTERVAL IF REQUIRED (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1,3. REMOVED EXISTING REPAIR NOT IN COMPLIANCE WITH SRM IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTIO N AND FABRICATED REPAIR DOUBLER (AL7075T6 0.063") (2EA) INTERNAL FINGER DOUBLER (AL7075T6 0.032") IAW SRM 53-2-1 FIG 7 S HEET 1,3 SRM 53-5-3 FIG 1 ITEM "E". CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAI R PARTS IAW SRM 53-2-1 FIG 7 SHEET 1-3, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE). THIS IS A CLASS 1 2 L 7 4 4F RT 4A25 2008033100221 20080331 00221 NM 2008 3 31 QXEA200800315 1 20080320 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX -C4- CORROSION ON ANGLE BY NUTPLATE HOLE AT STA X597.5 AND Y22.0 RT SIDE. DRILLED OUT NUTPLATE AND REMOVED CORROSIO N IAW CPCM CHAPTER 4. HFEC INSPECTED BLEND AREA FOR CRACKS IAW NDTM, PART 6, 51-00-01, NO CRACKS NOTED. UT THICKNESS C HECK OF BLENDED AREA IAW NDTM PART 1, 51-00-04 HIGH .080 LOW .074. AREA OF BLEND WITHIN LIMITS REF SRM 51-20-11. APPLI ED ETCH ALODINE AND PRIMER IAW SRM 51-20-16 AND 51-20-36. REINSTALLED NUTPLATE REF SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008033100223 20080331 00223 NM 2008 3 31 QXEA200800317 1 20080320 A 5230 FRAME DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX -C4- CORROSION ON AFT BAG DOOR CANTED FRAME JUST FWD OF THE LOWER AFT DOOR STOP (ON FUSELAGE) STA X580.5. REMOVED L IGHT SURFACE CORROSION BYBLEND MARKED AREAS, NOMINAL AMOUNT OF MATERIAL REMOVED, REF CPCM CHAPTER 4. HFEC INSPECTED BLE ND AREA FOR CRACKS IAW NDTM, PART 6, 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECK OF BLENDED AREA IAW NDTM PART 1, 51-0 0-04 HIGH .066 LOW .064. AREA OF BLEND WITHIN LIMITS REF SRM 51-20-11. APPLIED ETCH ALODINE AND PRIMER IAW SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2008033100227 20080331 00227 NM 2008 3 31 QXEA200800324 1 20080320 A 5414 SKIN DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX -C4- NR 1 NACELLE SKIN FWD MLG DOOR APERTURE INBD FWD CORNER HAS A 1/4" CRACK. REPAIRED IAW RD8-54-873. HFEC INSPE CTED BLEND AREA FOR CRACKS IAW NDTM, PART 6, 51-00-01, NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2008033100228 20080331 00228 NM 2008 3 31 QXEA200800326 1 20080320 A 5320 INTERCOSTAL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX -C4- CORROSION ON UNDERSIDE OF TOP FLANGE ON INTERCOSTAL BY NUTPLATE I/B END AT STA X591 AND Y11.0 JUST O/B OF LT I/ B SEAT TRACK. REMOVED 2 NUTPLATES AND REMOVED CORROSION IAW CPCM CHAPTER 4. HFEC INSPECTED BLEND AREA FOR CRACKS IAW N DTM PART 6, 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECK OF BLENDED AREA IAW NDTM PART 1, 51-00-04 HIGH .040 LOW .036. BLEND WITHIN LIMITS PER SRM 51-20-11. APPLIED ALODINE AND PRIMER IAW SRM 51-20-16 AND 51-20-36. INSTALLED TWO NUTPLA TES IAW SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008033100235 20080331 00235 WP 2008 3 31 DHL2008805511 1 20080318 A 5753 FLAP DOUG DC8 DC873F 302199F WP RT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 RT OUTBD FLAP L/E PLATING HOLES ELONGATED (STA XF 325.000 - 243.000). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-12-08, ASTAR EVA D857-00049 REV IR DATED 03-12-08, SEMAN DWG NR ED-4719 DATED 02-25-08. PERFORMED NDT INSP OF DAMAGE D AREA IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK NO CORROSION FOUND. ENCLOSED SMN FORM 242-2. FABRICATED EXTERNAL R EPAIR DOUBLER (AL2024T3 0.100") IAW SEMAN DWG ED-4719. PERFORMED NDT INSPECTED REPAIR DOUBLER IAW DC8 NDT SPM PART 06-1 0-01-001. NO CRACK NO CORROSION FOUND. ENCLOSED SMN FORM 242-2. CLEANED, TREATED AND PRIMED AREA AND EXT REPAIR DOUBL ER IAW SRM 51-1-8B. INSTALLED EXT REPAIR DOUBLER IAW SEMAN DWG NR ED-4719, SRM 51-1-11, SRM 51-1-21, SRM 51-3-0, SRM 51 2 L 7 4 4F RT 4A25 2008033100239 20080331 00239 WP 2008 3 31 DHL2008805524 1 20080312 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 AFT CARGO COMPT BILGE FITTING CRACKED 2" (STA 1160.000 - 1180.000, L-35L) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1- 8B. INSTALLED NEW FITTING IAW SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2008033100242 20080331 00242 WP 2008 3 31 DHL2008805510 1 20080228 A 5414 SKIN DOUG DC8 DC873F 302199F WP CFMINT CFM56 CFM563C 13802 EU NR 2 NACELLE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 NR 2 ENG NACELLE INLET COWL UPPER SKIN WORN, STA YN 147.334 AT 12 O'CLOCK POS. (MAJOR REPAIR). PERFORMED MAJOR REPAIR I AW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED SKIN (AL2024 T3 0.080") AND SPLICE (SHEET CRESS TYPE 17-7 PH) IAW SRM 71-5-2 FIG 2 SHEET 1, 2. HEAT TREATED SPLICE FROM 17-7- PH TO CRESS 17-7PH (H1050) IAW SRM 51-1-6. CLEANED,TREATED AND PRIMED AREA SKIN INNER IAW SRM 51-1-8B. INSTALLED REPAIR PART S IAW SRM 71-5-2 FIG 2 SHEET 1, 2, SRM 51-1-11, SRM 51-1-21, SRM 51-1-21A. 2 L 7 4 4F 4 F RT 4A25 E21EU 2008033100243 20080331 00243 WP 2008 3 31 DHL2008805536 1 20080324 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP CARGO BAY WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 UPPER CARGO COMPT NR 3 TRACK LUG WORN (STA 590.000 - 620.000) MAJOR REPAIR. CUT OUT TRACK SEGMENT AND FABRICATED (3EA) SPLICES (AL7075T6 0.100", 0.125" AND 0.160") IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA AND SPLIC ES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT (P/N S2772660) AND SPLICES IAW SRM 51-1-21,SRM 51-3-0, SRM 51-3-1 (TORQ UE). PERFORMED MAJOR REPAIR IAW SRM 53-2-3 PG 49-50 FIG 14. 2 L 7 4 4F RT 4A25 2008033100246 20080331 00246 WP 2008 3 31 DHL2008805505 1 20080302 A 5753 SKIN DOUG DC8 DC873F 302199F WP T/E FLAP DEFORMED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 RT OUTBD FLAP LOWER PLATING DEFORMED STA XF 399.000. PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 4 TR NR 57-94 DATED 10-0 1-02. REMOVED DEFORMED PANEL PLATING IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.025") AND BO NDED DOUBLER (AL2024T3 0.020") IAW SRM 57-7-1 FIG. 4, TR NR 57-94 ITEM "U" AND "Q". BONDED BOTH PARTS WITH HYSOL IAW SR M 51-1-9, TR NR 51-142, SRM 51-1-9A, TR NR 51-141. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF NEW PANEL PLATING IAW SRM 51-1-8B. INSTALLED NEW PANEL PLATING IAW SRM 51-1-11, SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2008033100252 20080331 00252 WP 2008 3 31 DHL2008805517 1 20080304 A 5320 ANGLE DOUG DC8 DC873F 302199F WP LT MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 31089 46125 LT MLG W/W CEILING ANGLE CRACKED 1.500" STA 857.000. REMOVED CRACKED ANGLE IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED N EW ANGLE (AL2024T6 0.071") IAW SRM 53-2-0 PG 1. CLEANED, TREATED AND PRIMED AREA AND ANGLE IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21 PG 1, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2008033100253 20080331 00253 WP 2008 3 31 DHL2008805518 1 20080226 A 5712 FRAME DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 RT FLAP WELL UPPER FORMER CRACKED 1" STA XW 5.000. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICAT ED ANGLE DOUBLER (AL2024T3 0.063") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 5 1-1-8B. INSTALLED ANGLE DOUBLER IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2008033100255 20080331 00255 WP 2008 3 31 DHL2008805500 1 20080310 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 FUSELAGE SKIN CORRODED AT STA 980.000 L-29R TO L-30R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 0 3-06-08, EVA D853-00045 REV IR DATED 02-22-08 SEMAN DWG ED-4711-1 DATED 02-14-08. REMOVED FASTENERS IAW SRM 51-1-20D, S RM 51-3-0. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SECTI ON IAW EVA D853-00045 REV IR. PERFORMED NDT INSP IAW EVA D853-00045, DPS 4.707-1. NEITHER CRACK NOR CORROSION FOUND. E NCLOSED SMN FORM 242-4. FABRICATED REPAIR DOUBLER (AL7075T6 0.050") REPAIR TRIPLER (AL7075T6 0.080") AND FILLER (AL7075 T6 0.125") IAW SEMAN DWG ED-4711-1. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAI 2 L 7 4 4F RT 4A25 2008033100256 20080331 00256 WP 2008 3 31 DHL2008805507 1 20080225 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 LT WING UPPER SKIN CRACK 1" STA XRS 74.000 S-9. PERFORMED MAJOR REPAIR IAW SRM 57-2-1- FIG 17 PG 87-88. REMOVED FASTEN ERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW SRM 57-2-1 FIG 17 PG 87-88. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND AFTER CUT OUT. ENCLOSED SMN FORM 242-2. FABRICATED REPAIR DOUBLER (AL 7075T6 0.0160") AND FILLER PLUG (AL7075T6 0.200") IAW SRM 57-2-1 FIG 17 PG 87-88, SRM 57-3-3 FIG 12 ITEM "A". TAPERED R EPAIR DOUBLER FROM 0.160" TO 0.080" IAW SRM 57-2-1 FIG 17 PG 87-88, SRM 51-10-0 PG 22 FIG 1. CLEANED AND APPLIED POLYUR ETHANE TOP YELLOW COATING TO AREA AND REPAIR PARTS IAW SRM 51-1-12 PG 7. INSTALLED REPAIR PARTS IAW SRM 57-2-1 FIG 17 P 2 L 7 4 4F RT 4A25 2008033100260 20080331 00260 WP 2008 3 31 DHL2008805508 1 20080223 A 5753 SKIN DOUG DC8 DC873F 302199F WP T/E FLAP BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 LT INBD FLAP UPPER SKIN BROKEN 0.500" AND HAS SIX DENTS (STA XW 71.000 - 91.000). PERFORMED MAJOR REPAIR IAW SRM 57-7-1 FIG 1. REMOVED DAMAGED PLATING IAW SRM 57-1-0 PG 1 AND SRM 51-1-21. FABRICATED NEW PLATING OF AL 2024-T3 0.040" IAW S RM 57-7-1 FIG 1 ITEM "D". CLEANED, TREATED AND PRIMED AREA AND NEW PLATING INTERNAL PART IAW SRM 51-1-8B. INSTALLED NE W PLATING IAW SRM 51-1-21, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2008032800104 20080328 00104 NE 2008 3 28 I5PA2008001 2 20080307 A 7261 LINE LINE BOEING 727 727212 138407G NM PWA JT8 JT8D17R 52049 NE NR 1 ENGINE BROKEN A I5PA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 WP 15 86425 21459 674583 AT FLIGHT LEVEL 30K FEET 263 NM OUT OF MAJURO, NR 1 OIL QUANTITY STARTED TO DECREASE FROM 4 GALLONS TO ZERO, CREW THEN S HUT DOWN ENGINE AND DESCENDED TO FL 26K FEET, RETURNED TO MAJURO. WINDMILLING OCCURRED FOR 43 MINUTES WITH OIL PRESSURE AT 17-18 PSI. ON INSPECTION FOUND NR 6 BEARING OIL PRESSURE LINE BROKEN. REPLACED LINE FULL POWER RUN NO LEAK, PERFOR M TEST HOP SYSTEM OIL NO LEAK, RELEASED AIRCRAFT FOR SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2008032800130 20080328 00130 WP 2008 3 28 UPS08851902 1 20080320 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW MM 33-50-01-2. OPS CHEC K OK. 2 L 7 4 4F RT 4A25 2008032800133 20080328 00133 NE 2008 3 28 UPS08851886 2 20080319 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE NR 4 MALFUNCTIONED A IPXA D RETURN TO BLOCK A FLAME/FIRE IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE:N/A BTB - NR 4 ENGINE TAIL PIPE FIRE; FUEL LEAK. REMOVED AND REPLACED NR 4 ENGINE PER TASK CARD 9071-2. 2 L 7 4 4F 4 F RT 4A25 E2GL 2008032800136 20080328 00136 NM 2008 3 28 UPS08M51911 1 20080207 A 5313 7150T61511 STRINGER DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 285UP 48457 INSPECTION TYPE:C CENTER ACCESSORY COMP STR 45L CORRODED AT FRAME FWD OF DOOR 131AB F/S1129/6-90. REPAIRED STRINGER 45L IAW MAINTENANCE MANUAL 52-31-00-02 PARA 2 TASK 52-31-00-00-801. 2 L 7 3 4F RT A22WE 2008032800166 20080328 00166 NM 2008 3 28 SWAA081594 1 20080325 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED MV4 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008032800173 20080328 00173 NM 2008 3 28 SWAA081610 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032800193 20080328 00193 NM 2008 3 28 SWAA081618 1 20080325 A 5311 65C22908 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008033100006 20080331 00006 NM 2008 3 31 QXEA200800302 1 20080313 A 5320 THRESHOLD BOMBDR DHC8 DHC8402 1390042 NM CARGO DOORWAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX -C4- THE MCD ENTRY THRESHOLD HAS CORROSION AT THE FASTENER LOCATIONS BETWEEN STA X1.0 TO X32.4 ON TOP AND BOTTOM SUR FACES. REMOVED THE MCD THRESHOLD, LOWER FWD AND AFT CORNER CASTINGS, THE LOWER SEAL RETAINER AND LOWER SILL PLATE. INS TALLED NEW LOWER SILL PLATE, FWD AND AFT CORNER LOWER SEAL RETAINER AND THE NEW THRESHOLD REF DHC-8(400) SRM 51-42-05 AN D 51-42-45. 2 H 7 2 4T RT A13NM 2008033100022 20080331 00022 WP 2008 3 31 08FDEA00985 1 20080317 A 5321 AGA38633 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 AFT PIT FLOOR PANEL NR 187 AF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL NR 187 AF; LOCATED HOLES; POTTED EDGES; COMPLETED CURE; SANDED EDGES AND INSTALLED INSERTS. FABRICATED TOP SHEET AND LAYED UP UNDER A VAC BAG; C OMPLETED CURE; COUNTER SUNK HOLES AND APPLIED NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008033100027 20080331 00027 NM 2008 3 31 SWAA081659 1 20080326 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008033100069 20080331 00069 NM 2008 3 31 AMTA200800153 1 20080228 A 5347 RAIL BOEING 737 73783N 13844HI NM BS 727 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 RAIL ASSY LBL 17.24, STA 727I (T) UNION AREA HAVE LIGHT CORROSION. REMOVED CORROSION, ORG MAT .071, MAT LOSS .011, REM MAT .060, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A, FABRICTED REPAIR PART FROM BAC 1509-100688 IAW EA 737-5300-08-A 0037. (K) 2 L 7 2 4F RT A16WE 2008033100070 20080331 00070 NM 2008 3 31 AMTA200800155 1 20080228 A 5347 RAIL BOEING 737 73783N 13844HI NM BS 767 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 RAIL ASSY RBL 3.0, STA 767 HAVE HAD GENERAL CORROSION. REMOVED CORROSION, ORG MAT .071, MAT LOSS .036, REM MAT .035, FO UND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A, FIG 103. DETAIL D, FABRICATED REPAIR PART IAW EA 737-5300-08-A0036. (K) 2 L 7 2 4F RT A16WE 2008033100092 20080331 00092 NM 2008 3 31 AMTA200800174 1 20080228 A 5730 SKIN PANEL BOEING 737 73783N 13844HI NM LT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LT WING FUEL TANK ACCESS 532FB HAS PITTING CORROSION ON LWR SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROSIO N ON LT WING FUEL TANK ACCESS LANDING IAW B737-800, SRM 51-10-02-0G, ROG MAT .205, MAT LOSS .003, REM MAT .202, FOUND TO BE WITHIN LIMITS IAW SRM 57-20-01-1A-1, PERFORMED FLAP PEENING IAW SRM 51-20-06 AND SOPM 20-10-03. (K) 2 L 7 2 4F RT A16WE 2008033100110 20080331 00110 NM 2008 3 31 AMTA200800186 1 20080228 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM BS 737-887 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 PANEL 140CF FOUND WITH LIGHT CORROSION. REMOVED CORROSION IAW SRM 51-10-02, ORG MAT .071, MAT LOSS .003, REM MAT .068, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53, ALODINED AND PRIMED IAW SRM 51-20-01. (K) 2 L 7 2 4F RT A16WE 2008033100116 20080331 00116 NM 2008 3 31 AMTA200800195 1 20080301 A 5320 FLOOR SUPPORT BOEING 737 73783N 13844HI NM BS 807-827 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 NUTPLATE AREA BETWEEN STA 827 AND 807, RBL 13.84. HAS LIGHT CORROSION. REMOVED LIGHT CORROSION, ORG MAT .071, MAT LOSS .025, REM MAT .046, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2, FABRICATED REPAIR STRAP FROM 7075-T6, .071 IAW EA 737-5300-08-A0038. (K) 2 L 7 2 4F RT A16WE 2008033100136 20080331 00136 EA 2008 3 31 A6WA200840100 1 20080215 A 2720 RUDDER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 31 417AW 7610 UNCOMMANDED FULL RT RUDDER AT HIGH ALTITUDE CLIMB 280 KNOTS WITH YAW DAMPER ENGAGED, STEPPED ON RUDDER TO CORRECT AND TR IMMED BACK IN POSITION, PROCEEDED NORMALLY. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008033100160 20080331 00160 EA 2008 3 31 SWIA200819384 1 20080317 A 2910 HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS LEAKING A SWIA O OTHER K FLUID LOSS UK UNKNOWN 1 NM 07 912SW 7595 FLT 6025 - RECEIVED A "HYD 1 LOW PRESS" CAUTION MESSAGE. REPLACED NR 1 HYDRAULIC SYSTEM SUCTION LINE AS REQUIRED. NO L EAKS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 2008033100172 20080331 00172 NM 2008 3 31 TAMF20080012S 1 20080313 A 5711 SPLICE BOEING 767 767200 1385120 NM GE CF6 CF680C2B2 30025 NE SPAR CRACKED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 770QT 23802 DURING C2 CHECK INSPECTION WAS FOUND A CRACK ON SPLICE PLATE FRONT SPAR LOWER CHORD STA ISS 256.15 261.26 - RT. DAMAGE D AREA WAS REPAIRED IAW EWO 767 57-041 AND MFG SERVICE REQUEST 1-789000676. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2008033100203 20080331 00203 WP 2008 3 31 NWAA081209858 1 20080223 A 5312 STIFFENER DOUG DC9 DC951 3022051 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 767NC 47724 DURING "H" CHECK, FOUND CRACK IN OUTBOARD LOWER END OF AFT LEFT LAVATORY NR 1 HORIZONTAL STIFFENER AT AFT PRESSURE BULKH EAD. REPAIRED PER EA 98-212123. 2 L 7 2 4F RT A6WE 2008033100208 20080331 00208 NM 2008 3 31 DHL2008763527 1 20080314 A 2782 6516275 SUPPORT FITTING BOEING 727 727264 138408M NM KRUEGER FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 NR 1 K-FLAP ACTUATOR MOUNT SPT FITTING CRACKED AT WS 307.5 AND 315.3. REMOVED ACTUATOR SUPPORT MOUNT ASSY, FABRICATED S UPPORT WEBS FROM 2024-T3, .063" BY 8" BY 3.5" (2 EA), PO NR 9006027, AND MOUNT DOUBLERS FROM 7075-T6, .125" BY 5" BY 2", (2 EA), PO NR 9005685, ASSEMBLED AND INSTALLED PER B727 SRM 51-30-2, 51-20-1 FIG 7, 51-30-5, AND BAC DWG 65-16275 REV D . 2 L 7 3 4F A3WE 2008033100236 20080331 00236 WP 2008 3 31 DHL2008805526 1 20080310 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 AFT CARGO COMPT BILGE FITTING CRACKED 2" STA 1280.000 L-35R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACK ED FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2008033100237 20080331 00237 WP 2008 3 31 DHL2008805527 1 20080311 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 AFT CARGO COMPT BILGE FITTING CRACKED 1" (STA 1180.000- 1200.000 L-35L) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53 -1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B . INSTALLED NEW FITTING IAW SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2008033100248 20080331 00248 NM 2008 3 31 DHL2008752601 1 20080204 A 5260 WEB BOEING 727 727223 1384074 NM AIRSTAIR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752 22466 LT SIDE OF AIRSTAIR WEB CRACKED AT LIGHTING HOLE BS 1223. CUTOUT DAMAGED AREA AT LT SIDE OF AIRSTAIR WEB SAT 1223 IAW B 727 SRM 51-40-2 FIG1. FABRICATED DOUBLER MAT USED 7075T6 0.032 DIMENSION 2.5" BY 2.5" PO NR 9006457 IAW B727 SRM 51-40- 2 FIG 1 AND B727 SRM 53-10-2 FIG 6. TREATED AND PRIMED AREA IAW B727 SRM 51-10-2. INSTALLED DOUBLER REPAIR AT LT SIDE OF AIRSTAIR WEB STA 1223 IAW B727 SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2008033100249 20080331 00249 WP 2008 3 31 DHL2008805506 1 20080324 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 LT WING INBD L/E LWR SURFACE HAS ELONGATED HOLES AT STA XILD 42. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 03-24 -08, EVA D853-00046, DWG AF12-57-101 REV IR DATED 02-22-08. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-3-0. CUT OUT DAM AGED SECTION IAW DWG AFR-57-101. PERFORMED NDT INSP IAW BOEING DC8 NDT SPM PART 06-10-01-001. NO CRACK, NO CORROSION F OUND. ENCLOSED SMN FORM 242-2. FABRICATED (2EA) FILLERS (AL7075T6 0.063") AND REPAIR DOUBLER (AL7075T6 0.071") IAW DWG AF12-57-101 REV IR. PERFORMED NDT INSP OF REPAIR PARTS IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK FOUND. ENCLOSED S MN FORM 242-2. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DWG AF12- 2 L 7 4 4F RT 4A25 2008033100254 20080331 00254 WP 2008 3 31 DHL2008805519 1 20080226 A 5320 WEB DOUG DC8 DC873F 302199F WP LT MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 LT MLG W/W WEB CRACKED 1.500" AT STA 857.000 LBL 18". REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRI CATED DOUBLER (AL2024T3 0.040") IAW SRM 53-2-0 FIG 23, SRM 53-8-3 FIG 1. CLEANED, TREATED AND PRIMED AREA AND DOUBLER I AW SRM 51-1-8B. INSTALLED DOUBLER IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2008033100258 20080331 00258 WP 2008 3 31 DHL2008805516 1 20080317 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 AFT FUS EXT SKIN CORRODED (STA 1730.000 - 1740.000 L-28R TO L-30R). PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DATED 02 -29-08, AD2007-02-02, S/B DC8 S3A080, DWG DOUGLAS SR08530032 AND BOEING MSG 1-7761393332 DATE3D 02-29-08, SEMAN DWG ED-4 715 DATED 02-21-08. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED EXIS TING REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL 7075T6 0.063") (2EA) FILLER (AL7075T6 0.050") (10EA) FINGER DOUBLER (AL7075 0.032") IAW SEMAN DWG NR ED-4715, DOUGLAS DW G SR0850032. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SEMAN DWG E 2 L 7 4 4F RT 4A25 2008033100261 20080331 00261 WP 2008 3 31 DHL2008805501 1 20080316 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 FWD ACCY COMPT CORROSION BETWEEN SKIN AND FINGER DOUBLER (STA 30.000 - 50.000 L-32R TO L-33R). PERFORMED MAJOR REPAIR I AW FAA FORM 8110-3 DATED 03-14-08, ASTAR EVA D853-00048 REV IR DATED 02-27-08 (SEMAN DWG ED-4714) DATED 02-18-08. REMOV ED CORROSION IAW SRM 51-1-21. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SECTION IAW SEMAN DWG ED-4714. FABRICATED REPAIR DOUBLER, FILLERS, AND INTERNAL REPAIR SPLICES, INTERNAL FINGER DOUBLER IAW SEMAN DWG ED-4714. PERFO RMED NDT INSP IAW BOEING DC8 NDT SPM PART 06-10-01-001. NO CRACK, NO CORROSION FOUND. ENCLOSED SMN FORM 242-2. CLEANE D, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW EVA D853-00048 AND SEMAN DWG NR 2 L 7 4 4F RT 4A25 2008033100273 20080331 00273 NM 2008 3 31 QXEA200800312 1 20080320 A 5320 ACCESS PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX -C4- CORROSION AROUND NUTPLATE HOLES (TOP AND BOTTOM SIDES) ON APERATURE FOR BAG BAY FLOOR PANEL 144HZ. REMOVED RI VETS TO FACILITATE BLEND, REF DHC 8 200 SRM 51-40-11. REMOVED NUTPLATES TO FACILITATE BLEND REF DHC 8 200 SRM 51-40-11. BLENDED LIGHT SURFACE CORROSION OF TOP SURFACE OF SKIN ON FWD AND OUTBOARD SIDE OF ACCESS PANEL, BLENDED CORROSION ON F WD UNDERSIDE OF ACCESS PANEL REF CPM CHAPTER 4 STEP 8. HFEC INSPECTED BLENDED AREA FOR CRACKS IAW D-8/200 NDTM PART 6, 51-00-01. NO CRACKS NOTED. UT THICKNESS CHECK OF BLENDED AREA IAW -8/200 NDTM PART 1, 51-00-04 HIGH .040 LOW .037. AR EA BLENDED WITHIN LIMITS PER DHC 8 SRM 51-20-11. APPLIED ETCH, ALODINE AND PRIMER IAW D8 200 SRM 51-20-16 AND 51-20-36 2 H 7 2 4T RT A13NM 2008032800049 20080328 00049 NM 2008 3 28 SWAA081528 1 20080319 A 5311 6546567 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 1006, STR 17R TO STR 19R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032800054 20080328 00054 SO 2008 3 28 C2XA08RI035 1 20080304 A 3150 WARNING SYSTEM EMB 145 EMB145XR 3260214 SO COCKPIT MALFUNCTIONED A C2XA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SW 27 12157 145787 FLIGHT 3098 - EWR - DURING PREFLIGHT, CREW REPORTED AIR/GRND FAIL MESSAGE ON EICAS. SYSTEM WAS RESET AND MESSAGE WENT A WAY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2008032800066 20080328 00066 NM 2008 3 28 SWAA081539 1 20080321 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008032800070 20080328 00070 NM 2008 3 28 SWAA081544 1 20080323 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032800072 20080328 00072 NM 2008 3 28 SWAA081546 1 20080323 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032800082 20080328 00082 NM 2008 3 28 SWAA081574 1 20080323 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008032700092 20080327 00092 NM 2008 3 27 08FDEA01087 1 20080320 A 5730 ARB2886503 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 522FE 48476 LEFT WING LEADING EDGE ANTI-ICE TELESCOPIC DUCT DOOR CUT OUT CORNER SKIN CRACKED. REPAIRED AS PER SRM 57-10-00, FIGURE 43, VOLUME 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032700114 20080327 00114 SO 2008 3 27 SIMA200808102 1 20080317 A 5315 14521721005 FLOORBEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 623AE 145109 DURING MBV INSPECTION, FOUND TOP SIDE OF FORWARD DIGITAL CORRODED AT FRAME 15. REPAIRED DIGITAL IAW ETA EM-5300-013. A IRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032700137 20080327 00137 EA 2008 3 27 SWIA200819368 1 20080315 A 3230 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 408SW 7055 FLT 3768 - DURING APPROACH MAIN GEAR DID NOT EXTEND. MANUAL EXTENSION REQUIRED TO EXTEND MAINS. REPLACED MLG SELECTOR VALVE IAW MM 32-32-10. OPS AND LEAK CHECK GOOD, PN 750005000, SN/OFF 0033. 2 L 7 2 4F RT A21EA 2008032700153 20080327 00153 NM 2008 3 27 DL76L080406 1 20080323 A 2797 WIRE BOEING 767 767332 1382001 NM SLAT SENSOR BROKEN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 197DN 28454 L/E SLAT ASYM MESSAGE DURING SLAT RETRACTION. SLAT LOCKED BETWEEN 1 AND UP. RETURNED TO ATL. MIP SUSPECTING NR 5 SLA T SENSOR OR TARGET. FOUND BROKEN WIRE AT SENSOR S280 REPAIRED SAME AND OPS CK GOOD. 2 L 7 2 4F RT A1NM 2008032700155 20080327 00155 EA 2008 3 27 MASA200800258 1 20080322 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 97325 7325 ASH FLT 2944 PHX-EUG, MAIN CABIN DOOR WILL NOT OPEN. LUBED DOOR. 2 L 7 2 4F RT A21EA 2008032700160 20080327 00160 SO 2008 3 27 SIMA200808401 1 20080323 A 3350 2013BR BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 935AE 14500920 ON FLIGHT 3890, CREW REPORTED EMERGENCY FLOOR TRACK LIGHTING BY SEATS 8-11 AND WING EMERGENCY EXIT LIGHTS AT THE BOTTOM OF BOTH DOORS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY PACK NR 3 IAW 145 AMM 33-50-04. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008032700166 20080327 00166 NM 2008 3 27 2008UALA01402 1 20080313 A 5320 SUPPORT FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FUSELAGE STRINGER 7L INTERCOSTAL SUPPORT CLIP IS CRACKED BS 294.5. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED WEB (CLI P). OBTAINED & INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700169 20080327 00169 NM 2008 3 27 2008UALA01405 1 20080313 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 MED (FORWARD ENTRY DOOR) CUTOUT LOWER HINGE 1 EA FASTENER ABOVE & 1 EA FASTENER BELOW HINGE CUTOUT HAS CRACK INDICATIONS . MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700172 20080327 00172 EU 2008 3 27 CPCP20080013 1 20080304 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 377AT 377 FOUND SEAT TRACK LT I/B FRAME 29 TO FRAME 35 CORRODED. FOUND SEAT TRACK LT I/B FRAME 29 TO FRAME 35. REPLACED IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2008032700179 20080327 00179 NM 2008 3 27 2008UALA01412 1 20080313 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FWD GALLEY DOOR LOWER FWD FRAME IS CRACKED IN TWO LOCATIONS AT STOP FITTING ATTACH POINT. MAJOR REPAIR ACCOMPLISHED: R EMOVED CRACKED LWR FWD FRAME & INSTALLED NEW SPLICE FRAME REPAIR KIT. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700185 20080327 00185 NM 2008 3 27 2008UALA01415 1 20080313 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FWD ENTRY DOOR CUTOUT LOWER HINGE 1 EA FASTENER HOLE ABOVE & 1 EA FASTENER HOLE BELOW HINGE CUTOUT HAS CRACK INDICATION. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700192 20080327 00192 NM 2008 3 27 2008UALA01427 1 20080313 A 5320 SUPPORT FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FUSELAGE STRINGER SUPPORT CLIP FOR INTERCOSTAL CRACKED BS 360 STR 11L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED CLIP . INSTALLED NEW REPLACEMENT CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700212 20080327 00212 NM 2008 3 27 08FDEA01112 1 20080323 A 5347 53FX139821 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 MAIN CABIN COMPARTMENT, SEAT TRACK CORRODED AT BS 950C, 8 BL 0. REMOVED SEAT TRACK SECTION- OUT OF LIMITS BL 0 STA 95 0C TO STA 1010 IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM ER 01-049 AND SRM 53-10-5 FIG7. T REATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW SEAT RTACK IAW SRM 53-30-2. 2 L 7 3 4F A3WE 2008032700221 20080327 00221 NM 2008 3 27 2008UALA01483 1 20080316 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 AFT GALLEY WALL EMERGENCY LIGHT LT INOP. REPLACED LIGHT ASSY. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032700222 20080327 00222 NM 2008 3 27 08FDEA01116 1 20080323 A 5311 ACA73511 FRAME DOUG MD11 MD11F 3023600 NM BS 535 S19-20L CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 522FE 48476 MAIN DECK LEFT FRAME AT BS 535, BETWEEN L19-20L, 01 EACH CHAFED MARK FOUND NEAR 9G NET YOKE. REPAIRED AS PER DRAWING SR Z-53-503. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008032700235 20080327 00235 WP 2008 3 27 08FDEA01125 1 20080324 A 5730 ABR25103 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LEFT WING LOWER INBD L/E PANEL 516 HB IS CHAFED ALONG THE EDGE. BLENDED THE AREA IAW SRM 57-00-01; VOL I. ORIGINAL MAT ERIAL .090; MATERIAL REMOVED .020; MATERIAL REMAINING .070 TOOL NR T8225P. FOUND TO BE OUT OF LIMITS IAW SRM 57-00-0 1; VOL I. FABRICATED DOUBLER AND FILLER IAW SRM 51-21-01; VOL I. ASSEMBLED PANEL; DOUBLER AND FILLER IAW SRM 51-35-01; VOL II. PAINTED PANEL AND DOUBLER IAW SRM 51-21-02; VOL II. 2 L 7 3 4F RT A22WE 2008032700236 20080327 00236 NM 2008 3 27 2008UALA01490 1 20080316 A 5210 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EPAS RESERVOIR BENT A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 768UA 26919 THE 4R DOOR EPAS RESERVOIR ELECTRIC PLUG PIN BENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032700241 20080327 00241 WP 2008 3 27 08FDEA01128 1 20080324 A 5753 ARC29911 PANEL DOUG MD10 MD1010F 3022112 WP TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LEFT INBD FLAP, LOWER INBD PANEL (P/N ARC 2991-1) IS DENTED AND DEFORMED. THE ACCESS DOOR WITHIN THE PANEL IS MOST DIFF ICULT TO CLOSE. REMOVED & REPLACED DOOR HUNGE IAW SRM 51-31-01 VOL II. FABRICATED DOUBLER REPAIR IAW SRM 57-10-00 FIG 85 VOL I. ALODINED & PRIMED IAW SRM 51-21-01 PGS 21 & 24 VOL II. PAINTED IAW SRM 51-21-02 PG 8 VOL II. 2 L 7 3 4F RT A22WE 2008032700262 20080327 00262 NM 2008 3 27 AALA200800493 1 20080304 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 966AN 30094 MIA - EMERGENCY LIGHT AT SEAT ROW 28 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 28. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008032700264 20080327 00264 NM 2008 3 27 AALA200800495 1 20080304 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 966AN 30094 MIA - EMERGENCY LIGHT AT SEAT ROW 28 HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008032700284 20080327 00284 NM 2008 3 27 AALA200800511 1 20080305 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT AT SEAT 31G HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700291 20080327 00291 NM 2008 3 27 AALA200800519 1 20080305 A 2560 STRAP BOEING 737 737823 13844BZ NM FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 928AN 29528 LGA - EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT SEAT HAS BROKEN SAFETY STRAP. REPLACED SAFETY STRAP FOR EMERGENCY FL ASHLIGHT AT AFT FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008032700298 20080327 00298 2008 3 27 C2XA08CL033 4 20080318 A 3160 7014331921 BEZEL EMB 145 EMB145LR 3260212 SO NR 2 INOPERATIVE A C2XA A UNSCHED LANDING O OTHER DE DESCENT 1 SW 27 29917 145414 EWR FLIGHT 2396 - THE CREW REPORTED THE F/O'S ALTIMETER ADJUSTMENT WAS INOPERATIVE DURING DESCENT INTO DTW. UNABLE TO L AND CAT II IN DTW THE FLIGHT WAS DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 PFD BEZEL. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008032700304 20080327 00304 NM 2008 3 27 DHL2008763523 1 20080316 A 5311 FRAME BOEING 727 727264 138408M NM BS 347 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 FRAME DAMAGED IN CARGO COMPT AT BS 347, ALONG STR 4L. CUT OUT DAMAGE, INSTALLED FRAME REPAIR PARTS, P/N AE727-2-360-11 AND AE727-2-360-12, PO NR 810972, PER B727 SRM 51-30-5, 51-30-2, AND AEI DWG AE727-2-360 REV G. 2 L 7 3 4F A3WE 2008033100277 20080331 00277 NM 2008 3 31 DL76G080410 1 20080326 A 5315 BAC1505100774 FLOORBEAM BOEING 767 7673P6 1385105 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 155DL 25269 FLOORBEAM CORRODED AT STA 654+66 AT LBL 18 TO LBL26. BEAM REPLACED PER 53-00-51D FIGURE 201 ON NR AVM511442. 2 L 7 2 4F RT A1NM 2008033100279 20080331 00279 NM 2008 3 31 DL76G080412 1 20080326 A 5315 BAC1505100744 FLOORBEAM BOEING 767 7673P6 1385105 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 155DL 25269 FLOORBEAM CORRODED AT STA 654+110 RBL 22 TO RBL 29. BEAM REPLACED PER 53-00-51D FIGURE 201 ON NR AVM5111491. 2 L 7 2 4F RT A1NM 2008033100280 20080331 00280 NM 2008 3 31 DLM90080413 1 20080324 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 CABIN SEAT TRK RBL 54.5 OUT OF LIMITS FS 1144-1316. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01 VOL I. 2 L 7 2 4F RT A6WE 2008033100283 20080331 00283 NM 2008 3 31 DLM90080416 1 20080323 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 FOUND CABIN SEAT TRACK RBL 54.5 OUT OF LIMITS, 1022-1050. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01 VOL I. 2 L 7 2 4F RT A6WE 2008033100286 20080331 00286 NM 2008 3 31 DLM90080419 1 20080324 A 5320 59364391 FITTING DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 REMOVED AND REPLACED FITTING, IAW MD90 SRM 51-30-01, 51-30-02 AND 51-10-05. 2 L 7 2 4F RT A6WE 2008033100288 20080331 00288 NM 2008 3 31 DLM90080421 1 20080318 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM CABIN CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 CABIN SEAT TRACK RBL 22 OUT OF LIMITS, 588-864. REMOVED AND REPLACED DAMAGED SEAT TRACK RBL22 588-864, IAW MD90 SRM 53- 40-01. 2 L 7 2 4F RT A6WE 2008033100290 20080331 00290 NM 2008 3 31 DLM90080423 1 20080316 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 97188 53392 CABIN SEAT TRACK LBL 22 OUT OF LIMITS 3 AREAS FS 731 TO 769. REPAIRED CABIN SEAT TRACK, IAW MD90 SRM 53-40-01 FIG 6. 2 L 7 2 4F RT A6WE 2008033100293 20080331 00293 NM 2008 3 31 DLM90080426 1 20080320 A 5320 9940443 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE BENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 LEFT FUSELAGE CUSP "T" CHORD WAS FOUND BENT BETWEEN FS 902 AND 924_LBL 60. REMOVED, FABRICATED AND INSTALLED "T" CHORD, IAW MD90 SRM 51-30-02. 2 L 7 2 4F RT A6WE 2008033100297 20080331 00297 NM 2008 3 31 DLM90080430 1 20080306 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 LT CABIN CUSP WEB FS 910-918 CORRODED. CUTOUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND INSTALLED DOUBLER IAW DRD 53- 05D, FIG 827D. 2 L 7 2 4F RT A6WE 2008033100301 20080331 00301 SO 2008 3 31 SIMA200808701 1 20080326 A 3234 7455503 LEVER EMB 145 EMB145LR 3260212 SO COCKPIT INOPERATIVE A SIMA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 619AE 145101 ON FLIGHT 4501 CREW REPORTED WHILE ON CLIMB-OUT LANDING/LEVER DISAGREE ON EICAS. GEAR WILL NOT RETRACT. CYCLED GEAR LE VER AND CONFIRMED 3 GREEN DOWN LIGHT. RETURN TO ORD. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LANDING GEAR SELECTOR LEVER IAW EMB AMM TASK 32-32-02-000-800A AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008033100302 20080331 00302 EU 2008 3 31 MALA080045 1 20080221 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 340B453 RT FUSELAGE SKIN DENT AT STA 294.5, 0.861 INCH ABOVE THE HYDRAULIC LINE CHANNEL COVER UPPER ATTACH ANGLE BETWEEN SL1624 AND 1625 MEASURING 0.475 INCH BY 0.425 INCH BY 0.33 INCH DEEP. HFEC AND DISBOND INSPECTIONS WERE ACCOMPLISHED. NO CRAC KS OR DISBONDS NOTED. ACCOMPLISHED REPAIR IAW EO NR S53529, SAAB REPAIR STATEMENT 340SDS014271 PARA 1 AND SRM 53-70-10 SPECIAL REPAIR PARA 4, FIG 210. 2 L 7 2 4T RT A52EU 2008033100304 20080331 00304 EU 2008 3 31 MALA080047 1 20080221 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 340B453 PCN4K FLOORPANEL, SEAT TRACK CORRODED FROM STA 288 TO STA 339 ALONG BL 0.0 AND BL 18.3. SEAT TRACK REPLACED IAW EOS5306 0. EXELTECH NR 2161. 2 L 7 2 4T RT A52EU 2008033100305 20080331 00305 SO 2008 3 31 CHQA200800056 1 20080323 A 3260 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COCKPIT MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 292SK 145488 CAE311794 ORF TO IAD - UPON DEPARTURE FROM ORF, THE LANDING GEAR WAS SELECTED UP, BUT WOULD NOT RETRACT. THIS WAS ACCOMPANIED BY AN LG AIR/GRD FAIL MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ALL THE WEIGHT ON WHEELS SWITCHES AND THE TARGETS AND FOUND NO DEFECTS. THE AIRCRAFT WAS THEN TAKEN ON A TEST FLIGHT A ND HAD NO FURTHER PROBLEMS. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008033100307 20080331 00307 NM 2008 3 31 DLM90080431 1 20080306 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM CABIN CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 CABIN SEAT TRACK FS 1321 LBL 44.5 CORRODED OUT OF LIMITS (100 PERCENT MATERIAL LOSS). REMOVED SEAT TRACK, FABRICATED AN D INSTALLED NEW SEAT TRACK, IAW MD90 SRM 53-40-01 FIG 6. 2 L 7 2 4F RT A6WE 2008033100312 20080331 00312 NM 2008 3 31 DLM90080436 1 20080318 A 5320 5940441 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 LT CABIN CUSP WEB FS 659 CORRODED AT LIGHTENING. REPAIRED CUSP WEB, IAW MD90 SRM 51-11-01 FIG 2 VOL I. 2 L 7 2 4F RT A6WE 2008032700330 20080327 00330 WP 2008 3 27 08FDEA01135 1 20080325 A 5753 ARC0502502 HINGE BRACKET DOUG DC10 DC1010F 3022111 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION, FOUND LT OUTBOARD INBOARD FLAP HINGE WITH ATTACH POINT (FWD) RUST AND BUSHING WITH PLAY. REPLACED BRACKET ASSY FOR DWG ARC0504. 2 L 7 3 4F A22WE 2008032700351 20080327 00351 NM 2008 3 27 HALA0800426 1 20080323 A 2622 2600301 BOTTLE BOEING 767 767332 1382001 NM CABIN DISCHARGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 598HA 23278 ON OVERNIGHT CK, FOUND PORTABLE FIREX AT R2 DOOR, EQUIP NR E48, WITH NEEDLE IN THE RECHARGE BAND. REMOVED AND REPLACED AFT RT PORTABLE FIRE EXTINGUISHER. 2 L 7 2 4F RT A1NM 2008032700354 20080327 00354 NM 2008 3 27 XXUA200800006 1 20080322 A 2560 A3060768 KNOB ACR BOEING 757 7572Q8 1384972 NM PWA PW2037 PW2037M 52117 NE MEGAPHONE MISSING A XXUA K NONE O OTHER IN INSP/MAINT 1 EA 15 401JS 26332 FORWARD MEGAPHONE MISSING VOLUME KNOB. REPLACED KNOB OPS CHECKS OK, KNOB P/N A3-06-0768. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032700361 20080327 00361 NM 2008 3 27 AALA200800522 1 20080306 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 608AA 27446 DFW EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 2008032700392 20080327 00392 NM 2008 3 27 AALA200800523 1 20080306 A 3350 LENS BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AA 27446 DFW - EMERGENCY LIGHT AT SEAT 22D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008032800039 20080328 00039 SO 2008 3 28 C2XA08IA082 1 20080318 A 3350 276005 FUSE EMB 145 EMB145EP 3260221 SO POWER SUPPLY BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14939 145030 IAH - DURING A-CK INSPECTION THE EMERGENCY LIGHT LOCATED ON THE SERVICE DOOR SWING ARM WAS FOUND TO BE INOPERATIVE. MAI NTENANCE REMOVED AND REPLACED THE SERVICE DOOR FUSE FROM THE NUMBER TWO BATTERY PACK POWER SUPPLY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008032800046 20080328 00046 NM 2008 3 28 SWAA081522 1 20080319 A 5753 65C30462 FLAP BOEING 737 7375H4 138449D NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD FOREFLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2008032800058 20080328 00058 NM 2008 3 28 SWAA081534 1 20080320 A 3350 417N5212 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 294WN 32540 EEPLS END CAP LENS LOOSE AT ROW 23 ABC. SECURED END CAP PER MM. 2 L 7 2 4F RT A16WE 2008032800077 20080328 00077 NM 2008 3 28 SWAA081550 1 20080320 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032800081 20080328 00081 NM 2008 3 28 SWAA081576 1 20080323 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 628SW 27703 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008032800088 20080328 00088 NM 2008 3 28 SWAA081557 1 20080323 A 5753 6546430 SKIN BOEING 737 7373G7 1384595 NM LT FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED C4 CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2008032800089 20080328 00089 NM 2008 3 28 SWAA081558 1 20080323 A 5330 65C33800 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN R1 DOOR CUTOUT UPPER FWD CORNER CRACKED. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008032800100 20080328 00100 NE 2008 3 28 U30A200800002 2 20080128 A 7230 COMPRESSOR AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE NR 2 ENGINE DETERIORATED A U30A A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 17 267AV 21429 1198 779705 FLT 270 ON CLIMBOUT, LEVEL 8000FT, FLT CREW HEARD 4-5 BANGS, WITH VIBRATION. CREW REVIEWED ENG & SYS PAGES OF ECAM, ALL NORM. NO ECAM MESSAGES OR WARNINGS. SUSPECT COMPRESSOR STALL, RETURNED TO EWR. LANDING UNEVENTFUL. BORESCOPED ENGIN ES NO DEFECTS NOTED. POWER ASSURANCE RUN PER AMM 71-00-00-710-008 UNSAT, DUE TO NR 2 ENG COMPRESSOR STALL ON GROUND RU N. ENG REPLACED. REMOVAL REASON CONFIRMED. CHORD WIDTH EROSION & DETERIORATION FOUND IN HPC. REMOVED/REPLACED HARDWARE , INCLUDING HPC BLADES & VANES IAW SBS & ENG MANUAL, TESTED PER THE 56-5B/P MANUAL. COMPLIED WITH AD 2002-13-03, AS APP LICABLE. RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E38NE 2008032800109 20080328 00109 EU 2008 3 28 UPS08151888 1 20080307 A 5330 SKIN AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 136UP 0819 INSPECTION TYPE:3C TRANSFERRED FROM LOG PAGE 954176 ITEM 2. REF DMI D370413. SKIN DENTS FWD AND RIGHT OF TAIL STAND FI TTING. CUT OUT DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER & FILLER IAW A300-600 SRM 53-10-12 FIG 210. 2 L 7 2 4F RT A35EU 2008032800110 20080328 00110 WP 2008 3 28 UPS08851864 1 20080224 A 5342 ATTACH ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 VERT FIN TO FUSELAGE ATTACH ANGLE CRACKED AND CORRODED LT SIDE STA 1766. REPAIRED VERT FIN TO FUSELA GE ATTACH ANGLE IAW SRM 53-02-05-FIG 16A. 2 L 7 4 4F RT 4A25 2008040100001 20080401 00001 NM 2008 4 1 TSAA0836017 1 20080322 A 3610 32895625 CONTROL VALVE BOEING 737 73773A 1384606 NM NR 2 ENGINE FAILED A TSAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 13 739AL 28500 ETOPS FLIGHT 841 SNA-HNL - DURING CLIMB, THE CREW NOTED THE RIGHT ENGINE BLEED TRIPPED OFF. THE CREW WAS UNABLE TO RESE T THE SYSTEM AND DIVERTED TO ONT. THE AIRCRAFT LANDED IN ONT WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACE D THE NR 2 ENGINE PRECOOLER CONTROL VALVE PER AMM 36-12-02-00-801 WITH ALL OPERATIONAL CHECKS SATISFACTORY. THE AIRCRAF T WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2008040100002 20080401 00002 WP 2008 4 1 IXXA08SMN036S 1 20080201 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AFT LOWER FUSELAGE BELLY AFT OF OUTFLOW VALVE "SUGAR SCOOP" AT STATION FS 1682 LONGERON 35.6 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND CORROSION FOUND. FABRICATED REPAIR DOUBLER, REPAIR TRIPL ER, SKIN FILLER, AND INTERNAL DOUBLER FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENE RS AND REPAIR PARTS IAW DC8 SRM 51-1-21, 51-1-20D, 51-3-1, FAA FORM 8110-3 NUMBER 08110 DATED 03-13-08, SEMAN DRAWING ED -4699 DATED 02-13-08, 51-3-0, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008040100003 20080401 00003 WP 2008 4 1 IXXA08SMN034S 1 20080201 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT FUSELAGE SKIN FORWARD OF FLAT AFT PRESSURE BULKHEAD AT LONGE RON 28. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFOR MED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED NEW SKIN, INTERNAL, EXTERNAL DOUBLERS. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8100-9 DATED 02-14-08, AD 2007 -02-02, S/B DC8-53A080 DATED 06-22-04, DRAWING DOUGLAS SR08530032 AND BOEING SKETCH 200802070028-0001, DC8 SRM 51-1-21, 51-3-0, 51-1-20D, AND DC8 NDT SPM PART 06-10-01-.001. 2 L 7 4 4F RT 4A25 2008040100009 20080401 00009 EU 2008 4 1 08FDEA01160 1 20080327 A 5315 A53781966200 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 658FE 752 FWD CARGO COMPT LEFT SIDE MAIN DECK FLOORBEAM FR 31 HAS 1 INCH CRACK, BETWEEN TRACKS NR 4 AND NR 5. REPAIRED MAIN DECK CRACKED FLOORBEAM AT FRAME 31 BETWEEN TRACK NR 4 AND TRACK NR 5 IAW A300-600 SRM 53-10-15, FIG 212. 2 L 7 2 4F RT A35EU 2008040100011 20080401 00011 WP 2008 4 1 08FDEA01163 1 20080327 A 5753 NRC6053 SKIN DOUG DC10 DC1030F 3023504 WP T/E FLAP LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 307FE 48291 LT WING OUTBD FLAP UPPER SURFACE FOUND 120 LOOSE FASTENERS ON SKIN. REPAIRED SKIN LOOSE FASTENERS IAW SRM 57-20-00 FIG 11 VOL I. 2 L 7 3 4F RT A22WE 2008040100021 20080401 00021 WP 2008 4 1 IXXA08SMN067S 1 20080208 A 5320 4750521U1 FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 847.000 LONGERON1. REMOVED C RACKED FITTING. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-1 -8-B, DC8 SRM 51-1-20D, AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2008040100022 20080401 00022 WP 2008 4 1 IXXA08SMN065S 1 20080208 A 5753 SKIN DOUG DC8 DC871F 302199D WP T/E FLAP DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP LOWER SKIN FORWARD SHOWS DENTS BETWEEN STATION XF 160.000 - XF 213.000. PERFORMED DETAILED VISUAL INSPECTION. NO CRACK NO CORROSION FOUND. PERFORMED MEASUREMENT DIA 2.00 BY 0.00 8" DEPTH WITHIN PERMISSIBLE LIMITS. APPLIED PRO-SEAL. CLEANED, TREATED, PRIMED AND PAINTED AREA IAW DC8 SRM 51-1-8B, D C8 57-1-0 PAGE 1, DC8 SRM 51-1-9 FIGURE 13B, 2 L 7 4 4F RT 4A25 2008040100027 20080401 00027 NM 2008 4 1 TSAA0827018 1 20080324 A 2750 FLAP BOEING 737 73776N 13844CH NM WING MALFUNCTIONED A TSAA K NONE F FLT CONT AFFECTED AP APPROACH 1 WP 13 748AL 30050 ETOPS FLIGHT 483 SNA -OGG - ON APPROACH, THE CREW EXTENDED THE TRAILING EDGE FLAPS BUT THE FLAPS STOPPED AT FLAPS 1. TH E CREW EXTENDED THE FLAPS USING THE ALTERNATE EXTENSION AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED AIRC RAFT FIM 27-51-00-810-836 WITH ALL OPERATIONAL CHECKS SATISFACTORY ON THE GROUND. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2008040100031 20080401 00031 NM 2008 4 1 UIEA200800074 1 20080313 A 5347 SEAT TRACK BOEING 747 747341 13848AM NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 MAIN DECK STA 1680 TO 1700 RBL 11 SEAT TRACK HAS LEVEL 1 CORROSION. CORROSION REMOVED AND TREATED IAW SRM 51-10-01. 2 L 7 4 4F RT A20WE 2008040100032 20080401 00032 NM 2008 4 1 UIEA200800075 1 20080313 A 5320 STRUCTURE BOEING 747 747341 13848AM NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 MAIN DECK STA 1680 TO 1700 RBL 11 BEAM UPPER CHORD HAS LEVEL 1 CORROSION. CORROSION REMOVED AND TREATED IAW SRM 51-10-0 1. 2 L 7 4 4F RT A20WE 2008040100033 20080401 00033 NM 2008 4 1 UIEA200800076 1 20080313 A 5347 BAC15201889 SEAT TRACK BOEING 747 747341 13848AM NM FUSELAGE BROKEN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 MAIN DECK STA 1840 TO 1900 LBL 11 SEAT TRACK FOUND BROKEN. SEAT TRACK REPAIRED PER SRM 53-10-05. 2 L 7 4 4F RT A20WE 2008040100035 20080401 00035 NM 2008 4 1 UIEA200800077 1 20080313 A 5347 BAC15201567 SEAT TRACK BOEING 747 747341 13848AM NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 MAIN DECK STA 2040 TO 2060 LBL 90 SEAT TRACK HAS CORROSION. SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 1A. 2 L 7 4 4F RT A20WE 2008040100038 20080401 00038 EU 2008 4 1 USAA920080643 1 20080318 A 3350 E0062B1A4AD0A SWITCH AIRBUS 320 A320231 3930325 EU CABIN DEFECTIVE A USAA K NONE O OTHER UK UNKNOWN 1 EA 19 629AW 76 FLT NR 228 - LAS-ORD - EEL - EMERGENCY EXIT LIGHTS REMAIN ON AT ALL TIMES. MAINTENANCE REMOVED AND REPLACED EMERGENCY L IGHT SWITCH. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A28NM 2008040100050 20080401 00050 NM 2008 4 1 USAA920080648 1 20080313 A 5310 DOOR FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 CLT - MAJOR REPAIR - B4 CHECK - FORWARD CARGO DOOR, CUT OUT FORWARD FRAME CRACKED, BS 440, S24R. REPAIRED FORWARD CARGO DOOR, CUT OUT FORWARD FRAME, BS 440, S24R IAW USAIRWAYS EA 100318. 2 L 7 2 4F RT A16WE 2008040100051 20080401 00051 NM 2008 4 1 USAA920080649 1 20080320 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 459UW 25023 CLT - MAJOR REPAIR - RON - CRACKED FUSELAGE SKIN, BS 727E - BS 727F, S24R - S26R. REPAIRED FUSELAGE SKIN, BS 727E - BS 727F, S24R - S26R IAW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008040100053 20080401 00053 NM 2008 4 1 USAA920080651 1 20080320 A 5330 6545774 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 526AU 23861 CLT - MAJOR REPAIR - C6 CHECK - CRACKED FUSELAGE SKIN BS 727E, S22L. REPAIRED FUSELAGE SKIN, BS 727E. S22L IAW B737 SRM 53-00-01. 2 L 7 2 4F RT A16WE 2008040100054 20080401 00054 NM 2008 4 1 USAA920080652 1 20080316 A 5753 6546435332MC FLAP BOEING 737 7373B7 1384580 NM RT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 526AU 23861 CLT - MAJOR REPAIR - C6 CHECK - RIGHT WING OUTBOARD TRAILING EDGE FLAP HAS AREA OF DELAMINATION. REPLACED RIGHT WING OU TBOARD TRAILING EDGE FLAP IAW B737 SRM 27-51-39. 2 L 7 2 4F RT A16WE 2008040100055 20080401 00055 EU 2008 4 1 USAA920080666 1 20080322 A 2560 P2070001 FLASHLIGHT AIRBUS 320 A320214 3930316 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 104UW 863 FLT NR 1070 - BDL-PHX - AFT CENTER EMERGENCY FLASHLIGHT INOP, NO CHARGE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT ASSEMBLY CENTER AFT POSITION. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008040100059 20080401 00059 NM 2008 4 1 USAA920080653 1 20080222 A 5711 654532422 SPAR BOEING 737 7373S3 1384711 NM RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - RIGHT WING REAR SPAR UPPER CHORD CRACKED, RSS 222.5. REPAIRED RIGHT WING REAR SPAR UPP ER CHORD CRACKED, RSS 222.5 IAW USAIRWAYS EA 100283. 2 L 7 2 4F RT A16WE 2008040100063 20080401 00063 CE 2008 4 1 DXTA20082968 1 20080328 A 2750 PDU CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL TE FLAPS MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED DE DESCENT 1 GL 07 999QS 7500203 UPON SELECTING FLAP 15 DEGREES, AMBER CAS MSG (FLAP FAIL) SLAT WERE EXTENDED FULL AND FLAPS SHOWED 7 DEGREES. FOUND PDU ONLY PULLING 108 AMPS. REMOVED PDU AND INSTALLED OVERHAULED UNIT IAW MM 27-52-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008040100070 20080401 00070 CE 2008 4 1 DXTA20082972 1 20080330 A 3244 WHEEL CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE NLG VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 398QS 5600522 VIOLENT NOSEWHEEL SHIMMY ON TAKEOFF BETWEEN 20-30 KNOTS (ABORTED TAKEOFF). 2 L 7 2 4F 4 F RT A22CE E25EA 2008040100071 20080401 00071 NM 2008 4 1 USAA920080660 1 20080227 A 5315 65494611 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FLOORBEAM WEB/DOUBLER, BS 663, BL 0, WL 208. REPAIRED FLOORBEAM WEB/DOUBLER, B S 663, BL 0, WL 208 IAW USAIRWAYS EA 100292. 2 L 7 2 4F RT A16WE 2008040100072 20080401 00072 CE 2008 4 1 DXTA20082973 1 20080330 A 3240 BRAKE ASSY RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP FAILED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 892QS 258592 BRAKES ARE VERY MUSHY AND GO TO THE FLOOR. INSPECTED SYSTEM FOR LEAKS NONE NOTED. PERFORMED OPS CHECK ALL CHECK GOOD BL EED BRAKE SYSTEM AND PERFORM TAXI CHECK ALL CHECK GOOD. ALL WORK IAW MM 32-40-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2008040100078 20080401 00078 NM 2008 4 1 AMTA200800233 1 20080317 A 3620 BLEED AIR SYS BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE MALFUNCTIONED A AMTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 314TZ 30640 AFTER DEPARTURE LT BLEED TRIP WOULD NOT RESET. RE-ACTIVATED HIGH STAGE VALVE, ACTURATED VALVE SEVERAL TIMES, NO FAULTS NOTED. PERFORMED NR1 ENG BLEED SYSTEM HEALTH CHECK IAW 36-11-00-5, NO FAULTS. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2008040100081 20080401 00081 NM 2008 4 1 AMTA200800236 1 20080317 A 3350 LIGHT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 (3) EGRESS LIGHTS AT SEAT 2 DEF ARE INOPERATIVE. RESET (3) EGRESS LIGHTS AT SEAT 2 DEF IAW MM 33-50-01. OPS CHECK GOOD . (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008040100086 20080401 00086 NM 2008 4 1 USAA920080667 1 20080321 A 5330 6545775 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 23885 CLT - MAJOR REPAIR - RON - CRACKED FUSELAGE SKIN, BS 727G, S25R. REPAIRED FUSELAGE SKIN, BS 727G, S25R IAW USAIRWAYS EA 100336. 2 L 7 2 4F RT A16WE 2008040100087 20080401 00087 NM 2008 4 1 USAA920080671 1 20080322 A 5313 6545776 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 23381 CLT - MAJOR REPAIR - RON - CORROSION ON STRINGER, BS 1006 - BS 1016, S26R. REPAIRED STRINGER, BS 1006 - BS 1016, S26R I AW B737 SRM 53-60-03. 2 L 7 2 4F RT A16WE 2008040100089 20080401 00089 NM 2008 4 1 USAA920080673 1 20080324 A 5330 6545775 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 PHX - MAJOR REPAIR - FOUND CRACKED FUSELAGE SKIN, BS 840, S18R. REPAIRED FUSELAGE SKIN, BS 840, S18R IAW B737 SRM 53-00 -01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008040100090 20080401 00090 EA 2008 4 1 AA6WA200840150 1 20080304 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NLG UNDERSERVICED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 453AW 7838 ON TAKEOFF RECEIVED NWS INOP AND GEAR DISAGREE, COMPLIED WITH QRH. GEAR DISAGREE ILLUMINATED APPROX 30 SECS. AFTER GEA R UP SELECTION. RETURNED FOR LANDING, LANDING WEIGHT= 41,000 LBS., MAX BTMS=2,2,2,2. SERVICE NOSE GEAR STRUT IAW 12-12 -32 OPS CHECK GOOD, GEAR SWING GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008033100080 20080331 00080 NM 2008 3 31 AMTA200800162 1 20080228 A 5340 ATTACH FITTING BOEING 737 73783N 13844HI NM LAVATORY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 FWD LAVATORY AFT IB MOUNTING BLOCK HAS SURFACE CORROSION. REPLACED MOUNTING BLOCK PN C23102-745-005 AND 2 EA BLOCK FLOO R PN C22102-155-101 IAW MM 25-46-99, REPAIR 2, PAGE 11. 2 L 7 2 4F RT A16WE 2008033100093 20080331 00093 NM 2008 3 31 AMTA200800175 1 20080228 A 5730 SKIN PANEL BOEING 737 73783N 13844HI NM LT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LT WING FUEL TANK ACCESS 532EB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROS ION ON LT WING FUEL TANK ACCESS LANDING 532EB IAW, SRM 51-20-02-0G, ORG MAT .204, MAT LOSS .001, REM MAT .203, FOUND TO BE WITHIN LIMITS IAW SRM 57-20-01-1A-1, PERFORMED FLAP PEENING IAW SRM 51-20-06 AND SOPM 20-10-03. (K) 2 L 7 2 4F RT A16WE 2008032800120 20080328 00120 NM 2008 3 28 UPS08551883 1 20080318 A 5610 SLIDING WINDOW BOEING 757 75724APF 1384969 NM COCKPIT BINDING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 475UP 28845 INSPECTION TYPE:N/A CAPTAIN'S SLIDING WINDOW BINDING (WILL NOT CLOSE). CLEANED, LUBED AND PERFORMED ADJUSTMENT TEST WIT H REF TO 56-11-02-5. OPS CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2008032800123 20080328 00123 NM 2008 3 28 UPS08551889 1 20080318 A 3350 67410312113 LENS BOEING 757 75724APF 1384969 NM COCKPIT BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 406UP 23728 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT LENS ASSY BROKEN. REMOVED AND REPLACED LIGHT LENS ASSY. 2 L 7 2 4F RT A2NM 2008032800126 20080328 00126 WP 2008 3 28 UPS08851892 1 20080227 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 RIVET HEAD MISSING ON LT FUSELAGE NOSE SECTION EXTERNAL SKIN. REPAIRED LT FUSELAGE NOSE SKIN IAW SRM 53-02-00, SRM 53-3-3 FIG 1, SRM 53-02-1 FIG 7 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 2008032800127 20080328 00127 WP 2008 3 28 UPS08851893 1 20080303 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP CABIN GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK GOUGED STA 415 RBL 24. REPAIRED MAIN CABIN SEAT TRACK AT STA 415 AND RBL 24 IA W SRM 53-02-03-0 FIG 012 AND FIG 006D. 2 L 7 4 4F RT 4A25 2008032800131 20080328 00131 EU 2008 3 28 UPS08151887 1 20080318 A 7830 ACTUATOR AIRBUS A300 A300F4622R 3930360 EU THRUST REVERSER MALFUNCTIONED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 168UP 0005 INSPECTION TYPE:N/A ATB - NR 2 ENG THRUST REVERSER UNLOCK LIGHT ILLUMINATED. CREW RETURNED TO SAT. ITEM DEFERRED PER M EL M371635 ASSIGNED. REMOVED AND REPLACED NR 2 T/R INBOARD MASTER ACTUATOR PER MM 78-31-15-04. ALL CHECKS GOOD PER SAM E THIS CLEARS M371635. 2 L 7 2 4F RT A35EU 2008032800132 20080328 00132 NM 2008 3 28 UPS08651895 1 20080319 A 2613 ELEMENT BOEING 767 76734AF 1385212 NM LT ENGINE DEFECTIVE A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 318UP 27746 INSPECTION TYPE:ETOP DIVERSION - DURING CLIMBOUT A LEFT ENGINE DUCT LIGHT ILLUMINATED THE CREW RAN THE CHECKLIST CONTACT ED DISPATCH, BUT WERE UNABLE TO CONTINUE TO BFI DUE TO ICING CONDITIONS. FLIGHT LANDED WITHOUT INCIDENT IN RFD. REMOVE D AND REPLACED LEFT WING DUCT LEAK SENSOR ELEMENT IAW MM 26-18-01-4. OPS CHECK LEAK SENSOR SYSTEM IAW MM 26-18-01-4. O PS CHECK GOOD. 2 L 7 2 4F RT A1NM 2008032800138 20080328 00138 NM 2008 3 28 SWAA081575 1 20080323 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 763SW 27877 DURING SCHEDULED 8Y CHECK, FOUND AFT CABIN EEPLS INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008032800142 20080328 00142 NM 2008 3 28 SWAA081581 1 20080324 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER 4R CRACKED AT BS 500. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008032800143 20080328 00143 NM 2008 3 28 SWAA081582 1 20080324 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032800150 20080328 00150 NM 2008 3 28 SWAA081590 1 20080324 A 5320 6517582 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED SPV CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178, LBL 17, WL 217. REPAIRED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2008032800152 20080328 00152 NM 2008 3 28 SWAA081592 1 20080324 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 L1 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008032800163 20080328 00163 WP 2008 3 28 UPS08851934 1 20080325 A 5210 CONTROL CABLE DOUG DC8 DC873F 302199F WP PAX DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 CREW ENTRY DOOR WILL NOT OPEN. REPLACED LOWER HINGED SEAL PUSH/PULL CONTROL CABLE AND ADJUSTED PER MM 52-11-01-5. PRESS URIZED A/C. NO LEAKS NOTED ON FWD ENTRY DOOR AND LOWER SEAL. 2 L 7 4 4F RT 4A25 2008032800164 20080328 00164 GL 2008 3 28 C2XA08ON107 2 20080321 A 7200 AE3007A1E ENGINE EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 13202 4610 4610 14500962 CAE312917 FLT 0224 - SMF - FLIGHT CREW REPORTED SMOKE IN THE COCKPIT WHILE CLIMBING; AIRCRAFT RETURNED TO BLOCK; FLIGHT CREW DID N OT DECLARED EMERGENCY; AIRCRAFT LANDED SAFELY. MX PERSONNEL REMOVED AND REPLACED NR 1 ENGINE OPERATIONALLY CHECKED SATI SFACTORY. AIRCRAFT WAS RELEASED TO RETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2008032800165 20080328 00165 NM 2008 3 28 SWAA081603 1 20080325 A 2761 65C25255 FITTING BOEING 737 7373H4 1384600 NM SPOILER ACTUATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND RIGHT WING NR 5 SPOILER INBOARD ACTUATOR FITTING WORN. REMOVED AND REPLACED FITTING P ER MM. 2 L 7 2 4F RT A16WE 2008032800167 20080328 00167 NM 2008 3 28 SWAA081604 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032800172 20080328 00172 NM 2008 3 28 SWAA081609 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032800179 20080328 00179 NM 2008 3 28 SWAA081644 1 20080325 A 5312 6545819 PRESSURE PANEL BOEING 737 7375H4 138449D NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT LBL 7.75. REPAIRED PANEL PER ACO. 2 L 7 2 4F RT A16WE 2008032800181 20080328 00181 NM 2008 3 28 SWAA081639 1 20080325 A 5523 65C26384 TAB BOEING 737 7375H4 138449D NM LT ELEVATOR DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND LT ELEVATOR TAB DISBONDED AT NR 1 UPPER HINGE CUTOUT. REPAIRED TAB PER ER. 2 L 7 2 4F RT A16WE 2008032800191 20080328 00191 2008 3 28 SWAA081602 4 20080325 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM EVAC SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 2008032800194 20080328 00194 NM 2008 3 28 SWAA081619 1 20080325 A 5311 6546550 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032800195 20080328 00195 NM 2008 3 28 SWAA081627 1 20080325 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 761RR 27875 DURING SCHEDULED 8Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 128. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032800196 20080328 00196 SO 2008 3 28 RAIA0803017 1 20080321 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 844HK 14500838 PRE FLT 8018 - IAD - EMERGENCY LIGHT FLOOR STRIP AT SEAT 17A INOPERATIVE. MAINTENANCE SECURED EMERGENCY LIGHT STRIP. S YSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008032800198 20080328 00198 SO 2008 3 28 RAIA00803018 1 20080323 A 5210 MECHANISM EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A RAIA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 03 822HK 145069 FLT 5506 - STL - PASSENGER DOOR DIFFICULT TO OPEN AND CLOSE. MAINTENANCE LUBRICATED THE DOOR OPERATING MECHANISM. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008032800204 20080328 00204 EA 2008 3 28 A6WA200840116 1 20080216 A 5344 HINGE CNDAIR CL600 CL6002B19 1900309 EA STOW PLATE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 430AW 7719 CARGO STOW PLATE, FWD, MID AND AFT HINGES ARE CRACKED. CARGO STOW PLATE REPLACED IAW SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2008032800205 20080328 00205 EA 2008 3 28 A6WA200840117 1 20080216 A 5310 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 430AW 7719 FOUND CRACK EXIST ON PASSENGER DOOR EDGE MEMBER FORWARD. REPAIR ON PASSENGER DOOR EDGE CARRIED OUT IAW REO 601R-52-11-2 79. (M) 2 L 7 2 4F RT A21EA 2008032800211 20080328 00211 WP 2008 3 28 IXXA08SMN048S 1 20080201 A 5522 SKIN DOUG DC8 DC871F 302199D WP LT ELEVATOR DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND LT ELEVATOR UPPER SKIN SHOWS DENTS AND CORROSION AT SEVERAL POINTS BETWEEN STAT ION XE 50.000 AND STA XE 132.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMI TS. REMOVED DAMAGED SKIN. FABRICATED SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. BALANCED AND FOUND TO BE WITHIN LIMITS WITH A MOMENT OF 1473.4 INCH-POUND. INSTALLED NEW FASTENERS A ND REPAIR PARTS IAW SRM 51-1-11, SRM 55-4-1 FIGURE 1 SHEET 1-2 ITEM "E" AND "F", SRM 51-1-8 PAGE 17-18, DC8 SRM 55-2-0 P AGE 12, SRM 55-1-0 PAGE 1, SRM 51-1-21, SRM 51-1-9, T/R NUMBER 51-142, SRM 51-1-9A, T/R 51-141, SRM 51-1-8B, AND SRM 51- 2 L 7 4 4F RT 4A25 2008033100009 20080331 00009 WP 2008 3 31 UPS08851932 1 20080303 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 FLOORBOARD SUPPORT CRACKED AT FWD CARGO PIT STA 520 BETWEEN L34R AND 33R. REMOVED DAMAGED AREA, FABB ED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-21A, 51-1-8, 51-1-24, 53-2-00. 2 L 7 4 4F RT 4A25 2008033100015 20080331 00015 NM 2008 3 31 SWAA081655 1 20080326 A 3350 100031 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 RIGHT OVERWING EMERGENCY EXIT LIGHT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2008033100017 20080331 00017 WP 2008 3 31 08FDEA00981 1 20080317 A 5321 AGA386315 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 AFT PIT FLOOR PANEL NR 187 KF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL 187 KF; POTTED EDGES; COM PLETED CURE AND SANDED EDGE POTTING. INSTALLED INSERTS AND FABRICATED TOP SHEET. LAY-UP PLACED UNDER VAC BAG; COMPLETE D CURE; COUNTERED SINK HOLES AND APPLIED NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008033100019 20080331 00019 NM 2008 3 31 SWAA081663 1 20080326 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008033100028 20080331 00028 WP 2008 3 31 08FDEA00988 1 20080317 A 5321 AGA38653 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 AFT PIT FLOOR PANEL NR 187 CF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL NR 187 CF. LOCATED HOLES ; POTTED EDGES; COMPLETED CURE; SANDED EDGE POTTING AND INSTALLED INSERTS. FABRICATED TOP SHEET; LAYED UP UNDER A VAC BAG; COMPLETED CURE; COUNTER SUNK HOLES AND APPLIED NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C. 2 L 7 3 4F RT A22WE 2008033100030 20080331 00030 WP 2008 3 31 08FDEA00989 1 20080317 A 5321 AGA387715 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 AFT PIT FLOOR PANEL NR 187 FF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL NR 187 FF. LOCATED HOLES ; POTTED EDGES; COMPLETED CURE; SANDED EDGE POTTING AND INSTALLED INSERTS. FABRICATED TOP SHEET; LAYED UP UNDER A VAC B AG; COMPLETED CURE; COUNTER SUNK HOLES AND APPLIED NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008032700195 20080327 00195 WP 2008 3 27 08FDEA01097 1 20080321 A 5320 ADA71121 CLAMP DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 IN THE AFT FUSELAGE COMPARTMENT, UPPER TORQUE BOX AREA, ABOVE LONGERON 4R HAS A CRACKED ELECTRICAL CLAMP. REMOVED ELECT RICAL CLIP THAT WAS DAMAGED IAW SRM 51-35-01 VOL II. REMOVED DAMAGED AREA ON THE CLIP IAW SRM 53-00-01 VOL I PG 4B VIEW A. ALODINED & PRIMED ELECTRICAL CLIP IAW SRM 51-21-01 VOL II. INSTALLED CLIP IAW SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2008032700207 20080327 00207 EU 2008 3 27 2008UALA01476 1 20080316 A 3350 321452 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 406UA 454 DURING EMERGENCY LIGHT TEST R BATTERY FAULTED. BATTERY FAILURE. REPLACED R EMER LIGHT BATTERY. OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008032700218 20080327 00218 NM 2008 3 27 2008UALA01481 1 20080316 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT SEAT 50 RT INOP. RESECURED CONNECTOR. OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008032700231 20080327 00231 NM 2008 3 27 2008UALA01488 1 20080315 A 3350 582233 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 656UA 25394 ALL FOUR INTERIOR OVERWING EMERGENCY EXIT SIGNS INOP. REPLACED BATTERY PACK. OPS CHK'D OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2008032700237 20080327 00237 NM 2008 3 27 2008UALA01491 1 20080316 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 225UA 30554 EMERGENCY LIGHT INOPERATIVE AT SEAT 39G. RELAMPED EMERGENCY LIGHT, CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008032700249 20080327 00249 EU 2008 3 27 08FDEA01133 1 20080324 A 5730 A5735003900000 PANEL AIRBUS 310 A310203 3930313 EU RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT WING FUEL PANEL 650LB HAS FITTING CORROSION ON THE INNER BOLT HOLES. FUEL PANEL WAS FOUND TO BE OUT OF LIMITS REF A310-200 SRM 57-20-16; FIG 103; SHEET 4, TO BE INSTALLED ON FEDEX WIC 46X5042ALI. 2 L 7 2 4F RT A35EU 2008032700250 20080327 00250 NM 2008 3 27 2008UALA01528 1 20080318 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 INTERCOSTAL IS CRACKED AT FWD I/B CORNER BS 294.5 AT STR 7L. 2 L 7 2 4F 4 F RT A16WE E21EU 2008032700260 20080327 00260 NM 2008 3 27 AALA200800492 1 20080304 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 966AN 30094 MIA - EMERGENCY LIGHT AT SEAT ROW 27 LENS BROKEN. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 27. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008032700273 20080327 00273 NM 2008 3 27 AALA200800506 1 20080304 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 921AN 29522 MIA - EMERGENCY LIGHT AT SEAT ROW 27 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 27. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008032700276 20080327 00276 SO 2008 3 27 C2XA08CL038 1 20080324 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 21537 145523 DURING ROUTINE MAINTENANCE THE MAIN CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LAMP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008032700303 20080327 00303 NM 2008 3 27 DHL2008763522 1 20080302 A 5311 FRAME BOEING 727 727264 138408M NM BS 660 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 FRAME DENTED AND GOUGED IN CARGO COMPT AT BS 660, ABOVE STR 17R. CUT OUT DAMAGE, FABRICATED FRAME REPAIR, AND INSTALLED PER B727 SRM 51-40-3 FIG 1, 53-10-2 FIG 3, AND 51-30-2. 2 L 7 3 4F A3WE 2008032700325 20080327 00325 SO 2008 3 27 C2XA08IA085 1 20080319 A 5210 14548868407 PANEL EMB 145 EMB145XR 3260214 SO PAX DOOR LOOSE A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 18102 145643 COS - FLIGHT 2422, THE CREW REPORTED THAT THE MAIN CABIN DOOR WOULD NOT OPEN FULLY. CONTRACT MAINTENANCE RE-SECURED A L OOSE INTERIOR DOOR PANEL, OPERATIONALLY CHECKED THE DOOR WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008032700342 20080327 00342 2008 3 27 HALA0800417 4 20080323 A 3140 8221033100 COMPUTER BOEING 767 7673G5 1385126 NM COCKPIT INOPERATIVE A HALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 584HA 24258 ATB - L EICAS COMPUTER WENT INOP JUST PRIOR TO DINTY. REMOVED AND REPLACED LEFT COMPUTER IAW 31-41-01. LOAD SOTWARE IA W 31-41-02, PERFORMED BITE. OPS CHECK NORMAL, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008032700355 20080327 00355 NM 2008 3 27 XXUA200800007 1 20080321 A 3350 767 LIGHT BOEING 757 7572Q8 1384972 NM PWA PW2037 PW2037M 52117 NE EXTERIOR INOPERATIVE A XXUA K NONE L NO TEST IN INSP/MAINT 1 EA 15 401JS 26332 R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED OPERATION NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008032700356 20080327 00356 NM 2008 3 27 AALA200800528 1 20080308 A 3350 SHROUD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 606AA 27057 DFW - EMERGENCY LIGHT AT SEAT 17D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008032700386 20080327 00386 WP 2008 3 27 AALA200800531 1 20080309 A 3350 SHROUD DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 DFW - EMERGENCY LIGHT AT SEAT 15D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008032700391 20080327 00391 WP 2008 3 27 AALA200800532 1 20080309 A 3350 SHROUD DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 DFW - EMERGENCY LIGHT AT SEAT 26D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008030600086 20080306 00086 2008 3 6 MWEA080036 4 20080224 A 2565 645343 SLIDE DOUG MD88 MD88 3023688 NM TAILCONE FAILED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 701ME 49760 DURING TAIL CONE SLIDE DEPLOYMENT CHECK, TAIL CONE SLIDE DID NOT DEPLOY & FOUND STRAPS INSIDE OF SLIDE COVER NOT CONNECT ED. REMOVED AND REPLACED TAIL CONE SLIDE. 2 L 7 2 4F RT A6WE 2008030600088 20080306 00088 SO 2008 3 6 RAIA00802023 1 20080222 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145 3260210 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 809HK 145187 PRE FLT 7969 - STL - OVERWING EMERGENCY EXIT LIGHTS AND FLOOR STRIP LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE NR 3 EMERGENCY LIGHT POWER SUPPLY. A SUCCESSFUL OPERATIONAL CHECK OF THE SYSTEM WAS COMPLETED AFTERWARDS. 2 L 7 2 4F RT T00011AT 2008030600092 20080306 00092 SO 2008 3 6 RAIA00802019 1 20080218 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN UNSECURE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 819HK 145062 PRE FLT 5559 - STL - EMERGENCY LIGHTS INOP AT ROW 17. MAINTENANCE RESECURED THE WIRING TO THE FLOOR PROXIMITY STRIP. P ERFORMED OPERATIONAL CHECK WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008030600106 20080306 00106 2008 3 6 SWAA081051 4 20080225 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008030600117 20080306 00117 NM 2008 3 6 2008UALA00942 1 20080219 A 3350 OL3071BPEGPL LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 530UA 25043 EXTERIOR EMERGENCY LIGHTS AT DOOR 2R AND AFT PIT DOOR ARE INOP. LAMPS INOP. RELAMPED ASSY, OPS CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030600119 20080306 00119 NM 2008 3 6 2008UALA00957 1 20080220 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN MALFUNCTIONED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 850UA 1653 EMERGENCY EXIT LIGHTS ARE ON. RESET CIDS AND NORMAL OPS RETURNED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030600123 20080306 00123 EU 2008 3 6 2008UALA00969 1 20080219 A 3250 4502310000600U PRESSURE SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG LEAKING A UALA D RETURN TO BLOCK W K INADEQUATE Q C FLUID LOSS TX TAXI/GRND HDL 1 WP 29 420UA 489 HYD G SYS LO PR LOST NW STEERING. NWS SYSTEM PRESSURE SWITCH LEAK. REPLACED NWS ELECTRICAL BOX WITH THE SYSTEM PRESSUR E SWITCH. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030600126 20080306 00126 NM 2008 3 6 2008UALA00975 1 20080221 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 385 SCRATCHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 EXTERNAL FUSELAGE SKIN HAS SCRATCHES, BS 385 AT AND ABOVE 3L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA. ACP INSU RANCE CUT OF 0.040". FABRICATED & INSTALLED EXTERNAL DOUBLER & STRUCTURAL FILLERS REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030600127 20080306 00127 NM 2008 3 6 2008UALA00976 1 20080221 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FUSELAGE FRAME SHEAR TIE IS CRACKED BS 360 BELOW STRINGER 14L. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030600128 20080306 00128 NM 2008 3 6 2008UALA00977 1 20080221 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 DOOR 2L UPPER HINGE ARM CUTOUT REQUIRES DOUBLER. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030600142 20080306 00142 NM 2008 3 6 2008UALA00988 1 20080221 A 5321 FLOORBOARD AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CARGO BAY DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 801UA 686 CARGO FLOORBOARD RPL S GLS PNL. MAJOR REPAIR ACCOMPLISHED AT LCQ (COA ACCOMPLISHED). 2 L 7 2 4F 4 F RT A28NM E40NE 2008030500020 20080305 00020 NM 2008 3 5 QXEA200802067 1 20080101 A 5740 BRACKET DHAV DHC8 DHC8202 2809007 NM LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - LEFT WING LOWER LEADING EDGE BRACKET IS CRACKED YW 139.0. REMOVED BRACKET AND INSTALL NEW BRACKET REF -8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008033100094 20080331 00094 EU 2008 3 31 08FDEA01148 1 20080326 A 5320 A59374322230 FLOOR SUPPORT AIRBUS 300 A300B4622 3930401 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 720FD 417 BULK CARGO COMPT FR 69 FLOOR SUPPORT CORRODED LBL20 AND TIE DOWN FITTING MISSING. REMOVED DAMAGED FLOOR CROSS BEAM IAW SRM 51-40-21. RECEIVED NEW FLOOR CROSS BEAM P/N NR A59374322230 BATCH NR 0001436243. LOCATED AND DRILLED IAW SRM 51-40 -44. INSTALLED AND SEALED IAW SRM 51-76-10 AND SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008033100096 20080331 00096 NM 2008 3 31 AMTA200800177 1 20080228 A 5730 SKIN PANEL BOEING 737 73783N 13844HI NM LT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LT WING FUEL TANK ACCESS 532BB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROS ION ON LT WING FUEL TANK LANDING IAW B737-800 SRM 51-10-02-0G, ORG AT .207, MAT LOSS .005, REM MAT .202, FOUND TO BE WIT HIN LIMITS IAW SRM 57-20-01-1A-1, PERFORMED FLAP PEENING IAW SRM 51-20-06 AND SOPM 20-10-03. (K) 2 L 7 2 4F RT A16WE 2008033100108 20080331 00108 NM 2008 3 31 AMTA200800184 1 20080228 A 5320 STRAP BOEING 737 73783N 13844HI NM BS 727-787 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 RT SIDE STRAP OF AFT CARGO COMPARTMENT FROM STA 727 TO 787 HAS CORROSION. REMOVED CORROSION, ORG MAT .063, MAT LOSS .00 4, REM MAT .059, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53-1A. (K) 2 L 7 2 4F RT A16WE 2008033100118 20080331 00118 NM 2008 3 31 AMTA200800197 1 20080301 A 5347 RAIL BOEING 737 73783N 13844HI NM BS 767 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 RAIL ASSY LBL 17.24, STA 767 HAVE A LIGHT CORROSION, AFT CARGO COMPARTMENT AREA. REMOVED CORROSION ON RAIL, ORG MAT .07 1, MAT LOSS .017, REM MAT.054, FOUND TO BE OUT LIMITS IAW SRM 53-00-53-1A DETAILED FABRICATED REPAIR PART FROM BAC 1509- 100688 IAW EA 737-5300-08-A0036. (K) 2 L 7 2 4F RT A16WE 2008033100130 20080331 00130 NM 2008 3 31 AMTA200800209 1 20080306 A 5320 SUPPORT FITTING BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 608 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 520AT 27976 SUPPORT FITTING ON FWD CARGO DOOR SILL CORRODED AR BS 608, BL25R. REMOVED AND REPLACED SUPPORT FITTING PN 69-45555Y10 I AW SRM 510-40-02. 2 L 7 2 4F 4 F RT A2NM E12EU 2008033100131 20080331 00131 NM 2008 3 31 AMTA200800210 1 20080306 A 5320 FLOOR SUPPORT BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE BS 1640-1681 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 520AT 27976 CORROSION AROUND ALL FASTENER HOLES ON OB FLOORBOARD SUPPORT JUST IB OF L-4 DOOR LWR SILL BS 1640-BS 1681.8, LBL 58.22. FOUND CORROSION ON LOWER AFT SILL SECTION OUT OF LIM SRM 53-60-15 DET V BLEND CORROSION LEW SILL FWD SECT IN LIM IAW SR M 53-60-15 TREATED 51-40-01. REPAIRS AFT SECTION AT STA 1661 TO 1681, LBL 65 51-P40-02. FAB AND INST REP SRM 51-40-02. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008033100137 20080331 00137 EU 2008 3 31 COEA0801912 1 20080301 A 3397 6018YY20 WIRE HARNESS AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE TAIL CONE WORN A COEA O OTHER O OTHER CR CRUISE 1 NM 13 912FX 047 OVER FLY. FLT NR 7202, ENROUTE, THE NAVIGATION LIGHT CIRCUIT BREAKERS ALL POPPED. THE CREW ATTEMPTED TO RESET THE CIRCU IT BREAKERS BUT THEY WOULD NOT STAY IN. A DECISION WAS MADE TO OVER FLY AND CONTINUE TO OTHER DESTINATION FOR MAINTENAN CE. NO EMERGENCY WAS DECLARED AND THE PLANE LANDED NORMALLY AND SAFELY. MAINT FOUND A BARE SPOT IN WIRE NR 6018`S INSU LATION NEXT TO THE VARISTOR FOR THE TAIL NAVIGATION LIGHT. REMOVED DAMAGED SECTION AND INSERTED A SPLICE IN WIRE NR 601 8 TO THE TAIL NAVIGATION LIGHT. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008033100169 20080331 00169 SO 2008 3 31 SWIA200819387 1 20080320 A 5210 DOOR EMB 120 EMB120ER 3260203 SO PAX DOOR OUT OF ADJUST A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 224SW 120294 FLT 5442 - PAX DOOR IS DIFFICULT TO OPEN AND CLOSE. ADJUSTED AND LUBED CABIN DOOR. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 2008033100194 20080331 00194 NM 2008 3 31 AALA200800598 1 20080311 A 2910 EM91805 SHUTOFF VALVE BOEING 767 767323 1385205 NM HYDRAULIC SYS LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 352AA 24033 DFW INFLIGHT T2473/11MAR - RIGHT HYDRAULIC SYSTEM FLUID LOSS DURING CLIMB. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT HAND WING LATERAL CONTROL SHUT OFF VALVE AND SERVICED HYDRAULIC RESERVOIR. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008033100229 20080331 00229 NM 2008 3 31 QXEA200800327 1 20080320 A 5315 FLOORBEAM DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX -C4- CORROSION FOUND ON RT FLOORBEAM CASTELLATION AT STA 565. REMOVED FIVE RIVETS FROM CASTELLATION AND BLENDED OUT CORROSION REF CPCM CHAPTER 4. HFEC INSPECTED BLEND AREA FOR CRACKS IAW NDTM PART 6, 51-00-01, NO CRACKS NOTED. UT THI CKNESS CHECK OF BLENDED AREA IAW NDTM PART 1, 51-00-04 HIGH .050 LOW .047. AREA OF BLEND WITHIN LIMITS PER SRM 51-20-11 . APPLIED ALODINE AND PRIMER IAW SRM 51-20-16 AND 51-20-36. INSTALLED RIVETS IN CASTELLATION REF SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008033100238 20080331 00238 WP 2008 3 31 DHL2008805525 1 20080310 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 AFT CARGO COMPT BILGE FITTING CRACKED 2" STA 1300.000 L-32R TO L-33R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53- 1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2008033100245 20080331 00245 NM 2008 3 31 2008747001 1 20080321 A 5753 652163261 WEDGE BOEING 727 727224 1384076 NM T/E FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 747DH 22253 UPON INSPECTION TO THE EXTERIOR OF THE AIRCRAFT, FOUND THE LEFT INBOARD TRAILING EDGE MIDFLAP WEDGE DELAMINATED AT WBL 2 03.0 4 1/2 BY 2 1/2 AREA OF DELAMINATION. REPAIRED BY FLIGHTSTAR AIRCRAFT SERVICES USING BOEING SRM 51-40-20,51-50--2 A ND 51-40-21. THIS IS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008033100276 20080331 00276 NM 2008 3 31 DL76G080409 1 20080326 A 5315 BAC1505100774 FLOORBEAM BOEING 767 7673P6 1385105 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 155DL 25269 FLOORBEAM CORRODED AT STA 654+121 AT RBL 30 TO RBL 51. FLOORBEAM REPLACED PER 53-00-51D FIGURE 201 ON NR AVM511426. 2 L 7 2 4F RT A1NM 2008033100296 20080331 00296 NM 2008 3 31 DLM90080429 1 20080306 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 LT CABIN CUSP WEB FS 1358 CRACKED AT LIGHTNING HOLE. REPAIRED LT CABIN CUSP WEB AT STA 1358, IAW MD9 SRM 51-11-01, TAGG ED, IAW DELTA PROCESS STANDARD 900-5-1 NR 4. 2 L 7 2 4F RT A6WE 2008033100303 20080331 00303 EU 2008 3 31 MALA080046 1 20080221 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 340B453 PON4K FUSELAGE, FORWARD LAVATORY, SEAT TRACK CORRODED. REPLACED SEAT TRACK WITH NEW P/N 7253721-495 IAW SRM 51-40-21. EXELTECH NR 2083. 2 L 7 2 4T RT A52EU 2008040100010 20080401 00010 EU 2008 4 1 08FDEA01161 1 20080327 A 5347 A5383202020400 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 658FE 752 MCDD FLOOR SEAT TRACK NR 3 RT INBD FLANGE HAS CORROSION 4 AREAS BETWEEN FR 40 AND FR 42 REMOVED LEVEL 1 CORROSION BY REM OVED AND REPLACED SEAT TRACK SECTION FROM FR 40 TO FRAME 46, NR 3 RT. 2 L 7 2 4F RT A35EU 2008040100015 20080401 00015 WP 2008 4 1 IXXA08SMN035S 1 20080201 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR SIDE SKIN LAP JOINT FORWARD OF AFT PRESSURE BULKHEAD AT LONGERO N 28. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, FINGER DOUBLERS, FILLER. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8100-9 DATED 02-14-08, AD 2007- 02-02, S/B DC8-53A080 DATED 06-22-04, DRAWING DOUGLAS SR08530032 AND BOEING SKETCH 200802070028-0001, DC8 SRM 51-1-21, 5 1-3-0, 51-1-20D, AND DC8 NDT SPM PART 06-10-01-.001. 2 L 7 4 4F RT 4A25 2008040100036 20080401 00036 NM 2008 4 1 TAMF20080013S 1 20080313 A 5246 DOOR BOEING 767 767200 1385120 NM GE CF6 CF680 30025 NE WING FUEL CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 770QT 23802 DURING C2 CHECK INSPECTION WAS FOUND CORROSION ON MAIN FUEL TANK ACCESS DOORS 541LB AND 541GB PN: 112N6101-3. DAMAGED A REA WAS BLENDED TO A MINIMUM DOOR THICKNESS OF 0.120 INCHES (541LB) AND 0.106” INCHES (541GB). NDT (EDDY CURRENT) INSPEC TION WAS PERFORMED AND NONE ADDITIONAL DAMAGES WERE FOUND AFTER BLENDING. BLENDED AREA WAS FLAP/ROTO PEENED AND ORIGINAL FINISHES WERE RESTORED. THOSE ACTIONS WERE PERFORMED IAW EWO 767 57-040 AND MFG SERVICE REQUEST 1-789704880. THIS REPAI R CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2008040100043 20080401 00043 NM 2008 4 1 SB08014 1 20080319 A 2910 HYDRAULIC LINE BOEING 737 7374B7 1384702 NM LT MLG WW BLOWN A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 435US 24557 MCO - FLT1926 - ON LIFTOFF AND GEAR RETRACTION OUT OF MCO, CREW LOST A SYSTEM HYDRAULICS AS LOW PRESSURE LIGHTS ILLUMINA TED. PUMPS WERE LEFT ON ABOUT FIVE MINUTES AFTER THE LOW PRESSURE LIGHTS ILLUMINATED. FLUID WAS DEPLETED. CREW DECLAR ED AN EMERGENCY AND RETURNED TO FIELD AT MCO WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A TEMPORARY FLEX LINE INSTALLE D IN THE LEFT WHEELWELL/WING ROOT AREA THAT HAD BLOWN. REPLACED TEMPORARY HYDRAULIC LINE AND INSPECTED FILTERS FOR DEBR IS. NONE FOUND. FLUSHED A SYSTEM HYDRAULIC LINES AND REPLACED FILTERS. ALSO, REPLACED A SYSTEM ELECTRIC MOTOR DRIVEN PUMP PER MM 29-15-22. SERVICED HYDRAULIC SYSTEM RESERVOIR TO FULL. LEAK CHECK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008040100056 20080401 00056 EU 2008 4 1 USAA920080669 1 20080323 A 2433 Y0053 TRANSFORMER AIRBUS 320 A320232 3930326 EU NR 2 DEFECTIVE A USAA O OTHER G MULTIPLE FAILURE AP APPROACH 1 EA 19 672AW 236 21 2193 FLT NR 188 - TPA-PHX - EMERGENCY LANDING, AIRCRAFT EXPERIENCED A DC BUS 2 FAULT. AFTER ONE RESET, THE FAULT REOCCURRED. DUE TO SLOW SLATS AND FLAPS, THE LOSS OF ONE REVERSER AND THE AUTOBRAKE SYSTEM, CREW DECLARED AN EMERGENCY ON APPROACH TO PHX RUNWAY 08. A NORMAL LANDING WAS REPORTED. MAINTENANCE REMOVED AND REPLACED CONTACTOR 3PX, RELAY 6XX, DIODE 242 0 VD, NO HELP. REPLACED THE NR 2 TRANSFORMER RECTIFIER AND OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008040100066 20080401 00066 NM 2008 4 1 USAA920080658 1 20080227 A 5315 6545410155 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FLOORBEAM CHORD, BS 663, LBL 24, WL 208. REPAIRED FLOORBEAM CHORD, BS 663, LBL 24, WL 208 IAW USAIRWAYS EA 100301. 2 L 7 2 4F RT A16WE 2008040100095 20080401 00095 EU 2008 4 1 USAA920080676 1 20080313 A 5347 D57130147200 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 621AW 53 SAL - MAJOR REPAIR - C6 CHECK - CORROSION ON CABIN SEAT TRACK, BS 1641/FR 37 - BS 1810/FR 41, -Y765. REPLACED CABIN SEA T TRACK, BS 1641/FR 37 - BS 1810/FR 41, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008040100097 20080401 00097 EA 2008 4 1 A6WA200840154 1 20080305 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 310-349 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 SERVICE DOOR LOWER SILL PLATE CORRODED. BLENDED IAW SRM 51-21-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008040100100 20080401 00100 EA 2008 4 1 A6WA200840155 1 20080229 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 PAX DOOR STAIR AFT WEB CRACK ON 1ST AND 2ND STEP CORNER AREA. REPAIRED IAW REO 601R-52-11-702 REV A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008040100103 20080401 00103 NM 2008 4 1 USAA920080696 1 20080321 A 3350 417T5097 POWER SUPPLY BOEING 767 7672B7ER 1385107 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 255AY 25257 BFM - EEL - DROP IN MAINTENANCE - MID LEFT SIDE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY ASSEMBLY IAW B767 A MM 33-51-07. 2 L 7 2 4F RT A1NM 2008040100104 20080401 00104 EA 2008 4 1 A6WA200840157 1 20080305 A 5230 TRACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 CHANNEL TRACK SUPPORT CRACK ON CARGO DOOR TRACK FS 574.0. (K) REPLACED IAW SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008040100105 20080401 00105 2008 4 1 USAA920080697 4 20080322 A 2565 D30665105 SLIDE RAFT AIRBUS A319 A319112 3930323 EU R2 DOOR DEFLATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 714US 22094 1116 1046 PIT - EES - C11 CHECK - R2 DOOR SLIDE FAILED CLEARANCE CHECK. REPLACED R2 DOOR SLIDE IAW USAIRWAYS TASKCARD 26C84252002 . 2 L 7 2 4F RT A28NM 2008040100115 20080401 00115 NM 2008 4 1 SA08017 1 20080322 A 7732 INDICATION SYS AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE VIBRATION DETECT MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 806AW 1056 V10575 PIT - FLT 257 - PHL TO PHX - DURING CRUISE, FLIGHT EXPERIENCED A HIGH, NUMBER TWO ENGINE VIBRATION INDICATION PROBLEM. AIRFRAME VIBRATION WAS NOT DETECTED OR INDICATED. THE CREW REDUCED POWER ON THE NUMBER TWO ENGINE TO IDLE. SINCE AIRSP EED AND ALTITUDE COULD NOT BE MAINTAINED, THE FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE P LACED THE ENGINE VIBRATION INDICATION SYSTEM ON MEL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040100119 20080401 00119 EU 2008 4 1 M7K2008F00000 1 20080204 A 5200 677120600 LATCH UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE DOOR FAILED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 821MH 4134 23319 THIS PART CALLED A SHOCK ABSORBER DEVICE BY THE MFG IS USED TO SEQUENCE THE DOOR LATCHING MECHANISM TO PREVENT DOOR CLOS URE WITH LATCH PINS EXTENDED AND IMPACTS WITH THE DOOR FRAME. IT IS MFG OF A VERY BRITTLE BRONZE TYPE MATERIAL THAT WIL L CRACK WITH JUST THE INSTALLATION OF BLIND RIVETS IN THE COUNTERSUNK HOLES PREDRILLED IN THE PART. CRACKS WERE FOUND E MANITING FROM THE HOLES AT THE RIVETS WITH A CORNER OF THE MOUNTING FLANGE FOUND MISSING. SUGGEST THIS PART BE MFG FROM STAINLESS STEEL FOR BETTER DURABILITY. (K) 1 G 7 2 3U 3 U H9EU E00054EN 2008040100122 20080401 00122 2008 4 1 SA08019 4 20080322 A 2565 D30665105 SLIDE RAFT AIRBUS A319 A319112 3930323 EU SERVICE DOOR BULGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 714US 22095 1117 1046 PIT - THE RIGHT, AFT SERVICE DOOR EMERGENCY ESCAPE SLIDE FAILED A CLEARANCE CHECK. MAINTENANCE REPLACED THE RIGHT AFT S ERVICE DOOR EMERGENCY ESCAPE SLIDE. INSPECTED OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2008030500023 20080305 00023 NM 2008 3 5 QXEA200800112 1 20080119 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - ON RIGHT SIDE OF AIRCRAFT JUST FORE AND AFT OF THE LAV SERVICE DOOR THE FUSELAGE SKIN HAS EVIDENCE OF S CRATCHES. REPAIRED IAW RD 8/4-53-666 AND Q400 SRM 51-14-00-350-803, 51-21-10 AND 51-25-05. 2 H 7 2 4T RT A13NM 2008030500024 20080305 00024 NM 2008 3 5 QXEA200800113 1 20080119 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - LAV SERVICE PANEL APERATURE, DOUBLER IS SEVERELY CORRODED. REPAIRED IAW Q400 RD 8/4-53-347. 2 H 7 2 4T RT A13NM 2008030500035 20080305 00035 NM 2008 3 5 QXEA200800161 1 20080130 A 5320 INTERCOSTAL DHAV DHC8 DHC8202 2809007 NM BS 201 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - SUSPECT CORROSION ON AVIONICS BAY INTERCOSTAL INBOARD AND OUTBOARD SIDES OF INTERCOSTAL AT STATION X201 .15 AND STR 31P. REPAIRED IAW DHC8 200 CPM CHAPTER 4 PG 4-25 PARA 9B(6)(A), DHC8 200 NDTM PT-6 51-00-01, PT-1 51-00-04, AND DHC8 200 SRM 51-20-11, 51-20-16, 51-40-11, 51-20-36 AND 51-20-41. 2 H 7 2 4T RT A13NM 2008030500051 20080305 00051 NM 2008 3 5 QXEA200800125 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 489-509 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - LEFT SEAT TRACK NR 7 BETWEEN FRAME 489.5 TO 509.5 HAS MULTIPLE CHAFES/GOUGES. REPAIRED IAW RD8/4-53-8 84, Q400 NDTM PT-6 51-00-01, AND Q400 SRM 51-21-10 2 H 7 2 4T RT A13NM 2008030500081 20080305 00081 NM 2008 3 5 QXEA200802086 1 20080101 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM BS 202 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - RIGHT INBOARD SEAT TRACK AFT SCREW HOLE FOR THE LAV ATTACH POINT HAS CORROSION AROUND THE HOLE APPROXIM ATELY STATION X202.0. REMOVED SEAT TRACK AND INSTALLED NEW TRACK FROM STOCK IAW RD8-53-1102, RD8-53-4473 AND-8 200 SRM 51-54-11 AND 51-40-11. 2 H 7 2 4T RT A13NM 2008030500086 20080305 00086 NM 2008 3 5 QXEA200802081 1 20080101 A 5320 FLOOR SUPPORT DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 348PH 484 PDX - C5 CHECK - THERE IS CORROSION ON THE OUTBOARD CLOSET FLOOR SUPPORT CHANNEL. REPAIRED IAW -8 200 SRM 51-40-11, 51- 20-11, -8 CPCM CHAPTER 4 PARA 8, AND NDTM 1-82-7A PT 6, 51-00-02 AND PT 1 51-00-04, RD8-53-9952. 2 H 7 2 4T RT A13NM 2008030500090 20080305 00090 NM 2008 3 5 QXEA200800135 1 20080119 A 5753 SKIN BOMBDR DHC8 DHC8402 1390042 NM TE FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - RIGHT INBOARD FLAP HAS A CHAFE SPOT ON THE UPPER SURFACE APPROXIMATELY 6 INCHES OUT FROM INBOARD END AN D 19 INCHES UP FROM THE TRAILING EDGE. BLENDED OUT CHAFE WITH SCOTHBRITE PAD, FOUND TO BE IN LIMITS IAW Q400 SRM 57-51- 30 PG 102. INSPECTED IAW Q400 NDTM PT-6 51-00-01, PAINTED IAW Q400 SRM 51-25-05 PG 206 PARA F(1)-(4). 2 H 7 2 4T RT A13NM 2008030500136 20080305 00136 NM 2008 3 5 QXEA200800115 1 20080119 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM BS 220-230 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - MILD SURFACE CORROSION ON RIVETS AND SKIN UNDER CABIN FLOOR AT STA X220.0 THROUGH STATION 230.0 STR 31 LEFT. REMOVED 17 CORRODED RIVETS IN STR 31S, AND CLEANED AREA AND FOUND NO CORROSION ON SKIN. INSTALLED 17 RIVETS IAW DASH 8 Q400 SRM 51-42-05 PG 201-218, PRIMED AREA IAW DASH 8 Q400 SRM 51-25-10 PG 201-205. 2 H 7 2 4T RT A13NM 2008030500144 20080305 00144 NM 2008 3 5 QXEA200800124 1 20080119 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 469-489 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 405QX 4047 PDX - C4 CHECK - LEFT SEAT TRACK NR 7 BETWEEN FRAME 469.5 TO 489.5 HAS MULTIPLE CHAFES/GOUGES. REPAIRED IAW RD8/4-53-88 4, Q400 NDTM PT-6 51-00-01, AND Q400 SRM 51-21-10 2 H 7 2 4T RT A13NM 2008030500192 20080305 00192 NM 2008 3 5 QXEA200800189 1 20080130 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 5 TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 350PH 488 PDX - C5 CHECK - LEFT NR 5 FLAP TRACK HAS PITTING ON THE LOWER SURFACE OF THE UPPER INBOARD FLANGE AT THE ROLLERS ZERO D EGREE POSITION. REPAIRED IAW DHC 8 200 RD8-57-989, NDTM PT-6 51-00-01. 2 H 7 2 4T RT A13NM 2008030600009 20080306 00009 2008 3 6 ABXA080056 4 20080214 A 2212 258668911ABX1 CONTROLLER DOUG DC9 DC931 3022065 WP COCKPIT DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 906AX 264 47072 ON GROUND AT ALB, NOTED HEAVY ODOR OF BURNING ELECTRICAL EQUIPMENT. AIRED OUT COCKPIT, CLOSED UP AGAIN AND SMELL RETURN ED WITHIN TWO MINUTES. FOUND SMELL COMING FROM THE AUTO PILOT CONTROLLER. DEFERRED THE AUTO PILOT SYSTEM. CLEARED DEF ERRED ITEM, REPLACED AUTO PILOT CONTROLLER IAW DC9 AMM 22-10-02. 2 L 7 2 4F A6WE 2008030600036 20080306 00036 NM 2008 3 6 HNAA0800088 1 20080218 A 2435 AJA4N176 CONTACTOR DHAV DHC8 DHC8102 2809003 NM STARTER SYS STUCK A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 EA 07 838EX 37198 37198 220 NR 2 ENGINE STARTED TO SPOOL WITH GPU CONNECTED TO AIRCRAFT. NR 2 STARTER/GENERATOR STARTED TO SMOKE. THE NR 2 PROP WA S SPINNING AT 200 RPM WHEN THE CREW POWERED DOWN. THE FIRE DEPARTMENT WAS CALLED TO THE AIRCRAFT, NO FIRE WAS DETECTED. FOUND THE START CONTACTOR STUCK, REMOVED AND REPLACED THE STARTER/GENERATOR AND START CONTACTOR. OPERATIONAL CHECK GO OD. 2 H 7 2 4T RT A13NM 2008030600097 20080306 00097 NM 2008 3 6 SWAA081057 1 20080225 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 18L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2008030600099 20080306 00099 NM 2008 3 6 SWAA081047 1 20080222 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 520, STR 28L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008030600101 20080306 00101 2008 3 6 SWAA081048 4 20080225 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008030600131 20080306 00131 2008 3 6 2008UALA00981 4 20080221 A 2565 HOUSING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE CRACKED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 651UA 25389 RIGHT OVERWING SLIDE DISCONNECT HOUSING IS CRACKED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040100130 20080401 00130 NM 2008 4 1 ASAA0842728 1 20080303 A 5311 6546548194 FRAME BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 CORROSION ON FRAME IN AFT CARGO PIT AT BS 747 STR 26L TO STR 26R, REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008040100134 20080401 00134 WP 2008 4 1 08FDEA01175 1 20080328 A 5414 AUB70389 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 NR 3 PYLON LT TOP PANELS 487CL & 487 BL INTERIOR IS CHAFED. BLENDED DISCREPANT AREAS ON THE NR 3 PYLON PANEL 487 CL WHER E CHAFING WAS PRESENT IAW SRM 54-00-01. CHECKED LIMITS IN DISCREPANT AREA IAW THE FOLLOWING SRMS 54-00-01 VOL I & 54-3 1-02 VOL III. ORIGINAL THICKNESS 0.090, MATERIAL LOSS 0.023. REMAINING MATERIAL 0.067 ON PANEL (OUT OF LIMITS). FABRICATED A REPAIR DOUBLER IAW SRM 54-00-01 VOL III. TREATED, PRIMED & INSTALLED DOUBLER IAW SRM 51-21-01 VOL II & 51 -31-01 VOL II. 2 L 7 3 4F RT A22WE 2008040100135 20080401 00135 NM 2008 4 1 ASAA0842726 1 20080303 A 5320 694347721 CHANNEL BOEING 737 737490 1384715 NM AFT CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 AFT CARGO PIT BS 794 TO BS 767 RBL 21 SHIELD IS CORRODED, REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008040100140 20080401 00140 NM 2008 4 1 ASAA0842719 1 20080227 A 5512 657378354 SKIN BOEING 737 737490 1384715 NM HORIZ STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 R N HORIZ STAB L/E SKIN DENTED AT STAB STA 249.10 AND 1.5, REPAIRED IAW B737 400 SRM 55 10 01 FIG 201. 2 L 7 2 4F RT A16WE 2008040100145 20080401 00145 NM 2008 4 1 ASAA0842713 1 20080303 A 5753 65C2631026 WEDGE BOEING 737 737490 1384715 NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 RN IB FLAP TRAILINES EDGE WEDGE 27 INCHES OUTBD OF INBD END AND 3.5 INCHES FWD OF TRAILING EDGE HAS DENT R N IB FLAP TRA ILING EDGE WEDGE WEDGE 27" OB OF IB END AND 3.5 INCHES FWD OF T/E DENT REPAIRED IAW B 737 400 SRM CH 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008040100147 20080401 00147 NM 2008 4 1 ASAA0842720 1 20080304 A 5753 654643099 SKIN BOEING 737 737490 1384715 NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 LT INBD FORE FLAP UPPER SURFACE HAS IRREGULARITY DENT ON UPPER SURFACE OF THE LT INBD FOREFLAP AT WBL 134. REPAIRED IAW B 737 400 SRM 51 70 10 REPAIR 3 PARA 7. 2 L 7 2 4F RT A16WE 2008040100148 20080401 00148 NM 2008 4 1 UPS08551878 1 20080315 A 5330 SKIN BOEING 757 75724APF 1384969 NM FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 444UP 27389 INSPECTION TYPE:N/A SKIN GOUGE ABOVE FWD ACTUATOR ON MAIN CARGO DOOR. FERRY PERMIT 9065 ISSUED. D371408 ISSUED. IDENT IFIED SKIN AS OUTER SKIN REF 52-30-01-1A FIG 101. MAX SKIN THK .041. MIN THK .028. HFEC PER NDTM 51-00-19. NO CRACKS NOT ED. REMOVED DAMAGE 52-30-01-1A GOUGE MAX TOTAL 6.5 IN 20 SQ INCHES. THIS DEF ALTERED TO EO B757-5280-28879A FOR PERMANEN T REPAIR. 2 L 7 2 4F RT A2NM 2008040100149 20080401 00149 WP 2008 4 1 UPS08851879 1 20080314 A 5753 SKIN DOUG DC8 DC873F 302199F WP T/E FLAP PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:N/A RIGHT WING O/B FLAP UPPER SKIN HAS PUNCTURE DAMAGE 2 INCHES I/B OF CUTOUT (ACTUATOR) AND 18 INCHES A FT OF LEADING EDGE. DAMAGE MEASURES .375" X .250". ACCOMPLISHED REPAIR PER DC8 SRM 57-02-01-0 FIG 002Q. CLASS B REPAIR . RAN FLAPS, NO INTERFERENCE NOTED. 2 L 7 4 4F RT 4A25 2008040100151 20080401 00151 NM 2008 4 1 UPS08M51866 1 20080218 A 5512 SKIN DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:3C FOUND CORROSION ON NR 32 RT (UPPER) BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLE D REPAIR BUSHING PER EO MD11-5510-19409-M. BUSHING O.D. 1.132 BORE I.D. 1.130 2 L 7 3 4F RT A22WE 2008040100154 20080401 00154 NM 2008 4 1 UIEA200800080 1 20080309 A 5730 SKIN BOEING 747 747341 13848AM NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 LEFT WING UPPER SKIN REAR SPAR CORRODED LEVEL 1. CORROSION CLEANED UP AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F RT A20WE 2008040100156 20080401 00156 NM 2008 4 1 UIEA200800081 1 20080307 A 5313 691U1042100 STRINGER BOEING 747 747341 13848AM NM BS 480 S10R CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 CABIN AND FLIGHT DECK UPPER DECK STA 480 STRINGER S-10 R FOUND CRACKED. REPAIRED STRINGER PER BOEING SERVICE BULLETIN 7 47-53A2484. 2 L 7 4 4F RT A20WE 2008040100159 20080401 00159 WP 2008 4 1 UPS08851880 1 20080316 A 5230 DOOR DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:N/A PIT 32 DOOR CRACKED. ACCOMPLISHED HFEC INSPECTION PER EO DC8-5230-28827 PAR 6 A2. ACCOMPLISHED STO P DRILL PER EO DC8-5230-28827 PAR 6 A3-A4. NEEDS HFEC. ALSO REMOVED MOUNT BOLTS & 2 EA RIVETS FOR ACCESS. PERFORMED E DDY CURRENT ON STOP DRILL. NO CRACKS NOTED. 2 L 7 4 4F RT 4A25 2008040100161 20080401 00161 EA 2008 4 1 TRAX200800425 1 20080316 A 3350 STRIP CNDAIR CL600 CL6002C10 1390015 EA CABIN DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 FLOOR EMERGENCY LIGHT STRIPS REMOVED DUE TO DAMAGE. 2 L 7 2 4F RT A21EA 2008040100163 20080401 00163 EA 2008 4 1 TRAX200800426 1 20080317 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 867AS 7463 FLAP FAIL AT 200 KTS AT ZERO DEGREES WHEN SELECTING 8. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF A N APPROPRIATE CORRECTIVE ACTION. EMERGENCY DECLARED. FLT 4568 DEL 279 MINS. (SKEW DETECTION SYSTEM) LUBED, RESHIMED AND RIGGED FLAP ACTUATORS NR 1-8. REMOVED AND REPLACED LT AND RT INB FLAP'S. FLAP SYSTEM OP CHECKS GOOD MESSAGE CLEARED IAW AMM 27-53-01. 2 L 7 2 4F RT A21EA 2008040100164 20080401 00164 EA 2008 4 1 TRAX200800427 1 20080317 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 914EV 7752 ROTTEN SMELL IN BACK OF CABIN ON TAKEOFF (APU OFF). PASSENGER COMPLAINED BOTH LEGS, TO AND FROM AVL. FLT 4790 DEL 74 M INS. 2 L 7 2 4F RT A21EA 2008040100169 20080401 00169 EA 2008 4 1 TRAX200800431 1 20080320 A 5210 SEAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF POSITION A ASOA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 980EV 7759 CLIMBING OUT THRU 17000 MCD SEAL BLEW OUT AND CABIN PRESSURIZATION WAS LOST. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERG ENCY DESCENT PERFORMED TO A LOWER ALTITUDE. REMOVED AND REPLACED PASSENGER DOOR SEAL IAW CRJ200 AMM 52-11-10, OPS CHECK GOOD. SDR CLOSED. 2 L 7 2 4F RT A21EA 2008040100176 20080401 00176 WP 2008 4 1 UPS08851922 1 20080228 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 RIGHT AFT FUSELAGE EXTERIOR STA 1550, L24R, FUSE SKIN LOOSE/ POPPED FASTENERS. REMOVED FASTENERS, RE MOVED AND REPLACED LONG 24R FROM 1510-1570, RE-INSTALLED FASTENERS. 2 L 7 4 4F RT 4A25 2008040100178 20080401 00178 WP 2008 4 1 UPS08851926 1 20080305 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 COURIER AREA FLOOR PNL F23 IS CRACKED, CORRODED AND DELAMINATED IN SEVERAL AREAS. FABBED FLOOR PANEL . 2 L 7 4 4F RT 4A25 2008040100182 20080401 00182 WP 2008 4 1 UPS08851929 1 20080303 A 5320 4641324U501 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 END FITTING CRACKED AT STA 1695 L34R. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-3-2, 51-1-8, 51-1-11. 2 L 7 4 4F RT 4A25 2008040100183 20080401 00183 WP 2008 4 1 UPS08851930 1 20080222 A 5347 3657502U509 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 STOP HOLES WORN IN CO-PILOTS LOWER SEAT TRACKS. REMOVED AND REPLACED SEAT TRACKS IAW EO DC8-5340-183 15-B, SRM 51-1-8, 51-1-20D. 2 L 7 4 4F RT 4A25 2008040100185 20080401 00185 WP 2008 4 1 UPS08851931 1 20080304 A 5347 DC853B003501 SEAT TRACK DOUG DC8 DC873F 302199F WP CABIN BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 PIECE OF SEAT TRACK BROKEN AWAY IN MAIN CABIN STA 75, RBL 47. REMOVED AND REPLACED SEAT TRACK IAW SR M 51-3-2, 51-3-0, 51-1-8. 2 L 7 4 4F RT 4A25 2008040100191 20080401 00191 EA 2008 4 1 TRAX200800466 1 20080324 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 926EV 7843 FLAP FAIL AT ZERO WHEN SELECTING 8 AT 200 KTS. EMERGENCY EQUIPMENT REQUESTED TO BE ON STANDBY AS A PRECAUTION. FLT4656 DEL 171 MINS. 2 L 7 2 4F RT A21EA 2008040100200 20080401 00200 NM 2008 4 1 MWEA080047 1 20080326 A 2560 P4010021 BATTERY BOEING 717 717200 1383700 NM FLASHLIGHT DEFECTIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 925ME 55191 LOWER FORWARD EMERGENCY FLASHLIGHT NOT CHARGING. REMOVED AND REPLACED BATTERY. 2 L 7 2 4F TR A6WE 2008040100201 20080401 00201 NM 2008 4 1 MWEA080048 1 20080326 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 913ME 55176 AFTER EMERGENCY LIGHTED BATTERY PACK RESTORATION EMERGENCY LIGHTS ABOVE ROW 4 FAILED TO ILLUMINATE. REMOVED AND REPLACE D BATTERY PACK. 2 L 7 2 4F TR A6WE 2008040100203 20080401 00203 NM 2008 4 1 SWAA081682 1 20080327 A 5753 6546434 FLAP BOEING 737 7375H4 138449D NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2008040100204 20080401 00204 NM 2008 4 1 SWAA081671 1 20080327 A 3350 101331 LENS BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008040100207 20080401 00207 NM 2008 4 1 SWAA081672 1 20080327 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040100218 20080401 00218 NM 2008 4 1 SWAA081677 1 20080327 A 5311 6546554 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040100240 20080401 00240 NM 2008 4 1 ASAA0892778 1 20080307 A 5320 146A750611 FLOOR SUPPORT BOEING 737 737990 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 323AS 30021 AFT CARGO PIT FLOOR SUPPORT SPLICE CORRODED STA 727 I RBL 8.1. REMOVED DAMAGED SPLICE, FABRICATED SPLICE CHANNEL IAW DW G 146A7506 FIG 2. LOCATED DRILLED AND INSTALLED IAW B737 900 SRM 51 40 2 PG 6 ASA EA 5310 02779. 2 L 7 4 4F RT A16WE 2008040100244 20080401 00244 NM 2008 4 1 SA08021 1 20080326 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 823AW 1463 PHX - AFT FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. 2 L 7 2 4F RT A28NM 2008033100167 20080331 00167 2008 3 31 AMTA200800229 4 20080316 A 3422 BATTERY BOEING 737 73783N 13844HI NM ISFD UNSECURE A AMTA O OTHER O OTHER LD LANDING 1 GL 11 310TZ 28243 ISFD WENT BLANK WITH NOSE WHEEL TOUCHDOWN. FOUND ISFD BATTERY NOT SEATED IN RACK. SECURED ISFD BATTERY. OPS TEST IAW FIM 34-24-00-810-804. OK FOR SERVICE. (K) 2 L 7 2 4F RT A16WE 2008033100170 20080331 00170 NE 2008 3 31 AMTA200800231 2 20080314 A 7320 VANE BOEING 737 73783N 13844HI NM CFMINT CFM567 CFM567B2US 13802 NE NR 1 ENGINE INOPERATIVE A AMTA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 11 323TZ 30033 NR 1 ENGINE ONLY WENT UP TO 75 PERCENT ON TAKEOFF AND KICKED OFF AUTO THROTTLES MX POWER 101.8 PERCENT, NR 2 ENG GOOD. DURING MANUAL ACTUATION TEST, FOUND RT VSV NOT OPENING, ON NR 1 ENG, BLED THE SYSTEM, PERFORMED MANUAL ACTUATION, RT VSV , OPS NORMAL IAW 75-31-00-2, PERFORMED TEST 12 ACTUATION TEST. TEST PASSED NO FAULTS. (K) 2 L 7 2 4F 4 F RT A16WE E2GL 2008033100180 20080331 00180 WP 2008 3 31 08FDEA01121 1 20080324 A 5320 AFS38665 ANGLE DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 ANGLE REQUIRES FABRICATION; ANGLE IS CRACKED. FABRICATED ANGLE IAW DWG AFA 3866. ALODINED & PRIMED ANGLE IAW DC/MD-10 SRM 51-21- 01; VOL II. INSTALLED ON JOB CARD N00128. 2 L 7 3 4F RT A22WE 2008033100187 20080331 00187 EA 2008 3 31 SWIA200819394 1 20080324 A 3234 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 862AS 7476 FLT 3905 - RECEIVED A LANDING GEAR DISAGREE MESSAGE WHEN SELECTED BEFORE LANDING. REPLACED BYPASS VALVE AND SELECTOR VA LVE. OPS AND LEAK CHECK GOOD IAW 32-32-10, PN 750004000-003, SN/OFF 719A, PN 750005000, SN/OFF 0734. 2 L 7 2 4F RT A21EA 2008033100205 20080331 00205 NM 2008 3 31 DHL2008763524 1 20080301 A 5322 SHEAR TIE BOEING 727 727264 138408M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 FRAME SHEAR TIE CORRODED AT BS 1130, BETWEEN STR 28R AND 29R, AFT SIDE. REMOVED, FABRICATED SHEAR TIE FROM 7075-T6, .05 0" BY 6" BY 2.5", PO NR 9006153, AND INSTALLED NEW SHEAR TIE PER B727 SRM 53-10-4 FIG 4, 53-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 2008033100207 20080331 00207 NM 2008 3 31 DHL2008763526 1 20080313 A 5347 BAC1520792 SEAT TRACK BOEING 727 727264 138408M NM CABIN CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 CABIN SEAT TRACK CORRODED AT BS 990 TO 1130, LBL 45.75. REMOVED, FABRICATED SEAT TRACK SECTION FROM BAC1520-792, 297.87 5" LONG, PO NR 9006020, AND INSTALLED PER B727 SRM 53-10-5 FIG 1, 53-10-1 FIG 7, AND 51-30-2. 2 L 7 3 4F A3WE 2008033100244 20080331 00244 WP 2008 3 31 DHL2008805537 1 20080324 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP CARGO BAY WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 UPPER CARGO COMPT NR 7 TRACK LUG WORN (STA 290.000 - 340.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2-3 PG 49 -50. REMOVED TRACK DAMAGED SEGMENT IAW SRM 53-2-3. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TR ACK SEGMENT IAW SRM 53-2-3, SRM 51-3-0, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2008033100247 20080331 00247 WP 2008 3 31 DHL2008805535 1 20080303 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP CARGO BAY WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 UPPER CARGO COMPT NR 5 TRACK LUG WORN (STA 1684.000 - 1700.000). CUT OUT TRACK WORN SEGMENT AND FABRICATED SPLICES (AL7 075T6 0.100") (AL7075T6 0.125") (AL7075T6 0.160") IAW SRM 53-2-3 PG 49-50 FIG 14. CLEANED, TREATED AND PRIMED AREA AND SPLICES IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 51-3-0, SRM 51-3-1 (TORQUE), PERFORMED MAJOR R EPAIR IAW SRM 53-2-3 PG 49-50. 2 L 7 4 4F RT 4A25 2008033100285 20080331 00285 NM 2008 3 31 DLM90080418 1 20080306 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM CABIN CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 UPON REMOVAL OF CABIN FLOORS FOR SEAT TRACK REPAIRS, ADDITIONAL CORROSION DAMAGE WAS FOUND OUT OF LIMITS ON THE FLOOR MA TING FLANGE OF SEAT TRACK LBL 22 FS 1250 TO 1344. REMOVED AND REPLACED SEAT TRACK, IAW MD90 SRM 51-30-01. 2 L 7 2 4F RT A6WE 2008033100295 20080331 00295 NM 2008 3 31 DLM90080428 1 20080306 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 LEFT CABIN CUSP WEB FS 1241, CRACKED AT GALLEY LINE SUPPORT ATTACHMENT. REPAIRED CRACKED CUSP WEB, IAW MD80 DRD 53-05D, FIG 827D. 2 L 7 2 4F RT A6WE 2008033100298 20080331 00298 NM 2008 3 31 QXEA200800314 1 20080320 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX -C4- CORROSION ON ANGLE BY NUTPLATE HOLE AT STA X597.5 AND Y6.0 JUST INBOARD OF LT INBOARD SEAT TRACK. DRILLED OUT NUTPLATE AND REMOVED CORROSION IAW DHC 8/200 CPCM CHAPTER 4. HFEC INSPECTED BLENDED AREA FOR CRACKS IAW D 8/200 NDTM, P ART 6, 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECK OF BLENDED AREA IAW -8/200 NDTM PART 1, 51-00-04 HIGH .080 LOW .07 3. AREA OF BLEND WITHIN LIMITS REF DHC 8 SRM 51-20-11. APPLIED ETCH ALODINE AND PRIMER IAW DHC 8 SRM 51-20-16 AND 51-2 0-36. REINSTALLED NUTPLATE REF DHC 8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008033100313 20080331 00313 EU 2008 3 31 08FDEA01155 1 20080326 A 5310 DOOR FRAME AIRBUS 310 A310203 3930313 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LOWER FUSELAGE FWD CARGO DOOR CUTOUT AT FRAME 25; STA 1711 LOWER VERTICAL SECTION HAS A GOUGE ON THE EDGE. REMOVED GOUG ES IAW A310-200 SRM 51-74-10. ORIGINAL THICKNESS 0.236; REMAINING MATERIAL 0.230; MATERIAL REMOVED 0.006. FOUND TO BE WITHIN LIMITS IAW A310-200 SRM 53-13-12. ALODINED IAW SRM 51-21-10. PRIMED AND PAINTED IAW SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008040100018 20080401 00018 SO 2008 4 1 SIMA200808801 1 20080327 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 691AE 14500860 ON FLIGHT 4371, CREW REPORTED ABNORMAL SMELL IN THE COCKPIT ON CLIMB-OUT FROM, ODOR WAS INTERMITTENT SMELLED LIKE A COMB INATION DIRTY SOCK AND CHEMICAL. CREW PERFORMED APPROPRIATE PROCEDURE IN AOM 1 DECLARED PRECAUTIONARY (NOT AN EMERGENCY ). RETURNED TO MDT. ALSO, LATER GOT PACK 1 OVLD AND PACK 1 OVHT AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF PACK SYSTEM IAW EMB 145 AMM 21-31-00-700-802. NOTED DIRTY SOCK SMELL WHILE RUNNING NR 1 PACK ALSO RECEIVED PAC K 1 OVLD MESSAGE MEL'D NR 1 PACK PER MEL 21-29 AUTH 031085D-C. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008040100024 20080401 00024 WP 2008 4 1 IXXA08SMN073S 1 20080214 A 5753 FLAP DOUG DC8 DC871F 302199D WP T/E FLAP DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBD FLAP UPPER PART SHOWS DENTS AT STATION XF 375.000 TO STA XF 404.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, DC8 SRM 57-7-1 FIGURE 4 T/R 57 - 94 ITEM "U" AND "Q".DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 51-1- 9 T/R 51, 142, DC8 SRM 51-1-9A T/R 51, 141, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008040100040 20080401 00040 NE 2008 4 1 BB08036 2 20080319 A 7314 BPU200MK2 PUMP BOEING 757 7572S7 1384962 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 903AW 45157 11198 23323 30503 HNL FLT 26 - EN-ROUTE OGG TO PHX, ON CLIMB-OUT FROM OGG, RECEIVED EICAS MESSAGE "R ENG LP PUMP". FLIGHT DIVERTED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE CHECKED WIRING FROM D321 E, J3 AND D319 E, J3 TO SWITCH S10134. NO FAULTS WE RE FOUND. CHECKED EICAS COMPUTER SYSTEM AND FOUND GOOD. REPLACED RIGHT ENGINE LP PUMP. OPERATIONALLY AND LEAK CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E12EU 2008040100052 20080401 00052 NM 2008 4 1 USAA920080650 1 20080313 A 5310 DOOR FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 CLT - MAJOR REPAIR - B4 CHECK - AFT CARGO DOOR, CUT OUT AFT FRAME CRACKED, BS 847, S21R. REPAIRED AFT CARGO DOOR, CUT O UT AFT FRAME, BS 847, S21R IAW USAIRWAYS EA 100315. 2 L 7 2 4F RT A16WE 2008040100180 20080401 00180 WP 2008 4 1 UPS08851928 1 20080305 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 ALL FASTENER HOLES ON MAIN CABIN FLOOR PANEL F23 BARE WORN, KNIFEDGED, CRACKED, BROKEN OUT, OR CORROD ED. PANEL SKIN IS CORRODED. REPLACED 1 EACH HAT CHANNEL, REPLACED SKIN ON PANEL IAW SRM 51-1-21, 51-1-8, 51-3-2. 2 L 7 4 4F RT 4A25 2008040100215 20080401 00215 NM 2008 4 1 SWAA081679 1 20080327 A 5311 65C22908 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008030600186 20080306 00186 NM 2008 3 6 2008UALA00996 1 20080223 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 196-208 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 340UA 24244 THREE DENTS ON FUSELAGE, STATIONS 196 TO 208, ABOVE STRINGERS 24R. REPAIRED DENTS PER UA-EVA 71181A. MAJOR REPAIR A CCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030600187 20080306 00187 NM 2008 3 6 2008UALA00997 1 20080222 A 2560 BRACKET BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU GIRT BAR LOOSE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 341UA 24245 DOOR 1R BRACKET THAT HOLDS GIRT BAR ON DOOR LOOSE. GIRT BAR COMES OUT TOO EASILY. ADJUSTED BRACKET. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030600189 20080306 00189 NE 2008 3 6 2008UALA01004 2 20080224 A 7260 BEARING BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE MAIN GEARBOX FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 228UA 30556 222171 FOUND EXCESSIVE BLACK METAL COVERING CHIP DETECTOR HEAD, AT NR 2 ENG MAIN OIL TANK (MCD). FOUND GEARBOX (MCD) FULL OF M ETAL CONTAMINATION. ENGINE REPLACED AT ORD. THE MB-7 AND MB-8 BEARINGS IN THE MAIN GEARBOX WERE FOUND TO HAVE FAILED. P RATT & WHITNEY HAS RECEIVED THIS HARDWARE, AND ARE INVESTIGATING FURTHER. THEIR HYPOTHESIS IS THAT THE MB-8 BEARING IS B ACKING OFF THE DRIVESHAFT SHOULDER. THIS CAUSES CROSS LOADING ON THE MB-7 BEARING, WHICH SUBSEQUENTLY FAILS. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008030600190 20080306 00190 NM 2008 3 6 2008UALA01006 1 20080222 A 4930 38005501 FUEL CONTROL BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 211UA 30217 APU NO START AT DISPATCH. FOUND FUEL& LUBE CLUSTER SHAFTS NOT TURNING. REPLACED FUEL CLUSTER. REPLACED LUBE CLUSTER . PENALTY RUN ACCOMPLISHED, FLITERS & OIL REPLACED, NO DISCREPANCIES FOUND AFTER RUNS. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008030600194 20080306 00194 NM 2008 3 6 2008UALA01028 1 20080223 A 3510 HOSE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OXYGEN SYS LEAKING A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 THE 2ND OBS OXYGEN HOSE IN STORAGE BOX LEAKS. SUSPECT DAMAGED FROM PRE FLIGHT CHECKS. REPLACED MASK AND BOX PER MM35-1 1-51. OPS CKD NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030600195 20080306 00195 NM 2008 3 6 2008UALA01029 1 20080224 A 8011 STARTER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 ENGINE FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 DURING NR 2 ENGINE STARTER SERVICE FOUND NUMEROUS METAL CHIPS ON DETECTOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030600252 20080306 00252 EA 2008 3 6 TRAX200800196 1 20080205 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 RIGHT SIDEWALL SEAT RAIL FS 708.0 TO FS 761.85 HAS CORROSION DAMAGE. REMOVED AND REPLACED RT SIDEWALL SEAT RAIL FS 708. 0 TO 761.85 IAW CRJ 700 AMM 53-00-49. TO7011593 02/12/08. SUPPLEMENTAL SDR CLOSED 2/14/08. 2 L 7 2 4F RT A21EA 2008030600254 20080306 00254 EA 2008 3 6 VNAA0802008 1 20080211 A 2750 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE T/E FLAP MALFUNCTIONED A VNAA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 GL 05 226JS 7895 CREW REPORTED A FLAPS FAIL MESSAGE ON APPROACH. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE RE SET FLAP CONTROLLER IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPS CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FO R SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008030600261 20080306 00261 2008 3 6 SWAA081064 4 20080226 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 265WN 32522 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008030600262 20080306 00262 NM 2008 3 6 SWAA081065 1 20080226 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008030600263 20080306 00263 NM 2008 3 6 SWAA081066 1 20080226 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008030600270 20080306 00270 NM 2008 3 6 SWAA081080 1 20080226 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 8L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008030600272 20080306 00272 NM 2008 3 6 SWAA081077 1 20080226 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008030600277 20080306 00277 NM 2008 3 6 SWAA081075 1 20080226 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SKIN PER BOEING SB. 2 L 7 2 4F RT A16WE 2008030600279 20080306 00279 NM 2008 3 6 SWAA081076 1 20080226 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 EEPLS LENS CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008030600282 20080306 00282 EU 2008 3 6 TRAX200800310 1 20080223 A 2910 HYDRAULIC SYSTEM AEROSP ATR72 ATR72 EU BLUE SYSTEM LOW A ASOA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 631AS 362 BLUE LO LEVEL IN FLIGHT. EMERGENCY DECLARED. 2 H 7 2 4T RT 2008030600284 20080306 00284 NM 2008 3 6 HALA0800195 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1370 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION RBL 54.75, SEAT TRACKS AT STA 1370, BASE OF TRACKS. CORROSION REMOVED PER SRM 51-10-02, REV 76 AND SR M 53-00-52/101. REWORK WITHIN LIMITS. 2 L 7 2 4F RT A1NM 2008030600287 20080306 00287 EA 2008 3 6 MASA200800162 1 20080223 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH FLT 2781 ELP - PHX, FLAPS FAIL AT 8 DEGREES AT GATE DURING POWER TRANSFER FROM GROUND TO APU. CONTRACT MX COMPLIED WITH PART A. 2 L 7 2 4F RT A21EA 2008030600291 20080306 00291 NM 2008 3 6 HALA0800147 1 20080211 A 5347 SEAT TRACK BOEING 767 7673G5 1385126 NM BS 1197 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 2 CORROSION SECTION 46 RBL 11, SEAT TRACK AT STA 1197.90. REWORKED IAW SRM 53-00-52-101. 2 L 7 2 4F RT A1NM 2008030600292 20080306 00292 NM 2008 3 6 DLM90080233 1 20080218 A 5322 99530629 SHEAR TIE DOUG MD90 MD9030 3023690 NM BS 1486 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DA 53391 AFT ACCESSORY COMPARTMENT STATION 1486 LEFT OF LONGERON 1 SHEAR TIE CRACKED. REMOVED AND REPLACED SHEAR TIE, IAW MD90 S RM 51-10-05 AND 51-30-05. 2 L 7 2 4F RT A6WE 2008030600293 20080306 00293 EA 2008 3 6 MASA200800164 1 20080225 A 4990 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA APU OVERSERVICED A MASA O OTHER W N INADEQUATE Q C FALSE WARNING NR NOT REPORTED 1 SW 07 37342 7342 FLT 7220 LAN-ORD, APU OVERTEMP FOLLOWED BY APU FIRE WARNING. FOUND APU OVER SERVICED. MX DESERVICED TO CORRECT LEVELS AND FOUND FIRE LOOPS GROUNDING OUT, REPOSITIONED LOOPS. 2 L 7 2 4F RT A21EA 2008030600295 20080306 00295 EA 2008 3 6 MASA200800165 1 20080225 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 516LR 10258 ASH FLT 7381 ORD-SAT. CEILING EMERGENCY FLOOD LIGHT ROW 2 INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008030600297 20080306 00297 EA 2008 3 6 MASA200800166 1 20080226 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A MASA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 SW 07 75998 7336 FLT 7392, ORD-MDT. FLAPS FAILED AT 0 ON RETRACTION. COMPLIED WITH PART A AND B INSPECTIONS. 2 L 7 2 4F RT A21EA 2008030600301 20080306 00301 EU 2008 3 6 USAA920080508 1 20080223 A 2424 740120C GCU AIRBUS 320 A320232 3930326 EU NR 1 ODOR A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 675AW 11483 11483 2405 FLT NR 335 - AT CRUISE FLT 340, GOT ELEC NR 1 IDG LO PSI. COMPLIED WITH ECAM ACTIONS. CREW DISCONNECTED GENERATOR & AL SO MENTIONED AN ELECTRICAL ODOR IN COCKPIT. MX CONTROL SUGGESTED CREW TURN OFF NR 1 BLEED & USE APU AS A SECOND BLEED S OURCE. CREW REPORTED FUMES CLEARED, BUT RETURNED 15 MINUTES LATER. ACFT DIVERTED TO STL. NO EMERGENCY DECLARED. MX R & R NR 1 GCU AND NR1 IDG. 2 L 7 2 4F RT A28NM 2008030600303 20080306 00303 EU 2008 3 6 USAA920080509 1 20080223 A 3350 321454 EPSU AIRBUS 320 A320231 3930325 EU ZONE 200 DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AW 53389 12353 76 FLT NR 284 - SJC-PHX - EEL - SEAT 19A EMERGENCY EXIT LIGHT AND SEAT BAR INOP. RETERMINATED AND REPLACED BROKEN TERMINAL S ON SEAT 19A EMERGENCY EXIT LIGHT. ALSO, REMOVED AND REPLACED L EPSU DUE TO INTERNAL FAULT CAUSED BY ABOVE FAULTS. OP ERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM GOOD. 2 L 7 2 4F RT A28NM 2008030600125 20080306 00125 NM 2008 3 6 2008UALA00974 1 20080221 A 3510 B-NUT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CREW O2 LOOSE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 907UA 25007 PREFLIGHT O2 SHOWS 400 PSI. REPLACED MASK AND SECURED B-NUT NO LEAKS FOUND. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030600148 20080306 00148 EU 2008 3 6 2008UALA00989 1 20080221 A 5321 FLOORBOARD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO BAY DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 488UA 1680 CARGO FLOORBOARD RPL S GLS PNL. ACCOMPLISHED FLOORBOARD REPLACEMENT. **MAJOR REPAIR**. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030600244 20080306 00244 2008 3 6 ASMF200801001 4 20080118 A 3430 ILS SYSTEM DOUG DC9 DC987 3022087 WP PWA JT8 JT8D* NE LEFT SIDE MALFUNCTIONED W ASMF O OTHER J WARNING INDICATION AP APPROACH 1 SW 23 216AM 10559 10549 49586 CAPTAIN REPORTED THAT DURING FINAL APPROACH, BOTH VHF NAVIGATORS IN THE SAME RADIAL SHOWED A DEVIATION OF 20 DEGREES IN THE TRAJECTORY, THE DIFFERENCE CONTINUED UNTIL LANDING AND RAMP. MAINT REPLACED VOR NR 1, VHF/ILS NAV 1 AND AHRS IAW MM 34-43-01 AND 34-22-02, BUT FAILURE CONTINUED, SO FAILURE WAS DEFERRED IAW MEL 34-21, CATEGORY (C). THE TX/RX VOR NR 2 AN D LT RDMI WERE REPLACED IAW MM 34-22-02 AND 34-21-12, TESTED CORRECT. DURING OVERNIGHT CHECK, VOR/ILS SYS WAS TESTED IAW MM 34-22-01, ALL CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2008030600253 20080306 00253 EA 2008 3 6 VNAA0802007 1 20080210 A 3200 H29X9015 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT MLG DAMAGED A VNAA O OTHER O OTHER LD LANDING 1 GL 05 242JS 221 7911 CREW REPORTED THE RIGHT INBOARD MAIN TIRE SHREDDED UPON LANDING IN PHL. MAINTENANCE REMOVED AND REPLACED BOTH RIGHT HAN D MAIN GEAR TIRES IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS FERRIED TO DAY FOR FURTHER EVALUATIO N AND TO REPAIR DAMAGE. MAINTENANCE ISSUED TEMP REPAIR 10995. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008030600267 20080306 00267 NM 2008 3 6 SWAA081070 1 20080226 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 423WN 29827 DURING SCHEDULED HC1 CHECK, RT OVERWING EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008040100217 20080401 00217 NM 2008 4 1 SWAA081678 1 20080327 A 5311 6546548 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040100263 20080401 00263 NM 2008 4 1 ASAA0842746 1 20080305 A 5315 656731633 FLOORBEAM BOEING 737 737490 1384715 NM BS 913 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 AFT CABIN FLOOR INTERCOSTAL AT BS 913.74 RBL 51 TO RBL 56 HAS EXISTING DOUBLE DRILLED FASTENER HOLE AT O B END (SUPPORT) INTERCOSTAL AT BS 913.74 RBL 56. REPLACED IAW B737 400 SRM CH. 51 40 05 USING BAC 1506 43 7075773511 PO NR 166385 AND INSTALLED IAW B737 400 SRM CH 51 40 02. 2 L 7 2 4F RT A16WE 2008040100264 20080401 00264 NM 2008 4 1 SWAA081585 1 20080324 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008040100265 20080401 00265 NM 2008 4 1 SWAA081615 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040100275 20080401 00275 NM 2008 4 1 SWAA081597 1 20080325 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 476WN 32475 DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008040100279 20080401 00279 NM 2008 4 1 SWAA081647 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008040100284 20080401 00284 NM 2008 4 1 SWAA081658 1 20080326 A 3350 20131A BATTERY PACK BOEING 737 7373T5 1384608 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED MV2 CHECK, FOUND LT AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008040100288 20080401 00288 NM 2008 4 1 SWAA081728 1 20080330 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040100290 20080401 00290 NM 2008 4 1 SWAA081709 1 20080330 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040100292 20080401 00292 NM 2008 4 1 SWAA081711 1 20080330 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040100298 20080401 00298 NM 2008 4 1 ASAA0842757 1 20080318 A 5340 STRINGER CLIP BOEING 737 737490 1384715 NM BS 867 S27R CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 AFT CARGO PIT STR 27R TIE CLIP AT STA 867 CRACKED FOUND DURING FLOOR PANEL CLOSING AFT CARGO PIT STR 27R CRACKED TIE CLI P AT STA 867. REPLACED WITH MADE REPAIR PART IAW B737 400 SRM CH 51 40 02. 2 L 7 2 4F RT A16WE 2008040100300 20080401 00300 NM 2008 4 1 QXEA200800334 1 20080320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - C4- RT INBD SEAT TRACK NR 7 HAS SEVERAL AREAS OF CORROSION AT STA X214 TO X228. REMOVED SEAT TRACK AND INSTALL NE W SEAT TRACK IAW SRM 51-40-00 AND 51-40-11. 2 H 7 2 4T RT A13NM 2008040200003 20080402 00003 NM 2008 4 2 SWAA081526 1 20080319 A 5523 BACB28M06B013A BUSHING BOEING 737 7375H4 138449D NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED C4 CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BUSHING AND BEAR ING PER SWA EA. 2 L 7 2 4F RT A16WE 2008040200005 20080402 00005 NM 2008 4 2 CALA0800244 1 20080321 A 5320 6517684Y642 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 THE 7L INTERCOSTAL FORWARD OF STA 294.5 CRACKED. REMOVED AND REPLACED INTERCOSTAL PER ECRA 5311-01400. 2 L 7 2 4F RT A16WE 2008040200006 20080402 00006 NM 2008 4 2 CALA0800245 1 20080321 A 5320 69489852 ATTACH FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 ATTACHING CLIP AT STRINGER 8L BETWEEN BS 350 AND 360 CRACKED. REMOVED AND INSTALLED NEW CLIP PER ECRA 5311-01400. 2 L 7 2 4F RT A16WE 2008040200023 20080402 00023 NM 2008 4 2 CALA0800234 1 20080318 A 5743 115A5211 SUPPORT FITTING BOEING 737 737724 13844BY NM LT MLG TRUNNION CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24715 28786 LEFT MLG TRUNNION SUPPORT HAS PITTING CORROSION AT LWR I/B BUSHING. REPAIRED PER EC/RA 5741-01106. 2 L 7 2 4F RT A16WE 2008040200024 20080402 00024 NM 2008 4 2 CALA0800235 1 20080318 A 5743 115A5211 SUPPORT FITTING BOEING 737 737724 13844BY NM LT MLG TRUNNION CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24715 28786 LEFT MLG FWD TRUNNION SUPPORT HAS PITTING CORROSION AT LWR O/B BUSHING. REPAIRED PER EC/RA 5741-01106. 2 L 7 2 4F RT A16WE 2008040200025 20080402 00025 NM 2008 4 2 CALA0800236 1 20080318 A 5311 65C25230 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 AFT CARGO BILGE AREA - CORROSION ON FRAME AT STA 727E APPROX LBL 24. FABRICATED REPAIR PARTS, TREATED, PRIMED AND INSTA LLED REF SRM 53-00-07 REPAIR 5. 2 L 7 2 4F RT A16WE 2008040200026 20080402 00026 NM 2008 4 2 CALA0800237 1 20080318 A 5311 6546551 BELTFRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 AFT CARGO BILGE AREA - CORROSION AT BELT FRAME, STA 807, APPROX LBL 24. REMOVED CORROSION AND INSTALLED REPAIR AT STA 8 07 APPROX LBL 24 REF SRM 53-00-07. 2 L 7 2 4F RT A16WE 2008040200028 20080402 00028 EU 2008 4 2 TRAX200800424 1 20080315 A 3020 ANTI-ICE SYSTEM AEROSP ATR72 ATR72 EU NR 1 ENGINE FAILED A ASOA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 642AS 395 NR 1 ENGINE ANTI-ICE FAILED IN FLT. FLT 4354 CX. EMERGENCY DECLARED. 2 H 7 2 4T RT 2008040200039 20080402 00039 NM 2008 4 2 CALA0800252 1 20080307 A 5320 6545834505 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INTERCOSTAL AT STA 324 LBL 40 CRACKED AT FORWARD ATTACH POINT. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008040200042 20080402 00042 NM 2008 4 2 CALA0800253 1 20080316 A 5320 65317875 SUPPORT CHANNEL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 CORROSION ON L1 ENTRY THRESHOLD SUPPORT CHANNEL AT STA 312 TO 338 LBL 61. REMOVED THRESHOLD DRAIN AND CORRODED CHANNEL, LOCATED AND DRILLED NEW CHANNEL ASSEMBLY. INSTALLED NEW CHANNEL ASSEMBLY AND RE-INSTALLED THRESHOLD DRAIN PER SRM 51-4 0-02. 2 L 7 2 4F RT A16WE 2008040200044 20080402 00044 NM 2008 4 2 CALA0800254 1 20080306 A 5320 6547957ULL STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 AFT CARGO STA 847 TO 857 AND RBL 19 THE UPPER AND LOWER STRAP ON THE INTERCOSTAL FLANGE ARE CORRODED. REMOVED LOWER AND UPPER STRAP AT STA 847 TO 857. REMOVED CORROSION FROM LOWER STRAP AND FOUND IT TO BE WITHIN LIMITS AND UPPER STRAP TO BE OUT OF LIMITS. PRIMED LOWER STRAP AND REPLACED UPPER STRAP PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008040200047 20080402 00047 NM 2008 4 2 ASAA0842739 1 20080305 A 5315 654681179 FLOORBEAM BOEING 737 737490 1384715 NM BS 986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 AFT CABIN FLOORBEAM AT STA 986.5 RBL 27 WL 207.5 CORRODED ON UNDERSIDE AT CLIPNUT ATTACH POINT. REPAIRED IAW EA NR 5320 01832. 2 L 7 2 4F RT A16WE 2008040200052 20080402 00052 NM 2008 4 2 ASAA0842734 1 20080303 A 5322 69353501 SHEAR TIE BOEING 737 737490 1384715 NM BS 807 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 CORROSION ON ATTACH CLIP AT BS 807 OUTBD OF RT CARGO TIE DOWN TRACK RBL 13.80 ON FWD SIDE AFT CARGO PIT CORROSION ON ATT ACH CLIP IN AFT CARGO AT BS 807 OUTBOARD OF RT CARGO TIE DOWN TRACK RBL 13.80 FOUND BEYOND LIMITS. REPLACED WITH NEW PA RT IAW B737 400 SRM LT 51 40 02. 2 L 7 2 4F RT A16WE 2008040200054 20080402 00054 NM 2008 4 2 SWAA081537 1 20080321 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008040200056 20080402 00056 EA 2008 4 2 TRAX200800441 1 20080320 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 CLIP AT FS 484 RBL 27 CRACKED. REMOVED DAMAGED CLIP, DUPLICATED SERVICEABLE CLIP AS SHOWN IN REO 601R-53-41-059. INSTAL LED NEW CLIP IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 2008040200058 20080402 00058 EA 2008 4 2 TRAX200800444 1 20080320 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 CLIP AT FS 484 LBL 27 CRACKED. REMOVED DAMAGED CLIP, DUPLICATED SERVICEABLE CLIP AS SHOWN IN REO 601R-53-41-059. INSTA LLED NEW CLIP IAW SRM 51-42-21 2 L 7 2 4F RT A21EA 2008040200059 20080402 00059 NM 2008 4 2 ASAA0842737 1 20080304 A 5320 6545855122 SILL BOEING 737 737490 1384715 NM BS 947-986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 R2 CABIN DOORWAY LOWER SILL CORROSION FOUND FROM BS 947 TO 986.50 CORROSION ON R2 CABIN DOORWAY LOWER SILL CHORD WAS BLE NDED OUT AND FOUND TO BE BEYOND LIMITS IAW 53-60-15 FIG 101. REMOVED DAMAGE PART IAW SRM 51-40-02 AND INSTALLED A NEW S ILL CHORD IAW SRM 51-40-05 AND 51-40-02. 2 L 7 2 4F RT A16WE 2008040200060 20080402 00060 EA 2008 4 2 TRAX200800446 1 20080320 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 CLIP AT FS 280 O/B RBL 9 CRACKED. REMOVED CRACKED CLIP AT FS280 OB OF RBL 9. FABRICATED -5 CLIP AS REF IN REO 601R-53 -11-171 REV D AND INSTALLED FABRICATED CLIP AT FS280 OB OF RBL9 PER CRJ SRM 51-42-21. 2 L 7 2 4F RT A21EA 2008040200061 20080402 00061 EA 2008 4 2 TRAX200800447 1 20080320 A 5320 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 RT BATTERY RIB DRAG ANGLE CRACKED IN GEAR BAY. REMOVED CRACKED DRAG ANGLE AND LOCATED FASTNER HOLES IN SERVICEABLE DRAG ANGLE IAW SRM 51-40-11. 2 L 7 2 4F RT A21EA 2008040200064 20080402 00064 NM 2008 4 2 ASAA0842718 1 20080229 A 5330 6546881175 SKIN BOEING 737 737490 1384715 NM BS 1070 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 FUSELAGE SKIN APPROX BS 1070 AT STR 14L DENTED FUSELAGE SKIN BS 1070 STR 14L. REPAIRED IAW B737 400 SRM 53 80 01. 2 L 7 2 4F RT A16WE 2008040200067 20080402 00067 EA 2008 4 2 TRAX200800450 1 20080320 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 AAR - INTERCOSTAL CLIP CRACKED AT FS 484 LBL 36. REMOVED AND REPLACED CRACKED CLIP FS 484 LBL36 IAW REO 601R-53-41-059 . 2 L 7 2 4F RT A21EA 2008040200068 20080402 00068 NM 2008 4 2 ASAA0842721 1 20080304 A 5755 654645170A SKIN BOEING 737 737490 1384715 NM NR 2 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 NR 2 SPOILER LWR SURFACE 4 INCHES FROM INBOARD EDGE 7 INCHES FROM L/E IS DENTED. NR 2 SPOILER LWR SURFACE DENT REPAIRED IAW B737 400 SRM 51 70 10, REPAIR NR 2. 2 L 7 2 4F RT A16WE 2008040200074 20080402 00074 NM 2008 4 2 ASAA0852747 1 20080321 A 2421 7588429101 FILTER BOEING 737 737890 1384527 NM NR 1 IDG CLOGGED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 587AS 35684 DURING SERVICE CHECK, FOUND NR 1 ENGINE IDG DELTA P INDICATOR EXTENDED. REPLACED NR 1 IDG FILTERS AND OILS. RESET INDI CATOR. RAN NR 1 ENGINE DELTA P INDICATOR RESET GOOD. 2 L 7 2 4F RT A16WE 2008040200075 20080402 00075 2008 4 2 ASAA0852752 4 20080322 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 584AS 35682 "FMC DISAGREE" ANNUNCIATED ON ND AND FMC SCRATCH PAD. VERIFIED FMC DISAGREE FAULT. RESET FMC NR 1 COMP AND FMC NR 2 CO MP C/B'S. FMC SYSTEMS LT AND RT GROUND TEST GOOD. 2 L 7 2 4F RT A16WE 2008040200076 20080402 00076 NM 2008 4 2 ASAA0842744 1 20080305 A 5330 6546811117 SKIN BOEING 737 737490 1384715 NM BS 1021 GOUGED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 02 788AS 28885 FUSELAGE SKIN AT BS 1016 + 52" BELOW STR 16L DENTED AND GOUGED FROM CONTACTS WITH SCISSOR LIFT. REPAIRED AREA WITH REPA IR PART. 2 L 7 2 4F RT A16WE 2008040200087 20080402 00087 NM 2008 4 2 SWAA081626 1 20080325 A 3350 MS155721 LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008040200094 20080402 00094 NM 2008 4 2 ASAA0852765 1 20080325 A 2820 2670136 RECEPTACLE BOEING 737 737890 1384527 NM RT WING FUEL LEAKING A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 587AS 35684 FUELING RECEPTACLE IS LEAKING WHILE TRANSFERRING FUEL. REPLACED FUELING RECEPTACLE AND O-RING. LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 2008040200098 20080402 00098 NM 2008 4 2 USAA920080701 1 20080325 A 5330 6545774 SKIN BOEING 737 7374B7 1384702 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 454UW 24996 CLT - MAJOR REPAIR - RON - CRACKED FUSELAGE SKIN, BS 727D, S23L. REPAIRED FUSELAGE SKIN, BS 727D, S23L IAW B737 SRM 53- 00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008040200101 20080402 00101 NM 2008 4 2 USAA920080704 1 20080324 A 5330 6545774 SKIN BOEING 737 7373B7 1384580 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 23380 CLT - MAJOR REPAIR - C4 CHECK - CRACKED FUSELAGE SKIN, BS 944, S24L. REPAIRED FUSELAGE SKIN, BS 944, S24L IAW USAIRWAYS EA 100339. 2 L 7 2 4F RT A16WE 2008033100269 20080331 00269 NM 2008 3 31 QXEA200800321 1 20080320 A 5320 FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX -C4- CORROSION AT MCD SEAL INFLATION FITTING ON SKIN ORIFICE BELOW THRESHOLD. REMOVED THE MCD SEAL INFLATION HOSE A ND 2 RIVETS FROM THE MCD SEAL RETAINER AND REMOVED CORROSION FROM AROUND THE HOLE IAW RD8-53-8921. BLENDED OUT CORROSIO N IAW DHC8/200 CPCM CHAPTER 4 AND ALODINED AREA IAW DHC8/200 SRM 51-20-16. MEASURED AREA AND FOUND AREA TO BE WITHIN LIM ITS IAW DHC 8/200 SRM 51-20-11. HFEC INSPECTED BLEND AREA FOR CRACKS IAW D 8/200 NDTM, PART 6, 51-00-01, NO CRACKS NOTED . PRIMED IAW DHC 8 SRM 51-20-36. REINSTALLED RIVETS REF DHC 8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008033100278 20080331 00278 NM 2008 3 31 DL76G080411 1 20080326 A 5315 BAC1505100774 FLOORBEAM BOEING 767 7673P6 1385105 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 155DL 25269 FLOORBEAM CORRODED AT STA 654+88 AT RBL 22 TO RBL 29. BEAM REPLACED PER 53-00-51D FIGURE 201 ON NR CARD AVM511467. 2 L 7 2 4F RT A1NM 2008033100287 20080331 00287 NM 2008 3 31 DLM90080420 1 20080318 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM CABIN CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 CABIN SEAT TRACK RBL 54.4 OUT OF LIMITS FS 503-550. REMOVED AND REPLACED SEAT TRACK, IAW MD90 SRM 53-40-01 VOL I. 2 L 7 2 4F RT A6WE 2008033100306 20080331 00306 SO 2008 3 31 CHQA200800057 1 20080324 A 3610 7276045 FILTER ELEMENT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BLEED AIR SYS DIRTY A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 275SK 145345 CAE312704 CLE TO RDU - WHILE CLIMBING THROUGH 7,000 FT, THE CREW RECEIVED A BLEED 1 OVERTEMP MESSAGE. THE PROPER CHECK LISTS WERE FOLLOWED IN THE QRH AND IT WAS DECIDED TO DIVERT TO CMH. THE FLIGHT DIVERTED AND LANDED WITHOUT INCIDENT IN CMH. MAIN TENANCE TROUBLESHOT THE BLEED SYSTEM AND REPLACED THE FAN AIR VALVE FILTER. AFTER RUNNING UP THE ENGINES AND CHECKING T HE BLEED SYSTEM, THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008040100016 20080401 00016 NE 2008 4 1 C8GA20080012 2 20080325 A 7260 AMS7245 HELICOIL BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE GEARBOX DAMAGED A C8GA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 SO 29 899AA 22014 FLT 708 FROM MCI TO PHX - DURING CRUISE OPERATION THE CAPTAIN WAS NOTIFIED THAT THE NR 1 ENGINE OIL QUANTITY WAS DECREAS ING. THE NR 1 ENGINE WAS SHUT DOWN AND EMERGENCY WAS DECLARED, THE AIRCRAFT DIVERTED TO ABQ WHERE IT LANDED WITHOUT INC IDENT. POST FLIGHT INSPECTION REVEALED THAT A BANJO FITTING ON THE GEARBOX WAS LEAKING. REMOVED AND REPLACED DAMAGED H ELICOIL. SERVICED OIL SYSTEM AND PERFORMED LEAK CHECK. NO LEAKS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 2008030600274 20080306 00274 NM 2008 3 6 SWAA081078 1 20080226 A 2560 6557463 FITTING BOEING 737 7375H4 138449D NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2008030600299 20080306 00299 EA 2008 3 6 MASA200800167 1 20080226 A 2560 PLACARD CNDAIR CL600 CL6002B19 1900309 EA FIRST AID KIT TORN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77260 7260 ASH FLT 2864 PHX-MFR. FIRST AID KIT INSPECTION STICKER WAS TORN. MX INSPECTED THE FIRST AID KIT AND INSTALLED A NEW IN SPECTION STICKER. 2 L 7 2 4F RT A21EA 2008030600305 20080306 00305 NM 2008 3 6 08FDEA00582 1 20080223 A 5313 BAC1498140 STRINGER BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 FWD PIT (STA 582) STR 27L CORRODED (MARKED ) REMOVED DAMAGED SECTION OF STR 27L . VERIFIED ORIGINAL MATERIAL AS .040 707 5-T6 REF SRM 53-10-2 FIG 9. REPLACEMENT CHANNEL SAME AS ORIGINAL, BAC1498-140, FX1376, PO1013862. VERIFIED MATERIAL FO R REPAIR SPLICES AS 7075-T6-.063 REF SRM 53-10-3 A 03332 PO 1015473. FABRICATED REPAIR PARTS REF SRM 53-10-3. TREATED AND PRIMED REF SRM 51-10-2. INSTALLED REF SRM 53-10-3 (CLASSFIED AS A MAJOR REPAIR). 2 L 7 3 4F A3WE 2008030600312 20080306 00312 EU 2008 3 6 USAA920080468 1 20080219 A 5554 D5537131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU ZONE 300 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - RUDDER HINGE NR 2 FITTING WORN, VERTICAL STABILIZER STATION 1926/RIB 4. REPLACED RUDDER HINGE NR 2 FITTING, VERTICAL STABILIZER STATION 1926/RIB 4 IAW A320 AMM 55-46-00. 2 L 7 2 4F RT A28NM 2008030600313 20080306 00313 EU 2008 3 6 USAA920080469 1 20080219 A 5554 D5537131800200 HINGE FITTING AIRBUS 320 A320232 3930326 EU ZONE 300 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - RUDDER HINGE NR 4 FITTING WORN, VERTICAL STABILIZER STATION 2632/RIB 6. REPLACED RUDDER HINGE NR 4 FITTING, VERTICAL STABILIZER STATION 2632/RIB 6 IAW A320 AMM 55-46-00. 2 L 7 2 4F RT A28NM 2008030600315 20080306 00315 NM 2008 3 6 USAA920080486 1 20080201 A 5754 114T3100 ANGLE BOEING 767 7672B7ER 1385107 NM NR 6 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AY 26847 MIA - MAJOR REPAIR - C4 CHECK, LEFT WING LEADING EDGE NR 6 SLAT LOWER FORWARD SUPPORT BRACKET ANGLES CRACKED, LES 280. REPLACED LEFT WING LEADING EDGE NR 6 SLAT LOWER FORWARD SUPPORT BRACKET ANGLES, LES 280 IAW BOEING DRAWING 114T3100 AND B767 SRM 51-10-02. 2 L 7 2 4F RT A1NM 2008030600318 20080306 00318 NM 2008 3 6 USAA920080488 1 20080212 A 5315 FLOORBEAM BOEING 767 7672B7ER 1385107 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AY 26847 MIA - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN FLOORBEAM, BS 347, RBL 34 - RBL 88. REPAIRED CABIN FLOORBEAM , BS 347, RBL 34 - RBL 88 IAW B767 SRM 53-00-51. 2 L 7 2 4F RT A1NM 2008030600319 20080306 00319 NM 2008 3 6 USAA920080489 1 20080214 A 5347 SEAT TRACK BOEING 767 7672B7 1385107 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AY 26847 MIA - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 426 - BS 665, RBL 88.5. REPLACED CABIN CABIN SEAT TRACK, BS 426 - BS 665, RBL 88.5 IAW B767 SRM 53-00-52. 2 L 7 2 4F RT A1NM 2008030600320 20080306 00320 NM 2008 3 6 USAA920080490 1 20080219 A 5347 SEAT TRACK BOEING 767 7672B7ER 1385107 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AY 26847 MIA - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 1055 -BS 1099, LBL 88.6. REPLACED CABIN SEAT TRACK, BS 1055 -BS 1099, LBL 88.6 IAW B767 SRM 53-00-52. 2 L 7 2 4F RT A1NM 2008030600321 20080306 00321 NM 2008 3 6 USAA920080500 1 20080221 A 5330 6545775 SKIN BOEING 737 737301 1384611 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 23934 CLT - MAJOR REPAIR - C1 CHECK - CRACKED FUSELAGE SKIN, BS 754, S24R. REPAIRED FUSELAGE SKIN, BS 754, S24R IAW B737 SRM 53-00-01 REPAIR. 2 L 7 2 4F RT A16WE 2008030600322 20080306 00322 NM 2008 3 6 USAA920080501 1 20080221 A 5320 6517684 WEB BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 23934 CLT - MAJOR REPAIR - C1 CHECK - CRACKED WEB, BS 294.5, S16L. REPLACED WEB, BS 294.5, S16L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008030600326 20080306 00326 NM 2008 3 6 ABXA080064 1 20080225 A 3350 20131A BATTERY PACK BOEING 767 767281 1385109 NM CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 786AX 23019 ALL EMERGENCY LAMPS INOPERATIVE. DEFERRED: 59239. EMERGENCY LIGHT BATTERY PACKS SWAPPED FROM PRIMARY TO SPARE POSITION S. OPS CHECKED GOOD. ALL WORK DONE IAW AMM 33-51-07-2. THE SPARE EMERGENCY LIGHT BATTERY HAS BEEN DEFERRED FOR TRACKI NG IAW ABX GMM 01-07-04. CLEARED DI: REMOVED AND REPLACED THE SPARE EMERGENCY LIGHTS BATTERY PACK IAW B767 33-50-00. 2 L 7 2 4F RT A1NM 2008030600327 20080306 00327 WP 2008 3 6 ABXA080057 1 20080206 A 5320 99578606 INTERCOSTAL DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DURING WINDOW FRAME MOD TO COCKPIT STRUCTURE, FOUND FORWARD INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW D C9 SRM 51-30-2 AND 51-10-4 PER WO 600283624. 2 L 7 2 4F A6WE 2008030600328 20080306 00328 WP 2008 3 6 ABXA080058 1 20080206 A 5310 99115056 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DURING WINDOW FRAME MOD TO COCKPIT STRUCTURE, FOUND RIGHT SIDE FRAME CRACKED LESS THAN 2.50 INCHES. REPAIRED IAW DC9 SR M 53-03, FIG 34 PER WO 600283624. 2 L 7 2 4F A6WE 2008030600330 20080306 00330 WP 2008 3 6 ABXA080083 1 20080226 A 2740 920710296 RELAY DOUG DC9 DC932 3022066 WP TRIM SYSTEM DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 939AX 650 47201 CENTER PRIMARY TRIM CIRCUIT BREAKER TRIPPED DURING TRIM SETTING. FOUND UP TRIM RELAY BURNT AT TERMINALS A1 & A2. REPLA CED NOSE UP PRIMARY TRIM RELAY AND TERMINALS A1 & A2. OPS CHECK GOOD IAW DC9 AMM 27-40-04-5-0002. 2 L 7 2 4F A6WE 2008030700001 20080307 00001 NM 2008 3 7 2008UALA00944 1 20080219 A 5210 INSERT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 R4 DOOR HANDLE BOX INSERTS CORRODED. REMOVED AND REPLACED HANDLE BOX ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030700002 20080307 00002 NM 2008 3 7 USAA920080503 1 20080219 A 5340 STRINGER CLIP BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 23934 CLT - MAJOR REPAIR - C1 CHECK - CRACKED STRINGER CLIP, BS 360, S14L. REPLACED STRINGER CLIP, BS 360, S14L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008030700006 20080307 00006 NM 2008 3 7 2008UALA00945 1 20080219 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 DOOR 2R UPPER HINGE ARM CUTOUT REQUIRES DOUBLER. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030700008 20080307 00008 EU 2008 3 7 USAA920080510 1 20080219 A 5321 D5367180500500 FLOORBOARD AIRBUS 320 A320232 3930326 EU ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 653AW 1003 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBOARD 262FF, BS 3158/FR 66 - BS 3257/FR 68, -Y1292 TO -Y1732. R EPLACED CABIN FLOORBOARD 262FF, BS 3158/FR 66 - BS 3257/FR 68, -Y1292 TO -Y1732 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008030700010 20080307 00010 NM 2008 3 7 2008UALA00947 1 20080219 A 5320 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 576UA 26690 DAMAGE FOUND 4 FT AFT AND ONE FOOT ABOVE DOOR SILL AT DOOR 4R. ACCOMPLISHED MAJOR REPAIR AT SFO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030700011 20080307 00011 EU 2008 3 7 BA08010 1 20080222 A 3097 301VT TERMINAL BLOCK AIRBUS 330 A330323 3930335 EU WINDOW HEAT FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 272AY 0333 PHL CLT-LGW FLT NR 704, CREW REPORTED L1 WINDOW NOT HEATING, FLIGHT DIVERTED TO PHL WITHOUT FURTHER INCIDENT. MAINTENAN CE REPLACED TERMINAL BLOCK 301VT. OPS CHECKS OK. 2 L 7 2 4F RT A46NM 2008030700012 20080307 00012 2008 3 7 BB08021 4 20080224 A 2565 BATTERY PACK BOEING 767 767201 1385125 NM ESCAPE SLIDE FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 250AY 23902 MUC - OVERWING ESCAPE SQUIB TEST 1 FAILED. MAINTENANCE REPLACED BATTERY PACK. 2 L 7 2 4F RT A1NM 2008030700021 20080307 00021 NM 2008 3 7 2008UALA00953 1 20080219 A 2560 HANDLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOOR OBSTRUCTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 830UA 1243 RIGHT AFT SLIDE INDICATION INOP ON DOOR-OXY SYSTEM ECAM PAGE - DOOR-OXY CREW COMMENTS: UNABLE TO ARM SLIDE FOR DOOR 2R. FOUND RUBBER TRIM AROUND DOOR ARM HANDLE NOT SECURE. REPOSITIONED AND SECURED TRIM, DOOR ARMS AND DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030700028 20080307 00028 NM 2008 3 7 2008UALA00946 1 20080219 A 3350 SPRING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LIGHT SWITCH OUT OF ADJUST A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 541UA 25253 COCKPIT EMERGENCY EXIT LIGHTS SWITCH WILL DISARM WITH COVER DOWN. COVER SPRING OUT OF ADJUSTMENT. SECURED THE SPRING A ND SWITCH OPERATES NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030700029 20080307 00029 2008 3 7 USAA920080513 4 20080224 A 2565 CONTROL ARM AIRBUS 320 A320232 3930326 EU ARMING LEVER OUT OF ADJUST A USAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 19 619AW 527 FLT NR 310, EMERGENCY EQUIP SLIDE AT R2 IS DISARMING WHILE IN FLIGHT. MAINTENANCE REPLACED THE R2 GIRT BAR. AFTER EX TENSIVE TROUBLESHOOTING, MAINTENANCE ADJUSTED THE VERTICAL CONTROL ROD OF ARMING LEVER, 3/4 TURN COMPLIED WITH TO TIGHTE N ARMING LEVER DOWN. OPERATIONAL CHECK WAS GOOD. NO REPEAT EVENTS. 2 L 7 2 4F RT A28NM 2008030700032 20080307 00032 SO 2008 3 7 CHQA200800040 1 20080223 A 2400 14521325407 ELECTRICAL SYS EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL MALFUNCTIONED A CHQA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 11 562RP 19263 1945 145451 CAE311207 CVG TO STL. DURING CLIMB, WHILE PASSING THROUGH 10,000FT THE CABIN EMERGENCY LIGHTS FLASHED ON, OFF, ON AND THE CREW RE CEIVED AN EMERGENCY LIGHTS NOT ARMED MESSAGE. ALL OTHER INDICATIONS WERE NORMAL AND ALL INDICATIONS ON THE ELECTRICAL P AGE OF THE MFD WERE NORMAL. THE QRH WAS FOLLOWED AND THE AIRCRAFT RETURNED TO FIELD AT CVG, WHERE IT LANDED WITHOUT INC IDENT. MAINTENANCE RESET THE AIRCRAFT POWER BUT THE MESSAGE WOULD NOT CLEAR. AN ELECTRICAL PANEL WAS SLAVED IN AND THE ELECTRICAL SYSTEM OPERATED NORMALLY. THE ELECTRICAL PANEL WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008030700033 20080307 00033 NM 2008 3 7 ASAA0852671 1 20080225 A 2425 233A32041 SYMBOL GENERATOR BOEING 737 737890 1384527 NM COCKPIT MALFUNCTIONED A ASAA K NONE O OTHER NR NOT REPORTED 1 NM 02 577AS 35186 NR 2 GENERATOR "OFF BUSS" LIGHT SYMBOLOGY INVERTED. CORRECTED NR 2 GENERATOR "OFF BUSS" ANNUNCIATOR FORMAT. 2 L 7 2 4F RT A16WE 2008030700040 20080307 00040 NM 2008 3 7 ASAA0842664 1 20080127 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 1 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 LEFT WING NR 1 SPOILER UPPER SURFACE DENTED. PREPARED DAMAGED AREA, FABRICATED FILLER SKIN AND DOUBLER AND BONDED IAW B 737 400 SRM 51 70 10 PAGES 211 213 214 223 231 254 257 REPAIR 4. 2 L 7 2 4F RT A16WE 2008030700047 20080307 00047 NM 2008 3 7 ASAA0842673 1 20080127 A 5755 654645268A SKIN BOEING 737 7374Q8 138447Q NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 RIGHT WING NR 5 SPOILER DENTED ON UPPER SURFACE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BONDED IAW B737 4 00 SRM 51 70 10 PGS 212 214 223 241 AND 254 257 REPAIR 2. 2 L 7 2 4F RT A16WE 2008030700052 20080307 00052 NM 2008 3 7 GTIA0800033 1 20080201 A 5320 BEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 501NK 2424 LEFT Z BEAM AT Y 1292 BETWEEN FRAME 66 AND 68 SHOWS SIGNS OF CORROSION. REPLACED Z BEAM. 2 L 7 2 4F RT A28NM 2008030700055 20080307 00055 NM 2008 3 7 GTIA0800032 1 20080109 A 5320 WEB AIRBUS A321 A321231 3940032 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 LEFT CORNER WEB CORRODED, FRAME 70 AND Y1292 AT FLOOR LINE. REPLACED LT CORNER WEB. 2 L 7 2 4F RT A28NM 2008030700058 20080307 00058 NM 2008 3 7 ASAA0842680 1 20080127 A 5755 654645258 SKIN BOEING 737 7374Q8 138447Q NM LT SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 LEFT WING I/B GROUND SPOILER HAS MULTIPLE DENTS ON UPPER SURFACE AT WBL 162 AND WBL 144 AREAS. PREPARED DAMAGED AREAS, FABRICATED REPAIR DOUBLERS AND BONDED IAW B737 400 SRM 51 70 10 PGS 201 REPAIR 2, 2 EACH DOUBLERS INSTALLED. 2 L 7 2 4F RT A16WE 2008030700059 20080307 00059 NM 2008 3 7 KNNA20080002 1 20080227 A 2612 FIRE WARNING BOEING 737 7372L9 1384497 NM APU BAY FALSE ACTIVATION A KNNA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 WP 25 737Q 21279 APU FIRE WARNING ON APPROACH. APU WAS NOT OPERATING AND WAS CURRENTLY ON MEL 49-01 DMI 737-08-20. CAPTAIN'S AFTER LAND ING INSPECTION FOUND NO EVIDENCE OF FIRE OR/OVERHEAT. PILOTS FOLLOWED AFM PROCEDURES AND FIRED APU FIRE EXTINGUISHER BO TTLE. 2 L 7 2 4F RT A16WE 2008030700061 20080307 00061 EA 2008 3 7 COMA0860142 1 20080221 A 2421 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 804CA 166 7352 FLIGHT 5313 - DURING TAKEOFF RECEIVED IDG NR 1 CAUTION MESSAGE. ABORTED TAKEOFF. RECEIVED GEN NR 1 OFF CAUTION. RETUR NED TO GATE. REPLACED NR 1 IDG. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008030700064 20080307 00064 EA 2008 3 7 COMA0860145 1 20080225 A 3010 ANTI-ICE SYSTEM CNDAIR CL600 CL6002B19 1900309 EA RT WING MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 969CA 7141 FLIGHT 5652 - RECEIVED RIGHT WING ANTI-ICE CAUTION MESSAGE ON TAKEOFF. REJECTED TAKEOFF. RETURNED TO GATE WITHOUT INCI DENT. PERFORMED HIGH POWER RUNS. COULD NOT DUPLICATE PROBLEM. COMPLIED WITH RTO INSPECTION. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008030700067 20080307 00067 WP 2008 3 7 IXXA08SMN005S 1 20080114 A 5730 PANEL DOUG DC8 DC862F 3021972 WP ZONE 600 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 41CX 83204 2971 46129 DURING ROUTINE C CHECK INSPECTION, FOUND WING FUSELAGE PANEL NUMBER 716 FILLET PANEL RIGHT SIDE CRACKED AT STATION 690. 000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR REMOVED DAMAGED AREA. FABRICATED FILLER AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 53-8-1 PAGES 3-4, DC8 SRM 51-1-9 PAGE 1, DC8 SRM 53-2-4 PARAGRAPH 3, 51-1-9 PARAGRAPH 3AND 2. 2 L 7 4 4F 4A25 2008030700070 20080307 00070 EA 2008 3 7 TRAX200800311 1 20080220 A 5310 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA RT MLG WW CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 858AS 7417 RT WHEEL WELL I/B BATT RIB ATTACH ANGLE CRACKED 2 L 7 2 4F RT A21EA 2008030700090 20080307 00090 NM 2008 3 7 UPS08551723 1 20080226 A 3350 LIGHT BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 405UP 23727 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY LIGHT. OPERATES NORMALLY, OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2008030700091 20080307 00091 WP 2008 3 7 NWAA080709751 1 20080221 A 4990 OIL SYSTEM DOUG DC9 DC941 302207N WP APU OVERSERVICED A NWAA A UNSCHED LANDING W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 751NW 47115 THE FLIGHT ATTENDANT AND PASSENGER BOTH REPORTED A BURNING ODOR IN THE CABIN. FLIGHT CONTINUED AS SCHEDULED AND LANDED AT MEM WITHOUT INCIDENT. MAINTENANCE INSPECTED EVERY POSSIBLE SOURCE OF FUMES ABOARD THE AIRCRAFT AND FOUND THE APU OIL OVER SERVICED. OIL WAS DRAINED FROM THE APU, BOTH OF THE PACKS UNDERWENT BURNOUT PROCEDURES AND IT WAS DETERMINED THEN THAT "THE LT PACK WAS CAUSING THE SMOKE". BURNOUT PROCEDURES REPEATED, BOTH COALESCER BAGS REPLACED, AND A FUNCTIONAL CHECK PERFORMED. NO SMOKE OR ODOR EXPERIENCED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2008030700096 20080307 00096 WP 2008 3 7 NWAA080699952 1 20080227 A 3350 FUSE DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS FAULTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 916RW 47144 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY OVERWING EXIT SIGN ON THE RIGHT SIDE AT ROW 12 WAS INOPERATIVE. A FAULTED FUSE WAS REPLACED PER THE MAINTENANCE MANUAL, AN OPERATIONAL CHECK WAS SATISFACTORY, AND THE AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4F A6WE 2008030700099 20080307 00099 NM 2008 3 7 UPS08M51712 1 20080212 A 5754 SKIN DOUG MD11 MD11F 3023600 NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:1C RT WING TELESCOPING DUCT CUT CRACK IN UPPER CORNERS. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER & FILLERS IAW MD-11 SRM 57-10-00. 2 L 7 3 4F RT A22WE 2008030700100 20080307 00100 NM 2008 3 7 UPS08M51713 1 20080212 A 5720 ARB39547 STRAP DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:1C LEFT WING L/E COMPARTMENT XORS 683 HAS STRAP CRACKED. REMOVED STRAP, FABRICATED AND INSTALLED REPLAC EMENT STRAP IAW DWG ARB3954 & SRM 51-33-01. 2 L 7 3 4F RT A22WE 2008030700101 20080307 00101 NM 2008 3 7 UPS08M51714 1 20080212 A 5720 ARB293345 SUPPORT ANGLE DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:1C LEFT WING ACCESS PNL LANDING XORS 540 CRACKED. REMOVED SUPPORT ANGLE, FABRICATED AND INSTALLED REPLA CEMENT SUPPORT ANGLE IAW DWG ARB2933 AND MD-11 SRM 51-33-01 & 51-35-01. 2 L 7 3 4F RT A22WE 2008030700104 20080307 00104 SO 2008 3 7 FDKA200802074 1 20080221 A 3234 7455503 CONTROL LEVER EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A FDKA O OTHER O OTHER TO TAKEOFF 1 SW 07 846MJ 4411 145507 FDM 6095 MSY-MCO (1000 PHX LCL). N/G CYCLING AFTER T/O WHEN SELECTED UP. MX REMOVED AND REPLACED LANDING GEAR CONTROL LEVER. 2 L 7 2 4T RT T00011AT 2008030700106 20080307 00106 NM 2008 3 7 ASAA0852682 1 20080226 A 4990 38809381 FILTER BOEING 737 737890 1384527 NM APU CLOGGED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 577AS 35186 MAINTENANCE CONTROL REQUEST TO INSPECT APU OIL FILTER DELTA P INDICATOR. DELTA P INDICATOR IS INDEED POPPED. REMOVED & REPLACED FILTER & DELTA P INDICATOR. OP & LEAK CHECKS OK. 2 L 7 2 4F RT A16WE 2008030700108 20080307 00108 SO 2008 3 7 FDKA200802077 1 20080221 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN & COCKPIT ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 852MJ 145567 FDM 6034 JFK (1740 PHX LCL). STRONG BURNING SMELL IN CABIN AND COCKPIT. MX PERFORMED ENGINE RUNS, RAN PACKS, INSPECTED RELAY SUPPORTS. MX COULD NOT DUPLICATE, NO FAULTS FOUND. 2 L 7 2 4T RT T00011AT 2008030700120 20080307 00120 NM 2008 3 7 2008UALA00870 1 20080217 A 3350 20121 BATTERY BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 933UA 26659 AFT EMERGENCY FLOOR EEL LIGHT INOP. REPLACED POWER SUPPLY AND BATTERY. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700122 20080307 00122 NM 2008 3 7 2008UALA00901 1 20080216 A 3350 GE1317 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 642UA 25092 EEL LIGHT AT SEAT 35FG INOPERATIVE. REPLACED LAMP, OP CHECKS OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030700124 20080307 00124 NM 2008 3 7 NWAA080736302 1 20080228 A 2530 OVEN BOEING 747 747451 1384940 NM GALLEY CONTAMINATED A NWAA F A ACTIVATE FIRE EXT. UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 662US 23720 AFTER TAKEOFF, NR 2 MAIN TANK FORWARD PUMP MESSAGE AND LIGHT CAME ON, FOLLOWED BY RIGHT UTILITY BUSS LIGHT AND MESSAGE. PERFORMED FUEL PUMP PROCEDURE AS PER COM FIRST AND COMPLIED. THEN PERFORMED RIGHT UTILITY PROCEDURE AS PER COM AND COO RDINATED WITH PURSER. HER REPORT THERE AFTER WAS ACRID ODOR AND FUZZY VISIBILITY BUT NO FIRE WAS VISIBLE. ODOR WAS REP ORTED AT BOTH ENDS OF THE CABIN. AN EMERGENCY WAS DECLARED AND AN IMMEDIATE LANDING (UNEVENTFUL) WAS MADE BACK AT NRT. MAINTENANCE REMOVED AND REPLACED CONTROL UNIT BUSS, BOOST FUEL PUMP, LOAD CONTROL UNIT, EPESC (ENHANCED PASSENGER ENTER TAINMENT SYSTEM), RELAY R50, AND C/B C401, OVEN CONTROLLER, AND NEED TO REPLACE 2 OVEN RELAYS AND OVEN. ALSO INSPECTED 2 L 7 4 4F RT A20WE 2008030700125 20080307 00125 NM 2008 3 7 2008UALA00903 1 20080217 A 3350 767 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EXTERIOR INOPERATIVE A UALA O OTHER O OTHER CL CLIMB 1 WP 29 647UA 25284 THE 2L EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED PART NUMBER 563-3045. OP CHECKS OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030600105 20080306 00105 NM 2008 3 6 SWAA081050 1 20080225 A 5610 6531914102 MECHANISM BOEING 737 7373H4 1384600 NM R2 WINDOW DIRTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED BRDG CHECK, FOUND FLIGHT DECK R2 WINDOW DOES NOT OPEN WHEN EXTERNAL EMERGENCY RELEASE HANDLE IS PULLED. CLEAN AND LUBED HANDLE MECHANISM PER MM. 2 L 7 2 4F RT A16WE 2008030600111 20080306 00111 NM 2008 3 6 SWAA081056 1 20080225 A 3350 8210248801 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 787SA 29812 DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2008030600259 20080306 00259 EA 2008 3 6 VNAA0802011 1 20080214 A 7830 1267588 PDU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE THRUST REVERSER FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 05 246PS 9263 7920 CREW REPORTED A RIGHT HAND REV UNLOCK MESSAGE IN FLIGHT. CREW ELECTED TO DIVERT TO PIT AND LANDED WITHOUT INCIDENT. MA INTENANCE INSPECTED AND DEFERRED THE RIGHT HAND THRUST REVERSER PER MEL 78-30-1-1. MAINTENANCE REMOVED AND REPLACED THE POWER DRIVE UNIT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPS CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008030600280 20080306 00280 EA 2008 3 6 TRAX200800309 1 20080223 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 937EV 8042 AFT RIFGR EMERGENCY LIGHT BULB INOP. 2 L 7 2 4F RT A21EA 2008030700005 20080307 00005 NM 2008 3 7 USAA920080506 1 20080222 A 5753 SKIN BOEING 737 7374B7 1384702 NM TE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 445US 24863 CLT - MAJOR REPAIR - C1 CHECK - RIGHT WING OUTBOARD AFT FLAP UPPER SURFACE HAS DELAMINATION. REPAIRED RIGHT WING OUTBOA RD AFT FLAP UPPER SURFACE IAW B737 SRM 51-70-10. 2 L 7 2 4F RT A16WE 2008032800043 20080328 00043 SO 2008 3 28 C2XA08RI032 1 20080307 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 21130 145704 FLIGHT 2663 - EWR - CREW REPORTED LIGHT SMELL OF SMOKE ODOR IN COCKPIT ON TAXI OUT AND WENT AWAY PRIOR TO TAKEOFF. ON I NITIAL CLIMBOUT SAME SMELL IN COCKPIT. FLIGHT ATTENDANT STATED, SMELLED THE SAME SMOKE AS WELL IN THE FORWARD PART OF C ABIN, NO DE-ICE AT THIS TIME. EWR MX INSPECTED FOR SMELL IN COCKPIT AND RAN PACKS, NO SMELL WAS NOTICED. ACFT WAS APPR OVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2008032800045 20080328 00045 NM 2008 3 28 SWAA081520 1 20080319 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008032800074 20080328 00074 NM 2008 3 28 SWAA081547 1 20080321 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 406WN 27894 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 2 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008032800087 20080328 00087 NM 2008 3 28 SWAA081556 1 20080323 A 5330 6545777 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032800096 20080328 00096 NM 2008 3 28 SWAA081577 1 20080324 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 219WN 32490 EEPLS LOOSE AT ROW 3 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008032800116 20080328 00116 WP 2008 3 28 UPS08851872 1 20080302 A 5720 ATTACH ANGLE DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 INTERGRANULAR CORROSION IN UPPER T/E ATTACH ANGLE ON LEFT I/B AUX TANK NEAR STA XFS 67. REMOVED CORR OSION, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-8, 57-2-0 FIG 37. 2 L 7 4 4F RT 4A25 2008032800118 20080328 00118 WP 2008 3 28 UPS08851875 1 20080222 A 5347 3657503501 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 2ND OBSERVERS FWD SEAT TRACK CORRODED AT RBL 12-16 AROUND MOUNT SCREW COUNTERSINKS. REMOVED AND REPL ACED SEAT TRACKS IAW SRM 51-3-0, 51-1-8. 2 L 7 4 4F RT 4A25 2008032800148 20080328 00148 NM 2008 3 28 SWAA081588 1 20080324 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008032800149 20080328 00149 NM 2008 3 28 SWAA081589 1 20080324 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 AFT CABIN EMERGENCY EXIT SIGN MISSING. INSTALLED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2008032800151 20080328 00151 NM 2008 3 28 SWAA081591 1 20080324 A 5320 6517582 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED SPV CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178, RBL 17, WL 217. REPAIRED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2008032800156 20080328 00156 NM 2008 3 28 UPS08551924 1 20080325 A 2560 MR10042N PBE BOEING 757 75724APF 1384969 NM LAVATORY UNSERVICEABLE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 448UP 27737 INSPECTION TYPE:N/A PBE IN LAV SHOWS PINK ON MOISTURE INDICATOR. REMOVED AND REPLACED PBE. 2 L 7 2 4F RT A2NM 2008032800157 20080328 00157 WP 2008 3 28 UPS08851916 1 20080306 A 5347 3657502U501 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 BOTH PILOTS LOWER SEAT TRACKS WORN, BOTH HAVE BEEN PREVIOUSLY REPAIRED. REMOVED AND REPLACED 2 EACH SEAT TRACKS, OPS CHECK GOOD IAW EO DC8-5340 -18315-B, SRM 51-1-8, 51-1-24. 2 L 7 4 4F RT 4A25 2008032800178 20080328 00178 NM 2008 3 28 SWAA081645 1 20080325 A 5312 6545819 PRESSURE PANEL BOEING 737 7375H4 138449D NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND NLG W/W CEILING PANEL CRACKED AT RBL 7.75. REPAIRED PANEL PER ACO. 2 L 7 2 4F RT A16WE 2008032800197 20080328 00197 SO 2008 3 28 RAIA00803016 1 20080320 A 3260 BRACKET EMB 145 EMB145LR 3260212 SO RT MLG WOW LOOSE A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 850HK 145003 FLT 7933 - GSP - LANDING GEAR AIR/GND FAIL MESSAGE UPON ROTATION. MAINTENANCE RESECURED THE RIGHT MLG NR 2 WOW SWITCH B RACKET AND PERFORMED MULTIPLE LANDING GEAR OPERATIONAL CHECKS WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008032800208 20080328 00208 EA 2008 3 28 A6WA200840120 1 20080216 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 589-621 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 420AW 7719 FS 589 TO FS 621 WL 73.50 LBL 27 FLOOR SUPPORT CORRODED. FLOOR SUPPORT CORROSION REMOVED IAW SRM 51-21-06. (M) 2 L 7 2 4F RT A21EA 2008032800209 20080328 00209 EA 2008 3 28 A6WA200840121 1 20080217 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 285-310 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 430AW 7719 FOUND CORROSION EXISTS ON FLOOR SUPPORTS FS 285-310 WL 73.5 LBL 27 TO LBL 20. CORROSION ON FLOOR SUPPORTS REMOVED IAW S RM 51-21-06. (M) 2 L 7 2 4F RT A21EA 2008033100005 20080331 00005 WP 2008 3 31 UPS08851907 1 20080220 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 CABIN STA 1500 LBL 45 SEAT TRACK AND PLUG GOUGED. REPLACED CABIN SEAT TRACK SECTION AT STA 1500 AND LBL 45 IAW SRM 51-3-0, SRM 51-3-01 AND SRM 53-21-01-04. 2 L 7 4 4F RT 4A25 2008033100016 20080331 00016 NM 2008 3 31 SWAA081656 1 20080326 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 497WN 32479 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008033100023 20080331 00023 NM 2008 3 31 SWAA081662 1 20080326 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 908, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008033100025 20080331 00025 NM 2008 3 31 SWAA081657 1 20080326 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008033100038 20080331 00038 NM 2008 3 31 UPS08651940 1 20080321 A 5315 STIFFENER BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 314UP 27742 INSPECTION TYPE:C FX- MEC STA 246 LBL 40 CABIN FLOORBEAM STIFFENER FOUND CRACK (CRACK LENGTH 2"). FX MEC STA 246 LBL 40 " CABIN FLOORBEAM STIFFENER REPAIRED AS PER SRM 53-10-51-2R4 FIG 201, REF UPS MPI P19656. 2 L 7 2 4F RT A1NM 2008033100049 20080331 00049 CE 2008 3 31 HNJ2008F00000 1 20080204 A 5751 SPAR WTHRLY 620 620B 9630605 CE PWA R985 R985* 52008 NE AILERONS CRACKED D HNJG K NONE O OTHER IN INSP/MAINT 1 NM 02 9024F 1890 1629 236938 LT AILERON SPAR CRACKED AT CENTER AND OB HINGE BRACKET ATTACH POINTS. POSSIBLY DUE TO TWISTING EFFECT OF AILERON ACTUAT OR INSTALLED AT EXTREME IB END OF AILERON. (K) 1 L 7 1 3R 3 R NC A26WE 5E1 2008040100057 20080401 00057 NM 2008 4 1 USAA920080670 1 20080321 A 2910 651782120 MODULE BOEING 737 73733A 1384673 NM HYDRAULIC SYS LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 166AW 47946 3086 23627 FLT NR 280 - IAH - PHX - CREW REPORTED, FELL DIFFERENTIAL LIGHT ILLUMINATED ON TAKEOFF, FOLLOWED BY "B" FLT CONTROL LOW PRESS LIGHT. HYD QTY'S WERE INITIALLY MATCHED, OVER TIME "B" QTY WAS DROPPING WHILE "A" QTY WAS INCREASING. CREW DIVER TED TO SAN ANTONIO, TX. NO EMERGENCY WAS DECLARED. THE LANDING WAS UNEVENTFUL. MX REPLACED THE"A" SYSTEM PRESSURE MOD ULE. OPERATIONAL/LEAK CHECK WAS GOOD. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2008040100069 20080401 00069 NM 2008 4 1 USAA920080659 1 20080222 A 5315 6545410163 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FLOORBEAM CHORD, BS 662, BL 0. REPAIRED FLOORBEAM CHORD, BS 662, BL 0 IAW USAI RWAYS EA 100292. 2 L 7 2 4F RT A16WE 2008040100074 20080401 00074 NM 2008 4 1 USAA920080661 1 20080227 A 5315 6545410 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - CRACKED FLOORBEAM WEB, BS 663, BL 0, WL 208. REPAIRED FLOORBEAM WEB, BS 663, BL 0, WL 208 IAW USAIRWAYS EA 100292. 2 L 7 2 4F RT A16WE 2008040100094 20080401 00094 EA 2008 4 1 A6WA200840152 1 20080304 A 2760 PCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE SPOILERS FAILED A A6WA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 31 469AW 7917 SPOILERONS FAULT STATUS MESSAGE ILLUMINATED. NOTE: THIS OCCURRED ON THE GROUND. AFTER MDC INTERROGATION FOUND SECU 2A LABEL 350 CODE: 00402 CODE: LT IB PCU FAIL. SWAPPED SECU UNITS TO PUT 49-164-05 IN THE NR 1 POSITION AND PLACED PCU ON MEL 27-62-03. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008040100099 20080401 00099 NM 2008 4 1 USAA920080678 1 20080320 A 5754 114N407637 PANEL BOEING 757 7572G7 1384963 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 908AW 24233 MCN - MAJOR REPAIR - C3 CHECK - LEFT WING NR 2 SLAT COVE PANEL CRACKED, OSS 658. REPLACED LEFT WING NR 2 SLAT COVE PANE L, OSS 658 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008040100110 20080401 00110 2008 4 1 MCC2008F00000 4 20080221 A 6122 89741015 GOVERNOR SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33110UA 01514 WP MCAULY 4HFR34 4HFR34C652 NE PROP FAILED E MCCA O OTHER O OTHER NR NOT REPORTED 1 SW 11 26991 AC666 P44484C WHILE TRAINING FOR A CHECK RIDE, POWER WAS PULLED BACK TO SIMULATE ENGINE AT CONDITION. WHEN POWER WAS REAPPLIED, ENGIN E FAILED TO RESPOND ENGINE WAS SECURED, TROUBLESHOOTING DECIDED PROP GOV FAILED. PROP GOV WAS REPALCED WITH OVERHAULED UNIT, ALL CHECK SAT. SUSPECT BROKEN COUNTERWEIGHT IN GOVN WAS THE PROBLEM. (K) 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 2008030700149 20080307 00149 SO 2008 3 7 SMIA200806004 1 20080219 A 5320 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 679AE 9357 5000 14500814 DURING MBV INSP, THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REPAIR, PERFORMED A CUT OUT ON LEFT OMEGA BEAM. PRE PARED EXTERNAL ANGLE, FILLER AND TWO SHIMS. PARTS CLEANED AND TREATED AND INSTALLED IN AIRCRAFT. REPAIR DONE IAW EMBRA ER 145 SRM (SRM EMB-145/1142 REV 39) CHAPTER 53-00-10 FIG 201. 2 L 7 2 4T RT T00011AT 2008030700151 20080307 00151 NM 2008 3 7 2008UALA00936 1 20080220 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 128UA 30023 SEAT 57H IN SEAT EMERGENCY PATH LIGHT MISSING. REPLACED EEL STRIP. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700154 20080307 00154 NM 2008 3 7 2008UALA00948 1 20080219 A 3397 20131A POWER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 660UA 27115 AFT GALLEY XAISLE EEL INOP. REPLACED EEL POWER RIBBON, CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030700157 20080307 00157 NM 2008 3 7 2008UALA00949 1 20080219 A 3350 1317 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 660UA 27115 EXT EMERGENCY LIGHT, AFT OF WING RT SIDE IS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030700158 20080307 00158 NM 2008 3 7 2008UALA00963 1 20080220 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 310UA 23671 AFT HALF OF 1ST CLASS FLOOR EEL LIGHTS INOP. SECURED EEL LIGHT STRIP. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700166 20080307 00166 WP 2008 3 7 NWAA080749863 1 20080223 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 772NC 47774 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WERE IN OPERATIVE. MAINTENANCE REPLACED THE APPLICABLE BATTERIES AND OPERATIONALLY CHECKED THE SYSTEM. ALL TESTS WERE GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008030700173 20080307 00173 NM 2008 3 7 2008UALA00965 1 20080221 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY LIGHT ROW 5A AFT INOP. RESECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700177 20080307 00177 SO 2008 3 7 SWIA200819269 1 20080226 A 5210 DOOR EMB 120 EMB120ER 3260203 SO MAIN PAX BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 295SW 120322 FLT 5744 - CABIN DOOR IS VERY DIFFICULT TO CLOSE. LUBRICATED DOOR AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008030700182 20080307 00182 NM 2008 3 7 2008UALA00970 1 20080220 A 5753 FLAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT WING DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 502UA 24623 LEFT WING, INBOARD FLAP, OUTBOARD LOWER TRAILING EDGE IS DENTED. PERFORMED REPAIR ON AREA. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030700184 20080307 00184 EU 2008 3 7 2008UALA00973 1 20080222 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 497UA 1847 CREW O2 NEEDS SERVICING 1420 PSI. SERVICED CREW O2 TO FULL. NO LEAKS WERE NOTED FROM THE SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030700185 20080307 00185 EA 2008 3 7 TRAX200800315 1 20080222 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 681BR 7680 PASSENGER DOOR FORWARD ANCHOR FITTING IS CRACKED. 2 L 7 2 4F RT A21EA 2008030700193 20080307 00193 EA 2008 3 7 TRAX200800323 1 20080225 A 3350 LENS CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 EMERGENCY EXIT LIGHT ON WARDROBE JUST BELOW FLASHLIGHT, LENS COVER CRACKED. REMOVED AND REPLACED EXIT LIGHT LENS COVER IAW 33-51-01. 2 L 7 2 4F RT A21EA 2008030700197 20080307 00197 EU 2008 3 7 2008UALA00990 1 20080223 A 3350 CIRCUIT BREAKER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN OUT OF TOLERANCE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 417UA 483 FOUND EXT LOADS AFT L ON 3 SVC. RESET EMERGENCY LIGHT CIRCUIT BREAKER, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030700202 20080307 00202 EA 2008 3 7 TRAX200800328 1 20080226 A 5553 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA STAB TO FUSE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 RT VERTICAL STAB-TO-FUSELAGE DRAG ANGLE CRACKED AT AFT END. 2 L 7 2 4F RT A21EA 2008030700204 20080307 00204 EA 2008 3 7 TRAX200800332 1 20080226 A 5321 FLOOR PANEL CNDAIR CL600 CL6002C10 1390015 EA COCKPIT BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 AFT LAND OF CENTER COCKPIT FLOOR BADLY CORRODED. REMOVED AND REPLACED AFT FLOOR LAND OF CENTER COCKPIT PER SRM 51-42-21 . 2 L 7 2 4F RT A21EA 2008030700209 20080307 00209 NM 2008 3 7 2008UALA01008 1 20080222 A 3350 582233 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 663UA 27160 EMERGENCY LIGHTS ON LEFT + MID SIDE OF 1ST CLASS GALLEY + LEFT SIDE OF CABIN FROM 1L TO MID LAVS. REPLACED EEL BATTERY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030700210 20080307 00210 NM 2008 3 7 2008UALA01010 1 20080223 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EEL LIGHT INOP: SEAT 6G FWD SECTION. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700213 20080307 00213 NM 2008 3 7 2008UALA01013 1 20080223 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EEL INOP: ROWS 55 THRU 59 LT. SECURED LOOSE CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700221 20080307 00221 NM 2008 3 7 2008UALA01018 1 20080224 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 UPPER DECK CEILING 2 EA EMERGENCY LIGHT IS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700224 20080307 00224 NM 2008 3 7 2008UALA01019 1 20080224 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 SEAT 55HJK EMERGENCY LIGHT IS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700225 20080307 00225 NM 2008 3 7 2008UALA01020 1 20080224 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 ZONE D CEILING RIGHT SIDE EMERGENCY 2 EA LIGHT 2 EA IS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700228 20080307 00228 EU 2008 3 7 2008UALA01025 1 20080223 A 2530 2714 CHILLER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AFT GALLEY SHORTED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 457UA 1146 SMELL OF ELECTRICAL SMOKE LAST 5 MIN OF FLIGHT. AFT GALLEY, FWD CHILLER SHORTED. REPLACED CHILLER. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030700232 20080307 00232 EU 2008 3 7 TRAX200800343 1 20080227 A 5720 ANGLE AEROSP ATR72 ATR72212 8680945 EU RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 RT SPLICE ANGLE ON WING PRESSURE AT FR 27 STR 4 CRACKED. 2 H 7 2 4T RT A53EU 2008030700241 20080307 00241 NM 2008 3 7 USAA920080476 1 20080209 A 5753 SKIN BOEING 737 7373G7 1384595 NM FORE FLAP DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 1307 24009 MCN - MAJOR REPAIR - C18 CHECK - LEFT WING INBOARD FORE FLAP LOWER SURFACE HAS AREA DEBONDED, WBL 175 - WBL 178. REPAIR ED AREA OF DISBOND LEFT WING INBOARD FORE FLAP LOWER SURFACE, WBL 175 - WBL 178 IAW B737 SRM 51-70-10. 2 L 7 2 4F RT A16WE 2008033100055 20080331 00055 EU 2008 3 31 TRBA2008034 1 20080324 A 2910 AS117060143 HYDRAULIC LINE AEROSP ATR72 ATR72212 8680945 EU HYHDRAULIC SYS FAILED A TRBA O OTHER O OTHER DE DESCENT 1 SO 29 369AT 369 GREEN SYSTEM LOW LEVEL LOST GREEN SYSTEM PRESSURE. REMOVED AND REPLACED HYDRAULIC HOSE, OPS CHECK GOOD IAW JIC 29-00-00 . 2 H 7 2 4T RT A53EU 2008033100066 20080331 00066 2008 3 31 AMTA200800125 4 20080224 A 3410 C16221KA02 DISPLAY BOEING 737 73783N 13844HI NM ISFD UNSERVICEABLE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 319TZ 30643 ISFD HAS STRIPES AND GOING DARK ON RT SIDE. REMOVED AND REPLACED ISFD IAW MM 34-24-02. PERFORMED ALTERNATE STATIC AND ALTERNATE PITOT LEAK CHECKS IAW MM 34-11-00. (K) 2 L 7 2 4F RT A16WE 2008033100073 20080331 00073 NM 2008 3 31 AMTA200800156 1 20080228 A 5347 RAIL BOEING 737 73783N 13844HI NM BS 767 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 RAIL ASSY RBL 13.84, STA 767, HAVE LIGHT CORROSION. REMOVED CORROSION, ORG MAT .44, FOUND TO BE OUT OF LIMITS IAW SRM 5 3-00-53-1A, DETAIL D, FABRICATED REPAIR PART FROM IAW EA 737-5300-08-A0036. 2 L 7 2 4F RT A16WE 2008033100074 20080331 00074 NM 2008 3 31 AMTA200800157 1 20080228 A 5347 RAIL BOEING 737 73783N 13844HI NM BS 727 MISREPAIRED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 AFT CARGO RAIL ASSY AT STA 727I, LBL 12.5, UNION AREA WAS TRIMMED BY MISTAKE. FABRICATED REPAIR PART IAW EA 737-5300-08 -A0037. (K) 2 L 7 2 4F RT A16WE 2008033100077 20080331 00077 NM 2008 3 31 AMTA200800160 1 20080228 A 5320 SCUFF PLATE BOEING 737 73783N 13844HI NM BS 847 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 AFT CARGO COMPARTMENT SCUFF PLATE CUT OUT, STA 847 OUTSIDE AREA HAS LIGHT CORROSION. REMOVED LIGHT CORROSION, ORG MAT . 080, MAT LOSS .002, REM MAT .078, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01-1A, FIG 103, ALODINED AND PRIMED IAW SRM 51 -20-01. (K) 2 L 7 2 4F RT A16WE 2008033100079 20080331 00079 NM 2008 3 31 AMTA200800161 1 20080228 A 5340 ATTACH FITTING BOEING 737 73783N 13844HI NM LAVATORY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LAV E AFT OB ATTACH FITTING HAS SURFACE CORROSION. REPLACED ATTACHMENT FITTING BLOCK PN C23602-159-003 AND BLOCK FLOOR PN C22102-445-107 IAW 25-46-99, REPAIR 1 PG 76. (K) 2 L 7 2 4F RT A16WE 2008033100082 20080331 00082 EU 2008 3 31 08FDEA01146 1 20080326 A 5712 A57940896 RIB AIRBUS 300 A300B4622R 3930312 EU RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 DURING SB 28-6028 EMBODIMENT, 2 HOLES WERE MIS-DRILLED IN RIB 2 AFT WEB, BOTH WINGS. REPAIR PERFORMED BY INSTALLATION O F RIVETS TO FILL MIS-DRILLED HOLES, WITH REMAINING ACTIONS AS PER SB, ALL IAW EA6-5720-115257 AND RAS/BAE/1006544/2008 I SSUE A. 2 L 7 2 4F RT A35EU 2008033100085 20080331 00085 NM 2008 3 31 AMTA200800166 1 20080228 A 5730 SKIN PANEL BOEING 737 73783N 13844HI NM LT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LT WING FUEL TANK ACCESS 532PB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROS ION ON LT FUEL TANK ACCESS LANDING 532PB IAW SRM 51-01-02-0G, ORG MAT .175, MAT LOSS .003, REM MAT .170, FOUND WITHIN LI MITS IAW SRM 57-20-01-1A, PERFORMED FLAP PEENING IAW SRM 51-20-06 AND SOPM 20-10-03. 2 L 7 2 4F RT A16WE 2008033100089 20080331 00089 NM 2008 3 31 AMTA200800170 1 20080228 A 5730 SKIN PANEL BOEING 737 73783N 13844HI NM LT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LT WING FUEL TANK ACCESS 532KB HAS PITTING CORROSION ON LWR SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING ON LWR F UEL TANK ACCESS LANDING 532KB IAW B737-800, SRM 51-10-01-0G, ORG MAT .205, MAT LOSS .003, REM MAT .202, FOUND TO BE WITH IN LIMITS IAW SRM 57-20-01-1A, PERFORMED FLAP PEENING IAW SRM 51-20-06 AND SOPM 20-10-03. (K) 2 L 7 2 4F RT A16WE 2008033100095 20080331 00095 NM 2008 3 31 AMTA200800176 1 20080228 A 5730 SKIN PANEL BOEING 737 73783N 13844HI NM LT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LT WING FUEL TANK ACCESS 532CB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROS ION ON LT FUEL TANK ACCESS LANDING 532 CB IAW B737-800, SRM 51-10-02-0G, ORG MAT .202, MAT LOSS .003, REM MAT .199, FOUN D TO BE WITHIN LIMITS IAW SRM 57-20-01-1A-1, PERFORMED FLAP PEENING IAW SRM 51-20-06 AND SOPM 20-10-03. (K) 2 L 7 2 4F RT A16WE 2008033100097 20080331 00097 NM 2008 3 31 AMTA200800178 1 20080228 A 5730 SKIN PANEL BOEING 737 73783N 13844HI NM LT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LT WING FUEL TANK ACCESS 532AB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROS IN ON LT WING FUEL TANK ACCESS LANDING IAW B737-800, SRM 51-20-02-0G, ORG MAT .202, MAT LOSS .002, REM MAT .200, FOUND T O BE WITHIN LIMITS IAW SRM 57-20-01-1, PERFORMED FLAP PEENING IAW SRM 51-20-06 AND SOPM 20-10-03. (K) 2 L 7 2 4F RT A16WE 2008033100099 20080331 00099 NM 2008 3 31 AMTA200800180 1 20080228 A 5730 SKIN PANEL BOEING 737 73783N 13844HI NM LT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LT WING FUEL TANK ACCESS 531AB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROS ION ON LT FUEL TANK ACCESS LANDING IAW SRM 51-10-02-0G, ORG MAT .202, MAT LOSS .005, REM MAT .197, FOUND TO BE WITHIN LI MITS IAW SRM 57-20-01-1A-1, PERFORMED FLAP PEENING IAW SRM 51-20-06 AND SOPM 20-10-03. (K) 2 L 7 2 4F RT A16WE 2008033100100 20080331 00100 WP 2008 3 31 08FDEA01151 1 20080326 A 5753 ARC0502501 HINGE BRACKET DOUG DC10 DC1010F 3022111 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MODIFICATION MD10 ACF RT OUTBOARD FLAP INBOARD HINGE WITH RUST, BUSHING WITH PLAY AND SHIM WITH OXIDE. REPLACED HINGE FLAP P/N ARC0502-501 FOR DWG ARC0504. 2 L 7 3 4F A22WE 2008033100105 20080331 00105 NM 2008 3 31 AMTA200800181 1 20080228 A 5730 SKIN PANEL BOEING 737 73783N 13844HI NM LT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LT WING FUEL TANK ACCESS 532DB HAS PITTING CORROSION ON LWR SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORRODIO N ON LT WING FUEL TANK ACCESS LANDING, SRM 51-20-002-0G, ORG MAT .204, MAT LOSS .004, REM MAT .200, FOUND TO BE WITHIN L IMITS IAW SRM 57-20-01-1A-1, PERFORMED FLAP PEENING IAW SRM 51-20-06 AND SOPM 20-10-03. (K) 2 L 7 2 4F RT A16WE 2008033100106 20080331 00106 NM 2008 3 31 AMTA200800182 1 20080228 A 5740 CLAMP BOEING 737 73783N 13844HI NM RT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 RT WING FUEL TANK ACCESS 632RB HAS PITTING CORROSION ON CLAMP RING. REMOVED PITTING CORROSION ON CLAMP RING IAW B737-80 0, SRM 51-10-02-0G, ORG MAT .129, MAT LOSS .002, REM MAT .127, FOUND TO BE WITHIN LIMITS IAW SRM 57-20-01-1A, ALODINE CL AMP RING IAW SRM 51-10-01-0G. (K) 2 L 7 2 4F RT A16WE 2008033100113 20080331 00113 NM 2008 3 31 AMTA200800190 1 20080301 A 5347 RAIL BOEING 737 73783N 13844HI NM BS 727 OUT OF LIMITS A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 RAIL ASSY RBL 13.84, STA 727I (T-UNION) AREA, ORG MAT .071, MAT LOSS .034, REM MAT .037, FOUND TO BE OUT OF LIMITS, IAW SRM 53-00-53-1A, FIG 103, DETAIL D, FABRICATED REPAIR PART FROM BAC 1509-100688 IAW EA 737-08-A0037. (K) 2 L 7 2 4F RT A16WE 2008033100119 20080331 00119 NM 2008 3 31 AMTA200800198 1 20080301 A 5347 RAIL BOEING 737 73783N 13844HI NM BS 767 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 RAIL ASSY LBL 8.1, STA 767, HAVE A UNIFORM CORROSION, AFT CARGO COMPARTMENT. REMOVED CORROSION ON RAIL, ORG MAT .071, M AT LOSS .030, REM MAT .041, FOUND TO OUT OF LIMITS IAW SRM 53-00-53-1A. DETAIL D, FABRICATED REPAIR PART FROM BAC 1510- 1355 IAW EA 737-5300-08-10036. (K) 2 L 7 2 4F RT A16WE 2008033100120 20080331 00120 NM 2008 3 31 AMTA200800199 1 20080301 A 5347 RAIL BOEING 737 73783N 13844HI NM BS 767 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 RAIL ASSY LBL 3.0, STA 767, HAVE A LIGHT CORROSION, AFT CARGO COMPARTMENT. REMOVED CORROSION ON RAIL ASSY, ORG MAT .071 , MAT LOSS .025, REM MAT .046, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A DETAIL D, FABRICATED REPAIR PART FROM BAC 1 510-1355 IAW EA 737-5300-08-A0036. (K) 2 L 7 2 4F RT A16WE 2008033100126 20080331 00126 EA 2008 3 31 SWIA200819376 1 20080323 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR DEFECTIVE A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 460SW 7803 FLT 3775 - SERVICE DOOR WON'T OPEN OR CLOSE USING OUTER HANDLE. REPLACED SERVICE DOOR OUTER HANDLE ASSEMBLY IAW AMM 52- 41-03. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008033100127 20080331 00127 NM 2008 3 31 AMTA20800205 1 20080303 A 3150 NONE BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE WX RADAR FALSE INDICATION A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 519AT 27975 WX RADAR DISP MESSAGE ON HSI. PERFORMED BITE CHECK IAW FIM 34-43-00, NO FAULTS FOUND. SYSTEM CHECKS GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008033100128 20080331 00128 EA 2008 3 31 SWIA200819377 1 20080323 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF RIG A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 498CA 7792 FLT 2640 - MAIN CABIN DOOR WOULD NOT SHUT PROPERLY. RIGGED PASSENGER DOOR ASSEMBLY IAW AMM 52-11-25. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008033100132 20080331 00132 EA 2008 3 31 SWIA200819378 1 20080323 A 2621 4739163 EXTINGUISHER CNDAIR CL600 CL6002C10 1390015 EA LT ENGINE LOW PRESSURE A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 767SK 6861 6861 10233 FLT 6151 - RECEIVED AN "ENG BOT LO 1" EICAS CAUTION MESSAGE. REPLACED LEFT ENGINE FIRE BOTTLE IAW CRJ 700 MM 26-21-07. MESSAGE EXTINGUISHED. 2 L 7 2 4F RT A21EA 2008033100140 20080331 00140 SO 2008 3 31 SWIA200819379 1 20080311 A 2150 SWITCH EMB 120 EMB120ER 3260203 SO LT A/C PACK MALFUNCTIONED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 07 583SW 120351 FLT 3708 - RECEIVED A "SMOKE" AURAL WARNING WITH SMOKE IN THE CABIN. REPLACED LEFT PACK SELECTOR SWITCH. OPS CHECK GOO D. 2 L 7 2 4T RT A31SO 2008033100141 20080331 00141 SO 2008 3 31 SWIA200819380 1 20080315 A 2913 PV302229 PUMP EMB 120 EMB120ER 3260203 SO HYDRAULIC SYS LEAKING A SWIA O OTHER K FLUID LOSS UK UNKNOWN 1 NM 07 586SW 17792 17792 120354 FLT 3678 - LOST BLUE HYDRAULIC SYSTEM FLUID. REPLACED BLUE SYSTEM MECHANICAL ENGINE DRIVEN PUMP AND RESERVOIR RELIEF VA LVE. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008032700365 20080327 00365 NM 2008 3 27 AALA200800565 1 20080310 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT SEAT 40C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 40C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700370 20080327 00370 NM 2008 3 27 AALA200800553 1 20080310 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 929AN 30078 MIA - EMERGENCY LIGHT AT OVERHEAD SEAT 22C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008032700374 20080327 00374 NM 2008 3 27 AALA200800525 1 20080307 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 787AL 30010 DFW - EMERGENCY LIGHT AT SEAT 40G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 40G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700398 20080327 00398 NM 2008 3 27 AALA200800572 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032700401 20080327 00401 NM 2008 3 27 AALA200800575 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800007 20080328 00007 NM 2008 3 28 AALA200800584 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT SEAT 40G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 40G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008032800014 20080328 00014 WP 2008 3 28 AALA200800530 1 20080309 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 449AA 49475 DFW - EMERGENCY LIGHTS AT OVERHEAD AFT CABIN INOPERATIVE. REPLACED BATTERY PACK B5 27 FOR EMERGENCY LIGHTS AT OVERHEAD AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008032800025 20080328 00025 EA 2008 3 28 A6WA200840107 1 20080216 A 5347 CARGO TRACK CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 430AW 7719 FS 574 CHANNEL CARGO TRACK CRACKED LBL 40 WL 80. CHANNEL FOR CARGO TRACK REMOVED PER SRM 51-42-06, FABRICATED IAW SRM 5 1-24-21, 51-12-00 AND INSTALLED IAW SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2008032800027 20080328 00027 WP 2008 3 28 IXXA08SMN037S 1 20080201 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND EXTERNAL DOUBLER LOWER FUSELAGE BELLY AFT EDGE OF A-PIT BASKET DOOR HAS IMPROPE R REPAIR AT STATION FS 330 LONGERON 34 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DO UBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED REPAIR DOUBLER, TRIPL ER, FILLER SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA F ORM 8110-3 NUMBER 08110 DATED 03-13-08, SEMAN DRAWING ED-4700 DATED 02-12-08, DC8 SRM 51-1-21, 51-3-0, 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, AND 51-3-1. 2 L 7 4 4F RT 4A25 2008032800057 20080328 00057 NM 2008 3 28 SWAA081533 1 20080322 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 251WN 32510 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008032800071 20080328 00071 NM 2008 3 28 SWAA081545 1 20080323 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032800094 20080328 00094 NM 2008 3 28 SWAA081563 1 20080320 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED HC2 CHECK, RT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008032800117 20080328 00117 WP 2008 3 28 UPS08851873 1 20080228 A 5230 DOUBLER DOUG DC8 DC873F 302199F WP CARGO DOOR BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 MAIN CARGO DOOR AFT DOOR JAMB HAS A REPAIR DOUBLER WITH 1 INCH PIECE BROKEN OFF. REMOVED DAMAGED DOU BLER, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-2, 51-1-8, 52-4-0 FIG 4. 2 L 7 4 4F RT 4A25 2008032800119 20080328 00119 EU 2008 3 28 UPS08151885 1 20080229 A 5330 A53610265204 SKIN PANEL AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 149UP 0832 INSPECTION TYPE:5 YR NOSE SECTION LT EXTERNAL FUSELAGE 6 INCH LONG DENT AS MARKED FOUND 3 DENTS ON LEFT LATERAL FUSELAGE SKIN PANEL BETWEEN FR8-10 BELOW Z-1166.4. REPAIRED DENTS NR 1 AND NR 3 PER EO A300-5330-27788-B, AND EA 300-5330 -01-A 1312. DENT NR 2 FOUND WITHIN LIMITS PER EA 300-5330-01-A1312. 2 L 7 2 4F RT A35EU 2008032800121 20080328 00121 WP 2008 3 28 UPS08851884 1 20080318 A 2910 577412083800 HYDRAULIC LINE DOUG DC8 DC871F 302199D WP RT MLG WW CRACKED A IPXA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 01 715UP 45915 INSPECTION TYPE:N/A ATB - ON CLIMBOUT STARTED TO LOSE HYD PRESS/QTY. REMOVED AND REPLACED HYD LINE ON RT MLG BUNGEE CYL INDER. 2 L 7 4 4F RT 4A25 2008032800125 20080328 00125 WP 2008 3 28 UPS08851891 1 20080227 A 5313 5615530228 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 A/C COMPT STA 8 FWD BULKHEAD RT SIDE LONGERON HAS ELONGATED HOLE. REPAIRED STA 8 FWD BULKHEAD RT SID E LONGERON ELONGATED HOLE IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-2 AND SRM 51-1-14. 2 L 7 4 4F RT 4A25 2008032800137 20080328 00137 NM 2008 3 28 SWAA081564 1 20080320 A 3350 20121 CHARGER BOEING 737 7377H4 1384404 NM CABIN FAULTY A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 763SW 27877 DURING SCHEDULED 8Y CHECK, FOUND LT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK CHARGER PER MM. 2 L 7 2 4F RT A16WE 2008032800139 20080328 00139 NM 2008 3 28 SWAA081565 1 20080321 A 3350 417A56014 SIGN BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 792SW 27887 AFT CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2008032800147 20080328 00147 NM 2008 3 28 SWAA081587 1 20080324 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, STR 26L TO STR 27L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032800153 20080328 00153 SO 2008 3 28 C2XA08SH049 1 20080326 A 5230 14523918001 SKIN EMB 145 EMB145XR 3260214 SO CARGO DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 21129 145703 SHV - DURING C-CHECK IT WAS FOUND THAT THE CARGO DOOR INNER SKIN HAD CORROSION AROUND SEVERAL SCREW HOLES. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5230-01173. THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 L 7 2 4F RT 2008032800171 20080328 00171 NM 2008 3 28 SWAA081608 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032800175 20080328 00175 NM 2008 3 28 SWAA081612 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008032800199 20080328 00199 SO 2008 3 28 RAIA00803019 1 20080323 A 2150 8152917 SWITCH EMB 145 EMB145LR 3260212 SO NR 2 PACK MALFUNCTIONED A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CE 03 812HK 145373 PRE FLT 5581 - STL - REMOVED AND REPLACED NR 2 PACK DUCT OVERTEMP SWITCH AND THE CROSSOVER DUCT. OPS CHECKED GOOD WITH NO ADDITIONAL SMOKE PRESENT. 2 L 7 2 4T RT T00011AT 2008030700247 20080307 00247 NM 2008 3 7 USAA920080482 1 20080216 A 5340 143N581220 STRINGER CLIP BOEING 757 7572S7 1384962 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 901AW 23321 MCN - MAJOR REPAIR - C12 CHECK - CRACKED STRINGER CLIP, BS 845, S22R. REPLACED STRINGER CLIP, BS 845, S22R IAW B757 SR M 51-40-02. 2 L 7 2 4F RT A2NM 2008030700249 20080307 00249 NM 2008 3 7 USAA920080484 1 20080210 A 5320 146N832853 SILL BOEING 757 7572S7 1384962 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 901AW 23321 MCN - MAJOR REPAIR - C12 CHECK - CORROSION ON L2 DOOR CUT OUT LOWER SILL INNER CHORD, BS 692 - BS 728, LBL 48, WL 208. REPLACED L2 DOOR CUT OUT LOWER SILL INNER CHORD, BS 692 - BS 728, LBL 48, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008030700251 20080307 00251 NM 2008 3 7 USAA920080492 1 20080221 A 5340 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 CLT - MAJOR REPAIR - C17 CHECK - CRACKED STRINGER TIE CLIP, BS 937, S25R. REPLACED STRINGER TIE CLIP, BS 937, S25R IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008030700253 20080307 00253 NM 2008 3 7 USAA920080494 1 20080212 A 5320 694122616 ANGLE BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CORROSION ON ANGLE, BS 993, RBL 43. REPLACED ANGLE, BS 993, RBL 43 IAW B737 SRM 51-40- 02. 2 L 7 2 4F RT A16WE 2008030700254 20080307 00254 NM 2008 3 7 USAA920080495 1 20080208 A 5320 65528942 CHANNEL BOEING 737 7373G7 1384595 NM BS 540 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK, CRACKED CHANNEL, BS 540, RBL 2.2, WL 208. REPLACED CHANNEL, BS 540, RBL 2.2, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008030700255 20080307 00255 NM 2008 3 7 USAA920080496 1 20080215 A 5340 69353521 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER TIE CLIP, BS 927, S24R. REPLACED STRINGER TIE CLIP, BS 927, S24R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008030700259 20080307 00259 NM 2008 3 7 USAA920080517 1 20080225 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 456UW 25020 PIT - MAJOR REPAIR - FBH INSPECTION, CRACKED BULKHEAD, BS 178, RBL 5.7, WL 218. REPAIRED BULKHEAD, BS 178, RBL WL 218 I AW B737 SRM 53-10-08 AND USAIRWAYS EO 5300V152. 2 L 7 2 4F RT A16WE 2008030700264 20080307 00264 NM 2008 3 7 USAA920080520 1 20080228 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 PHX - MAJOR REPAIR - OVERNIGHT CHECK - CRACKED FUSELAGE SKIN, BS 727D - BS 727E, S23L. REPAIRED FUSELAGE SKIN, BS 727D - BS 727E, S23L IAW USAIRWAYS TYPICAL REPAIR 53-33. 2 L 7 2 4F RT A16WE 2008030700271 20080307 00271 EU 2008 3 7 2008UALA01032 1 20080225 A 2730 3945128102 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELAC FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 456UA 1128 CREW REPORTS ELAC 2 FAULT. ELAC FAULT/FAILURE-NFF. REPLACED ELAC2. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030700279 20080307 00279 NM 2008 3 7 USAA920080533 1 20080222 A 5340 143N534531 ATTACH FITTING BOEING 757 7572S7 1384962 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 901AW 23321 MCN - MAJOR REPAIR - C12 CHECK, CRACKED CLIP, BS 620, S24R - S26R, WL 163. REPLACED CLIP, BS 620, S24R - S26R, WL 163 I AW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008030700283 20080307 00283 NM 2008 3 7 08FDEA00476 1 20080218 A 5320 146N5447U14 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD STRINGER R.755, STA 1460-1480. TO EVALUATE EXISTING REPAIR. EXISTING REP AIR FOUND NOT IAW B757 SRM 51-70-11 FIG 1, DETAIL I, II. STRINGER R 7.55 FROM STA 1460 TO STA 1480 REPLACED IAW B757 SRM 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 8-2-100 CRITIERIA. 2 L 7 2 4F RT A2NM 2008030700285 20080307 00285 NM 2008 3 7 08FDEA00479 1 20080218 A 5320 146N5447U11 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD STRINGER L10.45, STA 1460-1480, TO EVALUATE EXISTING REPAIR. EXISTING REP AIR FOUND NOT IAW B757 SRM 51-70-11 FIG 1, DETAIL I, II STRINGER L10.45. REPLACED IAW B757 SRM 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008030700289 20080307 00289 NM 2008 3 7 08FDEA00652 1 20080229 A 5313 A6A7112511 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 HFEC INSPECTION CARRIED OUT AND FOUND CRACK AT LONGERON NR 2 SPLICE WITH CRACK LENGTH OF APPROXIMATELY 1 INCH AT STATI ON 6-100. CRACKED LONGERON SPLICE AT STATION 6-100, REMOVED AS PER SRM 51-31-01, VOL 2. NEW LONGERON SPLICE FABRICATED AS PER DRAWING A6A7112 AND INSTALLED AS PER SRM 51-31-01, VOL 2. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008030700292 20080307 00292 EU 2008 3 7 08FDEA00655 1 20080229 A 5347 A53612524200 SEAT TRACK AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND CORROSION ON SEAT TRACK C14-19, Y450. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008030700294 20080307 00294 EU 2008 3 7 08FDEA00657 1 20080229 A 5330 A53777983 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 PREVIOUS REPAIR IN AREA OF STATIC PORTS FOUND. REPAIR PERFORMED BY REWORK TO MINIMUM SKIN THICKNESS OF 1.04MM IAW RAS/D ABRE/7009009/2008 ISS B, APPROVED BY EA 6-5314-115247. 2 L 7 2 4F RT A35EU 2008033100032 20080331 00032 WP 2008 3 31 08FDEA00990 1 20080317 A 5321 AGA38654 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 AFT PIT FLOOR PANEL NR 187 JF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL NR 187 JF. POTTED EDGES; COMPLETED CURE; SANDED EDGE POTTING AND INSTALLED INSERTS. FABRICATED TOP SHEET; LAYED UP TOP SHEET UNDER A VAC BAG; COMPLETED CURE; COUNTER SUNK HOLES AND APPLIED NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008033100086 20080331 00086 NM 2008 3 31 AMTA200800168 1 20080228 A 5730 SKIN PANEL BOEING 737 73783N 13844HI NM LT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LT WING FUEL TANK ACCESS 532MB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROS ION ON LT FUEL TANK ACCESS LANDING 532MB IAW SRM 51-01-02-0G, ORG MAT .176, MAT LOSS .003, REM MAT .173, FOUND WITHI8N L IMITS IAW SRM 57-20-01-1A, PEFORMED FLAP PEENING IAW SRM 51-10-06 AND SOPM 20-10-03. (K) 2 L 7 2 4F RT A16WE 2008033100088 20080331 00088 NM 2008 3 31 AMTA200800169 1 20080228 A 5730 SKIN BOEING 737 73783N 13844HI NM LT WING CORRODED E AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LT WING FUEL TANK ACCESS 532LB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING. REMOVED PITTING CORROSION ON LWR FUEL TANK ACCESS LANDING IAW SRM 51-01-02-0G, ORG MAT .205, MAT LOSS .003, REM MAT .202, FOUND TO BE WITHIN LIMITS IAW 57-20 -01-1A, PERFORMED FLAP PEENING IAW SRM 51-20-06 AND SOPM 20-10-03. (K) 2 L 7 2 4F RT A16WE 2008033100135 20080331 00135 SO 2008 3 31 XGN2008F00005 2 20080227 A 8530 ECITISN712BAC CYLINDER CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO ENGINE CRACKED A XGNA K NONE O OTHER IN INSP/MAINT 1 SW 05 5421M 544 402B0021 815088 CYLINDER CRACKED BETWEEN NR 1-3 FIN BEHIND INJECTOR, DEFECTIVE PRODUCT. (K) 1 L 7 2 3O 3 O A7CE E8CE 2008033100148 20080331 00148 EA 2008 3 31 SWIA200819381 1 20080320 A 3234 SELECTOR CNDAIR CL600 CL6002D24 1390016 EA LANDING GEAR MALFUNCTIONED A SWIA O OTHER O OTHER AP APPROACH 1 NM 07 807SK 15082 FLT 3945 - RECEIVED A "GEAR DISAGREE" WARNING MESSAGE. REPLACED VALVE SELECTOR ASSEMBLY WITH SERVICEABLE VALVE SELECTOR ASSEMBLY. OPS AND LEAK CHECK GOOD, PN 53340-7 SN OFF NGL/1394/04. 2 L 7 2 4F RT A21EA 2008033100150 20080331 00150 NM 2008 3 31 AMTA200800212 1 20080309 A 2560 GIRT BAR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE L2 DOOR OUT OF POSITION A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 520AT 27976 DURING OPERATIONAL CHECK OF L-2 DOOR ESCAPE SLIDE SAMPLING W/C 222M2503 INTERIOR DOOR HANDLE WAS DIFFICULT TO OPEN. INS PECTED AND FOUND GIRT SLIDE MATERIAL RUBBING AGAINST LOWER GATE SEAL. ADJUSTED L-2 DOOR FLOOR FITTINGS TO RELEIVE TENSI ON BETWEEN LOWER DOOR GATE AND GIRT MATERIAL IAW MM 52-11-25. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008033100151 20080331 00151 WP 2008 3 31 AMTA200800214 1 20080309 A 3350 RPS1B CHARGER DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL EMERGENCY LIGHTS UNSERVICEABLE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 705TZ 46915 FWD GALLEY EMERGENCY LIGHTING AND LT AND RT ROWS 2-4 EGRESS LIGHTING INOPERATIVE. FOUND FWD BATTERY POWER SUPPLY FAULTY . REMOVED AND REPLACED FWD POWER SUPPLY ASSY IAW MM 33-51-01. SEAT ROWS 2-4, OPS CKS GOOD. (K) 2 L 7 3 4F 4 F A22WE A23EA 2008033100152 20080331 00152 2008 3 31 AMTA200800215 4 20080308 A 2310 TRANSMITTER BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE LT HF SYSTEM INOPERATIVE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 519AT 27975 L HF TRANSMITTER INOP AT ALL CREW STATIONS. REMOVED AND REPLACED TRANSCEIVER IAW AMM 23-11-03-4, OPS CK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008033100154 20080331 00154 EA 2008 3 31 SWIA200819383 1 20080318 A 7603 CABLE CNDAIR CL600 CL6002B19 1900309 EA POWER LEVER OUT OF ADJUST A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 449SW 7699 FLT 3942 - LEFT THRUST LEVER IS VERY STIFF. ADJUSTED AND REPOSITIONED ATR TO GEARBOX CABLE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008033100159 20080331 00159 NM 2008 3 31 AMTA200800224 1 20080313 A 3350 D71701100 BATTERY PACK BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE EMERGENCY LIGHTS UNSERVICEABLE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 550TZ 32584 EMERGENCY EXIT SIGN AT MID AFT OVERHEAD RAFT, RT EMERGENCY DOOR OVERHEAD EXIT SIGN, AND LT EMERGENCY DOOR AFT EXIT SIGN INOPERATIVE. REMOVED AND REPLACED BATTERY PACK GROUND CKD NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008033100161 20080331 00161 NM 2008 3 31 AMTA200800225 1 20080301 A 2841 INDICATOR BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE FUEL SYS INOPERATIVE A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 518AT 27974 LT FUEL QUANTITY INDICATOR INOPERATIVE. REPLACED FQIS HARNESS IAW MM 28-41-09, PERFORMED BITE/ SELF TEST IAW MM 28-41-0 0-5. OPS CK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008033100164 20080331 00164 2008 3 31 AMTA200800227 4 20080316 A 3421 H341BWM INDICATOR BOEING 737 73783N 13844HI NM ATTITUDE UNSERVICEABLE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 301TZ 20008 20008 28239 STANDBY ATTITUDE INDICATOR GYRO FLAG SHOWS AND WILL NOT ALINE. REMOVED AND REPLACED STANDBY ATTITUDE INDICATOR REF AMM 34-24-01-4 AND TESTED REF AMM 34-24-00-5. OPS CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 2008033100171 20080331 00171 2008 3 31 AMTA200800232 4 20080317 A 2565 BATTERY DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL ESCAPE SLIDE INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 705TZ 46915 INSPECT INSTALLATION AND OPERATION OF THE R-2 DOOR REMOTE SLIDE PACK IND SYS BATTERIES. INSPECTED INSTALLATION AND OPER ATION OF THE R-2 DOOR REMOTE SLIDE PACK INDICATION SYSTEM BATTERIES; C/W IAW MM 25-61-01. OPS NORMAL. (K) 2 L 7 3 4F 4 F A22WE A23EA 2008033100177 20080331 00177 NM 2008 3 31 TAMF20080017S 1 20080315 A 5712 RIB BOEING 767 767241 1385115 NM GE CF6 CF680C2B2 30025 NE LT WING CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 770QT 23802 CORROSION ON LT WING OB L/E RIB LOWER CHORD STA 779.44 AND 784.44. (2) RIBS WERE FABRICATED AND INSTALLED IAW P0214296 A ND P0214326, AND DRAWINGS 114T2217 AND 114T2218 AND SRM 51-40-02 PG 1-7. 2 L 7 2 4F 4 F RT A1NM E13NE 2008033100179 20080331 00179 SO 2008 3 31 SWIA200819389 1 20080313 A 2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203 SO LAVATORY INOPERATIVE A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 566SW 120341 FLT 3738 - LAV SMOKE DETECTOR INOP. REPLACED LAV SMOKE DETECTOR ASSEMBLY. OPS CHECKS GOOD AT THIS TIME, PN FAV751A-4, SN/OFF 041532. 2 L 7 2 4T RT A31SO 2008030700295 20080307 00295 WP 2008 3 7 08FDEA00662 1 20080229 A 5347 60450818 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 363FE 48263 SEAT TRACK LUG CHIPPED AT FS 845 TRACK 75R. BLENDED AREA AND CHECKED LIMITS FOUND OUT OF LIMITS IAW SRM 51-31-01 VOL II . REMOVED 3 FLOOR PANELS AND CUT OUT DAMAGE AREA OF SEAT TRACK IAW SRM 51-31-01. NEW TRACK MANUFACTURED ON MAE TRAVELE R T8/725393. INSTALLED NEW SEAT TRACK AND 3 EACH FLOOR PANELS IAW SRM 53-31-01 AND 53-21-08-2. FILLED OUT RDR. CLASSI FIED AS A MAJOR REPAIR AND IS RII. 2 L 7 3 4F RT A22WE 2008030600245 20080306 00245 NE 2008 3 6 CALS097002 2 20080120 A 7314 82550112 PUMP BOEING 747 747400 13848AT NM PWA 4056 PW4056 NE FUEL SYS CONTAMINATED W SAJF C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 03 168CL 15 29906 727845 RTO AT SGN DUE TO ENG-3 CONT MSG COME ON DURING T/O ROLL, THE DETAILED DESCRIPTION AS FOLLOWS: 1) DUE TO ENG-3 SVA ACTUA TOR FAILURE TO CAUSE N2 OVERSPEED AND ENG-3 CONT MSG DURING A/C TAKE OFF ROLLING. 2) EEC FAULT MSG: ENG-3 SVA FAIL, ENG- 3 OVERSPEED GOVERNOR FAIL, ENG-3 AOC VALVE FAIL. 3) EEC GROUND ACTUATION TEST FAULT MSG : AOC AND TCC ACTUATOR FAULT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030600271 20080306 00271 NM 2008 3 6 SWAA081073 1 20080226 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008030600300 20080306 00300 EA 2008 3 6 MASA200800169 1 20080226 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A MASA O OTHER O OTHER IN INSP/MAINT 1 SW 07 592ML 7410 C/W REPAIR TO LINTEL FITTING. 2 L 7 2 4F RT A21EA 2008030600302 20080306 00302 EA 2008 3 6 MASA200800170 1 20080226 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A MASA O OTHER O OTHER IN INSP/MAINT 1 SW 07 592ML 7410 PERMANENT REPAIR TO RIGHT REAR PRESSURE BULKHEAD OBLIQUE. 2 L 7 2 4F RT A21EA 2008030700053 20080307 00053 NM 2008 3 7 ASAA0842676 1 20080127 A 5753 6546430129 SKIN BOEING 737 7374Q8 138447Q NM FOREFLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 LEFT WING AFT FLAPS I/B FORE FLAP LOWER SURFACE HAS MULTIPLE DENTS. PREPARED DAMAGED AREA, FABRICATED FILLERS AND 3 EA DOUBLERS AND BONDED IAW B737 400 SRM 51 70 10 PGS 212 241 214 AND 254 3 EA REPAIR DOUBLERS LOCATED AT WBL 90 115 AND 121 . 2 L 7 2 4F RT A16WE 2008030700054 20080307 00054 NM 2008 3 7 GTIA0800034 1 20080201 A 5320 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 501NK 2424 RT SHEAR PLATE BETWEEN FRAME 69 AND 70 SHOWS SIGNS OF CORROSION. REPLACED SHEAR PLATE. 2 L 7 2 4F RT A28NM 2008030700066 20080307 00066 SW 2008 3 7 WGEA200800035 1 20080225 A 2621 FX002002 FIRE BOTTLE ECLIPS EA500 ECLIPSEEA500 3350000 SW RT NACELLE LEAKING E WGEA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 27 136DJ 170 000037 RIGHT ENGINE FIRE BOTTLE LEAKING. REMOVED ENGINE COWLINGS AND PYLON PANELS, RIGHT SIDE FOR ACCESS. REMOVED RIGHT FIRE BOTTLE IAW EA500 AMM 26-20-10. INSTALLED A NEW RIGHT ENGINE FIRE BOTTLE IAW EA500 AMM 26-20-10. RE INSTALLED ENGINE CO WLINGS AND PYLON PANELS AS REQUIRED IAW EA500 AMM 26-20-10. 1 L 7 2 4J RT A00002AC 2008030700071 20080307 00071 EA 2008 3 7 TRAX200800312 1 20080224 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA MAIN PAX BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 FA SAID DOOR WAS A LITTLE DIFFICULT TO CLOSE IN THE LAST INCH OR SO OF TRAVEL, IT SEEMED TO BIND A LITTLE BUT OPERATED N ORMALLY OTHERWISE. 2 L 7 2 4F RT A21EA 2008030700116 20080307 00116 NM 2008 3 7 2008UALA00842 1 20080215 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 EEL LIGHT INOP: SEAT 5E AFT. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700150 20080307 00150 NM 2008 3 7 2008UALA00927 1 20080219 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY LIGHT ROW 5F INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700169 20080307 00169 EA 2008 3 7 SWIA200819264 1 20080221 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA CABIN AIR ODOR A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 909SW 7558 FLT 5924 - AFTER TAKEOFF RECEIVED SMOKE TOILET CAUTION MESSAGE. REPLACED LEFT AND RIGHT COALESCER BAGS IAW AMM 21-51-13 . REMOVED AND REPLACED LAVATORY SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008030700201 20080307 00201 EU 2008 3 7 2008UALA00992 1 20080222 A 5321 FLOORBOARD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO BAY DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 438UA 678 CARGO FLBRD RPL S GLS PNL. MAJOR REPAIR ACCOMPLISHED AT LCQ VIA COA PROJECT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030700203 20080307 00203 EA 2008 3 7 TRAX200800329 1 20080226 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 CEILING AFT MOST EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008030700229 20080307 00229 EA 2008 3 7 TRAX200800340 1 20080228 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA ILLUMINATED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 978EV 7723 MACH TRIM CAUTION AFTER FLAPS FAIL ALONG WITH THE LOSS OF COPILOTS PFD, PFD REAPPEARD ON FINAL APPROACH. EMERGENCY DECL ARED. 2 L 7 2 4F RT A21EA 2008030700278 20080307 00278 NM 2008 3 7 USAA920080532 1 20080208 A 5320 146N545018 INTERCOSTAL BOEING 757 7572S7 1384962 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 901AW 23321 MCN - MAJOR REPAIR - C12 CHECK - CORROSION ON INTERCOSTAL CHORD, BS 1540 - BS 1564, S26R - S27R. REPLACED INTERCOSTAL C HORD, BS 1540 - BS 1564, S26R - S27R IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008030700282 20080307 00282 2008 3 7 2008UALA01035 4 20080225 A 2565 PIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EVAC SLIDE MISSING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 376UA 24641 DOOR 2L SLIDE PACK MISSING SAFETY PIN, NOT LOCATED INSIDE THE POUCH WHEN THE SLIDE WAS REMOVED. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700287 20080307 00287 NM 2008 3 7 08FDEA00484 1 20080218 A 5320 146N541614 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND AT CARGO FLOORBOARD STRINGER R16.10, STA 1320-1340. TO EVALUATE EXISTING REPAIR. EXISTING REPAI R FOUND NOT IAW B757 SRM 51-70-11 FIG 1 DETAIL I, II STRINGER R16.10. REPLACED IAW B757 SRM 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008030700297 20080307 00297 EU 2008 3 7 08FDEA00665 1 20080229 A 5420 CHANNEL AIRBUS 310 A310324 3930206 EU NR 2 PYLON FRACTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 NR 2 PYLON AFT POWER FAIRING 485 AL AFT SUPPORT CHANNEL HAS A FRACTURE AT THE OUTBD EDGE. REMOVED CHANNEL & FABRICATE W EB & CHANNEL ON OPS 00748 & 00749. ASSEMBLED & INSTALLED TO NR 2 PYLON IAW SRM 51-40-01 PG 7. 2 L 7 2 4F RT A35EU 2008030700303 20080307 00303 EU 2008 3 7 2008UALA01042 1 20080227 A 5210 ACCUMULATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R1 DOOR LOW A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 446UA 834 R1 DOOR ACCUM PRESS NEEDS SERVICING. SERVICED TO FULL, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030700305 20080307 00305 NM 2008 3 7 2008UALA01044 1 20080226 A 3350 20131A BATTERY PACK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 330UA 24191 EEL STRIP INOP ROW 15 AFT GALLEY. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700313 20080307 00313 NM 2008 3 7 QXEA200800228 1 20080226 A 2497 CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM GPU SMOKE A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 430QX 4163 PDX - FLIGHT 2432, NOTICED GPU CONNECTOR SMOKING. MAINTENANCE FOUND GPU CONNECTOR FAULTY. NO AIRCRAFT DAMAGE NOTED. U SED ANOTHER GPU. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008030700315 20080307 00315 2008 3 7 2008UALA01052 4 20080226 A 2565 D30654122U1 HINGE PIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 533UA 25073 L1 DOOR SLIDE LOWER LATCH ASSY HINGE PIN IS BROKEN. UNKNOWN DAMAGE. REPLACED L1 DOOR SLIDE ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030700317 20080307 00317 NM 2008 3 7 2008UALA01053 1 20080226 A 2421 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 669UA 30025 LEFT GEN DRIVE LIGHT ILLUM ON TAXI, LEFT IDG RISE TEMP 18. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030700318 20080307 00318 NM 2008 3 7 DHL2008752500 1 20080204 A 5754 STRUCTURE BOEING 727 727223 1384074 NM NR 5 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 RT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/ B BULK SEAL IAW B727 SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR A T L/E SLAT MATERIAL USED 2024T3 .063 PO NR 9006288 DIMENSION 7 INCH BY 8.5 INCH IAW B727 SRM 57-30-4 FIG 11 AND B727 SRM 57-30-2 FIG3 TREATED AND PRIMED DOUBLER REPAIR AND AREA IAW B727 SRM 51-10-2. INSTALLED NEW DOUBLER REPAIR AND REINSTA LLED FASTENERS IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008030700323 20080307 00323 NM 2008 3 7 DHL2008752606 1 20080223 A 5740 6517327U3 ATTACH FITTING BOEING 727 727223 1384074 NM NR 1 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 NR 1 SLAT ACTUATOR INBD ATTACHING RIB (AT SLAT) CRACKED. REMOVED RIB AND "U" CHANNEL FOUND CRACK IAW B727 SRM 51-30-2. LOCATED, DRILLED AND DEBURRED RIB P/N 65-17327U3 PO 7375239 IAW B727 SRM 51-30-5. FABRICATED CHANNEL USING 2024-T3 .07 1 PO 9005922 DIM 6.5 INCH BY 3.5 INCH IAW BDW NR 65-17327 AND B727SRM 51-20-01, 51-20-2, 51-30-5. INSTALLED RIB AND CHA NNEL IAW B727 SRM 51-30-2 AT NR 1 SLAT ACTUATOR. 2 L 7 3 4F A3WE 2008030700328 20080307 00328 NM 2008 3 7 DL757080280 1 20080223 A 2130 211080112 CONTROL PANEL BOEING 757 757232 1384965 NM A/C PACKS MALFUNCTIONED A DALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SO 27 676DL 25981 CREW REPORTS BOTH PACKS FAILED AT FL 40. PERFORMED EMERGENCY DESCENT. MASKED DROPPED AND WERE USED BY APPROXIMATELY 78 PAX AND CREW. REPLACED COCKPIT CABIN CONTROL PANEL FOR MANUAL CONTROL PROBLEM. PERFORMED BITE ON BOTH L/AUTO PRESSURE CONTROLLERS OK. PRESSURIZED A/C OK WITH LT PA AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2008030700331 20080307 00331 NM 2008 3 7 DL76L080298 1 20080301 A 2910 O-RING BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE HYD SYSTEM CUT A DALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 184DN 27111 580327 FLIGHT 117 - DECLARED EMERGENCY INTO ATL DUE TO LOSS OF CENTER SYSTEM HYD QTY AND PRESS LOST. UNEVENTFUL LANDING AND TA XI. FOUND CUT O-RING ON CTR SYS LCCA FILTER BOWL. REPLACED SAME CKS OK. 2 L 7 2 4F 4 F RT A1NM E13NE 2008030700332 20080307 00332 NM 2008 3 7 2008UALA01055 1 20080227 A 5414 RETAINER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 PYLON WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 WEAR WAS FOUND AT SEAL RETAINER OF NR 2 STRUT AFT FAIRING AT SAF STA 362, FAIRING OUTBOARD FRAME. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008030700342 20080307 00342 NM 2008 3 7 USAA920080550 1 20080302 A 3350 FUSE BOEING 737 7373G7 1384595 NM EMERGENCY LIGHTS INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 155AW 23777 FLT NR 298 - LAS-SEA - EEL - AFT CENTER EMERGENCY EXIT SIGN AND PATHWAY LIGHTS FROM LT ROWS 19-23 INOP. MAINTENANCE REP LACED THE POWER SUPPLY FUSES AND PINS 11/12 AND 13/14. EMERGENCY EXIT LIGHTING SYSTEM OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A16WE 2008033100181 20080331 00181 SO 2008 3 31 SWIA200819390 1 20080321 A 7921 OIL COOLER EMB 120 EMB120ER 3260203 SO RT ENGINE LEAKING A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 233SW 120307 FLT 5557 - RIGHT ENGINE OIL PRESSURE DROPPED ON TAKEOFF. REPLACED OIL COOLER IAW EMB 79-21-01. OPS AND LEAK CHECKS GOO D. 2 L 7 2 4T RT A31SO 2008033100182 20080331 00182 EA 2008 3 31 SWIA200819391 1 20080322 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 935SW 7725 FLT 6618 - LEFT WING EMERGENCY LIGHT IS INOP. REPLACED EMERGENCY LIGHT BULB IAW AMM 33-51-00. 2 L 7 2 4F RT A21EA 2008033100192 20080331 00192 NM 2008 3 31 AALA200800596 1 20080311 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 798AN 30797 MIA - EMERGENCY LIGHT AT SEAT 39G LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 39G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008033100193 20080331 00193 NM 2008 3 31 AALA200800594 1 20080311 A 3350 CTR90SR1S HOUSING BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR MISSING HOUSING COVER. REPLACED HOUSING FOR EMERGENCY LIGHT AT LEFT NUM BER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008033100195 20080331 00195 NM 2008 3 31 AALA200800595 1 20080311 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 961AN 30092 MIA - EMERGENCY LIGHT AT SEAT 19D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A16WE 2008033100198 20080331 00198 2008 3 31 AALA200800600 4 20080311 A 2565 D30654122 SLIDE BOEING 757 757223 1384957 NM L1 DOOR FAILED A AALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 610AA 24486 SNA LEFT NUMBER ONE DOOR SLIDE FAILED TO DEPLOY WHEN DOOR OPENED IN ARMED POSITION. REPLACED SLIDE AND POWER RESERVOIR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008033100209 20080331 00209 NM 2008 3 31 DHL2008763528 1 20080314 A 2782 6516275 SUPPORT FITTING BOEING 727 727264 138408M NM KRUEGER FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 NR 6 K-FLAP ACTUATOR MOUNT SPT FITTING CRACKED AT WS 307.5. REMOVED ACTUATOR SUPPORT MOUNT ASSY. FABRICATED SUPPORT WE BS FROM 2024-T3, .063" BY 8" BY 3.5" (2 EA), PO NR 9006027, AND MOUNT DOUBLERS FROM 7075-T6, .125" BY 5" BY 2", (2 EA), PO NR 9005685, ASSEMBLED AND INSTALLED PER B727 SRM 51-30-2, 51-20-1 FIG 7, 51-30-5, AND BAC DWG 65-16275 REV D. 2 L 7 3 4F A3WE 2008033100210 20080331 00210 EU 2008 3 31 08FDEA01150 1 20080326 A 5414 A5461140000100 PANEL AIRBUS 310 A310203 3930313 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 PYLON PANEL NR 424 ER IS CORRODED ON THE INNER AND OUTER SURFACES. REMOVED CORROSION & CHECKED LIMITS IAW SRM 54-5 2-21 PG 104. FOUND TO BE OUT OF LIMITS IAW SRM 54-52-51 PG 104. INSTALLED REPAIR IAW SRM 51-52-51 PGS 219-220. ALODINE D PARTS IAW SRM 51-21-10. PRIMED & PAINTED PARTS IAW SRM 51-32-10 PG 1. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008033100213 20080331 00213 NM 2008 3 31 DHL2008763529 1 20080319 A 5754 651728113 RIB BOEING 727 727264 138408M NM L/E SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 NR 5 L/E SLAT INB TRACK INTERIOR, O/B RIB IS CRACKED. REMOVED AND REPLACED RIB ASSY (I/B AND O/B) WITH P/N 65-17281-13, PO3 8109195, PER B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008033100215 20080331 00215 NM 2008 3 31 QXEA200800308 1 20080313 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM BS 435 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX - C4- SUSPECT CORROSION ON FRAME CASTELLATION FWD SIDE AT STA X435.5 AND STR 24P LT UNDER FLOOR. REMOVED CORROSION IAW CPCM CHAPTER 4. HFEC INSPECTED BLEND AREA FOR CRACKS IAW NDTM PART 6, 51-00-01. NO CRACKS NOTED. UT THICKNESS CHE CK BLENDED AREA IAW NDTM PART 1, 51-00-04 HIGH .032 LOW.029. BLENDED AREA WITHIN LIMITS IAW SRM 51-20-11. APPLIED ALOD INE AND PRIMER IAW SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 2008033100216 20080331 00216 WP 2008 3 31 DHL2008805520 1 20080312 A 5523 SKIN DOUG DC8 DC873F 302199F WP RT ELEVATOR TAB DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 RT ELEV GEAR TAB LWR SKIN DELAMINATED 1.500". CUT OUT DAMAGED SECTION IAW SRM 55-2-2 PAR 4D, PAR 2 FIG 3. FABRICATED DOUBLER (AL2024T3 0.016") IAW SRM 55-4-0 PG 10. BONDED CORE AND DOUBLER IAW SRM 51-1-9 PAR 4. REFER TO NR 108672 FOR W EIGHT AND BALANCE. 2 L 7 4 4F RT 4A25 2008033100217 20080331 00217 WP 2008 3 31 DHL2008805533 1 20080325 A 5320 STIFFENER DOUG DC8 DC873F 302199F WP RT MLG WW CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 RT MLG W/W STIFFENER CORRODED AT STA 857.000. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18 AND FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED ANGLE IAW SRM 51-1-20D, SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-20D, SRM 51-3-1, SRM 51-1-21. LEAK CHECKED GOOD IAW MM 21-31-0 PG 208. REFER TO JC EC-00816-001 (WO 3457) FOR FABRICATION. 2 L 7 4 4F RT 4A25 2008033100220 20080331 00220 WP 2008 3 31 DHL2008805512 1 20080305 A 5320 STRUCTURE DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 INSPECT PREVIOUS REPAIR AT STA 1750 LONGERON L-15L - 17L. ASSURE REPAIR WAS ACCOMPLISHED WITH APPROVED DATA. INDICATE CATEGORY OF REPAIR AND REINSPECTION INTERVAL IF REQUIRED. PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1,4,5. REM OVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL70 75T6 0.071") 2 FILLERS (AL7075T6 0.063") AND (1EA) INTERNAL FINGER DOUBLER (AL7075T6 0.040") IAW SRM 53-2-1 FIG 7 SHEET 1, 4, 5, SRM 53-5-3 FIG 1 ITEM D. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIG 7 SHEET 1, 4, 5, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE) THIS IS A CLASS 1 2 L 7 4 4F RT 4A25 2008033100222 20080331 00222 NM 2008 3 31 QXEA200800316 1 20080320 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - C4- CORROSION ON FRAME CASTELLATION AFT SIDE OF FRAME X597.5 JUST OUTBOARD OF STR 31S. DRILLED OUT THREE RIVETS A ND REMOVED CORROSION IAW CPCM CHAPTER 4. HFEC INSPECTED BLEND AREA FOR CRACKS IAW NDTM, PART 6, 51-00-01, NO CRACKS NOT ED. UT THICKNESS CHECK OF BLENDED AREA IAW NDTM PART 1, 51-00-04 HIGH .050 LOW .048. AREA OF BLEND WITHIN LIMITS REF SR M 51-20-11. APPLIED ETCH ALODINE AND PRIMER IAW SRM 51-20-16 AND 51-20-36. REINSTALLED RIVETS REF SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008033100224 20080331 00224 NM 2008 3 31 QXEA200800318 1 20080320 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM THRESHOLD CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX -C4- CORROSION ON AFT BAG DOOR THRESHOLD ANGLE, ANGLE IS CONNECTING THRESHOLD BULKHEAD AT STA X597.5. REMOVED THRES HOLD ANGLE BY DRILLING OUT RIVETS, REMOVING LOCK FASTENERS AND SCREWS. DRILLED UP NEW ANGLE FROM STOCK INSTALLED 2 NUTP LATES. INSTALL NEW ANGLE BY INSTALLING RIVETS, LOCK FASTENERS AND SCREWS REF SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008033100225 20080331 00225 NM 2008 3 31 QXEA200800320 1 20080320 A 5320 THRESHOLD DHAV DHC8 DHC8202 2809007 NM CARGO DOORWAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX -C4- MCD THRESHOLD CORROSION 2 AREA AND FWD END BETWEEN THRESHOLD AND SILL PLATE. REMOVED THE MCD THRESHOLD BY DRIL LING OUT THE RIVETS HOLDING THE THRESHOLD TO LOWER SILL PLATE, REMOVED 5 NUT PLATES. REMOVED CORROSION FROM LOWER SILL PLATE IAW RD8-53-8921 STEP 1. BLENDED OUT CORROSION AND ALODINED BLENDED AREA IAW RD8-53-8921. HFEC INSPECTED BLEND AR EA FOR CRACKS IAW NDTM, PART 6, 51-00-01, NO CRACKS NOTED. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW RD8-53-8921. REM OVED LESS THAN .009" MATERIAL, REMAINING THICKNESS .041". PRIMED BLENDED AREA IAW RD8-53-8921. 2 H 7 2 4T RT A13NM 2008030700344 20080307 00344 EU 2008 3 7 USAA920080552 1 20080303 A 2750 664700500A4D CONTROL UNIT AIRBUS 320 A320231 3930325 EU TE FLAPS DEFECTIVE A USAA O OTHER J WARNING INDICATION LD LANDING 1 EA 19 625AW 23544 4313 64 FLT NR 441 - YVR-LAS - EMERGENCY LANDING, F/CTL FLAPS LOCKED ALIGNMENT FAULT ON LANDING. FLAPS LOCKED AT ZERO. CREW DE CLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL INTERFACE UNIT. OPERATI ONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008030700345 20080307 00345 EA 2008 3 7 TRAX200800354 1 20080227 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA BS 295 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 CORROSION AT LT FLOOR SILL AT FS 295. BLENDED CORROSION AT FS 295 MEASURED THICKNESS, ALL WORK DONE IAW SRM 53-21-43. 2 L 7 2 4F RT A21EA 2008030700346 20080307 00346 EA 2008 3 7 TRAX200800355 1 20080228 A 5415 ATTACH ANGLE CNDAIR CL600 CL6002C10 1390015 EA RT PYLON CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 RT PYLON INBD ATTACH ANGLE CRACKED FS 1108.0. C/W REPAIR ON RT PYLON INBOARD ATTACH ANGLE AT FS 1108.0. 2 L 7 2 4F RT A21EA 2008030700350 20080307 00350 NM 2008 3 7 2008UALA01064 1 20080227 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 FWD GALLEY DOOR FWD LWR CORNER FRAME CRACKED. MAJOR REPAIR: REPLACED LOWER FORWARD FRAME. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700353 20080307 00353 NM 2008 3 7 2008UALA01067 1 20080227 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 AFT CABIN RIGHT CREASE BEAM INNER CHORD UPPER SURFACE CORRODED BS 947.5 TO 995 AT STR 17R. MAJOR REPAIR: REMOVED CORRODE D CREASE BEAM. REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700356 20080307 00356 NM 2008 3 7 2008UALA01086 1 20080226 A 3260 893501 SENSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT MLG OUT OF ADJUST A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 653UA 25391 AN 'AIR-GND DISAGREE' EICAS MSG DISPLAYED. PERFORMED THE MM32-09-07-210 AIR-GRD SENSOR TEST IN AIR MODE BY JACKING TH E ACFT. FOUND S268 TILT SENSOR OUT OF RANGE PER MM 32-61-99 PG 601. REPLACED S268 TILT SENSOR. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030700357 20080307 00357 NM 2008 3 7 2008UALA01087 1 20080227 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 663UA 27160 EEL LIGHT COVER ON FLOOR AT 13AB AND 14AB IS PULLED UP. SUSPECT NORMAL CREW AND PASSENGER BOARDING AND DEBOARDING. SPLI CED IN NEW EEL STRIP OPS CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030700358 20080307 00358 NM 2008 3 7 2008UALA01088 1 20080227 A 3510 OXYGEN MASK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 351UA 24319 HARNESS ON F/O MASK LEAKS. REPLACED O2 MASK. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700360 20080307 00360 NM 2008 3 7 2008UALA00782 1 20080209 A 2497 BACC45FT1624P5 CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LT GCU SHORTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 LEFT BUSS TIE WILL NOT GO ON LINE. PERFORMED TROUBLESHOOTING. FOUND WIRE SHORT TO GRND FROM L-GENERATOR CONTROL UNIT B -CONNECTOR PIN C11, TO L-GEN DPCT-2. CONFIRMED CONNECTOR D5849P AT FAULT, REPLACED CONNECTOR D5848P, LT BUSS TIE OPER ATED NORMALLY. SUSPECT VIBRATION & HEAT LED TO LOOSENED CONNECTION. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030700362 20080307 00362 NM 2008 3 7 2008UALA00832 1 20080213 A 2130 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE UNKNOWN A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 334UA 24229 RTFL DUE TO A PRESSURIZATION INDICATION. PRESSURIZED AIRCRAFT AND FOUND NO LEAKS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700366 20080307 00366 NM 2008 3 7 SWAA081084 1 20080227 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 13L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008030700367 20080307 00367 NM 2008 3 7 SWAA081085 1 20080227 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND STRINGER 23R CRACKED AT BS 328. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008030700369 20080307 00369 NM 2008 3 7 SWAA081087 1 20080227 A 3350 MS155721 LIGHT BOEING 737 7373K2 13844BA NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008030700377 20080307 00377 NM 2008 3 7 SWAA081095 1 20080227 A 5753 6546430167 SKIN BOEING 737 7373H4 1384600 NM FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED MV2 CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2008030700379 20080307 00379 2008 3 7 SWAA081097 4 20080227 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED C4 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008033100226 20080331 00226 NM 2008 3 31 QXEA200800323 1 20080320 A 5414 SKIN DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - C4- NR 1 NACELLE SKIN FWD MLG DOOR APERATURE, O/B FWD CORNER, HAS A 1/2" CRACK. CUTOUT DAMAGE REF RD8-54-873. PE RFORMED HFEC AROUND CUT OUT IAW NDTM PART 6, 51-00-01, NO CRACKS NOTED. COMPLETED REPAIR IAW RD8-54-873 NOTES 2-5. 2 H 7 2 4T RT A13NM 2008033100231 20080331 00231 WP 2008 3 31 DHL2008805513 1 20080318 A 5720 FITTING DOUG DC8 DC873F 302199F WP WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 NR 4 STUB WING INTERIOR FITTING CRACKED 0.500" STA 562.500 CANT (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DOUGLAS DRAW ING NR 5754705. REMOVED CRACKED FITTING IAW SRM 57-1-0 PG 1, SRM 51-1-21, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AR EA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-21, SRM 51-1-20D. REFER TO JC EC-00812-001 (WO 3457) FOR FABRIC ATION. 2 L 7 4 4F RT 4A25 2008033100232 20080331 00232 WP 2008 3 31 DHL2008805514 1 20080305 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 L2 DOOR, FWD LOWER CORNER REPAIR DOES NOT C/W SR08530021, AD2000-20-08 AND S/B 53-075. PERFORM REPAIR AND DOCUMENT IN A /C LOG AND ON 337 FORM. PERFORMED MAJOR REPAIR IAW AD2000-20-08, S/B DC8 53-075, DOUGLAS DWG 5750776, SR08530021. REMO VED EXISTING REPAIR DOUBLER IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION IAW DOUGLAS DWG SR08530021. PERFORMED NDT INSP I AW DC8 NDT SPM PART 06-10-01-001. NEITHER CRACK NOR CORROSION FOUND. ENCLOSED SMN FORM 242-2. FABRICATED REPAIR DOUBL ER (AL7075T6 0.090") FILLER (AL7075T6 0.080") AND REPAIR TRIPLER (AL7075T6 0.125") IAW DOUGLAS DWG SR08530021. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DOUGLAS DWG SR08530021, SRM 51-1- 2 L 7 4 4F RT 4A25 2008033100233 20080331 00233 WP 2008 3 31 DHL2008805515 1 20080318 A 5320 STRUCTURE DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 "D" BELLY, FWD LOWER CORNER REPAIR C/W IAW SR08530021 AT SEMANS, HOWEVER, INCORRECT STEEL FASTENERS ARE INSTALLED. REPL ACE WITH TITANIUM AS REQUIRED AND ENSURE REPAIR IS IAW SR08530019 AND AD. PERFORMED MAJOR REPAIR IAW FAA FORM 8100-9 DA TED 03-07-08, AD2005-18-07, S/B DC8 53-078 DOUGLAS DWG NR SR08530019, SEMAN DWG ED-4720 DATED 02-26-08. REMOVED EXISTIN G NON STANDARD REPAIR IAW SRM 51-1-21, SRM 51-1-20D. FABRICATED EXTERNAL REPAIR DOUBLER (AL7075T6 0.090") EXTERNAL REPA IR TRIPLER (AL7075T6 0.125") AND FILLER (AL7075T6 0.071") IAW SEMAN DWG ED 47-20, DOUGLAS DWG NR SR08530019. CLEANED, T REATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SEMAN DWG NR ED-4720, DOUGLAS DWG N 2 L 7 4 4F RT 4A25 2008033100240 20080331 00240 WP 2008 3 31 DHL2008805528 1 20080311 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 AFT CARGO COMPT BILGE FITTING CRACKED 2" (STA 1160.000 - 1180.000 L-35R) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 5 3-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8 B. INSTALLED NEW FITTING IAW SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2008033100241 20080331 00241 WP 2008 3 31 DHL2008805509 1 20080228 A 5414 SKIN DOUG DC8 DC873F 302199F WP CFMINT CFM56 CFM563C 13802 EU NR 1 NACELLE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 NR 1 ENG NACELLE INLET COWL UPPER EXTERNAL SKIN WORN, STA YN 147.534 AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED SKIN (AL2024T3 0.080") AND SPLICE (SHEET CRES TYPE 17-7 PH) IAW SRM 71-5-2 FIG 2 SHEET 1. HEAT TREATED SPLICE FROM CRES 17- 7PH TO CRES 17-7PH (H1050) IAW SRM 51-1-16. CLEANED,TREATED AND PRIMED AREA AND SKIN INNER FACE IAW SRM 51-1-8B. INSTA LLED REPAIR PARTS IAW SRM 71-5-2 FIG 2 SHEET 1-2, SRM 51-1-11, SRM 51-1-21, SRM 51-1-21A. 2 L 7 4 4F 4 F RT 4A25 E21EU 2008033100251 20080331 00251 WP 2008 3 31 DHL2008805503 1 20080228 A 5320 STRUCTURE DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 ACCOMPLISH REPAIR AT STA 140 - 160 L-26L - L-27L PER SRM TO INCLUDE FINGER DOUBLERS (MAJOR REPAIR.) PERFORMED MAJOR REP AIR IAW SRM 53-2-1 FIG 7 SHEET 1,3. REMOVED NON STANDARD REPAIR NOT IN ACCORDANCE WITH SRM AS PER SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL7075T6 0.071") AND (2EA) INTERNAL FINGER DOUBLER (AL7075T6 0.040") IAW SRM 53-2-1 FIG 7 SHEET 1, 3, SRM 53-4-1 FIG 5C ITEM B. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1- 8B. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIG 7 SHEET 1,3, SRM 51-1-11, SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D, SRM 51-3 -1 (TORQUE). THIS IS A CLASS I TYPE REPAIR (INITIAL INSP 4.000 LANDING CYCLES, REPETITIVE 4.000, REPLACEMENT N/A, METHO 2 L 7 4 4F RT 4A25 2008033100257 20080331 00257 WP 2008 3 31 DHL2008805532 1 20080325 A 5711 FITTING DOUG DC8 DC873F 302199F WP CENTER WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 CENTER WING REAR SPAR UPPER CAP FITTING CRACKED STA 857.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D, CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D AND SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2008033100259 20080331 00259 WP 2008 3 31 DHL2008805534 1 20080323 A 5320 RIB DOUG DC8 DC873F 302199F WP LT MLG WW WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 LT MLG W/W DOOR UPLATCH RAIL RIB WORN AT STA 890.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW JC EC-00840-001D, DWG D OUGLAS NR 5653490. REMOVED WORN RIB IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1 (TORQUE). REFER TO JC EC-00840-001-D (WO 3457) FOR RIB FABRICATION. REFER TO JC BZ2M2383 FOR OPS CHECK. 2 L 7 4 4F RT 4A25 2008032800086 20080328 00086 2008 3 28 SWAA081555 4 20080320 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032800099 20080328 00099 EU 2008 3 28 U30A200800001 1 20080126 A 2750 D9550011400300 CONTROL UNIT AIRBUS 320 A320214 3930316 EU T/E FLAP STICKING A U30A K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 EA 17 266AV 1152 FLT 561, PUJ-ORD, ON APPROACH THE FLAPS WOULD NOT EXTEND FROM ZERO POSITION. SLATS EXTENDED NORMALLY (ECAM FLAP FAULT W HEN FLAPS 2 SELECTED). ECAM WERE ACTIONS FOLLOWED, AND FCOM & QRH WERE CONSULTED, AND IT WAS NECESSARY TO PREPARE & BRI EF FOR A ZERO FLAP APPROACH. THE CAPT DECLARED AN EMERGENCY & HAD THE FIRE/RESCUE VEHICLES STANDBY. THE APPROACH WAS M ADE IN ACCORDANCE WITH THE QRH WITH NECESSARY ADJUSTMENTS TO CONFIGURATION & SPEED. LANDING WAS UNEVENTFUL. MAINTENANC E C/W TSM 27-51-00-810-803 & OPS CK'D FLAP SYS OK, & FOUND NO TORQUE LIMITERS TRIPPED. FOUND FLAP CONTROL UNIT ASSY TO GET JAMMED/STICKING BETWEEN 0 AND 1 DETENT. REMOVED AND REPLACED FLAP CONTROL UNIT ASSY PER AMM 27-51-43PB401 & OP'S CH 2 L 7 2 4F RT A28NM 2008032800101 20080328 00101 EU 2008 3 28 U30A200800003 1 20080129 A 2752 791A000006 ACTUATOR AIRBUS 320 A320214 3930316 EU T/E FLAP MALFUNCTIONED A U30A L A ABORTED APPROACH UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 EA 17 266AV 21479 21479 1152 FLT 690 ORD-SRQ. ON APPROACH, THE FLAPS JAMMED AT ZERO, AND THE SLATS EXTENDED NORMALLY. CREW PERFORMED A GO-AROUND, A ND DECIDED TO DIVERT TO PIE AND NOTIFIED ATC & DECLARED AN EMERGENCY AS A PRECAUTION. THE APPROACH WAS COMMENCED, AND T HE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE C/W TSM 27-51-00-810-810 RESET BOTH SFCC'S AND NO FAULTS NOTED. FLAP OP'S CHECKED OK, WITH NO DEFECTS NOTED. FURTHER TROUBLESHOOTING FOUND LEFT FLAP DRIVE SYSTEM NEEDED RIGGING & MAINT. C /W ADJUSTMENT OF LEFT FLAP DRIVE TORQUE TUBES & ADJUSTED RIGHT APPU 30CV TO NULL POSITION PER AMM 27-54-00. ALSO FOUND FLAP TRACK NR 1 ACTUATOR HAD TORQUE LIMITER TRIPPED. REMOVED AND REPLACED NR 1 FLAP TRACK ACTUATOR 6205CM PER AMM 27-54 2 L 7 2 4F RT A28NM 2008032800105 20080328 00105 SO 2008 3 28 RAIA00803009 1 20080311 A 2740 TRIM SYSTEM EMB 145 EMB145LR 3260212 SO STABILIZER MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 817HK 145058 FLT 5505 - JAX - PITCH TRIM FAILURE. MAINTENANCE RESET THE SYSTEM AND PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008032800108 20080328 00108 NM 2008 3 28 SWAA081523 1 20080319 A 5512 65C25727 SKIN BOEING 737 7375H4 138449D NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED C4 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 140. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008032800140 20080328 00140 2008 3 28 SWAA081566 4 20080320 A 2565 63550 SLIDE BOEING 737 7377AD 1384502 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 798SW 28436 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008030700382 20080307 00382 NM 2008 3 7 SWAA081102 1 20080227 A 3350 3071BPEGPL LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 22 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008030700386 20080307 00386 NM 2008 3 7 SWAA081114 1 20080227 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008030700387 20080307 00387 NM 2008 3 7 SWAA081113 1 20080227 A 5322 6546569 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008030700390 20080307 00390 NM 2008 3 7 SWAA081103 1 20080227 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008030700391 20080307 00391 NM 2008 3 7 SWAA081104 1 20080227 A 3350 417A5701 LENS BOEING 737 73776Q 13845AA NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 550WN 30279 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008030700392 20080307 00392 NM 2008 3 7 SWAA081115 1 20080227 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031000005 20080310 00005 SO 2008 3 10 SIMA200806301 1 20080228 A 2120 UNKNOWN EMB 135 EMB135KL 3260302 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 855AE 145747 ON FLIGHT 3616, CREW REPORTED CLIMBING THRU FL 250 NOTICED A SWEET BURNING ODOR FOR APPROX 45 SEC TO 1 MIN AND THEN IT W ENT AWAY. NO OTHER ABNORMALITIES OR EICAS MESSAGES AIRCRAFT REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK WITH APU AND PAC AIR TO FULL HOT AND FULL COLD. FOUND NO ODOR IAW EMB 140 AMM 36-00-00. OPERATIONAL CHECK GOOD. NO PARTS REMO VED, TRIAD PASSED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008031000009 20080310 00009 2008 3 10 USAA920080553 4 20080123 A 2565 TUBE BOEING 767 7672B7ER 1385107 NM RT OWING SLIDE COLLAPSED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AY 26847 MIA - EES - C4 CHECK - RIGHT OVERWING SLIDE INFLATION HOSE HAS SOFT SPOTS AND COLLAPSED IN SEVERAL AREAS. REPLACED RIGH T OVERWING SLIDE INFLATION HOSE IAW B767 AMM 25-65-00. 2 L 7 2 4F RT A1NM 2008031000011 20080310 00011 NM 2008 3 10 08FDEA00593 1 20080225 A 5340 140N2063U16 ATTACH FITTING BOEING 757 75727B 1384921 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 CORROSION FOUND ON ATTACH FITTING AT STA 1540, S-15R. CLIP REPLACED IAW B757 SRM 51-10-02 REV 93 AS PER STA ENG EAR P33 7-24137-C0016. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008031000015 20080310 00015 SO 2008 3 10 FDKA200802080 1 20080226 A 3350 SIGN EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6121 ORF-ATL (0442 PHX LCL). SEAT 12A EMERGENCY EXIT SIGN INOP. CONTRACT MX PERFORMED OPS CHECK. NO DEFECTS NOTED . 2 L 7 2 4T RT T00011AT 2008031000017 20080310 00017 NM 2008 3 10 08FDEA00660 1 20080229 A 5720 65162101 SUPPORT BEAM BOEING 727 727233 138408A NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 NR 8 SPOILER FITTING TO FALSE SPAR ATTACHMENT REPAIR CRACKED AT WS 198. REMOVED ACTUATOR FITTING IAW SRM 51-30-2. REPA IRED NR 8 SPOILER SUPPORT BEAM (SPAR) IAW DWG NR SR27-57-038 REV C. REINSTALLED SPOILER ACTUATOR FITTING IAW SRM 51-30- 2. 2 L 7 3 4F RT A3WE 2008031000020 20080310 00020 NM 2008 3 10 08FDEA00670 1 20080229 A 5320 143N51361 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 FLOOR SUPPORT BY L2 DOOR, BETWEEN STATION 680 TO 700, LBL 60, WL 208 HAS CORROSION. REMOVED CORROSION, FOUND TO BE OU T OF SRM 53-00-51, FIGURE 101, DETAIL III LIMITS, L=1.5 INCH, W= 1 INCH, D= 100 PERCENT. FABRICATED NEW SUPPORT ON MAE TRAVELER NR T7/713362, FROM 7075-0 .050C, HEAT TREATED TO T6. REMOVED AND REPLACED SUPPORT (PN: 143N5136-1) IAW SRM 51 -40-02 AND 51-40-05. THIS IS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP ACTION REQUIRED. 2 L 7 2 4F RT A2NM 2008031000024 20080310 00024 NM 2008 3 10 CALA0800179 1 20080227 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM CABIN FAILED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 76064 29459 EMERGENCY BATTERY DID NOT TEST AFTER REPLACEMENT AT MULTIPLE STA. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGERS . 2 L 7 2 4F RT A1NM 2008031000026 20080310 00026 NM 2008 3 10 KCSA081126 1 20080228 A 5347 SEAT TRACK BOEING 747 747209B 138489B NM COCKPIT CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 CAPTAINS FWD O/B SEAT TRACK CRACKED .25 INCH AT STOP. 2 L 7 4 4F RT A20WE 2008031000028 20080310 00028 NM 2008 3 10 KCSA081128 1 20080228 A 5420 STIFFENER BOEING 747 747209B 138489B NM NR 2 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 NR 2 PYLON INTERNAL O/B STIFFENER CRACKED .5 INCH AT ATTACH ANGLE NAC STA-130. 2 L 7 4 4F RT A20WE 2008031000029 20080310 00029 NM 2008 3 10 KCSA081129 1 20080228 A 5320 FITTING BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 AFT BILGE FWD STOP FITTING IS CORRODED AT STA-1484 LBL-47. 2 L 7 4 4F RT A20WE 2008031000032 20080310 00032 NM 2008 3 10 CALA0800181 1 20080204 A 5310 6520723U54 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 FOUND CRACK ON FORWARD CARGO AFT BOTTOM DOOR STOP. REMOVED AND INSTALLED NEW FRAME AT STA 492.4 PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008030700003 20080307 00003 NM 2008 3 7 USAA920080504 1 20080222 A 5230 SKIN BOEING 737 7374B7 1384702 NM ZONE 800 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 445US 1826 24863 CLT - MAJOR REPAIR - C1 CHECK - AFT CARGO DOOR SKIN CRACKED. REPLACED AFT CARGO COMPARTMENT DOOR IAW USAIRWAYS TASK CAR DS 03C21952004 AND 03C21952008. 2 L 7 2 4F RT A16WE 2008030700017 20080307 00017 NM 2008 3 7 USAA920080514 1 20080202 A 5320 141N51911 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 202UW 27811 BFM - MAJOR REPAIR - CORROSION ON CABIN FLOOR SUPPORT, BS 365 - BS 395, BL 0, WL 208. REPLACED CABIN FLOOR SUPPORT, BS 365 - BS 395, BL 0, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008030700034 20080307 00034 NM 2008 3 7 ASAA0842674 1 20080126 A 5754 65C26601389 SKIN BOEING 737 7374Q8 138447Q NM L/E SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 LEFT WING NR 1 L/E SLAT LOWER SURFACE O/B SIDE DELAMINATED. REMOVED DAMAGE DELAMINATION UNDER 2" DIAMETER, FABRICATED R EPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008030700035 20080307 00035 NM 2008 3 7 ASAA0842677 1 20080202 A 5755 654645258 SKIN BOEING 737 7374Q8 138447Q NM NR 4 SPOILER DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 LEFT WING NR 4 SPOILER BLADE SEAL RETAINING FASTENER INSERTS HAVE AREAS OF DELAMINATION AROUND THEM ON UPPER SURFACE. P REPARED DAMAGED AREA FABRICATED FILLER AND DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 PGS 212 214 254 REPAIR 4. 2 L 7 2 4F RT A16WE 2008030700045 20080307 00045 NM 2008 3 7 ASAA0842669 1 20080127 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 2 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 LEFT WING NR 2 SPOILER LOWER SURFACE SHARP DENT NEAR O/B CORNER 3" FRM EDGE. PREPARED DAMAGED AREA, FABRICATED REPAIR D OUBLER AND BONDED IAW B737 400 SRM 51 70 10 PGS 212 214 223 241 AND 254 257 REPAIR 2. 2 L 7 2 4F RT A16WE 2008030700141 20080307 00141 SO 2008 3 7 SIMA200806007 1 20080228 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 680AE 14500820 ON FLIGHT 9804, CREW REPORTED DURING PREFLIGHT DUTIES THE F/A FOUND THE FLOOR PROXIMITY LIGHTS FROM ROW 7 THRU 12 INOP. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 3 BATTERY EMERGENCY BATTERY PACK IAW AMM 33-50-11. OPERATIONA L CHECKED GOOD. ALSO, REPLACED NR 5 INVERTER IAW AMM 30-50-11. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE . 2 L 7 2 4T RT T00011AT 2008030700143 20080307 00143 SO 2008 3 7 SIMA200806005 1 20080221 A 5310 BEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 679AE 9357 5000 14500814 DURING AN IMBV INSP, THE CENTER HAT BEAM WAS FOUND TO BE CORRODED ON THE LEFT SIDE. REPAIR, REMOVED CENTER BEAM GUSSET, MADE A CUTOUT TO REMOVE THE CORROSION. FABRICATED A DOUBLER USING AL2024T3, TH-.040. CLEANED AND TREATED REPAIR PART . REPAIR DONE IAW AEA ETA-EM-53MR-030 AND EMBRAER SRM (SRM145/1142 REV. 39) CHAPTER 51-40-02. 2 L 7 2 4T RT T00011AT 2008030700160 20080307 00160 SO 2008 3 7 CHQA200800044 1 20080226 A 3610 B-NUT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BLEED SYSTEM LOOSE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 257JQ 145812 CAE311677 LGA TO GSP - AFTER TAKEOFF WHILE CLIMBING IN ICING CONDITIONS, THE CREW RECEIVED AN ENGINE NR 1 BLEED OVERHEAT AND ENGIN E ANTI-ICE FAIL MESSAGE ON EICAS. THE CREW EXITED THE ICING CONDITIONS AND RETURNED TO LGA. MAINTENANCE OPENED THE AIR CRAFT AND INSPECTED FOR BLEED LEAKS, AND FOUND A B-NUT ON THE E1 BLEED VALVE LOOSE AND LEAKING. THE B-NUT WAS TIGHTENED AND THE BLEED SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008030700164 20080307 00164 SO 2008 3 7 CHQA200800041 1 20080225 A 3610 23073461125 CLAMP EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CUSTOMER AIR MISSING A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 571RP 145827 CAE312629 CVG TO GSP - DURING CLIMB-OUT THE CREW RECEIVED AN E1 EXCEEDANCE MESSAGE ON EICAS. THE ITT REACHED 901 FOR 25 SECONDS. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. EMINENCE PERFORMED A GVI OF THE ENGINE AND FOUND THE CUSTO MER MANIFOLD DUCTING V-BAND CLAMP MISSING. THE GASKET AND CLAMP WERE REPLACED, THE ENGINE WAS RUN AT HIGH POWER AND ALL PARAMETERS WERE WITHIN LIMITS. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008030700174 20080307 00174 EA 2008 3 7 SWIA200819267 1 20080225 A 2611 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA LAV SMOKE ILLUMINATED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 932SW 7714 RECEIVED SMOKE TOILET CAUTION MESSAGE AFTER TAKEOFF, FLIGHT NR 6689. INVESTIGATED LAV FIRE SUPRESSION BOTTLE IN TRASH C OMPARTMENT IAW CRJ 200 AMM 26-26-01. NO EVIDENCE OF ANY FIRE. SYSTEM CHECKS GOOD. 2 L 7 2 4F RT A21EA 2008030700176 20080307 00176 EA 2008 3 7 SWIA200819268 1 20080225 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 437SW 7564 FRONT PORTION OF EMERGENCY LIGHTING FAILS TO ILLUMINATE, FLIGHT NR 3946. REPLACED FLOOR TRACK LIGHTING STRIP. 2 L 7 2 4F RT A21EA 2008030700190 20080307 00190 EU 2008 3 7 TRAX200800320 1 20080225 A 5720 BRACKET AEROSP ATR72 ATR72212 8680945 EU LT WING BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 ON LT WING, AT RIB 8, OMEGA BRACKET WITH TEFLON PROTECTION FOUND BROKEN ON I/B SIDE OF FLAP BEAM. 2 H 7 2 4T RT A53EU 2008030700211 20080307 00211 NM 2008 3 7 2008UALA01011 1 20080223 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 WALL EEL INOP: DOOR 5L CROSS AISLE. SECURED LOOSE CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700215 20080307 00215 EA 2008 3 7 TRAX200800333 1 20080226 A 5553 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA STAB TO FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 LHS VERTICAL STAB-TO-FUSELAGE DRAG ANGLE CRACKED AT AFT END. REPAIRS PERFORMED IAW REO 670-55-31-018, REO 670-55-31-031 , AND REO 670-55-31-031A 2 L 7 2 4F RT A21EA 2008032800141 20080328 00141 2008 3 28 SWAA081580 4 20080324 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 290WN 36632 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008032800154 20080328 00154 SO 2008 3 28 C2XA08SH050 1 20080326 A 5751 14569009409 BRACKET EMB 145 EMB145XR 3260214 SO AILERON GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 21129 145703 SHV - DURING C-CHECK IT WAS FOUND THAT THE LT PCA BRACKET ON THE AILERON WAS GOUGED. MAINTENANCE REMOVED AND REPLACED T HE AFFECTED BRACKET IAW CONTINENTAL EXPRESS EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008032800187 20080328 00187 NM 2008 3 28 SWAA081633 1 20080325 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, STR 27L TO STR 27R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008032800188 20080328 00188 NM 2008 3 28 SWAA081599 1 20080325 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008032800207 20080328 00207 EA 2008 3 28 A6WA200840119 1 20080223 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 574-621 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 430AW 7719 FS 574 TO 621 WL 73.50 RBL 9 FLOOR SUPPORT IS CORRODED. CORROSION REMOVED IAW SRM 51-21-06. (M) 2 L 7 2 4F RT A21EA 2008033100013 20080331 00013 NM 2008 3 31 QXEA200800303 1 20080313 A 5320 ANGLE BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX -C4- ANGLE CORRODED ON FWD SIDE OF WEB AND ATTACHED TO SKIN SURFACE AT STA X6.7 STR 24P (UNDER LAYSHAFT). DRILLED O UT RIVETS SECURING ANGLE TO AIRFRAME AND REMOVED ANGLE. FABRICATED NEW ANGLE FROM 7075T6 .050 ALUMINUM, DRILLED AND INS TALLED NEW BRACKETS IAW DHC-8 400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 2008033100014 20080331 00014 NM 2008 3 31 SWAA081654 1 20080326 A 5523 65C25798 HINGE BOEING 737 7373H4 1384600 NM L ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED C2 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE ASSY PER SWA EA. 2 L 7 2 4F RT A16WE 2008030700031 20080307 00031 NM 2008 3 7 2008UALA01021 1 20080223 A 5320 STIFFENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NLG WW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 LEFT VERTICAL STIFFENER CHORD, NLG WW, STA 287 HAS 3" CRACK, INDICATION LOCATED 10.75" FROM THE NOSE WW TOP PANEL. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030700041 20080307 00041 NM 2008 3 7 ASAA0842665 1 20080127 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 3 SPOILER DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 LEFT WING NR 3 SPOILER LOWER SURFACE CREASED O/B OF ACTUATOR. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BOND ED IAW B737 400 SRM 51 70 10 PGS 212 214 223 241 AND 254 257 REPAIR 2. 2 L 7 2 4F RT A16WE 2008030700048 20080307 00048 NM 2008 3 7 SB08009 1 20080224 A 3397 WIRE BOEING 737 7374B7 1384702 NM EMERGENCY LIGHTS BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 441US 24812 DFW - MAINTENANCE REPORTED THE LOWER EMERGENCY PATH LIGHTING AT SEAT 17, LEFT SIDE, INOPERATIVE. MAINTENANCE REPAIRED W IRING BENEATH SEAT 17L. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008030700063 20080307 00063 EA 2008 3 7 COMA0860144 1 20080224 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 589CA 7072 FLIGHT 5146 - RECEIVED PAX DOOR OUTER HANDLE MESSAGE. PERFORMED QRH, MESSAGE DID NOT CLEAR. RETURNED TO JAX WITHOUT IN CIDENT. PERFORMED OPERATIONAL CHECK OF PAX DOOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008030700083 20080307 00083 NM 2008 3 7 UPS08551721 1 20080222 A 3350 SWITCH BOEING 757 75724APF 1384969 NM COCKPIT LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 418UP 23905 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS SWITCH LOOSE IN PANEL. TIGHTENED SWITCH JAM NUT. 2 L 7 2 4F RT A2NM 2008030700103 20080307 00103 NM 2008 3 7 UPS08M51722 1 20080227 A 2120 UNKNOWN DOUG MD11 MD11F 3023600 NM COCKPIT ODOR A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 258UP 48416 INSPECTION TYPE:N/A A STRONG FOUL ODOR NOTICED IN COCKPIT ON CLIMB. LAV SERVICED, PACKS 1, 2, 3 OPERATED INDIVIDUALLY F OR 30 MINUTES EACH WITH NO ODOR NOTED ON GROUND. A/C OK FOR SERVICE. 2 L 7 3 4F RT A22WE 2008030700135 20080307 00135 NM 2008 3 7 2008UALA00910 1 20080217 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHT INOP: CEILING 23A. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700138 20080307 00138 NM 2008 3 7 2008UALA00911 1 20080217 A 3350 276005 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BLOWN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHTS INOP: LT OVERWING 2 FWD MOST ASSYS. REPLACED FUSE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700226 20080307 00226 EA 2008 3 7 TRAX200800338 1 20080227 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 839AS 7284 FLAPS FAIL AT ZERO DEGREE'S, FLT 4709 CX, FLT 4472 DEL 19 MINS. 2 L 7 2 4F RT A21EA 2008030700256 20080307 00256 NM 2008 3 7 USAA920080497 1 20080213 A 5320 65548624 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED INTERCOSTAL, BS 1034 - BS 1038, LBL 10 - LBL 24, WL 210. REPLACED INTERCOSTAL, BS 1034 - BS 1038, LBL 10 - LBL 24, WL 210 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008030700269 20080307 00269 NM 2008 3 7 USAA920080524 1 20080212 A 5312 651758245 BULKHEAD BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED WEB, BS 178, RBL 17.1, WL 220. REPAIRED WEB, BS 178, RBL 17.1, WL 220 IAW B737 SRM 53-10-08-2R12. 2 L 7 2 4F RT A16WE 2008030700291 20080307 00291 EU 2008 3 7 08FDEA00654 1 20080229 A 5347 A53612518200 SEAT TRACK AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND CORROSION ON SEAT TRACK C15A-19, Y-953. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008030700306 20080307 00306 NM 2008 3 7 2008UALA01045 1 20080227 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 LEFT OVERWING EMERGENCY EXIT LIGHTS INOP, 4 EACH. FOUND WIRE SHORTED TO CASE. REPAIRED WIRE REF SWPM 20-10-13. REPLAC ED BULBS & FUSES, OP CHECK OK REF MM 33-51-03. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700319 20080307 00319 NM 2008 3 7 DHL2008752550 1 20080204 A 5754 STRUCTURE BOEING 727 727223 1384074 NM NR 5 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 RT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/ B BULK SEAL IAW B727 SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR A T L/E SLAT MATERIAL USED 2024T3 .063 PO NR 9006288 DIMENSION 7 INCHES BY 8.5 INCHES IAW B727 SRM 57-30-4 FIG 11 AND B727 SRM 57-30-2 FIG3. TREATED AND PRIMED DOUBLER REPAIR AND AREA IAW B727 SRM 51-10-2. INSTALLED NEW DOUBLER REPAIR AND R EINSTALLED FASTENERS IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008030700336 20080307 00336 NM 2008 3 7 2008UALA01057 1 20080227 A 2710 AILERON BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE WING BINDING A UALA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 WP 29 673UA 29241 AILERONS BINDING WHEN ROLLING TO THE LEFT. BINDING IS NOT SEVERE BUT CAN BE FELT, ABOUT EVERY THIRD TRY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030700341 20080307 00341 EA 2008 3 7 MALA080031 1 20080225 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ODOR A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 8944B 7944 SMOKE "TOILET" WENT OFF AFTER TAKEOFF. FA SMELLED SOMETHING BURNING IN THE LAV AREA AND REPORTED A LIGHT HAZE IN THE CA BIN. FLIGHT RETURNED TO MSP. COMPLETED MM409 NR 273156 REPLACEMENT OF LAV LIGHTING BALLAST AND LAV SMOKE DETECTOR. AL SO NOTED R PACK HAS STRONG OIL SMELL. REF LOG NR 1709548 FOR FERRY FLIGHT TO T/S R PACK. 2 L 7 2 4F RT A21EA 2008030700372 20080307 00372 NM 2008 3 7 SWAA081090 1 20080227 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 733E AND BS 731E, STR 25L AND STR 22L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008040100117 20080401 00117 NM 2008 4 1 SA08018 1 20080322 A 2560 P2070001214 FLASHLIGHT AIRBUS A319 A319132 3930340 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 813AW 1223 PHX - THE FORWARD FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT. 2 L 7 2 4F RT A28NM 2008040100124 20080401 00124 NM 2008 4 1 USAA920080686 1 20080311 A 5311 65458076 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C-18 CHECK - R1 DOOR CUTOUT FORWARD UPPER STUB FRAME CRACKED, BS 294, S7R, WL 276. REPLACED R1 DO OR CUTOUT FORWARD UPPER STUB FRAME CRACKED, BS 294, S7R, WL 276 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008040100131 20080401 00131 WP 2008 4 1 08FDEA01168 1 20080328 A 5320 AKC72523 STANCHION DOUG MD10 MD1010F 3022112 WP ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 TAIL CONE LEFT PATIO DOOR HOLD OPEN STANCHION IS WORN FROM FRETTING. REPLACED TUBE ASSEMBLY IAW AMM 52-46-02-2. 2 L 7 3 4F RT A22WE 2008040100142 20080401 00142 NM 2008 4 1 ASAA0842723 1 20080304 A 5754 65C26602312A SKIN BOEING 737 737490 1384715 NM L/E SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 NR 5 SLAT INBD AND OUTBD END DELAMINATED NR 5 SLAT DELAMINATIONS. REPAIRED IAW B737 400 SRM CH 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 2008040100160 20080401 00160 EA 2008 4 1 TRAX200800394 1 20080309 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 917EV 7769 LEFT AND RIGHT SIDE CLIPS ARE CRACKED ON THE AFT SIDE OF THE PRESSURE BULKHEAD FS 625.3. DRILLED UP LEFT AND RIGHT CLIP S AND INSTALLED PER CRJ 200 SRM 51-42-20. SUPPLEMENTAL SDR CLOSED 3/19/08. 2 L 7 2 4F RT A21EA 2008040100175 20080401 00175 NM 2008 4 1 MWEA080046 1 20080324 A 5320 59107845 FLANGE BOEING 717 717200 1383700 NM LT MLG WW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 905ME 55169 LEFT MAIN LANDING GEAR WHEEL WELL FORWARD JAMB IS CRACKED ON INNER FLANGE NEAR DOOR PROX SENSOR. STOP DRILLED CRACK AND REPAIRED FLANGE. 2 L 7 2 4F TR A6WE 2008030700140 20080307 00140 NM 2008 3 7 2008UALA00913 1 20080218 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 DOOR 4R, DOOR MOUNTED EMERGENCY EVACUATION LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700144 20080307 00144 NM 2008 3 7 2008UALA00923 1 20080218 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 FWD EEL INOP, SEAT 5J. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700148 20080307 00148 SO 2008 3 7 SIMA200806003 1 20080219 A 5320 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 679AE 9357 5000 14500814 DURING MBV INSP, THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REPAIR, PERFORMED A CUT OUT ON LEFT OMEGA BEAM. PRE PARED EXTERNAL ANGLE, FILLER AND TWO SHIMS. PARTS CLEANED AND TREATED AND INSTALLED IN AIRCRAFT. REPAIR DONE IAW EMBRA ER 145 SRM (SRM EMB-145/1142 REV 39) CHAPTER 53-00-10 FIG 201. 2 L 7 2 4T RT T00011AT 2008030700165 20080307 00165 SW 2008 3 7 WGEA200800038 1 20080226 A 2710 271058201002 BELLCRANK ECLIPS EA500 ECLIPSEEA500 3350000 SW AILERONS BINDING E WGEA O OTHER F S FLT CONT AFFECTED AFFECT SYSTEMS CR CRUISE 1 EA 27 139DJ 112 000054 AILERONS STIFF, A/P HAS DIFFICULTY RESPONDING TO FD COMMANDS ALSO. INSTALLED A NEW LEFT AILERON BELLCRANK IAW EA500 AMM 27-11-17. INSTALLED A NEW LEFT AILERON JOINT ASSEMBLY IAW EA500 AMM 27-11-18. C/W FLIGHT CONTROLS ADJUSTMENT/TEST (FU NCTIONAL CHECK) IAW EA500 AMM 27-00-00-071-801-B. 1 L 7 2 4J RT A00002AC 2008030700170 20080307 00170 EA 2008 3 7 SWIA200819265 1 20080225 A 5220 ROD END CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 LEFT EMERGENCY EXIT ACTUATING HANDLE AT PIN ROD ENDS ARE CORRODED. REPLACED CLEVIS PINS IAW 52-21-02. 2 L 7 2 4F RT A21EA 2008030700180 20080307 00180 NM 2008 3 7 2008UALA00967 1 20080220 A 2721 251N300110 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER TRIM FAULTY A UALA O OTHER W F INADEQUATE Q C FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 564UA 26666 RUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. CREW COMMENTS: RUDDER TRIM INTERMITTENT. RUDDER TRIM ACTUATOR FAILURE , TRANSMITTER ISSUE. REPLACED RUDDER TRIM ACTUATOR, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030700186 20080307 00186 NM 2008 3 7 2008UALA00980 1 20080221 A 3350 767 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 546UA 25367 AFT CARGO DOOR EXTERIOR EMERGENCY LIGHT INOP. LAMP INOP. RELAMPED EMERGENCY LIGHT, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030700187 20080307 00187 EA 2008 3 7 TRAX200800316 1 20080225 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 EMERGENCY FLOOD LIGHT CEILING ROW 8 INOP, CABIN EMERGENCY LIGHTS, CEILING LEVEL FLOODLIGHTS. 2 L 7 2 4F RT A21EA 2008030700192 20080307 00192 NM 2008 3 7 2008UALA00986 1 20080221 A 3350 8100133801 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN MISSING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 206UA 30212 SEAT 2E, AFT EMERGENCY LIGHT IS MISSING. REPLACED LIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008030700194 20080307 00194 NM 2008 3 7 2008UALA00987 1 20080221 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 206UA 30212 SEAT 3E EMERGENCY LIGHTS ARE INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008030700195 20080307 00195 EA 2008 3 7 TRAX200800325 1 20080226 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 CEILING EMERGENCY LIGHT 2ND FROM FRONT INOP. 2 L 7 2 4F RT A21EA 2008030700196 20080307 00196 EA 2008 3 7 TRAX200800326 1 20080226 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 879AS 7600 LT FORWARD MOST EXTERNAL EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008030700199 20080307 00199 EU 2008 3 7 2008UALA00991 1 20080223 A 3350 CIRCUIT BREAKER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN OUT OF TOLERANCE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 427UA 512 EXT LOAD EMERGENCY LEFT, AND INTERNAL LOAD EMERGENCY LEFT MESSAGE ON EMERGENCY LIGHT TEST. RESET EMERGENCY LIGHT CIRCUI T BREAKER, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030700200 20080307 00200 NM 2008 3 7 USAA920080526 1 20080228 A 3397 GROUND STUD BOEING 737 7373G7 1384595 NM EMERGENCY LIGHTS BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 309AW 24711 PHX - EEL - FLT NR 640 - MX REPORTED LEFT EXTERIOR EMERGENCY LIGHT INOP. MX REPLACED THE BROKEN GROUNDING LUG IN AFT BA G PIT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2008030700205 20080307 00205 NM 2008 3 7 2008UALA00998 1 20080223 A 3350 68671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 116UA 26908 EMERGENCY EXIT PATH LIGHTS DISCONNECTED AT 5A. REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040100192 20080401 00192 EA 2008 4 1 TRAX200800467 1 20080324 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 906EV 7642 FLAPS FAIL EICAS APPEARED WHEN SELECTING FLAPS 8 DEGREES ON APPROACH. LANDED FLAPS 0 DEGREES. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2008040100202 20080401 00202 NM 2008 4 1 SWAA081670 1 20080327 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008040100269 20080401 00269 NM 2008 4 1 SWAA081616 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040100291 20080401 00291 NM 2008 4 1 SWAA081710 1 20080330 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040100301 20080401 00301 NM 2008 4 1 SWAA081713 1 20080330 A 5753 6546435277 FLAP BOEING 737 7373A4 1384585 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED MV2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP P ER MM. 2 L 7 2 4F RT A16WE 2008040200001 20080402 00001 NM 2008 4 2 SWAA081518 1 20080319 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 287WN 32537 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 5 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008040200008 20080402 00008 NM 2008 4 2 CALA0800247 1 20080321 A 5313 65617775 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 STRINGER 16L U-CHANNEL CRACKED AT STA 360. REMOVED AND REPLACED U-CHANNEL PER ECRA 5311-01400. 2 L 7 2 4F RT A16WE 2008040200010 20080402 00010 NM 2008 4 2 DU4R2008191 1 20080119 A 5330 SKIN BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE BS 661-666 CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 289MT 22467 S/O 304002 N/R NR26444 CORROSION FWD CARGO BILGE AREA BS 660 S-28L - S-28R. REPAIRED BY CUTTING OUT CORRODED AREA BS 66 1 TO BS 664.5, NDT VERIFIED NO CRACKS IAW NPTM PT. 6 51-00-00 FIG. 23. FABRICATED AND INSTALLED REPAIR DOUBLER 11.6 INCH X 16.25 INCH FROM 2024-T3 .071 INCH MATERIAL IAW SRM 53-30-3 FIG. 1. 2 L 7 3 4F 4 F A3WE E2EA 2008040200045 20080402 00045 NM 2008 4 2 CALA0800255 1 20080322 A 5320 141A5310U31 SILL BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 38257 30612 R-1 SERVICE DOOR SILL CORD CORRODED. REMOVED AND REPLACED R-1 SILL CORD PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008040200049 20080402 00049 EA 2008 4 2 TRAX200800439 1 20080319 A 5346 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 RIGHT UPPER ANGLE CRACKED ON ENGINE BEAM AT RBL 45 WL 119.12. REMOVED CRACKED RT UPPER ANGLE ON ENGINE BEAM. LOCATED NEW SERVICEABLE ANGLE PN 601-35006-62 IAW SRM 51-40-11. OK TO INSTALL INSTALLED ANGLE IAW SRM 51-42-21. OK TO TOPCOAT FASTE NERS. APPLIED FINISH TO FASTNERS IAW SRM 51-21-16. 2 L 7 2 4F RT A21EA 2008040200053 20080402 00053 NM 2008 4 2 SWAA081536 1 20080320 A 3350 1619 LIGHT BOEING 737 7373Y0 1384671 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008040200055 20080402 00055 NM 2008 4 2 ASAA0842736 1 20080303 A 5315 654681163 FLOORBEAM BOEING 737 737490 1384715 NM BS 986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 AFT ENTRY AREA RT FLOORBEAM AT STA 986 RBL 43.5 WL 207.5 DOUBLER STRAP, UNDER FWD FLOORBEAM CAP CORRODED. PREVIOUS REPA IR REPAIRED IAW EA 5320 01832. 2 L 7 2 4F RT A16WE 2008040200066 20080402 00066 NM 2008 4 2 ASAA0842727 1 20080303 A 5320 69434961 CHANNEL BOEING 737 737490 1384715 NM BS 867-887 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 AFT CARGO PIT BS 867 TO BS 887 RBL 21 SHIELD IS CORRODED. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008040200073 20080402 00073 2008 4 2 ASAA0852754 4 20080323 A 2310 8220987004 COUPLER BOEING 737 737890 1384527 NM NR 2 HF SYSTEM FAULTY A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 570AS 35185 UNABLE TO TUNE OR TRANSMIT ON NR 2 HF. REPLACED NR 2 HF COUPLER. GROUND VERIFICATION TEST PASSED. 2 L 7 2 4F RT A16WE 2008040200080 20080402 00080 NM 2008 4 2 SWAA081600 1 20080323 A 5753 6546431279 FLAP BOEING 737 7373H4 1384600 NM LT WING BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 LEFT WING FOREFLAP MECHANISM PROTRUDING UNDER WING. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2008040200103 20080402 00103 NM 2008 4 2 USAA920080706 1 20080320 A 5755 65737309 PANEL BOEING 737 7373B7 1384580 NM LT WING SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 23380 CLT - MAJOR REPAIR - C4 CHECK - LEFT WING SPOILER PANEL NR 0 UPPER SURFACE HAS DELAMINATION. REPLACED LEFT WING SPOILER PANEL NR 0 IAW B737 AMM 27-62-91. 2 L 7 2 4F RT A16WE 2008040200107 20080402 00107 EU 2008 4 2 USAA920080709 1 20080313 A 5530 D5537123500600 HINGE FITTING AIRBUS 320 A320231 3930325 EU ZONE 300 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 621AW 53 SAL - MAJOR REPAIR - C6 CHECK - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 3, VERTICAL STABILIZER STATION 2279/RIB 5. RE PLACED RUDDER HINGE FITTING NR 3, VERTICAL STABILIZER STATION 2279/RIB 5 IAW A320 AM 55-36-41. 2 L 7 2 4F RT A28NM 2008040200115 20080402 00115 NM 2008 4 2 2008UALA01619 1 20080321 A 3150 WARNING MESSAGE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE BATTERY CHARGER ILLUMINATED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 664UA 29236 MAIN BATTERY CHARGER STATUS MESSAGE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040200116 20080402 00116 NM 2008 4 2 2008UALA01620 1 20080322 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 558UA 26654 DOOR 1R EMERGENCY LIGHT INOP. SUPPLEMENTAL DATA UPDATE CAUSE, FOUND BROKEN WIRE AT LIGHT L30. REPAIRED WIRE AT L30 AND REPLACED POWER SUPPLY M730. OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200124 20080402 00124 NM 2008 4 2 2008UALA01630 1 20080323 A 2730 3945128102 CONTROL UNIT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ELAC 1 FAULTY A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 817UA 873 ELEVATOR SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. CAUSE, ELAC1 FAULTY, ISSUES WITH CPS BOARD (INTERNAL). REPLACED E LAC1, ALL TEST PASS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200125 20080402 00125 2008 4 2 2008UALA01631 4 20080323 A 2565 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L1 DOOR SLIDE NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 805UA 783 3SV EEL LIGHT FAP TEST FAILED EPSU EXT LOAD FWD L. CAUSE, ELECTRICAL SHORT IN SLIDE NR 1 LT MED SLIDE. REPLACED SLIDE NR 1 LT MED. OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200126 20080402 00126 NM 2008 4 2 2008UALA01632 1 20080324 A 3397 362624 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT EEL LIGHT INOP, AT SEAT 36 RIGHT. FOUND LOOSE CONNECTION. SECURED LOOSE CONNECTOR. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200128 20080402 00128 NM 2008 4 2 CALA0800265 1 20080306 A 5320 6943477 ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 AFT CARGO TOP & BOTTOM SURFACES OF FLOOR SUPPORT TRANSITION ANGLE AT STA 767 TO 787, RBL 22 ARE CORRODED. REMOVED AND R EPLACED TRANSITION ANGLE P/N 69-43477U2 & INSTALLED NEW NUT PLATES IAW B737 SRM 51-40-02, STA 767-787 RBL 22 IAW B737-30 0 SRM 51-40-02 SL776. 2 L 7 2 4F RT A16WE 2008040200141 20080402 00141 NM 2008 4 2 2008UALA01638 1 20080323 A 5320 CHANNEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 348 S15L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 DURING HMV4 INSPECTION, DAMAGE WAS FOUND AT BS 348 CHANNEL AT STR S-15L. MAJOR REPAIR: REMOVED DAMAGED COMPONENTS. OBTA INED/FABRICATED AND INSTALLED REPLACEMENT PARTS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200143 20080402 00143 NM 2008 4 2 2008UALA01639 1 20080323 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 DURING HMV INSPECTION, FOUND DAMAGE AT BS 294 WEB AT STR S-12L. MAJOR REPAIR: REMOVED DAMAGE COMPONENTS. OBTAINED/FABRI CATED AND INSTALLED REPLACEMENT PARTS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200148 20080402 00148 EA 2008 4 2 TRAX200800459 1 20080321 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 836AS 7263 LEFT AFT MOST EXTERNAL EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008040200151 20080402 00151 EA 2008 4 2 TRAX200800465 1 20080323 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA RIGHT MALFUNCTIONED A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 917EV 7769 RIGHT PACK UNCONTROLLABLE, CAUSING SMOKE (AIR CONDITIONING PACK - RT SIDE). 2 L 7 2 4F RT A21EA 2008040200155 20080402 00155 NM 2008 4 2 2008UALA01650 1 20080323 A 3500 OXYGEN SYSTEM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 211UA 30217 OXYGEN SYSTEM NEEDS SERVICING. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040200158 20080402 00158 NM 2008 4 2 2008UALA01653 1 20080322 A 3510 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CAPTAIN'S MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 574UA 26686 CAPT'S RESET-TEST LEVER ON O2 MASK DOOR IS INOP. SUPPLEMENTAL DATA UPDATE CAUSE, MASK NOT STOWED PROPERLY. REINSTALLED MASK ASSY IN POSITION. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200159 20080402 00159 NM 2008 4 2 2008UALA01654 1 20080322 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 661UA 27158 EMERGENCY EXIT LIGHTS FLASH ON AND OFF IN COACH AISLE LEFT SIDE ONLY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030700206 20080307 00206 NM 2008 3 7 2008UALA00999 1 20080223 A 3350 276005 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY EXIT LIGHTS INOP: RT OVERWING 2 FWD ASSY. REPLACED FUSE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700207 20080307 00207 NM 2008 3 7 2008UALA01005 1 20080222 A 3350 1317 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 677UA 30029 EEL LIGHT ON END OF SEAT 21H MISSING. REPLACED LIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030700208 20080307 00208 NM 2008 3 7 2008UALA01007 1 20080222 A 3350 D71702001 POWER SUPPLY BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 216UA 30549 DOOR 2R EMERGENCY SLIDE LIGHT INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008030700216 20080307 00216 NM 2008 3 7 2008UALA01015 1 20080224 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 SEAT 49ABC EMERGENCY LIGHT IS INOP. SECURED LOOSE CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700220 20080307 00220 EU 2008 3 7 TRAX200800335 1 20080226 A 5220 BEAM AEROSP ATR72 ATR72212 8680945 EU EMERGENCY DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 LT EMERGENCY DOOR, AFT AND FWD ANGLE ON BOTTOM OF BEAM FOUND CRACKED, TO BE FABRICATED. 2 H 7 2 4T RT A53EU 2008030700223 20080307 00223 EA 2008 3 7 TRAX200800337 1 20080226 A 5755 PANEL CNDAIR CL600 CL6002C10 1390015 EA SPOILER CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 RT MULTIFUNCTION SPOILER CLOSEOUT PANEL CRACKED AT INBD AFT CORNER. REPAIRED SHROUD IAW EO 700-57-065, REO 670-57-51-15 3A AND 51-75-18. 2 L 7 2 4F RT A21EA 2008030700227 20080307 00227 EA 2008 3 7 TRAX200800339 1 20080227 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA ILLUMINATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 974EV 7594 STALL FAIL CAUTION MESSAGE APPEARED AFTER TAKEOFF AND REMAINED ON FOR ENTIRE FLIGHT, EN ROUTE TO ATL A/C DIVERTED TO CVG DUE TO MTC. THE TOWER DECLARED AN EMERGENCY AND ROLLED EMERGENCY VEHICLES AS A PRECAUTION, FLT 4451 DEL 245 MINS. 2 L 7 2 4F RT A21EA 2008030700230 20080307 00230 EA 2008 3 7 TRAX200800341 1 20080227 A 3350 COVER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 EMERGENCY LIGHT COVER (FLOOR) BROKE OFF AROUND ROW 5. 2 L 7 2 4F RT A21EA 2008030700233 20080307 00233 EU 2008 3 7 TRAX200800344 1 20080227 A 5720 ANGLE AEROSP ATR72 ATR72212 8680945 EU LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 LT SPLICE ANGLE ON WING PRESSURE AT FR 27 STR 4 CRACKED. 2 H 7 2 4T RT A53EU 2008030700234 20080307 00234 NM 2008 3 7 USAA920080442 1 20080208 A 5315 65528941 FLOORBEAM BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED CABIN FLOOR SUPPORT CRACKED, BS 540, LBL 2.5. REPLACED CABIN FLOOR SUPPORT, BS 540, LBL 2.5 IAW B737 SRM 51-40-04. 2 L 7 2 4F RT A16WE 2008030700235 20080307 00235 NM 2008 3 7 USAA920080443 1 20080208 A 5340 66244912 ATTACH FITTING BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - CRACKED R1 DOOR CUTOUT INTERCOSTAL ATTACH CLIP, BS 332.1, S8R. REPLACED R1 DOOR CUTOUT INTERCOSTAL ATTACH CLIP, BS 332.1, S8R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008030700236 20080307 00236 NM 2008 3 7 USAA920080445 1 20080212 A 5320 6545834 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CORROSION ON INTERCOSTAL, BS 312 BS 328, S12R. REPLACED INTERCOSTAL, BS 312 BS 328, S1 2R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008030700237 20080307 00237 NM 2008 3 7 USAA920080470 1 20080217 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER TIE CLIP, BS 440, S9R. REPLACED STRINGER TIE CLIP, BS 440, S9R IAW B7 37 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008030700238 20080307 00238 NM 2008 3 7 USAA920080471 1 20080210 A 5755 SKIN BOEING 737 7373G7 1384595 NM NR 5 SPOILER DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW MA3225 24009 MCN - MAJOR REPAIR - C18 CHECK - RIGHT WING NR 5 SPOILER UPPER SURFACE HAS AREA OF DISBOND, WS 123 - WS 128. REPAIRED R IGHT WING NR 5 SPOILER UPPER SURFACE, WS 123 - WS 128 IAW B737 SRM 51-70-02. 2 L 7 2 4F RT A16WE 2008030700239 20080307 00239 NM 2008 3 7 USAA920080472 1 20080210 A 5340 69389396 STRINGER CLIP BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - CRACKED STRINGER TIE CLIP, BS 344, S10R. REPLACED STRINGER TIE CLIP, BS 344, S10R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008030700243 20080307 00243 NM 2008 3 7 USAA920080478 1 20080215 A 5320 140N250538 INTERCOSTAL BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 901AW 23321 MCN - MAJOR REPAIR - CRACKED INTERCOSTAL, BS 661, RBL 48, WL 207. REPLACED INTERCOSTAL, BS 661, RBL 48, WL 207 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008030700252 20080307 00252 NM 2008 3 7 USAA920080493 1 20080221 A 5320 WEB BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 CLT - MAJOR REPAIR - C17 CHECK - CRACKED WEB, BS 500D, BL0. REPLACED WEB, BS 500D, BL0 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008030700261 20080307 00261 NM 2008 3 7 2008UALA01027 1 20080223 A 3350 20121 POWER SUPPLY BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 202UA 24717 EMERGENCY PATH LIGHTS INOP AFT OF ROW 15. REPLACED POWER SUPPLY BATTERY. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700265 20080307 00265 NM 2008 3 7 2008UALA01031 1 20080225 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 INTERCOSTAL IS CRACKED AT BS 291.5 JUST BELOW STR 9R. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700272 20080307 00272 NM 2008 3 7 USAA920080527 1 20080213 A 5320 65C334191 WEB BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED SHEAR WEB, BS 1023 - BS 1040, BL 0 - LBL 38, WL 208. REPLACED SHEAR WEB, BS 10 23 - BS 1040, BL 0 - LBL 38, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008030700273 20080307 00273 NM 2008 3 7 USAA920080528 1 20080208 A 5311 6546541504 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 663.75, S3L - S3R. REPAIRED FRAME, BS 663.75, S3L - S3R IAW B737 SRM 53-00-07-2R9. 2 L 7 2 4F RT A16WE 2008030700274 20080307 00274 NM 2008 3 7 USAA920080529 1 20080211 A 5312 651758353 BULKHEAD BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED BULKHEAD CHORD, BS 178, LBL 5.7, WL 184. REPAIRED BULKHEAD CHORD, BS 178, LBL 5.7, WL 184 IAW B737 SRM 53-10-03-2R5. 2 L 7 2 4F RT A16WE 2008030700276 20080307 00276 NM 2008 3 7 USAA920080530 1 20080209 A 5755 SKIN BOEING 737 7373G7 1384595 NM NR 4 DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW MA3211 24009 MCN - MAJOR REPAIR - C18 CHECK - LEFT WING NR 4 SPOILER HAS AREA DEBONDED, WBL 169.05 - WBL 180.75. REPAIRED LEFT WING NR 4 SPOILER, WBL 169.05 - WBL 180.75 IAW B737 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2008030700277 20080307 00277 NM 2008 3 7 USAA920080531 1 20080218 A 5420 311N504017 STIFFENER BOEING 757 7572S7 1384962 NM ZONE 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 901AW 23321 MCN - MAJOR REPAIR - C12 CHECK - CRACKED STIFFENER ON NR 1 PYLON STRUT, PYLON STATION 153.90. REPLACED STIFFENER ON NR 1 PYLON STRUT, PYLON STATION 153.90 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008030700281 20080307 00281 NM 2008 3 7 08FDEA00472 1 20080218 A 5320 146N5447U15 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD STRINGER L16.10, STA 1460-1480, TO EVALUATE EXISTING REPAIR. EXISTING REP AIR FOUND NOT IAW B757 SRM 51-70-11 FIG 1 DETAIL I, II. STRINGER L16.10 FROM STA 1460 TO STA 1480 REPLACED IAW B757 SRM 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008030700286 20080307 00286 NM 2008 3 7 08FDEA00480 1 20080218 A 5320 146N541614 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOOR BOARD STRINGER R7.55, STA 1260-1280. TO EVALUATE EXISTING REPAIR. EXISTING RE PAIR FOUND NOT IAW B757 SRM 51-70-11 FIG 1 DETAIL I, II STRINGER R7.55. REPLACED IAW B757 SRM 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008030700288 20080307 00288 NM 2008 3 7 08FDEA00594 1 20080225 A 5340 140N2063U16 ATTACH FITTING BOEING 757 75727B 1384921 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 CORROSION FOUND ON CLIP AT STA 1520, S-15R. CLIP REPLACED IAW B757 SRM 51-10-02 REV 93 AND STA ENG EAR NR P337-24137-C 0012. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008032600186 20080326 00186 NM 2008 3 26 QXEA200800290 1 20080313 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 409QX 4051 PDX-C4 - FRAME CASTELLATION ON FRAME X136.0 BETWEEN STRINGERS 27P AND 28P HAS SUSPECT CORROSION AROUND RIVET TAILS. REM OVED RIVETS(3) IAW DASH 8 Q400 SRM 51-42-05. REMOVED CORROSION IAW Q400 SRM 51-21-00. HFEC INSPECTED BLENDED AREA FOR CRACK IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECK IAW Q400 NDTM PART 1, 51-00-04, HIGH .040" LO W .038". ALL WITHIN LIMITS IAW Q400 SRM 51-14-00, ALODINED AREA IAW Q400 SRM 51-21-10, PAINTED AREA IAW Q400 SRM 51-21- 15. INSTALLED 3 RIVETS IAW Q400 SRM CHAPTER 51-42-05. 2 H 7 2 4T RT A13NM 2008030600255 20080306 00255 NE 2008 3 6 VNAA0802009 2 20080212 A 7230 6018T30P14 BLADES CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 2 ENGINE DAMAGED A VNAA O OTHER C F.O.D. AP APPROACH 1 GL 05 256PS 7937 CREW REPORTED A BIRD STRIKE TO THE RIGHT HAND ENGINE ON APPROACH. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE ENGI NE AND FOUND REMAINS AND DAMAGE TO SEVERAL BLADES. MAINTENANCE REMOVED AND REPLACED DAMAGED BLADES IN ACCORDANCE WITH T HE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE ALSO BORESCOPED THE ENGINE, COMPLETED POWER ASSURANCE AND VIBE CHECKS. ALL OPS CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008030600264 20080306 00264 NM 2008 3 6 SWAA081067 1 20080226 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER M M. 2 L 7 2 4F RT A16WE 2008040200160 20080402 00160 NM 2008 4 2 2008UALA01655 1 20080322 A 2611 CIRCUIT CARD BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FIRE DETECTION FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 787UA 26939 FIRE CARD APU FIRE DETECTION CARD FAULT OR FAILURE OR LOSS OF ARINC 629-429 COMMUNICATION WITH CARD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040200168 20080402 00168 EA 2008 4 2 TRAX200800476 1 20080326 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 859AS 7421 LEFT AND RIGHT SIDE CLIPS ARE CRACKED ON THE AFT SIDE OF THE PRESSURE BULKHEAD FS 625. COMPLIED WITH EC REO 670-55-31-0 32. 2 L 7 2 4F RT A21EA 2008040200172 20080402 00172 NM 2008 4 2 2008UALA01664 1 20080325 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 34 LH INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 FOUND EMERGENCY LIGHT ROW 34 LT INOP. RESECURED EMERGENCY LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200174 20080402 00174 NM 2008 4 2 2008UALA01665 1 20080325 A 3397 362624 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 116UA 26908 FOUND EMERGENCY LIGHT ROW 43 LT INOP. FOUND LOOSE CONNECTION. SECURED EMERGENCY LIGHT CONNECTOR. OP CK NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200177 20080402 00177 NM 2008 4 2 2008UALA01667 1 20080324 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1400 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 AFT PIT FS 1400 FRAME DENTED STR 26L. CAUSE, UNKNOWN. AFT PIT FS 1400 FRAME DENTED STR 26L. REMOVED DAMAGED SECTION O F FRAME INBOARD FLANGE. FABRICATED -5 'J' DOUBLER AND STRINGER CLIPS AND INSTALLED PER REPAIR 5. THIS IS A CAT B REPAI R IN ZONE 2 AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS TO BEGIN 25,000C AFTER REPAIR INSTALLATION, AND REPETIT IVE INSPECTIONS EVERY 11,000C THEREAFTER. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200181 20080402 00181 NM 2008 4 2 2008UALA01672 1 20080324 A 2622 EXTINGUISHER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LAVATORY FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 209UA 30215 TRASH CAN EXTINGUISHER AT LAV 4R DISCHARGED WITH NO SIGN OF FIRE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040200184 20080402 00184 NM 2008 4 2 2008UALA01674 1 20080324 A 3510 OXYGEN BOTTLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AFT READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 AFT O2 BOTTLE LOW PRESSURE. REPLACED BOTTLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200186 20080402 00186 NM 2008 4 2 2008UALA01675 1 20080324 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT OVERWING INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 651UA 25389 EMERGENCY FLOOR LIGHTS BY RIGHT OVERWING INOPERATIVE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040200188 20080402 00188 NM 2008 4 2 CALA0800278 1 20080317 A 5320 6545833435 SUPPORT ANGLE BOEING 737 7373T0 1384582 NM NLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 UPPER SUPPORT ANGLE FOR NOSE WHEEL WELL VIEWING WINDOW HAS A CRACK AT FWD LT CORNERS. REMOVED AND REPLACED DAMAGED CHAN NEL IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008040200189 20080402 00189 NM 2008 4 2 2008UALA01677 1 20080325 A 3510 CYLINDER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW OXYGEN UNDERSERVICED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 806UA 788 OXYGEN CYLINDER CREW NEED SERVICE. SUPPLEMENTAL DATA UPDATE CAUSE, UNKNOWN. SERVICED CREW O2, NO LEAKS WERE NOTED AT T IME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200194 20080402 00194 NM 2008 4 2 CALA0800280 1 20080324 A 5330 6545800 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INITIATE A DIP ON RT FUSELAGE BETWEEN STA 340 & 360 AND BETWEEN S-20 RT AND S-21 RT HAS CREASE JUST ABOVE SHEET METAL RE PAIR. COMPLETED REPAIR INSTALLATION PER CAL EC/RA 5331-01260. 2 L 7 2 4F RT A16WE 2008040200195 20080402 00195 EU 2008 4 2 2008UALA01681 1 20080325 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 419UA 487 CREW O2 LOW. SUPPLEMENTAL DATA UPDATE CAUSE, UNKNOWN. SERVICED CREW O2, NO LEAKS WERE NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200202 20080402 00202 NM 2008 4 2 2008UALA01686 1 20080323 A 3510 OXYGEN SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 568UA 26674 CREW O2 READING 1200 (LOW). CAUSE, UNKNOWN. SERVICED CREW O2 TO FULL, NO LEAKS NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200203 20080402 00203 NM 2008 4 2 2008UALA01687 1 20080325 A 3510 MXP147 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 1ST OFFICER'S NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 581UA 26701 F/O OXYGEN MASK WILL NOT TEST. CAUSE, UNKNOWN. REPLACED STOW BOX ASSY, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200212 20080402 00212 2008 4 2 2008UALA01694 4 20080325 A 2565 HOUSING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT OWING SLIDE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 LT OVERWING SLIDE COMPARTMENT DOOR DISCONNECT HOUSING CRACKED AT WELD SEAM. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040100102 20080401 00102 NM 2008 4 1 USAA920080679 1 20080321 A 5230 6547952340X SKIN BOEING 737 7374B7 1384702 NM AFT CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 459UW 42303 1457 25023 CLT - MAJOR REPAIR - AFT CARGO DOOR SKIN IS CRACKED AT THE HANDLE CUT OUT. REPLACED AFT CARGO COMPARTMENT DOOR IAW USAI RWAYS TASK CARD 03L21952008. 2 L 7 2 4F RT A16WE 2008040100123 20080401 00123 NM 2008 4 1 BB08041 1 20080322 A 2560 P2070001214 FLASHLIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 202UW 27811 MCO - THE FLASHLIGHT NEAR THE L2 DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT. 2 L 7 2 4F RT A2NM 2008040100132 20080401 00132 NM 2008 4 1 ASAA0842729 1 20080303 A 5311 654654997 FRAME BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 FOUND CORROSION ON FRAME IN AFT CARGO PIT AT BS 767 STR 26R TO STR 27R. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008040100133 20080401 00133 NM 2008 4 1 ASAA0842730 1 20080303 A 5311 6546548194 FRAME BOEING 737 737490 1384715 NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 DRILL MARKS ON FRAME IN CARGO PIT AT BS 747 RBL3 TO LBL3, REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008040100136 20080401 00136 NM 2008 4 1 ASAA0842731 1 20080303 A 5320 69353501 FITTING BOEING 737 737490 1384715 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 TIE CLIP FWD SIDE OF BS 787 OUTBD OF THE RT TIE DOWN TRACK RBL 13.80 CORRODED. AFT CARGO PIT REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008040100138 20080401 00138 NM 2008 4 1 ASAA0842716 1 20080309 A 5512 657378354 SKIN BOEING 737 737490 1384715 NM HORIZ STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 ON PRE FLIGHT, FOUND NICKEL SIZE ON HORIZONTAL STAB RT SIDE LEADING EDGE DENT AT HORIZ STAB L/E SKIN AT STAB STA 102. R EPAIRED IAW B737 400 SRM 55 10 01 REPAIR 2. 2 L 7 2 4F RT A16WE 2008040100179 20080401 00179 WP 2008 4 1 UPS08851927 1 20080228 A 5347 36575041 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 F/E AND OBSERVERS SEAT TRACK HAS ELONGATED HOLES AND BARE METAL. REMOVED AND REPLACED SEAT TRACK. 2 L 7 4 4F RT 4A25 2008040100205 20080401 00205 NM 2008 4 1 ASAA0892772 1 20080307 A 5320 143A7501113 FLOOR SUPPORT BOEING 737 737990 NM BS 500C-500D DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 323AS 30021 FWD CARGO BAY FLOOR SUPPORT TRACK BETWEEN STA 500C AND STA 500D RBL 5" TWO HOLES DRILLED THROUGH AT EDGE OF FLOOR SUPPOR T. REMOVED DAMAGED SECTION OF FLOOR SUPPORT TRACK LOCATED DRILLED AND INSTALLED REPAIR ANGLES IAW SRM 53-00-53 PG 203 F IG 201. 2 L 7 4 4F RT A16WE 2008040100208 20080401 00208 NM 2008 4 1 ASAA0892773 1 20080307 A 5320 146A750342 FLOOR SUPPORT BOEING 737 737990 NM BS 772-775 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 323AS 30021 AFT CARGO COMPT FLOOR SUPPORT CORRODED AROUND NUTPLATES AT STA 772 RBL 3. CUT OUT DAMAGED AREA OF FLOOR SUPPORT UPPER C AP ONLY. FABRICATED LOCATED DRILLED AND INSTALLED REF SRM 53-40-05 & 53-40-06 AND ASA EA 5310 02778. 2 L 7 4 4F RT A16WE 2008040100209 20080401 00209 NM 2008 4 1 SWAA081684 1 20080327 A 5330 65C381921 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 508D, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008040100210 20080401 00210 NM 2008 4 1 SWAA081683 1 20080327 A 5330 65C381921 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 512D, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008040100214 20080401 00214 NM 2008 4 1 ASAA0892775 1 20080307 A 5320 146A750611 FLOOR SUPPORT BOEING 737 737990 NM BS 727I CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 323AS 30021 AFT CARGO PIT FLOOR SUPPORT CORRODED AT STA SPLICE 727 I LBL 8.1. REMOVED DAMAGED SPLICE, FABRICATED SPLICE CHANNEL IAW DRWG 146A7506 FIG 2. LOCATED DRILLED AND INSTALLED IAW B737 900 SRM 51 40 2 PG 6 ASA EA 5310 02779. 2 L 7 4 4F RT A16WE 2008040100222 20080401 00222 NE 2008 4 1 ASAA0852762 2 20080325 A 7200 ENGINE BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE LEFT OIL CONSUMPTION A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 585AS 35683 LEFT ENGINE OIL CONSUMPTION SEEMS EXCESSIVE ESPECIALLY FOR AN ETOPS AIRCRAFT. CURRENT OIL CONSUMPTION FOR NR 1 ENGINE I S 0.25 QTS HR. WELL WITHIN LIMITS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040100226 20080401 00226 NE 2008 4 1 ASAA0852763 2 20080325 A 7200 ENGINE BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE RIGHT OIL CONSUMPTION A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 585AS 35683 RIGHT ENGINE OIL CONSUMPTION SEEMS HIGH ESPECIALLY FOR AN ETOPS AIRCRAFT. CURRENT OIL CONSUMPTION FOR NR 2 ENGINE IS 0. 17 QTS HOUR. WELL WITHIN LIMITS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008030600310 20080306 00310 WP 2008 3 6 ABXA080059 1 20080206 A 5310 99115055 WINDOW FRAME DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DURING WINDOW FRAME MOD TO COCKPIT STRUCTURE, FOUND LEFT SIDE FRAME CRACKED LESS THAN 2.50 INCHES. REPAIRED IAW DC9 SRM 53-05, FIG 34 PER WO 600283624. 2 L 7 2 4F A6WE 2008030700050 20080307 00050 NM 2008 3 7 ASAA0842675 1 20080127 A 5753 6546430130 SKIN BOEING 737 7374Q8 138447Q NM FOREFLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 RIGHT I/B FOREFLAP HAS MULTIPLE DENTS ON LOWER SURFACE 32" FRM I/B AND 34" FRM O/B SIDES. PREPARED DAMAGED AREA, FABRIC ATED FILLERS AND DOUBLERS AND BONDED IAW B737 400 SRM 51 70 10 PGS 212 241 214 AND 254. 2 L 7 2 4F RT A16WE 2008030700057 20080307 00057 NM 2008 3 7 GTIA0800031 1 20080109 A 5310 STRUCTURE AIRBUS A321 A321231 3940032 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 585NK 1438 Y-1292 FRAME 18-24 HAS CORROSION BEYOND LIMITS. REPAIRED DAMAGED AREA 18-24 Y1292 IAW SRM 51-00-14. 2 L 7 2 4F RT A28NM 2008030700084 20080307 00084 NM 2008 3 7 HALA0800357 1 20080228 A 5711 SPAR BOEING 767 7673G5 1385126 NM LWS 825 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 LEVEL 1 CORROSION AROUND 2 FASTENERS AT LT WING STA 825, ON TOP SURFACE, ON FRONT SPAR. REPAIRED PER SRM 57-20-01. 2 L 7 2 4F RT A1NM 2008030700089 20080307 00089 NM 2008 3 7 NWAA080643141 1 20080219 A 5320 SILL AIRBUS A319 A319114 3930350 NM FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 341NB 1738 DURING "H" CHECK, FOUND CORROSION ON AFT RT DOOR SILL PLATE FORWARD UPPER ATTACHMENT FLANGE AT FRAME 66. REPAIRED PER E A 31-211685. 2 L 7 2 4F RT A28NM 2008030700121 20080307 00121 NM 2008 3 7 2008UALA00900 1 20080216 A 3350 9F19948501 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 642UA 25092 EXTERIOR EMERGENCY LIGHT JUST AFT OF LEFT WING INOP. REPLACED LAMP, OP CHECKS OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030700123 20080307 00123 NM 2008 3 7 2008UALA00902 1 20080217 A 3397 7945243 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 647UA 25284 THE 13B SEAT EMERGENCY LIGHT INOP. SECURED UNDER SEAT CONNECTOR. LIGHT OP CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030700142 20080307 00142 NM 2008 3 7 2008UALA00922 1 20080218 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 LEFT OVERWING FWD EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY EXIT LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700161 20080307 00161 SO 2008 3 7 CHQA200800043 1 20080225 A 3610 14504743411 DUCT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 BLEED CRACKED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 288SK 145461 CAE312717 IAH TO STL - THE CREW RECEIVED A BLEED 1 LEAK MESSAGE DURING CLIMB AND RETURNED TO FIELD AT IAH. MAINTENANCE SECURED TH E BLEED 1 SYSTEM CLOSED AND DEFERRED THE NR 1 BLEED SYSTEM. ON THE 26TH MAINTENANCE TROUBLESHOT THE BLEED SYSTEM AND FO UND A LEAK COMING FROM THE LEFT UPPER T-DUCT IN THE CARGO COMPARTMENT. MAINTENANCE REPLACED THE T-DUCT AND THERE WERE N O FURTHER BLEED LEAKS NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008030700178 20080307 00178 EA 2008 3 7 SWIA200819270 1 20080223 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 913SW 7597 FLT 6657 - FIRST OFFICERS SIDE WINDOW SHATTERED IN FLIGHT. REPLACED RIGHT SIDE WINDOW IAW CRJ 200 MM 56-12-01, PN NP139 322-12, SN OFF 03010H4039. 2 L 7 2 4F RT A21EA 2008030700189 20080307 00189 EU 2008 3 7 TRAX200800318 1 20080225 A 3350 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN MAKING METAL A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 EMERGENCY PAX DOOR LIGHT INOP. EMERGENCY PAX DOOR LIGHT REPLACED AND TESTED IAW 33-50-00. FOUND SERVICEABLE. 2 H 7 2 4T RT A53EU 2008030700198 20080307 00198 EA 2008 3 7 TRAX200800327 1 20080226 A 5242 HANDLE CNDAIR CL600 CL6002C10 1390015 EA E/E BAY DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 MAIN AVIONICS BAY DOOR HANDLE CRACKED AT BASE. REMOVED AND REPLACED MAIN AVIONICS BAY DOOR HANDLE IAW AMM 51-42-03 AND SRM 51-42-06 SG7020421 2 L 7 2 4F RT A21EA 2008030700219 20080307 00219 NM 2008 3 7 2008UALA01017 1 20080224 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 SEAT 1A FWD EMERGENCY LIGHT IS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700222 20080307 00222 EA 2008 3 7 TRAX200800336 1 20080226 A 5755 PANEL CNDAIR CL600 CL6002C10 1390015 EA SPOILER CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 LT MULTIFUNCTION SPOILER CLOSEOUT PANEL CRACKED AT INBD AFT CORNER. REPAIRED SHROUD IAW EO 700-57-065, REO 670-57-51-15 3A AND 51-75-18. 2 L 7 2 4F RT A21EA 2008030700240 20080307 00240 NM 2008 3 7 USAA920080473 1 20080209 A 5320 69366564 INTERCOSTAL BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - CRACKED INTERCOSTAL ANGLE, BS 927 - BS 947, BL 0, WL 208. REPLACED INTERCOSTAL ANGLE, BS 927 - BS 947, BL 0, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008030700246 20080307 00246 NM 2008 3 7 USAA920080481 1 20080216 A 5320 143N581215 GUSSET BOEING 757 7572S7 1384962 NM INTERCOSTAL CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 901AW 23321 MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL GUSSET, BS 845, S22R. REPLACED INTERCOSTAL GUSSET, BS 845, S22R IA W B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008030700260 20080307 00260 NM 2008 3 7 USAA920080518 1 20080225 A 5230 FITTING BOEING 737 73733A 1384673 NM ZONE 800 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 168AW 23629 PHX - MAJOR REPAIR - FORWARD CARGO DOOR LOWER FORWARD CORNER FITTING CRACKED. REPLACED FORWARD CARGO DOOR LOWER FORWARD CORNER FITTING IAW USAIRWAYS EO 52-31-04. 2 L 7 2 4F RT A16WE 2008030700262 20080307 00262 NM 2008 3 7 USAA920080519 1 20080218 A 5754 SKIN BOEING 767 7672B7ER 1385107 NM NR 6 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AY 26847 MIA - MAJOR REPAIR - C4 CHECK - LEFT WING NR 6 SLAT LOWER FORWARD EDGE SKIN CRACKED. REPAIRED LEFT WING NR 6 SLAT LOWER FORWARD EDGE SKIN IAW B767 SRM 51-70-03. 2 L 7 2 4F RT A1NM 2008030700266 20080307 00266 NM 2008 3 7 USAA920080521 1 20080217 A 5310 DOOR FRAME BOEING 737 7374B7 1384702 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 455UW 24997 PIT - MAJOR REPAIR - FPBH - FORWARD CARGO DOOR CUTOUT AFT FRAME CRACKED, BS 492.4, S24R. REPAIRED FORWARD CARGO DOOR CU TOUT AFT FRAME, BS 492.4, S24R IAW USAIRWAYS EA 110692. 2 L 7 2 4F RT A16WE 2008030700284 20080307 00284 NM 2008 3 7 08FDEA00477 1 20080218 A 5320 146N5447U14 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD STRINGER R2.90, STA 1460-1480. TO EVALUATE EXISTING REPAIR. EXISTING REP AIR FOUND NOT IAW B757 SRM 51-70-11 FIG 1 DETAIL I, II, STRINGER R.290 FROM STA 1460 TO STA 1480 REPLACED IAW B757 SRM 5 1-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008030700296 20080307 00296 EU 2008 3 7 08FDEA00664 1 20080229 A 5415 A54612172 ATTACH ANGLE AIRBUS 310 A310324 3930206 EU CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 PYLON NR 1 LEFT SIDE, FWD ATTACH ANGLE FOR PANEL 413 CL IS CRACKED. REMOVED AND REPLACED BRACKET PER A310-300 SRM 51-40 -21, PG 7. 2 L 7 2 4F RT A35EU 2008030700298 20080307 00298 NM 2008 3 7 08FDEA00666 1 20080229 A 5320 65585021 SUPPORT BOEING 727 727227 1384078 NM CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 PANEL "T" SUPPORT BRACKET HAS CORROSION, BETWEEN LEFT AND RIGHT RAM AIR FIBERGLASS DUCTS, BETWEEN STA 720E AND 720F, L EFT SIDE. REMOVED PANELS FOR ACCESS, REMOVED "T" SUPPORT, REMOVED CORROSION, NDT FOR MATERIAL LOSS ORIG .058'", REMAIN ING .053' INCH, WITHIN LIMITS. TREAT AND PRIMED AND PAINTED "T" SUPPORT. INSTALL "T" SUPPORT AND PANELS REMOVED. REF SRM 53-10-1, 51-102, 51-30-2, MM51-20-151-7 51-10-6, THIS IS CLASSIFIED AS A MINOR REPAIR LEVEL 1 CORROSION. 2 L 7 3 4F A3WE 2008030700299 20080307 00299 NM 2008 3 7 08FDEA00667 1 20080229 A 5320 652956711 ANGLE BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 MAIN DECK FLOOR DITCH PAN ASSY FWD AND AFT CHORD ANGLES ARE CRACKED BS 1177 - 1883, LBL 47 -64, WL 208. REPLACED FWD A ND AFT CHORD ANGLES IAW DWG 65-29548. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008030700304 20080307 00304 EU 2008 3 7 2008UALA01043 1 20080227 A 2560 256302008 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 458UA 1163 DOOR 1L FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY DEAD. BATTERY FAILURE. REPLACED BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030700307 20080307 00307 NM 2008 3 7 2008UALA01046 1 20080227 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EEL INOP, SEAT 2A FWD, SEAT 4J AFT. RELAMPED EMERGENCY LIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700309 20080307 00309 NM 2008 3 7 2008UALA01048 1 20080226 A 2611 SMOKE DETECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LAVATORY NONE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 LAV 5L 106 SMOKE ALARM INOP. OP CHECKED SMOKE ALARM PER MM 26-13-00-501. ALARM INDICATES NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700311 20080307 00311 NM 2008 3 7 2008UALA01050 1 20080226 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 AFT PIT FRAME GOUGED NUMEROUS PLACES AT BS 1520 BETWEEN STR 22R THRU STR 24R. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030700312 20080307 00312 NM 2008 3 7 2008UALA01051 1 20080226 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 595UA 28748 SEAT 16A EMERGENCY EXIT LIGHT BURNT OUT. LAMP BURNT OUT. RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030700314 20080307 00314 NM 2008 3 7 QXEA200800232 1 20080226 A 5210 HANDLE BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR OUT OF RIG A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 418QX 4143 LAX - FLIGHT 2304 - DURING CLIMB RECEIVED A FUSELAGE DOOR WARNING. F/A CAN'T CONFIRM THAT THE RIGHT AFT SERVICE DOOR IS CLOSED. NO LOSS OF PRESSURIZATION. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. FERRIED AIRCRAFT TO PDX FOR REPAIRS. IN PDX FOUND HANDLE OUT OF RIG NOT ALLOWING A FLUSH FIT. RIGGED DOOR. OPERATIONAL CHECKS GOOD. AIRC RAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008030700316 20080307 00316 2008 3 7 135818022608 4 20080225 A 2300 RADIO CESSNA 402 402C 207590R CE MALFUNCTIONED E HYIA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 61 818AN 402C0501 THIS IS A PRELIMINARY REPORT WITH A FINAL REPORT TO FOLLOW. ON APPROACH TO MVY, AIRCRAFT WAS UNABLE TO TRANSMIT ON EITH ER COMM 1 OR COMM 2 RADIO WITH PILOTS PTT OR MICROPHONE, ACCOMPANIED BY A SMALL WISP OF SMOKE. THE PILOT PERFORMED THE APPROPRIATE BOX MEMORY ITEMS AND NO MORE SMOKE WAS SEEN. THE PILOT THEN RESTORED POWER FOR GEAR AND FLAPS WITH NO ADDIT IONAL SMOKE DETECTED. PILOT CONTACTED TOWER USING CELL PHONE AND WAS ABLE TO LAND WITHOUT INCIDENT. MAINTENANCE WAS DI SPATCHED TO MVY AND INSPECTED AIRCRAFT. AIRCRAFT WAS FLOWN ON A SPECIAL FLIGHT PERMIT TO MAINTENANCE BASE AT HYA. THE SFP WAS PERFORMED IN VFR CONDITIONS USING HAND HELD COMM RADIOS. MAINTENANCE CURRENTLY STILL TROUBLESHOOTING THE DISCRE 1 L 7 2 3O A7CE 2008030700322 20080307 00322 NM 2008 3 7 DHL2008752603 1 20080208 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1130 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 AFT PIT STA1130 HAS DENT IN RADIUS OF FRAME AT S-26L. CUTOUT DAMAGED AREA AT AFT CARGO COMP STA 1130 STR 26L DIMENSION 3/4" BY 1/2" IAW B727 SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR MATERIAL USED 7075-O .071 PO NR 9006377 DIMENSION 9 IN CH BY 4 INCHES IAW B727 SRM 51-40-3 FIG 1 AND IAW B727 SRM 53-10-2 FIG 5. HEAT TREAT PART 7075-O TO 7075T6 IAW B727 FLI GHTSTAR AIRCRAFT SERVICES ENGINEERING REPORT NR 2-37153-801 REVA TREATED AND PRIMED PART AND AREA IAW B727 SRM 51-10-2. INSTALLED REPAIR IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008030700324 20080307 00324 NM 2008 3 7 DHL2008752609 1 20080226 A 7160 SKIN BOEING 727 727223 1384074 NM NOSE COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 NR 3 NOSE COWL O/B T/E SKIN CRACKED ABOVE COWL LATCH. INSTALLED REPAIR IAW B727 SRM 54-30-2 FIG 1. 2 L 7 3 4F A3WE 2008030700325 20080307 00325 NM 2008 3 7 GTIA0800035 1 20080223 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 522NK 2893 FOUND SIGNS OF CORROSION ON BEAM Y765 BETWEEN FR67 AND FR70. REMOVED AND REPLACED BEAM AT Y765 BETWEEN FR67 AND FR70 IA W SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008030700327 20080307 00327 NM 2008 3 7 NWAA070766309 1 20080221 A 5313 STRINGER BOEING 747 747451 1384940 NM BS 480 S10L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING "M" CHECK, FOUND CRACKS IN STRINGER 10R AND STRINGER 10L AT BS 480. REPAIRED PER EA 63-212201. 2 L 7 4 4F RT A20WE 2008030700330 20080307 00330 NE 2008 3 7 DL76S080297 2 20080229 A 7520 ELBOW BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 1 ENGINE CRACKED A DALA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 27 126DL 53153 580327 24076 580327 L ENG FIRE LP1 STATUS MESSAGE ABOUT 15 MINUTES INTO FLIGHT FOLLOWED BY ILLUMINATION OF L ENGINE FIRE WARNING LIGHTS. EN GINE SHUTDOWN IN ACCORDANCE WITH QRH. NOTE, FIRE SWITCH WAS PULLED, HOWEVER, FIRE BOTTLE WERE NOT DISCHARGED. FOUND NR 1 ENG LT HIGH PRESSURE RECOUP LINE ELBOW CRACKED WITH HOLE IN IT. REMOVED AND REPLACED ELBOW REF IPC 75-23-01-10 ITEM 475. RESET FIRE HANDLE AND GEN FIELD. PERFORMED ENG RUN ON NR 1ENG. GEN CKS NORMAL. FIRE WARNING CHKS NORMAL AND EN G INDICATIONS NORMAL ON NR 1 ENG. 2 L 7 2 4F 4 F RT A1NM E13NE 2008030700335 20080307 00335 NM 2008 3 7 2008UALA01056 1 20080227 A 2730 ELEVATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RIGHT OUT OF ADJUST A UALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 29 508UA 24744 AIRCRAFT REQUIRES 4 UNITS OF RUDDER TRIM IN LEVEL FLT. CHECKED RUDDER AND RUDDER TRIM SYSTEM OK. FOUND RT ELEVATOR NOT WITHIN LIMITS ON INDEX PLATE AND E-ST9 RIG PIN HOLE NOT LINING UP. ADJUSTED, ALL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030700337 20080307 00337 NM 2008 3 7 2008UALA01058 1 20080226 A 3020 ANTI-ICE VALVE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 ENGINE DEFECTIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 217UA 30550 NR 1 ENGINE ANTI-ICE VALVE WILL NOT INDICATE PROPER POSITION. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008030700343 20080307 00343 NM 2008 3 7 2008UALA01060 1 20080227 A 5210 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD ENTRY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 FWD ENTRY DOOR INNER SKIN AFT SIDE CRACKED 4TH & 5TH DOOR STOP HOLES FROM BOTTOM OF DOOR. MAJOR REPAIR: ROUTED OUT CRAC KS. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700347 20080307 00347 NM 2008 3 7 2008UALA01061 1 20080227 A 5230 TEE FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 AFT CARGO DOOR, LWR FWD TEE CRACKED OUT OF FASTENER HOLE. MAJOR REPAIR: REPLACED TEE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700351 20080307 00351 NM 2008 3 7 2008UALA01065 1 20080227 A 5210 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD ENTRY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 FWD ENTRY DOOR FRAME CRACKED AT AFT DOOR STOP NUMBER 4 AND 5. MAJOR REPAIR: CUT OUT CRACKS. INSTALLED REPAIR ANGLES. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700355 20080307 00355 NM 2008 3 7 2008UALA01085 1 20080227 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 MAIN CABIN FLOORBEAM STA 287, RBL 70.5 UPPER FLANGE IS CORRODED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008030700371 20080307 00371 NM 2008 3 7 SWAA081089 1 20080227 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 354SW 25219 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008030700373 20080307 00373 NM 2008 3 7 SWAA081091 1 20080227 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008030700374 20080307 00374 NM 2008 3 7 SWAA081092 1 20080227 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008030700375 20080307 00375 2008 3 7 SWAA081093 4 20080227 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED C3 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008030700376 20080307 00376 2008 3 7 SWAA081094 4 20080227 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED C3 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008030700384 20080307 00384 NM 2008 3 7 SWAA081100 1 20080227 A 3350 MS155721 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008030700388 20080307 00388 NM 2008 3 7 SWAA081112 1 20080227 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER 15L CRACKED AT BS 380. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008030700393 20080307 00393 NM 2008 3 7 SWAA081116 1 20080227 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008030700397 20080307 00397 NM 2008 3 7 SWAA081118 1 20080227 A 5322 6546546 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008030700399 20080307 00399 NM 2008 3 7 SWAA081107 1 20080227 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 767SW 29807 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008030700400 20080307 00400 NM 2008 3 7 SWAA081108 1 20080227 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED HC2 CHECK, RT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008031000001 20080310 00001 SO 2008 3 10 FDKA200802072 1 20080219 A 7830 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO THRUST REVERSER MALFUNCTIONED A FDKA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 856MJ 145626 FDM 6192 BOS (1805 PHX LCL). ABORTED TAKEOFF DUE TO ENGINE NR 1 REVERSER DISAGREE MESSAGE. MX TROUBLESHOT AND OPS CHEC KED GOOD. 2 L 7 2 4T RT T00011AT 2008031000002 20080310 00002 SO 2008 3 10 FDKA200802075 1 20080221 A 2120 FDS765A2 DUCT EMB 145 EMB145LR 3260212 SO CABIN UNKNOWN A FDKA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 07 837MJ 145367 FDM 6061 ATL-SYR (1154 PHX LCL). LAV SMOKE WARNING AND SMELL OF SMOKE. MX REMOVED AND REPLACED DISTRIBUTION DUCT. 2 L 7 2 4T RT T00011AT 2008031000003 20080310 00003 EA 2008 3 10 TRAX200800357 1 20080229 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 926EV 7843 FLAPS FAILED AT 0 AFTER TAKEOFF IN ATL RETURNED FOR LANDING IN ATL, EMERGENCY DECLARED. AIRCRAFT RETURNED TO ATL AFTER T/O. 2 L 7 2 4F RT A21EA 2008031000008 20080310 00008 WP 2008 3 10 NWAA080799751 1 20080302 A 3397 WIRE DOUG DC9 DC941 302207N WP EMERGENCY LIGHTS DISCONNECTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 751NW 47115 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR ROWS 5, 6, 7, 8, 14, AND 17 WERE FOUND TO B E INOPERATIVE. MAINTENANCE FOUND A DISCONNECTED WIRE AND RE-INSERTED IN THE CONNECTOR. THE AIRCRAFT RETURNED TO SERVIC E. 2 L 7 2 4F A6WE 2008031000010 20080310 00010 EU 2008 3 10 NWAA080803225 1 20080226 A 3260 UPLOCK SENSOR AIRBUS 320 A320211 3930320 EU MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 325US 281 ON CLIMB FROM DTW THROUGH 12,000 ACCELERATING AUDIBLE GEAR DOOR NOISE WITH ASSOCIATED RIGHT MAIN LANDING GEAR RED "UNLK" LIGHT MOMENTARILY. LIGHT EXTINGUISHED AS WELL AS NOISE. REOCCURRED TWICE BUT WITH NO ASSOCIATED ECAM MESSAGE. CONTIN UED FLIGHT AT 250 KNOTS WITH INDICATIONS. AIRCRAFT LANDED UNEVENTFULLY. INSPECTED AIRCRAFT FOUND SAFE FOR FERRY FLIGHT . REPLACED RT ISOLATION SAFETY VALVE 49GA, LANDING GEAR DOOR SELECTOR VALVE, RT MLG DOOR UPLOCK PROXIMITY SENSORS 26G A ND 28GA, GND SERVICE BUS CHG OVER RELAY 53GA. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 2008031000012 20080310 00012 NM 2008 3 10 08FDEA00659 1 20080229 A 5347 BAC1520792 SEAT TRACK BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 MAIN CABIN CARGO COMPARTMENT, SEAT TRACK HAS CORROSION AT STA 950A - 1030, BL 46R. REMOVED CORROSION AND FOUND OUT OF L IMITS IAW SRM 53-10-1 FIG 3. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. FABRICATED NEW SEAT TRACK SECTION IAW SRM 53- 10-5 FIG 1. TREATED AND PRIMED SEAT TRACK IAW SRM 51-10-2. INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2 AND 53-10-5 FIG 1. 2 L 7 3 4F RT A3WE 2008031000022 20080310 00022 NM 2008 3 10 KCSA081122 1 20080227 A 5312 FITTING BOEING 747 747209B 138489B NM BULKHEAD CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 STA-2360 AFT PRESSURE BULKHEAD HOLE 158 IS CORRODED IN FITTING AT STR-46R. 2 L 7 4 4F RT A20WE 2008031000023 20080310 00023 NM 2008 3 10 KCSA081123 1 20080227 A 5312 FITTING BOEING 747 747209B 138489B NM CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 STA-2360 AFT PRESSURE BULKHEAD HOLE 159 IS CORRODED AT STR-46R. 2 L 7 4 4F RT A20WE 2008031000030 20080310 00030 NM 2008 3 10 KCSA081125 1 20080228 A 5347 SEAT TRACK BOEING 747 747209B 138489B NM COCKPIT CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 F/O FWD O/B SEAT TRACK CRACKED .25 INCH AT STOP. 2 L 7 4 4F RT A20WE 2008040100228 20080401 00228 NM 2008 4 1 ASAA0872787 1 20080311 A 5320 141A511014 INTERCOSTAL BOEING 737 737790 13844CN NM BS 1965 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 607AS 29751 CRACKED INTERCOSTAL BS 196.5 AND RBL 1.5" BELOW FLIGHT DECK DOOR. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008040100234 20080401 00234 NM 2008 4 1 ASAA0872796 1 20080314 A 5315 143A52409 FLOORBEAM BOEING 737 737790 13844CN NM BS 540 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 607AS 29751 FLOOR SUPPORT CHANNEL AT STA 540 LBL0 24.75 IS CRACKED AT INBD ATTACH POINTS FLOOR SUPPORT CHANNEL AT BS 540 LBL0 LBL24. 75. REPLACED IAW B737 700 SRM 51 40 02 AND DRWG NR 143A5240. 2 L 7 2 4F RT A16WE 2008040100238 20080401 00238 EU 2008 4 1 BA08014 1 20080328 A 2560 P04010021 BATTERY AIRBUS 330 A330323 3930335 EU FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 272AY 0333 FRA - THE LEFT AFT INBOARD FLIGHT ATTENDANT SEAT FLASHLIGHT LOCATED UNDERNEATH THE SEAT DOES NOT WORK. MAINTENANCE REPL ACED THE BATTERY OF THE LEFT AFT INBOARD FLIGHT ATTENDANT SEAT FLASHLIGHT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A46NM 2008040100280 20080401 00280 2008 4 1 SWAA081648 4 20080325 A 2565 D31591478 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, R1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED E VAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008040100293 20080401 00293 NM 2008 4 1 SWAA081726 1 20080330 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040100294 20080401 00294 NM 2008 4 1 SWAA081727 1 20080330 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040200016 20080402 00016 EA 2008 4 2 TRAX200800419 1 20080312 A 2760 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT SPOILERON CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 AAR - CORROSION ON LOWER MOUNT BOLT SAFETY BRACKET MOUNT BOLT FOR RT SPOILERON I/B PCU (I/B BRACKET). 2 L 7 2 4F RT A21EA 2008040200033 20080402 00033 NM 2008 4 2 CALA0800242 1 20080319 A 5330 141N3231 SKIN BOEING 757 757224 1384958 NM FUSELAGE BULGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14115 27557 FUSELAGE SKIN HAD BULGE WITH RIVETS PULLING AT REINFORCING DOUBLER FOR FWD LAV SERVICE PAN, STA 424-434 LBL 5 APPROX. C UT OUT DAMAGED SECTION OF SKIN AND INSTALLED REPAIR DOUBLER AND STRUCTURAL FILLER REF ECRA5331-01397 AND DIPPED TO PERFO RM A PERMANENT REPAIR PER PART 3 WITHIN 12 MONTHS. 53-DIP CONTROL NUMBER 871501. 2 L 7 2 4F RT A2NM 2008040200065 20080402 00065 EA 2008 4 2 TRAX200800449 1 20080320 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 AAR - INTERCOSTAL CLIP CRACKED AT FS 484 LBL 28. REMOVED AND REPLACED CRACKED CLIP FS 484 LBL36 IAW REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2008040200071 20080402 00071 EA 2008 4 2 TRAX200800457 1 20080319 A 5534 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 355CA 10067 SUSPECTED CRACK FWD OF FS 1181 ON LT VERTICAL BASE. COMPLIED WITH EC REO 670-55-31-032. 2 L 7 2 4F RT A21EA 2008040200083 20080402 00083 NM 2008 4 2 SWAA081625 1 20080325 A 3350 MS155721 LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008040200090 20080402 00090 NM 2008 4 2 ASAA0842755 1 20080229 A 5753 6546434369 SKIN BOEING 737 737490 1384715 NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 LEFT INBOARD T/E AFT FLAP HAS A DENT IN THE LEADING EDGE 26 INCHES OUTBOARD OF THE INBOARD EDGE. DENT REPAIRED IAW B737 400 SRM CH 57 53 01 REPAIR 4. 2 L 7 2 4F RT A16WE 2008040200104 20080402 00104 NM 2008 4 2 USAA920080707 1 20080320 A 5755 657373010 PANEL BOEING 737 7373B7 1384580 NM ZONE 600 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 23380 CLT - MAJOR REPAIR - C4 CHECK - RIGHT WING SPOILER PANEL NR 8 UPPER SURFACE HAS DELAMINATION. REPLACED RIGHT WING SPOIL ER PANEL NR 8 IAW B737 AMM 27-61-11. 2 L 7 2 4F RT A16WE 2008040200119 20080402 00119 NM 2008 4 2 CALA0800262 1 20080325 A 5340 69353523 STRINGER CLIP BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11641 28902 STRINGER TIE CLIP CRACKED STA 787 S-15R. REMOVED CRACKED TIE CLIP AT STA 787, STR 15R. LOCATED, DRILLED AND INSTALLED NEW STRINGER TIE CLIP P/N 69-35352-3 AT SAME LOCATION IAW B737-5 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008040200136 20080402 00136 NM 2008 4 2 CALA0800273 1 20080328 A 5753 65C263434 CARRIAGE BOEING 737 737524 1384721 NM T/E FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 46625 27529 NR 3 MID FLAP CARRIAGE, BOTH ARMS PITTED WITH CORROSION. REMOVED AND REPLACED WITH SERVICEABLE I/B AND O/B CARRIAGE HAL VES ON O/B SIDE OF NR 3 MID FLAP. 2 L 7 2 4F RT A16WE 2008040200144 20080402 00144 NM 2008 4 2 CALA0800275 1 20080305 A 5330 6545774 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 DENT AT STA 887 BETWEEN STR 19L + 20L DENT AREA FWD OF STA 887 IS 3.1 X 2.2 X .065 WITH A/Y RATIO OF 33.8 DENT AFT OF ST A 887 IS 7.6 X 2.6 X .057 WITH A/Y RATIO OF 45.6 B737 SRM 53-00-01 FIG 101, SHT 2 NOTE: V DOES NOT PERMIT DENTS IN ADJAC ENT BAYS. REPAIRED DENTS BS887 BETWEEN STR 19LT & 20LT PER PACE EA350-53-001 CAL REVA EC/RA5330-03789. 2 L 7 2 4F RT A16WE 2008031000031 20080310 00031 NM 2008 3 10 CALA0800180 1 20080206 A 5320 6520726 SILL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 FOUND CORROSION AT FORWARD CARGO DOOR SILL WEB. NEW WEB WAS FABRICATED AND INSTALLED. 2 L 7 2 4F RT A16WE 2008030700009 20080307 00009 NM 2008 3 7 USAA920080511 1 20080222 A 5340 STRINGER CLIP BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 589US 23934 CLT - MAJOR REPAIR - C1 CHECK - CRACKED STRINGER TIE EXTENSION, BS 360, S15R. REPLACED STRINGER TIE EXTENSION, BS 360, S15R IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008030700020 20080307 00020 EU 2008 3 7 2008UALA00952 1 20080219 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 471UA 1432 CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED CREW O2 SYSTEM TO 1900 PSI AND LEAK CHECKED. NO LEAKS NOTED AT THE TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030700022 20080307 00022 NM 2008 3 7 2008UALA00954 1 20080220 A 3260 WARNING SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT ACTIVATED A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION AP APPROACH 1 WP 29 116UA 26908 THE 'GEAR DISAGREE' EICAS CAUTION MSG DISPLAYED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700038 20080307 00038 NM 2008 3 7 ASAA0842662 1 20080127 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 0 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 LEFT WING NR 0 SPOILER LOWER SURFACE HAS A SHARP DENT 5" FROM I/B SIDE AND 15" FRM T/E. PREPARED DAMAGED AREA, FABRICAT ED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 PGS 212 214 223 241 AND 254. 2 L 7 2 4F RT A16WE 2008030700060 20080307 00060 2008 3 7 ASAA0852672 4 20080225 A 3140 2233000815 WARNING MESSAGE BOEING 737 737890 1384527 NM UNKNOWN A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 587AS 35684 WHILE PERFORMING TASKCARD 78131002 FOUND NR 4 BEARING MESSAGE FOR ENGINE NR 1 LEVEL 2. ACCOMPLISHED EA7731 01027. EA RE QUIRES MM TASK 77 31 00 970 805 F00 (AAVM DATA DOWNLOAD) WITHIN 25 FLIGHT CYCLES FROM 24FEB08. DOWNLOADED ENGINES 1, 2 NR 4 BEARING DATA AND FORWARDED TO AS POWERPLANT ENG'G MAINT CNTL & AOG ENG'G. 2 L 7 2 4F RT A16WE 2008030700075 20080307 00075 NM 2008 3 7 NOCA01508 1 20080226 A 2560 7024091001 COVER BOEING 757 75728A 1384976 NM EXIT SIGN MISSING A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 756NA NT247 R4 EMERGENCY EXIT SIGN COVER MISSING. REPLACED EXIT LIGHT ASSY AT R4 DOOR. 2 L 7 2 4F RT A2NM 2008030700105 20080307 00105 NM 2008 3 7 ASAA0852681 1 20080226 A 4990 38809381 FILTER BOEING 737 737890 1384527 NM APU CLOGGED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 577AS 35186 APU OIL FILTER DELTA P POPPED. REPLACED APU OIL FILTER. GROUND VERIFICATION ACCOMPLISHED DELTA P REMAINS IN. 2 L 7 2 4F RT A16WE 2008030700155 20080307 00155 GL 2008 3 7 SIMA200806009 2 20080224 A 7200 UNKNOWN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL ENGINE SMOKE A SIMA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 905JH 14500892 CAE312756 ON FLIGHT 4200, CREW REPORTED A ABORTED TAKEOFF AT 100 KNOTS AFTER F/O NOTICED EVIDENCE OF SMOKE IN THE COCKPIT. THE F/ A ALSO REPORTED VISIBLE SMOKE AROUND GALLEY AREA AND AFTER SHUTDOWN THE PACKS THE SMOKE WENT AWAY. THE SMOKE DID NOT HA VE A ODOR OF ELECTRICAL OR OIL ODOR LIKE. THE SMOKE ODOR LIKE BURNING PAPER AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER ONE ENGINE. OPERATIONAL CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008033100020 20080331 00020 WP 2008 3 31 08FDEA00983 1 20080317 A 5321 AGA38623 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 AFT PIT FLOOR PANEL NR 187 GF REQUIRES FABRICATION PER SRZ 25-011. FABRICATED NEW FLOOR PANEL 187 GF; POTTED EDGES; COMP LETED CURE AND SANDED EDGE POTTING. INSTALLED INSERTS; FABRICATED TOP SHEET; LAYED UP UNDER VAC BAG COMPLETED CURE; COU NTER SUNK HOLES AND NON-SKID IAW SRZ 25-005; REV F AND 25-011; REV C. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008033100098 20080331 00098 NM 2008 3 31 AMTA200800179 1 20080228 A 5730 SKIN PANEL BOEING 737 73783N 13844HI NM LT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LT WING FUEL ACCESS 531BB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVE PITTING CORROSION ON LT FUEL TANK ACCESS LANDING IAW B737-800, SRM 51-10-02-0G, ORG MAT .201, MAT LOSS .004, REM MAT .197, FOUND TO BE WITHI N LIMITS IAW SRM 578-20-01-1A, PERFORMED FLAP PEENING IAW SRM 520-06 AND SOPM 20-10-03. (K) 2 L 7 2 4F RT A16WE 2008033100107 20080331 00107 NM 2008 3 31 AMTA200800183 1 20080228 A 5315 FLOORBEAM BOEING 737 73783N 13844HI NM BS 727 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 AFT CARGO COMPARTMENT TEE ASSY CORRODED AT STA 727I. REMOVED CORROSION ON TEE ASSY, ORG MAT .078, MAT LOSS .003, REM MA T .075, IAW SRM 51-10-02, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53, ALODINED AND PRIME IAW SRM 51-20-0A. (K) 2 L 7 2 4F RT A16WE 2008033100114 20080331 00114 NM 2008 3 31 AMTA200800193 1 20080301 A 5315 FLOORBEAM BOEING 757 75723N 1384973 NM BS 1637-1382 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 520AT 27976 LIGHT CORROSION AND BARE METAL ON UPPER SURFACE OF FLOORBEAM BETWEEN BS 1637 AND BS 1682. (82561) LBL 58.82 TO RBL 58.8 2. REMOVED LIGHT CORROSION IWA SRM 51-10-02-06, PG-1. ORIG MATL THK .130 AT BS 1637 MAT LOSS .005. MATL THK AT BS 168 2 IS .090 MAT LOSS .004. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-51-1A. TREATED AND PRIMED AREA SRM 51-20-01. (K) 2 L 7 2 4F RT A2NM 2008033100124 20080331 00124 NM 2008 3 31 AMTA200800202 1 20080302 A 2130 UNKNOWN BOEING 737 73783N 13844HI NM CABIN PRESSURE UNKNOWN A AMTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 11 305TZ 30706 AC DID NOT PRESSURIZE AFTER TAKEOFF, NON NORMAL CHECKLIST NO HELP. LOUD NOISE IN FWD CABIN NEAR L1 NO DOOR LIGHTS. NO WARNING LIGHTS. PERFORMED EXCESSIVE CABIN PRESSURE LEAKAGE CK IAW AMM 05-51-91-2. AC PRESSURIZED NORMAL, NO EXCESSIVE LEAKS NOTED, PERFOMED DCPC BITE NR 1 AND NR 2, NO CURRENT FAULTS. (K) 2 L 7 2 4F RT A16WE 2008033100146 20080331 00146 CE 2008 3 31 HYT2008F00000 1 20080226 A 2820 HOSE CESSNA 207 207 2073602 CE CONT O550 IO550* SO FUEL SYS FAILED E HYTA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 91027 20700018 824041R METERED FUEL PRESSURE HOSE FAILED. THIS HOSE RUNS FROM THE FUEL INJECTOR DISTRIBUTOR TO THE FIREWALL. LOW PRESSURE TES T OF FAILED HOSE REVEALED MULTIPLE LEAKS ALONG LENGTH OF HOSE. HOSE WAS INSTALLED NEW ON 4/8/03/ HOSE FAILURE NOTED ON 2/26/08 WHEN ENGINE WOULD NOT CONTINUE TO RUN. FOLLOWING INFO ON HOSE TAG: STRATOFLEX PT/BA, 156MA001-3SO350, CD1Q02WO 8316, OP1500PSI, TSOC53A, C751/II-A-S/P, A12/12/02, OT275F. HOSE WAS PART OF HOSE KIT 2738916 DATED 12/12/02. IN RECE NT PAST SAME HOSE ON ANOTHER AIRCRAFT IN FLEET HAD SAME TYPE OF FAILURE AT APPROX 1600 HRS IN SERVICE. (K) 1 H 7 1 3O 3 O A16CE E3SO 2008033100173 20080331 00173 NM 2008 3 31 TAMF20080016S 1 20080317 A 5320 SILL BOEING 767 767200 1385120 NM FUSELAGE CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 770QT 23802 DURING C2 CHECK WAS FOUND CORROSION ON AFT CARGO DOOR SURROUND STRUCTURE MAIN SILL - INNER CHORD - RT. CORROSION WAS RE MOVED IAW SRM 51-10-02 PAGE 12-13. THICKNESS OUT OF LIMITS. TEMPORARY REPAIR WAS PERFORMED IAW EWO 767 53-076 PART I AND MFG SERVICE REQUEST 1-792508203. 2 L 7 2 4F RT A1NM 2008033100196 20080331 00196 NM 2008 3 31 AALA200800597 1 20080311 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 798AN 30797 MIA - EMERGENCY LIGHT AT SEAT 39G LAMP BROKEN. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 39G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008033100201 20080331 00201 WP 2008 3 31 NWAA081199762 1 20080321 A 5320 WEB DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 762NW 47395 DURING "M" CHECK, FOUND CRACK IN WEB AT BS 110 FROM LBL 42 TO LBL 48. REPAIRED PER EA 97-212129. 2 L 7 2 4F A6WE 2008033100218 20080331 00218 WP 2008 3 31 DHL2008805531 1 20080226 A 5712 FRAME DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 NR 4 STUB WING UPPER FORMER CRACKED 0.500" STA XFS 541.000. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED (2EA) ANGLE DOUBLER (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DO UBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLER (2EA) IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2008033100234 20080331 00234 WP 2008 3 31 DHL2008805529 1 20080225 A 5320 5651221 ANGLE DOUG DC8 DC873F 302199F WP LT MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 LT MLG W/W ANGLE CRACKED 0.500" AT STA XW -3.125. REMOVED CRACKED ANGLE IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED A REA IAW SRM 51-1-8B. INSTALLED NEW ANGLE IAW SRM 51-1-21. REFER TO JC EC-00794-001 (WO 3457) FOR ANGLE FABRICATION. 2 L 7 4 4F RT 4A25 2008033100262 20080331 00262 WP 2008 3 31 DHL2008805504 1 20080303 A 5320 STRUCTURE DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 ACCOMPLISH REPAIR AT STA 420 LONGERON 32 - 33L PER SRM TO INCLUDE FINGER DOUBLERS. PERFORMED MAJOR REPAIR IAW SRM 53-2- 1 FIG 7 SHEET 1, 4, 5. REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED R EPAIR DOUBLER (AL7075T6 0.080") FILLER (AL7075T6 0.071") AND (2EA) INTERNAL FINGER DOUBLER (AL7075T6 0.050") IAW SRM 53- 2-1 FIG 7 SHEET 1, 4, 5, SRM 53-4-1 FIG 5C ITEM "C". CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIG. 7 SHEET 1,4,5, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE). THIS IS A CLASS 1 TYPE REPAIR (INITIAL INSP: 4000 LANDING CYCLES, REPETITIVE INSP: 4.000 LANDING CYCLE. REPLACEMENT: N/ 2 L 7 4 4F RT 4A25 2008033100264 20080331 00264 WP 2008 3 31 DHL2008805522 1 20080311 A 5720 FITTING DOUG DC8 DC873F 302199F WP LT WING WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 LT WING T/E "ZEE" WORN AT STA XW -3.126. REMOVED WORN ZEE IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51 -1-8B. INSTALLED NEW ZEE IAW SRM 51-1-21. REFER TO JC EC-00796-001 (WO 3457) FOR FABRICATION. 2 L 7 4 4F RT 4A25 2008033100266 20080331 00266 NM 2008 3 31 QXEA200800309 1 20080320 A 5320 ANGLE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX -C4- SUSPECT CORROSION ON CLIP ANGLE FWD SIDE OF FRAME STA X488 CONNECTING TO STR 24P LT UNDER FLOOR. BLENDED CORRO SION ON CLIP ANGLE IAW DHC 8 CPCM CHAPTER 4. HFEC INSPECTED BLEND AREA FOR CRACKS IAW D-8 200 NDTM PART 6, 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECK OF BLENDED AREA IAW -8 200 NDTM PART 1, 51-00-04. HIGH .063 LOW .059. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW SRM 51-20-11 WITH .004" MATERIAL REMOVED. 2 H 7 2 4T RT A13NM 2008033100271 20080331 00271 NM 2008 3 31 QXEA200800325 1 20080320 A 5414 SKIN DHAV DHC8 DHC8202 2809007 NM NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX -C4- NR 1 NACELLE SKIN INBD SIDE HAS 3/4" CRACK, AFT UPPER CORNER OF PANEL 416AR APERATURE. REPAIRED DAMAGE REFERE NCING RD8-54-1193. HFEC INSPECTED AREA FOR CRACKS IAW D 8/200 NDTM, PART 6, 51-00-01, NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 2008033100274 20080331 00274 NM 2008 3 31 QXEA200800313 1 20080320 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - C4 - CORROSION ON BOTTOM SIDE OF FLOOR LEVEL SKIN AT NUT PLATE HOLE STA X597.5 AND Y22 LT (LT SIDE ANGLE AT X597.5 ). DRILLED OUT NUT PLATE AND REMOVED CORROSION IAW DHC 8/200 CPCM CHAPTER 4. HFEC INSPECTED BLENDED AREA FOR CRACKS IA W D 8/200 NDTM, PART 6, 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECK OF BLENDED AREA IAW -8/200 NDTM PART 1, 51-00-04 HIGH .040 LOW .036. AREA OF BLEND WITHIN LIMITS REF DHC 8 SRM 51-20-11. APPLIED ETCH ALODINE AND PRIMER IAW DHC 8 SRM 51-20-16 AND 51-20-36. REINSTALLED NUT PLATE REF DHC 8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008033100281 20080331 00281 NM 2008 3 31 DLM90080414 1 20080324 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 CABIN SEAT TRACK RBL 54.5 OUT OF LIMITS, FS 731. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01 VOL I. 2 L 7 2 4F RT A6WE 2008033100282 20080331 00282 NM 2008 3 31 DLM90080415 1 20080323 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 CABIN SEAT TRACK RBL 22 OUT OF LIMITS, 1210-1364. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01 VOL I. 2 L 7 2 4F RT A6WE 2008033100284 20080331 00284 NM 2008 3 31 DLM90080417 1 20080323 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 FOUND CABIN SEAT TRACK RBL 54.5 OUT OF LIMITS, 590-674. 2 L 7 2 4F RT A6WE 2008033100291 20080331 00291 NM 2008 3 31 DLM90080424 1 20080324 A 5347 9530085 SEAT TRACK DOUG MD90 MD9030 3023690 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 CABIN SEAT TRACK LBL 54.5 IS OUT OF LIMITS AT FUSELAGE STA 760-899. REMOVED AND REPLACED SEAT TRACK FS 760-899, IAW MD9 0 SRM 53-40-01 FIG 6. 2 L 7 2 4F RT A6WE 2008033100294 20080331 00294 NM 2008 3 31 DLM90080427 1 20080320 A 5320 5940441 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 LT CABIN CUSP WEB FS 568-572 CORRODED. CUTOUT DAMAGED AREA, FABRICATED REPLACEMENT WEB DOUBLER AND INSTALLED, IAW MD90 SRM 53-05D, FIG 827D. 2 L 7 2 4F RT A6WE 2008033100300 20080331 00300 EU 2008 3 31 MALA080044 1 20080326 A 5320 WEB SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 RT AFT CORNER OF AFT GALLEY FLOOR WEB IS CHAFED FROM AIR STAIRS SLIDE PLATE. BLENDED OUT DAMAGE INSTALLED DOUBLER COMPL ETED REPAIR IAW MAL EO S53362. 2 L 7 2 4T RT A52EU 2008033100309 20080331 00309 NM 2008 3 31 DLM90080433 1 20080306 A 5320 99305389 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 LT CABIN CUSP WEB FS 584 CORRODED AT LIGHTENING HOLE ON UNDERSIDE. REPLACED LT CABIN CUSP WEB FS 584, IAW MD90 SRM 51-1 0-05. 2 L 7 2 4F RT A6WE 2008033100310 20080331 00310 NM 2008 3 31 DLM90080434 1 20080313 A 5313 LONGERON DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 LONGERON 29.5R CORRODED FROM Y-1268.0 TO Y-1276.5. REMOVED CORROSION NO NOTABLE LOSS. TREATED AND PRIMED, IAW MD90 SRM 51-10-03. INSTALLED FASTENERS, IAW MD90 SRM 51-30-05 VOL II. 2 L 7 2 4F RT A6WE 2008033100311 20080331 00311 NM 2008 3 31 DLM90080435 1 20080306 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 LT CUSP WEB CABIN FS 683-690 CORRODED. BLENDED CORRODED AREA, FOUND TO BE OUT OF LIMITS AND REPAIRED, IAW MD90 SRM 53-1 0-02, 51-10-03 AND MD80 DRD 53-05D FIG 827D. 2 L 7 2 4F RT A6WE 2008040100006 20080401 00006 EU 2008 4 1 08FDEA01157 1 20080326 A 5755 A5777020920400 SPOILER AIRBUS 310 A310203 3930313 EU RT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT WING NR 7 SPOILER TRAILING EDGE IS KNIFED EDGED. REMOVED DAMAGED RIGHT WING SPOILER TRAILING EDGE SEAL AND REPLAC ED WITH A NEW SEAL P/N A5777020920400, PO 612493-3 BOTH IAW FEDEX A310-200 SRM 51-40-21; PG 11-24. PRIMED AND TOP COAT PAINTED BOTH IAW FEDEX A310-200; SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008040100007 20080401 00007 EU 2008 4 1 08FDEA01158 1 20080326 A 5730 A5735005700000 PANEL AIRBUS 310 A310203 3930313 EU LT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LEFT WING FUEL TANK PLATE NR 540 FB HAS FRETTING FROM THE MESH GASKET. EVALUATED AND FOUND TO BE OUT OF LIMITS FOR PANE L 540 FB DUE TO NO DAMAGE ALLOWED IN AREA PER FEDEX A310 SRM 57-20-16; PG 109. ORDERED AND RECEIVED A NEW CLAMP PLATE F OR PANEL 540 FB P/N A5735005700000, PO 613410.1. PANEL TO BE INSTALLED ON FEDEX WORK CARD 45C0529. 2 L 7 2 4F RT A35EU 2008040100013 20080401 00013 WP 2008 4 1 08FDEA01165 1 20080327 A 5712 ARB300618 RIB DOUG DC10 DC1030F 3023504 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 307FE 48291 RT WING L/E INT ZONE FOUND CRACK ON RIB. REPAIRED RIB IAW SRM 57-00-01 FIG 10 VOL I. 2 L 7 3 4F RT A22WE 2008040100017 20080401 00017 WP 2008 4 1 IXXA08SMN054S 1 20080207 A 5751 SKIN DOUG DC8 DC871F 302199D WP AILERON SCRATCHED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD AILERON LOWER SKIN SCRATCHED BETWEEN STATION XA 737.000 AND XA 76 3.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED P ARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE FOUND AT MOMENT WITHIN TOLERANCE MOMENT 3324.57 INCH POUND. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, DC8 SRM 51-4-3 PAGE S 1 AND 3, DC8 SRM 57-8-1 FIGURE 4 ITEM "E" AND "L", DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 51-1-9 T/R 51-142, AND DC8 SRM 51-1-9A T/R 51-141, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008040100019 20080401 00019 WP 2008 4 1 IXXA08SMN63S 1 20080208 A 5753 SKIN DOUG DC8 DC871F 302199D WP T/E FLAP DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP LOWER SKIN SHOWS DENTS AT STATION XF 434.000. REMOVED FASTE NERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-7-1 FI GURE 4 T/R 57 - 94 ITEM "U" AND "Q", DC8 SRM 57-1-0 PAGE 1, 51-1-21, DC8 SRM 51-1-9 T/R 51-142 DATED 04-05-06, DC8 SRM 5 1-1-9A T/R 51-141 DATED 04-03-06, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008040100020 20080401 00020 NM 2008 4 1 TAMF20080020S 1 20080313 A 7830 3114M90001 FITTING BOEING 767 767200 1385120 NM GE CF6 CF680 30025 NE THRUST REVERSER CRACKED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 770QT 23802 DURING C CHECK INSPECTION WAS FOUND A CRACK ON CF6-80C2, THRUST REVERSER FITTING P/N 3114M90-001 AT 2 O’CLOCK. DAMAGED A REA WAS REPAIRED IAW EWO 767 54-036 AND TAC-080316. THIS REPAIR IS CLASSIFIED AS TEMPORARY REPAIR AND THE AFFECTED FITTI NG MUST BE CHANGED AT NEXT MAJOR MAINTENANCE INSPECTION, C CHECK. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2008040100023 20080401 00023 WP 2008 4 1 IXXA08SMN070S 1 20080214 A 5320 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO INTERCOSTAL END CLIP CRACKED AT STATION 857.000 LONGERON 18 RIGHT. REMOVED CRACKED INTERCOSTAL END CLIP. FABRICATED INTERCOSTAL END CLIP. PERFORMED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND INTERCOSTAL END CLIP. INSTALLED NEW INTERCOSTAL END CLIP IAW DC8 SRM 51-1-21, ATI REPAIR SPECIFICATION NUMBER 2003-05, DC8 SRM 51-1-1 PAGES 1, 13 AND 17, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008040100025 20080401 00025 NM 2008 4 1 ANCF200800006 1 20080323 A 3610 312N53061 DUCT BOEING 757 757236 1384971 NM RROYCE RB211 RB211* 54555 NE LT ENGINE DAMAGED W ANCF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 23 522NA 25133 ENG OVHT DISPLAYED WITH ENG OVHT LIGHT ILLUM. LIGHT EXTING AFTER THRUST REDUCTION AND CAUTION LIGHT ON. 4AW AMM 36-11-0 1 P.401 / 36-11-07 P.401. REMOVED AND REPLACED BOTH HP2 AND HP6 DUCT ASSY IAW AMM 71-00-00 ENG RUN PERFORMED SATISFACTO RY. P/N 312N5306-1 HP2 ; S/N ON: 05881143 S/N OFF: 12900828. DURING TROUBLESHOOTING FOUND EICAS MSG TURBINE OVHT LP1 DISPLAYED. IAW AMM 26-13-01 P401 REMOVED AND REPLACED LOOP 1 TURBINE OVHT SWITCH. OPS CHECK SATISFACTORY. 2 L 7 2 4F 4 F RT A2NM A12EU 2008040100026 20080401 00026 NM 2008 4 1 TAMF20080014S 1 20080314 A 5711 SPAR BOEING 767 767200 1385120 NM GE CF6 CF680 30025 NE CENTER WING CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 770QT 23802 DURING C2 CHECK INSPECTION WAS FOUND CORROSION ON THE CENTER WING REAR SPAR WEB NEAR RBBL 75 AT THE REAR SPAR BULKHEAD F ITTINGS. DAMAGED AREA WAS BLENDED TO A MINIMUM WEB THICKNESS OF 0.288 INCHES AND NDT (EDDY CURRENT) INSPECTION DID NOT R EVEAL ANY REMAINING DAMAGE. BLENDED AREA WAS SHOT PEENED AND ORIGINAL FINISHES WERE RESTORED. THOSE ACTIONS WERE PERFORM ED IAW EWO 767 57-039 AND MFG SERVICE REQUEST 1-789568476. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS I SSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2008040100028 20080401 00028 NM 2008 4 1 UIEA200800070 1 20080313 A 5347 SEAT TRACK BOEING 747 747341 13848AM NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 MAIN DECK STA 1700 LBL 75 SEAT TRACK HAS LEVEL 1 CORROSION. CORROSION REMOVED AND TREATED IAW SRM 51-10-01. 2 L 7 4 4F RT A20WE 2008040100030 20080401 00030 NM 2008 4 1 UIEA200800073 1 20080313 A 5315 65B38753U2 FLOORBEAM BOEING 747 747341 13848AM NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 MAIN DECK STA 2020 RBL 62 FLOORBEAM CRACKED. REPLACED FLOORBEAM LOWER SUPPORT FITTING IAW SRM 51-10-01. 2 L 7 4 4F RT A20WE 2008040100034 20080401 00034 NM 2008 4 1 TAMF20080015S 1 20080316 A 5320 SILL BOEING 767 767200 1385120 NM GE CF6 CF680 30025 NE BS 500-522 CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 770QT 23802 DURING C2 CHECK WAS FOUND CORROSION ON LOWER SILL OF LARGE CARGO DOOR CUTOUT BETWEEN STA 500-522. DAMAGED AREA WAS REPAI RED IAW EWO 767 53-074 AND MFG SERVICE REQUEST 1-791518899. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2008040200170 20080402 00170 NM 2008 4 2 2008UALA01662 1 20080325 A 3350 1013392001 LENS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS MISINSTALLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 116UA 26908 EXIT SIGN ON GALLEY AT 4R INOP. FOUND MISINSTALLED. REINSTALLED EXIT LENS. OP CK NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200175 20080402 00175 NM 2008 4 2 2008UALA01666 1 20080324 A 3350 767 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 524UA 24977 EXTERIOR EMERGENCY LIGHT INOP AT DOOR 4R. CAUSE, LAMP INOP. RELAMPED ASSY, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200207 20080402 00207 EA 2008 4 2 TRAX200800434 1 20080320 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 355CA 10067 RIGHT SIDE FLOOR SILL CORRODED AT FS 280 CROSSBEAM. REPAIRED RT SIDE FLOOR SILL AT FS 280 CROSSBEAM ON WO 86003 T/C REO 670-53-21-139, JOB COMPLETE. [SUPPLEMENTAL SDR CLOSED 3/31/08. 2 L 7 2 4F RT A21EA 2008040200217 20080402 00217 NM 2008 4 2 SWAA081718 1 20080327 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 326, STR 26R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008040200218 20080402 00218 NM 2008 4 2 2008UALA01695 1 20080325 A 2700 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FLT CONTROLS UNKNOWN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 221UA 30552 PER CREW WHEN ONLY ELEVATOR MOVEMENT, HAD TOO MUCH RESISTANCE. WHEN ONLY AILERON MOVEMENT, RIGHT SIDE TOO MUCH RESISTAN CE. WITH SPOILERS DEPLOYED AILERONS OK. ELEVATORS ALWAYS HAD TOO MUCH RESISTANCE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040200219 20080402 00219 NM 2008 4 2 SWAA081719 1 20080330 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008040200221 20080402 00221 NM 2008 4 2 2008UALA01696 1 20080325 A 3350 POWER SUPPLY BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 223UA 30224 RIGHT AISLE EMERGENCY EXIT LIGHT AT DOOR 1R IS INOP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040200235 20080402 00235 NM 2008 4 2 SWAA081700 1 20080330 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040200238 20080402 00238 NM 2008 4 2 SWAA081702 1 20080330 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040200244 20080402 00244 NM 2008 4 2 SWAA081721 1 20080330 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040200245 20080402 00245 NM 2008 4 2 2008UALA01714 1 20080326 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 600 S24L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 FWD PIT AT STA 600 AT STR 24L, FRAME INBOARD FLANGE DENTED. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR IAW SRM. T HIS IS A CAT B ZONE 2 RPR WHICH REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS TO BEGIN WHEN ACFT REACHES 45,636C AND 11,000C THEREAFTER. CURRENT CYCLES IS 20,636 PER SRM 53-00-07 RPR 5 TABLE II. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200252 20080402 00252 2008 4 2 2008UALA01720 4 20080327 A 2565 81020401 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR SLIDE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 575UA 26689 FOUND DOOR 2R SLIDE LIGHT INDICATOR INOP. FOUND A WEAK PROX SENSOR. REPLACED PROX SENSOR 585-3162 AT DOOR 2R AT AFT POS ITION. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200259 20080402 00259 NM 2008 4 2 ASAA0852783 1 20080327 A 2421 UA5385513 OIL COOLER BOEING 737 737890 1384527 NM NR 1 IDG DIRTY A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 587AS 35684 NR 1 IDG OIL SAMPLE ANALYSIS SHOWS HIGH LEVELS OF DIRT CONTAMINATION AND TRACE METAL VALUES. REPLACED NR 1 IDG OIL COOL ER. OP AND LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 2008040200260 20080402 00260 NM 2008 4 2 ASAA0852782 1 20080327 A 3040 8300005604 CONTROL UNIT BOEING 737 737890 1384527 NM WINDOW HEAT FAULTED A ASAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 02 558AS 35177 RIGHT FWD WINDOW OVERHEAT LIGHT ILLUMINATED IN FLIGHT. FOUND RT FRONT WINDOW HEAT PWR C/B OUT. VISUAL INSPECTION OF WI RING AT WINDOW AND RACK GOOD. RESET C/B. UNABLE TO VERIFY DISCREPANCY REPLACED RT FWD WINDOW HEAT CONTROLLER PRECAUTIO NARY. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2008040200268 20080402 00268 NM 2008 4 2 08FDEA01171 1 20080328 A 5320 6516350299 VERTICAL BEAM BOEING 727 727225 1384077 NM ZONE 100 SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 STA 1183 FWD SIDE VERTICAL BEAM AT APPROX LBL 12 HAS FASTENERS WITH NO EDGE DISTANCE. REPAIRED IAW EA 7-5310-116973. 2 L 7 3 4F A3WE 2008040100037 20080401 00037 NM 2008 4 1 TAMF20080018S 1 20080315 A 5712 RIB BOEING 767 767241 1385115 NM GE CF6 CF680 30025 NE LT WING CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 770QT 23802 CORROSION ON LT WING OB L/E RIB LOWER OUTER SHROUD AT STA 933.73 AND 938.73. (2) RIBS WERE FABRICATED AND INSTALLED IAW MFG AUTHORIZATION PO214294 AND PO214297, DRAWINGS 117T2224 AND 114T2223 AND SRM 51-40-02/1-3 AND 7. 2 L 7 2 4F 4 F RT A1NM E13NE 2008040100039 20080401 00039 NM 2008 4 1 SA08015 1 20080318 A 3397 WIRE AIRBUS A319 A319132 3930340 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 838AW 2615 PHX - ROW 16 EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED WIRING AT THE WALL DISCONNECT. OPERATIONALL Y CHECKS OK. 2 L 7 2 4F RT A28NM 2008040100042 20080401 00042 EU 2008 4 1 BA08011 1 20080320 A 3234 SELECTOR VALVE AIRBUS 330 A330323 3930335 EU LANDING GEAR FAILED A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 275AY 0370 PHL FLT 741 MAD TO PHL, CREW STATED 'NLG WHEEL STEERING FAULT DISPLAYED ON ECAMS WHEN NLG EXTENDED.' CREW RECYCLED THE GEAR TO SEE IF THE INDICATION WOULD DISAPPEAR AND IT DID NOT. THE GEAR INDICATION SHOWED THREE GREEN FOR BOTH CYCLES. FLIGHT LANDED AND TAXIED OFF THE ACTIVE RUNWAY UNDER ITS OWN POWER AND STOPPED, REQUESTING A TOW IN BY TUG. AN EMERGENC Y WAS DECLARED AS A PRECAUTIONARY MEASURE. MAINTENANCE REPLACED NWS SELECTOR VALVE. 2 L 7 2 4F RT A46NM 2008040100047 20080401 00047 NM 2008 4 1 USAA920080644 1 20080318 A 5330 6545772 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 PHX - MAJOR REPAIR - WEEKLY - CRACKED FUSELAGE SKIN, BS 907, S4L. REPAIRED FUSELAGE SKIN, BS 907, S4L IA155AWW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008040100048 20080401 00048 NM 2008 4 1 USAA920080645 1 20080319 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 157AW 23779 PHX - MAJOR REPAIR - OVERNIGHT CHECK - CRACKED FUSELAGE SKIN, BS 727E, S23L. REPAIRED FUSELAGE SKIN, BS 727E, S23L IAW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008040100058 20080401 00058 2008 4 1 BA08012 4 20080321 A 3441 46502003030316 ADIRU AIRBUS 330 A330323 3930335 EU NR 3 FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 274AY 28311 1297 0342 PHL - FLT 704 - CLT TO FRA - PRIOR TO COAST OUT, RECEIVED 'NAV IR3 FAULT'. FLIGHT COULD NOT CONTINUE ETOPS PER PROCEDUR ES. FLIGHT DIVERTED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADIRU NUMBER 3. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A46NM 2008040100060 20080401 00060 NM 2008 4 1 USAA920080654 1 20080226 A 5711 6545321513 SPAR BOEING 737 7373S3 1384711 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - LEFT WING REAR SPAR UPPER CHORD CRACKED, RSS 222.5. REPAIRED LEFT WING REAR SPAR UPPER CHORD CRACKED, RSS 222.5 IAW USAIRWAYS EA 100282. 2 L 7 2 4F RT A16WE 2008040100062 20080401 00062 NM 2008 4 1 USAA920080656 1 20080219 A 5743 6549488 SUPPORT FITTING BOEING 737 7373S3 1384711 NM LT MLG CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - LEFT WING MLG AFT SUPPORT FITTING CRACKED, WBL 187. REPLACED LEFT WING MLG AFT SUPPORT FITTING CRACKED, WBL 187 IAW USAIRWAYS EA 100282. 2 L 7 2 4F RT A16WE 2008040100075 20080401 00075 NM 2008 4 1 USAA920080662 1 20080226 A 5315 D53472189202 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801AW 889 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON FLOORBEAM, BS 2884/FR 68, -Y1292. REPLACED FLOORBEAM, BS 2884/FR 68, -Y129 2 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008040100076 20080401 00076 NM 2008 4 1 USAA920080663 1 20080226 A 5315 D53472172203 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801AW 889 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON FLOORBEAM, BS 2786/FR 66 - BS 2884/FR 68, -Y1292. REPLACED FLOORBEAM, BS 2 786/FR 66 - BS 2884/FR 68, -Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008040100079 20080401 00079 WP 2008 4 1 AMTA200800234 1 20080318 A 3397 WIRE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL EMERGENCY LIGHTS DAMAGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 706TZ 46582 CARPET BY EMERGENCY FLOOR PATH LIGHTING AT D LAV PULLED UP, WIRES PULLED FROM SPLICE AT LIGHT STRIP. REAPIRED WIRES IAW SWPM 20-00-00 EMERGENCY LIGHTS. OPS CKS GOOD IAW MM 33-50-00. RESECURED CARPET AS REQUIRED. (K) 2 L 7 3 4F 4 F A22WE A23EA 2008040100082 20080401 00082 NM 2008 4 1 AMTA200800237 1 20080318 A 2420 1152466250 CONVERTER BOEING 737 73783N 13844HI NM UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 304TZ 30675 DURING ETOPS PREDEPARTURE CHECK, FOUND MSG NR 49-41-244 FOR APU BITE TEST. START CONVERTER SHOWS FAILED GENERATOR DIODE . T/S IAW FIM 49-40-00-810-806. FOUND START CONVERTER UNIT FAILED. REMOVED AND REPLACED START CONVERTER UIT IAW MM 49 -41-61. OPS CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 2008040100085 20080401 00085 EA 2008 4 1 A6WA200840149 1 20080302 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS FAILED A A6WA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 428AW 7695 AFTER LANDING, ON TAXI, FLAPS FAILED CAS MESSAGE (45 DEGREES) PERFORMED RESET IAW SUPPLEMENT 98-018B. DURING TEST FLAPS FAILED AT 20 DEGREES. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008033100040 20080331 00040 WP 2008 3 31 UPS08851935 1 20080301 A 5753 PANEL DOUG DC8 DC873F 302199F WP T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 LEFT I/B FLAP STRUCTURE CRACKED AT NUT PLATE FOR SURFBOARD PANEL INSTALLATION NEAR O/B TRAILING EDGE. STOP DRILL CRACK, FABBED DOUBLER AND INSTALLED IAW SRM 57-2-0, 51-1-21, 51-1-8, 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 2008033100067 20080331 00067 2008 3 31 AMTA200800149 4 20080225 A 3460 DISPLAY BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT INOPERATIVE A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 518AT 27974 FO CDU DISPLAY BLANK. SELECTING ALTN FMC CORRECTS THE FAULT. PERFORMED FMC BITE PROCEDURE, IAW 34-61-00. COULD NOT DU PLICATE, OPS CK GOOD. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008033100068 20080331 00068 NM 2008 3 31 AMTA200800151 1 20080228 A 5347 RAIL BOEING 737 73783N 13844HI NM BS 727 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 RAIL ASSY RBL 8.1, STA 727I (T) UNION AREA HAVE LIGHT CORROSION. REMOVED CORROSION ORG MAT .071, REM MAT .036, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A, FIG 103, DAIL D, FABRICATED REPAIR IAW EA 737-5300-08-A0037. 2 L 7 2 4F RT A16WE 2008033100071 20080331 00071 WP 2008 3 31 08FDEA01141 1 20080325 A 5514 AUB7108139 PANEL DOUG MD10 MD1010F 3022112 WP HORIZ STAB CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LEFT HORIZONTAL STABILIZER PANEL NR 335 BB IS CHAFED. BLENDED CHAFED AREA. ORIGINAL MATERIAL 0.071; REMOVED 0.015; REM AINING MATERIAL 0.056 IAW DC/MD-10 SRM 54-00-02; VOL I. FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 54- 51-02; VOL III. FABRICATED DOUBLER IAW DC/MD-10 SRM 54-00-01; VOL I AND DC/MD-10 SRM 54-51-02; VOL III. ALODINED AND PRIMED IAW DC/MD -10 SRM 51-21-01; VOL II. ASSEMBLED DOUBLER IAW DC/MD-10 SRM 51-35-01; VOL II. 2 L 7 3 4F RT A22WE 2008033100076 20080331 00076 NM 2008 3 31 AMTA200800159 1 20080228 A 5320 SILL BOEING 737 73783N 13844HI NM CARGO DOORWAY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 AFT CARGO DOOR LOWER SILL WITH LIGHT CORROSION (SCUFF PLATE AREA). REMOVED LIGHT CORROSION, ORG MAT .045, MAT LOSS .002 , REM MAT .043, FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53-1A-2, ALODINED AND PRIMED IAW SRM 51-20-01. 2 L 7 2 4F RT A16WE 2008033100081 20080331 00081 NM 2008 3 31 AMTA200800163 1 20080228 A 5730 SKIN PANEL BOEING 737 73783N 13844HI NM LT WING CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 LT WING FUEL TANK ACCESS 532AB HAS PITTING CORROSION ON LOWER SKIN PANEL LANDING AND CLAMP RING. REMOVED PITTING CORROS ION ON LT WING FUEL TANK ACCESS LANDING IAW SRM 51-01-02-0G, ORG MAT .176, MAT LOSS .001, REM MAT .175, FOUND WITHIN LIM ITS IAW 57-20-01-1A, FLAP PEENING IAW SRM 51-20-06 AND SOPM. (K) 2 L 7 2 4F RT A16WE 2008033100087 20080331 00087 EU 2008 3 31 08FDEA01147 1 20080326 A 5320 SHEAR PLATE AIRBUS 300 A300B4622 3930401 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 720FD * 417 MCD FR79-80 STRING 26L ATTACH WEB CRACKED REMOVED SHEAR PLATE IAW SRM 51-40-21. FABBED SHEAR PLATE IAW MAE TRAVLER T8/7 31840. LOCATED AND DRILLED IAW SRM 51-40-44, ALODINED IAW SRM 51-20-10. PRIMED IAW SRM 51-20-10. INSTALLED SHEAR PLAT E IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008033100109 20080331 00109 NM 2008 3 31 AMTA200800185 1 20080228 A 5321 FLOOR PANEL BOEING 737 73783N 13844HI NM BS 400 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 314TZ 30640 120AF FLOOR PANEL HAS CORROSION AROUND EDGES. REMOVED CORROSION, ORG MAT .080, MAT LOSS .001, REM MAT .079, FOUND TO BE WITHIN LIMITS 53-0053-1A, ALODINED AND PRIMED IAW SRM 51-20-01-0G. (K) 2 L 7 2 4F RT A16WE 2008033100125 20080331 00125 WP 2008 3 31 AMTA200800204 1 20080303 A 3350 EMBS1392 BATTERY DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2B 30018 NE EMERGENCY LIGHTS UNSERVICEABLE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 701TZ 46583 IAW L/S CHECK, ITEM 9D EMERGENCY LIGHT TEST GREEN LIGHT DOES NOT ILLUMINATE. BATT PACK TEST SWITCH USED, MID CABIN DISP LAYED. REMOVED AND REPLACED POWER FAILURE BATTERY POWER SUPPLY UNIT, IAW AMM 33-51-01 AND TEST IT OPS CHECK GOOD TEST G REEN LIGHT TESTING OK. (K) 2 L 7 3 4F 4 F A22WE E23EA 2008033100162 20080331 00162 NM 2008 3 31 AMTA200800226 1 20080315 A 3150 WARNING LIGHT BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE APU FALSE INDICATION A AMTA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 11 552TZ 32586 APU FAULT LIGHT DISPLAYED 1ST AND 2ND START ATTEMPT NO RPM OR EGT RISE. PERFORMED VISUAL INSP OF APU NO DEFECTS NOTED. COMPLIED WITH FIM PROCEDURES 49-11-00, FIG 104, OPS TEST ON GROUND NORMAL, FAULT MESSAGE CLEARED. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008033100189 20080331 00189 EA 2008 3 31 SWIA200819396 1 20080325 A 3520 MASK CNDAIR CL600 CL6002D24 1390016 EA CABIN DEPLOYED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 806SK 15070 ALL O2 MAKS DROPPED FROM OVERHEAD PANELS DURING BOARDING. FLIGHT NR 3809. INSPECTED AND RESTOWED ALL O2 MASKS IAW CRJ 900 AMM 35-20-00. 2 L 7 2 4F RT A21EA 2008033100214 20080331 00214 NM 2008 3 31 DHL2008754001 1 20080312 A 5753 652163254 WEDGE BOEING 727 727223 1384074 NM T/E FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 754DH 22008 UPON INSPECTING THE EXTERIOR OF THE AIRCRAFT, FOUND THE RIGHT INBOARD TRAILING EDGE MID FLAP WEDGE DELAMINATED AT THE IN BOARD END. ABOUT 20 INCHES FROM THE INBOARD END HAS A DELAMINATION APPROX 6 INCHES LONG SPANWISE AND THE WIDTH OF THE W EDGE. PART REPAIRED UTILIZING BOEING STRUCTURAL REPAIR MANUAL 51-40-20. ALUMINUM HONEYCOMB REPAIR, 51-50-2 MATERIAL ID ENTIFICATION, AND 51-40-21. MATERIAL USED 7075-T6 .016" PO NR 9005802. THIS IS A MAJOR REPAIR AND PERMANENT REPAIR. 2 L 7 3 4F A3WE 2008033100230 20080331 00230 NM 2008 3 31 QXEA200800328 1 20080320 A 5320 SILL DHAV DHC8 DHC8202 2809007 NM CARGO DOORWAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - C4- MCD THRESHOLD UPPER SILL PLATE HAS CORROSION AT SEVERAL FASTENER HOLES. REMOVED MCD UPPER SILLPLATE BY REMOVI NG RIVETS, INSTALLED NEW THRESHOLD AND NUTPLATE REF SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008033100250 20080331 00250 WP 2008 3 31 DHL2008805523 1 20080310 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 AFT CARGO COMPT BILGE FITTING CRACKED 2" STA 1280.000 L-33R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACK ED FITTING IAW SRM 53-1-0 PG 1, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2008033100265 20080331 00265 WP 2008 3 31 DHL2008805521 1 20080311 A 5720 FITTING DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 RT WING T/E ZEE CRACKED 0.500" AT STA XW -3.125. REMOVED CRACKED ZEE IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ZEE IAW SRM 51-1-21. REFER TO JC EC-00797-001 (WO 3457) FOR ZEE FABRICATION. 2 L 7 4 4F RT 4A25 2008033100268 20080331 00268 NM 2008 3 31 QXEA200800319 1 20080320 A 5330 SKIN PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX -C4- CORROSION ON BAG FLOOR LEVEL SKIN PANEL AT FWD EDGE OF CIRCULAR PANEL JUST O/B FROM PANEL 144HZ, STAX593. REMO VED CIRCULAR PANEL BY REMOVING SCREWS TO FACILITATE BLEND. REMOVED ONE NUTPLATE REF DHC 8/200 SRM 51-40-11 TO FACILITAT E BLEND. BLENDED LIGHT SURFACE CORROSION REF DHC 8/200 CPCM CHAPTER 4. HFEC INSPECTED BLEND AREA FOR CRACKS IAW D 8/200 NDTM, PART 6, 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECK OF BLENDED AREA IAW -8/200 NDTM PART 1, 51-00-04 HIGH .040 LOW .037. AREA OF BLEND WITHIN LIMITS REF DHC 8 SRM 51-20-11. APPLIED ETCH ALODINE AND PRIMER IAW DHC 8 SRM 51-20-16 AND 51-20-36. REINSTALLED NUTPLATE REF DHC 8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008033100289 20080331 00289 NM 2008 3 31 DLM90080422 1 20080320 A 5320 99305385 CUSP WEB DOUG MD90 MD9030 3023690 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 CUSP WEB AT FS 830 LBL 54.5 HAS PREVIOUS DAMAGE CONSISTING OF 2 EA DRILL STARTS. REMOVED AND REPLACED WEB, IAW MD90 SRM 51-30-01 AND 51-30-02. 2 L 7 2 4F RT A6WE 2008040200269 20080402 00269 EU 2008 4 2 08FDEA01173 1 20080328 A 5511 SPAR AIRBUS 310 A310203 3930313 EU ZONE 300 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 445FE 297 PREVIOUS REPAIR LOCATED ON RIGHT THS UPPER REAR SPAR CHORD BETWEEN RIBS 4 AND 5 HAS 1 EACH REPAIR ANGLE ON LOWER SURFACE OF FLANGE MEASURING 15.2 INCH LONG BY 1.65 INCH TALL REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INST ALLED CORRECT REPAIR ANGLE IAW A310 SRM 55-11-21 FIG 211, 213 AND 218. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART N UMBER AND IS A RESULT OF AGING, AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008040200282 20080402 00282 NM 2008 4 2 CALA0800282 1 20080307 A 5320 69489856 ATTACH ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INTERCOSTAL ATTACH ANGLE TO FRAME AT STA 360 AND STR 11 LT LOCATION IS CRACKED (MARKED). REMOVED AND REPLACED INTERCOST AL ATTACH ANGLE TO FRAME AT STA 360 AND STR 11 LT IAW B737 SRM 51-40-02 AND PACE EA 350-53-003 CAL AND EC/RA 5310-04741. 2 L 7 2 4F RT A16WE 2008040200283 20080402 00283 EU 2008 4 2 08FDEA01186 1 20080328 A 5321 A5378198422200 FLOOR PANEL AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 MAIN DECK FLOOR STRUCTURE HAS CORROSION ON THE UPPER SURFACE OF THE FLOOR WEBBING AT FRAME 35; APPROX LBL 87. BLENDED O UT CORROSION REF A310-200 SRM 51-74-10; PARA 5. ORIGINAL MATERIAL THICKNESS OF 0.094 AND 0.065 AFTER BLEND OUT FOR A TO TAL MATERIAL LOSS OF 0.029. FOUND TO BE OUT OF LIMITS REF A310-200 SRM 53-14-13; FIG 1. UT GAUGE 82750 USED. REMOVED WEBBING REF A310-200 SRM 51-40-21; PGS 6-7. LOCATED AND DRILLED WEBBING P/N A5378198422200, PO 612403.1 REF A310-200 SRM 51-40-44; PGS 6-7. ALODINED AND PRIMED WEBBING REF A310-200 SRM 51-21-10. INSTALLED WEBBING REF A310-200 SRM 51-4 0-21; PGS 6-7. APPLIED CIC REF A310-200 AMM 51-22-00-0. 2 L 7 2 4F RT A35EU 2008040200284 20080402 00284 WP 2008 4 2 08FDEA01187 1 20080328 A 5310 ADA36751 FITTING DOUG DC10 DC1010F 3022111 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION MAIN CARGO DOOR LOWER JAM SUPPORT FITTING AFTER INSPECTION FOUND BORE "B", "A" AND "D" OF FITTING NR 4 WITH CORROSION (DIAMETER .456") (REF EO FEDEX 8-5230-117635. PERFORMED REWORK HOLE FOR SRM 53-50-00 FIG 17, PERFORMED NDI AND INSTALLED BUSHING FOR SRM 53-50-00 FIG 17 VOL. I 2 L 7 3 4F A22WE 2008040200285 20080402 00285 NM 2008 4 2 CALA0800283 1 20080307 A 5320 69489852 ATTACH ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INTERCOSTAL ATTACH ANGLE TO FRAME AT STA 360 AND 8 LT LOCATION IS CRACKED (MARKED). REMOVED AND REPLACED INTERCOSTAL AT TACH ANGLE TO FRAME AT STA 360 AND STR 8 LT IAW B737 SRM 51-40-02 AND PACE EA 350-53-003 CAL AND EC/RA 5310-04741. 2 L 7 2 4F RT A16WE 2008040200298 20080402 00298 NM 2008 4 2 KCSA081184 1 20080320 A 5412 BULKHEAD BOEING 747 747209B 138489B NM NR 3 PYLON GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 NR 3 PYLON REAR ENGINE MOUNT BULKHEAD IS GOUGED AT NAC STA 222 ABOVE EXISTING REPAIR. 2 L 7 4 4F RT A20WE 2008040200302 20080402 00302 NM 2008 4 2 KCSA081187 1 20080320 A 5311 FRAME BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 STA-1600 FRAME UPPER CHORD DAMAGED AT RBL-15. 2 L 7 4 4F RT A20WE 2008040200304 20080402 00304 NM 2008 4 2 KCSA081189 1 20080320 A 5210 DOOR FRAME BOEING 747 747SR46 1384816 NM R2 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 R-2 DOOR FWD LOWER CORNER VERTICAL FRAME CRACKED IN RADIUS APPROX 11 INCHES. 2 L 7 4 4F RT A20WE 2008040200306 20080402 00306 NM 2008 4 2 KCSA081191 1 20080320 A 5411 FRAME BOEING 747 747146 1384905 NM NR 2 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 NR 2 PYLON AFT ENGINE MOUNT BULKHEAD FRAME CRACKED 1.25 INCH AT NAC STA 221.9. 2 L 7 4 4F RT A20WE 2008040200307 20080402 00307 NM 2008 4 2 HALA0800431 1 20080319 A 3397 WIRE BOEING 767 767332 1382001 NM EMERGENCY LIGHTS DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 DAMAGED WIRE FOR SEAT 2J ESCAPE PATH LIGHTING. REPAIR IN WORK. 2 L 7 2 4F RT A1NM 2008040200308 20080402 00308 NM 2008 4 2 HALA0800432 1 20080325 A 2620 8981501 CARTRIDGE BOEING 717 717200 1383700 NM FIRE BOTTLE MALFUNCTIONED A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 484HA 55129 "AGENT NR 1 LOW" ON. REMOVED AND REPLACED NR 1 FIRE BOTTLE PER AMM 26-21-01, OPS CHK GOOD OK TO CONTINUE. REMOVED AND REPLACED FIRE CONTAINER DISCHARGE CARTRIDGE PER AMM 26-21-02. 2 L 7 2 4F TR A6WE 2008040200313 20080402 00313 NM 2008 4 2 HALA0800433 1 20080324 A 3150 WARNING MESSAGE BOEING 767 76733A 1385209 NM ILLUMINATED A HALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, EICAS MSG, AILERON BLOCK OUT. PERFORMED FIM 27-11-00. OK FOR SERVICE. NO FAULTS NOTED. 2 L 7 2 4F RT A1NM 2008040200315 20080402 00315 NM 2008 4 2 KCSA081197 1 20080321 A 5320 STIFFENER BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 STA-1760 FRAME STIFFENER DAMAGED AT RBL-65. 2 L 7 4 4F RT A20WE 2008040200318 20080402 00318 NM 2008 4 2 KCSA081198 1 20080321 A 5320 SUPPORT BOEING 747 7472B4B 138481B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA-1260 LT BODY GEAR UP LOCK SUPPORT HORIZONTAL WEB CRACKED .75 INCH. 2 L 7 4 4F RT A20WE 2008040200319 20080402 00319 NM 2008 4 2 HALA0800438 1 20080327 A 2560 FLASHLIGHT BOEING 767 76733A 1385209 NM CABIN INOPERATIVE A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 587HA 33421 F/A PRE-FLIGHT EMERGENCY FLASHLIGHT AT R1 INOP. REMOVED AND REPLACED EMERGENCY FLASH LIGHT AT R1. 2 L 7 2 4F RT A1NM 2008040200322 20080402 00322 NM 2008 4 2 KCSA081199 1 20080324 A 5320 TENSION TIE BOEING 747 747SR46 1384816 NM FUSELAGE BROKEN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 FUSELAGE FRAME TENSION TIE BROKEN BETWEEN BS 1880 AND 1900 ABOVE STR-36L. 2 L 7 4 4F RT A20WE 2008033100292 20080331 00292 NM 2008 3 31 DLM90080425 1 20080324 A 5347 9530085 SEAT TRACK DOUG MD90 MD9030 3023690 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 CABIN SEAT TRACK LBL 54.5 IS OUT OF LIMITS AT FUSELAGE STA 972-1090. REMOVED AND REPLACED SEAT TRACK FS 899 TO 1090, IA W MD90 SRM 53-40-01 FIG 6. 2 L 7 2 4F RT A6WE 2008033100299 20080331 00299 NM 2008 3 31 NWAA081226310 1 20080222 A 5311 FRAME BOEING 747 747451 1384940 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING "M" CHECK, FOUND CRACKS IN 4 FRAME WEB FASTENER HOLES COMMON TO TENSION TIE AREA AT BS 1220. REPAIRED PER EA 63- 212263. 2 L 7 4 4F RT A20WE 2008033100308 20080331 00308 NM 2008 3 31 DLM90080432 1 20080319 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM CABIN CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 CABIN SEAT TRACK LBL 54.5 HAS AREAS WITH NICKS, GOUGES, CORROSION AND BARE METAL FROM FS 196.25 TO FS 1364. REMOVED DAM AGE, FOUND THE FOLLOWING OUT OF SRM LIMITS: FS 421-620, 761-890 AND 1051-1090. ALL OTHER AREAS WITHIN SRM LIMITS, 53-40 -01 FIG 4. ALL REPAIRS TO BE ACCOMPLISHED ON 1003548-2000.0228, 2000.0229, 2400.0230 AND 2400.0231. 2 L 7 2 4F RT A6WE 2008040100004 20080401 00004 NM 2008 4 1 DXTA20082966 1 20080327 A 2750 1250A000002 CONTROL UNIT GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE TE FLAPS INOPERATIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 708QS 069 LEAVING TQPF AFTER GEAR RETRACTION, SELECTED FLAPS TOP 0 DEG AND FLAPS WOULD NOT RETRACT FROM 20 DEG. REMOVED ORIGINAL FSECU AND INSTALLED INSPECTED UNIT. PERFORMED SATISFACTORY RIG AND OPS CHECK OF FLAP SLAT SYSTEM. FOR ALL WORK REF MM 27 -51-00, 27-50-05 AND 27-51-45. 2 L 7 2 4F 4 F RT A53NM E35NE 2008040100041 20080401 00041 NM 2008 4 1 BB08037 1 20080320 A 7330 WARNING SYSTEM BOEING 757 7572S7 1384962 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT ACTIVATED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 903AW 23323 30503 HNL FLT 9010 EN-ROUTE HNL TO PHX, RECEIVED AN "R ENG LP PUMP" MESSAGE ON EICAS. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT IS BEING MAINTENANCE FERRIED TO PHX. 2 L 7 2 4F 4 F RT A2NM E12EU 2008040100044 20080401 00044 EU 2008 4 1 BB08038 1 20080321 A 3397 CONNECTOR AIRBUS 330 A330323 3930335 EU CABIN LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 250AY 23902 BRU - FLOOR EMERGENCY LIGHTS 09G TO 12G AND 16G TO 22G INOP. MAINTENANCE FOUND 2 CONNECTORS LOOSE. SECURED CONNECTORS. OPS CHECKS OK. 2 L 7 2 4F RT A46NM 2008040800155 20080408 00155 2008 4 8 SWAA081782 4 20080402 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008040100064 20080401 00064 NM 2008 4 1 USAA920080657 1 20080222 A 5315 6545410155 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - CRACKED FLOORBEAM CHORD, BS 663 AND BS 670, LBL 24, WL 208. REPAIRED FLOORBEAM CHORD, BS 663 AND B S 670, LBL 24, WL 208 IAW USAIRWAYS EA 100302. 2 L 7 2 4F RT A16WE 2008040100065 20080401 00065 CE 2008 4 1 DXTA20082969 1 20080329 A 3222 STRUT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG DAMAGED E DXTA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 07 946QS 7500195 DURING CLIMB THRU APPROX FL390 AT M.80 GOT RED GEAR UNSAFE LIGHT ACCOMPANIED BY A LOUD THUMP. FOUND UPLOCK ENGAGEMENT B ELOW MINIMUM, AND SWITCH ENGAGEMENT BELOW MINIMUM AND NOSE GEAR STRUT OUT OF TOLERANCE, DISASSEMBLED NLG STRUT, REPACKED STRUT WITH NEW SEALS REASSEMBLED, SERVICED NOSE STRUT. ACCOMPLISHED GEAR BUMP CHECKS IAW MM 12-10-38 AND 32-30-00. OPER ATIONAL CHECKS GOOD 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008040100067 20080401 00067 NM 2008 4 1 DXTA20082970 1 20080330 A 2780 SLAT SYSTEM GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE LE SLATS MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 707QS 066 ON DEPARTURE, GOT FLAP / SLAT MAINT MESSAGE. SLATS DID NOT COME ALL THE WAY UP. PERFORMED FUNCTIONAL TEST OF THE FLAP/ SLAT CONTROL AND DRIVE SYSTEM WITH NO DEFECTS NOTED AT THIS TIME. ALL WORK COMPLETED IAW CMP 275101. 2 L 7 2 4F 4 F RT A53NM E35NE 2008040100077 20080401 00077 NM 2008 4 1 USAA920080664 1 20080305 A 5315 D53472190204 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 801AW 889 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON FLOORBEAM, BS 2670/FR 64 - BS 2786/FR 66, +Y1292. REPLACED FLOORBEAM, BS 2 670/FR 64 - BS 2786/FR 66, +Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008040100080 20080401 00080 NM 2008 4 1 AMTA200800235 1 20080317 A 3350 COVER BOEING 757 75723N 1384973 NM EMERGENCY LIGHTS MISSING A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 514AT 27971 COVER MISSING FROM EGRESS LIGHTING STRIP AT SEAT 5D, WIRES EXPOSED. REINSTALLED EGRESS LIGHT TRACK STRIP AT 5D. OPS CH ECK GOOD. (K) 2 L 7 2 4F RT A2NM 2008040100091 20080401 00091 NM 2008 4 1 USAA920080674 1 20080320 A 5320 SUPPORT ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - LEVEL 2 CORROSION ON GALLEY "Z" SUPPORT ANGLE, BS 969, RBL 33 - RBL 45. REPLACED GALLEY "Z" SUPPORT ANGLE, BS 969, RBL 33 - RBL 45 IAW B737 53-60-51. 2 L 7 2 4F RT A16WE 2008040100096 20080401 00096 EA 2008 4 1 A6WA200840153 1 20080307 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE SERVICE STIFF A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 466AW 7899 SERVICE DOOR HARD TO OPEN. LUBED AND OPS CHECKED IAW 52-40-00, OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008040100106 20080401 00106 EA 2008 4 1 A6WA200840158 1 20080307 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PAX DOOR STUCK A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 421ZW 7346 FLIGHT CREW REPORTS PAX DOOR OUTER HANDLE DOES NOT RELEASE WHEN THE TRIGGER IS PRESSED. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008040200324 20080402 00324 NM 2008 4 2 KCSA081200 1 20080324 A 5320 TENSION TIE BOEING 747 747SR46 1384816 NM FUSELAGE BROKEN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 FUSELAGE FRAME TENSION TIE BROKEN BETWEEN BS 1860 AND 1880 ABOVE STR-36L. 2 L 7 4 4F RT A20WE 2008040200327 20080402 00327 NM 2008 4 2 GTIA0800047 1 20080311 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 502NK 2433 EVIDENCE OF CORROSION ON FLOORBEAM Y1292 FROM FR66 THROUGH FR 68. REMOVED AND REPLACED FLOORBEAM Y1292 FROM FR 66 THROU GH FR 68 IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008040200335 20080402 00335 NM 2008 4 2 NSVA2008012 1 20080320 A 5230 HANDLE BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR UNSECURE A NSVA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 187WQ 4187 CARGO DOOR WARNING AND AIRCRAFT WOULD NOT PRESSURIZE. CYCLED HANDLE, PRESSURIZED AIRCRAFT, NO DEFECTS FOUND. SUSPECT H ANDLE NOT STOWED PROPERLY. 2 H 7 2 4T RT A13NM 2008040100247 20080401 00247 NM 2008 4 1 GTIA0800044 1 20080311 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 502NK 2433 FLOORBEAM AT STATION Y765 BETWEEN FR 66 AND FR 70 CORRODED. REMOVED AND REPLACED FLOORBEAM AT STATION Y765 BETWEEN FR 6 6 AND FR 70 IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008040100248 20080401 00248 NM 2008 4 1 GTIA0800045 1 20080311 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 502NK 2433 EVIDENCE OF CORROSION ON FLOORBEAM Y254 BEAM 175. REPLACED FLOORBEAM Y254 BEAM 175 IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008040100250 20080401 00250 NM 2008 4 1 SB08015 1 20080323 A 3260 655825029 CIRCUIT CARD BOEING 737 7374B7 1384702 NM MLG FAULTY A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 426US 24548 FLL - FLT919 - ON APPROACH TO FLL, UPON LOWERING LANDING GEAR, CREW RECEIVED A NOSE LANDING GEAR RED UNSAFE LIGHT WITH N O MAIN GEAR INDICATION. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND RESET A CIRCUIT BREAKER. CREW THEN R ECEIVED A NORMAL GEAR INDICATION OF THREE GREEN LIGHTS. A FLY-BY THE TOWER WAS ALSO ACCOMPLISHED TO CONFIRM GEAR WAS DO WN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM USING AMM FAULT ISOLATION 32-61-00, LANDING GEAR POSITION INDICATION AND WARNING SYSTEM. REPLACED FILE CARD M983 (GEAR RED LIGHT). ACCOMPLISHED TESTS PER AMM 32- 33-00 (NOSE GEAR EXT AND RETRACT) AND 32-09-10-725 (TEST OF PROX CARDS). NO FAULTS. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2008040100251 20080401 00251 NM 2008 4 1 SB08016 1 20080326 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM EMERGENCY LIGHTS DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 451UW 24934 PHL - MAINTENANCE REPORTED SEVERAL EMERGENCY LIGHTS IN THE MID CABIN WILL NOT STAY ILLUMINATED DURING TEST. MAINTENANCE REMOVED AND REPLACED BATTERY PACK M1479. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008040100252 20080401 00252 EU 2008 4 1 USAA920080711 1 20080313 A 5530 D5537123500600 HINGE FITTING AIRBUS 320 A320231 3930325 EU ZONE 300 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 621AW 53 SAL - MAJOR REPAIR - C6 CHECK - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 5, VERTICAL STABILIZER STATION 2985/RIB 7. RE PLACED RUDDER HINGE FITTING NR 5, VERTICAL STABILIZER STATION 2985/RIB 7 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2008040100256 20080401 00256 EA 2008 4 1 MALA080048 1 20080322 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA ODOR A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 15 8974C 7974 DURING APPROACH NOTICED STRONG FUEL SMELL WHEN APU AIR SELECTED. INSPECTED APU AND COMPLETED RUNS WITH NO SMELL NOTED. 2 L 7 2 4F RT A21EA 2008040100259 20080401 00259 NM 2008 4 1 ASAA0872797 1 20080314 A 5315 143A524010 FLOORBEAM BOEING 737 737790 13844CN NM BS 540 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 607AS 29751 FLOOR SUPPORT CHANNEL AT STA 540 RBL0 RBL 24.75 INBD AND OUTBD ATTACH POINTS CRACKED FLOOR SUPPORT CHANNEL AT STA 540 RB L0 24.75. REPLACED IAW B737 700 SRM 51 40 02 AND B. DRWG 143A5240. 2 L 7 2 4F RT A16WE 2008040100260 20080401 00260 NM 2008 4 1 ASAA0842741 1 20080305 A 5320 615C333675 FLOOR SUPPORT BOEING 737 737490 1384715 NM BS 947-967 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 AFT CABIN UPPER SIDE OF FLOOR SUPPORT AT BS STA 960 RB 46 WL 207.5 HAS CORRODED. REPLACED WITH MADE REPAIR PART. 2 L 7 2 4F RT A16WE 2008040100289 20080401 00289 NM 2008 4 1 SWAA081708 1 20080330 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM. 2 L 7 2 4F RT A16WE 2008040100296 20080401 00296 NM 2008 4 1 SWAA081712 1 20080329 A 5523 REP4HE8 BEARING BOEING 737 7373A4 1384585 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED SPV CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BEARING PER MM. 2 L 7 2 4F RT A16WE 2008040200086 20080402 00086 NM 2008 4 2 SWAA081624 1 20080325 A 3350 3071BPEGPL LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008040200091 20080402 00091 NM 2008 4 2 CALA0800257 1 20080325 A 5320 693874002 STIFFENER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 CORROSION FOUND ON FLANGE AND RADIUS OF INTERCOSTAL AT BL 0 BETWEEN STA 219 TO STA 227. REMOVED CORRODED STIFFENER, DAM AGE FOUND TO BE OUT OF LIMITS IAW B737 SRM 53-10-08. INSTALLED NEW STIFFENER P/N 69-38740U2 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008040200112 20080402 00112 NM 2008 4 2 BB08043 1 20080325 A 3350 417T52280205 LIGHT BOEING 767 7672B7 1385107 NM ZONE 200 BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 PHL - THE EMERGENCY FLOOR LIGHT TRACK WAS FOUND BROKEN AT SEAT 4B. MAINTENANCE REPLACED THE FLOOR LIGHT TRACK AT SEAT 4 B. 2 L 7 2 4F RT A1NM 2008040100114 20080401 00114 NM 2008 4 1 BB08039 1 20080322 A 5730 PANEL BOEING 757 757225 1384959 NM LT WING SEPARATED A USAA K NONE D S INFLIGHT SEPARATION AFFECT SYSTEMS CR CRUISE 1 EA 19 921UW 22201 PHL- FLT 1250 - MCO TO PHL - AFTER A JOLT FROM APPARENT WAKE TURBULENCE, APPROXIMATELY 45 MILES FROM BWI, AT FL 270 AND 320 KIAS, A PANEL ON THE UPPER LEFT WING SEPARATED FROM THE AIRCRAFT IN FLIGHT. THE PANEL WAS LOCATED AFT OF THE REAR S PAR BUT FORWARD OF THE TRAILING EDGE FLAPS, AND FROM ABOUT WBL 79.2 TO ABOUT WBL 130.5. UPON SEPARATION, A PAIR OF HYDR AULIC LINES WERE SEVERED AND A PASSENGER WINDOW AT SEAT ROW 19, LEFT SIDE, WAS CRACKED. AIRCRAFT WAS TEMPORARY REPAIRED AND MAINTENANCE FERRIED TO A HEAVY MAINTENANCE FACILITY. 2 L 7 2 4F RT A2NM 2008040100116 20080401 00116 NM 2008 4 1 BB08040 1 20080322 A 3350 LIGHT BOEING 757 757225 1384959 NM CABIN BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 915AW 22209 PHX - THE EMERGENCY LIGHT ASSEMBLY WAS FOUND BROKEN AT THE AFT LEFT LAVATORY. MAINTENANCE RESECURED THE EMERGENCY LIGHT ASSEMBLY AT THE AFT LEFT LAVATORY. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2008040100118 20080401 00118 WP 2008 4 1 MCC2008F00001 2 20080226 A 7261 ENGINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE LEAKING A MCCA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 11 2699Y AC666 P44484C ON DESCENT TO DESTINATION, ENGINE BYPASS LIGHT ILLUMINATED, ATTEMPTED TO PULL POWER BACK, BUT ENGINE SEEMED TO NOT RESPO ND AND TEMP STARTED TO RISE. ENGINE SECURED AND UNEVENTFUL LANDING MADE. ON GROUND, NOTICED OIL LEAKING FROM ENGINE. FOUND ENGINE WOULD NOT ACTIVATE. ENGINE REMOVED FOR FURTHER INSPECTION AND LOANER INSTALLED. (K) 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 2008040100126 20080401 00126 NM 2008 4 1 USAA920080692 1 20080314 A 5340 69468314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C-18 CHECK - CRACKED STRINGER CLIP, BS 360 S5L. REPLACED CRACKED STRINGER CLIP, BS 360 S5L IAW BOE ING SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008040100128 20080401 00128 EU 2008 4 1 USAA920080698 1 20080324 A 2910 D2917002900300 HYDRAULIC LINE AIRBUS 320 A320214 3930316 EU PTU CRACKED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 109UW 1065 FLT NR 1584 - CREW REPORTED DURING CLIMB-OUT, LOST GREEN HYDRAULIC PUMP THEN YELLOW SYSTEM OVERHEAT MESSAGE ILLUMINATED. CREW DECLARED AN EMERGENCY, PERFORMED A MANUAL GEAR EXTENSION AND RETURNED TO FIELD. MX DISCOVERED PTU LINE LEAKING. MX REPLACED LINE, LEAK CHECK WAS GOOD. AS A PRECAUTION, MX REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP. OPERATIONA L/LEAK CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008040100139 20080401 00139 NM 2008 4 1 ASAA0842717 1 20080227 A 5512 657378354 SKIN BOEING 737 737490 1384715 NM HORIZ STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 R N HORIZ STABILIZER E SKIN DENTED AT STAB STA 147.90 AND 8 DENT AT RT HORIZ STAB L/E SKIN AT STAB STA 147.90 AND 8. RE PAIRED IAW B737 400 SRM 55 10 01 REPAIR 2. 2 L 7 2 4F RT A16WE 2008040100143 20080401 00143 NM 2008 4 1 ASAA0842724 1 20080304 A 5754 65C26603201A SKIN BOEING 737 737490 1384715 NM L/E SLAT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 NR 3 SLAT LWR SURFACE DENTED. DENT REPAIR IAW SRM 51 70 10, REPAIR NR 4. 2 L 7 2 4F RT A16WE 2008040100146 20080401 00146 NM 2008 4 1 ASAA0842714 1 20080305 A 5753 6546435340 SKIN BOEING 737 737490 1384715 NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 RT OUTBOARD AFT FLAP UPPER SKIN HAS DENTS AT SECOND TO INBD FITTING (68 INCHES FROM INBOARD END AND 6 INCHES FROM T/E) A ND 113 INCHES FROM INBOARD END AND 3 INCHES FROM T/E DENTS. REPAIRED IAW B737 400 SRM CH 51 70 10 REP 2. 2 L 7 2 4F RT A16WE 2008040100150 20080401 00150 NM 2008 4 1 UIEA200800078 1 20080313 A 5754 STRUCTURE BOEING 747 747341 13848AM NM KRUEGER FLAP CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 NR 11 KRUEGER FLAP OUTBOARD END INNER FACE CRACKED. DAMAGE TRIMMED OFF AND REPAIR CARRIED OUT WITH FIBERGLASS AS PER SR M 51-40-14 PARA 4H. 2 L 7 4 4F RT A20WE 2008040100152 20080401 00152 NM 2008 4 1 UIEA200800079 1 20080309 A 5755 STRUCTURE BOEING 747 747341 13848AM NM NR 6 SPOILER CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 NR 6 SPOILER LOWER FACE DOUBLER CRACKED NEAR ACTUATOR FITTING. DAMAGED SPOILER REMOVED AND REPLACED WITH SERVICEABLE SP OILER IAW AMM 27-62-01. 2 L 7 4 4F RT A20WE 2008040100153 20080401 00153 NM 2008 4 1 UPS08M51874 1 20080208 A 5511 ALC8121501 SPAR CAP DOUG MD11 MD11F 3023600 NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:1C CORROSION FOUND IN HORIZONTAL STAB LT UPPER FWD SPAR CAP BARREL NUT HOLE NR 1. REMOVED CORROSION FRO M ABOVE AREA AND REPAIRED PER EA 011-5510-01 -A1297. 2 L 7 3 4F RT A22WE 2008040100155 20080401 00155 NM 2008 4 1 MWEA080043 1 20080317 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM COCKPIT DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 927ME 55193 EMERGENCY LIGHTS IN COCKPIT DO NOT COME ON WHEN THE EMERGENCY SWITCH IS TURNED ON. REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F TR A6WE 2008040100157 20080401 00157 CE 2008 4 1 EPUA032808 1 20080327 A 7120 26510291 ATTACH BRACKET CESSNA 208 208B 2073701 CE ENGINE MOUNT CRACKED E EPUA K NONE O OTHER IN INSP/MAINT 1 AL 03 411GV 12195 208B0672 DURING ENGINE MAINTENANCE, 2 CRACKS APPROX .5 INCH LONG WERE DISCOVERED ON THE UPPER ENGINE MOUNT BRACKET ASSY-COWL ATTA CH EMANATING FROM THE BOLT HOLE. A NEW BRACKET AND BOLT WERE INSTALLED AND AIRCRAFT WAS RETURNED TO SERVICE. 1 H 7 1 3T A37CE 2008040100162 20080401 00162 NM 2008 4 1 ASAA0892768 1 20080306 A 5315 143A948537 FLOORBEAM BOEING 737 737990 NM BS 500 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 323AS 30021 FWD CARGO PIT AFT PANEL BULKHEAD LWR FLOORBEAM CORRODED STA 500 L RBL 24 TO LBL 24. REMOVED DAMAGED FLOORBEAM FABRICAT ED LOCATED DRILLED AND INSTALLED A REPLACEMENT PART IAW SRM 53-00-53 FIG 103 DWG 143A9485 & 5.0 P.M. 20 41 02 PGS 2 7. 2 L 7 4 4F RT A16WE 2008040100166 20080401 00166 EA 2008 4 1 TRAX200800430 1 20080318 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 859AS 7421 ON ROTATION RECEIVED WOW INPUT CAUTION MSG. INTERMITTENT THROUGHOUT FLIGHT, MOST ON. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2008040100170 20080401 00170 EA 2008 4 1 TRAX200800429 1 20080318 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 917EV 7769 EMERGENCY LIGHT ABOVE SERVICE DOOR, BASE IS BROKEN. 2 L 7 2 4F RT A21EA 2008040100172 20080401 00172 EA 2008 4 1 TRAX200800445 1 20080320 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 CLIP AT FS 280 O/B LBL 9 CRACKED. REMOVED CRACKED CLIP AT FS 280 O/B OF LBL 9 AND FABRICATED -2 CLIP AS REF IN REO 601R -53-11-171 REV D AND INSTALLED FABRICATED CLIP AT FS 280 O/B OF LBL PER CRJ SRM 51-42-21. 2 L 7 2 4F RT A21EA 2008040100173 20080401 00173 NM 2008 4 1 MWEA080045 1 20080324 A 5220 FITTING BOEING 717 717200 1383700 NM TAILCONE OUT OF ADJUST A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 907ME 55171 AFT ENTRY DOOR EMERGENCY TAIL CONE RELEASE MECHANISM FAILED OPERATIONAL CHECK, DOOR OPENS BUT TAIL CONE DID NOT RELEASE. ADJUSTED INTERNAL JETTISON RELEASE MECHANICAL CLIPS. 2 L 7 2 4F TR A6WE 2008040100177 20080401 00177 WP 2008 4 1 UPS08851923 1 20080324 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:N/A EMERGENCY LIGHTS STAY LIT FOR SHORT PERIOD OF TIME. REMOVED AND REPLACED THE EMERGENCY BATTERY PACK AND RELAY UNIT PER MM 33-50-01-2. OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 2008040100188 20080401 00188 EA 2008 4 1 TRAX200800462 1 20080322 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA A/C BAY MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SO 27 916EV 7757 ACFT BEGAN TO LOSE PRESSURIZATION. BEGAN DESCENT THROUGH 14,000, DEPLOYED CABIN OXYGEN MASKS. CABIN ALTITUDE REACHED 8 ,500. C/W QRH EMERGENCY PROCEDURE 3-2. CONTINUED DESCENT. LANDING WAS UNEVENTFUL. AIRCRAFT RETURNED TO ATL AFTER T/O . EMERGENCY DECLARED. AIR CONDITIONING PACK - LEFT SIDE. 2 L 7 2 4F RT A21EA 2008040100193 20080401 00193 EA 2008 4 1 TRAX200800468 1 20080324 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN CABIN UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 849AS 7347 F/A REPORTS A LOUD SQUEAL COMING FROM THE MAIN CABIN DOOR. THE DOOR IS ALSO DIFFICULT TO CLOSE. 2 L 7 2 4F RT A21EA 2008040100194 20080401 00194 EU 2008 4 1 TRAX200800469 1 20080324 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 630AS 336 F/A REPORTS EMERGENCY LIGHT ON MAIN CABIN DOOR IS INOP. 2 H 7 2 4T RT 2008040100195 20080401 00195 EA 2008 4 1 TRAX200800470 1 20080324 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 719EV 10099 EMERGENCY LIGHTS WILL NOT TEST. 2 L 7 2 4F RT A21EA 2008040100196 20080401 00196 EA 2008 4 1 TRAX200800471 1 20080324 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 859AS 7421 CENTER BOX BEAM CRACKED REPAIR PER REO 601R-53-61-345 AND COMPLY WITH EO 600-53-0072 REV B. REPAIRS PERFORMED IAW: REO 601-53-61-345 AND REO 601R-53-61-2563 2 L 7 2 4F RT A21EA 2008040100197 20080401 00197 EA 2008 4 1 TRAX200800472 1 20080326 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 867AS 7463 REPEAT FLAP SYSTEM FAILURE, FLAPS FAILED AT ZERO ON APPROACH INTO ROC ON 3/23/08, FERRIED TO ATL 3/24/08; REFER TO DEFEC T 373059-3. 2 L 7 2 4F RT A21EA 2008040100198 20080401 00198 EA 2008 4 1 TRAX200800473 1 20080326 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 859AS 7421 RIGHT OUTBOARD CLIP FS 280 RBL 9 CRACKED. 2 L 7 2 4F RT A21EA 2008040100199 20080401 00199 EA 2008 4 1 TRAX200800432 1 20080320 A 5320 ANGLE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 355CA 10067 CORROSION ON COCKPIT ENTRANCE FLOOR PANEL AFT ANGLE. CORROSION ON AFT ANGLE OUT OF LIMITS. REMOVED AND REPLACED WITH N EW ANGLE PER CRJ 700 SRM 51-42-06. BAT 7023167. 3/272008 JOB COMPLETE. SUPPLEMENTAL SDR CLOSED 3/28/08. 2 L 7 2 4F RT A21EA 2008040100206 20080401 00206 NM 2008 4 1 SWAA081676 1 20080327 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040100219 20080401 00219 2008 4 1 SWAA081673 4 20080327 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008040100225 20080401 00225 NM 2008 4 1 SWAA081705 1 20080330 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008040100227 20080401 00227 NM 2008 4 1 SWAA081723 1 20080330 A 5313 6551698 STRINGER SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2008040200121 20080402 00121 NM 2008 4 2 2008UALA01625 1 20080322 A 5210 TORQUE TUBE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 DOOR R1 HAS GOUGE ON INNER DOUBLER AT UPPER HINGE TORQUE TUBE. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR, REPAIR ACCOMPLIS HED AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200127 20080402 00127 NM 2008 4 2 CALA0800263 1 20080327 A 2560 694147322 FITTING BOEING 737 737524 1384721 NM GIRT BAR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11641 28902 L1 ENTRY GIRT BAR ATTACH PTS (2) ARE CORRODED. L-1 GIRT BAR FITTING, STA 312, REMOVED CORROSION FOUND TO BE WITHIN LIMI TS IAW B737 SRM 53-10-15. ALODINED, PRIMED AND PAINTED L-1 AFT GIRT BAR FITTING OUT OF LIMITS. REMOVED AND REPLACED WIT H NEW GIRT BAR FITTING IAW B737 SRM 51-10-02. ALODINE, PRIME, AND PAINT IAW B737 SRM 51-20-01. 2 L 7 2 4F RT A16WE 2008040200135 20080402 00135 NM 2008 4 2 CALA0800272 1 20080328 A 2750 65522111 TORQUE TUBE BOEING 737 737524 1384721 NM T/E FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 46625 27529 NR 3 MID FLAP I/B AND O/B TORQUE TUBES CORRODED AND PITTED. REMOVED AND REPLACED WITH SERVICEABLE TORQUE TUBES I/B AND O/B REF CMM 57-53-17. 2 L 7 2 4F RT A16WE 2008040200157 20080402 00157 NM 2008 4 2 2008UALA01652 1 20080323 A 3397 58791 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 563UA 26665 MID CABIN FLOOR EMERGENCY ESCAPE PATH LIGHTS INOP AT SEAT ROW 9ABC-13ABC. SUPPLEMENTAL DATA UPDATE CAUSE, JUMPER CABLE AT ROW 13ABC SHORTED. REPLACED JUMPER CABLE ASSY FOR ROW 13 ABC. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200169 20080402 00169 EA 2008 4 2 TRAX200800477 1 20080327 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 752EV 10166 LEFT OVERWING EMERGENCY EXIT LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS. 2 L 7 2 4F RT A21EA 2008040200179 20080402 00179 EA 2008 4 2 TRAX200800437 1 20080319 A 5755 CLOSEOUT PANEL CNDAIR CL600 CL6002C10 1390015 EA LT SPOILER CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 355CA 10067 LEFT MULTIFUNCTION SPOILER CLOSEOUT PANEL CRACKED AT INBOARD AFT CORNER. COMPLIED WITH EC/TC EO 700-57-0065. SUPPLEMEN TAL SDR CLOSED 3/28/08. 2 L 7 2 4F RT A21EA 2008040200198 20080402 00198 NM 2008 4 2 CALA0800281 1 20080329 A 5210 HRSC4CFR6 BEARING BOEING 737 737724 13844BY NM L1 DOOR UNKNOWN A CALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 39728 28944 FWD ENTRY DOOR L-1 VERY DIFFICULT TO OPEN TO THE LOCKED POSITION FULL OPEN. FOUND BEARING BEHIND CAM ASSY REF IPC 52-1 1-51-05 ITEM 290. REPLACED REF CMM 52-16-01 INSTALLED LINING REF AMM 52-11-31. 2 L 7 2 4F RT A16WE 2008040200209 20080402 00209 NM 2008 4 2 SWAA081685 1 20080329 A 3350 MS155721 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 207WN 34012 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008040200224 20080402 00224 NM 2008 4 2 2008UALA01697 1 20080326 A 5330 141W3310 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE BS 400-445 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 798UA 43876 26928 THE EXTERIOR SKIN HAS A CAT "C" BLIND FASTENER REPAIRS AT BS 400, 404, 423, 444 AND 445 AT STR 20L. REPLACED FASTENERS WITH SOLID FASTENERS DURING OVERHAUL VISIT. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040200226 20080402 00226 2008 4 2 SWAA081720 4 20080327 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008040200231 20080402 00231 NM 2008 4 2 SWAA081694 1 20080330 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040200236 20080402 00236 NM 2008 4 2 SWAA081701 1 20080330 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040200246 20080402 00246 NM 2008 4 2 SWAA081696 1 20080330 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040200247 20080402 00247 NM 2008 4 2 2008UALA01715 1 20080326 A 3350 BULB AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE RT OWING LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 848UA 1647 EMERGENCY LIGHTS TEST FAULTS EPSU INT LOAD EMER R 33-51-38. CAUSE, SEVERAL BULBS OUT AT EXIT AREA. RELAMPED ALL BULBS OUT, ALL CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200248 20080402 00248 EU 2008 4 2 SWAA081703 2 20080329 A 7200 CFM567B24 ENGINE BOEING 737 7377H4 1384404 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 FAILED A SWAA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 29 408WN 27895 888538 DECLARED EMERGENCY / INFLIGHT SHUTDOWN / AIR TURNBACK. CLIMBING OUT OF DAL NR 1 ENGINE FAILED. REMOVED AND REPLACED NR 1 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E21EU 2008040200258 20080402 00258 NM 2008 4 2 2008UALA01726 1 20080327 A 2750 FLAP SYSTEM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE TE FLAPS STUCK A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 29 665UA 29237 FLAP HANDLE AT 5, FLAPS LOCKED UP AT 1 EICAS, T/E FLAP DISAGREE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040200263 20080402 00263 SO 2008 4 2 CHQA200800059 1 20080325 A 2760 SPOILER SYS EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL MALFUNCTIONED A CHQA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 11 579RP 145871 CAE311509 CVG TO STL - ON APPROACH TO STL, THE CREW RECEIVED A SPOILER FAIL MESSAGE. THE CREW EXECUTED A GO AROUND AND FOLLOWED T HE APPROPRIATE QRH CHECKLISTS AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE AIRCRAFT POWER AND OPERATED THE SPOILE R SYSTEM WITHOUT DEFECTS AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008040200265 20080402 00265 EU 2008 4 2 08FDEA01162 1 20080327 A 2930 647520181 TRANSMITTER AIRBUS 300 A300F4605R 3930327 EU HYD SYSTEM FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 670FE 777 DURING CLIMB-OUT GOT ECAM YELLOW HYD SYS LOW PRESSURE. OVERHEAD QTY GAUGE INDICATED NO QUANTITY. AFTER LANDING QTY APP EARED NORMAL. COMPLIED WITH ECAM AND REFERRED TO QRH PROCEDURE HYD LOW PRESSURE. OPERATED YELLOW SYS WITH PTU, PRESSUR E WAS 3000 AND QUANTITY WAS IN THE TOP HAT. OPERATED YELLOW ENGINE PUMP WHILE MOVING FLAPS AND ALL OTHER FLT CONTROLS, YELLOW PRESSURE WHILE MOVING CONTROLS DROPPED TO 2300 AT THE LOWEST. CONTINUED TROUBLESHOOTING IN PROGRESS. REMOVED AN D REPLACED YELLOW SYSTEM HYDRAULIC QUANTITY TRANSMITTER. RAN ALL THREE HYD SYSTEMS AND LEAK CHECKED REMAINING FILTER, N O LEAKS NOTED. 2 L 7 2 4F RT A35EU 2008040200279 20080402 00279 NM 2008 4 2 08FDEA01184 1 20080328 A 5315 BAC1518338 FLOORBEAM BOEING 727 727227 1384078 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 MAIN DECK FLOORBEAM BS 1166, RBL 44-50, WEB HAS SEVERAL DOUBLE DRILLED HOLES. REMOVED AND REPLACED. FABRICATED REPAIR P ARTS AT LT AND RT FUEL SHROUD CUT OUTS AND INSTALLED. REFERENCE EA 7-5310-113796. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008040200280 20080402 00280 WP 2008 4 2 08FDEA01185 1 20080328 A 5310 ADA36751 FITTING DOUG DC10 DC1010F 3022111 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION MAIN CARGO DOOR LOWER JAM SUPPORT FITTING AFTER INSPECTION FOUND BORE "C" OF FITTING NR 1 W ITH CORROSION (DIAMETER .456"), REF EO FEDEX 8-5230-117635. PERFORMED REWORK HOLE FOR SRM 53-50-00 FIG 17, PERFORMED ND I AND INSTALLED BUSHING FOR SRM 53-50-00 FIG 17 VOL I. 2 L 7 3 4F A22WE 2008040200301 20080402 00301 NM 2008 4 2 KCSA081186 1 20080320 A 5320 STIFFENER BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 STA-1740 FRAME VERTICAL STIFFENER DAMAGED AT RBL-18. 2 L 7 4 4F RT A20WE 2008040200314 20080402 00314 NM 2008 4 2 KCSA081196 1 20080321 A 5320 STIFFENER BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 STA-1580 FRAME VERTICAL STIFFENER DAMAGED AT RBL-18. 2 L 7 4 4F RT A20WE 2008040200317 20080402 00317 NM 2008 4 2 HALA0800439 1 20080327 A 2910 LINE BOEING 767 767332 1382001 NM HYD SYSTEM LEAKING A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, RUDDER HYD RETURN LINE LEAKING AT FITTING REMOVED LINE. FOUND TO BE "T" FITTING. REINSTALLED RETURN LINE LEAK CK PEND. REPLACED "T" FITTING. REPLENISHED C HYD SYS OPS AND LEAK CK OK. 2 L 7 2 4F RT A1NM 2008040200343 20080402 00343 NM 2008 4 2 KCSA081206 1 20080326 A 5347 SEAT TRACK BOEING 747 747SR46 1384816 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 MAIN DECK SEAT TRACK CORRODED AT BS 1800, LBL-99. 2 L 7 4 4F RT A20WE 2008040900078 20080409 00078 NM 2008 4 9 08FDEA01277 1 20080403 A 5730 ARB74023 ACCESS PANEL DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 06 EACH FASTENER HOLES FOUND WITH CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOO R CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-120550, REPAIR CLASSIFIED AS M INOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008040900079 20080409 00079 NM 2008 4 9 08FDEA01278 1 20080403 A 5730 ARB74024 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 08 EACH FASTENER HOLES FOUND WITH CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RIGHT WING LOWER SKIN ACCESS DO OR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-120551, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008040900081 20080409 00081 EU 2008 4 9 08FDEA01280 1 20080403 A 5340 A53980047210 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND A CLIP AT C 76, P 33-34 LT WITH NOT ENOUGH EDGE DISTANCE. REPAIR PERFORMED BY MANUFACTURING AND INSTALLING OF NEW CLIP IAW RAS/EFW9000026/2008 ISS A, APPROVED BY EA 6-5318-117152. 2 L 7 2 4F RT A35EU 2008040200353 20080402 00353 EU 2008 4 2 2008UALA01736 1 20080327 A 5754 SLAT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 490UA 1728 8 INCH BY 5 INCH BY 1 INCH DEEP DENT TO LEADING EDGE OF LEFT WING NR 1 SLAT. DAMAGE CONTAINED TO AREA 3. REPLACED DAM AGED SLAT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200354 20080402 00354 NM 2008 4 2 2008UALA01737 1 20080327 A 5210 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE L1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 DOOR 1L AFT SIDE SKIN AND FRAME CRACKED AT NR 6 STOP PIN. MAJOR REPAIR: REMOVED DAMAGE. INSTALLED REPAIR PARTS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200355 20080402 00355 NM 2008 4 2 2008UALA01740 1 20080327 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 560 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 FOUND FWD PIT FRAME DENTED AT STA 560 STR 25L. REPAIRED PER REO G 12282 R EV D AND EVA 71349. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040100239 20080401 00239 NM 2008 4 1 ASAA0892777 1 20080307 A 5320 146A750611 FLOOR SUPPORT BOEING 737 737990 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 323AS 30021 AFT CARGO PIT FLOOR SUPPORT SPLICE CORRODED AT STA 727 I RBL 3. REMOVED DAMAGED SPLICE, FABRICATED SPLICE CHANNEL IAW D WG 146A7506 FIG 2. LOCATED DRILLED AND INSTALLED IAW B737 900 SRM 51 40 2 PG 6 ASA EA 5310 02779. 2 L 7 4 4F RT A16WE 2008040100241 20080401 00241 NM 2008 4 1 ASAA0892779 1 20080307 A 5320 146A750614 FLOOR SUPPORT BOEING 737 737990 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 323AS 30021 AFT CARGO PIT FLOOR SUPPORT SPLICE CORRODED AT STA 727 I RBL 13.84. REMOVED DAMAGED SPLICE. FABRICATED SPLICE CHANNEL IAW DWG 146A7506 FIG . 1 LOCATED, DRILLED AND INSTALLED IAW B737 900 SRM 51 40 02 PG 6 ASA EA 5310 02779. 2 L 7 4 4F RT A16WE 2008040100242 20080401 00242 NM 2008 4 1 GTIA0800043 1 20080311 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 502NK 2433 FLOORBEAM AT STAT -Y765 CORRODED BETWEEN FR 66 AND FR 70. REMOVED AND REPLACED FLOORBEAM -Y765 BETWEEN FR 66 AND FR 70 IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008040100245 20080401 00245 2008 4 1 EMB08001 4 20080326 A 3140 70265421901 MODULE EMB ERJ190 ERJ190100IGW 3260408 NM INOPERATIVE A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 949UW 1173 19000102 FLIGHT 1092 - PHL-RDU: CREW RECEIVED EICAS MESSAGE "AVNX MAU 3 FAIL". THE AIRCRAFT RETURNED TO PHL PER THE QRH PROCEDUR E. MAINTENANCE REMOVED AND REPLACED THE NIC/PROC MODULE FIVE. 2 L 7 2 4F RT A57NM 2008040100246 20080401 00246 NM 2008 4 1 GTIA0800041 1 20080311 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 502NK 2433 FLOORBEAM AT STATION Y254 BETWEEN FR 66 AND FR 68 CORRODED. REMOVED AND REPLACED FLOORBEAM AT STATION Y254 BETWEEN FR 6 6 AND FR 68. 2 L 7 2 4F RT A28NM 2008033100149 20080331 00149 EA 2008 3 31 SWIA200819382 1 20080319 A 5210 ROD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 427SW 7497 FLT 3789 - PAX DOOR IS DIFFICULT TO CLOSE. ADJUSTED PAX DOOR LATCH ROD IAW 52-11-21. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008033100176 20080331 00176 NE 2008 3 31 SWIA200819388 2 20080317 A 7230 FAN CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE LT ENGINE OUT OF BALANCE A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 727SK 10191 FLT 6434 - LEFT ENGINE VIBE GAUGE BEGAN TO INCREASE. COMPLIED WITH ENGINE FAN TRIM BALANCE IAW 71-00-00. OPS CHECK GOO D. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008033100178 20080331 00178 NM 2008 3 31 TAMF20080019S 1 20080315 A 5712 RIB BOEING 767 767200 1385120 NM GE CF6 CF680 30025 NE LT WING CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 770QT 23802 CORROSION ON LT WING OB L/E RIB LOWER OUTER CHORD AT STA 441.60. CORRECTIVE ACTION: RIB WAS FABRICATED AND INSTALLED IAW MFG AUTHORIZATION PO214240, DRAWING 114T2200 AND SRM 51-40-02 PG 1-7. 2 L 7 2 4F 4 F RT A1NM E13NE 2008033100184 20080331 00184 WP 2008 3 31 08FDEA01122 1 20080324 A 5340 AFA386611 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 FITTING REQUIRES FABRICATION; FITTING IS CRACKED. FABRICATED FITTING IAW SRM 51-31-01; VOL II & DWG AFA 3866. ALODIN ED & PRIMED IAW SRM 51-21-01; VOL II. INSTALLED ON JOB CARD N00128. 2 L 7 3 4F RT A22WE 2008033100185 20080331 00185 EU 2008 3 31 08FDEA01104 1 20080321 A 5510 A5517740100200 FAIRING AIRBUS 310 A310203 3930313 EU ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT HORIZONTAL STABILIZER FWD APRON IS TORN. REPLACED NEW APRON FAIRING ON N00181. 2 L 7 2 4F RT A35EU 2008033100186 20080331 00186 EA 2008 3 31 SWIA200819393 1 20080320 A 2150 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA RIGHT INOPERATIVE A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 907SW 7511 FLT 6590 - DURING CLIMB-OUT, THE CABIN WOULD NOT PRESSURIZE. REPLACED RIGHT PRSOV PER AMM 21-52-43 AND PRESSURE TRANSDU CER IAW MM 21-51-40. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2008033100202 20080331 00202 NM 2008 3 31 NWAA081216310 1 20080324 A 5311 FRAME BOEING 747 747451 1384940 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING "M" CHECK, FOUND CRACK IN FRAME RT WEB AT BS 1265 S26R. REPAIRED PER EA 63-212257 SECT I. REPETITIVE INSPECTION S TO BE ACCOMPLISHED AT 2000 CYCLE INTERVALS PER SECT II UNTIL SECT III PERMANENT REPAIR IS ACCOMPLISHED. 2 L 7 4 4F RT A20WE 2008033100263 20080331 00263 WP 2008 3 31 DHL2008805502 1 20080318 A 5342 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 84609 46125 CORROSION AT RT VERT STAB TO FUSELAGE JOINT LWR ANGLE, STA 1800.000 L-2R - L-3R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-5 FIG 16A SHEET 1, 2. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P . CUT OUT DAMAGED SECTION IAW SRM 53-2-5 FIG 16A SHEET 1, 2. PERFORMED NDT INSP IAW NDT SPM PART 08-00-02 TO 07. NO C RACK FOUND. ENCLOSED SMN FORM 242-4. FABRICATED ANGLE CRES 17-7PH 0.080") AND FILLER (AL7075T6 0.160") IAW SRM 53-2-5 FIG 16A SHEET 1, 2. HEAT TREATED ANGLE FROM CRES 17-7PH TO CRES 17-7PH (H1050) IAW SRM 51-1-16. CLEANED, TREATED AND P RIMED AREA AND FILLER IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-5 FIG 16A SHEET 1, 2, SRM 51-1-11, SRM 51-1- 2 L 7 4 4F RT 4A25 2008033100270 20080331 00270 NM 2008 3 31 QXEA200800322 1 20080320 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX -C4- SUSPECT CORROSION ON FRAME CASTELLATION AT FRAME X580.5 JUST O/B OF STR 31S. REMOVED RIVETS FROM CASTELLATION AND BLENDED OUT CORROSION REF DHC8/200 CPCM CHAPTER 4. HFEC INSPECTED BLEND AREA FOR CRACKS IAW D 8/200 NDTM, PART 6, 51 -00-01, NO CRACKS NOTED. UT THICKNESS CHECK OF BLENDED AREA IAW -8/200 NDTM PART 1, 51-00-04 HIGH .050 LOW .047. AREA OF BLEND WITHIN LIMITS REF DHC 8 SRM 51-20-11. APPLIED ETCH ALODINE AND PRIMER IAW DHC 8 SRM 51-20-16 AND 51-20-36. REINST ALLED RIVETS IN CASTELLATION REF DHC 8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 2008033100275 20080331 00275 NM 2008 3 31 DL76L080407 1 20080323 A 2797 WIRE BOEING 767 767332 1382001 NM L/E SLAT BROKEN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 197DN 28454 AFTER T/O DURING FLAP RETRACTION, EICAS MESSAGE LE SLAT ASSY WITH TE FLAP INDICATOR BETWEEN 0 AND 1. BITE TEST OF FSEU NR 5 SLAT O/B SENSOR FAULTING FOUND BROKEN RED WIRE AT S280 SPLICE REPAIRED SAME CHECKS GOOD PER AMM. 2 L 7 2 4F RT A1NM 2008040200358 20080402 00358 NM 2008 4 2 2008UALA01743 1 20080328 A 3260 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 595UA 28748 ON APPROACH FLT EXPERIENCED A YELLOW GEAR DOOR WHEN LANDING GEAR WAS LOWERED. WHEELS SHOWED 3 GREEN. ALSO, A YELLOW AU TO SPEEDBRAKE LIGHT WHEN ATTEMPTED TO ARM. FLT EXECUTED A GO AROUND AND CONTACTED DISPATCH. ACCOMPLISHED BITE OF PSEU N O FAULTS NOTED. OPERATED DOORS MANUALLY AND PINNED GEAR AND OPERATED LANDING GEAR HANDLE ALL DOOR AND GEAR INDICATIONS N ORMAL PER MM 32-00-15-201 OPERATED GEAR AND DOOR THROUGH SEVERAL CYCLES ALL INDICATIONS AND DOORS CHECK NORMAL, NO REPEA TS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200363 20080402 00363 NM 2008 4 2 2008UALA01749 1 20080327 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 FOUND EEL STRIP AT SEAT 17B LOOSE AND INOP. REPLACED LIGHT OPS CHECKED OK. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200364 20080402 00364 NM 2008 4 2 2008UALA01750 1 20080327 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN UNSECURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 655UA 25393 EMERGENCY LIGHT STRIP COMING UP AT RT SIDE OF BUS GALLEY AT ROWS 10E-F. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040200371 20080402 00371 NM 2008 4 2 2008UALA01758 1 20080327 A 3350 COVER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN MISSING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 778UA 26940 FOUND EMERGENCY LIGHT AT SEAT 13F LIGHT IS MISSING COVER. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040200372 20080402 00372 NM 2008 4 2 2008UALA01759 1 20080327 A 3150 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 641UA 25091 APU GEN OFF EICAS MSG WITH ASSOC SWITCH LIGHT ILLUMINATED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040200374 20080402 00374 WP 2008 4 2 NWAA081249918 1 20080330 A 3397 WIRE HARNESS DOUG DC9 DC932 3022066 WP CABIN DEFECTIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 940N 47572 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY ESCAPE LIGHT FOR THE AFT MOST POSITION WAS NOT FUNCTIONAL. MAIN TENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM. 2 L 7 2 4F A6WE 2008040200377 20080402 00377 2008 4 2 08FDEA01194 4 20080328 A 3444 A5397355400200 HOUSING AIRBUS 310 A310203 3930313 EU RADIO ALTIMETER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 1 RADIO ALTIMETER TRANSMISSION ANTENNA MOUNT RING HOUSING CAVITY AND DOME NUTS ARE CORRODED. REMOVED AND REPLACED HO USING IAW A310-200 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008040200379 20080402 00379 WP 2008 4 2 08FDEA01196 1 20080328 A 5753 ARC24442 SKIN DOUG MD10 MD1010F 3022112 WP T/E FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT INBD FLAP LOWER SURFACE AT STE XIFH 255 HAS A DENT. DEPTH OF THE DENT IS .225. ORIGINAL THICKNESS OF THE SKIN IS 0.040. OUT OF LIMITS IAW DC/MD-10 SRM 57-00-01; FIG 1A; VOL I. USED DEPTH GAUGE TWS 8358A IAW DC/MD-10 SRM 57-00-01; FIG 1 A; VOL I. REMOVED DAMAGED AREA OF THE SKIN IAW DC/MD-10 SRM 57-00-01; FIG 4; VOL I. FABRICATED REPAIR IAW DC/MD -10 SRM 57-00-01; FIG 4; VOL I. ALODINED IAW DC/MD-10 SRM 51-21-01; VOL II. PRIMED IAW DC/MD-10 SRM 51-21-01; VOL II AND INSTALLED IAW DC/MD-10 SRM 57-00-01; FIG 4. 2 L 7 3 4F RT A22WE 2008040200382 20080402 00382 WP 2008 4 2 08FDEA01199 1 20080328 A 5754 ARB137918 COVER DOUG MD10 MD1010F 3022112 WP L/E SLAT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT WING NR 2 SLAT TRACK COVER FWD END IS CHAFED. REMOVED TRACK COVER IAW SRM 51-31-01; VOL II. FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01; VOL II. MACHINED NR 2 SLAT TRACK COVER IAW DWG ARB 1379; REV G. FORMED SLAT TRACK COVER TO CONTOUR IAW SRM 51-10-00; VOL II. DRILLED UP SLAT TRACK COVER IAW SRM 51-31-01; VOL II. ALODINED & PRIMED IAW SRM 5 1-21-01; VOL II. INSTALLED SLAT TRACK COVER IAW SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 2008040200384 20080402 00384 NM 2008 4 2 08FDEA01202 1 20080329 A 5320 141N51609 CHANNEL BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 U CHANNEL ON MCD, AT STA. 341, WL 208, LBL 21 TO 31 IS CORRODED. REMOVED CORROSION, L=9.2", W= 1.8", D= .008", ORIGINAL MATERIAL THICKNESS .054". FOUND TO BE OUT OF SRM 53-00-51, FIG 101, DETAIL III LIMITS. REMOVED U CHANNEL IAW SRM 51-4 0-02. FABRICATED REPLACEMENT CHANNEL ON MAE TRAVELER NR T7/713524, FROM 7075 -0 .050C HEAT TREATED TO T6. TREATED AND PRIMED CHANNEL IAW SRM 51-20-01. TOP COATED CHANNEL IAW AMM 51-21-00-7. INSTALLED REPLACEMENT U CHANNEL IAW SRM 51-40 -02. THIS IS A CATEGORY "A" MAJOR REPAIR WITH NO RECURRING INSPECTIONS. 2 L 7 2 4F RT A2NM 2008040200387 20080402 00387 EU 2008 4 2 08FDEA01207 1 20080331 A 5713 A573140936290 STRINGER AIRBUS 300 A300B4622R 3930312 EU LT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND VENT TANK CHAFING MARKS AROUND NACA OPENING (INBOARD RIB 28, STRINGER 17A AND REAR STIFFENER) ON LT WING. REPAI R PERFORMED BY REWORK OF CHAFING MARKS AND NDT FOR CRACK FREE IAW RAS/BAE/1006860/2008 ISS A, APPROVED BY EA 6-5720-1171 69. 2 L 7 2 4F RT A35EU 2008040300002 20080403 00002 SW 2008 4 3 02082008203CG 1 20080208 A 2913 206076030101 SHAFT BELL BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL HYD PUMP STRIPPED E E30A A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 11 203CG BMC00639 51025 CAE895108 WHILE ENROUTE, PILOT EXPERIENCED A HYDRAULIC FAILURE. PULLING THE CIRCUIT BREAKER HAD NO EFFECT (SYSTEM IS AUTOMATICALL Y ON WHEN POWER IS REMOVED). PILOT THEN TURNED SWITCH OFF AND PROCEEDED WITH AN UNEVENTFUL LANDING. UPON INSPECTION IT WAS DETERMINED THAT THE SPLINES ON THE HYDRAULIC PUMP AND THE TACH GENERATOR HAD STRIPPED. BOTH PARTS WILL BE REPLACED . 1 G 7 1 3U 3 U H2SW E1GL 2008040300010 20080403 00010 WP 2008 4 3 ABXR080103 1 20080228 A 5230 59101573 SKIN DOUG DC9 DC932F 3022067 WP AFT CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 205US 47690 AFT LOWER CARGO DOOR SKIN CRACKED AT DOOR HANDLE. REPAIRED DOOR IAW DC9 SRM 52-05, FIGURE 30, SHEET 1. 2 L 7 2 4F A6WE 2008040300011 20080403 00011 WP 2008 4 3 ABXR080108 1 20080303 A 5320 49568772 ATTACH ANGLE DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 205US 47690 ATTACH ANGLE FOR STA 41 TO STA 69 PRESSURE PANEL INTERCOSTAL CRACKED JUST RIGHT OF PLUG DOOR. REMOVED AND REPLACED ANGL ES IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2008040300014 20080403 00014 NM 2008 4 3 ABXA080113 1 20080310 A 5312 145T875282 PRESSURE PANEL BOEING 767 767281 1385109 NM RT MLG CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 775AX 22790 RIGHT CANTED PRESSURE DECK IN RIGHT WHEEL WELL HAD APPROXIMATELY 6 INCH CRACK. REPAIRED CANTED PRESSURE DECK IN RIGHT W HEEL WELL IAW B767 SRM. CRACK LENGTHS WERE: 7 AND 3 INCHES. 2 L 7 2 4F RT A1NM 2008040300015 20080403 00015 NM 2008 4 3 ABXA080111 1 20080307 A 5230 140T26033 BEAM BOEING 767 767281 1385109 NM FWD CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 775AX 22790 FORWARD CARGO DOOR BEAM CORRODED JUST BELOW PRESSURE DOORS. REMOVED AND REPLACED BEAM IAW B767 SRM 51-40-2. 2 L 7 2 4F RT A1NM 2008040300019 20080403 00019 NM 2008 4 3 KCSA081218 1 20080331 A 5313 STRINGER BOEING 747 747SR46 1384816 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 STR-48R CORRODED AT BS 1480 ON O/B SIDE. 2 L 7 4 4F RT A20WE 2008040300021 20080403 00021 NM 2008 4 3 KCSA081219 1 20080331 A 5320 FLOOR SUPPORT BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 FLOOR SUPPORT DAMAGED AT STA-2100 RBL-36. 2 L 7 4 4F RT A20WE 2008040300028 20080403 00028 NM 2008 4 3 ABXA080093 1 20080215 A 5330 1148T31111 SKIN BOEING 767 767281 1385109 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 769AX 22787 FUSELAGE SKIN CRACKED AT FASTENERS FS 1654, STRINGER 3 LEFT. REPAIRED FUSELAGE SKIN AT FS 1654 AND STRINGER 3 LEFT IAW B767 SRM 53-80-01, FIGURE 201. 2 L 7 2 4F RT A1NM 2008040300033 20080403 00033 NM 2008 4 3 ABXA080100 1 20080225 A 5315 143T12151 FLOORBEAM BOEING 767 767281 1385109 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 769AX 22787 FLOORBEAM CORRODED AROUND NUT PLATE AT FS 720, UNDER LEFT OUTER ROLLER TRAY. REPAIRED FLOORBEAM IAW SRM. 2 L 7 2 4F RT A1NM 2008040300035 20080403 00035 NM 2008 4 3 ABXA080091 1 20080215 A 5320 141T3330 DOUBLER BOEING 767 767281 1385109 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 769AX 22787 R1 DOOR CUTOUT LOWER AFT CORNER INNER DOUBLER HAD A CRACK INDICATION BOTH SIDES OF MARKED HOLE. REPAIRED AREA IAW REA B 653-57053-MR. 2 L 7 2 4F RT A1NM 2008040300041 20080403 00041 WP 2008 4 3 ABXA080109 1 20080319 A 2740 LIMIT SWITCH DOUG DC9 DC933F 302207A WP TRIM MOTOR FAULTY A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 935AX 47413 OPERATION OF ALTERNATE LONGITUDINAL TRIM SWITCHES CAUSES ONE 5 AMP CIRCUIT BREAKER TO TRIP. ALSO THERE IS A BURNT SMELL PRESENT. VERIFIED BAD ALTERNATE LONGITUDINAL TRIM MOTOR DOWN LIMIT SWITCH. REPLACED LIMIT SWITCH IAW DC9 AMM 27-40-10 -2. 2 L 7 2 4F A6WE 2008040300045 20080403 00045 NM 2008 4 3 KCSA081213 1 20080328 A 5311 FRAME BOEING 747 747SR46 1384816 NM FUSELAGE BENT A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 FRAME BENT AFT OF BULKHEAD 2160 RBL-32. 2 L 7 4 4F RT A20WE 2008040300058 20080403 00058 NM 2008 4 3 KCSA081210 1 20080326 A 5320 STIFFENER BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 STA-1920 BETWEEN STR-34L AND STR-35L FRAME STIFFENER HAS DAMAGED FLANGE. 2 L 7 4 4F RT A20WE 2008040300059 20080403 00059 NM 2008 4 3 KCSA081211 1 20080326 A 5330 SKIN BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 STA-1760 STR-38R SKIN DAMAGED. 2 L 7 4 4F RT A20WE 2008040300066 20080403 00066 NM 2008 4 3 KCSA081209 1 20080326 A 5320 WEB BOEING 747 747122 1384872 NM NLG WW CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 716CK 19753 NOSE WHEEL WELL RT SIDE STA-285 WL-160 WEB CRACKED .75 INCH UNDER BONDED STRAP. 2 L 7 4 4F RT A20WE 2008040300071 20080403 00071 NM 2008 4 3 2008UALA01623 1 20080322 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 350 S16L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FUSELAGE STRINGER 16L TO LOWER AFT DOOR STOP STRAP CRACKED, BS 350. MAJOR REPAIR ACCOMPLISHED: REPLACED STRAP & WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200110 20080402 00110 NM 2008 4 2 BB08042 1 20080321 A 2721 658D1005 ACTUATOR BOEING 757 7572S7 1384962 NM RUDDER INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 905AW 68801 13428 23567 PHX FLT 25 PHX TO HNL - THE RUDDER TRIM FAILED. DECISION WAS MADE TO RETURN TO FIELD PHX, AND LAND WITHOUT FURTHER IN CIDENT. MAINTENANCE REPLACED THE RUDDER TRIM ACTUATOR. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2008040200120 20080402 00120 NM 2008 4 2 2008UALA01622 1 20080321 A 5270 PROXIMITY SWITCH AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE OVERWING DOOR OUT OF ADJUST A UALA O OTHER N FALSE WARNING CL CLIMB 1 WP 29 827UA 1022 AFTER TAKEOFF HAD L OVERWING DOOR ECAM FOR 20 SEC WENT AWAY. PRESSURE FINE BUT FLIGHT ATTENDANT SAYS IT HAS A WIND. CA USE, PROX SWITCH OUT OF ADJUSTMENT AND LANYARD STUCK IN DOOR MECHANISM. ADJUSTED PROX SENSOR AND REPLACED PINCHED LANY ARD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200133 20080402 00133 NM 2008 4 2 CALA0800270 1 20080325 A 5610 58935577 SLIDING WINDOW BOEING 737 7373T0 1384582 NM COCKPIT OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 PILOTS NR 2 SLIDING WINDOW HARD TO CLOSE. ADJUSTED SHIMS ON THE PILOTS LT NR 2 SLIDING WINDOW IAW B737 AMM 56-12-11. 2 L 7 2 4F RT A16WE 2008040100005 20080401 00005 EU 2008 4 1 08FDEA01156 1 20080326 A 5755 A5777020920400 SPOILER AIRBUS 310 A310203 3930313 EU RT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT WING SPOILER NR 5 TRAILING EDGE IS KNIFE EDGES. REMOVED DAMAGED TRAILING EDGE IAW A310 SRM 51-40-02. LOCATED; DR ILLED; DEBURRED AND INSTALLED NEW TRAILING EDGE P/N A5777020920400 IAW A310 SRM 51-40-02. 2 L 7 2 4F RT A35EU 2008040100008 20080401 00008 EU 2008 4 1 08FDEA01159 1 20080327 A 5347 6022457 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 658FE 752 MDCC SEAT TRACK NR 1 HAS 1 EA GOUGED SCALLOP BETWEEN FRAMES 48 AND 49 ACCOMPLISHED SEAT TRACK REPAIR IAW A300-600 SRM 53 -10-16,FIG 201 2 L 7 2 4F RT A35EU 2008040100029 20080401 00029 NM 2008 4 1 UIEA200800072 1 20080313 A 5347 SEAT TRACK BOEING 747 747341 13848AM NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 MAIN DECK STA 1640 TO 1690 LBL 33 SEAT TRACK HAS LEVEL 1 CORROSION. CORROSION REMOVED AND TREATED IAW SRM 51-10-01. 2 L 7 4 4F RT A20WE 2008040100045 20080401 00045 EU 2008 4 1 USAA920080646 1 20080319 A 8010 D9550011500195 PANEL AIRBUS 320 A320231 3930325 EU COCKPIT DEFECTIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 625AW 64 FLT NR 540 - PHX-DFW - AIR TURNBACK - RETURNED TO GATE FOR START FAULT IGNITION B NR 2 ENGINE WITH IGNITION B NR 1 ENGIN E ALREADY ON MEL. ACCOMPLISHED MANUAL START PER MX CONTROL AND AIRCRAFT DEPARTED. IGNITION CIRCUIT BREAKERS P-39 THROU GH P-42 POPPED AFTER TAKEOFF. AIRCRAFT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED THE ENGINE START PANEL. 2 L 7 2 4F RT A28NM 2008040100049 20080401 00049 NM 2008 4 1 USAA920080647 1 20080320 A 5313 6546877144 STRINGER BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - CRACKED STRINGER, BS 727, S18A RIGHT. REPAIRED STRINGER, BS 727, S18A RIGHT IAW USAIRW AYS EA 100279. 2 L 7 2 4F RT A16WE 2008040100088 20080401 00088 NM 2008 4 1 USAA920080672 1 20080321 A 5310 6547960 DOOR FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 CLT - MAJOR REPAIR - B4 CHECK - AFT CARGO COMPARTMENT DOOR CUT OUT AFT FRAME CRACKED, BS 847, S21R. REPAIRED AFT CARGO COMPARTMENT DOOR CUT OUT AFT FRAME, BS 847, S21R - S24R IAW USAIRWAYS EA 100315 2 L 7 2 4F RT A16WE 2008040100098 20080401 00098 NM 2008 4 1 USAA920080677 1 20080308 A 5754 114N4078 PANEL BOEING 757 7572G7 1384963 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 908AW 24233 MCN - MAJOR REPAIR - C3 CHECK - RIGHT WING NR 10 SLAT COVE PANEL CRACKED, OSS 737 - OSS 749. REPLACED RIGHT WING NR 10 SLAT COVE PANEL, OSS 737 - OSS 749 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008040100108 20080401 00108 2008 4 1 COEA0801702 4 20080314 A 3421 2593996444 GYRO FOKKER F27 F27MK600 4990706 EU RROYCE DART DART5327R 54509 NE LT COMPASS FAILED A COEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 13 702FE 10350 RETURN TO BLOCKS. FLIGHT NR 7276 ITC TO AFW. WHILE PREPAIRING FOR DEPARTURE THE CREW DISCOVERED THE CAPT HEADING AND S ITUATION INDICATOR (HSI) COMPASS CARD WAS SPINNING ERRATICALLY. THE CREW REQUESTED TO RETURN TO THE RAMP, UPON WHICH TI ME THE HSI COMPASS CARD HAD SEIZED. LT DIRECTIONAL GYRO WAS REPLACED. (K) 2 H 7 2 4T 4 T A817 E297 2008040100125 20080401 00125 NM 2008 4 1 USAA920080690 1 20080313 A 5340 69374112 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C-18 CHECK - STRINGER CLIP CRACKED AT FUSELAGE FRAME IN MAIN CABIN, BS 277. REPLACED STRINGER CLIP AT FUSELAGE FRAME IN MAIN CABIN, BS 277 AND S15R IAW BOEING SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008040100141 20080401 00141 NM 2008 4 1 ASAA0842722 1 20080304 A 5754 65C26602311A SKIN BOEING 737 737490 1384715 NM L/E SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 NR 2 SLAT OUTBD UPPER CORNER DELAMINATED NR 2 SLAT O/B UPPER CORNER DELAMINATION. REPAIRED IAW B737 400 SRM 51 70 10 RE PAIR 4. 2 L 7 2 4F RT A16WE 2008040100167 20080401 00167 EU 2008 4 1 UPS08151910 1 20080307 A 2597 CONNECTOR AIRBUS A300 A300F4622R 3930360 EU EVAC SLIDE DIRTY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 136UP 0819 INSPECTION TYPE:1C ESCAPE SLIDE RELEASE WARNING FAILED OP CHECK, EMERGENCY EXIT LIGHT INTERMITTENT. TROUBLESHOT TO PINS "C" AND "F", CLEANED CONNECTOR, PINS, OP CHECKED ESCAPE SLIDE RELEASE WARNING, OP CHECKED GOOD, EMERGENCY EXIT LIGHT AL SO CHECKS GOOD PER A300 MM 52-73-00. 2 L 7 2 4F RT A35EU 2008040100171 20080401 00171 WP 2008 4 1 MWEA080044 1 20080322 A 5230 591014167 PAN DOUG DC9 DC981 3022081 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 804ME 48030 CENTER CARGO DOOR OUTER PAN HAS A .75 INCH CRACK IN PAN RADIUS AT THE FORWARD END OF DOOR, INLINE WITH BEAM NR 1. FABRI CATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 2008040100174 20080401 00174 NM 2008 4 1 ASAA0892769 1 20080307 A 5320 146A750129 FLOOR SUPPORT BOEING 737 737990 NM BS 772-887 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 323AS 30021 AFT CARGO PIT FLOOR SUPPORT CORRODED STA 800 AREA RBL 13 CUT OUT DAMAGED SECTION OF FLOOR TRACK LOCATED. FABRICATED DRI LLED AND INSTALLED A REPLACEMENT FLOOR TRACK AND SPLICE CHANNELS IAW SRM 53 00 53 VIA ASA EA 5310 02777. 2 L 7 4 4F RT A16WE 2008040100189 20080401 00189 EU 2008 4 1 TRAX200800463 1 20080322 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 642AS 395 LOWER EMERGENCY EXIT LIGHT JUST FORWARD OF SERVICE DOOR INOP. 2 H 7 2 4T RT 2008040100190 20080401 00190 WP 2008 4 1 UPS08851925 1 20080325 A 5523 5644420507 ATTACH FITTING DOUG DC8 DC871F 302199D WP LT ELEVATOR TAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:N/A LEFT ELEV OUTBOARD TAB INBOARD ATTACH FITTING CRACKED. A/C OOS. REMOVED AND REPLACED LT ELEVATOR A SSY PER AMM 27-30-01-4. 2 L 7 4 4F RT 4A25 2008040200147 20080402 00147 NM 2008 4 2 2008UALA01644 1 20080324 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 FOUND EMERGENCY EXIT LIGHT INOP, AT DOOR 5 LEFT FWD SILL LIGHT. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200164 20080402 00164 EA 2008 4 2 TRAX200800474 1 20080326 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 CLIP AT FS 280 I/B OF RBL 9.0 CRACKED. REMOVED CRACKED CLIP AT FS280 IB OF RBL 9 AND FABRICATED -5 CLIP AS REF IN REO 601R-53-11-171 REV D AND INSTALLED FABRICATED CLIP AT FS 280 IB OF RBL 9 PER CRJ SRM 51-42-21 2 L 7 2 4F RT A21EA 2008040200176 20080402 00176 EA 2008 4 2 TRAX200800458 1 20080321 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 355CA 10067 FLOOR SEAT RAIL IS CORRODED AT FS 364.00, RBL 9. DRILLED, REMOVED AND REPLACED SEAT FLOOR RAIL AT FS 364.00 RBL 9 SRM 5 1-41-00 CRJ 700. JOB COMPLETED. SUPPLEMENTAL SDR CLOSED 3/28/08. 2 L 7 2 4F RT A21EA 2008040200199 20080402 00199 NM 2008 4 2 2008UALA01684 1 20080321 A 3510 OXYGEN SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED OXYGEN SYSTEM 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200229 20080402 00229 NM 2008 4 2 SWAA081693 1 20080330 A 5720 65C26503 STIFFENER BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND LT WING VERTICAL STIFFENER CRACKED AT RIB WBL 542. REPAIRED STIFFENER PER ER. 2 L 7 2 4F RT A16WE 2008040200249 20080402 00249 NM 2008 4 2 2008UALA01717 1 20080327 A 3350 POWER SUPPLY BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 906UA 25006 FLOOR EEL LIGHTS INOP FROM ROW 15 TO AFT GALLEY. REPLACED WET POWER FEEDER. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050500121 20080505 00121 NM 2008 5 5 08FDEA01593 1 20080425 A 5320 65175186 ANGLE BOEING 727 7272S2F 1384O81 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 VENTRAL STAIRWELL RT SIDE BELOW AIRSTAIR ACTUATOR FITTING, TORQUE BOX BS 1263 UPPER ANGLE AFT SIDE OF BULKHEAD HAS CRACK . REMOVED UPPER ANGLE AFT SIDE IAW SRM 51-30-2. REMOVED WEB DOUBLER AND SEAL AND SEAL RETAINER FOR ACCESS IAW SRM 51-30 -2. CUT OUT WEB DIM 29" X 25" FOR ACCESS IAW SRM 51-10-1. LOCATED AND DRILLED NEW ANGLE IAW SRM 51-30-5. INSTALLED NEW A NGLE IAW SRM 51-20-0. FABRICATED NEW WEB IAW 51-20-01 AND 53-10-02. TREATED AND PRIMED NEW WEB IAW SRM 51-10-2. WEB INST ALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008040200261 20080402 00261 NM 2008 4 2 SA08016 1 20080321 A 3260 666000077 PROXIMITY SWITCH AIRBUS A319 A319132 3930340 NM MLG DOORS FAULTED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 803AW 0931 LAS - FLT 268 - YYZ TO LAS - AFTER TAKEOFF, RECEIVED ECAM MESSAGE "L/G DOORS NOT LOCKED". CREW RECYCLED THE GEAR AND RE CEIVED A SATISFACTORY INDICATION. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED PROXIMITY SENSOR FIN 23GA. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2008040200320 20080402 00320 NM 2008 4 2 QXEA20080033 1 20080320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - C4- LT INBD SEAT TRACK NR 4 HAS SEVERAL AREAS OF CORROSION AT STA X209, X228, X240, X250, X268. REMOVED SEAT TRAC K AND INSTALL NEW SEAT TRACK IAW DHC 8 (200) SRM 51-40-00 AND 51-40-11. 2 H 7 2 4T RT A13NM 2008040200326 20080402 00326 NM 2008 4 2 KCSA081201 1 20080324 A 5320 TENSION TIE BOEING 747 747SR46 1384816 NM FUSELAGE BROKEN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 FUSELAGE FRAME TENSION TIE BROKEN BETWEEN BS 1840 AND 1860 ABOVE STR-36L. 2 L 7 4 4F RT A20WE 2008040200334 20080402 00334 EA 2008 4 2 TRAX200800436 1 20080319 A 5342 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 355CA 10067 SUSPECTED CRACK AT LEFT SIDE BASE OF VERTICAL STAB AT FS 1181. WORK COMPLETED IN ACCORDANCE WITH: PERFORMED EDDY CURRE NT INSPECTION OF LEFT SIDE OF BASE OF VERTICAL STAB AT FS 1181 PER CRJ700 NDTM 51-20-006. AREA IS CONFIRMED CRACKED AND MARKED. 03/19/08 VTJ7010159. REMOVED OLD ANGLE AND DRILLED UP NEW ANGLE P/N AV670-21186-003 PER CRJ 700 SRM 51-42-13, 51-42-21, AND 51-42-22. BAT 7023167. INSTALLED DRAG ANGLE LOCATED ON LT SIDE OF VERTICAL STAB AT FS 1181 PER DWG NO P LBA 670-35002. APPLIED FAYING SEAL AND AO23 FINISH PER CRJ 700 SRM 51-23-00 AND 51-25-01. SM17032 JOB COMPLETE. SUPPL EMENTAL SDR CLOSED 3/31/08. 2 L 7 2 4F RT A21EA 2008040200380 20080402 00380 WP 2008 4 2 08FDEA01197 1 20080328 A 5522 NLC6041503 WEDGE DOUG MD10 MD1010F 3022112 WP LT ELEVATOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LEFT OUTBD ELEVATOR T/E WEDGE IS DISBONDED AND CRACKED. REPAIRED T/E WEDGE IAW DC/MD-10 SRM 55-30-00; FIG 1; VOL I. 2 L 7 3 4F RT A22WE 2008040200386 20080402 00386 NM 2008 4 2 08FDEA01205 1 20080329 A 5320 140N205420 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 906FD 27148 MCD FLOOR SUPPORT HAS CORROSION, STA 1660-1681, RBL1, WL 208. REMOVED CORROSION, L= 2", W= .75", D= .010", ORIGINAL MAT ERIAL THICKNESS .050" FOUND TO BE OUT OF SRM 53-00-51, FIG 101, DETAIL III LIMITS. REMOVED FLOOR SUPPORT CHANNEL IAW SR M 51-40-02. FABRICATED REPLACEMENT CHANNEL ON MAE TRAVELER NR T8/732409, FROM 7075-0 .050B, HEAT TREATED TO T6. INSTAL LED REPLACEMENT CHANNEL IAW SRM 51-40-02. THIS IS A CATEGORY "A", MINOR REPAIR WITH NO RECURRING INSPECTIONS. 2 L 7 2 4F RT A2NM 2008040300003 20080403 00003 SW 2008 4 3 2008F00003 1 20080215 A 5310 53116382005 WINDOW FRAME ECLIPS EA500 ECLIPSEEA500 3350000 SW COCKPIT DAMAGED B K NONE O OTHER IN INSP/MAINT 1 SO 16 152DJ 90 90 000062 PART WAS DAMAGED IN MAINTENANCE, DURING WINDSHIELD REPLACEMENT 1 L 7 2 4J RT A00002AC 2008040300004 20080403 00004 NM 2008 4 3 ABXA080110 1 20080319 A 3350 3017701 LIGHT BOEING 767 767281 1385109 NM CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 796AX 23146 MAINTENANCE AT ILN FOUND MAIN ENTRY DOOR EMERGENCY ESCAPE LIGHT LENS CRACKED AND LIGHT INOP. REMOVED AND REPLACED MAIN ENTRY DOOR EMERGENCY ESCAPE LIGHT ASSEMBLY IAW B767 AMM 33-51-06-2. 2 L 7 2 4F RT A1NM 2008040300006 20080403 00006 WP 2008 4 3 ABXR080106 1 20080303 A 5420 995816110 FITTING DOUG DC9 DC932F 3022067 WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 205US 47690 PYLON UPPER REAR SPAR STRAP CLIP JUST INSIDE PYLON CRACKED. REMOVED, FABRICATED, AND INSTALLED NEW CLIP IAW DC9 SRM 51- 30-1 AND 51-30-5. 2 L 7 2 4F A6WE 2008040300024 20080403 00024 WP 2008 4 3 ABXA080089 1 20080307 A 5330 59114103 SKIN DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 976AX 47596 DURING LINE MAINTENANCE, FOUND CORROSION OF FUSELAGE SKIN AROUND THE LEFT STATIC PORT PLATE. REMOVED LEFT STATIC PORT P LATE, FOUND FUSELAGE SKIN UNDER THE PLATE CORRODED BEYOND LIMITS. REPAIRED SKIN IAW DC9 SRM 53-04, FIGURE 31, SHEET 1. 2 L 7 2 4F A6WE 2008040300034 20080403 00034 NM 2008 4 3 ABXA080090 1 20080304 A 5420 313T3380173 ATTACH ANGLE BOEING 767 767281 1385109 NM NR 1 NACELLE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 788AX 23021 INBOARD ATTACH ANGLE FOR PANEL 437DB HAD APPROXIMATELY 3 INCH CRACK NEAR BOTTOM. REMOVED AND REPLACED CRACKED ATTACH PA RT IAW B767 SRM 51-40-2. 2 L 7 2 4F RT A1NM 2008040300060 20080403 00060 SW 2008 4 3 EGRR118893 1 20080212 A 2551 412140100 MOUNT BELL 412 412EP 1182205 SW PWA PT6 PT6* 52043 EA FUSELAGE SHEARED B EGRR K NONE O OTHER IN INSP/MAINT 1 EA 17 22PP 36219 DURING ROUTINE INSPECTION OF EXTERNAL HOIST NOTED BOLT PN NAS6204-54 SHEARED AT HEAD. THIS IS ONE OF THE (2) BOLTS SECUR ING THE HOIST ASSEMBLY TO THE HOIST SUPPORT ASSEMBLY. PERFORMED INSPECTION OF THE SECOND BOLT AND NOTED NO DEFECTS. REP LACED BOTH BOLTS WITH NEW PN NAS6204-54 BOLTS. INSTALLED BOLTS IAW INSTRUCTIONS FOR CONTINUED AIRWORTHINESS REPORT NR AA -02015. 1 G 7 2 4U 3 T H4SW E2NE 2008040300068 20080403 00068 NM 2008 4 3 200800303 1 20080317 A 5330 SKIN BOEING 747 747SPB5 1384813 NM FUSELAGE SCRATCHED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 708BA 22484 SCRIBE LINES IN FUSELAGE SKIN LOWER LEFT SIDE AFT WING TO BODY FAIRING AREA BS 1790 TO 1860 STRING 34L TO 51L APPROX DEP TH IS .002 BS 1840 STRINGER 39L. BLENDED OUT SCRIBE LINES, MATERIAL LOSS IS .002 WITHIN LIMITS, ALODINED AND PRIMED ARE A PER B747 SP SRM'S 51-10-01 PG 13-15, 53-31-00 PG 1-4, 51-10-02 PG 6-6B AND BSOPM 20-44-04 PG 1-4. 2 L 7 4 4F RT A20WE 2008040300075 20080403 00075 NM 2008 4 3 2008UALA01642 1 20080324 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT LIGHT INOP, UPPER DECK CEILING BETWEEN ROW 15 AND 16. RELAMPED. OPS CHKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040300076 20080403 00076 NM 2008 4 3 2008UALA01643 1 20080324 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 FOUND EMERGENCY EXIT EEL LIGHT INOP AT SEAT 58 LEFT. REPLACED LAMP ASSY. OPS CHKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040300077 20080403 00077 NM 2008 4 3 2008UALA01645 1 20080324 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 5A FWD LIGHT ASSY. REPLACED LAMP ASSY. OPS CHKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040300082 20080403 00082 NM 2008 4 3 200800310 1 20080317 A 5330 SKIN BOEING 747 747SPB5 1384813 NM FUSELAGE SCRATCHED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 708BA 22484 SCRIBE LINES IN FUSELAGE SKIN UPPER LEFT SIDE AFT WING TO BODY FAIRING AREA BS 1480 TO 1860 STRINGER 23L TO 34L APPROX D EPTH IS .003 BS 1820 STRINGER 32L. BLENDED OUT SCRIBE LINES, MATERIAL LOSS IS .003 WITHIN LIMITS, ALODINED AND PRIMED A REA PER B747 SP SRM'S 51-10-01 PG 13-15, 53-31-00 PG 6-6B AND BSOPM 20-44-04 PG 1-4. 2 L 7 4 4F RT A20WE 2008040300083 20080403 00083 NM 2008 4 3 2008UALA01689 1 20080326 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 4E INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 FOUND SEAT 4E, AFT EEL LIGHT IN INOPERATIVE. RELAMPED. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040300099 20080403 00099 EA 2008 4 3 COMA0860180 1 20080319 A 3020 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYSTEMM MALFUNCTIONED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 973CA 7146 ABORTED TAKE-OFF FOR ANTI-ICE MESSAGE. RETURNED TO GATE WITHOUT INCIDENT. INSPECTED 14TH STAGE DUCTS AND LOOPS, PERFOR MED OPS CHECK OF ANTI-ICE CONTROL AND INDICATION. NO WARNING OBSERVED. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008040300102 20080403 00102 EA 2008 4 3 COMA0860183 1 20080319 A 3020 53990001 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYSTEM FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 01 455CA 2968 7592 FLIGHT 5681- RIGHT COWL ANTI-ICE CAUTION MESSAGE RECEIVED. RETURNED TO CVG, LANDED WITHOUT INCIDENT. REPLACED RIGHT EN GINE ANTI-ICE VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008040300103 20080403 00103 EA 2008 4 3 COMA0880004 1 20080322 A 3241 90004433 CONTROL UNIT CNDAIR CL600 CL6002D24 1390016 EA ANTI-SKID SYS FAULTY A COMA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 01 676CA 1190 15127 FLIGHT 5105- RECEIVED BRAKE OVERHEAT MESSAGE ON TAKE-OFF ROLL. ABORTED TAKE-OFF, RETURNED TO GATE WITHOUT INCIDENT. RE PLACED ANTI-SKID CONTROL UNIT. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008040300105 20080403 00105 EA 2008 4 3 COMA0860185 1 20080320 A 3020 22856480801 RELIEF VALVE CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYSTEM FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 965CA 7131 FLIGHT 5103- RECEIVED RIGHT COWL ANTI-ICE MESSAGE WHEN ANTI-ICE SELECTED ON. RETURNED TO JFK, LANDED WITHOUT INCIDENT. REPLACED PRESSURE RELIEF VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008040300106 20080403 00106 WP 2008 4 3 IXXA08SMN072S 1 20080214 A 5522 SKIN DOUG DC8 DC871F 302199D WP LT ELEVATOR SCRATCHED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR UPPER SKIN SHOWS SCRATCHES AT STATION XE 273.000 TO STATION XE 28 3.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, FINGER DOUBLER. BON DED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. BALANCED AND FOUND TO BE WITHIN LIM ITS, MOMENT: 1473.4 INCH-POUND. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, DC8 SRM 51-1-21, DC8 SRM 55-4-1 FIGURE 1 SHEET 1 AND 2 ITEM "E" AND "F", DC8 SRM 55-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 51-1-9 T/R 51-142, DC8 S RM 51-1-9A T/R 51-141, DC8 SRM 51-1-8B, AND DC8 SRM 51-4-4 PAGE 1-3. 2 L 7 4 4F RT 4A25 2008040300130 20080403 00130 WP 2008 4 3 NWAA081289876 1 20080329 A 2150 HOSE DOUG DC9 DC951 3022051 WP ACM SEPARATED A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 785NC 23094 4634 48110 THE FLIGHT ATTENDANT REPORTED A THIN HAZE OF SMOKE AND A BURNING RUBBER SMELL IN THE CABIN. FLIGHT CREW NOTED THE SAME IN THE COCKPIT. THE SMOKE QUICKLY DISSIPATED SO THE FLIGHT CONTINUED TO SCHEDULED DESTINATION. LANDING AT DTW WAS NORM AL AND PASSENGERS DEPLANED NORMALLY. MAINTENANCE FOUND THE LEFT AIR CYCLE MACHINE COMPRESSOR INLET HOSE SEPARATED FROM CONNECTOR. NEW CLAMP AND HOSE INSTALLED, LEAK CHECK, ENGINE INSPECTION, AND ACM INSPECTION ALL LOOKED GOOD. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008040300138 20080403 00138 EA 2008 4 3 SWIA200819400 1 20080329 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 412SW 7101 FLT 5806 - PAX DOOR WAS DIFFICULT TO OPEN. LUBED MAIN CABIN DOOR HANDLE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008040300139 20080403 00139 EA 2008 4 3 SWIA200819401 1 20080328 A 5753 601R146992 FLAP CNDAIR CL600 CL6002B19 1900309 EA RT WING DAMAGED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 454SW 9 9 7749 FLT 3773 - OUTBOARD, RIGHT FLAP WAS DAMAGED BY BIRD STRIKE. REPLACED RIGHT, OUTBOARD FLAP IAW MM 27-54-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008040300140 20080403 00140 EA 2008 4 3 SWIA200819402 1 20080330 A 5751 AILERON CNDAIR CL600 CL6002B19 1900309 EA RT WING DAMAGED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 862AS 7476 FLT 3903 - AILERON DAMAGE FOUND ON THE RIGHT SIDE. REPLACED RIGHT AILERON ASSEMBLY IAW CRJ 200 MM 27-15-01, PN: CC670-1 3000-2, SN OFF: SBRJ364. 2 L 7 2 4F RT A21EA 2008040300141 20080403 00141 SO 2008 4 3 SWIA200819403 1 20080328 A 3350 SIGN EMB 120 EMB120ER 3260203 SO CABIN MISSING A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 232SW 120306 PAX DOOR EMERGENCY EXIT SIGN IS MISSING. INSTALLED SERVICEABLE EXIT SIGN. 2 L 7 2 4T RT A31SO 2008040300143 20080403 00143 2008 4 3 HALA0800440 4 20080328 A 2565 101651303 SLIDE BOEING 767 7673CB 1385187 NM R4 DOOR DEPLOYED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 590HA 33467 R4 DOOR SLID ACTIVATED AND BLOWN. REMOVED AND REPLACED R4 DOOR SLID PER AMM 25-66-01-404-036. 2 L 7 2 4F RT A1NM 2008040300145 20080403 00145 NM 2008 4 3 HALA0800442 1 20080330 A 2730 CONTROL CABLE BOEING 717 717200 1383700 NM ELEVATOR BROKEN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 487HA 55132 DUAL ELEVATOR SERVO FOLLOW UP CABLE BROKEN. FABRICATED ELEVATOR SERVO CABLE 207B PER AMM 91-10-02. INSTALLED ELEVATOR SERVO CABLE AND RIG PER AMM 27-30-00, OPERATIONAL CHECK OK. 2 L 7 2 4F TR A6WE 2008040300150 20080403 00150 NM 2008 4 3 HALA0800448 1 20080329 A 4920 APU BOEING 767 76733A 1385209 NM MALFUNCTIONED A HALA K NONE O OTHER TX TAXI/GRND HDL 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, APU FAILED TO START ON 3 ATTEMPTS AFTER LANDING. BITE CHECK ACCOMPLISHED PER FIM 49-11-00 FIG 103. STARTED 2 TIMES SUCCESSFULLY. NO FAULT NOTED. OK FOR SVC. 2 L 7 2 4F RT A1NM 2008040300151 20080403 00151 NM 2008 4 3 HALA0800449 1 20080330 A 2150 WARNING SYSTEM BOEING 717 717200 1383700 NM COCKPIT MALFUNCTIONED A HALA K NONE N FALSE WARNING CR CRUISE 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM, PRIOR TO DESCENT LT PACK INOP LIGHT ILLUMINATED, WENT TO STBY LT OUT. DID A BITE CHECK ON THE LEFT PACK TEMP CONTROLLER. LIGHT WENT OUT. OPS CKS NML PER AMM 21-61-00 AND FIM 21-51-00-101 FIG 103. 2 L 7 2 4F TR A6WE 2008040300156 20080403 00156 EA 2008 4 3 SWIA200819408 1 20080330 A 2913 6619005 PUMP CNDAIR CL600 CL6002C10 1390015 EA HYDRAULIC SYSTEM LEAKING A SWIA O OTHER K FLUID LOSS UK UNKNOWN 1 NM 07 753SK 10214 FLT 6428 - HYDRAULIC SYSTEM 1 QUANTITY FELL TO ZERO. REPLACED EDP IAW 29-11-01. OPS AND LEAK CHECK GOOD, P/N: 66190-05 , S/N OFF: K0722. 2 L 7 2 4F RT A21EA 2008040300158 20080403 00158 EA 2008 4 3 SWIA200819410 1 20080325 A 3350 STRIP CNDAIR CL600 CL6002C10 1390015 EA CABIN DAMAGED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 703SK 10139 FLT 5911 - FORWARD EMERGENCY LIGHT STRIP IS DAMAGED. REPLACED LIGHT STRIP IAW 33-31-01. 2 L 7 2 4F RT A21EA 2008040300176 20080403 00176 2008 4 3 HALA0800453 4 20080329 A 2310 HF COMM BOEING 767 767332 1382001 NM COCKPIT MALFUNCTIONED A HALA K NONE O OTHER CR CRUISE 1 WP 13 596HA 23276 ETOPS SIGNIFICANT SYSTEM, HF RADIO NR 2 UNABLE TO TRANSMIT. ACCOMPLISHED BITE ON NR 2 HF IAW DAL FIM 23-11-00, FIG 103. NO FAULT SHOWN, PER BIK NR 8 THE SYSTEM IS OK. 2 L 7 2 4F RT A1NM 2008040300181 20080403 00181 NM 2008 4 3 HALA0800459 1 20080327 A 5730 SKIN BOEING 767 767332 1382001 NM RT WING CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 CORROSION ON RIGHT WING LOWER SURFACE AT STRINGER L-15 AT WS 426. REWORKED IAW SRM 51-10-02. 2 L 7 2 4F RT A1NM 2008040300188 20080403 00188 NM 2008 4 3 HALA0800466 1 20080327 A 5720 SKATE ANGLE BOEING 767 767332 1382001 NM LT WING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 CRACK ON LT PYLON/WING, OUTBD SKATE ANGLE FWD EDGE,CRACK AT ATTACH FASTENER. REPAIR CARRIED OUT IAW SB 767-57-0023. 2 L 7 2 4F RT A1NM 2008040300189 20080403 00189 NM 2008 4 3 HALA0800467 1 20080327 A 5420 BRACKET BOEING 767 767332 1382001 NM RT NACELLE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 RT ENGINE RT COWL SKIRT PANEL, BRACKET CRACKED. SPLICED PLATE FABRICATED IAW BOEING DRAWING 311T1570-94, INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008040300191 20080403 00191 NM 2008 4 3 HALA0800469 1 20080327 A 5420 BRACKET BOEING 767 767332 1382001 NM RT NACELLE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 RT ENGINE RT COWL SKIRT PANEL, BRACKET CRACKED. SPLICED PLATE FABRICATE IAW BOEING DRAWING 311T1570-94, INSTALLED IAW S RM 51-40-02. 2 L 7 2 4F RT A1NM 2008040100212 20080401 00212 NM 2008 4 1 SWAA081681 1 20080327 A 5311 6546558 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040100221 20080401 00221 2008 4 1 SWAA081704 4 20080327 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 422WN 29826 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008040100224 20080401 00224 NM 2008 4 1 SWAA081725 1 20080330 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008040100267 20080401 00267 NM 2008 4 1 ASAA0842748 1 20080307 A 5320 65C335831 WEB BOEING 737 737490 1384715 NM BS 986-1016 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 AFT CABIN WEB 2 STA 986 5 1016 RBL 32 47 WL 207.5 DAMAGED, REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008040100270 20080401 00270 NM 2008 4 1 SWAA081614 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040100271 20080401 00271 NM 2008 4 1 SWAA081613 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040100277 20080401 00277 NM 2008 4 1 ASAA0842750 1 20080307 A 5320 65C3184768 FLOOR SUPPORT BOEING 737 737490 1384715 NM BS 1006-1016 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 FLOOR SUPPORT AT STA 1006 1016 RBL 37 WL 207.5 GOUGED, REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008040100278 20080401 00278 NM 2008 4 1 SWAA081638 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040100281 20080401 00281 NM 2008 4 1 SWAA081598 1 20080325 A 3350 6556633 SIGN BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM. 2 L 7 2 4F RT A16WE 2008040100282 20080401 00282 NM 2008 4 1 SWAA081664 1 20080326 A 5313 6551698 STRINGER SPLICE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2008040100283 20080401 00283 NM 2008 4 1 SWAA081665 1 20080326 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040100287 20080401 00287 NM 2008 4 1 SWAA081706 1 20080330 A 3350 3071BPEGPL LIGHT BOEING 737 73776Q 13845AA NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 551WN 30280 DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008040100295 20080401 00295 NM 2008 4 1 SWAA081707 1 20080330 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040100297 20080401 00297 NM 2008 4 1 ASAA0842751 1 20080307 A 5320 6545855125 WEB BOEING 737 737490 1384715 NM BS 986-992 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 AFT CABIN WEB AT STA 986.5 992 RBL 47 52 WL 207.5 HAS CORROSION, REPLACED WITH MADE REPAIR PART. 2 L 7 2 4F RT A16WE 2008040100299 20080401 00299 EU 2008 4 1 MALA080049 1 20080327 A 5260 TRACK SAAB SF340 340B 7860101 EU AIRSTAIR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 457XJ 340B457 AIRSTAIRS TRACK CORRODED. AIRSTAIR TRACK REMOVED AND NEW TRACK INSTALLED IAW SRM 51-40-21 AND 51-40-27, P/N 7253710-871 . 2 L 7 2 4T RT A52EU 2008040100303 20080401 00303 NM 2008 4 1 ASAA0872798 1 20080317 A 5320 146A81271 SHIELD BOEING 737 737790 13844CN NM BS 767-787 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 607AS 29751 AFT CARGO PIT STA 767-787 AT STR 25R FLOOR SHIELD HAS CORROSION AT FASTENERS HOLES. AFT CARGO PIT SHIELD REPLACED IAW D RWG 146A0081 AND SRM 53-60 15 AND 51 40 02. 2 L 7 2 4F RT A16WE 2008040100304 20080401 00304 NM 2008 4 1 SWAA081715 1 20080328 A 3350 8200048801 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 704SW 27838 LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008040200002 20080402 00002 NM 2008 4 2 SWAA081529 1 20080319 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, RBL 11 TO RBL 13. REMOVED AND REPLACED SHEAR TIE PER S RM. 2 L 7 2 4F RT A16WE 2008040200004 20080402 00004 NM 2008 4 2 CALA0800243 1 20080321 A 5320 6916970501 ATTACH FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 CLIP ON FORWARD END BOTTOM SIDE OF INTERCOSTAL AT STA 15L THAT ATTACHES INTERCOSTAL TO 348.2 FRAME HAS .875 INCH CRACK I N RADIUS AT I/B END. REMOVED AND REPLACED CLIP PER ECRA 5311-01400. 2 L 7 2 4F RT A16WE 2008040200011 20080402 00011 NM 2008 4 2 DU4R2008190 1 20080111 A 5330 SKIN BOEING 727 727 UTILSYS NM PWA JT8 JT8D* NE BS 1123 S24-25R DAMAGED B DU4R K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 15 289MT 22467 S/O 304002 N/R 26068 DEEP TOOL MARKS (5 EA) IN EXT. FUSELAGE SKIN AT BS 1123 FWD OF OUTFLOW VALVE RT SIDE. REPAIRED 5 E A TOOL MARKS BY CUTTING OUT AREA, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER 11 INCH X 10-3/4 INCH FROM 2024-T3. 071 INCH AND 2024-T3 .063 INCH IAW 53-30-3 FIG. 1, AND 51-10-2. 2 L 7 3 4J 4 F RT A3WE E2EA 2008040200012 20080402 00012 NM 2008 4 2 DU4R2008189 1 20080121 A 5311 FRAME BOEING 727 727 UTILSYS NM PWA JT8 JT8D* NE BS 720A S24-25L DENTED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 289MT 22467 S/O 304002 N/R 26446 DEEP DENT AT FLANGE AREA BS 720A S24 - 25L IN FWD PIT LT SIDE.REPAIRED BY CUTTING OUT DENT, FABRIC ATED FRAME REPAIR 8.5 INCH X 3 INCH X 1 INCH FROM 7075-T6 .063 INCH IAW SRM 51-40-3 FIG. 1, 51-30-2 AND 51-10-2 PARA. 2. 2 L 7 3 4J 4 F RT A3WE E2EA 2008040200015 20080402 00015 NM 2008 4 2 CALA0800248 1 20080321 A 5313 6561777505 STRINGER SPLICE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 STRINGER SPLICE CHANNEL AT STRINGER 14L BETWEEN STA 350 AND 360 CRACKED. REMOVED AND REPLACED SPLICE CHANNEL PER ECRA 5 311-01400. 2 L 7 2 4F RT A16WE 2008040200017 20080402 00017 EA 2008 4 2 TRAX200800420 1 20080312 A 5260 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 AAR - PAX DOOR TOP STEP ATTACH ANGLE IS BROKEN. 2 L 7 2 4F RT A21EA 2008040200019 20080402 00019 EA 2008 4 2 TRAX200800422 1 20080312 A 5755 NUT CNDAIR CL600 CL6002B19 1900309 EA RT SPOILER CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 AAR - CORROSION ON RT WING FLIGHT SPOILER HINGE POINT NUTS. 2 L 7 2 4F RT A21EA 2008040200020 20080402 00020 EA 2008 4 2 TRAX200800423 1 20080314 A 2913 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS LEAKING A ASOA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 27 835AS 7258 REMOVAL OF HYDRAULIC PUMP, LEAKING. EMERGENCY DECLARED. FLT 4915 DEL 68 MINS. 2 L 7 2 4F RT A21EA 2008040200030 20080402 00030 NM 2008 4 2 CALA0800239 1 20080306 A 5610 141N485065 WINDOW BOEING 757 757224 1384958 NM COCKPIT STUCK A CALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 18112 27302 CAPTAINS SIDE WINDOW WILL NOT OPEN. REMOVED AND REPLACED CAPTAINS NUMBER 2 SLIDING WINDOW IAW AMM 56-11-02. OPS CHECK GOOD REF LOG PAGE 7967323 FOR TRIM INSTALLATION. 2 L 7 2 4F RT A2NM 2008040200031 20080402 00031 NM 2008 4 2 CALA0800240 1 20080228 A 5610 141A48209 HANDLE BOEING 737 737824 13844BZ NM SLIDING WINDOW LACK OF LUBE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76254 30779 R2 SLIDING WINDOW DID NOT UNLOCK AND OPEN WHEN EXTERNAL RELEASE HANDLE WAS PULLED. LUBRICATED HANDLE AND OP'S CHECKED G OOD, IAW 737-800 MM 56-12-11, PAGE 516. 2 L 7 2 4F RT A16WE 2008040200032 20080402 00032 NM 2008 4 2 CALA0800241 1 20080307 A 2560 A3061402 MEGAPHONE BOEING 737 737824 13844BZ NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 36272 31590 AFT MEGAPHONE SIREN INOP. REMOVED AND REPLACED AFT MEGAPHONE. 2 L 7 2 4F RT A16WE 2008040200046 20080402 00046 NM 2008 4 2 ASAA0842732 1 20080303 A 5340 6547958504 ATTACH FITTING BOEING 737 737490 1384715 NM BS 795 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 CORROSION ON ATTACH CLIP BS 795 TO VERTICAL WEB OF KEELBEAM STR 27R (RBL 6 ) AFT CARGO PIT, CORRODED CHIP AT BS 795 FRAM E TO VERTICAL WEB OF KEEL BEAM STR 27R. REPLACED WITH MADE REPAIR PART IAW BAC DWG 65 47958 AND B737 400 SRM CH 51 30 0 1 AND 51 40 02. 2 L 7 2 4F RT A16WE 2008040200048 20080402 00048 NM 2008 4 2 ASAA0842733 1 20080303 A 5340 ATTACH FITTING BOEING 737 737490 1384715 NM BS 795 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 TIE CLIP AFT SIDE OF FRAME AT BS 795 OUTBD OF RT TIE DOWN TRACK RBL 13.80 CORRODED AFT CARGO PIT. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008040200051 20080402 00051 NM 2008 4 2 SWAA081532 1 20080322 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 251WN 32510 L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008040200057 20080402 00057 EA 2008 4 2 TRAX200800442 1 20080320 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 FITTING AT FS 484 RBL 9 CRACKED. REMOVED DAMAGED FITTING. DUPLICATED SERVICEABLE FITTING AS SHOWN IN REO 601R-53-41-059. INSTALLED NEW SERVICEABLE FITTING IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 2008040200069 20080402 00069 NM 2008 4 2 ASAA0842725 1 20080304 A 5753 65C3570329 SKIN BOEING 737 737490 1384715 NM FORE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 LT OUTBOARD FORE FLAP UPPER SURFACE DENTED. DENTS REPAIRED IAW SRM 51-70-10, REPAIR 3. 2 L 7 2 4F RT A16WE 2008040200070 20080402 00070 NM 2008 4 2 ASAA0852756 1 20080323 A 2130 8243921002 SELECTOR PANEL BOEING 737 737890 1384527 NM PRESSURE CONTROL FAULTED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 579AS 35187 PRESSURIZATION CONTROL "AUTO FAIL" AND "ALTN" ILLUMINATED NR 2 PRESSURE CONTROLLER LOGGED SEL PNL LRU FAILURE. PERFORME D FIM 21-31 TASK 801 AND FIM 21-31 TASK 803. FAULT CLEARED BITE CHECK GOOD. 2 L 7 2 4F RT A16WE 2008040200079 20080402 00079 NM 2008 4 2 SWAA081593 1 20080324 A 3350 101331 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 763SW 27877 LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008040200082 20080402 00082 NM 2008 4 2 SWAA081620 1 20080325 A 5320 6517582 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED SPV CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178, RBL 17, WL 232. REMOVED AND REPLACED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2008040200088 20080402 00088 NM 2008 4 2 SWAA081623 1 20080325 A 3350 3071BPEGPL LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008040200089 20080402 00089 NM 2008 4 2 CALA0800256 1 20080307 A 5313 BAC1498137 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 STRINGER CRACKED AT STA 297, STR 10LT. REPAIRED CRACKED STRINGER AT STA 297 - STRINGER 10LT PER SRM 51-70-11. 2 L 7 2 4F RT A16WE 2008040200092 20080402 00092 NM 2008 4 2 ASAA0852761 1 20080323 A 2420 761574B IDG BOEING 737 737890 1384527 NM NR 1 ENGINE LEAKING A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 585AS 35683 FOLLOW UP TO FREQUENT NR 1 IDG SERVICING. SEVERAL EXTERNAL LEAK CHECK ACCOMPLISHED WITH NO CHANGE TO EXCESSIVE SERVICIN G. REPLACED NR 1 IDG. OP CHECK PER MM24 11 00 PG 501. 2 L 7 2 4F RT A16WE 2008040200095 20080402 00095 NM 2008 4 2 ASAA0852759 1 20080325 A 3610 32145525 SHUTOFF VALVE BOEING 737 737890 1384527 NM NR 1 ENGINE LEAKING A ASAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 02 559AS 35178 DUCT PRESSURE SPLIT AT FLT LEVEL 350 IN CRUISE. NIS LEFT 87.7 RIGHT 87.7 PRESSURE LEFT 17 PSI RIGHT 42 PSI. ENGINE BLE EDS ON APU BLEED OFF. ISOLATION VALVE AUTO BOTH PACKS AUTO. PRESSURE THROUGHOUT CLIMB WAS L 12 R 42. FOUND PRSOV ON N R 1 ENGINE LEAKING AT BELLOWS SPLIT LINE IN CASE. REPLACED NR 1 ENGINE PRSOV. REPAIR CONFIRMATION GOOD. 2 L 7 2 4F RT A16WE 2008040200096 20080402 00096 NM 2008 4 2 USAA920080680 1 20080322 A 5330 6545775 SKIN BOEING 737 737401 1384701 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 23885 CLT - MAJOR REPAIR - RON - CRACKED FUSELAGE SKIN, BS 892 - BS 895, S25R. REPAIRED FUSELAGE SKIN BS 892 - BS 895, S25R I AW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008040200097 20080402 00097 NM 2008 4 2 USAA920080681 1 20080324 A 5330 6545774 SKIN BOEING 737 737401 1384701 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 23885 CLT - MAJOR REPAIR - RON - CRACKED FUSELAGE SKIN, BS 727D, S21L. REPAIRED FUSELAGE SKIN BS 727D, S21L IAW B737 SRM 53-0 0-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008040200099 20080402 00099 NM 2008 4 2 USAA920080702 1 20080326 A 5311 FRAME BOEING 757 757225 1384959 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918UW 22196 CLT - MAJOR REPAIR - CRACKED FRAME WEB, BS 560, S22R - S23R. REPAIRED FRAME WEB, BS 560, S22R - S23R IAW B737 SRM 53-00 -07 REPAIR 2. 2 L 7 2 4F RT A2NM 2008040200100 20080402 00100 NM 2008 4 2 USAA920080703 1 20080324 A 5330 6545775 SKIN BOEING 737 7373B7 1384580 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 23380 CLT - MAJOR REPAIR - C4 CHECK - CRACKED FUSELAGE SKIN, BS 883, S24R. REPAIRED FUSELAGE SKIN, BS 883, S24R IAW USAIRWAYS TYPICAL REPAIR 53-33. 2 L 7 2 4F RT A16WE 2008033100267 20080331 00267 NM 2008 3 31 QXEA200800310 1 20080320 A 5313 STRINGER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX -C4- CORROSION ON STR 24P FROM AFT SIDE OF FRAME AT STA X488 TO APPROXIMATELY STA X522, LT UNDER FLOOR. REMOVED COR ROSION IAW D-8 200 CPCM CHAPTER 4. HFEC INSPECTED BLEND AREA FOR CRACKS IAW D-8 200 NDTM PART 6, 51-00-01, NO CRACKS NO TED. UT THICKNESS CHECK OF BLENDED AREA IAW -8 200 NDTM PART 1, 51-00-04 HIGH .071 LOW .064. BLENDED AREA FOUND WITHIN LIMITS IAW SRM 51-20-11 WITH .007" MATERIAL REMOVED. 2 H 7 2 4T RT A13NM 2008033100272 20080331 00272 NM 2008 3 31 QXEA200800311 1 20080320 A 5330 SKIN PANEL DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - C4- CORROSION ON BAG BAY FLOOR LEVEL SKIN PANEL (LT SIDE) AROUND NUT PLATE HOLE (TOP AND BOTTOM) STA X580.5 AND Y2 8.0. REMOVED RIVETS HOLDING NUT PLATE RETAINER TO FACILITATE BLEND. REF DHC 8 200 SRM 51-40-11. REMOVED NUT PLATE FROM RETAINER TO CHECK FOR CORROSION REF DHC 8 200 SRM 51-40-11. BLENDED LIGHT SURFACE CORROSION OF TOP SURFACE OF MARKED S KIN REF CPCM CHAPTER 4 STEP 8. HFEC INSPECTED BLEND AREA FOR CRACKS IAW D-8 200 NDTM PART 6, 51-00-01. NO CRACKS NOTED . UT THICKNESS CHECK OF BLENDED AREA IAW -8 200 NDTM PART 1, 51-00-04 HIGH .040 LOW .037. AREA BLENDED WITHIN LIMITS P ER DHC 8/200 SRM 51-20-11. APPLIED ETCH, ALODINE AND PRIMER IAW D8 200 SRM 51-20-16 AND 51-20-36. REINSTALLED NUT PLA 2 H 7 2 4T RT A13NM 2008040300196 20080403 00196 WP 2008 4 3 08FDEA01214 1 20080331 A 5753 ARC196537 SKIN DOUG MD10 MD1010F 3022112 WP T/E FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT OUTBD FLAP LOWER SURFACE AT STA XOFH 703 HAS A DENT. CHECKED DENT, NOTED CREASES. FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00; FIG 48; VOL I. MATERIAL ID FOR THE REPAIR DOUBLER IS 2024-T3, 0.050, PO 610199.1. FABRICATED DO UBLER IAW DC/MD-10 SRM 57-10-00; FIG 85; VOL I. ALODINED; PRIMED AND PAINTED IAW DC/MD-10 SRM 51-21-01 PGS 21 THRU 24 AND 51-21-02; VOL II. INSTALLED IAW DC/MD-10 SRM 51-35-01; VOL II. 2 L 7 3 4F RT A22WE 2008040300198 20080403 00198 EU 2008 4 3 08FDEA01216 1 20080331 A 5347 251011405021 SEAT TRACK AIRBUS 310 A310203 3930313 EU COCKPIT WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 COCKPIT SEAT TRACK INBD SIDE IS WORN WITH 2 GOUGES. BLENDED AREAS IAW A310-200 SRM 51-74-01. FOUND TO BE OUT OF LIMITS IAW A310-200 CMM SOGERMA-SOCEA 25-13-00; PG 602; PARA 3. ORDERED AND RECEIVED NEW SEAT TRACK FROM STORES P/N 2510114 050-21, PO 613319.1. 2 L 7 2 4F RT A35EU 2008040300206 20080403 00206 EU 2008 4 3 08FDEA01224 1 20080401 A 5313 STRINGER AIRBUS 310 A310222 3930315 EU FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 448FE 260 PREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 56 RT BETWEEN FRAMES 67 TO 69, HAS REPAIR SECTION MEASURING 1 6" LONG AND 2 REPAIR SPLICES, THE FORWARD SPLICE IS 7.9 INCHES LONG AND THE AFT SPLICE IS 8.4 INCHES LONG. REPAIR NOT I AW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT STRINGER SPLICE REPAIR IAW A310-200 SRM 53-10-14 FIG 201. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008040300219 20080403 00219 WP 2008 4 3 08FDEA01237 1 20080401 A 5730 ARB128047 PANEL DOUG MD10 MD1010F 3022112 WP LT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LEFT WING OUTBD L/E PANEL NR 527 AB INNER SURFACE IS CHAFED AT THE END OF THE ACCESS DOOR HINGE. BLENDED AREA. FOUND T O BE OUT OF LIMITS IAW SRM 57-00-01 VOL I. FABRICATED DOUBLER IAW SRM 57-00-01 VOL I & 57-31-01 VOL III. ALODINED & PR IMED IAW SRM 51-21-01 VOL II. ASSEMBLED IAW SRM 51-35-01 VOL II. PAINTED IAW SRM 51-21-01 VOL II. 2 L 7 3 4F RT A22WE 2008040300222 20080403 00222 NM 2008 4 3 2008UALA01761 1 20080328 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 RT CREASE BEAM UPPER SURFACE CORRODED BETWEEN BS 907 TO 1006. MAJOR REPAIR ACCOMPLISHED, REPLACED CREASE BEAM AT DOOR 2 R. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200241 20080402 00241 NM 2008 4 2 SWAA081695 1 20080330 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040200253 20080402 00253 2008 4 2 2008UALA01721 4 20080326 A 2565 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L1 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 FOUND DOOR L1 SLIDE IS UNLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040200264 20080402 00264 EA 2008 4 2 CHQA200800060 1 20080327 A 4990 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE APU LOW A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 466CA 7627 GEE873331 IAH TO ATL - AFTER LEVELING OFF IN CRUISE FLIGHT, THE CREW RECEIVED AN APU HIGH TEMP MESSAGE ON EICAS. AFTER FOLLOWING THE APPROPRIATE QRH CHECKLISTS THE FLIGHT DIVERTED TO MGM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE A PU AND FOUND IT WAS LOW ON OIL. AFTER PROPERLY SERVICING THE APU WITH OIL, IT OPERATED NORMALLY AND THE AIRCRAFT WAS RE LEASED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008040200273 20080402 00273 WP 2008 4 2 08FDEA01178 1 20080328 A 5320 ADA713227 RETAINER DOUG MD10 MD1010F 3022112 WP ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 FWD CARGO PIT ENTRANCE; UPPER RIGHT CORNER CEILING RETAINING STRIP IS GOUGED. REMOVED DAMAGED RETAINING STRIP IAW DC/MD -10 SRM 51-31-01; VOL II; PG 1. FABRICATED NEW STRIP IAW DAC DWG ADA 7132; REV H. ALODINED AND PRIMER IAW DC/MD -10 SR M 51-21-01; VOL II; PGS 21 AND 24. PART MARKED FX-ADA7132-27 IAW FEDEX GMM 7-0-1000. INSTALLED IAW DC/MD-10 SRM 51-31- 01; VOL II; PG 1. 2 L 7 3 4F RT A22WE 2008040200294 20080402 00294 NM 2008 4 2 KCSA081181 1 20080318 A 5311 FRAME BOEING 747 747209B 138489B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 AFT PIT BS 2200 FAILSAFE CHORD DAMAGED AT APPROX STR-40L. 2 L 7 4 4F RT A20WE 2008040200329 20080402 00329 NM 2008 4 2 GTIA0800039 1 20080318 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 502NK 2433 FLOORBEAM AT -Y1732 BETWEEN FR 68 AND FR 70 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM ASSY IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008030700378 20080307 00378 NM 2008 3 7 SWAA081096 1 20080227 A 3350 65C27093 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED EXIT SIGN ASSY PER MM. 2 L 7 2 4F RT A16WE 2008030700381 20080307 00381 NM 2008 3 7 SWAA081098 1 20080227 A 3350 1619 LIGHT BOEING 737 7375H4 138449D NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008031000014 20080310 00014 SO 2008 3 10 FDKA200802079 1 20080222 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN CABIN DOOR OUT OF ADJUST A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FDM 6055 TPA-MCO (0923 PHX LCL). THE AIRCRAFT REPORTED MAIN CABIN DOOR HARD TO OPEN. MX ADJUSTED, CLEANED AND LUBED DO OR AFTER WHICH ALL CHECKS WERE NORMAL. 2 L 7 2 4T RT T00011AT 2008031000041 20080310 00041 SO 2008 3 10 FDKA200802081 1 20080225 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN SMOKE A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 839MJ 145416 FDM 6121 ATL-HSV (0727 PHX LCL). SMOKE IN CABIN. MX TROUBLESHOT AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008040100012 20080401 00012 WP 2008 4 1 08FDEA01164 1 20080327 A 5753 NRC6053 SKIN DOUG DC10 DC1030F 3023504 WP T/E FLAP LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 307FE 48291 LT WING OUTBD FLAP LWR SURFACE FOUND 100 LOOSE RIVETS ON SKIN. REPAIRED SKIN LOOSE FASTENERS IAW SRM 57-20-00 FIG 11 VO L I. 2 L 7 3 4F RT A22WE 2008040100014 20080401 00014 NM 2008 4 1 TAMF20080021S 1 20080316 A 5330 SKIN BOEING 767 767200 1385120 NM GE CF6 CF680 30025 NE BS 1417 S36R CORRODED W TAMF K NONE O OTHER IN INSP/MAINT 1 SO 23 770QT 23802 DURING (C2) CHECK WAS FOUND SKIN PN 146T3240 WITH CORROSION. STA 1417, STRINGER 36 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-075 AND SR 1-79124788. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR. 2 L 7 2 4F 4 F RT A1NM E13NE 2008040100046 20080401 00046 CE 2008 4 1 DXTA20082967 1 20080327 A 2170 COALESCER BAG CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL A/C PACK ODOR E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 900QS 7500123 STRONG ODOR FROM WATER SEPARATOR IN CABIN PAC. REMOVED CABIN AIR CYCLE MACHINE DUE TO OIL LEAK. CLEANED CABIN HEAT EXCH ANGE AND INSTALLED REPAIRED ACM IAW MM CH 21-51-00, OPS CHECKED GOOD & LEAK CHECKED GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008040100061 20080401 00061 NM 2008 4 1 USAA920080655 1 20080219 A 5743 6549488 SUPPORT FITTING BOEING 737 7373S3 1384711 NM RT MLG CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 314AW 23733 MCN - MAJOR REPAIR - C20 CHECK - RIGHT MLG AFT SUPPORT FITTING CRACKED, WBL 187. REPLACED RIGHT WING MLG AFT SUPPORT FI TTING CRACKED, WBL 187 IAW USAIRWAYS EA 1002823. 2 L 7 2 4F RT A16WE 2008040100068 20080401 00068 CE 2008 4 1 DXTA20082971 1 20080330 A 2170 COALESCER BAG CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN ODOR E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 921QS 7500241 CABIN ALTITUDE SPIKED TO 4000 FT /MIN CLIMB DURING GEAR RETRACTION . SHORTLY THERE AFTER SMOKE ENTERED THE CABIN THEN DI SSIPATED. REPLACED BOTH COALESCER SOCKS PER MM 12-10-01. ACCOMPLISHED MANUAL CONTROL VALVE PLUMBING LEAK TEST, LT AND R T CABIN PRESSURE CONTROL SYSTEM STATIC LEAK TEST AND ELECTROPNEUMATIC TRANSFER VALVE PLUMBING LEAK TEST PER MM 21-30-00. ALL TESTS AND LEAK CHECKS ARE GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008040100073 20080401 00073 CE 2008 4 1 DXTA20082974 1 20080330 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE FAILED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 399QS 5600510 CO-PILOT'S BRAKES FEEL MUSHY AND SOFT WITH MORE THEN USUAL TRAVEL DURING LANDING. BLED ANTI SKID BRAKE SYSTEM. OPS CHEC KED GOOD. LEAK CHECKED GOOD. WORK DONE IAW 560 M.M. CHAPTER 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2008040100083 20080401 00083 EA 2008 4 1 A6WA200840148 1 20080301 A 2613 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE DETECTION SYS MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 446AW 7806 RT 14TH DUCT FAIL MESSAGE ILLUMINATED AT 15,000 FT AFTER DEPARTURE. PERFORMED QRH, MESSAGE DID NOT EXTINGUISH FOR APPRO X 12 MINUTES. AIR DIVERSION DECLARED EMERGENCY LANDING. (K) REMOVED AND REPLACED FUSELAGE SENSING ELEMENT A46WK (RT SI DE) IAW AMM 36-21-04. OPS CHECK OK. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 2008040100084 20080401 00084 EU 2008 4 1 USAA920080665 1 20080301 A 5315 D5311218920001 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 651AW 866 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 709/FR 16 - BS 732/FR 17A, S19L. REPLACED CABIN FLOORB EAM, BS 709/FR 16 - BS 732/FR 17A, S19 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008040100092 20080401 00092 EA 2008 4 1 A6WA200840151 1 20080304 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE AOA HEAT ILLUMINATED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 424AW 7656 RT AOA HEAT CAUTION MESSAGE ILLUMINATED IMMEDIATELY AFTER TAKEOFF. COMPLIED WITH QRH, MESSAGE DID NOT EXTINGUISH. PERF ORMED AIR RETURN TO DEPARTURE. LANDED AT 46,900 LBS, BRAKE TEMPS 3-3-5-5. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008040100093 20080401 00093 NM 2008 4 1 USAA920080675 1 20080321 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - LEVEL 2 CORROSION ON AFT ENTRY DOOR "Z" ANGLE, BS 947 - BS 991, LBL 53. REPAIRED AFT EN TRY DOOR "Z" ANGLE, BS 947 - BS 991, LBL 53 IAW B737 SRM 51-70-11. 2 L 7 2 4F RT A16WE 2008040100101 20080401 00101 EA 2008 4 1 A6WA200840156 1 20080229 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 PAX DOOR AFT DRAG ANGLE FOUND CRACK. REPAIRED IAW REO 601R-52-11-513 REV A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008040100113 20080401 00113 CE 2008 4 1 CDN2008F00001 1 20080304 A 5280 542215120 DOOR LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP MLG MISSING A CDNA O OTHER O OTHER CR CRUISE 1 EA 05 1JG 055 AT 10,000 FT, CREW OBSERVED A LANDING GEAR UNSAFE LIGHT, FOLLOWED BY VIBRATION AND AIR NOISE. AC WAS SLOWED TO BELOW 25 0 KTS AND THEN CREW HEARD A (BANG) NOISE. AFTER LANDING IT WAS NOTICED THA THE RT OB GEAR DOOR HAD SEPARATED FROM THE A IRCRAFT. (K) 2 L 7 2 4F 4 F A10CE E6WE 2008040100127 20080401 00127 NM 2008 4 1 USAA920080693 1 20080314 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C-18 CHECK - STRINGER CLIP CRACKED, BS 400 S4L. REPLACED STRINGER CLIP, BS 400 S4L IAW BOEING SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008040100137 20080401 00137 NM 2008 4 1 ASAA0842735 1 20080229 A 5330 65468811174 SKIN BOEING 737 737490 1384715 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 FUSELAGE SKIN APPROX BS 1070 AT STR 146 DENTED FROM CONTACT WITH WORK SCAFFOLD FUSELAGE SKIN APPROX BS 1070 STR 14L DENT REPAIRED IAW B737 400 SRM CH 53 80 01. 2 L 7 2 4F RT A16WE 2008040100144 20080401 00144 NM 2008 4 1 ASAA0842712 1 20080313 A 5753 6546435339 SKIN BOEING 737 737490 1384715 NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 LT OUTBOARD AFT FLAP LWR SURFACE AT WBL 255 IS DENTED. DENT REPAIRED IAW B737 400 SRM CH 51 70 10. 2 L 7 2 4F RT A16WE 2008031000042 20080310 00042 SO 2008 3 10 FDKA200802082 1 20080227 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6075 MCO-CHS (1118 PHX LCL). EMERGENCY LIGHT SIGN OUT AT GALLEY. MX RESECURED CONNECTOR. 2 L 7 2 4T RT T00011AT 2008031000043 20080310 00043 NM 2008 3 10 08FDEA00672 1 20080229 A 5320 143N55225 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 FLOOR SUPPORT FROM STATION 720 TO 740, LBL 60, WL208, HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF SRM 53-00-51 , FIG 101, DETAIL III LIMITS, L= 8 INCH, W= 2 INCH, D= 0.15 INCH, ORIGINAL MATERIAL THICKNESS .056 INCH. FABRICATED NEW FLOOR SUPPORT ON MAE TRAVELER NR T7/713361, FROM 7075-0-.056 B, HEAT TREATED TO T6. REMOVED AND REPLACED FLOOR SUPPORT (PN: 143N5522-5) IAW SRM 51-40-02. THIS IS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP ACTION REQUIRED. 2 L 7 2 4F RT A2NM 2008031000044 20080310 00044 EU 2008 3 10 08FDEA00674 1 20080303 A 5320 A53810996 DIAPHRAGM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND DENTS AND NICKS IN DIAPHRAGMS, C47-48, TRACK 2 LT TO 2 RT REPAIR PERFORMED BY REWORK OF NICK AND NDT FOR CRACK FRE E CONDITION IAW RAS/70503778/2008 ISS A, APPROVED BY EA 6-5315-115283. 2 L 7 2 4F RT A35EU 2008031000056 20080310 00056 NM 2008 3 10 DHL2008752610 1 20080208 A 5711 SPAR BOEING 727 727223 1384074 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 RT WING INBOARD L/E AREA AT FSS 107.2 FWD WING SPAR TERMINAL JOINT ANGLE CRACK AT BOTTOM. STOP DRILLED CRACK DIM .250 I AW B727 SRM 51-10-1. HFEC VERIFIED THAT CRACK END ON STOP DRILL HOLE IAW B727 NDTM PT6 51-00-00 FIG 23. FABRICATED NEW ANGLE USING 7075-T6 .063 PO NR 9006027 DIM 11 INCHES BY 2.25 IAW B727 SRM 51-20-1, 51-30-5 AND 57-10-2 FIG 3. INSTALLE D NEW ANGLE IAW B727 SRM 51-30-2 AND 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2008031000065 20080310 00065 SO 2008 3 10 FDKA200802083 1 20080228 A 3350 SIGN EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 830MJ 145259 FDM 5973 ORF-JFK (0420 PHX LCL). FLOOR EMERGENCY AND CEILING EMERGENCY OVERWING EXIT SIGN FORWARD SIDE INOP. MX OPS CH ECK SYSTEM OPS GOOD. 2 L 7 2 4T RT T00011AT 2008031000068 20080310 00068 NM 2008 3 10 SWAA081121 1 20080228 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER 23R CRACKED AT BS 328. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008031000075 20080310 00075 NM 2008 3 10 SWAA081122 1 20080228 A 5310 6546956 CREASE BEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 415, RBL 68. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008031000076 20080310 00076 NM 2008 3 10 SWAA081132 1 20080228 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, LBL 7. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008031000079 20080310 00079 NM 2008 3 10 SWAA081129 1 20080228 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 25L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008031000084 20080310 00084 NM 2008 3 10 SWAA081133 1 20080228 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2008031000085 20080310 00085 EA 2008 3 10 TRAX200800360 1 20080229 A 3260 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA BRAKE OVERHEAT ILLUMINATED A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 730EV 10141 BRAKE OVHT MSG EMERGENCY IN FLIGHT AT FL 340 C/W QRH ALL INDICATIONS NORMAL. REOCCURRED APPROX 15 MINS LATER AGAIN FOLL OWED QRH ALL IND RET TO NORMAL BUT LEFT GEAR DOWN AND RET TO ATL. AIRCRAFT RETURNED BACK TO ATL AFTER T/O, EMERGENCY DE CLARED. 2 L 7 2 4F RT A21EA 2008031000093 20080310 00093 NM 2008 3 10 DHL2008752611 1 20080203 A 5320 6518636378 ANGLE BOEING 727 727223 1384074 NM BS 870 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 CRACK AT RT MLG WHEEL WELL STATION 870 FWD INBD LWR BULKHEAD 18: LEFT OF LOAD CONTROL VALVE 8" RIGHT OF CENTER. REMOVED AND REPLACED ANGLE AT RT MLG W/W STA 870 FWD INBOARD LOWER BULKHEAD IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008031000095 20080310 00095 NM 2008 3 10 DHL2008763500 1 20080302 A 5347 BAC15201466 SEAT TRACK BOEING 727 727264 138408M NM BS 850-870 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 SEAT TRACK CORRODED AT BS 850-870, RBL 45. REMOVED TRACK SECTION, FABRICATED SECTION FROM BAC1520-1466, PO NR 730788, 1 5.75" LONG, AND INSTALLED PER B727 SRM 53-10-2 FIG 7, 53-10-5 FIG 1 AND 51-30-2. 2 L 7 3 4F A3WE 2008031000097 20080310 00097 SO 2008 3 10 135991030408 2 20080229 A 8550 DIPSTICK CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO LT ENGINE UNKNOWN E HYIA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 61 991AA 402C0317 831937R DURING CLIMB-OUT, PILOT NOTED LT ENGINE MANIFOLD PRESSURE INCREASE FOLLOWED BY INCREASE IN OIL PRESSURE. PILOT TURNED B ACK AND SECURED LT ENGINE AS A PRECAUTIONARY MEASURE. WHITE SMOKE WAS NOTED COMING FROM LT ENGINE. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ENGINE FOR CONDITION AND COMPRESSION, DEGREASED ENGINE AND REPLACED DIPSTICK, PERFORME D RUN UP AND RELEASED AIRCRAFT RETURN TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 2008031000101 20080310 00101 2008 3 10 ARWA20080302 4 20080302 A 3416 4005123901 ALTIMETER DOUG DC10 DC1030 3023501 WP COCKPIT INTERMITTENT A ARWA O OTHER O OTHER CR CRUISE 1 SO 19 526MD 46998 FIRST OFFICER'S ALTIMETER INTERMITTENTLY STICKS IN FLIGHT; OCCASIONALLY HAS OFF FLAG IN VIEW. REMOVED AND REPLACED FIRS T OFFICER'S ALTIMETER IN ACCORDANCE WITH M/M 34-12-01; PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH M/M 34-12-00 AND 3 4-16-00 FOUND NORMAL. 2 L 7 3 4F A22WE 2008040100158 20080401 00158 2008 4 1 MWEA080042 4 20080314 A 3441 HG2080AC01 ADIRU BOEING 717 717200 1383700 NM COCKPIT OUT OF ALIGNMENT A MWEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 13 926ME 55192 CREW OBSERVED ON AUTO TRIM AND WIND SHEAR FAIL ALERT. FOUND NR 1 ADIRU WOULD NOT ALIGN PROPERLY, REMOVED AND REPLACED A DIRU. 2 L 7 2 4F TR A6WE 2008040100168 20080401 00168 EU 2008 4 1 UPS08151912 1 20080322 A 2780 JACKSCREW AIRBUS A300 A300F4622R 3930360 EU L/E SLAT UNSERVICEABLE A IPXA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 128UP 0812 INSPECTION TYPE:N/A CREW RECEIVED A FLAP/SLAT DISAGREE MESSAGE. CREW DECLARED AN EMERGENCY AND COMPLETED A SECOND APPRO ACH AND LANDED WITHOUT FURTHER INCIDENT. INSPECTED AND FOUND NR 6 SLAT JACKSCREW RIGHT WING LOCKOUT INDICATOR IN LOCKOU T. REPLACED JACKSCREW WITH SERVICEABLE UNIT IAW AMM, OPS CHECK GOOD ON GROUND. 2 L 7 2 4F RT A35EU 2008040100181 20080401 00181 NM 2008 4 1 ASAA0892770 1 20080307 A 5320 PANEL BOEING 737 737990 NM BS 727B-727C CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 323AS 30021 AFT CARGO PIT RT FLOOR TO SIDEWALL TRANSITION PANEL MULTIPLE AREAS OF CORROSION FWD OF CARGO DOOR (SIDEPLATE). CUT OUT DAMAGED AREA OF SIDEPLATE LOCATED DRILLED. INSTALLED A REPLACEMENT SIDEPLATE AND SPLICE PARTS IAW B737 900 SRM 53 00 53 PG 202 FIG 202 PG 204 REPAIR 5 TABLE 201. 2 L 7 4 4F RT A16WE 2008040100184 20080401 00184 NM 2008 4 1 ASAA0892771 1 20080307 A 5320 146A750219 PANEL BOEING 737 737990 NM BS 727F-727I CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 323AS 30021 AFT CARGO PIT LT FLOOR TO SIDEWALL TRANSITION PANEL (SIDEPANEL) HAS MULTIPLE AREAS OF CORROSION STA 727G AREA. CUT OUT DAMAGED SECTION OF SIDEPANEL. LOCATED DRILLED INSTALLED A REPLACEMENT SIDEPLATE AND SPLICE PARTS IAW B737 900 SRM 53 00 53 PG 202 FIG 202 PG 204 REPAIR 5 TABLE 201. 2 L 7 4 4F RT A16WE 2008040100223 20080401 00223 NM 2008 4 1 SWAA081724 1 20080330 A 5322 6546569 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 6L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008040100272 20080401 00272 NM 2008 4 1 SWAA081628 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040100273 20080401 00273 NM 2008 4 1 SWAA081629 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040200007 20080402 00007 NM 2008 4 2 CALA0800246 1 20080321 A 5320 69489856 ATTACH FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 ATTACHING CLIP AT STRINGER 11L BETWEEN BS 350 AND 360 CRACKED. REMOVED AND INSTALLED NEW CLIP PER ECRA 5311-01400. 2 L 7 2 4F RT A16WE 2008040200021 20080402 00021 NM 2008 4 2 CALA0800232 1 20080318 A 5743 115A5211 SUPPORT FITTING BOEING 737 737724 13844BY NM LT MGL TRUNNION CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24715 28786 LEFT MLG FWD TRUNNION SUPPORT HAS PITTING CORROSION AT UPPER O/B BUSHING. REPAIRED PER EC/RA 5741-01106. 2 L 7 2 4F RT A16WE 2008040200038 20080402 00038 NM 2008 4 2 CALA0800251 1 20080317 A 5320 69539711 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INTERCOSTAL CRACKED AT AFT BAG BIN UNLOCK ATTACH POINT. REMOVED AND REPLACED UPLOCK ATTACH CHANNEL ASSEMBLY PER SRM 51- 40-02. 2 L 7 2 4F RT A16WE 2008040200063 20080402 00063 EA 2008 4 2 TRAX200800448 1 20080320 A 5320 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 LT BATTERY RIB DRAG ANGLE CRACKED IN GEAR BAY. REMOVED UNSERVICEABLE RIB DRAG ANGLE. LOCATED HOLES IN NEW SERVICEABLE DRAG ANGLE IAW SRM 51-40-11. OK TO INSTALL. INSTALLED NEW DRAG ANGLE IAW SRM 51-42-21. OK TO TOPCOAT. TOPCOATED IAW SRM 51-26-16. 2 L 7 2 4F RT A21EA 2008040200072 20080402 00072 NM 2008 4 2 ASAA0852749 1 20080322 A 2150 3989083 VALVE BOEING 737 737890 1384527 NM A/C PACK FAULTY A ASAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 559AS 35178 OBSERVED FWD CONTROL CABIN ZONE TEMP ANNUNCIATION ON RECALL DURING AFTER START CHECKLIST. REPLACED CONTROL CABIN TRIM V ALVE. BITE CHECK GOOD. SOAP BUBBLE TEST GOOD. 2 L 7 2 4F RT A16WE 2008040200081 20080402 00081 NM 2008 4 2 SWAA081601 1 20080325 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED SPV CHECK, FOUND LT AFT CABIN EMERGENCY BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008040200085 20080402 00085 NM 2008 4 2 SWAA081622 1 20080325 A 3350 1619 LIGHT BOEING 737 7373Q8 1384670 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008040200106 20080402 00106 EU 2008 4 2 USAA920080708 1 20080313 A 5530 D5537123500600 HINGE FITTING AIRBUS 320 A320231 3930325 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 621AW 53 SAL - MAJOR REPAIR - C6 CHECK - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 4, VERTICAL STABILIZER STATION 2632/RIB 6. RE PLACED RUDDER HINGE FITTING NR 4, VERTICAL STABILIZER STATION 2632/RIB 6 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2008040200108 20080402 00108 NM 2008 4 2 CALA0800259 1 20080324 A 5310 65458076 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 R1 DOOR FRAME HAS CRACK AT FS 294.5 AND STRINGER 7R. REMOVED STUB FRAME IAW B737 SRM 51-40-02 FOR REPLACEMENT REF B737 SRM 51-10-02. LOCATED AND DRILLED NEW FRAME P/N 65-45807U6 IAW B737 SRM 51-40-02. INSTALLED NEW STUB FRAME IAW B737 SR M 51-40-02. 2 L 7 2 4F RT A16WE 2008040200109 20080402 00109 EU 2008 4 2 USAA920080710 1 20080321 A 5347 D53070011 SEAT TRACK AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 621AW 53 SAL - MAJOR REPAIR - C6 CHECK - CORROSION ON CABIN SEAT TRACK, BS 1483/FR 34, -Y765. REPAIRED CABIN SEAT TRACK, BS 1483 /FR 34, -Y765 IAW A320 SRM 53-00-15. 2 L 7 2 4F RT A28NM 2008040200113 20080402 00113 WP 2008 4 2 ASAA0882781 1 20080326 A 5241 5937601511 DOOR DOUG DC9 DC983 3022083 WP AFT GALLEY STUCK A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 944AS 55643 15827 53019 COULD NOT CLOSE AFTER GALLEY (L 2) DOOR. RESET DOOR GUIDE BRACKET. OP CHECKED OK. 2 L 7 2 4F RT A6WE 2008040200114 20080402 00114 NM 2008 4 2 CALA0800260 1 20080324 A 5310 65535951 DEPRESSOR BOEING 737 7373T0 1384582 NM R1 DOOR FRAME CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 SEAL DEPRESSOR CRACKED AT R1 DOOR FRAME UPPER FWD CORNER. REMOVED CRACKED SEAL DEPRESSOR P/N 65-53595-1 IAW B737 SRM 51 -40-02 REF BOEING DWG 65-53595. 2 L 7 2 4F RT A16WE 2008040200117 20080402 00117 NM 2008 4 2 CALA0800261 1 20080318 A 5320 6552878U125 ANGLE BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11641 28902 Z-ANGEL AT L2 DOOR IS CORRODED IN SEVERAL AREAS. REMOVED CORRODED Z-ANGLE AND LOCATED AND DRILLED NEW Z-ANGLE AT L-2 DO OR PER B737 SRM 51-40-02. INSTALLED NEW Z-ANGLE AT L-2 DOOR PER B737 SRM 51-40-02, 51-10-02. 2 L 7 2 4F RT A16WE 2008040200129 20080402 00129 NM 2008 4 2 CALA0800266 1 20080326 A 5420 311A12155 FITTING BOEING 737 7373T0 1384582 NM NR 2 PYLON CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 NR 2 ENGINE PYLON RIGHT FITTING HAS CORROSION INSIDE BUSHING HOLE. REPAIRED NR 2 ENGINE PYLON RIGHT FITTING IAW EC/RA 5 450-01735 AND PACE EA350-54-001. 2 L 7 2 4F RT A16WE 2008040200130 20080402 00130 NM 2008 4 2 CALA0800267 1 20080326 A 5230 6547952134 DOOR FRAME BOEING 737 7373T0 1384582 NM AFT CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 AFT CARGO DOOR FWD SIDE LOWER FRAME CRACKED. REPLACED AFT CARGO DOOR FWD LOWER FRAME REF SRM 51-10-2 & DWG 65-47952. 2 L 7 2 4F RT A16WE 2008040200132 20080402 00132 NM 2008 4 2 CALA0800269 1 20080328 A 3350 D71701100 BATTERY PACK BOEING 737 737824 13844BZ NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12221 30559 30559 28930 EPL HAS SEVERAL LIGHTS OUT. REPLACED BATTERY PACKS AT STA 322 WL 291 RBL & STA 565 WL 213 R BL RBC. REF WDW 33-91-11. 2 L 7 2 4F RT A16WE 2008040200137 20080402 00137 NM 2008 4 2 2008UALA01634 1 20080321 A 5511 SPAR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 RT HORIZONTAL STABILIZER CENTER SECTION FWD SPAR UPPER FWD AND AFT CLEVIS HAVE FRETTING CORROSION. MAJOR REPAIR: REMOVE D CORROSION. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200140 20080402 00140 NM 2008 4 2 2008UALA01637 1 20080323 A 5320 CHANNEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 348 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 DURING HMV INSPECTIONS, DAMAGE WAS FOUND AT BS 348 CHANNEL AT STR S-14L. MAJOR REPAIR: REMOVED DAMAGE COMPONENTS. OBTAI NED/FABRICATED AND INSTALLED REPLACEMENT PARTS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200142 20080402 00142 NM 2008 4 2 CALA0800274 1 20080313 A 5230 65917001054 DOOR FRAME BOEING 737 7373T0 1384582 NM AFT CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 AFT CARGO DOOR FWD SIDE UPPER FRAME CRACKED. REPLACED AFT CARGO DOOR UPPER FWD FRAME REF SRM 51-10-2 & DWG 65-47952. 2 L 7 2 4F RT A16WE 2008040200149 20080402 00149 NM 2008 4 2 2008UALA01646 1 20080324 A 3397 362624 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT EEL LIGHT INOP, AT RIGHT SIDE FWD SIDE OF FWD GALLEY LOWER WALL. FOUND LOOSE CONNECTION. SECURED CONNECTI ON OPS CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200150 20080402 00150 NM 2008 4 2 2008UALA01647 1 20080324 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT LIGHT INOP, RIGHT CLOSET LOWER WALL FWD OF LAV 102. REPLACED LAMP ASSEMBLY. OPS. CHECKS GOOD. AC OK FOR S ERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200152 20080402 00152 NM 2008 4 2 2008UALA01648 1 20080324 A 3500 OXYGEN SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 OXYGEN LEAKS, STARTED WITH 1620 SHUTDOWN WITH 1480. FOUND B-NUT LOOSE. TIGHTENED B-NUT. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200153 20080402 00153 EA 2008 4 2 TRAX200800413 1 20080312 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 AAR - LEFT OVERWING EMERGENCY EXIT FAIL PULL TEST ON EXIT HANDLE. LUBRICATED DOOR & RETESTED, NO DEFECTS NOTED AT THIS TIME IAW CRJ 200 MM 12-20-52 & 52-21-00. SUPPLEMENTAL SDR CLOSED 3/27/08. 2 L 7 2 4F RT A21EA 2008040200156 20080402 00156 NM 2008 4 2 2008UALA01651 1 20080321 A 3350 767 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 558UA 26654 DOOR 1L EMERGENCY LIGHT INOPERATIVE. SUPPLEMENTAL DATA UPDATE, CAUSE LAMP IS INOP. RELAMPED ASSY, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031000104 20080310 00104 NM 2008 3 10 08FDEA00663 1 20080229 A 2910 BACH30AX04R0157 HOSE BOEING 727 727233 138408A NM HYD SYSTEM CHAFED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 283FE 22350 IN FLIGHT TOTAL LOSS OF "A" SYSTEM HYDRAULICS. "A" SYSTEM HYD QTY WAS FOUND AT 2 GALLON SYSTEM DID NOT RUN EMPTY. FOUN D HYD LINE IN ELEVATOR PCP BROKEN AT CLAMPED AREA. REPLACED LINE REF MM 20-10-012-4. OPERATED HYD SYSTEM. OPERATED AND INSPECTED ALL FLIGHT CONTROLS AND ELEVATOR PCP, NO FURTHER LEAKS WERE FOUND. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 2008031000106 20080310 00106 NM 2008 3 10 KCSA081130 1 20080301 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 EXTERNAL FUSELAGE SKIN HAS CORROSION AROUND FASTENERS AT STA 1400 TO 1420, STR 4L. 2 L 7 4 4F RT A20WE 2008031000107 20080310 00107 NM 2008 3 10 KCSA081131 1 20080301 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 EXTERNAL FUSELAGE SKIN HAS CORROSION AROUND FASTENERS AT STA 1360 TO 1370, STR 4L. 2 L 7 4 4F RT A20WE 2008031000115 20080310 00115 NM 2008 3 10 08FDEA00684 1 20080303 A 5320 141N516033 CHANNEL BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 MAIN CARGO DECK FLOOR, U CHANNEL, BETWEEN STA 310 TO 324, LBL 21, WL 208, HAS CORROSION. REMOVED CORROSION FROM U CHA NNEL IAW SRM 51-10-02, L= 2.3 FT, W= 2.0 INCHES, D= .015 INCHES, ORIGINAL MATERIAL THICKNESS .054", FOUND TO BE OUT OF S RM 53-00-51, FIG 101, DETAIL III LIMITS. REMOVED U CHANNEL IAW SRM 51-40-02. FABRICATED NEW REPAIR CHANNEL ON MAE TRAV ELER NR T7/713522, FROM 7075-0 0.050C, HEAT TREATED TO T6. LOCATED AND DRILLED REPAIR CHANNEL IAW SRM 51-40-05. TREAT ED AND PRIMED REPAIR CHANNEL IAW SRM 51-20-01. INSTALLED REPAIR CHANNEL IAW SRM 51-40-02. THIS IS A CATEGORY "A", MAJO R REPAIR. 2 L 7 2 4F RT A2NM 2008031000120 20080310 00120 NM 2008 3 10 08FDEA00687 1 20080303 A 5320 141N516019 CHANNEL BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 MAIN CARGO DECK FLOOR CHANNEL BETWEEN STA 324 TO 333, LBL 21, WL 208 HAS CORROSION. REMOVED CORROSION FROM CHANNEL IA W SRM 51-10-02, L= 8.5 INCHES, W= 2.4 INCHES, D= .007 INCH, ORIGINAL MATERIAL THICKNESS 0.49 INCH. FOUND TO BE OUT OF S RM 53-00-51, FIG 101, DETAIL III LIMITS. REMOVED CHANNEL IAW SRM 51-40-02. FABRICATED NEW REPAIR CHANNEL ON MAE TRAVEL ER NR T7/713523, FROM 7075-0 0.050C, HEAT TREATED TO T6. LOCATED AND DRILLED REPAIR CHANNEL IAW SRM 51-40-05. TREATED AND PRIMED REPAIR CHANNEL IAW SRM 51-21-01. TOP COATED CHANNEL IAW AMM 51-21-00-07. INSTALLED REPAIR CHANNEL IAW SRM 51-40- 02. THIS IS A CATEGORY "A" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 2008031000122 20080310 00122 NM 2008 3 10 08FDEA00689 1 20080304 A 5754 654N02432 ANGLE BOEING 757 75727B 1384921 NM NR 6 SLAT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 RT WING INBD SLAT NR 6 HAS HEAVY CORROSION JUST BELOW PANEL 612GB. REPLACED OUTBOARD LOWER ANGLE IAW SRM 51-10-02 REV 9 3. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008031000130 20080310 00130 NM 2008 3 10 USAA920080534 1 20080302 A 5330 6545767 SKIN BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 591US 23936 CLT - MAJOR REPAIR - RON - CRACKED FUSELAGE SKIN, BS 500C, S15L. REPAIRED FUSELAGE SKIN, BS 500C, S15L IAW USAIRWAYS EA 100277. 2 L 7 2 4F RT A16WE 2008031000131 20080310 00131 NM 2008 3 10 USAA920080535 1 20080229 A 5311 90526911 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 767, S9L. REPAIRED FRAME BS, 767, S9L IAW USAIRWAYS EA 100286. 2 L 7 2 4F RT A16WE 2008031000133 20080310 00133 NM 2008 3 10 USAA920080537 1 20080228 A 5311 90526911 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 480, S9L AND S9R. REPAIRED FRAME BS 480, S9L AND S9R IAW USAIRWAYS EA 100286. 2 L 7 2 4F RT A16WE 2008031000137 20080310 00137 NM 2008 3 10 USAA920080541 1 20080207 A 5320 143N833817 INTERCOSTAL BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 901AW 23321 MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL, BS 680, S12L. REPLACED INTERCOSTAL, BS 680, S12L IAW USAIRWAYS TA SK CARD M1C53608. 2 L 7 2 4F RT A2NM 2008031000139 20080310 00139 NM 2008 3 10 USAA920080543 1 20080208 A 5311 65465252 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 380, S9R. REPAIRED FRAME BS, 380, S9R IAW USAIRWAYS EA 100286. 2 L 7 2 4F RT A16WE 2008031000144 20080310 00144 NM 2008 3 10 USAA920080548 1 20080218 A 5522 183N200323 SKIN BOEING 757 7572S7 1384962 NM LT ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 901AW 23321 MCN - MAJOR REPAIR - C12 CHECK - LEFT ELEVATOR HAS DELAMINATION, ELEVATOR STATION 310- 318. REPAIRED LEFT ELEVATOR, ELE VATOR STATION 310- 318 IAW B757 SRM 51-70-04. 2 L 7 2 4F RT A2NM 2008031000151 20080310 00151 NM 2008 3 10 USAA920080558 1 20080207 A 5210 507945264 WEB BOEING 737 7373G7 1384595 NM L1 DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED L1 DOOR INNER WEB, BS 347, S14L - S15L. REPAIRED L1 DOOR INNER WEB, BS 347, S 14L - S15L IAW USAIRWAYS EA 100247. 2 L 7 2 4F RT A16WE 2008031000153 20080310 00153 SO 2008 3 10 SWIA200819277 1 20080223 A 2131 CONTROLLER EMB 120 EMB120ER 3260203 SO CABIN PRESSURE FAILED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 237SW 120314 FLT 3731 - ON FINAL DESCENT, AUTO PRESSURIZATION SYSTEM WENT INOP. REPLACED AUTO PRESSURIZATION CONTROLLER IAW 21-30-07 , P/N 222DIT011400 S/N OFF 290. 2 L 7 2 4T RT A31SO 2008031000160 20080310 00160 NM 2008 3 10 KCSA081136 1 20080304 A 5320 FITTING BOEING 747 747209B 138489B NM CARGO BAY CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 AFT PIT CARGO STOP O/B SUPPORT FITTING CRACKED AT BS 1908, RBL-47. 2 L 7 4 4F RT A20WE 2008040200162 20080402 00162 NM 2008 4 2 2008UALA01656 1 20080320 A 5720 65B1091664 FAIRING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT MLG DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 128UA 30023 ON ARRIVAL, FOUND RIGHT WING FIX GEAR DOOR FAIRING 1 INCH BY 4 INCH MISSING. REPAIRED AND REPLACED FAIRING. AC OK FOR S ERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200166 20080402 00166 EA 2008 4 2 TRAX200800475 1 20080326 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 FWD FLOORBEAM ANGLE AT FS 280 CORRODED. REMOVED CORRODED ANGLE. LOCATED & DRILLED NEW ANGLE IAW SRM 51-40-11. OK TO IN STALL. INSTALLED SERVICEABLE ANGLE IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008040200167 20080402 00167 EU 2008 4 2 2008UALA01659 1 20080324 A 3350 LAMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 463UA 1282 ROW 21 EEL LIGHT INOP. SUPPLEMENTAL DATA UPDATE CAUSE, LAMP INOP. RELAMPED ASSY. OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200171 20080402 00171 NM 2008 4 2 2008UALA01663 1 20080325 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 46 RH INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 FOUND EMERGENCY LIGHT ROW 46 RT INOP. RELAMPED EMERGENCY LIGHT. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200173 20080402 00173 EA 2008 4 2 TRAX200800443 1 20080320 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 AAR - BATH TUB FITTING AT RBL 9 CRACKED. REMOVED UNSERVICEABLE BATHTUB FITTING AT RBL 9. LOCATED HOLES IN NEW SERVICEA BLE BATHTUB FITTING IAW CRJ 200 SRM 51-40-11. OK TO INSTALL. INSTALLED NEW BATHTUB FITTING IAW 51-42-21, DR 15098. SE RVICEABLE FITTING P/N 600-31068-19, RB 13335. SUPPLEMENTAL SDR CLOSED 3/28/08. 2 L 7 2 4F RT A21EA 2008040200178 20080402 00178 NM 2008 4 2 2008UALA01668 1 20080320 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 537UA 25157 NR 2 RT EXIT SIGN SLIDE LIGHT INOP. CAUSE, SHORT IN WIRING AT LIGHT SIGN ASSY AND POSSIBLE FAULTY PROX SENSOR ASSOCIATE D WITH SYSTEM. REMOVED AND REPLACED DOOR SLIDE LT ASSY, AND DOOR GIRT BAR PROX SENSORS, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200182 20080402 00182 NM 2008 4 2 CALA0800276 1 20080310 A 5230 6547953 SKIN BOEING 737 7373T0 1384582 NM AFTCARGO DOOR UNKNOWN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 RE-SKIN AFT CARGO DOOR. WORK ACCOMPLISHED BY SL761. COMPLETED REPLACEMENT OF AFT CARGO DOOR OUTER SKIN IAW SRM 52-3 0- 01 (WEIGHT OF OLD SKIN 13.55 LB, WEIGHT OF NEWLY INSTALLED SKIN 17.85 LB, EQUALS TOTAL ADDITIONAL WEIGHT OF 4.35 LB.) 2 L 7 2 4F RT A16WE 2008040200190 20080402 00190 NM 2008 4 2 2008UALA01678 1 20080325 A 2612 D261217800006 FIRE LOOP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 NACELLE FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 845UA 1585 FIRE LOOP A FAULT DISPLAYED ON UPPER ECAM SCREEN, ENG 2. CREW COMMENTS, ENG 2 LOOP A FAULT ECAM CAME ON INTERMITTENT. DURING FIRST HOUR OF FLIGHT. SUPPLEMENTAL DATA UPDATE CAUSE, SHORT INSIDE LOOP. REPLACED FIRE LOOP A, ENG 2. OPS CHEC KED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200191 20080402 00191 EU 2008 4 2 2008UALA01679 1 20080322 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 446UA 834 CREW O2 IS LOW (1430PSI) FOUND ON 3SVC. SUPPLEMENTAL DATA UPDATE CAUSE, UNKNOWN. SERVICED CREW O2, LEAK CHECK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200192 20080402 00192 NM 2008 4 2 CALA0800279 1 20080305 A 5544 65C2584151 STRUCTURE BOEING 737 7373T0 1384582 NM RUDDER DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 RUDDER TRAILING EDGE HAS EXPOSED COMPOSITE APPROXIMATELY 8 INCHES FROM BOTTOM, RT SIDE. REPAIRED DAMAGE TO SUBJECT RUDD ER IAW CONTINENTAL EC/RA NO 5540-01246. 2 L 7 2 4F RT A16WE 2008040200193 20080402 00193 EU 2008 4 2 2008UALA01680 1 20080323 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 418UA 485 CREW OXYGEN SYSTEM-LOW, RECORD PRESSURE PRIOR TO SERVICING. CREW COMMENTS: O2 PRESS 1370 PSI. SUPPLEMENTAL DATA UPDATE CAUSE, UNKNOWN. SERVICED CREW O2 TO FULL. NO LEAKS WERE FOUND. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200196 20080402 00196 EU 2008 4 2 2008UALA01682 1 20080322 A 3510 MF100511 MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FIRST OBSERVER'S LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 484UA 1609 FIRST OBSERVERS O2 MASK IS LEAKING. SUPPLEMENTAL DATA UPDATE CAUSE, MASK LEAKING AT PORT. REPLACED F OBS MASK. OPS CH ECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030700156 20080307 00156 EU 2008 3 7 SIMA200806006 1 20080131 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 320AE 21854 5000 340B320 DURING MBV INSP, A PREVIOUS REPAIR ON FRAME 258 WAS FOUND CORRODED. REPAIR, REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. PERFORMED A CUTOUT, FABRICATED A REPAIR ANGLE, FILLER AND DOUBLER. CLEANED AND TREATED THE REPAIR PARTS AND INS TALLED. REPAIR DONE IAW SAAB 340 SRM (SRM 72LKS 3079 REV 50) CHAPTERS 53-70-30. 2 L 7 2 4T RT A52EU 2008030700159 20080307 00159 SW 2008 3 7 WGEA200800037 1 20080223 A 2710 271093901002 BELLCRANK ECLIPS EA500 ECLIPSEEA500 3350000 SW AILERONS BINDING E WGEA K NONE O OTHER IN INSP/MAINT 1 EA 27 141DJ 59 000055 INSPECT LEFT AND RIGHT AILERON BELLCRANKS FOR CONDITION AND SECURITY. INSPECTED AILERON CONTROLS FROM AFT SECTOR TO BEL LCRANK AND FOUND RIGHT BELLCRANK WITH EXCESSIVE FRICTION SEE NR-00002. REMOVED RIGHT AILERON TO GAIN ACCESS. REPLACED A ILERON JOINT FITTING ASSEMBLY WITH NEW UNIT IAW EA500 AMM 27-11-18. INSTALLED AILERON AND CHECKED FOR PROPER RIGGING IA W EA500 AMM 27-11-21. CHECKED AILERON SYSTEM FOR FRICTION, NO DEFECTS NOTED. 1 L 7 2 4J RT A00002AC 2008030700162 20080307 00162 SO 2008 3 7 CHQA200800042 1 20080225 A 3610 40303925SD O-RING EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL AFT AVIONICS BAY LEAKING A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 288SK 145461 CAE312717 IAH TO STL. DURING CLIMB THE CREW RECEIVED A BLEED 1 LEAK MESSAGE AT 4,000FT. THE MESSAGE DISAPPEARED AND THEN RETURNE D AT 8,000 FT. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE BLEED 1 SYSTEM FO R LEAKS AND REPAIRED A LEAKING JOINT IN THE AFT AVIONICS COMPARTMENT. AFTER REPLACING THE O-RING IN THE JOINT, THE BLEE D SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008030700175 20080307 00175 NM 2008 3 7 2008UALA00966 1 20080221 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY LIGHT ROW 5E INOP. RESECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700188 20080307 00188 EA 2008 3 7 TRAX200800317 1 20080225 A 5210 ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 858AS 7417 PAX DOOR FWD STAIR ANGLE CRACKED IN RADIUS. 2 L 7 2 4F RT A21EA 2008030700212 20080307 00212 NM 2008 3 7 2008UALA01012 1 20080223 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EEL INOP: SEAT 61L. SECURED LOOSE CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700250 20080307 00250 EU 2008 3 7 USAA920080491 1 20080220 A 5755 D5754148420000 HINGE PIN AIRBUS 320 A320232 3930326 EU NR 1 SPOILER CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AW 661 PIT - MAJOR REPAIR - C8 CHECK - LEVEL 2 CORROSION ON LEFT WING NR 1 SPOILER HINGE PIN. REPLACED LEFT WING NR 1 SPOILER HINGE PIN IAW A320 SRM 27-64-41. 2 L 7 2 4F RT A28NM 2008030700280 20080307 00280 NM 2008 3 7 2008UALA01034 1 20080225 A 2611 SMOKE WARNING AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CARGO BAY MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 828UA 1031 CARGO SMOKE TEST FAILS. CYCLE SYSTEM CB'S - ALL TESTED NORMAL AFTER. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030700293 20080307 00293 NM 2008 3 7 08FDEA00656 1 20080229 A 5320 146N54174 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 CORRODED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 916FD 24137 AFT CARGO FS 1400-1420 R.1610 HAS CORROSION ON FLOOR NUT PLATE STRIPS 3 PLACES, MARKED. CORROSION REMOVED FROM AFT CARG O FLOOR NUT PLATE STRIPS FROM STA 1400 TO STA 1420 IAW B757 SRM 51-10-02 REV 93. DEFECT FOUND EXCEED ALLOWABLE LIMIT PE R B757 SRM 53-00-53 REV 93, DAMAGE 1 FIG 101 DETAIL V. STRINGER R16.10 FROM STA 1400 TO STA 1420 REPLACED IAW B757 SRM 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008030700300 20080307 00300 NM 2008 3 7 2008UALA01036 1 20080225 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EXTERIOR CONTAMINATED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 386UA 24661 RIGHT LOWER FUSELAGE AFT OF LOWER WING TO BODY FAIRING EMERGENCY LIGHT HAS MOISTURE IN IT. CLEANED HOUSING AND DRAIN HO LE. INSTALLED NEW GASKET. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700310 20080307 00310 NM 2008 3 7 2008UALA01049 1 20080226 A 5230 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FWD CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 DENTED FORWARD CARGO DOOR EXTERNAL SKIN, 40 INCHES AFT OF FORWARD EDGE, 22 INCHES ABOVE BOTTOM EDGE. MAJOR REPAIR ACCOM PLISHED AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030700334 20080307 00334 NM 2008 3 7 DL764080300 1 20080229 A 8012 START VALVE BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 1 ENGINE INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 837MH 14489 14489 29710 706233 L ENGINE START VALVE FAILED TO OPEN. AIR PRESSURE WAS NORMAL-30PSI. VALVE DISAGREE LIGHT REMAINED ON. L ENGINE START VALVE FAILED TO OPEN. AIR PRESSURE WAS NORMAL-30PSI. VALVE DISAGREE LIGHT REMAINED ON. FWD TO MCO PLACARD PER MEL 80 -20-02. 2 L 7 2 4F 4 F RT A1NM E23EA 2008030700354 20080307 00354 NM 2008 3 7 2008UALA01079 1 20080228 A 5210 DIAPHRAGM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOOR ASSIST LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 849UA 1649 R2 DOOR ASSIST BOTTLE NOT HOLDING PRESSURE. FOUND ASSIST BOTTLE DIAPHRAGM LEAKING. REPLACED ASSIST BOTTLE DIAPHRAGM. LEAK CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030700361 20080307 00361 NM 2008 3 7 2008UALA00829 1 20080214 A 2701 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU UNKNOWN A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 332UA 24193 CREW REPORTS, YOKE HAS A BUMP WHEN MOVING. FULL FORWARD TO AFT APPROX 3 INCHES AFT OF THE ELEVATOR FORWARD STOPS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700363 20080307 00363 2008 3 7 SWAA081081 4 20080226 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR UNWANTED DEPLOY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 204WN 29855 R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008030700370 20080307 00370 NM 2008 3 7 SWAA081088 1 20080227 A 2560 65C16820 HOOK BOEING 737 7373K2 13844BA NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2008030700389 20080307 00389 NM 2008 3 7 SWAA081111 1 20080227 A 5322 6546536 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 559, STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008030700394 20080307 00394 NM 2008 3 7 SWAA081117 1 20080227 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031000161 20080310 00161 EA 2008 3 10 SWIA200819281 1 20080228 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE BINDING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 947SW 7786 FLT 6730, SERVICE DOOR IS DIFFICULT TO OPEN AND CLOSE. CLEANED AND LUBED DOOR SEAL. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008030700153 20080307 00153 NM 2008 3 7 2008UALA00937 1 20080220 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY EXIT EEL LIGHT INOPERATIVE AT SEAT 3A FWD LIGHT ASSY. RELAMPED EMERGENCY EXIT LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700171 20080307 00171 EA 2008 3 7 SWIA200819266 1 20080225 A 5220 ROD END CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 RIGHT EMERGENCY EXIT ACTUATING HANDLE AT PIN ROD ENDS ARE CORRODED. REPLACED CLEVIS PINS AND LUBED IAW 52-21-02. 2 L 7 2 4F RT A21EA 2008030700191 20080307 00191 EA 2008 3 7 TRAX200800321 1 20080225 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 PAX DOOR WILL NOT CLOSE PROPERLY. 2 L 7 2 4F RT A21EA 2008030700231 20080307 00231 EA 2008 3 7 TRAX200800342 1 20080227 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA CABIN UNSECURE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 FLIGHT ATTENDANT REPORTS "EXIT" PLACARD ON MAIN CABIN DOOR IS UNSECURE, FLT 4429 DEL 29 MINS. 2 L 7 2 4F RT A21EA 2008030700242 20080307 00242 NM 2008 3 7 USAA920080477 1 20080208 A 5320 65479576 WEB BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL VERTICAL WEB CRACKED, BS 818, S26R. REPL ACED AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL VERTICAL WEB, BS 818, S26R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008030700244 20080307 00244 NM 2008 3 7 USAA920080479 1 20080215 A 5320 284N102037 INTERCOSTAL BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 901AW 23321 MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL, BS 480, LBL 38.25, WL 208. REPLACED INTERCOSTAL, BS 480, LBL 38.2 5, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008030700248 20080307 00248 NM 2008 3 7 USAA920080483 1 20080207 A 5340 140N250532 ATTACH ANGLE BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 901AW 23321 MCN - MAJOR REPAIR - C12 CHECK - CRACKED CLIP, BS 660 - BS 680, BL 0, WL 208. REPLACED CLIP, BS 660 - BS 680, BL 0, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008030700258 20080307 00258 NM 2008 3 7 USAA920080515 1 20080226 A 5311 69719477 FRAME BOEING 737 737401 1384701 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 CLT - MAJOR REPAIR - RON CHECK - PILOTS WINDSHIELD OUTBOARD CORNER WINDOW POST FRAME CRACKED, BS 219.8. REPAIRED PILOTS WINDSHIELD OUT BOARD CORNER WINDOW POST FRAME, BS 219.8 IAW B737 SRM 53-10-01 REPAIR 10. 2 L 7 2 4F RT A16WE 2008030700263 20080307 00263 NM 2008 3 7 2008UALA01030 1 20080225 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FUSELAGE FRAME IS CRACKED IN E&E COMPT BS 380 1" INBOARD OF STR 26L ON FWD FACE OF FAIL SAFE CHORD. MAJOR REPAIR ACCOMPL ISHED: REMOVED DAMAGE. VERIFIED REMOVAL WITH HFEC. INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700267 20080307 00267 NM 2008 3 7 USAA920080522 1 20080211 A 5312 651758349 BULKHEAD BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED WEB, BS 178, RBL 5.7, WL 186. REPAIRED WEB, BS 178, RBL 5.7, WL 186 IAW B737 S RM 53-10-08-2R12. 2 L 7 2 4F RT A16WE 2008030700268 20080307 00268 NM 2008 3 7 USAA920080523 1 20080211 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED WEB, BS 178, BL 0, WL 190. REPAIRED WEB, BS 178, BL 0, WL 190 IAW B737 SRM 53- 10-08-2R12. 2 L 7 2 4F RT A16WE 2008030700270 20080307 00270 NM 2008 3 7 USAA920080525 1 20080215 A 5320 65C334192 WEB BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED SHEAR WEB, BS 1023 - BS 1040, BL 0 - RBL 38, WL 208. REPLACED SHEAR WEB, BS 10 23 - BS 1040, BL 0 - RBL 38, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008030700275 20080307 00275 NM 2008 3 7 2008UALA01033 1 20080226 A 5210 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L2 DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 A DENT WAS FOUND ON EXTERNAL SURFACE OF DOOR 2L FWD LWR CORNER. SUSPECT EQUIPMENT DAMAGE DUE TO LOADING OR UNLOADING AC . CUT OUT DAMAGE AND ACP HFEC FOR CRACKED FREE INSP. FABRICATED AND INSTALLED DOUBLER WORK IS ACP ON AMECO GFS 21480 AT HMV3. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008030700290 20080307 00290 NM 2008 3 7 08FDEA00653 1 20080229 A 5320 146N541613 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD STRINGER L2.90 FROM STA 1320 TO 1340 TO EVALUATE EXISTING REPAIR. EXISTIN G REPAIR FOUND NOT IAW B757 SRM 51-70-11 FIG 1 DETAIL I, II STRINGER L2.90 FROM STA 1320 TO STA 1340. REPLACED IAW B757 SRM 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008031000004 20080310 00004 SO 2008 3 10 SIMA200806302 1 20080229 A 3230 355022002 ELECTRONIC UNIT EMB 135 EMB135LR 3260305 SO MLG MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 721HS 145283 ON FLIGHT 4569, CREW REPORTED DURING TAKEOFF GEAR HANDLE WENT UP BUT THE GEAR DIDN'T. MSG WAS LANDING GEAR LEVER DISAGR EE. RETURN TO FIELD. DESCENT RATE AT 100 FT P MIN. LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. PERFORME D FIM TASK 32-32-00-810-803-A FOUND TO BE TRANSITORY CONDITION OF EXT/ RETRACTION AS PRECAUTION REMOVED AND REPLACED LEG U IAW EMB 135 AMM 32-32-01. NO FURTHER DEFECTS NOTED AT THIS TIME AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008031000021 20080310 00021 NM 2008 3 10 08FDEA00671 1 20080229 A 5320 143N55225 FLOOR SUPPORT BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 FLOOR SUPPORT FROM STATION 720 TO 740, LBL60, WL208, HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF SRM 53-00-51, FIG 101, DETAIL III LIMITS, L= 8 INCH, W= 2 INCH, D= 0.15 INCH, ORIGINAL MATERIAL THICKNESS .056". FABRICATED NEW FLOO R SUPPORT ON MAE TRAVELER NR T7/713361, FROM 7075-0-.056 B, HEAT TREATED TO T6. REMOVED AND REPLACED FLOOR SUPPORT (PN: 143N5522-5) IAW SRM 51-40-02. THIS IS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP ACTION REQUIRED. 2 L 7 2 4F RT A2NM 2008031000025 20080310 00025 NM 2008 3 10 KCSA081124 1 20080228 A 5347 SEAT TRACK BOEING 747 747209B 138489B NM COCKPIT CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 F/O AFT O/B SEAT TRACK IS CRACKED .5 INCH AT STOP. 2 L 7 4 4F RT A20WE 2008031000027 20080310 00027 NM 2008 3 10 KCSA081127 1 20080228 A 5420 ANGLE BOEING 747 747209B 138489B NM NR 3 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 NR 3 PYLON NAC STA-130 RT UPPER T-CHORD CRACKED .75 INCH. 2 L 7 4 4F RT A20WE 2008031000034 20080310 00034 NM 2008 3 10 CALA0800183 1 20080229 A 5322 6546550 SHEAR TIE BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 FOUND CORROSION AT AFT CARGO COMPARTMENT SHEAR TIE AT STA 787 LBL-4. REPAIRED SHEAR TIE AT STA 787 BETWEEN STRINGER 27L AND 27R PER SRM 53-00-07. 2 L 7 2 4F RT A16WE 2008031000035 20080310 00035 EA 2008 3 10 MASA200800172 1 20080227 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA SLAT SYSTEM MALFUNCTIONED A MASA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 508MJ 10087 ASH FLT 7174 DEN-SAT. PILOT DECLARED AN EMERGENCY INBOUND TO SAT DUE TO A SLATS FAIL CAUTION MESSAGE/SLATS FAILURE. MX RESET SYSTEM, INSPECTED AND FOUND NO FAULTS. 2 L 7 2 4F RT A21EA 2008031000037 20080310 00037 EA 2008 3 10 MASA200800174 1 20080227 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA DOOR STUCK A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651ML 7139 ASH FLT 7161 MSN-ORD, DIFFICULTY CLOSING THE DOOR, OUTER HANDLE GOT STUCK. MX FREED UP THE DOOR AND INSPECTED, OPS CHEC KED GOOD WITH NO DAMAGE OR FAULTS NOTED. 2 L 7 2 4F RT A21EA 2008031000040 20080310 00040 EA 2008 3 10 MASA200800177 1 20080225 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DENTED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 77195 7195 FUSE SKIN DENT STA 327 & 335 STR 25-26R. REPAIRED FUSE SKIN. 2 L 7 2 4F RT A21EA 2008031000046 20080310 00046 EU 2008 3 10 08FDEA00676 1 20080303 A 5712 A57246401202 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CHAFING MARKS ON LT WING LEADING EDGE STRUCTURE, SLAT JACK NR 1 INNER RIB HOLE EDGE. REPAIR PERFORMED BY BLEND OU T TO SMOOTH CONTOUR AND NDT FOR CRACK FREE CONDITION IAW RAS/BAE/1006441/2008 ISS A, APPROVED BY EA 6-5741-114935. 2 L 7 2 4F RT A35EU 2008031000047 20080310 00047 EU 2008 3 10 08FDEA00677 1 20080303 A 5754 RIB AIRBUS AIRBUS 300 A300B4622R 3930312 EU NR 2 SLAT CHAFED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 745FD FW1489 668 FOUND CHAFING MARKS ON RT SLAT NR 2 LEADING EDGE, RIB 5-15. REPAIR PERFORMED BY BLEND OUT IAW RAS/FOK/026/2008 ISS A, A PPROVED BY EA 6-5743-115268. 2 L 7 2 4F RT A35EU 2008031000049 20080310 00049 EU 2008 3 10 08FDEA00679 1 20080303 A 4980 A4987040000600 MUFFLER AIRBUS 310 A310203 3930313 EU APU CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 APU TAIL CONE EXHAUST PIPE IS CRACKED AND TORN APPROXIMATELY 6 FT INSIDE THE TAILCONE AT THE 6 O'CLOCK POSITION. REPLA CED APU EXHAUST MUFFLER WITH A NEW EXHAUST MUFFLER IAW REF 49-81-15-4. 2 L 7 2 4F RT A35EU 2008031000050 20080310 00050 EU 2008 3 10 08FDEA00680 1 20080303 A 5522 SKIN AIRBUS 310 A310203 3930313 EU LT ELEVATOR DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 THE LT ELEVATOR LOWER SURFACE TE APPROXIMATELY 4" FROM THE TE TO APPROXIMATELY 18 INCHES FROM THE TE; STA 276 ER 8 TO ST A 291 ER 9 IS DELAMINATED. UPON FURTHER INVESTIGATION FOUND THE AREA TO BE PREVIOUSLY REPAIRED PER EA 6-5520-118195 PT 1. NO DELAMINATION NOTED. 2 L 7 2 4F RT A35EU 2008031000051 20080310 00051 NE 2008 3 10 HALA0800364 2 20080302 A 7230 BLADE BOEING 767 7673G5 1385126 NM PWA PW4062 PW4062 NE NR 2 ENGINE NICKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 729124 NR 2 ENG FOUND NR 18 BLADE NICKED ON LEADING EDGE 6" FROM TIP. BLENDED DAMAGE 3/16" DEEP PER AMM 72-31-02-308-003, FIG 804 TO WITHIN REPAIRABLE LIMIT FOR AREA C. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031000052 20080310 00052 NM 2008 3 10 HALA0800363 1 20080302 A 3040 6240663 CONTROLLER BOEING 767 7673G5 1385126 NM WINDSHIELD HEAT FAULTY A HALA D RETURN TO BLOCK M OVER TEMP TX TAXI/GRND HDL 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEMS: F/O'S WINDSHIELD HOT TO TOUCH. SUSPECT HEAT CONTROL MALFUNCTION. REMOVED AND REPLACED RT WI NDOW HEAT CONTROL UNIT PER AMM 30-41-01. REPOSITIONED WIRES TO SPARE SENSOR PER FIM TBK11192, REPOSITIONED WIRES BACK, CLEANED PER FIM TB141 193. OPS CHECKED GOOD PER AMM 30-41-00. 2 L 7 2 4F RT A1NM 2008031000057 20080310 00057 NM 2008 3 10 SB08010 1 20080302 A 3397 WIRE BOEING 737 7374B7 1384702 NM EMERGENCY LIGHTS BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 455UW 24997 DFW - MAINTENANCE REPORTED THE LOW LEVEL EMERGENCY PATH LIGHTING AT SEAT ROWS 14 AND 15, LEFT SIDE, INOPERATIVE. MAINTE NANCE REPAIRED BROKEN WIRES ON SEAT ROWS 14 AND 15, LEFT SIDE. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008030700320 20080307 00320 NM 2008 3 7 2008UALA01054 1 20080227 A 5411 FRAME BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 PYLON WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 WEAR WAS FOUND AT FRAME OF NR 1 STRUT AFT FAIRING SAF STA 362 (OUTBOARD SIDE). 2 L 7 2 4F 4 F RT T0001SE E46NE 2008030700352 20080307 00352 NM 2008 3 7 2008UALA01066 1 20080227 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 CABIN DOOR 1L UPPER HINGE CUTOUT HAS 2 EA FASTENER HOLES CRACKED, JUST AFT OF BS 303. MAJOR REPAIR: FABRICATED AND INST ALLED EXTERNAL SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700368 20080307 00368 NM 2008 3 7 SWAA081086 1 20080227 A 3350 MS155721 LIGHT BOEING 737 7373K2 13844BA NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008030700395 20080307 00395 NM 2008 3 7 SWAA081105 1 20080227 A 3232 69446915 ACTUATOR BOEING 737 737301 1384611 NM LT MLG FAULTY A SWAA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 29 659SW 23229 CREW REPORTED LT MLG DID NOT EXTEND WITH GEAR HANDLE. CYCLED GEAR HANDLE RED LIGHTS REMAINED ILLUMINATED. LOWERED LT M LG MANUALLY. REMOVED AND REPLACED UPLOCK ACTUATOR AND TRANSFER CYLINDER PER MM. 2 L 7 2 4F RT A16WE 2008031000007 20080310 00007 WP 2008 3 10 NWAA080789952 1 20080301 A 3350 FUSE DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 916RW 47144 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN LIGHT FOR THE AFT RIGHT OVERWING HATCH WAS INOPERATIVE . MAINTENANCE REPLACED THE ASSOCIATED FUSE IN THE PERTINENT CIRCUIT BOARD. OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2008031000013 20080310 00013 SO 2008 3 10 FDKA200802078 1 20080224 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM FLT 5997 RDU (0840 PHX LCL). CABIN EMERGENCY LIGHT OUT AT ROW 12. MX INSPECTED AND FOUND A LOOSE CONNECTOR. RESEC URED CONNECTOR AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008031000016 20080310 00016 NM 2008 3 10 KCSA081121 1 20080227 A 5320 ANGLE BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 ANGLE AT BS 1480 LBL 25 FLOOR LEVEL IS CRACKED .5 INCH. 2 L 7 4 4F RT A20WE 2008031000018 20080310 00018 NM 2008 3 10 08FDEA00661 1 20080229 A 5720 6516101 SUPPORT BEAM BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 NR 7 SPOILER FITTING TO FALSE SPAR ATTACHMENT REPAIR CRACKED AT WS 198. REMOVED ACTUATOR FITTING SRM 51-30-2. REPAIRED NR 7 SPOILER SUPPORT BEAM (FALSE SPAR) IAW DWG NR 5127-57-038 REV C. REINSTALLED SPOILER ACTUATOR FITTING IAW SRM 51-3 0-2. 2 L 7 3 4F RT A3WE 2008031000063 20080310 00063 EU 2008 3 10 F3LA200800076 1 20080228 A 5321 D5367228200200 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 913FR 5647 1863 DURING C4/S1 C CHECK, INSPECTION REPORTED DAMAGE AND CORROSION WAS FOUND ON AFT CARGO PIT, REINFORCED FLOOR PANEL 151ZG. MAINTENANCE REPAIRED THE FLOOR PANEL BY FABRICATING A NEW COVER SHEET FROM 2024-T3 AL IN ACCORDANCE WITH THE REQUIREME NTS OF E0 53-42-319-002 AND A319 SRM 51-44-11. FOLLOWING COMPLETION OF THE REPAIR, THE FLOOR PANEL WAS INSPECTED AND FO UND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008031000069 20080310 00069 NM 2008 3 10 SWAA081134 1 20080228 A 2913 623337 PUMP BOEING 737 7373H4 1384600 NM NR 1 ENGINE FAILED A SWAA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 SW 29 312SW 23334 AIR TURNBACK / DECLARED EMERGENCY. HYDRAULIC "A" SYSTEM FAILED IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC P UMP AND CASE DRAIN LINE PER MM. 2 L 7 2 4F RT A16WE 2008031000090 20080310 00090 NM 2008 3 10 GTIA0800037 1 20080229 A 2611 HORN AIRBUS A319 A319132 3930340 NM SMOKE DETECTION NO TEST A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 517NK 2711 MECH CALL HORN FAILED TO COME ON DURING AVX COMPARTMENT SMOKE DETECTION TEST. REPLACED HORN 15WC AND RELAY 4WC. OPS CH ECK GOOD. 2 L 7 2 4F RT A28NM 2008031000098 20080310 00098 WP 2008 3 10 IXXA08SMN071S 1 20080214 A 5753 SKIN DOUG DC8 DC871F 302199D WP TE FLAP DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD FLAP LOWER AFT SKIN HAS DENTS AT STATION XF 434.000. REMOVED FA STENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WI TH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1- 11, DC8 SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 4 T/R 57 - 94 DATED 10-01-02, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 4 T/R 57 - 94 ITEM "U" AND "Q", DC8 SRM 51-1-9 T/R 51 - 142 AND 51-1-9A T/R 51, 141, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008031000145 20080310 00145 NM 2008 3 10 USAA920080549 1 20080208 A 5311 65465588 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 907, S9L AND S9R. REPAIRED FRAME BS 907, S9L AND S9R IAW USAIRWAYS EA 100286. 2 L 7 2 4F RT A16WE 2008031000157 20080310 00157 EA 2008 3 10 SWIA200819279 1 20080227 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 979SW 7954 FLT 5979 - EXIT SIGN BY MAIN CABIN DOOR IS BROKEN. INSTALLED NEW EXIT SIGN LIGHT ASSEMBLY BY MAIN CABIN DOOR IAW MM 32- 51-00. LIGHTS OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008031000164 20080310 00164 EA 2008 3 10 SWIA200819283 1 20080222 A 5610 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 766SK 10232 FLT 6628, CAPTAIN'S SIDE WINDOW IS CRACKED. REPLACED CAPTAIN'S SIDE WINDOW IAW MM 56-12-01, P/N NP139322-11, SN/OFF 051 86H4536. 2 L 7 2 4F RT A21EA 2008031000169 20080310 00169 NM 2008 3 10 CALA0800186 1 20080206 A 5313 6552928102 STRINGER BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 STA 986 STRINGER 27L CORRODED FORWARD AFT SIDE OF FRAME. REPAIRED PER ECRA 5330-03781. 2 L 7 2 4F RT A16WE 2008031000171 20080310 00171 NM 2008 3 10 CALA0800187 1 20080211 A 5320 65C51624 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 CORROSION ON INTERNAL BONDED STRAP BETWEEN STRINGER 27L AND 27R JUST FORWARD OF STA 986.5 FRAME. REPAIR PER ECRA 5330-0 3781. 2 L 7 2 4F RT A16WE 2008031000173 20080310 00173 EA 2008 3 10 SWIA200819288 1 20080301 A 3150 LIGHT CNDAIR CL600 CL6002B19 1900309 EA FIRE BOTTLE INOPERATIVE A SWIA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 NM 07 912SW 7595 FLT NR 1000, LEFT ENGINE FIRE BOTTLE "PUSH TO DISCHARGE" LIGHT WILL NOT ILLUMINATE. CLEANED AND RESEATED SWITCHLIGHT AS SEMBLY. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008031000174 20080310 00174 EA 2008 3 10 SWIA200819289 1 20080229 A 2701 BEARING CNDAIR CL600 CL6002B19 1900309 EA YOKE ROUGH A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 965SW 7871 FLT 5802 - RESISTANCE FELT IN THE FIRST OFFICERS YOKE AILERON MOVEMENT. REPLACED THE CONTROL YOKE SHAFT SUPPORT BEARING S IAW MM 27-11-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008031000175 20080310 00175 NM 2008 3 10 CALA0800188 1 20080206 A 5322 65C80735 SHEAR TIE BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 STA 986 FRAME TO SKIN ATTACHEMENT LEG CORRODED I/B OF STRINGER 27L. REMOVED AND REPLACED SHEAR TIE AT STA 986 STRINGER 27L PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008031000176 20080310 00176 EA 2008 3 10 SWIA200819290 1 20080301 A 2510 HOLDER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT SHORTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 943SW 7762 FLT 5879 - FIRST OFFICERS CHART HOLDER IS SHORTING OUT. TIGHTENED CHART HOLDER HARDWARE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008031000177 20080310 00177 SO 2008 3 10 SWIA200819291 1 20080229 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 215SW 120281 FLT 3679 - EMERGENCY EXIT LIGHT OVER ROW 9 IS INOP. REPAIRED WIRE ON OVERHEAD BIN IAW 20-00-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008031000178 20080310 00178 NM 2008 3 10 CALA0800189 1 20080228 A 5320 141T5107 FLOOR SUPPORT BOEING 767 767424ER 1385270 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59053 29448 CABIN STA 303 LBL 20 TO 40 FLOOR SUPPORT FOUND CORROSION. REPAIR PER SRM 53-00-51. 2 L 7 2 4F RT A1NM 2008031000181 20080310 00181 NM 2008 3 10 CALA0800191 1 20080303 A 2560 ACREM1A MEGAPHONE BOEING 737 737724 13844BY NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16713 28784 WHILE DOING SERVICE CHECK FOUND FORWARD L-1 DOOR MEGAPHONE INOP. REMOVED AND REPLACED MEGAPHONE WITH SERVICEABLE UNIT. 2 L 7 2 4F RT A16WE 2008031000186 20080310 00186 NM 2008 3 10 DHL2008763505 1 20080301 A 5311 FRAME BOEING 727 727264 138408M NM BS 520 S16-17R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 FRAME GOUGED AND DENTED AT BS 520, ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 707 5T6, .063 INCH BY 7.25 INCH BY 3.25 INCH, PO NR 9006027, PER B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2008031000187 20080310 00187 NM 2008 3 10 DHL2008763506 1 20080301 A 5311 FRAME BOEING 727 727264 138408M NM BS 540 S16-17R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 FRAME GOUGED AND DENTED AT BS 540, ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 707 5T6, .063 INCH BY 7.25 INCH BY 3.25 INCH, PO NR 9006027, PER B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2008031000189 20080310 00189 NM 2008 3 10 DHL2008763507 1 20080301 A 5311 FRAME BOEING 727 727264 138408M NM BS 560 S16-17R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 FRAME GOUGED AND DENTED AT BS 560, ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 707 5T6, .063 INCHES BY 7.25 INCHES BY 3.25 INCHES, PO NR 9006027, PER B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2008031000192 20080310 00192 NM 2008 3 10 08FDEA00478 1 20080218 A 5320 146N5447U13 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOOR BOARD STRUCTURE L7.55, STA 1460-1480, TO EVALUATE EXISTING REPAIR. EXISTING RE PAIR FOUND NOT IAW B757-200 SRM 51-70-11 FIG 1 DETAIL I, II REV 83 STRINGER L7.55, STA 1460-1480. REPLACED IAW B757-200 , SRM 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008031000198 20080310 00198 NM 2008 3 10 08FDEA00697 1 20080305 A 5230 6557204113 DEPRESSOR BOEING 727 727227 1384078 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 C2 DOOR FWD SEAL DEPRESSOR, 22 INCHES FROM TOP CORNER IS CRACKED. REPLACED FWD SEAL DEPRESSOR REF SRM 51-30-2. THIS I S CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008031000201 20080310 00201 NM 2008 3 10 HNAA0800092 1 20080215 A 2932 3031174001 SWITCH DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYS BROKEN A HNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 07 808EX 39864 299 DURING GEAR RETRACTION ALL GEAR DOOR AMBER LIGHTS AND NR 2 HYD ISO VALVE CAUTION LIGHT ILLUMINATED. HYDRAULIC QUANTITY AND PRESSURE WERE NORMAL. THE GEAR DID NOT EXTEND WHEN GEAR HANDLE WAS SELECTED DOWN. CREW PERFORMED ALTERNATE EXTENSI ON. REPLACED NR 2 HYDRAULIC SYSTEM RESERVOIR AND ISOLATION SWITCH. 2 H 7 2 4T RT A13NM 2008031000211 20080310 00211 EU 2008 3 10 08FDEA00707 1 20080305 A 5532 A5537247000000 PANEL AIRBUS 310 A310203 3930313 EU VERTICAL STAB DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 VERTICAL STABILIZER PANEL 325CR IS DELAMINATED. REMOVED DAMAGE, VERIFIED MAT. I D APPLIED PLYS, CURED, RESTORED FINISH IAW 55-33-13 & 51-77-00. 2 L 7 2 4F RT A35EU 2008031000213 20080310 00213 EA 2008 3 10 COMA0860148 1 20080226 A 2613 355862255 SENSING ELEMENT CNDAIR CL600 CL6002B19 1900309 EA RT FUSELAGE FAILED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 443CA 7539 FLIGHT 5104- EN ROUTE FROM BNA TO JFK RECEIVED ANTI-ICE DUCT WARNING MESSAGE. PERFORMED QRH, MESSAGE PERSISTED. EMERGE NCY DECLARED AND AIRCRAFT DIVERTED TO GSO AND LANDED SAFELY. REMOVED AND REPLACED RIGHT SIDE FUSELAGE SENSING ELEMENT ( A18WK). 2 L 7 2 4F RT A21EA 2008031000215 20080310 00215 EA 2008 3 10 COMA0860149 1 20080228 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 917CA 15821 7017 FLIGHT 5532 - RECEIVED FLAP FAIL CAUTION MESSAGE CAUTION ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PER FORMED SI-2-27I0001. REPLACED RIGHT SIDE BPSU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008031000217 20080310 00217 EA 2008 3 10 COMA0860151 1 20080301 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A COMA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 815CA 7397 FLIGHT 5104 - FLAPS FAIL CAUTION MESSAGE WHEN SELECTING FLAPS TO 8 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW-UP MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 2008031000219 20080310 00219 EA 2008 3 10 COMA0860153 1 20080301 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 819CA 7415 CORROSION FOUND ON WEB WHERE IT FASTENS TO COCKPIT FLOORBOARD TOP SUPPORT ANGLE AT FS 280.00 BETWEEN LBL 9 AND RBL 9. R EPAIRED COCKPIT THRESHOLD AT FS 280 USING EA 10-5310-02103 AND REO 601R-53-11-1355. 2 L 7 2 4F RT A21EA 2008031000220 20080310 00220 NM 2008 3 10 DHLA200800021 1 20080304 A 2612 FIRE WARNING BOEING 727 727225 1384077 NM APU BAY FALSE ACTIVATION A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 05 748DH 22440 DURING PUSH BACK ON GROUND, GOT INTERMITTENT FIRE BELL WARNING. FOUND LIGHT IN APU HANDLE ILLUMINATED. PERFORMED 1'S, PERFORMED CHECKLIST, CALL FIRE RESCUE AND HAD MX CHECK FOR FIRE. FIRE LIGHT IN HANDLE REMAIN ON. AS PER MAINT CONTROL APU OPERATION DEFERRED PER DMI CONTROL NR 31939, TRANSFERRED IAW ASTAR MEL 26-11. SPECIAL PROCEDURES C/W CAT C PLACARD. INSTALLED DROP DEAD 3/14. OPS CK APU FIRE DETECTION SYS, FOUND NO DEFECTS. APU FOUND TO BE SERVICEABLE IAW MM 26-15- 00. THIS CLEARS DMI 31939. PLACARD REMOVED, AIRCRAFT WAS GROUNDED. 2 L 7 3 4F A3WE 2008031000229 20080310 00229 EU 2008 3 10 TRAX200800345 1 20080227 A 5330 SKIN AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 CORROSION FOUND ON FUSELAGE SKIN UNDER 3 RIVETS HEAD AT FR 23B STRG 11 L. 2 H 7 2 4T RT A53EU 2008031000232 20080310 00232 SO 2008 3 10 BSYA2008008 1 20080304 A 2120 UNKNOWN PIPER PA31 PA31350 7103110 SO COCKPIT SMOKE E BSYA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 3590D 318052144 AIRCRAFT EN ROUTE FROM CPS TO BHM HAD SMOKE IN THE COCKPIT, RETURNED TO CPS. MAINTENANCE PULLED CIRCUIT BREAKER PANELS AND LOOKED ALL AROUND COCKPIT AND COULD NOT FIND ANY SIGNS OF BURNT WIRING OR ANYTHING ELSE THAT WOULD CAUSE SMOKE. 1 L 7 2 3O A20SO 2008031000233 20080310 00233 2008 3 10 BSYA2008009 4 20080304 A 3422 060001500 GYRO BEECH 58 58 1152740 CE COCKPIT FAILED E BSYA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 36673 TH1143 EN ROUTE FROM TEB TO HFD WHEN THE DIRECTIONAL GYRO QUIT AND FLAGED, DIVERTED INTO BDL. MAINTENANCE REMOVED AND REPLACED DIRECTIONAL GYRO (REMOTE), OPS CHECKS GOOD. 1 L 7 2 3O 3A16 2008031000236 20080310 00236 EA 2008 3 10 TRAX200800352 1 20080228 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 FOUND PAX DOOR BOTTOM STEP BROKEN. 2 L 7 2 4F RT A21EA 2008031000237 20080310 00237 EA 2008 3 10 TRAX200800353 1 20080228 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 FWD FLOOR EMERGENCY LIGHTS AND LEFT EMERGENCY DOOR EXIT LIGHT INOP. 2 L 7 2 4F RT A21EA 2008031000240 20080310 00240 EA 2008 3 10 TRAX200800350 1 20080227 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 CORROSION DAMAGE IN FWD MAIN AVIONICS BAY JUST FWD OF FS 280 FRAME AT NOSE JACK PAD SUPPORT STRUCTURE LHS (MARKED). REM OVED DIRT PRIMER AND PAINT, AT MARKED LOCATION, NO CORROSION FOUND INSPECTED LOCAL AREA NO CORROSION FOUND AT THIS TIME AT NOSE JACK PAD AREA. 2 L 7 2 4F RT A21EA 2008031000241 20080310 00241 NM 2008 3 10 KCSA081140 1 20080305 A 5420 STIFFENER BOEING 747 747209B 138489B NM NR 2 PYLON DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 NR 2 PYLON AT NAC STA-248 O/B LOWER STIFFENER DAMAGED. 2 L 7 4 4F RT A20WE 2008031000247 20080310 00247 EU 2008 3 10 AALA200800438 1 20080228 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80052 460 JFK - EMERGENCY LIGHT AT LEFT NR 2 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008031000252 20080310 00252 WP 2008 3 10 AALA200800430 1 20080227 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14551 53033 LGA - EMERGENCY FLASHLIGHT AT FORWARD JUMPSEAT HAS BROKEN SAFETY STRAP. REPLACED SAFETY STRAP FOR EMERGENCY FLASHLIGHT AT FORWARD JUMPSEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031000253 20080310 00253 WP 2008 3 10 AALA200800424 1 20080227 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 474 49649 MSP - EMERGENCY LIGHT AT SEAT ROW 10 MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 10. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031000255 20080310 00255 WP 2008 3 10 AALA200800380 1 20080222 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70529 49921 TPA - EMERGENCY LIGHT AT FORWARD BULKHEAD HAS BROKEN LENS. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD BULKH EAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031000258 20080310 00258 NM 2008 3 10 AALA200800393 1 20080223 A 3350 SIGN BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 177AN 32396 DFW - EMERGENCY LIGHT PLACARD AT RIGHT FORWARD DOOR INOPERATIVE. REPLACED PLACARD FOR EMERGENCY LIGHT AT RIGHT FORWARD DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008031000260 20080310 00260 NM 2008 3 10 AALA200800382 1 20080222 A 3230 841602 PSEU BOEING 757 757223 1384957 NM MLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 612AA 24488 LAS INFLIGHT T538/22FEB - CREW REPORTED LANDING GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER RETRACTION. RETURNED TO LAS AND LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SENSOR ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008031000262 20080310 00262 SO 2008 3 10 FDKA200803090 1 20080306 A 2430 BONDING STRAP EMB 145 EMB145LR 3260212 SO WING CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 835MJ 145353 THE BONDING STRAP ON PANEL 5732 IS CORRODED. THE DAMAGED STRAP HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008031000263 20080310 00263 NM 2008 3 10 KCSA081141 1 20080306 A 5311 FRAME BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 STA-2200 HAS CORROSION ON FRAME WEB LBL-40 FWD OF LEFT OUT FLOW VALVE. 2 L 7 4 4F RT A20WE 2008031000265 20080310 00265 NM 2008 3 10 AALA200800381 1 20080221 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 626AA 24584 MIA - EMERGENCY SLIDE LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY SLIDE LIGHT AT RIGHT NUMB ER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008031000269 20080310 00269 WP 2008 3 10 AALA200800388 1 20080222 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 289AA 49301 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 28 TO 30 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHE AD SEAT ROWS 28 TO 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031000270 20080310 00270 WP 2008 3 10 AALA200800389 1 20080222 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 289AA 49301 LGA - EMERGENCY LIGHTS AT FORWARD OVERWING EXIT SEAT ROW 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD OVERWING EXIT SEAT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031000273 20080310 00273 NM 2008 3 10 AALA200800398 1 20080224 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 DFW - EMERGENCY LIGHT AT LEFT NR 1 DOOR CLOSET AREA DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LEFT NR 1 D OOR CLOSET AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031000274 20080310 00274 WP 2008 3 10 AALA200800383 1 20080222 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 461AA 49566 MIA INFLIGHT T862/22FEB PBI TO ORD - CREW REPORTS NOSE GEAR WOULD NOT FULLY RETRACT AFTER TAKEOFF. LANDED MIA WITHOUT INCIDENT. ACCOMPLISHED NOSE GEAR SHOCK STRUT SEAL REPLACEMENT. 2 L 7 2 4F A6WE 2008031000276 20080310 00276 WP 2008 3 10 AALA200800390 1 20080222 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 289AA 49301 LGA - EMERGENCY LIGHTS AT OVERHEAD AISLE BETWEEN AFT LAVATORIES INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD AISLE BETWEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031000279 20080310 00279 WP 2008 3 10 AALA200800391 1 20080222 A 2560 P4010021000 BATTERY DOUG DC9 DC982 3022082 WP FLASHLIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7536A 49990 SFO - EMERGENCY FLASHLIGHT AT AFT CABIN INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT AFT CABIN. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031000280 20080310 00280 NM 2008 3 10 AALA200800399 1 20080224 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 DFW - EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031000281 20080310 00281 NM 2008 3 10 AALA200800401 1 20080224 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 DFW - EMERGENCY LIGHT AT SEAT 31C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031000283 20080310 00283 NM 2008 3 10 AALA200800402 1 20080224 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 DFW - EMERGENCY LIGHT AT SEAT 37C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 37C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031000284 20080310 00284 NM 2008 3 10 AALA200800403 1 20080224 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 DFW - EMERGENCY LIGHT AT SEAT 39C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 39C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008030700301 20080307 00301 2008 3 7 2008UALA01038 4 20080226 A 3160 DISPLAY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 536UA 25156 AFTER AIRCRAFT ARRIVED, RAMP PLUGGED GROUND POWER IN AND CREW NOTICED AN ACRID ODOR, FOUND UPPER CENTER EICAS CRT SCREEN BURNED UP AND RECEPTACLE ON AIRCRAFT BURNED PINS AND RUBBER INSULATION BURNED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008030700308 20080307 00308 NM 2008 3 7 2008UALA01047 1 20080227 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP, 4 EACH. RELAMPED EMERGENCY LIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700326 20080307 00326 NM 2008 3 7 NWAA070756309 1 20080221 A 5313 STRINGER BOEING 747 747451 1384940 NM BS 460 S10R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING "M" CHECK, FOUND CRACKS IN STRINGER 10R AT BS 460. REPAIRED PER EA 63-212199. 2 L 7 4 4F RT A20WE 2008030700329 20080307 00329 NM 2008 3 7 DL76L080296 1 20080229 A 5420 311T31571 ANGLE BOEING 767 767332 1382001 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 177DN 25122 NR 1 ENGINE PYLON MIDSPAR CLOSE OUT ANGLE FOUND CRACKED. REMOVED AND REPLACED CLOSE OUT ANGLE. 2 L 7 2 4F RT A1NM 2008031000036 20080310 00036 EA 2008 3 10 MASA200800173 1 20080227 A 3530 17696531 OXYGEN BOTTLE CNDAIR CL600 CL6002B19 1900309 EA PORTABLE O2 LOW A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 646BR 19900 7392 ASH FLT 1041 HNL-ITO. PORTABLE O2 BOTTLE WAS REPORTED AS DEPLETED. MX REPLACED THE PORTABLE O2 BOTTLE ASSEMBLY. 2 L 7 2 4F RT A21EA 2008031000045 20080310 00045 EU 2008 3 10 08FDEA00675 1 20080303 A 5754 SKIN AIRBUS AIRBUS 300 A300B4622R 3930312 EU NR 2 SLAT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD FW1489 668 FOUND SEVERAL SCRATCHES ON LT SLAT NR 2 UPPER SKIN TRACK RIB 5 REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS IAW RAS/F OK/025/2008 ISS A, APPROVED BY EA 6-5743-114932. 2 L 7 2 4F RT A35EU 2008031000064 20080310 00064 WP 2008 3 10 IXXA08SMN049S 1 20080207 A 5551 SE085500093 FITTING DOUG DC8 DC871F 302199D WP ZONE 300 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER FITTING INTERCOSTAL SIDE CRACKED AT STATION XFS 60.0 00. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-1-21, D C8 SRM 51-1-8B, AND 51-3-1. 2 L 7 4 4F RT 4A25 2008031000074 20080310 00074 NM 2008 3 10 SWAA081123 1 20080228 A 5311 6545808 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 294, RBL 53, WL 208. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008031000086 20080310 00086 EU 2008 3 10 TRAX200800361 1 20080229 A 3350 LIGHT AEROSP ATR72 ATR72212 8680945 EU CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 633AS 344 ASD EMERGENCY LIGHT INOP. 2 H 7 2 4T RT A53EU 2008031000091 20080310 00091 SO 2008 3 10 C2XA08IA068 1 20080228 A 3213 23092005005 SHOCK ABSORBER EMB 145 EMB145EP 3260221 SO LT MLG LEAKING A C2XA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 13935 17399 680 145022 LFT - FLIGHT 2907 THE CREW REPORTED A THUMPING SOUND ON T/O DURING GEAR RETRACTION WITH AN AMBER HASH MARK INDICATOR FOR THE LEFT MAIN GEAR. THE CREW CYCLED THE GEAR AND THE SOUND REMAINED BUT THE INDICATION CLEARED. THE AIRCRAFT LANDED I N LFT WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE RE MOVED AND REPLACED THE LEFT HAND MAIN LANDING GEAR SHOCK ABSORBER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008031000113 20080310 00113 NM 2008 3 10 KCSA081133 1 20080302 A 5414 SKIN BOEING 747 747209B 138489B NM NR 4 PYLON DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 NR 4 PYLON I/B SKIN DAMAGED ALONG LOWER EDGE BETWEEN NAC STA 220 AND 239. 2 L 7 4 4F RT A20WE 2008031000118 20080310 00118 EU 2008 3 10 08FDEA00686 1 20080304 A 5311 FRAME AIRBUS 310 A310324 3930206 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 FWD CARGO COMPT AT FR 36 AT RBL 29 FRAME CROSSBEAM IS CORRODED UNDER AND AROUND NUTPLATE. REMOVED CORROSION IAW SRM 51- 74-10. BLENDED AREA FOUND TO BE OUT OF LIMITS. REMOVED CENTER GUIDE; ROLLER TRAY AND LATERIAL WEB TO FOM IAW SRM 5 1-40-21. WEIGH DAMAGE & FABBED REPAIR PARTS IAW SRM 53-10-15. ALODINED IAW SRM 51-21-10. PRIMED & PAINTED REPAIR PARTS I AW SRM 51-23-10. INSTALLED REPAIR PARTS IAW SRM 53-10-15. REINSTALLED CENTER GUIDE; LATERIAL GUIDE & LATERIAL WEB IAW SRM 51-40-21. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008031000126 20080310 00126 NM 2008 3 10 USAA920080474 1 20080209 A 5320 65479765 CUSP WEB BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CORROSION ON MAIN CABIN FLOOR CUSP WEB, BS 800 - BS 827, S17L, WL 208. REPLACED MAIN CABIN FLOOR CUSP WEB, BS 800 - BS 827, S17L, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008031000136 20080310 00136 NM 2008 3 10 USAA920080540 1 20080228 A 5311 654655734 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - CRACKED FRAME, BS 887, S9L AND S9R. REPAIRED FRAME BS 887, S9L AND S9R IAW USAIRWAYS EA 100286. 2 L 7 2 4F RT A16WE 2008031000147 20080310 00147 EU 2008 3 10 USAA920080555 1 20080303 A 3210 D64433 PIN AIRBUS A319 A319112 3930323 EU ZONE 700 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 715UW 1051 DCA - MAJOR REPAIR - NOSE LANDING GEAR TORQUE LINK PIN CRACKED. REPLACED NOSE LANDING GEAR TORQUE LINK. 2 L 7 2 4F RT A28NM 2008031000159 20080310 00159 EA 2008 3 10 SWIA200819280 1 20080224 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX BINDING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 916SW 7634 MAIN CABIN DOOR IS HARD TO OPEN. INSPECTED, LUBED AND CLEANED MAIN CABIN DOOR LOCK AND UNLOCK ROLLER CAMS. DOOR OPERAT ES NORMALLY. 2 L 7 2 4F RT A21EA 2008031000197 20080310 00197 NM 2008 3 10 08FDEA00696 1 20080305 A 5230 6557204117 DEPRESSOR BOEING 727 727227 1384078 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 C2 DOOR AFT SEAL DEPRESSOR, 22 INCHES FROM UPPER CORNER IS CRACKED. REPLACED AFT SEAL DEPRESSOR REF SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008031000200 20080310 00200 NM 2008 3 10 08FDEA00699 1 20080305 A 5320 652954855 ANGLE BOEING 727 727227 1384078 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 MAIN DECK FLOOR DITCH PAN ASSY FWD AND AFT CHORD ANGLES ARE CRACKED, BS 1177 - 1183, RBL 47-64", WL 208. REMOVED RT DIT CHING PAN ASSY. FABRICATED ANGLES WITH PART NR`S 65-29548-11 AND 65-29548-55. FABRICATED AND HEAT ATTACH ANGLES (SHOP NR N00880/8130 FORM TRACKING NR 2008-02-231) PART NR 65-29548-18 AND INSTALLED DITCHING PAN ASSY REF BOEING DOCUMENT NR 65-29548. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008031000204 20080310 00204 EA 2008 3 10 COMA0870009 1 20080225 A 5270 895001 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA E&E BAY DOOR FAULTY A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 371CA 10082 FLIGHT 9651 - RECEIVED AVIONICS BAY DOOR CAUTION MESSAGE DURING TAKEOFF ROLL. ABORTED TAKEOFF APPROX 20 KTS AND RETURNE D TO GATE. REMOVED AND REPLACED PROX SENSOR (PX 41). 2 L 7 2 4F RT A21EA 2008031000209 20080310 00209 NM 2008 3 10 08FDEA00706 1 20080305 A 2430 SM600BA35N22 RCCB DOUG MD11 MD11F 3023600 NM DAMAGED A FDEA A UNSCHED LANDING G H MULTIPLE FAILURE ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 25 612FE 48605 A/P 1 KICKED OFF TWICE FL 360, GOT MOMENTARY FCC DATA FAULT ALERTS. A/P 2 OK, 5 MIN LATER GOT LVL 1 EMERG PWR ON ALERT, RECYCLED EMER PWR SW, ALERT RETURNED. DEPLOYED ADG, SELECTED ELEC MODE. DIVERT TO DEN. ON FINAL SLOWING THROUGH 170 KIAS A/P AND ATT FAILED LOST LEFT EMERGENCY BUS. INTEROGATED CFDS, EPCU FAULTED EMERG POWER RELAY INTERFACE. T/S PER M D11 FIM . FOUND RCCB FOR LT DC EMERG BUS B1-1754 OPEN AND SIGNS OF OVERHEATING AT TERMINAL A1. REMOVED AND REPLACED C/ B B1-1754 (LEFT EMERG DC FEED C/B). OPS CHECK NORMAL FOR LT EMERG BUSS AND EMER PWR TEST. FCC 1 RTS IS NORMAL. RETURN ED A/C TO SERVICE. 2 L 7 3 4F RT A22WE 2008031000225 20080310 00225 CE 2008 3 10 BSYA2008006 1 20080304 A 3230 LANDING GEAR LEAR 35 35A 5170602 CE RIGHT LACK OF LUBE E BSYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 25AN 35A259 AFTER TAKEOFF OUT OF LCK THE RIGHT MAIN INBOARD GEAR DOOR STAYED UNSAFE (LIGHT ON) ,PILOT RETURNED TO LCK. BROUGHT AIRC RAFT INTO WARM HANGAR, THAWED ICE OUT OF WHEEL WELLS, CLEANED AND LUBED GEAR AND OPS CHECKS GOOD. 2 L 7 2 4F A10CE 2008031000227 20080310 00227 EA 2008 3 10 TRAX200800363 1 20080228 A 5210 GATE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 861AS 7445 DIFFICULT CLOSING MAIN DOOR VENT FLAP WOULD NOT PULL SHUT. 2 L 7 2 4F RT A21EA 2008031000235 20080310 00235 NM 2008 3 10 NOCA01608 1 20080305 A 3397 WIRE BOEING 767 76739H 1385311 NM CABIN DAMAGED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 760NA 26257 EMERGENCY LIGHT INOP LEFT HAND SIDE FROM L1 DOOR TO L2 DOOR, CENTER AISLE AND L3 DOOR LOCATIONS AND LEFT HAND SECTION BY L3 DOOR. REPAIRED WIRING AS PER WIRING DIAGRAM 33-51-13 AND 33-51-16, ALL OPS CHECKED NORMAL. 2 L 7 2 4F RT A1NM 2008031000243 20080310 00243 SO 2008 3 10 FDKA200803085 1 20080303 A 3350 SIGN EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6104 MCO -TYS (0936 PHX LCL). ROW 12 EMERGENCY EXIT SIGN INOP. MX RESET SYSTEM AND PERFORMED OPS CHECKS. NO FURT HER DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008031000264 20080310 00264 NM 2008 3 10 AALA200800396 1 20080223 A 2761 15426001 ACTUATOR BOEING 767 767323 1385205 NM NR 10 SPOILER LEAKING A AALA J A DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 386AA 27060 MAN INFLIGHT T55/23FEB - CREW REPORTED CENTER HYDRAULIC SYSTEM FLUID LOSS. RETURNED TO MAN AND LANDED WITHOUT INCIDENT. REPLACED NR 10 SPOILER ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008031000266 20080310 00266 NM 2008 3 10 KCSA081142 1 20080306 A 5320 FITTING BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FITTING CRACKED 2 INCHES STA-1416 LBL-2 ABOVE VERTICAL STIFFENER. 2 L 7 4 4F RT A20WE 2008031000292 20080310 00292 NM 2008 3 10 AALA200800410 1 20080225 A 3040 CONTROLLER BOEING 737 737823 13844BZ NM WINDSHIELD HEAT ARCED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 961AN 30092 LBB INFLIGHT T1328/25FEB DFW TO SNA - LEFT NUMBER ONE WINDSHIELD ARCED AND CRACKED. LANDED LBB WITHOUT INCIDENT. REPLA CED LEFT NUMBER ONE WINDSHIELD AND HEAT CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008031000298 20080310 00298 NM 2008 3 10 AALA200800411 1 20080225 A 3040 CONTROLLER BOEING 757 757223 1384957 NM WINDSHIELD HEAT ARCED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 194AA 32388 IAH INFLIGHT T967/25FEB LAX TO MIA - RIGHT NUMBER ONE WINDSHIELD BEGAN TO ARC AND OUTSIDE PANE SHATTERED. LANDED IAH WI THOUT INCIDENT. REPLACED RIGHT NUMBER ONE WINDSHIELD AND HEAT CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008031000299 20080310 00299 NM 2008 3 10 AALA200800412 1 20080226 A 3350 0202503001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 NRT - EMERGENCY EXIT LIGHT AT FIRST CLASS GALLEY IS BROKEN. REPLACED LENS FOR EMERGENCY EXIT LIGHT AT FIRST CLASS GALLE Y. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031000302 20080310 00302 NM 2008 3 10 AALA200800418 1 20080227 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 343AN 33082 SFO - EMERGENCY LIGHT AT L389 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT L389. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A1NM 2008031000303 20080310 00303 NM 2008 3 10 AALA200800419 1 20080227 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 343AN 33082 SFO - EMERGENCY LIGHT AT L645 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT L645. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A1NM 2008031000305 20080310 00305 NM 2008 3 10 AALA200800422 1 20080227 A 3350 6011779 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9413T 53188 LAX - OVERWING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT B5 125 FOR OVERWING EXTERIOR EMERGENCY L IGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2008031000306 20080310 00306 EU 2008 3 10 AALA200800423 1 20080227 A 3350 OL3229BPE LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 JFK - EMERGENCY EXIT SIGN LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT R IGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008031000309 20080310 00309 NM 2008 3 10 AALA200800435 1 20080228 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 687AA 25695 DFW - EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP B7 FOR EXTERIOR EMERGENCY LIGHT AT R IGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008031000323 20080310 00323 EA 2008 3 10 TRAX200800348 1 20080227 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 CORROSION DAMAGE ON FLOORBOARD SUPPORT ANGLE IN MAIN AVIONICS BAY AT FS 280.00 (MARKED). REMOVED PRIMER AND PAINT BLEND ED MILD CORROSION PER SRM 53-00. REMOVED APPROX .002 ". REPRIMED AND PAINTED PER SRM 51-25-00. 2 L 7 2 4F RT A21EA 2008031000325 20080310 00325 NM 2008 3 10 08FDEA00482 1 20080218 A 5320 146N54173 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD STRINGER R10.45, STA 1420-1440 TO EVALUATE EXISTING REPAIR. EXISTING REPA IR FOUND NOT IAW B757-200 SRM 51-70-11 FIG 1, DETAIL I, II. AFT CARGO FLOORBOARD STRINGER R10.45 REPLACED IAW B757-200 SRM 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008031000326 20080310 00326 EU 2008 3 10 J1Q2008F00000 1 20080201 A 3010 60503104509 HOSE AMD FALC20 FALCON 2720302 EU GARRTT TFE731 TFE731* 01518 WP ANTI-ICE SYSTEM DISCONNECTED E J1QA O OTHER O OTHER IN INSP/MAINT 1 GL 15 724JC 310 UPON TROUBLESHOOTING, A PILOT SQUAWK (NO GREEN LIGHT, ON WING ANTI-ICE) IT WAS FOUND THAT THE RT IB DROOP LEADING EDGE A NTI-ICE HOSE HAD COME DISCONNECTED FROM THE IB CONNECTION. THIS RESULTED IN VISIBLE HEAT DAMAGE TO THE SMALL WIRE BUNDL E, DISCOLORATION TO THE AILERON TORQUE TUBE AND A SMALL KINK IN THE HOSE ITSELF. OPERATOR RECOMMENDS VISUALLY INSPECTIN G HOSES AND THEIR CLAMPS FOR CORRECT INSTALLATION AND TIGHTNESS. VERIFY CLAMPS INSTALLED ARE THAT OF A SAFETY REQURIED CLAMP. (K) 2 L 7 2 4F 4 F A7EU E6WE 2008031000328 20080310 00328 NE 2008 3 10 DJFA2008006 2 20080121 A 7321 79015510 HMU BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE ENGINE OUT OF ADJUST E DJFA E ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 EA 23 712TA 451 RK186 PCEJA0013 DURING TAXI, PRIOR TO FLIGHT, WHILE PERFORMING THE EFC AUTHORITY CHECK THE NR1 ENGINE SHUTDOWN. MAINT FOUND THE NR1 HMU OUT OF ADJUSTMENT. THE HMU WAS ADJUSTED IAW THE MM AND THE ENGINE OPERATIONAL CHECK WAS SUCCESSFUL. 2 H 7 2 4F 4 F RT A16SW E25EA 2008031000329 20080310 00329 CE 2008 3 10 AMWA89551BC 1 20080110 A 2430 51538001A GCU BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA RIGHT MALFUNCTIONED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 135YV 13539 13539 UE135 DURING FLIGHT THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED. MAINT PARALLELED BOTH GCU'S AND CLEARED DISCREPANCY. 2 L 7 2 4T 3 T RT A24CE E4EA 2008031000347 20080310 00347 NM 2008 3 10 AMTA200800068 1 20080209 A 4990 OIL CAP BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE APU LOOSE A AMTA K NONE K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 518AT 27974 APU SHUTDOWN AFTER ENGINE SHUTDOWN AT THE GATE, APU FAULT LIGHT CAME ON. PERFORMED APU LAST RUN BITE FOUND LOW OIL PRES S FAULT, FOUND OIL CAP NOT SECURED, ADDED 4 QTS, RESECURED CAP, RAN APU, PERFORMED EXTERNAL LEAK NO LEAKS NOTED. APU OP S CHECK NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008031000348 20080310 00348 NM 2008 3 10 AMTA200800070 1 20080212 A 5320 TEE FITTING BOEING 737 73783N 13844HI NM BS 767 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 317TZ 28246 AFT CARGO COMPARTMENT (TEE) ON STA 767 WITH EXFOLATION CORROSION (BOTH SIDES) INCLUDED ALL RAIL ASSEMBLIES ON THIS STA. REPAIRED IAW EO 737-5300-08-A0007. ALODINE, PRIMED AND PAINTED IAW SRM 51-20-01. (K) 2 L 7 2 4F RT A16WE 2008031000354 20080310 00354 2008 3 10 AMTA200800100 4 20080215 A 2565 5WD230600203 SLIDE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL RIGHT DEPLOYED A AMTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 11 706TZ 241 241 46582 RT OVERWING DOOR SLIDE DEPLOYED NOT USED. REMOVED AND REPLACED DOOR SLIDE IAW 25-61-07. OK FOR SERVICE. (K) 2 L 7 3 4F 4 F A22WE A23EA 2008031000356 20080310 00356 NM 2008 3 10 AMTA200800103 1 20080217 A 3150 WARNING SYSTEM BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT MALFUNCTIONED A AMTA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 514AT 27971 AFTER PUSHBACK EICAS DISPLAYED (APU STAT NO STBY) MESSAGE. PERFORMED SYSTEM RESET IAW FIM 24-31-30, FIG 105, MESSAGE CL EARED, NO OTHER DEFECTS ON GROUND NOTED. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008031000357 20080310 00357 NM 2008 3 10 AMTA200800111 1 20080217 A 2560 SPRING BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE GIRT BAR FAILED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 560TZ 33525 R2 DOOR GIRT BAR LEAF SPRING FAILED TEST TO RETAIN SLIDE. REMOVED R2 DOOR DIRT BAR LEAF SPRINGS IAW 51-40-02. INSTALLE D R2 DOOR GIRT BAR LEAF SPRINGS (2EA) IAW SRM 51-40-02 AND MM256614 TEST TO RETAIN SLIDER RE-ACCOMPLISHED AND TEST GOOD IAW EO 757-52-AD-3166. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008031000367 20080310 00367 EA 2008 3 10 A6WA200840068 1 20080212 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE WING MALFUNCTIONED A A6WA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 31 467AW 7900 FLAPS FAIL CAUTION DISPLAYED ON FINAL APPROACH, COMPLIED WITH QRH BOTH FLAPS DISPLAYED 45 DEGREES. RESET FLAPS, OPS CHE CK OK IAW AMM 27-50-AND AWAC SUPLEMENT 98-018B. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000058 20080310 00058 NM 2008 3 10 QXEA200800198 1 20080208 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM STA 669-675 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - SUSPECT CORROSION ON LEFT INBOARD SEAT TRACK, TOP OUTBOARD SIDE AT APPROXIMATELY STATION X669 TO X675. REPAIRED IAW Q400 RD 8/4-53-884, SRM 51-40-10, 51-21-10, 51-25-10 AND 51-25-00. 2 H 7 2 4T RT A13NM 2008031000059 20080310 00059 EU 2008 3 10 MALA080033 1 20080301 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY FALSE ACTIVATION A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 453XJ 340B453 AVIONICS SMOKE LIGHT ILLUMINATED FOR 20 SECONDS AND THEN WENT OUT. REPLACED AVIONICS SMOKE DETECTOR. 2 L 7 2 4T RT A52EU 2008031000062 20080310 00062 WP 2008 3 10 IXXA08SMN042S 1 20080201 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1747 L16R MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT EXTERNAL DOUBLER RIGHT AFT LOWER FUSELAGE FORWARD OF AFT PRE SSURE BULKHEAD AT STATION FS 1747, LONGERON 16-5 RIGHT. REMOVED FASTENERS AS A NEEDED TO PERFORM REPAIR. REMOVED EXIST ING REPAIR DOUBLER. REMOVED DAMAGE AREA. FABRICATED REPAIR DOUBLER, INTERNAL FINGER DOUBLER, AND FILLER. CLEANED, TREA TED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, SRM 51-3-1, DC8 SRM 53 -2-1 FIGURE 7 SHEETS 1, 3, AND 5, DC8 SRM 51-1-21, SRM 51-1-20D, DC8 SRM 53-5-1 FIGURE 1 ITEM "D", AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008031000067 20080310 00067 NM 2008 3 10 SWAA081120 1 20080228 A 5320 6545819 WEB BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND NOSE W/W UPPER CEILING PANEL CUTOUT WEB CRACKED AT INBOARD AFT CORNER. REPAIRED WEB P ER ACO. 2 L 7 2 4F RT A16WE 2008031000070 20080310 00070 NM 2008 3 10 SWAA081127 1 20080228 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031000071 20080310 00071 NM 2008 3 10 SWAA081126 1 20080228 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER 4L CRACKED AT BS 887. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008031000073 20080310 00073 NM 2008 3 10 SWAA081124 1 20080228 A 5313 6551698 STRINGER SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2008031000082 20080310 00082 EU 2008 3 10 TRAX200800358 1 20080226 A 5313 STRINGER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 CORROSION FOUND IN LT W/W AT FR 27 ON SPECIAL STRINGER UPPER SKIN. 2 H 7 2 4T RT A53EU 2008031000088 20080310 00088 EA 2008 3 10 TRAX200800362 1 20080229 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA OVERWING INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 906EV 7642 FORWARD EMERGENCY LIGHT OVERWING IS INOP. 2 L 7 2 4F RT A21EA 2008031000089 20080310 00089 NM 2008 3 10 DHLA200800020 1 20080303 A 3350 132719 LIGHT BOEING 727 727214 138407R NM COCKPIT INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 GL 05 786AT 396 396 21692 COCKPIT EMERGENCY LIGHT ASSY INOP, BATTERIES OK. REMOVED AND REPLACED PER B727 MM 33-50-101 AND OPS CKS GOOD. AIRCRAF T WAS GROUNDED. 2 L 7 3 4F A3WE 2008031000096 20080310 00096 NM 2008 3 10 DHL2008763501 1 20080302 A 5347 BAC15201466 SEAT TRACK BOEING 727 727264 138408M NM BS 850-870 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 SEAT TRACK CORRODED AT FLANGE, BS 850-870, LBL 24. REMOVED TRACK SECTION, FABRICATED SECTION FROM BAC1520-1466, PO NR 7 30788, 15.75 INCHES LONG, AND INSTALLED PER B727 SRM 53-10-2 FIG 7, 53-10-5 FIG 1 AND 51-30-2. 2 L 7 3 4F A3WE 2008031000100 20080310 00100 2008 3 10 ARWA20080301 4 20080302 A 3416 20676370703 ALTIMETER DOUG DC10 DC1010 3022110 WP COCKPIT INTERMITTENT A ARWA O OTHER J WARNING INDICATION CL CLIMB 1 SO 19 68041 46900 FIRST OFFICER'S RADIO ALTIMETER HAS FLAG IN VIEW INTERMITTENT ON THE GROUND; OK IN FLIGHT. REMOVED AND REPLACED FIRST O FFICER'S ALTIMETER AND CHECK TEST FOUND NORMAL IN ACCORDANCE WITH M/M 34-42-02. 2 L 7 3 4F A22WE 2008031000105 20080310 00105 SO 2008 3 10 C2XA08SH041 1 20080229 A 5751 14569009410 FITTING EMB 145 EMB145XR 3260214 SO RT AILERON WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11127 145697 SHV - DURING C-CHECK IT WAS FOUND THAT THE RT AILERON PCA ACTUATOR ATTACHMENT FITTING ON THE AILERON SPAR HAD MIGRATED H AT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW CONTINENTAL EXPRESS EC 5750-01177. THE AIRCRAFT WAS APPR OVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008031000112 20080310 00112 SO 2008 3 10 C2XA08SH042 1 20080302 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14174 14500876 SHV - DURING C-CHECK THE LT OMEGA SHAPE (BEAM) WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE FABRICATED AND INSTALL ED A DOUBLER REPAIR TO THE AFFECTED AREA IAW EMB 145XR SRM 53-00-10 DETAIL A FIG 201. THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. 2 L 7 2 4F RT 2008031000114 20080310 00114 NM 2008 3 10 MWEA080037 1 20080227 A 3213 BUSHING BOEING 717 717200 1383700 NM LT MLG DAMAGED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 904ME 55168 LEFT MAIN LANDING GEAR INDICATION REMAINED RED AFTER RETRACTION. PERFORMED GEAR SWING, ALL LIGHTS NORMAL. LEFT HAND MA IN LANDING GEAR BOTTLE ACTUATOR ATTACH BUSHINGS ARE ELONGATED. REMOVED AND REPLACED BUSHINGS, TRUNNION RETRACT FITTING INBOARD CUP BUSHING IS WORN. REMOVED AND REPLACED FITTINGS. 2 L 7 2 4F TR A6WE 2008031000117 20080310 00117 NM 2008 3 10 ZZDA2008074 1 20080228 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 924AT 55080 SEATS 25 THRU 31 EMERGENCY LIGHTS INOPERATIVE. REMOVED & REPLACED EMERGENCY LIGHT BATTERY & PWR SUPPLY REF AMM 33-51. OPS CHECK GOOD. 2 L 7 2 4F TR A6WE 2008031000119 20080310 00119 NM 2008 3 10 ZZDA2008075 1 20080229 A 3397 CONNECTOR BOEING 717 717200 1383700 NM CABIN BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 929AT 55075 EMERGENCY LIGHTS AT ROWS 25-31 DEF INOPERATIVE. REPAIRED BROKEN CONNECTOR AT ROW 30 IAW WDM. SWAPPED BATTERY PACKS 123 & 119 IAW 33-51-03. OP CHECKS GOOD. 2 L 7 2 4F TR A6WE 2008031000123 20080310 00123 NM 2008 3 10 08FDEA00690 1 20080304 A 5330 2024T30050 SKIN BOEING 757 75727B 1384921 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 DEEP DENT PROTRUDED OUTWARD AT LT FWD EXT FUSELAGE ON STA 335, S-23L. EXTERNAL REPAIR CARRIED OUT ON LT FUSELAGE AT STA 335, S-23L IAW B757-200 SRM 53-00-01 REV 93 FIG 201 REPAIR 3. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008031000125 20080310 00125 WP 2008 3 10 08FDEA00692 1 20080304 A 5344 HINGE DOUG MD10 MD1010F 3022112 WP CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 AFT CARGO DOOR, INTERIOR SIDE OF THE HINGE IS RUSTED. AFTER REMOVING THE CORROSION FOUND HINGE P/N AFA3953-525 OUT OF L IMITS IAW SRM 52-10-00 FIG 8 VOL I. REMOVED (TO GAIN ACCESS TO REMOVE THE HINGE) AND REINSTALLED FASTENERS ON PARTIAL INTERNAL SKIN, GUARD ASSEMBLY AFA 7384-39. GUARD SUPPORTS (2 EA) AFA7384-9 & -15 AND HANDLE VENT DOOR SPRING BRACKET IA W SRM 51-31-01 VOL II. REMOVED AND INSTALLED NEW HINGE P/N AFA3953-525 IAW SRM 51-31-01; VOL II; 51-38-01; VOL II; PG 12 & DWG AFA3953. 2 L 7 3 4F RT A22WE 2008031000128 20080310 00128 NM 2008 3 10 USAA920080498 1 20080213 A 5320 65548625 WEB BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CORROSION ON AFT PRESSURE BULKHEAD EXPANSION SEAL WEB, BS 1038 - BS 1040, BL 0 - LBL 1 0, WL 210. REPLACED AFT PRESSURE BULKHEAD EXPANSION SEAL WEB, BS 1038 - BS 1040, BL 0 - LBL 10, WL 210 IAW B737 SRM 51- 40-02. 2 L 7 2 4F RT A16WE 2008031000129 20080310 00129 NM 2008 3 10 USAA920080499 1 20080223 A 5320 65548623 WEB BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CORROSION ON AFT PRESSURE BULKHEAD EXPANSION SEAL WEB, BS 1030 - BS 1034, LBL 24 - LBL 36, WL 210. REPLACED AFT PRESSURE BULKHEAD EXPANSION SEAL WEB, BS 1030 - BS 1034, LBL 24 - LBL 36, WL 210 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008031000134 20080310 00134 NM 2008 3 10 USAA920080538 1 20080222 A 5754 114T4112 WEDGE BOEING 767 7672B7ER 1385107 NM ZONE 500 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 253AY 24894 BFM - MAJOR REPAIR - C3 CHECK, LEFT WING NR 2 SLAT WEDGE DELAMINATED, WS 852.9 AND WS 879.2. REPAIRED LEFT WING NR 2 SL AT WEDGE, WS 852.9 AND WS 879.2 IAW B767 SRM 57-43-02. 2 L 7 2 4F RT A1NM 2008031000141 20080310 00141 NM 2008 3 10 USAA920080545 1 20080208 A 5311 65465292 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 440, S9L AND S9R. REPAIRED FRAME BS 440, S9L AND S9R IAW USAIRWAYS EA 100286. 2 L 7 2 4F RT A16WE 2008031000142 20080310 00142 NM 2008 3 10 USAA920080546 1 20080208 A 5311 654655211 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 827, S9L AND S9R. REPAIRED FRAME BS 827, S9L AND S9R IAW USAIRWAYS E A 100286. 2 L 7 2 4F RT A16WE 2008031000143 20080310 00143 NM 2008 3 10 USAA920080547 1 20080208 A 5320 146N52307 STIFFENER BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 901AW 23321 MCN - MAJOR REPAIR - C12 CHECK - CRACKED STIFFENER, BS 1600, RBL 49, WL 208. REPLACED STIFFENER, BS 1600, RBL 49, WL 2 08 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008031000146 20080310 00146 NM 2008 3 10 USAA920080554 1 20080303 A 5330 6545776 SKIN BOEING 737 737301 1384611 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 588US 23933 CLT - MAJOR REPAIR -RON - CRACKED FUSELAGE SKIN, BS 930 - BS 932, S25R. REPAIRED FUSELAGE SKIN, BS 930 - BS 932, S25R I AW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008031000149 20080310 00149 NM 2008 3 10 USAA920080557 1 20080210 A 5312 65C28106 STIFFENER BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CORROSION ON BULKHEAD STIFFENER CHANNEL, BS 1016, BL 0. REPAIRED BULKHEAD STIFFENER C HANNEL, BS 1016, BL 0 IAW B737 SRM 51-70-11. 2 L 7 2 4F RT A16WE 2008031000150 20080310 00150 NM 2008 3 10 ZZDA2008077 1 20080229 A 3350 D71701100 POWER SUPPLY BOEING 737 7377BD 1384511 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 336AT 36716 LEFT WIDE OVERWING AND GRAND ILLUMINATION EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY ASSY M1668, RE SECURED GROUND BLOCK, RELAMPED LT GROUND ILLUMINATION EMERGENCY LIGHT, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2008031000152 20080310 00152 NM 2008 3 10 USAA920080559 1 20080303 A 5311 90526911 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 727E, S9R. REPAIRED FRAME BS, 727E, S9R IAW USAIRWAYS EA 100286. 2 L 7 2 4F RT A16WE 2008031000154 20080310 00154 SO 2008 3 10 FDKA200802084 1 20080229 A 5230 14527016001 SPRING EMB 145 EMB145LR 3260212 SO CARGO DOOR CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 835MJ 145353 THE FORWARD AND AFT CENTERING GUIDE SPRINGS FOR THE CARGO DOOR ARE CRACKED. THE DAMAGED PART HAD BEEN REMOVED AND REPLA CED. 2 L 7 2 4T RT T00011AT 2008031000155 20080310 00155 NM 2008 3 10 KCSA081134 1 20080304 A 5311 FRAME BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE FRAME CRACKED IN AFT PIT AT BS 1620, LBL-82. 2 L 7 4 4F RT A20WE 2008031000162 20080310 00162 EA 2008 3 10 SWIA200819282 1 20080227 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE BINDING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 952SW 7805 FLT 6020 - SERVICE DOOR WOULD NOT OPEN. LUBED SERVICE DOOR SEAL. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2008031000165 20080310 00165 NM 2008 3 10 CALA0800184 1 20080229 A 5313 BAC1498156 STRINGER BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16703 28764 STRINGER 15L IN CABIN CRACKED JUST FORWARD OF WING ILLUMINATION LIGHT HOUSING APPROX BETWEEN STA 460-480. INSTALLED REP AIR PARTS PER SRM 53-00-03. 2 L 7 2 4F RT A16WE 2008031000167 20080310 00167 NM 2008 3 10 CALA0800185 1 20080229 A 5330 6545776 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 FORWARD SIDE OF STA 986 SKIN HAS CORROSION I/B OF STRINGER 27L. REPAIRED PER ECRA 5330-03781. 2 L 7 2 4F RT A16WE 2008031000168 20080310 00168 EA 2008 3 10 SWIA200819285 1 20080301 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX DIRTY A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 916SW 7634 FLT 6378 - PASSENGER DOOR IS DIFFICULT TO OPEN AND CLOSE. INSPECTED, CLEANED AND LUBED TORQUE TUBE LINKAGE AND CAMS. O PS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008030700145 20080307 00145 NM 2008 3 7 2008UALA00925 1 20080219 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY LIGHT ROW 39 LT INOP. RESECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700146 20080307 00146 SO 2008 3 7 SIMA200806001 1 20080215 A 5320 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 679AE 9357 5000 14500814 DURING A IMBV INSP,THE CENTER OMEGA BEAM BETWEEN FRAME 24 AND 25 WAS FOUND CORRODED. REPAIR, PERFORMED A CUT OUT OF THE OMEGA BEAM. FAB AN EXTERNAL ANGLE, FILLER AND SHIMS. CLEANED AND TREATED PARTS AND INSTALLED IN AIRCRAFT. WORK DONE IAW EMBRAER 145 SRM (SRM EMB-145/1142) CHAPTER 53-00-10 FIGURE 203. 2 L 7 2 4T RT T00011AT 2008030700152 20080307 00152 GL 2008 3 7 SIMA200806010 2 20080227 A 7200 ENGINE EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL NR 2 ODOR A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 707EB 145195 CAE311010 ON FLIGHT 4870, CREW REPORTED LAV SMOKE ON EICAS IMMEDIATELY AFTER TAKEOFF, NO SMOKE FOUND BY FA, STAYED ON FOR APPROX 5 MINS AND WHEN OFF. RETURN TO CMH. REMOVED AND REPLACED NUMBER TWO ENGINE RUN OPERATIONAL CHECKED GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008030700163 20080307 00163 SO 2008 3 7 CHQA200800045 1 20080228 A 3150 WARNING MESSAGE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BRAKE OVERHEAT FALSE ACTIVATION A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 271SK 145305 CAE311922 IAD TO BUF - AFTER ROTATION THE CREW RECEIVED A BRAKE OVERHEAT MESSAGE ON EICAS. THE LEFT OUTBOARD BRAKE WAS INDICATING FULL HOT. THE GEAR WAS NOT RETRACTED AND THE AIRCRAFT RETURNED TO IAD AND LANDED WITHOUT INCIDENT AT WHICH TIME THE TE MPERATURE INDICATION FOR THE LEFT OUTBOARD BRAKE RETURNED TO NORMAL. MAINTENANCE INSPECTED THE BRAKE AND THERE WERE NO DEFECTS FOUND WITH THE BRAKE SO THE INDICATION WAS PLACED ON MEL. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008030700167 20080307 00167 EA 2008 3 7 SWIA200819262 1 20080222 A 3250 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 907SW 7511 FLT 5966 - NOSE GEAR FAILED TO SHOW UP AND LOCKED. REPLACED LEFT AND RIGHT STEERING ACTUATORS PER 32-52-01 AND REPACKED NOSE STRUT AND SERVICED PER 32-21-25. 2 L 7 2 4F RT A21EA 2008030700168 20080307 00168 EA 2008 3 7 SWIA200819263 1 20080225 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 951SW 7795 PAX DOOR FLOOR EMERGENCY FLOOD LIGHT ASSEMBLY IS BROKEN. REPLACED PAX DOOR FLOOR EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51 -00. 2 L 7 2 4F RT A21EA 2008030700172 20080307 00172 NM 2008 3 7 2008UALA00964 1 20080220 A 3397 58791 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 333UA 24228 EEL FLOOR LIGHT STRIP INOP FROM ROW 9 TO 15. REPAIRED CUT POWER FEEDER CABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700214 20080307 00214 NM 2008 3 7 2008UALA01014 1 20080224 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY CEILING LIGHT NEAR DOOR 2L IS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700217 20080307 00217 NM 2008 3 7 2008UALA01016 1 20080224 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 DOOR 5R AFT SILL EMERGENCY LIGHT IS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008030700218 20080307 00218 EU 2008 3 7 TRAX200800334 1 20080226 A 5313 STRINGER AEROSP ATR72 ATR72212 8680945 EU RT MLG WW CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 CORROSION FOUND IN RT W/W AT FR 27 ON SPECIAL STRINGER UPPER SKIN. 2 H 7 2 4T RT A53EU 2008030700245 20080307 00245 NM 2008 3 7 USAA920080480 1 20080215 A 5320 140N25061 INTERCOSTAL BOEING 757 7572S7 1384962 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 901AW 23321 MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL/SHEAR WEB, BS 1320, LBL 24, WL 133 - WL 138. REPLACED INTERCOSTAL/ SHEAR WEB, BS 1320, LBL 24, WL 133 - WL 138 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008030700257 20080307 00257 EU 2008 3 7 2008UALA01026 1 20080224 A 2730 D9238006000060 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELEVATOR SYS DEFECTIVE A UALA O OTHER W INADEQUATE Q C CL CLIMB 1 WP 29 486UA 1620 F-CTL ELEV SERVO FAULT ECAM AFTER T/O. EXCESSIVE PLAY IN ROD END CONNECTOR(S). REPLACED LT BLUE ELEVATOR SERVO CONTROL UNIT (34CE3), TESTS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031000373 20080310 00373 EA 2008 3 10 AA6WA200840030 1 20080118 A 5420 SEPARATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT PYLON DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 QTY 1 SEPARATOR HAS FRETTING ON LT PYLON ACCESS PANEL 412DB. QTY (1) SEPARATOR REPLACED ON LT PYLON ACCESS PANEL 412DB IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000375 20080310 00375 EA 2008 3 10 A6WA200840070 1 20080125 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 AFT PRESSURE BULKHEAD CRACKED AT FS 621.00 AT LINTEL FITTING AREA. AFT PRESSURE BULKHEAD AT FS 621.00 AT LINTEL FITTING AREA REPAIRED IAW REO 601R-53-61-1230 REV D. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000376 20080310 00376 EA 2008 3 10 A6WA200840071 1 20080126 A 5320 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE EXTERNAL POWER CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 AC EXTERNAL POWER CONNECTOR BOX SUPPORT MEMBER BTW FS 193.00 - 202.00 RT SIDE IS CRACKED AT TOP FWD AND LWR AFT ATTACHME NT POINTS. TOP FWD AND LWR AFT CRACKS IN SUPPORT MEMBER TEMPORARILY REPAIRED IAW REO 601R-24-41-002 PERMANENT REPAIR TO BE CARRIED OUT AT NEXT C-CHECK SCHEDULED 3/8/08. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000383 20080310 00383 EA 2008 3 10 A6WA200840078 1 20080209 A 5240 PLATE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE SERVICE DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 431AW 4256 SERVICE DOOR PLATE ASSY CORRODED. (K) SERVICE DOOR PLATE ASSY REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000385 20080310 00385 EA 2008 3 10 A6WA200840080 1 20080207 A 5347 CARGO TRACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 431AW 7256 AT FS 574.00, WL 73.50 CARGO TRACKS LT AND RT SIDE INNER OUTER SURFACE CORRODED. (K) BLENDED CARGO TRACKS IAW SRM 51-1 2-00. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000387 20080310 00387 EA 2008 3 10 A6WA200840082 1 20080211 A 5310 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 469AW 7917 EXTERNAL AIR COUPLING DOOR FRAME CRACKED AND BENT. (K) REPAIRED IAW BSC EO 601R-53-14474A. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000395 20080310 00395 EA 2008 3 10 A6WA200840090 1 20080204 A 5230 ANGLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 ANGLE CRACK AT FS 621.0 AND MEMBER BEAM OF CARGO DOOR. (K) ANGLE REPLACED IAW SRM 51-2-16 AND 51-42-20. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031100005 20080311 00005 NM 2008 3 11 2008UALA00650 1 20080204 A 3350 210013 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 4L DOOR BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 529UA 25019 L-4 DOOR SURROUND PANEL, EMERGENCY SWITCH TEST IS BROKEN. FOUND DAMAGE TO EMER LIGHT TEST SWITCH. REPLACED EMER LIGHT TEST SWITCH, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031100006 20080311 00006 NM 2008 3 11 2008UALA00651 1 20080204 A 3350 2100102 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 4R DOOR BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 R-4 DOOR SURROUND PANEL (BLACK) EMERGENCY LIGHT BROKEN. REMOVED AND REPLACED R4 DOOR SLIDE LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031100011 20080311 00011 EU 2008 3 11 08FDEA00441 1 20080214 A 5321 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 MAIN DECK CARGO COMPARTMENT FLOORBOARD (SR30B5327071400200252) VF IS TORN. FABRICATED NEW FLOORBOARD PANEL NR 252 VF IA W SRZ 25-005 REV F. 2 L 7 2 4F RT A35EU 2008031100015 20080311 00015 NM 2008 3 11 2008UALA00931 1 20080218 A 3350 CAP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SEATS 1B & 1F MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 663UA 27160 END CAPS MISSING FROM EEL LIGHTING AT SEATS 1B AND 1F. INSTALLED END CAPS 2 L 7 2 4F 4 F RT A1NM E24NE 2008031200002 20080312 00002 CE 2008 3 12 DXTA20082904 1 20080228 A 3222 STRUT CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE NLG UNKNOWN E DXTA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 07 385QS 6800115 UPON GEAR RETRACTION, A THUMPING NOISE WAS COMING FROM THE NOSEWHEEL COMPARTMENT ALONG WITH A FLASHING RED UNLOCK LIGHT. PERFORMED SEVERAL GEAR RETRACTIONS AND EXTENSIONS. SERVICED UPPER AND LOWER BARREL (STRUT) PRESSURES. ALL SYSTEMS OP S CHECK GOOD. IAW MM CH 32-20-00. 2 L 7 2 4F 4 F RC T00012WI E35NE 2008031200013 20080312 00013 NM 2008 3 12 08FDEA00673 1 20080301 A 5347 A5A7082502 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 MAIN DECK CARGO SEAT TRACK AT STA 5-33, RT = 75.25 UNDER FLOOR PANEL FOUND FLANGE DAMAGED. REPAIR CARRIED OUT AT MAIN D ECK CARGO SEAT TRACK STA 5-33, RT=75.25 UNDER FLOOR PANEL FLANGE AS PER SRM 53-70-00 FIGURE 6 VOLUME I. REPAIR CLASSIFIE D AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008031200015 20080312 00015 EU 2008 3 12 F3LA200800077 1 20080303 A 2121 EVT3454H COOLING FAN AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE CABIN BINDING A F3LA A UNSCHED LANDING E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 807FR 56 2276 DURING CRUISE, AT 35000, FLT CREW REPORTED LOUD NOISE AND VIBRATION FOLLOWED BY ACRID ODOR AND SMOKE IN COCKPIT. ECAM D ISPLAYED BLOWER AND EXTRACTOR FAN FAULT. FLIGHT CREW DECLARED AN EMERGENCY, DIVERTED TO OKC AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED AVIONICS COOLING BLOWER, PERFORMED AVEC BITE TEST IN ACCORDANCE WITH AMM 21- 26-51 PB 401. RII ALSO PERFORMED. TEST RESULTS WERE NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT 2008031000048 20080310 00048 WP 2008 3 10 08FDEA00678 1 20080303 A 5320 ACA31371 FITTING DOUG DC10 DC1010F 3022111 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MODIFICATION DC10 FREIGHTER TO MD10 ACF, FOUND IN AIR CONDITION COMPARTMENT NR 3 RT SIDE STA 555 X= -96 Z=-37,50 THE END FITTING FRAME WITH CRACK. INSPECTED AREA AND REPLACED SUPPORT P/N ACA3137-1. 2 L 7 3 4F A22WE 2008031000055 20080310 00055 EU 2008 3 10 TRBA2008025 1 20080303 A 3350 3012000 POWER SUPPLY AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA K NONE L NO TEST IN INSP/MAINT 1 SO 29 425MJ 425 AFT FLOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AT 10B IAW MM 33-51-21. OPS CHE CKS NORMAL. 2 H 7 2 4T RT A53EU 2008031000077 20080310 00077 NM 2008 3 10 SWAA081131 1 20080228 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, LBL 22. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008031000080 20080310 00080 NM 2008 3 10 SWAA081128 1 20080228 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 2008031000087 20080310 00087 WP 2008 3 10 IXXA08SMN050S 1 20080207 A 5551 SE85500094 FITTING DOUG DC8 DC871F 302199D WP ZONE 300 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER FITTING INTERCOSTAL SIDE CRACKED XFS 60.000. REMOV ED CRACKED FITTING. PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-14 , AND 51-3-1. 2 L 7 4 4F RT 4A25 2008031000138 20080310 00138 NM 2008 3 10 USAA920080542 1 20080208 A 5311 65582802 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 360, S9L. REPAIRED FRAME BS, 360, S9L IAW USAIRWAYS EA 100286. 2 L 7 2 4F RT A16WE 2008031000170 20080310 00170 2008 3 10 SWIA200819286 4 20080228 A 2216 SERVO CNDAIR CL600 CL6002C10 1390015 EA AILERONS ROUGH A SWIA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 07 771SK 10244 FLT 6653 - CONTROL YOKE FEELS LIKE THE AILERONS ARE STICKING. REPLACED AILERON SERVO IAW CRJ MM 23-11-21. OPS CHECK GO OD, P/N: 622-4404-101, S/N OFF: 1RTYY. 2 L 7 2 4F RT A21EA 2008031000223 20080310 00223 EA 2008 3 10 COMA0860156 1 20080303 A 3232 AIR917103 DOOR ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA NLG LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 932CA 33286 7038 FLIGHT 5686 - RECEIVED NOSE DOOR OPEN MESSAGE ON CLIMBOUT FROM BOS TO DCA. AIRCRAFT DIVERTED TO IAD AND LANDED SAFELY. REMOVED AND REPLACED NOSE GEAR DOOR ACTUATOR. 2 L 7 2 4F RT A21EA 2008031000238 20080310 00238 NM 2008 3 10 KCSA081138 1 20080305 A 5714 SKIN BOEING 747 747209B 138489B NM CENTER TANK CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 CENTER TANK SKIN HAS CORROSION AT SUMP DRAIN AREA AT STA-1057 RBL-114. 2 L 7 4 4F RT A20WE 2008031000293 20080310 00293 NM 2008 3 10 AALA200800413 1 20080226 A 3397 WIRE BOEING 777 777223 1385213 NM EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 MIA - EMERGENCY LIGHTS AT FIRST CLASS GALLEY CLOSET AREA INOPERATIVE. FOUND OUTBOARD FIRST CLASS GALLEY CLOSET FRAME EM ERGENCY LIGHT WIRES BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHTS AT FIRST CLASS GALLEY CLOSET AREA. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031000312 20080310 00312 WP 2008 3 10 AALA200800425 1 20080227 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 474 49649 MSP - EMERGENCY LIGHT AT SEAT ROW 10 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 10. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031000318 20080310 00318 NM 2008 3 10 AALA200800432 1 20080228 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 755AN 30263 JFK - EMERGENCY LIGHT AT SEAT 22G HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031000339 20080310 00339 CE 2008 3 10 CTU2008F00000 1 20080128 A 5610 10138402524 WINDSHIELD BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA COCKPIT CRACKED E CTUA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 21 911ND BB589 AFTER DEPARTURE CLIMBING THRU 8000 FT MSL CREW HEARD A POPPING NOISE, NOTICED CO-PILOTS WINDSHIELD HAD CRACKED. NO EME RGENCY DECLARED, AC RETURNED TO AIRPORT. NO OTHER AIRCRAFT DAMAGE. TYPICAL WINDSHIELD FAILURE TOLAMINATED HEATED WINDS HIELD. (K) 1 L 7 2 4T 4 T A24CE E4EA 2008031000349 20080310 00349 NM 2008 3 10 AMTA200800080 1 20080212 A 5340 ATTACH FITTING BOEING 737 73783N 13844HI NM LAVATORY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 317TZ 28246 AFT IB ATTACHMENT BLOCK CORROSION IN LAV E. REMOVED AND REPLACED ATTACHMENT BLOCK IAW 25-46-99. (K) 2 L 7 2 4F RT A16WE 2008031000350 20080310 00350 NM 2008 3 10 AMTA200800082 1 20080212 A 5315 FLOORBEAM BOEING 737 73783N 13844HI NM BS 986 CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 317TZ 28246 FLOORBEAM CORRODED AROUND NUTPLATE HOLES AT SAT 986. 5 FROM BL0 THRU BL45R. REMOVED CORROSION AND FOUND OUT OF LIMITS I AW SRM 53-70-51 FIG 03. ACCOMPLISHED REPAIR WITH NR 2015516001 EA 737-5370-A0003. (K) 2 L 7 2 4F RT A16WE 2008031000351 20080310 00351 NM 2008 3 10 AMTA200800083 1 20080212 A 5320 CHANNEL BOEING 737 73783N 13844HI NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 317TZ 28246 FLOOR SUPPORT STRUCTURE HAS Z CHANNEL CORRODED AT BS 992 FROM BL33 TO BL 45L. REMOVED CORROSION IAW SRM 51-10-2 FROM LB L 33 TO LBL 45 ORIG THICKNESS .063 REMAIN .031. FOUND OUT OF LIMITS IAW SRM 53-70-51. FABRICATED FLOOR SUPPORT IAW EA 737-5300-08-0011 WORK ACCOMPLISHED WITH NR 2015692001. (K) 2 L 7 2 4F RT A16WE 2008031000378 20080310 00378 EA 2008 3 10 A6WA200840073 1 20080129 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 423AW 7636 DAMAGE ON LT FUSALAGE AT STA 220. REPAIRED CUTOUT ON LT FUSELAGE IAW REO 601R-53-11-1332. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000384 20080310 00384 EA 2008 3 10 A6WA200840079 1 20080211 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 431AW 7256 PILOTS BULKHEAD WEB IS CRACKED AT FS 280.00, WL 85.00 LBL 27.00. (K) REPAIRED WEB IAW SRM 51-71-28 FIGURE 2. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000388 20080310 00388 EA 2008 3 10 A6WA200840083 1 20080211 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 469AW 7917 LT FUSELAGE FRAME AT STR 654.00 HAS CHAFED BETWEEN STR 8L AND STR 9L FROM THE 10TH STAGE BLEED DUCT TIE ROD. (K) REPAI RED FRAME IAW BSC EO 601R-53-14477 BY TRIMMING OUT DAMAGE AND INSTALLING REPAIR ANGLE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000389 20080310 00389 EA 2008 3 10 A6WA200840084 1 20080202 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 LT LWR NOSE COMPARTMENT CRACK FOUND ON PRESSURE BULKHEAD AROUND BRAKE FS 202. (K) JOB PERFORMED IAW REO 601R-53-11-563. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031100010 20080311 00010 EU 2008 3 11 08FDEA00436 1 20080214 A 5320 A5361027093 SUPPORT ANGLE AIRBUS 300 A300F4605R 3930327 EU BS 972 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 AVIONICS COMPARTMENT STRUCTURE UNDER THE COCKPIT FLOOR, INTERCOSTAL AFT SUPPORT ANGLE CRACKED AT THE BEAM ATTACHMENT; BS 972, LBL 39. REMOVED SUPPORT ANGLE IAW SRM 51-40-10 & 51-23-10. FABBED ANGLE IAW SRM 51-40-44 & TPS 1003 REV A. AL ODINED, PRIMED & TOP COATED IAW SRM 51-21-10 & 51-23-10. PART MARKED IAW GMM 7-0-1000. INSTALLED ANGLE IAW SRM 51 -40-21. 2 L 7 2 4F RT A35EU 2008031200018 20080312 00018 NM 2008 3 12 DXTA20082916 1 20080305 A 2780 CE5001300009 ACTUATOR GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE KRUEGERS LEAKING E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 706QS 1661 131 AFTER TAKEOFF AND ON SPEED, RETRACTED KRUEGERS FROM FLAPS UP POSITION TO KRUEGER/SLATS UP POSITION. THE KRUEGER UNBAL CA S MSG ILLUMINATED WITH KRUEGER POINTER INDICATOR YELLOW. FOUND THE RT KRUEGER ACTUATOR TO BE LEAKING. REMOVED ACTUATOR AND REPLACED WITH INSPECTED KRUEGER ACTUATOR. PERFORMED A SATISFACTORY KRUEGER FLAP SYSTEM FUNCTIONAL TEST IN REF. TO G2 00 MM 27-52-00, NO DEFECTS NOTED. ACTUATOR REPLACED IN REF. TO MM 27-52-05. 2 L 7 2 4F 4 F RT A53NM E35NE 2008031200019 20080312 00019 CE 2008 3 12 DXTA20082918 1 20080305 A 3230 SHRADER VALVE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG FAILED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 937QS 7500137 AFTER TAKE-OFF INITIAL CLIMB GEAR HANDLE GEAR WOULD NOT RETRACT. TROUBLESHOT & FOUND NOSE STRUT NOT PROPERLY EXTENDED D UE TO LEAKING LOWER NOSE STRUT SERVICE VALVE. REPLACED LOWER NOSE STRUT SERVICE VALVE WITH A NEW VALVE & SERVICED NOSE S TRUT PER MM 12-10-78. VERIFIED PROPER OPERATION OF LANDING HEAR HANDLE IN AIR MODEL PER MM 32-30-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008031200024 20080312 00024 EU 2008 3 12 08FDEA00766 1 20080306 A 5540 A5547032500000 STRAP AIRBUS 310 A310203 3930313 EU RUDDER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RUDDER L/E PANEL NR 326 LL; BRIDGING STRAP IS CORRODED UNDER THE NUT PLATES. REMOVED AND REPLACED BRIDGING STRAP REFERE NCE A310-200 SRM 51-40-21; PARA 5. 2 L 7 2 4F RT A35EU 2008031200027 20080312 00027 NM 2008 3 12 UPS08551724 1 20080129 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM BS 1100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 435UP 25466 INSPECTION TYPE:C4 CORROSION ON UPPER SURFACE OF FLOORBEAM STA 1100 LBL-23-RBL-43 WL 208. REPAIRED PER ENGINEERING REPA IR NR 08-1204. 2 L 7 2 4F RT A2NM 2008031200028 20080312 00028 NM 2008 3 12 UPS08551725 1 20080218 A 5347 CARGO TRACK BOEING 757 75724APF 1384969 NM BS 1181-1175 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 456UP 25477 INSPECTION TYPE:C2 CORROSION ON SEAT TRACK UPPER SURFACE BS 1181-1175 LBL 60 WL 208. CORROSION OUT OF LIMITS PER SRM 53 -00-52-1A; REMOVED AND REPLACED TRACK. 2 L 7 2 4F RT A2NM 2008031200029 20080312 00029 NM 2008 3 12 UPS08551726 1 20080218 A 5321 FLOOR PANEL BOEING 757 75724APF 1384969 NM BS 1488 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 456UP 25477 INSPECTION TYPE:C2 MAIN CARGO COMPARTMENT FLOOR PANEL DENTED AT BS 1488 RBL 42 WL 208. REMOVED DAMAGED FLOOR PANEL, FAB RICATED REPLACEMENT PANEL. INSTALLED REPLACEMENT PANEL PER B757-5320-9692F M/M 25-55-04-4. 2 L 7 2 4F RT A2NM 2008031200030 20080312 00030 NM 2008 3 12 UPS08551727 1 20080218 A 5321 FLOOR PANEL BOEING 757 75724APF 1384969 NM BS 1488 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 456UP 25477 INSPECTION TYPE:C2 MAIN CARGO COMPARTMENT FLOOR PANEL DENTED BS 1488 RBL 55 WL 208. REMOVED DAMAGED FLOOR PANEL, FABRIC ATED REPLACEMENT PANEL. INSTALLED REPLACEMENT PANEL PER B757-5320-9692-F M/M 25-55-04-4. 2 L 7 2 4F RT A2NM 2008031200033 20080312 00033 2008 3 12 UPS08851718 4 20080226 A 2565 BOTTLE DOUG DC8 DC873F 302199F WP ESCAPE SLIDE LOW PRESSURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 ESCAPE SLIDE PRESSURE OUT OF GREEN BAND. DEFERRED PER MEL 52-7-4. REMOVED AND REPLACED EVACUATION SLIDE ASSY PER AMM 2 5-60-01-2. 2 L 7 4 4F RT 4A25 2008031200035 20080312 00035 WP 2008 3 12 UPS08851734 1 20080221 A 5540 56562267 ANGLE DOUG DC8 DC873F 302199F WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 RUDDER L ANGLE CRACKED, JUST ABOVE LOWER HINGE CUT-OUT AT BALANCE WEIGHT. REPAIRED CRACKED L ANGLE B Y FABRICATION AND INSTALLATION PER DWG 56562 26, SRM 51-3-0 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 2008031200038 20080312 00038 NM 2008 3 12 UPS08M51735 1 20080228 A 2841 INDICATOR DOUG MD11 MD11F 3023600 NM FUEL SYSTEM INOPERATIVE A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 291UP 48477 ATB - ONE HOUR AFTER DEPARTURE, THE NR 1 FUEL QTY INDICATING SYSTEM FAILED. THE NR 2 FUEL FLOW INDICATOR WAS PREVIOUSLY DEFERRED. ACCORDING TO SYSTEM OPERATIONS, THE CREW COULDN'T COMPLY W/THE AOM REGARDING FUEL BURN AND FUEL INDICATION. CREW DUMPED 85.0 LBS OF FUEL AND RETURNED TO CGN FOR REPAIR. TROUBLESHOOTING PERFORMED PER FIM 28-41-00. FOUND NR 1 TA NK IB MJP FAULTING INTERMITTENTLY. SAME REPLACED PER MM 28-41-40. L/C & F/C OK. FQDU REPLACED PER TECH REQUEST IAW MM 2 8-41-91. F/C OK. 2 L 7 3 4F RT A22WE 2008031200041 20080312 00041 WP 2008 3 12 UPS08851736 1 20080219 A 5320 FLOOR SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 FLOOR PNL F25 HAS CRACKED U-CHANNEL. REPAIRED FLOOR PANEL F25 IAW SRM 53-07-03 FIG 001, SRM 51-1-21 AND SRM 51-1-8. 2 L 7 4 4F RT 4A25 2008031200042 20080312 00042 WP 2008 3 12 UPS08851737 1 20080219 A 5321 PANEL DOUG DC8 DC873F 302199F WP COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 COCKPIT FLOOR PNL 676E HAS CORROSSION. REPAIRED COCKPIT FLOOR PNL, BY FABRICATION IAW SRM 53-07-03 F IG 001. 2 L 7 4 4F RT 4A25 2008031300002 20080313 00002 NM 2008 3 13 2008UALA01106 1 20080228 A 5230 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 FWD CARGO DOOR, UPPER EXTERIOR SKIN ANGLE IS DAMAGED ON INNER SIDE (VIEWED FROM SNUBBER CAVITY). REPLACED DOWN STOP ON NR 3 INBD TRACK PER MM 27-81-21-401, NOTE THAT THE LT SLAT DOWNSTOP CHK ACP'D PER EG 7597 ON THIS VISIT. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300003 20080313 00003 NM 2008 3 13 2008UALA01107 1 20080228 A 5754 SLAT TRACK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 3 SLAT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 NR 3 SLAT OTBD TRACK DOWN STOP LOCK IS BROKEN, REF NR13349-5200-0009. REPLACED DOWN STOP ON NR 3 INBD T RACK PER MM 27-81-21-401, NOTE THAT THE LT SLAT DOWNSTOP CHK ACP'D PER EG 7597 ON THIS VISIT. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300004 20080313 00004 2008 3 13 68JV02 4 20080222 A 2211 8221019313 COMPUTER BEECH MU300 400A 1155402 CE AUTOPILOT FAILED E DBCA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 68JV 1439 RK296 ON CLIMBOUT FROM DSM CREW RECEIVED AUTOPILOT PITCH TRIM FAIL ANNUNCIATOR. AIRCRAFT RETURNED TO DSM, LANDING WAS UNEVENT FUL. AFTER LANDING, CREW PERFORMED PREFLIGHT OPS CHECKS OF AUTOPILOT SYSTEM AND COULD NOT DUPLICATE FAILURE. REPOSITIO NED AIRCRAFT FROM DSM TO EMERY AIR-RFD. FAULT MESSAGE DID NOT RE-OCCUR. DURING INITIAL TROUBLESHOOTING EMERY AIR COULD NOT DUPLICATE FAILURE. EMERY AIR LEFT AIRCRAFT SIT OUTSIDE OVERNIGHT TO COLD SOAK. AFTER COLD SOAK EMERY AIR WAS ABLE TO DUPLICATE FAILURE. EMERY AIR REPLACED NR 2 AUTOPILOT COMPUTER WITH OVH UNIT. OPERATIONS CHECKED OK. 2 H 7 2 4F RT A16SW 2008031300014 20080313 00014 NE 2008 3 13 ASAA0852684 2 20080226 A 7200 CFM567B27 ENGINE BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 1 OIL CONSUMPTION A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 570AS 35185 894536 NR 1 ENGINE OIL CONSUMPTION IS AT 0.8QTS HR OUT OF LIMITS FOR ETOPS OIL CONSUMPTION. ENGINE OIL CONSUMPTION RATE HAS RE TURNED TO NORMAL. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008031300016 20080313 00016 CE 2008 3 13 68JV02A 1 20080227 A 2435 1013690113 ADAPTER LUCAS BEECH MU300 400A 1155402 CE LT STARTER GEN FAILED E DBCA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 13 68JV 462 P1253 RK296 AFTER DEPARTING MKE THE LEFT GENERATOR DROPPED OFF LINE AND RESET WITHOUT ANY ACTION FROM CREW. AIRCRAFT RETURNED TO MK E. LANDING WAS UNEVENTFUL. INSPECTION OF LEFT STARTER/GENERATOR FOUND THE THREADS ON THE STARTER/GENERATOR GROUND TERM INAL ADAPTER HAD FAILED ALLOWING THE GROUND LEAD TO LOOSEN. GROUND TERMINAL ADAPTER WAS REPLACED WITH NEW. OPERATIONS CHECKS GOOD. 2 H 7 2 4F RT A16SW 2008031300017 20080313 00017 NE 2008 3 13 MASA200800178 2 20080219 A 7320 4128T48G09 ROD CNDAIR CL600 CL6002D24 1390016 EA GE CF34 CF348C5 30050 NE NR 1 ENGINE DEFECTIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 933LR 142 15033 NR 1 ENGINE, S/N 194271, EXPERIENCED ITT EXCEEDANCE OF 1031C FOR 2.7 SECONDS DURING START. BORESCOPE C/W WITH NO DEFECT S. MX REPLACED MASTER AND SLAVE VG TORQUE RODS. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008031300019 20080313 00019 2008 3 13 LYNX00009 4 20080228 A 3425 42000332501 AHRS BOMBDR DHC8 DHC8402 1390042 NM NR 1 MALFUNCTIONED A 3LYA O OTHER J WARNING INDICATION CR CRUISE 1 NM 21 506LX 4176 ELEVATOR FEEL CAUTION LIGHT IN FLIGHT. AHRS1 FAIL MESSAGE ON FMS AND ADC1 FAILED. NO OTHER ASSOCIATED LIGHTS. SCHEDUL ED LANDING IN DENVER. FOUND HARD FAULT IN NR 1 AHRS. REMOVED AND REPLACED NR 1 AHRS PER AMM34-21-01-000-801 AND 34-21- 01-400-801. PERFORMED OPERATIONAL TEST PER AMM 34-21-00-710-801. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2008031300020 20080313 00020 NM 2008 3 13 ASAA0852687 1 20080228 A 3040 8300005604 WARNING SYSTEM BOEING 737 737890 1384527 NM ANTI-ICE SYS MALFUNCTIONED A ASAA K NONE N FALSE WARNING NR NOT REPORTED 1 NM 02 558AS 35177 LEFT SIDE WINDOW OVERHEAT LIGHT CAME ON. COMPLIED WITH QRH THE LIGHT EXTINGUISHED. PERFORMED CNTL CABIN WINDOW ANTI IC E SYSTEM TEST. OP CHECKS GOOD. 2 L 7 2 4F RT A16WE 2008031300027 20080313 00027 WP 2008 3 13 UPS08851753 1 20080225 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 100 L34L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 CRACK AT FWD CARGO PIT STA 100 LONG 34L. FRAME REPAIRED AT STA 100 AND L34L IAW EO DC8-5320-6176-6 A ND SRM 51-1-8. 2 L 7 4 4F RT 4A25 2008031300029 20080313 00029 NM 2008 3 13 UPS08M51745 1 20080301 A 5330 SKIN DOUG MD11 MD11F 3023600 NM AFT FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 272UP 48571 CORROSION FOUND IN AFT FUSELAGE. REMOVED DAMAGED AND CORRODED SKIN. FABRICATED AND INSTALLED SKIN DOUBLER PER SRM 53-2 0-00. TRIMMED AND REPAIRED HORIZONTAL STAB AFT FAIRING SUPPORT ANGLE IAW EO 28738B. 2 L 7 3 4F RT A22WE 2008031300033 20080313 00033 NM 2008 3 13 2008UALA01091 1 20080228 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY LIGHT INOPERATIVE, RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031300034 20080313 00034 NM 2008 3 13 2008UALA01117 1 20080303 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROW 34 LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 582UA 26702 EXIT PATH LIGHTING FROM ROW 34 BACK IS LOOSE. RESECURED EEL STRIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031300037 20080313 00037 NM 2008 3 13 2008UALA01120 1 20080229 A 5230 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 FWD CARGO DOOR LWR FWD SIDE FRAME IS CRACKED IN RADIUS. MAJOR REPAIR ACCOMPLISHED: REPLACED LOWER FWD FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300040 20080313 00040 EA 2008 3 13 DATA200800004 2 20080228 A 7530 3032125 LINE PWA PT6A45R STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA LT ENGINE LEAKING E DATA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 13 336MV PCE84060 SH3018 PCE84060 AT 40 NM FROM DEPARTURE AT CRUISE ALTITUDE OBSERVED A GRADUAL DROP IN LEFT ENGINE FUEL FLOW, % NG, TORQUE AND ITT. DROP STABILIZED AT ABOUT 80% NG AND 240 LBS/HR FUEL FLOW. DECISION WAS MADE TO RETURN TO SBA. AT 20 NM OUT FROM SBA LEFT E NGINE BEGAN TO SURGE IN POWER. DECISION WAS MADE TO SECURE LEFT ENGINE. 2 H 7 2 4T 4 T A41EU E4EA 2008031300050 20080313 00050 NM 2008 3 13 2008UALA01128 1 20080302 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 303 S10L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 HINGE BOX AUX WEB IS CRACKED BS 303.9 ABOVE STR 10L. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED INTERCOSTAL & DISCARDED EXISTING ITEMS OF THE BUILD-UP. FABRICATED & INSTALLED FRAME WEB DOUBLER REPAIR. INSTALLED NEW FABRICATED PARTS IN INTE RCOSTAL BUILD-UP. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300054 20080313 00054 NM 2008 3 13 2008UALA01130 1 20080302 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 440-460 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 FORWARD CARGO DOOR CUT-OUT FWD AND AFT LOWER CORNERS HAVE SCRIBE LINES FROM BS440-460 BETWEEN STR S-25R TO S-26R AND FRO M BS 480-500 STR S-25R-26R. IN ADDITION A 1.5 INCH DENT WAS FOUND WITH A THREE SIXTEENTH INCH COUNTERSUNK RIVET ADJACEN T TO SCRIBES. MAJOR REPAIR ACCOMPLISHED: BLENDED OUT SCRIBE LINES. TRIMMED OUT DENT. FABRIC ATED & INSTALLED DOUBLER T RIPLER REPAIR INCORPORATING STATIC PORT FORWARD OF CARGO DOOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300060 20080313 00060 NM 2008 3 13 2008UALA01137 1 20080229 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1560 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 AFT PIT FRAME INBOARD FLANGE DENTED AT BS 1560 BETWEEN STR 26L AND STR 27L. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031300062 20080313 00062 NM 2008 3 13 2008UALA01140 1 20080302 A 5322 SHEAR TIE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE OUT OF TOLERANCE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 EXISTING FASTENER HOLE WAS FOUND LOCATED TOO FAR AFT. THE FASTENER IS COMMON TO THE SIDE LINK FITTING (012N8887), SHEAR TIE FITTING (112N7017) AND THE TENSION CLIP (012N8886). THIS FASTENER LOCATION WAS LOCATED AT THE FACTORY 85625 DURING OEM ASSEMBLY AND THE 112N7009-14 DRAG FITTING WAS MODIFIED TO MAKE ROOM FOR THE FASTENER. ACCOMPLISHED MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031300065 20080313 00065 SO 2008 3 13 RAIA00802026 1 20080224 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 822HK 145069 PRE FLT 5528 - STL - EMERGENCY LIGHT IN GALLEY INOPERATIVE. MAINTENANCE REPAIRED WIRING TO THE EMERGENCY LIGHT IN GALLE Y CEILING. OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008031300066 20080313 00066 NM 2008 3 13 2008UALA01142 1 20080302 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY EXIT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 535UA 25130 EXTERIOR EMERGENCY DOOR NR 2 SLIDE LIGHT IS INOP. RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031300069 20080313 00069 SO 2008 3 13 RAIA00802028 1 20080227 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 842HK 14500830 PRE FLT 7882 - STL - EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB AT THE AFFECTED LIGH T ASSEMBLY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4T RT T00011AT 2008031300077 20080313 00077 NM 2008 3 13 2008UALA01150 1 20080229 A 3350 FU305 FUSE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 533UA 25073 OVERHEAD EMERGENCY LIGHT AT CLASS DIVIDE CURTAIN IS INOP. REPLACED FUSE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031300086 20080313 00086 NM 2008 3 13 2008UALA01158 1 20080229 A 3350 1317 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 2E LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 218UA 30222 EMERGENCY SIDE LIGHT AT SEAT 2E LOOSE. SECURED EMERGENCY SIDE LIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008031300088 20080313 00088 NM 2008 3 13 2008UALA01160 1 20080301 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EEL INOP, G7 GALLEY. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2008031300093 20080313 00093 NM 2008 3 13 2008UALA01164 1 20080301 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 47 HJK INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY EXIT EEL LIGHT INOP, AT SEAT 47 HJK. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031300095 20080313 00095 NM 2008 3 13 2008UALA01165 1 20080302 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 58 HJK INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY LIGHT INOP AT 58 HJK. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031300105 20080313 00105 NM 2008 3 13 2008UALA01175 1 20080304 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 3J AFT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 FOUND SEAT EEL INOP, ROW 3J AFT SECTION. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031300108 20080313 00108 NM 2008 3 13 2008UALA01192 1 20080303 A 2611 FIRE LOOP BOEING 777 777236 1385220 NM PWA 4090 PW4090 52119 NE NR 2 NACELLE FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 228UA 30556 FIRE LOOP 2 ENG R RIGHT ENGINE FIRE DETECTION SYSTEM LOOP 2 FAILURE. STATUS MSG-2610232 ACTIVE ER HARD MSG-2610232 ACTI VE ER HARD. 2 L 7 2 4F 4 F RT T00001SE E46NE 2008031300109 20080313 00109 NM 2008 3 13 2008UALA01193 1 20080303 A 2425 SHAFT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GENERATOR SHEARED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 218UA 30222 FOUND BACKUP GENERATOR (L) HAS A SHEARED SHAFT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008031300112 20080313 00112 SO 2008 3 13 SIMA200806505 1 20080304 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 677AE 14500810 DURING IMBV, FOUND AFT BAGGAGE DOOR SILL TO BE CORRODED. REMOVED AND REPLACED SILL IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008031300114 20080313 00114 EA 2008 3 13 SIMA200806502 1 20080303 A 5610 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FAILED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 506AE 10056 ON FLIGHT 4467, CREW REPORTED AT FL 390 IN CRUISE FLIGHT THE CAPTAINS WINDSHIELD INNER PANE SHATTERED. CREW ELECTED TO DIVERT TO ATL. AIRCRAFT LANDED AND TAXIED TO THE GATE SAFELY WITH OUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE. 2 L 7 2 4F RT A21EA 2008031000216 20080310 00216 EA 2008 3 10 COMA0860150 1 20080228 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 815CA 15852 7397 FLIGHT 5669 - RECEIVED FLAP FAIL CAUTION. ABORTED APPROACH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED SI- 2-27I0002. REPLACED FLAP PDU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008031000224 20080310 00224 NM 2008 3 10 CALA0800194 1 20080304 A 5311 6516301 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 FOUND CRACK AROUND HI-LOK HOLE AT STA 188 LBL 10. FABRICATED AND INSTALLED REPAIR PER ECRA 5311-01397. 2 L 7 2 4F RT A16WE 2008031000239 20080310 00239 NM 2008 3 10 KCSA081139 1 20080305 A 5347 SEAT TRACK BOEING 747 747209B 138489B NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 SEAT TRACK AT STA-1485 RBL-76 HAS A 2 INCH CRACK. 2 L 7 4 4F RT A20WE 2008031000267 20080310 00267 NM 2008 3 10 KCSA081143 1 20080306 A 5412 BULKHEAD BOEING 747 747209B 138489B NM NR 1 PYLON GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 NR 1 PYLON REAR ENGINE MOUNT BULKHEAD IS GOUGED AT NAC STA-222. 2 L 7 4 4F RT A20WE 2008031000282 20080310 00282 NM 2008 3 10 AALA200800400 1 20080224 A 3350 COVER BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 DFW - EMERGENCY LIGHT MISSING PROTECTIVE COVER AT MID INTERIOR STOWAGE COMPARTMENT AND WIRING IS EXPOSED. REPLACED PROT ECTIVE COVER AT MID INTERIOR STOWAGE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031000307 20080310 00307 WP 2008 3 10 AALA200800433 1 20080228 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 447AA 49473 LGA - EMERGENCY LIGHTS AT SEAT ROWS 20 TO 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 20 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031000327 20080310 00327 CE 2008 3 10 DJFA2008005 1 20080121 A 3230 BUMPER BLOCK BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE MLG OUT OF ADJUST E DJFA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 23 447LX RK248 ON TAKEOFF, AFTER RAISING THE GEAR, THE RED LIGHT IN THE GEAR HANDLE STAYED ILLUMINATED. CREW RECYCLED THE GEAR AND SAME INDICATIONS RETURNED. FLY-BY OF TOWER CONFIRMED GEAR WAS UP AND MAIN GEAR DOORS WERE DEPLOYED. CREW RETURNED TO FTY WH ERE MAINT FOUND THE NOSE GEAR NOT LOCKING IN THE UP POSITION. MAINT ADJUSTED THE RUBBER BUMPER PADS ON THE UPLOCK ASSY AND CHECKED ALL CLEARANCES. ALL CHECKS WERE GOOD. 2 H 7 2 4F 4 F RT A16SW E25EA 2008031000338 20080310 00338 CE 2008 3 10 AMWA89557BC 1 20080110 A 2432 1013810087 BATTERY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA MASTER DISCHARGED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 135YV 14318 172 UE135 BATTERY CHARGE ANNUNCIATOR LIGHT ILLUMINATED IN FLIGHT. MAINT REPLACED BATTERY AND CLEARED DISCREPANCY. 2 L 7 2 4T 3 T RT A24CE E4EA 2008031000340 20080310 00340 EU 2008 3 10 2008UALA00645 1 20080204 A 3350 087021672 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SEAT 21 DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 412UA 465 FOUND SEAT 21 EEL DAMAGED. REPLACED DAMAGED SECTION OF EEL SYSTEM. OPS CHECKS ARE NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031000352 20080310 00352 NM 2008 3 10 AMTA200800085 1 20080212 A 2540 ATTACH FITTING BOEING 737 73783N 13844HI NM LAVATORY CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 317TZ 28246 AFT IB ATTACHMENT BLOCK CORRODED ON LAV A. REMOVED AND REPLACED ATTACHMENT BLOCK IAW 25-46-99 R1. (K) 2 L 7 2 4F RT A16WE 2008030700302 20080307 00302 EU 2008 3 7 2008UALA01041 1 20080226 A 3350 D9239003500060 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 29 412UA 465 EMERGENCY EXIT LIGHTS FLICKERING DURING TAXI IN. UNKNOWN ELECTRICAL (BATTERY) FAULT. REPLACED RT MID CABIN POWER SUPPL Y, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008030700349 20080307 00349 NM 2008 3 7 2008UALA01063 1 20080227 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 FWD GALLEY DOOR AFT LOWER CORNER, FRAME CRACKED. MAJOR REPAIR: INSTALLED REPAIR ANGLE AND FRAME SPLICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700364 20080307 00364 NM 2008 3 7 SWAA081082 1 20080227 A 3350 B21506 FUSE BOEING 737 7377H4 1384404 NM CABIN BLOWN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 297WN 32542 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT LT FWD CABIN. REMOVED AND REPLACED POWER SUPPLY FUSE PER MM. 2 L 7 2 4F RT A16WE 2008030700365 20080307 00365 NM 2008 3 7 SWAA081083 1 20080227 A 5311 65C22910 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500D, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008030700380 20080307 00380 NM 2008 3 7 SWAA081101 1 20080227 A 3350 3071BPEGPL LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 16 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008030700383 20080307 00383 NM 2008 3 7 SWAA081099 1 20080227 A 3350 1619 LIGHT BOEING 737 7375H4 138449D NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED MV1 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PE R MM. 2 L 7 2 4F RT A16WE 2008030700385 20080307 00385 NM 2008 3 7 SWAA081110 1 20080227 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008030700398 20080307 00398 NM 2008 3 7 SWAA081106 1 20080227 A 3097 286A2006 WIRE HARNESS BOEING 737 7377H4 1384404 NM COCKPIT ARCED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 749SW 29801 AIR TURNBACK/DECLARED EMERGENCY. FLIGHT DECK L2 WINDOW ARCED AT ROTATION. REMOVED AND REPLACED L2 WINDOW HEAT ELECTRIC HARNESS PER MM. 2 L 7 2 4F RT A16WE 2008031000054 20080310 00054 NM 2008 3 10 NWAA080816309 1 20080220 A 5330 SKIN BOEING 747 747451 1384940 NM BS 1480 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING "M" CHECK, FOUND CRACK IN FUSELAGE SKIN AT BS 1480 HOLE NR 11. REPAIRED PER EA 63-211896 SECT I. REPETITIVE INS PECTIONS TO BE ACCOMPLISHED EVERY 5,500 CYCLES THEREAFTER PER SECT II OF EA 63-211896. 2 L 7 4 4F RT A20WE 2008031000061 20080310 00061 WP 2008 3 10 IXXA08SMN040S 1 20080201 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1742 L16L MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT EXTERNAL DOUBLER LEFT AFT FUSELAGE SIDE FORWARD OF AFT PRES SURE BULKHEAD AT STATION FS 1742, LONGERON 16.5 LEFT. REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING R EPAIR DOUBLER. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, FILLER, INTERNAL FINGER DOUBLER. CLEANED, TREATED, PR IMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, SRM 51-3-1, DC8 SRM 53-2-1 FI GURE 7 SHEETS 1, 3, AND 5, DC8 SRM 51-1-21, 51-1-20D, DC8 SRM 53-5-1 FIGURE 1 ITEM D, DC8 SRM 51-1-8B, 2 L 7 4 4F RT 4A25 2008031000072 20080310 00072 NM 2008 3 10 SWAA081125 1 20080228 A 5313 6551698 STRINGER SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2008031000083 20080310 00083 EA 2008 3 10 TRAX200800359 1 20080229 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 839AS 7284 FLAP FAIL MSG WHEN SELECTING 8. FLAPS FAILED AT ZERO, EMERGENCY DECLARED, FLT 4218 CX. 2 L 7 2 4F RT A21EA 2008031000124 20080310 00124 NM 2008 3 10 ZZDA2008076 1 20080227 A 3350 8039251 FUSE BOEING 717 717200 1383700 NM POWER SUPPLY BLOWN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 972AT 55033 EMERGENCY LIGHTING INOP AT ROW 11 TO ROW 19 SEATING. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND POWER SUPPLY AT P OSITION 4 REF B717 MM 33-51. OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4F TR A6WE 2008031000127 20080310 00127 NM 2008 3 10 USAA920080475 1 20080209 A 5320 6546958503 CUSP WEB BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CORROSION ON MAIN CABIN FLOOR CUSP WEB, BS 460 - BS 480, S17R, WL 208. REPLACED MAIN CABIN FLOOR CUSP WEB, BS 460 - BS 480, S17R, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008031000166 20080310 00166 EA 2008 3 10 SWIA200819284 1 20080229 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE ACTIVATION A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 984CA 7171 FLT 1001 - SMOKE TOILET CAUTION MESSAGE ON APPROACH WITH NO SMOKE OBSERVED. INSPECTED AND CLEANED SMOKE DETECTOR. OPS CHECK GOOD PER 26-16-00. 2 L 7 2 4F RT A21EA 2008031000179 20080310 00179 NM 2008 3 10 CALA0800190 1 20080303 A 2560 MEGAPHONE BOEING 757 757224 1384958 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18112 27302 FORWARD MEGAPHONE INOP. MEGAPHONE BATTERY CONTACTS CLEANED, OPS GOOD FOR SERVICE. 2 L 7 2 4F RT A2NM 2008031000180 20080310 00180 SO 2008 3 10 SWIA200819292 1 20080301 A 3297 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY BUSS LOOSE A SWIA O OTHER N FALSE WARNING AP APPROACH 1 NM 07 568SW 120343 FLT 3687 - EMERGENCY BUSS OFF LIGHT ILLUMINATED ON APPROACH. RESET SYSTEM CIRCUIT BREAKER AND SECURED WIRING TERMINAL H ARDWARE. NO FAULTS NOTED. 2 L 7 2 4T RT A31SO 2008031000183 20080310 00183 NM 2008 3 10 CALA0800192 1 20080303 A 5315 141T5108 FLOORBEAM BOEING 767 767424ER 1385270 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59053 29448 STA 325 LBL 22 TO 50 FLOOR SUPPORT FOUND CORROSION. REPAIRED PER SRM 53-00-51. 2 L 7 2 4F RT A1NM 2008031000184 20080310 00184 NM 2008 3 10 DHL2008763503 1 20080301 A 5311 FRAME BOEING 727 727264 138408M NM BS 480 S16-17R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 FRAME GOUGED AND DENTED AT BS 480, ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 707 5T6, .063 INCHES BY 7.25 INCHES BY 3.25 INCHES, PO NR 9006027, PER B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2008031000190 20080310 00190 2008 3 10 BB08030 4 20080303 A 2310 7926140001 COUPLER BOEING 767 7672B7 1385107 NM HF RADIO FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 256AY 1770 1742 26847 PHL PHL-MXP FLT NR 716 RETF - CREW STATES, 'TRANSMISSION ON NR 2 (RT) HF INOP AT ALL STATIONS.' MAINTENANCE REPLACED RT COUPLER. TUNES CHKS OK. 2 L 7 2 4F RT A1NM 2008031000193 20080310 00193 NM 2008 3 10 HNAA0800091 1 20080221 A 5270 WARNING SYSTEM DHAV DHC8 DHC8102 2809003 NM SERVICE DOOR MALFUNCTIONED A HNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 07 328EN 281 DURING TAKEOFF ROLL THE SERVICE DOOR WARNING LIGHT ILLUMINATED. CREW ABORTED TAKEOFF. DOOR WAS CYCLED OPEN/CLOSED 2 TI MES AND PROXIMITY SENSOR RIGGING CHECKED IAW AMM 52-45-00. NO DISCREPANCIES FOUND. 2 H 7 2 4T RT A13NM 2008031000194 20080310 00194 EU 2008 3 10 08FDEA00693 1 20080305 A 5310 A53611516204 GUSSET AIRBUS 300 A300B4622R 3930312 EU PAX DOOR FRAME CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION FOUND ON GUSSET LT FWD PAX DOOR CUT OUT LOWER AFT CORNER. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51- 72-10. 2 L 7 2 4F RT A35EU 2008031000195 20080310 00195 EU 2008 3 10 08FDEA00694 1 20080305 A 5712 A57240810 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND WEAR IN RT MLG RIB 5 LUGS, FORWARD RIB 5 REPAIR PERFORMED BY REAM UP THE HOLES AND INSTALLING OVERSIZE BUSH IAW DR AWING R572-49221. 2 L 7 2 4F RT A35EU 2008031000196 20080310 00196 EU 2008 3 10 08FDEA00695 1 20080305 A 5320 A53973085 SILL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CORROSION ON AFT CARGO DOOR SILL BEAM C63-63A. REPAIR PERFORMED BY REMOVAL OF CORROSION, NDT FOR CRACK FREE CONDI TION AND FLAP PEENING IAW RAS/EFW/900011/2008 ISS A, APPROVED BY EA 6-5317-114871. 2 L 7 2 4F RT A35EU 2008031000199 20080310 00199 NM 2008 3 10 08FDEA00698 1 20080305 A 5340 69456791 ATTACH ANGLE BOEING 727 727227 1384078 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 INTERCOSTAL LOWER ATTACH ANGLE HAS ELONGATED HOLES, CRACK AND CORRODED AT 1110 TO FS 1130, BL 0. FABRICATED INTERCOSTAL LOWER ATTACH ANGLE AT FS 110 TO FS 1130 BL 0", REF DWG 69-4569. THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 2008031000203 20080310 00203 NM 2008 3 10 08FDEA00701 1 20080305 A 5330 6554583 SKIN BOEING 727 727227 1384078 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 AFT FUSELAGE BS 1166 BETWEEN S19L S20L, FRAME AND SKIN HAVE OVER SIZED HOLE (APPROX 3/8 DIA.) NDT TO VERIFY MATERIAL T HICKNESS .050". REMOVED DAMAGE ON SKIN. FABRICATED REPAIR DOUBLER AND FILLER 2024-T3 .063" A87331/P0 NR 1032671. OVER SIZED LAP SEAM HOLES AND NDT FOR 0 TIME, NO DEFECT FOUND. TREATED AND PRIMED REPAIR DOUBLER AND FILLER. INSTALLED DOUB LER AND FILLER. SEALED EDGES AND RESTORED FINISHES. REF SRM 53-30-2, SRM 51-10-1, SRM 51-10-2. THIS IS CLASSIFIED AS A MAJOR REPAIR CATEGORY "B" REPAIR. 2 L 7 3 4F A3WE 2008031000205 20080310 00205 NM 2008 3 10 08FDEA00702 1 20080305 A 5320 656724751 SUPPORT BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 CORROSION AND CRACK ON SIDEWALL "T" FRAME SUPPORT STA 1030 TO 1050, LT LOWER AFT PIT. REMOVED CORROSION ON "T' FRAME SU PPORT. REMOVED .022 INCH FROM ORIGINAL THICKNESS OF .065", REMAINING .043 INCH IS OUT OF LIMITS PER SRM 53-10-1 FIG 1. RECEIVED NEW PART, FABRICATED AND HEAT TREAT REF N/R N00866. DRILLED NEW PART REF. TREATED AND PRIMED REF SRM 51-10-2 . INSTALLED NEW PART NUMBER FX 65-67247-51. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008031000206 20080310 00206 WP 2008 3 10 08FDEA00703 1 20080305 A 5753 NRC6062510 VANE DOUG MD10 MD1010F 3022112 WP RT WING TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 RT WING INBD FLAP VANE INBD SIDE LOWER EXTERNAL SURFACE IS DELAMINATED AND DENTED AT THE L/E AREA. REMOVED & REPLACED R T I/B FLAP VANE IAW MM 27-50-03-2. 2 L 7 3 4F RT A22WE 2008031000207 20080310 00207 NM 2008 3 10 KCSA081137 1 20080304 A 5412 STIFFENER BOEING 747 747209B 138489B NM NR 4 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 NR 4 PYLON HAS CRACK IN I/B UPPER STIFFENER AT INTERNAL ANGLE AFT OF THE FWD ENGINE MOUNT BULKHEAD NAC STA 128. 2 L 7 4 4F RT A20WE 2008040800060 20080408 00060 EA 2008 4 8 HNAA0800113 1 20080327 A 3350 OL3071BPEGPL LIGHT DHAV DHC8 DHC8311 1386006 EA CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 327EN 261 WHITE LOW LEVEL EMERGENCY LIGHT AT ROW 7 INOP. RELAMPED WHITE LOW LEVEL EMERGENCY LIGHT AT ROW 7, OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2008031000208 20080310 00208 WP 2008 3 10 08FDEA00705 1 20080305 A 5347 NEA602217 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 1145 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 FOUND SEAT TRACK IS GOUGED AT BS 1145, RBL 75. BLENDED DAMAGED AREA. MATERIAL REMAINING .085. FOUND OUT OF LIMITS IAW SRM 53-70-00 VOL I. REMOVED AND REINSTALLED 4 FLOOR PANELS IAW AMM 53-21-08-2 . REMOVED DAMAGED TRACK AND INSTALLED NEW SECTION OF TRACK IAW SRM 51-31-01; VOL II; PG 1. FABBED NEW SECTION AND SPLICE HAT & PLATE IAW SRM 53-70-00; VO L I; PGS 3 & 4. ALODINED & PRIMED NEW SECTION IAW SRM 51-21-01; VOL II; PGS 21 & 24. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008031000212 20080310 00212 EU 2008 3 10 08FDEA00708 1 20080305 A 5753 A5797402000660 FAIRING AIRBUS 310 A310203 3930313 EU LT WING TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT WING FLAP FAIRING 535CB IS DELAMINATED. REPAIRED LT WING FLAP FAIRING 535CB BY REMOVING DELAMINATED SKIN AND CORE SEC TION AND APPLYING NEW CORE SECTION AND FIBERGLASS OVERLAY REPAIR IAW SRM 57-20-35. RESTORED FINISH IAW SRM 51-75-10. 2 L 7 2 4F RT A35EU 2008031000214 20080310 00214 EU 2008 3 10 08FDEA00709 1 20080305 A 5753 A5796502100000 FAIRING AIRBUS 310 A310203 3930313 EU LT WING TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LEFT WING FLAP FAIRING 532CB IS DELAMINATED IN TWO SPOTS. REMOVED DAMAGE, POTTED CORE, CURED, SANDED & PREPPED FOR WET LAY UP. LAYED UP REPAIR PLYS CURED & SANDED REPAIR PLYS; APPLIED SEALER RESIN, CURED & SANDED, REAPPLIED ANTI-STATI C PRIMER & FINISH TOP COAT IAW SRM 57-20-35. 2 L 7 2 4F RT A35EU 2008031000221 20080310 00221 EA 2008 3 10 COMA0860154 1 20080301 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 720SW 7297 FLIGHT 5478 - FLAPS FAIL CAUTION MESSAGE WHEN SELECTING FLAPS TO 8 DEGREES. EMERGENCY DECLARED. AIRCRAFT LANDED SAFELY . COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW-UP MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 2008031000226 20080310 00226 2008 3 10 DHLA200800019 4 20080301 A 2565 BOTTLE AIRCRUISERS AIRBUS 300 A300B4203 3930306 EU ZONE 800 READS LOW A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 365DH 851 359 A5490 149 R1 DOOR ESCAPE SLIDE PRESSURE IN RED. REMOVED AND REPLACED SLIDE ASSY. AIRCRAFT WAS GROUNDED. 2 L 7 2 4F RT A35EU 2008031000228 20080310 00228 EU 2008 3 10 TRAX200800282 1 20080219 A 5320 BRACKET AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 635AS 372 OMEGAS BRACKET ON FR 36 AND 1 OMEGA BRACKET ON FR 39, FOUND CRACKED AT STRG 15 R, RESOLVED ON W/O: 83239 TASKCARD: N/R-0 0226. TWO OMEGAS BRACKET ON FR 36 AND 1 OMEGA BRACKET ON FR 39 REPLACED IAW SRM 51-25-01 AND SRM 51-25-04. OMEGAS BRAC KET ON FR 36 AND FR 39, FABRICATED ON W/C 220-200. REPAIR DETERMINED NOT TO BE A MAJOR REPAIR IN ACCORDANCE WITH SP 663 AND FAR 43, APPENDIX A. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 51-25-01, 51-25-04. 2 H 7 2 4T RT A53EU 2008031000230 20080310 00230 EA 2008 3 10 TRAX200800347 1 20080227 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA BS 319 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 FOUND CORROSION AT RT FLOOR SILL AT FS 319. 2 L 7 2 4F RT A21EA 2008031000244 20080310 00244 EU 2008 3 10 MALA080035 1 20080304 A 2613 OVERHEAT SENSOR SAAB SF340 340B 7860101 EU TAILPIPE MALFUNCTIONED A MALA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 436XJ 340B436 TAIL PIPE HOT WARNING LIGHT ILLUMINATED IN FLIGHT, QRH COMPLETED. REMOVED AND REPLACED TAILPIPE OVERTEMP DETECTOR RDI C ODE 30WG, P/N OFF/ON 17343-62-450 IAW AMM 26-12-05-04. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008031000245 20080310 00245 SO 2008 3 10 FDKA200803086 1 20080304 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 5998 MCO (1611 PHX LCL). CEILING EMERGENCY LIGHT AT EMERGENCY EXIT INOPERATIVE. MX OPS CHECKED THE LIGHT AND OPS C HECKED GOOD. 2 L 7 2 4T RT T00011AT 2008031000246 20080310 00246 SO 2008 3 10 FDKA200803087 1 20080305 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6085 MCO-NAS (0740 PHX LCL). CABIN AISLE OVERHEAD EMERGENCY EXIT LIGHT OUT. MX RECYCLED EMERGENCY LIGHT SYSTEM. O PS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008031000250 20080310 00250 WP 2008 3 10 AALA200800441 1 20080228 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7508 49802 EWR - EMERGENCY LIGHT AT OVERHEAD COCKPIT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD COCKPIT. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031000251 20080310 00251 SO 2008 3 10 FDKA200803088 1 20080303 A 5230 14527016001 SPRING EMB 145 EMB145LR 3260212 SO CARGO DOOR CRACKED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 835MJ 145353 THE FORWARD AND AFT CENTERING GUIDE SPRINGS FOR THE CARGO DOOR ARE CRACKED. THE DAMAGED PART HAD BEEN REMOVED AND REPLA CED. (SUPPORT 145-27016-001) 2 L 7 2 4T RT T00011AT 2008031000257 20080310 00257 WP 2008 3 10 AALA200800392 1 20080223 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AA 49321 DFW - EMERGENCY LIGHT AT SEAT 10D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031000259 20080310 00259 NM 2008 3 10 AALA200800395 1 20080223 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 4B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 4B. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008040200197 20080402 00197 NM 2008 4 2 2008UALA01683 1 20080323 A 3510 OXYGEN SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 378UA 24653 CREW OXYGEN SYSTEM, LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED OXYGEN SYSTEM. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200200 20080402 00200 EA 2008 4 2 TRAX200800438 1 20080319 A 5755 CLOSEOUT PANEL CNDAIR CL600 CL6002C10 1390015 EA RT SPOILER CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 355CA 10067 RIGHT MULTIFUNCTION SPOILER CLOSEOUT PANEL CRACKED AT INBOARD AFT CORNER. REPAIRED CRACK ON MFS SHROUD IAW AMM SUPPLEME NT 51-75-00 REV B AND SRM CH 51-75-16. SUPPLEMENTAL SDR CLOSED 3/31/08. 2 L 7 2 4F RT A21EA 2008040200204 20080402 00204 EU 2008 4 2 2008UALA01688 1 20080325 A 5310 WINDOW FRAME AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 404UA 450 DENT 12 INCH BELOW F/O WINDOW FRAME 5.5 INCH HIGH 4.5 INCH WIDTH 0.1 DEEP. 12 INCHES ABOVE CF9026. SUPPLEMENTAL DATA U PDATE ACCOMPLISHED MAJOR REPAIR IN SFO. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200205 20080402 00205 NM 2008 4 2 2008UALA01691 1 20080325 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 600 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 FOUND FWD PIT FRAME DENTED STA 600 STR 25L. REMOVED DAMAGE FABRICATED REPAIR AND INSTALLED IAW SRM 53-00-07 RPR 5 ON NR 22857 BY MECH 111857 AND INSP BY QC 071. PER SRM 53-00-07 RPR 5 TABLE II THIS IS A CAT B REPAIR IN ZONE 2 AND REQ UIRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS TO BEGIN 25,000C AFTER RPR INSTALLED, AND REPET ATIVE INSPS 11,000C THEREA FTER CURRENT PTC IS 20,706C 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200206 20080402 00206 NM 2008 4 2 2008UALA01692 1 20080325 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 640 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 FOUND FWD PIT FRAME DENTED STA 640 STR 25L. REMOVED DAMAGE FABRICATED REPAIR AND INSTALLED IAW SRM 53-00-07 RPR 5 THIS IS A CAT B REPAIR IN ZONE 1 AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS TO BEGIN 29,294C AFTER RPR INSTALLED, A ND REPET ATIVE INSPS 12,000C THEREAFTER CURRENT PTC IS 20,706C 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200208 20080402 00208 NM 2008 4 2 2008UALA01693 1 20080325 A 5320 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 324 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 MAIN CABIN T-CAP PREVIOUS REPAIR CORRODED AT BS 324 AND RBL 35. REMOVED DAMAGED AREA, FABRICATED RPR MATERIAL AND INSTA LLED IAW SRM 51-40-02 AND MM 53-00- 98 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200210 20080402 00210 NM 2008 4 2 SWAA081686 1 20080328 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 219WN 32490 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008040200211 20080402 00211 NM 2008 4 2 SWAA081687 1 20080327 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 220WN 32491 R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 2008040200213 20080402 00213 NM 2008 4 2 SWAA081716 1 20080330 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 237WN 34632 EEPLS LIGHT LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008040200214 20080402 00214 NM 2008 4 2 SWAA081689 1 20080328 A 3397 W4142001220 WIRE BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 298WN 32543 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 4 ABC. REPAIRED BROKEN WIRE PER WDM. 2 L 7 2 4F RT A16WE 2008040200215 20080402 00215 NM 2008 4 2 SWAA081688 1 20080328 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 298WN 32543 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC TO ROW 3 ABC. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008040100107 20080401 00107 EA 2008 4 1 A6WA200840159 1 20080307 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE ILLUMINATED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 446AW 7806 AIR DIVERSION: RED 14TH STAGE RT DUCT CAS MESSAGE DISPLAYED IN FLIGHT. COMPLIED WITH QRH, WARNING MESSAGE CLEARED. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008040100112 20080401 00112 CE 2008 4 1 CDN2008F00000 1 20080304 A 5280 24922532 HINGE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP OB GEAR DOOR CRACKED E CDNA O OTHER O OTHER CR CRUISE 1 EA 05 78MC 15153 117 CREW NOTICED A LANDING GEAR DOOR UNSAFE INDICATION IN FLIGHT. THE GEAR WAS LOWERED WITH GEAR DOWN AND LOCKED INDICATION S NORMAL. INSPECTION REVEALED THAT THE OB RT GEAR DOOR HINGE WAS CRACKED WHICH CAUSED THE DOOR TO NOT FULLY CLOSE. THE CONDITION WAS AGRIVATED BY HIGHT AIRSPEED. (K) 2 L 7 2 4F 4 F A10CE E6WE 2008040100129 20080401 00129 NM 2008 4 1 ASAA0842715 1 20080229 A 5313 6546881200 STRINGER BOEING 737 737490 1384715 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 STR 14L AT BS 1070 DENTED STR 14L BS 1070, REPARIED IAW B737 400 SRM 53 00 03. 2 L 7 2 4F RT A16WE 2008040100165 20080401 00165 EA 2008 4 1 TRAX200800428 1 20080318 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 933EV 8022 FWD FACING EXIT LIGHT ON AISLE OVERWING EMERGENCY LIGHTS INOP. FLT 4898 DEL 166 MINS. 2 L 7 2 4F RT A21EA 2008040100186 20080401 00186 EA 2008 4 1 TRAX200800460 1 20080321 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 355CA 10067 LEFT SIDE 280 BULKHEAD WEB CORRODED AFT SIDE AT FLOOR LEVEL. REPAIRS PERFORMED IAW REO 670-53-11-052, SRM 51-42-06, REO 670-53-11-052 REV A, AND SRM 51-25-00. 2 L 7 2 4F RT A21EA 2008040100187 20080401 00187 EA 2008 4 1 TRAX200800461 1 20080321 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 355CA 10067 RIGHT SIDE 280 BULKHEAD WEB CORRODED AFT SIDE AT FLOOR LEVEL. REPAIRS PERFORMED IAW REO 670-53-11-052, SRM 51-42-06, REO 670-53-11-052 REV A AND SRM 51-28-00. 2 L 7 2 4F RT A21EA 2008031000374 20080310 00374 EA 2008 3 10 A6WA200840069 1 20080123 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 FRAME DENTED OVER LIMITS AT FS 700.00 BTW STR 22L TO STR 23L. FRAME SELECTOR REPLACED AT FS 700.00 BTW STR 22L TO 23L S RM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000390 20080310 00390 EA 2008 3 10 A6WA200840085 1 20080205 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 CRACK EXIST ON INTERCOSTAL FS 481, LBL 36 AND LBL 27 CRACK LENGTH .200. (K) REPAIRED IAW REO 601R-53-41-059. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031100007 20080311 00007 NM 2008 3 11 08FDEA00389 1 20080211 A 5330 65545776 SKIN BOEING 727 727233 138408A NM BS 720D CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 RT WING TO BODY FUSELAGE SKIN SURFACE SHOWS CORROSION AND GOUGE AT LAP JOINT, STA 720D, STR 19R. BURNISHED DAMAGED AREA IAW SRM 51-10-1 AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG1,2 AND 53-30-2 FIG2. CUT OUT DAMAGED, FABRICATED REPAIR DOU BLER AND REPAIR FILLER IAW 53-30-3 FIG 6 AND 53-30-2 FIG2. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PA RTS IAW SRM 53-30-3 FIG 6 AND 51-30-2. 2 L 7 3 4F RT A3WE 2008031200047 20080312 00047 NM 2008 3 12 2008UALA01072 1 20080227 A 5210 INSERT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR HANDLE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 R4 DOOR HANDLE BOX INSERTS CORRODED. ACCOMPLISHED A MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031200049 20080312 00049 NM 2008 3 12 2008UALA01074 1 20080227 A 5240 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 DOOR 2L UPPER HINGE ARM CUTOUT REQUIRES DOUBLER. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED A MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031200050 20080312 00050 NM 2008 3 12 2008UALA01075 1 20080227 A 5210 PAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR HANDLE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 DOOR 2L DOOR HANDLE PAN GOUGED AND HAS LIGHTNING STRIKES (3 EA). ACCOMPLISHED A MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031200051 20080312 00051 NM 2008 3 12 2008UALA01076 1 20080227 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1440 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 AFT LOWER CARGO COMPARTMENT, FUSELAGE FRAME DENTED ON INBOARD FLANGE, BS 1440, AT STR 25L-26L. ACCOMPLISHED MAJOR REPAI R AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031200052 20080312 00052 NM 2008 3 12 2008UALA01077 1 20080227 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1460 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 AFT LOWER CARGO COMPARTMENT FUSELAGE FRAME DENTED AT BS 1460 AT STR 26L, INBOARD FLANGE. ACCOMPLISHED A MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031200055 20080312 00055 NM 2008 3 12 2008UALA01081 1 20080227 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1480 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 AFT LOWER CARGO PIT, FUSELAGE FRAME UPPER CHORD DENTED AT BS 1480 BETWEEN STR 25L-26L. ACCOMPLISHED A MAJOR REPAIR AT G SO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031200058 20080312 00058 NM 2008 3 12 2008UALA01089 1 20080229 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 FLOOR EEL INOP, SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031200063 20080312 00063 NM 2008 3 12 2008UALA01096 1 20080229 A 5497 D4236J CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 NACELLE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 NR 2 PYLON J BOX CONNECTOR D4236J IS DAMAGED BY HEAT. REPLACED CONNECTOR D4236J REF BSWPM 20-63-13. OPS CHECK ACCOMP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031200064 20080312 00064 NM 2008 3 12 2008UALA01097 1 20080229 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1197 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 AFT CARGO PIT AT BS 1197 +22 LBL 38 TO LBL 44 FRAME T-CAP HAS CORROSION UNDER SIDE OF CAP. FOUND TO BE OUT OF LIMITS. REMOVED ENTIRE "T" CORD. INSTALLED NEW "T" CORD REF SRM 51-40-02. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031200066 20080312 00066 NM 2008 3 12 2008UALA01099 1 20080229 A 5497 D4266J CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 NACELLE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 NR 2 PYLON J BOX CONNECTOR D4240J IS DAMAGED BY HEAT. REPLACED CONNECTOR D4266J PER BSWPM 20-63-13. OPS CHECK ACCOMP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031200068 20080312 00068 NM 2008 3 12 2008UALA01101 1 20080228 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 947-1006 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 BS 947 TO 1006 INNER CREASE BEAM AT STR S- 17R CORRODED AT AFT GALLEY DOOR CUT-OUT. MAJOR REPAIR ACP'D BY REPLACING INN ER CHORD SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300009 20080313 00009 EU 2008 3 13 UPS08151752 1 20080304 A 2420 GENERATOR AIRBUS A300 A300F4622R 3930360 EU NR 1 FAILED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 158UP 0847 ATB - NR 1 GENERATOR FAILED ON CLIMB-OUT/APU GEN FAILED. REMOVED AND REPLACED NR 1 GENERATOR CONTROL UNIT IAW 24-22-12- 04. RAN ENGINES AND APU. PERFORMED A/C MONITORING OPERATIONAL AND FUNCTIONAL TESTS PER MM 24-27-00-05. PERFORMED GPCU BITE PER 24-41-00-05. PERFORMED AC MONITORING AND OPERATIONAL TESTS ON NR 2 AND APU PRECAUTIONARY. ALL PWR SYS FUNCTI ONS NORMALLY. A/C OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2008031300010 20080313 00010 WP 2008 3 13 UPS08851746 1 20080224 A 5730 DOUBLER DOUG DC8 DC873F 302199F WP LH WING BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 LT WING O/B UPPER AND LOWER SURFACE TE WEDGE DOUBLER HAS 2 UPPER FASTENERS PULLING THROUGH AND DOUBLE R BULGED. REPAIRED L-WING O/B TE IAW SRM 57-02-00 FIG 002A, SRM 51-01-21A. 2 L 7 4 4F RT 4A25 2008031300012 20080313 00012 NM 2008 3 13 ASAA0852685 1 20080227 A 2132 214C502 WARNING SWITCH BOEING 737 737890 1384527 NM CABIN PRESSURE FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 579AS 35187 WHILE DOING TASKCARD 72131000 ALTITUDE WARNING FAILED. REPLACED CABIN PRESSURE WARNING SWITCH. OP CHECKS GOOD. 2 L 7 2 4F RT A16WE 2008031300028 20080313 00028 WP 2008 3 13 UPS08851754 1 20080225 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT WING TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 LT INBOARD FLAP STA 98 EXTERIOR SKIN REPAIR DOUBLER GOUGED. REPAIRED LT INBOARD FLAP STA 98 EXTERIOR SKIN REPAIR DOUBLER IAW SRA 51-1- 21A, SRM 57-07-01 FIG 001 AND SRM 51-3-2. 2 L 7 4 4F RT 4A25 2008031300046 20080313 00046 NM 2008 3 13 2008UALA01126 1 20080301 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 906 WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 FUSELAGE SKIN WORN FROM CONTACT WITH DORSAL FIN SEAL. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED SINGLE LAYER DO UBLER FROM BS 906-910 & INSTALLED WEAR STRIPS REPAIR UNDER ENTIRE LANDING FROM BS 860-1006 ON BOTH SIDES. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300064 20080313 00064 2008 3 13 2008UALA01141 4 20080302 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 L-1 MED EVAC SLIDE HANDLE DOESN'T FULLY ENGAGE. HANDLE ONLY MOVES TWO-THIRDS TRAVEL IN ARM DIRECTION. OVERHEAD ANNUNCI ATOR DOESN'T TURN ON EITHER. FOUND SLIDE PACKED WAS NOT IN CORRECT SHAPE, THUS CAUSING THIS PROBLEM. REPLACED SLIDE AS SY, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031300070 20080313 00070 SO 2008 3 13 RAIA00802030 1 20080227 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 829HK 145281 PRE FLT 5587 - STL - HALF OF THE EMERGENCY LIGHT AT ROW 12 IS INOPERATIVE. MAINTENANCE SECURED A LOOSE WIRE AT THE AFFE CTED LIGHT. 2 L 7 2 4T RT T00011AT 2008031300071 20080313 00071 SO 2008 3 13 RAIA00802029 1 20080227 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 830HK 145313 PRE FLT 5559 - STL - EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB AT THE AFFECTED LIGH T. 2 L 7 2 4T RT T00011AT 2008031300075 20080313 00075 NM 2008 3 13 2008UALA01148 1 20080229 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1351 S24-25R GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 AFT PIT FRAME WEB GOUGED, STA 1351, STR 24R - 25R. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031300076 20080313 00076 NM 2008 3 13 2008UALA01149 1 20080229 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1197 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 AFT CARGO PIT AT BS 1197 +44 LBL 22 TO RBL 9 FRAME T-CAP HAS CORROSION UNDER NUT PLATE ATTACH FASTENER HOLES. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031300087 20080313 00087 NM 2008 3 13 2008UALA01159 1 20080301 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 UPPER DECK AFT CREW REST ROOM CEILING EEL INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031300098 20080313 00098 NM 2008 3 13 HNAA0800094 1 20080221 A 7712 30005000046 TSCU DHAV DHC8 DHC8102 2809003 NM NR 2 MALFUNCTIONED A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 906HA 39479 5657 009 ON TAKEOFF ROLE NR 2 PROP FEATHERED AT 30% TORQUE. ARM LIGHT WAS NOT ILLUMINATED. ABORTED TAKEOFF. UNABLE TO DUPLICAT E PROBLEM. REPLACED NR 2 TSCU. 2 H 7 2 4T RT A13NM 2008031300110 20080313 00110 NM 2008 3 13 2008UALA01195 1 20080303 A 2797 CONNECTOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FLT CONTROLS FAILED A UALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 787UA 26939 FLIGHT CONTROL SYS STATUS MSG ON PUSHBACK, WILL NOT CLEAR. AFTER EXTENSIVE TROUBLE SHOOTING FOUND BAD CONNECTOR. REPLA CED ACE L2 BENCH PLUG DM27122AC. PERFORMED ACE LRU TEST,ACE ACTUATOR MONITOR TEST PER MM 27-02-02-501,AND ACE ACTUATOR C ONFIDENCE TEST.ALL TEST NORMAL . NO DEFECTS NOTED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008031300111 20080313 00111 GL 2008 3 13 SIMA200806504 2 20080304 A 7261 23072308 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LT ENGINE WORN A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 699AE 14500883 CAE311195 ON FLIGHT 9811, CREW REPORTED CABIN ODOR DURING TAKEOFF IN COCKPIT. ODOR DISAPPEARED DURING CLIMB. ODOR RE-EXPERIENCED ON APPROACH BELOW 7000 MSL. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENGINE ZERO CARBON SEAL IAW EMB 145 AMM 72-25-25. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008031300113 20080313 00113 SO 2008 3 13 SMIA200806501 1 20080302 A 3397 480CC1 CONTACTOR EMB 135 EMB135LR 3260305 SO LANDING LIGHT INOPERATIVE A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 708AE 145205 ON FLIGHT 4778, CREW REPORTED ON CLIMB-OUT A OIL ODOR IN FORWARD PART OF THE CABIN. CREW DIVERTED TO BWI, NO OTHER PROB LEMS NOTED. AIRCRAFT REMOVED FROM SERVICE. DURING TROUBLE SHOOTING FOUND LEFT LANDING LIGHT CONTACTOR INOPERATIVE. RE MOVED AND REPLACED CONTACTOR IAW EMB135 AMM CHAPTER 33-41-03. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008031300116 20080313 00116 NM 2008 3 13 QXEA200800239 1 20080306 A 2611 4462531 SMOKE DETECTOR BOMBDR DHC8 DHC8402 1390042 NM LAVATORY MALFUNCTIONED A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 425QX 4039 SEA - FLIGHT 2228 - LAV SMOKE DETECTOR SOUNDS INTERMITTENTLY WITH NO SIGN OF SMOKE. PDX MAINTENANCE REMOVED AND REPLACE D SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008031300119 20080313 00119 NM 2008 3 13 08FDEA00483 1 20080218 A 5320 146N54173 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD STRINGER L2.90, STA 1400-1420. TO EVALUATE EXISTING REPAIR. TO EVALUATE E XISTING REPAIR. EXISTING REPAIR FOUND NOT IAW SRM 51-70-11 FIG 1 DETAIL I, II. AFT CARGO FLOORBOARD STRINGER L2.90, RE PLACED IAW SRM 51-10-02 REV.93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008031300120 20080313 00120 NM 2008 3 13 08FDEA00485 1 20080218 A 5320 146N541613 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD STRINGER R10.45, STA 1320-1340, TO EVALUATE EXISTING REPAIR. EXISTING REP AIR FOUND NOT IAW B757-200 SRM 51-70-11 FIG 1 DETAIL I, II. AFT CARGO FLOORBOARD STRINGER R.10.45 REPLACED IAW B757-200 SRM 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008031300128 20080313 00128 EU 2008 3 13 08FDEA00717 1 20080305 A 5510 A5517741100000 FAIRING AIRBUS 310 A310203 3930313 EU HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT HORIZONTAL STABILIZER UPPER APRON FAIRING IS CRACKED AND DELAMINATED IN SEVERAL PLACES. FABRICATED DOUBLER IAW SRM 55-15-11. REMOVED DAMAGED SECTION IAW SRM 55-15-11 FIG 201. INSTALLED DOUBLER IAW SRM 55-15-11 PGS 219/220. INSTALL SIL ICONE DOUBLER AND REPAIRED DAMAGED AREAS IAW SRM 55-15-11 PARAGRAPH 5 (4). 2 L 7 2 4F RT A35EU 2008031300132 20080313 00132 WP 2008 3 13 08FDEA00722 1 20080305 A 5730 ARC29061 PANEL DOUG MD10 MD1010F 3022112 WP LT WING PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 LT WING PANEL 541CR IS PUNCTURED AND DELAMINATED ON THE LOWER SIDE. REMOVED THE DAMAGE AND REPAIRED PANEL IAW SRM 51-71 -00; VOL II. ALODINED AND PRIMED THE REPAIR AREA IAW SRM 51-21-01; VOL II. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008031300134 20080313 00134 WP 2008 3 13 08FDEA00724 1 20080305 A 5520 SEALANT DOUG MD10 MD1010F 3022112 WP ELEVATOR DETERIORATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 LT HORIZONTAL STAB, OUTBD ELEVATOR T/E WEDGE IS DELAMINATED IN 2 PLACES AT BEAMS. AFTER FURTHER INVESTIGATION FOUND SEA LANT DETERIORATED AT THE SEAMS WITH NO DELAMINATION NOTED. RESEALED SEAMS IAW SRM 51-41-01; VOL II; PAGE 1. MINOR RE PAIR 2 L 7 3 4F RT A22WE 2008031300135 20080313 00135 WP 2008 3 13 08FDEA00725 1 20080305 A 5230 LINER DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 CENTER CARGO DOOR LINER IS CRACKED AND DISBONDED AT THE AFT END. REPAIRED THE CENTER CARGO DOOR LINER BY REMOVING THE D AMAGE, CLEANED, & PREPARED FOR A WET LAY-UP TO THE INTERIOR & EXTERIOR SURFACES. APPLIED, CURED, & SANDED THE WET LAY-UP ON THE INTERIOR & EXTERIOR SURFACES IAW SRM 51-43-01. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008031300137 20080313 00137 WP 2008 3 13 08FDEA00727 1 20080305 A 5230 LINER DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 LOWER FWD CARGO DOOR LINER IS CRACKED IN THE AFT UPPER AREA. 2 L 7 3 4F RT A22WE 2008031300142 20080313 00142 WP 2008 3 13 08FDEA00732 1 20080305 A 5730 ARC0542 PANEL DOUG MD10 MD1010F 3022112 WP LT WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 FOUND DELAMINATION ON PANEL NR 535BR AT EXTERNAL SKIN. REPAIRED THE DELAMINATED AREA BY REMOVING DAMAGED AREA, & BY FAB RICATING & BONDING A FILLER & DOUBLER IAW SRM 51-71-00 VOL II. RESTORED FINISH IAW SRM 51-71-00; VOL II. 2 L 7 3 4F RT A22WE 2008031300145 20080313 00145 WP 2008 3 13 08FDEA00736 1 20080305 A 5730 ARC0280507 PANEL DOUG MD10 MD1010F 3022112 WP LT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 LT WING MOST INBD LOWER T/E PANEL AT THE FUEL TANK SUMP PANEL HAS DENTS AND THE REPAIR DOUBLER IS MISSING. REPLACED MIS SING DOUBLER IAW SRM 51-71-11 VOL II. REFINISHED REPAIR IAW SRM 51-71-00 VOL II & SRM 51-21-01 VOL II. 2 L 7 3 4F RT A22WE 2008031300150 20080313 00150 NM 2008 3 13 08FDEA00741 1 20080306 A 5320 146N541613 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD STRINGER L7.55, STA 1280-1300, TO EVALUATE EXISTING REPAIR. EXISTING REPA IR FOUND NOT IAW B757-200 SRM 51-70-11 FIG 1, DETAIL I, II. AFT CARGO FLOORBOARD STRINGER L7.55, REPLACED IAW B757-200 SRM 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008031300152 20080313 00152 NM 2008 3 13 08FDEA00743 1 20080306 A 5320 146N541613 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD STRINGER L16.10, STA 1300 TO EVALUATE EXISTING REPAIR. EXISTING REPAIR FOUND NOT IAW B757-200 SRM 51-70-11 FIG 1, DETAIL I, II. AFT CARGO FLOORBOARD STRINGER REPLACED IAW B757-200, SRM 51-10 -02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-02-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008031300155 20080313 00155 NM 2008 3 13 08FDEA00746 1 20080306 A 5320 146N541614 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD STRINGER L10.45, STA 1320-1340, TO EVALUATE EXISTING REPAIR. EXISTING REP AIR FOUND NOT IAW B757-200 SRM 51-70-11 FIG 1 DETAIL I, II. AFT CARGO FLOORBOARD STRINGER REPLACED IAW B757-200 SRM 51- 10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008031300158 20080313 00158 EU 2008 3 13 08FDEA00749 1 20080306 A 5414 A57244103000 PANEL AIRBUS 310 A310324 3930206 EU NR 1 NACELLE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 L/E NR 1 PYLON TOP PANEL P/N A572-44103-000 BACK SIDE HAS CHAFING MARKS IN NUMEROUS PLACES. BLENDED CHAFE MARKS IAW S RM 57-41-12 PG 102. MAT THICKNESS IS .035 IAW SRM 57-41-12, ITEM 60. MAT LOSS .006; MAT REMAINING .024, CHECKS TO BE O UT OF LIMITS IAW SRM 57-41-12. PAINTED NEW PANEL NR A57244103000; PO 610703.2 IAW SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008031300164 20080313 00164 NM 2008 3 13 SWAA081189 1 20080229 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 8L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008040100211 20080401 00211 NM 2008 4 1 ASAA0892774 1 20080307 A 5320 146A750611 FLOOR SUPPORT BOEING 737 737990 NM BS 727I CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 323AS 30021 AFT CARGO PIT FLOOR SUPPORT CORRODED AT SPLICE STA 727 I LBL 12.5. REMOVED DAMAGED SPLICE, FABRICATED SPLICE CHANNEL IA W DRG 146A7506 FIG 2. LOCATED DRILLED AND INSTALLED IAW SRM 51-40-2 PG 6 AND ASA EA 5310 02779. 2 L 7 4 4F RT A16WE 2008040100213 20080401 00213 NM 2008 4 1 SWAA081680 1 20080327 A 5311 6546551 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040100216 20080401 00216 NM 2008 4 1 ASAA0892776 1 20080307 A 5320 146A750611 FLOOR SUPPORT BOEING 737 737990 NM BS 727I CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 323AS 30021 AFT CARGO PIT FLOOR SUPPORT SPLICE CORRODED AT STA 727 I LBL 3. REMOVED DAMAGED SPLICE, FABRICATED SPLICE CHANNEL IAW D WG 146A7506 FIG 2. LOCATED DRILLED AND INSTALLED IAW B737 900 SRM 51 40 2 PG 6 ASA EA 5310 02779. 2 L 7 4 4F RT A16WE 2008040100220 20080401 00220 NM 2008 4 1 ASAA0852760 1 20080325 A 3610 SENSOR BOEING 737 737890 1384527 NM NR 1 ENGINE MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 02 559AS 35178 LEVEL AT FL370, IN CRUISE LT BLEED TRIP OFF LIGHT ILLUMINATED. FOLLOWED QRH, PRESSED TRIP RESET BUTTON. LIGHT EXTINGUI SHED FOR ABOUT 20 SECONDS AND RE ILLUMINATED. SELECTED LT PACK OFF AND DUCT PRESSURES RETURNED TO NORMAL. CHANGED NR 1 ENGINE 450 DEGREE THERMOSTAT AND THE 390 DEGREE PRE COOLER VALVE SENSOR PRECAUTIONARY. NO SYSTEM DEFECTS AT HIGH POWER ENGINE RUN. 2 L 7 2 4F RT A16WE 2008040100229 20080401 00229 NM 2008 4 1 ASAA0872788 1 20080312 A 5310 141A851110 DOOR FRAME BOEING 737 737790 13844CN NM BS 323-351 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 607AS 29751 E/E COMP DOOR SURROUND RT WEB SCRATCHED ABOVE LATCH FITTING E/E COMPARTMENT DOOR SURROUND RT FRAME WEB AT BS 328 BS 355 RBL 11.5 WL 150. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 2008040100230 20080401 00230 NM 2008 4 1 ASAA0872790 1 20080319 A 5320 149A761115 WEB BOEING 737 737790 13844CN NM LT MLG WW WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 607AS 29751 LT MLG WW RING SUPPORT ASSY O/B AFT WEB WORN AND ELONGATED AT FASTENER HOLE. REPLACED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008040100231 20080401 00231 NM 2008 4 1 ASAA0872791 1 20080319 A 5320 149A761116 WEB BOEING 737 737790 13844CN NM RT MLG WW WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 607AS 29751 RT MLG WW RING SUPPORT ASSY O/B AFT WEB WORN AND ELONGATED AT FASTENER HOLE O/B AFT WEB AT RT MLG WW RING SUPPORT ASSY. REPLACED WITH NEW PART IAW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 2008040100232 20080401 00232 NM 2008 4 1 ASAA0872792 1 20080319 A 5320 SUPPORT BOEING 737 737790 13844CN NM RT MLG WW DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 607AS 29751 RT MLG WW RING SUPPORT ASSY O/B AFT LWR CHORD HAS ELONGATED FASTENER HOLE AT FAIRING ATTACHMENT O/B AFT LWR CHORD AT RT MLG WW RING SUPPORT ASSY. REPLACED WITH NEW PART IAW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 2008040100233 20080401 00233 NM 2008 4 1 ASAA0872793 1 20080319 A 5320 SUPPORT BOEING 737 737790 13844CN NM BS 727-277 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 607AS 29751 LT MLG WW RING SUPPORT ASSY O/B AFT LWR CHORD HAS ELONGATED FASTENER HOLE AT FAIRING ATTACHMENT. REPLACED WITH NEW PART IAW B737 700 SRM CH 51 40 05 AND 51 40 06 AND 51 40 02. 2 L 7 2 4F RT A16WE 2008040100235 20080401 00235 NM 2008 4 1 ASAA0892766 1 20080310 A 5320 143A7501168 ANGLE BOEING 737 737990 NM BS 500H-508 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 323AS 30021 FWD CARGO PIT RT FLOOR TO SIDEWALL "Z" ANGLE CORRODED STA 500 H + 10" TO 506L (SIDEPLATE). CUT OUT DAMAGED AREA. FABRI CATED, LOCATED, DRILLED AND INSTALLED IAW B737 900 SRM 53 00 53 PGS 204 205 REPAIR 5. 2 L 7 4 4F RT A16WE 2008040100236 20080401 00236 NM 2008 4 1 ASAA0892767 1 20080310 A 5320 ANGLE BOEING 737 737990 NM BS 500F-500L CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 323AS 30021 FWD CARGO PIT LT FLOOR TO SIDEWALL ZEE ANGLE CORRODED STA 500 F + 10" TO 500 L LBL 23. CUT OUT DAMAGED SECTION, FABRICA TED, LOCATED, DRILLED AND INSTALLED A REPLACEMENT SECTION IAW B737 900 SRM 53 00 53 FIG 201 202 REPAIR 5. 2 L 7 4 4F RT A16WE 2008040100237 20080401 00237 EU 2008 4 1 BA08013 1 20080327 A 2560 P4010021 BATTERY AIRBUS 330 A330323 3930335 EU FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 272AY 0333 MAN - THE EMERGENCY FLASHLIGHT AT D1L (OUTBOARD SEAT) WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLASHLI GHT BATTERY. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A46NM 2008040100268 20080401 00268 NM 2008 4 1 SWAA081631 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040100274 20080401 00274 NM 2008 4 1 SWAA081630 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040200022 20080402 00022 NM 2008 4 2 CALA0800233 1 20080318 A 5753 115A5211 SUPPORT FITTING BOEING 737 737724 13844BY NM LT MLG TRUNNION CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24715 28786 LEFT MLG FWD TRUNNION SUPPORT HAS PITTING CORROSION AT UPPER I/B BUSHING. REPAIRED PER EC/RA 5741-01106. 2 L 7 2 4F RT A16WE 2008031300170 20080313 00170 NM 2008 3 13 SWAA081166 1 20080229 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 512A, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300171 20080313 00171 NM 2008 3 13 SWAA081165 1 20080229 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505B, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300172 20080313 00172 NM 2008 3 13 SWAA081191 1 20080303 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008031300173 20080313 00173 NM 2008 3 13 SWAA081140 1 20080229 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 973, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008031300185 20080313 00185 NM 2008 3 13 SWAA081199 1 20080303 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031300186 20080313 00186 NM 2008 3 13 SWAA081198 1 20080303 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 428B, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031000289 20080310 00289 NM 2008 3 10 AALA200800408 1 20080224 A 3350 COVER BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 DFW - EMERGENCY LIGHT AT AFT AISLE MISSING WIRING COVER. REPLACED WIRING COVER FOR EMERGENCY LIGHT AT AFT AISLE. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031000290 20080310 00290 NM 2008 3 10 AALA200800409 1 20080225 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 791AN 30254 NRT - EMERGENCY EXIT LIGHT AT SEAT 21G MISSING LENS. REPLACED LENS FOR EMERGENCY EXIT LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031000301 20080310 00301 NE 2008 3 10 E0X2008F00000 2 20080118 A 7200 ENGINE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RIGHT BIRD INGESTION E E0XA O OTHER C F.O.D. AP APPROACH 1 SO 35 52AW 4624 RK115 AFTER FULLY CONFIGURING AC FOR LANDING, ON APPROACH, AT APPROX 1500 FT, AGL AND 5 MILES FROM RUNWAY, AC SUFFERED A BIRD INGESTION AND CATASTROPHIC RT ENGINE FAILURE. THIS WAS FOLLOWED BY A SUCCESSFUL EMERGENCY LANDING WITH NO INJURIES TO P ASSENGERS OR CREW. ON LANDING, IT WAS NOTED THAT THE NORMAL BRAKES HAD FAILED AND THE EMERGENCY BRAKING SYSTEM WAS USED WHICH LOCKED UP THE BRAKES AND BLEW OUT BOTH MAIN TIRES AFTER USE. ON EXAMINATION OF AC IT WAS FOUND THAT THE RT ENGIN E WAS DESTROYED, THE COMPRESSOR BLADES WERE GONE AND THE HYDRAULIC LINES TO THE RT ENGINE WERE SEVERED. IT WAS ALSO NOT ED THAT THE ENGINE APPLIANCES WERE DAMAGED AS WELL AS THE ENGINE NOSE COWL. ENGINE IS BEING REMOVED AND FURTHER INSPECT 2 H 7 2 4F 4 F RT A16SW E25EA 2008031000372 20080310 00372 EA 2008 3 10 A6WA200840029 1 20080111 A 5210 HINGE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PAX DOOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 428AW 7695 PASSENGER DOOR VERTICAL FOLDING STEP HINGE REPLACED IAW SRM 51-42-06. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031100017 20080311 00017 EU 2008 3 11 08FDEA00574 1 20080222 A 5330 A53611494202 SKIN AIRBUS 310 A310324 3930206 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 EXTERIOR SKIN AT THE AFT EDGE OF THE NOSE WW CUTOUT TRIPLER IS CORRODED AT FR 17, BETWEEN STR 55 R AND STR 54 R. BLENDE D AFT EDGE OF THE NOSE W/W CUTOUT TRIPLER IAW SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM 53-12-12, DIAGRAM 102. A LODINED IAW SRM 51-21-10. PRIMED IAW SRM 51-23-10. INSTALLED FASTENERS IAW SRM 51-40-21. PAINTED IAW SRM 51-23-10. M INOR REPAIR. 2 L 7 2 4F RT A35EU 2008031200004 20080312 00004 CE 2008 3 12 DJFA2008020 1 20080227 A 3260 DOWNLOCK SWITCH BEECH MU300 400A 1155402 CE MLG FAILED E DJFA B EMER. DESCENT N FALSE WARNING DE DESCENT 1 EA 23 470LX RK478 CREW REPORTED ON APPROACH THE LT MAIN GEAR DOWN LIGHT DID NOT ILLUMINATE. THE LIGHT ILLUMINATED DURING THE TEST. EMERGE NCY PROCEDURES WERE FOLLOWED AND THE AC LANDED NORMALLY. THE DOWNLOCK SWITCH WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4F RT A16SW 2008031200006 20080312 00006 CE 2008 3 12 DXTA20082906 1 20080229 A 2130 1303581 RELAY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE CABIN PRESSURE INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 312QS 11124 5600312 CABIN CLIMBED AT MAX RATE, 10,000 FT, CABIN PRESSURE LIGHT CAME ON. THE PNUEMATIC RELAY WAS REMOVED AND REPLACED S/N OF F 15-2131. WORK PERFORMED IAW MM 21-31. SYSTEM OP'S AND LEAK CHECKED GOOD. ALSO REMOVED AND REPLACED FAULTY LT MLG SQUAT SWITCH IAW MM 32-61. SWITCH OP'S CHECKED GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2008031200007 20080312 00007 CE 2008 3 12 DXTA20082907 1 20080201 A 3200 UNKNOWN CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LANDING GEAR UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 315QS 5600315 AFTER DEPARTING, A CONTAMINATING RUNWAY GEAR UNLOCKED LIGHT, ILLUMINATED. CLEANED GEAR AND FLAP WELLS, INSPECTED, AND O PERATED SYSTEMS NUMEROUS TIMES WITH NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A22CE E25EA 2008031200009 20080312 00009 CE 2008 3 12 DXTA20082909 1 20080302 A 2720 B-NUT RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP RUDDER LOOSE E DXTA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 07 875QS 258375 AT THROTTLE ADVANCE FOR T/O, AT 75 PERCENT N1 HAD ABRUPT FULL RT RUDDER DEFLECTION. OPERATED BOTH ENGINES AND PERFORMED FUNCTIONAL TEST OF RUDDER BIAS SYSTEM, OPS CHECKS NORMAL. NO RUDDER DEFLECTION NOTED AND NO AIR LEAKS NOTED UNDER EACH ENGINE PYLON AREA. BROUGHT PLANE IN HANGAR. OPENED BOTH ENGINE COWLS AND REMOVED REAR TAILCONE. INSPECTED ALL BLEED LINE S FOR SECURITY. FOUND RT AFT B-NUT SLIGHTLY LOOSE ON RT RUDDER BIAS STRUT- TIGHTENED SAME. ALL OTHER LINES CHECKS GOOD. CLOSED BOTH ENGINE COWLS AND REINSTALLED AFT TAILCONE. ALL WORK PERFORMED IAW AMM 27-20-00. PERFORMED ENGINE RUN AND RUD DER BIAS CHECK OPS CHECK GOOD. NO KICK AND NO DEFECTS NOTED. ALL WORK PERFORMED IAW MM CHAPTER 27-20-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2008040200029 20080402 00029 2008 4 2 CALA0800238 4 20080119 A 2565 D30655123 SLIDE BOEING 757 757224 1384958 NM L2 DOOR MALFUNCTIONED A CALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 19141 8191 724 30354 DOOR 2L SLIDE BLOWN (BOTTLE DISCHARGED) BUT THE SLIDE DID NOT DEPLOY, FOUND SLIDE ON JETWAY AND UNRAVELED. REMOVED AND REPLACED SLIDE PER AMM 25-66-01. REMOVED AND REPLACED ASSIST BOTTLE PER 52-11-30. 2 L 7 2 4F RT A2NM 2008040200034 20080402 00034 NM 2008 4 2 CALA0800249 1 20080321 A 5320 141A81301 SILL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59338 23576 SILL ASSEMBLY AT STA 303.9 FORWARD LATERAL FRAME CRACKED. REMOVED AND REPLACED SILL AT STA 303.9 PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008040200050 20080402 00050 NM 2008 4 2 SWAA081531 1 20080321 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 229WN 32498 DURING SCHEDULED MV1 CHECK, FOUND EEPPLS LENS CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008040200077 20080402 00077 NM 2008 4 2 ASAA0842745 1 20080306 A 5753 6571909107 STRUCTURE BOEING 737 737490 1384715 NM TE FLAP DAMAGED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 02 788AS 28885 WHILE PERFORMING FLAP RIGGING LT O/B MIDFLAP CONTACTED WITH NR 2 SPOILER LOCK ON LEADING EDGE DAMAGE ON LT O/B MIDFLAP L EADING EDGE WAS REPAIRED IAW B737 400 SRM CH 57 53 01 FIG 201 REPAIR 7. 2 L 7 2 4F RT A16WE 2008040200084 20080402 00084 NM 2008 4 2 SWAA081621 1 20080325 A 3350 101073 LENS BOEING 737 7373Q8 1384670 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2008040200093 20080402 00093 NM 2008 4 2 ASAA0852764 1 20080325 A 2822 O-RING BOEING 737 737890 1384527 NM BOOST PUMP LEAKING A ASAA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 NM 02 587AS 35684 LT CTR BOOST PUMP IS LEAKING. REMOVED IMPELLER. FILLED CTR TANK WITH 14200. HOUSING LEAK CHECK GOOD. REPLACED LT CTR IMPELLER ASSY AND O-RINGS. LEAK AND OP CHECKS GOOD. 2 L 7 2 4F RT A16WE 2008040200105 20080402 00105 NM 2008 4 2 CALA0800258 1 20080326 A 5311 143A1120 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24715 28786 CABIN, LEFT SIDE STA 480, FRAME CRACKED BETWEEN S-8L AND S-9L AT PSU RAIL SUPPORT BRACKET. REMOVED DAMAGED SECTION OF F RAME, FAB'D REPAIR PARTS, TREATED, PRIMED AND INSTALLED IN REF TO ECRA5310-04736. 2 L 7 2 4F RT A16WE 2008040200123 20080402 00123 NM 2008 4 2 2008UALA01629 1 20080322 A 5754 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 5 SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 927UA 26649 NR 5 LE SLAT, OUTBD T/E REPAIR IS DELAMINATING FROM UPPER SKIN SURFACE. MAJOR REPAIR: REPAIRED DELAMINATION. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200134 20080402 00134 NM 2008 4 2 CALA0800271 1 20080325 A 5610 58935578 SLIDING WINDOW BOEING 737 7373T0 1384582 NM COCKPIT OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 CO-PILOTS NR 2 SLIDING WINDOW HARD TO CLOSE. ADJUSTED THE CO-PILOTS RT NR 2 WINDOW IAW B737 AMM 56-12-11. 2 L 7 2 4F RT A16WE 2008040200138 20080402 00138 NM 2008 4 2 2008UALA01635 1 20080321 A 5551 BUSHING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 RT HORIZONTAL STABILIZER FWD SPAR UPPER ATTACH LUG AFT BUSHING SHOW SIGNS OF CORROSION. MAJOR REPAIR: REMOVED CORROSION . 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200145 20080402 00145 NM 2008 4 2 2008UALA01640 1 20080321 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 339UA 24243 FOUND EEL LIGHTS INOP FROM ROW 15 BACK. REPLACED EEL LIGHT SECTION IN AFT GALLEY, OPS CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200161 20080402 00161 EA 2008 4 2 TRAX200800067 1 20080110 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 317CA 10055 FS 280 TRANSVERSE BEAM CORRODED BEYOND LIMITS AND CRACKED. REPAIRS PERFORMED IN ACCORDANCE WITH BOMBARDIER REO 670-53-1 1-047 & BOMBARDIER SERVICE BULLETIN SB670-BA-53-026. SUPPLEMENTAL SDR CLOSED 3/27/08. 2 L 7 2 4F RT A21EA 2008040200220 20080402 00220 NM 2008 4 2 SWAA081690 1 20080329 A 2121 6454051 FAN BOEING 737 7373H4 1384600 NM E&E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 29 349SW 24408 CREW REPORTED ELECTRICAL ODOR IN CABIN. TURNED OFF RECIRC AND GASPER FANS, ODOR DISSIPATED. REMOVED AND REPLACED RECIR C FAN PER MM. 2 L 7 2 4F RT A16WE 2008040200222 20080402 00222 NM 2008 4 2 SWAA081691 1 20080327 A 5753 6546434301 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED HC2 CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PE R MM. 2 L 7 2 4F RT A16WE 2008040200223 20080402 00223 NM 2008 4 2 SWAA081692 1 20080327 A 5755 654645262A HINGE BOEING 737 7373H4 1384600 NM LT SPOILER WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 4 SPOILER INBOARD HINGE WORN. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2008031200010 20080312 00010 NM 2008 3 12 DXTA20082910 1 20080302 A 5270 SWITCH AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE CARGO DOOR OUT OF ADJUST E DXTA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 07 290QS 190 RED DOOR LIGHT CAME ON DURING T/O ROLL, APPROXIMATELY 100 YRDS AFTER BRAKE RELEASE AND FULL POWER. INSPECTED CONDITION AND ADJUSTMENT OF ALL DOOR SWITCHES AND PROX SENSORS, FOUND BAGGAGE BAY FWD SWITCH (43MV) OUT OF ADJUSTMENT AND STICKING . ADJUSTED AND CLEANED IAW MM CH 52-700, OPERATIONAL CHECK GOOD. NO FURTHER DEFECTS FOUND. 2 L 7 2 4F 4 F RT A50NM E44NE 2008031200011 20080312 00011 CE 2008 3 12 DXTA20082911 1 20080302 A 3260 41HE16 SQUAT SWITCH BEECH MU300 400A 1155402 CE MLG DEFECTIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 132QS 1371 RK427 SPEED BRAKES WORK INTERMITTENTLY IN FLIGHT. TROUBLE SHOT SPEED BRAKE SYSTEM & FOUND LH WOW SWITCH DEFECTIVE AND LT THRO TTLE LEVER 85 PERCENT SWITCH OPERATING ARM OUT OF ADJUSTMENT. REMOVED UNSERVICEABLE LT WOW SWITCH & INSTALLED A NEW SWI TCH. ADJUSTED LT THROTTLE LEVER 85 PERCENT SWITCH OPERATING LEVER. JACKED ACFT & PERFORMED LT WOW SWITCH ADJUSTMENT AN D SPEED BRAKE OPERATIONAL CHECKS, NO DISCREPANCIES WERE NOTED. ACCOMPLISHED IAW MM. 32-60-00, 27-60-00 2 H 7 2 4F RT A16SW 2008031200021 20080312 00021 EU 2008 3 12 08FDEA00719 1 20080305 A 2750 B471ABM3 COMPUTER AIRBUS 310 A310324 3930206 EU NR 1 MALFUNCTIONED A FDEA A UNSCHED LANDING J S WARNING INDICATION AFFECT SYSTEMS CL CLIMB 1 SO 25 815FD 638 UPON FLAP RETRACTION GOT SLAT SYS 1 AND SLAT SYS 2 FAULTS ALONG WITH FLAP SYS 1 FAULT. AT SAME TIME LOST ALL SPD LIMIT INDICATORS ON PFDS. ALL FAULTS RESET UPON LOWERING GEAR FOR PRECAUTIONARY LANDING. A/C IN WORK, IND MX. COULD NOT DU PLICATE FAULTS - JACKED A/C AND CHECKED AOA SENSORS, PITOT SYSTEM , R&R FAC NR 1, 5 GOOD LEGS. 2 L 7 2 4F RT A35EU 2008031200022 20080312 00022 EU 2008 3 12 08FDEA00752 1 20080306 A 5270 350B53005313 COMPUTER AIRBUS 300 A300B4622 3930401 EU CARGO DOOR FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 716FD 206 206 358 ECAM WARNING OF MAIN DECK DOOR UNLOCKED TWICE CLIMBING THROUGH FL240 AND WENT OUT DESCENDING THROUGH 14000, ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01. NO PRESSURIZATION PROBLEMS NOTED. TSI OPENED FOR T/S. LT ECAM SHOWED CARGO DOOR O PEN WARNING, BUT THE RH ECAM DR PAGE SHOWED CLOSED AND LOCKED. PERFORMED FWC BITE DISPLAY IAW A300 TSM 31-50-00. FOUND F WC1 WITH CURRENT FAULTS. R&R FWC1 IAW A300 AMM 2 L 7 2 4F RT A35EU 2008031300052 20080313 00052 NM 2008 3 13 2008UALA01129 1 20080302 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 961-972 S17L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 AFT ENTRY DOOR CUTOUT FORWARD LOWER CORNER FROM BS 961 TO 972 APPROX AT STRINGER S-17L LOCATED INSIDE THE RESTRICTED ZON E SCRIBE LINE MEASURING 7.25 INCHES LONG AND 0.0035 INCHES AT DEEPEST POINT AT SCUFF PLATE LOWER EDGE IS DAMAGED. MAJOR REPAIR ACCOMPLISHED: BLENDED OUT SCRIBE LINES & FOUND A CRACKED FASTENER HOLE. REAMED HOLE & BONDED DOUBLER TO REMOVE C RACK. FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300056 20080313 00056 NM 2008 3 13 2008UALA01131 1 20080302 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 440 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 NEED TO CUTOUT CABIN FLOOR CREASE BEAM FLANGE FOR ACCESS, FWD AND AFT OF BS 440 FRAME, TO COMPLETE BS 440 FRAME REPAIR. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED 2 EA NESTED ANGLE REPAIRS AT FWD & AFT ENDS OF THE CREASEBEAM SPLICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300061 20080313 00061 EU 2008 3 13 YENA2008019 1 20080301 A 2121 20092455102 COOLING FAN AIRBUS 320 A320232 3930326 EU E&E BAY SEIZED A YENA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 15 554JB 19680 8878 1898 FLT 708, SJU-JFK, 8:00Z, AFT SMOKE AVIONICS COMPARTMENT HORN ALERT. FOUND LTV RACK FAN SEIZED. REMOVED & REPLACED RACK FAN IAW AMM 23-39-00, LIVE TV SYSTEM, OPS CHECKS GOOD. 2 L 7 2 4F RT A28NM 2008031300067 20080313 00067 SO 2008 3 13 RAIA00802027 1 20080225 A 2750 FLAP EMB 145 EMB145 3260210 SO WING FAILED A RAIA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 CE 03 803HK 145077 FLT 3538 - PIT - FLAP FAIL MESSAGE ON THE EICAS DURING LANDING. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE FLAP SYSTEM AFTER RESETTING THE FLAP SYSTEM. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2008031300068 20080313 00068 NM 2008 3 13 2008UALA01143 1 20080302 A 2720 PCU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 544UA 25322 ON PREFLIGHT, FOUND FLUID LEAKING DOWN RIGHT SIDE OF TAILCONE. FOUND INTERNAL HYD FAILURE OF LT RUDDER PCU. REPLACED LT RUDDER PCU. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031300091 20080313 00091 NM 2008 3 13 2008UALA01162 1 20080229 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R4 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 FOUND FLOOR EEL ACROSS DR 4R INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031300092 20080313 00092 NM 2008 3 13 2008UALA01163 1 20080301 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 34HJK INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY EXIT EEL LIGHT INOP, AT SEAT 34HJK. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031300101 20080313 00101 NM 2008 3 13 2008UALA01170 1 20080229 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 FLOOR EMERGENCY LIGHT FWD OF LAV 102 INOP. SECURED CONNECTOR. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031300103 20080313 00103 NM 2008 3 13 2008UALA01173 1 20080302 A 2751 18129962 INDICATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE TE FLAPS MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 339UA 24243 FLAPS DID NOT RETRACT FROM 1 ON TAKEOFF. CAME UP WITH ALTERNATE. FOUND FAULTY FLAP POSITION INDICATOR. TAPPING THE IND ICATOR WOULD UNLOCK FLAPS. REPLACED THE FLAP POSITION INDICATOR. SHOP FOUND NO FAULT WITH INDICATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300125 20080313 00125 EU 2008 3 13 08FDEA00714 1 20080305 A 5510 FAIRING AIRBUS 310 A310203 3930313 EU HORIZONTAL STAB DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT HORIZONTAL STABILIZER FWD APRON FAIRING IS DELAMINATED. INSTALLED NEW APRON FAIRING. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008031300127 20080313 00127 EU 2008 3 13 08FDEA00716 1 20080305 A 5350 A53575533000 FILLET AIRBUS 310 A310203 3930313 EU ZONE 100 PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT FILLET PANEL NR 577BL IS PUNCTURED. REPAIRED PUNCTURES IAW SRM 51-77-12. 2 L 7 2 4F RT A35EU 2008031300157 20080313 00157 WP 2008 3 13 08FDEA00748 1 20080306 A 5512 ALC74392 SKIN DOUG MD10 MD1010F 3022112 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 RT HORIZONTAL STABILIZER; UPPER INBOARD SKIN PLANK SHOWS EVIDENCE OF A CRACK FROM INBOARD TO FORWARD, APPROXIMATELY 1 IN CH, AFT PLANK. COMPLIED WITH EA 8-5510-116961. 2 L 7 3 4F RT A22WE 2008031300195 20080313 00195 NM 2008 3 13 SWAA081177 1 20080229 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 602SW 27953 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT LOWER FWD CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008031300201 20080313 00201 NM 2008 3 13 SWAA081209 1 20080303 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300203 20080313 00203 NM 2008 3 13 SWAA081182 1 20080303 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300204 20080313 00204 NM 2008 3 13 SWAA081181 1 20080303 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300205 20080313 00205 NM 2008 3 13 SWAA081180 1 20080303 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300208 20080313 00208 NM 2008 3 13 SWAA081146 1 20080229 A 5753 6546430190 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED MV2 CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2008031300211 20080313 00211 NM 2008 3 13 SWAA081147 1 20080229 A 3350 20131A BATTERY PACK BOEING 737 7373A4 1384585 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008031300212 20080313 00212 NM 2008 3 13 SWAA081213 1 20080229 A 5330 6545774 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 773, STR 22L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300219 20080313 00219 EA 2008 3 13 MASA200800179 1 20080301 A 3260 CC670321221 BRACKET CNDAIR CL600 CL6002B19 1900309 EA NLG DEFECTIVE A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 75991 7422 ASH 7230 ORD-MSN. NOSE GEAR DISAGREE ON RETRACTION. CAPT DECLARED AN EMERGENCY AND THE LANDING WAS UNEVENTFUL. REMOVE D AND REPLACED SENSOR BRACKET, GEAR SWINGS GOOD. 2 L 7 2 4F RT A21EA 2008031300221 20080313 00221 NM 2008 3 13 SWAA081221 1 20080304 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 16R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008031300225 20080313 00225 NM 2008 3 13 SWAA081164 1 20080302 A 3350 8200048401 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 284WN 32535 L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008031300226 20080313 00226 NM 2008 3 13 SWAA081187 1 20080302 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008031300230 20080313 00230 NM 2008 3 13 SWAA081190 1 20080303 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008031300237 20080313 00237 2008 3 13 SWAA081192 4 20080229 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031300241 20080313 00241 2008 3 13 SWAA081156 4 20080229 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031300244 20080313 00244 2008 3 13 SWAA081174 4 20080302 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 483WN 32472 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031300251 20080313 00251 NM 2008 3 13 SWAA081144 1 20080302 A 5523 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM RT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BEARING PER MM . 2 L 7 2 4F RT A16WE 2008031300257 20080313 00257 NM 2008 3 13 SWAA081145 1 20080302 A 5523 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 TAB HINGE BEARING PER MM . 2 L 7 2 4F RT A16WE 2008031300261 20080313 00261 NM 2008 3 13 SWAA081220 1 20080304 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER 19R CORRODED BETWEEN BS 312 AND BS 360. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008031300263 20080313 00263 NM 2008 3 13 SWAA081223 1 20080304 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 413WN 29819 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300264 20080313 00264 NM 2008 3 13 SWAA081232 1 20080304 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031300270 20080313 00270 NM 2008 3 13 SWAA081229 1 20080304 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482B, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031300272 20080313 00272 NM 2008 3 13 SWAA081233 1 20080304 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031300286 20080313 00286 EA 2008 3 13 SWIA200819316 1 20080303 A 3397 WIRE CNDAIR CL600 CL6002C10 1390015 EA CHART HOLDER SHORTED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 750SK 10207 FLT 6336 - CAPTAINS CHART HOLDER WIRING IS SHORTING OUT. SECURED HARDWARE ON CHARTHOLDER AND RESET CIRCUIT BREAKER. OP S CHECK GOOD. 2 L 7 2 4F RT A21EA 2008031300291 20080313 00291 EA 2008 3 13 SWIA200819320 1 20080304 A 2701 BEARING CNDAIR CL600 CL6002C10 1390015 EA CONTROL COLUMN ROUGH A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 771SK 10244 FLT 6272 - AILERON FLIGHT CONTROLS DO NOT FEEL SMOOTH AT LOWER AIRSPEEDS. REPLACED FIRST OFFICERS CONTROL COLUMN BEARIN GS PER AMM 27-11-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008031300292 20080313 00292 EA 2008 3 13 SWIA200819321 1 20080304 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER DE DESCENT 1 NM 07 916SW 7634 FIRST OFFICERS SIDE WINDOW OUTER PANE CRACKED ON DESCENT INTO BIS. REPLACED SIDE WINDOW IAW AMM 56-12-01, P/N NP-139322 -12, S/N OFF 00151H8821. 2 L 7 2 4F RT A21EA 2008031300298 20080313 00298 NM 2008 3 13 DLM88080311 1 20080212 A 7120 K22199SA32 ISOLATOR DOUG MD88 MD88 3023688 NM NR 2 ENG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 961DL 49980 52101 PITTING CORROSION ON RT ENGINE AFT ISOLATOR SEAT AREA OF CONE BOLT. TASK CARD 82-54300. RT ENGINE ISOLATOR AFT MOUNT R /R ON OPN 7251. REFERENCE N/R TOO84804 AT HMV-3 IN GDL. 2 L 7 2 4F RT A6WE 2008031300300 20080313 00300 EA 2008 3 13 MASA200800180 1 20080301 A 2510 SEAT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75998 7336 ASH 7409 HSV-IAD. CAPT REPORTS THE F/A SEAT WILL NOT RETRACT. CONTRACT MX WAS ABLE TO GET THE SEAT RETRACTED. 2 L 7 2 4F RT A21EA 2008031300301 20080313 00301 EA 2008 3 13 MASA200800182 1 20080302 A 5210 FASTENER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 649BR 7414 ASH 7322 ORD-MBS. PAX DOOR WILL NOT LATCH CLOSED. MX SECURED A LOOSE HI-LOK, OPS GOOD. 2 L 7 2 4F RT A21EA 2008031300302 20080313 00302 NM 2008 3 13 DLM88080313 1 20080216 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 849-860 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 961DL 49980 EXFOLIATION CORROSION ON RT CUSP WEB BETWEEN STA 849-860, BELOW CUSP WEB. REPAIRED PER ERA 398191-14MA REV A ON N/R T00 83346 AT HMV-3 IN GDL. 2 L 7 2 4F RT A6WE 2008031300310 20080313 00310 EA 2008 3 13 MASA200800183 1 20080302 A 2612 SWITCH CNDAIR CL600 CL6002C10 1390015 EA FIRE SYSTEM DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 506MJ 10073 ASH 7262 RDU-ORD. CARGO FIRE GREEN PUSH TO DISCHARGE SWITCH LIGHT ILLUMINATED. MX CLEANED SWITCHES, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008031300312 20080313 00312 WP 2008 3 13 NWAA080839917 1 20080306 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 967N 47573 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN LIGHT FOR THE RIGHT OVERWING HATCH WAS INOPERATIVE. M AINTENANCE REPLACED THE EMERGENCY EXIT SIGN POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM. THE AIRCRAFT HAS RETURNE D TO SERVICE. 2 L 7 2 4F A6WE 2008031300314 20080313 00314 NM 2008 3 13 2008UALA01002 1 20080225 A 2130 CABIN PRESSURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE UNKNOWN A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 302UA 23643 FLIGHT DIVERTED WITH A PRESSURIZATION PROBLEM. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300318 20080313 00318 NM 2008 3 13 2008UALA01003 1 20080225 A 3800 TOILET BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 3 LAVATORY LEAKING A UALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 29 788UA 26942 FLIGHT DIVERTED DUE TO WATER LEAK/OVERFLOW FROM DOOR 3 LAVATORY COMPLEX. FOUND FAULTY WATER VALVE. REPLACED TOILET. TE ST SYSTEM OPS NORMAL NO LEAKS. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008031300319 20080313 00319 EA 2008 3 13 MASA200800188 1 20080305 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 905J 15005 ASH FLT 2683 CLT-MEM. ROW 12 CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED, OPS GOOD. 2 L 7 2 4F RT A21EA 2008031300326 20080313 00326 WP 2008 3 13 UPS08851764 1 20080306 A 8011 PACKING DOUG DC8 DC873F 302199F WP STARTER UNKNOWN A IPXA E ENGINE SHUTDOWN K FLUID LOSS CL CLIMB 1 SO 01 805UP 46117 IFSD - LOSS OF OIL QTY OIL QTY JUST ABOVE ZERO, OIL PRESSURE FLUCTUATING AT 40 PSI DURING ENGINE SHUTDOWN NR 2 ENG WINDM ILLING SHUTDOWN AT 15 PSI PRESS FOR ONE HOUR. REMOVED AND REPLACED STARTER REDUCER PLUG PACKING IAW DC8 IPC 80-10-00/30 ITEM 150. SERVICE NR 2 ENG STARTER IAW DC8 MM 80-10-01-2. T/S IAW CFM MM 71-00-00. PERFORMED ENG RUN AND LEAK CHECK. NO LEAKS FOUND. OK TO RETURN TO SERVICE IAW CFM MM 72-00-00. 2 L 7 4 4F RT 4A25 2008031300330 20080313 00330 NM 2008 3 13 QXEA200800240 1 20080228 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - SMALL ROCK CHIP IN FUSELAGE SKIN LOCATED ON THE RIGHT SIDE APPROXIMATELY STATION X15.00 BETWEEN STRINGER 26R AND STRINGER 27R. REPAIRED IAW DASH 8 Q400 SRM 51-26-10, 51-21-10, 51-25-15, RD 8/4-53-2037, AND NDTM PART 6 51-00-01. 2 H 7 2 4T RT A13NM 2008031300332 20080313 00332 NM 2008 3 13 HALA0800366 1 20080305 A 8011 35054367 STARTER BOEING 767 76733A 1385209 NM RT ENGINE FAILED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, (BTB) RT ENG N2 FAILED TO ROTATE WHEN START SELECTOR IN GRD, START VALVE LIGHT EXTINGUISHED AN D DUCT PRESSURE NORMAL. FOUND STARTER BLOWN AND ADAPTER SHEARED. REMOVED AND REPLACED ADAPTER AND REMOVED AND REPLACED STARTER PER AMM 80-11-01. OPS AND LK CK OK. 2 L 7 2 4F RT A1NM 2008031300333 20080313 00333 NM 2008 3 13 HALA0800367 1 20080305 A 2841 PROCESSOR BOEING 767 76733A 1385209 NM FUEL QTY MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, LT F/Q INDICATOR BLANK, STATUS MSG LT FUEL QTY AND LT FUEL QTY IND. PER FIM 28-41-00-1 BITE O N F/Q PROCESSOR FAULT CODE 63 INSP WIRING AT LT WING SPAR AND RACK OF F/Q PROCESSOR CKS OK. CLEARED FAULT AND BIT/VERIF Y TEST NORMAL OK TO CONTINUE. 2 L 7 2 4F RT A1NM 2008031300337 20080313 00337 NM 2008 3 13 QXEA200800242 1 20080227 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 564-547 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - SEAT TRACK NR 7 AT STATION 564 TO STATION 547 GOUGED. REPAIRED IAW DASH 8 Q400 RD 8/4-53-884 AND NDTM PART 6 51-00-01. 2 H 7 2 4T RT A13NM 2008031300340 20080313 00340 NM 2008 3 13 QXEA200800245 1 20080227 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 509-529 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - SEAT TRACK NR 13 AT STATION 529 TO 509 GOUGED. REPAIRED IAW Q400 RD8/4-53-884 AND NDTM PART 6-51-00-01. 2 H 7 2 4T RT A13NM 2008031300342 20080313 00342 NM 2008 3 13 QXEA200800248 1 20080227 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - MINOR CORROSION ON SEAT TRACK NR 10 STARTING AT X1.00 TO 6.00 ON THE TOP LUGS. REMOVED AND INSTALLED NEW SEA T TRACK IAW DASH 8 Q400 SRM 51-40-15. 2 H 7 2 4T RT A13NM 2008031300344 20080313 00344 NM 2008 3 13 SA08007 1 20080306 A 3350 32145410 EPSU AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS FAULTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 820AW 26896 1397 PHX - THE LEFT, MID-CABIN, EMERGENCY POWER SUPPLY UNIT FAULTED AND WOULD NOT RESET. MAINTENANCE REPLACED THE LEFT, MID- CABIN, EMERGENCY POWER SUPPLY UNIT AND BATTERY. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A28NM 2008040200338 20080402 00338 EA 2008 4 2 TRAX200800464 1 20080320 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 AAR - PAX DOOR AFT EDGE MEMBER CRACKED UNDER STEP 832ET. REPAIRED PAX DOOR AFT EDGE MEMBER CRACK UNDER STEP 832ET IAW R EO 601R-52-11-279. NDF 15062. COMPLIED WITH EC/TC EO600-52-43 C/W. VS 13330 03/26/08. SUPPLEMENTAL SDR CLOSED 4/1/08 . 2 L 7 2 4F RT A21EA 2008040200351 20080402 00351 NM 2008 4 2 2008UALA01734 1 20080328 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EEL INOP AT LAV 112, ADJACENT TO 3R MED. FOUND BROKEN WIRE UNDER CARPET. REPAIRED WIRE AND OP CHECKED GOOD. AC OK FOR S ERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200356 20080402 00356 NM 2008 4 2 2008UALA01741 1 20080327 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 540 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 FOUND FWD PIT FRAME DENTED 2 PLACES AT STA 540 STR 25L. REPAIRED PER REO G 12281 R EV B AND EVA 71348. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200225 20080402 00225 2008 4 2 2008UALA01698 4 20080325 A 2565 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE ARM INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 515UA 24840 DOOR 2L ARM LIGHT NOT ILLUMINATED WITH DOOR ARMED. CYCLED ARMING LEVER, NO HELP. FOUND LAMP IS OUT IN INDICATOR. REL AMPED DOOR ARM SWITCH AT DOOR 2L AND RESET GIRT BAR, OVERHEAD CB OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200227 20080402 00227 NM 2008 4 2 2008UALA01699 1 20080322 A 3350 LAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 206UA 30212 EMERGENCY ROW LIGHT INDICATORS AT SEATS 19L AND 40R ARE INOP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040200233 20080402 00233 NM 2008 4 2 SWAA081699 1 20080330 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040200234 20080402 00234 NM 2008 4 2 2008UALA01703 1 20080324 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ROWS 15-18 FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 661UA 27158 EMERGENCY EXIT LIGHTS ROW 15-18 FLASH ON AND OFF. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040200237 20080402 00237 NM 2008 4 2 2008UALA01711 1 20080326 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 DOOR 1L DOES NOT DISARM. FOUND GIRT BAR ASSY BENT/DAMAGED. REPLACED GIRT BAR ASSY AND DOOR ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200242 20080402 00242 NM 2008 4 2 2008UALA01713 1 20080326 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1500 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 AFT PIT FRAME INBOARD FLANGE IS DENTED AT STA 1500 AND STR 26L. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR IAW SRM 53-00-07 RPR 5. THIS IS A CAT B ZONE 1 RPR WHICH REQU IRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS TO BEGIN WHEN ACFT RE ACHES 50,000C AND 12,000C THEREAFTER. CURRENT CYCLES IS 20,636 PER SRM 53-00-07 RPR 5 TABLE II. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200250 20080402 00250 NM 2008 4 2 2008UALA01718 1 20080326 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 330UA 24191 EMERGENCY EEL LIGHTS FROM MID TO AFT CABIN INOP. REPLACED LIGHT ASSEMBLY. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200254 20080402 00254 NM 2008 4 2 2008UALA01722 1 20080326 A 2421 IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEFT DISCONNECTED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 655UA 25393 EICAS MSG L GEN DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUM. GEN DRIVE DISCONNECTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040200257 20080402 00257 NM 2008 4 2 2008UALA01725 1 20080327 A 5310 PLATE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 305UA 23666 FLAP STAINLESS STEEL WEAR PLATE ON RIGHT FUSELAGE FAIRING AFT OF WHEEL WELL IS CRACKED APPROX 1.5 INCH AT FWD LOWER SECT ION. REPLACED STAINLESS STEEL WEAR PLATE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200266 20080402 00266 NM 2008 4 2 08FDEA01166 1 20080327 A 5320 149N75232 STIFFENER BOEING 757 7572B7 1384964 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 906FD 27148 RIGHT MLG WHEEL WELL, STIFFENER FOR FAIRING STRUCTURE BETWEEN STA 1128-1146, RBL 75 IS CORRODED. AFTER CORROSION REMOVA L FOUND STIFFENER TO BE OUT OF SRM 53-00-71, FIG 101, DETAIL VII LIMITS. ORIGINAL MATERIAL THICKNESS .050", AFTER CORRO SION REMOVAL .036 INCH. REMOVED STIFFENER IAW SRM 51-40-02. FABRICATED REPLACEMENT STIFFENER ON MAE TRAVELER NR T8/729 363 FROM 7075 - O .050", HEAT TREATED TO T6 IAW SRM 53-40-71. INSTALLED REPLACEMENT STIFFENER IAW SRM 51-40-05 AND 51- 40-02. 2 L 7 2 4F RT A2NM 2008040200267 20080402 00267 NM 2008 4 2 08FDEA01167 1 20080327 A 5320 146N539117 PANEL BOEING 757 7572B7 1384964 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 AFT CARGO FLOOR, SIDE PANEL (THRESHOLD AREA) HAS SURFACE CORROSION BETWEEN STA 1380-1440. REMOVED CORROSION, L= 3", W= 3", D= .020", FOUND TO BE OUT OF LIMITS PER SRM 53-60-35 WHICH REFERS ALLOWABLE DAMAGE TO SRM 53-00-53, FIGURE 101, DETA IL V. REMOVED SIDE PANEL IAW SRM 51-40-02. FABRICATED REPLACEMENT SIDE PANEL ON MAE TRAVELER NR T7706722 FROM 7075 - 0 .063C, HEAT TREATED TO T6 IAW SRM 51-10-02. LOCATED AND DRILLED REPLACEMENT SIDE PANEL IAW SRM 51-40-05. TREATED AND PRIMED REPLACEMENT SIDE PANEL IAW SRM 51-20- 01. TOP COATED SIDE PANEL IAW AMM 51-20-00. INSTALLED REPLACEMENT SIDE PANEL IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008040200270 20080402 00270 WP 2008 4 2 08FDEA01174 1 20080328 A 5210 ABA71263 INTERCOSTAL DOUG MD10 MD1010F 3022112 WP R1 DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 ON THE R-1 DOOR, LOWER, FWD AND AFT INTERCOSTALS ARE GOUGED. FOUND TO BE WITHIN LIMITS IAW SRM 52-00-01 VOL I. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. INSTALLED 2 EA INTERCOSTALS IAW SRM 51-31-01 VOL III & 51-33-01 VOL III. 2 L 7 3 4F RT A22WE 2008040200272 20080402 00272 NM 2008 4 2 08FDEA01177 1 20080328 A 5315 BAC1518338 FLOORBEAM BOEING 727 727227 1384078 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 MAIN DECK FLOORBEAM UPPER FLG IS DAMAGED BS 1148, RBL 43-49 , WL 208. REMOVED SURROUNDING STRUCTURE, REMOVED UPPER T-CAP , PREFORMED 10X VISUAL INSPECTION OF TRIMMED TREATED, PRIMED AREA. FABRICATED SURROUNDING STRUCTURE. REF SRM 51-30- 2 PG 2. SRM 53-10-08 FIG 3, AND EA 7-5310-118248, CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008040200274 20080402 00274 WP 2008 4 2 08FDEA01179 1 20080328 A 4910 TSCP7004B LINER DOUG MD10 MD1010F 3022112 WP ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LINER OF APU INTAKE HAS SOME EROSION TAKING PLACE ON THE LOWER HALF. APU LINER AT THE INTAKE WAS FOUND TO BE WITHIN SER VICEABLE LIMITS AND TO BE TRACKED AT B-CHECK INTERVALS IAW FEDEX EA 8-4920-119704. 2 L 7 3 4F RT A22WE 2008040200275 20080402 00275 WP 2008 4 2 08FDEA01180 1 20080328 A 5347 ADA361512 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1099 BETWEEN SEAT TRACK X= -78 AND X=-81 FOUND CORROSION ON FLOOR SUPPORT REMOVED CORROSION IS OUT LIMIT THE REWORK. REPLACED SUPPORT FOR DWG ADA3615 AND SRM 51-35-01 VOL II. 2 L 7 3 4F A22WE 2008040200276 20080402 00276 WP 2008 4 2 08FDEA01181 1 20080328 A 5754 ARB137910 COVER DOUG MD10 MD1010F 3022112 WP SLAT TRACK CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT WING 1 SLAT TRACK COVER FWD END IS CHAFED. REMOVED DAMAGED COVER. LOCATED AND DRILL HOLES IN THE NEW COVER REF D C/MD-10 SRM 51-31-01; VOL II INFO: ADJUSTMENTS TO BE PERFORMED ON FEDEX W/C NR 27X8501. 2 L 7 3 4F RT A22WE 2008040200277 20080402 00277 WP 2008 4 2 08FDEA01182 1 20080328 A 5310 ADA36751 FITTING DOUG DC10 DC1010F 3022111 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION MAIN CARGO DOOR COVER JAM SUPPORT FITTING AFTER INSPECTION FOUND BORE "B" OF FITTING NR 3 WITH CORROSION (DIAMETER .58") (REF EO FEDEX 8-5230-117635). PERFORMED REWORK HOLE FOR SRM 53-50-00 FIG 17, PERFORMED N DI AND INSTALLED BUSHING FOR SRM 53-50-00 FIG 17 VOL I. 2 L 7 3 4F A22WE 2008040200281 20080402 00281 NM 2008 4 2 SWAA081722 1 20080327 A 3350 8100022608 STRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 RIGHT AFT CABIN EEPLS STRIP LOOSE. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008040200286 20080402 00286 EU 2008 4 2 08FDEA01188 1 20080328 A 5321 A5378198422200 FLOOR PANEL AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 MAIN DECK FLOOR STRUCTURE HAS CORROSION ON THE UPPER SURFACE OF THE FLOOR WEBBING AT APPROX LBL 87 BETWEEN FRAMES 34 AND 35. BLENDED OUT THE CORROSION REF A310-200 SRM 51-74-10; PARA 5. ORIGINAL THICKNESS 0.094 AND 0.087 REMAINING. MATER IAL REMOVED 0.007. FOUND TO BE OUT OF LIMITS IAW A310-200 SRM ; SUPP 53-14-15; FIG 1. UT GAUGE T82750 USED. REMOVED FLOOR WEB IAW A310- 200 SRM 51-40-21; PGS 6-7. DRILLED HOLES IN NEW WEB P/N A5378198422200, PO 612403.1 IAW A310-200 SRM 51-40-44; PGS 1-7. ALODINED HOLES IAW A310-200 SRM 51-21-10 AND PRIMED HOLES IAW A310-200 SRM 51-23-10. INSTALLED FLOOR WEB P/N A5378198422200, PO 612403.1 IAW A310-200 SRM 51-40-21. APPLIED CIC REF A310-200 AMM 51-22-00-0. 2 L 7 2 4F RT A35EU 2008040200287 20080402 00287 NM 2008 4 2 CALA0800284 1 20080307 A 5320 69489854 ATTACH ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INTERCOSTAL ATTACH ANGLE TO FRAME AT STA 360 AND STR 10 LT LOCATION IS CRACKED (MARKED). REMOVED AND REPLACED INTERCOST AL ATTACH ANGLE TO FRAME AT STA 360 AND STR 10 LT IAW B737 SRM 51-40-02 AND PACE EA350-53-003 CAL AND EC/RA 53-10-04741. 2 L 7 2 4F RT A16WE 2008040200288 20080402 00288 EU 2008 4 2 08FDEA01189 1 20080328 A 5720 A5777020920400 RUB STRIP AIRBUS 310 A310203 3930313 EU ZONE 500 CHAFED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 425FE 264 LEFT WING SPOILER T/E RUB STRIP IS CHAFED. REMOVED T/E RUB STRIP IAW AIRBUS CMM 57-73-11. RECEIVED NEW RUB STRIP P/N A 5777020920400, PO 612493.2. LOCATED AND DRILLED IAW AIRBUS CMM 57-73-11. INSTALLED RUB STRIP IAW AIRBUS CMM 57-73-11. PRIMED AND TOP COATED IAW A310-200 SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008040200289 20080402 00289 NM 2008 4 2 CALA0800285 1 20080307 A 5320 694688210 ATTACH ANGLE BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INTERCOSTAL ATTACH ANGLE TO FRAME AT STA 360 AND STR 10 LT LOCATION IS CRACKED (MARKED). REMOVED AND REPLACED INTERCOST AL ATTACH ANGLE TO FRAME AT STA 360 AND STR 10 LT IAW B737 SRM 51-40-02 AND PACE EA350-53-003 CAL AND EC/RA 53-10-04741. 2 L 7 2 4F RT A16WE 2008040200291 20080402 00291 EU 2008 4 2 08FDEA01191 1 20080328 A 5730 A5721023600000 PANEL AIRBUS 310 A310203 3930313 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT WING ROOT HYD SHELF GROUND CONNECTION ACCESS PANEL MATING SURFACE IS WORN. CLEANED CUTOUT AREA REF A310-200 SRM 5 1-73-10. (NO MATERIAL LOSS); FOUND ONLY PAINT MISSING. ALODINED REF A310-200 SRM 51-21-10; PG 4. PRIMED AND PAINTED R EF A310-200 SRM 51-23-10; PG 1. 2 L 7 2 4F RT A35EU 2008040200295 20080402 00295 NM 2008 4 2 KCSA081182 1 20080319 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 EXTERNAL FUSELAGE SKIN, INTERNAL SURFACE IS CORRODED AT STA 1239 BETWEEN STR 4L & 5L. 2 L 7 4 4F RT A20WE 2008040200303 20080402 00303 NM 2008 4 2 KCSA081188 1 20080320 A 5320 STIFFENER BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 STA-1540 FRAME VERTICAL STIFFENER DAMAGE AT RBL-14. 2 L 7 4 4F RT A20WE 2008040200305 20080402 00305 NM 2008 4 2 KCSA081190 1 20080320 A 5411 FRAME BOEING 747 747146 1384905 NM NR 2 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 NR 2 PYLON AFT ENG MOUNT BULKHEAD FRAME CRACKED .5 INCH AT NAC STA 221.9. 2 L 7 4 4F RT A20WE 2008040200309 20080402 00309 NM 2008 4 2 KCSA081193 1 20080321 A 5330 SKIN BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 STA-400 STR-39R TO STR-40R AT BUTT SPLICE AREA SKIN DAMAGED. 2 L 7 4 4F RT A20WE 2008040200311 20080402 00311 2008 4 2 HALA0800434 4 20080325 A 3400 INDICATION SYS BOEING 767 767300 1385204 NM COCKPIT MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 580HA 28140 ETOPS SIGNIFICANT SYSTEM, YELLOW RA BOX JUST BELOW GREEN DH VALUE ON CAPT ADI DISPLAYED STEADY OK IN ALT EFI AUTO LAND N O LAND 3. RERACKED CAPT R/A LEFT PER AMM 34-33-01-404-006, OPS CHECKS NORMAL PASSED TEST 40. 2 L 7 2 4F RT A1NM 2008040200312 20080402 00312 NM 2008 4 2 KCSA081195 1 20080321 A 5311 FRAME BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 STA-1780 FRAME WEB DAMAGED AT RBL-17 ABOVE STR-43R. 2 L 7 4 4F RT A20WE 2008040200321 20080402 00321 NM 2008 4 2 QXEA200800333 1 20080320 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 352PH 494 PDX - C4 - LT INBD SEAT TRACK NR 4 HAS SEVERAL AREAS OF CORROSION AT STA X209, X228, X240, X250, X268. REMOVED SEAT TRA CK AND INSTALL NEW SEAT TRACK IAW DHC 8 (200) SRM 51-40-00 AND 51-40-11. 2 H 7 2 4T RT A13NM 2008040200323 20080402 00323 EU 2008 4 2 TRBA2008035 1 20080330 A 2612 WARNING LIGHT AEROSP ATR72 ATR72212 8680945 EU FIRE WARNING FALSE INDICATION A TRBA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 29 308AE 309 WHEN MOVING CONDITION LEVERS FWD, FIRE INDICATION ON CAP AND FIRE HANDLE. AFTER CONDITION LEVERS WERE MOVED TO FUEL S/O , FIRE INDICATION ON CAP AND FIRE HANDLE EXTINGUISH. PERFORMED SEVERAL OPERATIONAL CHECK ON BOTH ENGINE FIRE DETECTION SYSTEM WITH ENGINES RUNNING AS PER MM NR 26-12-00. ALSO, RESET MFC SYSTEM AS PER MM NR 31-48-00. AFTER INVESTIGATION, CONCLUDE THIS WAS A FALSE INDICATION. 2 H 7 2 4T RT A53EU 2008040200328 20080402 00328 NM 2008 4 2 GTIA0800042 1 20080311 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 502NK 2433 EVIDENCE OF CORROSION ON BEAM Y1292 FR 66 THROUGH FR 69. REMOVED AND REPLACED FLOORBEAM Y1292 FROM FR 66 THROUGH FR 69 IAW A319 SRM 51-72-1. 2 L 7 2 4F RT A28NM 2008040200331 20080402 00331 NM 2008 4 2 ASAA0852784 1 20080328 A 2150 3989083 VALVE BOEING 737 737890 1384527 NM A/C PACK FAULTY A ASAA O OTHER J WARNING INDICATION DE DESCENT 1 NM 02 583AS 35681 RIGHT "PACK" LIGHT ILLUMINATED WITH RECALL PUSHED DURING LANDING CHECKLIST, RAN CHECKLIST ON TAXI IN PACK RESET. PERFOR MED FIM 21 62 TASK 801 NR 2 LOGGED "THIS PACK TCV". REPLACED RT PACK TEMP CONTL VLV. PERFORMED LEAK CHECK, NO LEAKS NO TED. PERFORMED OP CHECK, CHECKED GOOD. PERFORMED BITE CHECK, NO FAULTS NOTED. 2 L 7 2 4F RT A16WE 2008040200332 20080402 00332 NM 2008 4 2 ASAA0852785 1 20080329 A 2150 AS13806N0130L SENSE LINE BOEING 737 737890 1384527 NM NR 2 ACM LEAKING A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 583AS 35681 WHILE WORKING RT PACK ISSUE, FOUND SENSE LINE LEAKING IN 3 SPOTS. REPLACED RT ACM SENSE LINE WITH TEMPORARY FLEX LINE. REPLACED TEMPORARY FLEX LINE WITH PERMANENT LINE. 2 L 7 2 4F RT A16WE 2008040200336 20080402 00336 EA 2008 4 2 TRAX200800435 1 20080319 A 5342 ATTACH ANGLE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 355CA 10067 SUSPECTED CRACK AT RIGHT SIDE BASE OF VERTICAL STAB AT FS 1181. WORK COMPLETED IN ACCORDANCE WITH: PERFORMED EDDY CURR ENT INSPECTION OF RIGHT SIDE BASE OF VERTICAL STAB AT FS 1181 IAW CRJ700 NDTM 51-20-006. AREA IS CONFIRMED CRACKED AND MARKED. 03/19/08 VTJ7010159. REMOVED DAMAGE PER REO 670-55-31-018. PERFORMED EDDY CURRENT INSPECTION OF CUT LINE ON RIGHT DRAG ANGLE IAW REO 670-55-31-018 PER CRJ 700 NDTM 51-20-006. NO DEFECTS NOTED. 03/20/08 VTJ7010159. STARTED FAB RICATING 670-55-31-018-3 DOUBLER AND -4 FILLER FROM 2024T3 .090" PO# TO3606 RT SIDE V/STAB TO FUSELAGE ATTACH ANGLE PER REO 670-55-31-018. FINISHED FABRICATING DOUBLER -3 AND FILLER -4 PER REO 670-55-31-018. INSTALLED FILLER AND DOUBLER I 2 L 7 2 4F RT A21EA 2008040200337 20080402 00337 EA 2008 4 2 TRAX200800440 1 20080320 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 AAR - BRACKET AT FS 484 LBL 36 CRACKED. REMOVED BRACKET AT FS 484 LBL 36, FABRICATED AND INSTALLED IN ACCORDANCE WITH E C/TC REO 601R-53-41-059. DR 15098. SUPPLEMENTAL SDR CLOSED 4/1/08. 2 L 7 2 4F RT A21EA 2008040100249 20080401 00249 NM 2008 4 1 GTIA0800048 1 20080311 A 5310 BEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 502NK 2433 EVIDENCE OF CORROSION ON WEB BEAM Y1292 FR69 THROUGH FR70 RT SIDE. REMOVED AND REPLACED WEB ASSY IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008040100253 20080401 00253 EU 2008 4 1 USAA920080712 1 20080313 A 5320 D534880048203 SILL AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 621AW 53 SAL - MAJOR REPAIR - C6 CHECK - CORROSION ON THE R2 DOOR CUT OUT LOWER SILL SHAPE SILL, BS 3207/FR 67, S23R. REPLACED T HE R2 DOOR CUT OUT LOWER SILL SHAPE SILL, BS 3207/FR 67, S23R IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008040100254 20080401 00254 NM 2008 4 1 USAA920080713 1 20080328 A 5531 65476461 RIB BOEING 737 7374B7 1384702 NM ZONE 300 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 456UW 25020 MIA - MAJOR REPAIR - PAINT LINE - VERTICAL STABILIZER HINGE RIB CRACKED. REPAIRED VERTICAL STABILIZER HINGE RIB IAW USA IRWAYS EA 100364. 2 L 7 2 4F RT A16WE 2008040100255 20080401 00255 SO 2008 4 1 SIMA200809101 1 20080324 A 5320 14522178603 SILL EMB 145 EMB145LR 3260212 SO CARGO DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 685AE 9563 5000 14500836 DURING A IMBV INSPECTION, THE CARGO DOOR CUT OUT CENTER SILL WAS FOUND TO BE CORRODED. REMOVED CORRODED CENTER SILL. O BTAINED NEW SILL, POSITIONED AND DRILLED FOR FASTENERS. CLEANED, ALODINED AND PRIMED FASTENER HOLES AND INSTALLED IAW E MBRAER SRM (SRM 145-1142 REV 39) CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008040100257 20080401 00257 2008 4 1 ASAA0852758 4 20080323 A 2210 721101A1 SWITCH BOEING 737 737890 1384527 NM GLARESHIELD FAULTY A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 583AS 35681 AUTOPILOT A WILL NOT ENGAGE. CAPT'S DISCONNECT SWITCH BAD. REPLACED AND CHECKED PER MM 22 11 41, TASK 000 801, NORMAL. 2 L 7 2 4F RT A16WE 2008040100258 20080401 00258 NM 2008 4 1 ASAA0842740 1 20080305 A 5320 6545855124 WEB BOEING 737 737490 1384715 NM BS 951-986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 AFT CABIN UNDERSIDE OF WEB 2 STA 975 986.5 RBL 48 WL 207.5 CORRODED. REPLACED WITH MADE REPAIR PART. 2 L 7 2 4F RT A16WE 2008040100261 20080401 00261 NM 2008 4 1 ASAA0842742 1 20080305 A 5340 BRACKET BOEING 737 737490 1384715 NM BS 787 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 AFT CARGO PIT RT FLOOR SHIELD FWD GUSSET BRACKET CORREODED AT BS 787 RBL 23, REPLACED WITH MADE REPAIR PART. 2 L 7 2 4F RT A16WE 2008040100262 20080401 00262 NM 2008 4 1 ASAA0842743 1 20080305 A 5340 BRACKET BOEING 737 737490 1384715 NM BS 787 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 AFT CARGO PIT RT FLOOR SHIELD FWD GUSSET BRACKET CORRODED AT BS 787 RBL 23, REPLACED WITH MADE REPAIR PART. 2 L 7 2 4F RT A16WE 2008040100266 20080401 00266 NM 2008 4 1 SWAA081632 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040100276 20080401 00276 NM 2008 4 1 SWAA081646 1 20080325 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008040100285 20080401 00285 NM 2008 4 1 SWAA081674 1 20080327 A 5330 6545800 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008040100286 20080401 00286 2008 4 1 SWAA081675 4 20080327 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 779SW 27884 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008040100302 20080401 00302 NM 2008 4 1 SWAA081714 1 20080327 A 5330 6545768 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 300, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008040200018 20080402 00018 EA 2008 4 2 TRAX200800421 1 20080312 A 5755 NUT CNDAIR CL600 CL6002B19 1900309 EA RT SPOILERON CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 CORROSION ON RT WING SPOILERON HINGE POINT NUTS. REMOVED AND REPLACED O/B HINGE POINT NUT ON RT WING SPOILERON WITH NE W SERVICEABLE NUT IAW AMM 27-64-01. 2 L 7 2 4F RT A21EA 2008040200036 20080402 00036 NM 2008 4 2 CALA0800250 1 20080306 A 5310 6520722U70 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 FORWARD CARGO DOOR CUTOUT FORWARD FRAME IS CRACKED AT THE STOP PAD FITTING ATTACH POINT AT STRINGER 21R. REMOVED CRACKE D FRAME PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008040200062 20080402 00062 NM 2008 4 2 ASAA0842738 1 20080304 A 5315 654681179 FLOORBEAM BOEING 737 737490 1384715 NM BS 986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 AFT CABIN STA 986.50 FLOORBEAM UPPER CAP TOP SURFACE CORROSION FOUND BETWEEN RBL35 AND 40. REPAIRED WITH MADE REPAIRED PART. 2 L 7 2 4F RT A16WE 2008040200078 20080402 00078 NM 2008 4 2 ASAA0842753 1 20080312 A 5753 6546430190 SKIN BOEING 737 737490 1384715 NM RT FORE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 788AS 28885 DENTS FOUND ON INBD RT FOREFLAP UPPER SURFACE. DENTS ON UPPER SURFACE OF RT INBOARD FOREFLAP 8" FROM T/E APPROX 48" AND 77" FROM 18 END REPAIRED IAW B737 400 SRM 51 70 10 REPAIR 3. 2 L 7 2 4F RT A16WE 2008040200111 20080402 00111 NM 2008 4 2 SA08022 1 20080324 A 3240 21684 BRAKE AIRBUS A319 A319132 3930340 NM ZONE 700 OVERHEATED A USAA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 19 838AW 29022 4161 2615 DFW - FLT 393 - LAS TO DFW - AFTER TAKEOFF, THE NR 3 MLG BRAKE HEATED UP TO 310 DEGREES CELSIUS. THE CREW LOWERED THE L ANDING GEAR AND ALLOWED THE BRAKES TO COOL TO 250 DEGREES CELSIUS. THE LANDING GEAR WAS THEN RETRACTED AND THE FLIGHT C ONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE NUMBER THREE BRAKE TEMPERATURE INDICATION SYSTEM ON MEL. THE NUMBER THREE BRAKE ASSEMBLY WAS LATER REPLACED. 2 L 7 2 4F RT A28NM 2008040200122 20080402 00122 NM 2008 4 2 2008UALA01627 1 20080322 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 849UA 1649 CREW OXYGEN SYSTEM NEEDS SERVICE, CAUSE UNKNOWN. SERVICED CREW O2 SYSTEM, NO LEAKS WERE NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200165 20080402 00165 2008 4 2 2008UALA01658 4 20080321 A 2565 BOTTLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ESCAPE SLIDE READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 ESCAPE SLIDE BOTTLE LOW . 2 L 7 2 4F 4 F RT A1NM E24NE 2008040200187 20080402 00187 NM 2008 4 2 2008UALA01676 1 20080323 A 3510 89151114 CYLINDER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW OXYGEN READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 180UA 25224 CREW OXYGEN CYLINDER PRESSURE LOW. REPLACED WITH SERVICEABLE CYLINDER AND THEN OPERATION AND LEAK CHECKED GOOD PER AMM 1 2-15- 08 P301. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200230 20080402 00230 NM 2008 4 2 2008UALA01701 1 20080322 A 2120 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 792UA 26934 SMOKE OR FUMES IN CABIN, SOURCE UNKNOWN CREW COMMENTS: RECIRC FANS WERE OFF HOT DUCT ODOR IN COCKPIT AND 1ST CLASS. RAN PACK FULL HOT FOR 20 MINUTE, ALL NORMAL. RAN RECIRCULATING FAN, ALL OK UNABLE TO DUPLICATE SMOKE OR FUMES WHILE A-C ON GROUND. ALL SYS OPERATE NORMAL SUSPECT FOOD BURNING. ACFT OK FOR SERVICE. NFF 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040200255 20080402 00255 2008 4 2 2008UALA01723 4 20080325 A 2565 OXYGEN BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L3 DOOR SLIDE READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 174UA 24381 FOUND DOOR 3L O2 BOTTLE PRESSURE LOW. SUSPECT FAULTY SEAL. REPLACED OXYGEN BOTTLE. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200256 20080402 00256 NM 2008 4 2 2008UALA01724 1 20080326 A 3510 OXYGEN SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 303UA 23644 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED OXYGEN SYSTEM. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200292 20080402 00292 NM 2008 4 2 KCSAO81179 1 20080315 A 5330 SKIN BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE SKIN IS CORRODED AT STA 1239 BETWEEN STR 7L & 8L. 2 L 7 4 4F RT A20WE 2008040200297 20080402 00297 NM 2008 4 2 HALA0800435 1 20080322 A 3150 WARNING LIGHT BOEING 767 76733A 1385209 NM AILERON LOCK FALSE ACTIVATION A HALA O OTHER N FALSE WARNING AP APPROACH 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, AILERON LOCK OUT CAME ON APPROACH AT 250 KTS STAYED ON FOR 1.5 MINUTES. T/S AS PER FIM 27 11 00 AILERON LOCK OUT WOULD NOT FAIL ON GROUND MCDP SHOWS NO LAST FLIGHT FAULTS REPLACED LEFT ADC AS PER MM 34 12 01 404. 2 L 7 2 4F RT A1NM 2008040200300 20080402 00300 NM 2008 4 2 KCSA081185 1 20080320 A 5330 SKIN BOEING 747 747SR46 1384816 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 STA-2120 STR-39R TO STR-41R AREAS OF CORROSION AROUND FASTENERS. 2 L 7 4 4F RT A20WE 2008040200310 20080402 00310 NM 2008 4 2 KCSA081194 1 20080321 A 5311 FRAME BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 STA-1760 RBL-16 FRAME WEB DAMAGED AROUND FASTENERS. 2 L 7 4 4F RT A20WE 2008040200339 20080402 00339 EA 2008 4 2 TRAX200800478 1 20080320 A 5270 1961002 LIGHT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FAILED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 PASSENGER DOOR HANDLE LEVER, "EXIT/PULL" BETA LIGHT FAILED FUNCTIONAL TEST. REMOVED DOOR HANDLE LEVER LIGHT AND REPLACE D WITH SERVICEABLE LIGHT P/N 1961002 IAW SRM 51-41-02. PASSED FUNCTIONAL TEST IAW AMM 33-51-09-720-801. 2 L 7 2 4F RT A21EA 2008040200340 20080402 00340 NM 2008 4 2 KCSA081202 1 20080224 A 5411 FRAME BOEING 747 747146 1384905 NM NR 2 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 NR 2 PYLON AFT ENGINE MOUNT BULKHEAD FWD O/B FRAME CRACKED 1.375 INCH LONG EXTENDING FROM FASTENER HOLE LOWER END OF CUT OUT NAC STA 221.9. 2 L 7 4 4F RT A20WE 2008040200341 20080402 00341 NM 2008 4 2 KCSA081204 1 20080325 A 5411 FRAME BOEING 747 747246F 1384850 NM NR 3 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 NR 3 PYLON FRAME CRACKED AT NAC STA 268.06. 2 L 7 4 4F RT A20WE 2008040200344 20080402 00344 NM 2008 4 2 KCSA081207 1 20080326 A 5311 FRAME BOEING 747 747SR46 1384816 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 FWD PIT FUSELAGE FRAME UPPER CHORD DENTED AT BS 800. 2 L 7 4 4F RT A20WE 2008040200347 20080402 00347 NM 2008 4 2 USAA920080714 1 20080330 A 5512 SKIN BOEING 737 7373G7 1384595 NM ZONE 300 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 CLT - MAJOR REPAIR -B-CHECK - .5 INCH CRACK ON RT HORIZ STAB LWR SKIN AT STA 125 - 128 AT REAR SPAR. REPAIRED IAW EA 10 0338, US AIRWAYS TYPICAL REPAIR 55-10-07, REV C. 2 L 7 2 4F RT A16WE 2008040200357 20080402 00357 EU 2008 4 2 2008UALA01742 1 20080327 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS WEAK A UALA O OTHER W INADEQUATE Q C CL CLIMB 1 WP 29 497UA 1847 F/A REPORTED THAT DURING CLIMB-OUT THE EMERGENCY EXIT LIGHTS CAME ON ALL ON THEIR OWN. FOUND EMERGENCY POWER SUPPLY WEAK . REPLACED EPSU AT DL1. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200366 20080402 00366 NM 2008 4 2 2008UALA01752 1 20080327 A 2697 PIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FIRE BOTTLE BENT A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 224UA 30225 BENT PIN ON FWD DUMP CARGO FIRE BOTTLE PRESS SWITCH. INSTALLED NEW FIRE BOTTLE PER MM 26 23 01.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040200368 20080402 00368 NM 2008 4 2 2008UALA01754 1 20080328 A 2421 VALVE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LT IDG POPPED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 669UA 30025 CB M4 "IDG VALVE" LEFT ENG POPPED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040200375 20080402 00375 WP 2008 4 2 NWAA081259928 1 20080329 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8921E 45836 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN LIGHT FOR THE FWD RIGHT OVERWING HATCH WAS INOPERATIVE . MAINTENANCE REPLACED THE BATTERIES. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F A6WE 2008040200376 20080402 00376 2008 4 2 08FDEA01193 4 20080328 A 3444 A539735540040096 HOUSING AIRBUS 310 A310203 3930313 EU RADIO ALTIMETER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 RADIO ALTIMETER TRANSMISSION ANTENNA MOUNT RING HOUSING CAVITY AND DOME NUTS ARE CORRODED. REMOVED ANTENNA HOUSING IAW A310-200 AMM 34-43-11-4. REMOVED CORROSION IAW FEDEX A310-200 SRM 51-74-10. 100 PERCENT MATERIAL LOSS; FOUND T O BE OUT OF LIMITS IAW FEDEX A310-200 SRM 53-10-00. RECEIVED NEW HOUSING A539735540040096; PO 613251.1. INSTALLED HOUS ING IAW FEDEX A310-200 AMM 34-42-11-4. 2 L 7 2 4F RT A35EU 2008040200381 20080402 00381 WP 2008 4 2 08FDEA01198 1 20080328 A 5320 AGA38749 FLOOR SUPPORT DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 AFT PIT FS 1840 LBL 19 FLOORBOARD SUPPORT IS CORRODED. CUT OUT DAMAGE IAW SRM 53-00-01; FIG 8 VOL I. FABBED REPAIR DOU BLERS & FILLER PER SRM 53-00-01 FIG 8 SHEET 2 VOL I. ALODINED & PRIMED REPAIR DOUBLERS & FILLER PER SRM 51-21-01 PGS 21 & 24 VOL II. INSTALLED REPAIR DOUBLERS & FILLER PER SRM 51-33-01 PG 34 VOL II & SRM 53-00-01 FIG 8 SHEET 2 VOL I. 2 L 7 3 4F RT A22WE 2008040200383 20080402 00383 NM 2008 4 2 08FDEA01201 1 20080328 A 5320 143N85603 ATTACH BRACKET BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 NR 1 CARGO DOOR, CUT OUT LOWER SILL, THRESHOLD TIE DOWN ATTACH BRACKET, THIRD ONE FROM FWD END HAS CORROSION. REMOVED C ORROSION IAW SRM 51-10-02, L= 1.75", W= .625", D= .009", ORIGINAL MATERIAL THICKNESS .063". FOUND TO BE OUT OF SRM 53-3 0-15, FIG 101, DETAIL IV LIMITS. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02 AND 51-40-01. 2 L 7 2 4F RT A2NM 2008040200389 20080402 00389 WP 2008 4 2 08FDEA01209 1 20080331 A 5330 NFA6013501 SKIN DOUG DC10 DC1010F 3022111 WP FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING REPAIR ASSESSMENT AN EXISTING REPAIR AT FUSELAGE SKIN WAS FOUND NOT IN CONFORMITY WITH APPROVED DATA REPAIR HAS B EEN REPLACED WITH A NEW IAW SRM 53-50-00 FIG 26, VOL I. 2 L 7 3 4F A22WE 2008040200365 20080402 00365 NM 2008 4 2 2008UALA01751 1 20080327 A 2621 FIRE BOTTLE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE AFT DUMP FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 224UA 30225 NEWLY REPLACED AFT DUMP FIRE BOTTLE FAILED TEST. REPLACED DUMP BOTTLE. AC OK FORE SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040200373 20080402 00373 NE 2008 4 2 NWAA081239989 2 20080328 A 7230 COMPRESSOR DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7 52053 NE NR 2 ENGINE STALLED A NWAA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 8945E 47181 654682 DURING TAKEOFF ROLL AT 110 KNOTS, ENGINE NR 2 EXPERIENCED 2 COMPRESSOR STALLS. FLIGHT CREW ABORTED TAKEOFF AND RETURNED TO GATE. FLIGHT CREW REPORTED SNOW CONTAMINATED RUNWAYS. MAINTENANCE PERFORMED POST STALL INSPECTIONS AND GROUND RUN ON ENGINE NR 2. 2 L 7 2 4F 4 F A6WE E2EA 2008040200385 20080402 00385 NM 2008 4 2 08FDEA01204 1 20080329 A 5320 6519606109 INTERCOSTAL BOEING 727 727227 1384078 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 MAIN DECK FLOORBEAM U CHANNEL INTERCOSTAL IS CORRODED, BS 1133, RBL 62, WL 208. REMOVED CORROSION AND FOUND CHANNEL TO BE OUT OF LIMITS. RECEIVED NEW CHANNEL/SUPPORT AND DRILLED HOLES, REFERENCE BOEING DOCUMENT NR 65-19606/ITEM -109, CLAS SIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008040300023 20080403 00023 NM 2008 4 3 ABXA080098 1 20080222 A 5320 141T3211 STRUCTURE BOEING 767 767281 1385109 NM FUSELAGE MISREPAIRED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 769AX 22787 ENGINEERING REQUESTED REMOVE EXISTING DOUBLER LOCATED AT STA 220.5, STRINGER 24 LEFT. REPAIR DID NOT MEET SRM REQUIREME NTS. REMOVED AND REPLACED DOUBLER IAW REA B653-57078-MR. 2 L 7 2 4F RT A1NM 2008040300031 20080403 00031 NM 2008 4 3 ABXA080099 1 20080225 A 5322 140T21021 SHEAR TIE BOEING 767 767281 1385109 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 769AX 22787 SHEAR TIE CORRODED AT FS 748, BETWEEN STRINGER 37 - STRINGER 38, RIGHT AFT SIDE OF FRAME. REMOVED SHEAR TIE. FABRICATE D AND INSTALLED SHEAR TIE IAW SRM 51-40-2. 2 L 7 2 4F RT A1NM 2008040300080 20080403 00080 NM 2008 4 3 200800309 1 20080317 A 5350 SKIN BOEING 747 747SPB5 1384813 NM FAIRING SCRATCHED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 708BA 22484 RT UPPER AFT WING TO BODY FAIRING, FROM STA 1480 TO STA 1860 FROM STR 23R TO STR 34R HAS SCRIBE MARKS. APPROX STA 1560 STR 39R .003 DEPTH. BLENDED OUT SCRIBE LINES, MATERIAL LOSS IS .003 WITHIN LIMITS ALODINED AND PRIMED AREA PER B747 SP SRM'S 53-31-00 PG 1-4 51-10-02 PG 6-6B AND BSOPM 20-44-04 PG 1-4. 2 L 7 4 4F RT A20WE 2008040300108 20080403 00108 NM 2008 4 3 ASAA0872794 1 20080313 A 5755 113A46001 SKIN BOEING 737 737790 13844CN NM NR 6 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 607AS 29751 NR 6 SPOILER LWR SURFACE DENT AT 46.75 INCH FROM IB EDGE AND 12.25" FROM T/E. REPAIR DENT IAW B737 700 SRM. 2 L 7 2 4F RT A16WE 2008040300159 20080403 00159 SO 2008 4 3 SWIA200819411 1 20080325 A 2150 22045404 ACM EMB 120 EMB120ER 3260203 SO LEFT MALFUNCTIONED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 07 301YV 6737 6737 120301 LEFT PACK PRODUCES SMOKE. REPLACED LEFT AIR CYCLE MACHINE IAW MM 21-50-05. 2 L 7 2 4T RT A31SO 2008040300199 20080403 00199 EU 2008 4 3 08FDEA01217 1 20080331 A 5755 A57246948201 RETAINER AIRBUS 310 A310203 3930313 EU NR 4 SPOILER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT WING NR 4 SPOILER OUTBD END HINGE RIB SEAL RETAINED IS CRACKED AND THE SEALS TORN. REMOVED CHANNEL IAW A310-200 S RM 51-40-21. MATERIAL ID IS 2024-0, 0.050; PO 583365.1 IAW A310-200 BRITISH AEROSPACE DWG A-572-46948; SRM 51-31-00; TA BLE 3 AND SRM 57-51-11; FIG 7. FABRICATED CHANNEL IAW A310-200 BRITISH AEROSPACE DWG A 572-46948. HEAT TREATED 2024-0 TO 2024-T42 IAW TP 51003; REV A; HRD 57/58 LOAD NR HTO 31908-6. ALODINED; PRIMER AND PAINTED IAW A310-200 SRM 51-23-10 . ASSEMBLED SEAL AND RETAINER TO CHANNEL IAW A310-200 BRITISH AEROSPACE DWG A 572-46948. INSTALLED CHANNEL IAW A310-20 0 SRM 51-40-21; PARA 6 AND 57-51-11; PG 56. 2 L 7 2 4F RT A35EU 2008040300204 20080403 00204 EU 2008 4 3 08FDEA01222 1 20080401 A 5313 STRINGER AIRBUS 310 A310222 3930315 EU FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 448FE 260 PREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 54 RT BETWEEN FRAMES 65 TO 67 HAS 1 REPAIR SECTION MEASURIN G 40" LONG AND 1 REPAIR SPLICE MEASURING 8 INCHES LONG. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND I NSTALLED 1 CORRECT REPAIR SPLICE IAW A310-200 SRM 53-10-14 FIG 201. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMB ER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008040300216 20080403 00216 WP 2008 4 3 08FDEA01234 1 20080401 A 5311 70750080C FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 MCD-FUSELAGE UPPER LOBE-FRAME AT FS 635, 655, 675, 695, 715, 735, 755 AND 775, LONGERON 13R HAS CHAFED DAMAGED FROM LI NER MOUNT FASTENER. EVALUATED FRAME BLENDED ROUGH EDGES DRILLED HOLE REMOVING ALL DAMAGE FILLED HOLE WITH RIVET IAW SRM 530001 FIG 1A. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ATTENTION RECORDS, THIS IS A CLASS "B" REPAIR AND HAS AN INITI AL REINSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES. 2 L 7 3 4F RT A22WE 2008040300226 20080403 00226 NM 2008 4 3 2008UALA01765 1 20080328 A 5320 SUPPORT BRACKET BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 FWD GALLEY FWD UPPER MECHANISM BOX MOUNT SUPPORT BRACKET CRACKED IN RADIUS. MAJOR REPAIR ACCOMPLISHED, REMOVED CRACKED BRACKET AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040400015 20080404 00015 CE 2008 4 4 N568CS032008 1 20080319 A 3297 661812812 CIRCUIT BREAKER CESSNA 560 560XL 2076702 CE FLIGHT DECK DEFECTIVE E Z5FA O OTHER O OTHER AP APPROACH 1 EA 63 568CS 1658 5605637 AFTER LOWERING LANDING GEAR, DID NOT GET 3 GREEN DOWN AND LOCKED LIGHTS. FOLLOWED AFM PROCEDURES AND LANDING GEAR INDIC ATION NORMAL: (3 GREEN LIGHTS). COMPLETED NORMAL LANDING. REMOVED AND REPLACED LANDING GEAR WARNING CIRCUIT BREAKER. L ANDING GEAR OPERATIONALLY CHECKED OK, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A22CE 2008040400040 20080404 00040 NM 2008 4 4 2008UALA01785 1 20080329 A 3350 363624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 44C LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 EEL STRIP RIPPED OFF SEAT 44C. REPLACED LIGHT ASSEMBLY OPS CHECKED OK. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040400082 20080404 00082 NM 2008 4 4 2008UALA01833 1 20080401 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 4A AFT LIGHT ASSY. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040400095 20080404 00095 NM 2008 4 4 2008UALA01846 1 20080331 A 3350 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 777UA 26916 AFT EMERGENCY LIGHT OUT AT SEAT 8D. REPLACED LAMP. OP CHK'D OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040400123 20080404 00123 EU 2008 4 4 08FDEA01258 1 20080317 A 5753 A5797020022600 FLAP TRACK AIRBUS 310 A310203 3930313 EU TE FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT FLAP VANE TRACK NR 1 IS WORN. RECEIVED NEW TRACK FOR INSTALLATION; SEE FEDEX JOB CARD 46S5181CP. OLD TRACK IS O UT OF LIMITS. MAX LIMIT 0.0315; MEASURED 0.065. 2 L 7 2 4F RT A35EU 2008040400129 20080404 00129 EU 2008 4 4 08FDEA01264 1 20080317 A 5753 A5797020021200 FLAP TRACK AIRBUS 310 A310203 3930313 EU TE FLAPS WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT FLAP VANE NR 2 TRACK HAS WORN AREAS MARKED REPAIRED NR 2 FLAP VANE TRACK IAW AIRBUS CMM 57-52-15. 2 L 7 2 4F RT A35EU 2008040400136 20080404 00136 NM 2008 4 4 08FDEA01271 1 20080402 A 5330 6554580 SKIN BOEING 727 727225 1384077 NM BS 980-990 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 AFT LOWER CARGO DOOR LOWER AFT FUSELAGE EDGE BENT AND CRACKED AT STA 980-990. REPAIRED BY TRIMMING THE AFFECTED PER EA 7-5330-116976. 2 L 7 3 4F A3WE 2008040400139 20080404 00139 NM 2008 4 4 DL76G080440 1 20080327 A 5315 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 155DL 25269 FLOORBEAM CORRODED BOTTOM SIDE AT STA 1197+132 LBL40. REPAIRED ON NR AVM523900 PER 53-00-07 FIGURE 201 REPAIR 4. 2 L 7 2 4F RT A1NM 2008040400155 20080404 00155 NM 2008 4 4 DLM90080459 1 20080306 A 5313 LONGERON DOUG MD90 MD9030 3023690 NM 29R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 97069 53392 FOUND LONGERON R29 CORRODED AT Y-1344.0. BLENDED CORROSION ON LONG R29, OUT OF LIMITS. REMOVED DAMAGED SECTION, INSTAL LED NEW SECTION AND SPLICES IAW MD90 SRM 53-00-01, 51-30-02, 51-30-03 AND 53-10-01 (STA 1338 TO 1374). 2 L 7 2 4F RT A6WE 2008040400156 20080404 00156 NM 2008 4 4 DLM90080460 1 20080326 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 984-4003 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 LT CABIN CUSP WEB FS 984-1003 CORRODED. REPAIRED CUSP WEB, IAW MD90 SRM 51-11-01 FIG 2. 2 L 7 2 4F RT A6WE 2008040400157 20080404 00157 NM 2008 4 4 DLM90080461 1 20080306 A 5330 SKIN DOUG MD90 MD9030 3023690 NM BS 218 S18L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 C/W SRM 53-30-01 REPAIR FUSELAGE SKIN DENT STA 218 BELOW STR L-18. REPAIR FUSELAGE SKIN STA 218 BELOW STR L-18, IAW MD8 0 SRM 53-04D FIG 12B. 2 L 7 2 4F RT A6WE 2008040400159 20080404 00159 NM 2008 4 4 DLM90080463 1 20080306 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 410-588 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 97463 53392 CABIN SEAT TRACK LBL 54.5 IS OUT OF LIMITS AT FUSELAGE STA 410-588, LBL 54.5 IAW MD90 53-40-01, FIG 6. REMOVED AND REPL ACED SEAT TRACK STA 410 TO 588, LBL 54.5 IAW MD90 53-40-01, FIG 6. 2 L 7 2 4F RT A6WE 2008040400162 20080404 00162 NM 2008 4 4 DLM90080466 1 20080326 A 5753 993594021 SKIN DOUG MD90 MD9030 3023690 NM TE FLAP DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 C/W ER/A 096112-14 REPAIR LEFT WING INBOARD MAIN FLAP LOWER SKIN X1F1=41.5 DENT. REPAIRED LEFT WING INBOARD MAIN FLAP L OWER SKIN, IAW ER/A 096112-14 REV B 01-28-06 AND MD90 SRM 57-03D FIG 807D PERMANENT REPAIR. NO FURTHER ACTION REQUIRED. 2 L 7 2 4F RT A6WE 2008040400165 20080404 00165 NM 2008 4 4 DLM88080472 1 20080402 A 5340 FITTING DOUG MD88 MD88 3023688 NM DOOR FRAME CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV CORROSION WAS FOUND ON FWD DOOR JAMB LOWER CORNER FITTING AT C3. FITTING WAS REPLACED IAW SRM 51-30-5. 2 L 7 2 4F RT A6WE 2008040400170 20080404 00170 NM 2008 4 4 DLM88080477 1 20080402 A 5320 FLOOR SUPPORT DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV EXFOLIATION CORROSION WAS FOUND ON FLOOR PANEL SUPPORT STA Y=180 TO 200 X=-44 FWD WET AREA. FLOOR SUPPORT WA S REPLACED IAW DOUGLAS DWG 9936534. 2 L 7 2 4F RT A6WE 2008040400178 20080404 00178 NM 2008 4 4 DLM88080485 1 20080402 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV CORROSION WAS FOUND ON RIGHT CUSP WEB BETWEEN STA Y=1155 AND 1174. CUSP WEB WAS REPAIRED IAW SRM 51-70-4 FIG 2. 2 L 7 2 4F RT A6WE 2008040400185 20080404 00185 NM 2008 4 4 DLM88080492 1 20080402 A 5712 RIB DOUG MD88 MD88 3023688 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV A CRACKED RIB WAS FOUND AT LEFT WING FIXED LEADING EDGE STA XIS=136 LOWER SIDE. RIB WAS REPAIRED IAW ER/A 46 6349-14 REV ORIG. 2 L 7 2 4F RT A6WE 2008040400188 20080404 00188 NM 2008 4 4 DLM88080495 1 20080402 A 5320 SUPPORT DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV A CRACK WAS FOUND ON PILOT REGULATOR VALVE SUPPORT AT STA Y=1358 LONG 13 LT. SUPPORT WAS REPLACED IAW SRM 51 -30-1. 2 L 7 2 4F RT A6WE 2008040400191 20080404 00191 NM 2008 4 4 DLM88080498 1 20080402 A 5320 FLOOR SUPPORT DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV A CRACKED WAS FOUND ON SUPPORT FOR CABIN FLOOR PANEL 389A. SUPPORT WAS REPLACED IAW DOUGLAS DWG 9952521-5. 2 L 7 2 4F RT A6WE 2008040400196 20080404 00196 NM 2008 4 4 DLM88080503 1 20080402 A 5320 SUPPORT DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, A CORRODED AND DEFORMED SLANT PANEL SUPPORT WAS FOUND AT STA Y=1250 BETWEEN LONG 27 LT AND 25 RT. SUPPORT W AS REPLACED IAW ER/A 413029-14MA. 2 L 7 2 4F RT A6WE 2008040700002 20080407 00002 NM 2008 4 7 AALA200800603 1 20080312 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AA 24617 DFW - EMERGENCY LIGHT AT AFT SEAT 14D HAS A BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT AFT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040700005 20080407 00005 NM 2008 4 7 AALA200800602 1 20080312 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AA 24617 DFW - EMERGENCY LIGHT AT AFT SEAT 6E HAS A BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT AFT SEAT 6E. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040700008 20080407 00008 NM 2008 4 7 AALA200800605 1 20080312 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 659AA 24617 DFW - EMERGENCY LIGHTS AT FORWARD CABIN SEATS AND EXIT IDENTIFIERS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIG HTS AT FORWARD CABIN SEATS AND EXIT IDENTIFIERS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040700010 20080407 00010 NM 2008 4 7 AALA200800614 1 20080312 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 379AA 25448 DFW - EMERGENCY LIGHT AT LEFT SIDE AFT OF WING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT SIDE AFT OF WING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008040700011 20080407 00011 NM 2008 4 7 AALA200800615 1 20080312 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AA 25201 SFO - EMERGENCY LIGHT AT SEAT 29B BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LEFT SEAT 29B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008040700019 20080407 00019 NM 2008 4 7 AALA200800612 1 20080312 A 3350 CM767 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 346AN 33085 LGA - EMERGENCY LIGHT AT OVERHEAD SEATS 37HJ INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEATS 37HJ. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008040700022 20080407 00022 SO 2008 4 7 SIMA200809302 1 20080331 A 3350 20131A BATTERY EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 702AE 145164 ON FLIGHT 4620, CREW REPORTED OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE, OVERHEAD EMERGENCY EXIT SIGN AT ROW-9 INOPERAT IVE AND LAST TWO ROWS (9-13) EMERGENCY EXIT LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BA TTERY POWER SUPPLY NR 4 IAW EMB AMM 33-50-04. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008040700027 20080407 00027 NM 2008 4 7 DLM88080505 1 20080402 A 5320 FLOOR SUPPORT DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV A CRACKED FLOOR SUPPORT WAS FOUND AT STA Y=1271 BETWEEN LONG 30 AND 25 RT. SUPPORT WAS REPLACED IAW ER/A 413 029-14MA. 2 L 7 2 4F RT A6WE 2008040700032 20080407 00032 NM 2008 4 7 DLM88080510 1 20080402 A 5320 ANGLE DOUG MD88 MD88 3023688 NM BS 1463 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, TWO CRACKED ANGLES WAS FOUND ON STA Y=1463 AT 11:00 POSITION AT AFT ACCESSORY COMPARTMENT. ANGLES WERE REPL ACED IAW DOUGLAS DWG 9977839. 2 L 7 2 4F RT A6WE 2008040700037 20080407 00037 NM 2008 4 7 DLM88080515 1 20080401 A 5330 59364335 DOOR FRAME DOUG MD88 MD88 3023688 NM BS 1209 S29R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV AT GDL, CORROSION WAS FOUND IN THE AFT CARGO COMPARTMENT INTERNAL DOOR JAMB DOUBLER AT STA 1209 BETWEEN S-29R AND S-30R. THE DAMAGE WAS REPAIRED PER BOEING INSTRUCTIONS. 2 L 7 2 4F RT A6WE 2008040700039 20080407 00039 NM 2008 4 7 DL76G080517 1 20080402 A 3610 80217010 SHUTOFF VALVE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 1605 30198 704233 RT HPSOV CAUTION LIGHT ILLUMINATED AT CRZ APPROX 2 HRS INTO FLT. DEACTIVATED RT ENG HPSOV IN CLOSED POSITION PER MEL 36 -11-02 AND ALSO DEACTIVATED RT ENG THRUST REVERSER PER MEL 78-31-01, FWD TO MCO AND PLAC PER MEL 36-11-02. 2 L 7 2 4F 4 F RT A1NM E13NE 2008040700041 20080407 00041 NE 2008 4 7 DL76L080519 2 20080402 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 MALFUNCTIONED A DALA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 178DN 16964 900 25143 724716 REPLACED NR 1 ENGINE DUE TO HIGH EGT INSTALLED 727650. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040700044 20080407 00044 NM 2008 4 7 DLM88080522 1 20080403 A 5523 TAB DOUG MD88 MD88 3023688 NM LT ELEVATOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, LIGHTNING STRIKE WAS FOUND ON TRAILING EDGE ON LEFT ELEVATOR CONTROL TAB. TAB WAS REPAIRED IAW SRM 55-04D P ARAGRAPH 3 FIG 2. WEIGHT AND BALANCE IAW SRM 55-20-2D. 2 L 7 2 4F RT A6WE 2008040700045 20080407 00045 NM 2008 4 7 DLM88080523 1 20080403 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV A CRACK WAS FOUND ON FUSELAGE SKIN AT STA Y=499 BETWEEN LONGERON 3 AND 4 LT. CRACK WAS REPAIRED IAW SRM 53-0 4D FIG38 AND 51-30-2 PAR 13. 2 L 7 2 4F RT A6WE 2008040200391 20080402 00391 WP 2008 4 2 08FDEA01211 1 20080331 A 7110 NLT6012507 SKIN DOUG MD10 MD1010F 3022112 WP NR 2 COWLING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 NR 2 ENGINE LEFT FAN COWL INNER SKIN CHAFED. REMOVED DAMAGED AREA, FABRICATED REPAIR DETAILS, PREPPED DETAILS & REPAIR AREA, LAYED UP REPAIR, VACUUM BAGGED REPAIR, CURED REPAIR, PERFORMED POST CURE INSPECTION, INSTALLED RIVETS & SEALED IAW SRM 54-00-01 VOL I. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. 2 L 7 3 4F RT A22WE 2008040200392 20080402 00392 WP 2008 4 2 08FDEA01212 1 20080331 A 5350 ARC702532 FRAME DOUG MD10 MD1010F 3022112 WP TAILCONE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 TAIL CONE RIGHT UPPER PATIO DOOR HINGE FRAME IS GOUGED, MATERIAL ID 2024-T3; PO 600955.2 PER DC/MD-10 SRM 53-52-01; VOL III. ALODINED AND PRIMED PER DC/MD-10 SRM 51-21-01; VOL II. INSTALLED DOUBLER PER DC/MD-10 SRM 53-00-01; VOL I. 2 L 7 3 4F RT A22WE 2008040300001 20080403 00001 NM 2008 4 3 ZZDA2008082 1 20080320 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DEFECTIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 717JL 55042 EMERGENCY LIGHTS ON SEATS 1 - 10 INOPERATIVE. OVERHEAD LIGHTS IN AREA OKAY. FOUND LAMPS AT SEAT 30 DAMAGED. SUSPECT D AMAGED LAMPS CAUSED ON OUTPUT AT B5-118 BATTERY PACK TO BLOW FUSE. REMOVED AND REPLACED BATTERY SUPPLY ASSY IAW EM CMM 33-50-02. OPS CHECK OK. 2 L 7 2 4F TR A6WE 2008040300007 20080403 00007 WP 2008 4 3 ABXR080107 1 20080303 A 5320 49568771 ATTACH ANGLE DOUG DC9 DC932F 3022067 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 205US 47690 ATTACH ANGLE FOR STA 41 TO STA 69 PRESSURE PANEL INTERCOSTAL CRACKED. SECOND INTERCOSTAL TO THE LEFT OF THE PLUG DOOR. REMOVED AND REPLACED IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2008040300008 20080403 00008 WP 2008 4 3 ABXR080104 1 20080229 A 5312 5931960513 ATTACH ANGLE DOUG DC9 DC932F 3022067 WP RT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 205US 47690 INBOARD BULKHEAD STA 718 ATTACH ANGLE CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 2008040300009 20080403 00009 WP 2008 4 3 ABXR080102 1 20080228 A 5230 5910143 SKIN DOUG DC9 DC932F 3022067 WP AFT CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 205US 47690 FORWARD LOWER CARGO DOOR SKIN CRACKED AT DOOR HANDLE. REPAIRED AND PAINTED IAW DC9 SRM 25-05 AND 51-10. 2 L 7 2 4F A6WE 2008040300013 20080403 00013 NM 2008 4 3 ABXA080114 1 20080310 A 5312 145T875281 PRESSURE PANEL BOEING 767 767281 1385109 NM LT MLG CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 775AX 22790 LEFT CANTED PRESSURE DECK IN LEFT WHEEL WELL HAD APPROXIMATELY 4 INCH CRACK. REPAIRED CANTED PRESSURE DECK IN LEFT WHEE L WELL IAW B767 SRM 53-50-51. 2 L 7 2 4F RT A1NM 2008040300018 20080403 00018 SW 2008 4 3 2008F00005 1 20080215 A 5310 531116392005 WINDOW FRAME ECLIPS EA500 ECLIPSEEA500 3350000 SW FUSELAGE DAMAGED B K NONE O OTHER IN INSP/MAINT 1 SO 16 152DJ 90 90 000062 DAMAGED IN MAINT DURING WINDSHIELD REPLACEMENT. 1 L 7 2 4J RT A00002AC 2008040300020 20080403 00020 NM 2008 4 3 ABXA080096 1 20080221 A 5320 96FS6677068 FITTING BOEING 767 767281 1385109 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 769AX 22787 LEVEL I CORROSION ON FITTING AT FS 368, LEFT BUTT LINE 28. REPAIRED IAW REA B653-57097-MR. 2 L 7 2 4F RT A1NM 2008040300027 20080403 00027 SO 2008 4 3 2008F00007 1 20080213 A 3245 650X10 TUBE PIPER PA31 PA31350 7103110 SO TIRE MISMANUFACTURED E K NONE O OTHER TX TAXI/GRND HDL 1 AL 05 1 AFTER LANDING AND TAXI, IT WAS DISCOVERED THAT THE LT MAIN TIRE WAS FLAT. ON FURTHER INSP OF THE TUBE, IT WAS DISCOVERED THAT THE SIDEWALL CONTAINED (2) PIN HOLES LOCATED WITHIN A FLAP OF RUBBER APPROXIMATELY 0.5 INCHES LONG. THIS IS THE L ATEST OF TUBE FAILURES OF MFG INNERTUBES. ALL OF WHICH CONTAIN SMALL PINHOLES OR CRACKS IN EITHER THE SIDEWALL OR OUTER CIRCUMFERENCE OF THE TUBE. SO FAR WE HAVE EXPERIENCED AT LEAST 18 FAILURES OF EITHER NOSE OR MAIN TUBES IN THE LAST 4 MO NTHS WITH THIS PROBLEM. AFTER CONSULTATION WITH MFG, AND AT THEIR SUGGESTION, WE HAVE REPLACED ALL INNERTUBES WITH INNER TUBES DESIGNATED AS "MADE IN USA". WE HAVE HAD NO FAILURES OF THE "MADE IN USA" TUBES AS OF THIS DATE. CONVERSATIONS WI 1 L 7 2 3O A20SO 2008040300029 20080403 00029 NM 2008 4 3 ABXA080097 1 20080222 A 5320 96FS6677068 PANEL BOEING 767 767281 1385109 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 769AX 22787 PANEL 221F LEFT BUTT LINE 51 TO LEFT BUTT LINE 86 HAD LEVEL I CORROSION AT CLIP NUTS. REPAIRED IAW REA B653-57098-MR. 2 L 7 2 4F RT A1NM 2008040300030 20080403 00030 NM 2008 4 3 ABXA080092 1 20080218 A 2710 148T31212 BEARING BOEING 767 767281 1385109 NM LT AILERON WORN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 769AX 22787 THE LEFT INBOARD AILERON OUTBOARD PCA SUMMING LINKAGE HAD A WORN BEARING. REPLACED LEFT INBOARD AILERON OUTBOARD PCA IA W B767 AMM 27-11-48-2. 2 L 7 2 4F RT A1NM 2008040300037 20080403 00037 NM 2008 4 3 ABXA080095 1 20080221 A 5315 96FS6677068 FLOORBEAM BOEING 767 767281 1385109 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 769AX 22787 CORROSION ON FLOORBEAM AT FS 368, RIGHT BUTT LINE 25. REPAIRED 9G NET STRAP FITTING IAW REA B653-57096-MR. 2 L 7 2 4F RT A1NM 2008040300047 20080403 00047 NM 2008 4 3 KCSA081214 1 20080328 A 5311 FRAME BOEING 747 747SR46 1384816 NM FUSELAGE BENT A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 FRAME BENT BETWEEN STA-2200 AND STA-2220 LBL-28. 2 L 7 4 4F RT A20WE 2008040300053 20080403 00053 NM 2008 4 3 KCSA081216 1 20080328 A 5320 CAP BOEING 747 747SR46 1384816 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 FWD CARGO STA-920 LBL-12 UPPER CAP DENTED. 2 L 7 4 4F RT A20WE 2008040700050 20080407 00050 NM 2008 4 7 DLM88080528 1 20080403 A 5320 INTERCOSTAL DOUG MD88 MD88 3023688 NM BS 1380 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, CORROSION WAS FOUND ON INTERCOSTAL AT STA Y=1380 LONGERON 28 RT. INTERCOSTAL WAS REPAIRED IAW SRM 51-70-05 FIG 1. 2 L 7 2 4F RT A6WE 2008040700052 20080407 00052 EA 2008 4 7 A6WA200840127 1 20080226 A 5414 PANEL CNDAIR CL600 CL6002B19 1900309 EA RT NACELLE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 RIGHT PYLON PANEL 422DB, SEPARATORS ABRADED. RIGHT PYLON PANEL 422DB, SEPARATORS REPLACED IAW CRJ200 SRM 51-42-06. (M ) 2 L 7 2 4F RT A21EA 2008040700060 20080407 00060 NE 2008 4 7 HALA0800476 2 20080331 A 7230 BLADE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE LT ENGINE FAN DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICNAT SYSTEM, LT ENG FAN BLADE HAS NICK NR 36. REPAIRED PER AMM TASK 72-31-02. EDDY CURRENT GOOD. NO CRAC KS IND NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040800002 20080408 00002 SO 2008 4 8 N93A29032008 1 20080329 A 3297 CONNECTOR GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU DOWNLOCK SWITCH LOOSE E N93A O OTHER N FALSE WARNING AP APPROACH 1 SO 13 487QS 1287 AFTER GEAR WAS EXTENDED FOR LANDING, RT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED. FOUND RT MLG DOWNLOCK SWITCH CONNEC TOR NOT FULLY SEATED. RESEATED CONNECTOR, OPS CHECKS WERE ACCOMPLISHED SUCESSFULLY. 2 L 7 2 4F 4 F RT A12EA E25NE 2008040800004 20080408 00004 GL 2008 4 8 SIMA200809303 2 20080330 A 7261 230735623072 CARBON SEAL EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL LT ENGINE LEAKING A SIMA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 815AE 145545 ON FLIGHT 3861, CREW REPORTED STRONG OIL BURNING SMELL IN CABIN DURING TAKEOFF WITH APU ON. ALSO GOT STRONGER OIL BURNI NG SMELL ON DESCENT WITH APU OFF. AIRCRAFT REMOVED FROM SERVICE. C/A-REMOVED AND REPLACED LEFT ENGINE ZERO CARBON SEAL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008040800009 20080408 00009 NM 2008 4 8 RYNA200800001 1 20080314 A 3270 CARTRIDGE BOEING 737 73786N 13844CD NM CFMINT CFM56 CFM567B26US NE TAILSKID DAMAGED A RYNA O OTHER O OTHER TO TAKEOFF 1 CE 07 DJT 28592 DURING TAKEOFF AT MKE AIRPORT TAIL SKID OF THE AIRCRAFT SCRATCHED THE RUNWAY AND THE IMPACT DAMAGED TAIL SKID CARTRIDGE ASSEMBLY. ACCOMPLISHED FUSELAGE, TAIL SECTION AND OVER WEIGHT INSPECTION PER AMM 05-51-35, AND FOUND NO ADDITIONAL DEFE CT. REPLACED TAIL SKID CARTRIDGE ASSEMBLY PER AMM 32-71-00 AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008040800012 20080408 00012 SO 2008 4 8 FDKA200803115 1 20080318 A 5610 SEAL EMB 145 EMB145LR 3260212 SO WINDSHIELD DEFECTIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 849MJ 145534 FDM RON CLT (1759 PHX LCL). LOUD SQUEAL FROM CAPTAIN'S SIDE WINDOW ON CLIMBOUT. MX RESEALED CAPT'S WINDSHIELD AND RETO RQUED SCREWS. 2 L 7 2 4T RT T00011AT 2008040300101 20080403 00101 EA 2008 4 3 COMA0860182 1 20080319 A 3020 SR1030200001 PRESSURE VALVE CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYSTEM FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 01 455CA 7592 FLIGHT 5681- RIGHT COWL ANTI-ICE CAUTION MESSAGE RECEIVED. RETURNED TO CVG, LANDED WITHOUT INCIDENT. REPLACED RIGHT EN GINE PRESSURE VALVE. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008040300120 20080403 00120 NM 2008 4 3 NACA20080003 1 20080317 A 5330 SKIN BOEING 737 737232 1384475 NM FUSLEAGE CRACKED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 321DL 23093 FUSELAGE SKIN CRACKED AT STRINGER 21R, BS 931-BS 934.0625. CRACK IS 3.0625" LONG. REPAIRED PER BOEING REPAIR SKETCH AN D SERVICE REQUEST MESSAGE 1-79197357-1 THRU -21, FAA FORM 8100-9, DATED 21 MARCH 2008. 8100-9 STATES ALTERNATE REPAIR H AS BEEN APPROVED AS AN ALTERNATIVE METHOD OF COMPLIANCE (AMOC) TO PARAGRAPH (D) OF AD 2004-18-06. 2 L 7 2 4F RT A16WE 2008040300124 20080403 00124 NM 2008 4 3 2008UALA01739 1 20080327 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 390-405 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 FUSELAGE LOWER SKIN AT E/E BAY COOLING DUCT OUTLET CUTOUT AT BS 390-405 STR 28R-28L HAS DAMAGE. MAJOR REPAIR ACCOMPLISH ED: RMV'D EXISTING DOUBLER. INSTALLED REPAIR DOUBLER & PREVENTIVE MODIFICATION DOUBLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040300144 20080403 00144 NM 2008 4 3 HALA0800441 1 20080329 A 2613 3500833 CIRCUIT CARD BOEING 767 76733A 1385209 NM OVERHEAT DETECT FAULTY A HALA K NONE N FALSE WARNING CR CRUISE 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, RT DUCT LEAK LT ON AND EICAS R BLD DUCT LEAK. PERFORMED FIM 26-18-00, NO DEFECT NOTED. REMOV ED AND REPLACED WHEEL WELL OVERHEAT DUCT LEAK DETECTION CARD PER AMM 26-10-01. 2 L 7 2 4F RT A1NM 2008040300146 20080403 00146 NE 2008 4 3 HALA0800443 2 20080330 A 7230 BLADE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE RT ENGINE DAMAGED A HALA K NONE O OTHER AP APPROACH 1 WP 13 583HA 25531 OPEN - BIRD STRIKE INSPECTION OF RT ENG REVEALED A CORNER PIECE MISSING FROM ENG STATOR VANE PLATFORM BASE AT 3 O'CLOCK POSITION. OK TO OPERATE IAW AMM 72-33-02-206--00-N00 TABLE 603. TRANSCRIBED TO MIC SHEET, NO OTHER DAMAGE NOTED AS PER FIM 71 FAULT INDES, INSPECTION OF RIGHT ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040300160 20080403 00160 SO 2008 4 3 SWIA200819412 1 20080212 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 584SW 120352 LEFT WING AREA NEAR THE NR 2 FUEL PANEL HAS A LEAKING RIVET, FOUND AT C-CHECK. REPAIRED STRINGER 10 IAW EMB 120 SRM 57- 20-03. 2 L 7 2 4T RT A31SO 2008040300161 20080403 00161 SO 2008 4 3 SWIA200819413 1 20080212 A 2752 BEARING EMB 120 EMB120ER 3260203 SO FLAP ACTUATOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 584SW 120352 FOUND AT C-CHECK, RIGHT OUTBOARD FLAP ACTUATOR ROD END BEARING AND BOLT IS CORRODED. REPLACED ACTUATOR ROD END AND BOLT IAW CMM 25-50-23. 2 L 7 2 4T RT A31SO 2008040300180 20080403 00180 NM 2008 4 3 HALA0800458 1 20080327 A 7110 COWLING BOEING 767 767332 1382001 NM NR 1 ENGINE DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 NR 1 ENG I/B CORE COWL HAS VARIOUS DEFECTS ALONG THE BOTTOM STRUCTURE. BLENDED THE DAMAGED AREA IAW SRM 54-41-02, FIG 1 01. 2 L 7 2 4F RT A1NM 2008040300183 20080403 00183 NM 2008 4 3 HALA0800461 1 20080327 A 5730 SKIN BOEING 767 767332 1382001 NM RT WING CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 LEVEL 1 CORROSION ON RIGHT WING LOWER SURFACE AT STRINGER L-15, WS 522-552. REWORKED IAW SRM 51-10-02. 2 L 7 2 4F RT A1NM 2008040300190 20080403 00190 NM 2008 4 3 HALA0800468 1 20080327 A 5511 RIB BOEING 767 767332 1382001 NM HORIZ STAB CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 CRACK LOWER CHORD OF HORIZIONAL STABILIZER CENTER SECTION RIB, JUST FORWARD OF STRINGER 2 AT RBL 13.83. TRIMMED DAMAGED MATERIAL, INSTALLED FILLER AND REPAIRED ANGLE SECTION, RE-PROTECTED AND REFINISHED PER SRM BOEING APPROVAL SR 1-7936539 37. 2 L 7 2 4F RT A1NM 2008040300194 20080403 00194 EU 2008 4 3 08FDEA01206 1 20080330 A 2760 NAS16128 O-RING AIRBUS 310 A310222 3930315 EU SPOILER VALVE LEAKING A FDEA B EMER. DESCENT K FLUID LOSS CR CRUISE 1 SO 25 453FE 267 DURING CRUISE GREEN SYSTEM LOW QUANTITY ALERT. LOSS OF GREEN HYD KRUEGER FLAP ALERT DURING APPROACH. CREW DECLARED FOR EMERGENCY LANDING. ACCORDING TO CREW THE A/C LANDED SMOOTHLY AT WSSS 02L AND NO OVERWEIGHT. THE GREEN HYD FLUID QTY INDICATION AT LOWER SIDE OF "TOP CAP". FOUND HYD LEAK FROM NR 5 RT SPOILER VALVE GROUP REPLACED 'O' RING PER MM 27-64-1 3-4. SERVICED GREEN HYD SYSTEM RESERVOIR PER MM 12-12-29-0 TO NML QTY. PRESSURIZED HYD AND LEAK CHK OK. RUN BOTH ENG PER A310 JRH AND CYCLE ALL FLIGHT CONTROLS, FLAPS AND SLATS FOUND ALL INDICATIONS NML. 2 L 7 2 4F RT A35EU 2008040300205 20080403 00205 EU 2008 4 3 08FDEA01223 1 20080401 A 5313 STRINGER AIRBUS 310 A310222 3930315 EU FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 448FE 260 PREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 55 RT BETWEEN FRAMES 65 TO 69 HAS 1 REPAIR SECTION MEASURIN G 80" LONG AND 1 REPAIR SPLICE MEASURING 8.2 INCHES LONG, REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT STRINGER REPAIR SPLICE IAW A310-200 SRM 53-10-14 FIG 201. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED P ART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008040300214 20080403 00214 EU 2008 4 3 08FDEA01232 1 20080401 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 448FE 260 PREVIOUS REPAIR LOCATED ON MAIN CABIN SEAT TRACK NR 4 RT - Y1456 BETWEEN FRAMES 62 TO 63, HAS 2. REPAIR ANGLES MEASURIN G 9.5" LONG BY 1.9" TALL AND 1. REPAIR PIECE 4 INCHES LONG. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED REPAIR AND INSTA LLED CORRECT SEAT TRACK REPAIR IAW A310-200 SRM 53-10-16 FIG 201. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008040300220 20080403 00220 NM 2008 4 3 2008UALA01748 1 20080328 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 CEILING EMERGENCY LITE INBRD OF LAV 101 INOP. RELAMPED CEILING EMG LIGHT. OPS CK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040400046 20080404 00046 NM 2008 4 4 2008UALA01792 1 20080329 A 5551 LUG BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 LT HORIZONTAL OUTBOARD STABILIZER REAR SPAR UPPER LUG FWD BUSHING HAS FRETTING CORROSION. MAJOR REPAIR: REMOVED CORROSI ON AND ACCOMPLISHED REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040400064 20080404 00064 NM 2008 4 4 2008UALA01813 1 20080329 A 3210 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OXYGEN BOX LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 CHECK FOR O2 LEAK LOST 100 PSI DURING 4 HOUR FLIGHT. FOUND LEAKING SEAL WITHIN CAPT O2 BOX. REMOVED AND REPLACED CAPT O 2 BOX, NO LEAKS NOTED AFTER. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040400069 20080404 00069 NM 2008 4 4 2008UALA01819 1 20080331 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S14-15L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 STA 360 FRAME ANGLE ATTACHED TO FUSELAGE SKIN CRACKED, BETWEEN STR 14L AND 15L. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040400073 20080404 00073 NM 2008 4 4 2008UALA01823 1 20080331 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1197 S39L-R CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 AFT CARGO COMPARTMENT AT BS 1197+88 BETWEEN S-39L-39R SHEAR TIE IS CORRODED. MAJOR REPAIR ACCOMPLISHED, REMOVED AND REP LACED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040400094 20080404 00094 NM 2008 4 4 2008UALA01845 1 20080331 A 3350 3071BPEGPL LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 777UA 26916 FOUND EMERGENCY LIGHT AT SEAT 25C INOP. REPLACED LAMP. OP CHK'D OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040400107 20080404 00107 EU 2008 4 4 08FDEA01241 1 20080401 A 5730 A5724410800100 PANEL AIRBUS 310 A310203 3930313 EU RT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT WING PANEL NR 612 AT IS CHAFED ON THE MATING SURFACES. COMPLIED WITH EA 6-5720-118459 PT 1. 2 L 7 2 4F RT A35EU 2008040400113 20080404 00113 EU 2008 4 4 08FDEA01248 1 20080402 A 5330 A53772518204 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND SKIN PLATE DETACHED AT C20A, P28 RT REPAIR PERFORMED BY INSTALLING A REPAIR DOUBLER IAW RAS/EFW/9000018/2008 ISS. B, APPROVED BY EA 6-5313-115242. 2 L 7 2 4F RT A35EU 2008040400116 20080404 00116 EU 2008 4 4 08FDEA01251 1 20080402 A 5313 A53980852212 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CORROSION ON STRINGER P 56 LT, C 76-78. REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CRACK FREE AND FLAP PEEN ING IAW RAS/EFW/9000015/2008 ISS A, APPROVED BY EA 6-5318-114879. 2 L 7 2 4F RT A35EU 2008040400132 20080404 00132 EU 2008 4 4 08FDEA01267 1 20080402 A 5540 A55471556256 PLATE AIRBUS 300 A300B4622R 3930312 EU ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND ON RUDDER LIGHTNING PLATE CORRODED AND DISBONDED. REPAIR PERFORMED BY LAMINATING AND INSTALLING A NEW LIGHTNING P LATE IAW RAS/DAHAM/4024036/2007 ISS A, APPROVED BY EA 6-5540-114862. 2 L 7 2 4F RT A35EU 2008040400137 20080404 00137 NM 2008 4 4 DL76G080408 1 20080326 A 5315 BAC1505100744 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 654 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 155DL 25269 FLOORBEAM CORRODED AT STA 654+44 RBL 20 TO RBL 40. FLOORBEAM REPLACED PER 53-00-51D FIGURE 201 ON NR AVM529188. 2 L 7 2 4F RT A1NM 2008040400146 20080404 00146 NM 2008 4 4 DLM88080449 1 20080331 A 2120 UNKNOWN DOUG MD88 MD88 3023688 NM CABIN ODOR A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 27 953DL 49884 BOTH LAV SMOKE DETECTORS BEEPED ON FINAL, F/A REPORT NO INDICATIONS OF SMOKE OR FIRE, HAD SMOKE ODOR IN COCKPIT FOR A FE W MOMENTS. 2 L 7 2 4F RT A6WE 2008040400187 20080404 00187 NM 2008 4 4 DLM88080494 1 20080402 A 5320 ANGLE DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV A CRACK WAS FOUND ON ANGLE AT STA Y=1474 CANT BELOW ACCUMULATOR. ANGLE WAS REPLACED IAW DOUGLAS DWG 5917686. 2 L 7 2 4F RT A6WE 2008040400195 20080404 00195 NM 2008 4 4 DLM88080502 1 20080402 A 5313 LONGERON DOUG MD88 MD88 3023688 NM BS 1193-1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, A CRACK WAS FOUND ON SPLICE BETWEEN STAY=1193 AND 1212 LONG 28LH. SPLICE WAS REPLACED IAW DOUGLAS DWG 39146 77-507. 2 L 7 2 4F RT A6WE 2008040700007 20080407 00007 NM 2008 4 7 AALA200800604 1 20080312 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AA 24617 DFW - EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040700047 20080407 00047 NM 2008 4 7 DLM88080525 1 20080403 A 5210 PAN DOUG MD88 MD88 3023688 NM L1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, A CRACK WAS FOUND ON INNER PAN OF L1 DOOR AFT LOWER CORNER. DOOR WAS REPAIRED IAW SRM 52-05 FIG 18A. 2 L 7 2 4F RT A6WE 2008040700055 20080407 00055 2008 4 7 HALA0800471 4 20080331 A 2311 2305794 TRANSCEIVER BOEING 767 7673G5 1385126 NM LT HF SYSTEM MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 17689 17689 24259 ETOPS SIGNIFICANT SYSTEM, L HF TRANSMITTER UNABLE TO TRANSMIT OR RECEIVE. REMOVED AND REPLACED LT HF TRANSCEIVER IAW AM M 23-11-00, OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 2008040800006 20080408 00006 CE 2008 4 8 N71CK 1 20080318 A 2120 660021125 LIMITER LEAR 35 36A 5170603 CE A/C BAY DAMAGED E KC8A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 71CK 321 035 DURING CLIMB, THE CREW NOTICED THE CABIN ALTITUDE CLIMBING. FOLLOWING PROCEDURES IN THE AIRCRAFT FLIGHT MANUAL, THE CRE W NOTIFIED ATC OF THE PROBLEM AND DESCENDED TO A LOWER ALTITUDE AND RETURNED TO YIP. MAINTENANCE PERSONNEL FOUND THE PR ESSURIZATION DUCT TEMPERATURE LIMITER FLANGE BROKEN AND LEAKING. VALVE REPLACED WITH SERVICEABLE VALVE AND SYSTEM OPERA TION TESTED. ALL WORK PERFORMED IN ACCORDANCE WITH THE LEARJET 35/36/35A/36A MAINTENANCE MANUAL. 2 L 7 2 4F A10CE 2008040800017 20080408 00017 SO 2008 4 8 FDKA200803118 1 20080319 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 5984 JFK-BDL (0611 PHX LCL). TWO FLOOR EMERGENCY LIGHT STRIPS OUT. MX RESET EMERGENCY LIGHTING SYSTEM. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008040800027 20080408 00027 EA 2008 4 8 COMA0860188 1 20080323 A 5320 POST CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 934CA 33024 7042 CRACK AT FS 409+128 RBL 36.00 INBOARD LOWER POST. REPAIRED LOWER POST IAW REO 601R-53-41-189. 2 L 7 2 4F RT A21EA 2008040800032 20080408 00032 NM 2008 4 8 WRNA200800007 1 20080315 A 2197 CONNECTOR BOEING 747 7472U3B 1384846 NM NR 1 PACK DIRTY A WRNA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 05 923FT 22769 AFTER TAKEOFF FROM MIA, NR 1 PACK INOP, UNABLE TO MAINTAIN PRESSURIZATION WITH NR 3 PACK. RETURNED TO FIELD FOR A SAFE LANDING. WHILE TROUBLESHOOTING, FOUND CONNECTOR FOR NR 1 PACK DIRTY, CLEANED AND REINSTALLED CONNECTOR IAW 747 MM 21-51 -01 PAGE 401. OPS CHECKED GOOD IAW 747 MM 21-51-01 PAGE 404. A/C RELEASED TO SERVICE. 2 L 7 4 4F RT A20WE 2008040800035 20080408 00035 EA 2008 4 8 COMA0860194 1 20080324 A 3030 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA NR 2 ADS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 933CA 7040 FLIGHT 5501 - RECEIVED TAT PROBE HEAT, RIGHT AOA HEAT, RIGHT STATIC HEAT AND RIGHT PITOT HEAT CAUTION MESSAGES. RESET N R 2 ADS CONTROLLER. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008040800039 20080408 00039 SO 2008 4 8 C2XA08IA090 1 20080325 A 3610 BLEED AIR SYS EMB 135 EMB135LR 3260305 SO CONTAMINATED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 17524 145399 IAH - FLIGHT 2127, THE CREW REPORTED A LAV SMOKE INDICATION DURING DEPARTURE. THE AIRCRAFT RETURNED TO IAH WHERE IT LAN DED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND DETERMINED THE CAUSE TO BE RESIDUAL OIL IN THE BLEED AIR SYSTEM FROM PREVIOUS ENGINE CHANGE. THE SYSTEM WAS CLEANED, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008040800043 20080408 00043 SO 2008 4 8 FDKA200803124 1 20080323 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6115 MCO-TYS (1447 PHX LCL). THE 12A EMERGENCY LIGHT INOP. MX RE-SECURED CONNECTORS. 2 L 7 2 4T RT T00011AT 2008040800044 20080408 00044 SO 2008 4 8 FDKA200803125 1 20080324 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6150 TYS-CVG (0218 PHX LCL). EMERGENCY EXIT LIGHT ROW 12C INOP. MX RE-SECURED CONNECTOR ON LIGHT ASSY, OPS CHECK G OOD. 2 L 7 2 4T RT T00011AT 2008040800047 20080408 00047 EA 2008 4 8 FDKA200803127 1 20080325 A 5220 DOOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT OPEN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 600LR 15142 FDM 5965 JFK-DFW (1225 PHX LCL). FWD LT & RT EMERGENCY DOORS OPENED. MX RE-INSTALLED DOORS. 2 L 7 2 4F RT A21EA 2008040800053 20080408 00053 SO 2008 4 8 FDKA200803132 1 20080324 A 5347 14532606003 SEAT TRACK EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 LEFT OUTBOARD SEAT TRACK AT FRAME 30 TO 36 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK (145-32606-003). 2 L 7 2 4T RT T00011AT 2008040800054 20080408 00054 SO 2008 4 8 FDKA200803133 1 20080324 A 5220 14525737405 SKIN EMB 145 EMB145LR 3260212 SO ESCAPE HATCH DENTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 PASSENGER CABIN ESCAPE HATCH SKIN DENT. REPAIRED DOOR. 2 L 7 2 4T RT T00011AT 2008040800055 20080408 00055 SO 2008 4 8 C2XA08RI039 1 20080313 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY FAULTY A C2XA K NONE N FALSE WARNING DE DESCENT 1 SW 27 22971 2152 148149 FLIGHT 3128 - EWR - CREW REPORTED LAVATORY SMOKE DETECTOR WARNING DURING DESCENT. EWR MX REMOVED AND REPLACED SMOKE DET ECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008040800063 20080408 00063 NM 2008 4 8 HNAA0800039 1 20080119 A 3350 6038443LB POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN UNKNOWN A HNAA K NONE O OTHER CL CLIMB 1 EA 07 810EX 387 387 308 DURING CLIMBOUT, THE EMERGENCY LIGHTS FLICKERED ON AND OFF. UPON REACHING AN OVERNIGHT MAINTENANCE BASE, ALL SIX POWER SUPPLY BASES WERE CHANGED, AS WELL AS TERMINAL BLOCKS 9811-TB14-2, 9811-TB14-5 AND CONNECTOR 9811-P73. GROUND OPS CHECK S WERE GOOD AND AN EVALUATION FLIGHT WAS SCHEDULED. AFTER A SUCCESSFUL EVALUATION FLIGHT, THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 2008040800083 20080408 00083 SO 2008 4 8 C2XA08TY039 1 20080328 A 5730 SKIN EMB 145 EMB145EP 3260221 SO WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16927 145006 WING SKIN CRACK ON LEFT I/B CENTER SPOILER HINGE CUTOUT. REPAIRED CRACK IAW EC5740-01143. AIRCRAFT RELEASED AND RETURN ED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008040800084 20080408 00084 SO 2008 4 8 C2XA08CL040 1 20080330 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11127 145697 CLE FLIGHT2252 - THE CREW REPORTED CABIN CEILING EMERGENCY LIGHT WAS INOPERATIVE AT THE OVERWING EMERGENCY EXIT. MAINTE NANCE INSPECTED AND REPLACED THE NR 5 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2008040800090 20080408 00090 EA 2008 4 8 COMA0870011 1 20080327 A 3350 E520005705A PRINTED CKT BOAR CNDAIR CL600 CL6002C10 1390015 EA E&E BAY FAULTY A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 641CA 3648 10122 FLIGHT 5499 - EMERGENCY LIGHTS CYCLED ON AND OFF IN ARMED POSITION DURING TAXI. FOUND RELAY K135 MOUNTED ON PCB FAILING . REMOVED AND REPLACED PRINTED CIRCUIT BOARD ASSEMBLY. 2 L 7 2 4F RT A21EA 2008040800093 20080408 00093 EU 2008 4 8 WRNA20080009 1 20080328 A 3397 PIN AIRBUS 300 A300B4203 3930306 EU CABIN DISCONNECTED A WRNA K NONE L NO TEST IN INSP/MAINT 1 SO 05 821SC 211 DURING DAILY CHECK, MAINTENANCE FOUND R1 EMERGENCY EXIT LIGHTS INOP. FOUND PIN NR 3 DISCONNECTED FROM LIGHT ASSY, RECON NECTED, OPS CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A35EU 2008040800096 20080408 00096 EA 2008 4 8 COMA0860202 1 20080331 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 597SW 12705 7293 FLIGHT 5450 - AT LEVEL OFF FROM CLIMB AT 260 KTS, HIGH SPEED CLACKER SOUNDED FOLLOWED SHORTLY BY FLAPS FAIL CAUTION MESS AGE. FLAPS WERE AT 0 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY IN TYS. REMOVED AND REPLACED RIGHT BPSU. AL SO COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW-UP MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 2008040800101 20080408 00101 EU 2008 4 8 08FDEA01302 1 20080401 A 5321 A5378198422200 FLOOR SKIN AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 MAIN DECK FLOOR STRUCTURE, CORROSION ON UPPER SURFACE OF FLOOR WEBBING AT APPROX LBL 88 BETWEEN FRAMES 32 AND 33. BLEND ED CORROSION REF SRM 51-74-10 PAR 5. ORIGINAL MATERIAL THICKNESS OF .094 AND .065 AFTER BLEND OUT FOR TOTAL MATERIAL LOS S OF .029 FOUND TO BE OUT OF LIMITS REF SRM SUPP 53-74-15 FIG 1. REMOVED FLOOR WEBBING REF SRM 51-40-21 P 6-7. LOCATED AND DRILLED NEW FLOOR WEBBING REF SRM 51-40-21 P 6-7. ALODINED AND PRIMED FLOOR WEBBING REF SRM51-21-10. INSTALLED FL OOR WEBBING REF SRM 51-40-21 P 6-7 APPLIED C.I.C ON FLOOR WEBBING REF MM 51-22-00-0. 2 L 7 2 4F RT A35EU 2008040800104 20080408 00104 EU 2008 4 8 08FDEA01303 1 20080402 A 5753 A5797065000013 SKIN AIRBUS 310 A310203 3930313 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT FLAP VANE L/E SKIN CHAFED AT NR 3 TRACK ATTACH POINT. GENERATED RFTS N425FE-25-33028. RECEIVED EA NR 6-5750-118464. REMOVED FASTENER FROM BLENDED AREA. HFEC INSPECTED THE HOLE PER NTM 51-10-01 PART 6. NO FINDINGS. INSPECTED BLENDED AREA PER NTM 51-10-08 PART 6. NO FINDINGS. FINISHED BLENDED AREA WITH CORROSION PROTECTION PER SRM 51-23-10. INSTALL ED FASTENER IAW SRM 51-40-21 PARA 6. PRIMED AND PAINTED TO MATCH IAW SRM 51-23-10. RECORDED PART NR AND SERIAL NR PER EA 6-5750-118464. 2 L 7 2 4F RT A35EU 2008040800105 20080408 00105 NM 2008 4 8 SWAA081729 1 20080330 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 218WN 32489 R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008040800106 20080408 00106 NM 2008 4 8 SWAA081730 1 20080330 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 244WN 34864 DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS MISSING AT ROW 11 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008040800107 20080408 00107 NM 2008 4 8 SWAA081731 1 20080330 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008040800109 20080408 00109 NM 2008 4 8 SWAA081732 1 20080330 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510B, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008040300067 20080403 00067 NM 2008 4 3 200800302 1 20080317 A 5330 SKIN BOEING 747 747SPB5 1384813 NM FUSELAGE SCRATCHED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 708BA 22484 RT LOWER WING TO BODY, FROM STA 1860 TO STA 1790, FROM STRINGER 34R TO STRINGER 51R, SKIN HAS SCRIBE MARKS. APPROX STA 1820., STRINGER 46R, .005 DEPTH. BLENDED OUT SCRIBE LINES, MATERIAL LOSS IS .005, WITHIN LIMITS, ALODINED AND PRIMED AR EA PER B747 SP SRM'S 53-31-00 PG 1,3,4, 51-10-02 PG 6-6 B AND BSOPM 20-44-04-PG 1-4 2 L 7 4 4F RT A20WE 2008040300069 20080403 00069 NM 2008 4 3 200800304 1 20080317 A 5330 SKIN BOEING 747 747SPB5 1384813 NM FUSELAGE SCRATCHED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 708BA 22484 SCRIBE LINES IN FUSELAGE SKIN LOWER LEFT SIDE FORWARD WING TO BODY FAIRING AREA BS 580 TO 620 STRINGER 34L TO 47L APPROX . DEPTH IS .002 AT BS 620 STRINGER 46L. BLENDED OUT SCRIBE LINES, MATERIAL LOSS IS .006 ALODINED AND PRIMED AND INSTAL LED RUB STRIPS PER B747 SP SRM'S 51-10-01 PG 13-15, 53-51-00 PG 1-4, 51-10-02 PG 6-6B AND BSOPM 20-44-04 PG 1-4, MATERIA L LOSS WITHIN LIMITS. 2 L 7 4 4F RT A20WE 2008040200118 20080402 00118 NM 2008 4 2 2008UALA01621 1 20080321 A 2560 LEVER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE AFT GIRT BAR OBSTRUCTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 801UA 686 DOOR 1R WILL NOT ARM. CAUSE, INTERFERENCE WITH BENT FLOOR PLATE, UNKNOWN DAMAGE. REWORKED FLOOR COVER PLATE TO ALLOW C LEARANCE FOR DOOR, OPS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200131 20080402 00131 NM 2008 4 2 CALA0800268 1 20080327 A 5320 6552878U124 CHANNEL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 70330 23460 FOUND CORROSION ON Z-CHANNEL UNDER L2 DOOR SILL PLATE. REMOVED AND REPLACED Z-ANGLE PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008040200139 20080402 00139 NM 2008 4 2 2008UALA01636 1 20080321 A 2560 GIRT BAR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AFT GALLEY DOOR OUT OF TOLERANCE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 AFT GALLEY DOOR EVAC SLIDE GIRT FABRIC VERY DIRTY AND STARTING TO FRAY. REPAIRED RUBBER STRIP AND PATCHED GIRT FABRIC. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200146 20080402 00146 NM 2008 4 2 2008UALA01641 1 20080323 A 3320 5106WW LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW REST AREA FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 127UA 28813 CREW REST AREA OVERHEAD FLUORESCENT CEILING LIGHT ABOVE UPPER BUNK STRONG ELECTRICAL BURNING ODOR. FOUND MATERIAL ON BU LB THAT CAUSED ODOR. REPLACED NIGHT LIGHT LAMP. OPS CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200154 20080402 00154 NM 2008 4 2 2008UALA01649 1 20080322 A 3150 WARNING LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU FIRE BOTTLE ILLUMINATED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 211UA 30217 APU FIRE BOTTLE DISCHARGE ILLUMINATED AT WHEELWELL LOCATION. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040200163 20080402 00163 2008 4 2 2008UALA01657 4 20080322 A 2330 ENTERTAIN SYS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SEAT15 SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 845UA 1585 ARMRESTS 15ABC HOT ELEC SMOKE SMELLED BY PAX & FASCB PFS MUSIC CABIN LT POPPED SMOKE STOPPED. NEED FURTHER DETAILS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200180 20080402 00180 NM 2008 4 2 2008UALA01669 1 20080324 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 596UA 28749 EXIT PATH LIGHTING NOT SECURED TO FLOOR AT ROW 13 ABC. CAUSE, UNKNOWN. SECURED EEL LIGHT TO FLOOR TRACK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200183 20080402 00183 EU 2008 4 2 2008UALA01673 1 20080324 A 2700 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELAC 1 MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 436UA 638 ELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CAUSE, ELAC 1 FAILURE. REPLACED ELAC 1, ACCOMPLISHED OPS TESTS, OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200185 20080402 00185 NM 2008 4 2 CALA0800277 1 20080317 A 5315 BAC15171489 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 STA 70 FLOORBEAM BL 0 TO RBL 12 HAS CORROSION DAMAGE AT BS 270 FLOORBEAM FOUND TO BE OUT OF LIMITS PER 737-300 SRM 53-10 -51 FIG 101. REMOVED DAMAGE & REPAIRED PER AVO 350-53-007 CAL REV A. WEIGHT OF REPAIR WITH FASTENERS AS INSTALLED IS L ESS THAN 5 LBS. 2 L 7 2 4F RT A16WE 2008040200201 20080402 00201 NM 2008 4 2 2008UALA01685 1 20080325 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 EEL STRIP INOP IN FRONT OF MID AFT LAV. CAUSE, DAMAGED WIRING FROM UNKNOWN SOURCE. SPLICED WIRE ON EEL STRIP. OPS CHE CKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200216 20080402 00216 2008 4 2 SWAA081717 4 20080327 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008040200228 20080402 00228 NM 2008 4 2 2008UALA01700 1 20080326 A 3510 OXYGEN SYSTEM BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 792UA 26934 CREW O2 NEEDS SVC 1350 PSI. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040200232 20080402 00232 NM 2008 4 2 2008UALA01702 1 20080326 A 5210 DOOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 OUT OF RIG A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 DOOR 2 LEFT UNABLE TO ARM, FOUND DOOR OUT OF RIG. FOUND UPPER AND LOWER JAMB NUTS ON TORQ TUBE LOOSE. ON INSP FOUND TA NG WASHER INSTALLED INCORRECTLY. LOWER GATE IS STRIKING DOOR THRESHOLD UPON DOOR CLOSURE. BY- 124277 :LOWER JAM NUT LOCK WASHER IS INSTALLED UPSIDE DOWN. LOCK WASHER IS NOW INEFFECTIVE AND WILL NOT SECURE LOWER JAM NUT. AS DOOR IS OPENED AN D CLOSED LOWER JAM NUT WORKS LOOSE AND DOOR BEGINS TO SAG AGAIN. DOOR REMOVED FROM A/C AND RE-RIGGED, REWORKED JAMB WASH ER. DOOR INSTALLED AND OPENS AND CLOSES PROPERLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200239 20080402 00239 NM 2008 4 2 2008UALA01712 1 20080326 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 430 S22-26R BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 BURN IN SKIN STA 430 BETWEEN STR 22R AND 23R. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200240 20080402 00240 NM 2008 4 2 SWAA081697 1 20080330 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040200243 20080402 00243 NM 2008 4 2 SWAA081698 1 20080330 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040200290 20080402 00290 EU 2008 4 2 08FDEA01190 1 20080328 A 5755 A5777020920000 SKIN AIRBUS 310 A310203 3930313 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT WING NR 6 SPOILER TRAILING EDGE IS KNIFE EDGED. REMOVED DAMAGED TRAILING EDGE IAW A310 SRM 51-40-21. LOCATED; D RILLED; AND INSTALLED NEW TRAILING EDGE IAW A310-200 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008040200293 20080402 00293 EU 2008 4 2 08FDEA01192 1 20080328 A 5755 A5771006820851 SKIN AIRBUS 310 A310203 3930313 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT WING NR 4 SPOILER T/E IS CHAFED. REMOVED DAMAGED SEALS AND REPLACED THEM WITH NEW SEALS P/N A5771006820851, PO 61 2443.6 BOTH IAW FEDEX A310-200 SRM 51-40-21; PGS 11-26. PRIMED AND TOP COAT PAINT BOTH IAW FEDEX A310-200 SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008040200296 20080402 00296 NM 2008 4 2 KCSA081183 1 20080319 A 5330 SKIN BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 EXTERNAL FUSELAGE SKIN IS DAMAGED AT STA 530 BETWEEN STR 41L & 42L. 2 L 7 4 4F RT A20WE 2008040200316 20080402 00316 NM 2008 4 2 HALA0800437 1 20080327 A 2841 300710607 PROCESSOR BOEING 767 76733A 1385209 NM FUEL QTY MALFUNCTIONED A HALA O OTHER P NO WARNING INDICATION CL CLIMB 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, DURING CLIMB CTR FUEL TANK AND TOTALIZER WENT BLANK. RETURNED TO NML W/I 1 HOUR. REMOVED AND REPLACED FUEL QTY PROCESSOR PER MM 28-41-08, CKS GOOD. 2 L 7 2 4F RT A1NM 2008040200325 20080402 00325 2008 4 2 SA08023 4 20080329 A 2210 4911710 COMPUTER AIRBUS A319 A319132 3930340 NM FLAP SLATS MALFUNCTIONED A USAA O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 19 818AW 51926 9690 1375 SNA FLIGHT 139 LAS-SNA - DURING FLIGHT, EXPERIENCED A 20 DEGREE UNCOMMANDED ROLL WITH THE SPEED BRAKE APPLIED AND FLAP L OWERED. MAINTENANCE REPLACED THE NUMBER ONE SLAT AND FLAP CONTROL COMPUTER. 2 L 7 2 4F RT A28NM 2008040200333 20080402 00333 2008 4 2 ASAA0852786 2 20080329 A 7261 UNKNOWN BOEING 737 737890 1384527 NM LEAKING A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 587AS 35684 OIL DRIPPING FROM NR 1 ENGINE. OIL APPEARS TO BE COMING FROM AREA OF IDG OR HYDRAULIC PUMP PAD. OPERATED ENGINE AND PE RFORMED LEAK CHECK. NO LEAKS NOTED ON 5 MIN ENGINE RUN. 2 L 7 2 4F RT A16WE 2008040200348 20080402 00348 NM 2008 4 2 2008UALA01327 1 20080310 A 2750 UNKNOWN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE TE FLAPS UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 334UA 24229 CREW NOTED TWO C/B'S OUT AFTER FLAP RETRACTED. P6-2 D12 FLAPS (SHUTOFF VLV) AND P6-2 D13 FLAP LOAD RELIEF. SUPPLEMENTA L DATA UPDATE CAUSE, UNKNOWN. NO FINDINGS. NO FURTHER INCIDENTS. CLEANED CONNECTOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200352 20080402 00352 NM 2008 4 2 2008UALA01735 1 20080328 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EEL LIGHT INOP AT LAV 116, ADJACENT TO DOOR 5R. SUSPECT BROKEN CONNECTION. REPAIRED EEL LIGHT. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200370 20080402 00370 NM 2008 4 2 2008UALA01757 1 20080328 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 588UA 26717 FOUND DOOR 1R GIRT BAR IS FAULTY. FOUND DIRT ACCUMULATING UNDER GIRT BAR. CLEANED GIRT BAR TRACKS, DOOR OPERATES, ARMS/D ISRAMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040200378 20080402 00378 WP 2008 4 2 08FDEA01195 1 20080328 A 5330 ACA3019505 SKIN DOUG MD10 MD1010F 3022112 WP FUSELAGE BULGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 BULGING ON THE EXTERIOR FUSELAGE SKIN; LEFT AT STA 515 TO 521; LONGERON 27L TO LONGERON 28L. REMOVED RIVETS IAW DC/MD-1 0 SRM 51-31-01; VOL II. FORMED SKIN IAW DC/MD-10 SRM 53-20-00; VOL II. INSTALLED RIVETS IAW DC/MD-10 SRM 51-31-10; VOL II. REMOVED AND REINSTALLED FLOOR PANELS; SIDEWALLS AND VENT PANELS IAW DC/MD-10-10 AMM 53-21-01- 2. ALODINED AN D PRIMED IAW DC/MD-10 SRM 51-21-01; VOL II AND COMPLIED WITH FEDEX EA 8- 5330-118542 "FUSELAGE, FINGER DOUBLER REPAIR S TA 517 AND LONGERON 27L. 2 L 7 3 4F RT A22WE 2008040200390 20080402 00390 WP 2008 4 2 08FDEA01210 1 20080331 A 7110 NTL6012509AE SKIN DOUG MD10 MD1010F 3022112 WP NR 2 COWLING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 NR 2 ENGINE RIGHT FAN COWL INNER SKIN IS CHAFED. REMOVED DAMAGED AREA, FABRICATED REPAIR DETAILS, PREPPED DETAILS FOR B ONDING, BONDED REPAIR; INSTALLED RIVETS & SEALED IAW SRM 54-00-01 VOL I. PRIMED IAW SRM 51-21-01 VOL II. 2 L 7 3 4F RT A22WE 2008040300005 20080403 00005 WP 2008 4 3 ABXR080105 1 20080302 A 5314 5931960511 ATTACH ANGLE DOUG DC9 DC932F 3022067 WP KEEL WEB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 205US 47690 LEFT WHEEL WELL KEEL WEB UPPER ATTACH ANGLE AT STA 718 CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51 -30-5. 2 L 7 2 4F A6WE 2008040300016 20080403 00016 NM 2008 4 3 ABXA080112 1 20080307 A 5230 140T26033 BEAM BOEING 767 767281 1385109 NM AFT CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 775AX 22790 AFT LOWER CARGO DOOR BEAM CORRODED JUST BELOW PRESSURE DOOR. REMOVED AND REPLACED BEAM IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008040300032 20080403 00032 NM 2008 4 3 ABXA080094 1 20080216 A 2782 114T61241 MOUNT FITTING BOEING 767 767281 1385109 NM FLAP ACTUATOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 769AX 22787 KRUEGER FLAP ACTUATOR OUTBOARD MOUNT FITTING CRACKED. REMOVED AND REPLACED FITTING IAW B767 SRM. 2 L 7 2 4F RT A1NM 2008040300072 20080403 00072 NM 2008 4 3 200800307 1 20080317 A 5330 SKIN BOEING 747 747SPB5 1384813 NM FUSELAGE SCRATCHED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 708BA 22484 SCRIBE LINES IN FUSELAGE SKIN UPPER LEFT SIDE FORWARD WING TO BODY FAIRING AREA BS 620 TO BS 1000 STRINGER 23L TO STRING ER 34L. APPROX DEPTH IS .002 AT BS 780 STRINGER 24L. BLENDED OUT SCRIBE LINES, MATERIAL LOSS IS .002 WITHIN LIMITS ALO DINED AND PRIMED AND INSTALLED RUB STRIPS PER B747 SP SRM 51-10-01 PG 13-15, 53-31-00 PG 1-4, 51-10-02 PG 6-6B AND BSOPM 20-44-04 PG 1-4. 2 L 7 4 4F RT A20WE 2008040300073 20080403 00073 NM 2008 4 3 2008UALA01624 1 20080322 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE S16L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FUSELAGE STRINGER 16L, INBD WEB HAS 2 ATTACH CLIPS CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED BOTH CLIPS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040300078 20080403 00078 NM 2008 4 3 2008UALA01661 1 20080324 A 5230 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 FWD CARGO DOOR EXTERNAL SKIN HAS 8 EACH DENTS. MAJOR REPAIR ACCOMPLISHED: EVALUATED ALL DENTS & FOUND ALL BUT TWO DENTS AT UPPER MID SPAN OF DOOR IN UPPER HALF ABOVE HANDLE ASSY OUT OF LIMITS. CUT OUT DAMAGED AREA & FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040300079 20080403 00079 NM 2008 4 3 2008UALA01670 1 20080324 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 3E INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 782UA 26948 FOUND SEAT 3E FWD EEL INOP. REPLACED LIGHT STRIP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040300081 20080403 00081 NM 2008 4 3 2008UALA01671 1 20080324 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 22C INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 782UA 26948 FOUND SEAT 22C EEL INOP. REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040300097 20080403 00097 NM 2008 4 3 233321 1 20080305 A 3240 511531 HOUSING BOEING 737 737* NM BRAKE SYS CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 HOUSING CRACKED IN MOUNTING HOLE. 2 L 7 2 4F RT A16WE 2008040300100 20080403 00100 EA 2008 4 3 COMA0860181 1 20080319 A 4990 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA APU MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 597SW 7293 FLIGHT 5539- RECEIVED APU OIL TEMP CAUTION MESSAGE. DECLARED EMERGENCY, DIVERTED TO CRW, LANDED WITHOUT INCIDENT.CHECK ED APU OIL LEVEL AND PERFORMED OPS CHECK OF APU. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008040300114 20080403 00114 EU 2008 4 3 NWAA081273353 1 20080328 A 2910 51U742 HYDRAULIC LINE AIRBUS A330 A330223 3940031 EU HYDRAULIC SYSTEM BROKEN A NWAA H DEACTIVATE SYST/CIRCUITS K FLUID LOSS CL CLIMB 1 GL 01 853NW 0618 ON CLIMB-OUT OF NRT, THE BLUE HYDRAULIC SYSTEM QUANTITY WENT TO ZERO, FOLLOWED COM AND RETURNED TO NRT AND THE LANDING W AS UNEVENTFUL. FOUND HYDRAULIC SYSTEM HOSE BROKEN, REPLACED HOSE AND ENGINE DRIVEN HYDRAULIC PUMP AND TESTS OK AND AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A46NM 2008040300115 20080403 00115 SO 2008 4 3 FFKA127 2 20080327 A 8530 654970CN CYLINDER CONT LTSIO360EB PIPER PA34 PA34200T 7103406 SO CONT O360 LTSIO360EB 17025 SO RT ENGINE FAILED B FFKA E B ENGINE SHUTDOWN EMER. DESCENT E K VIBRATION/BUFFET FLUID LOSS CR CRUISE 1 SO 05 39545 154 807957R 347870389 807957R DURING CRUISE FLIGHT, THE PILOT NOTICED THAT THE MANIFOLD PRESSURE ON THE RIGHT ENGINE WAS CREEPING LOWER AND LOWER, PIL OT COMPENSATED BY ADVANCING RIGHT ENGINE THROTTLE UNTIL THERE WAS NO MORE THROTTLE TO ADVANCE. THERE WAS NO OTHER INDIC ATION OF SOMETHING WRONG. AT THE TIME OF MAKING A DECISION ON SECURING THE ENGINE THERE WAS A LOUD BANG AND SMOKE/OIL C OMING FROM THE RIGHT ENGINE NACELLE. AFTER LANDING IT WAS DISCOVERED THAT THE NUMBER 6 CYLINDER HAD BLOWN OFF ITS MOUNT SHEARING 4 OUT OF 6 STUDS AND STRIPPING THE NUTS ON THE OTHER 2. 1 L 7 2 3O 3 O A7SO E9CE 2008040300117 20080403 00117 SO 2008 4 3 FFKA126 1 20080326 A 2910 67700123 HYDRAULIC LINE PIPER PA32 PA32R300 7103213 SO HYDRAULIC SYSTEM LEAKING B FFKA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 05 4498F 4940 151 32R7680453 SHORTLY AFTER TAKEOFF AND THE LANDING GEAR RETRACTED, THE PILOT NOTICED THAT THE GEAR UNSAFE LIGHT ILLUMINATED AND THEN WITH IN A FEW SECONDS HIS GEAR INDICATED DOWN AND LOCK. MAINTENANCE INVESTIGATED THE PROBLEM AND FOUND A SMALL HOLE IN A HARD LINE THAT RELEASED THE HYDRAULIC PRESSURE ALLOWING THE GEAR TO EXTEND. HARD LINE WAS REPLACED AND NO FURTHER DEF ECTS WERE NOTED. 1 L 7 1 3O A3SO 2008040300119 20080403 00119 SO 2008 4 3 FFKA128 2 20080331 A 8520 402711 STUD BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO LT ENGINE BACKED OUT B FFKA C E ABORTED TAKEOFF ENGINE SHUTDOWN K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 05 7351R 820 TH481 244309R PILOT ABORTED TAKEOFF AFTER SEEING SOME SMOKE COMING FROM THE LEFT ENGINE NACELLE. AFTER INVESTIGATION IT WAS FOUND THA T A STUD HAD BACKED OFF AND FELL OFF THE ENGINE ALLOWING ENGINE OIL TO COME OUT OF THE HOLE AND DRIP ONTO THE EXHAUST PI PES. 1 L 7 2 3O 3 O 3A16 E5CE 2008040300121 20080403 00121 NM 2008 4 3 NACA20080004 1 20080317 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 322DL 23094 FUSELAGE SKIN CRACK AT STRINGER 23R STA 950 APPROXIMATELY 2 3/8" LONG. CRACK HAS BEEN TRIMMED OUT PER BOEING 737 SRM 53 -30-03, FIG 48 TO 2,9375 INCH LONG AND .5625 INCH WIDE. LOCATED AT STR 23R, BS 950.75 - BS 953.6875. INSTALLED REPAIR DOUBLER, TRIPLER, TEAR STRAP REPAIR PER BOEING SERVICE REQUEST MESSAGES 1-793858201-1 THRU -14, AND 8100-9, DATED 26 MAR CH 2008. THIS INTERIM REPAIR DOES ENCOMPASS THE PREVIOUS REPAIR. 2 L 7 2 4F RT A16WE 2008040300125 20080403 00125 NM 2008 4 3 NACA20080005 1 20080317 A 5330 SKIN BOEING 737 737232 1384475 NM FUSELAGE CRACKED A NACA K NONE O OTHER IN INSP/MAINT 1 AL 03 322DL 23094 FUSELAGE SKIN CRACK AT STRINGER 24R STA 953 APPROXIMATELY 2 1/2" LONG. CRACK HAS BEEN TRIMMED OUT PER BOEING 737 SRM 53 -30-03, FIG 48 TO 2,9375 INCH LONG AND .5625 INCH WIDE. LOCATED AT STR 24R, BS 953.125-BS 956.0625. INSTALLED REPAIR D OUBLER, TRIPLER, TEAR STRAP REPAIR PER BOEING SERVICE REQUEST MESSAGES 1-793858201-1 THRU -14, AND 8100-9, DATED 26 MARC H 2008. THIS INTERIM REPAIR DOES ENCOMPASS THE PREVIOUS REPAIR. 2 L 7 2 4F RT A16WE 2008040300129 20080403 00129 EA 2008 4 3 CHQA200800062 1 20080328 A 4990 1603662 OIL COOLER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE APU LEAKING A CHQA A UNSCHED LANDING K M FLUID LOSS OVER TEMP CR CRUISE 1 GL 11 466CA 1716 1716 7627 GEE873331 FLIGHT 5601, IAH TO JAX - DURING CRUISE THE CREW RECEIVED AN APU OIL TEMP MESSAGE ON EICAS. THE PROPER QRH CHECKLISTS W ERE FOLLOWED, AND THE FLIGHT DIVERTED TO PNS, WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU AND FOUND THAT IT WAS LOW ON OIL. AFTER SERVICING THE OIL TO THE CORRECT LEVEL THE APU THEN OPERATED NORMALLY AND THE AIRCRAFT W AS RELEASED FOR SERVICE. ON THE 31ST OF MARCH, THE APU WAS TROUBLESHOT DUE TO THE HIGH OIL TEMPERATURE PROBLEMS AND THE APU OIL COOLER WAS FOUND TO BE CLOGGED AND LEAKING OIL. THE OIL COOLER WAS REPLACED AND THE APU OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 2008040300131 20080403 00131 WP 2008 4 3 NWAA081299935 1 20080330 A 2150 COUPLING DOUG DC9 DC931 3022065 WP RT A/C PACK LEAKING A NWAA O I OTHER CABIN DEPRESSURIZATION O OTHER CR CRUISE 1 GL 01 1332U 47404 THE RED "CABIN PRESS" WARNING LIGHT ILLUMINATED AS THE CABIN LOST PRESSURIZATION IN FLIGHT. THE FLIGHT CREW CONFIRMED T HAT THE CABIN WAS AT 11,000 FEET AND UTILIZED THE RED BORDERED CHECKLIST TO CORRECT IT. CABIN PRESSURE CONTROL WAS RECO VERED AFTER SECURING WING AND ENGINE ANTI-ICE. THE AIRCRAFT ALSO WAS DESCENDED FROM FL340 TO FL300 FOR REMAINDER OF CRU ISE FLIGHT. MAINTENANCE FOUND THE RIGHT PACK COUPLING LEAKING AND REPLACED IT AND ITS PERI-SEAL. LEAK CHECKS WERE GOOD AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2008040300133 20080403 00133 EU 2008 4 3 NWAA081313301 1 20080330 A 3350 BATTERY AIRBUS 330 A330323 3930335 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 801NW 0524 TEST FAULTED EPSU BATTERY (12WL) DOOR NR 1. REPLACED BATTERY AND TESTED GOOD. 2 L 7 2 4F RT A46NM 2008040300134 20080403 00134 NM 2008 4 3 NWAA081323155 1 20080330 A 3350 32145410 EPSU AIRBUS A319 A319114 3930350 NM CABIN DISCHARGED A NWAA K NONE O OTHER TX TAXI/GRND HDL 1 GL 01 355NB 15241 15241 1839 THE EMERGENCY PATHWAY LIGHTS FLASHING AFTER LANDING AND ALL THE WAY TO THE GATE. REPLACED EPSU 11WL, TESTS GOOD. 2 L 7 2 4F RT A28NM 2008040300135 20080403 00135 WP 2008 4 3 IXXA08SMN077S 1 20080214 A 5311 S2537716 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT FRAME LOWER FLANGE CRACKED AT STATION 480.000 LONGERO N 34 RIGHT. REMOVED DAMAGED AREA. FABRICATED NEW FRAME SEGMENT, SPLICES, ANGLES. HEAT TREATED EXTRUSION FRAME SEGMENT . CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, DC8 SRM 53-2-0 FIGURE 2 SHEET 1, 2, 6, DC8 SRM 53-4-1 FIGURE 40 SHEET 14-15, DC8 SRM 51-2-0 FIGURE 50 SHEET 49A, DC8 SRM 53-2-0 FIGURE 2 SHEET 7-8, T/R NR 53-110 DATED 11-10-00, DC8 SRM 51-1-1 PAGE 1, 13, 17, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008040300136 20080403 00136 EA 2008 4 3 SWIA200819398 1 20080327 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 418SW 7446 FLT 6433 - MAIN CABIN DOOR FLOOR LEVEL EMERGENCY LIGHT IS BROKEN. REPLACED LIGHT ASSEMBLY PER CRJ 200 MM 33-57-19. 2 L 7 2 4F RT A21EA 2008040300142 20080403 00142 EA 2008 4 3 SWIA200819404 1 20080330 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 957SW 7829 FLT 6722 - THE FIRST OFFICERS SIDE WINDOW IS CRACKED. REPLACED WINDOW IAW 56-12-01, P/N NP-139322-12, S/N OFF 03105H184 0. 2 L 7 2 4F RT A21EA 2008040300148 20080403 00148 NM 2008 4 3 HALA0800445 1 20080328 A 2132 INDICATOR BOEING 767 7673G5 1385126 NM CABIN PRESSURE DEFECTIVE A HALA K NONE O OTHER CR CRUISE 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, PER VERBAL FROM CAPTAIN CABIN PRESSURE IND RATE OF CLIMB NEEDLE FLUCTUATES WITH NO CHANGE IN C ABIN RATE OF CLIMB. REMOVED AND REPLACED CABIN PRESSURE INDICATOR IAW AMM 21-33-01 O9 OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008040300149 20080403 00149 NM 2008 4 3 HALA0800446 1 20080331 A 3350 POWER STRIP BOEING 767 7673G5 1385126 NM CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 588HA 33466 FLOOR EMERGENCY LIGHTS INOP ADJ TO LAV C. REPLACED POWER STRIP PER AMM 33 51 10, OPS CHECKS GOOD. 2 L 7 2 4F RT A1NM 2008040300153 20080403 00153 EA 2008 4 3 SWIA200819405 1 20080330 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 910SW 7566 FLT 6701 - LEFT WINDSHIELD SHATTERED. REPLACED WINDOW IAW AMM 56-11-01, P/N OFF NP139321-9, S/N OFF 02287H7797. 2 L 7 2 4F RT A21EA 2008040300155 20080403 00155 2008 4 3 SWIA200819407 4 20080327 A 3170 DCU CNDAIR CL600 CL6002C10 1390015 EA NR 1 FAULTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 728SK 10192 FLT 6083 - RECEIVED A R REV WARNING MESSAGE ALONG WITH OTHER INDICATIONS ON CLIMB-OUT. REPLACED NR 1 DCU IAW MM 31-31-0 1. OPS CHECKS GOOD, P/N 822-1310-104, S/N 1MB3N. 2 L 7 2 4F RT A21EA 2008040300157 20080403 00157 SO 2008 4 3 SWIA200819409 1 20080326 A 3397 WIRE EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA O OTHER L NO TEST UK UNKNOWN 1 NM 07 581SW 120349 FLT 5714 - EXIT LIGHT AT ROW 9 IS INOP. REPAIRED WIRING AT EXIT SIGN. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008040300178 20080403 00178 NM 2008 4 3 HNL0800456 1 20080327 A 5320 BRACKET BOEING 767 767332 1382001 NM FUSELAGE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 CRACKED BRACKET IN WHEELWELL, SECONDARY STRUCTURE. BRACKET REPAIRED IAW B767-300, SRM 51-70-11. 2 L 7 2 4F RT A1NM 2008040300179 20080403 00179 NM 2008 4 3 HALA0800457 1 20080327 A 5320 SILL BOEING 767 767332 1382001 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 LEVEL 1 CORROSION ON AFT CARGO DOOR CUTOUT MAIN SILL UPPER SURFACE AT STN 1351 - 1357. BLENDED REPAIR, IAW SRM 53-00-15 /101. 2 L 7 2 4F RT A1NM 2008040300185 20080403 00185 NM 2008 4 3 HALA0800463 1 20080327 A 5730 SKIN BOEING 767 767332 1382001 NM RT WING CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 LEVEL 1 CORROSION ON RIGHT WING LOWER SURFACE AT STRINGER L-15, WS 620-646. REWORKED IAW SRM 51-10-02. 2 L 7 2 4F RT A1NM 2008040300187 20080403 00187 NM 2008 4 3 HALA0800465 1 20080327 A 2530 GALLEY BOEING 767 767332 1382001 NM CABIN CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 MID GALLEY COMPARTMENT M106 LT O/B PARTITION SHOWS SIGNS OF CORROSION BETWEEN PLATES ADJACENT TO BENCH TOP. REPAIRED IA W SRM 51-10-01. 2 L 7 2 4F RT A1NM 2008040300193 20080403 00193 NM 2008 4 3 08FDEA01203 1 20080329 A 5315 BAC1505100617 FLOORBEAM BOEING 727 727225 1384077 NM BS 560 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 MAIN CARGO COMPARTMENT, FLOORBEAM CORRODED AT BS 560, RBL 0-25. REMOVED CORROSION IAW SRM 51-10-6, AND FOUND OUT OF LIM ITS IAW SRM 53-10-1 FIG 4. REMOVED SPLICE ANGLE AND DISPLACED SEAT TRACK FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGED S ECTION FROM RBL 32 TO LBL 14. FABRICATED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS AND PREVIOUSLY REMOVED A ND DISPLACED PARTS IAW SRM 53-10-8 FIG1 AND 51-30-2. 2 L 7 3 4F A3WE 2008040300197 20080403 00197 WP 2008 4 3 08FDEA01215 1 20080331 A 5720 ARB07892 FITTING DOUG MD10 MD1010F 3022112 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 STRINGER BUTTERFLY FITTING NR 43 IS CRACKED APPROX 1/2 TOTAL LENGTH ON THE RIGHT WING, STA XORS 372. THE FITTING IS INS IDE THE FUEL TANK AT STRINGER 43, RIB XORS 372. REMOVED & REPLACED FITTING REF SRM 51-33-01; VOL II 2 L 7 3 4F RT A22WE 2008040300201 20080403 00201 EU 2008 4 3 08FDEA01219 1 20080401 A 5753 SEAL AIRBUS 310 A310222 3930315 EU FLAP DOUBLER MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 448FE 260 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING OUTBOARD FLAP LOWER MAIN SKIN BETWEEN RIBS 4 AND 5 MEASURES 10.6 I NCHES BY 9 INCHES. REPAIR NOT IAW SRM REQUIREMENTS DUE TO REPAIR MISSING FILLET SEAL AND PAINT. REPAIRED PROTECTIVE CO ATING AND RE-SEALED EDGES IAW A310-200 SRM 57-53-12 FIG 210. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008040300210 20080403 00210 WP 2008 4 3 08FDEA01228 1 20080401 A 5311 70750080C FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 MCD-FUSELAGE UPPER LOBE AT FS 635, 655, 675, 695, 715, 735, 755 AND 775, LONGERON 13R HAS CHAFED DAMAGED FROM LINER MOUN T FASTENER. REMOVED FRAME SPLICE, FABED NEW SPLICE ON TRAVELER T8/729478, LOCATED AND DRILLED HOLES AND INSTALLED NEW S PLICE AT STA 675 IAW SRM 51-31-01, 53-30-00 FIG 4. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ATTENTION RECORDS, THIS IS A CLASS "B" REPAIR AND HAS AN INITIAL REINSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES. 2 L 7 3 4F RT A22WE 2008040300211 20080403 00211 WP 2008 4 3 08FDEA01229 1 20080401 A 5311 70750080C FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 MCD-FUSELAGE UPPER LOBE-FRAME AT FS 635, 655, 675, 695, 715, 735, 755 AND 775, LONGERON 13R HAS CHAFED DAMAGED FROM LI NER MOUNT FASTENER. REMOVED FRAME SPLICE, FABED NEW SPLICE ON TRAVELER T8/29478, LOCATED AND DRILLED HOLES AND INSTALLE D NEW SPLICE AT STA 695 IAW SRM 51-31-01, 53-30-00 FIG 4. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ATTENTION RECORDS, T HIS IS A CLASS "B" REPAIR AND HAS AN INITIAL REINSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES. 2 L 7 3 4F RT A22WE 2008040300212 20080403 00212 WP 2008 4 3 08FDEA01230 1 20080401 A 5311 70750080C FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 MCD-FUSELAGE UPPER LOBE-FRAME AT FS 635, 655, 675, 695, 715, 735, 755 AND 775, LONGERON 13R HAS CHAFED DAMAGE FROM LIN ER MOUNT FASTENER. REMOVED FRAME SPLICE, FABED NEW SPLICE ON TRAVELER T8/29475, LOCATED AND DRILLED HOLES AND INSTALLED NEW SPLICE AT STA 715 IAW SRM 51-31-01, 53-30-00 FIG 4. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ATTENTION RECORDS, TH IS IS A CLASS "B" REPAIR AND HAS AN INITIAL REINSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES. 2 L 7 3 4F RT A22WE 2008040300213 20080403 00213 WP 2008 4 3 08FDEA01231 1 20080401 A 5311 70750080C FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 MCD-FUSELAGE UPPER LOBE-FRAME AT FS 635, 655, 675, 695, 715, 735, 755 AND 775, LONGERON 13R HAS CHAFED DAMAGED FROM LI NER MOUNT FASTENER. REMOVED FRAME SPLICE, FABED NEW SPLICE ON TRAVELER T8/729477, LOCATED AND DRILLED HOLES AND INSTALL ED NEW SPLICE AT STA 735 IAW SRM 51-31-01, 53-30-00 FIG 4. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ATTENTION RECORDS, THIS IS A CLASS "B" REPAIR AND HAS AN INITIAL REINSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES. 2 L 7 3 4F RT A22WE 2008040300218 20080403 00218 WP 2008 4 3 08FDEA01236 1 20080401 A 5753 NRC6055505 SKIN DOUG MD10 MD1010F 3022112 WP T/E FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT WING INBD FLAP LOWER SURFACE AT STA XIFH 162 TO XIFH 175 FROM THE FRONT SPAR PLANE TO THE REAR SPAR PLANE HAS 3 EA DENTS THAT REQUIRE REPAIR. CUT OUT DAMAGE IN REF TO SRM 57-10-00 FIG 85 VOL I. FABRICATED DOUBLERS IN REF TO SRM 57-1 0-00 FIG 85 VOL I. ALODINED & PRIMED DOUBLERS IN REF TO SRM 51-21-01 VOL II. INSTALLED DOUBLERS IN REF TO SRM 57-10-00 FIG 85 VOL I & 51-35-01 VOL II. PAINTED AREAS IN REF TO SRM 51-21-01 VOL II. 2 L 7 3 4F RT A22WE 2008040300221 20080403 00221 NM 2008 4 3 2008UALA01755 1 20080327 A 3350 FU305 FUSE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE POWER SUPPLY BLOWN A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 534UA 25129 1L DOOR EXT EMERGENCY SLIDE LIGHT INOP STA 385 AND AISLE EXIT SIGN FWD SIDE, FWD OF S LAV INOP STA 535. SUPPLEMENTAL DA TA UPDATE, REMOVED AND REPLACED BLOWN FUSE ON EMERGENCY LIGHTS POWER SUPPLY M731. OP CHK'D GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040300225 20080403 00225 NM 2008 4 3 2008UALA01764 1 20080328 A 5320 STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 FUSELAGE STRINGER 16L STRAP CRACKED, FROM BS 348-354. MAJOR REPAIR ACCOMPLISHED, REPLACED INTERCOSTAL WEB STRAP. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040200262 20080402 00262 SO 2008 4 2 CHQA200800058 1 20080325 A 3610 40303925SD O-RING EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BLEED SYSTEM LEAKING A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 573RP 145837 CAE312348 CVG TO GSP - DURING CLIMB, THE CREW RECEIVED A BLEED 2 LEAK MESSAGE ON EICAS. THE AIRCRAFT THEN RETURNED TO FIELD AND L ANDED WITHOUT INCIDENT. MAINTENANCE RAN THE BLEEDS AND INSPECTED FOR LEAKS. A LEAK WAS FOUND AT JOINT 4 AND AFTER REPL ACING THE O-RINGS AT JOINT FOUR THERE WERE NO FURTHER LEAKS FOUND. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008040200271 20080402 00271 WP 2008 4 2 08FDEA01176 1 20080328 A 5514 ALC739281 RUB STRIP DOUG MD10 MD1010F 3022112 WP ZONE 300 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LEFT HORIZONTAL STABILIZER PANEL NR 335 BB IS CHAFED. REMOVED GOUGES ON THE PANEL IAW DC/MD-10 SRM 55-00-01; VOL I. F OUND TO BE WITHIN LIMITS IAW DC/MD-10-10 SRM 55-00-01; VOL I AND UT GAUGE T8225P; CAL DATE 12-19-08. REMOVED AND REPLAC ED WORN THROUGH RUB STRIP IAW DC/MD-10-10 SRM 51-31-01; VOL II; PG 1. 2 L 7 3 4F RT A22WE 2008040200278 20080402 00278 WP 2008 4 2 08FDEA01183 1 20080328 A 5310 ADA36751 FITTING DOUG DC10 DC1010F 3022111 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION MAIN CARGO DOOR LOWER JAM SUPPORT FITTING AFTER INSPECTION FOUND BORE "B", "C" AND "D" OF FITTING NR 7 WITH CORROSION DIAMETER .456 INCH (REF.E.O. FEDEX 8-5230-117635). PERFORMED REWORK HOLE FOR SRM 53-50-00 F IG 17, PERFORMED NDI AND INSTALLED BUSHING FOR SRM 53-50-00 FIG 17 VOL I. 2 L 7 3 4F A22WE 2008040200299 20080402 00299 2008 4 2 HALA0800436 4 20080325 A 3416 4039892904 ALTIMETER BOEING 767 76733A 1385209 NM COCKPIT FAULTED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, FIM 34120801 OFF FLAG IN VIEW ON CAPT'S ALTIMETER SELECTING ALTN AIR DATA SW CLEARS THE FAULT. LATER ON IN DESCENT OFF FLAG RTND FFM FL 380 TO 3500'. REPLACED CAPT'S ALTIMETER IND, OPS CK OK PER AMM 34-13-01. OK FOR SVC. 2 L 7 2 4F RT A1NM 2008040200330 20080402 00330 NM 2008 4 2 GTIA0800040 1 20080317 A 5344 BEARING AIRBUS A319 A319132 3930340 NM L1 DOOR HINGE DISPLACED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 502NK 2433 L1 DOOR UPPER HINGE BEARING IS DISPLACED FROM ITS BORE. REPLACED UPPER AND LOWER L1 DOOR HINGE FITTINGS IAW AMM 52-11-0 0. 2 L 7 2 4F RT A28NM 2008040200350 20080402 00350 2008 4 2 2008UALA01733 4 20080327 A 2565 FLAPPER VALVE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DOOR SLIDE MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 RT UD SLIDE DEPLOYED. SLIDE PARTIALLY DEFLATED AFTER DEPLOYMENT DURING FAA EVACUATION DRILL.. FLAPPER VALVE RELEASED FR OM SLIDE. INSTALLED RT UPPER DECK SLIDE PER MM 25-68-00 REPLACED ASSIST BOTTLE. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200361 20080402 00361 NM 2008 4 2 2008UALA01746 1 20080328 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 FOUND SEAT 1A AFT FLOOR EMERGENCY LIGHT INOP. RECONNECTED LAMP ASSEMBLY OPS CHECK OK. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040300017 20080403 00017 NM 2008 4 3 ABXA080116 1 20080310 A 5230 140T261673 INTERCOSTAL BOEING 767 767281 1385109 NM AFT CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 775AX 22790 CORRODED INTERCOSTAL AT DOOR STA 181 BETWEEN BEAM NR 3 AND NR 4 AFT LOWER CARGO DOOR. REPAIRED AREA IAW B767 SRM 51-70- 11. 2 L 7 2 4F RT A1NM 2008040300039 20080403 00039 2008 4 3 FCPR200800100 3 20080218 A 6114 3AF32C87N2 HUB CESSNA 402 402C 207590R CE PROPELLER CORRODED B FCPR K NONE O OTHER IN INSP/MAINT 1 NM 09 17548 UPON DISASSEMBLY OF PROPELLER, FOUND CORROSION IN HUB BEYOND LIMITS, FOUND HUB HAD BEEN REPAIRED IN AN AREA WHERE NO REP AIR ALLOWED. 1 L 7 2 3O A7CE 2008040300043 20080403 00043 NM 2008 4 3 KCSA081212 1 20080328 A 5312 PRESSURE PANEL BOEING 747 747SR46 1384816 NM WHEEL WELL CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 BELOW MAIN DECK FLOOR UPPER WHEEL WELL PRESSURE WEB SURFACE HAS CORROSION AT BS 1460 LBL-69. 2 L 7 4 4F RT A20WE 2008040300084 20080403 00084 NM 2008 4 3 2008UALA01690 1 20080326 A 3350 276005 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 LEFT OVERWING 2 FORWARD MOST EMERGENCY LIGHTS ARE INOP. REPLACED FUSE IN EPSU. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040300087 20080403 00087 NM 2008 4 3 2008UALA01705 1 20080326 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 616 S17L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 BS 616L FRAME WEB IS CRACKED IN 2 HOLES COMMON TO INBD CHORD ANGLE. UPPER HOLE IS 0.5 INCH BELOW STRINGER S-17L AND LOW ER HOLE IN WEB IS 7 INCH BELOW STRINGER S-17L. MAJOR REPAIR ACCOMPLISHED: REAMED HOLES & ACCMP NDT FOR CRACK CONTAINMEN T. FABRICATED & INSTALLED FREEZE PLUG. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040300093 20080403 00093 NM 2008 4 3 2008UALA01708 1 20080326 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 FWD GALLEY DOOR LOWER AFT CORNER FRAME CRACKED. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGED FRAME SECTION. INSTALLED FRAM E SPLICE REPAIR KIT. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040300095 20080403 00095 NM 2008 4 3 2008UALA01710 1 20080326 A 5753 RIB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT WING TE FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 LT INBD FLAP, MIDDLE FOREFLAP TRACK BEARING SUPPORT HOLE WORN IN RIB. MAJOR REPAIR ACCOMPLISHED: REPLACED DAMAGED RIB. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040300126 20080403 00126 SO 2008 4 3 CHQA200800063 1 20080328 A 3260 8005701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LT MLG FAULTY A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 292SK 145488 CAE311794 FLIGHT 7847, IAD TO YYZ - AFTER TAKEOFF, WHEN THE CREW ATTEMPTED TO RAISE THE LANDING GEAR THEY RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON EICAS AND THE GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. THE FLIGHT RETURNED TO IAD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TESTED THE PROX SENSORS AND FOUND THE AFT WEIGHT ON WHEELS PROX SENS OR ON THE LEFT MAIN LANDING GEAR WOULD NOT TEST. MAINTENANCE REPLACED THE FAULTY PROX SENSOR AND THE AIR/GROUND SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008040300162 20080403 00162 SO 2008 4 3 SWIA200819414 1 20080212 A 2752 BOLT EMB 120 EMB120ER 3260203 SO FLAP ACTUATOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 584SW 120352 RIGHT INBOARD FLAP ACTUATOR ROD END BEARING AND BOLT IS CORRODED, FOUND AT C-CHECK. REPLACED ACTUATOR ROD END AND BOLT IAW CMM 27-50-23. 2 L 7 2 4T RT A31SO 2008040300177 20080403 00177 NM 2008 4 3 HALA0800454 1 20080330 A 2432 32669001 BATTERY BOEING 767 767332 1382001 NM MAIN FAULTY A HALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 13 596HA 23276 ETOPS SIGNIFICANT SYSTEM , EICAS MSG MAIN BATTERY CHARGER DISP BATTERY DISCHARGE LT DID NOT ILLUM. REMOVED AND REPLACED MAIN BATTERY PER AMM 24-31-01, OPS AND SECURITY CHECK GOOD. 2 L 7 2 4F RT A1NM 2008040300186 20080403 00186 NM 2008 4 3 HALA0800464 1 20080327 A 5720 FITTING BOEING 767 767332 1382001 NM LT WING CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 LT WING DRY BAY FRONT SPAR BULKHEAD FITTING AND MATING SURFACE HAS PITTING CORROSION. FITTING REPLACED, MATING SURFACE BLENDED WITHIN LIMITS IAW SRM 57-20-10 REV 76. 2 L 7 2 4F RT A1NM 2008040300227 20080403 00227 NM 2008 4 3 2008UALA01766 1 20080328 A 5241 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 FWD GALLEY DOOR SKIN AT UPPER EDGE OF LOWER HINGE CUTOUT IS BENT AT CRACKED AT RIVET. MAJOR REPAIR ACCOMPLISHED, REMOVE D DAMAGE. INSTALLED FILLER AND DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040400018 20080404 00018 CE 2008 4 4 ZESA030808001 1 20080308 A 5344 6511695204 HINGE CESSNA CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE PAX DOOR CRACKED E ZESA K NONE O OTHER IN INSP/MAINT 1 EA 03 400LX 5033 513 5600453 POST FLIGHT, PILOTS COULD NOT CLOSE AND LATCH MAIN CABIN DOOR. FOUND CABIN DOOR HINGE CRACKED THROUGH ON LOWER ARM. 2 L 7 2 4F 4 F RT A22CE E25EA 2008040400023 20080404 00023 NM 2008 4 4 2008UALA01767 1 20080328 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 FWD GALLEY DOOR AFT SIDE FRAME CRACKED AT 4TH FROM TOP STOP FITTING. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHE D, REMOVED DAMAGE. INSTALLED FRAME REPAIR ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040400025 20080404 00025 EU 2008 4 4 2008UALA01769 1 20080328 A 2700 3945128102 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ELAC FAULTED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 404UA 450 F-CTL ELAC 2 FAULT ON UPPER ECAM. PERFORMED RESET AND RECURRED. ELAC INTERMITTANT, BAD MPS BOARD INTERNAL. REPLACED EL AC 2, ALL TESTS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040400030 20080404 00030 NM 2008 4 4 2008UALA01774 1 20080329 A 2421 GENERATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 548UA 25396 EICAS MSG APU GEN OFF DISPLAYED AND APU GEN OFF LIGHT ILLUM WITH APU RUNNING. APU FIELD OFF LIGHT ON. APU GEN FIELD WO ULD NOT RESET, RESET THEN RETRIPPED. FOUND APU GENERATOR FAILED. REPLACED APU GEN, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040400031 20080404 00031 NM 2008 4 4 2008UALA01775 1 20080330 A 3510 MC1019101 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CAPTAIN'S CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 CAPTAIN'S OXYGEN MASK CRACKED. REPLACED MASK, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040400035 20080404 00035 NM 2008 4 4 2008UALA01780 1 20080329 A 3150 FILTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EQUIPMENT COOL CLOGGED A UALA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 29 597UA 28750 EQUIPMENT COOLING HORN AT DEPARTURE. FOUND EQ COOLING FAN FILTER CLOGGED. REPLACED FILTER, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040400036 20080404 00036 NE 2008 4 4 2008UALA01781 2 20080330 A 7261 M834851270 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 543UA 25698 726718 NR 2 ENGINE HIGH OIL CONSUMPTION EXCEEDS LIMIT. FOUND STARTER DRIVE SHAFT SEAL FAILED. REPLACED STARTER DRIVE SEAL, LE AK CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040400041 20080404 00041 NM 2008 4 4 2008UALA01787 1 20080330 A 2120 FILTER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EQUIPMENT AIR CLOGGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 204UA 28713 EQUIPMENT COOLING AIR FILTER IS CHOKED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040400043 20080404 00043 NE 2008 4 4 2008UALA01789 2 20080329 A 7320 3800035114 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENG SVA FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 551UA 25399 726522 LOWER EICAS R ENG PRI CONT WARNING ILLUM. FOUND NR 2 ENG SVA FAILURE. REPLACED NR 2 ENG SVA 2 L 7 2 4F 4 F RT A2NM E17NE 2008040400045 20080404 00045 NM 2008 4 4 2008UALA01791 1 20080329 A 3350 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 853UA 1688 EMERGENCY LIGHT TEST FAIL. REPLACED EPSU BATTERY EMER R. CKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040400053 20080404 00053 NM 2008 4 4 2008UALA01799 1 20080330 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 4J INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 FOUND SEAT 4J EMERGENCY LIGHT IS INOPERATIVE. REPLACED AFT LIGHT STRIP. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040400058 20080404 00058 NM 2008 4 4 2008UALA01804 1 20080329 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 4F UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 199UA 28717 FOUND 4F EEL LT IS LOOSE. SECURED EEL STRIP. 2 L 7 4 4F 4 F RT A20WE E24NE 2008043000007 20080430 00007 NM 2008 4 30 KCSA081225 1 20080424 A 5412 BULKHEAD BOEING 747 747123 1384873 NM NR 1 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 NR 1 PYLON BULKHEAD HAS A CHAFED AREA AT NAC STA 221.90. 2 L 7 4 4F RT A20WE 2008040800119 20080408 00119 WP 2008 4 8 WRLA2008036 1 20080223 A 5330 SKIN PANEL DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 138WA 47844 DURING C-CHECK INSPECTION FOUND CORROSION ON THE FUSELAGE SKIN PANELS IN AREA OF THE WING TO BODY FAIRINGS AT LT STA 153 1 TO 1821 BETWEEN L-35L AND L-46L AND RT STA 1531 TO 1700 BETWEEN L-43R AND L-46R. REMOVED LWR AFT RUB STRIPS FROM A/C AT AFT WING TO BODY FAIRING AND CORROSION WAS REMOVED AS PER ECRA 242NW-53-DC10-011. 2 L 7 3 4F 4 F A22WE E23EA 2008040800122 20080408 00122 WP 2008 4 8 WRLA2008038 1 20080307 A 5544 PANEL DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE RUDDER DAMAGED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 138WA 47844 DURING C-CHECK INSPECTION FOUND UPPER RUDDER PANEL 376RL 2EA SCREW HOLES DAMAGED. REPAIRED UPPER RUDDER PANEL 376RL SCR EW HOLES PER ECRA 242NW-55-DC10-014, 242NW-55-DC10-015. 2 L 7 3 4F 4 F A22WE E23EA 2008040800124 20080408 00124 NM 2008 4 8 SWAA081762 1 20080401 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER TEE CAP CORRODED AT BS 986, LBL 18 TO RBL 36. REPAIRED TEE CAP PER SR M. 2 L 7 2 4F RT A16WE 2008040800127 20080408 00127 NM 2008 4 8 SWAA081764 1 20080401 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040800128 20080408 00128 NM 2008 4 8 SWAA081763 1 20080401 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040800131 20080408 00131 NM 2008 4 8 SWAA081774 1 20080401 A 5522 65C25746142A SKIN BOEING 737 7375H4 138449D NM RT ELEVATOR DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND RT ELEVATOR UPPER SURFACE DISBONDED. REMOVED AND REPLACED ELEVATOR PER MM. 2 L 7 2 4F RT A16WE 2008040800132 20080408 00132 NM 2008 4 8 SWAA081769 1 20080401 A 3350 3071BPEGPL LIGHT BOEING 737 73776Q 13845AA NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 551WN 30280 DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008040800134 20080408 00134 NM 2008 4 8 SWAA081772 1 20080401 A 5311 6545805 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040800140 20080408 00140 SO 2008 4 8 FDKA200803145 1 20080331 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 837MJ 145367 FDM 6107 MCO-MIA (0925 PHX LCL). BURNING SMELL IN CABIN. MX INSPECTED A/C SYSTEM AND COULD NOT DUPLICATE. 2 L 7 2 4T RT T00011AT 2008040800143 20080408 00143 SO 2008 4 8 C2XA08SH054 1 20080403 A 5751 14569382607 BRACKET EMB 145 EMB145XR 3260214 SO AILERON GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12172 14500864 SHV - DURING C-CHECK THE LEFT HAND DAMPER BRACKET WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008040800145 20080408 00145 SO 2008 4 8 C2XA08SH056 1 20080403 A 5320 14525381009 BUTTSTRAP EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12172 14500864 SHV - DURING C-CHECK THE RIGHT HAND BUTTSTRAP WAS FOUND TO BE CORRODED OUT OF LIMITS BETWEEN FRAMES 65 AND 66. MAINTENA NCE REMOVED THE CORRODED AREA AND PERFORMED A DOUBLER REPAIR IAW EXPRESSJET EC5320-01405. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008040800147 20080408 00147 NM 2008 4 8 PIDA08017 1 20080330 A 3350 1000679 LIGHT BOEING 737 7372K5 138448X NM CABIN INOPERATIVE A PIDA K NONE O OTHER UK UNKNOWN 1 SO 05 249TR 22598 EMERGENCY EXIT LIGHT ABOVE R2 DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ABOVE R2 DOOR IAW 737-200 MM 33-51- 101. 2 L 7 2 4F RT A16WE 2008040400014 20080404 00014 CE 2008 4 4 032108N318CS 1 20080321 A 3260 328 BULB CESSNA 500 550 2076604 CE LIGHT ASSY BLOWN E Z5FA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 63 318CS 5501029 UPON LOWERING THE LANDING GEAR THERE WAS NO RT MAIN GEAR DOWN AND LOCKED GREEN LIGHT. LANDING GEAR ROTARY TEST SELECTED AND RT MAIN GEAR GREEN LIGHT DID NOT TEST. GEAR BLOW DOWN WAS PERFORMED AND AIRCRAFT LANDED UNEVENTFULLY. ALL DOWN AND L OCKED (GREEN LIGHTS) LIGHT BULBS WERE REPLACED THE LANDING GEAR OPERATIONALLY CHECKED SATISFACTORY AND THE AIRCRAFT RETU RNED TO SERVICE. 1 L 7 2 4F A22CE 2008040400044 20080404 00044 NM 2008 4 4 2008UALA01790 1 20080329 A 3510 OXYGEN MASK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE 1ST OFFICER'S LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 F/O OXYGEN MASK LEAKS FROM THE HEADBAND. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040400048 20080404 00048 NM 2008 4 4 2008UALA01794 1 20080329 A 5551 LUG BOEING 737 737322 1384676 NM HORIZONTAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 LT HORIZONTAL STABILIZER CENTER SECTION FRONT SPAR UPPER CLEVIS FWD AND AFT LUGS HAVE EVIDENCE OF FRETTING CORROSION. M AJOR REPAIR: REMOVED CORROSION AND ACCOMPLISHED REPAIR. 2 L 7 2 4F RT A16WE 2008040400056 20080404 00056 NM 2008 4 4 2008UALA01802 1 20080329 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 39ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 FOUND SEAT 39ABC EMERGENCY FLOOR LIGHT INOP. REPLACED LIGHT ASSEMBLY OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040400061 20080404 00061 NE 2008 4 4 2008UALA01810 2 20080331 A 7261 OIL FILTER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 ENGINE CLOGGED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 209UA 30215 222010 ENG OIL FILTER R RIGHT ENGINE PRIMARY OIL FILTER APPROACHES BYPASS (LARGE PRESSURE DIFFERENTIAL ACROSS NORMAL FILTER) WI TH ENGINE RUNNING. REPLACED OIL FILTER & CHANGED OIL. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040400062 20080404 00062 NM 2008 4 4 2008UALA01811 1 20080329 A 2622 SEAL BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FIRE BOTTLE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 204UA 28713 FA REPORTED DOOR 4R WATER FIRE EXTINGUISHER SEAL BROKEN. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008050200069 20080502 00069 NM 2008 5 2 USAA920080881 1 20080424 A 5414 SKIN BOEING 737 7374B7 1384702 NM RT NACELLE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 24893 PIT - MAJOR REPAIR - CRACKED RIGHT PYLON SKIN, NACELLE STATION 224, AT ACCESS OPENING 5828R. REPAIRED RIGHT PYLON SKIN , NACELLE STATION 224, AT ACCESS OPENING 5828R IAW USAIRWAYS TYPICAL REPAIR 54-30-07. 2 L 7 2 4F RT A16WE 2008040400079 20080404 00079 NM 2008 4 4 2008UALA01830 1 20080331 A 2560 MXP21000 SMOKE GOGGLES BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 F/O SMOKE GOGGLES BROKEN. REPLACED FO SMOKE GOGGLES. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040400084 20080404 00084 NM 2008 4 4 2008UALA01835 1 20080401 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY EXIT EEL LIGHT INOP, JUST FWD OF LAV 104 BELOW CLOSET. REPLACED LAMP ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040400104 20080404 00104 GL 2008 4 4 CHQA200800066 2 20080329 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 LEAKING A CHQA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 294SK 17324 10004 145497 CAE311697 FLIGHT 7820, CMH-IAD, AFTER TAKEOFF AT 400 FEET, THE CREW RECEIVED A LAV SMOKE MESSAGE. THE FLIGHT ATTENDANT REPORTED T HAT THERE WAS NO SMOKE PRESENT IN THE LAVATORY OR CABIN. THE FLIGHT RETURNED TO CMH AND LANDED WITHOUT INCIDENT. MAINT ENANCE RAN THE ENGINES AND ISOLATED THE FAULT TO E1. WHEN RUNNING ON THE NUMBER 1 ENGINE THE COCKPIT FILLED WITH SMOKE THAT HAD AN OILY SMELL. NO EXTERNAL LEAKS WERE FOUND AND THE ZERO CARBON SEAL WAS DRY. E1 WAS REPLACED AND THERE WAS N O FURTHER SMOKE OR ODOR. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008040400114 20080404 00114 EU 2008 4 4 08FDEA01249 1 20080402 A 5730 A57260300006 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND CORROSION UNDER STATIC DISCHARGER SUPPORT PLATE, LT WING TIP. REPAIR PERFORMED BY REMOVE OF CORROSION AND INSTALL ING A REPAIR PATCH IAW, RAS /FOK/047/2008 ISS A, APPROVED BY EA 6-5730-117164. 2 L 7 2 4F RT A35EU 2008040400115 20080404 00115 NM 2008 4 4 08FDEA01250 1 20080402 A 5730 ARB2887504 ACCESS PANEL DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 RIGHT WING, LEADING EDGE LOWER SURFACE ACCESS PANEL 619CB INBOARD CORNER CUTOUT AREA FOUND CRACK. REPAIR CARRIED OUT PE R SRM 57-10-00 FIGURE 21 VOLUME I. FABRICATED FILLER AND DOUBLER INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIF IED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008040400121 20080404 00121 NM 2008 4 4 08FDEA01256 1 20080402 A 5713 ARB29324 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 RIGHT WING, AFTER PANEL REMOVAL FOUND LEADING EDGE STRINGER CRACK AT XOS 667. REPAIR CARRIED OUT PER EA 1-5710-120544, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008040400141 20080404 00141 NM 2008 4 4 DL757080442 1 20080327 A 5311 141N121751 FRAME BOEING 757 757232 1384965 NM BS 345 S18L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 659DL 24421 THE STA 345 FUSELAGE FRAME WAS DAMAGED BETWEEN S-18L AND S-20L. THE DAMAGE SECTION OF FRAME WAS REMOVED AND A NEW FRAME SECTION WAS SPLICED IN. 2 L 7 2 4F RT A2NM 2008040400144 20080404 00144 2008 4 4 DLM88080446 4 20080330 A 2340 HANDSET DOUG MD88 MD88 3023688 NM CABIN FIRE A DALA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 972DL 53215 F/A FORWARD HOLD HANDSET SPARKED AND CAUGHT FIRE AT HANDSET CONNECTOR. FOUND WIRING ON HANDSET SHORTED NEAR HANDSET. R EPLACED HANDSET. CKS OK. 2 L 7 2 4F RT A6WE 2008040400147 20080404 00147 NM 2008 4 4 DL76G080450 1 20080331 A 5315 BAC15051007743 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1480 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 155DL 25269 FLOORBEAM CORRODED AT STA 1480 RBL 32 TO BRL 48. BEAM REPAIRED ON NR AVM506152 PER SRM 53-00-51D FIGURE 201. 2 L 7 2 4F RT A1NM 2008040400154 20080404 00154 NM 2008 4 4 DLM90080458 1 20080306 A 5330 SKIN DOUG MD90 MD9030 3023690 NM BS 195 L21R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 C/W ERA 454243-14 REPAIR FUSELAGE SKIN FS 195 L-21R. REPAIR OF DENT AND GOUGE. REMOVED DAMAGED AREA, IAW MD90 SRM 53-3 0-01. INSTALLED REPAIR DOUBLERS AND FILLER, IAW MD90 SRM 53-30-01 FIG 1. 2 L 7 2 4F RT A6WE 2008040400167 20080404 00167 NM 2008 4 4 DLM88080474 1 20080402 A 5347 SEAT TRACK DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV BLEND OUT IS OUT OF LIMIT ON SEAT TRACK X=22 STA Y=485, SEAT TRACK WAS REPAIRED IAW SRM 53-05 FIG 4A. 2 L 7 2 4F RT A6WE 2008040400177 20080404 00177 NM 2008 4 4 DLM88080484 1 20080402 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV CORROSION WAS FOUND ON RIGHT CUSP WEB BETWEEN STA Y=1136 AND 1148. CUSP WEB WAS REPAIRED IAW SRM 51-70-4 FIG 2. 2 L 7 2 4F RT A6WE 2008040400186 20080404 00186 NM 2008 4 4 DLM88080493 1 20080402 A 5320 FITTING DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV A CRACKED WAS FOUND ON FITTING AT STA Y=927 X=-44. FITTING WAS REPLACED IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F RT A6WE 2008040700014 20080407 00014 WP 2008 4 7 AALA200800613 1 20080312 A 2612 ELECTRONIC UNIT DOUG DC9 DC983 3022083 WP FIRE DETECTION INOPERATIVE A AALA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 21 970TW 53620 DFW - INFLIGHT T1507/12MAR - CREW REPORTED AFT CARGO FIRE LIGHT ILLUMINATED. DISCHARGED BOTTLES ONE AND TWO. LANDED WI THOUT INCIDENT. NO EVIDENCE OF FIRE FOUND. REPLACED FIRE EXTINGUISH BOTTLE AND AFT CARGO LINE FILTER. REPLACED AFT CA RGO ELECTRONIC UNIT AND NUMBER TWO SMOKE DETECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008040700025 20080407 00025 WP 2008 4 7 NWAA081359852 1 20080330 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 761NC 47709 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY OVERWING EXIT SIGNS ON ROWS 11, 13, AND 14 WERE INOPERATIVE. TH E POWER SUPPLY/BATTERY PACK WAS REPLACED AND SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A6WE 2008040700026 20080407 00026 NM 2008 4 7 DLM88080504 1 20080402 A 5320 WEB DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV CORROSION WAS FOUND ON WEB BETWEEN STA Y=1155 AND 1212 AND BETWEEN LONG 29 RT AND BOTTOM OF C3 DOOR JAMB. WE B WAS REPLACED IAW DOUGLAS DWG 5936442. 2 L 7 2 4F RT A6WE 2008040700040 20080407 00040 NM 2008 4 7 DLM88080518 1 20080402 A 3397 CONNECTOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE EMERGENCY LIGHT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 977DL 53258 726088 FOUND SEAT 26CD EMERGENCY LIGHT INOP. SECURED PIN INTO CONNECTOR OF LIGHT ASSY, OPS OK. 2 L 7 2 4F 4 F RT A6WE E9NE 2008040800007 20080408 00007 NM 2008 4 8 ZZDA2008080 1 20080315 A 3350 8039251 CRADLE BOEING 717 717200 1383700 NM CABIN DEFECTIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 959AT 55021 EMERGENCY LIGHTS OUT ON ROWS 1-10. REMOVED AND REPLACED BATTERY SUPPLY CRADLE ASSY IAW B717 MM 33-51. 2 L 7 2 4F TR A6WE 2008040800008 20080408 00008 NM 2008 4 8 ZZDA2008081 1 20080317 A 3230 MS21042L4 NUT BOEING 717 717200 1383700 NM RT MLG DOOR LOOSE A ZZDA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SO 37 964AT 55025 ON DESCENT, THE RIGHT MAIN GEAR UNSAFE (RED) ILLUMINATED WITH THE GEAR LEVER UP. FOUND RIGHT MLG DOOR LATCH ROLLER LOOS E. REMOVED AND REPLACED ALL 4 NUTS ON ROLLER AND TIGHTENED AS REQ'D REF M/M 32-34. RETRACTED GEAR, ALL OPS NORMAL REF M/M 32-33. 2 L 7 2 4F TR A6WE 2008040800041 20080408 00041 SO 2008 4 8 C2XA08IA091 1 20080323 A 3260 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 11535 145518 IAH - FLIGHT 2156, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. THE AIRCRAFT RETURNED TO IAH WHER E IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, TEST FLEW WITH NO DISCREPANCIES NOTED, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008040800075 20080408 00075 SO 2008 4 8 FDKA200803135 1 20080327 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 FDM RON TPA (1619 PHX LCL). PAX DOOR WILL NOT CLOSE. MX LUBED THE DOOR ROLLERS AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2008040800089 20080408 00089 SO 2008 4 8 C2XA08RI041 1 20080304 A 3350 602043 SIGN EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16151 145758 RIC - DURING ROUTINE INSPECTION, RIC MX FOUND BOTTOM EXIT SIGN AT SEAT 12C INOPERATIVE. MX REMOVED AND REPLACED SIGN AN D PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2008040800098 20080408 00098 EA 2008 4 8 COMA0860204 1 20080331 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 01 819CA 18030 7415 FLIGHT 5485 - FLAPS FAILED AT 0 DEGREES WHEN SELECTED TO 8 DEGREES DURING APPROACH. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY IN BGR. REMOVED AND REPLACED LT BPSU. ALSO COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FO LLOW-UP MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 2008040800102 20080408 00102 SO 2008 4 8 C2XA08IA097 1 20080326 A 3231 22250100003 SOLENOID VALVE EMB 145 EMB145EP 3260221 SO NLG INOPERATIVE A C2XA O OTHER O OTHER CL CLIMB 1 SW 27 16927 12820 4895 145006 IAH - FLIGHT 2638, THE CREW REPORTED A NOISE COMING FROM UNDER THE CENTER CONSOLE DURING FLIGHT, AND THE CREW SUSPECTED THE NOSE GEAR DOORS TO BE OPEN. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOOR SOLENOID VALVE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. 2 L 7 2 4F RT T00011AT 2008040800123 20080408 00123 WP 2008 4 8 WRLA2008039 1 20080313 A 5730 SKIN DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE RT WING CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 138WA 47844 DURING C-CHECK INSPECTION FOUND RIGHT WING UPPER SURFACE AT REAR SPAR, FROM XORS 264 TO XORS 480 SKIN CORRODED AT SEVERA L PLACES. REPAIRED RIGHT WING SURFACE AT REAR SPAR FROM XORS 264 - XORS 480 AT AREAS OF CORROSION PER ECRA 242NW-57-DC1 0-017. 2 L 7 3 4F 4 F A22WE E23EA 2008040800137 20080408 00137 SO 2008 4 8 C2XA08ON108 1 20080330 A 2810 2810051104 VALVE EMB 145 EMB145XR 3260214 SO RT WING LEAKING A C2XA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 27 27190 14500934 FLT 220 - ONT - FLIGHT CREW REPORTED FUEL LEAKING OUT OF RIGHT WING. MX REMOVED AND REPLACED RT OUTBOARD WING VENT VALV E. OPERATIONALLY AND LEAK CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008040800154 20080408 00154 NM 2008 4 8 SWAA081780 1 20080402 A 3350 1619 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 411WN 29821 DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008040800159 20080408 00159 EA 2008 4 8 COMA0860205 1 20080401 A 3297 864202 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 916CA 7014 FLIGHT 9649 - EN ROUTE FROM YUL TO PVD RECEIVED GEAR DISAGREE WARNING AT FLT LEVEL 280, WITH RED NOSE GEAR INDICATION. EMERGENCY DECLARED, PERFORMED MANUAL RELEASE TO LANDING GEAR. AIRCRAFT LANDED SAFELY IN PVD. REMOVED AND REPLACED NLG RIGHT DOWNLOCK PROX SENSOR WIRE HARNESS. 2 L 7 2 4F RT A21EA 2008040800161 20080408 00161 NE 2008 4 8 COMA0860207 2 20080402 A 7320 5047T75G01 TUBE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30068 NE RT ENGINE CRACKED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 595SW 7292 807043 FLIGHT 5451 - EN ROUTE FROM YYZ TO CVG, NR 2 ENGINE LOW FUEL PRESSURE CAUTION MESSAGE. ENGINE REMAINED AT 56%, 70 DEG O IL TEMP, 50 PSI OIL PRESS, AND NO RESPONSE FROM THRUST LEVER. PERFORMED IFSD ON NR 2 ENGINE, EMERGENCY DECLARED AND A/C DIVERTED TO CMH AND LANDED SAFELY. INSPECTED ENGINE, FOUND P3 TUBE ASSY CRACKED AT FUEL CONTROL. REMOVED AND REPLACED P3 TUBE ASSY. 2 L 7 2 4F 4 F RT A21EA E15NE 2008040800163 20080408 00163 2008 4 8 C2XA08RI044 4 20080330 A 3418 0020BN4 COMPUTER EMB 145 EMB145LR 3260212 SO STALL WARNING FAULTY A C2XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 14998 23296 14714 145302 FLIGHT 2642 - EWR - CREW REPORTED SPS ADVANCE MESSAGE ON EICAS IN CRUISE. CREW PERFORMED AIR RETURN AND LANDED UNEVENTF ULLY. EWR MX REMOVED AND REPLACED STALL PROTECTION COMPUTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008040800164 20080408 00164 2008 4 8 C2XA08RI045 4 20080329 A 3418 0861DT5 SENSOR EMB 145 EMB145LR 3260212 SO STALL WARNING FAULTY A C2XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 14998 24676 16304 145302 FLIGHT 1231 - EWR - CREW REPORTED SPS ADV MESSAGE ON EICAS IN CRUISE. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY . EWR MX REMOVED AND REPLACED ANGLE OF ATTACK SENSORS AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPRO VED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008040800165 20080408 00165 2008 4 8 C2XA08RI046 4 20080329 A 3418 0861DT5 SENSOR EMB 145 EMB145LR 3260212 SO STALL WARNING FAULTY A C2XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 14998 24676 16304 145302 FLIGHT 1231 - EWR - CREW REPORTED SPS ADV MESSAGE ON EICAS IN CRUISE. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY . EWR MX REMOVED AND REPLACED ANGLE OF ATTACK SENSORS AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPRO VED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008040800166 20080408 00166 SO 2008 4 8 C2XA08RI047 1 20080313 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG DEFECTIVE A C2XA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 27 48901 145501 FLIGHT 3156 - EWR - CREW REPORTED BANGING NOISE COMING FROM NOSE LANDING GEAR AREA DURING TAXIING. CREW RETURNED TO GAT E. EWR MX REMOVED AND REPLACED UPLOCK BOX PROXIMITY SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008040800168 20080408 00168 NM 2008 4 8 SWAA081791 1 20080403 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 246LV 32507 L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008040800174 20080408 00174 NM 2008 4 8 SWAA081797 1 20080403 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 920, STR 24L AND STR 23L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008040800175 20080408 00175 NM 2008 4 8 SWAA081798 1 20080403 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 831, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008040800176 20080408 00176 NM 2008 4 8 SWAA081800 1 20080403 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008040800178 20080408 00178 NM 2008 4 8 SWAA081809 1 20080403 A 5312 6545409 PRESSURE PANEL BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, LBL 31. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008040800179 20080408 00179 NM 2008 4 8 SWAA081810 1 20080403 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040800180 20080408 00180 NM 2008 4 8 SWAA081812 1 20080403 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 460, BL 0. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008040800181 20080408 00181 NM 2008 4 8 SWAA081811 1 20080403 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008040400060 20080404 00060 NM 2008 4 4 2008UALA01809 1 20080330 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE SEAT 41H OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 SEAT MOUNTED EMERGENCY LIGHT AT SEAT 41H RIPPED OFF. SUPPLEMENTAL DATA UPDATE, REPLACED LIGHT ASSY. CHECK OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040400065 20080404 00065 NM 2008 4 4 2008UALA01814 1 20080331 A 2560 MXP21000 SMOKE GOGGLES BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CAPTAIN'S DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 CAPT SMOKE GOGGLE DAMAGED. REPLACED SMOKE GOOGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040400070 20080404 00070 NM 2008 4 4 2008UALA01820 1 20080331 A 5320 STIFFENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 246 FLOORBEAM CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 BS 246 FLOORBEAM AT APPROX RBL 16 HAS A CRACKED VERTICAL STIFFENER. MAJOR REPAIR ACCOMPLISHED, REMOVED AND REPLACED ST IFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031000271 20080310 00271 NM 2008 3 10 AALA200800394 1 20080223 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 177AN 32396 DFW - EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008031000277 20080310 00277 NM 2008 3 10 KCSA081145 1 20080306 A 5320 WEB BOEING 747 747209B 138489B NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 SEAT TRACK SUPPORT WEB AT LBL-44 STA-1840 TO STA-1860 IS DAMAGED. 2 L 7 4 4F RT A20WE 2008031000278 20080310 00278 WP 2008 3 10 AALA200800387 1 20080222 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 289AA 49301 LGA EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 20 TO 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEA D SEAT ROWS 20 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031000286 20080310 00286 NM 2008 3 10 AALA200800405 1 20080224 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 DFW - EMERGENCY LIGHT AT SEAT 34G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 34G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008030700321 20080307 00321 NM 2008 3 7 DHL2008752570 1 20080204 A 5754 STRUCTURE BOEING 727 727223 1384074 NM NR 5 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 752DH 22466 RT WING NR 5 L/E SLAT WING L/E I/B BULKSEAL HAS SURFACE CRACKED. REMOVED FASTENERS AT RT WING NR 5 L/E SLAT WING L/E I/ B BULK SEAL IAW B727 SRM 51-30-2. STOP DRILLED 0.250 AT END OF CRACK IAW B727 SRM 51-10-1. FABRICATED DOUBLER REPAIR A T L/E SLAT MATERIAL USED 2024T3 .063 PO NR 9006288 DIMENSION 7 INCH BY 8.5 INCH IAW B727 SRM 57-30-4 FIG 11 AND B727 SRM 57-30-2 FIG 3. TREATED AND PRIMED DOUBLER REPAIR AND AREA IAW B727 SRM 51-10-2. INSTALLED NEW DOUBLER REPAIR AND REIN STALLED FASTENERS IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008030700333 20080307 00333 NM 2008 3 7 DLM90080299 1 20080301 A 2730 272010002 SHUTOFF VALVE DOUG MD90 MD9030 3023690 NM ELEVATORS FAILED A DALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SO 27 916DN 53396 ON CLIMB-OUT FROM SLC THRU 23000, AIRCRAFT BEGAN VERTICLE OSCILLATIONS MORE THAN USUAL. AUTOPILOT WAS DISCONNECTED AND ELEV FEEL WAS STIFF. NO COCKPIT INDICATIONS TO IND ELEV IN MANUAL CONTROL. AIRCRAFT FLOWN MANUALLY TO LAS. T/S PER TS M ACS FAULT MOSV1 PRM REMOVED AND REPLACED ELEV POWER MOTOR SHUT OFF VALVE PER AMM. 2 L 7 2 4F RT A6WE 2008030700348 20080307 00348 NM 2008 3 7 2008UALA01062 1 20080227 A 5241 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 FORWARD GALLEY DOOR AFT FRAME CRACKED AT 4TH FROM TOP STOP FITTING. MAJOR REPAIR: REMOVED DAMAGE. INSTALLED REPAIR ANGL E. 2 L 7 2 4F 4 F RT A16WE E21EU 2008030700359 20080307 00359 EU 2008 3 7 2008UALA00719 1 20080208 A 2700 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE UNKNOWN A UALA O OTHER W INADEQUATE Q C LD LANDING 1 WP 29 449UA 851 DEBRIEFED WITH FLT CREW, CAPT WAS FLYING AIRCRAFT AND AT TOUCH DOWN (MAIN LANDING GEAR WAS ON RUNWAY) CAPT RELAXED STICK TO NEUTRAL AND THEN AIRCRAFT NOSE AGGRESSIVELY PITCHED UP. UNKNOWN (UNABLE TO DUPLICATE- POST FLIGHT). NO INFO ON PFR , NO HISTORY ON PREVIOUS FLIGHTS, AFS TEST OK, ADR 1, 2, 3, OK. EFCS 1, 2 TEST OK, LAND TEST OK, ELAC1 REPLACED 1-07-08 .AOA TEST OK ALL USING CF DS TEST. COULD NOT DUPLICATE, TEST FLIGHT = REQUEST DIAGNOSTICS AS FOLLOWS: AT LEAST 3 LANDI NGS (MAY BE TOUCH & GO) WITH CAPT IN CONTROL, F/O IN CONTROL AND FULL AP 1+2 AUTO LAND TO DETERMINE IF FAULT IS PRESENT. RESULTS: ALL CHECKS INCLUDING 3 LANDINGS WERE SATISFACTORY. NO PITCH-UPS NOTICED. SUCCESSFUL TEST FLIGHT - NO REPEA 2 L 7 2 4F 4 F RT A28NM E40NE 2008030700396 20080307 00396 NM 2008 3 7 SWAA081119 1 20080227 A 5310 6947960 DOOR FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 3 DOOR STOP. REMOVED AND REPLACED FRAME PER BOEING DRAWING. 2 L 7 2 4F RT A16WE 2008030700401 20080307 00401 NM 2008 3 7 SWAA081109 1 20080227 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED HC2 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008031000006 20080310 00006 EU 2008 3 10 MALA080032 1 20080222 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 634-650 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 429XJ 340B429 FUSELAGE SKIN UNDER CARGO DOOR HAS 2 DENTS BETWEEN FS 634.5 AND FS 650.5 AND BETWEEN S.L. 1524-1528 FROM BAGGAGE CART. COMPLETED REPAIR TO SKIN DENTS IAW EO S53532. COMPLETED REPAIRS TO FRAMES 640 AND 649 IAW EO S53532. 2 L 7 2 4T RT A52EU 2008031000019 20080310 00019 NM 2008 3 10 08FDEA00669 1 20080229 A 5310 143N832853 CREASE BEAM BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 CREASE BEAM BY L2 DOOR, FROM STATION 660 TO 740, LBL60, WL 208 HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION FROM C REASE BEAM, L= 2", W= 1", D= 100 PERCENT, EXFOLIATED COMPLETELY THROUGH, BEYOND SRM 53-30-15, FIG 101, DETAIL IV LIMITS. REMOVED AND REPLACED INNER CHORD, PN: 143N8328-53 (BEAM) IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008040800182 20080408 00182 2008 4 8 SWAA081801 4 20080403 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008040800184 20080408 00184 NM 2008 4 8 SWAA081808 1 20080403 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 792, RBL 13. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040800187 20080408 00187 NM 2008 4 8 SWAA081806 1 20080403 A 5311 6546543 BELTFRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 663, STR 3L. REPAIRED BELTFRAME PER SRM. 2 L 7 2 4F RT A16WE 2008040800194 20080408 00194 SO 2008 4 8 C2XA08IA099 1 20080331 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13997 145298 MCI- DURING MAINTENANCE INSPECTION THE LOWER GALLEY EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS A PPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008040800195 20080408 00195 SO 2008 4 8 C2XA08IA102 1 20080401 A 4920 23080013A STARTER GEN EMB 135 EMB135LR 3260305 SO APU INOPERATIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 12519 5905 367 145366 FLT 2632, THE CREW REPORTED THAT THE APU FAILED ACCOMPANIED BY A BURNING ODOR. THE AIRCRAFT LANDED AT IAH WITHOUT INCID ENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE APU ON MEL 49-00-00 CAT C. MAINTENANCE REMOVED AND REPLACED THE APU STARTER GENERATOR, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008040800197 20080408 00197 SO 2008 4 8 C2XA08SH057 1 20080406 A 2742 14525021407 ATTACH BRACKET EMB 145 EMB145LR 3260212 SO HORIZ STAB DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV - DURING C-CHECK LT HORIZONTAL STABILIZER ACTUATOR ATTACHMENT POINT O/B LUG O/B HAT BUSHING HOLE IS ELONGATED. MX R EMOVED AND REPLACED LT UPPER HORIZONTAL STAB ACTUATOR ATTACHMENT BRACKET IAW EMB 145 SRM 51-40-04 (DRILLING), 51-20-01 ( SEALING), SRM 51-40-02 AND AMM 20-10-01 (BOLT TORQUE). NEW ATTACH FITTING INSTALLED WITH NEW HAT BUSHING LUGS. 2 L 7 2 4T RT T00011AT 2008040800201 20080408 00201 SO 2008 4 8 C2XA08SH061 1 20080407 A 5320 14532637401 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12136 145719 SHV - DURING C-CHECK CENTER OMEGA BEAM AT PREVIOUS REPAIR HAS CORROSION FR 24-25. MX REMOVED AND REPLACED PREVIOUS REPA IR AT CENTER OMEGA BEAM BETWEEN FR 24-25 IAW EMB 145 XR SRM 53-00-10 FIG 203 DET A. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008040800206 20080408 00206 NM 2008 4 8 SWAA081817 1 20080404 A 2560 P2070003001 FLASHLIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 238WN 34713 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2008040800207 20080408 00207 NM 2008 4 8 SWAA081818 1 20080404 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 285WN 32536 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008040800210 20080408 00210 NM 2008 4 8 SWAA081819 1 20080406 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 514, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008040900005 20080409 00005 EU 2008 4 9 TRBA2008036 1 20080401 A 3320 S2521658700000 PSU AEROSP ATR72 ATR72212 8680945 EU CABIN LIGHTS FAILED A TRBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 29 451AT 451 SMOKE FROM PASSENGER READING LIGHT AT 5AB. FLIGHT DIVERTED TO MIA FROM FLL. REMOVED AND REPLACED PSU (PASSENGER SERVIC E UNIT) AT SEAT 5AB. PERFORMED OPT CK IAW JIC NR 25-23-22 RAI 10000. 2 H 7 2 4T RT A53EU 2008040900007 20080409 00007 NM 2008 4 9 F3LA200800134 1 20080401 A 3350 321430 BATTERY AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE EMERGENCY LIGHTS INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 931FR 571 2253 DURING HEAVY SERVICE CHECK INSPECTION REPORTED RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 33-51-38-420-052. FOLLOWING INSTALLAT ION THE SYSTEM WAS TESTED AND CHECKED OKAY. 2 L 7 2 4F 4 F RT A28NM 2008040900010 20080409 00010 NE 2008 4 9 HALA0800477 2 20080331 A 7230 FAN BLADE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE LT ENGINE DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, LT ENG FAN BLADE NR 25 HAS NICK. REPAIRED PER AMM TASK 72-31-02. EDDY CURRENT GOOD. NO CRAC KS IND NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040900011 20080409 00011 NM 2008 4 9 HALA0800478 1 20080331 A 2897 WIRE BOEING 767 76733A 1385209 NM FUEL QTY IND OPEN A HALA O OTHER P NO WARNING INDICATION CR CRUISE 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, PER VERBAL FROM FLIGHT CREW: CENTER FUEL TANK AND TOTAL FUEL QTY INDICATORS MOMENTARILY WENT B LANK. PERFORMED FUEL QTY PROCESSOR BITE PER FIM 28-41-00 FIG 104 FAULTED "LAST FLIGHT LEG" CENTER HI Z WIRE OPEN AT SPA R A09 TO PROCESSOR A03-FAULT CLEARED CHECKS NORMAL. PERFORMED FQI TEST PER AMM 28-41-00, SYSTEM CHECKS NML. 2 L 7 2 4F RT A1NM 2008040900012 20080409 00012 NE 2008 4 9 HALA0800479 2 20080401 A 7321 EEC BOEING 767 76733A 1385209 NM GE CF680 CF680A2 NE LT ENGINE MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM, LEFT ENG CONTROL EICAS ILLUMIN BTB. ACCOMP FIM 73-21-00 FIG 112. NO FAULTS NOTED. RESET LEF T ENG EEC DISCREDE C/B. ACCOMP GROUND RUN UP OF LEFT ENG, OPS CK GOOD. EICAS MSG CLEARED. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E13NE 2008040900017 20080409 00017 EA 2008 4 9 CHQA200800068 1 20080330 A 4990 1603662 OIL COOLER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE APU CLOGGED A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 466CA 1716 1716 7627 GEE873331 FLIGHT 5756, IAH TO SDF - DURING CRUISE, THE CREW RECEIVED AN APU HIGH OIL TEMPERATURE MESSAGE ON EICAS. THE FLIGHT DIV ERTED TO LIT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU AND VERIFIED THE OIL WAS SERVICED TO THE CORREC T LEVEL. THE CONNECTOR TO THE HIGH OIL TEMPERATURE BULB WAS CLEANED AND RESECURED. THE APU WAS RUN WITHOUT FURTHER DEF ECTS. ON THE 31ST,THE OIL COOLER WAS REPLACED DUE TO INTERNAL CLOGGING AND LEAKAGE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008040900018 20080409 00018 EA 2008 4 9 CHQA200800069 1 20080331 A 5610 NP13932113 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE COCKPIT CRACKED A CHQA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 11 656BR 14686 14686 7485 GEE872933 FLIGHT 5598, DFW TO CLE, DURING CRUISE, THE FLIGHT CREW REPORTED THAT THE LEFT WINDSHIELD CRACKED. THE FLIGHT DIVERTED TO CMH AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT WINDSHIELD AND RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008040900019 20080409 00019 SO 2008 4 9 CHQA200800070 1 20080401 A 3310 12315660401 HOLDER EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL COCKPIT CHAFED A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 843RP 145599 CAE312124 FLIGHT 6217, CAK TO CVG. WHILE CRUISING AT FL200, THE FLIGHT CREW NOTICED THE COCKPIT BEGAN TO FILL WITH SMOKE. THE PR OPER QRH CHECKLISTS WERE FOLLOWED AND THE FIRST OFFICER NOTICED THE SMOKE WAS COMING FROM HIS CHART HOLDER. AFTER TURNI NG OFF THE CHART HOLDER LIGHT, THE SMOKE BEGAN CLEARING. THE FLIGHT LANDED IN CVG WITHOUT INCIDENT. MAINTENANCE INSPEC TED THE CHART HOLDER AND FOUND THE WIRES GOING TO THE LIGHT WERE CHAFED AND SHOWED BURN MARKS. THE CHART HOLDER WAS REP LACED AND NO FURTHER DEFECTS WERE NOTED. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008040900020 20080409 00020 GL 2008 4 9 CHQA200800071 2 20080401 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 MAKING METAL A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 11 566RP 14394 4449 145691 CAE312032 FLIGHT 6221, CHA TO CVG - JUST OUTSIDE THE OUTER MARKER THE FLIGHT CREW SMELLED SMOKE AND BEGAN RUNNING THROUGH THE QRH CHECKLISTS. ONCE CLEARED TO LAND A LAV SMOKE EICAS MESSAGE WAS DISPLAYED. AT THE SAME TIME THE NUMBER 1 ENGINE WAS TEM PING OUT. THE THRUST WAS REDUCED TO 50 PERCENT TO LOWER THE TEMP. THE ENGINE TEMPERATURE REMAINED IN THE RED AND THE T HROTTLE WAS REDUCED TO IDLE. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND IT WAS DECIDED TO REPLACE THE NUMBER 1 ENGINE. AFTER REPLACING THE NUMBER 1 ENGINE, THERE WERE NO FURTHER DEFECTS NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008040900022 20080409 00022 WP 2008 4 9 NWAA081379863 1 20080402 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 772NC 47774 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WERE IN OPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE EMERGENCY LIGHTS IN THE TAIL COMPARTMENT CATWALK. OPERATIONAL CH ECK WAS GOOD. 2 L 7 2 4F RT A6WE 2008040900029 20080409 00029 WP 2008 4 9 AALA200800647 1 20080315 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7549A 53031 DFW - EMERGENCY LIGHT AT SEAT 7D LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F A6WE 2008040900030 20080409 00030 2008 4 9 AALA200800646 4 20080315 A 2565 D30654122 SLIDE BOEING 757 757223 1384957 NM L1 DOOR FAILED A AALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 612AA 24488 MIA - LEFT NUMBER ONE DOOR SLIDE PARTICIALLY DEPLOYED DUE TO FLIGHT ATTENDANT AND CREW INTERVENTION. REPLACED SLIDE FOR LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900031 20080409 00031 NM 2008 4 9 AALA200800660 1 20080316 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 2D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 2D. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900037 20080409 00037 NM 2008 4 9 AALA200800649 1 20080315 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 612AA 24488 MIA - EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A2NM 2008040900040 20080409 00040 NM 2008 4 9 AALA200800641 1 20080314 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 674AN 29424 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900041 20080409 00041 NM 2008 4 9 AALA200800654 1 20080316 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 785AN 30005 DFW - EMERGENCY LIGHT AT SEAT 37G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 37G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900043 20080409 00043 NM 2008 4 9 AALA200800624 1 20080313 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900045 20080409 00045 NM 2008 4 9 AALA200800626 1 20080313 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT AT L1 DOOR STOWAGE COMPARTMENT IS DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT L1 DOOR STOWAGE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900046 20080409 00046 NM 2008 4 9 AALA200800627 1 20080313 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900047 20080409 00047 NM 2008 4 9 AALA200800656 1 20080316 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 DFW - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900055 20080409 00055 NM 2008 4 9 AALA200800635 1 20080313 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 390AA 27450 MIA - EMERGENCY LIGHT AT SEAT 38B LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 38B. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008040400164 20080404 00164 NM 2008 4 4 DL76G080470 1 20080401 A 5315 BAC1505101498 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 287 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 155DL 25269 CABIN FLOORBEAM STA 287 RBL 54-64 UPPER CORD FOUND CORRODED. REPAIRED ON NR AVM508026 PER SRM 53-00-51D FIGURE 201. 2 L 7 2 4F RT A1NM 2008040400168 20080404 00168 NM 2008 4 4 DLM88080475 1 20080402 A 5340 ATTACH BRACKET DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMY EXFOLIATION CORROSION WAS FOUND ON ATTACH BRACKET STA Y=198 AND X=-55 FWD WET AREA. BRACKET WAS REPLACED IAW DOUGLAS DWG 9436534. 2 L 7 2 4F RT A6WE 2008040400175 20080404 00175 NM 2008 4 4 DLM88080482 1 20080402 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV CORROSION WAS FOUND ON RIGHT CUSP WEB AT STA Y=551. CUSP WEB WAS REPAIRED IAW ER/A 398191-14MA. 2 L 7 2 4F RT A6WE 2008040700006 20080407 00006 NM 2008 4 7 AALA200800607 1 20080312 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AA 24617 DFW - EMERGENCY EXIT IDENTIFIER LIGHT AT AFT OF RIGHT AFT PASSENGER DOOR AT L00762 IS BROKEN. REPLACED LIGHT FOR EMERGE NCY EXIT IDENTIFIER LIGHT AT AFT OF RIGHT AFT PASSENGER DOOR AT L00762. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040700024 20080407 00024 NM 2008 4 7 NWAA081365527 1 20080401 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 527US 23842 DURING OVERNIGHT LINE CHECK, FOUND FLOOR TRACK EMERGENCY LIGHTS ROW 33 TO 40 INOP. MAINTENANCE REMOVED AND REPLACED POW ER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 2008040700034 20080407 00034 NM 2008 4 7 DLM88080512 1 20080402 A 5340 ATTACH FITTING DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV A CRACK WAS FOUND ON CLIP AT STA Y=1437 BETWEEN LONGERON 1 AND 2 LT. CLIP WAS REPLACED IAW SRM 51-30-5. 2 L 7 2 4F RT A6WE 2008040700035 20080407 00035 NM 2008 4 7 DLM88080513 1 20080402 A 5320 CHANNEL DOUG MD88 MD88 3023688 NM BS 1354 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV PITTING CORROSION WAS FOUND ON CHANNEL AT STA Y=1354 AND X=-32 AT RT AFT LAVATORY. CHANNEL WAS REPLACED IAW DOUGLAS DWG 5925005. 2 L 7 2 4F RT A6WE 2008040800010 20080408 00010 NM 2008 4 8 WRLA2008031 1 20080320 A 5753 NRC67622 FLAP DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE RT WING DEBONDED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 48407 DURING C-CHECK INSPECTION FOUND RIGHT WING INBOARD FLAP DISBONDED. REF EGAT NRC U07003. REPAIRED PER ENGINEERING INSTRU CTION NO.W2008A57B-202 REV.00 2 L 7 3 4F 4 F RT A22WE E24NE 2008040800033 20080408 00033 NE 2008 4 8 WRNA200800006 2 20080316 A 7200 CF650C2 ENGINE AIRBUS 300 A300B4203 3930306 EU GE CF6 CF650C2 30018 NE NR 1 FAILED A WRNA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 05 505TA 84878 4303 271 517425 AFTER TAKEOFF FROM MFM, CLIMBING THROUGH 15,000 FEET A LOUD EXPLOSION WAS HEARD FROM NR 1 ENGINE FOLLOWED BY SEVERE VIBR ATION, ENGINE WAS RETARDED TO IDLE POWER, VIBRATION CONTINUED FOLLOWED BY LOW OIL PRESS LIGHT AND EGT INCREASE TO 963 DE GREES C. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO FIELD AND MADE A SAFE LANDING. 2 L 7 2 4F 4 F RT A35EU E23EA 2008040800034 20080408 00034 EA 2008 4 8 COMA0860193 1 20080323 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 915CA 19167 7013 FLIGHT 5532 - RECEIVED FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED RIGHT BPSU . NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008040800036 20080408 00036 EA 2008 4 8 COMA0860195 1 20080325 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 934CA 33024 7042 CRACK ON REAR PRESSURE BULKHEAD WEB AT LBL 27.50 ABOVE DOOR TRACK. REPAIRED AFT PRESSURE WEB AT LBL 27.50 IAW REO 601R- 53-61-1541. 2 L 7 2 4F RT A21EA 2008040800038 20080408 00038 GL 2008 4 8 C2XA08IA089 2 20080324 A 7200 AE3007A13 ENGINE EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL RIGHT LEAKING A C2XA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 27 17524 16761 6169 145399 CAE311393 IAH - FLIGHT 2725, THE CREW REPORTED SMOKE IN THE LAV AND CARGO COMPARTMENT ON LANDING. THE CREW DISCHARGED BOTH FIRE B OTTLES, AND THE AIRCRAFT WAS EVACUATED. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE NUMBER TWO ENG INE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008040800042 20080408 00042 SO 2008 4 8 FDKA200803122 1 20080323 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN CABIN DOOR OUT OF RIG A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 852MJ 145567 FDM 6035 CVG-EYW (0700 PHX LCL). MAIN CABIN DOOR HARD TO CLOSE. MX RE-RIGGED DOOR. 2 L 7 2 4T RT T00011AT 2008040800058 20080408 00058 NM 2008 4 8 HNAA0800112 1 20080327 A 3350 OL3071BPEGPL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN DEFECTIVE A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 938HA 152 EXIT LIGHT UNDER EMERGENCY EXIT DOOR IS DIM. REMOVED AND REPLACED EXIT LIGHT BULB, OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2008040800116 20080408 00116 NM 2008 4 8 SWAA081754 1 20080330 A 5312 6546568 BULKHEAD BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 761RR 27875 DURING SCHEDULED 8Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CORRODED AT BS 1016, RBL 4 TO RBL 13. REPAIRED WEB PER ER. 2 L 7 2 4F RT A16WE 2008040800133 20080408 00133 NM 2008 4 8 SWAA081773 1 20080401 A 5311 65C22908 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040800173 20080408 00173 NM 2008 4 8 SWAA081796 1 20080403 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 496WN 32478 DURING SCHEDULED HC1 CHECK, LEFT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F RT A16WE 2008040800188 20080408 00188 NM 2008 4 8 SWAA081807 1 20080403 A 5311 6558280 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040800211 20080408 00211 NM 2008 4 8 SWAA081830 1 20080406 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 383, STR 28R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008040800212 20080408 00212 NM 2008 4 8 SWAA081831 1 20080403 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 444WN 29839 DURING SCHEDULED MV1 CHECK, FOUND EEPLS LIGHT INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008040800213 20080408 00213 NM 2008 4 8 SWAA081820 1 20080405 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 457WN 33856 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008040900025 20080409 00025 NM 2008 4 9 AALA200800661 1 20080316 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 608AA 27446 DFW - EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900066 20080409 00066 NM 2008 4 9 HALA0800489 1 20080403 A 3150 WARNING LIGHT BOEING 767 7673CB 1385187 NM LT GENERATOR FALSE INDICATION A HALA O OTHER N FALSE WARNING CR CRUISE 1 WP 13 592HA 33468 ETOPS SIGNIFICANT SYSTEM, GEN FIELD OFF LIGHT ILLUMINATED, LEFT ENGINE. RAN NR 1 ENG AT IDLE. CYCLED LEFT GEN. GENERA TOR FIELD LIGHT OFF, EXTINGUISHED. FREQ AND VOLTS OK. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008040900071 20080409 00071 NM 2008 4 9 HALA0800494 1 20080402 A 5314 KEELBEAM BOEING 767 76733A 1385209 NM BS 960 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 587HA 33421 LEVEL 1 CORROSION ON THE INTER-PANEL TEE SECTION P/N 1458623-3 C LWR KEEL BEAM STA 960 RBL 9.5 TO LBL 9.5. CORROSION AR OUND ANCHOR NUT FASTENERS. TEE SECTION REPLACED. 2 L 7 2 4F RT A1NM 2008040900083 20080409 00083 EU 2008 4 9 08FDEA01282 1 20080403 A 5330 A53974427202 DOUBLER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CORROSION ON ANTENNA DOUBLER NEAR C 65, P56-57 LT. REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CRACK AND FLA P PENNING IAW RAS/EFW/9000031/2008 ISS A, APPROVED BY EA 6-5317-117175. 2 L 7 2 4F RT A35EU 2008040900084 20080409 00084 NM 2008 4 9 HALA0800486 1 20080403 A 4997 CIRCUIT BREAKER BOEING 767 76733A 1385209 NM APU TRIPPED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM, EICAS MESSAGE APU FAULT APU FAILED TO START APU DOOR DISPLAYED. FOUND APU INLET DOOR C/B TRIP PED, RESET C/B INSPECTED INLET DOOR AND ACTUATOR FOR BINDING, NONE NOTED, STARTED APU THREE TIMES. OPS CHECK GOOD EACH TIME, PER FIM 29-11-00 PG 103. 2 L 7 2 4F RT A1NM 2008040900090 20080409 00090 NM 2008 4 9 08FDEA01283 1 20080403 A 5330 65236887 SKIN BOEING 727 727225 1384077 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 DENT LT AFT FUSELAGE STA 1350 STR 17L, FOUND OUT OF LIMITS IAW SRM, EVALUATED DENT AND FOUND OUT OF LIMITS. CUT OUT DAM AGED AREA DIM 1 1/2 BY 1 INCH AND FABRICATED REPAIRED DOUBLER IAW SRM 54-30-3 FIG7. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER AT FUSELAGE STA 1350, STR 17L IAW SRM 54 30-3 FIG 7 AND 51-30-2. 2 L 7 3 4F A3WE 2008040900095 20080409 00095 EU 2008 4 9 08FDEA01288 1 20080403 A 5755 A57771010006 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 3 SPOILER LT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 SPOILER NR 3 LT WAS DAMAGED (CRACKED AND DELAMINATED) AT INBOARD AND OUTBOARD END DURING DELIVERY. REPAIR PERFORMED BY REMOVING OF DAMAGED TOP SKIN PLIES AND REPAIR AS PER SRM 57-72-11 FIG 205, APPROVED BYB RAS/BABRE/7009341/2008 ISS A AND EA 6-5772-117182. 2 L 7 2 4F RT A35EU 2008040900096 20080409 00096 NM 2008 4 9 08FDEA01290 1 20080403 A 5753 SKIN BOEING 727 727225 1384077 NM LT TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 LT I/B FLAP HAS AN AREA OF DELAMINATION ON UPPER SURFACE, WS 275 CUT OUT DELAMINATED AREA 7 1/2 INCH BY 7 1/2 INCH ON LT I/B FORG FLAP UPPER SURFACE AND REMOVED DAMAGED CORE 7 1/2 BY 7 1/2. SHAPED SECTION OF CORE 7 1/2 INCH BY 7 1/2 INCH. FABRICATED DOUBLER 10 1/2 INCH BY 10 1/2 INCH. BONDED CORE PLUG AND DOUBLER, CLEANED, PRIMED AND SEALED IAW SRM 51-40 -24 FIG 1. 2 L 7 3 4F A3WE 2008040900098 20080409 00098 NM 2008 4 9 08FDEA01292 1 20080403 A 5347 BAC1520792 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 MAI CARGO COMPARTMENT, SEAT TRACK CORRODED STA 570-580 RBL 45 REMOVED SEAT TRACK SECTION OUT OF LIMITS AT STA 530 TO 690 RBL 45 IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM ER-01-049 AND SRM 53-10-5 FIG 7. TREA TED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED SEAT TRACK IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008040900100 20080409 00100 NM 2008 4 9 HALA0800496 1 20080405 A 2740 84D1007 MOTOR BOEING 717 717200 1383700 NM INOPERATIVE A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 477HA 55122 PRIMARY TRIM INOP. REMOVED AND REPLACED PRIMARY TRIM MOTOR PER AMM 27-41-10. OPS AND SECURITY CK OK. 2 L 7 2 4F TR A6WE 2008040900101 20080409 00101 2008 4 9 HALA0800497 4 20080404 A 2310 2305794 TRANSCEIVER BOEING 767 767332 1382001 NM HF SYSTEM INOPERATIVE A HALA O OTHER O OTHER CR CRUISE 1 WP 13 598HA 8500 8500 23278 ETOPS SIGNIFICANT SYSTEM, TRANSMISSION L HF INOP. TUNING LAST FOR 15 SECONDS AND OCCURS EACH TIME MIC IS KEYED. HAPPEN S ON MULTIPLE FREQUENCIES. REPLACED LT HF TRANSCEIVER PER AMM 23-11-03. OP CHECKS OK. 2 L 7 2 4F RT A1NM 2008040900104 20080409 00104 EU 2008 4 9 08FDEA01295 1 20080402 A 5312 A53984651200 BULKHEAD AIRBUS 310 A310203 3930313 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 EMPENNAGE AFT PRESSURE BULKHEAD IS DENTED AT THE 9 O'CLOCK POSITION APPROX 32 INCH FROM THE CENTER LINE. DENT IS SHALLO W AND SMOOTH. REPAIRED AREA IAW EA NR 6-5310-118458 "FUSELAGE AFT PRESSURE BULKHEAD WEB DENT". 2 L 7 2 4F RT A35EU 2008040900110 20080409 00110 WP 2008 4 9 AALA200800690 1 20080321 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 955U 49427 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 28 TO 30 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 29 FOR EMERGENCY LI GHT AT OVERHEAD SEAT ROWS 28 TO 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008040900111 20080409 00111 NM 2008 4 9 AALA200800691 1 20080321 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 766AN 32880 JFK - EMERGENCY LIGHT AT FORWARD GALLEY FLOOR INOPERATIVE. REPLACED BATTERY PACK AT LEFT NUMBER ONE DOOR FORWARD GALLEY FOR EMERGENCY LIGHT AT FORWARD GALLEY FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900122 20080409 00122 NM 2008 4 9 DLM88080529 1 20080403 A 5320 NOZZLE DOUG MD88 MD88 3023688 NM RADIO RACK CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, CRACKS WERE FOUND ON FWD CORNERS OF RADIO RACK FAN AIR EXHAUST NOZZLE. EXHAUST NOZZLE WAS REPAIRED IAW ER/A 464964-14MA. 2 L 7 2 4F RT A6WE 2008040900123 20080409 00123 NM 2008 4 9 DLM88080530 1 20080403 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, A CRACK LEFT CUSP WEB WAS FOUND AT STA Y=800. CUSP WEB WAS REPAIRED IAW SRM 53-05D FIG 827D. 2 L 7 2 4F RT A6WE 2008040900125 20080409 00125 NM 2008 4 9 DLM88080532 1 20080403 A 5712 RIB DOUG MD88 MD88 3023688 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, A CRACK RIB WAS FOUND AT RIGHT WING FIXED LEADING EDGE AT STA XRS=164. RIB WAS REPLACED IAW SRM 51-30-5,51- 30-2 AND DWG 9937517 REVE-J. 2 L 7 2 4F RT A6WE 2008040900126 20080409 00126 NM 2008 4 9 DLM88080533 1 20080403 A 5320 FLOOR SUPPORT DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, GALVANIC CORROSION WAS FOUND ON FLOOR PANEL SUPPORT AT STA Y=160 TO 200 X=-8 FWD WET AREA. SUPPORT WAS REPL ACED IAW SRM 51-30-01. 2 L 7 2 4F RT A6WE 2008040900133 20080409 00133 NM 2008 4 9 AALA200800678 1 20080319 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 DFW - EMERGENCY LIGHT AT OVERHEAD RIGHT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD RI GHT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900134 20080409 00134 NM 2008 4 9 AALA200800679 1 20080319 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 DFW - EMERGENCY LIGHT AT SEAT ROW 29 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 29. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900135 20080409 00135 NM 2008 4 9 AALA200800680 1 20080319 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 661AA 25295 DFW - EMERGENCY LIGHT AT SEAT 25D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 25D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900136 20080409 00136 NM 2008 4 9 AALA200800681 1 20080319 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 DFW - EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900151 20080409 00151 EA 2008 4 9 SWIA200819435 1 20080402 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 411SW 7067 FLT 3951 - RIGHT WINDSHIELD CRACKED ON TAXI OUT. REPLACED THE FIRST OFFICER WINDSHIELD IAW AMM 56-11-01, P/N NP-139321 -6, S/N OFF 016095H3873. 2 L 7 2 4F RT A21EA 2008040900157 20080409 00157 WP 2008 4 9 AALA200800670 1 20080316 A 5321 FLOOR PANEL DOUG DC9 DC983 3022083 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9403W 53139 TUL - FOUND CORROSION ON CABIN SUB FLOOR, AREA OF DISCREPANCY IS 18 BY 18 INCHES AT STATION 218. INSTALLED REPAIR DOUBL ER PER AARD 53 20 00 16. 2 L 7 2 4F RT A6WE 2008040900162 20080409 00162 WP 2008 4 9 IXXA08SMN087S 1 20080215 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER INNER SKIN INBOARD SPLICE CRACKED AT STATI ON XFS 341.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFOR MED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLERS. CLEANED, TREA TED, PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XFS 297.500 TO STATION XFS 341.50 0 IAW DC8 SRM 51-1-11, DC8 SRM 51-3-1, FAA FORM 8110-3 NUMBER 08086 DATED 02-27-08, SEMAN DRAWING NUMBER ED-4706 DATED 0 2-09-08, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008031000053 20080310 00053 NM 2008 3 10 NWAA080756309 1 20080221 A 5313 STRINGER BOEING 747 747451 1384940 NM BS 460 S10R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING "M" CHECK, FOUND CRACKS IN STRINGER 10R AT BS 460. REPAIRED PER EA 63-212199. 2 L 7 4 4F RT A20WE 2008031000092 20080310 00092 WP 2008 3 10 IXXA08SMN059S 1 20080207 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1766 L17R CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND EMPENNAGE LONGERON 17 RIGHT CRACKED AT STATION 1766.00. REMOVED FASTENERS AS NE EDED TO PERFORM REPAIR. REMOVED CRACKED LONGERON SEGMENT. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FASTENERS A ND LONGERON SEGMENT IAW DC8 SRM 53-5-1 FIGURE 7 SHEET 37 PAG 22, DC8 SRM 51-2-0 FIGURE 50 SHEET 37, 51-3-0, 51-3-1, DC8 SRM 53-5-1 FIGURE 7 SHEET 1 PAG 22, DC8 SRM 51-1-21, 51-1-20D, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008031000094 20080310 00094 WP 2008 3 10 IXXA08SMN064S 1 20080208 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP LOWER SKIN DENTS AT STATION XF 169.000 - XF 213.000. REMOVE D FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTS AS NEEDE D WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 5 1-1-11, DC8 SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 4 T/R 57-94 DATED 10-01-02, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 S RM 57-7-1 FIGURE 4 T/R 57 - 94 ITEM "P" AND "Q", DC8 SRM 51-1-9 T/R 51-142, DC8 SRM 51-1-9A T/R 51 141, AND DC8 SRM 51-1 -8B. 2 L 7 4 4F RT 4A25 2008031000099 20080310 00099 NM 2008 3 10 DHL2008763502 1 20080302 A 5347 BAC15201466 SEAT TRACK BOEING 727 727264 138408M NM BS 850-870 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 SEAT TRACK CORRODED AT FLANGE, BS 850-870, LBL 45. REMOVED TRACK SECTION, FABRICATED SECTION FROM BAC 1520-1466, PO NR 730788, 15.75 INCHES LONG, AND INSTALLED PER B727 SRM 53-10-2 FIG 7, 53-10-5 FIG 1 AND 51-30-2. 2 L 7 3 4F A3WE 2008031000108 20080310 00108 EU 2008 3 10 08FDEA00681 1 20080303 A 5730 A5735003900000 PANEL AIRBUS 310 A310324 3930206 EU RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 RT WING VENT TANK PANEL 650 LB, HAS FRETTING AT THE INTERIOR FASTENER HOLES. CLEANED FRETTING AROUND THE FASTENER HOLES ; CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW A310-300 SRM 57-20-16; PAGE 108; FIG 103. REPLACED WITH NEW PART A57 35003900000 PO 610289.1. INSTALLED ON JOB CARD 46S5109CP. 2 L 7 2 4F RT A35EU 2008031000111 20080310 00111 NM 2008 3 10 08FDEA00683 1 20080303 A 5754 114N4076920 SKIN BOEING 757 7572B7 1384964 NM NR 9 SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 RT WING NR 9 L/E SLAT HAS A CRACK PROPAGATING FROM RIVET HOLE, I/B SKIN FWD OF I/B SLAT TRACK. REMOVED I/B SKIN FROM NR 9 L/E SLAT IAW SRM 51-40-02. FABRICATED NEW REPAIR SKIN ON MAE TRAVELER NR T8/719344 FROM 7075-T6 .050C. INSTALLED NE W REPAIR SKIN IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008031000116 20080310 00116 NM 2008 3 10 08FDEA00685 1 20080303 A 5310 146N561015 CREASE BEAM BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 903FD 27124 MAIN CARGO DECK FLOOR, CREASE BEAM WEB CORRODED AT STA 1360, RBL 60, WL 208. REMOVED CORROSION IAW SRM 51-10-02, L= 2.5 , W= 2.5, D= 0.031, ORIGINAL MATERIAL THICKNESS 0.040. FOUND TO BE OUT OF SRM 53-60-13, FIG 101, DETAIL III LIMITS. RE MOVED WEB IAW SRM 51-40-02. FABRICATED NEW REPAIR WEB ON MAE TRAVELER NR T8/722696, FROM 7075-0 .040C, HEAT TREATED TO T6. LOCATED AND DRILLED WEB IAW SRM 51-40-05. TREATED AND PRIMED WEB IAW SRM 51-20-01. INSTALLED REPAIR WEB IAW SRM 51-40-02. THIS IS A CATEGORY "A" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 2008031000121 20080310 00121 2008 3 10 08FDEA00688 4 20080304 A 3417 ADC AIRBUS 310 A310203 3930313 EU NR 2 UNKNOWN A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 415FE 349 ON TAKEOFF ROLL, CAPT/FO AIRSPEED DIFFERENCE OF 40 KNOTS (120/80) REJECTED TAKEOFF. PERFORMED ADS SYSTEM CHECK IAW TSM 34-10-00. NO FAULTS NOTED. NO FAULTS ON ADC NR 1 OR NR 2. PERFORMED VISUAL INSPECTION OF ALL PITOT PROBES, NO BLOCKA GE FOUND. PERFORMED PRESSURE BLOW OUT ON BOTH CAPT AND F/O PITOT LINE FOR OBSTRUCTION. NONE FOUND. PERFORMED PITOT S TATIC/TEST TO VERIFY SPEEDS WITH DIGITAL BARFIELD BOX IAW MM 34-10-00-5 02. ALL INDICATION CHECK WITH BOX AND NO SPLIT FOUND. CHANGED NR 2 ADC AS PRECAUTIONARY IAW 34-11-34-4. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A35EU 2008031000135 20080310 00135 NM 2008 3 10 USAA920080539 1 20080228 A 5311 90526911 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - CRACKED FRAME, BS 500C, S9L. REPAIRED FRAME BS, 500C, S9L IAW USAIRWAYS EA 100286. 2 L 7 2 4F RT A16WE 2008031000148 20080310 00148 NM 2008 3 10 USAA920080556 1 20080303 A 5311 65465262 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 400, S9L. REPAIRED FRAME BS, 400, S9L IAW USAIRWAYS EA 100286. 2 L 7 2 4F RT A16WE 2008031000156 20080310 00156 EA 2008 3 10 SWIA200819278 1 20080224 A 3230 864808 ELECTRONIC UNIT CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 943SW 16303 16303 7762 FLT 6722 - NOSE GEAR EXTENDED UNCOMMANDED DURING CLIMB. REPLACED PSEU AS REQUIRED IN REF CRJ 200 AMM 32-61-05. NO FURT HER FAULTS NOTED. 2 L 7 2 4F RT A21EA 2008031000158 20080310 00158 NM 2008 3 10 KCSA081135 1 20080304 A 5320 SUPPORT FITTING BOEING 747 747209B 138489B NM CARGO BAY CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 AFT PIT CARGO STOP I/B SUPPORT FITTING CRACKED AT BS 1908, RBL-47. 2 L 7 4 4F RT A20WE 2008031000163 20080310 00163 NM 2008 3 10 HNAA0800089 1 20080221 A 3350 85 LIGHT DHAV DHC8 DHC8102 2809003 NM LIGHT SWITCH INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 824EX 30182 387 FOUND F/A EMERGENCY LIGHT SELECT SWITCH INTERNAL INDICATION LIGHT INOP. REPLACED BULB. 2 H 7 2 4T RT A13NM 2008031000182 20080310 00182 EA 2008 3 10 SWIA200819293 1 20080224 A 2150 GG670950091 ACM CNDAIR CL600 CL6002C10 1390015 EA RIGHT SMOKE A SWIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 718SK 10184 FLT 6579 - ON TAXI OUT, GOT SMOKE IN THE CABIN. REPLACED RIGHT ACM IAW AMM 21-51-08. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008031000191 20080310 00191 NM 2008 3 10 HNAA0800090 1 20080219 A 3350 1013075 LENS DHAV DHC8 DHC8102 2809003 NM CABIN FADED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 941HA 48259 161 FOUND TWO OF THE FOUR FLOOR LEVEL EMERGENCY EXIT MARKER LIGHTS AT ROW 1 WERE NO LONGER RED. REPLACED LENSES. 2 H 7 2 4T RT A13NM 2008031000202 20080310 00202 NM 2008 3 10 08FDEA00700 1 20080305 A 5320 146N541614 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD STRINGER R7.55, STA 1320-1340. TO EVALUATE EXISTING REPAIR. EXISTING REPA IR FOUND NOT IAW B757-200 SRM 51-70-11 FIG 1 DETAIL I, II REV.93. AFT CARGO FLOORBOARD STRINGER AT R7.55, FROM STA 1200 TO STA 1343.5, REPLACED IAW B757-200 SRM 51-10-02 REV 93. 2 L 7 2 4F RT A2NM 2008031000234 20080310 00234 EA 2008 3 10 TRAX200800351 1 20080227 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA RT OVERWING INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 885AS 7521 RT OVERWING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008031000249 20080310 00249 WP 2008 3 10 AALA200800440 1 20080228 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7508 49802 EWR - EMERGENCY LIGHTS AT OVERHEAD COCKPIT INOPERATIVE. REPLACED BATTERY PACK B5 23 FOR EMERGENCY LIGHTS AT OVERHEAD CO CKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031000254 20080310 00254 NM 2008 3 10 AALA200800397 1 20080224 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 640A 24598 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008031000287 20080310 00287 NM 2008 3 10 AALA200800406 1 20080224 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 DFW - EMERGENCY LIGHT AT SEAT 26G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031000288 20080310 00288 NM 2008 3 10 AALA200800407 1 20080224 A 3350 1008G12A11200B COVER BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET AREA MISSING PROTECTIVE COVER AND WIRING IS EXPOSED. REPLACED COVE R FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031000291 20080310 00291 NM 2008 3 10 AMTA200800065 1 20080203 A 5320 SCUFF PLATE BOEING 737 73783N 13844HI NM FUSELAGE CORRODED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 317TZ 28246 AFT CARGO COMPARTMENT DOOR SCUFF PLATE CENTRAL AREA WITH FILIFORM CORROSION AND SOME SCRATCHES. ORIGINAL MATERIAL .056, REMAINING MATERIAL AFTER CLEAN UP WAS .039 AND FOUND OUT OF LIMITS IAW SRM 53-60-15, REPAIRED IAW SRM 53-60-15 AND EA 2015738001. (K) 2 L 7 2 4F RT A16WE 2008031000294 20080310 00294 NM 2008 3 10 AALA200800414 1 20080226 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 MIA - EMERGENCY LIGHTS AT FIRST CLASS GALLEY CLOSET AREA INOPERATIVE. REPLACED BATTERY PACK AT LEFT NUMBER ONE DOOR FOR EMERGENCY LIGHTS AT FIRST CLASS GALLEY CLOSET AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031000296 20080310 00296 NM 2008 3 10 AALA200800416 1 20080226 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 761AJ 31478 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR AISLE DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RIGHT NUMB ER ONE DOOR AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031000297 20080310 00297 NM 2008 3 10 AALA200800417 1 20080226 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 761AJ 31478 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET AREA DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031000300 20080310 00300 WP 2008 3 10 AALA200800421 1 20080227 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 467AA 49597 LGA EMERGENCY LIGHT AT OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031000304 20080310 00304 NM 2008 3 10 AALA200800420 1 20080227 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 343AN 33082 SFO - EMERGENCY LIGHT AT L391 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT L391. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A1NM 2008031000308 20080310 00308 WP 2008 3 10 AALA200800434 1 20080228 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 973TW 53623 LGA - EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008031000311 20080310 00311 EU 2008 3 10 AALA200800437 1 20080228 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80052 460 JFK - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008031000316 20080310 00316 WP 2008 3 10 AALA200800429 1 20080227 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14551 53033 LGA - EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F A6WE 2008031000319 20080310 00319 EU 2008 3 10 MALA080025 1 20080220 A 5311 FRAME SAAB SF340 340B 7860101 EU BS 294 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 340B453 DURING HEAVY CHECK REPAIRED FRAME AT STA 294.0 BETWEEN BL 0.0 AND BL 18.3 IAW EO NR S53108. 2 L 7 2 4T RT A52EU 2008031000320 20080310 00320 NM 2008 3 10 BB08028 1 20080302 A 3233 ACTUATOR BOEING 757 757225 1384959 NM MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 916UW 22192 SJU STT-PHL FLT NR 1012 - AFTER TAKEOFF, THE GEAR WOULD NOT RETRACT AND THE GEAR LEVER WOULD NOT RAISE PAST THE OFF POSI TION. CREW HAD THREE GREEN LIGHTS AND ELECTED TO LEAVE THE GEAR DOWN AND DIVERT TO SJU. AIRCRAFT LANDED WITHOUT FURTHE R INCIDENT. MAINTENANCE REPLACED THE LEFT TRUCK TILT ACTUATOR. OPS CHECKED OK. 2 L 7 2 4F RT A2NM 2008031000321 20080310 00321 NM 2008 3 10 BB08031 1 20080304 A 3397 WIRE BOEING 757 7572S7 1384962 NM EMERGENCY LIGHT BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 902AW 23322 PHX - EMERGENCY EXIT SIGN LIGHT AT R-1 DOOR IS INOP DURING TEST. MAINTENANCE REPAIRED BROKEN WIRE. OPS CHECKS OK. 2 L 7 2 4F RT A2NM 2008031000322 20080310 00322 NM 2008 3 10 BB08029 1 20080229 A 3297 W840203B18 WIRE BOEING 767 7672B7 1385107 NM BROKEN A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 256AY 26847 MIA FLT NR 9241 MIA-PHL - AFTER TAKEOFF, CREW RECEIVED EICAS MESSAGE OF AIR/GRND DISAGREE. FLIGHT RETURNED TO MIA WITHO UT FURTHER INCIDENT. MAINTENANCE REPAIRED WIRE W840-203B-18, BETWEEN CONNECTOR D4302J AND D5554J. SYSTEM OPS CHK NORMA L. 2 L 7 2 4F RT A1NM 2008031000337 20080310 00337 CE 2008 3 10 AMWA89563BC 1 20080111 A 2432 10136457217 PCB BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BATTERY CHARGE MALFUNCTIONED A AMWA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 162ZV 887 UE162 BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLIGHT. MAINT REPLACED PCB A130 AND CLEARED DISCREPANCY. 2 L 7 2 4T 3 T RT A24CE E2NE 2008031000358 20080310 00358 NM 2008 3 10 AMTA200800112 1 20080219 A 2560 SPRING BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE GIRT BAR FAILED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 560TZ 33525 R1 DOOR GIRT BAR LEAF SPRINGS FAILED TEST TO RETAIN SLIDER. REMOVED AND REPLACED R1 DOOR GIRT BAR LEAF SPRINGS IAW CMM 256614, REPAIR 2-1, FIG 601 AND 602. TEST TO RETAIN SLIDER RE-ACCOMPLISHED AND TEST GOOD IAW EO 757-52AD-3166. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008031000359 20080310 00359 WP 2008 3 10 AMTA200800114 1 20080219 A 5210 BOTTLE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL L1 DOOR BLOWN A AMTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 11 705TZ 46915 L1 EMERGENCY ASSIST BOTTLE BLOWN INADVERTENTLY. SERVICE L1 DOOR EMERGENCY ASST BOTTLE IAW MM 52-11-07. (K) 2 L 7 3 4F 4 F A22WE A23EA 2008031000360 20080310 00360 2008 3 10 AMTA200800115 2 20080219 A 7310 FUEL BOEING 737 73783N 13844HI NM NR 2 ENGINE LEAKING A AMTA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 GL 11 305TZ 30706 ON PREFLIGHT FOUND FUEL DRIPPING UNDER NR 2 ENG. BEFORE ENG RUN THE LEAK WAS AT 13 DROPS/MIN DURING AND AFTER RUN, LEAK WAS 1 DROP/MIN, THIS IS UNDER THE THRESHOLD LIMITS IAW AMM 71-71-00-6, PAR 1.F (1) (8). (K) 2 L 7 2 4F RT A16WE 2008031000361 20080310 00361 EA 2008 3 10 A6WA20080046 1 20080123 A 2700 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FLIGHT CONTROL MALFUNCTIONED A A6WA K NONE F FLT CONT AFFECTED LD LANDING 1 GL 31 460AW 7867 HIGHER THAN NORMAL BACK PRESSURE NEEDED DURING LANDING WITH YOKE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000362 20080310 00362 EA 2008 3 10 A6WA200840053 1 20080126 A 2611 SMOKE WARNING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LAVATORY MALFUNCTIONED A A6WA O OTHER N FALSE WARNING AP APPROACH 1 GL 31 468AW 7818 INFLIGHT DURING BLEED TRANSFER (SMOKE TOILET) CAS MESSAGE APPEARED. COMPLIED WITH QRH. MESSAGE WENT AWAY. FLIGHT ATTE NDANT REPORTED ACRID SMELL IN CABIN. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000363 20080310 00363 EA 2008 3 10 A6WA200840064 1 20080210 A 3297 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE WOW DAMAGED A A6WA K NONE J WARNING INDICATION TO TAKEOFF 1 GL 31 451AW 7832 WOW INPUT CAUTION MESSAGE DISPLAYED ON T/O ROLL AT 100 KNOTS, MESSAGE CLEARED ON GEAR RETRACTION. MESSAGE REAPPEARED ON GEAR EXTENSION DURING LANDING. PROXY FAULTS STATUS DISPLAYED ON GROUND. REPOSITIONED MLG NR 1 WOW HARNESS AS REQUIRED , CLEANED AND RESEATED CONNECTOR PLUG IAW 32-46. PERFORMED GEAR SWINGS. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000364 20080310 00364 EA 2008 3 10 A6WA200840065 1 20080210 A 2750 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS FAILED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED DE DESCENT 1 GL 31 421ZW 7346 FLAPS FAIL AT ZERO DEGREE, WHEN MOVING TO FLAPS 8 DEGREE ON DESCENT. COMPLIED WITH RESET PROCEDURE IWA AWAC SUPP 98-018 B STEPS 1.3 AND 1.4. FLAP SYS RESET OK. (K) FOUND LT DRIVE SHAFT NR 5 UNSEREVICEABLE. REMOVED AND REPLACED PER AMM 2 7-53-10, OPS CHECK GOOD. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000365 20080310 00365 2008 3 10 A6WA200840066 4 20080210 A 3417 ADC CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 1 FAILED A A6WA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 435AW 7724 AIR DATA COMPUTER NR 1 FAILED IN FLIGHT. COMPLIED WITH QRH , SWITCHED TO AIR DATA COMPUTER NR 2, ALL INDICATING NORMAL AIR DIVERSION AND LANDING UNEVENTFUL. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000368 20080310 00368 EA 2008 3 10 A6WA200840097 1 20080218 A 2751 BRAKE ASSY CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE MOTOR BRAKE MALFUNCTIONED A A6WA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 31 441ZW 7777 FLAPS HALF SPEED MESSAGE ON ED2. REMOVED AND REPLACED MOTOR BRAKE UNIT IAW 27-52-05. OPS CHECK GOOD AT THIS TIME. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000381 20080310 00381 EA 2008 3 10 A6WA200840076 1 20080109 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 431AW 7256 FLOOR SUPPORT CORRODED AT FS 589.0 TO 605.0 NL 73.50 LBL 10.0. (K) REPAIRED IAW REO 601R-53-00-027 REV C. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000382 20080310 00382 EA 2008 3 10 A6WA200840077 1 20080201 A 5320 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE GROUND POWER CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 431AW 7256 AC GROUND POWER RECEPTACLE SUPPORT MEMBER IS CRACKED. (K) SUPPORT MEMBER REPLACED IAW SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000393 20080310 00393 EA 2008 3 10 A6WA200840088 1 20080204 A 5240 SCUFF PLATE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE SERVICE DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 SCUFF PLATE OF SERVICE DOOR FOUND CORRODED. (K) SCUFF PLATE REPLACED IAW SRM 51-42-06 AND 51-41-02. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031100001 20080311 00001 CE 2008 3 11 DJFA2008009 1 20080125 A 5511 45A21104012 RIB BEECH MU300 400A 1155402 CE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 746TA 1005 127 RK146 DURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNI QUE' NR 70. MAINTENANCE REPLACED BOTH RIBS WITH IMPROVED ASSEMBLIES. 2 H 7 2 4F RT A16SW 2008031100002 20080311 00002 NE 2008 3 11 DJFA2008011 2 20080126 A 7320 79015510 HMU BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LT ENGINE MALFUNCTIONED E DJFA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 EA 23 482LX 2168 RK413 PCEJA0612 DURING CRUISE, CREW NOTED LT ENGINE ROLL BACK FROM 95.7 TO 91.0 WITH SIMULTANEOUS FUEL FLOW AND ITT FLUX. AC WAS AT FL 380 WITH AN OAT OF -33 C IN CLEAR AIR. ENGINE ANTI-ICE WAS OFF. MAINTENANCE FOUND THE LEFT HMU FAILED. IT WAS REPLACE D 2 H 7 2 4F 4 F RT A16SW E25EA 2008031100003 20080311 00003 CE 2008 3 11 DJFA2008012 1 20080129 A 5511 128620022002 RIB BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 443LX 1095 1095 RK237 DURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNI QUE' NR 70. OPEN 2 H 7 2 4F 4 F RT A16SW E25EA 2008031100004 20080311 00004 CE 2008 3 11 DJFA2008013 1 20080201 A 3020 45A35042003 RING BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE RT ENGINE INLET CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 408CW RK108 DURING INSP, MAINT FOUND THE RT ENGINE INLET RING CRACKED BETWEEN THE 1200 AND 0100 O CLOCK POSITION. MAINTENANCE REPLA CED THE INLET RING. 2 H 7 2 4F 4 F RT A16SW E25EA 2008031100014 20080311 00014 2008 3 11 08FDEA00526 4 20080220 A 2565 35124406402 INDICATOR DOUG DC10 DC1030F 3023504 WP R1 DOOR SLIDE INOPERATIVE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 R-1 SLIDE DISARM LIGHT IS INTERMITTENT. REMOVED AND REPLACED R-1 DOOR "SLIDE DISARMED" ANNUNCIATOR IAW DC10 AMM 33-00- 00-2. OPS CHECK GOOD IAW DC10 AMM 52-70-00-2. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008031100016 20080311 00016 NM 2008 3 11 2008UALA00933 1 20080218 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEAT 28AB INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 667UA 29239 EEL LIGHT STRIP AT SEAT 28AB INOP. REPAIRED CONNECTION AT CABLE CONNECTOR UNDER SEAT. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031100018 20080311 00018 NM 2008 3 11 2008UALA01059 1 20080228 A 3350 BR964421 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SEAT 20ABC BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 839UA 1507 EMERGENCY PATH LIGHTING AT SEAT 20ABC BULB BURNT OUT. REPLACED LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031100019 20080311 00019 NM 2008 3 11 2008UALA01068 1 20080228 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY LIGHTS INOP: DOOR 2L FWD SILL ILLUM. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2008031200001 20080312 00001 NM 2008 3 12 2008UALA01071 1 20080228 A 3350 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EEL POWER SUPPLY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY ESCAPE LIGHTS INOP: RT OVERWING 2 AFT ASSY'S. REPLACED FUSE ON POWER SUPPLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031200005 20080312 00005 NM 2008 3 12 08FDEA00651 1 20080228 A 5347 ACA7106505 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 608FE 48548 MAIN DECK CARGO, SEAT TRACK AT STA 555, RT X=27.5 FOUND CORRODED. REPAIR CARRIED OUT AS PER SRM 53-70-00 VOLUME I. REP AIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008031200008 20080312 00008 CE 2008 3 12 DXTA20082908 1 20080302 A 2731 TRIM TAB CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ELEVATOR MISRIGGED E DXTA A UNSCHED LANDING W F INADEQUATE Q C FLT CONT AFFECTED CL CLIMB 1 GL 07 650QS 5605150 TRIM INDICATOR GOES .5 IN BEYOND FWD WHITE BAND AND ONLY BACK AS FAR AS THE O IN (TO) EXCESSIVE FWD CONTROL PRESSURES RE QUIRED DURING TAKEOFF WITH INDICATOR IN TO RANGE. PERFORMED ELEVATOR TRIM SURVEY. FOUND EXCESSIVE CLEARENCE BETWEEN PIN AND SPACER. REMOVED ONE SPACER IAW MM CH 27-32-01 TO GET CLEARANCE OF .050 TO .080 REINSTALLED TRIM WHEEL. OPS CHECKED SATISFACTORY. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008031200014 20080312 00014 CE 2008 3 12 DXTA20082912 1 20080303 A 2731 INDICATOR CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE ELEVATOR TRIM LOOSE E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 814QS 5600776 ELEVATOR TRIM POSITION INDICATOR INOP. INDICATES INCORRECT TRIM POSITION. FOUND TRIM LOOSE. SHIMMED & RESECURED INDICA TOR IAW MM 27-31-00. OPERATIONAL AND TRAVEL CHECK NORMAL. 2 L 7 2 4F 4 F RT A22CE E00053EN 2008031200016 20080312 00016 CE 2008 3 12 DXTA20082913 1 20080304 A 4990 APU CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE OVERSERVICED E DXTA K NONE W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 07 611QS 5605548 WHILE RUNNING APU, ELECTRICS AND BLEED ON, RT WING O'HEAT ANN ILLUMINATED. RAN BOTH ENGINES W/APU ELECTRICS AND BLEED ON , O`HEAT ANN DID NOT ILLUMINATE, BUT STRONG BLEED AIR ODOR AND SMOKE FILLED THE AIRCRAFT. REMOVED APU BLEED AIR CHECK V ALVE. NO DEFECTS FOUND. REINSTALLED VALVE. PERFORMED BORESCOPE INSPECTION OF ENTIRE APU. NO EVIDENCE OF OIL CONTAMIN ATION. CLEANED ENTIRE APU AREA AND RAN FOR 1 HR. NO SMOKE NOTED AND NO EXTERNAL OIL LEAKS. FOUND APU WAS OVERSERVICED THE DAY BEFORE, SUSPECT SMOKE FROM EXCESS OIL. CLOSED PANELS WORK DONE IAW HONEYWELL BE 100XL CMM 49-10-00 2 L 7 2 4F 4 F RT A22CE E00059EN 2008031200017 20080312 00017 NE 2008 3 12 DXTA20082915 2 20080305 A 7320 10052742 METERING UNIT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LT ENGINE MALFUNCTIONED E DXTA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 GL 07 658QS 930 5605665 PCEDD0341 NR1 ENGINE FUEL BOOST PUMP LIGHT FLASHED UPON DESCENT. A FEW SECONDS AFTER THE FLASH THE NR1 ENGINE FAILED. REMOVED/REP LACED FUEL METERING UNIT, FUEL FLOW DIVIDER, AND FUEL FLOW TRANSMITTER. REMOVED FUEL LINES AND INSPECTED FOR CONTAMINATI ON, NONE FOUND, REINSTALLED. REPLACED FUEL FILTER IAW PWC MM 3052242R-7 CH 73-10-05. PERFORMED GROUND CHECKS FOLLOWING M AJOR COMPONENT REPAIR/REPLACEMENT IAW PWC MM 3052242S-7 CH 71-00-00. OPERATED ENGINE AT 80 PERCENT N1 FOR ONE HOUR. NO F AULTS FOUND, ENGINE OPERATES NORMALLY. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008031000033 20080310 00033 NM 2008 3 10 CALA0800182 1 20080210 A 5330 6516352 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69351 23589 FOUND CORROSION ON INTERNAL SKIN AT BS 483 LOCATED AT FORWARD CARGO DOOR CUTOUT LOWER AFT CORNER. FABRICATED AND INSTAL LED REPAIR DOUBLER PER SRM 53-00-01. 2 L 7 2 4F RT A16WE 2008031000060 20080310 00060 NM 2008 3 10 QXEA200800227 1 20080208 A 5330 PANEL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 406QX 4048 PDX - C4 CHECK - SUSPECTED CORROSION UNDER 2 MARKED NUTPLATES FOR AFT CARGO BAY PANEL 144JZ. REPAIRED IAW Q400 SRM 51-4 2-05, 51-21-00, 51-21-00, 51-14-00 NDTM PART 6 51-00-01, PART 1 51-00-04, AND Q400 RD 8/4-53-2265. 2 H 7 2 4T RT A13NM 2008031000066 20080310 00066 SO 2008 3 10 LR7A08024 1 20080228 A 5330 SKIN LKHEED 382 382G 526414U SO FS 826 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 334 4590 DURING SCHEDULED A-1 CHECK, PER JOB CARD HA1200, FOUND CRACKED SKIN AT FS 826, WL178, RBL64.5. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-12 ON LOG PAGE 28130 ITEM M4. 2 H 7 4 4T A1SO 2008031000078 20080310 00078 NM 2008 3 10 SWAA081130 1 20080228 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008031000102 20080310 00102 WP 2008 3 10 ARWA20080303 1 20080303 A 2432 BATTERY DOUG DC10 DC1030F 3023504 WP DISCHARGED A ARWA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 19 450ML 47831 ON PRE-FLIGHT, FOUND BATTERY VOLTS READS ZERO. REMOVED 02 BATTERY IN ACCORDANCE WITH A/M/M 24-34-01. CHARGED 02 BATTER Y IN ACCORDANCE WITH DC-10-A/M/M 24-34-01; REINSTALLED 02 BATTERY IN ACCORDANCE WITH 24-34-01. TEST CHECK OK IN ACCORDA NCE WITH A/M/M 24-34-00. 2 L 7 3 4F RT A22WE 2008031000103 20080310 00103 SO 2008 3 10 C2XA08SH040 1 20080229 A 5751 14569009410 FITTING EMB 145 EMB145XR 3260214 SO RT AILERON WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17138 145727 SHV - DURING C-CHECK IT WAS FOUND THAT THE RT AILERON PCA ACTUATOR ATTACHMENT FITTING ON THE AILERON SPAR HAD MIGRATED H AT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW CONTINENTAL EXPRESS EC5750-01177. THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008031000109 20080310 00109 NM 2008 3 10 KCSA081132 1 20080301 A 5313 STRINGER BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 FUSELAGE STRINGER IS CORRODED AT STA 2205, STR 36L. 2 L 7 4 4F RT A20WE 2008031000110 20080310 00110 EU 2008 3 10 08FDEA00682 1 20080303 A 5730 A5735003900000 PANEL AIRBUS 310 A310324 3930206 EU RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 RT WING PANEL 650 MB; INTERIOR SURFACE HAS FRETTING AROUND THE FASTENER HOLES. CLEANED AREAS AROUND THE FASTENER HOLES; CHECKED THE LIMITS AND FOUND TO BE OUT OF LIMITS IAW A310-300 SRM 57-20-16; PAGE 108; FIG 103. REPLACED WITH NEW PART A5735003900000; PO610289.2. INSTALLED ON JOB CARD 46S5109CP. 2 L 7 2 4F RT A35EU 2008031000132 20080310 00132 NM 2008 3 10 USAA920080536 1 20080228 A 5311 90526911 FRAME BOEING 737 7373G7 1384595 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 747, S9L. REPAIRED FRAME BS, 747, S9L IAW USAIRWAYS EA 100286. 2 L 7 2 4F RT A16WE 2008031000140 20080310 00140 NM 2008 3 10 USAA920080544 1 20080207 A 5320 143N833818 INTERCOSTAL BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 901AW 23321 MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL, BS 680, S11R - S12R. REPLACED INTERCOSTAL, BS 680, S11R - S12R IA W USAIRWAYS TASK CARD M1C53608. 2 L 7 2 4F RT A2NM 2008031000172 20080310 00172 EA 2008 3 10 SWIA200819287 1 20080228 A 2701 BEARING CNDAIR CL600 CL6002B19 1900309 EA YOKE ROUGH A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 447SW 7677 CLICKING NOISE IN RIGHT YOKE WHEN AILERONS MOVED TO FULL TRAVEL, FLIGHT NR 3932. REPLACED BEARINGS IN RIGHT YOKE IAW MM 27-11-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008031000231 20080310 00231 CE 2008 3 10 BSYA2008007 1 20080304 A 3230 LANDING GEAR LEAR 35 35LEAR 5170600 CE LACK OF LUBE E BSYA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 900JC 178 AFTER TAKEOFF OUT OF LCK BOTH INBOARD GEAR DOOR LIGHTS STAYED ON AFTER GEAR WAS SELECTED UP. TRIED CYCLING GEAR, NO HEL P. AIRCRAFT RETURNED TO LCK. BROUGHT AIRCRAFT INTO WARM HANGAR AND THAWED ICE OUT OF WHEEL WELLS, CLEANED AND LUBED GE AR AND OPS CHECKS GOOD. 2 L 7 2 4F A10CE 2008031000242 20080310 00242 EU 2008 3 10 MALA080034 1 20080227 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 340B428 EMERGENCY POWER SUPPLY 23LN FAILED TEST. REMOVED AND REPLACED POWER SUPPLY AT 23LN P/N ON AND OFF 330151, S/N ON 2175 S N OFF 1334 IAW AMM 33-50-10-04-1. OPS CK GOOD. 2 L 7 2 4T RT A52EU 2008031000248 20080310 00248 EU 2008 3 10 AALA200800439 1 20080228 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80052 460 JFK - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008031000268 20080310 00268 WP 2008 3 10 AALA200800384 1 20080222 A 3222 STRUT DOUG DC9 DC983 3022083 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 589AA 53252 ORD INFLIGHT T1613/22FEB - NOSE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. RETURNED TO ORD AND LANDED WITHOUT INCIDE NT. ACCOMPLISHED NOSE LANDING GEAR SHOCK STRUT REPACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008031000285 20080310 00285 NM 2008 3 10 AALA200800404 1 20080224 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 DFW - EMERGENCY LIGHT AT SEAT 37G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 37G. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031000295 20080310 00295 NM 2008 3 10 AALA200800415 1 20080226 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 619AA 24577 MIA - EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. CLEANED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008031000315 20080310 00315 WP 2008 3 10 AALA200800428 1 20080227 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14551 53033 LGA - EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F A6WE 2008031000355 20080310 00355 NM 2008 3 10 AMTA200800102 1 20080218 A 5514 SUPPORT BOEING 737 73783N 13844HI NM HORIZ STAB DAMAGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 317TZ 28246 ELONGATED HOLES AT E-STA 231.70 AND 225.70 FOR SUPPORT PANEL 333FB ONT EH LT HORIZ STABILIZER. REPAIRED IAW EA737-5510- 08-A0010 NOTE ELONGATED HOLES WERE SELF INDUCED, FRE ERA 737-55R-6237. (K) 2 L 7 2 4F RT A16WE 2008031000392 20080310 00392 EA 2008 3 10 A6WA200840087 1 20080212 A 5320 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 CRACK SUSPECTED IN AC GROUND POWER BOX. (K) A/C CONNECTOR SUPPORT MEMBER REPLACED IAW SRM 51-42-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031100008 20080311 00008 NM 2008 3 11 08FDEA00422 1 20080214 A 5280 ANB7216504 DOOR DOUG MD11 MD11F 3023600 NM ZONE 700 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 589FE 48491 RT MLG WW, FOUND DOOR ASSEMBLY PANEL NR 741AL WITH EDGES WORN. REPAIRED AS PER EA 1-5280-117392, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008031100009 20080311 00009 EU 2008 3 11 08FDEA00431 1 20080214 A 5321 B5327032200200 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU CARGO BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 MAIN CARGO FLOOR PANEL 261AH IS CRACKED ACROSS THE LOWER SURFACE. FABRICATED NEW PANEL 261AH IAW SRZ 25-005 REV F. 2 L 7 2 4F RT A35EU 2008031100012 20080311 00012 EU 2008 3 11 08FDEA00421 1 20080213 A 5230 A5237405220400 BUSHING AIRBUS 300 A300F4605R 3930327 EU CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 AFT CARGO DOOR ECCENTRIC BUSHING SUPPORT INNER BORE CORRODED. REMOVED AND REPLACED AFT CARGO DOOR NR 2 ECCENTRIC BUSHIN G REF FEDEX ROUTINE CARD 61X5030ALI AND AMM 52-32-11-5. T/W TWS 8330A. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008031100013 20080311 00013 EU 2008 3 11 08FDEA00430 1 20080214 A 5230 A5237405220400 BUSHING AIRBUS 300 A300F4605R 3930327 EU CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 684FE 802 AFT CARGO DOOR NR 1 ECCENTRIC BUSHING SUPPORT INNER BORE IS CORRODED. REMOVED AND REPLACED THE AFT CARGO DOOR NR 1 ECCE NTRIC BUSHING REF FEDEX ROUTINE CARD 61X5030ALI AND A300-600 AMM 52-32-11-5. T/W TWS 8330A. MINOR REPAIR. 2 L 7 2 4F RT A35EU 2008031200025 20080312 00025 NM 2008 3 12 P5CA0801546 1 20080222 A 5280 DOOR BOEING 747 74746NF 13848BT NM RT MLG DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 453PA 30811 RIGHT WING GEAR INBD STRUT DOOR HAS SKIN DELAMINATION. ACCOMPLISHED PART 1 OF THE TIME LIMITED REPAIR OF MA NR A45280-0 2:00. COI NR 453-031 WAS OPENED FOR A 5-CYCLE VISUAL INSPECTION. 2 L 7 4 4F RT A20WE 2008031200026 20080312 00026 2008 3 12 UPS08151715 4 20080225 A 2565 SLIDE AIRBUS A300 A300F4622R 3930360 EU L1 DOOR UNSECURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 134UP 0817 FOUND L1 DOOR EMERGENCY EVACUATION SLIDE NOT SECURE IN SLIDE ASSY DOOR MOUNTS, DOOR REMOVED. DEFERRED MAIN CABIN SLIDE PER MEL 52-11-01-3 M-369937 ASSIGNED. INSTALLED NEW SLIDE PER MM 25-61-21-4. 2 L 7 2 4F RT A35EU 2008031200031 20080312 00031 NM 2008 3 12 UPS08551729 1 20080227 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM BS 1200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 456UP 25477 INSPECTION TYPE:C-2 MAIN DECK FLOORBEAM UPPER CHORD FWD FLANGE, NUT PLATE HOLES HAS CORROSION, BS 1200, LBL 55-RBL 55. REPAIRED FLOORBEAM UPPER CHORD FWD FLANGE IAW ATS ER NR 08-1351 AND UPS EO B757-5310-28698-A. 2 L 7 2 4F RT A2NM 2008031200032 20080312 00032 NM 2008 3 12 UPS08551732 1 20080227 A 3350 SWITCH BOEING 757 75724APF 1384969 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 411UP 23851 AT EMERGENCY EXIT LIGHT CONTROL SWITCH, THE UNARMED ANNUNCIATOR HAS ONE LAMP INOP. RELAMPED PER AMM 33-16-02-2. OPS CK OK. 2 L 7 2 4F RT A2NM 2008031200034 20080312 00034 WP 2008 3 12 UPS08851733 1 20080228 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 FOUND EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW 33-50-01-2. 2 L 7 4 4F RT 4A25 2008031200036 20080312 00036 NM 2008 3 12 UPS08M51730 1 20080227 A 3020 ANTI-ICE SYSTEM DOUG MD11 MD11F 3023600 NM NR 2 ENGINE INOPERATIVE A IPXA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SO 01 252UP 48768 ATB - AFTER DEPARTURE FROM SYD, THE CREW ADVISED DISPATCHER THAT THEY HAD AN ANTI-ICE ISSUE ON THE NR 2 ENGINE AND WOULD RETURN TO SYD. THE FLIGHT LANDED W/O FURTHER INCIDENT. NO EMERGENCY DECLARED AND THEY DID NOT DO AN OVERWEIGHT LANDIN G. REMOVED AND REPLACED 3 EA SENSE ELEMENT IAW AMM 30-22-11-4 AND REQ TEST C/W SATS IAW AMM 30-22-11-5, PN-35512-61/SN- TAG1276636A (POS BANJO NR 2) PN-3551943102 (2 EA BANJO NR 4) SN-TAG00679239 (UPPER ELEMENT) SN-TAG00953446 (LOWER ELEMEN T). 2 L 7 3 4F RT A22WE 2008031200037 20080312 00037 NM 2008 3 12 UPS08M51731 1 20080228 A 2841 4061969903 INDICATOR DOUG MD11 MD11F 3023600 NM FUEL SYSTEM INOPERATIVE A IPXA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SO 01 291UP 48477 ATB - CREW ACCOMPLISHED AN ATB, AFTER THE NR 1 FUEL QTY INDICATING SYSTEM FAILED. THE NR 2 FUEL FLOW INDICATOR WAS PREV IOUSLY DEFERRED. ACCORDING TO SYSTEM OPS, THE CREW DUMPED 85.0-100LBS OF FUEL IN ORDER TO LAND UNDER MAX LANDING WEIGHT . FOUND IN CFDS FSC FAULT REVIEW FQGS-A FAULT. T/S PER FIM 28-08-00-1. R&R FSL IAW AMM 28-08-01-2.PRECAUTIONARY R & R A FSC PER AMM 28-80-03-4 R&R SEM IAW AMM 28-41-92-4. ALL TESTS PASSED. 2 L 7 3 4F RT A22WE 2008031200039 20080312 00039 NM 2008 3 12 UPS08551728 1 20080228 A 5270 SWITCH BOEING 757 75724APF 1384969 NM PAX DOOR MALFUNCTIONED A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 465UP 28269 EICAS MSG L FWD ENT DOOR DISPLAYED DURING TAKEOFF ROLL. ENTRY DOORS OPEN LIGHT ILLUMINATED W/DOOR CLOSED. RETURNED TO FIELD, FRM CODE 52-71. DEF PER MEL 52-71-1. ACCOMPLISHED DMP 52-71-1. VERIFIED CLOSED. M370236 ASSIGNED. REMOVED AN D REPLACED CREW ENTRY DOOR SWITCH AND OPS CHECK PER MM 52-71-00-5. 2 L 7 2 4F RT A2NM 2008031200040 20080312 00040 NM 2008 3 12 UPS08551740 1 20080229 A 5420 ANGLE BOEING 757 75724APF 1384969 NM NR 1 NACELLE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 435UP 25466 INSPECTION TYPE:4 DAMAGED I/B SIDE OF FORWARD FAIRING "L" ANGLE ON NR 1 ENGINE PYLON. REPAIRED PER ER 08-1337 AND SRM 5 1-40-02. 2 L 7 2 4F RT A2NM 2008031200043 20080312 00043 WP 2008 3 12 UPS08851741 1 20080220 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1520 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 CABIN STA 1520 LBL60 SEAT TRACK GOUGED. CABIN SEAT TRACK AT STA 1520 AND LBL 60, REPAIRED IAW EO DC8 -5340-7779-B. 2 L 7 4 4F RT 4A25 2008031200044 20080312 00044 WP 2008 3 12 UPS08851742 1 20080109 A 5720 36440462 FITTING DOUG DC8 DC871F 302199D WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:C2 NR 4 ALT5-65 TO FRONT SPAR FITTING CRACKED. REPAIRED FWD SPAR FITTING BY FABRICATION AND INSTALLATIO N IAW SRM 51-01-20D, SRM 51-03-02, SRM 51-01-08 AND SRM 51-01-12. 2 L 7 4 4F RT 4A25 2008031200045 20080312 00045 NM 2008 3 12 UPS08M51738 1 20080212 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:1C RIGHT LE NR 14 SLAT TRACK CUT OUT CRACKED ON LWR O/B CORNER, CUTOUT DAMAGE. FABRICATED DOUBLER AND I NSTALLED DOUBLER IAW MD-11 SRM 57-10-00 FIG 21. 2 L 7 3 4F RT A22WE 2008031200071 20080312 00071 NM 2008 3 12 2008UALA01104 1 20080228 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 616 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FUSELAGE FRAME CRACKED BELOW CABIN FLOOR, OVER WING SECTION BS 616 RT SIDE. MAJOR REPAIR ACP'D. REMOVED DAMAGE AND VER IFIED WITH HFEC. INSTALLED A FILLER AND A REPAIR ANGLE PER MM 53-11-89-801. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300001 20080313 00001 NM 2008 3 13 2008UALA01105 1 20080228 A 5712 RIB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 RT WING RIB AT WBL 135.5 IS CRACKED AT AFT LOWER RIB CLIP NR 13349-6000-0033. ACP'D PER EVA 080161. MAJOR REPAIR: REPA IR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300007 20080313 00007 2008 3 13 WGEA200800039 4 20080304 A 3457 GPS ECLIPS EA500 ECLIPSEEA500 3350000 SW MALFUNCTIONED E WGEA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 153DJ 000072 DME AND GS INDICATIONS FAILED IN FLIGHT. TRIED GNV, OCF, LAL BUT NO DME. DURING RTB, DME AND GS CAME BACK INTERMITTENT . SUPPLEMENTAL INFORMATION, PERFORMED GPS ADJUSTMENT TEST IAW EA 500 AMM 34-50-10. NO DEFECTS NOTED AT THIS TIME. PER FORMED A/C TAXI AND VERIFIED GROUND SPEED INDICATION ON BOTH PFD'S IAW EA500 AMM 9-20-00. 1 L 7 2 4J RT A00002AC 2008031300011 20080313 00011 EU 2008 3 13 DATA200800002 1 20080227 A 5270 SWITCH STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA DOOR OUT OF ADJUST E DATA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 936M SH3036 AFTER DEPARTING MYR, THE RED DOOR WARNING LIGHT ON CWP ILLUMINATED AT 600 AGL. AFTER PERFORMING THE LIMITS CHECKLIST TH E PILOT TURNED ON THE CABIN LIGHT BECAUSE THE DOOR WARNING LIGHT REQUIRES IMMEDIATE ACTION. THE PILOT NOTICED A SMOKE/F OG BANK IN THE CABIN. PILOT DECIDED TO RETURN TO MYR FOR AN IMMEDIATE LANDING TO INVESTIGATE THE PROBLEM. UPON LANDING , IT WAS NOTED THAT THE SMOKE/FOG HAD DISSIPATED. THE SMOKE DETECTION SYSTEM HAD NOT ACTIVATED. THERE WAS NO EVIDENCE OF A FIRE. IT IS BELIEVED THAT THE FOG OCCURRED DUE TO HIGH HUMIDITY AND DEW POINT. FOUND WATER CONDENSATION THROUGH O UT AIRCRAFT, DRIED AIRCRAFT WITH BLEED AIR SYSTEM. DOOR WARNING LIGHT MICROSWITCH WAS ADJUSTED AND AIRCRAFT RETURNED TO 2 H 7 2 4T 4 T A41EU E4EA 2008031300013 20080313 00013 NM 2008 3 13 ASAA0852683 1 20080227 A 3150 1762000101 WARNING SYSTEM BOEING 737 737890 1384527 NM COCKPIT MALFUNCTIONED A ASAA K NONE N FALSE WARNING NR NOT REPORTED 1 NM 02 558AS 35177 BOTH ND'S DISPLAY "FMC DISAGREE" PERFORMED FIM 34 61 TASK 835. NO FLIGHT FAULTS SYSTEM FUNCTIONS NORMALLY. UNABLE TO C ONFIRM ORIGINAL FAULTS. 2 L 7 2 4F RT A16WE 2008031300021 20080313 00021 WP 2008 3 13 UPS08851747 1 20080221 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP BS 785-1000 ELONGATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 RT STA 785-1000 FLOORBOARD F94A/F94B HAS SEVERAL ELONGATED FASTENER HOLES. REPAIRED RT F94A/F94B FLO ORBOARD FASTENER HOLES IAW DWG 5758265 AND SRM 53-02-03-0 FIG 010. 2 L 7 4 4F RT 4A25 2008031300023 20080313 00023 2008 3 13 DATA200800003 4 20080226 A 3442 TRANSCEIVER STBROS SD3 SD330 8100602 EU WEATHER RADAR INOPERATIVE E DATA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 13 334AC SH3029 AFTER TAKEOFF PILOT NOTICED SMELL OF SMOKE. PILOT ASKED COPILOT TO CONFIRM WHICH HE DID. NO SMOKE INDICATION OCCURRED. COPILOT CHECKED CARGO COMPARTMENT AND NOTICED WHITE SMOKE. SMELL OF SMOKE WAS STILL PRESENT. FLIGHT CREW DECLARED AN D EMERGENCY AND RETURNED TO DHN. DURING DESCENT THE FLIGHT CREW NOTICED THE SMOKE HAD DISSIPATED. AFTER LANDING THERE WAS NO EVIDENCE OF SMOKE PRESENT. MAINTENANCE FOUND A WEATHER RADAR TRANSCEIVER INOP AND FAINT BURNT SMELL. APPARENTLY SMOKE WAS CONDENSATION, NOT SMOKE. 2 H 7 2 4T A41EU 2008031300024 20080313 00024 WP 2008 3 13 UPS08851749 1 20080226 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 COCKPIT, FE'S FWD SEAT TRACK HAS WORN SEAT LOCKPIN HOLES. REPAIRED FE'S FWD SET TRACK BY REPLACEMENT IAW SRM 51-01-24 AMD SRM 51-03-00. 2 L 7 4 4F RT 4A25 2008031300032 20080313 00032 NE 2008 3 13 QXEA200800234 2 20080303 A 7230 311171201 SERVO DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE NR 1 ENGINE INOPERATIVE A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 349PH 486 PDX - FLIGHT 2122 - ENGINE "SURGE" NOISE INTERMITTENT ABOUT EVERY 5-6 MINUTES DURING CLIMB. RTF PDX MAINTENANCE FOUND N R 1 ENGINE IBV SERVO INOPERATIVE, REMOVED AND REPLACE IBV SERVO COMPLETED GROUND RUNS, ALL OPERATIONAL CHECKS GOOD. AIR CRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2008031300038 20080313 00038 NM 2008 3 13 2008UALA01122 1 20080229 A 5230 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 FWD CARGO DOOR AFT SIDE FRAME LWR END IS CRACKED INNER RADIUS. MAJOR REPAIR ACCOMPLISHED: REPLACED AFT LOWER FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300039 20080313 00039 NM 2008 3 13 2008UALA01123 1 20080301 A 5340 ATTACH ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 S8L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 FOUND FUSELAGE INTERCOSTAL ATTACH ANGLE CRACKED STR 8L AT BS 294.5. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW INTERCOSTAL (P/N 65-17684-629). 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300041 20080313 00041 NM 2008 3 13 2008UALA01124 1 20080301 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 S7L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 INTERCOSTAL FRAME ANGLE CRACKED BS 294.5 AT STR 7L. MAJOR REPAIR ACCOMPLISHED: REPLACE WEB (P/N 65-17684Y642). 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300043 20080313 00043 NM 2008 3 13 2008UALA01125 1 20080301 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 AFT GALLEY DOOR CUTOUT, FWD LOWER CORNER AT SCUFF PLATE LOWER EDGE HAS FUSELAGE SKIN TOOLING DAMAGE, 3.75 INCH AFT OF PL ATE LE. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED SCRIBE LINE REPAIR EXTERNAL SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300049 20080313 00049 NM 2008 3 13 2008UALA01127 1 20080229 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 2080-2100 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 104UA 26902 FUSELAGE INTERNAL SKIN CORRODED, BS 2080-2100 STR 35-36R AT LAVATORY VENT EXHAUST. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL DOUBLER & TRIPLER. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031300051 20080313 00051 NM 2008 3 13 ASAA0852689 1 20080302 A 2160 3989083 VALVE BOEING 737 737890 1384527 NM CABIN TEMP FAULTY A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 558AS 35177 ZONE TEMP ILLUMINATED ON RECALL, "CONT CAB" FOUND RT CONTROLLER FLT DECK TRIM AIR VALVE FAULT LIGHT ON. REPLACED FLIGHT DECK TRIM AIR VALVE. OP & LEAK CHECK OK. CLEARED PACK ZONE TEMP CONTROLLER FAULT. 2 L 7 2 4F RT A16WE 2008031300053 20080313 00053 NM 2008 3 13 ASAA0852690 1 20080302 A 3040 8300005604 CONTROLLER BOEING 737 737890 1384527 NM WINDOW HEAT FAULTY A ASAA K NONE J WARNING INDICATION CL CLIMB 1 NM 02 559AS 35178 DURING CLIMB F/O'S SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. TURNED SWITCH OFF WAITED 5 MINS TURNED BACK ON. FIVE MINS L ATER OVERHEAT LIGHT CAME BACK ON. RESET AGAIN LIGHT REMAINED OUT. NUMEROUS OP CHECKS GOOD. PER FIM 30 41 TASK 801 BIT E PROCEDURE BIT VERIFY TEST OK. LAST 10 FLIGHTS SHOW "WINDOW SENSOR FAULT". PER FIM 30 41 TASK 811 RANG OUT RT SIDE WI NDOW TEMP SENSORS. SENSORS CHECK GOOD. SHAKE DOWN OF SAME WINDOW COIL CORD GOOD. TEMP SENSOR WIRING TO WINDOW HEAT CN TL UNIT GOOD. PER FIM REPLACED WINDOW HEAT CNTL UNIT, OPS NORMAL. 2 L 7 2 4F RT A16WE 2008031300059 20080313 00059 NM 2008 3 13 2008UALA01133 1 20080229 A 5322 6948204U2 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S14-15L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 FRAME SHEAR TIE CRACKED BS 360 BTWN STR'S 14L-15L. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300072 20080313 00072 SO 2008 3 13 RAIA0803001 1 20080302 A 3260 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO LANDING GEAR DIRTY A RAIA B A EMER. DESCENT UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 830HK 145313 FLT 5513 - ATL - LANDING GEAR AIR/GROUND FAILURE MESSAGE ON THE EICAS. MAINTENANCE CLEANED THE WEIGHT ON WHEELS SWITCHE S AND PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM WITH NO FURTHER DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008031300073 20080313 00073 NM 2008 3 13 2008UALA01146 1 20080303 A 2612 WARNING HORN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU FIRE DETECT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 598UA 28751 APU FIRE WARNING HORN INOP. FOUND HORN FAULTY. REPLACED APU FIRE WARNING HORN. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031300079 20080313 00079 NM 2008 3 13 2008UALA01152 1 20080229 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 533UA 25073 EEL FIRST CLASS AND MID LAV INOP. RESEATED CONNECTORS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031300082 20080313 00082 NM 2008 3 13 2008UALA01155 1 20080302 A 3350 1317 BULB BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 772UA 26930 NR 2 LT DOOR EMERGENCY LIGHT INOP. SECURED BULB. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008031300085 20080313 00085 NM 2008 3 13 2008UALA01157 1 20080301 A 3150 WARNING MESSAGE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 791UA 26933 HYD PUMP DEMAND RIGHT STATUS MSG. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040900165 20080409 00165 NM 2008 4 9 DLM88080542 1 20080403 A 5311 FRAME DOUG MD88 MD88 3023688 NM BS 1287 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, EXFOLIATION CORROSION WAS FOUND ON FRAME AT STA Y=1287 LONGERON 30 IN AFT CARGO COMPARTMENT. FRAME WAS REPA IRED IAW SRM 53-03D FIG 2A. 2 L 7 2 4F RT A6WE 2008040900166 20080409 00166 NM 2008 4 9 DLM88080543 1 20080403 A 5230 PAN DOUG MD88 MD88 3023688 NM CARGO DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, A CRACK WAS FOUND ON FWD CARGO COMPARTMENT DOOR INBD PAN. DOOR WAS REPAIRED IAW SRM 52-05 FIG 26A. 2 L 7 2 4F RT A6WE 2008040200342 20080402 00342 NM 2008 4 2 KCSA081203 1 20080324 A 5311 FRAME BOEING 747 747146 1384905 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 LOWER FUSELAGE FRAME CRACKED AT BS 2742, BL-0. 2 L 7 4 4F RT A20WE 2008040200349 20080402 00349 NM 2008 4 2 2008UALA01716 1 20080326 A 3350 D9239003500060 BATTERY PACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 853UA 1688 CABIN EMERGENCY LIGHT TEST FAILED. FAULTS EPSU BATT EMERG R. SUPPLEMENTAL DATA UPDATE CAUSE, BATTERY PACK FAILURE. RE PLACED BATTERY PACK, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041000003 20080410 00003 CE 2008 4 10 CSI0108 1 20080319 A 3297 FFJ131 WIRE AMP CESSNA 500 550 2076604 CE PWA 530 PW530A NE BRAKE SYSTEM BACKED OUT E ZZTA K NONE J WARNING INDICATION CR CRUISE 1 SO 00 100WT 2154 2154 5500858 DA0126DA012 DURING FLIGHT, APPROACHING KSUS (SPIRIT OF ST LOUIS AIRPORT, MO), THE CREW OBSERVED THAT THE BRAKE PRESSURE LOW AND ANTI -SKID INOP, ANNUNCIATOR LIGHTS WERE ILLUMINATED. CHECKLIST PROCEDURES WERE FOLLOWED AND ATC WAS ADVISED. ATC HAD EMERG ENCY EQUIPMENT RESPOND. A NORMAL APPROACH AND LANDING WERE MADE. NORMAL BRAKING WAS AVAILABLE AFTER LANDING. THE AIRC RAFT WAS TAXIED TO PARKING AND SHUTDOWN. SYSTEM INVOLVED: TROUBLESHOOTING DETECTED A WIRING PROBLEM IN THE ANNUNCIATIN G SYSTEM. APPARENT CAUSE OF MALFUNCTION: PIN FF IN AMP CONNECTOR J131 WAS NOT CRIMPED. NOTE: IT APPEARS THE PIN WAS NOT CRIMPED WHEN IT LEFT THE FACTORY. OTHER PERTINENT INFORMATION. THE TERMINAL PIN IN AMP CONNECTOR J131 WAS REPLACED 1 L 7 2 4F 4 F A22CE E00053EN 2008040200369 20080402 00369 NM 2008 4 2 2008UALA01756 1 20080327 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 556UA 26650 FOUND EMERGENCY LIGHTS AT DOOR 4R AND FWD LEFT OVERWING INOP. RELAMPED BULBS AND OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040300036 20080403 00036 NM 2008 4 3 ABXA080101 1 20080229 A 5347 S232T30114 SEAT TRACK BOEING 767 767281 1385109 NM COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 769AX 22787 FIRST OFFICER'S FORWARD OUTBOARD SEAT TRACK CRACKED AT FORWARD STOP FITTING. REMOVED AND REPLACED TRACK ASSEMBLY IAW B7 67 SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008040300063 20080403 00063 NM 2008 4 3 KCSA081208 1 20080326 A 5320 WEB BOEING 747 747SR46 1384816 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 FWD PIT BILGE TORQUE BOX UPPER WEB CRACKED AT BS 866, LBL-3. 2 L 7 4 4F RT A20WE 2008040300074 20080403 00074 NM 2008 4 3 200800308 1 20080317 A 5350 SKIN BOEING 747 747SPB5 1384813 NM FAIRING SCRATCHED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 708BA 22484 RT LOWER FWD WING TO BODY FAIRING, FROM STA 620 TO STA 580 FROM STR 34R TO STR 47R SKIN HAS SCRIBE MARKS. APPROX STA 60 0 STR 32R .005 DEPTH. BLENDED OUT SCRIBE LINES, MATERIAL LOSS IS .005 WITHIN LIMITS, ALODINED AND PRIMED AREA PER B747 SP SRM'S 63-31-00 PG 1-4, 51-10-02 PG 6-6B AND BSOPM 20-44-04 PG 1-4. 2 L 7 4 4F RT A20WE 2008040300085 20080403 00085 NM 2008 4 3 2008UALA01704 1 20080326 A 5230 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AFT CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 AFT CARGO DOOR LOWER BEAM TEE COMMON TO EXTERNAL SKIN IS CRACKED AT AFT LOWER CORNER. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040300088 20080403 00088 NM 2008 4 3 2008UALA01706 1 20080326 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 616 S17L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 MID CABIN AREA BS 616L BODY FRAME INNER CHORD IS CRACKED BELOW STRINGER S-17L. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGE D AREA ON FRAME. ACCMP NDT FOR CRACKS. FABRICATED & INSTALLED STAINLESS STEEL NESTED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040300092 20080403 00092 NM 2008 4 3 2008UALA01707 1 20080326 A 5210 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 FWD GALLEY DOOR FWD LWR CORNER FRAME HAS 2 CRACKS. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGED SECTION OF FRAME. INSTALLE D FRAME SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040300094 20080403 00094 NM 2008 4 3 2008UALA01709 1 20080326 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 277-360 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 FOUND FWD GALLEY DOOR CREASE BEAM IS CORRODED FROM STA 277 TO 360. MAJOR REPAIR ACCOMPLISHED: REPLACED DOOR CREASE BEAM . 2 L 7 2 4F 4 F RT A16WE E2GL 2008040300109 20080403 00109 NM 2008 4 3 ASAA0872795 1 20080313 A 5755 113A46002 SKIN BOEING 737 737790 13844CN NM NR 7 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 607AS 29751 NR 7 SPOILER LWR SURFACE 46 INCHES FROM I/B DENTED REPAIR DENT ON NR 7 SPOILER LWR SURFACE IAW B737 700 SRM. 2 L 7 2 4F RT A16WE 2008040300116 20080403 00116 WP 2008 4 3 08FDEA01169 1 20080328 A 5340 ADA7875509 BRACKET DOUG MD10 MD1010F 3022112 WP ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 BRACKET CHAFED AND REQUIRES FABRICATION, TO BE INSTALLED ON JOB CARD N00009. REMOVED BRACKET IAW SRM 51-31-01; VOL II . FABBED BRACKET (REF DWG: ADA 7875). ALODINED & PRIMED IAW SRM 51-21-01; VOL II. INSTALLED NUTPLATE IAW SRM 51-3 5-01; VOL II. 2 L 7 3 4F RT A22WE 2008040300118 20080403 00118 WP 2008 4 3 08FDEA01170 1 20080328 A 5340 ADA78751 BRACKET DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 BRACKET CRACKED AND REQUIRES FABRICATION, TO BE INSTALLED ON JOB CARD N00009. REMOVED BRACKET IAW SRM 51-31-01 VOL II. FABBED BRACKET (REF DWG: ADA 7875). ALODINED & PRIMED IAW SRM 51-21-01 VOL II. INSTALLED NUTPLATES IAW SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2008040300122 20080403 00122 WP 2008 4 3 08FDEA01172 1 20080328 A 5340 ADA7875513 BRACKET DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 BRACKET CRACKED AND REQUIRES FABRICATION, TO BE INSTALLED ON JOB CARD N00414. REMOVED BRACKET IAW SRM 51-31-01 VOL II. FABBED BRACKET (REF DWG: ADA 7875). ALODINED & PRIMED IAW SRM 51-21-10 VOL II. INSTALLED NUTPLATE IAW SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2008040300152 20080403 00152 NM 2008 4 3 HALA0800450 1 20080329 A 2161 CONTROLLER BOEING 767 767332 1382001 NM CABIN TEMP MALFUNCTIONED A HALA K NONE O OTHER CR CRUISE 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, FWD CABIN TEMP CONTROL TO CONTROL DESIRED TEMP. CHECKED OPERATION OF FWD CABIN TEMP CONTROL, NO FAULTS NOTED ON BITE TEST. RESET CONTROLLER, ALL OPERATIONS NORMAL. 2 L 7 2 4F RT A1NM 2008040300182 20080403 00182 NM 2008 4 3 HALA0800460 1 20080327 A 5730 SKIN BOEING 767 767332 1382001 NM RT WING CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 LEVEL 1 CORROSION ON RIGHT WING LOWER SURFACE AT STRINGER L-15, AT WS 470-491. REWORKED IAW SRM 51-10-02. 2 L 7 2 4F RT A1NM 2008040300207 20080403 00207 EU 2008 4 3 08FDEA01225 1 20080401 A 5347 DAN2001T79511 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 448FE 260 MDCC NR 3 LT SEAT TRACK BETWEEN FRAMES 54.3 TO 54.2 HAS 2 AREAS OF DAMAGED SCALLOPS REMOVED AND REPLACED DAMAGED SEAT TRACK IN MDCC NR 3 LT AT FRAMES 54.2 TO 58 IAW A310-200 SRM 53-10-16 AND SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008040300209 20080403 00209 WP 2008 4 3 08FDEA01227 1 20080401 A 5311 70750080C FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 MCD-FUSELAGE UPPER LOBE-FRAME AT FS 635, 655, 675, 695, 715, 735, 755 AND 775, LONGERON 13R HAS CHAFED DAMAGED FROM LI NER MOUNT FASTENER. REMOVED FRAME SPLICE, FABED NEW SPLICE ON TRAVELER T8/729478, LOCATED AND DRILLED HOLES AND INSTALL ED NEW SPLICE AT STA 655 IAW SRM 51-31-01, 53-30-00 FIG 4 REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ATTENTION RECORDS, THIS IS A CLASS "B" REPAIR AND HAS AN INITIAL REINSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES. 2 L 7 3 4F RT A22WE 2008040300217 20080403 00217 EU 2008 4 3 08FDEA01235 1 20080401 A 5320 A5378198422200A WEB AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 MAIN CARGO FLOOR STRUCTURE HAS CORROSION ON THE UPPER SURFACE OF THE FLOOR WEBBING AT APPROX LBL 88 BETWEEN FRAMES 32 AN D 33. BLENDED CORROSION IAW SRM 51-74-10, PARA 5. ORIGINAL MATERIAL THICKNESS OF .094 AND .065 AFTER BLEND OUT FOR A T OTAL LOSS OF .029. FOUND TO BE OUT OF LIMITS IAW SRM SUPP 53-74-15; FIG 1. REMOVED WEB IAW SRM 51-40-21 PGS 6-7. LOCAT ED AND DRILLED NEW WEB IAW SRM 51-40-21 PGS 6-7. ALODINED AND PRIMED WEB IAW SRM 51-21-10. INSTALLED WEB IAW SRM 51- 40-21 PGS 6-7. APPLIED CIC ON WEB IAW AMM 51-22-00-0. 2 L 7 2 4F RT A35EU 2008040300223 20080403 00223 NM 2008 4 3 2008UALA01762 1 20080328 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 LT CREASEBEAM UPPER SURFACE CORRODED BETWEEN BS 847.5 TO 980. MAJOR REPAIR ACCOMPLISHED, REPLACED DOOR 2L CREASEBEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040300224 20080403 00224 NM 2008 4 3 2008UALA01763 1 20080328 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 FLOORBEAM AT BS 947.5 UPPER SURFACE CORRODED LBL9 TO LBL22 AND RBL21 TO RBL56. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR A CCOMPLISHED: REPLACED UPPER T-CAP BS 947.5 FLOORBEAM FROM LBL 49 TO RBL 60. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040400013 20080404 00013 NM 2008 4 4 232587 1 20080320 A 2910 AJG704119 HOUSING BOEING DOUG DC10 DC10 N/A-SDR NM CONTROL VALVE CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 EFS19503 HOUSING IS CRACKED NEAR PRESSURE PORTS. 2 L 7 3 4F RT A22WE 2008040400019 20080404 00019 2008 4 4 N93A23032008 4 20080223 A 2200 UNKNOWN GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU MALFUNCTIONED E N93A A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SO 13 486QS 1386 FLYING THRU MODERATE TURBULENCE THE AUTO PILOT , YAW DAMPENER, FLIGHT GUIDANCE COMPUTER, AND MACH TRIM. ALSO, STICK SHA KER ACTIVATED ALTHOUGH AIRCRAFT WAS TRAVELING AT 270 KNOTS. AIRCRAFT WAS INSPECTED AND SYSTEM OPS CHECKS COMPLETED. NO D EFECTS FOUND. 2 L 7 2 4F 4 F RT A12EA E25NE 2008040400024 20080404 00024 EU 2008 4 4 2008UALA01768 1 20080329 A 3510 MF100511 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CAPTAIN'S FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 431UA 571 CAPTAIN'S O2 MASK RED PRESS TO TEST BUTTON MISSING SMALL PIECE OF BUTTON. MASK IS FULLY FUNCTIONAL. REPLACED CAPT O2 M ASK ASSY, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040400026 20080404 00026 NM 2008 4 4 2008UALA01770 1 20080328 A 3320 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN SMOKE A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 670UA 29240 READ LT AT 41B REPORTED TO HAVE HAD ELEC ODOR AND PUFF OF SMOKE COMING FROM IT, DISSIPATED AFTER A FEW MINUTES. UNABLE TO DUPLICATE PROBLEM. ALL GROUNDS CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040400027 20080404 00027 NM 2008 4 4 2008UALA01771 1 20080328 A 4900 BACR13CG2A RELAY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE APU FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 672UA 30027 APU SHUT DOWN JUST AFTER NR 2 ENGINE STARTED APU HAS NO POWER ON INITIAL TESTING. SUSPECT RELAY. REPLACED RELAY STARTS N ORMALLY AND ACCEPTS POWER TRANSFERS. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT A1NM E24NE 2008040400028 20080404 00028 NM 2008 4 4 2008UALA01772 1 20080328 A 2560 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1R GIRT BAR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 585UA 26709 CANNOT GET DOOR 1R TO ARM. FOUND LANYARD HANGING DOWN, CAUSING INTERFERENCE. RESTOWED LANYARD, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040400029 20080404 00029 NM 2008 4 4 2008UALA01773 1 20080330 A 2530 OVEN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE GALLEY ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 819UA 893 RTFL DUE TO CREW REPORTS OF A STRONG ELECTRICAL ODOR IN AFT GALLEY. FOUND NO ODORS FROM AIR CON SYSTEM. FOUND STRONG E LECTRICAL ODOR EMITTING FROM R42 OVEN. INTERNAL SHORTING IN OVEN. REPLACED R42 OVEN, NO ODOR NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040400033 20080404 00033 EU 2008 4 4 2008UALA01778 1 20080329 A 3150 WARNING MESSAGE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT ILLUMINATED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 461UA 1266 EMERGENCY POWER SUPPLY UNIT INTERNAL LOAD LEFT MSG DISCOVERED ON 3SVC CHECK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040400034 20080404 00034 NM 2008 4 4 2008UALA01779 1 20080329 A 3510 MXP1472 OXYGEN MASK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CAPTAIN'S FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 CAPTAIN'S O2 MASK FAILS SELF TEST. FOUND FAULTY OXYGEN BOX AND MASK. REPLACED OXYGEN BOX AND MASK. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040400037 20080404 00037 NM 2008 4 4 2008UALA01782 1 20080331 A 3232 273N20055 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT MLG DOOR WEAK A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 595UA 28748 GEAR SELECTED DOWN "DOORS" LIGHT AND "GEAR DOORS" EICAS. DURING TAXI IN TO GATE RT MLG DOOR WAS NOT CLOSED, DOOR WAS H ANGING OPEN. FOUND ACTUATOR (DOOR) WEAK- POSSIBLE WATER CONTAMINATION. REPLACED RIGHT MLG DOOR ACT, PERFORMED SEVERAL DOOR/GEAR SWINGS, ALL SATISFACTORY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040400038 20080404 00038 EU 2008 4 4 2008UALA01783 1 20080331 A 5300 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AIRFRAME VIBRATION A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 403UA 442 AFTER TAKEOFF, THE FLIGHT EXPERIENCED AIRFRAME VIBRATIONS UPON FLAP RETRACTION. STOPPED AFTER LEVEL OFF AND CONTINUED T O DESTINATION. PERFORMED SEVERAL FLAP TESTS, ACCOMPLISHED EFCS1 & EFCS2 ELEVATOR DAMPING AND AILERON DAMPING TEST -NO F AULTS NOTED OPERATIONAL CHECK OK. NO FAULTS NOTED AUTOLAND TEST ACCOMPLISHED SYS CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040400039 20080404 00039 NM 2008 4 4 2008UALA01784 1 20080330 A 2420 IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 FAILED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 655UA 25393 L GENERATOR DRIVE LIGHT ILLUMINATED. LOST LEFT GENERATOR. NR 1 ENGINE IDG DISCONNECTED DUE TO FAULTS. REPLACED IDG AN D GEN CONTROL UNIT (PRECAUTIONARY). GENERATING SYSTEM OP CHKD OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040400047 20080404 00047 NM 2008 4 4 2008UALA01793 1 20080329 A 5551 LUG BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 LT HORIZONTAL OUTBOARD STABILIZER FWD SPAR UPPER LUG FWD BUSHING HAS FRETTING CORROSION. MAJOR REPAIR: REMOVED CORROSIO N AND ACCOMPLISHED REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040400049 20080404 00049 NM 2008 4 4 2008UALA01795 1 20080329 A 5551 LUG BOEING 737 737322 1384676 NM HORIZONTAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 LT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR UPPER CLEVIS FWD AND AFT LUGS HAVE EVIDENCE OF FRETTING CORROSION. MA JOR REPAIR: REMOVED CORROSION AND ACCOMPLISHED REPAIR. 2 L 7 2 4F RT A16WE 2008040400052 20080404 00052 NM 2008 4 4 2008UALA01798 1 20080330 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EMERGENCY LIGHT BETWEEN MID LAVS IS INOP. SECURED ELECTRICAL CONNECTION OF LIGHT STRIP. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040400054 20080404 00054 NM 2008 4 4 2008UALA01800 1 20080330 A 3350 1317 BULB BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 RIGHT EXT SLIDE LIGHT, 3RD LIGHT AFT HAS ONE BULB INOP. REPLACED LAMP OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040400057 20080404 00057 NM 2008 4 4 2008UALA01803 1 20080329 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS SEPARATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EEL STRIP INBOARD OF LAV 110 INOP. FOUND EEL CABLE CONNECTION SEPARATED. RECONNECTED AND OP CKD NORMAL 2 L 7 4 4F 4 F RT A20WE E24NE 2008042900016 20080429 00016 EU 2008 4 29 2008UALA02285 1 20080418 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 493UA 1821 CORROSION ON R2 DOOR SILL AT FASTENER HOLE NEAR AFT GIRT FITTINGS. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040400059 20080404 00059 NM 2008 4 4 2008UALA01808 1 20080328 A 3397 CONTACT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 661UA 27158 EXTERIOR EMERGENCY LIGHT AFT OF RT WING INOP. SUSPECT BAD CONTACT. CLEANED CONTACT OPS CHECKED GOOD. AC OK FOR SERVICE . 2 L 7 2 4F 4 F RT A1NM E24NE 2008040400063 20080404 00063 NM 2008 4 4 2008UALA01812 1 20080329 A 4990 ENGINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE APU OIL CONSUMPTION A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 787UA 26939 APU HIGH OIL CONSUMPTION GENERATED RED ALERT. UNABLE TO DUPLICATE PROBLEM. APU HOC TROUBLE-SHOOTING DUE TO INCREASE A PU OIL CONSUMPTION, ACCOMPLISH HIGH OIL CONSUMPTION TROUBLESHOOTING PER 777 FIM 49-20-00-810-818 TASK 818 PG252 REPAIR ALL LEAKS. 26MAR SFO ACP: TASK ACCOMPLISHED PER CALLOUT NO LEAKAGE, NO BLACK SMOKE DETECTED. APU SERVICED TO FULL, RAN FOR APPROX 30 MINUTES NO OIL CONSUMPTION INDICATED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040400068 20080404 00068 NM 2008 4 4 2008UALA01818 1 20080331 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S15L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 FWD ENTRY DOORWAY STR 15L, STRINGER CHANNEL CRACKED AT STA 360, AFT SIDE OF THE FRAME. MAJOR REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040400072 20080404 00072 NM 2008 4 4 2008UALA01822 1 20080331 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1197 S39L-R CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 AFT CARGO PIT, BS 1197+66 BETWEEN S-39L-39R, SHEAR TIE IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED SH EAR TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040400074 20080404 00074 NM 2008 4 4 2008UALA01824 1 20080331 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 580 S26-24L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 FWD PIT AT STA 580 BETWEEN STR 23L AND 24L , FRAME INBOARD FLANGE DENTED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPA IR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040400075 20080404 00075 NM 2008 4 4 2008UALA01825 1 20080331 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1530 S26R DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 AFT PIT FRAME INBOARD FLANGE AT STA 1560 AND STR 26R IS DENTED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040400077 20080404 00077 NM 2008 4 4 2008UALA01827 1 20080331 A 5210 STRUCTURE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L2 DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 855UA 1737 L2 DOOR GOUGED IN SEVERAL PLACES ALONG BOTTOM OF DOOR. THIS IS A MAJOR REPAIR. BLENDED AREA WITHIN LIMIT REF SRM 52-13- 00. NDT NO CRACKS FOUND. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040400081 20080404 00081 NM 2008 4 4 2008UALA01832 1 20080331 A 2560 256302008 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FLASHLIGHT DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 846UA 1600 EMERGENCY FLASHLIGHT CHARGE LIGHT NOT FLASHING AT 1L. FOUND BATTERY IN DISCHARGED. REPLACED FLASHLIGHT BATTERY, OPS CH ECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040400083 20080404 00083 NM 2008 4 4 2008UALA01834 1 20080401 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 4E AFT LIGHT ASSY. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040400093 20080404 00093 NM 2008 4 4 2008UALA01844 1 20080331 A 3350 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 777UA 26916 EXTERIOR EMERGENCY LIGHT INOP AT DOOR 1L 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040400096 20080404 00096 NM 2008 4 4 2008UALA01847 1 20080331 A 2150 CONTROL VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE A/C PACK MALFUNCTIONED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 777UA 26916 PACK FCV R ONE (BUT NOT BOTH) OF THE TWO RIGHT PACK FLOW CONTROL VALVES (FCV) ARE NOT IN THE COMMANDED POSITION. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040400101 20080404 00101 WP 2008 4 4 NWAA081339613 1 20080329 A 3397 WIRE DOUG DC9 DC932 3022066 WP EMERGENCY LIGHTS PINCHED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 613NW 47438 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR ROWS 18 THROUGH 21 IN COACH SEATS HAD FAILE D. AFTER MAINTENANCE FOUND THE EXIT IDENTIFIER POWER PACK FUSE BY THE AFT FLIGHT ATTENDANT PANEL HAD BLOWN THEY INVESTI GATED FURTHER. THE POWER SUPPLY WIRE WAS FOUND PINCHED BETWEEN THE SEAT RAIL AND THE SEAT TRACK AT ROW 18. THE WIRE WA S REPAIRED, THE FUSE REPLACED, AND OPERATIONAL CHECK COMPLETE. 2 L 7 2 4F A6WE 2008040400106 20080404 00106 EU 2008 4 4 08FDEA01240 1 20080401 A 5730 A5724410800 PANEL AIRBUS 310 A310203 3930313 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LEFT WING PANEL 512 AT IS CHAFED IN SEVERAL AREAS ON THE BACK SIDE. COMPLIED WITH EA 6-5720-118459 PT1. 2 L 7 2 4F RT A35EU 2008040400112 20080404 00112 EU 2008 4 4 08FDEA01246 1 20080402 A 5320 A53612214201 FLOOR SUPPORT AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND FLOOR SUPPORT CORRODED AT C11-13A, Y-730. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008040400118 20080404 00118 NM 2008 4 4 08FDEA01253 1 20080402 A 5753 ARC27364 SKIN DOUG MD11 MD11F 3023600 NM TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 RIGHT WING, INBOARD FLAP LOWER SURFACE FOUND DENTS AT XIFH 150. DENTED AREA MEASURED FOUND OUT OF LIMIT PER SRM 57-10-0 0 FIGURE 17 VOLUME I. DEPTH = 0.048" AND DIAMETER = 0.5". REPAIR CARRIED OUT PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAI R CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008040400124 20080404 00124 EU 2008 4 4 08FDEA01259 1 20080402 A 5310 A53973085 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 ON AFT CARGO DOOR SILL BEAM A HOLE WAS MISDRILLED, AT C 59-59A. REPAIR PERFORMED BY FREEZE PLUG INSTALLATION WITH SHOUL DERED BUSHING IAW. RAS/9000023/2008 ISS. A, APPROVED BY EA 6-5317-115265. 2 L 7 2 4F RT A35EU 2008040400126 20080404 00126 EU 2008 4 4 08FDEA01261 1 20080317 A 5753 A5797020020300 FLAP TRACK AIRBUS 310 A310203 3930313 EU TE FLAPS WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT FLAP VANE TRACK IS WORN, NR 5 TRACK. REPAIRED RIGHT WING NR 5 FLAP VANE TRACK IAW AIRBUS CMM 57-52-15. 2 L 7 2 4F RT A35EU 2008040400131 20080404 00131 EU 2008 4 4 08FDEA01266 1 20080402 A 5540 A55471556257 PLATE AIRBUS 300 A300B4622R 3930312 EU ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND ON RUDDER LIGHTNING PLATE CORRODED AND DISBONDED. REPAIR PERFORMED LAMINATING AND INSTALLING A NEW LIGHTNING PLAT E IAW RAS/DAHAM/4024036/2007 ISSA, APPROVED BY EA 6-5540-114862. 2 L 7 2 4F RT A35EU 2008040400134 20080404 00134 EU 2008 4 4 08FDEA01269 1 20080317 A 5753 A5797020021600 FLAP TRACK AIRBUS 310 A310203 3930313 EU TE FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT FLAP VANE NR 4 TRACK HAS WORN AREAS MARKED. REPAIRED L/W NR 4 FLAP VANE TRACK IAW AIRBUS CMM 57-52-15. 2 L 7 2 4F RT A35EU 2008040400140 20080404 00140 NM 2008 4 4 DL757080441 1 20080327 A 5330 141N33317 SKIN BOEING 757 757232 1384965 NM BS 345 S18L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 659DL 24421 FUSELAGE SKIN HAS A DENT AT STA 345 BETWEEN S-18L AND S-20L. THE DAMAGED SKIN WAS CUTOUT AND A REPAIR DOUBLER/TRIPLER W AS INSTALLED. 2 L 7 2 4F RT A2NM 2008040400148 20080404 00148 NM 2008 4 4 DL76G080451 1 20080131 A 5315 BAC15051008170 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1480 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 155DL 25269 FLOORBEAM CORRODED AT 1480 RBL 28 TO RBL56. REPAIRED ON AVM508455 PER SRM 53-00-51D FIGURE 201 AT HMV. 2 L 7 2 4F RT A1NM 2008040400149 20080404 00149 NM 2008 4 4 DL76L080452 1 20080401 A 3150 WARNING LIGHT BOEING 767 767332 1382001 NM FALSE INDICATION A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 199DN 28456 T/A AS WE SET TAKEOFF POWER EICAS MESSAGE UNSKED STAB TRIM ILLUMINATED DISCONTINUED T/O SPEED BELOW 80 KNOTS. ACCOMPLIS HED FIM 27-09-00 AND FOUND SATIS FOR FURTHER SERVICE. 2 L 7 2 4F RT A1NM 2008042100001 20080421 00001 NM 2008 4 21 2008UALA02123 1 20080412 A 2130 MOTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN PRESSURE MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 529UA 25019 FLIGHT DIVERTED DUE TO A CABIN PRESSURIZATION PROBLEM. REPLACED AC MOTOR ASSY AND NR 2 AUTO PRESSURE CONTROLLER, OPS CH ECKED GOOD, NO REPEATS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042100008 20080421 00008 NM 2008 4 21 2008UALA02129 1 20080411 A 5230 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 FWD GALLEY DOOR, AFT LOWER FRAME CRACKED IN SEVERAL AREAS, INCLUDING RADIUS. MAJOR REPAIR ACCOMPLISHED: INSTALLED FRAME SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042100010 20080421 00010 NM 2008 4 21 2008UALA02131 1 20080411 A 5712 RIB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 NR 2 MAIN FUEL TANK, WBL 135 RIB WHERE L2 STRINGER PASSES THROUGH THE LWR CHORD ANGLE CUTOUT, CHORD IS CRACKED IN UPPER- FWD RADIUS. MAJOR REPAIR ACCOMPLISHED: PERFORMED S/B REPAIR CONSISTING OF NEW "T" AND FILLER ASSY. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042100012 20080421 00012 NM 2008 4 21 2008UALA02133 1 20080411 A 5210 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 DOOR L1 HAS SKIN DENT LWR MID AREA OF SKIN ABOVE GATE. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA. ACCOMPLISHED H FEC. NO CRACK INDICATED. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042100015 20080421 00015 NM 2008 4 21 2008UALA02061 1 20080409 A 3350 SIGN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY EXIT EEL LIGHT EXIT SIGN INOP, AT DOOR 4 LEFT AFT SIGN. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042100020 20080421 00020 NM 2008 4 21 2008UALA02066 1 20080408 A 5230 DOOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CARGO DOOR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 FOUND AFT LOWER CORNER OF FWD CARGO DOOR NOT FLUSH WITH FUSELAGE GAP OF 5-32 OF INCH BETWEEN INNER DOOR SKIN AND OUTER F USELAGE SKIN. PERMANENT REPAIR ACCOMPLISHED PER SRM 52-30-01. CONDITION IS ACCEPTABLE PER MM52-34-00. NO FURTHER ACTION REQUIRED. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042100021 20080421 00021 NM 2008 4 21 2008UALA02067 1 20080409 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 620-640 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 LEFT EXTERNAL FUSELAGE AT BS 620-640 AT STR 15L-16L SKIN IS DENTED. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR . 2 L 7 2 4F 4 F RT A2NM E17NE 2008042100023 20080421 00023 2008 4 21 2008UALA02069 4 20080409 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 DOOR R1 SLIDE PRESSURE LOW. REPLACED SLIDE R1, PRESSURE OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042100029 20080421 00029 NM 2008 4 21 2008UALA02074 1 20080410 A 5320 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE OXYGEN SYSTEM FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 CAPTAINS O2 FITTING SNAPPED OFF IN STOWAGE BOX. REPLACED CAPTS O2 MASK BOX PER MM 35-12-96. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042100031 20080421 00031 NE 2008 4 21 2008UALA02076 2 20080409 A 7261 PRESSURE SWITCH BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE ENGINE OIL FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 216UA 30549 ENG OIL FILTER SENSOR RT THE PRESSURE SWITCH FOR DETECTING IMPENDING OIL FILTER BYPASS ON THE RIGHT ENGINE HAS FAILED. REPLACED OIL FILTER DELTA-P SWITCH. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008031300090 20080313 00090 2008 3 13 ASAA0852691 4 20080303 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 02 584AS 35682 THE "FMC DISAGREE" DISPLAYED ON FMC. ACCOMPLISHED FIM 34 61 TASK 835 & FMC BITE, OK. NO FURTHER DISCREPANCIES NOTED. 2 L 7 2 4F RT A16WE 2008031300096 20080313 00096 NM 2008 3 13 2008UALA01166 1 20080302 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 RIGHT EXTERIOR EMERGENCY LIGHT ASSY NR 3 FROM TOP HAS ONE LAMP INOP, RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031300099 20080313 00099 NM 2008 3 13 2008UALA01168 1 20080229 A 2711 69600817 CONTROL ROD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AILERON TAB FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 AILERON TAB CONTROL RODS ARE FAULTY. REPLACED CONTROL RODS 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300100 20080313 00100 NM 2008 3 13 2008UALA01169 1 20080229 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 5J AFT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY LIGHT ROW 5J AFT INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031300104 20080313 00104 NM 2008 3 13 2008UALA01174 1 20080303 A 5730 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 965 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 FOUND CORROSION ON CENTER WING UPPER SURFACE AT BS 965, BL0. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. FABRICATED & INSTALLED REPAIR SHIMS. ACCMP HFEC OF HOLES, NO DEFECT NOTED OVER SIZED HOLES. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031300106 20080313 00106 NM 2008 3 13 2008UALA01176 1 20080304 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 1J INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 FOUND SEAT EEL INOP:ROW 1J AFT SECTION. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031300115 20080313 00115 SO 2008 3 13 SIMA200806503 1 20080303 A 2150 A/C PACK EMB 145 EMB145LR 3260212 SO ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 21 699AE 14500883 ON FLIGHT 3856, CREW REPORTED DURING DESCENT, PACKS PRODUCED ODD ODOR (POSSIBLY OIL) FOLLOWED BY PACK 2 OVERHEAT, AIRCRA FT REMOVED FROM SERVICE. PERFORMED VISUAL INSPECTION OF OIL LEAKAGE AND ALSO PERFORMED BOROSCOPE INSPECTION FOR OIL LEA KAGE. NO EVIDENCE OF OIL FOUND. GROUND RUN A/C AND NO ABNORMAL OIL SMELL DETECTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008031000185 20080310 00185 NM 2008 3 10 DHL2008763504 1 20080301 A 5311 FRAME BOEING 727 727264 138408M NM BS 500 S16-17R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 763AT 22983 FRAME GOUGED AND DENTED AT BS 500 ABOVE STR 17R. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED FRAME REPAIR FROM 7075 T6, .063 INCH BY 7.25 INCH BY 3.25 INCH, PO NR 9006027, PER B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2008031000210 20080310 00210 EA 2008 3 10 COMA0860147 1 20080226 A 2613 355862255 SENSING ELEMENT CNDAIR CL600 CL6002B19 1900309 EA RT FUSELAGE FAILED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 938CA 7046 FLIGHT 5450- EN ROUTE FROM CVG TO GRR RECEIVED ANTI-ICE DUCT WARNING MESSAGE. PERFORMED QRH, MESSAGE WENT OUT, WING AN TI-ICE WAS TURNED TO STANDBY AND AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED RIGHT FUSELAGE S ENSING ELEMENT. 2 L 7 2 4F RT A21EA 2008031000218 20080310 00218 EA 2008 3 10 COMA0860152 1 20080301 A 5346 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 819CA 7415 ENGINE BEAM UPPER CENTER SKIN IS CRACKED ON AFT SIDE FS 640 BETWEEN RBL 0 AND RBL 9 AT FIRE LOOP FASTENER HOLE. REPAIRE D UPPER ENGINE BEAM CENTER SKIN WITH A PERMANENT REPAIR PER REO 601R-53-61-345 REV F. 2 L 7 2 4F RT A21EA 2008031000222 20080310 00222 EA 2008 3 10 COMA0860155 1 20080301 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 958CA 7111 FLIGHT 5359 - ON CLIMBOUT FROM LEX, RECEIVED PAX DOOR WARNING MESSAGE, MESSAGE WENT OUT 15-20 SECONDS LATER. RAN QRH AN D AIRCRAFT RETURNED BACK TO LEX AND LANDED SAFELY. PERFORMED OPS CHECK OF PAX DOOR WARNING SYSTEM. OPS CHECK GOOD AND NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2008031000256 20080310 00256 WP 2008 3 10 AALA200800385 1 20080222 A 3000 GASKET DOUG DC9 DC982 3022082 WP ICE PROTECTION LEAKING A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 402A 49313 TPA INFLIGHT T1679/22FEB - DURING CLIMB, TAIL COMPARTMENT HIGH TEMPERATURE AND PRESSURE FLOW INDICATION ILLUMINATED. RE TURNED TO TPA AND LANDED WITHOUT INCIDENT. FOUND AIR LEAKING AT BASE OF RIGHT ICE PROTECTION HIGH TEMPERATURE SENSOR. REPLACED SENSOR GASKET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031000261 20080310 00261 SO 2008 3 10 FDKA200803089 1 20080304 A 2430 BONDING STRAP EMB 145 EMB145LR 3260212 SO WING CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 835MJ 145353 BONDING STRAP ON PANEL 6731 IS CORRODED. THE CORRODED STRAP HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008031000272 20080310 00272 NM 2008 3 10 KCSA081144 1 20080306 A 5312 BULKHEAD BOEING 747 747209B 138489B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 AFT PRESSURE BULKHEAD HOLE 95L HAS PITTING AT STR-18L ON FWD SIDE. 2 L 7 4 4F RT A20WE 2008031000275 20080310 00275 WP 2008 3 10 AALA200800386 1 20080222 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 289AA 49301 LGA - EMERGENCY FLASHLIGHT AT AFT CABIN MISSING STRAP. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT CABIN. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008042100034 20080421 00034 2008 4 21 2008UALA02079 4 20080409 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR SLIDE UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 597UA 28750 1R WILL NOT ARM. FOUND SLIDE LANYARD INTERFERENCE. SECURED LOOSE RAFT LANYARD, DOOR ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042100037 20080421 00037 NM 2008 4 21 2008UALA02138 1 20080412 A 2121 033638500 FAN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 652UA 25390 "FWD DET FAN" MAINTENANCE MESSAGE, WILL NOT CLEAR. SUSPECT FAULTY FAN AND OR PRESSURE SWITCH. REPLACED FAN AND PRESSUR E SWITCH OPS CHECK GOOD MESSAGE CLEARED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042100039 20080421 00039 NM 2008 4 21 2008UALA02140 1 20080412 A 3610 VALVE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE PNEUMATIC SYS FAILED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 673UA 29241 RIGHT ENG PRV EICAS CAME ON IN DESCENT. FOUND FAULTY PRESSURE REGULATING VALVE AND CONTROLLER REPLACED PRV PER MM36-11 -18 & CONTROLLER PER MM36-11-08. OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042100041 20080421 00041 EU 2008 4 21 2008UALA02142 1 20080412 A 2560 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FLASHLIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 415UA 475 FLASHLIGHT AT FWD F/A JUMPSEAT INOP. FOUND BATTERY INOP. REPLACED FLASHLIGHT BATTERY OPS CKS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042100042 20080421 00042 EA 2008 4 21 REXA200800008 1 20080413 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A REXA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 SO 25 8623A 7623 ON APPROACH, FLAPS FAILED AT ZERO WHEN SELECTED DOWN. QRH FOLLOWED UNEVENTFUL ZERO FLAP LANDING. SYSTEM RESET PER FIM 27-50 AND PLACED ON SEVENTY TWO HOUR WATCH. 2 L 7 2 4F RT A21EA 2008042100046 20080421 00046 NM 2008 4 21 2008UALA02002 1 20080404 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 781UA 26945 AFT EMERGENCY LIGHT MISSING FROM ARMREST AT SEAT 1F. SUPPLEMENTAL DATA UPDATE REPLACED BROKEN EEL LIGHT WITH NEW ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042100047 20080421 00047 2008 4 21 2008UALA02032 4 20080408 A 2565 101655305 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DOOR SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 ASPIRATOR LEAKS. REPLACED ASPIRATOR LEAK CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042100048 20080421 00048 NM 2008 4 21 2008UALA02003 1 20080405 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 1F AFT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 1F MISSING 1 AFT EMERGENCY LIGHT STRIP. SUPPLEMENTAL DATA UPDATE, REPLACED LIGHT STRIP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042100049 20080421 00049 NM 2008 4 21 2008UALA02033 1 20080408 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 947 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 AFT CABIN FLOORBEAM UPPER CAP AT BS 947.5 IS CORRODED FROM RBL12 TO LBL 24. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCO MPLISHED: INSTALLED 'T' CHORD AND SPLICE ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042100050 20080421 00050 NM 2008 4 21 2008UALA02034 1 20080409 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 809UA 825 FOUND FLOORBEAM 145 CORRODED WHILE ACCOMPLISHING EQ3700 CALLOUT. REMOVED BEAM. INSTALLED SECTION 145,140 AND 90 AS A UN IT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042100056 20080421 00056 NM 2008 4 21 2008UALA02018 1 20080407 A 5320 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 809UA 825 FOUND RT AFT DOOR SILL BEAM CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED, REMOVED RT AFT DOOR SILL. PI CKED UP HOLES IN FUSELAGE SKIN AND FWD AND AFT FRAMES ON SILL. REWORKED SILL. REPLACED SILL ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042100060 20080421 00060 EU 2008 4 21 YENA2008031 1 20080408 A 7830 THRUST REVERSER AIRBUS 320 A320232 3930326 EU MALFUNCTIONED A YENA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 510JB 1280 FLT 553, EWR-RSW, DIVERTED TO CLT, ENG 1 REVERSER FAULT (THRUST REVERSER SYSTEMS). REACTIVATED NR 1 T/R IAW MM 78-30-00 , PERFORMED OPERATIONAL CHECK IAW MM 78-31-00, COULD NOT DUPLICATE ANY OF THE FAULT. OK FOR SERVICE. 2 L 7 2 4F RT A28NM 2008042100061 20080421 00061 NM 2008 4 21 UPS08M51973 1 20080127 A 5751 SKIN DOUG MD11 MD11 3023602 NM RT IB AILERON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP INSPECTION TYPE:C RIGHT I/B AILERON FOUND CHAFE MARKS ALONG L/E LOWER SKIN I/B SIDE. CHAFED SKIN REMOVED PER SRM 51-35- 01V.2R.40. HOLES ON NEW SKIN PICKED UP PER SRM 51-31-01 V.2 R.40. NEW SKIN INSTALLED AS PER SRM 51-35-01 V.2 R.40. 2 L 7 3 4F RT A22WE 2008042100062 20080421 00062 NM 2008 4 21 CALA0800197 1 20080305 A 5340 6916970501 ATTACH FITTING BOEING 737 7373T0 1384582 NM BS 384 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69333 23571 STA 384.2 LEFT SIDE S-15 ATTACH CLIP CRACKED. REMOVED AND REPLACED CRACKED CLIP AT BS 348.2 STRINGER 15 LT PER ECRA 531 0-04726. 2 L 7 2 4F RT A16WE 2008042100063 20080421 00063 EU 2008 4 21 WRNA20080010 1 20080408 A 7500 A3111028200000 DUCT AIRBUS 300 A300B4203 3930306 EU BLEED SYS CRACKED A WRNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 504TA 216 AFTER TAKEOFF, NR 1 AND NR 2 BLEED FAULT LIGHTS AND APU MANIFOLD LIGHTS CAME ON AND WOULD NOT RESET. DUMPED 18,000 POU NDS OF FUEL AND RETURNED TO FIELD FOR A SAFE LANDING. FOUND NR 2 ENGINE BLEED AIR DUCT IN AIR CONDITIONING BAY CRACKED. REPLACED DUCT IAW 36-11-00 PG 605, LEAK CHECKED IAW 71-00-00. CHECKED FAULT LIGHTS IAW 26-16-00 PAGE 501, ALL SYSTEM S WORK NORMAL. AIRCRAFT RELEASED TO SERVICE. 2 L 7 2 4F RT A35EU 2008042100066 20080421 00066 EA 2008 4 21 COMA0870013 1 20080404 A 3010 GG670804023 ELEMENT CNDAIR CL600 CL6002C10 1390015 EA ANTI ICE SYS FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 391CA 10108 FLIGHT 5100 - EN ROUTE PIT-CVG RECEIVED AN ANTI-ICE DUCT WARNING MESSAGE, CREW DECLARED EMERGENCY AND FLIGHT LANDED WITH OUT INCIDENT. REPLACED THE LEFT WING INBOARD LEADING EDGE WING SENSING ELEMENT. 2 L 7 2 4F RT A21EA 2008042100070 20080421 00070 EA 2008 4 21 COMA0860216 1 20080407 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA FS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 957CA 7109 DURING HMV - NR 6 INSPECTION, NDT INSPECTION FOUND A CRACK ON THE FS 559 WEB. CUT OUT DAMAGE AND INSTALLED DOUBLERS IAW REO 601R-53-41-260. 2 L 7 2 4F RT A21EA 2008042100071 20080421 00071 EA 2008 4 21 COMA0860217 1 20080407 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA FS 202.75 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 957CA 7109 DURING HMV NR 6 INSPECTION, VISUAL INSPECTION FOUND FS 202.75 PRESSURE WEB CRACKED AT PARKING BRAKE CABLE CUTOUT. ENLAR GED CUTOUT TO REMOVE DAMAGE AND INSTALLED A DOUBLER PER CRJ REO 601R-53-11-563. 2 L 7 2 4F RT A21EA 2008042100073 20080421 00073 NM 2008 4 21 CALA0800321 1 20080411 A 3297 1061226211 LOGIC CARD BOEING 737 7373T0 1384582 NM MLG MALFUNCTIONED A CALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 27 76354 23592 C/B AIR GROUND RELAY, LIGHTS AND LATCH, AND PRESSURE WARNING C/B POPPED IN FLIGHT. GEAR DID SHOW NO GREEN MISSED APPROA CH, RAN CHECKLIST AND SHOWED THREE GREEN FINALLY. T/S PER WD 32-31-01 PAGES 1, 2 AND 3 SHORT TO GROUND ON WIRES W242-05 6-22, W154-193-22 AND W328-043-22. REPLACED M991 LOGIC CARD FOR AIR SENSE SQUAT SWITCH. PERFORMED GEAR SWING, OPS CHEC K OF LOGIC CARD PER 32-09-20 SATISFACTORY. 2 L 7 2 4F RT A16WE 2008042100076 20080421 00076 NM 2008 4 21 CALA0800323 1 20080403 A 5311 654654967 FRAME BOEING 737 737524 1384721 NM BS 767 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 FRAME AT BILGE AREA AT STA 767 RBL 10" IN AFT CARGO FOUND CORRODED. CORROSION FOUND TO BE OUT OF LIMITS PER B737-500 SR M 53-00-07 & 53-60-07. REMOVED CORROSION PER B737-500 SRM 53-00-07, ACCOMPLISHED REPAIR PER 13-737-500 SRM 53-00-07 REP AIR 8. 2 L 7 2 4F RT A16WE 2008042100080 20080421 00080 NM 2008 4 21 CALA0800318 1 20080410 A 5210 507945 PAN BOEING 737 737524 1384721 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 46625 27529 L1 DOOR PAN CRACKED AT AFT EDGE AROUND STOP PIN BRACKET 4TH FROM BOTTOM. INSTALLED REPAIR ANGLE REF ECRA 5210-02014. 2 L 7 2 4F RT A16WE 2008042100081 20080421 00081 NM 2008 4 21 CALA0800319 1 20080410 A 5315 141T5107 FLOORBEAM BOEING 767 767224 1385170 NM BS 303 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76151 30430 CABIN FLOOR SUPPORT FOUND CORRODED AT BS 303 BETWEEN LBL 21 - 54, AFTER FLOOR PNL REMOVED. CABIN STA 303 BETWEEN LBL 17 "- 68" FLOORBEAM REPAIRED AS PER SRM 53-00-51 FIG 201 REPAIR 1 AND HFEC NO CRACK FOUND. 2 L 7 2 4F RT A1NM 2008042100082 20080421 00082 2008 4 21 WRNA20080011 4 20080408 A 2565 D30457104 SLIDE AIRBUS 300 A300B4203 3930306 EU R1 DOOR NO TEST A WRNA K NONE L NO TEST IN INSP/MAINT 1 SO 05 506TA 207 DURING OPERATIONAL TEST, THE R-1 DOOR ESCAPE SLIDE/RAFT FAILED TEST, DID NOT FULLY INFLATE. REPLACED ESCAPE SLIDE/RAFT CONTACTED MAINTENANCE STATION WERE TEST WAS ACCOMPLISHED. SLIDE BOTTLE PRESSURE INDICATOR WAS IN THE 'GREEN', SLIDE DEP LOYED BUT DID NOT FULLY INFLATE, APPEARED TO RUN OUT OF AIR. THE VENDOR HAS BEEN NOTIFIED OF FAILURE AND RELATED EVENTS , WAITING ON VENDOR TEARDOWN REPORT AS TO CAUSE OF PARTIAL INFLATION. AIRCRAFT HAS BEEN RELEASED TO SERVICE. 2 L 7 2 4F RT A35EU 2008042100090 20080421 00090 NM 2008 4 21 ZZDA2008088 1 20080411 A 5320 J0602289 PAN BOEING 717 717200 1383700 NM CARGO DOOR FRAME CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 987AT 55088 AFT CARGO COMPARTMENT LOWER DOOR FRAME PAN CORRODED BEYOND LIMITS. TRIMMED OUT AFT CARGO AREA, PERFORMED HFEC INSTALLED SPLICES AND NEW PAN PER B717 SRM 52-20-15. 2 L 7 2 4F TR A6WE 2008042100091 20080421 00091 NM 2008 4 21 CALA0800329 1 20080414 A 5320 65C3397053 INTERCOSTAL BOEING 737 737524 1384721 NM BS 344-360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 INTERCOSTAL BETWEEN STA 344 AND 360 BL 0 CRACKED. REMOVED AND REPLACED INTERCOSTAL PART NUMBER 65C33970-53 STA 344-360, BL 0, REF SRM 51-40-02 & BOEING INSTALLATION DWG 65C33970. 2 L 7 2 4F RT A16WE 2008042100092 20080421 00092 2008 4 21 CALA0800330 4 20080413 A 2565 65C199015 LATCH BOEING 737 737524 1384721 NM R2 DOOR SLIDE FRAYED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16607 27320 R-2 DOOR ESCAPE SLIDE LATCH CABLE HAS BROKEN STRANDS. REPLACED SLIDE CABLE P/N 65C19901-15 PER 737-3/5 MM 25-61-35. 2 L 7 2 4F RT A16WE 2008042100096 20080421 00096 EA 2008 4 21 COMA0860224 1 20080413 A 2731 70623 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA ELEVATOR TRIM FAULTY A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 587SW 980 7062 FLIGHT 5665 - MOMENTARY ELEVATOR DOWN TRIM ON TAKEOFF. ABORTED TAKEOFF SAFELY. REMOVED AND REPLACED MCU. 2 L 7 2 4F RT A21EA 2008042100102 20080421 00102 2008 4 21 YENA2008032 4 20080414 A 2330 LSEBUTK1400101 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU ENTERTAIN SYS FAULTY A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 598JB 1410 1410 2314 FLT 760, SJU-BOS, FLT ATTENDANT DETECTED BURNED ELECTRICAL ODOR AROUND MID CABIN (ROWS 6-8) ABOUT 1 HOUR AND 20 MINUTES INTO FLT. THE LTV'S WERE TURNED OFF AND THE AFT AVIONICS COMP WAS TURNED OFF. ODOR QUICKLY DISSIPATED. ACCOMPLISHED E LEC ODOR SYS INTEGRITY CK IAW LTV MM 23-39-00. INSPECTED ROWS 4 THRU 10 A,B,C,D,E,F. FOUND J-1 CABLE AT 8A,B,C PARTIAL LY DISCONNECTED. REMOVED AND REPLACED 8 THRU 7 A,B,C XEB CABLE AND 8A,B,C SEB IAW LTV MM 44-20-17, 23-39-00. FOUND BEN T PIN AT 6D,E,F J-3 CABLE. REMOVED AND REPLACED J-3 CABLE AND SEB AT 6D,E,F IAW LTV MM 44-20-17, 23-39-00. SYS OPS CHE CKS GOOD IAW LTV MM 23-39-00 AND 44-20-17. 2 L 7 2 4F RT A28NM 2008042100104 20080421 00104 2008 4 21 WRLA2008044 4 20080414 A 2565 SWD23100101 SLIDE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE L1 DOOR DISLODGED A WRLA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 11 14075 46922 L1 DOOR SLIDE DROPPED OUT WHEN DOOR OPENED PNEUMATICALLY, SLIDE DID NOT DEPLOY CORRECTLY. REMOVED AND REPLACED SLIDE AS SY IAW MM 25-61-01. SERVICED PNEUMATIC DOOR ASSIST. 2 L 7 3 4F 4 F A22WE E23EA 2008042100106 20080421 00106 NM 2008 4 21 CALA0800331 1 20080405 A 5320 BAC1505100120 INTERCOSTAL BOEING 737 737524 1384721 NM BS 344-360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 INTERCOSTAL FOUND CRACKED BETWEEN BS 344 TO BS 360 AT LBL 10". REPAIRED INTERCOSTAL AT STA 344-360 LBL 10 IAW EC/RA 531 0-03585 (REV C). 2 L 7 2 4F RT A16WE 2008031000310 20080310 00310 NM 2008 3 10 AALA200800436 1 20080228 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 687AA 25695 DFW - EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RI GHT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008031000317 20080310 00317 NM 2008 3 10 AALA200800431 1 20080228 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 755AN 30263 JFK EMERGENCY LIGHT AT SEAT 22C HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008031000324 20080310 00324 EA 2008 3 10 TRAX200800356 1 20080228 A 2751 DETECTOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 867AS 7463 FLAPS FAIL AT 0, EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS A PRECAUTION, FLT 4902 CX. DURING FERRY FLT NR 9 953 GRR-ATL, EMERGENCY EQUIPMENT WAS ALSO REQUESTED TO BE ON STANDBY INTO ATL. REMOVED AND REPLACED SKEW DETECTOR AND A DJUSTED LT O/B BPSU AS REQUIRED, OP CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2008031000344 20080310 00344 EU 2008 3 10 2008UALA00646 1 20080205 A 3260 SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG OUT OF ADJUST A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 442UA 780 RTFL DUE TO INABILITY TO RETRACT LANDING GEAR. FOUND NLG SENSORS 24GA & 25GA OUT OF ADJ. ADJUSTED SENSORS 24GA AND 2 5GA. ACCOMPLISHED SEVERAL TESTS OF NLG INCLUDING MANUAL EXTENSION, ALL SATISFACTORY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031000353 20080310 00353 WP 2008 3 10 AMTA200800099 1 20080217 A 3350 LIGHT DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A AMTA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 11 705TZ 46915 EMERGENCY LIGHT (FLOOR RED) L-2 DOOR INOPERATIVE. REMOVED AND REPLACED L2 DOOR FLOOR RED LIGHT MODULE IAW 33-51-03. OP S CHECK GOOD. (K) 2 L 7 3 4F A22WE 2008031000369 20080310 00369 EA 2008 3 10 A6WA200840099 1 20080214 A 2820 FUEL LINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUEL SYSTEM LEAKING A A6WA O OTHER K FLUID LOSS NR NOT REPORTED 1 GL 31 425AW 7663 FUEL LEAKING FROM DRAIN UNDER AFT FUSELAGE. REMOVED AND REPLACED FUEL LINE ASSY IAW 28-20-01. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000371 20080310 00371 EA 2008 3 10 A6WA200840001 1 20080103 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 CRACK FOUND ON AFT PRESSURE BULKHEAD FWD FACE IN LINTEL FITTING ARE FS 621.00 LT. REPAIR PERFORMED ON AFT PRESSURE BULK HEAD FWD FACE IN LINTER FITTING AREA AT FS 621.00 LT IAW REO 601R-53-61-1230, REV C. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000377 20080310 00377 EA 2008 3 10 A6WA200840072 1 20080128 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PAX DOOR TORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 423AW 7636 PAX DOOR STAIR HAVE APPROX 1.5 IN X 1.5 IN TEAR IN FWD FACE SKIN AT FWD HANDRAIL DOWN STOP BRACKET POINT. REPAIRED IAW REO 601R-52-11-702, REV A. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000379 20080310 00379 EA 2008 3 10 A6WA200840074 1 20080201 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 431AW 7256 FLOOR LANDING PLATE CORRODED BETWEEN FS 559 + 112 TO FS 621, AROUND NUT PLATE HOLES. (K) CORROSION ON FLOOR LANDING PL ATE BETWEEN FS 559 PLUS 112 TO FS 621 AROUND NUT PLATE HOLES, BENDED IAW SRM 51-21-06. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000386 20080310 00386 EA 2008 3 10 A6WA200840081 1 20080207 A 5347 CARGO TRACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CARGO BAY CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 431AW 7256 AT FS 559.96 WL 73.50 CARGO TRACK LT AND RT SIDE INNER, OUTER SURFACE CORRODED. (K) BLENDED CARGO TRACKS IAW SRM 51-12 -00. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000394 20080310 00394 EA 2008 3 10 A6WA200840089 1 20080204 A 5350 RADOME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 LIGHT GLAZING ON RADOME FOUND CRACK. (K) REPLACED IAW SRM 51-42-20. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031200023 20080312 00023 EU 2008 3 12 08FDEA00765 1 20080306 A 5414 A54611357200 PANEL AIRBUS 310 A310203 3930313 EU NR 2 NACELLE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 PYLON PANEL NR 424 BR; CHAFED ON THE MATING SURFACES. CUT OUT DAMAGED AREA OF PANEL 424BR IAW SRM 54-52-51 FIG 203 .; SHEETS 1-3. FABBED REPAIR DOUBLER & SHIM. INSTALLED BOTH IAW SRM 54-51-51; FIG 203; SHEETS 1-3. MINOR REPAIR . 2 L 7 2 4F RT A35EU 2008031200046 20080312 00046 NM 2008 3 12 UPS08M51739 1 20080212 A 5720 STRAP DOUG MD11 MD11F 3023600 NM LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:1C LEFT WING LE COMPARTMENT XORS 580 HAS STRAP CRACKED. REMOVED, FABRICATED, AND INSTALLED STRAP IAW MD -11 SRM 51-33-01, MD-11 SRM 51-21-01, AND DWG: ARB3954. 2 L 7 3 4F RT A22WE 2008031200048 20080312 00048 NM 2008 3 12 2008UALA01073 1 20080227 A 5210 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 DOOR 2R UPPER HINGE ARM CUTOUT REQUIRES DOUBLER. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED A MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031200053 20080312 00053 NM 2008 3 12 2008UALA01078 1 20080227 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1520 S22-24R GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 AFT PIT FRAME GOUGED NUMEROUS PLACES AT BS 1520 BETWEEN STR 22R AND STR 24R. ACCOMPLISHED A MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031200054 20080312 00054 NM 2008 3 12 2008UALA01080 1 20080227 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1520 S24-26R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 AFT PIT FRAME AT BS 1520R, STR 24.5R - 26R HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031200056 20080312 00056 NM 2008 3 12 2008UALA01082 1 20080227 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1420 S26L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 AFT PIT FUSE STA 1420 AT STR 26L HAS DAMAGE. ACCOMPLISHED A MAJOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031200057 20080312 00057 NM 2008 3 12 2008UALA01083 1 20080227 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1620 S26R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 533UA 25073 AFT PIT FUSELAGE STA 1620 FRAME AT STR 26R. ACCOMPLISHED A MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031200059 20080312 00059 NM 2008 3 12 2008UALA01090 1 20080229 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 47 INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 FOUND EMERGENCY LIGHT SEAT 47 HJK INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031200060 20080312 00060 NM 2008 3 12 2008UALA01092 1 20080229 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 104UA 26902 EEL INOP E ZONE RT FWD COLUMN. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008031200061 20080312 00061 NM 2008 3 12 2008UALA01093 1 20080229 A 5497 D4256J CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 NACELLE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 NR 2 PYLON J BOX CONNECTOR D4256J IS DAMAGED BY HEAT. REPLACED CONNECTOR D4256J PER BSWPM 20-63-13. OPS CHECK ACCOMP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031200062 20080312 00062 NM 2008 3 12 2008UALA01095 1 20080229 A 5497 D4148J CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 NACELLE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 NR 2 PYLON J BOX CONNECTOR D4148J IS DAMAGED BY HEAT. REPLACED CONNECTOR D4148J PER BSWPM 20-63-13. OPS CHECK ACCOMP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031200065 20080312 00065 NM 2008 3 12 2008UALA01098 1 20080229 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 266 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 MAIN CABIN AT STA 266.5 FLOORBEAM AT RBL 70.5 IS CRACKED ON UPPER FLANGE. REMOVED DAMAGE SECTION OF "T" CAP, INSTALLED "T" CORD AND 2 EA REPAIR ANGLE PER SRM 53-00-5 1, RPR 6. DAMAGE REMOVED STA 266.5, RBL 71 TO 49. 2 L 7 2 4F 4 F RT A1NM E24NE 2008031200067 20080312 00067 NM 2008 3 12 2008UALA01100 1 20080228 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 963-984 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 AFT ENTRY DOOR CUTOUT INNER CREASE BEAM CORRODED AT NUT PLATE HOLES AND UPPER SURFACE, BS 963-984 STR 17L. MAJOR REPAIR ACP'D BY REPLACING CREASE BEAM REF SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031200069 20080312 00069 NM 2008 3 12 2008UALA01102 1 20080228 A 5320 FLOOR SUPPORT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 1006-1016 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 AFT CABIN DIAGONAL FLOOR SUPPORT CORRODED AT FASTENER HOLES ON UPPER FLANGE BS 1006 TO 1016 AT LBL6 TO LBL8. REPLACED A FT CABIN DIAGONAL FLOOR SUPPORT REF SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031200070 20080312 00070 NM 2008 3 12 2008UALA01103 1 20080228 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 616 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 FUSELAGE FRAME IS CRACKED BELOW CABIN FLOOR AND OVERWING ON LT SIDE BS 616 (REFMM53-11-89-801) REF NR13410-2400-0007. M AJOR REPAIR ACP'D. REMOVED DAMAGE AND VERIFIED WITH HFEC. INSTALLED A FILLER AND A REPAIR ANGLE PER MM 53-11-89-801. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300005 20080313 00005 NM 2008 3 13 2008UALA01108 1 20080228 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S10L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 STRINGER CLIP CRACKED BS 360 STR 10L, REF NR13349-8600-0008. REMOVED AND REPLACED DAMAGED STRINGER CLIP REF SRM 51-40-0 2 PG 1-4. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300006 20080313 00006 NM 2008 3 13 CALA0800195 1 20080305 A 5311 69489852 FRAME BOEING 737 737524 1384721 NM BS 360 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18622 27526 FRAME CRACKED AT STA 360 BETWEEN STRINGER 8L AND 9L. TRIMMED OUT CRACKED AREA ON FRAME AND INSTALLED REPAIR DOUBLERS PE R ECRA 5310-04728. REPLACED INTERCOSTAL CLIP AT STA 360 STRINGER 8L PER ECRA 5310-04728. 2 L 7 2 4F RT A16WE 2008031300018 20080313 00018 2008 3 13 LYNX009 4 20080228 A 3425 42000332501 AHRS BOMBDR DHC8 DHC8402 1390042 NM NR 1 MALFUNCTIONED A 3LYA O OTHER J WARNING INDICATION CR CRUISE 1 NM 21 506LX 4176 ELEVATOR FEEL CAUTION LIGHT IN FLIGHT. AHRS1 FAIL MESSAGE ON FMS AND ADC1 FAILED. NO OTHER ASSOCIATED LIGHTS. SCHEDUL ED LANDING IN DENVER. FOUND HARD FAULT IN NR 1 AHRS. REMOVED AND REPLACED NR 1 AHRS PER AMM34-21-01-000-801 AND 34-21- 01-400-801. PERFORMED OPERATIONAL TEST PER AMM 34-21-00-710-801. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2008031300022 20080313 00022 WP 2008 3 13 UPS08851748 1 20080221 A 5511 SPAR DOUG DC8 DC873F 302199F WP HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 LT HORIZ STAB REAR SPAR WEB CRACKED AT FASTENER HOLES IN 2 PLACES O/B OF I/B HINGE. REPAIRED LT HORI Z STAB REAR SPAR WEB IAW SRM 55-02-00 FIG 002 AND SRM 5 1-1-21. 2 L 7 4 4F RT 4A25 2008031300035 20080313 00035 NM 2008 3 13 2008UALA01118 1 20080301 A 3350 SIGN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 530UA 25043 DOOR 2L EXIT SIGN NOT ILLUMINATED PER CREW. RESECURED STRIP. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031300058 20080313 00058 NM 2008 3 13 2008UALA01132 1 20080302 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 1016 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 AFT CABIN FLOORBEAM CORRODED BS 1016 LBL 8 INCHES-10 INCHES. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED STRAP RE PAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008031300063 20080313 00063 SO 2008 3 13 RAIA00802025 1 20080224 A 5210 LINKAGE EMB 145 EMB145 3260210 SO PAX DOOR LACK OF LUBE A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 801HK 145053 POST FLT 3564 - PIT - MAIN PASSENGER DOOR DIFFICULT TO OPEN AND CLOSE FROM INSIDE THE CABIN. MAINTENANCE LUBED THE DOOR LINKAGE. OPERATIONAL CHECK OF THE DOOR WAS SATISFACTORY. 2 L 7 2 4F RT T00011AT 2008031300081 20080313 00081 NE 2008 3 13 2008UALA01154 2 20080302 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 FAILED A UALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 677UA 30029 727574 NR 2 ENGINE COMPRESSOR STALL AT 1.1 EPR ON T-O ROLL. AFTER RETURN TO THE GATE, MM FOUND METAL IN THE TAILPIPE. ENGINE REPLACED PRIOR TO FURTHER FLIGHT. ESTIMATING SHOP INPUT AT END OF MARCH. TEARDOWN FINDINGS EXPECTED BY END OF APRIL 2 L 7 2 4F 4 F RT A1NM E24NE 2008031300097 20080313 00097 NM 2008 3 13 2008UALA01167 1 20080229 A 2720 PDU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 29 553UA 25277 A/C REQUIRES 4 UNITS R RUDDER TRIM, A-S 255 IAS FL370 CRUISE 4.0 RWD. REPLACED RUDDER RATIO CHANGER, PREVIOUSLY REPLACE D TE FLAP PDU CONTROL VALVE OUTBD CHECK VALVE ADJUSTED RIG OF RUDDER RATIO CHANGER, RUDDER RIG FOUND TO BE OUT OF LIMITS ADJUSTED POGO ROD OF RATIO CHANGER, REPLACED LOWER RUDDER PCU. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031300121 20080313 00121 EU 2008 3 13 08FDEA00710 1 20080305 A 5753 A5796507100200 FAIRING AIRBUS 310 A310203 3930313 EU LT WING TE FLAP MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LEFT WING FLAP FAIRING 533CB IS DELAMINATED IN TWO SPOTS. REPAIRED LEFT WING FLAP FAIRING BY REMOVING THE DAMAGE. CLEAN ED & PREPED FOR THE APPLICATION OF A WET LAY UP. APPLIED, CURED & SANDED THE WET LAY UP. CLEANED & PREPPED FOR REFINIS H. APPLIED REFINISH IAW SRM 57-20-35, SRM 51-40-13, SRM 51-23-10 & SRM 51-40-10. 2 L 7 2 4F RT A35EU 2008031300123 20080313 00123 EU 2008 3 13 08FDEA00712 1 20080305 A 7830 SLEEVE AIRBUS 310 A310203 3930313 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 2 ENGINE OUTBD T/R TRANSLATOR SLEEVE IS CRACKED IN THE UPPER CORNER. REMOVED OLD SEALANT AND RESEALED IAW SRM 51-76- 10 AND 51-10-30. PAINTED IAW SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008031300129 20080313 00129 EU 2008 3 13 08FDEA00718 1 20080305 A 5532 PANEL AIRBUS 310 A310203 3930313 EU VERTICAL STAB DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 VERTICAL STABILIZER PANEL 325DL (ACTUATOR ACCESS PNL), FWD SECTION IS DELAMINATED. RESTORED FINISH PER SRM 51-75-10. REPAIRED BY REMOVING DAMAGE AND APPLYING A 250 DEGREE PREPREG LAYUP IAW SRM55-33-13. 2 L 7 2 4F RT A35EU 2008031300130 20080313 00130 EU 2008 3 13 08FDEA00720 1 20080305 A 5420 A54610805 DRAIN PAN AIRBUS 310 A310324 3930206 EU NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 NR 2 ENGINE PYLON HYDRAULIC/FUEL DRAIN PAN IS CRACKED IN 4 PLACES ON THE BOTTOM SIDE OF THE PAN. REMOVED DRIP PAN IAW A IRBUS A310 SRM 51-40-21; PG 7, WELD REPAIRED CRACKS IAW AEROSPATIALE DWG 41A54610805. REINSTALLED DRIP PAN IAW AIRBUS A 310 SRM 51-40-21; PG 7. 2 L 7 2 4F RT A35EU 2008031300131 20080313 00131 WP 2008 3 13 08FDEA00721 1 20080305 A 5730 ARC0267503 ACCESS PANEL DOUG MD10 MD1010F 3022112 WP LT WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 LT WING PANEL 541BB IS DELAMINATED ON THE BACK SIDE. REPAIRED LT WING CONTROL ACCESS PANEL 541 BB BY FABRICATING & BOND ING NEW INNER & OUTER SKINS, DOUBLERS & CORE IAW EA 8-5710-116968; 2 L 7 3 4F RT A22WE 2008031300133 20080313 00133 WP 2008 3 13 08FDEA00723 1 20080305 A 5730 ARC0264541 PANEL DOUG MD10 MD1010F 3022112 WP LT WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 LT WING PANEL 541GB IS DELAMINATED ON THE BACK SIDE. REPAIRED PANEL 541GB LT WING PANEL BY FABRICATING AND BONDING A SK IN DOUBLER & REPAIR PARTS IAW SRM 51-71-00; VOL II CH 17 & ARC0264 DWG. MINOR REPAIR 2 L 7 3 4F RT A22WE 2008031300139 20080313 00139 WP 2008 3 13 08FDEA00729 1 20080305 A 5350 ANB71042 PANEL DOUG MD10 MD1010F 3022112 WP WING TO FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 RT FUSELAGE, TO WING FILLET PANEL 152GT HAS A CHUNK OUT OF THE LOWER EDGE. REMOVED DAMAGED, CLEANED & PREPPED REPAIR. APPLIED REPAIR PLYS & VAC BAGGED. CURED & SANDED. APPLIED FIBERGLASS SEALER, CURED & SANDED SMOOTH IAW SRM 51-43-01 VOL II PARA 16-A (4) & 16-A (10). APPLIED REFINISH IAW SRM 51-21-02; VOL II. MINOR REPAIR 2 L 7 3 4F RT A22WE 2008031300141 20080313 00141 WP 2008 3 13 08FDEA00731 1 20080305 A 5730 ARC2231 SKIN DOUG MD10 MD1010F 3022112 WP WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 FOUND DELAMINATION ON PANEL NR 535HL EXTERIOR SKIN. REMOVED DAMAGE & REPAIRED PANEL IAW SRM 51-21-01; VOL II. ALODIN ED & PRIMED REPAIR AREA IAW SRM 51-21-01 VOL II. PAINTED PANEL IAW SRM 51-21-01; VOL II. MINOR REPAIR 2 L 7 3 4F RT A22WE 2008032500265 20080325 00265 NM 2008 3 25 2008UALA01614 1 20080321 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INTERMITTENT A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 661UA 27158 EMERGENCY EXIT ROW LIGHTING COMES ON SPORADICALLY FROM ROW 27AB TO DOOR 2L. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042100111 20080421 00111 EA 2008 4 21 COMA0860214 1 20080407 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FS 235 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 957CA 7109 DURING HMV - NR 6 INSPECTION, NDT INSPECTION FOUND CRACKS AT AFT RADIUS LEFT AND RIGHT FOR NLG SPADE DOOR CUTOUT. CUT O UT DAMAGE AND INSTALLED DOUBLERS IAW REO 601R-53-11-010. 2 L 7 2 4F RT A21EA 2008042100119 20080421 00119 NM 2008 4 21 CALA0800328 1 20080405 A 5240 6545855U122 ANGLE BOEING 737 737524 1384721 NM R2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 R2 DOOR Z-ANGLE CORRODED AT SILL AREA. REMOVED R-2 DOOR Z-ANGLE IAW B737 SRM 51-40-02. LOCATED AND DRILLED NEW Z-ANGLE IAW B737 SRM 51-40-02. INSTALLED Z-ANGLE IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008042100124 20080421 00124 NM 2008 4 21 08FDEA01452 1 20080418 A 5340 69202616 BRACKET BOEING 727 727232 1384082 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 E/E COMPARTMENT LEFT SIDE E1-1 RACK, SHELF FOR POWER SUPPLY TRANSFER RECTIFIER UNIT CRACKED AT FOWARD INBOARD SIDE. REM OVED MOUNTING SHELF, REMOVED DAMAGED BRACKET, FABRICATED NEW BRACKET, TREATED AND PRIMED AND INSTALLED BRACKET, RE SECUR ED E1-1 SHELF. REF DWG 69-20261, SRM 51-30-2 PG 2, 51-10-2 PG 1. 2 L 7 3 4F A3WE 2008042100127 20080421 00127 NM 2008 4 21 08FDEA01455 1 20080418 A 3230 TORQUE LINK DOUG MD11 MD11F 3023600 NM LT MLG SHEARED A FDEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 574FE 48499 LEFT MAIN LANDING GEAR TORQUE LINK SHEARED DURING PUSH-BACK. 2 L 7 3 4F RT A22WE 2008042100129 20080421 00129 NM 2008 4 21 QXEA200800385 1 20080414 A 2721 8DK4075001 CONTROL PANEL BOMBDR DHC8 DHC8402 1390042 NM RUDDER TRIM MALFUNCTIONED A QXEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 09 405QX 4047 LAX- FLIGHT 2472. RUDDER TRIM RUNAWAY TO THE RIGHT. CREW WAS APPLYING TRIM TO THE LEFT. RETURNED TO THE FIELD AND ACCO MPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE AILERON/RUDDER TRIM CONTROL PANEL. OPERATIONAL CHECKS GOOD. AI RCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008042100131 20080421 00131 NM 2008 4 21 QXEA200800379 1 20080416 A 5240 SEAL BOMBDR DHC8 DHC8402 1390042 NM SERVICE DOOR DIRTY A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 404QX 4046 PDX- FLIGHT 2339 - RIGHT SERVICE DOOR HARD TO CLOSE. MAINTENANCE CLEANED AND LUBRICATED THE DOOR SEAL. OPERATIONAL CHE CKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008042100132 20080421 00132 EA 2008 4 21 QXEA200800380 1 20080416 A 5210 LATCH CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR LACK OF LUBE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 609QX 10031 SJC - FLIGHT 2577 - MAIN CABIN DOOR HARD TO LATCH SHUT. MAINTENANCE LUBRICATED THE LATCH. OPERATIONAL CHECKS GOOD. A IRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2008042100134 20080421 00134 NM 2008 4 21 QXEA200800382 1 20080416 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM MAIN PAX MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 428QX 4160 SEA - FLIGHT 2278 - AFT PASSENGER DOOR HARD TO CLOSE. MAINTENANCE COULD NOT DUPLICATE PROBLEM. RETURNED TO SERVICE. N O PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008042100139 20080421 00139 CE 2008 4 21 GUUA04160801 1 20080416 A 5313 1144200271 LONGERON BEECH 1900 1900D 1154162 CE BS 107 CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 231YV UE231 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED TWO INCH CRACK ON COCKPIT RIGHT UPPER LONGERON AT FS 107.0 AND WL 119.0. REMOVED DAMAGED SECTION OF LONGERON AND INSTALLED FILLER PROFILE TO MATCH REMOVED SECTION OF LONGERON. FABRICATED AND INSTALLED REINFORCEMENT ANGLE IN ACCORDANCE WITH FAA APPROVED DATA CONTAINED IN BEECHCRAFT FIELD REPAIR FR-CO-01729, RE V 2. 2 L 7 2 4T RT A24CE 2008042100140 20080421 00140 WP 2008 4 21 NWAA081629944 1 20080416 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1309T 47316 DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 2 L 7 2 4F A6WE 2008042100143 20080421 00143 SO 2008 4 21 SWIA200819481 1 20080228 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 251YV 120251 FLOOR FRAME IN CARGO AREA IS CORRODED, FOUND AT C-CHECK. REPLACED FLOOR FRAME IN CARGO AREA IAW EMB 120 51-10-02 PG 3 S ECT 3A. 2 L 7 2 4T RT A31SO 2008042100148 20080421 00148 EA 2008 4 21 SWIA200819486 1 20080415 A 2910 LINE CNDAIR CL600 CL6002D24 1390016 EA HYD SYSTEM LEAKING A SWIA O OTHER K FLUID LOSS AP APPROACH 1 NM 07 809SK 15086 FLT 3747 - "HYD EDP 2A" CAUTION MESSAGE APPEARED ON APPROACH AND QUANTITY SHOWED 0 PERCENT. REPAIRED LEAKING THRUST REV ERSER HYDRAULIC LINE. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2008042300003 20080423 00003 WP 2008 4 23 NWAA081679988 1 20080418 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8944E 47167 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINT ENANCE REPLACED THE BATTERIES IN THE BATTERY PACK B5-28. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F A6WE 2008042300005 20080423 00005 NM 2008 4 23 2008UALA02175 1 20080415 A 2612 G718505 CONTROL PANEL BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CARGO FIRE FAILED A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 918UA 25385 FOUND NR 1 CARGO FIRE BOTTLE DISCHARGED TO DIVERTER VALVE. LOOSENED LINE AT BOTTOM OF BOTTLE TO RELIEVE HALON TRAPPED I N LINE. CONNECTOR FOR PRESSURE SWITCH ON BOTTLE DISCONNECTED. PER FLT CREW, DISCHARGE BUTTON WAS NOT PUSHED. REPLACED THE CARGO FIRE DETECTION AND SUPPRESSION CONTROL PANEL. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042300011 20080423 00011 EA 2008 4 23 MASA200800291 1 20080404 A 2150 GG670950091 ACM CNDAIR CL600 CL6002D24 1390016 EA A/C BAY MALFUNCTIONED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 929LR 8791 15029 ASH FLT 2944 PHX - EUG. SMOKE & SMELL FROM RIGHT PACK IN CABIN. PLACED RIGHT PACK ON MEL. 2 L 7 2 4F RT A21EA 2008031300148 20080313 00148 NM 2008 3 13 08FDEA00739 1 20080306 A 5313 A6A7112511 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 604FE 48460 CRACK FOUND DURING X-RAY INSPECTION AT STATION 6-100, LONGERON NR 3R STRINGER SPLICE. FOUND CRACK LENGTH APPROXIMATELY 1 INCH. CRACKED SPLICE AT STATION 6-100, LONGERON 3R REMOVED AS PER SRM 51-31-01, VOL.2. NEW SPLICE FABRICATED AS PER DRAWING A6A7112 AND INSTALLED AS PER SRM 51-31-01, VOL.2. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008031300153 20080313 00153 NM 2008 3 13 08FDEA00744 1 20080306 A 5320 146N541613 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD STRINGER L7.55, STA 1320-1340, TO EVALUATE EXISTING REPAIR. EXISTING REPA IR FOUND NOT IAW B757-200 SRM 51-70-11 FIG 1 DETAIL I, II. AFT CARGO FLOORBOARD STRINGER REPLACED IAW B757-200 SRM 51-1 0-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008031300154 20080313 00154 NM 2008 3 13 08FDEA00745 1 20080306 A 5320 146N541613 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD STRINGER L16.10, STA 1320-1340, TO EVALUATE EXISTING REPAIR. EXISTING REP AIR FOUND NOT IAW B757-200 SRM 51-70-11 FIG 1 DETAIL I, II. AFT CARGO FLOORBOARD STRINGER REPLACED IAW B757-200 SRM 51- 10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008031300156 20080313 00156 NM 2008 3 13 08FDEA00747 1 20080306 A 5312 BULKHEAD BOEING 727 727227 1384078 NM ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 486FE 21489 NOSE W/W BS 351 BULKHEAD RBL 6", SKIN IS WORN FROM CONTACT WITH HYD HOSE CLAMP. BLENDED DAMAGE AREA AT NOSE W/W BS 351 BULKHEAD RBL 6. SKIN REF SRM 53-10-1 FIG 1, MEASURED THICKNESS, ORIGINAL "T" .073", MATERIAL REMAINING .058", FOUND TO BE WITHIN LIMITS REF EA NR 7-5310-113972. TREATED AND PRIMED AND PAINTED AREA REF SRM 51-10-2, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008031300163 20080313 00163 NM 2008 3 13 SWAA081151 1 20080302 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER 16R CRACKED AT BS 500C. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008031300165 20080313 00165 NM 2008 3 13 SWAA081153 1 20080229 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, STR 13R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300167 20080313 00167 NM 2008 3 13 SWAA081152 1 20080229 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED MV1 CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR LBL 16. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008031300168 20080313 00168 NM 2008 3 13 SWAA081138 1 20080229 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300169 20080313 00169 NM 2008 3 13 SWAA081137 1 20080229 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515D, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300174 20080313 00174 NM 2008 3 13 SWAA081169 1 20080301 A 3350 8200048801 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008031300175 20080313 00175 NM 2008 3 13 SWAA081170 1 20080301 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 416WN 32453 DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008031300176 20080313 00176 NM 2008 3 13 SWAA081172 1 20080229 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 421LV 32452 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 133. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008031300177 20080313 00177 NM 2008 3 13 SWAA081171 1 20080229 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 421LV 32452 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 133. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008031300178 20080313 00178 NM 2008 3 13 SWAA081141 1 20080229 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 442WN 32459 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 11 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2008031300181 20080313 00181 NM 2008 3 13 SWAA081200 1 20080303 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031300182 20080313 00182 NM 2008 3 13 SWAA081195 1 20080303 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300189 20080313 00189 NM 2008 3 13 SWAA081196 1 20080303 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031000313 20080310 00313 WP 2008 3 10 AALA200800426 1 20080227 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 474 49649 MSP - EMERGENCY LIGHT AT SEAT ROW 13 MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 13. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031000314 20080310 00314 WP 2008 3 10 AALA200800427 1 20080227 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 474 49649 MSP - EMERGENCY LIGHT AT SEAT ROW 13 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 13. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008031000341 20080310 00341 CE 2008 3 10 O7Z2008F00000 1 20080128 A 5711 SPAR CAP BEECH 90 E90 1152914 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL WING CRACKED E O7ZA K NONE O OTHER IN INSP/MAINT 1 WP 17 152D LW119 FWD OB LOWER WING SPAR CAPS ARE CRACKED. LT AND RT ASSY CRACKS RADIATE FROM THE (4) HUCK RIVET FWD THROUGH WING ATTACH HINGE. THE AIRCRAFT WAS INSPECTED 15 MONTHS AND 404.2 HOURS AGO BY EDDY CURRENT AND NO CRACKS WERE FOUND AT THAT TIME. (K) 1 L 7 2 3T 4 T 3A20 E4EA 6 C P15EA 2008031000366 20080310 00366 2008 3 10 A6WA200840067 4 20080211 A 3425 AHRS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 1 MALFUNCTIONED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 449AW 7818 COMPLETE NR 1 AHRS FAILURE IN FLIGHT. COMPLIED WITH QRH. NO ALTITUDE OR COMPASS INFORMATION. AFTER REVERSIONARY SLELE CTION TO NR 2, ALL DISPLAY INFO WAS NORMAL ON CAPTAINS SIDE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000370 20080310 00370 EA 2008 3 10 A6WA200840101 1 20080204 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 CRACK FOUND ON LOWER SILL FS 572, LBL 40, UNDER BRACKET SCUFF PLATE RETAINER. LOWER SILL PLATE REPLACED IAW REO 601R53- 61-690 REV D. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000380 20080310 00380 EA 2008 3 10 A6WA200840075 1 20080201 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 431AW 7256 TWO CRACKS ON FLOOR LANDING PLATE AT FS 589 AND FS 605. (K) REPAIRED IAW REO 601R-53-61-433. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031000391 20080310 00391 EA 2008 3 10 A6WA200840086 1 20080205 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 429AW 7711 CRACK EXIST ON INTERCOSTAL FS 484, RBL 36 CRACK LENGTH .200. (K) REPAIRED INTERCOSTAL IAW REO 601R-53-41-059. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 2008031100020 20080311 00020 NM 2008 3 11 2008UALA01069 1 20080228 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 32 RT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EEL LIGHT INOP: ROW 32RT. REPLACED LIGHT ASSY 2 L 7 4 4F 4 F RT A20WE E24NE 2008031100021 20080311 00021 NM 2008 3 11 2008UALA01070 1 20080228 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R3 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY EXIT LIGHT INOP: DOOR 3R AFT DOOR SIGN. REPLACED LIGHT ASSY 2 L 7 4 4F 4 F RT A20WE E24NE 2008031200012 20080312 00012 NM 2008 3 12 USAA920080551 1 20080302 A 2933 65449815 FILTER BOEING 737 737301 1384611 NM ZONE 100 LEAKING A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 589US 23934 FLT NR 1767- AIR TURNBACK - ON TAKEOFF RAISING LANDING GEAR "A" HYDRAULIC QUANTITY WENT TO ZERO. ENGINE DRIVEN PUMP LIG HT ILLUMINATED. PUMP TURNED OFF. MX DICOVERED THE "A" HYDRAULIC SYSTEM EMDP ACOUSTIC FILTER LEAKING. MX REPLACED THE EM DP ACOUSTIC FILTER. OPERATIONAL / LEAK CHECK WAS GOOD. THE A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2008031200020 20080312 00020 NM 2008 3 12 08FDEA00481 1 20080218 A 5320 146N541614 FLOOR SUPPORT BOEING 757 75727B 1384921 NM ZONE 100 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 EXISTING REPAIR FOUND IN AFT CARGO FLOORBOARD STRINGER R2.90 INTERSECTION AT STA 1240 TO EVALUATE EXISTING REPAIR. EXIS TING REPAIR FOUND NOT IAW B757-200 SRM 51-70-11 FIG 1, DETAIL I, II. AFT CARGO FLOORBOARD STRINGER REPLACED IAW B757-20 0, SRM 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-02-100. 2 L 7 2 4F RT A2NM 2008031300074 20080313 00074 NM 2008 3 13 2008UALA01147 1 20080229 A 3510 REGULATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OXYGEN MASK LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 560UA 26660 FIRST OFFICER OXYGEN MASK HARNESS LEAKING AIR AND WILL NOT INFLATE. FOUND LEAKING REGULATOR. REPLACED FO O2 MASK. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008031300084 20080313 00084 NM 2008 3 13 2008UALA01156 1 20080301 A 2410 OIL SYSTEM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE IDG LOW PRESSURE A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 214UA 30220 ELEC GEN DRIVE R RIGHT IDG FAULT (LOW INTERNAL OIL PRESSURE). 2 L 7 2 4F 4 F RT T0001SE E46NE 2008031300089 20080313 00089 NM 2008 3 13 2008UALA01161 1 20080301 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EEL INOP, LAV 104 LOWER AREA. RELAMPED 2 L 7 4 4F 4 F RT A20WE E24NE 2008031300126 20080313 00126 EU 2008 3 13 08FDEA00715 1 20080305 A 5510 FAIRING AIRBUS 310 A310203 3930313 EU HORIZONTAL STAB DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT HORIZONTAL STABILIZER LOWER APRON FAIRING IS DISBONDED. RE-APPLIED ADHESIVE PER SRM 55-15-11 PARAGRAPH 5 SECTIONS H & I TO DISBONDED SILICONE MATERIAL. 2 L 7 2 4F RT A35EU 2008031300138 20080313 00138 WP 2008 3 13 08FDEA00728 1 20080305 A 5230 ADA019343 LINER DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 384FE 46617 LOWER FWD CARGO DOOR LINER IS CRACKED IN THE AFT UPPER AREA. REPAIRED FWD CARGO DOOR LINER CRACK WITH A WET LAY-UP IAW DC/MD-10 SRM 51-43-01. VOL II. MINOR REPAIR. 2 L 7 3 4F RT A22WE 2008032500208 20080325 00208 NM 2008 3 25 2008UALA01444 1 20080315 A 5320 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 808UA 804 BEAM 140 IS CORRODED. MAJOR REPAIR WAS ACCOMPLISHED AT DEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008031300188 20080313 00188 NM 2008 3 13 SWAA081197 1 20080303 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031300193 20080313 00193 NM 2008 3 13 SWAA081205 1 20080303 A 5311 6546539 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME INBOARD CHORD CRACKED AT BS 616, LBL 64. REMOVED AND REPLACED CHORD PE R SRM. 2 L 7 2 4F RT A16WE 2008031300194 20080313 00194 NM 2008 3 13 SWAA081208 1 20080228 A 5755 654645262A CASTING BOEING 737 7373H4 1384600 NM NR 4 SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 602SW 27953 DURING SCHEDULED HC1 CHECK, FOUND LT WING NR 4 SPOILER OUTBOARD CASTING CRACKED. REMOVED AND REPLACED NR 4 SPOILER PER MM. 2 L 7 2 4F RT A16WE 2008031300196 20080313 00196 2008 3 13 SWAA081206 4 20080228 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 602SW 27953 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031300197 20080313 00197 NM 2008 3 13 SWAA081207 1 20080228 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 602SW 27953 DURING SCHEDULED HC1 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS CRACKED AT ROW 7 DEF. REMOVED AND REPLACED LENS P ER MM. 2 L 7 2 4F RT A16WE 2008031300199 20080313 00199 NM 2008 3 13 SWAA081211 1 20080303 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300200 20080313 00200 NM 2008 3 13 SWAA081178 1 20080303 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300207 20080313 00207 NM 2008 3 13 SWAA081210 1 20080303 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 629SW 27704 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300218 20080313 00218 NM 2008 3 13 SWAA081161 1 20080229 A 3350 3071BPEGPL LIGHT BOEING 737 7377AD 1384502 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 798SW 28436 RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008031300220 20080313 00220 NM 2008 3 13 ASAA0852693 1 20080304 A 4990 38809381 FILTER BOEING 737 737890 1384527 NM APU CLOGGED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 585AS 35683 REFERENCE TASKCARD 78349013 APU OIL FILTER DELTA P POPPED. REPLACED FILTER RESET INDICATOR. LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 2008031300224 20080313 00224 NM 2008 3 13 SWAA081135 1 20080229 A 3350 101331 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 281WN 36528 DURING SCHEDULED HC1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2008031300228 20080313 00228 NM 2008 3 13 SWAA081186 1 20080302 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008031300238 20080313 00238 NM 2008 3 13 SWAA081167 1 20080229 A 5330 6545768208 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008031300240 20080313 00240 2008 3 13 SWAA081168 4 20080302 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008031300254 20080313 00254 NM 2008 3 13 SWAA081160 1 20080303 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 847, LBL 70. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008031300260 20080313 00260 NM 2008 3 13 SWAA081148 1 20080229 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 516A, STR 20R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008031300267 20080313 00267 NM 2008 3 13 SWAA081226 1 20080304 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031300273 20080313 00273 NM 2008 3 13 SWAA081234 1 20080304 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031300274 20080313 00274 NM 2008 3 13 SWAA081235 1 20080304 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008031300279 20080313 00279 NM 2008 3 13 SWAA081242 1 20080304 A 5312 6517583 BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND VERTICAL BEAM CRACKED AT BS 178, RBL 17, WL 182. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 2008031300285 20080313 00285 NM 2008 3 13 SWAA081240 1 20080304 A 3350 311500 LENS BOEING 737 7373Q8 1384670 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 19 DEF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008031300290 20080313 00290 EA 2008 3 13 HNAA0800096 1 20080227 A 8010 AJA4N176 CONTACTOR DHAV DHC8 DHC8311 1386006 EA START SYS DAMAGED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 326EN 31266 31266 234 WHILE TAXIING IN EWN, NR 2 SIDE DC BUSS FAULTED AND THERE WAS SOME SMOKE ON NR 2 SIDE. THE SMOKE WAS FOUND TO BE COMING FROM THE APU. FOUND THE STARTER GENERATOR OVERHEATED AND APU START CONTACTOR WELDED. NO DAMAGE FOUND IN THE APU AREA. REPLACED THE START CONTACTOR K-62 AND INSPECTED WIRING, NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 2008031300293 20080313 00293 WP 2008 3 13 NWAA080829959 1 20080302 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1121 S26-28L DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING GROUND OPERATIONS, FUSELAGE SKIN WAS DAMAGED AT BS 1121 L26L AND L28L. REPAIRED PER EA 99-212444. 2 L 7 2 4F A6WE 2008031300296 20080313 00296 NM 2008 3 13 DL76G080308 1 20080302 A 3150 WARNING MESSAGE BOEING 767 7673P6 1385105 NM ILLUMINATED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 154DL 25241 LDG GEAR MONITOR STATUS MSG ON PUSH BACK. 2 L 7 2 4F RT A1NM 2008031300306 20080313 00306 GL 2008 3 13 DL764080317 2 20080305 A 7230 BLADES BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 2 COMPRESSOR SHEARED A DALA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 843MH 23034 706381 29716 706381 CREW REPORTS RT ENG COMPRESSOR STALL DURING INITIAL PWR FOR T/O. ABORTED T/O AT 10 KTS, CREW OBSERVED RT EGT DROP TO NE AR ZERO FOR A BRIEF SECOND AFTER BANG. NO EICAS MESSAGES, MTC IN PROGRESS. ALITALIA BORO INSP IN WORK. BOROSCOPE INSP ECTION REVEALED 3 BLADE ON THE 3RD STAGE HPC SHEARED. ALSO HAVE DAMAGE ON ALL STAGES AFT. METAL FLAKES IN THE TAILPIPE . ENG CHANGE REQUIRED. 1ST AND 2ND STAGES HAVE NO DAMAGE. 2 L 7 2 4F 4 F RT A1NM E23EA 2008031300308 20080313 00308 NM 2008 3 13 DL757080321 1 20080306 A 3350 BULB BOEING 757 757232 1384965 NM EMERGNECY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 618DL 22908 EMERGENCY LIGHT OUTSIDE R4 DOOR INOP. RELAMPED. 2 L 7 2 4F RT A2NM 2008031300311 20080313 00311 2008 3 13 WGEA200800041 4 20080304 A 2200 AUTOPILOT SYS ECLIPS EA500 ECLIPSEEA500 3350000 SW MALFUNCTIONED E WGEA O OTHER F FLT CONT AFFECTED CR CRUISE 1 EA 27 160DJ 000077 ON FLIGHT FROM SAV TO GNV DURING CRUISE, AUTO PILOT TRIMMED 79 PERCENT LWD. AIRPLANE FLEW NORMALLY WITH A/P DISCONNECTE D, 79 PERCENT LWD EARLIER LEGS, AILERON TRIM 0 TO 10 PERCENT LWD. PERFORMED FLIGHT CONTROL CHECKS IAW EA500 AMM 27-00-0 0. NO DEFECTS NOTED. 1 L 7 2 4J RT A00002AC 2008031300313 20080313 00313 EA 2008 3 13 MASA200800184 1 20080305 A 5270 PSEU CNDAIR CL600 CL6002C10 1390015 EA DOOR WARNING NOT SEATED A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 506MJ 10073 ASH FLT 7319 IAD-SAV. PAX DOOR WARNING MESSAGE ON T/O. RESEATED PSEU, CLEANED DOOR SENSORS, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008031300316 20080313 00316 EA 2008 3 13 MASA200800186 1 20080305 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 154SF 7154 FLT 7332, IAD-SAV. EMERGENCY OVERWING LOWER EXIT SIGN INOP. MX RESCURED CONNECTOR. 2 L 7 2 4F RT A21EA 2008031300317 20080313 00317 EA 2008 3 13 MASA200800187 1 20080305 A 3350 BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77181 7181 FLT 7148, IAD-GSP. EMERGENCY LIGHTS WILL NOT COME ON. CHARGED BATTERIES, OPS GOOD. 2 L 7 2 4F RT A21EA 2008031300323 20080313 00323 WP 2008 3 13 UPS08851758 1 20080220 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 FLT, DECK FLOOR PNL 678 HAS MANY BADLY BUCKED RIVETS WITH SOME HAT CHANNEL RADIUS, ALSO CORROSION ARO UND FASTENER HOLES. FABRICATED FLT DECK FLOOR PANEL NR 678 IAW SRM 57-07-00 FIG 049B. 2 L 7 4 4F RT 4A25 2008031300324 20080313 00324 NM 2008 3 13 ASAA0872695 1 20080304 A 5210 141A650020 DOOR BOEING 737 737790 13844CN NM SERVICE DOOR OBSTRUCTED A ASAA K NONE O OTHER NR NOT REPORTED 1 NM 02 618AS 30543 FWD SERVICE DOOR IS NOT CLOSING PROPERLY. INSPECTED FRAME FOR OBSTRUCTIONS SUSPECT SAFETY STRAP INTERFERENCE. DOOR OP CHECKS NORMALLY. 2 L 7 2 4F RT A16WE 2008031300325 20080313 00325 WP 2008 3 13 UPS08851759 1 20080304 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 MAIN ENTRY DOOR HAD DENT WITH CREASE JUST OUTBD OF BAYONET FITTING DENT MEASURES 1.25 LENGTH BY .750 WIDE AND .150 D EEP. CON'T ON ECA FORM 011317: FABRICATED DOUBLER. COLD WORKED AREA TO PROPER LIMITS OF .0 08 IAW UPS EO DC8-5310-28745 -A, APPX PARA 3. ACCOMPLISHED ADDITIONAL HFEC AFTER REWORK OF AREA-REF NDTSPM 06-10-0. NO CRACKS DETECTED IN WEB ANGLE OR INTERNAL ANGLE ALODINE AND PRIMED AREA, COMPLETED INSTALLATION. 2 L 7 4 4F RT 4A25 2008031300336 20080313 00336 NM 2008 3 13 QXEA200800241 1 20080227 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - SMALL ROCK CHIP IN FUSELAGE SKIN LOCATED ON RIGHT SIDE APPROXIMATELY STATION X8.00 BETWEEN STRINGER 26R AND 2 7R. REPAIRED IAW DASH 8 Q400 SRM 51-26-10, 51-21-10, 51-25-10, 51-25-15, RD8/4-53-2037 AND NDTM PART 6 51-00-01. 2 H 7 2 4T RT A13NM 2008031300339 20080313 00339 NM 2008 3 13 QXEA200800244 1 20080227 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 547-564 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - SEAT TRACK NR 13 AT STATION 564 TO 547 GOUGED. REPAIRED IAW Q400 RD8/4-53-884 AND NDTM PART 6-51-00-01. 2 H 7 2 4T RT A13NM 2008031300341 20080313 00341 NM 2008 3 13 QXEA200800246 1 20080227 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 644-664 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 408QX 4050 PDX - C4 - RIGHT INBOARD SEAT TRACK NR 15 HAS SEVERAL CORRODED AREAS ON UPPER TRACK SURFACE AT APPROXIMATELY STATION 664 .0 TO 644.0. REMOVED SEAT TRACK NR 15 AND INSTALLED NEW SEAT TRACK IAW DASH 8 Q400 SRM 51-40-07, 51-42-00 AND 51-40-15. 2 H 7 2 4T RT A13NM 2008031300343 20080313 00343 NM 2008 3 13 BB08032 1 20080306 A 2121 6457053 FAN BOEING 757 7572B7 1384964 NM ZONE 200 FAILED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 937UW 2190 27245 TPA FLT 1961 CLT TO TPA - THE CREW RECEIVED EICAS MESSAGE "OUTBRD EX VAL OPEN". A BURNING ODOR WAS ALSO NOTED IN THE COCKPIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT RECIRCULATION FAN. SYSTEM OPERATIONALL Y CHECKS NORMAL. 2 L 7 2 4F RT A2NM 2008040200345 20080402 00345 NM 2008 4 2 KCSA081205 1 20080325 A 5340 STRINGER CLIP BOEING 747 747SR46 1384816 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 STRINGER CLIP DAMAGED AT BS 1520, STR-33R. 2 L 7 4 4F RT A20WE 2008040200346 20080402 00346 EU 2008 4 2 NSVA2008013 1 20080329 A 3350 6013211 POWER SUPPLY SAAB SF340 SF340A 7850100 EU EMERGENCY LIGHT INOPERATIVE A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 121CQ 121 DURING ENGINE SHUTDOWN IN BKW, EMERGENCY LIGHT CAME ON AND CREW NOTICED THE FIRST 2 FLOOR PROX LIGHTS WERE OUT ALONG WIT H ONE EMERGENCY EXIT LIGHT. REPLACED POWER SUPPLY. 2 L 7 2 4T RT A52EU 2008040800157 20080408 00157 NM 2008 4 8 SWAA081783 1 20080402 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008040200359 20080402 00359 NM 2008 4 2 2008UALA01744 1 20080328 A 5220 RESERVOIR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY EXIT UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 RT UPPER DECK EMERGENCY ESCAPE DOOR INOPENED UNUSABLE PER MEL. REPLACED UPPER RIGHT DECK DOOR EMERGENCY POWER RESERVOIR PER MM 52-23-13-0401. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200360 20080402 00360 NM 2008 4 2 2008UALA01745 1 20080328 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 FOUND SEAT 48 ABC LOWER EMERGENCY FLOOR LIGHT INOP. REPLACED LIGHT OPS CHECKED OK. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300012 20080423 00012 NM 2008 4 23 2008UALA02205 1 20080416 A 2400 UNKNOWN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE UNKNOWN A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 776UA 26937 ELEC BACKUP GEN L LEFT BACKUP GENERATOR OFF DUE TO A PROTECTIVE TRIP. STATUS MSG01- LATCHED CRUISE MODE DEPENDENT; BACK UP GENERATOR (L) OIL PRESSURE IS LOW. DB- BACKUP CONVERTER MSG-2446080 LATCHED ER MODE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042300014 20080423 00014 NE 2008 4 23 2008UALA02206 2 20080417 A 7261 CARBON SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A UALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 595UA 28748 FLIGHT DIVERTED WITH A FUEL ODOR ON THE FLIGHT DECK. FOUND CARBON SEAL FAILED AT NR 3 BEARING, OIL WETTING OF AREA. REP LACED NR 1 ENG, PERFORMED PACK BURN OUT. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300021 20080423 00021 NM 2008 4 23 UPS08652042 1 20080416 A 3150 WARNING LIGHT BOEING 767 76734AF 1385212 NM LT ENGINE ILLUMINATED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 329UP 27755 ATB - CREW REPORTED DURING CLIMB THEY RECEIVED A LT DUCT EICAS MESSAGE. LIGHT EXTINGUISHED AFTER ENG BLEED AIR SUPPLY A ND ISOLATION VALVE CLOSED. OPS CHECKS NORMAL PER FIM 26-18-00 FIG 104 SHEET 1. 2 L 7 2 4F RT A1NM 2008042300025 20080423 00025 NM 2008 4 23 UPS08M52029 1 20080203 A 5753 SKIN DOUG MD11 MD11 3023602 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C RT I/B TE FLAP O/B LOWER SEGMENT BOTTOM SKIN TO BE REPLACED DUE TO MULTIPLE DENTS AND CORROSION. NEW SKIN FABRICATED PER BOEING DRAWING ARC2444 USING MATL 2024T3-0.040" NEW SKIN HOLES PICKED UP PER SRM 51-31-01 V.2R40. N EW SKIN PROTECTED PER SRM 51-21-01 V.2R40. NEW SKIN PAINTED PER SRM 51-21-01V.2R.40. NEW SKIN INSTALLED PER SRM 51-35- 01V.2R.40. RHW I/B FLAP ASSY O/B SEGMENT INSTALLED PER CMM 57-52-03 R.40. 2 L 7 3 4F RT A22WE 2008042300026 20080423 00026 EU 2008 4 23 F3LA200800185 1 20080410 A 5315 D5347039420800 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AT NUT PLATES AFT PIT LEFT HAND FLOORBEAM UNDER COVER PROFILE AT FRAME 5 8 LOCATED FROM STRINGER 38 LEFT TO 38 RIGHT. MAINTENANCE FABRICATED AND REPLACED FLOORBEAM SUPPORT FITTING IN ACCORDANC E WITH THE REQUIREMENTS OF AIRBUS DRAWING D53470394 SHEET 3 REVISION H AND SRM 51-44-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008040900168 20080409 00168 NM 2008 4 9 DLM88080545 1 20080403 A 5312 SPLICE DOUG MD88 MD88 3023688 NM BULKHEAD CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, CORROSION WAS FOUND ON AFT P-DOME WEB SPLICE AT 6HRS POSITION. WEB SPLICE WAS REPLACED IAW DOUGLAS DWG 5910 130. 2 L 7 2 4F RT A6WE 2008040900171 20080409 00171 NM 2008 4 9 C8GA20080013 1 20080401 A 2613 356644400 OVERHEAT LOOP BOEING 727 727223 1384074 NM NR 3 NACELLE FAULTED A C8GA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 29 708AA 22465 CLT TO BNA - DURING CLIMB OPERATION, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. THE AIRCRAFT DIVERTED TO TOL WHE RE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE NR 3 STRUT OVERHEAT DETECTOR LOOP AT FAULT. RE MOVED AND REPLACED NR 3 STRUT OVERHEAT DETECTOR LOOP, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 2008040900172 20080409 00172 NM 2008 4 9 DL76L080548 1 20080402 A 5330 146T32311 SKIN BOEING 767 767332 1382001 NM FS 1440 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 184DN 27111 BLENDS TO SKIN FS 1440-1540 AND STR 28L-36L. DTA INSPECTION ADDED. 2 L 7 2 4F RT A1NM 2008040900173 20080409 00173 2008 4 9 DL777080549 2 20080402 A 7210 ENGINE BOEING 777 777232 1385232 NM NR 1 MALFUNCTIONED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 862DA 37497 29734 511188 NR 1 ENGINE REPLACED DUE TO HOC. 2 L 7 2 4F RT T00001SE 2008040900181 20080409 00181 NM 2008 4 9 QXEA20080339 1 20080329 A 2697 CONNECTOR DHAV DHC8 DHC8202 2809007 NM SMOKE DETECTOR DAMAGED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 09 355PH 500 SEA - FLIGHT 2101 - LAVATORY SMOKE DETECTOR GOES OFF INTERMITTENTLY IN FLIGHT. MAINTENANCE PLACED ON MEL 26-4. AIRCRAF T RETURNED TO SERVICE. MEL CLEARED ON 3/31 BY CONNECTING THE PINS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERV ICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008040900184 20080409 00184 WP 2008 4 9 IXXA08SMN088S 1 20080215 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP LOWER FORWARD PANEL PLATING DENTED AT STATION XW 2.000 - STA XW 91.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, AND BONDED DOUBLE R. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 1 ITEM "B" AND "L", DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-9 T/R 51 -142, 51-1-9A T/R 51-141, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008040900185 20080409 00185 NM 2008 4 9 QXEA20080342 1 20080330 A 5520 BRACKET DHAV DHC8 DHC8202 2809007 NM ELEVATOR LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX C5 CHECK - ELEVATOR BUMP STOP BRACKET IS LOOSE ON THE RIGHT SIDE WHERE IT ATTACHES TO THE HORIZ STAB. REMOVED THE J O-BOLTS AS REQUIRED. REPLACED FASTENERS PER INSTRUCTIONS IN RD 8-55-112. 2 H 7 2 4T RT A13NM 2008040900186 20080409 00186 NM 2008 4 9 QXEA20080343 1 20080330 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX C5 CHECK, AFT BAGGAGE PIT HAS LIGHT CORROSION AT Z100 X 600 AND 21L UNDERSIDE AT NUTPLATE. REMOVED NUTPLATE AND BLE NDED MINOR SURFACE CORROSION. BLENDED AREA WITHIN LIMITS. ALODINED PRIMED AND PAINTED AREA. 2 H 7 2 4T RT A13NM 2008040900187 20080409 00187 NM 2008 4 9 QXEA20080344 1 20080330 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 356PH 502 PDX C5 CHECK, AFT BAGGAGE PIT Z100 X600 AND 27R THERE IS LIGHT CORROSION FORMING TOPSIDE AND UNDERSIDE OF THE NUTPLATE. REMOVED THE NUTPLATE AND BLENDED LIGHT CORROSION. AREA REMOVED WAS .005". ALODINED PRIMED AND PAINTED AREA. 2 H 7 2 4T RT A13NM 2008040900188 20080409 00188 NM 2008 4 9 2008UALA01854 1 20080401 A 3510 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT SHORTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 597UA 28750 CAPT O2 MASK MIC INOP. FOUND SHORT INSIDE MIC. REPLACED MASK AND STOWAGE BOX ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040900195 20080409 00195 NM 2008 4 9 HALA0800503 1 20080407 A 4990 OIL SYSTEM BOEING 767 76733A 1385209 NM APU LOW A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, ATTEMPTED APU START AFTER LANDING/FAULT LIGHT ILLUMINATED LOWER EICAS SHOWING "ADD" OIL. BITE CHECK ECU, NO FAULTS NOTED. SERVICED APU WITH OIL. GND RUN CHECK OKAY. 2 L 7 2 4F RT A1NM 2008040900199 20080409 00199 NM 2008 4 9 HALA0800508 1 20080405 A 5310 STRUCTURE BOEING 767 767332 1382001 NM FUSELAGE DAMAGED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 596HA 23276 LIGHTNING STRIKE AT FUSELAGE ST 188.5 LONG 28R. OK TO CONTINUE PER SRM 53-00-01. 2 L 7 2 4F RT A1NM 2008041000020 20080410 00020 EA 2008 4 10 MASA200800274 1 20080329 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 930LR 15030 ASH FLT 2696 CLT-EWR. AFT CEILING EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2008041000021 20080410 00021 EA 2008 4 10 MASA200800276 1 20080330 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75987 5987 ASH FLT 7456 IAD-ORF. PAX DOOR HARD TO OPEN FROM THE OUTSIDE. LUBED DOOR, OPS GOOD. 2 L 7 2 4F RT A21EA 2008041000026 20080410 00026 WP 2008 4 10 UPS08851945 1 20080303 A 5347 DC853B007002 SEAT TRACK DOUG DC8 DC873F 302199F WP CABIN GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 MAIN CABIN SEAT TRACK GOUGED STA 270 LBL 65. REMOVED DAMAGE, INSTALLED SEAT TRACK PLUG IAW SRM 51-3- 0, 53-2-3 FIG 12, 51-1-8. 2 L 7 4 4F RT 4A25 2008041000027 20080410 00027 EU 2008 4 10 YENA2008027 1 20080331 A 2161 761B000001 ACTUATOR AIRBUS 320 A320232 3930326 EU CABIN TEMP MALFUNCTIONED A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 585JB 17565 17565 2159 FLT 491, BOS-DEN, AIR RETURN TO BOS, CABIN TEMP ZONE 1 RAN AWAY, STAYING AT 156 DEGREES, CYCLED HOT AIR VALVE, NO HELP. REMOVED AND REPLACED RAM AIR INLET ACTUATOR PER 21-61-00 AND REMOVED AND REPLACED NR 2 PACK CONTROLLER, ALL OPS CHECK G OOD PER AMM 21-61-00. 2 L 7 2 4F RT A28NM 2008041000028 20080410 00028 NM 2008 4 10 NWAA081465640 1 20080321 A 5330 SKIN BOEING 757 757251 1384970 NM BS 625 S14L DENTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 540US 26487 DURING "M" CHECK FOUND DENT IN FUSELAGE SKIN AT BS 625 S14L. REPAIRED PER EA 56-210586 SECTION I, SECTION II REQUIRES S UPPLEMENTAL INSPECTION ON OR BEFORE 37,500 CYCLES ARE REACHED. SECTION III REQUIRES REPEAT INSPECTION NOT TO EXCEED EVE RY 3000 CYCLES AFTER ACCOMPLISHMENT OF SECTION II. 2 L 7 2 4F RT A2NM 2008041000033 20080410 00033 EU 2008 4 10 08FDEA01315 1 20080406 A 7170 2215459501 DRAIN LINE AIRBUS 310 A310324 3930206 EU NR 2 ENGINE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 803FD 378 NR 2 ENGINE DRAIN MANIFOLD TUBE CRACKED REMOVED DRAIN MANIFOLD IAW FEDEX AMM 71-70-14-4. WELDED DRAIN MANIFOLD IAW EA 6 -7170- 118466, POWER PLANT, DRAIN MANIFOLD ASSEMBLY CRACK, REPAIR. REINSTALLED DRAIN MANIFOLD IAW FEDEX AMM 71-70-14-4 . 2 L 7 2 4F RT A35EU 2008041000042 20080410 00042 NM 2008 4 10 08FDEA01320 1 20080406 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK CARGO DOOR LOWER JAMB SPOOL FITTING NR 6 FOUND THIRD LAYER CRACK INDICATION AFTER BORE TO MAXIMUM 0.519". REM OVED AND REPLACED PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041000044 20080410 00044 NM 2008 4 10 08FDEA01321 1 20080406 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK CARGO DOOR LOWER JAMB SPOOL FITTING NR 7 FOUND THIRD LAYER CRACK INDICATION AFTER BORE TO MAXIMUM 0.519". REM OVED AND REPLACED PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041000045 20080410 00045 SO 2008 4 10 RAIA00803029 1 20080330 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 841HK 145382 DURING SCHEDULED MAINTENANCE - STL - EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE EMERGENCY LIGHT. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008041000054 20080410 00054 EU 2008 4 10 08FDEA01329 1 20080407 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT RT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND OLD DOUBLER REPAIR ON SLAT NR 1 RT LOWER SKIN BETWEEN TRACK 3 AND RIB 20 WITHOUT DOCUMENTATION. REPAIR PERFORMED BY CUT OUT THE SKIN AND INSTALLING A DOUBLER IAW RAS/FOK/004/2008 ISS D, APPROVED BY EA 6-5742-114858. 2 L 7 2 4F RT A35EU 2008041000055 20080410 00055 WP 2008 4 10 08FDEA01330 1 20080407 A 5512 ALC7290502 SKIN PANEL DOUG DC10 DC1010F 3022111 WP HORIZONTAL STAB DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION ON HORIZONTAL STABILIZER RT SIDE FOUND DISBONDING THE UPPER SKIN TIP OUTBOARD ELEVATOR REP LACED SKIN ASSY FOR SRM 51-35-01 AND DWG ALC7347,ALC7348, ALC7602. 2 L 7 3 4F A22WE 2008041000058 20080410 00058 SO 2008 4 10 RAIA00803027 1 20080328 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 803HK 145077 PRE FLT 3517 - PIT - EMERGENCY LIGHT AT ROW 17 INOPERATIVE. MAINTENANCE DEFERRED THE LIGHT STRIP IAW MEL. 2 L 7 2 4F RT T00011AT 2008041000060 20080410 00060 EU 2008 4 10 08FDEA01333 1 20080407 A 5330 A5377263600200 WEB AIRBUS 310 A310203 3930313 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FWD CARGO DOOR CUTOUT, LWR FWD WEB DENTED. FABRICATED, POTTED EDGES, COMPLETED CURE AND SANDED EDGE POTTNG. INSTALLED INSERTS & APPLIED NON-SKID IAW DWG 25-005 REV F. 2 L 7 2 4F RT A35EU 2008041000062 20080410 00062 NM 2008 4 10 ASAA0892802 1 20080331 A 2810 341A31011 DRAIN BOEING 737 737990 NM CTR FUEL TANK LEAKING A ASAA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 02 307AS 30015 DURING DESCENT TO ANC, CREW NOTICED FUEL SMELL. FOUND CENTER TANK SUMP DRAIN LEAK. REPAIRED CENTER FUEL TANK. 2 L 7 4 4F RT A16WE 2008041000066 20080410 00066 SW 2008 4 10 WGEA200800052 1 20080401 A 5270 SWITCH ECLIPS EA500 ECLIPSEEA500 3350000 SW PAX DOOR OUT OF ADJUST E WGEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 158DJ 000071 DURING CRUISE FLIGHT PASSENGER DOOR WARNING LIGHT CAS MESSAGE POSTED. ADJUSTED FWD DOORS SWITCH LAW EA 500 AMM 52-00-00 . OPS CHECK GOOD LAW EA 500 AMM 21-30-03, CABIN PRESSURE VESSEL ADJ/TEST. 1 L 7 2 4J RT A00002AC 2008041000068 20080410 00068 WP 2008 4 10 08FDEA01338 1 20080407 A 5730 ARB087238 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT WING FUEL PANEL 635 BT; INTERNAL SURFACE HAS AREAS OF CORROSION. FABRICATED FUEL PANEL P/N IAW DAC DWG ARB 0872-3 8 AND PART MARKED. 2 L 7 3 4F RT A22WE 2008041000071 20080410 00071 NM 2008 4 10 ASAA0872801 1 20080330 A 5755 SKIN BOEING 737 737790 13844CN NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 607AS 29751 DENT ON TOP SURFACE OF NR 6 SPOILER FWD INBOARD CORNER. REPLACED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008041000074 20080410 00074 EU 2008 4 10 USAA920080716 1 20080330 A 5610 NP1653116 WINDSHIELD AIRBUS 320 A320232 3930326 EU COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 659AW 30787 30779 1166 FLT 17 - JFK - PHX - DIVERSION - FIRST OFFICER'S OUTER PANE WINDSHIELD CRACKED. AIRCRAFT DIVERTED TO PHL WHERE THE F/O' S WINDSHIELD WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A28NM 2008041000076 20080410 00076 EU 2008 4 10 Y2LA200800017 1 20080326 A 5330 SKIN AIRBUS A319 A319112 3930323 EU FUSELAGE DAMAGED A Y2LA K NONE O OTHER TX TAXI/GRND HDL 1 GL 07 554SX 3309 PORTABLE STAIRS AT AFT LEFT DOOR STRUCK A/C AND PUNCTURED HOLE IN FUSELAGE BETWEEN FRAME 79 AND 80 JUST ABOVE AND AFT OF APU FIRE DISC DAMAGE IS A TRIANGLE CUT APPROX SIZE 3.625" X 2.5". HEFC INSPECTION PERFORMED WITH NO DEFECTS NOTED OTHE R THAN DAMAGE RECORDED ON LOG 0008165. C/W EA 19-53-006-R3-OT HOLE ON LT FUSELAGE FR 79 TO FR 80 THIS RETURNED A/C TO S ERVICE. 2 L 7 2 4F RT A28NM 2008041000085 20080410 00085 EU 2008 4 10 08FDEA01345 1 20080408 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 ANTI-ROTATING DEVICE CAN NOT BE INSTALLED IAW SB 29-6057 ON LT WING HOLE NR 2 AND NR 4. REPAIR PERFORMED BY ADDITIONAL DRILLING HOLE FOR SECOND FASTENER AND CUTTING ANTI ROTATING DEVICE IAW, TA-SEE53-2008-226024-1, APPROVED BY AND EA 6-291 0-115253. 2 L 7 2 4F RT A35EU 2008041000086 20080410 00086 EU 2008 4 10 08FDEA01346 1 20080408 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CORROSION FINDINGS ON EXISTING REPAIR BETWEEN RIB 7-8, AFT OF REAR SPAR LT WING BOTTOM SKIN REPAIR PERFORMED BY RENEWING DOUBLER REPAIR, BLEND OUT CORROSION IAW RAS/BAE/1006289/2008 ISS A, APPROVED BY EA 6-5720-114855. 2 L 7 2 4F RT A35EU 2008041000093 20080410 00093 NM 2008 4 10 2008040101 1 20080401 A 2611 WARNING SYSTEM BOEING 727 7272J7 138400E NM PWA JT8 JT8D17 52049 NE SMOKE WARNING MALFUNCTIONED A PCSA K NONE N FALSE WARNING CR CRUISE 1 SO 17 128NA 20879 AMERIJET FLIGHT 8110 FROM TSSJ TO KMIA - MAIN CARGO COMPARTMENT SMOKE WARNING CAME ON IN CRUISE FLIGHT. VISUALLY CHECKE D FALSE WARNING. ON ARRIVAL KMIA THE MAIN CARGO SMOKE DETECTION SYSTEM WAS OPERATIONALLY TESTED AND NO DEFECTS WERE FOU ND. 2 L 7 3 4F 4 F A3WE E2EA 2008041000099 20080410 00099 EU 2008 4 10 08FDEA01355 1 20080408 A 5514 A55176100245 WEB AIRBUS 300 A300B4622R 3930312 EU ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 THS -DURING INSTALLATION OF LT THS TIP SOME HOLES FOUND MISDRILLED. REPAIR PERFORMED BY INSTALLING NEW WEB WITH LOCK FA STENERS DAN7-6 IAW RAS/CASA/6544/2008 IS B, APPROVED BY EA 6-5514-117183. 2 L 7 2 4F RT A35EU 2008041000101 20080410 00101 EU 2008 4 10 08FDEA01357 1 20080408 A 5714 A57771000004 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 5 SPOILER LT DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 DELAMINATION OUT OF LIMIT FOUND ON SPOILER NR 5 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 27-61-53 PB 400. 2 L 7 2 4F RT A35EU 2008041000115 20080410 00115 EU 2008 4 10 NWAA081383351 1 20080403 A 2121 VR410004 FAN AIRBUS A330 A330223 3940031 EU ODOR A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 851NW 16473 16473 0609 JUST PRIOR TO LEVEL OFF AFTER TAKE OFF THE FLIGHT ATTENDANT AT DOOR 4R CALLED TO REPORT SHE SMELLED ELECTRICAL SMOKE AND IT WAS HAZY. RECEIVED "COND R CAB VENT FAULT" FOLLOWED COM AND SHUT OFF CABIN FANS AND THE SMELL AND HAZE DISSIPATED A ND LANDING WAS UNEVENTFUL. FOUND RECIRCULATION FAN RT (210HG) FAULT AND FAN FROZEN. 2 L 7 2 4F RT A46NM 2008041000122 20080410 00122 NM 2008 4 10 SWAA081761 1 20080331 A 5310 6978062 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 27720 DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT NR 5 DOOR STOP. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 2008041000144 20080410 00144 NM 2008 4 10 ASAA0852804 1 20080402 A 3040 BACC18X25 CIRCUIT BREAKER BOEING 737 737890 1384527 NM COCKPIT DAMAGED A ASAA K NONE J WARNING INDICATION CR CRUISE 1 NM 02 558AS 35177 UPON LEVEL OFF AT FL370 RT FWD WINDOW HEAT OVERHEAT LIGHT ILLUMINATED AND WINDOW HEAT POWER C/B POPPED OPEN. FOUND HEAT DAMAGE ON WIRE AND LUG AT WINDOW HEAT PWR C/B. REPLACED C/B C394 (RT WINDOW HEAT PWR). REPLACED TERM LUG TO C/B C394. WINDOW HEAT CONTROL UNIT BITE TESTS GOOD. RT WINDOW HEAT OPS NORMALLY. 2 L 7 2 4F RT A16WE 2008041000150 20080410 00150 NM 2008 4 10 UPS08551946 1 20080329 A 3610 1082853 SENSE LINE BOEING 757 75724APF 1384969 NM LT ENGINE LEAKING A IPXA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SO 01 459UP 25480 INSPECTION TYPE:N/A ATB - DURING CLIMB LT ENGINE OVERHEAT LIGHT CAME ON. REDUCED POWER, LIGHT WENT OUT. RE-APPLIED POW ER, LIGHT CAME BACK ON. REDUCED POWER, RETURNED TO MIA. ACCOMPLISHED 757 FIM 26-11-00 FIG 103A FOUND LEFT ENG HPSOV SE NSE LINE AND UNION LEAKING. REMOVED AND REPLACED HP6 SENSE LINE AND UNION REF ITEM 3 OF THIS LP. ACCOMPLISHED AMM 71-0 0-00-5 TEST 13. OPS AND LEAK CHECK NORMAL. 2 L 7 2 4F RT A2NM 2008041000158 20080410 00158 NM 2008 4 10 AALA200800634 1 20080313 A 2750 SELECTOR VALVE BOEING 757 757223 1384957 NM TE FLAPS INTERMITTENT A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 612AA 24488 MIA INFLIGHT T1455/13MAR - CREW REPORTED TRAILING EDGE FLAP DISAGREE LIGHT ILLUMINATED DURING FLAP RETRACTION. RETURNE D TO MIA AND LANDED WITHOUT INCIDENT. REPLACED FLAP ROTARY SELECTOR VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040200362 20080402 00362 NM 2008 4 2 2008UALA01747 1 20080328 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 FOUND SEAT 1J AFT EMERGENCY FLOOR LIGHT INOP. FOUND LIGHT FAULTY. REPLACED LIGHT ASSEMBLY. OPS CHECKED OK. AC OK FOR SER VICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040200367 20080402 00367 NM 2008 4 2 2008UALA01753 1 20080327 A 2612 360191 FIRE LOOP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 ENGINE FALSE ACTIVATION A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 850UA 1653 "ENGINE 1 FIRE LOOP A" ECAM MESSAGE AFTER NR 1 ENGINE CHANGE. SUSPECT A BAD LOOP IN THE ENGINE PYLON AREA. REPLACED LO OP, INSPECTED ALL CONNECTORS. ALL SATISFACTORY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040200388 20080402 00388 WP 2008 4 2 08FDEA01208 1 20080331 A 5330 NDA6012501 SKIN DOUG DC10 DC1010F 3022111 WP FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING REPAIR ASSESSMENT AN EXISTING REPAIR AT FUSELAGE SKIN WAS FOUND NOT IN CONFORMITY WITH APPROVED DATA REPAIR HAS B EEN REPLACED WITH A NEW IAW SRM 53-20-00 FIG 6, SH 3/4. 2 L 7 3 4F A22WE 2008040200393 20080402 00393 NM 2008 4 2 ASAA0872789 1 20080312 A 5610 WINDOW FRAME BOEING 737 737790 13844CN NM COCKPIT GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 607AS 29751 CAPTAIN'S SLIDING WINDOW FWD FRAME GOUGED ON FWD FACE 1" FROM TOP. CAPTAIN SLIDING WINDOW REPLACED WITH NEW SERVICEABLE UNIT IAW 737 700 AMM 56 12 11 AND ASA SUPPLEMENT 56 12 11. 2 L 7 2 4F RT A16WE 2008040300012 20080403 00012 NM 2008 4 3 ABXA080115 1 20080310 A 5320 141T3330 STRUCTURE BOEING 767 767281 1385109 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 775AX 22790 CRACK IN LOWER AFT CORNER OF THE FORWARD SERVICE DOOR CUTOUT. REPAIRED R1 LOWER AFT DOOR CORNER IAW REA B653-57148-MR. 2 L 7 2 4F RT A1NM 2008040300050 20080403 00050 NM 2008 4 3 KCSA081215 1 20080328 A 5311 FRAME BOEING 747 747SR46 1384816 NM FUSELAGE BENT A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 FRAME BENT BETWEEN STA-2180 AND STA-2200 LBL-28. 2 L 7 4 4F RT A20WE 2008040300057 20080403 00057 NM 2008 4 3 KCSA081217 1 20080329 A 5412 BULKHEAD BOEING 747 747122 1384872 NM NR 2 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 716CK 19753 NR 2 PYLON HYDRAULIC PRESSURE LINE FITTING CHAFED ON AFT SIDE OF NAC STA 221.9 BULKHEAD. 2 L 7 4 4F RT A20WE 2008040300070 20080403 00070 NM 2008 4 3 200800305 1 20080317 A 5350 SKIN BOEING 747 747SPB5 1384813 NM FAIRING SCRATCHED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 708BA 22484 UPPER WING TO BODY FAIRING, FROM STA 620 TO STA 1000 FROM STR 23R TO STR 34R HAS SCRIBE MARKS. APPROX STA 670 STR 31R .005 DEPTH. BLENDED OUT SCRIBE LINES, MATERIAL LOSS IS .005 WITHIN LIMITS, ALODINED AND PRIMED AREA PER B747 SP SRM'S 53-31-00 PG 1-4, 51-10-02 PG 6-6B AND B747 SOPM 20-44-04 PG 1-4 2 L 7 4 4F RT A20WE 2008040300111 20080403 00111 WP 2008 4 3 IXXA08SMN075S 1 20080214 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER OUTER SKIN SHOWS IMPROPER REPAIR AT STATIO N XOLDI 6.2246. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORM ED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLERS. CLEANED, TREAT ED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 DATED 02-27-08 NUMBER 08 086, SEMAN DRAWING NUMBER ED-4707 DATED 02-08-08, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-3-0, AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 2008040300127 20080403 00127 SO 2008 4 3 CHQA200800064 1 20080328 A 3620 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BLEED AIR SYS MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 267SK 145268 CAE311659 FLIGHT 5953 - PHL TO CLE - THE CREW RECEIVED A BLEED 1 LEAK MESSAGE DURING CLIMB, RAN THE APPROPRIATE QRH CHECKLISTS AND LANDED BACK AT PHL WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NR 1 BLEED SYSTEM AND COULD FIND NO LEAKS. MAINTENANCE RAN THE ENGINES AND BLEED SYSTEM WITH THE CREW AND THE BLEED LEAK COULD NOT BE DUPLICATED. THE AIRCRAFT WAS THEN RELEA SED BACK TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008040300132 20080403 00132 WP 2008 4 3 NWAA081309952 1 20080331 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 916RW 47144 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK AND THE TAILCONE EGRESS LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE TAILCONE EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM. 2 L 7 2 4F A6WE 2008040300154 20080403 00154 SO 2008 4 3 SWIA200819406 1 20080324 A 2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203 SO CARGO BAY MALFUNCTIONED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 07 220SW 120288 FLT 5560 - INTERMITTENT SMOKE LIGHT WHEN TESTING CARGO SMOKE SYSTEM. REPLACED NR 2 CARGO SMOKE DETECTOR, PN 473597-13, SN/OFF 1144. 2 L 7 2 4T RT A31SO 2008040300184 20080403 00184 NM 2008 4 3 HALA0800462 1 20080327 A 5730 SKIN BOEING 767 767332 1382001 NM RT WING CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 LEVEL 1 CORROSION ON RIGHT WING LOWER SURFACE AT STRINGER L-15 AT WS 577-608. REWORKED IAW SRM 51-10-02. 2 L 7 2 4F RT A1NM 2008040300192 20080403 00192 WP 2008 4 3 08FDEA01200 1 20080328 A 5753 ARC30063 SKIN DOUG MD10 MD1010F 3022112 WP T/E FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT INBD FLAP LOWER SURFACE FWD PANEL; 2ND FROM THE INBD END HAS SEVERAL DENTS. REMOVED PANEL IAW DC/MD-10 SRM 51-31- 01; VOL II. DEPTH OF THE DENTS ARE 0.125 THRU 0.325 USING DEPTH GAUGE T8492C. ORIGINAL THICKNESS OF THE SKIN IS 0.040 IAW DC/MD-10 SRM 57-52-01; FIG 1; VOL III. DENTS ARE OUT OF LIMITS IAW DC/MD-10 SRM 51-80-01; PG 2; VOL I. FABRICATED REPAIRS (3 EA) IAW DC/MD-10 SRM 57-10-00; VOL I. ALODINED IAW DC/MD-10 SRM 51-21-01; VOL II. PRIMED IAW DC/MD-10 SRM 51-21-01; VOL II. INSTALLED REPAIRS IAW DC/MD-10 SRM 57-52-01; VOL I. TOP COATED IAW DC/MD-10 SRM 51-21-01; VOL II. INSTALLED PANEL IAW DC/MD-10 SRM 51-51-31-01; VOL II. 2 L 7 3 4F RT A22WE 2008040300200 20080403 00200 EU 2008 4 3 08FDEA01218 1 20080401 A 5330 DOUBLER AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 448FE 260 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT LEFT SIDE UPPER FWD FUSELAGE SKIN BETWEEN FRAMES 0 TO 1 AND JUST FORWARD OF THE CAPTAINS WINDSHIELD MEASURES 9.5 INCHES BY 11.6 INCHES WITH A SKIN CUTOUT MEASURING 6.7 INCH BY 5.6 INCH REPAIR NOT IAW SRM REQUIREMENTS DUE TO LEVEL 1 SURFACE CORROSION FOUND ON REPAIR. REMOVED LEVEL 1 CORROSION BY HAND WITH NEGLIGIBL E MATERIAL LOSS AND RESTORED PROTECTIVE COATING IAW A310-200 SRM 53-12-12 FIG 201 SHEET 1, SRM 51-74-10, AND SRM 51-72-1 0. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008041000161 20080410 00161 NM 2008 4 10 AALA200800632 1 20080313 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 191AN 32385 DFW - EMERGENCY LIGHT AT AFT LEFT NUMBER FOUR DOOR EXIT LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT AFT LEFT NUM BER FOUR DOOR EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041000164 20080410 00164 WP 2008 4 10 AMTA200800243 1 20080327 A 3397 CONNECTOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2B 30018 NE EMERGENCY LIGHTS DAMAGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 701TZ 46583 ISLE EGRESS LIGHT AT SEAT 22JH INOPERATIVE. REPINNED 1 SOCKET IN CONNECTOR ON SEAT 22JH FLOOR PATH MARKING LIGHT WIRE H ARNESS IAW WDM STANDARD PRACTICES CH 20, LIGHT CHECKS GOOD AT THIS TIME. (K) 2 L 7 3 4F 4 F A22WE E23EA 2008041000167 20080410 00167 CE 2008 4 10 GUUA03260801 1 20080326 A 3243 9038000133 MASTER CYLINDER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BRAKES BYPASSING A GUUA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 29 17541 7882 UE203 FLIGHT: 9182, DURING TAXI RT BRAKES FAILS OCCASIONALLY. REPLACED CAPTAINS RT MASTER CYLINDER. 2 L 7 2 4T 4 T RT A24CE E26NE 2008041000174 20080410 00174 CE 2008 4 10 DXTA20082983 1 20080406 A 3260 WARNING LIGHT CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE MLG ILLUMINATED E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 806QS 5600614 AFTER SELECTING GEAR DOWN, RT MAIN GREEN LIGHT AND GEAR UNLOCKED RED LIGHT BEGAN TO FLICKER INTERMITTENT (3 GREEN NO RED ). 2 L 7 2 4F 4 F RT A22CE E00053EN 2008041000180 20080410 00180 2008 4 10 DXTA20082980 4 20080405 A 2210 TRIM SYSTEM AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 284QS 185 DURING DESCENT AP TRIM FAIL LIGHT ILLUMINATED WITH ASSOCIATED AMBER (E). 2 L 7 2 4F 4 F RT A50NM E44NE 2008041000189 20080410 00189 NM 2008 4 10 YENA2008029 1 20080401 A 2752 C1558161 ACTUATOR EMB ERJ190 ERJ190100IGW 3260408 NM T/E FLAP FAILED A YENA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 15 190JB 6354 6354 19000011 FLT 626, HOU-JFK, FLAP FAIL EICAS MESSAGE ON FLAP/SLAT RETRACTION AFTER TAKEOFF (FLAP 3). PERFORMED QRH PROCEDURE AND L ANDED BACK AT HOU (LANDING WEIGHT 92,000 LBS) NORMAL TOUCHDOWN. REMOVED AND REPLACED RIGHT NR 4 FLAP ACTUATOR IAW E190 AMM 27-51-01, OPERATIONAL CHECK NORMAL. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A57NM 2008041000199 20080410 00199 NM 2008 4 10 MASA200800281 1 20080331 A 5753 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 4 WORN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 988HA 426 LEFT NR 4 FLAP TRACK WORN UPPER, LOWER, AND MID. REPAIRED FLAP TRACK. 2 H 7 2 4T RT A13NM 2008041000207 20080410 00207 SO 2008 4 10 RAIA00804002 1 20080401 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 813HK 145044 PRE FLT 5578 STL - EMERGENCY LIGHT AT ROW 17 INOPERATIVE. MAINTENANCE RE-SECURED A LOOSE WIRE TO THE LIGHT ASSEMBLY. 2 L 7 2 4T RT T00011AT 2008041000208 20080410 00208 NM 2008 4 10 CALA0800298 1 20080402 A 5315 BAC1518338 FLOORBEAM BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 21108 27298 CABIN FLOORBEAM CORROSION AT STA 365, RBL 15. INSTALLED REPAIR TO FLOORBEAM UPPER CHORD PER SRM 53-00-51 REPAIR 3. 2 L 7 2 4F RT A2NM 2008041000211 20080410 00211 NM 2008 4 10 SWAA081787 1 20080402 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 701GS 27836 DURING SCHEDULED HC1 CHECK, RIGHT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008041000225 20080410 00225 NM 2008 4 10 2008UALA01867 1 20080402 A 3350 BATTERY PACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 808UA 804 DOOR 1L EPSU FAULT. REPLACED BATTERY PACK. 2 L 7 2 4F 4 F RT A28NM E40NE 20080521 EU 2008 5 21 2008UALA02514 1 20080429 A 2730 3945128102 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ELAC FAILED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 470UA 1427 ELAC 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. F-CTL CREW COMMENTS, MULTIPLE ELAC 2 FAULTS ON DESC INTO DEN. AP2 WAS ENG AGED AT THE TIME. SWITCH TO AP1 NO ELAC2. INTERNAL CARD Q4 FAILING CH 2 INITIALIZING TEST. ELAC FAULTING. REPLACED E LAC 2, OPS TESTING GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041000227 20080410 00227 NM 2008 4 10 2008UALA01869 1 20080402 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY CEILING LIGHT ABOVE ROW 12 INOP. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041000239 20080410 00239 NM 2008 4 10 2008UALA01876 1 20080402 A 5314 KEELBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 727 WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 ANGLE AT KEEL BEAM IS WORN ON LOWER SURFACE, LT WHEEL WELL, BS 727 LBL 12. BLENDED AREA TO REMOVED DAMAGE WITH MATERIAL LOSS OF .005" IN THE DEEPEST AREA. WITHIN LIMITS OF ARM. TREATED & PRIMED. 2 L 7 2 4F 4 F RT A16WE E21EU 2008041000255 20080410 00255 NM 2008 4 10 2008UALA01896 1 20080402 A 5210 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 535UA 25130 L-4 DOOR EMERGENCY POWER BOTTLE HAS LOW PRESSURE INDICATION. REPLACED L4 DOOR EMERGENCY POWER BOTTLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041000256 20080410 00256 NM 2008 4 10 2008UALA01897 1 20080403 A 5210 PAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 L-1 DOOR HANDLE PAN GOUGED. REPLACED PAN. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041000259 20080410 00259 NM 2008 4 10 2008UALA01898 1 20080403 A 2520 MOUNT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BARRIER BAR OBSTRUCTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 593UA 28144 SECONDARY BARRIER DOES NOT LOCK. FOUND DEBRIS IN FLOOR MOUNT HOLE WHERE SLIDE BAR SITS IN. CLEANED HOLE OF DEBRIS, LUB ED BAR AND LATCHES, INSTALLED BARRIER, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041000262 20080410 00262 NM 2008 4 10 2008UALA01899 1 20080402 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY LIGHT SEAT 53 RT INOP. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041000263 20080410 00263 NM 2008 4 10 2008UALA01900 1 20080402 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 171UA 24322 LAV 111 SIDEWALL EEL LIGHT PIN BROKEN. FOUND CONNECTOR PIN BROKEN. REPLACED PIN OPS CHECKED OK. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041000265 20080410 00265 NM 2008 4 10 2008UALA01901 1 20080402 A 2560 G3060 PANEL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMER EVAC SYS FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY EVACUATION SYSTEM INTERMITTENT AT L3. FOUND EMERGENCY EVACUATION PANEL FAULTY. REPLACED EMERGENCY EVACUATION P ANEL OP CHECK NORMAL PER MM25-63-01 PB400 PARA 2. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041000277 20080410 00277 NM 2008 4 10 2008UALA01906 1 20080402 A 3350 S283T0143 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 658UA 27113 EXTERNAL EMERGENCY LIGHT RT OVERWING INOP. REMOVED AND REPLACED BATTERY PACK OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041000278 20080410 00278 NM 2008 4 10 2008UALA01907 1 20080402 A 3350 S283T0143 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 658UA 27113 EXTERNAL EMERGENCY LIGHT RT OVERWING INOP. REMOVED AND REPLACED BATTERY PACK OPS CHECKED GOOD. AC OK FOR SERVICE. REMOV ED AND REPLACED BATTERY PACK AND OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041000279 20080410 00279 NM 2008 4 10 2008UALA01908 1 20080402 A 3350 S283T0143 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 658UA 27113 EXTERNAL EMERGENCY LIGHT LT AFT OF OVERWING SLIDE INOP. RELAMPED AND REPLACED BATTERY PACK OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041000280 20080410 00280 NM 2008 4 10 2008UALA01909 1 20080402 A 3350 582233582240 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN DEFECTIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 672UA 30027 EMERGENCY EXIT LIGHTS COME ON OCCL NEAR 2L. REPLACED POWER SUPPLY M737 & BATTERY FOR POWER SUPPLY UNIT M1559. OP CHKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041000282 20080410 00282 NM 2008 4 10 2008UALA01911 1 20080403 A 2820 SHUTOFF VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE FUEL SYSTEM LEAKING A UALA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 29 671UA 30026 LEFT O/B FUEL VALVE LEAKING THROUGH MANUAL OPERATION KNOB. FOUND LEAKING FUEL SHUT OFF VALVE ALSO FOUND A FAULTY RELAY K 180 FOR VALVE OPERATION.REPLACED 1 EACH VALVE AND 1 EACH RELAY. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041000288 20080410 00288 NM 2008 4 10 2008UALA01917 1 20080403 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 FWD PIT AT STA 620 BETWEEN STR 24L AND 25L, FRAME INBOARD FLANGE DENTED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SEC TION OF FRAME INBD FLANGE. FABRICATED & INSTALLED A REPAIR ANGLE, STRINGER CLIP (140N2001-80) & SHEAR TIE (140N2002-724 ). 2 L 7 2 4F 4 F RT A2NM E17NE 2008041000290 20080410 00290 NM 2008 4 10 2008UALA01919 1 20080403 A 5311 FRAME SPLICE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 AFT PIT STA 1520 BETWEEN STR 22R AND STR 25R FRAME SPLICE HAS TOOL MARKS. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED FRAME SPLICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041000291 20080410 00291 NM 2008 4 10 2008UALA01920 1 20080403 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 FLOORBEAM AT STA 365 RBL 5R MAIN CABIN. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED T-CAP. FABRICATED AND INSTALLED NE W T-CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041000304 20080410 00304 EA 2008 4 10 MASA200800286 1 20080403 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 933LR 15033 ASH FLT 2709 PHX. TWO PASSENGER DOOR EMERGENCY LIGHTS INOP. RELAMPED EMERGENCY LIGHTS. 2 L 7 2 4F RT A21EA 2008041000305 20080410 00305 EA 2008 4 10 MASA200800288 1 20080404 A 2510 MECHANISM CNDAIR CL600 CL6002B19 1900309 EA JUMP SEAT LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37342 7342 ASH FLT 7136 ORD-OVERNIGHT. F/A JUMP SEAT WAS DIFFICULT TO UNLATCH TO STOW. MX LUBED THE LATCH MECHANISM AND THE SEAT OP CHECKED GOOD. 2 L 7 2 4F RT A21EA 2008041000306 20080410 00306 EA 2008 4 10 MASA200800289 1 20080404 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27172 7172 FLT 7280, ORD-BHM. PASSENGER DOOR WILL NOT CLOSE FROM THE CABIN. CLEANED AND LUBED DOOR HANDLE. 2 L 7 2 4F RT A21EA 2008041000309 20080410 00309 EA 2008 4 10 MASA200800294 1 20080405 A 5210 ROD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27172 7172 FLT 7287, IAD-PVD. PAX DOOR PLUNGER WILL NOT ENGAGE FROM THE INSIDE. MX ADJUSTED DOOR ROD. 2 L 7 2 4F RT A21EA 2008041000310 20080410 00310 SO 2008 4 10 RAIA00804003 1 20080401 A 3350 RPSB1 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 844HK 14500838 PRE FLT 7922 IAD - EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY . SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008041000179 20080410 00179 WP 2008 4 10 UPS08851957 1 20080402 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK. 2 L 7 4 4F RT 4A25 2008041000181 20080410 00181 CE 2008 4 10 DXTA20082981 1 20080406 A 3246 WHEEL CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 943QS 7500043 SEVERE NOSEWHEEL SHIMMY ON T/O ROLL, PRIOR TO 80 KTS. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008041000222 20080410 00222 NM 2008 4 10 2008UALA01864 1 20080330 A 2560 GIRT BAR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOOR OUT OF ADJUST A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 819UA 893 DOOR 2R DIFFICULT TO ARM ON GRD AND DISARMED IN FLT AT 7.0 AGL. ADJUSTED AFT FLOOR GIRT BAR FITTING TO PROVIDE CLEARANC E, DOOR ARMS AND DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041000242 20080410 00242 EU 2008 4 10 2008UALA01888 1 20080403 A 2920 GEARBOX AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RAM AIR TURBINE LEAKING A UALA O OTHER W K INADEQUATE Q C FLUID LOSS IN INSP/MAINT 1 WP 29 459UA 1192 RAM AIR TURBINE LEAKING OIL FROM GEAR BOX. FOUND GROUND POWER PUMP SEAL FAILED AND FORCED FLUID INTO GEAR. REPLACED RAT . ALL OPS CHECKS WERE OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041000267 20080410 00267 CE 2008 4 10 DGCA032008001 1 20080320 A 7714 30738275 MONOPOLE RAYTHN DH125 HAWKER800 7450004 CE GARRTT TFE731 TFE731* 01518 WP LT ENGINE INOPERATIVE E DGCA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 5119 54 258177 P91479 N1 INDICATION SHOWED ZERO. NR 1 ENGINE COMPUTER DROPPED OFF LINE. 2 L 7 2 4F 4 F RT A3EU E6WE 2008041000268 20080410 00268 NM 2008 4 10 08FDEA01294 1 20080403 A 5330 SKIN BOEING 727 727225 1384077 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 DENT RT AFT LWR FUSELAGE BS 1243 S21R CUT OUT DAMAGED AREA 3" BY 3/4" IAW SRM 53-30-3 FIG 1. FABRICATED DOUBLER REPAIR IAW SRM 53-30-3 FIG 1, AND 53-30-2 FIG 3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 . 2 L 7 3 4F A3WE 2008041000269 20080410 00269 NM 2008 4 10 2008UALA01877 1 20080402 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 305 S13L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 FUSELAGE INTERNAL SKIN BEAR STRAP CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT BS 305 ABOVE STR 13L. MAJOR REPAIR ACCOM PLISHED: REMOVED DAMAGE. INSTALLED REPAIR FILLER & DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008041000271 20080410 00271 NM 2008 4 10 2008UALA01880 1 20080402 A 5314 KEELBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 712-727 WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 KEELBEAM UPPER FLANGE HAS WEAR AT FASTENER HOLES, LT MLG WW, BS 727-712. MAJOR REPAIR ACCOMPLISHED: BLENDED OUT THE DAMA GE. INSTALLED REPAIR ANGLE WITH FILLERS. 2 L 7 2 4F 4 F RT A16WE E21EU 2008041000272 20080410 00272 NM 2008 4 10 2008UALA01881 1 20080402 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 294 S7L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 UPPER FUSELAGE INTERIOR FORWARD ENTRY DOOR CUTOUT INTERCOSTAL WEB CRACKED AT BS 294.5 AND STRINGER S-7L. ALSO INTERCOST AL WEB AT BS 294.5 STR 12L IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED INTERCOSTAL WEBS BS 294.9 AT S-7L AND S-12L. 2 L 7 2 4F 4 F RT A16WE E21EU 2008041000311 20080410 00311 EU 2008 4 10 YENA2008028 1 20080331 A 2150 753C000002 HEAT EXCHANGER AIRBUS 320 A320232 3930326 EU A/C BAY UNCONTROLLABLE A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 585JB 21653 8063 2159 FLT 433, BOS-MCO, AIR RETURN TO BOS, COCKPIT AND CABIN TEMP UNCONTROLLABLE, FULL COLD SET AND AIR TEMP 156/COCKPIT TEMP GREATER THAN 100 FWD TEMP GREATER 90 IN DESCENT BACK TO BOS, TEMP WENT FROM 156 TO 110 WHEN A/C IN IDLE FOR A WHILE INCR EASED BACK UP WITH PWR UP. REMOVED AND REPLACED ZONE TEMP CONTROLLER & NR 1 PACK TEMP CONTROLLER IAW 21-63-34-04 & 21-6 1-34-04-01, GND CHECK OK. ACCOMPLISHED CONFIDENCE FLIGHT, ISOLATED TEMP RUNAWAY TO LEFT PACK, REMOVED AND REPLACED PRIM ARY HEAT EXCHANGER UNIT, OPS CHECK OK. 2 L 7 2 4F RT A28NM 2008041000314 20080410 00314 NM 2008 4 10 SWAA081825 1 20080406 A 5520 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, RIGHT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 1 HINGE BEARING AND BOLT PE R MM. 2 L 7 2 4F RT A16WE 2008040300208 20080403 00208 WP 2008 4 3 08FDEA01226 1 20080401 A 5311 70750080C FRAME DOUG MD10 MD1010F 3022112 WP FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 MCD-FUSELAGE UPPER LOBE-FRAME AT FS 635, 655, 675, 695, 715, 735, 755 AND 775, LONGERON 13R HAS CHAFED AND DAMAGED FRO M LINER MOUNT FASTENER. REMOVED FRAME SPLICE, FABED NEW SPLICE ON TRAVELER T8/729476, LOCATED AND DRILLED HOLES AND I NSTALLED NEW SPLICE AT STA 635 IAW SRM 51-31-01, 53-30-00 FIG 4. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ATTENTION REC ORDS, THIS IS A CLASS "B" REPAIR AND HAS AN INITIAL REINSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CY CLES. 2 L 7 3 4F RT A22WE 2008040300215 20080403 00215 WP 2008 4 3 08FDEA01233 1 20080401 A 5311 70750080C FRAME DOUG DC10 DC1030F 3023504 WP FUSELAGE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 MCD-FUSELAGE UPPER LOBE-FRAME AT FS 635, 655, 675, 695, 715, 735, 755 AND 775, LONGERON 13R HAS CHAFED DAMAGED FROM LI NER MOUNT FASTENER. REMOVED FRAME SPLICE, FABED NEW SPLICE ON TRAVELER T8/729477, LOCATED AND DRILLED HOLES AND INSTALL ED NEW SPLICE AT STA 755 IAW SRM 51-31-01, 53-30-00 FIG 4. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ATTENTION RECORDS, THIS IS A CLASS "B" REPAIR AND HAS AN INITIAL REINSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTIONS AT 9,500 CYCLES. 2 L 7 3 4F RT A22WE 2008040400032 20080404 00032 EU 2008 4 4 2008UALA01776 1 20080329 A 5210 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 492UA 1755 RAMP REPORTS DENT IN BOTTOM OF DOOR 2 LEFT. MAJOR REPAIR WAS ACCOMPLISHED, CUT OUT DAMAGE AND REPAIRED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040400042 20080404 00042 NM 2008 4 4 2008UALA01788 1 20080330 A 3520 B-NUT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE PAX OXYGEN LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 PAX O2 READS 1460 PSI FROM COCKPIT EICAS. AFTER EXTENSIVE TROUBLE SHOOTING FOUND LEAK IN OXYGEN LINE B-NUT. TIGHTENED B-NUT SERVICED OXYGEN SYSTEM. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040400050 20080404 00050 NM 2008 4 4 2008UALA01796 1 20080328 A 3350 20121 CHARGER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 936UA 26667 FWD ENTRY AND RT EMERGENCY LIGHTS INOP, REPLACED CHARGER M1132 AND CHKD OK, REF WD 33-51-12. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040400051 20080404 00051 NM 2008 4 4 2008UALA01797 1 20080329 A 2611 CGAB140001 SMOKE DETECTOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO BAY FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 332UA 24193 CARGO FIRE FWD A FAIL AMBER LIGHT REMAINS ON AFTER TEST. FOUND FAULTY SMOKE DETECTOR. REPLACED SMOKE DETECTOR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040400067 20080404 00067 NM 2008 4 4 2008UALA01817 1 20080331 A 5320 SUPPORT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE INTERCOSTAL CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 INTERCOSTAL WEB SUPPORT CLIP, C-T FUSELAGE SKIN, BETWEEN STA 348.2 TO 360 CRACKED AT STR 14L. MAJOR REPAIR ACCOMPLISHED . 2 L 7 2 4F 4 F RT A16WE E2GL 2008040400071 20080404 00071 NM 2008 4 4 2008UALA01821 1 20080331 A 5311 146T1513 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1351 S26-28R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 FRAME IS TORN OUT STA 1351 BETWEEN STR 28R-26R. REPAIRED FRAME IAW SRM 53-00-01 FIG 201 DETAIL II AND SRM 51-40-02. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040400076 20080404 00076 NM 2008 4 4 2008UALA01826 1 20080331 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 365 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 CORROSION ON FLOORBEAM AT STA 365 RBL 5R MAIN CABIN. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED T-CAP. FABRICATED NEW T -CAP & INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040400080 20080404 00080 NM 2008 4 4 2008UALA01831 1 20080331 A 3397 CONNECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 845UA 1585 19 ABC 20 ABC EMERGENCY GENERATOR LIGHT INOP. FOUND CONNECTOR BY SEAT 20 ABC LOOSE AND UNSECURED. RECONNECTED CONNECTOR AND SECURED WIRE, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040400086 20080404 00086 NM 2008 4 4 2008UALA01837 1 20080401 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY EXIT EEL LIGHT INOP, AT SEAT 40L. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040400092 20080404 00092 NM 2008 4 4 2008UALA01843 1 20080331 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 777UA 26916 EMERGENCY LIGHTS INOP ENTIRE D ZONES SEATS BOTH SIDES. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040400102 20080404 00102 SO 2008 4 4 LR7A08047 1 20080331 A 5230 3410587 FITTING LKHEED 382 382G 526414U SO CARGO DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 621 4676 DURING SCHEDULED B-1 CHECK, PER JOB CARD HB5302, FOUND RAMP DOOR RT ACTUATING HORN FITTING CRACKED AT RS8.4 RT. REPAIR ACCOMPLISHED BY REPLACING FITTING IAW SMP581-91-00 PARA 10, PG 209. 2 H 7 4 4T A1SO 2008040400151 20080404 00151 NM 2008 4 4 DLM90080455 1 20080331 A 5230 59101419 SKIN DOUG MD90 MD9030 3023690 NM CARGO DOOR DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 AFT CARGO DOOR FRONT SKIN HAS SEVERAL DENTS. REPAIRED DENT IN CARGO DOOR, IAW MD80 SRM 52-05D, FIG 3. ALL OTHER DENTS COND 1A, IAW MD90 SRM 53-30-02, PG 11 TABLE 3. 2 L 7 2 4F RT A6WE 2008041000317 20080410 00317 NM 2008 4 10 SWAA081826 1 20080405 A 3350 65C27093 LIGHT BOEING 737 7373Q8 1384670 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008041000318 20080410 00318 NM 2008 4 10 SWAA081843 1 20080404 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, BETWEEN STR 16R AND STR 17R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008041000319 20080410 00319 NM 2008 4 10 SWAA081842 1 20080404 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 FUSELAGE SKIN CRACKED BETWEEN BS 312 AND BS 317, STR 18R AND STR 20R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008041000320 20080410 00320 NM 2008 4 10 SWAA081827 1 20080406 A 3350 8200048901 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 715SW 27849 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2008041000321 20080410 00321 NM 2008 4 10 SWAA081841 1 20080405 A 5610 141A48501 WINDOW BOEING 737 7377H4 1384404 NM COCKPIT ARCED A SWAA K NONE O OTHER CR CRUISE 1 SW 29 744SW 29490 FLIGHT DECK L1 WINDOW ARCED AND WINDOW CRACKED. REMOVED AND REPLACED L1 WINDOW AND HEAT CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2008041000322 20080410 00322 NM 2008 4 10 SWAA081835 1 20080403 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 770SA 30589 DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 15 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008041000323 20080410 00323 2008 4 10 SWAA081836 4 20080403 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 770SA 30589 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008041000325 20080410 00325 NM 2008 4 10 SWAA081837 1 20080403 A 5743 115A5211 FITTING BOEING 737 7377Q8 1384418 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 799SW 28209 DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION FITTING LUG CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008041000326 20080410 00326 NM 2008 4 10 SWAA081838 1 20080403 A 5743 115A5211 FITTING BOEING 737 7377Q8 1384418 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 799SW 28209 DURING SCHEDULED MV2 CHECK, FOUND LEFT MLG FWD TRUNNION FITTING LUG CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008041000331 20080410 00331 NM 2008 4 10 2008UALA01886 1 20080402 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1197 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 AFT PIT AT BS 1197+132 AND LBL 40 FRAME T-CAP IS CORRODED UNDER AND AROUND NUT PLATE. MAJOR REPAIR ACCOMPLISHED: REMOVE D & REPLACED T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041000332 20080410 00332 NM 2008 4 10 CALA0800290 1 20080317 A 5320 651768465 ATTACH FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 BODY STA 303 STRINGER 10L CRACK FOUND AT DOOR HINGE LOWER WEB, SKIN ATTACH CLIP MARKED. REPAIRED STRINGER 10LT LOWER WE B SKIN ATTACH CLIP AT BS 303 PER PACE EA 350-53-003 CAL AND EC/RA 5310-04741. 2 L 7 2 4F RT A16WE 2008041000333 20080410 00333 NM 2008 4 10 CALA0800302 1 20080404 A 5320 65458078 WEB BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 46625 27529 WEB CRACKED STA 277 AT S14R. INSTALLED WEB ASSY IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041000334 20080410 00334 NM 2008 4 10 CALA0800303 1 20080404 A 5330 65C32357 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE MISREPAIRED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14346 23584 SKIN REPAIR AT STA 420 TO 440 BETWEEN STR 16L TO 20L MISSING FIELD FASTENERS. REMOVED EXISTING DOUBLER, FABRICATED AND INSTALLED NEW REPAIR IN REF TO SRM 53-00-01, REPAIR 31. PLACED ON DIP PER ECRA 5331-01399 ACCOMPLISH PERMANENT REPAIR B EFORE 60,000 FLT CYCLES. 2 L 7 2 4F RT A16WE 2008041000336 20080410 00336 NM 2008 4 10 CALA0800305 1 20080311 A 5320 9086105 ATTACH BRACKET BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11641 28902 INTERCOSTAL ATTACH CLIP TO FRAME STA 348 AT STR 12 LT IS CRACKED. REPAIRED PER PACE EA 641-53-001CAL AND EC/RA 5310-047 42. 2 L 7 2 4F RT A16WE 2008041100005 20080411 00005 EA 2008 4 11 A6WA200840229 1 20080319 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION AP APPROACH 1 GL 31 452AW 7835 AFTER SELECTING GEAR DOWN GOT GEAR DISAGREE MESSAGE, RT MLG DID NOT EXTEND. COMPLIED WITH QRH, ALL THREE GEAR EXTENDED DOWN AND LOCKED AND ALL GREEN. DURING GEARDOWN SELECTION, HEAVY SIDE WIND GUST. (M) 2 L 7 2 4F RT A21EA 2008041100009 20080411 00009 EU 2008 4 11 08FDEA01372 1 20080410 A 5755 A57771000004 SPOILER PANEL AIRBUS 300 A300B4622R 3930312 EU NR 3 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND DELAMINATION OUT OF LIMIT ON SPOILER NR 3 LT. REPAIR PERFORMED BY REPLACEMENT OF IAW AMM 25-61-51. 2 L 7 2 4F RT A35EU 2008041100015 20080411 00015 EA 2008 4 11 A6WA200840146 1 20080219 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 S14L CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 BTW - FS 621 AND 625.3 AT STRINGER 14 LEFT AND RIGHT SIDE, INTERCOSTAL FITTING FOUND CRACKED. REPLACED INTERCOSTAL FITT ING IAW SRM 51-42-20. (M) 2 L 7 2 4F RT A21EA 2008041100016 20080411 00016 EA 2008 4 11 A6WA200840233 1 20080322 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY DOOR ILLUMINATED A A6WA O OTHER N FALSE WARNING CR CRUISE 1 GL 31 440AW 7766 RIGHT EMERGENCY DOOR OVERWING CAUTION MESSAGE IN CRUISE. COMPLIED WITH QRH MESSAGE DISAPPEARED AFTER LANDING AND AIRCRA FT DEPRESSURIZED. CLEARED PSEU FAULTS REF AMM 32-60-00 AND PRESSURIZED AIRCRAFT, NO DEFECTS NOTED AT THIS TIME, AIRCRAF T OK TO CONTINUE SERVICE. (M) 2 L 7 2 4F RT A21EA 2008041100020 20080411 00020 NM 2008 4 11 GTIA0800052 1 20080325 A 2620 PIPE AIRBUS A319 A319132 3930340 NM FIRE EXTING CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 503NK 2470 ENGINE FIRE EXTINGUISHING PIPE OVER THE HOT SECTION (NR 2 ENG) IS CRACKED. REMOVED AND REPLACED PIPE AFT SECTION IAW A3 19 AMM 26-21-49. 2 L 7 2 4F RT A28NM 2008041100021 20080411 00021 WP 2008 4 11 IXXA08SMN081S 1 20080215 A 5340 FITTING DOUG DC8 DC871F 302199D WP BS 857 L1 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 857.000 LONGERON 1. REMOVED CRACKED FITTING. FABRICATED FITTING PERFORMED LIQUID PENETRANT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TRE ATED AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING DC8 SRM 51-3-1, DC8 SRM 51-1-20D, DC8 SRM 51-1-8B, ATI REPAIR S PECIFICATION NUMBER 2003-05, DRAWING DOUGLAS 3779900, AND SPM PART 08-00-02 TO 07. 2 L 7 4 4F RT 4A25 2008041100023 20080411 00023 EA 2008 4 11 A6WA200840200 1 20080317 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION AP APPROACH 1 GL 31 455AW 7848 FLAPS FAIL CAUTION MESSAGE FLAPS FAILED AT 0 DURING EXTENSION. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEP S 1.3 AND 1.4 FLAP SYSTEM RESET, OK. (M) 2 L 7 2 4F RT A21EA 2008041100025 20080411 00025 EA 2008 4 11 A6WA200840169 1 20080229 A 5210 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 ON PAX DOOR, STIFFENER ANGLE FOUND CRACK. STIFFENER ON PAX DOOR FS 349. REPLACED IAW SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2008041100029 20080411 00029 EU 2008 4 11 08FDEA01374 1 20080410 A 5320 A53974210210 SPLICE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CORROSION ON SPLICE, C 72, P55-56 LT REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CRACK FREE AND FLAP PEENING IAW RAS/EFW/9000017/2008 ISS C, APPROVED BY EA 6-5317-115240. 2 L 7 2 4F RT A35EU 2008041100030 20080411 00030 EU 2008 4 11 08FDEA01375 1 20080410 A 5313 A5397321420000 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 BULK PIT STR 46 RT FR 67-68 IS CORRODED. REMOVED CORROSION IAW A310-200 SRM 51-22-00. CHECKED LIMITS; MATERIAL REMOVED 100%. FOUND TO BE OUT OF LIMITS IAW SRM 51-10-00. REMOVED STRINGER IAW SRM 51-40-21. RECEIVED NEW STRINGER. DRILLED & LOCATED IAW SRM 51-40-40 & DWG A53973214. INSTALLED IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008041100033 20080411 00033 EU 2008 4 11 NSVA2008019 1 20080409 A 3397 CONNECTOR SAAB SF340 340B 7860101 EU CABIN LIGHT SMOKE A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 350CJ 340B350 FA SMELLED AND SAW SMOKE COMING FROM LIGHTED AREA AT A, PERFORMED PRECAUTIONARY EVACUATION. FOUND SMOKE WAS COMING FROM SEAT 2A BALLAST CONNECTOR, DISCONNECTED POWER TO BALLAST FOR SEAT 2A HAD POWER ON AIRCRAFT NO SMOKE NOTICED AT SEAT 2A, LIGHT SYSTEM REMAINS ON MEL. 2 L 7 2 4T RT A52EU 2008041100034 20080411 00034 EA 2008 4 11 A6WA200840181 1 20080316 A 3310 LIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT SHORTED A A6WA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 31 441ZW 7777 BOTH CAPTAIN AND FIRST OFFICER MAP LIGHTS ARE OUT, CBP2 U6 POPPED. RECYCLED BREAKER ONCE, FIRST OFFICER MAP LIGHT SPARK ED AND SHORTED WHEN MOVED, CBP2 U6 POPPED AGAIN. (M) 2 L 7 2 4F RT A21EA 2008041100035 20080411 00035 EA 2008 4 11 A6WA200840180 1 20080311 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 430AW 7719 EMERGENCY FLOOR LIGHTS ROW 6 AND 7 INOPERATIVE. (M) 2 L 7 2 4F RT A21EA 2008041100037 20080411 00037 NM 2008 4 11 DL757080552 1 20080404 A 5330 143N352110 SKIN PANEL BOEING 757 757232 1384965 NM BS 690 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 644DL 23998 HMV AT SAA, CORROSION WAS FOUND ON THE EXTERNAL SKIN AT THE DME ANTENNA MOUNT AT STA 690, BL 0. THE CORROSION WAS REMOV ED AND A REPAIR WAS INSTALLED WITH BOEING APPROVAL. LFEC INSPECTIONS ARE REQUIRED BEGINNING AT 37,500 CYCLES AND EVERY 3000 CYCLES THEREAFTER. 2 L 7 2 4F RT A2NM 2008041100040 20080411 00040 NM 2008 4 11 DLM88080555 1 20080404 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 719 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DL 49546 FUSELAGE SKIN FOUND WITH CORROSION AT STA 719, L30. CUTOUT DAMAGED SKIN/DOUBLER AND INSTALLED REPAIR DOUBLER/TRIPLER. 2 L 7 2 4F RT A6WE 2008041100043 20080411 00043 2008 4 11 DL76S080560 4 20080405 A 3410 INDICATOR BOEING 767 767332 1382001 NM COCKPIT HOT A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 139DL 25984 EN ROUTE AT FL350 HAD STRONG BURNING SMELL IN COCKPIT. AT ABOUT THAT TIME CAPTS VSI BLANKED. ODOR SUBSIDED AND 5 MINU TES OR SO VSI DISPLAY RETURNED. CONTINUED TO HAVE VERY LIGHT BURNING ODOR. SEEMED TO BE MORE OR SLIGHTLY STRONGER ODOR WHEN ENGINES ACCELERATE. NO C/B`S POPPED. REMOVED CAPTS VSI INDICATOR AND FOUND IT TO BE VERY HOT WITH A BURNING ODOR COMING FROM INDICATOR. REMOVED AND REPLACED SAME. 2 L 7 2 4F RT A1NM 2008041100084 20080411 00084 NM 2008 4 11 070189 1 20080319 A 3350 408822101 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 892GA 49826 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE DEPARTMENT PERSONNEL REPORTED THE RIGHT AND LEFT OVER W ING EXIT LIGHT, FWD EMERGENCY EXIT DOOR (L1)AND THE LEFT FWD FLOOR EMERGENCY EXIT LIGHT INOP WOULD NOT TEST. MAINTENANC E PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACKS. A SATISFACTORY OPERATIONAL CHECK WAS ACCOM PLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT 2008040400158 20080404 00158 NM 2008 4 4 DLM90080462 1 20080326 A 5754 99359406 SKIN DOUG MD90 MD9030 3023690 NM RT WING TE FLAP GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 97118 53392 RIGHT WING I/B FLAP HAS A SHARP DING ON LOWER SURFACE JUST AFT OF NUMBER 3 TIRE. FABRICATED AND INSTALLED NEW SKIN, IAW MD90 SRM 57-03D FIG 807D. 2 L 7 2 4F RT A6WE 2008040400160 20080404 00160 NM 2008 4 4 DLM90080464 1 20080327 A 5322 993607410 SHEAR TIE DOUG MD90 MD9030 3023690 NM CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 FOUND CORROSION ON FRAME Y 1193.0 AT 30L. REMOVED AND REPLACED SHEAR TIE, IAW MD90 SRM 51-30-02 AND 51-30-05. 2 L 7 2 4F RT A6WE 2008040400163 20080404 00163 NM 2008 4 4 DLM90080467 1 20080306 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 588-627 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 CABIN SEAT TRACK LBL 54.5 IS OUT OF LIMITS AT FUSELAGE STA 588-627. REMOVED AND REPLACED SEAT TRACK STA 588-627 LBL 54. 5, IAW MD90 SRM 53-40-01, FIG 6. 2 L 7 2 4F RT A6WE 2008040400169 20080404 00169 NM 2008 4 4 DLM88080476 1 20080402 A 5315 FLOORBEAM DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV GALVANIC CORROSION WAS FOUND ON FLOOR PANEL SUPPORT STA Y=180 FROM X=-1O TO -40 FWD WET AREA. SUPPORT WAS RE PLACED IAW SRM 51-30-2. 2 L 7 2 4F RT A6WE 2008040400171 20080404 00171 NM 2008 4 4 DLM88080478 1 20080402 A 5315 FLOORBEAM DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT STA Y=200 AND X-10 TO -40 FWD WET AREA. FLOOR SUPPORT WAS R EPLACED IAW DOUGLAS DWG 9936534. 2 L 7 2 4F RT A6WE 2008040400172 20080404 00172 NM 2008 4 4 DLM88080479 1 20080402 A 5315 FLOORBEAM DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT STA Y=166 AND X=52 FWD WET AREA. FLOOR SUPPORT WAS REPLACED IAW DOUGLAS DWG 9936534. 2 L 7 2 4F RT A6WE 2008040400173 20080404 00173 NM 2008 4 4 DLM88080480 1 20080402 A 5315 FLOORBEAM DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT STA Y=196 AND X=52 FWD WET AREA. FLOOR SUPPORT WAS REPLACED IAW DOUGLAS DWG 9936534. 2 L 7 2 4F RT A6WE 2008040400176 20080404 00176 NM 2008 4 4 DLM88080483 1 20080402 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV CORROSION WAS FOUND ON RIGHT CUSP WEB BETWEEN STA Y=700 AND 712. CUSP WEB WAS REPAIRED IAW ER/A 398191-14MA. 2 L 7 2 4F RT A6WE 2008040400179 20080404 00179 NM 2008 4 4 DLM88080486 1 20080402 A 5320 SUPPORT DOUG MD88 MD88 3023688 NM BS 275 L27L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV CRACK WAS FOUND ON LT SLANT PANEL SUPPORT AT STA Y=275 AND LONGERON 27 LT. SUPPORT WAS REPLACED IAW ER/A 413 029-14MA REV ORG. 2 L 7 2 4F RT A6WE 2008040400189 20080404 00189 NM 2008 4 4 DLM88080496 1 20080402 A 5230 SUPPORT DOUG MD88 MD88 3023688 NM CARGO DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, A CRACKED STOP SUPPORT WAS FOUND AT AFT UPPER SIDE OF C3 DOOR. SUPPORT WAS REPLACED IAW DOUGLAS DWG 5910141 REV EY. 2 L 7 2 4F RT A6WE 2008040400190 20080404 00190 NM 2008 4 4 DLM88080497 1 20080402 A 5320 SUPPORT DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV A CRACKED SUPPORT WAS FOUND FOR PANEL NR 693A. SUPPORT WAS REPLACED IAW DWG 9952521. 2 L 7 2 4F RT A6WE 2008040400192 20080404 00192 NM 2008 4 4 DLM88080499 1 20080402 A 5740 ATTACH FITTING DOUG MD88 MD88 3023688 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV A CRACK WAS FOUND ON RIGHT WING LEADING EDGE CLIP AT STA XRS=271. CLIP WAS REPLACED IAW SRM 51-30-2 AND 51-3 0-5. 2 L 7 2 4F RT A6WE 2008040400193 20080404 00193 NM 2008 4 4 DLM88080500 1 20080402 A 5320 FLOOR SUPPORT DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV A CRACK WAS FOUND ON SUPPORT FOR CABIN FLOOR PANEL NR 927E. SUPPORT WAS REPAIRED IAW SRM 51-90-0D. 2 L 7 2 4F RT A6WE 2008040700003 20080407 00003 NM 2008 4 7 AALA200800608 1 20080312 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AA 24617 DFW - EMERGENCY EXIT IDENTIFIER LIGHT AT AFT OF LEFT AFT PASSENGER DOOR AT L00760 IS BROKEN. REPLACED LIGHT FOR EMERGEN CY EXIT IDENTIFIER LIGHT AT AFT OF LEFT AFT PASSENGER DOOR AT L00760. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040700009 20080407 00009 NM 2008 4 7 AALA200800606 1 20080312 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AA 24617 DFW - EMERGENCY EXIT IDENTIFIER LIGHT AT AFT RIGHT NUMBER ONE DOOR BROKEN. REPLACED LIGHT FOR EMERGENCY EXIT IDENTIFIER LIGHT AT AFT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040700013 20080407 00013 NM 2008 4 7 AALA200800620 1 20080312 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 794AN 30256 DFW - EMERGENCY EXIT LIGHT AT OVERHEAD LEFT SEAT ROW 11 HAS DAMAGED LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD LEFT SEAT ROW 11. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040700015 20080407 00015 NM 2008 4 7 AALA200800618 1 20080312 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 794AN 30256 DFW - EMERGENCY EXIT LIGHT AT OVERHEAD LEFT NUMBER THREE DOOR HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVE RHEAD LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040700017 20080407 00017 WP 2008 4 7 AALA200800610 1 20080312 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70524 49916 LGA - EMERGENCY LIGHT AT OVERWING RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERW ING RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008040700018 20080407 00018 NM 2008 4 7 AALA200800611 1 20080312 A 3350 CM767 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 346AN 33085 SFO - EXTERIOR EMERGENCY LIGHT AT AFT RIGHT OVERWING DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT AF T RIGHT OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008040700020 20080407 00020 NM 2008 4 7 AALA200800616 1 20080312 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 686AA 25343 DFW - EMERGENCY LIGHTS AT OVERHEAD WING EXIT INOPRATIVE. REPLACED BATTERY PACK AT SEAT ROW 25 RIGHT FOR EMERGENCY LIGHT S AT OVERHEAD WING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040700021 20080407 00021 NM 2008 4 7 AALA200800617 1 20080312 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 686AA 25343 DFW - EMERGENCY EXIT LIGHT AT SEAT ROW 27 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040700031 20080407 00031 NM 2008 4 7 DLM88080509 1 20080402 A 5320 ANGLE DOUG MD88 MD88 3023688 NM BS 1485 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV A CRACK ANGLE WAS FOUND AT STA Y=1485 AND 1:00 POSITION AT AFT ACCESSORY COMPARTMENT. ANGLE WAS REPLACED IAW DWG 9911842. 2 L 7 2 4F RT A6WE 2008040700033 20080407 00033 NM 2008 4 7 DL76G080511 1 20080401 A 5711 112T2001107 SPAR BOEING 767 767332 1382001 NM LT WING DAMAGED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 1605 30198 LT WING FRONT SPAR CONTACTED RT HORIZ STAB OF 737 WHILE PARKING AT HANGAR. LT SPAR UPPER AND LOWER CAPS AND WEB SPLICED . 2 L 7 2 4F RT A1NM 2008040700036 20080407 00036 NM 2008 4 7 DLM88080514 1 20080402 A 5347 SEAT TRACK DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV BLEND OUT AREA WAS FOUND TO BE OUT OF LIMIT ON SEAT TRACK AT STA Y=1025 X=54. SEAT TRACK WAS REPAIRED IAW SR M 53-05D FIG 4F. 2 L 7 2 4F RT A6WE 2008040700038 20080407 00038 NM 2008 4 7 DLM88080516 1 20080402 A 5347 SEAT TRACK DOUG MD88 MD88 3023688 NM BS 996 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, BLEND OUT AREA WAS FOUND TO BE OUT OF LIMIT ON SEAT TRACK AT STA Y=996 X=54. SEAT TRACK TO BE REPLACED ON N RC T0088136. 2 L 7 2 4F RT A6WE 2008040700046 20080407 00046 NM 2008 4 7 DLM88080524 1 20080403 A 5313 LONGERON DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, A CRACK WAS FOUND ON LONGERON 24 LT AT STA Y=200AT E/E COMPARTMENT. LONGERON WAS REPAIRED IAW SRM 53-02 FIG 18. 2 L 7 2 4F RT A6WE 2008040700048 20080407 00048 NM 2008 4 7 DLM88080526 1 20080403 A 5230 PAN DOUG MD88 MD88 3023688 NM AFT CARGO DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, A CRACK WAS FOUND ON PAN FWD EDGE OF C3 AT BEAM NR 2 PAN WAS REPAIRED IAW SRM 52-05D FIG 50. 2 L 7 2 4F RT A6WE 2008040700051 20080407 00051 EA 2008 4 7 A6WA200840126 1 20080226 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 BULKHEAD WEB FLOORBEAM CRACK AT FS 280 RBL 9.0. REPAIR PERFORMED IAW REO 601R53-11-171 REV D SCHEM B. (M) 2 L 7 2 4F RT A21EA 2008040700053 20080407 00053 EA 2008 4 7 A6WA200840128 1 20080228 A 5230 HOUSING CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 GOUGE ON CARGO DOOR HANDLE HOUSING OF .300 LONG BY .140 WIDE AND .100 DEEP. REPLACED WITH NEW PART IAW SRM 51-42-21. ( M) 2 L 7 2 4F RT A21EA 2008040700054 20080407 00054 EA 2008 4 7 A6WA200840129 1 20080226 A 5200 STOP CNDAIR CL600 CL6002B19 1900309 EA DOOR BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 LT WING DOOR STOP ASSY BROKEN W/S 163.00. REPLACED IAW SRM 51-42-06, 51-42-13. (M) 2 L 7 2 4F RT A21EA 2008040700057 20080407 00057 NE 2008 4 7 HALA0800473 2 20080331 A 7230 BLADE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE RT ENG FAN DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, RT ENG FAN BLADE 22 HAS NICK. REPAIRED PER AMM TASK 72-31-02. EDDY CURRENT GOOD. NO CRACKS IND NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040700058 20080407 00058 NE 2008 4 7 HALA0800474 2 20080331 A 7230 BLADE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE LT ENGINE FAN DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, LT ENG FAN BLADE HAS NICK ON NR 18. REPAIRED PER AMM 72-31-02. EDDY CURRENT CHECKED. NO CRA CKS IND NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040700059 20080407 00059 NM 2008 4 7 HALA0800475 1 20080331 A 7330 BLADE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE LT ENGINE FAN DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, LT ENG FAN BLADE HAS NICK ON NR 17. REPAIRED PER AMM 72-31-02. EDDY CURRENT CHECKED. NO CRA CKS IND NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040800003 20080408 00003 CE 2008 4 8 DJFA200837 1 20080401 A 2130 DUCT RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP CABIN AIR LOOSE E DJFA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 EA 23 817LX 258516 DURING CLIMB AT FL 320 THE CABIN PRESSURE BEGAN CLIMBING AT 2000 FPM. THE CREW FOLLOWED THERE EMERGENCY PROCEDURES AND M ADE A EMERGENCY DESCENT. DURING THE DESCENT THE CABIN PRESSURE RATE MATCHED THE AIRCRAFT DESCENT RATE. THE AIRCRAFT DIVE RTED TO KORF AND LANDED SAFELY. MX PERFORMED VISUAL INSPECTION OF DUCTING IN REAR BAY AND FOUND DUCTS LOOSE AT THE SIL ENCER DUCT. THEY RESECURED AND PERFORMED A FULL OPS AND LEAK CHECK. 2 L 7 2 4F 4 F RT A3EU E6WE 2008040800011 20080408 00011 NM 2008 4 8 ZZDA2008083 1 20080319 A 2120 UNKNOWN BOEING 717 717200 1383700 NM CABIN ODOR A ZZDA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 37 942AT 55005 BURNING PLASTIC SMELL IN FWD CABIN AREA. ALL 3 F/A'S VERIFIED SMELL. PILOT AND COPILOT SMELLED ODOR IN COCKPIT. AFT F /A STATED GETTING ODOR IN AFT CABIN. DECLARED EMERGENCY AND LANDED UNEVENTFULLY LANDING WT 103,500 AFT SECTION OF CABIN PASSENGERS ALSO SMELLED PLASTIC ODOR. PERFORMED SPECIAL INSPECTION REF AIR TRAN GMM 8115. INSPECTED AIRCRAFT, ALL ELE CTRICAL POWER, LIGHTING, ENGINES, APU, PNEUMATIC SYS OR UNUSUAL ODORS NOTED. PERFORMED HIGH POWER RUN PER M/M 71-00, OP S CK'D GOOD. NO ODORS DETECTED, UPON INITIAL ENTRY INTO CABIN NO UNUSUAL ODORS NOTED. 2 L 7 2 4F TR A6WE 2008040800013 20080408 00013 SO 2008 4 8 FDKA200803116 1 20080318 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO A/C BAY MALFUNCTIONED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 852MJ 13689 145567 FDM 6014 JFK- BUF (1856 PHX LCL). COCKPIT FILLED WITH SMOKE AND HAD A BURNING PLASTIC SMELL. MX REMOVED AND REPLACED A IR CYCLE MACHINE. 2 L 7 2 4T RT T00011AT 2008040800014 20080408 00014 SO 2008 4 8 FDKA200803120 1 20080319 A 3350 SIGN EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6199 JFK-RIC (1401 PHX LCL). EMERGENCY LIGHT/SIGN OUT AT ROW 12. MX RESET EMERGENCY LIGHTING SYSTEM. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008040800015 20080408 00015 SO 2008 4 8 FDKA200803121 1 20080319 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6008 JFK-RDU (1922 PHX LCL). ROW 12 OVERHEAD EMERGENCY EXIT LIGHT WAS INOPERATIVE. MX RE-SECURED THE WIRE AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2008040300086 20080403 00086 SW 2008 4 3 HEER118982 1 20080229 A 5330 407030450101 SKIN BELL 407 407 1182206 SW FUSELAGE CORRODED B HEER K NONE O OTHER NR NOT REPORTED 1 SW 99 407PH 53003 CORROSION ON TUB AT APICAL FLOAT AND LIFE RAFT BOTTLE MOUNT AREA. REMOVED CORRODED AREAS OF SKIN AND REPAIRED USING PRE -BOND MATERIAL FOR FILLERS AND DOUBLERS. INSTALLED USING 934 AND CHERRY MAX BLIND FASTENERS. 1 G 7 1 3U O H2SW 2008040300104 20080403 00104 EA 2008 4 3 COMA0860184 1 20080320 A 3097 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYSTEM LOOSE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 914CA 7012 RECEIVED RIGHT COWL ANTI-ICE CAUTION MESSAGE WHEN SELECTING ANTI-ICE OFF. FOLLOWED QRH, DIVERTED TO IND, LANDED WITHOUT INCIDENT. RESECURED RIGHT COWL ANTI-ICE PLUG. NO FURTHER INCIDENT. 2 L 7 2 4F RT A21EA 2008040300107 20080403 00107 WP 2008 4 3 IXXA08SMN074S 1 20080214 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE LOWER OUTER SKIN SHOWS IMPROPER REPAIR AT STATIO N XFS 304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORM ED NDT INSP. NO CRACK, NO CORROSION FOUND. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLERS. CLEANED, TREATED, PR IMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS AT XFS 297.500 - STA XFS 341.500 IAW DC8 SRM 51-1-1 1, DC8 SRM 51-1-21, DC8 SRM 51-3-1, FAA FORM 8110-3 NUMBER 08086 DATED 02-27-08, SEMAN DRAWING NUMBER ED-4706 DATED 02-0 9-08, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008040300112 20080403 00112 WP 2008 4 3 IXXA08SMN076S 1 20080214 A 5522 SKIN DOUG DC8 DC871F 302199D WP LT ELEVATOR DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND ELEVATOR LEFT UPPER SKIN SHOWS DENTS AND CORROSION AT DIFFERENT POINTS AT STATI ON XE 146.000 AND XE 270.000. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM RE PAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, AND FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TRE ATED AND PRIMED AREA AND REPAIR PARTS. BALANCED AND FOUND TO BE WITHIN LIMITS MOMENT: 1473.4 INCH-POUND. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, DC8 SRM 51-1-8 PAGES 17 AND 18, DC8 SRM 55-2-0 PAGE 12, DC8 SRM 55-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 55-4-1 FIGURE 1 SHEETS 1 AND 2 ITEMS "E" AND "F", DC8 SRM 51-1-9 T/R 51-142, DC8 SRM 51-1-9 2 L 7 4 4F RT 4A25 2008040300113 20080403 00113 WP 2008 4 3 NWAA081269858 1 20080318 A 5330 SKIN DOUG DC9 DC951 3022051 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 767NC 47724 DURING "H" CHECK, FOUND CRACK IN LT FUSELAGE SKIN AT THE UPPER FORWARD CORNER OF PASSENGER ENTRY DOOR 1L JAMB. REPAIRED PER EA 98-212124 SECTION I. SECTION II REQUIRES REPETITIVE INSPECTIONS EVERY 3,000 CYCLES. SECTION III PERMANENT REPA IR TO BE ACCOMPLISHED ON OR BEFORE 24 MONTHS AFTER SECTION I. 2 L 7 2 4F RT A6WE 2008040300123 20080403 00123 NM 2008 4 3 2008UALA01738 1 20080327 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 986 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 FLOORBEAM UPPER SURFACE CORRODED AT BS 986 FROM RBL12 TO LBL46 AROUND FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED: REPL ACED BS 986.5 FLOORBEAM UPPER CAP FROM LBL 51 TO RBL 51 WITH SPLICE AT BL 0. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040300128 20080403 00128 SO 2008 4 3 CHQA200800065 1 20080328 A 3610 40303925SD O-RING EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BLEED AIR SYS BLOWN A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 267SK 145268 CAE311659 FLIGHT 5984 -JAX TO CLE - DURING CLIMB, THE FLIGHT CREW RECEIVED A BLEED 1 LEAK MESSAGE AND RETURNED TO JAX AND LANDED W ITHOUT INCIDENT. MAINTENANCE FOUND SEVERAL PANELS IN THE CARGO COMPARTMENT THAT WERE ABNORMALLY WARM, AND THE SOURCE WA S FOUND TO BE THE O-RING AT JOINT 19 WHICH HAD BLOWN OUT BEHIND THOSE PANELS. MAINTENANCE THEN REPLACED THE O-RING AND RECONNECTED THE BLEED DUCTS AND THE BLEED SYSTEM, OPS AND LEAK CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008040300137 20080403 00137 SO 2008 4 3 SWIA200819399 1 20080329 A 3397 TERMINAL EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DEFECTIVE A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 295SW 120322 LEFT OVERWING EMERGENCY LIGHT IS INOP. REPLACED TERMINALS ON EMERGENCY LIGHT ASSEMBLY. 2 L 7 2 4T RT A31SO 2008040300147 20080403 00147 NM 2008 4 3 HALA0800444 1 20080327 A 5610 5912290508 WINDSHIELD BOEING 717 717200 1383700 NM COCKPIT CRACKED A HALA K NONE O OTHER CR CRUISE 1 WP 13 484HA 55129 ATB - F/O WINDSHIELD HAS A ONE INCH CRACK LOCATED UPPER RIGHT CORNER. REMOVED F/O'S WINDSHIELD PER AMM56-11-02. INSTAL LED F/O WINDSHIELD PER AMM56-11-02 FINISHED STEP 4 E(17), FINISHED M/M56-11-02 COND AND OPS CK GOOD. 2 L 7 2 4F TR A6WE 2008040300195 20080403 00195 WP 2008 4 3 08FDEA01213 1 20080331 A 5753 ARC300741 SKIN PANEL DOUG MD10 MD1010F 3022112 WP T/E FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LEFT INBD FLAP LOWER SURFACE FWD PANEL 2ND FROM THE OUTBD END HAS 1 DENT. REMOVED LEFT FLAP LOWER SURFACE PANEL TO FOM IN REF TO DC/MD-10 SRM 51-31-01; VOL II. REPAIRED GOUGED DENT IN REF TO DC/MD-10 57-00-01; FIG 1 A; SHEET 2. INSTALLED PANEL IN REF TO DC/MD-10 SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 2008040300202 20080403 00202 EU 2008 4 3 08FDEA01220 1 20080401 A 5753 PAINT AIRBUS 310 A310222 3930315 EU FLAP DOUBLER MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 448FE 260 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING OUTBOARD FLAP LOWER MAIN SKIN BETWEEN RIBS 3 AND 4 MEASURES 10.4" BY 9.9". REPAIR NOT IAW SRM REQUIREMENTS DUE TO REPAIR DOUBLER MISSING FILLET SEAL AND PAINT. REPAIRED PROTECTIVE COAT ING AND RESEALED EDGES IAW A310-200 SRM 57-53-12 FIG 210. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008040300203 20080403 00203 EU 2008 4 3 08FDEA01221 1 20080401 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU CABIN MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 448FE 260 PREVIOUS REPAIR LOCATED ON MAIN CABIN SEAT TRACK NR 3 LT Y953 BETWEEN FRAMES 61 TO 62 HAS 2. REPAIR SPLICES MEASURING 7 .1" LONG BY 3" TALL AND 1. REPAIR SECTION 73" LONG FROM FRAME 55/58 TO BETWEEN FRAMES 61 AND 62 ALSO THE INBOARD AND OU TBOARD PRODUCTION SPLICES BETWEEN FRAMES 55/58 TO 59 ARE PREVIOUSLY MISLOCATED BY A .200" GAP BETWEEN SPLICES AND THE TO P FLANGES OF THE SEAT TRACK. REPAIR NOT IAW WITH SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT SEAT TRACK REPAIR SECTION IAW A310-200 SRM 53-10-16 FIG 208 SHEET 1. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER A ND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008040400005 20080404 00005 SW 2008 4 4 GVNA119127 1 20080301 A 5210 LATCH BOLKMS 117 BK117C2 5626002 SW TMECA ARRIEL ARRIEL1E 60034 NE PAX DOOR LOOSE B GVNA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 09 456TK 214 9130 DURING CRUISE FLIGHT AT 120 KTS, THE LT SLIDING CABIN DOOR CAME OPEN, SLID ALL THE WAY TO THE STOP AT A HIGH RATE OF SPE ED AND POPPED OUT OF THE CENTER GUIDE RAIL. THE MECHANICS FOUND A BOLT VERY LOOSE (3 OR 4 TURNS LOOSE) IN THE LATCHING MECHANISM FRICTION SYS, WHICH ALLOWED THE DOOR HANDLE TO VIBRATE OPEN. THE CENTER GUIDE ARM ABOVE WAS BENT, THE CENTER GUIDE RAIL P/N B520M0037801 WAS BENT OPEN WHERE THE GUIDE POPPED OUT AND THE BACKSTOP P/N B520M4025102 WAS CRACKED. TH E DAMAGED PARTS WERE REPLACED, THE LOOSE BOLT WAS REMOVED, CLEANED AND REINSTALLED TO PROPER TORQUE WITH THREAD LOCKING FLUID. NO FURTHER PROBLEMS HAVE OCCURED. 1 G 7 2 3U 3 U H13EU E19EU 2008040400020 20080404 00020 CE 2008 4 4 ZESA032008004 1 20080320 A 5270 WARNING LIGHT CESSNA 500 550 2076604 CE PWA 530 PW530A NE PAX DOOR FALSE ACTIVATION E ZESA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 03 824CB 5500824 AFTER TAKE OFF, PILOT NOTICE CABIN DOOR WARNING LIGHT, PILOT RETURNED TO AIRPORT, LANDED UNEVENTFULLY. PILOT RESET DOOR HANDLE AND LIGHT WENT OUT, PILOT VERIFIED THAT ALL LOCK FLAGS WERE VISIBLE WITH THE DOOR HANDLE SECURE PIN ENGAGED. NO F URTHER OCCURRENCE OF THE CABIN DOOR LIGHT. 1 L 7 2 4F 4 F A22CE E00053EN 2008040400066 20080404 00066 NM 2008 4 4 2008UALA01815 1 20080401 A 2121 FAN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE AVIONICS BAY ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 850UA 1653 RTFL DUE TO SMELL OF SMOKE IN THE A/C. FOUND AVIONICS BLOWER 20HQ FAN BEARING SEIZED. REPLACED AVIONICS BLOWER FAN, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040400085 20080404 00085 NM 2008 4 4 2008UALA01836 1 20080401 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY EXIT LIGHT INOP, AT DOOR 2L AFT SILL LIGHT. AFTER TROUBLESHOOTING, FOUND DOOR 2L SILL LIGHT FAILED. REPLACED LAMP. OP CHECKED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040400117 20080404 00117 EU 2008 4 4 08FDEA01252 1 20080402 A 5313 A53971006208 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CORROSION AT STRINGER 56LT, P54.3-57.2. REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CRACK FREE AND FLAP PEEN ING IAW RAS/EFW/9000014/2008 ISS A, APPROVED BY EA 6-5316-114880. 2 L 7 2 4F RT A35EU 2008040400133 20080404 00133 EU 2008 4 4 08FDEA01268 1 20080317 A 5753 A5797020023000 FLAP TRACK AIRBUS 310 A310203 3930313 EU TE FLAPS WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT FLAP VANE NR5 TRACK HAS WORN AREAS MARKED. REPAIRED NR 5 L/W FLAP VANE TRACK IAW AIRBUS CMM 57-52-15. 2 L 7 2 4F RT A35EU 2008040400135 20080404 00135 EU 2008 4 4 08FDEA01270 1 20080317 A 5753 A5797020022600 FLAP TRACK AIRBUS 310 A310203 3930313 EU NR 1 FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LT FLAP VANE NR 1 TRACK HAS WORN AREAS MARKED. REPAIRED NR 1 FLAP VANE TRACK IAW AIRBUS CMM 57-52-15. 2 L 7 2 4F RT A35EU 2008040400138 20080404 00138 NM 2008 4 4 DL76G080439 1 20080327 A 5330 084405780101 SKIN BOEING 767 7673P6 1385105 NM BS 1197 S36R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 155DL 25269 AFT CARGO STA 1197+12 TO 1197+26 AT STR 36R SKIN LAP INNER SKIN FOUND CORRODED AND SUBJECT SKIN REPAIR PER 53-00-01 FIGU RE 201 REPAIR 12 TOTAL WEIGHT ADDED 14LBS. WORKED ON NR CARD AVM 510907. 2 L 7 2 4F RT A1NM 2008040400153 20080404 00153 NM 2008 4 4 DLM90080457 1 20080330 A 5330 SKIN DOUG MD90 MD9030 3023690 NM BS 792-876 L29R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 96828 53392 FOUND FUSELAGE SKIN CORRODED 792 TO 876 LONG 29R. REPAIRED FUSELAGE SKIN, IAW MD80 SRM 53-04 FIG 53. 2 L 7 2 4F RT A6WE 2008040400180 20080404 00180 NM 2008 4 4 DLM88080487 1 20080402 A 5320 SUPPORT DOUG MD88 MD88 3023688 NM BS 1308 L28R CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV A CRACKED WAS FOUND ON FIBERGLASS SUPPORT AT STA Y=1308 LONG 28 RT. SUPPORT WAS REPLACED IAW ER/A 413029-14M A. 2 L 7 2 4F RT A6WE 2008040400181 20080404 00181 NM 2008 4 4 DLM88080488 1 20080402 A 5320 SUPPORT DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, A CRACK WAS FOUND ON SLANT PANEL SUPPORT WITHIN C2 STA Y=579 RT SIDE. SUPPORT WAS REPLACED IAW ER/A 413029- 14MA REV ORIG. 2 L 7 2 4F RT A6WE 2008040400183 20080404 00183 NM 2008 4 4 DLM88080490 1 20080402 A 5320 STIFFENER DOUG MD88 MD88 3023688 NM BULKHEAD CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, A BROKEN P-DOME STIFFENER WAS FOUND AT 12:00 POSITION. STIFFENER WAS REPLACED IAW DOUGLAS DWG 9915562. 2 L 7 2 4F RT A6WE 2008041100086 20080411 00086 NE 2008 4 11 070192 2 20080404 A 7200 JT8D219 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RIGHT MALFUNCTIONED A WX0A E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 19 875GA 53468 728014 FLT 400, FLIGHT CREW REPORT RIGHT ENGINE BANG AND A DECREASE IN EPR INDICATIONS, RETURNING TO NORMAL. SUBSEQUENTLY 2 MO RE BANGS FROM THE RIGHT ENGINE AND THE CREW ELECTED TO SHUTDOWN THE RIGHT ENGINE AND RETURN. MAINTENANCE PERSONNEL REMO VED AND REPLACED THE RIGHT ENGINE. RETURN TO SERVICE OPERATIONAL CHECK WAS PERFORMED AND ALL SYSTEM PARAMETERS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E9NE 2008041100087 20080411 00087 2008 4 11 ARWA20080402 4 20080407 A 3417 HG280D80 ADC DOUG DC10 DC1030F 3023504 WP NR 1 MALFUNCTIONED A ARWA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 478CT 47819 NR 1 AUTO PILOT PORPOSES IN CRUISE; TRANSFERRED TO DMI NR 21586 AS PER MEL NR 22-1-2(A) CAT "C". REMOVED AND REPLACED N R 1 AIR DATA COMPUTER IN ACCORDANCE WITH M/M 34-16-01. CHECK GOOD IN ACCORDANCE WITH MM 34-16-00 AND MM 22-10-00 CLEARE D DMI NR 21586; PLACARD REMOVED. 2 L 7 3 4F RT A22WE 2008041100133 20080411 00133 EA 2008 4 11 MASA200800296 1 20080407 A 3397 ELECTRICAL BOX CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 511MJ 10104 ASH FLT 7278 ORD-CLT. EMERGENCY LIGHTS COME ON INTERMITTENTLY IN CABIN. REMOVED AND REPLACED PCB5 IN JUNCT BOX 11. 2 L 7 2 4F RT A21EA 2008041100134 20080411 00134 NM 2008 4 11 CALA0800313 1 20080404 A 2121 731376A COOLING FAN BOEING 757 757224 1384958 NM E&E COMPT FAILED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 18112 27302 AFTER TAKEOFF A STRONG SMOKE SMELL APPEARED, SMELL DISSIPATED IN 5 MIN JUST PRIOR TO COAST, THE SMELL RETURNED STRONGER. DIVERTED TO SNN RECEIVED EICAS MSG - EQUIPMENT COOLING FAN ON DESCENT TO SNN. COMPLIED WITH SMOKE IN FLIGHT DECK / CA BIN MAINTENANCE CHECK IAW AMM 05-51-58, FOUND PRIMARY FWD EQUIPMENT COOLING SUPPLY FAN NR 1 FAILED, CIRCUIT BREAKER POPP ED. REMOVED AND REPLACED PRIMARY EQUIPMENT COOLING FAN NR 1 IAW AMM 21-58-06. RESET OF SYSTEM COMPLIED WITH IAW AMM 20 -60-01. 2 L 7 2 4F RT A2NM 2008041100136 20080411 00136 NM 2008 4 11 CALA0800308 1 20080311 A 5320 BAC150518761 INTERCOSTAL BOEING 737 737524 1384721 NM BS 348 S13L MISSING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11641 28902 INTERCOSTAL ATTACH POINT TO INBOARD FLANGE OF FRAME STA 348 AND STR 13 LT, MISSING FASTENERS 2 (MARKED). INSTALLED 2 FA STENERS AT INTERCOSTAL ATTACH POINT TO INBOARD FLANGE OF FRAME STA 348 AND STR 13 LT PER PACE EA 641-53-001CAL AND EC/RA 5310-04742. 2 L 7 2 4F RT A16WE 2008041100138 20080411 00138 NM 2008 4 11 CALA0800310 1 20080311 A 5311 FRAME BOEING 737 737524 1384721 NM BS 348 S12L DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11641 28902 TWO RIVET HEADS SHEARED OFF ON AFT SIDE OF FRAME STA 348 AND THE AREA OF STR 12 LT (MARKED). REPLACED 2 RIVETS THAT WER E SHEARED OFF ON AFT SIDE OF FRAME AT STA 348 AND STR 12 LT PER PACE EA 641-53-001 CAL AND EC/RA 5310-04742. 2 L 7 2 4F RT A16WE 2008042300035 20080423 00035 EA 2008 4 23 MASA200800306 1 20080409 A 5210 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 77302 7302 PAX DOOR UPPER AFT FRAME CRACKED. REPAIRED FRAME. 2 L 7 2 4F RT A21EA 2008042300037 20080423 00037 EA 2008 4 23 MASA200800307 1 20080409 A 5210 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED G MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 77302 7302 PAX DOOR FWD UPPER FRAME CRACKED. REPAIRED FRAME. 2 L 7 2 4F RT A21EA 2008042300041 20080423 00041 NM 2008 4 23 2008UALA02215 1 20080416 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1600 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 AFT PIT STA 1600 RT SIDE STR 24R HAS DENTED FRAME. REMOVED DAMAGE FABRICATED AND INSTALLED RPR PER SRM 53-00-07 RPR 5 TA BLE II ZONE 1. RPR IS A CAT B RPR AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS STARTING AT 50,000 TOTAL FLIGHT C YCLES AND 12,000FC THERE AFTER. CURRENT FC= 14767 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300043 20080423 00043 NM 2008 4 23 2008UALA02217 1 20080416 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1580 S22R DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 AFT PIT STA 1580 STR 22R HAS DENTED FRAME. REMOVED DAMAGE FABRICATED AND INSTALLED RPR PER SRM 53-00-07 RPR 5 TABLE II ZONE 1. RPR IS A CAT B RPR AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTION S STARTING AT 50,000 TOTAL FLIGHT CYCLES AND 12,000FC THERE AFTE R. CURRENT FC= 14767. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300044 20080423 00044 EU 2008 4 23 USAA920080901 1 20080416 A 5320 D5311282600200 RAIL AIRBUS A321 A321211 3930370 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 188US 1724 PIT - MAJOR REPAIR - CORROSION ON RAIL AT C14 - 16, Y503.2. REPLACED RAIL IAW SRM 51-72-00. 2 L 7 2 4F RT A28NM 2008042300046 20080423 00046 EU 2008 4 23 USAA920080903 1 20080417 A 5320 26543130023 SHEAR PLATE AIRBUS A321 A321211 3930370 EU ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 188US 1724 PIT - MAJOR REPAIR- CORROSION ON RT SHEAR PLATE AT FR70, STR 23R. REPLACED RT SHEAR PLATE IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008042300047 20080423 00047 WP 2008 4 23 UPS08852026 1 20080407 A 5347 3657501U1 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 BOTH UPPER SEAT TRACKS WORN AT PILOTS SEAT. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-1-20D, 51-3- 1, 51-1-24. 2 L 7 4 4F RT 4A25 2008042300049 20080423 00049 EA 2008 4 23 MASA200800275 1 20080330 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 654BR 7454 ASH FLT 1034 HNL - LEFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2008042300050 20080423 00050 WP 2008 4 23 UPS08852027 1 20080306 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 NR 1 ALT STRINGER 65 TO FRONT SPAR FITTING CRACKED. REMOVED AND REPLACED STRINGER 65 TO FRONT SPAR F ITTING IAW DC 8 SRM 51-03-02, 51-01-20D, 51-01-12, AND 51-1-8. 2 L 7 4 4F RT 4A25 2008042300051 20080423 00051 NM 2008 4 23 UPS08M52030 1 20080212 A 5730 SKIN DOUG MD11 MD11 3023602 NM LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C LT WING FIXED L/E LOWER SURFACE ABOVE NR 1 ENGINE PYLON O/B SIDE AT APPROXIMATELY STA XORS 299 FOUND S CRATCH MARKS AS MARKED. DAMAGE SKIN REMOVED PER SRM 51-31-01V.2R.40. NEW SKIN FAB PER BOEING DRAWING ARB2363 USING MAT L 7075T6-0.090". NEW SKIN HOLES PICKED UP PER SRM 51-31 -01V.2R.40. NEW SKIN PROTECTED PER SRM 51-21-01V.2R.40. NEW S KIN INSTALLED PER SRM 51-31-01V.2R.40. LEAK CHECK CARRIED OUT IAW AMM 36-00-04 REV 53, "NO LEAK". 2 L 7 3 4F RT A22WE 2008042300053 20080423 00053 EU 2008 4 23 UPS08151980 1 20080408 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU COCKPIT LOW A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 157UP 0846 INSPECTION TYPE:N/A EMERGENCY LIGHTS ARE DIM. CYCLED C/B U82 AS SVC CONTROL DMP 33-51-08, SYS CHECKS NORMAL IAW AMM 33- 51-00-05. 2 L 7 2 4F RT A35EU 2008042300056 20080423 00056 NM 2008 4 23 2008UALA02221 1 20080416 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1520 S26L CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 AFT PIT STA 1520 AT STR 26L, FRAME CHAFED. REMOVED DAMAGE FABRICATED AND INSTALLED RPR PER SRM 53-00-07 RPR 5 TABLE II ZONE 1. RPR IS A CAT B RPR AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTION S STARTING AT 50,000 TOTAL FLIGHT CYCLES AND 12,000 FC THERE AFTE R. CURRENT FC= 14767. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300058 20080423 00058 NM 2008 4 23 2008UALA02224 1 20080417 A 3350 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS CUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 539UA 25223 EEL LIGHT STRIP INOP IN FRONT OF MID LAV. SPLICED EEL STRIP, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300062 20080423 00062 NM 2008 4 23 2008UALA02227 1 20080417 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EMERGENCY EXIT LIGHT INOP, AT DOOR 1 RIGHT AFT SILL. FOUND LAMP BURNED OUT. REPLACED LAMP. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300069 20080423 00069 NM 2008 4 23 2008UALA02234 1 20080416 A 5240 HOUSING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR HANDLE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 R-1 DOOR HANDLE BOX CRACKED AT CAM MOUNT HOLES. REPLACED HANDLE BOX. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300071 20080423 00071 NM 2008 4 23 2008UALA02236 1 20080417 A 5246 PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 ACFT HAS DENT AFT OF FWD LAV SERVICE PNL. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042300075 20080423 00075 NM 2008 4 23 2008UALA02239 1 20080416 A 5754 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 9 SLAT PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 RT WING FIXED L/E UNDER NR 9 OTBD SLAT HAS PUNCTURE AND DENT. REPAIRED FIXED LEADING EDGE UNDER NR 9 SLAT PER SRM 57-41- 01 TABLE 3 REPAIR 1 PAGE 207 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300076 20080423 00076 NM 2008 4 23 2008UALA02240 1 20080416 A 3510 OXYGEN BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 CREW O2 PRESSURE LOW AT 1500 PSI. SERVICED O2 BOTTLE. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300079 20080423 00079 EU 2008 4 23 F3LA200800183 1 20080419 A 2520 WA25BYU3YS01054 SEAT AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AT MOUNTING HOLES AFT LEFT FLIGHT ATTENDANT SEAT. MAINTENANCE REMOVED A ND REPLACED AFT LEFT FLIGHT ATTENDANT SEAT IN ACCORDANCE WITH THE REQUIRMENTS OF AMM 25-22-41-400-011. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042300083 20080423 00083 NM 2008 4 23 2008UALA02241 1 20080415 A 2611 824101 FIRE LOOP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 NACELLE FAULTY A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 180UA 25224 'ENG 4 FIRE LP B' EICAS STATUS MSG DISPLAYED. ENG 4 FIRE LOOP B FIRE OR FAULT OUTPUT. FOUND TS683 PCN 585-1677 DAMAGED REPLACED THE SAME IAW MM 26-11-02. OPS CHK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300090 20080423 00090 NM 2008 4 23 USAA920080893 1 20080414 A 5330 SKIN BOEING 737 7373B7 1384580 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 531AU 24478 CLT - MAJOR REPAIR-C3- ONE INCH CRACK ON FUSELAGE SKIN AT BS 737, STR 24R. INSTALLED REPAIR IAW SRM 53-00-01 REPAIR 31 . 2 L 7 2 4F RT A16WE 2008042300096 20080423 00096 WP 2008 4 23 UPS08852000 1 20080410 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:N/A EMERGENCY LIGHTING SYSTEM INOP. REPLACED EMERGENCY LIGHT BATTERY PACK AND OPS CHECKED AS PER DC8 MM 33-50-01-2. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2008042300107 20080423 00107 NM 2008 4 23 UPS08M51992 1 20080319 A 5730 ARB3954504 SPLICE DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 256UP 48405 INSPECTION TYPE:2C RIGHT WING L/E SPLICE STRAP XFS 791 CRACKED. REMOVED SPLICE STRAP, FABRICATED REPLACEMENT SPLICE STR AP AND INSTALLED IAW DWG ARB3954 AND MD-11 SRM 51-33-01. 2 L 7 3 4F RT A22WE 2008042300121 20080423 00121 NM 2008 4 23 USAA920080822 1 20080315 A 5240 6545871132 GATE BOEING 737 7374B7 1384702 NM R2 DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT- MAJOR REPAIR - Q6 CHECK - 4 INCH AREA OF CORROSION ON THE R2 DOOR LOWER GATE. REPLACED LOWER GATE IAW SRM 51-10-02 . 2 L 7 2 4F RT A16WE 2008042300130 20080423 00130 NM 2008 4 23 USAA920080890 1 20080410 A 5320 69366564 ANGLE BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21- NR 6112731, .75 INCH CRACK ON SUPPORT ANGLE (CHORD) AT BS 927 - 947, WL207, BL0. REPLACED CHO RD ANGLE IAW SRM 51-40-02-0G FIG 8 AND FIG 12. 2 L 7 2 4F RT A16WE 2008042300131 20080423 00131 NM 2008 4 23 USAA920080891 1 20080410 A 5320 65479574 WEB BOEING 737 73733A 1384673 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR-C21-NR 6112723, CORROSION ON WEB AT BS 767 - 787, STR 25R - STR 26R. REPLACED WEB IAW SRM 51-40-02-0 G PART D, FIG 8 AND FIG 12. 2 L 7 2 4F RT A16WE 2008042300162 20080423 00162 EU 2008 4 23 F3LA200800191 1 20080416 A 5321 222EF FLOORBOARD AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE CABIN PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED FORWARD GALLEY FLOORBOARD 222EF HAS TWO PUNCTURES IN TOP RIGHT EDGE OF FLOORBOARD. MAINTENANCE REPAIRED PUNCTURES IN GALLEY FLOORBOARD 222EF IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-12-00 PAGE 205 AND PAGE 206. MAINTENANCE SANDED RESIN SMOOTH IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-12-00 PAGE 205 AND PAGE 20 6. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042300179 20080423 00179 NM 2008 4 23 UPS08M52046 1 20080417 A 2800 4059024901 CONTROL PANEL DOUG MD11 MD11F 3023600 NM FUEL SYSTEM INOPERATIVE A IPXA E ENGINE SHUTDOWN A FLAME/FIRE CL CLIMB 1 SO 01 251UP 48744 ON CLIMB-OUT (5000') RECEIVED LVL 1 TANK2 PUMPS OFF ALERT. FSC WAS IN MANUAL. TURNED TANK 2 PUMPS BACK TO ON LVL 1 ALE RT WENT OUT. APPROACHED ING TOC APPROX 08:50Z. RECEIVED THE SAME ALERT BUT WITH A CORRESPONDING NUMBER 2 ENGINE FLAME OUT. TRIED TO TURN THE NR 2 PUMPS ON WITHOUT SUCCESS. TURNED NR 2 TRANSFER PUMP AND CROSSFEET ON. ENG OPERATED NORMAL . REPLACED FUEL SYSTEM CONTROL PANEL. CHKD WIRING PER WDM 28-22-02, PG 503 S SH1 FOR GRD AT PIN 1E OF CONNECTOR R5. A LSO C/O SATIS ENG RUN OF NR 2 ENG USING NR 2 PUMPS. OPS OK. 2 L 7 3 4F RT A22WE 2008042300180 20080423 00180 NM 2008 4 23 UPS08M52047 1 20080324 A 5754 ARB2850506 FITTING DOUG MD11 MD11F 3023600 NM RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:4C RIGHT WING NR 16 SLAT TRACK FITTING IB CRACKED. REMOVED AND REPLACED NR 16 SLAT TRACK IB RIB FITTING IAW MD-11 SRM 51-31-01 AND 51-33-01. 2 L 7 3 4F RT A22WE 2008042300199 20080423 00199 EA 2008 4 23 MASA200800309 1 20080411 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27172 7172 ASH FLT 7116 ORD-CID. PASSENGER DOOR OUTER HANDLE WILL NOT STOW FROM THE INSIDE. ADJUSTED OUTER DOOR HANDLE. 2 L 7 2 4F RT A21EA 2008042300208 20080423 00208 EA 2008 4 23 A6WA200840240 1 20080319 A 5340 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 718 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 439AW 7753 CRACK FOUND ON HYDRAULIC MANIFOLD SUPPORT BRACKET FS 718. REPAIRED IAW REO 601R-53-02-031 REV A. (M) 2 L 7 2 4F RT A21EA 2008042300213 20080423 00213 NM 2008 4 23 2008UALA02248 1 20080418 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY LIGHT ROW 39 ABC INOP. RELAMPED EMERGENCY LIGHT. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300216 20080423 00216 NM 2008 4 23 2008UALA02250 1 20080418 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY LIGHT ROW 4F AFT INOP. RELAMPED EMERGENCY LIGHT. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300222 20080423 00222 NM 2008 4 23 UPS08552018 1 20080412 A 2510 SHOULDER BELT BOEING 757 75724APF 1384969 NM COCKPIT TANGLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 404UP 23726 INSPECTION TYPE:N/A SHOULDER HARNESS INERTIA REEL AT CAPTAIN'S SEAT FAILED TO RETRACT. UNTANGLED SHOULDER STRAP GOING I NTO INERTIA REEL. OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2008042300227 20080423 00227 SO 2008 4 23 SIMA200810904 1 20080414 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO CARGO BAY MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 21 676AE 14500807 ON FLIGHT 3528, CREW REPORTED EICAS BAGG SMOKE WARNING. PRESSED BAGGAGE EXTINGUISHER BUTTON AND COMPLETED BAGG SMOKE A OM-1 PROCEDURE. AFTER 2 MORE BAGG SMOKE INDICATIONS MESSAGE EXTINGUISHED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BAGGAGE SMOKE DETECTOR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008042300228 20080423 00228 NM 2008 4 23 SWAA081932 1 20080412 A 3350 311500 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 200WN 32482 L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008042300250 20080423 00250 NM 2008 4 23 SWAA081944 1 20080413 A 5315 6545834 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 17. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2008042300257 20080423 00257 NM 2008 4 23 F3LA200800192 1 20080420 A 5320 D5347112420100 PLATE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 45 1841 DURING C4 S1 C CHECK INSPECTION NOTED MAIN DECK WEB AT FRAME 70 RBL 52 WAS CORRODED. MAINTENANCE REMOVED AND REPLACED M AIN DECK WEB AT FRAME 70 RBL 52 IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT W AS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042300292 20080423 00292 NM 2008 4 23 2008UALA02150 1 20080414 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 CEILING EMERGENCY LIGHT INOP AT STAIRWAY OVERHEAD. REPLACED LAMP OP CHKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040700030 20080407 00030 NM 2008 4 7 DLM88080508 1 20080402 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 1309 L6-7L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV A CRACK WAS FOUND ON FUSELAGE SKIN AT STA Y=1309 BETWEEN LONGERON 6 AND 7 LT. SKIN WAS REPAIRED IAW SRM 51-3 0-2 AND 51-20. 2 L 7 2 4F RT A6WE 2008040700042 20080407 00042 NM 2008 4 7 DL764080520 1 20080402 A 5610 561701281 WINDSHIELD BOEING 767 767432ER 1385134 NM COCKPIT ARCED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 833MH 29706 ELECTRICAL ARCING IN RT FWD WINDSHIELD. REMOVED AND REPLACED RT FORWARD WINDSHIELD PER MM. 2 L 7 2 4F RT A1NM 2008040700043 20080407 00043 NM 2008 4 7 DLM88080521 1 20080403 A 5320 MEMBRANE DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV A CRACKED WAS FOUND ON MEMBRANE AT STA Y=218 AND X=10. MEMBRANE WAS REPAIRED IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F RT A6WE 2008040800020 20080408 00020 NE 2008 4 8 HNAA0800108 2 20080323 A 7200 PW123 ENGINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 1 MAKING METAL A HNAA O OTHER Y ENGINE STOPPAGE CR CRUISE 1 EA 07 333EN 19526 14606 221 123246 NR 1 ENGINE FAILED INFLIGHT. CREW WAS FLYING ALONG AT 9000 FT ABOUT 5 MILES WEST OF CLT WHEN NR 1 ENGINE SHUT ITSELF DO WN. THE CREW FEATHERED THE ENGINE AND DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE PULLED THE FDR A ND WILL SHIP TO ROA. MAINTENANCE INSPECTED THE ENGINE, PULLED THE STARTER AND SPUN THE ENGINE BY HAND AND THE ENGINE WA S MAKING NOISE. MAINTENANCE THEN PULLED NL PROBE AND FOUND THE NL PROBE PACKED WITH METAL. MORE INFORMATION TO FOLLOW. 2 H 7 2 4T 4 T RT A13NM E20NE 2008040800021 20080408 00021 NE 2008 4 8 HNAA0800109 3 20080323 A 6110 14SF7 PROPELLER DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF7 NE NR 2 ENGINE OUT OF BALANCE A HNAA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 07 942HA 18250 2394 163 940408 AIRCRAFT WAS EN ROUTE FROM LGA TO ORF, THE CAPTAIN NOTIFIED DISPATCH NORTH OF SBY THAT THE AIRCRAFT WAS ENCOUNTERING A M ODERATE TO HEAVY PROPELLER VIBRATION AT ALL RPM SETTINGS. THE AIRCRAFT WAS DIVERTED TO SBY. IT WAS DETERMINED THAT NR 2 PROPELLER WAS CAUSING THE VIBRATION. THE PROPELLER WAS REMOVED, STATIC BALANCED AND RE-INSTALLED, GROUND RUN WAS SATI SFACTORY. 2 H 7 2 4T RT A13NM 6 C P7NE 2008040800023 20080408 00023 NM 2008 4 8 PIDA08015 1 20080322 A 3350 6104789 BATTERY PACK BOEING 737 737291 138448W NM CABIN DISCHARGED A PIDA K NONE O OTHER UK UNKNOWN 1 SO 05 583CC 21069 EMERGENCY EXIT LIGHT EXTERIOR OF R-2 DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK AND OPS TEST NOR MAL PER AMM 33-50-00. 2 L 7 2 4F A16WE 2008040800024 20080408 00024 NM 2008 4 8 PIDA08014 1 20080322 A 3350 873100272 LIGHT BOEING 737 737291 138448W NM CABIN INOPERATIVE A PIDA K NONE O OTHER UK UNKNOWN 1 SO 05 583CC 21069 L1 DOOR INTERVALVE EMERGENCY EXIT LIGHT ASSY INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AND BATTERY. OPS TEST GOOD PER INTERVALVE OPS. TEST PROCEDURES. BATTERY P/N 97-2-1050, BATCH 19. 2 L 7 2 4F A16WE 2008040800050 20080408 00050 SO 2008 4 8 FDKA200803128 1 20080322 A 5411 RIB EMB 145 EMB145LR 3260212 SO LT COWLING CHAFED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 THE PREVIOUS REPAIR ON THE L/B UPPER RIB ON THE LT LOWER COWLING IS CHAFED. THE RIB HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008040800056 20080408 00056 NM 2008 4 8 HNAA0800110 1 20080326 A 3350 1013075 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 933HA 133 THE 3RD EMERGENCY FLOOR PATH LIGHT INOP. REMOVED AND REPLACED LAMP, OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2008040800059 20080408 00059 SO 2008 4 8 C2XA08CL030 1 20080316 A 2611 FAU751A4 PANEL EMB 145 EMB145LR 3260212 SO SMOKE WARNING INTERMITTENT A C2XA K NONE N FALSE WARNING CL CLIMB 1 SW 27 22971 145149 CLE FLIGHT 2905 - THE CREW REPORTED A FALSE LAV SMOKE WARNING DURING CLIMBOUT. MAINTENANCE INSPECTED AND REPLACED THE L AV SMOKE TEST PANEL. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008040800066 20080408 00066 NM 2008 4 8 HNAA0800116 1 20080328 A 3350 1013073 MODULE DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 807EX 40823 40823 292 DURING OVERNIGHT MAINTENANCE CHECKS, ONE OF THE ROW 4DF EMERGENCY FLOOR PATH LIGHTS WAS FOUND TO BE INOPERATIVE. THE MO DULE WAS CHANGED AND OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2008040800067 20080408 00067 2008 4 8 HNAA0800117 4 20080327 A 3425 7003360941 AHRS DHAV DHC8 DHC8102 2809003 NM NR 2 MALFUNCTIONED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 940HA 42166 24990 156 DURING FLIGHT, IT WAS NOTED THAT THE NR 2 AHRS WAS 10 DEGREES OFF FROM WHAT THE STANDBY HEADING SYSTEM AND THE WET COMPA SS WERE READING. AIRCRAFT WAS RETURNED TO DEPARTURE POINT. MAINTENANCE COULD NOT DUPLICATE PROBLEM ON GROUND. NR 2 AH RS COMPUTER WAS RE-RACKED AND OPS CHECKS WERE GOOD. AIRCRAFT WAS THEN RETURNED TO SERVICE WITH NO FURTHER DIFFICULTIES NOTED. 2 H 7 2 4T RT A13NM 2008040800070 20080408 00070 NM 2008 4 8 LYNX00011 1 20080323 A 3231 483023 SEQUENCE VALVE BOMBDR DHC8 DHC8402 1390042 NM MLG DOOR FAULTY A 3LYA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 21 501LX 4165 DEN - SHORTLY AFTER TAKEOFF LEFT MAIN GEAR DOOR ADVISORY LIGHT REMAINED ILLUMINATED. EXTENDED GEAR USING ALTERNATE LAND ING GEAR EXTENSION SYSTEM. MX REMOVED AND REPLACED LEFT AND RIGHT MLG DOOR SOLENOID SEQUENCE VALVE. NO DEFECTS NOTED P ER AMM 32-31-41-04. 2 H 7 2 4T RT A13NM 2008040800071 20080408 00071 NM 2008 4 8 PIDA08016 1 20080320 A 3350 873100171 LIGHT BOEING 737 737291 138448W NM CABIN INOPERATIVE A PIDA O OTHER O OTHER UK UNKNOWN 1 SO 05 583CC 21069 MID-CABIN BELOW SEAT EMERGENCY LIGHT INOP. DEFERRED PER MEL 33-19-01, CONTROL NUMBER 030002. REMOVED AND REPLACED MID- CABIN RT AISLE SEAT EMERGENCY LIGHT PER SRM 51-30-02, OPS CHECKED GOOD PER INTERVALVE LIGHT SYSTEM TEST. THIS CLEARED T HE MEL. 2 L 7 2 4F A16WE 2008040800072 20080408 00072 NM 2008 4 8 ZZDA2008084 1 20080327 A 3350 D71701100 BATTERY PACK BOEING 737 73776N 13844CH NM CABIN FAILED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 261AT 32660 R1 DOOR EMERGENCY EXIT LIGHT FAILED EMERGENCY BATTERY PACK CAPACITY FUNCTIONAL CHECK. REMOVED AND REPLACED BATTERY PACK REPLACEMENT IAW AMM 33-51-06. 2 L 7 2 4F RT A16WE 2008042300307 20080423 00307 NM 2008 4 23 SWAA081950 1 20080413 A 5311 6546539 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT LEFT BS 616 INBOARD LOWER END. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008042300318 20080423 00318 NM 2008 4 23 SWAA081957 1 20080413 A 2560 6557463 FITTING BOEING 737 7373Q8 1384670 NM GIRT BAR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CRACKED. REMOVED AND REPLACED FITTI NG PER SRM. 2 L 7 2 4F RT A16WE 2008042300330 20080423 00330 NM 2008 4 23 SWAA081997 1 20080414 A 5523 BACB28AK04 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 3 TAB BUSHING PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300331 20080423 00331 NM 2008 4 23 SWAA081998 1 20080414 A 5523 BACB28AK04 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, RIGHT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 2 TAB BUSHING PER SWA EA . 2 L 7 2 4F RT A16WE 2008042300341 20080423 00341 NM 2008 4 23 SWAA081991 1 20080414 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 416WN 32453 DURING SCHEDULED 6Y CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 142. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042300342 20080423 00342 2008 4 23 SWAA081992 4 20080414 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042300343 20080423 00343 NM 2008 4 23 SWAA082011 1 20080414 A 5312 6545409 PRESSURE PANEL BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, RBL 39. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008042300351 20080423 00351 EA 2008 4 23 MASA200800316 1 20080412 A 3010 32144424 MODULATING VALVE CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYS MALFUNCTIONED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 154SF 8591 7154 ASH FLT 7181 ORD-LAN. RIGHT WING OVERHEAT WARNING AND A WING ANTI-ICE DUCT WARNING IN THE NORMAL POSITION. CREW DECLA RED EMERGENCY AND RETURNED TO THE FIELD. REMOVED AND REPLACED WING OVERHEAT SENSOR & 14TH STAGE MODULATING VALVE. 2 L 7 2 4F RT A21EA 2008042300354 20080423 00354 EA 2008 4 23 MASA200800319 1 20080414 A 5270 PROXIMITY SWITCH CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT DIRTY A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 504MJ 10066 ASH FLT 7219 ORD-ORF. RIGHT WING EMERGENCY EXIT CAUTION MESSAGE INTERMITTENT. MX CLEANED PROX SENSOR. 2 L 7 2 4F RT A21EA 2008042300355 20080423 00355 EA 2008 4 23 MASA200800321 1 20080415 A 5210 601R317731 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77278 7278 ASH 1949 LIH - HNL. PAX DOOR BOTTOM HINGE STEP BROKEN. MX REPLACED LOWER STEP. 2 L 7 2 4F RT A21EA 2008042300363 20080423 00363 NM 2008 4 23 SWAA082027 1 20080415 A 5310 6545874 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED BRDG CHECK, FOUND FWD SERVICE DOOR CUTOUT FWD FRAME LOWER CORNER CRACKED. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008042300371 20080423 00371 NM 2008 4 23 SWAA082025 1 20080415 A 5330 6545777 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AFT ENTRY DOOR FWD LOWER CORNER. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300372 20080423 00372 NM 2008 4 23 SWAA082026 1 20080415 A 5340 65C27314 STRINGER CLIP BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED HC1 CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300384 20080423 00384 NM 2008 4 23 SWAA082043 1 20080416 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300387 20080423 00387 2008 4 23 SWAA082037 4 20080416 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 R2 DOOR EMERGENCY EVAC SLIDE OUT OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042300388 20080423 00388 NM 2008 4 23 SWAA082038 1 20080416 A 5311 6545805 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 277, BETWEEN STR 14R AND STR 16R. REMOVED AND REPLAC ED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008042300391 20080423 00391 NM 2008 4 23 2008UALA02256 1 20080416 A 5320 SILL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 FWD CARGO DOOR SILL PLATE HAS A .625 LONG CRACK 3 INCHES FROM FWD EDGE. FWD CARGO THRESHOLD BULLNOSE REPAIRED. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042300393 20080423 00393 NM 2008 4 23 SWAA082040 1 20080416 A 5310 6546818 CREASE BEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 978 AND BS 992, STR 17L. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008042300404 20080423 00404 NM 2008 4 23 SWAA082049 1 20080417 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 27L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042400019 20080424 00019 NM 2008 4 24 2008UALA02158 1 20080414 A 2697 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE CONTROL DAMAGED A UALA O OTHER B A SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE NR NOT REPORTED 1 WP 29 87UA 26713 WHEN CHECKING FIRST OFFICERS WIPER MOTOR FOR OPERATION, FOUND STRONG ELECTRICAL ODOR AND SMOKE COMING FROM BACK OF FIRST OFFICER'S INSTRUMENT PANEL. EXTINGUISHED FLAMES WITH FIRE EXTINGUISHER BOTTLE. FOUND SHORTED WIRING IN HARNESS LEADIN G TO WIPER MOTOR- FOUND FO'S WIRE HARNESS BURNED BEHIND CENTER UPPER DISPLAY PANEL. REPLACED ALL WIRING IN AFFECTED HAR NESS AND REPLACED CB AS WELL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400066 20080424 00066 NM 2008 4 24 2008UALA02258 1 20080417 A 5754 SPAR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 SLAT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 NR 2 SLAT OUTBOARD WEDGE CORNER IS DELAMINATED. REPAIRED LWR SPAR BY BLENDING THE SHARP EDGES & INSTALLING A DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042400068 20080424 00068 NM 2008 4 24 2008UALA02260 1 20080415 A 3510 6350A33XA OXYGEN SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. OXYGEN BOTTLE SERVICED TO 1850. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042400079 20080424 00079 NM 2008 4 24 2008UALA02271 1 20080417 A 5240 DOOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE R3 OBSTRUCTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 195UA 26899 DOOR 3R DIFFICULT TO CLOSE AND ARM. FOUND GIRT BAR FITTINGS CONTAMINATED WITH DEBRIS. REMOVED DEBRIS OPERATED DOOR AND LATCH SEVERAL TIMES DOOR OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042400085 20080424 00085 NM 2008 4 24 NWAA081643133 1 20080417 A 2530 COFFEEMAKER AIRBUS A319 A319114 3930350 NM GALLEY ODOR A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 333NB 1582 DURING CLIMB-OUT, STRONG BURNING SMELL IN FLIGHT DECK AND CABIN. FLIGHT ATTENDANT FOUND THAT 1ST CLASS GALLEY COFFEEMAK ER WAS OVERHEATING AND NOT TURNING OFF WITH SWITCH. COFFEEMAKER CB PULLED FOR REMAINDER OF FLIGHT. REPLACED COFFEEMAKE R. 2 L 7 2 4F RT A28NM 2008042400086 20080424 00086 EU 2008 4 24 F3LA200800171 1 20080410 A 5340 D5311201500100 FITTING AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED R1 FORWARD GIRT BAR FITTING PLATE WAS CORRODED IN SEVERAL PLACES. MAINTENANCE REM OVED AND REPLACED FITTING PLATE. OKAY TO INSTALL AND INSTALL WILL BE ACCOMPLISHED ON WORK CARD CP7553-12. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042400101 20080424 00101 NM 2008 4 24 DLM90080603 1 20080306 A 5230 SKIN DOUG MD90 MD9030 3023690 NM CARGO DOOR DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 MID CARGO DOOR, FOUND TO BE AFT SECTION, SKIN DENTED 12 INCHES FROM RIGHT AND 14.5 INCHES FROM TOP. REPAIRED, IAW MD90 SRM 51-00-01 AND MD80 SRM 52-05D. 2 L 7 2 4F RT A6WE 2008042400102 20080424 00102 NM 2008 4 24 DLM90080604 1 20080306 A 5730 SKIN DOUG MD90 MD9030 3023690 NM RT WING GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 96892 53392 REPAIR ON RT WING L/E STA XCW 121 IS GOUGED. REPAIRED RT WING L/E, IAW DELTA ERA 467132-14 REV ORIG DATE ISSUED 26MAR08 VIA AAR EA 12567 REV I/R DATE ISSUED 26MAR08. 2 L 7 2 4F RT A6WE 2008042400103 20080424 00103 NM 2008 4 24 DLM90080605 1 20080306 A 5753 VANE DOUG MD90 MD9030 3023690 NM LT WING TE FLAP DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 97148 53392 LT WING I/B FLAP FIXED VANE LOWER SURFACE HAS MULTIPLE DENTS. REPAIRED LT WING I/B FLAP I/B VANE, IAW MD90 SRM 57-50-04 . 2 L 7 2 4F RT A6WE 2008042400106 20080424 00106 NM 2008 4 24 DLM88080609 1 20080418 A 5751 FAIRING DOUG MD88 MD88 3023688 NM AILERON DAMAGED A DALA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 SO 27 967DL 53116 LT AILERON TRIM TAB ACTUATOR ROD MISSING A PORTION OF FAIRING. DRILLED AND INSTALLED PANEL O/B OF AILERON TRIM SURFACE NEED PAINTED. REMOVED PNL PAINTED AND REINSTALLED. LEFT ALL CONT TAB AND LEFT AILERON PER JIC OPERATION NR 7037 7038 7 039. REQUIRED INSPECTION COVERED. 2 L 7 2 4F RT A6WE 2008042400108 20080424 00108 NM 2008 4 24 DLM88080616 1 20080420 A 2410 249001200 CSD DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE UNSERVICEABLE A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 933DL 49720 726047 LEFT GEN FAILED DURING INITIAL CLIMB-OUT WITH AN OPEN BUS TIE THE APU GEN WAS RUNNING AT THE TIME AND CARRIED THE LEFT G EN LOAD FWD LT GEN TO MCO AND PLAC PER MEL24-00-01A LT CSD DISC VERIFIED APU OIL FULL AND PERFORMED A CROSSTIE CK. CKD GCU. NO FAULTS. CHKD CSD CHIP DETECTOR. NO METAL FOUND. REPLACED LT GEN CSD PER M/M. ALSO REPLACED LT ENG GCU. RAN ENGINE CKD GEN/CSD OUTPUT OPERATION PER M/M. ALL CKS GOOD MCO PLAC REMOVED. GCU OFF S/N UM 3656C ON XJ2125B DPN. 2 L 7 2 4F 4 F RT A6WE E9NE 2008042400110 20080424 00110 NM 2008 4 24 DL76G080619 1 20080421 A 2750 LIMITER BOEING 767 767332 1382001 NM FLAP TORQUE MALFUNCTIONED A DALA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 SO 27 174DZ 29693 TE FLAP DISAGREE ON GO AROUND. A/C DECLARED EMERGENCY LANDING. TE FLAP SHUTDOWN EICAS MSG WITH FLAPS LOCKED AT 24 DEG. ON ARRIVAL AT GATE, MTC PERFORMED, BITE OF FSPM CARDSALL TEST OK, PSEU BITE IS GO. FLAP TORQUE LIMITERS WERE NOT TRIP PED. ALL T/DONE PER FIM. RESET ALT FLAP SWITCHES AND MSG EXTINGUISHED. RAN FLAPS ALL OP CKS NORMAL. FLAP HANDLE DE TENT AND PIN INSP OK. 2 L 7 2 4F RT A1NM 2008042400112 20080424 00112 NM 2008 4 24 NWAA081706740 1 20080417 A 5320 STRUCTURE BOEING 747 747251F 1384898 NM MISREPAIRED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING "L" CHECK WHILE ACCOMPLISHING VERTICAL BEAM INSPECTION FOUND DISCREPANT EXISTING REPAIR DOUBLER AND CRACK COMMON TO THE NOSE WHEEL WELL VERTICAL BEAM WEB AT BS 320 RT BETWEEN WL 180-WL 190. THE EXISTING REPAIR DOUBLER OBSTRUCTS THE SURFACE SCAN HFEC REQUIRED BY INSPECTION. REPAIRED PER EA 67-212651. 2 L 7 4 4F RT A20WE 2008042400117 20080424 00117 NM 2008 4 24 DHLA200800041 1 20080422 A 2612 FIRE WARNING BOEING 727 72764 1384069 NM MALFUNCTIONED A DHLA O OTHER N FALSE WARNING CR CRUISE 1 GL 05 765AT 23014 FLT NR 1489 FIRE WARNING BELL ONLY AT CRUISE FL 330 COMPLETED ABNORMAL PROCEDURES ALL SYSTEMS TESTED NORMAL. PERFORMED SYSTEM CK OF FIRE DETECTION SYSTEM OPS NORMAL IAW MM 26-11-0. AIRCRAFT WAS GROUNDED. 2 L 7 3 4F RT A3WE 2008042400120 20080424 00120 NM 2008 4 24 NWAA081746301 1 20080421 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 661US 23719 DURING OVERNIGHT CHECK, FOUND EXTERNAL EMERGENCY LIGHTS INOP RIGHT SIDE (2BOTTOM). MAINTENANCE REMOVED AND REPLACED OVE RWING EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008042400124 20080424 00124 EU 2008 4 24 F3LA200800202 1 20080412 A 5320 D53476483200 SUPPORT FITTING AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION, NOTED CENTER FLOORBEAM SUPPORT FITTING BETWEEN C59 AND C60 CORRODED. MAINTENANCE REMOV ED CORROSION ON SUPPORT FITTING AND REINSTALLED SUPPORT FITTING AND CENTER FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 AND EA A9-53R-30227. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042400125 20080424 00125 EU 2008 4 24 F3LA200800204 1 20080404 A 5320 D53480043205 SILL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED R2 DOOR SILL HAS CORROSION AROUND NUT CLIP HOLE AT FRAME 66. MAINTENANCE FABRICAT ED REPAIR ANGLE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-41-14, FABRICATED LEFT AND RIGHT REPAIR ANGLES IN ACCORDAN CE WITH THE REQUIREMENTS OF EA A0-53F-12234. REMOVED CORROSION IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-41-14 FIGU RE 201, MATERIAL FOR ANGLE REPAIR 7075T7351. INSTALLED REPAIR SPLICE IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-3 0218 AND SRM 53-41-14 FIGURE 201. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042400127 20080424 00127 SO 2008 4 24 CHQA200800080 1 20080419 A 2913 PV303211MODA PUMP EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL HYD SYSTEM OVERHEATED A CHQA O OTHER M J OVER TEMP WARNING INDICATION CR CRUISE 1 GL 11 287SK 19569 4324 145460 CAE312670 FLIGHT 5901, CLE TO MSY - WHILE CRUISING AT FL360 THE FLIGHT CREW RECEIVED A MASTER CAUTION AND EICAS MESSAGE FOR HYD SY S 1 OVHT. THE CREW RAN THROUGH THE APPROPRIATE QRH CHECKLISTS AND SHUT OFF THE SYSTEM. AFTER WAITING THE QRH RECOMMEND ED TIME, THE NR 1 HYDRAULIC SYSTEM WAS RE-ENERGIZED. AFTER RE-ENERGIZING THE HYDRAULIC SYSTEM IT WOULD NOT INDICATE AN ACCEPTABLE PRESSURE. ON DESCENT, THE MFD INDICATION FOR THE NR 1 SYSTEM BEGAN TO SHOW PRESSURE, AND DURING APPROACH ALL SYSTEM 1 INDICATIONS WERE NORMAL AND THE HYD SYS 1 OVHT MESSAGE WAS GONE. MAINTENANCE TROUBLESHOT THE HYDRAULIC SYSTEM AND REPLACED THE SYSTEM 1 RESERVOIR AND FILTERS AND THE HYDRAULIC SYSTEM OPERATED NORMALLY. LATER THAT DAY THE HYD SYS 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008042300118 20080423 00118 NM 2008 4 23 ASAA0852812 1 20080409 A 3610 32895625 CONTROL VALVE BOEING 737 737890 1384527 NM BLEED AIR SYS FAILED A ASAA K NONE O OTHER CL CLIMB 1 NM 02 587AS 1801 35684 PNEUMATIC DUCT PRESSURE SPLIT BETWEEN LEFT AND RIGHT SYSTEMS NOTED DURING CLIMB. REPLACED RIGHTHAND ENGINE PRECOOLER CO NTROL VALVE. 2 L 7 2 4F RT A16WE 2008042300119 20080423 00119 EU 2008 4 23 SA08029 1 20080416 A 2560 P2070001214 BATTERY PACK AIRBUS A319 A319112 3930323 EU FLASHLIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 757UW 1342 LAX - AFT FLIGHT ATTENDANT LEFT JUMPSEAT FLASHLIGHT IS INOP. MAINTENANCE REPLACED BATTERY PACK ASSEMBLY. OPS CHECKS OK . 2 L 7 2 4F RT A28NM 2008042300128 20080423 00128 NM 2008 4 23 USAA920080888 1 20080416 A 5313 STRINGER BOEING 737 7373B7 1384580 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 23379 CLT - MAJOR REPAIR - NR 4364480, CORROSION ON STR 27L AT BS 1007. INSTALLED NEW SECTION OF STRINGER IAW SRM 53-60-03. 2 L 7 2 4F RT A16WE 2008042300132 20080423 00132 2008 4 23 ASAA0852813 2 20080409 A 7261 SEAL BOEING 737 737890 1384527 NM IDG DAMAGED A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 587AS 35684 OIL LEAK DISCOVERED AT IDG MOUNT SEAL. REPLACED SEAL AND REINSTALLED IDG. 2 L 7 2 4F RT A16WE 2008042300144 20080423 00144 NM 2008 4 23 UPS08M52035 1 20080326 A 5730 ARB39546 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:4C RIGHT WING LE SKIN SPLICE STRAP XFS669 CRACKED. REMOVED CRACKED SPLICE STRAP, FABRICATED AND INSTALL ED REPLACEMENT SPLICE STRAP IAW DWG ARB3954 AND MD-11 SRM 51-33-01. 2 L 7 3 4F RT A22WE 2008042300159 20080423 00159 NM 2008 4 23 SA08028 1 20080415 A 2421 IDG AIRBUS A319 A319132 3930340 NM NR 2 MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 829AW 1563 ORD, FLIGHT 59, PHX-IAD - DURING CRUISE THE APU SHUT DOWN. THE CREW DIVERTED TO ORD DUE TO THE NUMBER TWO IDG ON MEL. MAINTENANCE REPLACED THE IDG THAT WAS ON MEL, SERVICED THE APU WITH OIL. NO LEAKS WERE NOTED WITH THE APU RUNNING FOR S EVERAL HOURS. 2 L 7 2 4F RT A28NM 2008042300217 20080423 00217 EA 2008 4 23 MASA200800314 1 20080411 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 77302 7302 RIGHT WING PLANK IS CRACKED. REPAIRED PLANK. 2 L 7 2 4F RT A21EA 2008042300221 20080423 00221 2008 4 23 UPS08152015 4 20080411 A 2565 WARNING LIGHT AIRBUS A300 A300F4622R 3930360 EU COCKPIT MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 143UP 0826 INSPECTION TYPE:N/A RED SLIDE WARNING LIGHT IS INOP. AURAL HORN TESTS OK. PERFORMED ADJUSTMENT/TEST EMERGENCY ESCAPE S LIDE RELEASE WARNING LIGHT, AURAL HORN OPERATING NORMALLY AT THIS TIME. OK FOR SERVICE IAW MM 52-73-00-05. 2 L 7 2 4F RT A35EU 2008040800073 20080408 00073 NM 2008 4 8 ZZDA2008085 1 20080326 A 2120 UNKNOWN BOEING 737 7377BD 1384511 NM CABIN ODOR A ZZDA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 37 292AT 33926 STRONG ELECTRICAL SMELL IN BACK OF CABIN MOVED FORWARD. DISSIPATED RAPIDLY DURING INITIAL CLIMBOUT FROM AIRPORT. EXTEN DED DOWNWIND TO BURN OFF FUEL TO LAND UNDERWEIGHT FLIGHT CREW NEVER SMELLED UNTIL TAXI IN, ACTUAL LANDING WEIGHT WAS 127 500 LB. (MAX WEIGHT IS 128600). RAN BOTH ENGINES AND POWERED ALL ELECTRICAL SYSTEMS, HYDRAULIC SYSTEMS AND PRESSURIZED AIRCRAFT DURING INSPECTION OF COCKPIT AND CABIN FOR ANY SMOKE OR BURNING SMELL. NO ODOR OR SMOKE WAS NOTED ALL AIRCRAFT SYSTEMS OPERATE NORMAL REF B737 AMM 71-00 AND 21-31. UPON ARRIVAL AT GATE FOUND NO ODOR WITHIN CABIN. 2 L 7 2 4F RT A16WE 2008040800077 20080408 00077 SO 2008 4 8 FDKA200803137 1 20080327 A 5270 SWITCH EMB 145 EMB145LR 3260212 SO CARGO DOOR OUT OF ADJUST A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 860MJ 145773 FDM 6159 CVG-GSO (0503 PHX LCL). BAG DOOR WARNING LIGHT STAYS ILLUMINATED WITH DOOR VERIFIED CLOSED. MX ADJUSTED MICRO -SWITCH OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008040800078 20080408 00078 SO 2008 4 8 FDKA200803138 1 20080327 A 3350 20131A POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 8726 145568 FDM RON FLL (2115 PHX LCL). LEFT OVERWING EXTERNAL EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED POWER SUPPLY. 2 L 7 2 4T RT T00011AT 2008040800079 20080408 00079 SO 2008 4 8 FDKA200803139 1 20080329 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6008 JFK-RDU (1501 PHX LCL). GALLEY SERVICE DOOR EXIT LIGHT WAS INOPERATIVE. MX REPLACED THE BATTERY PACK AND FIXE D THE BROKEN WIRE AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2008040800085 20080408 00085 NM 2008 4 8 HNAA0800120 1 20080330 A 3350 OL3071BPEGPL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 824EX 30366 30366 387 ONE FLOOR LEVEL EMERGENCY LIGHT INOP. MX RELAMPED, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 2008040800087 20080408 00087 NM 2008 4 8 WRLA2008032 1 20080401 A 5320 AGA7170U78911 STIFFENER DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 48407 DURING C-CHECK INSPECTION FOUND FLOORBEAM SUPPORT 5 EA STIFFENERS CRACKED STA Y=1841 X=-9.5, X=26, X=30.5, X=38, X=-38. REPLACED STIFFENERS PER MD11 SRM 51-35-01 VOL II REV 40. 2 L 7 3 4F 4 F RT A22WE E24NE 2008040800088 20080408 00088 SO 2008 4 8 C2XA08RI040 1 20080331 A 5210 14540853405 DOOR EMB 145 EMB145XR 3260214 SO MAIN CABIN DOOR OUT OF RIG A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 34110 15382 145658 FLIGHT 2965 - EWR - CREW REPORTED MAIN CABIN DOOR DIFFICULT TO OPEN. EWR MX RE-RIGGED DOOR AND PERFORMED OPERATIONAL CH ECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2008040800092 20080408 00092 EA 2008 4 8 COMA0860199 1 20080329 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 451CA 15870 7562 FLIGHT 5440 - ON CLIMBOUT FROM JFK RECEIVED FLAPS FAIL CAUTION MESSAGE AT 8 DEGREES. EMERGENCY DECLARED, AIRCRAFT RETUR NED BACK TO JFK AND LANDED SAFELY. REMOVED AND REPLACED LEFT BPSU. 2 L 7 2 4F RT A21EA 2008040800094 20080408 00094 EA 2008 4 8 COMA0860200 1 20080330 A 2750 860D10018 ECU CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAULTY A COMA K NONE F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 SO 01 597SW 22187 7293 FLIGHT 5301 - DURING DESCENT THROUGH 17,800FT AT 280 KTS INTO SRQ, RECEIVED FLAPS HALF SPEED MESSAGE FOLLOWED BY FLAPS F AIL CAUTION MESSAGE. FLAPS WERE AT 0 DEGREES. EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED FECU. ALSO, COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW-UP MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 2008040800097 20080408 00097 EA 2008 4 8 COMA0860203 1 20080331 A 2421 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA NR 1 ENGINE FAILED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 804CA 29607 7352 FLIGHT 5523 - ON TAKEOFF ROLL NR 1 IDG CAUTION MESSAGE, FOLLOWED BY NR 1 GENERATOR CAUTION MESSAGE. TAKEOFF ABORTED AT LOW SPEED 30 KTS. REMOVED AND REPLACED NR 1 IDG. 2 L 7 2 4F RT A21EA 2008040800099 20080408 00099 SO 2008 4 8 C2XA08IA094 1 20080330 A 5730 14537011006 SKIN EMB 145 EMB145EP 3260221 SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14947 145054 IAH - FLIGHT 2695, DURING PREFLIGHT INSPECTION, THE CREW REPORTED CRACKS AT THE SPOILER HINGE POINTS. MAINTENANCE INSPE CTED THE AIRCRAFT, AND DETERMINED THAT ONLY THE RIGHT HAND UPPER CENTER HINGE CUTOUT TO HAVE AN 18MM CRACK. THE CRACK W AS PLACED ON DMI FOR 500 FLIGHT CYCLES WITH RE-INSPECTIONS AT EVERY 50FC FOR PROPAGATION, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SDR FILED OPEN PENDING FINAL REPAIR. 2 L 7 2 4F RT T00011AT 2008040800108 20080408 00108 EU 2008 4 8 08FDEA01307 1 20080402 A 5320 AC400184610 SHIELD AIRBUS 310 A310203 3930313 EU ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 BULK PIT DOORWAY NET SHIELD CHAFED REF EA 6-2550-90213. COMPLIED WITH EA 6-2550-90213. 2 L 7 2 4F RT A35EU 2008040800110 20080408 00110 NM 2008 4 8 SWAA081733 1 20080330 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 20L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008040800112 20080408 00112 NM 2008 4 8 SWAA081735 1 20080330 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008040800113 20080408 00113 NM 2008 4 8 SWAA081736 1 20080331 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 939 AND BS 943, STR 25R AND STR 24R. REPAIRED SKIN P ER SRM. 2 L 7 2 4F RT A16WE 2008040800115 20080408 00115 NM 2008 4 8 SWAA081748 1 20080330 A 2121 21520 GASPER FAN BOEING 737 7373H4 1384600 NM E&E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 29 343SW 24151 CREW REPORTS ELECTRICAL SMELL IN CABIN. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2008040800117 20080408 00117 WP 2008 4 8 WRLA2008033 1 20080229 A 5312 ANB71122 BOLT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE RT MLG WW SHEARED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 138WA 47844 DURING C-CHECK INSPECTION FOUND RIGHT HAND MAIN LANDING GEAR WHEEL WELL INTERIOR OUTBOARD BULKHEAD STA 1481 30 INCHES BE LOW THE HORIZONTAL BULKHEAD AFT SIDE OF THE VERTICAL SUPPORT BEAM HAS A BOLT HEAD SHEARED OFF. REAMED HOLE TO REMOVE TH E DEFECT AND ACCOMPLISHED HFEC INSPECTION TO CHECK FOR POSSIBLE CRACKS, NONE WAS FOUND. REMOVED AND REPLACED BOLT PER E CRA 242NW-57-DC10-019. 2 L 7 3 4F 4 F A22WE E23EA 2008040800118 20080408 00118 WP 2008 4 8 WRLA2008035 1 20080123 A 5230 SKIN DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE FWD CARGO DOOR DENTED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 138WA 47844 DURING C-CHECK INSPECTION FOUND DENT ON THE FWD CARGO DOOR APPROX 12" FROM THE BOTTOM OF THE DOOR, OUT OF LIMITS PER DC1 0 SRM 53-20-00. REMOVED DAMAGE AND REPAIRED ON FWD CARGO DOOR APPROX 12" FROM THE BOTTOM OF THE DOOR PER ECRA 242NW-52- DC10-010 AND VOL II SRM CHAP 51. 2 L 7 3 4F 4 F A22WE E23EA 2008040800120 20080408 00120 WP 2008 4 8 WRLA2008034 1 20080205 A 5330 SKIN DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 138WA 47844 DURING C-CHECK INSPECTION FOUND CORROSION AT Y1531L AFT OF LT MLG WHEEL WELL OUTBOARD SIDE. REMOVED CORROSION AND REPAI RED AREA AT Y1531L AFT OF LT MLG WHEEL WELL OUTBOARD SIDE IAW ECRA 242NW-53-DC10-012. 2 L 7 3 4F 4 F A22WE E23EA 2008040800125 20080408 00125 NM 2008 4 8 SWAA081766 1 20080401 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008040800129 20080408 00129 NM 2008 4 8 SWAA081767 1 20080401 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 420WN 29825 DURING SCHEDULED MV1 CHECK, FOUND LT AFT CABIN EEPLS INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008040800130 20080408 00130 NM 2008 4 8 SWAA081768 1 20080401 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 EEPLS LENS MISSING AT ROW 3 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008040800135 20080408 00135 NM 2008 4 8 SWAA081771 1 20080401 A 3350 MS155721 LIGHT BOEING 737 737317 138447P NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008040800138 20080408 00138 SO 2008 4 8 C2XA08ON109 1 20080330 A 3610 2305591728 DUCT CLAMP EMB 145 EMB145XR 3260214 SO R 1 ENGINE MISSING A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 17185 6951 6951 14500922 FLT 0412 - SAN - FLIGHT CREW ABORTED T/O DUE TO NR 1 ENG EXCEEDANCE ON TAKEOFF ROLL. MX INSPECTED BLEED DUCTS AND COMPR ESSOR BLEED AIR DUCTING ON ENGINE AND FOUND CLAMP MISSING ON COMPRESSOR DISCHARGE TUBE. INSTALLED NEW CLAMP OPERATIONAL LY AND LEAK CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008040800139 20080408 00139 SO 2008 4 8 FDKA200803140 1 20080330 A 4950 O-RING EMB 145 EMB145LR 3260212 SO APU DAMAGED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 837MJ 145367 FDM 6133 CVG-SDF (0749 PHX LCL). FUEL SMELL IN CABIN FROM APU BLEED. MX REMOVED AND REPLACED O-RINGS ON SOLENOID. 2 L 7 2 4T RT T00011AT 2008040800141 20080408 00141 SO 2008 4 8 C2XA08SH052 1 20080403 A 5310 14524061008 DOOR FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11547 145563 SHV - DURING C-CHECK THE SERVICE DOOR CUTOUT WAS FOUND TO BE CORRODED AROUND A NUT PLATE AT FRAME 22, STRINGER 16R. MAI NTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5310-01373. THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008040800146 20080408 00146 SO 2008 4 8 C2XA08TY041 1 20080401 A 5751 14569009410 BUSHING EMB 145 EMB145XR 3260214 SO RT AILERON LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13132 145708 RIGHT AILERON O/B PCA BRACKET FITTING HAS LOOSE BUSHING. REMOVED AND REPLACED AILERON PCA FITTING IAW EC 5750-01177 REV B. AIRCRAFT STILL IN C-CHECK. 2 L 7 2 4F RT 2008040800148 20080408 00148 SO 2008 4 8 C2XA08RI042 1 20080329 A 3222 2666A000001 STRUT EMB 145 EMB145XR 3260214 SO NLG LOW A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13118 15133 145675 FLIGHT 2076 - EWR - CREW REPORTED GEAR WOULD NOT RETRACT. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. EWR MX SE RVICE THE NOSE LANDING GEAR STRUT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERV ICE. 2 L 7 2 4F RT 2008040400002 20080404 00002 NM 2008 4 4 IU6R080304001 1 20080304 A 7830 0711346100 HOUSING DOUG MD88 MD88 3023688 NM VALVE ASSY LEAKING B IU6R K NONE K FLUID LOSS IN INSP/MAINT 1 NM 01 1370A PIN HOLE LEAK ON THE SIDE OF THE PRESSURE PORT. 2 L 7 2 4F RT A6WE 2008040400055 20080404 00055 NM 2008 4 4 2008UALA01801 1 20080329 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 CEILING EMERGENCY LIGHT INOP DOOR 3R. SUPPLEMENTAL DATA UPDATE, RELAMP. OPS CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300229 20080423 00229 2008 4 23 SWAA081933 4 20080411 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 248WN 32509 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042300241 20080423 00241 NM 2008 4 23 SWAA081938 1 20080412 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008042300256 20080423 00256 EA 2008 4 23 A6WA200840147 1 20080303 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA NR 2 OVERHEATED A A6WA O OTHER M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 435AW 7724 PACK NR 2 OVERHEATED ON GROUND CAUSING SMOKE IN THE CABIN. UNCONTROLLABLE IN AUTO OR MANUAL. (M) 2 L 7 2 4F RT A21EA 2008042300261 20080423 00261 EU 2008 4 23 2008UALA02144 1 20080412 A 3510 CMK8001 SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OXYGEN SYSTEM ILLUMINATED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 423UA 504 ECAM MSG O2 REG LOW PRESS WITH SWITCH ON. FOUND LOW OXYGEN PRESSURE SWITCH FAILED. REPLACED LOW OXYGEN LOW PRESSURE SWI TCH. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042300268 20080423 00268 NM 2008 4 23 2008UALA02145 1 20080411 A 3397 FEEDER CABLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 301UA 23642 AFT CABIN EEL LIGHTING INOPERATIVE. REPLACED AFT SECTION POWER LEAD & AFT GALLEY EEL LIGHT. OPS CKS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042300277 20080423 00277 NM 2008 4 23 SWAA081989 1 20080413 A 5311 65C34356 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300286 20080423 00286 NM 2008 4 23 SWAA081981 1 20080413 A 5311 65C33511 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300340 20080423 00340 NM 2008 4 23 SWAA082010 1 20080414 A 5310 6547684 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR CUTOUT LOWER STOP FITTING CUTOUT CRACKED AT STA 303. REMOVED AND REPLACED WE B PER SRM. 2 L 7 2 4F RT A16WE 2008042300385 20080423 00385 NM 2008 4 23 SWAA082036 1 20080416 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2008042300386 20080423 00386 NM 2008 4 23 SWAA082035 1 20080416 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 435, STR 1. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008042300401 20080423 00401 NM 2008 4 23 SWAA082061 1 20080417 A 5512 65C25727 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 141. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042400001 20080424 00001 EU 2008 4 24 08FDEA01469 1 20080422 A 5320 A5398038920000 SHEAR WEB AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 MAIN DECK CARGO DOOR RIGHT SIDE SHEAR WEB IS CRACKED BETWEEN FRAME 76 AND FRAME 77. REMOVED WEB IAW SRM 51-40-21. FABR ICATED WEB IAW SRM 51-26-00 & MARKED IAW GMM 7-0-1001. HEAT TREATED IAW TPS 1003, REV A. ALODINED; PRIMED & PAINTED IAW SRM 51-21-10; PG 1. INSTALLED WEB IAW SRM 51-40-21; PG 7. HEAT TREAT LOAD HT050608-3. 2 L 7 2 4F RT A35EU 2008042400005 20080424 00005 EU 2008 4 24 08FDEA01473 1 20080422 A 5230 A5397822421000 DEPRESSOR AIRBUS 300 A300F4605R 3930327 EU CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 AFT CARGO DOOR FWD CUTOUT PRESSURE SEAL DEPRESSOR IS GOUGED FROM TOP TO BOTTOM. REMOVED & REPLACED SEAL DEPRESSOR IAW S RM 51-40-21. 2 L 7 2 4F RT A35EU 2008042400007 20080424 00007 WP 2008 4 24 08FDEA01475 1 20080422 A 5315 AEA03611 FLOORBEAM DOUG MD10 MD1010F 3022112 WP BS 1276 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 CABIN OVERWING FLOOR SUPPORT BEAM IS CRACKED AT STA 1276 RBL 107; AT R-3 DOOR THRESHOLD. REPAIRED CRACKED BEAM AT STA 1 276 BY SPLICING IN A NEW SECTION IN REF TO E.A. 8-5310-118481. 2 L 7 3 4F RT A22WE 2008042400013 20080424 00013 EU 2008 4 24 08FDEA01460 1 20080420 A 5743 R57249121 TRUNNION AIRBUS 310 A310203 3930313 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 445FE 297 RT MLG RIB 5 CENTER TRUNNION LUG FWD INBD RADIUS CHAFED APPROX .60 IN LONG BLENDED CHAFED AREA IAW FEDEX EA 6-5710-11810 8, RELEASE DATE 19 MARCH, 2008. 2 L 7 2 4F RT A35EU 2008042400036 20080424 00036 WP 2008 4 24 UPS08852022 1 20080413 A 3350 BULB DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 EMERGENCY EXIT LIGHT AT THE C1 DOOR HAS 2 BULBS OUT. REMOVED AND REPLACED 2 BULBS FOR THE EMERGENCY EXIT LIGHTING AS NE EDED. 2 L 7 4 4F RT 4A25 2008042400041 20080424 00041 SO 2008 4 24 CHQA200800078 1 20080413 A 3600 4800112 SWITCH EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BLEED SYSTEM FAULTY A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 568RP 145800 CAE312367 FLIGHT 6360, CVG TO STL - DURING CLIMB IN ICING CONDITIONS, CREW RECEIVED AN E1 BLEED VALVE FAIL MESSAGE, WITH THE ASSOC IATED BLEED VALVE CLOSED AND WING ANTI-ICE FAIL MASTER WARNING. THE CREW RAN THE APPROPRIATE QRH CHECKLISTS AND RETURNE D TO CVG. THE AIRCRAFT LANDED WITHOUT INCIDENT IN CVG. MAINTENANCE TROUBLESHOT THE FAULT THE PUSH BUTTON FOR THE NUMBE R 1 BLEED SYSTEM. AFTER REPLACING THE PUSH BUTTON, THE BLEED SYSTEM OPS CHECKED GOOD PER AMM 36-11-05. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008042400056 20080424 00056 NM 2008 4 24 2008UALA02197 1 20080414 A 3397 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 596UA 28749 EEL LIGHTS STRIP INOP FROM ROW 31 TO 34. FOUND A SHORT IN THE EEL STRIP. REPLACED EEL LIGHT STRIPS, OPS CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400067 20080424 00067 NM 2008 4 24 2008UALA02259 1 20080418 A 2560 BATTERY BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FLASHLIGHT DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FWD LT EMERGENCY FLASHLIGHT AT FWD FA SEAT WAS USED AND NOT PUT INTO BRACKET PROPERLY. BATTERY NEEDS TO BE REPLACED. FO UND BATTERY DISCHARGED. REPLACED BATTERY. CHECKS GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042400077 20080424 00077 NM 2008 4 24 2008UALA02269 1 20080417 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 842UA 1569 CREW OXYGEN LOW. SERVICED CREW O2, NO LEAKS NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042400090 20080424 00090 2008 4 24 08FDEA01463 2 20080420 A 7310 AC9227F1740 FILTER AIRBUS 300 A300F4605R 3930327 EU NR 1 ENG FUEL CLOGGED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 25 681FE 799 NR 1 ENGINE FUEL FILTER CLOG LIGHT CAME ON DURING TAKEOFF ROLL AT 80 KTS WITH STD POWER SET. LIGHT AND ECAM WARNING WEN T OUT AS SOON AS THROTTLES WERE RETARDED TO IDLE. REMOVED NR 1 ENGINE FUEL FILTER. FOUND FILTER CLOGGED WITH DEBRIS. INSTALLED NEW FUEL FILTER, REF MM 73-12-02-4. LEAK CHECK GOOD, REF MM 71-00-00. OK TO CONTINUE. 2 L 7 2 4F RT A35EU 2008042400094 20080424 00094 NM 2008 4 24 08FDEA01468 1 20080421 A 3200 PIN DOUG MD11 MD11F 3023600 NM MLG INSTALLED A FDEA J A DUMP FUEL UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SO 25 617FE 48748 AFTER TAKEOFF AND GEAR RETRACTION. CENTER MAIN LANDING GEAR SHOWED RED. EXTENDED GEAR ALL POSITIONS GREEN. DUMPED 30K FUEL. RETURNED TO MEM LANDED UNEVENTFULLY. REMOVED CENTER LANDING GEAR SAFETY LOCK PIN. RETURNED TO SERVICE. 2 L 7 3 4F RT A22WE 2008042400096 20080424 00096 EU 2008 4 24 NWAA081693275 1 20080416 A 5330 SKIN AIRBUS 320 A320212 3930322 EU FUSELAGE DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 375NC 1789 DURING GROUND OPERATIONS FUSELAGE SKIN WAS DAMAGED FROM S41L-S43L AT FR 57 TO FR 58. REPAIRED PER EA 32-212764 SECT II SECT III PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 60 DAYS OF SECT II. 2 L 7 2 4F RT A28NM 2008042400100 20080424 00100 NM 2008 4 24 DLM90080602 1 20080306 A 5320 CHANNEL DOUG MD90 MD9030 3023690 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 97017 53392 RT GEAR WHEEL WELL CUTOUT FWD FRAME EXISTING REPAIR AT I/B END CRACKED. REMOVED AND REPLACED 5930584412 CHANNEL, IAW MD 90 SRM 51-10-05. 2 L 7 2 4F RT A6WE 2008042400121 20080424 00121 EU 2008 4 24 F3LA200800198 1 20080409 A 5320 D53477101000 SUPPORT AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED FRAME 59 COVER PROFILE NUT PLATE HOLES WERE CORRODED FROM STRINGER 38 RIGHT TO 38 LEFT. MAINTENANCE BLENDED OUT CORROSION AND INSTALLED NEW SUPPORT AT FRAME 59 STRINGER 41 LEFT IN ACCORDANCE WITH THE R EQUIREMENTS OF SRM 51-42-11. INSTALLED REPAIR DOUBLER AND FILLER IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30247 . UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042400133 20080424 00133 NM 2008 4 24 08FDEA01485 1 20080423 A 5312 BULKHEAD BOEING 727 727232 1384082 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 BS 178 BULKHEAD EXT SURFACE WL 187 - 193 LBL 19" TO 24" HAS CORROSION PITS. CHEMICALLY REMOVED CORROSION FROM BS 178 BUL KHEAD EXT SURFACE WL 185-193 LBL 19" TO 24". THICKNESS OF MATERIAL IS .055, MATERIAL REMAINING IS .053 A LOSS OF .022 F OUND TO BE WITH-IN LIMITS. TREATED AND PRIMED AREA REF SRM 53-30-1 FIG 1, SRM 53-10-2 PG 7. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR. LEVEL 1 CORROSION. 2 L 7 3 4F A3WE 2008042400134 20080424 00134 NM 2008 4 24 08FDEA01486 1 20080423 A 5720 6521795350 FAIRING BOEING 727 727200 138407E NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 RT WING NR 6 FLAP TRACK FWD FAIRING HAS SEVERAL CRACKS REMOVED FASTENERS AND FABRICATED NEW REPAIR DOUBLER. INSTALLED N EW DOUBLER REF SRM 57-20-4 FIG 1. TREATED AND PRIMED AND PAINTED REF SRM 51-10-2 P2. THIS IS CLASSIFIED AS A MINOR REP AIR. 2 L 7 3 4F RT A3WE 2008042400135 20080424 00135 WP 2008 4 24 08FDEA01487 1 20080423 A 5512 NLC6031 SKIN DOUG DC10 DC1010 3022110 WP HORIZONTAL STAB DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 LT HORIZONTAL STABILIZER DENT ON INBOARD L/E, DIM: 3 INCH BY 1.5 INCH BY .100 INCH. REPAIR AREA IAW SRM 55-00-01 FIG.3 SHT 2 VOL.1. 2 L 7 3 4F A22WE 2008042400142 20080424 00142 NM 2008 4 24 08FDEA01494 1 20080423 A 5330 6518636280 SKIN BOEING 727 727232 1384082 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 MLG W/W KEEL BEAM LWR EXT SKIN PANEL AT BS 940 TO 950 PLUS 12, LBL 5- RBL 5 HAS SEVERAL AREAS OF CORROSION REMOVED ARE AS OF CORROSION. REMOVED 0.005 INCH FROM ORIGINAL SKIN THICKNESS OF 0.071 INCH. 0.066 INCH REMAINING AND SKIN PANEL IS WITHIN LIMITS. TREATED, PRIMED AND PAINTED AFFECTED AREA. REFERENCE SRM 51-10-6/PAGES 12-15, SRM 53-10-1/FIGURES 1 AN D 2 MM 51-20-021-7, MS51-20-031-7 AND MM 51-20-013-7. CLASSIFIED AS A MAJOR REPAIR, LEVEL 1 CORROSION. 2 L 7 3 4F A3WE 2008042400150 20080424 00150 EU 2008 4 24 08FDEA01502 1 20080423 A 7160 2242101569 NOSE COWL AIRBUS 300 A300F4605R 3930327 EU NR 1 ENGINE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 NR 1 ENGINE NOSE COWL IS DELAMINATED AT THE FWD LOWER END. REMOVED & REPLACED THE NR 1 NOSE COWL IAW AMM 71-11-00-4. FA N COWL DOORS TO BE ADJUSTED & CLOSED ON THE NR 1 ENGINE INSTALLATION W/C 64T0700-1. 2 L 7 2 4F RT A35EU 2008050200068 20080502 00068 NM 2008 5 2 USAA920080877 1 20080331 A 5753 STRUCTURE BOEING 757 757225 1384959 NM LT WING TE FLAP CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 921UW 22201 BFM - MAJOR REPAIR - LEFT WING INBOARD FLAP TRAILING EDGE CRACKED. REPAIRED LEFT WING INBOARD FLAP TRAILING EDGE CRACKE D IAW B757 SRM 57-53-01. 2 L 7 2 4F RT A2NM 2008040400089 20080404 00089 NM 2008 4 4 2008UALA01840 1 20080331 A 2421 IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 MALFUNCTIONED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 653UA 25391 R GEN DRIVE LIGHT ON CONTINUOUSLY. REPLACED NR 2 ENG IDG. OP CHECKED AND LEAK CHKD OK. A/C OK FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040400097 20080404 00097 NM 2008 4 4 2008UALA01848 1 20080331 A 3397 FEEDER CABLE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 777UA 26916 EMERGENCY LIGHTS INOP AT SEATS 17-20 BOTH SIDES. FOUND FEEDER CABLE DISCONNECTED AT SEAT 21. RECONNECTED CABLE. EEL S YSTEM OP CHECKD GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040400099 20080404 00099 NM 2008 4 4 2008UALA01850 1 20080401 A 2697 CONNECTOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FIRE LOOP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 NR 1 ENG FIRE LOOP A/B, INOP. REPLACED BAD CONNECTORS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008040400122 20080404 00122 EU 2008 4 4 08FDEA01257 1 20080402 A 5411 A54611750 SPAR AIRBUS 300 A300B4622R 3930312 EU NR 2 NACELLE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND OVERSIZED HOLE ON PYLON NR 2 LOWER SPAR, BETWEEN RIB 12-18. REPAIR PERFORMED BY BORING THE HOLE TO 21,5 MM, FREEZ E INSTALLATION OF SHOULDERED BUSH IAW RAS 70503539/004/2008 AND REPAIR DRAWING R546-10338, APPROVED BY EA 6-5451-11 4870. 2 L 7 2 4F RT A35EU 2008040400127 20080404 00127 EU 2008 4 4 08FDEA01262 1 20080317 A 5753 A5797020021200 FLAP TRACK AIRBUS 310 A310203 3930313 EU TE FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LEFT FLAP VANE NR 3 TRACK HAS WORN AREAS (MARKED). REPAIRED LEFT FLAP VANE NR 3 TRACK IAW AIRBUS CMM 57-52-15. 2 L 7 2 4F RT A35EU 2008040400145 20080404 00145 NM 2008 4 4 DLM88080448 1 20080331 A 2780 SLAT SYSTEM DOUG MD88 MD88 3023688 NM LE SLATS INOPERATIVE A DALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 27 919DE 53422 SLATS WILL NOT RETRACT FROM ZERO DEGREE POSITION. 2 L 7 2 4F RT A6WE 2008040400182 20080404 00182 NM 2008 4 4 DLM88080489 1 20080402 A 5313 LONGERON DOUG MD88 MD88 3023688 NM BS 160 L2 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, A BROKEN LONGERON WAS FOUND AT STA Y=160 LONG 2. LONGERON WAS REPAIRED IAW SRM 53-02 FIG 18. 2 L 7 2 4F RT A6WE 2008040700016 20080407 00016 NM 2008 4 7 AALA200800609 1 20080312 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN WRONG PART A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 659AA 24617 DFW - EMERGENCY LIGHT AT AFT RIGHT LAVATORY DOOR NEAR FLOOR AT L09007 HAS WRONG LIGHT. REPLACED LIGHT FOR EMERGENCY LIG HT AT AFT RIGHT LAVATORY DOOR NEAR FLOOR AT L09007. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040700028 20080407 00028 NM 2008 4 7 DLM88080506 1 20080402 A 5313 LONGERON DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, GALVANIC CORROSION AND WEAR WAS FOUND ON LONGERONS OF LT LAVATORY FLOOR PAN. LONGERON WAS REPLACED IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F RT A6WE 2008040700029 20080407 00029 NM 2008 4 7 DLM88080507 1 20080402 A 5313 LONGERON DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV GALVANIC CORROSION AND WEAR WAS FOUND ON LONGERONS OF RT LAVATORY FLOOR PAN. LONGERONS WAS REPLACED IAW SRM 51-30-2. 2 L 7 2 4F RT A6WE 2008040800018 20080408 00018 SO 2008 4 8 FDKA200803117 1 20080319 A 3350 SIGN EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6199 JFK-RIC (0350 PHX LCL). EMERGENCY LIGHT/SIGN OUT AT ROW 12. MX RESET EMERGENCY LIGHTING SYSTEM. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008040800026 20080408 00026 EA 2008 4 8 COMA0860187 1 20080321 A 3350 364911 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 917CA 7017 FLIGHT 5696 - EMERGENCY EXIT LIGHT AT SEAT 1C IS INOP. INSTALLED SERVICEABLE LIGHT STRIP. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008040800029 20080408 00029 EA 2008 4 8 COMA0860190 1 20080323 A 5320 601R3401725S CHANNEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 934CA 33024 7042 CRACK AT FS 280 GALLEY THRESHOLD FLOOR SUPPORT CHANNEL. REPLACED FLOOR SUPPORT CHANNEL IAW REO 601R-53-11-136. 2 L 7 2 4F RT A21EA 2008040800040 20080408 00040 SO 2008 4 8 C2XA08IA092 1 20080322 A 3350 66367 LIGHT EMB 135 EMB135LR 3260305 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14516 145323 IAH - FLIGHT 2326, DURING POST FLIGHT INSPECTION THE CREW REPORTED THAT THE THIRD FROM THE FORWARD AISLE PATH EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECK ED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008040800051 20080408 00051 SO 2008 4 8 FDKA200803130 1 20080324 A 5347 14532606001 SEAT TRACK EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 LEFT OUTBOARD SEAT TRACK AT FRAME 24 TO 30 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK. 2 L 7 2 4T RT T00011AT 2008040800057 20080408 00057 NM 2008 4 8 HNAA0800111 1 20080326 A 3350 OL3071BPEGPL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 812EX 312 ROW 5 EMERGENCY FLOOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULBS, OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2008040800100 20080408 00100 SO 2008 4 8 C2XA08IA095 1 20080331 A 2150 8152403 ACM EMB 135 EMB135LR 3260305 SO NR 1 SEIZED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 28518 16212 16212 145334 IAH - FLIGHT 2005, THE CREW REPORTED THAT THE NUMBER ONE PACK BLOWS HOT AIR AND BLACK SMOKE ON CLIMB WITH SOOT ON C/B'S FROM SMOKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ACM, OPER ATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008040800111 20080408 00111 NM 2008 4 8 SWAA081734 1 20080330 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 910, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008040800142 20080408 00142 SO 2008 4 8 C2XA08SH053 1 20080403 A 5210 14534499001 DOOR FRAME EMB 145 EMB145XR 3260214 SO PAX DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12172 14500864 SHV - DURING C-CHECK THE MAIN DOOR WAS FOUND TO HAVE CORROSION ON THE BOTTOM FRAME AROUND THE FORWARD NUT PLATE HOLE. M AINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5210-01154. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008040800151 20080408 00151 NM 2008 4 8 SWAA081777 1 20080402 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 12 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008040800170 20080408 00170 2008 4 8 SWAA081793 4 20080403 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008040800171 20080408 00171 NM 2008 4 8 SWAA081794 1 20080403 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD T/E. REMOVED AND REPLACED SLAT PER M M. 2 L 7 2 4F RT A16WE 2008040800183 20080408 00183 NM 2008 4 8 SWAA081802 1 20080403 A 5523 6959227 BUSHING BOEING 737 7373H4 1384600 NM LT ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED HC2 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 2 TAB BUSHING AND BOLT PER SWA EA. 2 L 7 2 4F RT A16WE 2008040800185 20080408 00185 NM 2008 4 8 SWAA081804 1 20080403 A 5311 6546543 BELTFRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELTFRAME CRACKED AT BS 663, STR 1. REPAIRED BELTFRAME PER SRM. 2 L 7 2 4F RT A16WE 2008040800199 20080408 00199 SO 2008 4 8 C2XA08SH059 1 20080407 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12136 145719 SHV - DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT FR 21-23. MX REPAIRED LT OMEGA BEAM AT FR 21-23 IAW EC 5320-01406. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008040800203 20080408 00203 NM 2008 4 8 SWAA081813 1 20080404 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 200WN 32482 DURING SCHEDULED HC1 CHECK, LEFT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F RT A16WE 2008040800204 20080408 00204 NM 2008 4 8 SWAA081815 1 20080405 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 219WN 32490 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008040800216 20080408 00216 NM 2008 4 8 SWAA081824 1 20080406 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008040800217 20080408 00217 NM 2008 4 8 SWAA081823 1 20080406 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008040900001 20080409 00001 NE 2008 4 9 865FLP2936 2 20080328 A 7230 COMPRESSOR DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 1 ENGINE STALLED A U2RA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 23 865F 46088 671364 NR 1 ENGINE COMPRESSOR STALLED AT 1000 FT AND WAS SECURED. ENGINE WAS RELIT PRIOR TO LANDING. ENGINE POWER ASSURANCE R UN ON GROUND DETECTED NO DISCREPANCIES. 2 L 7 4 4F 4 F 4A25 1E8 2008040900004 20080409 00004 NM 2008 4 9 QXEA200800332 1 20080326 A 2913 6617303 PUMP BOMBDR DHC8 DHC8402 1390042 NM HYD SYSTEM FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 427QX 2496 4156 FLT 2459 - IN CRUISE THE NR 2 HYDRAULIC PUMP CAUTION ILLUMINATED FOLLOWED BY THE RUDDER CONTROL FOLLOWED BY THE NR 2 ISO LATION VALVE. NORMAL CHECKLIST DIRECTED PTU ON NR 1. HYDRAULIC FLUID HOT CAUTION LIGHT ON APPROACH. FLAPS SELECTED AN D RECEIVED A FLAP POWER CAUTION LIGHT. LANDED WITH NO FLAPS, ALSO NO WHEEL BRAKES ON LANDING. STOPPED WITH THE EMERGE NCY PARKING BRAKE. MAINTENANCE REPLACED THE ENGINE DRIVEN PUMP, THE PTU, PTU SELECTOR VALVE, HYDRAULIC RESERVOIR TEMP S WITCH. BLED THE NR 2 HYDRAULIC SYSTEM AND BLED NR 1 AND NR 2 HYDRAULIC SYSTEM, BLED BRAKES, AND TAXI CHECKED FOR NOSE W HEEL STEERING AND PARKING BRAKES. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008040900006 20080409 00006 NM 2008 4 9 F3LA200800132 1 20080329 A 5343 D5288024720101 HINGE FITTING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE RT MLG CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 904FR 5357 1579 DURING C5 C CHECK INSPECTION REPORTED CORROSION WAS FOUND IN THE MOUNTING HOLES OF THE RIGHT MAIN LANDING GEAR FORWARD H INGE BEARING SUPPORT BRACKET. MAINTENANCE REAMED FITTING ONE SIZE OVER AND INSTALLED NEW BUSHING IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-52R-30180. UPON COMPLETION OF THE MAINTENANCE ACTION THE INSTALLATION WAS INSPECTED AND FOUND AC CEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008040900008 20080409 00008 NM 2008 4 9 F3LA200800133 1 20080329 A 5713 D57443513235 STRINGER AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE WING DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 904FR 5357 1579 DURING C5 C CHECK INSPECTION REPORTED DURING PERFORMANCE OF REPAIR STRINGER WAS DAMAGED. MAINTENANCE REPAIRED THE STRIN GER IN ACCORDANCE WITH THE REQUIREMENTS OF SRM A319 51-27-00 PAGE 1 AND SRM 51-42-11 PAGE 7. FOLLOWING COMPLETION OF T HE REPAIR, THE STRINGER WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008040900009 20080409 00009 NM 2008 4 9 P5CA0801551 1 20080321 A 7700 15EW2 SENSOR BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL NR 2 ENGINE MALFUNCTIONED A P5CA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 15 451PA 30809 AIR TURN BACK DUE TO NR 2 ENGINE SURGING N1, N2, EGT PARAMETERS ON TAKEOFF AND CONTINUED THROUGH CLIMB-OUT AND CRUISE, N 1 +/- 5%, N2 +/- 5%, EGT +/- 40. TROUBLESHOT AND FOUND A BAD T2.5 SENSOR. REMOVED AND REPLACED SAME. OPERATIONAL CHEC K NORMAL DURING ENGINE RUN. 2 L 7 4 4F 4 F RT A20WE E23EA 2008040900013 20080409 00013 NM 2008 4 9 HALA0800480 1 20080401 A 3610 79275516 CONTROLLER BOEING 767 7673G5 1385126 NM PRV MALFUNCTIONED A HALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, ATB A/C DIVERTED TO HNL. EICAS MESSAGE: L ENG BLEED OFF DISPLAYED ENG BLEED AIR VALVE OFF LIG HT ILLUM WITH SWT ON AND ENG RUNNING. DUCT PRESS 0 PSI. ACCOMPLISHED AMM 36-11-705-115. 2A TO 2I (4) 4/1/08, 2I (5) TO 2K PENDING. ACCOMPLISHED 2I (5) THRU STEP 2K, REPLACED PRVC PER AMM 36-11-19. REPLACED PRV PER AMM 36-11-18 LEAK CHK PEND ENG IDLE RUN CHK GOOD. ENG HIGH PWR RUN CHECKED GOOD. 2 L 7 2 4F RT A1NM 2008040900015 20080409 00015 2008 4 9 HALA0800482 4 20080401 A 3417 4039891906 INDICATOR BOEING 767 7673CB 1385187 NM AIRSPEED MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 588HA 33466 ETOPS SIGNIFICANT SYSTEM, CAPT AIRSPEED IND AIRSPEED FLAG INTERMITTENTLY IN VIEW. REPLACED CAPT'S A/S INDICATOR, GND CK OK PER MM 34-13-02. 2 L 7 2 4F RT A1NM 2008040900021 20080409 00021 EU 2008 4 9 MALA080052 1 20080331 A 2613 SEAL SAAB SF340 340B 7860101 EU OVERHEAT DETECT LOOSE A MALA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 403XJ 340B403 R TAILPIPE HOT INDICATION ON TAKEOFF CLIMB-OUT. RESEALED DETECTOR IAW SAAB MM 26-00-00, ALL CKS GOOD. 2 L 7 2 4T RT A52EU 2008040900026 20080409 00026 EU 2008 4 9 AALA200800663 1 20080317 A 2913 PUMP AIRBUS 300 A300B4605R 3930308 EU HYD SYSTEM INOPERATIVE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 70073 516 JFK INFLIGHT T1881/17MAR - CREW REPORTED LOSS OF YELLOW HYDRAULIC SYSTEM DURING CLIMB. RETURNED TO JFK AND LANDED WITH OUT INCIDENT. REPLACED NUMBER TWO ENGINE YELLOW SYSTEM HYDRAULIC PUMP AND CASE DRAIN FILTER. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A35EU 2008040900033 20080409 00033 NM 2008 4 9 AALA200800664 1 20080317 A 7700 SENSOR BOEING 757 757223 1384957 NM LT ENGINE FAULTED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 608AA 27446 LAX INFLIGHT T297/17MAR - CREW REPORTED LEFT ENGINE BLEED LIGHT ILLUMINATED WITH LEFT ENGINE PACK OFF INDICATION. RETU RNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED COMPRESSOR OUTLET SENSOR ON LEFT PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900034 20080409 00034 NM 2008 4 9 AALA200800650 1 20080316 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 914AN 29515 DFW - EMERGENCY LIGHTS AT SEAT ROWS 12D TO 14D AND OVERWING HATCH INOPERATIVE. REPLACED BATTERY PACK M1695 FOR EMERGENC Y LIGHTS AT SEAT ROWS 12D TO 14D AND OVERWING HATCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008040900036 20080409 00036 WP 2008 4 9 AALA200800645 1 20080315 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 489AA 49682 LGA - EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS SECTION INOPERATIVE. REPLACED BATTERY PACK B5 23 FOR EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008040900039 20080409 00039 NM 2008 4 9 AALA200800658 1 20080316 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 DFW - EMERGENCY LIGHT AT SEAT 26G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900052 20080409 00052 WP 2008 4 9 AALA200800640 1 20080314 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 591AA 53254 SEA - EMERGENCY LIGHTS IN TAIL CONE COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK B5 28 FOR EMERGENCY LIGHTS IN TAIL C ONE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008040900053 20080409 00053 WP 2008 4 9 AALA200800642 1 20080314 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 582AA 53159 LGA - EMERGENCY LIGHT AT OVERHEAD FLIGHT ATTENDANT SEAT BY VENTRAL DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD FLIGHT ATTENDANT SEAT BY VENTRAL DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008040900054 20080409 00054 EU 2008 4 9 AALA200800643 1 20080315 A 3350 SWITCH AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80084 675 MIA - EMERGENCY LIGHT AT SEAT ROW 29 TO AFT GALLEY INOPERATIVE. REPLACED SWITCH ON ARM TO RECHARGE BATTERY FOR EMERGENC Y LIGHT AT SEAT ROW 29 TO AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008040900057 20080409 00057 WP 2008 4 9 AALA200800662 1 20080317 A 2613 GASKET DOUG DC9 DC982 3022082 WP THERMOSTAT BLOWN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 485AA 49678 PBI INFLIGHT T862/17MAR - CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE INDICATION. RETURNED TO PBI AND LANDED WITHOU T INCIDENT. FOUND THE LEFT HAND PACK HIGH THERMOSTAT GASKET BLOWN. REPLACED THERMOSTAT, GASKET AND RIGHT PACK TEMPERAT URE CONTROL VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008040900061 20080409 00061 NM 2008 4 9 P5CA0801552 1 20080326 A 3600 80217010 RELIEF VALVE BOEING 747 74746NF 13848BT NM WRONG PART A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 452PA 30810 RETURN TO BLOCKS DUE TO "BLD 1 OVHT/PRV" EICAS MESSAGE. FINDING THAT THE INCORRECT PRV VALVE WAS DELIVERED, MAINTENANCE SWAPPED THE NR 3 HPSOV WITH NR 1 PRV AND THEN DEFERRED THE NR 3 HPSOV, PER MM 36-11-00. 2 L 7 4 4F RT A20WE 2008040900065 20080409 00065 NE 2008 4 9 HALA0800491 2 20080403 A 7230 FAN BLADE BOEING 767 7673G5 1385126 NM PWA 4060 PW4060 52119 NE LT ENGINE DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, LT ENGINE FAN BLADE HAS NICK ON NR 22 BLADE. BLENDED FAN BLADE PER AMM TASK 72-31-02. EDDY C URRENT. NO IND NOTED. OK TO CONTINUE. FAN BLADE WITHIN LIMITS OF AMM 72-31-02. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040900072 20080409 00072 EU 2008 4 9 08FDEA01272 1 20080403 A 2750 FLAP SYSTEM AIRBUS 310 A310222 3930315 EU TE FLAPS MALFUNCTIONED A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 25 455FE 331 WHEN SELECTED FLAPS 15 ON APPROACH SFPI SHOWED FLAPS LIGHT AND FLAPS WOULD NOT EXTEND, RE-CYCLED FLAPS AND ON SECOND ATT EMPT FLAPS EXTENDS NORMALLY. PERFORMED WIRING CHECK HIGH SPEED SOL V/V, ENABLE V/V AND RETRACT SOL V/V ALL RESISTANCE V ALUE WITHIN LIMIT. CHECKED BOTH TORQUE LIMIT ARE NO FAULTS NOTED, ALL SCREW JACK TORQUE LIMITER NO JAM NOTED. RAN NR 2 ENG AGAIN AND FLAP/SLAT SYS OPS CHECKED ALL IND SYS WORKS OK. CARRIED OUT BITE CHK OF SFCC NR1/NR 2, NO FAULT NOTED PE R AMM 27-50-00-0/5, JRH CHAP 5. 2 L 7 2 4F RT A35EU 2008040900073 20080409 00073 WP 2008 4 9 IXXA08SMN090S 1 20080226 A 5340 FITTING DOUG DC8 DC871F 302199D WP BS 70 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 5 TRACK NUT BARRIER FITTING CRACKED AT STATION 70 .000. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED MAGNETIC PARTICLE INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 51-3-0, DC8 SRM 51-3-1, DC8 SRM 51 -3-0, ATI REPAIR SPECIFICATION 2003-05, DRAWING DOUGLAS 3774645, NDT SPM PARA 07-00-02/07, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008040400161 20080404 00161 NM 2008 4 4 DLM90080465 1 20080317 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 1145-1153 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 97331 53392 FOUND CABIN SEAT TRACK RBL 22 OUT OF LIMITS FS 1145-1153. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01 FIG 6 VOL 1. 2 L 7 2 4F RT A6WE 2008040400166 20080404 00166 NM 2008 4 4 DLM88080473 1 20080402 A 5347 SEAT TRACK DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, BLEND OUT IS OUT OF LIMIT ON SEAT TRACK X=22 STA Y732. SEAT TRACK WAS REPAIRED IAW SRM 53-05 FIG 4A. 2 L 7 2 4F RT A6WE 2008040400174 20080404 00174 NM 2008 4 4 DLM88080481 1 20080402 A 5315 FLOORBEAM DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV EXFOLIATION CORROSION WAS FOUND ON FLOOR PANEL SUPPORT STA Y=255 X=34 FWD WET AREA. FLOOR SUPPORT WAS REPLAC ED IAW DOUGLAS DWG 5930544. 2 L 7 2 4F RT A6WE 2008040400184 20080404 00184 NM 2008 4 4 DLM88080491 1 20080402 A 5320 SUPPORT DOUG MD88 MD88 3023688 NM MLG DOOR FRAME CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV A BROKEN OBD SUPPORT WAS FOUND AT LT MLG FWD DOOR JAMB. SUPPORT WAS REPLACED IAW DOUGLAS DWG 5930516. 2 L 7 2 4F RT A6WE 2008040400194 20080404 00194 NM 2008 4 4 DLM88080501 1 20080402 A 5310 BEAM DOUG MD88 MD88 3023688 NM DOOR FRAME CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, GALVANIC CORROSION WAS FOUND ON C2 DOOR JAMB UPPER BEAM STA Y=684 TO 694. DOOR JAMB BEAM WAS REPLACED IAW D OUGLAS DWG 5936072. 2 L 7 2 4F RT A6WE 2008040700001 20080407 00001 NE 2008 4 7 492AE0278 2 20080326 A 7200 ENGINE UROCOP EC135 EC135P2 5620027 EU PWA PW206 PW206A NE NR 1 MALFUNCTIONED E E3MA O OTHER A FLAME/FIRE NR NOT REPORTED 1 EA 03 492AE 0278 BJ0101 AFTER A NORMAL SHUT DOWN NR 1 ENGINE RESTARTED ON ITS OWN AFTER ALL POWER AND SWITCHES WERE IN THE OFF POSITION. AFTER INSPECTING THE ENGINE, FOUND MANY POWER TURBINE BLADES MELTED. THIS ENGINE JUST CAME BACK 30.4 HOURS AGO AT OVERHAUL FA CILITY. THE ENGINE IS A PW206B, I COULD NOT FIND THAT IN THE ABOVE SERIAL NUMBER SECTION 1 G 7 2 3U 3 U H88EU E42NE 2008040700004 20080407 00004 NM 2008 4 7 AALA200800601 1 20080312 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AA 24617 DFW - EMERGENCY LIGHT AT AFT SEAT 9D HAS A BROKEN BACK PLATE. REPLACED BACK PLATE FOR EMERGENCY LIGHT AT AFT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040700012 20080407 00012 NM 2008 4 7 AALA200800619 1 20080312 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 794AN 30256 DFW - EMERGENCY EXIT LIGHT AT LEFT NUMBER ONE COAT CLOSET HAS BROKEN LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY FOR EMERGE NCY LIGHT AT LEFT NUMBER ONE COAT CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040700023 20080407 00023 SO 2008 4 7 SIMA200809301 1 20080331 A 2120 UNKNOWN EMB 145 EMB145 3260210 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 613AE 145081 ON FLIGHT 4227 - DURING CRUISE, CREW REPORTED A STRONG ELECTRICAL ODOR AT FL280. THE F/A NOTED THE ODOR AS SHE APPROACH ED THE COCKPIT DOOR. ODOR DISSIPATED SHORTLY BEFORE THE APPROACH TO DSM. AIRCRAFT REMOVED FROM SERVICE. PERFORMED INS PECTION OF COCKPIT AND FORWARD AVIONICS. NO DEFECTS NOTED IAW AMM 06-41-02, 30-42-03 AND 20-17-03. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F RT T00011AT 2008040700049 20080407 00049 NM 2008 4 7 DLM88080527 1 20080403 A 5230 PAN DOUG MD88 MD88 3023688 NM FWD CARGO DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, A CRACK WAS FOUND ON FWD CARGO COMPARTMENT DOOR OUTBD PAN WAS REPAIRED IAW SRM 52-03D FIG 10. 2 L 7 2 4F RT A6WE 2008040700056 20080407 00056 NE 2008 4 7 HALA0800472 2 20080331 A 7230 BLADE BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE RT ENG FAN DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, RT ENG FAN BLADE 25 HAS NICK. REPAIRED PER AMM TSK 72-31-02, EDDY CURRENT GOOD. EDDY CURRENT CHECKED. NO CRACKS IND NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040800005 20080408 00005 EU 2008 4 8 08FDEA01247 1 20080402 A 5754 A57840120200 PAN AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 INNER PAN OF SLAT NR 1 FOLDING NOSE IS CRACKED REPAIR PERFORMED BY REPLACEMENT OF PART IAW SB A300-57-6067. 2 L 7 2 4F RT A35EU 2008040800028 20080408 00028 EA 2008 4 8 COMA0860189 1 20080323 A 5320 601R31101157SA FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 934CA 33024 7042 FLOOR SUPPORT CLIP CRACKED AT FS 280 RBL 9.00 INBOARD. REPLACED BRACKET IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 2008040800052 20080408 00052 SO 2008 4 8 FDKA200803131 1 20080324 A 5320 14520609007 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 RIGHT OUTBOARD FLOOR SILL AT FRAME 29 TO 35 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED FLOOR SILL. 2 L 7 2 4T RT T00011AT 2008040800068 20080408 00068 NM 2008 4 8 HNAA0800118 1 20080321 A 2612 TDH60505000 RELAY DHAV DHC8 DHC8102 2809003 NM FIRE DETECTION FAULTY A HNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 07 826EX 31153 31153 389 AFTER AIRCRAFT WAS PUSHED BACK FROM GATE AND APU SHUT DOWN, 'CHECK FIRE DETECT' WARNING LIGHT ILLUMINATED AND FAULT LIGH T ON APU FIRE DETECT PANEL ILLUMINATED. AIRCRAFT WAS RETURNED TO GATE WHERE MAINTENANCE INSPECTED SYSTEM. NO DEFECTS W ERE NOTED AROUND THE FIRE DETECTION LINE OR FIRE BOTTLE. FIRE BOTTLE WAS NOTED AS BEING CHARGED. RELAY 2622-K3 WAS CHA NGED ALONG WITH THE WARNING CONTROL BOX. OPS CHECKS WERE GOOD AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 2008040800076 20080408 00076 SO 2008 4 8 FDKA200803136 1 20080327 A 5610 WINDOW EMB 145 EMB145LR 3260212 SO COCKPIT OBSTRUCTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 829MJ 145228 FDM 6070 MCO-FLL (1229 PHX LCL). CAPT'S DV WINDOW DIFFICULT TO CLOSE. MX INSPECTED AND FOUND DEBRIS IN TRACK OF WINDOW . REMOVED DEBRIS AND OPS GOOD. 2 L 7 2 4T RT T00011AT 2008040800081 20080408 00081 GL 2008 4 8 C2XA08CL039 2 20080326 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 MALFUNCTIONED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 22971 145149 CAE311683 CLE FLIGHT 2890 - THE CREW REPORTED ENGINE NR 2 CAUSING SMOKE SMELL IN THE CABIN. MAINTENANCE INSPECTED AND REPLACED TH E NR 2 ENGINE. OPERATIONAL CHECKS WERE GOOD. SUPPLEMENT TO FOLLOW. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008040800086 20080408 00086 NM 2008 4 8 HNAA0800121 1 20080330 A 2910 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM LT WING CRACKED A HNAA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 EA 07 906HA 59393 59393 009 ON TAXI OUT LOST HYDRAULIC QTY ON NR 2 SYSTEM WENT DOWN TO .6 QTS. RETURNED TO GATE. UPON INVESTIGATION FOUND LEFT OUT BOARD SPOILER ACTUATOR LINE LEAKING, MECHANICS INSTALLED A TEMP FLEX LINE. GROUND RAN AIRCRAFT, LEAK CHECK GOOD. SERVI CED NR 2 HYDRAULIC SYSTEM AS REQUIRED. 2 H 7 2 4T RT A13NM 2008040800091 20080408 00091 EA 2008 4 8 COMA0860198 1 20080328 A 2421 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE FAILED A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 487CA 29655 7729 FLIGHT 5431 - TAKEOFF ABORTED FOR NR 1 IDG CAUTION MESSAGE DURING TAKEOFF. REMOVED AND REPLACED NR 1 IDG. 2 L 7 2 4F RT A21EA 2008040800136 20080408 00136 NM 2008 4 8 SWAA081770 1 20080401 A 3350 MS155721 LIGHT BOEING 737 737317 138447P NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008040800144 20080408 00144 SO 2008 4 8 C2XA08SH055 1 20080403 A 5320 14532636401 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12172 14500864 SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 24. MAINTENANCE REMOVED THE CORROSION A ND PERFORMED A DOUBLER REPAIR IAW EXPRESSJET EC5320-01404. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008040800156 20080408 00156 NM 2008 4 8 SWAA081781 1 20080402 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 644SW 28329 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER SRM. 2 L 7 2 4F RT A16WE 2008040800162 20080408 00162 SO 2008 4 8 C2XA08RI043 1 20080330 A 2131 912R0201 CONTROLLER EMB 145 EMB145XR 3260214 SO CABIN PRESSURE ERRATIC A C2XA K NONE O OTHER DE DESCENT 1 SW 27 24103 145645 FLIGHT 1245 - EWR - CREW REPORTED CABIN PRESSURE WOULD NOT DESCENT UNTIL CABIN IS WITHIN 700 FEET OF AIRCRAFT ALTITUDE. CREW TRIED TO USE "MAN" MODE BUT IT DID NOT WORK, "AUTO" MODE DID NOT WORK. THE CABIN PRESSURE DID WHAT IT WANTED REGA RDLESS OF CREW INPUT. WHEN CREW SWITCHED TO "MAN" CABIN ALTITUDE INITIALLY CLIMBED AT 3000 FPM. IT THEN BECAME UNRESPO NSIVE AND KEPT THE CABIN ALTITUDE 700 FEET BELOW AIRCRAFT ALTITUDE. CREW LANDED AIRCRAFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED MANUAL PRESS CONT IAW EMB145XR AMM 21-31-02 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APP ROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2008040800169 20080408 00169 2008 4 8 SWAA081792 4 20080403 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 260WN 32518 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008040800189 20080408 00189 SO 2008 4 8 C2XA08ON110 1 20080401 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18556 14077 14077 145595 FLT 444 - SAN - WHILE PERFORMING SERVICE CHECK MX PERSONNEL FOUND AISLE 1 EMERGENCY LIGHTING AND LT FWD EXTERNAL EMERGEN CY LIGHTING INOP. MX PERSONNEL REMOVED AND REPLACED NR 1 BATTERY POWER SUPPLY ASSY, OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008040800196 20080408 00196 SO 2008 4 8 C2XA08TY042 1 20080404 A 3350 744436 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27962 145110 RIGHT EMERGENCY EXIT DOOR LIGHT STRIP INOP. REMOVED AND REPLACED LIGHT STRIP IAW EMB 145 AMM 33-50-13, OPS CK GOOD. AI RCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008040800200 20080408 00200 SO 2008 4 8 C2XA08SH060 1 20080407 A 5320 14532363401 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12136 145719 SHV - DURING C-CHECK LT OMEGA BEAM AT PREVIOUS REPAIR BETWEEN FR 24-25 IS CORRODED. MX REMOVED AND REPLACED LT PREVIOUS REPAIR BETWEEN FR 24-25 IAW EMB 145 XR SRM 53-00-10 ITEM 3. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008040800202 20080408 00202 NM 2008 4 8 SWAA081814 1 20080404 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 200WN 32482 DURING SCHEDULED HC1 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008040800209 20080408 00209 NM 2008 4 8 SWAA081829 1 20080402 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008040800214 20080408 00214 NM 2008 4 8 SWAA081821 1 20080406 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 EEPLS END CAP LOOSE AT ROW 1 ABC. SECURED END CAP PER MM. 2 L 7 2 4F RT A16WE 2008040900003 20080409 00003 CE 2008 4 9 EPUA33108 1 20080331 A 5330 SKIN BEECH 1900 1900C 1154161 CE BS 523-531 CORRODED E EPUA K NONE O OTHER IN INSP/MAINT 1 AL 03 1553C UC24 DURING ROUTINE CAMP UNDERFLOOR INSPECTION, DISCOVERED CORROSION ON SKIN AND BETWEEN SKIN AND DOUBLER AT FS 523 TO FS 531 . A REPLACEMENT SKIN APPROX 18 INCH BY 30 INCH WAS FABRICATED AND INSTALLED IN ACCORDANCE WITH THE BEECH SRM AND AIRCRA FT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 2008040900016 20080409 00016 SO 2008 4 9 CHQA200800067 1 20080330 A 2150 BWT138003 NOISE ATTENUATOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 ACM MELTED A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 575RP 145847 CAE311168 FLIGHT 6380, STL TO CVG - AFTER LEVELING OFF AT FL230, THE FLIGHT CREW NOTICED AN ELECTRICAL BURNING ODOR IN THE FLIGHT DECK. THE AIRCRAFT DIVERTED TO IND AND LANDED WITHOUT INCIDENT. DURING ENGINE RUNS, MAINTENANCE WAS ABLE TO DUPLICATE THE SMELL AND INSPECTED THE RECIRCULATION FANS AND DUCTING FOR DEFECTS BUT FOUND NONE. THE NR 2 PACK WAS THEN IDENTIFIE D AS PRODUCING THE ODOR WHILE RUNNING. AFTER INSPECTING THE NR 2 PACK, THE ATTENUATOR DUCT NEAR THE FORWARD RECIRCULATI ON FAN WAS FOUND BLOWN AND APPEARED TO HAVE MELTED. THE DUCT WAS REPLACED AND THERE WAS NO FURTHER SMELL NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008040900028 20080409 00028 NM 2008 4 9 AALA200800633 1 20080313 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 695AN 26975 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900032 20080409 00032 NM 2008 4 9 AALA200800651 1 20080316 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 914AN 29515 DFW - EMERGENCY LIGHTS AT SEAT ROWS 13C TO 20C AND LEFT EXTERIOR OVERWING INOPERATIVE. REPLACED BATTERY PACK M1670 FOR EMERGENCY LIGHTS AT SEAT 13C TO 20C AND LEFT EXTERIOR OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008040900049 20080409 00049 NM 2008 4 9 AALA200800630 1 20080313 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 659AA 24617 DFW - EMERGENCY LIGHT AT SEAT ROW 24 DEF LENS BROKEN. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 24DEF. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900056 20080409 00056 NM 2008 4 9 AALA200800636 1 20080313 A 2697 FBE1094501 WIRE HARNESS BOEING 757 757223 1384957 NM FIRE WARNING INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 699AN 27051 SJU INFLIGHT T412/13MAR STT TO JFK - CREW REPORTED RIGHT ENGINE FIRE WARNING INTERMITTENT. LANDED SJU WITHOUT INCIDENT. REPLACED RIGHT ENGINE FIRE LOOP HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900059 20080409 00059 WP 2008 4 9 AALA200800638 1 20080314 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 582AA 53159 LGA - EMERGENCY LIGHT IN TAIL CONE COMPARTMENT BY WATER SEPARATORS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN TA IL CONE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008040900064 20080409 00064 NM 2008 4 9 AALA200800655 1 20080316 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 DFW - EMERGENCY LIGHT AT SEAT 40G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 40G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900068 20080409 00068 2008 4 9 HALA0800490 4 20080403 A 2565 101651303 SLIDE BOEING 767 7673G5 1385126 NM L4 DOOR LOOSE A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 L4 DOOR SLIDE PARTIALLY UNPACK. REMOVED AND REPLACED 4L EVAC DOOR SLIDE PER TASK CARD 767-3-205003. 2 L 7 2 4F RT A1NM 2008040900074 20080409 00074 NM 2008 4 9 08FDEA01273 1 20080403 A 5347 A5A70821 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK SEAT TRACK FLANGE BELOW FLOOR PANEL NR 272HF AT STA 5-73, X = -8 HAS EXFOLIATION CORROSION. REPAIRED BY SECTI ONAL REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008040900087 20080409 00087 NM 2008 4 9 HALA0800483 1 20080402 A 4920 APU BOEING 767 7673G5 1385126 NM SHUTDOWN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM, APU AUTO SHUTDOWN AT GATE FAULT LIGHT ILLUMINATED. BITE CHECKED APU ECU. NO DEFECTS NOTED ON ECU. "NORM SHUTDOWN SIG" SHOWN ON LAST ROW. RAN APU, NO DEFECTS NOTED, ON START UP. OK FOR SVC. 2 L 7 2 4F RT A1NM 2008040900089 20080409 00089 NM 2008 4 9 HALA0800485 1 20080402 A 3610 SPRING BOEING 767 76733A 1385209 NM CHECK VALVE BROKEN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, FOUND LT ISOLATION BYPASS CHECK VALVE SPRING BROKEN. REMOVED AND REPLACED LT ISOLATION BYPASS CHECK VALVE PER AMM 36-11-04. OPS AND LEAK CK OK. 2 L 7 2 4F RT A1NM 2008040900091 20080409 00091 EU 2008 4 9 08FDEA01284 1 20080403 A 5755 A57771000004 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 5 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND DELAMINATION ON SPOILER NR 5 RT . DELAMINATION IS OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 276153. 2 L 7 2 4F RT A35EU 2008040900093 20080409 00093 EU 2008 4 9 08FDEA01286 1 20080403 A 5755 A57771000004 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 5 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND DELAMINATION ON SPOILER NR 5 LT . DELAMINATION IS OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 276153. 2 L 7 2 4F RT A35EU 2008040900094 20080409 00094 EU 2008 4 9 08FDEA01287 1 20080403 A 5755 A57771000004 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 3 SPOILER LT DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND DELAMINATION ON SPOILER NR 3 LT . DELAMINATION IS OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 276151. 2 L 7 2 4F RT A35EU 2008040900097 20080409 00097 NM 2008 4 9 08FDEA01291 1 20080403 A 5347 BAC15207927178 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 MAIN CARGO COMPARTMENT, SEAT TRACK CORRODED STA 950B BL 0. REMOVED SEAT TRACK-OUT OF LIMITS BETWEEN STA 890-950C BL 0 IAW SRM 51-30-2 LOCATED AND DRILLED NEW SEAT TRACK IAW SRM ER-01-049 AND 53-10-5 FIG 7. TREATED AND PRIMED PARTS IAW SR M 51-10-2. INSTALLED NEW SEAT TRACK IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008040900102 20080409 00102 2008 4 9 HALA0800498 4 20080405 A 3452 ANTENNA BOEING 717 717200 1383700 NM ATC DAMAGED A HALA O OTHER O OTHER LD LANDING 1 WP 13 481HA 55126 STRUCK BIRD ABOVE CAPTAIN'S SIDE EYEBROW WINDOW ON LANDING. REMOVED AND REPLACED TOP NR 1 ATC ANTENNA PER AMM 34-54-01, OPS CK OKAY. 2 L 7 2 4F TR A6WE 2008040900103 20080409 00103 NM 2008 4 9 HALA0800499 1 20080405 A 5330 SKIN BOEING 767 767332 1382001 NM BS 642 PUNCTURED A HALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 13 598HA 23278 SECTION 43 STATION 642 BETWEEN STRINGERS S-29R AND S-30R PUNCTURE IS APPROX 4" BY 3". REPAIR IN WORK. 2 L 7 2 4F RT A1NM 2008040900105 20080409 00105 EU 2008 4 9 08FDEA01296 1 20080403 A 5730 A5796512000751 FAIRING AIRBUS 310 A310203 3930313 EU ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 NR 5 RIGHT WING FLAP FAIRING OUTER SKIN IS DELAMINATED 5 INCHES AFT OF THE FWD ATTACH POINT. REPAIRED THE DELAMINATION BY REMOVING DAMAGE & APPLYING A WET PAY UP IAW SRM 57-20-35. PAINTED IAW AMM 51-75-10-08. 2 L 7 2 4F RT A35EU 2008040900114 20080409 00114 NM 2008 4 9 AALA200800665 1 20080318 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 JFK - EMERGENCY LIGHT IN CABIN MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900117 20080409 00117 NM 2008 4 9 AALA200800672 1 20080319 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 782AN 30003 JFK - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900118 20080409 00118 EU 2008 4 9 AALA200800674 1 20080319 A 7332 9377M62P03 PRESSURE SWITCH AIRBUS 300 A300B4605R 3930308 EU LT ENGINE INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 14056 463 MIA INFLIGHT T588/19MAR - LEFT ENGINE FUEL CLOG LIGHT ILLUMINATED WITH ALERT. RETURNED TO MIA AND LANDED WITHOUT INCIDE NT. REPLACED NUMBER ONE ENGINE FUEL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008040900119 20080409 00119 WP 2008 4 9 AALA200800675 1 20080319 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7517A 49894 LGA - EMERGENCY LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008040900129 20080409 00129 NM 2008 4 9 DLM88080536 1 20080403 A 5347 SEAT TRACK DOUG MD88 MD88 3023688 NM BS 705 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, BLEND OUT WAS FOUND OUT OF LIMIT ON SEAT TRACK AT STA Y=705 X=22. SEAT TRACK WAS REPAIRED IAW SRM 53-05 FIG 4A. 2 L 7 2 4F RT A6WE 2008040900130 20080409 00130 NM 2008 4 9 DLM88080537 1 20080403 A 5347 SEAT TRACK DOUG MD88 MD88 3023688 NM BS 531 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, A BLEND OUT WAS FOUND OUT OF LIMIT ON SEAT TRACK AT STA Y=531 X=22. SEAT TRACK WAS REPAIRED IAW SRM 53-05 F IG 4A. 2 L 7 2 4F RT A6WE 2008042400152 20080424 00152 EU 2008 4 24 08FDEA01504 1 20080423 A 7160 A2242201523000 COWLING AIRBUS 300 A300F4605R 3930327 EU NR 2 ENGINE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 NR 2 ENGINE INBD FAN COWL IS DENTED. REMOVED DAMAGE, PREPED FOR THE APPLICATION OF FILLER MATERIAL. APPLIED FILLER, CUR ED, SANDED & PREPPED FOR PRIMER. APPLIED PRIMER & PAINTED IAW SRM 54-10-00, 54-20-00 & 51-75-10. 2 L 7 2 4F RT A35EU 2008042400153 20080424 00153 EU 2008 4 24 08FDEA01505 1 20080423 A 7160 A2242201523000 SKIN AIRBUS 300 A300F4605R 3930327 EU FAN COWL DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 NR 2 ENGINE INBD FAN COWL INNER SKIN IS DELAMINATED. REMOVED DAMAGED INNER SKIN AND REPAIRED IAW SRM 54-20-00. RESTOR ED FINISH IAW SRM 54-20-00 & SRM 51-75-10. 2 L 7 2 4F RT A35EU 2008042400154 20080424 00154 EU 2008 4 24 08FDEA01506 1 20080423 A 7160 A2242201523000 SKIN AIRBUS 300 A300F4605R 3930327 EU FAN COWL CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 NR 2 ENGINE INBD FAN COWL INNER SKIN DOUBLER IS WORN AND CHAFED. REMOVED AND REPLACED DAMAGED CHAFE PLATE ITEM 9 IAW SR M 54-02-01 & 54-20-00. RESTORED THE SURFACE FINISH IAW SRM 54-20-00. 2 L 7 2 4F RT A35EU 2008042400155 20080424 00155 EU 2008 4 24 08FDEA01507 1 20080423 A 7830 SKIN AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 NR 2 ENGINE OUTBD T/R CORE COWL SKIN IS PEELING. REPAIRED BY REMOVING THE PEELING WIRE MESH & SEALING THE EDGES IAW CMM 78-32-02; REPAIR NR 13. 2 L 7 2 4F RT A35EU 2008042400162 20080424 00162 EU 2008 4 24 08FDEA01514 1 20080423 A 5753 A5796552500200 PANEL AIRBUS 300 A300F4605R 3930327 EU TE FLAP ERODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 LEFT WING FLAP FAIRING 532 BB LEADING EDGE IS ERODED. REMOVED DAMAGE AND REPAIRED BY APPLYING FIBERGLASS WET LAY UP IAW SRM 57-20-35 & E.A. 6-5720-118496. 2 L 7 2 4F RT A35EU 2008042400163 20080424 00163 EU 2008 4 24 08FDEA01515 1 20080423 A 5753 A5796564000200 FAIRING AIRBUS 300 A300F4605R 3930327 EU TE FLAP ERODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 LEFT WING FLAP FAIRING 535 AB L/E IS ERODED IN 2 AREAS. REMOVED FINISH & DAMAGE AT 2 AREAS TOP & BOTTOM OF THE FAIRING IAW SRM 57-20-35. LAYED UP; BAGGED & CURED REPAIRS IAW SRM 57-20-35. REINSTALLED SEAL PARTIALLY REMOVED TO F.O.M. & RESTORED FINISH IAW SRM 51-75-10. 2 L 7 2 4F RT A35EU 2008042400164 20080424 00164 EU 2008 4 24 08FDEA01516 1 20080423 A 5753 FAIRING AIRBUS 300 A300F4605R 3930327 EU TE FLAP ERODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 LEFT WING FLAP FAIRING 534 AB L/E IS ERODED IN 2 AREAS. REMOVED DAMAGE & LAYED UP REPAIR PLIES & STARTED CURE. COMPLE TED CURE & SANDED. APPLIED ANTI-STATIC COATING; APPLIED FR PRIMER & APPLIED PAINT. 2 L 7 2 4F RT A35EU 2008042400165 20080424 00165 EU 2008 4 24 08FDEA01517 1 20080423 A 5753 A57965660000 FAIRING AIRBUS 300 A300F4605R 3930327 EU TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 LEFT WING FLAP FAIRING 535 AT IS DELAMINATED. REPAIRED BY REMOVING THE DAMAGE & APPLYING A CORE; CLOSING PLIES AND A FI BERGLASS OVERLAY REPAIR IAW SRM 57-20-35. APPLIED THE ANTI-STATIC COATING IAW SRM 51-23-20. APPLIED PORE FILLER & PR IMER IAW SRM 51-75-10. PREPPED & PAINTED THE AREA IAW AMM 51-23-10-0. 2 L 7 2 4F RT A35EU 2008042400171 20080424 00171 EA 2008 4 24 SWIA200819494 1 20080414 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 394-409 DENTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 925SW 7682 FLT 6053 - FOUND DENT ON RIGHT SIDE OF FUSELAGE. REPAIRED RIGHT SIDE OF FUSELAGE BETWEEN STR15R AND STR 16R AND FS 394 AND FS 409 + 16 PER REO 601R-53-00-251. 2 L 7 2 4F RT A21EA 2008042400180 20080424 00180 SO 2008 4 24 SWIA200819501 1 20080420 A 2150 ACM EMB 120 EMB120ER 3260203 SO RIGHT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 07 221SW 120290 FLT 5712 - REPORTED SMOKE IN THE CABIN. REPLACED RIGHT PACK ACM PER MM 21-50-05, P/N 2204540-4, S/N OFF 987R. 2 L 7 2 4T RT A31SO 2008042400185 20080424 00185 EA 2008 4 24 SWIA200819506 1 20080420 A 7603 2100140007 GEARBOX CNDAIR CL600 CL6002B19 1900309 EA THROTTLE CONTROL STUCK A SWIA E ENGINE SHUTDOWN O OTHER AP APPROACH 1 NM 07 910EV 15482 6239 7727 FLT 3921 - LEFT THRUST LEVER WOULD NOT RETURN TO FLIGHT IDLE. REPLACED LEFT ENGINE THROTTLE CONTROL CABLE IAW MM 76-11- 09 AND REPLACED LEFT ENGINE THROTTLE GEARBOX IAW 76-11-17. 2 L 7 2 4F RT A21EA 2008042400188 20080424 00188 SO 2008 4 24 SWIA200819509 1 20080326 A 5330 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 226SW 120296 FRAME 22 LOWER SKIN IS CORRODED, FOUND AT C-CHECK. REPAIRED CORRODED AREA IAW SRM 120 53-00-01 FIGURE 202 PG 214. 2 L 7 2 4T RT A31SO 2008042400190 20080424 00190 EA 2008 4 24 SWIA200819511 1 20080121 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 758SK 10222 COCKPIT FLOOR SUPPORT CRACKED AT LBL 11, FOUND AT C-CHECK. INSTALLED COCKPIT FLOOR SUPPORT REPAIRS PER SRM 51-42-06-001 -001-A01. 2 L 7 2 4F RT A21EA 2008042400195 20080424 00195 NM 2008 4 24 08FDEA01484 1 20080423 A 5320 ANGLE BOEING 727 727232 1384082 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 CORROSION ON WEB TO BODY SKIN ANGLE ON WEB BETWEEN BS 950A TO 950B, RBL 3, WL 139. REMOVED AND REPLACED INTERCOSTAL WEB AND AFT ATTACH CLIP REF 51-30-2 PG 8. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008042400197 20080424 00197 WP 2008 4 24 IXXA08SMN100S 1 20080314 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAP DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD FLAP SKIN UPPER PART DENTED AT STATION XW 114.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-1-21, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57 -7-1 FIGURE 1 ITEM "D", AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008042500002 20080425 00002 NM 2008 4 25 AMTA200800239 1 20080317 A 5270 SWITCH BOEING 737 73783N 13844HI NM CFMINT CFM56 CFM567B27 13046 NE APU DOOR MALFUNCTIONED A AMTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 304TZ 30675 APU MAINT LIGHTS ON. REMOVED AND REPLACED APU AIR INLET DOOR SWITCH REF A MM 49-15-41-4. OPS NORMAL. REMOVED PLACARD. (K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2008042500004 20080425 00004 EU 2008 4 25 USA2008F00001 1 20080221 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 712US 18332 843 1038 THE EMERGENCY LIGHT IN THE FWD CABIN WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY PWR SUPPLY UNIT, FIN10W L, AND BATTERY. OPERATIONALLY CHECKS OK. (K) 2 L 7 2 4F 4 F RT A28NM 2008042500006 20080425 00006 NM 2008 4 25 AMTA200800240 1 20080326 A 4900 APU BOEING 737 73783N 13844HI NM CFMINT CFM56 CFM567B27 13046 NE DAMAGED A AMTA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 304TZ 30675 DURING TAXI OUT, APU MAINT LIGHT ILLUMINATED, RETURNED TO GATE. INSTALLED MISSING HARDWARE AND REPLACED BENT WASHERS. REINSTALLED ACTUATOR ARMS IAW AMM 49-15-31-4. OPS CHECK APU NO MANT MSG NOTICE ON OVERHEAD. CURRENT STATUS SHOWED NO F LIGHT DECK LIGHT WITH MSG 49-1518. (K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2008042500009 20080425 00009 EA 2008 4 25 TRAX200800532 1 20080410 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 AAR - CLIP AT FS 484 LBL 27 CRACKED (MARKED). 2 L 7 2 4F RT A21EA 2008042500015 20080425 00015 NM 2008 4 25 BJNA080201 1 20080228 A 2560 P4010021 BATTERY BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C1 13802 EU FLASHLIGHT DISCHARGED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 43XA 24796 F/A EMERGENCY FLASHLIGHT BATTERY DISCHARGED. REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT BATTERY. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2008042500021 20080425 00021 NM 2008 4 25 ASAA0842817 1 20080413 A 5210 507945272 PIN BOEING 737 7374Q8 138447Q NM L1 DOOR JAMMED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 782AS 47802 1948 25113 L1 FORWARD ENTRY DOOR WAS DIFFICULT TO OPEN. REPLACED GUIDE ARM PIN WHICH WAS FOUND JAMMED. 2 L 7 2 4F RT A16WE 2008042500023 20080425 00023 EU 2008 4 25 COEA0801914 1 20080324 A 5347 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE FUSELAGE DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 914FX 293 FOUND DURING HEAVY CHECK. MAJOR REPAIR. FOUND TOOL DAMAGE (MISDRILLED HOLE) (2) PLACES ON UPPER FLANGE OF LT OB SEAT T RACK AT FLOOR CROSSBEAMS 20 AND 21. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK FROM END AT FRAME 23 TO PREVIOUS LY INSTALLED SPLICE BETWEEN FRAMES 18 AND 19. CUT OUT DAMAGED SECTION OF FLOORBEAMS 20 AND 21 UNDER LT OB SEAT TRACK TO LT OB END. FABRICATED REPAIR SPLICE AND REPLACED THE LT SIDE OF FLOORBEAMS 20 AND 21. SEAT TRACK PN S53375001200, FLO ORBEAM PN S53372411200. WO: 200039, 200040. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008042500032 20080425 00032 NM 2008 4 25 HNAA0800134 1 20080416 A 3242 21565 BRAKE DHAV DHC8 DHC8102 2809003 NM NR 1 SMOKE A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 942HA 163 AFTER LANDING AND TAXI, SMOKE COMING FROM NR 1 BRAKE ASSEMBLY. INSPECTED NR 1 BRAKE ASSEMBLY, NO DEFECTS NOTED AT THIS TIME. OK FOR SERVICE. 2 H 7 2 4T RT A13NM 2008042500037 20080425 00037 SO 2008 4 25 FDKA200804156 1 20080412 A 2120 A/C PACK EMB 145 EMB145LR 3260212 SO A/C BAY MALFUNCTIONED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 844MJ 145481 FDM FLT 5964 BWI-JFK (1749 PHX LCL). AC RETURNED TO FIELD AND DECLARED AN EMERGENCY AFTER RECEIVING SMOKE IN THE COCKPI T. MX PLACED PACK ON MEL. 2 L 7 2 4T RT T00011AT 2008042300293 20080423 00293 NM 2008 4 23 2008UALA02151 1 20080414 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEATS 1J & 4E WRONG PART A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 121UA 29167 SEAT 1J AND 4E (AFT) EEL LIGHT HAS WRONG PART (WITHOUT ARROW). FOUND WRONG PART INSTALLED. REPLACED LIGHT ASSEMBLY WITH CORRECT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300302 20080423 00302 NM 2008 4 23 SWAA081947 1 20080410 A 5754 65C26601 SLAT BOEING 737 7375H4 138449D NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND RIGHT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008042300314 20080423 00314 2008 4 23 SWAA081973 4 20080410 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042300316 20080423 00316 NM 2008 4 23 SWAA081975 1 20080413 A 5755 654645168A SPOILER BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED MV4 CHECK, FOUND LEFT WING NR 3 SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER SRM. 2 L 7 2 4F RT A16WE 2008042300317 20080423 00317 NM 2008 4 23 SWAA081976 1 20080413 A 2910 65C26839 HYDRAULIC LINE BOEING 737 737301 1384611 NM MLG WW KINKED A SWAA D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 SW 29 660SW 23230 AIRTURN BACK - INFLIGHT HYDRAULIC A-SYSTEM LOW PRESSURE LIGHT ILLUMINATED. REMOVED AND REPLACED SUPPLY HOSE TO A-SYSTEM RESERVOIR PER MM. 2 L 7 2 4F RT A16WE 2008042300337 20080423 00337 NM 2008 4 23 SWAA082007 1 20080414 A 5753 6549456 FITTING BOEING 737 7373H4 1384600 NM FLAP TRACK CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED BRDG CHECK, FOUND LEFT WING NR 1 FLAP TRACK AFT SPAR FITTING CORRODED. REMOVED AND REPLACED FITTING PE R SRM. 2 L 7 2 4F RT A16WE 2008042300349 20080423 00349 NM 2008 4 23 SWAA082005 1 20080414 A 5743 115A5211 FITTING BOEING 737 7377AD 1384502 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 798SW 28436 DURING SCHEDULED MV2 CHECK, FOUND RIGHT MLG FWD TRUNNION LUG FITTING CORRODED. REMOVED AND REPLACED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300352 20080423 00352 EA 2008 4 23 MASA200800317 1 20080414 A 5270 DOOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT OUT OF ADJUST A MASA O OTHER J WARNING INDICATION LD LANDING 1 SW 07 916FJ 15016 ASH FLT 2934 PHX-MEM. LEFT FWD EMERGENCY DOOR CAUTION TRANSIENT MESSAGE DURING LANDING. MX CLEANED AND ADJUSTED DOOR. OPS GOOD. 2 L 7 2 4F RT A21EA 2008042300368 20080423 00368 NM 2008 4 23 SWAA082019 1 20080415 A 5751 65C25911 SKIN BOEING 737 7375H4 138449D NM RT AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING AILERON LOWER SURFACE DELAMINATED. REPAIRED AILERON PER SRM. 2 L 7 2 4F RT A16WE 2008042300398 20080423 00398 NM 2008 4 23 SWAA082059 1 20080417 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 22R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2008042300407 20080423 00407 NM 2008 4 23 SWAA082051 1 20080417 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 885, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042400003 20080424 00003 EU 2008 4 24 08FDEA01471 1 20080422 A 4910 A5398943020500 RETAINER AIRBUS 300 A300F4605R 3930327 EU APU BAY BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 APU ACCESS CUTOUT AFT SEAL RETAINER IS BENT AND THE SEAL IS TORN. REMOVED SEAL RETAINER & ANGLE IAW SRM 51-40-21. INSTAL LED ANGLE & RETAINER IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008042400014 20080424 00014 EU 2008 4 24 08FDEA01461 1 20080420 A 5743 A5724244220200 BUSHING AIRBUS 310 A310203 3930313 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 445FE 297 RT MLG RIB 5 FWD BORE ON TRUNNION LUG IS CORRODED ON INSIDE AFTER BUSHING WAS REMOVED. REMOVED LEVEL 1 CORROSION AND RE PAIRED WITH OVERSIZE BUSHINGS IAW FEDEX EA 6-5710-118108, RELEASE DATE 19 MARCH, 2008. 2 L 7 2 4F RT A35EU 2008042400015 20080424 00015 EU 2008 4 24 08FDEA01462 1 20080420 A 5743 R57249121 TRUNNION AIRBUS 310 A310203 3930313 EU ZONE 600 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 445FE 297 RT MLG RIB 5 CENTER TRUNNION LUG FWD FACE HAS 2 GOUGES, 1 IS 3/8 IN WIDE BY 1.25 IN LONG BY .020 DEEP, AND 1 IS .25 I N WIDE BY 1 IN LONG BY .032 DEEP. ACCOMPLISHED REPAIR ON RT MLG TRUNNION LUG IAW FEDEX EA 6- 5710-118108, RELEASE DATE 19 MARCH, 2008. 2 L 7 2 4F RT A35EU 2008042400022 20080424 00022 NM 2008 4 24 2008UALA02162 1 20080412 A 5551 CLEVIS BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 RT HORIZONTAL STABILIZER CENTER SECTION AFT SPAR UPPER CLEVIS FWD AND AFT LUG HAVE EVIDENCE OF CORROSION. SPOTFACED FWD AND AFT FACES OF THE LUGS TO REMOVE CORROSION TO THE FINAL DIMENSION OF 1.110" ON THE FWD LUG AND 1.126 INCH ON THE AFT LUG. REAMED FWD LUG TO THE FINAL DIMENSION OF 1.5312 INCH. ALL WITHIN LIMITS. REPAIRS ACP'D REF SRM 55-10-10. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042400052 20080424 00052 NM 2008 4 24 2008UALA02192 1 20080415 A 3350 FUSE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS BLOWN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 507UA 24743 EEL LIGHTS INOP AT ROW 16 THRU 20. FOUND INVERTER FAULTY, BLOWN FUSE. REPLACED EEL LIGHT INVERTER M10830, BLOWN FUSE IN M10770 EMER LIGHT PWR SUPPLY AND LAMP IN BULLNOSE AT SEAT 14ABC. EEL LIGHTS AT ROW 16-20 AND AISLE LIGHT AT 14ABC. CHECK S OK 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400055 20080424 00055 NE 2008 4 24 2008UALA02196 2 20080415 A 7261 471111171 HEAT EXCHANGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 596UA 28749 726699 LEFT ENGINE OIL LEAK OUT OF LIMITS. LEAK FROM NR 5 DRAIN. FOUND LEAK AT FUEL OIL HEAT EXCHANGER. REMOVED NR 1 ENG FUEL OIL HEAT EXCHANGER AND BYPASS VLV. REPLACED, LEAK CHECKED AND ENGINE RUNS WERE GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400062 20080424 00062 NM 2008 4 24 F3LA200800169 1 20080408 A 2597 087021673 WIRE HARNESS AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE EMERGENCY LIGHT MISSING A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 45 1841 DURING C4 S1 C CHECK INSPECTION REPORTED EMERGENCY LIGHT CONNECTOR MISSING MATE LOCK CAP SEAT ROW 1 HARNESS 350WLI. MAI NTENANCE REPLACED CONNECTOR HARNESS, HARNESS TO BE INSTALLED ON AIRCRAFT IN CONJUNCTION WITH INSTALLATION OF CARPET, SEA TS IN ACCORDANCE WITH WORK CARD CP725-1 ITEM 9601 STEP 4 D 2. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042400071 20080424 00071 NM 2008 4 24 2008UALA02263 1 20080417 A 2612 FIRE LOOP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 2 NACELLE INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 914UA 25381 NR 2 ENG FIRE LOOP 'A' INOPERATIVE. AFTER EXSTENSIVE TROUBLE SHOOTING FOUND FIRE LOOP FAULTY. REPLACED ENGINE NR 2 LOW ER FAN FIRE LOOP DETECTION. SYSTEM TESTED NORMAL IAW MM 26-11-11-401. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042400076 20080424 00076 NM 2008 4 24 2008UALA02268 1 20080418 A 2410 CIRCUIT BREAKER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BATTERY BUSS OPEN A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 590UA 28708 APU GEN DOES NOT TAKE L BUSS AUTOMATICALLY WHEN L GEN TAKEN OFF LINE PER CREW. OUND APU BATTERY BUSS CIRCUT BREAKER OPE N. CLOSED BUSS CIRCUT BREAKER . RERACKED BPCU AND APU ECU. ACCOMPLISHED ENG IDLE RUN. POWER TRANSFER CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400078 20080424 00078 EU 2008 4 24 2008UALA02270 1 20080417 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 440UA 702 DENT IN FUSELAGE, APPROX 4 TO 6 FEET AFT OF AFT CARGO DOOR. DAMAGE IS 54 INCHES AFT FROM LOWER CORNER OF AFT CARGO DOOR AND APPROX 2 INCHES BELOW THAT LEVEL. DAMAGE MEASURES 3 INCHES LONG BY 2 INCHES WIDE AND APPROX .0625 DEEP. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042400081 20080424 00081 2008 4 24 2008UALA02273 4 20080418 A 3400 DISPLAY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NAVIGATION MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 473UA 1469 CAPTAIN'S NAVIGATION DISPLAY IS MALFUNCTIONING. FLIGHT DIVERTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008040900139 20080409 00139 NM 2008 4 9 AALA200800685 1 20080321 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 696AN 26976 JFK - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008040900140 20080409 00140 WP 2008 4 9 AALA200800686 1 20080321 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 274AA 49271 LGA - EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 7 TO 11 INOPERATIVE. REPLACED BATTERY PACK AT ROW 9DEF FOR EMERGENCY LIGHT AT SEAT ROWS 7 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008040900142 20080409 00142 NM 2008 4 9 AALA200800692 1 20080321 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 344AN 33083 LAX - EMERGENCY LIGHTS AT SEAT ROWS 32HJ TO 37HJ INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 3 2HJ TO 37HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008040900147 20080409 00147 EA 2008 4 9 SWIA200819431 1 20080318 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DAMAGED A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 608SK 10252 FLT 4088 - FOUND DAMAGE TO RIGHT NOSE SKIN, RIGHT PITOT TUBE AND RIGHT INBOARD SLAT LEADING EDGE DUE TO BIRD STRIKE. RE PLACE RIGHT PITOT IAW 34-11-01. REPAIRED RIGHT SLAT IAW REO 570-57-42-158. REPAIRED RIGHT NOSE SKIN IAW RE0 670-53-11- 288. 2 L 7 2 4F RT A21EA 2008040900152 20080409 00152 SO 2008 4 9 SWIA200819436 1 20080329 A 3397 CONNECTOR EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 291SW 120318 EMERGENCY LIGHT ON FORWARD CABIN BULKHEAD IS INOP. REPLACED WIRING CONNECTOR ON EXIT SIGN. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2008040900153 20080409 00153 EA 2008 4 9 SWIA200819437 1 20080330 A 3260 SENSOR CNDAIR CL600 CL6002C10 1390015 EA NLG DOOR MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 716SK 10180 FLT 6564 - "NOSE GEAR DOOR OPEN" WARNING MESSAGE AFTER RETRACTING GEAR. ADJUSTED THE GAP ON THE NOSE GEAR DOOR SENSORS IAW CRJ MM 32-61-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008040900158 20080409 00158 NM 2008 4 9 AALA200800673 1 20080319 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 782AN 30003 JFK - EMERGENCY LIGHT AT SEAT 23C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008040900163 20080409 00163 NM 2008 4 9 DLM88080540 1 20080403 A 5320 FLOOR SUPPORT DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, A CRACK SUPPORT WAS FOUND FOR CABIN FLOOR PANEL 465A. SUPPORT WAS REPAIRED IAW ER/A 466354-14. 2 L 7 2 4F RT A6WE 2008040900170 20080409 00170 NM 2008 4 9 DLM88080547 1 20080403 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM BS 541-580 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 958DL 49977 DURING HMV, CORROSION WAS FOUND ON LEFT CUSP WEB BETWEEN STA Y=541 AND 560. CUSP WEB WAS REPAIRED IAW DOUGLAS DWG SG095 30003. 2 L 7 2 4F RT A6WE 2008040900177 20080409 00177 NM 2008 4 9 QXEA20080354 1 20080406 A 6123 CONNECTOR BOMBDR DHC8 DHC8402 1390042 NM AUTOFEATHER SYS LOOSE A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 408QX 4050 BOI- FLIGHT 2385 - ON TAKEOFF, AUTO-FEATHER SYSTEM FAILED TO ARM. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANC E TIGHTENED THE CONNECTOR TO THE CONFIG MODULE 9811-J5003. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008040900178 20080409 00178 NM 2008 4 9 QXEA20080356 1 20080406 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM MAIN PAX STIFF A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 408QX 4050 SEA - AFT PASSENGER DOOR HARD TO OPEN. MAINTENANCE CLEANED AND LUBED THE DOOR. OPERATIONAL CHECKS GOOD. NO DEFECTS NO TED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008040900179 20080409 00179 NM 2008 4 9 QXEA20080341 1 20080330 A 6123 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM PROPELLER MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 430QX 4163 YYJ - FLIGHT 2079 - ON TAKEOFF, AUTOFEATHER SYSTEM FAILED TO ARM. ABORTED TAKEOFF AT 80 KNOTS AND RETURNED TO THE GATE. MAINTENANCE FOUND FAULT CODE 941 IN THE SYSTEM AND CLEARED THE CODE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SE RVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008040900192 20080409 00192 NM 2008 4 9 2008UALA01858 1 20080401 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1440 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 AFT PIT LT SIDE FRAME INBOARD FLANGE IS DENTED AT BS 1440 ABOVE STR 26L. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGE. HFE C INSPECTED. NO CRACKS NOTED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008040900194 20080409 00194 NM 2008 4 9 HALA0800502 1 20080406 A 7997 CONNECTOR BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE OIL QTY LOOSE A HALA O OTHER O OTHER DE DESCENT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, "RIGHT ENGINE OIL QTY DOWN TO 8 QTS LEFT AT 16 QTS. WENT TO ENGINE AFTER SHUTDOWN, VISUALLY I NSPECTED FOR LEAKS, NONE NOTED. VISUALLY CKD QTY ADDED 2 PINTS. CREW SAID QTY DROPPED AT TOP OF DESCENT AND CAME BACK UP. CKD QTY CONNECTOR, FOUND TO BE LOOSE. REMOVED CONN AND CLEANED. REINSTALLED SAME. EICAC OIL QTY 23, NOTIFIED MX CTL. NO HISTORY, AMM79-31-00, OK FOR SERVCE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040900196 20080409 00196 NM 2008 4 9 HALA0800505 1 20080405 A 5510 STRUCTURE BOEING 767 767332 1382001 NM HORIZONTAL STAB DAMAGED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 596HA 23276 LIGHTNING STRIKE ON LT HORIZ STAB O/B TIP T/E BY STATIC WICK. OK TO CONTINUE PER M105-596086. 2 L 7 2 4F RT A1NM 2008042400097 20080424 00097 NM 2008 4 24 DLM88080598 1 20080416 A 4940 A400G1 RELAY DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE APU STUCK A DALA H DEACTIVATE SYST/CIRCUITS H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 SO 27 920DE 27371 P80210 53423 P80210 OUTBOUND CREW OF FLT 782 CALLED MTC TO REPORT CLOCKS INOP. MX FOUND THE MAIN BATTERY CHARGER INOP AND BATTERIES LOW. R EPLACED CHARGER AND BATTERIES AND CLEARED ITEM. WHEN CREW NEXT ATTEMPTED TO START APU THEY HAD A FAULT LIGHT AND ECU FA ULTED THE STARTER MOTOR. MTC INVESTIGATED AND FOUND STARTER MOTOR SHOWED SIGNS OF ELECTRICAL OVERHEAT AND DAMAGED. ELE CTRICAL HARNESS FOR STARTER AND APU GEN ALSO DAMAGED. REPLACED APU ASSY PER M/M. REPLACED R2-63 RELAY PER M/M MCO/PLAC REMOVED. 2 L 7 2 4F 4 F RT A6WE E9NE 2008042400098 20080424 00098 NM 2008 4 24 DLM88080600 1 20080416 A 3397 MS25226103 BUSS BAR DOUG MD88 MD88 3023688 NM EMERGENCY LIGHTS MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 909DL 49540 CEILING EMERGENCY LIGHTS AT LT 3B 4B 10C AND 10D INOP. REPLACED POWER SUPPLY, NO HELP FOUND BUS BAR MISSING REPLACED SA ME. 2 L 7 2 4F RT A6WE 2008042400109 20080424 00109 NM 2008 4 24 DL757080617 1 20080420 A 3510 HOSE BOEING 757 75726D 1384907 NM COCKPIT OXYGEN RUPTURED A DALA O OTHER O OTHER CR CRUISE 1 SO 27 900PC 28446 IRR ON DESCENT CAPTS O2 DEVELOPED A LEAK, MILD POP HEARD FOLLOWED BY HISSING UNTIL O2 DEPLETION. FOUND CAPTS O2 MASK BO X SUPPLY LINE HOSE RUPTURED. REPLACED SAME LEAK CHECK OK. 2 L 7 2 4F RT A2NM 2008042400145 20080424 00145 EU 2008 4 24 08FDEA01497 1 20080423 A 5320 A7557557100200 PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 AFT CARGO PANEL 151 PW IS CRACKED IN 3 PLACES. REMOVED DAMAGE, STOPPED DRILLED THE CRACKS & PREPPED AREA FOR REPAIRS TO BE LAYED UP, 3 EA FIBERGLASS WET LAY UP REPAIRS & APPLIED THE FINISH COAT IAW DWG SRZ 25-013. 2 L 7 2 4F RT A35EU 2008042400147 20080424 00147 EU 2008 4 24 08FDEA01499 1 20080423 A 5753 A579636900000 FAIRING AIRBUS 300 A300F4605R 3930327 EU TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 LEFT WING FLAP FAIRING 536 AB RIGHT SIDE HAS A DENT. REPAIRED THE DENT BY REMOVING THE DAMAGED AREA, POTTING THE CORE, APPLYING A WET LAY UP REPAIR AND REFINISHING THE AREA IAW SRM 57-20-35. 2 L 7 2 4F RT A35EU 2008042400186 20080424 00186 EA 2008 4 24 SWIA200819507 1 20080421 A 3230 750006000 VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG SELECTOR FAILED A SWIA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 07 506CA 7793 FLT 2669 - RECEIVED GEAR DISAGREE ON SHORT FINAL. REPLACED NOSE LANDING GEAR SELECTOR VALVE IAW AMM 32-33-10. OPS CHEC K GOOD. 2 L 7 2 4F RT A21EA 2008042400196 20080424 00196 WP 2008 4 24 IXXA08SMN099S 1 20080314 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAP MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD FLAP SKIN UPPER PART HAS IMPROPER REPAIR AT STATION XW 114.0 00. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, BONDED DOUBLER. BON DED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-1-21, DC8 SRM 57-7-1 FIGURE 1 ITEM "A" AND "L", DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-9 T/R 51-142, 51-1-9A T/R 51-141, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008042500011 20080425 00011 EA 2008 4 25 TRAX200800533 1 20080411 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 EXIT SIGN ABOVE SERVICE DOOR IS BROKEN. 2 L 7 2 4F RT A21EA 2008042500012 20080425 00012 NM 2008 4 25 AMTA200800245 1 20080329 A 2560 BATTERY BOEING 737 73783N 13844HI NM CFMINT CFM56 CFM567B27 13046 NE FLASHLIGHT DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 301TZ 28239 FWD EMERGENCY FLASH LIGHT BATTERY NEEDS REPLACING. REMOVED AND REPLACED FWD EMERGENCY FLASH LIGHT BATTERY IAW AMM 25-64 -00-900-806, OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2008042500048 20080425 00048 NM 2008 4 25 ASAA0852818 1 20080415 A 2160 3989083 MODULATING VALVE BOEING 737 737890 1384527 NM CABIN TEMP DEFECTIVE A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 584AS 2671 2671 35682 CABIN ZONE TEMPERATURE ANNUNCIATED ON MASTER CAUTION PANEL. REPLACED TEMPERATURE TRIM MODULATING VALVE. 2 L 7 2 4F RT A16WE 2008042500049 20080425 00049 SO 2008 4 25 C2XA08ON113 1 20080416 A 2611 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO LAVATORY DIRTY A C2XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 11192 14500936 FLT 982 - ONT - FLIGHT CREW REPORTED LAV SMOKE INDICATION. DECLARED EMERGENCY, LANDED SAFELY WITHOUT INCIDENT. MIX PER SONNEL CLEANED SMOKE DETECTOR OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008042500050 20080425 00050 SO 2008 4 25 C2XA08ON114 1 20080415 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 14907 145468 FLT 444 - MRY - FLIGHT CREW REPORTED BURNING SMELL IN COCKPIT AFTER LANDING. MX COULD NOT DUPLICATE FAULT CAUSING THE S MOKE. OPERATIONALLY CHECKED SATISFACTORY, AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008042500070 20080425 00070 NM 2008 4 25 SWAA082054 1 20080417 A 5344 907822 HINGE FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 DURING SCHEDULED HC1 CHECK, FOUND FWD ENTRY DOOR LOWER HINGE FITTING CRACKED. REMOVED AND REPLACED HINGE FITTING PER SR M. 2 L 7 2 4F RT A16WE 2008042500071 20080425 00071 NM 2008 4 25 SWAA082053 1 20080417 A 5344 907822 HINGE FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 DURING SCHEDULED HC1 CHECK, FOUND FWD ENTRY DOOR UPPER HINGE FITTING CRACKED. REMOVED AND REPLACED HINGE FITTING PER SR M. 2 L 7 2 4F RT A16WE 2008042500080 20080425 00080 EA 2008 4 25 TRAX200800543 1 20080416 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 AFT PRESSURE BULKHEAD CRACKED JUST ABOVE CARGO DOOR TRACK. REPAIRED PER REO 601R-53-61-1541 AND REO 601R-53-61-2599. R EMOVED FASTENERS AS REQUIRED PER REO 601R-53-61-1541. CUT OUT DAMAGED AREA AS SHOWN PER REO 601R-53-61-1541. PERFORMED E T INSPECTION OF REWORKED AREA PER REO 601R-53-61-1541 IAW NDTM 51-20-06. NO DEFECTS NOTED. TOUCHED UP EDGES PER REO 60 1R-53-61-1541. FABRICATED DOUBLERS AND FILLERS PER REO 601R-53-61-1541. PERFORMED ET INSPECTION OF REWORKED WEB IAW C AR 38413 PER CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. OK TO INSTALL REPAIR PARTS PER REO 601R-53-61-1541. JOB COMPLET E. 2 L 7 2 4F RT A21EA 2008040900197 20080409 00197 NM 2008 4 9 HALA0800506 1 20080405 A 5310 STRUCTURE BOEING 767 767332 1382001 NM FUSELAGE DAMAGED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 596HA 23276 LIGHTNING STRIKE AT FUSELAGE STA 143.5 LONG 28R. OK TO CONTINUE PER SRM 53-00-01. 2 L 7 2 4F RT A1NM 2008040900198 20080409 00198 NM 2008 4 9 HALA0800507 1 20080405 A 5310 STRUCTURE BOEING 767 767332 1382001 NM FUSELAGE DAMAGED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 596HA 23276 LIGHTNING STRIKE AT FUSELAGE STA 164.75 LONG 28R. OK TO CONTINUE PER SRM 53-00-01. 2 L 7 2 4F RT A1NM 2008041000009 20080410 00009 EA 2008 4 10 MASA200800262 1 20080326 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 917FJ 15017 ASH 2653 RIC-CLT. ONE FLOOR LEVEL EMERGENCY FLOOD LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2008041000015 20080410 00015 2008 4 10 MASA200800270 4 20080329 A 2561 P0640101 LIFE VEST CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 646BR 7392 ASH FLT 1007 HNL-KOA. INFANT LIFE VEST WAS MISSING. MX INSTALLED A NEW LIFE VEST. 2 L 7 2 4F RT A21EA 2008041000018 20080410 00018 EA 2008 4 10 MASA200800272 1 20080329 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77286 7286 ASH FLT 2849 PHX-YUM. LAV SMOKE DETECTOR WOULD NOT TEST. MX TESTED THE SMOKE DETECTOR WITH NO FAULTS. 2 L 7 2 4F RT A21EA 2008041000022 20080410 00022 NM 2008 4 10 UPS08551948 1 20080329 A 3350 SIGN BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 431UP 25462 INSPECTION TYPE:N/A EMERGENCY EXIT SIGN HAS 4 LAMPS OUT. RELAMPED EMERGENCY EXIT SIGN PER AMM 33-51-01-2. OPS CHECK NO RMAL. 2 L 7 2 4F RT A2NM 2008041000025 20080410 00025 WP 2008 4 10 UPS08851943 1 20080305 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 MAIN CABIN CORROSION ON FLOORBEAM, STA 80 BETWEEN RBL 20 AND RBL 48 (TOP AND BOTTOM). REPAIRED FLOOR BEAM AT STA 80 BETWEEN RBL 20 AND RBL 48 IAW SRM 51-02-00 FIG 1. 2 L 7 4 4F RT 4A25 2008041000029 20080410 00029 EU 2008 4 10 YENA2008026 1 20080322 A 3150 350E053020404 FWC AIRBUS 320 A320232 3930326 EU NR 2 FAULTY A YENA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 564JB 21856 17072 2020 FLT 234, LGB-SLC, AIR RETURN TO LGB, LAND ASAP IN AMBER AFTER TAKEOFF. NO OTHER ABNORMAL INDICATIONS. DUE TO HISTORY O F FAULT T/S PER TSM 21-26-00-810-811 COULD NOT DUPLICATE FAULT. REPLACED SMOKE WARNING RELAY (2WA) PRECAUTIONARY, ALSO DIODE MODULE (1800VD). CHECKED OK. SUSPECT FAULT IN FWC'S. REMOVED AND REPLACED FWC 1 & FWC 2 PER 31-53-34-04 AND 31- 51-00-03, OPS CHECK OK, NO FAULT NOTED. 2 L 7 2 4F RT A28NM 2008041000036 20080410 00036 SO 2008 4 10 RAIA00803028 1 20080329 A 3200 STRUT EMB 145 EMB145LR 3260212 SO LANDING GEAR LOW A RAIA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CE 03 834HK 145269 FLT 7937 IAD - AIR/GROUND FAILURE MESSAGE ON THE EICAS AFTER LIFTOFF. MAINTENANCE SERVICED THE LANDING GEAR STRUTS AND PERFORMED SEVERAL EXTENSION AND RETRACTION OPERATIONAL CHECKS OF THE LANDING GEAR WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008041000039 20080410 00039 2008 4 10 RAIA00803020 4 20080325 A 3422 FLUX DETECTOR EMB 145 EMB145LR 3260212 SO OUT OF ADJUST A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 817HK 145058 FLT 5593 STL - HEADING COMPARE ERROR ON THE EICAS. ERROR OF MORE THAN 7 DEGREES. MAINTENANCE ADJUSTED THE SYSTEM AND P ERFORMED A COMPASS SWING. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008041000040 20080410 00040 SO 2008 4 10 RAIA0803021 1 20080325 A 3297 PIN EMB 145 EMB145EP 3260221 SO WOW CONNECTOR BACKED OUT A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 827HK 145021 FLT 5579 STL - LANDING GEAR AIR/GROUND FAILURE MESSAGE ON THE EICAS. MAINTENANCE INSPECTED THE SYSTEM AND FOUND A PUSH ED PIN ON THE NLG WOW CONNECTOR. AFTER PIN WAS RE-SECURED, AN OPERATIONAL CHECK OF THE SYSTEM WAS PERFORMED WITH NO OTH ER DEFECTS NOTED. 2 L 7 2 4F RT T00011AT 2008041000041 20080410 00041 NM 2008 4 10 08FDEA01319 1 20080406 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK CARGO DOOR LOWER JAMB SPOOL FITTING NR 4 FOUND THIRD LAYER CRACK INDICATION AFTER BORE TO MAXIMUM 0.519". REM OVED AND REPLACED PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041000043 20080410 00043 SO 2008 4 10 RAIA00803023 1 20080326 A 5512 14522634403 CAP EMB 145 EMB145EP 3260221 SO HORIZ STAB DAMAGED A RAIA B A EMER. DESCENT UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 826HK 145016 FLT 5593 STL - AIRCRAFT RECEIVED A LIGHTNING STRIKE IN FLIGHT. MAINTENANCE PERFORMED A LIGHTNING STRIKE INSPECTION IN A CCORDANCE WITH THE AIRCRAFT MANUFACTURERS MAINTENANCE INSTRUCTIONS. FOUND HORIZONTAL STAB END CAP TO HAVE AN EXIT HOLE. MAINTENANCE REMOVED AND REPLACED THE END CAP. 2 L 7 2 4F RT T00011AT 2008041000048 20080410 00048 EU 2008 4 10 08FDEA01324 1 20080407 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT RT MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 741FD 611 IT EXISTS AN OLD RAS/BAE 310/97 FOR A FOLDING NOSE REPAIR ON SLAT NR 1 RT. THE EXISTING REPAIR ARE NOT PERFORMED IAW R AS. REPAIR PERFORMED BY PERFORMING SB A300-57-6067 ON SLAT NR 1 FOLDING NOSE, APPROVED BY EA 6-5742-117181. 2 L 7 2 4F RT A35EU 2008041000050 20080410 00050 EU 2008 4 10 08FDEA01325 1 20080407 A 5414 2210081166 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 CRACKS FOUND ON PYLON NR 2 AFT FAIRING FWD SKIN PANEL REPAIR PERFORMED BY STOP DRILLING THE CRACK AND INSTALLING A DOUBL ER IAW, RAS/ROHR/0162/2008 , APPROVED BY EA 6-5455-115264. 2 L 7 2 4F RT A35EU 2008041000052 20080410 00052 EU 2008 4 10 08FDEA01327 1 20080407 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT LT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND 2 DEEP NICKS ON SLAT NR 1 LT LOWER SKIN, INNER RIB 18. REPAIR PERFORMED BY CUT OUT THE SKIN AND INSTALLING A DOUB LER IAW RAS/FOK/003/2008, APPROVED BY EA 6-5742-114860. 2 L 7 2 4F RT A35EU 2008041000061 20080410 00061 EU 2008 4 10 08FDEA01334 1 20080405 A 5330 A5377816020000 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 EXTERNAL FUSELAGE, FRAME 38, 9 INCHES ABOVE STRINGER 43 RIGHT, SMALL DENT ON RIVET. FOUND DENT TO BE OUT OF LIMITS IAW SRM 53-10-12, REMOVED DAMAGE IAW SRM 53-10-12. FABBED REPAIR PARTS IAW SRM 53-10-12. ALODINED IAW SRM 51-21-10. PRIMED AND PAINTED IAW SRM 51-23-10. INSTALLED REPAIR IAW SRM 53-10-12 & 51-40-21. NDT ACCOMPLISHED PER NTM 51-10-08. NO FUTHER DAMAGE NOTED. 2 L 7 2 4F RT A35EU 2008041000063 20080410 00063 EU 2008 4 10 08FDEA01335 1 20080405 A 5330 A5377816020000 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 EXTERNAL FUSELAGE, FRAME 38, 4 INCHES ABOVE STRINGER 43 RIGHT, SMALL DENT ON RIVET. FOUND DENT TO BE OUT OF LIMITS IAW SRM 53-10-12, FABBED REPAIR DOUBLER AND FILLER IAW SRM 53-10-12. REMOVED DAMAGE IAW SRM 53-10-12. ALODINED IAW SRM 51-21 -10. PRIMED & PAINTED IAW SRM 51-23-10. INSTALLED REPAIR IAW SRM 53-10-12 & 51-40-21. NDT ACCOMPLISHED PER NTM 51-10-08. NO FUTHER DAMAGE NOTED. 2 L 7 2 4F RT A35EU 2008041000065 20080410 00065 NM 2008 4 10 ASAA0852800 1 20080331 A 5210 141A61607 DOOR BOEING 737 737890 1384527 NM L1 STICKS A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 583AS 35681 FLIGHT ATTENDANT REPORTS L1 IS STICKY. COULD NOT DUPLICATE PROBLEM. OPENED & CLOSED L1 DOOR SEVERAL TIMES OPERATES SMO OTHLY. OP CHECKS NORMALLY, OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2008041000077 20080410 00077 EU 2008 4 10 Y2LA200800018 1 20080327 A 5313 STRINGER AIRBUS A319 A319112 3930323 EU FUSELAGE CRACKED A Y2LA K NONE O OTHER IN INSP/MAINT 1 GL 07 501SX 3331 FUSELAGE DAMAGED LOWER SURFACE FORWARD OF THE APU EXHAUST NOZZLE. REMOVED AND REPLACED STRINGER 21 AND STRINGER 19R IAW A319 SRM 51-42-11. REFORMED SKIN, STRINGER 17R, STRINGER 19L AND FRAME 85 IAW A319 SRM 51-26-00. ALSO PERFORMED HFEC IAW A319 NTM MANUAL 51-10-08 ON DAMAGE BETWEEN FRAME 85 AND FRAME 86 ON THE LOWER SURFACE BETWEEN STRINGER 19L TO 17R. NO CRACKS FOUND ON SKIN OR STRINGERS EXCEPT FOR STRINGER 21 WHICH WAS REPLACED AS NOTED ABOVE. 2 L 7 2 4F RT A28NM 2008041000078 20080410 00078 NM 2008 4 10 NSVA2008017 1 20080408 A 5230 HANDLE BOMBDR DHC8 DHC8402 1390042 NM AFT CARGO DOOR UNSECURE A NSVA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 196WQ 4196 ON CLIMB-OUT, CREW GOT AFT DOOR WARNING LIGHT, AIRCRAFT RETURNED TO FIELD. MX CALLED AND VERIFIED HANDLE WASN'T STOWED, RESECURED HANDLE OPS CHECK OK. 2 H 7 2 4T RT A13NM 2008041000081 20080410 00081 NM 2008 4 10 NWAA081426314 1 20080404 A 3397 CONNECTOR BOEING 747 747451 1384940 NM EMERGENCY LIGHTS LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 674US 30269 DURING INSPECTION FLOOR LEVEL ESCAPE PATH LIGHTING FROM ROW 51 TO ROW 61 AIRCRAFT LEFT SIDE WOULD NOT ILLUMINATE. MAINT ENANCE FOUND AN ELECTRICAL CONNECTOR AT ROW 61 THAT HAD COME UNDONE, RECONNECTED AND ALL OPS NORMAL. 2 L 7 4 4F RT A20WE 2008041000083 20080410 00083 EU 2008 4 10 08FDEA01343 1 20080408 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND ON RT WING ELONGATED HOLES DURING INSPECTION IAW SB 29-6058. REPAIR PERFORMED BY OVERSIZING THE HOLES AND BUSH IN STALLATION IAW DRAWING R571-50532 AND SB 29-6058, APPROVED BY TA-SEE53-2008-226024-1 AND EA 6-2910-115253. 2 L 7 2 4F RT A35EU 2008041000090 20080410 00090 NM 2008 4 10 08FDEA01350 1 20080408 A 5347 AEA73256 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK SEAT TRACK FLANGE BELOW FLOOR PANEL 262AF AT STA 1159 TO 1245, X = -8 FOUND CORROSION ON UPPER SURFACE. CORRO DED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041000091 20080410 00091 NM 2008 4 10 08FDEA01351 1 20080408 A 5347 AFA7789539 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 UPON REMOVAL OF MAIN DECK FLOOR PANEL 292BF, FOUND SEAT TRACK AT STA 1831 TO STA 1887, X = -75.5 WITH EXFOLIATION CORROS ION. CORRODED SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJ OR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041000094 20080410 00094 EU 2008 4 10 08FDEA01353 1 20080408 A 5415 A54611024002 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND CORROSION IN PYLON NR 1 REAR ATTACH FITTING REPAIR PERFORMED IAW SB A300-54-6018 (REAM UP THE HOLE, CADMIUM PLATIN G), APPROVED BY EA 6-5451-114851. 2 L 7 2 4F RT A35EU 2008041000102 20080410 00102 EU 2008 4 10 08FDEA01359 1 20080408 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 CENTER ARTICULATING SEAT TRACK FITTING AT FRAME 38.2 IS CRACKED. REMOVED FITTING IAW FEDEX A310 SRM 51-40-21; PARA 7. MATERIAL ID FOR BRACKET 7075-T7351 IAW AIRBUS DWG A53781977 AND A310 SRM 51-31-00. MACHINED A FITTING IAW AIRBUS DWG A53781977. ALODINED AND PRIMED FITTING IAW FEDEX A310 SRM 51-21-10. PAINTED FITTING IAW A310 SRM 51-23-10. LOCATED AN D DRILLED NEW FITTING IAW A310 51-40-44. PART MARKED NEW FITTING IAW FEDEX GMM 7-0-1000; PARA 7-B. INSTALLED NEW FITTI NG IAW A310 SRM 51-40-21; PARA 7. 2 L 7 2 4F RT A35EU 2008041000103 20080410 00103 WP 2008 4 10 NWAA081349935 1 20080331 A 2100 UNKNOWN DOUG DC9 DC931 3022065 WP UNKNOWN A NWAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 01 1332U 47404 AT FL340 FLT CREW CAUGHT CABIN ALTITUDE CLIMBING. UNABLE TO GAIN CONTROL OF THE CABIN CLIMB, CREW REQUESTED A LOWER ALT ITUDE ASSIGNMENT. AIRCRAFT IN GRADUAL DESCENT THE CABIN CLIMB INCREASED TO 1500 FPM. AN EMERGENCY DESCENT WAS THEN INIT IATED. CREW REGAINED CONTROL OF CABIN PRESSURE AT FL 250 AND CONTINUED TO SCHEDULED DESTINATION WITH NO FURTHER SYSTEM P ROBLEMS. PASSENGER MASKS DID NOT DEPLOY. MAX CABIN ALTITUDE REACHED WAS 10,500 FEET. MAINTENANCE DID PERFORM BITE BUT NEITHER PRESSURE CONTROLLER SHOWED ANY EXISTING FAULTS. THE NR 2 CONTROLLER DID HAVE SOME HISTORY OF FAULTS FROM PREVI OUS FLIGHTS. VESSEL LEAK CHECK WAS SATISFACTORY. THE RIGHT AUGMENTATION VALVE, WORN DUCTING, CLAMPS, WIRING FAULTS, AN 2 L 7 2 4F A6WE 2008041000104 20080410 00104 EU 2008 4 10 NWAA081043318 1 20080321 A 2120 UNKNOWN AIRBUS 330 A330323 3930335 EU CABIN SMOKE A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 818NW 0857 SMOKE AND FUMES REPORTED IN FLIGHT ATTENDANT CREW REST AREA (LDMCR) BY FLIGHT ATTENDANT AND CONFIRMED BY PILOT, FOLLOWED COM AND SMOKE AND FUMES SUBSIDED AND LANDING WAS UNEVENTFUL. REPLACED LDMCR HEATER AND TESTED OK, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A46NM 2008041000106 20080410 00106 NM 2008 4 10 SWAA081740 1 20080331 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041000111 20080410 00111 2008 4 10 Q2SA740009 4 20080405 A 3417 HG480C1 CADC BOEING 747 747230B 1384889 NM NR 1 DEFECTIVE A Q2SA J A DUMP FUEL UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 EA 63 740SA 21380 CAPTAIN'S COMPASS AND ALTIMETER INTERMITTENTLY FAILED. ATC NR 1 AND NR 2 FAILED. REPLACED NR 1 CENTRAL AIR DATA COMPUT ER (CADC) IN ACCORDANCE WITH AMM 34-12-01, OPS NORMAL IN ACCORDANCE WITH AMM 34-13-04. ACCOMPLISHED ATC TEST IN ACCORDA NCE WITH AMM 34-53-00. OPERATIONALLY CHECKED COMPASS SYSTEM AND COULD NOT DUPLICATE MALFUNCTION. 2 L 7 4 4F RT A20WE 2008041000116 20080410 00116 NM 2008 4 10 SWAA081749 1 20080329 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED MV1 CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, STR 28R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008042500081 20080425 00081 EA 2008 4 25 TRAX200800544 1 20080416 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 STA 280 FWD SUPPORT ANGLE HAS CORROSION. 2 L 7 2 4F RT A21EA 2008042500093 20080425 00093 SW 2008 4 25 EVCA200804118 1 20080410 A 6330 LINK BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL TRANSMISSION BROKEN E EVCA R AUTOROTATION E VIBRATION/BUFFET NR NOT REPORTED 1 CE 03 89AE 8 45433 FAILURE OF THE LT REAR TRANSMISSION LINK IN FLIGHT. HEARD NOISE AUTOROTATION TO A SAFE LANDING IN FIELD. INVESTIGATION SHOWED THE LINK HAD SEPARATED, TRANS UP STOP HELD. 1 G 7 1 3U 3 U H2SW E1GL 2008042500099 20080425 00099 SO 2008 4 25 C2XA08IA114 1 20080417 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NR 2 MLG INOPERATIVE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 13956 145078 IAH - FLIGHT 2643, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON TAKEOFF. THE AIRCRAFT RETURNED TO IAH WH ERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO MAIN LANDING GEAR AFT DOWN & LOCK PROXI MITY SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008042500102 20080425 00102 NM 2008 4 25 HNAA0800135 1 20080318 A 5753 85410611001 SUPPORT BEAM DHAV DHC8 DHC8102 2809003 NM NR 3 FLAP TRACK DAMAGED A HNAA K NONE A FLAME/FIRE IN INSP/MAINT 1 EA 07 815EX 39914 39914 321 DURING INSPECTION AFTER INFLIGHT FIRE, THE OUTBOARD NR 3 FLAP TRACK SUPPORT BEAM WAS FOUND TO HAVE FIRE DAMAGE. MAINTEN ANCE REPLACED SUPPORT BEAM. 2 H 7 2 4T RT A13NM 2008042500109 20080425 00109 WP 2008 4 25 I5HA041108001 1 20080411 A 2436 153911 VOLT REGULATOR CVAC 580 580 2422806 WP ALLSN 501D 501D13A 03004 GL DC GENERATOR OUT OF ADJUST A I5HA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 GL 25 585P 163 AFTER CLIMB OUT, THE CREW LOST THE NR1 DC GENERATOR. AS A PRECAUTIONARY MEASURE THEY RETURNED TO DEPARTURE FOR MAINT TO CORRECT THE PROBLEM. MAINT RERACKED THE NR1 DC GEN CONTROL PANEL AND PARALLEL THE DC GENERATORS IAW THE MM. THE AC WAS R ETURNED TO SERVICE AND RETURNED WITHOUT FURTHER PROBLEMS. 2 L 7 2 4T 4 T RT E282 2008042500110 20080425 00110 CE 2008 4 25 DJFA040908001 1 20080409 A 3000 LIGHT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL DEICE SYS FAILED E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 23 708LX 7500109 WHILE AC WAS DESCENDING, THE CREW NOTED A BURNING ODOR IN THE COCKPIT. AT THE SAME INSTANCE THE SMELL WAS NOTICED THE LT PANEL CIRCUIT BREAKER TRIPPED, AND THE LT SIDE INSTRUMENT PANEL BACKLIGHTING, AS WELL AS THE STANDBY INSTRUMENT BACKLIG HTING WAS LOST. SINCE THE AC WAS ON FINAL APPROACH FOR THE ATTENDED DESTINATION NO DIVERSION WAS PERFORMED. ONCE ON THE GROUND, MAINT TROUBLESHOT THE CAUSE OF THE SMELL/ TRIPPED CIRCUIT BREAKER TO THE LT WINDSHIELD ICE DETECT LIGHT. IN ADDI TION TO THE SHORTED LIGHT ASSY, THERE WAS A SPLICE ASSY REPLACED FOR PRECAUTION. ALL ASSOCIATED WIRING WAS INSPECTED WIT H NO OTHER DISCREPANCY’S NOTED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008042500114 20080425 00114 CE 2008 4 25 GUUA04050802 1 20080405 A 5210 1295140591 CABLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE DOOR FAILED A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 81556 UE239 FLIGHT: 955, PILOT REPORTED FWD AIRSTAIR DOOR CAMS DO NOT TURNREPLACED FWD BOTTOM AIRSTAIR DOOR CABLE. 2 L 7 2 4T 4 T RT A24CE E26NE 2008042500118 20080425 00118 NM 2008 4 25 CALA0800340 1 20080418 A 5320 141A5410U12 INTERCOSTAL BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24706 28767 PAX CABIN FLOOR STRUCTURE HAS CRACKED INTERCOSTAL BETWEEN STA 312 AND STA 328 AT ABOUT LBL46. REMOVED AND REPLACED INTE RCOSTAL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008042500119 20080425 00119 NM 2008 4 25 CALA0800341 1 20080417 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 RIGHT SIDE FRAME 907 BETWEEN S-8 AND S-9 AC BRACKET HOLE CRACKED. REPAIRED RIGHT FRAME AT STATION 907 BETWEEN S-8 AND S -9 AC BRACKET PER EA5310-04498. 2 L 7 2 4F RT A16WE 2008042500125 20080425 00125 EA 2008 4 25 COMA0860228 1 20080417 A 3234 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG INTERMITTENT A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 597SW 4816 7293 FLIGHT 5662 - ON FINAL APPROACH INTO CVG SELECTED GEAR DOWN AND RECEIVED GEAR DISAGREE WARNING FOR THE NOSE LANDING GEAR . EMERGENCY DECLARED, RAN QRH, CYCLE GEAR HANDLE ALL GEAR SHOWED DOWN AND LOCKED. A/C LANDED SAFELY AT CVG. REMOVED A ND REPLACED NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 2008042500137 20080425 00137 EA 2008 4 25 MASA200800326 1 20080419 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17156 7156 ASH FLT 7083 ORD-BNA. ROW 10 EMERGENCY LIGHTS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2008042500139 20080425 00139 2008 4 25 MASA200800328 4 20080420 A 2562 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA ELT ACTIVATED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 571ML 7209 ASH FLT 7185 IAD-CLE. CREW REPORTED A POSSIBLE LIGHTNING STRIKE AND ELT ON CAUTION MESSAGE WHICH CAME ON IMMEDIATELY AF TER A LIGHTNING FLASH DURING THE FLIGHT. C/W DETAILED LIGHTNING INSPECTION, NO DAMAGE NOTED AND REPLACED THE ELT. 2 L 7 2 4F RT A21EA 2008042500145 20080425 00145 EA 2008 4 25 TRAX200800534 1 20080411 A 5313 STRINGER CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 723EV 10132 STRINGER 25RT CORRODED BETWEEN FS 295 AND FS 310 BLENDED STRINGER AND FOUND TO BE OUT OF LIMITS. REMOVED STRINGER SECTI ON FROM 290 - 310 PER SRM 51-42-06. INSTALLED NEW STRINGER, DRILLED HOLES TO SIZE, INSTALLED AFT FASTENERS FROM SPLICE TO SKIN PATCH PER SRM 51-42-06. INSTALLED FASTENERS INTO STRINGER 25RT FORWARD OF REPAIR DOUBLER IAW CRJ 700 SRM 51-42- 06, SM 7023171 04-12-08, JOB COMPLETE. SUPPLEMENTAL SDR CLOSED 4/21/08. 2 L 7 2 4F RT A21EA 2008042500151 20080425 00151 SO 2008 4 25 FDKA200804168 1 20080417 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 FDM 6025 CVG-CLT (0650 PHX LCL). EMERGENCY PLACARD AT LEFT ROW 12 EMERGENCY EXIT DOES NOT ILLUMINATE. MX RESECURED CON NECTORS ON LIGHT ASSY AND RESET LIGHTING SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008042500153 20080425 00153 SO 2008 4 25 FDKA200804170 1 20080418 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN & COCKPIT SMOKE A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 838MJ 145384 FDM 6095 MCO-MSY (0402 PHX LCL). SMOKE IN COCKPIT AND CABIN. MX RAN ENGINES, PACKS, LIGHTS AND ELECTRICS AND COULD NOT DUPLICATE. 2 L 7 2 4T RT T00011AT 2008042500156 20080425 00156 NM 2008 4 25 2008UALA02310 1 20080419 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT EEL LIGHT INOP, ACROSS DOOR 4 RIGHT LOWER WALL EEL. REPLACED LAMP OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500165 20080425 00165 NM 2008 4 25 2008UALA02312 1 20080419 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT EEL LIGHT INOP, LEFT SIDE LOWER WALL BY LAV 111. SUSPECT FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD.AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500164 20080425 00164 NM 2008 4 25 CALA0800347 1 20080411 A 5311 6546526 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 LEFT SIDE STA 400 BETWEEN S-8 AND AC BRACKET FASTENER HOLE CRACKED. REPAIRED LEFT FRAME 400 BETWEEN S-8 AND S-9 PER EA 5310-04498, OP 02. 2 L 7 2 4F RT A16WE 2008042500166 20080425 00166 NM 2008 4 25 2008UALA02313 1 20080419 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 40 RIGHT. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500176 20080425 00176 NM 2008 4 25 HNAA0800127 1 20080406 A 5210 8SC0156 LIFT STRUT DHAV DHC8 DHC8102 2809003 NM PAX DOOR WORN A HNAA K NONE J WARNING INDICATION CR CRUISE 1 EA 07 934HA 139 PAX DOOR UNLATCHED ITSELF (HANDLE POPPED TO THE FIRST DETENT) FOLLOWED BY PAX DOOR WARNING LIGHT IN FLIGHT COMPARTMENT. F/A LATCHED DOOR AND DOOR REMAINED LATCHED FOR REMAINDER OF FLIGHT. REMOVED AND REPLACED AIRSTAIR DOOR LIFT MECHANISM GAS SPRING AND ADJUSTED DOOR PRESSURE STOPS. 2 H 7 2 4T RT A13NM 2008042500177 20080425 00177 EU 2008 4 25 2008UALA02322 1 20080420 A 3350 321454 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 433UA 589 EMERGENCY LIGHT POWER SUPPLY 13WL SELF-TEST FUNCTION INOP. FOUND EPSU FAILED. REPLACED POWER SUPPLY, OPS CHECKED GOOD . 2 L 7 2 4F 4 F RT A28NM E40NE 2008042500179 20080425 00179 NM 2008 4 25 2008UALA02377 1 20080422 A 2611 SMOKE DETECTOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AFT CARGO BAY INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 AFT CARGO COMPARTMENT LOOP 'A' SMOKE DETECTOR INOPERATIVE. FOUND DETECTOR SCREENS DIRTY. CLEAN ALL AFT PIT SMOKE DETEC TOR SCREENS. TEST OK PER MM 26-16-00. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042500180 20080425 00180 NM 2008 4 25 HNAA0800137 1 20080421 A 2997 WIRE DHAV DHC8 DHC8102 2809003 NM PWA PW121 PW121 52124 NE HYDRAULIC SYS BROKEN A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 815EX 321 121091 AFTER TAKEOFF NR 1 ENGINE HYD PUMP C/L CAME ON AND WOULD NOT RESET, QTY AND PRESS NORMAL. SBY MX MET A/C, FOUND BROKEN WIRE AT HYD PRESSURE SWITCH CONNECTOR. REPAIRED BROKEN WIRE IAW CHAPTER 20 STANDARD MTN PRACTICES. 2 H 7 2 4T 4 T RT A13NM E20NE 2008042500181 20080425 00181 NM 2008 4 25 2008UALA02398 1 20080424 A 5310 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 906 STR 26L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 305UA 23666 FOUND STA 906 STR 26L HAS DAMAGE. INSTALLED REPAIR AT STA 90 6 STR 26L. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042500182 20080425 00182 NM 2008 4 25 ZZDA2008091 1 20080415 A 5514 STRUCTURE BOEING 737 73776N 13844CH NM HORIZ STAB DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 289AT 32673 MDDR 115767T - RT HORIZONTAL STABILIZER HAS DENT AT STA 120. REPAIRED PER B737 SRM 55-10-01 P205 FIG 202. 2 L 7 2 4F RT A16WE 2008042500189 20080425 00189 EU 2008 4 25 2008UALA02324 1 20080418 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 497UA 1847 LWR EMERGENCY LIGHT AT DOOR 1L INOP. FOUND LOOSE CONNECTOR. RESEATED CONNECTOR, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042500190 20080425 00190 NM 2008 4 25 2008UALA02325 1 20080419 A 3510 OXYGEN SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE UNDERSERVICED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 O2 REQUIRES SERVICING. SERVICED OXYGEN BOTTLE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042400107 20080424 00107 NM 2008 4 24 DLM88080610 1 20080415 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM PAX CABIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 960DL 49979 DUE AT HMV ERA 087344-14 CODE 9-53-21-03 REV A REPAIR FOR MAIN CABIN SUBFLOOR CUSP WEB AT STA Y=224 LT. REPAIRED CUSP W EB IAW ERA 087344-14 REV A AS A PERMANENT REPAIR. 2 L 7 2 4F RT A6WE 2008042400111 20080424 00111 NM 2008 4 24 NWAA081716740 1 20080417 A 5320 STRUCTURE BOEING 747 747251F 1384898 NM BS 320 MISREPAIRED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING "L" CHECK WHILE ACCOMPLISHING VERTICAL BEAM INSPECTION FOUND DISCREPANT EXISTING REPAIR DOUBLER COMMON TO THE NOS E WHEEL WELL VERTICAL BEAM WEB AT BS 320 LT BETWEEN WL 180-WL 190. THE EXISTING REPAIR DOUBLER OBSTRUCTS THE SURFACE SC AN HFEC REQUIRED BY INSPECTION. REPAIRED PER EA 67-212651. 2 L 7 4 4F RT A20WE 2008042400115 20080424 00115 SO 2008 4 24 SIMA200811301 1 20080419 A 2597 7277011505 WIRE HARNESS EMB 145 EMB145LR 3260212 SO SEAT PSU 17A DAMAGED A SIMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 658AE 145760 ON FLIGHT 3403 CREW REPORTED SEAT BELT/NO SMOKING SIGN AT 17A IS MISSING AND SPARKS WERE COMING FROM THE WIRES WHERE THE SIGN WAS LOCATED. DEADHEAD CAPT SEPARATED THE WIRES AND THE FLYING CAPT TURNED THE SEATBELT/NO SMOKING SIGN SWITCHES O FF. AIRCRAFT REMOVED FROM SERVICE. ISSUED MEL FOR SEAT BELT SIGN, INSULATED WIRES, REPLACED SEAT BELT SIGN. MEL RESTO RED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008042400130 20080424 00130 NM 2008 4 24 EIA2008018 1 20080419 A 5753 STRUCTURE BOEING 747 747230B 1384889 NM FORE FLAP DAMAGED A EIAA O OTHER O OTHER CL CLIMB 1 NM 09 488EV 23287 AIRCRAFT TOOK BIRDSTRIKE OUT OF JFK, ON BIRDSTRIKE INSP AT DOV FOUND RT OUTBOARD FOREFLAP LEADING EDGE DAMAGE. REMOVED AND REPLACED RIGHT WING OUTBOARD FOREFLAP ASSY IAW MM 27-51-05 2 L 7 4 4F RT A20WE 2008042400176 20080424 00176 EA 2008 4 24 SWIA200819497 1 20080416 A 5210 HANDLE CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 810SK 15093 EXTERIOR MAIN CABIN DOOR HANDLE IS BROKEN. REPLACED EXTERIOR HANDLE ON MAIN CABIN DOOR IAW 52-11-03. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008042400178 20080424 00178 EA 2008 4 24 SWIA200819499 1 20080417 A 3350 RELAY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS FAULTY A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 946SW 7776 FLT 6399 - EMERGENCY LIGHTS ARE ON DURING FLIGHT. INSTALLED A/C ESSENTIAL BUSS SENSE RELAY K1XD AS REQUIRED. 2 L 7 2 4F RT A21EA 2008042500003 20080425 00003 2008 4 25 AMTA200800238 4 20080323 A 3460 1762000101 FMC BOEING 737 73783N 13844HI NM CFMINT CFM56 CFM567B27 13046 NE RT UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 314TZ 16720 16720 30640 SINGLE FMC FAILURE. REMOVED AND REPLACED NEW RT FMC IAW AMM 34-61-02-4. OPS CHECK NORMAL. (K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2008042500017 20080425 00017 EU 2008 4 25 COEA0802703 1 20080319 A 2420 N04063 ALTERNATOR FOKKER F27 F27MK600 4990706 EU RROYCE DART DART5327R 54509 NE LT ENGINE FAILED A COEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 13 703FE 176 10420 RETURN TO BLOCKS. FLT NR7276, DURING TAXI TO THE RUNWAY, THE LT ALTERNATOR FAILED. THE AC RETURNED TO THE RAMP (BLOCKS ) WITHOUT ANY FURTHUR INCIDENT. LT ALTERNATOR WAS REPLACED ON THE LT ENGINE. 2 H 7 2 4T 4 T A817 E297 2008042500019 20080425 00019 NM 2008 4 25 ASAA0852815 1 20080413 A 2150 WARNING SYSTEM BOEING 737 737890 1384527 NM COCKPIT MALFUNCTIONED A ASAA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 NM 02 559AS 35178 LEFTHAND AIRCON PACK ANNUNCIATION. BITE CHECK REVEALED TCV FAULT. RESET FAULT. RETESTED OK.. 2 L 7 2 4F RT A16WE 2008042500038 20080425 00038 GL 2008 4 25 FDKA200804157 2 20080413 A 7200 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 MALFUNCTIONED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 844MJ 14157 145481 CAE311513 FDM FLT 9962 BWI-JFK (0650 PHX LCL). LAV SMOKE WARNING IN FLIGHT WITH SMOKE IN THE CABIN AND FLIGHT DECK. MX REMOVED A ND REPLACED NR 2 ENG, OPS GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008042500047 20080425 00047 SO 2008 4 25 FDKA200804166 1 20080415 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6133 CVG-LIT (0533 PHX LCL). RIGHT ROW 12 EMERGENCY LIGHT INOP. MX RESECURED CONNECTORS. 2 L 7 2 4T RT T00011AT 2008042500079 20080425 00079 EA 2008 4 25 TRAX200800542 1 20080416 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 AFT PRESSURE BULKHEAD CRACKED AT LINTEL FITTING. REPAIRS PERFORMED IN ACCORDANCE WITH REO 601R-53-61-1230. 2 L 7 2 4F RT A21EA 2008042500087 20080425 00087 EU 2008 4 25 TRAX200800554 1 20080416 A 5240 DOOR AEROSP ATR72 ATR72 EU SERVICE DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 SERVICE DOOR WILL NOT CLOSE. 2 H 7 2 4T RT 2008042500124 20080425 00124 EU 2008 4 25 J1Q2008F00002 1 20080329 A 2133 OUTFLOW VALVE AMD FALC20 FALCON 2720302 EU GARRTT TFE731 TFE731* 01518 WP CABIN PRESSURE MALFUNCTIONED E J1QA K NONE O OTHER IN INSP/MAINT 1 GL 15 724JC 310 DURING ROUTINE SERVICING AND CLEANING OF OUTFLOW VALVES, (3) PNEUMATIC LINES WERE FOUND SEVERELY DAMAGED AN FLARES DUE T O OVERTIGHTENING. (2) OF THE LINES, PN MY20721-207 AND MY207212-218, ATTACH TO THE LT OUTFLOW VALVE. THE (3RD) LINE PN MY20721-219 ATTACHES TO THE RT OUTFLOW VALVE. THE AN FLARE ON LINE MY20721-207 HAD WALL THICKNESS REDUCTION AND A SMAL L PIECE MISSING FROM THE FLARE. THE FLARE ON LINE MY20721-218 WAS COMPLETELY DESTROYED WITH THE PIECES OF THE FLARE CON TAINED IN THE B-NUT. THE FLARE ON LINE MY20721-219 HAD WALL THICKNESS REDUCTION AND WAS CRACKED ALMOST COMPLETELY AROUN D AT APPROXIMATELY THE MID POINT OF THE FLARE. RECOMMEND CAREFUL EXAMINATION OF ALL AN AND MS CONNECTIONS AT THE NEXT O 2 L 7 2 4F 4 F A7EU E6WE 2008042500133 20080425 00133 NM 2008 4 25 DXTA200802991 1 20080412 A 3240 50128891 BRAKE ASSY GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE MLG WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 731QS 2207 123 MAIN BRAKES REQUIRE EXCESSIVE PRESSURE ON TOE BRAKES TO SLOW OR STOP ACFT. REMOVED AND REPLACED NR 2 BRAKE REF MM 32-40 -21 REF CMP 324302 COMPLIED WITH BRAKE BLEED AND OPS CHECK REF CMP 324005 AND 324017. 2 L 7 2 4F 4 F RT A53NM E35NE 2008042500147 20080425 00147 EA 2008 4 25 TRAX200800545 1 20080416 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 RIGHT CABIN FLOOR SEAT RAIL STARTING AT FS 394.00 HAS CORROSION DAMAGE. JOB COMPLETE. BLENDED AREAS OF CORROSION START ING AT FS 394.00 TO WITHIN LIMITS & ALODINED BLENDED AREAS PER CRJ 200 SRM 53-21-49SP 7025126 04/18/2008. SUPPLEMENTA L SDR CLOSED 4/21/08. 2 L 7 2 4F RT A21EA 2008042500154 20080425 00154 SO 2008 4 25 FDKA200804171 1 20080418 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6049 JFK-ORF (0423 PHX LCL). SERVICE DOOR EMERGENCY LIGHT INOP. MX RESECURED CONNECTORS ON LIGHT ASSY, OPS CHECK G OOD. 2 L 7 2 4T RT T00011AT 2008042500163 20080425 00163 NM 2008 4 25 2008UALA02311 1 20080419 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT LIGHT INOP, AT DOOR 4 RIGHT BUSTLE LIGHT. REPLACED BUSTLE LIGHT ASSEMBLY. OP CHECKS OK. ACFT OK FOR SER VICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041000117 20080410 00117 NM 2008 4 10 NWAA081456310 1 20080331 A 5311 FRAME BOEING 747 747451 1384940 NM BS 1265 S26L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING "M" CHECK FOUND CRACK IN FRAME WEB AT BS 1265 S26L. REPAIRED PER EA 63-212256 SECTION I. REPETITIVE INSPECTIONS TO BE ACCOMPLISHED AT 2000 CYCLE INTERVALS PER SECTION II UNTIL SECTION III PERMANENT REPAIR IS ACCOMPLISHED. 2 L 7 4 4F RT A20WE 2008041000121 20080410 00121 NM 2008 4 10 SWAA081752 1 20080329 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 480, BL 0. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008041000127 20080410 00127 NM 2008 4 10 SWAA081758 1 20080331 A 5311 6546593 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041000128 20080410 00128 NM 2008 4 10 SWAA081757 1 20080331 A 5311 6546526 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041000132 20080410 00132 NM 2008 4 10 SWAA081747 1 20080329 A 5314 6562125 KEELBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED MV2 CHECK, FOUND RT KEEL BEAM CORRODED AT BS 527, RBL 7. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2008041000136 20080410 00136 EU 2008 4 10 08FDEA01299 1 20080404 A 5311 A5377880420000 FRAME AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FWD LOWER CARGO COMPARTMENT/CORROSION ON FWD FACE OF FRAME 35 BETWEEN STRINGER 43 AND 44. FRAME 35 BETWEEN STR 43 AND 4 4 R CORRODED OUT OF LIMITS IAW A310 SRM 53-10-00. FRAME REPAIRED IAW A310 SRM 53-10-13 FIG 203. MATERIAL ID 2024-0, .0 63 PO NR 597274.1: HEAT TREATED IAW TIMCO TPS 1003 REV A FRAME (PO NR 612789.5). 2 L 7 2 4F RT A35EU 2008041000139 20080410 00139 EU 2008 4 10 08FDEA01341 1 20080408 A 5730 A57240087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND ON LT OUTER WING CORROSION ON SKIN INSIDE AROUND HYDRAULIC FITTING HOLES 3 AND 4. REPAIR PERFORMED BY BLEND OUT C ORROSION, REPAIR IAW. DRAWING R571-50532 AND INSTALLING A RETAINING PLATE IAW RAS/BAE/1006804/2008 ISS A, APPROVED BY EA 6-5720-117167. 2 L 7 2 4F RT A35EU 2008041000140 20080410 00140 NM 2008 4 10 BB08046 1 20080401 A 2710 A2864010 ACTUATOR BOEING 767 7672B7 1385107 NM AILERON FAULTY A USAA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 EA 19 252AU 75758 3994 24765 PHL FLT 799 AMS TO PHL. PILOT REPORTS THAT THE AILERONS WERE BINDING FROM BOTH CAPTAIN'S AND F/O'S CONTROL WHEELS, ON THE GROUND AND IN FLIGHT. MAINTENANCE REPLACED THE LEFT UPPER LATERAL CENTER CONTROL ACTUATOR. OPERATIONALLY CHECKS O K. 2 L 7 2 4F RT A1NM 2008041000143 20080410 00143 EU 2008 4 10 08FDEA01304 1 20080403 A 5230 SKIN AIRBUS 310 A310203 3930313 EU CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FWD CARGO DOOR EXTERNAL SURFACE AFT LWR CORNER GOUGED. DEPTH OF GOUGE WAS .048 FOUND TO BE OUT OF LIMITS IAW SRM 52-30- 00. REMOVED EDGE MEMBER IAW SRM 51-40-21. REMOVED SEAL RETAINER IAW SRM 51-40-21. RECIEVED NEW EDGE MEMBER IAW SRM 52-31 -00. FABBED DOUBLER AND FILLER IAW SRM 52-30-00, INSTALLED DOUBLER & FILLER IAW SRM 51-40-21, INSTALLED EDGE MEMBER & SE AL RETAINER IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008041000148 20080410 00148 WP 2008 4 10 08FDEA01311 1 20080404 A 5740 ARB137935 ATTACH FITTING DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 LEFT WING INBD L/E, NR 1 SLAT TRACK FWD ATTACHMENT TO SLAT TRIM PANEL AFT SUPPORT "C" CHANNEL HAS FASTENERS LOOSE. UP ON FURTHER INVESTIGATION FOUND SIDE BRACKET ON THE SLAT TRACK ATTACHMENT CRACKED. REMOVED CRACKED BRACKET AND INSTALLED A NEW BRACKET REF DC/MD-10 SRM 51-35-01; VOL II. REINSTALLED SLAT TRACK ATTACHMENT REF DC/MD-10 SRM 51-31-01; VOL II. SLAT TRACK COVER TO BE ADJUSTED ON WORK CARD 27X8501. 2 L 7 3 4F RT A22WE 2008041000149 20080410 00149 WP 2008 4 10 IXXA08SMN089S 1 20080215 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING LEADING CENTER LEADING EDGE OUTER SKIN LOWER SHOWS IMPROPER REPAIR A T STATION XFS 385.200. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, FILLERS, INTERNAL SPLICE DOUBLER S EGMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, D C8 SRM 51-3-0, DC8 SRM 51-3-1, FAA FORM 8110-3 NUMBER 08086 DATED 02-27-08, SEMAN DRAWING NUMBER ED-4706 DATED 02-09-08, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008041000152 20080410 00152 WP 2008 4 10 UPS08851949 1 20080229 A 5755 SUPPORT ANGLE DOUG DC8 DC873F 302199F WP SPOILER BENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 SPOILER LANDING SUPPORT FRAME BENT IN LT FLAP WELL I/B SIDE OF STA 98 FLAP HINGE. REMOVED DAMAGE AND FABBED REPAIR ANGLES AND INSTALLED IAW SRM 57-2-0 FIG 2, 51-1-8, 51-1-20D, 51-3-1, 51-1-21. 2 L 7 4 4F RT 4A25 2008041000155 20080410 00155 WP 2008 4 10 UPS08851953 1 20080331 A 3350 LIGHT DOUG DC8 DC873F 302199F WP CABIN INTERMITTENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INTERMITTENT ON OPS CHECK. PERFORMED OPS CHECK OF EMERGENCY LIGHTS REF MM 33- 50-02-2. OPS CHECK. 2 L 7 4 4F RT 4A25 2008041000159 20080410 00159 NM 2008 4 10 AALA200800622 1 20080313 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT AT SEAT 26C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041000160 20080410 00160 NM 2008 4 10 AALA200800623 1 20080314 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT AT SEAT 44C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 44C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041000162 20080410 00162 NM 2008 4 10 AALA200800629 1 20080313 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT AT SEAT 20G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 20G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008042500178 20080425 00178 SO 2008 4 25 C2XA08RI054 1 20080421 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 11536 145520 FLIGHT 2197 - EWR - FLIGHT CREW REPORTED FLOOR EMERGENCY LIGHTS SEAT ROW 17A INOPERATIVE. EWR MX REMOVED AND REPLACED N R 6 INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008042500193 20080425 00193 EA 2008 4 25 TRAX200800560 1 20080418 A 5341 BEARING CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 723EV 10132 RIGHT WING-TO-FUSELAGE ATTACH LINK AT FS 797.00 UPPER SPHERICAL BEARING CRACKED. 2 L 7 2 4F RT A21EA 2008042500195 20080425 00195 EA 2008 4 25 TRAX200800562 1 20080418 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 720EV 10115 PAX ENTRANCE DOOR DIFFICULT TO OPEN. FLT 4188 DEL 31 MINS. 2 L 7 2 4F RT A21EA 2008042500200 20080425 00200 NM 2008 4 25 SWAA082067 1 20080420 A 5314 6547980 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM CORRODED AT BS 540, RBL 6.50. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 2008042500202 20080425 00202 NM 2008 4 25 SWAA082068 1 20080420 A 5320 65C28106 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND RADIAL STIFFENER CRACKED AT BS 1016, 6 0'CLOCK POSITION. REPAIRED STIFFENER PER BOEI NG DRAWING. 2 L 7 2 4F RT A16WE 2008042500214 20080425 00214 2008 4 25 SWAA082120 4 20080420 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 412WN 29818 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042500219 20080425 00219 NM 2008 4 25 SWAA082084 1 20080421 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 763, BETWEEN STR 19L AND STR 22L. REPAIRED SKIN PER SWA E A. 2 L 7 2 4F RT A16WE 2008042500220 20080425 00220 NM 2008 4 25 SWAA082108 1 20080421 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042500223 20080425 00223 NM 2008 4 25 SWAA082109 1 20080421 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULE 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042500224 20080425 00224 NM 2008 4 25 SWAA082085 1 20080418 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 885, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042500238 20080425 00238 NM 2008 4 25 2008UALA02330 1 20080420 A 2600 BOTTLE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 WHILE ACCOMPLISHING EG8515 FOR CARGO PIT FIRE BOTTLE CHECK, NOTICED THAT WHEN DISC SWITCH IS PUSHED THAT VOLTAGE AT SQB CONN SPIKES TO 24.96 VDC FOR A SPLIT SECOND THEN GOES BACK TO APPROX ZERO AND STAYS ZERO UNTIL 20 MINS WHEN IT GOES TO A PPROX 24 VDC AS STATED IN MM. SHOULD NOT HAVE THAT INITIAL SPIKE OF 24.96 VDC AT BOTTLE 2C. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042500241 20080425 00241 2008 4 25 2008UALA02333 4 20080418 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR WILL NOT ARM A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 FOUND DOOR 3R WILL NOT ARM. ADJUSTED/REPAIRED DOOR 3R, OPS CHECKED GOOD, ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042500243 20080425 00243 2008 4 25 2008UALA02335 4 20080419 A 2565 O-RING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L3 DOOR SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 LOW BOTTLE. SUPPLEMENTAL, GAUGE FITTING BACK UP RING LEAKS. REPLACED BACK UP RING. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042500250 20080425 00250 NM 2008 4 25 2008UALA02342 1 20080421 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 S7L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 FUSELAGE STRINGER 7L INTERCOSTAL WEB CRACKED AT BS 294.5. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW INTER COSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042500252 20080425 00252 NM 2008 4 25 2008UALA02344 1 20080421 A 5314 KEELBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 716-726 WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 KEEL BEAM RT LOWER CHORD ANGLE, UPPER SURFACE HAS 4 WORN FASTENER HOLES, BS 716-726. REMOVED DAMAGE. FABRICATED AND I NSTALLED NESTED ANGLE/FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041000168 20080410 00168 CE 2008 4 10 GUUA03270801 1 20080327 A 3260 DOWNLOCK SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT MLG OUT OF ADJUST A GUUA O OTHER N FALSE WARNING AP APPROACH 1 SO 29 17541 UE203 FLIGHT:9265, DURING APPROACH WHEN PLACING LANDING GEAR DOWN LT GREEN LIGHTS WILL NOT ILLUMINATE. ADJUSTED LT DOWNLOCK S WITCH. 2 L 7 2 4T 4 T RT A24CE E26NE 2008041000172 20080410 00172 CE 2008 4 10 DXTA20082977 1 20080402 A 3260 WARNING LIGHT BEECH MU300 400A 1155402 CE MLG ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 138QS RK492 AFTER DEPARTURE, THE RED, GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED. 2 H 7 2 4F RT A16SW 2008041000173 20080410 00173 2008 4 10 DXTA20082978 4 20080402 A 3414 INDICATOR CESSNA 500 560CESSNA 2076750 CE AIRSPEED FAILED E DXTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 352QS 5600352 ABOVE 40 KTS LT AIRSPEED FAILED WITH RED X ACCOMPANIED BY GPWS WINDSHEAR FAIL ANNUNCIATOR. 2 L 7 2 4F RT A22CE 2008041000192 20080410 00192 CE 2008 4 10 DJFA8033 1 20080330 A 2612 FIRE WARNING RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP ILLUMINATED E DJFA O OTHER J WARNING INDICATION CR CRUISE 1 EA 23 807LX 258413 WHILE AT CRUISE THE CREW REPORTED THE REAR BAGGAGE FIRE LIGHT ILLUMINATED INTERMITTENTLY. THE AIRCRAFT DIVERTED. OPEN 2 L 7 2 4F 4 F RT A3EU E6WE 2008041000202 20080410 00202 NM 2008 4 10 MASA200800283 1 20080402 A 5523 TRIM TAB DHAV DHC8 DHC8202 2809007 NM ELEVATOR DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 988HA 426 REPAIR TO ELEVATOR TRIM TAB. 2 H 7 2 4T RT A13NM 2008041000210 20080410 00210 NM 2008 4 10 SWAA081784 1 20080402 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008041000216 20080410 00216 NM 2008 4 10 CALA0800301 1 20080327 A 5320 6545834551 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11641 28902 INTERCOSTAL FWD WET AREA BETWEEN FLOORBEAM 328 & 344 LBL 46 CRACKED AT CLIP NUT HOLE. REMOVED & REPLACED INTERCOSTAL BE TWEEN STATIONS 328 & 344 LBL 46 IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041000223 20080410 00223 EU 2008 4 10 2008UALA01865 1 20080401 A 2611 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FAULTY A UALA O OTHER W N INADEQUATE Q C FALSE WARNING IN INSP/MAINT 1 WP 29 432UA 587 LAV CARGO SMOKE DETECTOR FAULT DISPLAYED, RESETS NO HELP. RUN TEST AT PTP PANEL AND DETERMINE THE SOURCE OF THE FAULT. RERACKED SCDCU PER MM26-17-34, ACCOMPLISHED GRND SCAN, NO FAULTS NOTED 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 EA 2008 7 24 A6WA200840431 1 20080618 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 CORROSION ON FLOOR ANGLE BETWEEN FS 409+128 TO FS 559 TO LBL 46. CORROSION ON FLOOR ANGLE FS 409+128 TO FS 559 AT LBL 4 6, REMOVED IAW CRJ 200 SRM 53-41-45 FIG 101. (A) 2 L 7 2 4F RT A21EA 2008041000247 20080410 00247 EA 2008 4 10 S9BA200800015 1 20080325 A 5413 C6W15125141 LONGERON DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA RT NACELLE DAMAGED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 562CP 125 562 DURING SCHEDULED 125HR INSPECTION FOUND: RT ENGINE NACELLE IB LONGERON DAMAGED FORWARD OF LEADING EDGE AT STATION 60.8. REMOVED AND REPLACED RT NACELLE IB LONGERON ASSY IAW AC 43-131B CHP7 EMERGENCY MEASURES EXECUTED: NO AIRCRAFT. GROUNDED : BEING REPAIRED DURING 125 HR CAMP INSPECTION, "NO". 1 H 7 2 3T 4 T RT A9EA E4EA 2008041000249 20080410 00249 NM 2008 4 10 2008UALA01892 1 20080402 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA 4084 PW4084 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 795UA 26927 EMERGENCY ESCAPE PATH LIGHT (AFT) IS INOP AT SEAT 3F. REPLACED LIGHT. OP CHKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008041000250 20080410 00250 EU 2008 4 10 2008UALA01893 1 20080403 A 5241 STRAP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AFT GALLEY DOOR UNSECURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 405UA 452 AFT GALLEY DOOR WON'T ARM PROPERLY. FOUND LOOSE STRAP AROUND DOOR 2R GIRT BAR PREVENTING FULL MOVEMENT. RESECURED STRAP , CYCLED DOOR AND ARMED TWICE. NORMAL COCKPIT INDICATIONS, NO FURTHER JAMMING NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041000251 20080410 00251 NM 2008 4 10 2008UALA01894 1 20080403 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 SEAT EEL ASSY BROKEN AT SEAT 59BC. REPLACED EEL ASSY. OP CK'D NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041000252 20080410 00252 NM 2008 4 10 2008UALA01895 1 20080402 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 EMERGENCY TRACK LIGHTING BY ROWS 27-29 HAS POPPED OUT. SECURED FLOOR TRACK COVER CHKS OK 2 L 7 2 4F 4 F RT A2NM E17NE 2008041000257 20080410 00257 WP 2008 4 10 ASMF200803003 1 20080330 A 7400 5D04232 SWITCH DOUG DC9 DC983 3022083 WP PWA JT8 JT8D1 52044 NE LT SIDE BURNED W ASMF D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 23 583MD 49659 AIRCRAFT RETURNED TO PLATFORM DUE TO SMOKE IN THE CABIN. MAINTENANCE DETECTED A SHORT CIRCUIT IN THE LT ENGINE SYS (A) I GNITION SWITCH, SO BREAKERS K-26 AND L26 WERE PULLED OUT AND AC WAS SENT TO THE HANGAR. AT HANGAR, SWITCH S1-35 WAS DETE CTED BURNED SO IT WAS REPLACED IAW MM 74-30-02, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E2EA 2008041000275 20080410 00275 NM 2008 4 10 2008UALA01904 1 20080402 A 3350 1317 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN WRONG PART A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 502UA 24623 DOOR 2L AND 2R LOWER EMERGENCY LIGHTS INOP. FOUND SMALL OVERHEAD EMERGENCY LIGHT IN MID GALLEY ON VERY DIMLY. IT HAD A 1308 BULB IN IT. SHOULD BE A 1317 BULB. RELAMPED WITH CORRECT BULB. ALL EMERGENCY LIGHTS AT DOOR 2L & 2R CHECKED OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041000276 20080410 00276 NM 2008 4 10 2008UALA01905 1 20080402 A 3350 S283T0143 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 658UA 27113 EXTERNAL EMERGENCY LIGHT RT DOOR R4 INOP. REMOVED AND REPLACED BATTERY PACK OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041000281 20080410 00281 NM 2008 4 10 2008UALA01910 1 20080402 A 2560 GIRT BAR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L4 DOOR CONTAMINATED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 199UA 28717 THE 4L DOOR WILL NOT ARM. FOUND GIRT BAR FLOOR ASSEMBLY CONTAMINATED. CLEANED AND LUBRICATED GIRT BAR FLOOR FITTINGS. A RM AND DISARM OK. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041000289 20080410 00289 NM 2008 4 10 2008UALA01918 1 20080403 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 R-1 DOOR IS OUT OF ADJUSTMENT, FAILS THE MIDWAY CHECK, GIRT BAR DOES NOT RELEASE. GIRT BAR OUT OF ADJUSTMENT. ADJUSTED GIRT BAR, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041000301 20080410 00301 2008 4 10 CALA0800286 4 20080331 A 2565 60176104 SLIDE BOEING 767 767424ER 1385270 NM R3 DOOR UNSERVICEABLE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76055 29450 CABIN - R3 EMERGENCY DOOR SLIDE PACKING TOO LOOSE. BUSTLE CANNOT FIT PROPERLY. CABIN - R3 EMERGENCY DOOR SLIDE ASSY RE PLACED AS PER AMM 25-66- 10. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1270979 SN OFF 00301 SLIDE, B767-400 OFF 64-2566 -9-0006 0301 ON 64-2566-9-0006 0386. 2 L 7 2 4F RT A1NM 2008041000302 20080410 00302 NM 2008 4 10 CALA0800287 1 20080307 A 5313 6561777 CHANNEL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 STRINGER SPLICE CHANNEL IS CRACKED, STA 361 AND STR 15 LT (MARKED). REMOVED & REPLACED STRINGER SPLICE CHANNEL BS 361 & S15L IAW PACE EA 350-53-003 CAL AND EC/RA 5310-04741. 2 L 7 2 4F RT A16WE 2008041000303 20080410 00303 EA 2008 4 10 MASA200800285 1 20080403 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCONNECTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH FLT 2925 PHX - ICT. FLOOR EMERGENCY LIGHTS AT ROWS 6, 7 AND 8 INOP. MX FOUND THE CONNECTOR AT THE LIGHT STRIP OFF AND RECONNECTED. OPS GOOD. 2 L 7 2 4F RT A21EA 2008041000307 20080410 00307 EA 2008 4 10 MASA200800290 1 20080404 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN SMOKE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 75994 7367 ASH FLT 7088 AVP-ORD. RIGHT PACK WAS BLOWING SMOKE AND AN OIL BURNING SMELL FROM THE FLIGHT DECK GASPER VENTS. OP CHEC KED GOOD. 2 L 7 2 4F RT A21EA 2008041000308 20080410 00308 EA 2008 4 10 MASA200800293 1 20080404 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 921FJ 15021 ASH FLT 2653 CLT-PNS. ROW 17 CEILING EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2008041000185 20080410 00185 NM 2008 4 10 CALA0800297 1 20080402 A 5320 656571022 BRACKET BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 46625 27529 AFT CARGO BETWEEN STA 747 AND 767, ANTENNA BRACKET CORROSION MARKED. REPLACED AFT CARGO ANTENNA BRACKET AT STA 747-767 PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041000218 20080410 00218 NM 2008 4 10 2008UALA01860 1 20080401 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 578UA 26694 LEFT FUSELAGE SKIN AT STA 1715 STR 15L & I-16A HAS DAMAGE. LT FUSELAGE SKIN REPAIR AT BS 1715 S15L & I-16A IS TIME LIMI TED REPAIR. APPROVED VIA FAA FORMS 8100-9 PER EVA UA-EVA-71357 A A CATEGORY "B" REPAIR PER PARAGRAPH "E" MUST BE ACP BY 31MAR10 2 L 7 2 4F 4 F RT A2NM E17NE 2008041000221 20080410 00221 2008 4 10 2008UALA01862 4 20080401 A 2565 SEAL BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 3 SLIDE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 776UA 26937 NR 3 LEFT MED SLIDE SHOWS NEEDLE BELOW GREEN BAND. DISCHARGE VALVE SEAL LEAKING. REPLACED NR 3 LT ESCAPE SLIDE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008050500205 20080505 00205 NM 2008 5 5 DHL2008760500 1 20080419 A 5311 SEEABOVE FRAME BOEING 727 7272B7 138407L NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 9G BARRIER FRAME AT BS 348.8 DENTED AT STR 5L TO 6L. CUT OUT DAMAGED AREA AND INSTALLED REPAIR ANGLES P/N AE727-2-360-1 2 AND AE727-2-360-11 PER AEI DWG AE727-360 REV G. 2 L 7 3 4F A3WE 2008041000264 20080410 00264 CE 2008 4 10 DJFA2008035 1 20080329 A 5514 45A21085004 BRACKET BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE HORIZONTAL STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 792TA 724 RK264 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER IB RIB AND BRACKET ASSEMBLIES, THE RT ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AR EA ARE OUTLINED IN COMMUNIQUE' NR 70. THE LEFT AND RIGHT H STAB INBOARD RIB ASSEMBLIES WERE REPLACED. 2 H 7 2 4F 4 F RT A16SW E25EA 2008041000266 20080410 00266 NM 2008 4 10 2008UALA01902 1 20080402 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 G5 GALLEY AREA EEL LIGHT INOP. REPLACED CABLE ASSY AND COVER OP CHECK NORMAL PER MM 33-51-12 PB 200 CONFIGURE 2 PARA 2. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041000270 20080410 00270 NM 2008 4 10 2008UALA01878 1 20080402 A 5330 BEAR STRAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 303 S9-10L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 BEAR STRAP CRACKED AT 2 EACH FASTENER HOLES AT FWD ENTRY DOOR UPPER CUTOUT STA 303.9. LOWER CRACK IS AT STR 10L AND UPP ER CRACK IS AT STR 9L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. INSTALLED REPAIR FILLER & DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 2008041000312 20080410 00312 NM 2008 4 10 SWAA081832 1 20080403 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED SPV CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008041000313 20080410 00313 NM 2008 4 10 SWAA081833 1 20080403 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008041000315 20080410 00315 NM 2008 4 10 SWAA081839 1 20080406 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 849, RBL 13. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041000316 20080410 00316 NM 2008 4 10 SWAA081840 1 20080406 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 829, RBL 13. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041000324 20080410 00324 NM 2008 4 10 SWAA081834 1 20080403 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 770SA 30589 DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008041000327 20080410 00327 NM 2008 4 10 CALA0800289 1 20080307 A 5320 6517684638 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 INTERCOSTAL ATTACH ANGLE TO FRAME AT STA 294.5 AND STR 12 LT LOCATION IS CRACKED (MARKED). REMOVED & REPLACED ATTACH AN GLE AT BS 294.5 & S12L IAW PACE EA 350-53-003 CAL AND ECRA 5310-04741. 2 L 7 2 4F RT A16WE 2008041000328 20080410 00328 NM 2008 4 10 2008UALA01883 1 20080403 A 5313 STRINGER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 294-303 S7L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 FUSELAGE STRINGER 7L HAS ELONGATED FASTENER HOLES COMMON TO SKIN & ONE VERTICAL HOLE WITH CRACK INDICATION BS 294-303. MAJOR REPAIR ACCOMLISHED: INSTALLED STRINGER SPLICE. 2 L 7 2 4F 4 F RT A16WE E21EU 2008041000329 20080410 00329 NM 2008 4 10 2008UALA01884 1 20080402 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1197 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 AFT CARGO COMPT AT BS 1197 + 66 AT LBL 14 FRAME T-CAP IS CORRODED UNDER AND AROUND NUT PLATES. MAJOR REPAIR ACCOMPLISHED : REMOVED & REPLACED T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041000330 20080410 00330 NM 2008 4 10 2008UALA01885 1 20080402 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1219 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 AFT CARGO COMPT AT BS 1219 AND RBL 33, FRAME T-CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED T-CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041000335 20080410 00335 NM 2008 4 10 CALA0800304 1 20080405 A 5313 BAC1493248 STRINGER BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 46625 27529 S16L CRACKED STA 482B-4". REPAIRED S16L STA 482B-4" REF SRM 53-00-03 REPAIR 1 FIG 201 PG 201. 2 L 7 2 4F RT A16WE 2008041000337 20080410 00337 NM 2008 4 10 CALA0800306 1 20080311 A 5320 BAC150518761 FASTENER BOEING 737 737524 1384721 NM INTERCOSTAL MISSING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11641 28902 INTERCOSTAL ATTACH POINT TO INBOARD FLANGE OF FRAME STA 348 AND STR 14 LT FASTENERS (2) MISSING (MARKED). INSTALLED 2 F ASTENERS AT BS 348 STR 14 LT AT INTERCOSTAL ATTACH POINT TO INBOARD FLANGE OF FRAME PER PACE EA 641-53-0001 CAL AND EC/R A 5310-04742. 2 L 7 2 4F RT A16WE 2008041100006 20080411 00006 EU 2008 4 11 08FDEA01369 1 20080410 A 5755 A57771000004 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 3 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND DELAMINATION OUT OF LIMIT ON SPOILER NR 3 RT REPAIR PERFORMED BY REPLACEMENT OF IAW AMM 25-61-51. 2 L 7 2 4F RT A35EU 2008041100007 20080411 00007 EU 2008 4 11 08FDEA01370 1 20080410 A 5755 A57771000004 SPOILER PANEL AIRBUS 300 A300B4622R 3930312 EU NR 4 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND DELAMINATION OUT OF LIMIT ON SPOILER NR 4 RT. REPAIR PERFORMED BY REPLACEMENT OF IAW AMM 25-61-51. 2 L 7 2 4F RT A35EU 2008041100008 20080411 00008 EU 2008 4 11 08FDEA01371 1 20080410 A 5755 A57771000004 SPOILER PANEL AIRBUS 300 A300B4622R 3930312 EU NR 5 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND DELAMINATION OUT OF LIMIT ON SPOILER NR 5 RT. REPAIR PERFORMED BY REPLACEMENT OF IAW AMM 25-61-53. 2 L 7 2 4F RT A35EU 2008042500261 20080425 00261 NM 2008 4 25 2008UALA02352 1 20080422 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT LIGHT INOP, ROW 26 RIGHT CEILING. REPLACED LAMP. OP CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500264 20080425 00264 NM 2008 4 25 2008UALA02355 1 20080422 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT LIGHT INOP, UPPER DECK CEILING ROW 13. REPLACED LAMP. OP CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500266 20080425 00266 NM 2008 4 25 2008UALA02357 1 20080422 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT LIGHT INOP, AT DOOR 2 LEFT FWD SILL. FOUND FAULTY BULB. REPLACED LAMP OPS CHECKED GOOD. AC OK FOR SERVIC E. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500270 20080425 00270 NM 2008 4 25 2008UALA02361 1 20080422 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 197UA 26901 F/A REPORTS EMERGENCY LIGHTS AT FC RT SIDE SEATS ON J SIDE ARE INTERMITTENT. FOUND LOOSE CONNECTION. RECONNECTED BATTER Y PACKS. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500275 20080425 00275 NM 2008 4 25 2008UALA02366 1 20080422 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 907 S26L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 305UA 23666 FOUND DAMAGED SKIN AT STA 907 STR 26L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SKIN. INSTALLED DOUBLER, TRIPLER & ST RUCTURUAL FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042500276 20080425 00276 NM 2008 4 25 2008UALA02367 1 20080422 A 5754 STRUCTURE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 SLAT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 819UA 893 DAMAGE TO NR 1 L/E SLAT. REPLACED NR 1 LE SLAT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042500278 20080425 00278 EU 2008 4 25 2008UALA02369 1 20080422 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 448UA 842 FLOORBEAM CORROSION WHERE BEAM Y254 CROSSES FRAME 68 THIS LOCATION IS JUST AFT OF LAV WASTE TANK AND TO LEFT OF AIRCRAFT CENTERLINE ON LEFT SIDE OF FLOORBEAM. REMOVED CORROSION IAW SRM 51-74-00. REMOVED FLOORBEAM IAW SRM 51-42-11. LOCATED , DRILLED AND DEBURRED IAW SRM 51-44-11. TREATED, PRIMED & TOP COATED IAW SRM 51-21-11. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042500282 20080425 00282 NM 2008 4 25 2008UALA02380 1 20080423 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 SEAT 1A FWD EMERGENCY LIGHT IS INOP. REPLACED LAMP, CHKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500283 20080425 00283 NM 2008 4 25 2008UALA02381 1 20080423 A 3350 20131A LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEATS 46-52ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 SEAT 46-52ABC EMERGENCY LIGHTS IS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500289 20080425 00289 EU 2008 4 25 08FDEA01522 1 20080424 A 2597 CONNECTOR AIRBUS 300 A300F4605R 3930327 EU L1 DOOR SLIDE MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 L-1 DOOR SLIDE ASSY, BATTERY TEST CONNECTOR IS MISSING. RECEIVED SERVICABLE SLIDE FOR FR 15B (L-1 DOOR) TO BE INSTALLED ON WIC 68S5001CP. 2 L 7 2 4F RT A35EU 2008042500290 20080425 00290 2008 4 25 08FDEA01523 4 20080424 A 2565 D31023101 SLIDE AIRBUS 300 A300F4605R 3930327 EU R1 DOOR SLIDE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 R-1 DOOR SLIDE ASSY, BOX IS CRACKED ON THE OUTER SURFACE, UPPER FWD SIDE. RECEIVED SERVICEABLE SLIDE TO BE INSTALLED ON W/C 68S1500CP; STEP 5-B. 2 L 7 2 4F RT A35EU 2008042500293 20080425 00293 NM 2008 4 25 KNNA20080008 1 20080424 A 5310 STRUCTURE BOEING 737 7372L9 1384497 NM BS 727 CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 464AT 21278 AFTER OPEN UP FOUND STA 727 RT CHORD CRACKED AT LWR END. CUTOUT OUT CHORD AND SPLICED IN NEW SECTION OF CHORD IAW SB 73 7-53-1088 AND ACO-085313. 2 L 7 2 4F RT A16WE 2008042500295 20080425 00295 NM 2008 4 25 2008UALA02417 1 20080424 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EXT EMERGENCY LT INOP:RT OVERWING 3RD ASSY AFT BULB. RELAMPED. CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500296 20080425 00296 NM 2008 4 25 HALA0800536 1 20080417 A 5751 SKIN BOEING 717 717200 1383700 NM LT WING AILERON DAMAGED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 486HA 55131 LIGHTNING STRIKE DAMAGE, L WING AILERON STATIC WICK AND AILERON BURNED TOP SIDE. REMOVED AND REPLACED LT AILERON AND TA B ASSY PER AMM 27-10-01. FUNCTIONAL CK OK. 2 L 7 2 4F TR A6WE 2008042500299 20080425 00299 NM 2008 4 25 2008UALA02399 1 20080423 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 STRINGER CHANNEL CRACKED AT STRINGER 14L, 15L AND 16L BS 359. REPAIRED PER UA-EVA-71481 AND UA-EVA-71482 AND REO-O1065. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042500302 20080425 00302 NM 2008 4 25 2008UALA02389 1 20080422 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEAT 34H MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 669UA 30025 EMERGENCY LIGHT MISSING ON SIDE OF SEAT 34H. REPLACED LIGHT STRIP ON SIDE OF SEAT 34H. OPS CHK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042500312 20080425 00312 NM 2008 4 25 CALA0800349 1 20080421 A 5210 6552878U125 ANGLE BOEING 737 737524 1384721 NM L2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 L-2 DOOR Z-ANGLE HAS SEVERAL AREAS OF CORROSION STA 951 TO 986.5+12. CORROSION AT L-2 DOOR DETERMINED TO BE BEYOND ALLO WABLE LIMITS PER 737-500 SRM 53-60-15 FIG 101. REMOVED AND REPLACED L-2 DOOR Z-ANGLE, REF 737-500 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008042500324 20080425 00324 NM 2008 4 25 SWAA082165 1 20080423 A 5313 BAC1498 STRINGER BOEING 737 7377H4 1384404 NM BS 520 S26L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 DURING SCHEDULED HC1 CHECK, STRINGER 26L CORRODED AT BS 520. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008042500325 20080425 00325 NM 2008 4 25 SWAA082164 1 20080423 A 5520 DAS623B BEARING BOEING 737 7377H4 1384404 NM LT ELEVATOR FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 DURING SCHEDULED HC1 CHECK, LEFT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED LEFT ELEVATOR CONTROL BEARING PE R MM. 2 L 7 2 4F RT A16WE 2008042500333 20080425 00333 NM 2008 4 25 ASAA0892832 1 20080322 A 5330 146A320116 SKIN BOEING 737 737990 NM BS 810-833 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 317AS 30856 LEFT AFT FUSELAGE SKIN DENT ON FRAME STA 827 STR 21L WITH DENT AT STA 817. CUT OUT DAMAGED AREA IAW AAR EA 12569, FABRI CATED FILLER DOUBLER AND TRIPLER IAW AAR EA 12569, INSTALLED REPAIR PARTS IAW AAR EA 12569 AND ASA EA 5330 02325. 2 L 7 4 4F RT A16WE 2008042800004 20080428 00004 EA 2008 4 28 A6WA200840263 1 20080325 A 5240 SKIN CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 SERVICE DOOR CORROSION FOUND WL 73.50, FS 319.70 TO FS 349 RBL 40. (M) SERVICE WL 73.50, FS 319.70 TO FS 349.00, RBL 4 0.00, CORROSION REMOVED IAW SRM 51-21-06. (K) 2 L 7 2 4F RT A21EA 2008042800006 20080428 00006 EA 2008 4 28 A6WA200840264 1 20080324 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 FS 484, LBL 9, FLOOR SUPPORT ANGLE FOUND CRACKED LENGTH OF CRACK IS .400 INCH. FLOOR SUPPORT ANGLE AT FS 484, LBL 9 REP LACED IAW CRJ200 SRM 51-42-06 AND 51-42-20. (M) 2 L 7 2 4F RT A21EA 2008042800015 20080428 00015 WP 2008 4 28 MWEA080056 1 20080418 A 5330 59114003 SKIN DOUG DC9 DC981 3022081 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 814ME 48010 NOSE SECTION LEFT SIDE STATION 8 APPROXIMATELY 10 INCHES BELOW SKIN JOINT. SKIN HAS IMPACT DAMAGE. FABRICATED AND INST ALLED DOUBLER. 2 L 7 2 4F A6WE 2008042800018 20080428 00018 2008 4 28 MWEA080058 4 20080422 A 2565 D29982225 PIN BOEING 717 717200 1383700 NM EVAC SLIDE PULLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 912ME 55175 FOUND FORWARD SERVICE DOOR ESCAPE SLIDE INFLATION CABLE PINS PULLED OUT OF SLIDE. REMOVED AND REPLACED SERVICE DOOR ESC APE SLIDE. 2 L 7 2 4F TR A6WE 2008042800022 20080428 00022 NM 2008 4 28 ASAA0852822 1 20080417 A 2150 3989083 MODULATING VALVE BOEING 737 737890 1384527 NM RT A/C PACK MALFUNCTIONED A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 583AS 35681 CABIN ZONE TEMPERATURE ANNUNCIATION OCCURRED. BITE TEST INDICATED RIGHTHAND PACK TRIM MODULATING VALVE AT FAULT. RESET , OP CHECKED OK. 2 L 7 2 4F RT A16WE 2008042400131 20080424 00131 SO 2008 4 24 CHQA200800081 1 20080419 A 3297 14521585405 WIRE HARNESS EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RT MLG FAULTY A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 292SK 145488 CAE311794 FLIGHT 7844, IAD TO CMH - DURING CLIMB WHEN THE CREW ATTEMPTED TO RAISE THE GEAR THEY RECEIVED A LG AIR/GND FAIL MESSAGE ON EICAS AND THE LANDING GEAR WOULD NOT RETRACT. THE CREW PERFORMED THE APPROPRIATE CHECK LISTS AND LANDED WITHOUT INC IDENT. MAINTENANCE TROUBLESHOT THE LANDING GEAR PROXIMITY SENSORS AND HARNESS AND FOUND THE RIGHT WEIGHT ON WHEELS HARN ESS FAULTY. THE HARNESS WAS MEGGED AND CONFIRMED BAD. THE HARNESS WAS REPLACED ALONG WITH THE RIGHT FORWARD MAIN LANDI NG GEAR PROX SWITCH. THE LANDING GEAR SYSTEM THEN OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008042400132 20080424 00132 WP 2008 4 24 070194 1 20080420 A 2121 66054577 FAN DOUG DC9 DC987 3022087 WP RECIRCULATION INOPERATIVE A WX0A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 19 952MA 49673 FLIGHT ATTENDANTS REPORTED TO A BURNING ELECTRICAL ODOR AND SMOKE IN THE REAR OF THE CABIN. CABIN TEMP GAUGE EXCEEDED 1 50'F. FLIGHT DECK CREW ELECTED TO RETURN TO TYS. THE AIRCRAFT WAS INSPECTED BY MAINTENANCE DEPARTMENT PERSONNEL, TROUB LESHOOTING DETERMINED THE RECIRCULATION FAN WAS INOPERATIVE AND THE FAN WAS REPLACED. AN OPERATIONAL CHECK WAS PERFORME D AND THE SYSTEM CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008042400144 20080424 00144 NM 2008 4 24 08FDEA01496 1 20080423 A 5522 6572784 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 RT ELEVATOR LWR SKIN HAS A DENT 97 INCHES FROM I/B EDGE, 7 INCHES FWD OF REAR SPAR. MEASURED DENT FOUND TO BE WITHIN LI MITS, MEASURED DENT Y = .040 A = 4 INCHES FOUND TO BE 100 REF SRM 55-10-1 PG 7 FIG 2. THIS IS CLASSIFIED AS A MINOR R EPAIR. 2 L 7 3 4F A3WE 2008042400167 20080424 00167 WP 2008 4 24 08FDEA01478 1 20080423 A 5347 WSP0413523 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1273 AND X -47.250 FOUND MISSING MATERIAL ON SEAT TRACK. REPAIRED SEAT TRACK FOR SRM 53-10-00 FIG 1 VOL I. 2 L 7 3 4F A22WE 2008042400175 20080424 00175 SO 2008 4 24 SWIA200819496 1 20080417 A 5210 DOOR EMB 120 EMB120ER 3260203 SO MAIN PAX BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 581SW 120349 FLT 5567 - FORWARD DOOR IS DIFFICULT TO OPEN. ADJUSTED PAX DOOR IAW EMB 120 AMM 52-11-00. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2008042400187 20080424 00187 SO 2008 4 24 SWIA200819508 1 20080317 A 2731 ROD END EMB 120 EMB120ER 3260203 SO ELEVATOR TAB CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 585SW 120353 RIGHT ELEVATOR TRIM TAB ROD ENDS ARE CORRODED, FOUND AT C-CHECK. REPLACED ELEVATOR TRIM TAB ROD ENDS. 2 L 7 2 4T RT A31SO 2008042500018 20080425 00018 EU 2008 4 25 COEA0801903 1 20080331 A 5610 NP1588014 WINDSHIELD AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE COCKPIT CRACKED A COEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 13 903FX 179 AIR TURNBACK, FLT NR 100. ON CLIMB OUT, THE FO WINDSHIELD CRACKED. CABIN PRESSURE WAS REDUCED AND THE WINDSHIELD HEAT WAS TURNED OFF. THE CREW ELECTED TO RETURN TO DEPARTURE. THE AC MADE A SAFE AND NORMAL FLIGHT AND LANDING. REPLACED R T WINDSHIELD. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008042500025 20080425 00025 EU 2008 4 25 OZC2008F00000 1 20080326 A 2910 L38710SA SWIVEL SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE HYD LINE BROKEN A OZCA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 19 641BC SF340A069 GE PILOT NOTED THE HYD LIGHT ON DUE TO LOSS OF PRESSURE IN MAIN ACCUMULATOR AND HYD QUANTITY READING ZERO. PERFORMED AN EM ERGENCY GEAR EXTENSION IAW QRH AND HAD AN UNEVENTFUL LANDING. MAINT INSPECTED THE AC AND FOUND THE HYD SWIVEL IN THE RT MAIN GEAR WELL PN L38710SA BROKEN. THE PART WILL BE REPLACED AND THE ENTIRE HYD SYS INSPECTED PRIOR TO THE AC RETURNED TO SERVICE. (K) 2 L 7 2 4T 4 T RT A52EU E8NE6 2008042500027 20080425 00027 EA 2008 4 25 TRAX200800535 1 20080412 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY ACTIVATED A ASOA J A DUMP FUEL UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SO 27 908EV 7654 REC CARGO SMOKE MSG IN FLT BLEW BOTH CARGO BOTTLES, DECLARED AN EMERGENCY LANDING INTO MEI. FLT 9971 DEL 92 MINS. EN R OUTE TO ATL AIRCRAFT DIVERTED TO MEI DUE TO MTC. 2 L 7 2 4F RT A21EA 2008042500042 20080425 00042 SO 2008 4 25 FDKA200804160 1 20080412 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM FLT 6092 MCO-HSV.(0437 PHX LCL) RIGHT OVERWING EXIT MARKER OUT. MX INSPECTED AND FOUND A LOOSE CONNECTOR. SECURED CONNECTOR. SYSTEM OPS GOOD. 2 L 7 2 4T RT T00011AT 2008042500051 20080425 00051 SO 2008 4 25 C2XA08SH067 1 20080418 A 5751 14569009407 ATTACH FITTING EMB 145 EMB145LR 3260212 SO LT AILERON GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12569 145630 SHV - DURING C-CHECK THE LEFT HAND OUTBOARD AILERON TO PCA ATTACH FITTING WAS FOUND TO BE GOUGED AND ALSO HAD MIGRATED H AT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW CONTINENTAL EXPRESS EC5750-01177. THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008042500054 20080425 00054 EU 2008 4 25 J1Q2008F00001 1 20080316 A 2910 F50B751313 LINE AMD FALC50 FALCON50MYST 2730106 EU HYD SYSTEM FAILED A J1QA O OTHER O OTHER CR CRUISE 1 GL 15 751JC 129 AC WAS ENROUTE, DURING FLIGHT THE CREW NOTICED THE NR 2 HYDRAULIC QUANTITY GOING DOWN. CREW SHUTOFF THE STANDBY HYD PUM P IAW THE CHECK LIST. CREW CONTINUED TO MONITOR THE HYD QUIT DURING THE FLIGHT. DURING THE APPROACH, THE 3 HYDRAULIC P UMP WARNING LIGHT CAME ON AND HYD PRESSURE DROPPING. PILOTS DIVERTED, FOR FIELD LENGTH RESTRICTIONS. AC LANDED. IN T HE AFT BAGGAGE COMPARTMENT BAY, THE LEAK APPEARS TO BE LOCATED WHERE THE LINE HAD COME INTO CONTACT WITH A TOOL THAT HAD GROUNDED TO SOME SORT OF A POWER SOURCE. THERE IS NOT ANY POWER SOURCE LOCATED IN THE SAME VICINITY WERE THE LINE IS L OCATED. SUSPECT LINE MAY HAVE BEEN DAMAGED DURING SOME TYPE OF HEAVY MAINTENANCE OR ELECTRICAL MODS TO THE AC. THE HYD 2 L 7 3 4F A46EU 2008042500059 20080425 00059 SO 2008 4 25 C2XA08TY046 1 20080411 A 5751 14569009608 BRACKET EMB 135 EMB135LR 3260305 SO RT AILERON WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17513 145292 RIGHT AILERON PCA BRACKET BORE FOR THE BUSHING WORN. REMOVED AND REPLACED PCA BRACKET IAW EMB EC5750-01177, AIRCRAFT ST ILL IN C-CHECK. 2 L 7 2 4F RT T00011AT 2008042500063 20080425 00063 NM 2008 4 25 ZZDA2008090 1 20080417 A 3397 WIRE BOEING 717 717200 1383700 NM CABIN BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 950AT 55012 ROWS 27, 28, AND 29 EMERGENCY PATH LIGHTS INOPERATIVE. REPAIRED BROKEN WIRES AT QUICK DISCONNECTS AT ROWS 27, 28, AND 2 9 IAW SWPM 20-31-00. OPS CHECK NORMAL IAW AMM 33-51-00. 2 L 7 2 4F TR A6WE 2008042500064 20080425 00064 SO 2008 4 25 RAIA00804015 1 20080413 A 3610 O-RING EMB 145 EMB145EP 3260221 SO BLEED AIR SYS WORN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 827HK 145021 FLT 5468 - STL - BLEED NR 1 & 2 LEAK MESSAGE ON THE EICAS FOLLOWED BY A BURNING SMELL IN THE COCKPIT. MAINTENANCE REMOV ED AND REPLACED THE O-RINGS AND CLAMP ON THE BLEED DUCT FOLLOWED BY SUCCESSFUL OPERATION OF THE BLEED AIR SYSTEM. 2 L 7 2 4F RT T00011AT 2008042500068 20080425 00068 SO 2008 4 25 RAIA0804018 1 20080415 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 PRE FLT 7882 - STL - VARIOUS EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INVERTER. LIGHT OPS CH ECKED GOOD. 2 L 7 2 4T RT T00011AT 2008042500088 20080425 00088 EA 2008 4 25 TRAX200800555 1 20080416 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 921EV 7819 GALLEY LOWER EMERGENCY LIGHT HAS SEVERAL INOP BULBS. 2 L 7 2 4F RT A21EA 2008042500129 20080425 00129 CE 2008 4 25 DXTA200802989 1 20080411 A 3241 42901 CONTROL UNIT BEECH MU300 400A 1155402 CE ANTI-SKID SYS MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 122QS 1228 RK467 AFTER LANDING AND INITIAL LT SEAT APPLICATION, BRAKES WORKED PROPERLY FOR A COUPLE OF SECONDS. THEN NO BRAKING. REPLACE D ANTI-SKID CONTROL BOX. BRAKES OPS CHECK GOOD AT THIS TIME. IAW MM 32-40-00. 2 H 7 2 4F RT A16SW 2008042500140 20080425 00140 EA 2008 4 25 MASA200800331 1 20080420 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 506MJ 10073 ASH FLT 7057 ORD-DSM. LEFT WING LOWER EMERGENCY EXIT LIGHT INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 2008042500143 20080425 00143 NM 2008 4 25 KCSA08032 1 20080420 A 2612 FIRE WARNING BOEING 747 747209F 1384800 NM PWA JT9 JT9D7Q 52054 NE NR 3 ENGINE ACTIVATED A KCSA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 23 704CK 22299 702254 NR 3 ENG FIRE INDICATION DURING CLIMBOUT THROUGH 4000 FT APPROX 5 MIN INTO FLIGHT. 2 L 7 4 4F 4 F RT A20WE E3NE 2008042500152 20080425 00152 SO 2008 4 25 FDKA200804169 1 20080418 A 2611 DETECTION SYS EMB 145 EMB145LR 3260212 SO CARGO BAY MALFUNCTIONED A FDKA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 831MJ 145273 FDM 6042 RDU-JFK. BAGGAGE SMOKE DETECTION LIGHT ON IN FLIGHT. MX VERIFIED THERE WAS NO SMOKE IN BAGG COMP AND RESET TH E SYSTEM. 2 L 7 2 4T RT T00011AT 2008042500160 20080425 00160 SO 2008 4 25 C2XA08SH069 1 20080422 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13202 14500962 SHV - DURING C-CHECK CORROSION ON LEFT OMEGA BEAM AT FR 20. MX REPAIRED LEFT OMEGA BEAM AT FR 20 IAW EMB 145XR SRM 53-0 0-10. THE AIRCRAFT WAS APPROVED FOR RETURN FOR SERVICE. 2 L 7 2 4F RT 2008042500188 20080425 00188 2008 4 25 2008UALA02323 4 20080420 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DOOR SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 433UA 589 EMERGENCY LIGHT TEST RESULT SHOW 'EXT LOAD AFT L' AT FAULT. FOUND RT AFT SLIDE SHORTED INTERNALLY. REPLACED RH AFT S LIDE AND RETESTED EMER LIGHTS SYSTEM OK 2 L 7 2 4F 4 F RT A28NM E40NE 2008042500196 20080425 00196 EA 2008 4 25 TRAX200800528 1 20080410 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 AAR - BATH TUB FITTING CRACKED AT RBL 9. REMOVE UNSERVICEABLE TUB FITTING IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-4 2-21. TRANSFERRED HOLES TO SERVICEABLE TUB FITTING FROM UNSERVICEABLE FITTING, IAW CRJ 200 SRM 51-40-11, OK TO INSTALL PLJ 14922 04/13/08. INSTALLED SERVICEABLE FITTING IAW CRJ SRMM 51-42-21. OK TO TOPCOAT. APPLIED TOPCOAT IAW CRJ SRM 5 1-25-11. DR 15098. SUPPLEMENTAL SDR CLOSED 4/22/08. 2 L 7 2 4F RT A21EA 2008042500197 20080425 00197 SO 2008 4 25 C2XA08IA117 1 20080421 A 3350 7287580507 LIGHT EMB 135 EMB135LR 3260305 SO CABIN DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 29515 145309 IAH - DURING MAINTENANCE INSPECTION A FLOOR PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIR CRAFT, AND PLACED THE LIGHT STRIP ON MEL 33-50-00/2 CAT "C" CONTROL NUMBER 143990, AND THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. ON FLIGHT 2664, THE AIRCRAFT LANDED IN IAH WHERE MAINTENANCE RECONNECTED THE NR 3 AISLE PATH LIGHT STRI P, OPERATIONALLY CHECKED WITH NO DEFECTS. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008042500203 20080425 00203 NM 2008 4 25 SWAA082119 1 20080421 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042500221 20080425 00221 NM 2008 4 25 SWAA082122 1 20080420 A 5330 6550570 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042500291 20080425 00291 2008 4 25 2008UALA02406 4 20080423 A 2565 O-RING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE R1 DOOR SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 CREW REPORTS 1R DOOR SLIDE LOW PRESSURE. SUSPECT FAULTY O-RING.REPLACED 1R DOOR SLIDE ASSEMBLY REF MM 25-66-01.AC OK FO R SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042500294 20080425 00294 NM 2008 4 25 2008UALA02416 1 20080424 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EXT EMERGENCY LT INOP: LT OVERWING 2ND AFT ASSY FWD BULB. RELAMPED. CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500297 20080425 00297 NM 2008 4 25 HALA0800541 1 20080423 A 3244 3910797513 TIRE BOEING 717 717200 1383700 NM MLG FAILED A HALA O OTHER O OTHER LD LANDING 1 WP 13 475HA 486 486 55121 NEED TO REPLACE NR 4 MLG TIRE DUE TO RECAP SEPARATION. REPLACED NR 4 MLG TIRE PER AMM 32-41-01, SPIN CK GOOD. 2 L 7 2 4F TR A6WE 2008042500309 20080425 00309 NM 2008 4 25 2008UALA02400 1 20080424 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 S7L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 INTERCOSTAL WEB CRACKED AT AFT SIDE OF BS 294.5 STR 7L UPPER SURFACE INBD. REPAIRED PER UA-EVA 71481 AND REO-L-01065. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042500311 20080425 00311 NM 2008 4 25 CALA0800348 1 20080421 A 5420 313A1380214 ANGLE BOEING 737 737524 1384721 NM RT NACELLE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 RIGHT ENGINE PYLON VERTICAL ANGLE AFT SIDE OF PANEL OPENING NR 5858R CRACKED. INSTALLED SUPPORT ASSY 313A1380-214 AND PYLON PANEL 15852R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008042500323 20080425 00323 NM 2008 4 25 SWAA082163 1 20080423 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM BS 986 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 18L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042800007 20080428 00007 EA 2008 4 28 A6WA200840265 1 20080325 A 5320 LONGERON CNDAIR CL600 CL6002B19 1900309 EA BS 319-349 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 AT PAX DOOR, FS 319.70 TO FS 349, CORROSION WAS FOUND ON LOWER SILL LONGERON. (M) CORROSION REMOVED IAW SRM 51-21-06. 2 L 7 2 4F RT A21EA 2008041100012 20080411 00012 EA 2008 4 11 A6WA200840138 1 20080225 A 5280 DOOR CNDAIR CL600 CL6002B19 1900309 EA LT MLG DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 LT MLG FIXED DOOR FOUND WORN ON LT END SECTION. REPAIRED IAW REO 601R-52-82-034 SHEET 1 THROUGH 4. (M) 2 L 7 2 4F RT A21EA 2008040400078 20080404 00078 2008 4 4 2008UALA01828 4 20080331 A 2565 SLIDE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L2 DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 DOOR 2L SLIDE PRESSURE GAUGE BELOW GREEN BAND. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040400087 20080404 00087 NM 2008 4 4 2008UALA01838 1 20080401 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY EXIT EEL LIGHT INOP, AT SEAT 49L. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040400088 20080404 00088 NM 2008 4 4 2008UALA01839 1 20080401 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 60R. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 2008040400090 20080404 00090 NM 2008 4 4 2008UALA01841 1 20080331 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INTERMITTENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 672UA 30027 EXIT ROW EMERGENCY LIGHTS GO ON AND OFF INTERMITTENTLY. COULD NOT DUPLICATE LIGHT MALFUNCTION. TEST OK NO FAULTS DETECT ED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008040400091 20080404 00091 NM 2008 4 4 2008UALA01842 1 20080331 A 2622 EXTINGUISHER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT DISLODGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 673UA 29241 REINSTALL COCKPIT FIRE EXTINGUISHER FELL OFF BRACKET. REINSTALLED BOTTLE IN HANGER ASSY. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT A1NM E24NE 2008040400098 20080404 00098 NM 2008 4 4 2008UALA01849 1 20080331 A 3350 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 777UA 26916 FLOOR PROXIMITY EMERGENCY PATH MARKING LIGHT AT SEAT 18C INOP. FLOOR PROXIMITY EMERGENCY PATH MARKING LIGHT AT SEAT 18 C INOPERATIVE. RELAMPED. CHECKED GOOD FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008040400100 20080404 00100 NM 2008 4 4 2008UALA01851 1 20080401 A 2730 251N20101 JACKSCREW BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HORIZONTAL STAB GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 556UA 26650 HORIZONTAL STAB JACKSCREW MIDDLE SECTION HAS .001 GOUGE. HORIZONTAL STAB BALLSCREW SHOWS SIGNS OF GALLING AND WEAR AL ONG MIDDLE 2 FOOT LENGTH OF BALLSCREW, JACKSCREW REMOVED AND REPLACED, 2 L 7 2 4F 4 F RT A2NM E17NE 2008040400103 20080404 00103 SO 2008 4 4 LR7A08048 1 20080331 A 5320 33383532 FITTING LKHEED 382 382G 526414U SO FS 497 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 621 4676 DURING SCHEDULED B-1 CHECK, PER JOB CARD HB5301, FOUND RT UPPER MWW BOW BEAM FITTING CRACKED AT FS 497, WL 260, RBL 62. REPAIR ACCOMPLISHED BY REPLACING FITTING IAW SMP583 CHAPTER 51-60 AND 51-70. 2 H 7 4 4T A1SO 2008040400105 20080404 00105 EU 2008 4 4 08FDEA01239 1 20080401 A 5320 A53811507201 FITTING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LEFT MLG WHEEL WELL CUTOUT; INTERNAL LOWER INBD CORNER HAS CORROSION AND BARE METAL. COMPLIED WITH EA 6-5310-118456; F USELAGE LT MLG DOOR OPENING CORNER FITTING REPAIR. 2 L 7 2 4F RT A35EU 2008040400108 20080404 00108 EU 2008 4 4 08FDEA01242 1 20080401 A 5313 A5397420322500 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 BULK PIT; FRAME 68; STRINGER 53R AND STRINGER 54R HAS SURFACE CORROSION. REMVOED CORROSION IAW AMM 51-74-10-8. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00, DRILLED UP SPLICES AND STRINGERS IAW SRM 51-72-10, ALODINED & PRIMED AREAS AND PAR TS IAW 51-21-10, 51-23-10, INSTALLED PARTS STRINGERS AND SPLICES IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008040400109 20080404 00109 WP 2008 4 4 08FDEA01243 1 20080401 A 5310 DOOR FRAME DOUG DC10 DC1030F 3023504 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 86037 46871 FWD CARGO DOOR CUT-OUT AFT JAMB CORRODED AT LWR AFT SIDE UNDER GUIDE ROLLER FITTING. REMOVED CORROSION, REMOVED AND REP LACED INTERCOSTAL,STRAP, CORNER FITTING, SEAL RETAINER AND FORMER IAW SRM 51-31-01 AND 53-50-00 FIG 1. 2 L 7 3 4F RT A22WE 2008040400110 20080404 00110 EU 2008 4 4 08FDEA01244 1 20080402 A 3231 2103000000 ACTUATOR AIRBUS 310 A310222 3930315 EU MLG DOOR FAILED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 25 422FE 16902 16902 346 WHEN THE LANDING GEAR WERE LOWERED THE GREEN HYDRAULIC SYSTEM FAILED. ALL LANDING GEAR SHOWED DOWN WITH 3 GREEN LIGHTS EACH ON THE FRONT PANEL AND THE OVERHEAD PANEL. THE LEFT MAIN GEAR DOOR LIGHT WAS ON WITH AN ECAM MESSAGE SAYING THAT IT WAS NOT UP. AFTER LANDING, WE WERE TOLD THE LEFT MAIN GEAR DOOR ACTUATOR FAILED RESULTING IN HYDRAULIC FLUID LOSS. REMOVED AND REPLACED LEFT MAIN GEAR DOOR ACTUATOR IN REF TO MM 32-31-35-4. OPS CHECK DOOR OPERATION REF 32-31-00. PER FORMED LEAK CHECK OF ACTUATOR, NOLEAKS NOTED. REPLENISHED GREEN SYSTEM HYDRAULIC RESERVOIRS REF MM 12-12-29-0, OFF MFG 21030-000-00 SRL CV0011. 2 L 7 2 4F RT A35EU 2008040400111 20080404 00111 EU 2008 4 4 08FDEA01245 1 20080402 A 5340 A53974005222 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CLIP WITH MISDRILLED HOLES AT C70, P43 LT. REPAIR PERFORMED Y REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008040400119 20080404 00119 EU 2008 4 4 08FDEA01254 1 20080402 A 5330 A53985240204 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 741FD 611 FOUND IMPACT/TOOLING MARKS ON SKIN AT STRINGER 4 RT, C 83-84. REPAIR PERFORMED BY REWORK OF DAMAGE TO SMOOTH CONTOUR, N DT FOR CRACK FREE AND FLAP PEENING IAW RAS/EFW/9000016/2008 ISS A, APPROVED BY EA 6-5319-114883. 2 L 7 2 4F RT A35EU 2008042800017 20080428 00017 EA 2008 4 28 TRAX200800502 1 20080408 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 AAR - 1021 - FUSELAGE EXTERIOR SKIN HAS SIGNS OF CORROSION (UNDER PAINT) JUST AFT OF PAX DOOR CUTOUT, LWR, AFT CORNER. BLENDED FUSELAGE EXTERIOR SKIN JUST AFT OF PAX DOOR CUTOUT, IAW CRJ 200 SRM 53-00-31. ORIGINAL THICKNESS OF SKIN IS 0.0 63, AFTER BLENDING SKIN, IS FOUND TO BE STILL WITHIN LIMITS. TO BE PRIMED AND TOPCOAT. TOPCOATED, IAW CRJ 200 SRM 51-2 5-16. SUPPLEMENTAL SDR CLOSED 4/22/08. 2 L 7 2 4F RT A21EA 2008042800020 20080428 00020 NM 2008 4 28 ASAA0852820 1 20080418 A 2161 233A3101 CONTROLLER BOEING 737 737890 1384527 NM CABIN TEMP MALFUNCTIONED A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 584AS 35682 BOTH AIRCON PACKS ANNUNCIATED AFTER ENGINE START. BITE TESTED EACH TEMPERATURE CONTROLLER PER FIM 21 62 AND RESET. 2 L 7 2 4F RT A16WE 2008042800025 20080428 00025 NM 2008 4 28 BB08065 1 20080419 A 2560 LIGHT BOEING 757 7572B7 1384964 NM GIRT BAR INOPERATIVE A USAA K NONE O OTHER NR NOT REPORTED 1 EA 19 201UU 27810 CLT - THE R4 DOOR SLIDE GIRT BAR ENGAGEMENT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE PLACED THE SYSTEM ON MEL. FURTHER ACTION PENDING. 2 L 7 2 4F RT A2NM 2008042800028 20080428 00028 NM 2008 4 28 SWAA082071 1 20080418 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 247WN 32508 DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008042800030 20080428 00030 NM 2008 4 28 SWAA082072 1 20080420 A 5310 6547955 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT STR 17R. REPAIRED FRAME PER BOEING DRAWING . 2 L 7 2 4F RT A16WE 2008042800034 20080428 00034 EA 2008 4 28 SWIA200819514 1 20080115 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA WING TO BODY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 983CA 7169 LEFT FUSELAGE TO WING STIFFENER IS CRACKED AT FS473.0 AND WL72.0, FOUND AT C-CHECK. REPLACED BRACKET ANGLE PER CRJ200 S RM 51-42-06 PG 2-4 AND SRM 51-42-21 PG 15-18. 2 L 7 2 4F RT A21EA 2008042800036 20080428 00036 EA 2008 4 28 SWIA200819516 1 20080115 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 983CA 7169 FS 280 LBL 9 AND RBL 9 UPPER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED ALL REPAIR PARTS TO FS280 LBL/RBL9 U PPER FLOOR SUPPORT PER CRJ200 REO601R 53-11-136. 2 L 7 2 4F RT A21EA 2008042800037 20080428 00037 EA 2008 4 28 SWIA200819517 1 20080115 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 983CA 7169 STA 280 BEAM CRACK FOUND AT CENTER FLOORBEAM UPPER SUPPORT, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ200 SRM 51-4 2-06 PG 11. 2 L 7 2 4F RT A21EA 2008042800039 20080428 00039 NM 2008 4 28 SWAA082103 1 20080421 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 19R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008042800042 20080428 00042 NM 2008 4 28 SWAA082113 1 20080421 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042800046 20080428 00046 NM 2008 4 28 SWAA082114 1 20080421 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042800060 20080428 00060 EA 2008 4 28 SWIA200819519 1 20080115 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 983CA 7169 FS 280 AT RBL 9 LOWER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED ALL REPAIR PARTS TO RBL 9 AND FS 280 LOWER FLOOR SUPPORT PER REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2008042800063 20080428 00063 NM 2008 4 28 SWAA082121 1 20080420 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 718SW 27852 R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008042800064 20080428 00064 2008 4 28 SWAA082102 4 20080418 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 739GB 29275 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042800069 20080428 00069 NM 2008 4 28 ABXA080126 1 20080313 A 5310 141T3330 DOOR FRAME BOEING 767 767200 1385120 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 752AX 23434 R1 DOOR CUTOUT LOWER AFT CORNER INTERIOR DOUBLER HAD A .125 INCH CRACK AT THE FASTENER HOLE. REPLACED R1 DOOR CUTOUT LO WER AFT CORNER IAW REA 13653-57164-MA. 2 L 7 2 4F RT A1NM 2008042800072 20080428 00072 NM 2008 4 28 ABXA080128 1 20080313 A 5330 148T31111 SKIN BOEING 767 767200 1385120 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 752AX 23434 CRACK IN SKIN APPROXIMATELY 1.375" LONG AT FASTENER FS 1654 AT STRINGER 6 LEFT. REPAIRED AREA IAW B767 SRM 53-80-01. 2 L 7 2 4F RT A1NM 2008040400120 20080404 00120 NM 2008 4 4 08FDEA01255 1 20080402 A 5753 ARC24441 SKIN DOUG MD11 MD11F 3023600 NM TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 LEFT WING, INBOARD FLAP LOWER SKIN FOUND WITH DENT AT STA XIFH 299. DENT AREA MEASURED AND FOUND OUT OF LIMIT PER SRM 5 7-10-00 FIGURE 17 VOLUME I. REPAIR CARRIED OUT PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008040400125 20080404 00125 EU 2008 4 4 08FDEA01260 1 20080317 A 5753 A5797020020300 FLAP TRACK AIRBUS 310 A310203 3930313 EU TE FLAPS WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT FLAP VANE TRACK NR 2 IS WORN. REPAIRED RIGHT WING NR 2 FLAP VANE TRACK IAW AIRBUS CMM 57-25-15. 2 L 7 2 4F RT A35EU 2008040400128 20080404 00128 EU 2008 4 4 08FDEA01263 1 20080317 A 5753 A5797020021700 FLAP TRACK AIRBUS 310 A310203 3930313 EU TE FLAPS WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT FLAP VANE TRACK NR 4 IS WORN REPAIRED R/W NR 4 FLAP VANE TRACK IAW AIRBUS CMM 57-52-15. 2 L 7 2 4F RT A35EU 2008040400130 20080404 00130 EU 2008 4 4 08FDEA01265 1 20080317 A 5753 A5797020021400 FLAP TRACK AIRBUS 310 A310203 3930313 EU TE FLAPS WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT WING INBD FLAP VANE MID TRACK INBD SIDE HAS WORN AREA. REPAIRED NR 3 R/W FLAP VANE TRACK IAW AIRBUS CMM 57-52-15. 2 L 7 2 4F RT A35EU 2008040400142 20080404 00142 NM 2008 4 4 DL76G080444 1 20080329 A 5315 BAC1505100774 FLOORBEAM BOEING 767 7673P6 1385105 NM BS 1197 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 155DL 25269 FLOORBEAM CORRODED AT STA 1197 RBL 34. BEAM REPAIRED ON NRAVM 523371 PER SRM 52-00-07 FIGURE 201 REPAIR 4 AT HMV3. 2 L 7 2 4F RT A1NM 2008040400143 20080404 00143 NE 2008 4 4 DLM88080445 2 20080328 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 975DL 39658 53243 726088 TAKEOFF DISCONTINUED AT 100KTS BECAUSE EPR WOULD NOT RISE ABOVE 1.68 AND N1 BEGAN TO FLASH AT 102 PERCENT. REMOVED AND REPLACED NR 2 ENG EPR TRANS AND SNUBBER PER MM. COMPLETE THRU 77-11-02-201 ST 3.B.11 984600. C/W EPR IND SYS OPR NR 2 ENG PER AMM. CKS NORMAL. 2 L 7 2 4F 4 F RT A6WE E9NE 2008040400150 20080404 00150 NM 2008 4 4 DLM90080454 1 20080306 A 5311 FRAME DOUG MD90 MD9030 3023690 NM BS 1364 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 97397 53392 BS 1364 FROM LONG. 28R TO 24L THERE IS EDGE DAMAGE FROM FLOORBOARD FASTENERS (AFT CARGO BAY UNDERNEATH AFT BULKHEAD). B LENDED GOUGES, CHECKED LIMITS. OUT OF LIMITS IN SEVERAL PLACES. REMOVED SECT. OF FRAME, SPLICED NEW SECT. IN IAW MD90 SR M 51-10-10, 53-00-01, 51-3-02 AND 53-10-02D. 2 L 7 2 4F RT A6WE 2008040400152 20080404 00152 NM 2008 4 4 DLM90080456 1 20080330 A 5310 591746311 DOOR FRAME DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 97413 53392 AFT VENTRAL DOOR JAMB HAS CORROSION ON LOWER SECTION AT SEAL ATTACHMENT AREA. REPAIRED AFT VENTRAL DOOR JAMB, IAW DELTA ER/A 467131-14 REV ORIG. 03-25-08 VIA EA 12541, REV I/R 03-25-08. 2 L 7 2 4F RT A6WE 2008042100004 20080421 00004 EU 2008 4 21 2008UALA02125 1 20080414 A 2910 LINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD SYSTEM LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 428UA 523 FLIGHT DIVERTED TO DUE TO YELLOW SYSTEM HYDRAULIC LOSS. PYLON HYD LINE WAS LEAKING AT RIB 5, REPLACED PYLON HYD LINE IN NR 2 PYLON. ALSO -REPLACE NR 1 ENG HYD FILTER DUE TO SYS RUN DRY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042100005 20080421 00005 NE 2008 4 21 2008UALA02126 2 20080414 A 7261 CARBON SEAL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 ENGINE LEAKING A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 199UA 28717 717688 FLIGHT DIVERTED UNDER AMBER ALERT WITH NR 4 ENGINE SHUT DOWN DUE TO LOSS OF OIL QUANTITY. REPLACED ENGINE. SHOP TEARDO WN SHOWED OIL COKE ON THE DRY SIDE OF THE NR 1 AND 2 CARBON SEAL ASSEMBLIES. THIS SUGGESTS THAT OIL WAS LEAKING PAST THE SE SEALS DURING ENGINE OPERATION. HOWEVER, THERE WAS NO NOTABLE DAMAGE TO THESE SEALS. NO OTHER DISCREPANCIES WERE NOT ED. POOR BREATHER PRESSURE AND/OR SCAVENGING IS SUSPECTED, BUT COULD NOT BE PROVED. ALL OIL SYSTEM COMPONENTS WERE REPLA CED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042100011 20080421 00011 NM 2008 4 21 2008UALA02132 1 20080411 A 5712 RIB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 NR 1 MAIN FUEL TANK WBL 135 RIB WHERE L2 STRINGER PASSES THROUGH THE LWR CHORD ANGLE CUTOUT, CHORD IS CRACKED IN UPPER F WD RADIUS. MAJOR REPAIR ACCOMPLISHED: PERFORMED S/B REPAIR CONSISTING OF NEW "T" AND FILLER ASSY. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042100019 20080421 00019 NM 2008 4 21 2008UALA02065 1 20080409 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY EXIT EEL LIGHTS INOP, AT SEAT 17 BOTH LIGHT ASSY'S. REPLACED BATTERY. OPS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042100024 20080421 00024 NM 2008 4 21 2008UALA02070 1 20080409 A 3350 SIGN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY EXIT DISLODGED A UALA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 WP 29 563UA 26665 EMERGENCY OVERWING EXIT SIGN FELL OFF RT SIDE. ADJUSTED LATCHING MECHANISM AND REINSTALLED SIGN PLATE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042100030 20080421 00030 NM 2008 4 21 2008UALA02075 1 20080409 A 2425 M832481210 O-RING BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GENERATOR FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 226UA 30226 ELEC BACKUP GEN L LEFT BACKUP GENERATOR OFF DUE TO A PROTECTIVE TRIP. STATUS MSG03, ACTIVE CRUISE MODE DEPENDENT; BACK UP GENERATOR (L) SPEED IS OUT OF RANGE. SUSPECT FAULTY BEARING. REPLACED BACK UP GEN. AND DRIVE OIL SEAL. PER AMM 24-2 5-01 OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042100033 20080421 00033 NM 2008 4 21 2008UALA02078 1 20080409 A 3600 PNEUMATIC SYSTEM BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CONTAMINATED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 668UA 30024 DURING ENGINE START LEFT ENGINE GOT CAUTION: L ENG PRV WITH LEFT BLEED LIGHT. AFTER EXTENSIVE TROUBLE SHOOTING OF LT PN EUMATIC SYSTEM. FOUND WATER INSIDE OF SENSE LINE PORT OF OVER PRESSURE SWITCH. REPLACED OVER PRESSURE SWITCH PER MM 36-2 1-03. ALSO COMPLETED OPS CHECK OF SWITCH NO DEFECTS NOTED. RAN ENGINE FOR 5 MINUTES NO FAULTS. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT A1NM E24NE 2008042800073 20080428 00073 NM 2008 4 28 ABXA080129 1 20080314 A 5314 145T8611 KEELBEAM BOEING 767 767200 1385120 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 752AX 23434 LOWER RIGHT KEEL BEAM CORD APPROXIMATELY STA 1030 - CORRODED. BLENDED CORROSION ON LOWER RIGHT KEEL BEAM STA 1030 IAW B 767 SRM. 2 L 7 2 4F RT A1NM 2008042800084 20080428 00084 EU 2008 4 28 08FDEA01525 1 20080424 A 5415 A5461139320400 ATTACH ANGLE AIRBUS 300 A300F4605R 3930327 EU NR 2 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 NR 2 PYLON ATTACH ANGLE AND RIB 3-A (OUTBD) IS CRACKED. REMOVED SHIM IAW A300-600 SRM 51-40-21 PG 7. PART IS IDENTIFI ED AS A SHIM WITH A CRACK 1 INCH LONG IAW SRM 54-52-31 FIG 2 ITEM 15. FABRICATED SHIM. SHIM IS INSTALLED IAW SRM 51-4 0-2 PG 7. 2 L 7 2 4F RT A35EU 2008042800095 20080428 00095 NM 2008 4 28 ABXA080137 1 20080313 A 5330 141T83207 SKIN BOEING 767 767200 1385120 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 752AX 23434 L1 DOOR CUTOUT LOWER AFT CORNER INTERIOR DOUBLER HAD 2 EACH .25 INCH CRACKS AT THE FASTENER HOLE AND THE EXTERIOR SKIN H AD A .125 INCH CRACK AT SAME HOLE. REPAIRED L1 DOOR CUTOUT LOWER AFT CORNER IAW REA B653-57165-MR. 2 L 7 2 4F RT A1NM 2008042800098 20080428 00098 2008 4 28 2008UALA02409 4 20080423 A 2565 D31393109 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT OVERWING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 LT OVERWING ESCAPE SLIDE FOUND UNLACED. REPLACED EMERGENCY SLIDE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042800100 20080428 00100 NM 2008 4 28 HALA0800544 1 20080423 A 5280 DOOR BOEING 717 717200 1383700 NM MLG DAMAGED A HALA O OTHER O OTHER LD LANDING 1 WP 13 475HA 55121 RT MLG OUTBOARD DOOR AFT STAINLESS STEEL EDGE DENTED BETWEEN 6" AND 14" FROM TOP EDGE. ALL LDG GEAR PINS INSTALLED AND SAFETY WIRED. REMOVED AND REPLACED RT MLG OUTBD DOOR SEAL. INSTALLED NOSE LANDING GEAR DOOR PER AMM TASK 32-14-0-400-8 01. ADJUSTMENT ACCOMP PER AMM 32-10-00. FUNCTIONAL AND TEST OF MAIN AND NOSE LANDING GEAR EXTENSION AND RETRACT PER AM M 32-30-00. OPS CK GOOD. 2 L 7 2 4F TR A6WE 2008042800106 20080428 00106 NM 2008 4 28 HALA0800538 1 20080420 A 2612 89873202 CIRCUIT CARD BOEING 767 76733A 1385209 NM FIRE DETECTION INOPERATIVE A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 ETOPS SIGNIFICANT SYSTEM, APU NR 2 FIRE LOOP APPEARS ON EICAS PAGE. REMOVED AND REPLACED APU FIRE OVERHEAT DETECTION CA RD PER AMM 26-10-01, OPS CK GOOD. 2 L 7 2 4F RT A1NM 2008042800112 20080428 00112 NM 2008 4 28 HALA0800534 1 20080419 A 4990 1589353 VALVE BOEING 767 7673G5 1385126 NM OIL COOLER MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 584HA 24258 ETOPS SIGNIFICANT SYSTEM, APU AUTOSHUT DOWN AT GATE. PERFORMED APU BITE PROCEDURE PER 49-11-00. FOUND HIGH OIL TEMP FA ULT. PERFORMED FIM "HIGH OIL TEMP" 49-11-00. REMOVED AND REPLACED OIL COOLER BYPASS VALVE PER 49-27-10. RESERVICED AP U. GROUND RUN APU AND LEAK CHECK GOOD. 2 L 7 2 4F RT A1NM 2008042800113 20080428 00113 EA 2008 4 28 A6WA200840259 1 20080324 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 FS 484, LBL 36 FLOOR SUPPORT ANGLE FOUND CRACKED LENGTH OF CRACK IS .880 INCH. (M) FS 484.00, LBL 36, FLOOR SUPPORT ANG LE REPAIRED IAW REO 601R-53-41-059, REV A. (K) 2 L 7 2 4F RT A21EA 2008042800116 20080428 00116 EA 2008 4 28 A6WA200840262 1 20080325 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 RIGHT WING INBOARD L/E OUTSIDE UPPER RIB CORRODED WS 148. CORROSION REMOVED IAW SRM 51-21-06. (M) 2 L 7 2 4F RT A21EA 2008042800129 20080428 00129 NM 2008 4 28 CALA0800351 1 20080422 A 5320 652072619 ANGLE BOEING 737 737524 1384721 NM CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 FWD CARGO FWD RIGHT Z-ANGLE (FWD OF DOOR) HAS CORROSION ON BOTTOM SIDE AT NUT PLATE. REMOVED AND INSTALLED FWD CARGO FW D RIGHT Z-ANGLE FWD OF DOOR PER SRM 53-00-04 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008042800132 20080428 00132 NM 2008 4 28 CALA0800354 1 20080424 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 CABIN STA 907 BETWEEN S8R AND S9R PASSENGER SERVICE UNIT (PSU) RAIL ATTACH BRACKET TO FRAME CRACKED. FRAME REPAIRED AT STA 907 BETWEEN S8R-S9R PSU RAIL ATTACH BRACKET, PER EA5310-04498, STEPS 8 -18. 2 L 7 2 4F RT A16WE 2008042800133 20080428 00133 NM 2008 4 28 SWAA082128 1 20080421 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 223WN 32492 DURING SCHEDULED MV1 CHECK, FOUND LT MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008042500040 20080425 00040 SO 2008 4 25 FDKA200804159 1 20080411 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 FDM FLT 5976 CVG- PVD (1155 PHX LCL). EMERGENCY EXIT MARKER OUT (LT OVERWING). MX SECURED CONNECTOR AND OPS CHECKED GO OD. 2 L 7 2 4T RT T00011AT 2008042500044 20080425 00044 SO 2008 4 25 FDKA200804163 1 20080412 A 5210 LATCH EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 FDM FLT RON ORF (1816 PHX LCL). MAIN CABIN DOOR HARD TO CLOSE. MX LUBED DOOR LATCH, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008042500055 20080425 00055 SW 2008 4 25 MT92008F00000 1 20080222 A 2752 196002 ACTUATOR SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE331* 01514 WP RT FLAP SYS CRACKED E MT9A O OTHER O OTHER NR NOT REPORTED 1 SW 05 370AE 448 AC506 AC WAS ON A TRAINING FLIGHT IN THE LANDING PATTERN AT AROUND 2130 HOURS. THE TRAINING OFFICER NOTICED THE HYD PRESSURE GOING BETWEEN 400 AND 1800 PSI. HE SELECTED GEAR DOWN AND VERIFIED 3 GREENS BUT MINIMUM PRESSURE WAS LOW. THE CREW SEL ECTED EMERGENCY GEAR EXTENSION AND USED THE HAND PUMP TO BOOST PRESSURE WAS LOW. THE CREW SELECTED EMERGENCY GEAR EXTEN SION AND USED THE HAND PUMP TO BOOST PRESSURE TO 1200 PSI, MIN PRESSURE. AC THEN COMPLETED A ZERO FLAP LANDING AND RETU RNED TO RAMP. HYD PRESSURE NEVER WENT TO ZERO AND NO EMERGENCY WAS DECLARED. MAINT FOUND A HYD LEAK AT THE CENTER SHAF T OF THE RT FLAP ACTUATOR. AFTER REMOVAL FROM THE AC, IT WAS DISCOVERED THAT THE RT FLAP ACTUATOR HOUSING HAD A 2.5 INC 2 L 7 2 4T 3 T RT A8SW E2WE 2008042500094 20080425 00094 SW 2008 4 25 EVCA200841008 1 20080410 A 6330 206033554101 LINK BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL TRANSMISSON BROKEN E EVCA R AUTOROTATION E VIBRATION/BUFFET NR NOT REPORTED 1 CE 03 89AE 8 45433 FAILURE OF THE LT REAR TRANSMISSION LINK IN FLIGHT. HEARD NOISE AUTOROTATION TO A SAFE LANDING IN FIELD. INVESTIGATION SHOWED THE LINK HAD SEPARATED, TRANS UP STOP HELD. 1 G 7 1 3U 3 U H2SW E1GL 2008042500096 20080425 00096 NM 2008 4 25 NOCA02208 1 20080417 A 3350 BPS73 POWER SUPPLY BOEING 757 75728A 1384976 NM CABIN DISCHARGED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 756NA 32448 R2 DOOR INTERIOR EMERGENCY LIGHTS INOP AT THE MIDDLE OF THE DOOR. FOUND POWER SUPPLY M732 AT FAULT. REMOVED AND REPLAC ED POWER SUPPLY BY R2 DOOR (M732) IAW MM 3-51-07. OPS CHECKED NORMAL. 2 L 7 2 4F RT A2NM 2008042500103 20080425 00103 NM 2008 4 25 HNAA0800136 1 20080318 A 5414 85411436001 ACCESS PANEL DHAV DHC8 DHC8102 2809003 NM DAMAGED A HNAA O OTHER A FLAME/FIRE IN INSP/MAINT 1 EA 07 815EX 39914 39914 321 DURING INSPECTION AFTER INFLIGHT FIRE, ACCESS PANEL 419AT WAS FOUND TO HAVE FIRE DAMAGE. MAINTENANCE REPLACED THE PANEL . 2 H 7 2 4T RT A13NM 2008042500104 20080425 00104 NM 2008 4 25 NOCA02408 1 20080420 A 3350 BPS73 POWER SUPPLY BOEING 767 76736N 1385152 NM CABIN DISCHARGED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 768NA 29898 E-PATH LIGHTS FROM L2 DOOR TO ROW 19 INOP. REMOVED AND REPLACED POWER SUPPLY IAW AMM 33-51-7, OPS CHECKED OK. 2 L 7 2 4F RT A1NM 2008042500117 20080425 00117 NM 2008 4 25 CALA0800339 1 20080419 A 3350 276005 FUSE AD20131A BOEING 737 737524 1384721 NM BATTERY PACK BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 62631 27535 AISLE PATH LIGHTING INOP, BETWEEN OVERWING HATCH AND STA 727C. FOR SDR REPORTING. FUSE IN POSITION 3 ON LEFT HAND POWE R SUPPLY AT ROW 19 BAD. REMOVED AND REPLACED FUSE IAW B737-500MM CHAPTER 33-51-51, OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 2008042500130 20080425 00130 SO 2008 4 25 C2XA08CL052 1 20080420 A 3350 P2070005120 BRACKET EMB 145 EMB145LR 3260212 SO CABIN FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16571 145633 CLE FLIGHT 2866 - THE CREW REPORTED THE FORWARD CABIN FLASHLIGHT WAS NOT CHARGING. MAINTENANCE REPLACED THE FORWARD CAB IN FLASHLIGHT BRACKET. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008042500131 20080425 00131 GL 2008 4 25 DXTA200802990 2 20080412 A 7200 ENGINE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL LT ENGINE SMOKE E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 982QS 7500182 IMMEDIATELY AFTER TAKEOFF SMELLED AND SAW SMOKE IN THE COCKPIT MOVING FROM LT TO RT ACROSS THE PILOT'S SEAT. REMOVED AN D REPLACED LT ENGINE IAW 750 MM 71-00-03 & MM 72-00-00. OPS & LEAK CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008042500132 20080425 00132 EA 2008 4 25 MASA200800323 1 20080417 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A MASA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 07 593ML 7465 ASH 7167 ORD-GSO - FLAP FAIL WHILE IN CRUISE AT FLAPS ZERO. DECLARED AN EMERGENCY AND LANDED IN GSO WITHOUT INCIDENT. MX COMPLIED WITH THE FLAP FAIL INSPECTIONS AND COMPLIED WITH PART A. 2 L 7 2 4F RT A21EA 2008042500146 20080425 00146 EA 2008 4 25 TRAX200800552 1 20080416 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 FS 280 FRAME UPPER AFT ANGLE CRACKED AT RBL 12.0. JOB COMPLETE. STARTED REMOVING FS 280 UPPER ANGLE AT RBL 12.0 PER CR J 200 SRM 51-42-20. REPAIRED J-ANGLE ON THE PILOT`S BULKHEAD AT FS 280.0 RT BL 9.0 IAW EO 600-53-0091. PERFORMED ET IN SPECTION OF CUT LINES AT FS 280 IAW REO 601R-53-11-136 PER CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. 4/18/08. FABRICAT ED -3 AND -4 SPLICE ANGLES OUT OF 7075 -0 .050" BATCH 511928, PO 20040439. HEAT TREATED -3 & -4 SPLICE ANGLES TO +62 CO NDITION AS PER CRJ 200 SRM 51-24-06 IAW REO 601R-53-11-136. HARDNESS TEST GOOD. FINAL TRIMMED, DRILLED, AND FINISHED - 3, -4, AND -1 REPAIR PARTS IAW REO 601R-53-11-136. OK TO INSTALL. INSTALLED ALL 280 REPAIR PARTS INCLUDING RBL 9 INBOA 2 L 7 2 4F RT A21EA 2008042500159 20080425 00159 SO 2008 4 25 C2XA08SH070 1 20080422 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13202 14500962 SHV - DURING C-CHECK CORROSION ON CENTER OMEGA BEAM AT FR 20. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FR 20 IAW EM B 145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008042500161 20080425 00161 NM 2008 4 25 NOCA02508 1 20080422 A 3350 1317 LIGHT BOEING 767 767304 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 769NA 28039 RIGHT HAND AISLE BY ROW 36 CEILING EMERGENCY LIGHT INOP. REPLACED BULB IAW 33-50-00. 2 L 7 2 4F RT A1NM 2008042500162 20080425 00162 NM 2008 4 25 CALA0800346 1 20080421 A 5320 654580730 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 INTERCOSTAL CRACKED STA 291.5 BELOW STR 13R. REMOVED AND REPLACED INTERCOSTAL REF SRM 51-40-05 AND SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008042500171 20080425 00171 NM 2008 4 25 2008UALA02318 1 20080419 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 55R INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 55 RIGHT. SUPPLEMENTAL, REPLACED LIGHT ASSY. OPS CHKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500173 20080425 00173 NM 2008 4 25 2008UALA02319 1 20080419 A 3350 89151114 OXYGEN SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE PASSENGER READS LOW A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 PASSENGER O2 SHOWS 1520. SERVICED O2 SYSTEM TO FULL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500198 20080425 00198 SO 2008 4 25 C2XA08IA115 1 20080419 A 3350 LIGHT EMB 145 EMB145XR 3260214 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11150 145756 FLIGHT 2383, DURING PREFLIGHT INSPECTION THE CREW REPORTED, ROW 12 OVERHEAD EMERGENCY LIGHT EXIT SIGN NOT LIGHTING UP. MAINTENANCE RESET THE EMERGENCY LIGHT SYSTEM, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. 2 L 7 2 4F RT 2008042100036 20080421 00036 NM 2008 4 21 2008UALA02137 1 20080411 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 813UA 858 AFT OVERHEAD EMERGENCY EXIT LIGHT ON W-SWITCH IN OFF POSITION. FOUND EPSU FAILED. REPLACED AFT L EPSU AND BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042100040 20080421 00040 NM 2008 4 21 2008UALA02141 1 20080412 A 2700 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE UNKNOWN A UALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 WP 29 806UA 788 UNCOMMANDED DUTCH ROLL DURING ENTIRE APPROACH. ACCOMPLISHED AILERON DAMP ING CHECK, POWERED UP SYSTEM AND CHECKED SPOI LERS FOR FLOAT, EFC S CHECK,CAT 3 CHECK COMPLETED, NO MSG OR FAULTS FOUND, REPLACED BOTH FAC 1 AND 2 AS PRECAUTIONARY. THIS EVENT NEVER REPEATED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042100044 20080421 00044 EA 2008 4 21 A6WA200840244 1 20080318 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 439AW 7753 CRACK EXIST ON INTERCOSTAL FS 484 RBL 36. REPAIRED IAW REO 601R-53-41-059 REV A. (M) 2 L 7 2 4F RT A21EA 2008042100055 20080421 00055 NM 2008 4 21 2008UALA02014 1 20080407 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 490 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 CABIN CREASE BEAM INNER CHORD NEEDS CUT TO FROM BS 490 STR 17R. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED: RE PAIRED SECTION OF CREASE BEAM CUT TO FACILITATE CARGO PIT DOOR FRAME REPLACEMENT, CONSISTING OF NESTED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042100057 20080421 00057 NM 2008 4 21 2008UALA02019 1 20080408 A 5310 STRUCTURE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 809UA 825 FOUND SHEAR WEB SUPPORT STRUCTURE UNDER WEB BETWEEN FR 69 AND FR 70 CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR AC COMPLISHED, REMOVED SHEAR WEB. REPLACED SHEAR PLATE SUPPORT STRUCTURE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042100058 20080421 00058 NM 2008 4 21 2008UALA02020 1 20080408 A 5320 WEB AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 809UA 825 FOUND RT FLOOR SHEAR PLATE CORRODED BETWEEN FR 69 AND 70. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED, REMOVED B EAM. REPLACED SHEAR PLATE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042100064 20080421 00064 NM 2008 4 21 CALA0800314 1 20080408 A 5310 652072366 DOOR FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 46625 27529 FWD CARGO DOOR CUTOUT AFT FRAME HAS 1 INCH CRACK, AT BOTTOM DOOR STOP PAD FOOT PRINT. REMOVED & REPLACED FWD CARGO DOOR CUTOUT AFT FRAME REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008042100067 20080421 00067 EA 2008 4 21 COMA0870015 1 20080406 A 3080 GG43640067 DETECTOR CNDAIR CL600 CL6002C10 1390015 EA ICE DETECTION FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 641CA 11897 10122 FLIGHT 5086 - DURING TAKEOFF ROLL RECEIVED AN ICE CAUTION MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED T HE LEFT ICE DETECTOR. 2 L 7 2 4F RT A21EA 2008042100072 20080421 00072 EA 2008 4 21 COMA0860210 1 20080405 A 2750 601R930507 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 989CA 25411 7215 FLIGHT 5163 - EN ROUTE CVG-FSD PRIOR TO APPROACH RECEIVED A FLAPS FAIL CAUTION, CREW DECLARED AN EMERGENCY AND FLIGHT LA NDED WITHOUT INCIDENT. REPLACED THE FLAP ELECTRONIC UNIT. 2 L 7 2 4F RT A21EA 2008042100075 20080421 00075 NM 2008 4 21 CALA0800322 1 20080411 A 3300 251005 FUSE BOEING 767 767224 1385170 NM BATTERY CHARGER BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 73152 30431 PATH WAY AISLE LIGHT INOP 3D AND ROWS 29 THROUGH 37 AND 20/21/22 D FOUND FUSES AT BATTERY POWER SUPPLY BURNED AND CONNEC TIONS PLUGS LOOSE AT SEATS 29 TO 37. 2 L 7 2 4F RT A1NM 2008042100079 20080421 00079 NM 2008 4 21 CALA0800317 1 20080410 A 5210 507945 PAN BOEING 737 737524 1384721 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 46625 27529 L1 DOOR PAN CRACKED AT AFT EDGE AROUND NR 5 STOP PIN BRACKET FROM BOTTOM. INSTALLED REPAIR ANGLE REF ECRA 5210-02014. 2 L 7 2 4F RT A16WE 2008042100083 20080421 00083 NM 2008 4 21 CALA0800296 1 20080402 A 5315 141T5108 FLOORBEAM BOEING 767 767424ER 1385270 NM BS 325 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76055 29450 CABIN - STA 325, LBL 24-46 FLOOR SUPPORT FOUND CORROSION. CABIN STA 325, FLOOR BEAM LBL 63" TO RBL 59" REPAIRED AS PER SRM 53-00-51 REPAIR FIG 201, HFEC NO CRACK FOUND. 2 L 7 2 4F RT A1NM 2008042100100 20080421 00100 EA 2008 4 21 COMA0860221 1 20080408 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 938CA 32500 7046 FS 280 BEAM COCKPIT/CABIN FLOORBOARD SUPPORT BRACKETS CORRODED. REPAIRED CORROSION IAW EA 10-5310-02156. 2 L 7 2 4F RT A21EA 2008042100105 20080421 00105 NM 2008 4 21 UPS08M51972 1 20080125 A 5711 SPAR DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48455 INSPECTION TYPE:C LEFT WING FIXED WING FRONT SPAR ENCLOSURE APPROX STA XORS 506 UPPER SKIN FOUND CRACKED. CRACKED AREA TRIMMED OFF AS PER SRM 57-10-00 FIG.27V.1R.40. HFEC C/OUT IAW DA CNDTSPM R.13 PART 06-10-01.001, FOUND NO CRACK EVIDENT . REP ANGLES FAB USING 7075-0-0.063 MATL PER SRM 57-10-00 FIG 27 V.1R.40. REP ANGLES HEAT TREATED TO T6 COND PER DPS7. 00-1 & HARDNESS OBTAINED HRB79.1, ACCEPTABLE PER DPS1-05-3. REP PARTS PROTECTED PER SRM 51-21-01V.2R.40. OK TO INSTALL . 2 L 7 3 4F RT A22WE 2008042100107 20080421 00107 NM 2008 4 21 CALA0800332 1 20080405 A 5320 65C3397335 INTERCOSTAL BOEING 737 737524 1384721 NM BS 312-328 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 INTERCOSTAL FOUND CRACKED BETWEEN BS 312 TO BS 328 AT LBL 44". REMOVED AND REPLACED DAMAGED INTERCOSTAL BS 312-328, REF SRM 51-40-02 & BOEING INSTALLATION DWG 65C33970. 2 L 7 2 4F RT A16WE 2008042500217 20080425 00217 NM 2008 4 25 SWAA082083 1 20080418 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 465WN 33829 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042500233 20080425 00233 NM 2008 4 25 SWAA082100 1 20080419 A 5753 113A270021 SKIN BOEING 737 7377H4 1384404 NM T/E FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 726SW 27858 DURING SCHEDULED SPV CHECK, FOUND LT WING INBOARD T/E AFT FLAP LOWER SURFACE DISBONDED. REMOVED AND REPLACED FLAP PER M M. 2 L 7 2 4F RT A16WE 2008042500235 20080425 00235 NM 2008 4 25 2008UALA02327 1 20080418 A 2810 VENT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE WING FUEL LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 194UA 26892 AIRCRAFT HAD 2 MAJOR FUEL SPILLS OUT OF RT WING VENT WHILE DEFUELING TO FERRY. ALL WING TANKS WERE FULL AT THE TIME EXC EPT CENTER WHICH WAS BEING PUMPED OUT. PROBLEM HAS TO BE FUEL LEAKING INTO A TANK, NOT VTO PROBLEM. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500242 20080425 00242 2008 4 25 2008UALA02334 4 20080421 A 2565 BOTTLE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L1 DOOR SLIDE READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 LOW BOTTLE. SUPPLEMENTAL, FILLER VALVE LOOSE. TIGHTENED FILLER VALVE AND TOPPED OFF CYLINDER. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042500263 20080425 00263 NM 2008 4 25 2008UALA02354 1 20080422 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 50R INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT EEL LIGHT INOP AT ROW 50 RIGHT. FOUND LOOSE CONNECTION. SECURED CONNECTION LIGHT OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500273 20080425 00273 NM 2008 4 25 2008UALA02364 1 20080421 A 3397 80172424 FEEDER CABLE BOEING 777 777222 1385219 NM EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 204UA 28713 SEAT 2E BOTH EEL LTS INOP. DURING TROUBLESHOOT, FOUND UNDER SEAT PWR CABLE FOR BOTH SEATS FAILED. REPLACED THIS CABLE. OP CHKS OKAY. 2 L 7 2 4F RT T0001SE 2008042500301 20080425 00301 NM 2008 4 25 2008UALA02388 1 20080422 A 3350 176435Y767 PCU BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS SHORTED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 660UA 27115 PAX COMMENTS BLUE SPARKS SEEN FROM AROUND THE SIDES OF SEAT 24E PCU ARMREST WHILE CHANGING CHANNELS. NO SMOKE OR ODOR N OTED BY FLT ATTENDANT. REPLACED DIGITAL PCU. NO OTHER WIRES FOUND CHAFED OR BAD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042500305 20080425 00305 NM 2008 4 25 KNNA20080007 1 20080424 A 5314 KEELBEAM BOEING 737 7372L9 1384497 NM PWA JT8 JT8D9A 52048 NE BS 727 CORRODED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 464AT 21278 AFTER OPEN UP FOUND CORROSION AT RT KEEL BEAM AT STA 727, AREA WENT OUT OF LIMITS AFTER CORROSION REMOVAL. REPAIRED ARE A IAW BOEING MESSAGE 1-522105282 AND IAW SKY KING ACO-0753105. 2 L 7 2 4F 4 F RT A16WE E2EA 2008042500310 20080425 00310 NM 2008 4 25 2008UALA02408 1 20080423 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 848UA 1647 CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. CREW COMMENTS, O2 WAS 1460 AT PUSHBACK AND 1300 AT START O F DESCENT AFTER 5 HOURS. FOUND LEAKAGE AT LOWER FITTING OF BOX. REPLACED BOX, PERFORMED LEAK CHECK AND SERVICE SYSTEM TO FULL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042500317 20080425 00317 NM 2008 4 25 SWAA082186 1 20080423 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042500318 20080425 00318 NM 2008 4 25 SWAA082189 1 20080423 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042500319 20080425 00319 NM 2008 4 25 SWAA082190 1 20080423 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042500320 20080425 00320 NM 2008 4 25 SWAA082146 1 20080422 A 3350 101331 LENS BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2008042800029 20080428 00029 2008 4 28 SWAA082069 4 20080415 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 295WN 32541 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042800038 20080428 00038 NM 2008 4 28 SWAA082073 1 20080420 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 485, STR 26R. REPAIRED SKIN PER ACO. 2 L 7 2 4F RT A16WE 2008042100109 20080421 00109 EA 2008 4 21 COMA0860212 1 20080406 A 3040 16591 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA WINDSHIELD HEAT FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 963CA 28570 7127 FLIGHT 5620 - EN ROUTE CVG-YUL RECEIVED A LEFT WINDSHIELD CAUTION MESSAGE, FLIGHT RETURNED TO CVG. REPLACED THE LEFT WI NDSHIELD HEAT CONTROLLER. 2 L 7 2 4F RT A21EA 2008042100110 20080421 00110 EA 2008 4 21 COMA0860213 1 20080406 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN NO TEST A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 965CA 7131 FLIGHT 5027 - THE AFT EMERGENCY EXIT FLOOR LIGHTS FAILED TO TEST. DEFERRED PER MEL 33-51-01-6. 2 L 7 2 4F RT A21EA 2008042100112 20080421 00112 NM 2008 4 21 HNAA0800129 1 20080407 A 3350 6013211X BATTERY PACK DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS INOPERATIVE A HNAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 07 975HA 18690 149 176 OVERHEAD CENTER AISLE E-EXIT SIGN ROW 4 INOP ON FORWARD SIDE. REMOVED AND REPLACED BATTERY PACK NR 6, OPS CHECK GOOD IA W 33-51-01. 2 H 7 2 4T RT A13NM 2008042100115 20080421 00115 EA 2008 4 21 COMA0860220 1 20080410 A 5240 601R313613 DOOR SEAL CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR TORN A COMA B EMER. DESCENT O OTHER CR CRUISE 1 SO 01 963CA 7127 FLIGHT 5689 - EN ROUTE MHT-CVG THE SERVICE DOOR SEAL FAILED TO HOLD PRESSURIZATION AS INDICATED BY SEAL NOISE, CREW DECL ARED AN EMERGENCY AND DIVERTED TO ALB. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE SERVICE DOOR SEAL. 2 L 7 2 4F RT A21EA 2008042100117 20080421 00117 NM 2008 4 21 CALA0800326 1 20080407 A 5340 69414372 STRINGER CLIP BOEING 737 737524 1384721 NM BS 663 S10R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 MAIN CABIN STRINGER CLIP CRACKED AT STA 663 AND S10R. REPLACED STRINGER TIE CLIP AT STA 663R AND STR 10R IAW SRM 51-10- 2 (B737-500) AND SRM 51-40-02 (B737-500). 2 L 7 2 4F RT A16WE 2008042100118 20080421 00118 NM 2008 4 21 CALA0800327 1 20080413 A 5330 6545774 SKIN BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 LEFT AFT FUSELAGE- 8" AFT OF EMERGENCY LIGHT, 2.5 INCH LONG CRACK IN SKIN. REPAIRED PER SRM 53-00-01 REPAIR 31, PROCEDU RE 5, INITIATED DIP TO INSPECT EVERY 4,000 FLIGHT CYCLES AFTER INITIAL SCHEDULED INSPECTION. 2 L 7 2 4F RT A16WE 2008042100121 20080421 00121 EA 2008 4 21 COMA0870014 1 20080406 A 3080 GG43640067 DETECTOR CNDAIR CL600 CL6002C10 1390015 EA ICE DETECTION FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 641CA 11897 10122 FLIGHT 5086 - DURING TAKEOFF ROLL RECEIVED AN ICE CAUTION MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED T HE RIGHT ICE DETECTOR. 2 L 7 2 4F RT A21EA 2008042100128 20080421 00128 NM 2008 4 21 08FDEA01456 1 20080418 A 3230 ARG733501 TORQUE LINK DOUG MD11 MD11F 3023600 NM LT MLG SHEARED A FDEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 574FE 48499 LEFT MAIN LANDING GEAR TORQUE LINK SHEARED DURING PUSH-BACK. 2 L 7 3 4F RT A22WE 2008042100135 20080421 00135 NM 2008 4 21 QXEA200800387 1 20080417 A 6123 699018002 PCU BOMBDR DHC8 DHC8402 1390042 NM AUTOFEATHER SYS FAILED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 409QX 7485 4051 SEA - FLIGHT 2357. ON TAKEOFF, THE AUTOFEATHER SYSTEM DID NOT ARM. ABORTED TAKEOFF AT 91 KNOTS AND RETURNED TO THE GATE . MAINTENANCE REPLACED THE NR 2 PECU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008042100136 20080421 00136 NM 2008 4 21 QXEA200800386 1 20080417 A 6123 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM NR 2 MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 409QX 4051 SEA- FLIGHT 2250. DURING THE PILOT DAILY CHECK OF THE AUTOFEATHER SYSTEM, THE NR 2 SYSTEM TEST FAILED. MAINTENANCE FOUN D CODE 402A AND CLEARED CODES IAW 61-20-00-710-804. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS R EPLACED. 2 H 7 2 4T RT A13NM 2008042100141 20080421 00141 EU 2008 4 21 NWAA081633212 1 20080407 A 5320 SILL AIRBUS 320 A320211 3930320 EU FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 312US 152 DURING "H" CHECK, FOUND SURFACE CORROSION ON AFT LT PASSENGER DOOR SILL AT FR 66. REPAIRED PER EA 32-212484. 2 L 7 2 4F RT A28NM 2008042100142 20080421 00142 2008 4 21 HALA08000530 4 20080418 A 2210 285T1122102 MODULE BOEING 767 76733A 1385209 NM STABILIZER TRIM FAULTY A HALA O OTHER O OTHER CR CRUISE 1 WP 13 HA587 33421 UNSCHEDULED STAB TRIM MESSAGE APPEARED INTERMITTENTLY. DISPLAYED FOR FEW SECONDS THEN DISAPPEARED. NIL MOVEMENT EVIDENT IN STAB TRIM GAUGE NIL EFFECT ON AIRCRAFT. NIL EXISTING FAULT, FOP M838 REPLACED IAW AM 27-58-01 IN P50 CARD FILE, MAD TEST 4/65 CHECKED OUT SATISFACTORY. ALSO 'L' Y/DAMPER STAB TRIM MODULE REPLACED OK IAW AM 22-21-04, STAB TRIM OPS CHEC K SATISFACTORY. NIL MESSAGE EVIDENT RAY ALSO CHECKED OUT OK. Y/DAMPER STAB TRIM MODULE REPLACED SATISFACTORY IAW AM 22- 21-04. NIL MSG EVIDENT STAB TRIM OPERATES SATISFACTORY. 2 L 7 2 4F RT A1NM 2008042100144 20080421 00144 SO 2008 4 21 SWIA200819482 1 20080228 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 251YV 120251 LEFT WING FUEL PANEL NR 10 HAS A CRACKED STRINGER, FOUND AT C-CHECK. COMPLIED WITH STRINGER REPAIR IAW EMB 120 SRM 57-2 0-03. 2 L 7 2 4T RT A31SO 2008042100145 20080421 00145 SO 2008 4 21 SWIA200819483 1 20080228 A 5310 WINDOW POST EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 251YV 120251 CAPTAINS FORWARD WINDOW POST IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS ON WINDOW POST IAW SB 120-53-0072. 2 L 7 2 4T RT A31SO 2008042100147 20080421 00147 EA 2008 4 21 SWIA200819485 1 20080415 A 3520 OXYGEN MASK CNDAIR CL600 CL6002C10 1390015 EA LAVATORY UNWANTED DEPLOY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 606SK 10250 FLT 4001, FORWARD LAV O2 MASK DEPLOYED. INSPECTED AND STOWED O2 MASK IAW AMM 35-20-00. 2 L 7 2 4F RT A21EA 2008042300004 20080423 00004 2008 4 23 USAA920080904 4 20080418 A 2565 D31354437 SLIDE BOEING 737 7373B7 1384580 NM LT SERVICE DOOR LOW A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 512AU 49520 1571 23595 FLT NR 9186 PIT - EES - AFT LT SERVICE DOOR SLIDE HAS LOW PRESSURE. MAINTENANCE REMOVED AND REPLACED THE AFT LT SERVICE DOOR SLIDE. 2 L 7 2 4F RT A16WE 2008042300006 20080423 00006 NM 2008 4 23 2008UALA02176 1 20080415 A 5280 SKIN BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT MLG DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 670UA 29240 LT MLG LWR FWD CORNER OF TRUNNION DOOR SKIN BENT AND PULLED FROM DOOR STRUCTURE AND UPPER FWD EDGE OF STRUT DOOR SKIN DA MAGED. REMOVED TRUNNION DOOR. FOUND LT MLG TRUNNION DOOR BENT. SENT TO SHOP AND PERFORMED SHEET METAL REPAIR. REINSTALL ED TRUNNION DOOR RH GEAR. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042300016 20080423 00016 NM 2008 4 23 2008UALA02208 1 20080415 A 2432 18550000 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE MASTER FAULTY A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 655UA 25393 MAIN BATTERY CHARGER STATUS MSG. SUSPECT FAULTY BATTERY. REPLACED MAIN BATTERY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042300017 20080423 00017 EA 2008 4 23 MASA200800300 1 20080408 A 2510 JUMPSEAT CNDAIR CL600 CL6002B19 1900309 EA CABIN LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37178 7178 ASH FLT 2881 PHX - ELP. F/A JUMP SEAT HARD TO MOVE FROM AND TO STOW. MX LUBED THE F/A JUMP SEAT, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008050600006 20080506 00006 EU 2008 5 6 08FDEA01660 1 20080411 A 5210 F5218221400000 ARM AIRBUS 300 A300B4622R 3930312 EU PAX DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 LT PAX DOOR SUSPENSION LOWER ARM (PN 5211134600000) WITH CORROSION ON JUMPER HOLE. THE ARM WAS REPLACED IN ACCORDANCE W ITH AMM 52-10-12. 2 L 7 2 4F RT A35EU 2008042300023 20080423 00023 EA 2008 4 23 MASA200800303 1 20080410 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH 2825 PHX - ONE CABIN EMERGENCY EXIT LIGHT INOP. MX RESECURED A LOOSE CONNECTOR ON THE LIGHT ASSY. 2 L 7 2 4F RT A21EA 2008042300027 20080423 00027 EA 2008 4 23 MASA200800304 1 20080410 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 649BR 7414 ASH FLT 7058 GRR - ORD. CAPT REPORTED THE SERVICE DOOR WAS HARD TO OPEN FROM THE INSIDE. MX TROUBLESHOT AND FOUND THE DOOR TO OPERATE NORMALLY. 2 L 7 2 4F RT A21EA 2008042300033 20080423 00033 EU 2008 4 23 F3LA200800187 1 20080406 A 5321 D5367179900000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 221PF LAV A HAS CORROSION ON BOLT HOLES. MAINTENANCE RECEIVED NEW FLO OR PANEL 221PK, OKAY TO INSTALL AND INSTALL WILL BE ACCOMPLISHED ON ROUTINE CARD CP753-12. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042300054 20080423 00054 NM 2008 4 23 2008UALA02219 1 20080416 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1440 S24-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 AFT PIT STA 1440 HAS 3 EACH DENTS STRINGER 26L - 24L. REMOVED DAMAGE FABRICATED AND INSTALLED RPR PER SRM 53-00-07 RPR 5 TABLE II ZONE 1. RPR IS A CAT B RPR AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS STARTING AT 50,000 TOTAL FLI GHT CYCLES AND 12,000FC THERE AFTER. CURRENT FC= 14767. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300055 20080423 00055 NM 2008 4 23 2008UALA02220 1 20080416 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1420 S27L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 AFT PIT STA 1420, STR 27L HAS 1 FRAME DENT. REMOVED DAMAGE FABRICATED AND INSTALLED RPR PER SRM 53-00-07 RPR 5 TABLE II ZONE 2. RPR IS A CAT B RPR AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTION S STARTING IN 25,000 FLIGHT CYCLES AND 1 1,000FC THERE AFTER. CURRENT FC= 14767 RPR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300059 20080423 00059 NM 2008 4 23 2008UALA02225 1 20080417 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS CUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 539UA 25223 EEL LIGHT STRIP INOP IN FRONT OF MID AFT LAV. SPLICED EEL STRIP, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300074 20080423 00074 NM 2008 4 23 UPS08551998 1 20080410 A 5610 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT OBSTRUCTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 471UP 28842 INSPECTION TYPE:N/A CAPTAIN'S WINDOW UNLATCH HANDLE REQUIRES HEAVY FORCE TO MOVE. CHECKED WINDOW. FOUND HARNESS (COIL) INTERFERING WITH TRACK. REPOSITIONED HARNESS. CHECKED LATCH HANDLE. LATCHES AND CAMS FOUND OK. LUBED AND CHECK OPER ATION OF WINDOW MECHANISM PER AMM 56-11-02-5. OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2008042300081 20080423 00081 NM 2008 4 23 08FDEA01457 1 20080419 A 5340 66124343 STRINGER CLIP BOEING 727 727232 1384082 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 AFT PIT BILGE BODY FRAME, STR CLIP IS BUCKLED/CRACKED, BS 970, STR 27L. REMOVED AND REPLACED STRINGER CLIP AT BS 970, S TRINGER 27L. IAW SRM 51-30-2, SRM 51-30-5. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008042300082 20080423 00082 NM 2008 4 23 08FDEA01458 1 20080419 A 5320 6526173 FLOOR SUPPORT BOEING 727 727232 1384082 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 FLOOR SUPPORT CORRODED AT BS 344, LBL 30 REMOVED CORROSION ON FLOOR SUPPORT STA 344, LBL 30, REF SRM 51-10- 6 PG 12. M ATERIAL LOSS 50 PERCENT. FOUND TO BE OUT OF LIMITS, REF SRM 53-10-1 PG 1-3. FABRICATED NEW FLOOR SUPPORT AND SHIM, RE F BOEING DWG 65-96173. TREATED AND PRIMED AND PAINTED AND INSTALLED FLOOR SUPPORT REF SRM 51-10-2 AND AMM 51-10-151-7, SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008042300084 20080423 00084 EU 2008 4 23 F3LA200800186 1 20080406 A 5320 D5361019720140 STRIP AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED BOTH LEFT 1 AND RIGHT 1 GAP STRIPS CORRODED ON LOWER SURFACE. MAINTENANCE REMOVED AND REPLACED LEFT 1 AND RIGHT 1 GAP STRIPS IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 53-12-12 PAGE BREAK 401. UPON CO MPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042300089 20080423 00089 NM 2008 4 23 USAA920080892 1 20080417 A 5330 SKIN BOEING 737 7373B7 1384580 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 531AU 24478 ONE INCH CRACK ON FUSELAGE SKIN AT BS 525, LBL2. INSTALLED REPAIR IAW EA100427. 2 L 7 2 4F RT A16WE 2008042300091 20080423 00091 NM 2008 4 23 USAA920080894 1 20080415 A 5330 SKIN BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 531AU 24478 CLT-MAJOR REPAIR-C3- ONE INCH CRACK ON FUSELAGE SKIN AT BS 947.5R, STR 15R. INSTALLED REPAIR IAW SRM 53-60-01 FIG 201 D ETAIL 3. 2 L 7 2 4F RT A16WE 2008042300094 20080423 00094 WP 2008 4 23 UPS08851995 1 20080227 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 CORROSION AND MISSING FASTENERS ON FLOORBEAM AT STA 55 RBL 31-48. CUT OUT DAMAGE, FABBED AND INSTALL ED REPAIR DOUBLERS IAW SRM 51-1-8, 5 1-2-0, 53-2-0 FIG 1F. 2 L 7 4 4F RT 4A25 2008042300099 20080423 00099 WP 2008 4 23 UPS08852006 1 20080410 A 3250 STEERING SYS DOUG DC8 DC871F 302199D WP NLG MALFUNCTIONED A IPXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 715UP 45915 INSPECTION TYPE:N/A ON T/O THE A/C BEGAN TO VEER TO THE RIGHT. THE CREW WAS UNABLE TO CONTROL THE A/C AND ABORTED TAKEO FF. A/C IS OOS. *SDR FILED OPEN*. 2 L 7 4 4F RT 4A25 2008042300100 20080423 00100 NM 2008 4 23 USAA920080897 1 20080328 A 5312 BULKHEAD BOEING 737 73733A 1384673 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 23634 CLT - MAJOR REPAIR-C22- ONE INCH CRACK ON WEB AT BS 178, WL 187, BL0. INSTALLED REPAIR IAW SRM 53-10-08-2 REPAIR 2. 2 L 7 2 4F RT A16WE 2008042300106 20080423 00106 EA 2008 4 23 A6WA200840130 1 20080225 A 3250 RVDT CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 31 461AW 7870 STEERING INOPERATIVE CAUTION MESSAGE INFLIGHT. COMPLIED WITH QRH BUT MESSAGE RETURNED. THE GEAR AND FLAP ICONS ARE STI LL ON ED-1. DIVERTED TO ORF. REMOVED AND REPLACED LT NOSE WHEEL STEERING RVDT IAW AMM 32-51-20. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2008042300147 20080423 00147 NM 2008 4 23 UPS08M52039 1 20080326 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:4C LEFT WING LE ACCESS PNL LANDING XOS 550 STRINGER CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER IA W MD-11 SRM 57-10-00 FIG 18 AND 51-33-01. 2 L 7 3 4F RT A22WE 2008042300166 20080423 00166 NM 2008 4 23 UPS08M52041 1 20080326 A 5730 SKIN DOUG MD11 MD11F 3023600 NM LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:4C LEFT WING LE NR 14 SLAT TRACK CUT OUT CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR FILLE R AND DOUBLER IAW MD-11 SRM 57-10-00 FIG 21 AND 51-33-01. 2 L 7 3 4F RT A22WE 2008042300204 20080423 00204 NM 2008 4 23 NWAA081683154 1 20080418 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHT NO TEST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 354NB 15418 15418 1833 EMERGENCY EGRESS LIGHTS WILL NOT PASS TEST. MESSAGE NO COMMUNICATION. REPLACED EPSU 10WL AND BATTERY PACK, CHECKS GOOD . 2 L 7 2 4F RT A28NM 2008042300205 20080423 00205 EA 2008 4 23 MASA200800310 1 20080411 A 3350 110049 CHARGER CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 932LR 7948 15032 ASH FLT 2944 PHX - EUG. FORWARD INTERIOR LOWER LEVEL EMERGENCY EXIT LIGHT INOP ALONG WITH LEFT FWD AND RIGHT AFT EXTERI OR EMERGENCY LIGHTS INOP. MX CHANGED THE NR 5 BATTERY CHARGER. 2 L 7 2 4F RT A21EA 2008042300219 20080423 00219 SO 2008 4 23 SIMA200810901 1 20080410 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO CARGO DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 632AE 19993 5000 145143 DURING A MBV INSPECTION, THE BAGGAGE DOOR CUTOUT LOWER SILL WAS FOUND CORRODED. REMOVED THE DAMAGED SILL AND CLEANED TH E AREA. POSITIONED NEW SILL AND MARKED AND DRILLED, COUNTERSUNK AND ALODINED PART. INSTALLED NEW PART. REPAIR DONE IA W EMBRAER 145 SRM (SRM EMB 145/1142 REV. 39) CHAPTERS 51-20-01, 03, 51-40-02, 04 AND 51-40-06. AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4T RT T00011AT 2008042300232 20080423 00232 NM 2008 4 23 SWAA081935 1 20080413 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 266WN 32523 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008042300233 20080423 00233 NM 2008 4 23 SWAA081934 1 20080410 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 266WN 32523 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008042300239 20080423 00239 NM 2008 4 23 SWAA081937 1 20080410 A 3350 MS155721 LIGHT BOEING 737 7373Y0 1384671 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008042300247 20080423 00247 CE 2008 4 23 20080401 1 20080413 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE FAILED E CWQA O OTHER O OTHER LD LANDING 1 GL 05 400MC 5600440 ON TOUCHDOWN, BRAKE PEDALS WENT TO FLOOR WITHOUT SLOWING AIRCRAFT. 2 L 7 2 4F RT A22CE 2008042300273 20080423 00273 NM 2008 4 23 SWAA081970 1 20080413 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300274 20080423 00274 NM 2008 4 23 SWAA081977 1 20080413 A 5610 571762 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT DELAMINATED A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 398SW 27692 FLIGHT DECK R2 WINDOW ARCED AND DELAMINATED OUTER PANE. REMOVED AND REPLACED WINDOW AND HEAT CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 2008042300289 20080423 00289 NM 2008 4 23 SWAA081984 1 20080413 A 5311 6546550 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300296 20080423 00296 NM 2008 4 23 2008UALA02154 1 20080411 A 5240 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 DOOR 2R UPPER HINGE ARM CUTOUT REQUIRES DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. ACCMP'D HFE C. PERFORMED INSURANCE CUT. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300304 20080423 00304 NM 2008 4 23 SWAA081952 1 20080413 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300309 20080423 00309 NM 2008 4 23 SWAA081953 1 20080412 A 3350 100031 SIGN BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 FWD CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM. 2 L 7 2 4F RT A16WE 2008042300322 20080423 00322 NM 2008 4 23 SWAA081961 1 20080411 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 917WN 36624 DURING SCHEDULED MV1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008042300323 20080423 00323 EU 2008 4 23 MAC020804 1 20080214 A 5751 S57610025204 TEE FITTING AEROSP AEROSP ATR42 ATR42300 8680920 EU RT AILERON CORRODED A MTNA K NONE O OTHER IN INSP/MAINT 1 EA 68 915FX NT1231 269 DURING INSPECTION LEVEL 2 CORROSION WAS FOUND ON A TEE FITTING INSIDE THE RIGHT WING AILERON. THE AILERON WAS REPLACED. 2 H 7 2 4T RT A53EU 2008042300327 20080423 00327 NM 2008 4 23 SWAA081995 1 20080414 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008042300364 20080423 00364 NM 2008 4 23 SWAA082015 1 20080415 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 830, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300373 20080423 00373 NM 2008 4 23 SWAA082021 1 20080415 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 719SW 27853 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008042300382 20080423 00382 NM 2008 4 23 SWAA082034 1 20080416 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 508D, 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300389 20080423 00389 NM 2008 4 23 SWAA082039 1 20080416 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM GIRT BAR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK BROKEN. REMOVED AND REPLACED HOOK PER MM. 2 L 7 2 4F RT A16WE 2008042300402 20080423 00402 NM 2008 4 23 SWAA082047 1 20080417 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 416WN 32453 DURING SCHEDULED 6Y CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 135. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042300408 20080423 00408 NM 2008 4 23 SWAA082055 1 20080417 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 DURING SCHEDULED HC1 CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BL 0. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008042400010 20080424 00010 EU 2008 4 24 F3LA200800200 1 20080403 A 5280 GA65896 SUPPORT BRACKET AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE NLG DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED THE NOSE LANDING GEAR DECORATIVE DOOR LOWER ATTACH POINTS ON STRUT WERE CORRODED A ND WORN. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR SUPPORT BRACKET IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 32-22-15-400-001 AND EA A0-32T-11699. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042400034 20080424 00034 NM 2008 4 24 UPS08652021 1 20080409 A 3350 LAMP BOEING 767 76734AF 1385212 NM ANNUNCIATOR INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 308UP 27761 LAMP INOP IN EMERGENCY LIGHT ANNUNCIATOR. RELAMPED PER MM 33-16-02-2. 2 L 7 2 4F RT A1NM 2008042400037 20080424 00037 WP 2008 4 24 UPS08852023 1 20080414 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 AFTER BLOCKOUT WITH ENGINES RUNNING NORMAL, EMERGENCY LIGHTS OPERATED CONTINUOUSLY. REMOVED AND REPLACED EMERGENCY BATT ERY PACK. RESET CIRCUIT BREAKER. OPS CHECK NORMAL PER AMM 33-50-01-2. 2 L 7 4 4F RT 4A25 2008042400042 20080424 00042 NM 2008 4 24 2008UALA02179 1 20080416 A 2530 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GALLEY COFFEMAKE ARCED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 547UA 25368 SMOKE AND ARC'S IN FWD GALLEY PER CREW. FOUND WIRE ON TOP OF COFFEE MAKER M10 THAT HAD BEEN GROUNDED AND ARCING. REPL ACED COFFEE MAKER M10-ALL OPS WERE GOOD 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400043 20080424 00043 NM 2008 4 24 2008UALA02180 1 20080415 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 813UA 858 AFT EMERGENCY LIGHT FROM APPROX ROW 15-16, AFT IS ILLUMINATED. AFTER SWAPPING BATTERY PACKS WAS NO HELP, THE ORIGINAL C ONFIG WAS RESTORED AND LIGHTS WENT OUT AND STARTED WORKING PROPERLY. NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042400044 20080424 00044 2008 4 24 2008UALA02181 4 20080415 A 2565 HOSE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOOR SLIDE SHEARED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 833UA 1401 NR 2 RT MAIN ENTRY SLIDE DEPLOYMENT TEST FAIL, INFLATION HOSE SHEARED OFF AT THE ASPIRATOR END FITTING. REPLACED HOSE A ND OVERHAULED SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042400057 20080424 00057 NM 2008 4 24 2008UALA02198 1 20080413 A 3510 OXYGEN SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 597UA 28750 CREW OXYGEN LOW. SERVICED CREW OXYGEN TO 1500PSI, NO LEAKS WERE NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400058 20080424 00058 NE 2008 4 24 2008UALA02199 2 20080416 A 7230 FAN BLADE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 727686 NR 2 ENGINE SEVERAL FAN BLADES DAMAGED NR 11, 25 AND 30. LEADING EDGE CLOSE TO TIP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042400065 20080424 00065 CE 2008 4 24 0811001 1 20080419 A 3260 1EN18 DOWNLOCK SWITCH LEAR 35 31A 5170531 CE RT MLG OUT OF LIMITS E CVGA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 05 431DA 163 ON APPROACH, RIGHT MAIN LANDING GEAR DOWNLOCK INDICATOR DID NOT ILLUMINATE. AFTER GO-AROUND, CYCLED LANDING GEAR AND RE SULTED IN SATISFACTORY EXTENSION. MAINTENANCE FOUND RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH RESISTANCE OUT OF LIMITS. REPLACED SWITCH AND PERFORMED LANDING GEAR OPERATIONAL CHECKS WITH SATISFACTORY RESULTS. 2 L 7 2 4F RT A10CE 2008042400074 20080424 00074 NM 2008 4 24 2008UALA02266 1 20080418 A 3350 COVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 EEL LIGHT LENS COVER CRACKED FWD OF MAIN ENTRY DOOR 2R BUSINESS CLASS GALLEY. REPLACED LENS/EXIT SIGN. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400075 20080424 00075 NM 2008 4 24 2008UALA02267 1 20080418 A 2910 NAS1611112 PACKING AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE HYD SYSTEM LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 803UA 748 LANDED WITH LOSS OF GREEN HYDRAULIC SYSTEM. FOUND PTU MANIFOLD CHECK VALVE LEAKING, O-RING FAILURE. REMOVED AND REPLACE PACKINGS ON VALVE, CKS OK NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042400080 20080424 00080 NM 2008 4 24 2008UALA02272 1 20080417 A 2433 757183F CONVERTER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RT BACKUP FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 792UA 26934 ELEC BACKUP GEN R RIGHT BACKUP GENERATOR IS OFF OR HAS FAILED. RESET ONCE, TRIPPED AGAIN. TURNED OFF, MSG-2446090 LATC HED ER MODE. SUSPECT BUG CONVERTER HAS INTERNAL FAULT. REPLACED CONVERTER POWER TEST GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042400083 20080424 00083 NM 2008 4 24 2008UALA02275 1 20080418 A 4920 APU BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE MALFUNCTIONED A UALA O OTHER M J OVER TEMP WARNING INDICATION CR CRUISE 1 WP 29 668UA 30024 APU FAULT CAUTION LT AND EICAS MSG. TEMP SPIKED TO +600 ON SHUTDOWN IN FLIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042400084 20080424 00084 NE 2008 4 24 NACA20080007 2 20080418 A 8530 356994 CYLINDER DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE ENGINE FAILED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 AL 03 2907F 583 583 533265 CP450668 NR 4 ENGINE SHUTDOWN DUE TO NR 1 CYLINDER DOUBLE SHORTED SECONDARY. REMOVED AND REPLACED NR 1 CYLINDER DUE TO RING LAND FAILURE. REF: DC6MM SECT V PG 16, OP CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2008042400089 20080424 00089 EA 2008 4 24 A6WA200840131 1 20080225 A 2520 PSU CNDAIR CL600 CL6002B19 1900309 EA ROW 8A&C DETACHED A A6WA O OTHER O OTHER CL CLIMB 1 GL 31 405AW 7362 PSU AND OXYGEN MASK UNIT DETACHED FROM ROW 8A AND C. RESECURED PSU, COMPLIED WITH OPS CHECK OF PSU ABOVE SEATS 8A AND 8 C, OPS CHECK GOOD IAW AMM 25-20. PSU PROPERLY INSTALLED AT THIS TIME. (M) 2 L 7 2 4F RT A21EA 2008042800054 20080428 00054 NM 2008 4 28 SWAA082096 1 20080418 A 5523 6545166 PUSHROD BOEING 737 7373G7 1384595 NM LT ELEVATOR TAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND LT ELEVATOR TAB PUSH RODS CORRODED AT FWD END. REMOVED AND REPLACED PUSH RODS PER MM . 2 L 7 2 4F RT A16WE 2008042800062 20080428 00062 EA 2008 4 28 A6WA200840284 1 20080402 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA INTERCOSTAL CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 CRACK EXIST ON ANGLE OF INTERCOSTAL FS 484, RBL 27. (M) NEW ANGLE INSTALLED IAW SRM 51-42-20 . 2 L 7 2 4F RT A21EA 2008042800067 20080428 00067 NM 2008 4 28 ABXA080138 1 20080420 A 3350 LIGHT BOEING 767 767281 1385109 NM EXTERIOR INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 784AX 23017 RNO - MAINTENANCE FOUND FORWARD ENTRY DOOR EXTERIOR SLIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED LAMP HOLDER ASSEMB LY IAW AMM 33-51-06-02. OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 2008042800074 20080428 00074 NM 2008 4 28 ABXA080130 1 20080314 A 5314 145T8611 KEELBEAM BOEING 767 767200 1385120 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 752AX 23434 LOWER RIGHT KEEL BEAM APPROXIMATELY STA 970 CORRODED. BLENDED CORROSION ON LOWER RIGHT KEEL BEAM STA 970 IAW B767 SRM. 2 L 7 2 4F RT A1NM 2008042800078 20080428 00078 NM 2008 4 28 ABXA080131 1 20080314 A 5711 114T022318 STRAP BOEING 767 767200 1385120 NM RT WING SPAR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 752AX 23434 STRAP ON UPPER CAP OF FRONT SPAR WAS CRACKED LES 485. REMOVED AND REPLACED UPPER SPAR CAP STRAP SECTIONS IAW B767 SRM. 2 L 7 2 4F RT A1NM 2008042800103 20080428 00103 NM 2008 4 28 HALA0800539 1 20080422 A 2410 727810C GENERATOR BOEING 767 7673G5 1385126 NM FAILED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM, APU WILL NOT STAY ON LINE WITH HEAVY LOADS. MUST TURN OFF RECIRC FANS. ELECTRIC ONLY. REMOV ED AND REPLACED APU GENERATOR PER AMM 24-21-01, OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2008042800107 20080428 00107 NM 2008 4 28 HALA0800531 1 20080402 A 5710 STRUCTURE BOEING 767 76733A 1385209 NM RT WING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 587HA 33421 CRACK ON RT WING CAVITY AT WS 671, CRACK IN L/E STRUCTUE. REPLACED L/E STRUCTURE. 2 L 7 2 4F RT A1NM 2008042800122 20080428 00122 NM 2008 4 28 ASAA0852830 1 20080422 A 2160 412A160041 FILTER BOEING 737 737890 1384527 NM CABIN CLOGGED A ASAA K NONE O OTHER NR NOT REPORTED 1 NM 02 583AS 35681 WITH FWD & CONT CABIN PACK CONTROLLERS IN 12:00 AFT CABIN CONTROLLER REQUIRED 4:00 POSITION TO MAINTAIN AFT CABIN TEMP A T 26 DEGS C. NO FAULTS LOGGED IN NR 1, 2 CONTROLLERS. FOUND AFT CABIN TEMP SENSOR FILTER CLOGGED. CLEANED FILTER. GR OUND VERIFICATION PASSED. ACCOMPLISHED ZONE TEMP BITE CHECK. NO FAULTS LOGGED 1&2. RAN BOTH PACKS TEMP IN FWD AFT CAB IN PAIRED UP AT ALL SETTINGS. 2 L 7 2 4F RT A16WE 2008042800156 20080428 00156 NM 2008 4 28 SWAA082154 1 20080423 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042800158 20080428 00158 NM 2008 4 28 SWAA082155 1 20080423 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER 7L CRACKED AT BS 1010. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008042800160 20080428 00160 NM 2008 4 28 SWAA082173 1 20080423 A 3350 MS21069L3 INSERT BOEING 737 7373H4 1384600 NM EXIT LIGHT PANEL PULLED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED BRDG CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT PANEL HAS ONE INSERT PULLED OUT. REMOVED AND REPLACED INSERT PER MM. 2 L 7 2 4F RT A16WE 2008042800161 20080428 00161 NM 2008 4 28 SWAA082174 1 20080423 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FIT TING PER SRM. 2 L 7 2 4F RT A16WE 2008042800162 20080428 00162 NM 2008 4 28 SWAA082175 1 20080423 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING OUTBOARD T/E AFT INBOARD END DELAMINATED. REMOVED AND REPLACED FLAP PER M M. 2 L 7 2 4F RT A16WE 2008042800167 20080428 00167 2008 4 28 SWAA082133 4 20080421 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042800169 20080428 00169 2008 4 28 2008UALA02278 4 20080418 A 3442 RADAR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE WX SYSTEM MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 932UA 26658 FLIGHT DIVERTED DUE TO WEATHER RADAR PROBLEM. RESET WEATHER RADAR R/T. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042800170 20080428 00170 EU 2008 4 28 2008UALA02279 1 20080418 A 5321 FLOORBOARD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO BAY DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 440UA 702 CARGO FLOORBOARD RPL S GLS PNL. ACCOMPLISHED MAJOR REPAIR AT LCQ THROUGH UAL EG PROJECT TO REPLACE FLOORBOARDS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042800175 20080428 00175 NM 2008 4 28 2008UALA02396 1 20080423 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 303 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 FWD ENTRY DOOR UPPER HINGE CUTOUT, FWD FASTENER HOLE CRACKED AND BENT AT FRAME BS 303.9. REPAIR ACCOMPLISHED: CUTOUT DA MAGE. FABRICATED & INSTALLED FRAME REPAIR ANGLE, INTERCOSTAL & CLIPS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042800177 20080428 00177 NM 2008 4 28 2008UALA02283 1 20080420 A 2121 MOTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE VENT FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 818UA 882 VENT BLOWER FAULT DISPLAYED WITH ELECTRICAL ODOR IN COCKPIT, NO SMOKE REPORTED. VENT BLOWER MOTOR FAILURE, BEARING. R EPLACED AVX VENT BLOWER FAN MOTOR. OPS CHECKED NORMALLY, NO SMELL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042800178 20080428 00178 NM 2008 4 28 2008UALA02284 1 20080421 A 2613 OVERHEAT LOOP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT NACELLE WORN A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 548UA 25396 "L ENG OVHT LOOP 1" STATUS MESSAGE ON EICAS. FOUND OVER HEAT LOOP 1 WORN. REPLACED OVERHEAT LOOP 1, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 NM 2008 5 21 2008UALA02770 1 20080512 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW O2 LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 848UA 1647 OXYGEN LOW. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042800183 20080428 00183 EU 2008 4 28 2008UALA02374 1 20080422 A 5310 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 467UA 1359 BOTTOM OF DOOR 1L DAMAGED. AFTER VISUAL INSPECTION FOUND DENT TO BE WITHIN LIMITS THICKER THEN .063 CANNOT BE DRESSED O UT. WILL REQUIRE DOUBLER REPAIR. SCHEDULED FOR A PERMANENT REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042800188 20080428 00188 NM 2008 4 28 2008UALA02246 1 20080417 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1681 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 RT FRAME REPAIR WAS ACP'D BS 1681, WL-209. ACCOMPLISHED MAJOR, PER EVA MOC1-8433 REVA. AFTER DTA, THIS REPAIR IS CONS IDERED TO BE A CAT 'A' TIME LIMITED REPAIR. THIS REPAIR MUST BE REPLACED PER REVISED EVA-40093, NO LATER THAN NEXT HMV CURRENTLY SCHEDULED 06JUN08 AND REPAIR IS TO BE RE-INSPECTED AT EACH 'C' CHK PER EVA INSTRUCTIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042800189 20080428 00189 NE 2008 4 28 DL76G080620 2 20080421 A 7200 ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1608 30235 30573 706112 METAL FOUND ON B-SCAV DETECTOR SCREEN. FOUND SMALL AMOUNT OF METAL DEBRIS ON MCD AND LARGE QT OF DEBRIS ON B SCAV MCDON LUBE PUMP, PER MSU REQ ENG CHG. NR 2 ENG REPLACED PER TRANS 1T161. 2 L 7 2 4F 4 F RT A1NM E13NE 2008042800192 20080428 00192 2008 4 28 DL76G080622 4 20080421 A 3442 INDICATOR BOEING 767 767332 1382001 NM WX RADAR SYS OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 173DZ 29692 IN FLIGHT HEATED ELECTRICAL WIRE SMELL FROM WX RADAR LOST DISPLAY BOTH C/B`S PULLED. FOUND WX RADAR SCREEN OVERHEATED. COOLING TUBE FOR WX RADAR SCREEN RACK BROKEN NEEDS NEW COOLING TUBE AND WX RADAR SCREEN. REPLACED COOLING TUBE. REPLA CED WX RADAR DISPLAY PER M/M. 2 L 7 2 4F RT A1NM 2008042800198 20080428 00198 NM 2008 4 28 DLM88080629 1 20080424 A 2120 UNKNOWN DOUG MD88 MD88 3023688 NM GE CF6 CF680C2B6F 30025 NE CABIN SMOKE A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 907DE 53416 704736 STRANGE ODOR THROUGHOUT CABIN WITH ASSOCIATED HAZE. SMOKE ALARM WENT OFF IN AFT LAV. REMOVED BORO PLUGS ON BOTH ENGINE S PER AMM 72-00-00-6012. PERFORMED BORESCOPE OF 6TH AND 7TH STAGE AND 8TH STAGE BLEED DUCT ON NR 1 AND NR 2 ENGINES. N O OIL OR RESIDUE WAS NOT INSTALLED BORO PLUGS AND SECURED ENGINE COWLING. REMOVED BOTH WATER SEPARATORS. INSPECTED WAT ER SEPARATORS AND REINSTALLED. REMOVED APU DOOR. CLEANED AREA AND DOOR. REINSTALLED DOOR. TROUBLESHOT IAW OPN 5088. COULD NOT FIND ANY PROBLEMS. EVERYTHING CHECKS GOOD. 2 L 7 2 4F 4 F RT A6WE E13NE 2008042800206 20080428 00206 NM 2008 4 28 2008UALA02397 1 20080423 A 5230 BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 FWD CARGO DOOR AFT LOWER CROSS BEAM CRACKED JUST INBOARD OF STOP FITTING. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGE. FAB RICATED & INSTALLED FILLER DOUBLER TO CROSSBEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042800211 20080428 00211 NM 2008 4 28 2008UALA02410 1 20080423 A 7830 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE THRUST REVERSER DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 NR 1 ENGINE FOUND LT REVERSER HALF DAMAGED CONSISTENT WITH SERVICE TIP, LATCH ACCESS DOOR ALSO DAMAGED. REPLACED THRUST REVERSER HALF. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042800213 20080428 00213 NM 2008 4 28 SWAA082138 1 20080422 A 3350 101331 LENS BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2008042800214 20080428 00214 NM 2008 4 28 2008UALA02411 1 20080424 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1R DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 DOOR 1R WILL CLOSE BUT NOT ARM. FOUND DEBRIS UNDER GIRT BAR. CLEANED DEBRIS, DOOR ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400091 20080424 00091 EU 2008 4 24 08FDEA01465 1 20080421 A 5320 A5398111320100 SHEAR PLATE AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 25 661FE 760 THE SHEAR PLATE IS CRACKED AT FR 79, STRINGER 16R - STRINGER 17R. REMOVED AND REPLACED THE SHEAR WEB IAW A300-600 SRM 5 1-40-21; PARAGRAPH 7. 2 L 7 2 4F RT A35EU 2008041100013 20080411 00013 EA 2008 4 11 A6WA200840139 1 20080226 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 RIGHT AND LEFT BRACKET CRACK AT FS 280 LBL 9. REPLACED IAW SRM 51-42-06 PG 11 AND SRM 51-42-21 PAGE 18. (M) 2 L 7 2 4F RT A21EA 2008041100014 20080411 00014 EA 2008 4 11 A6WA200840143 1 20080219 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 529 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 CRACK FOUND ON HYDRO BRACKET IS MLG BAY FS 529 LBL 27. REMOVED AND REPLACED IAW SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2008041100017 20080411 00017 NM 2008 4 11 GTIA0800049 1 20080323 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 503NK 2470 FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN ST FR76 7 FR70. REMOVED AND REPLACED FLOOR SUPPORT IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008041100018 20080411 00018 NM 2008 4 11 GTIA0800050 1 20080323 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 503NK 2470 FOUND CORROSION ON FLOOR SUPPORT -Y765 BETWEEN STA FR 67 AND FR 70. REMOVED AND REPLACED FLOOR SUPPORT IAW A319 SRM 51- 72-11. 2 L 7 2 4F RT A28NM 2008041100019 20080411 00019 NM 2008 4 11 GTIA0800051 1 20080329 A 3397 WIRE AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHT LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 503NK 2470 EMERGENCY LIGHT ON DOOR 2R IS INOP. REATTACHED LOOSE CONNECTION, OPS CHK GOOD IAW AMM33-51-16. 2 L 7 2 4F RT A28NM 2008041100022 20080411 00022 EA 2008 4 11 A6WA200840142 1 20080225 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 435AW 7724 PAX DOOR STAIR AFT DRAG ANGLE CRACK. (M) 2 L 7 2 4F RT A21EA 2008041100024 20080411 00024 EA 2008 4 11 A6WA200840168 1 20080307 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 202 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 FORWARD PRESSURE BULKHEAD AT FS 202.75 LBL 23.71, WL 69 IS CRACKED. REPAIRED IAW REO 601R-53-11-563. (M) 2 L 7 2 4F RT A21EA 2008041100026 20080411 00026 NM 2008 4 11 DHL2008753510 1 20080308 A 5310 DOOR FRAME BOEING 727 727223 1384074 NM BS 950E CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 58284 22468 WHILE AT C CHECK, AFT CARGO COMPARTMENT DOOR FRAME AT STA 950E CRACKED. REPAIRED WEB AND CHORD IAW B727 S/B 727-53A0199 FIG 2 DETAIL 2 AND 13.5 INCH BY 4.5 INCH WEB 1 1/2 INCH BY 12 INCH CHORD IAW B727 S/B 727-53A0199 FIG 1 TABLE 1. 2 L 7 3 4F A3WE 2008041100027 20080411 00027 NM 2008 4 11 DHL2008753511 1 20080403 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1148 S29-30R DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 C CHECK, AFT COMPT FUSELAGE SKIN HAS OPEN HOLES BETWEEN STA 1148- 166 BETWEEN STR30- 29R AT PREVIOUS REPAIR. REMOVED, F ABRICATED AND INSTALLED EXTERNAL DOUBLER 18" BY 7" IAW SRM 53-30-3 FIG 3 AND EA38100001-001-B INTERNAL DOUBLER 18" BY 4" IAW SRM 53-30-3 FIG3 AND EA38100001-001-B. 2 L 7 3 4F A3WE 2008041100028 20080411 00028 WP 2008 4 11 IXXA08SMN041S 1 20080201 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1733 S26L MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 822BX 92877 2986 45813 DURING ROUTINE C CHECK INSPECTION, FOUND EXTERNAL DOUBLER AFT LOWER FUSELAGE AFT OF L-2 DOOR WITH IMPROPER REPAIR AT STA TION FS 1733 LONGERON 26 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVE D DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND CORROSION FOUND. FABRICATED REPAIR DOUBLER, FINGER DOUBLERS, F ILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW 51-3-1, DC8 SRM 51-1-21, 51-3-0, 51-1-20D, DC8 NDT SPM PART 06-10-01.001, DOUGLAS DRAWING SR08530032, SKETCH 200802070028-0001, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008041100031 20080411 00031 EU 2008 4 11 08FDEA01376 1 20080318 A 5330 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 BULK PIT DOOR CUTOUT, FWD LWR AREA, GOUGED. COMPLIED WITH EA 6-5310-118471 PT 1 2 L 7 2 4F RT A35EU 2008041100032 20080411 00032 EU 2008 4 11 MALA080054 1 20080409 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 288-389 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 421XJ 340B421 SEAT TRACK CORRODED. REPLACED AT STA 288 TO 389 ALONG BL 18.3 REPAIRED IAW EO NR S530602. 2 L 7 2 4T RT A52EU 2008041100036 20080411 00036 NM 2008 4 11 DL76G080551 1 20080404 A 5315 146T51181 FLOORBEAM BOEING 767 7673P6 1385105 NM FS 1480 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 155DL 25269 DURING CURRENT HMV, HEAVY CORROSION WAS FOUND ON THE FS 1480 FLOORBEAM UPPER CHORD. ADDITIONAL INSPECTION REVEALED THAT THE CORROSION WAS ON AN EXISTING REPAIR (TEE REPAIR) BETWEEN LBL 73 AND LBL 44. THE EXISTING REPAIR WAS REMOVED AND A MODIFIED SRM REPAIR INSTALLED PER BOEING INSTRUCTIONS, AS DOCUMENTED IN ERA/ 466277-14 2 L 7 2 4F RT A1NM 2008041100038 20080411 00038 NM 2008 4 11 DL76G080553 1 20080404 A 5330 143T32114 SKIN BOEING 767 767332 1382001 NM FS 440-630 S32L GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1609 30574 SKIN BLENDS AT FS 440 - 630 BETWEEN STRINGERS S-32L AND 35L. 2 L 7 2 4F RT A1NM 2008041100039 20080411 00039 GL 2008 4 11 DL764080554 2 20080404 A 7230 BLADE BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 2 HPC BROKEN A DALA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 27 844MH 23704 706121 29717 706121 AFTER START OF THE RIGHT ENGINE NOTICED TO HAVE N2 VIBS OF 5.0 AND CAN BE FELT. UNUSUAL SOUND ALSO. RETURNED TO GATE. NO METAL IN TAIL PIPE. CHIP DETECTORS CLEAN BUT ENG HAS RUMBLE SOUND WHEN RUNNING. BOROSCOPE REVEALED 1ST HPC BLADE BROKEN OFF. ENGINE CHANGE IN PROGRESS. 2 L 7 2 4F 4 F RT A1NM E23EA 2008042800215 20080428 00215 NM 2008 4 28 SWAA082162 1 20080423 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008042800216 20080428 00216 2008 4 28 SWAA082139 4 20080422 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042800217 20080428 00217 NM 2008 4 28 SWAA082187 1 20080423 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042800228 20080428 00228 NM 2008 4 28 SWAA082143 1 20080422 A 5753 6546430122 SKIN BOEING 737 7373H4 1384600 NM FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2008042800232 20080428 00232 EU 2008 4 28 2008UALA02303 1 20080420 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 466UA 1343 AVIONICS SMOKE DISPLAYED ON UPPER ECAM SCREEN, SMOKE CREW COMMENTS, AVIONICS SMOKE ECAM. S/O BLOWERS ETC. RESET, ECAM GONE, BUT WE STILL ODOR OF FAINT SMOKE. AVIONICS SMOKE ECAM. S-OBLOWERS ETC. RESET. ECAM GONE. BUT WE STILL SMELL FAIN T SMOKE. INSPECTED AVIONICS AREAS, RAN BLOWER & EXTRACT FANS, NO SMOKE OR ANY OTHER DEFECTS NOTED. ACPD BITE CHK OF SDC U & AEVC, NO FAULTS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042800237 20080428 00237 NM 2008 4 28 SWAA082145 1 20080422 A 3350 101331 LENS BOEING 737 7373Y0 1384671 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 LT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2008042800241 20080428 00241 WP 2008 4 28 MWEA080060 1 20080424 A 2910 HYDRAULIC LINE DOUG DC9 DC982 3022082 WP LT MLG WW CHAFED A MWEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 13 809ME 48071 SMOKE IN CABIN. FOUND 2 CHAFED HYDRAULIC LINES. REMOVED AND REPLACED HYDRAULIC LINES ON LEFT WHEEL WELL. 2 L 7 2 4F A6WE 2008042800246 20080428 00246 EA 2008 4 28 SWIA200819531 1 20080118 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 431SW 7536 CRACK FOUND AT STA 280 AND RBL9.0 LOWER BEAM, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2008042800251 20080428 00251 EA 2008 4 28 SWIA200819536 1 20080421 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 758SK 10222 OVERHEAD CURVED EMERGENCY EXIT ROW SIGN IS MISSING, FLIGHT NR 6709. INSTALLED NEW EXIT SIGN ASSEMBLY. 2 L 7 2 4F RT A21EA 2008042800258 20080428 00258 EU 2008 4 28 08FDEA01532 1 20080424 A 5320 A2151037700000 PANEL AIRBUS 300 A300F4605R 3930327 EU DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 AIR CONDITION EXTERNAL FAIRING PANEL NR 144 GR IS DELAMINATING ON THE INTERNAL SKIN. REPAIRED PANEL 144 GR BY REMOVING T HE DAMAGE AND APPLYING A WET LAY UP IAW SRM 51-77-12 AND RESTORED THE FINISH IAW SRM 51-75-10. 2 L 7 2 4F RT A35EU 2008042500212 20080425 00212 NM 2008 4 25 SWAA082078 1 20080420 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 908, STR 15R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008042500213 20080425 00213 NM 2008 4 25 SWAA082079 1 20080418 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 R1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008042500225 20080425 00225 NM 2008 4 25 SWAA082086 1 20080421 A 5311 65C33509 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 28R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008042500234 20080425 00234 NM 2008 4 25 SWAA082101 1 20080419 A 3350 10107451 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 FWD RIGHT CABIN EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 2008042500240 20080425 00240 NM 2008 4 25 2008UALA02332 1 20080421 A 2612 FIRE DETECTOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 NACELLE FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 795UA 26927 FIRE LOOP 2 ENG R RIGHT ENGINE FIRE DETECTION SYSTEM LOOP 2 FAILURE. STATUS MSG01, ACTIVE CLIMB INTERMITTENT; FIRE LOO P 2 (RIGHT ENGINE) IS SHORTED. DB- ENGINE FIRE DETECTION CARD (RIGHT) MSG02, ACTIVE CLIMB HARD. ENGINE FIRE DETECTION CARD (RIGHT) HAS AN INTERNAL FAILURE. DB- ENGINE FIRE DETECTION CARD (RIGHT) MSG03, ACTIVE CLIMB HARD; ENGINE FIRE DETE CTION CARD (RIGHT) HAS AN INTERNAL FAILURE. ITEM CNX PER PLF SHOWS NOT ACTIVE MSG-2610232 ACTIVE CL INTER MSG-2610012 A CTIVE CL HARD MSG-2610012 ACTIVE CL HARD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080521 NM 2008 5 21 2008UALA02401 1 20080424 A 5320 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 FRAME CLIP CRACKED AT BS 360 STR 14L,10L AND BS 349 STR 16L SUPPLEMENTAL DATA UPDATE MAJOR REPAIR, REPAIRED PER UA-EVA- 71481 AND UA-EVA-71482 AND REO-L01065. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042500253 20080425 00253 NM 2008 4 25 2008UALA02345 1 20080421 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD CARGO BAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 FWD CARGO DOOR CUTOUT, AFT FRAME CRACKED IN RADIUS ABOVE LOWEST DOOR STOP FITTING. MAJOR REPAIR ACCOMPLISHED, REMOVED D AMAGE. INSTALLED NESTED ANGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042500255 20080425 00255 NM 2008 4 25 2008UALA02346 1 20080421 A 5230 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AFT GALLEY DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 AFT GALLEY DOOR, LOWER INNER SKIN HAS EVIDENCE OF DAMAGE CUTOUT AND NO REINFORCEMENT REPAIR. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED INNER SKIN EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042500256 20080425 00256 NM 2008 4 25 2008UALA02347 1 20080422 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 344-360 S19R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 STRINGER 19R BETWEEN STA 360 AND 344 IS DAMAGED. REMOVED DAMAGE. INSTALLED NEW INTERCOSTAL, ANGLE REPAIR, STRINGER SPL ICE, FILLERS, AND PATCHES. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042500288 20080425 00288 NM 2008 4 25 2008UALA02386 1 20080423 A 5310 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 428-430 GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 527UA 24995 TWO GOUGES FOUND DURING SCRIBE MARK INSPECTION BETWEEN BS 428 AND 430, 1 INCH OTBD OF STR 2L. MAJOR REPAIR ACCOMPLISHED : INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042500304 20080425 00304 NM 2008 4 25 2008UALA02391 1 20080422 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 217UA 30550 SEAT MOUNTED EMERGENCY LIGHT AT 2F AFT MISSING. REPLACED LIGHT ASSY. OP CHK OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042800002 20080428 00002 EA 2008 4 28 A6WA200840292 1 20080407 A 5753 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT WING TE FLAP BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 BRACKET BROKEN AT THE CENTER HINGE ARM OF THE RIGHT WING OUTBOARD FLAP. (M) BROKEN BRACKET AT CENTER HINGE ARM OF RIGH T WING OUTBOARD FLAP REPLACED IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008042800009 20080428 00009 EA 2008 4 28 A6WA200840285 1 20080404 A 5312 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA BS 409-559 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 CORROSION ON PRESSURE FLOOR FS 409 PLUS 128 TO FS 559, RBL 45. (M) CORROSION REMOVED ON PRESSURE FLOOR IAW SRM 51-21-0 6 . 2 L 7 2 4F RT A21EA 2008042800027 20080428 00027 NM 2008 4 28 SWAA082070 1 20080415 A 5313 6551698 STRINGER SPLICE BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 234WN 32502 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 791, STR 26L. REPAIRED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2008042800048 20080428 00048 NM 2008 4 28 SWAA082094 1 20080421 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042800049 20080428 00049 NM 2008 4 28 SWAA082111 1 20080421 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042800051 20080428 00051 NM 2008 4 28 SWAA082095 1 20080418 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CRACKED AT BS 927, STR 21R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008042800053 20080428 00053 NM 2008 4 28 SWAA082097 1 20080418 A 3350 311500 LENS BOEING 737 7373G7 1384595 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 16 DEF. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008042800056 20080428 00056 NM 2008 4 28 SWAA082127 1 20080420 A 5753 65C26343 CARRIAGE BOEING 737 737317 138447P NM T/E FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 7 MID FLAP CARRIAGE ASSY BEARING SUPPORT WORN. REMOVED AND REPLACED FLAP C ARRIAGE PER MM. 2 L 7 2 4F RT A16WE 2008042800076 20080428 00076 EA 2008 4 28 A6WA200840258 1 20080325 A 5720 ANGLE CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 RIGHT WING AT WS 148 INBOARD AND OUTBOARD ANGLE CRACKED 1 INCH BY 2 INCH. (M) RT WING AT W/S 148 IB AND OB ANGLE REPLAC ED IAW SRM 51-41-02. (K) 2 L 7 2 4F RT A21EA 2008041100041 20080411 00041 NM 2008 4 11 DLM88080556 1 20080404 A 5330 593600419 SKIN DOUG MD88 MD88 3023688 NM BS 643 L30 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DL 49546 FUSELAGE SKIN FOUND WITH CORROSION AT STA 643, L30. CUTOUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER/TRIPLER. 2 L 7 2 4F RT A6WE 2008041100042 20080411 00042 NM 2008 4 11 DLM88080559 1 20080404 A 5753 SKIN DOUG MD88 MD88 3023688 NM LT WING TE FLAP DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 962DL 49981 DURING HMV A DENT WAS FOUND ON LOWER SKIN OF OUTBD GUIDE VANE LT OUTBD FLAP. VANE WAS REPAIRED IAW SRM 51-70-2D. 2 L 7 2 4F RT A6WE 2008041100044 20080411 00044 NM 2008 4 11 DLM88080561 1 20080405 A 5330 593600419 SKIN DOUG MD88 MD88 3023688 NM BS 750 L30 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DL 49546 FUSELAGE SKIN FOUND WITH CORROSION AT STA 750, L-30. CUTOUT DAMAGED SKIN AND INSTALLED REPAIR. 2 L 7 2 4F RT A6WE 2008041100045 20080411 00045 NM 2008 4 11 DL76L080564 1 20080406 A 2400 066500002120 PROCESSOR BOEING 767 767332 1382001 NM E AND E HOT A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 195DN 28452 DURING FLIGHT, ELECTRICAL ODOR PRESENT IN COCKPIT AFTER ENTERING E/E COMPARTMENT ODOR SEEMED TO BE MAINTAIN FRPM TCAS EQ UIPMENT. TCAS EQUIPMENT BOX WAS ALSO VERY WARM TO TOUCH. PULLED TCAS C/B ON RECOMMENDATION FROM MCC AND ODOR DISSIPATE D. REMOVED TCAS COMPUTER VISUALLY EXAMINED CONNECTOR AND SURROUNDING AREA NOTHING ABNORMAL FOUND ALSO HOLES FOR COOLING NOT OBSTRUCTED AND AIRFLOW NORMAL VISUALLY CHECKED AREA BEHIND PILOTS INSTRUMENTS PANEL NOTHING FOUND EQUIPMENT COOLING MONITOR TEST OK ACCOMPLISHED TCAS OPERATIONAL TEST PER AMM34-45-00-501 TEST PASSED. TCAS SYS OPERATIONAL MCC CONTACTED ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS. 2 L 7 2 4F RT A1NM 2008041100046 20080411 00046 EA 2008 4 11 A6WA200840249 1 20080325 A 3510 OXYGEN BOTTLE CNDAIR CL600 CL6002B19 1900309 EA INOPERATIVE A A6WA O OTHER O OTHER CL CLIMB 1 GL 31 418AW 7618 ONE PORTABLE OXYGEN BOTTLE INOPERATIVE, ONE PORTABLE OXYGEN BOTTLE USED BELOW MIN. REMOVED AND REPLACED PORTABLE OXYGEN BOTTLE ASSEMBLY PER AMM 35-32-01. (M) 2 L 7 2 4F RT A21EA 2008041100082 20080411 00082 EA 2008 4 11 A6WA200840172 1 20080229 A 5260 HINGE CNDAIR CL600 CL6002B19 1900309 EA FOLDING STEP CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 PAX DOOR FOLDING STEP UPPER HINGE, REF P/N 601R31980-41, AND LOWER HINGE, REF P/N 601R31980-63, FOUND CRACKED. REPLACED PAX DOOR FOLDING STEP UPPER HINGE IAW SRM 51-42-02 AND REPLACED LOWER HINGE IAW SRM 51-41-02. (M) 2 L 7 2 4F RT A21EA 2008041100083 20080411 00083 WP 2008 4 11 070190 1 20080330 A 3350 408822101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 869GA 53294 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENC Y EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BA TTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008041100135 20080411 00135 NM 2008 4 11 CALA0800307 1 20080311 A 5320 BAC150518761 INTERCOSTAL BOEING 737 737524 1384721 NM BS 348-360 MISSING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11641 28902 INBOARD ATTACH BRACKET FOR STIFFENERS ON TOP AND BOTTOM OF INTERCOSTAL, BETWEEN FRAMES STA 348 & 360, AT STR 8 LT LOCATI ON, FASTENERS (4) MISSING (MARKED). INSTALLED 4 FASTENERS AT INBOARD ATTACH BRACKET FOR STIFFENERS ON TOP & BOTTOM OF I NTERCOSTAL BETWEEN FRAMES 348 & 360 AT STR 8LT PER PACE EA 641-53-001 CAL AND EC/RA 5310-04742. 2 L 7 2 4F RT A16WE 2008041100137 20080411 00137 NM 2008 4 11 CALA0800309 1 20080311 A 5320 6562276 INTERCOSTAL BOEING 737 737524 1384721 NM BS 348 S12L MISSING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11641 28902 INTERCOSTAL ATTACH POINT TO INBOARD FLANGE OF FRAME STA 348 AND STR 12 LT, MISSING FASTENERS 2 (MARKED). INSTALLED 2 FA STENERS AT INTERCOSTAL ATTACH POINT TO INBOARD FLANGE OF FRAME STA 348 STR 12 LT PER PACE EA 641-53-001CAL AND EC/RA5310 -04742. 2 L 7 2 4F RT A16WE 2008041400020 20080414 00020 CE 2008 4 14 DJFA2008032 1 20080325 A 2611 SMOKE DETECTOR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP CARGO BAY INOPERATIVE E DJFA O OTHER N FALSE WARNING CL CLIMB 1 EA 23 809LX 258432 AFTER TAKEOFF THE CREW REPORTED THE BAGGAGE FIRE LIGHT ILLUMINATED. A FLASHING SEQUENCE WAS NOTED AND THE BAGGAGE LIGHT WAS INTERMITENT DURING THE FLIGHT. THE AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED VISUAL INSP ECTION OF FWD/AFT LAV SMOKE DETECTORS. FOUND FWD SMOKE DETECTOR PHOTO CELL HOUSING WITH BACKED OFF NUTS AND ALSO FOUND DETECTOR CAGE CONTACTING SOLDER JOINTS INTERNAL OF DETECTOR. SECURED LOOSE CONNECTION AND REPOSITIONED CAGE. PERFORMED SMOKE DETECTOR TEST ON GROUND AND CKS GOOD 2 L 7 2 4F 4 F RT A3EU E6WE 2008041400028 20080414 00028 CE 2008 4 14 GLBA20061086 1 20080328 A 5311 12944004473 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 482 S3L BENT A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 261GL UE261 FRAME SECTION AT FS 482.75 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 482.75 STRINGER 3L IAW SRM 51-40. P/N 129-440044-73 2 L 7 2 4T 4 T RT A24CE E26NE 2008041400031 20080414 00031 CE 2008 4 14 DJFA2008033 1 20080330 A 2611 WARNING LIGHT RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP CARGO SMOKE FALSE ACTIVATION E DJFA O OTHER N FALSE WARNING CR CRUISE 1 EA 23 807LX 258413 WHILE AT CRUISE THE CREW REPORTED THE REAR BAGGAGE FIRE LIGHT ILLUMINATED INTERMITTENTLY. THE AIRCRAFT DIVERTED. MX PERF ORMED SEVERAL OPS CHECK AND COULD NOT DUPLICATE THE PROBLEM. 2 L 7 2 4F 4 F RT A3EU E6WE 2008041400034 20080414 00034 EA 2008 4 14 DXYA200800001 2 20080401 A 7322 383493 PLUG PREAIR RSA5 CESSNA 177 177RG 2073709 CE LYC O360 IO360A1B6 41514 EA MCAULY 3D36C B3D36C424 GL FUEL SERVO LOOSE E DXYA K NONE O OTHER IN INSP/MAINT 1 GL 07 34072 100 42298 177RG0960 L1573251A 070212 DURING COMPLIANCE WITH EMERGENCY AD2008-06-51 FOUND FUEL INJECTION SERVO PLUG PN 383493 LOOSE AS DISCRIBED IN AD. UNIT L EAKING FUEL. UNIT OVH WITHIN DATES NOTED BY REPAIR STATION. 1 H 7 1 3O 3 O A20CE 1E10 5 C P58GL 2008041400042 20080414 00042 CE 2008 4 14 J00A200800001 1 20080312 A 3000 S101813PG THERMAL SWITCH CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL DE ICE SYSTEM FAULTY E J00A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 01 706VP 4335 7500006 TEMPERATURE MONITORING DEVICE INDICATED LEADING EDGE SLAT COLD CAUSING EICAS MESSAGE STAB/SLAT COLD TO REMAIN ANNUNCIATE D. THIS EICAS MESSAGE SHOULD HAVE EXTINGUISHED, BUT DUE TO THE DURATION OF HAVING ANTI-ICE SYSTEMS ON THE STABILIZER EI CAS MESSAGE TRANSITIONED TO STAB HOT PREVENTING DISPATCH OF AC. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008041400050 20080414 00050 CE 2008 4 14 DXTA20082985 1 20080407 A 3230 LANDING GEAR RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP RIGHT MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 873QS 258573 ON TAKEOFF, RT MLG DID NOT FULLY RETRACT . 2 L 7 2 4F 4 F RT A3EU E6WE 2008042800099 20080428 00099 WP 2008 4 28 ABXA080136 1 20080324 A 5411 995815957 FRAME DOUG DC9 DC941 302207N WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 PANEL 8105 FRAME CRACKED, LOWER PYLON BELOW AND FORWARD OF AFT ENGINE MOUNT. INSTALLED SPLICE REPAIR IAW DC9 DWG K05683 . 2 L 7 2 4F A6WE 2008042800126 20080428 00126 NM 2008 4 28 ASAA0892833 1 20080322 A 5330 148A33111 SKIN BOEING 737 737990 NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 317AS 30856 AFT LEFT EXTERNAL FUSELAGE DENT WITH A GOUGE AT STA 1030 BELOW STR 12 LT. CUT OUT DAMAGED AREA, FABRICATED, LOCATED, DR ILLED AND INSTALLED REPAIR DOUBLER IAW 737 900 SRM 53 00 01 PGS 201 THRU 207 REPAIR 3. 2 L 7 4 4F RT A16WE 2008042800138 20080428 00138 NM 2008 4 28 SWAA082129 1 20080422 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 927, STR 26L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008042800149 20080428 00149 NM 2008 4 28 SWAA082130 1 20080422 A 3233 654482515 UPLOCK ACTUATOR BOEING 737 7373H4 1384600 NM RT MLG FAULTY A SWAA K NONE J WARNING INDICATION AP APPROACH 1 SW 29 346SW 24153 DURING LANDING GEAR EXTENSION RT MLG RED WARNING LIGHT ILLUMINATED AND NO GREEN LIGHT. CYCLED LANDING GEAR ONCE AND RT MLG GREEN LIGHT ILLUMINATED. INSPECTED WIRING, SENSOR AND TARGET PER MM. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR P ER MM. 2 L 7 2 4F RT A16WE 2008042800151 20080428 00151 NM 2008 4 28 SWAA082131 1 20080422 A 3350 100031 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2008042800172 20080428 00172 NM 2008 4 28 2008UALA02280 1 20080418 A 3150 SOFTWARE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EICAS MALFUNCTIONED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 543UA 25698 L EICAS STATUS MSG WILL NOT CLEAR. -L EICAS STATUS MSG WILL NOT CLEAR -L EICAS COMP REPLACED EARLIER TODAY. REPLACED L EICAS COMPUTER REF MM 31-41-02 AND LOADED OPS SOFTWARE REF MM31-41-02. MSGS HAVE CLEARED AND ALL DISPLAYS NORMAL 2 L 7 2 4F 4 F RT A2NM E17NE 2008042800185 20080428 00185 EA 2008 4 28 A6WA200840286 1 20080404 A 5312 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA BS 409-559 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 CORROSION ON PRESSURE FLOOR FS 409 PLUS 128 TO FS 559, LBL 45. CORRSION REMOVED IAW SRM 51-21-06. 2 L 7 2 4F RT A21EA 2008042800196 20080428 00196 NM 2008 4 28 SWAA082156 1 20080423 A 5315 6546811 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986.5, LBL 18 TO RBL 50. REPAIRED CHORD PER ER. 2 L 7 2 4F RT A16WE 2008042800204 20080428 00204 NM 2008 4 28 SWAA082197 1 20080423 A 5315 6546816 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM WEB CORRODED BETWEEN BS 1006 AND BS 1016, LBL 38 AND LBL 39. REMOVED AND RE PLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008042800220 20080428 00220 NM 2008 4 28 SWAA082188 1 20080423 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042800222 20080428 00222 NM 2008 4 28 SWAA082192 1 20080423 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042800234 20080428 00234 NM 2008 4 28 2008UALA02305 1 20080419 A 3150 UNKNOWN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE UNKNOWN A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 374UA 24639 LANDED UNDER AMBER ALERT DUE TO NOSE GEAR PROBLEM. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042800235 20080428 00235 NM 2008 4 28 SWAA082144 1 20080422 A 3260 WARNING SYSTEM BOEING 737 7373Q8 1384670 NM COCKPIT MALFUNCTIONED A SWAA K NONE N FALSE WARNING AP APPROACH 1 SW 29 663SW 23256 AFTER CONFIGURATION FOR LANDING AND VERIFYING ALL GEARS DOWN AND LOCKED (THREE GREEN LIGHTS ILLUMINATED), RECEIVED "TOO LOW GEAR" AURAL WARNING AT 1000 AGL, ALL GEARS HAD RED AND GREEN LIGHTS ILLUMINATED. DID A GO AROUND. PERFORMED SI ON LANDING GEAR HANDLE, CHECKS GOOD PER MM. 2 L 7 2 4F RT A16WE 2008042800240 20080428 00240 NM 2008 4 28 2008UALA02308 1 20080419 A 3520 OXYGEN BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE PAX OXYGEN LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 121UA 29167 PASSENGER OXYGEN PRESSURE READS LOW. BOTTLE LEAK AT REGULATOR.REPLACED 2 EACH OXYGEN BOTTLES PRESSURE CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042800245 20080428 00245 EA 2008 4 28 SWIA200819530 1 20080118 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 431SW 7536 CRACK FOUND AT STA 280 AND LBL9.0 LOWER BEAM, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2008042800262 20080428 00262 EA 2008 4 28 SWIA200819540 1 20080423 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 441SW 7602 FLT 3789 - CAPTAINS SIDE WINDOW CRACKED INFLIGHT. REPLACED CAPTAINS SIDE WINDOW IAW MM 56-12-01. 2 L 7 2 4F RT A21EA 2008042800263 20080428 00263 EU 2008 4 28 08FDEA01535 1 20080424 A 7830 STRUCTURE AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 NR 2 ENGINE OUTBD T/R UPPER T/E COMPOSITE REPAIR EDGES ARE LOOSE. REPLACED NR 2 ENGINE OUTBOARD THRUST REVERSER TRANSLA TOR COWL IAW A300-600 AMM 78-32-11-4. REFERRED ALL WORK TO NON-ROUTINE N01042. 2 L 7 2 4F RT A35EU 2008042800265 20080428 00265 EU 2008 4 28 08FDEA01537 1 20080424 A 7830 STRUCTURE AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 NR 2 ENGINE OUTBD T/R TRANSLATING COWL HAS EXPOSED COMPOSITE CORE. REPLACED THE NR 2 ENGINE OUTBD THRUST REVERSER TRANS LATOR COWL IAW AMM 78-32-11-4. REFERRED ALL WORK TO NON-ROUTINE N01042. 2 L 7 2 4F RT A35EU 2008042800273 20080428 00273 NM 2008 4 28 QXEA200800393 1 20080419 A 3240 UNKNOWN DHAV DHC8 DHC8202 2809007 NM BRAKES ASSY UNKNOWN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 353PH 496 SEA - BRAKES ARE MUSHY. SIGNIFICANT EFFORT ON PEDALS RESULTS IN NO BRAKING. HIGH FORCE APPLIED TO PEDALS RESULTS IN AD EQUATE BRAKING. MAINTENANCE TAXIED THE AIRCRAFT WITH THE ANTI-SKID ON AND OFF WITH NO DEFECTS NOTED. BRAKING FORCES AR E NORMAL. COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008042800275 20080428 00275 EA 2008 4 28 SWIA200819520 1 20080115 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 983CA 7169 FORWARD FLOOR SUPPORT ANGLE AT STA 280 IS CORRODED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ200 SRM 51-44-04 FIG 6 AND 51-42-06 FIG 8. 2 L 7 2 4F RT A21EA 2008042800276 20080428 00276 EA 2008 4 28 SWIA200819521 1 20080115 A 5753 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA TE FLAP CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 983CA 7169 LEFT INBOARD FLAP INTERIOR STRUCTURE HAS SIGNS OF CORROSION, FOUND AT C-CHECK. REPLACED FLAP ASSEMBLY PER CRJ200 AMM 57 -52-08. 2 L 7 2 4F RT A21EA 2008042800278 20080428 00278 EA 2008 4 28 SWIA200819523 1 20080101 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 609SK 10020 FS 280 FLOOR SUPPORT BEAM IS CORRODED AND CRACKED, FOUND AT C-CHECK. REPAIRED FS 280 FLOOR SUPPORT BEAM PER CRJ7/9 SRM 51-42-06 AND REO 620-33-11-265. 2 L 7 2 4F RT A21EA 2008042800281 20080428 00281 NM 2008 4 28 QXEA200800388 1 20080416 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY MALFUNCTIONED A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 355PH 500 SEA - LAVATORY SMOKE DETECTOR WENT OFF. NO EVIDENCE OF SMOKE, OR FIRE. MAINTENANCE COMPLIED WITH A OPERATIONAL CHECKS OF THE SYSTEM AND FOUND NO DEFECTS. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008042800287 20080428 00287 NM 2008 4 28 UPS08M52055 1 20080213 A 5753 HINGE FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING MOUNTED HINGE PIVOT BORE HOLE AND FACE AREA FOUND RUSTY AS MARKED . (PIVOT BEARING REMOVED). LEFT FWD O/B FLAP I/B HINGE PIVOT BORE HOLE & FACE AREA CORROSION REMOVED & FOUND EXCEED LI MIT PER CMM57-44-08. FPI C/OUT IAW DAC NDTSPM R.13 PART08. FOUND NO CRACK EVIDENT. REWORK AREA ETCH INSPECTED & FOUND SATIS PER EN1092-0 8. FLAP PEELING & CADMIUM PLATING C/OUT PER EN1092-08. BUSHING & SHIM FAB PER EN1092-08. BUSHING & SHIMS CADMIUM PLATED AND INSTALLED PER EN1092-08. 2 L 7 3 4F RT A22WE 2008042800289 20080428 00289 NM 2008 4 28 UPS08M52057 1 20080121 A 5753 HINGE FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING HINGE MOUNTED SIDE ATTACHMENT UPPER BORE HOLE AND FACE AREA RUSTY AS MARKED. LEFT FWD O/B FLAP I/B HINGE BARREL NUT UPR BORE & SPOTFACE CORROSION REMOVED & FOUND WITHIN LIMIT PER CMM57 -44-08 PG 613-615R.60. FPI C/OUT IAW DAC NDT SPM R.13. FOUND NO CRACK & CORROSION EVIDENT. LEFT FWD O/B FLAP I/B HING E BARREL NUT UPPER HOLE SPOTFACE THK OF 0.400" ACCEPTED PER EN1092-08. REWORKED AREA ETCHED INSP FOUND SATIS PER EN1092 -08. 2 L 7 3 4F RT A22WE 2008042800293 20080428 00293 NM 2008 4 28 USAA920080913 1 20080418 A 5330 6545774 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 23879 CLT - MAJOR REPAIR - RON - CRACKED FUSELAGE SKIN, BS 727F, S24L. REPAIRED FUSELAGE SKIN, BS 727F, S24L IAW USAIRWAYS EA 100413. 2 L 7 2 4F RT A16WE 2008042800305 20080428 00305 EA 2008 4 28 YOL2008F00000 1 20080324 A 5344 HINGE CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* 30015 NE CABIN DOOR CRACKED E YOLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 21 604BB 5582 AC CURRENTLY IN FOR INSPECTION. CABIN DOOR WAS FOUND TO HAVE CRACKED HINGE. OUR OFFICE IS AWAITING FURTHER INFORMATION AT THIS TIME. (K) 2 L 7 2 4F 4 F RT A21EA 2008042800310 20080428 00310 NE 2008 4 28 EY2R041408001 3 20080414 A 6111 RFC11M1P6A BLADE EMB 120 EMB120 3260201 SO HAMSTD 14RF 14RF9 NE PROPELLER CRACKED B EY2R K NONE O OTHER IN INSP/MAINT 1 GL 03 19126 9544 ZONE 2B CRACK EXCEEDS LIMIT. 2 L 7 2 4T RT A31SO 6 C P11NE 2008042800311 20080428 00311 EA 2008 4 28 N6WA0080401 1 20080413 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE CABIN INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 157GJ 10230 AFT CEILING LEVEL FLOODLIGHT INOPERATIVE. DEFERRED LIGHT IAW MEL 33-51-01-2A. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008042800313 20080428 00313 NE 2008 4 28 EGRR119440 1 20080414 A 5330 7620323033045 SKIN PANEL SKRSKY S76 S76B 8143007 NE PWA PT6 PT6B36 52043 EA BS 254 CRACKED B EGRR K NONE O OTHER IN INSP/MAINT 1 EA 17 176BA 760317 DURING PRELIMINARY INSP FOUND 6.5 INCH CRACK ON LT SIDE SKIN PANEL AT AC STA 254, WATERLINE 107. THE LT SIDE SKIN PANEL WILL BE REPLACED WITH SERVICEABLE ONE. 1 G 7 2 4U 4 U H1NE E4EA 2008042800316 20080428 00316 NM 2008 4 28 CALS097007B 1 20080302 A 2497 FEEDER CABLE BOEING 747 747409 13848AU NM APU GENERATOR CHAFED W SAJF K NONE O OTHER IN INSP/MAINT 1 WP 03 18202 28710 ASKED TO PERFORM THE INSPECTION "APU GENERATOR FEEDER CABLES AND CLAMP STANDOFF FOR CHAFING AGAINST THE WASTE TANK DUCT" , AND FOUND THAT B-18202 LT BULK CARGO COMPARTMENT STA 2060 APU GENERATOR FEEDER CABLE CLAMP STANDOFF BROKEN. THIS HAS B EEN CORRECTED AND RECORDED. IT HAS ALSO BEEN REPORTED TO MFG. 2 L 7 4 4F RT A20WE 2008042800329 20080428 00329 CE 2008 4 28 DJFA041208001 1 20080412 A 2497 CIRCUIT BREAKER BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE ARCED E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 790TA RK252 CREW EXPERIENCED A STRONG ELECTRICAL SMELL IN THE COCKPIT DURING FLIGHT. MAINT FOUND THE 15 AMP STANDBY POWER CIRCUIT B REAKER ARCING. THE CIRCUIT BREAKER WAS REPLACED. FUNCTIONAL CHECKS WERE GOOD AND THE AC WAS RETURNED TO SERVICE. 2 H 7 2 4F 4 F RT A16SW E25EA 2008042800336 20080428 00336 EA 2008 4 28 S9BA200800018 1 20080414 A 5751 CV431 CHANNEL DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6* 52043 EA AILERON WEIGHT CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 888PV 125 620 DURING CAMP INSPECTION, FOUND LT AILERON OB WEIGHT BALANCE CHANNEL CORRODED. REMOVED AND REPLACED WEIGHT AND BALANCE CH ANNEL, AND STATIC BALANCED AILERON IAW SRM 57-50-21 PAGE 3 AND SRM RD6-57-085. 1 H 7 2 3T 3 T RT A9EA E2NE 2008042800337 20080428 00337 SO 2008 4 28 GUUA04120801 1 20080412 A 5210 UNKNOWN EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE DOOR NONE A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 29 261AS 120141 FLIGHT: 9216 F/A COMPLAINS CABIN DOOR HARD TO OPEN. OPERATIONAL CHECK NORMAL, COULD NOT DUPLICATE. 2 L 7 2 4T 4 T RT A31SO E20NE 2008042800338 20080428 00338 2008 4 28 DXTA200803001 4 20080416 A 2210 7022090901 COMPUTER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL YAW ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 918QS 7500223 UPPER YAW DAMP FAIL (A-B) ILLUMINATED AFTER TAKE-OFF. REPLACED B SYSTEM YSAC COMPUTER, IAW 750 MM CH 27-29-01, OP'S CHEC K GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008042800341 20080428 00341 CE 2008 4 28 N760PT041708 1 20080417 A 2120 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN SMOKE E AWKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 25 760PT 7500260 CAE330542 CREW CALLED IN AND REPORTED A LIGHT BLUE HAZE AND OIL SMELL IN THE COCKPIT THAT CLEARED WITHIN (2) MINUTES. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008042800342 20080428 00342 GL 2008 4 28 I5HA08580004 3 20080417 A 6114 HUB CVAC 580 580 2422806 WP ALLSN 501D 501D13A 03004 GL ALLSN A6441 A6441* GL PROPELLER LEAKING A I5HA E ENGINE SHUTDOWN K E FLUID LOSS VIBRATION/BUFFET AP APPROACH 1 GL 25 587X 361 HC2769 ON APPROACH, THE CREW FELT A VIBRATION ON THE NR1 ENGINE AND SHUT IT DOWN AS A PRECAUTIONARY MEASURE. MAINT INSPECTED TH E AC AND FOUND THE NR 1 PROP LEAKING BETWEEN THE HUB AND REGULATOR. THE PROP WAS REMOVED AND REPLACED WITH A SERVICEABLE PROP, RIG CHECKS COMPLETED, THE ENGINE RAN AND THE AC WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT E282 6 C P898 2008042800343 20080428 00343 CE 2008 4 28 4535703312008 1 20080331 A 3150 WARNING LIGHT LEAR 45 45LEAR 5170805 CE ILLUMINATED E J7SA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 441FX 357 RED STAB OVERHEAT CAS MESSAGE ILLUMINATED. PERFORMED CHECKLIST AND LIGHT WENT OUT AFTER SEVERAL MINUTES. IFE DECLARED BY ATC. AIR DIVERSION WITH UNEVENTFUL LANDING AND TAXI. PERFORMED GROUND RUNS WITH BOTH ENGINES AT VARIOUS POWER SETTIN G, CHECKED CONNECTORS AT ECS CONTROLLER, ALL WITH NO DEFECTS NOTED. 2 L 7 2 4F RT T00008WI 2008042800347 20080428 00347 EU 2008 4 28 O2G2008F00000 2 20080329 A 7240 RD5118 BLADE GULSTM G1159 G1159A 3970109 SO RROYCE SPEY SPEY511* 54523 EU NR 1 ENGINE FAILED E O2GA A UNSCHED LANDING C F.O.D. CL CLIMB 1 EA 63 800TD 11387 6189 452 1132 HIGH T,V,I INDICATION AFTER TAKEOFF ON LT ENGINE. AC LANDED, FOUND 2.5 OF 1ST STAGE BLADE MISSING AND DAMAGE TO OTHER B LADES. (K) 2 L 7 2 4F 4 F A12EA E2EU 2008042800349 20080428 00349 EU 2008 4 28 USAA920080910 1 20080422 A 2910 AE2463921G0181 HYDRAULIC LINE AIRBUS A321 A321211 3930370 EU RT MLG LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 182UW 1536 FLT 1585 - PHL-MCO - RTF - AFTER T/O EXPERIENCED LOSS OF FLUID IN 'G' HYDRAULIC SYSTEM FOLLOWED BY SYSTEM LOSS. THE CRE W DECLARED AN EMERGENCY, RETURNED TO PHL AND AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE REPLACED RT MLG DOOR ACTUATOR FLEX LINE AND NR 1 ENGINE HYDRAULIC PUMP. OPERATIONAL CHECK GOOD. INSPECTION OF 'G' SYSTEM FILTERS REVEALED NO CONTAMI NATION. 2 L 7 2 4F RT A28NM 2008042800350 20080428 00350 EU 2008 4 28 USAA920080912 1 20080422 A 2560 P2070001214 FLASHLIGHT AIRBUS A321 A321211 3930370 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 191UW 1447 FLT 1548 SEA-CLT - EMERG EQUIP - F/A FLASHLIGHT AT 2R INOP. MAINTENANCE REPLACED 2R F/A FLASHLIGHT. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A28NM 2008042800358 20080428 00358 NM 2008 4 28 USAA920080878 1 20080415 A 5311 6520722U70 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED FRAME, BS 440, S26R. REPLACED FRAME, BS 440, S26R IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008042800359 20080428 00359 NM 2008 4 28 USAA920080880 1 20080418 A 5311 654652555 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED FRAME, BS 380, S20L - S21L. REPAIRED FRAME, BS 380, S20L - S21L IAW USAIRWAYS E A 100383. 2 L 7 2 4F RT A16WE 2008042800360 20080428 00360 NM 2008 4 28 USAA920080886 1 20080422 A 5330 65458001205 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED FUSELAGE SKIN, BS 344, S16R - S17R. REPAIRED FUSELAGE SKIN, BS 344, S16R - S17R IAW USAIRWAYS EA 100375. 2 L 7 2 4F RT A16WE 2008042800361 20080428 00361 NM 2008 4 28 USAA920080899 1 20080417 A 5712 654544585 RIB BOEING 737 7374B7 1384702 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR-Q6 - LEFT WING RIB CRACKED, WBL 135.5. REPAIRED LEFT WING RIB, WBL 135.5 IAW USAIRWAYS EA 100356. 2 L 7 2 4F RT A16WE 2008042800364 20080428 00364 EU 2008 4 28 UPS08152070 1 20080424 A 3350 SIGN AIRBUS A300 A300F4622R 3930360 EU COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 170UP 0005 INSPECTION TYPE:N/A EXIT SIGN ON BEFORE GEAR EXTENSION, W/SW IN AUTO POS. OPS CHECK GOOD PER AMM 33-51-00-05. 2 L 7 2 4F RT A35EU 2008042800372 20080428 00372 EU 2008 4 28 USAA920080911 1 20080422 A 5210 MS288892 VALVE AIRBUS 320 A320231 3930325 EU R2 DOOR LEAKING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 632AW 81 FLT 514 PHX - EES - R-2 DOOR ASSIST BOTTLE LOW 400 LBS, SUSPECT LEAK. MAINTENANCE REMOVED AND REPLACED VALVE IN THE CYL INDER DOOR DAMPER ASSEMBLY AND SERVICED TO FULL. LEAK CHECK GOOD. 2 L 7 2 4F RT A28NM 2008042800383 20080428 00383 CE 2008 4 28 DXTA200803004 1 20080418 A 3297 CONNECTOR CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE MLG CONTAMINATED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 669QS 5605689 AFTER SELECTING GEAR DOWN, LT MAIN GEAR DID NOT INDICATE DOWN. (2 GREEN 1 RED) FOUND LEFT GEAR DOWNLOCK SWITCH CONNECTO R CONTAMINATED. CLEANED REINSTALLED INDICATIONS NOW CK GD SWUNG GEAR IAW 32-01-00 SYSTEM CHECK GOOD RESET & SERVICED PNE UMATIC BRAKE & GEAR BOTTLE IAW 12-13-01 2 L 7 2 4F 4 F RT A22CE E00059EN 2008042800385 20080428 00385 NE 2008 4 28 DXTA200803007 2 20080421 A 7200 ENGINE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LEFT MALFUNCTIONED E DXTA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 07 684QS 5605084 AFTER TAKEOFF, WHILE CLIMBING OUT OF 6000 FT, RED MASTER WARNING LIGHT ILLUMINATED AND LOW OIL PRESS LT LIGHT WAS FLASHI NG. LT OIL PRESS GAUGE WAS CHECKED AND INDICATED 0 PSI. EMERGENCY CHECKLIST ACCOMPLISHED AND LT ENGINE WAS SHUTDOWN. ENGINE PERFORMED INITIAL TROUBLESHOOTING. INSPECTED OIL FILTER AND OIL FILTER AND COLD START VALE WITH NO DEFECTS IAW E NGINE MM 79-20. (REF SQK 1.4) REMOVED LT ENGINE OIL PUMP IAW ENGINE MM 79-20-02. (REF. SQWK 1.10) ENGINE STILL HAS NO OI L PRESSURE; ENGINE IS TO BE CHANGED. REMOVED ENGINE AND INSTALLED A REPAIRED ENGINE IAW ENGINE MM 71-00-03. AND THE MM 7 1-00-03. REF SQK 1.41 ALL LEAK AND OPERATIONAL CHECKS OK. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008042800393 20080428 00393 CE 2008 4 28 GUUA04170801 1 20080417 A 3260 ANNUNCIATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT LOOSE A GUUA O OTHER N FALSE WARNING AP APPROACH 1 SO 29 17541 UE203 FLIGHT: 9208, DURING APPROACH, LT LANDING GEAR INDICATOR DID NOT ILLUMINATE WITH GEAR DOWN, ATTEMPTED TO PUMP GEAR DOWN. THE ANNUNCIATOR CAME ON BY ITSELF. INSPECTED LANDING GEAR SYS, SECURED ANNUNCIATOR LEGEND. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2008042800023 20080428 00023 NM 2008 4 28 ASAA0852823 1 20080420 A 2432 115195214 CIRCUIT BREAKER BOEING 737 737890 1384527 NM STANDBY POWER OPEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 557AS 35176 FOUND BATTERY STANDBY POSITION INDICATOR CIRCUIT BREAKER OPEN. RESET STANDBY POWER CONTROL UNIT CIRCUIT BREAKER. 2 L 7 2 4F RT A16WE 2008042800033 20080428 00033 EA 2008 4 28 A6WA200840302 1 20080409 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA STUCK A A6WA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 31 468AW 7916 UNABLE TO OPEN SERVICE DOOR USING OUTSIDE HANDLE. (M) 2 L 7 2 4F RT A21EA 2008042800041 20080428 00041 NM 2008 4 28 SWAA082112 1 20080421 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042800066 20080428 00066 NM 2008 4 28 WRLA2008045 1 20080422 A 3232 AYG7378503 ATTACH FITTING DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE LT DOOR ACTUATOR MISSING A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 273WA 48519 KBGR/EDDP - DURING POST-FLIGHT INSPECTION, MAINTENANCE FOUND AFT LT CENTER GEAR DOOR MECHANICAL ACTUATOR ATTACH FITTING AND HARDWARE MISSING. REPLACED BRACKET ASSY AND R&R ROD END IAW MM 32-59-03, RETRACTED & EXTENDED CRT CREA IAW MM 32-35 -00 OPS CK OK LEAK CK OK RII 3058880. REF LP 288467 (A) 2 L 7 3 4F 4 F RT A22WE E24NE 2008042800071 20080428 00071 NM 2008 4 28 ABXA080127 1 20080313 A 5330 141T333055 SKIN BOEING 767 767200 1385120 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 752AX 23434 L1 DOOR CUTOUT LOWER AFT CORNER INTERIOR DOUBLER HAD 2 EACH .25 INCH CRACKS AT THE FASTENER HOLE AND THE EXTERIOR SKIN H AD A .125 INCH CRACK AT THE SAME HOLE. REPAIRED L1 DOOR CUTOUT LOWER AFT CORNER IAW REA B653-57165-MR. 2 L 7 2 4F RT A1NM 2008051600033 20080516 00033 NM 2008 5 16 SWAA082482 1 20080506 A 5230 6547952318 SEAL BOEING 737 7373H4 1384600 NM AFT CARGO DOOR TORN A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 29 615SW 27698 DIVERSION/DECLARED EMERGENCY, AT FL 360 THE CABIN WARNING HORN SOUNDED. VERIFIED LOSS OF CABIN PRESSURE. ACCOMPLISHED EMERGENCY DESCENT CHECKLIST, DECLARED EMERGENCY. INSPECTED AIRCRAFT FOUND AFT CARGO DOOR SEAL TORN AND PARTIALLY OUT OF TRACK. REMOVED AND REPLACED DOOR SEAL PER MM. 2 L 7 2 4F RT A16WE 2008042800104 20080428 00104 WP 2008 4 28 MWEA080059 1 20080422 A 2170 210101 COALESCER BAG DOUG DC9 DC981 3022081 WP A/C BAY DIRTY A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 13 814ME 48010 CABIN CREW AND PASSENGERS REPORTED A BURNING SMELL, THEN DISSIPATED. REMOVED AND REPLACED LEFT AND RIGHT WATER SEPARATO R COALESCER BAGS. 2 L 7 2 4F A6WE 2008042800121 20080428 00121 NM 2008 4 28 ASAA0852828 1 20080422 A 2150 32149721 VALVE BOEING 737 737890 1384527 NM A/C SYSTEM FAULTY A ASAA K NONE O OTHER NR NOT REPORTED 1 NM 02 559AS 35178 CABIN TEMPERATURE VERY DIFFICULT TO CONTROL IN ALL ZONES. ACCOMPLISHED FIM 21 61 TASKS 861 862 863 & 864. FOUND ALL FI LTERS WITH HEAVY SEDIMENT. CLEANED FILTERS AND ACCOMPLISHED MM 21 61 00. CHECKS OK. ACCOMPLISHED FIM 21 61 TASK 862E( 3C). NO DEFECTS FOUND, NO FAULTS NOTED. REPLACED TRIM AIR PRESSURE REGULATOR AND SHUTOFF VALVE. ACCOMPLISHED TRIM AIR PRSOV ADJUSTMENT TEST AS PRECAUTIONARY ACTION. 2 L 7 2 4F RT A16WE 2008042800127 20080428 00127 NM 2008 4 28 ASAA0852831 1 20080406 A 5730 116A441010 SKIN BOEING 737 737890 1384527 NM RT WING DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 577AS 35186 REF L P 6418789 BIRD STRIKE RIGHT WING REQUIRES REPAIR. BIRD STRIKE RIGHT WING REF TO L P 6418789 REPAIRED IAW B737 800 SRM CH 57 41 01AND BOEING DRAWING 116A4521. 2 L 7 2 4F RT A16WE 2008042800135 20080428 00135 NM 2008 4 28 SWAA082191 1 20080423 A 5310 6546818 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 887 TO BS 907, RBL 65. REMOVED AND REPLACED WEB PER SR M. 2 L 7 2 4F RT A16WE 2008042800165 20080428 00165 2008 4 28 SWAA082132 4 20080421 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 433LV 33716 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042800166 20080428 00166 NM 2008 4 28 SWAA082181 1 20080423 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 483WN 32472 EEPLS LENS MISSING AT ROW 3 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008042800174 20080428 00174 NM 2008 4 28 2008UALA02282 1 20080419 A 3510 OXYGEN SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 597UA 28750 OXYGEN PRESSURE DECREASING. EICAS STATUS PARAMETERS DISPLAYED, OXY PRESS. CREW COMMENTS, AT TAKEOFF PRESS 1690, AT LDG 1530. RECONNECTED BOTH CREW OXYG EN MASKS AND LEAKED CHECKED GOOD.RESERVICED CREW OXYGEN PER AMM LEAKED CHECKED ALL FI TTINGS AT CREW OXYGEN BOTTLE AND R EGULATOR AREA AND NO LEAKS FOUND.EICAS READING AND BOTTLE PRESSU RE ONLY 40 PSI DIFF ERENCE.GOOD FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042800180 20080428 00180 NM 2008 4 28 2008UALA02292 1 20080418 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1540 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 AFT PIT AT BS 1540 AND STR 26L, FRAME INBOARD FLANGE DENTED. REMOVED DAMAGE FABRICATED AND INSTALLED RPR IAW 53-00-07 R PR 5.THIS IS A CAT B RPR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSPECTIONS STARTING AT 50,000 TOTAL FLIGHT CYCLES AND 12,0 00FC THEREAFTER. INSPECTIONS CONSISTS O F BOTH VISUAL AND NDT PER SRM 53-00-07 RPR 5 TABLE II. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042800195 20080428 00195 NM 2008 4 28 SWAA082157 1 20080423 A 5311 6516301 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008042800207 20080428 00207 NM 2008 4 28 SWAA082198 1 20080423 A 5315 6546816 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM WEB CORRODED BETWEEN BS 1016 AND BS 1040, BL 0 AND RBL 38. REMOVED AND REPL ACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008042800243 20080428 00243 EA 2008 4 28 SWIA200819528 1 20080118 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 431SW 7536 CABIN EMERGENCY TRACK LIGHTING IS BROKEN, FOUND AT C-CHECK. REPLACED EMERGENCY LIGHTING UPPER TRACK PER CRJ200 AMM 33-5 1-01-020-001 AND 33-51-01-420-001. 2 L 7 2 4F RT A21EA 2008042800244 20080428 00244 EA 2008 4 28 SWIA200819529 1 20080118 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 431SW 7536 CRACK FOUND AT STA280 AND LBL9.0 UPPER ANGLE, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R-53-11-136 -1. 2 L 7 2 4F RT A21EA 2008042800253 20080428 00253 EA 2008 4 28 SWIA200819538 1 20080422 A 3310 LIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT SHORTED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 967SW 7872 FLT 6704 - FIRST OFFICERS YOKE LIGHT IS SHORTING OUT. RESECURED LOOSE HARDWARE ON MAP LIGHT ASSEMBLY. 2 L 7 2 4F RT A21EA 2008042800286 20080428 00286 NM 2008 4 28 UPS08M52054 1 20080121 A 5753 HINGE FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING MOUNTED HINGE SIDE ATTACHMENT LOWER BORE HOLE AND FACE AREA RUSTY AS MARKED. LEFT FWD O/B FLAP I/B HINGE BARREL NUT LWR BORE & SPOTFACE CORROSION REMOVED & FOUND WITHIN LIMIT PER CMM57 -44-08 PG 613-615R.60. FPI C/OUT IAW DACNDT SPM R.13 PART08. NO CORROSION EVIDENT. LEFT FWD O/B FLAP I/B HINGE BARREL NUT LWR HOLE SPOTFACE THK OF 0.392" EVALUATED & FOUND ACCEPTED PER EN1092-08 CADMIUM PLATING C/OUT ON REWORKED AREA & B USHING FAB PER EN1092-08. 2 L 7 3 4F RT A22WE 2008042800371 20080428 00371 NE 2008 4 28 USAA920080909 2 20080421 A 7530 ACTUATOR AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE VSV FAILED A USAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 19 113UW 1141 FLT 1490 - CLT-LGA - RTF - CREW REPORTED TWO AUDIBLE COMPRESSOR STALLS ON THE NR 1 ENGINE ON TAKEOFF. THE AIRCRAFT RETU RNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE VARIABLE STATOR VANE ACTUATOR. ACCELERATION CHECK AN D POWER ASSURANCE RUNS WERE GOOD. (S) 2 L 7 2 4F 4 F RT A28NM E38NE 2008042800384 20080428 00384 NM 2008 4 28 DXTA200803006 1 20080420 A 2782 ACTUATOR GULSTM 200 200 4500308 NM PWC PW306 PW306C 52169 NE SLATS OUT OF ADJUST E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 712QS 073 SLATS FAILED TO RETRACT SLAT UNBALANCED AND FLAP/SLAT MAINT CAS MESSAGES PRESENT. ADJUSTED RT NR 2 SLAT BALLSCREW ACTUA TOR OK TO CONTINUE SERVICE. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A53NM E35NE 2008042900002 20080429 00002 CE 2008 4 29 DXTA200802993 1 20080413 A 3260 1EN18N119 UPLOCK SWITCH RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 873QS 4366 258573 RT MLG INDICATOR RED LIGHT STAYED ON. TROUBLESHOT SYSTEM. REMOVED AND REPLACED RT MLG DOOR UPLOCK SWITCH WITH NEW SWITC H IAW MM 32-60-00. REMOVED RT MLG DOOR FOR X-RAY. RT MLG DOOR X-RAYED BY CERTIFIED INSPECTION SERVICES CRS XI8R997N, PRO JECT NR 15515 AND DETERMINED TO HAVE NO HIDDEN DAMAGE. REINSTALLED RT MLG DOOR ASSY. RETRACTION TESTS GOOD. GAINED ACCES S TO RT MLG NON RETURN VALVE AND ASSOCIATED FILTER. REMOVED CLEANED AND INSPECTED. NO DEFECTS NOTED. INSPECTED WIRING FR OM RT MLG UPLOCK SWITCH TO FWD WING CENTER SECTION. FOUND TO MEET WIRING DIAGRAM 25-8NA5-616A. REPLACED BROKEN FIXED PIL LAR AT JK TERMINAL BOARD IN LEFT WING ROOT WITH NEW FIXED PILLAR. 2 L 7 2 4F 4 F RT A3EU E6WE 2008042900003 20080429 00003 CE 2008 4 29 DXTA200802996 1 20080414 A 3240 991228113 PUMP CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE BRAKE ASSY INOPERATIVE E DXTA O OTHER O OTHER LD LANDING 1 GL 07 353QS 7419 5600530 CREW REPORTED LIGHT ILLUMINATED AS SOON AS SQUAT SWITCH MADE ON LANDING, THEY ONLY GOT 2 GOOD APPLICATIONS BEFORE PREX D EPLETED. AFTER LANDING "POWER BRAKE LOW PRESS" LIGHT CAME ON. NOISE CAME FROM NOSE LIKE ACCUMULATOR IS TRYING TO CHARG E. AFTER SHUTDOWN, BRAKE PEDALS FEEL LOOSE, NO PRESSURE.TROUBLESHOT SYSTEM AND FOUND HYD PUMP ASSY TO BE DEFECTIVE. REMO VED PUMP ASSY P/N 6517102-12 S/N UNKNOWN AND INSTALLED REPAIRED PUMP ASSY P/N 6517102-12 S/N J. REINSTALLED ALL AVIONICS AND PANELS. SERVICED HYD BRAKES, BLED BRAKES AND PERFORMED A GOOD OPERATIONAL CHECK OF BRAKES SYSTEM IAW MM 32-40-00 AN D PERFORMED A GOOD OEPRATIONAL CHECK OF ALL AVIONICS. REF MM 34-10-00. 2 L 7 2 4F 4 F RT A22CE E25EA 2008042900007 20080429 00007 NM 2008 4 29 2008UALA02184 1 20080415 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 FWD ENTRY DOOR UPPER HINGE CUTOUT HAS 2 HOLES SHOWING CRACK INDICATIONS, JUST ABOVE FWD END OF CUTOUT. MAJOR REPAIR ACC OMPLISHED: NO DAMAGE FOUND IN UPPER HOLE ABOVE HINGE CUTOUT BY NDT. REMOVED CRACK FROM LWR HOLE IN BEAR-STRAP. FABRICATE D & INSTALLED FILLER & DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041400052 20080414 00052 CE 2008 4 14 DXTA20082987 1 20080408 A 3230 LANDING GEAR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 960QS 7500160 AFTER T/O, GEAR FAILED TO RETRACT. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008041400054 20080414 00054 CE 2008 4 14 GUUA04050801 1 20080405 A 5520 1016100195 TORQUE TUBE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87555 UE234 DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED LT ELEVATOR TORQUE TUBE EXFOLIATED. REPLACED LT ELEVATOR TORQUE TUBE. 2 L 7 2 4T 3 T RT A24CE E4EA 2008041400057 20080414 00057 NE 2008 4 14 2008040423235 2 20080404 A 7322 0164548720 FUEL CONTROL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE FUEL CONTROL FAULTY E RMXA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 05 350A 418 3127 9301 THE PILOT STATES THAT THE AC LIFTED OFF AND BEGAN A CLIMB TO CLEAR OBSTACLES AND UPON REACHING 100 FEET AGL, A DISTINCT CHANGE IN ENGINE SOUND WAS DETECTED ALONG WITH A SLIGHT YAW TO THE RT FROM THE LOSS OF POWER. THE PILOT IMMEDIATELY LOWE RED THE COLLECTIVE TO PRESERVE ROTOR RPM AND FORTUNATELY THE RPM STABILIZED AT 365-370 RPM AT A LOWER POWER SETTING. I E LECTED TO SET UP FOR A LOW POWER RUN ON LANDING TO THE PARKING LOT, WE WOULD BE LANDING SHORTLY. AS WE APPROACHED THE G ROUND AND AT A SKID HEIGHT OF APPROX. 1-2 FT I APPLIED COLLECTIVE PITCH TO CUSHION THE LANDING, THE ROTOR RPM BEGAN TO B LEED OFF AND THE LOW RPM HORN SOUNDED JUST BEFORE TOUCHDOWN. THE AC TOUCHED DOWN SOFTLY WITH ABOUT A 20 FOOT GROUND SLID 1 G 7 1 3U 3 U H9EU E19EU 2008041400072 20080414 00072 CE 2008 4 14 DXTA200802962 1 20080324 A 7603 501291851 THROTTLE CABLE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT ENGINE FROZEN E DXTA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 322QS 9328 5600421 LT (NR 1) THROTTLE CABLE FROZE IN POSITION AT FL400 AT -40 DEG C RAM. REPLACED THE LT AFT THROTTLE CABLE. CONDUCTED ENG INE RUN AND VERIFIED PROPER RIGGING IAW MM CH 76-11-02. 2 L 7 2 4F 4 F RT A22CE E25EA 2008041400073 20080414 00073 CE 2008 4 14 DXTA200802963 1 20080324 A 4900 38005761 APU CESSNA 750 750 2076810 CE ALLSN AE300 AE3007A GL APU BAY DEFECTIVE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 923QS 3886 7500023 STRONG ODOR COMMING FROM AIR CONDITION AND IN CABIN OF AC. REMOVED DEFECTIVE APU AND INSTALLED A REPAIRED APU. PERFORME D AN OPERATIONAL AND LEAK CHECK. ALL CHECKS PASSED. ALL WORK ACCOMPLISHED IAW MM CHAPTER 49-10-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008041400097 20080414 00097 NM 2008 4 14 ANCF200800007 1 20080408 A 2750 FLAP SYSTEM BOEING 767 7673Y0 NM PWA 4060 PW4060 52119 NE TE FLAPS MALFUNCTIONED W ANCF B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 SO 23 948AV 24948 PILOT REPORT: EICAS MSG TE FLAP DISAGREE DISPLAYED TRAILING EDGE LIGHT ILLUMINATE WHEN ANY TE FLAP POSITION SELECTED. FL APS FAIL TO MOVE TO SELECTED POSITION. IAW FIM 27-51-00 FIG 105. FLAPS OPERATED CORRECTLY TO SELECTED POSITIONS FSEU SH OWS NO FAULTS. MESSAGE SELF CLEARED SUBSEQUENT OPERATION OF FLAPS. DURING SEVERAL CYCLES OK. PLEASE MONITOR AND REPORT I F NECESSARY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041400105 20080414 00105 NE 2008 4 14 Q2SA708001 2 20080407 A 7322 7788004 FUEL CONTROL BOEING 747 7472B5F 1384839 NM PWA JT9 JT9D7R4G2 52054 NE NR 4 ENGINE MALFUNCTIONED A Q2SA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 63 708SA 87406 87406 24196 715288 ATB AT ANC DUE TO ENGINE PROBLEM. NR 4 ENGINE STALLED DURING CLIMB AT 33,600 FT. REDUCED THRUST TO IDLE. IDLE PARAMET ERS N1 37 PERCENT, N2 61 PERCENT, EPR ERRATIC, EGT 483, FF 800. ALL BLEEDS ON, 2 AIR CONDITIONING PACKS ON. 2 AIR COND ITIONING PACKS ON. REMOVED/REPLACED FUEL CONTROL PER AMM 73-12-10. ALSO REMOVED/REPLACED NR 4 ENGINE VANE AND BLEED CONT ROL (EVBC) PER AMM 75-31-09. LEAK CHECK AND ENGINE TRIM SUCCESSFULLY ACCOMPLISHED. 2 L 7 4 4F 4 F RT A20WE E3NE 2008041400112 20080414 00112 EU 2008 4 14 08FDEA01378 1 20080410 A 5712 A57840056203 RIB AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT RT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOLDING SLAT NR 1 RT , FOUND MISDRILLED HOLE DURING EMBODIMENT OF SB 57-6067 REPAIR PERFORMED DURING EMBODIMENT OF SB 57 -6067 BY INSTALLING OVERSIZED BLIND RIVET AND 4,00MM RIVETS IN OFFSET HOLES IAW RAS/BAE/1006919/2008 ISS A, APPROVED BY EA 6-5742-115256. 2 L 7 2 4F RT A35EU 2008041400140 20080414 00140 EU 2008 4 14 NWAA081513318 1 20080407 A 2160 CONTROLLER AIRBUS 330 A330323 3930335 EU CABIN TEMP MALFUNCTIONED A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 818NW 0857 FUMES OF MELTING PLASTIC OR HEATED WIRING REPORTED IN FLIGHT ATTENDANT CREW REST AREA (LDMCR) BY FLIGHT ATTENDANT AND LA NDING WAS UNEVENTFUL. REPLACED LDMCR TEMPERATURE CONTROLLER AND TESTED OK, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A46NM 2008041400144 20080414 00144 SO 2008 4 14 SWIA200819459 1 20080403 A 4900 RELAY EMB 120 EMB120ER 3260203 SO APU SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 293SW 120320 FLT 3523 - SMELLED SMOKE IN COCKPIT. REPLACED APU FEEDER PROTECTION RELAY. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008041400145 20080414 00145 EA 2008 4 14 SWIA200819460 1 20080405 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 706SK 10149 LEFT SIDE AFT PIECE OF EMERGENCY FLOOR LIGHTING IS BROKEN. REPLACED LEFT SIDE AFT PIECE OF EMERGENCY FLOOR LIGHTING IAW CRJ 700 AMM 33-51-01. 2 L 7 2 4F RT A21EA 2008041400146 20080414 00146 EA 2008 4 14 SWIA200819461 1 20080409 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 471CA 7655 FLT 2555 - CAPTAINS SIDE WINDOW IS SHATTERED. REPLACED CAPTAINS SIDE WINDOW PER AMM 56-12-01, PN: NP-139322-5, SN OFF: 02035H7795. 2 L 7 2 4F RT A21EA 2008041400147 20080414 00147 EA 2008 4 14 SWIA200819462 1 20080406 A 3350 COVER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT MISSING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 448SW 7678 FLT 3288 - COVER ON EXIT LIGHT MISSING. INSTALLED A SERVICEABLE LIGHT COVER AS NEEDED. 2 L 7 2 4F RT A21EA 2008041400150 20080414 00150 EA 2008 4 14 SWIA200819465 1 20080409 A 2440 RECEPTACLE CNDAIR CL600 CL6002C10 1390015 EA GROUND POWER LOOSE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 608SK 10252 FLT 4082 - WHEN CONNECTING GROUND POWER TO AIRCRAFT, SAW A PUFF OF SMOKE. INSPECTED AREA AND SYSTEMS WITH NO DISCREPENC IES NOTED. RESECURED GROUND POWER RECEPTICLE. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008041400153 20080414 00153 EA 2008 4 14 SWIA200819468 1 20080108 A 5510 PIVOT ASSY CNDAIR CL600 CL6002C10 1390015 EA HORIZONTAL STAB WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 756SK 10221 INNER AND OUTER HORIZONTAL STABILIZERS PIVOT PINS ARE WORN, FOUND AT C-CHECK. COMPLIED WITH REPAIRS IAW REO 670-55-11-1 12 AS REQUIRED. 2 L 7 2 4F RT A21EA 2008041400158 20080414 00158 NM 2008 4 14 08FDEA01384 1 20080410 A 5347 BAC1520792 SEAT TRACK BOEING 757 75727B 1384921 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 CORROSION ON SEAT TRACK AT STA 1266, STA 1280, RBL 24. SEAT TRACK AT STA 1266 TO STA 1280, RBL 24 REPLACED NEW TRACK AS PER B757-200 SRM 51-10-02 REV 93. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008041500074 20080415 00074 2008 4 15 SWAA081865 4 20080408 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 204WN 29855 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008041400162 20080414 00162 WP 2008 4 14 NWAA081539861 1 20080410 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 770NC 47758 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY FLOOD LIGHT FOR THE AFT EVACUATION SLIDE WAS NOT FUNCTIONAL. MA INTENANCE FOUND THE BATTERY PACK B5-28 FAULTY AND REPLACED IT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A6WE 2008041400168 20080414 00168 NM 2008 4 14 F3LA200800143 1 20080330 A 3350 TDL30WB40 LAMP AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE EMERGENCY LIGHTS DEFECTIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 343 1841 DURING C4 S1 C CHECK, INSPECTION REPORTED THE EMERGENCY EXIT LIGHT, ABOVE THE L1 DOOR ENTRANCE, FLICKERED. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-21-11-020-50 AND AMM 33-21-11-42-050. THE LAMP WAS OPERATIONALLY TESTED IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 32-21-11-710-050 AND TESTED OKAY. 2 L 7 2 4F 4 F RT A28NM 2008041400174 20080414 00174 EU 2008 4 14 AALA200800695 1 20080322 A 2720 359301001 MODULE AIRBUS 300 A300B4605R 3930308 EU RUDDER TRIM FAILED A AALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 70072 515 AUA INFLIGHT T2106/22MAR CCS TO MIA - CREW REPORTED SMOKE IN COCKPIT. LANDED AUA WITHOUT INCIDENT. FOUND RUDDER TRIM M ODULE FAILED DURING FLIGHT. REPLACED RUDDER TRIM MODULE AND INSPECTED WIRING HARNESSES AND COCKPIT SYSTEMS. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008041400176 20080414 00176 NM 2008 4 14 AALA200800697 1 20080322 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT AT SEAT 22C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041400181 20080414 00181 NM 2008 4 14 AALA200800700 1 20080322 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT AT SEAT 24C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041400182 20080414 00182 NM 2008 4 14 AALA200800702 1 20080323 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 MIA - EMERGENCY LIGHT AT SEAT 24C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041400198 20080414 00198 NM 2008 4 14 AALA200800727 1 20080326 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 752AN 30260 DFW - EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041500002 20080415 00002 NM 2008 4 15 USAA920080720 1 20080327 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 590US 23935 CLT - MAJOR REPAIR - C2 CHECK - CRACKED FUSELAGE SKIN, BS 742, S24L. REPAIRED FUSELAGE SKIN, BS 742, S24L IAW USAIRWAYS TYPICAL REPAIR 53-33 REPAIR 31. 2 L 7 2 4F RT A16WE 2008041500003 20080415 00003 NM 2008 4 15 USAA920080721 1 20080328 A 5311 652072240 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 460UW 25024 PIT - MAJOR REPAIR - FPBH INSPECTION, CRACKED FRAME, BS 440, S24R. REPAIRED FRAME, BS 440, S24R IAW USAIRWAYS EA 110807 . 2 L 7 2 4F RT A16WE 2008041500008 20080415 00008 EA 2008 4 15 TRAX200800453 1 20080321 A 5210 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 AAR - 8011 - PAX DOOR UPPER TORQUE TUBE AFT COVER PLATE ATTACHMENT, 1 EACH ANGLE IS CRACKED. REMOVED CRACKED PAX DOOR U PPER TORQUE TUBE COVER AFT ATTACHMENT ANGLE AND REPLACED WITH SERVICEABLE ANGLE P/N: 601R31902-555 IAW CRJ 200 SRM 51-41 -02. NF15062 03/26/08. SUPPLEMENTAL SDR CLOSED 4/3/08. 2 L 7 2 4F RT A21EA 2008041500010 20080415 00010 EA 2008 4 15 TRAX200800390 1 20080309 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 917EV 7769 LEFT AND RIGHT SIDE CLIPS ARE CRACKED ON THE AFT SIDE OF THE PRESSURE BULKHEAD FS 625.3. LUBED PAX DOOR IAW CRJ MM 12-2 0-52. PERFORMED FUNCTIONAL TEST OF INNER HANDLE WITH NO DEFECTS NOTED IAW CRJ MM 52-11-00. SUPPLEMENTAL SDR CLOSED 4/3 /08. 2 L 7 2 4F RT A21EA 2008041500013 20080415 00013 EU 2008 4 15 SA08024 1 20080403 A 2560 P2070003001 FLASHLIGHT AIRBUS A319 A319112 3930323 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 722US 1097 PIT - FLIGHT ATTENDANT AFT LEFT JUMPSEAT LOWER FLASHLIGHT NOT BLINKING. MAINTENANCE REPLACED THE FLASHLIGHT. 2 L 7 2 4F RT A28NM 2008041500018 20080415 00018 NM 2008 4 15 USAA920080733 1 20080401 A 5230 453N1735 SEAL BOEING 737 7373G7 1384595 NM CARGO DOOR TORN A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 308AW 24710 FLT 70 - PHX-SEA - CREW REPORTED AFTER LEVELING OFF AT FL340, RECEIVED A "CABIN ALTITUDE WARNING HORN" FOLLOWED BY A RIS E IN CABIN PRESSURE ALTITUDE. CREW DESCENDED TO FL 200 AND DECLARED AN EMERGENCY. CREW DIVERTED TO LAS. CABIN WAS NOT PREPPED. THE LANDING WAS UNEVENTFUL. MX DISCOVERED AFT CARGO DOOR SEAL TORN. MX REPLACED SEAL. PRESSURIZATION CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2008041500023 20080415 00023 NM 2008 4 15 BB08047 1 20080404 A 2560 ACREM1A MEGAPHONE BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 937UW 27245 PHL - THE AFT MEGAPHONE WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE AFT MEGAPHONE. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 2008041500026 20080415 00026 EA 2008 4 15 TRAX200800452 1 20080321 A 5320 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 355CA 10067 RIGHT SIDE 280 CROSSBEAM CORRODED UPPER SURFACE. REPAIRS PERFORMED IAW BOMBARDIER REO 670-53-11-046 AND CRJ 700 SRM 51- 42-06 AND 51-24-28. SUPPLEMENTAL SDR CLOSED 4/4/08. JOB COMPLETE. 2 L 7 2 4F RT A21EA 2008041500030 20080415 00030 NM 2008 4 15 USAA920080695 1 20080310 A 5320 650335912 REVEAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED L1 DOOR CUTOUT REVEAL, BS 348, WL 220. REPLACED L1 DOOR CUTOUT REVEAL, BS 348, WL 220 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041500031 20080415 00031 NM 2008 4 15 USAA920080729 1 20080311 A 5320 65C3267723 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED SHEAR WEB, BS 990, RBL 38, WL 208. REPLACED SHEAR WEB, BS 990, RBL 38, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041500032 20080415 00032 NM 2008 4 15 USAA920080730 1 20080311 A 5330 6545775594 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FUSELAGE SKIN, BS 727E, S24R. REPAIRED FUSELAGE SKIN, BS 727E, S24R IAW B737 S RM 53-00-01-2R31. 2 L 7 2 4F RT A16WE 2008041500034 20080415 00034 NM 2008 4 15 USAA920080732 1 20080312 A 5311 6546529 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 440, S8L - S9L AND S8R - S9R. REPAIRED FRAME, BS 440, S8L - S9L AND S8R - S9R IAW USAIRWAYS EA 5311-01019. 2 L 7 2 4F RT A16WE 2008041500036 20080415 00036 NM 2008 4 15 USAA920080735 1 20080312 A 5311 6546550 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 787, S8L - S9L AND S8R - S9R. REPAIRED FRAME, BS 787, S8L - S9L AND S8R - S9R IAW USAIRWAYS EA 5311-01019. 2 L 7 2 4F RT A16WE 2008041500039 20080415 00039 NM 2008 4 15 USAA920080738 1 20080312 A 5311 65C25229 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 727D, S8L - S9L. REPAIRED FRAME, BS 727D, S8L - S9L IAW USAIRWAYS EA 5311-01019. 2 L 7 2 4F RT A16WE 2008041500041 20080415 00041 NM 2008 4 15 USAA920080740 1 20080314 A 5312 651758243 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED BULKHEAD WEB, BS 178, LBL 17.1, WL 230. REPAIRED BULKHEAD WEB, BS 178, LBL 17. 1, WL 230 IAW 737 SRM 53-10-08-2R12. 2 L 7 2 4F RT A16WE 2008041500042 20080415 00042 NM 2008 4 15 USAA920080741 1 20080318 A 5320 655289414 COVER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED INTERCOSTAL WEB / COVER, BS 540, RBL 24 - RBL 44, WL 208. REPLACED INTERCOSTAL WEB / COVER, BS 540, RBL 24 - RBL 44, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041500047 20080415 00047 NM 2008 4 15 USAA920080746 1 20080314 A 5313 654988630 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER, BS 500C, S16R. REPAIRED STRINGER, BS 500C, S16R IAW AWA ER 03-5312-0 1094-DD1. 2 L 7 2 4F RT A16WE 2008041500048 20080415 00048 EA 2008 4 15 TRAX200800484 1 20080403 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 855AS 7395 EN ROUTE THE COVER ON ONE OF THE FLOOR EMERGENCY LIGHTS CAME OFF AND IT STOPPED WORKING. 2 L 7 2 4F RT A21EA 2008041500051 20080415 00051 NM 2008 4 15 SWAA081845 1 20080407 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 224WN 32493 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008041500053 20080415 00053 NM 2008 4 15 SWAA081847 1 20080407 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 350, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500055 20080415 00055 2008 4 15 SWAA081848 4 20080407 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008041500057 20080415 00057 NM 2008 4 15 SWAA081850 1 20080407 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008041500058 20080415 00058 NM 2008 4 15 SWAA081851 1 20080407 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 414WN 29820 EEPLS LENS LOOSE AT ROW 3 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008041500065 20080415 00065 NM 2008 4 15 SWAA081856 1 20080407 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008041500070 20080415 00070 NM 2008 4 15 SWAA081858 1 20080407 A 3350 311500 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 715SW 27849 DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS BROKEN AT ROW 2 DEF. REMOVED AND REPLACED LIGHT LE NS PER MM. 2 L 7 2 4F RT A16WE 2008041500075 20080415 00075 NM 2008 4 15 SWAA081866 1 20080408 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 243WN 34863 DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 23 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008041500077 20080415 00077 NM 2008 4 15 SWAA081881 1 20080408 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008041500088 20080415 00088 NM 2008 4 15 SWAA081874 1 20080408 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 411WN 29821 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008041500094 20080415 00094 NM 2008 4 15 SWAA081890 1 20080408 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041500095 20080415 00095 NM 2008 4 15 SWAA081876 1 20080408 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041500097 20080415 00097 NM 2008 4 15 SWAA081891 1 20080408 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 27R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041500098 20080415 00098 NM 2008 4 15 SWAA081893 1 20080408 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 849, RBL 13. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041500099 20080415 00099 NM 2008 4 15 SWAA081892 1 20080408 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 792, RBL 13. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041500106 20080415 00106 EA 2008 4 15 TRAX200800454 1 20080321 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 AAR - 1022 - FS 280 CRACKED O/B OF LBL 9 JUST O/B OF PULLEY BRACKET. COMPLIED WITH EO 600-53-91. REPAIR OF AFT FLAP SU PPORT ANGLE AT FS 280 AND REO 601R-53-11-311. REPAIRED J-ANGLE ON THE PILOTS BULKHEAD AT FS 280.0 LEFT BL 9.0 IAW EO 60 0-53-0091. SUPPLEMENTAL SDR CLOSED 4/10/08. 2 L 7 2 4F RT A21EA 2008041500112 20080415 00112 NM 2008 4 15 SWAA081900 1 20080409 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008041500116 20080415 00116 NM 2008 4 15 SWAA081905 1 20080409 A 5310 6546564 DOOR FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR CUTOUT FWD FRAME CRACKED AT BS 951, BETWEEN STR 10R AND STR 11R. REMOVED AND REPLACED FRAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 2008041500118 20080415 00118 EA 2008 4 15 VNAA0804003 1 20080404 A 2133 1037708 OUTFLOW VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CABIN PRESSURE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 206PS 8089 7860 CREW REPORTED A CABIN ALTITUDE CAUTION MESSAGE ON CLIMBOUT OF CLT. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INC IDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE PRESSURIZATION SYSTEM. MAINTENANCE REMOVED AND REPLACED THE PRI MARY OUTFLOW VALVE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008041500120 20080415 00120 EA 2008 4 15 VNAA0803012 1 20080328 A 5730 PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT WING DAMAGED A VNAA O OTHER O OTHER DE DESCENT 1 GL 05 229PS 7898 CREW REPORTED A LIGHTNING STRIKE DURING DESCENT INTO LEX. MAINTENANCE PERFORMED AN EN ROUTE AND A DETAILED LIGHTNING ST RIKE INSPECTION. MAINTENANCE FOUND DAMAGE TO THE RIGHT WING PANELS. MAINTENANCE REPAIRED DAMAGE PER REO 601R-57-31-100 5. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008041500121 20080415 00121 EA 2008 4 15 VNAA0803013 1 20080328 A 2120 DUCT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE CABIN CONTAMINATED A VNAA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 05 705PS 10144 CREW REPORTED AN ERRONEOUS AFT LAVATORY "FIRE WARNING" ON CLIMBOUT OF CLT INSTEAD OF SMOKE DETECTOR WARNING. CREW DECLA RED AN EMERGENCY AND RETURNED TO LAND IN CLT WITHOUT FURTHER INCIDENT. MAINTENANCE AND THE FIRE DEPARTMENT INSPECTED TH E LAVATORY AND FOUND NO EVIDENCE OF FIRE. MAINTENANCE SUSPECTED THE "SMOKE DETECTOR" WENT OFF WHEN THE AIRCRAFT BLEED A IR SYSTEM WAS TURNED ON DUE TO CONTAMINATION IN THE DUCT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE LAVATORY SMOK E DETECTION SYSTEM AND ALL BLEED AIR SOURCES IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL WITH NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008041500129 20080415 00129 EA 2008 4 15 TRAX200800497 1 20080407 A 5210 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA ASD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 723EV 10132 ASD FWD SIDEWALL CRACKED AT 2ND STEP RISER. 2 L 7 2 4F RT A21EA 2008041500138 20080415 00138 EA 2008 4 15 TRAX200800511 1 20080408 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 CRACK IN INTERCOSTAL ATTACH ANGLE STA 484 RBL 36 (MARKED). REMOVED CRACKED ATTACH ANGLE. FABRICATED PER REO 601R-53-41- 059 NEW SERVICEABLE ATTACH ANGLE. OK TO INSTALL. INSTALLED NEW SERVICEABLE ATTACH ANGLE IAW SRM 51-25-16, 51-41-21 AND REO 601R-53-41-059. NEW SERVICEABLE ATTACH ANGLE. AAR356. OK TO INSTALL NEW SERVICEABLE ATTACH ANGLE. INSTALLED NEW SE RVICEABLE ATTACH ANGLE IAW SRM 51-25-16, 51-41-21 AND REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 2008051500032 20080515 00032 NM 2008 5 15 F3LA200800233 1 20080501 A 5311 D5347112320300 FRAME AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED UPON REMOVAL OF SHEAR PLATE FOUND FRAME SUPPORT TO BE CORRODED ON UNDER SIDE. MAI NTENANCE REMOVED CORRODED FRAME SUPPORT AND REPLACED WITH NEW SERVICEABLE FRAME SUPPORT IN ACCORDANCE WITH THE REQUIREME NTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008041500140 20080415 00140 EA 2008 4 15 TRAX200800513 1 20080408 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 PAX DOOR STEP 832 CT AFT STEP LANDING IS CRACKED IN THE CORNER RADIUS. REPAIRED PAX DOOR STEP LANDING 832CT IAW REO 601 R-52-11-702. 2 L 7 2 4F RT A21EA 2008041500150 20080415 00150 EA 2008 4 15 TRAX200800524 1 20080410 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 724EV 10138 LEFT AFT MOST EXTERNAL EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008041500153 20080415 00153 EA 2008 4 15 TRAX200800527 1 20080410 A 5313 STRINGER CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 723EV 10132 STRINGER 25 RT HAS CORROSION DAMAGE JUST AFT OF FS 333.00 IN MAIN AVIONICS BAY. REMOVED CORRODED STRINGER PER SRM 51-4 2-06, BLEND SPLICE FOUND TO BE OUT OF LIMITS. DRILLED AND INSTALLED NEW STRINGER SPLICE 25 RT PER SRM 51-40-11, 51-42-06 AND 51-42-21. 2 L 7 2 4F RT A21EA 2008041500154 20080415 00154 NM 2008 4 15 SWAA081906 1 20080410 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 201LV 29854 DURING SCHEDULED HC1 CHECK, FOUND EEPLS LENS CRACKED AT ROW 2 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008041500158 20080415 00158 NM 2008 4 15 08FDEA01306 1 20080404 A 5315 BAC15061108 FLOORBEAM BOEING 727 727200 138407E NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 MAIN CARGO COMP STA 760-848 LBL 24 T-CAP CORRODED REMOVED SEAT TRACK AND T-CAP IAW SRM 51-30-2. LOCATED AND DRLLED NEW T-CAP IAW SRM 53-10-2 FIG 7 AND 51-30-5. TREATED AND PRIMED NEW T-CAP IAW SRM 51-10-2. INSTALLED NEW T-CAP AND SEAT TRACK AT MAIN CARGO COMPARTMENT STA 760 TO 848, LBL 24 IAW SRM 51-30-2 AND 53-10-2 FIG 7. 2 L 7 3 4F RT A3WE 2008043000045 20080430 00045 EA 2008 4 30 A6WA200840237 1 20080318 A 2721 601R5122623 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA RUDDER TRIM MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 31 402AW 7281 RUDDER TRIM STICKS IN RIGHT RUDDER. RUDDER TRIM IS CENTERED. REMOVED AND REPLACED RUDDER TRIM PANEL, OPS CHECK OK PER AMM 27-20. (M) 2 L 7 2 4F RT A21EA 2008041500159 20080415 00159 EA 2008 4 15 A6WA200840271 1 20080325 A 5720 ANGLE CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 LT WING OUT AND INBOARD ANGLES AT WS 148 CRACKED 1 INCH BY 2 INCH. (M) ANGLES REPLACED IAW SRM 51-40-11. 2 L 7 2 4F RT A21EA 2008041500163 20080415 00163 EA 2008 4 15 A6WA200840225 1 20080317 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 31 404AW 7294 FLAPS FAIL CAS MESSAGE AFTER LANDING WHEN FLAPS SELECTED TO ZERO FLAPS READ ZERO ON FLIGHT CONTROL PAGE. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4, FLAPS RESET AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2008041400074 20080414 00074 CE 2008 4 14 DXTA200802964 1 20080325 A 3230 1283640667 CIRCUIT BOARD BEECH MU300 400A 1155402 CE MLG FALSE INDICATION E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 138QS 759 RK492 UPON GEAR RETRACTION,ALL GREEN DOWN AND LOCKED LIGHTS EXTINGUISHED. HOWEVER,RED IN TRANSIT LIGHT REMAINED ILLUMINATED. R EPLACED GROUND SAFE PCB A161. OPS CHECK GOOD. IAW MM 32-60-00. 2 H 7 2 4F RT A16SW 2008041400075 20080414 00075 CE 2008 4 14 DXTA200802965 1 20080325 A 2731 99145584 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL PITCH FEEL INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 933QS 5994 7500133 AFTER TAKEOFF, WHILE ACCELERATING THROUGH 240 KIAS AT5000 FT, PITCH FEEL FAIL CAS MESSAGE ILLUMINATED. REMOVED RT PITCH FEEL ACTUATOR AND REPLACED IAW MM 27-33-00. ALL OPS CHECKS IAW MM 27-30-00. ALL CHECKS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008041400080 20080414 00080 CE 2008 4 14 DXTA200802975 1 20080331 A 2170 COALESCER BAG CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 900QS 7500123 STRONG ODOR COMING FROM PACS, UNABLE TO ISOLATE WHICH PACK. SMELLS LIKE BURNING OFF OF CHEMICALS. REMOVED CABIN AND C OCKPIT COALESCER SOCKS. INSTALLED NEW SOCKS. CLEANED AND REASSEMBLED CABIN AND COCKPIT COALESCERS. BOTH SYSTEMS OPS AND LEAK CHECK GOOD. WORK PERFORMED REF THE MM 21-51-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008041400092 20080414 00092 CE 2008 4 14 DXTA200802987 1 20080408 A 3222 STRUT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG LOW PRESSURE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 960QS 7500160 AFTER T/O, GEAR FAILED TO RETRACT. T/S: FOUND NOSE STRUT PRESSURE LOW ALLOWING STRUT TO COMPRESS FROM FWD AIRSPEED PRES S DURING TAKEOFF CAUSING NOSE STRUT TO MISS UPLOCK. SERVICED NOSE STRUT. ALL OPS CHECKS GOOD IAW MM 12-10-38 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008041400100 20080414 00100 GL 2008 4 14 R025878 3 20080409 A 6110 83867 CLAMP HARTZL HCB3TN3B BEECH 90 E90 1152914 CE PWA PT6 PT6A28 EA HARTZL HCB3T HCB3TN3 GL PROPELLER BLADE CRACKED B SJ3R K NONE O OTHER IN INSP/MAINT 1 GL 05 SJ3R 1441 BUA24770 BUA24770 838-67 CLAMP ASSY SN EF3099. CRACK FOUND INTERSECTING THE THREADED LINK SCREW HOLE. 1 L 7 2 3T 4 T 3A20 E4EA 6 C P15EA 2008041400109 20080414 00109 EU 2008 4 14 NSVA2008016 1 20080406 A 2930 INDICATION SYS SAAB SF340 340B 7860101 EU HYD SYSTEM MALFUNCTIONED A NSVA B EMER. DESCENT N FALSE WARNING AP APPROACH 1 EA 27 369PX 340B295 ON DESCENT, EMERGENCY DECLARED DUE TO HYD QTY INDICATOR READING ZERO. MAINTENANCE RESET CB M, SYSTEM OPS CHECK NORMAL I AW AMM 29-31-10. NO LEAKS NOTED. 2 L 7 2 4T RT A52EU 2008041400113 20080414 00113 EU 2008 4 14 08FDEA01379 1 20080410 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 448FE 260 PREVIOUS REPAIR LOCATED ON MAIN CABIN SEAT TRACK NR 2 LT Y450 BETWEEN FRAMES 51 TO 52 HAS 2 EA REPAIR SPLICES MEASURING 7 IN LONG BY 3 IN TALL AND 1 REPAIR SECTION 51.9 IN LONG FROM FR 54 TO BETWEEN FRAMES 51 AND 52 REPAIR NOT IAW SRM REQUI REMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT SEAT TRACK REPAIR IAW A310 SRM 53-10-16, PAR 7 PAGES 227 - 232, FIG 20. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008041400116 20080414 00116 WP 2008 4 14 08FDEA01382 1 20080410 A 5347 60715870750T6 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 361FE 48260 MCD SEAT TRACK RBL 77 BETWEEN STA 840 TO 920 IS IN BARE METAL AND SUPERFICAL CORROSION. REMOVED LIGHT CORROSION FOUND T O BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED AND INSTALLED NEW TRACK IAW SRM 53-70-00. FABBED NEW TRACK AND SPLICE ON TRAVELERS T8/733283 AND T8/733215. CLASSIFIED AS MAJOR REPAIR. 2 L 7 3 4F RT A22WE 20081010 NM 2008 10 10 UIE2008F00040 1 20080914 A 5311 FRAME BOEING 747 7472D7B 1384803 NM BS 1780 S12-13R DENTED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 523MC 21782 BS 1780 FRAME BETWEEN S-12R AND S-13R DENT. REPAIRED IAW MFG SERVICE REQUEST 1-954640956 APPROVED BY FORM 8100-9 DATED 1 2 SEPT 2008, DETAILS OF WORK KEPT AT EO 4753B201. (K) 2 L 7 4 4F RT A20WE 2008041400133 20080414 00133 EU 2008 4 14 F3LA200800138 1 20080404 A 5320 D53471123203 SUPPORT AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 C-CHECK, INSPECTION REPORTED CORROSION WAS FOUND AT FRAME SUPPORT OF FLOORBEAM Y1732 AFT OF FRAME 69. MAIN TENANCE REMOVED AND REPLACED FRAME SUPPORT IN ACCORDANCE WITH SRM 51-42-11 PARAGRAPH 6, 7 AND 14 AND EA A9-53R-30196. UP ON COMPLETION OF THE INSTALLATION THE FRAME SUPPORT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041400143 20080414 00143 EA 2008 4 14 SWIA200819458 1 20080404 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 945SW 7770 FLT 6681 - RIGHT REAR OVERWING EMERGENCY LIGHT IS INOP. REPLACED RIGHT MOST AFT OVERWING EMERGENCY LIGHT IAW RJ 200 MM 33-51-21. 2 L 7 2 4F RT A21EA 2008041400155 20080414 00155 EA 2008 4 14 SWIA200819470 1 20080111 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 947SW 7786 FS 280 AT LBL9.0 LOWER FLOORBEAM IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-53-11-171 REV D DATED 02-13-07 REPAIR SCHEME B. 2 L 7 2 4F RT A21EA 2008041400156 20080414 00156 EA 2008 4 14 SWIA200819471 1 20080111 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 947SW 7786 FS 280 AND RBL 9.0 LOWER FLOORBEAM IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-53-11-171 R EV D DATED 02-13-07 REPAIR SCHEME B. 2 L 7 2 4F RT A21EA 2008041400157 20080414 00157 EU 2008 4 14 08FDEA01383 1 20080410 A 5740 A5387003720100 FITTING AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RT UPPER CIRCUMFERINTIAL FITTING LOWER FASTENER INDICATES EDDY CURRENT CRACK INDICATION PER NTM 57-10-54. REMOVED AND R EINSTALLED FLOOR TRIM AND AIRDUCT, AND FLOOR FITTING IAW A310 SRM 51-40-21 PARA 5, EDDY CURRENT INSP, INDICATION OF CRAC K IN FITTING IAW A310NTM 57-10-54 PT 6, MAT ID AND FAB NEW FITTING IAW AIRBUS DWG A53870037 REV G, LOCATED FITTING IAW A 310 SRM 51-40-44 TABLE 1, ALODINED, PRIMED, AND PAINTED FITTING IAW A310 AMM 51-75-10-8. 2 L 7 2 4F RT A35EU 2008041400159 20080414 00159 EU 2008 4 14 08FDEA01385 1 20080411 A 5330 SKIN AIRBUS 310 A310222 3930315 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 448FE 260 1 FASTENER HOLE AT FR 54, STRINGER 40 RT HAS DOUBLE DRILL AND DAMAGE IN COUNTERSINK REPAIRED DAMAGE HOLE IAW FED EX EA 6-5310-118123. 2 L 7 2 4F RT A35EU 2008041400170 20080414 00170 NM 2008 4 14 F3LA200800144 1 20080403 A 5347 D5311278220201 SEAT TRACK AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 5380 1841 DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON SEAT TRACK Y-1292, AT FUSELAGE STATION 810, ON THE RIGH T SIDE, EXTENDING FORWARD TOWARD FRAME 20. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IN ACCORDANCE WITH THE REQUI REMENTS OF A319 SRM 51-72-11, PAGES 1 AND 2. UPON COMPLETION OF THE INSTALLATION, IT WAS INSPECTED AND FOUND ACCEPTABLE . 2 L 7 2 4F 4 F RT A28NM 2008042400092 20080424 00092 EU 2008 4 24 08FDEA01466 1 20080421 A 5797 WIRE HARNESS AIRBUS 300 A300F4605R 3930327 EU RT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 RIGHT WING ABOVE THE NR 2 ENGINE PYLON INSIDE THE WING FIXED L/E; A WIRE BUNDLE HAS SEVERAL WIRES WITH THE INSULATION CH AFED THROUGH EXPOSING INDIVIDUAL WIRES. PREVIOUS REPAIR IS CHAFED THROUGH & TORN. INSTALLED A PROTECTIVE SLEEVE ON THE WIRES REF ESPM 20-53-51. REPOSITIONED AND RESECURED WIRE HARNESS REF ESPM 20-33-44. NO WIRING WAS DISCONNECTED OR DIS TURBED. 2 L 7 2 4F RT A35EU 2008042900008 20080429 00008 NM 2008 4 29 2008UALA02187 1 20080415 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 290 S3L GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 UPPER FUSELAGE REPAIR DOUBLER IS GOUGED AT BS 290 AND STRINGER 3L IS GOUGED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED DOUBLER. INSTALLED NEW REPAIR. REPAIR INSTALLED WITH SOLID RIVETS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042900014 20080429 00014 NM 2008 4 29 FE5F200800001 1 20080422 A 5711 SPAR DOUG MD80 MD83 3023681 NM PWA JT8 JT8D217C 52053 NE LT WING CORRODED W FE5F K NONE O OTHER IN INSP/MAINT 1 WP 03 28035 15491 53480 P726959 FOUND LT WING REAR SPAR HAS CORROSION MARKS AT STA 367-361 C (EO) (L-5.875 IN,W-0.875 IN,D-0.125 IN). 2 L 7 2 4F 4 F RT E9NE 2008043000001 20080430 00001 SO 2008 4 30 C2XA08ON115 1 20080414 A 2612 902061 CONTROL MODULE EMB 145 EMB145LR 3260212 SO CABIN FAULTY A C2XA K NONE N FALSE WARNING DE DESCENT 1 SW 27 22909 16171 16171 145459 FLT 7764 - LAX - FLIGHT CREW REPORTED ENG NR 2 FIRE DETECTION FAIL MSG ON EICAS FOR 15 SEC DURING DESCENT. MX PERSONNEL REMOVED NR 2 ENG FIRE LOOP ASSY AND CONTROL MODULE OPERATIONALLY CHECKED SATISFACTORY, AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008043000017 20080430 00017 NM 2008 4 30 ASAA0892841 1 20080323 A 5315 147A55068 FLOORBEAM BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 317AS 30856 CABIN FLOORBEAM CORRODED IN 2 EACH AREAS STA 986.5. REMOVED UPPER CHORD DAMAGED HORIZONTAL FLANGE, FABRICATED, LOCATED, DRILLED AND INSTALLED REPLACEMENT UPPER T-CHORD AND REPAIR ANGLES AND STRAPS IAW AREA 12566 AND ASA EA 5310 02782. 2 L 7 4 4F RT A16WE 2008043000024 20080430 00024 NM 2008 4 30 ASAA0872844 1 20080401 A 5311 148A111011 FRAME BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 609AS 29752 BS 1112 FRAME CRACKED AT UPPER END IN THE RADIUS. STUB TORSION BAY COMPARTMENT RT VERTICAL FRAME AT BS 1112 REPAIRED IA W B737 700 SRM 51 70 11 FIG 201. 2 L 7 2 4F RT A16WE 2008043000027 20080430 00027 NM 2008 4 30 ASAA0872845 1 20080406 A 5320 146A75022 CHANNEL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 609AS 29752 BS 727B TO BS 787 RBL 21 2 CHANNEL HAS CORROSION. REPLACED 2 CHANNEL WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008043000028 20080430 00028 NM 2008 4 30 ASAA0872846 1 20080406 A 5320 146A75058 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 609AS 29752 BS 747 + 767 RBL 21 INTERCOSTAL HAS CORROSION COMMON TO ANCHOR NUTS. REPLACED INTERCOSTAL WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008043000029 20080430 00029 NM 2008 4 30 ASAA0872847 1 20080403 A 5330 143A32524 SKIN BOEING 737 737790 13844CN NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 609AS 29752 PREVIOUS LIGHTNING STRIKE REPAIR AT RT FUSELAGE SKIN STA 500 + 16.5", 0.5" BELOW STR 20R REQUIRE HFEC OR DYE PENETRANT I NSPECTION PER SRM 53 00 01 REPAIR 13 PARA 6. MATERIAL LOSS FROM PREVIOUS LIGHTNING DAMAGE REMOVAL 0.020" ORIGINAL THICK NESS IS 0.080" PER B737 700 SRM 53 30 01 FIG 2. DAMAGE IS BEYOND ALLOWABLE LIMITS IAW B737 700 SRM 53 00 01 REPAIR MAT. MADE IAW B737 700 SRM 53 00 01. REPAIR PARTS INSTALLED IAW B737 700 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008043000037 20080430 00037 NM 2008 4 30 2008UALA02288 1 20080418 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 384 S15L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 UPPER LT FUSELAGE SKIN HAS DENT BS 384 1 INCH ABOVE STR 15L. MAJOR REPAIR ACCOMPLISHED, REMOVED THE DAMAGE. VERIFIED D AMAGE REMOVAL WITH HFEC. INSTALLED REPAIR DOUBLER, TRIPLER AND FILLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008043000039 20080430 00039 NM 2008 4 30 2008UALA02290 1 20080418 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 660-686 S12L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 MAIN CABIN INTERCOSTAL FWD OF DOOR 2L APPROX STR 12L BETWEEN STA 660 AND 686 IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REPL ACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008043000048 20080430 00048 NM 2008 4 30 CALA0800359 1 20080424 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 PASSENGER SERVICE UNIT (PSU) RAIL ATTACHMENT BRACKET TO FRAME CRACKED AT CABIN STATION 747 BETWEEN S8L AND S9L. CUT OUT DAMAGE AND INSTALLED REPAIR ANGLES IAW ECRA 5310-04498. 2 L 7 2 4F RT A16WE 2008043000050 20080430 00050 NM 2008 4 30 CALA0800361 1 20080404 A 5320 6516300 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 INSTALLED SRM REPAIR AT BS 178-188 LBL 24.67 FLOORBEAM WEB FOR ACCESS. REMOVED EXISTING WEB & STIFFENER, MODIFIED WEB & FABRICATED NEW STIFFENER & REPAIR PARTS FOR SRM REPAIR BS 178-188 LBL 24.67 FOR FLOORBEAM FOR ACCESS, IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2008043000060 20080430 00060 NM 2008 4 30 SWAA082200 1 20080424 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 22R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008043000062 20080430 00062 NM 2008 4 30 SWAA082237 1 20080424 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 10, WL 234. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008043000064 20080430 00064 NM 2008 4 30 SWAA082201 1 20080424 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008043000065 20080430 00065 NM 2008 4 30 SWAA082239 1 20080424 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 25R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008043000072 20080430 00072 NM 2008 4 30 SWAA082209 1 20080424 A 3350 3071BPEGPL LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008043000076 20080430 00076 NM 2008 4 30 SWAA082229 1 20080424 A 5322 6546569 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 947, STR 11L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008043000077 20080430 00077 NM 2008 4 30 SWAA082230 1 20080424 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 482B, LBL 9, WL 148. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008043000080 20080430 00080 NM 2008 4 30 SWAA082220 1 20080424 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000085 20080430 00085 NM 2008 4 30 SWAA082219 1 20080424 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000087 20080430 00087 NM 2008 4 30 SWAA082218 1 20080424 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000097 20080430 00097 NM 2008 4 30 SWAA082226 1 20080424 A 5330 66545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000098 20080430 00098 NM 2008 4 30 SWAA082228 1 20080424 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 775SW 30590 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008043000101 20080430 00101 NM 2008 4 30 CALA0800364 1 20080425 A 5320 65458078 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 INTERCOSTAL CRACKED AT STATION NUMBER 277 S14R. INSTALLED INTERCOSTAL PER REFERENCE SRM-51-40-02. 2 L 7 2 4F RT A16WE 2008043000104 20080430 00104 NM 2008 4 30 CALA0800367 1 20080425 A 2560 65C161215 ATTACH FITTING BOEING 737 737524 1384721 NM GIRT BAR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 L-1 DOOR FWD GIRT BAR ATTACH MOUNT AT CABIN FLOOR FOUND CORRODED. REMOVED DAMAGED GIRT BAR ATTACH MOUNT IAW B737 SRM 51 -40-02. LOCATED AND DRILLED SERVICEABLE ATTACH FITTING IAW B737 SRM 51-40-02. INSTALLED GIRT BAR FITTING ATTACH MOUNT IAW B737 SRM 51-40-02, L-1 DOOR FWD. 2 L 7 2 4F RT A16WE 2008043000111 20080430 00111 NM 2008 4 30 CALA0800374 1 20080408 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 CRACK IN FRAME AT STATION 360 ABOVE S8LT. REPAIRED CRACKED FRAME AT STATION 360 ABOVE S8LT IAW EA 5310-0 498 CAL EC/RA5 310-04752. 2 L 7 2 4F RT A16WE 2008043000124 20080430 00124 NM 2008 4 30 SWAA082273 1 20080423 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 5R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008043000129 20080430 00129 NM 2008 4 30 SWAA082298 1 20080427 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000130 20080430 00130 NM 2008 4 30 SWAA082297 1 20080427 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042400095 20080424 00095 2008 4 24 TRBA2008044 2 20080418 A 7200 ENGINE AEROSP ATR72 ATR72212 8680945 EU NR 2 MALFUNCTIONED A TRBA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 29 407AT 407 AFTER TAKEOFF LEVEL AT 6000 FT, NR 2 ENG INTERMITTENT OVERTORQUE. SHUT DOWN THE ENGINE AS PER AOM VOL 2. EMERGENCY WAS DECLARED AND RETURNED TO SLU. PERFORMED SEVERAL ENGINE RUNS (RT) AT ALL POWER SETTINGS AND NO TORQUE SURGE OR OVERTORQ UE NOTICED. ALSO VERIFIED RT ENGINE INTERCOMPRESSOR BLEED VALVE AND FOUND OK. ALSO PERFORMED ENGINE GROUND OPERATIONAL CHECK AS PER WORK CARD NR 055007-CS-20000-001 AND FOUND ALL PARAMETERS WITHIN LIMITS. MANUALS USED JIC NR 72-00-00 AND MM NR 72-00-03. FCF PASSED OK. 2 H 7 2 4T RT A53EU 2008042400113 20080424 00113 NM 2008 4 24 NWAA081726740 1 20080421 A 5412 BULKHEAD BOEING 747 747251F 1384898 NM NR 4 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 640US 23888 DURING "L" CHECK, FOUND CRACK IN NR 4 ENGINE PYLON AFT BULKHEAD RT FRAME WEB AT NAC STA 221.9. REPAIRED PER EA 67-21266 1. 2 L 7 4 4F RT A20WE 2008042400114 20080424 00114 EU 2008 4 24 F3LA200800194 1 20080420 A 5240 D5211155400140 BRACKET AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE R2 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED R2 DOOR SLIDE UPPER AFT MOUNT BRACKET HAD CORROSION. MAINTENANCE REMOVED AND REPL ACED R2 DOOR SLIDE UPPER AFT MOUNT BRACKET IN ACCORDANCE WITH SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPEC TED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042400116 20080424 00116 EU 2008 4 24 F3LA200800195 1 20080420 A 5340 D5211155400040 BRACKET AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE L2 DOOR SLIDE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED L2 DOOR SLIDE UPPER AFT MOUNT BRACKET HAD CORROSION. MAINTENANCE REMOVED AND REPL ACED L2 DOOR SLIDE UPPER AFT MOUNT BRACKET IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042400118 20080424 00118 EU 2008 4 24 F3LA200800196 1 20080421 A 3350 GE1810 LAMP AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE EMERGENCY LIGHTS BURNED OUT A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED LIGHT OUT IN AFT LEFT OVERWING EXIT. MAINTENANCE REMOVED AND REPLACED LAMP IN AFT LEFT EMERGENCY OVERWING LIGHT 63WL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-15-000-001 AND AMM 33-51-15-400-001 . UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042400119 20080424 00119 NM 2008 4 24 NWAA081735501 1 20080421 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 501US 23190 DURING OVERNIGHT MAINTENANCE, OPERATIONAL CHECK OF THE FLOOR TRACK EMERGENCY EXIT LIGHTS REVEALED THAT THE FIRST CLASS S ECTION INCLUDING THE FLOOR LEVEL EXIT LIGHTS AT DOORS 1 LEFT AND 1 RIGHT WERE INOPERATIVE. MAINTENANCE REMOVED AND REPL ACED THE BATTERY PACK AND OPERATION RETURNED TO NORMAL. 2 L 7 2 4F RT A2NM 2008042400122 20080424 00122 EU 2008 4 24 F3LA200800199 1 20080405 A 5321 D5367175302200 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE CABIN DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 261HG HAS DELAMINATION AROUND EDGES. MAINTENANCE REPAIRED FLOOR PANEL 261HG IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30226. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042300098 20080423 00098 NM 2008 4 23 USAA920080896 1 20080414 A 5230 6547956524A FRAME BOEING 737 73733A 1384673 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 23634 CLT-MAJOR REPAIR-C22- TWO INCH CRACK ON FWD SIDE OF AFT CARGO DOOR AT PULLEY MOUNTING BOLT. REPLACED DOOR IAW AMM 52-3 1-00-4. 2 L 7 2 4F RT A16WE 2008042300104 20080423 00104 NM 2008 4 23 UPS08M51986 1 20080319 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 256UP 48405 INSPECTION TYPE:2C RIGHT WING L/E NR 14 SLAT TRACK CUTOUT CRACKED LOWER O/B CORNER. CUT OUT DAMAGE, FABRICATED AND INST ALLED REPAIR DOUBLER & FILLER IAW MD-11 SRM 57-10-00 FIG 21. 2 L 7 3 4F RT A22WE 2008042300127 20080423 00127 NM 2008 4 23 USAA920080887 1 20080416 A 5313 STRINGER BOEING 737 7373B7 1384580 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 23379 CLT - MAJOR REPAIR-NR 4364480, CORROSION ON STR 26R AT BS 1007. INSTALLED NEW SECTION OF STRINGER IAW SRM 53-60-03. 2 L 7 2 4F RT A16WE 2008042300248 20080423 00248 NM 2008 4 23 SWAA081943 1 20080413 A 5315 6545834 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 13 TO RBL 31. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2008042300263 20080423 00263 WP 2008 4 23 UPS08852014 1 20080411 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 EMERGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-50-01-2 PARA 4. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2008042300272 20080423 00272 NM 2008 4 23 SWAA081969 1 20080413 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300283 20080423 00283 NM 2008 4 23 2008UALA02149 1 20080414 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 121UA 29167 CEILING EMERGENCY LIGHT INOP AT G1A GALLEY RT. REPLACED LIGHT. OP CHECK GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300284 20080423 00284 NM 2008 4 23 SWAA081979 1 20080413 A 5311 65C34355 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300290 20080423 00290 NM 2008 4 23 SWAA081985 1 20080413 A 5311 6546552 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300303 20080423 00303 NM 2008 4 23 SWAA081948 1 20080413 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300305 20080423 00305 NM 2008 4 23 SWAA081951 1 20080413 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND STRINGER 16L CRACKED AT BS 380. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008042300329 20080423 00329 NM 2008 4 23 SWAA081996 1 20080414 A 5523 BACB28AK04 BUSHING BOEING 737 7373H4 1384600 NM ELEVATOR TAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, LEFT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED NR 2 TAB BUSHING PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300357 20080423 00357 NM 2008 4 23 SWAA082013 1 20080415 A 3233 654610918 ACTUATOR BOEING 737 7373H4 1384600 NM LT MLG CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED MV2 CHECK, FOUND LEFT MLG ACTUATOR BEAM ARM FWD LUG CRACKED. REMOVED AND REPLACED ACTUATOR BEAM ARM PE R MM. 2 L 7 2 4F RT A16WE 2008042300360 20080423 00360 NM 2008 4 23 SWAA082022 1 20080415 A 5754 65C26601 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED 16Y CHECK, FOUND LEFT WING NR 1 L/E SLAT CRACKED AT LOWER OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008042300379 20080423 00379 NM 2008 4 23 SWAA082045 1 20080416 A 5312 6517853 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008042300380 20080423 00380 NM 2008 4 23 SWAA082032 1 20080416 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737E, 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042300390 20080423 00390 NM 2008 4 23 2008UALA02255 1 20080415 A 2560 HOOK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GIRT BAR MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 372UA 24637 1R SLIDE PACK DOESN'T LINE UP WITH GIRT BAR STOW HOOKS. FOUND MISMARKED. REINSTALLED HOOKS IN CORRECT LOCATION. AC OK FO R SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042400009 20080424 00009 EU 2008 4 24 F3LA200800203 1 20080406 A 5321 D5361067400000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE CABIN DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 222EF DELAMINATED AT EDGE. MAINTENANCE REPAIRED FLOOR PANEL 222EF IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30217 AND SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AN D FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042400030 20080424 00030 NM 2008 4 24 2008UALA02171 1 20080414 A 2421 IDG BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RIGHT FAULTED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 792UA 26934 ELEC GEN DRIVE R RIGHT IDG FAULT (LOW INTERNAL OIL PRESSURE). AFTER EXTENSIVE TROUBLE SHOOTING AND PART REPLACEMENT. FO UND IGD FAULTY SUSPECT FAULTY BEARING. BUG REPLACED SUSPECT FAULTY BEARING. BACK UP CONVERTER REPLACED SUSPECT INTERNAL FAULT. ALL OPS AND CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042400038 20080424 00038 WP 2008 4 24 UPS08852025 1 20080407 A 5347 36575031 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 FE,S FWD SEAT TRACK WORN. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-1-20D, 51-1-24, 51-3-0. 2 L 7 4 4F RT 4A25 2008042400048 20080424 00048 NM 2008 4 24 2008UALA02188 1 20080415 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 FWD CARGO DOOR CUTOUT AFT DOORWAY FRAME IS CRACKED ON THE AFT SIDE OF THE FRAME IN RADIUS ABOVE THE INBOARD UPPER CORNER OF LOWER STOP FITTING. MAJOR REPAIR: REMOVED DAMAGE. REINSTALLED NESTED ANGLES. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042400049 20080424 00049 NM 2008 4 24 2008UALA02189 1 20080415 A 3350 363674 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ROW 15, AFT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 338UA 24242 EEL LIGHTING IS INOP FROM ROW 15, AFT. REPLACED LIGHT OPS CHECKED OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042400059 20080424 00059 NM 2008 4 24 2008UALA02200 1 20080415 A 7500 773228915 CONTROLLER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 RIGHT ENGINE HIGH PRESSURE SHUTOFF VALVE (HPSOV) INOPERATIVE SECURED CLOSED. SUSPECT FAULTY HIGH PRESSURE CONTROLLER. REPLACED HIGH PRESSURE CONTROLLER IAW MM 36-11-08 PERFORMED BITE IAW MM 36-23-00 OK RUN ENGINE PER JRH 2-6-1 BLEED OPS CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042400060 20080424 00060 NM 2008 4 24 2008UALA02201 1 20080414 A 2841 0335KPU01 PROCESSING UNIT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUEL QTY IND FAULTED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 212UA 30218 FUEL QUANTITY PROCESSOR HAS AN INTERNAL FAULT, CMC MSG 28-20050, ACTIVE. FOUND CHANNEL-L INOP, REPLACED FUEL QUANTITY PROCESSOR UNIT PER MM28-41-01-401, OPS NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042400061 20080424 00061 NM 2008 4 24 2008UALA02202 1 20080415 A 7330 INDICATION SYS BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUEL FLOW MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 221UA 30552 222042 FUEL FLOW INDICATION (ENGINE), BLANK MSG01, ACTIVE DESCENT HARD; FUEL FLOW TRANSMITTER (R ENG) SIGNAL IS OUT OF RANGE. DB-ELECTRONIC ENGINE CONTROL (R ENG, CH A) MSG02- ACTIVE DESCENT HARD; FUEL FLOW TRANSMITTER (R ENG) SIGNAL IS OUT OF R ANGE, MSG-7360952 ACTIVE DC HARD MSG-7360952 ACTIVE DC HARD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008043000201 20080430 00201 NM 2008 4 30 SWAA082300 1 20080428 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 373, STR 26L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008042400087 20080424 00087 WP 2008 4 24 NWAA081659886 1 20080415 A 2730 ACTUATOR DOUG DC9 DC951 3022051 WP ELEVATORS MALFUNCTIONED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 600TR 47783 FLIGHT CREW REMARKED THAT THE AIRCRAFT WANTED TO ROTATE ON ITS OWN PRIOR TO V1 AND THAT A NOTICEABLE VIBRATION IN THE YO KE WAS FELT AFTER TAKEOFF. AIRCRAFT LEVELED AT 16000 FEET AND CREW ESTABLISHED COMMUNICATION WITH MAINTENANCE CONTROL. FLIGHT WAS DIRECTED TO DIVERT TO THE CLOSEST SUITABLE AIRPORT AND THEY LANDED AT ROC WITHOUT FURTHER INCIDENT. MAINTEN ANCE FOUND THE RIGHT ELEVATOR WAS LEVEL AND IN A NEUTRAL POSITION WHILE THE LEFT ELEVATOR WAS IN THE FULL UP POSITION. THE ELEVATOR POWER ACTUATION CYLINDER WAS REPLACED. 2 L 7 2 4F RT A6WE 2008042400128 20080424 00128 NM 2008 4 24 EIA2008015 1 20080318 A 3350 1317 BULB BOEING 747 747230B 1384889 NM EMERGENCY LIGHT ACTIVATED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490EV 23287 EMERGENCY LIGHT UPPER DECK ABOVE LADDER IS INOP. RELAMPED BULBS AND OPS CHECKED AS PER MM 33-51-00, PASSED SATISFACTORY . 2 L 7 4 4F RT A20WE 2008042400129 20080424 00129 NM 2008 4 24 EIA2008014 1 20080320 A 3310 900206 LIGHT BOEING 747 747212B 1384886 NM COCKPIT LOOSE A EIAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 09 482EV 20713 DURING DESCENT, ABOUT 30 MILES OUT, 2 VISIBLE PUFFS OF SMOKE WITH ASSOCIATED ELECTRICAL ODOR UNDER F/OS GLARESHIELD. HA PPENED 2 TIMES WITHIN A 3 MINUTE PERIOD. AIRCRAFT OPERATED 15 ADDITIONAL MINUTES UNTIL LANDING WITHOUT FURTHER OCCURREN CE. ALL SYSTEMS OPERATED NORMALLY, NO C/BS TRIPPED. MAINTENANCE REMOVED F/O INSTRUMENT PANEL AND INSPECTED ALL WIRING AND ALL COMPONENTS FOR LOOSE OR DAMAGED ITEMS. NO SMOKE OR FUMES NOTED. INSPECTED FLUORESCENT LIGHT AND SURROUNDING AR EA AND FOUND IT LOOSE AND SMOKE ODOR IN THAT AREA. THE LIGHT WAS DEFERRED AND ITS C/B PULLED AND COLLARED. 2 L 7 4 4F RT A20WE 2008042400138 20080424 00138 EU 2008 4 24 08FDEA01490 1 20080423 A 5420 PANEL AIRBUS 300 A300F4605R 3930327 EU NR 2 NACELLE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 NR 2 PYLON LEFT FWD LOWER FAIRING; PANEL 485BL IS CHAFED AT THE ATTACHMENT POINTS. REMOVED PANEL AND CHECKED THE LIMI TE. THE STIFFENER WAS OUT OF LIMITS. FABBED A NEW STIFFENER ON N/R N01141 & INSTALLED THE STIFFENER IAW SRM 51-40-21. INSTALLED THE PANEL IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008042400139 20080424 00139 EU 2008 4 24 08FDEA01491 1 20080423 A 5420 PANEL AIRBUS 300 A300F4605R 3930327 EU NR 2 NACELLE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 NR 2 PYLON; RIGHT FWD LOWER FAIRING; PANEL 486R IS CHAFED AT THE ATTACHMENT POINTS. REMOVED PANEL AND CHECKED LIMITS. ST IFFENER WAS OUT OF LIMITS. FABBED A NEW STIFFENER ON N/R N01140. INSTALLED STIFFENER IAW SRM 51-40-21; PG 7 AND REI NSTALLED PANEL IAW SRM 51-40-21; PG 7. 2 L 7 2 4F RT A35EU 2008042400140 20080424 00140 EU 2008 4 24 08FDEA01492 1 20080423 A 4910 SKIN AIRBUS 300 A300F4605R 3930327 EU APU DOOR BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 RIGHT APU DOOR SKIN IS BENT AND THE EDGE IS CRACKED AT THE CENTER LINE OF THE A/C WITH THE DOOR CLOSED. REMOVED BENT & CRACKED EDGE DAMAGE IAW SRM 51-27-00. FOUND EDGE DISTANCE TO FASTENERS TO BE 2-D & WITHIN LIMITS IAW SRM 51-40-50. PRIME D AREA IAW A300-600 SRM 51-21-10. PAINTED AREA IAW SRM 51-21-10. 2 L 7 2 4F RT A35EU 2008042400141 20080424 00141 NM 2008 4 24 08FDEA01493 1 20080423 A 5340 69144732 STRINGER CLIP BOEING 727 727232 1384082 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 STRINGER TIE ON STR 26R AT FS 941A HAS CORROSION ON OUTER SIDE OF TIE. REMOVED DAMAGED STRINGER TIE REPLACED NEW STRING ER TIE, REF SRM 51-30-2 PG1. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008042400143 20080424 00143 NM 2008 4 24 08FDEA01495 1 20080423 A 5330 65207799 SKIN BOEING 727 727232 1384082 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 MLG WW KEEL BEAM LWR EXT SKIN PANEL AT BS 940 TO 950-12, LBL 5-RBL 5 2 EA CRACKED FASTENER HOLES BS 947, RBL 5 (MKD). R EMOVED DAMAGE AND FABRICATED A REPAIR FILLER AND A REPAIR DOUBLER. TREATED, PRIMED AND PAINTED ALL REPAIR PARTS AND INS TALLED. EDGE SEALED REPAIR DOUBLER. REFERENCE SRM 51-40-2/FIGURE NR 1 AND BOEING DOCUMENT NR 65-18636/ITEM NR 280. CL ASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008042400146 20080424 00146 EU 2008 4 24 08FDEA01498 1 20080423 A 5320 A2557562100400 PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 100 PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 BULK CARGO PANEL 161 BW IS PUNCTURED IN 2 PLACES. REPAIRED BY REMOVING THE DAMAGE. APPLYING A WET LAY UP, CURING THE W ET LAY UP AND PAINTING THE REPAIRED SURFACE. 2 L 7 2 4F RT A35EU 2008042400148 20080424 00148 EU 2008 4 24 08FDEA01500 1 20080423 A 5280 A5283062500000 DOOR AIRBUS 300 A300F4605R 3930327 EU LT NLG DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 NLG LEFT MAIN DOOR IS GOUGED ON THE EDGE. REPAIRED LEFT NOSE; LEFT MAIN GEAR DOOR BY REMOVING DAMAGED AREA & BONDING C ARBON WET LAY UP REPAIR IAW A300-600 SRM 52-82-11 & 51-77-10 PARA 3.0; FIG 209. REMOVED FINISH AT SECOND DAMAGE LOC ATION AFTER FURTHER EVALUATION FOUND NO FIBER DAMAGE OR DEFECTS. 2 L 7 2 4F RT A35EU 2008042400156 20080424 00156 EU 2008 4 24 08FDEA01508 1 20080423 A 5753 A5796000001551 RUB STRIP AIRBUS 300 A300F4605R 3930327 EU TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 RIGHT WING FLAP UPPER SKIN RUB STRIP IS DELAMINATED AT 3 SPOTS. REMOVED & REPLACED THE CHAFE / RUB STRIP IAW SRM 57-50- 00; PARA 3-G FIG 207. 2 L 7 2 4F RT A35EU 2008042400157 20080424 00157 EU 2008 4 24 08FDEA01509 1 20080423 A 5753 A5796000001551 RUB STRIP AIRBUS 300 A300F4605R 3930327 EU TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 LEFT WING INBD FLAP UPPER SURFACE CHAFING PLATE IS PEELING AND WORN. REMOVED &B REPLACED THE CHAFE STRIPS IAW SRM 57-50 -00; PARA 3-G; FIG 207. 2 L 7 2 4F RT A35EU 2008042400158 20080424 00158 EU 2008 4 24 08FDEA01510 1 20080423 A 5350 A215104200001 PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 A/C FAIRING LEFT PANEL 143 FL IS DAMAGED FROM FRETTING. REMOVED DAMAGE; PREPPED THE AREA FOR REPAIR; APPLIED LAY-UP RE PAIR & REFINISHED THE SURFACE IAW A300-600 SRM 51-77-12 & SRM 53-15-73. 2 L 7 2 4F RT A35EU 2008042400159 20080424 00159 EU 2008 4 24 08FDEA01511 1 20080423 A 5753 FAIRING AIRBUS 300 A300F4605R 3930327 EU TE FLAP PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 LEFT WING FLAP FAIRING 533BB FWD SECTION IS PUNCTURED INTERNALLY. REMOVED DAMAGE FROM PANEL; FABRICATED REPLACEMENT CO RE PLUG; POTTED CORE & STARTED CURE; COMPLETED CURE & SANDED; LAYED UP REPAIR PLYS UNDER VAC BAG & STARTED CURE; COMPLETED CURE & LIGHTLY SANDED. 2 L 7 2 4F RT A35EU 2008042400161 20080424 00161 EU 2008 4 24 08FDEA01513 1 20080423 A 5753 A5796564000251 FAIRING AIRBUS 300 A300F4605R 3930327 EU TE FLAP PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 LEFT WING FLAP FAIRING 535 BB IS PUNCTURED ON THE FWD LOWER SECTION. REMOVED DAMAGE & APPLIED A WET LAY-UP IAW SRM 57-2 0-35. 2 L 7 2 4F RT A35EU 2008042400177 20080424 00177 EA 2008 4 24 SWIA200819498 1 20080418 A 3520 OXYGEN MASK CNDAIR CL600 CL6002C10 1390015 EA CABIN UNWANTED DEPLOY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 730SK 10193 FLT 5825 - OXYGEN MASKS IN ROW 3C AND 3D INADVERTENTLY DROPPED. INSPECTED AND RESTOWED MASKS AS REQUIRED. NO DISCREPAN CIES NOTED. 2 L 7 2 4F RT A21EA 2008042400181 20080424 00181 SO 2008 4 24 SWIA200819502 1 20080415 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 308SW 120326 FLT 5590 - ROW 1 EMERGENCY LIGHT IS INOP. REPAIRED WIRING AT EMERGENCY LIGHT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008042400182 20080424 00182 EA 2008 4 24 SWIA200819503 1 20080417 A 3297 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA MLG FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 927SW 7693 FLT 6495 - RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN MESSAGES. REPLACED RIGHT GEAR INBOARD ELECTRICAL HARNESS PER AMM 3 2-61-20. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008042400183 20080424 00183 EA 2008 4 24 SWIA200819504 1 20080418 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA RIGHT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 927SW 14437 14437 7693 FLT 5991 - SMELLED SMOKE IN CABIN. REPLACED RIGHT PACK IAW 21-51-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008042400184 20080424 00184 EA 2008 4 24 SWIA200819505 1 20080418 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA LEFT SMOKE A SWIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 929SW 13223 13223 7703 FLT 6416 - REPORTED SMOKE IN THE CABIN. REPLACED LEFT AIR CYCLE MACHINE IAW CRJ 200 MM 21-51-10. 2 L 7 2 4F RT A21EA 2008042400191 20080424 00191 EA 2008 4 24 SWIA200819512 1 20080104 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 755SK 10220 FS 280 BEAM CRACKED AT RBL 9.0, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ7/9 SRM 51-42-21 PG 9-11. 2 L 7 2 4F RT A21EA 2008042400193 20080424 00193 NM 2008 4 24 08FDEA01482 1 20080423 A 5340 6522531501 FITTING BOEING 727 727232 1384082 NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 MAIN DECK 1R DR BOTTOM CROSS BEAM AFT STOP FITTING IS CRACKED REMOVED AND REPLACED STOP FITTING REF SRM 51-30-2. DOOR A DJUSTEMENT ACCOMPLISED ON W/0 40304 N00067, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008042400198 20080424 00198 EU 2008 4 24 08FDEA01518 1 20080423 A 5753 A57965660000 FAIRING AIRBUS 300 A300F4605R 3930327 EU TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 LEFT WING FLAP FAIRING 535 AT IS DENTED. REPAIR BY REMOVING THE DAMAGE & APPLYING A CORE; CLOSING PLIES AND A FIBERGLAS S OVERLAY REPAIR IAW SRM 57-20-35. APPLIED AN ANTI-STATIC COATING IAW SRM 51-23-20. APPLIED PORE FILLER & PRIMER IAW SR M 51-75-10. PREPPED & PAINTED AREA IAW AMM 51-23-10-0. 2 L 7 2 4F RT A35EU 2008042500007 20080425 00007 2008 4 25 AMTA200800241 4 20080323 A 2310 9460452012 TRANSCEIVER BOEING 737 73783N 13844HI NM CFMINT CFM56 CFM567B27 13046 NE LT HF SYSTEM UNSERVICEABLE A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 305TZ 30706 ON HFI, NO LIGHT, NO CHIME ON SELCAL CONTROL PANEL SIGNAL WEAK. REMOVED AND REPLACED NR 1 HF TRANSCEIVER IAW AMM 23-11- 21-4. CALLED SFO RADIO AND RECEIVED SELCAL FROM THE M. GOT LIGHT AND CHIME. (K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2008042500008 20080425 00008 NM 2008 4 25 AMTA200800097 1 20080213 A 5330 SKIN BOEING 757 75733N 1384931 NM RROYCE RB211 RB211535E4 54555 NE BS 780 DAMAGED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 561TZ 33526 SUBMIT TO MFG, THE REPAIR PERFORMED IN EAR 757-53R-6056 FOR EVALUATION AND POSSIBLE RECATAGORIZATION TO CATEGORY B INTER M REPAIRS OR TO PROVIDE REPLACEMENT REPAIR INSTRUCTIONS. ACCOMPLISHED CATEGORY B REPAIR IAW EA 757-5300-09-A1277. INST ALLED TRIPLER REPAIR TO FUSELAGE LIGHTENING STRIKE NEW REPAIR CLASSIFIED AS CATEGORY B REPAIR WITH REPEAT INSPECTION INT ERVAL EVERY 12,000 FLIGHT CYCLES. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 2008042500014 20080425 00014 NM 2008 4 25 BJNA080202 1 20080210 A 3350 BPS73 POWER SUPPLY BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 42XA 25729 EMERGENCY LIGHT AT ROW 21 WILL NOT TEST. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2008042500020 20080425 00020 EU 2008 4 25 COEA0802908 1 20080403 A 3097 ASNE0261 WIRE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE WINDSHIELD HEAT SHORTED A COEA D RETURN TO BLOCK A FLAME/FIRE TX TAXI/GRND HDL 1 NM 13 908FX 023 RETURN TO BLOCKS. AS THE ACFT WAS TAXIING INTO THE DEICE AREA THE PILOT NOTICED A FLASH OF LIGHT FOLLOWED BY SPARKS FAL LING NEAR THE COPILOTS FEET. ELECTRICAL POWER AND THE MAINT INDICATOR ON THE MAINT PANEL WAS POPPED. WIRE HARNESS WIRE S SHORTED TO EACH OTHER AND TO THE BACK SHELL, WHERE THE HARNESS CONNECTS TO THE BACK SHELL ON THE CONNECTOR TO THE LT W INDSHIELD HEAT TEMP CONTROLLER. CUT ALL WIRES BACK IN HARNESS PAST DAMAGED AREA, REPAIRED THE WIRES AND REPLACED THE CO NNECTOR TO THE LT WINDSHIELD HEAT TEMPERATURE CONTROLLER. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008042500022 20080425 00022 EU 2008 4 25 COEA0801821 1 20080327 A 3097 7654841 WIRE AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW127 NE NR2 PROP DEICE BROKEN A COEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 13 821FX 253 RETURN TO BLOCKS. FLIGHT NR 8906. THE CREW RECEIVED A PROP ANTI-ICE FAULT ON THE NR 2 ENGINE DURING TAXI OUT FOR DEPAR TURE. DUE TO WEATHER CONDITIONS THE CREW ELECTED TO RETURN TO THE RAMP FOR MAINT. REPLACED THE DEICE WIRE LEAD TO THE NR 2 PROPELLER BLADE. FROM THE SLIP RING TERMINAL TO THE BLADE HEATER LEAD TERMINAL BLOCK, ON THE RT PROP. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008042500028 20080425 00028 CE 2008 4 25 U5QA06011 1 20080416 A 2434 66085122 GENERATOR LEAR 60 60LEAR 5170707 CE FAILED E U5QA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 CE 05 8811A 912 119 PILOT REPORTED VIBRATION FOLLOWED BY GENERATOR LOAD DROPPING TO 0 AND GENERATOR FAIL LIGHT COMING ON. VIBRATION CONTINU ED AND WAS INCREASING IN INTENSITY. MADE A PRECAUTIONARY LANDING. 2 L 7 2 4F RT A10CE 2008042500029 20080425 00029 NM 2008 4 25 HNAA0800131 1 20080406 A 3320 BR9120WW LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 814EX 318 OVERHEAD LIGHT AT SEAT 7AC INOP WITH ELECTRICAL HOT SMELL IN CABIN. CABIN INTERIOR NORMAL SYSTEM INSPECTED AND FOUND 7A C BULB INOP. REMOVED BULB AND INSPECTED BULB CONTACTS, NO DEFECTS NOTED. REINSTALLED INOP BULB. 2 H 7 2 4T RT A13NM 2008042500031 20080425 00031 EA 2008 4 25 HNAA0800130 1 20080404 A 3350 82520974101 LIGHT DHAV DHC8 DHC8311 1386006 EA CABIN UNSECURE A HNAA O OTHER O OTHER UK UNKNOWN 1 EA 07 326EN 234 CABIN AFT FLOOR EMERGENCY LIGHTS NOT SECURE. RESECURED LIGHTS AS REQUIRED. 2 H 7 2 4T RT A13NM 2008042500034 20080425 00034 EA 2008 4 25 TRAX200800530 1 20080410 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 AAR - AFT REPAIR ANGLE AT FS 280 LBL 9 CRACKED. REMOVED DINOTROL AND CLEANED SUSPECTED DAMAGE AREA. AFTER FURTHER INVE STIGATION FOUND AFT REPAIR ANGLE AT FS 280.00 LBL 9.00 TO BE A MARK NOT CRACKED. C/W HFEC INSP OF ANGLE. NO DEFECTS NO TED IAW CRJ 200 NDTM 51-20-06. NO FURTHER ACTION REQUIRED. SUPPLEMENTAL SDR CLOSED 4/17/08. 2 L 7 2 4F RT A21EA 2008042500035 20080425 00035 EA 2008 4 25 TRAX200800531 1 20080410 A 5320 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 AAR - CLIP CRACKED AT FS 280 O/B OF RBL 9. REMOVED DAMAGED CLIP AT FS 280.00 O/B OF RBL 9.00. INSTALLATION OF SERVICEA BLE ATTACH CLIP. ALL WORK DONE IAW CRJ 200 SRM 51-42-21. SUPPLEMENTAL SDR CLOSED 4/17/08. 2 L 7 2 4F RT A21EA 2008042500039 20080425 00039 SO 2008 4 25 FDKA200804158 1 20080411 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 14896 145568 FDM FLT 6069 MCO-MIA (0558 PHX LCL). FWD FLOOR EMERGENCY PROX LIGHTS OUT. MX REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008042300319 20080423 00319 2008 4 23 SWAA081958 4 20080412 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 747SA 29799 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042300321 20080423 00321 NM 2008 4 23 SWAA081960 1 20080411 A 3350 100031 SIGN BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 782SA 29808 FWD CABIN EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED SIGN PER MM. 2 L 7 2 4F RT A16WE 2008042300332 20080423 00332 NM 2008 4 23 2008UALA02254 1 20080414 A 3510 HARNESS BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE OXYGEN MASK LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. FOUND FIRST OBSERVERS O2 MASK INFLATABLE HARNESS HAS HOLE AND WON`T INFLATE.SERVICED SYSTEM. AND REPLACED MASK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042300362 20080423 00362 NM 2008 4 23 SWAA082028 1 20080415 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300400 20080423 00400 NM 2008 4 23 SWAA082063 1 20080417 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2008042400008 20080424 00008 EU 2008 4 24 08FDEA01476 1 20080422 A 5320 A5398111320051 SHEAR PLATE AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 SHEAR PLATE IS CRACKED AT FRAME 79 BETWEEN STRINGER 16L AND 17L. REMOVED AND REPLACED THE SHEAR PLATE IAW A300 SRM 51-4 0-21. 2 L 7 2 4F RT A35EU 2008042400017 20080424 00017 NM 2008 4 24 2008UALA02156 1 20080412 A 3150 WARNING MESSAGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 543UA 25698 EICAS MESSAGE 'R ENG PRI CONT' DISPLAYED. REPLACED THE NR 2 ENGINE PERFORMED ALL REQUIRED TESTS AND RUNS, PERFORMED A SATISFACTORY VERIFICATION FLIGHT. NO REPEATS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400018 20080424 00018 2008 4 24 2008UALA02157 4 20080413 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR INOPERATIVE A UALA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 WP 29 581UA 26701 DOOR 1L ARMED LIGHT DOES NOT COME ON. REPLACED DOOR 1L SLIDE LIGHT ASS'Y. OPS CK NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400021 20080424 00021 NM 2008 4 24 2008UALA02161 1 20080411 A 5551 CLEVIS BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 RT HORIZONTAL STABILIZER CENTER SECTION FWD SPAR UPPER CLEVIS FWD AND AFT LUG HAVE EVIDENCE OF CORROSION. SPOTFACE FWD AND AFT FACES ON BOTH LUGS TO REMOVED CORROSION WITH FINAL DIMENSION OF .596 INCH ON THE FWD AND .577 INCH ON THE AFT LU G. REAMED THE BORES TO FINAL DIMENSION OF 1.1395 INCH ON THE FWD AND 1.1398 INCH ON THE AFT LUG. ALL WITHIN LIMITS. R EPAIRS ACP'D REF SRM 55-10-10. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042400026 20080424 00026 NM 2008 4 24 2008UALA02166 1 20080414 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1540 S25-27L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 AFT PIT STA 1540, BETWEEN STR 25L AND 27L FRAME DENTED (3 EA DENTS). AFT PIT STA 1540, BETWEEN STR 25L AND 27 L FRAME D ENTED (3 EA DENTS) REPAIRED FRAME DENTS IAW S RM 53-00-07 RPR 5 TABLE II ZONE 1.THIS REPAIR MUST BE REINSPECT ED STARTIN G AT 50000 TOTAL FLIGHT CYCLES AND 12000FC THERE AFTER. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400051 20080424 00051 NM 2008 4 24 2008UALA02191 1 20080416 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE G5 GALLEY WALL INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EEL LIGHT INOP AT G5 GALLEY WALL. FOUND LIGHT ASSEMBLY INOP. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD IAW MM33-51-12 PB2 00 CONFIGURE 2 PARAGRAPH 2. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042400053 20080424 00053 NM 2008 4 24 2008UALA02193 1 20080415 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 566UA 26670 EMERGENCY EXIT LIGHT STRIP MISSING AT 34C. FOUND MISSING STRIP AND RESECURED IT. OPS TESTED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400063 20080424 00063 NM 2008 4 24 F3LA200800181 1 20080415 A 5321 D5361060500100 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 45 1841 DURING C4 S1 C CHECK INSPECTION REPORTED CORROSION ON MAIN CABIN R1 DOOR ENTRY FLOOR PANEL LOWER SURFACE AND AT VARIOUS FASTENER HOLES. MAINTENANCE REMOVED AND REPLACED R1 DOOR ENTRY PANEL 222FF. INSTALLATION WILL BE ACCOMPLISHED ON WORK CARD CP753-12. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042400082 20080424 00082 2008 4 24 2008UALA02274 4 20080417 A 2565 5A29011 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SLIDE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 SLIDE HAS A DAMAGED ASPIRATOR. BARREL IS BENT FROM EXTERNAL PRESSURE OR CONTACT. NO VISIBLE DAMAGE TO SLIDE MATERIAL. RE PLACED ASPIRATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042400088 20080424 00088 EU 2008 4 24 F3LA200800172 1 20080406 A 5320 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AROUND NUT PLATES AFT CARGO PIT FLOOR PROFILE BETWEEN C55 AND C56. MAIN TENANCE CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-35-0 0 AND SRM 51-42-11 PAGE 7. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042400099 20080424 00099 NM 2008 4 24 DLM90080601 1 20080406 A 5740 3913194511 FITTING DOUG MD90 MD9030 3023690 NM LEFT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 LEFT WING GROUND SPOILER PANEL O/B HINGE MOUNT FITTNG IS CRACKED. REMOVED AND REPLACED FITTING, IAW MD90 SRM 51-30-02. 2 L 7 2 4F RT A6WE 2008042400123 20080424 00123 EU 2008 4 24 F3LA200800201 1 20080406 A 5315 D53476572000 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED AFT CARGO PIT CENTER FLOORBEAM BETWEEN C58 AND C59 NUT PLATES HAVE SIGNS OF CORROS ION. MAINTENANCE REMOVED OLD FLOORBEAM AND REPAIR ANGLES, FABRICATED NEW FLOORBEAM AND REPAIR ANGLES IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30229 AND INSTALLED NEW PARTS IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042400126 20080424 00126 NM 2008 4 24 P5CA0801557 1 20080417 A 5350 FAIRING BOEING 747 74746NF 13848BT NM WING TO BODY DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 450PA 30808 LT WING TO BODY FAIRING PANEL 191KL SKIN DENTED EO NR 4453A160 ISSUED AND REQUIRES RE-INSPECTION EVERY 25 FLIGHT CYCLES. 2 L 7 4 4F RT A20WE 2008042400149 20080424 00149 EU 2008 4 24 08FDEA01501 1 20080423 A 5753 A5796569000100 FAIRING AIRBUS 300 A300F4605R 3930327 EU TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 RIGHT WING FLAP FAIRING 636 AB LEFT SIDE UPPER POINT IS DELAMINATED. REMOVED FINISH AND DAMAGE IAW SRM 57-20-35. LAYE D UP & CURED REPAIR PLYS IAW SRM 57-20-35 PAPAGRAPHS 5; G-M. APPLIED FINISH IAW SRM 51-75-10. 2 L 7 2 4F RT A35EU 2008042400160 20080424 00160 EU 2008 4 24 08FDEA01512 1 20080423 A 5753 A5794255760261 FAIRING AIRBUS 300 A300F4605R 3930327 EU TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 LEFT WING FLAP FAIRING 534 BB IS DENTED ON THE LOWER FWD SECTION. REMOVED DAMAGE AND APPLIED A WET LAY-UP IAW SRM 57-20 -35 & RESTORED FINISH IAW SRM 57-75-10 & AMM 51-23-10-0. 2 L 7 2 4F RT A35EU 2008042400170 20080424 00170 NM 2008 4 24 08FDEA01481 1 20080423 A 5330 6554573 SKIN BOEING 727 727232 1384082 NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 EXT FUSELAGE SKIN IS GOUGED AT BS 670 O/B OF STR S-28L REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER REPAIR REF SRM-30-3 FIG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR AND A CATEGORY "B" REPAIR. 2 L 7 3 4F A3WE 2008042400174 20080424 00174 SO 2008 4 24 SWIA200819495 1 20080416 A 2611 BATTERY EMB 120 EMB120ER 3260203 SO SMOKE DETECTOR DISCHARGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 295SW 120322 FLT 5718 - SMOKE DETECTOR IS INOP. REPLACED BATTERY IN SMOKE DETECTOR. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008042400189 20080424 00189 EA 2008 4 24 SWIA200819510 1 20080121 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 758SK 10222 FS 280 BEAM CRACKED AT RBL 11, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ7/9 SRM 51-42-06/REO670-53-11-265. 2 L 7 2 4F RT A21EA 2008042500024 20080425 00024 EU 2008 4 25 COEA0802914 1 20080324 A 5315 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE FUSELAGE CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 914FX 293 FOUND DURING HEAVY CHECK. MAJOR REPAIR. EO 5315-01: THE RT OB LONGITUDINAL FLOOR BEAM IS CRACKED IN (4) PLACES. AT FR AME 21 AND 24 ALSO FWD AND AFT OF FRAME 30. THE LT OB LONGITUDINAL FLOORBEAM IS CRACKED IN (2) PLACES. AT FRAME 28 AND FRAME 34. REMOVED AND REPLACED DAMAGED SECTIONS OF THE FLOORBEAM BY ADDING SPLICES IAW EO 5315-01. REMOVED SECTIONS R T BEAM FROM FRAME 21 TO 22, 24 TO 25 AND 29 TO 31. REMOVED SECTIONS OF THE LT BEAM FROM FRAMES 25 TO 28 AND 34 TO 36. RT BEAM PN WASBV-03, LT BEAM PN WASB-01. WO: 200042-44,46,50. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008042500030 20080425 00030 NM 2008 4 25 HNAA0800132 1 20080406 A 3320 BV033021148 HOLDER DHAV DHC8 DHC8102 2809003 NM CABIN DEFECTIVE A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 814EX 318 STRONG ELECTRICAL BURNING ODOR AT MID CABIN AREA. INSPECTED FOR HIDDEN DAMAGE, NONE FOUND. DEACTIVATED IAW SPECIAL PRO CEDURE 33.1, REFERENCE LOG PAGE 261100-1. 2 H 7 2 4T RT A13NM 2008042500052 20080425 00052 2008 4 25 N382008F00000 2 20080317 A 7250 BEARING GULSTM G1159 G1159 3953505 SO TURBINE FAILED E N38A O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 EA 05 192FG 192 AT START UP OF THE RT ENGINE, THE PILOT NOTICED A VIBRATION AND THE ENGINE WAS SHUT DOWN, TROUBLESHOT PROBLEM. IT WAS D ETERMINED THAT A HIGH PRESSURE TURBINE BEARING HAD FAILED. (K) 2 L 7 2 4F RT A12EA 2008042500056 20080425 00056 EU 2008 4 25 109RX042008 1 20080407 A 5302 1090371231 LONGERON AGUSTA A109 A109K2 0260502 EU TMECA ARRIEL ARRIEL1K1 60030 NE TAIL BOOM CRACKED E I7LA K NONE O OTHER IN INSP/MAINT 1 NM 07 109RX 2161 2161 10016 DURING A 3,000-HOUR INSPECTION THE UPPER LT TAILBOOM ATTACH FITTING WAS FOUND TO HAVE A 2-INCH CRACK. THIS EXACT LONGERO N/ATTACH FITTING WAS REPLACED JUNE 2004 AT AIRCRAFT TOTAL TIME 5626.7 THE ORIGINAL REPAIR WAS COMPLETED AND APPROVED ON FAA FORM 337 DATED JUNE 17,2004 - DWG 109-0951-60. 1 G 7 2 3U 3 U RT H7EU E19EU 2008042500060 20080425 00060 2008 4 25 HNAA0800133 4 20080416 A 3497 M3902957354 PIN DHAV DHC8 DHC8311 1386006 EA CONNECTOR DEFECTIVE A HNAA D RETURN TO BLOCK O OTHER CL CLIMB 1 EA 07 335EN 375 NUMBER 2 VOR FLASHES BACK AND FORTH BETWEEN VOR AND ILS WHEN A VOR FREQUENCY IS SELECTED. DUPLICATED FAULT ON GROUND BY MOVING WIRE BUNDLE APPROXIMATELY 6 INCHES BEHIND NR 2 SYMBOL GENERATOR. REPLACED PIN 53 OF 3428-P65-2-1B TO CORRECT FA ULT. OPERATIONAL CHECK GOOD USING 402AP TEST SET. 2 H 7 2 4T RT A13NM 2008042500061 20080425 00061 WP 2008 4 25 ABXA080123 1 20080415 A 3397 WIRE DOUG DC9 DC933F 302207A WP COCKPIT BROKEN A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 23 933AX 47291 AFTER LANDING AT ILN, FIRST OFFICER'S MAP LIGHT SPARKED AND SMOKED WHEN TURNED ON. TURNED OFF LIGHT, SMOKE AND SPARKS S TOPPED. REPAIRED BROKEN WIRE FROM FIRST OFFICER'S MAP LIGHT. OPS CHECK GOOD IAW DC9 AMM 33-00-00. 2 L 7 2 4F A6WE 2008042500065 20080425 00065 SO 2008 4 25 RAIA00804014 1 20080413 A 3610 8166248 VALVE EMB 145 EMB145LR 3260212 SO BLEED AIR SYS MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 813HK 145044 FLT 5497 - STL - BLEED NR 1 OVERTEMP MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 1 BLEED FAN AIR VALV E. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008042500066 20080425 00066 SO 2008 4 25 RAIA00804016 1 20080414 A 7830 THRUST REVERSER EMB 145 EMB145LR 3260212 SO NR 1 ENGINE MALFUNCTIONED A RAIA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 812HK 145373 FLT 5576 - RDU -CREW REPORTED NR 1 THRUST REVERSER FAIL MESSAGE IN FLIGHT. CREW PERFORMED AN INFLIGHT SHUT DOWN OF THE NR 1 ENGINE. MAINTENANCE DEFERRED THE THRUST REVERSER SYSTEM IAW MEL PROCEDURES. 2 L 7 2 4T RT T00011AT 2008042500072 20080425 00072 NM 2008 4 25 SWAA082056 1 20080417 A 5610 571623121 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 649SW 27719 CREW REPORTED FLIGHT DECK L2 WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 2008042500073 20080425 00073 2008 4 25 SWAA082057 4 20080417 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042500074 20080425 00074 NM 2008 4 25 SWAA082058 1 20080417 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 940 AND BS 980, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008042500075 20080425 00075 EA 2008 4 25 TRAX200800537 1 20080414 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 SERVICE DOOR HARD TO OPEN FROM OUTSIDE. 2 L 7 2 4F RT A21EA 2008042500076 20080425 00076 EA 2008 4 25 TRAX200800538 1 20080414 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 F/A UNABLE TO CLOSE PAX DOOR HANDLE, CAN ONLY BE CLOSE FROM OUTSIDE. 2 L 7 2 4F RT A21EA 2008042500077 20080425 00077 EA 2008 4 25 TRAX200800539 1 20080415 A 5210 LOCK CNDAIR CL600 CL6002B19 1900309 EA ASD BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 908EV 7654 ASD EXTREMELY HARD TO UNLOCK WHEN DOOR IS CLOSED AND LOCKED FOR LONGER THAN 10 SECONDS BUT IF UNLOCKED IMMEDIATELY AFTE R CLOSING THE DOOR UNLOCKS FINE. FLT 4892 DEL 31 MINS. 2 L 7 2 4F RT A21EA 2008042500078 20080425 00078 EA 2008 4 25 TRAX200800540 1 20080415 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 748EV 10158 RIGHT AFT EXTERIOR EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008042500083 20080425 00083 EA 2008 4 25 TRAX200800549 1 20080416 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 FS 280 INBOARD BRACKET CRACKED AT LBL 9.0 (MARKED). 2 L 7 2 4F RT A21EA 2008042500086 20080425 00086 EA 2008 4 25 TRAX200800553 1 20080416 A 5242 HANDLE CNDAIR CL600 CL6002C10 1390015 EA E&E DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 379CA 10102 AVIONIC DOOR HANDLE CRACKED. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE A CTION. 2 L 7 2 4F RT A21EA 2008042500090 20080425 00090 EU 2008 4 25 TRAX200800558 1 20080417 A 5240 DOOR AEROSP ATR72 ATR72 EU SERVICE DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 637AS 383 SERVICE DOOR WILL NOT CLOSE. FLT 4344 DEL 60 MINS. 2 H 7 2 4T RT 2008042500091 20080425 00091 EA 2008 4 25 TRAX200800559 1 20080417 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 MAIN DOOR DIFFICULT TO OPEN. FLT 4653 DEL 20 MINS. 2 L 7 2 4F RT A21EA 2008042500092 20080425 00092 NM 2008 4 25 NOCA02108 1 20080417 A 2612 FIRE DETECTOR BOEING 757 75728A 1384976 NM LT ENGINE DIRTY A NOCA K NONE N FALSE WARNING UK UNKNOWN 1 EA 15 754NA 29381 LEFT ENG FIRE LP 2 STATUS MSG. CLEANED NR 3 DETECTOR PLUG AND SECURED LOOSE DETECTOR PLUG NR 2, OPS CHECKS NORMAL PER M M 26-11-00. 2 L 7 2 4F RT A2NM 2008042500095 20080425 00095 GL 2008 4 25 CHQA200800073 2 20080409 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 2 LEAKING A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 291SK 15514 6303 145486 CAE312631 FLIGHT 5940. CREW RETURNED TO FIELD FOR A LAV SMOKE INDICATION ON EICAS. MAINT FOUND THE LAVATORY SMOKE DETECTOR FULL OF DUST. AFTER CLEANING THE SMOKE DETECTOR THE SYS WAS OPS CHECKED GOOD. LATER THAT DAY THE MESSAGE RETURNED WHILE ON APPROACH AND CLEARED WITHIN 40 SECONDS. THE CREW PERFORMED A NORMAL APPROACH AND LANDING. MAINT ISOLATED THE FAULT TO E2 WHILE AT HIGH POWER. THE AC WAS THEN FERRIED TO CMH WHERE E2 WAS REPLACED. AFTER REPLACING E2 THERE WERE NO FURTHER FAULTS NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008042500097 20080425 00097 NM 2008 4 25 NOCA02308 1 20080418 A 3350 767 LIGHT BOEING 767 76739H 1385311 NM EXTERIOR INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 760NA 26257 DOOR R-4 EXTERIOR SLIDE EMERGENCY FLOOD LIGHT INOP. RELAMPED DOOR R-4 EXTERIOR SLIDE EMERGENCY FLOOD LIGHT AND OPS CHEC KS NORMAL AS PER THE AMM 33-51-06. 2 L 7 2 4F RT A1NM 2008042500105 20080425 00105 EA 2008 4 25 COMA0870016 1 20080415 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 658CA 10148 FLIGHT 5571 - CEILING EMERGENCY FLOODLIGHT INOP AT ROW 15. RELAMPED ROW 15 CEILING FLOODLIGHT. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008042500107 20080425 00107 EA 2008 4 25 S9BA200800017 1 20080410 A 5511 C6TP101613 SPAR DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6* 52043 EA ZONE 300 CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 125 573 DURING CAMP INSPECTION FOUND CORROSION ON LT AFT STABILIZATION SPARE WHERE THE SEA FIN ATTACHMENT BRACKET IS LOCATED. RE MOVED AND REPLACED OUTER HORIZONTAL REAR SPAR IAW AC 43 13 1B CHP. 7. EMERGENCY DECLARED? NO AIRCRAFT GROUNDED? NOT REPA IRED DURING INSPECTION. 1 H 7 2 3T 3 T RT A9EA E2NE 2008042500108 20080425 00108 EA 2008 4 25 S9BA200800016 1 20080410 A 5500 13A1200024 ATTACH BRACKET DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6* 52043 EA CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 125 573 DURING CAMP INSPECTION, FOUND CORROSION ON LT AFT (SEA FIN) ATTACHMENT BRACKET. REMOVED AND REPLACED SEA FIN ATTACHMENT BRACKET. EMERGENCY DECLARED? NO, AIRCRAFT GROUNDED, REPAIRED DURING INSPECTION NO. 1 H 7 2 3T 3 T RT A9EA E2NE 2008042500115 20080425 00115 CE 2008 4 25 GUUA04090801 1 20080409 A 3240 LINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BRAKE LOOSE A GUUA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 29 87554 UE227 FLIGHT:9140, DURING TAXI LT BRAKE PEDAL DROPPED TO THE FLOOR. SECURED MAIN LINE ON LT BRAKE ASSY, PERFORMED BRAKE BLEED ING AND SERVICED RESERVOIR. 2 L 7 2 4T 4 T RT A24CE E26NE 2008042500122 20080425 00122 NM 2008 4 25 CALA0800344 1 20080421 A 5320 143A541011 FLOOR SUPPORT BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24706 28767 CABIN FLOOR SUPPORT STA 380 TO 400 BL 0 CRACKED. REMOVED AND REPLACED FLOOR SUPPORT STA 380-400 BL 0 REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008042500123 20080425 00123 NM 2008 4 25 CALA0800345 1 20080421 A 5320 143A541011 FLOOR SUPPORT BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24706 28767 CABIN FLOOR SUPPORT STA 380 TO 400 RBL 13 CRACKED. REMOVED AND REPLACED CABIN FLOOR SUPPORT PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008042500126 20080425 00126 EA 2008 4 25 COMA0860229 1 20080419 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAULTY A COMA K NONE J WARNING INDICATION DE DESCENT 1 SO 01 590SW 7077 FLIGHT 5018 - RECEIVED FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED RIGHT BPSU . ALSO PERFORMED SE-27I001. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008042500138 20080425 00138 EA 2008 4 25 MASA200800327 1 20080419 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH FLT 2891 PHX-OMA. EMERGENCY LIGHT PANEL & EMERGENCY PATH LIGHTS INOP. MX FOUND LOOSE CONNECTOR AND RESECURED, OP C HECK GOOD. 2 L 7 2 4F RT A21EA 2008042500141 20080425 00141 EA 2008 4 25 MASA200800332 1 20080420 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT FALSE ACTIVATION A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 504MJ 10066 ASH FLT 7219 ORD-ORF. RIGHT WING EMERGENCY EXIT CAUTION MESSAGE INTERMITTENT. RE-CYCLED DOOR. 2 L 7 2 4F RT A21EA 2008042500142 20080425 00142 EA 2008 4 25 MASA200800325 1 20080419 A 3234 601R751451 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 654BR 7454 ASH FLT 1012 HNL-OGG. GEAR DISAGREE WARNING, MAIN GEAR INDICATED RED. CREW DECLARED AN EMERGENCY. REMOVED AND REPLACE D MAIN GEAR SELECTOR AND PRIORITY VALVES, OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2008042500150 20080425 00150 SO 2008 4 25 FDKA200804167 1 20080417 A 2611 DETECTION SYS EMB 145 EMB145LR 3260212 SO CARGO BAY MALFUNCTIONED A FDKA K NONE L NO TEST NR NOT REPORTED 1 SW 07 849MJ 145534 FDM 5992 BNA-JFK (0430 PHX LCL). BAGGAGE SMOKE DETECTION WILL NOT TEST. MX RESET SYSTEM. 2 L 7 2 4T RT T00011AT 2008042500155 20080425 00155 SO 2008 4 25 FDKA200804172 1 20080418 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FDM 6044 JFK-ALB. SERVICE DOOR EMERGENCY LIGHT INOP. MX RESET SYSTEM. 2 L 7 2 4T RT T00011AT 2008042500157 20080425 00157 SO 2008 4 25 FDKA200804173 1 20080419 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FDM RON JFK (1300 PHX LCL). EMERGENCY EXIT LIGHT ON SERVICE DOOR W/N ILLUMINATE. MX RESET. 2 L 7 2 4T RT T00011AT 2008042500158 20080425 00158 SO 2008 4 25 FDKA200804174 1 20080420 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 828MJ 145218 FDM 6169 RIC-MCO (0630 PHX LCL). EMERGENCY LIGHT AT ROW 12 IS INTERMITTENT. MX RESET LIGHT. 2 L 7 2 4T RT T00011AT 2008042500167 20080425 00167 NM 2008 4 25 2008UALA02314 1 20080419 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 39 RIGHT. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500168 20080425 00168 NM 2008 4 25 2008UALA02315 1 20080419 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 33R INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 33 RIGHT. SUPPLEMENTAL, REPLACED LIGHT ASSY. OP CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500169 20080425 00169 NM 2008 4 25 2008UALA02316 1 20080419 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 43L INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 43 LEFT. SUPPLEMENTAL, REPLACED LIGHT ASSY. OP CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500170 20080425 00170 NM 2008 4 25 2008UALA02317 1 20080419 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 18 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT LIGHT INOP, JUST AFT OF ROW 18 CEILING LIGHT. SUPPLEMENTAL, RELAMPED. OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500174 20080425 00174 NM 2008 4 25 2008UALA02320 1 20080419 A 3350 90085 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY EXIT LIGHTS IN FWD CABIN ILLUMINATED FOR A SHORT PERIOD THEN EXTINGUISHED. FOUND FAULTY BATTERY PACK. REPLACE D BATTERY PACK LIGHTS CHECK OK. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500183 20080425 00183 NM 2008 4 25 2008UALA02405 1 20080424 A 4900 32896961 VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 662UA 27159 APU WILL NOT PRODUCE COOL AIR 89 DEGREES IN CABIN AT GATE. ACCOMPLISHED EXSTENSIVE TROUBLE SHOOTING FOUND LOW LIMIT VAL VE TO BE FAULTY. REPLACED LOW LIMIT VALVE PER MM21-51-11. PERFORMED LEAK CHK NO LEAKS NOTED. OP CHECKED GOOD.AC OK F OR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042500185 20080425 00185 NM 2008 4 25 2008UALA02415 1 20080424 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EEL LT INOP, ROW 36 RT. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECKED OK. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500187 20080425 00187 2008 4 25 HNAA0800138 4 20080421 A 3442 071131900 ANTENNA DHAV DHC8 DHC8102 2809003 NM WEATHER RADAR INOPERATIVE A HNAA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 EA 07 804EX 37646 126 227 DURING CRUISE FLIGHT APPROACHING ORF THE RADAR UNIT STOPPED PAINTING THE SURROUNDING WEATHER AND THE GROUND. THE CREW C ALLED PDT DISPATCH TO ADVISE. DUE TO WEATHER IN ORF, MX HAD THE AIRCRAFT DIVERT INTO SBY FOR REPLACEMENT OF RADAR ANTEN NA. 2 H 7 2 4T RT A13NM 2008042500191 20080425 00191 NM 2008 4 25 2008UALA02326 1 20080420 A 3350 LENS BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 RT OVERWING EMERGENCY EXIT LIGHT LENS IS CRACKED. SUPPLEMENTAL, REMOVED AND REPLACED RT OVERWING EEL LENS ASSY. OP CH KS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042400093 20080424 00093 EU 2008 4 24 08FDEA01467 1 20080421 A 5522 A5527000000000 SKIN AIRBUS 310 A310203 3930313 EU ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 RIGHT ELEVATOR UPPER SURFACE TRAILING EDGE; INBD SECTION HAD 2 DENTS AND A PUNCTURE ON THE INBD T/E WEDGE. REPAIRED DAM AGE TO RT ELEVATOR UPPER SURFACE BY, REMOVING DAMAGED AREAS AND FABBED AND BONDING CORE, AND APPLYING FIBERGLASS LAYUPS IAW A310SRM 55-21-11. RESTORED FINISH IAW A310 SRM 51-75-10. 2 L 7 2 4F RT A35EU 2008042400104 20080424 00104 NM 2008 4 24 DLM90080606 1 20080306 A 5753 VANE DOUG MD90 MD9030 3023690 NM LT WING TE FLAP DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 LT WING I/B FLAP O/B FIXED VANE LOWER SURFACE HAS MULTIPLE DENTS. REPAIRED LT WING INBD FLAP O/B FIXED VANE, IAW MD90 S RM 51-50-04. 2 L 7 2 4F RT A6WE 2008042400105 20080424 00105 NM 2008 4 24 DLM90080607 1 20080402 A 5310 DOOR FRAME DOUG MD90 MD9030 3023690 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DN 53392 FWD CARGO PIT LWR DOOR JAMB IS CORRODED AROUND MULTIPLE FASTENER HOLES. REPAIRED DOOR JAMB, IAW MD80 SRM 53-05D. 2 L 7 2 4F RT A6WE 2008042400136 20080424 00136 NM 2008 4 24 08FDEA01488 1 20080423 A 5414 STRUCTURE BOEING 727 727232 1384082 NM NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 NR 2 ENGINE LEFT FWD COWLING OUTER AFT CORNER MULTIPLE LAYERS OF SHEET METAL ARE CRACKED. REMOVED DAMAGED AREA REF SRM 51-40-2. MATERIAL ID AT 2024 T3 .080 REF SRM 65-10-3 A48140 FOR DOUBLER. MATERIAL ID AT 2024 T3 .100 A 11734 REF SRM 5 4-30-2 FOR FILLER. TREATED AND PRIMED DOUBLER AND FILLER REF SRM 51-10-2 PG 7 PG 2. INSTALLED DOUBLER AND FILLER WET W ITH SEALANT REF SRM 54-10-3 PG 24. APPLIED TEFLON FINISH REF AMM 51-20-071-7. FABRICATION OF DOUBLER SRM 54-10-3, FILL ER SRM 51-30-3. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008042400151 20080424 00151 EU 2008 4 24 08FDEA01503 1 20080423 A 7160 A2242201523 NOSE COWL AIRBUS 300 A300F4605R 3930327 EU NR 2 ENGINE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 NR 2 ENGINE INBD FAN COWL IS DENTED. REMOVED DAMAGE, PREPPED FOR THE APPLICATION OF FILLER MATERIAL. APPLIED FILLER, CU RED, SANDED & PREPPED FOR PRIMER. APPLIED PRIMER & PAINTED IAW SRM 54-10-00, SRM 54-20-00 & SRM 51-75-10. 2 L 7 2 4F RT A35EU 2008042400173 20080424 00173 EA 2008 4 24 SWIA200819493 1 20080420 A 5610 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT DELAMINATED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 732SK 10194 PILOT'S SIDE WINDOW IS DELAMINATING. REPLACED PILOT'S SIDE WINDOW, P/N OFF 601R33033-19, S/N OFF 0419H9492. 2 L 7 2 4F RT A21EA 2008042400192 20080424 00192 EA 2008 4 24 SWIA200819513 1 20080104 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 755SK 10220 COCKPIT FLOOR SUPPORT AT FS 280 IS CRACKED AT LBL9, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ700/900 SRM 51-23-0 0 PG 1-10 AND 51-42-06 PG 7-8. 2 L 7 2 4F RT A21EA 2008042500016 20080425 00016 NM 2008 4 25 ASAA0852814 1 20080412 A 2421 7588429101 INDICATOR BOEING 737 737890 1384527 NM LT IDG FILTER ACTIVATED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 577AS 35186 LEFTHAND IDG DELTA P INDICATOR FOUND EXTENDED INDICATING CLOGGED FILTER. REPLACED BOTH IDG CHARGE AND SCAVENGE FILTERS. NO FILTER CONTAMINATION NOR OIL DISCOLORATION NOTED. 2 L 7 2 4F RT A16WE 2008042500036 20080425 00036 EA 2008 4 25 TRAX200800536 1 20080413 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 AAR - 2081 - CARGO COMPARTMENT FLOOR PANEL 282ERF CRACKED. 2 L 7 2 4F RT A21EA 2008042500053 20080425 00053 SO 2008 4 25 N382008F00001 1 20080320 A 3200 MS202194 PULLEY GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU LT MLG WW OBSTRUCTED A N38A K NONE O OTHER IN INSP/MAINT 1 EA 05 970SJ 11861 1146 AT PREFLIGHT, THE PILOT NOTICED THAT THE SPEED BRAKES DID NOT CLOSE COMPLETELY. MAINT WAS CALLED AND AFTER SOME OPERATI ONAL CHECKS AND A VISUAL INSPECTION OF THE CONTROL SYS AT THE LT MAIN GEAR WHEEL WELL A STONE WAS FOUND AT A CONTROL CAB LE PULLEY AND THE STONE WOULD NOT ALLOW THE CABLE TO CLOSE THE SPEED BRAKES ALL THE WAY. STONE LOGED IN PULLEY. (K) 2 L 7 2 4F 4 F RT A12EA E25NE 2008042500062 20080425 00062 WP 2008 4 25 ABXA080124 1 20080416 A 3213 39140165505 BUNGEE CYLINDER DOUG DC9 DC941 302207N WP LT MLG LEAKING A ABXA K NONE K FLUID LOSS CR CRUISE 1 GL 23 951AX 8545 47616 RIGHT HYDRAULIC QUANTITY LOSS TO ZERO. FOUND LEFT MAIN LANDING GEAR HYDRAULIC BUNGEE CYLINDER LEAKING. REPLACED LEFT B UNGEE CYLINDER IAW DC9 AMM 32-32-03-2. 2 L 7 2 4F A6WE 2008042500084 20080425 00084 EA 2008 4 25 TRAX200800550 1 20080416 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 SURFACE CORROSION ON LEFT PRESSURE FLOOR LANDING FS 449.85 AT LBL 45. REMOVED CORROSION PER SRM 53-41-45. COMPLIED WITH UT THICKNESS CHECK IAW NDTM 51-20-04. FOUND BLENDED AREA MINIMUM THICKNESS TO BE .068". PERFORMED EDDY CURRENT INSPE CTION OF BLENDED AREAS IAW NDTM 51-20-06. NO DEFECTS NOTED. BLENDOUT OUT OF LIMITS IAW SRM 53-41-45. MAPPED DAMAGE & SUBMITTED PER SRM 51-13-00. R & R FASTENERS PER REO 601R-53-41-714, PRIMED AND PAINTED PER SRM 51-25-00. APPLIED A FILL ET SEAL &CIC TO REWORK AREA. COMPLIED WITH EC/TC REO 601R-53-41-714. 2 L 7 2 4F RT A21EA 2008042500085 20080425 00085 EA 2008 4 25 TRAX200800551 1 20080416 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 SURFACE CORROSION ON LT PRESSURE FLOOR LANDING FS 484.00 AT LBL 45. REMOVED PRESSURE FLOOR LANDING FS 484 LBL 45 PER SR M 53-41-45. COMPLIED WITH UT THICKNESS CHECK OF BLENDED AREAS IAW NDTM 51-20-04. FOUND BLENDED AREA MINIMUM THICKNESS T O BE .068". PERFORMED EDDY CURRENT INSPECTION OF BLENDED AREAS IAW NDTM 51-20-06. NO DEFECTS NOTED. BLENDOUT IS OUT O F LIMITS IAW SRM 53-41-45. MAPPED DAMAGE & SUBMITTED PER SRM 51-13-00. R & R FASTENERS IN BLENDED AREA PER REO 601R-53-4 1-714, PRIMED & PAINTED PER SRM 51-25-00. APPLIED A FILLET SEAL & CIC TO REWORK AREA. COMPLIED WITH EC/TC REO 601R-53-4 1-714. 2 L 7 2 4F RT A21EA 2008042500113 20080425 00113 EA 2008 4 25 COMA0860227 1 20080421 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 7012 DURING FS 640 FRAME INSPECTION FOUND FORWARD FRAME CRACKED ON RT SIDE BELOW ENGINE SUPPORT BEAM. CUT OUT DAMAGED SECTIO N OF FRAME AND REPLACED WITH SPLICED IN REPAIR TO FRAME AND BONDED DOUBLER PER SB 601R-53-061, PART C, MOD 2-53M00003, R EO 601R-53-61-506, AND REO 53-61-569. 2 L 7 2 4F RT A21EA 2008042500134 20080425 00134 CE 2008 4 25 DXTA200802994 1 20080413 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 396QS 5600396 BOTH COPILOTS BRAKE PEDALS GO ALMOST TO THE FLOOR. VERIFIED NO LEAKAGE UNDER PEDALS IN COCKPIT. BLED BRAKES PER CESSNA MODEL 560 MM 32-42-00. OPERATIONAL CHECKED GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2008042500144 20080425 00144 SO 2008 4 25 C2XA08RI053 1 20080420 A 3350 2013BR BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14568 8318 2717 145628 RIC - DURING ROUTINE MAINTENANCE, MX FOUND SEVERAL EMERGENCY LIGHT POWERED BY NR 2 BATTERY INOPERATIVE. MX REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008042500149 20080425 00149 EA 2008 4 25 TRAX200800541 1 20080415 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 SEVERAL SEAT TRACKS IN CARGO COMPARTMENT HAVE CORROSION DAMAGE. JOB COMPLETE. REMOVED SEAT TRACKS AND INSTALLED NEW IA W CRJ200 SRM 53-41-49 COMPLETE. SUPPLEMENTAL SDR CLOSED 4/21/08. 2 L 7 2 4F RT A21EA 2008042500186 20080425 00186 2008 4 25 08FDEA01521 4 20080424 A 2565 DOOR FRAME AIRBUS 300 A300F4605R 3930327 EU SLIDE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 L-1 DOOR SLIDE ASSY; LOWER INTERNAL FRAME IS CRACKED AT THE FWD CORNER. NEW SERVICEABLE SLIDE RECEIVED. INSTALLED ON WI C 68S5001CP. 2 L 7 2 4F RT A35EU 2008042500192 20080425 00192 2008 4 25 USAA920080907 4 20080421 A 2565 D30665105 A/C PACK AIRBUS 320 A320214 3930316 EU EVAC SLIDE DETACHED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 113UW 18276 1093 1141 A-9 CK LAX - EES - R-2 SLIDE RAFT FWD COVER ASSEMBLY STRAP IS DETACHED FROM THE SLIDE ASSEMBLY. MAINTENANCE REMOVED AND REPLACED THE R-2 SLIDE/RAFT. 2 L 7 2 4F RT A28NM 2008042500199 20080425 00199 NM 2008 4 25 SWAA082065 1 20080420 A 5315 6546540 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND LONGITUDINAL FLOORBEAM VERTICAL STIFFENER CRACKED AT BS 639, LBL 46. REMOVED AND RE PLACED STIFFENER PER SWA EA. 2 L 7 2 4F RT A16WE 2008042500201 20080425 00201 NM 2008 4 25 SWAA082066 1 20080420 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 907 AND BS 927, STR 17L. REMOVED AND REPLACED WE B PER SRM. 2 L 7 2 4F RT A16WE 2008042500205 20080425 00205 NM 2008 4 25 SWAA082075 1 20080420 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 21R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008042500206 20080425 00206 2008 4 25 SWAA082077 4 20080420 A 2565 6557463 BRACKET BOEING 737 7373H4 1384600 NM EVAC SLIDE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT SLIDE BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM. 2 L 7 2 4F RT A16WE 2008042500207 20080425 00207 NM 2008 4 25 SWAA082076 1 20080420 A 2750 6546430189 TORQUE TUBE BOEING 737 7373H4 1384600 NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND LEFT WING INBOARD FORE FLAP OUTBOARD TORQUE TUBE CORRODED AT TOGGLE SUPPORTS. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2008042500208 20080425 00208 NM 2008 4 25 SWAA082104 1 20080421 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, RBL 20, WL 164. REMOVED AND REPLACED FRAME PER ACO. 2 L 7 2 4F RT A16WE 2008042500209 20080425 00209 NM 2008 4 25 SWAA082107 1 20080421 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, LBL 3. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008042500210 20080425 00210 NM 2008 4 25 SWAA082106 1 20080421 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SKIN P ER ER. 2 L 7 2 4F RT A16WE 2008042500215 20080425 00215 2008 4 25 SWAA082080 4 20080420 A 2565 5A30775 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 412WN 29818 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042500216 20080425 00216 2008 4 25 SWAA082081 4 20080418 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 423WN 29827 L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042500218 20080425 00218 NM 2008 4 25 SWAA082082 1 20080418 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 465WN 33829 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 175. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042500222 20080425 00222 2008 4 25 SWAA082123 4 20080420 A 2565 61620468 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR CANVASS WORN. REMOVED AND REPLACED EVAC SLIDE P ER MM. 2 L 7 2 4F RT A16WE 2008043000132 20080430 00132 NM 2008 4 30 SWAA082296 1 20080427 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17, WL 225. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008043000139 20080430 00139 NM 2008 4 30 SWAA082253 1 20080427 A 3350 6574550 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR LOWER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008043000143 20080430 00143 NM 2008 4 30 SWAA082275 1 20080427 A 5754 65C26601 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 L/E SLAT UPPER SURFACE DISBONDED. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 2008043000146 20080430 00146 NM 2008 4 30 SWAA082254 1 20080427 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042800164 20080428 00164 NM 2008 4 28 SWAA082180 1 20080423 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 431WN 29845 EEPLS END CAP LOOSE AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 2008042800208 20080428 00208 NM 2008 4 28 SWAA082199 1 20080423 A 5311 6546564 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 986, RBL 43. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008042800227 20080428 00227 NM 2008 4 28 2008UALA02300 1 20080419 A 5240 BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 4R FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 4R DOOR WILL NOT ARM. EMERGENCY LINKAGE TORQUE TUBE BEARINGS SEIZED. REPLACED TORQUE TUBE BEARINGS, DOOR OPS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042800231 20080428 00231 NM 2008 4 28 2008UALA02302 1 20080420 A 2432 263BA1012 BATTERY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE WEAK A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 781UA 26945 APU ARRIVED AT GATE WITH AN APU WEAK BATTERY MESSAGE AND APU CHARGER MESSAGE. BATTERY VOLTS AT 24 VDC, CHARGER NO MORE THAN 1 AMP CHARGE. FOUND FAULTY CHARGER. REPLACED APU BATTERY CHARGER AND APU BATTERY, REF MM 24-31-06 AND MM 24-31-05 . OPS TEST OK.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042800252 20080428 00252 SO 2008 4 28 SWIA200819537 1 20080423 A 3240 BRAKE ASSY EMB 120 EMB120ER 3260203 SO MLG MALFUNCTIONED A SWIA O OTHER O OTHER LD LANDING 1 NM 07 566SW 120341 FLT 5751 - POWER LEVERS WOULD NOT GO INTO REVERSE ALONG WITH A MOMENTARY LOSS OF BRAKING FORCE. SERVICED RIGHT STRUT AN D INSPECTED AND CLEANED MAIN LANDING GEAR PROX SWITCH AND HARNESS. BLED BRAKE SYSTEM. ALL OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2008042800272 20080428 00272 NM 2008 4 28 QXEA200800391 1 20080421 A 3230 483025 SEQUENCE VALVE BOMBDR DHC8 DHC8402 1390042 NM MLG FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 412QX 8977 4059 SEA - FLIGHT 2341 - AFTER TAKEOFF DURING GEAR RETRACTION, THE LEFT MAIN GEAR DOOR LIGHT REMAINED ON (AMBER). DID ALTERN ATE GEAR EXTENSION AND RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE LEFT MAIN GEAR SEQUENCE VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008042800274 20080428 00274 NM 2008 4 28 QXEA200800392 1 20080421 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY INOPERATIVE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 352PH 494 PSC - FLIGHT 2097 - BOTH BAGGAGE SMOKE DETECTORS INOP. MAINTENANCE REPAIRED A CHAFED WIRE AT 2612-P3 CONNECTOR. OPERAT IONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008042800317 20080428 00317 NM 2008 4 28 CALS097007C 1 20080303 A 2497 FEEDER CABLE BOEING 747 747409 13848AU NM JACOBS R915 L6 35005 EA APU GENERATOR CHAFED W SAJF K NONE O OTHER IN INSP/MAINT 1 WP 03 18205 28712 AIRLINES WAS ASKED TO PERFORM THE INSPECTION (APU GENERATOR FEEDER CABLES AND CLAMP STANDOFF FOR CHAFING AGAINST THE WAS TE TANK DUCT), AND FOUND THAT B-18205 LT BULK CARGO COMPARTMENT STA 2060 APU GENERATOR FEEDER CABLE CLAMP STANDOFF RIVET LOOSEN. THIS HAS BEEN CORRECTED AND RECORDED. IT HAS ALSO BEEN REPORTED TO MFG. 2 L 7 4 4F 3 R RT A20WE TC195 2008042800323 20080428 00323 EU 2008 4 28 RMXA011408001 1 20080114 A 5310 DOOR FRAME AGUSTA A109 A119 0261102 EU PWA PT6 PT6* 52043 EA BS 2044 CRACKED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 820NA 3467 14011 PU0105 MAJOR REPAIRS: LT CORNER DOOR POST FRAME STA. 2044 WL 1400 CRACKED. LT INNER DOOR FRAME CRACKED. LT/RT INNER UPPER DO OR FRAME CRACKED. LT INNER DOOR FRAME, PATCH. MINOR REPAIRS: LT/RT UPPER FRAME AT THE GREENHOUSE WINDOW SUPPORT FRAME . INSTALLED NEW UPPER AFT ANGLE P/N 109-0320-26-59. 1 G 7 2 3U 3 T H7EU E2NE 2008042800325 20080428 00325 CE 2008 4 28 DXTA200802999 1 20080415 A 2120 104968 CONTROL VALVE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP CABIN AIR SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 821QS 2406 258709 SMOKE COMING FROM FLOOD VENT REAR CABIN. ACCESSED CABIN TEMP CONTROL VALVE, ACCOMPLISHED FUNCTIONAL TEST OF VALVE, NO D EFECTS NOTED. REMOVED VALVE & INSPECTED BUTTERFLY, NO DEFECTS NOTED. REINSTALLED VALVE. FUNCTIONAL TEST TEMP CONTROL SYS IN BOTH AUTO & MANUAL, NO DEFECTS NOTED. NO SMOKE DETECTED. ACCESSED WATER SEPARATER. REMOVED & INSPECTED SOCK. NO DEFE CTS NOTED. REINSTALLED CONDENSOR SOCK & WATER SEPARATOR. TEMP CONTROL VALVE REPLACED AS A PRECAUTION. REMOVED VALVE & IN STALLED O/H VALVE ACCOMPLISHED OPS CHECKS LEAK CHECKS. NO DEFECTS NOTED. IAW MM 21-60-00, 21-10-95, 21-60-67. 2 L 7 2 4F 4 F RT A3EU E6WE 2008042800330 20080428 00330 WP 2008 4 28 2008F00013 1 20080407 A 2711 TRIM TAB DOUG DC6 DC6A 3021706 WP PWA R2800 CB3 52026 NE HAMSTD 43E 43E60 NE AILERONS BINDING I EVAB A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 AL 01 7780B 45372 AILERONS BINDING ON TAKEOFF AFTER GEAR RETRACTION (BEFORE TAKEOFF CONTROL CHECK) NORMAL. FOUND THAT THE AILERON SPRING TAB MECHANISM WAS BINDING PREVENTING MOVEMENT OF THE TAB SYSTEM WHICH IN TURN INCREASED THE FORCES REQUIRED TO MOVE THE AILERONS. 2 L 7 4 4R 4 R 6A3 E264 6 C P871 2008042800345 20080428 00345 NM 2008 4 28 ASMF200804002 1 20080417 A 3230 273A33018 MODULE BOEING 737 737 UTILSYS NM CFMINT CFM567 CFM567B22 13802 NE MLG FAILED W ASMF O OTHER J WARNING INDICATION CL CLIMB 1 SW 23 851AM 13276 13276 29363 DURING TAKEOFF, THE (3) LIGHTS OF LANDING GEAR TURNED ON; CAPTAIN PERFORMED AN ADDITIONAL LANDING GEAR CYCLE AND LIGHTS TURNED OFF. MAINT PERFORMED FIM 32-61 TASK 809, FOUNDING INTERMITTENT FAILURE OF THE LANDING GEAR MODULE, SO IT WAS REPL ACED AND TESTED IAW MM 32-31-11 AND 32-31-00 TASK 730-802, ALL CORRECT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008042800356 20080428 00356 EU 2008 4 28 BA08016 1 20080423 A 7711 8112507 RELAY AIRBUS 330 A330323 3930335 EU PWA 4168 PW4168 NE NR 1 ENGINE UNSERVICEABLE A USAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 19 271AY 8683 969 0323 P733468 PHL FLT 754 - EN ROUTE PHL - CDG. DURING FLIGHT, RECEIVED ECAM MESSAGE "AUTO FLT A/THR OFF", AND " ENG 1 EPR MODE FAULT ". THE FLIGHT RETURNED TO FIELD PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMBER ONE ENGINE RE LAY UNIT. OPERATIONALLY CHECKS OK. 2 L 7 2 4F 4 F RT A46NM E36NE 2008042800367 20080428 00367 WP 2008 4 28 UPS08852064 1 20080412 A 5347 DC853B007002 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 SEAT TRACK STA 960 RIGHT, DAMAGED MDCC RBL48. CUT OUT DAMAGE AND INSTALL PLUG IAW SRM 51-1-8, 53-2-3 FIG 6D. 2 L 7 4 4F RT 4A25 2008043000016 20080430 00016 NM 2008 4 30 ASAA0892840 1 20080324 A 5315 147A550414 FLOORBEAM BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 317AS 30856 CABIN FLOORBEAM CORRODED STA 947.5 AT BL 0 AREA. REMOVED CORROSION, HFEC INSPECTED REWORKED AREA NO CRACKS NOTED. FABR ICATED REPAIR STRAP, REPAIR PARTS, LOCATED, DRILLED AND INSTALLED IAW AAR EA 12572 AND ASA EA 5310 02783. 2 L 7 4 4F RT A16WE 2008043000031 20080430 00031 NM 2008 4 30 KCSA081229 1 20080424 A 3350 LIGHT BOEING 747 747249F 1384849 NM EXTERIOR INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 706CK 21827 RIGHT SIDE UPPER DECK EXTERIOR EMERGENCY SLIDE EXIT LIGHT INOP. 2 L 7 4 4F RT A20WE 2008043000040 20080430 00040 NM 2008 4 30 2008UALA02291 1 20080418 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 585 S23L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 EXTERNAL FUSELAGE HAS A SKIN DENT STA 585, STR 23L. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008043000041 20080430 00041 NM 2008 4 30 2008UALA02293 1 20080419 A 5320 STIFFENER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 377 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 CABIN FLOORBEAM STIFFENER CRACKED, STA 377.7, BL 0. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED NEW STIFFENER. 2 L 7 2 4F 4 F RT A2NM E17NE 2008043000043 20080430 00043 NM 2008 4 30 2008UALA02295 1 20080419 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 365 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 MAIN CABIN BS 365 TEE CAP HAS CORROSION AT RBL 42. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGE, 1" X 2" FWD EDGE OF TEE C AP. INSTALLED FILLER & ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008043000044 20080430 00044 NM 2008 4 30 2008UALA02298 1 20080420 A 5240 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 1R DOOR INNER SKIN HAS A CRACK PROTRUDING FROM LIGHTENING HOLE, LWR AFT END OF DOOR. CRACK IS APPROX 0.100 INCH. MAJOR REPAIR ACCOMPLISHED: MFG'D & INSTALLED FILLERS, REPAIR STRAP, TRIM & DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2008043000047 20080430 00047 NM 2008 4 30 CALA0800358 1 20080424 A 5311 6546539 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 BS 616 INBOARD CHORD AT RBL 66 IS CRACKED. REPAIRED CRACKED CHORD AT BS 616 IAW ECRA 5311-01158 AND B737-500 SRM 51-40- 02. 2 L 7 2 4F RT A16WE 2008043000053 20080430 00053 EU 2008 4 30 TRAX200800568 1 20080421 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 631AS 362 EMERGENCY LIGHTING WILL NOT TURN OFF. 2 H 7 2 4T RT 2008043000057 20080430 00057 EA 2008 4 30 TRAX200800572 1 20080424 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 858AS 7417 FWD EMERGENCY LIGHTS INOP. 2 L 7 2 4F RT A21EA 2008043000071 20080430 00071 NM 2008 4 30 SWAA082210 1 20080424 A 3350 MS155721 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008043000081 20080430 00081 NM 2008 4 30 SWAA082212 1 20080424 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000082 20080430 00082 NM 2008 4 30 SWAA082213 1 20080424 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000099 20080430 00099 NM 2008 4 30 SWAA082227 1 20080424 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 775SW 30590 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008043000100 20080430 00100 NM 2008 4 30 KCSA081231 1 20080426 A 3350 LIGHT BOEING 747 747249F 1384849 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 706CK 21827 RIGHT UPPER DECK DOOR FRAME EMERGENCY LIGHT IS OUT. 2 L 7 4 4F RT A20WE 2008043000113 20080430 00113 NM 2008 4 30 CALA0800376 1 20080408 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 STATION 400 LT BETWEEN S8LT & S9LT AT AC BRACKET I/B FASTENERS ARE CRACKED. REPAIRED CRACKED FRAME AT STATION 400 BETWE EN S8LT AND S9LT AT AC BRACKET IAW EA5310-04498. 2 L 7 2 4F RT A16WE 2008043000114 20080430 00114 NM 2008 4 30 CALA0800377 1 20080408 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 STATION 827 LT BETWEEN S8LT AND S9LT AT AC BRACKET I/B FASTENER HOLE IS CRACKED. REMOVED AC BRACKET IAW B737 SRM 51-40- 02, CUT OUT DAMAGED HOLES IAW EA5310-04498, MATERIAL ID FOR REPAIR ANGLES "A" & "B" 7075-0 .040 IAW B73753-60-07 AND EA5 310-04498, HEAT TREATED REPAIR ANGLES TO 70 75T6 IAW BAC5602 LOAD NUMBERS 354+360, INSTALLED REPAIR IAW EA5310-04498, CO LD WORKED & INSTALLED FASTENERS IN REQUIRED HOLES. 2 L 7 2 4F RT A16WE 2008043000126 20080430 00126 NM 2008 4 30 SWAA082274 1 20080427 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 28L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008043000128 20080430 00128 NM 2008 4 30 SWAA082244 1 20080425 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008043000149 20080430 00149 NM 2008 4 30 SWAA082255 1 20080427 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER 4R CRACKED AT BS 311. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008043000150 20080430 00150 NM 2008 4 30 SWAA082256 1 20080425 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008043000155 20080430 00155 NM 2008 4 30 SWAA082280 1 20080427 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER 5L CRACKED AT BS 1010. REPAIRED STRINGER PER EA. 2 L 7 2 4F RT A16WE 2008043000160 20080430 00160 NM 2008 4 30 SWAA082264 1 20080427 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, RBL 7 TO RBL 15, WL 152. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008043000164 20080430 00164 NM 2008 4 30 SWAA082285 1 20080427 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000167 20080430 00167 NM 2008 4 30 SWAA082262 1 20080427 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND NLG W/W CEILING PANEL WEB CUTOUT CRACKED AT BS 252, RBL 8. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 2008043000168 20080430 00168 NM 2008 4 30 SWAA082288 1 20080427 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000176 20080430 00176 NM 2008 4 30 SWAA082269 1 20080427 A 3350 20131A BATTERY BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008043000181 20080430 00181 NM 2008 4 30 CAKA0800384 1 20080428 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 CABIN STATION 440 AT S9L PASSENGER SERVICE UNIT RAIL BRACKET TO FRAME CRACKED. INSTALLED REPAIR DOUBLERS PER EA 5310-04 498. 2 L 7 2 4F RT A16WE 2008043000182 20080430 00182 NM 2008 4 30 CALA0800382 1 20080428 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 CABIN STATION 747 BETWEEN S8R AND S9R PASSENGER SERVICE UNIT RAIL ATTACH BRACKET TO FRAME CRACKED. REPAIRED FRAME AT ST ATION 747 BETWEEN S8R AND S9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008043000185 20080430 00185 NM 2008 4 30 CALA0800386 1 20080428 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 CABIN STATION 867 BETWEEN S8R AND S9R PASSENGER SERVICE UNIT RAIL ATTACH BRACKET TO FRAME CRACKED. INSTALLED REPAIR ANG LES REF EA 5310-04498. 2 L 7 2 4F RT A16WE 2008043000194 20080430 00194 NM 2008 4 30 CALA0800395 1 20080426 A 7830 491B1330011 TORQUE BOX BOEING 767 767224 1385170 NM THRUST REVERSER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 73152 30431 NUMBER 2 ENGINE RIGHT C-DUCT FWD TORQUE BOX ATTACH WEB AT 1 O’CLOCK POSITION FOUND CRACKED. NUMBER 2 ENGINE RIGHT C-DUC T FWD TORQUE BOX WEB AT 1 O'CLOCK POSITION REPAIRED PER MRAS CMM78-32-02 REPAIR 24. 2 L 7 2 4F RT A1NM 2008043000195 20080430 00195 NE 2008 4 30 TRAX200800575 2 20080424 A 7200 ENGINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* 30015 NE LEFT SURGES A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 27 720EV 10115 ON TAKEOFF - LT ENGINE SURGING FROM TAKEOFF POWER TO IDLE. FOLLOWED QRH AND PERFORMED LT ENGINE SHUTDOWN AND RETURNED T O MEM. FLT 4230 CX. AIRCRAFT RETURNED TO ATL AFTER T/O. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION O F AN APPROPRIATE CORRECTIVE ACTION. EMERGENCY DECLARED. 2 L 7 2 4F 4 F RT A21EA 2008043000196 20080430 00196 NM 2008 4 30 SWAA082299 1 20080428 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 202WN 33999 EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008043000208 20080430 00208 NM 2008 4 30 SWAA082323 1 20080428 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 421LV 32452 DURING SCHEDULED 6Y CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 133. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008043000209 20080430 00209 NM 2008 4 30 SWAA082321 1 20080428 A 5322 6546536 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 559, STR 17L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008043000211 20080430 00211 NM 2008 4 30 SWAA082313 1 20080428 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000213 20080430 00213 NM 2008 4 30 SWAA082315 1 20080428 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 444, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008050100012 20080501 00012 NM 2008 5 1 GTIA0800054 1 20080401 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 525NK 2942 AFT GALLEY FLOORBEAM, Y765 BETWEEN FR 67 AND FR 70 CORRODED. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2008050100013 20080501 00013 NM 2008 5 1 GTIA0800055 1 20080403 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 525NK 2942 AFT GALLLEY FLOORBEAM -Y765 BETWEEN FR 67 AND FR 64 CORRODED. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2008050100014 20080501 00014 SO 2008 5 1 CHQA200800082 1 20080420 A 2121 4611028900 FAN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL RECIRCULATION FAULTY A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 977RP 20044 20044 145185 CAE312736 FLIGHT 7795, IAD TO YYZ - AFTER TAKEOFF, UPON GEAR RETRACTION, FLT CREW NOTICED A SLIGHT HAZE IN COCKPIT. FLT CREW PERF ORMED CHECKLISTS AND RECIRCULATION FAN TURNED OFF, AFTER WHICH THE SMOKE DISAPPEARED. FLT ATTENDANT VERIFIED SLIGHT HA ZE IN CABIN AS WELL. ACFT RETURNED TO IAD AND LANDED WITHOUT INCIDENT. MX INSPECTED ACFT PER MM 21-20-00-810-810A, AND OPERATED BOTH 1 AND 2 BLEED SYSTEMS AND FOUND NO SMOKE OR ABNORMAL ODORS. MX UNABLE TO DUPLICATE FAULT. NEXT DAY, HAZ E RETURNED DURING A PREFLT RUN-UP AND ACFT FERRIED TO CMH FOR FURTHER TROUBLESHOOTING. ACFT TROUBLESHOT AND FAULT TRACE D DOWN TO RT RECIRCULATION FAN. AFTER REPLACING RECIRCULATION FAN ACFT RUN AT HIGH POWER AND BLEEDS RUN AS WELL AS THE 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008050100015 20080501 00015 WP 2008 5 1 NWAA081759987 1 20080422 A 3397 WIRE DOUG DC9 DC932 3022066 WP TAXI LIGHT BURNED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 01 987US 47458 ON APPROACH FOR LANDING AT IAD, THE PILOTS DETECTED A VERY STRONG ELECTRICAL HOT ODOR CIRCULATING THE COCKPIT. APPROACH AND LANDING CONTINUED WITHOUT ANY FURTHER INCIDENT. CREW STATED THE ODOR DISSIPATED WHEN TAXIING TO THE GATE. MAINTEN ANCE FOUND THE NOSE TAXI LIGHT SWITCH HAS A BURNED WIRE END LUG DUE TO A LOOSE TERMINAL. THE SWITCH WAS REPLACED, THE D AMAGED WIRE WAS REPAIRED, AND TERMINALS WERE VERIFIED SECURE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 2008050100016 20080501 00016 EA 2008 5 1 MASA200800336 1 20080423 A 3233 17008111 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 650ML 17152 7137 ASH 7045 IAD-HSV - GEAR DISAGREE AFTER TAKEOFF. REPLACED RT MLG SIDE STAY ACTUATOR. 2 L 7 2 4F RT A21EA 2008050100018 20080501 00018 2008 5 1 MASA200800337 2 20080423 A 7261 PACKING DHAV DHC8 DHC8202 2809007 NM PRESSURE PROBE LEAKING A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 991HA 431 ASH INBD FLT 2907 PHX-GJT - OIL ODOR WHEN BLEEDS ON. REMOVED AND REPLACED PACKINGS AT LOW PRESSURE PROBES AND REMOVED F OD FROM DRAIN. 2 H 7 2 4T RT A13NM 2008050100019 20080501 00019 EA 2008 5 1 MASA200800339 1 20080424 A 5210 601R317043 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7305V 7305 ASH FLT2825 PHX - PAX DOOR HARD TO OPEN AND CLOSE. REMOVED AND REPLACED OUTER HANDLE, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008050100020 20080501 00020 EA 2008 5 1 MASA200800340 1 20080424 A 3350 59257 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH FLT 2985 PHX-SLC - INTERIOR EMERGENCY LIGHT BELOW THE LEFT OVERWING EXIT INOP. MX REMOVED AND REPLACED THE NR 3 IN VERTER, OPS CHECK NORMAL. 2 L 7 2 4F RT A21EA 2008050100021 20080501 00021 NM 2008 5 1 MASA200800342 1 20080422 A 5754 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM NR 3 FLAP WORN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 455YV 455 LT NR 3 FLAP TRACK HAS 3 AREAS OF WEAR. REPAIRED FLAP TRACK. 2 H 7 2 4T RT A13NM 2008050100022 20080501 00022 NM 2008 5 1 MASA200800341 1 20080422 A 5754 FLAP TRACK DHAV DHC8 DHC8202 2809007 NM TE FLAP CORRODED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 455YV 455 WEAR AND CORROSION ON FLAP TRACK NR 1. REPAIRED FLAP TRACK. 2 H 7 2 4T RT A13NM 2008050100024 20080501 00024 EU 2008 5 1 08FDEA01540 1 20080425 A 5420 A54610053 BUSHING AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CORROSION ON PYLON NR 2, RIB 12 OUTBOARD WING LUGS. REPAIR PERFORMED BY REPLACEMENT OF BUSHINGS IAW SRM 57-20-34 PB 200, APPROVED BY EA 6-5451-117148. 2 L 7 2 4F RT A35EU 2008050100025 20080501 00025 EU 2008 5 1 08FDEA01541 1 20080425 A 5740 A57140336 BUSHING AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CORROSION ON PYLON NR 2, RIB 12 OUTBOARD WING LUGS. REPAIR PERFORMED BY REPLACEMENT OF BUSHINGS IAW SRM 57-20-34 PB 200, APPROVED BY EA 6-5451-117148. 2 L 7 2 4F RT A35EU 2008050100030 20080501 00030 EU 2008 5 1 08FDEA01546 1 20080425 A 5320 A53973085 SILL AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 CRACK FINDING ON C 60A-62 RT IN UPPER FLANGE OF AFT CARGO DOOR SILL BEAM REPAIR PERFORMED IAW SRM 53-17-18 WITH DEVIATIO N IN FASTENER USE (CHANGE FROM MS20426DD6 TO HL11VF5/NSA 5075-5) APPROVED BY RAS/EFW/9000020/2008 AND EA 6-5317-117138. 2 L 7 2 4F RT A35EU 2008050100032 20080501 00032 EU 2008 5 1 08FDEA01548 1 20080425 A 5311 A53981706 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND DEFORMED FLANGE AT C 75, P26 RT REPAIR PERFORMED BY REWORK OUTER FLANGE TO ELIMINATE THE DEFORMATION, NDT FOR CRAC K FREE IAW AS/EFW/9000019/2008 ISS A, APPROVED BY EA 6-5318-117150. 2 L 7 2 4F RT A35EU 2008050100033 20080501 00033 EU 2008 5 1 08FDEA01549 1 20080425 A 5330 A53610318255 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND OLD LIGHTNING STRIKE REPAIR AT C 1-40 LT WITH BAD DOCUMENTATION. REPAIR PERFORMED BY CORRECTION IAW SRM 53-10-12 FIG 219 WITH 2 DEVIATION ON C8-9, P27LT. REPAIRED BY PERFORMING ROTO AND EC-TEST AND INSTALLING DAN5-6Y AND C11 P28 LT, WHICH WAS REPAIRED BY OVERSIZING AND INSTALLING OF BUSH IAW SRM 53-10-12 FIG 219. APPROVED BY RAS 70504312/009/2008 IS S A AND EA 6-5312-117146. 2 L 7 2 4F RT A35EU 2008050100034 20080501 00034 EU 2008 5 1 08FDEA01550 1 20080425 A 5540 A55471500026 PLATE AIRBUS 300 A300B4622R 3930312 EU RUDDER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CORROSION ON RUDDER LIGHTING PROTECTION PLATE LT SIDE. REPAIR PERFORMED BY REMOVAL OF CORROSION, LAMINATE THE DAM AGED AREA AND INSTALLING A NEW PLATE IAW RAS/DAHAM/4024150/2008 ISS A, APPROVED BY EA 6-5541-114926. 2 L 7 2 4F RT A35EU 2008050100035 20080501 00035 EU 2008 5 1 08FDEA01551 1 20080425 A 5540 PLATE AIRBUS 300 A300B4622R 3930312 EU RUDDER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CORROSION ON RUDDER LIGHTING PROTECTION PLATE RT SIDE. REPAIR PERFORMED BY REMOVAL OF CORROSION, LAMINATE THE DAM AGED AREA AND INSTALLING A NEW PLATE IAW RAS/DAHAM/4024150/2008 ISS A, APPROVED BY EA 6-5541-114926. 2 L 7 2 4F RT A35EU 2008050100037 20080501 00037 EU 2008 5 1 08FDEA01553 1 20080425 A 5754 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT RT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CHAFING MARKS ON SLAT NR 1 RT, FOLDING NOSE AREA. REPAIR PERFORMED BY BLEND OUT DAMAGE TO SMOOTH CONTOUR IAW RAS/ FOK/032/2008 ISS A, APPROVED BY EA 6-5742-115274. 2 L 7 2 4F RT A35EU 2008050100039 20080501 00039 EU 2008 5 1 08FDEA01556 1 20080425 A 5710 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 CORROSION AND LIGHTNING STRIKE FOUND ON RT WING TIP. REPAIR PERFORMED BY BLEND OUT AREA IAW RAS/FOK/037/2008 ISS A, APP ROVED BY EA 6-5730-115275. 2 L 7 2 4F RT A35EU 2008050100041 20080501 00041 EU 2008 5 1 08FDEA01558 1 20080425 A 5330 A53978124219 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 TOOLING MARK FOUND ON SKIN AT C 58-59, P 13 RT REPAIR PERFORMED BY CUT OUT THE DAMAGED SKIN AND INSTALLING AN EXTERNAL D OUBLER IAW RAS/EFW/9000021/2008 ISS B, APPROVED BY EA 6-5316-117141. 2 L 7 2 4F RT A35EU 2008050100042 20080501 00042 EU 2008 5 1 08FDEA01559 1 20080425 A 5754 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU NR 3 SLAT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CHAFING MARKS ON SLAT NR 3 TRACK 10 OUT OF LIMIT. REPAIR PERFORMED BY BLEND OUT THE DAMAGE AND INSTALLING AN EXTE RNAL PATCH IAW RAS FOK/049/2008 ISS A, APPROVED BY EA 6-5744-117139. 2 L 7 2 4F RT A35EU 2008042800271 20080428 00271 NM 2008 4 28 QXEA200800390 1 20080422 A 5230 HANDLE BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR UNSECURE A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 424QX 4006 SEA - FLIGHT 2295 - ABORTED TAKEOFF DUE TO AFT CARGO DOOR INDICATION. THERE WAS ENOUGH RUNWAY TO STOP WITHOUT EXCESSIVE BREAKING. RETURNED TO THE GATE. MAINTENANCE FOUND THE DOOR HANDLE OUT AND ALSO SOME GREASE AND DEBRIS IN THE AREA. C LEANED AREA. DOOR OPERATED NORMALLY. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008042800283 20080428 00283 EA 2008 4 28 SWIA200819526 1 20080101 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 609SK 10020 RIGHT SIDE OF FS 280 BULKHEAD WEB HAS CORROSION, FOUND AT C-CHECK. REPAIRED AREA PER CRJ700/900 SRM 52-11-10-201-003-A0 1 AND REPAIR NR 601R-53-0076A. 2 L 7 2 4F RT A21EA 2008042800288 20080428 00288 NM 2008 4 28 UPS08M52056 1 20080121 A 5753 HINGE FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING MOUNTED HINGE AFT LOWER I/B BORE HOLE AND FACE AREA RUSTY AS MARK ED. LEFT FWD O/B FLAP I/B HINGE LWR MOUNT I/B BORE & SPOT FACE CORROSION REMOVED & FOUND EXCEED LIMIT PER CMM57-44-08 P G602-607R.60. FPI C/OUT IAW DACNDTSPM R.13 PART 06-10-01.001. FOUND NO CRACK & CORROSION EVIDENT. LEFT FWD O/B FLAP I /B HINGE LWR MOUNT I/B HOLE SPOTFACE THK OF0.521" ACCEPTED PER EN1092-0 8. REWORKED AREA ETCH INSPECTED AND FOUND SATIS PER EN1092-08. 2 L 7 3 4F RT A22WE 2008042800306 20080428 00306 NE 2008 4 28 F2P2008F00000 2 20080228 A 7320 2525499 HOSE HONEYWELL CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE NR 2 FCU LOOSE E F2PA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 19 716SX C4102 5600281 500048 DURING TAKEOFF ROLL, NR 2 ENGINE LOST POWER AND ROLLED BACK TO LOW IDLE, TAKEOFF WAS ABORTED WITH NO FURTHER INCIDENT. CAUSE OF TROUBLE WAS FOUND TO BE THAT THE P2/T2 SENSOR LINE, PN 2525499 FROM PT/T2 SENSOR TO FUEL CONTROL UNIT(FCU) CAM E LOOSE AND SEPARATED FROM THE P2/T2 SENSOR. IT WAS FOUND THAT THIS LINE HAS 2 90 DEGREE FITTINGS WITH PN MS27068UCL (S TAMPED ON IT) INSTALLED ON BOTH ENDS OF LINE, THIS FITTING HAS A B-NUT SIDE THAT IS SAFTIED BUT THE (MALE) SIDE OF FITT ING THAT SCREWS INTO HOSE HAS NO PROVISION TO ATTACH SAFETY WIRE. THIS NUT CAME LOOSE. A NEW LINE WITH SAME PN WAS INS TALLED, THIS NEW LINE DOES NOT HAVE THE MS27068-4CL FITTING. THE NEW HOSE ASSY ORDERED IS MODIFIED WHICH WOULD PREVENT 2 L 7 2 4F 4 F RT A22CE E25EA 2008042800315 20080428 00315 NM 2008 4 28 CALS097007A 1 20080226 A 2497 FEEDER CABLE BOEING 747 747409 13848AU NM APU GENERATOR CHAFED W SAJF K NONE O OTHER IN INSP/MAINT 1 WP 03 18273 24311 ASKED TO PERFORM THE INSPECTION "APU GENERATOR FEEDER CABLES AND CLAMP STANDOFF FOR CHAFING AGAINST THE WASTE TANK DUCT" , AND FOUND THAT B-18273 APU GENERATOR FEEDER CABLE OUTER JACKET CHAFING AT STA 2060 LT. THIS HAS BEEN CORRECTED AND REC ORDED. IT HAS ALSO BEEN REPORTED TO MFG. 2 L 7 4 4F RT A20WE 2008042800321 20080428 00321 NE 2008 4 28 DXTA200802998 2 20080414 A 7261 ENGINE GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE LEFT OVERSERVICED E DXTA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 708QS 069 SHORTLY AFTER ROTATION THERE WAS AND OVERWHELMING ODOR SIMILAR TO BURNED RUBBER. INSPECTED LT & RT ENGINES FOR ABNORMAL CONDITIONS, INSPECTED ECS SYS, FOUND NO DEFECTS. TECHS PERFORMED ENGINES RUN. AN ODOR LIKE BURNED OIL FROM LT ENGINE AT BOTH LOW & HIGH POWER SETTINGS. SHUTDOWN ENGINES, PERFORMED ENGINES OIL LEVEL CHECK. FOUND LT ENGINE OVERSERVICED. RESER VICED LT ENGINE OIL PER MM 12-17-00. TECHS PERFORMED ENGINES RUN FOR 45 MINUTES AT HIGH POWER & WITH ECS SELECED TO FULL HOT & COLD POSITION. DURING FINAL 15 MINUTES OF ENGINES RUN, THERE WAS NO NOTABLE OF BURNED OIL ODOR AT ANY POWER SETTI NG, AT THIS TIME. ALL WORKS WERE PERFORMED IAW MM. 2 L 7 2 4F 4 F RT A53NM E35NE 2008042800334 20080428 00334 CE 2008 4 28 GUUA04130801 1 20080413 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81533 UE137 DURING SCHEDULED ROUTINE MAINT, DISCOVERED LT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED LT OB ELEVATOR HINGE ASSY. 2 L 7 2 4T 4 T RT A24CE E26NE 2008042800348 20080428 00348 EU 2008 4 28 USAA920080908 1 20080421 A 2131 CONTROLLER AIRBUS 320 A320214 3930316 EU CABIN PRESSURE FAILED A USAA B A EMER. DESCENT UNSCHED LANDING J G WARNING INDICATION MULTIPLE FAILURE CR CRUISE 1 EA 19 110UW 1112 FLT 1697 - CLT-RSW - DIV - CREW REPORTED BOTH PACKS FAULTED SIMULTANEOUSLY AT FL 360 AND WOULD NOT RESET CAUSING AN EMER GENCY DESCENT. PACKS RESET THEMSELVES AUTOMATICALLY ON DESCENT, THEN FAULTED AGAIN CAUSING CABIN ALTITUDE WARNING. REA CHED APPROX 10,200 FT. CREW ELECTED TO DIVERT TO TPA FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE OUTFLOW VAL VE AND CABIN PRESSURE CONTROLLER. TEARDOWN REPORTS INDICATES THE CABIN PRESSURE CONTROLLER WAS A CONFIRMED FAILURE. R EASON FOR REMOVAL JUSTIFIED. FOUND SHORTED T14 TRANSISTOR. (S) 2 L 7 2 4F RT A28NM 2008042900009 20080429 00009 NM 2008 4 29 2008UALA02194 1 20080415 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1183 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 RT CREASE BEAM CORRODED AROUND SEVERAL FASTENERS AT STA 1183, RBL 67, WL 208.10. MAJOR REPAIR ACCOMPLISHED: INSTALLED NE W CREASE BEAM. 2 L 7 2 4F 4 F RT A2NM E17NE 2008043000046 20080430 00046 NM 2008 4 30 CALA0800357 1 20080424 A 5320 BAC1493248 CHANNEL BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 AFT CARGO, AT STATION 847 & 4" STRINGER 24R TIE CLIP CORRODED. REMOVED CORRODED STRINGER CHANNEL PER B737 SRM 51-40-02, FABRICATED NEW STRINGER TIE CLIP CHANNEL AT STATION 847+4 STR 24R, TREATED AND INSTALLED STRINGER TIE CLIP CHANNEL AT S TATION 847 + 4 STR 24R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008043000058 20080430 00058 EA 2008 4 30 TRAX200800573 1 20080424 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 738EV 10146 LEFT AFTMOST EXTERNAL EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008043000059 20080430 00059 EA 2008 4 30 TRAX200800574 1 20080424 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 823AS 7196 NR 4 EXTERIOR EMERGENCY LIGHTS OUT. 2 L 7 2 4F RT A21EA 2008043000067 20080430 00067 NM 2008 4 30 SWAA082203 1 20080424 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 463WN 32467 DURING SCHEDULED HC2 CHECK, LEFT FWD CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY P ACK PER MM. 2 L 7 2 4F RT A16WE 2008043000073 20080430 00073 NM 2008 4 30 SWAA082208 1 20080424 A 3350 3071BPEGPL LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008043000103 20080430 00103 NM 2008 4 30 CALA0800366 1 20080425 A 2560 65C16126 ATTACH FITTING BOEING 737 737524 1384721 NM GIRT BAR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 L-1 DOOR AFT GIRT BAR ATTACH MOUNT FOUND CORRODED AT CABIN FLOOR. REMOVED DAMAGED GIRT BAR ATTACH MOUNT IAW B737 SRM 51 -40-02. LOCATED AND DRILLED SERVICEABLE MOUNT FITTING IAW B737 SRM 51-40-02. INSTALLED L-1 GIRT BAR AFT FITTING IAW B7 37 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008043000106 20080430 00106 NM 2008 4 30 CALA0800369 1 20080425 A 5311 6546596 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 CABIN STATION 727B LT BETWEEN S8LT AND S9LT PASSENGER SERVICE UNIT (PSU) RAIL ATTACH BRACKET TO FRAME CRACKED. INSTALLE D REPAIR DOUBLERS PER EA 5310-04498 OPS 2. 2 L 7 2 4F RT A16WE 2008043000135 20080430 00135 NM 2008 4 30 SWAA082245 1 20080424 A 5755 654485113 HINGE BOEING 737 7373H4 1384600 NM NR 5 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED C2 CHECK, FOUND RIGHT WING NR 5 SPOILER HINGE AT OUTBOARD ACTUATOR BROKEN. REMOVED AND REPLACED SPOILE R PER MM. 2 L 7 2 4F RT A16WE 2008042500227 20080425 00227 NM 2008 4 25 SWAA082087 1 20080421 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042500229 20080425 00229 NM 2008 4 25 SWAA082090 1 20080421 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042500232 20080425 00232 NM 2008 4 25 SWAA082110 1 20080421 A 5523 65C34548 BEARING BOEING 737 7373H4 1384600 NM ELEVATOR TAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND RIGHT ELEVATOR TAB NR 1 HINGE BEARING CORRODED. REMOVED AND REPLACED BEARING PER BOEI NG DRAWING. 2 L 7 2 4F RT A16WE 2008042500236 20080425 00236 NM 2008 4 25 2008UALA02328 1 20080419 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 EMERGENGY LIGHT L313 AT DOOR IL HAS BROKEN WIRE. LIGHT ASSY LOCATED AT FWD UPPER CORNER OF DOOR FRAME VISIBLE FROM OUTS IDE WITH DOOR OPEN. FOUND BROKEN WIRE AT LIGHT ASSEMBLY. REPAIRED WIRE AND OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042500239 20080425 00239 NM 2008 4 25 2008UALA02331 1 20080419 A 3350 767 LAMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 209UA 30215 FOUND DOOR 3L EXTERIOR EMERGENCY LIGHT INOP. FOUND FAULTY LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042500246 20080425 00246 NM 2008 4 25 2008UALA02338 1 20080421 A 5314 KEELBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 716-726 WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 KEEL BEAM LT LOWER CHORD ANGLE UPPER SURFACE HAS 4 WORN FASTENER HOLES BS 716-726. MAJOR REPAIR ACCOMPLISHED: TRIMMED O UT DAMAGE. FABRICATED AND INSTALLED NESTED ANGLE AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042500249 20080425 00249 NM 2008 4 25 2008UALA02341 1 20080421 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 S8L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 FUSELAGE STRINGER 8L INTERCOSTAL WEB CRACKED AT FWD END TO FRAME BS 294.5. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND IN STALLED REPLACEMENT INTERCOSTAL WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042500251 20080425 00251 NM 2008 4 25 2008UALA02343 1 20080421 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294STR 12L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 FUSELAGE STRINGER 12L INTERCOSTAL CRACKED AT BS 294.5. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW INTERCOS TAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042500257 20080425 00257 NM 2008 4 25 2008UALA02348 1 20080421 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1500 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 AFT PIT LEFT SIDE FRAME HAS DENT AT BS 1500 ABOVE STR-26L. ACCOMPLISHED MAJOR REPAIR. CUT OUT DAMAGE, FABRICATED AND IN STALLED REPAIR PER SRM. THIS IS A CAT B REPAIR AND REQUIRES SUPPLEMENTAL INSPECTIONS STARTING AT 50,000 TOTAL FLT CYCL ES AND 12,000FC THERE AFTER. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042500258 20080425 00258 NM 2008 4 25 2008UALA02349 1 20080421 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR SLIDE OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 FOUND DOOR 3R WILL NOT ARM. ADJUSTED GIRT BAR, DOOR ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042500259 20080425 00259 NM 2008 4 25 2008UALA02350 1 20080421 A 3510 OXYGEN SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 CREW REPORTS CREW O2 LOW AT 1120 PSI. SERVICE CREW O2, NO LEAKS NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042500260 20080425 00260 NM 2008 4 25 2008UALA02351 1 20080422 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT LIGHT INOP, RIGHT SIDE CEILING BY LAV 101. REPLACED LAMP. OP CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500262 20080425 00262 NM 2008 4 25 2008UALA02353 1 20080422 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT LIGHT INOP AT DOOR 4 RIGHT AFT SILL. FOUND FAULTY BULB. REPLACED LAMP OP CHECKED NORMAL. AC OK FOR SERV ICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500265 20080425 00265 NM 2008 4 25 2008UALA02356 1 20080422 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT LIGHT INOP UPPER DECK ROW 17 CEILING. REPLACED LAMP. OP CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008043000165 20080430 00165 NM 2008 4 30 SWAA082286 1 20080427 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000172 20080430 00172 NM 2008 4 30 SWAA082263 1 20080427 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN WORN AT BS 881 TO BS 907, BETWEEN STR 2L AND STR 2R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008043000184 20080430 00184 NM 2008 4 30 CALA0800385 1 20080428 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 CABIN STATION 787 BETWEEN S8L AND S9L PASSENGER SERVICE UNIT RAIL ATTACH BRACKET FRAME CRACKED. REPAIRED FRAME AT STATI ON 787 BETWEEN S8L AND S9L PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008043000186 20080430 00186 NM 2008 4 30 CALA0800387 1 20080428 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 CABIN STATION 787 BETWEEN S8R AND S9R PASSENGER SERVICE UNIT RAIL ATTACH BRACKET TO FRAME CRACKED. INSTALLED REPAIR DOU BLERS PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008043000199 20080430 00199 NM 2008 4 30 SWAA082304 1 20080428 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 502D AND BS 514D, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000207 20080430 00207 NM 2008 4 30 SWAA082324 1 20080428 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008043000215 20080430 00215 NM 2008 4 30 SWAA082322 1 20080428 A 2121 215201 GASPER FAN BOEING 737 7377H4 1384404 NM CABIN MALFUNCTIONED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 786SW 29811 AT FL 330 A STRONG ELECTRICAL SMELL BEGAN IN CABIN AND THEN ODOR ENTERED FLIGHT DECK. TURNED OFF RT PACK, GASPER AND REC IRC SWITCHES, SMELL DISSIPATED. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 2008050100002 20080501 00002 EU 2008 5 1 08FDEA01567 1 20080425 A 5730 PANEL PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 RIGHT WING LEADING EDGE PANEL NR 612 BB INNER SKIN LAMINATE IS WORN/TORN AROUND THE FASTENERS. APPLIED ANTI-ERROSION TAP E 7 PRIMED IAW A300-600 SRM 51-75-10; PG 213. 2 L 7 2 4F RT A35EU 2008050100044 20080501 00044 EU 2008 5 1 08FDEA01561 1 20080425 A 5320 A53813303200 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND DURING ACCOMPLISHMENT OF WIC 6-5310-7-5001 PART 2 SEVERAL FASTENER WITH LARGER DIAMETER AS REQUIRED IAW SB A300-53 -6063. REPAIR PERFORMED BY REAM UP THE HOLES AND PERFORM REPAIR INSTRUCTION IAW SB A300-53-6048 AND -6063, APPROVED BY RAS 70504678/020/2008 ISS A AND EA 6-5310-117151. 2 L 7 2 4F RT A35EU 2008050100047 20080501 00047 EU 2008 5 1 08FDEA01564 1 20080425 A 5730 A5724661800200 PANEL AIRBUS 300 A300F4605R 3930327 EU RT WING ERODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 RIGHT WING LEADING EDGE PANEL NR 623 HB IS ERODED AT THE FWD EDGE. REPAIRED ERRODED AREAS BY APPLYING FIBREGLASS OVERLA YS IAW SRM 57-41-12 & 51-77-12. REAPPLIED FOIL IAW SRM 57-41-12; FIG 208. ALODINED IAW SRM 51-21-10. PRIMED IAW SRM 51- 23-10. RESTORED PAINT FINISH IAW SRM 51-75-10. INSTALLED PANEL ON THE AIRCRAFT IAW AMM 57-41-41. 2 L 7 2 4F RT A35EU 2008050100049 20080501 00049 EU 2008 5 1 08FDEA01566 1 20080425 A 5730 A5724660600300 PANEL AIRBUS A300 A300F4622R 3930360 EU RT WING WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 RIGHT WING LEADING EDGE PANEL NR 612 DB HAS LANDING AREA INTERIOR LAMINATE WORN/TORN. REPAIRED THE DAMAGED AREA BY APPL YING ALUMINUM FOIL IAW SRM 57-41-12. REMOVED & REATTACHED THE PANEL RESTRAINING CORDS REF AMM 57-41-41-4. PREPPED THE BO NDING SURFACE FOR THE FOIL APPLICATION REF SRM 57-41-12. ALODINED THE SURFACE REF SRM 51-21-10. PRIMED THE SURFACE REF S RM 51-23-10. 2 L 7 2 4F RT A35EU 2008050100051 20080501 00051 EU 2008 5 1 08FDEA01569 1 20080425 A 5347 A5361252410000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 MAIN CABIN, FR 15B TO FR 18, LBL 38, SEAT TRACK CORRODED. REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-21. RECEIVED NEW SE AT TRACK P/N A5361252410000, PO 617268.2. LOCATED; DRILLED & INSTALLED IAW SRM 51-40- 21 & 51-72-13. 2 L 7 2 4F RT A35EU 2008050100053 20080501 00053 EU 2008 5 1 08FDEA01571 1 20080425 A 5347 A5361251820000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 MAIN CABIN, FR14C TO FR18, LBL19, SEAT TRACK CORRODED. REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-21. RECEIVED NEW SEAT TRACK, LOCATED; DRILLED & INSTALLED IAW SRM 51-40- 21. 2 L 7 2 4F RT A35EU 2008050100058 20080501 00058 EU 2008 5 1 08FDEA01576 1 20080425 A 5730 A5724660200000 PANEL AIRBUS 300 A300F4605R 3930327 EU WING ERODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 PANEL 612 CB MATING SURFACES ARE ERODED. REPLACED ERRODED FOIL ON PANEL 612 CB MATING SURFACE IAW SRM 57-41-12. 2 L 7 2 4F RT A35EU 2008050100059 20080501 00059 EU 2008 5 1 08FDEA01577 1 20080425 A 5512 A5517706500151 PANEL AIRBUS 300 A300F4605R 3930327 EU FUSELAGE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 PANEL 344FT DELAMINATED 2 AREAS. REPAIRED PANEL 344 FT BY REMOVING THE DAMAGE; CLEANING; PREPARING THE AREA; POTTING AND APPLYING A FIBERGLASS WET LAY-UP REPAIR IAW ARM 51-77-12; PARA 2-A (2); FIG 202 AND SRM 51-77-10; PARA 3. RES TORED SURFACE REPAIR IAW SRM 51-77-12; PARA (2)-L AND SRM 51-75-10. 2 L 7 2 4F RT A35EU 20080520 NM 2008 5 20 UIEA200800175 1 20080505 A 5210 DOOR FRAME BOEING 747 7472D7B 1384803 NM L5 DOOR DEFORMED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK 5L DOOR FORWARD UPPER EDGE FRAME FOUND DEFORMED. PERFORMED DOOR EDGE RE-WORK AS PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 2008050100061 20080501 00061 WP 2008 5 1 08FDEA01579 1 20080425 A 5347 NCA60225 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 MAIN CABIN FLOOR SEAT TRACK SCALLOPS GOUGED AT STA 635 RBL 28. BLENDED GOUGES. GAP BETWEEN SCALLOPS IS 0.500 MAX ALLOW ED. REMAINING 0.515. OUT OF LIMITS IAW SRM 53-70-00; VOL I; PG 21. REMOVED & REINSTALLED (2) FLOOR PANELS IAW SRM 5 1-31-01; VOL II; PG 1. REMOVED DAMAGED TRACK SECTION & INSTALLED FABBED SECTION IAW SRM 51-31-01; VOL II. SPLICE HA T & PLATE IAW SRM 53-70-00; VOL I; PG 4 & DAC DWG 1428; REV I . ALODINED; PRIMED & TOP COATED IAW SRM 51-21-01; V OL II; PGS 1-24. 2 L 7 3 4F RT A22WE 2008050100062 20080501 00062 EU 2008 5 1 08FDEA01580 1 20080425 A 5512 A5517701800051 PANEL AIRBUS 300 A300F4605R 3930327 EU HORIZONTAL STAB DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 PANEL 334 AT IS DELAMINATED AS MARKED. REPAIRED PANEL 334AT BY REMOVING THE BRUSH SEAL; CONDUCTIVE PLATE & OUTER SKIN D AMAGE IAW SRM 55-13-13 & 51-77-10. APPLIED FIBERGLASS OVERLAY REPAIR TO THE OUTER SKIN; FABBED & BONDED NEW CONDUCTIVE PLATE & WASHERS IAW SRM 55-13-13. PAINTED PANEL IAW SRM 51-75-10. THE BRUSH SEAL REINSTALLED. 2 L 7 2 4F RT A35EU 2008050100064 20080501 00064 EU 2008 5 1 08FDEA01582 1 20080425 A 5512 PANEL AIRBUS 300 A300F4605R 3930327 EU HORIZONTAL STAB DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 PANEL 334 FT IS DELAMINATED. REPAIRED PANEL 334 FT BY DRILLING OUT DAMAGED AREA AND APPLYING ADHESIVE / FIBERGLASS OVERL AY REPAIR IAW SRM 51-77-12; PG 225 & 55-13-13 PG 215. APPLIED CONDUCTIVE COAT IAW SRM 51-23-20. PRIMED & PAINTED IAW AMM 51-23-10-0. 2 L 7 2 4F RT A35EU 2008050100065 20080501 00065 EU 2008 5 1 08FDEA01583 1 20080425 A 5512 PANEL AIRBUS 300 A300F4605R 3930327 EU HORIZONTAL STAB DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 PANEL 334 BT IS DELAMINATED ON THE UPPER AND LOWER SIDES. RECEIVED SERVICEABLE SLIDE TO BE INSTALLED ON W / C 68S1500CP; STEP 5B. 2 L 7 2 4F RT A35EU 2008050100067 20080501 00067 EU 2008 5 1 08FDEA01585 1 20080425 A 5512 A5517708500151 PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 PANEL 344 HT IS DELAMINATED. REPAIRED PANEL BY REMOVING THE DAMAGE ; CLEANING; PREPARING AREA; POTTING AND APPLYING A FIBERGLASS LAY-UP REPAIR IAW SRM 51-77-72; PARA 2-A; FIG 202 AND SRM 51-77-10; PARA 3. RESTORED SURFACE REPAIR IAW SRM 51-77-12; PARA 2-A (2)-L AND SRM 51-75-10. 2 L 7 2 4F RT A35EU 2008050100070 20080501 00070 NM 2008 5 1 08FDEA01588 1 20080425 A 5320 6517510119 WEB BOEING 727 7272S2F 1384O81 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 LT AIRSTAIR LOWER TORQUE BOX OUTER WEB CRACKED AT LIGHTING HOLE BS 1239. CUT OUT DAMAGE AREA DIM CUT OUT IAW SRM 51-10- 1 AND 51-40-2. FAB REPAIR PARTS IAW SRM 51-40-2 & 53-10-2. TREATED AND PRIMED IAW SRM 51-10-2 INSTALLED REPAIR PARTS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008050100072 20080501 00072 NM 2008 5 1 08FDEA01590 1 20080425 A 5755 6516216172 SPAR BOEING 727 7272S2F 1384O81 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 RT FALSE SPAR CRACKED JUST AFT OF NR 8 SPOILER FITTING. REPAIRED IAW DRAWING SR 27-57-038 REV C. 2 L 7 3 4F A3WE 2008050100074 20080501 00074 SO 2008 5 1 CHQA200800083 1 20080421 A 3350 RPS1B BATTERY EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHTS INOPERATIVE A CHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 259JQ 14734 738 145763 CAE311619 DURING INSPECTION, MAINTENANCE FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOPERATIVE. THE EMERGENCY LIGHT BATT ERY ABOVE ROW 15 WAS REPLACED AND THE EMERGENCY LIGHTING SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008050100079 20080501 00079 EU 2008 5 1 MALA080060 1 20080418 A 5311 FRAME SAAB SF340 340B 7860101 EU BS 288 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 454XJ 340B454 AT STA 288 ON RIGHT UPPER FLANGE ON THE BOTTOM FRAME CORROSION WAS FOUND. REPAIRED AREA IAW EOS53108. 2 L 7 2 4T RT A52EU 2008050100080 20080501 00080 NM 2008 5 1 KNNA20080009 1 20080417 A 5753 6546434139 SKIN BOEING 737 7372L9 1384497 NM TE FLAP DELAMINATED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 465AT 21528 DELAMINATION OF LEFT WING INBOARD AFT FLAP TRAILING EDGE WAS ORIGINALLY FOUND TO BE WITHIN LIMITS SO SPEED TAPE WAS APPL IED AS A TEMPORARY REPAIR AND THEN PLACED ON CARRY OVER. THE FLAP WAS MONITORED UNTIL THE CONDITION DETERIORATED BEYOND LIMITS SO IT WAS RECOMMENDED BY MAINTENANCE CONTROL TO REMOVED AND REPLACED IT. 2 L 7 2 4F RT A16WE 2008050100081 20080501 00081 SO 2008 5 1 SIMA200811903 1 20080424 A 5320 14521725015 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 630AE 145132 DURING MBV INSPECTION FOUND AFT SERVICE DOOR SILL TO BE CORRODED. REPAIRED AFT SILL BY INSTALLING A DOUBLER IAW ETA-EM- 5300-065. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008050100082 20080501 00082 SO 2008 5 1 SIMA200811904 1 20080424 A 5320 14521725613 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 630AE 145132 DURING MBV INSPECTION, FOUND FORWARD SERVICE DOOR SILL TO BE CORRODED. REMOVED AND REPLACED FORWARD SERVICE DOOR SILL I AW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008050100084 20080501 00084 SO 2008 5 1 SIMA200811902 1 20080424 A 2160 CONTROL VALVE EMB 145 EMB145LR 3260212 SO CABIN TEMP MALFUNCTIONED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 638AE 145172 ON FLIGHT 4331, CREW REPORTED SMOKE IN CABIN BEFORE BOARDING WITH APU RUNNING. AIRCRAFT REMOVED FROM SERVICE. FOUND MA IN DISTRIBUTION DUCT OVERHEATED. REMOVED AND REPLACED MAIN DISTRIBUTION DUCT, DUAL TEMP CONTROL VALVE, PACK OVER TEMP S WITCH IAW AMM 21-51-08. OPERATIONAL CHECK GOOD AND NR 8194, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008050100085 20080501 00085 EU 2008 5 1 MALA080061 1 20080425 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 402XJ 340B402 PWI TO REPAIR LT FUSELAGE DENT 12.5 INCH FWD OF PASSENGER ENTRANCE DOOR. INSTALLED DOUBLER/TRIPLER REPAIR TO DAMAGED AR E IAW EO S53009. FRAME STATIONS 236.5-248.5 AND STRINGERS 1532-1536. 2 L 7 2 4T RT A52EU 2008050100086 20080501 00086 EU 2008 5 1 NSVA2008021 1 20080427 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 370PX 340B300 DURING OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM ON A LINE CHECK, 3 EMERGENCY COVE LIGHTS WERE FOUND NOT ILLUMINATING. EMERGENCY LIGHT POWER SUPPLY 20LN WAS REPLACED AND SYSTEM TESTED SATISFACTORILY. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2008050200012 20080502 00012 NM 2008 5 2 UPS08552083 1 20080409 A 5320 STRAP BOEING 757 75724APF 1384969 NM BS1787-1806 S6R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 458UP 25479 INSPECTION TYPE:C2 CORROSION ON APU DOOR CUTOUT OUTBOARD STRAP. REMOVED, FABRICATED, INSTALLED STRAP. 2 L 7 2 4F RT A2NM 2008050200015 20080502 00015 WP 2008 5 2 UPS08852074 1 20080420 A 5712 RIB DOUG DC8 DC873F 302199F WP LWS 822 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING OUTBD LE UPPER RIB CRACKED JUST OUTBD OF ACCESS PNL 517B AT XFS 822.5. REPAIRED LT WING OUTB D LE UPPER RIB AT XFS 822.5 IAW SRM 57-02-00 FIG0 02 AND DWG 5769470. 2 L 7 4 4F RT 4A25 2008050200016 20080502 00016 WP 2008 5 2 UPS08852075 1 20080420 A 5712 576947037 RIB DOUG DC8 DC873F 302199F WP LWS 816 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING OUTBD LE UPPER RIB CRACKED JUST OUTBD OF ACCESS PNL 518A XFS816.0. REPAIRED LT WING OUTBD LE UPPER RIB AT XFS816.0 IAW SRM 57-02-00 FIG 0 02 AND DWG 5769470-37. 2 L 7 4 4F RT 4A25 2008050200017 20080502 00017 WP 2008 5 2 UPS08852076 1 20080421 A 5712 RIB DOUG DC8 DC873F 302199F WP LWS 386 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING CENTER LE UPPER RIB CRACKED XFS 386. REPAIRED LT WING CENTER LE RIB AT XFS 386 IAW SRM 57-02 -00 FIG 002 AND SRM 57-03-03-0 FIG 005. 2 L 7 4 4F RT 4A25 2008050200024 20080502 00024 NM 2008 5 2 UPS08M52082 1 20080321 A 2720 ABH7239503504 ARM DOUG MD11 MD11F 3023600 NM RUDDER PEDAL DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 256UP 48405 INSPECTION TYPE:2C 4 RUDDER PEDAL ARM ASSEMBLIES REQUIRE NDT FOR PREVIOUSLY DRILLED LOCK FASTENER HOLES. REMOVED LOCK F ASTENER, PERFORMED FP INSPECTION, NO CRACKS NOTED, APPLIED ALODINE TO HOLES, INSTALLED HLT334-6-22 FASTENERS AND HL386-6 COLLARS AND MARKED IAW UPS EO MD11-2720-28975-A AND SAA EA 011-2720-01-A0932 REV A. 2 L 7 3 4F RT A22WE 2008050200025 20080502 00025 NM 2008 5 2 UPS08M52084 1 20080204 A 5711 SPAR DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP INSPECTION TYPE:C LT WING FRONT SPAR ENCLOSURE APPROX STA XORS 514 UPPER SKIN FOUND CRACKED. CRACK AREA TRIM OFF PER EN 1007-08. HFEC CARRIED OUT IAW DAC NDT SPM R.13 PART06-10-01.001 FOUND NO CRACK EVIDENT. REPAIR ANGLES FAB USING 7075-0 -0.063" MAT`L PER SRM57-10-00 FIG 27V.1R.40 AND EN1007-08. FASTENER HOLES DRILLED ON REPAIR PARTS PER SRM 57-10-00 FIG 27 V.1R.40 AND EN1007-08. REPAIR PARTS PROTECTED PER SRM 51-21-01V.2R.40. OK TO INSTALL. 2 L 7 3 4F RT A22WE 2008050200029 20080502 00029 WP 2008 5 2 NWAA081779950 1 20080425 A 3397 CONNECTOR DOUG DC9 DC932 3022066 WP EMERGENCY LIGHTS LOOSE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9346 47376 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE LAST FOUR ROWS OF COACH SEATS CABIN HAD FAILED. MAINTENANCE RESEATED THE CONNECTOR FOR THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM. 2 L 7 2 4F A6WE 2008050200033 20080502 00033 NE 2008 5 2 USAA920080920 2 20080427 A 7532 AC69924 BLEED VALVE AIRBUS 320 A320231 3930325 EU IAE V2500 V2500A1 NE NR 1 ENGINE INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 637AW 51875 9302 99 FLT NR 455 PHX-SLC - ATB - ON CLIMB-OUT AT ABOUT 7500 FT, CREW REPORTED TWO AUDIBLE LOUD BOOMS FROM THE NR 1 ENGINE. NO ECAM WARNINGS CAME UP. REDUCED POWER TO IDLE, ALL PARAMETERS REMAINED NORMAL INCLUDING OIL PRESSURE AND TEMPERATURE. AIRCRAFT RETURNED TO PHX. MAINTENANCE REMOVED AND REPLACED THE LOWER RIGHT 7TH STAGE (7B) BLEED VALVE, NR 1 ELECTRONIC ENGINE CONTROL (EEC), AND SWAPPED N1 PROBE LEADS FROM TERMINALS 1 AND 2 TO TERMINALS 3 AND 4. ENGINE RUN OPERATIONAL CH ECK GOOD. 2 L 7 2 4F 4 F RT A28NM E311NE 2008050200034 20080502 00034 EU 2008 5 2 USAA920080921 1 20080425 A 2910 112441 HOSE AIRBUS 320 A320214 3930316 EU ZONE 400 RUPTURED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 103US 861 FLT NR 1910 CLT-LGA - DIV - CREW REPORTED GREEN HYDRAULIC LOW LEVEL LIGHT DURING CRUISE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO PHL. AIRCRAFT WAS TOWED TO GATE DUE TO LOSS OF NOSE WHEEL STEERING. MAINTENANCE REPLACED RUPTURED HYD RAULIC SENSE LINE, AND DUE TO FILTER DEBRIS, REPLACED HYDRAULIC PUMP AND ASSOCIATED FILTERS. 2 L 7 2 4F RT A28NM 2008050200036 20080502 00036 2008 5 2 HALA0800547 4 20080426 A 3461 FMC BOEING 767 76733A 1385209 NM RIGHT FAILED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 580HA 28140 ETOPS SIGNIFICANT SYSTEM, BTB, RT FMC FAIL, NO HISTORY FOUND ON FMS TIMED OUT RESELECT MESSAGE ON FMC CDU SCRATCH PAD RE FERENCE FIM 34-61-00, ALL STEPS COMPLIED WITH NO FAULTS NOTED. ALL STEPS SATISFACTORY BOTH FMC OPERATION SATISFACTORY. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008050200038 20080502 00038 2008 5 2 HALA0800546 4 20080424 A 3413 INDICATOR BOEING 767 767332 1382001 NM VERTICAL SPEED INOPERATIVE A HALA O OTHER P NO WARNING INDICATION CR CRUISE 1 WP 13 594HA 33423 ETOPS SIGNIFICANT SYSTEM, F/O'S VERTICAL SPEED INDICATOR INOP. RESET C/B. GND CHECK OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008050200039 20080502 00039 NM 2008 5 2 RYNA200800005 1 20080111 A 5330 SKIN BOEING 757 7572G5 1384912 NM BS 1692 DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 151GX 24451 LOWER FUSELAGE SKIN HAS A DENT AT BS 1692.5 BETWEEN STR 17L AND 18L. REPAIRED IAW EO C00-5-53-013-08. 2 L 7 2 4F RT A2NM 2008050200042 20080502 00042 NM 2008 5 2 RYNA200800008 1 20080112 A 5330 SKIN BOEING 757 7572G5 1384912 NM BS 1696 DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 151GX 24451 LOWER FUSELAGE SKIN HAS A DENT AT BS 1696 BETWEEN STR 17L AND 18L. REPAIRED IAW EO C00-5-53-013-08. 2 L 7 2 4F RT A2NM 2008050200050 20080502 00050 NM 2008 5 2 RYNA200800013 1 20080111 A 5330 SKIN BOEING 757 7572G5 1384912 NM BS 1700 DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 151GX 24451 UPPER FUSELAGE SKIN HAS A DENT AT BS 1700 BETWEEN STR 14L AND 15L. REPAIRED IAW EO C00-5-53-015-08. 2 L 7 2 4F RT A2NM 2008042500267 20080425 00267 NM 2008 4 25 2008UALA02358 1 20080422 A 3350 90085 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 LEFT WING EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP, MOST FWD TWO LIGHT ASSY'S. FOUND FAULTY POWER SUPPLY. REPLACED POWER SUPPLY OVERWING LIGHTS OPS. CK. NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500268 20080425 00268 NM 2008 4 25 2008UALA02359 1 20080421 A 2497 POWER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE POWER OUTLET FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 193UA 26890 LAPTOP POWER OUTLET INOPERATIVE AT 6D. CREW COMMENTS, OUTLET SMOKING WITH NEW POWER CABLE. SUSPECT FAULTY RECEPTACLE. REPLACED OUTLET & CHECKED WIRING OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500271 20080425 00271 NM 2008 4 25 2008UALA02362 1 20080421 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 EMERGENCY EXIT PATH LIGHT STRIP BROKEN BY LEFT MID GALLEY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042500272 20080425 00272 NM 2008 4 25 2008UALA02363 1 20080421 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 672UA 30027 EEL SEAT MOUNTED LIGHT INOP AT 3F. INSTALLED NEW EEL SEAT LIGHT AT 3F. OP CHKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042500274 20080425 00274 NM 2008 4 25 2008UALA02365 1 20080421 A 3397 80172424 FEEDER CABLE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 204UA 28713 SEAT 2F BOTH EEL LTS INOP. DURING TROUBLESHOOT, FOUND UNDER SEAT POWER CABLE LOOSE. SECURED THIS CABLE. OP CHK'D OKAY . 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042500279 20080425 00279 EU 2008 4 25 2008UALA02370 1 20080421 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 457UA 1146 SKIN IS WORN THROUGH AT FR 69 STRINGER 44 AND MEASURES .5 INCH WIDE BY 2 INCH LONG. SKIN WORN THROUGH TO FRAME AT FR70 STGR 44 DAMAGE MEASURES APPROX 6"X 4" FROM TAIL STRIKE: CUT DAMAGED SKIN FOR ACCES S TO FRAME 70 DAMAGE EVALUATION.BLEND ED DAMAGE ON FRAME. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042500281 20080425 00281 NM 2008 4 25 2008UALA02379 1 20080422 A 3350 30043231 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN CONTAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 EMERGENCY EXIT LIGHT AFT OF DOOR 2R HAS MOISTURE INSIDE THE LENS. SUSPECT IMPROPERLY INSTALLED. REMOVED MOISTURE OP CH ECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042500287 20080425 00287 NM 2008 4 25 2008UALA02385 1 20080422 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SEAT 21ABC LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 522UA 24931 EMERGENCY LIGHT STRIP AT SEAT 21ABC LOOSE. SECURED LIGHT STRIP 21 ABC. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042500298 20080425 00298 NM 2008 4 25 HALA0800542 1 20080423 A 5730 SKIN BOEING 717 717200 1383700 NM WING DENTED A HALA O OTHER O OTHER LD LANDING 1 WP 13 475HA 55121 UNDER SIDE OF WING PANEL P/N 5912161-4512 ABOVE NR 3 MLG TIRE AREA HAS DENT APPROX 1.5 INCH DIAMETER AND .25 DEEP. OK T O CONTINUE PER GMM43.1. OK TO CONTINUE PER HAL M105 FILE NR 475127 INSPECTION FIRST FLIGHT EACH DAY, TAP TEST MARKED BO UNDARY OF DENT ENSURE NO DELAMINATION BEYOND BOUNDARY. COMPLIED WITH HAL M105 FILE NR 475127, PERFORMED TAP TEST OF DEN T INSTALLED SILVER DOT. 2 L 7 2 4F TR A6WE 2008042500300 20080425 00300 NM 2008 4 25 2008UALA02387 1 20080422 A 5320 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1440-1460 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 CABIN FLOOR SUPPORT CORRODED AT FS 1440-1460 RBL 64-60. MAJOR REPAIR ACCOMPLISHED: REMOVED SUPPORT. FABRICATED AND INST ALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042500303 20080425 00303 NM 2008 4 25 2008UALA02390 1 20080422 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 775UA 26947 EMERGENCY LIGHTS ON SIDES OF SEATS 32G, 2F AND 9F ARE INOP. RELAMPED & REPLACED LIGHT ASSY AS NEEDED. OPS CK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042500306 20080425 00306 EU 2008 4 25 08FDEA01520 1 20080424 A 5210 D31023101 SLIDE AIRBUS 300 A300F4605R 3930327 EU L1 DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 L-1 DOOR SLIDE ASSY, UPPER EXTERNAL FRAME INSERTS ARE PULLED OUT OF THE BOX AT THE FWD END. NEW SERVICEABLE SLIDE RECEI VED INSTALLED ON WIC 68S5001CP. 2 L 7 2 4F RT A35EU 2008042500307 20080425 00307 NM 2008 4 25 DL757080631 1 20080424 A 5311 146N8711 FRAME BOEING 757 757232 1384965 NM BS 1640 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 646DL 24217 DURING HMV AT SAA, CORROSION WAS FOUND ON THE STA 1640 FRAME AT WL 210. THE CORRODED SECTION WAS REMOVED AND A REPAIR W AS INSTALLED PER BOEING DIRECTIONS. 2 L 7 2 4F RT A2NM 2008042500313 20080425 00313 NM 2008 4 25 SWAA082149 1 20080422 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 747 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008050200051 20080502 00051 NM 2008 5 2 RYNA200800012 1 20080111 A 5330 SKIN BOEING 757 7572G5 1384912 NM BS 1696 DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 151GX 24451 UPPER FUSELAGE SKIN HAS A DENT AT BS 1696 BETWEEN STR 14L AND 15L. REPAIRED IAW EO C00-5-53-015-08. 2 L 7 2 4F RT A2NM 2008050200052 20080502 00052 NM 2008 5 2 WRNA20080028 1 20080227 A 5311 FRAME BOEING 747 747230B 1384889 NM BS 2662 DAMAGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 512MC 21220 DURING B CHECK, FOUND MISSING FASTENER AND ELONGATED HOLE RIGHT SIDE OF FRAME AND INTERCOSTAL AT STATION 2662 W/L 305. FABRICATED REPAIR DOUBLER IAW SRM 51-40-03 FIGURE 01 AND INSTALLED DOUBLER IAW SRM 51-30-02. 2 L 7 4 4F RT A20WE 2008050200054 20080502 00054 NM 2008 5 2 WRNA20080029 1 20080324 A 5330 SKIN BOEING 747 747230B 1384889 NM BS 1810 DAMAGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 508MC 21644 DURING C CHECK, FOUND FUSELAGE SKIN DAMAGED AT STATION 1810 STRINGER 45R TO 46R. CUT OUT DAMAGE AND FABRICATED REPAIR F ILLER AND DOUBLER IAW SRM 53-30-03 FIGURE 17. INSTALLED REPAIR IAW SRM 53-30-03 FIGURE 17. 2 L 7 4 4F RT A20WE 2008050200056 20080502 00056 NM 2008 5 2 WRNA20080035 1 20080324 A 5347 SEAT TRACK BOEING 747 747230B 1384889 NM BS 1900 DAMAGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 508MC 21644 DURING C CHECK, WHILE ACCOMPLISHING CPCP TASK C53-210-01, SEAT TRACK AT STATION 1900 LBL 99 WAS FOUND DAMAGED. REMOVED DAMAGED SEAT TRACK FROM STATION 1890 - 1905 AT LBL 99. INSTALLED SEAT TRACK IAW SRM 53-10-01 FIGURE 1A. 2 L 7 4 4F RT A20WE 2008050200058 20080502 00058 NM 2008 5 2 WRNA20080032 1 20080324 A 5330 SKIN BOEING 747 747230B 1384889 NM BS 370 S14L DAMAGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 508MC 21644 DURING C CHECK, WHILE ACCOMPLISHING SSID F25-1, A CRACK WAS FOUND BY HFEC INSPECTION UNDER COUNTERSUNK HEAD AT STRINGER 14L STATION 370, CRACK EXTENDED 1/8 INCH AFT OF HOLE. REMOVED DAMAGED SECTION OF SKIN IAW SRM 53-30-03 FIG 17. FABRICA TED FILLER AND DOUBLER IAW SRM 53-30-03 AND INSTALLED REPAIR IAW 51-30-02, 53-30-02, 51-10-06, AND 53-30-03 FIG 17. 2 L 7 4 4F RT A20WE 2008050200059 20080502 00059 NM 2008 5 2 WRNA20080033 1 20080324 A 5347 SEAT TRACK BOEING 747 747230B 1384889 NM BS 778 CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 508MC 21644 DURING C CHECK, WHILE ACCOMPLISHING CPCP TASK C53-210-01, LEVEL LL CORROSION WAS FOUND AT SEAT TRACK SPLICE AT STATION 7 78 LBL 47. INSTALLED SEAT TRACK SPLICE AND ANGLES IAW SRM 53-10-05 FIGURE 1A DETAIL LLL AND SRM 51-30-02. 2 L 7 4 4F RT A20WE 2008050200060 20080502 00060 NM 2008 5 2 WRNA20080030 1 20080324 A 5330 SKIN BOEING 747 747230B 1384889 NM BS 1960 DAMAGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 508MC 21644 DURING C CHECK, WHILE ACCOMPLISHING CPCP TASK C53-100-01 LEVEL LL CORROSION WAS NOTED AT BUTT SPLICE, STATION 1960 STRIN GER 47R - 51R. REMOVED 11 3/4 INCH BY 2 INCH SECTION OF SKIN CORRODED OUT OF LIMIT IAW SRM 53-30-03. FABRICATED FILLER AND REPAIR DOUBLER IAW SRM 53-30-03 AND INSTALLED IAW SRM 53-30-03. 2 L 7 4 4F RT A20WE 2008042900011 20080429 00011 EA 2008 4 29 TRAX200800557 1 20080417 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 CARGO COMPT DOOR TRACK CROSSBEAM HAS CRACKED ATTACH FITTING AT AFT PRESSURE BULKHEAD. REMOVED AND REPLACE ATTACH FITTIN G PER SRM 51-42-20. 2 L 7 2 4F RT A21EA 2008043000013 20080430 00013 NM 2008 4 30 KCSA081226 1 20080424 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 FORWARD BILGE FUSELAGE FRAME UPPER CAP IS DAMAGED AT STA 700, RBL 80. 2 L 7 4 4F RT A20WE 2008043000014 20080430 00014 NM 2008 4 30 KCSA081227 1 20080424 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 FORWARD BILGE FUSELAGE FRAME UPPER CAP IS DAMAGED AT STA 760, RBL 80. 2 L 7 4 4F RT A20WE 2008043000015 20080430 00015 NM 2008 4 30 ASAA0892838 1 20080322 A 5314 149A76159 KEELBEAM BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 317AS 30856 MLG W/W KEEL BEAM SUPPORT PANEL MATING SURFACE CORRODED STA 686 RBL 8 TO LBL 8. REMOVED, DAMAGED SUPPORT FITTING, LOCAT ED, DRILLED AND INSTALLED A REPLACEMENT SUPPORT FITTING IAW B737 900 SRM 51 40 02 PG 6 7 AND SRM 51 40 05 FIG 2 PG 3. 2 L 7 4 4F RT A16WE 2008043000030 20080430 00030 NM 2008 4 30 KCSA081228 1 20080424 A 3350 LIGHT BOEING 747 747249F 1384849 NM EXTERIOR INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 706CK 21827 LEFT SIDE UPPER DECK EXTERIOR EMERGENCY SLIDE EXIT LIGHT INOP. 2 L 7 4 4F RT A20WE 2008043000032 20080430 00032 NM 2008 4 30 KCSA081230 1 20080424 A 5230 SKIN BOEING 747 747123 1384873 NM AFT CARGO DOOR DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 AFT CARGO DOOR SKIN EDGE DAMAGED AT BS 1830, STR 42R. 2 L 7 4 4F RT A20WE 2008043000035 20080430 00035 NM 2008 4 30 CALA0800356 1 20080404 A 5320 6516300 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 INSTALLED SRM REPAIR AT BS 178-188 RBL 24.67 FLOORBEAM WEB FOR ACCESS. REMOVED EXISTING WEB & STIFFENER, MODIFIED WEB & FABRICATED NEW STIFFENER & REPAIR PARTS FOR SRM REPAIR BS 178-188 RBL 24.67 FOR FLOORBEAM FOR ACCESS IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2008043000061 20080430 00061 NM 2008 4 30 SWAA082238 1 20080424 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008043000066 20080430 00066 NM 2008 4 30 SWAA082202 1 20080424 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 463WN 32467 DURING SCHEDULED HC2 CHECK, LEFT MID CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY P ACK PER MM. 2 L 7 2 4F RT A16WE 2008043000070 20080430 00070 NM 2008 4 30 SWAA082211 1 20080424 A 3397 51822 WIRE BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. FOUND BROKEN WIRE AT D2992. REPAIRED WIRE PER WDM. 2 L 7 2 4F RT A16WE 2008043000088 20080430 00088 NM 2008 4 30 SWAA082231 1 20080424 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000089 20080430 00089 NM 2008 4 30 SWAA082232 1 20080424 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000092 20080430 00092 2008 4 30 SWAA082221 4 20080424 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008043000112 20080430 00112 NM 2008 4 30 CALA0800375 1 20080408 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 STATION 867 LT SIDE BETWEEN S8LT AND S9LT AT AC BRACKET I/B FASTENER HOLE IS CRACKED. REMOVED A/C BRACKET IAW B737 SRM 51-40-02. MADE ID FOR REPAIR ANGLES "A" & "B" 7075-0 040 IAW EA5310-04498, HEAT TREATED ANGLES TO 7075T6 IAW BAC5602. ALODINED & PRIMED IAW B737 SRM 51-20-01, INSTALLED ANGLES & BRACKET IAW EA5310-04498. 2 L 7 2 4F RT A16WE 2008043000123 20080430 00123 NM 2008 4 30 SWAA082272 1 20080423 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 395, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000127 20080430 00127 NM 2008 4 30 SWAA082243 1 20080425 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 13L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000158 20080430 00158 NM 2008 4 30 SWAA082261 1 20080427 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000169 20080430 00169 NM 2008 4 30 SWAA082290 1 20080427 A 5311 6935350 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, RBL 16. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008043000170 20080430 00170 NM 2008 4 30 SWAA082291 1 20080427 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 27R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008043000193 20080430 00193 NM 2008 4 30 CALA0800394 1 20080426 A 7830 491B1330011 ATTACH FITTING BOEING 767 767224 1385170 NM THRUST REVERSER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 73152 30431 NUMBER 2 ENGINE LEFT C-DUCT FWD TORQUE BOX ATTACH WEB AT 11 O/CLOCK POSITION FOUND CRACKED. NUMBER 2 ENGINE LEFT C-DUCT FWD TORQUE BOX ATTACH WEB REPAIRED PER MRAS CMM78-32-02 REPAIR 24 FIG 602. 2 L 7 2 4F RT A1NM 2008043000212 20080430 00212 NM 2008 4 30 SWAA082314 1 20080428 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 820, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008050100001 20080501 00001 EU 2008 5 1 08FDEA01524 1 20080424 A 5320 A5341046200000 WEB AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 LEFT AIR CONDITION FAIRING SUPPORT WEB FOR FAIRING 143 FL; AFT WEB OUTER ATTACH POINT TO BODY IS CRACKED. REMOVED SUPPO RT AND WEB REF FEDEX A300-600 SRM 51-40-21. MATERIAL ID IS 2024-T3, 0.050 REF FEDEX A300-600 SRM 53-15-73. FORMED DO UBLER REF FEDEX A300-600 SRM 51-71-30; PG 202. ALODINED DOUBLER REF FEDEX A300-600 SRM 51-21-10. PRIMED AND PAINTED DO UBLER REF FEDEX A300-600 SRM 51-23-10. PART MARKED DOUBLER REF FEDEX A300-600 SRM 51-71-30. INSTALLED DOUBLER AND SUPP ORT WEB REF A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008050100009 20080501 00009 WP 2008 5 1 ARWA20080405 1 20080424 A 7830 WARNING LIGHT DOUG DC10 DC1030F 3023504 WP THRUST REVERSER FALSE ACTIVATION A ARWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 29 450ML 47831 DURING TAKEOFF ROLL ENGINE NR 3 REVERSER OPEN (REV OIL) LIGHT ON. ABORTED TAKEOFF, RETURNED TO THE RAMP 78-34-4-3. INS PECTED ENGINE THRUST REVERSER, NO DAMAGE NOTED. DEACTIVATED REVERSER AND LOCKED IN ACCORDANCE WITH MM 78-00-01; ENTERED ON DMI NR 21655 IN ACCORDANCE WITH MEL 78-1-1 CAT "C". COMPLIED WITH AOM RTO BRAKES COOLING PERIOD, PLACARD INSTALLED. CLEARED DMI # 21655; OPERATIONAL CHECK FOUND OK IN ACCORDANCE WITH MM 78-00-00. 2 L 7 3 4F RT A22WE 2008050500002 20080505 00002 NM 2008 5 5 SWAA082303 1 20080428 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 512D, STR 21R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008042500314 20080425 00314 NM 2008 4 25 SWAA082196 1 20080423 A 5311 6547959 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CORRODED AT LOWER INBOARD CORNER. REMOVED AND REPLACE D FRAME PER BOEING DRAWING AND ACO. 2 L 7 2 4F RT A16WE 2008042500315 20080425 00315 NM 2008 4 25 SWAA082179 1 20080423 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 423WN 29827 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 16 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008042500316 20080425 00316 2008 4 25 SWAA082158 4 20080423 A 2565 61621469 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR CANVASS FRAYED AND WORN. REMOVED AND REPLACED E VAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042500321 20080425 00321 NM 2008 4 25 HNAA0800139 1 20080421 A 2910 82960011001 LINE DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYS CHAFED A HNAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 07 940HA 156 DURING TAXI, NR 1 HYDRAULIC CONTENTS LEAKED, MAKING BRAKES UNUSABLE. INSP AIRCRAFT, FOUND HYDRAULIC FLUID LEAKING FROM NR 1 RUDDER FULL PRESSURE LINE. INSTALLED TFL, SERVICED HYDRAULICS, GROUND RAN AIRCRAFT, OPS CHECK AND LEAK CHECK GOOD. ASSIGNED 70 HOUR DMT. 2 H 7 2 4T RT A13NM 2008042500327 20080425 00327 EA 2008 4 25 HNAA0800140 1 20080422 A 3234 5352011 SELECTOR PANEL DHAV DHC8 DHC8311 1386006 EA MLG FALSE INDICATION A HNAA O OTHER N FALSE WARNING AP APPROACH 1 EA 07 330EN 15148 15148 274 AFTER GEAR WAS SELECTED DOWN, THE RIGHT MAIN INDICATION DID NOT LIGHT UP GREEN. THE ALTERNATE EXTENSION INDICATIONS ALL INDICATED GREEN AS NORMAL. THE FLIGHT LANDED SAFELY AND DID NOT DECLARE AN EMERGENCY BUT ISP TOWER SENT OUT EMERGENCY VEHICALS ANYWAY, INDICATING IT IS THEIR PROCEDURE TO TREAT THIS AS AN EMERGENCY. 2 H 7 2 4T RT A13NM 2008042500328 20080425 00328 NM 2008 4 25 SWAA082161 1 20080423 A 5322 6546536 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 559, STR 17R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008042500329 20080425 00329 NM 2008 4 25 SWAA082136 1 20080422 A 5315 6546812 FLOORBEAM BOEING 737 7375H4 138449D NM BS 944 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 944, RBL 3. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 2008042500331 20080425 00331 NM 2008 4 25 ASAA0892835 1 20080324 A 5321 147A581019 FLOORBOARD BOEING 737 737990 NM BS 887-907 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 317AS 30856 AFT CABIN FLOORBOARD STA 887 TO STA 907 RBL 47 TO RBL 67 IS DELAMINATED. PREPARED DAMAGED AREA APPLIED POTTING COMPOUND BMS 5 28 TYPE 19 AND 4 LAYERS BMS 9 3, FABRIC REPAIR PLY BONDED AREA IAW B737 900 SRM 53 00 50 REP 6 PGS 201 203. 2 L 7 4 4F RT A16WE 2008042800001 20080428 00001 EA 2008 4 28 A6WA200840303 1 20080408 A 5753 ANGLE CNDAIR CL600 CL6002B19 1900309 EA LT WING TE FLAP BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 LEFT WING OUTBOARD FLAP, INBOARD HINGE ARM, LEFT ANGLE IS BROKEN. (M) ANGLE FABRICATED IN S6144-13 IAW SRM 51-24-36 PR IMER AND PAINT APPLIED IAW SRM 51-25-01 AND INSTALLED IAW SRM 51-42-06. (A) 2 L 7 2 4F RT A21EA 2008042800005 20080428 00005 WP 2008 4 28 UPS08852049 1 20080413 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 BROKEN FITTING ON TOP OF KEEL BEAM INSIDE LT BELLY STRESS PABEL STA 7 00 LBL 2. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-1-8, 51-3-0, 51-1-24. 2 L 7 4 4F RT 4A25 2008042800008 20080428 00008 EA 2008 4 28 A6WA200840267 1 20080324 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 559-621 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 CORROSION FOUND IN CARGO FLOOR SUPPORT STRUCTURE RBL 45 WL 73.50 FS 559 PLUS 80 FS 621. (M) CORROSION REMOVED IAW SRM 51-21-06. 2 L 7 2 4F RT A21EA 2008042800010 20080428 00010 EA 2008 4 28 A6WA200840291 1 20080403 A 5344 HINGE CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 FOUND CARGO DOOR STEP PLATE HINGE CRACKED. REPLACED CARGO DOOR STEP PLATE HINGERS IAW SRM 51-42-06. . 2 L 7 2 4F RT A21EA 2008042800011 20080428 00011 EA 2008 4 28 A6WA200840277 1 20080219 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 438AW 7748 FLAP FAIL AT ZERO ON APPROACH, COMPLIED WITH REST PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4 FLAP SYSTEM RE SET OK. RESET NOTED BY MAINTENANCE. (M) 2 L 7 2 4F RT A21EA 2008042800013 20080428 00013 WP 2008 4 28 UPS08852051 1 20080408 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 AFT EXTERIOR FUSELAGE STA 1690, L34L, FUSE SKIN BULGED AND CRACKED. CUT OUT DAMAGE, FABBED AND INSTA LLED NEW DOUBLER IAW SRM 51-1-21D, 51 -1-8, 53-2-0 FIG 007, 51-1-26. 2 L 7 4 4F RT 4A25 2008042800014 20080428 00014 WP 2008 4 28 UPS08852052 1 20080413 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 FLOOR PANEL F30A CRACKED AT END. STOP DRILLED CRACK, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51- 1- 8, 53-2-3-FIG 10, 51-3-2, 51-1-26. 2 L 7 4 4F RT 4A25 2008042800016 20080428 00016 EA 2008 4 28 TRAX200800519 1 20080409 A 5511 RIB CNDAIR CL600 CL6002B19 1900309 EA STABILIZER DEBONDED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 AAR - 3016 - LEFT HAND STAB TIP I/B AFT SUPPORT RIB CRACKED. RIB FOUND NOT TO BE CRACKED, DISBONDED ONLY. REBONDED DIS BONDED AREAS BY USING EP50A IAW CRJ SRM 51-74-14. SUPPLEMENTAL SDR CLOSED 4/22/08. 2 L 7 2 4F RT A21EA 2008050500023 20080505 00023 NM 2008 5 5 SWAA082334 1 20080429 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND STRINGER 4R CRACKED AT BS 312. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008050500030 20080505 00030 WP 2008 5 5 08FDEA01621 1 20080426 A 5414 AUB710027 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 1 PYLON 437ER HAS DAMAGED FASTENER HOLES. FABBED DOUBLER TO REPAIR FASTENER HOLE DAMAGE REF DC/MD-10 SRM 54-00-01; VOL III. ALODINED & PRIMED DOUBLER REF DC/MD-10 SRM 51-21-01; VOL II. INSTALLED DOUBLER REF DC/MD-10 SRM 51-35- 01; VOL II. 2 L 7 3 4F RT A22WE 2008050500039 20080505 00039 NM 2008 5 5 SWAA082332 1 20080429 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 EEPLS LENS CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008050500042 20080505 00042 NM 2008 5 5 SWAA082348 1 20080501 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008050500044 20080505 00044 NM 2008 5 5 SWAA082351 1 20080501 A 5754 65C30462 HINGE FITTING BOEING 737 7373H4 1384600 NM KRUEGER FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND RT WING NR 4 KRUEGER FLAP INBOARD HINGE FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2008050500046 20080505 00046 NM 2008 5 5 SWAA082375 1 20080501 A 5315 6545410144 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 665, RBL 24.50. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2008050500050 20080505 00050 NM 2008 5 5 SWAA082377 1 20080501 A 5315 6545410144 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 667, LBL 24.75. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2008050500056 20080505 00056 NM 2008 5 5 SWAA082356 1 20080501 A 2761 654485113 ACTUATOR BOEING 737 7375H4 138449D NM NR 4 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND LEFT WING NR 4 SPOILER INBOARD ACTUATOR AFT ATTACH POINT BROKEN. REMOVED AND REPLACED ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2008050500058 20080505 00058 NM 2008 5 5 SWAA082359 1 20080501 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 963, STR 21L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008050500064 20080505 00064 NM 2008 5 5 SWAA082364 1 20080501 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, LBL 4 TO LBL 14, WL 152. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008050500065 20080505 00065 NM 2008 5 5 SWAA082370 1 20080501 A 5330 6545774 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 779 AND BS 799, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008050500077 20080505 00077 SO 2008 5 5 FDKA200804178 1 20080423 A 5210 SKIN EMB 145 EMB145LR 3260212 SO PAX DOOR DENTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 837MJ 145367 DENT ON BOTTOM RIGHT CABIN DOOR SKIN. MX REPAIRED DOOR. 2 L 7 2 4T RT T00011AT 2008050500081 20080505 00081 NM 2008 5 5 ZZDA2008093 1 20080423 A 2170 23078391 COALESCER BAG BOEING 717 717200 1383700 NM A/C BAY DIRTY A ZZDA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 37 891AT 55043 ELECTRIC ODOR DETECTED IN FORWARD GALLEY. ON FIRST ENTRY INTO AIRCRAFT, MORE OF A HEAT SMELL THAN AN ELECTRICAL SMELL. T/S REF FIM 21-22. NO ODORS NOTED, ALSO INSPECTED XM STATIONS, COFFEE MAKERS, ENGINE AND APU AREAS FOR LEAKS. NO DEFE CTS NOTES. REPLACED COALESCER BAGS REF 21-54. 2 L 7 2 4F TR A6WE 2008050500083 20080505 00083 NM 2008 5 5 HNAA0800143 1 20080424 A 3234 574205A SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM LANDING GEAR DEFECTIVE A HNAA K NONE J WARNING INDICATION CL CLIMB 1 EA 07 911HA 5425 5425 034 AFTER SELECTING GEAR HANDLE UP, GEAR DOWN LIGHTS ILLUMINATED FOR APPROXIMATELY 5 MINUTES PLUS GEAR HANDLE LIGHT. THEN H EARD A CLUNK IN NOSE WHEEL AREA AND GEAR RETRACTED NORMALLY. AFTER INSPECTION, REMOVED AND REPLACED LANDING GEAR SELECT OR VALVE PER W/C 32-30-41R. FUNCTIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 2008050500084 20080505 00084 WP 2008 5 5 08FDEA01639 1 20080428 A 5414 AUB7108180 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 3 PYLON PANEL 487 FL IS CHAFING AT THE INNER SURFACE. BLENDED OUT. ORIGINAL MATERIAL 0.071 IAW SRM 54-51-02; VOL II I. MATERIAL REMOVED 0.027. MATERIAL REMANING 0.044; AND FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01; VOL I; WTG T8225 P. REMOVED THE SEAL RETAINER TO F.O.M.IAW SRM 51-31-01; VOL II. FABRICATED A REPAIR DOUBLER IAW SRM 54-00-01; VOL I. ALODINED & PRIMED IAW SRM 51-21-01; PGS 21 & 34; VOL II. INSTALLED DOUBLER REPAIR IAW SRM 51-35-01; VOL II. INSTA LLED THE SEAL RETAINER IAW SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 2008050500085 20080505 00085 NM 2008 5 5 08FDEA01645 1 20080428 A 3210 NYG62085513 LANDING GEAR DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 595FE 48553 FOUND CTR LANDING GEAR SHOCK STRUT CYLINDER CRACK FROM TOP DOWN ABOUT 33 INCHES. REMOVED AND REPLACE CENTER MAIN LANDING GEAR AND PERFORMED MLG RETRACTION TEST. 2 L 7 3 4F RT A22WE 2008050500086 20080505 00086 WP 2008 5 5 08FDEA01647 1 20080428 A 5330 ACA31557 PLATE DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 FWD CARGO COMP BILGE AT BS 753, THE DOUBLER BETWEEN STRINGER 48R TO STRINGER 49R IS CORRODED. REMOVED THE SPLICE IN REF TO SRM 51-33-01. FOUND TO BE CRACKED & CORRODED OUT OF LIMITS IN REF TO SRM 53-00-01. FABRICATED A NEW ARC3155-7 SPLICE IN REF TO DWG ACA 3155. ALODINED & PRIMED IN REF TO SRM 51-21-01. TOP COATED IN RF TO SRM 51-21-01. INSTALLED SPLICE IN REF TO SRM 51-33-01. 2 L 7 3 4F RT A22WE 2008050500090 20080505 00090 SO 2008 5 5 FDKA200804180 1 20080427 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6067 CVG-TYS. EMERGENCY FLOOR PROXIMITY LIGHTS OUT BETWEEN ROW 3-7. MX TROUBLESHOT AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008050500092 20080505 00092 SO 2008 5 5 FDKA200804182 1 20080429 A 5320 14522461011 STRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 837MJ 145367 THE RIGHT STRAP AT Y=479 AND FRAME NR 20 IS CORRODED. THE DAMAGED STRAP HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008050500094 20080505 00094 SO 2008 5 5 FDKA200804183 1 20080430 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6006 ORF-JFK. RIGHT EMERGENCY LT ROW 12 INOP. MX RECONNECTED LOOSE CONNECTOR, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008050500097 20080505 00097 NM 2008 5 5 SWAA082367 1 20080501 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 724SW 27856 DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008050500107 20080505 00107 NM 2008 5 5 USAA920080929 1 20080422 A 5310 6547959U67 STRAP BOEING 737 73733A 1384673 NM DOOR FRAME CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON THE AFT CARGO DOOR CUT OUT FORWARD FRAME STRAP, BS 800, S25R, WL 157. REP LACED THE AFT CARGO DOOR CUT OUT FORWARD FRAME STRAP, BS 800, S25R, WL 157 IAW B737 SRM 51-40-05. 2 L 7 2 4F RT A16WE 2008050500108 20080505 00108 NM 2008 5 5 USAA920080930 1 20080422 A 5320 654585546 ANGLE BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON THE R2 DOOR CUT OUT LOWER SILL ANGLE, BS 967- BS 986.5, RBL 49, WL 208. R EPLACED THE R2 DOOR CUT OUT LOWER SILL ANGLE, BS 967- BS 986.5, RBL 49, WL 208 IAW B737 SRM 51-40-05. 2 L 7 2 4F RT A16WE 2008050500114 20080505 00114 NM 2008 5 5 USAA920080936 1 20080422 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CRACKED BULKHEAD WEB, BS 178, RBL 3, WL 207. REPAIRED BULKHEAD WEB, BS 178, RBL 3, WL 207 IAW B737 SRM 53-10-08 2R11. 2 L 7 2 4F RT A16WE 2008050500116 20080505 00116 SW 2008 5 5 N984ME9080 1 20080423 A 2150 30001 PULLEY BOLKMS 117 BK117C2 5626002 SW TMECA ARRIEL ARRIEL1E 60034 NE A/C BAY CHAFED E E3MA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 03 984ME 1446 9080 AIR CONDITIONING DRIVE PULLEY BOLTS SHEARED AND THE PULLEY DETACHED FROM THE DRIVE. IT LOOKS LIKE THE BOLTS LOST TORQUE SLIGHTLY, BOLT HEADS WERE SAFETIED, THE THE PULLEY WORKED THE THE BOLTS UNTIL THEY SHEARED. I HAVE OPERATED 8500 HOURS O N 5 DIFFERENT EC-145S WITH THIS PULLY SYSTEM WITHOUT ANY PROBLEMS. I HAVE CHECKED MY OTHER 5 EC-145 HELICOPTERS FOR AIR- CONDITIONG PULLY ATTACHMENT AND THEY ARE ALL PERFECT. THIS SEEMS TO BE AN ISOLATED INCIDENT. --- AFTER FURTHER INVESTIGA TION OF THE ATTACHING BOLTS, THE BOLT SHANKS THAT WERE STILL IN THE PULLEY WERE TIGHT HOWEVER FRETTING WAS FOUND ON THE PULLEY ATTACHING SURFACE. IT IS QUITE POSSIBLE THAT THE INSTALLER OF THIS STC (HELI-DYNE)INSTALLED THE WRONG LENGTH BOLT 1 G 7 2 3U 3 U H13EU E19EU 2008050500117 20080505 00117 EU 2008 5 5 USAA920080938 1 20080422 A 5347 D5311278220200 SEAT TRACK AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 188US 1724 PIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 760/FR 18 - BS 808/FR 20, -Y1292. REPLACED CA BIN SEAT TRACK, BS 760/FR 18 - BS 808/FR 20, -Y1292 IAW A321 SRM 53-21-15. 2 L 7 2 4F RT A28NM 2008050500123 20080505 00123 NM 2008 5 5 08FDEA01595 1 20080425 A 5330 65921444 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 LWR FUSELAGE STA 1125 6.5 INCHES RIGHT OF CENTER LINE SKIN HAS A PULLED THROUGH RIVET STR 29R. CUT-OUT DAMAGED AREA (DI MENSION 4" X 3") IAW SRM 51-10-1 & FABRICATED REPAIR DOUBLER & REPAIR FILLER IAW SRM 53-30-3 & 53-30-2 FIGURE 2, TREAT ED & PRIMED PARTS IAW SRM 51-10-2, INSTALLED REPAIR WASHERS & REPAIR PARTS IAW SRM 51-30-28, 53-30-3 & 51-30-2 SEALED RE PAIR IAW SRM 51-20-4. 2 L 7 3 4F A3WE 2008050500131 20080505 00131 NM 2008 5 5 08FDEA01605 1 20080425 A 5313 65168124 STRINGER BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 LOWER FUSELAGE AFT PIT CORROSION ON 29R STRINGER FROM STA 885-890. REMOVED CORROSION AT AFT PIT ON STIFFENER , ORIG MA T 0.063, MAT LOSS 0.003, MAT REMAINING 0.060", TREATED AND PRIMED IAW SRM 51-10-01, 53-10-02, 53-10-01. 2 L 7 3 4F A3WE 2008050500134 20080505 00134 NM 2008 5 5 08FDEA01608 1 20080425 A 5313 65168124 STRINGER BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 LWR FUSELAGE STR 29 R AT STA 990 CORROSION ON SPARE TIES, CLIPS, AND TOP OF STRINGER. REMOVED CORROSION FROM SHEAR TIE IAW SRM 51-10-6, ORIG. MAT. 0.063, MAT. LOSS 0.004, REMAINING MAT. 0.059 AND FOUND WITHIN LIMITS IAW SRM 53-10-2, 53-1 0-1, CLEANED AREA CLIPS AND STRINGER IAW SOPM 20-30-03 AND NO CORROSION FOUND IAW SRM 51-1-6.TREATED AND PRIMED AREA IAW SRM 51-10-2. 2 L 7 3 4F A3WE 2008050500135 20080505 00135 EU 2008 5 5 TRBA2008047 1 20080428 A 3240 BRAKE AEROSP ATR72 ATR72212 8680945 EU MLG WEAK A TRBA O OTHER O OTHER LD LANDING 1 SO 29 270AT 270 NO PEDAL BRAKE UPON LANDING EITHER SIDE. AWAITING AML PAGE FOR DETAILS. 2 H 7 2 4T RT A53EU 2008050500140 20080505 00140 NM 2008 5 5 08FDEA01613 1 20080428 A 5230 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 628FE 48447 MAIN DECK CARGO DOOR NR 4 LOWER JAMB SUPPORT FITTING 'B' HOLE FOUND CRACK AT 1 O'CLOCK POSITION. MAIN DECK CARGO DOOR N R 4 LOWER JAMB CRACKED SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100. 2 L 7 3 4F RT A22WE 2008050500145 20080505 00145 WP 2008 5 5 08FDEA01618 1 20080426 A 5730 ARC0264508 PANEL DOUG MD10 MD1010F 3022112 WP RT WING DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 RIGHT WING LOWER I/B T/E PANEL 641EB HAS SEVERAL DENTS. REPAIRED ( 3 EA ) DAMAGED AREAS BY FABRICATING & BONDING A COR ES; FILLERS & DOUBLERS IAW SRM 51-71-00 VOL II. 2 L 7 3 4F RT A22WE 2008050500149 20080505 00149 WP 2008 5 5 08FDEA01623 1 20080426 A 5720 AUB7108132 RETAINER DOUG MD10 MD1010F 3022112 WP NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 1 PYLON PANEL 437HL HAS A CRACKED SEAL RETAINER. REMOVED AND REPLACED THE SEAL RETAINER IAW SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2008050500153 20080505 00153 WP 2008 5 5 08FDEA01630 1 20080425 A 5347 NCA60223 SEAT TRACK DOUG MD10 MD1010F 3022112 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 MAIN CABIN SEAT TRACK IN BALLMAT AREA SCALLOPS BROKEN AND SEVERAL GOUGES AT STA 755 TO STA 763 LBL 9. DAMAGED SCALLOPS ON THE SEAT TRACK AT LBL 9 BS 755-763, FOUND TO BE OUT OF LIMITS REF SRM 53-70-00. REMOVED FLOOR PANELS TO GAIN ACCESS A T BS 615-890 LBL 9-28. REMOVED THE SEAT TRACK FROM BS 725-755 LBL 9. SPLICED A NEW SECTION AT BS 755 IAW SRM 53-70-00 V OL I FIG I SHEET I. 2 L 7 3 4F RT A22WE 2008050500154 20080505 00154 WP 2008 5 5 08FDEA01631 1 20080428 A 5347 AFA774010 SEAT TRACK DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE ON SEAT TRACK X -107 STA 1581 TO 1661 FOUND SEVERAL POINT OF CORROSION. REPAIRED FOR SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F A22WE 2008050500156 20080505 00156 EU 2008 5 5 08FDEA01601 1 20080425 A 5753 A5796001220000 FLAP AIRBUS 330 A300* EU ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 LEFT WING INBD FLAP HAS TWO DENTS LOCATED 55" AND 57 1/4 " FROM THE INBD ENDAND 7 3/4 " & 5" FROM THE T / E THAT HAVE BEEN FOUND OUT OF LIMITS ON N/R N00417. LABELED A & B ON N/R N00417. FABRICATED DOUBLER IAW SRM 57-50-00; FIG 205; PG 219. LOCATED & DRILLED IAW SRM 57-50-00. ALODINED IAW SRM 51-21-10; PRIMED & PAINTED IAW SRM 51-23-10. IN STALLED DOUBLER IAW SRM 57-50-00. 2 L 7 2 4F RT A26NM 2008050500157 20080505 00157 WP 2008 5 5 08FDEA01633 1 20080428 A 5310 AEA0115505 DOOR FRAME DOUG DC10 DC1010F 3022111 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1256 JAMB DOOR R3 FOUND CRACK 0.5" LONG ON THE WEB UPPER SIDE REPA IRED FOR SRM 53-50-00 FIG 19 VOL I. 2 L 7 3 4F A22WE 2008050500166 20080505 00166 NM 2008 5 5 08FDEA01644 1 20080428 A 5320 6517510119 WEB BOEING 727 7272S2F 1384O81 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 LT AIRSTAIR LWR TORQUEBOX OUTER WEB CRACKED AT LIGHTING HOLE BS 1329. TRIMMED OUT DAMAGED AREA IAW SRM 51-10-1, 51-40-2 FIG 1. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALL ED REPAIR PART IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008050500171 20080505 00171 EA 2008 5 5 MASA200800343 1 20080425 A 3260 TARGET CNDAIR CL600 CL6002B19 1900309 EA LT MLG OUT OF ADJUST A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 17275 7275 ASH FLT 2825 PHX-TUS - LT MLG DISAGREE WARNING MESSAGE AFTER TAKEOFF. DECLARED EMERGENCY. ADJUSTED LT MLG UPLOCK TARGE T. 2 L 7 2 4F RT A21EA 2008050500177 20080505 00177 EA 2008 5 5 MASA200800349 1 20080428 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 932LR 12474 15032 ASH FLT 2773 PHX-RNO - EMERGENCY FLOOR LIGHTS 15AC, 15DF AND ROW 15 EMERGENCY EXIT LIGHT SIGN INOP. CHANGED NR 5 BATTER Y. 2 L 7 2 4F RT A21EA 2008050500182 20080505 00182 EU 2008 5 5 MALA080062 1 20080429 A 5320 WEB SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 453XJ 340B453 FLOOR WEB AT STA 288 CHAFED FROM AIRSTAIR DOOR SLIDE. BLENDED OUT DAMAGE. FABRICATED AND INSTALLED DOUBLER. COMPLETED REPAIR IAW MAL EO NR S53362. 2 L 7 2 4T RT A52EU 2008050500183 20080505 00183 NM 2008 5 5 F3LA20800205 1 20080426 A 5210 72CF894500 CONTROL CABLE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE R1 DOOR RUPTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK, INSPECTION REPORTED THE R1 DOOR FLEXIBLE CONTROL CABLE FOR THE EMERGENCY DOOR SYSTEM ARM/DISARM HANDL E WAS RUPTURED. MAINTENANCE REMOVED AND REPLACED THE RUPTURED CABLE IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 52-11-22 -020 AND AMM 52-11-22-020-51. UPON COMPLETION OF THE INSTALLATION OF THE CABLE, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008050500184 20080505 00184 NE 2008 5 5 ASAA0852851 2 20080428 A 7261 OIL SYSTEM BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE LOW A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 557AS 35176 892792 OIL SERVICE NEEDED. SERVICED ENGINE OIL. OIL ADDED TO NR 1=4QTS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050500188 20080505 00188 SO 2008 5 5 CHQA200800088 1 20080428 A 2760 8005701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL SPOILER DIRTY A CHQA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 11 285SK 145435 CAE312124 FLIGHT 5809 CLE TO DCA - DURING TAKEOFF ROLL, THE FLIGHT CREW RECEIVED A MASTER WARNING FOR A SPOILER TAKEOFF CONFIGURAT ION MESSAGE ON THE EICAS. AT THAT TIME THE CREW DECIDED TO ABORT TAKEOFF AND RETURN TO THE GATE WITHOUT INCIDENT. MAIN TENANCE CHECKED ALL HYDRAULIC LEVELS, SPOILERS, AND CONDUCTED AN OPERATIONAL CHECK OF THE SPEED BRAKE WITH THROTTLES ADV ANCED WITH NO DEFECTS NOTED. MAINTENANCE THEN CLEANED ALL PROXIMITY SENSORS AND CONDUCTED ANOTHER OPERATIONAL CHECK IN ACCORDANCE WITH ERJ-145 MM 27-62-00 WITH NO DEFECTS NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008050500190 20080505 00190 SO 2008 5 5 CHQA200800089 1 20080428 A 2810 2810051102 VALVE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL RT WING LEAKING A CHQA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 11 373SK 17854 17854 145543 CAE311999 FLIGHT 5312 STL TO EWR - WHILE CLIMBING TO CRUISE ALTITUDE, A PASSENGER HAD NOTICED A STEADY STREAM OF FLUID TRAILING OF F OF THE RIGHT WING. AT THAT TIME THE FLIGHT ATTENDANT CONFIRMED THE STREAM AND NOTIFIED THE CREW OF THE SITUATION. TH E FLIGHT CREW THEN RAN THEIR QRH AND DECIDED TO RETURN TO FIELD WITHOUT INCIDENT. MAINTENANCE ARRIVED AT THE AIRCRAFT A ND FOUND THE RIGHT VENT VALVE LEAKING. MAINTENANCE REPLACED THE VENT VALVE AND CONDUCTED AN OPERATIONAL CHECK WITH NO D EFECTS NOTED. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008042800021 20080428 00021 NM 2008 4 28 ASAA0852821 1 20080419 A 3610 32144464 VALVE BOEING 737 737890 1384527 NM BLEED AIR SYS TRIPPED A ASAA K NONE O OTHER CL CLIMB 1 NM 02 579AS 34753 1766 35187 RIGHTHAND ENGINE BLEED TRIPPED DURING CLIMB AT 2000 MSL. REPLACED HIGH STAGE VALVE. 2 L 7 2 4F RT A16WE 2008042400137 20080424 00137 NM 2008 4 24 08FDEA01489 1 20080423 A 5322 651593240 SHEAR TIE BOEING 727 727232 1384082 NM CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 FWD PIT SHEAR TIE STA 520 BETWEEN STR 28L-28R CORRODED. REMOVED FASTENER'S TO ACCESS CORROSION IN REF TO SRM 51-30-2 PG 2. REMOVED CORROSION ON FWD SIDE OF SHEAR TIE BS 520 STR 28L-28R IN REF TO SRM 53-10-1. CHECK SHEAR TIE FOR MAT'L L OSS ORIGINAL THICKNESS .042 INCH. REMOVED .003 INCH, REMAINING MAT'L .039 INCH. PER ITEM 3 MAT'L LOSS IS LESS THAN 109 .3 IS WITHIN LIMITS REF SRM 53-10-1 FIG 1. TREATED AND PRIMED SHEAR TIE IN REF TO SRM 51-10-2 PG 7. PAINTED SHEAR TIE IN REF TO M/M 51-20-151-07. REINSTALLED FASTENERS IN REF TO SRM 51-30-2 PG 2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008042400166 20080424 00166 WP 2008 4 24 08FDEA01477 1 20080423 A 5311 ADA01111 FRAME DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 68059 46907 DURING MODIFICATION IN CENTER ACCESSORY COMPARTMENT AT STA 1099 FROM LONGERON 49 TO LONGERON 48 RT SIDE FOUND LIGHT CORR OSION AND CRACK LONG 0.5" ON CAP FRAME. REMOVED CORROSION FOR SRM 51-21-01 VOL II AND PERFORMED FRAME CAP REPAIR FOR SR M 53-30-00 FIG 8 VOL I. 2 L 7 3 4F A22WE 2008042400168 20080424 00168 NM 2008 4 24 08FDEA01479 1 20080423 A 5414 311N51932 SKIN BOEING 757 75727B 1384921 NM ZONE 400 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 PYLON NUMBER ONE RIGHT FORWARD SKIN FOUND DENT. EVALUATE AND RECTIFY. REPLACED PYLON NUMBER ONE RIGHT FORWARD SKIN IN ACCORDANCE WITH B757- 200, SRM 51-10-02 AND BOEING DRAWING NUMBER 311N5002. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GM M 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008042400169 20080424 00169 NM 2008 4 24 08FDEA01480 1 20080423 A 5320 655615023 INTERCOSTAL BOEING 727 727232 1384082 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 MAIN DECK 1R DR CROSS BEAM, INTERCOSTAL I/B FLANGE IS CRACKED AT 4TH BEAM FROM BOTTOM, 13 INCHES FROM FWD END. REMOVED OLD INTERCOSTAL 4TH FROM BOTTOM 13 INCHES FROM FWD END. HAD SHOP FABRICATE N00557. DRILLED NEW INTERCOSTAL, INSTALLED INTERCOSTAL TREATED AND PRIMED AN PAINTED, EXTERIOR FASTENERS INSTALLED UPPER HINGE COVER PLATE. 2 L 7 3 4F A3WE 2008042400172 20080424 00172 2008 4 24 SWIA200819492 2 20080420 A 7320 FMU CNDAIR CL600 CL6002C10 1390015 EA RT ENGINE LEAKING A SWIA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 NM 07 760SK 10223 FLT 6617 - RIGHT ENGINE WOULD NOT MAKE POWER. REPLACED RIGHT FMU PER RJ 200 MM 73-21-03, P/N 8061-926, S/N OFF WYGB1135 . 2 L 7 2 4F RT A21EA 2008042400179 20080424 00179 2008 4 24 SWIA200819500 3 20080411 A 6110 O-RING EMB 120 EMB120ER 3260203 SO PROPELLER UNKNOWN A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 236SW 120312 FLT 5747 - THE RIGHT PROPELLER NP EXCEEDED 100 PERCENT. REPLACED RIGHT PROP TRANSFER TUBE O-RINGS. OPS CHECKS GOOD PER AMM 61-00-00. 2 L 7 2 4T RT A31SO 2008042400194 20080424 00194 NM 2008 4 24 08FDEA01483 1 20080423 A 5414 SKIN BOEING 757 75727B 1384921 NM CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 CRACK ON INNER PERFORATED SKIN OF OUTER DUCT ASSEMBLY AT THREE O'CLOCK SIDE STRUT LOCATION. TO EVALUATE AND RECTIFY. R EPAIR CRACK ON INNER PERFORATED SKIN OF OUTER DUCT ASSEMBLY AT THREE O'CLOCK SIDE STRUT LOCATION. A NEW REPAIR DOUBLER WAS FABRICATED AND INSTALLED IN ACCORDANCE WITH THE TECHNICAL VARIANCE (ROLLS ROYCE) APPROVAL EASA DOA NR EASA 215.035. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-02-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008042500001 20080425 00001 2008 4 25 CLCA0408 4 20080406 A 3442 6225127001 ANTENNA DOUG DC10 DC1030F 3023504 WP GE CF6 CF6* 30020 GL WX RADAR SYS SEIZED A CLCA J A DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 SO 29 614GC 46931 BOTH WEATHER RADAR WILL NOT SWEEP. 2 L 7 3 4F 4 F RT A22WE E23EA 2008042500005 20080425 00005 EA 2008 4 25 TRAX200800529 1 20080410 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 AAR - CLIP AT FS 484 RBL 27 CRACKED. 2 L 7 2 4F RT A21EA 2008042500010 20080425 00010 NM 2008 4 25 AMTA200800244 1 20080329 A 2560 BATTERY PACK BOEING 737 73783N 13844HI NM CFMINT CFM56 CFM567B27 13046 NE FLASHLIGHT INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 323TZ 30033 EMERGENCY FLASH LIGHT AT L2 DOOR IB RED LIGHT IS NOT FLASHING. REMOVED AND REPLACED POWER SUPPLY PACK, SECURED AND OPS CHECK OK. (K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2008042500013 20080425 00013 2008 4 25 AMTA200800246 4 20080329 A 3460 1762000101 FMC BOEING 737 73783N 13844HI NM CFMINT CFM56 CFM567B27 13046 NE RT UNSERVICEABLE A AMTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 314TZ 18200 57 30640 SINGLE FMC FAILURE. REMOVED AND REPLACED FMCS COMPUTER IAW 34-61-02-4. OPS NORMAL. (K) 2 L 7 2 4F 4 F RT A16WE E00055EN 2008042500026 20080425 00026 NM 2008 4 25 ASAA0852816 1 20080413 A 2150 CONTROLLER BOEING 737 737890 1384527 NM A/C BAY MALFUNCTIONED A ASAA K NONE N FALSE WARNING CL CLIMB 1 NM 02 559AS 35178 LEFTHAND AIRCON PACK ANNUNCIATION DURING CLIMB. COULD NOT RESET. LIGHT DID GO OUT DURING DESCENT BUT CAME BACK ON DURI NG LANDING. PERFORMED FIM 21 53 TASK 809 AND TEMPERATURE CONTROL RESET OK THEN PERFORMED ETOPS VERIFICATION FLIGHT. 2 L 7 2 4F RT A16WE 2008042500033 20080425 00033 EA 2008 4 25 TRAX200800501 1 20080408 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 AAR - 2123 - UPPER INTERCOSTAL FRAME (JUST FWD OF FS 280.0) IS CRACKED AT CUTOUT FOR ESCAPE HATCH LEFT AFT HINGE POINT. ACCESSED STIFFENER ATTACHED TO UPPER INTERCOSTAL FRAME FWD OF FS 28 AT LOCATION OF EDGE DAMAGE IN CUT-OUT OF FRAME FOR ESCAPE HATCH LEFT HINGE POINT. VISUAL INSPECTION FOUND NO CRACK. FOUND SMALL AREA OF EDGE DAMAGE, BLENDED A MAXIMUM OF .003". FOUND TO BE WITHIN SERVICEABLE LIMITS IAW CRJ 200 SRM 53-00-00 PAGE 102 FIG 101. REQ NDT C/W HFEC OF BLENDED A REA IAW CRJ 200 NDTM 51-20-06: NO DEFECTS NOTED. REINSTALLED FRAME STIFFENER IAW CRJ SRM 51-42-06. SUPPLEMENTAL SDR C LOSED 4/17/08. 2 L 7 2 4F RT A21EA 2008042500041 20080425 00041 SO 2008 4 25 C2XA08IA112 1 20080416 A 3230 355022002MOD4 ELECTRONIC UNIT EMB 145 EMB145LR 3260212 SO LANDING GEAR INOPERATIVE A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 13956 23004 2908 145078 IAH - FLIGHT 2037, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LAN DED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LGEU (LANDING GEAR ELECTRONICS UNIT), OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008042500043 20080425 00043 SO 2008 4 25 FDKA200804162 1 20080412 A 2612 FIRE WARNING EMB 145 EMB145LR 3260212 SO LAVATORY MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 844MJ 145481 FDM 5964 BWI-IAD (1537 PHX LCL). LAVATORY FIRE WARNING IN-FLIGHT WITH THE WARNING EXTINGUISHING AFTER A PERIOD OF TIME. THE CREW REPORTED, INSPECTED THE LAVATORY AREA FOR SIGNS OF FIRE OR SMOKE WITH NONE NOTED. MX COULD NOT DUPLICATE, NO DEFECTS NOTED, OPS NORMAL. 2 L 7 2 4T RT T00011AT 2008042500046 20080425 00046 SO 2008 4 25 FDKA200804165 1 20080413 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DISCONNECTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 FDM FLT 5996 MCO-LIT (0735 PHX LCL). OVERHEAD EMERGENCY LIGHT ROW 12 INOP. MX RECONNECTED CONNECTOR, OPS GOOD. 2 L 7 2 4T RT T00011AT 2008042500082 20080425 00082 EA 2008 4 25 TRAX200800548 1 20080416 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 LEFT CABIN FLOOR SEAT RAIL STARTING AT FS 379.00 HAS CORROSION DAMAGE. 2 L 7 2 4F RT A21EA 2008042500089 20080425 00089 EA 2008 4 25 TRAX200800556 1 20080417 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 FS 280 CLIP CRACKED AT LBL 9.0 OUTBOARD. 2 L 7 2 4F RT A21EA 2008042500098 20080425 00098 SO 2008 4 25 C2XA08IA113 1 20080417 A 3260 8005701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO LT MLG INOPERATIVE A C2XA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SW 27 13956 145078 IAH - FLIGHT 2264, AFTER LANDING THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS. MAINTENANCE REMOVED AND REPLACED THE LEFT SHOCK ABSORBER PROXIMITY SENSOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPR OVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008042500120 20080425 00120 NM 2008 4 25 CALA0800342 1 20080419 A 5320 141A5410U23 INTERCOSTAL BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24706 28767 PAX CABIN FLOOR STRUCTURE SUPPORT HAS CRACKED INTERCOSTAL BETWEEN STA 344 AND STA 360 AT BL 0. REMOVED AND REPLACED INT ERCOSTAL IN REF TO SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008042500121 20080425 00121 NM 2008 4 25 CALA0800343 1 20080418 A 5315 65C33947 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 AFT CABIN STATION 927 BL 0, CORROSION AT CLIP NUT HOLE. BLENDED CORROSION, DAMAGE FOUND TO BE OUT OF LIMITS PER 737-500 SRM 53-60-51 FIG 101. REPAIRED FLOORBEAM AT BS 927 BL-0 PER 737-500 SRM REFS, 53-60-51 FIG 201 REPAIR 3, AND 51-70-11 FIG 1. 2 L 7 2 4F RT A16WE 2008042500148 20080425 00148 EA 2008 4 25 TRAX200800547 1 20080416 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 RIGHT CABIN FLOOR SEAT RAIL STARTING AT FS 379.00 HAS CORROSION DAMAGE. JOB COMPLETE. BLENDED AREAS OF CORROSION START ING AT FS 379.00 TO WITHIN LIMITS & ALODINED BLENDED AREAS PER CRJ 200 SRM 53-21-49SP 7025126 04/18/2008. SUPPLEMENTA L SDR CLOSED 4/21/08. 2 L 7 2 4F RT A21EA 2008042500175 20080425 00175 NM 2008 4 25 2008UALA02321 1 20080419 A 2611 SMOKE DETECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LAVATORY FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 849UA 1649 LAVATORY DET FAULT DISPLAYED ON UPPER ECAM SCREEN. RESET SCDU CHANNEL AND SYSTEM OPS NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042500194 20080425 00194 EU 2008 4 25 TRAX200800561 1 20080418 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN ILLUMINATED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 AFTER STARTING ENGINE NR 1 EMERGENCY LIGHTS ILLUMINATED FROM ROW 8 TO 17 TURNED EMERGENCY EXIT SWITCH TO DISARM AND LIGH TS WENT OUT. 2 H 7 2 4T RT 2008042500204 20080425 00204 NM 2008 4 25 SWAA082074 1 20080420 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 445, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008042500228 20080425 00228 NM 2008 4 25 SWAA082088 1 20080421 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042500237 20080425 00237 NM 2008 4 25 2008UALA02329 1 20080419 A 2721 TRIM SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RUDDER INOPERATIVE A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 652UA 25390 LEFT RUDDER TRIM INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042500247 20080425 00247 NM 2008 4 25 2008UALA02339 1 20080421 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S15L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 FUSELAGE STRINGER 15L SPLICE CHANNEL CRACKED AT LOWER FLANGE BS 360. MAJOR REPAIR ACCOMPLISHED, REPLACED SPLICE CHANNEL . 2 L 7 2 4F 4 F RT A16WE E2GL 2008042500277 20080425 00277 NM 2008 4 25 2008UALA02368 1 20080422 A 5330 65B23791 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 2210 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 70528 24380 DAMAGE FOUND RT BS 2210 WL 200 FUSELAGE. SCRATCH MARK WITH CRACKED 3.5 INCH BY 3.5 INCH. SUSPECT GROUND EQUIPMENT DAMA GE. DAMAGED AREA REPAIRED AS EVA-71460B AND INSPECTION CHECKED SATISFACTORY. ACFT OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008050500197 20080505 00197 WP 2008 5 5 IXXA08SMN105S 1 20080314 A 5320 FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FORWARD FITTING CRACKED AT STATION 717.000 LEFT BOTTOM L INE 22". REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 S RM 51-3-1, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008043000166 20080430 00166 NM 2008 4 30 SWAA082287 1 20080427 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000180 20080430 00180 NM 2008 4 30 ASAA0852850 1 20080426 A 2160 WARNING SYSTEM BOEING 737 737890 1384527 NM COCKPIT MALFUNCTIONED A ASAA K NONE N FALSE WARNING CL CLIMB 1 NM 02 579AS 35187 LEFTHAND AIR CONDITIONING PACK ANNUNCIATED DURING CLIMB WITH A TRIM AIR CHECK VALVE FAULT INDICATION. RESET FAULT. 2 L 7 2 4F RT A16WE 2008043000191 20080430 00191 NM 2008 4 30 CALA0800392 1 20080428 A 3350 CONTACT BOEING 767 767224 1385170 NM CABIN DIRTY A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 73152 30431 DOOR 2 LEFT EXTERNAL EMERGENCY EGRESS LIGHT INOP. CLEANED CONTACT AND RELAMPED. TEST SYS PER AMM 33-51-00 P.501. 2 L 7 2 4F RT A1NM 2008043000214 20080430 00214 2008 4 30 SWAA082316 4 20080428 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 731SA 27863 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008050100003 20080501 00003 NM 2008 5 1 2008UALA02420 1 20080424 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 986 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 AFT FLOORBEAM CORRODED AT FLOOR BOARD HOLES STA 986.5 RBL 20-32 UPPER AND LOWER SURFACE. MAJOR REPAIR ACCOMPLISHED: FAB RICATED & INSTALLED FLOORBEAM UPPER TEE CAP SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050100004 20080501 00004 NM 2008 5 1 2008UALA02421 1 20080424 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 947-986 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 AFT GALLEY DOOR INNER CREASE BEAM UPPER SURFACE CORRODED AT STA 947-986. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050100005 20080501 00005 NE 2008 5 1 2008UALA02428 2 20080424 A 7261 FILTER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 ENGINE WARNING LIGHT A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 675UA 63035 21407 29243 724383 NR 2 ENG OIL FILTER STATUS MSG DISPLAYED. DID NOT ERASE. OIL TEMP ABOVE 35C PER CREW. RTN BLKS TO CHECK ALL 6 CHIP DE TECTORS AND MAIN OIL FILTER. CHECKED NR 2 ENGINE MAIN CHIP DETECTOR - FOUND OK. REPLACED MAIN OIL FILTER AND DELTA-P SWI TCH. 2 L 7 2 4F 4 F RT A1NM E24NE 2008050100011 20080501 00011 EU 2008 5 1 08FDEA01628 1 20080424 A 5753 A5796000001562 SKIN AIRBUS 300 A300F4605R 3930327 EU RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 RT WING INBD FLAP LWR SKIN HAS A NUMBER OF DENTS. MEASURED DEEPEST DENT TO BE D= .028 INCH DEEP AND X= .500" WIDE. FOU ND TO BE WITHIN LIMITS PER SRM 57-50-00 PG 101 DEPTH GAUGE NR T8492F. GOUGE BLENDED ORIG MAT .031" REMAINING .021, REM OVED .010" FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00 PG 107 GAUGE NR T8492F. FABBED AND INSTALLED DOUBLER IAW SRM 57-5 0-00. ALODINED .IAW SRM 51-21-10. PRIMED AND PAINTED IAW SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008050100089 20080501 00089 NM 2008 5 1 NSVA2008022 1 20080425 A 3150 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM TRIM FALSE ACTIVATION A NSVA O OTHER N FALSE WARNING CL CLIMB 1 EA 27 203WQ 4203 AFTER FLAPS RETRACTION ON TAKEOFF WITH NO AUTOPILOT. THE PITCH TRIM ANNUNCIATOR ILLUMINATED, THEN AUTO TRIM FAIL APPEAR ED ON PFD AND TRIM DEFLECTED TO FULL NOSE UP POSITION INDICATING FULL "NU" COULD NOT MOVE TRIM FROM THAT POSITION. PERF ORMED SYSTEM RESET PROCEDURE IAW AMM 45-00-27, FAULTS CLEARED. PERFORMED SYSTEM OPERATIONAL CHECK IAW AMM 27-30-00, NO FAULTS NOTED. AIRCRAFT OK FOR SERVICE. 2 H 7 2 4T RT A13NM 2008050100090 20080501 00090 NM 2008 5 1 2008UALA02418 1 20080425 A 3150 WARNING LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ILLUMINATED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 341UA 24245 724415 ABORTED TAKEOFF AT 100 KTS DUE TO A FUEL FILTER BYPASS LIGHT ON NR 2 ENGINE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050100091 20080501 00091 EU 2008 5 1 2008UALA02419 1 20080425 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 457UA 1146 SKIN WORN THROUGH TO FRAME AT FR 70 STGR 44 DAMAGE MEASURES APPROX 6 INCH BY 4 INCH FROM TAIL STRIKE. SKIN WORN THROUGH TO FRAME AT FR70 STGR 44 DAMAGE MEASURES APPROX 6"X 4" FROM TAIL STRIKE BY- 254125 :CUT DAMAGED SKIN FOR ACCES S TO FRA ME 70 DAMAGE EVALUATION.BLENDED DAMAGE ON FRAME. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050100092 20080501 00092 NM 2008 5 1 2008UALA02422 1 20080424 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1340 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 AFT PIT FUSELAGE FRAME AT STA 1340 BETWEEN STRINGERS 25R AND 26R DENTED. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR IAW SRM 53-00-07 RPR 5. PER SRM 53-00-07 RP R 5 TABLE II THIS RPR REQUIRES SUPPLEMENTAL INSPECTIONS STARTING AT 50,000 TOTAL FLIGHT CYCLES AND 12,000 FC THERE AFTER THIS IS A CAT B RPR. INSPECTIONS ARE BOTH VISUAL AND NDT. 2 L 7 2 4F 4 F RT A2NM E17NE 2008050100093 20080501 00093 NM 2008 5 1 2008UALA02423 1 20080424 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1580 GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 AFT PIT LEFT SIDE FRAME HAS GOUGE AT BS 1580 BTWN STRS 27L AND 26L. CUT OUT DAMAGE FABRICATED AND INSTALLED REPAIR IAW SRM 53-00-07 RPR 5. PER SRM 53-00-07 RP R 5 TABLE II THIS RPR REQUIRES SUPPLEMENTAL INSPECTIONS STARTING AT 50,000 TOTAL FLIGHT CYCLES AND 12,000 FC THERE AFTER THIS IS A CAT B RPR. INSPECTIONS ARE BOTH VISUAL AND NDT. 2 L 7 2 4F 4 F RT A2NM E17NE 2008050100097 20080501 00097 NM 2008 5 1 2008UALA02429 1 20080425 A 3520 OXYGEN MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SEAT 10DEF UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 852UA 1671 O2 MASKS AT SEAT 10DEF WILL NOT STOW. DUE TO REPEAT REPACKINGS, REPLACED THE COMPARTMENT WITH REPACKED O2 MASKS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042500280 20080425 00280 NM 2008 4 25 2008UALA02378 1 20080422 A 3350 LENS BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 EMERGENCY EXIT LIGHT AFT OF DOOR 1R HAS MOISTURE INSIDE THE LENS. FOUND IMPROPERLY INSTALLED SEAL. REMOVED LENS REMOVED MOISTURE LIGHT OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042500284 20080425 00284 NM 2008 4 25 2008UALA02382 1 20080423 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 ZONE B CEILING EMERGENCY LIGHTS 2 EACH IS INOP. RELAMPED, CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500285 20080425 00285 NM 2008 4 25 2008UALA02383 1 20080423 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 DOOR 5 RIGHT SILL EMERGENCY LIGHT IS INOP. REPLACED LAMP OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500286 20080425 00286 NM 2008 4 25 2008UALA02384 1 20080423 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 FLIGHT DECK CEILING EMERGENCY LIGHT IS INOP. RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500292 20080425 00292 NM 2008 4 25 2008UALA02407 1 20080424 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 526UA 24994 CREW REPORT, MULTIPLE SECTIONS EMERGENCY LIGHTS INOP IN COACH. EMERGENCY LIGHT SYS IS STILL INOP AT DOOR 4L. TEST SW102 95 IS INOP. WHILE AC IS ONLY BEING SUPPLIED BY GROUND SERVICE BUSS AFTER A TIME DELAY OF ABOUT 20 MINUTES THE GROUP OF E MERGENCY LIGHT PWR SUPPLYS THAT ARE IN SERIES WITH DOOR 4L TEST SW TURN ON AND DRAIN BATTERY PACKS. ALL OK WHEN ON SHIPS PWR. FOUND CONTACT FROZEN. REPLACED S10295 AT DOOR 4L BECAUSE CONTACTS C (COMMON) AND NO (NORM OPEN) STUCK CLOSED CAUS ING LIGHTS TO COME ON WITH AIRCRAFT POWER ON AND OFF SEQUENCE AND GND PWR SEQUENCE, EMERG LGHTS OP CK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042500308 20080425 00308 NE 2008 4 25 2008UALA02392 2 20080423 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEFT MALFUNCTIONED A UALA O OTHER O OTHER AP APPROACH 1 WP 29 648UA 25285 724366 LT ENGINE APPROACH IDLE OUT OF LIMITS. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042500322 20080425 00322 EA 2008 4 25 MASA200800334 1 20080421 A 2620 365000183 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY WARNING MESSAGE A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 7264V 12473 7264 FLT 2838 PHX-BUR. CARGO BOTTLE LOW CAUTION MESSAGE. DECLARED EMERGENCY AND DIVERTED TO LAS. REPLACED LEFT CARGO FIREX BOTTLE. 2 L 7 2 4F RT A21EA 2008042800012 20080428 00012 WP 2008 4 28 UPS08852050 1 20080413 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP NLG WW WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 RIGHT NOSE W/W TUNNEL REPAIR ON CEILING U-CHANNEL WORN THROUGH STA NEG 60 RBL 32. REMOVED OLD DOUBLE R, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1 -21A, 53-3-3 FIG 6, 51-1-8, 53-2-0. 2 L 7 4 4F RT 4A25 2008042800031 20080428 00031 EA 2008 4 28 A6WA200840278 1 20080402 A 2410 GENERATOR CNDAIR CL600 CL6002B19 1900309 EA NR 1 FAILED A A6WA O OTHER G MULTIPLE FAILURE CL CLIMB 1 GL 31 429AW 7711 DEPARTING BUFFALO, GENERATOR NR 1 DROPPED OFF LINE AT 700 FT PER QRH RESET. GENERATOR 2 DROPPED OFF LINE AT 1200 FT AND RESET PER QRH. BOTH GENERATORS OFF LINE FOR APPROXIMATELY 1 MINUTE. SERVICED GEN/IDG 1 WITH 4-5 PUMPS OF OIL. OPS CH ECK GOOD. NO LEAKS NOTED REF MM 12-13-24-610-801. OPS CHECK PER 24-20-00-710-801. ACFT OK FOR SERVICE. 2 L 7 2 4F RT A21EA 2008042800032 20080428 00032 EA 2008 4 28 A6WA200840298 1 20080314 A 5220 SHAFT CNDAIR CL600 CL6002B19 1900309 EA HATCH HANDLE CORRODED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 440AW 12016 7766 CREW ESCAPE HATCH OUTER HANDLE CORRODED ON SHAFT DURING C-CHECK. REPLACED HANDLE ASSEMBLY. (M) 2 L 7 2 4F RT A21EA 2008042800035 20080428 00035 EA 2008 4 28 SWIA200819515 1 20080115 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA WING TO BODY CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 983CA 7169 LEFT FUSELAGE TO WING STIFFENER IS CRACKED AT FS 461.0 AND WL 72.0, FOUND AT C-CHECK. COMPLIED WITH REPAIRS AT FS 461.0 0 WL 72.0 IAW CRJ200 SRM 51-42-06, PG 18 PARA 11 AND SRM 51-42-21 PG 19 PARA 11. 2 L 7 2 4F RT A21EA 2008042800040 20080428 00040 NM 2008 4 28 SWAA082064 1 20080420 A 5315 6546540 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND LONGITUDINAL FLOORBEAM VERTICAL STIFFENER CRACKED AT BS 639, RBL 46. REMOVED AND RE PLACED STIFFENER PER SWA EA. 2 L 7 2 4F RT A16WE 2008042800044 20080428 00044 NM 2008 4 28 SWAA082117 1 20080421 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042800047 20080428 00047 NM 2008 4 28 SWAA082118 1 20080421 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042800052 20080428 00052 NM 2008 4 28 SWAA082124 1 20080421 A 3320 412N1132 BALLAST BOEING 737 737301 1384611 NM CABIN FAULTY A SWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 660SW 23230 CREW REPORTED VISIBLE SMOKE AND ELECTRICAL SMELL AT ROW 12 ABC. INSPECTED AND FOUND LIGHT BALLAST AT ROW 12 ABC CAUSE O F SMOKE. REMOVED AND REPLACED LIGHT BALLAST PER MM. 2 L 7 2 4F RT A16WE 2008050100098 20080501 00098 EU 2008 5 1 2008UALA02430 1 20080424 A 3397 WIRE HARNESS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 412UA 465 SEAT 20 ABC FLOOR PROXIMITY ESCAPE PATH LIGHT IS INOP. FOUND DAMAGED HARNESS. REPLACED HARNESS, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050100101 20080501 00101 EU 2008 5 1 2008UALA02433 1 20080425 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 457UA 1146 SKIN IS WORN THROUGH AT FR 68 STR 44 AND MEASURES .5 INCH WIDE BY 2 INCH LONG. CUT DAMAGED SKIN FOR ACCES S TO FRAME 70 DAMAGE EVALUATION.BLENDED DAMAGE ON FRAME. CONT OF AMIS ITEM 8572009 :MFG FILLER FOR FR70 PER EVA71452. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050100112 20080501 00112 NM 2008 5 1 SA08031 1 20080428 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 807AW 1064 BOS - FOUND AFT GALLEY FLIGHT ATTENDANT FLASH LIGHT INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY. 2 L 7 2 4F RT A28NM 2008050200006 20080502 00006 EU 2008 5 2 WRNA200800017 1 20080226 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 501TR 53 DURING M96 CHECK, WHEN ACCOMPLISHING CPCP TASK CARD ZL-220-L403-9-01, CABIN SEAT TRACK WAS FOUND CORRODED AT FRAME 13B - 14C LBL 55. REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN FRAME 13B - 14C LBL 55 IAW A300 SRM 51-30-30 WITH SEAT TRA CK FABRICATED FROM EXTRUSION 60-22457. 2 L 7 2 4F RT A35EU 2008050200008 20080502 00008 EU 2008 5 2 WRNA200800014 1 20080326 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 501TR 53 DURING M96 CHECK, FOUND OUT OF LIMIT CORROSION ON FUSELAGE AT STR 6 TO FRAME 76. CUT OUT DAMAGED AREA 2.75 INCHES BY .7 5 INCHES AND INSTALLED FILLER FABRICATED FROM 2024 T3 0.090 AND REPAIR DOUBLER FABRICATED FROM 2024 T3 0.100 IAW A300 SR M 53-10-10. 2 L 7 2 4F RT A35EU 2008050200044 20080502 00044 NM 2008 5 2 RYNA200800010 1 20080112 A 5330 SKIN BOEING 757 7572G5 1384912 NM BS 1712 DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 151GX 24451 LOWER FUSELAGE SKIN HAS A DENT AT BS 1712 BETWEEN STR 25L AND 26L. REPAIRED IAW EO C00-5-53-011-08. 2 L 7 2 4F RT A2NM 2008050200063 20080502 00063 NE 2008 5 2 WRNA20080008 2 20080323 A 7200 ENGINE BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE MALFUNCTIONED A WRNA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 05 512MC 21220 517718 BECAUSE OF HIGH HEAT AND HUMIDITY AT DUBAI, ENGINES WERE UNABLE TO MAKE TAKEOFF POWER, ABORTED TAKE-OFF BEFORE 80 KNOTS AND RETURNED TO RAMP. PERFORMED MAIN ENGINE CONTROL TRIM ON NR 1 ENGINE IAW 71-00-00 PAGE 563 TEST 5. PERFORMED ENGINE PERFORMANCE RUN, OPS CHECKED GOOD. AIRCRAFT RELEASED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E23EA 2008050200066 20080502 00066 EU 2008 5 2 USAA920080875 1 20080418 A 5320 FITTING AIRBUS A321 A321211 3930370 EU BS 3851 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 188US 1724 PIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON THE L2 DOOR CUT OUT LOWER SILL FITTING, BS 3851/FR 66, S23L. REPAI RED THE L2 DOOR CUT OUT LOWER SILL FITTING, BS 3851/FR 66, S23L IAW USAIRWAYS TYPICAL REPAIR 53-41-01. 2 L 7 2 4F RT A28NM 2008050500003 20080505 00003 NM 2008 5 5 SWAA082306 1 20080428 A 5230 6546921 SKIN BOEING 737 7373H4 1384600 NM FWD CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED HC1 CHECK, FOUND FWD CARGO DOOR OUTER SKIN CRACKED AT DOOR HANDLE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008050500004 20080505 00004 NM 2008 5 5 SWAA082305 1 20080428 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT UPPER AFT CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008050500029 20080505 00029 NM 2008 5 5 SWAA082347 1 20080429 A 2761 654485113 ACTUATOR BOEING 737 7373H4 1384600 NM NR 5 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 5 SPOILER OUTBOARD ACTUATOR CASTING BROKEN. REMOVED AND REPLACED ACTUA TOR PER MM. 2 L 7 2 4F RT A16WE 2008050500031 20080505 00031 NM 2008 5 5 SWAA082346 1 20080429 A 5310 6517684 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME VERTICAL WEB CRACKED AT FWD ENTRY DOOR CUTOUT BS 303, STR 16L. REMOVE D AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008050500035 20080505 00035 NM 2008 5 5 SWAA082340 1 20080429 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND LEFT WING NR 2 L/E SLAT INBOARD UPPER SURFACE DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008050500055 20080505 00055 NM 2008 5 5 SWAA082357 1 20080501 A 5755 654645262A HINGE BOEING 737 7375H4 138449D NM NR 4 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND LEFT WING NR 4 SPOILER OUTBOARD ACTUATOR HINGE BROKEN. REMOVED AND REPLACED SPOILER P ER MM. 2 L 7 2 4F RT A16WE 2008050500059 20080505 00059 NM 2008 5 5 SWAA082358 1 20080501 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482B, RBL 2 TO RBL 10, WL 148. REPAIRED SHEAR TIE PER ER. 2 L 7 2 4F RT A16WE 2008050500067 20080505 00067 NM 2008 5 5 SWAA082365 1 20080501 A 5330 6546881 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 1045, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008050500068 20080505 00068 NM 2008 5 5 SWAA082366 1 20080501 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 723SW 27855 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008050500099 20080505 00099 NM 2008 5 5 USAA920080883 1 20080411 A 5320 STRAP BOEING 757 75723N 1384973 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 204UW 30886 BFM - MAJOR REPAIR - C1 CHECK - CRACKED FLOOR SUPPORT STABILIZATION STRAP, BS 365.25 - BS 377.7, LBL 40. REPAIRED FLOOR SUPPORT STABILIZATION STRAP, BS 365.25 - BS.377.7, LBL 40 IAW USAIRWAYS TYPICAL REPAIR 53-35-01. 2 L 7 2 4F RT A2NM 2008050500104 20080505 00104 NM 2008 5 5 USAA920080926 1 20080422 A 5320 6546812 WEB BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CRACKED WEB, BS 993, RBL 44, WL 208. REPLACED WEB, BS 993, RBL 44, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008050500106 20080505 00106 NM 2008 5 5 USAA920080928 1 20080422 A 5320 65C807351 SILL BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK, CORROSION ON THE R2 DOOR CUT OUT LOWER SILL INNER CHORD, BS 927, RBL 58, WL 208. REPLAC ED THE R2 DOOR CUT OUT LOWER SILL INNER CHORD, BS 927, RBL 58, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008050500118 20080505 00118 EU 2008 5 5 USAA920080939 1 20080422 A 5320 D53471124201 SHEAR PLATE AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 188US 1724 PIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON CABIN LEFT SHEAR PLATE, BS 4003/FR 69 - BS 4059/FR 70, S23L. REPLA CED CABIN LEFT SHEAR PLATE, BS 4003/FR 69 - BS 4059/FR 70, S23L IAW A321 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008050500128 20080505 00128 EU 2008 5 5 08FDEA01600 1 20080425 A 5420 A546114001000 PANEL AIRBUS 300 A300F4605R 3930327 EU NR 2 PYLON WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 NR 2 PYLON PANEL NR 424 CR IS WORN FROM FRETTING AROUND THE EXTERIOR FASTENER HOLES. REMOVED DAMAGE REF A300-600 SRM 51 -73-10. ORIGINAL THICKNESS .078. REMAINING THICKNESS .032. REMOVED .046. BEYOND LIMITS REF A300-600 SRM 54-52-51. F ABRICATED DOUBLER AND FILLER REF A300-600 SRM 54-52-51; FIG 203. CUT OUT DAMAGE REF A300-600 SRM 54-52-51. ALODINED R EF A300-600 SRM 51-21-10. PRIMED REF A300-600 SRM 51-23-10. INSTALLED DOUBLER AND FILLER REF A300-600 SRM 51-40-21, PA RA 5. PAINTED REF A300-600, SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008050500141 20080505 00141 NM 2008 5 5 08FDEA01614 1 20080428 A 5311 AFA00283 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 628FE 48447 UPPER FUSELAGE INTERIOR FRAME AT RIGHT STA 1681 LONGERON 11 FOUND DAMAGED. UPPER FUSELAGE INTERIOR, DENT FRAME AT RT BS 1681 LONGERON 11 REPAIRED AS PER SRM 53-30-00. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,50 0 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008050500162 20080505 00162 EU 2008 5 5 08FDEA01638 1 20080428 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 MAIN DECK FLOOR, BL O, AT FRAME 51 THE CENTER OF THE TRACK IS CRACKED AND CORRODED. REMOVED CORROSION; OUT OF LIMITS I AW A300-600 SRM 53-10-16; FIG 101. ORIGINAL MATERIAL 0.134. MATERIAL LOSS 0.055. MATERIAL REMAINING 0.079. REMOVED AN D REPLACED WITH A NEW SEAT TRACK IAW SRM 51-40-21 & 51-40-40. 2 L 7 2 4F RT A35EU 2008050500167 20080505 00167 WP 2008 5 5 08FDEA01646 1 20080428 A 7110 NSL6051511 SKIN DOUG MD10 MD1010F 3022112 WP NR 3 NOSE COWL DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 3 ENGINE NOSE COWL HAS DENTS ON THE EXTERNAL SKIN AT APPROX 5 O'CLOCK POSITION. REWORKED SKIN IN REF TO EA 8-5410-11 6980. 2 L 7 3 4F RT A22WE 2008050500178 20080505 00178 EA 2008 5 5 MASA200800320 1 20080415 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27314 7314 ASH FLT 1950 LIH-HNL - RT EMERGENCY DOOR EXTERIOR LIGHT INOP. MX RELAMPED, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008050500179 20080505 00179 EA 2008 5 5 MASA200800330 1 20080420 A 2621 8978892 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA APU LOW PRESSURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77181 13130 7181 ASH FLT 7058 ORD-GRR - APU BOTTLE LOW MESSAGE. REPLACED FIREX BOTTLE. 2 L 7 2 4F RT A21EA 2008050500207 20080505 00207 NM 2008 5 5 DHL2008760502 1 20080413 A 5720 BAC1506860 BEAM BOEING 727 7272B7 138407L NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 L/WING T/E "J" BEAM CRACKED AT LWBL 128. REMOVED, FABRICATED, AND INSTALLED NEW SUPPORT BEAM FROM WBL 70.5 TO 154.0, PE R ASTAR J/C EC-00873-001 AND B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008050500209 20080505 00209 NM 2008 5 5 Q2SA751004 1 20080428 A 7110 COWLING BOEING 747 747228F 1384895 NM NR 2 ENGINE INFLT SEPARATION A Q2SA K NONE D F INFLIGHT SEPARATION FLT CONT AFFECTED CL CLIMB 1 EA 63 751SA 22678 INFLIGHT ON CLIMB-OUT AT ABOUT 10,000 FT, LOUD NOISE HEARD WITH SLIGHT YAW TO THE LEFT. INFLIGHT INSPECTION REVEALED PA NELS MISSING ABOVE THE NR 2 ENGINE PYLON AND DAMAGE TO THE LEADING EDGE OF THE WING JUST ABOVE THE NR 2 ENGINE PYLON. N O ABNORMAL FLIGHT INDICATIONS AFTERWARDS, AND FLIGHT CONTINUED UNEVENTFUL TO DESTINATION. FURTHER INSPECTION ON GROUND REVEALED THAT LEFT AND RIGHT CORE COWLS TO THE NR 2 ENGINE CAME OFF, CREATING FURTHER SIGNIFICANT DAMAGE TO MULTIPLE AIR CRAFT AREAS. 2 L 7 4 4F RT A20WE 2008050500216 20080505 00216 EU 2008 5 5 08FDEA01655 1 20080429 A 5532 A55373311108 PANEL AIRBUS 300 A300F4605R 3930327 EU VERTICAL STAB DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 VERTICAL STAB L/E PANEL 322 CL LEADING EDGE IS DISBONDED. REPAIRED ERROSION STRIP LOWER END OF THE VERTICAL L / E PANEL 322 CL IAW AMM 55-32-11-8. 2 L 7 2 4F RT A35EU 2008050500218 20080505 00218 EU 2008 5 5 08FDEA01657 1 20080429 A 5532 A55373311108 PANEL AIRBUS 300 A300F4605R 3930327 EU VERTICAL STAB DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 VERTICAL STAB L/E PANEL 322 CL IS DISBONDED AROUND THE HOIST POINT. REPAIRED VERTICAL SATBILIZER L / E PANEL 322 CL HOI ST POINT AREA BY TRIMMING BURRS & RESEALING IAW AMM 55-32-11-8. 2 L 7 2 4F RT A35EU 2008050600008 20080506 00008 NM 2008 5 6 08FDEA01662 1 20080429 A 5347 A5327400500053 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 611FE 48604 MAIN CARGO COMPT CENTER SEAT TRACK IS CORRODED ON THE BOTTOM AT FRAME 78. SPLICED IN A NEW SEAT TRACK SECTION IAW SRM 53 -10-16; FIG 208. 2 L 7 3 4F RT A22WE 2008050600009 20080506 00009 WP 2008 5 6 IXXA08SMN107S 1 20080314 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 822 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT BS 822.000 LEFT BOTTOM LINE 22". REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, T REATED AND PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, 51-3-1, SRM 51-1-8B, ATI REPAIR SPECIFI CATION 2003-05, DRAWING 3755222, AND DPS 4.707. 2 L 7 4 4F RT 4A25 2008050600017 20080506 00017 NM 2008 5 6 USAA920080949 1 20080427 A 5320 140N2502 INTERCOSTAL BOEING 757 7572S7 1384962 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL ATTACH CLIP, BS 1280, LBL 45.5, WL 208. REPLACED INTERCOSTAL ATTAC H CLIP, BS 1280, LBL 45.5, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008050600018 20080506 00018 NM 2008 5 6 USAA920080951 1 20080417 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 812AW 1178 SAL - EMERGENCY EQUIPMENT - BC6 CHECK - FORWARD FLIGHT ATTENDANTS LEFT FLASHLIGHT BATTERY LOW. REPLACED THE BATTERY IN THE FORWARD FLIGHT ATTENDANTS LEFT FLASHLIGHT. 2 L 7 2 4F RT A28NM 2008050600021 20080506 00021 WP 2008 5 6 IXXA08SMN110S 1 20080314 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 700 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STATION 700.000 LBL 22. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AN D PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATION NUMBER 2003-05, DRA WING DOUGLAS 3755222, DPS 4.707, DC8 SRM 51-1-8B, AND 51-3-1. 2 L 7 4 4F RT 4A25 2008050600023 20080506 00023 NM 2008 5 6 ASAA0842858 1 20080330 A 5311 FRAME BOEING 737 737490 1384715 NM BS 616 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 CRACK FOUND ON INNER FRAME CHORD AT BS 616 RT WL200 AT STUB BEAM CRACK ON INNER CHORD WAS REPAIRED IAW ASA EA NR 5310 02 790. 2 L 7 2 4F RT A16WE 2008050600026 20080506 00026 NM 2008 5 6 ASAA0842863 1 20080414 A 5315 654681180 FLOORBEAM BOEING 737 737490 1384715 NM BS 986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 AFT CABIN BS 986.5 FLOORBEAM CORRODED AT RBL 40 TO RBL 46 (PREVIOUS REPAIR). REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008050600029 20080506 00029 NM 2008 5 6 ASAA0842860 1 20080407 A 5330 65C357672 SKIN BOEING 737 737490 1384715 NM BS 382 S16L DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 TEMPORARY FASTENER AT BS 382 STR 16L TO 17L WL 208 DAMAGE AT BS 382 STR 16L TO 17L WL 208. REPAIRED IAW B737 400 SRM 53 00 01, REPAIR 26 FIG 201. 2 L 7 2 4F RT A16WE 2008050600036 20080506 00036 NM 2008 5 6 NWAA081855642 1 20080421 A 5414 SKIN BOEING 757 757251 1384970 NM NR 2 NACELLE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 542US 26489 DURING ENGINE CHANGE, FOUND CRACK IN NR 2 PYLON SKIN AT ACCESS HOLE OUTBOARD SIDE NEAR THRUST REVERSER CENTER HINGE POIN T. REPAIRED PER EA 55-212947. 2 L 7 2 4F RT A2NM 2008050600037 20080506 00037 NM 2008 5 6 ASMF200804004 1 20080422 A 3231 273A33018 CONTROL MODULE BOEING 737 737* NM CFMINT CFM567 CFM567B22 13802 NE MLG FAILED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 851AM 27 29363 CAPTAIN REPORTED THAT LANDING GEAR LEVER DID NOT MOVE UP AFTER TAKE OFF, SO HE PERFORMED ABNORMAL PROCEDURE QRH PAGE 14. 4. AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE REPLACED THE LANDING GEAR CONTROL LEVER MODULE IAW MM 32-31-11, TES TED CORRECT IAW 32-31-00. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008050600038 20080506 00038 NM 2008 5 6 2008UALA02505 1 20080429 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 807UA 798 CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED CREW O2, PERFORMED LEAK CHECK WITH NO NOTED LEAKS AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050600041 20080506 00041 EU 2008 5 6 08FDEA01686 1 20080430 A 5755 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 5 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND DELAMINATION OUT OF LIMIT ON SPOILER 5 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 27-61-53/401. 2 L 7 2 4F RT A35EU 2008050600045 20080506 00045 EU 2008 5 6 08FDEA01690 1 20080430 A 5755 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 4 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND DELAMINATION OUT OF LIMIT ON SPOILER 4 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 27-61-51/401. 2 L 7 2 4F RT A35EU 2008050600049 20080506 00049 NM 2008 5 6 2008UALA02506 1 20080428 A 3510 MF20010 OXYGEN MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE 1ST OFFICER'S DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 813UA 858 FO'S OXYGEN FACE SHIELD IS DAMAGED. CREW COMMENTS, F/O O2 MASK INSIDE RUBBER CRACKED. TOP OF NOSE CONFORMING AREA. REP LACED MASK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050600055 20080506 00055 EU 2008 5 6 2008UALA02512 1 20080429 A 3500 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 449UA 851 OXYGEN PRESSURE LOW. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050600056 20080506 00056 NM 2008 5 6 DHL2008760529 1 20080402 A 5311 FRAME BOEING 727 7272B7 138407L NM BS 640 S16R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 FABRICATED AND INSTALLED FRAME REPAIR AT BS 640, AND STR 16R, PER B727 SRM 53-10-2 FIG 3 AND SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2008050600061 20080506 00061 NM 2008 5 6 AALA200800814 1 20080403 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 DFW - EMERGENCY LIGHT AT SEAT 27B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 27B. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050600065 20080506 00065 WP 2008 5 6 08FDEA01698 1 20080430 A 5320 AEA01121 WEB DOUG DC10 DC1010F 3022111 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1305 JAMB DOOR L3 FOUND CRACK 0.5 INCH LONG ON THE WEB UPPER SIDE. PERFORMED REPAIR FOR SRM 53-50-00 FIG 19 VOL. I 2 L 7 3 4F A22WE 2008050600070 20080506 00070 WP 2008 5 6 AALA200800816 1 20080404 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7537A 49991 LGA - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008050600071 20080506 00071 NM 2008 5 6 AALA200800817 1 20080404 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 931AN 30079 MIA - EMERGENCY LIGHT AT SEAT 18D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008050600073 20080506 00073 WP 2008 5 6 AALA200800815 1 20080404 A 3260 833704 SENSOR DOUG DC9 DC982 3022082 WP MLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 298AA 49310 SFO INFLIGHT T324/04APR - AFTER TAKEOFF, NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED TO SFO AND LANDED WITHOUT INCID ENT. REPLACED NOSE GEAR UPLOCK PROXIMITY SENSOR, STRUT SEAL, AND BOTH NOSE LANDING GEAR WHEEL SPIN BRAKES. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008050600092 20080506 00092 EU 2008 5 6 08FDEA01743 1 20080503 A 5753 SKIN AIRBUS 300 A300F4605R 3930327 EU TE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 673FE 780 RT WING INBD FLAP UPPER SURFACE HAS 2 GOUGES APPROX .50 IN LONG AT WS 265. PERFORMED SKIN PATCH REPAIR ON RT INBD FLAP UPPER SKIN AT FLAP RIB 17, 12 INCHES AFT OF FRONT SPAR IAW A300-600 SRM 57-50-00, FIG 205. 2 L 7 2 4F RT A35EU 2008050600093 20080506 00093 EU 2008 5 6 08FDEA01753 1 20080505 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU K FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 720FD 417 UPON SLAT/ K-FLAP EXTENSION, THE RT/K-FLAP PANEL CONTACTED THE UPPER CLOSE-OUT PANEL RESULTING IN DEFORMATION OF PANEL E DGES AND ATTACH LINK. REPLACED K-FLAP SKIN IAW SRM 51-40-21, REPLACED K-FLAP VANE ASSY IAW AMM 27-87-12-4. REPLACED WI NG WEB/FORMER IAW SRM 51-40-21. OPS CHECKED GOOD IAW AMM 27-84--00-5. 2 L 7 2 4F RT A35EU 2008050600096 20080506 00096 NM 2008 5 6 DHL2008760520 1 20080407 A 5347 BAC1520841 SEAT TRACK BOEING 727 7272B7 138407L NM BS 760-840 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND REPLACED SEAT TRACK SECTION AT LBL 24, FROM BS 760 TO 850, PER B727 SRM 53-10-2 FIG 7 AND 53-10 -5 FIG 1. 2 L 7 3 4F A3WE 2008050600101 20080506 00101 NM 2008 5 6 AALA200800807 1 20080402 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 36C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 36C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050600112 20080506 00112 EU 2008 5 6 08FDEA01745 1 20080503 A 5347 A53274005202 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 673FE 780 MAIN DECK CARGO SEAT TRACK NR 3 RT HAS 3 AREAS OF CORROSION, 5 SQ INCHES BETWEEN FR 26 AND FR 31. REMOVED LEVEL 1 CORRO SION AND REPAIRED SEAT TRACK NR 3 RT WITH SPLICE REPAIR BETWEEN FR 26 AND FR 29 IAW A300-600 SRM 53-10-16, FIG 201, PAGE 207/208. 2 L 7 2 4F RT A35EU 2008050600117 20080506 00117 EA 2008 5 6 REXA200800010 1 20080430 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 834AY 8034 FLAPS FAILED WHEN SELECTED FROM 20 TO 30 ON APPROACH. SYSTEM RESET AND PLACED ON SEVENTY TWO HOUR WATCH PER AD 2006-12- 21. 2 L 7 2 4F RT A21EA 2008050200001 20080502 00001 EU 2008 5 2 WRNA200800021 1 20080228 A 5347 A257727800101 TRACK AIRBUS 300 A300B4203 3930306 EU CARGO BAY CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 501TR 53 DURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD ZL-150-L403-501, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN A FT CARGO COMPARTMENT AT FRAMES 54 TO 57. REMOVED AND REPLACED ROLLER TRACK IAW SRM 51-30-30. 2 L 7 2 4F RT A35EU 2008050200014 20080502 00014 WP 2008 5 2 UPS08852073 1 20080420 A 5712 576947027 RIB DOUG DC8 DC873F 302199F WP LWS 747 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING OUTBD LE UPPER RIB CRACKED JUST OUTBD OF ACCESS PNL 518C XFS 747.5. REPAIRED LT WING OUTBD L E UPPER RIB AT XFS 747.5 IAW SRM 57-02-00 FIG 002 AND DWG 5769470-27. 2 L 7 4 4F RT 4A25 2008050200026 20080502 00026 NM 2008 5 2 UPS08M52085 1 20080127 A 5751 SKIN DOUG MD11 MD11 3023602 NM RT AILERON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP INSPECTION TYPE:C RT I/B AILERON FOUND CHAFF MARKS ALONG L/E LOWER SKIN, O/B SIDE. RT I/B AILERON CHAFF SKIN REMOVED PE R SRM 51-35-01 V.2R.40. NEW SKIN HOLES PICKED UP PER SRM 51-31-01V.2R.40. NEW SKIN INSTALLED PER SRM 51-35- 01V.2R.40. RHW I/B AILERON LOWER L/E ACCESS PANEL NR 645BB, INSTALLED PER AMM20-50-02 REV.53. 2 L 7 3 4F RT A22WE 2008050200031 20080502 00031 EU 2008 5 2 USAA920080918 1 20080425 A 3397 WIRE AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625AW 64 NR 329 - PHX - EEL - EMERGENCY LIGHT AT SEAT 13 INOP. MAINTENANCE RECONNECTED LOOSE WIRES AND ASSEMBLY. OPERATIONAL CH ECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008050200032 20080502 00032 2008 5 2 USAA920080919 4 20080426 A 2330 RDAX443110 ELECTRICAL BOX AIRBUS 320 A320214 3930316 EU ENTERTAIN SYS DEFECTIVE A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 119US 1268 FLT NR 1005 PHL-SJU - BURNING ODOR, CREW REPORTED ELECTRICAL SMOKE IN THE AFT CABIN AND DECLARED AN EMERGENCY. IT WAS R EPORTED THAT THE ELECTRICAL SMOKE AND ODOR APPEARED TO BE GENERATED FROM THE 17A/B PASSENGER ENTERTAINMENT SYSTEM BOX. AIRCRAFT DIVERTED TO BDA AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE SEAT ELECTRONIC BOX AT 17ABC . AUDIO ENTERTAINMENT SYSTEM OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008050200049 20080502 00049 NM 2008 5 2 RYNA200800011 1 20080111 A 5330 SKIN BOEING 757 7572G5 1384912 NM BS 1697 DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 151GX 24451 UPPER FUSELAGE SKIN HAS A DENT AT BS 1697 BETWEEN STR 14L AND 15L. REPAIRED IAW EO C00-5-53-015-08. 2 L 7 2 4F RT A2NM 2008050500017 20080505 00017 NM 2008 5 5 SWAA082333 1 20080429 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 14R. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2008050500075 20080505 00075 SO 2008 5 5 FDKA200804176 1 20080422 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6072 MCO-RDU. EMERGENCY FLOOD LIGHT ON RT SIDE ROW 12 INOP. MX RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008050500076 20080505 00076 SO 2008 5 5 FDKA200804177 1 20080423 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6092 MCO-HSV. ROW 12 EMERGENCY LIGHTS INOP. MX RESET AND OPS CHECKED SYSTEM GOOD. 2 L 7 2 4T RT T00011AT 2008050500078 20080505 00078 SO 2008 5 5 FDKA200804179 1 20080424 A 5320 14521725615 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 837MJ 145367 THE RIGHT FLOOR SILL AT FRAME NR 22 IS CORRODED OUT OF LIMITS. THE DAMAGED SILL HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008050500082 20080505 00082 NM 2008 5 5 ZZDZ2008094 1 20080424 A 3350 0201804002 LENS BOEING 717 717200 1383700 NM CABIN IMPROPER PART A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 933AT 55071 FAA FOUND ROW 21 EMERGENCY EXIT ROW HAS A WHITE LENS, RATHER THAN A RED LENSE COVER IAW MM 33-51. REPLACED WHITE LENS C OVER IN ROW 21 WITH A RED LENS COVER. 2 L 7 2 4F TR A6WE 2008050500109 20080505 00109 NM 2008 5 5 USAA920080931 1 20080422 A 5312 6545833U428 GUSSET BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CRACKED BULKHEAD GUSSET, BS 178, RBL 20, WL 207. REPLACED BULKHEAD GUSSET, BS 178, RBL 20, WL 207 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008050500138 20080505 00138 NM 2008 5 5 08FDEA01610 1 20080426 A 5753 ARC27361 SKIN DOUG MD11 MD11F 3023600 NM LT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 628FE 48447 LEFT WING INBOARD FLAP LOWER SURFACE CENTER LOWER SEGMENT FOUND DENT. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG 17 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008050500139 20080505 00139 EU 2008 5 5 08FDEA01612 1 20080428 A 5411 A54611750 SPAR AIRBUS 300 A300B4622R 3930312 EU LT PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 CRACK FINDING ON LT PYLON NR 2 LOWER SPAR AT RIB 10. REPAIR PERFORMED BY CUTTING AREA AND INSTALLING A DOUBLER IAW DRA WING R546-10342 ISS A , APPROVED BY RAS/AS/0040/2008 AND EA 6-5451-115284. 2 L 7 2 4F RT A35EU 2008050500165 20080505 00165 EU 2008 5 5 08FDEA01642 1 20080427 A 5720 A5724007120100 ANGLE AIRBUS 300 A300F4605R 3930327 EU RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 AFT OF R/WING REAR SPAR, CRACKED ANGLE AT T/E TOP PANEL SUPPORT ANGLE, OUTBD SIDE OF RIB 9, FWD OF SPOILER NR 3 INBD HIN GE PIN. REMOVED CRACKED ANGLE IAW A300-600 SRM 51-40-21. RECEIVED NEW BRACKET P/N A5724007120100, P/O NR 617032.1. IN STALLED NEW BRACKET IAW A300-600 SRM 51-40-21 PARA 7. 2 L 7 2 4F RT A35EU 2008050500187 20080505 00187 EA 2008 5 5 TRAX200800193 1 20080204 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 902EV 7620 CLIP CRACKED AT FS 280, FLOOR LEVEL AT RBL 9 I/B (RESOLVED ON W/O: 82203 TASKCARD: N/R-00023). REPAIRED DAMAGE TO FS 28 0 WEB O/B OF RBL 9 IAW EO 6+00-53-90 C/W. 2 L 7 2 4F RT A21EA 2008050500189 20080505 00189 EA 2008 5 5 TRAX200800192 1 20080204 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 902EV 7620 CLIP CRACKED AT FS 280, FLOOR LEVEL AT LBL 9 I/B (RESOLVED ON W/O: 82203 TASKCARD: N/R-00022). REPAIRED DAMAGED TO FS 2 80 WEB O/B OF LBL 9 IAW EO 600-53-90 C/W JB13225. 2 L 7 2 4F RT A21EA 2008050500192 20080505 00192 GL 2008 5 5 CHQA200800090 2 20080428 A 7200 AE3007A16 ENGINE EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A CHQA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 11 977RP 5339 5339 145185 CAE311280 FLIGHT 7820 CMH TO MTR - DURING TAKEOFF ROLL AT 80KTS, THE CREW REPORTED SEEING WHITE SMOKE IN THE COCKPIT AND CABIN. A T THAT TIME, THE CREW DECIDED TO ABORT TAKEOFF AND RETURN TO GATE WITHOUT INCIDENT. MAINTENANCE ARRIVED AND CONDUCTED A N ENGINE RUN AND NOTED WHEN THROTTLES WERE ADVANCED SMOKE BECAME PRESENT AND HAD AN OIL BURNING SMELL. MAINTENANCE REPL ACED THE NR 1 ENGINE AND CONDUCTED A FUNCTIONAL TEST WITH NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008050500198 20080505 00198 NM 2008 5 5 DL764080634 1 20080425 A 7830 32829363 ACTUATOR BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL THRUST REVERSER OUT OF ADJUST A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 834MH 21097 29707 706433 ON T/O, ROLL LT ENG ACHIEVED ONLY 55 PERCENT N1. TAKEOFF ROLL ABORTED AT APPROX 40 KNOTS. FOUND LEFT ENGINE THRUST REV ERSER RIGHT SIDE T/R L AND T/R R 26 PERCENT. ADJUSTED FEEDBACK ACTUATOR POSITION. VERIFIED L ENG REVERSER LOCKED OUT P ER MEL 78-31-01 ENGINE THRUST INDICATION NORMAL. 2 L 7 2 4F 4 F RT A1NM E23EA 2008050500208 20080505 00208 WP 2008 5 5 IXXA08SMN106S 1 20080314 A 5320 FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STATION 781.000 RIGHT BOTTOM LINE 22". REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEA NED, TREATED AND PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-1-8B, 51-3-1, ATI REPAIR SPECIFICATION 2003-05, DRAWING DOUGLAS 3755222, AND DPS 4.707. 2 L 7 4 4F RT 4A25 2008050600014 20080506 00014 NM 2008 5 6 USAA920080944 1 20080410 A 5313 6545775592 STRINGER BOEING 737 73733A 1384673 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON STRINGER, BS 767 - BS 787, S25R. REPAIRED STRINGER, BS 767 - BS 787, S25R IAW B737 SRM 53-00-03-2R1. 2 L 7 2 4F RT A16WE 2008050600016 20080506 00016 NM 2008 5 6 USAA920080946 1 20080410 A 5315 6546812185 FLOORBEAM BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPLACED - C21 CHECK - LEVEL 2 CORROSION ON FLOORBEAM, BS 1002, LBL 11, WL 208. REPLACED FLOORBEAM, BS 100 2, LBL 11, WL 208 IAW B737M SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008050600043 20080506 00043 EU 2008 5 6 08FDEA01688 1 20080430 A 5755 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 3 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND DELAMINATION OUT OF LIMIT ON SPOILER 3 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 27-61-51/401. 2 L 7 2 4F RT A35EU 2008050600048 20080506 00048 EU 2008 5 6 08FDEA01693 1 20080430 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND ELONGATED HOLES ON LT BOTTOM WING SKIN AND SUPPORT BRACKET FOR HYDRAULIC LINES. REPAIR PERFORMED BY OVERSIZING AND SPOTFACING THE HOLES, INSTALLING FREEZE PLUG IAW DRAWING R571-50532, APPROVED BY RAS /BAE/1006364/2008 ISS A AND EA 6-2900-114925. 2 L 7 2 4F RT A35EU 2008050600063 20080506 00063 NM 2008 5 6 08FDEA01696 1 20080430 A 5730 65267832 PANEL BOEING 727 727232 1384082 NM ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 RIGHT WING L/E LWR PANEL 6402 HAS 2 INCH BY 6 INCH AREA OF DISBOND CORE FROM INNER AND OUTER SURFACES. REPAIRED PANEL 6 402 REF SRM 51-40-9 PARAGRAPHS 3D, 4B, 4E, 4F AND AMM 51-20-051-7, 51-20-151-7 TAP TEST GOOD. THIS IS CLASSIFIED AS A M INOR REPAIR. 2 L 7 3 4F A3WE 2008050600066 20080506 00066 EU 2008 5 6 08FDEA01699 1 20080414 A 5720 A5796553520000 FRAME AIRBUS 300 A300B4622R 3930312 EU WING TO BODY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 RT WING, FAIRING 632BB WITH FRAME ATTACHMENT SIDE LOAD CRACK. FRAME REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5720-117327. 2 L 7 2 4F RT A35EU 2008050600068 20080506 00068 EU 2008 5 6 08FDEA01701 1 20080318 A 5510 A55177411003 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU HORIZONTAL STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 HORIZONTAL STAB, UPPER APRON RT SIDE DAMAGED RT UPPER RT SIDE WAS REPAIRED IAW FEDEX EA 6-5510-117324. 2 L 7 2 4F RT A35EU 2008050600074 20080506 00074 NM 2008 5 6 AALA200800804 1 20080402 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR GALLEY AREA IS DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT R IGHT NUMBER ONE DOOR GALLEY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050600111 20080506 00111 2008 5 6 MASA200800358 4 20080430 A 2562 4530150 ELT CNDAIR CL600 CL6002D24 1390016 EA UNKNOWN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 916FJ 5233 15016 ASH FLT 2681 CLT-ATL - ELT ON CAUTION MESSAGE. MX REPLACED THE ELT, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008050600115 20080506 00115 WP 2008 5 6 08FDEA01748 1 20080505 A 5330 NDA6013501 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING REPAIR ASSESSMENT WAS FOUND AN EXISTING EXTERNAL REPAIR AT FUSELAGE SKIN STA 1019, LONG NR 37R REPAIR FOUND NOT I N CONFORMITY WITH APPROVED DATA AND HAS BEEN REPLACED WITH A NEW IAW SRM 53-20-00 FIG 6 SH 3 AND 4. 2 L 7 3 4F A22WE 20080519 EU 2008 5 19 08FDEA01772 1 20080506 A 5315 A53781041200 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 673FE 780 AFT CARGO COMPARTMENT HAS A .250 INCH CRACK ON FLOORBEAM AT FR 64 OUTBD OF SEAT TRACK NR 3 RT. REMOVED CRACK AND INSTAL LED CROSSBEAM REPAIR AT FRAME 64 BETWEEN SEAT TRACKS NR 3 RT AND NR 4 IAW A300-600 SRM 53-10-15, FIG 21. 2 L 7 2 4F RT A35EU 2008050600121 20080506 00121 NM 2008 5 6 08FDEA01707 1 20080501 A 5714 APB74451 SKIN DOUG MD11 MD11F 3023600 NM CENTER WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 628FE 48447 MAIN DECK CENTER WING UPPER SKIN SURFACE AT STA 1341 X = 101 FOUND CORROSION. REPAIR CARRIED OUT AS PER EA 1-5710-11314 5, CLASSIFIED AS A MINOR REPAIR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008050600122 20080506 00122 WP 2008 5 6 08FDEA01708 1 20080501 A 5347 60449818 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 309FE 48298 MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT FS 1501-1531 LBL 8. REPLACED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1 SE AT TRACK. FABRICATED ON TRAVELER T8/737384. SPLICES FABRICATED ON TRAVELER T8/737385, F/S 1501-1531 LBL 8. 2 L 7 3 4F RT A22WE 2008042800055 20080428 00055 NM 2008 4 28 SWAA082098 1 20080418 A 5330 6545800 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042800058 20080428 00058 EA 2008 4 28 SWIA200819518 1 20080115 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 983CA 7169 FS 280 AT LBL9 LOWER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED ALL REPAIR PARTS AT FS 280 AND LBL9 PER CRJ2 00 REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2008042800061 20080428 00061 NM 2008 4 28 SWAA082099 1 20080420 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 718SW 27852 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008042800065 20080428 00065 EA 2008 4 28 A6WA200840256 1 20080320 A 5751 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT AILERON DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 439AW 7753 LT AILERON LEADING EDGE UPPER SKIN FOUND ABRADED. LT AILERON LEADING EDGE UPPER SKIN SHROUD REPLACED IAW CRJ 200 SRM 51 -42-21. (M) 2 L 7 2 4F RT A21EA 2008042800070 20080428 00070 WP 2008 4 28 ABXA080132 1 20080320 A 5320 99100787 WEB DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 SUB FLOOR WEB CRACKED AT STA 179, LEFT BUTT LINE 20. REPAIRED SUB FLOOR WEB IAW DC9 SRM 53-01, FIGURE 2. 2 L 7 2 4F A6WE 2008042800075 20080428 00075 EA 2008 4 28 A6WA200840266 1 20080324 A 5200 DOOR CNDAIR CL600 CL6002B19 1900309 EA GROUND POWER CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 AT FS 200 INSIDE AC GROUND POWER DOOR (122BR), CORROSION WAS FOUND ON FWD SIDE. (M) CORROSION REMOVED IAW SRM 51-21-06 . 2 L 7 2 4F RT A21EA 2008042800080 20080428 00080 EA 2008 4 28 A6WA200840257 1 20080325 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 LT SIDE OUTBOARD LEADING EDGE UPPER RIB INBOARD SIDE CORROSION. (M) LT SIDE OB LEADING EDGE UPPER RIB CORROSION REMOVED IAW SRM 51-21-06. (K) 2 L 7 2 4F RT A21EA 2008042800082 20080428 00082 WP 2008 4 28 ABXA080133 1 20080320 A 5720 59559151 SUPPORT BRACKET DOUG DC9 DC941 302207N WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 LEFT REAR SUPPORT BRACKET FORWARD PATCH 2108 WAS CRACKED. REPAIRED CRACK IAW DC9 SRM 51-70-1. 2 L 7 2 4F A6WE 2008042800085 20080428 00085 EU 2008 4 28 08FDEA01526 1 20080424 A 5330 A53812109200 SKIN AIRBUS 300 A300F4605R 3930327 EU RT WING GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 RIGHT WING ROOT AREA EXTERNAL SKIN HAS NUMEROUS GOUGED PLACES BETWEEN FRAME 51 AND FRAME 52. REMOVED THE DAMAGE & FOUND SKIN TO BE OUT OF LIMITS. COMPLIED WITH E.A. 6-5310-118492. 2 L 7 2 4F RT A35EU 2008042800086 20080428 00086 NE 2008 4 28 08FDEA01527 2 20080424 A 7532 9788422 BLEED VALVE AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4E1 52054 NE NR 2 ENGINE MALFUNCTIONED A FDEA B EMER. DESCENT G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SO 25 451FE 4632 4632 303 WHILE CRUISING AT FL400, BOTH AUTO PRESS REGULATORS FAULTED ALMOST SIMULTANEOUSLY. COMPLIED W/ECAM AND QRH. ATTEMPTED RESET BUT BOTH FAULTED AGAIN. SHORTLY THERE AFTER BOTH ENG BLEED 1 AND 2 FAULTED. DONNED O2 AND DESCENDED. BLEED VALV ES WOULD NOT RESET. DESCENDED TO 10,000 FEET AND CONTINUED TO KMEM. O2 MASKS DEPLOYED IN LAV. REMOVED AND REPLACED NR 2 ENGINE FAN AIR VALVE IAW AMM 36-11-16-4. RAN NR 1 & 2 ENGINES AT HIGH POWER IAW JRH CHAP 5, ALL INDICATIONS NORMAL. NR 1 & 2 PERCOOLER INLET TEMPS READ 175C AND 180C RESPECTIVELY. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A35EU E3NE 2008042800088 20080428 00088 WP 2008 4 28 ABXA080134 1 20080320 A 5320 3917285504 BRACKET DOUG DC9 DC941 302207N WP RT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 INBOARD BULKHEAD FORWARD VERTICAL STIFFENER BRACKET FORWARD SIDE CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-3 0-1. 2 L 7 2 4F A6WE 2008042800090 20080428 00090 EU 2008 4 28 2008UALA02393 1 20080423 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOORWAY CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 443UA 820 R2 DOOR SILL HAS CORROSION ON INBOARD FLANGE AT FRAME 68. ACCOMPLISHED MAJOR REPAIR. MAJOR REPAIR. R2 DOOR SILL HAS CORR OSION ON I-B FLANGE AT FRAME. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042800092 20080428 00092 WP 2008 4 28 ABXA080135 1 20080321 A 5730 59121566 SKIN DOUG DC9 DC941 302207N WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 RIGHT WING UPPER SURFACE XRS 164.00, THE BONDED PANEL JUST INBOARD OF INBOARD SPOILER BOARD HAD 6 EACH SHEARED FASTENERS . REPAIRED CRACKED SKIN IN AREA OF LOOSE RIVETS IAW DC9 SRM 57-01, FIGURE 2. 2 L 7 2 4F A6WE 2008042800093 20080428 00093 EA 2008 4 28 A6WA200840255 1 20080326 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A A6WA O OTHER O OTHER CR CRUISE 1 GL 31 429AW 7711 FIRST OFFICERS SIDE WINDOW CRACKED. REMOVED AND REPLACED WINDOW IAW AMM 56-12-01. 2 L 7 2 4F RT A21EA 2008042800094 20080428 00094 NM 2008 4 28 2008UALA02371 1 20080422 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 500D CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 346UA 24250 EXTERNAL FUSELAGE SKIN CRACKED AT CHEM MILLED STEP BELOW STRINGER S-12R FROM BS 500D+17" TO BS 500D+19". MAJOR REPAIR ACCOMPLISHED, CUTOUT DAMAGE. FABRICATED AND INSTALLED EXTERNAL SKIN DOUBLER/TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042800101 20080428 00101 EA 2008 4 28 A6WA200840288 1 20080404 A 5313 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 310-340 DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 LOWER SILL LONGERON OF PAX DOOR CORRODED BETWEEN FS 310 TO 340 LBL 45. (M) CORROSION ON LOWER SILL OF PAX DOOR REMOVED IAW SRM 51-21-06. 2 L 7 2 4F RT A21EA 2008042800105 20080428 00105 NM 2008 4 28 HALA0800540 1 20080421 A 2121 033638500 FAN BOEING 767 7673CB 1385187 NM NR 1 OVERHEATED A HALA K NONE M OVER TEMP IN INSP/MAINT 1 WP 13 588HA 33466 CONTROL RELAY TEST FAILED. NUMBER 1 FAN OVERHEATED AND STOPPED, DET FAN PRESSURE SWITCH HAD ALSO FAILED DUE TO A PIN BE ING BENT ON THE PRESSURE SWITCH. REMOVED AND REPLACED FAN AND DET AIR PRESSURE SWITCH. OPS CHECK GOOD. OK FOR SERVICE . 2 L 7 2 4F RT A1NM 2008042800108 20080428 00108 NM 2008 4 28 HALA0800535 1 20080417 A 5710 STRUCTURE BOEING 717 717200 1383700 NM RT WING DAMAGED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 486HA 55131 LIGHTNING STRIKE DAMAGE, RIGHT WING TIP TRAIL EDGE. REMOVED RT WING TIP. INSTALLED WING TIP ASSY PER AMM 57-30-01. SE CURITY CK AND OPS CK OK. 2 L 7 2 4F TR A6WE 2008042800109 20080428 00109 NM 2008 4 28 HALA0800533 1 20080419 A 7922 15622000 HEAT EXCHANGER BOEING 767 76733A 1385209 NM GE CF680 CF680A2 NE NR 2 ENGINE LEAKING A HALA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, ON ARRIVAL AT GATE FOUND NR 2 ENGINE HEAT EXCHANGER AIR OIL LEAKING. REMOVED AND REPLACED AIR OIL HEAT EXCHANGER PER AMM 79-21-09-404-013-N00 AND AMM 71-00-00/501. OPS CHECK GOOD AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E13NE 2008042800110 20080428 00110 NM 2008 4 28 HALA0800532 1 20080412 A 2710 3F8202A MODULE BOEING 717 717200 1383700 NM AILERONS MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 480HA 55125 AILERON STUCK 1/2 WAY LEFT OF CENTER IN FLIGHT. CKED FREEDOM OF MOVEMENT OF AILERON, NO DEFECT NOTED. FOUND AILERON TR IM IND OF CONFIG PG 1/2 LWD OF CENTER. ACCOMP FIM 27-10-00 TASK 801 MAINTENANCE MSG ON ATCL WAS NR 43 ACCOMP FIM 27-10- 00 TASK 812. REPLACED AIL AND RUDDER TRIM CTL MODULE PER AMM 27-10-07. 2 L 7 2 4F TR A6WE 2008042800111 20080428 00111 NM 2008 4 28 USAA920080906 1 20080421 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 527AU 23862 MX CHECK - PHL - RIGHT HAND MIDDLE EMERGENCY EXIT LIGHT INOP. MX REPLACED THE BATTERY CHARGER, OPERATIONAL CHECK WAS GO OD. 2 L 7 2 4F RT A16WE 2008042800114 20080428 00114 EA 2008 4 28 A6WA200840279 1 20080219 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER O OTHER DE DESCENT 1 GL 31 421ZW 7346 FLAPS FAIL INDICATION ON APPROACH DIVERTED TO ORD, FLAPS AT 5 DEGREES. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMEN T 98-018B STEPS 1.3 AND 1.4. FLAPS SYSTEM RESET OK. (M) 2 L 7 2 4F RT A21EA 2008042800120 20080428 00120 EA 2008 4 28 A6WA200840260 1 20080325 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 LT INBOARD LEADING EDGE OUTBOARD SIDE UPPER RIB CORROSION. (M) CORROSION REMOVED IAW SRM 51-21-06. (K) 2 L 7 2 4F RT A21EA 2008042800123 20080428 00123 NM 2008 4 28 ASAA0852826 1 20080421 A 2424 762185H GCU BOEING 737 737890 1384527 NM APU DEFECTIVE A ASAA K NONE O OTHER CL CLIMB 1 NM 02 584AS 2734 2734 35682 DURING CLIMB APU GENERATOR INDICATED 16 AMPS WITH APU NOT RUNNING. REPLACED GCU GENERATOR CONTROL UNIT. 2 L 7 2 4F RT A16WE 2008042800125 20080428 00125 NM 2008 4 28 ASAA0852827 1 20080422 A 4960 2118966222 ECU BOEING 737 737890 1384527 NM APU DEFECTIVE A ASAA K NONE O OTHER CL CLIMB 1 NM 02 584AS 2740 2740 35682 APU GENERATOR INDICATES 15 AMPS WITH APU OFF JUST AS OCCURRED THE DAY BEFORE. REPLACED ECU APU ELECTRONIC CONTROL UNIT AFTER REPLACING GCU THE DAY BEFORE. 2 L 7 2 4F RT A16WE 2008042800128 20080428 00128 NM 2008 4 28 CALA0800350 1 20080424 A 2612 CGAB140000 FIRE LOOP BOEING 737 737524 1384721 NM CARGO BAY FAULTY A CALA F ACTIVATE FIRE EXT. N FALSE WARNING LD LANDING 1 SW 27 18611 27324 UPON TOUCHDOWN AND T/R ACTIVATION THE A-LOOP NR 2 AFT CARGO SMOKE DETECTOR LIGHT ILLUMINATED. QUICK REFERENCE HANDBOOK FOR CARGO FIRE DETECTION/FIRE WARNING LIGHT DID NOT ILLUMINATE. COMPLETED THE CARGO FIRE INDICATION CHECK LIST - BOTTLE DISCHARGED, FIRE OR SMOKE NOT PRESENT IN AFT CARGO PIT. FOUND AIRCRAFT A-LOOP DETECTION LIGHT ON. REMOVED AND REPLACE D AFT CARGO A-LOOP, MFG P/N CGAB1400-00. A3 DETECTOR SYSTEM OPERATION CHECK GOOD PER AMM 26-16-10. 2 L 7 2 4F RT A16WE 2008042800130 20080428 00130 NM 2008 4 28 CALA0800352 1 20080422 A 5320 6547957U3 SILL BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 AFT CARGO DOOR SILL WEB IS CORRODED. REMOVED AND REPLACED CARGO DOOR SILL WEB REF 737-500 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008042800131 20080428 00131 NM 2008 4 28 CALA0800353 1 20080423 A 5315 141T5107 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 73152 30431 CABIN - STA 303 LBL 17 TO 35 FLOOR SUPPORT FOUND CORRODED. CABIN STA 303 LBL 17 TO LBL 35 FLOORBEAM REPAIRED PER SRM 53 -00-51 FIG 201 REPAIR 1, HFEC FOUND NO CRACK. 2 L 7 2 4F RT A1NM 2008042800134 20080428 00134 EU 2008 4 28 SWAA082193 2 20080423 A 7200 ENGINE BOEING 737 7373H4 1384600 NM CFMINT CFM56 CFM563B2 13802 EU NR 2 SHUTDOWN A SWAA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SW 29 304SW 22944 725524 INFLIGHT SHUTDOWN/DIVERSION. NR 2 ENGINE FAILED DURING CLIMB THRU 33,000 FT. NO ABNORMAL INDICATIONS ON ANY ENGINE INST RUMENT. FUEL WAS BEING TRANSFERRED FROM NR 1 TANK TO NR 2 TANK WHEN ENGINE FAILURE OCCURRED. PERFORMED VISUAL CHECK OF NR 2 ENGINE FUEL CONTROL NO DEFECTS NOTED. COMPLIED WITH ENGINE FUEL SUCTION FEED OPERATION TEST PER MM. 2 L 7 2 4F 4 F RT A16WE E21EU 2008042800137 20080428 00137 NM 2008 4 28 SWAA082148 1 20080422 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 344, STR 18R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008050600128 20080506 00128 EA 2008 5 6 MASA200800351 1 20080428 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 17337 15516 7337 ASH FLT 2721- PHX-SBA - FLAPS FAIL CAUTION AT 2 DEGREES, WOULD NOT RESET. DECLARED AN EMERGENCY AND DIVERTED TO LAX. C /W PART A/B, REPLACED LT/RT BPSU AND PDU. 2 L 7 2 4F RT A21EA 2008050700007 20080507 00007 NM 2008 5 7 NOCA03008 1 20080429 A 3350 72914 LIGHT BOEING 757 75728A 1384976 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 THE 3L EMERGENCY LIGHT INOP. RELAMPED 3L EMERGENCY LIGHT AS PER MM 33-51-10. 2 L 7 2 4F RT A2NM 2008050700010 20080507 00010 NM 2008 5 7 NOCA02708 1 20080429 A 3350 LP101 LIGHT BOEING 757 75728A 1384976 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 TOP POSITION LAMP INOP IN EXIT LOCATOR SIGN AT 3R DOOR SIDEWALL. REPLACED LAMP AT 3R EXIT SIGN AS PER MM 33-51-10. 2 L 7 2 4F RT A2NM 2008050700015 20080507 00015 EU 2008 5 7 CPCP20080016 1 20080327 A 5320 FLOOR SUPPORT AEROSP ATR72 ATR72212 8680945 EU AFT CARGO CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 270AT 270 RT 2 FLOOR CORRODED. RT ZEE FLOOR REPLACED IAW SRM 51-25-03. 2 H 7 2 4T RT A53EU 2008050700018 20080507 00018 WP 2008 5 7 IXXA080015O 1 20080430 A 3040 CONTROLLER DOUG DC8 DC871F 302199D WP WINDSHIELD HEAT MALFUNCTIONED A IXXA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 11 820BX 90411 1332 46065 DURING CLIMB-OUT FROM KTOL, FIRST OFFICERS WINDSHIELD SHATTERED IN FLIGHT CLIMBING THROUGH 25000 FT. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FIRST OFFICERS WINDOW AND WINDOW TEMP CONTROLLER. OPERATIONAL CHECK WAS GOOD IAW DACO MAINTENANCE MANUAL 56-10-2. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2008050700031 20080507 00031 WP 2008 5 7 AALA200800795 1 20080402 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG UNDERSERVICED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7508 49802 DFW INFLIGHT T348/02APR - NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. CREW REPORTED AIR NOISE. FOUND NOSE LAND ING GEAR UNDER SERVICED AND NOSE GEAR SPRAY DEFLECTOR HITTING BRACKET CAUSING GEAR NOT TO RETRACT. SERVICED NOSE LANDIN G GEAR STRUT AND ADJUSTED NOSE GEAR SPRAY DEFLETOR. REPLACED SCHRADER VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008050700035 20080507 00035 SO 2008 5 7 C2XA08RI056 1 20080423 A 3320 BR90002 BALLAST EMB 145 EMB145EP 3260221 SO CABIN DEFECTIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14940 145033 FLIGHT 3074 - EWR - FLIGHT CREW REPORTED NR 1 FLUORESCENT TUBE BULB ARCING WITH SMOKE. EWR MX REMOVED AND REPLACED BALL AST AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008050700036 20080507 00036 NM 2008 5 7 UPS08M52105 1 20080120 A 5713 STRINGER DOUG MD11 MD11 3023602 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C RIGHT WING UPPER STRINGER END S-12 SUSPECT CRACK AS MARKED, THRU ACCESS 635BT. HFEC INSP C/OUT PER DA C NDTSPM R.13PART06.10.01.001 & CRACK APPROX 11" FOUND AS MARKED. CRACK AT STR 12 TRIMMED OFF PER SRM 57-20-00 FIG 10V. 1 & EN1064-08. NEW STR 12 & 03EA REP PARTS FAB USING100164 MATL PER SRM 57-20-00 FIG 10V.1.FPI C/OUT PER NDTSPMR.13PART 8 FOUND NO CRACK. HOLES ON NEW STR 12 & REP PARTS PICKED UP PER SRM 57-20-00 FIG 10V.1&EN1064-08. 2 L 7 3 4F RT A22WE 2008050700037 20080507 00037 EU 2008 5 7 CPCP20080026 1 20080404 A 5320 STIFFENER AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 348AE 349 LT UPPER BONDING SPOT BTW STIFFENER ON BL 187.5 AND BL 350 FIND CORRORED. LT UPPER BONDING SPOT BTW STIFFENER ON BL 187 .5 AND BL 350 CORROSION REPAIRED IAW SRM 53-11-10 FIG 403. 2 H 7 2 4T RT A53EU 2008050700038 20080507 00038 WP 2008 5 7 IXXA08SMN123S 1 20080410 A 5347 S2772660 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 3 TRACK WITH CORROSION AT STATION 590.000. REMOV ED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED EXINTING SPLICES (FWD SIDE) AND REMOVED SEGMENT OF DAMAGED TRACK. FABRICATED SPLICES. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW SEGMENT OF TRACK AND SPLICES IAW DC8 SRM 53-2-3 FIGURE 14 PAGES 49-50, DC8 SRM 51-1-8 PAGES 17-18,DC8 SRM 53-2-3 FIGURE 12, DC8 SRM 51-1-8B, 53-7-3 FIGUR E 3E ITEM "H", 51-2-0 FIGURE 50 SHEET 73, 51-3-0, AND 51-3-1. 2 L 7 4 4F RT 4A25 2008050700043 20080507 00043 WP 2008 5 7 08FDEA01718 1 20080501 A 5312 AJC73723 SUPPORT ANGLE DOUG MD10 MD1010F 3022112 WP AFT PRESS BLKHD CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 UPPER INTERMEDIATE AFT FUSELAGE (ZONE 312); AFT PRESSURE BULKHEAD (STA 2007), AFT FACE UPPER CENTER SECTION. THE FUSEL AGE SKIN SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-31-01 & 51-35-01; VOL II; PG 1. ALODINED & PRIMED IAW SRM 51-21-01; VOL II; PG 1. REINSTALLED PANEL IAW SRM 51-31-01; VOL II; PG 1. SEALED PAN EL IAW SRM 51-41-01; VOL II; PG 1. 2 L 7 3 4F RT A22WE 2008050700046 20080507 00046 NM 2008 5 7 UPS08M52106 1 20080120 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C LEFT WING UPPER STRINGER END S11 SUSPECT CRACK AS MARKED, THRU ACCESS 536AB. HFEC INSP C/OUT PER DACN DTSPM R.13 PART06-10.01.001 & CRACK APPROX 11" FOUND CRACK AT STR 11 LT WING TRIMMED OFF PER SRM 57-20-00 FIG 10V.1&EN10 56-08 NEW STR 11 & 03EA REP PARTS FAB USING 1D0164 MATL PER SRM 57-20-00 FIG 1 0V.1R.40&EN1056-08. FPI C/OUT PER NDTSPM R.13 PART8 FOUND NO CRACK. HOLES ON NEW STR 11&03EA REP PARTS PICKED UP PER SRM 57-20-00&EN1056-08. 2 L 7 3 4F RT A22WE 2008050700048 20080507 00048 EA 2008 5 7 A6WA200840324 1 20080414 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING LE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 RIGHT WING L/E AT WS 185.95 QTY 1 L/E SCREW HOLE IS CRACKED IN THE L/E EXTERIOR SKIN AND EDGING. (M) REPLACED IAW REO 601R-57-41-510. (A) 2 L 7 2 4F RT A21EA 2008050700051 20080507 00051 WP 2008 5 7 IXXA08SMN121S 1 20080410 A 5347 S2772660 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 310-425 WORN B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK WITH LUGS WORN AT STATION 310.000 - 425.0 00. REMOVED DAMAGED SEGMENT OF TRACK AND EXISTING SPLICES. CLEANED, TREATED AND PRIMED AREA AND EXISTING SPLICES. INS TALLED SEGMENT OF NEW TRACK AND REINSTALLED SPLICES IAW DC8 SRM 53-2-3 FIGURE 14 PAGES 49-50, 53-7-3 FIGURE 3E SHEETS 1 AND 2, 51-2-0 FIGURE 50 SHEET 73, 51-3-0, 51-3-1, DC8 SRM 53-2-3 FIGURE 14 PAGES 49-56, DC8 SRM 53-1-0 PAGE 1, 51-3-0, A ND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008050700060 20080507 00060 NM 2008 5 7 DHL2008760553 1 20080427 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272B7 138407L NM BS 870-950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED CORRODED SEAT TRACK, FABRICATED, AND INSTALLED SEAT TRACK SECTION AT BS 870 TO 950, RBL 45.5, PER B727 SRM 53-10 -2 FIG 7 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 2008050700061 20080507 00061 NM 2008 5 7 DHL2008760554 1 20080424 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272B7 138407L NM BS 870-950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED CORRODED SEAT TRACK, FABRICATED, AND INSTALLED SEAT TRACK SECTION AT BS 870 TO 950, LBL 24.75, PER B727 SRM 53-1 0-2 FIG 7 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 2008042500045 20080425 00045 EA 2008 4 25 FDKA200804164 1 20080413 A 2611 CONTROL UNIT CNDAIR CL600 CL6002D24 1390016 EA SMOKE WARNING MALFUNCTIONED A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 602LR 15151 FDM FLT 6027 JFK-BOS (0641 PHX LCL). FWD LAV SMOKE WARNING ON GROUND AFTER GROUND CREW PULLED GROUND POWER. MX RE-RACK ED BOTH DCU'S & FIDEX RESET, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008042500058 20080425 00058 SO 2008 4 25 C2XA08SH068 1 20080418 A 5751 14569009410 ATTACH FITTING EMB 145 EMB145LR 3260212 SO RT AILERON WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12569 145630 SHV - DURING C-CHECK THE RIGHT HAND AILERON TO PCA ATTACH FITTING WAS FOUND TO HAVE MIGRATED HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW CONTINENTAL EXPRESS EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008042500067 20080425 00067 SO 2008 4 25 RAIA00804017 1 20080414 A 3350 RPS1B BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 844HK 14500838 PRE FLT 7936 - MSN - SEVERAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BA TTERY. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008042500100 20080425 00100 NE 2008 4 25 ASAA0852819 2 20080417 A 7320 2042M67P02 CONTROL UNIT BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE LT ENGINE MALFUNCTIONED A ASAA O OTHER O OTHER CR CRUISE 1 NM 02 557AS 35176 LEFTHAND ENGINE THROTTLE HAD UNCOMMANDED ADVANCE DISENGAGING THE AUTO THROTTLE. REPLACED ENGINE ELECTRONIC CONTROL. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008042500101 20080425 00101 NM 2008 4 25 KCSA081222 1 20080419 A 5210 ACCESS DOOR BOEING 747 747209B 138489B NM COCKPIT MISRIGGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 714CK 22446 CREW UPPER DECK ACCESS DOOR WILL NOT SHUT PROPERLY. 2 L 7 4 4F RT A20WE 2008042500116 20080425 00116 NM 2008 4 25 YENA2008034 1 20080415 A 2131 2160902AD CONTROLLER EMB ERJ190 ERJ190100IGW 3260408 NM CABIN PRESSURE FAULTY A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 193JB 5409 4908 19000017 FLT 437, BOS-MCO, CABIN ALTITUDE CLIMBING AS LEVELING OFF AT ALT. STARTED DESCENT AND GOT CABIN ALT HI WARNING. KEPT D ESCENDING TO 20,000 FT AND CABIN ALT STABILIZED. DIVERTED TO JFK. MAX CABIN ALT 9800 FT. TROUBLESHOT PER FIM 21-31-00 -810-806-A00. FAULT CODE 2111008CPC. REMOVED AND REPLACED CPCS CONTROLLER FROM FWD AVIONICS IAW 21-31-01. OPS CHECK G OOD, NO FAULTS NOTED. A/C OK FOR SERVICE. 2 L 7 2 4F RT A57NM 2008042500128 20080425 00128 NM 2008 4 25 YENA2008035 1 20080416 A 2120 10014524 CHECK VALVE EMB ERJ190 ERJ190100IGW 3260408 NM NR 2 RAM AIR SYS INOPERATIVE A YENA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 EA 15 193JB 6335 6335 19000017 FLT 1117, SYR-FLL, DIVERTED TO IAD. DURING CRUISE CABIN ALT STARTED CLIMBING UP TO 8200, TRIED MANUAL CONTROL NO RESPON SE. STARTED DESCENT INTO IAD CABIN KEPT CLIMBING TO 9800. THE DIFF MAX WAS 7.0-7.7 AFTER LANDING MAN OUTFLOW VALVE CON TROL WORKED. AUTO PRESS NEVER WORKED AFTER MULTIPLE ATTEMPT TO RESET. PERFORMED GVI OF RAM AIR INLET DUCTS IAW 21-25-0 5, NO DEFECTS NOTED. PERFORMED PACK OUTLET DUCT GVI IAW 21-51-21, NO DEFECTS NOTED. PERFORMED OPS CHECK OF COOLING PAC KS. FOUND NR 2 PACK DISCHARGE AIR ESCAPING THROUGH RAM AIR CHECK VALVE AND FREEZING NR 2 WATER SPRAY NOZZLE. PERFORMED EMERGENCY RAM AIR CHECK VALVE OPERATIONAL. CHECK OPS TEST FAIL IAW AMM 21-25-03-710. FOUND FLAPPER HOLD OPEN ROD MISS 2 L 7 2 4F RT A57NM 2008042500135 20080425 00135 NM 2008 4 25 DXTA200802995 1 20080413 A 3150 SHROUD AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE APU CONTAMINATED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 259QS 159 STRONG ODOR OF HOT OIL DURING DESCENT. EVALUATED AND FOUND BURNED OIL IN APU BLEED AIR SHROUD. REMOVED APU P/N 3800548 -2 S/N P-295 AND INSTALLED REPAIRED UNIT P/N 3800548-2 S/N P-358 (T.T. 3165, CYCLES 3212). RUN UP, LEAK CHECK, AND OPER ATIONAL CHECK GOOD. ALL MAINTENANCE PERFORMED IAW MM 49-00-00. 2 L 7 2 4F 4 F RT A50NM E44NE 2008042500136 20080425 00136 NE 2008 4 25 MASA200800324 2 20080419 A 7261 6087T04P06 SCAVENGE PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT ENGINE MALFUNCTIONED A MASA O OTHER O OTHER CR CRUISE 1 SW 07 75995 10215 7361 ASH FLT 7140 ORD. RT ENGINE OIL PRESSURE FLUCTUATES AT +/- 6 ABOVE IDLE. CREW DECLARED AN EMERGENCY. REPLACED LUBE S CAVENGE PUMP, OP CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2008042500172 20080425 00172 EA 2008 4 25 COMA0860230 1 20080420 A 2711 AL00102 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA AILERON TRIM FAULTY A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 784CA 30449 7319 FLIGHT 9657 - HESITATION FELT IN CONTROLS WHEN TURNING RIGHT, AUTO-PILOT OFF, ALL HYDRAULICS ON, PILOT AND CO-PILOT SIDE S. DECLARED EMERGENCY, RETURNED TO CVG, LANDED WITHOUT INCIDENT. REPLACED AILERON TRIM ACTUATOR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008042500184 20080425 00184 NM 2008 4 25 ZZDA2008092 1 20080415 A 5514 STRUCTURE BOEING 737 73776N 13844CH NM HORIZ STAB DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 289AT 32673 MDDR 115768T - RT HORIZONTAL STABILIZER HAS DENT AT STA 184. REPAIRED PER B737 SRM 55-10-01 FIG 202. 2 L 7 2 4F RT A16WE 2008042500231 20080425 00231 NM 2008 4 25 SWAA082093 1 20080421 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, RBL 16, WL 152. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042500248 20080425 00248 NM 2008 4 25 2008UALA02340 1 20080421 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S8L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 FUSELAGE STRINGER 8L, STR ATTACH CLIP IS CRACKED AT LWR INBD CORNER BS 360. MAJOR REPAIR ACCOMPLISHED, INSTALLED NEW CL IP. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042500330 20080425 00330 NM 2008 4 25 ASAA0892834 1 20080324 A 5321 147A581016 FLOORBOARD BOEING 737 737990 NM BS 887-907 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 317AS 30856 CABIN FLOORBOARD STA 887 TO STA 907 DELAMINATED LBL 47 TO LBL 63. PREPARED DAMAGED AREA APPLIED POTTING COMPOUND BMS 5 28 TYPE 19 AND 4 LAYERS BMS 9 3, FABRIC REPAIR PLY BONDED DAMAGED AREA IAW B737 900 SRM 53 00 50 REP 6 PG 201 203. 2 L 7 4 4F RT A16WE 2008042500332 20080425 00332 NM 2008 4 25 ASAA0892836 1 20080324 A 5321 147A5810345 FLOORBOARD BOEING 737 737990 NM BS 907-946 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 317AS 30856 CABIN AFT FLOORBOARD STA 907 TO STA 946 LBL 17 TO LBL 50 IS DELAMINATED AT INSERTS. PREPARED DAMAGED AREA APPLIED POTTI NG COMPOUND BMS 5 28 TYPE 19 AND 4 LAYERS OF BMS 9 3 1581, FABRIC REPAIR PLY BONDED IAW B737 900 SRM 53 00 50 REP 1 PGS 201 202. 2 L 7 4 4F RT A16WE 2008042800003 20080428 00003 EA 2008 4 28 A6WA200840261 1 20080325 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 FOUND CORROSION ON RIGHT OUT LE, WS 249 INBOARD SIDE UPPER RIB. (M) CORROSION REMOVED IAW SRM 51-21-06 AND TREATED IAW SRM (51-21-11) (51-25-06). 2 L 7 2 4F RT A21EA 2008042800019 20080428 00019 WP 2008 4 28 MWEA080057 1 20080421 A 3320 2LA00727850 LIGHT DOUG DC9 DC981 3022081 WP CABIN BURNED OUT A MWEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 13 814ME 48010 PASSENGER AT RIGHT EXIT ROW CLAIMED HE SAW A PUFF OF SMOKE AND SMELLED A SULFUR ODOR, ODOR DISSIPATED NOTHING ELSE ABNOR MAL. FOUND READING LIGHT AT 19F BURNED OUT. REMOVED AND REPLACED READING LIGHT ASSEMBLY. 2 L 7 2 4F A6WE 2008042800026 20080428 00026 NM 2008 4 28 BB08066 1 20080420 A 3320 LIGHT BOEING 757 7572S7 1384962 NM CABIN BURNED OUT A USAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 905AW 23567 PHX FLT 332 - EN ROUTE PHX TO SJD. THE CABIN CREW REPORTED AN ELECTRICAL SMOKE ODOR IN THE REAR CABIN OF THE AIRCRAFT. THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC, AND REQUESTED THE CABIN CREW TO TURN OFF THE IN-FLIGHT ENTERTAINMENT E QUIPMENT. WITH THE EQUIPMENT TURNED OFF, THE ODOR DISSIPATED WHILE THE FLIGHT RETURNED TO PHX, LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE IN-FLIGHT ENTERTAINMENT SYSTEM, AIR CONDITIONING SYSTEM, THE AFT GALLEY AND LAVATOR IES, CABIN LIGHTING SYSTEMS, AND THE AFT CARGO BAY FOR ELECTRICAL ODORS AND OVERHEAT CONDITIONS. NO ODORS WERE DETECTED , HOWEVER, THE CEILING LIGHTS BY ROW 30 WERE REPLACED. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2008042800043 20080428 00043 NM 2008 4 28 SWAA082116 1 20080421 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042800077 20080428 00077 EA 2008 4 28 A6WA200840282 1 20080401 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 CRACK FOUND ON CARGO BAY FLOOR SILL FS 562.72-589. (M) CARGO BAY FLOOR SILL FS 562.72 TO FS 589.00 REPAIRED IAW REO 60 1R-53-61-690 REV D. 2 L 7 2 4F RT A21EA 2008042800079 20080428 00079 EA 2008 4 28 A6WA200840283 1 20080404 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 605-621 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 CARGO FLOOR SILL CORRODED FS 605 TO 621, RBL 45. (M) CORROSION REMOVED ON CARGO FLOOR SILL IAW SRM 51-21-06. 2 L 7 2 4F RT A21EA 2008042800115 20080428 00115 NM 2008 4 28 ASAA0852825 1 20080421 A 2160 3989083 MODULATING VALVE BOEING 737 737890 1384527 NM CABIN TEMP MALFUNCTIONED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 577AS 4403 4403 35186 CABIN TEMPERATURE ZONE CONTROL ANNUNCIATED. REPLACED TEMPERATURE TRIM MODULATING VALVE. 2 L 7 2 4F RT A16WE 2008042800117 20080428 00117 EA 2008 4 28 A6WA200840268 1 20080324 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 461 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 FS 461 RBL 9 FLOOR SUPPORT FITTING FOUND CRACKED LENGTH OF CRACK IS .400 INCH. (M) NEW FLOOR BEAM FITTING INSTALLED IA W SRM 51-42-21. 2 L 7 2 4F RT A21EA 2008042800118 20080428 00118 EA 2008 4 28 A6WA200840269 1 20080325 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 FLOORBEAM 280 FOUND CRACKED AT LBL 9 AND RBL 9 WL 73.50 (2 PLACES). (M) REPAIRED IAW REO 601R-53-11-171 REV D SCHEME B . 2 L 7 2 4F RT A21EA 2008042800119 20080428 00119 EA 2008 4 28 A6WA200840323 1 20080411 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 31 431AW 7265 ABORTED TAKEOFF DUE TO CONFIG FLAP WARNING. FLAP INDICATION SHOWED 3 DEGREES WHEN SELECTED TO 8 DEGREES. TAKEOFF ABORT ED AT 60 KNOTS. BTMS INDICATED 3-3-5-3. INTERROGATED FECU PER AMM 27-50-00. NO DEFECTS NOTED. RESET FLAP SYSTEM IAW FIM PROCEDURES. OPS CHECK OF FLAP SYSTEM GOOD IAW AMM 27-51-01. ACFT OK FOR RETURN TO SERVICE. 2 L 7 2 4F RT A21EA 2008042800139 20080428 00139 NM 2008 4 28 SWAA082171 1 20080423 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, LBL 7 TO RBL 4.5, WL 198 TO WL 206. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008042800140 20080428 00140 NM 2008 4 28 SWAA082170 1 20080423 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042800141 20080428 00141 NM 2008 4 28 SWAA082169 1 20080423 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008042800143 20080428 00143 NM 2008 4 28 SWAA082167 1 20080423 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2008042800144 20080428 00144 NM 2008 4 28 SWAA082178 1 20080423 A 3350 20131A BATTERY PACK BOEING 737 7373K2 13844BA NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED MV3 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008042800145 20080428 00145 NM 2008 4 28 SWAA082176 1 20080423 A 3350 MS155721 LIGHT BOEING 737 7373K2 13844BA NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008042800146 20080428 00146 NM 2008 4 28 SWAA082177 1 20080423 A 3350 MS155721 LIGHT BOEING 737 7373K2 13844BA NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 340LV 23738 DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008042800148 20080428 00148 NM 2008 4 28 SWAA082150 1 20080422 A 5755 654645168A SKIN BOEING 737 7373H4 1384600 NM NR 6 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 RIGHT NR 6 SPOILER DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2008042800154 20080428 00154 NM 2008 4 28 SWAA082194 1 20080423 A 5524 69444273 ROD END BOEING 737 7373H4 1384600 NM LT ELEVATOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND LT ELEVATOR CONTROL SYSTEM UPPER CONTROL ROD END CORRODED. REMOVED AND REPLACED ROD E ND PER MM. 2 L 7 2 4F RT A16WE 2008042800157 20080428 00157 NM 2008 4 28 SWAA082153 1 20080423 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042800159 20080428 00159 NM 2008 4 28 SWAA082172 1 20080423 A 5753 6546435339 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP INBOARD UPPER AND LOWER SURFACE DELAMINATED. REMOVED A ND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2008042800168 20080428 00168 NM 2008 4 28 SWAA082134 1 20080422 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 840, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042800171 20080428 00171 NM 2008 4 28 2008UALA02403 1 20080424 A 2150 106050610 ACM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE LEFT FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 902UA 25002 SIGNIFICANT OIL SMELL IN CABIN ON START UP AND DESCENT. FOUND RT AIR CYCLE MACHINE FAILED. REPLACED AIR CYCLE MACHINE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042800173 20080428 00173 NM 2008 4 28 2008UALA02281 1 20080419 A 5730 PANEL BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE RT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 666UA 29238 MOST INBOARD LOWER RT LEADING EDGE PANEL INBD CORNER BROKEN OFF. APPROX. 3 INCH BY 1-2 INCH REINFORCED LEADING EDGE SEC TION MISSING. REMOVED FOR REPAIR. REPAIRED BY SHOP. REINSTALLED PANEL. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042800181 20080428 00181 NM 2008 4 28 2008UALA02372 1 20080422 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1600-1620 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 AFT PIT INTERCOSTAL HAS CORROSION BETWEEN BS 1600 AND 1620 STR 29L AND 30. MAJOR REPAIR ACCOMPLISHED, REMOVED EXISTING INTERCOSTAL AND INSTALLED NEW INTERCOSTAL AT STA 1600 TO 1620 BTWN STR S29L AND 30. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042800186 20080428 00186 EA 2008 4 28 A6WA200840289 1 20080403 A 5210 COVER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 PAX DOOR FORWARD AND AFT UPPER CORNER COVERS FOUND CRACK. (M) PAX DOOR FWD AND AFT UPPER CORNER COVERS REPLACED WITH S ERVICEABLE ITEMS IAW SRM 51-42-13. 2 L 7 2 4F RT A21EA 2008042800187 20080428 00187 NM 2008 4 28 2008UALA02245 1 20080417 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1700 S19-20L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 DOUBLER INSTALLED STA 1700 STR 19 TO 20L. SUPPLEMENTAL , REPAIR ACCOMPLISHED: REMOVED EXISTING REPAIR DOUBLER AND VERIF IED ALL DAMAGE REMOVED BY HFEC INSPECTION. FABRICATED AND INSTALLED A NEW DOUBLERAND STRUCTURAL FILLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042800197 20080428 00197 NM 2008 4 28 SWAA082160 1 20080423 A 5754 65C26601 SLAT BOEING 737 7375H4 138449D NM RT WING DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 L/E SLAT INBOARD T/E DISBONDED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008042800201 20080428 00201 NM 2008 4 28 SWAA082184 1 20080423 A 3350 65C27093 LIGHT BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080523 NM 2008 5 23 USAA920081047 1 20080418 A 5322 146N542111 SHEAR TIE BOEING 757 7572S7 1384962 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - CORROSION ON SHEAR TIE, BS 1376, RBL 24. REPLACED SHEAR TIE, BS 1376, RBL 24 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008042800209 20080428 00209 NM 2008 4 28 2008UALA02404 1 20080423 A 5753 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FORE FLAP GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 RT OB TRAILING EDGE FOREFLAP HAS GOUGE APPROX .020 IN DEEP LOCATED .75IN INBD OF WBL 414.38. REPAIRED THE RIGHT HAND OU TBOARD FORE FLAP LEADING EDGE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042800212 20080428 00212 NM 2008 4 28 SWAA082137 1 20080422 A 3350 20131A BATTERY PACK BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED MV2 CHECK, FOUND MID CABIN CENTER AISLE OVERWING EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTER Y PACK PER MM. 2 L 7 2 4F RT A16WE 2008042800219 20080428 00219 NM 2008 4 28 SWAA082185 1 20080423 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042800221 20080428 00221 NM 2008 4 28 SWAA082140 1 20080422 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042800223 20080428 00223 NM 2008 4 28 2008UALA02413 1 20080424 A 3510 89151114 BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 CREW AND PASSENGER OYXGEN LOW AT 1620 AND 1590 PSI RESPECTIVELY . SERVICED OXYGEN SYSTEM NO LEAKS NOTED. AC OK FOR SERVI CE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042800225 20080428 00225 NM 2008 4 28 2008UALA02414 1 20080424 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EEL LT INOP, ROW 58 LT. FOUND FAULTY LAMP. REPLACED LAMP OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042800226 20080428 00226 NM 2008 4 28 2008UALA02299 1 20080419 A 5240 BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1R FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 DOOR 1R WILL NOT ARM. EMERGENCY LINKAGE TORQUE TUBE BEARINGS SEIZED. REPLACED TORQUE TUBE BEARINGS, DOOR OPS NORMAL LY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042800233 20080428 00233 NM 2008 4 28 2008UALA02304 1 20080420 A 5753 STRUCTURE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE TE FLAP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 905UA 25005 RT INBD FWD FLAP LWR SURFACE HAS 1-2 INCH HOLE FROM EMBEDDED ROCK 1 FOOT FROM INBD EDGE AND 6 INCH FROM TRAILING EDGE. FOUND FOD DAMAGE. REPLACED INBOARD FORE FLAP PER MM 27-51-07. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042800236 20080428 00236 NM 2008 4 28 2008UALA02306 1 20080420 A 2150 ACM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LEFT FROZEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 LEFT PACK AIR CYCLE MACHINE FROZEN. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042800238 20080428 00238 NM 2008 4 28 SWAA082166 1 20080423 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 756SA 27872 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008042800247 20080428 00247 EA 2008 4 28 SWIA200819532 1 20080118 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 431SW 7536 RIGHT ENGINE MOUNT THRUST SHAFT BALL FITTING IS CORRODED, FOUND AT C-CHECK. REPLACED RIGHT ENGINE THRUST SHAFT PER CRJ2 00 AMM 71-22-01-000-801. 2 L 7 2 4F RT A21EA 2008042800250 20080428 00250 2008 4 28 SWIA200819535 2 20080422 A 7320 4120T02P03 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA COMPRESSOR LEAKING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 701SK 10133 FLT 6438 - FUEL LEAK FROM RIGHT ENGINE. REPLACED MASTER COMPRESSOR ACTUATOR PER CRJ 700 MM 75-30-03. 2 L 7 2 4F RT A21EA 2008042800256 20080428 00256 EU 2008 4 28 08FDEA01530 1 20080424 A 5320 A2151040100000 FAIRING AIRBUS 300 A300F4605R 3930327 EU ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 AIR CONDITIONING EXTERNAL FAIRING NR 143 GL IS DELAMINATED. REMOVED THE DAMAGE; PREPPED AREA FOR REPAIR; APPLIED A LAY -UP REPAIR; REFINISHED SURFACE IAW SRM 51-77-12 & SRM 53-15-73. 2 L 7 2 4F RT A35EU 2008042800257 20080428 00257 EU 2008 4 28 08FDEA01531 1 20080424 A 5350 A2151037700100 PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 AIR CONDITION EXTERNAL FAIRING PANEL NR 144 HR IS DELAMINATING ON THE INTERNAL SKIN. REPAIRED PANEL BY REMOVING THE DAMA GE AND APPLYING A WET LAY UP IAW SRM 51-77-12 AND RESTORED THE FINISH IAW SRM 51-75-10. 2 L 7 2 4F RT A35EU 2008042800259 20080428 00259 EU 2008 4 28 08FDEA01533 1 20080424 A 7830 STRUCTURE AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 NR 2 ENGINE OUTBD T/R T/E HAS LOOSE COMPOSITE REPAIR EDGE. REPLACED THE NR 2 ENGINE OUTBOARD TRANSLATOR COWL IAW AMM 78- 32-11-4. REFERRED ALL WORK TO NON-ROUTINE N01042. 2 L 7 2 4F RT A35EU 20080516 NM 2008 5 16 SWAA082612 1 20080513 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 234WN 32502 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 10 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008042500211 20080425 00211 NM 2008 4 25 SWAA082105 1 20080421 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 390, RBL 2. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008042500226 20080425 00226 NM 2008 4 25 SWAA082089 1 20080421 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042500230 20080425 00230 NM 2008 4 25 SWAA082091 1 20080421 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042500244 20080425 00244 NM 2008 4 25 2008UALA02336 1 20080421 A 2781 834503 PROXIMITY SWITCH BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 4 SLAT MALFUNCTIONED A UALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 29 676UA 30028 RTFL DUE TO L/E SLAT PROBLEM. REPLACED SLAT 4 INBOARD PROXIMITY SWITCH (S285). 2 L 7 2 4F 4 F RT A1NM E24NE 2008042500269 20080425 00269 NM 2008 4 25 2008UALA02360 1 20080421 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 193UA 26890 EEL LIGHT BROKEN AT SEATS 33HJK. REPLACED LAMP ASSY ON SEAT 33H. OPERATION CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042500326 20080425 00326 NE 2008 4 25 NOCA02608 2 20080422 A 7200 68E3812 CONTROL UNIT BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE FAILED A NOCA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 15 752NA 28174 31331 LEFT ENG AIRBORNE VIBRATION N1 INDICATION 5.0 AMBER BAND AT FL 350. VIBRATION WAS FELT IN THROTTLE AND CONTROL COLUMN. SHORTLY AFTER VIBRATION ONSET AND COMPLETION OF HIGH VIBRATION QRH CHECKLIST. EXPERIENCED A COMPRESSOR STALL AND HIGH EGT, AIRCRAFT DIVERTED TO BKO. ACCOMPLISHED BOROSCOPE AS PER MM 72-00-00, NO DEFECTS NOTED REMOVED AND REPLACED BVCU A ND TPU AS PER MM 75-32-01 AND 75-32-15 OPS CHECK OK 2 L 7 2 4F 4 F RT A2NM E12EU 2008042800024 20080428 00024 NM 2008 4 28 YENA2008036 1 20080420 A 3233 17071000407 UPLOCK ACTUATOR EMB ERJ190 ERJ190100IGW 3260408 NM RT MLG FAILED A YENA O OTHER J WARNING INDICATION AP APPROACH 1 EA 15 192JB 395 395 19000014 FLT 4152, IAD-BOS, UPON LANDING GEAR EXTENSION, BRK CONTROL FAULT LG LEVER DISAG, RIGHT MAIN LANDING GEAR DISPLAYED UNSA FE INDICATION. ALL INDICATIONS RETURNED TO NORMAL WITHIN 1 MINUTE. CYCLED GEARS MANY TIMES AND COULD NOT DUPLICATE FAU LT, AS PRECAUTIONARY REMOVED AND REPLACED RT MLG UPLOCK ACT ASSY WITH 2 EACH NEW SENSORS ALREADY INSTALLED PER MM 32-31- 03. ALSO LUBED MLG UPLOCK ROLLER ASSY PER CMM 32-11-14 MLG SHOCK STRUT PER EMBRAER TECH SUPPORT ENGINEER. OPS CHECKED MANY TIMES, NO FAULTS FOUND. A/C OK FOR CONTINUED SERVICE PER EMBRAER I/C 2008-190/02336A. 2 L 7 2 4F RT A57NM 2008042800059 20080428 00059 NM 2008 4 28 SWAA082126 1 20080420 A 5753 65C26343 CARRIAGE BOEING 737 737317 138447P NM T/E FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 2 MID FLAP CARRIAGE ASSY BEARING SUPPORT WORN. REMOVED AND REPLACED FLAP C ARRIAGE PER MM. 2 L 7 2 4F RT A16WE 2008042800091 20080428 00091 EU 2008 4 28 2008UALA02394 1 20080423 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOORWAY CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 443UA 820 CORROSION ON R2 DOOR SILL AT FRAME 66. ACCOMPLISHED MAJOR REPAIR. CORROSION, INSTALLED REPAIR PER SRM. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042800097 20080428 00097 EU 2008 4 28 2008UALA02402 1 20080423 A 3510 OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE 1ST OBSERVER'S LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 446UA 834 SUSPECT O2 LEAK CAPTOR 1ST OBS MASK FITTING. FOUND 2ND OBS. MASK DISCONNECTED. SUSPECT LEAK FROM THERE. CONNECTED MASK AND CHECKED FITTINGS FOR LEAKS, NONE NOTED, SERVICED CREW O2 TO FULL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042800102 20080428 00102 EA 2008 4 28 A6WA200840280 1 20080330 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS INOPERATIVE A A6WA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 31 441ZW 7777 FLAPS FAILED AT 20 DEGREES, COMPLIED WITH QRH, LANDED DCA. LANDED NORMAL, MAX BTMS READING 4 FOR ALL BRAKES. RESET PER AWAC SUPPLEMENT 98-018B. (M) 2 L 7 2 4F RT A21EA 2008042800150 20080428 00150 EA 2008 4 28 A6WA200840281 1 20080401 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 PAX DOOR LOWER SILL FORWARD AND AFT CLEATS CORRODED. (M) CORROSION REMOVED IAW ARM 51-21-06. 2 L 7 2 4F RT A21EA 2008042800152 20080428 00152 EU 2008 4 28 08FDEA01519 1 20080424 A 5210 FRAME AIRBUS 300 A300F4605R 3930327 EU R1 DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 R-1 DOOR SLIDE ASSY, LOWER INTERNAL FRAME IS CRACKED AT THE AFT CORNER. RECEIVED SERVICEABLE SLIDE TO BE INSTALLED ON W /C 68S5001CP. 2 L 7 2 4F RT A35EU 2008042800153 20080428 00153 NM 2008 4 28 SWAA082152 1 20080420 A 3233 65446916 UPLOCK ACTUATOR BOEING 737 7373H4 1384600 NM NLG FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 NLG DROPS OUT OF WHEEL WELL WHEN GEAR SELECTED TO OFF POSITION. REMOVED AND REPLACED NLG UPLOCK ACTUATOR AND NLG PRIORI TY VALVE PER MM. 2 L 7 2 4F RT A16WE 2008042800155 20080428 00155 NM 2008 4 28 SWAA082195 1 20080423 A 5524 69444273 ROD END BOEING 737 7373H4 1384600 NM LT ELEVATOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND LT ELEVATOR CONTROL SYSTEM LOWER CONTROL ROD END CORRODED. REMOVED AND REPLACED ROD E ND PER MM. 2 L 7 2 4F RT A16WE 2008050700062 20080507 00062 NM 2008 5 7 DHL2008760555 1 20080422 A 5347 BAC15201466 SEAT TRACK BOEING 727 7272B7 138407L NM BS 850-870 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED CORRODED SEAT TRACK, FABRICATED, AND INSTALLED SEAT TRACK SECTION AT BS 850 TO 870, LBL 45.5, PER B727 SRM 53-10 -2 FIG 7 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 2008050700063 20080507 00063 NM 2008 5 7 UPS08452094 1 20080429 A 5330 SKIN BOEING 747 747121 1384871 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 LOWER BELLY SKIN CORROSION. REPAIR DOUBLER INSTALLED AT STA 1780 SRT 50R PER SRM 53-30-03 FIG 1. CATEGORY B REPAIR REQU IRES REPEAT INSPECTION AT 15000 RIGHT CYCLES AND THEN EVERY 3000 FLIGHT CYCLES. 2 L 7 4 4F RT A20WE 2008050700069 20080507 00069 NM 2008 5 7 YENA2008038 1 20080428 A 2740 4165001002 ELECTRONIC UNIT EMB ERJ190 ERJ190100IGW 3260408 NM HORIZ STAB MALFUNCTIONED A YENA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 15 266JB 4962 3502 19000054 AT GATE, NR 2 TRU FAILED UPON SHUTDOWN. FOLLOWED BY RECIRC, SMOKE AND SMELL OF SMOKE IN FWD CABIN. OCCURRED FOLLOWING ENGINE SHUTDOWN AFTER GPU CONNECTED. PERFORMED FIM TASK 21-20-00-810-801-A AND FOUND HS-ACE IMPLODED. NO DAMAGE FOUND IN SURROUNDING AREA. REMOVED AND REPLACED HS-ACE REF MM 27-43-01, OPS CHECK GOOD AFTER HS-ACE REPLACED REF FIM 24-31-00 . 2 L 7 2 4F RT A57NM 2008050700080 20080507 00080 EU 2008 5 7 USAA920080954 1 20080424 A 5347 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 272AY 333 BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 4417 / FR 54 - BS 4842 / FR 58, +Y1959. REPAIRED CABI N SEAT TRACK, BS 4417 / FR 54 - BS 4842 / FR 58, +Y1959 IAW A330 SRM 53-00-15. 2 L 7 2 4F RT A46NM 2008050700083 20080507 00083 WP 2008 5 7 IXXA08SMN118S 1 20080327 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT WING TE FLAP DAMAGED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP SKIN UPPER PLATING NICKED AT STATION XW 112.000. REMOVED FAS TENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC 8 SRM 57-7-1 FIGURE 1 ITEM "D", AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008050700084 20080507 00084 EU 2008 5 7 USAA920080956 1 20080428 A 5347 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 272AY 333 BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 5584 / FR 72 - BS 5759 / FR 75, +Y450. REPAIRED CABIN SEAT TRACK, BS 5584 / FR 72 - BS 5759 / FR 75, +Y450 IAW A330 SRM 53-00-15. 2 L 7 2 4F RT A46NM 2008050700089 20080507 00089 NM 2008 5 7 USAA920080962 1 20080425 A 5320 6546812188 BEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON CABIN BEAM, BS 1011, RBL 7, WL 208. REPLACED CABIN BEAM, BS 1011, RBL 7, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008050700092 20080507 00092 NM 2008 5 7 USAA920080965 1 20080409 A 5320 656731147 CHANNEL BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON CABIN FLOOR HAT CHANNEL, BS 993.5, RBL 13 - RBL 44, WL 208. REPAIRED CABI N FLOOR HAT CHANNEL, BS 993.5, RBL 13 - RBL 44, WL 208 IAW B737 SRM 53-60-51-1A1. 2 L 7 2 4F RT A16WE 2008050700094 20080507 00094 NM 2008 5 7 USAA920080967 1 20080429 A 5320 65479573 WEB BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON WEB, BS 787, - BS 847, S24R, RBL 20. REPLACED WEB, BS 787 - BS 847, S24R, RBL 20 IAW B737 SRM 51-40-05. 2 L 7 2 4F RT A16WE 2008041100139 20080411 00139 NM 2008 4 11 CALA0800311 1 20080311 A 5340 6948985502 ATTACH FITTING BOEING 737 737524 1384721 NM BS 348 S13L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11641 28902 INTERCOSTAL ATTACH CLIP TO FRAME STA 348 AT STR 13 LT IS CRACKED (MARKED). REPAIRED PER PACE EA 641-53-001 CAL AND EC/R A5310-04742. 2 L 7 2 4F RT A16WE 2008041100140 20080411 00140 NM 2008 4 11 CALA0800312 1 20080407 A 5310 6520723U54 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17329 23459 FWD CARGO COMPARTMENT DOOR CUTOUT, AFT FRAME SHOWS CRACK INDICATION WITH HFEC AT LOWER STOP UPPER AREA. REMOVED AND REP LACED FWD CARGO AFT DOOR CUTOUT FRAME PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041100141 20080411 00141 NM 2008 4 11 CALA0800288 1 20080307 A 5340 ATTACH ANGLE BOEING 737 7373T0 1384582 NM BS 294 S11L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18350 23588 CLIP AND ATTACH ANGLE ARE BOTH CRACKED, THAT ATTACH INTERCOSTAL TO FRAME AT STA 294.5 AND STR 11 LT (MARKED). REMOVED & REPLACED CLIP & ATTACH ANGLE THAT ATTACH INTERCOSTAL TO FRAME AT BS 294.5 & S11L PER PACE EA 350-53-003 CAL AND ECRA 53 10-04741. 2 L 7 2 4F RT A16WE 2008041100142 20080411 00142 NM 2008 4 11 CALA0800291 1 20080401 A 5320 654580734 INTERCOSTAL BOEING 737 737524 1384721 NM BS 277-290 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 46625 27529 RT SIDE OF FUSELAGE STA 277 TO 290 NR 9 INTERCOSTAL CRACKED. REPLACED INTERCOSTAL AS REQUIRED IN SRM 51-10-2. 2 L 7 2 4F RT A16WE 2008041100143 20080411 00143 NM 2008 4 11 CALA0800292 1 20080401 A 5330 143T3451 SKIN BOEING 767 767424ER 1385270 NM BS 654 S13R DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76055 29450 FUSELAGE SKIN FOUND DENT AT BS 654A - 654A+22 BETWEEN PAX WINDOW TOP TO S13R. FUSELAGE SKIN BS 654A - 654A+22 REPAIRED AS PER SRM 53-00-01 FIG 201 REPAIR 14 AND MX WORK SHEET FORM 44.0008 ITEM 1-23 ACCOMPLISHED, 53-DIP, PERFORM REPEAT INSP PER SRM 53-00-01 REPAIR 14 TABLE V AFTER 30,000 FROM DELIVERY. 2 L 7 2 4F RT A1NM 2008041100144 20080411 00144 NM 2008 4 11 CALA0800293 1 20080331 A 5315 FLOORBEAM BOEING 767 767424ER 1385270 NM BS 246 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76055 29450 BS 246 FLOORBEAM FWD SIDE STIFFENER FOUND CRACK AT LBL 40. BS 246 FLOORBEAM FWD SIDE STIFFENER AT LBL 40 IS REPAIRED AS PER SRM 53-10-51 REPAIR 4 FIG 201 & EC/RA#5310-04739. 53-DIP RAISED TO INSPECT PER ECRA 5310-04739 PART 2 AT OR BEFORE 3000 CYCLES FROM MAR 27, 2008 AND PERMANENT REPAIR PER PART 3. 2 L 7 2 4F RT A1NM 2008042800163 20080428 00163 NE 2008 4 28 2008UALA02277 2 20080419 A 7210 CHIP DETECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE G/B LEAKING A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 573UA 26685 DIVERTED UNDER AMBER ALERT DUE TO NR 1 ENGINE SHUTDOWN. FOUND MAIN GEARBOX CHIP DETECTOR BAYONET PINS NOT LOCKED & PART IAL INSTALLED & UNSEATING CHIP DETECTOR ASSY POPPET. CLEANED ENGINE, REINSTALLED CHIP DETECTOR. ADDED 16QTS OF MAINTENA NCE OIL. ACCOMPLISHED IDLE ENGINE RUN PER JRH2-5-63 PG2 ITEM 3.A.(2) . AFTER 5 MIN ENG RUN RECHECKED CHIPS ALL NORMAL NO OIL LEAKS 2 L 7 2 4F 4 F RT A2NM E17NE 2008042800182 20080428 00182 NE 2008 4 28 2008UALA02373 2 20080423 A 7230 BLADES BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HPC DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 214UA 30220 777105 NR 1 ENG HPC STG 7 HAS SEVERAL DAMAGED BLADES BEYOND LIMITS AND ARE NOT BLENDABLE. ALSO, HPC STAGE 12 HAS 1 BLADE WITH CRACK BEYOND LIMITS. ENGINE CONDITION MONITORING (ECM) DETECTED AN ENGINE GASPATH PARAMETER SHIFT. SUBSEQUENT BORESCOP E INSPECTION (BSI) FOUND HP COMPRESSOR BLADE DAMAGE. THE ENGINE WAS REPLACED PRIOR TO FURTHER FLIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042800190 20080428 00190 NM 2008 4 28 DL76S080621 1 20080422 A 5330 SKIN BOEING 767 767332 1382001 NM BS 772 S36R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 128DL 24078 FUSELAGE SKIN CORROSION AT FS 772, S-36R LAP JOINT. DAMAGED SKIN CUT OUT AND REINFORCED WITH EXTERNAL DOUBLERS. 2 L 7 2 4F RT A1NM 2008042800199 20080428 00199 NM 2008 4 28 SWAA082159 1 20080423 A 5754 65C26602 SLAT BOEING 737 7375H4 138449D NM RT WING DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND RIGHT WING NR 6 L/E SLAT INBOARD T/E DISBONDED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008042800210 20080428 00210 NM 2008 4 28 SWAA082183 1 20080423 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST DUCT. REPAIRED SKIN PER BOEING SB AND EA. 2 L 7 2 4F RT A16WE 2008042800224 20080428 00224 NM 2008 4 28 SWAA082141 1 20080422 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 635SW 27708 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2008042800248 20080428 00248 EA 2008 4 28 SWIA200819533 1 20080118 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 431SW 7536 LEFT ENGINE THRUST SHAFT BALL FITTING IS CORRODED, FOUND AT C-CHECK. REPLACED LEFT THRUST SHAFT FITTING PER CRJ200 AMM 71-22-01-000-801. 2 L 7 2 4F RT A21EA 2008042800254 20080428 00254 EU 2008 4 28 08FDEA01528 1 20080424 A 5321 A2557158022800 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU FUSELAGE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 EMPENNAGE ACCESS THRU 312 AR, THE FLOORBOARD ON THE LEFT SIDE OF THE A/C FWD OF THE PNEUMATIC DUCT AT FRAME 84 IS DELAMI NATED. FABRICATED NEW PANEL. LOCATED & DRILLED NEW HOLES USING OLD FLOORBOARD AS A TEMPLATE; INSTALLED INSERTS; POTT ED & CURED BOARD EDGES; SANDED EDGES AS NEEDED. APPLIED NON-SKID & PART MARKED PANEL IAW DWG SRZ 25-005, AMM 11-00-00- 00 & GMM 7-0-100. REMOVED AND INSTALLED FLOOR PANEL IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008042800264 20080428 00264 EU 2008 4 28 08FDEA01536 1 20080424 A 7830 SKIN AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER ERODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 NR 2 ENGINE OUTBD T/R, ALL BLOCKER DOORS HAVE EXPOSED COMPOSITE CORE, SKIN IS ERODED. REPLACED THR NR 2 ENGINE THRUST R EVERSER TRANSLATOR COWL IAW AMM 78-32-11-4. REFERRED ALL WORK TO NON-ROUTINE N01042. 2 L 7 2 4F RT A35EU 2008042800266 20080428 00266 NM 2008 4 28 08FDEA01538 1 20080424 A 3150 113851501 HOSE DOUG MD11 MD11F 3023600 NM LEAKING A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 613FE 48749 LEVEL 3 ENG 2 A-ICE DUCT ALERT, COMPLIED WITH QRH, ENG 2 SHUTDOWN. FLIGHT CREW VERBAL REPORTED ALERT CAME ON 45 MINS BE FORE LAND TO NRT. DUCT SENSOR RESISTANCE. PER FIM 30-22-00. FOUND SHORT TO GROUND AT P1-1843, PIN 10 WAS 15KOHM AND PIN 11 WAS 15KOHM. CHECKED BANJO COWL DUCT OVHT SENSORS (D1-90 & D1-91) WAS BOTH SHORT TO GROUND. R/RED BOTH SENSORS (D 1-90 & D1-91) AND RESISTANCE CHECKED NORMAL PER MM 30-22-11-4. AIR SYS TEST PASSED. BOTH PN SAME 35519-4-310. DURING T /S, FOUND WORN AND SEPARATED B-NUT AND FITTING ON AIR TUBE BETWEEN ANTI-ICE MANIFOLD SHROUD AND POPOUT INDICATOR. REPAI RED PIPES PER AMM20-10-01-2 AND INSTALLED HOSE P/N113851-501. 2 L 7 3 4F RT A22WE 2008042800267 20080428 00267 NM 2008 4 28 QXEA200800396 1 20080423 A 3150 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM WARNING LIGHT UNKNOWN A QXEA O OTHER J WARNING INDICATION TO TAKEOFF 1 NM 09 422QX 4150 PDX - ON TAKEOFF ROLL, THE AUTO FEATHER ARM LIGHT ILLUMINATED. DISAPPEARED WITH NO ANNUNICATION AT V1 SPEED. MAINTENAN CE FOUND FAULT CODE 66 AND CLEARED IAW FIM 61-20-02-810-822. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008042800269 20080428 00269 EA 2008 4 28 QXEA200800394 1 20080418 A 3350 M220D4N RELAY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INTERMITTENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 617QX 10130 PDX - FLIGHT 2634 - EMERGENCY LIGHTS CYCLE ON AND OFF. MAINTENANCE REPLACED THE K-135 RELAY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008042800270 20080428 00270 EA 2008 4 28 QXEA200800397 1 20080424 A 3310 LIGHT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT SHORTED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 602QX 10010 SEA - FLIGHT 2507 - CAPTAIN'S CHART HOLDER LIGHT SPARKED AND POPPED THE CIRCUIT BREAKER. MAINTENANCE TIGHTENED THE SCRE WS AND APPLIED LOCKTITE AND ISOLATED THE SCREW HEADS WITH NO CONDUCTIVE TAPE. OPERATIONALS CHECKS GOOD, AIRCRAFT RETURN ED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2008042800277 20080428 00277 EA 2008 4 28 SWIA200819522 1 20080115 A 5510 PIN CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 983CA 7169 LEFT HORIZONTAL STABILIZER PIVOT PIN HAS CORROSION, FOUND AT C-CHECK. REPLACED STABILIZER PIVOT PIN AS REQUIRED PER CRJ 200 AMM 55-10-00-000/400-801 SUBTASK 55-10-00-020/420-001. 2 L 7 2 4F RT A21EA 2008042800279 20080428 00279 EA 2008 4 28 SWIA200819524 1 20080101 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 609SK 10020 COCKPIT FLOOR SUPPORT ANGLE IS CRACKED AT LBL 9, FOUND AT C-CHECK. REPAIRED COCKPIT FLOOR SUPPORT AT FS 280.00 PER CRJ7 00/900 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008042800280 20080428 00280 EA 2008 4 28 SWIA200819525 1 20080101 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 609SK 10020 WEB STIFFENER AT FS 280 AND RBL 26 IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ700 SRM 51-42-06-001-001- A01. 2 L 7 2 4F RT A21EA 2008042800285 20080428 00285 WP 2008 4 28 UPS08852060 1 20080421 A 3350 BATTERY DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:N/A EMERGENCY LIGHTS WON'T TEST. REMOVED AND REPLACED EMERGENCY BATTERY ASSY PER MM 25-00-00. OPS CHEC K GOOD. 2 L 7 4 4F RT 4A25 2008042800290 20080428 00290 NM 2008 4 28 SB08020 1 20080423 A 3230 CIRCUIT BREAKER BOEING 737 7374B7 1384702 NM COCKPIT TRIPPED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 433US 24555 BWI - FLT 1924 - AFTER TAKEOFF FROM BWI, EN ROUTE TO CLT, CAPTAIN REPORTED TO DISPATCH VIA ACARS THAT HE WAS UNABLE TO R ETRACT THE LANDING GEAR. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARE D. MAINTENANCE RESET THE LANDING GEAR LATCH CIRCUIT BREAKER AND LUBED THE GEAR HANDLE. OPERATIONAL CHECK GOOD WITH AIR CRAFT IN SIMULATED AIR MODE. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2008042800294 20080428 00294 NM 2008 4 28 USAA920080914 1 20080328 A 5312 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 23634 CLT - MAJOR REPAIR - C22 CHECK - CRACKED BULKHEAD WEB, BS 178, LBL 5.5, WL 213. REPAIRED BULKHEAD WEB, BS 178, LBL 5.5, WL 213 IAW B737 SRM 53-10-08 REPAIR 9. 2 L 7 2 4F RT A16WE 2008042800296 20080428 00296 EU 2008 4 28 USAA920080916 1 20080419 A 5347 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 272AY 333 BFM - MAJOR REPAIR - C2 CHECK, CORROSION ON CABIN SEAT TRACK, BS 4258 / FR 53.7 - BS 4417 / FR 54, -Y450. REPAIRED CABI N SEAT TRACK, BS 4258 / FR 53.7 - BS 4417 / FR 54, -Y450 IAW A330 SRM 53-31-15. 2 L 7 2 4F RT A46NM 2008042800297 20080428 00297 NM 2008 4 28 USAA920080917 1 20080412 A 5753 6546431279SP FLAP BOEING 737 73733A 1384673 NM LT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - LEFT WING OUTBOARD FOREFLAP HAS DELAMINATED AREA, WBL 278.69 - WBL 280.69. REPAIRED LE FT WING OUTBOARD FOREFLAP, WBL 278.69 - WBL 280.69 IAW B737 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2008042800301 20080428 00301 CE 2008 4 28 106CG041108 1 20080411 A 3242 50041905 BRAKE ASSY BEECH MU300 400A 1155402 CE MLG LOCKED E UVCA O OTHER E VIBRATION/BUFFET LD LANDING 1 CE 03 106CG 47 RJ12 RT MAIN BRAKE LOCKED ON LANDING, CAUSING TIRE TO GO FLAT. 2 H 7 2 4F RT A16SW 2008042800319 20080428 00319 EA 2008 4 28 010804CR01 1 20080115 A 2741 84541 ACTUATOR CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* 30015 NE HORIZONTAL STAB DISENGAGED E TVMA O OTHER J WARNING INDICATION CR CRUISE 1 EA 03 604CR 5778 5418 HORIZONTAL STAB TRIM ACTUATOR CHANNEL ONE DISENGAGES WHEN ACTIVATED. 2 L 7 2 4F 4 F RT A21EA 2008042800332 20080428 00332 CE 2008 4 28 GUUA04110801 1 20080411 A 3230 LANDING GEAR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE MALFUNCTIONED A GUUA O OTHER O OTHER CL CLIMB 1 SO 29 69547 UE189 FLIGHT:9197, AFTER TAKEOFF LANDING GEAR TOOK MANY ATTEMPTS TO RETRACT EVEN WITH THE (J) HOOK PUSHED DOWN. CONTINUED, LAN DED WITHOUT INCIDENT. PERFORMED LANDING GEAR OPERATIONAL CHECK NO DEFECTS NOTED. 2 L 7 2 4T 4 T RT A24CE E26NE 2008042800335 20080428 00335 CE 2008 4 28 GUUA04130802 1 20080413 A 5540 10164001415 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE UPPER RUDDER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81533 UE137 DURING SCHEDULED ROUTINE MAINT, DISCOVERED UPPER RUDDER HINGE BRACKET EXFOLIATED. REPLACED UPPER RUDDER HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2008050100007 20080501 00007 CE 2008 5 1 DXTA200803002 1 20080416 A 3240 38581501 PRESSURE SENSOR CESSNA 500 560CESSNA 2076750 CE BRAKES INOPERATIVE E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 312QS 6974 5600312 ON TAXI OUT TO RUNWAY, CAPTAIN PRESSED BRAKES AND BRAKES WENT TO STOPS WITH NO PRESSURE.TROUBLESHOT TO DEFECTIVE PRESSUR E SWITCH. REMOVED AND INSTALLED NEW CUSTOMER SUPPLIED SWITCH PER 560 MM 32-42-05 ACCOMPLISHED OPS CHECKS LEAK CHECKS NO DEFECTS NOTED. 2 L 7 2 4F RT A22CE 2008042800339 20080428 00339 SW 2008 4 28 EVCA022308001 1 20080223 A 5302 206032308103 FRAME BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL BS 230 CRACKED E EVCA K NONE O OTHER IN INSP/MAINT 1 CE 03 4338D 51560 CAE895152 TAILBOOM ATTACH FRAME FOUND CRACKED DURING SCHEDULED INSPECTION. 1 G 7 1 3U 3 U H2SW E1GL 2008042800346 20080428 00346 CE 2008 4 28 041508N521CS1 1 20080415 A 3260 GE387 BULB CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG INDICATOR BURNED OUT E Z5FA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 63 521CS 5605362 ON APPROACH, WHEN GEAR WAS EXTENDED, NOSE GEAR DOWN INDICATION FAILED TO ILLUMINATE. CREW CONTACTED ATC AND ABORTED APP ROACH TO WORK AFM CHECK LIST FOR GEAR PROBLEM. STILL UNABLE TO GET GEAR DOWN INDICATION, CREW DECLARED EMERGENCY, BLEW GEAR DOWN AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH NOSE GEAR ANNUNCIATOR BULBS INOPERATIVE. BULBS WERE REP LACED, EMERGENCY GEAR BOTTLE WAS RESET AND SERVICED, GEAR RETRACTION SYS FUNCTIONALLY CHECKED SATISFACTORY AND AC RETURN ED TO SERVICE. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008042800352 20080428 00352 NM 2008 4 28 BB08067 1 20080420 A 2560 P2070001214 FLASHLIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 924UW 22204 CLT - THE FLASHLIGHT AT DOOR L-2 WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT AT DOOR L-2. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 2008042800353 20080428 00353 NM 2008 4 28 BB08068 1 20080421 A 2560 PA010021 BATTERY BOEING 757 7572B7 1384964 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 934UW 27200 LAS - THE LEFT OUTBOARD FLASHLIGHT IN AFT GALLEY WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN THE LEFT OU TBOARD FLASHLIGHT IN AFT GALLEY. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 2008041400017 20080414 00017 EA 2008 4 14 N6WA0080303 1 20080326 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE CABIN INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 154GJ 10224 5399-ORD- 2ND FROM REAR CEILING EMERGENCY FLOODLIGHT INOP. DEFERRED IAW MEL 33-51-02A. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008041400022 20080414 00022 SO 2008 4 14 DJFA2008036 1 20080329 A 3150 DISPLAY EMB 135 EMB135BJ 3260306 SO ALLSN AE300 AE3007A GL NR 3 EICAS SMOKE E DJFA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 904LX 145780 IN FLIGHT CREW REPORTED EICAS FAIL ACCOMPANIED WITH SMOKE IN THE COCKPIT. THE EICAS DISPLAY CIRCUIT BREAKER TRIPPED AND THE SMOKE DISSIPATED. MAINTENANCE FOUND THE NR 3 EICAS DISPLAY INOPERATIVE. AN INSPECTION OF ALL ASSOCIATED WIRING WAS COMPLIED WITH. NO DEFECTS WERE NOTED. THE DISPLAY WAS REPLACED, NO FURTHER SMOKE WAS NOTED AND THE AIRCRAFT WAS RETUR NED TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 2008041400027 20080414 00027 CE 2008 4 14 20061087 1 20080328 A 5311 12944004471 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS495 S3L BENT A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 261GL UE261 FRAME SECTION AT FS. 495.75 STRINGER 3L BENT. MAINTENANCE REPLACED THE BENT INTERCOSTAL AT FS 495.75 STRINGER 3L IAW SRM 51-40. PN 129-440044-71. 2 L 7 2 4T 4 T RT A24CE E26NE 2008041400035 20080414 00035 CE 2008 4 14 DXYA200800003 1 20080401 A 7820 20500121 BOLT CESSNA 177 177RG 2073709 CE LYC O360 IO360A1B6 41514 EA MUFFLER BROKEN E DXYA K NONE O OTHER IN INSP/MAINT 1 GL 07 34072 100 177RG0960 L1573251A PILOTS HAD REPORTED SLIGHT ROUGHNESS AT IDLE. DURING INSPECTION FOUND RT OB MUFFLER SUPPORT BRACKET UPPER ATTACH BOLT N R 2050012-1 BROKEN. THIS BOLT SUPPORTS BRACKET AS WELL AS NR 3 CYLINDER INTAKE TUBE. INTAKE TUBE LOOSE ALLOWING INDUCT ION AIR LEAK AS WELL AS FUEL LEAKAGE INTO ENGINE COMPARTMENT. PART FAILURE DUE TO LOAD AND VIBRATION. 1 H 7 1 3O 3 O A20CE 1E10 2008041400039 20080414 00039 CE 2008 4 14 0805714 1 20080327 A 3260 824006 PROXIMITY SWITCH RKWELL NA265 NA26565 7630107 CE MLG UNKNOWN E DGCA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 570R 46575 RED LIGHT IN MLG HANDLE. 2 L 7 2 4J A2WE 2008041400046 20080414 00046 CE 2008 4 14 DJFA2008039 1 20080406 A 3240 C100169 VALVE BEECH MU300 400A 1155402 CE MLG MALFUNCTIONED E DJFA O OTHER O OTHER LD LANDING 1 EA 23 470LX RK478 CREW REPORTED LOSS OF BRAKES UPON TOUCHDOWN WITH ANTI-SKID IN THE ON OR OFF POSITION. EMERGENCY BRAKES WERE USED TO STO P THE AIRCRAFT. MAINTENANCE REPLACED BOTH BRAKE MIXING VALVES. 2 H 7 2 4F RT A16SW 2008041400051 20080414 00051 NM 2008 4 14 DXTA20082986 1 20080407 A 3150 WARNING MESSAGE GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 708QS 069 AFTER TAKEOFF, ELEVATOR FEEL FAIL MESSAGE CAME ON. 2 L 7 2 4F 4 F RT A53NM E35NE 2008041400055 20080414 00055 SO 2008 4 14 GUUA04010801 1 20080401 A 5210 DOOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE JAMMED A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 285AS 120265 FLIGHT: 9154, PILOT REPORTED FWD DOOR DOES NOT OPEN SMOOTHLY, IT JAMS WHEN OPERATING LEVER. FWD DOOR OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 2008041400084 20080414 00084 CE 2008 4 14 DXTA200802979 1 20080404 A 2150 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT ODOR E DXTA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 07 921QS 7500241 DURING GEAR RETRACTION, CABIN SPIKED 4000 FPM (CLIMB) AND A STRONG ENVIROMENTAL BURNING ODOR APPEARED. REMOVED & REPLAC ED COCKPIT ACM, OPERATIONALY CHECKS GOOD. IAW MM 21-51-00, CLEANED WATER SEPARATOR CLOTHS. IAW MM 12-10-01. ACCOMPLISHE D PRESSURIZATION MAINTENANCE TESTS WITH NO DISCREPANCIES NOTED IAW MM 21-30-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008041400107 20080414 00107 NM 2008 4 14 HALA0800518 1 20080405 A 5314 KEELBEAM BOEING 767 76733A 1385209 NM BS 966 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 587HA 33421 LEVEL 1 CORROSION AROUND KEEL BEAM CHORD FLANGE AT FAIRING PANEL ATTACH HOLE RBL 9.5, STA 966. REWORK OF CORROSION AREA IAW SRM 53-50-12 /1AO1 REV 76 TABLE 2 REV 76, WITHIN LIMITS AND COMPLETED SRM 53-50-12/2RO1, REV 76 REPAIR 2, WITHIN SR M LIMITS. 2 L 7 2 4F RT A1NM 2008041400110 20080414 00110 EU 2008 4 14 MALA080057 1 20080331 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 231-258 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 457XJ 340B457 GALLEY SEAT TRACK CORRODED AT STA 231 TO STA 258. NEW GALLEY SEAT TRACK INSTALLED IAW SRM 51-40-22. 2 L 7 2 4T RT A52EU 2008041400111 20080414 00111 EU 2008 4 14 08FDEA01377 1 20080410 A 5754 A57840056202 PANEL AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT LT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOLDING NOSE SLAT NR 1 LT WITH CRACK FINDINGS REPAIR PERFORMED BY PERFORMING SB 57-6067 (INNER PAN REPLACEMENT). 2 L 7 2 4F RT A35EU 2008041400115 20080414 00115 WP 2008 4 14 08FDEA01381 1 20080410 A 5347 6071587075T6 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 361FE 48260 MCD SEAT TRACK RBL 27 STA 755 HAS A LOBE GOUGED. BLENDED DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED AN D INSTALLED NEW TRACK IAW SRM 53-70-00. NEW TRACK AND SPLICE FABBED ON TRAVELER T8/733018 AND T8/733020. REMOVED AND R EINSTALLED AND SEALED FLOOR PANELS IAW MM 53-21-08-2. REPAIR CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008041400120 20080414 00120 EA 2008 4 14 A6WA200840251 1 20080326 A 2760 SWITCH CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A A6WA O OTHER N FALSE WARNING CL CLIMB 1 GL 31 440AW 7766 CPLT ROLL CMD MESSAGE ON ED2 INFLIGHT. GREEN CPLT ROLL LIGHT ILLUMINATED ON GLARESHIELD. ALL FLIGHT CONTROL RESPONDED NORMAL. REPLACED CO-PILOT ROLL PRIORITY SWITCH PER AMM 27-61-20. OPS TEST GOOD. ALSO, PERFORMED OPS TEST OF ROLL PRIO RITY SYSTEM PER AMM TASK 27-61-20-710-810. NO DEFECTS NOTED. OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2008041400126 20080414 00126 NM 2008 4 14 NWAA081505813 1 20080409 A 3350 LAMP BOEING 757 757351 1384991 NM EXTERNAL E LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 593NW 32993 DURING OVERNIGHT MAINTENANCE, TECHNICIAN FOUND THE EXTERIOR EMERGENCY LIGHT INOP AT DOOR 2 LEFT. MAINTENANCE RELAMPED TH E EXTERIOR EMERGENCY LIGHT AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A2NM 2008041400130 20080414 00130 EU 2008 4 14 F3LA200800136 1 20080406 A 5347 D53112827201 DUMMY RAIL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 C-CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON DUMMY RAIL Y503.2 AT FRAME 16. MAINTENANCE REMOVED AND REPLACED DUMMY RAIL IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE INSTALLATION THE NEW R AIL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041400134 20080414 00134 EU 2008 4 14 F3LA200800139 1 20080404 A 5320 D53471124201 SHEAR PLATE AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 C-CHECK INSPECTION REPORTED CORROSION WAS FOUND ON SHEAR PLATE AT FLOORBEAM Y1732 AFT OF FRAME 69. MAINTEN ANCE REMOVED AND REPLACE SHEAR PLATE IN ACCORDANCE WITH SRM 51-42-11 PARAGRAPH 6, 7, 13 AND EA A9-53R-30196. UPON COMPL ETION OF THE INSTALLATION OF THE SHEAR PLATE IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041400135 20080414 00135 NM 2008 4 14 HALA0800520 1 20080408 A 3150 UNKNOWN BOEING 717 717200 1383700 NM UNKNOWN A HALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 487HA 55132 ENGINE AND ALERT DISPLAY WHITE BOXED FLAP INDICATION. ACCOMPLISHED AMM 27-50-01, NO FAULTS NOTED. ACCOMPLISHED FIM 27- 50-00 FIG 104 NO FAULTS. ACCOMPLISHED FIM 31-51 TASK 817, VIABLE PER FIM 31-61 TASK 801, AUTO FLT BITE PER FIM 22-10 TA SK 801, NO FAULTS NOTED. OK FOR SERVICE. 2 L 7 2 4F TR A6WE 2008041400137 20080414 00137 EU 2008 4 14 TRBA2008038 1 20080408 A 3350 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU EMERGENCY LIGHT FAILED A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 29 529AM 529 FLOOR EMERGENCY LIGHTS ILLUMINATES DIM WHEN OPERATED. REMOVED AND REPLACED BATTERY PACK FIN NR 61WL AND 73WL. ALSO REM OVED AND REPLACED POWER SUPPLY FIN NR 73WL AS PER M/M NR 33-51-21. PERFORMED OPT CK IAW JIC NR 33-50-00 AND FOUND SATIS FACTORY. FOR P/N AND S/N INFO PLEASE REFER TO NRWC NR 202165, CAS AWAITING FROM RECORDS DEPT TO FORWARD THIS NRWC IN OR DER TO FILL OUT P/N AND S/N INFO BLOCKS.. 2 H 7 2 4T RT A53EU 2008041400142 20080414 00142 SO 2008 4 14 SWIA200819457 1 20080404 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 220SW 120288 FOUND CORROSION AT FRAME 21 AT LOWER RIGHT SIDE. REPAIRED IAW IC2008-12/02091. 2 L 7 2 4T RT A31SO 2008041400164 20080414 00164 WP 2008 4 14 NWAA081559861 1 20080318 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 770NC 47758 DURING LINE CHECK, THE EMERGENCY OVERWING EXIT SIGNS AT ROWS 10, 11, AND 12 WERE FOUND TO BE INOPERATIVE. MAINTENANCE R EPLACED THE EMERGENCY EXIT LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM. 2 L 7 2 4F RT A6WE 2008041400165 20080414 00165 WP 2008 4 14 NWAA081529859 1 20080410 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 768NC 47729 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE COCKPIT WAS INOPERATIVE. MAINTENANCE REPLACED C OCKPIT EMERGENCY LIGHTING BATTERY PACK AND LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 2 L 7 2 4F RT A6WE 2008041400166 20080414 00166 NM 2008 4 14 F3LA200800150 1 20080411 A 3350 32145440 EPSU AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE EMERGENCY LIGHTS INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 928FR 360 2236 DURING RON SERVICE, INSPECTION REPORTED EMERGENCY EXIT PATH LIGHTING AT SEATS 6 ABC DID NOT ILLUMINATE. MAINTENANCE REM OVED AND REPLACED EPSU 10WL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-38 PB 401. UPON COMPLETION OF THE INSTALLA TION THE LIGHTS TESTED OKAY. 2 L 7 2 4F 4 F RT A28NM 2008041400169 20080414 00169 NM 2008 4 14 F3LA2008OO144 1 20080403 A 5347 D5311278220201 SEAT TRACK AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 5380 1841 DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON SEAT TRACK Y-1292, AT FUSELAGE STATION 810, ON THE RIGH T SIDE, EXTENDING FORWARD TOWARD FRAME 20. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IN ACCORDANCE WITH THE REQUI REMENTS OF A319 SRM 51-72-11, PAGES 1 AND 2. UPON COMPLETION OF THE INSTALLATION, IT WAS INSPECTED AND FOUND ACCEPTABLE . 2 L 7 2 4F 4 F RT A28NM 2008041400175 20080414 00175 WP 2008 4 14 AALA200800696 1 20080322 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7538A 49992 LGA - EMERGENCY LIGHTS AT SEAT ROWS 8 TO 13 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 8 TO 1 3. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008041400177 20080414 00177 NM 2008 4 14 AALA200800699 1 20080322 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT AT SEAT 24C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041400178 20080414 00178 NM 2008 4 14 AALA200800701 1 20080323 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 MIA - EMERGENCY LIGHT AT SEAT 24C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041400179 20080414 00179 EU 2008 4 14 AALA200800714 1 20080324 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7062A 474 MIA - EMERGENCY LIGHTS AT SEAT ROWS 6G TO 18G INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 6G T O 18G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008041400180 20080414 00180 NM 2008 4 14 AALA200800698 1 20080322 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041400194 20080414 00194 NE 2008 4 14 AALA200800723 2 20080326 A 7230 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RT ENGINE DAMAGED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 481AA 49656 725713 DFW INFLIGHT T1649/26MAR - NUMBER TWO ENGINE COMPRESSOR STALLED AT 200 FEET DURING TAKEOFF. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND LARGE AREA OF DAMAGE TO ACOUSTIC LINER AND HONEYCOMB IN FAN BYPASS DUCT. REPLACED NUMBER TWO E NGINE ON 27 MAR AT DFW. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 2008041400201 20080414 00201 NM 2008 4 14 AALA200800731 1 20080326 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 752AN 30260 DFW - EMERGENCY LIGHT AT SEAT 24G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041500005 20080415 00005 EU 2008 4 15 SA02024 1 20080403 A 2560 P2070003001 FLASHLIGHT AIRBUS A319 A319112 3930323 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 722US 1097 PIT - FLIGHT ATTENDANT AFT LEFT JUMPSEAT LOWER FLASHLIGHT NOT BLINKING. MAINTENANCE REPLACED THE FLASHLIGHT. 2 L 7 2 4F RT A28NM 2008041500015 20080415 00015 NM 2008 4 15 USAA920080725 1 20080328 A 2560 P2070001201 FLASHLIGHT BOEING 737 7373S3 1384711 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 313AW 23712 FLT 586 - PHX - CREW REPORTED FWD FLASHLIGHT INOP. MX REPLACED THE FWD FLASHLIGHT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2008041500016 20080415 00016 NM 2008 4 15 USAA920080726 1 20080328 A 2560 P2070001201 LIGHT BOEING 737 7373G7 1384595 NM FLASHLIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 154AW 23776 FLT 592 - SEA - CREW REPORTED FWD F/A FLASHLIGHT WORKS BUT NEGATIVE FLASHING TEST LIGHT INOP. MX REPLACED THE FWD F/A F LASHLIGHT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2008041500022 20080415 00022 EU 2008 4 15 BA08015 1 20080402 A 5210 DOOR AIRBUS 330 A330323 3930335 EU L4 OBSTRUCTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AY 0337 SJU - DOOR 4L WOULD NOT OPEN. MAINTENANCE REMOVED OBSTRUCTION FROM TOP FORWARD DOOR FRAME. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A46NM 2008041500025 20080415 00025 EA 2008 4 15 TRAX200800451 1 20080321 A 5320 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 355CA 10067 LEFT SIDE 280 CROSSBEAM CORRODED UPPER SURFACE. REPAIRS PERFORMED IAW BOMBARDIER REO 670-53-11-046 AND CRJ 700 SRM 51-2 4-28. SUPPLEMENTAL SDR CLOSED 4/4/08. JOB COMPLETE. 2 L 7 2 4F RT A21EA 2008041500027 20080415 00027 NM 2008 4 15 USAA920080689 1 20080312 A 5754 65C26601197SP WEDGE BOEING 737 7373G7 1384595 NM L/E SLAT DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK, LEFT WING NR 1 SLAT WEDGE UPPER AND LOWER SURFACE DISBONDED, WS 259.13 - WS 264.43 AND WS 384.75 - WS 389. REPAIRED LEFT WING NR 1 SLAT WEDGE UPPER AND LOWER SURFACE DISBONDED, WS 259.13 - WS 264.43 AND WS 384.75 - WS 389 IAW B737 SRM 51-70-10-2R4. 2 L 7 2 4F RT A16WE 2008041500035 20080415 00035 NM 2008 4 15 USAA920080734 1 20080312 A 5311 6546532 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 480, S8L - S9L AND S8R - S9R. REPAIRED FRAME, BS 480, S8L - S9L AND S8R - S9R IAW USAIRWAYS EA 5311-01019. 2 L 7 2 4F RT A16WE 2008041500038 20080415 00038 NM 2008 4 15 USAA920080737 1 20080312 A 5311 6546593 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 500A, S8L - S9L. REPAIRED FRAME, BS 500A, S8L - S9L IAW USAIRWAYS EA 5311-01019. 2 L 7 2 4F RT A16WE 2008041500044 20080415 00044 NM 2008 4 15 USAA920080743 1 20080313 A 5320 69735271 ATTACH BRACKET BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED INTERCOSTAL ATTACH BRACKET / CLIP, BS 500D, S28L. REPLACED INTERCOSTAL ATTACH BRACKET / CLIP, BS 500D, S28L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041500060 20080415 00060 NM 2008 4 15 SWAA081854 1 20080407 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 EEPLS LENS LOOSE AT ROW 7 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008041500061 20080415 00061 NM 2008 4 15 SWAA081853 1 20080407 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008041500062 20080415 00062 GL 2008 4 15 SWAA081844 2 20080404 A 7311 69202300 HEAT EXCHANGER BOEING 737 7375H4 138449D NM CFMINT CFM56 CFM563B1US GL NR 1 ENGINE DEFECTIVE A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 502SW 24179 INFLIGHT SHUTDOWN / AIR TURNBACK / DECLARED EMERGENCY. NR 1 ENGINE OIL TEMP IN YELLOW BAND AFTER TAKEOFF, THEN TEMP WEN T TO RED BAND. MAX OIL TEMP AT 190 DEGREES, SHUTDOWN ENGINE PER QRH. REMOVED AND REPLACED NR 1 ENGINE TEMP BULB AND FU EL OIL HEAT EXCHANGER PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041500063 20080415 00063 NM 2008 4 15 SWAA081863 1 20080407 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008041500066 20080415 00066 NM 2008 4 15 SWAA081859 1 20080407 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 645SW 28330 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 2008041500068 20080415 00068 NM 2008 4 15 SWAA081861 1 20080407 A 5313 BAC1498 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 27L CRACKED AT BS 390. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008041500069 20080415 00069 NM 2008 4 15 SWAA081862 1 20080407 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008041500080 20080415 00080 NM 2008 4 15 SWAA081868 1 20080408 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULE SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500081 20080415 00081 NM 2008 4 15 SWAA081884 1 20080408 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500082 20080415 00082 NM 2008 4 15 SWAA081885 1 20080408 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500087 20080415 00087 2008 4 15 SWAA081872 4 20080408 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 400WN 27891 L2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008041500089 20080415 00089 NM 2008 4 15 SWAA081873 1 20080408 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 411WN 29821 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 18 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008041500090 20080415 00090 NM 2008 4 15 SWAA081896 1 20080408 A 5340 6940367 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 1138, STR 13L. REPAIRED STRINGER CLIP PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500104 20080415 00104 NM 2008 4 15 SWAA081879 1 20080408 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 766, STR 20R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008041500108 20080415 00108 NM 2008 4 15 SWAA081897 1 20080409 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 266WN 32523 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008041500123 20080415 00123 EA 2008 4 15 VNAA0803016 1 20080331 A 5242 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE EXTERNAL POWER OPEN A VNAA A UNSCHED LANDING O OTHER TO TAKEOFF 1 GL 05 725PS 10186 CREW REPORTED AN EXTERNAL POWER DOOR LEFT OPEN DURING FLIGHT. CREW ELECTED TO RETURN TO TLH AND LANDED WITHOUT INCIDENT . MAINTENANCE INSPECTED AND SECURED THE DOOR CLOSED. NO DAMAGE NOTED AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008041500124 20080415 00124 EA 2008 4 15 TRAX200800490 1 20080407 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 LEFT BATTERY RIB IS CRACKED. REMOVED TWO SUPPORT BRACKETS FOR F.O.M. C/W REO 601R-57-51-046 REPAIR TO LT BATTERY RIB AS SY WS 53.60. OK TO INSTALL SUPPORT BRACKETS. INSTALLED SUPPORT BRACKETS IAW SRM 51-41-04. C/W ASA REO 601R-57-51-046. 2 L 7 2 4F RT A21EA 2008041500125 20080415 00125 EA 2008 4 15 TRAX200800491 1 20080407 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 PAX DOOR STEP RISER AFT DRAG ANGLE IS CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513. C/W ASA REO 601R-52-11-513. 2 L 7 2 4F RT A21EA 2008041500126 20080415 00126 EA 2008 4 15 TRAX200800492 1 20080407 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 PAX DOOR WILL NOT CLOSE. FLT 4209 DEL 39 MINS. 2 L 7 2 4F RT A21EA 2008041500127 20080415 00127 EA 2008 4 15 TRAX200800493 1 20080407 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 CABIN DOOR DIFFICULT TO CLOSE. 2 L 7 2 4F RT A21EA 2008041500130 20080415 00130 EA 2008 4 15 TRAX200800498 1 20080408 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 FORWARD DOOR HARD TO CLOSE. FLT 4852 DEL 29 MINS. 2 L 7 2 4F RT A21EA 2008041500142 20080415 00142 EA 2008 4 15 TRAX200800515 1 20080408 A 5320 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 723EV 10132 COCKPIT FLOOR, AFT LAND IS CORRODED BEYOND LIMITS. 2 L 7 2 4F RT A21EA 2008041500145 20080415 00145 EA 2008 4 15 TRAX200800520 1 20080409 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 971EV 7528 LEFT OVERWING EMERGENCY LIGHT IS OUT. 2 L 7 2 4F RT A21EA 2008041500147 20080415 00147 NM 2008 4 15 DHL2008785001 1 20080411 A 5330 SKIN BOEING 727 727214 138407R NM ZONE 100 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 785AT 21691 MULTIPLE LIGHTNING STRIKES FOUND DURING SERVICE CHECK. CUT OUT LIGHTNING STRIKE DAMAGE AT BS 435 TO 440, STR 25R, FABRI CATED REPAIR DOUBLER AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 3A, 53-30-2 FIG 2, AND 51-30-2. 2 L 7 3 4F A3WE 2008041500148 20080415 00148 EA 2008 4 15 TRAX200800522 1 20080410 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA AV DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 977EV 7720 AV BAY DOOR HANDLE CRACKED. 2 L 7 2 4F RT A21EA 2008041500149 20080415 00149 EA 2008 4 15 TRAX200800523 1 20080410 A 3350 PLATE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 FORWARD EMERGENCY FLOODLIGHTS BASE PLATE BROKEN AT ENTRYWAY. 2 L 7 2 4F RT A21EA 2008041500157 20080415 00157 NM 2008 4 15 SWAA081909 1 20080410 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739E, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008041500160 20080415 00160 EA 2008 4 15 A6WA200840199 1 20080320 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 FLOORBEAM CRACKED AT FS 280 RBL 9. FLOORBEAM AT FS 280 RBL 9 REPAIRED IAW CRJ 200 REO 601R-53-11-171 REV D. (M) 2 L 7 2 4F RT A21EA 2008041500161 20080415 00161 EA 2008 4 15 A6WA200840196 1 20080305 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 461 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 FITTING CRACKED AT FS 461, RBL 9 AND WL 73. NEW FITTING INSTALLED IAW SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2008041500162 20080415 00162 EU 2008 4 15 F3LA200800160 1 20080411 A 5320 D5391559320001 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE BULKHEAD CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE AFT BULKHEAD FLOOR SUPPORT PLATE, IN THE FORWARD CA RGO PIT, AT FRAME 31, BETWEEN STRINGERS 38 LEFT AND 38 RIGHT. MAINTENANCE REMOVED AND REPLACED THE PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPH 6. UPON COMPLETION OF THE INSTALLATION, THE NEW PLATE WAS INSPECT ED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041400082 20080414 00082 CE 2008 4 14 DXTA200802977 1 20080402 A 3230 UPLOCK BEECH MU300 400A 1155402 CE MLG OUT OF RIG E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 138QS RK492 AFTER DEPARTURE, THE RED GEAR IN TRANSIT LIGHT REMAINED ILLUMINATED. PERFORMED LANDING GEAR SWINGS AT FULL HYDRO POWER ALL CHECK OK. PERFORMED SWINGS AT LOWER HYDRO SETTINGS AND FOUND NOSE GEAR NOT RETRACTING FULLY AND CAUSING MAIN DOORS T O STAY OPEN. CHECK RIGGING ON NOSE GEAR UPLOCK MECHANISM AND FOUND OUT OF RIG. ADJUSTED UPLOCK HOOK AND ADDED SHIMS TO C ATCH PIN. PERFORMED SEVERAL GEAR SWINGS AND LOW AND FULL POWER. OPS CHECK. ALL WORK IAW MM 32-20-00 - NO DEFECTS NOTED W ITH LANDING LIGHT. 2 H 7 2 4F RT A16SW 2008041400086 20080414 00086 CE 2008 4 14 DXTA200802981 1 20080406 A 3246 WHEEL CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 943QS 7500043 SEVERE NOSEWHEEL SHIMMY ON TO ROLL, PRIOR TO 80 KTS. REMOVED BOTH NOSE WHEEL ASSEMBLIES AND INSTALLED OVERHAULED ASSEMB LIES WITH NEW TIRES. ADJUSTED NOSE GEAR CASTER. SERVICED NOSE STRUT LOWER CHAMBER PRESSURE AND RE-TORQUED THE UPPER AND LOWER GROVE LINK HARDWARE. WORK PERFORMED IAW MM 32-41-01, 12-10-38, AND 32-30-03 & LMM 32-20-02. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008041400096 20080414 00096 GL 2008 4 14 DXTA200802988 2 20080410 A 7261 O-RING CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL SPEED SENSOR LEAKING E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 982QS 7500182 CKPT PAC NOTICEABLE FUMES DURING TAKEOFF POWER. M2B-LT ENGINE N1A AND N1B SPEED SENSORS LEAKING OIL PAST O-RINGS. INSTA LLED NEW O-RINGS AND LEAK CHECK GOOD PER ENG MM 72-00-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20081010 NM 2008 10 10 SWAA085335 1 20081001 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT 500D, STR 23L TO STR 24L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008041400114 20080414 00114 WP 2008 4 14 08FDEA01380 1 20080410 A 5347 6044987075T6 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 361FE 48260 MCD SEAT TRACK LBL 7 STA 1691 HAS TWO LOBES GOUGED BLENDED DAMAGED AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00. NEW TRACKED FABBED ON TRAVELER T8/732523, NEW SPLICE FABBED ON TRAVELER T8/732524. TRACK INSTALLED IAW SRM 53-70-00. 2 L 7 3 4F RT A22WE 2008042800354 20080428 00354 NM 2008 4 28 BB08069 1 20080420 A 3020 7612B000 ANTI-ICE VALVE BOEING 757 7572S7 1384962 NM LT ENGINE FAULTY A USAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 901AW 58316 38059 23321 HNL FLT 26 - EN ROUTE OGG TO PHX. AFTER TAKEOFF, THE CREW TURNED ON THE ENGINE ANTI-ICE AND NOTICED A POWER LOSS AND FL UCTUATION ON THE LEFT ENGINE. THE ENGINE ANTI-ICE WAS TURNED OFF, AND THE LEFT ENGINE POWER PARAMETERS RETURNED TO NORM AL. THE FLIGHT DIVERTED TO HNL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE ANTI-ICE VALV E. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 2008042800365 20080428 00365 NM 2008 4 28 UPS08552059 1 20080331 A 5320 STRAP BOEING 757 75724APF 1384969 NM APU PLENUM CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 451UP 27739 INSPECTION TYPE:C3 CORROSION FOUND ON SUPPORT STRUCTURE COMMON TO APU INLET PLENUM, LOWER AFT CORNER STA 1822 STR 6R AN D LOWER FWD CORNER STA 1789 STR 6R. CORROSION ON OUTER STRAP AT BS 1825 FROM STR 9R TO STR 2L CORROSION ON APU CUTOUT F WD STRAP AND UPPER & LOWER SUPPORT ANGLES FOUND TO BE OUT OF LIMITS. REPLACED THE FWD STRAP, UPPER AND LOWER SUPPORT AN GLES. 2 L 7 2 4F RT A2NM 2008042800391 20080428 00391 CE 2008 4 28 DJFA2008042 1 20080412 A 2450 CIRCUIT BREAKER BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE COCKPIT ARCED E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 790TA RK252 CREW EXPERIENCED A STRONG ELECTRICAL SMELL IN THE COCKPIT DURING FLIGHT. MAINT FOUND THE 15 AMP STANDBY POWER CIRCUIT B REAKER ARCING. THE CIRCUIT BREAKER WAS REPLACED. FUNCTIONAL CHECKS WERE GOOD AND THE AC WAS RETURNED TO SERVICE. 2 H 7 2 4F 4 F RT A16SW E25EA 2008042800392 20080428 00392 CE 2008 4 28 GUUA03080804 1 20080308 A 5210 12951407627 HANDLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE AIRSTAIR DOOR CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 47542 UE198 DURING SCHEDULED ROUTINE MAINT, DISCOVERED AIRSTAIR DOOR INTERIOR HANDLE CRACKED. REPLACED AIRSTAIR DOOR INTERIOR HANDL E. 2 L 7 2 4T 4 T RT A24CE E26NE 2008042900010 20080429 00010 EA 2008 4 29 TRAX200800546 1 20080416 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 394 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 LEFT CABIN FLOOR SEAT TRACK STARTING AT FS 394.00 HAS CORROSION DAMAGE. REMOVED CORROSION FROM SEAT TRACK. BLENDED OUT OF LIMITS PER 53-21-49. 2 L 7 2 4F RT A21EA 2008042800045 20080428 00045 NM 2008 4 28 SWAA082115 1 20080421 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042800050 20080428 00050 NM 2008 4 28 SWAA082092 1 20080421 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042800057 20080428 00057 NM 2008 4 28 SWAA082125 1 20080420 A 5753 65C26343 CARRIAGE BOEING 737 737317 138447P NM T/E FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 1 MID FLAP CARRIAGE ASSY BEARING SUPPORT WORN. REMOVED AND REPLACED FLAP C ARRIAGE PER MM. 2 L 7 2 4F RT A16WE 2008042800068 20080428 00068 NM 2008 4 28 ABXA080125 1 20080328 A 5330 148T31111 SKIN BOEING 767 767231 1385131 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 702AX 22566 FUSELAGE SKIN CRACKED STA 1654.5 BETWEEN STRINGER 4 LEFT AND STRINGER 5 LEFT, 3 EACH CRACKS, LONGEST CRACK 1 5/16". REP AIRED FUSELAGE SKIN CRACK AT STA 1654.5. 2 L 7 2 4F RT A1NM 2008042800081 20080428 00081 EA 2008 4 28 A6WA200840276 1 20080401 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 589-610 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 FLOORBEAM BETWEEN FS 589 AND 610 LBL 27 IS CORRODED ALONG ANCHOR NUTS. (M) REPAIRED IAW REO 601R-53-61-2439. 2 L 7 2 4F RT A21EA 2008042800083 20080428 00083 EA 2008 4 28 A6WA200840290 1 20080402 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 FOUND CRACK ON INTERCOSTAL FS 484 AND LBL 36. (M) INTERCOSTAL REPAIRED IAW REO 601R-53-41-059 REV A. 2 L 7 2 4F RT A21EA 2008042800087 20080428 00087 NM 2008 4 28 DL76L080632 1 20080424 A 5311 145T10017 FRAME BOEING 767 767332 1382001 NM BS 903 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 190DN 28447 DURING HMV AT HKG, CRACKS WERE FOUND IN THE STA 903.5 FRAMES ON THE LHS AND RHS. THE CRACKS WERE REMOVED AND BOTH FRAME S WERE REPAIRED PER BOEING INSTRUCTIONS. 2 L 7 2 4F RT A1NM 2008042800124 20080428 00124 NM 2008 4 28 ASAA0852829 1 20080420 A 3610 32895624 CONTROL VALVE BOEING 737 737890 1384527 NM PNEUMATIC SYSTEM FAULTY A ASAA K NONE J WARNING INDICATION CL CLIMB 1 NM 02 579AS 35187 RIGHT BLEED TRIP OFF LIGHT ILLUMINATED FOLLOWING A BLEEDS OFF TAKEOFF FROM LAS THE LIGHT ILLUMINATED APPROXIMATELY 60 SE CS AFTER RE-ESTABLISHING THE BLEEDS ON BOTH ENGINES. BLEED RE-ESTABLISHED WITH TRIP RESET PER QRH. PRECOOLER CNTL VLV PASSED HEALTH CHECK. ACCOMPLISHED BLEED AIR CROSSOVER OPS TEST OPS NORMAL. PERFORMED BLEED AIR REG PRSOV 450 DEGREE CH ECK. PRECOOLER CNTL VLV FAILED TO OPEN FULLY BEFORE CONTROL PRESSURE REACHED 3PSIG. REPLACED PRECOOLER CONTROL VALVE. 2 L 7 2 4F RT A16WE 2008042800136 20080428 00136 NM 2008 4 28 SWAA082147 1 20080422 A 5311 6545812 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, STR 21R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008042800142 20080428 00142 NM 2008 4 28 SWAA082168 1 20080423 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042800176 20080428 00176 NM 2008 4 28 SWAA082182 1 20080423 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 840, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042800184 20080428 00184 NM 2008 4 28 2008UALA02375 1 20080422 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 816UA 871 EMERGENCY LIGHTS TEST FAILED. FOUND EPSU FAILED. REPLACED EPSU 13WL, TEST PASSES. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042800191 20080428 00191 NM 2008 4 28 2008UALA02296 1 20080418 A 3510 MXP1472 OXYGEN MASK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CREW LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 309UA 23670 CREW O2 NEEDS SERVICE. FOUND FIRST OBSERVERS O2 MASK LEAKING AT QUICK DISCONNECT FITTING, REPLACED MASK AND STOWED PER AMM 35-12-85. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042800194 20080428 00194 NM 2008 4 28 SWAA082135 1 20080422 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 499, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042800200 20080428 00200 NM 2008 4 28 DL757080630 1 20080423 A 5330 SKIN BOEING 757 757232 1384965 NM BS 532 S26L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 646DL 24217 DURING HMV AT SAA, A CRACK WAS DISCOVERED IN THE SKIN LAP JOINT AT STA 532, S-26L. THE CRACK WAS REMOVED AND A PERMANEN T REPAIR WAS INSTALLED PER BOEING INSTRUCTIONS. REPETITIVE INSPECTIONS FOR FURTHER DAMAGE WILL BEGIN AT 37,500 TOTAL AI RCRAFT CYCLES AND EVERY 3000 CYCLES THEREAFTER. 2 L 7 2 4F RT A2NM 2008042800218 20080428 00218 EU 2008 4 28 2008UALA02412 1 20080424 A 2497 CONTACTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELEC GEN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 433UA 589 EMERGENCY ELECTRICAL GENERATING SYSTEM FAILS OPS TEST. FOUND CONTACTOR RELAY BASE BROKEN. REPLACED TRANSFORMER AND CON TACTOR BASE, ALL TESTS ARE NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042800229 20080428 00229 EU 2008 4 28 2008UALA02301 1 20080418 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 474UA 1475 CREW OXYGEN SYSTEM-LOW, RECORD PRESSURE PRIOR TO SERVICING. CREW COMMENTS, OXYGEN LOW 1390 PSI. SERVICED CREW O2 TO FUL L, NO LEAKS WERE NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042800230 20080428 00230 2008 4 28 SWAA082142 4 20080422 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042800242 20080428 00242 NM 2008 4 28 2008UALA02309 1 20080421 A 3510 OXYGEN SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA 24384 CREW OXYGEN IS LOW AT 1630 PSI, PASS OXYGEN IS GOOD AT 1760 PSI. SERVICED O2 SYSTEM TO PROPER LEVEL IAW MM12-15-08. AC O K FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042800249 20080428 00249 EA 2008 4 28 SWIA200819534 1 20080421 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 457SW 7773 FLT 3802 - SERVICE DOOR WILL NOT SHUT AND LOCK PROPERLY. REPLACED SERVICE DOOR HANDLE ASSEMBLY IAW SRM 51-42-13. 2 L 7 2 4F RT A21EA 2008042800255 20080428 00255 EU 2008 4 28 08FDEA01529 1 20080424 A 5321 A2557158022800 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU FUSELAGE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 EMPENAGE ACCESS THRU 312 AR, THE FLOORBOARD ON THE LEFT SIDE OF THE A/C AFT OF THE PNEUMATIC DUCT AT FRAME 84 IS DELAMIN ATED. FABRICATED NEW PANEL; LOCATED & DRILLED NEW HOLES; INSTALLED INSERTS; POTTED & CURED BOARD EDGES. SANDED E DGES AS NEEDED; APPLIED NON-SKID & PART MARKED PANEL IAW DWG SRZ 25-005, REV F; AMM 11-00-00-00 & GMM 7-0-1000.REMOVE D & INSTALLED FLOOR PANEL IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008042800292 20080428 00292 EU 2008 4 28 USAA920080885 1 20080407 A 5347 D53112782202 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 709UW 997 PIT - MAJOR REPAIR - ULTIMATE BREAKING MODIFICATION - CORROSION ON CABIN SEAT TRACK, BS 808 / FR 20 - BS 950 / BS 24, -Y 765. REPLACED CABIN SEAT TRACK, BS 808 / FR 20 - BS 950 / BS 24, -Y765 IAW A319 SRM 53-11-15. 2 L 7 2 4F RT A28NM 2008042800295 20080428 00295 EU 2008 4 28 USAA920080915 1 20080408 A 5540 D5537131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU NR 2 RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 642AW 584 SAL - MAJOR REPAIR - C7 CHECK - NR 2 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 1926 / RIB 4 HAS EXCESSIVE PLAY. REPLACED NR 2 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 1926 / RIB 4 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 2008042800302 20080428 00302 NM 2008 4 28 UPS08M52058 1 20080121 A 5753 HINGE FITTING DOUG MD11 MD11 3023602 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING MOUNTED HINGE AFT LOWER O/B BORE HOLE AND FACE AREA RUSTY AS MARK ED. LEFT FWD O/B FLAP I/B HINGE LWR MOUNT O/B BORE & SPOTFACE CORROSION REMOVED & FOUND EXCEED LIMIT PER CMM57-44-08 PG 602-607R.60. FPI C/OUT IAW DACNDTS PMR.13PART08. FOUND NO CRACK & CORROSION EVIDENT. LEFT FWD O/B FLAP I/B HINGE LWR MOUNT O/B HOLE SPOTFACE THK 0.0464" ACCEPTED PER EN1092-08. REWORKED AREA ETCH & INSP FOUND SATIS PER EN1092-08. 2 L 7 3 4F RT A22WE 2008042800303 20080428 00303 2008 4 28 JGV2008F00000 4 20080208 A 3417 SWITCH LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE731* 01518 WP ADC SHORTED E JGVA K NONE O OTHER IN INSP/MAINT 1 CE 09 645G 980 IND0095 056 THE ADC SWITCHING/ANNUNCIATOR PANEL DEVELOPED A HIGH RESISTANCE SHORT TO GROUND WHICH IN TURN OVERLOADED THE CIRCUIT IN THE AC AND CAUSED THE (A) ESSENTIAL BUS TIE BREAKER TO TRIP. LETTER 2/8/2008 FOR DETAILS. THIS PART WAS INSTALLED AS P ART OF STC-STO1199NY-D DUAL ALTIMETER SYSTEM AS PART OF THE RVSM SOLUTION FOR THIS AC. 2 L 7 2 4F 4 F A10CE E6WE 2008041400121 20080414 00121 NM 2008 4 14 P5CA0801555 1 20080410 A 2510 SEAT BELT BOEING 747 747243B 1384830 NM OBSERVERS SEAT MISSING A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 15 516MC 22507 AFTER PUSHBACK FLIGHT ENGINEER FOUND THE CROTCH SEATBELT MISSING FROM FIRST OBSERVER'S SEAT. AIRCRAFT CAME BACK TO GATE AND MAINTENANCE DEFERRED THE FIRST OBSERVER'S SEAT IAW MEL 25-23-1. 2 L 7 4 4F RT A20WE 2008041400122 20080414 00122 NM 2008 4 14 DHL2008753517 1 20080410 A 5740 MOUNT BOEING 727 727223 1384074 NM KRUEGER FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 WHILE AT C CHECK, NR 1 KRUEGER FLAP ACTUATOR O/B AND I/B MOUNT SUPPORT CRACKED. REMOVED, FABRICATED, AND INSTALLED NEW SUPPORT BRACKET IAW BOEING DWG 65-16275 REV D AND B727 SRM 51-20-1 FIG 2, 51-30-2, 51-10-2.7075 T6 .071 INCH 8 INCH BY 3 .5 INCH. 2 L 7 3 4F A3WE 2008041400124 20080414 00124 NM 2008 4 14 NWAA081485505 1 20080409 A 3350 LAMP BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 505US 23194 FLIGHT ATTENDANT REPORTED DOOR 4 RIGHT SLIDE LIGHT WOULD NOT ILLUMINATE. MAINTENANCE RELAMPED THE SLIDE LIGHT AND ALL O PERATIONS CHECKED GOOD. 2 L 7 2 4F RT A2NM 2008041400125 20080414 00125 NM 2008 4 14 NWAA081495523 1 20080409 A 3350 LAMP BOEING 757 757251 1384970 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 523US 23617 EXTERNAL EMERGENCY LIGHT AT DOOR 4 LEFT WOULD NOT TEST DURING A MAINTENANCE CHECK. MAINTENANCE RELAMPED THE EMERGENCY L IGHT AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A2NM 2008041400136 20080414 00136 NM 2008 4 14 HALA0800521 1 20080408 A 5740 BRACKET BOEING 767 76733A 1385209 NM WING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 587HA 33421 SLATS NR 9 AND NR 10 INBOARD AND OUTBOARD CONTROL ROD FORWARD BRACKETS CRACKED. REPLACED BRACKETS AND RIGGED PER AIRCRA FT MAINTENANCE MANUAL 27-81-02 AND 57-41-56. 2 L 7 2 4F RT A1NM 2008041400141 20080414 00141 NM 2008 4 14 F3LA200800141 1 20080410 A 3397 32511021 WIRE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE EMERGENCY LIGHTS SHORTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 948FR 444 2836 DURING PREDEPARTURE CABIN CHECK THE FLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHT AT ROW 11 ABC WAS INOPERATIVE. MAINTE NANCE TROUBLESHOT THE SYSTEM AND FOUND WIRE 3351-1021 OPEN AT CONNECTOR AT 11WLA PIN F TO TERMINAL BLOCK 7725VT BLOCK 3. MAINTENANCE REPAIRED THE WIRE IN ACCORDANCE WITH ESPM 20-51-21. FOLLOWING COMPLETION OF THE REPAIR THE SYSTEM OPERATI ONALLY CHECKED OKAY. 2 L 7 2 4F 4 F RT A28NM 2008041400149 20080414 00149 SO 2008 4 14 SWIA200819464 1 20080405 A 2150 A/C PACK EMB 120 EMB120ER 3260203 SO RIGHT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 216SW 120285 FLT 3708 - RIGHT AIR CONDITIONING PACK CREATES SMOKE IN CABIN. REPLACED RIGHT PACK GROUND COOLING FAN IAW EMB MM 21-51- 03. OPS CHECK GOOD, PN: EVAC2322C2, SN OFF: 53. 2 L 7 2 4T RT A31SO 2008041400151 20080414 00151 EA 2008 4 14 SWIA200819466 1 20080408 A 3244 TIRE CNDAIR CL600 CL6002C10 1390015 EA MLG FAILED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 800SK 15060 FLT 3747 - THE NR 3 AND NR 4 MAIN TIRES WERE FOUND FLAT AFTER LANDING. REPLACED BOTH WHEEL ASSEMBLIES IAW AMM 32-41-01, PN: 90001320-1, SN OFF: AUG06-0661, PN: 90001200-1, SN OFF: MAR06-0520. 2 L 7 2 4F RT A21EA 2008041400152 20080414 00152 EA 2008 4 14 SWIA200819467 1 20080108 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 756SK 10221 FS 280 BEAM CRACKED AT APPROX LBL15 AND RBL15, FOUND AT C-CHECK. REPLACED FS 280 BEAM PER CRJ700 SRM 51-42-06-001-001-A 01. 2 L 7 2 4F RT A21EA 2008041400160 20080414 00160 EU 2008 4 14 08FDEA01386 1 20080411 A 5310 A5361202539200 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 THE AVOINICS COMPARTMENT FLOOR STRUCTURE FROM FRAME 16 TO 17; STRINGER 44 L IS CRACKED. FORMED EDGING IAW DWG A53612025 . HEAT TREATED IAW TPS 1003; REV A. TREATED IAW SRM 51-21-10 & 51-23-10. PART MARKED IAW GMM 7-0-1000; STEP 7-B. 2 L 7 2 4F RT A35EU 2008041400184 20080414 00184 NM 2008 4 14 AALA200800704 1 20080323 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 767AJ 33539 JFK EMERGENCY LIGHT AT SEAT 26C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041400186 20080414 00186 WP 2008 4 14 AALA200800708 1 20080323 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 457AA 49562 LGA - EMERGENCY LIGHT AT FIRST CLASS GALLEY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FIRST CLASS GALLEY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008041400187 20080414 00187 NM 2008 4 14 AALA200800706 1 20080323 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 767AJ 33539 JFK - EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041400188 20080414 00188 NM 2008 4 14 AALA200800740 1 20080327 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AA 27054 DFW - EMERGENCY LIGHT AT SEAT 35D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 35D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041400189 20080414 00189 WP 2008 4 14 AALA200800707 1 20080323 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 583AA 53160 LGA - EMERGENCY LIGHT AT MID CABIN RIGHT EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT MID CABIN RIGHT EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008041400190 20080414 00190 GL 2008 4 14 AALA200800711 2 20080324 A 7310 VL1073GE1328 GASKET BOEING 767 767323 1385205 NM GE CF6 CF680C2* GL NR 2 ENGINE LEAKING A AALA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 SW 21 366AA 25193 695562 CDG - ON ARRIVAL FOUND NUMBER TWO ENGINE FUEL LEAK. REPLACED GASKET BETWEEN NUMBER TWO ENGINE FUEL PUMP AND FUEL INLET HOSE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E23EA 2008041400191 20080414 00191 NM 2008 4 14 AALA200800720 1 20080325 A 3350 PLATE BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 691AA 25697 DFW - EMERGENCY LIGHT AT SEAT 16D MISSING BACKPLATE. REPLACED BACKPLATE FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041400192 20080414 00192 NM 2008 4 14 AALA200800721 1 20080325 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 787AL 30010 DFW - EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. REPLACED LIGHT FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041500011 20080415 00011 EU 2008 4 15 USAA920080727 1 20080328 A 5347 A57227400584 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AY 337 BFM - MAJOR REPAIR -C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 4842 / FR 58 - BS 5266 / FR 66, +Y953. REPAIRED CABIN SEAT TRACK, BS 4842 / FR 58 - BS 5266 / FR 66, +Y953 IAW A330 SRM 53-00-15. 2 L 7 2 4F RT A46NM 2008041500017 20080415 00017 EU 2008 4 15 08FDEA01312 1 20080404 A 5730 A5724323700000 PANEL AIRBUS 310 A310203 3930313 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LEFT WING LOWER SURFACE L/E DROP PANEL (RIB 28) INTERIOR SKIN IS MISSING FOIL. REPAIRED LOWER SURFACE L/E DROP PANEL BY REMOVING DAMAGED FOIL, APPLYING NEW FOIL REPAIR, ALODINED FOIL REPAIR, AND APPLING FR PRIMER IAW SRM 57-41-12, 51-21-00 , AND 51-75-10. 2 L 7 2 4F RT A35EU 2008041500019 20080415 00019 NM 2008 4 15 08FDEA01314 1 20080405 A 5330 AEA753991 SKIN DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 580FE 48471 L3 DOOR CUT-OUT LOWER AFT CORNER FOUND CORRODED. COMPLIED WITH EA 1-5310-112608. CLASSIFIED AS MAJOR REPAIR AS PER FED EX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041500020 20080415 00020 EA 2008 4 15 TRAX200800495 1 20080407 A 5260 HANDLE CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 723EV 10132 ASD EXTERNAL HANDLE CRACKED. REMOVED AND REPLACED DOOR HANDLE. ACCOMPLISHED IAW T/C SB670BA-52-030. 2 L 7 2 4F RT A21EA 2008041500037 20080415 00037 NM 2008 4 15 USAA920080736 1 20080312 A 5311 6546555 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 867, S8L - S9L AND S8R - S9R. REPAIRED FRAME, BS 867, S8L - S9L AND S8R - S9R IAW USAIRWAYS EA 5311-01019. 2 L 7 2 4F RT A16WE 2008041500045 20080415 00045 NM 2008 4 15 USAA920080744 1 20080324 A 5320 69353654 ATTACH ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED ATTACH ANGLE, BS 500D, BL 0, WL 208. REPLACED ATTACH ANGLE, BS 500D, BL 0, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041500046 20080415 00046 NM 2008 4 15 USAA920080745 1 20080314 A 5313 6545768210 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER, BS 500C, S16R. REPAIRED STRINGER, BS 500C, S16R IAW USAIRWAYS EA 100 366. 2 L 7 2 4F RT A16WE 2008041500056 20080415 00056 NM 2008 4 15 SWAA081849 1 20080407 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CHORD CORRODED AT 947 TO BS 1016, STR 17R. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2008041500059 20080415 00059 NM 2008 4 15 SWAA081852 1 20080407 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 457WN 33856 EEPLS LENS MISSING AT ROW 3 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008041500073 20080415 00073 EA 2008 4 15 TRAX200800489 1 20080405 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BINDS A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 719EV 10099 PAX DOOR HARD TO OPEN FROM OUTSIDE. 2 L 7 2 4F RT A21EA 2008041500084 20080415 00084 NM 2008 4 15 SWAA081870 1 20080408 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, RBL 4. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500085 20080415 00085 NM 2008 4 15 SWAA081886 1 20080408 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008042800312 20080428 00312 EU 2008 4 28 HEER119378 1 20080401 A 6720 9220700 PIVOT UROCOP EC135 EC135P2 5620027 EU TAIL ROTOR FROZEN B HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 326PH 0435 BALL PIVOT FAILED INSPECTION OF ASB EC135-67A-017 REV. 2. FROZEN UNABLE TO MOVE PIVOT POINT. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H88EU 2008042800322 20080428 00322 NE 2008 4 28 020804CR 2 20080219 A 7320 6078T55P26 FUEL CONTROL CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF34* 30015 NE RT ENGINE INOPERATIVE E TVMA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 03 604CR 5815 5418 872538 RT ENGINE WOULD NOT START. 2 L 7 2 4F 4 F RT A21EA 2008042800326 20080428 00326 CE 2008 4 28 DXTA200803000 1 20080415 A 3230 UNKNOWN CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LANDING GEAR UNKNOWN E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 613QS 5605599 GEAR RETRACTED DURING LANDING ROLLOUT. MALFUNCTION UNDER INVESTIGATION. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008042800357 20080428 00357 NM 2008 4 28 BB08071 1 20080423 A 7720 INDICATION SYS BOEING 757 7572S7 1384962 NM LT ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 906AW 23568 PHX FLT 429 PHX TO OGG. ON TAKEOFF, THE LEFT ENGINE OVER TEMPED AT 871 AND FLUCTUATING. THE FLIGHT RETURNED TO PHX AN D LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED EGT THERMOCOUPLE PROBE TEST, A DETAILED VISUAL INSPECTION O F CONNECTORS, AND A COMPRESSOR AIRFLOW TEST. ALL CHECKS OK. 2 L 7 2 4F RT A2NM 2008042800362 20080428 00362 NM 2008 4 28 SB08022 1 20080424 A 3350 036000570010 FUSE BOEING 737 7374B7 1384702 NM BATTERY PACK BLOWN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 458UW 25022 CLT - MAINTENANCE REPORTED THE RIGHT LOWER EXTERIOR EMERGENCY LIGHT INOPERATIVE (JUST AFT OF WING-TO-BODY FAIRING). MAI NTENANCE REPLACED A BLOWN FUSE IN THE BATTERY PACK/CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008042800363 20080428 00363 EU 2008 4 28 UPS08152066 1 20080424 A 2780 JACKSCREW AIRBUS A300 A300F4622R 3930360 EU L/E SLAT OUT OF TOLERANCE A IPXA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SO 01 128UP 0812 INSPECTION TYPE:N/A LEFT AND RIGHT SLATS SYSTEM ONE AND TWO FAULT ON APPROACH. EMERGENCY DECLARED DUE TO INCREASED LAND ING SPEED. CHECKED SLAT SYSTEM. SFCC 1&2 HAVE SLAT JAM FAULTS. FOUND LEFT TORQUE LIMITER IND POPPED. CHECKED ALL 6 J ACKSCREWS IN LEFT WING FOUND NR 1 JACKSCREW TORQUE IND OUT OF SPECS PER FIM 27-80-02. REMOVED AND REPLACED LEFT WING NR 1 SLAT JACKSCREW PER AMM 27-84-22-04. SYSTEM OPS CHECKS GOOD. 2 L 7 2 4F RT A35EU 2008042900001 20080429 00001 NE 2008 4 29 DXTA200802992 2 20080412 A 7532 1988003 BLEED VALVE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE ZONE 100 BYPASSING E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 654QS 2277 5605611 UPON APPLICATION OF TAKEOFF THRUST THERE IS A OSCILLATING PRESSURE SURGE THAT CAN BE FELT STRONGLY AND HEARD. REMOVED P /N 9912492-1(1988-00-3) S/N 2317. INSTALLED OVERHAULED UNIT BY DUKES INC. CRS WUERE79L. OPERATIONAL AND LEAK CHECK GOOD. WORK DONE IAW MM 21-11-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008042900004 20080429 00004 NM 2008 4 29 2008UALA02159 1 20080413 A 3350 3071BPEGPL LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 12D AFT BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 774UA 26936 EMERGENCY LIGHT AT SEAT 12D AFT LIGHT IS BURNT OUT. RELAMPED. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042900005 20080429 00005 EU 2008 4 29 2008UALA02170 1 20080415 A 3350 3071BPEGPL BULB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 411UA 464 SEAT MOUNTED FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHT OUT AT SEAT 2B. REPLACED AFT LIGHT ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042900006 20080429 00006 NM 2008 4 29 2008UALA02183 1 20080415 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 FWD ENTRY DOOR, LOWER HINGE CUTOUT, 1 FASTENER HOLE SHOWS CRACK INDICATIONS, JUST ABOVE FWD END OF CUTOUT. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED EXTERNAL SKIN CRES DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042900015 20080429 00015 EA 2008 4 29 TRAX200800564 1 20080418 A 5242 HANDLE CNDAIR CL600 CL6002C10 1390015 EA E/E BAY DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 379CA 10102 AVIONICS DOOR HANDLE CRACKED. DRILLED AND INSTALLED NEW HANDLE ASSY. PAINTED HANDLE PER SRM 51-25-00, LOCK FASTENERS IN STALLED PER SRM 51-42-20. 2 L 7 2 4F RT A21EA 2008043000003 20080430 00003 SO 2008 4 30 C2XA08ON117 1 20080418 A 2742 3622001015 ACTUATOR EMB 145 EMB145XR 3260214 SO HORIZ STAB INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 14162 10982 10982 14500808 FLT 223 - SAT - FLIGHT CREW REPORTED MAIN PITCH TRIM FAIL INFLIGHT. MX PERSONNEL REMOVED AND REPLACED HORIZONTAL STAB A CTUATOR OPERATIONALLY CHECKED SATISFACTORY, AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008043000005 20080430 00005 NM 2008 4 30 KCSA081223 1 20080424 A 5412 BULKHEAD BOEING 747 747123 1384873 NM NR 3 PYLON GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 NR 3 PYLON FORWARD ENGINE MOUNT BULKHEAD CHORD INBOARD AND OUTBOARD LOWER ENDS ARE GOUGED / WORN AT NAC STA 128.95. 2 L 7 4 4F RT A20WE 2008043000008 20080430 00008 SO 2008 4 30 RAIA00804019 1 20080420 A 3230 355022002MOD ELECTRONIC UNIT EMB 145 EMB145LR 3260212 SO LANDING GEAR MALFUNCTIONED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 838HK 145321 FLT 7904 - LIT - LANDING GEAR WOULD NOT RETRACT. CONTROL LEVER WOULD NOT MOVE. MAINTENANCE REMOVED AND REPLACED THE LA NDING GEAR ELECTRONIC UNIT (LGEU) AND PERFORMED AN OPERATIONAL CHECK OF THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM . 2 L 7 2 4T RT T00011AT 2008043000010 20080430 00010 SO 2008 4 30 RAIA00804023 1 20080421 A 5210 DOOR EMB 145 EMB145EP 3260221 SO PAX DOOR LACK OF LUBE A RAIA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 03 827HK 145021 FLT 5590 - STL - PASSENGER DOOR HARD TO OPEN. MAINTENANCE LUBRICATED THE DOOR. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2008043000011 20080430 00011 SO 2008 4 30 RAIA00804020 1 20080420 A 3610 SEAL EMB 145 EMB145 3260210 SO BLEED AIR SYS WORN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 820HK 145064 FLT 5484 - STL - BLEED 1 LEAK MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED BLEED DUCT SEALS UNDER THE CARGO B AY FLOORBOARDS. SYSTEM CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2008043000018 20080430 00018 NM 2008 4 30 ASAA0892837 1 20080324 A 5321 147A5810137 FLOORBOARD BOEING 737 737990 NM CABIN CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 317AS 30856 CABIN AFT FLOORBOARD AT STA 947 TO STA 986 LBL 17 TO LBL 43 CORNER CRACKED. PREPARED DAMAGED AREA APPLIED POTTING COMPO UND BMS 5 28 TYPE 19 TO DAMAGED CORE: 8 LAYERS (4 EACH SIDE) OF BMS 9 3 1581, REPAIR PLY BONDED IAW B737 900 SRM 53 00 5 0 PG 201-203. 2 L 7 4 4F RT A16WE 2008050600007 20080506 00007 EU 2008 5 6 08FDEA01661 1 20080407 A 5320 A5361080420600 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 COCKPIT, CONNECTION ANGLE OF FR10 AT Y-953 TO INTERCOSTAL PANEL FOUND CRACKED. THE ANGLE WAS REPLACED IN ACCORDANCE WIT H SRM 51-40-21 AND SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008043000026 20080430 00026 NM 2008 4 30 ASAA0872843 1 20080406 A 5320 146A812713 SHIELD BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 609AS 29752 BS 767 787 RBL 21 SUPPORT SHIELD IS CRACKED. SUPPORT SHIELD AT BS 767 787 RBL 21 REPLACED IAW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 2008043000036 20080430 00036 NM 2008 4 30 2008UALA02287 1 20080418 A 5320 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 188-196 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FUSELAGE HORIZ WEB HAS CRACK, BS 188-196.5 AT FLOOR LEVEL LT SIDE EMANATING FROM AFT INBD CUTOUT AND PROMINATING FROM AF T INBD CUTOUT. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED REPLACEMENT WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2008043000038 20080430 00038 NM 2008 4 30 2008UALA02289 1 20080418 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 420 S6R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 UPPER RT FUSELAGE SKIN BS 420 STR 6R, EXISTING REPAIR DOUBLER HAS DEGRADED SEALANT CAUSING PRESS LEAK. MAJOR REPAIR ACC OMPLISHED, REPLACED THE REPAIR WITH A DOUBLER/TRIPLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2008043000051 20080430 00051 NM 2008 4 30 CALA0800362 1 20080425 A 2720 69152953 SUPPORT BRACKET BOEING 737 737524 1384721 NM RUDDER PEDAL CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 FIRST OFFICER RUDDER PEDAL ASSY, SUPPORT SHAFT BRACKET CRACKED. FABRICATED NEW 69-15295-3 RUDDER PEDDLE BRACKET PER BAC DWG 69-15295. 2 L 7 2 4F RT A16WE 2008043000055 20080430 00055 EA 2008 4 30 TRAX200800570 1 20080422 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 835AS 7258 F/A REPORTS SOME FLOOR LEVEL EMERGENCY LIGHTING IS INOP. FLT 4906 DEL 21 MINS. 2 L 7 2 4F RT A21EA 2008043000063 20080430 00063 NM 2008 4 30 SWAA082236 1 20080424 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008043000074 20080430 00074 NM 2008 4 30 SWAA082206 1 20080424 A 5315 6545410 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED FLOORBEAM PER ER AND BOEING SB. 2 L 7 2 4F RT A16WE 2008043000079 20080430 00079 NM 2008 4 30 SWAA082215 1 20080424 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000083 20080430 00083 NM 2008 4 30 SWAA082214 1 20080424 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000086 20080430 00086 NM 2008 4 30 SWAA082216 1 20080424 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000090 20080430 00090 NM 2008 4 30 SWAA082234 1 20080424 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, RBL 15, WL 152. REMOVED AND REPLACED STRINGER CLIP P ER SRM. 2 L 7 2 4F RT A16WE 2008043000091 20080430 00091 NM 2008 4 30 SWAA082233 1 20080424 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000093 20080430 00093 2008 4 30 SWAA082222 4 20080424 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008043000095 20080430 00095 NM 2008 4 30 SWAA082224 1 20080424 A 5753 6546435 FLAP BOEING 737 7373Q8 1384670 NM RT WING DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 22Y CHECK, FOUND RT WING INBOARD T/E AFT FLAP INBOARD END DISBONDED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2008043000096 20080430 00096 NM 2008 4 30 SWAA082225 1 20080424 A 5330 66545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000102 20080430 00102 NM 2008 4 30 CALA0800365 1 20080425 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 CABIN STATION 867 LT BETWEEN S9L AND S8L PASSENGER SERVICE UNIT (PSU) RAIL ATTACH BRACKET TO FRAME CRACKED. REPAIRED FR AME AT STA 867 LT BETWEEN S8L AND S9L PER EA5310-04498. 2 L 7 2 4F RT A16WE 2008043000105 20080430 00105 NM 2008 4 30 CALA0800368 1 20080414 A 5320 141N5170 FLOOR SUPPORT BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13138 30351 FOUND HEAVY CORROSION ON CABIN INTERCOSTAL AT BS 345 LBL 20. INSTALLED NEW FLOOR SUPPORT REFERENCE DRAWING 141N5170 ITE M 56 AND SRM 51-40-02 AND GMM 10-900-01. 2 L 7 2 4F RT A2NM 2008043000107 20080430 00107 NM 2008 4 30 CALA0800370 1 20080408 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 STATION 869 RT SIDE BETWEEN S8RT AND S9RT AT AC BRACKET I/B FASTENER CRACKED. ACCOMPLISHED FRAME REPAIR PER CAL EC/RA 5 310-04755. 2 L 7 2 4F RT A16WE 2008043000109 20080430 00109 NM 2008 4 30 CALA0800372 1 20080408 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 STATION 787 RT SIDE BETWEEN S8RT AND S9RT AT AC BRACKET I/B FASTENER HOLE IS CRACKED. ACCOMPLISHED REPAIR AT STA 787 RT SIDE BETWEEN S8RT & S9RT AC BRACKET I/B FASTENER HOLE PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008043000110 20080430 00110 NM 2008 4 30 CALA0800373 1 20080408 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 STATION 787 LT SIDE BETWEEN S8LT AND S9LT AT AC BRACKET I/B FASTENER HOLE IS CRACKED. REPAIRED CRACKED FRAME AT STA 787 LT SIDE BETWEEN S8LT AND S9LT AT AC BRACKET IAW EA 5310-04498. 2 L 7 2 4F RT A16WE 2008043000117 20080430 00117 NM 2008 4 30 CALA0800380 1 20080426 A 5315 141T5146 STIFFENER BOEING 767 767224 1385170 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 73152 30431 BODY STATION 246 FLOORBEAM VERTICAL STIFFENER CRACKED AT LBL 40". BODY STATION 246 FLOORBEAM VERTICAL STIFFENER REPAIRE D PER ECRA 5310-04725. 2 L 7 2 4F RT A1NM 2008043000119 20080430 00119 NM 2008 4 30 CALA0800355 1 20080424 A 3350 ADD71701100 BATTERY PACK BOEING 737 737724 13844BY NM CABIN DISCHARGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 38727 28797 FOUND 3 EA EMERGENCY LIGHT BATTERY PACKS BAD PER ACHK W/C 29-335 0-1-7100. REPLACED 3EA EMERGENCY BATTERY PACKS TWO IN AFT GALLEY AND ONE ROW 18A PER W/C 29-3350-1-7100, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2008043000120 20080430 00120 EA 2008 4 30 TRAX200800567 1 20080421 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 VERTICAL BEAMS AT FS 409.0+128 (WING BOX FWD BULKHEAD) CRACKED IN THE RADIUS ON THE BOTTOM OUTBOARD SIDE AT LBL-18 AND I NBOARD SIDE AT LBL 27. JOB COMPLETE. REPAIRED VERTICAL BEAMS AT FS 409.0+128 AT LBL-18 AND AT LBL-27 AS PER REO 601R-5 3-41-056. CUT OUT DAMAGE ON LBL 27 AND LBL 18 IAW REO 601R-53-41-08. PERFORMED EDDY CURRENT INSPECTION OF CUT LINES PE R MTC REQUEST IAW CRJ 200 NDTM 51-20-06. NO DEFECTS NOTED. FABRICATED REPAIR ANGLE -5 AND FILLER -7 AT LBL 18.0 FS 409 & 128 PER REO 601R-53-41-056. PICK UP ALL HOLES ON NEW REPAIR PARTS ALL WORK IAW REO 601R-53-41-056. INSTALLED REPAIR PARTS LBL 27 & LBL 18 FILLET SEALED AND RESTORED FINISH PER REO 601R-53-41-056. JOB COMPLETE. SUPPLEMENTAL SDR CLOSED 2 L 7 2 4F RT A21EA 2008043000121 20080430 00121 NM 2008 4 30 SWAA082240 1 20080427 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 202WN 33999 EEPLS LIGHT ASSY LOOSE AT ROW 1 ABC. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008043000125 20080430 00125 NM 2008 4 30 SWAA082242 1 20080427 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008043000131 20080430 00131 NM 2008 4 30 SWAA082293 1 20080427 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008043000133 20080430 00133 NM 2008 4 30 SWAA082295 1 20080427 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 2008043000134 20080430 00134 NM 2008 4 30 SWAA082294 1 20080427 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 2008043000138 20080430 00138 NM 2008 4 30 SWAA082246 1 20080425 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 729D, STR 19R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000140 20080430 00140 NM 2008 4 30 SWAA082252 1 20080427 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 23L. REMOVED AND REPLACED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008043000141 20080430 00141 NM 2008 4 30 SWAA082251 1 20080427 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008043000144 20080430 00144 NM 2008 4 30 SWAA082250 1 20080427 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 22L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008043000148 20080430 00148 NM 2008 4 30 SWAA082278 1 20080427 A 5310 6555885 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 767 TO BS 787, RBL 65, WL 208. REMOVED AND REPLACED WE B PER SRM. 2 L 7 2 4F RT A16WE 2008042800147 20080428 00147 NM 2008 4 28 SWAA082151 1 20080422 A 5755 654645168A SKIN BOEING 737 7373H4 1384600 NM NR 9 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 RIGHT NR 9 SPOILER DELAMINATED ON UPPER SURFACE. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 2008042800193 20080428 00193 NE 2008 4 28 DL76G080625 2 20080423 A 7200 ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 FOD A DALA E ENGINE SHUTDOWN C F.O.D. AP APPROACH 1 SO 27 1613B 36883 704736 32776 704736 ON APPROACH, THE A/C FLEW THROUGH A LARGE FLOCK OF BIRDS ON THE LEFT SIDE. THE NR 1 ENG INGESTED MANY BIRDS. THE CREW ADVISED THE VIBRATION KEPT CLIMBING ON THE NR 1 ENG AND THEY SHUT THE ENG DOWN ON ROLL OUT. MTC IN PROGRESS. REMOVED A ND REPLACED COMPLETE SET OF BLADES ON NR 1 ENG, PE AMM 680596PERF. TASK 71-00-00-735-267-H02 TEST 6 VIBE SURVEY ALL CHK S NML. ALSO, PERF POWER ASSURANCE CHK ALL PARAMETERS NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 2008042800203 20080428 00203 NM 2008 4 28 2008UALA02297 1 20080418 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1L OBSTRUCTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 586UA 26710 DOOR 1L WON'T ARM. FOUND VELCO D-RING NOT SECURED AND CAUGHT IN DOOR GIRT BAR. RESECURED D-RING, DOOR ARMS/DISARMS NOR MALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042800239 20080428 00239 NM 2008 4 28 2008UALA02307 1 20080418 A 3510 BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW O2 LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 104UA 26902 CREW O2 READING 20PSI ON EICAS STATUS PAGE. O2 BOTTLE LEAKING AT REGULATOR.REPLACED BOTTLE LEAK CHECKED GOOD. AC OK F OR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042800268 20080428 00268 NM 2008 4 28 QXEA200800395 1 20080421 A 5100 NONE BOMBDR DHC8 DHC8402 1390042 NM NONE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 404QX 4046 PDX- FLIGHT 2282 - FLIGHT ATTENDANT REPORTS THAT THE REAR PASSENGER DOOR (L2)IS HARD TO OPEN. MAINTENANCE OPERATED THE DOOR SEVERAL TIMES WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE, NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008042800320 20080428 00320 CE 2008 4 28 DXTA200802997 1 20080414 A 2150 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 948QS 7500149 UPON DESCENT BEFORE LANDING MOMENTARILY DETECTED SOMETHING SULFEROUS THAT DISSIPATED IMMEDIATELY - 5 MINUTES AFTER SHUTD OWN THE SAME ODOR RETURNED OUT OF CABIN RT SIDE WEMACS. REMOVED THE ACM DUCTING TO GAIN ACCESS TO THE COCKPIT ACM. REM OVED ACM. INSTALLED OVERHAULED ACM. REMOVED CABIN AND COCKPIT OZONE CONVERTERS CLEANED AND INSTALLED CONVERSIONS. REMOVE D BOTH WATER SEPERATORS AND COALESCERS AND CLEANED AND INSTALLED BOTH. INSTALLED ALL ACM DUCTING. PERFORMED OPS CHECKS A ND LEAK CHECKS ON ACM. OZONE CONVERTING AND WATER SEPARTORS. OPS CHECK AND LEAK CHECK GOOD. ALL WORK DONE IAW MM 21-51-0 0. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008042800333 20080428 00333 CE 2008 4 28 GUUA04100801 1 20080410 A 2697 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FIRE BOTTLE LOOSE A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 29 49543 UE181 FLIGHT:9263, DURING FLIGHT, RT DISCHARGE LIGHT ILLUMINATED INTERMITTENTLY. RESECURED WIRE AT RT FIRE BOTTLE. 2 L 7 2 4T 4 T RT A24CE E26NE 2008042800340 20080428 00340 SW 2008 4 28 EVCA022308002 1 20080223 A 5302 206032308103 FRAME BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL TAIL BOOM CRACKED E EVCA K NONE O OTHER IN INSP/MAINT 1 CE 03 4338D 51560 CAE895152 TAILBOOM ATTACH FRAME FOUND CRACKED DURING SCHEDULED INSPECTION. 1 G 7 1 3U 3 U H2SW E1GL 2008042800351 20080428 00351 NM 2008 4 28 USAA920080838 1 20080331 A 5315 SUPPORT ANGLE BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 23634 CLT - MAJOR REPAIR - C22 CHECK - AN 8 INCH CRACK ON FLOORBEAM UPPER CHORD SUPPORT ANGLE AT BS 380 - 400, BL 0. INSTALLE D REPAIR IAW SRM 51-20-01, 50-30-50-11 FIG 1 DETAIL 1 AND 51-40-03. *SUPPLEMENT* IDENTIFIED PART AS "FLOORBEAM UPPER C HORD SUPPORT ANGLE". 2 L 7 2 4F RT A16WE 2008042800368 20080428 00368 WP 2008 4 28 UPS08852067 1 20080425 A 2421 PANEL DOUG DC8 DC871F 302199D WP ELECTRICAL FAILED A IPXA B EMER. DESCENT G MULTIPLE FAILURE CR CRUISE 1 SO 01 702UP 45902 FL340 - LIGHTS FLICKERED AND NR 1, 3, 4 GEN UNPARALELLED LIGHTS CAME ON. VOLTS & FREQS OK ON 1-3-4. NR 2 VOLTS & FREQS AT 50 VOLTS & 385 CYS. CHECK LIST ACCOMPLISHED; GOT EVERYTHING BACK W/GEN PARALLELED. LATER SAME SENERIO, BUT NOTHING CAME BACK. LIGHT ELECTRIC BURN ODOR. NR 2 VRP/GCP C/B POPPED & BURNING SMELL COMING FROM IT. REPLACED NR 2 VOLTAGE R EG & GEN CONTROL PANEL. R&R NR 2 BTB; R & R BUSS PROTECTION PANEL. GROUND RUN ALL ENGINES, PERFORMED ADJUSTMENT TEST PER MM 24-20-03-4, 24-20-00-2, 24-20-07-2. 2 L 7 4 4F RT 4A25 2008042800369 20080428 00369 NM 2008 4 28 USAA920080882 1 20080423 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 CLT - MAJOR REPAIR - RON - CORROSION ON FUSELAGE SKIN, BS 500F, S28L. REPAIRED FUSELAGE SKIN, BS 500F, S28L IAW USAIRWA YS EA 100437. 2 L 7 2 4F RT A16WE 2008042800381 20080428 00381 NM 2008 4 28 SB08021 1 20080424 A 3350 1012721 LIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 456UW 25020 ORD - MAINTENANCE REPORTED THE EMERGENCY LIGHT LENSE AT SEAT 15C WAS MISSING AND THE LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND LENSE. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008042900012 20080429 00012 NM 2008 4 29 08FDEA01464 1 20080421 A 5414 311N51931 PANEL BOEING 757 75727B 1384921 NM ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 PYLON NR 1 SKIN CUTOUT AT ACCESS PANEL 433AL FOUND CORROSION. TO EVALUATE AND RECTIFY, REPLACED SKIN CUTOUT OF ACCESS P ANEL IAW SRM 51-10-02 AND DRAWING 311N5002. REPAIRED CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008042900013 20080429 00013 EU 2008 4 29 USAA920080905 1 20080418 A 2910 D2901005200100 LINE AIRBUS A321 A321211 3930370 EU ZONE 400 - NACE LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 190UW 1436 FLT NR 1193 - PHL-PHX - DIVERSION - CREW REPORTED ECAM MESSAGE FOR GREEN HYDRAULIC FLUID LOW PRESSURE. AIRCRAFT DIVERTE D TO PIT. EMERGENCY EQUIPMENT WAS CALLED AND AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE PRES SURE HYDRAULIC LINE IN THE OUTBOARD LT PYLON. LEAK CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008043000002 20080430 00002 SO 2008 4 30 C2XA08ON116 1 20080417 A 2612 M835366022M RELAY EMB 145 EMB145XR 3260214 SO FIRE DETECTION FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 33182 14500909 FLT MX - ONT - BAG FIRE DETECTION TEST LIGHT WILL NOT ILLUMINATE. MX PERSONNEL REMOVED AND REPLACED RELAYS K0629, K0625 , AND K0630 OPERATIONALLY CHECKED SATISFACTORY, AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008043000004 20080430 00004 SO 2008 4 30 C2XA08IA118 1 20080417 A 3350 66367 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15555 145594 AUS - DURING MAINTENANCE INSPECTION THE 4TH AISLE PATH LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT STRIP. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008043000009 20080430 00009 SO 2008 4 30 RAIA00804022 1 20080421 A 2611 DETECTION SYS EMB 145 EMB145 3260210 SO CARGO BAY MALFUNCTIONED A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 801HK 145053 FLT 3516 - BDL - BAGGAGE AREA SMOKE DETECTOR WENT OFF DURING CRUISE. MAINTENANCE PERFORMED AN INSPECTION OF THE CARGO B AY FOR EVIDENCE OF FIRE AND SMOKE WITH NO EVIDENCE OF EITHER. ALSO PERFORMED AN OPERATIONAL OF THE BAG SMOKE DETECTION SYSTEM WITH NO FAULTS NOTED. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4F RT T00011AT 2008043000012 20080430 00012 SO 2008 4 30 RAIA00804021 1 20080420 A 7830 THRUST REVERSER EMB 145 EMB145 3260210 SO NR 1 ENGINE MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 802HK 145066 FLT 3564 - STL - E1 THRUST REVERSER DISAGREE MESSAGE ON THE EICAS. MAINTENANCE DEFERRED THE T/R SYSTEM IAW MEL. 2 L 7 2 4F RT T00011AT 2008043000042 20080430 00042 NM 2008 4 30 2008UALA02294 1 20080419 A 5620 FLOOR SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1640-1660 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 CABIN FLOOR SUPPORT INTERCOSTAL CORRODED BETWEEN STA 1640 - 1660, RBL 57. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW INT ERCOSTAL (P/N 146N5246-8). 2 L 7 2 4F 4 F RT A2NM E17NE 2008043000054 20080430 00054 EA 2008 4 30 TRAX200800569 1 20080422 A 2560 GLOWSTRIP CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 RT EMERGENCY FLOOR STRIP FWD ARE MISSING/DAMAGED. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APP ROPRITE CORRECTIVE ACTION. CABIN EMERGENCY LIGHTS - PHOTOLUMINESCENT FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING. 2 L 7 2 4F RT A21EA 2008043000056 20080430 00056 EA 2008 4 30 TRAX200800571 1 20080423 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 CORROSION ON FLOOR SUPPORT STA 310 TO 349 AT ASD SILL. REMOVED FASTENERS ON LOWER SILL ANGLE AND UPPER ATTACH ANGLE. R EMOVED UPPER ATTACH ANGLE IAW SRM 51-42-06. REMOVED FLOOR SUPPORT ANGLE . DRILLED NEW SUPPORT ANGLE 601R31527-221 IAW SR M 51-40-11. READY TO INSTALL. INSPECTED PARTS AT FLOOR SUPPORT. OK TO INSTALL. INSTALLED ASD SILL & ANGLE FOR FLOOR SU PPORT PER SRM 51-42-06. SEALED, PRIMED, AND PAINTED ASD SILL LOWER AND UPPER ANGLES & ASSOCIATED FASTNER PER SRM 51-25 -00 AND 51-23-00. 2 L 7 2 4F RT A21EA 2008043000075 20080430 00075 NM 2008 4 30 SWAA082207 1 20080424 A 5315 6545410 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 701, BL 0. REPAIRED FLOORBEAM PER ER AND BOEING SB. 2 L 7 2 4F RT A16WE 2008043000078 20080430 00078 NM 2008 4 30 SWAA082235 1 20080424 A 3350 R340 RESISTOR BOEING 737 7375H4 138449D NM COCKPIT DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. FOUND RESISTOR M1219 DISCONNECTED. RECONNECTE D RESISTOR PER MM. 2 L 7 2 4F RT A16WE 2008043000108 20080430 00108 NM 2008 4 30 CALA0800371 1 20080408 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 STATION 747 LT SIDE BETWEEN S8LT AND S9LT AT AC BRACKET I/B FASTENER CRACKED. REPAIRED CRACKED FRAME AT STATION 747 LT SIDE BETWEEN S8LT & S9LT AT AC BRACKET IAW EA 5310-04498. 2 L 7 2 4F RT A16WE 2008043000116 20080430 00116 NM 2008 4 30 CALA0800379 1 20080427 A 5315 141T5108 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 73152 30431 BODY STATION 325, LBL 30 TO LBL 50 FLOOR SUPPORT FOUND CORRODED. BODY STATION 325 LBL 30 TO LBL 55 FLOOR SUPPORT REPAIR ED IAW SRM 53-00-51, REPAIR 1 FIG 201. 2 L 7 2 4F RT A1NM 2008041500086 20080415 00086 NM 2008 4 15 SWAA081871 1 20080408 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, LBL 4. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500091 20080415 00091 NM 2008 4 15 SWAA081887 1 20080408 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041500103 20080415 00103 NM 2008 4 15 SWAA081878 1 20080408 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500, LBL 25 TO LBL 29. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008041500113 20080415 00113 NM 2008 4 15 SWAA081901 1 20080409 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER 15R CRACKED AT BS 380. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008041500114 20080415 00114 NM 2008 4 15 SWAA081902 1 20080409 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041500115 20080415 00115 NM 2008 4 15 SWAA081904 1 20080409 A 5330 6545765 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500134 20080415 00134 EA 2008 4 15 TRAX200800507 1 20080408 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 AAR - 2081 - CRACK IN ATTACH ANGLE BETWEEN 280 FRAME AND FLOOR SUPPORT BEAM AT RBL 9 I/B SIDE (MARKED). REMOVED CRACK ATTACH ANGLE. FABRICATED REPLACEMENT ANGLE IAW REO 601R-53-11-171. INSTALLED REPAIR ATTACH ANGLE IAW REO 601R-53-11-171 . 2 L 7 2 4F RT A21EA 2008041500141 20080415 00141 EA 2008 4 15 TRAX200800514 1 20080408 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 830AS 7236 EMERGENCY LIGHT AT PAX DOOR BROKEN. 2 L 7 2 4F RT A21EA 2008041500190 20080415 00190 NM 2008 4 15 08FDEA01398 1 20080414 A 5730 ARB39545 DOUBLER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 525FE 48565 RIGHT WING LEADING EDGE SKIN RIB DOUBLER AT STATION XOS 667 FOUND CRACKED. REMOVED AS PER SRM 51-33-01 VOLUME II AND FA BRICATED NEW RIB DOUBLER PER DRAWING ARB3954 AND INSTALLED NEW DOUBLER PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041500198 20080415 00198 NM 2008 4 15 SWAA081928 1 20080410 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008041500199 20080415 00199 NM 2008 4 15 SWAA081929 1 20080410 A 5315 65C33948 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 947, LBL 5. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 2008050700101 20080507 00101 NM 2008 5 7 AALA200800856 1 20080407 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050700103 20080507 00103 NM 2008 5 7 AALA200800843 1 20080407 A 3350 OL3071BPEGPL LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 DFW - EMERGENCY LIGHT AT SEAT 44C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 44C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050700117 20080507 00117 NM 2008 5 7 QXEA200800428 1 20080428 A 2434 400SG163Q GENERATOR BOMBDR DHC8 DHC8402 1390042 NM DC SYSTEM OVERHEATED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 419QX 10826 563 4145 GEG - FLIGHT 2347 (MSO-SEA), CLIMBING THROUGH 19,000 FEET RECEIVED A MASTER CAUTION MESSAGE WITH THE DC BUS FAULT ALONG WITH LOSS OF PRESSURIZATION. PERFORMED UNEVENTFUL DESCENT. RESET BUS PER CHECKLIST AND THE BUS CAME BACK. ALSO HAD DC GEN HOT, STALL SYSTEM, AND PUSHER FAIL LIGHTS. ACCOMPLISHED UNEVENTFUL LANDING. MAINTENANCE FOUND GENERATOR OVERHEATE D WITH NO OTHER EXTERNAL AIRFRAME DAMAGE. INLET AIR SHROUD WAS BROKEN. REPLACED GENERATOR AND SHROUD. OPERATIONAL CHE CKS GOOD, AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008050700120 20080507 00120 EA 2008 5 7 MASA200800352 1 20080429 A 3520 DOOR CNDAIR CL600 CL6002B19 1900309 EA OXYGEN MASK LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37342 7342 ASH FLT 7309 ORD-BMI - CREW REPORTED THE SEAT 2 D/F PASSENGER O2 MASK DOOR IS LOOSE, POSSIBLY ACCIDENTALLY HIT BY A PASS ENGER. MX RESECURED THE DOOR. 2 L 7 2 4F RT A21EA 2008050700121 20080507 00121 NM 2008 5 7 DHL2008788003 1 20080502 A 5754 STRUCTURE BOEING 727 727214 138407R NM NR 3 K FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 NR 3 L/E K-FLAP HAS SMALL CRACK ON THE BOTTOM I/B CORNER. REPAIRED SMALL CRACK PER SRM 51-40-0. 2 L 7 3 4F A3WE 2008050500011 20080505 00011 EA 2008 5 5 VNAA0804005 1 20080405 A 5753 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT WING DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 216PS 7882 CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE PERFORMED A VISUAL EN ROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND DAMAGE TO THE RIGHT HAND INBOARD FLAP TRAILING EDGE AND REPAIRED THE DAMAGE UNDER REO 601R-57-52-732 AND THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE PERFORMED OPERATIONAL CHECKS. OPS CHECKS WERE GOOD. AIRCRAFT WAS REL EASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008050500028 20080505 00028 NM 2008 5 5 SWAA082335 1 20080429 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008050500032 20080505 00032 NM 2008 5 5 SWAA082345 1 20080429 A 5315 BAC15091000146 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 421LV 32452 DURING SCHEDULED 6Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, BETWEEN LBL 17 AND RBL 8. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2008050500033 20080505 00033 NM 2008 5 5 SWAA082329 1 20080429 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 495WN 33869 DURING SCHEDULED MV2 CHECK, FOUND EEPLS ASSY BROKEN AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008050500043 20080505 00043 NM 2008 5 5 SWAA082350 1 20080501 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008050500045 20080505 00045 NM 2008 5 5 SWAA082376 1 20080501 A 5315 6545410144 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 663, LBL 24.75. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2008050500071 20080505 00071 2008 5 5 HNAA0800142 4 20080422 A 3454 066107804 RECEIVER DHAV DHC8 DHC8102 2809003 NM NR 1 FAILED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 07 935HA 25991 229 142 ON APPROACH INTO CLT NR 1 NAVIGATION RECEIVER FAILED FOLLOWED BY A STRONG ODOR. REMOVED AND REPLACED NR 1 NAV RECEIVER IAW 34-55-05. RAMP CHECK GOOD. 2 H 7 2 4T RT A13NM 2008050500079 20080505 00079 NM 2008 5 5 HNAA0800144 1 20080427 A 2910 82920010229 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYS CRACKED A HNAA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 EA 07 984HA 32011 32011 377 HYDRAULIC LEAK AT PSU ROW 5DF. AIRCRAFT RETURNED TO GATE. MX CAPPED LINE OFF. AIRCRAFT FERRIED TO MDT. MX REPLACED N OSE GEAR DOWN LINE. 2 H 7 2 4T RT A13NM 2008050500080 20080505 00080 NM 2008 5 5 HNAA0800145 1 20080427 A 6123 AUTOFEATHER SYS DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTIONED A HNAA K NONE O OTHER TO TAKEOFF 1 EA 07 936HA 49735 49735 145 AUTOFEATHER FAILED TO ARM ON TAKEOFF ROLL. CYCLED ARM SWITCH OPS NORMAL AT THIS TIME. COULD NOT DETERMINE FROM THE INF ORMATION AVAILABLE IF THIS WAS AN ABORTED TAKEOFF. 2 H 7 2 4T RT A13NM 2008050500091 20080505 00091 SO 2008 5 5 FDKA200804181 1 20080429 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6083 MCO-EYW. CREW REPORTED A STRANGE ODOR IN THE COCKPIT. MX PERFORMED OPS CHECK OF PACK SYSTEM. NO DEFECTS NOTE D. 2 L 7 2 4T RT T00011AT 2008050500105 20080505 00105 NM 2008 5 5 USAA920080927 1 20080422 A 5340 69418856 STRINGER CLIP BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CRACKED STRINGER CLIP, BS 794, S18R, WL 199. REPLACED STRINGER CLIP, BS 794, S18R, WL 199 IAW B737 SRM 51-40-05. 2 L 7 2 4F RT A16WE 2008050500120 20080505 00120 EU 2008 5 5 08FDEA01592 1 20080425 A 5230 A52371015006 SKIN PANEL AIRBUS 310 A310203 3930313 EU CARGO BAY DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 403FE 230 MAIN CARGO DOOR UPPER END, OUTER SKIN DENTED, 9.4 IN LONG, 2 IN WIDE AND .100 IN DEEP, LOCATED 2 IN AFT OF FR 22 CUT OUT DAMAGED AND ACCOMPLISHED SKIN REPAIR IAW FEDEX EA 6-5230-118119, RELEASE DATE 28 MARCH, 2008. 2 L 7 2 4F RT A35EU 2008050500122 20080505 00122 NM 2008 5 5 08FDEA01594 1 20080425 A 5320 651751712 ANGLE BOEING 727 7272S2F 1384O81 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 VENTRAL STAIRWELL RT SIDE BELOW AIRSTAIR ACTUATOR FITTING, TORQUE BOX BS 1263 UPPER ANGLE FWD SIDE OF BULKHEAD HAS CRACK . REMOVED ANGLE FWD SIDE IAW SRM 51-30-2. LOCATED AND DRILLED NEW ANGLE IAW SRM 51-30-5. INSTALLED NEW ANGLE IAW SRM 5 1-30-2. 2 L 7 3 4F A3WE 20080519 WP 2008 5 19 08FDEA01841 1 20080513 A 5753 ARC25182 BRACKET DOUG MD10 MD1010F 3022112 WP T/E FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 RIGHT WING INBD FLAP, INBD HINGE POINT IS GOUGED. BLENDED AREA. FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01 AND DWG ARC 2518. REMOVED DAMAGED FAIL SAFE STRAP AND RECEIVED A NEW STRAP. LOCATED, DRILLED AND INSTALLED THE NEW STRAP IAW SRM 51 -35-01, SRM 1-31-01, SRM 51-33-01& DWG ARC 2518. REMOVED BUSHING; FABRICATED / MACHINED A NEW BUSHING & INSTALLED THE N EW BUSHING IAW CMM 51-52-01. ALODINED & PRIMED IAW SRM 51-21-01. 2 L 7 3 4F RT A22WE 2008050500142 20080505 00142 NM 2008 5 5 08FDEA01615 1 20080428 A 5730 ARB74023 SKIN DOUG MD11 MD11F 3023600 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 628FE 48447 16 EACH FASTENER HOLES FOUND WITH CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOO R CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. COMPLIED WITH E.A. 1-5710-113137, CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008043000122 20080430 00122 NM 2008 4 30 SWAA082241 1 20080427 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 223WN 32492 EEPLS LENS MISSING AT ROW 7 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008043000136 20080430 00136 NM 2008 4 30 SWAA082248 1 20080425 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008043000137 20080430 00137 NM 2008 4 30 SWAA082247 1 20080425 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 1. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008043000145 20080430 00145 NM 2008 4 30 SWAA082276 1 20080427 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 15R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008043000151 20080430 00151 NM 2008 4 30 SWAA082257 1 20080425 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 419WN 29824 DURING SCHEDULED 6Y CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 157. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008043000152 20080430 00152 NE 2008 4 30 SWAA082292 2 20080426 A 7200 CFM567B24G22 ENGINE BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE LEFT FAILED A SWAA O OTHER Y ENGINE STOPPAGE TO TAKEOFF 1 SW 29 467WN 33830 874806 ABORTED TAKEOFF/DECLARED EMERGENCY. NR 1 ENGINE FAIL LIGHT ILLUMINATED AS TAKEOFF THRUST SET, ACCOMPANIED BY LOUD POP. EGT GAUGE INDICATED 445 DEGREES WITH ENGINE FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008043000153 20080430 00153 NM 2008 4 30 SWAA082279 1 20080427 A 5320 6545833 ANGLE BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND ZEE CHORD CORRODED AT BS 270, LBL 11 TO RBL 11, WL 208. REMOVED AND REPLACED ZEE CHOR D PER SRM. 2 L 7 2 4F RT A16WE 2008043000156 20080430 00156 NM 2008 4 30 SWAA082281 1 20080427 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER 4L CRACKED AT BS 1010. REPAIRED STRINGER PER EA. 2 L 7 2 4F RT A16WE 2008043000159 20080430 00159 NM 2008 4 30 SWAA082260 1 20080427 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 520, STR 28R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008043000163 20080430 00163 NM 2008 4 30 SWAA082282 1 20080427 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND RIGHT WING NR 4 L/E SLAT DELAMINATED AT OUTBOARD CORNER. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008043000173 20080430 00173 NM 2008 4 30 SWAA082265 1 20080424 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2008043000174 20080430 00174 NM 2008 4 30 SWAA082267 1 20080426 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 444, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008043000175 20080430 00175 NM 2008 4 30 SWAA082266 1 20080426 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 820, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008043000177 20080430 00177 NM 2008 4 30 SWAA082268 1 20080427 A 3350 30043213 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008043000183 20080430 00183 NM 2008 4 30 CALA0800383 1 20080428 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 CABIN STATION 400 BETWEEN S8R AND S9R PASSENGER SERVICE UNIT RAIL ATTACH BRACKET TO FRAME CRACKED. REPAIRED FRAME AT ST ATION 400 BETWEEN S8R AND S9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008050500147 20080505 00147 WP 2008 5 5 08FDEA01620 1 20080426 A 5411 AUB70799 RIB DOUG MD10 MD1010F 3022112 WP NR 1 PYLON DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 1 PYLON PANEL 437EL HAS A DAMAGED RIB. REMOVED REPLACED RIB NR AUB7079-9 PO NR 577666.3 IAW DC/MD 10 SRM 51-35-01 VO L II. 2 L 7 3 4F RT A22WE 2008050500152 20080505 00152 WP 2008 5 5 08FDEA01629 1 20080428 A 5347 ADA765621 SEAT TRACK DOUG DC10 DC1010F 3022111 WP FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE ON SEAT TRACK STA 635- 615 X -28, FOUND USURED AND MISSING MATERIAL REPAI RED FOR SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F A22WE 2008050500155 20080505 00155 WP 2008 5 5 08FDEA01632 1 20080425 A 5347 NCA602225 SEAT TRACK DOUG MD10 MD1010F 3022112 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 MAIN CABIN SEAT TRACK IN BALLMAT AREA SCALLOPS BROKEN AND SEVERAL GOUGES AT STA 755 TO STA 763 LBL 28. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 VOL I FIG 5. REMOVED FLOOR PANELS AT BS 625-890 LBL 28-48 TO GAIN ACCESS. REMOV ED TRACK FROM BS 725-755 & SPLICED IN A NEW SECTION AT BS 755 IAW SRM 53-70-00 VOL I. INSTALLED FLOOR PANELS BS 675-8 90 LBL 28 & 48 IAW AMM 53-21-01-2. 2 L 7 3 4F RT A22WE 2008050500176 20080505 00176 EA 2008 5 5 MASA200800348 1 20080427 A 2510 1323905 SPRING CNDAIR CL600 CL6002B19 1900309 EA F/A SEAT BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 47202 7202 ASH FLT 7230 ORD - CAE FORWARD FLIGHT ATTENDANT SEAT RETRACT SPRING BROKE. REMOVED AND REPLACED OUTBOARD SPRING, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008050500196 20080505 00196 WP 2008 5 5 IXXA08SMN104S 1 20080314 A 5322 FITTING DOUG DC8 DC873F 302199F WP CARGO BAY CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STATION 759.000 RIGHT BOTTOM LINE 22". REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008050500215 20080505 00215 EU 2008 5 5 08FDEA01654 1 20080429 A 5532 A5537172600600 PANEL AIRBUS 300 A300F4605R 3930327 EU VERTICAL STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 VERTICAL STAB L/E 322 AL HAD GOUGES ABOVE THE HOIST POINT ON THE LEFT AND RIGHT SIDES. REMOVED GOUGED PAINT AND REFINISH ED AREA IAW SRM 55-32-00 & 51-75-10. 2 L 7 2 4F RT A35EU 2008050700127 20080507 00127 EA 2008 5 7 A6WA200840327 1 20080410 A 5510 DIAPHRAGM CNDAIR CL600 CL6002B19 1900309 EA STAB DRAG ANGLE MISSING A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 STABILIZER DRAG ANGLE DIAPHRAGM CLOTH MISSING. (M) REPAIRED IAW REO 601R-55-32-075 REV E. 2 L 7 2 4F RT A21EA 2008050700130 20080507 00130 EU 2008 5 7 08FDEA01758 1 20080505 A 5347 R5307008820200 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 MAIN DECK CARGO SEAT TRACK NR 1 HAS 2 AREAS OF CORROSION BETWEEN FR 57.1 AND FR 58. REMOVED LEVEL 1 CORROSION, REMOVED DAMAGED SECTION AND REPAIRED SEAT TRACK NR 1 WITH SPLICE REPAIR BETWEEN FR 57 AND FR 58 IAW A300-600 SRM 53-10-16, FIG 2 01. 2 L 7 2 4F RT A35EU 2008050700131 20080507 00131 WP 2008 5 7 08FDEA01760 1 20080505 A 5730 ARC12838 PANEL DOUG MD10 MD1010F 3022112 WP RT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 RIGHT WING T/E PANEL NR 645 BB L/E IS CHAFED. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IN REF TO SRM 57-00-01 VOL I. R ECEIVED NEW PART. DRILLED, DEBURRED AND COUNTERSUNK IN REF TO SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 2008050700133 20080507 00133 NM 2008 5 7 CALA0800405 1 20080430 A 5320 6546548 SUPPORT BRACKET BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 AIR CONDITIONING SUPPORT BRACKET CRACKED AT RIGHTHAND FRAME STATION 747 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT RIGHTHAND FRAME STATION 747 BETWEEN S-8 AND S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008050700136 20080507 00136 NM 2008 5 7 08FDEA01763 1 20080505 A 5313 655458350 STRINGER BOEING 727 7272S2F 1384O81 NM BS 1010-1030 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 STR 26 R HAS EXFOLIATION CORROSION BETWEEN STA 1010 AND 1030 CUT-OUT DAMAGED STRINGER SECTION (DIMENSION 12" LONG) AND F ABRICATED HAT SECTION AND 1 SPLICER IAW SRM 53-10-3 FIGURE 1 AND 53-10-2 FIGURE 9. TREATED AND PRIMED PARTS IAW SRM 51- 10-2 AND INSTALLED REPAIR PARTS AT STRINGER 26RT BETWEEN STA 1010 AND 1030 IAW SRM 53-10-3 FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 2008050700137 20080507 00137 NM 2008 5 7 CALA0800407 1 20080430 A 5320 6546555 SUPPORT BRACKET BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 AIR CONDITIONING SUPPORT BRACKET CRACKED AT RIGHTHAND FRAME STATION 867 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT RIGHTHAND FRAME STATION 867 BETWEEN S-8 AND S-9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 2008050700142 20080507 00142 NM 2008 5 7 MWEA080061 1 20080425 A 3350 8039251 BATTERY BOEING 717 717200 1383700 NM CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 914ME 55177 EMERGENCY LIGHT AT ROW 17 THROUGH 22 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY. 2 L 7 2 4F TR A6WE 2008050700145 20080507 00145 EA 2008 5 7 COMA0860234 1 20080430 A 3350 59257 INVERTER CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 965CA 7131 FLIGHT 5326 - EMERGENCY LIGHTS NOT WORKING FROM ROW 9 AFT. REPLACED NR 4 INVERTER. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008050700148 20080507 00148 NM 2008 5 7 MWEA080063 1 20080429 A 5330 991551733 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 822ME 49759 FUSELAGE SKIN LOWER TWO DENTS APU SHROUD AREA, FORWARD LOWER AREA RIGHT SIDE JUST FORWARD OF APU COMBUSTION. CUT OUT DA MAGE, FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F RT A6WE 2008050700149 20080507 00149 NM 2008 5 7 DHL2008760549 1 20080422 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272B7 138407L NM BS 870-950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED CORRODED SEAT TRACK, FABRICATED, AND INSTALLED SEAT TRACK SECTION AT BS 870 TO 950, LBL 45.5, PER B727 SRM 53-10 -2 FIG 7 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 2008050700152 20080507 00152 2008 5 7 USAA920080975 4 20080430 A 2565 D31516317 SLIDE AIRBUS 320 A320232 3930326 EU R1 DOOR LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 673AW 30413 5090 2312 FLT 640 - PHX - EES - R-1 DOOR SLIDE PRESSURE INDICATOR IS APPROX 1/8 OUT OF GREEN BAND. MAINTENANCE REMOVED AND REPLAC ED THE R-1 SLIDE. 2 L 7 2 4F RT A28NM 2008050700159 20080507 00159 NM 2008 5 7 DHL2008760515 1 20080416 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272B7 138407L NM BS 480-690 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND REPLACED SEAT TRACK SECTION AT LBL 24, FROM BS 480 TO 690, PER B727 SRM 53-10-2 FIG 7 AND 53-10 -5 FIG 1. 2 L 7 3 4F A3WE 2008050700165 20080507 00165 EA 2008 5 7 SWIA200819542 1 20080428 A 3233 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 464SW 7827 FLT 3951 - RECEIVED A "GEAR DISAGREE" MESSAGE WHILE EXTENDING GEAR. CYCLED GEAR HANDLE AND GEAR OPERATED NORMALLY. REP LACED LEFT GEAR SIDE STAY ACTUATOR PER AMM 32-32-01. OPS AND LEAK CHECK GOOD, P/N OFF 17008-115, S/N OFF 01774. 2 L 7 2 4F RT A21EA 2008050700167 20080507 00167 EA 2008 5 7 SWIA200819543 1 20080422 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CAIBN UNSECURE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 936SW 7726 FLT 6672 - AFT CEILING LEVEL EMERGENCY FLOOD LIGHT IS NOT SECURE. RESECURED AFT CEILING EMERGENCY FLOOD LIGHT COVER. 2 L 7 2 4F RT A21EA 2008050700172 20080507 00172 EA 2008 5 7 SWIA200819548 1 20080421 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN SMOKE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 970SW 7881 FLT 6676 - CREW SMELLED SMOKE IN THE COCKPIT FOLLOWED BY A "SMOKE TOILET" MESSAGE. INSPECTED AND PERFORMED HIGH POWER R UNS ON AIRCRAFT WITH NO DISCREPANCIES NOTED. REPLACED LAVATORY SMOKE DETECTOR IAW RJ 200 MM REF 26-16-01. OPS CHECK GO OD. 2 L 7 2 4F RT A21EA 2008050700174 20080507 00174 EA 2008 5 7 SWIA200819549 1 20080202 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 611SK 10035 STA 280 BEAM IS CRACKED AT RBL11 AND LBL11, FOUND AT C-CHECK. INSTALLED NEW CROSSBEAM PER CRJ7/9 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008050700175 20080507 00175 EA 2008 5 7 SWIA200819550 1 20080202 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 611SK 10035 COCKPIT FLOOR SUPPORT IS CORRODED AT FS 280, FOUND AT C-CHECK. REPLACED COCKPIT FLOOR SUPPORT AT FS 280 PER CRJ700 SRM 51-42-06-001-001-A01. 2 L 7 2 4F RT A21EA 2008050700176 20080507 00176 NM 2008 5 7 DHL2008760531 1 20080430 A 5344 SEEABOVE HINGE BOEING 727 7272B7 138407L NM CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED AND REPLACED CRACKED AFT HINGE SECTION, BS 620 TO 640, FOR MCD PER B727-200 FREIGHTER MM FIG 5201B AND CH 52 REV G, STOCK HINGE P/N MS20001-16-7200 2 L 7 3 4F A3WE 2008050700180 20080507 00180 SO 2008 5 7 SIMA200812105 1 20080425 A 5320 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 20174 5000 145121 DURING A MBV INSPECTION, THE LEFT OMEGA BEAM WAS FOUND CORRODED AROUND A NUT PLATE HOLE 8" AFT OF FRAME 22. BLENDED THE DAMAGED AREA TO REMOVE THE CORROSION AND PERFORM NDT. FILLED THE BLENDED AREA WITH HYSOL EA934NA RESIN AND CURDED. FA BRICATED. A REPAIR DOUBLER FROM AL 2024-T3, CLEANED AND TREATED REPAIR PART. REPAIR DONE IAW EMBRAER 145 SRM (SRM EMB 145/ 1142 REV 39) CHAPTER 53-21-10 FIGURE 206. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008050700184 20080507 00184 EA 2008 5 7 TRAX200800581 1 20080427 A 5242 CASTING CNDAIR CL600 CL6002C10 1390015 EA E&E DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 730EV 10141 AVIONICS DOOR HANDLE CASING CRACKED IN THE RADIUS AND CRACK CONFIRMED BY EDDY CURRENT. 2 L 7 2 4F RT A21EA 2008050700187 20080507 00187 NM 2008 5 7 USAA920080974 1 20080417 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 450UW 24933 PIT - MAJOR REPAIR - CRACKED FRAME, BS 492.4, S24R. REPAIRED FRAME, BS 492.4, S24R IAW USAIRWAYS EA 110913. 2 L 7 2 4F RT A16WE 2008050700188 20080507 00188 NM 2008 5 7 USAA920080976 1 20080418 A 5320 146N52819 FITTING BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL CLIP, BS 1300, LBL 45.5, WL 208. REPLACED INTERCOSTAL CLIP, BS 130 0, LBL 45.5, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008050700194 20080507 00194 NM 2008 5 7 USAA920080983 1 20080419 A 5320 143N51974 INTERCOSTAL BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL, BS 660, RBL 45.5. REPLACED INTERCOSTAL, BS 660, RBL 45.5 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008050700199 20080507 00199 NM 2008 5 7 SB08024 1 20080501 A 3350 20121 POWER SUPPLY BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 435US 24557 CLT - MAINTENANCE REPORTED BOTH FORWARD OVERWING EMERGENCY LIGHTS INOPERATIVE ALONG WITH SEVERAL INTERIOR BULL NOSE EMER GENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY M1435 AND RESECURED GROUND AT GD240. OPERATION AL CHECK OF LIGHTS GOOD. 2 L 7 2 4F RT A16WE 2008050700201 20080507 00201 NM 2008 5 7 ZZDA2008096 1 20080501 A 5280 DOOR BOEING 717 717200 1383700 NM MLG DAMAGED A ZZDA K NONE J WARNING INDICATION AP APPROACH 1 SO 37 992AT 55136 GEAR DOOR OPEN MESSAGE ON FINAL. PERFORMED OPS CHECK OF LANDING GEAR PER MM 32-30. CHECKS NORMAL. 2 L 7 2 4F TR A6WE 2008050700205 20080507 00205 EA 2008 5 7 TRAX200800586 1 20080430 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 926EV 7843 FLOOR EMERGENCY FLOODLIGHT DAMAGED. 2 L 7 2 4F RT A21EA 2008050700223 20080507 00223 EA 2008 5 7 A6WA200840336 1 20080414 A 5610 NP1393215 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A A6WA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 31 407AW 16874 7424 CAPTAIN WINDSHIELD SHATTERED IN FLIGHT AT FL 260. R & R CAPT WINDSHIELD IAW AMM 56-11-01. OPS CHECK GOOD. NO LEAKS. 2 L 7 2 4F RT A21EA 2008050700225 20080507 00225 EU 2008 5 7 NSVA2008023 1 20080504 A 7712 INDICATOR SAAB SF340 340B 7860101 EU RT TORQUE ERRATIC A NSVA E ENGINE SHUTDOWN N FALSE WARNING AP APPROACH 1 EA 27 249CJ 340B249 ON APPROACH, RT TORQUE GAUGE ERRATIC, DROPPED TO ZERO, TRIGGERED AUTO COARSEN, SHUT DOWN ENGINE AND LANDED UNEVENTFULLY. REMOVED AND REPLACED RT DECU P/N ON 6071T20P18, P/N OFF 6071T20P16 S/N ON LMAT2255, S/N OFF ECDTT1933 AND RT TQ SENSOR P/N ON 0774088T42P01, S/N ON EGNFB857, S/N OFF T1936. OPS CHECK GOOD IAW AMM 76-10-57. 2 L 7 2 4T RT A52EU 2008050700228 20080507 00228 GL 2008 5 7 SIMA200812601 2 20080429 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL LEFT LEAKING A SIMA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 650AE 8619 3806 145417 CAE312737 ON FLIGHT 4348, CREW REPORTED THAT ATOMIZED TURBINE OIL FUMES WERE INTRODUCED INTO THE CABIN CONDITIONED AIR WHEN USING ENG 1 BLEED AS SUPPLY SOURCE. WHEN USING BLEED 2 OR APU TO SUPPLY A/C PACKS CONDITIONED AIR IS GOOD. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR1 ENGINE IAW WORK CARD 71-00-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008050700229 20080507 00229 SO 2008 5 7 SIMA200812103 1 20080425 A 5320 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 827AE 5000 145602 DURING A MBV INSPECTION, THE RT OMEGA BEAM AT FRAME 23 WAS FOUND CORRODED. BLENDED THE CORRODED AREA TO REMOVE THE DAMA GE. APPLIED ALODINE AND EPOXY PRIMER TO THE REWORKED AREA. FAB A 4.0 BY 2.0 REPAIR DOULBER FROM AL - 2024-T3 INSTALLED REPAIR. WORK DONE WITH EMBRAER 145 SRM (SRM EMB-145/1142 REV.38) CHAPTER 53-21-10 FIGURE 206. AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4F RT T00011AT 2008050700231 20080507 00231 SO 2008 5 7 SIMA200812110 1 20080428 A 2131 92185A010200 CONTROLLER EMB 145 EMB145LR 3260212 SO CABIN PRESSURE MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 638AE 6459 145172 ON FLIGHT 4306, CREW REPORTED WHILE CLIMBING THRU 19000 THEY RECEIVED CABIN ALT WARNING AND AURAL WARN. CREW REQUESTED EMERGENCY DESCENT TO 10000 AND RETURNED TO CVG. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED DIGITAL PRESSURIZA TION CONTROLLER IAW AMM 21-31-01. OPERATIONAL CHECKED GOOD. NO FURTHER FAULTS FOUND AT THIS TIME. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4T RT T00011AT 2008050700234 20080507 00234 NM 2008 5 7 AALA200800840 1 20080407 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 DFW - EMERGENCY LIGHT AT SEAT 34C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 34C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050700235 20080507 00235 NM 2008 5 7 AALA200800841 1 20080407 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 DFW - EMERGENCY LIGHT AT SEAT 35C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 35C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050700239 20080507 00239 SO 2008 5 7 RAIA00804032 1 20080429 A 2730 ELEVATOR EMB 145 EMB145LR 3260212 SO STIFF A RAIA B A EMER. DESCENT UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CE 03 834HK 145269 FLT 7972 - EWR - DURING CRUISE, PITCH BECAME STIFF WHEN PULLING ON YOKE. A FEW DEGREES OF TRAVEL IT WOULD SEEM FINE, AF TER THAT IT WAS STIFF. MAINTENANCE PERFORMED A DETAILED VISUAL INSPECTION OF THE ELEVATOR CONTROL SYSTEM, ELEVATOR SURF ACES, TRIM TABS, AND SPRING TABS. NO DEFECTS NOTED. ELEVATOR SURFACE MOVED FREELY DURING GROUND OPERATION CHECK. NO D EFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008050700240 20080507 00240 SO 2008 5 7 RAIA00804034 1 20080430 A 2750 FLAP EMB 145 EMB145LR 3260212 SO WING MALFUNCTIONED A RAIA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 825HK 145510 FLT 5530 - STL - CREW REPORTED RECEIVING A SPS ADVANCED AND FLAP FAIL MESSAGE ON THE EICAS DURING CLIMBOUT. FLAP INDICA TION SHOWED AMBER DASHES. MAINTENANCE RESET THE FLAP SYSTEM AND PERFORMED AN OPERATIONAL CHECK OF THE SYSTEM WITH NO DE FECTS NOTED. 2 L 7 2 4T RT T00011AT 2008050700242 20080507 00242 SO 2008 5 7 RAIA00804035 1 20080430 A 7830 THRUST REVERSER EMB 145 EMB145 3260210 SO NR 1 MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 802HK 145066 FLT 3505 - RIC - NR 1 ENGINE THRUST REVERSER DISAGREE EICAS MESSAGE DURING CLIMB. MAINTENANCE DEFERRED THE NR 1 THRUST REVERSER SYSTEM IAW MEL PROCEDURES. 2 L 7 2 4F RT T00011AT 2008050700245 20080507 00245 NM 2008 5 7 BB08073 1 20080428 A 2697 WIRE BOEING 757 7572S7 1384962 NM FIRE LOOP CHAFED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 904AW 23566 PHX - FLT 45 EN-ROUTE PHX TO KOA. THE FLIGHT RECEIVED AN EICAS STATUS MESSAGE "R ENGINE FIRE LOOP 2" DURING CRUISE. T HE FLIGHT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED CHAFED WIRES BETWEEN CONNECTORS D10 08P AND D1408. SYSTEM CHECKS OK. 2 L 7 2 4F RT A2NM 2008050700248 20080507 00248 EA 2008 5 7 A6WA200840317 1 20080410 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 REPAIR CRACK IN PAX DOOR AT AFT EDGE MEMBER. (M) 2 L 7 2 4F RT A21EA 2008050700252 20080507 00252 NE 2008 5 7 BB08076 2 20080429 A 7200 ENGINE BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE LEFT UNKNOWN A USAA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 19 918UW 22196 30896 AUA - FLT 854 AUA TO PHL. SHORTLY AFTER TAKEOFF, THE LEFT ENGINE OIL PRESSURE DROPPED TO 10 PSI AND HAD A RESPECTIVE D ROP IN OIL QUANTITY. THE CREW SHUT DOWN THE LEFT ENGINE AND RETURNED TO FIELD AUA. FLIGHT LANDED WITHOUT FURTHER INCID ENT. MAINTENANCE ACTION PENDING. 2 L 7 2 4F 4 F RT A2NM E12EU 2008050700253 20080507 00253 NM 2008 5 7 DHL2008760539 1 20080420 A 5311 FRAME BOEING 727 7272B7 138407L NM BS 1070 S25-26L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND INSTALLED FRAME SHEAR TIE REPAIR AT BS 1070 BETWEEN STR 25L AND STR 26L PER B727 SRM 53-10-2 FI G 5 AND 53-10-4 FIG 14. 2 L 7 3 4F A3WE 2008043000187 20080430 00187 NM 2008 4 30 CALA0800388 1 20080428 A 5320 6548607272 SUPPORT BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 LOWER FUSELAGE RIGHT RAM AIR OPENING WING TO BODY FAIRING SUPPORT CHANNEL IS CRACKED AT 5TH BOLT HOLE AT OUTBOARD SIDE. REMOVED AND REPLACED WING TO BODY FAIRING SUPPORT REFERENCE SRM 51-10-02 AND SRM 51-40-00. 2 L 7 2 4F RT A16WE 2008043000192 20080430 00192 NM 2008 4 30 CALA0800393 1 20080426 A 7830 491B1330011 BULKHEAD BOEING 767 767224 1385170 NM THRUST REVERSER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 73152 30431 NUMBER 1 ENGINE RIGHT C-DUCT FWD BULKHEAD UPPER WEB AT 1 O'CLOCK POSITION FOUND CRACKED. NUMBER 1 ENGINE RIGHT C-DUCT F WD BULKHEAD UPPER WEB AT 1 O'CLOCK POSITION REPAIRED PER MRAS CMM78-32-02 REPAIR 24. 2 L 7 2 4F RT A1NM 2008043000197 20080430 00197 NM 2008 4 30 SWAA082325 1 20080428 A 2121 64505 FAN BOEING 737 7377H4 1384404 NM E&E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 29 262WN 32519 ON DESCENT STRONG ELECTRICAL SMELL REPORTED IN CABIN. RECIRC FAN TURNED OFF, SMELL DISSIPATED. REMOVED AND REPLACED RE CIRC FAN PER MM. 2 L 7 2 4F RT A16WE 2008043000198 20080430 00198 NM 2008 4 30 SWAA082301 1 20080428 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 443, STR 26L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008043000204 20080430 00204 NM 2008 4 30 SWAA082320 1 20080428 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008043000206 20080430 00206 NM 2008 4 30 SWAA082309 1 20080428 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008043000210 20080430 00210 NM 2008 4 30 SWAA082312 1 20080428 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, BL 0 AND LBL 10. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008050100010 20080501 00010 EU 2008 5 1 08FDEA01627 1 20080424 A 5751 A5766100117300 SKIN AIRBUS 300 A300F4605R 3930327 EU AILERON DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 RT WING INBD AILERON HAS NUMEROUS HAIL DENTS ON UPPER SKIN. DENT FOUND TO BE OUT OF LIMITS IAW SRM 57-61-11, MAT ID 202 4-T3 PO NR 605306.1 IAW SRM 57-61-11 AND 51-21-00, PAGE 23-24 TABLE 3 SHEET 3, FABBED DOUBLER AND FILLER IAW SRM 57-61-1 1, FIG 206. ALODINED IAW SRM 51-21-10. PRIMED AND PAINTED IAW SRM 51-23-10. INSTALLED IAW SRM 57-61-11. 2 L 7 2 4F RT A35EU 2008050100017 20080501 00017 2008 5 1 MASA200800335 2 20080423 A 7261 4119T04P01 OIL FILTER CNDAIR CL600 CL6002B19 1900309 EA NR 2 ENGINE UNKNOWN A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 77278 7278 ASH FLT 1028 HNL-KOA - NR 2 ENGINE HAD HIGH OIL TEMP AT 190 DEGREES CELSIUS AND LOW OIL PRESSURE AT 25 PSI. CREW SHUT D OWN THE NR 2 ENGINE AND DECLARED AN EMERGENCY. DRAINED AGB AND REPLACED FILTER. 2 L 7 2 4F RT A21EA 2008050100023 20080501 00023 EU 2008 5 1 08FDEA01539 1 20080425 A 5415 A54610042 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND ON PYLON NR 2 CORROSION ON PYLON TO WING SHACKLES 6/7/8 OUT OF SRM 54-51-71 LIMIT. REPAIR PERFORMED BY SMOOTH BLE ND OUT THE CORROSION, NDT FOR CRACK FREE IAW RAS/AS/0037/2008 ISS A, APPROVED BY EA 6-5451-117148. 2 L 7 2 4F RT A35EU 2008050100026 20080501 00026 EU 2008 5 1 08FDEA01542 1 20080425 A 5340 A53772997202 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND ON FWD CARGO DOOR HINGE FITTING AT C 23, A BROKEN ANTI-TWIST PLATE. REPAIR PERFORMED BY REMOVE THE BROKEN LOCKING DEVICE AND INSTALLING AN ANGLE BRACKET TO RESTORE THE LOCKING FUNCTION IAW RAS/DABRE/7009080/2008 ISS A, APPROVED BY EA 6-5313-115280. 2 L 7 2 4F RT A35EU 2008050100027 20080501 00027 EU 2008 5 1 08FDEA01543 1 20080425 A 5753 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU TE FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND ON LT INBOARD FLAP DURING ACCOMPLISHMENT OF SB A300-57-6100 SOME HOLES OVERSIZED. REPAIR PERFORMED BY VERIFICATIO N OF OVERSIZED HOLES IAW RAS/FOK/040/2008 ISS A, APPROVED BY EA 6-5752-115278. 2 L 7 2 4F RT A35EU 2008050100028 20080501 00028 EU 2008 5 1 08FDEA01544 1 20080425 A 5320 A53610996201 STIFFENER AIRBUS 300 A300B4622R 3930312 EU ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND ON C12A PREVIOUSLY EMBODIED SB A300-53-6137, IMPROVEMENT OF FITTING ON C12A, IN BAD CONDITION (DAMAGED FASTENER, D ENTS IN STIFFENER A536-10996-201. REPAIR PERFORMED BY REAM UP THE SEVERAL HOLES, INSTALL OVERSIZED FASTENER AND REPLACE STIFFENER IAW RAS/70503839/019/2008 ISS A, APPROVED BY EA 6-5312-115285. 2 L 7 2 4F RT A35EU 2008050100029 20080501 00029 EU 2008 5 1 08FDEA01545 1 20080425 A 5320 A53610318265 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND ON C 12A PREVIOUSLY EMBODIED SB A300-53-6137, IMPROVMENT OF FITTING ON C12A, IN BAD CONDITION (ANGLE A536-10318-26 5. REPAIR PERFORMED IAW SRM 53-12-13 FIG 201 IAW RAS/70503839/019/2008 ISS A, APPROVED BY EA 6-5312-115285. 2 L 7 2 4F RT A35EU 2008050100031 20080501 00031 EU 2008 5 1 08FDEA01547 1 20080425 A 5311 A53980044 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND DEFORMED FLANGE AT C 74, P26-27 LT/RT REPAIR PERFORMED BY REWORK OUTER FLANGE TO ELIMINATE THE DEFORMATION, NDT FO R CRACK FREE IAW RAS/EFW/9000019/2008 ISS A, APPROVED BY EA 6-5318-117150. 2 L 7 2 4F RT A35EU 2008050700258 20080507 00258 EU 2008 5 7 CPCP20080020 1 20080327 A 5310 CREASE BEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 270AT 270 RT FWD CARGO CREASE BEAM LOWER CHORD CORRODED ON BTW FR 13-17. REPLACED RT FWD CARGO CREASE BEAM LOWER CHORD IAW SRM 51 -25-01, 51-25-03 AND 51-24-04. 2 H 7 2 4T RT A53EU 2008050700260 20080507 00260 EU 2008 5 7 08FDEA01740 1 20080503 A 5320 A53980301202 COVER AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CORROSION ON COVER PLATE C 73, P9 LT REPAIR PERFORMED BY REMOVING CORROSION IAW SRM 51-74-10, NDT FOR CRACK FREE, FLAP PEENING AND RENEWING THE RIVETS IAW RAS/EFW/9000027/2008 ISS B, APPROVED BY EA 6-5318-117153. 2 L 7 2 4F RT A35EU 2008050700266 20080507 00266 NM 2008 5 7 ZZDA2008098 1 20080420 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 987AT 55088 LIGHTNING STRIKE LT SIDE FUSELAGE. REPLACED WINDOW BELT SKIN PANELS STA 313 - STA 403 PER B717 SRM 51-41-02. REPLACED CABIN WINDOWS SAME AREA. 2 L 7 2 4F TR A6WE 2008050700270 20080507 00270 NM 2008 5 7 DHL2008760542 1 20080420 A 5313 BAC1498146 STRINGER BOEING 727 7272B7 138407L NM BS 1065-1080 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 CUT OUT, FABRICATED, AND INSTALLED STRINGER REPAIR AT BS 1065 TO BS 1080, ON STR 26L PER B727 SRM 53-10-2 FIG 9 AND 53-1 0-3 FIG 1. 2 L 7 3 4F A3WE 2008050700274 20080507 00274 NM 2008 5 7 DHL2008760523 1 20080416 A 5347 BAC15201466 SEAT TRACK BOEING 727 7272B7 138407L NM BS 850-870 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND REPLACED SEAT TRACK SECTION AT RBL 24, FROM BS 850 TO 870, PER B727 SRM 53-10-2 FIG 7 AND 53-10 -5 FIG 1. 2 L 7 3 4F A3WE 2008050700275 20080507 00275 WP 2008 5 7 DHL2008807506 1 20080425 A 5711 FRAME DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 LT WING CTR L/E FORMER CRACKED 0.500" STA XW 454.000. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRI CATED ANGLE DOUBLERS (AL7075T6 0.040") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER AND AREA IAW S RM 51-1-8B. INSTALLED ANGLE DOUBLES IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2008050700276 20080507 00276 NM 2008 5 7 NOCA03308 1 20080501 A 2781 3A12601 SENSOR BOEING 767 767324 1385203 NM L/E SLAT FAILED A NOCA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 767NA 27569 LEADING EDGE FLAP ASYM EICAS MESSAGE IN FLIGHT RETURN TO AFW, A/C HAD 2 AIR TURNBACKS TO AFW. REMOVED AND REPLACED O/B SLAT RVDT M548, ADJUSTED O/B SLAT RVDT M544 IAW 27-81-11-424-029. FOUND L/E SLAT SENSOR S285 BAD. REMOVED AND REPLACED AND ADJUSTED SENSOR S285 PER MM 27-88-01/27-88-02, OPS CHECK SLATS NORMAL. ITEM CLOSED. 2 L 7 2 4F RT A1NM 2008050700280 20080507 00280 EU 2008 5 7 CPCP20080017 1 20080327 A 5315 FLOORBEAM AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 270AT 270 FLOORBEAM AT FR 36 CORRODED. CORROSION ON FLOORBEAM FR 36 REPAIRED IAW SRM 53-00-00 FIG 435. 2 H 7 2 4T RT A53EU 2008050700282 20080507 00282 NE 2008 5 7 NOCA03208 2 20080430 A 7321 FFG022AC FUEL CONTROL BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE NR 1 ENGINE MALFUNCTIONED A NOCA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 EA 15 752NA 28174 DURING TAXI OUT OIL PRESSURE DROPPED BELOW 10 PSI AND OIL PRESSURE WARNING AND SHUT DOWN NR 1 ENGINE STATUS MESSAGE L EN G LP PUMP. DUE TO SUSPECTED ROLL BACK OR RUN DOWN BELOW SUB IDLE AFTER FURTHER TALKS WITH THE CREW. REPLACED HP FUEL P UMP AND FFG AS PER MM 73-21-01 AND 73-11-01, OPS CHECK AND ENG RUNS ACCOMPLISHED PER MM 71-00-00, ITEM CLOSED. 2 L 7 2 4F 4 F RT A2NM E12EU 2008050700290 20080507 00290 EU 2008 5 7 BA08017 1 20080501 A 7797 420651 WIRE HARNESS AIRBUS 330 A330323 3930335 EU PWA 4168 PW4168 NE NR 1 ENGINE FAULTY A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 277AY 23445 5808 380 733465 PHL - FLT 754 EN-ROUTE PHL TO CDG. THE AIRCRAFT FAILED THE VERIFICATION FLIGHT FOR AN ENGINE 1 EGT INDICATION INOPERAT IVE. THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ENGINE 1 EGT WIRE HARNESS. OPERATIONALLY CHECKS OK. 2 L 7 2 4F 4 F RT A46NM E36NE 2008050700295 20080507 00295 EU 2008 5 7 USAA920080992 1 20080503 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 649AW 803 FLT 320 LAX - LAS - EE - AFT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY. OPERATIONAL CHECK W AS NORMAL. 2 L 7 2 4F RT A28NM 2008050700296 20080507 00296 EU 2008 5 7 USAA920080993 1 20080504 A 2560 P4010021 BATTERY AIRBUS 320 A320231 3930325 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 627AW 66 FLT 570 PHX-MSP - EE - FLASHLIGHT AT 1L INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY. OPERATIONAL CHECK WAS GOOD . 2 L 7 2 4F RT A28NM 2008050500217 20080505 00217 EU 2008 5 5 08FDEA01656 1 20080429 A 5532 A55373311108001 PANEL AIRBUS 300 A300F4605R 3930327 EU VERTICAL STAB ERODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 VERTICAL STAB L/E PANEL 322 CL LEFT SIDE IS ERODED JUST AFT OF THE L/E. REMOVED ERRODED PAINT FOUND NO SIGNS OF DELAMIN ATION IAW SRM 55-32-00. 2 L 7 2 4F RT A35EU 2008050700298 20080507 00298 NM 2008 5 7 USAA920080957 1 20080429 A 5311 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 480, S8L - S9L. REPAIRED FRAME, BS 480, S8L - S9L IAW USAIRWAYS EO 5 311-01019. 2 L 7 2 4F RT A16WE 2008050700303 20080507 00303 EU 2008 5 7 USAA920080984 1 20080428 A 5320 D5347208900400 BEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 188US 1724 PIT - MAJOR REPAIR -S3 CHECK - LEVEL 2 CORROSION ON CABIN BEAM, BS 3736 / FR 64 - BS 3950 / FR 68, +Y1160. REPLACED CAB IN BEAM, BS 3736 / FR 64 - BS 3950 / FR 68, +Y1160 IAW A321 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008050100036 20080501 00036 EU 2008 5 1 08FDEA01552 1 20080425 A 5754 A57863251162 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CHAFING MARKS ON SLAT NR 1 LT, FOLDING NOSE AREA REPAIR PERFORMED BY BLEND OUT DAMAGE TO SMOOTH CONTOUR IAW RAS/FO K/031/2008 ISS A, APPROVED BY EA 6-5742-115274. 2 L 7 2 4F RT A35EU 2008050100038 20080501 00038 EU 2008 5 1 08FDEA01555 1 20080425 A 5710 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 CORROSION AND LIGHTNING STRIKE FOUND ON LT WING TIP (4 AREAS) REPAIR PERFORMED BY CUT OUT DAMAGED AREA 1 AND 4 AND INSTA LLING AN EXTERNAL PATCH WITH SHIM, BLEND OUT AREA 2 AND 3 AND INSTALLING EXTERNAL PATCH UNDER STATIC DISCHARGER , APPR OVED BY RAS/FOK/037/2008 ISS A AND EA 6-6-5730-115275. 2 L 7 2 4F RT A35EU 2008050100040 20080501 00040 EU 2008 5 1 08FDEA01557 1 20080425 A 5330 A53970852200 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CORROSION ON SKIN C57 1-57.2, P21-22 LT REPAIR PERFORMED BY EXTERNAL DOUBLER INSTALLATION IAW RAS/EFW/9000024/2008 ISS B, APPROVED BY EA 6-5316-117143. 2 L 7 2 4F RT A35EU 2008050100043 20080501 00043 EU 2008 5 1 08FDEA01560 1 20080425 A 5330 A5361151322500 SKIN AIRBUS 310 A310203 3930313 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 FOUND 5 HOLES AT FRAME 16A TO HAVE PRE EXISTING TOOLING DAMAGE IN HOLES, FASTENERS MARKED AS A, B, C, D,AND E. COMPLI ED WITH EA NR 6-5310-118477 TITLE: " FUSELAGE, AD 2007-11-12 5653-2037-SKIN AT FRAME 16A, OVERSIZED FASTENERS HOLES ". 2 L 7 2 4F RT A35EU 2008042800282 20080428 00282 NM 2008 4 28 QXEA200800389 1 20080416 A 2120 UNKNOWN DHAV DHC8 DHC8202 2809007 NM CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 355PH 500 SEA - LAVATORY SMOKE DETECTOR WENT OFF FOR THE SECOND TIME. NO SMOKE OR FIRE NOTED. ON THE FLIGHT DECK THOUGH NOTICED A ODOR IN THE AIR AND BOTH PILOTS SENSED A SCRATCHING IN THEIR THROATS. MAINTENANCE FOUND ENGINE OIL IN THE NR 1 LP FOR THE ENGINE. AIRCRAFT FERRIED TO PDX FOR REPAIRS. 2 H 7 2 4T RT A13NM 2008042800284 20080428 00284 EA 2008 4 28 SWIA200819527 1 20080101 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA BS 282 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 609SK 10020 RIGHT OUTBOARD FLOOR SILL AT FS 282 HAS AREA OF CORROSION, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER BOMBARDIER REO 6 70-53-21-324 AND CRJ700/900 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008042800291 20080428 00291 NM 2008 4 28 USAA920080874 1 20080412 A 5330 69719477 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 23379 CLT - MAJOR REPAIR - A .5 INCH CRACK ON FUSELAGE SKIN AT BS 219, LBL 29 (PILOTS WINDOW B-POST AREA). INSTALLED DOUBLER REPAIR IAW SRM 53-10-01 REPAIR 10. 2 L 7 2 4F RT A16WE 2008042800314 20080428 00314 GL 2008 4 28 YTRR040408001 2 20080404 A 7230 E23057112 COMPRESSOR WHEEL BELL 206 206B3 1181506 SW ALLSN 250B 250B* GL ENGINE CRACKED B YTRR O OTHER J WARNING INDICATION CL CLIMB 1 SW 03 18HT 1544 2210 ON DEPARTURE PILOT EXPERIENCED A DECELERATION OF THE ENGINE AND LOSS OF POWER. ON INSPECTION FOUND THE NR 2-3 COMPRESSOR WHEEL HAD SHED A BLADE WHICH SUBSEQUENTLY DESTROYED THE REMAINING COMPRESSOR WHEELS. NO FOD DAMAGE NOTED AS NR 1 COMPRE SSOR WHEEL STILL IN TACT AND UNDAMAGED. 1 G 7 1 3U 3 T H2SW E10CE 2008042800331 20080428 00331 EU 2008 4 28 2008F00011 1 20080415 A 3150 UNKNOWN UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE WARNING LIGHT E HCMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 13 11QG 3534 23043 AC DEPARTED AIRPORT ON A SIGHT SEEING FLIGHT AFTER APPROX 20 MINUTES INTO THE FLIGHT THE PILOT OBSERVED A FLICKERING ENG INE CHIP LIGHT, THEN A SOLID ENGINE CHIP LIGHT. THE PILOT PERFORMED A PRECAUTIONARY LANDING. AN ADDITIONAL AC WAS DISPAT CHED (WITH MAINT) TO PICK UP THE PASSENGERS AND CREW. MAINT INSPECTED ALL ENGINE CHIP PLUGS AND THE ENGINE OIL FILTER. A VERY SMALL METAL SLIVER (HAIR SIZE) WAS FOUND ON THE FULL FLOW CHIP DETECTOR, NO OTHER DEFECTS FOUND. PERFORMED MAINT A CTIONS IAW TEC. MM 71-02-07 LEVEL A. PERFORMED OPERATIONAL CHECK FLIGHT, AND RE-INSPECTED DETECTORS AGAIN, NO PARTICLES FOUND. NOTE: RECENT OIL ANALYSIS RESULTS WERE ALL NORMAL, NO FURTHER DEFECTS FOUND. REF: TEC MM 71-02-07. NOTE; 100 HR 1 G 7 2 3U 3 U H9EU E00054EN 2008042800355 20080428 00355 NE 2008 4 28 BB08070 2 20080420 A 7314 WARNING SYSTEM BOEING 757 7572G7 1384963 NM RROYCE RB211 RB211535E4 54555 NE COCKPIT ACTIVATED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 910AW 24523 30560 HNL FLT 47 - EN ROUTE LIH TO PHX. AIRCRAFT DISPLAYED EICAS MESSAGE "L ENG LP PUMP". THE CREW DECIDED TO DIVERT BACK T O HNL. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. (OPEN) 2 L 7 2 4F 4 F RT A2NM E12EU 2008042800366 20080428 00366 WP 2008 4 28 UPS08852063 1 20080410 A 5347 3657502U509 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 FLIGHT COMPARTMENT, FIRST OFFICERS LWR APT SEAT TRACK HAS ELONGATED HOLES. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-1-20D, 51-1-8, 53-0-1. 2 L 7 4 4F RT 4A25 2008042800382 20080428 00382 NE 2008 4 28 DXTA200803003 2 20080418 A 7320 FLOW DIVIDER CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT ENGINE OUT OF ADJUST E DXTA O OTHER Y ENGINE STOPPAGE TX TAXI/GRND HDL 1 GL 07 302QS 5600402 DURING SPEED BRAKE TEST, LT ENGINE SHUTDOWN AND RT ENGINE SHUTDOWN. ADJUSTED TENSION ON BALL PLUNGER ON THE FUEL FLOW D IVIDER, PERFORMED OPS CHECK WITH NO DEFECTS NOTED REF ENGINE MM 71-01-03 2 L 7 2 4F 4 F RT A22CE E25EA 2008043000006 20080430 00006 NM 2008 4 30 KCSA081224 1 20080424 A 5320 TORQUE BOX BOEING 747 747123 1384873 NM FUSELAGE PUNCTURED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 FORWARD BILGE TORQUE BOX WEB HAS A PUNCTURED HOLE AT STA 660 TO 680, RBL 70. 2 L 7 4 4F RT A20WE 2008043000022 20080430 00022 EA 2008 4 30 TRAX200800518 1 20080409 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 AAR - PAX DOOR STEP 832FT CRACKED OR DISBONDED ON FWD END. REMOVED AND REPLACED DAMAGED PAX DOOR STEP 832 FT (P/N 601R3 1980-59), WITH SERVICEABLE STEP (P/N 601R31980-59) AS PER CRJ 200 AMM 52-11-04. PERFORMED OPERATIONAL TEST OF PAX DOOR STEPS AS PER CRJ 200 AMM 52-11-04 (NO DEFECTS NOTED). SW 14394 04/20/08. SUPPLEMENTAL SDR CLOSED 4/24/08. 2 L 7 2 4F RT A21EA 2008043000033 20080430 00033 NM 2008 4 30 ASAA0872848 1 20080406 A 5320 146A75022 CHANNEL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 609AS 29752 BS 727B 787 RBL 21 ZEE CHANNEL CORRODED RE-PLUGGED ZEE CHANNEL WITH REPAIR PART IAW B737 700 SRM 51 40 05 51 40 08 AND 5 1 40 02. 2 L 7 2 4F RT A16WE 2008050700312 20080507 00312 NM 2008 5 7 USAA920080994 1 20080502 A 2560 P2070001214 FLASHLIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 158AW 23780 PHX - EMERGENCY EQUIPMENT - FLT 640 - FORWARD FLIGHT ATTENDANTS NR 2 FLASHLIGHT IS INOPERATIVE. REPLACED AND OPERATIONA L CHECKED THE FORWARD FLIGHT ATTENDANTS NR 2 FLASHLIGHT. 2 L 7 2 4F RT A16WE 2008050700314 20080507 00314 SO 2008 5 7 C2XA08CL055 1 20080505 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14959 145091 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT ON THE PASSENGER DOOR WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACE D THE LAMP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008050700326 20080507 00326 NM 2008 5 7 UIEA200800163 1 20080501 A 3610 8988061 REGULATOR VALVE BOEING 747 7472D7B 1384803 NM LEAKING A UIEA O OTHER J WARNING INDICATION TO TAKEOFF 1 EA 15 528MC 22472 NR 1 ENGINE FULL POWER TAKEOFF ON CLIMB-OUT BOTH A/B LOOPS REACHED 3.0. AFTER POWER REDUCTION BOTH LOOPS CAME BACK DOWN TO 2.0. REST OF FLIGHT WAS OK. OPENED COWL AND FOUND LEAKING PRV. REPLACED THE PRV IAW AMM 36-11-13. OPS AND LEAK C HECKED OK. 2 L 7 4 4F RT A20WE 2008050700329 20080507 00329 NM 2008 5 7 2008UALA02440 1 20080425 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 847-867 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 AFT CARGO BAY BETWEEN BS 847 AND 867 AN INTERCOSTAL WAS BLENDED BEYOND LIMITS AT S26R. MAJOR REPAIR ACCOMPLISHED, REPLA CED THE INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050700331 20080507 00331 NM 2008 5 7 2008UALA02442 1 20080425 A 5412 BULKHEAD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 NACELLE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 NR 1 PYLON AFT BULKHEAD OTBD SIDE LWR FLANGE HAS EXISTING GOUGES. BLENDED OUT DAMAGE. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008050700333 20080507 00333 NM 2008 5 7 2008UALA02444 1 20080425 A 3150 4911710 COMPUTER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SLAT/FLAP FAULTED A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 824UA 965 ALTERNATE LAW (PROT LOST) DISPLAYED ON UPPER ECAM SCREEN. ECAM SHOWS MOMENTARILY AS FLAPS AND SLATS MOVE OUT TO POSITIO N. FOUND SLAT/FLAP COMPUTER 22CV FAULTING. REPLACED SLAT AND FLAP CONTROL COMPUTER 22CV 2 L 7 2 4F 4 F RT A28NM E40NE 2008050700342 20080507 00342 NM 2008 5 7 GTIA0800063 1 20080408 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 504NK 2473 FLOORBEAM CORRODED FRAME 67-68 Y1732. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2008050700354 20080507 00354 NM 2008 5 7 SWAA082392 1 20080503 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008050700365 20080507 00365 NM 2008 5 7 SWAA082431 1 20080504 A 5310 6545834 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED DAL CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 291 TO BS 332, STR 17R. REMOVED AND REPLACED WEB PER S RM. 2 L 7 2 4F RT A16WE 2008050700373 20080507 00373 NM 2008 5 7 SWAA082380 1 20080501 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008050700379 20080507 00379 NM 2008 5 7 SWAA082398 1 20080503 A 3232 65448105 UPLOCK ACTUATOR BOEING 737 7373H4 1384600 NM RT MLG FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 380SW 26587 AIR TURNBACK. RIGHT MLG WARNING LIGHT ILLUMINATED WITH HANDLE IN OFF POSITION. RIGHT MLG FELL OUT OF EXTENDED POSITION . REMOVED AND REPLACED UPLOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2008050700380 20080507 00380 NM 2008 5 7 SWAA082399 1 20080503 A 5753 6546435 FLAP BOEING 737 7377H4 1384404 NM RT WING WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 419WN 29824 DURING SCHEDULED 6Y CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP WORN AT OUTBOARD END. REMOVED AND REPLACED FLAP PER M M. 2 L 7 2 4F RT A16WE 2008050700382 20080507 00382 NM 2008 5 7 SWAA082402 1 20080502 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 464WN 32468 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008050700383 20080507 00383 NM 2008 5 7 SWAA082401 1 20080502 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 464WN 32468 DURING SCHEDULED HC2 CHECK, FOUND EEPLS END CAP LOOSE AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 2008050700384 20080507 00384 NM 2008 5 7 SWAA082403 1 20080502 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 474WN 33861 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 16 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008050700385 20080507 00385 NM 2008 5 7 SWAA082381 1 20080501 A 3350 100031 SIGN BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 LEFT OVERWING EMERGENCY EXIT LIGHT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2008050700386 20080507 00386 NM 2008 5 7 SWAA082382 1 20080501 A 2730 6545187 TORQUE TUBE BOEING 737 7375H4 138449D NM LT ELEVATOR FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, LEFT ELEVATOR FAILS FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR OUTPUT TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2008050700390 20080507 00390 NM 2008 5 7 SWAA082420 1 20080504 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008050700391 20080507 00391 NM 2008 5 7 SWAA082421 1 20080504 A 5313 6551698 STRINGER SPLICE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2008050700392 20080507 00392 NM 2008 5 7 SWAA082422 1 20080504 A 5754 65C26601 SLAT BOEING 737 7375H4 138449D NM LT WING WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND LEFT WING NR 3 L/E SLAT WORN AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 2008050700395 20080507 00395 NM 2008 5 7 SWAA082423 1 20080504 A 3350 1619 LIGHT BOEING 737 7373T5 1384608 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED OTS CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008050700398 20080507 00398 NM 2008 5 7 SWAA082404 1 20080504 A 5330 6545774 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008050800003 20080508 00003 EA 2008 5 8 A6WA200840294 1 20080407 A 5320 SCUFF PLATE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 CORROSION UNDER SERVICE DOOR SCUFF PLATE. (K) CORROSION REMOVED IAW SRM 51-21-06. 2 L 7 2 4F 4 F RT A21EA E15NE 2008050800017 20080508 00017 EA 2008 5 8 JIK2008F00000 2 20080115 A 8520 DOWEL PIN PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540* 41533 EA RT ENGINE SHEARED E JIKA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 01 42079 40 317405488 ON TAKEOFF ROLL, THE RT ENGINE QUIT. AFTER TROUBLESHOOTING, AND CHANGING MAGS, THE ENGINE STILL ONLY RAN ROUGH, AT BEST . THE ENGINE WAS REPLACED AND SENT BACK TO OVERHAUL FACILITY. AT TEAR DOWN IT WAS FOUND THAT THE DOWEL THAT ALIGNS THE CRANKSHAFT GEAR TO THE SHAFT HAD SHEARED, ALLOWING THE GEAR TO SLIP. (K) 1 L 7 2 3O 3 O A20SO E14EA 2008050800018 20080508 00018 NE 2008 5 8 DXTA200802954 2 20080320 A 7200 ENGINE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE LEFT POWER LOSS E DXTA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 07 693QS 5605657 LT ENGINE WILL NOT MAKE TAKEOFF POWER IN THE TAKEOFF DETENT AND WITH EECS IN AUTO AND FAILED TO MANUAL. RAN ENGINES AT 88.4 PERCENT N1 WITH SEVERAL ACCELERATIONS AND DECELERATIONS WITH NO FAULTS FOUND IAW FAULT ISOLATION SECTION OF MM 72-0 0-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008050800020 20080508 00020 CE 2008 5 8 DXTA200802969 1 20080329 A 3222 STRUT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG DEFECTIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 946QS 7500195 DURING CLIMB THRU APPROX FL390 AT M.80 GOT RED GEAR UNSAFE LIGHT ACCOMPANIED BY A LOUD THUMP. FOUND UPLOCK ENGAGEMENT B ELOW MINIMUM, AND SWITCH ENGAGEMENT BELOW MINIMUM AND NOSE GEAR STRUT OUT OF TOLERANCE, DISASSEMBLED NOSE GEAR STRUT, RE PACKED STRUT WITH NEW SEALS REASSEMBLED, SERVICED NOSE STRUT. ACCOMPLISHED GEAR BUMP CHECKS IAW MM CHAP 12-10-38 AND 32- 30-00. OPERATIONAL CHECKS GOOD 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008050800031 20080508 00031 SO 2008 5 8 SWIA200819559 1 20080427 A 3350 SIGN EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 270YV 120270 FLT 5455 - EMERGENCY EXIT SIGN AT ROW 6 IS BROKEN. REPLACED EMERGENCY EXIT SIGN. 2 L 7 2 4T RT A31SO 2008050800032 20080508 00032 SO 2008 5 8 SWIA200819560 1 20080425 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 299SW 13498 9348 120329 FLT 5464 - EMERGENCY EXIT SIGNS WILL NOT ILLUMINATE WHILE TESTING. REPLACED ELBP ABOVE ROW 6. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008050800034 20080508 00034 EU 2008 5 8 BAQA20080005 1 20080419 A 2150 S8990132 O-RING ALIDSG BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE A/C BAY DAMAGED E BAQA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 03 118NC 7067 CRUISE FLIGHT, CLOSE TO FLIGHT DESTINATION, CREW SMELT "STRANGE ODOR" IN CABIN/COCKPIT. PILOT TURNED OFF THE ENVIRONMEN TAL CONTROL UNIT (ECU) AND SMELL CEASED. INSPECTION OF ECU REVEALED THAT THE "INDUCTOR" PIPE TEMPERATURE CONTROLLER TO COOLING TURBINE HAD A SMALL SPLIT AT THE TURBINE AND PIECES OF THE SEALING O-RING (PACKING) WAS EXPOSED AND MISSING. 1 G 7 2 3U 3 U H13EU E5NE 2008050800041 20080508 00041 SO 2008 5 8 SWIA200819562 1 20080424 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 229SW 120305 LEFT WING STRINGER 8 IS CRACKED INBOARD OF RIB 5. REPAIRED STRINGER ON LEFT WING PER EMB 120 SRM 57-20-03 FIG 202. 2 L 7 2 4T RT A31SO 2008043000069 20080430 00069 NM 2008 4 30 SWAA082205 1 20080424 A 5330 654767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 387 AND BS 454, RBL 1 AND LBL 3. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008043000118 20080430 00118 NM 2008 4 30 CALA0800381 1 20080427 A 5315 141T5147 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 73152 30431 M/D - BS 246 FLOORBEAM MID CHORD AT LBL 40 FOUND RADIUS AREA CRACKED APPROX 1 INCH LONG. M/D BS 246 FLOORBEAM MID CHORD AT LBL 40" REPAIRED PER ECRA 5310-04725 AND HFEC NO CRACK FOUND. 2 L 7 2 4F RT A1NM 2008043000142 20080430 00142 NM 2008 4 30 SWAA082249 1 20080427 A 5315 65C33940 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM TEE CAP CRACKED AT BS 294.5, STR 17R. REMOVED AND REPLACED TEE CAP PER SRM. 2 L 7 2 4F RT A16WE 2008043000162 20080430 00162 NM 2008 4 30 SWAA082283 1 20080427 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000178 20080430 00178 NM 2008 4 30 SWAA082270 1 20080425 A 5755 6550818 HINGE FITTING BOEING 737 7373T5 1384608 NM NR 6 SPOILER CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED SPV CHECK, FOUND RIGHT WING NR 6 SPOILER INBOARD HINGE FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2008043000190 20080430 00190 NM 2008 4 30 CALA0800391 1 20080428 A 5311 143A1111 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24706 28767 CABIN STATION 400 BETWEEN S8L AND S9L HAS PASSENGER SERVICE UNIT RAIL ATTACH BRACKET TO FRAME CRACKED. REPAIRED FRAME R EF EA 5310-04498. 2 L 7 2 4F RT A16WE 2008043000200 20080430 00200 NM 2008 4 30 SWAA082302 1 20080428 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505C, STR 17R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000202 20080430 00202 NM 2008 4 30 SWAA082317 1 20080428 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008050100006 20080501 00006 NM 2008 5 1 UPS08M52071 1 20080214 A 5310 STRUCTURE DOUG MD11 MD11 3023602 NM CARGO BILGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP INSPECTION TYPE:C CENTER CARGO BILGE RT L48 STA 1715-1695 FOUND MAJOR CORROSION ON LONGERON AS MARKED, LONGERON MAJOR CO RROSION REMOVED. FOUND EXCEEDED LIMIT PER SRM 53-10-00 FIG 2A V.1R.40. MAT`L REMOVED:0.075 INCH ORIG THK:0.105 INCH. NEW LONG REWORK C/OUT FR MAT`L ID0558TX7150T6511 PER DWG AFA7776.FPI C/OUT IAW DAC NDTSPM R.13 PAR T08 FOUND NO CRACK EV IDENT. NEW LONGERON AND SPLICES 2 HOLES P/UP PER SRM 51-31-01V.2R.40 AND REPROTECTED PER SRM 51-21-01 V2R.40. 2 L 7 3 4F RT A22WE 2008050100045 20080501 00045 EU 2008 5 1 08FDEA01562 1 20080425 A 5753 A5796000001551 RUB STRIP AIRBUS 300 A300F4605R 3930327 EU RT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 RIGHT WING INBD FLAP UPPER SKIN RUB STRIP IS WORN. REMOVED & REPLACED THE CHAFE / RUB STRIP IAW SRM 57-50-00. 2 L 7 2 4F RT A35EU 2008050100046 20080501 00046 EU 2008 5 1 08FDEA01563 1 20080425 A 5320 A53813303201 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND DURING ACCOMPLISHMENT OF WIC 6-5310-7-5001 PART 2 SEVERAL FASTENER WITH LARGER DIAMETER AS REQUIRED IAW SB A300-53 -6063. REPAIR PERFORMED BY REAM UP THE HOLES AND PERFORM REPAIR INSTRUCTION IAW SB A300-53-6048 AND -6063, APPROVED BY RAS 70504678/020/2008 ISS A AND EA 6-5310-117151. 2 L 7 2 4F RT A35EU 2008050100048 20080501 00048 EU 2008 5 1 08FDEA01565 1 20080425 A 5730 A5724660600300 PANEL AIRBUS 300 A300F4605R 3930327 EU RT WING WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 RIGHT WING LEADING EDGE PANEL NR 612 GB HAS LANDING AREA SKIN LAMINATE WORN/TORN. REPAIRED DAMAGED AREA IAW SRM 57-41-1 2; FIG 208. REMOVED & RE-ATTACHED THE PANEL RESTRAINT CORDS REF AMM 57-41-41-4; PG 1.PREPARED THE BONDING SURFACE FOR THE FOIL APPLICATION IAW SRM 57-41-12; FIG 208. ALODINED SURFACE REF SRM 51-21-10. PRIMED THE SURFACE REF SRM 5 1-23-10. 2 L 7 2 4F RT A35EU 2008050100050 20080501 00050 EU 2008 5 1 08FDEA01568 1 20080425 A 5320 A25276495056009 PANEL AIRBUS 300 A300F4605R 3930327 EU LAVATORY DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 CABIN LAVATORY COVER PANEL IS DAMAGED. REMOVED DAMAGE. PREPPED SURFACE FOR REPAIR; POTTED; LAYED UP WET LAY-UP REPA IR & REFINISHED SURFACE IAW SRM 51-77-12. 2 L 7 2 4F RT A35EU 2008050100052 20080501 00052 EU 2008 5 1 08FDEA01570 1 20080425 A 5344 A2528286204600 COVER AIRBUS 300 A300F4605R 3930327 EU R1 DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 R-1 DOOR INTERIOR HINGE MECHANISM COVER IS DAMAGED. REMOVED DAMAGE; CLEANED & PREPPED FOR WET LAY UP. LAYED UP REPAIR PLIES & STARTED CURE, COMPLETED CURE & LIGHTLY SANDED, CLEANED & PREPPED FOR FINISH COAT; APPLIED FINISH COAT IAW SRM 51-77-10 & 51-77-11. 2 L 7 2 4F RT A35EU 2008050100054 20080501 00054 EU 2008 5 1 08FDEA01572 1 20080425 A 5200 A5247122600000 ACCESS DOOR AIRBUS 300 A300F4605R 3930327 EU FUSELAGE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 ACCESS DOOR 313 AL AFT OUTBD CORNER IS DELAMINATED. REPAIRED ACCESS DOOR 313 AL BY REMOVING THE DAMAGED SKIN PLIES & TH E PREVIOUS REPAIR. APPLIED A WET LAYED UP FIBERGLASS REPAIR TO THE INNER & OUTER SURFACES & REFINISHED IAW SRM 51-77-12 . 2 L 7 2 4F RT A35EU 2008050100055 20080501 00055 EU 2008 5 1 08FDEA01573 1 20080425 A 5320 A5398675120500 INTERCOSTAL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 EMPENNAGE FR 86 STRINGER 34 LT INTERCOSTAL BENT. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2008050100056 20080501 00056 EU 2008 5 1 08FDEA01574 1 20080425 A 5730 A5724660200000 PANEL AIRBUS 300 A300F4605R 3930327 EU WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 PANEL 612 CB LEADING EDGE IS CRACKED AND ERODED. REPAIRED CRACK & ERROSION ON PANEL 612 CB L/E WITH WET LAY UP IAW SRM 5 7-41-12. 2 L 7 2 4F RT A35EU 2008050100057 20080501 00057 EU 2008 5 1 08FDEA01575 1 20080425 A 5320 A5398675120400 INTERCOSTAL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 EMPENAGE FR 86 STRINGER 34 RT INTERCOSTAL BENT. REMOVED & REPLACED INTERCOSTAL IAW SRM 51-72-10 & 51-40-21. 2 L 7 2 4F RT A35EU 2008050100063 20080501 00063 EU 2008 5 1 08FDEA01581 1 20080425 A 5510 A5517705800152 PANEL AIRBUS 300 A300F4605R 3930327 EU HORIZONTAL STAB DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 PANEL 344 EP DELAMINATED. REPAIRED PANEL 344 EP BY REMOVING THE DAMAGE; CLEANING; CLEANING THE AREA, POTTING REPAIR AN D APPLYING A FIBERGLASS WET LAY UP REPAIR IAW SRM 51-77-12 PARA 2-A (2) FIG 202 AND SRM 51-77-10 PARA 3. RESTORED SUR FACE REPAIR IAW SRM 51-77-12; PARA 2-A (2), L & SRM 51-75-10. 2 L 7 2 4F RT A35EU 2008050100066 20080501 00066 EU 2008 5 1 08FDEA01584 1 20080425 A 5321 A53210045004000 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 PANEL 121SF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL 121 SF; POTTED EDGES; COMPLETED CURE & SANDED EDGE POTTING; INSTALLED INSERTS; APPLIED NON-SKID & PART MARKED. REMOVED HAREWARE FROM THE OLD PANEL & REINSTALLED ON THE NEW PANEL I AW DWG SRZ 25-005; REN F & SRM 51-40-00. 2 L 7 2 4F RT A35EU 2008050100068 20080501 00068 NM 2008 5 1 08FDEA01586 1 20080425 A 5311 6517663 FRAME BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 FWD PIT, FRAME AT STA 720D HAS CORROSION ON THE FWD FACE AROUND CABLE CUT OUT AT LBL 1. FOUND WITHIN LIMITS IAW SRM 53-1 0-2. 2 L 7 3 4F A3WE 2008050100071 20080501 00071 NM 2008 5 1 08FDEA01589 1 20080425 A 5330 65921444 SKIN BOEING 727 7272S2F 1384O81 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 RT LWR FUSELAGE SURFACE STA 1030 STA 1050, BELOW STR 26R HAS DENT. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2, CUT OUT DAM AGED AREA , FABRICATED REPAIR DOUBLER AND STRUCTURAL FILLER IAW SRM 53-30-3, TREATED AND PRIMED PARTS IAW SRM 51-30-2, I NSTALLED COUNTERSINK WASHERS AND REPAIR PARTS IAW SRM 51-30-8 AND 51-30-2. 2 L 7 3 4F A3WE 2008050100073 20080501 00073 NM 2008 5 1 08FDEA01591 1 20080425 A 5315 146N5006 FLOORBEAM BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 906FD 27148 FLOORBEAM HAS CORROSION BS 1300, RBL 28, BELOW UPPER T-CAP FWD SIDE, AT FLOOR PANEL HOLE. REMOVED CORROSION ON FLOORBEA M IAW SRM 51-00-51. AFTER CORROSION REMOVAL FOUND FLOORBEAM TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3. R EWORK DIMENSIONS ARE AS FOLLOWS: L=1.0", W=2.0", D=.035". FABRICATED REPAIR ANGLES PER MAE TRAVELER NR T8/734293 AND T8/ 734294. FABRICATED REPAIR STRAPS IAW SRM 53-00-51. FABRICATED REPAIR TEE SECTION IAW SRM 53-00-51. LOCATED AND DRILLE D ALL REPAIR PARTS AND TREATED/PRIMED IAW SRM 53-00-51. INSTALLED ALL REPAIR PARTS IAW SRM 53-00-51. THIS REPAIR IS A CATEGORY "A" REPAIR AND MAJOR. NO FOLLOW UP TRACKING IS REQUIRED. 2 L 7 2 4F RT A2NM 2008050100075 20080501 00075 GL 2008 5 1 CHQA200800085 2 20080422 A 7200 AE3007A13 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 1 FAILED A CHQA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 GL 11 378SK 22018 12002 145593 CAE311170 FLIGHT 5328, STL TO MKE, DURING CLIMB THE FLIGHT CREW REPORTED HEARING A LOUD BANG FROM THE LEFT SIDE OF THE AIRCRAFT AN D AN EICAS ENG 1 OUT MESSAGE. THE PROPER QRH CHECKLISTS WERE FOLLOWED AND THE APU WAS STARTED IN FLIGHT. THE CREW ATTE MPTED AN INFLIGHT RESTART USING THE APU BUT THE ENGINE FAILED TO START. THE AIRCRAFT DIVERTED TO BLV AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND REPORTED THAT THE QUILL SHAFT APPEARED TO BE SHEARED. THE N1 WAS REPOR TED TO BE EASY TO ROTATE BY HAND WHILE ATTEMPTING ENGINE START AND N2 WOULD SPOOL UP QUICKLY WITH NO N1 ROTATION. THE N UMBER 1 ENGINE WAS REPLACED. AFTER REPLACING E1 THERE WERE NO FURTHER DEFECTS. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008050100076 20080501 00076 EA 2008 5 1 CHQA200800084 1 20080421 A 2751 855D1009 POSITION SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 639BR 1330 1330 7313 GEE872507 FLIGHT 5612, IAH TO CMH - DURING CLIMB, THE FLIGHT CREW RECEIVED A FLAP FAIL CAUTION MESSAGE WITH THE FLAPS FAILED AT ZE RO DEGREES. THE FLIGHT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE FLAP CONTROL CHANNELS 1 AND 2 AND THE FAULT CLEARED. THE FLAPS WERE OPERATED SEVERAL TIMES WITH NO FURTHER FAULTS PER CRJ AMM 27-50-00. FECU CODES WERE RETRIEVED AND CONTAINED CODES FOR THE LEFT BRAKE POSITION SENSING UNIT. EI003222 HAS BEEN ISSUED TO INSPECT AND T EST THE WIRING TO THE LEFT BRAKE POSITION SENSING UNIT AND REPLACE THE UNIT IF NO FAULTS ARE FOUND IN THE WIRING. 2 L 7 2 4F 4 F RT A21EA E15NE 2008050100077 20080501 00077 GL 2008 5 1 P5CA0801558 2 20080417 A 7200 CF680C2B5F ENGINE BOEING 747 74746NF 13848BT NM GE CF6 CF680C2* GL LEFT FAILED A P5CA O OTHER E VIBRATION/BUFFET AP APPROACH 1 EA 15 451PA 30809 706215 AT 3000' ON FINAL, A LOUD BANG WAS HEARD ON THE LEFT SIDE OF THE AIRCRAFT, FOLLOWED BY 2 MORE TIMES. ENGINE VIBRATIONS EXCEEDED ON NR 2, ALL ENGINE INDICATIONS THEN APPEARED NORMAL. NR 2 ENGINE CHANGE. 2 L 7 4 4F 4 F RT A20WE E23EA 2008050100078 20080501 00078 EU 2008 5 1 MALA080059 1 20080422 A 5210 SKIN SAAB SF340 340B 7860101 EU PAX DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 441XJ 340B441 THE MAIN ENTRANCE DOOR OUTER SKIN WAS FOUND TO HAVE 1 DENT WITH A CREASE, MEASURING 1.5 INCH BY 0.75 INCH BY 0.024 INCH DEEP, LOCATED 5.75 INCH AFT OF DOOR FORWARD EDGE, 32 INCH FROM BOTTOM OF DOOR AND 0.5" ABOVE THE AFT STOP ATTACHMENT SCR EW. DISTANCE BETWEEN EDGE OF DENTS AND AN EXISTING BONDED DOUBLER REPAIR IS 1.75 INCH. HFEC AND DISBOND INSPECTIONS WE RE ACCOMPLISHED. NO CRACKS NOTED, BUT A SMALL AREA OF DISBOND WAS FOUND. REPAIRED IAW EO NR S52117. 2 L 7 2 4T RT A52EU 2008050100083 20080501 00083 GL 2008 5 1 SIMA200811901 2 20080425 A 7200 ENGINE EMB 135 EMB135LR 3260305 SO ALLSN AE300 AE3007A GL CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 713AE 145249 CAE132438 ON FLIGHT 4820, CREW REPORTED OIL SMELL IN COCKPIT IN FLIGHT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMB ER ONE ENGINE IAW AE WORK CARD 71-00-00, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008050200005 20080502 00005 EU 2008 5 2 WRNA200800016 1 20080226 A 5330 SKIN AIRBUS 300 A300B4203 3930306 EU FUSELAGE DAMAGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 501TR 53 DURING M96 CHECK, A 8 INCH BY 2 INCH CUT WAS FOUND IN SKIN BETWEEN FRAME 51 AND 52 AT STRINGER 36R TO 39R AFT OF RMLG DO OR CUT OUT. INSTALLED SKIN REPAIR DOUBLER AT FUSELAGE FRAME 51 TO 52 AND STRINGER 36R TO 39R IAW A300 SRM 53-10-10. 2 L 7 2 4F RT A35EU 2008050200007 20080502 00007 EU 2008 5 2 WRNA200800018 1 20080226 A 5522 SKIN AIRBUS 300 A300B4203 3930306 EU LT ELEVATOR CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 501TR 53 DURING M96 CHECK, WHEN ACCOMPLISHING CPCP TASK CARD 55-2007-0602-1-01 SEVERAL AREAS OF CORROSION WERE FOUND OUT OF LIMIT S ON LT ELEVATOR SKIN FROM CENTER LINE RIVETS TO I/B END CAP. REPLACED ELEVATOR IAW A300 MM 27-31-24. 2 L 7 2 4F RT A35EU 2008050200009 20080502 00009 EU 2008 5 2 WRNA200800019 1 20080228 A 5347 A2577230001471 TRACK AIRBUS 300 A300B4203 3930306 EU CARGO BAY CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 501TR 53 DURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD Z:-150-L403-5-01, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN AFT CARGO COMPARTMENT BETWEEN FRAMES 58 TO 59. REMOVED AND REPLACED ROLLER TRACK IAW SRM 51-30-30. 2 L 7 2 4F RT A35EU 2008050200010 20080502 00010 EU 2008 5 2 WRNA200800020 1 20080228 A 5347 A2577228320001 TRACK AIRBUS 300 A300B4203 3930306 EU CARGO BAY CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 501TR 53 DURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD ZL-150-L403-501, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN A FT CARGO COMPARTMENT AT FRAME 57. REMOVED AND REPLACED ROLLER TRACK IAW SRM 51-30-30. 2 L 7 2 4F RT A35EU 2008050200018 20080502 00018 WP 2008 5 2 UPS08852077 1 20080421 A 5712 RIB DOUG DC8 DC873F 302199F WP LWS 350 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING CENTER LE UPPER RIB CRACKED XFS 350. REPAIRED LT WING CENTER LE UPPER RIB AT XFS 350 IAW SRM 57-02-00 FIG 0 02 AND SRM 57-03-03-0 FIG 005. 2 L 7 4 4F RT 4A25 2008050200019 20080502 00019 WP 2008 5 2 UPS08852078 1 20080421 A 5712 RIB DOUG DC8 DC873F 302199F WP LWS 362 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING CENTER LE UPPER RIB CRACKED XFS 362. REPAIRED LT WING CENTER LE UPPER RIB AT XFS 362 PER SRM 57-02 00-0 FIG 002 AND SRM 57-03-03-0 FIG 005. 2 L 7 4 4F RT 4A25 2008050200022 20080502 00022 NM 2008 5 2 UPS08M52079 1 20080320 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 830-899 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP INSPECTION TYPE:C CABIN - CORROSION ON SEAT TRACK CROWN & CHANNEL AT STA 830-899 X=-75. CORR AT AFFECTED AREA REMVD. MAT'L THK:0.145"(CROWN), MAT'L REMVD:0.05 0" (STA840), MAT'L REMN:0.095". FOUND OUT OF LMT. DISCREPANT SEAT TRAC K (STA 830-929) TRIMMED OUT. HFEC C/O IAW DAC NDT SPM REV13 PART 06-10- 01.001 ON TRIM EDGE & FOUND NO CRACK. NEW SEAT TRACK RE WORKED. NEW S.T RACK & REPAIR PARTS REPRTECTED & INSTL PER SRM53-70-00FIG1VOLIREV35. 2 L 7 3 4F RT A22WE 2008050200027 20080502 00027 SO 2008 5 2 CHQ20080087 1 20080427 A 2760 8005701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL SPOILER DIRTY A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 284SK 145427 CAE312531 FLIGHT 5906 ORD TO CLE - DURING TAKEOFF ROLE, THE FLIGHT CREW RECEIVED A SPOILER TAKEOFF CONFIGURATION MESSAGE ON THE EI CAS. AT THAT POINT THE CREW DECIDED TO ABORT TAKEOFF AND RETURN TO THE GATE WITH NO INCIDENT. MAINTENANCE FOUND NUMERO US PROXIMITY SWITCHES CONTAMINATED WITH FLUID. MAINTENANCE CLEANED ALL INBOARD SPOILER PROXIMITY SWITCHES AND CONDUCTED AN OPERATIONAL CHECK OF THE SYSTEM WITH NO FAULTS FOUND. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008050200028 20080502 00028 EU 2008 5 2 TRBA2008045 1 20080427 A 3350 G44 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 342AT 345 PAX DOOR EMERGENCY STAIR LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP IAW MM NR 33-51-00. 2 H 7 2 4T RT A53EU 2008050200030 20080502 00030 NM 2008 5 2 NWAA081786304 1 20080425 A 3350 BATTERY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 664US 23819 DURING OVERNIGHT CHECK, FOUND UPPER DECK EMERGENCY CEILING LIGHTS BETWEEN UPPER DOORS INOP. MAINTENANCE REMOVED AND REP LACED BATTERY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008050200035 20080502 00035 NM 2008 5 2 HALA0800548 1 20080427 A 2910 MODULE BOEING 767 767332 1382001 NM HYD SYSTEM MALFUNCTIONED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, BOTH C1 AND C2 HYD PUMPS LOST PRESSURE DURING FLAP RETRACTION. AS PART OF O/N INSPECTION NOW NEITHER PUMP PRODUCES MORE THAN 1700 PSI BY ITSELF AND NOT MORE THAN 2700 PSI COMBINED. BEGAN REMOVAL OF ADP FILTER/PRE SSURE MODULE TO CK PRESSURE RELIEF VLV, SYSTEM DEPRESURIZED. REPLACED CTR SYSTEM RETURN FILTER MODULE AND COMPONENTS PE R MM 29-11-16-404-034. OPS CK GOOD, NO LEAKS FOUND. 2 L 7 2 4F RT A1NM 2008050200040 20080502 00040 NM 2008 5 2 RYNA200800006 1 20080112 A 5330 SKIN BOEING 757 7572G5 1384912 NM BS 1702 DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 151GX 24451 LOWER FUSELAGE SKIN HAS A DENT AT BS 1702 BETWEEN STR 18L AND 19L. REPAIRED IAW EO C00-5-53-013-08. 2 L 7 2 4F RT A2NM 2008050200041 20080502 00041 NM 2008 5 2 RYNA200800007 1 20080112 A 5330 SKIN BOEING 757 7572G5 1384912 NM BS 1693 DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 151GX 24451 LOWER FUSELAGE SKIN HAS A DENT AT BS 1693 BETWEEN STR 17L AND 18L. REPAIRED IAW EO C00-5-53-013-08. 2 L 7 2 4F RT A2NM 2008050200043 20080502 00043 NM 2008 5 2 RYNA200800009 1 20080112 A 5330 SKIN BOEING 757 7572G5 1384912 NM BS 1712 DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 151GX 24451 UPPER FUSELAGE SKIN HAS A DENT AT BS 1712 BETWEEN STR 14L AND 15L. REPAIRED IAW EO C00-5-53-012-08. 2 L 7 2 4F RT A2NM 2008050200053 20080502 00053 NM 2008 5 2 WRNA20080026 1 20080227 A 5313 LONGERON BOEING 747 747230B 1384889 NM BS 2700 GOUGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 512MC 21220 DURING B CHECK, A GOUGE WAS FOUND ON RT LONGERON AT STATION 2700 W/L 285. REMOVED DAMAGED AREA AND FABRICATED REPAIR DO UBLER IAW SRM 51-40-03 FIGURE 01 USING .100" 7075 T6 FORMED SECTION. INSTALLED REPAIR DOUBLER IAW SRM 51-30-02. 2 L 7 4 4F RT A20WE 2008050200055 20080502 00055 NM 2008 5 2 WRNA20080034 1 20080324 A 5347 SEAT TRACK BOEING 747 747230B 1384889 NM BS 500-540 CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 508MC 21644 DURING C CHECK, WHILE ACCOMPLISHING CPCP TASK C53-210-01, LEVEL II CORROSION WAS FOUND AT SEAT TRACK BETWEEN STATION 500 - 540 RBL 48. REMOVE CORRODED SEAT TRACK SECTION. INSTALLED SEAT TRACK SECTION IAW SRM 53-10-05 FIG 6 AND SRM 51-30-0 2. 2 L 7 4 4F RT A20WE 2008050200061 20080502 00061 NE 2008 5 2 WRNA20080024 2 20080323 A 7200 ENGINE BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE MALFUNCTIONED A WRNA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 512MC 21220 528419 BECAUSE OF HIGH HEAT AND HUMIDITY AT DUBAI, ENGINES WERE UNABLE TO MAKE TAKEOFF POWER, ABORTED TAKEOFF BEFORE 80 KNOTS A ND RETURNED TO RAMP. PERFORMED MAIN ENGINE CONTROL TRIM ON NR 3 ENGINE IAW 71-00-00 PAGE 563 TEST 5. PERFORMED ENGINE PERFORMANCE RUN, OPS CHECKED GOOD. AIRCRAFT RELEASED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E23EA 2008050200064 20080502 00064 NE 2008 5 2 WRNA20080015 2 20080323 A 7200 ENGINE BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE MALFUNCTIONED A WRNA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 05 512MC 21220 530279 BECAUSE OF HIGH HEAT AND HUMIDITY AT DUBAI, ENGINES WERE UNABLE TO MAKE TAKEOFF POWER, ABORTED TAKEOFF BEFORE 80 KNOTS A ND RETURNED TO RAMP. PERFORMED MAIN ENGINE CONTROL TRIM ON NR 2 ENGINE IAW 71-00-00 PAGE 563 TEST 5. PERFORMED ENGINE PERFORMANCE RUN, OPS CHECKED GOOD. AIRCRAFT RELEASED TO SERVICE. 2 L 7 4 4F 4 F RT A20WE E23EA 2008050200065 20080502 00065 NM 2008 5 2 WRNA20080031 1 20080324 A 5330 SKIN BOEING 747 747230B 1384889 NM BS 515 DENTED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 508MC 21644 DURING C CHECK, WHILE ACCOMPLISHING CPCP TASK C53-100-01 FUSELAGE SKIN WAS FOUND WITH A DENT AND 1/2 INCH LONG CRACK AT STATION 515 JUST BELOW STRINGER 39R. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER, INSTALLED REPAIR IAW SRM 53-30-03 F IGURE 48. 2 L 7 4 4F RT A20WE 2008050200067 20080502 00067 NM 2008 5 2 USAA920080876 1 20080330 A 5754 STRUCTURE AIRBUS A319 A319132 3930340 NM NR 2 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802AW 924 SAL - MAJOR REPAIR - C7 CHECK - CRACKED LEFT WING NR 2 SLAT. REPAIRED LEFT WING NR 2 SLAT IAW A319 SRM 57-43-21. 2 L 7 2 4F RT A28NM 2008043000019 20080430 00019 NM 2008 4 30 ASAA0892839 1 20080327 A 5347 146A750130 SEAT TRACK BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 317AS 30856 CARGO FLOOR TRACK CORRODED ON UPPER AND LOWER SURFACE MOSTLY AROUND NUT PLATE HOLES RBL 13 TO RBL 14 STA 802 TO STA 846. REMOVED DAMAGED CARGO TRACK SECTION STA 767 TO STA 887, LOCATED, FABRICATED A REPLACEMENT TRACK AND SPLICE DRILLED AND INSTALLED IAW B737 900 SRM 53 00 53 REP 4. 2 L 7 4 4F RT A16WE 2008043000034 20080430 00034 NM 2008 4 30 ASAA0872849 1 20080408 A 5720 115A55509 FITTING BOEING 737 737790 13844CN NM LT WING DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 609AS 29752 L N WING RSS 260 FITTING FOUND WITH DRILL HOLD. REPLACED WITH NEW PART. 2 L 7 2 4F RT A16WE 2008043000049 20080430 00049 NM 2008 4 30 CALA0800360 1 20080424 A 5320 182A52014 ATTACH BRACKET BOEING 737 737724 13844BY NM CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24706 28767 PASSENGER SERVICE UNIT (PSU) RAIL ATTACHMENT BRACKET TO FRAME CRACKED AT CABIN STATION 747 BETWEEN S8L AND S9L. CUT OUT DAMAGE AND INSTALLED REPAIR ANGLES IAW ECRA 5310-04498. 2 L 7 2 4F RT A16WE 2008043000052 20080430 00052 NM 2008 4 30 CALA0800363 1 20080425 A 5311 654654997 FRAME BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 FRAME AT BILGE AREA AT STATION 767 LBL 9 IN AFT CARGO COMPARTMENT FOUND CORRODED. CORROSION FOUND TO BE OUT OF LIMITS P ER B 737-500 SRM 53-00-07 AND 53-60-07. REMOVED CORROSION AND ACCOMPLISHED REPAIR PER B 737-500 SRM 53-00-07 REPAIR 8. 2 L 7 2 4F RT A16WE 2008043000068 20080430 00068 NM 2008 4 30 SWAA082204 1 20080424 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 463WN 32467 DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F RT A16WE 2008043000084 20080430 00084 NM 2008 4 30 SWAA082217 1 20080424 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000094 20080430 00094 NM 2008 4 30 SWAA082223 1 20080424 A 5315 6545810 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED HC1 CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 293.5, RBL 5. REMOVED AND REPLACED UPPER CHORD P ER SRM. 2 L 7 2 4F RT A16WE 2008043000115 20080430 00115 NM 2008 4 30 CALA0800378 1 20080408 A 5311 65C33510 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 STATION 440 LT SIDE BETWEEN S8LT AND S9LT AT AC BRACKET I/B FASTENER HOLE IS CRACKED. CUT OUT DAMAGED HOLE AT STATION 4 40 LT BETWEEN S9LT & S8LT, REPAIRED DAMAGED FRAME PER EA5310-04498. 2 L 7 2 4F RT A16WE 2008043000147 20080430 00147 NM 2008 4 30 SWAA082277 1 20080427 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000154 20080430 00154 NM 2008 4 30 SWAA082258 1 20080424 A 3350 100031 SIGN BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND FWD CABIN EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 2008043000157 20080430 00157 NM 2008 4 30 SWAA082259 1 20080427 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BL 0. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008043000161 20080430 00161 NM 2008 4 30 SWAA082289 1 20080427 A 5311 65C25230 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000179 20080430 00179 NM 2008 4 30 SWAA082271 1 20080424 A 3350 20131A BATTERY PACK BOEING 737 737317 138447P NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008043000203 20080430 00203 NM 2008 4 30 SWAA082311 1 20080428 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008050100008 20080501 00008 WP 2008 5 1 NWAA081769762 1 20080425 A 3510 LINE DOUG DC9 DC941 302207N WP 13TH STAGE LEAKING A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 762NW 47395 WHILE IN CRUISE FLIGHT AT FL320, THE CABIN ALTITUDE BEGAN CLIMBING UNCONTROLLABLY. FLIGHT CREW DECLARED AN EMERGENCY WI TH ATC AND BEGAN A RAPID DESCENT TO LOWER ALTITUDES. AT FL280 THE CREW WAS ABLE TO REGAIN CONTROL OF THE CABIN ALTITUDE AND RECEIVED CLEARANCE TO REMAIN AT THE LEVEL FOR THE CRUISE PROFILE OF FLIGHT. THE EMERGENCY WAS CANCELLED AND FLIGHT ARRIVED IN ATL WITHOUT FURTHER INCIDENT. MAINTENANCE DID PERFORM BITE AND BOTH CONTROLLERS WERE NTF. THE NR 1 AIR DAT A SYSTEM CHECKED GOOD WITH NO LEAKS FOUND. BOTH THE LEFT AND RIGHT AUGMENTATION VALVES WERE CHANGED AND A LEAKING 13TH S TAGE PRESSURE LINE WAS SECURED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 2008050200002 20080502 00002 EU 2008 5 2 WRNA200800022 1 20080303 A 5347 SEAT TRACK AIRBUS 300 A300B4203 3930306 EU FUSELAGE CRACKED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 501TR 53 DURING M96 CHECK, MAIN CABIN SEAT TRACK AT FRAME 40 RBL 54 WAS FOUND CRACKED. REPLACED SEAT TRACK AT RBL 54 FROM FRAME 40 TO FRAME 44 +12 INCHES IAW SRM 53-10-10. 2 L 7 2 4F RT A35EU 2008050200004 20080502 00004 EU 2008 5 2 WRNA200800023 1 20080223 A 5552 ATTACH FITTING AIRBUS 300 A300B4203 3930306 EU LT ELEVATOR CORRODED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 501TR 53 DURING M96 CHECK, CORROSION WAS FOUND OUT OF LIMITS ON NR 3 (FROM OUTBOARD END) LEFT ELEVATOR ATTACH HINGE AT BONDING WI RE ATTACH POINT. REPLACED HINGE ATTACH IAW A300 M/M 55-51-31. 2 L 7 2 4F RT A35EU 2008050200020 20080502 00020 WP 2008 5 2 UPS08852086 1 20080415 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1771 L11L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 END FITTING CRACKED IN 60 COMPARTMENT, L11L STA 1771. REMOVE AND REPLACE END FITTING IAW SRM 51-1-21 , 51-1-8, 51-1-20D, 51 -3-2. 2 L 7 4 4F RT 4A25 2008050200045 20080502 00045 NM 2008 5 2 RYNA200800004 1 20080111 A 5330 SKIN BOEING 757 7572G5 1384912 NM BS 276 DENTED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 151GX 24451 LOWER FUSELAGE SKIN HAS A DENT AT BS 276 BETWEEN STR 19R AND 20R. REPAIRED IAW EO C00-5-53-009-08. 2 L 7 2 4F RT A2NM 2008050200057 20080502 00057 NM 2008 5 2 WRNA20080036 1 20080324 A 5311 FRAME BOEING 747 747230B 1384889 NM BS 2664 CHAFED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 508MC 21644 DURING C CHECK, FRAME AT STATION 2664.19 LBL 38, WL 295 WAS FOUND CHAFED. REMOVED DAMAGE AND FABRICATED REPAIR PARTS IA W SRM 51-40-03 FIGURE 1. INSTALLED REPAIR PARTS IAW SRM 51-40-03-FIG 1. 2 L 7 4 4F RT A20WE 2008050500006 20080505 00006 NM 2008 5 5 SWAA082308 1 20080428 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008050500008 20080505 00008 NM 2008 5 5 SWAA082318 1 20080428 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008050500018 20080505 00018 NM 2008 5 5 SWAA082344 1 20080429 A 5311 6546536 BELTFRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND BELTFRAME CRACKED AT BS 616, RBL 65. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008050500020 20080505 00020 NM 2008 5 5 SWAA082342 1 20080429 A 5315 6584176 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 708, RBL 24.82. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2008050500022 20080505 00022 2008 5 5 SWAA082327 4 20080429 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008050500026 20080505 00026 NM 2008 5 5 SWAA082338 1 20080429 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008050500037 20080505 00037 WP 2008 5 5 08FDEA01626 1 20080428 A 5410 AUB710813 DOOR DOUG MD10 MD1010F 3022112 WP ZONE 400 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 1 PYLON PANEL NR 437LL, INNER SURFACE HAS CHAFED THROUGH. NR 1 PYLON PANEL NR 437 LL REQUIRES AN SRM REPAIR. IAW DC/ MD-10 54-51-01; VOL III; PG 3. FABRICATED REPAIR DOUBLER & FILLER IAW SRM 54-00-01; VOL I. ALODINE & PRIMED REPAIR DOUBLER & FILLER IAW SRM 51-21-01; VOL II. INSTALLED REPAIR DOUBLER & FILLER IAW SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 2008050500038 20080505 00038 NM 2008 5 5 SWAA082331 1 20080429 A 3234 6554219 HANDLE BOEING 737 7373H4 1384600 NM COCKPIT DIRTY A SWAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 29 629SW 27704 ON FINAL APPROACH TO DAL AT 600 FEET 3 GREEN AND 3 RED GEAR LIGHTS ILLUMINATED, AT 500 FEET "TOO LOW GEAR" WARNING SOUND ED. INITIATED A GO-AROUND LOWERED GEAR, NORMAL INDICATIONS. INSPECTED FOUND LANDING GEAR SELECTOR HANDLE INNER SHAFT S TICKING, CLEANED AND LUBED PER MM. 2 L 7 2 4F RT A16WE 2008050500040 20080505 00040 EU 2008 5 5 08FDEA01720 1 20080501 A 5310 A5361215121100 FLOOR SUPPORT AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 THE INTERCOSTAL END FITTING IS CRACKED AT FRAME 10 IN THE FWD AVIONICS BAY; RT TUNNEL. REMOVED RT AFT COCKPIT FLOOR PA NEL IAW SRM 51-40-21. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-40-21. HEAT TREAT IAW SRM 51-31-00. FABRICATED ; LOCATE D & DRILLED ANGLE IAW SRM 51-40-44. ALODINED NEW ANGLE IAW SRM 51-21-10. PRIMED ANGLE IAW SRM 51-23-20. PAINTED ANG LE IAW SRM 51-23-10. INSTALLED ANGLE & FLOOR PANEL IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008050500047 20080505 00047 NM 2008 5 5 SWAA082374 1 20080501 A 5315 6545410143 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 670, LBL 24.75. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2008050500049 20080505 00049 NM 2008 5 5 SWAA082372 1 20080501 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7, WL 187. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2008050500051 20080505 00051 NM 2008 5 5 SWAA082352 1 20080501 A 3350 100031 SIGN BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 RIGHT OVERWING EMERGENCY EXIT SIGN FELL OFF. INSTALLED SIGN PER MM. 2 L 7 2 4F RT A16WE 2008050500052 20080505 00052 NM 2008 5 5 SWAA082354 1 20080501 A 2761 6544850 ACTUATOR BOEING 737 7373H4 1384600 NM NR 5 SPOILER CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND RIGHT WING NR 5 SPOILER OUTBOARD ACTUATOR ROD END CORRODED. REMOVED AND REPLACED ACTU ATOR PER MM. 2 L 7 2 4F RT A16WE 2008050500054 20080505 00054 NM 2008 5 5 SWAA082355 1 20080501 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 416WN 32453 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008050500060 20080505 00060 NM 2008 5 5 SWAA082362 1 20080501 A 3350 3071BPEGPL LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008050500061 20080505 00061 NM 2008 5 5 SWAA082361 1 20080501 A 3350 3071BPEGPL LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 23 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008050500066 20080505 00066 NM 2008 5 5 SWAA082371 1 20080501 A 5743 6552235 FITTING BOEING 737 7373T5 1384608 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 667SW 23063 DURING SCHEDULED OTS CHECK, FOUND LT WING AFT STABILIZER BEAM FITTING CORRODED. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2008050500087 20080505 00087 NM 2008 5 5 HNAA0800146 1 20080418 A 3350 82520974101 COVER DHAV DHC8 DHC8102 2809003 NM FLOOR LOOSE A HNAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 07 806EX 263 FLOOR EMERGENCY LIGHTING COVER DETACHED. RESECURED EMERGENCY LIGHT COVER. OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 2008050500093 20080505 00093 WP 2008 5 5 NWAA081799869 1 20080424 A 2910 LINE DOUG DC9 DC951 3022051 WP HYD SYSTEM CHAFED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 778NC 48100 FIRST OFFICER NOTICED THAT THE RIGHT HYDRAULIC SYSTEM QUANTITY WAS LOSING FLUID. COM PROCEDURES WERE COMPLIED WITH AND T HE CREW ALSO DECLARED AN EMERGENCY IN ANTICIPATION OF NEEDING CFR EQUIPMENT. THE LANDING GEAR EXTENDED NORMALLY HOWEVER HYDRAULIC QUANTITY DECREASED TO ZERO BUT HYDRAULIC PRESSURE REMAINED AT 3000 PSI. GEAR WAS LOCKED IN PLACE WITHOUT PROBL EM AND HAD GREEN INDICATIONS. ALL INDICATIONS WERE NORMAL AFTER LANDING EXCEPT FOR THE ZERO QUANTITY ON THE RIGHT HYDRAU LIC SYSTEM. AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE FOUND THE RH HYDRAULIC SYSTEM RETURN LINE TO TH E O/B SPOILER CHAFED AND LEAKING. LINE WAS REPLACED WITH A TEMPORARY ONE AND CORRECT PART PLACED ON ORDER. 2 L 7 2 4F RT A6WE 2008050500095 20080505 00095 SO 2008 5 5 FDKA200804184 1 20080430 A 2510 SWITCH EMB 145 EMB145LR 3260212 SO CONTROL COLUMN SHORTED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 826MJ 145214 FDM 6169 RIC-MCO. ELECTRICAL BURN / SMOKE SMELL COMING FROM F/O'S CONTROL COLUMN (YOKE). MX INSPECTED AREA AND FOUND F /O'S YOKE CHART HOLDER SWITCH SHORTING OUT. MX REMOVED AND REPLACED CHART HOLDER. 2 L 7 2 4T RT T00011AT 2008050500098 20080505 00098 2008 5 5 SWAA082368 4 20080428 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 454WN 29851 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008050500102 20080505 00102 NM 2008 5 5 USAA920080924 1 20080428 A 5320 65412259 SUPPORT FITTING BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CRACKED SUPPORT ZEE FITTING, BS 915, LBL 59, WL 208. REPLACED SUPPORT ZEE FITTING, BS 915, LBL 59, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008050500103 20080505 00103 NM 2008 5 5 USAA920080925 1 20080417 A 5320 65528783 CUSP WEB BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CRACKED CUSP WEB, BS 907 - BS 927, LBL 59. REPLACED CUSP WEB, BS 907 - BS 927, LBL 59 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008050800044 20080508 00044 2008 5 8 U662008F00000 4 20080304 A 3425 INDICATION SYS SKRSKY S76 S76B 8143007 NE PWA PT6 PT6B36 52043 EA COCKPIT UNKNOWN E U66A O OTHER O OTHER CR CRUISE 1 EA 63 150US 760312 PILOT REPORTED LOSS OF ALTITUDE AND HEADING INDICATIONS ON HIS SIDE (RT SIDE) WITH ASSOCIATED MALFUNCTION OF AUTOPILOT N R 2. FLOATS WERE DEPLOYED AS PRECAUTIONARY MEASURE DUE TO BEING IMC OVER WATER. NOTE: NO DISCREPANCIES HAVE BEEN FOUND YET. TROUBLESHOOTING STILL IN PROGRESS WITH THE ASSISTANCE OF MFG ENGINEERING. (K) 1 G 7 2 4U 4 U H1NE E4EA 2008050800046 20080508 00046 2008 5 8 BJNA032908001 4 20080329 A 2220 69733611 SPRING BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C1 13802 EU ELEVATOR BROKEN A BJNA K NONE O OTHER CR CRUISE 1 WP 11 43XA 24796 BJNA080401- ALTITUDE HOLD INTERMITTENT. FOUND ELEVATOR LOAD FEEL CENTERING SPRING (OUTER) BROKEN. REMOVED AND REPLACED ELEVATOR LOAD FEEL CENTERING SPRINGS (INNER AND OUTER). (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2008050800047 20080508 00047 NM 2008 5 8 BJNA032908002 1 20080402 A 2740 654997025 JACKSCREW BOEING 737 737400 138449A NM CFMINT CFM56 CFM563C1 13802 EU STABILIZER DAMAGED A BJNA K NONE F FLT CONT AFFECTED DE DESCENT 1 WP 11 43XA 24796 STABILIZER TRIM WOULD NOT KEEP UP WITH THE COMMANDED POSITION, ASSOCIATED WITH A STAB OUT OF TRIM ANNUNCIATION. STABILI ZER TRIMMED (UP), OK. REMOVED AND REPLACED STABILIZER JACK SCREW ASSY. WAITING FOR TEAR DOWN REPORT ON REMOVED UNIT. (K) 2 L 7 2 4F 4 F RT A16WE E21EU 2008050800062 20080508 00062 WP 2008 5 8 NWAA081979885 1 20080505 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 401EA 47682 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 12 AND 19 OF THE CABIN GO DIM AFTER ABO UT 3 SECONDS. MAINTENANCE REPLACED THE BATTERY PACK AT THE OVERWING AFT LEFT EXIT LIGHT ASSEMBLY. LIGHTS RETURNED TO N ORMAL FUNCTION AND OPERATIONAL DURATION. 2 L 7 2 4F RT A6WE 2008050800063 20080508 00063 WP 2008 5 8 NWAA081969885 1 20080505 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 401EA 47682 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 9 AND 13 OF THE CABIN GO DIM AFTER ABOU T 3 SECONDS. MAINTENANCE REPLACED THE BATTERY PACK AT THE OVERWING FWD LEFT EXIT LIGHT ASSEMBLY. LIGHTS RETURNED TO NO RMAL FUNCTION AND OPERATIONAL DURATION. 2 L 7 2 4F RT A6WE 2008050800066 20080508 00066 NM 2008 5 8 LYNX000012 1 20080421 A 3246 BEARING BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA NR 4 MLG FAILED A 3LYA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 21 502LX 4168 NR 4 MLG WHEEL ASSY OB BEARING ASSY FAILED DURING TAXI. REMOVED AND REPLACED RT MLG AXEL. REMOVED AND REPLACED RT MLG W HEEL SPEED TRANSDUCER. REMOVED AND REPLACED RT MLG NR 4 BRAKE ASSY. REMOVED AND REPLACED NR4 MLG WHEEL ASSY. REF LOG PAGES 005765,005766 AND 005767. 2 H 7 2 4T 4 T RT A13NM E00062EN 2008050800068 20080508 00068 EU 2008 5 8 NWAA081943316 1 20080504 A 2121 FAN AIRBUS 330 A330323 3930335 EU RECIRCULATION ODOR A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 816NW 0827 CREW REPORTED SMOKE AND ODOR IN CABIN. ECAM SHOWS CIRCUIT BREAKER TRIPPED FOR RIGHT RECIRCULATION FAN AND RECEIVED "CON D R CAB VENT FAULT". FOLLOWED COM, APPLIED MEL 21-21-01 AND ADVISED DISPATCH AND MAINTENANCE CONTROL. LANDING WAS UNEV ENTFUL. REF LOGPAGES 4518676 AND 4518672. 2 L 7 2 4F RT A46NM 2008050800069 20080508 00069 NM 2008 5 8 2008UALA02551 1 20080501 A 5241 WEB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD GALLEY DOOR INTERIOR SIDE OF UPPER HINGE SUPPORT WEB GOUGED AT GUIDE ARM BOLT COVER PLATE. MAJOR REPAIR ACCOMPLISHE D, REPLACED SUPPORT WEB. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050800070 20080508 00070 NM 2008 5 8 2008UALA02558 1 20080501 A 3350 30043231 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 332UA 24193 EMERGENCY LIGHT AFT OF DOOR 1 LEFT FUSELAGE. SUSPECT FAULTY LAMP. REPLACED LAMP OP CHECKED GOOD.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050800085 20080508 00085 SO 2008 5 8 GUUA04210804 1 20080421 A 3220 2052000002 SPRING EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE NLG DEFECTIVE A GUUA K NONE O OTHER AP APPROACH 1 SO 29 285AS 120265 FLIGHT 9300, DURING APPROACH, LANDING GEAR EXTENSION NOSE WHEEL DELAYS 4-5 SECONDS AFTER MAINS ARE DOWN AND LOCKED. REP LACED NOSE GEAR SPRING CARTRIDGE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 2008050800099 20080508 00099 NE 2008 5 8 HALA0800557 2 20080503 A 7300 9510RTC3 THERMOCOUPLE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE RT ENGINE FAILED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 479HA 55124 ENG R SYS FAIL. REMOVED AND REPLACED RIGHT ENGINE T-30 THERMOCOUPLE PER AMM 73-21-07. ALSO REMOVED AND REPLACED RIGHT ENGINE DEDICATED GENERATOR PER AMM 73-21-04. ENGINE RUN UP AND RTS CHECK OK. OK FOR SERVICE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2008050800102 20080508 00102 NM 2008 5 8 HALA0800567 1 20080423 A 5512 SKIN BOEING 767 7673CB 1385187 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 588HA 33466 LEVEL 2 CORROSION ON HORIZONTAL STAB CENTER SECTION UPPER SURFACE SKIN AT RBL 10, STR. 1, AROUND 2 FASTENERS. REWORKED PER SRM 55-10-01 FIG 101, REV 76. 2 L 7 2 4F RT A1NM 2008050800108 20080508 00108 NM 2008 5 8 HALA0800565 1 20080423 A 5512 SKIN BOEING 767 7673CB 1385187 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 588HA 33466 LEVEL 11 CORROSION ON THE HORIZONTAL STAB CENTER SECTION UPPER SURFACE SKIN AT LBL 1, STR 3, AROUND 2 FASTENERS. REMOVE D CORROSION AND REPROTECTED SURFACE IAW SRM 55-10-01 FIG 101, REV 76. 2 L 7 2 4F RT A1NM 2008050800111 20080508 00111 NM 2008 5 8 HALA0800572 1 20080506 A 3150 UNKNOWN BOEING 767 76733A 1385209 NM UNKNOWN A HALA O OTHER O OTHER CR CRUISE 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, CTR FUEL TANK AND TOTAL FUEL QTY INDICATORS INTERMITTENT. EICAS MSG FUEL QTY IND NOT DISPLAYE D, FUEL QTY IND DISPLAYED ON STATUS PAGE. INFO NOTED, BITE CHECK FQP PER AMM 28-41-00, NO CTR TANK FAULTS TOTAL FQTY IN DICATIONS AND FUEL SYST CK OK FOR SVC, MPCW. 2 L 7 2 4F RT A1NM 2008050800112 20080508 00112 SW 2008 5 8 AC2A119524 1 20080421 A 6520 222042411101 GEARBOX BELL 430 430 1182150 SW ALLSN 250C 250C40B 03032 NE TAIL ROTOR CRACKED B AC2A K NONE O OTHER IN INSP/MAINT 1 SW 31 430CH 49037 FLANGE MOUNTING EAR COMPLETELY CRACKED ON TAIL ROTOR GEAR BOX OUTPUT SLEEVE HOUSING. 1 G 7 2 3U 3 U RT H9SW E1GL 2008050800118 20080508 00118 NM 2008 5 8 HALA0800555 1 20080501 A 2100 UNKNOWN BOEING 767 767332 1382001 NM UNKNOWN A HALA O OTHER O OTHER CR CRUISE 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM, AFT COMPT TEMP STUCK AT 99 DEG F (ECS PG SHOWS "BLANK" AFT DUCT TEMP). AFT COMP TEMP SELECTOR CYCLED FULL COLD THEN FULL HOT. INDICATION ALL NORMAL THROUGHOUT RANGE. OK FOR FURTHER SERVICE. BOTH LEFT AND RIGHT EICAS COMPUTERS BITE CHECK CARRIED OUT. NO FAULTS FOUND. ECS PAGE IND NORMAL. 2 L 7 2 4F RT A1NM 2008050800120 20080508 00120 NM 2008 5 8 2008UALA02549 1 20080501 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD GALLEY DOOR LOWER AFT FRAME CRACKED UNDER STOP FITTING. MAJOR REPAIR ACCOMPLISHED, REPLACED AFT LWR FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050800121 20080508 00121 NM 2008 5 8 2008UALA02550 1 20080501 A 5241 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD GALLEY DOOR INTERIOR WINDOW BAY SUPPORT ANGLE FOR MECHANISM BOX IS CRACKED. MAJOR REPAIR ACCOMPLISHED, REPLACED SUP PORT ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050800123 20080508 00123 NM 2008 5 8 2008UALA02556 1 20080501 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD CARGO DOOR FRAME CRACKED AT LOWER AFT STOP FITTING. MAJOR REPAIR ACCOMPLISHED: REPLACED LOWER AFT FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050800122 20080508 00122 NE 2008 5 8 DXTA200803023 2 20080425 A 7320 LINE AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE NR 2 DISCONNECTED E DXTA O OTHER Y ENGINE STOPPAGE TX TAXI/GRND HDL 1 GL 07 280QS 181 UNCOMMANDED SHUTDOWN OF NR 2 ENGINE BY FADEC AFTER STARTUP. TROUBLESHOT TO A DISCONNECTED PS AIR LINE AT THE H2B FADEC. CONNECTED LINE PERFORMED NUMEROUS ENGINE STARTS AND RUNS NO DISCREPANCIES NOTED. ENGINE OPERATIONAL CHECK GOOD. ALL WOR K IAW MM 71-002 AND 71-008. 2 L 7 2 4F 4 F RT A50NM E44NE 2008050800124 20080508 00124 NM 2008 5 8 2008UALA02557 1 20080501 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD CARGO DOOR FWD FRAME IS CRACKED AT LWR STOP FITTING. MAJOR REPAIR ACCOMPLISHED, INSTALLED NESTED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050800129 20080508 00129 NM 2008 5 8 2008UALA02570 1 20080502 A 2120 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 823UA 952 F/A REPORTS BURNING ODOR IN REAR OF CABIN. COULD NOT DUPLICATE ODOR. NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050800130 20080508 00130 NM 2008 5 8 2008UALA02571 1 20080501 A 2800 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUEL SYSTEM UNKNOWN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 793UA 26946 RIGHT TANK QTY INCREASES 300 LBS EVERY 10 MINUTES WITH CENTER TANK PUMPS ON. OCCURS IN NORMAL CONFIGURATION, JUST CENTER TANK RIGHT AND LEFT PUMPS ON. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008050800132 20080508 00132 NM 2008 5 8 2008UALA02573 1 20080501 A 3320 362624 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE SEAT 1F UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 217UA 30550 LIGHT STRIP LOOSE AT SEAT 1F ARMREST. FOUND LOOSE LIGHT STRIP. SECURED LIGHT STRIP OPS CHECK GOOD.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008050800134 20080508 00134 2008 5 8 DXTA200803026 4 20080427 A 3460 8221019313 COMPUTER BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE FWD AVIONICS BAY INOPERATIVE E DXTA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 07 132QS 224 224 RK427 1 HOUR INTO FLIGHT, AT FL380, THE RUDDER BOOST FAIL LIGHT CAME ON. REMOVED AND REPLACED WITH OVERHAULED FGC COMPUTER. RU DDER BOOST OPS CHECKED GOOD IAW MM 27-21. 2 H 7 2 4F 4 F RT A16SW E25EA 2008050800137 20080508 00137 NM 2008 5 8 F3LA200800212 1 20080501 A 5321 D5367314700000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO DOOR DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO MID FLOOR PANEL 152WG HAS DAMAGED END. MAINTENANCE REMOVED DAMAGE AND P REPPED FOR REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PARAGRAPH 8C. APPLIED REPAIR TREATED AND PRIMED A ND APPLIED TOP COAT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PARAGRAPH 8C, SRM 51-75-12 AND SRM 51-75-12. UP ON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050800138 20080508 00138 NM 2008 5 8 F3LA200800214 1 20080501 A 5321 D5367204701000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED BULK CARGO PANEL 161BF HAS A PUNCTURE. MAINTENANCE CLEANED AREA FOR DAMAGE PREPPE D AND REPAIRED, APPLIED PRIMER AND TOP COAT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PARAGRAPH C AND SRM 51-7 5-12 AND SRM 51-75-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050800141 20080508 00141 CE 2008 5 8 GUUA04250801 1 20080425 A 3297 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT WING CHAFED A GUUA O OTHER O OTHER CL CLIMB 1 SO 29 231YV UE231 FLIGHT: 5401, AFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT. LANDING GEAR CIRCUIT BREAKER POPPED, UNABLE TO RESET. RETU RNED TO DEPARTURE. LANDED WITHOUT INCIDENT. REPAIRED CHAFED WIRE G15C22 AT LT WING ROOT. OPS CHECK NORMAL. 2 L 7 2 4T 4 T RT A24CE E26NE 2008050800143 20080508 00143 EA 2008 5 8 SWIA200819563 1 20080428 A 3234 HANDLE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A SWIA O OTHER O OTHER AP APPROACH 1 NM 07 466SW 7856 FLT 6139 - RECEIVED A NOSE GEAR DISAGREE WARNING WHEN EXTENDING GEAR. REPLACED NOSE GEAR SELECTOR VALVE IAW 32-33-10 AN D LANDING GEAR HANDLE ASSEMBLY IAW 32-31-01. OPS CHECK GOOD, PN 750006000, S/N OFF 02861, PN OFF 601R50967-11, S/N OFF 1468. 2 L 7 2 4F RT A21EA 2008050800149 20080508 00149 CE 2008 5 8 FFSA200800002 1 20080426 A 3246 13600LA902A1 BEARING BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA NR 4 WHEEL DISINTEGRATED A FFSA O OTHER O OTHER LD LANDING 1 AL 01 575Y 285 NOV962957 UC162 RT OB (NR 4) MAIN WHEEL AND TIRE ASSEMBLY SEPARATED FROM AIRCRAFT ON LANDING ROLL. WHEEL BEARINGS FAILED ALLOWING WHEEL TO SEPARATE OVER THE AXLE NUT. THERE WERE 285 HOURS AND 256 CYCLES ON THE ASSEMBLY SINCE SCHEDULED BEARING INSPECTION AN D LUBRICATION. 2 L 7 2 4T 4 T RT A24CE E4EA 2008050800150 20080508 00150 EU 2008 5 8 08FDEA01773 1 20080428 A 5311 A5383312720400 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 MAIN CABIN FRAME 40 L BETWEEN STRINGER 15L AND STRINGER 16 L THE FRAME IS GOUGED. PERFORMED SMOOTH BLENDOUT FOR THE DAM AGED AREA IAW EA 6-5312-118485 "FUSELAGE FRAME 40 AT STRINGER 15L AND STRINGER 16L GOUGE REPAIR". RESTORED THE SURFACE PROTECTION IAW EA 6-5310-118485. 2 L 7 2 4F RT A35EU 2008050800151 20080508 00151 CE 2008 5 8 GUUA04270802 1 20080427 A 5540 10164001415 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RUDDER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81546 26091 UE187 DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED UPPER RUDDER HINGE BRACKET SHOW SIGNS OF EXFOLIATION. REPLACED UPPER R UDDER HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2008050600001 20080506 00001 NM 2008 5 6 HALA0800549 1 20080428 A 3610 SHUTOFF VALVE BOEING 767 7673G5 1385126 NM PWA 4060 PW4060 52119 NE LEFT MALFUNCTIONED A HALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM, ATO, LT HPSOV EICAS MSG UPON SPOOL-UP FOR TAKEOFF, ABORTED TAKEOFF, AT 60-80 KNOTS AIRSPEED. LOCKED-OUT HPSOV VALVE PER MEL MPCW, ALSO ACCOMPLISHED HIGH ENERGY STOP INSPECTION, FOR ABORTED T/O PER TASK 05-51-14-21 2-089. OK TO CONTINUE PER FIG 201. ALL CHECKS ARE OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2008050600024 20080506 00024 NM 2008 5 6 ASAA0842861 1 20080413 A 5320 65C335831 WEB BOEING 737 737490 1384715 NM BS 986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 R2 DOOR FLOOR STRUCTURE CORROSION FOUND AT BS 986.5 RBL 44 UPPER SURFACE OF WEB. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008050600028 20080506 00028 NM 2008 5 6 ASAA0842859 1 20080328 A 5320 654582952 WEB BOEING 737 737490 1384715 NM DOOR FRAME CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 E/E BAY DOOR LATCH PIN RUBBING ON RT WEB OF DOOR CUT OUT. WEB OF DOOR CUT OUT REPLACED IAW 51-40-02. 2 L 7 2 4F RT A16WE 2008050600031 20080506 00031 NM 2008 5 6 ASAA0842853 1 20080331 A 5754 65C26602312A WEDGE BOEING 737 737490 1384715 NM NR 5 SLAT DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 RT WING NR 5 LE SLAT T/E OUTBOARD END FILLING COMPOUND DAMAGE. RT WING L/E SLAT NR 5 T/E OUTBOARD END REPAIRED IAW B 73 7 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 2008050600039 20080506 00039 NM 2008 5 6 DHL2008760514 1 20080416 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272B7 138407L NM BS 480-690 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND REPLACED SEAT TRACK SECTION AT LBL 45, FROM BS 480 TO 690, PER B727 SRM 53-10-2 FIG 7 AND 53-10 -5 FIG 1. 2 L 7 3 4F A3WE 2008050600042 20080506 00042 EU 2008 5 6 08FDEA01687 1 20080430 A 5755 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 4 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND DELAMINATION OUT OF LIMIT ON SPOILER 4 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 27-61-51/401. 2 L 7 2 4F RT A35EU 2008050600046 20080506 00046 EU 2008 5 6 08FDEA01691 1 20080430 A 5755 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 5 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND DELAMINATION OUT OF LIMIT ON SPOILER 5 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 27-61-53/401. 2 L 7 2 4F RT A35EU 2008050600050 20080506 00050 2008 5 6 2008UALA02507 4 20080427 A 2565 D2569000200060 SLIDE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE DOOR 1L DISLODGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 DOOR 1L SIDE FELL OUT OF PACK. REPLACED SLIDE WITH SERVICEABLE UNIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050600081 20080506 00081 EU 2008 5 6 TRBA2008048 1 20080427 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 425MJ 425 FWD EMERGENCY EXIT SIGN INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK FROM POWER SUPPLY 61WL AS PER MM NR 33-51-26 . 2 H 7 2 4T RT A53EU 2008050600083 20080506 00083 NM 2008 5 6 DHL2008760503 1 20080420 A 5754 RIB BOEING 727 7272B7 138407L NM NR 3 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED AND REPLACED INBOARD AND OUTBOARD RIBS AT NR 3 SLAT ACTUATOR ROD END ATTACH POINT, P/N 65-17294U14 AND 65-17294U 13, AT LWS 519.0, PER B727 SRM 51-30-2 AND 51-30-5. 2 L 7 3 4F A3WE 2008050600085 20080506 00085 NM 2008 5 6 DHL2008760528 1 20080402 A 5311 FRAME BOEING 727 7272B7 138407L NM BS 600 S16R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 FABRICATED AND INSTALLED FRAME REPAIR AT BS 600, AND STR 16R, PER B727 SRM 53-10-2 FIG 3 AND SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2008050600087 20080506 00087 WP 2008 5 6 AALA200800794 1 20080402 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7526A 49918 LGA - EMERGENCY LIGHTS AT OVERHEAD AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD AFT G ALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008050500113 20080505 00113 NM 2008 5 5 USAA920080935 1 20080422 A 5312 65175829 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CRACKED BULKHEAD VERTICAL BEAM WEB, BS 178, RBL 17.1, WL 183. REPAIRED BULKHEAD VERTIC AL BEAM WEB, BS 178, RBL 17.1, WL 183 IAW B737 SRM 53-10-08 2R12. 2 L 7 2 4F RT A16WE 2008050500115 20080505 00115 NM 2008 5 5 USAA920080937 1 20080411 A 5312 65163007 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CRACKED BULKHEAD WEB, BS 178, LBL 10, WL 234. REPAIRED BULKHEAD WEB, BS 178, LBL 10, W L 234 IAW B737 SRM 53-10-08 2R9. 2 L 7 2 4F RT A16WE 2008050500119 20080505 00119 EU 2008 5 5 USAA920080940 1 20080428 A 5320 D5347217220500 BEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 188US 1724 PIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON CABIN BEAM, BS 3756/FR 64 - BS 4003/FR 69, +Y1292. REPLACED CABIN BEAM, BS 3756/FR 64 - BS 4003/FR 69, +Y1292 IAW A321 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008050500124 20080505 00124 NM 2008 5 5 08FDEA01596 1 20080425 A 5330 6554583155 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 LWR FUSELAGE SKIN SURFACE DENT AT STR 21 L APPROX STA 1130. CUT OUT DAMAGED AREA DIM CUT OUT (4" X 1') IAW SRM 53-30-3 FAB REPAIR. TREATED AND PRIMED DOUBLER REPAIR AND AREA IAW SRM 51-10-2. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2. TREAT ED AND PRIMED DOUBLER REPAIR AND AREA IAW SRM 51-10-2 INSTALLED REPAIR DOUBLER IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008050500125 20080505 00125 EU 2008 5 5 08FDEA01597 1 20080425 A 5420 A546114000000 PANEL AIRBUS 300 A300F4605R 3930327 EU NR 2 PYLON WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 NR 2 PYLON PANEL NR 423 CL IS WORN FROM FRETTING AT TWO LOCATIONS FRONT AND BACK. REMOVED DAMAGE REF A300-600 SRM 51-73 -10. ORIGINAL THICKNESS .078. REMAINING THICKNESS .052. REMOVED .026. BEYOND LIMITS REF A300-600 SRM 54-52-51. FABR ICATED DOUBLER AND FILLER REF A300-600 SRM 54-52-51, FIG 203. CUT OUT DAMAGE REF A300-600 SRM 54-52-51. ALODINED REF A 300-600 SRM 51-21-10. PRIMED REF A300-600 SRM 51-23-10. INSTALLED DOUBLER AND FILLER REF A300-600 51-40-21, PARA 5. P AINTED REF A300-600 SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008050500132 20080505 00132 NM 2008 5 5 08FDEA01606 1 20080425 A 5320 INTERCOSTAL BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 LWR FUSELAGE AFT PIT CORROSION ON INTERCOSTAL AT STA 885 FROM 28L TO 29L. REMOVED CORROSION AND EVALUATED AREA ORIGINAL MAT 0.032, MAT. REMAINING 0.029, MAT LOSS 0.003". TREATED AND PRIMED IAW SRM 51-10-06, 51-10-01 FIG 1, 51-10-02 AND S OPM 20-30-03. 2 L 7 3 4F A3WE 2008050500136 20080505 00136 2008 5 5 DXTA200803010 4 20080421 A 2210 7022090901 COMPUTER CESSNA 750 750 2076810 CE INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 930QS 3096 7500130 YD FAIL UPPER B CAS MSG CAME ON DURING CLIMB THRU FL 350 AFTER PASSING THRU LIGHT TURBULANCE. REPLACED AND OPS CHECKED B YSAC IAW M/M 27-24-01 2 L 7 2 4J RT T00007WI 2008050500137 20080505 00137 NM 2008 5 5 DXTA200803008 1 20080421 A 2731 02112112 ACTUATOR AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE INOPERATIVE E DXTA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 07 284QS 5565 185 NORMAL TRIM SYS FAILED INFLIGHT AND WOULD NOT RE-ENGAGE, (ELEVATOR). REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATO R WITH A REPAIRED/MODIFIED ASSEMBLY PER MM W/C 27-406, 27-404. 2 L 7 2 4F 4 F RT A50NM E44NE 2008050500144 20080505 00144 WP 2008 5 5 08FDEA01617 1 20080426 A 7110 ASL00401 COWLING DOUG MD10 MD1010F 3022112 WP NR 3 ENGINE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 3 ENG LT CORE COWL INNER SURFACE OF LEADING EDGE WORN. REMOVED ASL 0040-0 ADAPTER. LOCATED & DRILLED HOLES IAW SRM 51-35-01 & ASL 0040. INSTALLED ASL 0040 ADAPTER IAW SRM 51-35-01 & ASL 0040. PAINTED IAW SRM 51-23-01. 2 L 7 3 4F RT A22WE 2008050500146 20080505 00146 WP 2008 5 5 08FDEA01619 1 20080426 A 5730 ARB11137 SKIN DOUG MD10 MD1010F 3022112 WP RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 RIGHT WING UPPER I/B L/E PANEL 618AT INNER SKIN IS DAMAGED. REMOVED DAMAGED SECTION INNER SKIN IAW SRM 57-10-00. FABRIC ATED FILLERS 2 EA AND A REPAIR DOUBLER IN REF TO SRM 57-10-00. PRIMED REPAIR PARTS IN REF TO SRM 51-21-01. INSTALLED FIL LERS AND REPAIR COUBLER IN REF TO SRM 51-35-01. 2 L 7 3 4F RT A22WE 2008050500150 20080505 00150 WP 2008 5 5 08FDEA01624 1 20080425 A 5350 AKC715026 INTERCOSTAL DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 TAIL CONE, PATIO DOOR, LATCHING MECHANISM, LT SIDE, INTERCOSTAL CRACKED. REMOVED CRACKED INTERCOSTAL FROM THE TAIL CONE IAW SRM 51-35-01; VOL II. HEAT TREATED IAW DWG HT 042808-6, TESTED 58-60 ON RWD. FABRICATED NEW INTERCOSTAL IAW DWG AKC 7150. ALODINED & PRIMED THE INTERCOSTAL IAW SRM 51-21-01 VOL II. INSTALLED THE INTERCOSTAL IAW SRM 51-31-01 VOL I I. 2 L 7 3 4F RT A22WE 2008050500151 20080505 00151 WP 2008 5 5 08FDEA01625 1 20080425 A 5350 AKC708255 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 200 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 TAIL CONE, PATIO FLOOR; DOOR; DELAMINATED. FABRICATED NEW PATIO FLOOR DOOR; POTTED EDGES, COMPLETED CURE & SANDED THE EDGE POTTING, INSTALLED INSERTS; APPLIED NON-SKID. PART MARKED PANEL; REMOVED HARDWARE FROM THE OLD PANEL & REINST ALLED THE HARDWARE ON THE NEW PANEL IAW DWG SRM 25-005; REV F. 2 L 7 3 4F RT A22WE 2008050500158 20080505 00158 WP 2008 5 5 08FDEA01634 1 20080425 A 5347 NCA602223 SEAT TRACK DOUG MD10 MD1010F 3022112 WP FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 MAIN CABIN SEAT TRACK IN BALLMAT AREA SCALLOPS BROKEN AND SEVERAL GOUGES STA 753 TO STA 763 RBL 9. THE DAMAGED SCALLOPS ON THE SEAT TRACK AT RBL 9 & BS 753-763 FOUND TO BE OUT OF LIMITS IN REF TO SRM 53-70-00 VOL I FIG 5 SHEET 1. REMOVED DAMAGED SECTION AT BS 725-784 RBL 9. INSTALLED FABBED SEAT TRACK SECTION IAW SRM 53-70-00 VOL I FIG 1. REMOVED & REINS TALLED THE FLOOR PANELS IAW SRM 51-31-00 VOL II PG 1. MATERIAL ID SECTION; SPLICE HAT & PLATE IAW SRM 53-70-00 VOL I FIG 1 SHEET 2 & RAM DRAWING 1428, REV I. ALODINED & PRIMED PATS IAW SRM 51-21-1 VOL II PGS 1-25. 2 L 7 3 4F RT A22WE 2008050500159 20080505 00159 WP 2008 5 5 08FDEA01635 1 20080428 A 5347 AFA7789521 SEAT TRACK DOUG DC10 DC1010F 3022111 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE ON SEAT TRACK AT STA 502 X= 63, FOUND CORROSION AND SCREW BROKEN. REPLAC ED TRACK AFA7789-521 FOR DWG AND SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F A22WE 2008050500161 20080505 00161 WP 2008 5 5 08FDEA01637 1 20080428 A 5310 AEA01121 DOOR FRAME DOUG DC10 DC1010F 3022111 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1305 JAMB DOOR R3 FOUND CRACK 0.5 INCH LONG ON THE WEB. REPAIRED FOR SRM 53-50-00 FIG 19 VOL I. 2 L 7 3 4F A22WE 2008050500163 20080505 00163 EU 2008 5 5 08FDEA01640 1 20080428 A 5330 SKIN AIRBUS 310 A310 EU FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 445FE 297 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT RIGHT SIDE FUSELAGE SKIN BETWEEN FRAMES 16A TO 18 AND BETWEEN STRINGERS 41 A ND 43 RT MEASURES 11 INCH BY 8.1. "REPAIR NOT IAW WITH SRM 53-12-12 FIG 201, REPAIR NOT APPLICABLE TO AREA. REMOVED AN D REPLACED REPAIR IAW EA 6-5310-118112. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008050500164 20080505 00164 EU 2008 5 5 08FDEA01641 1 20080428 A 5330 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 445FE 297 REPAIR FOUND TO NOT BE IAW SRM 53-12-12- FIG 201 SHEET 1. REPAIR NOT APPLICABLE TO AREA. RESULT OF AGING AIRCRAFT INSP ECTION REMOVED AND REPLACED REPAIR IAW EA 6-5310-118130. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT. 2 L 7 2 4F RT A35EU 2008050500172 20080505 00172 NM 2008 5 5 MASA200800344 1 20080427 A 2910 849557 SPU DHAV DHC8 DHC8202 2809007 NM HYDRAULIC SYS LEAKING A MASA O OTHER K FLUID LOSS CR CRUISE 1 SW 07 437YV 3498 437 ASH FLT 2743 - PHX-PSP - DECLARED AN EMERGENCY AND RETURNED TO FIELD DUE TO NR 2 HYDRAULIC SYSTEM COMPLETE FLUID LOSS. REMOVED AND REPLACED NR 2 SPU. 2 H 7 2 4T RT A13NM 2008050500175 20080505 00175 EA 2008 5 5 MASA200800347 1 20080427 A 2120 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA CABIN ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 07 914FJ 15014 ASH FLT 2672 CLT- EWR - FAINT/BRIEF BURNING SMELL IN CABIN ON DESCENT. MX FOUND NO DEFECT. 2 L 7 2 4F RT A21EA 2008050500180 20080505 00180 NM 2008 5 5 P5CA0801560 1 20080427 A 7810 NOZZLE BOEING 747 74746NF 13848BT NM NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 454PA 30812 DURING WALK AROUND A 15" LONG CRACK WAS FOUND ON THE NR 2 ENGINE EXHAUST NOZZLE ON THE UPPER RIGHT QUADRANT. AN INTERIM REPAIR WAS ACCOMPLISHED PER EO 4478A069 AND 8110-3 DATED 27 APRIL 2008 ISSUED. 2 L 7 4 4F RT A20WE 2008050500181 20080505 00181 NM 2008 5 5 SB08023 1 20080429 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 457UW 25021 MIA - DURING OPERATIONAL CHECK OF EMERGENCY LIGHTS, MAINTENANCE FOUND THE AFT RIGHT OVERWING EXTERIOR LIGHT WOULD ONLY S TAY ON FOR ABOUT 10 TO 15 SECONDS AND THE INTERIOR CABIN EMERGENCY LIGHTS FROM ROW 5 FORWARD STAYING ON FOR ONLY 5 SECON DS. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT M1137 FOR THE EXTERIOR LIGHT AND THE BATTERY PACKS AT M1132 AN D M1133 FOR THE INTERIOR LIGHTS PER MM 33-51-51. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008050500200 20080505 00200 NM 2008 5 5 DL764080636 1 20080425 A 3246 BEARING 328040006 BOEING 767 767432ER 1385134 NM MLG FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 832MH 29704 ON PUSH BACK, RAMP REPORTED NOISE FROM NR 1 MAIN TIRE. FOUND NR 1 MAIN TIRE BEARING FAILING. REPLACED NR 1 MAIN WHEEL ASSY PER MM. 2 L 7 2 4F RT A1NM 2008050500201 20080505 00201 NM 2008 5 5 DL757080640 1 20080425 A 5420 311N31108 STRUCTURE BOEING 757 757232 1384965 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 646DL 24217 HMV AT SAA, A CRACK WAS FOUND IN THE UPPER CHORD OF THE NR 1 PYLON, RT SIDE, AT NACELLE STA 136. THE CRACK WAS REPAIRED PER BOEING INSTRUCTIONS. 2 L 7 2 4F RT A2NM 2008050500202 20080505 00202 NM 2008 5 5 DL757080641 1 20080425 A 5420 311N3150 STRUCTURE BOEING 757 757232 1384965 NM NR 1 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 646DL 24217 DURING HMV AT SAA, THE NR 1 PYLON INBOARD SIDE HAD AN ELONGATED HOLE IN THE UPPER CHORD AT N STA 128. THE ELONGATED HOL E WAS REPAIRED PER BOEING INSTRUCTIONS. 2 L 7 2 4F RT A2NM 2008043000171 20080430 00171 NM 2008 4 30 SWAA082284 1 20080427 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008043000188 20080430 00188 NM 2008 4 30 CALA0800389 1 20080428 A 5311 146A1131 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24706 28767 CABIN STATION 747 AT S9L PASSENGER SERVICE UNIT RAIL BRACKET TO FRAME CRACKED. REPAIRED FRAME REF EA 5310-04498. 2 L 7 2 4F RT A16WE 2008043000205 20080430 00205 NM 2008 4 30 SWAA082310 1 20080428 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008050100094 20080501 00094 NM 2008 5 1 2008UALA02425 1 20080424 A 2400 CONTROL PANEL BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FAULTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 228UA 30556 ELMS P310 PANEL THE ELECTRICAL LOAD MANAGEMENT SYSTEM (ELMS) P310 PANEL IS FAULTED SUCH THAT IT CANNOT SUPPORT AIRPLANE DISPATCH. AIMS HAS LOST ARINC 629 COMMUNICATION WITH THE P310 PANEL, OR ONE P310 PANEL CHANNEL IS LOST AND THE OTHER FA ULTED AND IS OPERATING IN A DEGRADED MODE, OR BOTH P310 PANEL CHANNELS ARE FAULTED AND A STATUS MSG01- ACTIVE CRUISE HAR D; ELMS P310, POWER MANAGEMENT PANEL, (STDBY) HAS NO OUTPUT ON ANY BUSS, MSG-2418803 ACTIVE ER HARD. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008050100095 20080501 00095 NM 2008 5 1 2008UALA02426 1 20080424 A 3510 OXYGEN MASK BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CAPTAIN'S FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 942UA 26679 CAPT O2 MASK MIC INOP SAMC TEXT: REPLACE CAPTAINS O2 MASK STOWAGE BOX. REPLACED OXYGEN MASK STOWAGE BOX. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050100096 20080501 00096 NM 2008 5 1 2008UALA02427 1 20080424 A 4900 APU BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 PRIOR TO DEPARTURE APU FAILED TO START. 2 L 7 2 4F 4 F RT A1NM E24NE 2008050600097 20080506 00097 NM 2008 5 6 DHL2008760521 1 20080407 A 5347 BAC1520841 SEAT TRACK BOEING 727 7272B7 138407L NM BS 760-850 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND REPLACED SEAT TRACK SECTION AT RBL 24, FROM BS 760 TO 850, PER B727 SRM 53-10-2 FIG 7 AND 53-10 -5 FIG 1. 2 L 7 3 4F A3WE 2008050600098 20080506 00098 NM 2008 5 6 DHL2008760522 1 20080407 A 5347 BAC1520841 SEAT TRACK BOEING 727 7272B7 138407L NM BS 760-850 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND REPLACED SEAT TRACK SECTION AT RBL 45, FROM BS 760 TO 850, PER B727 SRM 53-10-2 FIG 7 AND 53-10 -5 FIG 1. 2 L 7 3 4F A3WE 2008050600105 20080506 00105 WP 2008 5 6 AALA200800820 1 20080405 A 2150 97968011 VALVE DOUG DC9 DC983 3022083 WP A/C PACK INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 592AA 53255 SAV INFLIGHT T1914/05APR DFW TO JAX - CREW REPORTED LOSING LEFT AIR CONDITIONING PACK IN ICING CONDITIONS. FLIGHT WAS I N HOLDING PATTERN FOR JAX DUE TO THUNDERSTORMS. LANDED SAV WITHOUT INCIDENT. REPLACED LEFT AIR CONDITIONING PACK ANTI ICE VALVE AND REPLACED WATER SEPARATOR BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008050600123 20080506 00123 WP 2008 5 6 08FDEA01709 1 20080501 A 5347 601096418 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 309FE 48298 MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT F/S 1481-1531 RBL 28 BLENDED AREA ORIG MAT .145 MAT LOSS .050 AFTER REWO RK FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5 VOL 1. REMOVED IAW SRM 51-31-01. REPLACED SEAT TRACK IAW 53-70- 0 0 FIG 1 VOL 1. INSTALLED NEW SEAT TRACK IAW SRM 53-70-00 FIG 1. FABRICATED SEAT TRACK ON MAE TRAVELER T8/737387 F/S 14 81-1531 RBL 28. 2 L 7 3 4F RT A22WE 2008050600125 20080506 00125 WP 2008 5 6 08FDEA01711 1 20080501 A 5347 60450818 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 309FE 48298 MCD FLOOR SEAT TRACK AT STA 635 LBL 28 HAC GOUGES MARK. REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1 SEAT TRACK FABRICATE D ON MAE TRAVELER T8/737329 STA 635 LBL 28. 2 L 7 3 4F RT A22WE 2008050700003 20080507 00003 SO 2008 5 7 RAIA00804024 1 20080423 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 831HK 145232 PRE FLT NR 7892 - STL - EMERGENCY LIGHT AT ROW 12 INOPERATIVE. MAINTENANCE CLEANED THE CONNECTOR TO THE AFFECTED LIGHT ASSEMBLY. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008050700004 20080507 00004 SO 2008 5 7 RAIA00804027 1 20080425 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 813HK 145044 PRE FLT 5452 - STL - EMERGENCY LIGHTS AT ROW 17 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY FOR THE AFFECTED LIGHTS. OPS CHECKED GOOD AFTER THE CHANGE. 2 L 7 2 4T RT T00011AT 2008050700013 20080507 00013 NM 2008 5 7 AALA200800839 1 20080407 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 DFW - EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050700021 20080507 00021 NM 2008 5 7 DHL2008760544 1 20080421 A 5330 SKIN BOEING 727 7272B7 138407L NM BS 680-708 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED EXISTING REPAIR AND ALL CORROSION ON FUSELAGE SKIN AT BS 680 TO 708, STR 27R TO 27L. FABRICATED NEW DOUBLER REP AIR, AND INSTALLED PER B727 SRM 53-30-3 FIG 3A AND 53-30-2 FIG 2. 2 L 7 3 4F A3WE 2008050700025 20080507 00025 WP 2008 5 7 AALA200800853 1 20080407 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 968TW 53618 LGA - BATTERY PACK FOR EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT CAB IN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008050700028 20080507 00028 NM 2008 5 7 AALA200800792 1 20080402 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 350AN 33089 MIA - EMERGENCY LIGHTS AT SEAT ROWS 39B TO 41B INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT ROWS 39B TO 41B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008050700029 20080507 00029 EA 2008 5 7 COMA0860232 1 20080422 A 7330 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA FUEL SYSTEM UNKNOWN A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 721CA 7259 FLIGHT 4972 - ON TAKEOFF ROLL NR 2 ENGINE FUEL FLOW READ OUT WAS 1300 LBS. ABORTED TAKEOFF SAFELY. TRANSFERRED TO DMI LIST PER 73-31-01. 2 L 7 2 4F RT A21EA 2008050700041 20080507 00041 WP 2008 5 7 08FDEA01716 1 20080501 A 5347 601096418 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 309FE 48298 MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT FS 1481-1531 RBL 48. REPLACED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1 S EAT TRACK FABRICATED ON MAE TRAVELER T8/737389. MAIN CARGO COMPARTMENT RBL 48 STA 1481-1531. 2 L 7 3 4F RT A22WE 2008050700045 20080507 00045 NM 2008 5 7 DHL2008788001 1 20080325 A 5754 65162255 SKIN BOEING 727 727214 138407R NM NR 3 K FLAP GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 788AT 21958 NR 3 K-FLAP HAS SMALL GOUGE ON LOWER I/B EDGE. DEFECT WAS BLENDED IAW B727SRM 57-50-1 DETAIL 4 GOUGE REMOVED, MINIMAL M ATERIAL LOSS. 2 L 7 3 4F A3WE 2008050700049 20080507 00049 EA 2008 5 7 A6WA200840329 1 20080414 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 202 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 CRACK EXIST ON FORWARD PRESSURE BULKHEAD F/S 202.75 BL 45, WL 69, 684 AROUND PARKING BRAKE (.250 LONG). (M) FWD PRESSUR E BULKHEAD REPAIRED IAW REO 601R5311536. (P) 2 L 7 2 4F RT A21EA 2008050700067 20080507 00067 WP 2008 5 7 UPS08852092 1 20080418 A 5347 3657502U509 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 COCKPIT FIRST OFFICERS LT AFT SEAT TRACK HAS ELONGATED HOLES. REMOVED AND REPLACED SEAT TRACKS IAW S RM 51-3-1, 51-1-20D, 51-1-8, 51 -1-24. 2 L 7 4 4F RT 4A25 2008050700075 20080507 00075 NM 2008 5 7 USAA920080947 1 20080409 A 5320 655287897 SILL BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON THE L2 DOOR CUTOUT LOWER SILL INNER CHORD UPPER SURFACE, BS 956 - BS 996, LBL 50, WL 208. REPLACED THE L2 DOOR CUTOUT LOWER SILL INNER CHORD UPPER SURFACE, BS 956 - BS 996, LBL 50, WL 208 IAW B 737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008050700077 20080507 00077 WP 2008 5 7 AALA200800846 1 20080407 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 505AA 49799 LGA - BATTERY PACK AT B5 3 FOR EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 3 FOR EMERGENCY LIGHT S IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008050700091 20080507 00091 NM 2008 5 7 USAA920080964 1 20080409 A 5320 9H53461221 BEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON CABIN BEAM UPPER CHORD, BS 1016, RBL 7, WL 208. REPAIRED CABIN BEAM UPPER CHORD, BS 1016, RBL 7, WL 208 IAW USAIRWAYS EA 130007. 2 L 7 2 4F RT A16WE 2008050700097 20080507 00097 EU 2008 5 7 08FDEA01755 1 20080505 A 5347 A5383202020400 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 MAIN DECK CARGO SEAT TRACK NR 2 LT, HAS 3 AREAS OF CORROSION BETWEEN FR 40 AND FR 45. REMOVED LEVEL 1 CORROSION, REMOVE D AND REPLACED SEAT TRACK NR 2 LT FROM FR 40 TO FR 45 IAW A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008050700098 20080507 00098 WP 2008 5 7 AALA200800848 1 20080407 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 505AA 49799 LGA - BATTERY PACK AT B5 101 FOR EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 101 FOR EMERGENCY L IGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008050700112 20080507 00112 WP 2008 5 7 NWAA081889873 1 20080430 A 2120 UNKNOWN DOUG DC9 DC951 3022051 WP CABIN SMOKE A NWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 782NC 48107 AFTER TAKEOFF FLT ATTENDANT REPORTED SMOKE IN CABIN. FLT CREW COMPLIED WITH COM PROCEDURES FOR SMOKE REMOVAL & INITIATE D A RETURN. PILOTS NOTED RT AC SYS INDICATING FULL HOT IN AUTOMATIC MODE, TRIED FULL COLD IN AUTO MODE. VALVE POSITION REMAINED IN FULL HOT UNTIL CREW SELECTED FULL COLD IN MANUAL MODE, & SMOKE & HEAT SOON DISSIPATED. ATB LANDING UNEVENT FUL. MX INSPECTED ALL POSSIBLE OIL LEAK SOURCES, FOUND MINIMAL RESIDUE. REPLACED WATER SEPARATOR SOCKS & CABIN TEMP CO NTROLLER (AT A2-5) & ACCOMPLISHED PACK BURNOUT PROCEDURES. COALESCER BAGS WERE SPECIFICALLY DESCRIBED AS DIRTY BUT NOT OIL SOAKED. AFTER PACK BURNOUT PROCEDURES COMPLETED & NO OTHER EVIDENCE OF SMOKE NOTED, ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008050700114 20080507 00114 EA 2008 5 7 MASA200800353 1 20080429 A 3350 COVER CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 903FJ 15003 ASH FLT 2632 - EMERGENCY FLOOR LIGHT STRIP COVER LOOSE ROW 1-3. MX RESECURED COVER. 2 L 7 2 4F RT A21EA 2008050700128 20080507 00128 NM 2008 5 7 CALA0800404 1 20080430 A 5320 6546555 SUPPORT BRACKET BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 AIR CONDITIONING SUPPORT BRACKET CRACKED AT LEFTHAND FRAME STATION 867 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING S UPPORT BRACKET AT LEFTHAND FRAME STATION 867 BETWEEN S-8 AND S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008050700132 20080507 00132 NM 2008 5 7 08FDEA01761 1 20080505 A 5753 65217912 SUPPORT ANGLE BOEING 727 7272S2F 1384O81 NM RT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 RT WING INBD MID-FLAP AFT LOWER SUPPORT ANGLE IS CRACKED 2 PLACES AT WBL 100. REMOVED I/B MID FLAP LOWER PANEL FOR ACCE SS IAW SRM 51-30-2. CUT OUT DAMAGE SECTION DIM CUT OUT (61 INCHES BY 2 INCHES) IAW SRM 51-10-1, AND 51-40-4 FIG 3. FAB REPAIR ANGLE IAW SRM 57-50-2 FIG 5 AND 51-40-03 FIG 3. TREAT AND PRIMED ALL PARTS IAW SRM 57-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2. INSTALLED LWR SKIN PANEL IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008050700134 20080507 00134 NM 2008 5 7 CALA0800406 1 20080430 A 5320 6546550 SUPPORT BRACKET BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 AIR CONDITIONING SUPPORT BRACKET CRACKED AT RIGHTHAND FRAME STATION 787 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT RIGHTHAND FRAME STATION 787 BETWEEN S-8 AND S-9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 2008050700143 20080507 00143 WP 2008 5 7 MWEA080062 1 20080426 A 3350 60030457 BATTERY PACK DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 805ME 48031 EMERGENCY FLOOR TRACK LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 2008050700153 20080507 00153 SO 2008 5 7 C2XA08TY047 1 20080429 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26549 145571 SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB ON SERVICE DOOR IAW EMB 145AMM 33-50-10, OPS CHECK GO OD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008050700163 20080507 00163 NM 2008 5 7 AALA200800793 1 20080402 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 JFK - EMERGENCY LIGHTS AT FIRST CLASS GALLEY CENTER COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK M33093 FOR EMERGENCY LIGHTS AT FIRST CLASS GALLEY CENTER COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050700186 20080507 00186 NM 2008 5 7 200805011 1 20080428 A 3250 WARNING SYSTEM EMB ERJ170 ERJ170100SE 3260406 NM COCKPIT MALFUNCTIONED A UHLA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 11 863RW 17000100 FLIGHT 6433 ATL TO MTY ON APPROACH CREW RECEIVED A STEER FAIL MESSAGE ON THE EICAS WHEN EXTENDING THE LANDING GEAR. CRE W COMPLETED THE QRH PROCEDURES, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET B 25 C/B. MESSAGE CLEARED. NO OTHER MAINTENANCE WAS PERFORMED. HAS NOT DUPLICATED. 2 L 7 2 4F RT A56NM 2008050700189 20080507 00189 NM 2008 5 7 USAA920080977 1 20080418 A 5320 146N52819 FITTING BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL CLIP, BS 1300, RBL 45.5, WL 208. REPLACED INTERCOSTAL CLIP, BS 130 0, RBL 45.5, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008050700200 20080507 00200 NM 2008 5 7 SB08025 1 20080501 A 2560 P4010021 BATTERY BOEING 737 7374B7 1384702 NM FLASHLIGHT DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 453UW 24980 MIA - MAINTENANCE REPORTED AN INOPERATIVE EMERGENCY FLASHLIGHT ON AFT GALLEY. MAINTENANCE REMOVED AFT GALLEY EMERGENCY FLASHLIGHT AND FOUND INTERNAL BATTERY DISCONNECTED. DISCONNECTED/RECONNECTED BATTERY, INSTALLED FLASHLIGHT AND FOUND NO RMAL IAW USAIRWAYS MPPM 543-20, PAGE 7. 2 L 7 2 4F RT A16WE 2008050700206 20080507 00206 EU 2008 5 7 TRAX200800587 1 20080430 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 EMERGENCY LIGHTS COME ON WHEN SWITCH IS PLACED IN THE ARM POSITION. 2 H 7 2 4T RT 2008050700208 20080507 00208 EA 2008 5 7 TRAX200800589 1 20080501 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 861AS 7445 MAIN PAX DOOR HARD TO CLOSE HAD TO GET GROUND PERSONNEL TO CLOSE IT FROM OUTSIDE. 2 L 7 2 4F RT A21EA 2008050700210 20080507 00210 SO 2008 5 7 RAIA00805002 1 20080501 A 7897 WIRE EMB 145 EMB145 3260210 SO THRUST REVERSER BROKEN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 802HK 145066 FLT 3562 - STL - NR 1 THRUST REVERSER DISAGREE MESSAGE ON THE EICAS DURING CLIMB. MAINTENANCE REPAIRED A BROKEN WIRE AT THE RELAY SOCKET K0481. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2008050700241 20080507 00241 EA 2008 5 7 A6WA200840304 1 20080401 A 5320 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA BS 574 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 CRACK FOUND CARGO DOOR SURROUNDING STRUCTURE CHANNEL AT FS 574 WL 79 LBL 45. (M) REPLACED IAW SRM 51-42-06. (A) 2 L 7 2 4F RT A21EA 2008050700247 20080507 00247 2008 5 7 BB08074 4 20080428 A 3442 20414440406 ANTENNA BOEING 767 7672B7 1385107 NM WEATHER RADAR INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 255AY 70566 305 25257 PHL - FLT 714 PHL TO VCE. DURING CLIMBOUT TO THE TRACK SYSTEM, THE WEATHER RADAR BECAME INOPERATIVE IN THE NORMAL MODE. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE WEATHER RADAR ANTENNA. OK FOR S ERVICE. 2 L 7 2 4F RT A1NM 2008050700249 20080507 00249 NM 2008 5 7 BB08075 1 20080429 A 2421 727792H IDG BOEING 757 7572S7 1384962 NM NR 2 INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 904AW 59703 17679 23566 PHX - FLT 432 PHX TO OGG. DURING CLIMBOUT FROM PHX, THE RT GEN & RT GEN DRIVE LIGHTS ILLUMINATED, WITH GEN FAIL AND DR IVE LIGHTS ON IN EICAS. THE FLIGHT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 IDG. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 2008050700263 20080507 00263 NM 2008 5 7 ZZDA2008100 1 20080502 A 5280 DOOR BOEING 717 717200 1383700 NM NLG OPEN A ZZDA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 37 956AT 55018 SEVERE VIBRATION AFTER TAKEOFF. DISCOVERED LEFT NOSE GEAR DOOR OPEN DURING INSPECTION (WALKAROUND). RELATCHED NOSE GEA R DOOR, NO DAMAGE NOTED. BOTH LEFT AND RIGHT NOSE GEAR DOORS LOCK NORMAL. REF TO AMM 32-20. 2 L 7 2 4F TR A6WE 2008050700267 20080507 00267 EU 2008 5 7 08FDEA01742 1 20080503 A 5347 A53278450200 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 673FE 780 MAIN CARGO SEAT TRACK NR 2 LT HAS 2 AREAS OF CORROSION AT FR 72 TO FR 74. REMOVED LEVEL 1 CORROSION AND REPAIRED SEAT T RACK NR 2 LT, Y450, WITH SPLICE REPAIR BETWEEN FR 74 AND FR 80 IAW A300-600 SRM 53-10-16, FIG 201, PAGE 207/208. 2 L 7 2 4F RT A35EU 2008050700269 20080507 00269 NM 2008 5 7 ZZDA2008099 1 20080423 A 5320 J0602289 PAN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 985AT 55090 AFT CARGO COMPARTMENT DOOR FRAME LOWER PAN, CORRODED BEYOND LIMITS. INSTALLED SPLICE REPAIR PER B717 SRM 51-41-05. 2 L 7 2 4F TR A6WE 2008050700297 20080507 00297 2008 5 7 SWIA200819582 3 20080502 A 6197 SWITCH EMB 120 EMB120ER 3260203 SO AUTOFEATHER SYS DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 218SW 120287 FLT 5538 - LEFT AUTO-FEATHER SYSTEM FAILED. REPLACED PIN 1 ON AUTO-FEATHER TEST SWITCH. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 2008050700301 20080507 00301 EA 2008 5 7 SWIA200819584 1 20080502 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 903SW 7425 FLT 6603 - FIRST OFFICERS WINDSHIELD BROKE ON CLIMB-OUT. REPLACED RIGHT WINDSHIELD IAW MM 56-11-01, P/N OFF 601R33033-1 0, S/N OFF 00080H3197. 2 L 7 2 4F RT A21EA 2008050700304 20080507 00304 EA 2008 5 7 SWIA200819585 1 20080214 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 461 FAILED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 438SW 7574 RIVET SHEARED ON FLOOR SUPPORT BEAM BRACKET AT FS 461 AND LBL9, FOUND AT C-CHECK. COMPLIED WITH NECESSARY REPAIRS PER C RJ200 SRM 51-42-06 PG 11. 2 L 7 2 4F RT A21EA 2008050700305 20080507 00305 EU 2008 5 7 USAA920080985 1 20080426 A 5320 D5348004320501 SILL AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 188US 1724 PIT - MAJOR REPAIR -S3 CHECK - LEVEL 2 CORROSION ON R3 DOOR CUTOUT LOWER SILL FORWARD END, BS 3851 / FR 66, S20R. REPLA CED R3 DOOR CUTOUT LOWER SILL FORWARD END, BS 3851 / FR 66, S20R IAW A321 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008050700313 20080507 00313 NM 2008 5 7 USAA920080995 1 20080502 A 3350 1146801 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 322AW 25400 SEA - EEL - FLIGHT 0070 - ROW 3 EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AND OPERATIONAL CHECKED ROW 3 EMERGENCY EXIT LIGHT ASSEMBLY. 2 L 7 2 4F RT A16WE 2008050700332 20080507 00332 NM 2008 5 7 2008UALA02443 1 20080425 A 5753 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT WING TE FLAP CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 RT WING INBD FLAP UPPER SURFACE CHAFED IN AREA OF PREVIOUS REPAIR ON INBD TOP SIDE OF FLAP. ACCOMPLISHED MAJOR REPAIR, R EMOVED PREVIOUS REPAIR AND REPLACED WITH PERMANENT REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080519 SO 2008 5 19 CHQA200800092 1 20080503 A 3297 14521492405 WIRE HARNESS EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NLG CORRODED A CHQA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 11 292SK 145488 CAE311794 FLIGHT 7827, CMH TO IAD - ON FINAL APPROACH WHEN GEAR WAS SELECTED DOWN, THE FLIGHT CREW RECEIVED A LDG GEAR LEVER DISAG REE MESSAGE AND RED HATCHED BOX FOR NOSE WHEEL INDICATION. THE AIRCRAFT PERFORMED A GO AROUND AND THE CREW WENT THROUGH THE QRH CHECKLISTS. THE AIRCRAFT WAS SLOWED TO 200KTS AND THE GEAR EXTENDED NORMALLY. THE AIRCRAFT LANDED WITHOUT INC IDENT. MAINTENANCE INSPECTED THE LANDING GEAR AND FOUND THE NOSE LANDING GEAR DOWNLOCK INDICATION HARNESS CONNECTOR LOO SE. THE CONNECTOR WAS SECURED AND ALL GEAR INDICATIONS WERE NORMAL. THE AIRCRAFT WAS THEN FERRIED TO CMH FOR FURTHER T ROUBLESHOOTING. THROUGH FURTHER TROUBLESHOOTING THE NOSE LANDING GEAR DOWN LOCK HARNESSES WERE FOUND TO BE CORRODED AND 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008050100100 20080501 00100 EU 2008 5 1 2008UALA02432 1 20080425 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 457UA 1146 SKIN IS GOUGED AT FR 67 STRINGER 44 FROM TAIL STRIKE. SKIN WORN THROUGH TO FRAME AT FR70 STGR 44 DAMAGE MEASURES APPROX 6"X 4" FROM TAIL STRIKE BY- 254125 :CUT DAMAGED SKIN FOR ACCES S TO FRAME 70 DAMAGE EVALUATION.BLENDED DAMAGE ON FRAME. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050100102 20080501 00102 EU 2008 5 1 2008UALA02434 1 20080425 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 457UA 1146 SKIN IS WORN THROUGH AT FR 68 STR 44 AND MEASURES .5 INCH WIDE BY 2 INCH LONG. CUT DAMAGED SKIN FOR ACCES S TO FRAME 70 DAMAGE EVALUATION.BLENDED DAMAGE ON FRAME. CONT OF AMIS ITEM 8572009 :MFG FILLER FOR FR70 PER EVA71452. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050100103 20080501 00103 NM 2008 5 1 2008UALA02435 1 20080424 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 526UA 24994 FOUND EEL FLOOR LIGHTS INOP AT AFT LAV, ROWS 34 THRU 30, ROWS 22 THRU 16 AND EMERGENCY AISLE LIGHTS INOP AT ROWS 34 THRU 26 BOTH SIDES AND ROWS 18 THRU 14 LT SIDE. FOUND INVERTER FAILED. REPLACED INVERTER AT ROW 17ABC LT BATTERY PACK REPLA CED AT M10818 AND FUSES CHKD ON PWR SUPPLY AT M735.ORANGE EGRESS EEL LIGHT STRIP AND FC EEL LIGHT STRIP REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008050100104 20080501 00104 2008 5 1 2008UALA02436 4 20080424 A 2565 LATCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ESCAPE SLIDE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 RT OVERWING EMERGENCY SLIDE NR 1 LATCH IS HARD TO OPERATE. SUSPECT FAULTY BEARING. REPLACED NR 1 HATCH AT RT OVERWING SLIDE COMPT DOOR PER MM 25-65-09 ALIGNMENT CHECK GOOD IAW MM 25- 65-09.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008050100105 20080501 00105 NM 2008 5 1 2008UALA02437 1 20080424 A 5220 BACC2A4D00134JJ CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY EXIT FRAYED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 RT AFT EMERGENCY EXIT HATCH STEP FWD CABLE IS FRAYED. REPLACED CABLE IAW SRM 51- 40-02 AND OPS CHECKED GOOD IAW MM52-21 -01.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008050100106 20080501 00106 NM 2008 5 1 USAA920080922 1 20080425 A 3350 P4010021 BATTERY PACK BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHTS FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 334AW 23748 FLT NR 281 - PHX - MX REPORTED 2 FORWARD EMERGENCY FLASHLIGHTS INOP. MX REPLACED BOTH BATTERY ASSEMBLIES. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2008050200011 20080502 00011 SO 2008 5 2 CHQA200800086 1 20080426 A 2760 8005701 PROXIMITY SWITCH EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL SPOILERS CONTAMINATED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 297SK 145522 CAE311245 FLIGHT 5302 STL TO AUS - DURING TAKEOFF ROLE, THE FLIGHT CREW RECEIVED A SPOILER TAKEOFF CONFIGURATION MESSAGE ON THEIR EICAS. AT THAT POINT THE CREW DECIDED TO ABORT TAKEOFF AND RETURN TO THE GATE WITHOUT INCIDENT. MAINTENANCE FOUND NUME ROUS PROXIMITY SWITCHES CONTAMINATED WITH DE-ICING FLUID. MAINTENANCE CLEANED ALL SPOILER PROXIMITY SWITCHES AND CONDUC TED AN OPERATIONAL CHECK OF THE SYSTEM WITH NO FAULTS FOUND. 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008050200013 20080502 00013 WP 2008 5 2 UPS08852072 1 20080420 A 5712 RIB DOUG DC8 DC873F 302199F WP RWS 785 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 RT WING OUTBD, L/E UPPER RIB CRACKED JUST OUTBD OF ACCESS PNL 518 B XFS785.0. REPAIRED LT WING OUTBD LE UPPER RIB AT XFS785.0 IAW SRM 57-02-0 FIG 0 02 AND DWG 5769470. 2 L 7 4 4F RT 4A25 2008050200021 20080502 00021 WP 2008 5 2 UPS08852088 1 20080428 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP EMERGENCY LIGHTS DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 EMERGENCY LIGHTS FOR INTERIOR AND BATTERY TEST FAILED. SUSPECT BATTERY PACKS DEPLETED. OPS CHECK C/W PER MC 005 AND MM 33-50-01. NO DEFECTS NOTED. 2 L 7 4 4F RT 4A25 2008050200023 20080502 00023 NM 2008 5 2 UPS08M52081 1 20080325 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 919-969 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C CABIN, SEAT TRACK AT STA 919 - 969 X=-75.25 FOUND CORROSION. CORROSION AT AFFECTED AREA REMOVED. MAT 'L THK:0.145", MAT'L REMOVED 0.040 INCH (STA 939), MAT'L REMOVED: 0.105 INCH. FOUND OUT OF LIMIT. DISCREPANT SEAT TRAC K TRIM OUT. C HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. NEW SEAT TRACK REWORKED, 1 SPLICE HAT SECT AND 1 SPLICE PLATE FAB. NEW SEAT TRACK AND REPAIR PARTS REPROTECTED, PAINTED AND INSTALLED PER SRM 53-70-00 FIG 1 VIR35. 2 L 7 3 4F RT A22WE 2008050200037 20080502 00037 NM 2008 5 2 HALA0800545 1 20080425 A 2841 INDICATOR BOEING 767 76733A 1385209 NM FUEL QTY FAILED A HALA O OTHER P NO WARNING INDICATION CR CRUISE 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, CREW REPORTED CENTER FUEL TANK QUANTITY INDICATOR WENT BLANK. NO EICAS MESSAGE DISPLAYED. NO RMAL INDICATIONS RETURNED DURING FLIGHT. T/S PER FIM 28-41-00 FIG 114. PERFORMED FQIS PROCESS OR BITE PER FIM 28-41-00 /101 FIG 104. NO PRESENT FAULTS. RECORDED FAULT HISTORY AND FORWARDED TO TECH SERVICES. REF TSI 00054031. ERASED FAU LT HISTORY. PER FIM, SYSTEM CHECKS OK. 2 L 7 2 4F RT A1NM 2008050500005 20080505 00005 NM 2008 5 5 SWAA082307 1 20080428 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008050500007 20080505 00007 NM 2008 5 5 SWAA082319 1 20080428 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008050500009 20080505 00009 EU 2008 5 5 08FDEA01609 1 20080425 A 2910 9023A000401 PRESSURE SWITCH AIRBUS 310 A310203 3930313 EU HYD SYSTEM FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 415FE 349 AFTER DEPARTURE GOT A FLAP FAULT, FOUND FAULT CODE ON SFCC 1 LT WING HIGH SPEED PRESS SWITCH. PERFORMED TEST PER AMM 27 -51-00-5, ALL PASSED. SWITCHED SFCC NR 1 AND 2 NO FAULTS FOUND. SWITCHED BACK TO ORG PLACES. STARTED T/S PER PER A310 TSM 27-50-0 6. SECTION 1 PASSED. ASK FOR AV FOR CHECK OF PRESSURE SWITCH. READ PINS P TO B AND P TO C PER TSM 27-5 0-06. P TO B READ OPEN P TO C READ 73K OHMS PER FIG 102 RECOMMEND CHANGE HIGH SPEED PRESS SW AT 23CV PCU VALVE BLOCK. REMOVED AND REPLACED YELLOW VALVE BLOCK (23CV) HIGH SPEED PRESS SWITCH. OPS AND LEAK CHECK OK. REF MM 27-54-33-4. PER MOCC REQUEST, REMOVED AND REPLACED NR 1 SFCC CANNED OFF A/C 411. OPS CHECK OK. REF MM 27-51-18-4. 2 L 7 2 4F RT A35EU 2008050500010 20080505 00010 WP 2008 5 5 08FDEA01611 1 20080427 A 2110 3966361 CONTROL VALVE DOUG MD10 MD1010F 3022112 WP NR 2 FLOW MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 384FE 46617 RECEIVED A LEVEL 1 PACK 2 FLOW DISAGREE ALERT IN FLIGHT 6 TIMES. REMOVED AND REPLACED PACK 2 FLOW CONTROL VALVE, REF M M 21-51-02-4. REMOVED AND REPLACED PACK 2 FLOW TRANSMITTER. REF MM 21-52-01-4. OPS AND LEAK CHECK OK. 2 L 7 3 4F RT A22WE 2008050500012 20080505 00012 CE 2008 5 5 DJFA2008041 1 20080409 A 3097 WIRE CESSNA 750 750 2076810 CE DAMAGED E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 23 708LX 7500109 WHILE AIRCRAFT WAS DESCENDING INTO KLGA THE CREW NOTED A BURNING SMELL IN THE COCKPIT. AT THE SAME INSTANCE THE ODOR WAS NOTICED THE LT PANEL CIRCUIT BREAKER TRIPPED, AND THE LT INSTRUMENT PANEL BACKLIGHTING, AS WELL AS THE STANBY INSTRUMEN T BACKLIGHTING WAS LOST. SINCE THE AIRCRAFT WAS ON FINAL APPROACH FOR THE ATTENDED DESTINATION NO DIVERSION WAS PERFORME D. ONCE ON THE GROUND, MAINTENANCE TROUBLESHOT THE CAUSE OF THE ODOR / TRIPPED CIRCUIT BREAKER TO THE LT WINDSHIELD ICE DETECT LIGHT. IN ADDITION TO THE SHORTED LIGHT ASSY, THERE WAS A SPLICE ASSEMBLY REPLACED FOR PRECAUTION. ALL ASSOCIATE D WIRING WAS INSPECTED WITH NO OTHER DISCREPENCY'S NOTED. 2 L 7 2 4J RT T00007WI 2008050500014 20080505 00014 EA 2008 5 5 VNAA0804008 1 20080410 A 5730 WINGLET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT WING CRACKED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 259PS 7945 CREW REPORTED A CRACK IN THE RIGHT HAND WINGLET. MAINTENANCE INSPECTED AND FOUND THE RIGHT HAND WINGLET TO BE WITHIN LI MITS IN ACCORDANCE WITH THE CRJ200 STRUCTURAL REPAIR MANUAL. MAINTENANCE APPLIED SPEED TAPE. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008050500027 20080505 00027 NM 2008 5 5 SWAA082339 1 20080429 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008050500063 20080505 00063 NM 2008 5 5 SWAA082363 1 20080501 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500B, STR 27R TO STR 26L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008050500072 20080505 00072 CE 2008 5 5 GLBA20061089 1 20080422 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE BS 228 CORRODED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 255GL UE255 BELLY SKIN CORRODED AT FS 228.25 STRINGERS 15L AND 16L. MAINTENANCE REPAIRED BELLY SKIN AT F.S. 228.25 I.A.W. BEECH 1900 D SRM 51-70. REPAIR APPROXIMATELY 7.5" BY 9.5. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2008050500073 20080505 00073 CE 2008 5 5 GLBA20061090 1 20080422 A 5320 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 255GL UE255 RT WING TO FUSELAGE HEAVY ANGLE CRACKED ATH FWD BEND RADIUS APPROX 1.125 INCH IN LENGTH. MAINTENANCE INSTALLED REPAIR AN GLE I.A.W. SRM 53-90-23. REPAIR ANGLE 13.5 ". RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2008050500088 20080505 00088 EA 2008 5 5 HNAA0800147 1 20080418 A 2910 82910009145 HYDRAULIC LINE DHAV DHC8 DHC8311 1386006 EA HYDRAULIC SYS LEAKING A HNAA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 EA 07 337EN 284 LOSS OF NR 2 HYD FLUID AFTER GEAR EXTENSION FOLLOWED BY ISO VALVE & OUTBOARD SPOILER HYD CAUTION LIGHTS. NR 2 HYD SYSTE M QTY AT .5 QTS. INSTALLED TFL FROM DOOR CONTROL SOLENOID TO UNION IN FRONT OF NOSE GRAVEL GUARD IAW SPECIAL PROCEDURES 20.1 SERVICED NR 2 HYD SYSTEM IAW MAINT MANUAL 12-10-29. OPS & LEAK CHECK GOOD. PLACED ON 70 HR DMT WC 20-50-52T. RE F SAME LOG PAGE SEQ NR 1. 2 H 7 2 4T RT A13NM 2008050500110 20080505 00110 NM 2008 5 5 USAA920080932 1 20080422 A 5312 65175823 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CRACKED BULKHEAD CHORD, BS 178, LBL 5.7, WL 184. REPAIRED BULKHEAD CHORD, BS 178, LBL 5.7, WL 184 IAW B737 SRM 53-10-08-2R5. 2 L 7 2 4F RT A16WE 2008050500127 20080505 00127 NM 2008 5 5 08FDEA01599 1 20080425 A 5313 65168124 STRINGER BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 CORROSION ON OUTBRD SIDE OF STRINGER 26L AT STA 1133 (AFT PIT). CLEANED AND EVALUATED AREA, NO CORROSION FOUND IAW SOPM 20-30-03, SRM 51-10-06 PAR. 3 2 L 7 3 4F A3WE 2008050500168 20080505 00168 NM 2008 5 5 NWAA081805507 1 20080415 A 5512 SKIN PANEL BOEING 757 757251 1384970 NM HORIZ STAB DELAMINATED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 507US 23196 DURING "M" CHECK, FOUND DELAMINATION ON LT HORIZONTAL STABILIZER UPPER SKIN PANEL BETWEEN STA 68 AND STA 107. REPAIRED PER EA 55-212538. 2 L 7 2 4F RT A2NM 2008050500174 20080505 00174 EA 2008 5 5 MASA200800346 1 20080427 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651ML 7139 ASH FLT 7159, IAD-CLE - PAX DOOR OUTER HANDLE WILL NOT STOW. MX PERFORMED OP CHECK OF PAX DOOR, OP CHECK NORMAL. 2 L 7 2 4F RT A21EA 2008050500186 20080505 00186 NM 2008 5 5 HALA0800550 1 20080426 A 2780 3A1260A RVDT BOEING 767 767332 1382001 NM L/E SLAT MALFUNCTIONED A HALA K NONE F FLT CONT AFFECTED AP APPROACH 1 WP 13 596HA 23276 TE FLAP DISAGREE LIGHT WHEN FLAPS 15 SELECTED. USED ALTN FLAPS FOR LANDING W/ABOUT 13 DEG FLAPS LANDING SPEED 160 KITS. ACCOMPLISHED FIM 27-51-00 FIG 114C. FOUND M548 SLAT OUTBOARD RVDT FAULT REMOVED AND REPLACED SLAT OUTBOARD RVDT (M548 ) PER AMM 27-81-11. OPERATIONAL CK GOOD. 2 L 7 2 4F RT A1NM 2008050500193 20080505 00193 EA 2008 5 5 TRAX200800578 1 20080425 A 5210 INTERCOSTAL CNDAIR CL600 CL6002C10 1390015 EA ASD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 730EV 10141 ASD INTERCOSTAL CRACKED BETWEEN ACCESS PANELS 832AR AND 832BR (MARKED). 2 L 7 2 4F RT A21EA 2008050500194 20080505 00194 EA 2008 5 5 TRAX200800577 1 20080425 A 5210 SKIN CNDAIR CL600 CL6002C10 1390015 EA DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 730EV 10141 VDOOR INNER SKIN AT UPPER AFT CORNER (DOOR OPEN) CRACKED (MARKED) (RESOLVED ON W/O: 89292 TASKCARD: N/R-00122). JOB CO MPLETE. 2 CUT OUT DAMAGED AREA. FABRICATED FILLER. FABRICATED DOUBLER DRILLED FILLER. SMOOTHED OUT ROUGH EDGES ON ASD INNER SKIN AT UPPER AFT CORNER PER REO 670-52-11-154. PERFORMED ET INSPECTION OF REWORKED AREA PER REO 670-52-11-154 I AW CRJ 700 NDTM 51-20-006. NO DEFECTS NOTED. PICKED UP EXISTING HOLES, LAYED OUT NEW HOLES AND ALODINED, AND PRIMED AN D INSTALLED IAW REO 670-52-11-154. INSTALLED UPPER STIFFENER ON ASD DOOR IAW CRJ 700 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008050500195 20080505 00195 WP 2008 5 5 IXXA08SMN103S 1 20080314 A 5753 SKIN DOUG DC8 DC873F 302199F WP T/E FLAP DEFORMED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER PANEL DEFORMED AT STATION XW 104.000 TO STATION XW 115. 000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BO NDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, DC8 SRM 57-7-1 FIGURE 1 ITEM "A" AND "L", DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 51 -1-9 TR NUMBER 51-142, DC8 SRM 51-1-9A TR NUMBER 51-141, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008050600010 20080506 00010 NM 2008 5 6 USAA920080941 1 20080428 A 2560 P2070001214 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 322AW 25400 FLT NR 337 - LAS - FLIGHT ATTENDANT REPORTED AFT FLASHLIGHT INOP, NEEDS TO BE REPLACED. MX REPLACED AFT FLASHLIGHT BATT ERY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2008050600022 20080506 00022 WP 2008 5 6 IXXA08SMN109S 1 20080314 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 759 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STATION 759.000 LBL 22. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AN D PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, ATI REPAIR SPECIFICATION NUMBER 2003-05, DRAWING 3755222, DPS 4.707, SRM 51-1-8B, AND 51-3-1. 2 L 7 4 4F RT 4A25 2008050600040 20080506 00040 EU 2008 5 6 08FDEA01685 1 20080430 A 5755 SPAR AIRBUS 300 A300B4622R 3930312 EU NR 2 SPOILER CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 CHAFING MARKS AND ABRASION ON NR 2 LT SPOILER OUTBOARD SPAR REPAIR PERFORMED BY CUT THE DAMAGED AREA AND INSTALLING A DO UBLER IAW RAS 70503484/017/2008 ISS, APPROVED BY EA 6-5771-115271. 2 L 7 2 4F RT A35EU 2008050600051 20080506 00051 NM 2008 5 6 2008UALA02508 1 20080429 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 848UA 1647 O2 PRESSURE LOW. SERVICED CREW O2, NO LEAKS NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050600054 20080506 00054 EU 2008 5 6 2008UALA02511 1 20080427 A 5320 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 448UA 842 FOUND CORROSION IN FLOOR SUPPORT STRUCTURE AT FRAME 68 UNDER DOOR 2R THRESHOLD. MAJOR REPAIR ACCOMPLISHED, REPLACED FLO ORBEAM -Y1292 FROM FR 64-69. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050600057 20080506 00057 NM 2008 5 6 DHL2008760505 1 20080413 A 5720 6516275 WEB BOEING 727 7272B7 138407L NM CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED AND REPLACED NR 1 K-FLAP INBOARD AND OUTBOARD ACTUATOR MOUNT SUPPORT WEBS BY FABRICATION, LWS 307.5 TO 315.2, PE R B727 SRM 51-10-2, 51-30-2, 51-20-1 FIG 3, 51-30-5, AND BAC DWG 65-16275 REV D. 2 L 7 3 4F A3WE 2008050600058 20080506 00058 NM 2008 5 6 DHL2008760508 1 20080425 A 5753 65890861 FITTING BOEING 727 7272B7 138407L NM TE FLAP CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED AND REPLACED DAMAGED FITTING AT LT INBOARD AFT FLAP AT LWBL 124.2, P/N 65-89086-1, PER B727 SRM 51-30-2 AND 51-3 0-5. 2 L 7 3 4F A3WE 2008050600062 20080506 00062 NM 2008 5 6 08FDEA01695 1 20080430 A 5320 6525551 STRUCTURE BOEING 727 727232 1384082 NM WING TO BODY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 LWR EXT FUSE WING BODY FILLET FAIRING SUPPORT FRAME LWR CHORD ANGLE IS BUCKLED/CRACKED AT I/B END 950A, LBL 14. REPAIRE D SUPPORT FRAME LOWER CHORD ANGLE FOR WING TO BODY FAIRING AT 950A, LBL 14 REF SRM 51-40-3. THIS IS CLASSIFIED AS A MIN OR. 2 L 7 3 4F A3WE 2008050600067 20080506 00067 NM 2008 5 6 08FDEA01700 1 20080430 A 5210 65561502 SKIN BOEING 727 727232 1384082 NM R1 DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 MAIN DECK 1R DOOR EXT SKIN IS BUCKLED/CRACKED AT UPPER HINGE CUT OUT UPPER EDGE, 4 INCHES FROM FWD END. REMOVED DAMAGE AND CHECKED WITH HFEC, NO DEFECTS FOUND. REMOVED LINER SUPPORT, VERIFIED MATERIAL, MADE A .040 INSURANCE CUT REF SRM 52 -00-3 FIG 3 STEP 2. FABRICATED UPPER DOUBLE, TREATED AND PRIMED. INSTALLED DOUBLER AND PAINTED. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008050600072 20080506 00072 NM 2008 5 6 AALA200800811 1 20080403 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 780AN 29956 JFK - EMERGENCY LIGHT AT SEAT 26C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050600082 20080506 00082 NM 2008 5 6 DHL2008760527 1 20080402 A 5311 FRAME BOEING 727 7272B7 138407L NM BS 580 S16R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 FABRICATED AND INSTALLED FRAME REPAIR AT BS 580, AND STR 16R, PER B727 SRM 53-10-2 FIG 3 AND SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2008050600086 20080506 00086 WP 2008 5 6 IXXA08SMN115S 1 20080327 A 5740 FITTING DOUG DC8 DC873F 302199F WP BS 902 L19R CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT INTERCOSTAL SUPPORT FITTING CRACKED AT STATION 902.000 L ONGERON19 RIGHT. REMOVED CRACKED INTERCOSTAL SUPPORT. FABRICATED NEW INTERCOSTAL SUPPORTS. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA AND INTERCOSTAL SUPPORT IAW DC8 SRM 51-1-20D, 51-3-1, ATI REPAIR SPECIFICATIONS NUMBER 2003-05, DOUGLAS DRAWING 3779498, AND DPS 4.707. 2 L 7 4 4F RT 4A25 2008050600091 20080506 00091 NM 2008 5 6 HALA0800551 1 20080429 A 4900 024147000 BATTERY BOEING 767 76733A 1385209 NM APU INOPERATIVE A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 ETOPS SIGNIFICANT SYSTEM, APU DID NOT START-APU FAULT INDICATED. REPLACED APU BATTERY PER FIM 49-11-00 FIM 106A AND AMM 24-31-04. OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 2008050600104 20080506 00104 NM 2008 5 6 AALA200800808 1 20080402 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 39G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 39G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050700337 20080507 00337 NM 2008 5 7 2008UALA02448 1 20080426 A 5220 DOOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY EXIT MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 DOOR DIFFICULT TO ARM AT 2R DOOR NOT TO BE USED AS EMERGENCY EXIT BY FLT CREW. FOUND GLOB EPOXY ON BOTTOM OF GIRT BAR,C AUSING GIRT BAR SLIDERS HARD TO SLIDE IN TO FLOOR FITTINGS. CLEANED FLOOR FITTINGS AND GIRT BAR SLIDERS,LUBED BOTH WITH PINK GREASE.OPS CHECKED NORMAL. FOR THE RETRACTABLE DOOR FOUND THE PLACARD WAS GETTING STUCK IN LINER, REMOVED THE LITT LE EDGE OF THE PLACARD THAT WAS GETTING STUCK. DOOR OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008050700338 20080507 00338 NM 2008 5 7 KNNA20080010 1 20080417 A 5330 SKIN BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 464AT 21278 FOUND CRACK ON FUSELAGE SKIN DURING C-CHECK. WHILE REMOVING FASTENERS FOUND CORROSION ON UPPER SKIN FWD OF CRACK, OPENE D UP ENTIRE LAP JOINT AND REMOVED CORROSION ON UPPER SKIN. PERFORMED NDT IAW THE SRM AND FOUND 27 CRACKED COUNTERSINKS. CUTOUT ALL DAMAGE AND INSTALLED A REPAIR IAW BOEING MESSAGE 1-533791124 AND ACO-085315. 2 L 7 2 4F RT A16WE 2008050700341 20080507 00341 NM 2008 5 7 GTIA0800062 1 20080408 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 504NK 2473 FLOORBEAM CORRODED STATION 66.5 AT -Y765. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2008050600025 20080506 00025 NM 2008 5 6 ASAA0842862 1 20080413 A 5320 69774772 ANGLE BOEING 737 737490 1384715 NM BS 993 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 R2 DOOR FLOOR STRUCTURE CORROSION FOUND AT BS 993 RBL 42 ON ZEE REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008050600044 20080506 00044 EU 2008 5 6 08FDEA01689 1 20080430 A 5755 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 3 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND DELAMINATION OUT OF LIMIT ON SPOILER 3 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW AMM 27-61-51/401. 2 L 7 2 4F RT A35EU 2008050600059 20080506 00059 EA 2008 5 6 A6WA200840305 1 20080408 A 3340 LENS CNDAIR CL600 CL6002B19 1900309 EA LIGHT CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 RIGHT LIGHT LENS CRACKED. (M) RT WING LIGHT LENS REPLACED IAW AMM 57-30-01-400-801 AWAC SUPPLEMENT 07-009. (A) 2 L 7 2 4F RT A21EA 2008050600080 20080506 00080 NM 2008 5 6 AALA200800806 1 20080402 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050600095 20080506 00095 EU 2008 5 6 08FDEA01739 1 20080503 A 5730 A57244727202 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND ON LT ASA BOOSTER DOOR A CRACK IN HOLE FOR RUBBER STRIP ATTACHMENT. REPAIR PERFORMED BY CUT OUT AND INSTALLING A FILLER AND DOUBLER IAW, RAS/BAE/1006711/2008 ISS A, APPROVED BY EA 6-5751-117144. 2 L 7 2 4F RT A35EU 2008050600103 20080506 00103 NM 2008 5 6 AALA200800809 1 20080402 A 3350 HOUSING BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 779AN 29955 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE FORWARD CLOSET HAS BROKEN HOUSING. REPLACED HOUSING FOR EMERGENCY LIGHT AT LEF T NUMBER ONE FORWARD CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050600124 20080506 00124 WP 2008 5 6 08FDEA01710 1 20080501 A 5347 601096418 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 309FE 48298 MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT FS 1481-1531 RBL 28 BLENDED AREA ORIG MAT .145 MAT LOSS .050 AFTER REWOR K FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5 VOL 1. REMOVED IAW SRM 51-31-01. REPLACED SEAT TRACK IAW 53-70-00 F IG 1 VOL 1. INSTALLED NEW SEAT TRACK IAW SRM 53-70-00 FIG 1. FABRICATED SEAT TRACK ON MAE TRAVELER T8/737387 F/S 1481- 1531 RBL 28. 2 L 7 3 4F RT A22WE 2008050600127 20080506 00127 NM 2008 5 6 DHL2008760513 1 20080422 A 5320 AND101331202 STIFFENER BOEING 727 7272B7 138407L NM BS 227 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED CORRODED STIFFENER, FABRICATED, AND INSTALLED NEW VERTICAL STIFFENER FOR NLG RT FWD DOOR FWD SUPPORT LINK, BS 22 7.8, PER B727 SRM 53-10-2 FIG 1, 51-30-5, AND 51-30-2. 2 L 7 3 4F A3WE 2008050700026 20080507 00026 WP 2008 5 7 AALA200800860 1 20080408 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 59523 49915 TUL - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD BIN SEAT 6E FAILED OPERATIONAL TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD BIN SEAT 6E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008050700044 20080507 00044 EU 2008 5 7 08FDEA01719 1 20080501 A 5311 A5377321322400 WEB AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 THE FWD CARGO PIT FROM FRAME 21 - 22 HAS A CRACKED WEB AT THE FWD UPPER AND AFT LOWER CORNERS ABOVE STRINGER 44L. REMOV ED WEB & RAIL ASSEMBLY IAW SRM 51-40-21. REMOVED CRACKED WEB IAW SRM 51-40-21. INSTALLED NEW WEB IAW SRM 51-40-21. R EINSTALLED WEB & RAIL ASSEMBLY IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008050700047 20080507 00047 NM 2008 5 7 UPS08M52107 1 20080120 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C LEFT WING UPPER STRINGER END S9 SUSPECT AS MARKED, THRU ACCESS 38AB. HFEC INSP C/OUT PER DACNDTSPM R. 13 PART06.10.01.001&CRACK APPROX 12" FOUND. STR 9 CRACKED AREA TRIMMED OFF PER SRM 57-20-00 FIG 10V.1&EN1055-0 8. NEW STR & 03EA REP PARTS FABRICATED USING 1D0164 MATL PER SRM 57-20-00F IG.10V.1R.40&EN1055-08.FPI INSP C/OUT PER NDTSPMR.13 PART6 FOUND NO CRACK. HOLES ON NEW STR 9 & REP PARTS P/UP PER SRM 57-20-00 FIG 10&EN1055-08. 2 L 7 3 4F RT A22WE 2008050700052 20080507 00052 WP 2008 5 7 ABXA080139 1 20080425 A 2510 SEAT DOUG DC9 DC941 302207N WP COCKPIT UNLOCKED A ABXA K NONE O OTHER TO TAKEOFF 1 GL 23 959AX 47761 CAPTAIN'S SEAT BECAME UNLOCKED DURING ROTATION WHILE CAPTAIN WAS FLYING AND SLIDE TO REAR STOP. SEAT WAS VERIFIED LOCKE D DURING PUSHBACK. INSPECTED CAPTAIN'S SEAT IN ALL LOCKING POSITIONS. NO DEFECTS FOUND. MOVED SEAT VIGOROUSLY IN ALL LOCKING POSITIONS AND SEAT REMAINED LOCKED. CAPTAIN'S SEAT FORWARD & AFT LOCKS CHECK GOOD IAW DC9 AMM CHAPTER 25. 2 L 7 2 4F A6WE 2008050600107 20080506 00107 EA 2008 5 6 MASA200800354 1 20080430 A 7830 1267587 PDU CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER SEIZED A MASA O OTHER O OTHER CR CRUISE 1 SW 07 75994 21143 7367 ASH FLT 7116 CID-ORD - LT REV UNLOCK CAUTION. CREW PERFORMED IN FLIGHT ENGINE SHUTDOWN AND DECLARED EMERGENCY. ADJUSTE D STOW SWITCH. REMOVED AND REPLACED PDU. 2 L 7 2 4F RT A21EA 2008050600108 20080506 00108 EA 2008 5 6 MASA200800355 1 20080430 A 3397 CONNECTOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 939LR 15039 ASH FLT 2821 LGB-PHX - EMERGENCY EXIT SIGN ROW 15 AND 16 FORWARD PORTION INOP. MX RESECURED CONNECTOR TO SIGN, OPS CHEC K GOOD. 2 L 7 2 4F RT A21EA 2008050600113 20080506 00113 NM 2008 5 6 08FDEA01746 1 20080503 A 5753 6521795333A FAIRING BOEING 727 727232 1384082 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 LEFT WING INBOARD MID FLAP OUTBOARD JACK SCREW FAIRING INTERIOR SKIN CRACKED AT ATTACH HOLE REPAIRED LEFT WING INBD MID FLAP O/B JACK SCREW FAIRING REF SRM 57-20-4 PG 5 AND SRM 51-30-2 PG 2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008050600118 20080506 00118 EU 2008 5 6 08FDEA01756 1 20080505 A 5347 A5383202020400 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 MAIN DECK CARGO SEAT TRACK NR 3 LT HAS 3 AREAS OF CORROSION BETWEEN FR 45 AND FR 48. REMOVED LEVEL 1 CORROSION, REMOVED AND REPLACED SEAT TRACK NR 3 LT FROM FR 45 TO FR 48 IAW A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008050100087 20080501 00087 EU 2008 5 1 NSVA2008020 1 20080411 A 5751 725761061 AILERON SAAB SF340 340B 7860101 EU DAMAGED A NSVA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 27 347CJ 340B347 AIRCRAFT WAS STOPPED ON TAXIWAY ANOTHER ACFT TAXIED AROUND OUR ACFT ON THE RIGHT SIDE. LEFT WINGTIP/WINGLET IMBEDDED IN TO RT AILERON. AIRCRAFT RETURNED TO GATE FOR MX INSPECTION. REMOVED RT AILERON, INSPECTED RT AILERON AIRFRAME HINGES I AW SAAB SRM 51-10-00, NO DEFECTS NOTED. INSTALLED SERVICEABLE RT AILERON ASSY IAW SAAB MM 27-11-50. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 2008050100088 20080501 00088 EU 2008 5 1 NSVA2008015 1 20080401 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 203CJ 340B203 DURING RON IN TXK, AIRCRAFT SUSTAINED HAIL DAMAGE TO FUSELAGE, HORIZONTAL STAB, AND FLIGHT CONTROLS APPROX 67 DENTS NOTE D. AIRCRAFT FERRIED TO HOT SPRINGS ARK FOR REPAIR. 2 L 7 2 4T RT A52EU 2008050200062 20080502 00062 NM 2008 5 2 WRNA20080027 1 20080227 A 5311 FRAME BOEING 747 747230B 1384889 NM BS 2674-2680 DAMAGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 512MC 21220 DURING 'B' CHECK, FASTENERS WERE FOUND LOOSE AND MISSING RIGHT SIDE FRAME TO INTERCOSTAL AT STATION 2674 TO 2680 W/L 305 . FABRICATED REPAIR DOUBLER ANGLES IAW SRM 51-40-03 FIGURE 01 AND INSTALLED IAW SRM 51-30-02. 2 L 7 4 4F RT A20WE 2008050500001 20080505 00001 NM 2008 5 5 SWAA082326 1 20080429 A 3350 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 235WN 34630 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008050500015 20080505 00015 EA 2008 5 5 VNAA0804009 1 20080411 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE FUSELAGE DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 720PS 10178 CREW REPORTED A LIGHTNING STRIKE BELOW THE FIRST OFFICERS WINDOW. MAINTENANCE PERFORMED AN EN ROUTE AND A DETAILED LIGH TNING STRIKE INSPECTION. MAINTENANCE FOUND DAMAGE TO THE RIGHT SIDE OF THE FUSELAGE AND RIGHT WING TIP. MAINTENANCE RE PAIRED ALL DAMAGE IN ACCORDANCE WITH THE CRJ 700 STRUCTURAL REPAIR MANUAL. OPERATIONAL CHECKS WERE GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008050500021 20080505 00021 NM 2008 5 5 SWAA082341 1 20080429 A 5310 6546818 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CRACKED BETWEEN BS 540 AND BS 560, STR 17R. REMOVED AND REPLACED CRE ASE BEAM WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2008050500024 20080505 00024 NM 2008 5 5 SWAA082337 1 20080429 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008050500036 20080505 00036 NM 2008 5 5 SWAA082330 1 20080429 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 727E, LBL 7 TO LBL 12. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008050500041 20080505 00041 NM 2008 5 5 SWAA082349 1 20080501 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008050500053 20080505 00053 NM 2008 5 5 SWAA082353 1 20080501 A 2761 6544960 ACTUATOR BOEING 737 7373H4 1384600 NM NR 5 SPOILER LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND RIGHT WING NR 5 SPOILER INBOARD ACTUATOR UPPER ATTACH BOLT LOOSE. REMOVED AND REPLACE D SPOILER ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2008050500057 20080505 00057 NM 2008 5 5 SWAA082360 1 20080501 A 5311 6516301 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008050500069 20080505 00069 CE 2008 5 5 GLBA20061092 1 20080425 A 5312 BULKHEAD BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 255GL UE255 FWD PRESSURE BULKHEAD CRACKED AT FS 84.0 AT RT AVIONICS BAY AT INTERSECTION A OF ANGLE AT WL 92.0 AND STIFFNER AT RBL 15 .75. MAINTENANCE REPAIRED CRACK IN FORWARD PRESSURE BULKHEAD IAW SERVICE BULLETIN STEPS 3 THROUGH 8 & STEPS 1- THROUGH 2 2 AT F.S. 84.0. REPAIR AREA APPROXIMATELY 7.5" BY 5". RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1. 2 L 7 2 4T 4 T RT A24CE E26NE 2008050500074 20080505 00074 SO 2008 5 5 FDKA200804175 1 20080421 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN DISCONNECTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 855MJ 145614 FDM 6038 CVG-IAD. LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. MX RECONNECTED THE WIRE AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2008050500096 20080505 00096 SO 2008 5 5 FDKA200804185 1 20080430 A 5320 14521725001 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 837MJ 145367 RIGHT FLOOR SILL AT FRAME NR 22 IS CORRODED OUT OF LIMITS. THE DAMAGED SILL HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 2008050500111 20080505 00111 NM 2008 5 5 USAA920080933 1 20080422 A 5312 651630087 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CRACKED BULKHEAD CHORD, BS 178, RBL 29, WL 206 - WL 208. REPLACED BULKHEAD CHORD, BS 1 78, RBL 29, WL 206 - WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008050500112 20080505 00112 NM 2008 5 5 USAA920080934 1 20080422 A 5312 651758335 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CRACKED BULKHEAD VERTICAL BEAM WEB, BS 178, RBL 5.7, WL 180 - WL 184. REPAIRED BULKHEA D VERTICAL BEAM WEB, BS 178, RBL 5.7, WL 180 - WL 184 IAW B737 SRM 53-10-08 2R12. 2 L 7 2 4F RT A16WE 2008050500126 20080505 00126 NM 2008 5 5 08FDEA01598 1 20080425 A 5313 65168124 STRINGER BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 AFT PIT CORROSION ON INBD SIDE OF STRINGER 28R AT BS 990. CLEANED AND EVALUATED AREA, NO CORROSION FOUND IAW SOPM 20-30 -03 AND SRM 51-10-01. 2 L 7 3 4F A3WE 2008050500130 20080505 00130 EU 2008 5 5 08FDEA01604 1 20080425 A 5753 A5796001220000 SKIN AIRBUS 300 A300F4605R 3930327 EU LT WING DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 LEFT WING FLAP HAS A DENT LOCATED 62 INCHES FROM THE OUTBD END AND 26 INCHES FROM THE T/E THAT HAVE BEEN FOUND TO BE OUT OF LIMITS ON N/R N00417. FABRICATED DOUBLER IAW SRM 57-50-00. LOCATED & DRILLED IAW SRM 57-50-00. ALODINED IAW SRM 51 -21-10. PRIMED IAW SRM 51-23-10. INSTALLED IAW SRM 57-50-00. PAINTED & SEALED IAW SRM 51-23-10. 2 L 7 2 4F RT A35EU 2008050500143 20080505 00143 NM 2008 5 5 08FDEA01616 1 20080428 A 5730 ARB74024 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 628FE 48447 14 FASTENER HOLES FOUND WITH CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CU TOUT BETWEEN STA XORS = 690 AND STA XORS = 700. COMPLIED WITH E.A. 1-5710-113138, CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008050500170 20080505 00170 WP 2008 5 5 070195 1 20080425 A 3350 57761 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A WX0A K NONE O OTHER NR NOT REPORTED 1 WP 19 880GA 49625 IT HAS BEEN REPORTED BY THE FLIGHT CREW, THE FORWARD RIGHT AND LEFT CABIN DOOR "EXIT" EMERGENCY EVACUATION LIGHT WAS FOU ND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008050500173 20080505 00173 EA 2008 5 5 MASA200800345 1 20080425 A 3350 BATTERY CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 516LR 10258 ASH FLT 7257 IAD-MHT - EMERGENCY LIGHTS WILL NOT STAY ON. MX CHARGED BATTERIES, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008050500191 20080505 00191 EA 2008 5 5 TRAX200800576 1 20080425 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 833AS 7246 LEFT FWD OVERWING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008050500210 20080505 00210 EU 2008 5 5 08FDEA01649 1 20080429 A 5532 A55373211008 PANEL AIRBUS 300 A300F4605R 3930327 EU VERTICAL STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 VERTICAL STAB L/E PANEL 322 BL IS DAMAGED ON THE LEADING EDGE. REMOVED AND REPLACED THE ERROSION STRIP IAW AMM 55-32-11 -8 AND E.A. 6-5530-118505. 2 L 7 2 4F RT A35EU 2008050500212 20080505 00212 EU 2008 5 5 08FDEA01651 1 20080429 A 5532 A55373211008 PANEL AIRBUS 300 A300F4605R 3930327 EU VERTICAL STAB DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 VERTICAL STAB L/E PANEL 322 BL IS DISBONDING AROUND THE HOIST POINT AND THE UPPER LEFT CORNER. REMOVED AND REPLACED THE ERROSION STRIP IAW AMM 55-32-11-8 AND EA 6-5530-118505. 2 L 7 2 4F RT A35EU 2008050600003 20080506 00003 EU 2008 5 6 08FDEA01648 1 20080402 A 5720 A572408452000 PLATE AIRBUS 300 A300B4622R 3930312 EU LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 LT WING, L/E ACCESS PANEL ATTACHMENT CHORD (LANDING PLATE) CRACKED 523BB BETWEEN RIB 8 AND 9. REPAIRED IN ACCORDANCE WITH FEDEX ENGINEERING AUTHORIZATION 6-5720-117325. 2 L 7 2 4F RT A35EU 2008050600012 20080506 00012 NM 2008 5 6 USAA920080942 1 20080409 A 5315 6546812186 FLOORBEAM BOEING 737 73733A 1384673 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON CABIN FLOORBEAM, BS 1000, RBL 13, WL 208. REPLACED CABIN FLOORBEAM, BS 10 00, RBL 13, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008050600013 20080506 00013 NM 2008 5 6 USAA920080943 1 20080409 A 5320 6546812161 STRAP BOEING 737 73733A 1384673 NM BS 1012 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON FLOOR STRUCTURE STRAP, BS 1012, RBL 4, WL 208. REPLACED FLOOR STRUCTURE S TRAP, BS 1012, RBL 4, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008050600019 20080506 00019 NM 2008 5 6 USAA920080952 1 20080417 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 812AW 1178 SAL - EMERGENCY EQUIPMENT - BC6 CHECK - FORWARD FLIGHT ATTENDANTS RIGHT FLASHLIGHT BATTERY LOW. REPLACED THE BATTERY IN THE FORWARD FLIGHT ATTENDANTS RIGHT FLASHLIGHT. 2 L 7 2 4F RT A28NM 2008050600027 20080506 00027 NM 2008 5 6 ASAA0842864 1 20080415 A 5315 654681180 FLOORBEAM BOEING 737 737490 1384715 NM BS 986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 AFT CABIN BS 986.5 FLOORBEAM LBL 4 FOUND CORRODED AT FASTENER HOLE LOCATION (CLIP NUT). AFT CABIN FLOOR BEAM AT BS 986 LBL 4 CORROSION AT FASTENER LOCATION REPAIRED IAW B737 400 SRM 53 00 51 FIG 201 REPAIR 3. 2 L 7 2 4F RT A16WE 2008050600032 20080506 00032 NM 2008 5 6 ASAA0842854 1 20080331 A 5730 654645170A SKIN BOEING 737 737490 1384715 NM WING DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 TWO DENTS FOUND ON LWR SURFACE FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMITS, PERMANENT REPAIR IAW BOEING SRM 51-70-10 REPA IR 2. 2 L 7 2 4F RT A16WE 2008050600034 20080506 00034 NM 2008 5 6 ASAA0842857 1 20080329 A 5753 65C35705Y2 SKIN BOEING 737 737490 1384715 NM RT WING TE FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 RT OUTBOARD T/E FORE FLAP L/E GOUGED, REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008050600047 20080506 00047 EU 2008 5 6 08FDEA01692 1 20080430 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND ELONGATED HOLES ON LT/RT BOTTOM WING SKIN AND SUPPORT BRACKET FOR HYDRAULIC LINES. REPAIR PERFORMED BY ACCOMPLISH MENT OF SB A300-29-6057, APPROVED BY EA 6-2900-114925. 2 L 7 2 4F RT A35EU 2008050600060 20080506 00060 EU 2008 5 6 08FDEA01694 1 20080430 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND ELONGATED HOLES ON RT BOTTOM WING SKIN AND SUPPORT BRACKET FOR HYDRAULIC LINES. REPAIR PERFORMED BY OVERSIZING AND SPOTFACING THE HOLES, INSTALLING FREEZE PLUG IAW DRAWING R571-50532, APPROVED BY RAS/BAE/1006364/2008 ISS A AND EA 6 -2900-114925. 2 L 7 2 4F RT A35EU 2008050600069 20080506 00069 WP 2008 5 6 AALA200800818 1 20080404 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 581AA 53158 LGA - EMERGENCY LIGHTS AT TAIL COMPARTMENT INOPERATIVE. REPLACED BATTERY PACK AT AFT RIGHT LAVATORY FOR EMERGENCY LIGHT S AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008050600088 20080506 00088 WP 2008 5 6 08FDEA01738 1 20080427 A 2150 9273184 TRANSMITTER DOUG MD10 MD1010F 3022112 WP NR 1 PACK FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 384FE 46617 RECEIVED A LEVEL 1 PACK 2 FLOW DISAG ALERT IN FLIGHT 6 TIMES. REMOVED AND REPLACED PACK 2 FLOW CONTROL VALVE, REF MM 2 1-51-02-4. REMOVED AND REPLACED PACK 2 FLOW TRANSMITTER, REF MM 21-52-01-4. OPS AND LEAK CHECK OK. 2 L 7 3 4F RT A22WE 2008050600089 20080506 00089 NM 2008 5 6 08FDEA01704 1 20080430 A 5511 69331746 RIB BOEING 727 727232 1384082 NM HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 RT HORIZONTAL STAB, AFT SUPPORT RIB IS CRACKED NEAR ELEVATOR ATTACH POINT, ELEVATOR STA 99.79 REMOVED WIPER PLATES, REF SRM 51-30-2. FAB RADIUS FILLER FOR REPAIR, .100" 2024-T3 REF DWG 69-33174. TREATED AND PRIMED REF SRM 51-10-2. INSTAL LED REPAIR REF SRM 55-10-4, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008050600102 20080506 00102 WP 2008 5 6 AALA200800810 1 20080402 A 2910 37723745503 VALVE DOUG DC9 DC982 3022082 WP HYD SYSTEM LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 214AA 49162 DFW INFLIGHT T1468/02APR - RIGHT HYDRAULIC QUANTITY DECREASED TO ZERO DURING FLIGHT. REPORT OF ODOR OR SMOKE IN CABIN. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND RUDDER HYDRAULIC SHUTOFF VALVE BODY CRACKED AND LEAKING. REPLACED RUDDER HYDRAULIC SHUTOFF VALVE AND REPLACED APU DUE TO SKYDROL INGESTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008050600116 20080506 00116 NM 2008 5 6 DHL2008760524 1 20080421 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272B7 138407L NM BS 950-1135 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND REPLACED SEAT TRACK SECTION AT LBL 24, FROM BS 950 +10 TO 1135, PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 2008050700001 20080507 00001 2008 5 7 YENA2008037 4 20080424 A 2330 LSEBUTK1400101 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU CABIN MALFUNCTIONED A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 640JB 4503 4503 2832 FLT 704, SJU-JFK, F/A REPORTED BURNING SMELL AROUND ROW 11. LIVE TV MASTER TURNED OFF AND SMELL STOPPED. PERFORMED LTV ELECTRICAL ODOR SYSTEM INTEGRITY CHECK. REMOVED AND REPLACED XEB 10 RT. ALL AS PER LIVE TV MM 23-39-00. ALL OPS CHEC K NORMAL. 2 L 7 2 4F RT A28NM 2008050700014 20080507 00014 WP 2008 5 7 AALA200800847 1 20080407 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 505AA 49799 LGA - BATTERY PACK AT B5 100 FOR EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 100 FOR EMERGENCY L IGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008050700016 20080507 00016 NM 2008 5 7 AALA200800854 1 20080407 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEF T NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050700017 20080507 00017 NM 2008 5 7 ZZDA2008095 1 20080424 A 2720 CONTROL QUADRANT BOEING 717 717200 1383700 NM COCKPIT BROKEN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 943AT 55006 CAPTAIN'S FOOT PEDAL ADJUSTMENT BROKE LOOSE AND PEDALS NOT AT FULL EXTENSION WITH NO ADJUSTMENT BACK AVAILABLE. REMOVED & REPLACED RUDDER PEDAL ADJUSTMENT QUADRANT ASSEMBLY. CHECKS GOOD IAW MM 27-21. 2 L 7 2 4F TR A6WE 2008050700019 20080507 00019 NM 2008 5 7 DHL2008760547 1 20080416 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272B7 138407L NM BS 690-740 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED CORRODED SEAT TRACK, FABRICATED, AND INSTALLED SEAT TRACK SECTION AT BS 690 TO 740, RBL 24, PER SRM 53-10-2 FIG 7 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 2008050700020 20080507 00020 NM 2008 5 7 DHL2008760550 1 20080421 A 5311 FRAME BOEING 727 7272B7 138407L NM BS 700 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND INSTALLED NEW SHEAR TIE REPAIR AT BS 700, BETWEEN STR 27R AND 28R PER B727 SRM 53-10-4 FIG 13 A ND 53-10-2 FIG 3. 2 L 7 3 4F A3WE 2008050700027 20080507 00027 NM 2008 5 7 AALA200800791 1 20080402 A 3350 02021804001 LIGHT BOEING 777 777223 1385213 NM GALLEY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 JFK - EMERGENCY LIGHT AT FORWARD GALLEY INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD GALLEY. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050700030 20080507 00030 NM 2008 5 7 AALA200800799 1 20080402 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 187AN 32381 DFW - EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008050700032 20080507 00032 2008 5 7 COMA0860233 4 20080427 A 3418 3995100208 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING FAILED A COMA O OTHER N FALSE WARNING LD LANDING 1 SO 01 595SW 22115 7292 FLIGHT 5624 - EN ROUTE TO CVG RECEIVED STALL FAIL CAUTION MESSAGE. FOLLOWED QRH, EMERGENCY DECLARED, AIRCRAFT LANDED SA FELY IN CVG. REMOVED AND REPLACED STALL PROTECTION COMPUTER. 2 L 7 2 4F RT A21EA 2008050700034 20080507 00034 SO 2008 5 7 C2XA08RI055 1 20080419 A 2612 M8373110271 SWITCH EMB 145 EMB145XR 3260214 SO FIRE DETECTION INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 16149 145753 FLIGHT 2053 - EWR - FLIGHT CREW REPORTED BAG FIRE DETECTION LIGHT INOPERATIVE. EWR MX REMOVED AND REPLACED TEST SWITCH AND RELAY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2008050700039 20080507 00039 WP 2008 5 7 08FDEA01714 1 20080501 A 5347 601096418 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 309FE 48298 MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREA AT F/S 1401-1421 LBL48 REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 1. SE AT TRACK FABRICATED ON MAE TRAVELER T8/737382. SPLICE HAT AND PLATE FABRICATED ON MAE TRAVELER T8/737383. MAIN CARGO COMPARTMENT LBL 48 STA 1401-1421, MAJOR REPAIR. 2 L 7 3 4F RT A22WE 2008050700054 20080507 00054 EA 2008 5 7 A6WA200840316 1 20080410 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 575 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 CARGO BAY FLOOR SILL CRACKED AT FS 575. (M) REPAIR PERFORMED ON CARGO DOOR SURROUND LOWER SILL AT FS 575 IAW REO 601R- 53-61-1741. (A) 2 L 7 2 4F RT A21EA 2008050700055 20080507 00055 EA 2008 5 7 A6WA200840350 1 20080418 A 2731 TRIM SYSTEM CNDAIR CL600 CL6002B19 1900309 EA STAB MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 31 418AW 7618 STAB TRIM ACTIVATED NOSE UP AFTER TAKEOFF WITHOUT PILOT INPUT TRIMMING NOSE DOWN STOPPED UNCOMMENDED TRIM. CHECKED PILO T AND COPILOTS STAB TRIM SWITCHES FOR BINDING FREE MOVEMENT. FOUND PILOT AND COPILOT TRIM SWITCHES TO OPERATE NORMALLY. NO BINDING NOTED. SWITCHES NOT STICKING AT THIS TIME IAW AMM 27-40-00. CHECKED FOR MOISTURE CONTAMINATION ON HSTCU. FOUND NO MOISTURE CONTAMINATION. FUNCTIONAL CHECK OF THE HSTCU. OPS CHECK GOOD IAW 27-41-00. R&R HSTCU. OPS CHECK G OOD. 2 L 7 2 4F RT A21EA 2008050700056 20080507 00056 EA 2008 5 7 A6WA200840339 1 20080416 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 443AW 7781 CRACK FOUND AT FS 484 LBL 36 WL 72. (M) INTERCOSTAL REPAIRED AT FS 484, LBL 36, WL 72 IAW REO 601R-53-41-059 REV A. 2 L 7 2 4F RT A21EA 2008050700059 20080507 00059 EU 2008 5 7 CPCP20080024 1 20080404 A 5753 RETAINER AEROSP ATR72 ATR72212 8680945 EU RT WING TE FLAP CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 348AE 349 RT OUTB FLAP RIB 19 BRUSH RETAINER IS CORRODED. RT OUTB FLAP RIB 19 BRUSH RETAINER REPLACED IAW SRM 51-25-03. 2 H 7 2 4T RT A53EU 2008050700064 20080507 00064 WP 2008 5 7 UPS08852089 1 20080416 A 5347 3657502U507 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 STOP HOLES WORN, ROUNDED ON PILOTS LOWER SEAT TRACKS. REMOVED AND REPLACED LOWER SEAT TRACKS IAW SRM 51-3-1, 51-1-20D, 51-1- 24, 51-1-8. 2 L 7 4 4F RT 4A25 2008050700066 20080507 00066 WP 2008 5 7 UPS08852091 1 20080408 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1690-1776 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 LT AFT EXTERIOR FUSELAGE STA 1766, LONG 28L, FUSE SKIN SEAM BULGING. REMOVED CORRODED LONGERON 28L, CLEANED AREA. REMOVED AND REPLACED INTERNAL DOUBLER AND REPLACED L28L SECTION 1690-1766 IAW SRM 51-1-8, 51-1-21, 53-2-0 FIG 1F, 51-1-20D53-5-3. 2 L 7 4 4F RT 4A25 2008050700071 20080507 00071 NM 2008 5 7 ABXA080141 1 20080428 A 3350 BATTERY PACK BOEING 767 767231 1385131 NM CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 708AX 22571 ON PRE-DEPARTURE CHECK AT STA SAN, FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED WITH SPARE BATTERY PACK IAW B767 MM 33-51-07-02. 2 L 7 2 4F RT A1NM 2008050700072 20080507 00072 WP 2008 5 7 UPS08852097 1 20080408 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1766 L28L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 LT AFT EXTERIOR FUSELAGE STA 1766 L28L FUSELAGE SKIN SEAM BULGING. REMOVED LONGERON, FABBED LONGERON AND INTERNAL DOUBLER, INSTALLED LONGERON AND INTERNAL DOUBLER IAW DC8 SRM 51-1-21, 51-1-20D 53-05-03, AND 51-1-8. 2 L 7 4 4F RT 4A25 2008050700057 20080507 00057 WP 2008 5 7 IXXA08SMN101S 1 20080314 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAP MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD FLAP LOWER PANEL SKIN HAS IMPROPER REPAIR AT STATION XW 18.0 00. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPA IR PARTS IAW DC8 SRM 51-1-11, 51-1-21, DC8 SRM 57-7-1 FIGURE 1 ITEM "B" AND "L", DC8 SRM 57-1-0 PAGE 1, 51-1-21, DC8 SRM 51-1-9 TR NUMBER 51-142, 51-1-9A TR NUMBER 51-141, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008050700068 20080507 00068 WP 2008 5 7 UPS08852093 1 20080416 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 COCKPIT FLOOR PANEL 676D HAS ONE CORNER CRACKED AND ONE CORNER BROKEN OUT. FABBED AND INSTALLED REPA IR DOUBLERS IAW SRM 53-2-0 FIG1 B, 53-7-3, 5 1-1-8, 53-7-3 FIG1 A, 51-1-15. 2 L 7 4 4F RT 4A25 2008050700070 20080507 00070 NM 2008 5 7 YENA2008039 1 20080429 A 2751 WARNING SYSTEM EMB ERJ190 ERJ190100IGW 3260408 NM COCKPIT ACTIVATED A YENA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 EA 15 258JB 19000047 FLT 1295, BOS-PIT, HAD FLAP FAIL EICAS MESSAGE WHEN SELECTION FLAPS 1 DURING APPROACH INTO KPIT, RAN QRH WOULD NOT RESET HAD TO LAND FLAPS/SLATS 0, SLATS WORKED NORMALLY. RESET SYSTEM PER FIM 27-51-00-810-802-A00 FAULT CODES 275312014ACE, 27534007ACE, 27532018ACE CLEARED AT THIS TIME PER FIM, IS A TRANSITORY CONDITION, RAN SYSTEM TEST PER MM 27-53-02, OPS C HECK NORMAL AT THIS TIME. 2 L 7 2 4F RT A57NM 2008050700085 20080507 00085 WP 2008 5 7 IXXA08SMN122S 1 20080410 A 5347 S2772660 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 685 WORN B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK WITH LUGS WORN AT STATION 685.000. REMOV ED EXISTING SPLICES (FWD SIDE) AND REMOVED SEGMENT OF DAMAGED TRACK AFT SIDE. FABRICATED SPLICES. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED SEGMENT OF NEW TRACK AND REPAIR PARTS AND REINSTALLED EXISTING SPLICES IAW DC 8 SRM 53-2-3 FIGURE 14 PAGES 49-50, 51-3-0, DC8 SRM 51-1-8B, 53-7-3 FIGURE 3E SHEET 1, 2, 51-2-0 FIGURE 50 SHEET 73, 51- 3-0, AND 51-3-1. 2 L 7 4 4F RT 4A25 2008050700088 20080507 00088 NM 2008 5 7 USAA920080959 1 20080409 A 5320 656731197 CHANNEL BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON CABIN FLOOR HAT CHANNEL, BS 993.5, LBL 14, WL 208. REPLACED CABIN FLOOR H AT CHANNEL, BS 993.5, LBL 14, WL 208 IAW B737 SRM 53-60-51-1A1. 2 L 7 2 4F RT A16WE 2008050700095 20080507 00095 NM 2008 5 7 08FDEA01752 1 20080505 A 5210 FRAME BOEING 757 75727B 1384921 NM L2 DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 CORROSION ON L2 DOOR AFT FRAME WEB SURFACE BELOW HANDLE. TO REMOVE CORROSION AS PER SRM. REPAIR ON L2 DOOR AFT FRAME W EB SURFACE BELOW HANDLE WAS CARRIED OUT AS PER FEDEX EA NR F-5210-117342. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 CR ITERIA. 2 L 7 2 4F RT A2NM 2008050700115 20080507 00115 NM 2008 5 7 CALA0800397 1 20080430 A 5310 6520723U54 DOOR FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 AFT FRAME AT FWD CARGO DOOR CUTOUT IS CRACKED AT LOWER DOOR STOP. REMOVED AND REPLACED AFT FRAME AT FWD CARGO DOOR CUTO UT PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008050700151 20080507 00151 EA 2008 5 7 COMA0880006 1 20080430 A 2720 DL2428M9MOD1 LIMITER CNDAIR CL600 CL6002D24 1390016 EA RUDDER FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 692CA 1233 15092 FLIGHT 5211 - RECEIVED RUDDER LIMITER CAUTION MESSAGE IN FLIGHT. RUDDER FAILED AT FULL THROW. DECLARED EMERGENCY, RETU RNED TO CVG, LANDED WITHOUT INCIDENT. REPLACED RT RUDDER LIMITER. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 2008050700161 20080507 00161 EA 2008 5 7 A6WA200840334 1 20080412 A 3260 TARGET CNDAIR CL600 CL6002B19 1900309 EA MLG LOOSE A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 410AW 7490 ON DEPARTURE, AFTER LANDING GEAR RETRACTION RECEIVED GEAR DISAGREE MASTER WARNING RT MAIN GEAR C/W QRH DIVERTED IAD GEAR INDICATED 3 GREEN. FOUND RT MLG UPLOCK TARGET LOOSE. RETORQUED AND PERFORMED GEAR SWINGS PER AMM 32-30-00. REMOVED F ROM MEL. 2 L 7 2 4F RT A21EA 2008050700164 20080507 00164 EA 2008 5 7 SWIA200819541 1 20080423 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA MLG MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 724SK 10189 RECEIVED A GEAR DISAGREE MESSAGE ON EICAS AFTER TAKEOFF, FLT 5870. ADJUSTED NOSE WHEEL WELL PROXIMITY SENSOR PER AMM 32 -61-05 AND AMM 32-30-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008050700178 20080507 00178 SO 2008 5 7 SIMA200812102 1 20080425 A 5320 AL2024T3 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 827AE 5000 145602 DURING A MBV INSPECTION, A PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. PREPARED A DOUBLER AND FILLER. CLEANED AND TREATED REPAIR PARTS. REPAIR DONE IAW EMBRAER 145 SRM (SRM 145/1142 REV 39) CHAPTERS 53-00-10, FIGURE 206. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008050700193 20080507 00193 NM 2008 5 7 USAA920080982 1 20080419 A 5320 141N517040 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - LEVEL 2 CORROSION ON MAIN DECK FLOOR SUPPORT, BS 349 - BS 354, LBL 55. REPLACED MAIN D ECK FLOOR SUPPORT, BS 349 - BS 354, LBL 55 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008050700203 20080507 00203 EA 2008 5 7 TRAX200800584 1 20080428 A 2560 INDICATOR CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 871AS 7537 PHOTOLUMINESCENT AISLE PATH MARKERS MISSING END INDICATOR DOTS. 2 L 7 2 4F RT A21EA 2008050700221 20080507 00221 NM 2008 5 7 DHL2008760533 1 20080406 A 5322 SHEAR TIE BOEING 727 7272B7 138407L NM BS 720C S28L/R CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND REPLACED FRAME SHEAR TIE AT BS 720C, BETWEEN STR 28L AND 28R, PER B727 SRM 53-10-2 FIG 3 AND 53 -10-4 FIG 15. 2 L 7 3 4F A3WE 2008050700283 20080507 00283 EA 2008 5 7 TRAX200800590 1 20080428 A 5240 KNOB CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR OUT OF POSITION A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 SERVICE DOOR KNOB CAME OFF. SECURED SERVICE DOOR KNOB. OK FOR SERVICE. SDR CLOSED. 2 L 7 2 4F RT A21EA 2008050700292 20080507 00292 NM 2008 5 7 2008UALA02438 1 20080426 A 2121 6456701 FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT FAILED A UALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 567UA 26673 EMERGENCY DESCENT DUE TO LEFT PACK FAILURE. FLIGHT DIVERTED. FOUND EQUIPMENT COOLING VALVE STUCK IN OPEN POSITION-FAIL ING HULL CHECK. REPLACED EQ COOLING VALVE, ALSO REPLACED POSITIVE PRESSURE RELIEF AND OUTFLOW VALVE ACTUATOR AS PRECUAT IONARY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008050700294 20080507 00294 EU 2008 5 7 2008UALA02439 1 20080425 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 448UA 842 L2 DOOR SILL HAS CORROSION FWD OF FR68. MAJOR REPAIR, CORROSION OUT OF LIMITS. REPAIRED PER SRM 53-41-14 NR 4. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050700308 20080507 00308 EA 2008 5 7 SWIA200819587 1 20080214 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 438SW 7574 UPPER FLOOR ANGLE AT FS280 AND RBL9.0 IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS ON UPPER FLOOR ANGLE PER CRJ 200 REO 601R-53-11-137. 2 L 7 2 4F RT A21EA 2008050700334 20080507 00334 EU 2008 5 7 2008UALA02445 1 20080426 A 3150 3945128102 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELAC 1 FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 401UA 435 ELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. REPLACED ELAC 1, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050700345 20080507 00345 NM 2008 5 7 DHL2008760543 1 20080423 A 5320 WEB BOEING 727 7272B7 138407L NM BS 367-374 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND INSTALLED WEB SECTION IN CABIN AT BS 367 TO 374, STR 17R, RBL 65, PER B727 SRM 53-10-2 FIG 1, 5 1-20-1, AND 51-30-2. 2 L 7 3 4F A3WE 2008050700349 20080507 00349 SO 2008 5 7 C2XA08SH071 1 20080503 A 5240 14590016013 HINGE EMB 145 EMB145XR 3260214 SO SERVICE DOOR MIGRATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13133 145712 SHV - DURING C-CHECK SERVICE DOOR MAIN HINGE MECH HAS MIGRATED HAT BUSHING AT HINGE TO DOOR ATTACH POINT. MX REPAIRED S ERVICE DOOR MAIN HINGE IAW EC5240-01036. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008050700351 20080507 00351 NM 2008 5 7 ASAA0852871 1 20080501 A 2160 3989083 CONTROL VALVE BOEING 737 737890 1384527 NM CABIN TEMP MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 585AS 2621 35683 FWD CABIN ZONE TEMP ILLUMINATED. UNABLE TRIP RESET. VERIFIED DISCREPANCY RESET FAULT. GROUND VERIFICATION PASSED. 2 L 7 2 4F RT A16WE 2008050700353 20080507 00353 NM 2008 5 7 SWAA082391 1 20080502 A 5320 6545402 STIFFENER BOEING 737 7373H4 1384600 NM LT MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED SPV CHECK, FOUND LEFT MLG W/W FWD BULKHEAD STIFFENER CRACKED AT BS 663.75, LBL 6.15. REPAIRED STIFFENE R PER SWA EA. 2 L 7 2 4F RT A16WE 2008050700357 20080507 00357 2008 5 7 SWAA082412 4 20080501 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008050700359 20080507 00359 NM 2008 5 7 SWAA082413 1 20080501 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 772, STR 14R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008050700360 20080507 00360 NM 2008 5 7 SWAA082414 1 20080501 A 5752 69600814 ROD END BOEING 737 7373H4 1384600 NM LT AILERON LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED HC2 CHECK, FOUND LT WING AILERON TAB INBOARD HINGE LOOSE. REMOVED AND REPLACED BUSHING AND ROD END PER MM. 2 L 7 2 4F RT A16WE 2008050700363 20080507 00363 NM 2008 5 7 SWAA082428 1 20080504 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED DAL CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008050700366 20080507 00366 NM 2008 5 7 SWAA082394 1 20080502 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008050700369 20080507 00369 NM 2008 5 7 SWAA082415 1 20080501 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 21R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008050700387 20080507 00387 NM 2008 5 7 SWAA082383 1 20080501 A 2730 6545187 TORQUE TUBE BOEING 737 7375H4 138449D NM RT ELEVATOR FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, RIGHT ELEVATOR FAILS FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR OUTPUT TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 2008050700394 20080507 00394 NM 2008 5 7 SWAA082388 1 20080504 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, RBL 7 TO RBL 14. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008050800004 20080508 00004 EA 2008 5 8 A6WA200840295 1 20080331 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 202 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 CRACK FOUND ON PRESSURE BULKHEAD FSW 202.75, LBL 23.71, AROUND PARKING BRAKE. (K) REPAIR ON FWD PRESSURE BULKHEAD IAW REO 601R-53-11-563. 2 L 7 2 4F 4 F RT A21EA E15NE 2008050800006 20080508 00006 EA 2008 5 8 A6WA200840297 1 20080404 A 5320 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 589-605 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 CARGO DOOR FITTING ATTACHMENT FS 589 AND FS 605 CORRODED. (K) CORROSION REMOVED ON CARGO DOOR FITTING ATTCHMENT AT FS 589 AND 605 IAW SRM 51-21-06 . (A) 2 L 7 2 4F 4 F RT A21EA E15NE 2008050800019 20080508 00019 NM 2008 5 8 DXTA200802966 1 20080327 A 2750 1250A000002 FSEU GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE T/E FLAP INOPERATIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 708QS 524 069 LEAVING, AFTER GEAR RETRACTION, SELECTED FLAPS TOP 0 DEG AND FLAPS WOULD NOT RETRACT FROM 20 DEG. REMOVED ORIGINAL FSEC U AND INSTALLED INSPECTED UNIT. PERFORMED SATISFACTORY RIG AND OPS CHECK OF FLAP SLAT SYSTEM. FOR ALL WORK REF MM 27-51- 00, 27-50-05 AND 27-51-45. 2 L 7 2 4F 4 F RT A53NM E35NE 2008050800022 20080508 00022 CE 2008 5 8 DXTA200802971 1 20080330 A 2170 7464513 COALESCER BAG CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL A/C BAY DIRTY E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 921QS 3050 7500241 CABIN ALTITUDE SPIKED TO 4000 FT/MIN CLIMB DURING GEAR RETRACTION. SHORTLY THERE AFTER SMOKE ENTERED THE CABIN THEN DIS SIPATED. REPLACED BOTH COALESCER SOCKS IAW MM 12-10-01. ACCOMPLISHED MANUAL CONTROL VALVE PLUMBING LEAK TEST, LT AND R T CABIN PRESSURE CONTROL SYSTEM STATIC LEAK TEST AND ELECTROPNEUMATIC TRANSFER VALVE PLUMBING LEAK TEST IAW MM 21-30-00. ALL TESTS AND LEAK CHECKS ARE GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008050800029 20080508 00029 EU 2008 5 8 04222008 1 20080422 A 6720 11722118434 SUPPORT BRACKET BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE TAIL ROTOR LOOSE E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 527MB 12153 1800 7103 DURING SCHEDULED INSPECTION, A TAIL ROTOR CONTROL TUBE SUPPORT MOUNT WAS FOUND LOOSE INSIDE THE TAILCONE DUE TO WORKING RIVETS. 1 G 7 2 3U 3 U H13EU E5NE 2008050800030 20080508 00030 EU 2008 5 8 BAQA20080003 1 20080419 A 2150 S8990132 O-RING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE A/C BAY DAMAGED E BAQA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 03 118NC 7067 CRUISE FLIGHT, CLOSE TO FLIGHT DESTINATION, CREW SMELLED "STRANGE ODOR" IN CABIN/COCKPIT. PILOT TURNED OFF THE ENVIRONM ENTAL CONTROL UNIT AND SMELL CEASED. INSPECTION OF ECU REVEALED THAT THE "INDUCTOR" PIPE TEMPERATURE CONTROLLER TO COOL ING TURBINE HAD A SMALL SPLIT AT THE TURBINE AND PIECES OF THE SEALING O-RING (PACKING) WAS EXPOSED AND MISSING. 1 G 7 2 3U 3 U H13EU E5NE 2008050800045 20080508 00045 WP 2008 5 8 UPS08852161 1 20080413 A 5310 3755827U501 FITTING DOUG DC8 DC873F 302199F WP BS 270 L32R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 A-PIT RT STA 270 L32R, INSIDE A-PIT DOOR FWD TORQUE BOX IS CORRODED ON THE FITTING, AND AROUND FASTE NERS. REMOVED CORRODED FITTING, FABBED AND INSTALLED REPAIR FITTING IAW SRM 51-1-8, 51-1-20D, 53-2-00 FIG 1F. 2 L 7 4 4F RT 4A25 2008050800048 20080508 00048 NM 2008 5 8 08FDEA01768 1 20080506 A 5311 AFA00203 FRAME DOUG MD11 MD11F 3023600 NM BS 1701 L12L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 528FE 48623 AFT CABIN AT APPROXIMATELY STATION 1701 LEFT SIDE LONGERON 12 FOUND FRAME DENTED. REPAIRED PER SRM 53-30-00 FIG 1, VOL I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIG.1 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008050800050 20080508 00050 NM 2008 5 8 HALA0800556 1 20080502 A 2530 8102020000C01 OVEN BOEING 767 7673G5 1385126 NM GALLEY FIRE A HALA O OTHER A FLAME/FIRE CL CLIMB 1 WP 13 585HA 24257 FA REPORTED FIRE AROUND OVENS NR 1 AND NR 2 FWD GALLEY. REMOVED AND REPLACED OVENS NR 1 AND NR 2 IN FWD GALLEY VISUALLY INSP GALLEY CAVITIES OF FWD GALLEY FOR NR 1 AND NR 2 OVEN. NO RESIDUAL OF SMOKE NOTED. OPS CK OK IAW TR767 AMM 25-001 . 2 L 7 2 4F RT A1NM 2008050800074 20080508 00074 WP 2008 5 8 UPS08852125 1 20080415 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 FUSELAGE EXTERIOR SKIN, 8 INCH GOUGE IN SKIN STA -15 TO -20 L18L. CUT OUT DAMAGE, FABBED AND INSTALL ED DOUBLER AND FILLER IAW SRM 53-2- 0 FIG 1F, 53-2-1 FIG 7, 51-1-8, 51-1-20D53-2-1. 2 L 7 4 4F RT 4A25 2008050800079 20080508 00079 NM 2008 5 8 2008UALA02568 1 20080501 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1400 S25L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 AFT PIT STA 1400 STR 25L HAS ELONGATED HOLES IN SIDES OF STRINGER DUE TO REPLACEMENT STRINGER CLIPS ON FRAME REPAIR. MA JOR REPAIR ACCOMPLISHED, CUTOUT DAMAGE. INSTALLED FILLER AND 2 REPAIR SPLICES. 2 L 7 2 4F 4 F RT A2NM E17NE 2008050800080 20080508 00080 CE 2008 5 8 GUUA04210801 1 20080421 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA CABIN ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 81536 UE152 FLIGHT 9174, DURING FLIGHT, STRONG SMELL OF FUEL. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT. INSPECTED AC FUEL S YS, LT AND RT WING FUEL PANELS, LT AND RT ENGINE FOR LEAKS, NO LEAKS NOTED. PERFORMED ENGINE RUN FOR(15) MINUTES WITH B LEEDS ON AND OFF, NO STRONG FUEL SMELL NOTED. 2 L 7 2 4T 3 T RT A24CE E2NE 2008050800086 20080508 00086 CE 2008 5 8 GUUA04220801 1 20080422 A 3297 CONNECTOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA SQUAT SWITCH LOOSE A GUUA O OTHER O OTHER TO TAKEOFF 1 SO 29 69547 UE189 FLIGHT 9271, AFTER TAKEOFF, LANDING GEAR CONTROL HANDLE WOULD NOT RETRACT. RETURNED TO DEPARTURE. LANDED WITHOUT INCI DENT. RESECURED CONNECTOR ON RT MLG SQUAT SWITCH. 2 L 7 2 4T 3 T RT A24CE E2NE 2008050800095 20080508 00095 EA 2008 5 8 CIEA200800002 1 20080415 A 3234 555402 SELECTOR VALVE CNDAIR CL600 CL600* 1900302 EA LYC ALF502 ALF502* 41580 EA NLG FAILED E CIEA O OTHER O OTHER DE DESCENT 1 NM 03 643CR 8843 1055 DURING FINAL APPROACH THE FLIGHT CREW LOWERED THE LANDING GEAR AND THE NOSE GEAR DOORS OPENED BUT THE LANDING GEAR DID N OT EXTEND. THE CREW MANUALLY LOWERED THE NOSE GEAR USING THE EMERGENCY GEAR EXTENSION SYS AND THE SYS WORKED NORMAL. U PON LANDING MAINT INSPECTED THE GEAR AND DETERMINED THAT THE NOSE LANDING GEAR SELECTOR VALVE AND FAILED BY ALLOWING HYD FLUID TO ENTER THE ELECTRICAL CONTROLLING PART OF THE VALVE. THE PN AND SN WERE UNREADABLE UPON REMOVAL OF THE VALVE. A REVIEW OF THE CAMP CARDS PRODUCED THE VALVE INFORMATION. 2 L 7 2 4F 4 F RT A21EA E6NE 2008050700074 20080507 00074 WP 2008 5 7 UPS08852109 1 20080414 A 5320 4773295U2 FITTING DOUG DC8 DC873F 302199F WP CARGO DOOR FRAME CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 BACK UP FITTING CORRODED AT MCD JAMB NR 3 SPOOL REMOVED AND REPLACED FITTING IAW SRM 51-3-0, 51-3-2, 51-1-21A. 2 L 7 4 4F RT 4A25 2008050700079 20080507 00079 NM 2008 5 7 USAA920080950 1 20080426 A 5330 6545774 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 591US 23936 CLT - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 727E, S24L. REPAIRED FUSELAGE SKIN, BS 727E, S24L IAW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008050700081 20080507 00081 NM 2008 5 7 AALA200800861 1 20080408 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 696AN 26976 MIA - EMERGENCY LIGHT AT SEAT ROW 26 INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 26. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008050700086 20080507 00086 WP 2008 5 7 IXXA08SMN102S 1 20080314 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 55 L7L CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 55.000 LONGERON 7LEFT. REMOV ED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND AFTER INSPECTION. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATION NUMBER 2003-05, DPS 4.707, DC8 SRM 51-1-8B, AND 51-3-1. 2 L 7 4 4F RT 4A25 2008050700087 20080507 00087 EU 2008 5 7 USAA920080958 1 20080429 A 5347 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 272AY 333 BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 5584 / FR 72 - BS 5367 / FR 73, -Y450. REPLACED CABIN SEAT TRACK, BS 5584 / FR 72 - BS 5367 / FR 73, -Y450 IAW A330 SRM 51-42-00. 2 L 7 2 4F RT A46NM 2008050700090 20080507 00090 NM 2008 5 7 USAA920080963 1 20080425 A 5320 6546812186 BEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON CABIN BEAM, BS 986.5, LBL 4 - RBL 17, WL 208. REPAIRED CABIN BEAM, BS 986 .5, LBL 4 - RBL 17, WL 208 IAW USAIRWAYS EA 130005. 2 L 7 2 4F RT A16WE 2008050700099 20080507 00099 NM 2008 5 7 USAA920080969 1 20080429 A 5320 655486215 INTERCOSTAL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CRACKED INTERCOSTAL, BS 1016, LBL 44, WL 208. REPLACED INTERCOSTAL, BS 1016, LBL 44, W L 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008050700100 20080507 00100 NM 2008 5 7 AALA200800855 1 20080407 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050700104 20080507 00104 NM 2008 5 7 USAA920080970 1 20080409 A 5311 654795944 FRAME BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON FRAME, BS 800, S25R. REPLACED FRAME, BS 800, S25R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008050700108 20080507 00108 2008 5 7 BB08072 4 20080427 A 2565 D30655123 SLIDE BOEING 757 7572S7 1384962 NM R2 DOOR LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 904AW 4187 3396 23566 PHX - THE R2 DOOR EMERGENCY ESCAPE SLIDE PRESSURE WAS FOUND TO BE IN THE RED. MAINTENANCE REPLACED THE R2 DOOR EMERGENC Y ESCAPE SLIDE. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2008050700110 20080507 00110 SO 2008 5 7 C2XA08IA119 1 20080428 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 14116 145672 IAH - FLIGHT 2096, THE CREW REPORTED A NOTICEABLE SCENT PF JET FUEL WHEN THRUST LEVERS ADVANCED FOR T/O WITH THE PACKS O N, APU BLEED OPEN, AND ENGINE BLEEDS OFF. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE OPERATIONALLY C HECKED THE APU & BLEED SYSTEMS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008050700111 20080507 00111 SO 2008 5 7 C2XA08IA120 1 20080423 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12530 145533 IAH - DURING A-CHECK INSPECTION THE AISLE PATH LIGHTING BETWEEN ROWS 7 & 9 AND EMERGENCY EXIT ROW WERE FOUND TO BE INOPE RATIVE. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE AFFECTED LIGHTS WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008050700113 20080507 00113 NM 2008 5 7 CALA0800396 1 20080430 A 3350 767 LIGHT BOEING 757 757324 1384930 NM EXTERIOR INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 57852 32811 EXTERIOR EMERGENCY LIGHTS INOP AT DOORS 2L AND 2R. REMOVED AND REPLACED BULBS, OPS CHECK GOOD. REF MM 33-51-00. 2 L 7 2 4F RT A2NM 2008050700116 20080507 00116 NM 2008 5 7 QXEA200800434 1 20080426 A 2434 400SG163Q2 GENERATOR BOMBDR DHC8 DHC8402 1390042 NM NR 1 FAILED A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 401QX 11754 52 4031 STS - AFTER ENGINE START, RECEIVED A NR 1 DC GENERATOR HOT CAUTION LIGHT. MAINTENANCE REPLACED THE NR 1 ENGINE STARTER GENERATOR OIL SEAL AND THE DC STARTER GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008050700118 20080507 00118 NM 2008 5 7 QXEA200800435 1 20080430 A 2434 400SG163Q GENERATOR BOMBDR DHC8 DHC8402 1390042 NM NR 2 DC FAILED A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 09 432QX 10075 928 4166 SEA - FLIGHT 2280 - RECEIVED A DC BUS CAUTION ALONG WITH MESSAGES FOR THE NR 2 DC GENERATOR, MAIN BATTERY, ANTI-SKID, AN D RUDDER CONTROL LIGHT WAS ABLE TO RESET BUS PER THE CHECKLIST. MAINTENANCE TRIED TO PERFORM A GROUND RUN TO CONFIRM BU T FOUND THAT THE NR 2 ENGINE WOULD NOT ROTATE OR LIGHT OFF. REPLACED THE NR 2 DC STARTER GENERATOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008050800098 20080508 00098 CE 2008 5 8 DXTA200803016 1 20080424 A 2701 YOKE BEECH MU300 400A 1155402 CE COCKPIT LOCKED E DXTA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 07 153QS RK490 IN FLIGHT W/SPOILERS DEPLOYED, AC PITCHED FWD, YOKE LOCKED UP AND ROLL AUTHORITY WAS LOST UNTIL SPOILERS WERE STOWED. I NSPECTED SPOILERS AND SPOILER CABLES, NO DEFECTS NOTED. DEPLOYED SPOILERS WITH HYDRAULIC POWER AND CHECKED YOKE FOR FREE DOM OF MOVEMENT, CHECKS GOOD. INSPECTED PITCH TRIM AND ROLL BOTH OPERATE NORMALY. ALL WORK IAW MM 27-60-00, 27-10-00. 2 H 7 2 4F RT A16SW 2008050800105 20080508 00105 CE 2008 5 8 DXTA200803021 1 20080424 A 2170 COALESCER BAG CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN AIR ODOR E DXTA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 983QS 7500083 DURING CRUISE, AC HAS A SMELL OF DIRTY SOCKS. REMOVED AND CLEANED AND INSTALLED WATER SOCKS IAW CE750 MM CHAPTER 12-10-0 1-160. REMOVED CLEANED AND INSTALLED OZONE CONVERTER IAW CE 750 MM CHAPTER 12-10-01-161. OPERATIONAL AND LEAK CHECK GOOD . 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008050800113 20080508 00113 GL 2008 5 8 HEEA119526 2 20080424 A 7200 02920005250 ENGINE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL FAILED B HEEA K NONE O OTHER TO TAKEOFF 1 SW 03 5435V 13698 760158 ONE SECOND INTO TAKEOFF, AFTER DP AND ROTATION, NR1 ENGINE FAILED. LOUD NOISE, CHIP LIGHT AND DECEL. FLEW TO AIRPORT A ND LANDED. 1 G 7 2 3U 3 U H1NE E1GL 2008050800115 20080508 00115 NM 2008 5 8 HALA0800554 1 20080428 A 5100 UNKNOWN BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE UNKNOWN A HALA K NONE O OTHER CR CRUISE 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, LEFT THROTTLE MUST BE ADVANCED ONE INCH FURTHER THAN LEFT TO SYNCHRONIZE ENGINES IN CRUSE. PE RFORMED FIM 71-PIMIJ NO MSG FOUND LOOKED FOR ANY AUTO EVENTS NONE FOUND AND NO EICAS MSG. RAN BOTH ENG AT 80 PERCENT. NO THROTTLE SPLIT AND ENG IND NORMAL PERFORMED FIM 73-21-00. NO FAULTS FOUND, ALSO PERFORMED FIM 76-11-00 THROTTLE LEVE RS CHECK, ALL CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2008050700320 20080507 00320 NM 2008 5 7 GTIA0800057 1 20080408 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 504NK 2473 FLOORBEAM CORRODED AT Y765 FRAME 64- 66.5. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2008050700321 20080507 00321 SO 2008 5 7 C2XA08ON122 1 20080501 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO CABIN MALFUNCTIONED A C2XA D RETURN TO BLOCK N FALSE WARNING CL CLIMB 1 SW 27 11187 7501 7501 14500927 FLT 970 - ONT - FLIGHT CREW REPORTED LAV SMOKE DETECTOR AFTER T/O AND SHORT AFTER GALLEY SMOKE INDICATION ON EICAS. MX PERSONNEL REMOVED AND REPLACED GALLEY AND LAV SMOKE DETECTORS OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008050700328 20080507 00328 WP 2008 5 7 IXXA08SMN120S 1 20080327 A 5743 FITTING DOUG DC8 DC873F 302199F WP ZONE 700 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND RT MAIN LANDING GEAR WHEEL WELL FORWARD UPPER PART FITTING CRACKED AT STATION 8 57.125 AND STATION XCW 23.000. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK F OUND. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATI ON NUMBER 2003-05, DOUGLAS DRAWING 3646326, DPS 4.707, DC8 SRM 51-1-8B, AND 51-3-1. 2 L 7 4 4F RT 4A25 2008050700340 20080507 00340 EA 2008 5 7 SWIA200819551 1 20080208 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 760SK 10223 STA 280 BEAM IS CRACKED AT RIGHT BUTT LINE 9, FOUND AT C-CHECK. REPAIRED AREA PER CRJ700 SRM TASK 51-42-21-001-001-A01 AND REO 670-53-11-047. 2 L 7 2 4F RT A21EA 2008050700355 20080507 00355 NM 2008 5 7 SWAA082393 1 20080503 A 5753 6546435278 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP P ER MM. 2 L 7 2 4F RT A16WE 2008050700362 20080507 00362 NM 2008 5 7 SWAA082429 1 20080504 A 5315 6545410144 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED DAL CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 707, RBL 24.82. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2008050700393 20080507 00393 NM 2008 5 7 SWAA082389 1 20080504 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008050800021 20080508 00021 NM 2008 5 8 DXTA200802970 1 20080330 A 2780 SLAT GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE WING MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 707QS 066 ON DEPARTURE, GOT FLAP/SLAT MAINT MESSAGE. SLATS DID NOT COME ALL THE WAY UP. PERFORMED FUNCTIONAL TEST OF THE FLAP/SL AT CONTROL AND DRIVE SYS WITH NO DEFECTS NOTED AT THIS TIME. ALL WORK COMPLETED IAW CMP 275101. 2 L 7 2 4F 4 F RT A53NM E35NE 2008050800083 20080508 00083 NM 2008 5 8 08FDEA01769 1 20080506 A 5311 AFA00283 FRAME DOUG MD11 MD11F 3023600 NM BS 1681 L12L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 528FE 48623 AFT CABIN AT APPROXIMATELY STATION 1681 LEFT SIDE LONGERON 12 FOUND FRAME DENTED. REPAIRED AS PER SRM 53-30-00 FIG.1,VO L.I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00,FIG.1, VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008050800084 20080508 00084 EU 2008 5 8 08FDEA01770 1 20080506 A 5347 A53274788204 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 673FE 780 MAIN CARGO DECK SEAT TRACK NR 1 HAS 9 AREAS OF CORROSION BETWEEN FR 68 AND FR 76. REMOVED LEVEL 1 CORROSION ON MAIN CAR GO DECK SEAT TRACK NR 1 BETWEEN FR 68 AND FR72 IAW A300-600 SRM 51-74-10 AND INSTALLED SEAT TRACK SPLICE REPAIR BETWEEN FR 72 AND FR 77 IAW A300-600 SRM 53-10-16, FIG 208. 2 L 7 2 4F RT A35EU 2008050800096 20080508 00096 CE 2008 5 8 DXTA200803020 1 20080424 A 2150 73838433 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL A/C BAY LEAKING E DXTA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 926QS 7500026 DISCHARGE AIR FROM CABIN PAC EMITTING A OILY FOUL ODOR. REPEAT WRITE UP ISOLATED CABIN PAC IN FLIGHT. THE SMELL SEEMS TO BE COMING FROM THE CABIN PAC. TROUBLESHOT TO LEAKING ACM. REMOVED & REPLACED ACM ASSEMBLY WITH REPAIRED UNIT, IAW THE CE750 M/M CHAPTER 25-51-00. OPERATIONAL & LEAK CHECKS NORMAL. CLEANED COALESCER SOCKS IAW THE CE750 M/M CHAPTER 21-51-00 . LEAK & OPERATIONAL CHECKS NORMAL. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008050800157 20080508 00157 CE 2008 5 8 2008F00014 1 20080428 A 3230 130909B86 CLEVIS BOLT BEECH 65 65 1152802 CE LYC O480 IGSO480A1B6 41529 EA NLG CORRODED A O OTHER O OTHER NR NOT REPORTED 1 GL 01 5079E 2326 LF52 NO NOSE GEAR DOWNLOCK INDICATION CAUSED BY THE SEIZURE OF DOWNLOCK HOOK BOLT. 1 L 7 2 3O 3 O 3A20 E284 2008050800162 20080508 00162 SW 2008 5 8 AC2A119533 1 20080417 A 7800 3G2910A11631 BOLT AGUSTA AB139 AB139 0260110 SW PWA PT6 PT6* 52043 EA EXHAUST BROKEN E AC2A K NONE O OTHER NR NOT REPORTED 1 SW 31 139CW 31020 BOLT BROKEN. 2 G 7 2 4U 3 T R00002RD E2NE 2008050800168 20080508 00168 NM 2008 5 8 2008UALA00982 1 20080222 A 2421 M734284DF GCU BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 653UA 25391 EICAS MSG R GEN OFF DISPLAYED. R GEN OFF AND FIELD OFF LGT'S ILLUMINATED. SUSPECT FAULTY GENERATOR CONTROL UNIT. REPL ACED ENGINE NR 2 GCU PER AMM 24-22-02, CHECKS NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008050800170 20080508 00170 NM 2008 5 8 2008UALA02559 1 20080501 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 500D CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 CHEM MILLED POCKET OF FUSELAGE SKIN AT BS 500D+6 TO 500D+7 AT STRINGER S-12L INDICATES CRACK JUST BELOW CENTERLINE OF ST RINGER. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGE. FABRICATED AND INSTALLED EXTERNAL SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050800177 20080508 00177 NM 2008 5 8 ASAA0852869 1 20080504 A 2425 285A1840 WARNING SYSTEM BOEING 737 737890 1384527 NM COCKPIT MALFUNCTIONED A ASAA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 02 558AS 35177 AFTER ENGINE START "ELEC" LIGHT ON OVERHEAD PANEL CAME ON. ACCOMPLISHED FIM 24 31 TASK 801 & 24 34 TASK 802. FAULT COD E CLEARED. PER FIM FAULT WAS INTERMITTENT, OK FOR SERVICE. 2 L 7 2 4F RT A16WE 2008050800178 20080508 00178 2008 5 8 ASAA0852868 4 20080503 A 3460 1762000101 WARNING SYSTEM BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 579AS 4696 35187 THE "FMC DISAGREE" LIGHT ON AFTER ENGINE START. PERFORMED FIM 34 51 TASK 835 WITH NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A16WE 2008050800185 20080508 00185 NM 2008 5 8 SWAA082409 1 20080502 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 783SW 29809 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008050800187 20080508 00187 NM 2008 5 8 ASAA0842883 1 20080409 A 5311 654654965 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE MISREPAIRED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 02 769AS 25103 AFT PIT REPAIR FOR FRAME AT STA 767 BETWEEN STR 25 26R HAS IMPROPER EDGE DISTANCE. REMOVED IMPROPER REPAIR AND INSTALLE D NEW FRAME REPAIR IAW B737 400 SRM 51 70 11 FIG 1 AND 51 40 02. 2 L 7 2 4F RT A16WE 2008050800191 20080508 00191 NM 2008 5 8 ASAA0842886 1 20080422 A 5310 654795711 STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 AFT PIT DOOR CUTOUT STRAP AT STA 795 846 RBL 17 IS CORRODED. STRAP CORRODED OUT OF LIMITS. REPLACED STRAP IAW SRM 51 4 0 02 PG 2 & 3. ALSO FABBED 65 42949 2 CLIP AND 65 47957 5 WEB. FOUND TO BE DISCREPANT WHEN CHANGING STRAP IAW SRM 51 3 0 01 PG 7 & 8 AND INSTALLED IAW SRM 51 40 02 PG 2 & 3. 2 L 7 2 4F RT A16WE 2008050800193 20080508 00193 NM 2008 5 8 ASAA0842881 1 20080311 A 5330 655298865 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 DENT IN FUSELAGE SKIN BS 1014 STRINGER 12LT. REMOVED DENTED SECTION OF SKIN, FABRICATED AND BONDED SKIN AND DOUBLER INS TALLED REPLACEMENT SECTION OF SKIN IAW B737 400 SRM 51 70 10 AND BOEING DRWG 65 52988. 2 L 7 2 4F RT A16WE 2008050800194 20080508 00194 NM 2008 5 8 ASAA0842879 1 20080319 A 5523 65C2638428 TAB BOEING 737 7374Q8 138447Q NM ELEVATOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 RIGHT ELEVATOR TAB SEPARATING AT HINGE CUTOUTS. REMOVED DAMAGED AREAS, REBONDED HINGE CUTOUT AREAS IAW B737 400 SRM 51 70 17 REPAIR 10. 2 L 7 2 4F RT A16WE 2008050800197 20080508 00197 NM 2008 5 8 ASAA0842889 1 20080429 A 5754 WEDGE BOEING 737 7374Q8 138447Q NM L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 NR 5 SLAT T/E WEDGE LOWER SURFACE CHAFED 3 PLACES. PREPPED DAMAGED AREAS, FABRICATED AND INSTALLED REPAIR SKIN AND DOUB LER IAW B737 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 2008050800199 20080508 00199 NM 2008 5 8 ASAA0842878 1 20080312 A 5753 SKIN BOEING 737 7374Q8 138447Q NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 LEFT WING I/B FORE FLAP LOWER SIDE HAS MULTIPLE DENTS. PREPPED DENTED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLERS I AW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008050800201 20080508 00201 NM 2008 5 8 ASAA0842890 1 20080327 A 5753 SKIN BOEING 737 7374Q8 138447Q NM FORE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 LEFT I/B AFT FLAPS FORE FLAP LOWER SURFACE DENTED 4' FROM I/B END ON 4.5" FROM TIE. REMOVED PREVIOUS REPAIR, PREPPED AR EA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008050800209 20080508 00209 NM 2008 5 8 ASAA0852895 1 20080505 A 2150 23404041 CONDENSER BOEING 737 737890 1384527 NM AC BAY ODIFEROUS A ASAA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 02 584AS 2878 35682 AIRCRAFT HAS DIRTY SOCK SMELL FROM PACKS IN FLIGHT. REPLACED CONDENSER AND RE HEATER ASSEMBLIES ON RT AIR CONDITIONING BAY. 2 L 7 2 4F RT A16WE 2008050700119 20080507 00119 NM 2008 5 7 CALA0800398 1 20080430 A 5320 6546552 SUPPORT BRACKET BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 AIR CONDITIONING SUPPORT BRACKET CRACKED AT LEFTHAND FRAME STATION 827 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING S UPPORT BRACKET AT LEFTHAND FRAME STATION 827 BETWEEN S-8 AND S-9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 2008050700122 20080507 00122 NM 2008 5 7 CALA0800399 1 20080430 A 5320 6546550 SUPPORT BRACKET BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 AIR CONDITIONING SUPPORT BRACKET CRACKED AT LEFTHAND FRAME STATION 787 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING S UPPORT BRACKET AT LEFTHAND FRAME STATION 787 BETWEEN S-8 AND S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008050500013 20080505 00013 NE 2008 5 5 VNAA0804007 2 20080409 A 7230 FAN BLADE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE LT ENGINE STUCK A VNAA D RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 GL 05 716PS 10171 CREW REPORTED A LEFT HAND ENGINE VIBRATION MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCI DENT. MAINTENANCE INSPECTED THE LEFT HAND ENGINE FAN BLADES. MAINTENANCE FOUND AND UNSTUCK A FAN BLADE IN ACCORDANCE W ITH THE GE CF34-8C MAINTENANCE MANUAL. MAINTENANCE PERFORMED OPERATIONAL CHECKS AND FOUND TO BE WITHIN LIMITS AT THIS T IME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008050500016 20080505 00016 EA 2008 5 5 VNAA0804006 1 20080406 A 2810 FUEL TANK CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE LT WING DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 716PS 10171 CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE PERFORMED A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND DAMA GE TO THE LEFT HAND CENTER FUEL TANK AND REPAIRED THE DAMAGE UNDER REO 670-57-21-441. AIRCRAFT WAS RELEASED FOR SERVIC E. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008050500019 20080505 00019 NM 2008 5 5 SWAA082343 1 20080429 A 5315 6584176 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 709, RBL 24.82. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2008050500025 20080505 00025 NM 2008 5 5 SWAA082336 1 20080429 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008050500034 20080505 00034 NM 2008 5 5 SWAA082328 1 20080429 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 495WN 33869 DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008050500048 20080505 00048 NM 2008 5 5 SWAA082373 1 20080501 A 5315 6545410143 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 665, LBL 24.75. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 2008050500062 20080505 00062 NM 2008 5 5 SWAA082369 1 20080501 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 520, STR 26L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008050500070 20080505 00070 EA 2008 5 5 HNAA0800141 1 20080422 A 2731 7003032612 SERVO DHAV DHC8 DHC8311 1386006 EA ELEVATOR MALFUNCTIONED A HNAA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 EA 07 333EN 221 ELEVATOR TRIM IS DIFFICULT TO MOVE AND TRAVEL IS LIMITED. REMOVED AND REPLACED ELEVATOR TRIM SERVO. OPS CHECK GOOD IAW -8 MM. 2 H 7 2 4T RT A13NM 2008050500100 20080505 00100 NM 2008 5 5 USAA920080884 1 20080426 A 5330 6545774 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 441US 24812 CLT - MAJOR REPAIR - C1 CHECK - CRACKED FUSELAGE SKIN, BS 727F, S26L. REPAIRED FUSELAGE SKIN, BS 727F, S26L IAW B737 SR M 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008050500101 20080505 00101 NM 2008 5 5 USAA920080923 1 20080425 A 5320 655486216 INTERCOSTAL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CRACKED INTERCOSTAL, BS 1016, RBL 44. REPLACED INTERCOSTAL, BS 1016, RBL 44 IAW B737 S RM 51-40-02. 2 L 7 2 4F RT A16WE 2008050500133 20080505 00133 WP 2008 5 5 08FDEA01607 1 20080425 A 5730 SKIN PANEL DOUG MD10 MD1010F 3022112 WP LT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 LEFT WING LOWER INBD L/E PANEL 517 AB HAS DAMAGED ATTACHED HOLES. FABRICATED DOUBLER & FILLER IAW SRM 57-00-01 VOL I. A LODINED; PRIMED AND TOPCOAT PAINTED SRM REPAIR IAW SRM 51-21-01 VOL II. INSTALLED SRM REPAIR DOUBLER & FILLER IAW 57-3 1-01 VOL II. 2 L 7 3 4F RT A22WE 2008050500148 20080505 00148 WP 2008 5 5 08FDEA01622 1 20080426 A 5720 AUB7108132 RETAINER DOUG MD10 MD1010F 3022112 WP NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 1 PYLON PANEL 437AR SEAL RETAINER IS CRACKED. REMOVED & REPLACED THE SEAL RETAINER IAW SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 2008050500160 20080505 00160 WP 2008 5 5 08FDEA01636 1 20080428 A 5310 AEA01151 DOOR FRAME DOUG DC10 DC1010F 3022111 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION ON UPPER FUSELAGE AT STA 1256 JAMB DOOR R3 FOUND N2 CRACK TO 2 INCH LONG ON THE WEB LOWER S IDE. REPAIRED FOR SRM 53-50-00 FIG 19 VOL I AND REPLACED CHANNEL P/N AEA0210-40. 2 L 7 3 4F A22WE 2008050500169 20080505 00169 NM 2008 5 5 NWAA081815507 1 20080414 A 5210 SKIN BOEING 757 757251 1384970 NM L4 DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 507US 23196 DURING "M" CHECK, FOUND CRACK IN DOOR 4L INBOARD SKIN BEHIND THE UPPER HINGE TORQUE TUBE. REPAIRED PER EA 55-212537. 2 L 7 2 4F RT A2NM 2008050500185 20080505 00185 NE 2008 5 5 ASAA0852852 2 20080428 A 7261 OIL SYSTEM BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE NR 2 ENGINE LOW A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 557AS 35176 894103 OIL SERVICE NEEDED. SERVICED ENGINE OILS. OIL ADDED TO NR 2=4QTS. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008050500199 20080505 00199 NM 2008 5 5 DL76G080635 1 20080424 A 3397 WIRE BOEING 767 767332 1382001 NM CABIN DAMAGED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 1602 29694 ON ARRIVAL, ELECTRICAL SMELL DETECTED IN MID GALLEY. FOUND DAMAGED WIRING AT FLUORESCENT LIGHT ABOVE SEAT 16FG. SECURE D AFT OUTBD INDIRECT LIGHTING C/B AND INSULATED WIRES. FWD TO MCO AND PLACARD PER MEL 33-21-01. REPLACED 1 OF 2 SOCKET FWD SOCKET ABOVE 16GF 504125. REPLACED THE SECOND SOCKET AFT SOCKET AT 16GF AND RESET C/B P33 L4. OP CK OK. 2 L 7 2 4F RT A1NM 2008050500203 20080505 00203 NM 2008 5 5 DL757080643 1 20080425 A 5412 311N32701 FITTING BOEING 757 757232 1384965 NM NR 2 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 646DL 24217 DURING HMV, AN ELONGATED HOLE WAS FOUND IN THE AFT BULKHEAD FITTING OF THE NR 2 PYLON. THE HOLE WAS REPAIRED PER BOEING INSTRUCTIONS. 2 L 7 2 4F RT A2NM 2008050500206 20080505 00206 NM 2008 5 5 DHL2008760501 1 20080413 A 5720 BAC1506860 BEAM BOEING 727 7272B7 138407L NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 R/WING T/E "J" BEAM CRACKED AT RWBL 128. REMOVED, FABRICATED, AND INSTALLED NEW SUPPORT BEAM FROM WBL 70.5 TO 154.0, PE R ASTAR J/C EC-00874-001 AND B727 SRM 51-30-2. 2 L 7 3 4F A3WE 2008050500213 20080505 00213 EU 2008 5 5 08FDEA01652 1 20080429 A 5532 A5537172600600 PANEL AIRBUS 300 A300F4605R 3930327 EU VERTICAL STAB ERODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 VERTICAL STAB L/E PANEL 322 AL HAS AREAS OF EROSION. REMOVED ERRODED PAINT AND REFINISHED AREA IAW SRM 55-32-00 & 51-75- 10. 2 L 7 2 4F RT A35EU 2008050700123 20080507 00123 NM 2008 5 7 CALA0800400 1 20080430 A 5320 6546548 SUPPORT BRACKET BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 AIR CONDITIONING SUPPORT BRACKET CRACKED AT LEFTHAND FRAME STATION 747 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING S UPPORT BRACKET AT LEFTHAND FRAME STATION 747 BETWEEN S-8 AND S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008050700138 20080507 00138 NM 2008 5 7 08FDEA01764 1 20080505 A 5531 65174636 STRINGER BOEING 727 7272S2F 1384O81 NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 STRINGER 8L CRACKED AT RIB NR 8 STRINGER 8L, FIN STA 157.200 CRACK TERMINATES IN FASTENER HOLE AND HFEC INSPECTED AREA A ND VERIFIED IAW NDTM 51.00.00 PART 6. FABRICATED REPAIR ANGLE IAW SRM 55.30.5 FIGURE 1. TREATED AND PRIMED PARTS IAW S RM 51.10.2. INSTALLED REPAIR PARTS AT STRINGER 8LT RIB NR 8 FIN STA 157.2 IAW SRM 55.30.5 FIGURE 1 AND 51.30.2. 2 L 7 3 4F A3WE 2008050700144 20080507 00144 EU 2008 5 7 CPCP20080027 1 20080404 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 348AE 349 LT INBD SEAT TRACK CORRODED BTW FR 29-36. REPLACED SEAT TRACK BTW FR 29-36 AS PER SRM 51-25-04. 2 H 7 2 4T RT A53EU 2008050700146 20080507 00146 WP 2008 5 7 08FDEA01759 1 20080505 A 5710 ARC01624 FAIRING DOUG MD10 MD1010F 3022112 WP RT WING TE FLAPS CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 RIGHT WING INBD FLAP TRACK FAIRING NR 641 DL AFT EDGE IS CHAFED. BLENDED AREA; PERFORMED D.P.I. AODINED & PRIMED IN REF TO FEDEX E.A. 8-5720-116982" REMOVED & INSTALLED FAIRING IN REF TO SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 2008050700156 20080507 00156 SO 2008 5 7 C2XA08ON118 1 20080428 A 2611 SENSOR EMB 145 EMB145XR 3260214 SO SMOKE DETECTOR DIRTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27190 154500934 FLT 0032 - ONT - FLIGHT CREW REPORTED LAV SMOKE DETECTION WILL NOT TEST DURING PREFLIGHT CHECK. MX PERSONNEL CLEANED SM OKE DETECTOR SENSOR OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008050700157 20080507 00157 EA 2008 5 7 REXA200800009 1 20080501 A 2170 P1096 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA AIR CON SYS ODOR A REXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 25 8721B 7721 DURING TAXI, HAD SMOKE IN THE COCKPIT, RETURNED TO BLOCKS. COALESCER BAG FOUND CONTAMINATED LT AIR CYCLE MACHINE DEFERR ED UNTIL REPLACEMENT PART AVAILABLE 2 L 7 2 4F RT A21EA 2008050700166 20080507 00166 SO 2008 5 7 C2XA08ON119 1 20080430 A 2810 FLAPPER VALVE EMB 145 EMB145XR 3260214 SO FUEL SYSTEM LOOSE A C2XA K NONE K FLUID LOSS UK UNKNOWN 1 SW 27 21197 14500947 FLT 0422 - GEG - FLIGHT CREW REPORTED FUEL LEAKING FROM LEFT WING AT FL 340. ONT MX RESECURED LOOSE FLAPPER VALVE IN LE FT WING, OPERATIONALLY AND LEAK CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008050700168 20080507 00168 SO 2008 5 7 SWIA200819544 1 20080421 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO CABIN SMOKE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 218SW 120287 THE LAV SMOKE ALARM WENT OFF AFTER TAKEOFF, FLIGHT NR 5748. INSPECTED AND OPERATED PACKS IN ALL MODES. COULD NOT DUPLI CATE ANY DISCREPANCIES. 2 L 7 2 4T RT A31SO 2008050700169 20080507 00169 SO 2008 5 7 SWIA200819545 1 20080422 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 293SW 6386 6386 120320 FLT 5785 - EMERGENCY LIGHT SEGMENT IS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008050800210 20080508 00210 NM 2008 5 8 ASAA0852896 1 20080505 A 4990 38809381 FILLER BOEING 737 737890 1384527 NM APU CLOGGED A ASAA O OTHER J WARNING INDICATION IN INSP/MAINT 1 NM 02 584AS P7605 35682 WHILE ACCOMPLISHING TASKCARD 78349013 FOUND APU OIL FILTER EXTENDED. COMPLETED OIL DELTA P INDICATOR SERVICING. REMOVE D FILTER ELEMENT. LEAK AND OP CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2008050800215 20080508 00215 NM 2008 5 8 SWAA082438 1 20080505 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 908, BETWEEN STR 2L AND STR 3L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008050800216 20080508 00216 NM 2008 5 8 SWAA082439 1 20080505 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 26R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008050800224 20080508 00224 NM 2008 5 8 SWAA082454 1 20080505 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 810, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008050800227 20080508 00227 NM 2008 5 8 SWAA082444 1 20080505 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 18R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008050800228 20080508 00228 NM 2008 5 8 SWAA082455 1 20080505 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008050800230 20080508 00230 NM 2008 5 8 SWAA082457 1 20080505 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R AND STR 8L. REMOVED AND REPLACED STRINGER CLI P PER SRM. 2 L 7 2 4F RT A16WE 2008050800240 20080508 00240 NM 2008 5 8 SWAA082450 1 20080505 A 3350 3071BPEGPL LIGHT BOEING 737 73776Q 13845AA NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 551WN 30280 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 15 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008050800244 20080508 00244 NM 2008 5 8 ASAA0892903 1 20080413 A 5230 SKIN BOEING 737 737990 NM CARGO DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 318AS 30018 FWD CARGO DOOR EXTERNAL SKIN 2 EA AREAS OF DENTS WITH CREASES. CUT OUT DAMAGED AREAS, HFEC INSPECTED, NO DEFECTS NOTED. FABRICATED REPAIR DOUBLERS AND INSTALLED IAW B737 900 SRM 52 00 01 REPAIR 3, 1 EA AT STA 459 TO 469 WL 180 TO 172, 1 E A STA 445 TO 452 WL 165 TO 159. 2 L 7 4 4F RT A16WE 2008050800248 20080508 00248 NM 2008 5 8 ASAA0892901 1 20080414 A 5321 141A5810183 FLOORBOARD BOEING 737 737990 NM CABIN BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 318AS 30018 CABIN FLOORBOARD P/N 141A5810 183 STA 344 TO STA 380 LBL 56 O/B EDGE UPPER SURFACE BROKEN AT FWD END. PREPARED DAMAGED AREA REPAIR MATERIAL 4 LAYERS OF BMS 9 3 GLASS CLOTH. BONDED IAW B737 900 SRM 53 00 50 REPAIR 1. 2 L 7 4 4F RT A16WE 2008050800250 20080508 00250 NM 2008 5 8 ASAA0842897 1 20080415 A 5330 6545775 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 762AS 25099 LOWER FUSELAGE DENTED STA 7270+13. DENT REPAIRED AT STA 7270+13 IAW B737 400 SRM 53 00 01 REPAIR 31. 2 L 7 2 4F RT A16WE 2008050900005 20080509 00005 NM 2008 5 9 F3LA200800226 1 20080501 A 5320 D5347646000000 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO RIGHT FLOORBOARD SUPPORT PROFILE AT STRINGER 38 RIGHT BETWEEN FRAMES 52 AND 55 HAS AREAS OF CORROSION AROUND NUTPLATE HOLES. MAINTENANCE REMOVED AND REPLACED RIGHT FLOORBOARD SUPPORT PROFILE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUNDS ACCEPTAB LE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050900010 20080509 00010 WP 2008 5 9 IXXA08SMN138S 1 20080417 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 STUB WING DOUBLER SHOWS CRACK AT STATION XS 515.720. REMOV ED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW EXTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND EXTERNAL DOUBLER. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-2-1A FIGURE 2, DC8 SRM 51 -1-20D, DC8 SRM 51-1-8B, AND 51-3-1. 2 L 7 4 4F RT 4A25 2008050900011 20080509 00011 NM 2008 5 9 QXEA200800448 1 20080502 A 2721 8DK4075001 CONTROL PANEL BOMBDR DHC8 DHC8402 1390042 NM RUDDER TRIM MALFUNCTIONED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 427QX 2711 4156 SEA - EN ROUTE TO SEA, RUNAWAY RUDDER TRIM FULL RIGHT (FULL SCALE). WAS ABLE TO REVERSE WITH TRIM SWITCH. PULLED THE C IRCUIT BREAKER AT NEUTRAL POSITION. ACCOMPLISHED UNEVENTFUL LANDING. MAINTENANCE REPLACED THE RUDDER TRIM ACTUATOR (PN 399600-1007, SN 176) AND THE RUDDER TRIM CONTROL PANEL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008050900012 20080509 00012 NM 2008 5 9 QXEA200800449 1 20080504 A 5210 ROD END BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR DAMAGED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 422QX 4150 SEA - FLIGHT 2231 - MAIN CABIN DOOR HARD TO CLOSE. MAINTENANCE REPLACED THE AFT AND FORWARD UPPER HANDRAIL STRUT ROD EN DS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008050900014 20080509 00014 NM 2008 5 9 F3LA200800234 1 20080501 A 5320 D5391635420040 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 CHECK INSPECTION NOTED FORWARD CARGO LEFT FLOORBOARD SUPPORT PROFILE AT STRINGER 38 LEFT FROM FRAME 28 TO F ORWARD FRAME 34 HAS CORROSION AROUND SEVERAL NUT PLATE HOLES. MAINTENANCE REMOVED AND REPLACED LEFT FLOORBOARD SUPPORT PROFILE AT STRINGER 38 LEFT FROM FRAME 28 TO FRAME 34 IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-40-00 AND SRM 51-44- 11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050900017 20080509 00017 NM 2008 5 9 HALA0800574 1 20080506 A 3150 WARNING LIGHT BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE ILLUMINATED A HALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 484HA 55129 AFTER ENG START RT AND LT ENG FAILURE ALERTS CAME ON. ACCOMP FIM 73-22-806 AND 807 RTS CK GOOD. OK FOR SERVICE. 2 L 7 2 4F 4 F TR A6WE E00061EN 2008050900019 20080509 00019 NM 2008 5 9 F3LA200800235 1 20080501 A 5315 D5397496700000 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO LATERAL FLOORBOARD PROFILE AT FRAME 59 BETWEEN STRINGER 38 LEFT AND 38 R IGHT HAS AREAS OF CORROSION AROUND NUT PLATE HOLES. MAINTENANCE REMOVED AND REPLACED PROFILE AT FRAME 59 BETWEEN STRING ER 38 LEFT AND 38 RIGHT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPE CTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050900026 20080509 00026 EU 2008 5 9 2008UALA02578 1 20080503 A 5210 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 495UA 1842 DOOR 1L AREA IS GASHED. THIS IS A MAJOR REPAIR. CUT OUT DAMAGE AND REPAIRED PER SRM 53-11-11 ON NR D0453A DURING H MV V ISIT. PERMANENT REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050900027 20080509 00027 NM 2008 5 9 2008UALA02579 1 20080502 A 5512 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 RT HORIZONTAL STABILIZER LOWER EXTERNAL SKIN HAS 3 DENTS GROUPED TOGETHER 109 TO 124 INCHES FROM INBOARD EDGE AND 11 INC HES FROM LEADING EDGE. MAJOR REPAIR ACCOMPLISHED: REMOVED DENT DAMAGE. INSTALLED A NEW SKIN SEGMENT FROM RT STAB STA 1 05.7 TO 180.0. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900030 20080509 00030 NM 2008 5 9 2008UALA02582 1 20080504 A 5712 RIB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RWS 135 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 RT WING WBL 135.5 LOWER RIB LOWER CHORD BETWEEN WING STRINGERS S2 AND S3. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGE AND VERIFIED DAMAGE REMOVAL WITH HFEC. INSTALLED REPAIR TEE AND FILLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900031 20080509 00031 NM 2008 5 9 2008UALA02583 1 20080502 A 3350 58807 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 307UA 23668 EEL LIGHTS INOP ON FLOOR AT AFT GALLEY. REPLACED LIGHT STRIP, 560-0857. OPERATES NORMALLY. REPLACED LIGHT STRIP. OPE RATES NORMALLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900034 20080509 00034 NM 2008 5 9 2008UALA02588 1 20080502 A 2612 TFC120057 CONTROL PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FIRE DETECTION NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 341UA 24245 FWD PIT A DETECTOR LIGHT DOES NOT ILLUMINATE WITH CARGO FIRE SYS TEST OR WITH LIGHTS TEST. REPLACED TEST PANEL SYSTEMS CHECK GOOD.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900036 20080509 00036 NM 2008 5 9 2008UALA02590 1 20080502 A 3350 LENS BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS CONTAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 EEL LIGHT HAS MOISTURE INSIDE THE LENS JUST AFT OF DOOR 2R. REPLACED GASKET AND CLEANED THE LENS. OPS CHECK GOOD REF MM 33-51-02.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900039 20080509 00039 NM 2008 5 9 2008UALA02593 1 20080505 A 3350 30043231 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 348UA 24252 LT AFT FUSELAGE EEL LIGHT INOP AFT OF THE INBOARD TRAILING EDGE FLAP. CLEANED CONTACT REF GNMM 2-0-20-002. OPS CHECKS G OOD.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900041 20080509 00041 NM 2008 5 9 2008UALA02595 1 20080504 A 3350 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS OPEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY LIGHT LOWER WALL ACROSS DOOR 1R INOP. FOUND LIGHT ASSEMBLY HAS OPEN WIRE. SPLICED EEL CABLE. OP CK NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008050900046 20080509 00046 NM 2008 5 9 2008UALA02600 1 20080503 A 3510 MC1025154 OXYGEN MASK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE F/O'S FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FIRST OFFICER'S MASK LINES ARE FRAYED. REPLACED FIRST OFFICERS O2 MASK REF MM 25-11-11 PG 201 OP CHECKED GOOD. AC OK F OR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900048 20080509 00048 NM 2008 5 9 2008UALA02602 1 20080504 A 2497 WIRE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GENERATOR BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 FOUND GENERATOR LEAD WIRES BURNT AND ARCING ON OIL PUMP, NEED REPLACEMENT. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900063 20080509 00063 NM 2008 5 9 2008UALA02618 1 20080502 A 4900 APU BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SHUTDOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 APU AUTO SHUT DOWN. 2 L 7 2 4F 4 F RT A1NM E24NE 2008050900068 20080509 00068 NM 2008 5 9 2008UALA02623 1 20080502 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 SLIDE LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 DR 3L SLIDE LIGHT OUT. FOUND INOPERATIVE BULB. REPLACED BULB. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008050900069 20080509 00069 NM 2008 5 9 2008UALA02624 1 20080502 A 3350 582233 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 671UA 30026 EEL LIGHTS INOP LEFT SIDE FIRST CLASS. REPLACED BATTERY PACK. TEST OK. 2 L 7 2 4F 4 F RT A1NM E24NE 2008050900078 20080509 00078 NM 2008 5 9 NWAA081936315 1 20080504 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 675NW 33001 DURING OVERNIGHT CHECK, FOUND EMERGENCY PATH LIGHTS IN ZONE B RIGHT SIDE WON'T ILLUMINATE. MAINTENANCE REMOVED AND REPL ACED BATTERY POWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008050900084 20080509 00084 NM 2008 5 9 2008UALA02632 1 20080505 A 5210 DOOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 OBSTRUCTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 585UA 26709 DOOR 1L DOES NOT DISARM. FOUND FOD UNDER DOOR. REMOVED SCREW FROM UNDER AFT GATE AREA, DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008050900085 20080509 00085 2008 5 9 2008UALA02633 4 20080505 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR SLIDE UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 DOOR 4R WILL NOT ARM. FOUND SLIDE LANYARD INTERFERING. SECURED LANYARD, OPS ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008050900086 20080509 00086 NM 2008 5 9 2008UALA02634 1 20080505 A 5220 PIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LEFT OVERWING SHEARED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 810UA 843 LEFT OVERWING EXIT NOT ARMED. FOUND ROLL PIN HOLDING DISARM PIN SHEARED. REPLACED PIN AND REPLACED DOOR. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050900092 20080509 00092 NM 2008 5 9 2008UALA02642 1 20080505 A 3150 WARNING HORN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FALSE ACTIVATION A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 223UA 30224 EQUIPMENT COOLING HORN SOUNDING AT DEPARTURE. RESETED ECSMC CARD POWER SWITCH AND RESETED C-B (G27) PER FIM 21-27 TAS K 830. PERFORMED GROUND TEST PASSED, MSG DISAPPEAR. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008050900093 20080509 00093 EU 2008 5 9 MALA080068 1 20080505 A 5753 SKIN SAAB SF340 340B 7860101 EU TE FLAP DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 LT FLAP DAMAGE AT 2 PLACES AT NACELLE FAIRING AREA UPPER AND LOWER SKIN. LT FLAP AT NACELLE FAIRING AREA UPPER AND LOWE R SKIN REPAIRED IAW EO S51031: COLD BOND (WET LAYUP) REPAIR IN ACCORDANCE WITH SAAB SRM 51-70-50. 2 L 7 2 4T RT A52EU 2008050900097 20080509 00097 NM 2008 5 9 F3LA200800215 1 20080501 A 5754 D5746067700500 SKIN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE NR 1 SLAT DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED NUMBER ONE SLAT RIGHT WING APPROXIMATELY 36 INCHES FROM OUTBOARD END DENT MEASURES 7 INCHES BY 2 7/8 INCHES BY .252. DENT WITHIN LIMITS IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 57-40-00 PAGE BREAK 20 1 PARAGRAPH 5D FIGURE 204. MAINTENANCE REMOVED NUMBER ONE RIGHT SLAT, REPAIRED DENT ON RIGHT NUMBER ONE SLAT AND REINST ALLED RIGHT NUMBER ONE SLAT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 57-40-00 AND AMM 27-84-63-000-001. UPON COMPLETI ON OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050800153 20080508 00153 CE 2008 5 8 GUUA04270803 1 20080427 A 5540 10164001423 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RUDDER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81546 26091 UE187 DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED LWR RUDDER HINGE BRACKET SHOW SIGNS OF EXFOLIATION. REPLACED LOWER RUD DER HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2008050800158 20080508 00158 WP 2008 5 8 08FDEA01778 1 20080506 A 5522 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 300 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 LEFT STABILIZER DROOP ELEVATOR UPPER SURFACE HAS DENTS. SIX DENTS WITHIN LIMITS IAW DC/MD-10 SRM 51-80-01, VOL II. ONE DENT OUT OF LIMITS IAW DC/MD-10 SRM 51-80-01; VOL II. MATERIAL ID FOR DOUBLER IS 2024-T3, 0.03, PO 485358.1 IAW DC/MD- 10 SRM 55-00-01, VOL I. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01, VOL II. INSTALLED DOUBLER IAW DC/MD-10 SRM 55-0 0-01, VOL I. 2 L 7 3 4F RT A22WE 2008050800160 20080508 00160 WP 2008 5 8 08FDEA01779 1 20080506 A 5420 217000412 SEAL DOUG MD10 MD1010F 3022112 WP NR 3 PYLON BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 3 PYLON ACCESS PANEL NR 488 DR, SPRING SEAL IS BENT. REMOVED 2 SEALS IAW SRM 51-35-01; VOL II. FABBED 2 SEALS IAW S RM 51-10-00; VOL II; FIG 1 & 51-31-01; VOL II; FIG 2. PART MARKED PER GMM 7-0-1001. INSTALLED SEALS IAW SRM 51-35- 01; VOL II. 2 L 7 3 4F RT A22WE 2008050800161 20080508 00161 SW 2008 5 8 AC2A119531 1 20080417 A 6220 3G6220A00251 BOLT AGUSTA AB139 AB139 0260110 SW PWA PT6 PT6* 52043 EA MAIN ROTOR DAMAGED E AC2A K NONE O OTHER NR NOT REPORTED 1 SW 31 139CW 31020 MECHANICAL DAMAGE BEYOND LIMITS. 2 G 7 2 4U 3 T R00002RD E2NE 2008050800175 20080508 00175 NM 2008 5 8 UPS08M52151 1 20080117 A 5230 STRUCTURE DOUG MD11 MD11 3023602 NM CARGO DOOR BENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C EVALUATE CENTER CARGO DOOR C2 LOWER EDGE BENT BACK TO ORIGINAL CONTOUR PER DELTA ERA 36046-1-14. CORN ER DOUBLER FAB FR MATL 7075-0-0.063" PER DWG ADA3774 AND REPAIR ANGLE FAB FR MATL 7075-0-0.080" PER EN1085-08. CORNER D OUBLER AND REPAIR ANGLE HEAT TREATED PER DPS 7.00-1 AND HARDNESS VALUES HRB83.4 AND 81 IS ACCEPTABLE PER DO S1.05-3. RE PAIR DOUBLER AND ANGLE HOLES PICKED UP PER EN1085-08 AND REPROTECTED PER SRM 51-21-01 V.2R.40. HFEC INSP C/OUT FOUND NO CRACK EVIDENT. 2 L 7 3 4F RT A22WE 2008050800179 20080508 00179 2008 5 8 ASAA0852870 4 20080504 A 3460 1762000101 WARNING SYSTEM BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA O OTHER N FALSE WARNING UK UNKNOWN 1 NM 02 558AS 7082 35177 THE "FMC DISAGREE" MESSAGE ON CDU AND MAP DISPLAYS. ACCOMPLISHED FIM 34 61 TASK 835. THE "FMC DISAGREE" MESSAGE ERASED AND NO FURTHER DISCREPANCIES. 2 L 7 2 4F RT A16WE 2008050800192 20080508 00192 NM 2008 5 8 ASAA0842887 1 20080423 A 5330 6547955533 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 AFT PIT CORROSION ON INTERIOR SKIN (BEAR STRAP) UNDER TRANSITION PANEL (ZEE) IN LOWER TORQUE BOX IN FRONT OF CARGO DOOR. REMOVED EXISTING SKIN REPAIR, FABBED REPAIR PARTS AND INSTALLED IAW ASA EA 5330 02334. 2 L 7 2 4F RT A16WE 2008050800195 20080508 00195 NM 2008 5 8 ASAA0842876 1 20080311 A 5754 SKIN BOEING 737 7374Q8 138447Q NM L/E SLAT WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 NR 3 SLAT T/E LOWER SURFACE SKIN WORN INTO COMPOSITE LAYER. REMOVED DAMAGED SECTION OF SKIN, FABRICATED AND INSTALLED R EPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 2008050800200 20080508 00200 NM 2008 5 8 ASAA0842880 1 20080312 A 5753 6546486155 WEDGE BOEING 737 7374Q8 138447Q NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 LEFT I/B MID FLAP T/E WEDGE DENTED SEVERAL AREAS. REMOVED DAMAGED SECTIONS OF WEDGE, FABBED AND INSTALLED REPAIR DOUBLE RS IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008050800202 20080508 00202 NM 2008 5 8 ASAA0842891 1 20080429 A 5753 SKIN BOEING 737 7374Q8 138447Q NM FORE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 LEFT I/B FOREFLAP LOWER SURFACE IS DENTED 6' O/B 3" UP. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008050800206 20080508 00206 SO 2008 5 8 C2XA08CL053 1 20080501 A 4997 WIRE EMB 135 EMB135ER 3260203 SO APU CHAFED A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 16502 145166 CLE FLIGHT 2419 - THE CREW REPORTED A APU FIRE DETECT FAIL MESSAGE INTERMITTENTLY DURING FLIGHT. MAINTENANCE INSPECTED AND REPAIRED A CHAFED WIRE ON THE APU HARNESS. PERFORMED OPERATIONAL CHECKS OF THE SYSTEM. 2 L 7 2 4F RT T00011AT 2008050800211 20080508 00211 NM 2008 5 8 SWAA082432 1 20080505 A 3350 100031 SIGN BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 219WN 32490 FWD CABIN EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2008050800212 20080508 00212 NM 2008 5 8 SWAA082433 1 20080505 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 236WN 34631 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008050800229 20080508 00229 NM 2008 5 8 SWAA082456 1 20080505 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008050800233 20080508 00233 2008 5 8 SWAA082445 4 20080505 A 2565 D31591478 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPL ACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008050800234 20080508 00234 NM 2008 5 8 SWAA082463 1 20080505 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 2008050800235 20080508 00235 NM 2008 5 8 SWAA082464 1 20080505 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM TEE CAP CORRODED AT BS 986, RBL 38 TO LBL 44. REMOVED AND REPLACED TEE CAP PER SRM. 2 L 7 2 4F RT A16WE 2008050800236 20080508 00236 2008 5 8 SWAA082446 4 20080505 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008050800237 20080508 00237 NM 2008 5 8 SWAA082447 1 20080505 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008050800247 20080508 00247 NM 2008 5 8 ASAA0892900 1 20080414 A 5321 141A5810558 FLOORBOARD BOEING 737 737990 NM CABIN CRUSHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 318AS 30018 CABIN FLOORBOARD P/N 141A5810 558 IS CRUSHED AROUND EDGES IN SEVERAL AREAS. PREPARED DAMAGED AREAS, FILLED DAMAGED AREA S WITH BMS 5 28 TYPE 19 4 EA LAYERS OF BMS 9 3 120 FIBERGLASS CLOTH IAW B737 900 53 00 50 REPAIR 4 PAR 3 (BOTH SIDES). 2 L 7 4 4F RT A16WE 2008050800249 20080508 00249 NM 2008 5 8 ASAA0892902 1 20080414 A 5321 141A5810175 FLOORBOARD BOEING 737 737990 NM CNBIN DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 318AS 30018 FLOORBOARD UNDER FWD LAV CREASED AND BROKEN AT AFT O/B CORNER. PREPARED DAMAGED AREA, APPLIED BMS 5 28 TYPE 19 POTTING COMPOUND 4 EA LAYERS EACH SIDE OF BMS 9 3 120 FIBERGLASS CLOTH BONDED IAW B737 900 SRM 53 00 50 REPAIR 6. 2 L 7 4 4F RT A16WE 2008050800252 20080508 00252 NM 2008 5 8 F3LA200800224 1 20080501 A 5321 D5347047700800 FLOORBOARD AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO LEFT FLOORBOARD SUPPORT PROFILE AT STRINGER 38 LEFT BETWEEN FRAMES 56 AN D 58 HAS AREAS OF CORROSION AROUND NUT PLATE HOLES. MAINTENANCE REMOVED CORRODED PROFILE AT STRINGER 38 LEFT FROM FRAME 56 AND 58 LEFT AFT CARGO AND REPLACED WITH NEW PROFILE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11. UPON COMPL ETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 2008050700179 20080507 00179 EU 2008 5 7 SIMA200812107 1 20080416 A 5347 7253799381 SEAT TRACK SAAB SF340 340B 7860101 EU FS 297-314 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 329AE 5000 340B329 DURING A HMBV INSPECTION, THE SEAT TRACK AT BL 0.0 WAS FOUND TO BE CORRODED BETWEEN FS 297 TO FS 314. REMOVED 31 OF SEA T 31 OF SEAT TRACK FROM FS 297 TO FS 328. POSITIONED SPLICE SECTION P/N 7253799-381 AND U-BEAM REPAIR PIECE. TREATED A ND INSTALLED IAW SAAB SRM (72LKS 3079 REV 50) CHAPTER 53-70-60. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 2008050700181 20080507 00181 NM 2008 5 7 EMB08003 1 20080430 A 2560 P2070011100 FLASHLIGHT EMB ERJ190 ERJ190100IGW 3260408 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 947UW 19000078 PHL - FORWARD CABIN EMERGENCY FLASHLIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT AND BATTERY. 2 L 7 2 4F RT A57NM 2008050700182 20080507 00182 EA 2008 5 7 TRAX200800579 1 20080426 A 4970 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 821AS 7194 APU OVERTEMP WARNING MSG ON INFLIGHT 300 KTS AT FL 250, EMERGENCY DECLARED. FLT 4292 DEL 55 MINS. 2 L 7 2 4F RT A21EA 2008050700185 20080507 00185 EA 2008 5 7 TRAX200800582 1 20080427 A 2741 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 686BR 7715 DURING CRUISE AT FL 310, THE STAB TRIM AND MACH TRIM FAIL MESSAGES DISPLAYED ON EDI. RAN QRH PROBLEM PERSISTED. ALSO A CCOMPANYING MSG AP PITCH TRIM MSG. RAN QRH, AP PITCH TRIM MSG PERSISTED UNTIL A/P DISCONNECTED. FLT 4563 DEL 41 MINS. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2008050700192 20080507 00192 NM 2008 5 7 USAA920080981 1 20080419 A 5320 141N518619 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - LEVEL 2 CORROSION ON MAIN DECK FLOOR SUPPORT, BS 365, RBL 48. REPLACED MAIN DECK FLOOR SUPPORT, BS 365, RBL 48 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008050700196 20080507 00196 2008 5 7 200804291 4 20080424 A 3497 CONNECTOR EMB ERJ170 ERJ170100SE 3260406 NM TAT SHORTED A UHLA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 11 652RW 17000075 FLIGHT 7505 YYZ TO DEN CREW REPORTS TAT 1 FAIL W/ SMELL OF SMOKE. ON CALL MAINTENANCE FOUND CONNECTOR SEVERELY SHORTED WITH SEVERAL BURNT WIRES. AIRCRAFT FERRIED TO IND. IND MAINTENANCE REPLACED CONNECTOR, TAT SENSOR P/N: 102AW1AF, S/N: A68247 MANUFACTURER: ROSEMONT AEROSPACE, INC AND ADSP 1. 2 L 7 2 4F RT A56NM 2008050700198 20080507 00198 SO 2008 5 7 SIMA200812106 1 20080423 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 20174 5000 145121 DURING A MBV INSPECTION, THE BAGGAGE DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. REMOVED THE DAMAGED SILL AND CLEANED T HE AREA. POSITIONED THE NEW SILL P/N 145-25480-603, NEW ANGLES P/N 145-25681-607 AND 145-25681-007, MARKED AND DRILLED FASTENERS HOLES. WORK DONE IAW EMBRAER 145 SRM (SRM EMB-145/1142 REV 39) CHAPTERS 51-40-02, 51-21-04, 51-40-06 AND 51-2 0-03. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008050700202 20080507 00202 EU 2008 5 7 TRAX200800583 1 20080428 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 TWO MINUTE LIGHTING WILL NOT EXTINGUISH. 2 H 7 2 4T RT 2008050700207 20080507 00207 EA 2008 5 7 TRAX200800588 1 20080501 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 748EV 10158 RIGHT AFT EXTERIOR EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008050700211 20080507 00211 SO 2008 5 7 RAIA00804030 1 20080428 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 819HK 145062 PRE FLT 5469 - STL - EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE SECURED THE CONNECTOR TO THE AFFECTED FLOOR TRACK LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008050700220 20080507 00220 NM 2008 5 7 DHL2008760530 1 20080402 A 5311 FRAME BOEING 727 7272B7 138407L NM BS 660 S16R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 FABRICATED AND INSTALLED FRAME REPAIR AT BS 660, AND STR 16R, PER B727 SRM 53-10-2 FIG 3 AND SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2008050700230 20080507 00230 SO 2008 5 7 SIMA200812104 1 20080424 A 5320 15425599001 SUPPORT EMB 145 EMB145LR 3260212 SO LAV CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AE 20174 5000 145121 DURING A MBV INSPECTION, THE TOILET WASTE DRAIN SUPPORT WAS FOUND CORRODED. REMOVED DAMAGED SUPPORT AND CLEANED THE ARE A. POSITIONED NEW SUPPORT P/N 145-25599-001 MARKED AND DRILLED FASTENERS HOLES. REMOVED NEW SUPPORT, CLEANED AND TREAT ED THE SUPPORT AND THE REPAIR AREA. WORK DONE IAW 145 SRM (SRM EMB 145/1142 REV 39) CHAPTERS 51-40-02, 51-20-03, 51-20- 01, 51-40-04 AND 51-40-06. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008050700232 20080507 00232 NM 2008 5 7 DHL2008760541 1 20080409 A 5523 SKIN BOEING 727 7272B7 138407L NM RT ELEVATOR TAB DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 CUT OUT DENTED AREA ON RT ELEVATOR TAB SKIN AT ELEV STA 54.0, FABRICATED, AND INSTALLED REPAIR FILLER PER B727 SRM 55-20 -2 AND 51-40-20. 2 L 7 3 4F A3WE 2008050700233 20080507 00233 NM 2008 5 7 AALA200800833 1 20080407 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 DFW - EMERGENCY LIGHT AT SEAT 25G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 25G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050700236 20080507 00236 2008 5 7 RAIA00804033 4 20080429 A 2215 4006719906 SERVO EMB 145 EMB145LR 3260212 SO ELEVATOR MALFUNCTIONED A RAIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 03 834HK 18774 18774 145269 FLT 8092 - IAD - AFTER TAKEOFF, ELEVATOR CONTROL WAS GETTING STIFFER. MAINTENANCE REMOVED AND REPLACED THE ELEVATOR AUT OPILOT SERVO. SYSTEM OPS CHECKED GOOD DURING MAINTENANCE CHECK FLIGHT. NO OTHER DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008050700238 20080507 00238 WP 2008 5 7 AALA200800844 1 20080407 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 505AA 49799 LGA - BATTERY PACK AT B5 28 FOR EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 28 FOR EMERGENCY LIG HTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008050700243 20080507 00243 SO 2008 5 7 RAIA00805001 1 20080501 A 7830 TY256001A LOCK EMB 145 EMB145 3260210 SO THRUST REVERSER DEFECTIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 802HK 145066 FLT 3562 - STL - NR 1 THRUST REVERSER DISAGREE MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE TOP TERTIARY LOCK OF THE THRUST REVERSER. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 2008050700246 20080507 00246 EA 2008 5 7 A6WA200840331 1 20080408 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 319 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 CORROSION FOUND AT SERVICE DOOR FORWARD LOWER FRAME TO FLOOR SUPPORT BRACKET, FS 319. (M) SUPPORT BRACKET REPLACED IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 2008050700250 20080507 00250 EA 2008 5 7 A6WA200840320 1 20080408 A 5740 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 ON LEFT WING ANGLE BRACKET FOUND CRACK, CRACK LENGTH .900. (M) REPLACED ON LEFT WING AT WS 149.58 IAW SRM 51-41-02 AND SRM 51-41-04 (A) 2 L 7 2 4F RT A21EA 2008050700254 20080507 00254 NM 2008 5 7 BB08077 1 20080430 A 3350 SOCKET BOEING 757 7572B7 1384964 NM EXTERIOR LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 932UW 27198 CLT - THE L1 DOOR EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE SECURED LOOSE SOCKET ON LAMPHOLDER ASSEMB LY. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 2008050700257 20080507 00257 EU 2008 5 7 CPCP20080019 1 20080327 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 270AT 270 CORROSION FOUND ON LT O/B SEAT TRACK BTW FR 29-35. REPLACED LT O/B SEAT TRACK BTW FR 29-35 IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2008050700259 20080507 00259 NM 2008 5 7 BB08079 1 20080430 A 2560 P4010021 BATTERY BOEING 757 7572G7 1384963 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 909AW 24522 PHX - THE FLASHLIGHT AT DOOR L2 FLIGHT ATTENDANT SEAT WAS INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT BATTERY AT DOOR L2 FLIGHT ATTENDANT SEAT. 2 L 7 2 4F RT A2NM 2008050700261 20080507 00261 NM 2008 5 7 BB08080 1 20080430 A 2560 P4010021 BATTERY BOEING 757 7572G7 1384963 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 909AW 24522 PHX - THE FLASHLIGHT AT FLIGHT ATTENDANT SEAT AFT OF AFT RIGHT LAVATORY WAS INOPERATIVE. MAINTENANCE REPLACED THE FLASH LIGHT BATTERY. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2008050700268 20080507 00268 WP 2008 5 7 08FDEA01749 1 20080505 A 5347 601096418 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 309FE 48298 MCD SEAT TRACK FROM STA 735-795 LBL 48 HAS 3 PLACES OF GOUGES AND WORN MARKS REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 1. SEAT TRACK FABRICATED ON MAE TRAVELER T8/737330. SPLICE HAT AND PLATE FABRICATED ON MAE TRAVILER T8/737381. RE PLACED FLOORBOARD FROM STA 735 - 775 LBL 28 - 48 AND 735 - 824 LBL 48 - 75 FOR ACCESS REINSTALLED IAW MM 53-21-01-2. 2 L 7 3 4F RT A22WE 2008050700271 20080507 00271 WP 2008 5 7 DHL2008807508 1 20080421 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1500 S30-31L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 FUSELAGE EXTERNAL SKIN CORRODED STA 1500.000 L-30L - L-31L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1, 2, 5. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL7075T6 0.071") FILLER (AL7075T 6 0.063") AND 2 INTERNAL FINGER DOUBLERS (AL7075T6 0.040") IAW SRM 53-2-1 FIG 7 SHEET 1, 2, 5, SRM 53-4-1 FIG17A SHEET 2 ITEM "A". CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FI G 7 SHEET 1, 2, 5, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE). THIS IS A CLASS I TYPE REPAIR ( PERMANE 2 L 7 4 4F RT 4A25 2008050700272 20080507 00272 NM 2008 5 7 NOCA03408 1 20080504 A 3610 792755 CONTROLLER BOEING 767 767324 1385203 NM BLEED AIR SYS MALFUNCTIONED A NOCA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 767NA 27569 A/C HAD REJECTED TAKEOFF IN FRU. ON TAKEOFF ROLL L ENG PRV MESSAGE CAME ON. ACCOMPLISHED AIR SUPPLY BITE PROCEDURE PER MM 36-20-00, NO FAULTS FOUND. ACCOMPLISHED NR 1 ENG PRV VALVE AND CONTROLLER SENSE LINE CHECK, ALL LINES SECURED. INS PECTED AND CLEANED CANNON PER FIM 36-10-00, REPLACED PRV VALVE AND CONTROLLER AS PER MM 36-11-18 AND 36-11-19. 2 L 7 2 4F RT A1NM 2008050700273 20080507 00273 WP 2008 5 7 DHL2008807507 1 20080422 A 5755 SKIN DOUG DC8 DC873F 302199F WP NR 2 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 NR 2 RT SPOILER SKIN DELAMINATED (STA XW 106.000 - XRS 162.000). REMOVED AND REPLACED NR 2 RT SPOILER PANEL IAW MM 27-6 1-1 PG 201-206. REFER TO NR 118258 FOR OPS CHECK. 2 L 7 4 4F RT 4A25 2008050700277 20080507 00277 NE 2008 5 7 A6WA200840338 2 20080414 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LEFT BIRD INGESTION A A6WA A UNSCHED LANDING C F.O.D. CL CLIMB 1 GL 31 428AW 7695 873523 LARGE BIRD INGESTED, LEFT ENGINE AT 1000 AGL DURING TAKEOFF FROM PHL, GEAR EXTENDED PERFORMED AIR RETURN TO PHL, LANDED AT 43,700 LBS. C/W BIRDSTRIKE INSP REF AMM 05-51-25 REF W/O 123145 FOR AW WORK FOUND. 2 L 7 2 4F 4 F RT A21EA E15NE 2008050700284 20080507 00284 EU 2008 5 7 TRBA2008046 1 20080429 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 8680945 EU AIRSTAIR FAILED A TRBA O OTHER O OTHER NR NOT REPORTED 1 SO 29 414WF 414 EMERGENCY EVACUATION PATH LIGHT AT THE BOTTOM OF CABIN DOOR STAIR IS OUT. REMOVED AND REPLACED EMERGENCY GROUND ILLUMIN ATION FLOOD LIGHT ASSEMBLY ON MAIN CABIN DOOR STAIRS IAW AMM JIC NR 33-51-24. 2 H 7 2 4T RT A53EU 2008050700286 20080507 00286 EU 2008 5 7 CPCP20080022 1 20080404 A 5751 HINGE AEROSP ATR72 ATR72212 8680945 EU AILERON CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 348AE 349 (4) HINGE FITTINGS OF LT AILERON TRIM TAB ARE CORRODED. LT AILERON TRIM TAB HINGE FITTING REPLACED NR 2 AND 33 IAW SRM 51-25-03. 2 H 7 2 4T RT A53EU 2008050700288 20080507 00288 2008 5 7 MWEA080066 4 20080502 A 2565 275321353 FASTENER DOUG DC9 DC982 3022082 WP EVAC SLIDE FAILED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 809ME 48071 DURING TAIL CONE SLIDE DEPLOYMENT TEST, TAIL CONE SLIDE FAILED TO DEPLOY WHEN TAIL CONE WAS RELEASED FROM AIRCRAFT. FOU ND DEFECTIVE SNAP ON STRAP ASSEMBLY, REPLACED. 2 L 7 2 4F A6WE 2008050700289 20080507 00289 NM 2008 5 7 DHL2008760556 1 20080421 A 5347 BAC15201466 SEAT TRACK BOEING 727 7272B7 138407L NM BS 850-870 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED CORRODED SEAT TRACK, FABRICATED, AND INSTALLED SEAT TRACK SECTION AT BS 850 TO 870, LBL 24.75, PER B727 SRM 53-1 0-2 FIG 7 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 2008050500211 20080505 00211 EU 2008 5 5 08FDEA01650 1 20080429 A 5532 A55373211008 PANEL AIRBUS 300 A300F4605R 3930327 EU VERTICAL STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 VERTICAL STAB L/E PANEL 322 BL IS DAMAGED ON THE LEADING EDGE. REMOVED AND REPLACED THE ERROSION STRIP IAW AMM 55-32-11 -8 AND E.A. 6-5530-118505. 2 L 7 2 4F RT A35EU 2008050500214 20080505 00214 EU 2008 5 5 08FDEA01653 1 20080429 A 5532 A55371726006 PANEL AIRBUS 300 A300F4605R 3930327 EU VERTICAL STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 VERTICAL STAB L/E 322 AL HAS DAMAGE. REPAIRED VERTICAL STABILIZER L/E PANEL 322 AL BY REMOVING & BONDING A NEW SECTION OF ERROSION STRIP IAW AMM 55-32-11-8. 2 L 7 2 4F RT A35EU 2008050700299 20080507 00299 SO 2008 5 7 SWIA200819583 1 20080426 A 7712 PROBE EMB 120 EMB120ER 3260203 SO TORQUE CONTAMINATED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 295UX 120295 FLT 5732 - THE LEFT ENGINE WENT INTO AUTO-FEATHER WHILE ON GROUND. INSPECTED AND REMOVED MOISTURE FROM TORQUE PROBE. OP S CHECK GOOD. 2 L 7 2 4T RT A31SO 2008050700300 20080507 00300 NM 2008 5 7 USAA920080961 1 20080502 A 5315 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - CRACKED CABIN FLOORBEAM UPPER CHORD, BS 380 - BS 400, BL 0. REPAIRED CABIN FLOORBEAM U PPER CHORD, BS 380 - BS 400, BL 0 IAW B737 SRM 53-30-51. 2 L 7 2 4F RT A16WE 2008050700309 20080507 00309 NM 2008 5 7 USAA920080987 1 20080420 A 5320 143N54101 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK, LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 720 - BS 740, LBL 65. REPLACED CABIN FLOOR SUPPORT, BS 720 - BS 740, LBL 65 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008050700315 20080507 00315 NM 2008 5 7 DHL2008760535 1 20080408 A 5322 SHEAR TIE BOEING 727 7272B7 138407L NM BS 950C CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 SHEAR TIE CORRODED. REMOVED, FABRICATED, AND INSTALLED FRAME SHEAR TIE REPAIR AT BS 950C, BETWEEN STR 28R AND 29R, PER B727 SRM 53-10-2 FIG 5 AND 53-10-4 FIG 11. 2 L 7 3 4F A3WE 2008050700319 20080507 00319 NM 2008 5 7 GTIA0800056 1 20080408 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 504NK 2473 FLOORBEAM CORRODED AT Y765 FRAME 76-70. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2008050700322 20080507 00322 NM 2008 5 7 GTIA0800058 1 20080408 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 504NK 2473 FLOORBEAM CORRODED AT Y254 BETWEEN FRAME 68-70. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2008050700323 20080507 00323 NM 2008 5 7 GTIA0800059 1 20080408 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 504NK 2473 FLOORBEAM CORRODED AT Y1292 BETWEEN FRAME 63-66. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2008050700330 20080507 00330 NM 2008 5 7 2008UALA02441 1 20080425 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 386 S16L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 UPPER LT FUSELAGE SKIN HAS SHARP DENT BS 386 STR 16L. REMOVED AND REPLACED DAMAGE. VERIFIED DAMAGE REMOVAL WITH HFEC. INSTALLED REPAIR DOUBLER, TRIPLER AND FILLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050700335 20080507 00335 EU 2008 5 7 2008UALA02446 1 20080426 A 3510 MXP401600U HARNESS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OXYGEN SYSTEM LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 461UA 1266 FO'S OXYGEN HARNESS FAILS TO INFLATE (IS LEAKING). F/O`S O2 HARNESS LEAKING AT COUPLER. FOUND HARNESS COUPLER IS LEAKI NG O2. REPLACED F-O MASK STOWAGE BOX ASSY, NO LEAKS NOTED AFTER SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050700336 20080507 00336 2008 5 7 2008UALA02447 4 20080426 A 2300 SPEAKER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE COCKPIT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 902UA 25002 CREW REPORTS FAINT ELECTRICAL BURNING SMELL FROM FORWARD CABIN NEAR DOOR 1 POSSIBLY FROM FWD CABIN SPEAKER, CAPT ADVISED TO OPEN THE PA AMP CB P6-1 D5 IF NECESSARY TO REMOVE POWER FROM THE CABIN SPEAKERS AND WILL LOSE THE CHIME SYS IF IT'S PULLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050700344 20080507 00344 EU 2008 5 7 MALA080064 1 20080502 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 630 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 CORROSION FOUND ON CENTER SEAT TRACK 4H SIDE ON ANGLE REPAIR AT STA 630. ON CENTER SEAT TRACK LT ANGLE REPAIR REPLACED IAW EO S53079. 2 L 7 2 4T RT A52EU 2008050700346 20080507 00346 EA 2008 5 7 A6WA200840308 1 20080402 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 CRACK EXIST ON FRAME FS 280 RBL 9. (M) PILOTS BULKHEAD AT FS 280.00 RBL 9 REPAIRED IAW REO 601R-53-11-171 REV "D". (A ) 2 L 7 2 4F RT A21EA 2008050700350 20080507 00350 SO 2008 5 7 C2XA08SH72 1 20080504 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11176 14500881 SHV - DURING C-CHECK CENTER OMEGA BEAM HAS CORROSION AT FR 20. MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FR 20 IAW E MB 145 XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008050700352 20080507 00352 NM 2008 5 7 SWAA082390 1 20080504 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 261WN 32517 R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008050700364 20080507 00364 NM 2008 5 7 SWAA082427 1 20080504 A 5311 6546560 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED DAL CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 940, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008041400171 20080414 00171 NM 2008 4 14 F3LA200800145 1 20080403 A 5320 D5347112320300 WEB AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 5380 1841 DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND UNDER THE WEB AT FRAME 70 AND RIGHT BUTT LINE 52. MAINTEN ANCE REMOVED AND REPLACED THE WEB AT FRAME 70 IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-72-11. UPON COMPLETION OF THE INSTALLATION, THE NEW WEB WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041400173 20080414 00173 EU 2008 4 14 AALA200800710 1 20080323 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80084 675 MIA - EMERGENCY LIGHTS AT RIGHT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008041400183 20080414 00183 NM 2008 4 14 AALA200800703 1 20080323 A 3350 OL3071BPEGPL LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 767AJ 33539 JFK - EMERGENCY LIGHT AT SEAT 26C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041400185 20080414 00185 NM 2008 4 14 AALA200800705 1 20080323 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 767AJ 33539 JFK - EMERGENCY LIGHT AT SEAT 23C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041400193 20080414 00193 NM 2008 4 14 AALA200800722 1 20080326 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 690AA 25696 MIA - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FIRST CLASS CABI N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041400195 20080414 00195 NM 2008 4 14 AALA200800724 1 20080326 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 654A 24612 MIA - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041400196 20080414 00196 NM 2008 4 14 AALA200800725 1 20080326 A 3350 LIGHT BOEING 777 777223 1385213 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 752AN 30260 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET AREA DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041400199 20080414 00199 NM 2008 4 14 AALA200800712 1 20080324 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 605AA 27056 DFW - EMERGENCY LIGHT AT SEAT ROW 22DEF HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 22DEF. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041400202 20080414 00202 NM 2008 4 14 AALA200800732 1 20080327 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHTS AT SEAT ROW 38 INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT ROW 38. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041500004 20080415 00004 EU 2008 4 15 USAA920080722 1 20080401 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE O OTHER NR NOT REPORTED 1 EA 19 680AW 2630 FLT 296 - LAS-SEA - EMERGENCY EQUIP - AFT F/A NOTED EMERGENCY FLASHLIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BAT TERY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A28NM 2008041500006 20080415 00006 EA 2008 4 15 TRAX200800190 1 20080204 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 902EV 7620 AAR - 1003 - FS 280 CLIP AT LBL 9 O/B IS CRACKED. CLIP IS REPLACED ON REPAIR OF FLOORBEAM ASA EC/TC REO 601R-53-21-787 MH13328. SUPPLEMENTAL SDR CLOSED 4/2/08. 2 L 7 2 4F RT A21EA 2008041500007 20080415 00007 EA 2008 4 15 TRAX200800189 1 20080204 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 902EV 7620 AAR - 1002 - FS 280 CLIP AT RBL 9 O/B IS CRACKED. REPAIRED DAMAGE TO FS 280 WEB O/B OF RBL 9 IAW EO 600-53-90 C/W. SUP PLEMENTAL SDR CLOSED 4/3/08. 2 L 7 2 4F RT A21EA 2008050900002 20080509 00002 NM 2008 5 9 F3LA200800236 1 20080501 A 5315 D5347217220400 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 CHECK INSPECTION NOTED CORROSION ON AND AROUND NUT CLIPS ON FLOORBEAM JUST INSIDE OF THE L2 DOOR BETWEEN FR AMES 66 AND 68. MAINTENANCE REMOVED AND REPLACED BEAM JUST INSIDE OF L2 DOOR BETWEEN FRAMES 66 AND 68 IN ACCORDANCE WIT H THE REQUIREMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050900004 20080509 00004 NM 2008 5 9 F3LA200800225 1 20080501 A 2571 D5391408220000 MOUNT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE BATTERY TRAY WORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED AFT BATTERY TRAY FORWARD AND AFT OUTBOARD MOUNTS HAVE EXCESSIVE PLAY CAUSING FRETT ING. MAINTENANCE REMOVED AND REPLACED OUTBOARD FORWARD AND AFT MOUNTS ON BATTERY TRAY IN ACCORDANCE WITH THE REQUIREMEN TS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050900006 20080509 00006 NM 2008 5 9 F3LA200800237 1 20080507 A 2611 CGDU200000 SMOKE WARNING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE ZONE 100 ACTIVATED A F3LA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION LD LANDING 1 NM 03 928FR 93 2236 AFTER ENGINES WERE SHUTOFF, THE CREW REPORTED THE LIVE TV SMOKE ALARM WENT OFF AND MAIN TV POWER SWITCH WAS PUSHED TO OF F AND ALARM WAS SILENCED. MAINTENANCE PERFORMED VISUAL INSPECTION OF LIVE TV AVIONICS COMPARTMENT AND FOUND NO DAMAGE A ND NO SIGNS OF SMOKE DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF TCM 24-00-00-810-823. UPON COMPLETION THE WORK IT WA S INSPECTED AND FOUND ACCEPTABLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050900021 20080509 00021 NM 2008 5 9 F3LA200800207 1 20080501 A 2560 D53480229206 FITTING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION REPORTED L2 AFT DOOR GIRT BAR FITTING WAS CORRODED. MAINTENANCE REMOVED GIRT BAR FITTIN G, FABRICATED NEW GUIDES AND NUTPLATE STRIPS FROM 2024T3 .050. INSTALLED NEW FABRICATED PARTS AND REINSTALLED IN ACCORD ANCE WITH THE REQUIREMENTS OF SRM 51-40-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050900028 20080509 00028 NM 2008 5 9 2008UALA02580 1 20080503 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 348-380 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 STRINGER 15L END FITTING IS CRACKED BETWEEN BS 348.2 AND 380. MAJOR REPAIR ACCOMPLISHED, REPLACED SPLICE CHANNEL. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900037 20080509 00037 NM 2008 5 9 2008UALA02591 1 20080502 A 3350 1619 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 348UA 24252 EEL LIGHT INOP AFT OF LT IB FLAP ON THE FUSELAGE. RELAMPED AND PERFORMED OPS CHECK REF MM 33-51-22.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900038 20080509 00038 NM 2008 5 9 2008UALA02592 1 20080502 A 3350 20131A BATTERY PACK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 348UA 24252 EXT AND INTERNAL EEL LIGHTS INOP BEHIND 1L AND BEHIND LEFT OVERWING SLIDE. INTERNAL FLOOR EEL IN FIRST CLASS. REPLACED BATTERY PACK. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900044 20080509 00044 EU 2008 5 9 2008UALA02598 1 20080504 A 3150 WARNING LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELAC ILLUMINATED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 445UA 826 F-CTL ELAC 2 PITCH FAULT ECAM AFTER ENG START. ELAC2 FAILING-INTERNAL RELAY FAILING TEST. REPLACED ELAC , ALL OPS CHEC KS WERE NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050900049 20080509 00049 NM 2008 5 9 2008UALA02603 1 20080503 A 3150 672951001 VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 FWD EQUIPMENT VALVE EICAS MSG ON LANDING. FOUND OVERBOARD VALVE AND COOLING CONTROL PANEL FAULTY. REPLACED FORWARD OVER BOARD VALVE, AND EQUIPMENT COOLING CONTROL PANEL. OP CHECKS NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008050900051 20080509 00051 2008 5 9 2008UALA02605 4 20080504 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 DOOR 4R SLIDE BOTTLE PRESSURE IS ONE NEEDLE WIDTH TO THE LEFT OF THE GREEN BAND. SLIDE BOTTLE PRESSURE IS LOW. AFTER S ETTING FOR TWO HRS NEEDLE AT END OF GREEN BAND WITHIN CF LIMITS, SLIDE WAS SCHEDULED TO BE REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008050900054 20080509 00054 NM 2008 5 9 2008UALA02608 1 20080502 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1440 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 AFT PIT BS 1440 BETWEEN STRS 26L AND 25L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED, CUTOUT DAMAGE AND INSTALLED DOUBLER R EPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008050900056 20080509 00056 NM 2008 5 9 2008UALA02611 1 20080502 A 3397 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 BULL NOSE LIGHT AT STA 1370R AND FLOOR LIGHT AT K LAV INOP. FOUND CABLE DAMAGE TO LIGHT ASSY. R EPAIRED LIGHT CABLE ASS Y AND RELAMPED. OPS NORMAL 2 L 7 2 4F 4 F RT A2NM E17NE 2008050900057 20080509 00057 NM 2008 5 9 2008UALA02612 1 20080503 A 3050 0871DL6 DETECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RADOME FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 210UA 30216 ICE DETECTOR L LEFT ICE DETECTOR FAILURE. STATUS CREW COMMENTS, STATUS MESSAGE ICE DETECTOR L MSG-3010141 ACTIVE ES HAR D. REPLACED ICE DETECTOR LRU IAW MM30-81-01 OPS CHK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008050900058 20080509 00058 NM 2008 5 9 2008UALA02613 1 20080504 A 3150 WARNING HORN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE MALFUNCTIONED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 210UA 30216 EQUIPMENT COOLING HORN KEEPS GOING OFF. FOUND EQUIPMENT COOLING AIR FILTER DIRTY. REPLACED FILTER. RESET ECS CARD HO RN SILENCED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008050900064 20080509 00064 NM 2008 5 9 2008UALA02619 1 20080502 A 2612 69782143 MODULE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FIRE DETECTION FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 FIRE WARNING BELL FAILS TO RING. REPLACED WARNING BELL MODULE, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900070 20080509 00070 NM 2008 5 9 2008UALA02625 1 20080504 A 2432 AP10777 RELAY BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE BATTERY FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 229UA 30557 FOUND MSG 24-13783, ALSO APU BATTERY WILL NOT DROP BELOW 31 VOLT. REPLACED RELAY. MSG CLEARED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008050900072 20080509 00072 NE 2008 5 9 2008UALA02627 2 20080506 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 VIBRATION A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 228UA 30556 222050 NR 1 ENGINE VIBRATION. FLT 803-05 DIVERTED TO SEA DUE TO PHYSICAL VIBRATION. VIB FOLLOWED THROTTLE. AVM PEGGED AT 10 U NITS. AFTER SHUTDOWN AT SEA, N1 ROTOR LOCKED UP. ENGINE REPLACED AT SEA. TEARDOWN REVEALED THAT THE THRUST BALANCE AIRSE AL (TB AIRSEAL) WAS CRACKED, WITH 2 CHUNKS LIBERATED. THE 2 CHUNKS INCLUDED A KNIFE EDGE, AND AN ANGLED PORTION OF THE B ARREL. THE HARDWARE HAS BEEN RETURNED TO PRATT & WHITNEY FOR FURTHER INVESTIGATION. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008050900075 20080509 00075 2008 5 9 2008UALA02630 4 20080506 A 2565 D31038161 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DOOR 1R READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 426UA 510 SLIDE PRESSURE AT DOOR 1R SHOWS ON RED. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050900077 20080509 00077 EU 2008 5 9 08FDEA01787 1 20080507 A 5320 A53810771001 FLANGE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CHAFING MARKS ON MLG DOOR CENTER HINGE FLANGE REPAIR PERFORMED BY REPLACEMENT OF PART AND INSTALLING BUSH IN LOWER BORE AND IN OFF-CENTERED HOLE IAW RAS 70507037/014/2008 ISS A, APPROVED BY EA 6-5315-117159. 2 L 7 2 4F RT A35EU 2008050900079 20080509 00079 NM 2008 5 9 HALA0800564 1 20080423 A 5512 SKIN BOEING 767 7673CB 1385187 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 588HA 33466 LEVEL 2 CORROSION ON HORIZONTAL STAB CENTER SECTION UPPER SKIN AT LBL 33.5, STR 3, AROUND 7 FASTENERS. REMOVED CORROSIO N AND RESTORED TO ORIGINAL SURFACE FINISH, IAW SRM 55-10-01 FIG 101 REV 76 AND TI 190114804-0001. 2 L 7 2 4F RT A1NM 2008050900080 20080509 00080 NM 2008 5 9 HALA0800562 1 20080423 A 5512 SKIN BOEING 767 7673CB 1385187 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 588HA 33466 LEVEL 2 CORROSION ON THE HORIZONTAL STAB CENTER SECTION UPPER SKIN, RBL 29.5 AT STR. 8,ON THREE FASTENERS. REMOVED CORR OSION AND RESTORED ORIGINAL SURFACE FINISH IAW SRM 55-10-01, FIG 101 REV 76 AND ANZ T1190114804-0001. 2 L 7 2 4F RT A1NM 2008050900087 20080509 00087 EU 2008 5 9 2008UALA02635 1 20080505 A 3350 321431 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 435UA 613 RT OVERWING EMERGENCY LIGHT BATTERY FAILED TEST. REPLACED BATTERY. TEST OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050900094 20080509 00094 EU 2008 5 9 MALA080069 1 20080505 A 5320 ANGLE SAAB SF340 340B 7860101 EU BS 535 CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 DURING CHECK, TWO LT CABIN FRAME INNER FLANGE REINFORCEMENT ANGLES WERE FOUND CHAFED STA 363, 0.20 INCH BY 0.15 INCH BY 0.010 INCH DEEP, STA 535, 0.10 INCH BY 0.20 INCH BY 0.015 INCH DEEP. CHAFE DAMAGE IS BETWEEN STRINGERS SL 1505 AND 1506 . CHAFING IS SIMILAR TO, BUT LESS EXTENSIVE THAN DAMAGE REPAIRED IAW SAAB REPAIR STATEMENT 340SD014672 PARA 5 DATED 4/0 5/08 (AC 421). REPAIRED IN ACCORDANCE WITH THIS EO NR S53559. 2 L 7 2 4T RT A52EU 2008050900098 20080509 00098 WP 2008 5 9 UPS08852154 1 20080424 A 5712 RIB DOUG DC8 DC873F 302199F WP RWS 356 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 RT WING CENTER LE UPPER RIB CRACKED AT XFS356. REPAIRED RT WING CENTER LE UPPER RIB AT XFS 356 IAW S RM 57-03-03 FIG 005 AND SRM 57-02-00-0 FIG 002. 2 L 7 4 4F RT 4A25 2008050900106 20080509 00106 NM 2008 5 9 AALA200800862 1 20080408 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 696AN 26976 MIA - EMERGENCY LIGHT AFT OF COCKPIT DOOR INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AFT OF COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008050900107 20080509 00107 NM 2008 5 9 AALA200800863 1 20080407 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 696AN 26976 DFW - EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER THREE D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008050900109 20080509 00109 NM 2008 5 9 AALA200800870 1 20080408 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW - EMERGENCY LIGHT AT FORWARD GALLEY MISSING CLEAR LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FORWARD GALLEY. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050900103 20080509 00103 WP 2008 5 9 UPS08852159 1 20080414 A 5310 FITTING DOUG DC8 DC873F 302199F WP DOOR FRAME CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 BACKUP FITTING CORRODED AT MCD JAMB NR 5 SPOOL REMOVED AND REPLACED CORRODED FITTING IAW SRM 51-1 -8, 51-3-0, 51-3-2, RE F.DWR NR 47732951. 2 L 7 4 4F RT 4A25 2008050900104 20080509 00104 EU 2008 5 9 MALA080076 1 20080505 A 5330 PANEL SAAB SF340 340B 7860101 EU FUSELAGE DELAMINATED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 RT FUSELAGE PANEL 151CB DAMAGED COMPOSITE DELAMINATED. RT FUSELAGE PANEL 151CB REPAIRED IAW S51031 PAINTED IAW EO S5103 1 AND SRM 51-20-43. 2 L 7 2 4T RT A52EU 2008050900110 20080509 00110 NM 2008 5 9 AALA200800871 1 20080408 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050900111 20080509 00111 NM 2008 5 9 AALA200800872 1 20080408 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW - EMERGENCY LIGHT AT SEAT 25C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050900112 20080509 00112 NM 2008 5 9 AALA200800873 1 20080408 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW - EMERGENCY LIGHT AT SEAT 38G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 38G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 200805131 20080513 1 EU 2008 5 13 08FDEA01794 1 20080508 A 5320 A53410426204205 SUPPORT BRACKET AIRBUS 310 A310324 3930206 EU FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 RIGHT AIR CONDITIONING FAIRING SUPPORT BRACKET IS WORN, 9 INCH AFT OF FRAME 43. REMOVED DAMAGED BRACKET REF A310 SRM 51 -40-21. FORMED AND LOCATED FASTENER HOLES IAW AIRBUS DWG 53410426. ALODINED AND PRIMED NEW BRACKETS REF A310 SRM 51-21 -10. PAINTED NEW BRACKET REF A310 SRM 51-23-10. INSTALLED NEW BRACKET REF A310 SRM 51-40-21. 2 L 7 2 4F RT A35EU 200805131 20080513 1 WP 2008 5 13 08FDEA01795 1 20080508 A 5730 ARB12322 SKIN DOUG MD10 MD1010F 3022112 WP RT WING DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 RIGHT WING FIXED LEADING EDGE SKIN IS DENTED IN 4 PLACES AT STA XFS 627 TO XFS 653. DEPTH OF THE DENTS ARE0.045 TO 0.120 . DENTS ARE OUT OF LIMITS IAW SRM 57-00-01 VOL I FIG 1B. FABRICATED REPAIR IAW SRM 52-00-01 VOL I FIG 4. ALODINE D IAW SRM 51-21-01 VOL II. PRIMED IAW SRM 51-21-01 VOL II. INSTALLED THE REPAIR IAW SRM 51-00-01 VOL I FIG I. 2 L 7 3 4F RT A22WE 200805131 20080513 1 NM 2008 5 13 F3LA200800241 1 20080423 A 5321 D5367228300000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED AFT PIT FLOOR PANEL 151CE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE PANEL IN ACC ORDANCE WITH THE REQUIREMENTS OF AMM 53-42-14-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTAB LE. 2 L 7 2 4F 4 F RT A28NM E37NE 200805131 20080513 1 NM 2008 5 13 NWAA082005804 1 20080507 A 3350 BATTERY PACK BOEING 757 757351 1384991 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 584NW 32984 BATTERY PACK M11488 FAILED DURING EMERGENCY LIGHT BATTERY PACK CHECK AS PART OF A 1/2 A CHECK. MAINTENANCE REPLACED THE BATTERY PACK AND ALL OPERATIONS CHECKED GOOD. 2 L 7 2 4F RT A2NM 200805131 20080513 1 WP 2008 5 13 NWAA081999928 1 20080506 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8921E 45836 DURING LINE CHECK, THE RIGHT OVERWING EMERGENCY EXIT SIGN AND THE EMERGENCY PATHWAY LIGHTING AT ROWS 5, 6, AND 7 WERE FO UND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM. 2 L 7 2 4F A6WE 200805131 20080513 1 NM 2008 5 13 DL76S080647 1 20080429 A 5314 145T86119 KEELBEAM BOEING 767 767332 1382001 NM BS 965-993 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 121DE 23435 LT KEELBEAM CORRODED ON OUTBD FLANGE BETWEEN FS 965-933. DAMAGE REMVOED AND A REPAIR STRAP WAS INSTALLED. 2 L 7 2 4F RT A1NM 200805131 20080513 1 NM 2008 5 13 DLM88080649 1 20080430 A 2913 623337 PUMP DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE HYD SYSTEM INOPERATIVE A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 944DL 49817 718147 RIGHT ENGINE HYDRAULIC PUMP FAILED IN FLIGHT, ZERO PRESSURE PRESSURE GOOD WITH AUX HYD PUMP, RETURNED TO ATL. REPLACED ENGINE HYDRAULIC PUMP, CASE DRAIN AND PRESSURE FILTERS. REPLACED RT HYDRAULIC SYSTEM MAIN FILTERS- OPERATED ENG INE PRESSURE CKS GOOD, LK CKS GOOD. 2 L 7 2 4F 4 F RT A6WE E9NE 200805131 20080513 1 NM 2008 5 13 DLM90080672 1 20080430 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 1136-1174 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 CABIN SEAT TRACK FS 1136-1174 RBL 54 OUT OF LIMITS. REPAIRED SEAT, IAW MD90 SRM 53-40-01 VOL I. 2 L 7 2 4F RT A6WE 200805131 20080513 1 NM 2008 5 13 AALA200800883 1 20080408 A 3350 OL3071BPEGPL LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHT AT SEAT 26C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 200805131 20080513 1 NM 2008 5 13 F3LA200800240 1 20080501 A 5315 D5347218920400 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED CORROSION ON AND AROUND FASTENERS ON BEAM INBOARD OF R2 DOOR BETWEEN FRAME 68 AND 70. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11 AND SRM 51-42-00. U PON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 200805131 20080513 1 NM 2008 5 13 DLM88080681 1 20080505 A 2133 OUTFLOW VALVE DOUG MD88 MD88 3023688 NM CABIN PRESSURE BINDING A DALA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SO 27 910DL 49541 ON CLIMB-OUT AROUND 7000 FT AUTO PRESS INOP ILLUMINATED (ALONG WITH AUTO1 AND AUTO 2 PRESS) MANUAL PRESSURIZATION WHEEL WOULD NOT MOVE FORWARD OF THE 15 FLAP POSITION. UPON INSPECTION, FOUND 2 SCREWS IN CHANNEL OF OUTFLOW VALVE CONTROL WH EEL CAUSING IT TO BIND. REMOVED SCREWS AND INSPECT AREA, FOUND 2 SCREWS MISSING FROM UNDER FMS CONTROL PANEL. INSTALLE D SCREWS IN PANEL, PERFORMED BITE CK OF CABIN PRESS CONTROLLERS PER 21-32-00 OF AMM, NO FAULTS FOUND. PERFORMED T OF O UTFLOW VALVE MANUAL CONTROL PER AMM, NO DEFECTS FOUND. 2 L 7 2 4F RT A6WE 200805131 20080513 1 SO 2008 5 13 CHQA200800091 1 20080501 A 2731 9939015 SWITCH EMB EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL TRIM CONTROL DIRTY A CHQA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 578RP 14500864 145865 CAE312100 FLIGHT 6243, HSV TO CVG, DURING CRUISE THE AUTOPILOT DISENGAGED ASSOCIATED WITH PITCH TRIM MAIN AND BACKUP INOP MESSAGES ON EICAS. THE FLIGHT CREW PERFORMED THE APPROPRIATE QRH CHECKLISTS AND BOTH PITCH TRIM SYSTEMS BECAME OPERABLE AGAIN. THE FLIGHT LANDED WITHOUT INCIDENT IN CVG. MAINTENANCE CLEANED THE TRIM SWITCHES PER AMM 27-40-03 AND 24-40-04 AND THE TRIM SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 200805131 20080513 1 NM 2008 5 13 NWAA081986624 1 20080504 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 624US 21706 DURING THE DOD (DEPARTMENT OF DEFENSE) PRE-FLIGHT, FOUND CABIN EMERGENCY LIGHTS AT 3L DOOR INOP. MAINTENANCE REMOVED AN D REPLACED BATTERY PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 200805131 20080513 1 WP 2008 5 13 IXXA08SMN185S 1 20080507 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP CARGO BAY CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FLOOR PANEL WITH CORROSION AT STATION 1425.000 RIGHT BOT TOM LINE 50. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND R EPAIR PARTS IAW DC8 SRM 51-1-21, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 53-2-3 PAGES 39-40, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 200805131 20080513 1 NM 2008 5 13 2008UALA02560 1 20080501 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 348UA 24252 EMERGENCY LIGHTS OUT AT CENTER SECTION OF THE CABIN. SUSPECT FAULTY LIGHT ASSEMBLY. REPLACED 12 FT EEL SECTION REF MM 33-51-89-401. OPS CHECKS GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 200805131 20080513 1 NM 2008 5 13 2008UALA02561 1 20080501 A 5242 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE E/E DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 E/E COMPARTMENT DOOR EXTERIOR SKIN DENTED AT AFT RIGHT CORNER. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGED SKIN. INSTAL LED FILLER AND DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 200805131 20080513 1 NM 2008 5 13 2008UALA02563 1 20080501 A 2560 D31591478U1 GIRT BAR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY DOOR UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 FWD GALLEY DOOR EVAC SLIDE GIRT BAR CURTAIN PULLED OUT OF COVER. SECURED GIRT BAR REF MM 25-61-35.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 200805131 20080513 1 NM 2008 5 13 F3LA200800213 1 20080501 A 5321 D5367228200200 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO FLOOR PANEL 151ZG WAS DELAMINATED. MAINTENANCE TRIMMED BACK UPPER SKIN REMOVED CORE AND LOWER SKIN ABRADED BOTTOM SURFACE OF SKIN IN ACCORDANCE WITH THE REQUIREMENTS OF EA A0-53T-10131. MANU FACTURED FILLER PLATE AND DOUBLER PLATE, STEP SANDED AND APPLIED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF EA A0-53T -10131 AND SRM 53-02-00 AND 51-57-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 200805141 20080514 1 NM 2008 5 14 F3LA200800247 1 20080508 A 5210 D5348004220601 FITTING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE L2 DOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED L2 DOOR AFT LOWER CORNER CAST FITTING IS CORRODED. MAINTENANCE REMOVED AND REPLAC ED L2 DOOR AFT LOWER CORNER CAST FITTING IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11 AND AMM 53-45-15. UPON COM PLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 200805141 20080514 1 EA 2008 5 14 SWIA200819609 1 20080407 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 763SK 10228 FS 280 COCKPIT FLOORBEAM IS CORRODED, FOUND AT C-CHECK. COMPLIED WITH FLOORBEAM REPAIRS PER CRJ700/900 SRM 51-42-07 PG 10. 2 L 7 2 4F RT A21EA 200805141 20080514 1 EU 2008 5 14 MALA080083 1 20080508 A 3350 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS NO TEST A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425XJ 340B425 EMERGENCY LIGHT BATTERY PACK P/N 3301-51 S/N 2028 LOCATION 21LN FAILED FUNCTIONAL TEST IAW TASK CARD 335003. REMOVED AN D REPLACED EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-50-01. 2 L 7 2 4T RT A52EU 200805141 20080514 1 EA 2008 5 14 REXA200800011 1 20080407 A 2930 INDICATION SYS CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM MALFUNCTIONED A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 8495B 7495 AFTER TAKEOFF IN CLIMB HYDRAULIC QUANTITY INDICATION FOR NO SYSTEM DROPPED TO ZERO. QRH FOLLOWED RETURNED TO MSP WITH U NEVENTFUL LANDING. SYSTEM TESTED FOUND TO BE INDICATION ONLY DEFERRED UNDER MEL 29-32-01. DEFER CLEARED BY PERFORMING AMM TEST WITH NO FAULTS FOUND. 2 L 7 2 4F RT A21EA 200805141 20080514 1 NM 2008 5 14 F3LA200800249 1 20080501 A 5321 D5367414600000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO FLOOR PANEL 152TG HAS DAMAGED EDGE. MAINTENANCE REPLACED AFT CARGO MID FLOOR PANEL 152TG WITH NEW PANEL. PANEL WAS INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF NON ROUTINE 9623. UPON CO MPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 200805141 20080514 1 EU 2008 5 14 NWAA081833313 1 20080427 A 3350 BATTERY PACK AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 813NW 0799 EPSU FAULT (18WL), REPLACED BATTERY PACK (18WL) AND CHECKS GOOD. 2 L 7 2 4F RT A46NM 200805141 20080514 1 2008 5 14 DXTA200803029 4 20080428 A 3460 COMPUTER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FLIGHT GUIDANCE FAILED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 944QS 7500144 ON TAKEOFF, WE HAD MACH TRIM, LOWER YD, AND FGC COMPUTER FAIL. PURGED THE NR 1 AND 2 PITOT STATIC SYSTEMS. PERFORMED LE AK TEST OF THE NR 1 AND 2 PITOT STATIC SYSTEMS AND FUNCTION TESTS OF THE NR 1 AND 2 MADC'S SYSTEM TESTED NORMALLY. DONE IAW CESSNA 750 MM 34-11-01 AND 34-11-08. 2 L 7 2 4J 4 F RT T00007WI TE6CH 200805141 20080514 1 WP 2008 5 14 ASMF200804005 1 20080425 A 2910 7936907615 HYDRAULIC LINE DOUG DC9 DC987 3022087 WP HYDRAULIC SYS LEAKING W ASMF K NONE K FLUID LOSS IN INSP/MAINT 1 SW 23 754RA 49641 CAPTAIN REPORTED LT HYDRAULIC PUMP WITH FAILURE. MAINTENANCE CHECKED THE LT SYSTEM AND DETECTED A HYDRAULIC LEAK IN THE REVERSE CONTROL VALVE LINE. THE HYDRAULIC LINE WAS REPLACED BY A FLEXIBLE LINE IAW MM 12-13-01 AND HYDRAULIC PUMP WAS RE PLACED IAW MM 29-11-11, TESTED CORRECT. DURING OVERNIGHT CHECK, THE LT FLEXIBLE LINE, FILTER AND WATER SEPARATORS WERE R EPLACED AND PNEUMATIC SYSTEM DUCTS WERE CLEANED, TESTED CORRECT IAW MM 29-10-05 AND 29-01-02. 2 L 7 2 4F RT A6WE 200805141 20080514 1 NM 2008 5 14 LYNX00012 1 20080421 A 3246 BEARING BFGOODRICH BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA NR 4 MLG FAILED A 3LYA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 21 502LX 0960 4168 NR 4 MLG WHEEL ASSY OB BEARING ASSY FAILED DURING TAXI. REMOVED AND REPLACED RT MLG AXEL, WHEEL SPEED TRANSDUCER, NR4 BRAKE ASSY, AND NR4 MLG WHEEL ASSY. REF LOG PAGES 005765,005766 AND 005767. 2 H 7 2 4T 4 T RT A13NM E00062EN 200805141 20080514 1 2008 5 14 COEA0801873 3 20080422 A 6140 GAUGE CESSNA 208 208B 2073701 CE PWA PT6 PT6* 52043 EA COCKPIT DEFECTIVE A COEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 13 873FE 208B0202 RETURN TO BLOCKS. FLT NR 8797, ON TAXI TO RUNWAY PILOT NOTICED THAT THE PROP RPM GAUGE WAS STUCK AT 200 RPM. THE PAR ( POWER ANALIZER AND RECORDER) UNIT SHOWS PROP RPM NORMAL. AC WAS TAXIED BACK TO RAMP FOR MAINTENANCE. MAINTENANCE REPLA CED NP (PROP RPM) GAUGE. (K) 1 H 7 1 3T 3 T A37CE E2NE 200805141 20080514 1 EA 2008 5 14 SWIA200819553 1 20080205 A 5220 HANDLE CNDAIR CL600 CL6002C10 1390015 EA ESCAPE HATCH BINDING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 762SK 10226 CREW ESCAPE HATCH HANDLE BINDS, FOUND AT C-CHECK. RIGGED CREW ESCAPE HATCH LATCH MECHANISM PER CRJ7/9 AMM 52-22-02-820- 801-A01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 200805141 20080514 1 EU 2008 5 14 WRNA200800037 1 20080429 A 2421 707304E CSD AIRBUS 300 A300B4203 3930306 EU NR 1 MALFUNCTIONED A WRNA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 05 510TA 564 100 DURING FLIGHT, NR 1 CONSTANT SPEED DRIVE LOW OIL PRESSURE LIGHT ILLUMINATED FOLLOWED BY RISING OIL TEMPERATURE. DISCONN ECTED CSD AND RETURNED TO MFM FOR A SAFE LANDING. REPLACED CSD IAW MM 24-11-11 PG 401 AND CSD OIL COOLER IAW 24-11-21 P AGE 401. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A35EU 200805141 20080514 1 EU 2008 5 14 WRNA20080038 1 20080502 A 3230 A254215 UPLOCK AIRBUS 300 A300B4203 3930306 EU NLG UNSERVICEABLE A WRNA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 504TA 216 AFTER TAKEOFF, NOSE LANDING GEAR FAILED TO RETRACT. DUMPED FUEL AND RETURNED TO FIELD FOR A SAFE LANDING. REPLACED NOS E GEAR UP-LOCK ASSY IAW MM 32-31-14 PG 401. OPS CHECK GOOD IAW MM 32-30-00 PG 501. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A35EU 200805141 20080514 1 2008 5 14 08FDEA01673 2 20080429 A 7200 9082M50G01 CASE DOUG MD10 MD1010F 3022112 WP NR 3 EXIT GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 3 ENGINE FAN EXIT CASE FLANGE AT THE FAN HOLD OPEN ROD SUPPORT BRACKET HAS A GOUGE ON THE FLANGE. BLENDED GOUGED ARE A AND FOUND TO BE OUT OF LIMITS IN REF TO ENGINE MANUAL 72-23-01 PG 311. WELDED REPAIR AREA IN REF TO ENGINE MANUAL 72- 23-01 REPAIR 01. ALODINED 7 PRIMED IN REF TO SRM 51-21-01; VOL II. FPI IN REF TO SPM 70-32-01. NO DEFECTS NOTED. 2 L 7 3 4F RT A22WE 200805141 20080514 1 WP 2008 5 14 AALA200800821 1 20080405 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7549A 53031 LGA - EMERGENCY LIGHT AT OVERHEAD AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD AFT FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008051400002 20080514 00002 NM 2008 5 14 ASAA0842905 1 20080501 A 5754 WEDGE BOEING 737 7374Q8 138447Q NM L/E SLAT DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 RIGHT WING L/E SLAT NR 5 O/B TRAILING EDGE WEDGE CORNER UPPER SURFACE DAMAGED. PREPARED DAMAGED AREA, FABRICATED FILLER AND DOUBLER, BONDED IAW B737 400 SRM 51 70 10 PAGES 214, 212, 241 AND 249 PAR 20. 2 L 7 2 4F RT A16WE 2008051400003 20080514 00003 NE 2008 5 14 ASAA0852906 2 20080501 A 7321 1853M56P12 HYDROMECH UNIT BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 2 ENGINE FAULTY A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 596AS 60 35688 896459 ENGINE NR 2 SHUTDOWN WHILE TAXIING IN. REPLACED HMU HIGH STAGE VALVE & HIGH STAGE REGULATOR. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008051400005 20080514 00005 NM 2008 5 14 YENA2008043 1 20080503 A 2752 C1558121 ACTUATOR EMB ERJ190 ERJ190100IGW 3260408 NM T/E FLAP POPPED A YENA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 15 258JB 4685 4685 19000047 FLT 1205, HPN-RSW, FLAPS FAIL ON FINAL APPROACH, UNABLE TO RESET PER QRH, FLAP "0" LANDING, LANDING SPEED APPROX 180 KTS . T/S PER FIM TASK 27-51-00-810-802-A, REMOVED AND REPLACED L4 FLAP ACTUATOR DUE TO BEING POPPED IAW AMM 27-51-01, ALL OPS CHECKS NORMAL AMM 27-50-00-710-801-A1500. 2 L 7 2 4F RT A57NM 2008051400007 20080514 00007 NM 2008 5 14 ASAA0852908 1 20080506 A 4920 38007021 APU BOEING 737 737890 1384527 NM LEAKING A ASAA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 02 579AS 4712 35187 DURING TROUBLESHOOTING FOR SOURCES OF CABIN ODOR FOUND APU LOAD COMPRESSOR WITNESS HOLE TO HAVE OIL. OIL WAS PRESENT AB OVE CHECK VALVE ALSO. REPLACED APU. OP & LEAK CHECKS GOOD. 2 L 7 2 4F RT A16WE 2008051400010 20080514 00010 NM 2008 5 14 CALA0800414 1 20080506 A 5320 65499172 CHANNEL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14342 23580 DURING REMOVAL AND REPLACEMENT OF THE NR 3 VHF ANTENNA TWO CRACKS WERE FOUND ON THE ANTENNA MOUNTING CHANNEL LOCATED IN THE AFT CARGO COMPARTMENT. CHANNEL AT STATION 727C TO 727D BETWEEN S27L TO S27R FOUND WITH TWO CRACKS WAS REMOVED AND R EPLACED WITH NEW CHANNEL AND BRACKET FROM STATION 727C TO 727D, S27L TO S27R PER B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008051400014 20080514 00014 NM 2008 5 14 CALA0800417 1 20080507 A 5313 654988646 STRINGER BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 E&E COMPARTMENT APPROX 4" AFT OF STATION 360, S27L FOUND CORROSION AND CRACKS. FABRICATED AND INSTALLED REPAIR PER ECRA 5330-03803. 2 L 7 2 4F RT A16WE 2008051400019 20080514 00019 NM 2008 5 14 ASAA0842910 1 20080429 A 5754 65C26603202 SLAT BOEING 737 7374Q8 138447Q NM WING DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 NR 4 SLAT I/B END IS CHAFED. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 2008051400025 20080514 00025 NM 2008 5 14 CALA0800422 1 20080430 A 5754 65C26601389A SKIN BOEING 737 737524 1384721 NM L/E SLAT DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 NUMBER 1 SLAT HAS 2 DENTS 39" FROM OUTBOARD END WHICH ARE BEYOND ALLOWABLE DAMAGE PER 737-500 SRM 57-43-01 FIG 101. CUT OUT DAMAGED AREA IAW B737 SRM 57-43-01 FIG 201. MULT ID FOR REPAIR 7075-T6 .063 FOR PART 1 REPAIR PLATE, 7075-T6 .071 FOR DOUBLERS 2, 3, & 4 IAW B737 SRM 57-43-01. FABRICATED REPAIR PARTS IAW B737 SRM 57-43-01, ALODINED AND PRIMED REPAIR IAW B737 SRM 51-20-01. INSTALLED REPAIR IAW B737 SRM 57-43-01. 2 L 7 2 4F RT A16WE 2008051400026 20080514 00026 NM 2008 5 14 CALA0800423 1 20080508 A 3350 D71702030 CHARGER BOEING 737 737724 13844BY NM CABIN INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 54711 28782 EMERGENCY LIGHTS COME ON WHEN TESTED BUT GO OUT QUICKLY LOCATED AT RIGHT-SIDE BULLNOSE 2 THRU 15, OVERWING EMERGENCY EXI T, ALL THREE INSIDE AND OVERWING OUTSIDE, AND BOTH RT AND LT AFT FUSELAGE. REPLACED BOTH BATTERY PACKS AND CHARGERS P/N D717-01 -100, P/N D717-02-030 PER M/M 33-51-06, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A16WE 2008051400037 20080514 00037 NM 2008 5 14 ASAA0842918 1 20080501 A 5755 654645170M SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 LEFT WING NR 1 SPOILER HAS DENTS CLOSE TOGETHER AT O/B UPPER SURFACE AREA. PREPARED DAMAGED AREA, FABRICATED REPAIR DOU BLER, BONDED IAW 737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008051400038 20080514 00038 NM 2008 5 14 ASAA0842919 1 20080501 A 5755 654645170M SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 LEFT WING NR 1 SPOILER UPPER SURFACE HAS SEVERAL BUMP CLOSE TOGETHER I/B AREA. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008051400049 20080514 00049 NM 2008 5 14 CALA0800424 1 20080509 A 5320 141A541012 FLOOR SUPPORT BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23708 28769 CABIN FLOOR SUPPORT CRACKED STATION 312 STATION 328 RBL 31.60. REMOVED AND REPLACED FLOOR SUPPORT LOCATED AT RBL 31.60 BETWEEN STATIONS 312-328 REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008051400051 20080514 00051 NM 2008 5 14 CALA0800425 1 20080509 A 5320 141A541012 INTERCOSTAL BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23708 28769 CABIN FWD ENTRY, INTERCOSTAL BETWEEN STA 312 TO 328 BY L-1 DOOR CRACKED. REMOVED & REPLACED INTERCOSTAL REF SRM 51-40-0 2. 2 L 7 2 4F RT A16WE 2008051400074 20080514 00074 NM 2008 5 14 CALA0800433 1 20080509 A 7830 491B1330011 WEB BOEING 767 767224 1385170 NM THRUST REVERSER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76153 30432 NUMBER 1 ENGINE OUTBOARD C-DUCT BULKHEAD FORWARD UPPER ATTACH WEB CRACKED AT 11 O`CLOCK POSITION. NUMBER 1 ENGINE OUTBO ARD C-DUCT BULKHEAD FORWARD UPPER ATTACH WEB REPAIRED PER MRAS CMM 78-32-02 REPAIR 024. 2 L 7 2 4F RT A1NM 2008051400075 20080514 00075 NM 2008 5 14 CALA0800434 1 20080509 A 7830 491B1330011 WEB BOEING 767 767224 1385170 NM THRUST REVERSER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76153 30432 NUMBER 2 ENGINE RIGHTHAND C-DUCT FORWARD TORQUE BOX ATTACH WEB FOUND CRACKED AT 1 O`CLOCK POSITION. NUMBER 2 ENGINE RIG HTHAND C-DUCT FORWARD TORQUE BOX WEB REPAIRED PER MRAS CMM 78-32-02 REPAIR 024. 2 L 7 2 4F RT A1NM 2008051400076 20080514 00076 NM 2008 5 14 CALA0800435 1 20080505 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 RIGHT SIDE BS 827 INBOARD ATTACH FASTENER HOLE ON AIR CONDITIONING BRACKET CRACKED. REMOVED DAMAGE, DRILLED AND INSTALL ED REPAIR IAW EA5310-04498. 2 L 7 2 4F RT A16WE 2008051400085 20080514 00085 NM 2008 5 14 CALA0800412 1 20080502 A 3350 ADD71701100 BATTERY PACK BOEING 737 737724 13844BY NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16732 28948 OVERWING EMERGENCY "RED" ARMREST LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER IAW M/M 33-51-00. OPS CHECKS GOOD. 2 L 7 2 4F RT A16WE 200805131 20080513 1 WP 2008 5 13 08FDEA01796 1 20080508 A 5730 ARB1067 SKIN DOUG DC10 DC1010 3022110 WP RT WING LE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 RT WING EXT L/E CRACK ON SKIN (NEAR OLD REPAIR). REPAIRED SKIN IAW SRM 57-10-00 VOL I FIG 68 SHT 2. 2 L 7 3 4F A22WE 200805141 20080514 1 NM 2008 5 14 AALA200800900 1 20080410 A 3350 0201720002 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 932AN 29530 ATL - EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 200805141 20080514 1 EA 2008 5 14 MALA080086 1 20080429 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 8943A 7943 RT 625 OBLIQUE ANGLE IS CRACKED APPROX 1 INCH. REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE P/N 601-35012-52 IAW CRJ20 0 SRM 51-42-06. 2 L 7 2 4F RT A21EA 200805141 20080514 1 NE 2008 5 14 DXTA200803031 2 20080428 A 7320 GASKET CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE LEAKING E DXTA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 07 648QS 2822 5605574 DURING T/O ROLL, RT N1 ROLLED BACK FROM 90.8 (T/O PWR SETTING) TO 80 PERCENT N1. REMOVED AND REPLACED BOU TORQUE MOTOR BASE GASKET IAW MM 75-30-01 C/W RUNS ALL CHECKS GOOD LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 2008051400008 20080514 00008 NM 2008 5 14 2008UALA02450 1 20080428 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 FAILED A UALA O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 WP 29 220UA 30223 LEFT GENERATOR DROPPED OFF LINE. APU ON AND FLIGHT WILL CONTINUE. FOUND FAULTY IDG. REPLACED NR 1 IDG. RAN OP CHECKS. OKAY FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008051400009 20080514 00009 NM 2008 5 14 2008UALA02451 1 20080427 A 8011 8088846 STARTER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 ENGINE MISRIGGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 NR 1 ENGINE START VALVE APPEARS TO BE ASSEMBLED IMPROPERLY TO ALLOW MANUAL START, VALVE DOES NOT ALIGN WITH TUBE IN COWL . FOUND ALIGNMENT TANG TO BE 30 DEGREES OFF WHEN ASSEMBLED IN SHOP. REPLACED STARTER VALVE REF MM 80-11-02, OPS CHECKS OK.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008051400013 20080514 00013 NM 2008 5 14 2008UALA02452 1 20080427 A 5350 60252 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 EMERGENCY EXIT LIGHT STRIP ON FLOOR AT THE G6 GALLEY IS INOP. REMOVED AND REPLACED EEL STRIP AT G6 GALLEY FLOOR. OPS C HECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2008051400015 20080514 00015 NM 2008 5 14 2008UALA02453 1 20080427 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD GALLEY DOOR AFT FRAME CRACKED AT INBD SIDE OF OPENING FOR STOP FITTING, 3RD FROM BOTTOM. BLENDED DAMAGE FROM FRAME AND ACCMP'D NDT. FABRICATED AND INSTALLED EXTERNAL DOUBLER TO FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2008051400027 20080514 00027 CE 2008 5 14 DXTA200803014 1 20080423 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 151QS RK422 ELECTRICAL BURNING ODOR COMING FROM VANITY LIGHT AREA OF THE LAVATORY. PASSENGERS CAME UP TO THE COCKPIT TO COMPLAIN ABO UT THE ODOR. WE COULD DETECT IT FROM THE COCKPIT. TROUBLESHOT AND PERFORMED A DETAIL INSPECTION OF THE WHOLE LAV. AREA, INCLUDING SIDEWALL, ENGINE BLEED LINE, PC BOARDS, RELAYS, ELECTRICAL WIRES ETC, PERFORMED OPS CHECK OF A/C, BLEED SYSTEM AND ALL ELECTRICAL, COULD NOT DUPLICATE. WORK DONE IAW HAWKER 400XP MM 21-00 2 H 7 2 4F 4 F RT A16SW E25EA 2008051400032 20080514 00032 EU 2008 5 14 08FDEA01603 1 20080425 A 5753 A5796001220000 SKIN AIRBUS 300 A300F4605R 3930327 EU LT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 LEFT WING INBD FLAP HAS TWO DENTS LOCATED 65 1/2 INCH AND 61 1/2 INCH OUTBD END AND 14 INCH AND 16 1/4 INCH FROM THE T/E THAT HAVE BEEN FOUND OUT OF LIMITS ON N/R N00417, LABELED D/E ON N/R N00417. FABRICARED DOUBLER & FILLER IAW SRM 57-50- 00 FIG 205 PG 219. LOCATED & DRILLED IAW SRM 57-50-00. ALODINED IAW SRM 51-21-10. PRIMED & PAINTED IAW SRM 51-23-10. INSTALLED THE DOUBLER & FILLER IAW SRM 57-50-00. 2 L 7 2 4F RT A35EU 2008051400039 20080514 00039 NM 2008 5 14 ASAA0842920 1 20080501 A 5755 6546451707 SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 LEFT WING NR 3 SPOILER HAS BUMPS ON UPPER SURFACE O/B AREA. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008051400040 20080514 00040 NM 2008 5 14 ASAA0842921 1 20080501 A 5755 6546451707 SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 LEFT WING NR 3 SPOILER DENTS ON UPPER SURFACE I/B SIDE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER BONDED IAW B73 7 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008051400041 20080514 00041 NM 2008 5 14 ASAA0842922 1 20080501 A 5755 654645262A SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 LEFT WING NR 4 SPOILER LOWER SURFACE HAS MULTIPLE DENTS. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER BONDED IAW B7 37 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008051400050 20080514 00050 EU 2008 5 14 08FDEA01663 1 20080429 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 MAIN CARGO COMPT HAS CORROSION ON THE BOTTOM OF THE SEAT TRACK AT RBL 38 INCHES AND FRAME 56, 10 INCHES, AND ANOTHER SPO T 20 INCHES AFT OF IT. REMOVED AND REPLACED THE SEAT TRACK SECTION REF SRM 53-10-16 SHEET 1. ORIGINAL SEAT TRACK FOUND TO BE OUT OF LIMITS REF 53-10-16 FIG 101. 2 L 7 2 4F RT A35EU 2008051400053 20080514 00053 EU 2008 5 14 08FDEA01664 1 20080429 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 MAIN CARGO COMPT SEAT TRACK SCALLOPS ARE GOUGED AND ELONGATED AT FRAME C 58, 15 INCHES, RBL 37 INCHES. REMOVED AND REPL ACED THE SEAT TRACK SECTION IAW SRM 51-40-21 PARAGRAPH 7. 2 L 7 2 4F RT A35EU 2008051400054 20080514 00054 EU 2008 5 14 08FDEA01665 1 20080429 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 MAIN DECK FLOOR TRACK RBL 80, FRAME 44 HAS CORROSION AT THE UPPER CENTER OF THE TRACK. REMOVED CORRODED TRACK RAIL IAW SRM 51-72-10. LOCATED NEW TRACK RAIL IAW SRM 51-72-10 AND AIRBUS DWG 15A53813871. INSTALLED NEW TRACK RAIL IAW SRM 51- 72-10 AND DWG 15A53813871. ALODINED IAW SRM 51-21-10. APPLIED PRIMER IAW SRM 51-23-10. APPLIED PAINT IAW SRM 1-23-10. 2 L 7 2 4F RT A35EU 2008051400068 20080514 00068 NM 2008 5 14 2008UALA02458 1 20080425 A 2750 COMPUTER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ECAM FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 824UA 965 SLAT SYS 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. FOUND FAILURE OF SFCC-2. 22CV. REPLACED SFCC-2. 22CV, OPS TESTED NORMAL . 2 L 7 2 4F 4 F RT A28NM E40NE 2008051400073 20080514 00073 NM 2008 5 14 CALA0800432 1 20080509 A 7830 491B1330011 WEB BOEING 767 767224 1385170 NM THRUST REVERSER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76153 30432 NUMBER 1 ENGINE INBOARD C-DUCT BULKHEAD FORWARD UPPER ATTACH WEB CRACKED AT 1 O`CLOCK POSITION. NUMBER 1 ENGINE INBOARD C-DUCT BULKHEAD FORWARD UPPER ATTACH WEB AT 1 O`CLOCK POSITION REPAIRED PER MRAS CMM 78-32-02, REPAIR 024 AND HFEC NO C RACK FOUND. 2 L 7 2 4F RT A1NM 2008051400080 20080514 00080 NM 2008 5 14 CALA0800440 1 20080511 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 LEFT SIDE BS 867 I/B ATTACH FASTENER HOLE ON AIR CONDITIONING (A/C) BRACKET CRACKED. REPAIRED LEFT SIDE BS 867 I/B ATTA CH FASTENER HOLE ON A/C BRACKET PER EA5310-04498. 2 L 7 2 4F RT A16WE 2008051400090 20080514 00090 NM 2008 5 14 LYNX00013 1 20080429 A 3350 SWITCH BOMBDR DHC8 DHC8402 1390042 NM CABIN DEFECTIVE A 3LYA K NONE O OTHER IN INSP/MAINT 1 NM 21 509LX 594 4184 PILOT REPORT - UNABLE TO TURN OFF EMERGENCY LIGHTS. MAINTENANCE REPLACED EMERGENCY LIGHT SWITCH BEHIND FWD FLIGHT ATTEN DANT SEAT. OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2008051400092 20080514 00092 NE 2008 5 14 TRAX200800591 2 20080502 A 7200 CF343B1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* 30015 NE RIGHT MALFUNCTIONED A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 841AS 7300 872777 CLIMBING THROUGH 9000 OUT OF ATL, SUFFERED RIGHT ENGINE VIOLENT BANG AND COMPLETE LOSS OF N1, ITT SPIKED OVER 960 DEG WI TH RED ICON. PERFORMED ENG DAMAGE IN FLIGHT QRH PROCEDURE EXPERIENCED SUBSEQUENT SMALLER BANGS WITH ERRATIC N1 PRIOR TO SHUT DOWN , WITH N1 RETURNING TO NIL EACH TIME.---[AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. DEFECT TRA NSFERRED TO W/O 89988 N/R 00001 FROM AFDL 372229. DEFECT TRANSFERRED TO W/O 89988 N/R 00001 FROM AFDL 372229. REMOVED AND REPLACED NR 2 ENGINE IAW CRJ 200 AMM 71-00-00. 2 L 7 2 4F 4 F RT A21EA 2008051400100 20080514 00100 EA 2008 5 14 TRAX200800596 1 20080504 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OBSTRUCTED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 MAIN PAX DOOR STILL STICKING IN CLOSED POSITION, REQUIRES EXCESSIVE FORCE TO OPEN. FOUND BOTTLE CAP IN DOOR FRAME. REM OVED CAP, OPS CHECK GOOD REF CRJ-200MM 52-11-0. 2 L 7 2 4F RT A21EA 2008041500009 20080415 00009 EA 2008 4 15 TRAX200800455 1 20080321 A 5712 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 AAR - 7006 - RIGHT BATT RIB CRACKED. UPON FURTHER EVALUATION, FOUND RIGHT BATT RIB PREVIOUS REPAIR DOUBLER TO BE CRACKE D. REMOVED CRACKED REPAIR DOUBLER FROM RIGHT BATT RIB & DUPLICATED SERVICEABLE REPAIR DOUBLER FROM P/N S6144-4 .063 IAW REO 601R-57-51-046. INSTALLED SERVICEABLE REPAIR DOUBLER IAW REO 601R-57-51-046. SUPPLEMENTAL SDR CLOSED 4/3/08. 2 L 7 2 4F RT A21EA 2008041500012 20080415 00012 EU 2008 4 15 USAA920080728 1 20080328 A 5347 A532274005184 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AY 337 BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 5054 / FR 62 - BS 5584 / FR 72, +Y2462. REPAIRED CABI N SEAT TRACK, BS 5054 / FR 62 - BS 5584 / FR 72, +Y2462 IAW A330 SRM 53-00-15. 2 L 7 2 4F RT A46NM 2008041500014 20080415 00014 NM 2008 4 15 SB08018 1 20080403 A 5610 5893543129 WINDSHIELD BOEING 737 7374B7 1384702 NM COCKPIT CRACKED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 435US 12601 12601 24557 PHL FLT 954 EN ROUTE FROM FLL TO PHL, CREW REPORTED THE FIRST OFFICER'S NR 1 WINDSHIELD OUTER PANE ARCED AND THEN CRACKE D. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICER'S NR 1 WINDSHIELD PER JO B CARD. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 2008041500021 20080415 00021 EA 2008 4 15 TRAX200800496 1 20080407 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA CABIN LOOSE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 723EV 10132 ASD 'EXIT' PLACARD COMING LOOSE. REPLACED PLACARD IAW AMM 11-30-02. 2 L 7 2 4F RT A21EA 2008041500029 20080415 00029 NM 2008 4 15 USAA920080694 1 20080314 A 5312 65163007 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED BULKHEAD WEB, BS 178, RBL 5.7, WL 212 AND RBL 9, WL 234. REPAIRED BULKHEAD WEB , BS 178, RBL 5.7, WL 212 AND RBL 9, WL 234 IAW B737 SRM 53-10-08-2R10. 2 L 7 2 4F RT A16WE 2008041500033 20080415 00033 NM 2008 4 15 USAA920080731 1 20080312 A 5311 6546526 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 400, S8L - S9L AND S8R - S9R. REPAIRED FRAME, BS 400, S8L - S9L AND S8R - S9R IAW USAIRWAYS EA 5311-01019. 2 L 7 2 4F RT A16WE 2008041500040 20080415 00040 NM 2008 4 15 USAA920080739 1 20080312 A 5311 6546548 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 747, S8L - S9L. REPAIRED FRAME, BS 747, S8L - S9L IAW USAIRWAYS EA 5 311-01019. 2 L 7 2 4F RT A16WE 2008041500049 20080415 00049 EA 2008 4 15 TRAX200800485 1 20080403 A 2930 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 841AS 7300 NR 1 HYD LOW PRESS MSG, RAN FOR APPROX 30 MINUTES. EN ROUTE TO ATL A/C DIVERTED TO ORD DUE TO MTC. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 2008041500052 20080415 00052 NM 2008 4 15 SWAA081846 1 20080407 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 284WN 32535 EEPLS LENS MISSING AT ROW 3 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008041500054 20080415 00054 NM 2008 4 15 SWAA081864 1 20080407 A 5311 6546554 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, STR 27R. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 2008041500067 20080415 00067 NM 2008 4 15 SWAA08860 1 20080407 A 5311 6545805 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 2R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008041500076 20080415 00076 NM 2008 4 15 SWAA081882 1 20080408 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008041500078 20080415 00078 NM 2008 4 15 SWAA081883 1 20080408 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EXTERIOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS P ER MM. 2 L 7 2 4F RT A16WE 2008041500093 20080415 00093 NM 2008 4 15 SWAA081889 1 20080408 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND STRINGER 15R CRACKED AT BS 380. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008041500096 20080415 00096 NM 2008 4 15 SWAA081875 1 20080408 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041500110 20080415 00110 NM 2008 4 15 SWAA081899 1 20080409 A 5311 6978188 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 420, STR 13R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500128 20080415 00128 EA 2008 4 15 TRAX200800494 1 20080407 A 5240 LATCH CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 870AS 7530 EXTERNAL SERVICE DOOR AFT LATCH BROKEN. 2 L 7 2 4F RT A21EA 2008041500135 20080415 00135 EA 2008 4 15 TRAX200800508 1 20080408 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 AAR - 2080 - CRACK IN ATTACH ANGLE BETWEEN 280 FRAME AND FLOORBEAM AT LBL 9 I/B SIDE (MARKED). REMOVED CRACK ATTACH ANG LE. REPLACED ATTACH ANGLE IAW REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2008050600002 20080506 00002 NM 2008 5 6 08FDEA01643 1 20080428 A 2160 6075103 CONTROL BOX BOEING 727 7272S2F 1384O81 NM CABIN TEMP FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 215FE 22936 FL 340 SCHEDULE CABIN 5200 FEET CABIN UNCONTROLLED CLIMB TO 126500 FEET. REMOVED AND REPLACED TEMP CNTL BOX IAW MM 21-5 5-091-5, CONTROL BOX AND THE 35 DEGREE CONTROL VALVE OPS CHECK NORMAL. REPLACED LEFT FLOW CONTROL MODULATING AND SHUTO FF VALVE REF M/M 36-12-061, OPS CKS GOOD. PERFORMED HIGH PRESSURE BLEED CONTROL CHECK PER JRH CHAPTER 8. OPS CKS GOOD. ALSO, PERFORMED PRESSURIZATION CONTROL SYSTEM TEST REF 21-31-000. ALL CHECKS GOOD, OK FOR SERVICE. 2 L 7 3 4F A3WE 2008041500143 20080415 00143 EA 2008 4 15 TRAX200800516 1 20080409 A 5220 DOOR CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT FAILED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 723EV 10132 RIGHT OVERWING EMERGENCY DOOR FAILED FUNCTIONAL CHECK. 2 L 7 2 4F RT A21EA 2008041500146 20080415 00146 EA 2008 4 15 TRAX200800521 1 20080409 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 835AS 7258 OVERWING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008041500156 20080415 00156 NM 2008 4 15 SWAA081908 1 20080410 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503B, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500164 20080415 00164 EA 2008 4 15 A6WA200840224 1 20080320 A 2720 CONTROL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA RUDDER MALFUNCTIONED A A6WA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 31 453AW 7838 ON TAKEOFF ROLL, FULL RUDDER DEFLECTION UNABLE TO MAINTAIN CENTERLINE. ABORTED TAKEOFF AT APPROXIMATELY 60 KNOTS, MAX B TMS READING = 2. CROSSWING ABOUT 10 KNOTS. OPS CHECK OF NWS IAW 32-51-00. OP CHECK GOOD. PERFORMED OPS CHECK OF RUDD ER CONTROL SYSTEM IAW 27-21-00. PERFORMED OPS CHECK OF SPOILER SYSTEM IAW 27-61-00, OPS CHECK GOOD. PERFORMED OPS CHEC K OF AILERON SYSTEM IAW 27-11-00. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 2008041500189 20080415 00189 NM 2008 4 15 08FDEA01397 1 20080414 A 5311 ACA73511 FRAME DOUG MD11 MD11F 3023600 NM BS 535 L21L CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 525FE 48565 MAIN DECK, LEFT FRAME AT STATION 535, LONGERON 21 LT, ONE EACH CHAFED MARK FOUND CAUSED BY 9G NET YOKE. REPAIRED AS P ER DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041500191 20080415 00191 EA 2008 4 15 A6WA200840185 1 20080311 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 590 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 CRACK FOUND ON THE FLOORBEAM STRUCTURE AT FS 590, LBL 43 AND WL 73. FLOOR SUPPORT STRUCTURE REPAIRED IAW REO 601R-53-61 -433. (M) 2 L 7 2 4F RT A21EA 2008041500192 20080415 00192 NM 2008 4 15 AALA200800777 1 20080331 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 938AN 29533 DFW - EMERGENCY LIGHT AT AFT LEFT ENTRY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT LEFT ENTRY D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008041500193 20080415 00193 WP 2008 4 15 AALA200800781 1 20080326 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 443AA 49469 EMERGENCY LIGHT BATTERY PACK AT OVERHEAD BIN SEAT 29D FAILED OPERATIONAL CHECK. REPLACED BATTERY PACK FOR EMERGENCY LIG HTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008041500194 20080415 00194 NM 2008 4 15 AALA200800788 1 20080401 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 782AN 30003 DFW - EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041500196 20080415 00196 NM 2008 4 15 SWAA081910 1 20080410 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 540, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008041500200 20080415 00200 NM 2008 4 15 SWAA081911 1 20080410 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 320, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041500203 20080415 00203 NM 2008 4 15 SWAA081925 1 20080410 A 5311 65C34356 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 482A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500207 20080415 00207 NM 2008 4 15 SWAA081926 1 20080410 A 5311 6546555 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008051400103 20080514 00103 NM 2008 5 14 USAA920081014 1 20080420 A 5320 146N852217 WEB BOEING 757 7572S7 1384962 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - CORROSION ON WEB, BS 1380 - BS 1450, RBL 23. REPLACED WEB, BS 1380 - BS 1450, RBL 23 I AW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008051400104 20080514 00104 NM 2008 5 14 SWAA082524 1 20080507 A 2730 65C379714 FEEL UNIT BOEING 737 7373H4 1384600 NM ELEVATOR FAULTY A SWAA K NONE F FLT CONT AFFECTED CL CLIMB 1 SW 29 315SW 23337 DURING ROTATION A 2 INCH DEAD BAND INDICATION IN ELEVATOR. REMOVED AND REPLACED ELEVATOR FEEL & CENTERING UNIT PER MM. 2 L 7 2 4F RT A16WE 2008051400108 20080514 00108 EU 2008 5 14 NSVA2008024 1 20080505 A 2613 SEAL SAAB SF340 340B 7860101 EU TAILPIPE SENSOR MISSING A NSVA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 334CJ 340B334 RT TAIL PIPE HOT LIGHT ILLUMINATED ON CLIMB-OUT. SEALED TAIL PIPE SENSOR IAW SB 340-26-029, AFTER FINDING THE BACK OF T HE SENSORS EXPOSED TO THE ELEMENTS. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 2008051400111 20080514 00111 NM 2008 5 14 CALA0800442 1 20080511 A 5311 143A1110 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23708 28769 FRAME CRACKED AT STA 380 ABOVE S9R B737-53-3-0739. REPAIRED CRACKED FRAME BS 380 S9R PER EC/RA 5310-04763. 2 L 7 2 4F RT A16WE 2008051400112 20080514 00112 NM 2008 5 14 DHL2008780004 1 20080512 A 5320 BAC15201247 STIFFENER BOEING 727 727223 1384074 NM BS 920 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 REMOVED CORRODED VERTICAL STIFFENER AT LT W/WELL KEEL AREA BS 920, FABRICATED NEW STIFFENER, AND INSTALLED PER B727 SRM 53-10-2 FIG 4, 51-30-5, 51-30-2, AND 51-10-2. 2 L 7 3 4F A3WE 2008051400113 20080514 00113 NM 2008 5 14 CALA0800445 1 20080511 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 LEFT SIDE BS 747 I/B ATTACH FASTENER HOLE ON AIR CONDITIONING (A/C) BRACKET CRACKED. REPAIRED CRACKED FRAME AT LEFT BS 747 I/B ATTACH FASTENER PER EA5310-04498. 2 L 7 2 4F RT A16WE 2008051400117 20080514 00117 NM 2008 5 14 AALA200800901 1 20080410 A 3350 0201720002 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 932AN 29530 ATL - EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008051400120 20080514 00120 NM 2008 5 14 AALA200800910 1 20080410 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 756AM 30264 DFW - EMERGENCY LIGHTS AT OVERHEAD LEFT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK M33093 FOR EMERGENCY LIGHTS AT O VERHEAD LEFT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051400121 20080514 00121 NM 2008 5 14 CALA0800448 1 20080511 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 RIGHT SIDE BS 440 I/B ATTACH FASTENER HOLES ON AIR CONDITIONING (A/C) BRACKET CRACKED. REPAIRED FRAME BS 440 RIGHT AT A /C RAIL BRACKET PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008051400122 20080514 00122 NM 2008 5 14 SWAA082526 1 20080511 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 219WN 32490 DURING SCHEDULED MV1 CHECK, FOUND EEPLS LIGHT ASSY BROKEN AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008051400123 20080514 00123 NM 2008 5 14 AALA200800920 1 20080410 A 5330 146T32102 SKIN BOEING 767 767223 1385123 NM BS 1984-1093 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AA 22333 AFW - FUSELAGE SKIN AT STATION 1084 TO 1093 BETWEEN STRINGER 37 LEFT AND 38 LEFT HAD CORROSION ON THE OUTER AND INNER SU RFACE OF SKIN. AREA OF DISCREPANCY IS 11.8 INCH BY 2 INCH. REPAIRED PER MRB 767 3179 DATED 3 APR 2008. 2 L 7 2 4F RT A1NM 2008051400124 20080514 00124 NM 2008 5 14 AALA200800923 1 20080411 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 199AN 32393 MIA - EMERGENCY LIGHT AT SEAT 23D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051400125 20080514 00125 NM 2008 5 14 AALA200800922 1 20080411 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 199AN 32393 MIA - EMERGENCY LIGHT AT SEAT 23D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051400137 20080514 00137 NM 2008 5 14 SWAA082560 1 20080511 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008051400138 20080514 00138 NM 2008 5 14 SWAA082542 1 20080511 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2008051400140 20080514 00140 NM 2008 5 14 SWAA082541 1 20080511 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 2008051400156 20080514 00156 NM 2008 5 14 SWAA082551 1 20080511 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008051400158 20080514 00158 2008 5 14 SWAA082552 4 20080511 A 2565 6949956 CABLE BOEING 737 7373Q8 1384670 NM EVAC SLIDE MISROUTED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 2008051400160 20080514 00160 NM 2008 5 14 SWAA082553 1 20080511 A 3350 311500 LENS BOEING 737 7373G7 1384595 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 1 DEF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008051400179 20080514 00179 NM 2008 5 14 SWAA082570 1 20080508 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 470WN 33860 DURING SCHEDULED MV2 CHECK, FOUND LT LOWER AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008051400181 20080514 00181 NM 2008 5 14 DHL2008760534 1 20080419 A 5330 SKIN BOEING 727 7272B7 138407L NM UNKNOWN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 ACCOMPLISHED SKIN REPAIR TO L1 DOOR UPPER HINGE CUT-OUT, BS 303.9 AT WL 251.0 REMOVED EXISTING REPAIR AND FABRICATED AND INSTALLED NEW REPAIR AND FILLER PER ASTAR EVA B25300054 REV IR, AND BOEING TELEX NR 1-803757076-10, WITH APPROVAL PER F ORM 8100-9 DATED 4/24/2008. 2 L 7 3 4F A3WE 2008051400183 20080514 00183 EA 2008 5 14 REXA200800012 1 20080505 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA NOSE MALFUNCTIONED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8515F 7515 ON APPROACH WHEN SELECTING GEAR DOWN NOSE GEAR DID NOT EXTEND. FOLLOWED QRH MANUAL EXTENSION OF GEAR WITH THREE GREENS. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. GEAR RETRACTION SYSTEM DEFERRED PER MEL 32-30-01. 2 L 7 2 4F RT A21EA 2008051400187 20080514 00187 NM 2008 5 14 AALA200800909 1 20080410 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 756AM 30264 DFW - EMERGENCY LIGHTS AT FORWARD FIRST CLASS GALLEY INOPERATIVE. REPLACED BATTERY PACK M33096 FOR EMERGENCY LIGHTS AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051400189 20080514 00189 EU 2008 5 14 MALA080071 1 20080505 A 5311 FRAME SAAB SF340 340B 7860101 EU BS 710 BENT A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 FRAME BOTTOM IN CARGO AT STA 710 FOUND BENT ON TOP. FRAME (BOTTOM) IN CARGO AT STA 710 REPAIRED AS PER DRM 53-70-30 AND INSTALLED WITH SOLID RIVETS AS PER SRM 51-40-21 AND EO S53560 LPI INSPECTION DONE EO S53560 AND NO DEFECT FOUND 1132. 2 L 7 2 4T RT A52EU 2008051400190 20080514 00190 EU 2008 5 14 MALA080072 1 20080505 A 5523 TAB SAAB SF340 340B 7860101 EU LT ELEVATOR DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 LT ELEVATOR TAB T/E DAMAGED 8 INCH FROM INBOARD ENGINE. LT ELEVATOR TT T/E INBOARD REPAIRED WITHIN LIMITS OF SRM 51-70- 51 AND REPAIRED IAW EO S51029 ELEVATOR STATIC BALANCE C/OUT AS PER 51-60-00. 2 L 7 2 4T RT A52EU 2008051400193 20080514 00193 WP 2008 5 14 AALA200800974 1 20080415 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7530 49922 LGA - EMERGENCY LIGHT AT SEAT 17D INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008051400195 20080514 00195 NM 2008 5 14 AALA200800972 1 20080415 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 622AA 24580 DFW - EMERGENCY LIGHT AT SEAT 2EF BULLNOSE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 2EF BULLNOSE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051400204 20080514 00204 EU 2008 5 14 08FDEA01771 1 20080506 A 5315 A53781041200 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 673FE 780 AFT CARGO COMPARTMENT FLOORBEAM HAS .500 INCH CRACK AT FRAME 64 BETWEEN SEAT TRACKS NR 4 RT AND NR 5 RT REMOVED CRACK AN D INSTALLED CROSSBEAM REPAIR AT FRAME 64 BETWEEN SEAT TRACKS NR 4 RT AND NR 5 IAW A300-600 SRM 53-10-15, FIG 211. 2 L 7 2 4F RT A35EU 2008051400209 20080514 00209 NM 2008 5 14 UIEA200500165 1 20080505 A 5320 T08A003961 INTERCOSTAL BOEING 747 7472D7B 1384803 NM BS 1700-1720 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK 4R DOOR CUTOUT BS 1700 TO 1720 STRINGER 14R TO 15R INTERCOSTAL FOUND CRACKED. REPLACED INTERCOSTAL IAW 51-10- 01. 2 L 7 4 4F RT A20WE 2008051400210 20080514 00210 NM 2008 5 14 UIEA200800162 1 20080424 A 2611 SMOKE DETECTOR BOEING 747 747243B 1384830 NM MALFUNCTIONED A UIEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 15 540MC 22508 DIVERSION TO ICT DUE TO MAIN DECK CARGO SMOKE DETECTOR NR 1 FIRE WARNING CAME ON AFTER REACHING CRUISE ALTITUDE (FL410). INSPECTED AREA NO SIGNS OF SMOKE OR FUMES. DIVERTED TO ICT AT COMPANY REQUEST AS A PRECAUTION. LIGHT EXTINGUISHED AF TER LANDING. THE ABOVE ITEM HAS BEEN TRANSFERRED FROM LOG PAD 0159 PAGE NUMBER 367269. 2 L 7 4 4F RT A20WE 2008051400211 20080514 00211 NM 2008 5 14 UIEA200800164 1 20080424 A 2611 30284R9B SMOKE DETECTOR BOEING 747 747243B 1384830 NM CARGO BAY FAILED A UIEA O OTHER N FALSE WARNING CR CRUISE 1 EA 15 540MC 22508 NR 1 MAIN DECK CARGO SMOKE DETECTOR LIGHT CAME ON AGAIN AT CRUISE APPROXIMATELY 50 MINUTES INTO FLIGHT. REMAINED ON. R EF DMI M08-058. REPLACED NR 1A SMOKE DETECTOR PER 26-14-01 SYSTEM. OPS CHECKED NORMAL PER MM 26-14-00. ALSO IN ITEM M 3 REPLACED 1B SMOKE DETECTOR S/N 34151. 2 L 7 4 4F RT A20WE 2008041500210 20080415 00210 NM 2008 4 15 SWAA081916 1 20080410 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041500213 20080415 00213 NM 2008 4 15 SWAA081930 1 20080410 A 3350 65C27093 COVER BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008041500216 20080415 00216 NM 2008 4 15 SWAA081918 1 20080410 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 759GS 30544 DURING SCHEDULED MV2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008041500219 20080415 00219 NM 2008 4 15 USAA920080749 1 20080324 A 5320 6547973101 SHEAR WEB BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CORROSION ON CABIN SHEAR WEB, BS 616 - BS 639, S17L, WL 208. REPLACED CABIN SHEAR WEB, BS 616 - BS 639, S17L, WL 208 IAW B737 SRM 53-60-13. 2 L 7 2 4F RT A16WE 2008041500220 20080415 00220 NM 2008 4 15 USAA920080750 1 20080313 A 5320 65558853 SHEAR WEB BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CORROSION ON CABIN SHEAR WEB, BS 767 - BS 787, S17L, WL 208. REPLACED CABIN SHEAR WEB, BS 767 - BS 787, S17L, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041500223 20080415 00223 NM 2008 4 15 USAA920080682 1 20080314 A 5320 65535953 REVEAL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCM - MAJOR REPAIR-C18- R-1 DOOR CUTOUT FWD UPPER REVEAL CRACKED. REPLACED REVEAL IAW SRM 51-40-02-0G, FIG 3. 2 L 7 2 4F RT A16WE 2008041500224 20080415 00224 NM 2008 4 15 USAA920080683 1 20080311 A 5753 6546431280SP SKIN BOEING 737 7373G7 1384595 NM FOREFLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCM - MAJOR REPAIR-C18-NR 6067164, RIGHT T/E OUTBOARD FORE FLAP IS DELAMINATED UPPER SURFACE, WBL 292.69 - 295.69. INST ALLED REPAIR DOUBLER IAW SRM 51-70-10-2R3 & 2R4, FIG 201. 2 L 7 2 4F RT A16WE 2008041500230 20080415 00230 EU 2008 4 15 SA08025 1 20080405 A 2752 791A000005 ACTUATOR AIRBUS A319 A319112 3930323 EU T/E FLAP MALFUNCTIONED A USAA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 EA 19 733UW 23921 1240 1205 FLIGHT 835, BOS-SJU, ON APPROACH INTO SJU THE FLAPS DEPLOYED BUT THE SLATS DID NOT. THE FLIGHT DID A GO-AROUND AND AN E MERGENCY WAS DECLARED. THE FLIGHT LANDED WITHOUT ANY FURTHER PROBLEMS. MAINTENANCE REPLACED THE LEFT NUMBER ONE FLAP A CTUATOR FOR POPPED TORQUE INDICATOR. 2 L 7 2 4F RT A28NM 2008041500231 20080415 00231 NM 2008 4 15 BB08048 1 20080404 A 3350 LIGHT BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 252AU 24765 CLT - THE EMERGENCY FLOOR LIGHT STRIPS AT SEAT ROWS 9 RIGHT THROUGH 11 RIGHT, AND SEAT ROWS 20 RIGHT THROUGH 26 RIGHT, W ERE FOUND INOPERATIVE. MAINTENANCE REPAIRED THE EMERGENCY FLOOR LIGHTS FOR ALL AFFECTED ROWS. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A1NM 2008041500233 20080415 00233 NM 2008 4 15 BB08050 1 20080405 A 2560 SETSCREW BOEING 757 757225 1384959 NM MEGAPHONE BINDING A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 915AW 22209 DCA - THE AFT MEGAPHONE WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE MIC SET SCREW. OPERATIONALLY CHECKS GOOD. 2 L 7 2 4F RT A2NM 2008041500235 20080415 00235 NM 2008 4 15 USAA920080758 1 20080327 A 5312 BEAM BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 460UW 25024 PIT - MAJOR REPAIR - CRACKED BULKHEAD LEFT VERTICAL BEAM WEB, BS 178, LBL 17, WL 225. REPAIRED BULKHEAD LEFT VERTICAL B EAM WEB, BS 178, LBL 17, WL 225 IAW B737 SRM 53-10-08. 2 L 7 2 4F RT A16WE 2008041600008 20080416 00008 SO 2008 4 16 CHQA200800074 1 20080410 A 5610 163500109 WINDSHIELD EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COCKPIT CRACKED A CHQA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 11 285SK 18168 18168 145435 CAE312124 FLIGHT 5801, BDL TO CLE - IN CRUISE AT FL240, WITH WINDSHIELD HEAT ON, THE CREW HEARD A LOUD POP AND NOTICED THAT THE CA PTAIN'S WINDSHIELD HAD SHATTERED (SPIDER WEBBED). THE FLIGHT DIVERTED TO SYR AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD AND PRESSURE CHECKED THE AIRCRAFT, AND THERE WERE NO FURTHER DEFECTS. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008041600009 20080416 00009 SO 2008 4 16 CHQA200800075 1 20080410 A 3230 355022002 ELECTRONIC UNIT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL MLG FAULTY A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 292SK 17096 17096 145488 CAE311794 FLIGHT 7827, IAD TO CMH - AFTER TAKEOFF, CREW ATTEMPTED TO RAISE THE LANDING GEAR AND RECEIVED A "LG AIR/GND FAIL" MESSA GE AND THE GEAR WOULD NOT RETRACT. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT T HE FAULT TO THE LGEU USING THE CMC. THE LGEU WAS REPLACED AND THE TEST FLIGHT WAS SUCCESSFUL. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008041400127 20080414 00127 NM 2008 4 14 DHL2008753518 1 20080410 A 5740 BRACKET BOEING 727 727223 1384074 NM KRUEGER FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 753DH 22468 NR 3 KRUEGER FLAP ACTUATOR I/B MOUNT ANGLE (BRACKET) CRACKED. REMOVED, FABBED AND INSTALLED IAW BOEING DWG 65-16263 REV C AND B727 SRM 51-20-1 FIG 2, 51-10-2 AND 51-30-2 MATERIAL 7075 T6 .063 INCH 9 INCH BY 6 1/4 INCH. 2 L 7 3 4F A3WE 2008041400128 20080414 00128 NM 2008 4 14 TSAA0827019 1 20080408 A 2751 2061141 INDICATOR BOEING 737 737282C 13844AU NM TE FLAP FAILED A TSAA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 WP 13 826AL 23051 CARGO FLIGHT 940 HNL-KOA, ON DESCENT TO KOA, THE CREW WAS ONLY ABLE TO EXTEND THE FLAPS TO 8 UNITS. THE CREW DECLARED A N EMERGENCY AND RETURNED TO HNL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR AND OPERATIONALLY CHECKED THE FLAPS EXTENSION AND RETRACTION PER AMM 27-58-41. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 2008041400148 20080414 00148 SO 2008 4 14 SWIA200819463 1 20080406 A 2133 OUTFLOW VALVE EMB 120 EMB120ER 3260203 SO CABIN PRESSURE MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 308SW 120326 FLT 3695 - AUTO PRESSURIZATION FAILED ON CLIMB-OUT. REPLACED ELECTRONIC ALTITUDE CONTROLLER AND ELECTROPNEUMATIC OUTFLO W VALVE IAW AMM 21-30-03. OPS CHECK GOOD, PN 2091G010800, SN/OFF 205, PN 22201T011400, SN/OFF 527. 2 L 7 2 4T RT A31SO 2008041400161 20080414 00161 WP 2008 4 14 NWAA080529859 1 20080410 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 768NC 47729 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE COCKPIT WAS INOPERATIVE. MAINTENANCE REPLACED C OCKPIT EMERGENCY LIGHTING BATTERY PACK AND LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 2 L 7 2 4F RT A6WE 2008041400167 20080414 00167 NM 2008 4 14 F3LA200800142 1 20080401 A 3350 BR9279106 COVER AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE EMERGENCY LIGHTS BROKEN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 343 1841 DURING C4 S1 C CHECK, INSPECTION REPORTED A CRACK WAS FOUND IN THE EMERGENCY EXIT LIGHT LENS COVER LOCATED ON THE AFT SI DE OF THE FORWARD RIGHT DOOR FRAME. MAINTENANCE REMOVED AND REPLACED THE LENS COVER IN ACCORDANCE WITH AMM 33-51-13 PB 400-001. THE LIGHT WAS TESTED IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-13-400-001 AND OPERATIONALLY TESTED OKAY . 2 L 7 2 4F 4 F RT A28NM 2008041500050 20080415 00050 EA 2008 4 15 TRAX200800486 1 20080404 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA ASD BINDS A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 VERBALLY REPORTED BY FELLOW MTC CONTROLLER MERRICK REPORTED BY STATION PERSONNEL THAT ASD DIFFICULT TO OPERATE. 2 L 7 2 4F RT A21EA 2008041500071 20080415 00071 EA 2008 4 15 TRAX200800487 1 20080405 A 5240 DOOR CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 SERVICE DOOR HARD TO OPEN. FLT 4484 DEL 36 MINS. 2 L 7 2 4F RT A21EA 2008041500079 20080415 00079 NM 2008 4 15 SWAA081867 1 20080408 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULE SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500092 20080415 00092 NM 2008 4 15 SWAA081888 1 20080408 A 5313 BAC1498 STRINGER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND STRINGER 7L CRACKED AT BS 360. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008041500101 20080415 00101 NM 2008 4 15 SWAA081877 1 20080408 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737E, STR 22L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500105 20080415 00105 NM 2008 4 15 SWAA081880 1 20080408 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 717SA 27851 DURING SCHEDULED CV CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 21 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008041500111 20080415 00111 NM 2008 4 15 SWAA081898 1 20080409 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 21L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008041500119 20080415 00119 EA 2008 4 15 VNAA0803011 1 20080325 A 7603 THROTTLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE COCKPIT OUT OF RIG A VNAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 05 256PS 7937 CREW REPORTED THE RIGHT HAND THRUST LEVER AT FULL FORWARD DOES NOT PRODUCE POWER UP TO CLIMB BUGS. CREW ELECTED TO RETU RN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RIGGED THE RIGHT HAND THROTTLE CONTROLS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE GROUND RAN AIRCRAFT, POWER ASSURANCE CHECKS WERE GOOD. AIRCRAFT PROD UCING POWER TO MAX ALLOWABLE LIMITS AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008041500122 20080415 00122 NM 2008 4 15 DHLA200800039 1 20080409 A 2731 32EN614 TRIM SWITCH BOEING 727 727200 138407E NM ZONE 400 BROKEN A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 765AT 23014 FLT 589, WHEN THRUST LEVERS ADVANCED FOR TAKEOFF, TAKEOFF WARNING HORN ACTIVATED. FLAPS 15 SPEED BRAKES STOWED TRIM SE T AT 6.6. FOUND UPPER STAB. TRIM SWITCH (S532) RETURN MECHANISM BROKEN. R&R SWITCH IAW MM 31-26-24 & WDM 27-43-01. TESTE D TAKE-OFF WARNING IAW MM 31-26-0. OPS CHECKS GOOD. AIRCRAFT WAS GROUNDED. 2 L 7 3 4F RT A3WE 2008041500133 20080415 00133 EA 2008 4 15 TRAX200800506 1 20080408 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 CRACK IN VERTICAL LEG OF UPPER ATTACH ANGLE FOR FLOORBOARDS STA 280 LBL 12 (MARKED). REPAIRED VERTICAL LEG OF UPPER ATT ACH ANGLE IAW REO 601R-53-11-136 2 L 7 2 4F RT A21EA 2008041500137 20080415 00137 EA 2008 4 15 TRAX200800510 1 20080408 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 CRACK IN INTERCOSTAL ATTACH ANGLE STA 484 LBL 36 (MARKED). REPAIRED CRACK IN INTERCOSTAL ATTACH ANGLE REO 601R-53-059. 2 L 7 2 4F RT A21EA 2008041500152 20080415 00152 EA 2008 4 15 TRAX200800526 1 20080410 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 723EV 10132 FUSE SKIN CORRODED BETWEEN STA 295 AND 310 AND BETWEEN STRINGER 24RT AND 25RT. REMOVED CORROSION IAW SRM 53-21-01SP. MIN IMUM SKIN THICKNESS OF .030, .017 BLEND DEPTH (37 PERCENT) IS OUT OF LIMITS OF SRM 53-21-01 AND 53-00-01 FIG 53-00-01-99 1-805. FABRICATED REPAIR DOUBLER. CUTOUT REQUIRES NDT PER SRM 53-00-01 PG 207. INSTALLED REPAIR DOUBLER, FAY SEALED AN D APPLIED PRIMER TO REPAIR AREA PER SRM 53-00-01. PAINTED FASTENERS IN REPAIR AREA AND APPLIED CIC TO AREA PER SRM 51-21 -00. 2 L 7 2 4F RT A21EA 2008041500155 20080415 00155 NM 2008 4 15 SWAA081907 1 20080410 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 266WN 32523 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008041500197 20080415 00197 NM 2008 4 15 SWAA081919 1 20080410 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008041500206 20080415 00206 NM 2008 4 15 SWAA081927 1 20080410 A 5315 6546805 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 799, RBL 17. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 2008041500218 20080415 00218 NM 2008 4 15 USAA920080748 1 20080314 A 5755 654645170 SKIN BOEING 737 7373G7 1384595 NM NR 8 SPOILER DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - RIGHT WING NR 8 SPOILER UPPER SURFACE HAS AREA OF DISBOND, WS 425 - WS 434. REPAIRED R IGHT WING NR 8 SPOILER UPPER SURFACE HAS AREA OF DISBOND, WS 425 - WS 434 IAW B737 SRM 51-70-10-2R REPAIR 4. 2 L 7 2 4F RT A16WE 2008041500228 20080415 00228 NM 2008 4 15 USAA920080688 1 20080312 A 5754 6SC26602224 SKIN BOEING 737 7373G7 1384595 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR-C18- FOUR EA CRACKS .25" LONG EA BOTTOM #5 SLAT SKIN, SLAT STA 211.95 - 215.5. INSTALLED REPAIR IAW SRM 57-43-01-2R6, FIG 201. 2 L 7 2 4F RT A16WE 2008041500236 20080415 00236 NM 2008 4 15 USAA920080759 1 20080327 A 5312 BEAM BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 460UW 25024 PIT - MAJOR REPAIR - CRACKED BULKHEAD RIGHT VERTICAL BEAM WEB, BS 178, RBL 17, WL 185. REPAIRED BULKHEAD RIGHT VERTICAL BEAM WEB, BS 178, RBL 17, WL 185 IAW B737 SRM 53-10-08. 2 L 7 2 4F RT A16WE 2008041600020 20080416 00020 NM 2008 4 16 UIEA200800115 1 20080409 A 5320 REVEAL BOEING 747 747243B 1384830 NM R2 DOORWAY CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK R2 DOOR CUTOUT FWD LOWER REVEAL PANEL FOUND CRACKED. REPAIRED REVEAL IAW SRM 53-10-04. 2 L 7 4 4F RT A20WE 2008041600021 20080416 00021 NM 2008 4 16 AALA200800767 1 20080330 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 772AN 29580 DFW - EMERGENCY LIGHT AT SEAT 44G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 44G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041600022 20080416 00022 NM 2008 4 16 AALA200800768 1 20080330 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 772AN 29580 DFW - EMERGENCY LIGHT AT SEAT 44G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 44G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041600023 20080416 00023 NM 2008 4 16 AALA200800769 1 20080330 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 772AN 29580 DFW - EMERGENCY LIGHT AT SEAT 22G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041600033 20080416 00033 EU 2008 4 16 F3LA200800155 1 20080405 A 5321 D5361060500000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE UNDERSIDE OF FLOOR PANEL 221FF. MAINTENANCE REMOVE D CORRODED PANEL. THE NEW PANEL WAS INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF TASK CARD CP 753-12. FOLLOWING IN STALLATION OF THE NEW PANEL, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041600037 20080416 00037 EU 2008 4 16 08FDEA01403 1 20080414 A 5740 A57111092203 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND ON C 47 LOWER JUNCTION FITTING ON SEVERAL HOLES (HOLE 8, 5, 6, 41, 161) DAMAGES REPAIR PERFORMED BY OVERSIZING THE HOLES, COLD WORKING AND INSTALLING BUSHES IF NECESSARY IAW RAS 70503594/042/2008, APPROVED BY EA 6-5710-115255. 2 L 7 2 4F RT A35EU 2008041600038 20080416 00038 NM 2008 4 16 08FDEA01404 1 20080414 A 5310 FX146N559059 CREASE BEAM BOEING 757 75727B 1384921 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 CORROSION ON CREASE BEAM INBOARD CHORD AT BS 1280, S-17R. REPLACED THE CORRODED CREASE BEAM INBOARD CHORD, BS 1280, S-1 7R IN ACCORDANCE WITH FEDEX ENGINEERING AUTHORIZATION NR F-5310-117339 DATED JANUARY 25, 2008. REPAIR CLASSIFIED AS M INOR AS PER GMM 6-2-100. 2 L 7 2 4F RT A2NM 2008041600039 20080416 00039 EU 2008 4 16 08FDEA01405 1 20080414 A 5740 A57111092202 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND ON C 47 LOWER JUNCTION FITTING ON SEVERAL HOLES (HOLE 3, 4, 5, 36, 40, 42, 160, 165, 169) DAMAGES REPAIR PERFORM ED BY OVERSIZING THE HOLES, COLD WORKING AND INSTALLING BUSHES IF NECESSARY IAW RAS 70503594/042/2008, APPROVED BY EA 6- 5710-115255. 2 L 7 2 4F RT A35EU 2008041600041 20080416 00041 NM 2008 4 16 08FDEA01407 1 20080413 A 7700 4059011911 DISPLAY DOUG MD11 MD11F 3023600 NM COCKPIT FAILED A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 592FE 7285 7285 48550 ENGINE FAIL LIGHT CAME ON AT APPROX 85KT. REJECT TAKEOFF. NO OTHER INDICATIONS. LIGHT WENT OUT WHEN POWERED BACK. ON TAXI OUT DID NOTICE X ON NR 2 ENG OIL TEMP FOR A FEW SECONDS. WENT OUT-BACK TO NORMAL. FLIGHT CREW ALSO REPORTED THAT THERE WAS NOT ANY SIGNIFICANT SPLIT IN ANY OF THE ENGINE INDICATION, AND CHECKING THE DEU'S FCC'S ECU'S ON ALL THREE E NGINES SHOWED NO FAULTS. REMOVED AND REPLACED NR 1 AND NR 2 DEU. NR 1 FAILED TO BOOTUP, CAPT'S DISPLAYS ARE X'D OUT. INSTALLED ORIGINAL NR 1 DEU. SWAPPED NR 1 AND NR 3 DEU. PERFORMED RTS ON ALL THREE DEUS. PERFORMED PWR ASSUR RUNS, N O DEFECTS NOTED, ALL OIL PRESS INDICATIONS NORMAL W/NO ENG FAIL LIGHTS. OK FOR SERV. 2 L 7 3 4F RT A22WE 2008041600044 20080416 00044 NM 2008 4 16 P5CA0801556 1 20080410 A 3600 DUCT BOEING 747 747243B 1384830 NM LEAKING A P5CA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 15 516MC 22507 WITH NR 2 ENGINE FIRE LOOP "B" ON DEFERRAL AND APPROXIMATELY 140NM OUT OF ICN AT FL29 LOOP "A" FIRE DETECTOR LIGHT AND F AULT LIGHT ILLUMINATED FOLLOWED BY FIRE WARNING BELLS. THE ENGINE WAS SHUTDOWN AND FIRE HANDLE PULLED WITH OUT DISCHARG ING BOTTLES. OIL PRESSURE WAS MAINTAINED AT JUST OVER 4 PSI, 10 PERCENT N1; 7 PERCENT N2 NAC TEMP 2.0. MAINT FOUND THE DUCT FOR THE PRESSURE RELIEF VALVE LEAKING AND REPLACED SAME. ALSO, THE FORWARD AND AFT UPPER FIRE DETECTORS WERE REPL ACED. 2 L 7 4 4F RT A20WE 2008041600052 20080416 00052 EA 2008 4 16 A6WA200840195 1 20080305 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 PAX DOOR STAIRS AFT WEB FOUND CRACKED IN FIRST AND SECOND STEP CORNERS AREA. REPAIRED IAW REO 601R-52-11-702 REV A. (M ) 2 L 7 2 4F RT A21EA 2008041600057 20080416 00057 NM 2008 4 16 UIEA200800090 1 20080316 A 5230 707500125 BEAM BOEING 747 747341 13848AM NM CARGO DOOR CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 FORWARD CARGO DOOR INNER WEB LOWER BEAM FOUND SURFACE LEVEL ONE CORROSION AT RT STATION 560-670 STRINGER 40R. CLEANED CORROSION PER SRM 51-30-02 AND BOEING DRAWING 65B04697. 2 L 7 4 4F RT A20WE 2008041600061 20080416 00061 NM 2008 4 16 UIEA200800102 1 20080402 A 5320 FLOOR SUPPORT BOEING 747 747243B 1384830 NM BS 440-460 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 STA 440 -460 RIGHT OUTBOARD FLOOR SUPPORT HAS LEVEL 1 CORROSION. REMOVED CORROSION PER SRM 51-10-01 AND REPROTECTED PER 51-10-02. 2 L 7 4 4F RT A20WE 2008041600062 20080416 00062 NM 2008 4 16 UIEA200800103 1 20080402 A 5320 FLOOR SUPPORT BOEING 747 747243B 1384830 NM BS 440-460 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 STA 440 -460 LEFT OUTBOARD FLOOR SUPPORT HAS LEVEL 1 CORROSION. REMOVED CORROSION PER SRM 51-10-01, REPROTECTED PER 51- 10-02. 2 L 7 4 4F RT A20WE 2008041600067 20080416 00067 NM 2008 4 16 UIEA200800082 1 20080307 A 5711 SPAR BOEING 747 747341 13848AM NM RWS 610-615 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 RIGHT WING STA 610 TO WING STA 615 UPPER FACE REAR SPAR LEVEL 1 CORROSION EVIDENT. CORROSION CLEANED UP AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F RT A20WE 2008041600068 20080416 00068 NM 2008 4 16 UIEA200800083 1 20080310 A 5210 FRAME BOEING 747 747341 13848AM NM L4 DOOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 MAIN DECK L4 DOOR AFT LOWER CORNER FRAME CRACKED. CRACKED AREA REPAIRED PER SRM 52-10-02. 2 L 7 4 4F RT A20WE 2008041600069 20080416 00069 NM 2008 4 16 UIEA200800084 1 20080310 A 5310 DOOR FRAME BOEING 747 747341 13848AM NM ZONE 800 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 MAIN DECK L5 DOOR CUTOUT FWD UPPER REVEAL PANEL FOUND CRACKED. REPAIRED PER SRM 53-10-04. 2 L 7 4 4F RT A20WE 2008041600072 20080416 00072 EA 2008 4 16 A6WA200840183 1 20080306 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 TWO ANGLES CRACKED ON THE REAR PRESSURE BULKHEAD AT RBL AND LBL 46 FS 621 AND WL 93.50. TWO ANGLES ON THE REAR PRESSURE BULKHEAD REPLACED IAW REO 601R-53-61-100 REV A. (M) 2 L 7 2 4F RT A21EA 2008041600074 20080416 00074 EA 2008 4 16 A6WA200840192 1 20080305 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 PAX DOOR AFT DRAG ANGLE FOUND CRACKED. PAX DOOR AFT DRAG ANGLE REPAIRED IAW REO 601R-52-11-513 REV A. (M) 2 L 7 2 4F RT A21EA 2008041600079 20080416 00079 NM 2008 4 16 UIEA200800118 1 20080410 A 5347 BAC15201890717 SEAT TRACK BOEING 747 747243B 1384830 NM BS 1720-1760 BROKEN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK BS 1720 TO 1760 LBL 11 SEAT TRACK FOUND BROKEN AND WORN, SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 14. 2 L 7 4 4F RT A20WE 2008041600085 20080416 00085 NM 2008 4 16 UIEA200800124 1 20080404 A 5730 SKIN BOEING 747 747243B 1384830 NM LWS 1120-1540 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 LEFT WING UPPER SURFACE CORROSION FOUND FROM WS 1120-1540 BETWEEN FRONT SPAR AND REAR SPAR. BLENDED OUT CORROSION PER S RM 51-10-01, REPROTECTED PER SRM 51-10-02. 2 L 7 4 4F RT A20WE 2008041600086 20080416 00086 EA 2008 4 16 QXEA200800353 1 20080404 A 5210 601R318723 SEAL CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR DAMAGED A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 608QX 10026 FLT 2569 - AFTER DEPARTURE, THE MAIN CABIN DOOR STARTED SQUEALING. NO PRESSURIZATION PROBLEMS OR DOOR WARNINGS. SQUEAL BECAME LOUDER AND IT WAS DECIDED TO DIVERT TO PDX. MAINTENANCE REPLACED THE DOOR SEAL. OPERATIONAL CHECKS GOOD. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 2008041600091 20080416 00091 NM 2008 4 16 AALA200800733 1 20080327 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 358AA 24039 JFK - EXTERNAL EMERGENCY LIGHT AT LEFT AFT WING INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LEFT AFT WIN G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008041600093 20080416 00093 NM 2008 4 16 AALA200800735 1 20080327 A 3350 6832AS25 LAMP DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 951TW 53470 PHX - EMERGENCY LIGHT AT SEAT 19D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT 2008041600094 20080416 00094 NM 2008 4 16 AALA200800713 1 20080324 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 605AA 27056 DFW - EMERGENCY LIGHT AT SEAT ROW 33DEF HAS MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 33DEF. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041600113 20080416 00113 NM 2008 4 16 HALA0800523 1 20080410 A 2710 AILERON BOEING 767 767333 1385301 NM MALFUNCTIONED A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM ON CLIMB TO 320 W/AUTO PILOT ON BOTH (LT AND RT) INBD AILERON INDICES ON THE FLIGHT CONTROL STA TUS DISPLAYS WERE 1/3 OF TOTAL SCALE ABOVE THE MEDIAN LINE. AT LEVEL, BOTH INDICES WENT TO 1/4 SCALE ABOVE MEDIAN. TUR NING AUTO PILOT OFF PRODUCED NO NOTICABLE PITCH OR ROLL TENDENCIES. MCDP TEST CARRIED OUT FOR ALL 3 AUTO PILOTS. NO LA ST FLIGHT FAULTS FOUND. ACCOMP AMMM 27-11-00-715-002, OPS TEST AILERON AND AILERON TRIM CONTROL SYSTEM. OPS CK OK. 2 L 7 2 4F RT A1NM 2008041600125 20080416 00125 NM 2008 4 16 UIEA200800127 1 20080404 A 5210 SKIN BOEING 747 747243B 1384830 NM L1 DOOR DEFORMED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK L-1 DOOR LOWER AFT CORNER OF EXTERNAL SKIN FOUND DEFORMED. DEFORMED AREA RE-WORKED AS PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 2008041600133 20080416 00133 NM 2008 4 16 UIEA200800135 1 20080403 A 5730 SKIN BOEING 747 747243B 1384830 NM RWS 917-834 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 RIGHT WING WS 917 TO WBL 834 FROM MID SPAR SURROUND AREA TO REAR SPAR SURROUND AREA HAS CORROSION. BLENDED OUT CORROSIO N PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02. 2 L 7 4 4F RT A20WE 2008041600135 20080416 00135 NM 2008 4 16 UIEA200800137 1 20080404 A 5730 SKIN BOEING 747 747243B 1384830 NM ZONE 600 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 RT WING WBL 128 TO WS 510 FRONT SPAR TO REAR SPAR UPPER SKIN FOUND CORROSION. BLENDED OUT CORROSION PER SRM 51-10-01, R EPROTECTED PER SRM 51-10-02. 2 L 7 4 4F RT A20WE 2008041600142 20080416 00142 SO 2008 4 16 SIMA200810504 1 20080413 A 2731 3621001013 CONTROL UNIT EMB 145 EMB145LR 3260212 SO PITCH TRIM MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 659AE 145762 ON FLIGHT 4489, CREW REPORTED SHORTLY AFTER TAKEOFF ON CLIMB, THEY GOT A PITCH TRIM MAIN INOP. CREW DECLARING AN EMERGE NCY AND RETURN TO ORD. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED HSCU AND FO'S YOKE PITCH TRIM SWITCH, OPS C HECKS WERE GOOD AT THIS TIME. WORK PERFORMED IAW AMM 27-40-01 AND 27-40-03. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008041600147 20080416 00147 WP 2008 4 16 AALA200800752 1 20080329 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 553AA 53083 LGA - EMERGENCY LIGHT AT MID CABIN OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN OVERWI NG. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008041600149 20080416 00149 NM 2008 4 16 AALA200800754 1 20080329 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AA 24585 DFW - EMERGENCY LIGHT AT SEAT ROW 12DEF MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 12DEF. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041600150 20080416 00150 NM 2008 4 16 AALA200800755 1 20080329 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AA 24585 DFW - EMERGENCY LIGHT AT SEAT ROW 12DEF HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 12DEF. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041600151 20080416 00151 WP 2008 4 16 AALA200800747 1 20080328 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 468AA 49598 LGA - EMERGENCY LIGHT AT TAIL COMPARTMENT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT TAIL COMPARTMENT. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008041600153 20080416 00153 NM 2008 4 16 AALA200800745 1 20080328 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 901AN 29503 DFW - EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. RESEATED CONNECTOR AT SIDEWALL FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008041600154 20080416 00154 WP 2008 4 16 AALA200800746 1 20080328 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DISLODGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 468AA 49598 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROW 28 TO AFT OF CABIN INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHT A T OVERHEAD SEAT ROW 28 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008041600159 20080416 00159 NM 2008 4 16 NWAA081596310 1 20080304 A 5330 SKIN BOEING 747 747451 1384940 NM BS 460 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING "M" CHECK, FOUND SHORT EDGE MARGIN ON FUSELAGE SKIN FASTENER HOLES ABOVE DOOR 1 LT BS 460. REPAIRED PER EA 63-21 2523. 2 L 7 4 4F RT A20WE 2008041600161 20080416 00161 NM 2008 4 16 AALA200800756 1 20080330 A 3350 OL1098BPEGPL LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 678AN 29428 JFK - EMERGENCY LIGHT AT SEAT 34D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 34D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041600165 20080416 00165 NM 2008 4 16 AALA200800761 1 20080330 A 3350 OL3071BPEGPL LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 767AJ 33539 JFK - EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041500166 20080415 00166 WP 2008 4 15 NWAA080149992 1 20080411 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 943N 47647 DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY IN THE TAIL CONE AND OPERATIONALLY CHECKED THE SYSTEM. 2 L 7 2 4F A6WE 2008041500167 20080415 00167 WP 2008 4 15 NWAA081499929 1 20080412 A 3397 SWITCH DOUG DC9 DC931 3022065 WP TAXI LIGHT FAILED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 01 8923E 45838 DURING THE LANDING APPROACH INTO MBS, THE CREW SMELLED SMOKE AND WITNESSED SPARKS AND MOLTEN METAL COMING FROM UNDERNEAT H THE INSTRUMENT PANEL. THE LANDING WAS ACCOMPLISHED WITHOUT FURTHER TROUBLE BUT CREW REQUESTED THAT CFR MEET UP WITH T HE AIRCRAFT. AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. FLIGHT ATTENDANTS ALSO REPORTED SMELLING BURNING ODORS I N THE CABIN AREAS. MAINTENANCE FOUND THAT THE NOSE TAXI LIGHT POWER SWITCH, S-109, WAS LOOSE IN ITS MOUNTING AND HAD A LOOSE WIRE CONNECTION WHICH ALLOWED THE WIRE TO SHORT OUT AGAINST ANOTHER CONTACT. THE SWITCH AND THE TERMINAL ENDS OF THE SHORTED WIRES WERE ALL REPLACED. THE FUNCTIONAL CHECK WAS GOOD. 2 L 7 2 4F A6WE 2008041500168 20080415 00168 EA 2008 4 15 A6WA200840193 1 20080227 A 5340 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 ANGLE CRACKED AT FS 484, LBL 36 AND WL 73. REPAIR TO INTERCOSTAL ANGLE CARRIED OUT IAW REO 601R-53-41-059 REV A. (M) 2 L 7 2 4F RT A21EA 2008041500169 20080415 00169 EU 2008 4 15 F3LA200800153 1 20080404 A 5315 D2547030024000 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE FORWARD LAVATORY FLOOR ANGLE BRACKET, ON ITS UNDERS IDE. MAINTENANCE REMOVED AND REPLACED THE ANGLE BRACKET IN ACCORDANCE WITH THE REQUIREMENTS OF A0-25EO-20299. UPON COM PETION OF THE REPLACEMENT, THE BRACKET WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041500170 20080415 00170 2008 4 15 ARWA20080404 4 20080413 A 3441 37570838 COMPUTER DOUG DC10 DC1010 3022110 WP MALFUNCTIONED A ARWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 29 68041 46900 ON TAXI, BOTH CAPTAIN AND FIRST OFFICER'S FMAS WENT TO G/A INSTEAD OF TAKEOFF. T/O WHEN G/A BUTTON PUSHED. SWAPPED BOT H NR 1 AND NR 2 PITCH GUIDANCE COMPONENT FOR DISPATCH IN ACCORDANCE WITH M/M 22-11-02. CHECK OK IN ACCORDANCE WITH M/M 22-10-00 AND M/M 34-24-00. 2 L 7 3 4F A22WE 2008050700370 20080507 00370 NM 2008 5 7 SWAA082416 1 20080501 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FWD CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM. 2 L 7 2 4F RT A16WE 2008050700371 20080507 00371 NM 2008 5 7 SWAA082417 1 20080501 A 5311 6546538 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008050700372 20080507 00372 NM 2008 5 7 SWAA082379 1 20080501 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 944, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008050700378 20080507 00378 NM 2008 5 7 SWAA082397 1 20080503 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 366SW 26577 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008050700388 20080507 00388 NM 2008 5 7 SWAA082418 1 20080504 A 5311 6516301 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008050700396 20080507 00396 NM 2008 5 7 SWAA082384 1 20080501 A 5743 69878857 FITTING BOEING 737 7373A4 1384585 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C1 CHECK, FOUND LT MLG WALKING BEAM ACTUATOR FWD HANGER FITTING CRACKED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008050800002 20080508 00002 EA 2008 5 8 A6WA200840293 1 20080407 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 574-621 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 CARGO BAY FLOOR SILL BETWEEN FS 574 TO FS 621, ALL NUT PLATE HOLES CORRODED. CORROSION REMOVED IAW SRM 51-21-06 . 2 L 7 2 4F 4 F RT A21EA E15NE 2008050800013 20080508 00013 NM 2008 5 8 08FDEA01712 1 20080501 A 5534 6517544 ANGLE BOEING 727 727200 138407E NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 RIB NR 2 ATTACH ANGLE CRACKED AT STR 6R ATTACHMENT BOLT INSIDE VERTICAL STAB, STR 6R, RIB NR 2 FIN STA 22.5 CUT-OUT DA MAGED AREA IAW SRM 51-10-1 & 55-30-5 FIGURE 1, FABRICATED REPAIR ANGLE & REPAIR FILLER, TREATED & PRIMED PARTS IAW SRM 5 1-1-2, INSTALLED REPAIR PARTS IAW SRM 55.30.5 FIGURE 1 & 51-30-2 2 L 7 3 4F RT A3WE 2008050800016 20080508 00016 NM 2008 5 8 08FDEA01703 1 20080430 A 5330 65921444 SKIN BOEING 727 7272S2F 1384O81 NM BS 1055 S29R CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 CRACK IN LWR FUSELAGE AT STA 1055, 5.5 INCHES RIGHT OF CENTERLINE STR 29R. CUT-OUT DAMAGED AREA & FABRICATED REPAIR FILL ER & REPAIR DOUBLER IAW SRM 53-30-3 FGIURE 3 & 53-30-2 FIGURE 2, TREATED & PRIMED PARTS IAW SRM 51-10-2 & INSTALLED REP AIR PARTS IAW SRM 53-30-3 FIGURE 3 & 51-30-2. 2 L 7 3 4F A3WE 2008050800024 20080508 00024 CE 2008 5 8 DXTA200802973 1 20080330 A 3240 BRAKE SYS RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP LANDING GEAR CONTAMINATED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 892QS 258592 BRAKES ARE VERY MUSHY AND GO TO THE FLOOR. INSPECTED SYS FOR LEAKS, NONE NOTED. PERFORMED OPS CHECK, ALL CHECK GOOD. B LED BRAKE SYS AND PERFORMED TAXI CHECK, ALL CHECK GOOD. ALL WORK IAW MM 32-40-00. 2 L 7 2 4F 4 F RT A3EU E6WE 2008050800027 20080508 00027 SW 2008 5 8 907204142008 1 20080414 A 2497 WIRE BOLKMS 117 BK117C2 5626002 SW TMECA ARRIEL ARRIEL1E 60034 NE DAMAGED E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS AA AIR AMBULANCE 1 NM 03 145LF 9072 THIS REPORT IS THE 3RD OCCURRENCE OF SMOKE/ODOR CAUSED BY AN ELECTRICAL DISCHARGE FAULT IN THE OVERHEAD CIRCUIT BREAKER PANEL. MECHANICS REPLACED THE APPROPRIATE WIRING AND DUMMY CIRCUIT BREAKER INVOLVED IN THE INITIAL FAULT. AIRCRAFT WAS O PS CHECKED AND THEN RETURNED TO IT'S BASE. 1 G 7 2 3U 3 U H13EU E19EU 2008050800028 20080508 00028 CE 2008 5 8 FFSA200800001 1 20080413 A 5310 11442004137 DOOR FRAME BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA FUSELAGE CRACKED E FFSA K NONE O OTHER IN INSP/MAINT 1 AL 01 404GV 23775 UC154 DURING CONFORMITY INSPECTION, A CRACK WAS DISCOVERED IN THE OUTER FLANGE RADIUS RUNNING VERTICALLY DOWN FROM THE CUTOUT FOR THE AIRSTAIR DOOR SEAL JOGGLE. THE (2) RIVETS ATTACHING THE CENTER OF THE DOOR HINGE TO THIS STRUCTURE HAD BEEN WORK ING. 2 L 7 2 4T 4 T RT A24CE E4EA 2008051400212 20080514 00212 EA 2008 5 14 A6WA200840326 1 20080410 A 5540 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA RUDDER MISSING A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 RUDDER UPPER CLOSING RIB CLOTH MISSING. (M) REPAIRED IAW REO 601R-55-41-037 REV A. 2 L 7 2 4F RT A21EA 2008051400216 20080514 00216 NM 2008 5 14 AALA200800908 1 20080410 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 756AM 30264 DFW - EMERGENCY LIGHT AT SEAT 31G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051400217 20080514 00217 NM 2008 5 14 2008UALA00017 1 20080101 A 2560 KI10112 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FLASHLIGHT WEAK A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 F/A REPORTED DR 3L EMERGENCY FLASHLIGHT BATTERY WEAK. SUPPLEMENTAL DATA UPDATE SUSPECT BATTERY IN DISCHARGED CONDITION. REPLACED FLASHLIGHT BATTERY. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008051400220 20080514 00220 EA 2008 5 14 A6WA200840307 1 20080404 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 589 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 CARGO DOOR SILL CRACK AROUND RIVET FS 589 LBL 45. (M) CRACK REPAIRED IAW REO 601R-53-61-433 . (A) 2 L 7 2 4F RT A21EA 2008051400222 20080514 00222 NM 2008 5 14 DHL2008760545 1 20080420 A 5313 BAC1498146 STRINGER BOEING 727 7272B7 138407L NM BS 1040-1060 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 CUT OUT DAMAGED STRINGER, BS 1040 TO 1060, ON STR 27L. FABRICATED, AND INSTALLED STR REPAIR PER B727 SRM 53-10-2 FIG 9 AND 53-10-3 FIG 1. 2 L 7 3 4F A3WE 2008051400234 20080514 00234 NM 2008 5 14 SWAA082604 1 20080512 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008051400242 20080514 00242 NM 2008 5 14 SWAA082536 1 20080511 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 200805131 20080513 1 WP 2008 5 13 08FDEA01797 1 20080508 A 5730 NRC6041 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 600 LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 307FE 48291 RT WING UPPER SURFACE FOUND 8 EA RIVETS LOOSE ON UPPER SKIN OF OUTBD AILERON. REPAIRED AREA IAW SRM 57-10-00 FIG 85 VOL I. 2 L 7 3 4F RT A22WE 200805131 20080513 1 NM 2008 5 13 DLM90080673 1 20080430 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 1326 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 109940 53393 CABIN SEAT TRACK FS 1326-LBL 22 OUT OF LIMITS. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01, FIG 6 VOL I. 2 L 7 2 4F RT A6WE 200805131 20080513 1 NM 2008 5 13 DL738080646 1 20080428 A 3397 WIRE HARNESS BOEING 737 737832 13844CF NM EMERGENCY LIGHTS PINCHED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 394DA 30562 ROW 17-21 AND ROW 23-33 EMERGENCY PATH LIGHTS INOP. REPLACED RT CRADLE AT STA 550 R0W 17-21 OPS NML. REPLACED SEAT HAR NESS TO WALL HARNESS AT 27 DEF AND FUSE IN CHARGER UNIT. OPS OK. 2 L 7 2 4F RT A16WE 200805131 20080513 1 NM 2008 5 13 AALA200800879 1 20080408 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR FORWARD GALLEY BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LEF T NUMBER ONE DOOR FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 200805131 20080513 1 NM 2008 5 13 DLM90080668 1 20080430 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 1117-1136 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 LEFT CUSP WEB HAS CORROSION ON FWD END BETWEEN STA 1117 TO 1136. BLENDED CORROSION ON LEFT CUSP WEB STA 1117 TO 1136, F OUND TO BE OUT OF LIMITS, IAW MD90 SRM 53-00-01, FIG3. WORK WILL BE ACCOMPLISHED ON W/O S/N 109897 1003732 2400/0205. 2 L 7 2 4F RT A6WE 200805131 20080513 1 NM 2008 5 13 DLM88080679 1 20080505 A 3350 BATTERY PACK DOUG MD88 MD88 3023688 NM EMERGENCY LIGHT DISCONNECTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 918DL 49583 DURING L1 LETTER CHECK REF NR 99, FOUND FWD EMERGENCY FLOOR LIGHTS BATTERY PACK NOT CONNECTED TO EEPLS. FOUND ALL SEAT HARNESS CONNECTED END TO END FROM THE AFT BATTERY PACK ONLY. REWIRED PER WDM 33-51-14 2 L 7 2 4F RT A6WE 200805131 20080513 1 WP 2008 5 13 NWAA080929984 1 20080502 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 984US 47383 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT FOR THE AFT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE R EPLACED THE BATTERIES AND THE OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F A6WE 200805131 20080513 1 EU 2008 5 13 TRBA2008050 1 20080506 A 2435 8260121 STARTER GEN AEROSP ATR72 ATR72212A 8680902 EU RT ENGINE FAILED A TRBA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 29 533AT 533 AFTER RT ENG START NR 2 GENERATOR NEVER CAME ON LINE, THEN COCKPIT SMOKE STARTED BEHIND F/O SEAT. REMOVED AND REPLACED NR 2 STARTER/GENERATOR AND HALL EFFECT SENSOR FIN NR 8PU IAW JIC NR 24-32-61-RAI-10000-07 AND NR 24-00-00-RAI-10050-002. 2 H 7 2 4T RT A53EU 200805131 20080513 1 NM 2008 5 13 2008UALA02562 1 20080501 A 3510 MC1025154 OXYGEN MASK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FLIGHT OFFICER'S FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 348UA 24252 FLIGHT OFFICERS OXYGEN MASK FAILED LEAK CHECK. REPLACED FIRST OFFICERS O2 MASK, LEAK CHECKED GOOD.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 200805141 20080514 1 NM 2008 5 14 AALA200800932 1 20080411 A 5320 WEB BOEING 767 767223 1385123 NM BS 287 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AA 22333 AFW - NOSE WHEEL WELL RIGHT WEB AT STATION 287 RBL 25 BETWEEN WATER LINE 170 TO 180 DAMAGED. AREA OF DISCREPANCY IS 1.8 INCH BY 1.2 INCH. REPAIRED NOSE WHEEL WELL RIGHT WEB IN ACCORDANCE WITH MRB 767 3178. 2 L 7 2 4F RT A1NM 200805141 20080514 1 CE 2008 5 14 DXTA200803028 1 20080428 A 3260 WARNING SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT ACTIVATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 970QS 7500070 "UNSAFE" NOSE GEAR INDICATION ON DEPARTURE. CYCLED LANDING GEAR. RANG OUT NLG, R/L MLG UPLOCK SWITCHES, INSPECTED WIRIN G IN ALL 3 WHEEL WELLS. VERIFIED RIGGING ON NLG, R/L MLG UPLOCK SWITCHES. ALL TESTS PASS AT THIS TIME. DONE PER MM 32-30 -00. CANNOT DUPLICATE SQUAWK AS WRITTEN. 2 L 7 2 4J 4 F RT T00007WI TE6CH 200805141 20080514 1 CE 2008 5 14 GUUA04260801 1 20080426 A 3297 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE SHORTED A GUUA O OTHER O OTHER AP APPROACH 1 SO 29 231YV UE231 FLIGHT: 9275, DURING APPROACH LANDING GEAR WOULD NOT COME DOWN, CIRCUIT BREAKER POPPED. MANUALLY EXTENDED LANDING GEAR. LANDED WITHOUT INCIDENT. REPAIRED SHORTED WIRE G15F22 ON CABIN SIDEWALL NEAR MAIN DOOR. OPERATIONAL CHECK GOOD NO DEFE CTS NOTED. 2 L 7 2 4T 4 T RT A24CE E26NE 200805141 20080514 1 NM 2008 5 14 UIEA200800159 1 20080416 A 5743 BOLT BOEING 747 7472D7B 1384803 NM TRUNNION SHEARED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 2097 22337 FORWARD UPPER TRUNNION NUT LOCKING PLATE BOLTS SHEARED AND TRUNNION NUT REQUIRES TORQUE CHECK SUSPECT MOVEMENT IN HOUSIN G. TRUNNION HOUSING REMOVED AND REPLACED IAW AMM 57-43-01/ 401 AND 32-11-19. ALL FIT CLEARANCES AND NDT OF PINS SATISF ACTORY PER BSOPM 20-20-01. HOUSING ATTACHMENT BRACKETS NDT IAW D6-7170 PART 6 51-00-00, NO CRACKS EVIDENT. GEAR RETRAC TION AND EXTENSION PERFORMED. 2 L 7 4 4F RT A20WE 200805141 20080514 1 EA 2008 5 14 SWIA200819552 1 20080208 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 760SK 10223 COCKPIT AFT FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED NEW FLOOR SUPPORT PER CRJ700 SRM TASK 51-42-06-001-00 1-A01. 2 L 7 2 4F RT A21EA 200805141 20080514 1 EA 2008 5 14 SWIA200819558 1 20080205 A 5314 KEELBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 984CA 7171 FORWARD KEEL BEAM FITTING ATTACHMENT HARDWARE IS CORRODED, FOUND AT C-CHECK. REPLACED KEEL BEAM ATTACHING HARDWARE PER CRJ200 REO 601R-53-31-034 AND DRAWING 601R31060 FLAG NOTE 27. 2 L 7 2 4F RT A21EA 200805141 20080514 1 NM 2008 5 14 UPS08M52104 1 20080120 A 5713 STRINGER DOUG MD11 MD11 3023602 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C RT WING UPPER STRINGER END NR S9 SUSPECT CRACK AS MARKED, THRU ACCESS NR 638AB. HFEC INSP CARRIED OUT PER DACNDT SPM R.13 PART06.10.01.001 AND CRACK APPROX 9 INCH FOUND AS MARKED. CRACK AT RHW STR NR 9 SLOTTED OUT PER SR M 57-20-00 FIG 10V.1R.35. REPAIR ANGLES FABRICATED PER SRM 57-20-00FIG.10V.1R.35 AND HEAT TREATED TO T6 COND PER DPS7.0 0-1 AND AVERAGE HARDNESS HRB82.5 IS ACCEPTABLE PER DPS1.05-3. REP ANGLES HOLES PICK UP PER SRM 57-20-00 FIG 10. 2 L 7 3 4F RT A22WE 200805141 20080514 1 WP 2008 5 14 08FDEA01677 1 20080429 A 5280 ARC0468107 DEPRESSOR DOUG MD10 MD1010F 3022112 WP LT MLG DOOR SEAL CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 LT MLG WW OUTBD SEAL DEPRESSOR FOR THE MAIN GEAR DOOR IS WORN AND CRACKED. SEAL LAND WAS WORN & CRACKED RENDERING IT UN SERVICEABLE. REMOVED SEAL LAND IAW SRM 51-35-01. FABRICATED A NEW SEAL LAND IAW DWG ARC0467. HEAT TREATED SEAL LAND I AW TPS 1003. CONDUCTIVITY LOAD 35.2 / 35.5; HT050208-2. PART MARKED SEAL LAND ARC0468-107FX IAW GMM 7-0-1000. INSTALLE D SEAL LAND IAW SRM 51-31-01. 2 L 7 3 4F RT A22WE 200805141 20080514 1 NM 2008 5 14 08FDEA01680 1 20080429 A 5330 FX146N38107 SKIN BOEING 757 75727B 1384921 NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 SCRIBE MARK DEPTH OF 0.0053 INCH, LENGTH OF 1.0 INCH FOUND ON BUTT JOINT AT STA 1620, 10 INCHES ABOVE STRINGER 14L. EVA LUATE AND RECTIFY. REPAIRED BUTT JOINT AT STATION 1620 IN ACCORDANCE WITH FEDEX ENGINEERING AUTHORIZATION F-5310-117340 . REPAIR CLASSIFIED AS MINOR GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 200805141 20080514 1 EU 2008 5 14 08FDEA01681 1 20080430 A 5753 A57960000003 SKIN AIRBUS 300 A300B4622R 3930312 EU RT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND DURING PERFORMANCE OF EO 6-5750-7-5000 PT 4 SEVERAL CRACKED HOLES IN INNER FLAP RT, LOWER SIDE, REPAIR PERFORMED B Y REPLACEMENT OF RT INNER FLAP IAW AMM 27-50-11 PB400. 2 L 7 2 4F RT A35EU 200805141 20080514 1 2008 5 14 ZZDA2008101 4 20080501 A 2565 64210103 SLIDE BOEING 717 717200 1383700 NM TAIL CONE UNWANTED DEPLOY A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 893AT 55045 TAIL CONE AND TAIL SLIDE INADVERTENTLY DEPLOYED. REINSTALLED TAIL CONE ASSEMBLY REF MM 53-52-01. A/C FERRIED TO ATL FO R FURTHER MAINT. REINSTALLED NEW TAIL CONE SLIDE PER MM 25-61. 2 L 7 2 4F TR A6WE 2008051400011 20080514 00011 NM 2008 5 14 CALA0800415 1 20080425 A 5310 141A81121 DOOR FRAME BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24212 28772 L1 DOOR CHORD HAS CORROSION AT SEVERAL SCREW HOLES. REMOVED AND REPLACED L-1 DOOR CHORD PER SRM 51-40-02, B737-53-3-073 5. 2 L 7 2 4F RT A16WE 2008051400021 20080514 00021 NM 2008 5 14 ASAA0842912 1 20080429 A 5753 65C2632017 FLAP BOEING 737 7374Q8 138447Q NM WING CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 LEFT O/B MIDFLAP CHAFED AT LEADING EDGE I/B END. REMOVED PREVIOUSLY INSTALLED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 57 53 01. 2 L 7 2 4F RT A16WE 2008051400029 20080514 00029 NM 2008 5 14 ASAA0852913 1 20080507 A 2160 3989083 VALVE BOEING 737 737890 1384527 NM A/C SYSTEM FAULTY A ASAA O OTHER J WARNING INDICATION UK UNKNOWN 1 NM 02 579AS 4712 35187 DURING RECALL GOT THE AIR COND AND ZONE TEMP LIGHT ON OVERHEAD. BITE CHECK OF PACK ZONE TEMP CONTROLLER FAULTED FLT DEC K TRIM VLV. REPLACED FLT DECK ZONE TRIM VALVE. OPERATIONAL AND LEAK CHECKS OK. BITE CHECK OF PACK ZONE TEMP CONTROLLE R OK. 2 L 7 2 4F RT A16WE 2008050800033 20080508 00033 EU 2008 5 8 BAQA20080004 1 20080419 A 2150 S8990132 O-RING ALIDSG BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE A/C BAY DAMAGED E BAQA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 03 118NC 7067 CRUISE FLIGHT, CLOSE TO FLIGHT DESTINATION, CREW SMELLED "STRANGE ODOR" IN CABIN/COCKPIT. PILOT TURNED OFF THE ENVIRONM ENTAL CONTROL UNIT AND SMELL CEASED. INSPECTION OF ECU REVEALED THAT THE "INDUCTOR" PIPE TEMPERATURE CONTROLLER TO COOL ING TURBINE HAD A SMALL SPLIT AT THE TURBINE AND PIECES OF THE SEALING O-RING (PACKING) WAS EXPOSED AND MISSING. 1 G 7 2 3U 3 U H13EU E5NE 2008050800035 20080508 00035 EA 2008 5 8 SWIA200819561 1 20080427 A 3510 OXYGEN MASK CNDAIR CL600 CL6002D24 1390016 EA FLT ATTENDENT UNWANTED DEPLOY A SWIA O OTHER O OTHER LD LANDING 1 NM 07 812SK 15098 AFT FLIGHT ATTENDANT O2 MASK DEPLOYED ON LANDING. INSPECTED AND REINSTALLED O2 MASK. 2 L 7 2 4F RT A21EA 2008050800040 20080508 00040 EU 2008 5 8 BAQA20080041 1 20080419 A 2150 S8990132 O-RING BOLKMS 117 BK117A3 5626015 EU A/C BAY DAMAGED E BAQA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 03 118NC 7067 CRUISE FLIGHT, CLOSE TO FLIGHT DESTINATION, CREW SMELLED "STRANGE ODOR" IN CABIN/COCKPIT. PILOT TURNED OFF THE ENVIRONM ENTAL CONTROL UNIT AND SMELL CEASED. INSPECTION OF ECU REVEALED THAT THE "INDUCTOR" PIPE TEMPERATURE CONTROLLER TO COOL ING TURBINE HAD A SMALL SPLIT AT THE TURBINE AND PIECES OF THE SEALING O-RING (PACKING) WAS EXPOSED AND MISSING. 1 G 7 2 3U H13EU 2008050800056 20080508 00056 NE 2008 5 8 KNK2008F00000 2 20080409 A 7322 0292208230 MANIFOLD TMECA SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE FUEL INJECTION COKED E KNKA K NONE O OTHER IN INSP/MAINT 1 WP 13 112AK 10364 1090 9732 3254 FUEL COKING DEPOSITS FORMED IN FUEL INJECTION MANIFOLD AIR/FUEL LABRYNTH SEAL, CAUSING DRAG ON AXIAL ROTATING COMPONENTS OF THE ENGINE ASSY, PREVENTING THE START SEQUENCE OF THE ENGINE. (K) 1 G 7 1 3U 3 U H9EU E19EU 2008050800057 20080508 00057 2008 5 8 HALA0800559 4 20080503 A 3417 4040800912 ADC BOEING 767 767332 1382001 NM LEFT MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, AT CRUISE ALTITUDE FIRST OFFICER'S ALTIMETER IS 200' TOO LOW AT FL 340 ALT 34,300 CAPT =34,000 FO=33,800. IT CORRECT WHEN SELECTING ALT AIR DATA. REMOVED AND REPLACED LT ADC PER AMM 34-12-01. OPS CK OK. PERFORM ED TEST 30 PASS ALL TEST. A/C REMAINS IN LAND 3 STATUS. 2 L 7 2 4F RT A1NM 2008050800058 20080508 00058 NM 2008 5 8 HALA0800563 1 20080423 A 5300 SKIN BOEING 767 7673CB 1385187 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 588HA 33466 LEVEL 2 CORROSION ON THE CENTER HORIZONTAL STAB UPPER SURFACE SKIN AT LBL 35 STR 10, AROUND 2 FASTENERS. REMOVED CORROS ION IAW SRM 55-10-01, FIG 101 REV 76. REWORK APPROVED BY TI FILE NR 588030. 2 L 7 2 4F RT A1NM 2008050800060 20080508 00060 WP 2008 5 8 NWAA081959885 1 20080505 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 401EA 47682 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 5 AND 8 OF THE CABIN GO DIM AFTER ABOUT 3 SECONDS. MAINTENANCE REPLACED THE BATTERY PACK AT THE OVERWING FWD RIGHT EXIT LIGHT ASSEMBLY. LIGHTS RETURNED TO NO RMAL FUNCTION AND OPERATIONAL DURATION. 2 L 7 2 4F RT A6WE 2008050800078 20080508 00078 CE 2008 5 8 GUUA04190801 1 20080419 A 3610 1H755 REGULATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BLEED AIR SYS MALFUNCTIONED A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 29 81546 UE187 FLIGHT 9205, AFTER TAKEOFF, STRONG SCENT OF BURNED RUBBER IN COCKPIT. (NO SMOKE) THE PNEUMATIC PRESSURE GAUGE PEGGED OVE R THE RED LINE AND VACUUM PRESSURE GAUGE PEGGED AT ZERO, WHEN TRYING TO ADD HEAT, USE DEICE BOOTS ON ANY OTHER ENVIRONME NTAL PRESSURE FUNCTION, SMELL GETS SIGNIFICANTLY WORSE. REPLACED PRESSURE REGULATOR AND TEST RAN ENGINES. PERFORMED BLEE D AIR SYSTEM OPERATIONAL CHECK SYS, NO SMELL DETECTED. 2 L 7 2 4T 3 T RT A24CE E2NE 2008050800087 20080508 00087 CE 2008 5 8 GLBA 1 20080315 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA LT MLG WORN A GLBA O OTHER O OTHER DE DESCENT 1 NM 03 122UX 17431 2452 UE122 SIGNIFICANT EVENT, ENROUTE, THE LANDING GEAR WOULD NOT EXTEND NORMALLY WHICH REQUIRED THE PILOTS TO MANUALLY PERFORM THE GEAR EXTENSION. MAINT REMOVED AND REPLACED THE LT MLG ACTUATOR IAW MM 32-30. OPERATIONAL CHECKS OF THE GEAR SWINGS ALL CHECKED NORMAL. LANDING GEAR ACTUATOR PN 114-380041-15, SN OFF 0722A. 2 L 7 2 4T 3 T RT A24CE E2NE 2008050800094 20080508 00094 CE 2008 5 8 CIEA200800001 1 20080102 A 2612 24409135 FIRE LOOP LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP RT ENGINE DETERIORATED E CIEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 717EB 9636 016 THE MASTER CAUTION SYSTEM AND RT ENGINE FIRE WARNING LIGHTS ILLUMINATED NEAR THE TOP OF THE CLIMB. THRUST REDUCTION EXT INGUISHED THE LIGHTS. AFTER SOME CONSIDERATION, THRUST WAS THEN SLOWLY ADDED TO AN APPROXIMATE CRUISE SETTING. AFTER O NE MINUTE AT THE CRUISE SETTING, THE LIGHTS ILLUMINATED AGAIN. REDUCTION OF THE THRUST RESULTED IN THE LIGHTS EXTINGUIS HING. ENGINE WAS KEPT AT IDLE POWER DURING DIVERSION TO ALTERNATE SUITABLE AIRPORT. LIGHT NEVER ILLUMINATED AGAIN. MA INT CHECKED SYS AND DETERMINED THE ENG TAIL PIPE SECTION OF FIRE LOOP WAS BREAKING DOWN AND ALLOWING A FALSE FIRE WARNIN G. AS OF THIS REPORT THE FIRE LOOP WAS NOT YET REPLACED. THE ACTUAL TIME AND CYCLES ON THE FIRE LOOP IS BEING INVESTIG 2 L 7 2 4F 4 F A10CE E6WE 2008050800101 20080508 00101 NM 2008 5 8 HALA0800558 1 20080503 A 5230 SKIN BOEING 767 7673CB 1385187 NM CARGO DOOR GOUGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 592HA 33466 GOUGE ON EXTERNAL SKIN OF BULK CARGO DOOR, (22 INCH FROM FWD EDGE, 36 INCHES FROM BOTTOM EDGE) D=.008, L=3", W=1". CLEA NED, TREATED, PRIMED AND PAINTED DAMAGE PER SRM 51-10-02, BLEND REPAIR OVERLAPS 4 RIVETS, NO CRACK INDICATIONS WITH EDDY CURRENT, ACCOMP HAL M105 FILE NR 5920033 PERMANENT REPAIR WITHIN 50 FLT HRS, HRS 19688:54. OK FOR SERVICE, OK TO CONT PER HAL M105 FILE NR 592033. 2 L 7 2 4F RT A1NM 2008050800103 20080508 00103 NM 2008 5 8 HALA0800568 1 20080423 A 5512 SKIN BOEING 767 7673CB 1385187 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 588HA 33466 LEVEL 2 CORROSION ON THE HORIZONTAL STAB CENTER SECTION UPPER SURFACE SKIN AT LBL 14, STR 3, AROUND 5 FASTENERS. REWORK ED PER SRL 55-10-01 FIG 101, REV 76. 2 L 7 2 4F RT A1NM 2008050800104 20080508 00104 CE 2008 5 8 DXTA200803012 1 20080422 A 2120 73838433 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL AFT SERVICE BAY ODOR E DXTA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 982QS 7500182 WITH APU ON AN OILY MUSTY ODOR IS PRESENT WITH THE CABIN AND COCKPIT PAC'S COOLING THE AC. REMOVED AND REPLACED AFT ACM IAW MM CHAPTER 21-51-00. OPERATIONAL AND LEAK CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008050800107 20080508 00107 NM 2008 5 8 HALA0800566 1 20080423 A 5512 SKIN BOEING 767 7673CB 1385187 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 588HA 33466 LEVEL 2 CORROSION ON THE HORIZONTAL STAB CENTER SECTION UPPER SURFACE SKIN AT RBL 13, STR 3, ON 2 FASTENERS. REWORKED P ER SRM 55-10-01, FIG 101, REV 76. 2 L 7 2 4F RT A1NM 2008050800110 20080508 00110 NM 2008 5 8 HALA0800569 1 20080424 A 5512 SKIN BOEING 767 7673CB 1385187 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 588HA 33466 LEVEL 2 CORROSION ON THE HORIZONTAL STAB CENTER SECTION, UPPER SURFACE SKIN, RBL 32.5, STR 7, AROUND 1 FASTENER. CORROS ION REMOVED AND SURFACE FINISH RESTORED, IAW SRM 55-10-01, FIG 101, REV 76 AND ANZ T.I. 190114804-0001. 2 L 7 2 4F RT A1NM 2008051400042 20080514 00042 NM 2008 5 14 ASAA0842923 1 20080501 A 5755 654645262A SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 LEFT WING NR 4 SPOILER HAS MULTIPLE DENTS ON THE UPPER SURFACE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008051400047 20080514 00047 NM 2008 5 14 ASAA0852929 1 20080504 A 2120 UNKNOWN BOEING 737 737890 1384527 NM CABIN & COCKPIT ODOR A ASAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 02 579AS 35187 STRONG ODOR IN BOTH CABIN & FLIGHT DECK DURING DESCENT. STRONGEST IN MID DESCENT BELOW 10000, F/A'S CALLED F/O TO REPOR T STRONG DIRTY SOCK ODOR. OPERATED AC PACKS DURING HIGH POWER ENGINE OPERATION, TEMP SETTING OF PACKS WERE FROM HOT TO COLD, NO DIRTY SMELL NOTED. RAN APU AND OPERATED BOTH LEFT AND RIGHT PACKS, NO ODOR NOTED. AC REQUIRES FVR NON ETOPS R EVENUE FLIGHT TO DETERMINE NO UNUSUAL ODORS PRESENT. ACCOMPLISHED MAINTENANCE PER MM SUPP 05 60 00 PG 101. REF LOG PAG E 6436408 VERIFICATION FLT SATISFACTORY, THIS CLEARS THE FVR DEFERRAL. 2 L 7 2 4F RT A16WE 2008051400060 20080514 00060 WP 2008 5 14 08FDEA01672 1 20080429 A 5350 SKIN DOUG MD10 MD1010F 3022112 WP TAILCONE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 THE TAILCONE, RIGHT SIDE EXTERNAL SKIN HAS A DENT. REMOVED THE DAMAGE FROM THE RIGHT SIDE EXTERNAL SKIN OF THE TAILCONE IAW SRM 53-00-01; PGS 46 & 50; VOL I. FABRICATED REPAIR DOUBLER; ALODINED; PRIMED AND TOP COATED IAW SRM 51-21-01; VOL II. 2 L 7 3 4F RT A22WE 2008051400061 20080514 00061 WP 2008 5 14 08FDEA01674 1 20080429 A 5420 ASL00411 RUB STRIP DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 1 ENGINE OUTBD CORE COWL UPPER T/E CHAFE STRIP IS WORN. BLENDED AREA; ALODINED; PRIMED AND PAINTED IN REF TO EA 8-71 10-118486. 2 L 7 3 4F RT A22WE 2008051400062 20080514 00062 WP 2008 5 14 08FDEA01675 1 20080429 A 5420 ASL00402 RUB STRIP DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 1 ENGINE INBD CORE COWL FWD CHAFE STRIP IS WORN IN SEVERAL PLACES. REMOVED THE ASL 0040-2N ADAPTER IAW SRM 51-35-01; VOL II. DRILLED AND LOCATED NEW ASL 0040-2N ADAPTER IAW SRM 51-35-01; VOL II AND DWG ASL 0040 REV J. INSTALLED NEW ASL 0040-2N ADAPTER IAW SRM 51-35-01; VOL II AND DWG ASL 0040, REV J. 2 L 7 3 4F RT A22WE 2008051400082 20080514 00082 NM 2008 5 14 CALA0800443 1 20080511 A 5311 65C34355 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 LEFT SIDE BS 482 I/B ATTACH FASTENER HOLE ON AIR CONDITIONING (A/C) BRACKET CRACKED. REPAIRED CRACKED FRAME AT 482 S8 - S9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 2008051400093 20080514 00093 EU 2008 5 14 2008UALA02462 1 20080427 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 494UA 1840 FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHT OUT AT SEAT 26C. FOUND LOOSE PLUG. SECURED PLUG AND LIGHTS TEST OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008051400095 20080514 00095 NM 2008 5 14 2008UALA02472 1 20080425 A 2697 CONTACT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE SWITCH DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 WHEEL WELL FIRE LIGHT TESTS OK DURING LIGHT TEST DOESN'T ILLUM DURING FIRE TEST. FOUND SWITCH CONTACTS DIRTY. CLEANED S WITCH CONTACTS, REINSTALLED, WORKS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008051400097 20080514 00097 NM 2008 5 14 2008UALA02474 1 20080425 A 3350 284N140225 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 588UA 26717 EXTERIOR EMERGENCY LIGHTS INOP OUTSIDE DOORS 2R AND 4L. FOUND LAMPS INOPERATIVE. REPLAMPED, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 2008051400099 20080514 00099 2008 5 14 2008UALA02475 4 20080425 A 2565 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 DOOR SLIDE LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 510UA 24780 FOUND DOOR 3L SLIDE ARMED LIGHT INOP. FOUND LIGHT ASSY LOOSE. SECURED LIGHT ASSY AND ARMED DOOR AND LIGHT CAME ON. 2 L 7 2 4F 4 F RT A2NM E17NE 2008051400129 20080514 00129 EU 2008 5 14 AALA200800928 1 20080411 A 3350 321441 POWER SUPPLY AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14065 508 JFK - EMERGENCY LIGHT AT OVERHEAD LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED POWER SUPPLY UNIT FOR EMERGENCY LIGHT AT O VERHEAD LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008051400130 20080514 00130 EU 2008 5 14 NSVA2008025 1 20080509 A 2613 CONNECTOR SAAB SF340 340B 7860101 EU SENSOR DIRTY A NSVA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 242CJ 340B242 TAIL PIPE HOT LIGHT IN FLIGHT. CLEANED CONNECTIONS ON TAILPIPE HOT LIGHT SENSORS, OPS CHECK GOOD IAW SAAB MM 26-12-00. 2 L 7 2 4T RT A52EU 2008051400135 20080514 00135 NM 2008 5 14 SWAA082561 1 20080511 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008051400136 20080514 00136 EA 2008 5 14 SWIA200819592 1 20080504 A 5751 LINK CNDAIR CL600 CL6002C10 1390015 EA AILERON WORN A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 609SK 10020 FLT 4110 - EXCESSIVE AILERON TRIM REQUIRED IN ORDER TO MAINTAIN COORDINATED FLIGHT. REPLACED RIGHT AILERON LINKS, BOLTS AND BUSHINGS IAW 27-15-01. 2 L 7 2 4F RT A21EA 2008051400139 20080514 00139 SO 2008 5 14 SWIA200819593 1 20080504 A 4990 OIL SYSTEM EMB 120 EMB120ER 3260203 SO APU OVERSERVICED A SWIA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 297SW 120327 FLT 3573 - SMOKE REPORTED IN THE CABIN WHEN PACKS WERE RAN OFF OF APU. REMOVED EXCESS OIL FROM APU RESERVOIR. RAN APU AND BOTH PACKS FOR 15 MINUTES WITH NO EVIDENCE OF SMOKE. 2 L 7 2 4T RT A31SO 2008051400141 20080514 00141 SO 2008 5 14 SWIA200819594 1 20080505 A 6121 CONNECTOR EMB 120 EMB120ER 3260203 SO PROP SYNC CONTAMINATED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 236SW 120312 FLT 3605 - RIGHT PROP NP WAS FLUCTUATING IN FLIGHT. INSPECTED AND CLEANED OIL FROM RIGHT PROP SYNC PICK-UP SENSOR CONNE CTOR. OPS CHECK GOOD IAW EMB 120 MM 61-24-00. 2 L 7 2 4T RT A31SO 2008051400142 20080514 00142 EA 2008 5 14 SWIA200819595 1 20080502 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA CABIN AIR DIRTY A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 910EV 18437 17906 7727 FLT 3758 - RECEIVED A "SMOKE TOILET" MESSAGE ON ROTATION. REPLACED RIGHT ACM IAW CRJ MM 21-51-10 AND REPLACED BOTH COAL ESCER BAGS AS REQUIRED. NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A21EA 2008051400148 20080514 00148 NM 2008 5 14 SWAA082548 1 20080509 A 5330 6545777 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008051400150 20080514 00150 NM 2008 5 14 SWAA082547 1 20080509 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 779, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008051400151 20080514 00151 NM 2008 5 14 SWAA082549 1 20080509 A 5330 6545777 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008051400155 20080514 00155 EA 2008 5 14 SWIA200819600 1 20080507 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS CHAFED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 919SW 7657 FLT 6423 - CEILING EMERGENCY LIGHT IS INOP. REPAIRED A CHAFED WIRE TO NR 4 ELBP CONNECTOR IAW MM 20-00-00. OPS CHECK G OOD. 2 L 7 2 4F RT A21EA 2008051400157 20080514 00157 EA 2008 5 14 SWIA200819601 1 20080502 A 5320 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA POWER RECEPTICAL CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 930SW 7713 FLT 6043 - EXTERNAL POWER RECEPTACLE SUPPORT MEMBER IS CRACKED. REPLACED EXTERNAL POWER RECEPTACLE SUPPORT MEMBER PER R EO 601R53-11-009 AND REO 601R53-11-1391. 2 L 7 2 4F RT A21EA 2008051400163 20080514 00163 NM 2008 5 14 DHL2008780006 1 20080511 A 5320 WEB BOEING 727 727223 1384074 NM BS 1220 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 CUT OUT DAMAGE ON AFT STAIRWELL LT TORQUE BOX WEB AT BS 1220, LBL 21, FABRICATED REPAIR DOUBLER, AND INSTALLED PER B727 SRM 53-10-2 FIG 6, AND 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2008051400167 20080514 00167 EA 2008 5 14 SWIA200819608 1 20080407 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 763SK 10228 FS 280 FLOORBEAM IS CRACKED, FOUND AT C-CHECK. REPLACED WITH NEW FS280 FLOORBEAM PER REO670-53-11-047. 2 L 7 2 4F RT A21EA 2008051400168 20080514 00168 NM 2008 5 14 DHL2008780003 1 20080511 A 5320 WEB BOEING 727 727223 1384074 NM BS 1230 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 CUT OUT DAMAGE ON AFT STAIRWELL LT TORQUE BOX WEB AT BS 1230, LBL 21, FABRICATED REPAIR DOUBLER, AND INSTALLED PER B727 SRM 53-10-2 FIG 6, AND 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2008051400169 20080514 00169 NM 2008 5 14 DHLA200800048 1 20080513 A 3350 1000677 LIGHT BOEING 727 727214 138407R NM CABIN INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 GL 05 788AT 21958 FLT NR 177, FORWARD ENTRY DOOR EMERGENCY LIGHT INOP DURING STBY PWR CHECK. REMOVED AND REPLACED LIGHT ASSY IAW AMM 33-5 0-01. OPS CHECK NORMAL. AIRCRAFT WAS GROUNDED. 2 L 7 3 4F A3WE 2008051400171 20080514 00171 NM 2008 5 14 AALA200800930 1 20080411 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 LAX - SEAT MOUNTED AND OVERHEAD EMERGENCY LIGHTS AT LEFT SEAT ROWS 21 TO 24 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED AND OVERHEAD EMERGENCY LIGHTS AT LEFT SET ROWS 21 TO 24. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008051400175 20080514 00175 NM 2008 5 14 F3LA200800248 1 20080501 A 5311 D53477185000 FRAME AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO LATERAL FLOORBOARD FRAMES AT FRAME 59 BETWEEN STRINGERS 38 LEFT AND 38 R IGHT HAS CORROSION AROUND NUT CLIP HOLES. MAINTENANCE REMOVED CORROSION ON CONNECTING ANGLES, FABRICATED NEW CONNECTING ANGLE. TREATED, PRIMED, TOP COATED AND INSTALLED NEW CONNECTING ANGLE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42 -11, SRM 51-74-00, SRM 51-21-11 AND SRM 51-75-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008051400177 20080514 00177 NM 2008 5 14 AALA200800931 1 20080411 A 5320 WEB BOEING 767 767223 1385123 NM BS 287 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AA 22333 AFW - NOSE WHEEL WELL AFT WEB AT STATION 287 RBL 25 DAMAGED. AREA OF DISCREPANCY IS 1 INCH BY 1 INCH. REPAIRED NOSE WH EEL WELL AFT WEB PER MRB 767 3178. 2 L 7 2 4F RT A1NM 2008051400226 20080514 00226 2008 5 14 A6WA200840335 4 20080413 A 3420 FAN CNDAIR CL600 CL6002B19 1900309 EA INSTRUMENT PNL MISINSTALLED A A6WA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 GL 31 431AW 7256 CAPTAIN AND F/O RECEIVED DISPLAY TEMP MESSAGE ON PFD`S. BOTH ATTITUDE INDICATORS SHOW BLACK. FOUND COCKPIT DISPLAY COO L GROUND FAN CONNECTOR LOOSE. SECURED CONNECTOR AS REQUIRED. ALSO FOUND COCKPIT DISPLAY COOL FLIGHT FAN INSTALLED BACK WARDS. RE-INSTALLED FLIGHT FAN IAW AMM 21-24-19. DISPLAY COOL SYSTEM OPS CHECK GOOD IAW AMM 21-24-19. CAPT AND F/O`S PFD DISPLAY TEMP CAUSED BY FAULTY DISPLAY COOLING SYSTEM. BOTH PFD`S OPS CHECK GOOD IAW AMM 31-61-01. 2 L 7 2 4F RT A21EA 2008051400227 20080514 00227 NM 2008 5 14 2008UALA02534 1 20080430 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1400-1420 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 INTERCOSTAL AT STA 1400-1420 AND RBL 3 IS CRACKED. MAJOR REPAIR ACCOMPLISHED, INSTALLED ANGLE REPAIR WITH FILLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2008051400229 20080514 00229 NM 2008 5 14 2008UALA02536 1 20080430 A 4900 MR49613 CONTROLLER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE APU FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 671UA 30026 APU STARTED AND THEN QUIT. REPLACED CONTROLLER PER MM 49-61-05 OPS NORMALAC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008051400232 20080514 00232 NM 2008 5 14 2008UALA02541 1 20080501 A 3500 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 845UA 1585 O2 REQUIRES SERVICING. SERVICED CREW O2, NO LEAKS WERE NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008051400235 20080514 00235 NM 2008 5 14 SWAA082605 1 20080512 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008051400239 20080514 00239 NM 2008 5 14 SWAA082558 1 20080511 A 5311 6546537 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 578, STR 13R. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2008051400240 20080514 00240 NM 2008 5 14 SWAA082534 1 20080511 A 5551 6551524 FITTING BOEING 737 7373H4 1384600 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND RT AND LT HORIZONTAL STABILIZER FITTING CLEVIS LUG FACES CORRODED. REPAIRED FITTING P ER SRM. 2 L 7 2 4F RT A16WE 2008051500003 20080515 00003 2008 5 15 HALA0800577 4 20080512 A 2397 7926140001 COUPLER BOEING 767 767332 1382001 NM HF XMITER DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, NR 2 HF RADIO UNABLE TO TRANSMIT. REPLACED NR 2 HF COUPLER, OPS CK OK WITH SFO OK PER MM 23-1 1-03. 2 L 7 2 4F RT A1NM 2008051500004 20080515 00004 NM 2008 5 15 HALA0800500 1 20080405 A 5330 SKIN BOEING 767 767332 1382001 NM BS 143 L28R DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23276 LIGHTNING STRIKE AT FUSELAGE STA 143.5 LONG 28R. OK TO CONTINUE PER SRM-53-00-01. REPAIRED DAMAGED FASTENER PER REPAIR 8 (SRM 53-00-01 2R-8) USING "SOLID FASTENERS". 2 L 7 2 4F RT A1NM 2008051500005 20080515 00005 EU 2008 5 15 TRBA2008051 1 20080509 A 3240 BRAKE ASSY AEROSP ATR72 ATR72212 8680945 EU MLG INOPERATIVE A TRBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 29 270AT 270 CAPT REPORTED BRAKE PROBLEMS. CAPT RT BRAKE AND F/O LT BRAKE INOP. AWAITING AML PAGE FOR DETAILS. 2 H 7 2 4T RT A53EU 2008051500008 20080515 00008 WP 2008 5 15 IXXA08SMN112S 1 20080327 A 5753 SKIN DOUG DC8 DC873F 302199F WP RT WING TE FLAP DELAMINATED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 5 VANE FLAP DELAMINATED SKIN BETWEEN STATION XF 345.000 TO ST A XF 404.000. REMOVED AND REPLACED RIGHT WING NUMBER 5 VANE FLAP. PERFORMED OPS CHECK GOOD TO FLAP SYSTEM IAW DC8 MM 2 7-51-14 PAGES 201-202, AND DC8 MM 27-50-0 PAGES 506-507. 2 L 7 4 4F RT 4A25 2008051500010 20080515 00010 SW 2008 5 15 WGEA200800057 1 20080513 A 3244 M16901 TIRE ECLIPS EA500 ECLIPSEEA500 3350000 SW RT MLG FAILED E WGEA O OTHER O OTHER LD LANDING 1 EA 27 139DJ 000054 RIGHT MAIN TIRE BLEW ON FIRST APPLICATION AT 82 KTS, 3 WHEELS ON RUNWAY, STICK FWD AND INTO WIND. REMOVED RT MLG WHEEL ASSY, INSPECTED BRAKE ASSEMBLY, GEAR DOOR, WING AND FLAP SURFACE FOR DAMAGE. NO DEFECTS NOTED. INSTALLED SERVICEABLE W HEEL AND TIRE ASSEMBLY IAW EA 500 AMM 32-42-00. 1 L 7 2 4J RT A00002AC 2008051500018 20080515 00018 WP 2008 5 15 NWAA082049884 1 20080509 A 2913 FUSE DOUG DC9 DC951 3022051 WP HYD PUMP FAILED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 01 677MC 47756 AS THE AIRCRAFT WAS BEING PUSHED BACK FOR DEPARTURE, THE RIGHT HYDRAULIC SYSTEM LOST ALL FLUID. COM PROCEDURES WERE COM PLIED WITH AND THE AIRCRAFT RETURNED TO THE GATE WITHOUT ANY FURTHER PROBLEM. MAINTENANCE FOUND A HYDRAULIC FUSE IN THE RIGHT WHEEL WELL HAD FAILED. THE FAILED FUSE, THE ELECTRICAL AUXILIARY HYD PUMP, THE ENGINE DRIVEN HYD PUMP, AND ALL A PPLICABLE HYDRAULIC SYSTEM FILTERS WERE REPLACED. NO DEBRIS WAS FOUND IN ANY FILTER OR PUMP HOUSING. LEAK CHECK AND OP ERATIONAL CHECK WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008051500020 20080515 00020 NM 2008 5 15 NWAA082056729 1 20080511 A 3350 BATTERY PACK BOEING 747 747251F 1384898 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 DURING OVERNIGHT CHECK, FOUND UPPER DECK EXIT DOOR SLIDE EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED BATTER Y PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008051500021 20080515 00021 NE 2008 5 15 IXXA080020O 2 20080508 A 7320 MOTOR DOUG DC8 DC872F 302199E WP GE CFM56 CFM562C 13802 NE FUEL BLEED VALVE DEFECTIVE A IXXA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SW 11 721CX 30341 3179 46013 693261 DURING CLIMB-OUT FROM MLB AT FL350 NUMBER ONE ENGINE FLAMEOUT. THE CREW ACCOMPLISHED FLAMEOUT PROCEDURES AND DESCENDED TO FL210 FOR ENGINE RESTART. THE ENGINE RESTARTED NORMALLY AND THE CREW CONTINUED FLIGHT AND LANDED IN TOL WITHOUT INCI DENT. MAINTENANCE REMOVED AND REPLACED NUMBER ONE GEAR FUEL BLEED VALVE MOTOR. OPERATIONAL CHECK GOOD IAW CFM MAINTENA NCE MANUAL 75-31-10 AND GMM 3.116. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 2008051500026 20080515 00026 NM 2008 5 15 2008UALA02546 1 20080430 A 3350 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 665UA 29237 EMERGENCY LIGHTS AT RIGHT SIDE FROM ROW 26 BACK ON WITH SWITCH ARMED, WENT OFF WITH SWITCH OFF. REPLACED EMERGENCY LIGH T POWER SUPPLY FOR EEL LIGHTING PRECAUTIONARY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008050800125 20080508 00125 NM 2008 5 8 2008UALA02565 1 20080502 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EEL LIGHT INOP UPPER DECK CEILING, ROW 16. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008050800127 20080508 00127 NM 2008 5 8 2008UALA02566 1 20080502 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EEL LIGHT INOP UPPER DECK CEILING, ROW 17. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008050800128 20080508 00128 CE 2008 5 8 DXTA200803025 1 20080426 A 3240 38771 RELAY BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE BRAKES INOPERATIVE E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 161QS 236 RK435 DURING TAXI OUT, IT REQUIRED COMPLETE RUDDER PEDAL COMPRESSION TO ENGAGE THE BRAKES. TROUBLESHOT, REMOVED AND REPLACED POWER BRAKE VALVE. PERFORMED BRAKE SYSTEM FUNCTIONAL TESTING, NO DISCREPANCIES NOTED AT THIS TIME. SERVICES HYDRAULIC RESERVOIR. PERFORMED OPERATIONAL TEST, NO DISCREPANCIES NOTED AT THIS TIME. IAW AMM 32-40-00 & 12-10-00. 2 H 7 2 4F 4 F RT A16SW E25EA 2008050800131 20080508 00131 EU 2008 5 8 2008UALA02572 1 20080502 A 5610 WINDOW AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 433UA 589 F/O SLIDING WINDOW HAS BUBBLES FORMING ON ENTIRE WINDOW. HOT TO TOUCH. REPLACED F/O SLIDING WINDOW. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050800133 20080508 00133 NM 2008 5 8 2008UALA02574 1 20080502 A 2560 D31591478U1 GIRT BAR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE DOOR 1R OUT OF TOLERANCE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 302UA 23643 DOOR 1R GIRT BAR BROKE. FOUND GIRT BAR STOWAGE BRACKET FASTENERS LOOSE. SECURED BRACKET. BAR STOWS OK. AC OK FOR SERV ICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050800135 20080508 00135 NM 2008 5 8 2008UALA02552 1 20080501 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD GALLEY DOOR FWD LOWER FRAME IS CRACKED AT THREE FASTENER HOLES UNDER STOP FITTING. MAJOR REPAIR ACCOMPLISHED, REMOV ED DAMAGED SECTION. INSTALLED FRAME REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050800140 20080508 00140 NM 2008 5 8 F3LA200800220 1 20080501 A 5321 D5397497200200 FLOORBOARD AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO LATERAL FLOORBOARD PROFILE AT FRAME 56 BETWEEN STRINGER 38 LEFT AND 41 R IGHT HAS AREA OF CORROSION AROUND NUTPLATES. MAINTENANCE REMOVED AND REPLACED AFT CARGO FLOORBOARD PROFILE AT FRAME STA TION 56 IN ACCORDANCE WITH THE REQUIRMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND AC CEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050800142 20080508 00142 NM 2008 5 8 F3LA200800221 1 20080501 A 2571 D5391215720000 BATTERY BOX AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE LOOSE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED THE FORWARD BATTERY TRAY AFT OUTBOARD MOUNT HAS EXCESSIVE PLAY CAUSING FRETTING. MAINTENANCE REMOVED AND REPLACED AFT OUTBOARD MOUNT FROM FORWARD BATTERY TRAY IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050800144 20080508 00144 CE 2008 5 8 GUUA04240801 1 20080424 A 3234 1013841377 CONTROL SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE COCKPIT INOPERATIVE A GUUA O OTHER O OTHER CL CLIMB 1 SO 29 231YV UE231 FLIGHT: 9280, DOING A GO AROUND, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION UNLESS THE DOWN LOCK RELEASE SWITCH WAS USED, THE GEAR FAILED TO RETRACT WITH THE HANDLE IN THE UP POSITION, LANDING GEAR CIRCUIT BREAKER POPPED. RE PLACED LANDING GEAR HANDLE CONTROL SWITCH. OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 2008050800145 20080508 00145 WP 2008 5 8 UPS08852118 1 20080419 A 5320 5641543135 GUSSET DOUG DC8 DC873F 302199F WP SUBFLOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 A/C COMPARTMENT AT SUBFLOOR CEILING STA 60 APPROX RBL 45 GUSSET AT BOTTOM OF FLOORBEAM HAS MODERATE C ORROSION. FABRICATED AND REPLACED FLOORBEAM GUSSET AT STA 60 AND RBL 45 IAW SRM 51-1-8, SRM 53-02-00-0 FIG 001F AND DWG 5641543. 2 L 7 4 4F RT 4A25 2008050800146 20080508 00146 SO 2008 5 8 GLBA20061091 1 20080425 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE COCKPIT & CABIN SMOKE A GLBA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 297UX 120297 SMOKE/SMELL, FLIGHT 5120, PILOTS REPORTED SMOKE IN THE COCKPIT AND CABIN AFTER LANDING SMOKE ALARM WENT OFF AT THE GATE. MAINT INSPECTED BOTH AIR CONDITIONING PACKS NO DISCREPANCIES NOTED. PERFORMED DUAL ENGINE STARTS, TAXIED AC, PERFORMED HIGH POWER ENGINE RUNS, OPERATED ALL SYS, RECIRCULATION FANS, WINDSHIELD HEAT, GENERATORS, RAN AC APPROX 30 MINS, PERFO RMED TEST OF SMOKE DETECTION SYS IAW 26-13-00. NO DISCREPANCIES NOTED, COULD NOT DUPLICATE DISCREPANCY. SUBSEQUENT OPERA TIONAL CHECK FLIGHT WAS SATISFACTORY. 2 L 7 2 4T 4 T RT A31SO E20NE 2008050800147 20080508 00147 WP 2008 5 8 UPS08852119 1 20080424 A 5712 RIB DOUG DC8 DC873F 302199F WP RWS 458 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 RT WING CENTER LE UPPER RIB CRACKED XFS 458. REPAIRED RT WING CENTER LE UPPER RIB AT XFS 458 IAW SRM 57-03-03-FIG 0 05 AND SRM 57-02-00-0 FIG 002 SHT 2. 2 L 7 4 4F RT 4A25 2008050800148 20080508 00148 WP 2008 5 8 UPS08852120 1 20080420 A 5730 SKIN DOUG DC8 DC873F 302199F WP LH WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING OUTBD LE 5 CRACKS AT 3 SCREW HOLES XFS 603.75 TO XFS 606.75 UPPER SURFACE INBD END, EXTERIOR SKIN. REPAIRED LT WING OUTBD LE EXTERIOR SKIN FROM XFS 603.75 TO XFS 606.75 IAW SRM 57-02-01-0 FIG 038 AND SRM 57-02-01 -0. 2 L 7 4 4F RT 4A25 2008050600004 20080506 00004 EU 2008 5 6 08FDEA01658 1 20080429 A 5532 A55373311008 PANEL AIRBUS 300 A300F4605R 3930327 EU VERTICAL STAB DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 VERTICAL STAB L/E PANEL 322 CL IS DAMAGED ON THE L/E 6 INCHES FROM THE LOWER END. REPAIRED ERROSION STRIP LOWER END ON VERTICAL LE PANEL 300 CL IAW AMM 55-32-11-8 & SRM 55-32-00. 2 L 7 2 4F RT A35EU 2008050600005 20080506 00005 EU 2008 5 6 08FDEA01659 1 20080429 A 5532 A55373311108 PANEL AIRBUS 300 A300F4605R 3930327 EU VERTICAL STAB UNSECURE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 VERTICAL STAB L/E PANEL 322 CL HOIST POINT IS NOT SECURED ON THE INTERIOR SIDE. REPAIRED CRACKED POTTING WITH NEW POTTI NG EC 3500 MB / A IAW DWG 33-A53373311 AMM 55-32-11 AND SRM 51-35-10 PG 17. 2 L 7 2 4F RT A35EU 2008050600020 20080506 00020 NM 2008 5 6 USAA920080953 1 20080414 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 833AW 1844 PHX - EMERGENCY EQUIPMENT - FLIGHT NUMBER 0081, AFT FLIGHT ATTENDANT'S FLASHLIGHT IS INOPERATIVE. REPLACED THE BATTERY IN THE AFT FLIGHT ATTENDANT'S FLASHLIGHT. 2 L 7 2 4F RT A28NM 2008050600033 20080506 00033 NM 2008 5 6 ASAA0842855 1 20080330 A 5753 6546435281 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 LT OUTBOARD T/E AFT FLAP LWR SKIN HAS 3 DENTS AT WBL 231.5 TO 240 2.5" FROM T/E. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 2008050600035 20080506 00035 NM 2008 5 6 ASAA0842865 1 20080323 A 5753 6546434244 SKIN BOEING 737 737490 1384715 NM RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 RT WING TRAILING EDGE RT WING INBOARD AFT FLAP LOW SURFACE HAS A SHARP DENT IN LEADING EDGE CAP AT OUTBOARD ACTUATING RO D. DENT ON LT WING TRAILING EDGE RT WING AFT FLAP LOWER SURFACE WAS REPAIRED IAW B737 400 SRM 57 53 01. 2 L 7 2 4F RT A16WE 2008050600053 20080506 00053 NM 2008 5 6 2008UALA02510 1 20080428 A 2611 PPA120100 SMOKE DETECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LAVATORY FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 854UA 1731 SMOKE LAV DETECT FAULT ECAM. SMOKE DETECTOR NOT WORKING (AFT LAV). REPLACED AFT LAV SMOKE DETECTOR, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050600064 20080506 00064 NM 2008 5 6 08FDEA01697 1 20080430 A 5320 69448775 WEB BOEING 727 727232 1384082 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 CORROSION ON WEB TO BODY SKIN ON ANGLE ON WEB BETWEEN BS 950A TO 950B, LBL 18, WL 141 REPLACED WEB AT STA 950 - 950B, LB L AND CLIP AT STA 950A LBL 18 REF BOEING DWG 69-44877 AND SRM 51-30-3. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008050600075 20080506 00075 NM 2008 5 6 AALA200800805 1 20080402 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 24G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD SEAT 24G. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050600076 20080506 00076 NM 2008 5 6 AALA200800802 1 20080402 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 692AA 26972 DFW - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008050600079 20080506 00079 WP 2008 5 6 AALA200800823 1 20080405 A 3350 OL1098BPEGPL LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 419AA 49331 TPA - EMERGENCY LIGHT AT SEAT 17D MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008050600084 20080506 00084 EU 2008 5 6 08FDEA01702 1 20080430 A 5310 R53611166 DOUBLER AIRBUS 310 A310203 3930313 EU R1 DOOR FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 445FE 297 THE DOUBLERS AT THE AFT LOWER AND FWD LOWER CORNERS OF THE R1 DOOR ARE ALUMINUM AND REQUIRE REMOVAL FOR COMPLYING INSP ECTION OF AD TASK CARD EO E6-5310-7-3318. REMOVED EXISTING DOUBLERS BELOW R1 DOOR, FWD AND AFT LOWER CORNERS. FABRICAT ED REPAIR DOUBLERS AND INSTALLED IAW AIRBUS DRAWING R5361166 AND FEDEX EA6-5310-121243, DATED 11 APRIL, 2008. 2 L 7 2 4F RT A35EU 2008050600090 20080506 00090 NM 2008 5 6 HALA0800552 1 20080424 A 5347 SEAT TRACK BOEING 767 7673CB 1385187 NM BS 911 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 588HA 33466 LEVEL 2 CORROSION ON BOTH TRACK FITTINGS WHERE FEET OF STA 911 PARTITION ATTACHES TO FLOOR. BOTH TRACK FITTINGS REPLACE D IAW 767-300 SRM 51-40-02 REV 76 AND DWG 145T5222. 2 L 7 2 4F RT A1NM 2008050600094 20080506 00094 NM 2008 5 6 NWAA081866717 1 20080410 A 5330 SKIN BOEING 747 747251F 1384898 NM BS 2680-2690 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 617US 21121 DURING LINE MAINTENANCE, FUSELAGE SKIN WAS DAMAGED BETWEEN BS 2680 AND BS 2690 LBL 5. REPAIRED PER EA 67-211627. 2 L 7 4 4F RT A20WE 2008050600106 20080506 00106 EU 2008 5 6 08FDEA01744 1 20080503 A 5347 A53781975202 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 673FE 780 MAIN DECK CARGO SEAT TRACK NR 2 LT HAS CORROSION, 2 SQ INCHES BETWEEN FR 30 AND FR 31. REMOVED LEVEL 1 CORROSION AND RE PAIRED SEAT TRACK NR 2 LT, Y450 WITH SPLICE REPAIR BETWEEN FR 30 AND FR 33 IAW A300-600 SRM 53-10-16, FIG 201, PAGE 207 /208. 2 L 7 2 4F RT A35EU 2008050600109 20080506 00109 EA 2008 5 6 MASA200800356 1 20080430 A 2697 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA FIRE BOTTLE LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17358 7358 FLT 2751, SBP-PHX - CARGO BOTTLE LOW CAUTION MESSAGE. CLEANED AND RESEATED CONNECTOR ON CARGO FIRE BOTTLE, OP GOOD. 2 L 7 2 4F RT A21EA 2008050600114 20080506 00114 EU 2008 5 6 08FDEA01747 1 20080505 A 5720 672LB DEFLECTOR AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND DELAMINATION ON DEFLECTOR DOOR 672LB, INNER SIDE. REPAIR PERFORMED BY BONDING REPAIR IAW SRM 51-77-12, APPROVED B Y RADS/BAE/1006487/2008 IIS A AND EA 6-5755-115272. 2 L 7 2 4F RT A35EU 2008050600126 20080506 00126 NM 2008 5 6 08FDEA01713 1 20080501 A 5313 65562385 STRINGER SPLICE BOEING 727 727232 1384082 NM ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 SO 25 498FE 20867 FWD PIT STRINGER SPLICE AT 27L GOING THROUGH STA 680 CORRODED ON OUTBD SIDE REMOVED CORROSION FROM ORIGINAL THICKNESS OF 0.064 INCH FROM BUTT SPLICE STRAP WITH 0.054" REMAINING. OUT-OF-LIMITS DUE TO "NO REWORK PERMITTED IN BUTT SPLICE STRA P". FABRICATED REPAIR DOUBLER, TREATED, PRIMED AND INSTALLED, REFERENCE SRM 53-30-1 FIGURE NR 1 AND EA NR 7-5330-118259 . REMOVED CORROSION ON STRINGER SPLICE, FROM ORIGINAL THICKNESS OF 0.056 WITH 0.052 INCH REMAINING, 0.004 LOSS AND IS W ITHIN LIMITS. REFERENCE SRM 53-10-1/PAGES 1-2A. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008050600129 20080506 00129 NM 2008 5 6 AALA200800789 1 20080401 A 7997 WIRE BOEING 757 757223 1384957 NM OIL PRESS SWITCH CHAFED A AALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 21 696AN 26976 BOS INFLIGHT T1937/01APR - LEFT ENGINE OIL FILTER MESSAGE. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. FOUND CHAFED W IRE. REPLACED OIL PRESSURE SWITCH AND REPAIRED RELATED WIRE. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008050600130 20080506 00130 EU 2008 5 6 AALA200800790 1 20080401 A 2410 IDG AIRBUS 300 A300B4605R 3930308 EU NR 1 FAULTED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 70054 461 MIA INFLIGHT T618/01APR SDQ TO JFK - NUMBER ONE ENGINE INTEGRATED DRIVE GENERATOR FAULTED. LANDED MIA WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008050700002 20080507 00002 SO 2008 5 7 RAIA00804029 1 20080427 A 5210 DOOR EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 825HK 145510 POST FLT NR 5542 - STL - AIRCRAFT DOOR IS DIFFICULT TO CLOSE. MAINTENANCE CLEANED AND LUBED THE PASSENGER DOOR. OPS CH ECKED GOOD. 2 L 7 2 4T RT T00011AT 2008050700008 20080507 00008 NM 2008 5 7 NOCA02808 1 20080429 A 3350 LP101 LIGHT BOEING 757 75728A 1384976 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 TOP POSITION LAMP INOP AT 3L DOOR EXIT LOCATOR SIGN AT SIDEWALL. REPLACED LAMP AS PER MM 33-51-10. 2 L 7 2 4F RT A2NM 2008050700011 20080507 00011 WP 2008 5 7 DHL2008807502 1 20080420 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 660 DAMAGED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 807DH 91019 45990 MAIN CARGO COMPT FLOORBEAM HOLE MISDRILLED STA 660.000 RBL 32.250" (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 51-2- 1 FIG 1 SHEET 9-12, TR NR 51-130 DATED 01-26-04. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRI CATED REPAIR ANGLE, STRAP AND FILLER (EXTRUSION 7075 T6511 0.125") IAW SRM 51-2-1 FIG 1 SHEET 9-12, TR NR 51-130. CLEAN ED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 51-2-1 FIG 1 SHEET 9-12, T R NR 51-130, SRM 51-1-11, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2008050700012 20080507 00012 WP 2008 5 7 IXXA080016O 1 20080501 A 2612 FIRE LOOP DOUG DC8 DC873F 302199F WP ZONE 400 SHORTED A IXXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 11 606AL 96585 679 46044 DURING CRUISE FROM KTOL, NUMBER THREE ENGINE FIRE WARNING LIGHT AND BELL CAME ON INTERMITTENTLY. THE CREW ACCOMPLISHED THE ENGINE FIRE CHECKLIST AND DISCHARGED BOTH BOTTLES. AFTER BOTH BOTTLES WERE DISCHARGED THE FIRE WARNING CAME ON STEA DY AND STAYED ON JUST PRIOR TO LANDING. THE CREW LANDED IN KICT WITHOUT INCIDENT. MAINTENANCE INSPECTED NUMBER THREE E NGINE INTERNALLY AND REPLACED LEFT AND RIGHT FIRE LOOP CORE DETECTOR, AND LEFT AND RIGHT FIRE LOOP FAN DETECTOR'S. MAIN TENANCE ALSO REPLACED BOTH FIRE BOTTLES. OPERATIONAL CHECK GOOD IAW DACO DC-8 MAINTENANCE MANUAL 26-00, 26-10-0, AND 26 -20-1. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2008050700023 20080507 00023 WP 2008 5 7 AALA200800852 1 20080407 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 968TW 53618 LGA - BATTERY PACK FOR EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FOR WARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008050700024 20080507 00024 EA 2008 5 7 COMA0860231 1 20080422 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAULTY A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 989CA 25507 7215 FLIGHT 5021 - ON APPROACH INTO JFK SELECTED GEAR DOWN AND RECEIVED GEAR DISAGREE WARNING MESSAGE, FOLLOWED BY AMBER NOSE GEAR INDICATION AND NOSE DOOR WARNING. ALL CLEARED WITHIN APPROX 30 SECONDS. AIRCRAFT LANDED SAFELY IN JFK. REMOVED AND REPLACED MLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 2008050700033 20080507 00033 WP 2008 5 7 070196 1 20080427 A 2170 21D101 COALESCER BAG DOUG DC9 DC983 3022083 WP RT A/C PACK SMOKE A WX0A O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 19 864GA 49912 FLIGHT CREW REPORTED RIGHT AIR CONDITIONING PACK ON, SMOKE WAS ENTERING THE CABIN. THE DISCREPANCY WAS DEFERRED PER MEL 21-01 SITUATION 1 WITH ALL M PROCEDURES COMPLIED WITH. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE AIR CONDITIONING SYSTEM AND REPLACED THE RIGHT AND LEFT COALESCER BAGS IAW AMM 21-20-02. RIGHT AND LEFT AIR CONDITIONING SYSTEM OPERATI ONAL CHECK WAS NORMAL. NO SMOKE NOTED IN CABIN. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008050700040 20080507 00040 WP 2008 5 7 08FDEA01715 1 20080501 A 5347 604498 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 309FE 48298 MAIN CARGO COMPT SEAT TRACK HAS GOUGED AREAS AT FS 1381-1401 LBL 8 REPLACED SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1. SE AT TRACK FABRICATED ON MAE TRAVELER T8/737386. SPLICE HAT FABRICATED ON MAE TRAVELER T8/737372. SPLICE PLATES FABRICATE D IAW SRM 53-70-00 FIG 1 VOL 1 USING 7075-T6 .050C BAYCH NR 0001336047. MAIN CARGO COMPARTMENT LBL 8 STA 1381-1401. 2 L 7 3 4F RT A22WE 2008050700042 20080507 00042 WP 2008 5 7 08FDEA01717 1 20080501 A 5720 ARB116210 SUPPORT ANGLE DOUG MD10 MD1010F 3022112 WP RT WING LE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 RIGHT WING LEADING EDGE CAVITY PANEL SUPPORT ANGLE IS CRACKED, OUTBD OF THE NR 8 SLAT TRACK. REMOVED FORMER IAW SRM 51- 35-01 & 51-33-01; VOL II. FABRICATED PER DWG ARB1162, REV "S". ALODINED & PRIMED IAW SRM 51-21-01; VOL II; PGS 21 - 24. INSTALLED IAW SRM 51-35-01 & 51-33-01; VOL II. 2 L 7 3 4F RT A22WE 2008050700050 20080507 00050 NM 2008 5 7 UPS08M52108 1 20080124 A 5420 FAIRING DOUG MD11 MD11 3023602 NM NR 2 ENGINE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C ENG NR 2 EXHAUST FAIRING RT SIDE WITH EXISTING PATCH REPAIR. FPI C/OUT ON EXISTING REPAIR IAW DACNDTS PM R.13 PART08 FOUND NO CRACK EVIDENT ON FAIRING SKIN & REPAIR DOUBLER. NEW REPAIR DOUBLER FAB USING 2219-0 0.071" PER EN 1123-08&MD11-54-20173. REP DOUBLER HEAT TREATED TO T62 PER DPS7.00-1 HARDNESS OBTAINED HRB64.9 IS ACCEPTABLE PER DPS 1.05- REPAIR DOUBLER INSTALLED PER MD11-54-20173&EN1123-08. 2 L 7 3 4F RT A22WE 2008050700053 20080507 00053 WP 2008 5 7 ABXA080140 1 20080428 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 971AX 47497 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00-8. 2 L 7 2 4F A6WE 2008050700073 20080507 00073 WP 2008 5 7 UPS08852098 1 20080411 A 5311 FRAME DOUG DC8 DC873F 302199F WP FS 1580 BENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 MAIN CARGO COMPT STA 1580 RT SIDEWALL STRUCTURE FRAME IS BENT 10" ABOVE CUSP. REMOVED FRAME SECTION FABRICATED FRAME SECTION AND 2 SPLICES. INSTALLED FRAME SECTION AND 2 SPLICES. 2 L 7 4 4F RT 4A25 2008050700076 20080507 00076 WP 2008 5 7 UPS08852110 1 20080429 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 EMERGENCY LIGHTING DIM. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK ASSY IAW AMM 33-50-01-2-4. OPS CHECK NORM AL. 2 L 7 4 4F RT 4A25 2008051500029 20080515 00029 EU 2008 5 15 MALA080067 1 20080505 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 288-363 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 SEAT TRACK STA 288 TO 363 BL 18.3 CORRODED. SEAT TRACK STA 288 TO 363 BL 18.3 REPLACED AS PER EO S533060. 2 L 7 2 4T RT A52EU 2008051500030 20080515 00030 EU 2008 5 15 MALA080070 1 20080505 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 126 CANNING A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 OIL CANNING ON LT COCKPIT SKIN AT STA 126 AND WL 73 BETWEEN RANDOM LATCHES. HFEC C/O NO CRACK. REPAIR DOUBLER INSTALLE D ON LT COCKPIT SKIN AT STA 126 AND WL 73 BETWEEN RADOME LATCHES AS PER EO S53212 (ALUMINUM SHEET 2024T3 3.040 PO NR 121 33 NAS1097AD6-6 PO NR 4292. 2 L 7 2 4T RT A52EU 2008051400152 20080514 00152 NM 2008 5 14 SWAA082550 1 20080509 A 5330 65C3235726 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 489, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008051500014 20080515 00014 2008 5 15 SIMA200813401 4 20080512 A 3420 660011AL03 AHRS EMB 145 EMB145LR 3260212 SO NR 1 INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 906AE 14500894 ON FLIGHT 3794, CREW REPORTED THEY HAD AHARS 1 INOPERATIVE IN FLIGHT AND DESCENDED OUT OF RVSM BECAUSE THAT MESSAGE MAKE S THE AUTO PILOT INOPERATIVE. DID NOT HAVE ENOUGH FUEL AT FL280 TO MAKE IT TO DFW REMOVED AIRCRAFT REMOVED FROM SERVICE . REMOVED AND REPLACED NR 1 AHRS UNIT PER AMM 34-21-01. OPERATIONAL CHECKED GOOD ALSO DEFERRED RVSM 34-50 DUE TO REPLA CEMENT OF AHRS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008051500033 20080515 00033 NM 2008 5 15 F3LA200800246 1 20080508 A 5311 D5367227420000 FRAME AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO LEFT FLOORBOARD FRAME AT STRINGER 38 LEFT BETWEEN FRAMES 58 AND 59 HAS A REAS OF CORROSION AROUND NUT CLIP HOLES. MAINTENANCE REMOVED AND INSTALLED FLOORBOARD FRAME DOOR SILL PLATE AT STRINGER 38 LEFT BETWEEN FRAMES 58 AND 59 IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008051500034 20080515 00034 EU 2008 5 15 2008UALA02527 1 20080429 A 3510 MXP401600U OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CAPTAIN'S FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 470UA 1427 CAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. SWAPPED CAPTS AND 2ND OBS BOX. ALL LINES LEAK CHECKED GOOD. MASK AND RADIO OPS NORMAL AT CAPTAIN'S SPOT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008051500036 20080515 00036 NM 2008 5 15 AALA200800826 1 20080404 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 930AN 29529 MIA - EMERGENCY EXIT SIGN AT RIGHT NUMBER ONE DOOR HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT EXIT SIGN AT RIG HT NUMBER ONE (CLOSED) 2 L 7 2 4F RT A16WE 2008051500038 20080515 00038 EU 2008 5 15 2008UALA02548 1 20080501 A 5320 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 444UA 824 FLOOR SUPPORT CORRODED IN TWO AREAS BETWEEN C69 AND C70, LBL 8". MAJOR REPAIR ACCOMPLISHED, REPLACED FLOOR SUPPORT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008051500041 20080515 00041 WP 2008 5 15 08FDEA01726 1 20080502 A 5420 217000413 FAIRING DOUG MD10 MD1010F 3022112 WP NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 RIGHT SIDE NR 1 PYLON LOWER AFT FAIRING HAS A CRACK APPROX 2 INCHES LONG. REMOVED & INSTALLED FAIRING IN REF TO SRM 51- 31-01 VOL II. REMOVED DAMAGE; FABRICATED REPAIR AND INSTALLED REPAIR IN REF TO SRM 54-00-01 FIG 26 VOL I & SRM 51-33- 01 VOL II. 2 L 7 3 4F RT A22WE 2008051500048 20080515 00048 EU 2008 5 15 08FDEA01737 1 20080502 A 5347 A53275018214 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 673FE 780 MAIN DECK CARGO SEAT TRACK NR 4 LT HAS 2 AREAS OF CORROSION, 2 SQ IN, BETWEEN FR 54.3 AND FR 55 REMOVED LEVEL 1 CORROSIO N AND REMOVED AND REPLACED SEAT TRACK SECTION NR 4 LT IAW A300-600 SRM 53-10-16, FIG 201, PAGE 207/208 BETWEEN FR 54.3 A ND FR 55,-Y1456. 2 L 7 2 4F RT A35EU 2008051500052 20080515 00052 NM 2008 5 15 KNNA20080006 1 20080424 A 5314 KEELBEAM BOEING 737 7372L9 1384497 NM PWA JT8 JT8D9A 52048 NE ZONE 100 CORRODED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 464AT 21278 AFTER OPEN UP, FOUND CORROSION AT RT KEEL BEAM AT STA 727, AREA WENT OUT OF LIMITS AFTER CORROSION REMOVAL. REPAIRED AR EA IAW BOEING MESSAGE 1-522105282 AND IAW SKY KING ACO-0753105. 2 L 7 2 4F 4 F RT A16WE E2EA 2008051500053 20080515 00053 NM 2008 5 15 NWAA081916303 1 20080430 A 5340 ATTACH FITTING BOEING 747 747451 1384940 NM BS 1120 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 663US 23818 DURING SPECIAL VISIT INSPECTION, FOUND LT OUTBOARD STRINGER SHEAR WEB ATTACH PLATE CRACKED AT BS 1120. REPAIRED PER EA 63-210589. 2 L 7 4 4F RT A20WE 2008051500056 20080515 00056 NM 2008 5 15 2008UALA02569 1 20080501 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1400 S26L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 AFT PIT STA 1400 STR 26L HAS ENLONGATED HOLES IN SIDES OF STRINGERS DUE TO REPLACEMENT STRINGER CLIPS ON FRAME REPAIR. MAJOR REPAIR ACCOMPLISHED, CUTOUT DAMAGE, STA 1390 TO 1410. INSTALLED NEW SECTION AND FILLER AND REPAIR SPLICES. 2 L 7 2 4F 4 F RT A2NM E17NE 2008051500059 20080515 00059 NM 2008 5 15 AALA200800868 1 20080408 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 650AA 24608 DFW - EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER THREE D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051500061 20080515 00061 NM 2008 5 15 AALA200800882 1 20080408 A 3350 OL3071BPEGPL LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500065 20080515 00065 EU 2008 5 15 AALA200800865 1 20080408 A 3350 82400 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 25071 514 JFK - EMERGENCY EXIT DOME LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT DOME LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008051500075 20080515 00075 NM 2008 5 15 AALA200800892 1 20080409 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 617AM 24525 MIA - EXTERIOR EMERGENCY LIGHT AT FORWARD LEFT OVERWING DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT FORWARD LEFT OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051500077 20080515 00077 NM 2008 5 15 AALA200800885 1 20080408 A 3350 OL3071BPEGPL LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHT AT SEAT 31G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500083 20080515 00083 NM 2008 5 15 AALA200800902 1 20080410 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 756AM 30264 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET AREA IS DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LE FT NUMBER ONE DOOR CLOSET AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500084 20080515 00084 NM 2008 5 15 AALA200800903 1 20080410 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 756AM 30264 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR GALLEY COMPARTMENT DAMAGED AND WIRING IS EXPOSED. REPLACED LIGHT ASSEMB LY AND SECURED WIRING FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR GALLEY COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT T00001SE 2008051500090 20080515 00090 NM 2008 5 15 DHL2008780005 1 20080512 A 5320 BAC15201247 STIFFENER BOEING 727 727223 1384074 NM BS 930 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 REMOVED CORRODED MATERIAL ON VERTICAL STIFFENER IN LT W/WELL AT BS 930, FABRICATED TYPICAL EXTRUSION REPAIR, AND INSTALL ED REPAIR PER B727 SRM 53-10-2 FIG 4 AND 51-40-4 FIG 1. 2 L 7 3 4F A3WE 2008051500094 20080515 00094 NM 2008 5 15 AALA200800925 1 20080411 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 945AN 30085 DFW - EMERGENCY EXIT LOCATOR LIGHT AT RIGHT FORWARD OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LOC ATOR LIGHT AT RIGHT FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008051500103 20080515 00103 EA 2008 5 15 SWIA200819578 1 20080503 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 912SW 7595 FLT 6498 - CAPTAIN'S WINDSHIELD HAS SEVERAL SMALL CRACKS. REPLACED CAPTAIN'S WINDSHIELD IAW 56-11-01. OPS TEST GOOD, P /N 601R33033-13, S/N OFF 01183H2346. 2 L 7 2 4F RT A21EA 2008051500107 20080515 00107 NM 2008 5 15 DLM90080662 1 20080504 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 579-598 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 RIGHT CUSP WEB CORRODED ON LOWER SURFACE BETWEEN STA 579-598 AT LIGHTNING HOLES. REPAIRED RT CUSP WEB STA 579-598, IAW DELTA ER/A 398191-14MA REV ORIG 09-18-02. 2 L 7 2 4F RT A6WE 2008051500110 20080515 00110 NM 2008 5 15 2008UALA02464 1 20080426 A 3350 362624 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 902UA 25002 FLOOR EEL LIGHTS INOP FROM ROW 16 ON BACK. SUSPECT FAULTY LIGHT ASSEMBLY. REPLACED BAD LIGHT STRIP. OPS CK GOOD.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008051500111 20080515 00111 NM 2008 5 15 2008UALA02465 1 20080426 A 3350 7945243 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE ROW 3A INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT ROW 3A AFT INOP. REPLACED LIGHT CABLE. OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008051500121 20080515 00121 NM 2008 5 15 F3LA200800254 1 20080511 A 5321 GILFAB42234960C FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED AFT PIT FLOOR PANEL 151ZE DAMAGED. MAINTENANCE FABRICATED NEW FLOOR PANEL IN ACCORDA NCE WITH THE REQUIREMENTS OF SRM 53-02-00 PAGE BLOCK 201 8.G AND 8.H. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AN D FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008051500131 20080515 00131 WP 2008 5 15 AALA200800975 1 20080415 A 3350 8029001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7530 49922 LGA - EMERGENCY LIGHT AT OVERHEAD FIRST CLASS LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHE AD FIRST CLASS LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008051500136 20080515 00136 NM 2008 5 15 AALA200800981 1 20080415 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 197AN 32391 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 29D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 29D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051500137 20080515 00137 NM 2008 5 15 AALA200800942 1 20080413 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 DFW - EMERGENCY LIGHT AT SEAT 45C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 45C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500139 20080515 00139 NM 2008 5 15 AALA200800944 1 20080413 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 DFW - EMERGENCY LIGHT AT SEAT 34G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 34G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500140 20080515 00140 NM 2008 5 15 AALA200800945 1 20080413 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 DFW - EMERGENCY LIGHT AT SEAT 33G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 33G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500141 20080515 00141 NM 2008 5 15 AALA200800954 1 20080414 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 MIA - EMERGENCY LIGHT AT SEAT 12H INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 12H. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008051500153 20080515 00153 NM 2008 5 15 DLM90080701 1 20080508 A 5311 FRAME DOUG MD90 MD9030 3023690 NM AFT CARGO CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 AFT CARGO BAY FRAME CORRODED AFT SIDE STA 1364 BETWEEN LONG 27L AND 28R. REPAIRED FRAME, IAW MD90 53-10-02. 2 L 7 2 4F RT A6WE 2008051500156 20080515 00156 NM 2008 5 15 08FDEA01821 1 20080512 A 5414 311N504632 SKIN BOEING 757 75727B 1384921 NM NR 2 PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 PYLON NUMBER TWO INNER SKIN OF ACCESS PANEL 443BR FOUND WITH SURFACE CORROSION, FROM PPS 126 TO PPS 151. EVALUATE AND RECTIFY. PYLON NUMBER TWO INNER SKIN OF ACCESS PANEL 443BR, REPAIRED BY AERO MECHANICAL INDUSTRIES INC. (AMII) IN ACC ORDANCE WITH EA NR F-5450-118721. PYLON STRUT SKIN SIDE PANEL ASSEMBLY INSTALLED IN ACCORDANCE WITH BOEING DRAWING NUMB ER 311N5046 SHEET 2, BOEING DRAWING NUMBER 311N5002 AND BOEING B757-200 SRM 51-10-02 REVISION 93. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 2 4F RT A2NM 2008051500159 20080515 00159 NM 2008 5 15 DL75E080686 1 20080506 A 2160 CONTROLLER BOEING 757 7572Q8 1384972 NM CABIN TEMP MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 709TW 28168 COULD NOT GET CABIN TEMP BELOW 87 USING THE RIGHT PACK. STANDBY WAS NO USE. PERFORMED BITE RT PACK CONTROLLER FAULTS R T TEMP CONTROL VALVE NIS JFK FWD TO MCO PER MEL 21-51-04B. 2 L 7 2 4F RT A2NM 2008051500163 20080515 00163 NM 2008 5 15 08FDEA01812 1 20080510 A 5347 BAC1520792 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 377-440 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 906FD 27148 FOUND STA 377-440 LBL 45 SEAT TRACK HAS CORROSION. REMOVED SEAT TRACK, FAB`D FROM MAT BAC1520-792, IAW SRM 51-10-02. T REATED AND PRIMED AND INSTALLED NEW SEAT TRACK STA 377-440, LBL 45 IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008051500165 20080515 00165 NM 2008 5 15 08FDEA01814 1 20080510 A 5311 7075T6 FRAME BOEING 757 75727B 1384921 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 DENT FOUND ON LOWER FUSELAGE FRAME AT STA 480 BETWEEN STRINGER S-26L AND S-27L. EVALUATE AND REPAIR AS REQUIRED. REPAI R CARRIED OUT AS PER EA 757-5332-00-F0087 IN THE PTF MOD CARD NR 118250068DSSR02. REPAIR CLASSIFIED AS MAJOR AS PER FED EX GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 2008051500166 20080515 00166 NM 2008 5 15 08FDEA01815 1 20080510 A 5347 BAC1520792 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 780-879 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 906FD 27148 FOUND SEAT TRACK HAS CORROSION STA 780-879 LBL 45. REMOVED SEAT TRACK, FAB`D NEW FROM MAT BAC1520-792, AND INSTALLED SE AT TRACK STA 780-879 LBL 45 IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008051500168 20080515 00168 EU 2008 5 15 08FDEA01822 1 20080512 A 5411 RIB AIRBUS 310 A310324 3930206 EU NR 2 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 NR 2 PYLON AFT LOWER FAIRING PANEL NR 485 AL, RIB IS CRACKED AT THE LOWER ATTACH ANGLE. REMOVED CRACKED ANGLE AND REPLA CED WITH A NEW ANGLE PER SRM 51-40-21 PARA 6 & 7. LOCATED & DRILLED HOLES PER SRM 51-40-44. APPLIED PRIMER PER AMM 51-23-10-0. 2 L 7 2 4F RT A35EU 2008051500172 20080515 00172 NM 2008 5 15 F3LA200800257 1 20080503 A 5311 D53571131258 FRAME SPLICE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE BENT A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED FRAME COUPLING FOR FRAME 72 AND BETWEEN STRINGER 27 LEFT TO 28 LEFT HAS BEEN BENT WHI LE REMOVING RIVETS. MAINTENANCE REMOVED AND FABRICATED AND REPLACED COUPLING IN ACCORDANCE WITH THE REQUIREMENTS OF AIR BUS DRAWING D53571131 AND SRM 51-75-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008051500175 20080515 00175 NE 2008 5 15 DL76P080715 2 20080509 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 143DA 60474 25991 724146 BEARING MATERIAL FOUND ON MCD. REPLACING ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008051500177 20080515 00177 NM 2008 5 15 DLM90080718 1 20080510 A 3070 1T54051 HEATER DOUG MD90 MD9030 3023690 NM VENT SHORTED A DALA O OTHER M OVER TEMP CL CLIMB 1 SO 27 908DA NA 53388 WASTE OVBD VENT TEE HEATER SHORTED OUT AND BURNT A 3 INCH HOLE IN THE TEE THEN THE A/C COULD NOT PRESSURIZE WITH 1 PACK. 2 L 7 2 4F RT A6WE 2008051500179 20080515 00179 NM 2008 5 15 DLM90080702 1 20080508 A 5330 SKIN DOUG MD90 MD9030 3023690 NM BS 237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 PRIOR TO FIRST FLT OF THE DAY, FOUND FUSELAGE SKIN DENTED AT FS 237 BETWEEN LONGERON 18L AND 19L AND REPAIR ID TAG MISSI NG. REPAIRED DAMAGED AREA, IAW MD80 SRM 53-04D, FIG 12 B AND MD90 SRM VOL 1, 51-00-01. 2 L 7 2 4F RT A6WE 2008051500190 20080515 00190 NM 2008 5 15 DL738080720 1 20080512 A 3210 277A61111 HUB CAP BOEING 737 737832 13844CF NM NR 1 WHEEL MISSING A DALA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 SO 27 3738B 30382 ON WALKAROUND, FOUND MANY DEEP SCRATCHES AND A DENT IN FUSELAGE SKIN LT SIDE BEHIND LT WING. ALSO, NR 1 WHEEL HUB CAP A SSY IS MISSING. 2 L 7 2 4F RT A16WE 2008050700082 20080507 00082 EU 2008 5 7 USAA920080955 1 20080424 A 5347 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 272AY 333 BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 4895 / FR 59 - BS 5160 / FR 64, +Y450. REPAIRED CABIN SEAT TRACK, BS 4895 / FR 59 - BS 5160 / FR 64, +Y450 IAW A330 SRM 53-00-15. 2 L 7 2 4F RT A46NM 2008050700093 20080507 00093 NM 2008 5 7 USAA920080966 1 20080429 A 5320 69434772 CHANNEL BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON CHANNEL, BS 767 - BS 794, S25R - S26R, RBL 20. REPLACED CHANNEL, BS 767 - BS 794, S25R - S26R, RBL 20 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008050700102 20080507 00102 NM 2008 5 7 AALA200800857 1 20080407 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 26D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050700105 20080507 00105 EU 2008 5 7 USAA920080971 1 20080422 A 5347 SEAT TRACK AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 272AY 333 BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN SEAT TRACK, BS 4417 / FR 54 - BS 4682 / FR 57.2, -Y450. REPAIRED CAB IN SEAT TRACK, BS 4417 / FR 54 - BS 4682 / FR 57.2, -Y450 IAW A330 SRM 53-31-15. 2 L 7 2 4F RT A46NM 2008050700107 20080507 00107 NM 2008 5 7 USAA920080973 1 20080429 A 5314 KEELBEAM BOEING 767 767201 1385125 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 250AY 23902 BFM - MAJOR REPAIR - C3 CHECK - CORROSION ON KEEL BEAM LOWER CHORD, BS 1005, LBL 8, WL 106. REPAIRED KEEL BEAM LOWER CH ORD, BS 1005, LBL 8, WL 106 IAW B767 SRM 53-50-12. 2 L 7 2 4F RT A1NM 2008050700109 20080507 00109 EU 2008 5 7 USAA920080960 1 20080429 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 624AW 55 FLT 43 - PHX - EEL - EMERGENCY LIGHTS WILL NOT PASS TEST AT FLIGHT ATTENDANT PANEL. MAINTENANCE REMOVED AND REPLACED TH E BATTERY PACK AT 10WL. SYSTEM TEST OK. 2 L 7 2 4F RT A28NM 2008050700124 20080507 00124 NM 2008 5 7 CALA0800401 1 20080430 A 5320 65C33511 SUPPORT BRACKET BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 AIR CONDITIONING SUPPORT BRACKET CRACKED AT LEFTHAND FRAME STATION 440 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING S UPPORT BRACKET AT LEFTHAND FRAME STATION 440 BETWEEN S-8 AND S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008050700126 20080507 00126 NM 2008 5 7 CALA0800403 1 20080430 A 5320 6546558 SUPPORT BRACKET BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 AIR CONDITIONING SUPPORT BRACKET CRACKED AT LEFTHAND FRAME STATION 907 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING S UPPORT BRACKET AT LEFTHAND FRAME STATION 907 BETWEEN S-8 AND S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008050700129 20080507 00129 NM 2008 5 7 DHL2008760517 1 20080416 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272B7 138407L NM BS 690-740 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND REPLACED SEAT TRACK SECTION AT LBL 45, FROM BS 690 TO 740, PER B727 SRM 53-10-2 FIG 7 AND 53-10 -5 FIG 1. 2 L 7 3 4F A3WE 2008050700135 20080507 00135 NM 2008 5 7 08FDEA01762 1 20080505 A 5753 65217911 SUPPORT BOEING 727 7272S2F 1384O81 NM LT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 LT IB MID-FLAP LOWER T/E CHORD WBL 104 ON PUSH-ROD CUT OUT IS CRACKED ON BOTH CORNERS CUT OUT DAMAGE AREA DIM CUT-OUT 47 1/4 INCH LONG IAW SRM 51-40-3 FIG 1. FAB NEW ANGLE "CHORD" 1 SPLICER IAW SRM 57-50-2 FIG 8 AND 51.40.3 FIG 1. TREATE D AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 2008050700139 20080507 00139 NM 2008 5 7 CALA0800408 1 20080430 A 5320 6546552 SUPPORT BRACKET BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 AIR CONDITIONING SUPPORT BRACKET CRACKED AT RIGHTHAND FRAME STATION 827 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT RIGHTHAND FRAME STATION 827 BETWEEN S-8 AND S-9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 2008050700140 20080507 00140 NM 2008 5 7 08FDEA01765 1 20080505 A 5531 65168124 STRINGER BOEING 727 7272S2F 1384O81 NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 STRINGER 8R CRACKED AT RIB NR 8 STRINGER 8R, FIN STA 157.200 CRACK TERMINATES IN FASTENER HOLD AND HFEC INSPECTED AREA A ND VERIFIED IAW NDTM 51.00.00 PART 6. FABRICATED REPAIR ANGLE IAW SRM 55.30.5 FIGURE 7. TREATED AND PRIMED AREA IAW SR M 51.10.2. INSTALLED REPAIR PARTS AT STRINGER 8RT, RIB NR 8 FIN STA 157.2 IAW SRM 55.30.5 FIGURE 1 AND 51.30.2. 2 L 7 3 4F A3WE 2008050700141 20080507 00141 NM 2008 5 7 DHL2008760551 1 20080424 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272B7 138407L NM BS 950-950D CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED CORRODED SEAT TRACK, FABRICATED, AND INSTALLED SEAT TRACK SECTION AT BS 950 TO 950D +10, LBL 45.5, PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 2008050700150 20080507 00150 NM 2008 5 7 DHL2008760552 1 20080422 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272B7 138407L NM BS 870-950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED CORRODED SEAT TRACK, FABRICATED, AND INSTALLED SEAT TRACK SECTION AT BS 870 TO 950, RBL 24.75, PER B727 SRM 53-1 0-2 FIG 7 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 2008050700154 20080507 00154 WP 2008 5 7 ABXA080142 1 20080414 A 5320 5914617502 FLOOR SUPPORT DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 LATERAL FLOOR SUPPORT CRACKED AT FS 677, RIGHT BUTT LINE 30 & 34. REPLACED SUPPORT IAW DC9 SRM. 2 L 7 2 4F A6WE 2008050700173 20080507 00173 SO 2008 5 7 C2XA08ON120 1 20080424 A 5210 LINKAGE EMB 145 EMB145XR 3260214 SO PAX DOOR OUT OF ADJUST A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17196 14500945 FLT 0226 - SMF - FLIGHT CREW REPORTED MAIN CABIN DOOR HARD TO OPEN FROM INSIDE. PERSONNEL ADJUSTED HANDLE LINKAGE AND L UBED DOOR, OPERATIONALLY CHECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008050700177 20080507 00177 SO 2008 5 7 SIMA200812101 1 20080429 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 680AE 9926 500 14500820 DURING A MBV INSPECTION, THE BAGGAGE DOOR CUT OUT LOWER SILL WAS FOUND CORRODED. REMOVED THE EXISTING SILL TO REMOVE TH E DAMAGED AND CLEANED THE AREA. POSITIONED NEW SILL, MARK AND DRILLED FASTENERS HOLES. TREATED PART AND INSTALLED. RE PAIR DONE IAW EMBRAER 145 SRM, EMB-145/1142 REV 39, CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008050700183 20080507 00183 EA 2008 5 7 TRAX200800580 1 20080426 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 905EV 7632 WHITE EMERGENCY EXIT LIGHT BY PAX DOOR HAS SEVERAL BULBS INOP. REMOVED AND REPLACED WHITE EMERGENCY EXIT LIGHT BULBS IA W CRJ 200 AMM 33-51-19. OPS CHECK GOOD. SDR CLOSED. 2 L 7 2 4F RT A21EA 2008050700190 20080507 00190 NM 2008 5 7 USAA920080978 1 20080418 A 5320 143N52601 ANGLE BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL ANGLE, BS 795, BL 0, WL 208. REPLACED INTERCOSTAL ANGLE, BS 795, B L 0, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008050700191 20080507 00191 NM 2008 5 7 USAA920080980 1 20080419 A 5320 141N516095 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - LEVEL 2 CORROSION ON MAIN DECK FLOOR SUPPORT, BS 297, RBL 32.50. REPLACED MAIN DECK FL OOR SUPPORT, BS 297, RBL 32.50 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008050700195 20080507 00195 NM 2008 5 7 NOCA03108 1 20080430 A 2932 211C223296 PRESSURE SWITCH BOEING 757 75728A 1384976 NM HYDRAULIC SYS MALFUNCTIONED A NOCA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 15 750NA 26277 CENTER HYD SYSTEM PRESS EICAS & OVERHEAD PANEL LIGHT ILLUMINATED ON TAKEOFF ROLL, 60 KTS. T/S PER SSM 29-00-04 FOUND C HYD PRESS SWITCH AT FAULT S10002. REMOVED AND REPLACED S10002 PER MM 29-11-19, ALL OPS OK. PERFORMED SYS CHECK PER MM 29-11-00, ALL OK. 2 L 7 2 4F RT A2NM 2008050700204 20080507 00204 EA 2008 5 7 TRAX200800585 1 20080429 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA ASD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 730EV 10141 ASD OUTER HANDLE CRACKED. 2 L 7 2 4F RT A21EA 2008050700209 20080507 00209 NM 2008 5 7 YENA2008040 1 20080430 A 2752 C1558111 ACTUATOR EMB ERJ190 ERJ190100IGW 3260408 NM T/E FLAP FAILED A YENA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 15 258JB 4670 4670 19000047 FLT 1062, AUS-JFK, FLAPS FAIL UPON FLAP EXTENSION, FLAPS FAILED AT ZERO DEGREES, SLATS WERE OPERATIONAL. REMOVED AND RE PLACED NR 2L FLAP ACTUATOR PER MM 27-51-01, OPS CHECK OK, REF EA-E08-189. 2 L 7 2 4F RT A57NM 2008050700215 20080507 00215 NM 2008 5 7 RYNA200800014 1 20080112 A 5230 SKIN BOEING 757 7572G5 1384912 NM CARGO DOOR CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 151GX 24451 LOWER FUSELAGE, AFT CARGO DOOR OUTER SKIN IS CRACKED AT LOWER AFT CORNER. REPAIRED CRACK IAW B757-200 SRM 51-30-01. 2 L 7 2 4F RT A2NM 2008050700226 20080507 00226 NM 2008 5 7 DHL2008760540 1 20080421 A 5320 INTERCOSTAL BOEING 727 7272B7 138407L NM BS 700-720 S28R CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND INSTALLED INTERCOSTAL AT STR 28R FROM BS 700 TO 720 PER B727 SRM 53-10-2 FIG 3, 51-20-1, AND 51 -30-2. 2 L 7 3 4F A3WE 2008050700227 20080507 00227 EA 2008 5 7 SIMA200812602 1 20080504 A 5610 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FAILED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 516AE 10123 ON FLIGHT 3542 - CREW REPORTED THAT IN FLIGHT THAT THE FO’S FORWARD WINDOW SPIDER WEBBED. CREW ELECTED TO DIVERT TO XNA . 2 L 7 2 4F RT A21EA 2008050700251 20080507 00251 EA 2008 5 7 A6WA200840318 1 20080410 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 CORROSION EXIST ON FORWARD CLEAT AND AFT CLEAT OF PAX DOOR BETWEEN FS 313 AND FS 346. (M) CORROSION REMOVED ON BOTH CL EATS IAW SRM. (A) 2 L 7 2 4F RT A21EA 2008050700255 20080507 00255 NM 2008 5 7 NWAA081845532 1 20080419 A 5414 SKIN BOEING 757 757251 1384970 NM NR 2 NACELLE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 532US 24263 DURING "M" CHECK, FOUND CRACK IN NR 2 PYLON SKIN AT NAC STA 132 RT. REPAIRED PER EA 56-212921. 2 L 7 2 4F RT A2NM 2008050700256 20080507 00256 NM 2008 5 7 BB08078 1 20080430 A 3350 LIGHT BOEING 757 7572B7 1384964 NM EXTERIOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 932UW 27198 CLT - THE L2 DOOR EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED EXTERIOR EMERGENCY LIGHT AT DOOR L2. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 2008050700264 20080507 00264 NM 2008 5 7 DHL2008760526 1 20080402 A 5311 FRAME BOEING 727 7272B7 138407L NM B 540 S16R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 FABRICATED AND INSTALLED FRAME REPAIR AT BS 540, AND STR 16R, PER B727 SRM 53-10-2 FIG 3 AND SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 2008050700278 20080507 00278 EA 2008 5 7 A6WA200840319 1 20080408 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 ANGLE BRACKET FOUND CRACK ON LT WING WS 148.019, CRACK LENGTH .500. (M) NEW ANGLE BRACKET INSTALLED IAW 51-41-02 QND S RM 51-41-04 (A) 2 L 7 2 4F RT A21EA 2008050700281 20080507 00281 EU 2008 5 7 CPCP20080018 1 20080327 A 5330 SKIN AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 270AT 270 ON INTERNAL TAIL BUMPER LOWER SURFACE AT FR 39, BTW STGR 21L TO 21R, CORRODED AROUND THE FASTENERS. SKIN REPLACED ON IN TERNAL TAIL BUMPER, LWR SURFACE AT FR 39 BTW STRG 21L TO 21R IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2008050700285 20080507 00285 NM 2008 5 7 MWEA080064 1 20080501 A 5330 S27779223 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 822ME 49759 FUSELAGE SKIN HAS BULGING RIVETS PULLING THROUGH AT STATION 223-229 LONGERON 19 RIGHT & SUSPECT CORROSION. CUT OUT CORR OSION & FABRICATED AND INSTALLED SPLICE. 2 L 7 2 4F RT A6WE 2008050700287 20080507 00287 WP 2008 5 7 08FDEA01754 1 20080505 A 5730 ARB128450 SKIN DOUG MD10 MD1010F 3022112 WP RT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 RIGHT SKIN LEADING EDGE SKIN LOWER SURFACE IS KNIFE EDGED AT THE CUTOUT FOR THE ANTI-ICE "T" DUCT. BLENDED DAMAGED AREA. ORIGINAL MATERIAL 0.063 IAW DWG ARB1284, REV "AC". MATERIAL LOSS 0.045. FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01; VOL I. FABRICATED IAW DWG ARB1284, REV "AC". ALODINED & PRIMED IAW SRM 51-21-01 PGS 21-24 VOL II. INSTALLED IAW S RM 51-35-01 & 51-33-01; VOL II. 2 L 7 3 4F RT A22WE 2008050700291 20080507 00291 NM 2008 5 7 DHL2008760548 1 20080416 A 5347 BAC15201466 SEAT TRACK BOEING 727 7272B7 138407L NM BS 850-870 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED CORRODED SEAT TRACK. FABRICATED, AND INSTALLED SEAT TRACK SECTION AT BS 850 TO 870, RBL 45.5, PER B727 SRM 53-1 0-2 FIG 7 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 2008050700302 20080507 00302 NM 2008 5 7 USAA920080979 1 20080429 A 5311 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 887, S8L - S9L. REPAIRED FRAME, BS 887, S8L - S9L IAW USAIRWAYS EA 1 00441. 2 L 7 2 4F RT A16WE 2008050700307 20080507 00307 NM 2008 5 7 USAA920080986 1 20080430 A 5320 143N8336 INTERCOSTAL BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK, CRACKED INTERCOSTAL, BS 660, S15L. REPLACED INTERCOSTAL, BS 660, S15L IAW TASK CARD M1C 53614. 2 L 7 2 4F RT A2NM 2008050700310 20080507 00310 NM 2008 5 7 USAA920080988 1 20080419 A 5320 141N517031 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK, LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 316, LBL 21.50. REPLACED CABIN FLOOR SUPPO RT, BS 316, LBL 21.50 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008050700324 20080507 00324 NM 2008 5 7 GTIA0800061 1 20080408 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 504NK 2473 FLOORBEAM CORRODED STATION 67-70 AT Y765. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2008050700325 20080507 00325 WP 2008 5 7 AALA200800845 1 20080407 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 505AA 49799 LGA - BATTERY PACK AT B5 1 FOR EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 1 FOR EMERGENCY LIGHT S IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008050700327 20080507 00327 NM 2008 5 7 DHL2008760511 1 20080414 A 5730 SKIN BOEING 727 7272B7 138407L NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 STOP DRILLED CRACKED AT RWS 510.0, FABRICATED REPAIR DOUBLER, AND INSTALLED PER B727 SRM 51-10-1, 57-30-4 FIG 10, 51-10- 2 FIG 1, 51-30-2, AND B727 NDT PRT 6, 57-00-00 FIG 23. 2 L 7 3 4F A3WE 2008050700339 20080507 00339 NM 2008 5 7 DHL2008784002 1 20080502 A 5754 SKIN BOEING 727 727227 1384078 NM K FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 NR 3 L/E K-FLAP HAS SMALL CRACK ON THE BOTTOM I/B CORNER. 2 L 7 3 4F A3WE 2008050700343 20080507 00343 EU 2008 5 7 MALA080063 1 20080502 A 5311 FRAME SAAB SF340 340B 7860101 EU BS 294 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 AT STA 294.0 ON BOTTOM FRAME UPPER FLANGE CORRODED. AT STA 294-0 ON BOTTOM FRAME UPPER FRAME UPPER FLANGE REPAIRED IAW EO NR S53108. 2 L 7 2 4T RT A52EU 2008050600011 20080506 00011 WP 2008 5 6 IXXA08SMN108S 1 20080314 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 717 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FORWARD FITTING CRACKED AT STATION 717.000 RIGHT BOTTOM LINE 22". REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATION NUMBER 2003-05, DRAWING DOUGLAS 3755222, DPS 4.707, DC8 SRM 51-1-8B, AND 51-3-1. 2 L 7 4 4F RT 4A25 2008050600015 20080506 00015 NM 2008 5 6 USAA920080945 1 20080410 A 5320 654681282 WEB BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPLACED - C21 CHECK - CRACKED WEB, BS 944, LBL 44, WL 208. REPLACED WEB, BS 944, LBL 44, WL 208 IAW B737M SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008050600030 20080506 00030 NM 2008 5 6 ASAA0842856 1 20080305 A 5512 6573783501 SKIN BOEING 737 737490 1384715 NM HORIZONTAL STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 796AS 28891 RAMP REPORTS 2 DENTS ON HORIZONTAL STAB (LT) 2' FROM TIP. DENTS ON HORIZONTAL STAB (LT) 2' FROM TIP APPROX REPAIRED IAW SRM 55-10-01 FIG 201. 2 L 7 2 4F RT A16WE 2008050600052 20080506 00052 NM 2008 5 6 2008UALA02509 1 20080428 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE BS 899 S22L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 836UA 1460 DENT AND CRACK IN FUSELAGE SKIN STA 899 3" BELOW S22L. REPAIRED DAMAGED SKIN DAMA GE AT STA 899 PER SRM 53-00-11. PERFO RMED EDDY CURRENT INSPECTION NO DEFECTS NOTED 2 L 7 2 4F 4 F RT A28NM E40NE 2008051500196 20080515 00196 EA 2008 5 15 SWIA200819617 1 20080430 A 3397 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS UNSECURE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 763SK 10228 NR 3 OVERHEAD POD EMERGENCY LIGHT IS INOP. SECURED WIRING CONNECTION ON LIGHT ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008051500198 20080515 00198 NE 2008 5 15 SWIA200819619 2 20080508 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LEFT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 07 221SW 120290 FLT 5571 - CABIN FILLED WITH SMOKE ON DESCENT. REPLACED LEFT ENGINE IAW EMB 120 MM 71-00-00.P/N PW118A S/N OFF 1156 76 2 L 7 2 4T 4 T RT A31SO E20NE 2008051500202 20080515 00202 EA 2008 5 15 SWIA200819623 1 20080227 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 909SW 7558 LEFT ENGINE AFT MOUNT IS WORN, FOUND AT C-CHECK. REPLACED ENGINE THRUST MOUNT FITTING AND BOLTS IAW CRJ200 AMM 71-22-01 -400-801. 2 L 7 2 4F RT A21EA 2008051500203 20080515 00203 NM 2008 5 15 08FDEA01817 1 20080510 A 5347 BAC1520792 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 780-879 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 906FD 27148 FOUND SEAT TRACK HAS CORROSION STA 780-879, LBL 24. REMOVED SEAT TRACK, FAB`D NEW FROM MAT BAC1520-792 IAW SRM 53-00-52 . INSTALLED SEAT TRACK STA 780-879, LBL 24, IAW SRM 51-40-02. MINOR REPAIR. 2 L 7 2 4F RT A2NM 2008051600001 20080516 00001 NM 2008 5 16 SWAA082625 1 20080513 A 5315 6545834 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 344, LBL 29 TO RBL 2. REMOVED AND REPLACED CHORD PER S RM. 2 L 7 2 4F RT A16WE 2008051600003 20080516 00003 EA 2008 5 16 MASA200800359 1 20080501 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP JAMMED A MASA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 17337 14818 7337 ASH FLT 2986 SLC-LAS. FLAPS FAIL CAUTION AT ZERO DEGREES IN CLIMBOUT. FLAP HANDLE AT ZERO AND NOT MOVED. REPLACED THE RT BPSU. 2 L 7 2 4F RT A21EA 2008051600005 20080516 00005 EA 2008 5 16 MASA200800375 1 20080506 A 5210 SEAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH FLT 2925 PHX-ICT. LOUD NOISE FROM PAX DOOR DURING DESCENT. MX FOUND NO DAMAGE TO THE SEAL OR RETAINER BUT FOUND IT DIRTY. MX CLEANED THE SEAL AND OP AND PRESSURIZATION CHECKS WERE GOOD. 2 L 7 2 4F RT A21EA 2008051600007 20080516 00007 NM 2008 5 16 MWEA080070 1 20080508 A 5330 591140885 SKIN BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 927ME 55193 LIGHTNING STRIKE DAMAGE NOTED AT STATION 293 LONGERON RIGHT 7. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2008051600009 20080516 00009 EA 2008 5 16 MASA200800365 1 20080504 A 5270 SENSOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DIRTY A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 75998 7336 ASH FLT 7287 IAD-PVD. PAX DOOR LATCH CAUTION MESSAGE. MX CLEANED THE SENSORS, OPS GOOD. 2 L 7 2 4F RT A21EA 2008051600002 20080516 00002 NM 2008 5 16 MWEA080068 1 20080511 A 5523 SKIN BOEING 717 717200 1383700 NM ELEVATOR TAB DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 927ME 55193 RIGHT ELEVATOR CONTROL TAB UPPER SURFACE HAS LIGHTNING STRIKE DAMAGE AT TRAILING EDGE. 2 L 7 2 4F TR A6WE 2008051600006 20080516 00006 NM 2008 5 16 SWAA082465 1 20080506 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 450, BL 0. REPAIRED SKIN P ER EA. 2 L 7 2 4F RT A16WE 2008051600015 20080516 00015 NM 2008 5 16 SWAA082498 1 20080506 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 11L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008051600017 20080516 00017 NM 2008 5 16 SWAA082493 1 20080506 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 1016, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008051600019 20080516 00019 NM 2008 5 16 SWAA082491 1 20080506 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 2008051600024 20080516 00024 NM 2008 5 16 SWAA082475 1 20080506 A 5753 6546434 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD UPPER SURFACE. REMOVED AND R EPLACED AFT FLAP PER MM. 2 L 7 2 4F RT A16WE 2008051600026 20080516 00026 2008 5 16 SWAA082473 4 20080506 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008051600027 20080516 00027 NM 2008 5 16 SWAA082476 1 20080506 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 407WN 29817 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008051500009 20080515 00009 NM 2008 5 15 NWAA082086309 1 20080511 A 2810 ACCESS PANEL BOEING 747 747451 1384940 NM NR 2 RESER TANK LEAKING A NWAA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 01 669US 24224 2 HOURS INTO FLIGHT, THE CREW REPORTED A FUEL QUANTITY PROBLEM. ABOUT 6,000 LBS TO 7,000 LBS OF FUEL WAS LOST BY THE FI RST POSITION REPORT. FUEL FLOW ON ENGINES WAS NORMAL AND NO REPORTS OF ANY TRANSFERRING. THE FUEL LOSS STABILIZED AND NO ADDITIONAL FUEL WAS LOST EN ROUTE. ON ARRIVAL AT THE GATE THEY FOUND NR 1 ENGINE PYLON MISSING PANEL (452FL) AND FUE L LEAKING FROM A HOLE IN THE NR 2 RESERVE TANK LOWER ACCESS PANEL (553DB). MAINTENANCE REMOVED AND REPLACED PYLON PANEL (452FL) AND FUEL ACCESS PANEL (553DB). OPERATIONAL CHECKED GOOD, NO LEAKS, AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 2008051500017 20080515 00017 NE 2008 5 15 NWAA082079880 2 20080510 A 7320 MANIFOLD DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 2 ENG FUEL LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 675MC 47651 DURING TAKEOFF ENGINE NR 2 EPR ROLLED BACK FROM 2.17 TO 2.10. FLIGHT CREW ADVANCED ENG NR 2 THROTTLE TO STOPS BUT EPR R EMAINED AT 2.10. AFTER TAKEOFF ENGINE NR 2 APPEARED TO FUNCTION NORMAL REMAINDER OF FLIGHT. AT DESTINATION MAINTENANCE NOTICED ENG NR 2 EXHAUST PIPE FULL OF FUEL, OPENED COWLS AND FOUND THEM FULL OF FUEL AND FUEL LEAKING THROUGH THE ENGIN E CASE. SECONDARY FUEL MANIFOLD LEAK WAS DISCOVERED. ENGINE REPLACED. 2 L 7 2 4F 4 F RT A6WE E2EA 2008051500022 20080515 00022 WP 2008 5 15 IXXA08SMN111S 1 20080327 A 5753 SKIN DOUG DC8 DC873F 302199F WP NR 4 TE FLAP DELAMINATED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 VANE FLAP DELAMINATED SKIN BETWEEN STATION XF 225.000 TO ST A XF 335.000. REMOVED AND REPLACED RIGHT WING NUMBER 4 VANE FLAP. PERFORMED OPS CHECK GOOD TO FLAP SYSTEM IAW DC8 MM 2 7-51-14 PAGES 201-202, AND DC8 MM 27-50-0 PAGES 506-507. 2 L 7 4 4F RT 4A25 2008051500037 20080515 00037 NM 2008 5 15 AALA200800827 1 20080406 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 760AN 31477 DFW - EMERGENCY EXIT SIGN AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT EXIT SIGN AT L EFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500047 20080515 00047 EU 2008 5 15 08FDEA01736 1 20080502 A 5347 A53274788212 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 673FE 780 MAIN CARGO SEAT TRACK NR 1 HAS CORROSION BETWEEN FR 66 AND FR 68, 4 SQ IN LONG REMOVED LEVEL 1 CORROSION AND REMOVED AND REPLACED SEAT TRACK SECTION IAW A300-600 SRM 53-10-16, FIG 201, PAGE 207/208. 2 L 7 2 4F RT A35EU 2008051500069 20080515 00069 EU 2008 5 15 AALA200800878 1 20080408 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 41063 506 JFK - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMB ER FOUR DOOR EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008051500087 20080515 00087 NM 2008 5 15 NWAA082025642 1 20080423 A 5330 SKIN BOEING 757 757251 1384970 NM BS 630 S16L DENTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 542US 26489 DURING "M" CHECK, FOUND DENT IN FUSELAGE SKIN AND DAMAGE TO S16L AT BS 630. REPAIRED PER EA 56-210587. 2 L 7 2 4F RT A2NM 2008051500097 20080515 00097 EA 2008 5 15 SWIA200819572 1 20080425 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA RIGHT SMOKE A SWIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 433SW 13026 7550 FLT 3743 - ON TAXI OUT, CABIN FILLED WITH SMOKE. REPLACED RIGHT PACK AIR CYCLE MACHINE WITH SERVICEABLE UNIT AS REQUIRE D. OPS CHECK GOOD IAW CRJ AMM 21-51-10. 2 L 7 2 4F RT A21EA 2008051500098 20080515 00098 SO 2008 5 15 SWIA200819573 1 20080422 A 4920 APU EMB 120 EMB120ER 3260203 SO ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 217SW 120286 FUEL SMELL IN THE CABIN WHILE APU IS RUNNING. REPLACED APU IAW EMB 120 MM 49-00-01. OPS CHECK GOOD, P/N 3800376-2, S/N OFF P-322. 2 L 7 2 4T RT A31SO 2008051500128 20080515 00128 NM 2008 5 15 AALA200800967 1 20080415 A 3350 SIGN BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 689AA 25731 DFW - AFT OVERWING EMERGENCY LIGHT ARROW EXIT SIGN PLACARD DAMAGED. REPLACED PLACARD FOR AFT OVERWING EMERGENCY LIGHT A RROW EXIT SIGN PLACARD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051500132 20080515 00132 WP 2008 5 15 AALA200800977 1 20080415 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7530 49922 LGA - EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 23 TO 26 INOPERATIVE. SECURED LOOSE WIRE FOR EMERGENCY LIGHT AT OVERHEAD SE AT ROWS 23 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008051500138 20080515 00138 NM 2008 5 15 AALA200800943 1 20080413 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 DFW - EMERGENCY LIGHT AT SEAT 39G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 39G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500157 20080515 00157 WP 2008 5 15 08FDEA01830 1 20080512 A 5744 ARC05026 HINGE DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 RIGHT WING OUTBD FLAP, INBD HINGE LOCATION NR 3 OUTBD LUG FACE OUTER SURFACE IS CORRODED. LUG THICKNESS VERIFIED TO BE .421 IAW BAC CMM 57-44-01. CORROSION FOUND AND REMOVED FROM THE LUG FACE TO .405. LUG FOUND TO BE OUT OF LIMITS IAW BA C CMM 57-44-01. ETCHED NR 3 LUG FACE IAW SOPM 20-11-02. CAD PLATING REQUIRED AND ACCOMPLISHED ON N/R N00629 FOR THE TO TAL SURFACE AREA. 2 L 7 3 4F RT A22WE 2008051500174 20080515 00174 NM 2008 5 15 08FDEA01820 1 20080512 A 5415 331N500432 SUPPORT BRACKET BOEING 757 75727B 1384921 NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 PYLON NUMBER TWO UPPER AFT WING TO STRUT FAIRING SUPPORT BRACKET CRACKED, ADJACENT TO PPS 174.3. EVALUATE AND RECTIFY. REPLACED PYLON NUMBER TWO UPPER AFT WING TO STRUT FAIRING SUPPORT BRACKET IN ACCORDANCE WITH EA NR F-5450-118812 AND B757-200 SRM 51-00-02 REVISION 93. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100. 2 L 7 2 4F RT A2NM 2008051500184 20080515 00184 EU 2008 5 15 08FDEA01834 1 20080513 A 5730 A5735011720400 PANEL AIRBUS 310 A310324 3930206 EU RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 RIGHT WING FUEL PANEL ASSY NR 650 FB CLAMP RING HAS AREAS OF FRETTING. BLENDED AREA SMOOTH IAW 57-73-10. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-16. REMOVED OLE CLAMP RING AND REPLACED WITH A NEW RING. 2 L 7 2 4F RT A35EU 2008051500185 20080515 00185 EU 2008 5 15 08FDEA01835 1 20080513 A 5730 A5735011720200 PANEL AIRBUS 310 A310324 3930206 EU RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 RIGHT WING FUEL PANEL ASSY NR 650 CB CLAMP RING HAS AREAS OF FRETTING. BLENDED AREA SMOOTH IAW SRM 51-73-10. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-16. REMOVED AND REPLACED THE CLAMP RING. 2 L 7 2 4F RT A35EU 2008051500199 20080515 00199 EA 2008 5 15 SWIA200819620 1 20080323 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR INNER CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 705SK 10145 FOUND AT C-CHECK, INNER DOOR HANDLE CRACKED. REPLACED PAX DOOR INNER HANDLE ASSEMBLY PER CRJ700/900 AMM 52-11-02-400-80 9-A02. 2 L 7 2 4F RT A21EA 2008051500200 20080515 00200 EA 2008 5 15 SWIA200819621 1 20080323 A 5320 STRAP CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 705SK 10145 AFT BODY CENTER STRAP AT FS 195DL AND FS 196DR IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER SRM 51-42-13-001 -001-A01. 2 L 7 2 4F RT A21EA 2008051600006 20080516 00006 NM 2008 5 16 MWEA080069 1 20080512 A 5330 591140885 SKIN BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 927ME 55193 LIGHTNING STRIKE DAMAGE NOTED AT STATION 370 LONGERON RIGHT 7. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 2008051600012 20080516 00012 NM 2008 5 16 SWAA082490 1 20080506 A 5340 6936350 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 807, STR 27R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008051600021 20080516 00021 NM 2008 5 16 SWAA082497 1 20080506 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008051600031 20080516 00031 NM 2008 5 16 SWAA082480 1 20080506 A 3350 3071BPEGPL LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008051600041 20080516 00041 NM 2008 5 16 SWAA082487 1 20080506 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 752SW 29804 DURING SCHEDULED HC2 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008051600042 20080516 00042 NM 2008 5 16 SWAA082488 1 20080506 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 752SW 29804 DURING SCHEDULED HC2 CHECK, RIGHT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008051600048 20080516 00048 NM 2008 5 16 SWAA082515 1 20080507 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 335, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008051600057 20080516 00057 NM 2008 5 16 SWAA082504 1 20080507 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM L2 DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 421LV 32452 DURING SCHEDULED 6Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK MISSING. INSTALLED HOOK PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082525 1 20080508 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082540 1 20080511 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082535 1 20080511 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008050600077 20080506 00077 NM 2008 5 6 AALA200800803 1 20080402 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET AREA IS DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LE FT NUMBER ONE DOOR CLOSET AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050600078 20080506 00078 NM 2008 5 6 AALA200800801 1 20080402 A 3350 SOCKET BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 919AN 29520 DFW - EMERGENCY LIGHT AT SEAT 19D INOPERATIVE. RECONNECTED PINS ON SOCKET FOR EMERGENCY LIGHT AT SEAT 19D. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008050600099 20080506 00099 WP 2008 5 6 IXXA08SMN116S 1 20080327 A 5522 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR UPPER SKIN DENTED AT STATION XE 137.531 TO STATION XE 142.062. R EMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PAR TS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE FOUND MOMENT WITHIN TOLE RANCE, MOMENT 1448-2. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XE 132.000 TO XE 246.000 IAW SRM 51-1-11, SRM 55-4-1 FIGURE 1 SHEET 1 AND 2 ITEM "E" AND "F", SRM 55-1-0 PAGE 1, 51-1-21, SRM 51-1-9 TR NUMBER 51-142, 51-1-9A TR NUM BER 51-141, AND SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008050600100 20080506 00100 WP 2008 5 6 AALA200800796 1 20080402 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7526A 49918 LGA - EMERGENCY LIGHT AT OVERHEAD AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK B5107 FOR EMERGENCY LIGHT AT OVERHEAD A FT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008050600110 20080506 00110 NM 2008 5 6 MASA200800357 1 20080430 A 3260 SENSOR DHAV DHC8 DHC8202 2809007 NM MLG DIRTY A MASA O OTHER O OTHER DE DESCENT 1 SW 07 434YV 434 ASH FLT 7100 DEN-MTJ - CREW REPORTED A WOW CAUTION LIGHT ILLUMINATED AFTER GEAR EXTENSION AND EXTINGUISHED UPON TOUCHDOW N. CLEANED AND INSPECTED RT WOW OB SENSOR, CHECK GOOD. 2 H 7 2 4T RT A13NM 2008050600119 20080506 00119 NM 2008 5 6 08FDEA01705 1 20080430 A 5230 6557768U6 STOP FITTING BOEING 727 727232 1384082 NM ZONE 800 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 AFT LOWER NR 3 CARGO DOOR FORWARD FRAME LOWER STOP FITTING GOUGED. DOOR REMOVED REF AMM 52-35-071-4, LWR FORWARD FITTIN G REMOVED AND INSTALLED REF SRM 51-30-02. DOOR INSTALLED REF AMM 52-35-071, ADJUSTED STOPS. THIS IS CLASSIFIED AS A MA JOR REPAIR. 2 L 7 3 4F A3WE 2008050700005 20080507 00005 SO 2008 5 7 RAIA008040026 1 20080424 A 2932 O-RING EMB 145 EMB145EP 3260221 SO HYDRAULIC SYS DAMAGED A RAIA A B UNSCHED LANDING EMER. DESCENT K FLUID LOSS CR CRUISE 1 CE 03 826HK 145016 FLT 5596 - STL - CREW REPORTED THAT HYDRAULIC SYSTEM NR 1 QUANTITY WAS DROPPING DURING FLIGHT AND WAS FOLLOWED BY A LOW QTY MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED AN O-RING ON THE PRESSURE TRANSMITTER. SYSTEM OPS CHECKED G OOD AFTERWARDS. 2 L 7 2 4F RT T00011AT 2008050700006 20080507 00006 SO 2008 5 7 RAIA00804028 1 20080426 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 840HK 145341 PRE FLT 7897 - LIT - RIGHT OVERWING EXIT MARKER INOPERATIVE. MAINTENANCE CLEANED, INSPECTED AND RESEATED THE CONNECTOR TO THE AFFECTED LIGHT ASSEMBLY. SYSTEM OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008050700009 20080507 00009 NM 2008 5 7 NOCA02908 1 20080429 A 3350 72914 LIGHT BOEING 757 75728A 1384976 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 THE 2R EMERGENCY LIGHT INOP. RELAMPED 2R EMERGENCY PER MM 33-51-01. 2 L 7 2 4F RT A2NM 2008050700022 20080507 00022 NE 2008 5 7 COMA0870017 2 20080428 A 7230 4114T15P02 FAN BLADE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE LT ENGINE STUCK A COMA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 01 398CA 10112 FLIGHT 5311 - EN ROUTE FROM CVG TO COS, N1 VIBE ON NR 1 ENGINE WENT TO 1.9. EMERGENCY DECLARED AND AIRCRAFT DIVERTED TO MCI AND LANDED SAFELY. REMOVED AND REPLACED ALL FAN BLADES ON NR 1 ENGINE. 2 L 7 2 4F 4 F RT A21EA E00063EN 2008050700058 20080507 00058 NM 2008 5 7 DHL2008760546 1 20080421 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272B7 138407L NM BS 960-1135 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND INSTALLED SEAT TRACK SECTION AT BS 960 TO BS 1135, RBL 24, PER B727 SRM 53-10-5 FIG 1 AND 51-30 -2. 2 L 7 3 4F A3WE 2008050700065 20080507 00065 WP 2008 5 7 UPS08852090 1 20080414 A 5320 FITTING DOUG DC8 DC873F 302199F WP CARGO DOOR FRAME CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 BACK UP FITTING CORRODED AT MCD JAMB NR 1 SPOOL REMOVE AND REPLACE FITTING IAW, SRM 51-3-00. 2 L 7 4 4F RT 4A25 2008050700078 20080507 00078 NM 2008 5 7 USAA920080948 1 20080409 A 5313 655162829 STRINGER BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - LEVEL 2 CORROSION ON STRINGER BS 1006, S27L. REPAIRED STRINGER BS 1006, S27L IAW B737 SRM 53-00-03-2R1. 2 L 7 2 4F RT A16WE 2008050700096 20080507 00096 NM 2008 5 7 USAA920080968 1 20080422 A 5320 65479575 WEB BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON WEB, BS 787, - BS 794, S25R, WL 155. REPLACED WEB, BS 787, - BS 794, S25R , WL 155 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008050700106 20080507 00106 NM 2008 5 7 USAA920080972 1 20080425 A 5320 6546812186 BEAM BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON CABIN BEAM, BS 986.5, RBL 43, WL 208. REPAIRED CABIN BEAM, BS 986.5, RBL 43, WL 208 IAW USAIRWAYS EA 130005. 2 L 7 2 4F RT A16WE 2008050700125 20080507 00125 NM 2008 5 7 CALA0800402 1 20080430 A 5320 6546525 SUPPORT BRACKET BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 AIR CONDITIONING SUPPORT BRACKET CRACKED AT RIGHTHAND FRAME STATION 380 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT RIGHTHAND FRAME STATION 380 BETWEEN S-8 AND S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008050700147 20080507 00147 EU 2008 5 7 CPCP20080025 1 20080404 A 5347 SEAT TRACK AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 348AE 349 LT SEAT TRACK BTW FR 36-39 CORRODED. REPLACED SEAT TRACK BTW FRAME 36-39 IAW SRM 51-25-04. 2 H 7 2 4T RT A53EU 2008050700155 20080507 00155 NM 2008 5 7 AALA200800798 1 20080402 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 903AN 29505 MIA - EMERGENCY EXIT SIGN LIGHT AT SEAT 13A INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHT AT SEAT 13 A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008050700158 20080507 00158 WP 2008 5 7 IXXA080017O 1 20080501 A 7930 42D491C PRESSURE SWITCH DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE ENGINE OIL LEAKING A IXXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 11 799AL 49865 1052 450922 671276 DURING CRUISE FROM HIK, THE CREW SHUTDOWN NR 1 ENGINE AT 2102Z DUE TO FLUCTUATING OIL PRESSURE AND FLICKERING OIL PRESSU RE LIGHT. WIND MILLING OIL PRESSURE FLUCTUATION BETWEEN 18PSI TO 25PSI AT CRUISE ALTITUDE, OIL QUANTITY INDICATED 2.5 G ALLONS AND OIL TEMP 75C PRIOR TO SHUTDOWN. THE CREW LANDED WITHOUT INCIDENT AT SUU. MAINTENANCE INSPECTED AND FOUND LO W OIL DIFFERENTIAL PRESSURE SWITCH TO BE LEAKING. MAINTENANCE REPLACED LOW DIFFERENTIAL PRESSURE SWITCH, OPERATIONAL CH ECK GOOD IAW DACO DC-8 MAINTENANCE MANUAL 79-33-1 AND GENERAL MAINTENANCE MANUAL 3.116. AIRCRAFT WAS RETURNED TO SERVIC E. 2 L 7 4 4F 4 F 4A25 1E8 2008050700160 20080507 00160 NM 2008 5 7 DHL2008760516 1 20080407 A 5347 652363735 SEAT TRACK BOEING 727 7272B7 138407L NM BS 480-690 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED AND REPLACED SEAT TRACK SECTION AT RBL 45, FROM BS 480 TO 690, PER B727 SRM 53-10-2 FIG 7 AND 53-10-5 FIG 1. 2 L 7 3 4F A3WE 2008050700162 20080507 00162 WP 2008 5 7 AALA200800797 1 20080402 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7526A 49918 LGA - EMERGENCY LIGHT AT FORWARD ENTRY INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHTS AT FORWARD ENTRY. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008050700170 20080507 00170 SO 2008 5 7 SWIA200819546 1 20080421 A 5330 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 576SW 120345 SKIN DAMAGE ON KEELBEAM AND NACELLE, COMPLIED WITH REPAIRS OF SKIN ON KEELBEAM AND NACELLE AS REQUIRED. 2 L 7 2 4T RT A31SO 2008050700171 20080507 00171 EA 2008 5 7 SWIA200819547 1 20080422 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 934SW 7722 FLT 5987 - OVERHEAD EMERGENCY LIGHT IN CABIN IS OUT. RELAMPED EMERGENCY LIGHT IN CABIN IAW AMM 33-51-01. 2 L 7 2 4F RT A21EA 2008050700197 20080507 00197 SO 2008 5 7 SIMA200812108 1 20080427 A 2120 UNKNOWN EMB 135 EMB135KL 3260302 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 841AE 145667 ON FLIGHT 317, CREW REPORTED WITH APU BLEED OPEN AIR ON PACK 1 AND 2 ODOR OF OIL IN COCKPIT. AIRCRAFT REMOVED FROM SERV ICE. DEFERRED PER MEL 36-6 AUTH NR 041010DM-C, PERFORMED AIR BLEED THROUGH APU IAW EMB 140 AMM 36-00-00. COULD NOT DUP LICATE SMELL MEL RESTORED, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008050700212 20080507 00212 SO 2008 5 7 RAIA00804031 1 20080429 A 3350 LIGHT EMB 145 EMB145ER 3260211 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 808HK 145157 PRE FLT 7890 - IAD - EMERGENCY LIGHT INOPERATIVE AT THE PASSENGER DOOR. MAINTENANCE DEFERRED THE AFFECTED LIGHT IAW MEL PROCEDURES. 2 L 7 2 4F RT T00011AT 2008050700213 20080507 00213 SO 2008 5 7 SIMA200812109 1 20080428 A 3040 3801D2 CONTROLLER EMB 135 EMB135LR 3260305 SO WINDSHIELD HEAT ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 21 715AE 11489 145262 ON FLIGHT 4684, CREW REPORTED A ACRID SMELL IN COCKPIT ON APPROACH TURNED OFF WINDSHIELD HEAT 1 AND 2 SMELL DISSIPATED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FO'S WINDSHIELD TEMP CONTROLLER IAW EMB 135 AMM 30-42-01. OPERATI ON CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008050700222 20080507 00222 NM 2008 5 7 DHL2008760537 1 20080406 A 5330 SKIN BOEING 727 7272B7 138407L NM BS 1080-1099 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 ACCOMPLISHED SKIN REPAIR TO FUSELAGE AT BS 1080 TO 1099, BETWEEN STR 28R AND 29R. REMOVED EXISTING REPAIR, FABRICATED, AND INSTALLED NEW REPAIR PER B727 SRM 53-30-3 FIG 3, AND 53-30-2 FIG 2. 2 L 7 3 4F A3WE 2008050700224 20080507 00224 NM 2008 5 7 DHL2008760538 1 20080406 A 5322 SHEAR TIE BOEING 727 7272B7 138407L NM BS 970 S29-30L CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND INSTALLED FRAME SHEAR TIE REPAIR AT BS 970 BETWEEN STR 29L & STR 30 PER B727 SRM 53-10-2 FIG 5 AND 53-10-4 FIG 13. 2 L 7 3 4F A3WE 2008050700244 20080507 00244 EA 2008 5 7 A6WA200840325 1 20080414 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 CARGO DOOR AREA, LOWER SILL PLATE IS CORRODED. CORROSION REMOVED IAW SRM 51-21-06. (M) 2 L 7 2 4F RT A21EA 2008050700262 20080507 00262 NM 2008 5 7 DHL2008760525 1 20080402 A 5311 FRAME BOEING 727 7272B7 138407L NM BS 520 S16R DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 FABRICATED AND INSTALLED FRAME REPAIR AT BS 520, AND STR 16R, PER B727 SRM 53-10-2 FIG 3 AND SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20080516 NM 2008 5 16 SWAA082565 1 20080511 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT CRACKED AT BS 413, LBL 3. REP AIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082582 1 20080512 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 220WN 32491 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082583 1 20080512 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 235WN 34630 EEPLS LENS LOOSE AT ROW 3 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082584 1 20080512 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082589 1 20080512 A 2560 6557463 FITTING BOEING 737 7375H4 138449D NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082571 1 20080509 A 5753 654642943 FLAP TRACK BOEING 737 7375H4 138449D NM T/E FLAP LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 8 FLAP TRACK "A" FRAME LOOSE AT CARRIAGE. REMOVED AND REPLACED FLAP TR ACK PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082579 1 20080509 A 2782 65445517 ACTUATOR BOEING 737 7373H4 1384600 NM L/E SLAT MALFUNCTIONED A SWAA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 29 606SW 27926 ON APPROACH FLAPS EXTENDED TO 5 DEGREES HAD AMBER L/E FLAP TRANSIT LIGHT ILLUMINATED, AND HAD IMMEDIATE ROLL. REMOVED A ND REPLACED NR 3 L/E ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082577 1 20080512 A 5523 65C2638416M TAB BOEING 737 7373H4 1384600 NM ELEVATOR FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB AND NR 1 ELEVATOR TAB BUSHINGS PER MM. 2 L 7 2 4F RT A16WE 20080516 2008 5 16 SWIA200819564 4 20080427 A 3417 8220372445 ADC CNDAIR CL600 CL6002B19 1900309 EA NR 1 FAILED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 983SW 10939 10939 7961 FLT 6701 - THE AIRCRAFT INDICATED AIRSPEED WENT INOPERATIVE. REPLACED THE NR 1 AIR DATA COMPUTER PER AMM 34-13-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080516 EA 2008 5 16 SWIA200819565 1 20080427 A 3350 AD20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 919SW 7657 FLT 6643 - FLOOR LEVEL EMERGENCY LIGHTS AFT OF ROW 10 WILL NOT ILLUMINATE. REPLACED NR 4 BATTERY PACK WITH SERVICEABLE UNIT AS REQUIRED PER AMM 33-51-04, PN AD-2013-1A, S/N OFF 87601. 2 L 7 2 4F RT A21EA 20080516 NM 2008 5 16 SWAA082616 1 20080513 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082617 1 20080513 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND LEFT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082622 1 20080513 A 5753 6546430131 SKIN BOEING 737 7373A4 1384585 NM FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED SERVICE CHECK, FOUND LEFT WING INBOARD FORE FLAP DELAMINATED AT OUTBOARD UPPER SURFACE. REMOVED AND RE PLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082623 1 20080513 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 738CB 27870 DURING SCHEDULED MV1 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 2008UALA02486 1 20080425 A 3610 SHUTOFF VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BLEED AIR SYS MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 658UA 27113 RESET AIR SUPPLY MODULE, RAN NR 1 ENGINE, NO DUCT PRESSURE INDICATED, BOX FAULTED PRSOV VALVE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080516 NM 2008 5 16 2008UALA02494 1 20080428 A 5320 STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 TIE STRAP AT BS 348.2 STR 16L IS CRACKED. REPAIR ACCOMPLISHED: REPLACED TIE. 2 L 7 2 4F 4 F RT A16WE E2GL 20080516 NM 2008 5 16 2008UALA02496 1 20080428 A 2421 FILTER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RT GENERATOR BLOCKED A UALA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 29 795UA 26927 RIGHT BACKUP GENERATOR FILTER BLOCKED UPON ARRIVAL. REPLACED RT BACK UP GENERATOR PER MM 24-25-01 OP AND LEAK CHECK GO OD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080516 WP 2008 5 16 NWAA081879995 1 20080426 A 3350 LIGHT DOUG DC9 DC931 3022065 WP EXTERIOR INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8978E 47327 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE L IGHT ASSEMBLY AND FUNCTIONALLY CHECKED IT. 2 L 7 2 4F A6WE 20080516 WP 2008 5 16 UPS08852114 1 20080421 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING CENTER LE LOWER OUTBD EXTERIOR SKIN HAS OVERSIZED SCREW HOLES AT SLOT CUTOUT. REPAIRED LT WI NG LE LOWER OUTBD EXTERIOR SKIN SCREW HOLES IAW SRM 57-03 -03-0 FIG 005 AND EO DC8-5720-7767-A. 2 L 7 4 4F RT 4A25 20080516 WP 2008 5 16 UPS08852115 1 20080424 A 5712 DOUBLER DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 RT WING CENTER LE LOWER RIB REPAIR DOUBLER CRACKED XFS 368. FABRICATED RT WING CENTER LE LOWER RIB D OUBLER AND REPLACED IAW SRM 51-01-21, SRM 57-03-03-0 AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 20080516 WP 2008 5 16 UPS08852116 1 20080420 A 5712 10000001O RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING OUTBD LE UPPER RIB CRACKED JUST ABOVE ACCESS PNL 519B XFS 653. REPAIRED RT WING LE UPPER RIB AT XFS 653 IAW SRM 57-02-00-0 FIG 002 AND SRM 57-03-03-0 FIG 006. 2 L 7 4 4F RT 4A25 20080516 NM 2008 5 16 UPS08M52100 1 20080325 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C CABIN SEAT TRACK AT STA 859 - 909 X=+27.5 FOUND CORROSION. CORROSION ON AFFECTED AREA REMOVED MAT'L T HK: 0.145", MAT'L REMOVED: 0.040" (STA899), MAT'L REMN: 0.105". FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK AT STA 849 T O 929 X=+27.5 TRIMMED OUT. HFEC INSP C/O ON TRIMMED OUT AREA AND FOUND NO CRACK EVIDENT. NEW SEAT TRACK AND 2 SPLICE H AT-SECT REWORKED. TWO SPLICE PLATES FAB. NEW SEAT TRACK AND REPAIR PARTS INSTALLED. 2 L 7 3 4F RT A22WE 20080519 NM 2008 5 19 QXEA200800427 1 20080425 A 7712 54271168010 INDICATOR DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE COCKPIT FAILED A QXEA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 NM 09 356PH 502 PDX- FLIGHT 2011, RETURNED TO THE FIELD FOR A NR 1 ENGINE TORQUE SURGE. ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE PRESSURE TRANSDUCER WITH NO HELP. THEN REPLACED THE PRESSURE INDICATOR. OPERATIONAL CHECKS GOOD. AIRCRA FT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 20080519 NM 2008 5 19 QXEA200800429 1 20080426 A 6123 M390166105L RELAY DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 345PH 476 EUG - FLIGHT 2040 - ON TAKEOFF APPROACHING 70 KNOTS, THE AUTOFEATHER ARM LIGHT DID NOT ILLUMINATE. ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE AUTOFEATHER CONTROL RELAY 6121-K5. OPERATIONAL CHECKS GOOD. AIRCRA FT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080519 NM 2008 5 19 QXEA200800431 1 20080426 A 5210 SEAL BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR DIRTY A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 400QX 4030 SEA - AFTER PARKING AIRCRAFT, THE FLIGHT ATTENDANT REPORTS THAT THE AFT PASSENGER DOOR IS HARD TO OPEN AND CLOSE. MAINT ENANCE CLEANED THE DOOR SEAL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080519 NM 2008 5 19 DHL2008760509 1 20080409 A 5320 STIFFENER BOEING 727 7272B7 138407L NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED NEW CHORD ANGLE REPAIR FROM BAC1506-1532, AND INSTALLED, AT BS 227, BBL 0, PER B727 SRM 51-40-4 FIG 1, 53-10-2 FIG 1, 51-30-2, AND FASI ER NR 2-37153-801 REV A (HEAT TREAT). INSTALLED NEW STIFFENER P/N 69-15768-31 PER S AME. 2 L 7 3 4F A3WE 20080519 NM 2008 5 19 DHL2008760512 1 20080406 A 5753 SKIN BOEING 727 7272B7 138407L NM T/E FLAP DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 EVALUATED DENT/EXCEEDS LIMITS, FABRICATED AND INSTALLED FLUSH REPAIR ON RT I/B MID FLAP UPPER SKIN AT RWBL 110 PER B727 SRM 57-50-2 FIG 3 AND 57-50-4 FIG 2. 2 L 7 3 4F A3WE 20080519 NM 2008 5 19 DHL2008760532 1 20080411 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272B7 138407L NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION AT RBL 24, BS 480 TO 690, PER B727 SRM 53-10-5 FIG 1 AND 53-10 -2 FIG 7. 2 L 7 3 4F A3WE 20080519 WP 2008 5 19 DHL2008807504 1 20080417 A 7110 SKIN DOUG DC8 DC873F 302199F WP COWLING WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 NR 2 ENG NACELLE INLET COWL UPPER SKIN WORN STA YN 147.534 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 70 SRM 71-5-2 FIG. 2 (SHEET 1-2). REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED SKIN (AL2024T3 0.080") AND SPLICE (SHEET CRES 0.050" TYPE 17-7PH) IAW DC8 70 SRM 71-5-2 FIG. 2 SHEET 1-2. HEAT TREATED SPLICE FROM 17-7 PH TO CRES 17-7PH (H1050) IAW SRM 51-1-6. CLEANED, TREATED AND PRIMED AREA AND SKIN INNER FACE IAW SRM 51-1-8B. INSTALLED RE PAIR PARTS IAW DC8 70 SRM 71-5-2 FIG 2 SHEET 1,2, SRM 51-1-11, SRM 51-1-21A. 2 L 7 4 4F RT 4A25 20080519 WP 2008 5 19 DHL2008807505 1 20080422 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 FUSELAGE EXT SKIN CORRODED STA 1345.000 L-30L - L-31L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEE T 1,3,5. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIM ITS IAW SRM 53-2-0 PG 2P. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL7075T6 0.090") FILLER (AL7075T6 0.08 0") AND INTERNAL FINGER DOUBLER (AL7075T6 0.050") IAW SRM 53-2-1 FIG. 7 SHEET 1, 3, 5, SRM 53-4-1 FIG 17A SHEET 1 ITEM " C". CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIG 7 SHE ET 1, 3, 5, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE). THIS IS A CLASS 1 TYPE REPAIR (PERMANENET) INI 2 L 7 4 4F RT 4A25 20080519 WP 2008 5 19 IXXA08SMN098S 1 20080314 A 5320 3779762U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT BATH TUB FITTING CRACKED AT STATION 680.000. REMOVED CR ACKED FITTING. INSTALLED NEW BATH TUB FITTING IAW DC8 SRM 51-1-20D, AND 51-3-1. 2 L 7 4 4F RT 4A25 20080519 NM 2008 5 19 AALA200800831 1 20080407 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 DFW - EMERGENCY LIGHT AT SEAT ROW 37 HAS INOPERATIVE LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 37. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 NM 2008 5 19 AALA200800836 1 20080407 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 DFW - EMERGENCY LIGHT AT SEAT 38G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 38G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 NM 2008 5 19 AALA200800838 1 20080407 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 786AN 30250 DFW EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 WP 2008 5 19 AALA200800849 1 20080407 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 505AA 49799 LGA - BATTERY PACK AT B5 105 FOR EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 105 FOR EMERGENCY L IGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080519 NM 2008 5 19 DLM90080663 1 20080504 A 5320 BRACKET DOUG MD90 MD9030 3023690 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 FOUND CRACK AFT OF STA 1494 BETWEEN LONGERONS L-1 AND L-2. REMOVED AND REPLACED BRACKET, IAW MD90 SRM 51-30-05. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 DLM90080671 1 20080429 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM CABIN GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 FOUND CABIN SEAT TRACK FS 221 LBL 44 OUT OF LIMITS. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01, FIG 6 VOL I. 2 L 7 2 4F RT A6WE 2008051500002 20080515 00002 NM 2008 5 15 HALA0800575 1 20080506 A 5230 SKIN BOEING 717 717200 1383700 NM CARGO DOOR DENTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 476HA 55118 DENT ON AFT CARGO DOOR AFT DOOR FLANGE AFT EDGE, ABOUT 10 INCHES FROM BOTTOM OF DOOR DIMENSION = 5/8 BY 11 INCHES DEEP . 170. HFEC AREA NO CRACKS IND REPAIRED PER HALM105 FILE NR 476141. 2 L 7 2 4F TR A6WE 2008051500043 20080515 00043 NM 2008 5 15 AALA200800829 1 20080407 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 374AA 25201 SFO - EMERGENCY LIGHT AT SEAT 29B MISSING. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 29B. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008051500049 20080515 00049 EA 2008 5 15 MASA200800360 1 20080501 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE OUT OF RIG A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37342 7342 ASH FLT 7172 ORD - AIRCRAFT SERVICE DOOR BINDING AND WILL NOT CLOSE. RIGGED DOOR AND REPLACED SEAL. 2 L 7 2 4F RT A21EA 2008051500054 20080515 00054 NM 2008 5 15 UPS08452145 1 20080226 A 5210 INTERCOSTAL BOEING 747 747212B 1384886 NM L1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE:C CABIN LT NR 1 DOOR BEAM INSTL FOUND CRACKED AS MARKED. NEW BEAM INTERCOSTAL FABRICATED USING MATL 707 5-0.050" PER DWGABA7096. INTERCOSTAL HEAT TREATED TO T62 PER DPS7.00-1 HARDNESS HRB 78.4 IS ACCEPTABLE PER DPS1.05-3. HOLES PICKED UP ON NEW BEAM PER SRM 51-31-01 V.2R .40 AND REPROTECTED PER SRM 51-21-01 V.2R.40. NEW BEAM INTERCOSTAL I NSTALLED PER SRM 51-33-01 AND 51-35-01V.2R.40. 2 L 7 4 4F RT A20WE 2008051500062 20080515 00062 NM 2008 5 15 AALA200800893 1 20080409 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 617AM 24525 MIA - LEFT AFT EMERGENCY LIGHT AT AFT LEFT LAVATORY INOPERATIVE. REPLACED LAMP FOR LEFT AFT EMERGENCY LIGHT AT AFT LEFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051500070 20080515 00070 NM 2008 5 15 AALA200800895 1 20080409 A 5415 311T15875 FITTING BOEING 767 767223 1385123 NM LT PYLON DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AA 22333 AFW - LEFT PYLON INBOARD SIDE CORE COWL HINGE FITTING AT STATION 305 FORWARD LUG HAS ELONGATED HOLE, SIZE OF DISCREPANCY IS .6932 INCH BY .6932 INCH. REPAIRED PER MRB 767 3176. 2 L 7 2 4F RT A1NM 2008051500092 20080515 00092 NM 2008 5 15 AALA200800911 1 20080410 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 756AM 30264 DFW - EMERGENCY LIGHTS AT OVERHEAD RIGHT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK M33424 FOR EMERGENCY LIGHTS AT OVERHEAD RIGHT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500100 20080515 00100 EA 2008 5 15 SWIA200819575 1 20080429 A 3520 OXYGEN MASK CNDAIR CL600 CL6002B19 1900309 EA PAX CABIN UNWANTED DEPLOY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 927SW 7693 FLT 6689 - DURING INITIAL POWER-UP, THE PAX O2 MASKS DEPLOYED. INSPECTED AND RESTOWED MASKS PER AMM 35-21-09. MASKS RE MAINED SECURE. 2 L 7 2 4F RT A21EA 2008051500113 20080515 00113 NM 2008 5 15 2008UALA02467 1 20080426 A 3350 7945243 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE ROW 32ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT ROW 32ABC INOP. REPLACED CABLE. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008051500119 20080515 00119 NM 2008 5 15 DLM90080670 1 20080430 A 5322 591359619 SHEAR TIE DOUG MD90 MD9030 3023690 NM BS 1458 L14-15 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 FOUND CRACKED BRACKET AT STA. 1458 BETWEEN LONGERONS L14 AND L15. REMOVED, FABRICATED AND INSTALLED BRACKET, IAW MD90 S RM 51-10-05, VOL.II. 2 L 7 2 4F RT A6WE 2008051500143 20080515 00143 WP 2008 5 15 AALA200800938 1 20080412 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 494AA 49732 SFO - EMERGENCY LIGHTS IN MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008051500144 20080515 00144 NM 2008 5 15 AALA200800939 1 20080413 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LEFT NUMBE R ONE DOOR CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500148 20080515 00148 NM 2008 5 15 AALA200800933 1 20080412 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 348AN 33087 MIA - EMERGENCY LIGHT AT SEAT 29H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 29H. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A1NM 2008051500162 20080515 00162 NE 2008 5 15 NACA20080008 2 20080513 A 8530 356993 CYLINDER HEAD DOUG DC6 DC6 3021702 WP PWA R2800 R2800CB3 52026 NE NR 16 DAMAGED A NACA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 2907F 2510 2510 533265 31613 NR 1 ENGINE SHUT DOWN DUE TO BACKFIRING. REMOVED AND REPLACED NR 16 CYLINDER DUE TO BLOWN HEAD, REF: NAC DC-6MM SECT V PG 16 AND 16A. OP CHECKED GOOD. 2 L 7 4 4R 4 R A781 5E8 2008051500173 20080515 00173 EA 2008 5 15 SWIA200819611 1 20080511 A 5610 NP1393219 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 915SW 7615 FLT 6655 - LEFT WINDSHIELD IS CRACKED. REPLACED LEFT WINDSHIELD IAW CRJ MM 56-11-01. 2 L 7 2 4F RT A21EA 2008051500180 20080515 00180 NM 2008 5 15 DLM90080703 1 20080506 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 1204 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 SEAT TRACK EXFOLIATED AT FS 1204 LBL 22. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01, FIG 6. 2 L 7 2 4F RT A6WE 2008051500195 20080515 00195 EA 2008 5 15 SWIA200819616 1 20080506 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 751SK 10208 FLT 5834 - CEILING LEVEL EMERGENCY FLOOD LIGHT OVER ROW 14 IS INOP. REPLACED THE LAMP FOR THE EMERGENCY FLOOD LIGHT. O PS CHECKS ARE GOOD. 2 L 7 2 4F RT A21EA 2008051600008 20080516 00008 EA 2008 5 16 MASA200800363 1 20080504 A 2621 346000371 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY LOW PRESSURE A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 7264V 17019 7264 ASH FLT 2752 PHX - SBP. DECLARED AN EMERGENCY AND DIVERTED TO PSP DUE TO A CARGO BOTTLE LOW CAUTION MESSAGE. CAUTION MESSAGE WENT AWAY ON FINAL. REMOVED AND REPLACED RT BOTTLE, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008051600001 20080516 00001 EA 2008 5 16 MASA200800370 1 20080505 A 5210 HINGE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 75987 7405 FOUND DAMAGE TO PAX DOOR HINGE. DAMAGE IS 3 SMALL GOUGES ON THE LUG OF THE PAX DOOR HINGE. REPAIRED DAMAGE. 2 L 7 2 4F RT A21EA 2008051600018 20080516 00018 NM 2008 5 16 SWAA082492 1 20080506 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 947.5, STR 4L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008051600032 20080516 00032 NM 2008 5 16 SWAA082481 1 20080506 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 7 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008051600034 20080516 00034 NM 2008 5 16 SWAA082499 1 20080506 A 5534 6553744 STIFFENER BOEING 737 7373H4 1384600 NM VERTICAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND VERTICAL STABILIZER STIFFENER AFT OF STABILIZER MOUNT CRACKED AT STA 1088. REMOVED AN D REPLACED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082523 1 20080508 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 776WN 30591 DURING SCHEDULED MV1 CHECK, FOUND MID CABIN EMERGENCY BULLNOSE AND LT EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082568 1 20080510 A 7830 4114M41PO1 ISOLATOR BOEING 737 7373H4 1384600 NM THRUST REVERSER BROKEN A SWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 29 314SW 23336 ABORTED TAKEOFF, NR 1 ENGINE STARTED TO SPOOL UP SLOWLY, HUNG UP AT 51% AND WOULD NOT ADVANCE. INSPECTED AND FOUND NR 1 ENGINE OUTBOARD FWD ISOLATOR END BROKEN. REMOVED AND REPLACED FWD T/R ISOLATOR PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082592 1 20080512 A 5310 6969854 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FWD SERVICE DOOR CUTOUT AFT FRAME CRACKED AT LOWER DOOR STOP. REMOVED AND REPLACED F RAME PER BOEING DRAWING. 2 L 7 2 4F RT A16WE 20080516 2008 5 16 SWAA082614 4 20080513 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082615 1 20080513 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080516 2008 5 16 UPS08M52124 4 20080430 A 2565 SLIDE DOUG MD11 MD11F 3023600 NM CREW ENTRY UNWANTED DEPLOY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP 48774 DURING POST FLT CLEAN UP RT (R-1) EMERGENCY EVAC SLIDE WAS DEPLOYED AND EMERGENCY PNEUMATIC DOOR BOTTLE DISCHARGED (M374 716 ASSIGNED. REPLACED RT FWD CREW ENTRY DOOR EVACUATION SLIDE PER MM 25-61-51-4, SERVICED EMERGENCY PNEUMATIC BOTTLE P ER MM 12-25-04-3. M374716 CLEARED. 2 L 7 3 4F RT A22WE 20080519 NM 2008 5 19 DHL2008760504 1 20080416 A 5712 RIB BOEING 727 7272B7 138407L NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED AND REPLACED INBOARD AND OUTBOARD RIBS AT NR 4 SLAT ACTUATOR ROD END ATTACH POINT, P/N 65-17294-9 AND 65-17294U1 1, AT LWS 410.0, PER B727 SRM 51-30-2 AND 51-30-5. 2 L 7 3 4F A3WE 20080519 EU 2008 5 19 CPCP20080021 1 20080327 A 5320 PLATE AEROSP ATR72 ATR72212 8680945 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 270AT 270 CORROSION FOUND UNDER THE PLATE BTW FR 42-43, BL O. PLATE AT FR 42-43 BL O REPAIRED IAW SRI-DO/TS-1616/08-10077 AND EO NR E2-53MR-195. 2 H 7 2 4T RT A53EU 20080519 WP 2008 5 19 AALA200800850 1 20080407 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 505AA 49799 LGA - BATTERY PACK AT B5 23 FOR EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 23 FOR EMERGENCY LIG HTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080519 WP 2008 5 19 AALA200800851 1 20080407 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 505AA 49799 LGA - BATTERY PACK FOR EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN AFT CAB IN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080519 WP 2008 5 19 AALA200800859 1 20080408 A 5350 3913359545 RELEASE CABLE DOUG DC9 DC982 3022082 WP TAILCONE FRAYED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 479AA 49654 TUL - RELEASE HANDLE CABLE ASSEMBLY HAS WORN AND FRAYED CABLE ON LEFT SIDE ABOVE THE MID POINT PULLEY. AREA OF DISCREPA NCY WAS .125 INCH BY .125 INCH. REPLACED TAILCONE RELEASE CABLE ASSEMBLY ON LEFT SIDE. OPERATIONS CHECK NORMAL. 2 L 7 2 4F A6WE 20080519 NE 2008 5 19 F3LA200800227 2 20080501 A 7520 3381192020 SUPPORT BRACKET AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE LT ENGINE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED CRACK IN LPT COOLING TUBE SUPPORT BRACKET ON LEFT ENGINE RIGHT SIDE APPROXIMATELY FOUR O'CLOCK POSITION. MAINTENANCE REMOVED AND INSTALLED NEW LPT COOLING SUPPORT BRACKET ON LEFT ENGINE RIGHT SIDE IN A CCORDANCE WITH THE REQUIREMENTS OF AMM 20-21-11-991-034. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEP TABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080519 NE 2008 5 19 08FDEA01857 2 20080515 A 7261 2591112504 HOSE BOEING 727 727200 138407E NM PWA JT8 JT8D217C 52053 NE ENGINE OIL CHAFED A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 207FE 22929 CRUISING AT 380, OIL QUANITY DECREASED FROM 3 QUARTS TO JUST OVER 1 QUART. PRESSURE RANGED FROM 41-38 PSI. INSTALLED TEMP FLEX LINE IAW EA 7-7930-121858. LEAK CHECK GOOD. SERVICED OIL AS REQUIRED. REQUIRES TUBE MFG 259-1112-504 TO F INALIZE THE REPAIR BEFORE THE NEXT A CHECK. 2 L 7 3 4F 4 F RT A3WE E9NE 20080519 SO 2008 5 19 SIMA200812902 1 20080505 A 2915 156221 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO HYDRAULIC SYSTEM LEAKING A SIMA I CABIN DEPRESSURIZATION K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 619AE 20412 145101 ON FLIGHT 4371, CREW REPORTED LOSS OF HYDRAULIC FLUID THEN HYD SYSTEM 2 FAILED. CREW DECLARED EMERGENCY. AIRCRAFT LANDE D WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RT PRESSURE SWITCH LEAKING. REMOVED AND REPLACED PRESSURE SW ITCH IAW EMB145 32-41-04. ALSO REMOVED AND REPLACED NR 2 ENGINE DRIVEN PUMP IAW EMB-145 29-10-03. OPERATIONAL CHECK GO OD AT THIS TIME. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20080519 GL 2008 5 19 SIMA200812903 2 20080505 A 7200 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 MALFUNCTIONED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 907AE 15623 14500895 CAE311869 ON FLIGHT 3467, CREW REPORTED PARTICULAR ODOR NOTED IN COCKPIT AND CABIN AFTER TAKEOFF, SUSPECT PACK 1. ODOR DISSIPATED RAPIDLY AFTER TAKEOFF. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER ONE ENGINE IAW AMERICAN EAGLE WORK CARD 71-000-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080519 EU 2008 5 19 MALA080079 1 20080427 A 5260 RAIL SAAB SF340 340B 7860101 EU AIRSTAIR DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425XJ 340B425 AIRSTAIR SLIDE RAIL CORRODED; APPROX STA, 236 - 288. REMOVED DAMAGED RAIL AND INSTALLED NEW RAIL P/N: 7253710-871 AND A SSOCIATED HARDWARE IAW SAAB 340 AMM CH 20-10. 2 L 7 2 4T RT A52EU 20080519 EU 2008 5 19 MALA080078 1 20080427 A 5753 SKIN SAAB SF340 340B 7860101 EU T/E FLAP CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425XJ 340B425 HOLE CHAFED IN RT FLAP LEADING EDGE AT WS 225.4 FROM CONTACT WITH AILERON CABLE DAMPER BLOCK. REPAIRED CHAFE DAMAGE BY WET LAYUP REPAIR IAW MESABA EO NR S51031 AND APPLICABLE SECTIONS OF SAAB 340 SRM CH 51-70. 2 L 7 2 4T RT A52EU 20080519 EU 2008 5 19 08FDEA01786 1 20080507 A 2133 88005B0306 OUTFLOW VALVE AIRBUS 300 A300F4605R 3930327 EU CABIN PRESS SYS DAMAGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 671FE 778 CLIMBING THROUGH FL 320 RECEIVED CABIN PRESS ADVISORY. ATTEMPTED TO SLOW CABIN ALTITUDE BUT OBSERVED FWD OUTFLOW VALVE OPEN HALFWAY. ATTEMPTED CYCLING BETWEEN REG 1 AND 2 TO TRY AND GET PRESS SYSTEM TO RESPOND. SLOWED A/C CLIMB AND RECE IVED CABIN ALTITUDE ABV 10K. FOLLOWED CHECKLIST PROCEDURES AND DIVERTED TO KELP. REMOVED ACCESS PANEL IN LWR FWD CARGO PIT TO ACCESS FWD OUTFLOW VALVE. ON INSPECTION FOUND SMALL AMOUNT OF ADJACENT INSULATION BLANKET IN VALVE AND DAMAGE TO VALVES DEBRIS SCREEN. VALVE AND SCREEN ON ORDER. PART NIS ELP. REMOVED AND REPLACED FORWARD OUTFLOW CONTROL VALVE REF 21-31-12-4, OPS CK GOOD. 2 L 7 2 4F RT A35EU 20080519 EA 2008 5 19 SWIA200819606 1 20080215 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 971SW 7947 RBL9 LOWER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS FOR RBL 9 LOWER FLOOR SUPPORT PER CRJ200 REO 601R-53-11-171 REV D DATED 02/13/07. 2 L 7 2 4F RT A21EA 20080519 EA 2008 5 19 SWIA200819607 1 20080215 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 971SW 7947 LBL 9 LOWER FLOOR SUPPORT CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS FOR LBL 9 LOWER FLOOR SUPPORT PER CRJ200 RE O 601R-53-11-171 REV D DATED 02/13/07. 2 L 7 2 4F RT A21EA 2008050700265 20080507 00265 NM 2008 5 7 ZZDA2008097 1 20080416 A 5320 L0602289 PAN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 987AT 55088 AFT CARGO DOOR LOWER PAN CORRODED BEYOND LIMITS FS 954.0 TO 594.0. INSTALLED AFT CARGO LOWER PAN NEW SECTION IAW SRM 52 -20-15 TASK 201. 2 L 7 2 4F TR A6WE 2008050700279 20080507 00279 EA 2008 5 7 A6WA200840322 1 20080411 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA BS 589 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 CARGO DOOR FLOOR LANDING PLATE CRACKED AT FS 589. (M) CARGO DOOR FLOOR LANDING PLATE REPAIRED IAW REO 601R-53-61-433. (A) 2 L 7 2 4F RT A21EA 2008050700293 20080507 00293 EU 2008 5 7 USAA920080991 1 20080502 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 636AW 22594 14331 98 FLT 610 - PHX - EEL - FWD LEFT EMERGENCY POWER SUPPLY UNIT FAILS TEST PER T/C A1C33302. MAINTENANCE REMOVED AND REPLACE D THE FWD EPSU. OPERATIONAL CHECK WAS NORMAL. 2 L 7 2 4F RT A28NM 2008050700306 20080507 00306 EA 2008 5 7 SWIA200819586 1 20080214 A 5313 STRINGER CNDAIR CL600 CL6002B19 1900309 EA BS 640-654 S3R GOUGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 438SW 7574 STRINGER 3R IS GOUGED BETWEEN FS 640 AND FS 654, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ200 SRM 53-00-03 PG 201 -210. 2 L 7 2 4F RT A21EA 2008050700348 20080507 00348 NM 2008 5 7 ASAA0872867 1 20080430 A 5210 141A60791 GUIDE ARM BOEING 737 737790 13844CN NM PAX DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 644AS VAI001269 30795 L1 DOOR WAS HARD TO CLOSE. ADJUSTED UPPER GUIDE PIN. 2 L 7 2 4F RT A16WE 2008050700356 20080507 00356 NM 2008 5 7 SWAA082410 1 20080501 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008050700358 20080507 00358 NM 2008 5 7 SWAA082411 1 20080501 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008050700361 20080507 00361 NM 2008 5 7 SWAA082430 1 20080504 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED DAL CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008050700368 20080507 00368 NM 2008 5 7 SWAA082378 1 20080501 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008050700375 20080507 00375 NM 2008 5 7 SWAA082425 1 20080504 A 5313 6552988 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 7L CRACKED AT BS 1016. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008050700376 20080507 00376 NM 2008 5 7 SWAA082424 1 20080504 A 5312 6546568 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED BRDG CHECK, FOUND RADIAL STIFFENER CRACKED AT AFT PRESSURE BULKHEAD BS 1016, 3 O'CLOCK POSITION. REMOV ED AND REPLACED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2008050700377 20080507 00377 2008 5 7 SWAA082396 4 20080503 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008050700381 20080507 00381 2008 5 7 SWAA082400 4 20080502 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 423WN 29827 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008050700389 20080507 00389 NM 2008 5 7 SWAA082419 1 20080504 A 5754 65C26601 SLAT BOEING 737 7375H4 138449D NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008050700399 20080507 00399 NM 2008 5 7 SWAA082386 1 20080501 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 704SW 27838 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008050700400 20080507 00400 NM 2008 5 7 SWAA082385 1 20080501 A 3350 307BPEGPL LIGHT BOEING 737 7377H4 1384404 NM COCKPIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 704SW 27838 DURING SCHEDULED MV2 CHECK, FOUND FLIGHT DECK EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008050800005 20080508 00005 EA 2008 5 8 A6WA200840296 1 20080402 A 5720 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 CRACK FOUND ON RT WING, AFT OF LANDING EDGE AT WS 343, BTWN ACCESS PANEL 603 LZ AND 630 KZ. (K) RT WING L/E ON THE REA R SIDE AT WEB FABRICATED IAW SRM 51-24-16. RT WING L/E ON THE REAR SIDE AT WS 343 WEB INSTALLED IAW SRM 51-42-13. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 2008050800026 20080508 00026 EU 2008 5 8 706704192008 1 20080419 A 2150 ECS BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101* NE A/C BAY MALFUNCTIONED E QMLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 118NC 7067 AIRCRAFT WAS ALMOST AT DESTINATION WHEN THE CREW SMELLED SEVERAL STRANGE ODORS. CREW THOUGHT THE SMELLS WERE COMING FROM NUMEROUS FIRES ON THE GROUND IN THE AREA. NURSE IN BACK OF AIRCRAFT REPORTED SMOKE COMING FROM THE ENVIRONMENTAL SYSTEM VENTS IN THE AIRCRAFT CABIN. PILOT AND MEDICAL CREW MEMBER IN FRONT NEVER SAW SMOKE. THE ECU WAS BLOWING WARM AIR EVEN THOUGH IT WAS SET FOR AIR CONDITIONING. TURNING OFF THE ECU STOPPED BOTH THE SMOKE AND THE SMELL. THE CLOSEST PLACE TO L AND WAS THE DESTINATION, AND LANDING WAS COMPLETED WITHOUT INCIDENT. MECHANIC FOUND FAILED COMPONENTS IN THE AIR CONDITI ONING SYSTEM. MECHANIC TOOK ECU OUT OF SERVICE, COMPLETED MEL PAPERWORK, AND PLACARDED SYSTEM OUT OF SERVICE AS WELL. 1 G 7 2 3U 3 U H13EU E5NE 2008050800036 20080508 00036 EU 2008 5 8 BAQA20080006 1 20080419 A 2150 S8990132 O-RING ALIDSG BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE A/C BAY DAMAGED E BAQA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 03 118NC 7067 CRUISE FLIGHT, CLOSE TO FLIGHT DESTINATION, CREW SMELLED "STRANGE ODOR" IN CABIN/COCKPIT. PILOT TURNED OFF THE ENVIRONM ENTAL CONTROL UNIT AND SMELL CEASED. INSPECTION OF ECU REVEALED THAT THE "INDUCTOR" PIPE TEMPERATURE CONTROLLER TO COOL ING TURBINE HAD A SMALL SPLIT AT THE TURBINE AND PIECES OF THE SEALING O-RING (PACKING) WAS EXPOSED AND MISSING. 1 G 7 2 3U 3 U H13EU E5NE 2008050800038 20080508 00038 EU 2008 5 8 BAQA200800003 1 20080419 A 2150 S8990132 O-RING ALIDSG BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE A/C BAY DAMAGED E BAQA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 03 118NC 7067 CRUISE FLIGHT, CLOSE TO FLIGHT DESTINATION CREW SMELLED "STRANGE ODOR" IN CABIN/COCKPIT. PILOT TURNED OFF THE ENVIRONME NTAL CONTROL UNIT AND SMELL CEASED. INSPECTION OF ECU REVEALED THAT THE "INDUCTOR" PIPE TEMPERATURE CONTROLLER TO COOLI NG TURBINE HAD A SMALL SPLIT AT THE TURBINE AND PIECES OF THE SEALING O-RING (PACKING) WAS EXPOSED AND MISSING. 1 G 7 2 3U 3 U H13EU E5NE 2008050800039 20080508 00039 EU 2008 5 8 BAQA20080021 1 20080419 A 2150 S8990132 O-RING ALIDSG BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE A/C BAY BLOWN E BAQA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 03 118NC 7067 CRUISE FLIGHT, CLOSE TO FLIGHT DESTINATION, CREW SMELLED "STRANGE ODOR" IN CABIN/COCKPIT. PILOT TURNED OFF THE ENVIRONM ENTAL CONTROL UNIT AND SMELL CEASED. INSPECTION OF ECU REVEALED THAT THE "INDUCTOR" PIPE TEMPERATURE CONTROLLER TO COOL ING TURBINE HAD A SMALL SPLIT AT THE TURBINE AND PIECES OF THE SEALING O-RING (PACKING) WAS EXPOSED AND MISSING. 1 G 7 2 3U 3 U H13EU E5NE 2008050800043 20080508 00043 EU 2008 5 8 BAQA20080015 1 20080419 A 2150 S8990124 O-RING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101* NE A/C BAY DAMAGED E BAQA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 03 118NC 143 7067 DURING DESCENT TO LAND CREW SMELT (STRANGE ODOR) COMING FROM THE AIR CONDITIONING GASPERS. DEACTIVATING ENVIRONMENT CON TROL UNIT CEASED ODOR. AFTER LANDING INSPECTION MAINTENANCE PERSONNEL DISCOVERED A SPLIT IN THE (INDUCTOR) TUBE BETWEEN THE TEMPERATURE CONTROL UNIT AND THE COOLING TURBINE OF THE ECU. SEALING O-RING (PACKING) OF INDUCTOR AT COOLING TURBI NE END HAD DETERIORATED AND STARTED TO COME OUT OF TUBE AT SPLIT. 1 G 7 2 3U 3 U H13EU E5NE 2008050800055 20080508 00055 NM 2008 5 8 HALA0800571 1 20080505 A 2913 887673 PUMP BOEING 767 767332 1382001 NM LT ENGINE LEAKING A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM, ON OVERNIGHT CHECK FOUND LEFT ENG LEAKING HYD FLUID. TROUBLE SHOT FOUND LEFT ENGINE DRIVEN PU MP LEAKING. REMOVED AND REPLACED LEFT ENGINE DRIVEN PUMP IAW AMM 29-11-05. ACCOMPLISHED ENGINE RUN. NO LEAKS NOTED. 2 L 7 2 4F RT A1NM 2008050800071 20080508 00071 WP 2008 5 8 UPS08852121 1 20080424 A 5754 SKIN DOUG DC8 DC873F 302199F WP RWS 404 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 RT WING CENTER LE UPPER SKIN DOUBLER CRACKED AT XFS 404. FABRICATED AND REPLACED RT CENTER LE UPPER SKIN DOUBLER IAW DWG 576989 1. 2 L 7 4 4F RT 4A25 2008050800072 20080508 00072 WP 2008 5 8 UPS08852122 1 20080421 A 5712 RIB DOUG DC8 DC873F 302199F WP LWS 467 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING CENTER LE UPPER RIB CRACKED XFS 467. REPAIRED LT WING CENTER LE UPPER RIB AT XFS 467 IAW 57- 02-00-0 FIG 002 AND SRM 57-03-03-0 FIG 005. 2 L 7 4 4F RT 4A25 2008050800073 20080508 00073 WP 2008 5 8 UPS08852123 1 20080421 A 5712 RIB DOUG DC8 DC873F 302199F WP LWS 440 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING CENTER LE UPPER RIB CRACKED XFS 440. REPAIRED LT WING CENTER LE UPPER RIB AT XS 440 IAW SRM 57-02-00-0 FIG 002 AND SRM 57-03-03-0 FIG 005. 2 L 7 4 4F RT 4A25 2008050800075 20080508 00075 WP 2008 5 8 UPS08852127 1 20080413 A 5340 37535691 FITTING DOUG DC8 DC873F 302199F WP BS 270 L30R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 A-PIT RT STA 270 L30R, END FITTING HAS CORROSION AROUND AND UNDER FASTENERS. REMOVED AND REPLACED FI TTING IAW SRM 53-2-0, 51-1-21D, 51-1-8, 51-3-2, 51-1-20D. 2 L 7 4 4F RT 4A25 2008050800076 20080508 00076 WP 2008 5 8 UPS08852128 1 20080410 A 5720 ANGLE DOUG DC8 DC873F 302199F WP LWS 436 BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 LT WING T/E STA 436, RIB JUST O/B OF AILERON BUS CABLE SPRING ASSY HAS APPROX 4 INCHES BROKE OFF. FA BBED AND INSTALLED REPAIR ANGLE 51-1-21, 51-1-20D, 51-1-8. 2 L 7 4 4F RT 4A25 2008050800077 20080508 00077 NM 2008 5 8 2008UALA02567 1 20080502 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 663UA 27160 FLOOR LIGHT STRIP AFT OF 9AB BROKEN. 2 L 7 2 4F 4 F RT A1NM E24NE 2008050800081 20080508 00081 SO 2008 5 8 GUUA04210802 1 20080421 A 3260 922AA2YA6PZ722A PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT MLG INOPERATIVE A GUUA O OTHER N FALSE WARNING CL CLIMB 1 SO 29 280AS 120231 FLIGHT 9138, AFTER TAKEOFF, LANDING GEAR SELECTED UP RT MAIN GREEN (A) LIGHT ILLUMINATED. CONTINUED TO FLL. DURING APP ROACH, LANDING GEAR DID NOT EXTEND IN NORMAL MODE, USED ELECTRICAL OVERRIDE. REPLACED RT MLG (A) DOWNLOCK PROXIMITY SEN SOR. 2 L 7 2 4T 4 T RT A31SO E20NE 2008050800082 20080508 00082 CE 2008 5 8 GUUA04210803 1 20080421 A 3230 CAP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA AIR REGULATOR MISSING A GUUA O OTHER O OTHER TO TAKEOFF 1 SO 29 87555 UE234 FLIGHT 9197, AFTER TAKEOFF, NOSE LANDING GEAR TAKES EXCESS TIME TO RETRACT. INSTALLED AIR REGULATOR PORT CAP. OPERATIO NAL CHECK NORMAL. 2 L 7 2 4T 3 T RT A24CE E4EA 2008050800090 20080508 00090 NE 2008 5 8 0085782 3 20080424 A 6111 7826761 BEARING EMB 120 EMB120 3260201 SO HAMSTD 14RF 14RF9 NE CRACKED B EY2R K NONE O OTHER IN INSP/MAINT 1 GL 03 CRACKED RACE. 2 L 7 2 4T RT A31SO 6 C P11NE 2008050800092 20080508 00092 NM 2008 5 8 HALA0800560 1 20080421 A 5340 ATTACH FITTING BOEING 767 7673CB 1385187 NM BS 911 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 588HA 33466 PARTITION AT STA 911 BOTH LOWER ATTACH FITTINGS CORRODED. CORRROSION BEYOND SRM LIMITS. NEW BRACKETS MANUFACTURED IAW DRW 413T2047. 2 L 7 2 4F RT A1NM 2008050800093 20080508 00093 WP 2008 5 8 UPS08852129 1 20080415 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 840 LBL 60 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 CABIN STA 840, LBL60, SEAT TRACK FLANGE HAS CORROSION CUT OUT CORROSION FABBED AND INSTALLED SEAT TRACK SPLICE IAW, SRM 53- 2-3, 510108, 5101020D. 2 L 7 4 4F RT 4A25 2008050800100 20080508 00100 CE 2008 5 8 DXTA200803015 1 20080421 A 2120 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN & COCKPIT ODOR E DXTA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 900QS 7500123 FRESH OIL SMELL COMING FROM WEMACS IN CABIN AND COCKPIT. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008050800106 20080508 00106 CE 2008 5 8 DXTA200803022 1 20080424 A 3240 BRAKE SYS CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 07 318QS 5600418 COPILOT'S LT BRAKE PEDAL REQUIRES SIGNIFICANTLY MORE TILT TO ENGAGE BRAKE THAN RT PEDAL, NO VISIBLE FLUID OR LEAKS. BLE D BRAKES IAW MM 32-42-00. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E25EA 2008050800114 20080508 00114 NM 2008 5 8 HALA0800553 1 20080501 A 3150 WARNING LIGHT BOEING 767 76733A 1385209 NM FALSE ACTIVATION A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM, FMS UNABLE TO SEND REQ FOR DATA- MSG "UNABLE TO SEND MSG". PERFORMED FIM 23-22-00 FIG 103, AC ARS CHECKS NORMAL PERFORMED BUFFER DUMP, FMS MSG SEND OPS NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008050700316 20080507 00316 SO 2008 5 7 C2XA08ON121 1 20080503 A 3350 LIGHT EMB 145 EMB145XR 3260214 SO CABIN MISSING A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11193 14500938 FLT MX - ONT - WHILE PERFORMING PRELIMINARY INSPECTION ON AIRCRAFT, QC PERSONNEL FOUND A FLOOR PROXIMITY LIGHTING SEGMEN T MISSING AT 18BC. MX PERSONNEL INSTALLED A NEW PROXIMITY LIGHTING SEGMENT OPERATIONALLY CHECKED SATISFACTORY AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 2008050700317 20080507 00317 NM 2008 5 7 DHL2008760536 1 20080420 A 5330 SKIN BOEING 727 7272B7 138407L NM BS 1043-1088 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 ACCOMPLISHED SKIN REPAIR TO FUSELAGE AT BS 1043 TO 1088, BETWEEN STR 24L AND 27L. REMOVED EXISTING REPAIR, FABRICATED, AND INSTALLED NEW REPAIR PER B727 SRM 53-30-3 FIG 5, 53-30-3 FIG 3, AND 53-30-2 FIG 2. 2 L 7 3 4F A3WE 2008050700318 20080507 00318 NM 2008 5 7 GTIA0800060 1 20080408 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 504NK 2473 FLOORBEAM CORRODED AT Y1292 FRAME 68-69. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 2008050700347 20080507 00347 SO 2008 5 7 C2XA08TY048 1 20080428 A 5751 14569009406 ATTACH BRACKET EMB 145 EMB145XR 3260214 SO RT AILERON WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14143 145739 RIGHT AILERON PCA ATTACH BRACKET WORN. REMOVED AND REPLACED PCA BRACKET IAW EC5750-01177. OPS CHECK GOOD AIRCRAFT STIL L IN "C" CHECK. 2 L 7 2 4F RT 2008050700367 20080507 00367 NM 2008 5 7 SWAA082395 1 20080502 A 5210 507945272 DOOR FRAME BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR FWD FRAME CRACKED AT LOWER STOP FITTING. REMOVED AND REPLACED L1 DOOR PER MM. 2 L 7 2 4F RT A16WE 2008050700374 20080507 00374 NM 2008 5 7 SWAA082426 1 20080504 A 5310 6545808 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED BRDG CHECK, FOUND FWD SERVICE DOOR CUTOUT FWD FRAME CRACKED AT LOWER FWD CORNER. REPAIRED FRAME PER SR M. 2 L 7 2 4F RT A16WE 2008050700397 20080507 00397 NM 2008 5 7 SWAA082405 1 20080504 A 5312 6545819 PRESSURE PANEL BOEING 737 7373A4 1384585 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED MV1 CHECK, FOUND NLG W/W FWD LEFT PRESSURE WEB CRACKED AT BS 246, WL 170. REPAIRED WEB PER SWA EA. 2 L 7 2 4F RT A16WE 2008050800008 20080508 00008 WP 2008 5 8 08FDEA01676 1 20080429 A 5320 ARC0468107 BRACKET DOUG MD10 MD1010F 3022112 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 LT MLG W/W OUTBD SEAL DEPRESSOR FOR THE MAIN GEAR DOOR IS WORN & CRACKED. SEAL LAND WAS WORN & CRACKED RENDERING IT UNSE RVICEABLE. REMOVED SEAL LAND IAW DC/MD-10 SRM 51-35-01; VOL II. MATERIAL ID TO FAB SEAL LAND IS 7075-0, PO 55041 8.3 IAW DWG ARC0468, REV AW. FABRICATED NEW SEAL LAND IAW DWG ARC0467, REV AW. HEAT TREATED SEAL LAND TO 7075- 6 IAW TPS 1003, REV A. CONDUCTIVITY LOAD 35.2 / 35.5; HT050208-2. APPLIED ALODINE & PRIMER IAW SRM 51-21-01; VOL II. PART MARKED SEAL LAND ARC0468-107FX IAW GMM 7-0-1000. INSTALLED SEAL LAND IAW SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 2008050800023 20080508 00023 CE 2008 5 8 DXTA200802972 1 20080330 A 3233 99121204 ACTUATOR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE NLG VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 398QS 7068 5600522 VIOLENT NOSEWHEEL SHIMMY ON TAKEOFF BETWEEN 20-30 KNOTS (ABORTED TAKEOFF). REMOVED AND REPLACED NOSE GEAR ACTUATOR IAW THE CHAP 32-21-03. LEAK AND OPERATIONAL CHECK NORMAL. R7R SHIMMY DAMPER IAW THE MM CHAPTER 32-21-02. LEAK AND OPS CHE CK NORMAL. REMOVED AND REPLACED STEERING TRIM IAW THE MM CHAP 32-51-00. LEAK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F RT A22CE E25EA 2008050800037 20080508 00037 EU 2008 5 8 BAQA20080009 1 20080419 A 2150 S8990132 O-RING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE A/C BAY BLOWN E BAQA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 03 118NC 7067 CRUISE FLIGHT, CLOSE TO FLIGHT DESTINATION, CREW SMELLED "STRANGE ODOR" IN CABIN/COCKPIT. PILOT TURNED OFF THE ENVIRONM ENTAL CONTROL UNIT AND SMELL CEASED. INSPECTION OF ECU REVEALED THAT THE "INDUCTOR" PIPE TEMPERATURE CONTROLLER TO COOL ING TURBINE HAD A SMALL SPLIT AT THE TURBINE AND PIECES OF THE SEALING O-RING (PACKING) WAS EXPOSED AND MISSING. 1 G 7 2 3U 3 U H13EU E5NE 2008050800049 20080508 00049 EU 2008 5 8 COEA0801917 1 20080417 A 2121 EVAC2423FD COOLING FAN AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE CABIN FAILED A COEA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 NM 13 917FX 354 ODOR IN CREW COMPARTMENT, AFTER LANDING, WHILE TAXIING TO PARKING RAMP. THE CREW NOTICED A LIGHT BURNING SMELL IN COCKP IT, FOLLOWED BY NR1 PACK VALVE FAULT. SHORTLY AFTER ARRIVAL, PERFORMED A TEST ENGINE RUN WITH MECHANIC ON BOARD, TO DUP LICATE. WITH THE NR1 ENGINE PACK ON, AFTER 10 MINUTES, COCKPIT AND CABIN FILLED WITH WHITE SMOKE. CANCELLED FLIGHT DUE TO PROBLEM NOT BEING IDENTIFIED. TROUBLESHOOTING FOUND GROUND COOLING FAN INOPERATIVE AND AFT FLAP VANE DAMAGED. REPL ACED GROUND COOLING FAN. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 2008050800088 20080508 00088 CE 2008 5 8 GLBA20061088 1 20080315 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA LT MLG WORN A GLBA O OTHER O OTHER DE DESCENT 1 NM 03 122UX 17431 2452 UE122 ENROUTE, THE LANDING GEAR WOULD NOT EXTEND NORMALLY WHICH REQUIRED THE PILOTS TO MANUALLY PERFORM THE GEAR EXTENSION. M AINT REMOVED AND REPLACED THE LT MLG ACTUATOR IAW MM 32-30. OPERATIONAL CHECKS OF THE GEAR SWINGS ALL CHECKED NORMAL. L ANDING GEAR ACTUATOR PN 114-380041-15, SN OFF 0722A. 2 L 7 2 4T 3 T RT A24CE E2NE 2008050800119 20080508 00119 NM 2008 5 8 CO1Y200800005 1 20080428 A 5230 AFA3805505 SKIN DOUG MD11 MD11 3023602 NM CARGO DOOR CRACKED B CO1Y K NONE O OTHER IN INSP/MAINT 1 EA 33 725BC 48503 FOUND EXISTING REPAIR ON CTR CARGO DOOR FWD LWR CORNER. 2 L 7 3 4F RT A22WE 2008050800126 20080508 00126 2008 5 8 DXTA200803024 4 20080425 A 3160 6229978408 DISPLAY GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE COCKPIT MALFUNCTIONED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 719QS 162 CO-PILOT'S MFD WENT IN-OP IN FLT WITH A BURNING SMELL. REMOVED DISPLAY & INSTALLED PER CMP 342304 GAC SAV W/O 142032 SQ UAWK 6.1 OPS CHECK GOOD NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A53NM E35NE 2008050800136 20080508 00136 CE 2008 5 8 DXTA200803027 1 20080427 A 2150 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 905QS 7500105 WE HAD SMOKE OF AN UNKNOWN ORIGIN. REMOVED AND REPLACED COCKPIT (ART) AIR CYCLE MACHINE WITH A REPAIRED UNIT IAW 750 M/M 21-51-00. PRE-LUBED ACM IAW 750M/M 12-10-01 CLEANED COALESCER IAW 750M/M 12-10-01 OPS CHECKED PROVED SATISFACTORY. 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008050800139 20080508 00139 CE 2008 5 8 GUUA04220802 1 20080422 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 82539 26050 UE168 DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED RT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT OB ELEVATOR HINGE BRACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 2008050800159 20080508 00159 NE 2008 5 8 AC2A119527 2 20080415 A 7200 PW207D ENGINE BELL 427 427 1182207 SW PWC PW207 PW207D NE MAKING METAL E AC2A K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 21 427GT 56044 MAKING METAL, (2) CHIP LIGHTS IN 80 HOURS. 1 G 7 1 3U 3 U R00001RC E42NE 2008050800167 20080508 00167 NM 2008 5 8 UPS08M52146 1 20080501 A 5210 DOOR DOUG MD11 MD11F 3023600 NM STUCK A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 285UP 48457 L1 CREW ENTRY DOOR WILL NOT OPEN. DEFERRED PER MEL M374808 ASSIGNED. FOUND CONNECTOR BROKEN OFF OF UPLIMIT SWITCH. RE PLACED SWITCH. OPS CHECK GOOD, REF MM 52-11-02. THIS CLEARS M374808. PLACARD PULLED. 2 L 7 3 4F RT A22WE 2008050800169 20080508 00169 WP 2008 5 8 08FDEA01781 1 20080506 A 5420 2170004171 CHANNEL DOUG MD10 MD1010F 3022112 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 1 PYLON PANEL NR 438 CL, INNER CHANNEL IS CRACKED. REMOVED CRACKED CHANNEL AND INSTALLED A NEW CHANNEL REF DC/MD-10 SRM 51-31-01, VOL II. 2 L 7 3 4F RT A22WE 2008050800181 20080508 00181 NM 2008 5 8 SWAA082387 1 20080501 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 724SW 27856 DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008050800183 20080508 00183 2008 5 8 SWAA082407 4 20080502 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008050800184 20080508 00184 NM 2008 5 8 SWAA082408 1 20080502 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM GIRT BAR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK OUT OF ADJUST. ADJUSTED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 2008050800186 20080508 00186 NM 2008 5 8 ASAA0842882 1 20080409 A 5311 654654965 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 CORROSION ON BACKSIDE OF FRAME AT STR 25R AT SKIN ATTACH ANGLE STA 767. CUT OUT DAMAGED SECTION OF ATTACH ANGLE AND INS TALLED REPAIR SHEAR TIE AND DOUBLER IAW B737 400 SRM 53 00 07 FIG 201 AND 51 40 02. 2 L 7 2 4F RT A16WE 2008050800203 20080508 00203 NM 2008 5 8 ASAA0842892 1 20080429 A 5753 SKIN BOEING 737 7374Q8 138447Q NM FORE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 LEFT I/B FORE FLAP LOWER SURFACE IS DENTED 5 6' O/B AND 2" UP. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR S KIN AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008050800208 20080508 00208 SO 2008 5 8 C2XA08CL054 1 20080502 A 3412 CS500060D4A RELAY EMB 145 EMB145LR 3260212 SO COCKPIT BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 13913 145438 MKE FLIGHT 3009 - THE CREW REPORTED SMOKE IN THE CABIN AND FLIGHT DECK AT FLIGHT LEVEL 36,000.PRIOR TO SMOKE THERE WAS A (TAT 2 HEAT INOP) MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE NR 2 TAT CURRENT SENSOR RELAY KO494 AND SOCKET XK049 4. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008050800213 20080508 00213 NM 2008 5 8 SWAA082434 1 20080505 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 288WN 36611 R2 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008050800214 20080508 00214 NM 2008 5 8 SWAA082435 1 20080505 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 291WN 32539 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008050800217 20080508 00217 NM 2008 5 8 SWAA082440 1 20080505 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 832, STR 17L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008050800218 20080508 00218 NM 2008 5 8 SWAA082441 1 20080505 A 5753 6546430122 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND RIGHT WING INBOARD FORE FLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FLAP P ER MM. 2 L 7 2 4F RT A16WE 2008050800219 20080508 00219 NM 2008 5 8 SWAA082442 1 20080505 A 5753 6546431280 SKIN BOEING 737 7373H4 1384600 NM FORE FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND RIGHT WING OUTBOARD FORE FLAP UPPER SURFACE WORN. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2008050800220 20080508 00220 NM 2008 5 8 SWAA082443 1 20080505 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, STR 26R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008050800221 20080508 00221 NM 2008 5 8 SWAA082436 1 20080505 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 2R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008050800222 20080508 00222 NM 2008 5 8 SWAA082437 1 20080505 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, STR 2L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008050800223 20080508 00223 NM 2008 5 8 SWAA082453 1 20080505 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008050800226 20080508 00226 NM 2008 5 8 SWAA082461 1 20080505 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008050800231 20080508 00231 NM 2008 5 8 SWAA082458 1 20080505 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008050800239 20080508 00239 NM 2008 5 8 SWAA082449 1 20080505 A 2560 6557463 FITTING BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 473WN 33832 L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MT. 2 L 7 2 4F RT A16WE 2008050800241 20080508 00241 NM 2008 5 8 SWAA082460 1 20080505 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500C, STR 26L TO STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008050800242 20080508 00242 2008 5 8 SWAA082451 4 20080505 A 2565 63550 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008050800243 20080508 00243 2008 5 8 SWAA082452 4 20080505 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 912WN 36621 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008050900001 20080509 00001 NM 2008 5 9 F3LA200800229 1 20080501 A 5315 D5391323420002 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED LEFT AVIONICS COMPARTMENT FRAME C20 LATERAL BRACE IS FRETTING AT FRAME C20 MOUNT H OLE. MAINTENANCE REMOVED DAMAGED CROSSBEAM, DRILLED UP AND INSTALLED NEW CROSSBEAM AT FRAME C20 LEFT AVIONICS BAY IN AC CORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 AND SRM 51-44-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOU ND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050900008 20080509 00008 WP 2008 5 9 IXXA08SMN124S 1 20080417 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT WING TE FLAP MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER PART WITH IMPROPER REPAIR AT STATION XW -2.000. REMOVE D FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AR EA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 1 ITEM "E", DC8 SRM 57-1-0 PAGE 1, 51-1-21, DC8 SRM 51-1-8B, AND DC8 SRM 51-1-11. 2 L 7 4 4F RT 4A25 2008050900009 20080509 00009 NM 2008 5 9 F3LA200800223 1 20080501 A 5321 D5397496800400 FLOORBOARD AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO LATERAL FLOORBOARD PROFILE AT FRAME 58 BETWEEN STRINGER 38 LEFT AND STRI NGER 41 RIGHT HAS AREA OF CORROSION AROUND NUTPLATE HOLES. MAINTENANCE REMOVED AND REPLACED AFT CARGO FLOORBOARD PROFIL E AT FRAME STATION 58 BETWEEN STRINGER 38 LEFT AND STRINGER 41 RIGHT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-00 AND SRM 53-41-14. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 2008050900013 20080509 00013 NM 2008 5 9 F3LA200800230 1 20080501 A 5320 D5347047520600 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO LEFT FLOORBOARD SUPPORT PROFILE AT STRINGER 38 LEFT BETWEEN FRAMES 52 AN D 56 HAS AREAS OF CORROSION AROUND NUT PLATE HOLES. MAINTENANCE REMOVED PROFILE SUPPORT AT STRINGER 38 LEFT BETWEEN FRA MES 52 AND 56, DRILLED AND PREPPED NEW PROFILE FOR THE INSTALLATION, TREATED, PRIMED AND INSTALLED NEW PROFILE IN ACCORD ANCE WITH THE REQUIREMENTS OF SRM 53-41-14, SRM 51-42-00 AND SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECT ED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050900015 20080509 00015 WP 2008 5 9 IXXA08SMN184S 1 20080424 A 5347 S4889185 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 1580 WORN B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 6 TRACK WITH LUG WORN AT STATION 1580.000. REMOV ED EXISTING SPLICES (AFT SIDE). REMOVED SEGMENT OF DAMAGED TRACK. FABRICATED NEW SPLICES. CLEANED, TREATED AND PRIMED AREA, AND EXISTING SPLICES AND REPAIR PARTS. INSTALLED NEW TRACK AND SPLICES 53-7-3 FIGURE 3E ITEM "G", 51-2-0 FIGURE 5D SHEET 79, DC8 SRM 53-2-3 FIGURE 14 SHEETS 1 AND 2, DC8 SRM 51-3-0, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 2008050900016 20080509 00016 NM 2008 5 9 HALA0800573 1 20080506 A 2421 GCU BOEING 767 767332 1382001 NM APU MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, APU AC GENERATOR DROPPED OFF LINE AT THE GATE DEPARTURE TIME. SWAPPED APU GCU S/N 5295 WITH R T GEN GCU S/N 0815 FOR T/S NO HELP. REINSTALLED GCU'S TO ORIGINAL POSITIONS, PER FIM 24-20-00. REMOVED AND REPLACED AP U GENERATOR, OPS CK'D OK IAW AMM 24-21-01. 2 L 7 2 4F RT A1NM 2008050900023 20080509 00023 2008 5 9 2008UALA02575 4 20080428 A 2565 B14056916 O-RING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE BOTTLE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 584UA 26706 ESCAPE SLIDE HAS A LOW BOTTLE. BOTTLE TO VALVE O-RING LEAKING. REPLACED O-RING 2 L 7 2 4F 4 F RT A2NM E17NE 2008050900024 20080509 00024 EU 2008 5 9 2008UALA02576 1 20080502 A 5320 WEB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 444UA 824 FLOOR WEB CORRODED BETWEEN C69 AND C70, UPPER AND LWR SURFACE, RT SIDE. MAJOR REPAIR ACCOMPLISHED, REPLACED FLOOR WEB . 2 L 7 2 4F 4 F RT A28NM E40NE 2008050900025 20080509 00025 EU 2008 5 9 2008UALA02577 1 20080503 A 3350 BULB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 445UA 826 EXIT LIGHT UNDER AFT RIGHT OVERWING EXIT DOOR (90WL4) INOP. FOUND BULB INOPERATIVE. REPLACED LIGHT AT EXIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050900032 20080509 00032 NM 2008 5 9 2008UALA02586 1 20080502 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD SERVICE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 RIGHT FWD SERVICE DOOR FRAME CRACKED AFT LOWER CORNER. MAJOR REPAIR ACCOMPLISHED WITH EXTERNAL FUSELAGE DOUBLER/TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900040 20080509 00040 2008 5 9 2008UALA02594 4 20080503 A 2565 D31591478U1 SLIDE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE L1 DOOR UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 349UA 24253 DOOR 1 LEFT SLIDE FELL OUT DURING DOOR OPERATION. REINSTALLED DOOR 1 LEFT SLIDE ASSEMBLY PER 25-61-35. AC OK FOR SERVI CE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900042 20080509 00042 NM 2008 5 9 2008UALA02596 1 20080504 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY LIGHT DR 2R AFT SILL LIGHT INOP. FOUND LAMP FAULTY. REPLACED LAMP OP CHECKED NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008050900050 20080509 00050 NM 2008 5 9 2008UALA02604 1 20080504 A 5730 113T161329 PANEL BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LT WING MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 673UA 29254 29241 TEN INCH SQUARE SECTION OF PANEL MISSING FROM UNDER LT WING ABOVE MAIN GEAR. ACP TEMP REPAIR PER EVA 71522 .100 FILLER AND .100 DOUBLER. ACCOMPLISH INSPECTION OR RECHECK AS REQUIRED IN CF0477. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008050900053 20080509 00053 NM 2008 5 9 2008UALA02607 1 20080502 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1420 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 AFT PIT BS 1420 BETWEEN STRINGERS 26L AND 25L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED, CUTOUT DAMAGE AND INSTALLED DOU BLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008050900060 20080509 00060 NM 2008 5 9 2008UALA02615 1 20080502 A 5270 WARNING LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE SERVICE DOOR FALSE ACTIVATION A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 914UA 25381 AFT SERVICE DOOR SHOWED OPEN AFTER DEPARTURE. NO DEFECTS NOTED. UNABLE TO DUPLICATED ON GROUND. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900061 20080509 00061 2008 5 9 2008UALA02616 4 20080502 A 3442 RADAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE WX SYSTEM INOPERATIVE A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 401UA 435 WEATHER RADAR SYSTEM INOP. FLIGHT DIVERTED. REPLACED CONTROL PANEL AND REPLACED SCANNER, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050900062 20080509 00062 2008 5 9 2008UALA02617 4 20080504 A 3400 D2729B003 SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE INOPERATIVE A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 663UA 27160 RTFL DUE TO DOUBLE TRANSPONDER FAILURE. RPLACED ATC ANTENNA SWITCH. 2 L 7 2 4F 4 F RT A1NM E24NE 2008050900071 20080509 00071 NM 2008 5 9 2008UALA02626 1 20080506 A 2910 FITTING AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE HYD SYSTEM LEAKING A UALA O OTHER O OTHER AP APPROACH 1 WP 29 830UA 1243 GREEN HYD SYSTEM FAILURE. LT LANDING GEAR DOOR SWIVEL FITTING LEAKING. REPLACED LT LANDING GEAR DOOR ACTUATOR FWD SWIV EL FITTING. SERVICED GREEN HY SYS. CHECKED NR 1 ENGINE HYD CASE DRAIN FILTER, NO METAL NOTED, REPLACED FILTER. LEAK CHEC KED SWIVEL FITTING & FILTER. CHECKS OK.. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050900073 20080509 00073 NM 2008 5 9 2008UALA02628 1 20080506 A 2530 0289051 OVEN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE GALLEY MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 841UA 1545 FWD GALLEY OVEN 106 R12 COOKED VERY SLOWLY THEN GOT SO HOT IT BURNED PLASTIC CASING ON OUTSIDE. REPLACED OVEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050900082 20080509 00082 NM 2008 5 9 08FDEA01767 1 20080506 A 5311 AFA00193 FRAME DOUG MD11 MD11F 3023600 NM BS 1721 L12L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 528FE 48623 AFT CABIN AT APPROXIMATELY STATION 1721 LT LONGERON 12 FOUND FRAME DENTED. REPAIRED AS PER SRM 53-30-00 FIG.1,VOL.I. RE PETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES AS PER SRM 5 3-30-00, FIG.1, VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008050900083 20080509 00083 NM 2008 5 9 2008UALA02631 1 20080505 A 5754 WEDGE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 2 SLAT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 NR 3 SLAT T/E WEDGE ASSEMBLY HAS DAMAGE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900088 20080509 00088 EU 2008 5 9 2008UALA02636 1 20080505 A 5320 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 444UA 824 FLOOR SUPPORT CORRODED FROM C66 TO C68 RBL 30. MAJOR REPAIR ACCOMPLISHED: REPLACED BEAM SUPPORT & SEAT TRACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050900090 20080509 00090 NM 2008 5 9 2008UALA02640 1 20080505 A 5310 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 FUSELAGE DOOR FRAME GOUGED DUE TO LATCH ON ACCESS DOOR 113AL. TRIMMED OUT DAMAGE AND ACP 'D HFEC INSPECTION PER NDT 6-5 1-00-19, AND FABRICATED A REPAIR A NGLE AND FILLER AND INSTALLED PER REO G12327, REV. B ON NO N ROUTINE 28814. PER EVA 7 1516, 2 L 7 2 4F 4 F RT A2NM E17NE 2008050900091 20080509 00091 NM 2008 5 9 2008UALA02641 1 20080506 A 5330 SKIN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 799UA 26926 A DENT WAS FOUND ON EXTERNAL SKIN OF BULK CARGO DOOR AT FWD LOWER CORNER. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AR EA. ACCMP HFEC INSP FOR CRACK FREE CUTOUT. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008050900096 20080509 00096 NM 2008 5 9 F3LA200800211 1 20080501 A 5321 D5367221800000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED FWD CARGO FLOOR PANEL 132DG HAS A PUNCTURE. MAINTENANCE CLEANED AREA AND PREPPED AND APPLIED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PARAGRAPH 8C. UPON COMPLETION OF THE REPAIR IT W AS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050900099 20080509 00099 WP 2008 5 9 UPS08852155 1 20080424 A 5712 RIB DOUG DC8 DC873F 302199F WP RWS 410 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 RT WING CENTER LE UPPER RIB WORN AND GOUGED AT XFS 410. REPAIRED RT WING CENTER LE UPPER RIB AT XFS 410 IAW SRM 57-03-03-0 AND SRM 57-02-00-0 FIG 002. 2 L 7 4 4F RT 4A25 2008050900100 20080509 00100 WP 2008 5 9 UPS08852156 1 20080424 A 5712 RIB DOUG DC8 DC873F 302199F WP RWS 332 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 RT WING CENTER LE LWR RIB REPAIR DOUBLER CRACKED AT XFS 332. REPAIRED RT WING CENTER LE LOWER RIB AT XFS 332 IAW SRM 57-03-03-0 AND 57-02-00-0 FIG 002. 2 L 7 4 4F RT 4A25 2008050800152 20080508 00152 EU 2008 5 8 08FDEA01774 1 20080428 A 5311 A5383312720400 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 MAIN CABIN FRAME 40 BETWEEN STRINGERS 15R AND STRINGER 16R ARE GOUGED. SMOOTH BLEND OUT THE DAMAGED AREA IAW EA 6-5310- 118485 "FUSELAGE - FRAME 40 AT STRINGER 15 AND 16 LT AND RT GOUGE REPAIR". 2 L 7 2 4F RT A35EU 2008050800154 20080508 00154 EU 2008 5 8 08FDEA01775 1 20080501 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 MAIN CARGO COMPARTMENT, SEAT TRACK SCALLOPS ARE GOUGED AND ELONGATED AT FRAME C 58, 15 INCH, RBL 37 INCHES. THIS SDR WA S GENERATED IN ERROR. FOR DETAILS PLEASE SEE SDR TRACKING NR 08-1664. 2 L 7 2 4F RT A35EU 20080519 EU 2008 5 19 08FDEA01804 1 20080508 A 5730 A5726030620400 SKIN AIRBUS 300 A300F4605R 3930327 EU LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 LEFT WING TIP INBD SIDE SKIN HAS CORROSION AROUND THE STATIC WICK BASE. REMOVED STATIC WICK BASE AND REMOVED THE CORROS ION. ORIGINAL THICKNESS 0.056 IAW AA300-600 SRM 57-30-11. REMOVED MATERIAL 0.014. REMAINING THICKNESS 0.042 AND IS OU T OF LIMITS IAW A300-600 SRM 57-31-11; PARA 4. MATERIAL ID FOR REPAIRS 2024-T3 IAW A300-600 SRM 51-31-00; PGD 21-24. F ABBED JOINT PLATE AND FILLER IAW A300-600 SRM 57-30-11; FIG 201. INSTALLED NEW STATIC WICK BASE IAW A300-600 AMM 23-61- 21-4 AND COMPLETED MEG CHECK. INSTALLED JOINT PLATE AND FILLER IAW A300-600 SRM 57-30-11; FIG 201. 2 L 7 2 4F RT A35EU 20080519 NM 2008 5 19 AALA200800913 1 20080410 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 756AM 30264 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 30C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 30C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 EU 2008 5 19 TRB2008051 1 20080509 A 3240 BRAKE SYS AEROSP ATR72 ATR72212 8680945 EU MALFUNCTIONED A TRBA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 29 270AT 270 CAPT REPORTED BRAKE PROBLEMS. CAPT RT BRAKE AND F/O LT BRAKE INOP. AWAITING AML PAGE FOR DETAILS. 2 H 7 2 4T RT A53EU 20080519 EA 2008 5 19 MALA080084 1 20080424 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 8946A 7946 FS 621 TO FS 625 LT UPPER INTERCOSTAL (OBLIQUE) ANGLE AT STRINGER 14L IS CRACKED 1.5 INCH LONG IN AFT RADIUS. DRILLED A ND REMOVED FS 625 LT UPPER INTERCOSTAL ANGLE AND INSTALLED NEW INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND 51-42-21 AND BOM BARDIER REO 601R-53-61-422. WAITING MESABA EO FOR CLOSEOUT. C/W STA 621-625 INTERCOSTAL RE. 2 L 7 2 4F RT A21EA 20080519 EA 2008 5 19 MALA080085 1 20080429 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 8943A 7943 AT FS 625, LT SIDE, ANGLE IS CRACKED APPROX 1.0 IN. ANGLE WAS REPLACED WITH NEW. 2 L 7 2 4F RT A21EA 20080519 SO 2008 5 19 SWIA200819570 1 20080430 A 7712 300500052 SIGNAL COND UNIT EMB 120 EMB120ER 3260203 SO ENGINE TORQUE MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 218SW 120287 FLT 5098 - RECEIVED AN AUTO FEATHER AURAL WARNING ON TAKEOFF. REPLACED NR 2 ENGINE TORQUE SIGNAL CONDITIONER IAW EMB MM 77-11-01. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080519 WP 2008 5 19 08FDEA01832 1 20080512 A 5753 ARC05036 HINGE DOUG MD10 MD1010F 3022112 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 RIGHT WING OUTBD FLAP, OUTBD HINGE LOCATION NR 3 OUTBD BORE IS CORRODED. REMOVED CORROSION FROM THE OUTBD BORE OF THEN 3 LUG IAW CMM 57-44-01. MACHINED BUSHING FOR THE OUTBD BORE IAW 57-44-01. CAD PLATED BUSHING IAW QQP-416-TY2-CL2 7. I NSTALLED THE BUSHINGS IAW CMM 57-44-09. COMPLIED WITH FEDEX EA 8-5740-116979 DATED 5/1/2008. 2 L 7 3 4F RT A22WE 20080519 NM 2008 5 19 AALA200800964 1 20080415 A 2750 FSEU BOEING 737 737823 13844BZ NM E&E BAY INOPERATIVE A AALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 971AN 29547 LAX INFLIGHT T263/15APR - CREW REPORTED FLAPS STUCK AT 17 DEGREES. LANDED LAX WITHOUT INCIDENT. REPLACED FLAP SLAT ELE CTRONICS UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080519 WP 2008 5 19 AALA200800950 1 20080414 A 3260 PSEU DOUG DC9 DC982 3022082 WP E&E BAY INOPERATIVE A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 440AA 49459 DFW INFLIGHT T1174/14APR - CREW REPORTED NO GREEN LIGHT WHEN LANDING GEAR WAS EXTENDED. TOWER CONFIRMED GEAR DOWN AND L OCKED. LANDED DFW WITHOUT INCIDENT. REPLACED PROXIMITY ELECTRONIC SWITCH UNIT AS PRECAUTION. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F A6WE 20080519 WP 2008 5 19 AALA200800965 1 20080415 A 2752 ACTUATOR DOUG DC9 DC983 3022083 WP T/E FLAP LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 SW 21 569AA 49351 BOS INFLIGHT T1466/15APR - CREW REPORTED LOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY. LANDED BOS WITHOUT INCIDENT. FOUND RIGHT INBOARD FLAP ACTUATOR AND RUDDER SHUTOFF VALVE LEAKING. REPLACED RIGHT INBOARD FLAP ACTUATOR AND RUDDER SHUTOFF V ALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 AALA200800966 1 20080415 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 689AA 25731 DFW - EMERGENCY LIGHT AT SEAT 19C BULLNOSE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 19C BULLNOSE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080519 NM 2008 5 19 HALA0800537 1 20080417 A 2120 UNKNOWN BOEING 717 717200 1383700 NM CABIN ODOR A HALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 486HA 55131 LIGHTNING STRIKE LIH-HNL MID CHANNEL. NOTHING NOTICED IN COCKPIT HOWEVER FA'S SAY THEY SMELLED A HINT OF SMOKE AFTER ST RIKE AND THEN NOTHING. INSP AIRFRAME AND ENGS PER MM 05-52-03. DEFECTS ENTERED IN LOG BOOK. INSP OF WX RADAR AND GIS ANT CK OK. INSPECTION OF IRS AND STBY COMPASS CK OK. INSP OF CABIN AND GALLEY LIGHTING AND EQUIPMENT FOUND NO DEFECTS OR ODOR. COMPLIED WITH M-584-717, LIGHTNING STRIKE INSP. 2 L 7 2 4F TR A6WE 20080519 EU 2008 5 19 5102008N218CA 1 20080510 A 7997 MS3126F1210S CONNECTOR JAEGER AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE COCKPIT BURNED E CEDA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 05 218CA 218 304404B SMALL AMOUNT OF SMOKE NOTICED IN COCKPIT. 2 L 7 2 4F 4 F RT A7EU E7EA 20080519 NM 2008 5 19 DLM88080694 1 20080501 A 5313 LONGERON DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 960DL 49979 FOUND CRACK ON LONGERON 2 LT AT STA 1418. REPAIRED PER SRM 53-02D FIG 18 ON N/R T0092996 AT HMV-3 IN GDL. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 DLM88080695 1 20080509 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 960DL 49979 EXFOLIATION CORROSION ON LT CUSP WEB STA Y=586-598 AND X=60 REPLACED WEB PER DWG 9930538. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 DLM90080700 1 20080508 A 5313 LONGERON DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 AFT CARGO BAY LONG 27L CORRODED AROUND FASTENERS AND DRAIN HOLES STA 1344-1364. REPAIRED LONG, IAW MD90 SRM 53-10-01, F IG 7 VOL 1. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 DLM90080708 1 20080504 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 CABIN SEAT TRACK FS 1136-1174 RBL 54 OUT OF LIMITS. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01, VOL I. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 DLM90080709 1 20080504 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 LT STA 1360 CUSP WEB CRACKED. REPAIRED CUSP WEB, IAW MD90 SRM 51-11-01, FIG 2. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 DLM90080710 1 20080501 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 LT CUSP WEB HAS CORROSION AT LIGHT WING HOLE AFT OF STA 560 ON UPPER AND LOWER SURFACE. REPAIRED CUSP WEB, IAW MD80 SRM 53-05D, FIG 827D. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 DLM90080711 1 20080501 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 LT CUSP WEB HAS CORROSION ON UPPER SURFACE AT STA 541-560. REPAIRED CUSP WEB, IAW MD80 SRM 53-05D, FIG 827D. 2 L 7 2 4F RT A6WE 20080519 2008 5 19 2008UALA02537 4 20080430 A 2565 D30654122U1 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 1L SLIDE PRESS IS IN THE RED. REPLACED SLIDE PACK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080519 NM 2008 5 19 DLM88080727 1 20080512 A 5330 99115311 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 984DL 53311 LIGHTNING STRIKE FOUND ON UPPER AFT CORNER OF WINDOW 21L CUTOUT. AREA BLENDED AND INSPECTED. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 2008UALA02504 1 20080428 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROWS 9 - 13 DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 543UA 25698 EEL LIGHTS INOP ROW 9 - 13. FOUND EEL SEGMENT DISCONNECTED RECONNECTED EEL SEGMENTS, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080519 NM 2008 5 19 2008UALA02497 1 20080428 A 3350 SIGN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE DOOR 2R DISLODGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 817UA 873 DOOR 2R EMERGENCY LIGHT DISLODGED ON TAKEOFF AND HANGS BY WIRES. REPLACED EMER EXIT SIGN ASSY WITH NEW. 2 L 7 2 4F 4 F RT A28NM E40NE 20080519 WP 2008 5 19 AALA200801005 1 20080418 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 982TW 53632 LGA - EMERGENCY LIGHTS AT SEAT ROWS 7 TO 2O INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 7 TO 2 0. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080519 WP 2008 5 19 AALA200801007 1 20080418 A 3397 WIRE HARNESS DOUG DC9 DC983 3022083 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 982TW 53632 LGA - EMERGENCY LIGHTS AT SEAT ROWS 7 TO 2O INOPERATIVE. REPAIRED HARNESS AT SEAT 14DEF FOR EMERGENCY LIGHTS AT SEAT RO WS 7 TO 20. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080519 WP 2008 5 19 AALA200800997 1 20080417 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 491AA 49684 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 24 TO 26 INOPERATIVE. REPLACED BATTERY PACK AT B5 1 FOR EMERGENCY LIGHTS A T OVERHEAD SEAT ROWS 24 TO 26. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080519 WP 2008 5 19 AALA200800986 1 20080416 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9628W 53598 LGA - EMERGENCY LIGHT AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT AB5 4 FOR EMERGENCY LIGHT AT AFT CABIN. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080519 WP 2008 5 19 AALA200800987 1 20080416 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9628W 53598 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 6 TO 8 INOPERATIVE. REPLACED BATTERY PACK AT B5101 FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 6 TO 8. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 AALA200800989 1 20080416 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 MIA - MOUNTED EMERGENCY LIGHTS AT FIRST CLASS F5 GALLEY CLOSET INOPERATIVE. REPLACED BATTERY PACK FOR MOUNTED EMERGENCY LIGHTS AT FIRST CLASS F5 GALLEY CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500042 20080515 00042 WP 2008 5 15 AALA200800828 1 20080406 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9621A 53592 SFO - EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 25D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008051500050 20080515 00050 EA 2008 5 15 A6WA200840337 1 20080414 A 3260 TARGET CNDAIR CL600 CL6002B19 1900309 EA LT MLG LOOSE A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 465AW 7893 LT MLG DID NOT RETREAT AFTER TAKEOFF GEAR DISAGREE MSG C/W QRH RETURN TO LGA AT WS 39800 LBS. FOUND LT UPLOCK TARGET LO OSE AND OUT OF ADJUSTMENT. ADJUSTED TARGET FOR LT MLG UPLOCK. REF AMM 32-32-05. OPS TEST OF LANDING GEAR EXTENTION AN D RETRACTION SYSTEM NORMAL. REMOVED FROM MEL. 2 L 7 2 4F RT A21EA 2008051500074 20080515 00074 WP 2008 5 15 AALA200800890 1 20080409 A 3610 BOOT DOUG DC9 DC983 3022083 WP DUCT SPLIT A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 9615W 53562 DFW INFLIGHT T852/09APR - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH AND DUCT PRESSURE ANOMALY. REDUCED POWER FOR DESCENT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION AND REPAIR. FOUND BLOWN DUCT BOOT ON RIGHT TEMPERATURE CONTROL DUCT. REPLACED DUCT BOOT ON RIGHT TEMPERATURE CONTROL DUCT. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008051500076 20080515 00076 NM 2008 5 15 AALA200800884 1 20080408 A 3350 OL3071BPEGPL LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHT AT SEAT 32G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500089 20080515 00089 NM 2008 5 15 F3LA200800256 1 20080503 A 5322 D53571131258 SHEAR TIE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE MISALIGNED A F3LA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED FRAME 72 SHEAR TIE BETWEEN STRINGER 24 RIGHT AND 25 RIGHT HOLES DO NOT ALIGN WITH REP AIR. MAINTENANCE FABRICATED NEW SHEAR TIE IN ACCORDANCE WITH THE REQUIREMENTS OF AIRBUS DRAWING D53571161. INSTALLATIO N OF NEW SHEAR TIE WAS ACCOMPLISHED ON NON ROUTINE C043414. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND AC CEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008051500091 20080515 00091 NM 2008 5 15 F3LA200800251 1 20080501 A 5321 D5367302800000 FLOORBOARD AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED AFT CARGO FLOOR PANEL 151DE HAS DAMAGED EDGE AND CORNER. MAINTENANCE CLEANED AND PREPPED AREA, MANUFACTURED DOUBLER AND APPLIED REPAIR TO AREA. MANUFACTURED DOUBLER, APPLIED TREATED AND PRIMED AREA IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 AND 51-75-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUN D ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008051500142 20080515 00142 NM 2008 5 15 AALA200800955 1 20080414 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 MIA - EMERGENCY LIGHT AT SEAT 17H INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 17H. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008051500147 20080515 00147 NM 2008 5 15 AALA200800953 1 20080414 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 MIA - EMERGENCY LIGHTS AT SEAT ROWS 22H TO 24H INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT ROWS 22H TO 24H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008051500151 20080515 00151 NM 2008 5 15 AALA200800952 1 20080414 A 2740 RELAY BOEING 737 737823 13844BZ NM STAB TRIM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 958AN 30091 LAX INFLIGHT T465/14AP DFW TO SNA - CREW REPORTED BOTH AUTO PILOTS AND STABILIZER TRIM INOPERATIVE. LANDED LAX WITHOUT INCIDENT. REPLACED STABILIZER TRIM INTERLOCK RELAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008051500169 20080515 00169 EU 2008 5 15 08FDEA01823 1 20080512 A 5415 ATTACH ANGLE AIRBUS 310 A310324 3930206 EU NR 2 PYLON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 NR 2 PYLON AFT LOWER FAIRING PANEL NR 485 AL, LT UPPER ATTACH ANGLE IS CHAFED IN SEVERAL PLACES. REMOVED DAMAGED LONGER ON & INSTALLED NEW LONGERON PER SRM 51-40-21 PARA 6 - 7. LOCATED DRILLED HOLES PER SRM 51-40-44. ALODINED & PRIMED P ER AMM 51-23-00. 2 L 7 2 4F RT A35EU 2008051500183 20080515 00183 WP 2008 5 15 08FDEA01833 1 20080513 A 5730 ARB10712 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 EXISTING EXTERNAL REPAIR DOUBLER AT FIXED L/E STA XIS 150 REMOVE REPAIR AND ACCOMPLISH A NEW IAW SRM 57-10-00 FIG 40 BEC AUSE REPAIR DETECTED WAS FOUND WITH A SIGNIFICANT LOSS OF MATERIAL DUE TO A LIP CONTACT. 2 L 7 3 4F A22WE 2008051500189 20080515 00189 NM 2008 5 15 DLM90080706 1 20080506 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 674-760 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 CABIN SEAT TRACK FS 674-760 RBL 54 OUT OF LIMITS. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01, VOL 1. 2 L 7 2 4F RT A6WE 2008051500197 20080515 00197 EA 2008 5 15 SWIA200819618 1 20080508 A 2160 SWITCH CNDAIR CL600 CL6002B19 1900309 EA ACM TEMP FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 930SW 7713 FLT 5932 - WHITE SMOKE BEGAN TO FILL THE FLIGHT DECK WHILE AT THE GATE. REPLACED ACM HI TEMPERATURE SWITCH PER AMM 21-5 1-25. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008051500201 20080515 00201 EA 2008 5 15 SWIA200819622 1 20080227 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 909SW 7558 STN 280 AT LBL9.0 AND RBL9.0 UPPER FLOOR SUPPORT ANGLE IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO601R 53-11-136. 2 L 7 2 4F RT A21EA 2008051600010 20080516 00010 NM 2008 5 16 SWAA082466 1 20080506 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 430, BL 0. REPAIRED SKIN P ER EA. 2 L 7 2 4F RT A16WE 2008051600023 20080516 00023 NM 2008 5 16 SWAA082474 1 20080506 A 5754 65C26601 SLAT BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING NR 5 L/E SLAT OUTBOARD T/E DELAMINATED. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 2008051600045 20080516 00045 NM 2008 5 16 SWAA082510 1 20080507 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 540, STR 17R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082507 1 20080507 A 5312 148A22811 BULKHEAD BOEING 737 7377H4 1384404 NM FUSELAGE CANNING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 713SW 27847 DURING SCHEDULED MV2 CHECK, FOUND AFT PRESSURE BULKHEAD OIL CANNED AT BS 1016, BETWEEN STR 5L AND STR 6L. REPAIRED BULK HEAD PER SWA EA. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082559 1 20080511 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 AFT CABIN EMERGENCY EXIT LIGHTS WILL NOT TURN OFF. REMOVED AND REPLACED BATTERY PACK AND BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082567 1 20080511 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082566 1 20080511 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082593 1 20080512 A 5311 6545808 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, STR 3L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082606 1 20080512 A 5313 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082576 1 20080509 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080516 EU 2008 5 16 08FDEA01782 1 20080501 A 5730 A579655310000 PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 LEFT WING T/E PANEL 590 AB AFT CORNER IS BROKEN, BLENDED CORNER ON THE LEFT T/E PANEL, SEALED EDGE AND PAINTED IAW A300- 600 SRM 51-42-20. 2 L 7 2 4F RT A35EU 20080516 NM 2008 5 16 08FDEA01784 1 20080507 A 5311 ACA75311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 628FE 48447 MAIN DECK INTERIOR FUSELAGE AT LEFT STA 535 FRAME, UPPER SUPPORT YOKE FOUND DAMAGED. MAIN DECK INTERIOR FUSELAGE AT LEFT HAND STA 535, UPPER SUPPORT YOKE, DAMAGED FRAME REPAIRED AS PER FEDEX DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MINO R PER GMM 6-2- 100. 2 L 7 3 4F RT A22WE 20080516 NM 2008 5 16 2008UALA02473 1 20080427 A 3350 767 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 564UA 26666 EXT EMERGENCY EXIT LIGHT INOP DOOR 2R, RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080516 NM 2008 5 16 2008UALA02485 1 20080425 A 5753 654643662SP FLAP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RT WING DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 922UA 26642 RT INBOARD TRAILING EDGE FLAP HAS APPROX 10 IN DELAMINATION ON INBOARD TRAILING EDGE. REPAIRED TRAILING EDGE REF SRM 51 -70-10 P201 REPAIR 1. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 20080516 WP 2008 5 16 UPS08852117 1 20080420 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING OUTBD LE UPPER RIB CRACKED JUST INBD OF ACCESS PNL 519B AT XFS 641. REPAIRED RT WING LE UPPE R RIB AT XFS 641 IAW SRM 57-03-03-0 FIG 006 AND SRM 57-02-00-0 FIG 002. 2 L 7 4 4F RT 4A25 20080516 NM 2008 5 16 UPS08M52099 1 20080403 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C CABIN, CORROSION ON SEAT TRACK CROWN AND CHANNEL AT STA1199 X=-8. CORROSION AT AFFECTED AREA REMOVED MAT'L REMOVED 0.040" (STA1199), MAT'L REMN: 0.105", FOUND OUT OF LIMIT. NEW SEAT TRACK FROM STA 1129 TO 1209 X=-8 REWOR KED. HOLES PICKED UP ON NEW SEAT TRACK AND PAINTED. NEW SEAT TRACK INSTALLED AS PER SRM 53-70-00 FIG VIR35. 2 L 7 3 4F RT A22WE 20080519 WP 2008 5 19 NWAA081899885 1 20080501 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 401EA 47682 DURING LINE CHECK THE EMERGENCY OVERWING EXIT SIGNS AT ROW 19, 20, 21 AND 22 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE ASSOCIATED FUSE AND BATTERY, NEITHER CORRECTED THE PROBLEM. THE POWER SUPPLY WAS CHANGED AND THE SYSTEM CH ECKS NORMAL. 2 L 7 2 4F RT A6WE 20080519 WP 2008 5 19 DHL2008807503 1 20080417 A 7110 SKIN DOUG DC8 DC873F 302199F WP COWLING WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 NR 3 ENG NACELLE INLET COWL UPPER SURFACE WORN AT 12 O'CLOCK POS STA YN 147.534 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8-70 SRM 71-5-2 FIG 2 (SHEET 1-2). REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED S KIN (AL2024T3 0.080") AND SPLICE (SHEET CRES 0.050" TYPE 17-7 PH) IAW DC8-70 SRM 71-5-2 FIG. 2 SHEET 1-2. HEAT TREATED SPLICE FROM CRES 17-7PH TO CRES 17-7PH (H1050) IAW SRM 51-1-6. CLEANED, TREATED AND PRIMED AREA AND SKIN INNER FACE IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 71-5-2 FIG 2 SHEET 1-2, SRM 51-1-11, SRM 51-1-21A. 2 L 7 4 4F RT 4A25 20080519 NM 2008 5 19 AALA200800834 1 20080407 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 786AN 30250 DFW - EMERGENCY LIGHT AT SEAT 45G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 45G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050800155 20080508 00155 EU 2008 5 8 08FDEA01776 1 20080506 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 MAIN DECK FLOOR TRACK AT FRAME 53; RBL 20 IN CORRODED IN THE CENTER OF THE TRACK. REMOVED AND REPLACED SEAT TRACK IAW A300 SRM 51-40-21, PARAGRAPHS 5, 6 AND 7. 2 L 7 2 4F RT A35EU 2008050800156 20080508 00156 EU 2008 5 8 08FDEA01777 1 20080506 A 5315 A5381293420000 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 CROSSBEAM AT FRAME 52 BETWEEN RBL 20 - RBL 40 IS CORRODED. REMOVED AND REPLACED THE CROSSBEAM IAW A300 SRM 51-40-21, PA RA 5. 2 L 7 2 4F RT A35EU 2008050800163 20080508 00163 WP 2008 5 8 08FDEA01780 1 20080506 A 5414 AUB703625 PANEL DOUG MD10 MD1010F 3022112 WP NR 1 PYLON DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 1 PYLON PANEL 483 GL HAS 1 FASTENER HOLE WALLOWED OUT. ANNEALED TITANIUM IAW E.A. 8-5480-116981. FORMED & FABBED IAW DWG AUB 7036. REMOVED & INSTALLED DRAIN TUBE IAW E.A. 8-5480-116981. INSTALLED IAW SRM 51-35-01. LOCATED & DRILLE D HOLES IAW SRM 51-31-01. INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F RT A22WE 2008050800164 20080508 00164 NM 2008 5 8 UPS08M52137 1 20080125 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 840-859 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C CABIN, MAIN DECK SEAT TRACK AT BS 840-BS859 X=-7.5 (RT) FOUND CORROSION AS MARKED CORRODED SECTION TRI MMED OFF PER SRM 53-70-00 V.1FIG.R.40. HFEC INSP C/OUT IAW DAC NDTSPM 06-10-01.001R.13 FOUND NO CRACK EVIDENT. REPAIR SPLICES AND PLATES FABRICATED PER SRM 53-70-00 V.1R.40 FIG 1. HOLES PICK UP ON REPAIR PARTS PER SRM 53-70-00V.1R.40 FIG 1 AND REPROTECTED PER SRM 51-21-01 V .2R.40. REPAIR PARTS AND TRACK INSTALLED PER SRM 53-70-00 V1 FIG 1R 40. 2 L 7 3 4F RT A22WE 2008050800165 20080508 00165 NM 2008 5 8 UPS08M52138 1 20080125 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 840-859 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C CABIN-MAIN DECK SEAT TRACK AT BS 840-BS 859 X=+27.5 (LT) FOUND CORROSION AS MARKED. CORRODED SEAT TRA CK FRAME EXISTING SECTION REMOVED PER SRM 51-33-01 V.2R.40. HFEC INSP C/OUT IAW DACNDTSPM R.13 PART06.10.01.001 FOUND N O CRACK EVIDENT. REPAIR SPLICES AND PLATES FAB PER SRM 53-70-00 V.1R.40 FIG 1. HOLES PICK UP PER SRM 51-31-01V.2R.40. AND PROTECTED PER SRM 51-21-01V.2R.40. SEAT TRACK INSTALLED PER SRM 51-33-01 V.2R.40. AND SRM 57-00-01 V.1R.40 FIG 1. 2 L 7 3 4F RT A22WE 2008050800166 20080508 00166 NM 2008 5 8 UPS08M52139 1 20080130 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1964-1953 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C CABIN RT SEAT TRACK AT STA 1964-1953 RBL=107 FOUND CORRODED AS MARKED. CORRODED SEAT TRACK REMOVED PE R SRM 51-31-01V.2R.40. HFEC INSP C/OUT IAW DAC NDTSPM 06-10-01.001R.13 FOUND NO CRACK EVIDENT. NEW SEAT TRACK AND SPLI CE REWORK PER SRM 53-70-00V.1 FIG 1R.40. SPLICE PLATE FAB PER SRM 53-70-00V.1FIG 1R.40. REWORK AND FAB REPAIR PROTECTE D PER SRM 51-21-01 V.2R.40. SEAT TRACK INSTALLED PER SRM 51-31-01 V.2R.40 AND SRM 53-70-00 V.1FIG 1 R.40. 2 L 7 3 4F RT A22WE 2008050800171 20080508 00171 WP 2008 5 8 UPS08852164 1 20080503 A 5220 DOOR DOUG DC8 DC873F 302199F WP LT OVERWING BINDING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 LT OVERWING EMERGENCY EXIT DOOR BINDING. LUBRICATED SEAL AND ALL MOVING PARTS IAW MM 12-80-00. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 2008050800172 20080508 00172 NM 2008 5 8 UPS08M52148 1 20080125 A 5320 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1215 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C CABIN AT STA 1215, ADJACENT LONGERON 27 RT TOP INTERCOSTAL STIFFENER FOUND CRACKED AT FWD EDGE. NEW I NTERCOSTAL STIFFENER FABRICATED USING MATL 60-17778X7075T6511 PER EN1069-08. FPI C/OUT IAW BOEING DPS 4.707 REV.AW FOUN D NO CRACK EVIDENT. HOLES PICKED UP ON NEW INTERCOSTAL STIFFENER PER SRM 51-31-01 V.2R.40 AND REPROTECTED PER SRM 51-21 -01V.2R.40. NEW INTERCOSTAL STIFFENER INSTALLED PER SRM 51-31-01 V.2R.40 AND SRM 51-33-01 V.2R.40. 2 L 7 3 4F RT A22WE 2008050800173 20080508 00173 NM 2008 5 8 UPS08M52149 1 20080320 A 5420 FAIRING DOUG MD11 MD11 3023602 NM NR 2 PYLON DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C PYLON NR 2 EXHAUST FAIRING RT FWD SEAL 2ND MOUNT HOLE FROM BOTTOM FOUND ELONGATED AFTER REMOVAL OF SEA L AND RETAINER. DAMAGED AREA TRIMMED OUT PER EN1131-08 AND MD11-54-20174. HFEC INSP C/OUT PER DAC NDT SPM R.13 06-10-0 1.001 FOUND NO CRACK EVIDENT. EXTERNAL DOUBLER FABRICATED USING 2219-0.071" PER EN1131-08 AND MD11-54-20174. REPAIR DO UBLER HEAT TREATED TO T62 COND PER DPS7.00-1 HARDNESS OBTAINED HRB64.9 ACCEPTABLE PER DRPS1.05.3. REPAIR PART INSTALLED PER UPS RAA MD11-54-20174. 2 L 7 3 4F RT A22WE 2008050800174 20080508 00174 NM 2008 5 8 UPS08M52150 1 20080320 A 5420 FAIRING DOUG MD11 MD11 3023602 NM NR 2 PYLON DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C PYLON NR 2 EXHAUST FAIRING LT FWD SEAL MOUNT 3RD HOLE FROM BOTTOM FOUND ELONGATED AFTER REMOVAL OF SEA L AND RETAINER. DAMAGED AREA TRIMMED OUT PER EN1131-08. HFEC INSP C/OUT PER DAC NDTSPM R.13 06-10-01.001 FOUND NO CRAC K EVIDENT. EXTERNAL DOUBLER FABRICATED USING 2219-0 0.071" PER EN1131-08. REP DOUBLER HEAT TREATED TO T62 COND PER DPS 7.00-1 HARDNESS OBTAINED HRB64.9 IS ACCEPTABLE PER DPS1.05-3. REPAIR PARTS INSTALLED PER UPS RAA NR MD11-54-20174 AND E N 1131-08. 2 L 7 3 4F RT A22WE 2008050800176 20080508 00176 2008 5 8 ASAA0852873 4 20080503 A 2211 4082499903 COMPUTER BOEING 737 737890 1384527 NM COCKPIT FAULTY A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 570AS 35185 SPEED TRIM FAIL AND MACH TRIM FAIL LIGHTS CAME ON DURING RECALL CHECK AFTER ENGINE START. F/O'S FD FLAG ALSO CAME ON. VERIFIED FAULT. FCC "B" COMPUTER INOP. REPLACED FCC "B" COMPUTER. PERFORMED LRU TEST FOR FCC & LAND VERIFY TEST. HGS SENSOR TEST FOR FCC PASS. 2 L 7 2 4F RT A16WE 2008050800180 20080508 00180 NM 2008 5 8 ASAA0852872 1 20080503 A 4990 38810521 INDICATOR BOEING 737 737890 1384527 NM FILTER MALFUNCTIONED A ASAA O OTHER N FALSE WARNING IN INSP/MAINT 1 NM 02 577AS P7451 35186 APU OIL FILTER DELTA P INDICATOR EXTENDED. RESET APU OIL FILTER DELTA P INDICATOR. NO CONTAMINATION ON FILTER OR MAGNE TIC DRAIN PLUG. NO LEAKS. OP CHECKS GOOD ON RESET. 2 L 7 2 4F RT A16WE 2008050800182 20080508 00182 NM 2008 5 8 SWAA082406 1 20080502 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 726SW 27858 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008050800188 20080508 00188 NM 2008 5 8 ASAA0842884 1 20080322 A 5313 6552928254 STRINGER BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 STR 25R IS CRACKED AT FASTENER HOLE. REMOVED CRACKED SECTION OF STRINGER, FABRICATED AND INSTALLED REPAIR SECTION AND S PLICES IAW B737 400 SRM 53 00 03 FIG 201 REPAIR 1. 2 L 7 2 4F RT A16WE 2008050800189 20080508 00189 NM 2008 5 8 ASAA0842875 1 20080322 A 5340 69353501 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 STRINGER TIE STA 807 STR 26R IS CORRODED. REMOVED CORRODED STRINGER TIE, FABRICATED AND INSTALLED REPLACEMENT STRINGER TIE IAW B737 400 SRM 51 30 01 AND BOEING DRWG 69 35350. 2 L 7 2 4F RT A16WE 2008050800190 20080508 00190 NM 2008 5 8 ASAA0842885 1 20080422 A 5320 65479573 WEB BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 AFT PIT DOOR THRESHOLD AREA HAS MINOR CORROSION BOTTOM OF RBL 22 STA 787 847 (INSIDE LIP OF WEB). REMOVED CORROSION MAT ERIAL LOSS OF .017 IS OUT OF LIMITS IAW B737 400 SRM 53 60 15 FIG 101. REMOVED AND REPLACED WEB IAW B737 400 SRM 51 40 02 PG 3. 2 L 7 2 4F RT A16WE 2008050800196 20080508 00196 NM 2008 5 8 ASAA0842877 1 20080311 A 5754 WEDGE BOEING 737 7374Q8 138447Q NM L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 NR 4 SLAT T/E WEDGE LOWER SURFACE CHAFED. REMOVED DAMAGED SECTION OF SKIN, FABRICATED AND INSTALLED REPAIR FILLER AND D OUBLER IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 2008050800198 20080508 00198 NM 2008 5 8 ASAA0842874 1 20080312 A 5755 SKIN BOEING 737 7374Q8 138447Q NM NR 4 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 769AS 25103 NR 4 SPOILER HAS SEVERAL DENTS UPPER SURFACE. PREPPED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008050800204 20080508 00204 NM 2008 5 8 ASAA0842893 1 20080501 A 5755 SKIN BOEING 737 7374Q8 138447Q NM SPOILER BULGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 NR 7 SPOILER HAS 2 EACH BULGES ON UPPER SURFACE O/B END. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER A ND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 2008050800205 20080508 00205 NM 2008 5 8 ASAA0842894 1 20080427 A 5753 SKIN BOEING 737 7374Q8 138447Q NM FORE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 RIGHT I/B FORE FLAP LOWER SURFACE HAS SEVERAL DENTS AT WBL 73 95. PREPPED AREA, FABRICATED AND INSTALLED REPAIR DOUBLE RS IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008050800207 20080508 00207 SO 2008 5 8 C2XA08TY049 1 20080501 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13965 145125 FWD CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 6 INVERTER IAW EMB 145 MM 33-50-11. OPS CHECK GOOD. AIRCRAF T RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008050800225 20080508 00225 NM 2008 5 8 SWAA082462 1 20080505 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CREASED AT BS 787 TO BS 790, STR 27R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008050800232 20080508 00232 NM 2008 5 8 SWAA082459 1 20080505 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008050800238 20080508 00238 NM 2008 5 8 SWAA082448 1 20080505 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 416WN 32453 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008050800245 20080508 00245 NM 2008 5 8 ASAA0892898 1 20080415 A 5321 453A2610 FLOOR PANEL BOEING 737 737990 NM CABIN CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 318AS 30018 AFT CARGO NR 1 FLOOR PANEL HAS CORROSION AROUND EDGES. REMOVED DAMAGED FLOOR PANEL, FABRICATED, LOCATED, DRILLED AND IN STALLED A REPLACEMENT FLOOR PANEL IAW B737 900 SRM 51 10 02 PG 9. 2 L 7 4 4F RT A16WE 2008050800246 20080508 00246 NM 2008 5 8 ASAA0892899 1 20080414 A 5320 146A750218AND22 ANGLE BOEING 737 737990 NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 318AS 30018 AFT CARGO RT FLOOR TO SIDEWALL TRANSITION ANGLE MULTIPLE AREAS OF CORROSION STA 727 787. REMOVED DAMAGED SECTIONS, FABR ICATED A REPLACEMENT TRANSITION ANGLES SPLICES REPAIR PARTS, LOCATED, DRILLED AND INSTALLED IAW B737 900 SRM 53 00 53 PG 202 REPAIR 5. 2 L 7 4 4F RT A16WE 2008050800251 20080508 00251 NM 2008 5 8 ASAA0892904 1 20080411 A 5330 147A321214 SKIN BOEING 737 737990 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 318AS 30018 UPON FURTHER EVALUATION OF PLT G239695 FOUND EXTERNAL FUSELAGE SKIN DENT STA 381 JUST BELOW STR 17L TO BE CREASED IN DEN T. CUT OUT DAMAGED AREA, HFEC INSPECTED AREA, NO DEFECTS NOTED. FABRICATED DOUBLER, LOCATED DRILLED AND INSTALLED IAW ASA EA 5330 02335 AAR EA 12628 AND B737 900 SRM 53 00 01 REPAIR 3. 2 L 7 4 4F RT A16WE 2008050900003 20080509 00003 NM 2008 5 9 F3LA200800238 1 20080501 A 5320 D5391379020002 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED FORWARD CARGO LATERAL FLOORBOARD SUPPORT PROFILE AT FRAME 28 FROM STRINGER 38 LEFT TO 38 RIGHT HAS CORROSION AROUND SEVERAL NUT PLATE HOLES. MAINTENANCE BLENDED CORROSION AROUND SEVERAL NUT PLATE HOLES ON FLOORBOARD SUPPORT PROFILE AT FRAME 28 FROM STRINGER 38 LEFT TO 38 RIGHT. MAINTENANCE REMOVED FLOORBOARD SUPPORT AN D REPLACED IT WITH NEW FLOORBOARD SUPPORT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-00, SRM 53-00-14, SRM 53-00-0 0, SRM 53-74-00, SRM 53-21-14 AND SRM 51-44-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050900007 20080509 00007 NM 2008 5 9 F3LA200800228 1 20080501 A 5320 D53911609200 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 REFERENCE NON ROUTINE 31546. DURING C3 S1 C CHECK INSPECTION NOTED THE FORWARD CARGO LEFT FLOOR SUPPORT PROFILE AT STRIN GER 38 LEFT FROM FRAME 24A TO 28 HAS CORROSION AROUND SEVERAL NUT PLATE HOLES. MAINTENANCE REMOVED CORRODED PROFILE AND REPLACED WITH NEW FABRICATED PROFILE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11. UPON COMPLETION OF THE REPAI R IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050900018 20080509 00018 NM 2008 5 9 F3LA200800232 1 20080501 A 5320 D5347112420100 SHEAR PLATE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED CORROSION ON PLATE RIGHT SIDE OF AIRCRAFT MOST OUTBOARD BETWEEN FRAMES 69 AND 70. MAINTENANCE REMOVED DOUBLER STANDOFF BRACKET AND WIRE HARNESS, REMOVED AND REPLACED CORRODED SHEAR PLATE AND REINSTALLE D DOUBLER AND STANDOFF BRACKET AND REINSTALLED WIRE HARNESS IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11, SRM 51- 42-11 AND AMM 20-33-42. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050900020 20080509 00020 NM 2008 5 9 F3LA200800239 1 20080501 A 5210 D5311318520000 BEARING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE LT PAX DOOR SEIZED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED LEFT AFT ENTRY DOOR UPPER LATCH HOOK BEARING WAS SEIZED. MAINTENANCE LUBED AND CL EANED, ROLLER MOVED FREELY IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 12-22-52. UPON COMPLETION OF THE REPAIR IT WAS IN SPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080519 NM 2008 5 19 AALA200800858 1 20080407 A 3397 CONNECTOR BOEING 777 777223 1385213 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. REPAIRED LOOSE CONNECTION FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 NM 2008 5 19 QXEA200800451 1 20080507 A 5230 502213 SEAL BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR LOOSE A QXEA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 NM 09 414QX 4061 PDX- FLIGHT 2459 (SEA-STS) - EN ROUTE RECEIVED A CABIN PRESSURE CAUTION LIGHT. FLIGHT ATTENDANT REPORTED A LOUD NOISE F ROM THE REAR PASSENGER DOOR. NO EMERGENCY DECLARED. DIVERTED INTO PDX. ACCOMPLISHED UNEVENTFUL LANDING. MAINTENANCE FOUND THE AFT BAGGAGE DOOR SEAL TO BE LOOSE. REPLACED THE SEAL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 20080519 EU 2008 5 19 08FDEA01805 1 20080508 A 5230 A5237204320000 SKIN AIRBUS 310 A310324 3930206 EU CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 FWD CARGO PIT DOOR LOWER EXTERNAL SKIN PLATE IS CORRODED IN NUMEROUS PLACES. REMOVED AND REPLACED THE FWD CARGO DOOR LO WER EXTERNAL SKIN PLATE IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080519 NM 2008 5 19 AALA200800916 1 20080410 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 756AM 30264 DFW - EMERGENCY LIGHTS AT OVERHEAD LEFT BUSINESS CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERH EAD LEFT BUSINESS CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 NM 2008 5 19 AALA200800918 1 20080410 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 756AM 30264 DFW - EMERGENCY LIGHT AT BUSINESS CLASS LAVATORY INOPERATIVE. REPLACED BATTERY PACK M33097 FOR EMERGENCY LIGHT AT BUSIN ESS CLASS LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 EU 2008 5 19 08FDEA01825 1 20080512 A 5415 ATTACH FITTING AIRBUS 310 A310324 3930206 EU NR 2 PYLON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 NR 2 PYLON AFT LOWER FAIRING PANEL NR 485 AL, FWD UPPER LT ATTACH PLATE IS CHAFED ON THE INNER SURFACE. REMOVED CHAFED ATTACH PLATE & INSTALLED A NEW ATTACH PLATE PER SRM 51-40-21 PARA 6. LOCATED & DRILLED PER SRM 51-40-44. ALODINED PE R AMM 51-23-10-0. 2 L 7 2 4F RT A35EU 20080519 EU 2008 5 19 551008N218CA 1 20080510 A 7997 MS3126F1210S CONNECTOR JAEGER AMD FALCON FALCON20 2730103 EU GE CF700 CF7002D2 30010 NE COCKPIT BURNED E CEDA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 05 218CA 218 304404B SMALL AMOUNT OF SMOKE NOTICED IN COCKPIT. 2 L 7 2 4F 4 F RT A7EU E7EA 20080519 NM 2008 5 19 DLM88080696 1 20080509 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 960DL 49979 GOUGE ON FUSELAGE SKIN AT STA 237 BTW LONG 17 LT AND 18 LT. REPAIRED PER SRM 53-04D. 2 L 7 2 4F RT A6WE 20080519 WP 2008 5 19 AALA200801006 1 20080418 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 982TW 53632 LGA - EMERGENCY LIGHTS AT SEAT ROWS 7 TO 2O INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 7 TO 2 0. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 AALA200800996 1 20080417 A 4920 APU BOEING 757 757223 1384957 NM LEAKING A AALA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 688AA 25730 LAX INFLIGHT T285/17APR - CREW REPORTED STRONG ELECTRICAL SMELL IN AFT CABIN FOLLOWED BY SMOKE ALARM SOUNDING IN AFT LAV ATORY. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. FOUND OIL IN APU AIR DISCHARGE DUCT. REPLACED APU DUE TO OIL LEAK . ACCOMPLISHED CONTAMINATION REMOVAL. REPLACED AIR CYCLE MACHINES AND PRIMARY AND SECONDARY HEAT EXCHANGERS. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080519 NM 2008 5 19 2008UALA02487 1 20080425 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 DOOR 3R SLIDE LIGHT WILL NOT COME ON AFTER ARMING. FOUND SLIDER OUT OF ADJUSTMENT ADJUSTED SLIDER ASSY ON AFT END OF GIR T BAR, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080519 NM 2008 5 19 2008UALA02484 1 20080427 A 3150 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ELEVATOR WARNING MESSAGE A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 546UA 25367 ELEVATOR ASYMMETRY EICAS STATUS MESSAGE DISPLAYED. PERFORMED T-S PER FIM 27-0 9-00 FIG 106, AND OPS CHK PER MM 27-31-00 . ALL CHK'D NORMAL NO ECIAS MESSAGES NOTED. NO REPEATS SINCE INCIDENT. 2 L 7 2 4F 4 F RT A2NM E17NE 20080519 2008 5 19 AALA200801004 4 20080418 A 3140 AGS31311 CIRCUIT CARD BOEING 777 777223 1385213 NM E&E BAY NOT SEATED A AALA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 767AJ 33539 ANC INFLIGHT T61/18APR DFW TO NRT - CREW REPORTED MULTIPLE EICAS STATUS MESSAGES. LANDED ANC WITHOUT INCIDENT. FOUND L EFT SYSTEM CARD FILE ARINC SIGNAL GATEWAY INACTIVE. RESEATED CARDS AND RELOADED SOFTWARE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 EA 2008 5 19 MASA200800338 1 20080423 A 2150 GG670950091 ACM CNDAIR CL600 CL6002D24 1390016 EA A/C BAY FAILED A MASA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 07 918FJ 173 150018 ASH FLT 2677 RIC-CLT - RT PACK AUTO FAIL WITH FUMES IN CABIN AND FWD LAV SMOKE WARNING. REPLACED NR 2 ACM, OPS CHECK GO OD. 2 L 7 2 4F RT A21EA 20080519 WP 2008 5 19 UPS08852178 1 20080501 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 810UP 46001 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-00. OPS CHECKED OK. 2 L 7 4 4F RT 4A25 20080519 NM 2008 5 19 UPS08M52152 1 20080216 A 5313 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C CTR CARGO BILGE AREA STA 1541 LONGERON R48 FOUND WITH CORROSION AS MARKED (DECAL 7932) LONGERON CORROS ION REMOVED FOUND EXCEED LIMIT PER SRM 53-10-00 FIG 2A V OL1R.40 MATL REMOVED .118" ORIG THK:0.150". EXISTING SKIN STRA P REMOVED FR STA 5-93-1620 L48 RT PER SRM 51-31-01V.2R.40. LONG SPLICES 3 INSTALLED STA 5-93-1541 L48 RT PER SRM 51-33- 01 V.2R.40. EXISTING SKIN STRAP INSTALLED FROM STA 5-93-1620 L48 RT PER SRM 51-31-01 V.2R.40. 2 L 7 3 4F RT A22WE 20080519 NM 2008 5 19 UPS08M52162 1 20080325 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C CABIN SEAT TRACK AT STA 859 - 919 X=+8.5 FOUND CORROSION. CORROSION ON AFFECTED AREA REMOVED MAT'L TH K: 0.080" (FLANGE), MAT'L REMOVED: 0.050", MAT'L REMN: 0.030 INCH (STA 880) FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK A T STA 849 AND STA929 X=+8.5 TRIM OUT. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. NEW SEAT TRACK AND 01 SP LICE HAT SECT REWORKED. NEW SEAT TRACK AND REPAIR PARTS INSTALLED PER SRM 53-70-00 FIG 1 VIR35. 2 L 7 3 4F RT A22WE 20080519 NM 2008 5 19 UPS08M52163 1 20080418 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C AFT CABIN, CORROSION ON SEAT TRACK CROWN AND CHANNEL AT STA 1761 - 1781 X=-27.5. CORROSION ON AFFECTE D AREA REMOVED. MAT'L THK: 0.145 INCH (CROWN), MAT'L REMOVED 0.030 INCH (STA1767), MAT'L REMAINING: 0.115 INCH, FOUND O UT OF LIMIT. DISCREPANT SEAT TRACK AT STA1731 X=-27.5 TRIM OUT. HFEC INSP C/O ON TRIM OUT AREA, FOUND ON CRACK EVIDEN T. NEW SEAT TRACK AND 01 EA SPLICE HAT SECT REWORKED. ONE SPLICE PLATE FAB, NEW SEAT TRACK AND REPAIR PARTS INSTALLED PER SRM 53-70-00F1 VIR 35. 2 L 7 3 4F RT A22WE 20080519 NM 2008 5 19 UPS08M52173 1 20080320 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C CABIN CORROSION ON SEAT TRACK CROWN AND FLANGE AT STA 824-865 X=-27. CORROSION ON AFFECTED AREA REMOV ED. MATL THK:0.145 INCH (CROWN), MATL REMVD:0.060" (STA 859-861), MATL REMAINED:0.085 INCH FOUND OUT OF LIMIT. DISCREP ANT SEAT TRACK REMOVED SEAT TRACK FROM STA 781-869 X=-27 REWORKED. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDE NT, NEW SEAT TRACK ON EXISTING SPLICE HAT-SECTION LOCATION FROM STA 781 TO 869 X=-27 INSTALLED PER SRM 51-31-01VIIR35. 2 L 7 3 4F RT A22WE 20080519 EA 2008 5 19 MASA200800378 1 20080507 A 2560 90905A654 D-RING CNDAIR CL600 CL6002D24 1390016 EA ESCAPE ROPE MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 956LR 15056 ASH FLT 2872 PHX-SAT - D-RING FOR EMERGENCY ROPE LT WING FWD MISSING. MX REPLACED MISSING D-RING. 2 L 7 2 4F RT A21EA 20080519 EA 2008 5 19 MASA200800382 1 20080506 A 7603 2100140007 GEARBOX CNDAIR CL600 CL6002B19 1900309 EA THROTTLE WORN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 693BR 15911 7761 FOUND WEAR ON THE ENGINE THROTTLE CONTROL GEARBOX, WEAR GREATER THAT .010 INCH. REMOVED AND REPLACED NR 1 ENGINE THROTT LE CONTROL GEARBOX. 2 L 7 2 4F RT A21EA 20080519 NM 2008 5 19 KCSA081236 1 20080508 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 SMALL AREA OF DAMAGE ON FUSELAGE BELLY SKIN AT BS 610, LBL-2. 2 L 7 4 4F RT A20WE 20080519 NM 2008 5 19 KCSA081237 1 20080508 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 SMALL AREA OF DAMAGE ON FUSELAGE BELLY SKIN AT BS 647, RBL-2 2 L 7 4 4F RT A20WE 20080519 EA 2008 5 19 MASA200800384 1 20080508 A 2560 P2070011500 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77278 7278 ASH FLT 1930 LIH-HNL (RON) - F/O EMERGENCY FLASHLIGHT IS INOP. REPLACED FLASHLIGHT. 2 L 7 2 4F RT A21EA 20080519 NM 2008 5 19 KCSA081239 1 20080513 A 5311 STRAP BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 AFT BILGE FUSELAGE FRAME STABILIZER STRAP IS CRACKED AT STA 2050, RBL 66. 2 L 7 4 4F RT A20WE 20080519 EA 2008 5 19 MASA200800387 1 20080509 A 2560 MS295231 HOOK CNDAIR CL600 CL6002D24 1390016 EA ESCAPE ROPE MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 929FJ 15029 ASH FLT 2892 LAS - AUS RIGHT SIDE EMERGENCY EXIT DOOR ROPE HOOK-CLIP MISSING. MX REPLACED HOOK-CLIP. 2 L 7 2 4F RT A21EA 20080520 WP 2008 5 20 ABXR080144 1 20080416 A 5311 S277799223 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 231US 48114 LONGERON 25 LEFT HAD CRACK INDICATIONS AT BOTH ATTACH FASTENERS TO FRAME AT FS 160. REMOVED AND REPLACED DAMAGED SECTIO N IAW DC9 SRM. 2 L 7 2 4F A6WE 20080520 WP 2008 5 20 ABXA080147 1 20080418 A 5315 992348487 FLOORBEAM DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 FLOORBEAM CRACKED ON BOTH SIDES OF INTERCOSTAL AT STA 180, LEFT BUTT LINE 20. REPAIRED IAW DC9 SRM 53-05. 2 L 7 2 4F A6WE 20080520 WP 2008 5 20 ABXA080146 1 20080415 A 5210 591412157 PAN DOUG DC9 DC941 302207N WP MAIN ENTRY DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 MAIN ENTRY DOOR SWITCH STRIKER BRACKET LOWER ATTACH HOLE HAD A 3/8 INCH CRACK COMING FROM HOLE (MED PAN). REPAIRED AREA IAW DC9 SRM 52-03. 2 L 7 2 4F A6WE 20080520 EU 2008 5 20 UPS08152205 1 20080508 A 3233 ACTUATOR AIRBUS A300 A300F4622R 3930360 EU RT MLG MALFUNCTIONED A IPXA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 142UP 0825 AFTER T/O RIGHT GEAR DID NOT RETRACT, RT GEAR DOOR STAYED OPEN CONFIRMED BY BDL TOWER. ONCE LANDING GEAR HANDLE WAS LOW ERED, GOT 3 DOWN AND LOCKED AND ECAM LANDING GEAR RETRACTION INOP. REMOVED AND REPLACED BRACE STRUT ACTUATING CYLINDER IAW MM 32-31-55-04. LANDING GEAR OPS AND LEAK CHECKS C/W IAW MM 32-31-00. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 20080520 NM 2008 5 20 UPS08652187 1 20080429 A 5320 146T56516 SPLICE BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 329UP 27755 INSPECTION TYPE:C AFT OF BULK CARGO MAIN DECK FLOOR SUPPORT ATT SPLICE ANGLE CRACK, CRACK LENGTH 1.25 INCH. AFT OF BULK CARGO MAIN DECK FLOOR SUPPORT ATTACH SPLICE ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20080520 2008 5 20 MASA200800395 4 20080512 A 3140 8221310104 DCU CNDAIR CL600 CL6002C10 1390015 EA NR 2 MALFUNCTIONED A MASA O OTHER O OTHER CR CRUISE 1 SW 07 518LR 4399 10259 ASH 7257 IAD IAD-MHT - SEVERAL EICAS MESSAGES, DECLARED EMERGENCY AND RETURNED TO IAD. REMOVED AND REPLACED NR 2 DCU, O PS GOOD. 2 L 7 2 4F RT A21EA 20080520 EU 2008 5 20 08FDEA01734 1 20080502 A 5320 A5361221420001 INTERCOSTAL AIRBUS 300 A300B4605R 3930308 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 THE MAIN CABIN INTERCOSTAL AT FRAME 13 LBL 35 IS CORRODED ON THE UPPER SURFACE. REMOVED CORROSION IAW SRM 51-73-10 PG 20 9 ITEM 5. ORIGINAL MATERIAL THICKNESS IS 0.079 IAW SRM 53-12-15 CONFIG 2 PG 4-2 (B). REMAINING THICKNESS IS 0.050. FOU ND TO BE OUT LF LIMITS IAW SRM 53-12-11 PGS 107-108. REMOVED SUPPORT IAW SRM 51-40-21 PG 7. LOCATED, DRILLED & DEBUR RED THE NEW SUPPORT IAW DWG A53612214. INSTALLED IAW SRM 51-40-21 PGS 7 & 24. 2 L 7 2 4F RT A35EU 20080520 WP 2008 5 20 08FDEA01731 1 20080502 A 5730 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 RIGHT WING FIXED LEADING EDGE CAVITY UPPER SKIN DOUBLER IS CRACKED AT STA XFS 669, OUTBD OF THE NR 10 SLAT TRACK. FABRI CATED A REPAIR DOUBLER IAW SRM 57-10-00; FIG 71; VOL I. PRIMED REPAIR DOUBLER IAW SRM 51-21-01; VOL II AND 51-35-01 ; VOL II. 2 L 7 3 4F RT A22WE 20080520 EU 2008 5 20 08FDEA01844 1 20080514 A 5720 A57111092202 FITTING AIRBUS 300 A300B4622R 3930312 EU CENTER WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND ON SEVERAL HOLES IN CENTER WING BOX LOWER JUNCTION HORIZONTAL FLANGE C 47 WITH DAMAGE AND CRACKS (HOLE A, D, E, G ). REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL DAMAGE REMOVAL AND INSTALLING BUSHINGS, APPROVED BY RAS/70503969/045 /2008 ISS A AND EA 6-5710-117142. 2 L 7 2 4F RT A35EU 20080520 WP 2008 5 20 08FDEA01727 1 20080502 A 5410 ASL00401 ADAPTER DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 1 ENGINE OUTBD CORE COWL L/E RUB STRIP IS WORN IN SEVERAL AREAS. BLENDED WORN AREAS. MATERIAL LOSS 0.065. FOUND TO BE OUT OF LIMITS IAW AMM 71-13-01-02 & DWG S2929517. REMOVED & REPLACED RUB STRIP ASL 0040-1. IAW SRM 51-35-01; VOL II & DWG ASL 0040 REV "NC". 2 L 7 3 4F RT A22WE 20080520 WP 2008 5 20 08FDEA01847 1 20080514 A 5753 ARC274624 SKIN DOUG MD10 MD1010F 3022112 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 RIGHT WING INBD FLAP; INBD UPPER AFT SKIN IS CORRODED. REMOVED AND REPLACED THE SKIN IAW DC/MD-10 SRM 51-35-01; VOL II. FABRICATED NEW PANEL IAW DAC DWG NR ARC 2746, REV Z. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-08. PART MARKED P/N FX-ARC 2746-24 IAW FEDEX GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20080520 EU 2008 5 20 08FDEA01849 1 20080514 A 5320 A53781041200 CROSSBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 658FE 752 CROSSBEAM FR 60 HAS 1 INCH CRACK ON VERTICAL FLANGE OUTBD OF SEAT TRACK 3 RT, - Y1456 REMOVED CRACK AND INSTALLED CROSS BEAM REPAIR IAW A300-600 SRM 53-10-15, FIG 211. 2 L 7 2 4F RT A35EU 20080520 NM 2008 5 20 KCSA081240 1 20080515 A 5347 STIFFENER BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 FORWARD BILGE SEAT TRACK STIFFENER IS DAMAGED AT STA 585, LBL 25. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 KCSA081241 1 20080515 A 5311 STIFFENER BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 FUSELAGE FRAME STIFFENER IS DAMAGED AT STA 880, STR 39R. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800170 1 20080505 A 2150 32049581 DUMP VALVE BOEING 747 74747UF 1384812 NM NR 1 PACK FAILED A UIEA I G B A CABIN DEPRESSURIZATION O2 MASK DEPLOYED EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 499MC 29260 LOUD BANG FOLLOWED BY RAPID RISE IN CABIN ALTITUDE WITH "CABIN ALT" EICAS MESSAGE. FOUND NR 1 PACK DUMP VALVE AT FAULT. DEACTIVATED VALVE IN CLOSED POSITION. TRANSFERRED TO MEL M08-058 REF MEL 21-51-10 CAT C. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800172 1 20080505 A 5320 FLOOR SUPPORT BOEING 747 7472D7B 1384803 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 UPPER DECK STA 560-580 LBL 81 OUTBOARD FLOOR SUPPORT FOUND CORROSION. LEVEL 1, CORROSION REMOVED AS PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800173 1 20080505 A 5210 SKIN BOEING 747 7472D7B 1384803 NM R4 DOOR DEFORMED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK 4R DOOR AFT LOWER CORNER EXTERNAL SKIN FOUND DEFORMED. PERFORMED EXTERNAL SKIN RE-WORK AS PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 2008051600043 20080516 00043 NM 2008 5 16 SWAA082489 1 20080506 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 752SW 29804 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 2008051600054 20080516 00054 NM 2008 5 16 SWAA082517 1 20080507 A 5310 6546818 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 867 TO BS 887, RBL 70. REMOVED AND REPLACED WEB PER S RM. 2 L 7 2 4F RT A16WE 2008051600055 20080516 00055 NM 2008 5 16 SWAA082516 1 20080507 A 5310 6546818 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 727C TO BS 727D, RBL 70. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082505 1 20080507 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 432WN 33715 DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EEPLS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082506 1 20080507 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082594 1 20080512 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 707, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082595 1 20080512 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082578 1 20080512 A 5743 655223535 BEAM BOEING 737 7373Q8 1384670 NM RT WING WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 22Y CHECK, FOUND RIGHT MLG FWD STABILIZER LUG WORN. REMOVED AND REPLACED RIGHT MLG STABILIZER BEAM PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 2008UALA02495 1 20080428 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 303 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 CABIN FLOORBEAM UPPER SURFACE CORRODED, BS 303, RBL 54. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF "T" CAP. INSTALLED "T" CAP AND ANGLE REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20080519 NM 2008 5 19 UPS08M52134 1 20080222 A 5313 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C CTR CARGO COMPT BILGE AREA BETWEEN STA 1781 AND STA 1801 AT RT LONGERON 45 FOUND SUSPECTED CRACK. HFE C INSP C/OUT IAW DAC NDT SPM R.13 PART06-10-01.001 AND CRACK CONFIRM APPROX 1 1/4 INCH. CRACKED LONG REMOVED FR STA 167 1-1811 L45 RT PER SRM51-31- 01V.2R.40. NEW LONGERON AFA7097-501 HOLES PICKED UP PER SRM 51-31-01V.2 R.40A AND REPROTECT ED PER SRM 51-21-01V.2R.40. NEW LONG AFA7097-501. INSTALLED FR STA1671-1811 L45 RT PER SRM 51-31-01V.2R.40. 2 L 7 3 4F RT A22WE 20080519 NM 2008 5 19 UPS08M52135 1 20080325 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C CABIN SEAT TRACK AT STA 929 - 979 X=+8.5, FOUND CORROSION. CORROSION ON SEAT TRACK AT AFFECTED AREA R EMOVED MAT'L THK: 0.100"(BASE) MAT'L REMOVED: 0.040", MAT'L REMN: 0.060"(STA959), FOUND OUT OF LIMIT. DISCREPANT SEAT T RACK AT STA 929-989 X=+8.5 TRIM OUT. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. NEW SEAT TRACK AND 2 SPLI CE HAT SECTION REWORKED. TWO SPLICE PLATES FAB NEW SEAT TRACK FROM STA 929-979, X=+8.5 INSTALLED. 2 L 7 3 4F RT A22WE 20080519 WP 2008 5 19 NWAA081909927 1 20080502 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8920E 45835 DURING LINE CHECK MAINTENANCE FOUND THE EMERGENCY PATHWAY LIGHTING IN THE FIRST SIX ROWS OF COACH SEATS IN THE CABIN HAD FAILED. MAINTENANCE REPLACED THE APPLICABLE BATTERIES FOR THE EPSU. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F A6WE 20080519 EA 2008 5 19 MALA080077 1 20080415 A 2697 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA SMOKE DETECTOR DIRTY A MALA K NONE N FALSE WARNING DE DESCENT 1 GL 15 602XJ 8044 CARGO SMOKE EICAS AND AURAL WARNING MOMENTARILY INDICATED DURING ARRIVAL INTO CPR, TEN MINUTES BEFORE LANDING. NO OTHER INDICATIONS FOLLOWED, REMOVED AND CLEANED CONNECTORS ON NR 1 AND NR 2 CARGO SMOKE DETECTORS. COMPLETED OPERATIONAL TES T OF CARGO SMOKE DETECTORS PER TASK 26-15-00, PAGE 501. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 20080519 NM 2008 5 19 AALA200800837 1 20080407 A 3350 HOUSING BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 786AN 30250 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET AREA DAMAGED. REPLACED HOUSING FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 NM 2008 5 19 08FDEA01766 1 20080506 A 5311 AFA00183 FRAME DOUG MD11 MD11 3023602 NM FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 528FE 48623 CABIN : AFT CABIN AT APPROXIMATELY STATION 1741 LT LONGERON 12 FOUND FRAME DENTED. REPAIRED PER SRM 53-30-00 FIG.1, VOL .I. REPETITIVE INSPECTION REQUIRED, INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO B E CARRIED OUT AS PER SRM 53-30-00, FIG.1, VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080519 NM 2008 5 19 DLM90080665 1 20080424 A 5320 9940443 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 FOUND RIGHT CUSP WEB CORRODED ON SURFACE BETWEEN STA 636-655. REMOVED AND REPLACED RIGHT CUSP WEB BETWEEN STA 636-655, IAW MD90 SRM 51-10-05. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 08FDEA01785 1 20080507 A 5310 ACA73511 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 628FE 48447 MAIN DECK INTERIOR FUSELAGE AT LEFT STA 535 FRAME, LOWER SUPPORT YOKE, FOUND DAMAGED. REPAIRED AS PER DRAWING SRZ-53-503 . REPAIR CLASSIFIED AS MINOR PER GMM 6-2- 100. 2 L 7 3 4F RT A22WE 20080519 NM 2008 5 19 AALA200800919 1 20080410 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 756AM 30264 DFW - EMERGENCY LIGHT AT BUSINESS CLASS LAVATORY INOPERATIVE. REPLACED BATTERY PACK M33096 FOR EMERGENCY LIGHT AT BUSIN ESS CLASS LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 EA 2008 5 19 MASA200800362 1 20080502 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA O OTHER O OTHER CR CRUISE 1 SW 07 87353 5005 7353 ASH FLT 1024 KOA-HNL - NLG DISAGREE. AIRCRAFT DECLARED EMERGENCY. REMOVED AND REPLACED PRIORITY VALVE, OPS GOOD. 2 L 7 2 4F RT A21EA 20080519 EA 2008 5 19 MASA200800364 1 20080502 A 2510 TRACK CNDAIR CL600 CL6002B19 1900309 EA F/A SEAT DIRTY A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 17275 7275 ASH FLT 2752 PHX- SBP - FA SEAT HARD TO OPEN AND CLOSE. MAINTENANCE CLEANED AND LUBED THE SEAT TRACKS, OPS NORMAL. 2 L 7 2 4F RT A21EA 2008050900022 20080509 00022 NM 2008 5 9 F3LA200800208 1 20080501 A 5320 D5367225400000 PANEL AIRBUS A319 A319111 3930336 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED FWD CARGO LEFT SIDE PANEL 131EG PANEL RACK DAMAGED. MAINTENANCE CLEANED AND PREPP ED AREA IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 8C AND APPLIED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-02. TREATED, PRIMED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-75-12. UPON COMPLETION OF THE REPAIR IT W AS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E2GL 2008050900029 20080509 00029 NM 2008 5 9 2008UALA02581 1 20080503 A 5310 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD GALLEY DOOR, LOWER HINGE CUTOUT CRACKED IN TWO PLACES. MAJOR REPAIR ACCOMPLISHED, CRACK DAMAGES WERE CONTAINED AND REPAIR DOUBLER WITH FILLERS WAS INSTALLED. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900033 20080509 00033 NM 2008 5 9 2008UALA02587 1 20080502 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ROW 15 FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 327UA 24147 EEL LIGHTS FROM ROW 15 ON BACK DO NOT ILLUMINATE. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900035 20080509 00035 NM 2008 5 9 2008UALA02589 1 20080502 A 2612 CONTROL PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FIRE DETECTION NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 341UA 24245 AFT PIT A DET LIGHT DOES NOT ILLUMINATE WITH CARGO SYS FIRE TEST OR LIGHTS TEST. REPLACED FIRE TEST CONTROL PANEL, CHEC KS NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900043 20080509 00043 NM 2008 5 9 2008UALA02597 1 20080504 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR CUT OUT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 L-2 DOOR UPPER HINGE ARM CUT-OUT IS OUT-OF-TOLERANCE. INSTALLED NEW DOUBLER-L-2 DOOR UPPER HINGE ARM CUT-OUT REQUIRES D OUBLER PER MM 52-11-87, ACCOMPLISHED HFEC INSP AND FOUND .25 " CRACK AT AFT LOWER CORNER. 2 L 7 2 4F 4 F RT A2NM E17NE 2008050900045 20080509 00045 NM 2008 5 9 2008UALA02599 1 20080503 A 3510 MC1025154 OXYGEN MASK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CAPTAIN'S FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 CAPTAIN O2 MASK LINES ARE FRAYED. REPLACED CAPTAINS O2 MASK REF MM 25-11-11 PG 201 OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900047 20080509 00047 NM 2008 5 9 2008UALA02601 1 20080504 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 727D CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 AFT CARGO PIT AREA AROUND NR 3 VHF ANTENNA CUT-OUT AT BS 727D +10" IS CORRODED BETWEEN STRINGERS S-27L AND S- 27R AT BL0 AND WL148. MAJOR REPAIR ACCOMPLISHED, REPLACED VHF ANTENNA SUPPORT CHANNEL. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900052 20080509 00052 NM 2008 5 9 2008UALA02606 1 20080502 A 5347 SEAT TRACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 784-800 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 MAIN CABIN SEAT TRACK AT STA 784 TO STA 800, LBL 60 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED, CUT OUT DAMAGED SECTION O F SEAT TRACK. INSTALLED NEW SECTION. 2 L 7 2 4F 4 F RT A1NM E24NE 2008050900055 20080509 00055 NM 2008 5 9 2008UALA02609 1 20080502 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1500 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 AFT PIT BS 1500 BETWEEN STRS 26L AND 25L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED, CUTOUT DAMAGE AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008050900059 20080509 00059 NE 2008 5 9 2008UALA02614 2 20080504 A 7200 50B927 BEARING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 ENGINE MAKING METAL A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 222001 METAL DEBRIS FOUND ON NR 2 ENG MAGNETIC CHIP DETECTOR. SEM CONFIRMED BEARING MATERIAL. A/C FERRIED TO SFO FOR ENGINE CH ANGE. ENGINE REPLACED AT SFO ON 5/4/08. SHOP TEARDOWN REVEALED THAT THE NR 1 BEARING HAD ONE BALL WITH A LARGE AREA OF SPALLATION, AND ITS CAGE POCKET ALSO HAD DAMAGE. THERE WAS NO DAMAGE TO THE INNER AND OUTER RACES. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008050900065 20080509 00065 NM 2008 5 9 2008UALA02620 1 20080504 A 2530 CONTROL UNIT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GALLEY POWER FAILED A UALA O OTHER O OTHER CL CLIMB 1 WP 29 597UA 28750 LOST AFT GALLEY POWER ON CLIMB-OUT. THIS ISSUE WAS VERY DIFFICULT TO DIAGNOSE AND REQUIRED THREE WEEKS OF CONSTANT TROU BLESHOOTING. AFTER ALL WIRES WERE HAND OVER HAND CHECKED AND FOUND NORMAL, K1 AND K2 RELAYS WERE CHANGED, BUSS TIE BREA KERS WERE ALSO CHANGED- IT WAS FOUND THAT CHANGING THE ELCU WAS THE FINAL FIX. 2 L 7 2 4F 4 F RT A2NM E17NE 2008050900066 20080509 00066 NM 2008 5 9 2008UALA02621 1 20080504 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 3A MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 193UA 26890 FOUND SEAT 3A MISSING EEL LIGHT ON SIDE OF SEAT. REPLACED EEL LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 2008050900074 20080509 00074 EU 2008 5 9 2008UALA02629 1 20080506 A 5610 WINDOW AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT FAILED A UALA O OTHER C F.O.D. AP APPROACH 1 WP 29 437UA 655 ON APPROACH AT ABOUT 5000 FT, BIRD STRIKE ON F/O SIDE WINDOW. WINDOW CRACKED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050900076 20080509 00076 NM 2008 5 9 F3LA200800222 1 20080501 A 5320 D5391550320001 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED FORWARD CARGO AFT FLOORBOARD PARTITION AND PARTITION WALL SUPPORT ANGLE PROFILE JU ST FORWARD OF FRAME 34 FROM STRINGER 38 LEFT TO STRINGER 38 RIGHT HAS CORROSION AROUND SEVERAL NUT PLATES. MAINTENANCE REMOVED AFT FLOORBOARD PARTITION WALL SUPPORT ANGLE PROFILE FORWARD OF HOLES FRAME 34 FROM STRINGER 38 LEFT TO STRINGER 38 RIGHT AND LOCATED AND LAYOUT AND INSTALLED NEW SUPPORT ANGLE PROFILE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-44 -11, SRM 51-61-11, SRM 53-21-14, SRM 51-72-11 AND SRM 51-40-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUN D ACCEPTABLE. 2 L 7 2 4F RT A28NM 2008050900081 20080509 00081 NM 2008 5 9 HALA0800561 1 20080424 A 5347 SEAT TRACK BOEING 767 7673CB 1385187 NM BS 911 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 588HA 33422 CORROSION ON BOTH TRACK FITTINGS WHERE FEET OF STA 911 PARTITION ATTACH TO FLOOR, LBL, RBL. BOTH TRACK FITTINGS REPLACE D IAW 767-300 SRM 51-40-02 REV 76 AND DWR 145T522Z. 2 L 7 2 4F RT A1NM 2008050900089 20080509 00089 EU 2008 5 9 2008UALA02637 1 20080505 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 444UA 824 FLOORBEAM JUST INBD OF AFT LT MED IS CORRODED. MAJOR REPAIR ACCOMPLISHED: REPLACED FLOORBEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 2008050900095 20080509 00095 EU 2008 5 9 08FDEA01788 1 20080507 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 FOUND THE FLANGE CRACKED ON THE DUMMY SEAT TRACK LEFT NR 3 AT FRAME 38.1 TO FRAME 40. REMOVED AND REPLACED THE TRACK A5 327400500053, PO NR 617643.1. LOCATED AND DRILLED THE NEW TRACK IAW A300-600 SRM 51-40-44, PG 16. INSTALLED NEW TRACK IAW A300-600 SRM 51-40-21, PG 7. REMOVAL ACCOMPLISHED ON WRI NR 53100540. 2 L 7 2 4F RT A35EU 2008050900101 20080509 00101 WP 2008 5 9 UPS08852157 1 20080424 A 5712 RIB DOUG DC8 DC873F 302199F WP RWS 320 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 RT WING CENTER LE LOWER RIB DOUBLER CRACKED AT XFS320. REPAIRED RT WING CENTER LE LOWER RIB AT XFS32 0 IAW SRM 57-03-03-0 AND SRM 57-02-00-0 FIG 002. 2 L 7 4 4F RT 4A25 2008050900105 20080509 00105 NM 2008 5 9 2008UALA02643 1 20080504 A 3510 MC1025154 OXYGEN MASK BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE 1ST OFFICER'S FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 FO O2 MASK HISSES, LEAKS WHEN DONNED. REPLACED FIRST OFFICERS O2 MASK PER MM 35-12-86. OP CHECKED GOOD. AC OK FOR SER VICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008050900108 20080509 00108 NM 2008 5 9 AALA200800867 1 20080408 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 610AA 24486 BOS - EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 26D. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008050900113 20080509 00113 NM 2008 5 9 AALA200800874 1 20080408 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW - EMERGENCY LIGHT AT SEAT 38G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 38G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008050900102 20080509 00102 WP 2008 5 9 UPS08852158 1 20080424 A 5712 RIB DOUG DC8 DC873F 302199F WP RWS 326 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 RT WING CENTER LE LOWER RIB CRACKED AT XFS 326. REPAIRED RT WING CENTER LE LOWER RIB AT XFS 326 IAW SRM 57-03-03-0 AND SRM 57-02-00-0 FIG 002. 2 L 7 4 4F RT 4A25 200805131 20080513 1 NM 2008 5 13 08FDEA01789 1 20080507 A 5340 66124343 STRINGER CLIP BOEING 727 727232 1384082 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 ORIGINAL LOST, A86-143 REF AD 92-12-03, AFT PIT BILGE BODY FRAME STR CLIP IS BUCKLED, CRACKED, CORRODED BS 950F, STR 27L (EO 7-5310-7-2354) N00252. REMOVED AND REPLACED STR CLIP AT AFT PIT BILGE BODY FRAME STR 27L, STA 950F, REF SRM 51-30- 2 PG 2-4 . THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 200805131 20080513 1 NM 2008 5 13 08FDEA01791 1 20080508 A 5311 ACA73511 FRAME DOUG MD11 MD11F 3023600 NM BS 535 L24L CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 528FE 48623 FORWARD CABIN LEFT SIDE 9-G NET YOKE AREA, FRAME FOUND CHAFED AT STATION 535 LONGERON 24 LEFT. REPAIRED AS PER DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 200805131 20080513 1 NM 2008 5 13 08FDEA01792 1 20080508 A 5311 ACA73511 FRAME DOUG MD11 MD11F 3023600 NM BS 535 L20L CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 528FE 48623 FORWARD CABIN AT APPROXIMATELY STATION 535 LONGERON 20 LEFT FRAME FOUND CHAFED. REPAIRED AS PER DRAWING SRZ-53-503. REP AIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 200805131 20080513 1 NM 2008 5 13 DLM90080666 1 20080425 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 465 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 109886 53393 LEFT CUSP WEB HAS CORROSION ON UPPER SURFACE AT FIRST LIGHTNING HOLE FWD OF STA. 465. REPAIRED CUSP WEB ON AAR N/R 1003 732-2600-0194 S/N 109886. 2 L 7 2 4F RT A6WE 200805131 20080513 1 NM 2008 5 13 NWAA082015804 1 20080507 A 3350 BATTERY PACK BOEING 757 757351 1384991 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 584NW 32984 BATTERY PACK M736 FAILED DURING EMERGENCY LIGHT BATTERY PACK CHECK AS PART OF A 1/2 A CHECK. MAINTENANCE REPLACED THE B ATTERY PACK AND ALL OPERATIONS CHECKED GOOD. 2 L 7 2 4F RT A2NM 200805131 20080513 1 CE 2008 5 13 1356879R0501 1 20080501 A 3213 51411022 AXLE CESSNA 402 402C 207590R CE ZONE 900 BROKEN E HYIA O OTHER O OTHER TX TAXI/GRND HDL 1 NE 01 6879R 402C0611 RIGHT MAIN GEAR AXLE BROKE ON TAXI IN. 1 L 7 2 3O A7CE 200805131 20080513 1 NM 2008 5 13 F3LA200800242 1 20080423 A 5321 D5367228000000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED AFT PIT FLOOR PANEL 151PE DAMAGED. MAINTENANCE REMOVED AND REPLACED PANEL IN ACCORDA NCE WITH THE REQUIREMENTS OF AMM 53-42-17-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 200805131 20080513 1 NM 2008 5 13 DL76S080644 1 20080429 A 5330 143T32216 SKIN BOEING 767 767332 1382001 NM FS 500 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 121DE 23435 FUSELAGE SKIN CORRODED AT S-36L LAP JOINT NEAR FS 500. DAMAGED SKIN AND TEAR STRAP CUT OUT AND REINFORCED WITH DOUBLERS . 2 L 7 2 4F RT A1NM 200805131 20080513 1 NM 2008 5 13 DL76L080651 1 20080430 A 5420 311T31571 ANGLE BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 176DN 25061 WHILE ACCOMPLISHING OPN 5281AD MTC, FOUND THE CLOSE OUT ANGLE CRACKED. CLOSE OUT ANGLE WAS REPLACED. MTC ALSO FOUND TH EY NEEDED AN ADDITIONAL WASHER UNDER THE HEAD OF THE FASTENER FOR PROPER GRIPPING. THIS WAS AUTHORIZED. ADDITIONAL INS PECTIONS WERE ACCOMPLISHED PER 01-074944-12AD. 2 L 7 2 4F RT A1NM 200805131 20080513 1 NM 2008 5 13 DL76G080656 1 20080503 A 2410 241080105 IDG BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE INOPERATIVE A DALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 27 169DZ 29689 704823 5 HRS INTO FLT AT FL330, LT GEN DRIVE LIGHT. DISCONNECTED LEFT DRIVE PER QRH. APU STARTED. APU AUTO SHUTDOWN. DIVERT ED TO FRA FOR REPAIR. REMOVED AND REPLACED IDG PER AMM, RUN ENG NR 1 ALL IND NORMAL IDG, MFG P/N 729825G. 2 L 7 2 4F 4 F RT A1NM E13NE 200805131 20080513 1 NM 2008 5 13 DLM90080667 1 20080430 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 1079-1098 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 109897 53393 LT CUSP WEB HAS CORROSION ON O/B AFGT SURFACE BETWEEN STA 1079-1098. REMOVED AND REPLACED LT CUSP WEB STA 1079-1136 LBL 44.5.TO 58, IAW MD9 SRM 51-30-02, SRM 51-30-01. 2 L 7 2 4F RT A6WE 200805131 20080513 1 NM 2008 5 13 DLM90080674 1 20080430 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 560 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 LT CUSP WEB AT STA 560 O/B SEAT TRACK HAS A HOLE IN WEB ON O/B SIDE OF TRACK BELOW CLIP NUT. REPAIRED CUSP WEB, IAW MD9 0 SRM 51-11-01, FIG 6. 2 L 7 2 4F RT A6WE 200805131 20080513 1 NM 2008 5 13 DL738080676 1 20080505 A 5210 DOOR BOEING 737 737832 13844CF NM L1 OUT OF ADJUST A DALA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SO 27 3746H 30488 RETURNED TO JFK, FWD ENTRY DOOR NOT SEATED PROPERLY AND NO PRESSURIZATION. OVERWEIGHT LANDING 165 KTS. UPON ARRIVAL FO UND L1 DOOR NOT PROPERLY FAIRED. INSPECTED DOOR PER MM CHAP 52-11-00. FWD DOOR INSP, NO DEFECTS. OPENED AND CLOSED DO OR SEVERAL TIMES. ALL CKD NORMAL. 2 L 7 2 4F RT A16WE 200805131 20080513 1 NM 2008 5 13 DL757080677 1 20080505 A 5330 146N33308 SKIN BOEING 757 757232 1384965 NM BS 1337-1382 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 690DL 27585 FUSELAGE SKIN FOUND WITH LIGHTNING STRIKES AT STA 1337, 1358, 1385 AT STR 25L. THE DAMAGE WAS CUTOUT AND REPAIR DOUBLER S WERE INSTALLED. 2 L 7 2 4F RT A2NM 200805131 20080513 1 EU 2008 5 13 AALA200800864 1 20080408 A 3230 PSEU AIRBUS 300 A300B4605R 3930308 EU MLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 8067A 510 MIA INFLIGHT T2125/08APR - NOSE AND MAIN LANDING GEAR WOULD NOT RETRACT AND GEAR HANDLE COULD NOT BE PLACED IN UP POSIT ION FROM NEUTRAL POSITION. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED THE PROXIMITY SENSOR ELECTRONICS UNIT . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 200805131 20080513 1 EU 2008 5 13 MALA080074 1 20080505 A 5312 BULKHEAD SAAB SF340 340B 7860101 EU BS 733 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 RT UPPER AFT BULKHEAD AT STA 733 CRACK FOUND. RT UPPER AFT BULKHEAD AT STA 733 REPAIRED IAW EO S53561 LPI INSPECTION DO NE PER EO S53561 AND NO DEFECTS FOUND YG 1132. 2 L 7 2 4T RT A52EU 200805131 20080513 1 NM 2008 5 13 DL757080680 1 20080506 A 2121 731376 FAN BOEING 757 757232 1384965 NM BS 520 OVERHEATED A DALA O OTHER M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 682DA 26958 ON APPROACH TO LANDING, NOTICED A STRONG BURNING ELEC SMELL, DISSIPATED ON TAXI IN ALL IND INST NORMAL. REMOVED AND REP LACED NR 1 FWD EQUIPMENT COOLING FAN PER MM. OPN NML. ALSO, REPLACED EQUIPMENT COOLING FILTER. 2 L 7 2 4F RT A2NM 200805131 20080513 1 WP 2008 5 13 IXXA080018O 1 20080506 A 3231 MECHANISM DOUG DC8 DC873F 302199F WP MLG OUT OF ADJUST A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 604BX 88332 401 46046 DURING CLIMB-OUT FROM KTOL, THE CREW WAS UNABLE TO RAISE NOSE LANDING GEAR NORMALLY AFTER TAKEOFF. THE CREW ACCOMPLISHE D COM PROCEDURE'S, USING THE HANDLE LATCH FLIGHT RELEASE THE NOSE GEAR CAME UP AND LOCKED. WHEN THE GEAR WAS BEING RAIS ED THE CREW HEARD A GRINDING NOISE, UPLATCH CHECK WAS OK, THE DOOR NOT LATCHED LIGHT CAME ON AT APPROXIMATELY 300KTS. T HE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NOSE GEAR DOOR AND FOUND GROUND SHIFT O UT OF ADJUSTMENT. MAINTENANCE ADJUSTED THE NOSE GEAR GROUND SHIFT AND SPOILER CONTROL. OPERATIONAL CHECK GOOD IAW DACO DC-8 MAINTENANCE MANUAL 32-23-1, DACO DC-8 MAINTENANCE MANUAL 27-60-0, DACO DC-8 MAINTENANCE MANUAL 32-30-0, AND DACO 2 L 7 4 4F RT 4A25 200805131 20080513 1 NM 2008 5 13 2008UALA02553 1 20080501 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FWD GALLEY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD GALLEY DOOR AFT FRAME CRACKED AT INBOARD SIDE OF 3RD STOP FITTING FROM THE TOP. MAJOR REPAIR ACCOMPLISHED, INSTALLE D REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 200805131 20080513 1 NM 2008 5 13 2008UALA02564 1 20080502 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EEL LIGHT INOP AT ROW 49 ABC. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 200805131 20080513 1 EA 2008 5 13 SWIA200819588 1 20080214 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 438SW 7574 LOWER FLOOR FRAME AT FS 280 AND LBL9.0 IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS FOR LOWER FLOOR FRAME AT FS 280 AND LBL 9.0 PER CRJ200 REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 200805131 20080513 1 EA 2008 5 13 SWIA200819590 1 20080220 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 340CA 10062 FS 280 BEAM IS CRACKED AND CORRODED AT RBL9, FOUND AT C-CHECK. COMPLIED WITH REQUIRED REPAIRS PER CRJ700/900 SRM 51-42- 06. 2 L 7 2 4F RT A21EA 200805131 20080513 1 EA 2008 5 13 SWIA200819591 1 20080220 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 340CA 10062 COCKPIT FLOOR SUPPORT AT FS280 IS CRACKED AND CORRODED AT RBL9, FOUND AT C-CHECK. REPAIRED COCKPIT FLOOR SUPPORT PER CR J700/900 SRM 51-42-06. 2 L 7 2 4F RT A21EA 200805131 20080513 1 NM 2008 5 13 F3LA200800217 1 20080501 A 5321 D5367204500000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED BULK CARGO PANEL 161CF HAS A PUNCTURE. MAINTENANCE CLEANED AREA FOR DAMAGE AND PR EPPED, REPAIRED AND APPLIED PRIMER AND TOP COAT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-75-12 AND SRM 51-75-12. U PON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 200805131 20080513 1 NM 2008 5 13 F3LA200800218 1 20080501 A 5320 D5311278220201 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED HEAVY CORROSION FOUND ON FLOOR SUPPORT JUST FORWARD OF SEAT TRACK AT FRAME 20 RIGH T SIDE. MAINTENANCE REMOVED SEAT TRACK LOCATED AND DRILLED HOLES, INSTALLED BRACKETS, TREATED, PRIMED AND INSTALLED NEW SEAT TRACK IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11, SRM 51-21-11 AND SRM 51-44-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 200805141 20080514 1 NM 2008 5 14 AALA200800927 1 20080411 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 945AN 30085 DFW - EMERGENCY LIGHT AT AFT NUMBER THREE GALLEY DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT AFT NUMBER THR EE GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 200805141 20080514 1 NM 2008 5 14 F3LA200800206 1 20080427 A 5270 DHE1141 PROXIMITY SWITCH AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE EMERGENCY EXIT OUT OF ADJUST A F3LA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 927FR 1117 2209 DURING CLIMB-OUT, FLIGHT CREW REPORTED ECAM MESSAGE INDICATING RIGHT OVERWING EMERGENCY EXIT DOOR OPEN. FLIGHT CREW PER FORMED AIR TURNBACK AND EXECUTED UNEVENTFUL LANDING. MAINTENANCE TROUBLE SHOT SYSTEM AND FOUND DOOR PROXIMITY SWITCH OU T OF ADJUSTMENT. MAINTENANCE ADJUSTED SWITCH IN ACCORDANCE WITH REQUIREMENTS OF AMM 52-71-13-820-050. UPON COMPLETION OF ADJUSTMENT, SYSTEM WAS OPERATIONS TESTED AND FOUND OKAY. 2 L 7 2 4F 4 F RT A28NM 200805141 20080514 1 SW 2008 5 14 AC2A119534 1 20080417 A 7130 3G2150V02051 FIRESEAL AGUSTA AB139 AB139 0260110 SW PWA PT6 PT6* 52043 EA ENGINE TORN E AC2A K NONE O OTHER NR NOT REPORTED 1 SW 31 139CW 31020 FIRESEAL, TORN AND DETERIORATED. 2 G 7 2 4U 3 T R00002RD E2NE 200805141 20080514 1 WP 2008 5 14 BKE2008F00000 2 20080317 A 7200 ENGINE RAYTHN DH125 HAWKER800 7450004 CE GARRTT TFE731 TFE731* 01518 WP LEFT MALFUNCTIONED E BKEA E B A ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 WP 01 752CS 258323 AT FL 39,000 FT, THE PILOT NOTICED SMOKE COMING INTO THE CABIN. THE PILOT DECLARED AN EMERGENCY AND STARTED DESCENT. D URING DESCENT PILOT NOTICED THAT THE LT ENGINE’S FUEL COMPUTER ENUNCIATOR LIGHT CAME "ON", THE PWR LEVER WAS RETARDED TO MAINTAIN PROPER EGT ON THAT LT ENGINE. COPILOT NOTICED THE LT ENGINE`S OIL PRESSURE ENUNCIATOR LIGHT CAME ON AND THEN NOTICED THE LT ENGINE`S OIL PRESSURE DROPPING VERY QUICKLY; AT THIS POINT THE PILOT PROCEEDED TO SHUTDOWN THAT LT ENGINE . SHORTLY AFTER ENGINE SHUTDOWN, THE LT ENGINE, THE SMOKE CEASED AND THE CABIN CLEARED. THE PILOTS COMPLETED EMERGENCY PROCEDURES AND KEPT DESCENDING AND GETTING VECTORED, THE AC FINALLY LANDED WITHOUT ANY INCIDENT. AFTER LANDING THE AC 2 L 7 2 4F 4 F RT A3EU E6WE 200805141 20080514 1 NE 2008 5 14 KNK2008F00001 2 20080417 A 7310 0292208230 MANIFOLD SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE FUEL SYSTEM COKED E KNKA K NONE O OTHER IN INSP/MAINT 1 WP 13 111AK 1403 3092 4571 FUEL COKING MATERIAL IN THE FUEL MANIFOLD LABYRINTH SEAL AREA CAUSED SEIZURE BETWEEN MANIFOLD AND FUEL INJECTION WHEEL. ENGINE WILL NOT ROTATE. (K) 1 G 7 1 3U 3 U NC H9EU E19EU 200805141 20080514 1 NE 2008 5 14 UIEA200800160 2 20080419 A 7200 CF650E2 ENGINE BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 2 FAILED A UIEA A UNSCHED LANDING R E J PARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 EA 15 526MC 22337 517358 AT FL 32.0 HOURS AFTER TAKEOFF, NR 2 ENGINE STALLED AND ROLLED BACK. THROTTLE WAS PULLED TO IDLE AND STALLING QUIT. WH EN THE THROTTLE WAS PUSHED ABOVE 80 PERCENT N2 STALL AND VIBRATION REOCCURRED, EGT REMAINED IN LIMITS. REMOVED AND REPL ACED NR 2 ENGINE PER 71-00-02. 2 L 7 4 4F 4 F RT A20WE E23EA 200805141 20080514 1 EA 2008 5 14 SWIA200819554 1 20080205 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 762SK 10226 FS 280 BEAM IS CRACKED AT LBL 9, FOUND AT C-CHECK. REPAIRED FLOORBEAM AT FS 280 PER CRJ700/900 SRM 51-42-068 AND REO 67 0-53-11-265. 2 L 7 2 4F RT A21EA 200805141 20080514 1 EA 2008 5 14 SWIA200819557 1 20080205 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 984CA 7171 STN 280 AT RBL 9.0 ON LOWER FRAME IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIR PER REO601R 53-11-171 REV D. 2 L 7 2 4F RT A21EA 200805141 20080514 1 2008 5 14 YENA2008041 4 20080501 A 2330 3042865102 ELECTRONIC UNIT AIRBUS 320 A320232 3930326 EU CABIN MALFUNCTIONED A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 599JB 11840 11840 2336 AFTER FLT 740, PSE-JFK, OUTBOUND CREW REPORTED THAT INBOUND CREW HAD BURNING SMELL AT FWD GALLEY & ROW 11. PERFORMED LT V ELECTRICAL ODOR SYSTEM INTEGRITY CHECK. REMOVED AND REPLACED SEB'S AT 10 AND 11 RT. OPS CHECK NORMAL AS PER LTV MM 2 3-39-00. 2 L 7 2 4F RT A28NM 200805141 20080514 1 NM 2008 5 14 UPS08M52101 1 20080120 A 5713 STRINGER DOUG MD11 MD11 3023602 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C RT WING UPPER STRINGER END S11 SUSPECT CRACK AS MARKED THRU ACCESS NR 636AB. HFEC INSP C/OUT PER DAC NDTSPM R.13 PART06.10.01.001 AT UPPER STRINGER END NR S11 AND CRACK APPROX 9 INCH FOUND. CRACK AT RHW STR NR 11 SLOTTED PER SRM 57- 200-00 FIG 10V.1R.35. REPAIR ANGLES FABRICATED PER SRM 57-20-00 FIG 10V.R.3 5 AND HEAT TREATED TO T6 COND PER DPS7.00-1 AND AVERAGE HARDNESS HEB82.5 IS ACCEPTABLE PER DPS1.05-3. REPAIR ANGLES HOLES PICK UP PER SRM 57-20-00 FI G 10. 2 L 7 3 4F RT A22WE 200805141 20080514 1 NM 2008 5 14 UPS08M52103 1 20080120 A 5713 STRINGER DOUG MD11 MD11 3023602 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C RT WING UPPER STRINGER END NR S10 SUSPECT CRACK AS MARKED, THRU ACCESS NR 636CB. HFEC INSP CARRIED OU T PER DAC NDT SPM R.13 PART06.10.01.001 AND CRACK APPROX 11 INCHES FOUND AS MARKED. CRACK AT RHW STR NR 10 SLOTTED OUT PER SRM 57-20-00 FIG 10V.1 R.35. REPAIR ANGLES FAB PER SRM 57-20-00 FIG 10V.1 R35 AND HEAT TREATED TO T6 COND PER 7.00- 1 AND AVERAGE HARDNESS HRB82.5 IS ACCEPTABLE PER DPS1.05-3. REPAIR ANGLES HOLES PICK UP PER SRM 57-20-00. 2 L 7 3 4F RT A22WE 200805141 20080514 1 EU 2008 5 14 08FDEA01682 1 20080430 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 745FD 668 FOUND ON SLAT LT NR 1 FOLDING NOSE OLD REPAIR NOT ACCOMPLISHED IAW SB 57-6067 AND DRAWING R578-40005. REPAIR PERFORMED BY ACCOMPLISHMENT OF SB A300-57-6067, APPROVED BY EA 6-5742-115273. 2 L 7 2 4F RT A35EU 200805141 20080514 1 EU 2008 5 14 08FDEA01683 1 20080430 A 5754 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND ON SLAT RT NR 1 FOLDING NOSE OLD REPAIR NOT ACCOMPLISHED IAW SB 57-6067 AND DRAWING R578-40005. REPAIR PERFORMED BY ACCOMPLISHMENT OF SB A300-57-6067, APPROVED BY EA 6-5742-115273. 2 L 7 2 4F RT A35EU 200805141 20080514 1 EU 2008 5 14 08FDEA01684 1 20080430 A 5754 A57940119203 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND ELONGATED HOLE ON NOSE SKIN FOLDING NOSE RT SLAT NR 1. REPAIR PERFORMED BY REPLACEMENT OF SKIN IAW SRM 51-72-10, APPROVED BY EA 6-5742-115273. 2 L 7 2 4F RT A35EU 200805141 20080514 1 WP 2008 5 14 IXXA08SMN117S 1 20080327 A 5522 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR UPPER SKIN DENTED AT STATION XE 200.2379. REMOVED FASTENERS AS N EEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYS OL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE FOUND MOMENT WITHIN TOLERANCE, MOMENT 1448-2. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XE 132.000 TO XE 246.000 IAW DC8 SRM 51-1-11, DC8 SRM 55-4-1 FIGUR E 1 SHEET 1 AND 2 ITEM "E" AND "F", DC8 SRM 55-1-0 PAGE 1, 51-1-21, DC8 SRM 51-1-9 TR NUMBER 51-142, 51-1-9A TR NUMBER 5 1-141, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 200805141 20080514 1 2008 5 14 AALA200800819 4 20080405 A 2565 100504205 SLIDE DOUG DC9 DC982 3022082 WP L1 DOOR DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 274AA 49271 ORF - EMERGENCY SLIDE AT LEFT NUMBER ONE DOOR DISLODGED WHEN DOOR OPENED WITHOUT BEING DISARMED. SLIDE DID NOT INFLATE. DOOR NOT OPENED ENOUGH TO TRIGGER INFLATION OF SLIDE. REPLACED LEFT NUMBER ONE DOOR EMERGENCY SLIDE. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 200805141 20080514 1 NM 2008 5 14 ZZDA2008102 1 20080505 A 2120 UNKNOWN BOEING 717 717200 1383700 NM CABIN ODOR A ZZDA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 37 969AT 55030 FLIGHT ATTENDANT REPORTED A SULFUR SMOKE SMELL IN THE AFT CABIN SHORTLY AFTER TAKEOFF FROM LGA. NO VISIBLE SMOKE WAS NO TED. DIVERTED INTO EWR. A/C LANDED WITHOUT INCIDENT. THE SMELL ONLY LASTED FOR ABOUT 1 MINUTE. PERFORMED INSPECTION OF A/C AND GROUND RAN ENGINES AND PACKS. NO DEFECTS WERE NOTED. NO UNUSUAL SMELLS WERE NOTED AT ANY TIME BY MAINTENANC E. 2 L 7 2 4F TR A6WE 2008051400018 20080514 00018 NM 2008 5 14 ASAA0842911 1 20080502 A 5540 65C2584151 RUDDER BOEING 737 7374Q8 138447Q NM DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 RUDDER LOWER RIGHT SIDE DELAMINATED. REMOVED DAMAGED PLIES, CUT AND INSTALLED REPAIR PLIES IAW B737 400 SRM 51 70 17 RE PAIR 2. 2 L 7 2 4F RT A16WE 2008051400020 20080514 00020 NM 2008 5 14 ASAA0842909 1 20080429 A 5755 SKIN BOEING 737 7374Q8 138447Q NM SPOILER DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 NR 1 SPOILER HAS BUMPS ON UPPER SURFACE FROM SEAL SCREWS. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008051400024 20080514 00024 NM 2008 5 14 CALA0800421 1 20080508 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 FRAME CRACKED STATION 360 ABOVE STR 9L. REPLACED CLIP AND INSTALLED REPAIR DOUBLERS PER ECRA 5310-04759. 2 L 7 2 4F RT A16WE 2008051400028 20080514 00028 NM 2008 5 14 ASAA0852914 1 20080507 A 2131 8243921002 CONTROLLER BOEING 737 737890 1384527 NM CABIN PRESSURE MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 584AS 2895 35682 AUTO FAIL LIGHT AND ALT LIGHT ILLUMINATED ON PRESSURIZATION PANEL. CYCLED TO ALT & BACK TO AUTO, FAULT LIGHT OUT. NR 1 & 2 CABIN PRESSURE CONTROLLERS BITE TEST GOOD. 2 L 7 2 4F RT A16WE 2008051400030 20080514 00030 NM 2008 5 14 ZZDA2008103 1 20080501 A 5320 J0602289 PAN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 963AT 55024 AFT CARGO DOOR LOWER PAN CORRODED BEYOND LIMITS. REPLACED PAN PER B717 SRM 53-20-15. 2 L 7 2 4F TR A6WE 2008051400031 20080514 00031 NM 2008 5 14 ZZDA2008104 1 20080502 A 5320 J0602283 PAN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 963AT 55024 FWD CARGO DOOR SILL LOWER PAN CORRODED BEYOND LIMITS. REPLACED PAN PER B717 SRM 53-20-15. 2 L 7 2 4F TR A6WE 2008051400034 20080514 00034 NM 2008 5 14 ASAA0842915 1 20080501 A 5755 6546451707 SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 LEFT WING NR 3 SPOILER LOWER SURFACE DENTED AT AFT I/B END MULTIPLE AREAS. PREPARED DAMAGED AREA, FABRICATED REPAIR DOU BLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008051400035 20080514 00035 NM 2008 5 14 ASAA0842916 1 20080501 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM SPOILER DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 LEFT WING #0 SPOILER UPPER SURFACE HAS MULTIPLE BUMPS ON UPPER SURFACE I/B SIDE 5 INCHES FROM EDGE. PREPARED DAMAGED AR EA, FABRICATED REPAIR DOUBLER BONDED IAW 737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008051400043 20080514 00043 NM 2008 5 14 ASAA0842924 1 20080501 A 5755 654645262 SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 RIGHT WING NR 5 SPOILER NUMEROUS DENTS ON LOWER SURFACE. PREPARED DAMAGED AREAS, FABRICATED 2 EACH REPAIR DOUBLERS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008051400044 20080514 00044 NM 2008 5 14 ASAA0842925 1 20080501 A 5755 654645262 SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 RIGHT WING NR 5 SPOILER UPPER SURFACE HAS 2 EACH AREAS OF MULTIPLE DENTS. PREPARED DAMAGED AREAS, FABRICATED 2 EACH REP AIR DOUBLERS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080519 NM 2008 5 19 UPS08452165 1 20080504 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 521UP 21944 AFT L1 DOOR EMERGENCY LIGHT INOP. RELAMPED, OPS CHECK GOOD PER B747 MM 33-51-05. 2 L 7 4 4F RT A20WE 20080519 EA 2008 5 19 MASA200800372 1 20080506 A 3520 OXYGEN MASK CNDAIR CL600 CL6002D24 1390016 EA LAVATORY UNWANTED DEPLOY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 919FJ 15019 ASH FLT 2703 CLT-CMH - AFT LAV OXYGEN MASK DEPLOYED. MX RE-PACKED OXYGEN MASK. 2 L 7 2 4F RT A21EA 20080519 NM 2008 5 19 KCSA081238 1 20080508 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 SMALL AREA OF DAMAGE ON FUSELAGE BELLY SKIN AT BS 644, RBL-2. 2 L 7 4 4F RT A20WE 20080520 EA 2008 5 20 MASA200800392 1 20080511 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37342 6353 7342 ASH FLT 1101 HNL - 2 FWD EMERGENCY EXIT LIGHTS WERE REPORTED TO BE INOP. MX REPLACED THE BATTERY PACKS. 2 L 7 2 4F RT A21EA 20080520 EA 2008 5 20 MASA200800393 1 20080512 A 3397 2060441 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DEFECTIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75992 7401 ASH FLT 7233 IAD - FWD SECTION OF EMERGENCY FLOOR PATH LIGHTING INOP. REPLACED EMERGENCY FLOOR LIGHTING CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080520 EA 2008 5 20 MASA200800394 1 20080512 A 3350 58351 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 715SF 7115 ASH FLT 7211 CAE - EMERGENCY FLOOR PATH LIGHTING FORWARD THREE SECTIONS INOP. MX REPLACED LIGHT STRIPS. 2 L 7 2 4F RT A21EA 20080520 EU 2008 5 20 08FDEA01846 1 20080514 A 5720 A57111092203 FITTING AIRBUS 300 A300B4622R 3930312 EU CENTER WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND ON SEVERAL HOLES IN CENTER WING BOX LOWER JUNCTION HORIZONTAL FLANGE C 47 WITH DAMAGE AND CRACKS (HOLE C, E, G). REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL DAMAGE REMOVAL AND INSTALLING FASTENER NSA5356 AND NSA5350, APPROVED BY RAS/70503969/045/2008 ISS A AND EA6-5710-117142. 2 L 7 2 4F RT A35EU 20080520 EU 2008 5 20 08FDEA01724 1 20080501 A 2930 647520191 TRANSMITTER AIRBUS 310 A310304 3930339 EU HYD SYSTEM INOPERATIVE A FDEA L ABORTED APPROACH K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 25 817FD 676 552 ON FINAL APPROACH, RECEIVED SLAT SYS 1 AND 2 FAULT FOLLOWED UP SHORTLY W/GREEN HYD ECAM COMMAND TO TURN OFF BOTH GREEN H YD PUMPS. FAULTS ON OVERHEAD WERE AS FOLLOWS: GREEN SYS SERVO (GREEN PUMPS OFF), SLAT SYS 1 AND 2, SPOILER NR 5. DID GO AROUND FOUND RT MLG DOWNLOCK ACTUATOR FLEX HOSES LEAKING. RESERVOIR OVERSERVICED. DRAINED APPROX 3 GAL FROM GREEN S YS. REMOVED AND REPLACED GREEN SYS HYD XMITTER .25GQ. REF A310-300 MM 29-31-11-4, OPS AND LEAK CHECK NORMAL. STILL REQ UIRES SERVICE AFTER OPS OF GREEN SYS. REMOVED AND REPLACED LEAKING DOWNLOCK HYD LINES. C/W LEAK CHECK AND OPERATIONAL CHECK OF GREEN SYSTEM HYDRAULICS. LEAK AND OPS CHECK GOOD. TOPPED OFF SYSTEM. 2 L 7 2 4F RT A35EU 20080520 NM 2008 5 20 QXEA200800459 1 20080511 A 2721 TRIM PANEL DHAV DHC8 DHC8202 2809007 NM COCKPIT INOPERATIVE A QXEA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 09 352PH 494 PDX - RUDDER TRIM SWITCH FAILED, WOULD TRIM TO THE RIGHT BUT NOT TO THE LEFT. ON FINAL APPROACH, RUNAWAY TRIM FULL RIGH T RUDDER. ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE TRIM PANEL, SWITCH INOP. OPERATIONAL CHECKS GOO D. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080520 NE 2008 5 20 UIEA200800182 2 20080506 A 7230 9211M73P02 FAN BLADE BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE NR 1 ENGINE BIRD INGESTION A UIEA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 EA 15 506MC 91883 21252 517579 BIRD STRIKE AT TAKEOFF TO FUSELAGE AND ENGINE NR 1 FAN BLADES. ACCOMPLISHED BIRD STRIKE INSPECTION FOR FUSELAGE AND NR 1 ENGINE AND OVERWEIGHT LANDING CHECKS AS PER IAW 05-51-14, 05-51-39 AND 72-00-00 FOR FAN BLADES CHANGED AND ENGINE INSP ECTION. REPLACED NR 1 ENGINE FAN BLADES NR 2, NR 3, NR 21 AND NR 22. AS PER AMM 72-31-02. AS PER GE ENGINE MANUAL 72- 00-00 INSPECTION ACCOMPLISHED AND FOUND SATISFACTORY. 2 L 7 4 4F 4 F RT A20WE E23EA 20080520 CE 2008 5 20 DXTA200803038 1 20080501 A 2120 99120853 SENSOR CESSNA 500 560CESSNA 2076750 CE COCKPIT INOPERATIVE E DXTA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 304QS 7990 5600408 DURING DESCENT, W/S AIR O HEAT ILLUMINATED THEN CYCLED OFF THEN ILLUMINATED AGAIN BUT CONTINUOUS. THE SWITCH WAS IN LOW AND COULD SMELL BURNING ODOR. REPLACE WINDSHIELD TEMPERATURE SENSOR AND TEMPERATURE BULB WITH NEW. OPS/LEAK CHECKS GOO D. DONE IN REF. 2 L 7 2 4F RT A22CE 20080520 CE 2008 5 20 DXTA200803040 1 20080503 A 2740 45AS66010019 HEATER BEECH MU300 400A 1155402 CE COCKPIT INOPERATIVE E DXTA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 07 145QS 1513 RK421 HORIZ STAB FAIL ANNUNCIATOR LIGHT ILLUMINATED INFLIGHT. T/S SYSTEM FOUND LT HEAT HORN IN-OP. REMOVED AND REPLACED LT HE ATER HORN WITH NEW OPS CHECKS GOOD ALL WORK IAW MM 30-11-00. 2 H 7 2 4F RT A16SW 20080520 NM 2008 5 20 DXTA200803041 1 20080503 A 5270 WARNING LIGHT AMD FALC50 FALCON2000 2730170 NM COCKPIT ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 290QS 190 DOORS LIGHT ON MWP CAME ON AT 80 KTS DURING TAKEOFF. ADJUSTED SECONDARY CATCH ON BAGGAGE DOOR PERFORMED A DOOR WARNING C HECK, OPS CHECK GOOD REF FALCON 2000 MM 52-701 2 L 7 2 4F RT A50NM 20080520 NE 2008 5 20 DXTA200803042 2 20080504 A 7200 31B518002 ENGINE GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE RIGHT VIBRATION E DXTA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 07 723QS 099 PCECC0174 CLIMBING THROUGH 12,000 FEET HEARD A LOUD BANG, THE RIGHT ENGINE, VIB INDICATOR TURNED YELLOW AND CLIMBED ABOVE THE 3RD TICK MARK ON THE RIGHT ENGINE. REMOVED AND INSTALLED A INSPECTED ENG ON RT PYLON. ALL WORK DONE IAW MM AND MM PW306A. O PS AND LEAK CHECKS GOOD AT THIS TIME ENG TSN 153.4 CSN 80. 2 L 7 2 4F 4 F RT A53NM E35NE 20080520 NM 2008 5 20 USAA920081002 1 20080503 A 5311 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - CRACKED FRAME, BS 827, S8L - S9L. REPAIRED FRAME, BS 827, S8L - S9L IAW USAIRWAYS EA 100441. 2 L 7 2 4F RT A16WE 20080520 NM 2008 5 20 USAA920081003 1 20080503 A 5311 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - CRACKED FRAME, BS 887, S8L - S9L. REPAIRED FRAME, BS 887, S8L - S9L IAW USAIRWAYS EA 100441. 2 L 7 2 4F RT A16WE 20080520 NM 2008 5 20 USAA920081004 1 20080503 A 5311 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - CRACKED FRAME, BS 907, S8L - S9L. REPAIRED FRAME, BS 907, S8L - S9L IAW USAIRWAYS EA 100441. 2 L 7 2 4F RT A16WE 20080520 NM 2008 5 20 USAA920081005 1 20080503 A 5311 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - CRACKED FRAME, BS 807, S8R - S9R. REPAIRED FRAME, BS 807, S8R - S9R IAW USAIRWAYS EA 100441. 2 L 7 2 4F RT A16WE 20080520 NM 2008 5 20 USAA920081007 1 20080503 A 5311 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - CRACKED FRAME, BS 887, S8R - S9R. REPAIRED FRAME, BS 887, S8R - S9R IAW USAIRWAYS EA 100441. 2 L 7 2 4F RT A16WE 20080520 CE 2008 5 20 DXTA200803048 1 20080507 A 3230 CONTROL CABLE CESSNA 560 560XL 2076702 CE MLG OUT OF RIG E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 677QS 5605367 AFTER TAKEOFF AND GEAR RETRACTION RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. JACKED AIRCRAFT. WITH PORTABLE MULE, UNA BLE TO DUPLICATE DISCREPENCY. OPS AND RIG CHECK GOOD OF UPLOCK SWITCHES. CHECKED GEAR RELEASE CABLE TENSION, RIG GEAR UPLOCK HOOK/ROLLER ENGAGEMENT, CHECKED GOOD. FOUND PLAY IN LT MLG DOOR IN RETRACTED POSITION. ADJUSTED ROD END ON DOOR SIDE ON TURN IN. OPS AND CLEARANCE CHECK GOOD. WORKED REF MM 32-10-00. 2 L 7 2 4F RT A22CE 20080520 EU 2008 5 20 USAA920081015 1 20080507 A 3350 32145410 POWER SUPPLY AIRBUS A321 A321211 3930370 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 186US 22081 1901 1701 FLT NR 1418 LAX-PHL - EEL - WHILE ACCOMPLISHING EPSU BATTERY TIME CHANGE, FOUND 14WL UNABLE TO TEST. MAINTENANCE REMOVE D AND REPLACED 14WL EMERGENCY POWER SUPPLY UNIT. 2 L 7 2 4F RT A28NM 20080520 NM 2008 5 20 SA08032 1 20080505 A 2420 Y0052 TRANSFORMER AIRBUS A319 A319132 3930340 NM NR 1 INOPERATIVE A USAA K NONE H ELECT. POWER LOSS-50 PC DE DESCENT 1 EA 19 809AW 31864 31858 1111 BOS, FLIGHT 64, LAS-BOS, APPROXIMATELY 70 MILES OUT OF BOS, THE CREW HAS AN ESSENTIAL AC BUS FAULT FAILURE. THE COCKPIT WENT DARK FOR A BRIEF TIME BUT AFTER FOLLOWING PROCEDURES SOME INSTRUMENTS RETURNED. MAINTENANCE REPLACED THE NR 1 TRA NSFORMER UNIT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. 2 L 7 2 4F RT A28NM 20080520 2008 5 20 UIEA200800184 4 20080512 A 3441 46300181300413 INU BOEING 747 7472D7B 1384803 NM NR 1 FAILED A UIEA A UNSCHED LANDING G MULTIPLE FAILURE TO TAKEOFF 1 EA 15 524MC 21784 AIR TURN BACK: NR 1 INU RED WARNING LIGHT ILLUMINATED AFTER TAKEOFF, CDU SCREEN BLANKED, CAPTAINS HEADING AND ATTITUDE F LAGS IN VIEW. F/O ADI ATT FLAG CAME INTO VIEW BUT F/O ADI WORKED PROPERLY. F/O FLAG RETRACTED AFTER 5 MIN. REPLACED NR 1 INU PER AMM 34-41-03 AND UPDATE NAV DATA BASE OPS CHECKED OK. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 BB08084 1 20080508 A 2701 CONTROL COLUMN BOEING 767 7672B7 1385107 NM COCKPIT BINDING A USAA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 EA 19 252AU 24765 PHL FLT 0703 FRA TO PHL - DURING THE FLIGHT, THE FIRST OFFICER'S CONTROL WHEEL WAS BINDING WHILE USING THE AILERONS. THE FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE IS CURRENTLY INSPECTING THE AIRCRAFT. 2 L 7 2 4F RT A1NM 20080520 NM 2008 5 20 SB08027 1 20080507 A 3350 20131ASMI BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 424US 23991 CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS AT THE FORWARD RIGHT ENTRY DOOR AND AT THE FORWARD RIGHT ESCAPE SL IDE LIGHT WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1132 BATTERY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20080520 NM 2008 5 20 USAA920081020 1 20080418 A 5320 143N888718 INTERCOSTAL BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTEROSTAL, BS 660, S14R. REPAIRED INTEROSTAL, BS 660, S14R IAW USAIRWAYS EO 5 331-01021 AND TASK CARD M1C53611. 2 L 7 2 4F RT A2NM 20080520 NM 2008 5 20 USAA920081022 1 20080430 A 5320 143N833827 FITTING BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL CLIP, BS 660, S17L. REPLACED INTERCOSTAL CLIP, BS 660, S17L IAW EO 5331-01021 AND TASK CARD M1C53611. 2 L 7 2 4F RT A2NM 20080520 NM 2008 5 20 USAA920081023 1 20080505 A 5311 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 907, S8R - S9R. REPAIRED FRAME, BS 907, S8R - S9R IAW TASK CARD MIC5 3002. 2 L 7 2 4F RT A16WE 20080520 NM 2008 5 20 UIEA200800187 1 20080514 A 5347 02A043406 SEAT TRACK BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 SEAT TRACK AT STA 1440 LBL 11 FOUND CRACKED. SEAT TRACK REPAIRED AS PER SRM 53-10-05 AND 51-30-02. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 F3LA200800260 1 20080426 A 5313 D53571532235 STRINGER AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED STRINGER 33 RIGHT IS DAMAGED BETWEEN FRAME 72 AND FRAME 74 DAMAGE LOCATED 2.0 INCH FO RWARD OF FRAME 74. MAINTENANCE REPAIRED DAMAGED SECTION OF STRINGER WITH SPLICE AND INSTALLED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30262. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080520 NM 2008 5 20 UIEA200800194 1 20080511 A 5720 7075T6 BEAM BOEING 747 7472D7B 1384803 NM LT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 LEFT WING LEADING EDGE "D" BEAM UPPER CHORD CRACKED ILES 1120. D' BEAM UPPER CHORD FABRICATED AND REPLACED IAW DRAWING 65B07895-139. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800195 1 20080512 A 5330 SKIN BOEING 747 7472D7B 1384803 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 AFT CARGO STA 1860 STR 45R- 46R FUSELAGE SKIN FOUND WITH LEVEL 1 CORROSION. CORROSION REMOVED PER SRM 51-10-02 AND 51-3 0-01. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800200 1 20080508 A 5347 BAC15201682 SEAT TRACK BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 AFT CARGO STA 1590 LBL 45.5 SEAT TRACK FOUND CRACKED. AFT CARGO SEAT TRACK REPAIRED PER SRM 53-10-05. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800206 1 20080511 A 5210 DOOR FRAME BOEING 747 7472D7B 1384803 NM L3 DOOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK L3 DOOR AFT UPPER CORNER EDGE FRAME FOUND CRACKED. CRACKED AREA REPAIRED PER SRM 52-10-02. 2 L 7 4 4F RT A20WE 20080520 SO 2008 5 20 LR7A08051 1 20080513 A 5420 36001519 MOUNT LKHEED 382 382G 526414U SO NR 3 NACELLE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK, FOUND NR 3 ENGINE INBD TRUSS MOUNT DIAGONAL BRACE ATTACHMENT LUG CRACK. REPAIR ACCOMPLISHED BY REPLACING NR 3 ENGINE INBD TRUSS MOUNT IAW RELEVANT PARAGRAPHS OF SMP583 CHAP 54-30 AND FIG 54-30-06 SHEET 1, 2, 3, AND 5. 2 H 7 4 4T A1SO 20080520 SO 2008 5 20 LR7A08063 1 20080513 A 5230 3536074 BULKHEAD LKHEED 382 382G 526414U SO CARGO DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5211, FOUND RAMP DOOR FWD BHD WEB CRACKED AT RS0.0, WL143, BL0.0. REPAIR ACCO MPLISHED IAW SMP583 FIG 51-140-17. 2 H 7 4 4T A1SO 20080519 WP 2008 5 19 08FDEA01828 1 20080512 A 5753 ARC05026 HINGE DOUG MD10 MD1010F 3022112 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 RIGHT WING OUTBD FLAP, INBD HINGE LOCATION NR 3 MOUNTING SURFACE IS CORRODED. REMOVED THE CORROSION FROM THE NR 3 LUG F ACE IAW CMM 57-44-08. FABRICATED SHIMS IAW CMM 57-44-08. CAD PLATED SHIMS IAW QQP 416 TY2 CL2 AND INSTALLED SHIMS ON T HE NR 3 LUG IAW CMM 57-44-01. COMPLIED WITH FEDEX EA 8-5740-116978 DATED 5/1/2008. 2 L 7 3 4F RT A22WE 20080519 NM 2008 5 19 DLM88080697 1 20080415 A 5320 STRUCTURE DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 960DL 49979 DUE AT HMV ERA 087344-14 CODE 9-53-21-03 REV ORG, REPAIR MAIN CABIN FLOOR/STA 224 ACTL 2301/2201. REPAIRED PER ERA 0873 44-14 REV A ON N/R T0092783 AT HMV-3 IN GDL. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 DLM90080713 1 20080506 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 RIGHT CUSP WEB CORRODED ON LWR SURFACE BETWEEN STA 484-503 AT CENTER LIGHTENING HOLE. WEB FOUND TO BE OUT OF LIMITS, IA W MD90 SRM 53-00-01, FIG 3. WORK TO BE ACCOMPLISHED ON N/R 1003732 2400/0215. 2 L 7 2 4F RT A6WE 20080519 WP 2008 5 19 IXXA08SMN113S 1 20080327 A 5753 SKIN DOUG DC8 DC873F 302199F WP FLAP VANE DELAMINATED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 6 VANE FLAP DELAMINATED SKIN BETWEEN STATION XF 415.000 TO ST A XF 434.000. REMOVED AND REPLACED RIGHT WING NUMBER 6 VANE FLAP. PERFORMED OPS CHECK GOOD TO FLAP SYSTEM IAW DC8 MM 2 7-51-14 PAGES 201-202, AND DC8 MM 27-50-0 PAGES 506-507. 2 L 7 4 4F RT 4A25 20080519 WP 2008 5 19 AALA200800984 1 20080416 A 2560 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9628W 53598 LGA - EMERGENCY PROTABLE LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED PORTABLE LIGHT AT LEFT NUMBER ONE DOOR. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 AALA200800994 1 20080416 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 DFW - EMERGENCY LIGHT AT SEAT 23G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 NM 2008 5 19 AALA200800995 1 20080416 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 790AN 30251 DFW - EMERGENCY LIGHT AT SEAT 23G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 EU 2008 5 19 UPS08152166 1 20080503 A 2560 FASTENER AIRBUS A300 A300F4622R 3930360 EU ESCAPE ROPE DEFECTIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 142UP 0825 COVER OVER F/O'S ESCAPE ROPE WILL NOT STAY IN PLACE. VELCRO HAS PULLED AWAY FROM COVER. INSTALLED NEW VELCRO TO ESCAPE ROPE COVER. SECURED AND IN PLACE. 2 L 7 2 4F RT A35EU 20080519 NM 2008 5 19 UPS08652185 1 20080502 A 2560 FASTENER BOEING 767 76734AF 1385212 NM ESCAPE ROPE UNSECURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 316UP 27744 CAPTAIN OVERHEAD EMERGENCY ESCAPE ROPE TRIM WILL NOT SNAP INTO POSITION, HANGS DOWN. SECURED PANEL SNAPS AS REQUIRED IP C 25-61-02, MM 25-10-00. 2 L 7 2 4F RT A1NM 20080519 EA 2008 5 19 MASA200800373 1 20080506 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT OUT OF ADJUST A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 938LR 15038 ASH FLT 2652 CLT-RIC - RT EMERGENCY DOOR CAUTION MESSAGE INTERMITTENT. ADJUSTED PROX SENSOR. 2 L 7 2 4F RT A21EA 20080519 EA 2008 5 19 MASA200800385 1 20080508 A 3350 BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17156 7156 ASH FLT 7211, ORD-CAE - CREW REPORTED THAT ALL EMERGENCY LIGHTS ARE INOP. MX CHARGED BATTERIES. 2 L 7 2 4F RT A21EA 20080520 WP 2008 5 20 ABXR080145 1 20080416 A 5320 991050145 CUSP WEB DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 231US 48114 CUSP WEB CRACKED AT FS 218, LEFT BUTT LINE 44. INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 2008051400045 20080514 00045 NM 2008 5 14 ASAA0842926 1 20080502 A 5753 654643433 SKIN BOEING 737 7374Q8 138447Q NM T/E FLAP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 LEFT WING O/B TRAILING EDGE FLAP SEGMENT DENT WITH DELAMINATION LOWER I/B SURFACE 3 INCHES FROM T/E AND 24 INCHES FROM I /B EDGE. REMOVED DAMAGED SKIN, FABRICATED FILLER REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 2008051400046 20080514 00046 NM 2008 5 14 ASAA0842927 1 20080501 A 5753 6546435303 SKIN BOEING 737 7374Q8 138447Q NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 LEFT WING I/B AFT FLAP LOWER SURFACE 2 EACH DENTS 37 INCHES FROM I/B SIDE. PREPARED DAMAGED AREA, FABRICATED DOUBLER AN D BONDED IAW B737 400 SRM 51 70 01 REPAIR 2. 2 L 7 2 4F RT A16WE 2008051400052 20080514 00052 NM 2008 5 14 CALA0800426 1 20080509 A 5320 141A541016 INTERCOSTAL BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23708 28769 CABIN FWD ENTRY, INTERCOSTAL BETWEEN FLOORBEAMS STATION 312 TO 328 BY L-1 DOOR CRACKED. REMOVED AND REPLACED INTERCOSTA L REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008051400058 20080514 00058 WP 2008 5 14 08FDEA01670 1 20080429 A 5320 AFA015431 WEB DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 CENTER PIT DOORWAY AT STA 1770 THE WEB BELOW THE AFT PDU HAS SIGNS OF CORROSION. WEB AREA IS OUT OF LIMITS IN REF TO SR M 53-00-01 VOL I FIG 1-B. CHANNEL AREA IS OUT OF LIMITS IAW SRM 53-00-01 VOL I FIG 1B. FABRICATED NEW CHANNEL IAW DWG A FA0154, REV AD. FABRICATED DOUBLER & FILLER FOR THE WEB REPAIR IAW SRM 53-00-01 VOL I FIG 10. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. INSTALLED CHANNEL & REPAIR PARTS IAW SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 2008051400059 20080514 00059 WP 2008 5 14 08FDEA01671 1 20080429 A 5322 AJC736845 SHEAR TIE DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 SURFACE CORROSION FOUND AT BS 1997, BETWEEN LONGERON 50R AND LONGERON 49R IN THE AFT FUSELAGE COMPT. REMOVED THE CORROS ION IAW SRM 51-21-01. ORIGINAL METAL THICKNESS WAS 0.071 IAW DWG AJC 7363. AFTER CORROSION REMOVAL THERE WAS 100% MATE RIAL LOSS WHICH IS OUT OF LIMITS IAW SRM 53-00-01 VOL I FIG 1B. FABBED A NEW SHEAR TIE IAW DWG AJC 7363. INSTALLED SHEA R TIE IAW SRM 51-33-01. 2 L 7 3 4F RT A22WE 2008051400065 20080514 00065 NM 2008 5 14 CALA0800427 1 20080509 A 5412 313T3380 CHANNEL BOEING 767 767224 1385170 NM NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76153 30432 NR 2 PYLON AFT FAIRING AFT BULKHEAD ATTACH CHANNEL FOUND CRACKED. NR 2 PYLON AFT FAIRING AFT BULKHEAD ATTACH CHANNEL RE PLACED PER SRM 51-10-02 AND INSTALLED PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 2008051400069 20080514 00069 NM 2008 5 14 CALA0800428 1 20080508 A 5315 141T5107 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76153 30432 CABIN - BS 303 LBL 32 - 55 FLOOR SUPPORT FOUND CORRODED. BS 303 LBL 9 - 65 FLOORBEAM UPPER FLANGE REPAIRED PER SRM 53-0 0-51, REPAIR FIG 201. 2 L 7 2 4F RT A1NM 2008051400070 20080514 00070 NM 2008 5 14 CALA0800429 1 20080509 A 2121 6454051 FAN BOEING 737 737524 1384721 NM CABIN MALFUNCTIONED A CALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 24633 27901 SMELLED SMOKE IN MID CABIN, HEARD GRINDING NOISE AT THE SAME TIME. TROUBLESHOT SYSTEM, REPLACED RECIRCULATION FAN. OPS CHECKED GOOD, REF M/M 21-21-22 PG 401. ROTABLE PARTS CHANGE WAS INDICATED - TT 0828156, S/N OFF 02329 FAN, AIR, DISTR OFF 03-2168-9-0001 2329 ON 03-2168-9-0001 3267. 2 L 7 2 4F RT A16WE 2008051400071 20080514 00071 NM 2008 5 14 CALA0800430 1 20080510 A 5753 65C27552 STRUCTURE BOEING 737 737524 1384721 NM FOREFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 NUMBER 1 MIDFLAP AT INBOARD FOREFLAP TRACK CUTOUT IS CRACKED. INSTALLED REPAIR DOUBLER PER ECRA 5752-01303 REVISION A. 2 L 7 2 4F RT A16WE 2008051400072 20080514 00072 NM 2008 5 14 CALA0800431 1 20080428 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 CABIN STATION 907 LEFT BETWEEN S8L AND S9L PASSENGER SERVICE UNIT RAIL ATTACH BRACKET TO FRAME CRACKED. INSTALLED REPAI R DOUBLER PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008051400078 20080514 00078 NM 2008 5 14 CALA0800438 1 20080511 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 LEFT SIDE BS 787 I/B ATTACH FASTENER HOLE ON AIR CONDITIONING (A/C) BRACKET CRACKED. REPAIRED LEFT SIDE BS 787 I/B ATTA CH FASTENER HOLE ON A/C BRACKET PER EA5310-04498. 2 L 7 2 4F RT A16WE 2008051400079 20080514 00079 NM 2008 5 14 CALA0800439 1 20080511 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 LEFT SIDE BS 827 I/B ATTACH FASTENER HOLE ON AIR CONDITIONING (A/C) BRACKET CRACKED. REPAIRED LEFT SIDE BS 827 I/B ATTA CH FASTENER HOLE ON A/C BRACKET PER EA5310-04498. 2 L 7 2 4F RT A16WE 2008051400081 20080514 00081 NM 2008 5 14 CALA0800441 1 20080511 A 5311 65C34355 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 LEFT SIDE BS 482A I/B ATTACH FASTENER HOLE ON AIR CONDITIONING (A/C) BRACKET CRACKED. REPAIRED CRACKED FRAME AT 482A S8 - S9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008051400084 20080514 00084 NM 2008 5 14 CALA0800410 1 20080430 A 5320 65C33509 SUPPORT BRACKET BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19638 28899 AIR CONDITIONING SUPPORT BRACKET CRACKED AT RIGHTHAND FRAME STATION 400 BETWEEN S-8 AND S-9. REPAIRED AIR CONDITIONING SUPPORT BRACKET AT RIGHTHAND FRAME STATION 440 BETWEEN S-8 AND S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008051400086 20080514 00086 NM 2008 5 14 CALA0800413 1 20080501 A 5330 65C30802 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 39343 23581 FOUND SKIN DAMAGED 2 FT AFT OF LEFTHAND AFT WING TO BODY FAIRING JUST BELOW SPLICE BELT APP STATION 727. REPAIRED IN RE FERENCE SRM 53-00-01 REPAIR 31 AS REQUIRED. 2 L 7 2 4F RT A16WE 2008051400089 20080514 00089 NM 2008 5 14 CALA0800411 1 20080505 A 3350 BR964412 SOCKET BOEING 737 737524 1384721 NM CABIN DEFECTIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19621 27334 SEAT TRACK EMERGENCY LIGHT AT 12 BC INOPERATIVE. REPLACED LIGHT SOCKET ASSEMBLY AT SEAT 12 BC, OPERATIONAL CHECKED GOOD . 2 L 7 2 4F RT A16WE 200805131 20080513 1 NM 2008 5 13 08FDEA01790 1 20080507 A 5310 ACA72251 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 631FE 48454 UPPER CARGO DOOR CUT OUT NR 7 LOWER FUSELAGE JAMB SUPPORT FITTING HOLES FOUND WITH CORROSION. UPPER CARGO DOOR CUT OUT NR 7 LOWER FUSELAGE JAMB SUPPORT FITTING HOLES 2 EA REAMED TO DIAMETER 0.520" AND REPAIR BUSHING INSTALLED AS PER SRM 53 -50-00 FIG 10 VOL. I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 200805131 20080513 1 NM 2008 5 13 DLM88080642 1 20080428 A 2150 219101223 ACM DOUG MD88 MD88 3023688 NM INOPERATIVE A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 953DL 49884 AT FL 200 LOST PRESSURIZATION WITH FLOW LIGHT PRESSURIZATION SYSTEM MTC IN PROGRESS. REPLACED LT AND RT ACMS REF ITEM 8 AND 9 THIS LOG. PERFORMED VALVE CK OUT AN OPN 5089. CKS NML PER MCC REPLACED S1-115 AND C WIRING FROM S1-119, S1-121 , S1-115, TO S1 113. NO FAULTS NOTED. REPLACED APU ECU FOR PRECAUTION HRS 6297 CYC 13 NO FAULTS NOTED. AT REMOVAL, ON LT PACK REPLACED COMPR DISCHARGE TEMP SENSOR TURBINE INLET SENSOR AND CABIN 190 DEG PER MM. ALL CKS OK. PRESSURIZED T O 3 PSI WITH BOTH PACKS OPN NML. ALL CKS OK. 2 L 7 2 4F RT A6WE 200805131 20080513 1 NM 2008 5 13 DL76L080650 1 20080430 A 5320 FLOOR SUPPORT BOEING 767 767332 1382001 NM BS 654 BENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 190DN 28447 FLOOR SUPPORT AT STATION 654+44 LBL 2 CARGO FLOORBEAM DAMAGED. REPAIRED ON NR AXG522770 PER 53-00-07 FUGURE 201 REPAIR 4 AT HMV 2. 2 L 7 2 4F RT A1NM 200805131 20080513 1 NM 2008 5 13 F3LA200800243 1 20080501 A 5210 FE240004 BOTTLE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE DOOR ASSIST LOW A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED R1 DOOR ASSIST BOTTLE NEEDS RECHARGING. MAINTENANCE RECHARGED R1 DOOR ASSIST BOTT LE AT 66 DEGREES TO 1700 PSI IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 52-10-00-614-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 200805131 20080513 1 NM 2008 5 13 AALA200800881 1 20080408 A 3350 OL3071BPEGPL LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 200805131 20080513 1 NM 2008 5 13 DL757080659 1 20080504 A 5330 144N31201 SKIN BOEING 757 757232 1384965 NM FS1010 S2-3R DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 621DL 22911 FUSELAGE/SKIN/FS 1010 - 1038, S-1 TO S-3R, LIGHTNING STRIKES TOO CLOSE TOGETHER FOR SRM REPAIRS, AND ONE REPAIR ON FS 10 40 FRAME WHICH REQUIRED NON-SRM REPAIR. DAMAGE CUTOUT OUT, DOUBLERS INSTALLED. 2 L 7 2 4F RT A2NM 200805131 20080513 1 NM 2008 5 13 F3LA200800210 1 20080501 A 5321 D5367166600000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CABIN PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED CABIN FLOOR PANEL 241CF HAD A PUNCTURE. MAINTENANCE CLEANED AND PREPPED AREA IN A CCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 AND APPLIED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 P ARAGRAPH 8C. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 200805141 20080514 1 NM 2008 5 14 UIEA200800161 1 20080427 A 5522 SKIN BOEING 747 7472D3B 1384805 NM RT ELEVATOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 RT I/B ELEVATOR HAS A 2.0 INCH CRACK AT TRAILING EDGE OF ELEVATOR STA 154.0, CAUSED BY GROUND EQUIPMENT. ACCOMPLISHED I NTERIM REPAIR AS PER B747-200 SRM 51-40-09 FIG 8, SHEETS 1 AND 2, AND SRM 51-40-15. REFERENCE EO 4755A062, TO ACCOMPLIS H REPEAT INSPECTIONS AT EVERY A-CHECK UNTIL PART 3 PERMANENT REPAIR IS ACCOMPLISHED AT C-CHECK. 2 L 7 4 4F RT A20WE 200805141 20080514 1 EA 2008 5 14 SWIA200819556 1 20080205 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 682 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 984CA 7171 STN 682.00 AT LBL 4.0 AND WL47.5 FRAME IS CRACKED, FOUND AT C-CHECK. INSTALLED NEW FRAME ANGLE PER CRJ200 SRM 51-42-06 P 11 AND 51-42-21 P 17. 2 L 7 2 4F RT A21EA 200805141 20080514 1 NM 2008 5 14 AALA200800800 1 20080402 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 187AN 32381 DFW - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A2NM 200805141 20080514 1 NM 2008 5 14 AALA200800812 1 20080403 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 780AN 29956 JFK - EMERGENCY LIGHT AT SEAT 26C INOPERATIVE. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 200805141 20080514 1 EU 2008 5 14 YENA2008042 1 20080503 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 15 570JB 2099 FLT 316, SAN-IAD, ON TAXI OUT, RETURNED TO GATE, BURNING SMELL COMING FROM REAR OF LAVATORY OF AIRCRAFT. T/S RT & LT AF T LAVS. NO C/B POPPED. WATER HEATERS OK. FLUSH TIMERS OK. NO SMOKE SMELL FROM LAVS. BACK GALLEY C/B PANELS. NO POP PED C/B. FLIGHT CREW RAN ENGINES & PACKS. NO ELEC SMELL IN CABIN. OK FOR SERVICE. NO FAULTS NOTED. PERFORMED SDCU C HECK, NO FAULTS. OK FOR SERVICE PER AMM TASK 24-00-00-810-823. 2 L 7 2 4F RT A28NM 2008051400006 20080514 00006 NM 2008 5 14 ASAA0852907 1 20080506 A 2150 AS11708H0100 LINE BOEING 737 737890 1384527 NM RT ACM DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 579AS 4884 35187 RIGHT PACK BRAIDED LINE FROM ACM TO CONDENSER HAS 2 HOLES IN IT. REPLACED THE BRAIDED LINE FROM ACM TO CONDENSER. LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 2008051400012 20080514 00012 NM 2008 5 14 CALA0800416 1 20080501 A 5311 6546525 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 LEFTHAND SIDE BS 360 INBOARD ATTACH FASTENER HOLE ON AIR CONDITIONING BRACKET CRACKED. REPAIRED FRAME AT 360L PER EA 53 10-04498. 2 L 7 2 4F RT A16WE 20080520 NM 2008 5 20 F3LA200800259 1 20080503 A 5322 D53571554217 SHEAR TIE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED SHEAR TIE AT FRAME 75 FROM STRINGER 32 RIGHT TO STRINGER 33 RIGHT IS DAMAGED. MAINTE NANCE FABRICATED NEW SHEAR TIE AND INSTALLED SHEAR TIE IN ACCORDANCE WITH THE REQUIREMENTS OF AIRBUS DRAWING D53571554, EA A9-53R-30262 SRM 51-26-11 PARAGRAPH 2 AND SRM 51-42-11 PARAGRAPH 6. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED A ND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080520 NM 2008 5 20 UIEA200800185 1 20080511 A 2913 3508806 PUMP BOEING 747 747228F 1384895 NM HYDRAULIC SYS FAILED A UIEA O OTHER M J OVER TEMP WARNING INDICATION CR CRUISE 1 EA 15 809MC 20887 CREW REPORTED HYD SYSTEM NR 1 OVERHEAT. ADP AND EDP TURNED OFF. ALL PUMPS ON NR 1 OFF OCCASIONAL OVERHEAT INDICATION C ONTINUED. AFTER 1 HOUR NO OVERHEAT INDICATION. THEN THE PROBLEM RETURNED. REMOVED AND REPLACED NR 1 ENGINE EDP PER AM M 29-11-05, OPS AND LEAK CHECKED OKAY. CLEANED AND RESET CONNECTOR AT TEMP SWITCH SYSTEM CHECKED OKAY PER AMM 29-32-01. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800203 1 20080507 A 5311 FRAME BOEING 747 7472D7B 1384803 NM FUSELAGE DEFORMED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK STA 1900 STRINGER 13R TO 14R FRAME FOUND DEFORMED. REPAIRED FRAME PER SRM 53-10-04. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800208 1 20080511 A 5313 STRINGER BOEING 747 7472D7B 1384803 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 STATION 2160 STRINGER 44L FOUND LEVEL 1 CORROSION. CORROSION CLEANED UP IAW SRM 53-10-03. 2 L 7 4 4F RT A20WE 20080520 WP 2008 5 20 RYNA200800019 1 20080417 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 932RD 49233 PASSENGER CABIN LEFT INBOARD SEAT TRACK IS CORRODED AT BS 693. REPAIRED CORRODED AREA IAW MD-80 SRM 51-10-03. 2 L 7 2 4F A6WE 20080520 WP 2008 5 20 RYNA200800022 1 20080417 A 5752 FAIRING DOUG DC9 DC982 3022082 WP AILERON TAB CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 932RD 49233 RIGHT WING OUTBOARD AILERON TAB, OUTBOARD FAIRING IS CRACKED AT THE TOP. REPAIRED CRACKED AILERON IAW MD-80 SRM 51-70-4 . 2 L 7 2 4F A6WE 20080520 WP 2008 5 20 RYNA200800023 1 20080411 A 5350 BRACE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 932RD 49233 FUSELAGE TO LEFT WING FAIRING SUPPORT BRACES ARE CRACKED AT BS 807 NEAR WING LEADING EDGE AREA. REPLACED CRACKED SUPPOR T BRACES PER MD-80 SRM 51-10-2. 2 L 7 2 4F A6WE 20080520 2008 5 20 2008UALA02644 4 20080505 A 2565 D31516121 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R1 DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 426UA 510 SLIDE PRESS AT DOOR 1R SHOWS ON RED. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080520 2008 5 20 2008UALA02645 4 20080506 A 2565 D31591478U1 SLIDE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PAX DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 FWD ENTRY DOOR SLIDE IS HANGING OUT OF COVER ASSY. REINSTALLED SLIDE REF MM 25-61-35. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 20080520 NM 2008 5 20 2008UALA02647 1 20080506 A 2497 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT GENERATOR CHAFED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 651UA 25389 RIGHT GENERATOR OFF LINE. RTFL ORD. REPLACED CONNECTOR. WIRES FROM CONNECTOR WERE CHAFED AND SHORTED AGAINST THE BACKS HELL. 2 L 7 2 4F 4 F RT A1NM E24NE 20080520 NM 2008 5 20 2008UALA02657 1 20080507 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 CORROSION ON SHEAR TIE AT BS 1197+132, BETWEEN STR 39R-39L. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080520 NM 2008 5 20 2008UALA02664 1 20080507 A 8011 35054367 STARTER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT ENGINE FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 675UA 29243 DURING LEFT ENG START N2 DROPPED BELOW 20 PRIOR TO ADDING FUEL TUG ADVZD SPARKS AND FLUID. SUSPECT FAULTY STARTER. REP LACED STARTER & START VALVE. OP CHECKS GOOD. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080520 NM 2008 5 20 2008UALA02676 1 20080507 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 661UA 27158 EEL LIGHTS FLASH BETWEEN ROWS 15AB THRU 19AB. COULD NOT DUPLICATE PROBLEM. EEL LIGHTS OPS CHECKS OK.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080520 NM 2008 5 20 2008UALA02677 1 20080507 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 661UA 27158 EEL AISLE IN FRONT OF ROW 15CDEF INOP. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080520 2008 5 20 2008UALA02680 4 20080505 A 2565 O-RING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EVAC SLIDE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 117UA 28810 LOW BOTTLE PRESSURE. REPLACED O-RINGS IN VALVE ASSEMBLY. AC OK FOR SERVICE 2 L 7 4 4F 4 F RT A20WE E24NE 2008051400016 20080514 00016 NM 2008 5 14 CALA0800418 1 20080507 A 5313 654988946 STRINGER SPLICE BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 E&E COMPARTMENT AT STATION 354 TO 367, S27L SPLICE CORRODED. FABRICATED AND INSTALLED REPAIR PER ECRA 5330-03803. 2 L 7 2 4F RT A16WE 2008051400017 20080514 00017 NM 2008 5 14 2008UALA02454 1 20080427 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 348-360 S15 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 INTERCOSTAL WEB AT STR 15 BETWEEN STA 348 AND 360 HAS 7 EACH ELONGATED HOLES. INSTALLED REPAIR ANGLES. 2 L 7 2 4F 4 F RT A16WE E2GL 2008051400023 20080514 00023 CE 2008 5 14 DXTA200803011 1 20080422 A 2910 67421801 BARREL CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL MLG LEAKING E DXTA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 07 960QS 5309 7500160 AFTER TAKEOFF, GEAR FAILED TO RETRACT. (3) GEAR LIGHTS EXTINGUISHED BUT RED UNLOCK LIGHT ILLUMINATED. CREW FOLLOWED CHEC KLIST AND LOWERED GEAR. FOUND LOWER BARREL ASSEMBLY ON NOSE GEAR WITH 0 PSI AND LEAKING HYDRAULIC FLUID. REMOVED AND REP LACED UPPER AND LOWER BARREL ASSEMBLY PERFORMED GEAR SWINGS AND NOSE WHEEL STEERING FUNCTIONAL CHECK. OPS CHECK AND LEAK CHECK GOOD IAW CE750 MM CH 32-20-00 2 L 7 2 4J 4 F RT T00007WI TE6CH 2008051400033 20080514 00033 NM 2008 5 14 ZZDA2008105 1 20080502 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 963AT 55024 FUSELAGE SKIN HAS 2.5 INCH CRACK THROUGH LAP SEAM RIVETS AT STA 1022 LONG 14L. REPAIRED PER AIRTRAN EA 17-53-01127IR. 2 L 7 2 4F TR A6WE 2008051400048 20080514 00048 NM 2008 5 14 ASAA0852930 1 20080508 A 2160 412A160041 FILTER ELEMENT BOEING 737 737890 1384527 NM CABIN DIRTY A ASAA O OTHER O OTHER CR CRUISE 1 NM 02 570AS 35185 TO MAINTAIN A COMFORTABLE TEMPERATURE IN THE AFT CABIN THE AFT CABIN TEMP KNOB HAS TO BE TURNED FARTHER CLOCKWISE THAN U SUAL TO AROUND 3 O'CLOCK. THIS PRODUCES APPROX 20C DUCT TEMP. THE OTHER KNOBS WERE IN THE USUAL POSITION: CONTROL CAB 11:00 AND FWD CAB 12:00 FOUND AFT CABIN FILTER (SENSOR) DIRTY, CLEANED FILTER PER MM 21 61 06. UNABLE TO VERIFY DISCRP AFT CABIN TEMP CONTROL OPS CHECK NORMAL REF MM 21 61 00. THE VERIFICATION OF CORRECTIVE ACTION IS DEFERRED FOR NON ETO PS REVENUE FLT. PLEASE VERIFY AFT CABIN TEMP CONTROL KNOB MAINTAINS COMFORTABLE TEMP AROUND THE 12 O'CLOCK POS. PERFOR MED FVR ON AFT CABIN TEMP CONTROL. OPS NORMAL REF LG 6424971. DEFERRAL CLEARED. 2 L 7 2 4F RT A16WE 2008051400055 20080514 00055 EU 2008 5 14 08FDEA01666 1 20080429 A 5347 A5327828622300 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 MAIN DECK FLOOR TRACK AT RBL 38, FRAME 52 HAS CORROSION IN THE CENTER OF THE TRACK. ORIGINAL ADAPTER WAS FOUND TO BE OUT OF LIMITS REF 53-16-10; SRM. INSTALLED NEW ADAPTER REF SRM 51-40-21; PARA 7. 2 L 7 2 4F RT A35EU 2008051400063 20080514 00063 WP 2008 5 14 08FDEA01678 1 20080429 A 5753 ARC200915 PLATE DOUG MD10 MD1010F 3022112 WP ZONE 500 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 RIGHT WING T/E OUTBD FLAP, INBD TRACK, INBD SIDE, THE SUPPORT FOR PANEL NR 635 DL IS GOUGED. REMOVED PLATE DAMAGE IAW SRM 51-31-01; VOL II. FABBED NEW PLATE IAW DWG ARC 2009, REV Y. ALODINED & PRIMED IAW SRM 51-21-01 VOL II PGS 21-24. PART MARKED IAW GMM 7-0-1000. INSTALLED IAW SRM 51-35-01 VOL II. INSTALLED PANEL 635 FL IAW SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 2008051400064 20080514 00064 WP 2008 5 14 08FDEA01679 1 20080429 A 5753 ARC200910 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 600 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 RIGHT WING T/E OUTBD FLAP, INBD TRACK, INBD SIDE, SKIN HAS A GOUGE. REMOVED PLATE DAMAGE IAW SRM 51-25-01; VOL II. FA BRICATED IAW DWG ARC 2009, REV Y. ALODINED & PRIMED IAW SRM 51-21-01 VOL II PGS 21 & 24. INSTALLED IAW SRM 51-35-01 VOL II. PART MARKED IAW GMM 7-0-1000. PAINTED IAW SRM 51-21-02; VOL II; PG 8. 2 L 7 3 4F RT A22WE 2008051400066 20080514 00066 NE 2008 5 14 2008UALA02456 2 20080428 A 7261 M834851128 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE STARTER DRIVE WORN A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 548UA 25396 726695 NR 1 ENGINE HIGH OIL CONSUMPTION. FOUND STARTER DRIVE SEAL DRAIN TUBE LEAKING. REPLACED STARTER DRIVE SEAL, LEAK CHECK W AS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008051400067 20080514 00067 2008 5 14 2008UALA02457 4 20080426 A 2565 SHEAR PIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L1 DOOR SLIDE SHEARED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 FOUND DOOR 1 LEFT DOOR BOTTLE LOW AND SHEAR PIN, SHEARED IN REF TO SLIDE PACK ON JET WAY. REPLACED DIAPHRAGM AND SHEAR PIN AND SERVICED BOTTLE PER MM. ALSO REPLACED WITH SERVICABLE SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008051400077 20080514 00077 NM 2008 5 14 CALA0800437 1 20080511 A 5311 6546595 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 RIGHT SIDE BS 727A I/B ATTACH FASTENER HOLE ON AIR CONDITIONING BRACKET CRACKED. REPAIRED FRAME AT BS 727A 59R PER EA53 10-04498. 2 L 7 2 4F RT A16WE 2008051400087 20080514 00087 NM 2008 5 14 CALA0800409 1 20080504 A 5320 6547957 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INTERCOSTAL AT STATION 840-855 S-25-R IS CORRODED (LEVEL 2 CORROSION). REPLACED INTERCOSTAL AT STATION 840-855 S-25-R I AW SRM 51-30-01. 2 L 7 2 4F RT A16WE 2008051400096 20080514 00096 EA 2008 5 14 TRAX200800593 1 20080503 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 828AS 7213 NR 8 OVERWING EMERGENCY LIGHT, SECTION 9-13 FLOOR STRIP LIGHTING AND NR 3 DOME LIGHT INOP. REMOVED AND REPLACED NR 4 BA TTERY CHARGER IAW CRJ 200 AMM 33-51-05. REMOVED AND REPLACED NR 4 BATTERY CHARGER IAW CRJ 200 AMM 33-51-05. 2 L 7 2 4F RT A21EA 2008051400102 20080514 00102 NM 2008 5 14 SWAA082518 1 20080508 A 3350 100031 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 267WN 32525 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR LOWER EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED EMERGENCY EXIT L IGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008051400105 20080514 00105 WP 2008 5 14 DHL2008807509 1 20080502 A 5313 STRINGER SPLICE DOUG DC8 DC873F 302199F WP BS 440-460 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 FWD CARGO COMPT SPLICE FITTING CRACKED 2 INCHES (STA 440.000 - 460.000, L-31R). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 P G 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTIN G IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 2008051400106 20080514 00106 WP 2008 5 14 DHLA200800044 1 20080425 A 3310 BULB DOUG DC8 DC873F 302199F WP ZONE 900 MALFUNCTIONED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 05 804DH 46124 FLT NR 445, IF LIGHT OVER LIFE RAFT IN GALLEY AREA RIGHT COMP LIGHT SWITCH ILLUMINATED FOR 2 HRS THERE IS A STRONG CHEMI CAL ODOR. RELAMPED IAW MM 33-13-0. OPS CHECK GOOD NO ODOR DETECTED P/N 307. A/C WAS GROUNDED 2 L 7 4 4F RT 4A25 2008051400107 20080514 00107 NM 2008 5 14 SWAA082519 1 20080508 A 3350 65C27095 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR UPPER EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008051400109 20080514 00109 NM 2008 5 14 CALA0800436 1 20080511 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 RIGHT SIDE BS 787 INBOARD ATTACH FASTENER HOLE ON AIR CONDITIONING BRACKET CRACKED. REMOVED DAMAGE, DRILLED AND INSTALL ED REPAIR IAW EA5310-04498. 2 L 7 2 4F RT A16WE 2008051400110 20080514 00110 NM 2008 5 14 DHLA200800042 1 20080506 A 2121 500724620 GASPER FAN BOEING 727 727223 1384074 NM AFT CARGO ODOR A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 05 753DH 22468 FLT NR 213 WITH GASPER FAN ON, ELECTRICAL ODOR NOTED. REMOVED AND REPLACED GASPER FAN. OPS CHECK GOOD IAW MM 21-23-00. AIRCRAFT WAS GROUNDED. 2 L 7 3 4F A3WE 2008051400114 20080514 00114 NM 2008 5 14 F3LA200800250 1 20080501 A 5210 D5311318520000 BEARING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE DOOR HOOK SEIZED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED RIGHT HAND AFT ENTRY DOOR UPPER LATCH HOOK BEARING SEIZED. MAINTENANCE REMOVED AND REPLACED RIGHT AFT ENTRY DOOR UPPER LATCH HOOK BEARING IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 52-13-00-820-001. UP ON COMPLETION OF THE REPAIR IT WAS INSPECTED NAD FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008051400115 20080514 00115 NM 2008 5 14 CALA0800446 1 20080511 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 LEFT SIDE BS 440 I/B ATTACH FASTENER HOLE ON AIR CONDITIONING (A/C) BRACKET CRACKED. REPAIRED CRACKED FRAME AT BS 440 S 8 - S9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 2008051400116 20080514 00116 WP 2008 5 14 IXXA080019O 1 20080507 A 3230 LANDING GEAR DOUG DC8 DC873F 302199F WP ZONE 700 MALFUNCTIONED A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 604BX 88333 402 46046 DURING CLIMB-OUT FROM KTOL LANDING GEAR WOULD NOT RETRACT. THE CREW GOT A INFLIGHT INDICATION OF MECHANICAL AND ELECTRI CAL GROUND SHIFT FAILURE. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE RAISED THE AIRCRAFT OFF T HE GROUND AND PERFORMED NUMEROUS EXTENSION AND RETRACTION OF THE LANDING GEAR. OPERATIONAL CHECK GOOD IAW DACO DC-8 MAI NTENANCE MANUAL 32-30 AND DACO 7-10-0. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2008051400118 20080514 00118 NM 2008 5 14 AALA200800897 1 20080410 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 678AN 29428 DFW - EMERGENCY LIGHT AT AFT SEAT 5E INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT AFT SEAT 5E. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051400119 20080514 00119 NM 2008 5 14 CALA0800447 1 20080512 A 5320 BAC1505100120 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 INTERCOSTAL UPPER ANGLE HAS CRACK AT NUT PLATE BS 348 - 360 LBL 14". REMOVED DAMAGED INTERCOSTAL UPPER ANGLE IAW B737 S RM 51-40-02 MATERIAL ID FOR ANGLE, BAC1505-100120 EXTRUSION, AND MATERIAL ID FOR SHIM 7075-T6, 0125", PAC 75145Q, IAW EA 5310-03585, FABRICATED ANGLE AND SHIM IAW EA3510-03555. ALODINED AND PRIMED ANGLE AND SHIM IAW B737 SRM 51-20-01. INST ALLED ANGLE AND SHIM IAW EA5310-03585. 2 L 7 2 4F RT A16WE 2008051400127 20080514 00127 NM 2008 5 14 SWAA082557 1 20080511 A 3350 100031 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 LEFT OVERWING EMERGENCY EXIT LIGHT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 2008051400128 20080514 00128 NM 2008 5 14 SWAA082528 1 20080511 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 323, STR 20R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008051400131 20080514 00131 NM 2008 5 14 SWAA082563 1 20080511 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008051400162 20080514 00162 2008 5 14 SWAA082554 4 20080511 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 726SW 27858 R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008051400166 20080514 00166 NM 2008 5 14 SWAA082603 1 20080512 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008051400172 20080514 00172 NM 2008 5 14 SWAA082587 1 20080512 A 2560 94010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 380SW 26587 AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20080520 NM 2008 5 20 2008UALA02681 1 20080506 A 2621 342004051601U SQUIB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO BAY BLOWN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 312UA 23673 FOUND CARGO BOTTLE NR 1 SQUIB BLOWN. REPLACED FIRE SUPPRESSION BOTTLE NR 1 OF CARGO PITS. REF MM 26-23-01-401. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 20080520 NM 2008 5 20 2008UALA02524 1 20080429 A 3350 CONTACT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR DIRTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 586UA 26710 EXTERIOR EMERGENCY LIGHT INOP AT DOOR 1R AND DOOR 4R. LIGHT ASSY CONTACTS DIRTY. CLEANED LIGHT ASSY CONTACTS, OPS CHEC KED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080520 NM 2008 5 20 2008UALA02706 1 20080511 A 3610 CLAMP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE PNEUMATIC SYSTEM LOOSE A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 934UA 26662 RTFL DUE TO WING BODY OVERHEAT WARNING. FOUND PNEUMATIC LEAK JUST INBOARD OF NR 1 ENGINE PYLON AT CLAMP. REPLACED CLAM P. 2 L 7 2 4F 4 F RT A16WE E2GL 20080520 NM 2008 5 20 2008UALA02707 1 20080512 A 3810 COMPRESSOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GALLEY FAILED A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 798UA 26928 AIR COMPRESSOR MOTOR BURNED UP AT DEPT, INITIAL CALL WAS FOR SMOKE ODOR IN AFT GALLEY. SUSPECT FAULTY BEARING. REPLACE D AIR COMPRESSOR PER AMM 38-42-01. POTABLE WATER SYSTEM OPS CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080520 NM 2008 5 20 2008UALA02708 1 20080510 A 2910 LINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE HYDRAULIC SYS LEAKING A UALA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 29 216UA 30549 NR 2 ENG HYD FLUID DRIPPING FROM BOTTOM OF COWLING AT 1 DROP PER SECOND. FLUID IS HYDRAULIC OIL NOT ENGINE OIL FROM LIN E BEHIND PYLON PANEL 442BR. TIGHTENED "B" NUTS ON HYD LINES AND NOW ALL LEAK CHECKS OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080520 SO 2008 5 20 LR7A08064 1 20080513 A 7130 3635577 FIRE SEAL LKHEED 382 382G 526414U SO NR 2 ENGINE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC7201, FOUND NR 2 ENGINE FIRESEAL COLLAR ASSEMBLY FLANGE CRACKED. WELD REPAIR ACCOMPLISHED IAW LAC MEA 382-54-08-028. 2 H 7 4 4T A1SO 20080520 SO 2008 5 20 LR7A08066 1 20080513 A 3010 1026512 SUPPORT LKHEED 382 382G 526414U SO HORIZ STAB CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5511, FOUND LT HORIZ STAB LE ANTI-ICING COMPENSATOR TANG SUPPORT CRACKED, P/N1 0265-12. WELDING REPAIR ACCOMPLISHED IAW LAC MEA 382-30-08-031. 2 H 7 4 4T A1SO 20080520 2008 5 20 2008UALA02709 4 20080511 A 3442 RADAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WEATHER RADAR MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 518UA 24871 LOST WEATHER RADAR. FLIGHT DIVERTED. REPLACED WX TRANSCEIVER, INSTLD SVCBL SCANNER 2 L 7 2 4F 4 F RT A2NM E17NE 20080520 2008 5 20 2008UALA02711 4 20080512 A 2565 62773326 SLIDE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE PAX DOOR LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 797UA 26924 MAIN ENTRY DOOR 3R SLIDE PRESSURE LOW. SUSPECT FAULTY O-RING. REPLACED SLIDE ASSEMBLY PER AMM 25-66-01. OPS CHECK OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080521 EU 2008 5 21 2008UALA02716 1 20080508 A 2700 SDAC AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 496UA 1845 F-CTL ELAC 1 FAULT AND ELAC 2 FAULT. REPLACED SDAC NR 2, OPS TESTS OK. NO 2 L 7 2 4F 4 F RT A28NM E40NE 20080521 NM 2008 5 21 2008UALA02719 1 20080510 A 5712 RIB BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT WING GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 LT INBOARD WING FIXED LEADING EDGE WSTA 208 AIRLOAD RIB IS GOUGED. MAJOR REPAIR ACCOMPLISHED, BLENDED THE GOUGE. VERIF IED CRACK FREE WITH HFEC. INSTALLED REPAIR STRAP. 2 L 7 2 4F 4 F RT A16WE E2GL 20080521 NM 2008 5 21 2008UALA02720 1 20080510 A 5240 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE SERVICE DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 DURING LAP JOINT INSP, FOUND RIGHT FWD SERVICE DOOR FRAME CRACKED AT THE AFT LOWER CORNER. MAJOR REPAIR ACCOMPLISHED, T RIMMED OUT THE DAMAGE. VERIFIED DAMAGE REMOVAL WITH HFEC. INSTALLED INNER, MIDDLE AND OUTER REPAIR PLATES WITH FILLERS . 2 L 7 2 4F 4 F RT A16WE E2GL 20080521 NM 2008 5 21 2008UALA02729 1 20080508 A 2421 757183F CONVERTER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 BKUP GEN FAULTED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 772UA 26930 "MANUALLY INITIATED ENGINE START TEST". THIS TEST GIVES FAULT, "BACKUP CONVERTER HAS INTERNAL FAULT". SUSPECT FAULTY C ONVERTOR. REPLACED BACK UP GENERATOR CONVERTER PER MM 24-25-09. PASSED TEST PER MM 24-25-00. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080521 EU 2008 5 21 2008UALA02730 1 20080512 A 2730 WARNING SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 478UA 1533 ELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN. FCDC FAILED---NO SHOP FINDINGS. REPLACED FCDC-2. SYSTEM CKS NORMAL, NO MS G'S DISPLAYED. ACCOMPLISHED AFS & LAND TESTS. CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20080521 EU 2008 5 21 2008UALA02731 1 20080511 A 3350 BF964421 LENS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MISSING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 463UA 1282 EMERGENCY AISLE LIGHT AT SEAT 18C IS MISSING LENS. REPLACED SEAT LIGHT. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080521 NM 2008 5 21 2008UALA02738 1 20080510 A 2612 SWITCH BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FIRE SWITCH INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 FWD CARGO FIRE ARM SWITCH INTERNAL LIGHT IS INOP, RELAMP NO HELP. SUSPECT FAULTY SWITCH. REPLACED LIGHTED SWITCH. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080521 2008 5 21 2008UALA02743 4 20080509 A 2565 D31038201U1 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 535UA 25130 NR 1L DOOR ESCAPE SLIDE BOTTLE PRESSURE LOW. FOUND DURING NR 3 SERVICE. REPLACED SLIDE, TESTS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 NM 2008 5 21 2008UALA02745 1 20080511 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ODOR A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 556UA 26650 STRONG ODOR LIKE FAILING BEARING IN COCKPIT. CHRONIC WRITE-UP. ACP FULL INSPECTION IAW FI M 21-00-01 SMOKE OR FUMES. R AN ENGINES INDEPENDANTLY WITH PACKS ISOLATED. RAN APU AND PACKS. DID VISUAL OF ALL ASSOCIATED SYSTEM FOR HYD OR OIL LEAK S. NO OBVIOUS LEAKS OR CRACKS FOUND. COULD NOT DETECT SMELL OR REPEAT DEFECT ON GROUND. NO KNOWN SORCE. PACKS OPERATED N ORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 NM 2008 5 21 2008UALA02750 1 20080511 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 585UA 26709 DOOR NR 4R SLIDE LIGHT INOP. RELAMPED. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 NM 2008 5 21 2008UALA02752 1 20080510 A 3397 CONNECTOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 784UA 26951 AFT SECTION OF EEL STRIP ON SEAT 1F INOP. SUSPECT LOOSE CONNECTION. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SER VICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080521 NM 2008 5 21 2008UALA02762 1 20080513 A 3230 SEQUENCE VALVE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MLG MALFUNCTIONED A UALA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 WP 29 187UA 26877 RTFL WITH GEAR DISAGREE MESSAGE. REPLACED NLG SAFETY VALVE & GEAR OPERATED DOOR SEQUENCE VALVE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080520 EU 2008 5 20 08FDEA01803 1 20080508 A 5411 2210081327 LONGERON AIRBUS 310 A310 EU ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 NR 1 PYLON AFT LOWER FAIRING PANEL 475 AL; UPPER LT ATTACH ANGLE IS CHAFED ON THE INNER SURFACE. BLENDED CHAFED AREA PE R SRM 51-77-10. FOUND TO BE OUT OF LIMITS PER SRM 54-55-51 TABLE 101 SHEET 1. ORIGINAL MATERIAL 0.071. MATERIAL REMAININ G 0.047. MATERIAL REMOVED 0.024. REMOVED DAMAGED LONGERON AND REPLACED WITH A NEW LONGERON PER SRM 51-40-21; PARA 6. A LODINED; PRIMED PER AMM 51-10-0. LOCATED & DRILLED PER SRM 51-40-44. 2 L 7 2 4F RT A35EU 20080520 WP 2008 5 20 08FDEA01802 1 20080508 A 5411 AUB710739 RIB DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 1 PYLON STRINGER FOR PANEL 439 AL FWD LEFT LANDING IS WORN. REMOVED FWD RIB IAW SRM 51-31-01; VOL II & 51-35-01; VO L II. DRILLED UP NEW RIB IAW DWG AUB 7107, REV F & SRM 51-31-01; VOL II. INSTALLED NEW RIB IAW SRM 51-31-01, VOL II & 51-35-01; VOL II. 2 L 7 3 4F RT A22WE 20080520 NM 2008 5 20 KCSA081243 1 20080515 A 3350 LIGHT BOEING 747 7472B4B 138481B NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 713CK 21099 EMERGENCY LIGHT IN CEILING AFT OF P-6 C/B PANEL WILL NOT LIGHT. 2 L 7 4 4F RT A20WE 20080520 EU 2008 5 20 USAA920080997 1 20080502 A 5320 F5347823420000 FLOOR SUPPORT AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 272AY 333 BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON FLOOR SUPPORT, BS 5759/FR 75, +Y350 TO +Y450. REPAIRED FLOOR SUPPORT, BS 5 759/FR 75, +-Y350 TO +Y450 IAW USAIRWAYS EA 134009. 2 L 7 2 4F RT A46NM 20080520 2008 5 20 A6WA200840346 4 20080417 A 3444 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RADIO ALTIMETER LOOSE A A6WA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 31 464AW 7890 GROUND LIFT DUMP AUTO DEPLOY ON ENGINE START. TIGHTENED RADIO ALTIMETER ANTENNA COAX CONNECTOR AND PERFORMED BONDING TE ST PER AMM 51-80-00. SPOILER CONTROL SYSTEM OPS CHECK GOOD IAW AMM 27-65-00. RADIO ALTIMETER OPS CHECK GOOD IAW 34-44- 01. 2 L 7 2 4F 4 F RT A21EA E15NE 20080520 EA 2008 5 20 A6WA200840347 1 20080408 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BS 319-349 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 FLOOR SUPPORT ANGLE BTW FS 319.70 AND FS 349.0 IB OF SERVICE DOOR, BTW RBL 27.00, FOUND CORRODED. (K) FLOOR SUPPORT FA BRICATED WITH FORMED ANGLE RAW MATERIAL P/N S6144-14 IAW SRM 51-24-21 AND INSTALL IAW SRM 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 20080520 EA 2008 5 20 A6WA200840348 1 20080414 A 7830 SNUBBER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE THRUST REVERSER CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 NR 1 T/R ACTUATOR AT 2 O`CLOCK POSITION SNUBBER AND SNUBBER COVER FOUND CRACKED AND BRACKET. (K) REPLACED SNUBBER AND SNUBBER COVER IAW SRM 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 20080520 EA 2008 5 20 A6WA200840349 1 20080413 A 7830 SNUBBER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE THRUST REVERSER CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 T/R ACTUATOR AT 1 O`CLOCK POSITION, SNUBBER AND SNUBBER COVER FOUND CRACKED. (K) REPLACED IAW SRM 51-42-06. 2 L 7 2 4F 4 F RT A21EA E15NE 20080520 CE 2008 5 20 DXTA200803036 1 20080430 A 3150 WARNING MESSAGE CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 946QS 7500195 (REMOTE C B TRIPPED) CYAN MESSAGE APPEARED ON TAKE-OFF. INSPECTED REMOTE C/B IN MAIN JUNCTION BOX. NO DEFECTS FOUND. POWERED AIRCRAFT AVIONICS SYSTEM, NO ABNORMAL EICAS MESSAGES PRESENT. CHECKED FAULT HISTORY. NONE FOUND FOR REMOTE C/B . NO DEFECTS FOUND AT THIS TIME IAW 24-52-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080520 SW 2008 5 20 MD05012008 1 20080429 A 5302 206032400027 BULKHEAD BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL TAILBOOM CRACKED E EVCA K NONE O OTHER IN INSP/MAINT 1 CE 03 165SB 51327 CAE895520 FORWARD TAILBOOM BULKHEAD CRACKED. 1 G 7 1 3U 3 U H2SW E1GL 20080520 NM 2008 5 20 UIEA200800197 1 20080511 A 5315 FLOORBEAM BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 COCKPIT STA 330 RBL 65 FLOORBEAM UPPER CHORD CRACKED. REPAIRED FLOORBEAM CHORD AS PER SRM 51-40-04 FIG 2. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800201 1 20080507 A 5320 2024 WEB BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK STA 140 TO 150 RIGHT SIDE OUTBOARD WEB FOUND CRACKED. WEB REMOVED AND REPLACED PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 20080520 SO 2008 5 20 LR7A08052 1 20080513 A 5312 345367R STIFFENER LKHEED 382 382G 526414U SO RT MLG WW CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5321, FOUND RT MWW BHD STIFFENER CRACK AT FS 597-617, WL150, RBL62. REPAIR AC COMPLISHED BY FABRICATING AND REPLACING STIFFENER IAW SMP583 CHAPTER 51-60 AND 51-70 AND DWG 345367. 2 H 7 4 4T A1SO 20080520 NM 2008 5 20 2008UALA02655 1 20080507 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 CORROSION ON SHEAR TIE STA 1241, STR 39L TO 39R. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080521 NM 2008 5 21 2008UALA02721 1 20080510 A 5310 6547959U78 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 AFT CARGO DOOR CUTOUT FWD FRAME JUST ABOVE LWR DOOR STOP FITTING, MIS-DRILLED HOLE IN FRAME. MAJOR REPAIR ACCOMPLISHED, REPLACED FRAME AT BS 794.3. 2 L 7 2 4F 4 F RT A16WE E2GL 20080521 NM 2008 5 21 2008UALA02723 1 20080510 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 DOOR 2L UPPER HINGE ARM CUTOUT REQUIRES DOUBLER REPAIR. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 EU 2008 5 21 V2J2008F00001 1 20080119 A 2612 80909095007 CONTROL PANEL PIAGIO P180 P180 6960204 EU PWA PT6 PT6A66 52043 NE FIRE CONTROL INOPERATIVE E V2JA O OTHER N FALSE WARNING AP APPROACH 1 SO 15 149SL 1077 PCERK0034 ON APPROACH, THE FLIGHT CREW GOT INDICATION VIA THE FIRE CONTROL PANEL OF A NR (1) ENGINE FIRE. THE CREW FOLLOWED THE C HECKLIST AND PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN. AFTER THE ENGINE SHUTDOWN THE FIRE WARNING LIGHT EXTINGUISHED A ND THE AC LANDED WITHOUT INCIDENT. MAINT FOUND NO EVIDENCE OF AN ENGINE FIRE AND CONCLUDED THERE WAS AN INDICATION PROB LEM. AFTER SEVERAL ENGINE RUNS AND TEST FLIGHT MAINT WAS NOT ABLE TO DUPLICATE THE FIRE INDICATION. AFTER CHECKING THE FIRE LOOP AND WIRING IT WAS DETERMINED THE MOST LIKELY CAUSE WAS THE FIRE WARNING PANEL IN THE COCKPIT. THE FIRE WARNI NG PANEL WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. (K) 1 H 7 2 3O 4 T RT A59EU E26NE 20080521 NM 2008 5 21 2008UALA02763 1 20080512 A 3350 8100033901 LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 217UA 30550 SEAT 3F SEAT MOUNTED EMERGENCY LIGHT CAME OFF. FOUND LIGHT ASSEMBLY LOOSE. SECURED LIGHT ASSY. OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080521 SO 2008 5 21 LR7A08074 1 20080513 A 5341 WEB LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK, FOUND WEB CRACKED AT BOLT HOLE UPON REMOVAL OF RT WING ATTACH ANGLE AT FS 596, WL250, RBL61. 5. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-08-026. 2 H 7 4 4T A1SO 20080521 NM 2008 5 21 F3LA200800266 1 20080430 A 5320 D53571593000 PAD AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED TO REMOVE AIRCRAFT JACK PAD ASSEMBLY BETWEEN FRAME 73 AND FRAME 74 STRINGER 34. MAIN TENANCE FOUND JACK PAD ASSEMBLY BAD AND REPLACED JACK PAD ASSEMBLY IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-3026 2. UPON COMPLETION IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080521 WP 2008 5 21 AALA200801029 1 20080421 A 2822 3980001 PUMP DOUG DC9 DC982 3022082 WP CENTER TANK FAILED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 214AA 49162 DFW INFLIGHT T1164/21APR - CREW REPORTED THREE FORWARD CENTER FUEL TANK CIRCUIT BREAKERS POPPED IN FLIGHT. CENTER FUEL TANK STOPPED PUMPING. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED FORWARD TRANSFER FUEL CENTER BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080521 NM 2008 5 21 AALA200801034 1 20080421 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976AN 30099 DFW - EMERGENCY BULL NOSE LIGHT AT LEFT FIRST CLASS INOPERATIVE. REPLACED LAMP FOR EMERGENCY BULL NOSE LIGHT AT LEFT FI RST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 NM 2008 5 21 AALA200801014 1 20080419 A 2780 FSEU BOEING 767 767323 1385205 NM E&E BAY MALFUNCTIONED A AALA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 381AN 25450 CDG INFLIGHT T44/19APR - CREW REPORTED LEADING EDGE SLAT ASSEMBLY EICAS MESSAGE AND LEADING EDGE CAUTION LIGHT WHEN MOVI NG FLAP HANDLE TO 1 AT 205 KNOTS. COULD NOT LOWER FLAPS NORMALLY. DECLARED EMERGENCY AND LANDED CDG WITHOUT INCIDENT. RESET FLAP SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080521 NM 2008 5 21 AALA200801026 1 20080420 A 3350 HOUSING BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 784AN 29588 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET AREA IS DAMAGED. REPLACED LIGHT HOUSING FOR EMERGENCY LIGHT AT LEF T NUMBER ONE DOOR CLOSET AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051400174 20080514 00174 NM 2008 5 14 SWAA082569 1 20080508 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 429WN 33658 EEPLS LENS LOOSE AT ROW 3 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008051400182 20080514 00182 NM 2008 5 14 DHL2008780007 1 20080511 A 5320 WEB BOEING 727 727223 1384074 NM BS 1240 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 780DH 22006 CUT OUT DAMAGE ON AFT STAIRWELL LT TORQUE BOX WEB AT BS 1240, LBL 21, FABRICATED REPAIR DOUBLER, AND INSTALLED PER B727 SRM 53-10-2 FIG 6, AND 51-40-2 FIG 1. 2 L 7 3 4F A3WE 2008051400184 20080514 00184 WP 2008 5 14 08FDEA01800 1 20080508 A 5414 AUB703837 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 1 PYLON PANEL 437 EL IS CHAFED AT THE HINGE AND THE HINGE IS WORN. REMOVED AND REPLACED P/N AUB7038-37 HINGE ASSY AU B7038-39 HINGE IAW DC10/MD 10 SRM 51-35-01 VOL II; BLENDED AREA IAW DC/MD10 SRM 54-00-01 VOL I; FOUND TO BE OUT OF ALLOW ABLE LIMITS IAW DC/MD10 SRM 54-00-01 VOLI; MAT ID 2024-T3 .090 IAW DC/MD10 SRM 54-00-01 VOL I; FABBED DOUBLER IAW DC/MD1 0 SRM 54-00-01 VOL I; ALODINED AND PRIMED DOUBLER IAW DC/MD10 SRM 51-21-01 VOLII; INSTALLED DOUBLER IAW DC/MD10 SRM 51-3 5-01 VOL II. 2 L 7 3 4F RT A22WE 2008051400185 20080514 00185 WP 2008 5 14 08FDEA01801 1 20080508 A 5410 AUB7108145 HINGE DOUG MD10 MD1010F 3022112 WP ZONE 400 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 1 PYLON PANEL NR 437 HL HAS A BROKEN HINGE. BLENDED DOUBLER ORIGINAL MAT .100 REMOVED .030 REMAINING .070 FOUND TO B E OUT OF LIMITS IAW DC/MD10 SRM 57-00-01 VOL I FABBED -177 DOUBLER IAW DC/MD10 DWG. AUB7108 REV AN ALODINED AND PRIMED DOUBLER IAW DC/MD10 SRM 5121-01 VOL II. PART MARKED DOUBLER FEDEX GMM 7-0-1000. INSTALLED -177 DOUBLER AND HINGE IAW D C/MD10 SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 2008051400186 20080514 00186 NM 2008 5 14 AALA200800921 1 20080411 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 347AN 33086 MIA - EMERGENCY LIGHT FORWARD OF AFT CARGO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT FORWARD OF AFT CARGO DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008051400188 20080514 00188 NM 2008 5 14 F3LA200800219 1 20080501 A 5320 D5391635520000 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED FORWARD CARGO RIGHT FLOORBOARD SUPPORT PROFILE AT STRINGER 38 RIGHT FROM FRAME 25 TO FORWARD OF FRAME 34 HAS CORROSION AROUND SEVERAL NUT PLATE HOLES. MAINTENANCE REMOVED AND REPLACED RIGHT FLOORBOARD SUPPORT PROFILE AT STRINGER 38 RIGHT FROM FRAME 28 TO FRAME 34 AND INSTALLED FASTENER IN ACCORDANCE WITH THE REQUIREMENT S OF SRM 51-72-11 AND SRM 51-44-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008051400191 20080514 00191 NM 2008 5 14 2008UALA02554 1 20080501 A 5230 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AFT CARGO DOOR, DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 AFT CARGO DOOR, AFT SIDE INTERIOR FRAME HAS PREVIOUS TOOLING DAMAGE APPROX 8 INCH ABOVE LATCH TORQUE TUBE. MAJOR REPAIR ACCOMPLISHED, REPLACED AFT LOWER FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2008051400192 20080514 00192 NM 2008 5 14 2008UALA02555 1 20080501 A 5230 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AFT CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 AFT CARGO DOOR, UPPER FWD CORNER INTERIOR FRAME HAS SEVERAL PREVIOUS TOOLING MARKS. MAJOR REPAIR ACCOMPLISHED, REPLACED FWD UPPER FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2008051400194 20080514 00194 WP 2008 5 14 AALA200800976 1 20080415 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7530 49922 LGA - EMERGENCY LIGHT EXIT SIGN AT FIRST CLASS LAVATORY INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT EXIT SIGN AT FIRST CLASS LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008051400196 20080514 00196 WP 2008 5 14 AALA200800982 1 20080415 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9628W 53598 LGA - EMERGENCY LIGHT AT OVERHEAD FORWARD LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD F ORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008051400197 20080514 00197 NM 2008 5 14 AALA200800957 1 20080414 A 3397 CONNECTOR BOEING 767 767323 1385205 NM EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 MIA - EMERGENCY LIGHT AT SEAT 28H INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 28H. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008051400198 20080514 00198 NM 2008 5 14 AALA200800958 1 20080414 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR SLIDE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051400199 20080514 00199 NM 2008 5 14 AALA200800959 1 20080414 A 3397 WIRE BOEING 777 777223 1385213 NM EMERGENCY LIGHT EXPOSED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT WIRING AT MAIN DECK CREW REST CLOSET LEFT AFT SIDE EXPOSED. REPLACED COVER FOR EMERGENCY LIGHT WI RING AT MAIN DECK CREW REST CLOSET LEFT AFT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051400200 20080514 00200 NM 2008 5 14 AALA200800960 1 20080414 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT AT SEAT 40G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 40G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051400201 20080514 00201 NM 2008 5 14 AALA200800968 1 20080415 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT SEAT 39G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 39G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051400202 20080514 00202 NM 2008 5 14 AALA200800969 1 20080415 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT SEAT 39G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 39G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051400203 20080514 00203 NM 2008 5 14 AALA200800983 1 20080415 A 3350 8039001 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 182AN 29592 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051400205 20080514 00205 WP 2008 5 14 IXXA08SMN136S 1 20080417 A 5347 S4889185 CARGO TRACK DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 2 TRACK WITH LUGS, BROKEN AT STATION 55.000. REM OVED SEGMENT OF DAMAGED TRACK AND EXITING SPLICES. CLEANED, TREATED AND PRIMED AREA AND EXITING SPLICES. INSTALLED NEW TRACK AND REINSTALLED SPLICES IAW DC8 SRM 53-2-3 FIGURE 14 SHEETS 1-2, 51-3-0, DC8 SRM 51-1-8B, DC8 SRM 53-2-3 FIGURE 1 4, 53-7-3 FIGURE 3E SHEETS 1 AND 2 ITEM "K", 51-2-0 FIGURE 50 SHEET 79, 51-1-21, 51-3-0, AND 51-3-1. 2 L 7 4 4F RT 4A25 2008051400206 20080514 00206 EA 2008 5 14 MALA080089 1 20080506 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 8965E 7965 LT INTERCOSTAL OBLIQUE ANGLE AT FS 625 UPPER IN AFT EQUIPMENT COMPARTMENT IS CRACKED 1 INCH LONG. REMOVED/INSTALLED NEW INTERCOSTAL IAW CRJ 200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 2008051400207 20080514 00207 WP 2008 5 14 DHLA200800043 1 20080410 A 3320 LIGHT DOUG DC8 DC873 302199C WP GALLEY ODOR A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 05 804DH 46124 FLT NR 160 WITH COMP LIGHT SWITCH ON LIGHT OVER GALLEY ON A PHOSPHOROUS ODOR WAS DETECTED WITH GALLEY POWER OFF TURNED O FF COMP LIGHT SWITCH AND ODOR DISSIPATED, NO SMOKE DETECTED. TURNED ON COMP LIGHTS INSPECTED CARGO COMP LIGHTS, NO ODOR NOTED. OPS CK GOOD PER MM 33-30-0. OPS CK GALLEY PWR, NO ODOR NOTED. OPS CK GOOD PER MM 25-30-0. A/C WAS GROUNDED. 2 L 7 4 4F RT 4A25 2008051400208 20080514 00208 WP 2008 5 14 IXXA08SMN137S 1 20080417 A 5347 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 680 WORN B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK WITH LUGS WORN AT STATION 680.000. REMOV ED EXISTING SPLICES (FWD SIDE) AND REMOVED SEGMENT OF DAMAGED TRACK AFT SIDE. FABRICATED SPLICES. CLEANED, TREATED AND PRIMED AREA AND SPLICES. INSTALLED SEGMENT OF NEW TRACK AND NEW SPLICES AND REINSTALLED EXISTING SPLICES IAW DC8 SRM 5 3-2-3 FIGURE 14 PAGES 49-50, 51-3-0, DC8 SRM 51-1-8B, 53-7-3 FIGURE 3E SHEET 1 AND 2, 51-2-0 FIGURE 50 SHEET 73, AND 51- 3-1. 2 L 7 4 4F RT 4A25 2008051400213 20080514 00213 EA 2008 5 14 A6WA200840328 1 20080412 A 5540 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA RUDDER MISSING A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 RUDDER LOWER CLOSURE RIB CLOTH MISSING. (M) RUDDER LOWER CLOSURE RIB DIAPHRAGMS REPAIR IAW 601R-55-41-018. 2 L 7 2 4F RT A21EA 2008051400214 20080514 00214 EA 2008 5 14 A6WA200840330 1 20080414 A 5720 ANGLE CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 RIGHT WING, L/E EDGE 630JL, ANGLE CRACKED AT WS 149.58. (M) ANGLE REPLACED IAW SRM 51-41-02. 2 L 7 2 4F RT A21EA 2008051400215 20080514 00215 EU 2008 5 14 08FDEA01757 1 20080505 A 5347 R5307008820200 CARGO TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 MAIN DECK CARGO SEAT TRACK NR 4 LT HAS CORROSION BETWEEN FR 35 AND FR 36. REMOVED LEVEL 1 CORROSION, REMOVED DAMAGED SE CTION AND REPAIRED NR 4 LT SEAT TRACK WITH SPLICE REPAIR BETWEEN FR 35 AND FR 36 IAW A300-600 SRM 53-10-16, FIG 201. 2 L 7 2 4F RT A35EU 2008051400218 20080514 00218 NM 2008 5 14 2008UALA02223 1 20080416 A 5321 FLOORBOARD AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CARGO BAY DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 854UA 1731 CARGO FLOORBOARD RPL S GLS PNL. ACCOMPLISHED MAJOR REPAIR AT LCQ AS A PART OF UAL EG PROJECT TO REPLACE FLOORBOARDS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008051400219 20080514 00219 EA 2008 5 14 A6WA200840306 1 20080402 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 CRACK EXISTS ON PILOT BULKHEAD FS 280 LBL 9 WL 71. (M) PILOTS BULKHEAD REPAIRED IAW REO 601R-53-11-171 REV "D". (A) 2 L 7 2 4F RT A21EA 2008051400221 20080514 00221 EA 2008 5 14 A6WA200840332 1 20080414 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 574 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 443AW 7781 CARGO BAY FLOOR SILL CRACKED APPROX .200 IN AT FS 574. REPAIRED IAW CRJ 200 REO 601R-53-61-1741. (M) 2 L 7 2 4F RT A21EA 2008051400236 20080514 00236 NM 2008 5 14 SWAA082556 1 20080511 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 202WN 33999 EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2008051400237 20080514 00237 NM 2008 5 14 SWAA082530 1 20080511 A 5754 65C22602 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED CV CHECK, FOUND LT WING NR 4 L/E SLAT DELAMINATED AT UPPER SURFACE. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 2008051400243 20080514 00243 NM 2008 5 14 SWAA082537 1 20080511 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 200805131 20080513 1 EU 2008 5 13 08FDEA01793 1 20080508 A 5414 A546114001000 PANEL AIRBUS 310 A310324 3930206 EU NR 1 PYLON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 NR 1 PYLON PANEL NR 414 ER HAS CHAFING ON THE MATING SURFACE. REPAIRED THE IAW SRM 54-52-51, FIG 203. 2 L 7 2 4F RT A35EU 200805131 20080513 1 WP 2008 5 13 08FDEA01798 1 20080508 A 5730 ARB1068 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 307FE 48291 RT WING L/E EXT SURFACE FOUND WEAR ON SKIN. REPAIRED L/E WITH DOUBLER IAW SRM 57-10-00 FIG 40 VOL I. 2 L 7 3 4F RT A22WE 200805131 20080513 1 CE 2008 5 13 1356879R 1 20080501 A 3213 51411022 AXLE CESSNA 402 402C 207590R CE RT MLG BROKEN E HYIA O OTHER O OTHER TX TAXI/GRND HDL 1 NE 01 6879R 402C0611 RIGHT MAIN GEAR AXLE BROKE ON TAXI IN. 1 L 7 2 3O A7CE 200805131 20080513 1 NM 2008 5 13 ANCF200800009 1 20080505 A 3097 CABLE BOEING 757 757236 1384971 NM WINDOW HEAT OVERHEATED W ANCF H DEACTIVATE SYST/CIRCUITS M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 23 521NA 25592 WINDOW HEAT CABLES OF L SIDE WINDOW OVERHEATED PRODUCING FUMES L SIDE WINDOW HEAT SW WAS TURNED OFF. DEFERRED TO DMI LO G BOOK ITEM NR 307 WAS INSPECTED L SIDE WINDOW POWER LINES AND FOUND BURNT. DUE THIS CONDITION L SIDE WINDOW HEATING IS DEACTIVATED AND DEFERRED TO MEL. INSPECTED L SIDE WINDOW POWER LINES AND FOUND BURNED. WINDOW HEATING DEACTIVATED A ND DEFERRED TO MEL MAINTENANCE PROCEDURES ACCOMPLISHED. IAW AMM 56-11-02 OPENABLE WINDOW N2 LT WAS REPLACED OPERATIO NAL TEST SATISFACTORY. 2 L 7 2 4F RT A2NM 200805131 20080513 1 NM 2008 5 13 AALA200800880 1 20080408 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 200805131 20080513 1 EU 2008 5 13 MALA080065 1 20080505 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 630-686 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 LT INBOARD SEAT TRACK FOUND CORRODED ON TOP FROM STA 630-686. LT INBOARD SEAT TRACK REMOVED AND REPLACED WITH NEW PART AS PER SRM 51-40-21 AND E/O S53060 PART NUMBER B53004-1. 2 L 7 2 4T RT A52EU 200805131 20080513 1 EU 2008 5 13 MALA080073 1 20080505 A 5753 SKIN SAAB SF340 340B 7860101 EU RT TE FLAP DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 DENT ON RT FLAP INNER SKIN AT WS159 AND 4 INCH AFT OF FRONT SPAR DEPTH .048 INCH LENGTH 1 INCH. RT FLAP INNER SKIN WS 1 59 AND 4 INCH AFT FRONT SPAR .048 INCH DEPTH REPAIRED IAW EOS57060. 2 L 7 2 4T RT A52EU 200805131 20080513 1 EU 2008 5 13 MALA080075 1 20080505 A 5220 SKIN SAAB SF340 340B 7860101 EU EMERGENCY EXIT GOUGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 GOUGE RT EMERGENCY EXIT SKIN AT 8 INCH AFT OF FWD EDGE AND 2.4 INCH ABOVE LOWER EDGE. EMERGENCY EXIT DOOR SKIN DAMAGE A T 8 INCH AFT OF FWD EDGE AND 2.4 INCH ABOVE LOWER EDGE REPAIRED IAW EO S52028. UT DISBOND DONE IAW EO52028 NO DISBOND W /O 47152(1243). 2 L 7 2 4T RT A52EU 200805131 20080513 1 EA 2008 5 13 SWIA200819589 1 20080214 A 5220 DOOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 438SW 7574 LEFT OVERWING EMERGENCY EXIT DOOR HAS CORRODED HARDWARE, FOUND AT C-CHECK. REPLACED CORRODED HARDWARE PER SRM CRJ200 51 -41-02 PG 1-6. 2 L 7 2 4F RT A21EA 200805141 20080514 1 WP 2008 5 14 AALA200800899 1 20080410 A 2133 OUTFLOW VALVE DOUG DC9 DC982 3022082 WP CABIN PRESSURE INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 586AA 53249 DFW - INFLIGHT T468/10APR - CREW REPORTED UNABLE TO CONTROL CABIN PRESSURE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT . FOUND OUTFLOW VALVE UNABLE TO CLOSE. REPLACED OUTFLOW VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 200805141 20080514 1 SW 2008 5 14 MD04302008 1 20080419 A 6710 206001397001 SUPPORT BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL CYCLIC STICK LOOSE E EVCA K NONE O OTHER IN INSP/MAINT 1 CE 03 24AE 45646 CAE895242 CYCLIC STICK HAS VERTICAL FREE PLAY. (1) OF THE (3) SCREWS WHICH HOLD DOWN THE PIVOT BEARING WAS FOUND TO BE LOOSE. 1 G 7 1 3U 3 U H2SW E1GL 200805141 20080514 1 WP 2008 5 14 NWAA081829752 1 20080426 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 752NW 47116 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 12 THROUGH 15 OF COACH SEATS IN THE CAB IN HAD FAILED. MAINTENANCE REPLACED THE EMERGENCY PATHWAY LIGHT POWER SUPPLY AT THE OVERWING EXIT. INSTALLED NEW BATTE RIES AND OPERATIONALLY CHECKED THE SYSTEM. 2 L 7 2 4F A6WE 200805141 20080514 1 SO 2008 5 14 GUUA04270801 1 20080427 A 3260 PROXIMITY SWITCH EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE LT MLG LOOSE A GUUA K NONE N FALSE WARNING TO TAKEOFF 1 SO 29 261AS 120141 FLIGHT: 9175, AFTER TAKEOFF, AT RETRACTION, THE LT MLG RED (B) LIGHT REMAINED ILLUMINATED RECYCLED GEAR AND RETRACTED NO RMALLY. RESECURED LT MLG UPLOCK PROXIMITY SWITCH. 2 L 7 2 4T 4 T RT A31SO E20NE 200805141 20080514 1 EA 2008 5 14 SWIA200819555 1 20080205 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 762SK 10226 COCKPIT FLOOR SUPPORT IS CRACKED AT FS 280, FOUND AT C-CHECK. INSTALLED COCKPIT FLOOR SUPPORT PER CRJ700/900 SRM 51-42- 06-001-001-A01. 2 L 7 2 4F RT A21EA 200805141 20080514 1 NM 2008 5 14 UPS08M52102 1 20080120 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C LT WING UPPER STRINGER END NR S12 SUSPECT CRACK AS MARKED THRU ACCESS NR 535BT. HFEC INSP CARRIED OUT PER DAC NDT SPM R.13 PART 06.10.01.00 AND CRACK APPROX 7 INCHES FOUND. CRACK AT LHW STR NR 12 SLOTTED OUT PER SRM 57-2 0-00 FIG 10 V.1R.35. REPAIR ANGLES FABRICATED PER SRM 57-20-00 FIG 10V.1R.35 AND HEAT TREATED TO T6 PER DPS7.00-1 HARDN ESS OBTAINED HRB82.5 IS ACCEPTABLE PER DPS1.05.3. REPAIR ANGLES HOLES PICK UP PER SRM 57-20-00 FIG 10 V.1R.35. 2 L 7 3 4F RT A22WE 200805141 20080514 1 EU 2008 5 14 08FDEA01669 1 20080429 A 5347 A5378193220200 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU BS 1393-1658 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 MAIN CARGO COMPT SEAT TRACK AT LBL 97 HAS CORROSION SPOTS IN THE BOTTOM OF THE TRACK FROM STA 1393 TO 1658. REMOVED & R EPLACED SEAT TRACK IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 200805141 20080514 1 WP 2008 5 14 AALA200800824 1 20080405 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 419AA 49331 TPA - EMERGENCY LIGHT AT SEAT 17D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F A6WE 200805141 20080514 1 WP 2008 5 14 AALA200800822 1 20080405 A 3397 WIRE HARNESS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7549A 53031 LGA - EMERGENCY EXIT SIGN AT RIGHT FLOOR OPPOSITE FORWARD LAVATORY INOPERATIVE. REPAIRED WIRING FOR EMERGENCY EXIT SIGN AT RIGHT FLOOR OPPOSITE FORWARD LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 200805141 20080514 1 EU 2008 5 14 AALA200800813 1 20080403 A 3297 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU MLG LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 7082A 643 SJU INFLIGHT T618/03APR SDQ TO JFK - AFTER TAKEOFF UNABLE TO RETRACT MAIN LANDING GEAR. LANDED SJU WITHOUT INCIDENT. FOUND LOOSE CONNECTORS FOR RIGHT MAIN GEAR SYSTEM ONE AND TWO BOGIE BEAM SENSORS. CLEANED AND RECONNECTED BOTH CONNECTO RS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008051400004 20080514 00004 NM 2008 5 14 2008UALA02449 1 20080426 A 3510 RCF6705 TRANSDUCER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW O2 LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 802UA 690 DURING TOW TO GATE, NOTICED CREW OXYGEN PRESSURE DROPPING FROM 1580 TO 1500, FOUND LEAK TO BE AT SERVICE PORT. REPLACED PRESSURE REGULATOR/TRANSDUCER, NO LEAKS WERE NOTED AFTER SERVICING. 2 L 7 2 4F 4 F RT A28NM E40NE 2008051400022 20080514 00022 NM 2008 5 14 CALA0800420 1 20080507 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 CABIN STATION 827RT BETWEEN S8R AND S9R PASSENGER SERVICE UNIT RAIL ATTACH BRACKET TO FRAME CRACKED. REPAIRED FRAME AT STA 827AND STR 8R + STR 9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 2008051400036 20080514 00036 NM 2008 5 14 ASAA0842917 1 20080501 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 LEFT WING #0 SPOILER DENTED ON UPPER SURFACE I/B AREA 10 INCHES FROM I/B EDGE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER BONDED IAW 737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 2008051400056 20080514 00056 EU 2008 5 14 08FDEA01667 1 20080429 A 5310 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 MAIN DECK FLOOR TRACK AT RBL 20, FRAME 42 HAS CORROSION IN THE CENTER OF THE SEAT TRACK. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-21 PARA 6 & 7. 2 L 7 2 4F RT A35EU 2008051400057 20080514 00057 EU 2008 5 14 08FDEA01668 1 20080429 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 MAIN DECK FLOOR AT BL 0, FRAME 44, CENTER TRACK IS CRACKED AND CORRODED. REMOVED CORROSION ; OUT OF LIMITS IAW SRM 53-10 -16 FIG 101. 100% MATERIAL LOSS. REPLACED WITH A NEW SEAT TRACK P/N 5327400500053, IAW SRM 51-40-44 & 51-40-21. 2 L 7 2 4F RT A35EU 2008051400083 20080514 00083 NM 2008 5 14 CALA0800444 1 20080511 A 5311 143A1111 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23708 28769 FRAME CRACKED AT STA 400 ABOVE S9R B737-53-3-0739. REPAIRED CRACKED FRAME BS 400 S9R PER EC/RA 5310-04763. 2 L 7 2 4F RT A16WE 2008051400088 20080514 00088 EU 2008 5 14 2008UALA02459 1 20080425 A 2622 RELAY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FIRE EXTING FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 404UA 450 APU FIRE EXTINGUISHING CIRCUIT CHECK FAILS. FOUND FLIGHT GROUND RELAY 43WF FAILING. FLIGHT GROUND RELAY 43WF REPLACED, OPS TESTED SYSTEM NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008051400091 20080514 00091 EU 2008 5 14 2008UALA02460 1 20080425 A 2900 769105A MODULE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD GRND RAT MOD FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 440UA 702 TEST FLIGHT, PULLING CBZ25 AND Z26 DEPLOYED RAT BUT DID NOT SHOW HYD PRESSURE TO BLUE SYSTEM. EMERGENCY GEN DID NOT WOR K SINCE NO HYD PRESSURE. PUSH MAN RAT BUTTONS BUT NO CHANGE. FOUND THE GROUND CHECK MODULE FAILED. REPLACED GROUND CHEC K MODULE. OPS TESTED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008051400101 20080514 00101 NM 2008 5 14 2008UALA02483 1 20080427 A 2810 TANK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUEL CELL LEAKING A UALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 595UA 28748 FUEL ODOR IN COCKPIT FOR 5 SECONDS AFTER TAKEOFF. FOUND FUEL LEAK IN CENTER TANK CAUSING ODOR TO ENTER LT PACK. TANKS RE SEALED, PACK BURN OUT PERFORMED. 2 L 7 2 4F 4 F RT A2NM E17NE 2008051400132 20080514 00132 EU 2008 5 14 MALA080081 1 20080427 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 215-268 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425XJ 340B425 RT INBOARD SEAT TRACK PROFILE CORRODED UNDER LAVATORY; APPROX STA, 215 - 268. REMOVED DAMAGED TRACK PROFILE AND INSTALL ED NEW PROFILE P/N: 7253721-459 IAW SAAB 340 AMM CH. 20-10. 2 L 7 2 4T RT A52EU 2008051400133 20080514 00133 NM 2008 5 14 SWAA082562 1 20080511 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008051400134 20080514 00134 NM 2008 5 14 F3LA200800255 1 20080423 A 5330 D53570712212 SKIN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED FIVE DENTS ON TAIL FUSELAGE IN STRINGER AREA 3 AND 6 FRAME 82 AND 83. MAINTENANCE RE PAIR IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30256. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND A CCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008051400143 20080514 00143 SO 2008 5 14 SWIA200819596 1 20080503 A 5610 WINDOW EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 299SW 120329 FLT 5717 - FIRST OFFICERS DV WINDOW IS CRACKED. REPLACED COPILOT'S WINDOW IAW MM 56-11-01. 2 L 7 2 4T RT A31SO 2008051400144 20080514 00144 NM 2008 5 14 SWAA082544 1 20080510 A 2761 654456114 ACTUATOR BOEING 737 7373H4 1384600 NM SPOILER FAULTY A SWAA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 29 372SW 26599 WHEN SELECTING FLAPS TO 5 DEGREES DURING APPROACH A DEFINITE FLUTTER IS FELT, AND AT CRUISE A RAPID YAWING WAS NOTED. R EMOVED AND REPLACED NR 3 SPOILER ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2008051400145 20080514 00145 NM 2008 5 14 SWAA082543 1 20080510 A 2761 654456115 ACTUATOR BOEING 737 7373H4 1384600 NM SPOILER FAULTY A SWAA K NONE F FLT CONT AFFECTED AP APPROACH 1 SW 29 372SW 26599 WHEN SELECTING FLAPS TO 5 DEGREES DURING APPROACH A DEFINITE FLUTTER IS FELT, AND AT CRUISE A RAPID YAWING WAS NOTED. R EMOVED AND REPLACED NR 2 SPOILER ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 2008051400146 20080514 00146 SO 2008 5 14 SWIA200819597 1 20080506 A 2150 97962641 SHUTOFF VALVE EMB 120 EMB120ER 3260203 SO LT ACM MALFUNCTIONED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 578SW 17490 16820 120346 FLT 3614 - SMOKE AND BURNING SMELL REPORTED IN THE COCKPIT. REPLACED LEFT TURBINE INLET CONTROL VALVE IAW EMB AMM 21-50 -09 AND REPLACED LEFT P3 VALVE IAW EMB AMM 36-10-03. ALL OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 2008051400147 20080514 00147 NM 2008 5 14 SWAA082545 1 20080510 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 402WN 29814 R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008051400149 20080514 00149 EA 2008 5 14 SWIA200819598 1 20080502 A 3350 AD20131A INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 919SW 2093 2093 7657 CABIN EMERGENCY LIGHTS AT ROW 5 ARE INOP. REPLACED NR 3 INVERTER ASSEMBLY PER CRJ 200 WDM 33-51-00. ALL EMERGENCY LIGH TS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008051400153 20080514 00153 SO 2008 5 14 SWIA200819599 1 20080506 A 2435 CONTACTOR EMB 120 EMB120ER 3260203 SO APU GENERATOR DIRTY A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 235SW 120310 CREW REPORTS AN ELECTRICAL SMELL COMING FROM THE APU CONTACTOR. INSPECTED AND CLEANED CONTACTS FROM APU GENERATOR CONTA CTOR. NO DISCREPENCIES NOTED. 2 L 7 2 4T RT A31SO 2008051400154 20080514 00154 NM 2008 5 14 SWAA082546 1 20080509 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 413, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008051400159 20080514 00159 EA 2008 5 14 SWIA200819602 1 20080215 A 2710 BUSHING CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 971SW 7947 FOUND AT C-CHECK, HORIZONTAL STABILIZER HINGE BUSHINGS AND INNER PIN SHOWS SIGNS OF WEAR. REPLACED STABILIZER HINGE PIN AND BUSHINGS IAW CRJ200 AMM SUBTASK 12-20-27-640-008. 2 L 7 2 4F RT A21EA 2008051400161 20080514 00161 EA 2008 5 14 SWIA200819603 1 20080215 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 971SW 7947 FS 484 AT LBL 36 INTERCOSTAL IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO601R-53-059 REV A. 2 L 7 2 4F RT A21EA 2008051400164 20080514 00164 NM 2008 5 14 SWAA082602 1 20080512 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008051400165 20080514 00165 EA 2008 5 14 MALA080087 1 20080501 A 5753 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING TE FLAP DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 8944B 7944 LT WING, INBOARD FLAP LOWER SKIN DENTED AT TRAILING EDGE, INBOARD CORNER, MEASURING 3 INCH LONG BY 4 INCH WIDE BY .050 I NCH DEEP. REPAIRED IAW MESABA EOC57020. 2 L 7 2 4F RT A21EA 2008051400170 20080514 00170 NM 2008 5 14 SWAA082586 1 20080512 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND NLG W/W RIGHT CEILING PANEL WEB CUTOUT CRACKED AT RBL 2.7. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 2008051400173 20080514 00173 NM 2008 5 14 AALA200800924 1 20080411 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 916AN 29517 MIA - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. RECONNECTED LOOSE PLUG IN GRILL WALL FOR EMERGENCY LIGHT AT SEAT 22D. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008051400176 20080514 00176 NM 2008 5 14 AALA200800929 1 20080411 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 796AN 30796 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 31C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 31C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051400178 20080514 00178 EA 2008 5 14 MALA080088 1 20080506 A 5753 VANE CNDAIR CL600 CL6002B19 1900309 EA LT WING TE FLAP CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 8965E 7965 LT INBD FLAP VANE L/E CHAFED AT INBD STOP CONTACT .020" D. REMOVED I/B FLAP VANE L/E LOCATED AND DRILLED NEW L/E IAW CR J SRM 51-40-11. INSTALLED NEW L/E IAW CRJ SRM 51-42-06. PAINTED LT I/B FLAP VANE L/E STOP IAW CRJ SRM 51-25-26. 2 L 7 2 4F RT A21EA 20080521 NM 2008 5 21 AALA200801027 1 20080420 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 DFW - EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 WP 2008 5 21 AALA200801017 1 20080420 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 428AA 49340 LGA - EMERGENCY LIGHTS IN COACH SECTION INOPERATIVE. REPLACED BATTERY PACK AT B5 2 FOR EMERGENCY LIGHTS IN COACH SECTIO N. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080521 CE 2008 5 21 GUUA04050803 1 20080405 A 5210 10151417617 HANDLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA PAX DOOR WORN A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87550 UE205 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED AIRSTAIR DOOR OUTER HANDLE WORN. REPLACED AIRSTAIR DOOR OUTER HANDLE. 2 L 7 2 4T 3 T RT A24CE E2NE 20080521 NM 2008 5 21 AALA200801015 1 20080419 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 347AN 33086 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 2B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 2B. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080521 NM 2008 5 21 08FDEA01851 1 20080515 A 5320 BAC15171507 FLOOR SUPPORT BOEING 727 727233 138408A NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 220FE 20934 LOWER FWD CARGO COMPARTMENT, FLOOR SUPPORT ANGLE AT STA 580 15, STRINGER 29L IS CRACKED BEYOND STOP DRILL. REMOVED DAMA GE, FABRICATED REPAIR, REF SRM 51-40-04 PAGE 1-9. INSTALLED FLOOR SUPPORT ANGLE REPAIR PARTS REF SRM 51-40-4 PAGE 8. T HIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080521 NM 2008 5 21 F3LA200800268 1 20080515 A 5311 D53571551202 FRAME AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED FRAME 72 DAMAGED AT STRINGER 27 RIGHT. MAINTENANCE REPAIRED IN ACCORDANCE WITH THE R EQUIREMENTS OF EA A9-53R-30262 REV A AND SRM 51-42-11 PARAGRAPH 6. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND F OUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080521 NM 2008 5 21 F3LA200800269 1 20080515 A 5311 D53571552202 FRAME AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED FRAME 73 DAMAGED FROM STRINGER 26 LEFT TO 26 RIGHT. MAINTENANCE REPAIRED FRAME IN AC CORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30262 AND SRM 51-42-11 PARAGRAPH 6. UPON COMPLETION OF THE REPAIR IT WAS IN SPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080521 EA 2008 5 21 MASA200800350 1 20080428 A 3234 533407 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA LANDING GEAR MALFUNCTIONED A MASA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 508MJ 7519 10087 ASH FLT 7156 IAD-AUS - GEAR UP- GEAR DISAGREE WARNING MESSAGE. DECLARED EMERGENCY. REPLACED SELECTOR VALVE, OPS AND LE AK CHECK GOOD. 2 L 7 2 4F RT A21EA 20080520 CE 2008 5 20 DXTA200803037 1 20080501 A 3260 387 LAMP CESSNA 560 560XL 2076702 CE INSTRUMENT PNL BURNED OUT E DXTA O OTHER O OTHER DE DESCENT 1 GL 07 594QS 5605697 NOSE GEAR INDICATOR LIGHTS INOPERATIVE. REPLACED BOTH NOSE GEAR INDICATOR BULBS WITH NEW BULBS IAW MM 32-61-00. OP'S CH ECKED OKAY. 2 L 7 2 4F RT A22CE 20080520 2008 5 20 20082 4 20080428 A 2215 501111201 SERVO LEAR 35 35A 5170602 CE AUTOPILOT SYS UNKNOWN E V6NA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 19 39HJ 337 AT APPROXIMATELY 18,000 FT, VMC, PIC NOTED AUTOPILOT HAD DIFFICULTY BANKING AND TURNING LEFT. AUTO PILOT WAS DISENGAGED AND YAW DAMPERS SWITCHED WITH NEG RESULTS FOR LEFT TURN. PIC ESTIMATES 35 LBS OF FORCE WAS USED TO OVERCOME RESISTANCE WHILE TURNING LEFT. DURING APPLICATION OF LEFT FORCE TO YOKE, CONTROLS "BROKE FREE" AND OPERATED NORMALLY. A/C WAS RT B WITH UNEVENTFUL LANDING. SUBSEQUENT CHECK OF ENTIRE AILERON FLIGHT CONTROL SYSTEM FOUND SYSTEM TO BE NORMAL WITH NO I NDICATION OF FOD. GROUND CHECKS OF AUTO PILOT FOUND AUTO PILOT OPERATING NORMALLY. ROLL SERVO P/N 501-1112-01 S/N 1753 A CHANGED AS PRECAUTION AND PIREP OF MEETING RESISTANCE WHILE TURNING LEFT VS HARD LOCK UP. 2 L 7 2 4F A10CE 20080520 CE 2008 5 20 DXTA200803043 1 20080504 A 3260 WARNING LIGHT CESSNA 680 680CE 2076811 CE COCKPIT ILLUMINATED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 357QS 6800155 AFTER RAISING THE GEAR ON DEPARTURE FROM CLE, THE 3 GREEN GEAR LIGHTS EXTINGUISHED BUT THE UNLOCK LIGHT REMAINED ON. JA CKED ACFT. INSPECTED LANDING GEAR AND RETRACT/EXTEND COMPONENTS. SWANG GEAR MULTIPLE TIMES. COULD NOT DUPLICATE DESCREPA NCY. ALL OPS CHECKS GOOD. IAW MM 32-00-00. 2 L 7 2 4F RC T00012WI 20080520 NM 2008 5 20 USAA920081012 1 20080502 A 5330 6545775 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 24515 CLT - MAJOR REPAIR - RON - CRACKED FUSELAGE SKIN, BS 727E, S24R. REPAIRED FUSELAGE SKIN, BS 727E, S24R IAW B737 SRM 53- 00-01 AND USAIRWAYS TR 53-33. 2 L 7 2 4F RT A16WE 20080520 NM 2008 5 20 USAA920081017 1 20080507 A 5320 143N8338 INTERCOSTAL BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924UW 22204 PIT - MAJOR REPAIR - C3 - CORROSION ON L2 DOOR INTERCOSTAL AT THE UPPER HINGE AREA. REPLACED THE L2 DOOR INTERCOSTAL AT THE UPPER HINGE AREA IAW USAIRWAYS EA 5304R143. 2 L 7 2 4F RT A2NM 20080520 2008 5 20 DXTA200803049 4 20080508 A 2210 701700098826 COMPUTER CESSNA 500 560CESSNA 2076750 CE FWD E/E BAY INOPERATIVE E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 802QS 5600706 AUTOPILOT DISENGAGED TWICE ON CLIMB-OUT ON PFD1. REMOVED AND REPLACED 1IC-615 AND C/W SYS. OPS CHECK IAW MM 34-23-10 2 L 7 2 4F RT A22CE 20080520 NM 2008 5 20 SB08026 1 20080506 A 3297 654976730 WIRE HARNESS BOEING 737 7374B7 1384702 NM NLG FAULTY A USAA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 EA 19 457UW 25021 BOS - FLT738 - AFTER TAKEOFF FROM BOS, EN ROUTE TO PHL, CREW NOTICED THE AIRCRAFT WAS NOT PRESSURIZING. PROBLEMS WERE A LSO NOTED WITH ACARS, AUTO THROTTLES, MODE CONTROL AND OTHER AVIONICS’. CREW FELT THE AIRCRAFT WAS SENSING IT WAS ON TH E GROUND, NOT IN THE AIR. CAPTAIN DECIDED TO RETURN TO FIELD AT BOS. NO EMERGENCY WAS REPORTED AND A NORMAL LANDING WAS MADE. MAINTENANCE SUSPECTS A BROKEN WIRE. REMOVED AND REPLACED NLG AIR/GROUND SENSOR HARNESS. ALSO, REMOVED AND REPLAC ED RELAYS R320 AND R279 ALONG WITH CIRCUIT BOARD M990. ACCOMPLISHED SATISFACTORY NLG SAFETY SENSOR TEST PER MM 32-09-01 -725-008, MLG SAFETY SENSOR TEST PER MM 32-09-01-715-015 AND M990 CIRCUIT CARD TEST PER MM 32-09-20-844-048. 2 L 7 2 4F RT A16WE 20080520 NM 2008 5 20 F3LA200800261 1 20080425 A 5313 D53571532220 STRINGER AIRBUS A319 A319111 3930336 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED STRINGER 32 LEFT IS CRACKED AT FRAME 73. MAINTENANCE REPLACED STRINGER SECTION IN AC CORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30262. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20080520 SO 2008 5 20 LR7A08053 1 20080513 A 5312 342582 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE BUCKLED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND LT AFT FUSELAGE INTERIOR SIDE BHD BUCKLED AT FS 880, WL200, LBL66. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-17. 2 H 7 4 4T A1SO 20080520 SO 2008 5 20 LR7A08054 1 20080513 A 5522 3539381R SKIN LKHEED 382 382G 526414U SO RT ELEVATOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK, FOUND RT ELEVATOR INBD TRAILING EDGE SKIN CRACKED AT HSS52R. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-12. 2 H 7 4 4T A1SO 20080520 SO 2008 5 20 LR7A08059 1 20080513 A 5320 3417493 STIFFENER LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5321, FOUND FUSELAGE EXTERIOR UPPER SKIN STIFFENER CRACKED AT FS 1039, WL286, BL0.0. REPAIR ACCOMPLISHED BY FABRICATING AND REPLACING STIFFENER IAW SMP583 CHAP 51-60 AND 51-70. 2 H 7 4 4T A1SO 20080520 WP 2008 5 20 RYNA200800018 1 20080417 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 932RD 49233 PASSENGER CABIN LEFT INBOARD SEAT TRACK IS CORRODED AT BS 731. REPAIRED CORRODED AREA IAW MD-80 SRM 51-10-03. 2 L 7 2 4F A6WE 20080520 NM 2008 5 20 2008UALA02661 1 20080507 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 AFT PIT STA 1540 STR 26L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGE AND INSTALLED "J" ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080520 NM 2008 5 20 2008UALA02667 1 20080507 A 2612 330TS08Y PANEL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 815UA 867 'ENGINE FIRE EXTINGUISHING-SQUIB' LIGHT OF 'AGENT 1' PUSH BUTTON SWITCH IS OFF DURING 'LOOP-SQUIB TEST'. CREW COMMENTS, ENG 2 SQUIB LIGHT DOESN'T ILLUMINATE ON TEST. FOUND FIRE PANEL SHORTED. REPLACED FIRE PNL OP'S NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080520 SO 2008 5 20 LR7A08065 1 20080513 A 2120 3779101 MOUNT BRACKET LKHEED 382 382G 526414U SO CARGO BAY CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC2111, FOUND CARGO AIR CONDITION AUX VENT DUCT MOUNTING BRACKET CRACKED. WELD REPAIR ACCOMPLISHED IAW LAC MEA 382-21-08-032. 2 H 7 4 4T A1SO 20080521 NM 2008 5 21 2008UALA01760 1 20080329 A 2421 734285E GCU BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 FAULTED A UALA O OTHER J W WARNING INDICATION INADEQUATE Q C CR CRUISE 1 WP 29 647UA 25284 EICAS MSG L GEN OFF DISPLAYED. SUSPECT FAULTY BEARING IDG. REPLACED GENERATOR PER AMM24-11-01 AND GCU PRECAUTIONARY O PS CHECKED NORMAL. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080521 SO 2008 5 21 LR7A08072 1 20080513 A 5312 CAP LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND AFT FUSELAGE INTERIOR BULKHEAD INBD CAP CRACKED AT FS792, WL160, L BL66. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-08-019. 2 H 7 4 4T A1SO 20080521 NM 2008 5 21 AALA200801028 1 20080420 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 DFW - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801012 1 20080418 A 3350 LIGHT BOEING 767 767323 1385205 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 347AN 33086 DFW - EXTERIOR EMERGENCY LIGHT AT AFT LEFT OVERWING INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT AFT LEFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080521 NM 2008 5 21 AALA200801024 1 20080420 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 DFW - EMERGENCY LIGHT AT SEAT 33C INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 33C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 CE 2008 5 21 GUUA04090802 1 20080409 A 5210 MS166241075 RETAINING RING BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA DOOR HANDLE DISLODGED A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 87550 UE205 PILOT REPORTED FWD CABIN DOOR HANDLE CAME OFF. REATTACHED RING RETAINER AND SECURED FWD CABIN DOOR. 2 L 7 2 4T 3 T RT A24CE E2NE 20080521 NE 2008 5 21 HCM2008F00000 2 20080411 A 7200 ENGINE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE MAKING METAL E HCMA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 11QL 3738 23074 APPROX 45 MINUTES INTO A TOUR FLIGHT, THE (ENGINE CHIP) WARNING LIGHT ILLUMINATED. PILOT PERFORMED A PRECAUTIONARY LAND ING. MAINT DISPATCHED (ON SIGHT) INSP. REVEALED MANY METAL CHIPS ON THE MODULE 1 AND OIL TANK MAG PLUGS AND FULL FLOW ELECTRICAL CHIP DETECTOR. OIL FILTER CONTAMINATED WITH METAL PARTICLES. ENGINE REMOVED AND REPLACED (ON SIGHT) ENGINE OIL COOLER REPLACED, ALL OIL LINES CLEANED AND FLUSHED. PAST OIL ANALYSIS RESULTS NORMAL, NO HISTORY OF CHIP LIGHTS ETC . SINCE LAST O/H. METAL SENT TO LAB TO BE ANALYZED. SUSPECT ACCY GEARBOX OR MODULE 2 BEARING CAUSING METAL GENERATION . 1 G 7 2 3U 3 U H9EU E00054EN 20080521 NM 2008 5 21 BEFA200800003 1 20080414 A 5315 FLOORBEAM BOEING 757 757200 1384950 NM PWA 2037 PW2040 NE BS 1661 CORRODED A BEFA K NONE O OTHER IN INSP/MAINT 1 WP 19 741PA 55899 24737 AFT CABIN FLOORBEAM AT BS 1661 LBL 48 INCH AND LBL 53.5 CORROSION CLEAN-UP IS BEYOND 10 PERCENT LIMIT IAW SRM. REPLACED FLOORBEAM IAW THE SRM TREATED AND PRIMED AREA. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 EA 2008 5 21 MASA200800404 1 20080515 A 5280 CC67010520966 STRUCTURE CNDAIR CL600 CL6002D24 1390016 EA RT MLG DOOR CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 921FJ 10672 15021 FOUND RT MLG DOOR CROSS MEMBER CRACKED AND SEVERAL LOOSE RIVETS ON INNER SKIN LEADING EDGE NEXT TO FWD HINGE. REPLACED MLG DOOR. 2 L 7 2 4F RT A21EA 20080521 NM 2008 5 21 2008UALA00674 1 20080205 A 3510 89151114 BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW O2 LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 196UA 28715 CREW O2 PRESSURE 1550, SUPPLEMENTAL DATA UPDATE, SUSPECT PRE-FLIGHT CHECKS. SERVICED OXYGEN BOTTLE. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080521 NM 2008 5 21 2008UALA02646 1 20080506 A 2780 284N180022 CONTROL UNIT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L/E FLAP INTERMITTENT A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 502UA 24623 LEADING EDGE FLAP DISAGREE INDICATION. RTFL SFO. FSEU INTERMITTENT FAILURES. REPLACED FSEU NR 3 AND RIGGED PDU TRANSM ITTER AND LEFT SLAT TRANSMITTER. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 NM 2008 5 21 2008UALA02666 1 20080506 A 2810 408846 SHUTOFF VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RIGHT FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 595UA 28748 FUEL CONFIG LIGHT ON. IMBALANCE OF 3000 POUNDS BETWEEN LEFT AND RIGHT TANKS WITH BOTH CROSSFEED. SUPPLEMENTAL DATA UPD ATE, RT FUELING SHUTOFF VALVE INOP. REPLACED RT FUELING SHUTOFF VALVE, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 SO 2008 5 21 C2XA08RI060 1 20080505 A 3200 1170A350001 POTENTIOMETER EMB 145 EMB145XR 3260214 SO ALLSN AE3007 AE3007C GL MLG DEFECTIVE A C2XA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 27 10156 145786 FLIGHT 2678 - FLIGHT CREW REPORTED AIRCRAFT PULLS TO THE RT AT TAKEOFF AT 80 KNOTS. MX REMOVED AND REPLACED FEEDBACK POT ENTIOMETER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 20080521 CE 2008 5 21 DXTA200803050 1 20080508 A 2120 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL CABIN ODOR E DXTA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 07 934QS 7500034 ON POST FLIGHT, FOUND CABIN TO HAVE FOUL ROTTEN SEAFOOD ODOR. FOUND SPILL UNDER LEXAN COVER ON BAR, CLEANED SPILL SMELL S GOOD. IAW M/M 20-32-00. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080521 GL 2008 5 21 U0GA119633 2 20080509 A 7200 250C20B ENGINE BOLKMS 105 BO105CBS 5626008 EU ALLSN 250C 250C20 03013 GL NR 2 INOPERATIVE B U0GA O OTHER O OTHER NR NOT REPORTED 1 SW 03 290EH S850 UPON LANDING, ENGINE 2 MADE AND EXPLOSIVE SOUND. NG WENT TO 0 TORQUE WENT TO 0. FUEL SUPPLY TO ENGINE TO WAS CUT OFF, E NGINE 1 WAS INCREASED TO MAX POWER AND A SUCCESSFUL RUN ON LANDING WAS MADE ON RUNWAY 17. 1 G 7 2 3U 3 U NC H3EU E4CE 20080521 NM 2008 5 21 DU4R2008194 1 20080505 A 5210 STRUCTURE BOEING 737 737448 13844BU NM CFMINT CFM56 CFM563B2 13802 EU L1 DOOR CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 742VA 24773 S/O 312001 OPS NR 24701, CORROSION OUT OF LIMITS ON L-1 DOOR LOWER INNER CHORD AT BS 328,LBL 58 TO LBL 60. 2 L 7 2 4F 4 F RT A16WE E21EU 20080521 CE 2008 5 21 DXTA200803017 1 20080424 A 7932 OIL SYSTEM CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE ENGINE LOW PRESSURE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 672QS 1644 5605663 PCEDD0337 ABORTED T/O, WITH MASTER WARNING LIGHT AND L OIL PRESSURE LOW ILLUMINATED. PRIOR TO T/O ROLL OIL PRESSURE WAS IN THE GRE EN. NO OIL SHOWING IN SIGHT GAGE ON POST FLIGHT. NO OIL LEAKAGE APPARENT PREVIOUS FLIGHTS. POST FLIGHT OIL LEVEL WAS WIT HIN NORMAL RANGE. REPLACED LT ENGINE WITH REPAIRED UNIT IAW MM CHAP 71-00-03. PERFORMED ENGINE ADJUSTMENT/TEST IAW MM CH AP 71-00-04. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E00059EN 20080521 NM 2008 5 21 2008UALA02699 1 20080508 A 2421 6819007 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT FAILED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 590UA 28708 LEFT IDG RECHECK TOOK MORE THAN 75 PUMPS. IDG ARRIVED WORKING. BPP SHOWS LEFT IDG HIGH TEMP AND HIGH RISE LAST TWO LEG S. FUEL/OIL COOLER FAILURE CONTRIBUTED TO IDG FAILURE. REPLACED IDG AND FUEL/OIL COOLER. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 EU 2008 5 21 MALA080094 1 20080515 A 5720 257211515 STRUCTURE SAAB SF340 340B 7860101 EU LT WING DAMAGED A MALA K NONE O OTHER UK UNKNOWN 1 GL 15 418XJ 340B418 JET WAY HIT LT OUTBD WING LEADING EDGE. INSPECTED AIRCRAFT, ONLY DAMAGE FOUND WAS NR 7 POSITION LT OUTBD WING LEADING E DGE. REPLACED NR 7 LT LEADING EDGE IAW SAAB AMM 57-20. OPS CHECKED IAW SAAB AMM 30-10/ PN ON 7257211-515, SEALANT NOT APPLIED SEE BELOW FOR SHORT FUSE WATCH ITEM. 2 L 7 2 4T RT A52EU 20080521 EU 2008 5 21 MALA080092 1 20080505 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 EMERGENCY LIGHTING POWER SUPPLY 21LN AND 23LN FAILED TASK CARD 335003. REMOVED AND REPLACED POWER SUPPLY'S AT 21LN P/N ON/OFF 3301-51 IAW AMM 33-50-10 21LN S/N OFF 2036 S/N ON 2021. 2 L 7 2 4T RT A52EU 20080521 EU 2008 5 21 MALA080093 1 20080505 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 410XJ 340B410 EMERGENCY LIGHTING POWER SUPPLY 21LN AND 23LN FAILED TASK CARD 335003. REMOVED AND REPLACED POWER SUPPLY'S AT 23 LN P/N ON/OFF 3301-51 IAW AMM 33-50-10 23LN S/N OFF 2158 S/N ON 2059. 2 L 7 2 4T RT A52EU 20080521 NM 2008 5 21 AALA200801071 1 20080424 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT SEAT 33G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 33G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801076 1 20080424 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801079 1 20080424 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT SEAT 30C AFT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 30C. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801078 1 20080424 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN WRONG PART A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT SEAT 21C DIM. FOUND WRONG LAMPS INSTALLED. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801092 1 20080426 A 3350 SHROUD BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 962AN 30858 DFW - EMERGENCY LIGHT AT SEAT ROW 16DEF MISSING SHROUD. REPLACED SHROUDS FOR EMERGENCY LIGHT AT SEAT ROW 16DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 NM 2008 5 21 AALA200801098 1 20080426 A 1100 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 187AN 32381 DFW - EMERGENCY EXIT DECAL AT AFT LEFT FORWARD GALLEY DOOR DAMAGED. REPLACED DECAL FOR EMERGENCY EXIT LIGHT AT AFT LEFT FORWARD GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080521 NM 2008 5 21 AALA200801083 1 20080424 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT SEAT 24G INOPERATIVE. REPLACED LIGHT HOUSING ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 24G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 EU 2008 5 21 AALA200801101 1 20080427 A 2910 DRAIN LINE AIRBUS 300 A300B4605R 3930308 EU RT ENGINE LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 70072 515 SJU INFLIGHT T1845/27APR - DURING CRUISE, GREEN HYDRAULIC QUANTITY DROPPED TO ZERO. LANDING GEAR LOWERED MANUALLY. CR EW DECLARED AN EMERGENCY AND LANDED SJU WITHOUT INCIDENT. FOUND NUMBER TWO ENGINE HYDRAULIC PUMP CASE DRAIN LINE LEAKIN G AT B NUT. TIGHTENED CASE DRAIN LINE AND REPLACED ENGINE DRIVEN PUMP AND CASE DRAIN FILTER. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A35EU 20080521 NM 2008 5 21 AALA200801093 1 20080426 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 962AN 30858 DFW - EMERGENCY LIGHT AT BULLNOSE OVERHEAD SEAT ROW 22ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT BULLNOSE OV ERHEAD SEAT ROW 22ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 WP 2008 5 21 AALA200801061 1 20080423 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9620D 53591 TUL - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD SEAT ROW 6 FAILED TEST. REPLACED BATTERY PACK AT OVERHEAD SEAT 6 FOR EME RGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080521 NM 2008 5 21 AALA200801069 1 20080424 A 2781 PROXIMITY SENSOR BOEING 737 737823 13844BZ NM L/E SLAT DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 902AN 29504 LAX INFLIGHT T437/24APR DFW TO SNA - CREW REPORTED AMBER LEADING EDGE FLAP INDICATION WITH AMBER NUMBER THREE SLATS TRA NSIT LIGHT. FLIGHT DIVERTED TO LAX. LANDED WITHOUT INCIDENT. REPLACED SLAT NUMBER THREE INBOARD PROXIMITY SENSOR. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 NM 2008 5 21 AALA200801040 1 20080421 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 TUL - SEAT MOUNTED EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED TEST. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 NM 2008 5 21 AALA200801036 1 20080421 A 5210 BOTTLE BOEING 757 757223 1384957 NM R1 DOOR DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 608AA 27446 SAL - RIGHT NUMBER ONE DOOR SLIDE UNSUCCESSFULLY DEPLOYED. DISARM POSITION LEVER WAS HALF WAY BETWEEN ARM AND DISARM WH EN FLIGHT ATTENDANT STARTED TO OPEN THE DOOR AND HEARD A HISSING NOISE AND CLOSED THE DOOR. POWER ASSIST BOTTLE DISCHAR GED AND GIRT BAR DETACHED. SLIDE REMAINED IN PACK. REPAIRED GIRT BAR. REPLACED RIGHT NUMBER ONE SLIDE AND POWER ASSIS T BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080521 NM 2008 5 21 AALA200801048 1 20080422 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801049 1 20080422 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801050 1 20080422 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT AT SEAT 26C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801051 1 20080422 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN WRONG PART A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT AT SEAT 10G NOT LED BLUE LIGHT. REPLACED ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 10G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801041 1 20080422 A 3350 LIGHT BOEING 767 767323 1385205 NM EXTERIOR INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 372AA 25199 DFW - EXTERNAL EMERGENCY LIGHT AT LEFT AFT OVERWING INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LEFT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080521 NM 2008 5 21 AALA200801046 1 20080422 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AA 27054 DFW - EMERGENCY LIGHT AT SEAT 16D BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080521 WP 2008 5 21 AALA200801056 1 20080422 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9620D 53591 TUL - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD SEAT ROW 13 FAILED TEST. REPLACED BATTERY PACK AT OVERHEAD SEAT 13 FOR E MERGENCY LIGHTS IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080521 WP 2008 5 21 AALA200801057 1 20080422 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9620D 53591 TUL - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD SEAT ROW 25 FAILED TEST. REPLACED BATTERY PACK AT OVERHEAD SEAT 25 FOR E MERGENCY LIGHTS IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080521 NM 2008 5 21 AALA200801082 1 20080424 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT SEAT 44C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 44C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 WP 2008 5 21 AALA200801063 1 20080423 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 429AA 49341 LGA - EMERGENCY LIGHT AT OVERHEAD FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK AT B5 23 FOR EMERGENCY LIGHT AT OVERHE AD FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080521 NM 2008 5 21 AALA200801073 1 20080424 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT SEAT 25G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080520 NM 2008 5 20 2008UALA02654 1 20080507 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 CORROSION ON SHEAR TIE AT STA 1241, STR 38R TO 39R. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080520 NM 2008 5 20 2008UALA02669 1 20080507 A 2613 6937307149 MODULE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE OVERHEAT SYS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 330UA 24191 NR 1 OVERHEAT LIGHT FAILS TO COME ON DURING TEST. REPLACED THE ENGINE AND APU FIRE CONTROL MODULE PER MM26-21-51. AC O K FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 20080520 NM 2008 5 20 2008UALA02529 1 20080429 A 2121 217N11521 BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COOLING VALVE FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 545UA 25323 E/E VALVE IS CLOSED W-NO AIR COMING OUT. BEARING FAILURE IN UNIT. REPLACED EQUIPMENT COOLING VALVE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080520 NM 2008 5 20 2008UALA02652 1 20080506 A 5311 146N1022 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 AFT PIT BS 1620 AT STR 26L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED, CUTOUT DAMAGE. INSTALLED 'J' ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 NM 2008 5 21 2008UALA02748 1 20080510 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 546UA 25367 EXTERIOR EMERGENCY LIGHT INOP AT DOOR 3L. RELAMPED, OPS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 NM 2008 5 21 2008UALA02753 1 20080510 A 3350 8100033901 LENS BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 784UA 26951 EMERGENCY AISLE LIGHT IS MISSING LENS ON SEAT 1E. LENS MISSING ON SEAT 2E. SUSPECT FAULTY LIGHT ASSEMBLY. REPLACED 1E EEL LIGHT AND OPS NORMAL. SEAT 2E ALSO TESTS NORMAL. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080521 NM 2008 5 21 2008UALA02764 1 20080513 A 2613 WARNING SYSTEM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE OVERHEAT SYS ACTIVATED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 934UA 26662 RTFL DUE TO A WING/BODY OVERHEAT INDICATION. NORMAL LANDING. 2 L 7 2 4F 4 F RT A16WE E2GL 20080521 NM 2008 5 21 AALA200801021 1 20080420 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 DFW - EMERGENCY LIGHT AT SEAT 25G INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 25G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 EU 2008 5 21 08FDEA01856 1 20080515 A 5347 A5361252420002 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 MAIN DECK CARGO SEAT TRACK NR 3 RT HAS CORROSION AT FR 18 REMOVED LEVEL 1 CORROSION. REMOVED AND REPLACED SEAT TRACK NR 3 RT, BETWEEN FR 15A AND FR 19 WITH NEW PART IAW A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 2008051400180 20080514 00180 WP 2008 5 14 DHL2008807511 1 20080509 A 5330 PANEL DOUG DC8 DC873F 302199F WP BS 980-1050 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 WING TO FUS LWR PANEL NR 732 INTERNAL SKIN DELAMINATED (STA 980.000 - 1050.000). REMOVED WING TO FUS LWR PANEL NR 732 I AW SRM 51-3-0. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PANEL IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 2008051400223 20080514 00223 EA 2008 5 14 A6WA200840333 1 20080411 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA ILLUMINATED A A6WA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 431AW 7256 DISPLAY COOL MSG IN FLIGHT, FOLLOWED QRH MSG STAYED ON IN STANDBY FAN POSITION DIVERTED TO PHL MSG WENT OUT INBOUND OF P HL AFTER 10-15 MINUTES. (M) 2 L 7 2 4F RT A21EA 2008051400224 20080514 00224 NE 2008 5 14 2008UALA02532 2 20080501 A 7261 LINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OIL SYSTEM LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 411UA 464 V10327 A/C LOSING OIL QUANTITY. FLIGHT DIVERTED. OIL SUPPLY PRESSURE TUBE FOUND DAMAGED AND LEAKING. TUBE REPLACED CORRECT TH IS CONDITION. 2 L 7 2 4F 4 F RT A28NM E40NE 2008051400225 20080514 00225 NM 2008 5 14 2008UALA02533 1 20080501 A 2421 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 581UA 26701 726630 RTFL DUE TO NR 1 ENGINE GENERATOR FAILURE. REPLACED IDG, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008051400228 20080514 00228 NM 2008 5 14 2008UALA02535 1 20080430 A 3510 S417N4402 VALVE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CREW OXYGEN LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 303UA 23644 CREW REPORT, SERVICE COCKPIT O2, 820 PSI AT 6C. FOUND LEAK AT EXTERNAL FILLER VALVE. REPLACED VALVE ASSEMBLY PER MM35 -12-81. SERVICED TO 1800 PSI NO LEAKS. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008051400230 20080514 00230 NM 2008 5 14 2008UALA02538 1 20080430 A 4900 MR49112 APU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 APU FAILED TO START. FAULT LIGHT ILLUMINATED AND EICAS MSG APU FAULT DISPLAYED. APU HAD OVER 6,000 CYCLES AND WAS REPL ACED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080520 NM 2008 5 20 UIEA200800178 1 20080509 A 5730 SKIN PANEL BOEING 747 747228F 1384895 NM LT WING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 LT WING UPPER FIXED L/E PANEL DELAMINATED, INBOARD OF NR 2 ENGINE, 8.0 INCHES FROM AFT EDGE OF PANEL AT ILES STA 545.56. AREA OF DELAMINATION IS 2.0 BY 2.0 INCHES. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 18, SHEETS 3 AND 5 PREPREG 250 DEGREES CURE PER SRM 51-40-12. REF: ATLAS AIR EO NR 4757A438. 2 L 7 4 4F RT A20WE 2008051400233 20080514 00233 2008 5 14 2008UALA02542 4 20080430 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 405UA 452 DOOR 1L SLIDE-RAFT GIRT RUBS ON FLOOR AFTER INSTALLATION AND GIRT IS FRAYED. FOUND WEAR AND IMPROPER LANYARD INSTALLATIO N. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008051400248 20080514 00248 NM 2008 5 14 SWAA082608 1 20080512 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 8L CRACKED AT BS 500A. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008051500006 20080515 00006 NM 2008 5 15 HALA0800576 1 20080506 A 2697 CONNECTOR BOEING 717 717200 1383700 NM B FIRE LOOP LOOSE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 479HA 55124 LEFT ENG FIRE LOOP B DOES NOT TEST. FOUND LOOSE CONNECTOR ON FIRE LOOP B REPLACED CONNECTOR PER WDM 26-11-00, OPS OKAY PER AMM 26-11-00, OPS CK GOOD. 2 L 7 2 4F TR A6WE 2008051500007 20080515 00007 2008 5 15 WGEA200800056 4 20080507 A 3410 70000078103 DISPLAY ECLIPS EA500 ECLIPSEEA500 3350000 SW ZONE 100 FAILED E WGEA O OTHER G MULTIPLE FAILURE CL CLIMB 1 EA 27 152DJ 64 000071 AFTER TAKEOFF, CASS MESSAGE AS/ALT DISAGREE, YD FAIL, RED X RIGHT ATT/AS/ALT FOR DURATION OF FLIGHT. MFD RED X ATT ONLY . REMOVED AND REPLACED RT PFD WITH REPAIRED UNIT IAW EA5OO AMM 31-10-16. PERFORMED DISPLAY AND CONTROL PANEL-ADJ/TEST IAW EA500 AMM 31-10-00 AND TRANSPONDER SYSTEM ADJ/TEST IAW EA500 AMM 34-50-60. ALL CHECKS GOOD. VERIFIED TRANSPONDER N R 1 AND NR 2 COMPLY WITH FAR 91 .413, AND FAR PART 43 APP F. PERFORMED ALTITUDE REPORTING CORRELATION TEST PER PARA OF FAR PART 43 APP E, NO DATA CORRESPONDENCE ERRORS FOUND FOR TRANSPONDER NR 1 OR NR 2. 1 L 7 2 4J RT A00002AC 2008051500013 20080515 00013 SO 2008 5 15 SIMA200813402 1 20080508 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 900AE 14500885 ON FLIGHT 4401, CREW REPORTED OVER HEAD EMERGENCY LIGHT INOPERATIVE IN CABIN AIRCRAFT FROM SERVICE. FOUND COCKPIT FLOO DLIGHT AND LT FORWARD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT POWER SUPPLY AND BATTERY. FOUND WIRING SPLICE SP9003 BROKEN. REPAIRED SPLICE AND FOUND NR 1 EMERGENCY LIGHT POWER SUPPLY INOPERATIVE AGAIN DUE TO NO FAULT PROTECTION ON THIS CIRCUIT. REMOVED AND REPLACED NR 1 EMERGENCY POWER SUPPLY. OPERATIONAL CHECK GOOD. ALL LIGHTS WORKING NORMALLY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008051500023 20080515 00023 NM 2008 5 15 2008UALA02543 1 20080430 A 3350 LAMP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 930UA 26655 DOOR 1R EXTERIOR EMERGENCY LIGHT IS INOP. SUSPECT FAULTY LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008051500025 20080515 00025 NM 2008 5 15 2008UALA02545 1 20080501 A 5330 65B23791 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 2193 GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 ON ARRIVAL AT HKG, FOUND 3.5 DIA GOUGE AT FUSELAGE SKIN STA 2193 AND WL 200. DAMAGED AREA REPAIRED AS EVA-71460B AND IN SPECTION CHECKED SATISFACTORY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008051400094 20080514 00094 EU 2008 5 14 TRAX200800592 1 20080502 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 631AS 362 ASD EMERGENCY LIGHT INOP. REMOVED AND REPLACED ASD EMERGENCY LIGHT ASSY IAW ATR 72 JIC 33-51-05. CHECKED GOOD. 2 H 7 2 4T RT 2008051400098 20080514 00098 NM 2008 5 14 CALA0800419 1 20080507 A 5313 65C32357 STRINGER BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 32626 27530 FORWARD FUSELAGE LOWER LEFT-SIDE AT STATION 363.9, .5 INCH INBOARD OF S28L GOUGE APPROX .25 INCH IN DIA. FABRICATED AND INSTALLED REPAIR PER ECRA 5330-03803. 2 L 7 2 4F RT A16WE 2008051400126 20080514 00126 NM 2008 5 14 SWAA082527 1 20080511 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 220WN 32491 DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008051400238 20080514 00238 NM 2008 5 14 SWAA082529 1 20080511 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 910, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008051400241 20080514 00241 NM 2008 5 14 SWAA082533 1 20080511 A 5311 6546541 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 1. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2008051400244 20080514 00244 NM 2008 5 14 SWAA082538 1 20080511 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008051400245 20080514 00245 NM 2008 5 14 SWAA082539 1 20080511 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008051400246 20080514 00246 NM 2008 5 14 SWAA082588 1 20080512 A 2560 6557463 FITTING BOEING 737 7375H4 138449D NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 2008051400249 20080514 00249 NM 2008 5 14 SWAA082610 1 20080512 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008051500012 20080515 00012 WP 2008 5 15 NWAA082039863 1 20080512 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 772NC 47774 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN LIGHT FOR THE FWD LEFT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE EXIT LIGHT RETURNED TO AN OPERATIONAL CONDITION. 2 L 7 2 4F RT A6WE 2008051500045 20080515 00045 WP 2008 5 15 08FDEA01732 1 20080502 A 5753 ARC01542 FRAME DOUG MD10 MD1010F 3022112 WP RT WING TE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 RIGHT WING T/E FLAP OUTBD ACTUATOR FAIRING, OUTBD L/E UNDER FAIRING MOUNT FRAME HAS 2 GOUGES. BLENDED GOUGES AND FOUN D 1 EACH 0.030 DEEP TO BE OUT OF LIMITS IAW CMM 57-44-01. FABRICATION OF ANGLES WAS ACCOMPLISHED ON N/R N01025. REMOVED CLIPS FABBED IAW SRM 57-20-00; VOL I. ALODINED; PRIMED & PAINTED IAW SRM 51-21-01; VOL II. INSTALLED ANGLES IAW SRM 57-70-00. 2 L 7 3 4F RT A22WE 2008051500051 20080515 00051 NM 2008 5 15 KNNA20080005 1 20080424 A 5314 KEELBEAM BOEING 737 7372L9 1384497 NM PWA JT8 JT8D9A 52048 NE BS 725-727 CORRODED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 464AT 21278 AFTER OPEN UP, FOUND CORROSION AT RT KEEL BEAM AT STA 727, AREA WENT OUT OF LIMITS AFTER CORROSION REMOVAL. REPAIRED AR EA IAW BOEING MESSAGE 1-522105282 AND IAW SKY KING ACO-0753105. 2 L 7 2 4F 4 F RT A16WE E2EA 2008051500055 20080515 00055 WP 2008 5 15 UPS08852112 1 20080424 A 5712 RIB DOUG DC8 DC873F 302199F WP RWS 434 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 RT WING CENTER LE UPPER RIB CRACKED XFS 434. REPAIRED RT WING CENTER LE RIB AT XFS 434 IAW SRM 57-02 -00-0 FIG 002 AND SRM 57-03-03-0. 2 L 7 4 4F RT 4A25 2008051500057 20080515 00057 NM 2008 5 15 DHL2008760518 1 20080416 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272B7 138407L NM BS 690-740 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND REPLACED SEAT TRACK SECTION AT LBL 24, FROM BS 690 TO 740, PER B727 SRM 53-10-2 FIG 7 AND 53-10 -5 FIG 1. 2 L 7 3 4F A3WE 2008051500060 20080515 00060 NM 2008 5 15 AALA200800869 1 20080408 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 755AN 30263 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE FORWARD CLOSET BROKEN. REPLACED LIGHT ASSEMBLY AT LEFT NUMBER ONE FORWARD CLOS ET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500063 20080515 00063 NM 2008 5 15 AALA200800894 1 20080409 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 185AN 32379 DFW - EXTERNAL EMERGENCY LIGHT AT AFT LEFT SERVICE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT AFT LEFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051500064 20080515 00064 NM 2008 5 15 AALA200800866 1 20080408 A 3350 1317 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 681AA 25338 JFK - EMERGENCY LIGHT AT RIGHT SEAT ROW 21 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT SEAT ROW 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051500066 20080515 00066 EU 2008 5 15 AALA200800875 1 20080408 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 41063 506 JFK - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008051500067 20080515 00067 EU 2008 5 15 AALA200800876 1 20080408 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 41063 506 JFK - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBE R ONE DOOR EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008051500072 20080515 00072 WP 2008 5 15 AALA200800888 1 20080409 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 430AA 49342 LGA - EMERGENCY LIGHTS AT CAT WALK INOPERATIVE. REPLACED BATTERY PACK AT AFT LAVATORY FOR EMERGENCY LIGHTS AT CAT WALK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008051500073 20080515 00073 NM 2008 5 15 AALA200800889 1 20080409 A 2611 644501 CIRCUIT CARD BOEING 757 757223 1384957 NM FIRE DETECTION INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 634AA 24592 SJU INFLIGHT T809/09APR - CREW REPORTED NUMBER TWO ENGINE FIRE LOOP ONE STATUS MESSAGE DURING CLIMB. RETURNED TO SJU A ND LANDED WITHOUT INCIDENT. NO FIRE. REPLACED NUMBER TWO ENGINE FIRE LOOP ONE DETECTOR CARD M683. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051500078 20080515 00078 NM 2008 5 15 AALA200800886 1 20080408 A 3350 OL3071BPEGPL LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHT AT SEAT 21G MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500079 20080515 00079 NM 2008 5 15 AALA200800887 1 20080408 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHT AT SEAT 21G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500080 20080515 00080 NM 2008 5 15 AALA200800905 1 20080410 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 756AM 30264 DFW - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500081 20080515 00081 NM 2008 5 15 AALA200800906 1 20080410 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 756AM 30264 DFW - EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500082 20080515 00082 NM 2008 5 15 AALA200800907 1 20080410 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 756AM 30264 DFW - EMERGENCY LIGHT AT SEAT 31G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500088 20080515 00088 NM 2008 5 15 F3LA200800216 1 20080501 A 5321 D5367150500000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CABIN PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED CABIN FLOOR PANEL 252HF HAS A PUNCTURE IN THE TOP SURFACE. MAINTENANCE CLEANED AR EA, PREPPED AND APPLIED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PARAGRAPH 8A AND SRM 53-20-00 PARAGRA PH 8A. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008051500093 20080515 00093 NM 2008 5 15 AALA200800912 1 20080410 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 756AM 30264 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK M33094 FOR SEAT MOUNTED EME RGENCY LIGHTS AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500095 20080515 00095 NM 2008 5 15 AALA200800926 1 20080411 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 945AN 30085 DFW - EMERGENCY LIGHT AT FORWARD GALLEY AISLE MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FORWARD GALLEY AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008051500099 20080515 00099 NE 2008 5 15 SWIA200819574 2 20080428 A 7200 CF343B1 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LEFT MALFUNCTIONED A SWIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 07 924SW 17136 17136 7681 FLT 6723 - LEFT ITT CLIMBED TO 903°C AND TAKEOFF WAS ABORTED. REPLACED LEFT ENGINE ASSEMBLY IAW AMM 71-00-00. OPS CHEC K AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 2008051500101 20080515 00101 EA 2008 5 15 SWIA200819576 1 20080502 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 866AS 7517 FLT 3951 - MAIN CABIN EMERGENCY EXIT SIGN IS BROKEN. REPLACED MAIN CABIN EMERGENCY EXIT LIGHT ASSEMBLY. 2 L 7 2 4F RT A21EA 20080521 NE 2008 5 21 KCSA08035 2 20080514 A 7200 ENGINE BOEING 747 7472B4B 138481B NM PWA JT9 JT9D7J 52054 NE NR 2 FLAMED OUT A KCSA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 23 710CK 21097 685734 NR 2 ENG SURGED DURING CONSTANT PWR, ENG WAS SHUT DOWN (FLAME OUT). EPR 1.1, ENG BLEED OPEN, ANTI-ICE - OFF, IGN SW - O FF, FLT MODE - CRUISE, ALT - 31,100 FT, .84 MACH, NO ICING, NO TURB. 2 L 7 4 4F 4 F RT A20WE E20EA 20080521 NM 2008 5 21 2008UALA02674 1 20080507 A 5210 F1314 SPRING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE R2 DOOR DEFECTIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 656UA 25394 R2 DOOR FWD DEPLOYMENT CABLE RETRACTOR STICKS, CABLE DOES NOT RETRACT. REPLACED GAS SPRING. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20080521 NM 2008 5 21 31522 1 20080508 A 2540 LAVATORY EMB ERJ170 ERJ170200LR 3260121 NM BURNED A C77A A UNSCHED LANDING A FLAME/FIRE CR CRUISE 1 EA 27 620CZ 271 17000214 AIRLINES FLIGHT HAD A FIRE IN THE AFT LAVATORY. THE FLAMES WERE COMING FROM THE PAPER TOWEL/ TISSUE HOLDER. THERE IS DA MAGE TO THE COMPLETE LAVATORY ASSEMBLY. NO FURTHER INFORMATION IS AVAILABLE. 2 L 7 2 4F RT A56NM 20080521 CE 2008 5 21 GLBA20061095 1 20080501 A 5313 STRINGER BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BS 451 S10R CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 154GL UE154 STRINGER 10R CRACKED AT F.S. 451. CRACK LENGTH APPROXIMATELY.5 INCH. MAINT REPAIRED STRINGER 10R FLANGE AT F.S. 451 I.A. W. BEECH 1900D SRM 51-70. REPAIR DIMENSION APPROX 7.5 INCH BY 1 INCH. 2024-T3 .050 INCH. RII INSPECTION COMPLIED WITH IA W TASKCARD 8.2.1. 2 L 7 2 4T 3 T RT A24CE E2NE 20080521 NM 2008 5 21 2008UALA02698 1 20080506 A 2760 61GB191A320 RELAY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SPOILER SYS FAILED A UALA O OTHER W INADEQUATE Q C LD LANDING 1 WP 29 549UA 25397 SPOILERS ONLY PARTIALLY DEPLOYED ON LANDING. RELAY K217 FAILED ELECTRICALLY. REPLACED AUTO SPEEDBRAKE RELAY (EXTEND) K 217, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 EU 2008 5 21 MALA080095 1 20080514 A 5347 7253721495 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 452XJ 340B452 RIGHT FORWARD GALLEY SEAT TRACK CORRODED. REPLACED SEAT TRACK P/N 7253721-459 AND PROFILE P/N 7253721-495 IAW SRM 51-40 -21 AND 51-40-22. 2 L 7 2 4T RT A52EU 20080521 NM 2008 5 21 AALA200801095 1 20080426 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 962AN 30858 DFW - EMERGENCY LIGHT AT BULLNOSE OVERHEAD SEAT ROW 25ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT BULLNOSE OV ERHEAD SEAT ROW 25ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 NM 2008 5 21 AALA200801080 1 20080424 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT SEAT 32C INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 32C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801039 1 20080421 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 TUL - SEAT MOUNTED EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED TEST. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 2008 5 21 AALA200801043 4 20080422 A 2565 62772216 SLIDE BOEING 777 777223 1385213 NM R2 DOOR FAILED A AALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 798AN 30797 DFW - RIGHT NUMBER TWO DOOR SLIDE UNSUCCESSFULLY DEPLOYED. RIGHT NUMBER TWO DOOR FAILED TO DISARM AT GATE AND SKYCHEF S LOWLY OPENED DOOR. SLIDE FELL OUT OF PACK AND DID NOT DEPLOY. REPLACED SLIDE AND POWER ASSIST BOTTLE FOR RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 WP 2008 5 21 AALA200801085 1 20080424 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 554AA 53084 LGA - EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD FIRS T CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080521 WP 2008 5 21 AALA200801059 1 20080423 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9620D 53591 TUL - EMERGENCY LIGHT BATTERY PACK AT CENTER ROW BY FORWARD LAVATORY FAILED TEST. REPLACED BATTERY PACK AT CENTER ROW B Y FORWARD LAVATORY FOR EMERGENCY LIGHTS IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080521 NM 2008 5 21 AALA200801100 1 20080426 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 187AN 32381 DFW - EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25 DIM. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080521 NM 2008 5 21 KCSA081246 1 20080518 A 5340 STRINGER CLIP BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 STRINGER CLIP CORRODED AT BS 1680, STR-2R. 2 L 7 4 4F RT A20WE 20080521 NM 2008 5 21 KCSA081250 1 20080518 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 SMALL AREA OF DAMAGE ON FUSELAGE BELLY SKIN AT BS 787, LBL-2. 2 L 7 4 4F RT A20WE 20080521 NM 2008 5 21 KCSA081251 1 20080518 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 SMALL AREA OF DAMAGE ON FUSELAGE BELLY SKIN AT BS 680, RBL-5. 2 L 7 4 4F RT A20WE 20080522 NM 2008 5 22 DU4R2008196 1 20080505 A 5320 SHEAR WEB BOEING 737 737448 13844BU NM CFMINT CFM56 CFM563C 13802 EU BS 188-196 CRACKED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 742VA 24773 S/O 312001 OPS NR24728, FLIGHT COMPARTMENT CRACK AT SHEAR WEB BETWEEN SBS 188 - 196 RT FLOOR LEVEL (CRACK EMANATING AT E DGE CUT OUT). 2 L 7 2 4F 4 F RT A16WE E21EU 20080522 EA 2008 5 22 N6WA0080501 1 20080505 A 3397 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE EMERGENCY LIGHTS LOOSE A N6WA K NONE L NO TEST IN INSP/MAINT 1 CE 03 156GJ 10227 LT AFT OVERWING EMERGENCY LIGHT INOP. INSPECTED AND FOUND CONNECTOR ON NR 4 EMERGENCY BATTERY LOOSE. RESECURED CONNECT OR IAW AMM 33-51-17, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080522 SW 2008 5 22 GVNA119695 1 20080508 A 7600 B761M2007101 ACTUATOR BOLKMS 117 BK117C2 5626002 SW TMECA ARRIEL ARRIEL1E 60034 NE NR 2 ENGINE JAMMED B GVNA O OTHER O OTHER CR CRUISE 1 SW 09 452MH 428 9122 IN FLIGHT NR 2 ENGINE TRIM ACTUATOR FULLY RETRACTED, JAMMED, POPPED TRIM CIRCUIT BREAKER. AIRCRAFT LANDED USING MANUAL TRIM. REPLACED ACTUATOR. 1 G 7 2 3U 3 U H13EU E19EU 20080522 CE 2008 5 22 DXTA200803063 1 20080516 A 3260 66426521314 BRACKET CESSNA 560 560XL 2076702 CE PWA 530 PW535A NE MLG BENT E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 677QS 5605367 AFTER TAKEOFF AND GEAR RETRACTION, RED, GEAR UNLOCK LIGHT REMAINED ILLUMINATED. FOUND NOSE UPLOCK CATCH ROD BRACKETS BE NT. REMOVED OLD BRACKETS AND INSTALLED NEW BRACKETS REF MM 32-20-01. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A22CE E00053EN 20080522 NM 2008 5 22 LYNX00014 1 20080515 A 3260 401020101 PROXIMITY SENSOR BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA MLG OUT OF ADJUST A 3LYA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 21 508LX 4182 RIGHT AFTER ROTATION WHEN GEAR WAS SELECTED UP, LT, NOSE AND RT GREEN GEAR LIGHTS INDICATIONS STAYED ILLUMINATED. UPON SELECTING GEAR UP, RED LIGHTS (LT, NOSE AND RT HANDLE ILLUMINATED. AMBER LIGHTS NEVER ILLUMINATED. RAN QRH, SPEED REMA INED BELOW 185KIAS, LANDING WEIGHT WAS NOT EXCEEDED. TROUBLESHOT NLG CENTERING PROX SENSOR. ADJUSTED PROX SENSOR IAW AM M 32-61-06-830. TORQUE WRENCH SN F9TAB1567C CAL DUE 3/09. OPS CHECK GOOD. NO DEFECTS AT THIS TIME. PERFORMED A FUNCT IONAL TEST OF THE LANDING GEAR PRIMARY EXTENSION AND RETRACTION IAW AMM 32-31-00-720-80. OPS CHECK GOOD. 2 H 7 2 4T 4 T RT A13NM E00062EN 20080522 CE 2008 5 22 DXTA200803065 1 20080517 A 3233 991212044 ACTUATOR CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 GL 07 371QS 3108 5600471 UPON LOWERING LANDING GEAR, BOTH MAIN GEAR LIGHTS WERE GREEN, BUT THE NOSE GEAR LIGHT DID NOT ILLUMINATE. REPLACED NLG ACTUATOR WITH REPAIRED UNIT PERFORMED PROPER FUNCTION CHECKS. FUNCTION CHECK SATISFACTORY AT THIS TIME CE560 M/M 32-31-0 3. 2 L 7 2 4F 4 F RT A22CE E25EA 20080522 CE 2008 5 22 042908N319CS 1 20080429 A 3260 S33682 LAMP CESSNA 500 550 2076604 CE MLG INDICATOR BURNED OUT E Z5FA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 63 319CS 5501036 DURING APPROACH,RT MLG, DOWN AND LOCKED INDICATOR DID NOT ILLUMINATE. AC FLIGHT MANUAL PROCEDURES FOLLOWED, GEAR WAS BLO WN DOWN AND EMERGENCY DECLARED. AC LANDED WITHOUT INCIDENT. TROUBLESHOOTING REVEALED A BAD LIGHT BULB. LIGHT BULB REPLAC ED AND OPERATIONALLY CHECKED GOOD. AC RETURNED TO SERVICE. 1 L 7 2 4F A22CE 20080522 EU 2008 5 22 436905162008 1 20080516 A 2140 CONTROL LEVER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE HEATER MISALIGNED E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 556AM 4369 THE PILOT RAN THE HELICOPTER UP FOR NEARLY 20 MINUTES TESTING THE NEW RADIOS, AND THE AIR CONDITIONING UNIT. JUST AFTER DEPARTURE, AND IN CLOSED TRAFFIC, I STARTED TO SMELL AND SEE SMOKE IN THE COCKPIT. I RETURNED TO THE RAMP AND SHUTDOWN. SOURCE OF THE SMOKE IS THOUGHT TO BE VAPORS FROM THE DEMISTER, FOUND THE HEATER CONTROLS MISRIGGED AND TURNING ON THE DE MISTER AND HEATER FULL ON. THE AC IS NEW AND THIS WAS THE FIRST TIME THAT THE HEATERS WERE TURNED ON HIGH. 1 G 7 1 3U 3 U H9EU E19EU 20080522 NE 2008 5 22 399505152008 2 20080515 A 7320 9560170620 GARLOCK SEAL SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B 60037 NE HMU LEAKING E QMLA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 109LN 3995 23199 AC WAS REQUESTED TO RESPOND TO THE AIRPORT FOR A SCENE RENDEZVOUS WITH THE AMBULANCE. AFTER DEPARTURE FROM HOSPITAL, THE MEDICAL CREW NOTICED A FUEL ODOR. THE FLIGHT WAS ABORTED AND AC LANDED AT MEDICAL CENTER WITH ALL AIRCRAFT INDICATIONS NORMAL. ON FINAL APPROACH AND LANDING, THE FUEL ODOR BECAME STRONGER AND AFTER LANDING, A LARGE QUANTITY OF FUEL WAS NOT ED COMING FROM THE AC DRAINS AS WELL AS FUEL SPATTER ON THE SIDE CABIN WINDOWS. PARAMEDIC CREWMEMBER STOOD FIREGUARD AS AC WAS SHUTDOWN. AFTER SHUTDOWN THE ENGINE COWLING WAS OPENED AND LARGE QUANTITY OF FUEL WAS FOUND POOLING ON THE ENGINE DECK. MAINT HAD COMPLETELY REPLACED THE SEAL ON THE HMU EARLIER IN THE DAY AND MAINT RUNS HAD BEEN COMPLETED PRIOR TO 1 G 7 1 3U 3 U H9EU E00054EN 20080522 SO 2008 5 22 C2XA08RI061 1 20080502 A 2611 47359713 SMOKE DETECTOR EMB 135 EMB135ER 3260203 SO ALLSN AE3007 AE3007C GL CARGO BAY LOOSE A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 16502 16186 145166 FLIGHT 2424 - BAG SMOKE WARNING IN FLIGHT, BOTH LIGHTS AND EICAS MESSAGES STAYED FOR FEW SECONDS THEN WENT OFF. MX RESE CURED LOOSE CONNECTOR PLUG AT AFT SMOKE DETECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080522 SW 2008 5 22 MD0519802 1 20080518 A 6230 206040535005 MAST BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL MAIN ROTOR CRACKED E EVCA K NONE O OTHER IN INSP/MAINT 1 CE 03 116AE 4505 1517 54632 CAE900112 POST FLIGHT INSP DISCOVERED AN APPARENT CRACK IN THE MAST IN THE QUADRANT ABOVE THE SWASHPLATE. 1 G 7 1 3U 3 U H2SW E1GL 20080522 CE 2008 5 22 GUUA04290801 1 20080429 A 5524 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87551 24897 UE206 DURING SCHEDULED ROUTINE MAINT, DISCOVERED LT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED LT OB ELEVATOR HINGE BRACK ET. 2 L 7 2 4T 3 T RT A24CE E2NE 20080522 CE 2008 5 22 DXTA200803053 1 20080511 A 5797 CONNECTOR CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE SPOILERS CONTAMINATED E DXTA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 GL 07 650QS 5605150 NO TAKEOFF WARNING AND HORN , CAME ON AFTER JUST PASSING 70 KNTS. C/W FUNCTIONAL CHECK OF THE NO TAKEOFF SYSTEM. NO F AULTS FOUND. INSPECTED SPEEDBRAKE STOW SWITCHES & CONNCETORS. FOUND LT STOW SWITCH CONNECTOR IN SPEEDBRAKE COVE FULL O F WATER. CLEANED CONNECTOR & RECONNECTED. SATISFACTORY OPS & FUNCTIONAL CHECK OF SPEEDBRAKE & NO TAKE OFF SYSTEM IAW MM 27-61-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 20080522 NM 2008 5 22 DXTA200803056 1 20080512 A 3297 CONNECTOR GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE RT MLG CONTAMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 752QS 152 AFTER TAKEOFF, RT MLG WOULD NOT RETRACT WHEN GEAR WAS SELECTED UP. 2 L 7 2 4F 4 F RT A53NM E35NE 20080522 NM 2008 5 22 UG8A08P050601 1 20080506 A 5730 SKIN AMD FALC50 FALCON2000 2730170 NM GARRTT TFE731 TFE7313R1H 29001 WP RT WING CORRODED E UG8A K NONE O OTHER IN INSP/MAINT 1 GL 23 48FB 5069 11 MISSING PAINT WITH MINOR CORROSION ON MIDDLE RT WING, UNDER THE SLAT, AT THE WING LIFTING POINT. CORROSION IS LOCATED O N WING PLANK AT LIFT POINT IN MACHINED CUTOUT. CUTOUT IS FILLED WITH SEALANT. CORROSION LOCATED UNDER SEALANT ON WING PLANK. REMOVED CORROSION AND DETERMINED REMAINING MATERIAL THICKNESS. RECEIVED APPROVAL FROM MFG, DATED 05/08/08 TO PER FORM NDT INSPECTION FOR CRACKS, APPLY ANTI CORROSION PROTECTION IAW THE MM 20-600, APPLY PREVENTITIVE TO CAVITY, FILL WI TH 3M STRUCTURAL VOID FILLING COMPOUND NR3524 TO RESTORE CONTOUR AND APPLY PAINT IAW 20-605. AIRCRAFT WAS RETURNED TO SE RVICE. 2 L 7 2 4F 4 F RT A50NM E6WE 20080522 NE 2008 5 22 EGRR119590 1 20080507 A 5320 7620123014 ANGLE SKRSKY S76 S76B 8143007 NE PWA PT6 PT6B36 52043 EA FUSELAGE CRACKED B EGRR K NONE O OTHER IN INSP/MAINT 1 EA 17 176BA 760317 DURING INSP, TECH FOUND CRACKED TEE ANGLE P/N 76201-23014-138 AFT SECTION. REMOVED TEE ANGLE FOUND THE ENTIRE ANGLE CRAC KED AND THE FWD BATHTUB FITTING P/N 76209-03002-119 CRACKED AT THE MOUNT BOLT HOLE. THE FOLLOWING PARTS WERE REPLACED IA W SRM SA 4047-76-12: TEE FITTING P/N 76201-23014-138 LT FWD BATHTUB FITTING P/N 76209-03002-119 LT AFT BATHTUB FITTING P/N 76209-03002-125. 1 G 7 2 4U 4 U H1NE E4EA 20080522 NE 2008 5 22 EGRR119591 1 20080507 A 5260 0507610A010 MOTOR SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2S1 60057 NE STEP FAILED B EGRR O OTHER O OTHER NR NOT REPORTED 1 EA 17 91AE 269 760552 STEP MOTOR FAILED, REPLACED STEP MOTOR P/N M102M660. 1 G 7 2 3U 4 U NC H1NE E00054EN 20080522 2008 5 22 C2XA08RI057 4 20080502 A 3400 102AU1AF PROBE EMB 145 EMB145LR 3260212 SO TAT INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14568 13568 145628 FLIGHT 1386 -FLIGHT CREW REPORTED TAT 1 HEA INOP WARNING ON EICAS DURING CLIMBING. CREW PERFORMED AIR RETURN AND LANDED UNEVENTFULLY. MX REMOVED AND REPLACED TAT 1 PROBE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AC WAS APPROVED TO RETU RN TO SERVICE. 2 L 7 2 4T RT T00011AT 20080522 CE 2008 5 22 CWQR200804 1 20080512 A 5720 662121126 STIFFENER CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE WING CHAFED B DXTA K NONE O OTHER IN INSP/MAINT 1 GL 05 698QS 5605653 AC WAS IN SCHEDULED MAINTENANCE, AN INSP NOTICED THAT THE LT MAIN GEAR ACTUATOR WAS CHAFING ON THE WING SPAR WHEEL WELL STIFFENER, PN 6621211-26. UPON FURTHER INVESTIGATION WE FOUND THAT THE -26 STIFFENER WAS INSTALLED ON THE WRONG SIDE FRO M THE FACTORY. SINCE THE RT STIFFENER WAS INSTALLED ON THE LEFT, IT WAS NOT TAPERED TO PROVIDE CLEARANCE FOR THE MAIN G EAR ACTUATOR. THIS CAUSED CHAFING DAMAGE TO THE STIFFENER AND THE MAIN GEAR ACTUATOR. THIS DAMAGE HAS BEEN SUBMITTED TO MFG ENGINEERING FOR EVALUATION. SCR AND PHOTOS HAVE BEEN SUBMITTED TO MFG UNDER NR 359072. 2 L 7 2 4F 4 F RT A22CE E00059EN 20080522 NM 2008 5 22 DU4R2008197 1 20080505 A 5311 FRAME BOEING 737 737448 13844BU NM CFMINT CFM56 CFM563B2 13802 EU BS 188-196 CRACKED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 742VA 24773 S/O 312001 OPS NR27954 - FLIGHT COMPARTMENT HAS CRACK AT MAIN FRAME BS 188 - 196 LT FLOOR LEVEL (CRACK AT RADIUS) OB CHO RD W/L 208. 2 L 7 2 4F 4 F RT A16WE E21EU 20080522 NM 2008 5 22 DU4R2008199 1 20080502 A 5315 FLOORBEAM BOEING 737 737448 13844BU NM CFMINT CFM56 CFM563C1 13802 EU BS 985-986 CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 742VA 24773 S/O 312001 N/R 24568, CORROSION ON UNDERSIDE OF T-CAP REPLACEMENT 986.5 AROUND ATTACH HOLES BL-29R TO BL-29L NUMEROUS HO LES. 2 L 7 2 4F 4 F RT A16WE E21EU 20080522 SO 2008 5 22 N93A13052008 1 20080513 A 3250 STEERING SYS GULSTM G1159 GIV 3980115 SO RROYCE SPEY SPEY51114 54523 EU NLG MALFUNCTIONED E N93A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 13 477QS 1377 NOSE WHEEL STEERING FAILED (3) TIMES DURING TAXI. MAINT PERFORMED FUNCTIONAL CHECKS AND CREW PERFORMED TAXI CHECK, UNABL E TO DUPLICATE. 2 L 7 2 4F 4 F RT A12EA E2EU 20080522 CE 2008 5 22 GUUA05110803 1 20080511 A 5524 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 178YV 27822 UE178 DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED LT OB ELEVATOR HINGE BRACKET HAS CORROSION. REPLACED LT OB ELEVATOR HI NGE BRACKET. 2 L 7 2 4T 3 T RT A24CE E2NE 20080522 CE 2008 5 22 GLBA20061101 1 20080512 A 5310 DOOR FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BS 177 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 169GL UE169 AIRSTAIR DOOR FRAME ANGLE CRACKED AT LOWER SNUBBER MOUNT NUTPLATES. MAINT INSTALLED INSERT AND REPAIR PIECE CUT FROM NEW ANGLE IAW. SRM 53-90-28 AND MFG NEW COVER PLATE. REPAIR AREA APPROXIMATELY 7.7500 INCH BY 8.7500 INCH. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1. 2 L 7 2 4T 3 T RT A24CE E2NE 20080522 CE 2008 5 22 GLBA20061102 1 20080512 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BS 177 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 169GL UE169 FRAME AT FS 177.35 CRACKED AT STRINER 9R RELIEF CUTOUT.** MAINT REPAIRED CRACK AT STRINGER RELIEFHOLE AT STRINGER 9R AND FS 177.35 IAW SRM 51-70. REPAIR APPROXIMATELY 3 INCHES BY 4 INCHES. 2024-T3 .071. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1. 2 L 7 2 4T 3 T RT A24CE E2NE 20080522 SW 2008 5 22 EGRR119698 1 20080517 A 2897 WIRE BELL 412 412EP 1182205 SW PWA PT6T PT6T3B 52045 NE INDICATOR BROKEN B EGRR K NONE O OTHER IN INSP/MAINT 1 EA 17 120LA 15 36455 THIS UNIT WAS SENT TO MAKE THIS INSTRUMENT NVG COMPATIBLE. WHEN THEY CHECKED OUT THE UNIT THEY FOUND THE FOLLOWING PROBL EM: THE RT POINTER IS INOP, DUE TO COIL WIRE BROKEN FROM METER. RT POINTER WILL NOT CALIBRATE DUE TO HAIRSPRING BEING DE FORMED. GAUGE WILL BE REPLACED WITH A SERVICEABLE ONE. 1 G 7 2 4U 4 U H4SW E22EA 20080522 CE 2008 5 22 DXTA200803070 1 20080519 A 3233 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 665QS 5605165 AFTER TO AND GEAR RETRACTION, GEAR (UNLOCK) LIGHT REMAINED ILLUMINATED. REMOVED RT MAIN GEAR ACTUATOR AND REPLACED WITH NEW. LEAK AND OPERATIONAL CHECKS NORMAL. MAINTENANCE PERFORMED IAW THE MM CHAPTER 32-30-04. 2 L 7 2 4F 4 F RT A22CE E00059EN 20080521 SO 2008 5 21 LR7A08073 1 20080513 A 5753 RIB LKHEED 382 382G 526414U SO T/E FLAP CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5713, FOUND RT OBD FLAP RIB CRACKED AT ROWS 30. REPAIR ACCOMPLISHED IAW LAC M EA 382-27-08-024. 2 H 7 4 4T A1SO 20080521 NM 2008 5 21 F3LA200800263 1 20080503 A 5322 D53571551214 SHEAR TIE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION, FOUND CRACK INDICATION IN CIRCLED HOLES ON SHEAR TIE FOR FRAME 72 STRINGER 34 RIGHT AND ST RINGER 33 RIGHT. MAINTENANCE REMOVED AND REPLACED SHEAR TIES IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30262. U PON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008051500102 20080515 00102 EA 2008 5 15 SWIA200819577 1 20080502 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 465SW 7845 FLT 6515 - RIGHT SIDE WINDOW CRACKED ON PUSH BACK. REPLACED RIGHT SIDE WINDOW IAW CRJ 200 AMM 56-12-01. OPS CHECK GOOD , P/N NP-139322-12, S/N OFF 03122H3280. 2 L 7 2 4F RT A21EA 2008051500104 20080515 00104 EA 2008 5 15 SWIA200819579 1 20080503 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 912SW 7595 FLT 6498 - FIRST OFFICERS WINDSHIELD IS CRACKED. REPLACED RIGHT WINDSHIELD IAW MM 56-11-01, P/N OFF 601R33033-14, S/N O FF 01230H5902. 2 L 7 2 4F RT A21EA 2008051500105 20080515 00105 EA 2008 5 15 SWIA200819580 1 20080501 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA ILLUMINATED A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 932SW 7714 FLT 6595 - RECEIVED "SMOKE TOILET" CAUTION MESSAGE AFTER TAKEOFF. PERFORMED COMPRESSOR WASH ON LEFT AND RIGHT ENGINES. NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A21EA 2008051500106 20080515 00106 SO 2008 5 15 SWIA200819581 1 20080504 A 5753 STRUCTURE EMB 120 EMB120ER 3260203 SO NACELLE FLAP CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 288SW 120316 LEFT NACELLE FLAP IS CRACKED. REPLACED LEFT NACELLE FLAP IAW EMB MM CH 27-50-03. 2 L 7 2 4T RT A31SO 2008051500108 20080515 00108 EU 2008 5 15 2008UALA02461 1 20080427 A 3350 BR964421 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 453UA 1001 EEL LIGHT INOP . REPLACED LIGHT ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008051500109 20080515 00109 NM 2008 5 15 2008UALA02463 1 20080426 A 3350 1619 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE EXTERIOR OWING INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 923UA 26643 L EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED. 2 L 7 2 4F 4 F RT A16WE E2GL 2008051500114 20080515 00114 NM 2008 5 15 2008UALA02468 1 20080426 A 3350 BATTERY BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 DR 4 LT EMERGENCY SILL LIGHTS INOP. REPLACED BATTERY ON CHARGER. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008051500116 20080515 00116 NM 2008 5 15 2008UALA02470 1 20080426 A 3397 FEEDER CABLE BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT ROW 61 RH INOP. REPLACED EEL CABLE. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008051500117 20080515 00117 NM 2008 5 15 2008UALA02471 1 20080426 A 2530 RELAY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY FAULTED A UALA K NONE M OVER TEMP IN INSP/MAINT 1 WP 29 194UA 26892 GALLEY 415 ALL ELECTRICAL PANELS VERY HOT 1HR INTO FLT. SECURED GALLEY EMERGENCY POWER SWITCH PANELS COLD. FOUND FAULT Y CHILLER RELAY. REPLACED RELAY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008051500118 20080515 00118 NM 2008 5 15 DLM90080669 1 20080501 A 5347 CARGO TRACK DOUG MD90 MD9030 3023690 NM CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 AFT CARGO BAY RT CARGO TRACK CORRODED AROUND FASTENER STA 1269 TO 1307. REMOVED AND REPLACED TRACK, IAW MD90 SRM 51-30- 01. 2 L 7 2 4F RT A6WE 2008051500120 20080515 00120 NM 2008 5 15 F3LA200800253 1 20080513 A 5343 D53372613216 ATTACH FITTING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED, THE LEFT MAIN LANDING GEAR DOOR ACTUATOR ATTACH FITTING ON KEEL BEAM FORWARD LUG HAS NICK ON FORWARD EDGE. MAINTENANCE BLENDED AREA ON LEFT MAIN LANDING GEAR ACTUATOR FITTING ON KEEL BEAM DEPTH OF ARE A IS .013 INCH AND LENGTH IS .123 INCH AREA FOUND TO BE WITHIN LIMITS. REMOVED LEFT TO FACILITATE OTHER MAINTENANCE, PE RFORMED FLAP ROTO PEENING ON BLENDED AREA TO INTENSITY OF .015 MMN AND REINSTALLED LEFT MAIN LANDING GEAR DOOR ACTUATOR. ALL WORK WAS COMPLETED IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30270, SRM 51-73-00, SRM51-29-11 AND AMM 32-31 -25-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008051500122 20080515 00122 NM 2008 5 15 AALA200800940 1 20080413 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 DFW - EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500125 20080515 00125 NM 2008 5 15 AALA200800951 1 20080414 A 2910 CHECK VALVE BOEING 737 737823 13844BZ NM HYD SYSTEM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 910AN 29512 OMA INFLIGHT T1586/14AP LAX TO YYZ - CREW REPORTED NUMBER ONE ENGINE HYDRAULIC PUMP INDICATION FOLLOWED BY NUMBER TWO EN GINE LOW PRESSURE INDICATION. LANDED OMA WITHOUT INCIDENT. REPLACED PRESSURE MODULE TEE CHECK VALVE. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008051500126 20080515 00126 NM 2008 5 15 AALA200800963 1 20080414 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 672AA 25337 DFW - EMERGENCY LIGHT AT AFT OVERWING DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT AFT OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051500127 20080515 00127 EU 2008 5 15 AALA200800948 1 20080413 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 MIA - EMERGENCY LIGHT AT SEAT 31G INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008051500129 20080515 00129 NM 2008 5 15 AALA200800970 1 20080415 A 3350 SIGN BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AA 24580 DFW - EMERGENCY LIGHT EXIT PLACARD AT AFT LEFT OVERWING DAMAGED. REPLACED PLACARD FOR EMERGENCY LIGHT EXIT AT AFT LEFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051500130 20080515 00130 NM 2008 5 15 AALA200800971 1 20080415 A 3350 SIGN BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 622AA 24580 DFW - EMERGENCY LIGHT EXIT PLACARD AT FORWARD LEFT OVERWING DAMAGED. REPLACED PLACARD FOR EMERGENCY LIGHT EXIT AT FORWA RD LEFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051500133 20080515 00133 NM 2008 5 15 AALA200800978 1 20080415 A 3350 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 387AM 27184 MIA - EMERGENCY LIGHT AT SEAT 21A MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21A. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008051500135 20080515 00135 NM 2008 5 15 AALA200800980 1 20080415 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 197AN 32391 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 23C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051500145 20080515 00145 NM 2008 5 15 AALA200800941 1 20080413 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 DFW - EMERGENCY LIGHT AT SEAT 31C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500146 20080515 00146 WP 2008 5 15 AALA200800946 1 20080413 A 4920 APU DOUG DC9 DC982 3022082 WP CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 583AA 53160 ORD INFLIGHT T1861/13APR - CREW REPORTED SMELL OF BURNING DEICING FLUID IN AIR CONDITION SYSTEM. CABIN FILLED WITH SMO KE. CREW SHUT DOWN RIGHT PACK. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND APU HAD INGESTED FLUID. REPLACED A UXILIARY POWER UNIT AND ACCOMPLISHED BURNOUT OF HIGH PRESSURE PNEUMATIC DUCTING. SYSTEM GROUND CHECKED NORMAL OPERATION . 2 L 7 2 4F A6WE 2008051500149 20080515 00149 WP 2008 5 15 AALA200800935 1 20080412 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7531A 49923 LGA - EMERGENCY LIGHTS AT OVERHEAD TAIL COMPARTMENT CATWALK INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD TAIL COMPARTMENT CATWALK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008051500154 20080515 00154 NM 2008 5 15 DLM90080714 1 20080506 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 446-465 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 RIGHT CUSP WEB CORRODED ON UPPER AND LWR SURFACE FROM STA 446-465 RT. REMOVED AND REPLACED CUSP WEB, IAW MD90 SRM 51-30 -01, 51-30-02, 51-30-05 AND DELTA ER/A 398181-14MA DATED 9-18-02 REV 1, STEP NR 9 FIG NR 5. 2 L 7 2 4F RT A6WE 2008051500155 20080515 00155 EU 2008 5 15 08FDEA01811 1 20080510 A 5347 R5307008820400 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 MAIN CARGO DECK SEAT TRACK NR 2 LT HAS 2 AREAS OF CORROSION BETWEEN FR 57.1 AND FR 58 REMOVED LEVEL 1 CORROSION. REMOVE D DAMAGED SEAT TRACK SECTION AND INSTALLED SEAT TRACK REPAIR AT TRACK NR 2 LT BETWEEN FR 57.1 AND FR 58 IAW A300-600 SRM 53-10-16, FIG 208. 2 L 7 2 4F RT A35EU 2008051500160 20080515 00160 NE 2008 5 15 DL777080689 2 20080508 A 7200 ENGINE BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 1 MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 864DA 30160 29736 051200 FOUND M50 BEARING MATERIAL ON MCD ENG REMOVED AND REPLACED ON LOGSHEET H124922 ITEM 010 MSU REMOVED. 2 L 7 2 4F 4 F RT T00001SE E00050EN 2008051500161 20080515 00161 NM 2008 5 15 DLM88080690 1 20080429 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 960DL 49979 THREE CRACKS ON FUSELAGE SKIN AT THE STATIONS; Y=172 OF .050 Y=174.5 OF .125 AND Y=175.25 OF .562 IN THE UPPER FORWARD C ORNER OF THE FORWARD SERVICE DOOR JAMB. REPAIRED PER SRM 53-05D 112 ON N/R T0092302 AT HMV-3 IN GDL. 2 L 7 2 4F RT A6WE 2008051500164 20080515 00164 NM 2008 5 15 08FDEA01813 1 20080510 A 5347 BAC1520792 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 780-879 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 906FD 27148 FOUND SEAT TRACK STA 780-879 RBL 45 HAS CORROSION. REMOVED SEAT TRACK, FAB`D NEW FROM MAT BAC1520-792 IAW SRM 51-10-02. INSTALLED SEAT TRACK STA 780-879 RBL 45, IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008051500176 20080515 00176 NM 2008 5 15 DL757080717 1 20080510 A 2120 285T05545 DUCT BOEING 757 757232 1384965 NM INSTRUMENT PANEL OBSTRUCTED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 666DN 25034 ON TAXI OUT HAD ELECTRICAL SMELL IN COCKPIT. FOUND BLOCKAGE IN COOLING TUBE TO CAPT'S VOR/DME CONTROL PANEL. CLEARED B LOCKAGE. ALSO, REPLACED CAPT'S VOR/DME CONTROL PANEL WHICH WAS CAUSE OF SMOKE FROM OVERHEAT. PANEL REPLACED WAS MFG NR 285T0554-5, S/N DO3712. 2 L 7 2 4F RT A2NM 2008051500178 20080515 00178 NM 2008 5 15 DLM88080719 1 20080510 A 3350 AD3110 BATTERY PACK DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE EMERGENCY LIGHTS INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 939DL 49812 051200 EMERGENCY LIGHTS WOULD NOT TEST FROM FWD FLIGHT ATTENDANT PANEL DURING LAYOVER. REPLACED EMERGENCY LIGHT BATTERY PACK B 5-49 FOR OVERWING LIGHTS. CHECKS GOOD. 2 L 7 2 4F 4 F RT A6WE E9NE 2008051500182 20080515 00182 NM 2008 5 15 DLM90080705 1 20080506 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM BS 674-769 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 RIGHT CUSP WEB CORRODED ON DOUBLER FROM STA 674-769. REPLACED CUSP WEB, IAW MD90 SRM 51-10-05. 2 L 7 2 4F RT A6WE 2008051500187 20080515 00187 EU 2008 5 15 08FDEA01837 1 20080513 A 5315 A53275352200 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 MAIN DECK FLOOR FR 67 BETWEEN SEAT TRACKS NR 4 LT AND NR 5 LT HAS .125 IN CRACK REMOVED CRACK ON FR 67 AFT FACE STIFFENE R BETWEEN SEAT TRACKS NR 4 LT AND NR 5LT AND INSTALLED CROSSBEAM REPAIR IAW A300-600 SRM 53-10-15, FIG 212. 2 L 7 2 4F RT A35EU 2008051500188 20080515 00188 GL 2008 5 15 3611 1 20080511 A 7721 14880001 PROBE CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL ENGINE INOPERATIVE E J4PA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 13 820CN 1660 913916 FP3594B AIRCRAFT DEPARTED KPGV TO KGMU WITH 2 PASSENGERS. DURING CRUISE, THE NR 6 CHT INDICATOR FAILED AND THE PILOT MADE AN UN SCHEDULED LANDING AT KJQF. THE LANDING WAS WITH OUT INCIDENT. SATSAIR MAINTENANCE WAS FLOWN TO KJQF AND THE NR 6 CHT WA S REMOVED AND REPLACED AND AN OPERATIONAL CHECK WAS PREFORMED. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 2008051500191 20080515 00191 EA 2008 5 15 SWIA200819612 1 20080511 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 943SW 7762 FLT 6590 - LEFT SIDE WINDOW CRACKED INFLIGHT. REPLACED CAPTAIN'S SIDE WINDOW IAW 56-12-01. ALL OPS AND LEAK CHECKS GOO D. 2 L 7 2 4F RT A21EA 2008051500193 20080515 00193 EA 2008 5 15 SWIA200819614 1 20080509 A 2910 LINE CNDAIR CL600 CL6002D24 1390016 EA HYD SYSTEM LEAKING A SWIA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 800SK 15060 FLT 4020 - HYDRAULIC SYSTEM 2 LOST FLUID AND PRESSURE. REPLACED HYDRAULIC ENGINE DRIVEN PUMP AND SUCTION LINE IAW CRJ 9 00 29-11-01. LEAK AND OPS CHECK GOOD, P/N OFF GG190-4, S/N OFF K0753. 2 L 7 2 4F RT A21EA 2008051500194 20080515 00194 EA 2008 5 15 SWIA200819615 1 20080511 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 FOUND EMERGENCY LIGHTS ARE INOP BETWEEN ROWS 6 AND 7. REPLACED THE POWER STRIP FOR THE EMERGENCY LIGHTING TRACK. OPS C HECKS GOOD. 2 L 7 2 4F RT A21EA 2008051600004 20080516 00004 EA 2008 5 16 MASA200800374 1 20080506 A 5210 ROD END CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 7337 ASH FLT 2748 PHX-SBP. MAIN PAX DOOR WILL NOT LOCK. ADJUSTED ROD END ON PRESS DOOR. 2 L 7 2 4F RT A21EA 2008051600003 20080516 00003 NM 2008 5 16 SWAA082613 1 20080513 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 234WN 32502 DURING SCHEDULED MV2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008051600004 20080516 00004 NM 2008 5 16 MWEA080065 1 20080505 A 5320 9911841127 STIFFENER DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 822ME 49759 EXFOLIATION CORROSION ON STIFFENER ATTACHED TO FRAME STATION 1462 LONGERON 10 LEFT. FABRICATED AND INSTALLED STIFFENER. 2 L 7 2 4F RT A6WE 2008051600005 20080516 00005 NM 2008 5 16 SWAA082467 1 20080506 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BS 503D, STR 16L. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008051600013 20080516 00013 WP 2008 5 16 AALA200800985 1 20080416 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9628W 53598 LGA - EMERGENCY LIGHT AT FORWARD FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK AT AB5 1 FOR EMERGENCY LIGHT AT F ORWARD FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 2008051600014 20080516 00014 EU 2008 5 16 08FDEA01840 1 20080513 A 5320 A53986743200210 INTERCOSTAL AIRBUS 310 A310324 3930206 EU ZONE 100 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 EMPENAGE THRU DOOR 312 AR, RIGHT INTERCOSTAL BETWEEN FRAME 85 AND 86 IS BENT. REMOVED OLD INTERCOSTAL IAW A310 SRM 51-4 0-21. INSTALLED NEW INTERCOSTAL IAW A310 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008051600020 20080516 00020 NM 2008 5 16 SWAA082496 1 20080506 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008051600029 20080516 00029 NM 2008 5 16 SWAA082478 1 20080506 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 449WN 32469 DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008051600030 20080516 00030 NM 2008 5 16 SWAA082479 1 20080506 A 2560 6557463 FITTING BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 473WN 33832 L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER MM. 2 L 7 2 4F RT A16WE 2008051600036 20080516 00036 NM 2008 5 16 SWAA082483 1 20080506 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 725SW 27857 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008051400247 20080514 00247 NM 2008 5 14 SWAA082607 1 20080512 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 8L CRACKED AT BS 500B. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008051400250 20080514 00250 NM 2008 5 14 SWAA082609 1 20080512 A 5230 507945 SKIN BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008051500015 20080515 00015 SO 2008 5 15 SIMA200813403 1 20080508 A 3350 179803 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 629AE 145130 ON FLIGHT 4036, CREW REPORTED EMERGENCY EXIT LIGHT IS INOPERATIVE OVER GALLEY SERVICE DOOR. AIRCRAFT REMOVED FROM SERVI CE. REMOVED AND REPLACED INVERTER 2 (PS 8501-234) IAW EMB 145 33-50-11. OPERATIONAL CHECKED GOOD OF EMERGENCY LIGHT SYSTEM IAW EMB 145 AMM 33-50-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008051500019 20080515 00019 EU 2008 5 15 NWAA082063253 1 20080509 A 3350 BATTERY PACK AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 353NW 786 ON EMERGENCY LIGHT CHECK HAD "L" AFT EPSU MESSAGE ON FAP. REPLACED AFT BATTERY PACK.  2 L 7 2 4F RT A28NM 2008051500027 20080515 00027 NM 2008 5 15 2008UALA02547 1 20080501 A 2700 UNKNOWN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE UNKNOWN A UALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 WP 29 370UA 24539 VERTICAL FLUTTER IN INTERVALS OF THREE DURING ALL PHASES OF FLIGHT. 2 L 7 2 4F 4 F RT A16WE E2GL 2008051500028 20080515 00028 EU 2008 5 15 MALA080066 1 20080505 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 288-363 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 451XJ 340B451 SEAT TRACK CORRODED STA 288 TO 363 BL 0. SEAT TRACK STA 288 -363 BL 0 REPLACED AS PER EO 53060. 2 L 7 2 4T RT A52EU 2008051500046 20080515 00046 EU 2008 5 15 08FDEA01735 1 20080502 A 5347 A5381312720008 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 673FE 780 MAIN CARGO DECK SEAT TRACK NR 3 RT, BETWEEN FR 54 AND FR 54.1 HAS CORROSION APPROX 3 SQ IN. REMOVED LEVEL 1 CORROSION A ND REMOVED AND REPLACED NR 3 RT SEAT TRACK IAW A300-600 SRM 51-40-21 BETWEEN FR 54 TO FR 54.2 2 L 7 2 4F RT A35EU 2008051500068 20080515 00068 EU 2008 5 15 AALA200800877 1 20080408 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 41063 506 JFK - EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUM BER THREE DOOR EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008051500085 20080515 00085 NM 2008 5 15 AALA200800904 1 20080410 A 3350 COVER PLATE BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 756AM 30264 DFW - EMERGENCY LIGHT WIRING AT BUSINESS CLASS WHEEL CHAIR COMPARTMENT IS EXPOSED AND MISSING PROTECTIVE BUMPER. REPLAC ED PROTECTIVE BUMPER FOR EMERGENCY LIGHT WIRING AT BUSINESS CLASS WHEEL CHAIR COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500086 20080515 00086 NM 2008 5 15 AALA200800914 1 20080410 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 756AM 30264 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT LEFT BUSINESS CLASS INOPERATIVE. REPLACED BATTERY PACK M33098 FOR SEAT MOUNTED E MERGENCY LIGHTS AT LEFT BUSINESS CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500115 20080515 00115 NM 2008 5 15 2008UALA02469 1 20080426 A 3397 WIRE BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT ROW 1J AFT INOP. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008051500124 20080515 00124 NM 2008 5 15 AALA200800937 1 20080412 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 666A 25300 MIA - EMERGENCY LIGHTS AT SEAT ROWS 9 TO 15 INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER TWO DOOR FOR EMERGENCY L IGHTS AT SEAT ROWS 9 TO 15. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051500150 20080515 00150 EU 2008 5 15 AALA200800949 1 20080413 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 MIA - EMERGENCY LIGHTS AT SEAT ROWS 7C TO 18C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 7C T O 18C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008051500186 20080515 00186 EU 2008 5 15 08FDEA01836 1 20080513 A 5347 R5307008820400 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 MAIN DECK CARGO SEAT TRACK NR 2RT HAS 2 AREAS OF CORROSION BETWEEN FR 56 AND FR 57 REMOVED LEVEL 1 CORROSION. REMOVED D AMAGED SECTION OF SEAT TRACK NR 2RT BETWEEN FR 55 AND FR 57 AND INSTALLED REPAIR IAW A300-600 SRM 53-10-16, FIG 208. 2 L 7 2 4F RT A35EU 2008051600002 20080516 00002 EA 2008 5 16 MASA200800367 1 20080505 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 17175 7175 ASH FLT 7049 IAD. PAX DOOR STOW CAUTION MESSAGE. MX OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 2008051600016 20080516 00016 NM 2008 5 16 SWAA082494 1 20080506 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008051600035 20080516 00035 2008 5 16 SWAA082500 4 20080506 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008051600038 20080516 00038 NM 2008 5 16 SWAA082484 1 20080506 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 742SW 29278 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 2008051600044 20080516 00044 NM 2008 5 16 MWEA080067 1 20080507 A 3510 17469005 OXYGEN MASK BOEING 717 717200 1383700 NM COCKPIT LEAKING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 906ME 55170 FIRST OFFICER'S OXYGEN MASK HAS A SMALL LEAK ON THE INFLATION HARNESS. REMOVED AND REPLACED OXYGEN MASK. 2 L 7 2 4F TR A6WE 2008051600047 20080516 00047 NM 2008 5 16 SWAA082508 1 20080507 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008051600049 20080516 00049 NM 2008 5 16 SWAA082514 1 20080507 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008051600050 20080516 00050 NM 2008 5 16 SWAA082513 1 20080507 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 312, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 2008051600051 20080516 00051 NM 2008 5 16 2008UALA02638 1 20080505 A 5210 ARM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR HINGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 L2 DOOR UPPER HINGE ARM CUTOUT HAS CRACKS. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED & INSTALLED A REPAIR AN GLE & TAPERED FILLERS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008051600052 20080516 00052 NM 2008 5 16 SWAA082512 1 20080507 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008051600053 20080516 00053 NM 2008 5 16 SWAA082511 1 20080507 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008051600058 20080516 00058 NM 2008 5 16 SWAA082503 1 20080507 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 421LV 32452 DURING SCHEDULED 6Y CHECK, FOUND RIGHT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080516 2008 5 16 SWAA082521 4 20080508 A 2565 6567380 STRAP BOEING 737 7375H4 138449D NM EVAC SLIDE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EVACUATION SLIDE CONTAINER RETAINING STRAPS BROKEN. REMOVED AND REPLACED RETA INING STRAPS PER SRM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082531 1 20080511 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082532 1 20080511 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 25L. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082597 1 20080512 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082598 1 20080512 A 5311 6546547 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080521 NM 2008 5 21 BEFA200800002 1 20080410 A 5315 FLOORBEAM BOEING 757 757200 1384950 NM BS 1640 CORRODED A BEFA K NONE O OTHER IN INSP/MAINT 1 WP 19 741PA 55899 24737 MAIN CABIN FLOORBEAM UPPER CAP AT BS 1640 CORRODED FROM LT TO RT SIDE. CAP WAS REMOVED AND REPLACED WITH NEW CAP IAW SR M. 2 L 7 2 4F RT A2NM 20080521 EA 2008 5 21 MASA200800402 1 20080515 A 5220 SEAL CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT LACK OF LUBE A MASA O OTHER O OTHER CR CRUISE 1 SW 07 904FJ 15004 ASH FLT 2889 PHX-AUS - RT AFT EMERGENCY EXIT DOOR HIGH PITCH NOISE IN FLIGHT. LUBED DOOR SEALS, NO SQUEAK. 2 L 7 2 4F RT A21EA 20080521 NM 2008 5 21 F3LA200800270 1 20080515 A 5313 D53571532238 STRINGER AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED STRINGER 34 AT FRAME 74 CAP IS CUT FOR FRAME CLEARANCE. MAINTENANCE CUT STRINGER 34 AND INSTALLED REPAIR COUPLER STRINGER 34 IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30262 AND SRM 51-42-11.UPON CO MPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008041500201 20080415 00201 2008 4 15 SWAA081912 4 20080410 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 479WN 33990 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008041500208 20080415 00208 NM 2008 4 15 SWAA081922 1 20080410 A 5311 6546526 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500214 20080415 00214 NM 2008 4 15 SWAA081920 1 20080410 A 5314 6545866 KEELBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED HC2 CHECK, FOUND LEFT KEEL BEAM CORRODED BETWEEN BS 518 AND BS 520, LBL 6.5. REPAIRED KEEL BEAM PER SR M. 2 L 7 2 4F RT A16WE 2008041500215 20080415 00215 NM 2008 4 15 SWAA081921 1 20080410 A 2760 BACC2C400399 CONTROL CABLE BOEING 737 7377H4 1384404 NM LT SPOILER BROKEN A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 745SW 29491 CREW REPORTED CABLE SEEN DURING FLIGHT HANGING OUT AT LT WING. FOUND LT SPOILER CONTROL CABLE BROKEN. REMOVED AND REPL ACED CABLE PER MM. 2 L 7 2 4F RT A16WE 2008041500217 20080415 00217 NM 2008 4 15 USAA920080747 1 20080314 A 5313 6545765115 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED STRINGER, BS 500C, S8R. REPAIRED STRINGER, BS 500C, S8R IAW B737 SRM 53-00-03- 2R3. 2 L 7 2 4F RT A16WE 2008041500222 20080415 00222 NM 2008 4 15 USAA920080752 1 20080317 A 5320 654585569 SILL BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - LEVEL 2 CORROSION ON THE R2 DOOR CUTOUT LOWER SILL WEB, BS 986.5, RBL 60, WL 207. REPL ACED THE R2 DOOR CUTOUT LOWER SILL WEB, BS 986.5, RBL 60, WL 207 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041500227 20080415 00227 NM 2008 4 15 USAA920080687 1 20080312 A 5754 65C26603101 SKIN BOEING 737 7373G7 1384595 NM L/E SLAT DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR -C18- DISBOND AT NR 3 SLAT ON TOP. CUT OUT DAMAGE, INSTALLED FILLER /DOUBLER REPAIR IAW SRM 51-70-10 -2R4, FIG 202. 2 L 7 2 4F RT A16WE 2008041500232 20080415 00232 NM 2008 4 15 BB08049 1 20080405 A 2560 PA010021 BATTERY BOEING 757 7572B7 1384964 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 934UW 27200 PHL - THE FLIGHT ATTENDANT EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE AT DOOR 2L. MAINTENANCE REPLACED THE BATTERY IN T HE FLASHLIGHT AT DOOR 2L. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 2008041600003 20080416 00003 NM 2008 4 16 UIEA200800096 1 20080326 A 5730 PANEL BOEING 747 74747UF 1384812 NM ZONE 500 DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 498MC 29259 LT WING UPPER SURFACE FLYING PANEL AT T/E CLOSEST TO FUSELAGE HAS DELAMINATION AT OUTBOARD EDGE APPROX 18 INCHES INBOARD FROM NR 6 SPOILER. DELAMINATION REPAIRED IAW ATLAS EO NR 4457A137 AND SRM 51-70-07. 2 L 7 4 4F RT A20WE 2008041600004 20080416 00004 NM 2008 4 16 UIEA200800097 1 20080331 A 5754 STRUCTURE BOEING 747 7472D7B 1384803 NM LT WING LE FLAP DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 LT WING DAMAGED FROM BIRD STRIKE ON L/E OF INBOARD MID FLAP, WBL 391.50. AREA OF DAMAGE IS 3.250 INCHES LONG BY 3.0 INC HES WIDE. ACCOMPLISHED PERMANENT REPAIR AS PER B747-200 SRM 51-40-09 FIG 5, SHEETS 3 AND 8, 250 DEGREES F PER SRM 51-40 -12. REFERENCE ATLAS AIR EO NR 4757A424. 2 L 7 4 4F RT A20WE 2008041600005 20080416 00005 NM 2008 4 16 UIEA200800098 1 20080331 A 5347 BAC15201890 SEAT TRACK BOEING 747 7472D7B 1384803 NM BS 1689 BROKEN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 MAIN DECK CARGO SEAT TRACK AT BS 1689, RBL 11 HAS DAMAGE CROWN LUGS. ACCOMPLISHED PERMANENT REPAIR AS PER B747-200 SRM 53-10-05 FIG 14. 2 L 7 4 4F RT A20WE 2008041600006 20080416 00006 EU 2008 4 16 F3LA200800162 1 20080411 A 5315 D5347217220400 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 C CHECK INSPECTION REPORTED CORROSION WAS FOUND ON NUT CLIP HOLE FLOORBEAM Y1292 AT FRAME 67 AND WAS FOUND UNSERVICEABLE. MAINTENANCE REMOVED AND REPLACED FLOORBEAM Y1292 AT FRAME 67 IN ACCORDANCE WITH SRM 51-42-11 PARAGRAPHS 5 AND 7 AND AIRBUS DRAWINGS D53472815 AND E53474250. UPON COMPLETION OF THE INSTALLATION THE FLOORBEAM WAS INSPECTED AN D FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008041600010 20080416 00010 SO 2008 4 16 CHQA200800076 1 20080410 A 2910 HYDRAULIC SYSTEM EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL MALFUNCTIONED A CHQA O OTHER J WARNING INDICATION LD LANDING 1 GL 11 374SK 145544 CAE311206 FLT 5284, AFTER LANDING, THE AIRCRAFT ENCOUNTERED A HYDRAULIC FAILURE AFFECTING BRAKING AND STEERING. APPROXIMATELY 3 SECONDS INTO ROLL-OUT THE AIRCRAFT BEGAN TO VEER TO THE LEFT AND A RUDDER SYS 1-2 INOP MESSAGE APPEARED ON EICAS. NORMA L BRAKING THEN BECAME INEFFECTIVE. FULL BRAKE WAS APPLIED BY CAPTAIN AND FIRST OFFICER AND AIRCRAFT CONTINUED TO VEER L EFT. THE STEERING DISCONNECT BUTTON WAS HIT, FULL REVERSE WAS APPLIED WITH BOTH ENGINES, AND THE EMERGENCY BRAKE WAS AP PLIED AND AIRCRAFT REGAINED BRAKING. THE HYDRAULIC PAGE WAS CHECKED AND QUANTITY AND PRESSURE WERE BOTH GOOD. STEERING WAS RE-ENGAGED WITH THE HAND TILLER AND THE AIRCRAFT TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ST 2 L 7 2 4F 4 F RT T00011AT TE6CH 2008041600012 20080416 00012 NM 2008 4 16 UIEA200800107 1 20080404 A 5320 STIFFENER BOEING 747 7472D7B 1384803 NM BS 1920 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 AFT CARGO COMPARTMENT VERTICAL STIFFENER CRACKED AT DOOR WAY. ACCOMPLISHED PERMANENT REPAIR AS PER B747-200 SRM 51-40-0 4, FIG 1, SHEET 1,2,3 AND 4. ALSO, REFERENCE ATLAS AIR EO NR 4753B142. 2 L 7 4 4F RT A20WE 2008041600013 20080416 00013 NM 2008 4 16 UIEA200800108 1 20080404 A 5347 BAC15201566 SEAT TRACK BOEING 747 7472D7B 1384803 NM BS 1785 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 MAIN DECK CARGO SEAT TRACK DAMAGED AT BS 1785, LBL 99. ACCOMPLISHED PERMANENT REPAIR AS PER B747-200 SRM 53-10-05, FIG 1A, SHEET 1, 2 AND 4. ALSO, REFERENCE ATLAS AIR EO NR 4753B139. 2 L 7 4 4F RT A20WE 2008041600014 20080416 00014 NM 2008 4 16 UIEA200800109 1 20080404 A 5730 PANEL BOEING 747 7472D7B 1384803 NM LT WING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 523MC 21782 LT WING UPPER FIXED LEADING EDGE ON UPPER SURFACE HAS AN AREA OF 30.0 INCHES BY 10.0 INCHES OF DELAMINATION. ACCOMPLISH ED PERMANENT REPAIR AS PER B747-200 SRM 51-40-09, FIG 18, SHEET 3 AND 5, PREPREG 250 DEGREES F CURE PER SRM 51-40-12. A LSO, REFERENCE ATLAS AIR EO NR 4757A425. 2 L 7 4 4F RT A20WE 2008041400131 20080414 00131 NM 2008 4 14 F3LA200800135 1 20080406 A 5330 D53476410208 SKIN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 904FR 577 1579 DURING PRE FLIGHT INSPECTION, THE FLIGHT CREW REPORTED AFT LEFT FUSELAGE SKIN GOUGE AND DENT AT FRAME 61 AND STRINGER 38 LEFT. BLENDED THE GOUGE IN ACCORDANCE WITH EA A9-53R-30192. INTERIM REPAIR WAS INSPECTED AND FOUND ACCEPTABLE, TDI 10 61199 ISSUED FOR FOLLOW UP INSPECTION. INSPECTED THE DENT AND FOUND TO BE WITHIN LIMITS IN ACCORDANCE WITH SRM 53-41-11 FIGURE 101. DENT WAS TREATED, PRIMED AND PAINTED IN ACCORDANCE WITH EA A9-53R-30192. UPON COMPLETION OF THE WORK TDI 1061200 WAS ISSUED FOR A FOLLOW UP INSPECTION. UPON COMPLETION OF ALL WORK THE REPAIRS WERE INSPECTED AND FOUND ACCEPTA BLE. 2 L 7 2 4F 4 F RT A28NM 2008041400132 20080414 00132 EU 2008 4 14 F3LA200800137 1 20080404 A 5320 D53471123202 SUPPORT AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 C-CHECK, INSPECTION REPORTED CORROSION WAS FOUND AT FRAME SUPPORT OF FLOORBEAM Y1732 AFT OF FRAME 69. MAIN TENANCE REMOVED AND REPLACED FRAME SUPPORT IN ACCORDANCE WITH SRM 51-42-11 AND SRM 51-72-11 AND SRM 51-44-11. UPON COMP LETION OF THE INSTALLATION THE FRAME SUPPORT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041400138 20080414 00138 EU 2008 4 14 TRBA2008039 1 20080410 A 5610 NP1588013 WINDSHIELD AEROSP ATR72 ATR72212 8680945 EU COCKPIT CRACKED A TRBA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 29 410AT 410 CAPT DIVERTED TO PUJ DUE TO CAPT FWD WINDSHIELD CRACKED OR SHATTERED AFTER ELECTRICAL SHORT. REMOVED AND REPLACED CAPT WINDSHIELD AS PER ATR 72 JIC 56-11-10 RAI 10000. OPS CHECK GOOD AND LEAK CHECK FOUND SATISFACTORY AT THIS TIME. 2 H 7 2 4T RT A53EU 2008041400139 20080414 00139 EU 2008 4 14 F3LA200800140 1 20080404 A 5320 D53471124200 SHEAR PLATE AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 CHECK INSPECTION REPORTED CORROSION WAS FOUND ON SHEAR PLATE AT FLOORBEAM Y1732 AFT OF FRAME 69. MAINTENAN CE REMOVED AND REPLACED SHEAR PLATE IN ACCORDANCE WITH SRM 51-42-1 PARAGRAPH 6, 7 AND EA A9-53R-30196. UPON COMPLETION OF THE INSTALLATION OF THE SHEAR PLATE IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041400154 20080414 00154 EA 2008 4 14 SWIA200819469 1 20080111 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 947SW 7786 FS 280 AT LBL9.0 UPPER FLOOR ANGLE IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-53-11-138 D ATED 02-15-99. 2 L 7 2 4F RT A21EA 2008041400163 20080414 00163 WP 2008 4 14 NWAA081549884 1 20080410 A 3350 FUSE DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 677MC 47756 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAI LED. MAINTENANCE REPLACED THE ASSOCIATED FUSE IN THE PERTINENT POWER STRIP. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A6WE 2008041400172 20080414 00172 EU 2008 4 14 AALA200800709 1 20080323 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80084 675 MIA - EMERGENCY LIGHTS AT LEFT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT AFT CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008041400197 20080414 00197 NM 2008 4 14 AALA200800726 1 20080326 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 752AN 30260 DFW - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041400200 20080414 00200 NM 2008 4 14 AALA200800730 1 20080326 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 752AN 30260 DFW - EMERGENCY LIGHT AT SEAT 32G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041500001 20080415 00001 EA 2008 4 15 A6WA200840218 1 20080318 A 3240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PARKING BRAKE DAMAGED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 433AW 7289 PARKING BRAKE HANDLE OCCASIONALLY SLIPS OUT OF POSITION. (M) 2 L 7 2 4F RT A21EA 2008041500024 20080415 00024 EU 2008 4 15 USAA920080719 1 20080401 A 3260 GA62953 SUPPORT AIRBUS 320 A320231 3930325 EU LANDING GEAR DEFECTIVE A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 632AW 81 FLT 143 - SJC-PHX - CREW REPORTED THAT AFTER TAKEOFF GEAR DID NOT RETRACT, HANDLE LOCK DOWN. ECAM L/G SHOCK ABSORBER FA ULT. AUTO PILOT OFF AND AUTO FLIGHT AUTO THROTTLE OFF. AIRCRAFT RETURNED TO SJC AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO PHX. MAINTENANCE WAS ABLE TO DUPLICATE ON GROUND. PFR FAULT L/G SHOCK ABSORBER FAULT FAILURE MESSAGE F AULTS BOTH PROX SENSORS 24 & 25 GA. REMOVED AND REPLACED TARGET SUPPORT ROD. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008041500028 20080415 00028 NM 2008 4 15 USAA920080691 1 20080314 A 5322 6558280511 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED SHEAR TIE, BS 360, S14R - S15R. REPAIRED SHEAR TIE, BS 360, S14R - S15R IAW B7 37 SRM 53-00-07-2R7. 2 L 7 2 4F RT A16WE 2008041500043 20080415 00043 NM 2008 4 15 USAA920080742 1 20080312 A 5320 50797819 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - RIGHT HAND OVERWING EMERGENCY EXIT CUTOUT HAS A CRACKED "T" ANGLE, BS 627.5, RBL 66 - R BL 70, WL 224 - WL 230. REPLACED RIGHT HAND OVERWING EMERGENCY EXIT CUTOUT "T" ANGLE, BS 627.5, RBL 66 - RBL 70, WL 224 - WL 230 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041500064 20080415 00064 NM 2008 4 15 SWAA081855 1 20080407 A 3350 101073 LENS BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 2008041500072 20080415 00072 EA 2008 4 15 TRAX200800488 1 20080405 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 878AS 7590 AFT CEILING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 2008041500083 20080415 00083 NM 2008 4 15 SWAA081869 1 20080408 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, RBL 2. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500100 20080415 00100 NM 2008 4 15 SWAA081894 1 20080408 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 829, RBL 13. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041500102 20080415 00102 NM 2008 4 15 SWAA081895 1 20080408 A 5311 6546532 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 9R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500107 20080415 00107 EA 2008 4 15 TRAX200800456 1 20080321 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 AAR - 1023 - LEFT BATT RIB CRACKED. REMOVED LEFT BATT RIB DOUBLER LOCATED HOLES IN NEW SERVICEABLE BATT RIB DOUBLER IAW CRJ 200 SRM 51-40-11. OK TO ALODINE AND PRIME. ALODINED AND PRIMED IAW 51-25-06. OK TO INSTALL. INSTALLED NEW SERVI CEABLE BATT RIB DOUBLER IAW REO 601R-57-51-046. OK TO PAINT AND INSTALL RECEPTACLES. PAINTED AND INSTALLED RECEPTACLE S. PERFORMED OP CHECKS BTMU IAW CRJ AMM 32-46-06. PROX COMPUTER IAW CRJ AMM 32-61-00. ANTI SKID COMPUTER IAW CRJ AMM 32-44-06. RETRACTION / EXTENSION OF LANDING GEAR IAW CRJ AMM 32-30-00. ALL OPS CHECKS GOOD. SUPPLEMENTAL SDR CLOSED 4 /10/08. 2 L 7 2 4F RT A21EA 2008041500109 20080415 00109 NM 2008 4 15 SWAA081903 1 20080409 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 2008041500117 20080415 00117 EA 2008 4 15 VNAA0804002 1 20080403 A 7797 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT ENGINE LOOSE A VNAA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 GL 05 220PS 7887 CREW REPORTED A LEFT ENGINE MISCOMPARE MESSAGE DURING CRUISE. CREW REDUCED THRUST PER THE QRH AND CONTINUED TO STL AND LANDED WITHOUT INCIDENT. AN EMERGENCY WAS DECLARED AND THE EQUIPMENT DID RESPOND. MAINTENANCE INSPECTED AND FOUND THE LEFT ENGINES LEFT HAND THERMOCOUPLE HARNESS ELECTRICAL CONNECTOR LOOSE. MAINTENANCE CLEANED AND RE-TIGHTENED THE CONNEC TOR. MAINTENANCE PERFORMED OPERATIONAL CHECKS PER CRJ 200 77-11-07-710-001. ALL INDICATIONS NORMAL. AIRCRAFT WAS RELE ASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 2008041500131 20080415 00131 EA 2008 4 15 TRAX200800504 1 20080408 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 CRACK IN 280 FLOOR SUPPORT FRAME ATTACH ANGLE O/B SIDE OF FLOORBEAM AT LBL 9. REMOVED CRACKED ATTACH ANGLE. REPLACED A TTACH ANGLE IAW REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 2008041500132 20080415 00132 EA 2008 4 15 TRAX200800505 1 20080408 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 720EV 10115 MAIN PAX DOOR CANNOT BE OPENED FROM THE OUTSIDE. 2 L 7 2 4F RT A21EA 2008041500144 20080415 00144 EA 2008 4 15 TRAX200800517 1 20080408 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 919EV 7780 PAX DOOR AFT SWIVEL ANCHOR FITTING IS CRACKED. REMOVED PAX DOOR AFT ANCHOR FITTING IAW AMM 52-11-17. OK TO INSTALL. INS TALLED SERVICEABLE FITTING P/N 601R38074-5 IAW AMM 52-11-17. REQUIRES PAX DOOR CABLE CONNECTED TO FITTING AND OPS CHECK OF DOOR. CONNECTED PAX DOOR CABLE TO FITTING USING SERVICEABLE PIN P/N MS20392-3C23 IAW AMM 52-11-17. OPS CHECK STILL RE QUIRED. OPS CHECK GOOD IAW AMM 52-11-00. 2 L 7 2 4F RT A21EA 2008041500202 20080415 00202 NM 2008 4 15 SWAA081913 1 20080410 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 498WN 32480 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 2008041500205 20080415 00205 NM 2008 4 15 SWAA081923 1 20080410 A 5311 6546529 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041600007 20080416 00007 SW 2008 4 16 KL13037 1 20080414 A 2720 2742003902 BELLCRANK SWRNGN SA227 SA227BC 3377519 SW RUDDER CRACKED E KY7A K NONE O OTHER IN INSP/MAINT 1 NM 03 787KL 1403 BC787B RUDDER BELLCRANK FOUND DEFORMED AND CRACKED AT RUDDER TORQUE TUBE ATTACHMENT. 2 L 7 2 4T RT A8SW 2008041600019 20080416 00019 NM 2008 4 16 UIEA200800114 1 20080407 A 5330 SKIN PANEL BOEING 747 7472D7B 1384803 NM BS 1737-1745 S46 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 EVIDENCE OF CORROSION UNDER LAP JOINT STRINGER 46 RIGHT, BETWEEN STA 1737-1745. INTERIM REPAIR ACCOMPLISHED IAW SRM 53- 30-03 FIG 17 TABLE LLL WITH INITIAL INSPECTION SCHEDULED AT 15000 FLIGHT CYCLES AFTER INTERIM REPAIR AND REPEAT INSPECTI ON THEREAFTER AT EVERY 3000 FLIGHT CYCLES. 2 L 7 4 4F RT A20WE 2008041600024 20080416 00024 NM 2008 4 16 AALA200800770 1 20080330 A 3350 HOUSING BOEING 777 777223 1385213 NM EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 772AN 29580 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE CLOSET DAMAGED. REPLACED HOUSING ASSEMBLY FOR EMERGENCY LIGHT AT LEFT NUMBER O NE CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041600029 20080416 00029 NM 2008 4 16 AALA200800785 1 20080329 A 3350 D71701100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 912AN 29513 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED OPERATIONAL CHECK. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CAB IN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008041600031 20080416 00031 WP 2008 4 16 08FDEA01399 1 20080414 A 5347 ADA765621 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA.939 X -47.50 FOUND SEAT TRACK WITH HOLE OVALIZED REPAIRED FOR SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F A22WE 2008041600042 20080416 00042 EU 2008 4 16 F3LA200800156 1 20080405 A 5321 D5361060500100 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THE UNDERSIDE OF FLOOR PANEL 222FF. MAINTENANCE REMOVE D THE CORRODED PANEL. THE NEW PANEL WAS INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF TASK CARD CP 753-12. UPON COM PLETION OF THE INSTALLATION OF THE NEW PANEL, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041600043 20080416 00043 EU 2008 4 16 MALA080058 1 20080410 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU CABIN ODOR A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 421XJ 340B421 DIVERTED TO MBS DUE TO BURNING ODOR IN THE CABIN AND THE COCKPIT. MX HAS BEEN UNABLE TO FIND THE SOURCE OF ANY BURNING OR SMOKE ODOR, HAVE OPENED CB PANELS, RUN HEATERS, NOW ARE IN THE PROCESS OF REMOVING THE RT ACM PANEL (OUTSIDE) AND WIL L SERVICE. 2 L 7 2 4T RT A52EU 2008041600049 20080416 00049 EA 2008 4 16 A6WA200840186 1 20080311 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 CORROSION FOUND ON THE FLOOR SUPPORT STRUCTURE, UNDER THE BAGGAGE DOOR STEP PLATE. CORROSION REMOVED ON THE FLOOR SUPPO RT STRUCTURE UNDER THE BAGGAGE DOOR STEP PLATE IAW CRJ 200 SRM 51-21-06 AND 51-21-16. (M) 2 L 7 2 4F RT A21EA 2008041600050 20080416 00050 EA 2008 4 16 A6WA200840201 1 20080305 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 PAX DOOR FORWARD AND AFT UPPER CORNER FOUND DENTED. PAX DOOR FORWARD AND AFT UPPER CORNERS REINSTALLED IAW REO 601R-52- 11-827. (M) 2 L 7 2 4F RT A21EA 2008041600053 20080416 00053 NM 2008 4 16 UIEA200800086 1 20080314 A 5347 SEAT TRACK BOEING 747 747341 13848AM NM BS 1720-1740 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 MAIN DECK STA 1720 TO 1740 RBL 11 SEAT TRACK FOUND LEVEL 1 CORROSION. CORROSION REMOVED IAW SRM 51-10-01. 2 L 7 4 4F RT A20WE 2008041600059 20080416 00059 NM 2008 4 16 UIEA200800100 1 20080331 A 5347 SEAT TRACK BOEING 747 747243B 1384830 NM BS 1840-1860 CHAFED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK BS 1840 TO 1860 RBL 75 SEAT TRACK CHAFED. CHAFED AREA SMOOTHED OUT AND REPROTECTED IAW SRM 51-10-01. 2 L 7 4 4F RT A20WE 2008041600066 20080416 00066 2008 4 16 EIA2008016 2 20080116 A 7200 GUIDE VANE BOEING 747 747212B 1384886 NM NR 2 ENGINE SEPARATED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 ON WALK AROUND, FOUND NR 2 ENG FAN EXIT GUIDE VANE EXITED ENGINE AND DAMAGED LT INBOARD MID TRAILING EDGE FLAP. REMOVED DAMAGED GUIDE VANE AND PLACED ENGINE ON COI NR 114, AND REPLACED MID FLAP, OPS CHECKED GOOD. 2 L 7 4 4F RT A20WE 2008041600070 20080416 00070 EU 2008 4 16 F3LA200800151 1 20080404 A 5320 D53472188204000 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND AROUND THE NUT CLIP HOLES ON FLOOR BEAM Y1292 BETWEEN FRAM ES 68 AND 69. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPH 6. UPON COMPLETION OF THE INSTALLATION OF THE NEW BEAM, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041600075 20080416 00075 2008 4 16 WGEA200800054 4 20080409 A 3417 1008555REVA ADC ECLIPS EA500 ECLIPSEEA500 3350000 SW NR 1 FALSE INDICATION E WGEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 156DJ 36 000073 AIRSPEED DISAGREE CAS MESSAGE DISPLAYED DURING TAKEOFF. SUPPLEMENTAL INFORMATION, RESOLVED ON W/O: 1826 TASKCARD: NR-00 001. REMOVED NOSE ACCESS PANEL 211CT, PILOT'S AND CO-PILOTS SEATS, DRAINED PITOT/AOA PROBES IAW AMM SUBTASK 34-10-00-06 1-611-00; PERFORMED PITOT/AOA LEAK TEST IAW AMM SUBTASK 34-10-00-071-701-001. TEST GOOD; PERFORMED PITOT AND STATIC VER IFICATION TEST IAW AMM SUBTASK 34-10-00-071-701-005. FOUND LEFT PFD AIRSPEED TO BE OUT OF LIMITS AND SUSPECT FAULTY NR 1 ADC ME 0020195 04.08.08. REMOVED UNSERVICEABLE ADC FROM NR 1 POSITION. INSTALLED SERVICEABLE ADC, WHICH WAS REMOVED FROM N139DJ NR 1 POSITION, AND INSTALLED IN NR 1 POSITION IAW AMM 34-10-15. COMPLETED ADJUSTMENT/TEST OF AIR DATA COMPU 1 L 7 2 4J RT A00002AC 2008041600082 20080416 00082 NM 2008 4 16 UIEA200800121 1 20080408 A 5347 T08A020971 SEAT TRACK BOEING 747 747243B 1384830 NM BS 1600-1615 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK STA 1600 TO 1615 RBL 99 SEAT TRACK FOUND CRACKED. SEAT TRACK REPAIRED PER SRM 53-10-05. 2 L 7 4 4F RT A20WE 2008041600087 20080416 00087 NM 2008 4 16 QXEA200800369 1 20080408 A 5210 COVER BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR OUT OF POSITION A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 408QX 4050 STS- FLIGHT 2468 - LEFT REAR PASSENGER DOOR WILL NOT OPEN. MAINTENANCE RE-INDEXED THE INTERNAL COVER 1 HOLE CLOCKWISE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008041600089 20080416 00089 NM 2008 4 16 QXEA200800370 1 20080409 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM MAIN PAX OUT OF ADJUST A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 404QX 4046 BOI- FLIGHT 2269 - AFT PASSENGER DOOR ON NR 1 SIDE VERY HARD TO CLOSE. MAINTENANCE FOUND DOOR OFF STOP. RE-SEQUENCED D OOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008041600096 20080416 00096 NM 2008 4 16 AALA200800716 1 20080324 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 23C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041600097 20080416 00097 NM 2008 4 16 AALA200800717 1 20080324 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 793AN 30255 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE FORWARD GALLEY CLOSET HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LE FT NUMBER ONE FORWARD GALLEY CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041600099 20080416 00099 NM 2008 4 16 AALA200800719 1 20080325 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 916AN 29517 MIA - EMERGENCY LIGHT AT SEAT 16D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008041600104 20080416 00104 NM 2008 4 16 AALA200800728 1 20080326 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 752AN 30260 DFW - EMERGENCY LIGHT AT SEAT 24C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041600106 20080416 00106 NM 2008 4 16 AALA200800736 1 20080327 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 603AA 27054 DFW - EXTERNAL EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT RIGH T NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041600110 20080416 00110 NM 2008 4 16 F3LA200800147 1 20080402 A 5321 D5361067500000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE 222EF DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 5380 1841 DURING C4 S1 C CHECK, INSPECTION REPORTED FLOOR PANEL 222EF HAD PUNCTURE DAMAGE. MAINTENANCE REPAIRED THE PUNCTURE IN T HE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-12-00. UPON COMPLETION OF THE REPAIR, THE PANEL WAS I NSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041600115 20080416 00115 NM 2008 4 16 HALA0800526 1 20080409 A 2710 AILERON BOEING 767 76733A 1385209 NM UNKNOWN A HALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 13 580HA 28140 ETOPS SIGNIFICANT SYSTEM RT INBD AILERON SEEMS TO FLOAT UP AT HIGH SPEEDS. 2 UNITS OF LEFT YOKE AT 330-340 KNOTS IS REQ UIRED TO KEEP WINGS LEVEL. BOTH LT AND RT INBD AILERON INDICATORS SHOW 1/2 OF FULL DISPLACEMENT. AT SLOWER SPEEDS (BEL OW 300 KNOTS) INBD AILERON LOWERS TO APPROX 1/6 OF MAX DISPLC 1/4 OF UNIT OF LT YOKE WINGS LEVEL AT 265 KNOTS. OPS CK A ILERON PER MM 27-11-00-715-002 GOOD. 2 L 7 2 4F RT A1NM 2008041600117 20080416 00117 EA 2008 4 16 A6WA200840272 1 20080330 A 5410 RUB STRIP CNDAIR CL600 CL6002B19 1900309 EA ACCESS DOOR WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 RIGHT ENGINE TRAILING EDGE RUB STRIP IS WORN ON NOSE ACCESS COWL UPPER. (M) REPLACED IAW CMM TASK 71-14-01-300-814-A01 REPAIR SR5091. 2 L 7 2 4F RT A21EA 2008041600118 20080416 00118 NM 2008 4 16 UIEA200800126 1 20080403 A 5210 SKIN BOEING 747 747243B 1384830 NM L1 DOOR DEFORMED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK L-1 DOOR LOWER FWD CORNER OF EXTERNAL SKIN FOUND DEFORMED. DEFORMED AREA RE-WORKED AS PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 2008041600120 20080416 00120 EU 2008 4 16 F3LA200800159 1 20080411 A 5320 D5391635420040 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND AROUND THE NUT PLATE HOLES OF THE FLOOR SUPPORT PLATE ON T HE LEFT SIDE OF THE FORWARD CARGO COMPARTMENT BETWEEN FRAMES 28 TO 30. MAINTENANCE REMOVED AND REPLACED THE FLOOR PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE REPLACEMENT OF THE PLATE, IT WAS INSP ECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041600121 20080416 00121 EA 2008 4 16 A6WA200840273 1 20080327 A 5315 60034017351 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 AT FS 280, WL 73.10 BETWEEN LBL 9 AND RBL 9 FLOOR ANGLE (FWD) CRACKED, REPLACED IAW SRM 51-42-06 . 2 L 7 2 4F RT A21EA 2008041600123 20080416 00123 NM 2008 4 16 F3LA200800149 1 20080406 A 5321 D5361067800000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE 221DF DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 5380 1841 DURING C4 S1 C CHECK, INSPECTION REPORTED DELAMINATION, AT THE EDGES, AND A LARGE GOUGE, IN FLOOR PANEL 221DF. MAINTENA NCE REPAIRED THE FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-77-12. UPON COMPLETION OF THE REPAIR, T HE PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041600127 20080416 00127 NM 2008 4 16 UIEA200800129 1 20080404 A 5730 SKIN BOEING 747 747243B 1384830 NM LWS 150-470 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 LEFT WING FROM WS 150 TO 470 UPPER SKIN CORROSION EVIDENT BETWEEN FRONT SPAR AND MID SPAR. BLENDED OUT CORROSION PER SR M 51-10-01, REPROTECTED PER SRM 51-10-02. 2 L 7 4 4F RT A20WE 2008041600129 20080416 00129 NM 2008 4 16 UIEA200800131 1 20080403 A 5730 SKIN BOEING 747 747243B 1384830 NM LWS 640-1120 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 LEFT WS 640 TO 1120 HAS CORROSION EVIDENT BETWEEN MIDSPAR TO REAR SPAR. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTE CTED PER SRM 51-10-02. 2 L 7 4 4F RT A20WE 2008041600134 20080416 00134 NM 2008 4 16 UIEA200800136 1 20080404 A 5711 SPAR BOEING 747 747243B 1384830 NM RWS 1392-1485 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 RIGHT WING WS 1392 TO WS 1485 FROM (NR 24, AND 25 LEADING EDGE FLAP AREA) FRONT SPAR AREA SURROUNDING AND MID SPAR SURRO UND AREA FOUND 8 AREAS OF CORROSION. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02. 2 L 7 4 4F RT A20WE 2008041600137 20080416 00137 EA 2008 4 16 A6WA200840189 1 20080311 A 5414 GROUND STUD CNDAIR CL600 CL6002B19 1900309 EA LT NACELLE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 LT PYLON UPPER TRAILING EDGE GROUNDING PLATES CORRODED. LT PYLON UPPER TRAILING EDGE GROUNDING PLATES REPLACED IAW SRM 51-24-16 AND SRM 51-42-13. (M) 2 L 7 2 4F RT A21EA 2008041600139 20080416 00139 SO 2008 4 16 SIMA200810503 1 20080411 A 3320 BR900022 BALLAST EMB 135 EMB135LR 3260305 SO CABIN LIGHT BURNED OUT A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 707EB 145195 ON FLIGHT 4551, CREW REPORTED A BURNED CIRCUIT ODOR FROM THE 1ST OVERHEAD LIGHT IN CABIN. AIRCRAFT REMOVED FROM SERVICE . REMOVED AND REPLACED BALLAST FOR 1ST OVERHEAD LIGHT. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 2008041600143 20080416 00143 WP 2008 4 16 AALA200800748 1 20080328 A 2560 P4010021000 BATTERY DOUG DC9 DC982 3022082 WP FLASHLIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7514A 49891 TPA - EMERGENCY FLASHLIGHT AT FLIGHT ATTENDANT SEAT AT AFT GALLEY DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLAS HLIGHT AT FLIGHT ATTENDANT SEAT AT AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008041600145 20080416 00145 NM 2008 4 16 AALA200800750 1 20080329 A 3350 0201804001 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 678AN 29428 JFK - EMERGENCY LIGHT AT SEAT 36D INOPERATIVE. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 36D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041600148 20080416 00148 NM 2008 4 16 AALA200800753 1 20080329 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AA 24585 DFW - EMERGENCY LIGHT AT SEAT ROW 12DEF MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 12DEF. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041600156 20080416 00156 NM 2008 4 16 NWAA081576310 1 20080227 A 5347 SEAT TRACK BOEING 747 747451 1384940 NM BS 1090 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING "M" CHECK, FOUND SURFACE CORROSION ON SEAT TRACK AT BS 1090 RBL 98. REPAIRED PER EA 63-212530. 2 L 7 4 4F RT A20WE 2008041600160 20080416 00160 NM 2008 4 16 NWAA081606310 1 20080222 A 5315 FLOORBEAM BOEING 747 747451 1384940 NM BS 1040 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING "M" CHECK, FOUND CORROSION ON UPPER DECK FLOORBEAM AT BS 1040 RBL 42. REPAIRED PER EA 63-212526. 2 L 7 4 4F RT A20WE 2008041600162 20080416 00162 NM 2008 4 16 AALA200800759 1 20080330 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 767AJ 33539 JFK - EMERGENCY LIGHT AT SEAT 22C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041600164 20080416 00164 EA 2008 4 16 A6WA200840188 1 20080311 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 202 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 CRACK FOUND ON FORWARD PRESSURE BULKHEAD FS 202.75 AT PARKING BRAKE LT. FORWARD PRESSURE BULKHEAD AT LT FS 202.75 REPAI RED IAW REO 601R-53-11-563. 2 L 7 2 4F RT A21EA 2008041600166 20080416 00166 EU 2008 4 16 AALA200800762 1 20080329 A 3350 BR964B14 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 11060 470 JFK - EMERGENCY LIGHT AT SEAT 3D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 3D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008041600167 20080416 00167 NM 2008 4 16 AALA200800764 1 20080330 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 179AA 32397 DFW - EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041600168 20080416 00168 WP 2008 4 16 AALA200800763 1 20080330 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 416AA 49327 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 25DEF TO 27DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 25DEF TO 27DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008041600169 20080416 00169 NM 2008 4 16 UIEA200800139 1 20080403 A 5730 PANEL BOEING 747 747243B 1384830 NM ZONE 600 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 RIGHT WING LEADING EDGE FIXED PANEL AT WS 414 FOUND CORROSION/BULGE AT THE RABBET AREA. BLENDED OUT CORROSION PER SRM 5 1-10-01, REPROTECTED PER SRM 51-10-02. 2 L 7 4 4F RT A20WE 2008041600170 20080416 00170 EU 2008 4 16 F3LA200800161 1 20080411 A 5320 D5391635520000 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION AT NUT PLATES FWD CARGO PIT RIGHT SIDE FLOOR SUPPORT PLATE FRAME 28 TO FRAME 31. MAINTENANCE REMOVED AND REPLACED SUPPORT PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE INSTALLATION THE SUPPORT PLATE WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008041600171 20080416 00171 NM 2008 4 16 08FDEA01408 1 20080414 A 5730 ARB39548 DOUBLER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 525FE 48565 RIGHT WING LEADING EDGE SKIN RIB DOUBLER AT STATION XOS 799 FOUND CRACK. REMOVED PER SRM 51-33-01 VOLUME II AND FABRICA TED NEW DOUBLER PER DRAWING ARB3954 AND INSTALLED NEW DOUBLER PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041600172 20080416 00172 NM 2008 4 16 08FDEA01409 1 20080414 A 5230 FITTING DOUG MD11 MD11F 3023600 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 584FE 48436 MAIN DECK CARGO DOOR LOWER JAMB SPOOL FITTING NR 7 FOUND SECOND LAYER CRACK INDICATION AFTER BORE TO MAXIMUM 0.519 INCH. REPAIR CARRIED OUT PER EA 1-5310-120552, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041500165 20080415 00165 EA 2008 4 15 A6WA200840236 1 20080324 A 3240 SENSOR CNDAIR CL600 CL6002B19 1900309 EA RT BRAKE FAILED A A6WA O OTHER O OTHER AP APPROACH 1 GL 31 455AW 7848 FLAPS FAIL CAUTION MESSAGE ON APPROACH AT ZERO DEGREES, COMPLIED WITH QRH AND NORMAL LANDING. FOUND REPEAT RT BRAKE AND POSITION SENSOR UNIT FAILURES. REMOVED AND REPLACED RT BPSU PER AMM 27. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2008041500172 20080415 00172 EU 2008 4 15 F3LA200800157 1 20080411 A 5320 D5311278220201 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON FLOOR SUPPORT-Y1292, BETWEEN FRAMES 16 AND 20. MAINTEN ANCE REMOVED AND REPLACED THE CORRODED FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11 AND A319 SRM 5 1-72-11. UPON COMPLETION OF THE INSTALLATION, THE NEW SUPPORTWAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041500173 20080415 00173 EU 2008 4 15 F3LA200800158 1 20080411 A 5320 D5311282720100 DUMMY RAIL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON DUMMY RAIL Y503.2 AT FRAME 16. MAINTENANCE REMOVED AND REPLACED THE DUMMY RAIL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE INSTALLATION, THE NEW DUMMY RAIL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041500174 20080415 00174 SO 2008 4 15 LR7A08050 1 20080411 A 5230 PAD LKHEED 382 382G 526414U SO CARGO DOOR BROKEN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 70 4676 DURING SCHEDULED A CHECK PER JOB CARD HA1200, FOUND AFT OUTBD RAMP BUMPER PAD BROKEN AT LBL52, RAMP STATION 10, WL141. CARGO RAMP ASSY REPLACED WITH SERVICEABLE UNIT, RIGGED AND OPS CHECKED IAW SMP 581 52-30 PG 211-238. 2 H 7 4 4T A1SO 2008041500175 20080415 00175 WP 2008 4 15 08FDEA01388 1 20080412 A 5751 ARC10582 WEDGE DOUG MD10 MD1010F 3022112 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT OUTBD AILERON T/E WEDGE IS CRACKED ALONG THE EDGE AT THE INBD END. CUT OUT DAMAGED SECTION OF THE WEDGE IAW SRM 5 7-20-00; FIG 10; VOL I. FABRICATED A NEW WEDGE SECTION AND ZEE ANGLE IAW SRM 57-20-00; FIG 10; VOL I. ALODINED AND PRIMED IAW SRM 51-21-01; VOL II. INSTALLED IAW SRM 51-35-01; VOL II. 2 L 7 3 4F RT A22WE 2008041500176 20080415 00176 EA 2008 4 15 A6WA200840211 1 20080317 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION LD LANDING 1 GL 31 404AW 7294 FLAPS FAIL CAS MESSAGE AFTER LANDING WHEN FLAPS SELECTED TO ZERO POSITION, FLAPS READ 45 DEGREES LT, 45 DEGREES RT. (M) 2 L 7 2 4F RT A21EA 2008041500177 20080415 00177 EA 2008 4 15 A6WA200840197 1 20080305 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 461 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 FITTING CRACKED AT FS 461, LBL 9 AND WL 73. FITTING REPLACED AT FS 461, LBL 9 AND 73 IAW CRJ 200 SRM 51-42-06 AND SRM 5 1-42-21. (M) 2 L 7 2 4F RT A21EA 2008041500178 20080415 00178 EU 2008 4 15 TRBA2008041 1 20080413 A 3350 3012701 LIGHT AEROSP ATR72 ATR72212A 8680902 EU CABIN FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 536AT 536 MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW JIC NR 33-51-24. 2 H 7 2 4T RT A53EU 2008041500179 20080415 00179 EA 2008 4 15 A6WA200840206 1 20080317 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 31 417AW 7610 FLAP FAILED MESSAGE, FLAP FAILED AT ZERO. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4, FLAP S YSTEM RESET. OK. (M) 2 L 7 2 4F RT A21EA 2008041500180 20080415 00180 EA 2008 4 15 A6WA200840270 1 20080325 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 CROSSBEAM FS 280 LBL 9 WL 73 IS CRACKED. (M) REPAIRED IAW REO 601R-53-11-171 REV D SCHEME B. 2 L 7 2 4F RT A21EA 2008041500181 20080415 00181 WP 2008 4 15 08FDEA01389 1 20080412 A 2612 SMOKE DETECTOR DOUG DC10 DC1030F 3023504 WP CABIN MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 311FE 46871 CABIN SMOKE WARNING, TWO TIMES. FIRST TIME IN CLIMB PASSING FL310. BRIEF FLASH OF MASTER WARNING THEN WENT AWAY. 4-5 MIN LATER LEVEL AT FL330 GOT 2ND MASTER WARNING AND CABIN SMOKE FOR ABOUT 10 SECS. LANDED AT KPDX. FIRE DEPARTMENT I NSPECTION NO INDICATION OF HEAT. PER MX TURNOVER CREW REPORTED AREA 2 OF UPPER DECK WAS AREA CAUSING INPUT DURING FLIGH T. REMOVED AND REPLACED ALL NR 2 AREA DETECTOR UNITS PER MM 26-15-00. REMOVED AND REPLACED MSC PER MM 26-15-00. ALL OPS CKS C/W SYSTEM CKS NORMAL. ALSO CHECKED EACH VIA IN COMMAND MODE PER MM 26-15-01, OPS CK NORMAL. 2 L 7 3 4F RT A22WE 2008041500182 20080415 00182 NM 2008 4 15 08FDEA01390 1 20080413 A 2840 INDICATION SYS DOUG MD11 MD11F 3023600 NM FUEL QTY MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 628FE 48447 90 MINUTES INTO FLIGHT RECEIVED LATER FUEL IMBALANCE WITH FUEL CONTROLLER IN AUTO. RAN QRH AUTO CONTROLLER RESOLVED IMB ALANCE OF TNK 14000 LBS HEAVY. APPROXIMATELY 10 MINUTES LATER FP/R FUEL LOG INDICATED A CHANGE OF 2000 LBS UNACCOUNT ED FOR AND INCREASING OVER TIME. THEN RECEIVED LVL 2 ALERT: FUEL OFF SCHEDULE. RAN QRH AND PUT FUEL SYS CONTROLLER IN MANUAL. OVER NEXT 20 MINUTES EFOB AT DESTINATION CONTINUED TO DECREASE AND T/O FUEL MINUS USED CONTINUED TO INCREASE. REMOVED AND REPLACED NR 1 INBOARD AND OUTBOARD MJP IAW MM-28-41-40-4, LEAK CHECK GOOD. OPS TEST CHECKED GOOD IAW MM 28- 41-00-5. 2 L 7 3 4F RT A22WE 2008041500183 20080415 00183 NM 2008 4 15 08FDEA01391 1 20080414 A 5712 ARB2850506 RIB DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 525FE 48565 RIGHT WING LEADING EDGE RIB FOUND CRACKED AT INBOARD OF SLAT TRACK NR 16. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL UME II. SLAT CABLES 83 AND 84 ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-00-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041500185 20080415 00185 NM 2008 4 15 08FDEA01393 1 20080414 A 5311 AFA00203 FRAME DOUG MD11 MD11F 3023600 NM BS 1701 L12R DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 525FE 48565 MAIN DECK, RIGHT FUSELAGE FRAME AT STATION 1701, LONGERON 12 RIGHT FOUND DENTED. REPAIRED AS PER SRM 53-30-00- FIGURE 1 VOLUME I. REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYC LES TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041500188 20080415 00188 NM 2008 4 15 08FDEA01396 1 20080414 A 5311 ACA73511 FRAME DOUG MD11 MD11F 3023600 NM BS 535 L24L CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 525FE 48565 MAIN DECK, LEFT FRAME AT STATION 535, LONGERON 24 LEFT, ONE EACH CHAFED MARK FOUND CAUSED BY 9G NET YOKE. REPAIRED AS PER DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041500195 20080415 00195 NM 2008 4 15 SWAA081931 1 20080410 A 5310 65458721 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR CUTOUT LOWER FWD CORNER STUB FRAME CRACKED. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008041500209 20080415 00209 NM 2008 4 15 SWAA081914 1 20080410 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041500211 20080415 00211 NM 2008 4 15 SWAA081915 1 20080410 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041500225 20080415 00225 NM 2008 4 15 USAA920080684 1 20080311 A 5753 6546430100SP SKIN BOEING 737 7373G7 1384595 NM FOREFLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCM - MAJOR REPAIR-C18- RIGHT T/E INBOARD FORE FLAP IS DELAMINATED UPPER SURFACE, WBL 117.00. CUT OUT DAMAGED SKIN AND CORE, INSTALLED NEW CORE AND DOUBLER IAW SRM 51-70-10-2R4 FIG 203. 2 L 7 2 4F RT A16WE 2008041500229 20080415 00229 NM 2008 4 15 EMB08002 1 20080406 A 3350 340022 BATTERY PACK EMB ERJ190 ERJ190100IGW 3260408 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 954UW 642 19000139 CLT - EMERGENCY LIGHT MID CABIN, OVERWING CEILING PANEL EXIT SIGN, FORWARD SIDE AND CEILING EMERGENCY LIGHT AT PANEL FIV E ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY NICAD BATTERY PACK. 2 L 7 2 4F RT A57NM 2008041500234 20080415 00234 NM 2008 4 15 USAA920080757 1 20080328 A 5311 652072270 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 460UW 25024 PIT - MAJOR REPAIR - FPBH INSPECTION, FRAME CRACKED, BS 440, S24R. REPAIRED FRAME, BS 440, S24R, IAW US AIRWAYS EA 1108 07. 2 L 7 2 4F RT A16WE 2008041600001 20080416 00001 WP 2008 4 16 08FDEA01416 1 20080401 A 5753 ARC29912 PANEL DOUG MD10 MD1010F 3022112 WP TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 RIGHT WING INBD FLAP PANEL 644 AB IS DISBONDED. REPAIRED PANEL 644 AB BY REMOVING DAMAGED OUTER SKIN; INNER AND OUTER D OUBLERS. FABRICATED AND BONDED NEW SKIN; INNER AND OUTER DOUBLERS IAW DAC DWG NR ARC 2991; TPS 101, REV E AND FEDEX EA 8-5750-118470 TITLED "WINGS - INBD FLAP NR 1 ROLLER ACCESS COVER PANEL". FABRICATED AND INSTALLED NEW -33 STIFFENER IAW DAC DWG ARC 2991 AND FEDEX EA 8-5750-118470 TITLED "WINGS INBD FLAP NR 1 ROLLER ACCESS COVER PANEL". 2 L 7 3 4F RT A22WE 2008041600002 20080416 00002 WP 2008 4 16 NWAA081509872 1 20080414 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 781NC 48121 DURING LINE CHECK, THE EMERGENCY OVERWING EXIT SIGNS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PAC K (B5-49) AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 2 L 7 2 4F RT A6WE 2008041600011 20080416 00011 NM 2008 4 16 UIEA200800106 1 20080402 A 7830 AMS55180063IN LOCK PLATE BOEING 747 747243B 1384830 NM THRUST REVERSER WRONG PART A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 NR 1 ENGINE RIGHT SIDE THRUST REVERSER FORWARD EDGE LOWER THRUST REVERSER LOCK PLATE POSITION FOUND WRONG LOCK BOLT HOLE S. REPAIRED PER CF6-50 ENGINE MANUAL 78-32-03. 2 L 7 4 4F RT A20WE 2008041600028 20080416 00028 NM 2008 4 16 AALA200800784 1 20080329 A 3350 D71701100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 912AN 29513 TUL - EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED OPERATIONAL CHECK. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN CAB IN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008041600032 20080416 00032 EA 2008 4 16 A6WA200840179 1 20080311 A 2760 SWITCH CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 424AW 7656 CAPTAIN ROLL SELECT SWITCH GREEN AND YELLOW LIGHTS INSPECTION WHEN SELECTED DO NOT RECEIVE "PILOT ROLL COMMAND" EICAS ME SSAGE. FIRST OFFICERS ROLL SELECT SWITCH OPERATES NORMAL. (M) 2 L 7 2 4F RT A21EA 2008041600035 20080416 00035 WP 2008 4 16 08FDEA01401 1 20080414 A 5311 ABA7348U3 FRAME DOUG DC10 DC1010F 3022111 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 MODIFICATION TO ACF IN AVIONIC COMPARTMENT RT SIDE STA 469 X =-61 FOUND FRAME WITH CRACK 1 INCH REPAIRED FOR SRM 53-30-00 FIG 11 VOL I. 2 L 7 3 4F A22WE 2008041600040 20080416 00040 NM 2008 4 16 08FDEA01406 1 20080414 A 5320 146N8769U48 STIFFENER BOEING 757 75727B 1384921 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 CORROSION FOUND ON R4 DOOR SCUFF PLATE SUPPORT BRACKET AT STA 1656, STA 1678, RBL 66. INSTALLED NEW SUPPORT BRACKET AT STA 1656, STA 1678 RBL 66 IN ACCORDANCE WITH B757 SRM 51-40-02 REV 93. REPAIRED CLASSIFIED AS MINOR PER FEDEX GMM 6-02 -100. 2 L 7 2 4F RT A2NM 20080516 NM 2008 5 16 SWAA082585 1 20080512 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED SPV CHECK, FOUND LEFT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082581 1 20080512 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. REMOVED AND REPLACED GIRT BAR H OOK PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082575 1 20080509 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082574 1 20080509 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082573 1 20080509 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 20080516 EA 2008 5 16 SWIA200819566 1 20080429 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 919SW 7657 FLT 6055 - EMERGENCY FLOOD LIGHT IS INOP. REPLACED NR 4 ELBP BATTERY CHARGER IAW CRJ MM 33-51-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080516 EA 2008 5 16 SWIA200819567 1 20080429 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS UNSECURE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 453SW 7743 FLT 3775 - FLOOR ILLUMINATION STRIP IS INOP AFT OF EMERGENCY EXIT. RESECURED CONNECTION ON LIGHTING TRACK. OPS CHECK G OOD. 2 L 7 2 4F RT A21EA 20080516 SO 2008 5 16 SWIA200819568 1 20080420 A 3397 WIRE EMB 120 EMB120ER 3260203 SO GALLEY LIGHTS FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 232SW 120306 FLT 5570 - ELECTRICAL SMOKE REPORTED IN THE GALLEY AREA. REPAIRED GALLEY LIGHT WIRING AND REPLACED LIGHT BULB IAW MM 33 -21-05. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080516 NM 2008 5 16 SWAA082591 1 20080512 A 3350 MS155721 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 738CB 27870 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082580 1 20080512 A 5315 147A55068 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 762SW 27876 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 986.5, RBL 48 TO LBL 48. REPAIRED CHORD PER SWA EA. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082629 1 20080513 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082626 1 20080513 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 2008UALA02476 1 20080425 A 5320 SUPPORT BRACKET BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NLG TUNNEL CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 RT SIDE NLG TUNNEL AREA BS 246 FLOORBEAM HAS PULLEY SUPPORT BRACKET CRACKED AT RBL 15. REMOVED BRACKET AND INSTALLED NE W BRACKET. 2 L 7 2 4F 4 F RT A1NM E24NE 20080516 2008 5 16 2008UALA02478 4 20080426 A 2565 101651303 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE R2 DOOR DEFECTIVE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 648UA 25285 NEW SLIDE FOR DOOR 2 RT BECAME UNRAVELED. SLIDE IS IN ACFT NOT INSTALLED. SUSPECT IMPROPERLY PACKED SLIDE. REPLACED S LIDE PER MM 25-66-01. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080516 2008 5 16 2008UALA02479 4 20080425 A 2565 HOUSING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 RIGHT EMERGENCY EXIT SLIDE DISCONNECT HOUSING IS BROKEN (CRACKED). FOUND DISCONNECT HOUSING CRACKED. REPLACED DISCONNE CT HOUSING IAW MM 25-65-98 FREEDOM OF MOVEMENT CHECK GOOD IAW MM 25-65-04.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080516 2008 5 16 2008UALA02480 4 20080427 A 2565 SLIDE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE R2 DOOR MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 668UA 30024 DOOR SLIDE 2RH SLIDE PACK COMING UNHOOKED ON FWD SECTION OF SLIDE PACK. IMPROPERLY INSTALLED DOOR SLIDE. REPLACED SLI DE PACK ASSY REF MM 25-66-01. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080516 NM 2008 5 16 2008UALA02482 1 20080428 A 3350 D71702001 BATTERY BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHT DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 216UA 30549 CREW REST AREA EMERGENCY LIGHTS FAILED TIME TEST. SUSPECT LOW BATTERY PACK. RECHARGED SYSTEM. OPS CK'D GOOD PER MM 33- 51-00, PG 209.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080516 EU 2008 5 16 2008UALA02491 1 20080428 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 448UA 842 CORROSION ON R2 DOOR SILL AT FRAME 68. REPLACED SILL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080516 NM 2008 5 16 2008UALA02493 1 20080428 A 5310 SPLICE PLATE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD CARGO DOOR CUTOUT, FWD UPPER INNER CORNER, TOMAHAWK SPLICE SUPPORT PLATE HAS 20 ELONGATED HOLES, THIS PLATE TIES STR 18R INNER CHORD WITH THE BS 440 FRAME INNER CHORD. FABRICATED AND INSTALLED SPLICE PLATE, BS 430-450 STR 18R-19R. 2 L 7 2 4F 4 F RT A16WE E2GL 20080516 NM 2008 5 16 2008UALA02498 1 20080428 A 3350 60252 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 342UA 24246 LEFT AFT GALLEY AREA 3' STRIP INOP. REPLACED EEL STRIP. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 20080516 NM 2008 5 16 2008UALA02500 1 20080429 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 STAIRWAY EMERGENCY LIGHT INOP. SUSPECT FAULTY LAMP. REPLACED LAMP OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080516 NM 2008 5 16 2008UALA02501 1 20080429 A 3350 1317LAMP276005FU LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 RT OW EMERG LIGHT INOP 1ST AND 2ND POS. REPLACED LAMPS AND FUSES. OP CHK'D GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20080516 WP 2008 5 16 UPS08852113 1 20080420 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING LE OUTBD UPPER RIB CRACKED JUST OUTBD OF ACCESS PNL 520A AT XFS 603.0. REPAIRED LT WING LE O UTBD UPPER RIB AT XFS 603.0 IAW SRM 57-02-00-0 FIG 002 AND SRM 57-03-03 FIG 006. 2 L 7 4 4F RT 4A25 20080516 WP 2008 5 16 UPS08852132 1 20080401 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 COMPLY WITH MPI P19472 NON CONFORMING REPAIR AT L28L IAW ATTACHED WAN 1372778, MPI SUMMARY REPORT, AN D EO DC8-5330-20248-E APPX D. REMOVED OLD DOUBLER, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1 -8, 53-2-0, 51-1-26 , 51-3-1, EO DC8-5330-20248 APPX D. 2 L 7 4 4F RT 4A25 20080516 2008 5 16 UPS08852147 4 20080501 A 2565 SLIDE DOUG DC8 DC871F 302199D WP ENTRY DOOR UNSECURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 MAIN CABIN DOOR SLIDE NOT SECURE. RESECURED SLIDE HALVES AND SLIDE COVER TO ENTRY DOOR PER MM 25-60-01-2. 2 L 7 4 4F RT 4A25 20080519 NM 2008 5 19 QXEA200800432 1 20080425 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR DIRTY A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 419QX 4145 SEA - FLIGHT ATTENDANT REPORTS THAT THE FORWARD PASSENGER IS HARD TO OPEN. MAINTENANCE CLEANED AND LUBED THE DOOR. OPE RATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080519 EU 2008 5 19 08FDEA01826 1 20080512 A 5414 A2210081232000 PANEL AIRBUS 310 A310 EU ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 NR 2 PYLON AFT LOWER FAIRING PANEL 485 AL; FWD UPPER RT ATTACH PLATE IS CHAFED ON THE INNER SURFACE. REMOVED ATTACH P LATE & INSTALLED A NEW ATTACH PLATE PER SRM 51-40-21 PARA 6. LOCATED & DRILLED HOLES PER SRM 51-40-21 PARA 6. ALODINED P ER SRM 51-21-10. PRIMED PER SRM 54-23-10. APPLIED PAINT PER AMM 51-33-10-0. 2 L 7 2 4F RT A35EU 20080519 NM 2008 5 19 DHL2008760506 1 20080413 A 5754 6516269 WEB BOEING 727 7272B7 138407L NM KRUEGER FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED AND REPLACED NR 2 K-FLAP INBOARD AND OUTBOARD ACTUATOR MOUNT SUPPORT WEBS BY FABRICATION, LWS 236.2 TO 244.0, PE R B727 SRM 51-10-2, 51-30-2, 51-20-1 FIG 3, 51-30-5, AND BAC DWG 65-16269 REV C. 2 L 7 3 4F A3WE 20080519 NM 2008 5 19 DHL2008760507 1 20080416 A 5712 FIRESHIELD BOEING 727 7272B7 138407L NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 FABRICATED AND INSTALLED REPAIR DOUBLERS TO 5 EA CRACKS IN THE L/WING L/E FIRE SHIELD, LWS 115 TO 130, PER EVA B257-0005 2 REV IR, DWG NR 25700052-001-B REV IR, AND APPROVED BY 8110-3 DATED 4/2/08. 2 L 7 3 4F A3WE 20080519 WP 2008 5 19 08FDEA01827 1 20080512 A 5320 ADJ70031 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 CENTER CARGO COMPARTMENT LT TRANSITION PANEL SUPPORT FITTING HAS CORROSION; MOUNTED ON THE FRAME AT FS 1661 LBL 43. RE MOVED CORROSION IAW 51-21-01; VOL II. FOUND TO BE EXFOLIATED. REMOVED & REPLACED ADJ7003-1 FITTING. IAW SRM 51-33-01; VOL II. 2 L 7 3 4F RT A22WE 20080519 2008 5 19 08FDEA01838 4 20080513 A 3414 2083081 INDICATOR BOEING 727 727200 138407E NM AIRSPEED FAILED A FDEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 25 245FE 9929 4574 22016 CAPT'S AIRSPEED INDICATOR NOT WORKING. NO AIRSPEED INDICATION- AIARSPEED FLAG IN VIEW. REMOVED AND REPLACED CAPT'S AIR SPEED IND PER MM 34-12-021-4. AC OK TO CONTINUE. 2 L 7 3 4F RT A3WE 20080519 WP 2008 5 19 UPS08852160 1 20080413 A 5310 3755B27U2 FITTING DOUG DC8 DC873F 302199F WP DOOR FRAME CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 A-PIT RT STA 280 L32R, OUTER AFT SIDE OF TORQUE BOX, FITTING HAS HEAVY CORROSION. REMOVED AND REPLAC ED DOOR JAMB FRAME FITTING IAW SRM 51-1-8, 51-1-20D 51-3-2. 2 L 7 4 4F RT 4A25 20080519 EU 2008 5 19 08FDEA01839 1 20080513 A 5730 A5715132620200 PANEL AIRBUS 310 A310 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 LT WING FUEL PANEL ASSY 550 AT CLAMP RING HAS AREAS OF FRETTING. REMOVED & REPLACED THE CLAMP RING IAW SRM 57-20-16. 2 L 7 2 4F RT A35EU 20080519 WP 2008 5 19 08FDEA01842 1 20080513 A 5420 NSL601697 RUB STRIP DOUG MD10 MD1010F 3022112 WP ZONE 400 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 3 ENGINE INBD CORE COWL UPPER RUB STRIP IS WORN (GOUGED). REMOVED THE DAMAGED RUB STRIP IAW SRM 51-35-01 VOL II. FAB RICATED PER DWG NSL 6061, REV "BC". PRIMED & PAINTED IAW SRM 51-21-01; PG 21; 51-23-01; VOL II. INSTALLED IAW 51-2 3-01; VOL II. 2 L 7 3 4F RT A22WE 20080519 NM 2008 5 19 DHL2008784001 1 20080430 A 2782 SUPPORT BRACKET BOEING 727 727227 1384078 NM FLAP ACTUATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 784DH 22001 NR 5 K-FLAP ACTUATOR BOX HAS SMALL CRACK ON THE O/B SUPPORT BRACKET L/E STA 243.977 CRACK LOCATED AT LOWER FWD CORNER OF BRACKET. 2 L 7 3 4F A3WE 20080519 WP 2008 5 19 DHL2008807501 1 20080422 A 5712 FRAME DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 RT WING CTR L/E LWR FORMER CRACKED 0.250", STA XFS 304.000. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED (2EA) ANGLE DOUBLER (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DO UBLERS IAW SRM 51-1-8B. INSTALLED ANGLE DOUBLERS IAW SRM 57-2-0 PG 9-10, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 20080519 WP 2008 5 19 08FDEA01852 1 20080515 A 5340 ADJ70031 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 THE CENTER CARGO COMPARTMENT, LEFT TRANSITION PANEL SUPPORT HAS CORROSION AT STATION 1601, STRINGER 43L. REMOVED CORROSI ON IAW SRM 51-21-01; VOL II. FOUND TO TO BE EXFOILEATED. REMOVED AND REPLACED ADJ 7003-1 FITTING, IAW SRM 51-33-0 1; VOL II. 2 L 7 3 4F RT A22WE 20080519 NM 2008 5 19 AALA200800842 1 20080407 A 3350 OL3071BPEGPL LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 DFW - EMERGENCY LIGHT AT SEAT 41C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 41C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 EU 2008 5 19 08FDEA01848 1 20080512 A 5330 A537770532000 SKIN AIRBUS 310 A310 EU ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 FOUND EVIDENCE OF A CRACK STARTING AT A FASTENER HOLE ON THE RIGHT EXTERNAL SIDE OF THE FUSELAGE SKIN BETWEEN STRINGER 2 1R & STRINGER 22R & FRAMES 40 TO 41. BLENDED AREA IN REF TO SRM 51-74-10. ORIGINAL MATERIAL THICKNESS 0.061 IAW SRM 53 -14-12. MATERIAL REMOVED WAS 0.002. MATERIAL REMAINING IS 0.059. FOUND TO BE WITHIN LIMITS IAW SRM 53-10-12; DIA 0 .112. ACCOMPLISHED HFEC INSPECTION PER NTM PART 6; 51-10-8; NO CRACK NOTED. ALODINED IAW SRM 51-21-10. PRIMED & TOP COATED IN REF TO AMM 51-23-10-0. 2 L 7 2 4F RT A35EU 2008051500011 20080515 00011 EA 2008 5 15 SWIA200819610 1 20080511 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 817SK 15107 FLT 4016 - AFT EMERGENCY POD LIGHT IS INOP. RELAMPED AFT EMERGENCY POD LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008051500016 20080515 00016 SO 2008 5 15 SIMA200813404 1 20080508 A 3320 BR900022 BALLAST EMB 145 EMB145LR 3260212 SO CABIN LIGHTS ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 21 628AE 145124 ON FLIGHT 4183, CREW REPORTED FLIGHT ATTENDANT NOTED ELECTRICAL ODOR JUST BEFORE LANDING. AIRCRAFT REMOVED FROM SERVICE . REMOVED AND REPLACED LIGHTING BALLAST REF EMB 145 33-21-06. NO DEFECTS NOTED, NR 8194. AIRCRAFT RETURNED TO SERVICE . 2 L 7 2 4T RT T00011AT 2008051500024 20080515 00024 NM 2008 5 15 2008UALA02544 1 20080501 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE G2 GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EEL LIGHT INOP AT G2 GALLEY SIDE WALL. REPLACED EEL LIGHT. OP CHK GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 2008051500035 20080515 00035 NM 2008 5 15 AALA200800825 1 20080406 A 2910 271N61192 HOSE BOEING 757 757223 1384957 NM HYD SYSTEM LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 696AN 26976 AUA INFLIGHT T1780/06APR - CREW REPORTED LOSS OF QUANTITY AND PRESSURE ON LEFT HYDRAULIC SYSTEM. RETURNED TO AUA AND LA NDED WITHOUT INCIDENT. MANUALLY LOWERED FLAPS AND LANDING GEAR. AIRCRAFT WAS TOWED OFF RUNWAY. FOUND ONE HYDRAULIC LI NE ON RIGHT MAIN GEAR DOWN LOCK ACTUATOR LEAKING. REPLACED RIGHT MAIN GEAR DOWN LOCK ACTUATOR FLEX LINE WITH TEMPORARY HYDRAULIC FLEX LINE. SERVICED LEFT SYSTEM TO FULL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051500040 20080515 00040 WP 2008 5 15 08FDEA01722 1 20080501 A 5414 NSL6051517 NOSE COWL DOUG MD10 MD1010F 3022112 WP NR 1 NACELLE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 1 ENGINE NOSE COWL L/E HAS NUMEROUS AREAS OF PITTED CORROSION ALONG THE ENTIRE CIRCUMFERENCE OF EXTERNAL SKIN. REMOV ED THE CORROSION IN REF TO DC/MD-10 SRM 51-21-01; VOL II AND FOUND TO BE OUT OF LIMITS IN REF TO DC/MD-10 SRM 54-00-01; VOL I. REMOVED & REPLACED THE NR 1 ENGINE NOSE COWL REF MD-10-10 AMM 71-11-00-2. PERFORMED AN ANTI ICE OPS CHECK. OP'S CHECKED GOOD. 2 L 7 3 4F RT A22WE 2008051500044 20080515 00044 WP 2008 5 15 08FDEA01729 1 20080502 A 5730 ARB126331 ACCESS PANEL DOUG MD10 MD1010F 3022112 WP LT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 LEFT WING LEADING EDGE FIRE BOTTLE COMPARTMENT ACCESS PANEL IS CHAFING AROUND THE CONTACT SURFACE. REPAIRED PANEL BY B LENDING CHAFED AREA & CHECKING LIMITS IAW SRM 57-00- 01; VOL I. BLENDED AREAS FOUND TO BE OUT OF LIMITS. REMOVED PAN EL IAW SRM 51-31-01; VOL II. FABRICATED & BOUNED REPAIR DOUBLER IAW SRM 51-71-00; VOL II & EA 8-5720-118487. INSTALLE D IAW SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 2008051500071 20080515 00071 NM 2008 5 15 AALA200800891 1 20080409 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 343AN 33082 SFO - EMERGENCY LIGHT AT RIGHT AFT OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT AFT OVERWING. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008051500096 20080515 00096 EA 2008 5 15 SWIA200819571 1 20080425 A 5241 ROLLER CNDAIR CL600 CL6002B19 1900309 EA GALLEY DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 457SW 7773 FLT 3872 - GALLEY DOOR IS DIFFICULT TO OPEN. INSPECTED, CLEANED AND LUBRICATED OUTER HANDLE SLIDER AND CAM ROLLER. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008051500123 20080515 00123 NM 2008 5 15 AALA200800947 1 20080413 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 196AA 32390 DFW - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051500167 20080515 00167 NM 2008 5 15 08FDEA01816 1 20080510 A 5347 BAC1520792 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 780-879 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 906FD 27148 FOUND SEAT TRACK STA 780-879 RBL 24 HAS CORROSION. REMOVED SEAT TRACK, FAB`D NEW FROM MAT BAC1520-792 IAW SRM 53-00-52. INSTALLED SEAT TRACK STA 780-879, RBL 24 IAW SRM 51-40-05. 2 L 7 2 4F RT A2NM 2008051500170 20080515 00170 WP 2008 5 15 08FDEA01831 1 20080512 A 5744 ARC05026 HINGE DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 RIGHT WING OUTBD FLAP, OUTBD HINGE LOCATION NR 3 INBD BORE IS CORRODED. REMOVED THE CORROSION FROM THE INBD BORE IAW CM M 57-44-01. MACHINED NEW BUSHINGS FOR THE INBD BORE IAW CMM 57-44-09. CAD PLATED BUSHING IAW QQP-416-7Y2- CL2. INS TALLED THE NEW BUSHING INTO INBD THE BORE OF THE NR 3 LUG IAW CMM 57-44-01. COMPLIED WITH FEDEX EA 8-5740-116979 DATED 5/1/2008. 2 L 7 3 4F RT A22WE 2008051500181 20080515 00181 NM 2008 5 15 DLM90080704 1 20080506 A 5320 WEB DOUG MD90 MD9030 3023690 NM BS 200 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 FLOOR MEMBRANE CORRODED FS 200 RBL 48-54. REPAIRED FLOOR MEMBRANE, IAW MD90 SRM 51-30-02, VOL 3. 2 L 7 2 4F RT A6WE 2008051500192 20080515 00192 SO 2008 5 15 SWIA200819613 1 20080508 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DAMAGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 223SW 120291 FLT 5712 - EXIT LIGHT ON OVERHEAD BIN AT ROW 9 IS INOP. REPAIRED WIRING TO EMERGENCY LIGHT ON OVERHEAD BIN. 2 L 7 2 4T RT A31SO 2008051600007 20080516 00007 NM 2008 5 16 SWAA082471 1 20080506 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 366, STR 26L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008051600008 20080516 00008 NM 2008 5 16 SWAA082470 1 20080506 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED SPV CHECK, FOUND STRINGER 26R CORRODED AT BS 830 TO BS 840. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 2008051600009 20080516 00009 NM 2008 5 16 SWAA082468 1 20080506 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BS 394, STR 17R. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008051600011 20080516 00011 NM 2008 5 16 SWAA082469 1 20080506 A 5210 65458712 SKIN BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED SPV CHECK, FOUND R1 DOOR SKIN CRACKED AFT OF WINDOW. REMOVED AND REPLACED DOOR PER MM. 2 L 7 2 4F RT A16WE 2008051600022 20080516 00022 NM 2008 5 16 SWAA082495 1 20080506 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008051600025 20080516 00025 NM 2008 5 16 SWAA082472 1 20080506 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER MM. 2 L 7 2 4F RT A16WE 2008051600040 20080516 00040 NM 2008 5 16 SWAA082486 1 20080506 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 752SW 29804 DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 2008051600056 20080516 00056 2008 5 16 SWAA082502 4 20080507 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082522 1 20080508 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED MV1 CHECK, FOUND FWD EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082564 1 20080511 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082596 1 20080512 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082590 1 20080512 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 712SW 27846 DURING SCHEDULED MV2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 2008UALA02503 1 20080429 A 3350 210013 SWITCH BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT SWITCH GUARD SPRING BROKEN AND SW ASST BROKEN AT L1 ATTENDANT SEAT HANDSET CRADLE. REPLACED SW AND GUAR D OP CHK GOOD PER WDM 33-51-11, AMM33-51-00 PB 500 CONFIG 1 PARA 3. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080519 NM 2008 5 19 QXEA200800433 1 20080428 A 5240 DOOR BOMBDR DHC8 DHC8402 1390042 NM SERVICE DOOR DIRTY A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 418QX 4143 SEA - REAR SERVICE DOOR HARD TO OPEN FROM THE OUTSIDE. MAINTENANCE CLEANED AND LUBED THE DOOR HANDLE. OPERATIONAL CHEC KS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080519 NM 2008 5 19 DLM90080664 1 20080424 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 UPON REMOVAL OF SEAT TRACK, FOUND CUSP WEB CRACKED. REPAIRED CUSP WEB, IAW MD90 SRM 51-11-01. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 QXEA200800452 1 20080507 A 2120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 423QX 4153 PSC- FLIGHT 2222 - FLIGHT ATTENDANT AT "B" STATION REPORTED THE POSSIBLE SMELL OF SMOKE. NO VISUAL INDICATION OF ANY SM OKE. MAINTENANCE INSPECTED THE GALLEY AREA FOR SIGNS FOR SIGNS OF OVERHEATING, NONE FOUND. INSPECTED CIRCUIT BREAKERS, NONE TRIPPED AND NO SMOKE OR ELECTRICAL SMELLS NOTED. ALL GALLEY EQUIPMENT FUNCTIONS NORMAL. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080519 EA 2008 5 19 SWIA200819604 1 20080215 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 971SW 7947 LEFT SIDE OF STA 621 MOST OUTBOARD FLOOR FRAME IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ200 REO 601R 53-61-117 REV C DATED 2004-AUG-25. 2 L 7 2 4F RT A21EA 20080519 WP 2008 5 19 08FDEA01806 1 20080507 A 5522 STRUCTURE DOUG MD10 MD1010F 3022112 WP ELEVATOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 LT HORIZ STAB DROOP ELEVATOR UPPER AND LOWER SKIN HAVE WORKING FASTENERS NUMEROUS PLACES. REMOVED FSATENERS; HOLES IN THE SKIN & RIB DAMAGED. REMOVED DAMAGED RIB & SKIN. ALODINED; PRIMED & TOP COATED IAW SRM 51-21-01; VOL II. INSTALL ED DOUBLER; FILLERS AND ANGLE IAW SRM 55-10-00; VOL I & 55-20-00; VOL I. 2 L 7 3 4F RT A22WE 20080519 NM 2008 5 19 AALA200800917 1 20080410 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 756AM 30264 DFW - EMERGENCY LIGHTS AT OVERHEAD RIGHT BUSINESS CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVE RHEAD RIGHT BUSINESS CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 NM 2008 5 19 AALA200800896 1 20080410 A 3350 LIGHT BOEING 757 757223 1384957 NM EXIT SIGN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 678AN 29428 ORD - EMERGENCY EXIT LOCATION SIGN AT OVERHEAD BETWEEN LEFT AND RIGHT NUMBER ONE DOORS DIM. REPLACED LAMPS FOR EMERGENC Y EXIT LOCATION SIGN AT L25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080519 NM 2008 5 19 AALA200800898 1 20080410 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 689AA 25731 DFW - EMERGENCY LIGHT AT AFT SEAT 16D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT AFT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080519 NM 2008 5 19 F3LA200800252 1 20080425 A 5311 D5357155420200 FRAME AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C3 S1 C CHECK INSPECTION NOTED FRAME 72 DAMAGED AT STRINGER 26 LEFT. MAINTENANCE REMOVED AND REPLACED FRAME 72 I N ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 FIGURE 8. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND A CCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080519 NM 2008 5 19 08FDEA01808 1 20080510 A 5730 ARB74024 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 631FE 48454 06 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWE EN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-122445. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 2 L 7 3 4F RT A22WE 20080519 EU 2008 5 19 08FDEA01810 1 20080510 A 5347 A5327501820500 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 MAIN DECK SEAT TRACK NR 4 RT BETWEEN FR 57.1 AND FR 57.2 HAS 2 EA AREAS OF CORROSION REMOVED LEVEL 1 CORROSION. REMO VED AND REPLACED SEAT TRACK SECTION 4 RT BETWEEN FR 54.2 AND FR 58 IAW A300-600 SRM 53-1016. 2 L 7 2 4F RT A35EU 20080519 NM 2008 5 19 08FDEA01819 1 20080512 A 5414 311N51932 SKIN PANEL BOEING 757 75727B 1384921 NM NR 2 PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 916FD 24137 PYLON NUMBER TWO LEFT FORWARD STRUT SKIN CUT OUT AT ACCESS PANEL 443GL FOUND CORROSION, FROM PPS 100 TO PPS 126. EVAL UATE AND RECTIFY. REPLACED PYLON NUMBER TWO STRUT SKIN CUT OUT PANEL 443GL IN ACCORDANCE WITH BOEING DRAWING 311N5002 AND SRM 51-10-02 REVISION 93. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080519 EU 2008 5 19 08FDEA01824 1 20080512 A 5420 ATTACH ANGLE AIRBUS 310 A310324 3930206 EU NR 2 PYLON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 NR 2 PYLON LOWER FAIRING PANEL NR 485 AL, RT UPPER ATTACH ANGLE IS CHAFED IN SEVERAL PLACES. REMOVED THE NR 2 PYLON LOW ER FAIRING UPPER ATTACH ANGLE PER FEDEX SRM 51-40-21. LOCATED & DRILLED NEW UPPER ATTACH ANGLE IAW SRM 51-40-44. ALODI NED & PRIMED NEW ATTACH ANGLE IAW AMM 51-23-10-0. RECEIVED CLIP. LOCATED & DRILLED CLIP IAW SRM 51-40-40. INSTALLED CLI P & UPPER ATTACH ANGLE IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080519 SO 2008 5 19 SWIA200819569 1 20080429 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 218SW 120287 FLT 5706 - DURING CLIMB-OUT, THE LAV SMOKE DETECTOR ACTIVATED. NO VISIBLE SMOKE REPORTED. INSPECTED AND RAN BOTH PACK SYSTEMS WITH NO DISCREPENCIES NOTED. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080519 SO 2008 5 19 SMIA200812603 1 20080504 A 2130 M8353616022M RELAY EMB 135 EMB135LR 3260305 SO CABIN PRESS SYS FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 705AE 145184 FLT 4585, CREW REPORTED THAT THEY LOST CABIN PRESS AT LF 370, CREW PERFORMED EMERGENCY DESCENT AND CABIN SPIKED BETWEEN 14,000 AND 16,000, CREW HAD PRESSURIZATION AUTO FAIL MESSAGE, CABIN STARTED DESCENDING RAPIDLY, AT 10,000 CREW GOT CONTR OL OF PRESSURIZATION IN MANUAL MODE, DUMPED CABIN ON SHORT FINAL W/CABIN ALT 500 FEET BELOW FIELD ELEVATION, CABIN START ED RAPID DESCENT, 2500 FPM DOWN, AFTER ABOUT 30 SEC WENT TO MAN MODE TO REGAIN CONTROL. AIRCRAFT REMOVED FROM SERVICE. DEFERRED AUTO PRESSURIZATION. PER MEL 21-16 AUTH 050108DM-C. ENTERED ON MIC SHEET. PERFORMED FIM TASK 21-31-810-810-A. REMOVED AND REPLACED RELAY KO264 IAW AMM 20-13-02. PERFORMED OPERATIONAL CHECK OF AUTO AND MANUAL PRESSURIZATION IAW A 2 L 7 2 4F RT T00011AT 20080519 WP 2008 5 19 08FDEA01829 1 20080512 A 5753 ARC05026 HINGE DOUG MD10 MD1010F 3022112 WP T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 RIGHT WING OUTBD FLAP, INBD HINGE, LOCATION NR 3 INBD LUG FACE OUTER SURFACE IS CORRODED. LUG THICKNESS VERIFIED TO BE .421 IAW BAC CMM 57-44-01. CORROSION FOUND AND REMOVED FROM LUG FACE NR 3 INBD TO .405. LUG FOUND TO BE OUT OF LIMITS IAW BAC CMM 57-44-08. ETCHED NR 3 LUG FACE IAW SOPM 20-11-02. FLAP PEENED NR 3 INBD LUG FACE IAW SOPM 20-11-01. CAD PLATING REQUIRED AND ACCOMPLISHED ON N/R N00629 FOR THE TOTAL SURFACE AREA. 2 L 7 3 4F RT A22WE 20080519 EA 2008 5 19 SWIA200819624 1 20080227 A 7120 SHAFT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT ENGINE MOUNT WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 909SW 7558 RIGHT ENGINE AFT MOUNT THRUST SHAFT IS WORN, FOUND AT C-CHECK. REPLACED ENGINE THRUST SHAFT IAW CRJ200 AMM 71-00-00-400 -801. 2 L 7 2 4F 4 F RT A21EA E15NE 20080519 WP 2008 5 19 070197 1 20080508 A 5754 5922534506 SLAT DOUG DC9 DC983 3022083 WP RT WING DAMAGED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 868GA 49554 DURING A ROUTINE SERVICE CHECK INSPECTION BY ALLEGIANT AIR MAINTENANCE DEPARTMENT PERSONNEL DAMAGE TO THE RIGHT WING NR 4 SLAT WAS DISCOVERED CAUSED BY A BIRD STRIKE. THE NR 4 SLAT WAS REMOVED AND THE AIRCRAFT FERRIED FROM BELLINGHAM, WA T O LAS VEGAS, NV. A NEW SLAT WAS INSTALLED IAW AMM 27-80-01 AND ALL ALLEGIANT AIR GMM PROCEDURES. OPERATIONAL CHECK OF THE FLAP/SLAT SYSTEM WAS ACCOMPLISHED AND THE CHECK WAS NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 AALA200800962 1 20080414 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 795AN 30257 DFW - EMERGENCY LIGHT AT SEAT 20C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 WP 2008 5 19 AALA200800934 1 20080412 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7531A 49923 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 13 TO 16 INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHE AD SEAT ROWS 13 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080519 NM 2008 5 19 AALA200800936 1 20080412 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 623AA 24581 MIA - EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 20080519 NM 2008 5 19 AALA200800973 1 20080415 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 622AA 24580 DFW - EMERGENCY LIGHT AT SEAT ROW 18DEF INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 18DEF BULLNOSE. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080519 EA 2008 5 19 MALA080090 1 20080501 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 8944B 7944 ANGLE CRACKED AT FS 484, LBL 27, JUST BELOW FLOORBOARD. REMOVED AND REPLACED CRACKED ANGLE AT FS 484, LBL 27 AND REPLAC ED WITH NEW SERVICEABLE ANGLE IAW BOMBARDIER REO NR 601R-53-41-059, STEPS 5-14 STANDARD REPAIR 601R-53-0030A STEP 1. RE PAIRS COMPLIED WITH IAW MESABA EO C53032. 2 L 7 2 4F RT A21EA 20080519 EA 2008 5 19 MALA080091 1 20080501 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 8944B 7944 ANGLE CRACKED AT FS 484, RBL 27, AT FLOORBOARD SUPPORT. REMOVED CRACKED ANGLE AT FS 484, RBL 27. INSTALLED NEW SERVICE ABLE ANGLE IAW BSC SR 601R-53-0029B AND CRJ 200 SRM 51-42-21. WAITING MESABA EO FOR CLOSEOUT. REPAIRS COMPLIED WITH IA W MESABA EO C53032. 2 L 7 2 4F RT A21EA 20080519 EU 2008 5 19 NWAA082093313 1 20080511 A 2530 4306800001 OVEN AIRBUS 330 A330323 3930335 EU GALLEY SMOKE A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 813NW 6607 891 5047 AFTER TAKEOFF, SMOKE STARTED COMING OUT OF THE OVEN. LANDING WAS UNEVENTFUL AND OVEN WAS REPLACED. 2 L 7 2 4F RT A46NM 20080519 NM 2008 5 19 DLM88080693 1 20080509 A 5712 RIB DOUG MD88 MD88 3023688 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 960DL 49979 CRACK ON LT WING LEADING EDGE RIB AT STA XRS=289. REPAIRED PER SRM 57-06BD. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 DLM88080698 1 20080509 A 5320 CUSP WEB DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 960DL 49979 CRACK ON RT CUSP WEB STA Y=218-228 AND X=-58 AT PAX CABIN. REPLACED WEB PER DWG 9930538. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 DLM88080699 1 20080505 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 960DL 49979 DUE AT HMV, SRM 53-04 FIG 12B SHT 2, REPAIR T6 DOUBLER/2 FT BELOW FWD AIRSTAIR CONTROL BOX/LT SIDE STA 160. REPAIRED PE R ERA 467994-14 REV ORG ON N/R T0092778 AT HMV-3 IN GDL. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 DLM90080707 1 20080504 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 CABIN SEAT TRACK FS 845-879 LBL 54 OUT OF LIMITS. REPAIRED SEAT TRACK, IAW MD90 SRM 53-40-01, VOL I. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 DLM88080721 1 20080512 A 2120 UNKNOWN DOUG MD88 MD88 3023688 NM CABIN ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 942DL 49815 SMELLED SMOKE IN MID CABIN. NO OTHER INDICATIONS. SMELL WENTAWAY. CABIN LIGHTS WERE OFF. 2 L 7 2 4F RT A6WE 20080519 WP 2008 5 19 IXXA08SMN114S 1 20080327 A 5755 SKIN PANEL DOUG DC8 DC873F 302199F WP NR 4 SPOILER DELAMINATED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 SPOILER PANEL DELAMINATED BETWEEN STATION XRS 247.000 TO XR S 351.000. ADJUSTED LEFT AND RIGHT WING GROUND FLIGHT SPOILER CABLES. PERFORMED OPS CHECK, GOOD TO SPOILER SYSTEM IAW DC8 MM 27-60-0 PAGE 507 ITEMS 15-16 PAGE 509 ITEM 4, AND DC8 MM 27-60-0 PAGE 1. 2 L 7 4 4F RT 4A25 20080519 NM 2008 5 19 AALA200801000 1 20080417 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 796AN 30796 DFW - EMERGENCY LIGHT AT FORWARD GALLEY LEFT NUMBER ONE CLOSET BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT F ORWARD GALLEY LEFT NUMBER ONE CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 WP 2008 5 19 AALA200801003 1 20080418 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 293AA 49305 RDU - EMERGENCY LIGHT LAMP AT SEAT ROW 3AB BROKEN BY PASSENGER. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 3AB. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080519 NM 2008 5 19 AALA200800998 1 20080417 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 796AN 30796 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 12H MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD SEAT 12H. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 NM 2008 5 19 2008UALA02488 1 20080425 A 5210 LEVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 3R FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 3R ARMING LEVER DOES NOT CLICK SECURELY INTO THE ARMED POSITION. ALL OTHER ARMED IND R GOOD. RESTOWED LANYARD AND LUBE D GIRT BAR ASSY, DOOR ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080519 NM 2008 5 19 AALA200800993 1 20080416 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 790AN 30251 DFW - EMERGENCY LIGHT AT RIGHT CORNER OF G1 GALLEY BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RIGHT CORNER OF G1 GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 NM 2008 5 19 AALA200800988 1 20080416 A 3397 WIRE BOEING 777 777223 1385213 NM CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 MIA - MOUNTED EMERGENCY LIGHTS AT FIRST CLASS F5 GALLEY CLOSET INOPERATIVE. FOUND F5 GALLEY MODULE OUTBOARD FRAME EMERG ENCY LIGHT ASSEMBLY WIRES SHORTING. REPLACED LIGHT ASSEMBLY FOR MOUNTED EMERGENCY LIGHTS AT FIRST CLASS F5 GALLEY CLOSE T. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 WP 2008 5 19 AALA200800990 1 20080416 A 3297 CONNECTOR DOUG DC9 DC982 3022082 WP RT MLG LOOSE A AALA O OTHER J WARNING INDICATION DE DESCENT 1 SW 21 460AA 49565 ATL INFLIGHT T1297/16APR - CREW REPORTED UNSAFE GEAR INDICATION ON LEFT NOSE GEAR AND NO LIGHT INDICATION ON RIGHT GEAR. FIRST OFFICER CONFIRMED GEAR EXTENSION THROUGH PERISCOPE. LANDED ATL WITHOUT INCIDENT. FOUND LOOSE CONDUIT AT RIGHT GEAR IN WHEEL WELL. CLEANED AND SECURED CONDUIT CONNECTOR FOR RIGHT GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008051500031 20080515 00031 NM 2008 5 15 F3LA200800231 1 20080501 A 5320 D5347217220500 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED CORROSION ON AND AROUND NUT CLIPS ON FLOORBEAM JUST IN FRONT OF R2 DOOR BETWEEN FR AMES 66 AND 68. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-00 AND SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008051500039 20080515 00039 EU 2008 5 15 08FDEA01721 1 20080501 A 5347 A5378193720100 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 THE SEAT TRACK ADAPTER AT FRAME 29; RBL 40 IS CRACKED. REMOVED SEAT TRACK ADAPTER IAW A300-600 SRM 51-40-21; PARA E-7. RECEIVED NEW SEAT TRACKADAPTER P/N A5378193720100 PO 577701.4. DRILLED HOLES IAW A300-600 SRM 51-40-44. INSTALLED N EW SEAT TRACK ADAPTER IAW A300-600 SRM 51-40-21; PARA E-7. 2 L 7 2 4F RT A35EU 2008051500058 20080515 00058 NM 2008 5 15 DHL2008760519 1 20080407 A 5347 BAC1520841 SEAT TRACK BOEING 727 7272B7 138407L NM BS 760-850 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 REMOVED, FABRICATED, AND REPLACED SEAT TRACK SECTION AT LBL 45, FROM BS 760 TO 850, PER B727 SRM 53-10-2 FIG 7 AND 53-10 -5 FIG 1. 2 L 7 3 4F A3WE 2008051500112 20080515 00112 NM 2008 5 15 2008UALA02466 1 20080426 A 3350 362624 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE ROW 4A INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT ROW 4A AFT INOP. RELAMPED, OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 2008051500134 20080515 00134 NM 2008 5 15 AALA200800979 1 20080415 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 197AN 32391 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 3B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 3B. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008051500152 20080515 00152 NM 2008 5 15 AALA200800961 1 20080414 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT AT SEAT 39C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 39C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008051500158 20080515 00158 NM 2008 5 15 DL764080685 1 20080506 A 2910 261740794 CONTROL UNIT BOEING 767 767432ER 1385134 NM HYD SYSTEM MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 833MH 29706 AFTER RIGHT ENG START RCVD EICAS L HYD SYS PRESS AND RUDDER RATIO MSG. FOUND 31 VAC AT PLUG D480 B PHASE. SWAPPED L EL CU WITH C-2 ELCU, FWD CENTER SYS HYD ELECTRIC PUMP C-2 TO MCO AND PLAC. 2 L 7 2 4F RT A1NM 2008051500171 20080515 00171 NM 2008 5 15 F3LA200800258 1 20080513 A 5322 D53571131258 SHEAR TIE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED FRAME 72 SHEAR TIE BETWEEN STRINGER 27 LEFT AND 28 LEFT REQUIRES REMOVAL AND REPLACEM ENT. MAINTENANCE FABRICATED NEW SHEAR TIE, TREATED, PRIMED AND INSTALLED NEW SHEAR TIE IN ACCORDANCE WITH THE REQUIREME NTS OF AIRBUS DRAWING D53571131258, SRM 53-51-12 FIGURE 2, SRM 51-42-11 AND SRM 51-75-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008051600028 20080516 00028 NM 2008 5 16 SWAA082477 1 20080506 A 3350 8100022701 CONTACT BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT DIRTY A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 419WN 29824 DURING SCHEDULED 6Y CHECK, FOUND EEPLS INOP BETWEEN ROW 6 ABC AND ROW 11 ABC. FOUND LIGHT ASSY CONTACTS DIRTY. CLEANED CONTACTS PER MM. 2 L 7 2 4F RT A16WE 2008051600037 20080516 00037 NE 2008 5 16 SWAA082501 2 20080504 A 7200 CFM567B24G22 ENGINE BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE LEFT FAILED A SWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 29 732SW 27864 876336 DIVERSION, ON CLIMB AT 12000' HEARD A POP/BANG NOISE ACCOMPANIED BY LOUD WHIRRING NOISE. MAXIMUM VIBRATION ON NR 1 ENGI NE. REMOVED AND REPLACED NR 1 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E00055EN 2008051600039 20080516 00039 NM 2008 5 16 SWAA082485 1 20080506 A 5512 182A4002 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 752SW 29804 DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008051600046 20080516 00046 NM 2008 5 16 SWAA082509 1 20080507 A 5330 65C38815 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 430 AND BS 450, STR 28R AND STR 28L. REPAIRED SKIN P ER ER. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082611 1 20080512 A 5714 6946466 STIFFENER BOEING 737 7373H4 1384600 NM CENTER WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND CENTER FUEL TANK VERTICAL STIFFENER CRACKED AT STA 547, RBL 57. REMOVED AND REPLACED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082601 1 20080512 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082600 1 20080512 A 5312 65C28106 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CORRODED AT BS 1016, BL 0. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082572 1 20080509 A 2560 65C16820 HOOK BOEING 737 7375H4 138449D NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER SRM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082627 1 20080513 A 5313 6559964 STRINGER SPLICE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082628 1 20080513 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 22Y CHECK, FOUND STRINGER 25L CORRODED AT BS 988. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 2008UALA02477 1 20080425 A 5315 SUPPORT BRACKET BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NLG TUNNEL CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 RT SIDE NLG TUNNEL AREA BS 246 FLOORBEAM SUPPORT BRACKET CRACKED RBL 26. REMOVED AND REPLACED BRACKET. 2 L 7 2 4F 4 F RT A1NM E24NE 20080516 NM 2008 5 16 2008UALA02481 1 20080428 A 3350 BATTERY PACK BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 216UA 30549 CEILING AND EMERGENCY LIGHTS AT PED NR 1 LT FAILED TIME TEST. REPLACED POWER SUPPLY AT DOOR 1L AND CHARGED BATTERY PACK, OPS CHECK GOOD PER MM 33-51-00 PG 209.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080516 NM 2008 5 16 2008UALA02489 1 20080429 A 2751 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE COCKPIT ACTIVATED A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION AP APPROACH 1 WP 29 665UA 29237 CREW REPORTED A T/E FLAP DISAGREE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080519 NM 2008 5 19 QXEA200800430 1 20080428 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR DIRTY A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 402QX 4032 SEA - LEFT REAR PASSENGER DOOR IS HARD TO OPEN. MAINTENANCE CLEANED AND LUBED DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008041600054 20080416 00054 NM 2008 4 16 UIEA200800087 1 20080316 A 5343 65B1008133 BUSHING BOEING 747 747341 13848AM NM MLG TRUNNION WORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 NOSE LANDING GEAR TRUNNION FITTING RIGHT SIDE BUSHING WORN. REPLACED BUSHING IAW ATLAS EO 4753B122. 2 L 7 4 4F RT A20WE 2008041600055 20080416 00055 NM 2008 4 16 UIEA200800088 1 20080316 A 5343 65B1008133 BUSHING BOEING 747 747341 13848AM NM NLG TRUNNION CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 NOSE LANDING GEAR TRUNNION FITTING LEFT SIDE BUSHING CRACKED. REPLACED BUSHING IAW ATLAS EO 4753B122. 2 L 7 4 4F RT A20WE 2008041600056 20080416 00056 NM 2008 4 16 UIEA200800089 1 20080316 A 5230 BEAM BOEING 747 747341 13848AM NM CARGO DOOR CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 355MC 23395 AFT CARGO DOOR INNER WEB LOWER BEAM FOUND SURFACE LEVEL ONE CORROSION AT RT STATION 1810-1920 STRINGER 40R. LOWER BEAM WEB REMOVED AND REPLACED AS PER SRM 51-30-02 AND BOEING DRAWING 65B04719. 2 L 7 4 4F RT A20WE 2008041600058 20080416 00058 NM 2008 4 16 UIEA200800099 1 20080401 A 7797 8TK34ACB1 LEAD BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE THERMOCOUPLE CHAFED A UIEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 15 505MC 21251 517271 REJECTED TAKEOFF, NR 3 EGT WENT TO OFF SCALE HIGH WITH RED BALL. NR 3 ENGINE EGT SHOWED 1074 DEGREES FOR 1 SEC. FOUND THERMOCOUPLE LEAD WAS DEFECTIVE WHILE PERFORMING FIM PROCEDURE 71-03-00 AS NOTED IN AMM 72-00-00 PAGE 680G. REPLACED LE AD PER AMM 77-21-02 AND THE ENGINE OPS CHECKED OKAY 77-21-00 AND 71-00-00 TEST 4. 2 L 7 4 4F 4 F RT A20WE E23EA 2008041600071 20080416 00071 NM 2008 4 16 UIEA200800116 1 20080409 A 5315 65B38753U2 FLOORBEAM BOEING 747 747243B 1384830 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK STATION 2020 RBL 21 FLOORBEAM SUPPORT FITTING FOUND CRACKED. REPLACED FLOORBEAM SUPPORT FITTING IAW SRM 51-1 0-01. 2 L 7 4 4F RT A20WE 2008041600077 20080416 00077 EA 2008 4 16 A6WA200840198 1 20080305 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 FLOORBEAM CRACKED AT FS 280 LBL 9.0. FLOORBEAM AT FS 280 LBL 9 REPAIRED IAW REO 601R-53-11-171 REV D. (M) 2 L 7 2 4F RT A21EA 20080521 NM 2008 5 21 F3LA200800271 1 20080515 A 5322 D53571554 SHEAR TIE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED FRAME 75 ALL SHEAR TIES FROM STRINGER 22 LEFT TO STRINGER 22 RIGHT NEED GENERAL VISUA L INSPECTION AND HFEC IF NEEDED. MAINTENANCE INSTALLED ALL NEW SHEAR TIES AT FRAME 75 IN ACCORDANCE WITH THE REQUIREMEN TS OF EA A9-53R-30262 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080521 CE 2008 5 21 GUUA05090801 1 20080509 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 47542 24750 UE198 DURING SCHEDULED MAINT, DISCOVERED RT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT OB ELEVATOR HINGE BRACKET. 2 L 7 2 4T 3 T RT A24CE E2NE 20080521 CE 2008 5 21 GUUA04300801 1 20080430 A 5260 MS166241075 RETAINING RING BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA AIRSTAIR DETACHED A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 87550 UE205 DURING PREFLIGHT, PILOT REPORTED AIRSTAIR DOOR HANDLE CAME OFF WHEN OPENING DOOR. REATTACHED RING RETAINER AND SECURED AIRSTAIR DOOR HANDLE. 2 L 7 2 4T 3 T RT A24CE E2NE 20080521 CE 2008 5 21 GLBA20061097 1 20080501 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BS 163 S9R CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 154GL UE154 FUSELAGE FRAME CRACK AT FS 163.97 AT STRINGER 9R CUTOUT. CRACK APPROXIMATELY .5 INCH IN LENGTH. MAINT REPAIRED FUSELAGE FRAME AT FS 163.97 AT STRINGER 9R RELIEF HOLE IAW. SRM 51-70. REPAIR APPROXIMATELY 5.5 INCH BY 2.5 INCH. 2024-T3 .071. RII INSPECTION COMPLIED WITH IAW TASKCARD 8.2.1. 2 L 7 2 4T 3 T RT A24CE E2NE 20080521 NM 2008 5 21 AALA200801062 1 20080423 A 3397 0201720101 WIRE BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 787AL 30010 ORD - EMERGENCY LIGHT AT SEAT 11D WIRING DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 WP 2008 5 21 AALA200801058 1 20080423 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9620D 53591 TUL - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD SEAT ROW 20 FAILED TEST. REPLACED BATTERY PACK AT OVERHEAD SEAT 20 FOR E MERGENCY LIGHTS IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080521 WP 2008 5 21 AALA200801060 1 20080423 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9620D 53591 TUL - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD SEAT ROW 29 FAILED TEST. REPLACED BATTERY PACK AT OVERHEAD SEAT 29 FOR E MERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080521 NM 2008 5 21 KCSA081249 1 20080518 A 5322 SHEAR TIE BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 FUSELAGE FRAME SHEAR TIE CRACKED AT BS 2100 BETWEEN STR-24L AND 25L. 2 L 7 4 4F RT A20WE 20080522 SO 2008 5 22 N93A01052008 1 20080501 A 7714 ACA500 TRANSMITTER GULSTM G1159 GIV 3980115 SO RROYCE TAY TAYMK6108 NE AIRFLOW CONTROL MALFUNCTIONED E N93A O OTHER E VIBRATION/BUFFET DE DESCENT 1 SO 13 495QS 9922 1295 DURING DESCENT, AIRCRAFT EXPERIENCED VIBRATION FROM RT ENGINE THAT LASTED FOR 5 TO 10 SECONDS AND OCCURRED SEVERAL TIME S. TGT ROSE INTO YELLOW BAND. ENGINE WAS PLACED AT IDLE UNTIL LANDING. REPLACED ENGINE AIRFLOW CONTROL RPM SIGNAL TRANS MITTER. 2 L 7 2 4F 4 F RT A12EA E25NE 20080522 CE 2008 5 22 DXTA200803059 1 20080514 A 3260 6839 LAMP CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE MLG INDICATOR INOPERATIVE E DXTA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 07 818QS 5600778 ON ARRIVAL, THE "LT" GEAR DOWN INDICATION LIGHT DID NOT ILLUMINATE. JACKED ACFT, RESET EMERGENCY BLOW-DOWN BOTTLE. REM OVED AIR FROM SYSTEM. FOUND ROTARY KNOB WOULD NOT TEST. REPLACED ALL (4) LAMPS. SWITCH TEST NORMAL. PERFORMED GEAR S WINGS SEVERAL TIMES. ALL INDICATIONS ARE NORMAL. 2 L 7 2 4F 4 F RT A22CE E00053EN 20080522 CE 2008 5 22 DXTA200803060 1 20080514 A 3240 BRAKE SYS RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MLG INTERMITTENT E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 858QS 258691 WHEN APPLYING BRAKES, THEY TAKE A WHILE TO APPLY AND THEN GRAB ALL AT ONCE. DURING ENGINE RUNS APPLIED BRAKES AND NOTI CED SMOOTH INCREASE IN PRESSURE AS SHOWN ON BRAKE PRESSURE GAUGE. DURING TAXI, APPLIED AND RELEASE BRAKES MANY TIMES WIT H NO DEFECTS. 2 L 7 2 4F 4 F RT A3EU E6WE 20080522 CE 2008 5 22 DXTA200803062 1 20080515 A 3230 UPLOCK CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG LACK OF LUBE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 665QS 5605165 GEAR UNLOCKED INDICATION WHEN GEAR RETRACTED. DURING GEAR SWING FOUND LT GEAR UPLOCK STICKING & WOULD NOT LOCK GEAR UP. CLEANED & LUBED ALL THREE GEAR UPLOCKS. RAN GEAR 8 TIMES WITH NO PROBLEMS. GEAR SWING & OPS CK GOOD. RESERVICED N2 & HY D RESEVOIR ALL WORK IAW MM 32-01-00 & 12-13-01 2 L 7 2 4F 4 F RT A22CE E00059EN 20080522 CE 2008 5 22 T6F2008F00000 1 20080429 A 2822 BEARING LEAR 45 45LEAR 5170805 CE PUMP MOTOR WORN E T6FA K NONE O OTHER IN INSP/MAINT 1 GL 09 762EL 2000 107 DRIVE END BEARING FAILED IN PUMP MOTOR. (K) 2 L 7 2 4F RT T00008WI 20080522 NM 2008 5 22 DU4R2008204 1 20080512 A 5315 FLOORBEAM BOEING 737 737 UTILSYS NM CFMINT CFM56 CFM567B27 13046 NE BS 986 CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 321TZ 28249 S/O 245007 OPS NR25007, CORROSION ON UPPER SURFACE OF CABIN STRUCTURE BS 986.5 LBL 32 TO RBL 32 ON UPPER SURFACE OF TEE CAP, NUMEROUS AREAS AROUND FLOORBOARD ATTACH HOLES (AFT MAIN CABIN WET AREA). 2 L 7 2 4F 4 F RT A16WE E00055EN 20080522 SO 2008 5 22 C2XA08RI059 1 20080505 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13979 145181 FLIGHT 2172 -FLIGHT CREW REPORTED ELECTRICAL BURNING SMELL IN AC. MX PERFORMED EXTENSIVE INSPECTION AND ELECTRICAL TEST S, BUT COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080522 SO 2008 5 22 C2XA08CL058 1 20080505 A 3350 66368 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13955 145075 DURING ROUTINE MAINT THE AISLE PATH EMERGENCY LIGHT STRIP NR 6 WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 6 AIS LE PATH LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080522 CE 2008 5 22 DJFA2008045 1 20080516 A 2150 73838433 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL SEIZED E DJFA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 23 701LX 628 7500114 PILOT REPORTED: DURING TAXI THE CABIN FILLED WITH SMOKE; MX INSPECTED ACM'S AND NOTED THE CABIN ACM WAS SEIZED. THE CAB IN ACM WAS REMOVED AND REPLACED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080522 SW 2008 5 22 4756705112008 1 20080511 A 2823 10648BH11 SELECTOR SWITCH BELL 222 222U 1182140 SW LYC LTS101 LTS101* NE NR 2 WORN E QMLA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 NM 03 220LN 47567 PILOT, COMING ONTO SHIFT, REFUELED THE AIRCRAFT, DID HIS PREFLIGHT INSPECTION, AND SAW NOTHING UNUSUAL AT 0900. AT 1017, THE AIRCRAFT WAS LAUNCHED ON A SCENE CALL, CLIMBED TO 4,500 FEET MSL AND LEVELED OFF IN CRUISE FLIGHT WHEN THE AC YAWED AND THE NR2 ENGINE GAGES BEGAN TO SHOW A RAPID DECREASE. THE PILOT LOWERED THE COLLECTIVE AND WENT TO FULL BEEP WHILE M ONITORING ALL ENGINE GAGES. BY THIS TIME, THE NR2 NG AND N2 GAGES INDICATED ZERO. HE ANNOUNCED THAT THERE WAS AN ENGINE FAILURE AND TURNED BACK TOWARD THE BASE. THE PILOT HANDED THE CHECKLIST TO THE FRONT PASSENGER TO READ THOUGH THE LIST. WHEN THEY GOT TO THE FUEL VALVE SWITCH, SAW THAT THE NR2 FUEL VALVE SWITCH WAS ALREADY IN THE OFF POSITION. THE PILOT S 1 G 7 2 3U 3 U H9SW E5NE 20080522 NM 2008 5 22 F3LA200800276 1 20080518 A 2610 COMPUTER AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE ZONE 200 FALSE INDICATION A F3LA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 925FR 50 2103 AFTER TAKEOFF, THE FLIGHT CREW RECEIVED AN ECAM WARNING "LAND ASAP" AND RECALL FUNCTION DISPLAYED AVIONICS SMOKE. IAW TS M 26-15-00-810-803 AND TFU 26.15.15.001 FOUND FAULT WAS LATCHED IN FLIGHT WARNING COMPUTERS. MAINT RESET FLIGHT WARNING COMPUTERS IAW THE REQUIREMENTS TSM 26-15-00-810 OPERATION CHECK NORMAL AND THE AC WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080522 NM 2008 5 22 TAMF20080022O 1 20080501 A 3297 434093003 CIRCUIT CARD BOEING 767 767200 1385120 NM GE CF6 CF680 30025 NE MLG BURNED W TAMF O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 23 767QT 23804 AFTER TAKEOFF WHEN LANDING GEAR LEVER WAS MOVED TO UP A SMOKE FUME APPEARED IN THE COCKPIT (P3-1) WITH NO VISUAL EVIDENC E OF FIRE. AC RETURNED TO DEPARTURE. AFTER MAINT, INSP ON PANEL LIGHT DOOR MODULE KIT (P3-1) 2 DIODES FOUND BURN. NO A DDITIONAL DAMAGES WERE FOUND. (LANDING GEAR DOORS LIGHT INOP) FAULT WAS TRANSFERRED TO MEL 32-61-1. MAINT PROCEDURES WER E ACCOMPLISHED. THE AIRPLANE RETURNED TO OPERATION UNDER NORMAL CONDITIONS. 2 L 7 2 4F 4 F RT A1NM E13NE 20080522 CE 2008 5 22 CIEA200800003 1 20080505 A 3230 66710 CONTROL VALVE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E CIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 566VR 5894 5600480 AIRCRAFT WAS COMPLYING WITH FAA CHECK RIDE, AFTER TAKEOFF, THE LANDING GEAR APPEARED TO ONLY PARTIALLY RETRACT. FLIGHT C REW FOLLOWED APPROPRIATE CHECK LIST AND RETURN TO DEPARTURE AFTER GEAR EXTENDED NORMALLY. EMERGENCY GEAR EXTENSION WAS N OT REQUIRED. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS BROUGHT INTO MAINT AND INSP OF THE LANDING GEAR CONTROL VALV E WAS PERFORMED. PIN A HAD A GOOD GROUND AT 4 OHM RESISTANCE. PIN B REFLECTED 28 VOLTS. VERIFIED RIGGING, AND MINOR ADJU STMENTS OF THE GEAR AUXILIARY/EMERGENCY CONTROL CABLE IAW MM 32-31-08. REMOVED LANDING GEAR CONTROL VALVE PN 66710 SN 90 0 AND INSTALLED AN OVERHAULED LANDING GEAR CONTROL VALVE PN 66710 S/N 232 AND PERFORMED FUNCTIONAL CHECK IAW MM 32-31-02 2 L 7 2 4F 4 F RT A22CE E25EA 20080522 CE 2008 5 22 042908N412CS 1 20080429 A 2611 47359717 DETECTION SYS CESSNA 525 525 2076601 CE WILINT FJ44 FJ44 66000 GL CARGO SMOKE FALSE ACTIVATION E Z5FA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 EA 63 412CS 2132 525B0059 DURING APPROACH, BAGGAGE SMOKE DETECTOR LIGHT ILLUMINATED AND AC DIVERTED AND LANDED WITHOUT INCIDENT. NO SMOKE EVIDENT DURING AFTER LANDING CHECK. BOTH FWD AND AFT BAGGAGE SMOKE DETECTORS WERE REPLACED, OPERATIONALLY CHECKED GOOD AND THE A IRCRAFT RETURNED TO SERVICE. 1 L 7 2 4F 4 F RT A1WI E3GL 20080522 SO 2008 5 22 GLBA20061103 1 20080515 A 3230 12038594001 MODULE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE MLG CONTROL INOPERATIVE A GLBA O OTHER S AFFECT SYSTEMS AP APPROACH 1 NM 03 293UX 120293 FLIGHT NR 5148, ENROUTE, THE PILOTS REPORTED THAT UPON APPROACH TO LANDING, THEY LOWERED THE GEAR AND INITIALLY HAD 6 G REEN LIGHTS, BUT THEN HAD (3) (ALL "A" LIGHTS) GREEN. PILOTS INITIATED GO-AROUND AND GEAR WOULD NOT COME UP. PUT HANDLE DOWN AND LANDED WITH (3) GREEN "A" LIGHTS. MAINT REMOVED AND REPLACED THE LANDING GEAR CONTROL MODULE IAW MM 32-10. OPER ATIONAL CHECK WAS GOOD. P/N OFF 120-38594-001 S/N OFF 120290. 2 L 7 2 4T 4 T RT A31SO E20NE 20080522 NM 2008 5 22 QXEA200800494 1 20080513 A 2910 LINE BOMBDR DHC8 DHC8402 1390042 NM HYD SYSTEM FAILED A QXEA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 416QX 4083 YVR- FLIGHT 2276 (SEA-YVR) AFTER LANDING IN YVR AND EXITING THE RUNWAY HAD A NR 2 HYDRAULIC SYSTEM FAILURE. AIRCRAFT WA S TOWED OFF TAXIWAY. MAINTENANCE REPLACED THE LT MLG DOWNLOCK HYD LINE WITH A FLEX HOSE AND THE AIRCRAFT WAS FERRIED TO PDX. IN PDX, THE HOSE WAS REPLACED ON 5/14. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080519 NM 2008 5 19 AALA200800830 1 20080407 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 386AA 27060 ORD - EMERGENCY LIGHT AT SEAT 4B HIT BY PASSENGER BAG AND SEPARATED FROM SEAT. RESECURED LIGHT ASSEMBLY FOR EMERGENCY L IGHT AT SEAT 4B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080519 NM 2008 5 19 AALA200800832 1 20080407 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 DFW - EMERGENCY LIGHT AT SEAT 25G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 NM 2008 5 19 F3LA200800244 1 20080425 A 5322 D53570712212 SHEAR TIE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED FRAME 72 SHEAR WEBS DAMAGED IN THE AREA OF STRINGER 32 LEFT. MAINTENANCE REMOVED DAM AGED SHEAR TIES FROM STRINGER 32 LEFT TO 31 LEFT. REMOVED FRAME 72 FROM STRINGER 24 RIGHT TO 28 LEFT. FABRICATED NEW A NGLES IN ACCORDANCE WITH THE REQUIRMENTS OF EA A9-53R-30262, SRM 51-42-11 FIGURE 8 AND SRM 53-51-12. INSTALLATION WAS A CCOMPLISHED ON NR C043414. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080519 NM 2008 5 19 F3LA200800245 1 20080503 A 5311 D53570712212 COUPLING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED HOLES OUT OF ROUND AND SHOW CRACK INDICATIONS IN CIRCLED HOLES ON FRAME COUPLING FOR FRAME 72 STRINGER 27 LEFT TO 28 LEFT. MAINTENANCE INSTALLED NEW FRAME COUPLING ON FRAME 72 AT STRINGER 27 LEFT AND 28 L EFT IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30262. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND AC CEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080519 NM 2008 5 19 AALA200800956 1 20080414 A 3397 CONNECTOR BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 MIA - EMERGENCY LIGHT AT SEAT 26H INOPERATIVE. RECONNECTED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 26H. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080519 NM 2008 5 19 DLM88080692 1 20080505 A 5311 FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 960DL 49979 CRACK ON FRAME STA. Y=1451 LONG 1. REPAIRED PER DRAWING 9911860 AND SRM 51-10-3D ON N/R T0093001 AT HMV-3 IN GDL. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 2008UALA02539 1 20080430 A 2121 FILTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COOLING FAN DIRTY A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 598UA 28751 INTERMITTENT EQUIPMENT OVERHEAT LIGHT. FOUND EQUIPMENT FAN SYSTEM FILTER DIRTY. REPLACED EQUIPMENT COOLING FAN FILTER, OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080519 NE 2008 5 19 DL75A080723 2 20080512 A 7200 PW2037RTC ENGINE BOEING 757 757212 1384951 NM PWA 2037 PW2037 NE NR 1 MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 752AT 41192 23128 727150 UPON LEFT ENG START, NO THROTTLE RESPONSE AFTER BLEED VALVE RESET, OPS NORMAL. NO MSGS, RESTARTED LEFT ENG, ALL PARAMET ERS WERE NORMAL. ON THE GROUND,THE ENG IS RESPONSIVE IMMEDIATELY, ALL CHKS SUCCESSFULLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080519 NM 2008 5 19 AALA200800992 1 20080416 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 790AN 30251 DFW - EMERGENCY LIGHT AT LEFT CORNER OF G1 GALLEY BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LEFT CORNER OF G1 GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 EA 2008 5 19 MASA200800361 1 20080502 A 2910 M259881226 O-RING CNDAIR CL600 CL6002D24 1390016 EA HYDRAULIC SYS WORN A MASA O OTHER K FLUID LOSS CR CRUISE 1 SW 07 923FJ 15023 ASH 2622 CLT-JFK - NR 2 HYD SYSTEM WENT TO ZERO IN FLIGHT, DECLARED EMERGENCY. REMOVED AND REPLACED LINE AND O-RINGS, L EAK CHECK GOOD. 2 L 7 2 4F RT A21EA 20080519 NM 2008 5 19 KCSA081234 1 20080506 A 5210 DOOR FRAME BOEING 747 747212B 1384886 NM R5 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 R5 MAIN ENTRY DOOR FWD LOWER CORNER VERTICAL FRAME CRACKED IN RADIUS, BS 2241, WL-207. 2 L 7 4 4F RT A20WE 20080519 EU 2008 5 19 UPS08152171 1 20080506 A 2780 JACKSCREW AIRBUS A300 A300F4622R 3930360 EU L/E SLAT OVERTORQUED A IPXA O OTHER F FLT CONT AFFECTED LD LANDING 1 SO 01 160UP 0005 SLATS WOULD NOT DEPLOY FOR LANDING. CHECKLIST PROCEDURES DID NOT RESOLVE THE PROBLEM. CAPTAIN DECLARED AN EMERGENCY AN D LANDED WITHOUT FURTHER INCIDENT. FOUND RT INBOARD SLAT SCREWJACK OVERTORQUED. REMOVED AND REPLACED INBOARD SLAT SCRE WJACK IAW MM 27-84-22-04. L/E AND T/E FLAPS SYSTEMS CHECKS GOOD, REF MM 27-54-00-5 AND 27-51-00-5. 2 L 7 2 4F RT A35EU 20080519 2008 5 19 UPS08852167 4 20080502 A 2565 SLIDE DOUG DC8 DC873F 302199F WP ENTRY DOOR INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 WITH MAIN DOOR SHUT AND SLIDE ARMED, DOOR WAS OPENED AND SAFETY WIRE REMOVED FROM SLIDE HOUSING. REMOVED AND REINSTALLE D MAIN CABIN DOOR ESCAPE SLIDE IAW AMM 25-60-01-2. INSTALLATION CHECK WAS GOOD. 2 L 7 4 4F RT 4A25 20080519 WP 2008 5 19 UPS08852177 1 20080506 A 3350 6012235 BATTERY DOUG DC8 DC873F 302199F WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801UP 46101 EMERGENCY EXIT LIGHTS DO NOT TEST. EMERGENCY EXIT LIGHTING BATTERY AND RELAY UNIT REPLACED AND TESTED SERVICEABLE IAW D C8 33-50-01-2-4. 2 L 7 4 4F RT 4A25 20080519 NM 2008 5 19 UPS08M52174 1 20080407 A 5313 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C CENTER CARGO COMPT/BILGE AREA BETWEEN STA 5-113 AND STA 1541, RT LONGERON 47 FOUND SUSPECTED CRACK WIT H STICKER NR 5187 AND 5189. HFEC INSP C/O AND FOUND CRACK APPROX 4 INCHES. CRACKED LONG SPLICE BETWEEN STA 5- 113 AND 1541 REMOVED PER SRM 51-33-01VIIR35. HOLES PICKED UP ON NEW SPLICE AND PROTECTED. NEW LONG SPLICE INSTALLED PER SRM 51 -33-01VIIR35. 2 L 7 3 4F RT A22WE 20080519 EA 2008 5 19 MASA200800377 1 20080507 A 2560 P2070011100 FLASHLIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN DEFECTIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 935LR 15035 ASH FLT 2608 CLT-SDF - FORWARD F/A FLASHLIGHT WILL NOT CHARGE. REMOVED AND REPLACED FLASHLIGHT, OP CHECK GOOD. 2 L 7 2 4F RT A21EA 20080519 EA 2008 5 19 MASA200800381 1 20080506 A 5210 WEB CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 942LR 15042 REPAIRED PAX DOOR FWD AND AFT WEB CRACKS. 2 L 7 2 4F RT A21EA 20080519 NM 2008 5 19 KCSA081235 1 20080508 A 5330 SKIN BOEING 747 747123 1384873 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 SMALL AREA OF DAMAGE ON FUSELAGE BELLY SKIN AT BS 792, BL-0. 2 L 7 4 4F RT A20WE 20080519 EA 2008 5 19 MASA200800388 1 20080510 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 509MJ 10094 ASH FLT 7078 ATL-ORD - CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20080519 EA 2008 5 19 MASA200800390 1 20080510 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002D24 1390016 EA OVERWING DOOR OUT OF ADJUST A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 920FJ 15020 ASH FLT 2619 ATL-CLT - LEFT FORWARD OVERWING DOOR CAUTION. ADJUSTED PROX SENSOR. 2 L 7 2 4F RT A21EA 20080520 WP 2008 5 20 ABXA080148 1 20080424 A 5320 991555047 INTERCOSTAL DOUG DC9 DC941 302207N WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 INTERCOSTAL FS 1060, LONGERON 27 LEFT WAS CORRODED. REMOVED AND REPLACED INTERCOSTAL AT FS 1060, LONGERON 27 LEFT IAW D C9 SRM. 2 L 7 2 4F A6WE 20080520 WP 2008 5 20 ABXR080143 1 20080411 A 5220 99577351 STOP FITTING DOUG DC9 DC931 3022065 WP OVERWING EXIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 231US 48114 RIGHT AFT OVERWING EXIT DOOR HAD CRACK AT UPPER STOP. REPAIRED RIGHT AFT OVERWING EXIT DOOR AT UPPER STOP IAW DC9 SRM 5 2-05. 2 L 7 2 4F A6WE 20080520 NM 2008 5 20 UPS08M52175 1 20080407 A 5313 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C CENTER CARGO COMPT/BILGE AREA BETWEEN STA 5-113 AND STA 1541 RT LONGERON 45 FOUND SUSPECTED CRACK WITH STICKER NR 5125 AND 5786. HFEC INSP C/O AND FOUND CRACK APPROX 3 INCHES. CRACKED LONGERON SPLICE BETWEEN STA 5-113 AN D 1541, L-45R REMOVED PER SRM 51-33-01VIIR35. HOLES PICKED UP ON NEW SPLICE AND SPLICE PROTECTED. NEW SPLICE INSTALLED PER SRM 51-33-01 VIIR35. 2 L 7 3 4F RT A22WE 20080520 NM 2008 5 20 UPS08M52176 1 20080407 A 5313 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C CTR CARGO COMPT/BILGE AREA BETWEEN STA 5-113 AND STA 1541, RT LONGERON 44 FOUND SUSPECTED CRACK WITH S TICKER NR 5185 AND 5126. HFEC INSP C/O AND FOUND CRACK APPROX 1 INCH CRACKED LONGERON SPLICE BETWEEN STA 5-113 AND 154 1, L-44R REMOVED. HOLES PICKED UP ON NEW SPLICE AND SPLICE PROTECTED. NEW LONGERON SPLICE INSTALLED PER SRM 51-33-01VI IR35. 2 L 7 3 4F RT A22WE 20080520 NM 2008 5 20 UPS08552206 1 20080508 A 2450 CIRCUIT BREAKER BOEING 757 75724APF 1384969 NM COCKPIT POPPED A IPXA K NONE J WARNING INDICATION CL CLIMB 1 SO 01 419UP 23906 ATB - PASSING 17000 FT, LOST THE LT AC BUS WITH NUMEROUS ASSOCIATED INDICATIONS, ITEMS LOST IN FLIGHT ARE EUIP OHT, LAFT FUEL BOOST PUMP, RT FWD BOOST PUMP, PROB HEAT, CAPTS PITOT, L AUX PITOT, L AOA AND SYM GEN FOR BOTH CAPT/FO AIR ABORT. TROUBLESHOT PER WD 24-51-13 SH 1. RESET POPPED C/B ON P6-3 PANEL, BUS L SEC 3, 35 AMP. ALL CHECKS OK. 2 L 7 2 4F RT A2NM 20080520 NM 2008 5 20 UPS08652188 1 20080429 A 5320 140T0130U38 ANGLE BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 329UP 27755 INSPECTION TYPE:C AFT CARGO COMPT STA 1085 RBL 26" BELOW FLOOR VERTICAL WEB ATT ANGLE CRACK, CRACK LENGTH 3/4 INCH. AFT CARGO COMPT STA 1085 RBL 26 IINCHES VERTICAL WEB ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20080520 NM 2008 5 20 UPS08652190 1 20080430 A 5320 141T514616 STIFFENER BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 329UP 27755 INSPECTION TYPE:C CARGO MEC STA 246 LBL 50 INCH STIFFENER CRACK, CRACK LENGTH 3/8 INCH. MEC STA 246 LBL 50 INCH STIFFEN ER REPLACED AND INSTALLED AS PER SRM 51-40-02 AND 51-10-02. 2 L 7 2 4F RT A1NM 20080520 WP 2008 5 20 08FDEA01783 1 20080507 A 7603 2606270001 THROTTLE CABLE DOUG MD10 MD1010F 3022112 WP ZONE 400 STUCK A FDEA E ENGINE SHUTDOWN S J AFFECT SYSTEMS WARNING INDICATION CR CRUISE 1 SO 25 568FE 47827 DURING CRUISE ENG NR 2 THROTTLE WOULD NOT MOVE, STUCK IN HIGH THRUST SETTING.DURING DESCENT SHUTDOWN ENGINE. R&R NR 2 E NG THROTTLE PUSH PULL CABLE IAW AMM 76-11-01-2. INSPECTED AREA PRIOR TO CLOSE UP. CLOSED FAN COWL IAW AMM 71-00-00-2. E NG RUN-UP REQUIRED. TAXIED A/C OUT TO RWY AND PERFORMED MAX POWER ASSURANCE PER JRH. NR 2 ENGINE CHECKS NORMAL, OK FO R SERVICE. 2 L 7 3 4F RT A22WE 20080520 EA 2008 5 20 MASA200800397 1 20080513 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 510MJ 10101 ASH FLT 7221 IAD-ATL - PROX SYSTEM FAULT 2 STATUS MESSAGE. CYCLED DOOR OPEN/CLOSED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080520 EU 2008 5 20 08FDEA01733 1 20080502 A 5340 11A92420400202 ATTACH FITTING AIRBUS 310 A310324 3930206 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 815FD 638 RADAR MOUNT ATTACH FITTING ON THE FWD FACE OF THE FRONT PRESSURE BULKHEAD STRUCTURE IS CORRODED. REMOVED THE ANGLE IN RE F TO SRM 51-40-21; PARA 7. FABBED A NEW ANGLE IN REF TO DWG 11A92420400 & INSTALLED NEW ANGLE IN REF TO SRM 51-40-21 PARA 7. 2 L 7 2 4F RT A35EU 20080520 WP 2008 5 20 08FDEA01730 1 20080502 A 5410 AVB702433 SEAL DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 2 ENGINE CORE COWL FWD UPPER SPRING SEAL HAS HOLES WORN THROUGH THE SEALS. REMOVED & REPLACED THE UPPER SPRING SEAL I AW DC/MD-10 SRM 51-35-01; VOL II. 2 L 7 3 4F RT A22WE 20080520 WP 2008 5 20 08FDEA01728 1 20080502 A 5410 AUB710813 ACCESS PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 3 PYLON ACCESS PANEL NR 487 HR HAS FASTENERS ON A PREVIOUS REPAIR THAT ARE CHAFED IN HALF WITH ELONGATED HOLES AND NO ED AND BARE METAL. FABRICATED NEW PANEL IAW DWG AUB 7108 REV AN. ALODINED & PRIMED PANEL IAW SRM 51-21-01; VOL II. PART MARKED PANEL ASSY IAW GMM 07-0-1000. 2 L 7 3 4F RT A22WE 20080522 NM 2008 5 22 QXEA200800495 1 20080515 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM UNDERTORQUED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 400QX 4030 SEA - REAR PASSENGER DOOR IS HARD TO OPEN. MAINTENANCE LUBRICATED THE DOOR. OPERATIONAL CHECKS GOOD. NO PARTS REPLACE D. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080522 EU 2008 5 22 MALA080100 1 20080516 A 5751 SKIN SAAB SF340 340B 7860101 EU AILERON DELAMINATED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 452XJ 340B452 RT WING, RIGHT AILERON P/N 7294576-618 S/N 0266 INBOARD LEADING EDGE DELAMINATED. REPAIRED IAW EO NR S51031. COLD BOND (WET LAYUP) REPAIR IN ACCORDANCE WITH SAAB SRM 51-70-50. 2 L 7 2 4T RT A52EU 20080522 NM 2008 5 22 QXEA200800453 1 20080505 A 6123 30005000056 CONTROL UNIT DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS MALFUNCTIONED A QXEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 09 345PH 194 476 SEA - ON TAKEOFF, ABORTED AT 70 KNOTS, DUE TO AUTOFEATHER FAILED TO ARM. RETURNED TO THE GATE. MAINTENANCE REPLACED TH E TSCU AND THE AUTOFEATHER SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080522 NM 2008 5 22 QXEA200800456 1 20080508 A 5230 502213 SEAL BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 423QX 4153 SEA - FLIGHT 2232 (PDX-YVR) - LOSS OF PRESSURE AND CABIN PRESSURE WARNING AT 17,000 FEET. COMPLIED WITH A QUICK DESCENT AND LANDING AT SEA. FOUND A 2 INCH AREA OF SEAL MISSING FROM THE AFT CARGO DOOR. REPLACED SEAL. OPERATIONAL CHECKS G OOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080522 NM 2008 5 22 QXEA200800458 1 20080509 A 2997 CONNECTOR DHAV DHC8 DHC8202 2809007 NM HYD SYSTEM CORRODED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 348PH 484 PDX- FLIGHT 2187 (PDX-RDM) RETURNED TO THE FIELD FOR A HYDRAULIC PRESSURE FLUCTUATION AFTER TAKEOFF AND GEAR RETRACTION. LANDING UNEVENTFUL. MAINTENANCE WAS ABLE TO DUPLICATE AND FOUND CORROSION ON THE PINS FOR THE CONNECTOR FOR THE NR 2 TRANSDUCER. CLEANED UP PINS AND CONNECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080523 NM 2008 5 23 USAA920081032 1 20080508 A 5320 CHANNEL BOEING 757 7572B7 1384964 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 930UW 27145 CLT - MAJOR REPAIR - DROP IN - CRACKED CHANNEL, BS 845, RBL 2.90. REPAIRED CHANNEL, BS 845, RBL 2.90 IAW USAIRWAYS EA 1 00458. 2 L 7 2 4F RT A2NM 20080523 SO 2008 5 23 FDKA200805192 1 20080506 A 5320 14521721009 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 837MJ 145367 THE DIGITAL PLATE AT Y=0 IS CORRODED FROM FRAME 15 TO FRAME 19. THE CORRODED PART HAS BEEN REPAIRED BY REPLACING THE CO RRODED SECTIONS. 2 L 7 2 4T RT T00011AT 20080523 EU 2008 5 23 USAA920081048 1 20080503 A 5320 D53471124201 SHEAR WEB AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650AW 856 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON RIGHT SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, -Y1732. REPLACED R IGHT SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, -Y1732 IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 20080523 2008 5 23 USAA920081030 4 20080508 A 2565 D30664105 SLIDE AIRBUS 320 A320214 3930316 EU R1 DOOR FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 105UW 868 PIT - EES - C11 CHECK, R1 DOOR SLIDE FAILED OPERATIONAL CHECK. TIME REQUIRED TO FULLY INFLATE WAS 22 SECONDS AND THE LI GHTS DID NOT ILLUMINATE . REPLACED SLIDE. 2 L 7 2 4F RT A28NM 20080523 WP 2008 5 23 UPS08852197 1 20080424 A 5720 5769857304 INTERCOSTAL DOUG DC8 DC873F 302199F WP RWS 434 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 RIGHT WING CENTER L/E INTERCOSTAL CRACKED AT OUTBOARD PERI-SEAL STAND-OFF BRACKET AT XFS 434. FABRIC ATED AND REPLACED RIGHT WING CENTER L/E INTERCOSTAL AT XFS 434 IAW DWG 5769857 AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 20080523 WP 2008 5 23 UPS08852198 1 20080421 A 5720 5769857613 ANGLE DOUG DC8 DC873F 302199F WP LT WING GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LEFT WING CENTER L/E OUTBOARD UPPER Z-ANGLE GOUGED AND HAS 2 EA OVERSIZED HOLES. REPAIRED LEFT WING CENTER L/E OUTBOARD Z-ANGLE IAW DWG 5769857, SRM 57-02-00-0 FIG 2A AND SRM 57-02-00 FIG 007. 2 L 7 4 4F RT 4A25 20080523 EU 2008 5 23 USAA920081051 1 20080506 A 5320 D53472284008 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650AW 856 SAL - MAJOR REPAIR - C4 CHECK - CORROSION ON CABIN BEAM, BS 3101 / FR 65, -Y460. REPLACED CABIN BEAM, BS 3043 / FR 64 - BS 3207 / FR 67, -Y460 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20080523 EU 2008 5 23 USAA920081052 1 20080506 A 5320 D53472190205 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650AW 856 SAL - MAJOR REPAIR - C4 CHECK - CORROSION ON CABIN BEAM, BS 3043 / FR 64 - BS 3158 / FR 66, -Y1292. REPLACED CABIN BEAM , BS 3043 / FR 64 - BS 3158 / FR 66, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20080523 WP 2008 5 23 UPS08852199 1 20080411 A 5340 ATTACH FITTING DOUG DC8 DC873F 302199F WP BS 742 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 MDCC LEFT STA 742, CUSP AREA FRAME ATTACH FITTING GOUGED. REMOVED FITTING, FABBED AND INSTALLED FITT ING IAW SRM 51-1-8, 51-3-0, 51-1-20D, 51-1-15. 2 L 7 4 4F RT 4A25 20080523 SO 2008 5 23 FDKA200805200 1 20080512 A 3350 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 FDM 6106 CVG-CMH. OVERHEAD CEILING EMERGENCY EXIT SIGN INOP. FLIGHT CREW CYCLED POWER TO SYSTEM. NO FURTHER DEFECTS N OTED. 2 L 7 2 4T RT T00011AT 20080523 EA 2008 5 23 MASA200800405 1 20080516 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA MAIN PAX STIFF A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 509MJ 10094 ASH 7076 IAD - PAX DOOR HARD TO OPEN. MX INSPECTED DOOR. NO DEFECTS NOTED. DOOR ASSY OPS GOOD. 2 L 7 2 4F RT A21EA 20080523 WP 2008 5 23 UPS08852179 1 20080413 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1120 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 C-PIT RIGHT STA 1120, FLOORBEAM JUST I/B OF CUSP IS BLOWN OUT AT FASTENER HOLE WITH CORROSION. REMOV ED CORROSION, FABBED AND INSTALLED REPAIR ANGLE IAW SRM 51-1-8, 51-3-0, 53-2-0 FIG 1F, 51-1-20D. 2 L 7 4 4F RT 4A25 20080523 WP 2008 5 23 UPS08852202 1 20080421 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LEFT WING CENTER L/E REPAIR DOUBLER HAS OVERSIZED SCREW HOLES AT OUTBOARD END OF SLOT VANE. FABRICAT ED AND REPLACED FILLER AND DOUBLER AT LEFT WING CENTER L/E AT OUTBOARD END OF SLOT VANE IAW EO DC8-5720-7767-A. 2 L 7 4 4F RT 4A25 20080523 NM 2008 5 23 UPS08M52192 1 20080326 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1841 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C AFT CABIN - CORROSION IN SEAT TRACK CHANNEL AT STA 1841 X=107. CORROSION AT AFFECTED AREA REMOVED MAT L THK:0.100" (CHANNEL) MATL REMOVED:0.05 0" (STA1841-1853), MATL REMN:0.050". FOUND OUT OF LIMIT. DISCREPANT SEA TRACK AT STA1831 X=107, TRIM OUT. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. 01EA SPLICE HAT SECT & 01EA SPLICE PLATE FAB. NEW SEAT TRACK FROM STA 1831-2007 X=107 & REPAIR PARTS INSTALLED SRM 53-70-00 FIG 1 VI R35. 2 L 7 3 4F RT A22WE 20080523 WP 2008 5 23 UPS08852181 1 20080411 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 MDCC STA 100, LEFT BELOW FLOOR LEVEL, LAMINATED SHIM IS DELAMINATED. REMOVED FLOORBOARD, FABBED AND INSTALLED BROKEN FITTING, CLOSED FLOORBOARD IAW SRM 53-21-1, 51-1-21, 51-3-0, 51-1-8. 2 L 7 4 4F RT 4A25 20080523 WP 2008 5 23 UPS08852182 1 20080423 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 FLOOR PANEL F81/F81A HAS 3 EA. DAMAGED SCREW HOLES AS MARKED. REPAIRED FLOOR PANEL F81/F81A IAW SRM 53-02-03-0 FIG 010 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 20080523 WP 2008 5 23 UPS08852213 1 20080422 A 5347 DC853B007004 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 400-408 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 RIGHT SEAT TRACK DAMAGED RBL 46 FROM STA 400 TO 408. REPLACED SEAT TRACK CHANNEL AND PLUG AT RBL 46 AND STA 400 TO 408 IAW SRM 51-03-00, SRM 53-02-03 FIG 6D, SRM 51-9-00 FIG 065. 2 L 7 4 4F RT 4A25 20080527 NM 2008 5 27 SWAA082646 1 20080514 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 706 S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080527 NE 2008 5 27 ASAA0852936 2 20080510 A 7310 3400128020 LINE BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE NR 2 ENGINE FUEL LEAKING A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 587AS 35684 895978 NR 2 ENGINE FUEL FEED HOSE CHAFED AND LEAKING. REMOVED AND INSTALLED NR 2 ENGINE FUEL SUPPLY LINE. WILL REQUIRE TORQUE . TORQUED NR 2 ENG FUEL SUPPLY LINE REF MM 73 11 10 43570. INSP NR 10 HOSE ASSY VERFIED. RAN NR 2 ENG FUEL SUPPLY LIN E, LEAK CHECK GOOD. NO LEAKS AT THIS TIME. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080527 NE 2008 5 27 ASAA0852934 2 20080510 A 7320 5065691 ALTERNATOR BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE NR 2 ENGINE EEC BURNED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 587AS 2137 35684 895978 NR 2 ENG EEC ALTERNATOR HAS BURN MARK WITH MISSING MATERIAL. REF LG PG 6415951 FOR BREAKERS PULLED AND MIG 51A'S INSTALL ED. ROTABLE PART HAS BEEN VERIFIED. REMOVED ENG NR 2 EEC ALTERNATOR AND INSTALLED NEW SERVICEABLE EEC ALTERNATOR. TES T 3A LEAK CK AND TEST 13 EEC BITE CK. NO LEAKS OR RECENT FAULTS NOTED. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080527 WP 2008 5 27 UPS08852222 1 20080421 A 5720 WEB DOUG DC8 DC873F 302199F WP STUB WING GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 SEVERAL DEEP GOUGES IN INBOARD WEB AT NR 1 STUB WING. REPAIRED NR 1 STUB WING INBOARD WEB IAW SRM SR M 57-02-00, DWG 9753297, SRM 51-01-08 AND SRM 51-01-21. 2 L 7 4 4F RT 4A25 20080527 WP 2008 5 27 UPS08852223 1 20080421 A 5730 57699335 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LEFT WING CENTER L/E 4 EA SCREWS PULLING AND HAVE CORROSION ON SKIN INBOARD LOWER CORNER OF SLOT VANE . REPAIRED LEFT WING CENTER L/E INBOARD LOWER CORNER OF SLOT VANE IAW EO DC8- 5720-7767-A. 2 L 7 4 4F RT 4A25 20080521 2008 5 21 2008UALA02526 4 20080429 A 2350 SWITCH AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 848UA 1647 FIRST OFFICER O2 MASK MIC INOP. REPAIRED SWITCH IN STOWAGE BOX, MIC OPS PROPERLY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080521 NM 2008 5 21 AALA200801090 1 20080426 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 962AN 30858 DFW - EMERGENCY LIGHT AT SEAT ROW 16DEF MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT ROW 16DEF. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 WP 2008 5 21 AALA200801070 1 20080424 A 2612 FIRE DETECTOR DOUG DC9 DC983 3022083 WP CARGO BAY FAULTY A AALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 SW 21 9622A 53593 ABQ INFLIGHT T1178/24APR SFO TO DFW - CREW REPORTED B SYSTEM CARGO FIRE WARNING. CAPTAIN DECLARED EMERGENCY AND LANDED ABQ WITHOUT INCIDENT. NO INDICATION OF FIRE FOUND. REPLACED NUMBER ONE AND TWO FIRE EXTINGUISHER BOTTLES AND AFT FILT ER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080521 NM 2008 5 21 AALA200801037 1 20080421 A 3397 WIRE BOEING 777 777223 1385213 NM CABIN EXPOSED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 788AN 30011 DFW - EMERGENCY LIGHT AT MAIN DECK CREW REST FORWARD CLOSET HAS WIRES EXPOSED. SECURED EMERGENCY LIGHT WIRING IN WIRE C HANNEL DOWN WALL IN MAIN DECK CREW REST FORWARD CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801068 1 20080424 A 3350 HOUSING BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 396AN 29603 MIA - EMERGENCY FLOOD LIGHT AT RIGHT FIRST CLASS GALLEY HAS BROKEN HOUSING ASSEMBLY. REPLACED HOUSING ASSEMBLY FOR EME RGENCY FLOOD LIGHT AT RIGHT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080522 EA 2008 5 22 N6WA0080402 1 20080430 A 5270 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* 30015 NE EMERGENCY EXIT FALSE ACTIVATION A N6WA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 151GJ 10216 5285-IAD-RT EMERGENCY EXIT CAUTION MESSAGE AFTER LANDING. REMOVED AND CHECKED OPERATION IAW AMM 52-21-00. 2 L 7 2 4F 4 F RT A21EA 20080522 CE 2008 5 22 GUUA05110801 1 20080511 A 2697 CONNECTOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA ANNUNCIATOR DIRTY A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 69547 UE189 DURING FLIGHT AMBER DISCHARGE, ANNUNCIATOR ILLUMINATED. CLEANED CONNECTORS AT RT FIRE BOTTLE. 2 L 7 2 4T 3 T RT A24CE E2NE 20080522 EA 2008 5 22 2008F00015 1 20080428 A 3246 C3UT1449 SKI DHAV DHC3 DHC3 2800202 EA GARRTT TPE331 TPE33110 01514 WP MLG DAMAGED E D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 AL 03 565TA 46 UPON ROLL OUT AFTER LANDING IN DEEP SNOW PILOT WAS EXECUTING LT TURN. NOSE OF THE TAIL SKI DUG INTO THE EDGE OF THE TRAC KS MADE BY THE MAIN SKIS AT AN ANGLE. THE SUDDEN SIDE LOAD ON THE SKI CAUSED IT TO TWIST AND JAM INTO THE EMPENNAGE SKIN . DAMAGING FUSELAGE BULKHEAD AT STATION 444.38 ALONG WITH SEVERAL STRINGERS AND FUSELAGE SKIN BETWEEN FUSELAGE STATION'S 413 TO 467.5. 1 H 7 1 3R 4 T A815 E4WE 20080522 EA 2008 5 22 ACE0519080 2 20080519 A 7261 MS245884 NIPPLE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA ENGINE OIL CRACKED E YADA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AL 03 111AX UC81 32601 PILOT REPORTED LOSS OF OIL PRESSURE, NR1 ENGINE. ENGINE SECURED IN FLIGHT AND AC RETURNED TO DEPARTURE AIRPORT AND MADE AN UNEVENTFUL LANDING. MAINT REPLACED THE NR1 ENGINE TORQUE PRESSURE LINE DUE CRACKED NIPPLE IN HOSE END. INSPECTION OF CRACKED HOSE NIPPLE DID NOT INDICATE CAUSE OF FAILURE. DESTRUCTIVE TESTING (INTENSE OVER TORQUE) OF OTHER END OF SAM E HOSE DID NOT RESULT IN SIMILAR CRACKING FAILURE. DESTRUCTIVE TESTING OF SECOND SAMPLE OF SAME PN. NIPPLE DID NOT RES ULT IN SIMILAR CRACKING FAILURE. SUSPECT DEFECTIVE MATERIAL / PROCESSING OF HOSE NIPPLE AT MFG OR ORIGINAL ASSY. HOSE ASSY DATE A1Q08 AND 3Q07 ON WO NR 108987. 2 L 7 2 4T 4 T RT A24CE E4EA 20080522 CE 2008 5 22 051508N568CS 1 20080515 A 2910 AE6209H0300130 LINE CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE HYDRAULIC SYS BURST E Z5FA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 63 568CS 1786 5605637 LOST ALL HYDRAULIC FLUID ON TAKEOFF. DECLARED AND EMERGENCY AND LANDED WITHOUT INCIDENT. MAINT PERSONNEL FOUND SPLIT I N LT HYDRAULIC PUMP PRESSURE LINE AND REPLACED IT WITH A NEW LINE. ALSO, BOTH LT AND RT ENGINE HYD PUMPS AND FILTERS WE RE REPLACED AS PRECAUTION. THIS IS THE 3RD OCCURRENCE OF THIS PART FAILURE. PREVIOUS 2 EVENTS, REFERENCE SDR 120707N549 CS1 AND 021708N554CS1 2 L 7 2 4F 4 F RT A22CE E00059EN 20080522 CE 2008 5 22 DXTA200803058 1 20080513 A 2720 41044420208 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C 03047 GL RUDDER CONTROL INOPERATIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 933QS 2721 7500133 DURING CLIMB AND CRUISE, RUDDER OSCILLATES INTERMITTENTLY WITH UPPER RUDDER (A) SELECTED. REMOVED UPPER RUDDER ACTUATOR - INSTALLED A REPAIRED ACTUATOR. PERFORMED OPERATIONAL AND LEAK CHECK WITH SATISFACTORY RESULT. TRAVEL CHECKS NORMAL, MA INTENANCE PERFORMED IAW MM 27-74-01. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080522 NM 2008 5 22 DU4R2008205 1 20080512 A 5315 FLOORBEAM BOEING 737 737 UTILSYS NM CFMINT CFM56 CFM567B27 13046 NE BS 328 CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 321TZ 28249 S/O 245007 OPS NR 25025 - CORROSION BS 328 BL 10R FLOOR SUPPORT BEAM. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080522 WP 2008 5 22 ABXA080151 1 20080501 A 5340 591214159 ATTACH ANGLE DOUG DC9 DC932F 3022067 WP VERTICAL STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 LEFT VERTICAL STAB ATTACH ANGLE CRACKED, LOCATED AT BASE OF RUDDER. REPAIRED LEFT VERTICAL STAB ATTACH ANGLE IAW DC9 SR M 53-05. 2 L 7 2 4F A6WE 20080523 WP 2008 5 23 UPS08852196 1 20080418 A 5347 3657504501 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 COCKPIT OBSERVER SEAT AFT SEAT TRACK HAS ELONGATED HOLE. REMOVED AND REPLACED 2ND OBSERVERS AFT SEAT TRACK IAW SRM 51-03-00 AND SRM 51-01-24. 2 L 7 4 4F RT 4A25 20080523 NM 2008 5 23 USAA920081043 1 20080510 A 5330 D53571128204 SKIN AIRBUS A319 A319132 3930340 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 835AW 2458 SAL - MAJOR REPAIR - BC2 CHECK - CRACKED FUSELAGE SKIN, BS 3117 / FR 73, S22L - S23L. REPAIRED FUSELAGE SKIN, BS 3117 / FR 73, S22L - S23L IAW EA 120733. 2 L 7 2 4F RT A28NM 20080523 EU 2008 5 23 USAA920081040 1 20080510 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 661AW 1284 FLT 83 PHX-BWI - EMERG EQUIP - FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20080523 2008 5 23 USAA920081041 4 20080510 A 2565 62293106 SLIDE AIRBUS A321 A321211 3930370 EU R3 DOOR FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 172US 24568 1956 1472 FLT 1165 PHL-CLT - EES - R3 DOOR SLIDE INTERNAL LIGHTING FAILED. EMERGENCY LIGHT EPSU EXTERNAL LOAD FAULT (EXIT R). MA INTENANCE REMOVED AND REPLACED THE R3 DOOR SLIDE ASSEMBLY. ALSO REFERENCE LOG PAGE 4388428 FOR EMERGENCY LIGHTS FAILED CIDS TEST - MSGS (1) EPSU INT LOAD MID L, (2) EPSU INT LOAD MID R, (3) EPSU EXT LOAD EXIT R. RELAMPED VARIOUS EMERGENCY EXIT SIGNS AND LIGHTS AND REPLACED R3 DOOR SLIDE (AS INDICATED ABOVE). 2 L 7 2 4F RT A28NM 20080523 SO 2008 5 23 FDKA200805195 1 20080507 A 3397 JUMPER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 840MJ 145429 FDM 6101 JFK-RDU. EMERGENCY FLOOR PROXIMITY LIGHTS OUT BETWEEN ROW 3-7. MX RESECURED FLOOR LIGHT JUMPER, OPS GOOD. 2 L 7 2 4T RT T00011AT 20080523 WP 2008 5 23 UPS08852183 1 20080423 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP CABIN TORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 FLOOR PANEL F81B HAS 1EA SCREW HOLE TORN THROUGH EDGE. REPAIRED FLOOR PANEL F81B IAW SRM 53-02-03-0 FIG 010 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 20080527 NM 2008 5 27 UPS08552209 1 20080509 A 2497 BUSS BOEING 757 75724APF 1384969 NM LT INOPERATIVE A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 419UP 23906 AFTER TAKEOFF CREW LOST EFIS SYMBOLOGY. LEFT A/C BUS C/B POPPED. T/S FOUND C/B BUSS L-SEC3, 35 AMP POPPED. T/S PER WD 24-51-11. ACCOMP AMP LOAD TEST OF ALL C/B`S ON P6-3 PANEL. FOUND ALL LOADS NORMAL. CHECKED ALL WIRING FOR SHORTS/BUR NS AND LOOSE CONNECTIONS, ALL CHECKED OK. REPLACED C/B C310 BUSL SEL, SEC 3, 35 AMP. REPLACED LT GEN C/B C901 IN P31 P ANEL. APPLIED POWER TO A/C. ALL CHECKS OK. 2 L 7 2 4F RT A2NM 20080520 EU 2008 5 20 08FDEA01845 1 20080514 A 5720 A57111092203 FITTING AIRBUS 300 A300B4622R 3930312 EU CENTER WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND ON SEVERAL HOLES IN CENTER WING BOX LOWER JUNCTION VERTICAL FLANGE C 47 WITH DAMAGE AND CRACKS (HOLE H, I, W, N) . REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL DAMAGE REMOVAL AND INSTALLING FASTENER NSA5351 AND EN6115, APPROVED BY RAS/70503969/045/2008 ISS A AND EA 6-5710-117142. 2 L 7 2 4F RT A35EU 20080520 WP 2008 5 20 08FDEA01723 1 20080501 A 3620 350085 CONTROLLER DOUG MD10 MD1010F 3022112 WP CABIN AIR FAILED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 568FE 47827 FL 370 LEVEL 1 AIR SYS 2 FAIL. AIR SYS AUTO CONTROLLER SHUTDOWN NR 2 AIR SYSTEM 2 MINUTES LATER. LEVEL 3 AIR SYS FAIL FOLLOWED QRH. LAND AT NEAREST SUITABLE EVENTUALLY 10 MINUTES LATER APPROX AIR SYS 2 INDICATED NORMAL. SYSTEM DECAY CHE CK PER AMM 36-00-01-5 AND ALL PARAMETERS WERE WITHIN LIMITS. CHECKED NR 2 PACK BAY, FWD, CTR AND CAC COMPTS FOR LEAKS AND NONE FOUND. R & R MANIFOLD FAILURE DETECTION CONTROLLER AS PERCAUTIONARY PER AMM 36-23-01-4 AND SYSTEM CHECKS GOOD. RAN NR 2 ENG AT IDLE AND OP`S CHECK THE NO.2 PNUEMATIC SYSTEM AND NO DEFECTS NOTED PER FDX JRH. OK TO CONTINUE. 2 L 7 3 4F RT A22WE 20080520 NM 2008 5 20 QXEA200800457 1 20080512 A 3260 JAM-NUT BOMBDR DHC8 DHC8402 1390042 NM NLG LOOSE A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 414QX 4061 SEA - LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. RAN THE CHECKLIST BUT NO CHANGE. RETURNED TO THE FIELD AND ACCOMPLISH ED A UNEVENTFUL LANDING. FERRIED THE AIRCRAFT TO PDX FOR REPAIRS. IN PDX, FOUND LOOSE JAM NUTS AND MISSING SAFETY WIRE AT THE NOSE WHEEL CENTER PROX SENSOR. REPAIRED AND RIGGED SENSOR IAW 32-61-06-830-801. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080520 NM 2008 5 20 KCSA081242 1 20080515 A 5411 SPAR BOEING 747 7472B4B 138481B NM NR 3 PYLON GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NR 3 PYLON MID SPAR WEB IS GOUGED AT NAC STA 202. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 KCSA081244 1 20080515 A 3350 LIGHT BOEING 747 7472B4B 138481B NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 713CK 21099 EMERGENCY LIGHT IN CENTER OF DOME WILL NOT LIGHT. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800169 1 20080505 A 5230 MS20470B524 SHEAR PIN BOEING 747 7472D7B 1384803 NM CARGO DOOR BROKEN A UIEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 15 528MC 22472 AIR TURN BACK, SIDE CARGO DOOR LIGHT ILLUMINATED DURING TAKEOFF ROLL. RETURNED TO BLOCKS PER FHB. FOUND OUTSIDE MASTER LATCH LOCK HANDLE SHEAR PIN BROKEN. REMOVED AND REPLACED SHEAR PIN PER AMM 52-32-06. OPS CHECKED OKAY. 2 L 7 4 4F RT A20WE 20080516 NM 2008 5 16 SWAA082520 1 20080506 A 3350 33500006 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 419WN 29824 DURING SCHEDULED 6Y CHECK, FOUND EEPLS COVER MISSING AT ROW 6 ABC. INSTALLED COVER PER BAC DRAWING. 2 L 7 2 4F RT A16WE 20080516 2008 5 16 08FDEA01799 4 20080508 A 3442 6225132120 TRANSCEIVER BOEING 727 727225 1384077 NM WX RADAR SYSTEM FAILED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 462FE 22550 (AIR-TURN-BACK), WX RADAR PAINTS INTERMITTENT FALSE RETURNS ONE SIDE THEN THE OTHER, STABILIZED OR UNSTABILIZED. WHEN U NSTABILIZED, RADAR PAINTS A SINGLE SPOKE AT THE 11 -12 O'CLOCK POSITION. GOING BACK TO STABILIZED, IT PAINTS A DOUBLE S POKE. VERIFIED OLD RADAR RT PAINTING FALSE IMAGES EVEN ON GND. REMOVED AND REPLACED RADAR RT AND ALL FUNCTIONAL CHECKS GOOD PER M/M 34-41-000-5 PARA 1A-5J. A/C OK FOR SERVICE. 2 L 7 3 4F A3WE 20080516 NM 2008 5 16 2008UALA02639 1 20080505 A 5210 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 R2 DOOR UPPER HINGE ARM CUT-OUT HAS DAMAGE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED: RMV'D DAMAGE. FABRICATED & INSTALLED A REPAIR ANGLE & TAPERED FILLERS. 2 L 7 2 4F 4 F RT A2NM E17NE 20080516 NM 2008 5 16 SWAA082555 1 20080511 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 EEPLS END CAP MISSING AT ROW 1 ABC. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082599 1 20080512 A 5311 6546538 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080516 EA 2008 5 16 MASA200800389 1 20080510 A 5270 PROXIMITY SWITCH CNDAIR CL600 CL6002D24 1390016 EA OVERWING DOOOR DIRTY A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 931LR 15031 ASH FLT 2916 PHX-COS. CA GOT A LEFT FORWARD OVERWING DOOR CAUTION AT PUSHBACK. PILOT VERIFIED DOOR WAS SHUT, LATCHED A ND LOCKED AND THAT THE OUTER PLATE WAS FLUSH. CLEANED PROX SWITCH. 2 L 7 2 4F RT A21EA 20080516 NM 2008 5 16 SWAA082619 1 20080513 A 2560 65C1612113 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082618 1 20080513 A 2560 65C1612113 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082620 1 20080513 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 407WN 29817 EEPLS LENS MISSING AT ROW 5 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080516 NM 2008 5 16 SWAA082621 1 20080513 A 5312 6546568 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 ASAA0852937 1 20080507 A 2160 412A160041 FILTER BOEING 737 737890 1384527 NM A/CON SYS DIRTY A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 584AS 2895 35682 CONT CABIN ZONE TEMP ILLUM ON RECALL BITE CHECK BOTH TEMP CONTROLLERS RT CONTROLLER SHOWED FLT DECK TRIM VALVE FAULT WHI CH CLEARED. DUE PREVIOUS HISTORY 15 APR CONTINUED MEL 21 21C. INSTALLED PLAC VERIFIED FAULT REF MM 21 60 00, FOUND AIR FILTER OBSTRUCTED & SENSOR ELEMENT COVERED WITH CONTAMINANTS. CLEAN FILTER & SENSOR. OPERATED PACK & CONFIRMED GOOD T EMP RESPONSE SYS OPS NML. CLEARED MEL 21 21C CN 6424720 P C REM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 USAA920081058 1 20080430 A 5340 66235743 STRINGER CLIP BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED STRINGER TIE CLIP, BS 706, S11L. REPLACED STRINGER TIE CLIP, BS 706, S11L IAW B 737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 USAA920081060 1 20080508 A 5320 69374024 ANGLE BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - CRACKED STUB FRAME SUPPORT ANGLE, BS 294.5, RBL 55. REPLACED STUB FRAME SUPPORT ANGLE, BS 294.5, RBL 55 IAW B737 SRM 51-70-11. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 USAA920081061 1 20080509 A 5753 6546435366 SKIN BOEING 737 7373S3 1384711 NM RT WING TE FLAP WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - RIGHT WING OUTBOARD FORE FLAP HAS MANY RIVETS WORKING THRU THE SKIN. REMOVED AND REPLA CED THE RIGHT WING OUTBOARD FORE FLAP IAW USAIRWAYS TASK CARD C3R27002. 2 L 7 2 4F RT A16WE 20080527 EU 2008 5 27 USAA920081066 1 20080510 A 5347 D5311278220200 SEAT TRACK AIRBUS A319 A319112 3930323 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 715UW 1051 PIT - MAJOR REPAIR - C9 CHECK - CORROSION ON CABIN SEAT TRACK, BS 808 / FR 20, -Y765. REPAIRED CABIN SEAT TRACK, BS 605 / FR 12 - BS 1003 / FR 25, -Y765 IAW A319 SRM 53-00-45. 2 L 7 2 4F RT A28NM 20080527 NM 2008 5 27 USAA920081067 1 20080512 A 5230 SKIN BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 PHX - MAJOR REPAIR - B3 CHECK - AFT CARGO DOOR SKIN CRACKED, BS 827, S22R AT HANDLE HINGE FLAP AREA. REPAIRED AFT CARGO DOOR SKIN, BS 827, S22R AT HANDLE HINGE FLAP AREA IAW B737 SRM 52-00-01-2R-3. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082650 1 20080514 A 5330 65516242 SKIN BOEING 737 7373H4 1384600 NM BS 987 S23R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 987, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 UPS08M52211 1 20080331 A 5311 AEA7127502 FRAME DOUG MD11 MD11F 3023600 NM BS 1258 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:4C CRACK AT FRAME TO FLOOR BRACKET AT FS 1258 RBL 106. REMOVED, FABRICATED, AND INSTALLED FRAME PER EO MD11-5310-29275-A DAC DWG AEA7605, MD-11 SRM 53-33-01, AND SAA EA 011-5310-01-A1340. 2 L 7 3 4F RT A22WE 20080527 EA 2008 5 27 VNAA0805005 1 20080505 A 2751 DETECTION SYS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS MALFUNCTIONED A VNAA B EMER. DESCENT N FALSE WARNING AP APPROACH 1 GL 05 259PS 7945 CREW REPORTED ON APPROACH A FLAPS FAIL AT ZERO INDICATION. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAI NTENANCE RESET THE SKEW DETECTION UNIT AND CYCLED THE FLAP CIRCUIT BREAKER IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE M ANUAL. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080527 NM 2008 5 27 SWAA082634 1 20080514 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 804 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 804, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 ASAA0842938 1 20080511 A 5755 SKIN BOEING 737 7374Q8 138447Q NM NR 4 SPOILER DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 NR 4 SPOILER HAS BUMPS FROM SEAL SCREWS. REPAIRED SKIN DAMAGE ON OUTBOARD END OD NR 4 SPOILER IAW B737 400 SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 ASAA0842940 1 20080511 A 5753 FAIRING BOEING 737 7374Q8 138447Q NM RT WING TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 RIGHT OUTBOARD MID FLAP IS CHAFED AT NR 7 AFT FLAP TRACK FAIRING LWR SURFACE. REPAIRED MID FLAP TRACK FAIRING PANEL IAW B737 400 SRM 51 70 10 PGS 201 257. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082660 1 20080515 A 3350 417N5212 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 EEPLS END CAP LOOSE AT ROW 1 ABC. SECURED END CAP PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082670 1 20080515 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED 10Y CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082641 1 20080514 A 5312 6545819 PRESSURE PANEL BOEING 737 7375H4 138449D NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED 16Y CHECK, FOUND NLG W/W CEILING PANEL CUTOUT WEB CRACKED AT LBL 7.5. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082665 1 20080515 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM BS 370 S26L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, STR 26L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082666 1 20080515 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM BS 400 S26L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 26L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082667 1 20080515 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM BS 500A S26L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 26L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 ASAA0842947 1 20080429 A 5753 FLAP TRACK BOEING 737 7374Q8 138447Q NM TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 LEFT O/B MID FLAP CHAFED I/B OF NR 2 FLAP TRACK. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBL ER IAW B737 400 SRM 51 70 10 REPAIR GENERAL. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 ASAA0842950 1 20080511 A 5755 SKIN BOEING 737 7374Q8 138447Q NM NR 2 SPOILER DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 NR 2 SPOILER HAS BUMPS FROM SEAL SCREWS. PREPPED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 1 0 REPAIR 2. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 ASAA0842954 1 20080501 A 5755 SKIN BOEING 737 7374Q8 138447Q NM NR 8 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 NR 8 SPOILER UPPER SURFACE HAS PROTRUDING DENTS. PREPPED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B 737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082647 1 20080514 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 707 S6R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 707, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082633 1 20080514 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 804 S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 804, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082699 1 20080518 A 3350 6556633 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED SPV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082681 1 20080518 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 400 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082706 1 20080515 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM BS 360 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082707 1 20080518 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500A S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082671 1 20080515 A 3350 767 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 904WN 36616 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082708 1 20080518 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500A S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082692 1 20080516 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 520 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 9R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082711 1 20080515 A 2121 215201 FAN BOEING 737 7373H4 1384600 NM E&E BAY FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 380SW 26587 CREW REPORTED STRONG ELECTRICAL SMELL IN MID CABIN. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082675 1 20080518 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM BS 500 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082694 1 20080518 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 EEPLS LENS MISSING AROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082684 1 20080518 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 747 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 18L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080528 SO 2008 5 28 C2XA08RI067 1 20080511 A 2611 47359713 SMOKE DETECTOR EMB 135 EMB135ER 3260203 SO CARGO BAY FALSE ACTIVATION A C2XA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SW 27 16502 9143 3436 145166 FLIGHT 3096 - EWR - FLIGHT CREW REPORTED BAGGAGE EXTINGUISH WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. ALSO, I NTERMITTENT BAGGAGE SMOKE WARNING ON EICAS, BUT DISAPPEARED AFTER 1 SECOND. CREW PROCEEDED WITH EMERGENCY DESCENT AND L ANDED AIRCRAFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED BOTH CARGO SMOKE DETECTOR IAW EMB 135 AMM 26-15-01 AND PERFORM ED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. FWD SMOKE DETECTOR: P/N 473597-13 S/N 2907, TOTAL TIME= 9143, TOTAL CYCLES=6652, TIME SINCE INSPECTION=3436 AFT SMOKE DETECTOR: P/N 473597-13 S/N 1054, TOTAL TIME= 16222, TOTAL CYCLES=16372, TIME SINCE INSPECTION=16222 2 L 7 2 4F RT T00011AT 20080528 NM 2008 5 28 SWAA082741 1 20080520 A 3350 65C27063 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 293WN 36612 R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082742 1 20080520 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 947 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082754 1 20080520 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 616 S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082744 1 20080520 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 907 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082749 1 20080520 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 467WN 33830 EEPLS LENS LOOSE AT ROW 5 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080528 SO 2008 5 28 RAIA00805008 1 20080505 A 3260 852701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO MLG MALFUNCTIONED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 814HK 145046 FLT 5535 - STL - LANDING GEAR AIR/GROUND FAILURE MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE LT MLG FWD PROXIMITY SWITCH. SYSTEM CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080528 2008 5 28 SWAA082773 4 20080522 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 234WN 32502 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080528 2008 5 28 SWAA082778 4 20080522 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM R2 DOOR SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED EVAC SLIDE CABLE PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082779 1 20080522 A 3350 1619 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082712 1 20080518 A 3350 1619 LAMP BOEING 737 7375H4 138449D NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED C3 CHECK, FOUND LT FWD FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PE R MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082786 1 20080522 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 772SW 27880 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 120. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080528 2008 5 28 SWAA082787 4 20080522 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 776WN 30591 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080528 SO 2008 5 28 C2XA08IA125 1 20080513 A 2910 SYLC518361 ACTUATOR EMB 145 EMB145XR 3260214 SO RAT DOOR INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 11121 15396 15396 145683 IAH - FLIGHT 2172, DURING CLIMB THE CREW REPORTED A RAM AIR VALVE FAILURE MESSAGE WITH THE INABILITY TO HOLD CABIN ALTIT UDE BELOW 10K' ABOVE 21K' AIRCRAFT ALTITUDE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANC E INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE RIGHT HAND RAM AIR DOOR LINEAR ACTUATOR, OPERATIONALLY CHECKED WIT H NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20080516 EU 2008 5 16 2008UALA02490 1 20080428 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 448UA 842 CORROSION ON R2 DOOR FWD OF FRAME 66. REPLACED SILL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080516 NM 2008 5 16 2008UALA02499 1 20080429 A 3397 7945243 PIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 122UA 29168 EEL CABLE PIN BROKEN AT SEAT 46ABC. REPLACED CABLE ASSY. OP CHK GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20080516 NM 2008 5 16 2008UALA02502 1 20080429 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 122UA 29168 SEAT 58C EEL LIGHT BROKEN. REPLACED EEL LIGHT. OP CHK GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20080516 WP 2008 5 16 UPS08852130 1 20080413 A 5320 STIFFENER DOUG DC8 DC873F 302199F WP FUSELAGE BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 RT NOSE TUNNEL CEILING STIFFENER IS BULGED AND HAS POPPED RIVETS STA - 32 RBL 40. REMOVED DAMAGED, F ABBED AND INSTALLED REPAIR DOUBLER AND FILLER IAW, SRM 51-1-8, 51-1-21. 2 L 7 4 4F RT 4A25 20080516 WP 2008 5 16 UPS08852131 1 20080401 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 COMPLY WITH MPI P 19473 REGARDING NON CONFORMING REPAIR AT L28R IAW WA N 1322729, MPI SUMMARY REPORT, AND EO DC8-5330-20248-E APPX E. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-8, 51-1-26, 51-3-1, EO DC8-5 330-20248 APPEX E. 2 L 7 4 4F RT 4A25 20080519 NM 2008 5 19 UPS08M52136 1 20080211 A 5311 FRAME DOUG MD11 MD11 3023602 NM FUSELAGE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C RT RAM AIR EXHAUST CUTOUT FRAME STRUCTURE I/B FWD LOCATION FOUND DEEP CHAF CAUSED BY RAM AIR ACTUATOR LINKAGE. CHAFING MARK SMOOTHENED AND PROTECTED PER SRM 57-21-01V.2R.40. ORIG THK:0. 093 INCH, MATL REM:0.041" FOUND OU T OF LIMIT PER SRM 53-00-01V.1R.40. HFEC C/OUT IAW DACNDTSPM R.13 PART06-10-01.001 ON REWORKED AREA FOUND NO CRACK EVID ENT. FAB REPAIR STRIP 7075T6X0.100 INCH THK MATL PER EN1079-08. REPAIR STRIP PROTECTED AND FR PRIMED PER SRM 51-21-01V .2R.40. INSTALL REPAIR. 2 L 7 3 4F RT A22WE 20080519 NM 2008 5 19 DHL2008760510 1 20080402 A 5730 SKIN BOEING 727 7272B7 138407L NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 FABRICATED AND INSTALLED REPAIR DOUBLER AT R/WING NR 6 L/E SLAT O/B HOOK SEAL CUT-OUT, BETWEEN RWS 519 TO 546, PER B727 SRM 57-30-4 FIG 9. 2 L 7 3 4F A3WE 20080519 WP 2008 5 19 DHL2008807500 1 20080417 A 7110 SKIN DOUG DC8 DC873F 302199F WP COWLING WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 NR 1 ENG NACELLE INLET COWL UPPER SKIN WORN STA YN 147.534 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8-70 SRM 71-5-2 FIG 2 (SHEET 1-2). REMOVED FASTENERS IAW SRM 51-1-21A. CUT OUT DAMAGED SECTION AND FABRICATED SKIN (AL2024T3 0.080") AN D SPLICE (SHEET CRES 0.050 TYPE 17-7 PH) IAW DC8-70 SRM 71-5-2 FIG. 2 SHEET 1-2. HEAT TREATED SPLICE FROM CRES 17-7 PH TO CRES 17-7PH (H1050) IAW SRM 51-1-6. CLEANED, TREATED AND PRIMED AREA AND SKIN INNER FACE IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 71-5-2 FIG 2 SHEET 1-2, SRM 51-1-11, SRM 51-1-21A. 2 L 7 4 4F RT 4A25 20080519 NM 2008 5 19 AALA200800835 1 20080407 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 786AN 30250 DFW - EMERGENCY LIGHT AT SEAT 39G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 39G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 EU 2008 5 19 CPCP20080023 1 20080404 A 5752 HINGE FITTING AEROSP ATR72 ATR72212 8680945 EU AILERON TAB CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 348AE 349 HINGE FITTINGS OF RT AILERON TRIM TAB ARE CORRODED. RT AILERON TRIM TAB HINGE FITTINGS NR 1-3-4 REPLACED IAW SRM 51-25- 03. 2 H 7 2 4T RT A53EU 20080519 SO 2008 5 19 SIMA200812901 1 20080506 A 3320 BR90022 BALLAST EMB 135 EMB135LR 3260305 SO CABIN MALFUNCTIONED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 721HS 145283 ON FLIGHT 4742, CREW REPORTED ELECTRICAL SMELL IN GALLEY AREA DURING BOARDING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH BALLASTS ON GALLEY LIGHT IAW EMB-135 AMM 33-21-05. OPERATIONAL CHECK OK AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20080519 EU 2008 5 19 MALA080080 1 20080427 A 5320 STRUCTURE SAAB SF340 340B 7860101 EU LAVATORY CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425XJ 340B425 LAVATORY SERVICE SHELL (TRAY) HEAVILY CORRODED ON LOWER FORWARD EDGE; APPROX STA 225. REMOVED DAMAGED TRAY AND INSTALLE D NEW TRAY P/N: 7253680-117 IAW SAAB 340 SRM CHS 51-20 AND 51-40. 2 L 7 2 4T RT A52EU 20080519 EA 2008 5 19 SWIA200819605 1 20080215 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 971SW 7947 LBL9 AND RBL9 AT FS 280 UPPER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CR200 REO 601R-53- 11-136 DATED 02/13/99. 2 L 7 2 4F RT A21EA 20080519 NM 2008 5 19 AALA200800915 1 20080410 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 756AM 30264 DFW - SEAT MOUNTED EMERGENCY LIGHTS AT RIGHT BUSINESS CLASS INOPERATIVE. REPLACED BATTERY PACK M33099 FOR SEAT MOUNTED EMERGENCY LIGHTS AT RIGHT BUSINESS CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 NM 2008 5 19 DHLA200800045 1 20080513 A 3310 1315 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 749DH 22013 FLT NR 197 - CABIN EMERGENCY EXIT LIGHT HAS ONE BULB INOPERATIVE. RELAMP CABIN EMERGENCY EXIT LIGHT PER M/M 33-10-00 P/ N 1315. AIRCRAFT WAS GROUNDED. 2 L 7 3 4F A3WE 20080519 NM 2008 5 19 DHL200874301 1 20080506 A 5230 MOUNT BRACKET BOEING 727 727225 1384077 NM CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 743DH 22438 MAIN CARGO DOOR AT FORWARD HOOK ACTUATOR UPPER MOUNT BRACKET HAS CRACK AT AFT INBOARD CORNER RADIUS TO BOLT HOLE. NEW P ART FABRICATED USING DRAWING 52-523 FOR ONE TIME USE. MATERIAL USED 2024-T3 .090" PO NR 6193. INSTALLED NEW FABRICATE D IAW BOEING SRM 51-30-2 AND PEMCO M/M 52-32-01. ALL INFO ON NR 68262. 2 L 7 3 4F A3WE 20080519 NM 2008 5 19 08FDEA01807 1 20080510 A 5730 ARB74023 SKIN DOUG MD11 MD11F 3023600 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 631FE 48454 15 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LHW LOWER SKIN ACCESS DOOR CUTOUT BETWEEN X ORS = 690 AND STA XORS = 700. REPAIR CARRIED AS PER EA 1-5710-122444 REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-1 00 2 L 7 3 4F RT A22WE 20080519 NM 2008 5 19 08FDEA01809 1 20080510 A 5347 ADA7321519 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 631FE 48454 MAIN DECK CARGO COMPT, SEAT TRACK AT STA 879 X= 8.5 FOUND CORRODED. MAIN DECK CARGO COMPT: SEAT TRACK AT STA 879 X= 8.5 REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 3 VOL.I.REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080519 NM 2008 5 19 NWAA082105645 1 20080513 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 545US 26492 DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY LIGHTS AT ROWS THREE, FOUR AND THE EXIT SIGN AT DOOR ONE RIGHT INOPERATIV E. MAINTENANCE REPLACED BATTERY PACK NUMBER M730, ALL OPERATIONS CHECKED NORMAL. 2 L 7 2 4F RT A2NM 20080519 NM 2008 5 19 KCSA081232 1 20080506 A 5210 DOOR FRAME BOEING 747 747212B 1384886 NM L5 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 L5 MAIN ENTRY DOOR FWD LOWER CORNER VERTICAL FRAME CRACKED IN RADIUS ADJACENT TO DOOR STOP, BS 2241, WL-207. 2 L 7 4 4F RT A20WE 20080519 EU 2008 5 19 UPS08152169 1 20080506 A 5347 LOCK AIRBUS A300 A300F4622R 3930360 EU CARGO BAY BROKEN A IPXA O OTHER O OTHER CR CRUISE 1 SO 01 150UP 0833 AT LEVEL OFF, CREW HEARD A MUFFLED BOOM AND SLIGHT SHAKE OF THE A/C. UPON DESCENT, CREW REPORTED A LOAD SHIFT. MX INSP ECTED LOCKS AND SEAT TRACK. ONE BROKEN LOCK WAS DEFERRED. NO SEAT TRACK DAMAGE. CREW DECLARED AN EMERGENCY. UPON ENT ERING CARGO AREA NOTED CONTAINER FOR 5L HAD MOVED TO 4L. FOUND LEFT O/B LOCK BETWEEN POSITION 3L AND 4L BROKEN. VISUAL LY INSPECTED REMAINING LOCKS AND SEAT TRACKS BETWEEN 3L AND 4L WITH BRIGHT LIGHT AND MAGNIFYING GLASS. NO DEFECTS. REM OVED AND REPLACED BROKEN LOCK. 2 L 7 2 4F RT A35EU 20080519 EA 2008 5 19 MASA200800368 1 20080505 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR OUT OF ADJUST A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 503MJ 10058 ASH FLT 7281 IAD-AUS - SERVICE DOOR CAUTION MESSAGE IN FLIGHT. ADJUSTED PX38 PROX SENSOR, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080520 NM 2008 5 20 UPS08452200 1 20080508 A 5710 WING BOEING 747 747212B 1384886 NM LEFT DAMAGED A IPXA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 520UP 21943 LT WING DAMAGE ON CONTACT WITH POLE ON TAXI IN. 2 L 7 4 4F RT A20WE 20080520 WP 2008 5 20 08FDEA01725 1 20080502 A 7110 NSL6051517 NOSE COWL DOUG MD10 MD1010F 3022112 WP ZONE 400 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 567FE 46994 NR 1 ENGINE NOSE COWL L/E HAS A DENT AT THE 6-7 O'CLOCK POSITION. NR 1 ENGINE NOSE COWL DENTS FOUND TO BE OUT OF LIMITS DUE TO DREASE IAW SRM 54-11-00; VOL I. REMOVAL AND REPLACEMENT ACCOMPLISHED ON N/R N00284. 2 L 7 3 4F RT A22WE 20080520 NM 2008 5 20 UIEA200800180 1 20080509 A 5730 SKIN PANEL BOEING 747 747228F 1384895 NM RT WING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 RT WING UPPER FIXED L/E PANEL DELAMINATED, 6.0 FEET OUTBOARD OF NR 3 ENGINE, 12 INCHES FROM AFT EDGE OF PANEL AT ILES ST A 772.5. AREA OF DELAMINATION IS 14.0 INCH LONG BY 3.0 INCH WIDE. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51 -40-09, FIG 18, SHEETS 3 AND 5 PREPREG 250 DEGREES CURE PER SRM 51-40-12. REF: ATLAS AIR EO NR 4757A439. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800181 1 20080509 A 5730 SKIN PANEL BOEING 747 747228F 1384895 NM RT WING DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 RT WING UPPER FIXED T/E PANEL HAS LOOSE AND WORKING FASTENERS, PANEL IS DELAMINATED. PANEL LOCATED INBOARD OF INBOARD A ILERON, AT WBL STA 445.0, DELAMINATION AFT EDGE OF PANEL. AREA OF DELAMINATION IS 9.0 INCH LONG BY 1.5 INCH WIDE. PERM ANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 2, SHEET 1, 2 AND 5 PREPREG 250 DEGREES CURE PER SRM 51-40-1 2. REF: ATLAS AIR EO NR 4757A440. 2 L 7 4 4F RT A20WE 20080520 EU 2008 5 20 USAA920080996 1 20080502 A 5320 F5347823420100 FLOOR SUPPORT AIRBUS 330 A330323 3930335 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 272AY 333 BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON FLOOR SUPPORT, BS 5759/FR 75, -Y350 TO -Y450. REPAIRED FLOOR SUPPORT, BS 5759/FR 75, -Y350 TO -Y450 IAW USAIRWAYS EA 134009. 2 L 7 2 4F RT A46NM 20080520 NM 2008 5 20 USAA920080999 1 20080420 A 5320 146N54126 ANGLE BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - CORROSION ON INTERCOSTAL ANGLE, BE 1360 - BS 1380, RBL 24.5, WL 208. REPLACED INTERCOS TAL ANGLE, BE 1360 - BS 1380, RBL 24.5, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 20080520 NM 2008 5 20 USAA920081001 1 20080503 A 5311 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - CRACKED FRAME, BS 807, S8L - S9L. REPAIRED FRAME, BS 807, S8L - S9L IAW USAIRWAYS EA 100441. 2 L 7 2 4F RT A16WE 20080520 NM 2008 5 20 USAA920081006 1 20080503 A 5311 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - CRACKED FRAME, BS 827, S8R - S9R. REPAIRED FRAME, BS 827, S8R - S9R IAW USAIRWAYS EA 100441. 2 L 7 2 4F RT A16WE 20080520 NM 2008 5 20 USAA920081019 1 20080508 A 2560 P4010021 BATTERY BOEING 737 7373B7 1384580 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 332AW 23384 SEA - EMERGENCY EQUIPMENT, EMERGENCY FLASHLIGHT AT AFT FLT ATTENDANT STATION HAS A DEAD BATTERY. MX REPLACED FLASHLIGHT BATTERY. 2 L 7 2 4F RT A16WE 20080520 NM 2008 5 20 BB08083 1 20080506 A 2750 251N402234 TRANSMISSION BOEING 757 7572S7 1384962 NM T/E FLAP BINDING A USAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 EA 19 904AW 80292 25727 23566 PHX FLT 31 OGG TO PHX - DURING APPROACH, RECEIVED A TRAILING EDGE FLAP DISAGREE MESSAGE. THE CREW EMPLOYED THE ALTERNA TE EXTENSION METHOD TO EXTEND THE TRAILING EDGE FLAPS. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RESET T HE NR 1 OVERLOAD INDICATOR. FLAPS OPERATIONALLY CHECKED OK. AIRCRAFT PLACED ON MONITOR STATUS TO INSPECT THE OVERLOAD INDICATOR FOR EXTENSION. MAINTENANCE REPLACED THE NUMBER ONE TRAILING EDGE FLAP TRANSMISSION. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 20080520 EU 2008 5 20 BA08018 1 20080509 A 2560 P04010021 BATTERY AIRBUS 330 A330323 3930335 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 272AY 0333 MAN - THE R-4 DOOR FLASHLIGHT BELOW THE FLIGHT ATTENDANT SEAT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES TO THE FLASHLIGHT. OK FOR SERVICE. 2 L 7 2 4F RT A46NM 20080520 NM 2008 5 20 USAA920081013 1 20080506 A 5210 143N833420 INTERCOSTAL BOEING 757 757225 1384959 NM L2 DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924UW 22204 PIT - MAJOR REPAIR - C2 CHECK - CRACKED L2 DOOR INTERCOSTAL WEB AT THE NR 4 DOOR STOP. REPLACED L2 DOOR INTERCOSTAL WEB AT THE NR 4 DOOR STOP IAW USAIRWAYS EO 5304R143. 2 L 7 2 4F RT A2NM 20080520 NM 2008 5 20 USAA920081016 1 20080416 A 5320 146T20031 FITTING BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 MIA - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON FITTING, BS 1065, S23L. REPLACED FITTING, BS 1065, S23L IAW B767 S RM 53-60-05. 2 L 7 2 4F RT A1NM 20080520 NM 2008 5 20 UIEA200800188 1 20080513 A 5347 SEAT TRACK BOEING 747 7472D7B 1384803 NM FUSELAGE CHAFED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK STA 935 LBL 33 SEAT TRACK FOUND CHAFED. REPAIRED SEAT TRACK PER SRM 51-10-02. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 KCSA081245 1 20080515 A 3350 LIGHT BOEING 747 7472B4B 138481B NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 713CK 21099 LT EMERGENCY LIGHT IN CEILING JUST AFT OF GALLEY WILL NOT LIGHT. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800196 1 20080512 A 5210 T08T062611 STOP FITTING BOEING 747 7472D7B 1384803 NM L3 DOOR BROKEN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK L3 DOOR AFT SIDE NR 2 COUNTED FROM BOTTOM STOP FITTING BROKEN. REPLACED STOP FITTING PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800198 1 20080511 A 5330 SKIN BOEING 747 7472D7B 1384803 NM FUSELAGE CHAFED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 FUSELAGE LOWER LOBE STA 220 - 240 LEFT SIDE STR 36L - 37L FOUND CHAFING. CHAFED AREA SMOOTHED OUT PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800205 1 20080511 A 5330 SKIN BOEING 747 7472D7B 1384803 NM FUSELAGE DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 BODY STATION 220 STRINGER 28L FOUND AREA DENTED AS MARKED. DENTED AREA RE-WORKED AS PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 20080520 SO 2008 5 20 LR7A08057 1 20080513 A 5511 3702981 BULKHEAD LKHEED 382 382G 526414U SO HORIZ STAB CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK, FOUND HORIZ STABILIZER REAR BHD CRACKED AT FS 1138, RBL 27. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-17. 2 H 7 4 4T A1SO 20080520 SO 2008 5 20 LR7A08058 1 20080513 A 5312 34011437 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND AFT FUSELAGE INTERIOR UPPER BHD WEB CRACKED AT FS 1012, WL280, RBL 6. REPAIR ACCOMPLISHED IAW SMP583 FIG 51-140-71. 2 H 7 4 4T A1SO 20080520 SO 2008 5 20 LR7A08061 1 20080513 A 5347 372349 FITTING LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND RT CABIN TIE DOWN WELL CHINE CAP EXFOLIATION CORROSION AT FS 516, WL146, RBL59.5. REPAIR ACCOMPLISHED IAW SMP583 FIG 53-40-54. 2 H 7 4 4T A1SO 20080520 WP 2008 5 20 RYNA200800016 1 20080417 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 932RD 49233 PASSENGER CABIN RIGHT INBOARD SEAT TRACK IS CORRODED AT BS 579. REPAIRED CORRODED ARE IAW MD-80 SRM 51-10-03. 2 L 7 2 4F A6WE 20080520 WP 2008 5 20 RYNA200800015 1 20080417 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 932RD 49233 PASSENGER CABIN RIGHT INBOARD SEAT TRACK IS CORRODED AT BS 1022-1060. REPAIRED CORRODED ARE IAW SRM 51-10-03. 2 L 7 2 4F A6WE 20080519 NM 2008 5 19 F3LA200800209 1 20080501 A 5321 D5367221800000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 75 2103 DURING C3 S1 C CHECK INSPECTION NOTED FWD CARGO DOOR FLOOR PANEL HAD A PUNCTURE. MAINTENANCE CLEANED AREA, PREPPED AND APPLIED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PARAGRAPH 8C. UPON COMPLETION OF THE REPAIR IT WAS I NSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080519 SO 2008 5 19 SMIA200812904 1 20080506 A 5320 13500429403 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 832AE 145627 ON MBV INSPECTION, LEFT OMEGA BEAM WAS FOUND TO HAVE CORROSION AT CROSS MEMBER FRAME 25. REPAIRED OMEGA BEAM IAW SRM 53 -00-10 FIG 202. AIRCRAFT RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20080519 NM 2008 5 19 DLM88080691 1 20080502 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 960DL 49979 EXFOLIATION CORROSION ON LOWER DOOR JAMB OF C-3. REPAIRED PER SRM 53-05D FIG 63 ON N/R T0093048 AT HMV-3 IN GDL. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 DLM90080712 1 20080506 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 RIGHT CUSP WEB CORRODED AT FIRST LIGHTNING HOLE AFT OF STA 465 ON UPPER AND LWR SURFACE. WEB WAS FOUND TO BE OUT OF LIM ITS, IAW MD90 SRM 53-00-01, FIG 3. WORK TO BE ACCOMPLISHED ON N/R 1003732 2400/0215 S/N 109915. 2 L 7 2 4F RT A6WE 20080519 NM 2008 5 19 AALA200800999 1 20080417 A 3350 COVER BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 796AN 30796 DFW - EMERGENCY LIGHT WIRING AT MAIN DECK CREW REST FORWARD CLOSET EXPOSED. REPLACED PROTECTIVE COVER FOR EMERGENCY LIG HT WIRING AT MAIN DECK CREW REST FORWARD CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 NM 2008 5 19 AALA200801001 1 20080418 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 782AN 30003 JFK - EMERGENCY LIGHT AT SEAT 21G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 NM 2008 5 19 AALA200801002 1 20080418 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 782AN 30003 JFK - EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080519 EA 2008 5 19 MASA200800366 1 20080505 A 2560 SEAL CNDAIR CL600 CL6002D24 1390016 EA EEMK BROKEN A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 925FJ 15025 ASH FLT 2663 CLT-AUS - EEMK SEAL BROKEN. MX RESEALED EEMK. 2 L 7 2 4F RT A21EA 20080519 EA 2008 5 19 MASA200800380 1 20080507 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP OUT OF RIG A MASA O OTHER O OTHER DE DESCENT 1 SW 07 693BR 7761 ASH FLT 1908 HNL- OVERNIGHT - FLAPS FAIL CAUTION OCCURRED ON EXTENSION BETWEEN 20 AND 30 DEGREES WITH THE HANDLE SELECTE D TO 30 DEGREES. MX COMPLIED WITH THE FLAPS FAIL PARTS A AND B PROCEDURES AND RIGGED THE BPSU UNITS. 2 L 7 2 4F RT A21EA 20080519 EA 2008 5 19 MASA200800386 1 20080508 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 918FJ 15018 ASH FLT 2782 PHX-SAT - EMERGENCY LIGHTS INOP IN GALLEY AND ROW 16A AND 16F. MX PERFOMED, OPS CHECK OF EMERGENCY LIGHTIN G SYSTEM, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080520 EA 2008 5 20 MASA200800396 1 20080513 A 5210 DOOR CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 511MJ 10104 ASH FLT 7127 IAD-CLT - PASSENGER DOOR VERY HARD TO OPEN. LUBED DOOR. 2 L 7 2 4F RT A21EA 20080520 EU 2008 5 20 08FDEA01843 1 20080514 A 5720 A57111092202 FITTING AIRBUS 300 A300B4622R 3930312 EU CENTER WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND ON SEVERAL HOLES IN CENTER WING BOX LOWER JUNCTION VERTICAL FLANGE C47 WITH DAMAGE AND CRACKS (HOLE H, I, M, N, V) REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL DAMAGE REMOVAL AND INSTALLING FASTENER NSA5351-9 AND NSA5479, APPROVED B Y RAS/70503969/045/2008 ISS A AND EA 6-5710-117142. 2 L 7 2 4F RT A35EU 20080520 NM 2008 5 20 UIEA200800177 1 20080509 A 5730 SKIN PANEL BOEING 747 747228F 1384895 NM LT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 LT WING UPPER FIXED LEADING EDGE PANEL CRACKED AND DELAMINATED, ILES 833.00, 20 INCHES FROM AFT EDGE OF PANEL. PERMANEN T REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 18, SHEETS 3 AND 5 PREPREG 250 DEGREES CURE PER SRM 51-40-12. R EF: ATLAS AIR EO NR 4757A438. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 USAA920080998 1 20080503 A 5315 FLOORBEAM BOEING 757 75723N 1384973 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 203UW 30548 BFM - MAJOR REPAIR - C2 CHECK - CORROSION ON CABIN FLOORBEAM, BS 365, RBL 5 - RBL 15, WL 208. REPAIRED CABIN FLOORBEAM, BS 365, RBL 5 - RBL 15, WL 208 IAW B757 SRM 53-00-51. 2 L 7 2 4F RT A2NM 20080520 EU 2008 5 20 USAA920081008 1 20080505 A 5330 D5348002221300 SKIN AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 629AW 76 PHX - MAJOR REPAIR - CORROSION ON FUSELAGE SKIN, BS 3310/FR 69, S30R AT THE AFT LAVATORY VENT OUTLET. REPAIRED FUSELAGE SKIN, BS 3310/FR 69, S30R AT THE AFT LAVATORY VENT OUTLET IAW USAIRWAYS EA 120721. 2 L 7 2 4F RT A28NM 20080520 EU 2008 5 20 USAA920081010 1 20080506 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 626AW 65 FLT NR 616 PHX-ATL - EEL - AFT GALLEY EMERGENCY LIGHT BATTERY INOP. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EME RGENCY LIGHT BATTERY. 2 L 7 2 4F RT A28NM 20080520 NM 2008 5 20 BB08081 1 20080504 A 3350 S417N50911 LIGHT BOEING 767 767201 1385125 NM CABIN MISSING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245AY 23897 MXP - ONE FLOOR EMERGENCY LIGHT ASSEMBLY ON RIGHT SIDE, FIRST ONE BY THE R1 DOOR, IS MISSING. MAINTENANCE INSTALLED LIG HT ASSEMBLY. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A1NM 20080520 NM 2008 5 20 BB08082 1 20080505 A 2560 P4010021 BATTERY BOEING 767 7672B7 1385107 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 252AU 24765 PHL - AFT FLASHLIGHT INOP. MAINTENANCE REPLACED THE BATTERY IN THE AFT FLASHLIGHT. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20080520 NM 2008 5 20 USAA920081018 1 20080508 A 5330 6545778 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 23879 CLT - MAJOR REPAIR - C4 CHECK - CRACKED FUSELAGE SKIN, BS 947.5, S14R. REPAIRED FUSELAGE SKIN, BS 947.5, S14R IAW B737 SRM 53-60-01 REPAIR 7. 2 L 7 2 4F RT A16WE 20080520 NM 2008 5 20 SB08028 1 20080507 A 3350 3004321 LIGHT BOEING 737 7374B7 1384702 NM EXTERIOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 458UW 25022 CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT ESCAPE SLIDE LIGHT AT THE AFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20080520 NM 2008 5 20 USAA920081021 1 20080420 A 5320 143N55225 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - LEVEL 2 CORROSION ON FLOOR SUPPORT, BS 720 - BS 740, LBL 60 - LBL 65, WL 206. REPLACE D FLOOR SUPPORT, BS 720 - BS 740, LBL 60 - LBL 65, WL 206 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 20080520 NM 2008 5 20 UIEA200800189 1 20080513 A 5347 SEAT TRACK BOEING 747 7472D7B 1384803 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK STA 980 RBL 33 SEAT TRACK OUTBOARD FLANGE FOUND CORRODED. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800199 1 20080509 A 5315 FLOORBEAM BOEING 747 7472D7B 1384803 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK STA 980 RBL 45 TO RBL 55 FLOORBEAM UPPER CHORD FOUND WITH LEVEL 1 CORROSION. CORROSION REMOVED PER SRM 53-10- 01, 51-10-01, 51-10-02. 2 L 7 4 4F RT A20WE 20080520 WP 2008 5 20 RYNA200800017 1 20080417 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 932RD 49233 PASSENGER CABIN RIGHT INBOARD SEAT TRACK IS CORRODED AT BS 448. REPAIRED CORRODED AREA IAW MD-80 SRM 51-10-03. 2 L 7 2 4F A6WE 20080520 NM 2008 5 20 2008UALA02653 1 20080507 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 CORROSION ON SHEAR TIE AT BS 1197+132, BETWEEN STR 38R-39R. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080520 NM 2008 5 20 2008UALA02658 1 20080507 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 CORROSION ON SHEAR TIE AT BS 1197+132, BETWEEN STR 38L-39L. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080520 NM 2008 5 20 2008UALA02660 1 20080507 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 AFT PIT BS 1400 AT STR 26L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGE AND INSTALLED "J" ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080520 NM 2008 5 20 2008UALA02665 1 20080507 A 3610 ISOLATION VALVE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RT ENGINE UNKNOWN A UALA D RETURN TO BLOCK O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 RIGHT ENGINE ISOLATION ISLN VALVE WON`T OPEN. 2 L 7 2 4F 4 F RT A1NM E24NE 20080520 NM 2008 5 20 2008UALA02673 1 20080507 A 2910 LINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HYDRAULIC SYS LEAKING A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 642UA 25092 LEFT HYDRAULIC QTY BELOW RF (.72). FOUND PRESSURE LINE AT RH WING OUTBOARD SPOILER LEAKING REPLACED LINE WITH FLEX LINE PER GNMM 1-0-13-003 OPS AND LEAK CK OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080520 NM 2008 5 20 2008UALA02679 1 20080507 A 5280 DOOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NLG CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 226UA 30226 RT AFT NLG DOOR AFT LOWER CORNER CRACKED APPROX 3 INCH BY 1 INCH AREA. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080520 NM 2008 5 20 2008UALA02649 1 20080506 A 5311 146N1008 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 FRAME REPAIRED AT BS 580 BETWEEN STR'S 22L AND 23L. MAJOR REPAIR ACCOMPLISHED, INSTALLED NEW FRAME REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080520 NM 2008 5 20 2008UALA02651 1 20080506 A 5311 146N8611 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 AFT PIT BS 1540 AT STR 25R FRAME DENTED. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGE. INSTALLED "J" ANGLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080520 NM 2008 5 20 2008UALA02703 1 20080510 A 3260 WARNING SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT ACTIVATED A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION AP APPROACH 1 WP 29 825UA 980 LANDED UNDER AMBER ALERT DUE TO UNSAFE GEAR INDICATION. LANDING GEAR GRAVITY EXTENDED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080520 NM 2008 5 20 2008UALA02704 1 20080510 A 2913 4205401 PUMP BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE RIGHT OVERHEATED A UALA A UNSCHED LANDING W M INADEQUATE Q C OVER TEMP CL CLIMB 1 WP 29 666UA 29238 RIGHT HYDRAULIC SYSTEM OVERHEAT PROBLEM CAUSED FLIGHT DIVERSION. REPLACED RT EDP. NO SHOP RECORD FOUND. ROOT CAUSE UN KNOWN. 2 L 7 2 4F 4 F RT A1NM E24NE 20080528 NM 2008 5 28 SWAA082752 1 20080520 A 5753 SKIN BOEING 737 7377H4 1384404 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED 10Y CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD T/E. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082730 1 20080519 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 379 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER 15R CRACKED AT BS 379. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080521 NM 2008 5 21 KCSA081248 1 20080518 A 5210 WEB BOEING 747 747212B 1384886 NM L4 DOOR DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 L-4 MAIN ENTRY DOOR LOWER WEB ACCESS AREA DAMAGED AT BS 1700, STR 24L. 2 L 7 4 4F RT A20WE 20080522 CE 2008 5 22 DXTA200803072 1 20080520 A 3241 MP50B1 MOTOR CESSNA 500 560CESSNA 2076750 CE ANTI SKID SYS INOPERATIVE E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 830QS 26 5600784 LOW BRAKE PRESS ANNUNCIATOR ILLUMINATED UP ON REACHING HOLD LINE. GAINED ACCESS TO ANTI-SKID MOTOR. REMOVED AND REPLACE D MOTOR. OPS CK GOOD IAW MM 32-42-06. REMOVED AND REPLACED POWER BRAKE CIRCUIT BREAKER. OPS CK GOOD IAW MM 24-50-02. 2 L 7 2 4F RT A22CE 20080522 CE 2008 5 22 DXTA200803073 1 20080520 A 3233 99125373 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 623QS 5605299 LT MLG INDICATED AN UNSAFE CONDITION AFTER GEAR WAS EXTENDED NORMALY. REMOVED THE LT MLG ACTUATOR AND REPLACED WITH A R EPAIRED ACTUATOR (TOTAL CYCLES 3103) IAW THE MM 32-30-04. OPERATIONAL CHECKS AND LEAK CHECKS SATISFACTORY. 2 L 7 2 4F 4 F RT A22CE E00059EN 20080522 NM 2008 5 22 QXEA200800450 1 20080505 A 6123 SWITCH DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS LOOSE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 345PH 476 SEA - AUTOFEATHER SWITCH APPEARS LOOSE AND TAKES LONGER THEN NORMAL TO ARM. MAINTENANCE SECURED THE SWITCH. OPERATIONA L CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080522 NM 2008 5 22 QXEA200800465 1 20080509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 724-729 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 425QX 4039 PDX - C4 CHECK - LT CENTER NR 9 SEAT TRACK AT STATION 724-729 HAS MULTIPLE PLACES OF CORROSION AND PITTING. REPLACED TH E NR 9 SEAT TRACK. 2 H 7 2 4T RT A13NM 20080522 NM 2008 5 22 QXEA200800462 1 20080509 A 5320 ANGLE BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 425QX 4039 PDX- C4 CHECK- CORROSION AROUND SCREW HOLE AT STATION 783 (LOWER ANGLE FOR CARGO PIT STEP). BLENDED CORROSION AROUND SC REW HOLE IAW SRM 51-21-00. OUT OF LIMITS. INSTALLED NEW SHEAR WEB SUPPORT ANGLE. 2 H 7 2 4T RT A13NM 20080522 NM 2008 5 22 QXEA200800463 1 20080509 A 5320 STRUCTURE BOMBDR DHC8 DHC8402 1390042 NM CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 425QX 4039 PDX - C4 CHECK, NUTPLATE AND MATING SURFACE AREA ARE CORRODED AT STATION X763. DRILLED OUT RIVETS HOLDING NUTPLATE DOUB LER AND DRILLED NUTPLATE OFF. BLENDED CORROSION IAW SRM 51-21-00. .010 INCH REMOVED, WITHIN LIMITS. ALODINED AND PRIM ED AREA AND RE-INSTALLED. 2 H 7 2 4T RT A13NM 20080522 NM 2008 5 22 QXEA200800460 1 20080509 A 5420 SUPPORT BOMBDR DHC8 DHC8402 1390042 NM CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 425QX 4039 PDX - C4 CHECK, RT FINGERNAIL DECK LOWER AFT SUPPORT IS CRACKED AT ALL 4 BOLT HOLES. FABRICATED NEW SUPPORT CHANNEL FRO M 2024T3 .032 INCH REFERENCE Q400 SRM 54-35-20 REPAIR 2. INSTALLED. 2 H 7 2 4T RT A13NM 20080522 NM 2008 5 22 KCSA081252 1 20080518 A 5330 SKIN BOEING 747 747123 1384873 NM BS 788 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 SMALL AREA OF DAMAGE ON FUSELAGE BELLY SKIN AT BS 788, LBL-2. 2 L 7 4 4F RT A20WE 20080523 NM 2008 5 23 UPS08M52204 1 20080328 A 5330 N6A6708 SKIN DOUG MD11 MD11F 3023600 NM BS 1119 S1 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 272UP 48571 INSPECTION TYPE:C LIGHTNING STRIKE OUTER FUSE SKIN, FS 1119 STR 1. DISPLACED INSULATION FOR ACCESS IAW AMM 25-82-01-4 2 . REMOVED DAMAGED FASTENERS IAW SRM 51-35-01, BURN AROUND COUNTER SINK & OUTER SKIN DIA OR LENGTH: .420" DEEP: .060"D, NORMAL DIA OF CSK IS .290"~.30" LOCATION: STA 6-91.5 STRINGER 1R. DAMAGE IS BEYOND LIGHTNING STRIKE DAMAGE REPAIR LIMI T IAW SRM 53-20-00. 2 L 7 3 4F RT A22WE 20080523 EU 2008 5 23 USAA920081049 1 20080503 A 5320 D53471124200 SHEAR WEB AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650AW 856 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON LEFT SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, +Y1732. REPLACED LE FT SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / FR 70, +Y1732 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20080523 EU 2008 5 23 USAA920081050 1 20080506 A 5315 D53472098000 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650AW 856 SAL - MAJOR REPAIR - C4 CHECK - CORROSION ON CABIN FLOORBEAM BS 3158 / FR 65, +Y920. REPLACED CABIN BEAM, BS 3101 / FR 65 - BS 3207 / FR 67, +Y920 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20080523 SO 2008 5 23 FDKA200805190 1 20080505 A 2620 EXTINGUISHER EMB 145 EMB145LR 3260212 SO CARGO BAY INOPERATIVE A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 841MJ 145448 FDM 6132 MCO-RIC. BAG EXTINGUISHER BOTTLE INOP/ BAG LIGHT INDICATION. RESET SYSTEM, NO FURTHER ACTION REQUIRED. 2 L 7 2 4T RT T00011AT 20080523 EU 2008 5 23 USAA920081028 1 20080506 A 5320 D5311146100201 FLOOR SUPPORT AIRBUS 320 A320214 3930316 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 105UW 868 PIT - MAJOR REPAIR - C11 CHECK - CORROSION ON FLOORBEAM, BS 605 / FR 12 - BS 950 / FR 24, -Y254. REPLACED FLOORBEAM, BS 605 / FR 12 - BS 950 / FR 24, -Y254 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20080523 SO 2008 5 23 FDKA200805198 1 20080511 A 5210 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 849MJ 145534 FDM 6177 PNS-TPA. MAIN CABIN DOOR HARD TO LOCK CLOSED. MX CLEANED AND LUBED DOOR SEAL, OPS GOOD. 2 L 7 2 4T RT T00011AT 20080523 EA 2008 5 23 MASA200800407 1 20080518 A 5230 DOOR CNDAIR CL600 CL6002B19 1900309 EA OVERSERVICED A MASA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SW 07 649BR 7414 ASH 7163 IAD - REPORTED HAVING TROUBLE OPENING THE SERVICE DOOR. MX REMOVED EXCESS GREASE FROM DOOR. 2 L 7 2 4F RT A21EA 20080523 WP 2008 5 23 UPS08852180 1 20080408 A 5753 LINK DOUG DC8 DC873F 302199F WP LT WING TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 LEFT WING I/B ATTACH LINK AT STA XW 106 HAS DEEP GOUGE. BLENDED GOUGE, REWORKED FINISH AND HFEC, FLA P PEENED IAW SRM EO 008-2 760-01-A1360, DPS 4.999-2, 57-2-0. 2 L 7 4 4F RT 4A25 20080527 NM 2008 5 27 USAA920081068 1 20080509 A 3397 WIRE HARNESS BOEING 757 7572S7 1384962 NM EMERGENCY LIGHTS SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 902AW 23322 MCN - EES - C12 CHECK - EMERGENCY BATTERY WIRING HARNESS WIRING SHORTED IN FIRST CLASS CEILING AREA. REPAIRED AND OPERA TIONAL CHECKED EMERGENCY BATTERY WIRING HARNESS WIRING SHORTED IN FIRST CLASS CEILING AREA IAW BSWPM 20-30-12 AND B757 A MM 33-017AW. 2 L 7 2 4F RT A2NM 20080527 NM 2008 5 27 SWAA082635 1 20080514 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 407WN 29817 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 ASAA0842939 1 20080429 A 5755 SKIN BOEING 737 7374Q8 138447Q NM NR 4 SPOILER DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 NR 4 SPOILER LOWER SURFACE IS CREASED. REMOVED DAMAGED SECTION OF SKIN, FABRICATED AND INSTALLED REPAIR CORE FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 ASAA0842943 1 20080427 A 5753 SKIN BOEING 737 7374Q8 138447Q NM RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 RIGHT WING TRAILING EDGE I/B AFT FLAP LOWER SURFACE DENTED AT WBL 77. PREPPED DAMAGED AREA, CUT TO FIT AND INSTALLED PR EPREG GLASS IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082636 1 20080514 A 3350 417N5212 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 499WN 32481 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082652 1 20080515 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727B S25L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 ASAA0842948 1 20080511 A 5753 SKIN BOEING 737 7374Q8 138447Q NM RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 RIGHT WING TRAILING EDGE INBOARD AFT FLAPS LWR SURFACE IS DENTED AT WBL 89.5. DENT MEASURES A=.6 Y= .030. REPAIRED RIG HT INBOARD AFT FLAP TRAILING EDGE LWR SURFACE IAW B737 400 SRM 51 70 10 REPAIR 2 PG 201. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 UPS08M52221 1 20080510 A 5230 ACA73321 FITTING DOUG MD11 MD11F 3023600 NM CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 272UP 48571 INSPECTION TYPE:C REF: D368427 - MAIN CARGO DOOR ACTUATOR SUPPORT ASSY FITTING INTERIM REPAIR. REMOVED MAIN CARGO ACTUA TOR AND LINK ASSY AS PER AMM 52-34-01-4/EO N MD11-5230-28549-A. TEMP INSTALLED MAIN CARGO DOOR ACTUATOR TO FOM. REMOV ED MAIN CARGO DOOR ACTUATOR IAW AMM 52-34-01-4. REMOVED GOUGE FITTING BY REAMING HOLES 2EA UP TO .850" IAW EA11-523. 2 L 7 3 4F RT A22WE 20080527 NM 2008 5 27 SWAA082710 1 20080518 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 842 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 842, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082689 1 20080516 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727A S26L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082709 1 20080518 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082693 1 20080516 A 5753 6546435335 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED SERVICE CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP INBOARD END DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082720 1 20080518 A 2530 41600019 COFFEEMAKER BOEING 737 7377H4 1384404 NM GALLEY FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 919WN 36625 SMOKE DETECTED INFLIGHT FROM FWD COFFEEMAKER. SMOKE DISSIPATED AFTER GALLEY POWER SHUT OFF. FOUND COFFEEMAKER WIRES SH ORTED. REMOVED AND REPLACED COFFEEMAKER PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082736 1 20080519 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 855 S14L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND STRINGER 14L CRACKED AT BS 855. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082737 1 20080519 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 787, STR 27R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080528 2008 5 28 SWAA082725 4 20080519 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082727 1 20080519 A 3350 20131A BATTERY PACK BOEING 737 7373A4 1384585 NM EMERGENCY LIGHT FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED SERVICE CHECK, AFT CABIN EMERGENCY BATTERY PACKS WILL NOT CHARGE. REMOVED AND REPLACED BATTERY PACKS P ER MM. 2 L 7 2 4F RT A16WE 20080528 2008 5 28 SWAA082738 4 20080519 A 2565 6557463 FITTING BOEING 737 7373Q8 1384670 NM L2 DOOR GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082728 1 20080519 A 5754 SKIN BOEING 737 7377H4 1384404 NM NR 1 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 710SW 27844 DURING SCHEDULED 10Y CHECK, FOUND LT WING NR 1 L/E SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082769 1 20080521 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 360 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080528 2008 5 28 SWAA082771 4 20080521 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080528 2008 5 28 SWAA082770 4 20080521 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082772 1 20080521 A 5753 6546486 WEDGE BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED HC1 CHECK, FOUND LT WING INBOARD MID FLAP WEDGE DELAMINATED AT INBOARD END. REMOVED AND REPLACED WEDGE PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082759 1 20080521 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM BS 980-1002 WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED BRDG CHECK, FOUND UPPER FUSELAGE SKIN WORN BETWEEN BS 980 AND BS 1002, BELOW DORSAL FIN. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082760 1 20080521 A 5330 656938780 SKIN BOEING 737 7375H4 138449D NM BS 386 S25L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 386, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082761 1 20080521 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM BS 941 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082762 1 20080521 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 L1 DOOR EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082718 1 20080515 A 5310 6517688 CREASE BEAM BOEING 737 7373Q8 1384670 NM BS 314-343 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 314 AND BS 343, LBL 58 TO LBL 65. REMOVED AND REP LACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080528 SO 2008 5 28 SIMA200813702 1 20080513 A 2121 4611028900 FAN EMB 145 EMB145LR 3260212 SO RECIRCULATION ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 644AE 145204 ON FLIGHT 4409, CREW REPORTED WHILE CRUISING FL 270 A VERY STRONG ELECTRIC ODOR EMANATED FROM THE VENTS SUPPLIED PACK 1 IN CABIN. AIRCRAFT REMOVED FROM SERVICE. FOUND SOURCE OF ODOR TO BE FAILED LEFT RECIRCULATION FAN. REMOVED AND REPLAC ED LEFT RECIRCULATION FAN IAW EMB-145 AMM 21-24-01; OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20080528 SO 2008 5 28 SIMA200813703 1 20080509 A 3244 31641 TIRE EMB 145 EMB145LR 3260212 SO NR 2 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 21 941LT 14500926 ON FLIGHT 3386, OPERATIONS CALLED MOC AND REPORTED FOD FOUND ON RUNWAY FROM TIRE DEBRIS AFTER FLIGHT 3386 DEPARTED FROM THE RUNWAY. SOC INFORMED CREW OF POSSIBLE TIRE DAMAGE IN FLIGHT. AIRCRAFT PERFORMED FLYBY AT DFW AND LANDED WITH THE N R 2 MAIN TIRE BLOWN, FLAPS WERE DAMAGED AND NO OTHER PROBLEMS NOTED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLA CED NR 2 TIRE, REMOVED AND REPLACED E1 FAN BY-PASS VANES, E1 CONTAINMENT RING. TEMPORARY REPAIRED FLAP. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4T RT T00011AT 20080528 NM 2008 5 28 NWAA082125803 1 20080514 A 3350 BATTERY PACK BOEING 757 757351 1384991 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 583NW 32983 BATTERY PACK ASSOCIATED WITH THE ESCAPE PATH LIGHTING AT ROWS FOUR THROUGH SIX FAILED DURING EMERGENCY LIGHT BATTERY PAC K CHECK DURING SCHEDULED OVERNIGHT MAINTENANCE. MAINTENANCE REPLACED THE BATTERY PACK AND ALL OPERATIONS CHECKED GOOD. 2 L 7 2 4F RT A2NM 20080528 GL 2008 5 28 SIMA200814304 2 20080520 A 7210 4252070 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL NR 1 AGB UNSERVICEABLE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 941LT 14500926 CAE312728 ON FLIGHT 3738, DURING TAKEOFF CREW REPORTED STRONG BURNING OIL SMELL ON CLIMB-OUT, PACKS ON, BLEEDS ON. AIRCRAFT REMOV ED FROM SERVICE. REMOVED AND REPLACED NR 1 ENGINE AGB BREATHER CARBON SEAL IAW 72-63-10. OPERATIONAL CHECK GOOD. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080528 SO 2008 5 28 SIMA200814302 1 20080520 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 641AE 145191 ON FLIGHT 4186, DURING TAXI CREW REPORTS EMERGENCY EXIT SIGN LIGHT ABOVE FLIGHT ATTENDANT JUMP SEAT IS INOPERATIVE. AIR CRAFT REMOVED FROM SERVICE. RESECURED EXIT SIGN CONNECTOR IAW AMM 33-50-14. PERFORMED OPERATIONAL CHECK OF EMERGENCY L IGHTING IAW AMM 33-50-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20080528 NM 2008 5 28 NWAA082215649 1 20080515 A 5330 SKIN BOEING 757 757251 1384970 NM BS 633 S17L DENTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 549US 26496 DURING "M" CHECK FOUND DENT IN FUSELAGE SKIN AT BS 633 S17L. REPAIRED PER EA 56-210590. 2 L 7 2 4F RT A2NM 20080528 NM 2008 5 28 NWAA082335513 1 20080523 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 513US 23201 DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS AT DOOR 1R FAILED CHECKOUT. MAINTENANCE REMOVED AND REPLACED BATTERY PAC K M730, ALL OPERATIONS CHECKED OK. 2 L 7 2 4F RT A2NM 20080528 WP 2008 5 28 NWAA082299926 1 20080520 A 3397 WIRE HARNESS DOUG DC9 DC932 3022066 WP EMERGENCY LIGHTS CRUSHED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 926NW 47425 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 18-21 OF THE CABIN WERE INOPERATIVE. F URTHER INSPECTION REVEALED THAT THE WIRE HARNESS UNDER SEAT ROW 20 AND 21 WAS SMASHED AND CAUSING A SHORT. THE WIRING W AS REPLACED, AS WAS THE FUSE, AND THE SYSTEM FUNCTIONAL CHECK WAS GOOD. 2 L 7 2 4F A6WE 20080528 WP 2008 5 28 IXXA08SMN094S 1 20080313 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1446 L36 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND DOUBLER AFT LOWER FUSELAGE BELLY BELOW AND AFT OF D-PIT DOOR RIVET SPACING EXCE EDED ON SIDE FOUR, ALSO ALUMINUM FASTENERS IN FRAMES AT FS 1446 LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REP AIR. REMOVED DAMAGED AREA. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, FILLER SKIN, INTERNAL FINGER DOUBLER, FILLER INTERNAL DOUBLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR P ARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-1-12, 51-3-1,FAA FORM 8110-3 NUMBER 08205 DATED 04/29/08M, SEMAN DRAWING NUMBER ED-4735 DATED 03/24/08, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51- 2 L 7 4 4F RT 4A25 20080528 WP 2008 5 28 IXXA08SMN170S 1 20080419 A 5340 FITTING DOUG DC8 DC871F 302199D WP BS 798 L20L CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION; FOUND LEFT CUSP EXTRUSION UPPER SURFACE FORWARD FITTING CRACKED AT STATION 798.000 LO NGERON 20 LEFT. REMOVED CRACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED TREATED AND PRIMED FITTING AND AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-3-1, DC8 SRM 51-1-20D, DACO DPS 4.7 07, DC8 SRM 51-1-8B, ATI REPAIR SPECIFICATION NUMBER 2003-05, DOUGLAS DRAWING 3779970. 2 L 7 4 4F RT 4A25 20080528 WP 2008 5 28 IXXA08SMN180S 1 20080419 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING NR 1 LOWER PART STUB WING HAS IMPROPER REPAIR REMOVED FASTENERS AS NE EDED TP PERFORM REPAIR. REMOVED EXITING REPAIR. FABRICATED EXTERNAL DOUBLER, AND INTERNAL DOUBLER. PERFORMED HEAT TRE ATMENT. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-2-1A FIGURE 1, DC8 SRM 51-1-20D, DC8 SRM 51-1-1 PAGES 1 13 AND 17, DC8 SRM 51-1-8B, 51-1-11, 51-1-21, AND 51-3-1. 2 L 7 4 4F RT 4A25 20080528 NM 2008 5 28 NWAA082206311 1 20080514 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 671US 26477 DURING OVERNIGHT CHECK FOUND DOOR 2 LEFT EMERGENCY LIGHT WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED LIGHT AS SEMBLY AND BATTERY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20080528 NM 2008 5 28 NWAA082256302 1 20080514 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 662US 23720 DURING OVERNIGHT CHECK FOUND ZONE A LEFT SIDE EMERGENCY FLOOR LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PAC K. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20080528 WP 2008 5 28 IXXA08SMN178S 1 20080419 A 5347 S2772660 CARGO TRACK DOUG DC8 DC871F 302199D WP BS 70-340 DETERIORATED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK LUGS DETERIORATED AT STATION 70.000 TO 34 0.000. REMOVED SEGMENT OF DAMAGED TRACK AND EXISTING SPLICES. CLEANED, TREATED AND PRIMED AREA AND EXISTING SPLICES. INSTALLED NEW SEGMENT OF TRACK AND REINSTALLED SPLICES IAW DC8 SRM 53-2-3 FIGURE 14 SHEET 1 PAGES 49-50, DC8 SRM 53-1-0 PAGE 1, 51-3-0, DC8 SRM 51-1-8B, 51-3-0, AND 51-3-1. 2 L 7 4 4F RT 4A25 20080528 WP 2008 5 28 NWAA082309995 1 20080522 A 3397 WIRE DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8978E 47327 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 18-21 OF THE CABIN WERE INOPERATIVE. A BROKEN WIRE WAS DISCOVERED AS THE CAUSE AND MAINTENANCE REPAIRED IT WITH A SPLICE. FUNCTIONAL CHECK WAS GOOD. 2 L 7 2 4F A6WE 20080528 WP 2008 5 28 NWAA082119917 1 20080513 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 967N 47573 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN LIGHT FOR THE AFT EXIT DOOR WAS INOPERATIVE. MAINTENA NCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM. 2 L 7 2 4F A6WE 20080528 EA 2008 5 28 CHQA200800096 1 20080515 A 2741 706010 CONTROL MODULE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE STAB MALFUNCTIONED A CHQA O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 473 3136 1907 7671 GEE873457 FLIGHT 5723 SDF TO IAH - WHILE ON DESCENT INTO IAH THE CREW RECEIVED A TOTAL STAB FAILURE MESSAGE ON THE EICAS. THE CRE W RAN THEIR QRH, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. WHEN MAINTENANCE ARRIVED THEY RAN THE HSTCU SELF TE ST IAW MM 27-34-01, NO DEFECTS WERE NOTED AND THE PLANE WAS GOOD TO CONTINUE SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080528 NM 2008 5 28 KNNA200815 1 20080515 A 5753 SKIN BOEING 737 7372L9 1384497 NM TE FLAP CORRODED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 464AT BN63 21278 OPENED UP MIDFLAP AND FOUND SKIN AND UPPER CHORD CORRODED AT REAR SPAR ON O/B MID FLAP RT WING. REPLACED OUTBOARD MIDFL AP. 2 L 7 2 4F RT A16WE 20080528 SO 2008 5 28 LR7A08075 1 20080513 A 5712 RIB LKHEED 382 382G 526414U SO RT WING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC2811, FOUND RT AUX TANK OBD COMPARTMENT FWD LOWER RIB CAP CRACK AT RADIUS CWS1 41. REPAIR ACCOMPLISHED IAW LAC MEA 382-57-08-027. 2 H 7 4 4T A1SO 20080528 NM 2008 5 28 NWAA082236302 1 20080515 A 2910 LINE BOEING 747 747451 1384940 NM HYD SYSTEM CRACKED A NWAA J A DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 662US 23720 DURING CRUISE, LOST NR 1 HYDRAULIC SYSTEM. DUMPED 20,000 LBS OF FUEL. RETURNED TO MSP AND LANDING WAS UNEVENTFUL. MAI NTENANCE REMOVED AND REPLACED NR 1 EDP AND A CRACKED PRESSURE LINE. LEAK AND PRESSURE CHECKS OK. 2 L 7 4 4F RT A20WE 20080528 NM 2008 5 28 NWAA082286624 1 20080519 A 3350 POWER SUPPLY BOEING 747 747251B 1384892 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 624US 21706 DURING OVERNIGHT CHECK, FOUND MAIN DECK DOOR 2 LEFT EXIT SIGN ABOVE DOOR INOP. MAINTENANCE REMOVED AND REPLACED POWER S UPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20080528 WP 2008 5 28 IXXA08SMN119S 1 20080327 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 850 L24L CORRODED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN LEFT SIDE WITH CORROSION AT STATION FS 850.000 LONGERON 24. REMOVED FASTENERS FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED INNER TAPERED SPLICE REPAIR, FILLER SKIN. PERFORMED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-3-1, FAA FORM 8110-3 NUMBER 08205 DATED 04/29/08, DRAWING NUMBER ED-4752 DATED 03/29/08, DC8 SRM 51-1-20D, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 53-2-0 PAGE 2P, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-1 PAGES 1, 13 2 L 7 4 4F RT 4A25 20080528 WP 2008 5 28 IXXA080021O 1 20080513 A 3230 LANDING GEAR DOUG DC8 DC873F 302199F WP ZONE 700 MALFUNCTIONED A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 604BX 88355 424 46046 DURING TAKEOFF FROM GOOY, THE NOSE LANDING GEAR WOULD NOT RETRACT. THE CREW WAS ABLE TO RETRACT NOSE GEAR WITH HANDLE L ATCH FLIGHT RELEASE. WHEN NOSE GEAR RETRACTED THE TAKEOFF WARNING HORN SOUNDED, THE CREW PULLED GROUND SHIFT BREAKERS, WHEN THE LEFT BREAKER WAS PULLED THE HORN SOUNDED, PULLED THE RIGHT BREAKER PER PROCEDURE. THE CREW RETURNED TO GOOY AN D LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LANDING GEAR LEVER AND ALL SYSTEM CABLES, PULLY, BEARINGS FOR BINDING, LUBRICATED SYSTEM, ISSUED FERRY PERMIT FROM GOOY TO KTOL PER ATI GMM 3.107. FLIGHT LATCH RELEASE MECHANISM WAS USED IA W ATI DC8 COM PROCEDURES FOR GEAR RETRACTION. MAINTENANCE IN KTOL RERIGGED LANDING GEAR LEVER ANTI-RETRACT SYSTEM, OPER 2 L 7 4 4F RT 4A25 20080528 NM 2008 5 28 UIEA200800192 1 20080514 A 5280 65B1091930 DOOR BOEING 747 747228F 1384895 NM MLG DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 WHILE TROUBLESHOOTING INBOUND LOG ITEM FOR NR 1 HYD SYSTEM OVERHEAT BODY GEAR DOORS BOTH SIDES CAME IN CONTACT WITH THE TIRES WHEN HYD POWER WAS APPLIED. CAUSING DAMAGE TO BOTH DOORS. REMOVED AND REPLACED RT AND LT INBOARD BODY GEAR DOORS PER AMM 32-14-01. 2 L 7 4 4F RT A20WE 20080528 EA 2008 5 28 CHQA200800093 1 20080511 A 5200 600332801001 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE OXYGEN SERVICE OPEN A CHQA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 11 7406 7406 GEE872739 FLIGHT 5641, IAH TO LBB, AFTER TAKEOFF, THE FLIGHT CREW REPORTED A LOUD NOISE AND STALL FAIL CAUTION MESSAGE ON EICAS. THE FLIGHT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE OXYGEN SERVICI NG DOOR OPEN. THE DOOR AND LATCH WERE INSPECTED AND FOUND TO BE SERVICEABLE. THE OXYGEN SERVICING DOOR WAS CLOSED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080528 WP 2008 5 28 IXXA08SMN173S 1 20080419 A 5340 FITTING DOUG DC8 DC871F 302199D WP BS 940 L20L CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT CUSP EXTRUSION UPPER SURFACE AFT FITTING CRACKED AT STATION 940.000 LONGER ON 20 LEFT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DPS 4.707, DC8 SRM 51-1-8B, 51-3-1, ATI REPAIR SPECIFICATION NUMBER 2003-05, AND DOUGLAS DRAWING 3779874. 2 L 7 4 4F RT 4A25 20080528 WP 2008 5 28 IXXA08SMN171S 1 20080419 A 5340 FITTING DOUG DC8 DC871F 302199D WP BS 940 L20L CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT CUSP EXTRUSION UPPER SURFACE FORWARD FITTING CRACKED AT STATION 940.000 LO NGERON 20 LEFT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FO UND. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DPS 4.707, DC8 SRM 51-1 -8B, 51-3-1, ATI REPAIR SPECIFICATION NUMBER 2003-05, AND DOUGLAS DRAWING 3779874. 2 L 7 4 4F RT 4A25 20080528 WP 2008 5 28 08FDEA01881 1 20080519 A 5330 NDA6013503 SKIN DOUG DC10 DC1010 3022110 WP ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 10060 46970 DURING INSPECTION EXT LWR FUSELAGE FOUND DEEP WEAR ON SKIN AND ON EXISTING DOUBLER OF AFT JAMB FWD CARGO DOOR. 2 L 7 3 4F A22WE 20080529 NM 2008 5 29 08FDEA01891 1 20080520 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 MAIN DECK CARGO DOOR SPOOL FITTING NR 3 FOUND 3RD LAYER CRACK INDICATION AT FITTING BOLT HOLES 'A' , 'B', 'C' AND 'D'. FITTING REMOVED AND REPLACED AS PER SRM 51-31 -01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 EU 2008 5 29 08FDEA01874 1 20080517 A 5330 SKIN AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 FUSELAGE EXTERIOR SKIN HAS GOUGE AT FR 28, BETWEEN STR 8 AND STR 9RT, MEASURES 11.5 IN LONG BY .093 IN WIDE AND .003 IN DEEP INSTALLED EXTERNAL SKIN REPAIR DOUBLER AT FR 28, BETWEEN STR 8 RT AND STR 9RT IAW A300-600 SRM 53-10-12, FIG 208. 2 L 7 2 4F RT A35EU 20080529 WP 2008 5 29 08FDEA01899 1 20080520 A 5330 NGA6013 SKIN DOUG DC10 DC1010 3022110 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 EXT FUSELAGE LWR SURFACE FOUND DENT 1 INCH BY 1 INCH DEEP .080 INCH ON SKIN NEAR EDGE OF DOUBLER. REPAIRED AREA IAW SRM 53-20-00 FIG 13 SHEET 2 A & SHEET 5 VOL I. 2 L 7 3 4F A22WE 20080529 WP 2008 5 29 08FDEA01900 1 20080520 A 5230 AFA37771 SKIN DOUG DC10 DC1010 3022110 WP CARGO DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 68059 46907 DURING DC10 CARGO MODIFICATION TO ACF DURING INSPECTION FOUND ON THE CENTER LOWER CARGO DOOR LATERAL SKIN DAMAGE. REPAI RED CENTER CARGO DOOR PAN ASSEMBLY FOR SRM 52-10-00 FIG 3 VOL 1. 2 L 7 3 4F A22WE 20080529 NM 2008 5 29 08FDEA01901 1 20080520 A 5320 656724516 STRAP BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 C-2 PIT NR 3 AND NR 4 TIE STRAP HAS AREA OF LIGHT CORROSION ON BACK OF STRAP. FABRICATED NEW STRAP REF 65-67245, TREATE D AND PRIMED STRAP REF SRM 51-10-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080522 2008 5 22 DXTA200803051 4 20080509 A 2210 67083039 PITOT HEAD CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL FLT GUIDANCE FAILED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 921QS 3154 7500241 CLIMBING THROUGHT 10,000 FT, WE HAD A DUAL FGC FAILURE. INSPECTED LT AND RT PITOT PROBES. FOUND RT FWD DRAIN TO BE BLOC KED. THE RT AFT DRAIN, AND BOTH LT DRAINS HAVE DEBRIS INSIDE. REMOVED FAILED LT AND RT PITOT PROBES. INSTALLED NEW LT AN D RT PITOT PROBES, PILOTS PITOT/STATIC LEAK CHECKS GOOD. COPILOTS PITOT/STATIC LEAK CHECKS GOOD. PILOT AND COPILOT AIRSP EED .ALT, AND MACH ACCURACY CHECKS GOOD. NR 1 AND 2 TRANSPONDER ALT. ENCODING CHECKS GOOD. LT AND RT PITOT HEAT TESTS GO OD. REF MM 34-11-01 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080523 2008 5 23 UPS08M52170 2 20080506 A 7314 PUMP DOUG MD11 MD11F 3023600 NM FUEL SYSTEM FAILED A IPXA E ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 SO 01 273UP 48574 INSPECTION TYPE:N/A THE NR 1 ENGINE FLAMED OUT ON DESCENT. ATTEMPTED TO RESTART ENGINE TWICE, UNSUCCESSFUL. CREW DECLA RED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED FUEL PUMP ON NR 1 ENG. PERFORMED LEAK CHECK AND ENG TEST PER AMM 73-12-01-4. REMOVED AND REPLACED NR 1 ENG FMU. PERFORMED ENG AND LEAK CHECK PER AMM 73-31-01-00-868 AND 73-21-01-400-868. 2 L 7 3 4F RT A22WE 20080523 NM 2008 5 23 USAA920081033 1 20080507 A 5340 6935352U14 STRINGER CLIP BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED STRINGER TIE CLIP, BS 867, S4R. REPLACED STRINGER TIE CLIP, BS 867, S4R IAW B73 7 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20080523 NM 2008 5 23 USAA920081034 1 20080501 A 5340 693535214 STRINGER CLIP BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED STRINGER TIE CLIP, BS 727E, S4L. REPLACED STRINGER TIE CLIP, BS 727E, S4L IAW B 737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20080523 NM 2008 5 23 USAA920081035 1 20080506 A 5340 6935352U14 STRINGER CLIP BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED STRINGER TIE CLIP, BS 706, S10R. REPLACED STRINGER TIE CLIP, BS 706, S10R IAW B 737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20080523 NM 2008 5 23 USAA920081025 1 20080506 A 5320 907822 STRAP BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - CRACKED STRAP L1 DOOR CUTOUT, BS 320, S12L. REPAIRED STRAP L1 DOOR CUTOUT, BS 320, S12 L IAW BOEING DRAWING 90-7822. 2 L 7 2 4F RT A16WE 20080523 EU 2008 5 23 USAA920081053 1 20080506 A 5320 D534711230300 SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650AW 856 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON SUPPORT FRAME, BS 3310 / FR 69 - BS 3366 / FR 70, -Y1732. REPLACED SUPPOR T FRAME, BS 3310 / FR 69 - BS 3366 / FR 70, -Y1732 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20080527 WP 2008 5 27 UPS08852214 1 20080423 A 5340 4640162IN FITTING DOUG DC8 DC873F 302199F WP BS 1440 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 CORROSION ON T-FITTING ON TOP OF CUSP AT STA 1440 LT. REPLACED T-FITTING AT CUSP AND STA 1440 LT IAW SRM 51-03-02, SRM 51-01-20D AND 51-03-00. 2 L 7 4 4F RT 4A25 20080527 EA 2008 5 27 VNAA0804017 1 20080424 A 3244 H29X9015 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE MLG SEPARATED A VNAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 05 262PS 223 7962 CREW REPORTED ON TAKEOFF ROLL FELT A BUMP. AT DESTINATION, MAINTENANCE INSPECTED AND FOUND THE LEFT INBOARD MAIN TIRE H AD SEPARATED AND CAUSED DAMAGE TO THE UNDERNEATH PORTION OF THE LEFT WING AND LANDING GEAR. MAINTENANCE REMOVED AND REP LACED THE LEFT INBOARD MAIN TIRE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE REPAIRED ALL OTHER DAM AGE. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080527 EA 2008 5 27 VNAA0805007 1 20080505 A 2910 MS21908D6 ELBOW CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE HYD SYSTEM FAILED A VNAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 05 251PS 7931 CREW REPORTED A NR 3 HYDRAULIC LOW PRESSURE IN FLIGHT. CREW ELECTED TO DIVERT TO TYS AND LANDED WITHOUT INCIDENT. MAIN TENANCE REMOVED AND REPLACED THE BULKHEAD ELBOW IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE ALSO PR OPERLY SERVICED THE NR 3 HYDRAULIC SYSTEM. NO FURTHER LEAKS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080527 NM 2008 5 27 SWAA082640 1 20080514 A 5312 6545819 PRESSURE PANEL BOEING 737 7375H4 138449D NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED 16Y CHECK, FOUND NLG W/W CEILING PANEL CUTOUT WEB CRACKED AT RBL 7.5. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082658 1 20080515 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 787 S23R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 ASAA0842949 1 20080429 A 5755 SKIN BOEING 737 7374Q8 138447Q NM NR 4 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 NR 4 SPOILER UPPER SURFACE HAS SMALL DENTS. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 UPS08M52220 1 20080509 A 5310 STRUCTURE DOUG MD11 MD11F 3023600 NM BS 1009-1019 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:C4 WHILE GAINING ACCESS TO REPLACE A SHEARED FASTENER FOUND EXTENSIVE EXFOLIATION CORROSION BETWEEN L43R AND 45R, STA 1009 TO 1039. CORROSION DAMAGE REPAIRED PER EO 011-5310-29279-A AND EA 011- 5340-01-A1329, FINAL AND ADVA NCED COPIES. 2 L 7 3 4F RT A22WE 20080527 NM 2008 5 27 SWAA082683 1 20080518 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 380 S19L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080520 NE 2008 5 20 2008UALA02705 2 20080511 A 7230 BLADE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE HPC FAILED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 29 441UA 751 V10852 NR 2 ENGINE STALL. AMBER DECLARED, FLIGHT DIVERTED. ENGINE REPLACED. FOUND HPC 6TH STAGE BLADE FAILURE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080521 NM 2008 5 21 2008UALA02713 1 20080512 A 7930 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 552UA 26641 727201 LT ENGINE OIL FILTER MSG ON START. FOUND GEARBOX BEARING FAILURE. REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 2008 5 21 2008UALA02718 4 20080509 A 2565 LANYARD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 422UA 503 NO LANYARD VISIBLE ALL 4 DOOR SLIDES. REPOSITIONED LANYARD ON AL L SLIDES, OK FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080521 EU 2008 5 21 2008UALA02725 1 20080510 A 2700 3945122506 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELAC 1 FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 408UA 457 AIL SERVO FAULT, LAF DEGRADED L AIL AMBER HALF BOX B, R AIL AMBER HALF BOX G. REPLACED ELAC 1, ALL OPS TESTS WERE NORMA L. 2 L 7 2 4F 4 F RT A28NM E40NE 20080521 NM 2008 5 21 2008UALA02726 1 20080510 A 2150 3964622 CONTROL VALVE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE AIR CONDITIONER MALFUNCTIONED A UALA D RETURN TO BLOCK W INADEQUATE Q C IN INSP/MAINT 1 WP 29 673UA 29241 LEFT PACK WILL NOT TURN OFF. SUSPECT FAULTY FLOW CONTROL SHUTOFF VALVE. REPLACED LT PACK FLOW CONTROL AND SHUTOFF VAL VE. OPERATIONAL CHECK IS GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080521 EU 2008 5 21 2008UALA02733 1 20080510 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 469UA 1409 FOUND CREW OXYGEN LOW ON ECAM. SERVICED O2 TO FULL. NO LEAKS NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080521 NM 2008 5 21 2008UALA02747 1 20080509 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN UNSECURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 594UA 28145 EXIT PATH LIGHTING BY SEAT 13C IS PULLING AWAY FROM THE CARPET. SECURED EEL LIGHT COVER 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 NM 2008 5 21 2008UALA02754 1 20080510 A 2822 568129115004 PUMP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUEL SYSTEM LOW PRESSURE A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 798UA 26928 FUEL PUMP L FWD LEFT FORWARD (BOOST) FUEL PUMP SWITCH ON AND PUMP OUTPUT PRESSURE LOW. STATUS MSG01, LATCHED CRUISE MO DE DEPENDENT, L FWD FUEL BOOST PUMP PRESSURE SWITCH SIGNAL IS LOW WITH L FWD FUEL BOOST PUMP ON. DB- ELMS P310 ELECTRON ICS UNIT MSG-2813111 LATCHED ER MODE. REPLACED LOW PRESSURE S-W, NO HELP. L-FWD FUEL BOOST PUMP INOP. REPLACED BOOST PU MP AND DAMAGED HOUSING. TESTS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080521 EU 2008 5 21 2008UALA02756 1 20080512 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 464UA 1290 EMERGENCY LIGHT TEST FAILS PER "A" CHECK JOB CARD. "EPSU BATTERY EMER R" DISPLAYED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080519 NM 2008 5 19 AALA200800991 1 20080416 A 2913 PUMP BOEING 737 737823 13844BZ NM HYDRAULIC SYS INOPERATIVE A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 910AN 29512 BDL INFLIGHT T1966/16APR - CREW REPORTED LEFT ENGINE SYSTEM A HYDRAULIC PUMP LOW PRESSURE LIGHT CAME ON IN FLIGHT. LAN DED BDL WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE DRIVEN PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080519 NM 2008 5 19 KCSA081233 1 20080506 A 5210 DOOR FRAME BOEING 747 747212B 1384886 NM L1 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 L1 MAIN ENTRY DOOR FWD LOWER CORNER VERTICAL FRAME CRACKED IN RADIUS ADJACENT TO DOOR STOP FITTING, BS 441, WL-209. 2 L 7 4 4F RT A20WE 20080519 EU 2008 5 19 UPS08152168 1 20080502 A 5250 HANDLE AIRBUS A300 A300F4622R 3930360 EU EMERGENCY DOOR BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 156UP 0845 MAIN DECK (RIGID BARRIER DOOR) EMERGENCY ACCESS DOOR HANDLE IS BROKEN. DEFERRED RIGID BARRIER DOOR. LOCKED DOOR USING ALT METHOD PER MM 52-51-00. DEF 374910 ASSIGNED. REPLACED CARGO SLIDE LATCH HANDLE ON BARRIER DOOR PER 52-51-00 DEFERR AL CLEARED. 2 L 7 2 4F RT A35EU 20080519 EA 2008 5 19 MASA200800376 1 20080507 A 3350 BR9279013 CABLE ASSY CNDAIR CL600 CL6002B19 1900309 EA CABIN DEFECTIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27314 7314 ASH FLT 1019 KOA-HNL (RON) FLOOR EMERGENCY LIGHTS FROM ROW 2-6 ARE INOP. MX REPLACED EMERGENCY LIGHT CABLE ASSY, LIGHT S CHECK GOOD. 2 L 7 2 4F RT A21EA 20080519 EA 2008 5 19 MASA200800379 1 20080507 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY MALFUNCTIONED A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 77286 7286 FLT 2708, PHX-LAX - LAV SMOKE DETECTOR WILL NOT TEST. MX OP CHECKED SYSTEM NORMAL. 2 L 7 2 4F RT A21EA 20080519 EA 2008 5 19 MASA200800383 1 20080508 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 938LR 15038 ASH FLT 2652 CLT-RIC - CEILING EMERGENCY FLOOD LIGHT AT ROW 17 INOP. MX RELAMPED LIGHT. 2 L 7 2 4F RT A21EA 20080528 NM 2008 5 28 SWAA082753 1 20080520 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 520 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 10L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082743 1 20080520 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 616 S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082768 1 20080521 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 908WN 36620 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082784 1 20080522 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 704SW 27838 DURING SCHEDULED HC1 CHECK, AFT RT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082785 1 20080522 A 3350 MS155721 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 758SW 27873 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082731 1 20080519 A 5311 6546533 FRAME BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, BETWEEN LBL 1 AND RBL 4, WL 148. REPAIRED FRAME PE R SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082755 1 20080521 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 912 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 912, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 NWAA082196310 1 20080514 A 3320 SOCKET BOEING 747 747451 1384940 NM GALLEY LIGHT SMOKE A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 670US 24225 FLIGHT ATTENDANT REPORTED SMOKE IN FORWARD GALLEY AREA. FOUND SMOKE COMING FROM FLUORESCENT BULB ABOVE DOOR 1 RIGHT. T URNED OFF LIGHTS AND SMOKE DISAPPEARED FOR REMAINDER OF FLIGHT. MAINTENANCE REMOVED AND REPLACED LAMP SOCKET (M8301 MOD ULE) AND RELAMPED. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20080528 NM 2008 5 28 KNNA20080013 1 20080515 A 5330 SKIN BOEING 737 7372L9 1384497 NM BS 400-440 DENTED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 464AT 21278 FOUND SEVERAL DENTS ON FUSELAGE SKIN AROUND ALTERNATE STATIC PORT, RIGHT SIDE FROM STA 400 TO 440 AND STR 20R TO 24R. C UTOUT DAMAGE AND INSTALLED A REPAIR IAW SRM 53-30-3 FIG 46. 2 L 7 2 4F RT A16WE 20080528 WP 2008 5 28 IXXA08SMN181S 1 20080419 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LOWER LEADING EDGE HAS IMPROPER REPAIR AT STATION XFS 360.250. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECT ION. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-3-1, DC8 SRM 51-1-21, 51-1-20D, 51-3-0, DC8 ND T SPM PART 06-10-01-001, DC8 SRM 51-1-8B, FAA FORM 8110-3 NUMBER 08198 DATED 04-25-08, AND SEMAN DRAWING NUMBER ED-4773 DATED 04-22-08. 2 L 7 4 4F RT 4A25 20080528 EU 2008 5 28 NSVA2008031 1 20080520 A 3297 CONNECTOR SAAB SF340 340B 7860101 EU MLG LOOSE A NSVA O OTHER J WARNING INDICATION CL CLIMB 1 EA 27 350CJ 340B350 LANDING GEAR DOWN UNSAFE (LEFT) FOLLOWED CHECKLIST. NOSE AND RIGHT MAIN LIGHTS ILLUMINATED, NO LEFT MAIN AFTER EMERGENC Y RELEASE. REPLACED LIGHT BULBS RESET CB GEAR EXTENDED. INSTALLED GEAR PINS ON ALL GEAR. REMOVED AND REPLACED EXPLOSI VE BOLTS IAW WORKCARD 32-31-09S. TESTED LT AND RT EXPLOSIVE BOLT CIRCUITRY FOUND GOOD AFTER RESETTING CONNECTOR 3GBP1A IAW COLGAN WORKCARD 32-31-08S. PERFORMED GEAR SWINGS IAW AMM 32-30-00. NO DISCREPANCIES NOTED. 2 L 7 2 4T RT A52EU 20080528 WP 2008 5 28 IXXA08SMN167S 1 20080419 A 5340 FITTING DOUG DC8 DC871F 302199D WP BS 717 L19L CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT CUSP EXTRUSION UPPER SURFACE AFT FITTING CRACKED AT STATION 717.750 LONGER ON 19 LEFT. REMOVED CRACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CL EANED TREATED AND PRIMED FITTING AND AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-3-1, DC8 SRM 51-1-20D, DACO DPS 4.707, DC8 SRM 51-1-8B, ATI REPAIR SPECIFICATION NUMBER 2003-05, AND DOUGLAS DRAWING 3779978. 2 L 7 4 4F RT 4A25 20080529 NM 2008 5 29 08FDEA01858 1 20080516 A 5320 655624847 SUPPORT BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 274FE 22039 AFT CARGO COMPARTMENT AT BS 1105 UNDER STR 29R SHOWS CORROSION. FABRICATED NEW SUPPORT CHANNEL FOR STR 29R BS 1105 AND INSTALLED NEW CHANNEL IAW SRM 51-10-3, SRM 51-20- 01 FIG 3 AND DWG NR 65-56136, FABRICATED REPAIR DOUBLER, INSTALLED S HEAR TIE REPAIRS IAW SRM 53-10-4 FIG 11. ALL PARTS HEAT TREATED TO T6 CONDITION. 2 L 7 3 4F RT A3WE 20080529 EU 2008 5 29 08FDEA01908 1 20080520 A 5321 A2901115300100 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 815FD 638 MAIN WHEEL WELL CATWALK PANEL NR 148 BF IS DELAMINATED. MATERIAL ID IS A402H35039-003 PO 604814.1 IAW FEDEX DWG SRZ 25- 005, REV F. FABRICATED A NEW FLOOR PANEL AT THE MAIN WHEEL WELL CATWALK PANEL NR 148 BF USING THE OLD PANEL AS A TEMPLA TE IAW FEDEX DWG SRZ 25-005, REV F. MARKED PANEL NR 148 BF IAW FEDEX DWG SRZ 25-005, REV F AND GMM 7-0-1000. PANEL P ART ID IS FXA2901115300100. 2 L 7 2 4F RT A35EU 20080529 EU 2008 5 29 08FDEA01909 1 20080520 A 5321 A532B375200100 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 815FD 638 MAIN CABIN FLOOR PANEL AT FRAME 48 IS CRACKED AT RBL 57. MATERIAL ID IS A402H35039-003, PO 604814.1 IAW FEDEX DWG SRZ 2 5-005, REV F. FABRICATED NEW FLOORBOARD PANEL FOR THE MAIN CABIN AT FRAME 48 USING THE OLS PANEL AS A TEMPLATE IAW FEDE X DWG SRZ 25-005, REV F MARK PANEL NR 242AJ IAW FEDEX DWG SRZ 25-005, REV F AND GMM 7-0-1000. PANEL PART ID IS FX A532B 375200100. 2 L 7 2 4F RT A35EU 20080529 EU 2008 5 29 08FDEA01911 1 20080520 A 5321 A532B376600100 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 815FD 638 MAIN CABIN FLOOR PANEL AT FRAME 51, RBL 37 IS CRACKED. MATERIAL ID IS A402H35039-003, PO 604814.1 IAW FEDEX DWG SRZ 25- 005, REV F. FABRICATED NEW FLOORBOARD PANEL FOR THE MAIN CABIN FROM FRAME 51 TO FRAME 54 USING THE OLD PANEL AS A TEMPL ATE IAW FEDEX DWG SRZ 25-005, REV F. MARKED PANEL NR 252 EK IAW FEDEX DWG SRZ 25-005, REV F AND GMM 7-0-1000. PANEL PA RT ID IS FX R532B376600100. 2 L 7 2 4F RT A35EU 20080520 NM 2008 5 20 UPS08652189 1 20080429 A 5320 140T0130U39 ANGLE BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 329UP 27755 INSPECTION TYPE:C AFT CARGO COMPT STA 1085 LBL 26" BELOW FLOOR VERTICAL WEB ATT ANGLE CRACK, CRACK LENGTH 3/4 INCH. AFT CARGO COMPT STA 1085 LBL 26 INCHES VERTICAL WEB ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20080520 2008 5 20 08FDEA01818 2 20080511 A 7532 BLEED VALVE AIRBUS 310 A310 EU NR 2 FAULTED A FDEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 25 450FE 162 AT FL 370 BLEED VALVE NR 2 FAULTED. TURNED IT OFF AND OPENED BLEED CROSS FEED. APPROX 1 MIN LATER BLEED VALVE NR 1 FAU LTED. TURNED IT OFF, TRIED RESETTING AND WOULD NOT RESET. DURING DESCENT, NR 1 BLEED VALVE DID RESET. BY 10,000 BOTH BLEED VALVES RESET AND WORKED NORMALLY. CHECKED PNEUMATIC CONTROL SYSTEM IN REF TO AMM 21-31-00-5-01. NO FAULTS WHEN BITE CHECKING EITHER PNEUMATIC SYSTEM CONTROLLER. ALSO, AFTER DOING CHECKS ON MAINT PANEL NO FAULTS WERE NOTED AND ALL SYSTEMS CHECKED AS WORKING NORMALLY. 2 L 7 2 4F RT A35EU 20080520 EA 2008 5 20 MASA200800398 1 20080513 A 3250 TILLER CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING OUT OF ADJUST A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 47202 7202 ASH FLT 7245 ORD-TVC - NOSE WHEEL STEERING INOP MESSAGE IN FLIGHT, PILOT DECLARED EMERGENCY. CENTERED TILLER, OPS GOOD. 2 L 7 2 4F RT A21EA 20080520 EA 2008 5 20 MASA200800399 1 20080513 A 2510 TRACK CNDAIR CL600 CL6002B19 1900309 EA F/A SEAT LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75998 7336 ASH FLT 7117 IAD - CAE - FLT ATTENDANTS JUMP SEAT HARD TO STOW. MX INSPECTED SEAT, LUBED SEAT AND TRACKS AND CHECKED FOR PROPER OPERATION. SEAT OPERATES NORMALLY. 2 L 7 2 4F RT A21EA 20080520 NM 2008 5 20 UIEA200500168 1 20080505 A 5315 FLOORBEAM BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 COCKPIT STA 340 - 360 RIGHT SIDE OUTBOARD FLOORBEAM FOUND TO HAVE MINOR CRACK. WEB MINOR CRACK TRIMMED OFF PER SRM 51-1 0-01. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800171 1 20080505 A 2120 214U61101 DUCT BOEING 747 74747UF 1384812 NM CARGO BAY DAMAGED A UIEA I G B CABIN DEPRESSURIZATION O2 MASK DEPLOYED EMER. DESCENT O OTHER CL CLIMB 1 EA 15 499MC 29260 AFTER TAKEOFF UNABLE TO PRESSURIZE AIRCRAFT. FOUND CONDITIONED AIR CHECK VALVE CRACKED AND FOUND HOLE ON FORWARD CARGO COMPARTMENT AIR SUPPLY DUCT. REMOVED AND REPLACED CHECK VALVE AND ACCOMPLISHED LEAK CHECK IAW 21-28-08. AIR DUCT REMOV ED AND FORWARDED FOR REPAIR TO AVDUCT. RE-INSTALLED DUCT, LEAK CHECKED IAW 21-23-02. NO ABNORMALITIES. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800174 1 20080505 A 5210 DOOR FRAME BOEING 747 7472D7B 1384803 NM L5 DOOR DEFORMED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK 5L DOOR AFT UPPER EDGE FRAME FOUND DEFORMED. PERFORMED DOOR EDGE RE-WORK AS PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800176 1 20080502 A 3251 ACTUATOR BOEING 747 74747UF 1384812 NM STEERING SYS BURNED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 418MC 32840 DURING THE "A"4 CHECK PDU 6R STEERING ACTUATOR WAS DISCOVERED TO HAVE BURN MARKS. DEACTIVATED THE PDU AND PLACED ON DEF ERRAL. REF MEL 25-53-01 CAT D, DMI M08-036. THIS ITEM IS CONSIDERED OPEN UNTIL THE PDU IS REPLACED. 2 L 7 4 4F RT A20WE 20080520 CE 2008 5 20 DXTA200803046 1 20080506 A 3260 MS243311 UNLOCK SWITCH BEECH MU300 400A 1155402 CE COCKPIT INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 138QS RK492 AFTER TAKEOFF UPON GEAR RETRACTION, LANDING GEAR RED INTRANSIT LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED LT MAIN LANDING GEAR UPLOCK SWITCH P/N: MS24331-1. PERFORMED LANDING GEAR OPERATION CHECK. OP CHECKS GOOD. ALL MAINTENANCE PERF ORMED IAW MM 32-10-00, 32-30-00 AND 12-10-00. 2 H 7 2 4F RT A16SW 20080520 NM 2008 5 20 USAA920080990 1 20080506 A 5330 6545774 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 24515 CLT - MAJOR REPAIR - RON - CRACKED FUSELAGE SKIN, BS 727D, S24L. REPAIRED FUSELAGE SKIN, BS 727D, S24L IAW B737 SRM 53- 00-01 REPAIR 31 AND USAIRWAYS TYPICAL REPAIR 53-33. 2 L 7 2 4F RT A16WE 20080520 NM 2008 5 20 USAA920081000 1 20080502 A 5754 PANEL BOEING 737 7374B7 1384702 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 430US 24552 CLT - MAJOR REPAIR - C6 CHECK - RIGHT WING NR 5 SLAT COVE PANEL CRACKED. REPAIRED RIGHT WING NR 5 SLAT COVE PANEL IAW B 737 SRM 57-43-01. 2 L 7 2 4F RT A16WE 20080520 NM 2008 5 20 USAA920081009 1 20080505 A 5754 SKIN BOEING 757 7572B7 1384964 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937UW 27245 BFM - MAJOR REPAIR - C1 CHECK - LEFT WING NR 4 SLAT TRAILING EDGE LOWER SURFACE HAS AREA OF DELAMINATION. REPAIRED LEF T WING NR 4 SLAT TRAILING EDGE LOWER SURFACE HAS AREA OF DELAMINATION IAW B757 SRM 51-70-10. 2 L 7 2 4F RT A2NM 20080520 CE 2008 5 20 DXTA200803032 1 20080429 A 3240 651710214 MOTOR-BRAKE UNIT CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE FWD AVIONICS BAY INOPERATIVE E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 694QS 6179 5605194 (PWR BRAKES) CIRCUIT BREAKER POPPED RESULTING IN LOSS OF BRAKE PRESSURE. REPLACED HYD BRAKES POWER PACK AND HIGH PRESSU RE SWITCH, BLED BRAKES OPPS CHECKED SATISFACTORY. ALL WORK IAW MM 32-42-00. 2 L 7 2 4F 4 F RT A22CE E00059EN 20080520 CE 2008 5 20 DXTA200803033 1 20080430 A 3233 15500003 ACTUATOR CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE MLG INOPERATIVE E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 669QS 1262 5605689 AFTER SELECTING GEAR UP, THE LT MAIN GEAR INDICATION LIGHT REMAINED ILLUMINATED. REPLACED LT MAIN LANDING GEAR ACTUATOR IAW MM 32-30-04. OPS CHECK GOOD. LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 20080520 CE 2008 5 20 DXTA200803034 1 20080430 A 2170 COALESCER BAG RAYTHN 900 HAWKER900XP 4220011 CE GARRTT TFE731 TFE731* 01518 WP CABIN ODOR E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 889QS HA0021 DIRTY SOCK ODOR COMING FROM AIRSOURCE WEMACS IN FLIGHT, IN FLIGHT DECK AFTER APU WAS TURNED ON. INSTALLED NEW SOCK - LOW ERED LEFT AND RIGHT ENGINE OIL LEVELS. GROUND RUN APU & ENGINES NO ODOR NOTED WITH APU/ ENGINE BLEED AIR ON GROUND. REF MM 21-10-45 1 L 7 2 4F 4 F RT A3EU E6WE 20080520 CE 2008 5 20 DXTA200803035 1 20080430 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RT MLG WEAK E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 314QS 5600441 RT SEAT BRAKES ARE SPONGY. PERFORMED BRAKE BLEED ON BOTH BRAKES, NO LEAKS NOTED & BRAKES ARE GOOD REF CE560E 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 20080520 CE 2008 5 20 DJFA2008043 1 20080428 A 2910 O-RING CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C 03047 GL HYDRAULIC SYS RUPTURED E DJFA D RETURN TO BLOCK K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 EA 23 707LX 7500078 CREW REPORTED LOSS OF HYD PRESS AND SMOKE IN COCKPIT DURING TAXI. MAINTENANCE FOUND A HYDRAULIC LINE IN THE RT PYLON RU PTURED CAUSING HYD FLUID TO BE INGESTED IN THE RT ENGINE. FLUID MOVED THROUGH THE BLEED AIR SYS CAUSING SMOKE AND FOWL ODOR. MAINTENANCE REPLACED THE LT/RT COALESCER WATER SEPARATOR BAG’S REF: AMM 21-52-00. CLEANED AND INSPECTED HEAT EXCH ANGERS AND ACM PLUMBING AS REQUIRED. RAN APU WITH BLEED AIR ON HIGH HEAT AS NECESSARY FOR APPROX 3.0 HOURS WITH NO RESID UAL ODOR OF HYD FLUID REMAINING. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080520 NM 2008 5 20 UIEA200800186 1 20080514 A 5347 SEAT TRACK BOEING 747 7472D7B 1384803 NM FUSELAGE CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 CABIN AND FLIGHT DECK UPPER DECK STA 540 LBL 10 SEAT TRACK FOUND WITH MINOR CORROSION. CORROSION REMOVED AND RETREATED PER SRM 53-10-01 AND 51-10-02. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800190 1 20080513 A 5210 DOOR FRAME BOEING 747 7472D7B 1384803 NM R5 DOOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK R5 DOOR FORWARD LOWER CORNER EDGE FRAME FOUND CRACKED. CRACKED AREA REPAIRED PER SRM 52-10-02. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800191 1 20080513 A 5315 FLOORBEAM BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 FWD CARGO STA 640 LBL 20 FLOORBEAM UPPER CHORD FOUND CRACKED. FWD CARGO STA 640 LBL 20 FLOORBEAM UPPER CHORD CRACKED AR EA REPAIRED AS PER SRM 51-40-04. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800193 1 20080512 A 5347 SEAT TRACK BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK STA 1770 LBL 75 SEAT TRACK FOUND CRACKED. SEAT TRACK REPAIRED PER SRM 53-10-05. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 F3LA200800262 1 20080425 A 5313 D53571532224 STRINGER AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED STRINGER 32 RIGHT IS DAMAGED BETWEEN FRAME 72 AND THRU FRAME 74. MAINTENANCE REPLACE D THE STRINGER SECTION FROM AFT BULKHEAD TO FRAME 72 IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30262. UPON COMPL ETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080520 SO 2008 5 20 LR7A08056 1 20080513 A 5315 3938631 FLOORBEAM LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK, FOUND COCKPIT FLOORBEAM EXFOLIATION CORROSION AT FS 196, WL196, RBL30. REPAIR ACCOMPLISHED BY FABRICATING AND REPLACING SPLICE CAP IAW SMP583 FIG 51-60 AND 51-70 AND DWG 393863-1. 2 H 7 4 4T A1SO 20080520 SO 2008 5 20 LR7A08060 1 20080513 A 5312 3707846 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CHAFED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5324, FOUND RT MWW BULKHEAD FRAME CHAFED AT FS 477, WL176-200, RBL61.62-76. R EPAIR ACCOMPLISHED BY REPLACING BULKHEAD IAW SMP583 CHAP 51-60 AND 51-70 AND DWG 370784. 2 H 7 4 4T A1SO 20080520 WP 2008 5 20 RYNA200800020 1 20080417 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 932RD 49233 PASSENGER CABIN RIGHT INBOARD SEAT TRACK IS CORRODED AT BS 1078. REPAIRED CORRODED AREA IAW MD-80 SRM 51-10-03. 2 L 7 2 4F A6WE 20080520 2008 5 20 2008UALA02682 4 20080506 A 2565 69451433 WINDOW BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE SLIDE GAUGE MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 AFT GALLEY DOOR SLIDE MISSING PRESS GAUGE WINDOW. NEW WINDOW INSTALLED PER GNMM 6-0-2-50.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 20080521 NM 2008 5 21 2008UALA02724 1 20080510 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 L-2 DOOR LOWER GATE HAS ELONGATED AND OVERSIZE HOLES FROM RUB STRIP MOUNTING. WELDED LOWER GATE AND INSTALLED RUB STRIP . 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 NM 2008 5 21 2008UALA02744 1 20080510 A 2611 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SMOKE DETECTOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 539UA 25223 "R" LAV SMOKE DETECTOR RESET SWITCH BAD. REPLACED "R" LAV SMOKE DETECTOR., OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 NM 2008 5 21 2008UALA02771 1 20080510 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW O2 LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 827UA 1022 O2 LOW READS 1370. 2 L 7 2 4F 4 F RT A28NM E40NE 20080521 SO 2008 5 21 LR7A08070 1 20080513 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5313, FOUND RT CABIN BULKHEAD CRACKED AT FS 597, WL280, RBL61.5. REPAIR ACCOM PLISHED IAW LAC MEA 382-53-04-071 R1. 2 H 7 4 4T A1SO 20080521 SO 2008 5 21 LR7A08071 1 20080513 A 5320 BEAM LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5324, FOUND RT UPPER MWW ARMPIT PANEL BEAM CRACKED AT FS 522. REPAIR ACCOMPLI SHED IAW LAC MEA 382-53-08-021 AND MEA 382-53-08-022. 2 H 7 4 4T A1SO 20080521 NM 2008 5 21 F3LA200800265 1 20080425 A 5313 D53571532235 STRINGER AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED STRINGER 33 LEFT IS DAMAGED BETWEEN FRAME 72 THRU FRAME 74. MAINTENANCE REPLACED STR INGER SECTION IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30262. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AN D FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080521 NM 2008 5 21 AALA200801019 1 20080420 A 2450 CIRCUIT CARD BOEING 777 777223 1385213 NM FAULTY A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 767AJ 33539 ORD INFLIGHT T50/20APR DFW TO LHR - CREW REPORTED NUMEROUS STATUS MESSAGES. DECLARED EMERGENCY AND LANDED ORD WITHOUT I NCIDENT. REPLACED BOTH 629 ARINC LEFT CARDS IN LEFT AND RIGHT SYSTEM CARD FILES. SYSTEM GROUND CHECKED NORMAL OPERATIO N. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801030 1 20080421 A 3350 0201984001 LENS BOEING 767 767223 1385123 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 332AA 22331 JFK - EMERGENCY FLOOD LIGHT AT FORWARD GALLEY NEAR RIGHT NUMBER ONE DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY FLO OD LIGHT AT FORWARD GALLEY NEAR RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080521 NM 2008 5 21 AALA200801008 1 20080418 A 2560 TAB BOEING 737 737823 13844BZ NM FLASHLIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 917AN 29518 MIA - EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR TAMPER TAB MISSING. REPLACED TAMPER TAB FOR EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 WP 2008 5 21 AALA200801010 1 20080418 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 483A 49676 LGA - EMERGENCY LIGHTS AT TAIL COMPARTMENT INOPERATIVE. RESEATED BATTERIES AT AFT RIGHT LAVATORY FOR EMERGENCY LIGHTS I N TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080521 NM 2008 5 21 AALA200801011 1 20080418 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 347AN 33086 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 34H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 34H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080521 NM 2008 5 21 AALA200801022 1 20080420 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 DFW - EMERGENCY LIGHT AT SEAT 13G FORWARD POSITION INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 13G FORWARD POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801023 1 20080420 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 DFW - EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 BEFA200800001 1 20080404 A 5315 FLOORBEAM BOEING 757 757200 1384950 NM PWA 2037 PW2040 NE BS 1720 CORRODED A BEFA K NONE O OTHER IN INSP/MAINT 1 WP 19 741PA 55899 24737 BULK CARGO AFT SECTION CABIN FLOOR, ANGLE SUPPORT AT STATION 1720 LBL 35 INCHES, HAS CORROSION. CORROSION WAS OUT OF LI MITS IAW SRM. NEW ANGLE HAD TO BE FABRICATED, HEAT TREATED, PRIMED, AND INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 NM 2008 5 21 AALA200801033 1 20080421 A 3350 LIGHT BOEING 737 737823 13844BZ NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976AN 30099 DFW - EXTERNAL EMERGENCY LIGHT AT FORWARD LEFT OVERWING INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT FORW ARD LEFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 NM 2008 5 21 AALA200801035 1 20080421 A 3350 LIGHT BOEING 737 737823 13844BZ NM COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976AN 30099 DFW - EMERGENCY LIGHT IN COCKPIT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN COCKPIT. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A16WE 20080521 EU 2008 5 21 08FDEA01853 1 20080515 A 5315 A53274929202 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 MAIN DECK CARGO FLOORBEAM FR 60 BETWEEN SEAT TRACKS NR 2 RT AND NR 3 RT HAS CORROSION ON CLS ADAPTER REMOVED LEVEL 1 COR ROSION, REPAIRED BENT FLOORBEAM AND REPLACED CLS ADAPTER AT FR 60 BETWEEN SEAT TRACK NR 2 RT AND NR 3 RT IAW A300-600 SR M 53-10-15, FIG 205. 2 L 7 2 4F RT A35EU 20080521 EA 2008 5 21 MASA200800401 1 20080515 A 5210 MOTOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7264V 7264 ASH FLT 2838, PHX-BUR - PAX DOOR POWER ASSIST MOTOR INOP. RESET C/B. 2 L 7 2 4F RT A21EA 20080521 NM 2008 5 21 MASA200800371 1 20080429 A 2530 270023 ANGLE DHAV DHC8 DHC8202 2809007 NM GALLEY CORRODED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 455YV 455 FOUND CORROSION DAMAGE ON LOWER SHELF ANGLES LOCATED INSIDE GALLERY. REPLACED ANGLES 3 EACH. 2 H 7 2 4T RT A13NM 20080521 EA 2008 5 21 MASA200800391 1 20080511 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 518LR 10259 ASH FLT 7155 SYR-IAD - PILOT REPORTED THAT THE FAR AFT EMERGENCY CEILING LEVEL FLOOD LIGHT WAS INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20080521 NM 2008 5 21 F3LA200800272 1 20080504 A 5280 NSA813710 BEARING AIRBUS A319 A319111 3930336 NM RT MLG DOOR LOOSE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED RIGHT MAIN LANDING GEAR DOOR HINGE SPHERICAL BEARING IS LOOSE IN THE HOUSING. MAINTE NANCE INSTALLED REPAIR SLEEVE AND NEW BEARING IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-52R-30264. UPON COMPLETION O F THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20080529 EU 2008 5 29 08FDEA01912 1 20080520 A 5321 A532B88300200 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 815FD 638 THERE IS A BROKEN FLOOR PANEL FOR THE MAIN CARGO DECK FROM FRAME 66 TO 67; LBL 57 TO LBL 71. MATERIAL ID IS A402H35039 -003, PO 604814.1 IAW FEDEX DWG SRZ 25-005, REV F. FABRICATED A NEW FLOOR PANEL FOR THE MAIN CABIN FROM FRAME 66 TO FRA ME 67 USING THE OLD PANEL AS A TEMPLATE IAW FEDEX DWG SRZ 25-005, REV F. MARKED PANEL NR 251 BH IAW FEDEX DWG SRZ 25-00 5, REV F AND FEDEX GMM 7-0-1000. PANEL PART ID IS FXR 532B88300200. 2 L 7 2 4F RT A35EU 20080529 WP 2008 5 29 08FDEA01864 1 20080516 A 5420 AUB710746N FAIRING DOUG MD10 MD1010F 3022112 WP ZONE 400 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 567FE 46994 NR 3 PYLON STRINGER FAIRING NR 489 AL LOWER FRAME HAS MULTIPLE DRILLED HOLES ON BOTH SIDES. REPLACED FAIRING NR AUB 710 7-46, PO 619490.1 IAW DAC DWG 6 NR AUB 7107, REV "P". 2 L 7 3 4F RT A22WE 20080529 WP 2008 5 29 08FDEA01865 1 20080516 A 5420 AUB710746 FAIRING DOUG MD10 MD1010F 3022112 WP ZONE 400 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 567FE 46994 NR 3 PYLON STRINGER FAIRING NR 489 A, LOWER SECTION OF THE FAIRING IS DELAMINATED AND COMING APART. FAIRING 489 AL WAS REPLACED ON FEDEX N/R N00610. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA01867 1 20080516 A 5315 57156221 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 220FE 20934 BS 1148 FLOORBEAM UPPER T-CAP, AFT FLANGE LWR SURFACE IS CORRODED, RBL 43 BLENDED CORROSION, ROTO- PEENED BLENDED AREA, ALODINED AND PRIMED AND APPLIED BMS 3-23, REF EA 7-5310-118266. ORIGINAL THICKNESS OF .130 INCH, .109 INCH REMAINING A T DEEPEST AREA. THIS IS CLASSIFIED AS A MINOR REPAIR. LEVEL 1 CORROSION. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 UIEA200800216 1 20080520 A 3240 215152 BRAKE BOEING 747 74747UF 1384812 NM MLG FIRE A UIEA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 EA 15 492MC 29253 NR 1 BRAKE CAUGHT FIRE AFTER AIRCRAFT ON BLOCKS. FIRE EXTINGUISHED IMMEDIATELY, NO MORE THAN 10 SECONDS. BRAKE TEMP IN NORMAL BAND 3 UNITS. OVERHEAT INSPECTION CARRIED OUT IAW MM TASK 5-51-10-202-001 AS A PRECAUTION ONLY. REF LOG PAGE 3 73339 FOR BRAKE AND WHEEL CHANGE. 2 L 7 4 4F RT A20WE 20080529 NM 2008 5 29 08FDEA01602 1 20080425 A 5313 65168124 STRINGER BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 203FE 22925 LWR FUSELAGE AFT PIT CORROSION ON 29L OUTBRD SIDE AND STA 1010 CLEANED AND EVALUATED AREA, NO CORROSION FOUND IAW B727 S RM 51-10-01 AND SOPM 20-30-03. 2 L 7 3 4F A3WE 20080529 NM 2008 5 29 08FDEA01877 1 20080516 A 3230 LANDING GEAR DOUG MD11 MD11F 3023600 NM MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 594FE 48552 AFTER TAKEOFF RIGHT MAIN LANDING GEAR INDICATED UNSAFE AFTER RETRACTION ON BOTH THE LANDING GEAR INDICATOR AND ON THE SY NOPTIC DISPLAY. COMPLIED WITH QRH WHICH CALLED FOR ONE RECYCLING OF THE LANDING GEAR. IT WAS SUCCESSFUL , 2 L 7 3 4F RT A22WE 20080529 EU 2008 5 29 08FDEA01984 1 20080525 A 5315 A53779635200 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 423FE 281 MAIN CARGO DECK THRU FWD CARGO COMP CEILING FLOORBEAM HAS .250 INCH CRACK ON VERTICAL STIFFENER BETWEEN SEAT TRACKS NR 4 LT AND NR 5 LT AT FR 36 CUT OUT DAMAGE AND INSTALLED CROSSBEAM REPAIR AT FR 36 BETWEEN SEAT TRACKS NR 4LT AND NR 5LT IA W A310-200 SRM 53-10-15, FIG 206, PAGE 231/232. 2 L 7 2 4F RT A35EU 20080529 NM 2008 5 29 08FDEA01986 1 20080527 A 5340 69473751 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 FWD PIT BILGE BODY FRAME STRINGER CLIP IS MISDRILLED BS 720, STR 26L. INSTALLED STRINGER CLIP AT STA STA 720, STR 26L R EF SRM 51-30-02. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01987 1 20080527 A 5330 691487112 ANGLE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 CORROSION ON SKIN ATTACH ANGLE IN C-1 PIT, FS 700, BL 0, WL 148 REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRIC ATED REPLACEMENT ANGLE FROM 7075- T6, .040' REF BOEING DWG 69-14871 AND PRINT NR 65-15938. REMOVED OLD ANGLE REF SRM 51-10-2 AND MM 51-30-0, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01862 1 20080516 A 5330 65175291 SKIN BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 274FE 22039 SKIN OIL CANNED LEFT FUSELAGE STA 1243 STR 18L TO 19L. CUT OUT DAMAGED AREA APPROX DIM 3 7/8 BY 1 7/8, FABBED REPAIR DO UBLER FROM 2024- T3 .063 PO NR 9006713 APPROX DIM 13 3/4 BY 8 1/2 AND INSTALLED REPAIR DOUBLER AT BS 1243 STR 18-19 LEF T IAW B727 SRM 53-30-3 FIG 3 AND SRM 53-30-2 FIG 3 AND SRM 51-30-2. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01999 1 20080527 A 5311 65469521 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 AFT PIT BILGE BODY FRAME UPPER FLG IS BUCKLED/CORRODED BS 1050, STR 26L-28L, WL 148 (MKD). REMOVED CORROSION ON AFT PI T BILGE BODY FRAME UPPER FLG STA 1050 STR 26L 28L WL148. ORIGINAL THICKNESS IS .063 REMAINING MATERIAL IS .061, .002 RE MOVED FOUND TO BE IN LIMITS, TREAT, PRIMED. REMOVED BUCKLED AREA OF FRAME. FABRICATED TREATED, PRIMED AND INSTALLED RE PAIR DOUBLER REF SRM 51-40-3 FIG 1, SRM 53-10-1 PG 1 DETAIL I. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01859 1 20080516 A 5330 65175291 SKIN BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 274FE 22039 SKIN BULGE LT FUSELAGE STA 1323 ABOVE STRL 18. CUTOUT DAMAGED AREA APPROX 2 7/8 INCH BY 2 INCH IAW B727 SRM 53-30-3 FIG 14, FABRICATED DOUBLER REPAIR MATERIAL 2024-T3 .063 PO NR 9006773 DIM 11 INCH BY 10 INCH FILLER MATERIAL 2024-T3 .050 P O NR 9006742 DIM 2 INCH BY 1 INCH AND STRUCTURAL FILLER MATERIAL 2024-T3 .050 PO NR 9006742 DIM 2 INCH BY 13 1/4 INCH IA W SRM 53-30-3 FIG 14 AND 53-30-2 FIG 3. INSTALLED REPAIR PARTS ON LT FUSELAGE STA 1323 STR 18 IAW SRM 51-30-2 AND 53-30 -3 FIG 14. 2 L 7 3 4F RT A3WE 20080529 EU 2008 5 29 08FDEA01918 1 20080520 A 5321 A532B382900200 FLOOR PANEL AIRBUS 310 A310 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 815FD 638 THERE IS A BROKEN FLOOR FLOOR PANEL FOR THE MAIN CARGO DECK FROM FRAME 62 TO FRAME 65, RBL 57 TO RBL 74. MATERIAL ID IS A402H35039-003, PO 604814.1 IAW FEDEX DWG SRZ 25-005, REV F. FABRICATED A NEW FLOOR PANEL FOR THE MAIN CARGO DECK FROM FRAME 62 TO FRAME 65 USING THE OLD PANEL AS A TEMPLATE IAW FEDEX DWG SRZ 25-005, REV F. MARKED PANEL NR 252 YG IAW FE DEX DWG SRZ 25-005, REV F AND GMM 7-0-1000. PANEL PART ID IS FXR532B382900200. 2 L 7 2 4F RT A35EU 20080529 EU 2008 5 29 08FDEA01920 1 20080520 A 5321 A32B388400100 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 815FD 638 THERE IS A BROKEN FLOOR PANEL FOR THE MAIN CARGO DECK FROM FRAME 67 TO FRAME 69, RBL 54 TO RBL 72. MATERIAL ID IS A402H 35039-003, PO604814.1 IAW FEDEX DWG SRZ 25-005, REV F. FABRICATED A NEW FLOOR PANEL FOR THE MAIN CARGO DECK FROM FRAME 67 TO FRAME 69 USING THE OLD FLOOR PANEL AS A TEMPLATE IAW FEDEX DWG SRZ 25-005, REV F. MARKED PANEL NR 251 BH IAE FEDE X DWG SRZ 25-005, REV F AND GMM 7-0-1000. PANEL PART ID IS FXR532B388400100. 2 L 7 2 4F RT A35EU 20080529 NM 2008 5 29 08FDEA01943 1 20080521 A 5320 652954832 PAN BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 AFT MAIN DECK FLOOR DITCHING PAN ASSY IS CRACKED BS 1176 - 1183, LBL 27 - 37, WL 208. REPLACED DITCHING PAN AT STA 117 6 - 1183, LBL 27 - 37, WL 208 REF BOEING DWG 65-29548 AND SRM 51-30-2 AND 51-30-2 PG 1-10. THIS IS CLASSIFIED AS A MINO R REPAIR. 2 L 7 3 4F RT A3WE 20080520 NM 2008 5 20 UIEA200800179 1 20080509 A 5730 SKIN PANEL BOEING 747 747228F 1384895 NM RT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 RT WING UPPER FIXED TRAILING EDGE PANEL HAS COMPOSITE CRACK, 3.5 INCHES FROM FORWARD EDGE OF PANEL AT WBL STA 515. PERM ANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 2, SHEET 1, 2 AND 5 PREPREG 250 DEGREES CURE PER SRM 51-40-1 2. REF: ATLAS AIR EO NR 4757A440. 2 L 7 4 4F RT A20WE 20080520 NE 2008 5 20 UIEA200800183 2 20080508 A 7321 8062291 MEC BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE NR 1 ENGINE FAILED A UIEA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 15 506MC 21252 517579 INFLIGHT ENGINE SHUTDOWN. AT TOD, DURING ENGINE THROTTLE BACK NR 1 ENGINE ROLLED BACK DOWN TO 30 PERCENT N1 WITH NO THR OTTLE RESPONSE. CREW SHUT DOWN ENGINE AND PERFORMED INFLIGHT RE-START. AFTER SUCCESSFUL RE-START THERE WAS STILL NO TH ROTTLE RESPONSE ABOVE 50 PERCENT N1. MAINTENANCE REPLACED THE MEC AND FUEL PUMP PER 73-11-01 AND 73-21-01. 2 L 7 4 4F 4 F RT A20WE E23EA 20080520 CE 2008 5 20 DXTA200803044 1 20080505 A 2120 38007221 APU CESSNA 560 560XL 2076702 CE APU BAY LEAKING E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 592QS 615 5605706 ON THE GROUND WITH THE APU RUNNING FOR SEVERAL MINUTES, SECONDS AFTER SWITCHING BLEED AIR ON, SMOKE STARTED COMING INTO THE CABIN FROM ALL WEMACS VENTS. REPLACED APU IAW 560XL MM CH 49-10-00 SERVICED OIL RAN LK AND OPS CK GOOD. OLD APU SE RIAL P-638 TSN HOURS 615.2 AND CSN 1125, NEW APU SERIAL P-324 TSN HOURS 3044.9 CSN 4801. UNIT REPAIRED IAW 560XL MM 49- 10-00. APU WITH 2380 ENGINE OIL 2 L 7 2 4F RT A22CE 20080520 NM 2008 5 20 USAA920081011 1 20080506 A 5330 6545775 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 PHX - MAJOR REPAIR - DAILY CHECK - CRACKED FUSELAGE SKIN, BS 727E, S24R. REPAIRED FUSELAGE SKIN, BS 727E, S24R IAW B737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 20080520 WP 2008 5 20 ABXA080149 1 20080430 A 5330 59114103 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 DURING LINE MAINTENANCE WHILE CHANGING THE LEFT STATIC PORT PLATE, FOUND THE SKIN UNDER THE STATIC PORT PLATE CRACKED AP PROXIMATELY 1/2 INCH LONG BETWEEN LONGERONS 23 LEFT - 24 LEFT. REPAIRED AREA IAW DC9 SRM 53-04, FIGURE 12C. 2 L 7 2 4F A6WE 20080520 NM 2008 5 20 UIEA200800202 1 20080507 A 5210 SKIN BOEING 747 7472D7B 1384803 NM L4 DOOR DEFORMED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK L4 DOOR FORWARD LOWER CORNER EXTERNAL SKIN FOUND DEFORMED. L4 DOOR EXTERNAL SKIN REPAIRED AS PER SRM 51-10-01 . 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800204 1 20080510 A 5730 ACCESS DOOR BOEING 747 7472D7B 1384803 NM LT WING CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 NR 1 MAIN TANK ACCESS DOOR 552CB CUT OUT LOWER SURFACE CORROSION EVIDENT. BLENDED OUT CORROSION IAW SRM 57-30-03 AND RE PROTECTED AREA IAW SRM 51-10-02. 2 L 7 4 4F RT A20WE 20080520 NM 2008 5 20 UIEA200800207 1 20080511 A 5310 REVEAL BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK L4 DOOR CUTOUT FORWARD LOWER REVEAL PANEL FOUND CRACKED. REVEAL CRACKED AREA REPAIRED PER SRM 53-10-04. 2 L 7 4 4F RT A20WE 20080520 SO 2008 5 20 LR7A08055 1 20080513 A 5315 3725133 FLOORBEAM LKHEED 382 382G 526414U SO FUSELAGE CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK, FOUND COCKPIT FLOORBEAM EXFOLIATION CORROSION AT FS 196-216, WL196, LBL30. REPAIR ACCOMPLIS HED BY CUTTING OUT CORROSION AREA AND SPLICED IAW SMP583 FIG 51-140-22. 2 H 7 4 4T A1SO 20080520 SO 2008 5 20 LR7A08062 1 20080513 A 5230 3536075XX SUPPORT LKHEED 382 382G 526414U SO CARGO DOOR CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5211, FOUND RAMP DOOR LEADING EDGE WELL INTERGRANULAR CORROSION AT RS0.0, LBL6 2-RBL62, WL144. REPAIR ACCOMPLISHED BY REMOVING CORROSION AND REPLACING SUPPORTS P/N 353607-51, -52L, -53R IAW SMP583 C HAP 51-60 AND 51-70 AND DWG 353607. 2 H 7 4 4T A1SO 20080520 NM 2008 5 20 2008UALA02656 1 20080507 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 CORROSION ON SHEAR TIE AT STA 1241, STR 38 TO 39L. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080520 NM 2008 5 20 2008UALA02659 1 20080507 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 CORROSION UNDER NUTPLATE ON THE UNDERSIDE OF THE BILGE FRAME T-CAP AT BS 1197+132, LBL 18. MAJOR REPAIR ACCOMPLISHED: RE MOVED CORROSION. INSTALLED STRAP & ANGLE REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20080520 NM 2008 5 20 2008UALA02663 1 20080507 A 7930 OIL FILTER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT ENGINE FALSE ACTIVATION A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 798UA 26928 L ENG OIL FILTER STATUS MESSAGES. REPLACED MAIN OIL FILTER. NO SLUDGE OR CONTAMINATION NOTED, CHECKED MASTER CHIP DETEC TOR, NOTHING FOUND. RAN ENGINE, CLEARED MESSAGE, NO FURTHER ANOMALIES NOTED. NO LEAKS NOTED AFTER ENGINE RUN. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080520 NM 2008 5 20 2008UALA02530 1 20080429 A 3510 MC1019101 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 545UA 25323 OXYGEN MASK HOSE DEFECTIVE AT 2 (1=CAPT, 2=1ST OF, 3= 1ST OBS). CREW COMMENTS, HEADBAND HAS A HOLE IN IT. SUPPLEMENTAL DATA UPDATE, UNKNOWN DAMAGE. REPLACED O2 MASK ASSY-FO. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 NM 2008 5 21 2008UALA02727 1 20080510 A 3210 161T13103 BRACKET BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT MLG BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 663UA 27160 ON WALK AROUND, FOUND FRONT END OF LT GEAR BOGIE LOWER TRAY DAMAGED 4 RIVETS BROKEN AND 1 INCH CRACK ON MOUNTING BRACKET , BRACKET BEND. INSTALLED NEW FWD MOUNT BRACKET AND STRAIGHTENED LOWER TRAY. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080521 NM 2008 5 21 2008UALA02746 1 20080510 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 563UA 26665 BOTH 2 AND 3 DOOR EXTERIOR EMERGENCY LIGHTS INOP. RELAMPED, ALL LIGHTS WORK AS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 NM 2008 5 21 2008UALA02755 1 20080512 A 3320 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN ODOR A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 812UA 850 PAXS - FA SMELL ELEC BURN ODOR MID CAB MOVING FWD, ISOLATED TO READ LTS 18ABC TURNED OFF, SMELL STOPPED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080521 NE 2008 5 21 2008UALA02768 2 20080512 A 7200 FMU BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 1 ENGINE MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 674UA 29242 SLOW TO SPOOL TO IDLE ON NR 1 ENG, WHEN EEC CHANNEL 'B' WAS IN CONTROL. REPLACED THE FUEL METERING UNIT (FMU). 2 L 7 2 4F 4 F RT A1NM E24NE 20080521 SO 2008 5 21 LR7A08067 1 20080513 A 3010 37091111 SUPPORT BRACKET LKHEED 382 382G 526414U SO LT WING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5711, FOUND LT OW LEADING EDGE DIFFUSER P/N 370911-11 SUPPORT BRACKET CRACKED AT OWS54. WELD REPAIR ACCOMPLISHED IAW LAC MEA 382-30-08-025. 2 H 7 4 4T A1SO 20080521 SO 2008 5 21 LR7A08068 1 20080513 A 3010 351783 SUPPORT BRACKET LKHEED 382 382G 526414U SO LT WING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5711, FOUND LT OW LEADING EDGE ANTI-ICING DIFFUSER SUPPORT BRACKET CRACKED P/N 351783 OWS205-255. WELD REPAIR ACCOMPLISHED IAW LAC MEA 382-30-08-029. 2 H 7 4 4T A1SO 20080521 NM 2008 5 21 AALA200801009 1 20080418 A 5313 146T0220 STRINGER BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 357AA 24038 AFW - FUSELAGE STRINGER 35L AT STATION 1307 HAD CORROSION. REPAIRED FUSELAGE STRINGER 35L AT STATION 1307 PER MRB 767 3 181 DATED 08 APR 2008. 2 L 7 2 4F RT A1NM 20080521 NM 2008 5 21 AALA200801032 1 20080421 A 3397 0201875001 WIRE HARNESS BOEING 737 737823 13844BZ NM CABIN FAULTY A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 976AN 30099 DFW - EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPLACED WALL TO SEAT HARNESS FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 CE 2008 5 21 CWQR200803 1 20080417 A 2710 666000212 CONTROL CABLE CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE AILERONS IMPROPER PART B DXTA K NONE O OTHER IN INSP/MAINT 1 GL 05 679QS 5605279 DURING A ROUTINE CABLE REPLACEMENT OF AILERON CABLE PN 6660002-12, WE FOUND THAT THE CABLE HAD A SWAGED BALL AND A CLEVI S END INSTALLED. THIS CABLE ASSY SHOULD HAVE BEEN MANUFACTURED WITH THE SWAGED BALL WITHOUT THE CLEVIS. THE CABLE ASSY H AS BEEN SENT BACK TO MFG FOR EVALUATION. AN SCR AND PHOTO HAS BEEN SUBMITTED TO MFG UNDER NR 354900. 2 L 7 2 4F 4 F RT A22CE E00059EN 20080521 EU 2008 5 21 08FDEA01854 1 20080515 A 7830 1477M42P01 SPAR AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 NR 2 ENGINE OUTBD T/R UPPER FWD SPAR HAS 3 INCH CRACK REPAIRED NR 2 ENGINE OUTBD T/R IAW FEDEX EA 6-7830-121264, RELEASE DATE 30 APRIL, 2008. 2 L 7 2 4F RT A35EU 20080521 NM 2008 5 21 F3LA200800267 1 20080515 A 5311 D53571553202 FRAME AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED FRAME 74 DAMAGED FROM STRINGER 26 LEFT TO STRINGER 26 RIGHT. MAINTENANCE REPAIRED FR AME IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30262 AND SRM 51-42-11 PARAGRAPH 6. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080521 NM 2008 5 21 2008UALA02523 1 20080429 A 3397 90085 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY EXIT LIGHTING TURNED ON MID FLIGHT ROWS 6-8. SUSPECT LOOSE CONNECTION. SECURED CONNECTION AT BATTERY PACK OP CHECK OK. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080521 2008 5 21 2008UALA02648 4 20080506 A 2565 D31393110 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OVERWING EXIT OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 RT OVERWING SLIDE PACK FOUND UNLEASHED. SUPPLEMENTAL DATA UPDATE, UNKNOWN DAMAGE. REPLACED SLIDE PACK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 EU 2008 5 21 2008UALA02668 1 20080507 A 3350 20131A BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 485UA 1617 EMERGENCY LIGHTS WILL NOT PASS SYSTEM TEST. "EPSU BATTERY AFT L" MESSAGE. REPLACED BATTERY. TESTS OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080521 2008 5 21 2008UALA02670 4 20080507 A 2397 4251Y22 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE INTERPHONE SYS SHORTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 518UA 24871 INTERPHONE SYSTEM HOT TO FLIGHT DECK FROM ALL THREE FLIGHT ATTENDANT POSITIONS. WIRES SHORTED AT 4251Y-22 AND 4251G-22 AT PARTITION DOOR 1 LEFT HANDSET CONNECTOR D939. REPAIRED AND SOLDERED 4251Y-22 AND 4251G-22 AT PARTITION DOOR 1 LEFT H ANDSET CONNECTOR D939. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 NM 2008 5 21 2008UALA02671 1 20080418 A 2711 CONTROL MODULE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AILERON TRIM MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 29 545UA 25323 RUDDER TRIM INOP INTERMITTENT. PER CREW INBOUND CREW, AC REQUIRED FREQUENT RETRIMMING AND AT TIMES, RUDDER TRIM WOULD B E INOP AND OTHERS IT WOULD TRIM NORMALLY, ALL AT CRUISE. OCCURRED ON THE GROUND AS WELL AFTER ARRIVAL. SUSPECT INTERMIT TENT TRIM COMMAND FROM CONTROL PANEL. PRIOR TO REPLACING CONTROL PANEL, ATTEMPT (CONT). INTERMITTENT TRIM CONTROL MODU LE, NO SHOP DATA. REPLACED AILERON AND TRIM CONTROL MODULES, ALL OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 2008 5 21 2008UALA02672 4 20080507 A 2565 STRAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 579UA 26697 STRAP HANGING OUT OF SLIDE PACK AT 2L. SECURED D-RING STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 NM 2008 5 21 2008UALA02683 1 20080506 A 2597 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAVATORY MISLOCATED A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 539UA 25223 LAV "A" WIRE BURNED AT TOP OF VANITY LIGHT ASSY, HAS CHAFED WIRES, 1 SCREW MISSING FROM ASSY BASE. WIRES MISLOCATED, IN STALLED IMPROPERLY. REPLACED WIRES. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 CE 2008 5 21 DXTA200803064 1 20080517 A 3240 BRAKE SYS CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE MALFUNCTIONED E DXTA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 302QS 5600402 ON TAXI OUT BOTH PILOT AND CO-PILOT BRAKES WERE VERY HARD DURING APPLICATION, WHEN BRAKES WERE APPLIED (CO-PILOT OR PILO T), AIRCRAFT WOULD NOT SLOW UNTIL A GREAT DEAL OF PRESSURE WAS APPLIED. SUSPECTED AIR IN SYSTEM, BLED LEFT & RIGHT BRAK ES SEVERAL TIMES & PERFORMED SEVERAL OPS CHECKSOF LEFT & RIGHT SIDE PEDALS WITH NO DEFECTS IAW BRAKE BLEEDING PROCEDURE REVISED MEMO M344-08-106 MM 32-42-00. 2 L 7 2 4F 4 F RT A22CE E25EA 20080521 NM 2008 5 21 2008UALA02684 1 20080506 A 2910 FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYDRAULIC SYS LOOSE A UALA O OTHER W K INADEQUATE Q C FLUID LOSS NR NOT REPORTED 1 WP 29 595UA 28748 HYDRAULIC QUANTITY DECREASED TO 47. QUANTITY STABLE WITH PUMPS OFF, CENTER SYSTEM. CREW COMMENTS, C HYD QTY .38 WITH P UMPS ON. SUPPLEMENTAL DATA UPDATE, FOUND C2 PRESS INLET UNION TO FILTER MODULE SPRAYING HYDRAULIC FLUID. SECURED UNION FITTING AND SERVICED HYD, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 SO 2008 5 21 GUUA05190801 1 20080519 A 2497 44B258051002 RELAY EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE START SWITCH SHORTED A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 29 280AS 120231 FLIGHT: 9148, UPON STARTING, RT ENGINE, AFTER SELECTING THE START SWITCH TO START, A LOUD SIZZLE CAME FROM THE FIRST OFF ICERS SIDE PANEL, ALONG WITH A SMALL FLAME AND SMOKE. DETERMINED THAT AIRBORNE AUXILIARY POWER UNIT RELAY BOX AT FIRST OFFICERS SIDE PANEL HAD BURNED COMPONENTS, THE PROTECTION RELAY, BUS BAR HOUSING AND HARDWARE WERE REPLACED. 2 L 7 2 4T 4 T RT A31SO E20NE 20080521 NM 2008 5 21 2008UALA02715 1 20080509 A 5754 DOUBLER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE L/E SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 NR 1 SLAT JUST INBOARD OF REPAIR DOUBLER IS CRACKED AT AFT ROW OF FASTENERS. REMOVED EXISTING DOUBLER AND DAMAGED AREA. INSTALLED REPAIR SPLICE AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 20080521 NM 2008 5 21 AALA200801074 1 20080424 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR GALLEY DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RIGHT NUM BER ONE DOOR GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801075 1 20080424 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR OVERHEAD INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801077 1 20080424 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN WRONG PART A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT SEAT 20C DIM. FOUND WRONG BULBS INSTALLED. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 20C. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801086 1 20080425 A 2910 HYDRAULIC LINE BOEING 757 757223 1384957 NM NLG LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 177AN 32396 TUL INFLIGHT T1745/25APR ORD TO LAX - LEFT HYDRAULIC SYSTEM LOSS IN FLIGHT. DIVERTED TO TUL AND LANDED WITHOUT INCIDEN T. FOUND NOSE GEAR DOOR ACTUATOR HYDRAULIC HOSE LEAKING. REPLACED NOSE GEAR DOOR ACTUATOR HYDRAULIC HOSE. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080521 NM 2008 5 21 AALA200801087 1 20080425 A 3250 METERING VALVE BOEING 767 767223 1385123 NM NLG STEERING DEFECTIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 324AA 22325 JFK INFLIGHT T686/25APR - DURING TAKEOFF AIRCRAFT PULLED TO LEFT. REQUIRED .75 RUDDER PEDAL TO KEEP AIRCRAFT ON CENTERL INE. AFTER TAKEOFF ANOTHER AIRCRAFT REPORTED SMOKE FROM NOSE TIRES AND OBSERVED NOSE WHEEL TURNED LEFT OF CENTER. RETU RNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR STEERING METERING VALVE AND BOTH NOSE GEAR TIRE WHEEL ASSEM BLIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080521 NM 2008 5 21 AALA200801088 1 20080426 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 962AN 30858 DFW - EMERGENCY LIGHT AT SEAT ROW 10DEF MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT ROW 10DEF. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 NM 2008 5 21 AALA200801089 1 20080426 A 3350 LENS BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 962AN 30858 DFW - EMERGENCY LIGHT AT SEAT ROW 10DEF MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 10DEF. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 NM 2008 5 21 AALA200801038 1 20080421 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 906AN 29508 TUL - SEAT MOUNTED EMERGENCY LIGHT BATTERY PACK IN CABIN FAILED TEST. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS IN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 NM 2008 5 21 AALA200801102 1 20080427 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 794AN 30256 JFK - EMERGENCY LIGHTS IN COACH CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN COACH CABIN. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801052 1 20080422 A 3350 COVER BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT WIRING AT LEFT OVERHEAD SEAT ROW 30 MISSING PROTECTIVE COVER. REPLACED PROTECTIVE COVER FOR EMERG ENCY LIGHT WIRING AT LEFT OVERHEAD SEAT ROW 30. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801044 1 20080422 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 JFK - EMERGENCY LIGHT AT LEFT AND RIGHT FORWARD GALLEY INOPERATIVE. FOUND SHORTED LIGHT ASSEMBLY ON RIGHT SIDE FORWARD GALLEY. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RIGHT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801047 1 20080422 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 WP 2008 5 21 AALA200801055 1 20080422 A 3350 60030431 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9620D 53591 TUL - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD SEAT ROW 20 FAILED TEST. REPLACED BATTERY PACK AT OVERHEAD SEAT 20 FOR E MERGENCY LIGHTS IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080521 NM 2008 5 21 AALA200801042 1 20080422 A 3350 LENS BOEING 767 767323 1385205 NM EXTERIOR MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 372AA 25199 DFW - EXTERNAL EMERGENCY LIGHT AT LEFT AFT OVERWING MISSING LENS. REPLACED LENS FOR EXTERNAL EMERGENCY LIGHT AT LEFT AF T OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080521 NM 2008 5 21 AALA200801084 1 20080424 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT SEAT 21G INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801096 1 20080426 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 962AN 30858 DFW - EMERGENCY EXIT LIGHT AT AFT LEFT NUMBER FOUR DOOR DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY EXIT LIGHT AT AF T LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 NM 2008 5 21 AALA200801099 1 20080426 A 1100 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 187AN 32381 DFW - EMERGENCY EXIT DECAL AT AFT LEFT AFT GALLEY DOOR DAMAGED. REPLACED DECAL FOR EMERGENCY EXIT LIGHT AT AFT LEFT AFT GALLEY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080521 WP 2008 5 21 AALA200801065 1 20080423 A 3350 0200200001 LENS DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 495AA 49733 LGA - EMERGENCY LIGHT IN AFT CABIN MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080521 WP 2008 5 21 AALA200801067 1 20080424 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9621A 53592 LGA - EMERGENCY LIGHT AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD ELECTRONIC BAY FOR EMERGENCY LIGHT AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080521 NM 2008 5 21 AALA200701072 1 20080424 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT SEAT 32G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080520 WP 2008 5 20 RYNA200800021 1 20080417 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 932RD 49233 PASSENGER CABIN LEFT INBOARD SEAT TRACK IS CORRODED AT BS 1212 - 1287. REPAIRED CORRODED AREA IAW MD-80 SRM 51-10-03. 2 L 7 2 4F A6WE 20080520 NM 2008 5 20 2008UALA02662 1 20080508 A 5753 SPINDLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE T/E FLAP CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 369UA 24538 CORROSION SUSPECTED AT LT OB FLAP, INBD SPINDLE. 2 L 7 2 4F 4 F RT A16WE E2GL 20080520 NM 2008 5 20 2008UALA02710 1 20080512 A 2150 3964622 CONTROL VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT PACK MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 653UA 25391 LEFT PACK FLOW CONTROL VALVE WILL NOT OPEN. AFTER TROUBLE SHOOTING FOUND FLOW CONTROL, SHUTOFF VALVE FAULTY. REPLACED LT PACK FLOW CONTROL VALVE. OPS CHECKED GOOD.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080521 NM 2008 5 21 2008UALA02712 1 20080511 A 5247 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT ACTIVATED A UALA D RETURN TO BLOCK W J INADEQUATE Q C WARNING INDICATION IN INSP/MAINT 1 WP 29 647UA 25284 RTBL WITH A AUXILIARY POWER UNIT DOOR MESSAGE. REOCCURRED ON FLT 0907-11. 2 L 7 2 4F 4 F RT A1NM E24NE 20080521 NM 2008 5 21 2008UALA02722 1 20080510 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 DOOR 2R UPPER HINGE ARM CUTOUT CRACKED. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGE AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080529 NM 2008 5 29 08FDEA02007 1 20080528 A 5730 ARB39545 DOUBLER DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 529FE 48624 LEFT WING, LEADING EDGE RIB DOUBLER AT XOS 667 FOUND CRACKED. REMOVED CRACKED RIB DOUBLER AS PER SRM 51-31-01, VOL. II. FABRICATED NEW RIB DOUBLER AS PER DRAWING ARB3954. INSTALLED NEW RIB DOUBLER AT LT WING LEADING EDGE AT XOS 667 AS PER SRM 51-33-01, VOL.II. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA02015 1 20080528 A 5280 65377001 SKIN BOEING 727 727233 138408A NM MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 NOSE LANDING GEAR RIGHT FWD DOOR, CRACK AT AFT END EDGE SKIN AT O/B STOP ANGLE SUPPORT REPAIRED, R NLG DOOR REF 51-40-3, 51-30-5, 51-10-02, AND MM 32-22-001-4 . PERFORMED ADJUSTMENT AND TEST OF DOOR REF MM 32-22-001-5. OPS CHECK GOOD. TH IS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 SO 2008 5 29 C2XA08RI069 1 20080411 A 3040 272564 SWITCH EMB 145 EMB145LR 3260212 SO WINDSHIELD WIPER FAULTY A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 11536 145520 FLIGHT 2988 - EWR - FLIGHT CREW REPORTED STRONG ELECTRICAL BURN SMELL WITH WINDSHIELD WIPER ACTIVATED. EWR MX REMOVED A ND REPLACED LT WINDSHIELD WIPER SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20080529 NM 2008 5 29 HNAA0800157 1 20080427 A 2910 82920010307 LINE DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYS LEAKING A HNAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 07 984HA 377 HYDRAULIC LINE LEAK IN CABIN PRESSURE VESSEL, OVERHEAD AT ROW 5DF. 2 H 7 2 4T RT A13NM 20080529 EA 2008 5 29 HNAA0800155 1 20080508 A 7120 87110047001 MOUNT DHAV DHC8 DHC8311 1386006 EA NR 1 ENGINE BROKEN A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 333EN 8983 221 NR 1 ENGINE AFT OUTBOARD STRUT MOUNT FOUND TO BROKEN. INSP GENERATED BY INSPECTION CARD 71-20-03. 2 H 7 2 4T RT A13NM 20080529 SO 2008 5 29 C2XA08RI073 1 20080515 A 3350 602043 LAMP EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17108 145655 DURING ROUTINE MAINTENANCE, MX FOUND RIGHT HAND LOWER EMERGENCY LIGHT AT ESCAPE HATCH INOPERATIVE. MX REMOVED AND REPLA CED EMERGENCY LIGHT IAW EMB AMM 33-50-13 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20080529 NM 2008 5 29 08FDEA01952 1 20080522 A 5330 651842012 SKIN BOEING 727 727233 138408A NM BS 297 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 274FE 22039 LOWER FUSELAGE DENTED BS 297.5 BELOW STR 20R, BELOW FWD LAV SERVICE PANEL CUTOUT FWD LWR CORNER. REWORKED DENT IAW B727 SRM 51-40-1 AND EA 7-5330-116984 AND B727 SRM 53-30-01. REMOVED AND REPLACED RIVET IAW B727 SRM 51-30-. TREATED AND P RIMED AREA IAW B727 SRM 51-10-2. 2 L 7 3 4F RT A3WE 20080529 EU 2008 5 29 08FDEA01953 1 20080502 A 5730 A5724053500339 ACCESS DOOR AIRBUS 300 A300F4605R 3930327 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 661FE 760 RIGHT WING PANEL HAS NUMEROUS CHAFED SPOTS ON PANEL 675 CB. BLENDED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW A300-600 S RM 57-51-12, PG 101. REMOVED PANEL IAW A300-600 SRM 51-40-21, PARA 5. REMOVED FASTENERS FROM PANEL IAW EA 6-5750-11848 4 AND A300-600 SRM 51-77-10. REMOVED PAINT, FABRICATED DOUBLER, PREPPED DOUBLER AND PANEL FOR BONDING. LAYED UP REPAIR DOUBLER, VACUUM BAGGED, CURED REPAIR. REMOVED FLASH, ALODINED, SEALED AND INSTALLED FASTENERS IAW EA 6-5750-188484, A3 00-600 SRM 51-77-10, 51-77-12 AND 51-21-10, EA 6-5750-118484, RIGHT WING ALL SPEED AILERON JACK BAY ACCESS PANEL CHAFING . 2 L 7 2 4F RT A35EU 20080529 NM 2008 5 29 HALA0800582 1 20080515 A 2731 162000105 COMPUTER BOEING 767 76733A 1385209 NM ELEVATOR FEEL MALFUNCTIONED A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 587HA 21597 21597 33421 ETOPS SIGNIFICANT SYSTEM, ELEV FEEL STATUS MSG DISPLAYED. PERFORMED FIM 27-31-00. FOUND LEAD IN ELEVATOR FEEL COMPUTER . REMOVED AND REPLACED ELEVATOR FEEL COMPUTER PER AMM 27-31-19. OPS CHECK AND LEAK CHECK OK. PERFORMED FIM 27-31-00, MESSAGE CLEARED. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20080529 WP 2008 5 29 08FDEA01866 1 20080516 A 5730 ARB16182 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 567FE 46994 RIGHT WING NR 2 SLAT L/E HAS A DENT. CUT OUT DAMAGED AREA OF SLAT. FABRICATED DOUBLER AND FILLER IN REF TO DC/MD-10 SR M 57-10-00, FIG 43 VOL II. REMOVED RUB STRIP FROM THE NR 2 SLAT IAW DC/MD-10 SRM 51-35-01, VOL II. REMOVED NR 3 SLAT T RACK IN REF TO DC/MD-10 SRM 51-31-01, VOL II. ALODINED AND PRIMED IN REF TO DC/MD-10 SRM 51-21-01, VOL II. INSTALLED D OUBLER AND FILLER IN REF TO DC/MD-10 SRM 51-35-02, VOL II. INSTALLED RUB STRIP AND SLAT TRACK COVER IN REF TO DC/MD-10 SRM 51-35-01, VOL II AND 51-35-02, VOL II. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA01926 1 20080521 A 5313 A6A7003501 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 CRACK INDICATION FOUND DURING X-RAY INSPECTION AT STA 6-0, LONGERON 2L, AFT SECTION EDGE, CRACK LENGTH APPROX 1.5 INCH . REPAIRED AS PER SRM 53-10-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA01928 1 20080521 A 5311 65163421 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 AFT PIT BILGE BODY FRAME UPPER FLG IS CORRODED BS 103, STR 26R - 28R, WL 147 REMOVED .007 INCH FROM ORIGINAL MATERIAL OF .063 INCHES WITH .056 INCH REMAINING AND FOUND FRAME TO BE OUT OF LIMITS. HEAT TREATED, DRILLED TREATED, PRIMED AND PA INTED, REPAIR DOUBLER. INSTALLED REPAIR DOUBLER REFERENCE SRM 53-10-1/PAGE NR 2 SRM 51-30-2 PAGES 2, 8, 9. CLASSIFED A S A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 WP 2008 5 29 08FDEA01929 1 20080521 A 5730 ARB097533 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 567FE 46994 RIGHT WING TANK PLATE/PANEL 639 CB HAS ELONGATED FASTENER HOLE AND FOUND TO BE OUT OF LIMITS IAW DC/MD SRM 57-10-00, VOL I. MACHINED A NEW PANEL IAW DAC DWG ARB0975-33, REV "AY". FPI IAW DPS 4.707 AND DAC DWG ARB0975, REV "AY". NO CRAC KS NOTED. APPLIED ALODINE, PRIMER AND PAINT IAW DAC DWG ARB0975, REV "AY" AND DC/MD-10 SRM 51-21-01, VOL II. PART MARK ED IAW FEDEX GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA01930 1 20080521 A 5321 6567245116 FLOOR PANEL BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 C-2 PIT FLOOR PANELS NR 3 HAS CORROSION ALONG ONE SIDE EDGE FABRICATED NEW C-2 NR 3 PIT FLOOR PANEL REF DRAWING 65-67245 AND SRM 51-30-05 PG 13-21. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 EU 2008 5 29 YENA2008044 1 20080511 A 2121 VD390003 FAN AIRBUS 320 A320232 3930326 EU CABIN FAILED A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 519JB 29795 29795 1398 FLT 119, JFK-MSY, FWD CABIN FAN INOP ASSOCIATED WITH FUMES, TURNED OFF CABIN FAN & FUMES WENT AWAY (CABIN FANS-BOTH). P ERFORMED OPS CHECK OF CABIN RECERT FANS IAW AMM 21-21-00. NO SMELLS OR DEFECTS NOTED. REMOVED AND REPLACED RECIRCULATI ON FAN LEFT FWD IAW AMM 21-21-51-04. OPS CHECK NORMAL. 2 L 7 2 4F RT A28NM 20080527 NM 2008 5 27 USAA920081059 1 20080508 A 5340 6935352U14 STRINGER CLIP BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED STRINGER TIE CLIP, BS 500E, S14R. REPLACED STRINGER TIE CLIP, BS 500E, S14R IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082649 1 20080514 A 5330 65516242 SKIN BOEING 737 7373H4 1384600 NM BS 976 S23R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 976, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082648 1 20080514 A 5312 6936642 STIFFENER BOEING 737 7373H4 1384600 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND VERTICAL TEE CHORD CRACKED AT BS 178, LBL 5.7, WL 184. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 ASAA0842941 1 20080511 A 5753 SKIN BOEING 737 7374Q8 138447Q NM LT FORE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 LEFT OUTBOARD FORE FLAP LEADING EDGE DENTED AT RSS479. DENT MEASURES A=.59 Y=.017. REPLACED LEFT OUTBOARD FORE FLAP LE ADING EDGE OUTBOARD END IAW B737 400 SRM 51 40 02 & MM 20 50 11. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082651 1 20080515 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727A S25L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082659 1 20080515 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 380 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082657 1 20080515 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500C S26R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 ASAA0842946 1 20080511 A 5753 SKIN BOEING 737 7374Q8 138447Q NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 LEFT WING INBOARD TRAILING EDGE FLAP DENTED IN MIDDLE OF TRAILING EDGE FLAP. REPAIRED LEFT INBOARD AFT FLAP TRAILING ED GE LWR SURFACE IAW B737 400 SRM 51 70 10 REPAIR 2 PG 201. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082677 1 20080518 A 5754 SKIN BOEING 737 7373H4 1384600 NM NR 5 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT INBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082678 1 20080518 A 5754 SKIN BOEING 737 7373H4 1384600 NM NR 5 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082676 1 20080518 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR CUTOUT LOWER AFT CORNER. REPAIRED SKIN PER SW A EA. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082682 1 20080518 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 380 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080528 SO 2008 5 28 C2XA08RI068 1 20080111 A 2611 47359713 SMOKE DETECTOR EMB 135 EMB135ER 3260203 SO CARGO BAY INTERMITTENT A C2XA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SW 27 16502 16222 16222 145166 FLIGHT 3096 - EWR - FLIGHT CREW REPORTED BAGGAGE EXTINGUISH WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. ALSO, I NTERMITTENT BAGGAGE SMOKE WARNING ON EICAS, BUT DISAPPEARED AFTER 1 SECOND. CREW PROCEEDED WITH EMERGENCY DESCENT AND L ANDED AIRCRAFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED BOTH CARGO SMOKE DETECTOR IAW EMB 135 AMM 26-15-01 AND PERFORM ED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20080528 NM 2008 5 28 SWAA082763 1 20080521 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM FUSELAGE INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080528 SO 2008 5 28 RAIA00805003 1 20080502 A 5610 163500115 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT FAILED A RAIA B A EMER. DESCENT UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 837HK 2425 145255 FLT 7891 - DEN - CAPTAIN'S WINDSHIELD SHATTERED. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD ASSEMBLY. 2 L 7 2 4T RT T00011AT 20080528 SO 2008 5 28 C2XA08IA126 1 20080513 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11548 145565 LCH - DURING MAINTENANCE INSPECTION THE NR 2 & NR 3 AISLE PATH LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE R EMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20080528 NM 2008 5 28 SWAA082726 1 20080519 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082717 1 20080515 A 5744 654485114 MOUNT BOEING 737 7373H4 1384600 NM NR 4 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 4 SPOILER OUTBOARD MOUNT LUG BROKEN. REMOVED AND REPLACED SPOILER ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 20080528 WP 2008 5 28 NWAA082159886 1 20080514 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 600TR 47783 DURING LINE CHECK, THE EMERGENCY PATHWAY LIGHTING AT ROWS 5, 6, 7,AND 8 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLA CED THE BATTERY PACK AND THE LIGHTS IN THE ROWS SPECIFIED RETURNED TO AN OPERATIONAL CONDITION. 2 L 7 2 4F RT A6WE 20080528 2008 5 28 NSVA2008032 4 20080525 A 3100 CONTROL PANEL SAAB SF340 340B 7860101 EU COCKPIT ODOR A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 184CJ 340B184 C/D OVERHEAD PANEL BACKLIGHTING INOP WITH ASSOCIATED ELECTRICAL SMOKE SMELL. MAINTENANCE EVALUATED AND DEFERRED IAW MEL 33-40-1, ID NR 30932. 2 L 7 2 4T RT A52EU 20080528 WP 2008 5 28 IXXA08SMN164S 1 20080419 A 5340 FITTING DOUG DC8 DC871F 302199D WP BS 290 L19R CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT UPPER SURFACE OF CUSP EXTRUSION FWD FITTING CRACKED AT STATION 920.000 LO NGERON 19 RIGHT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION F OUND. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DPS 4.707, DC8 SRM 51- 1-8B, 51-3-1, ATI REPAIR SPECIFICATION NUMBER 2003-05, AND DOUGLAS DRAWING 3779874. 2 L 7 4 4F RT 4A25 20080528 NM 2008 5 28 NWAA082175803 1 20080514 A 3350 BATTERY PACK BOEING 757 757351 1384991 NM EMERGENCY LIGHTS DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 583NW 32983 BATTERY PACK ASSOCIATED WITH ESCAPE PATH LIGHTING AT ROWS 26 THROUGH 30 FAILED DURING EMERGENCY LIGHT BATTERY PACK CHECK DURING SCHEDULED OVERNIGHT MAINTENANCE. MAINTENANCE REPLACED THE BATTERY PACK AND ALL OPERATIONS CHECKED GOOD. 2 L 7 2 4F RT A2NM 20080528 NM 2008 5 28 NWAA082276624 1 20080519 A 3350 POWER SUPPLY BOEING 747 747251B 1384892 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 624US 21706 DURING OVERNIGHT CHECK, FOUND MAIN DECK GALLEY EMERGENCY EXIT SIGN WITH ARROWS INOP. MAINTENANCE REMOVED AND REPLACED P OWER SUPPLY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20080528 NM 2008 5 28 UIEA200800209 1 20080518 A 5230 DOOR BOEING 747 7472D7B 1384803 NM MAIN CARGO OPEN A UIEA J A DUMP FUEL UNSCHED LANDING O P OTHER NO WARNING INDICATION CL CLIMB 1 EA 15 524MC 21784 AFTER TAKEOFF UNABLE TO PRESSURIZE AIRCRAFT. CABIN WAS CLIMBING AT 2000 FPM EVEN WITH 3 PACKS TURNED. ALL DOOR WARNING LIGHTS ON F/E PANEL AND CARGO DOOR LIGHTS ON PILOTS MCP WERE OUT. INSPECTION OF THE MAIN DECK REVEALED LOUD NOISE COMI NG FROM BULK CARGO DOOR AREA. A/C WAS DEPRESSURIZED IAW WITH FHB AND LANDED AT NEAREST AIRPORT. ON WALK AROUND, FOUND BULK CARGO DOOR OPEN. CLOSED DOOR AND PRESSURE CHECKED GOOD IAW MM 52-63-01 601 AND 21-31-00. OPENED A DMI FOR THE BUL K CARGO DOOR WARNING LIGHT INOP. 2 L 7 4 4F RT A20WE 20080528 NM 2008 5 28 UIEA200800211 1 20080518 A 5315 FLOORBEAM BOEING 747 7472D7B 1384803 NM BS 1180 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK FLOORBEAM WEB FOUND CRACKED AT STA 1180 RBL 123. MAIN DECK FLOOR WEB CRACKED AREA REPAIRED PER EO 4753B153. 2 L 7 4 4F RT A20WE 20080528 EU 2008 5 28 08FDEA01883 1 20080519 A 5712 A5726007320251 RIB AIRBUS 310 A310324 3930206 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 815FD 638 LEFT WING TIP RIB WY 495 IS CRACKED. REPLACED LEFT WING TIP RIB WY 495 IAW WORK INSTRUCTIONS FOUND IN EO 6-5710-7-5012 E OCN 01 PI. 2 L 7 2 4F RT A35EU 20080529 NM 2008 5 29 08FDEA01890 1 20080520 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 MAIN DECK CARGO DOOR SPOOL FITTING NR 2 FOUND 3RD LAYER CRACK INDICATION AT FITTING BOLT HOLES 'A' AND 'B'. FITTING REM OVED AND REPLACED AS PER SRM 51-31 -01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA01892 1 20080520 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 MAIN DECK CARGO DOOR SPOOL FITTING NR 4 FOUND 3RD LAYER CRACK INDICATION AT FITTING BOLT HOLES 'A' AND 'B'. FITTING REM OVED AND REPLACED AS PER SRM 51-31 -01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA01893 1 20080520 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 MAIN DECK CARGO DOOR SPOOL FITTING NR 5 FOUND 3RD LAYER CRACK INDICATION AT FITTING BOLT HOLE 'C'. FITTING REMOVED AND REPLACED AS PER SRM 51-31 -01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA01903 1 20080520 A 5420 651950757 ANGLE BOEING 727 727233 138408A NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 NR 3 ENGINE LOWER COWL, O/B SIDE EDGE, COWL STRUCTURE AREA CRACKED OUT, JUST AFT OF THE 4TH LATCH CUT OUT FROM FWD END REMOVED AND REPLACED ANGLE REF DWG 65- 19507. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 EU 2008 5 29 08FDEA01875 1 20080517 A 5512 A5517800920500 ACCESS PANEL AIRBUS 300 A300F4605R 3930327 EU HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 RT HORIZONTAL STAB L/E REMOVABLE ACCESS PANEL 341AB HAS .50 IN CRACK ON UPPER MATING FLANGE, LOWER SIDE RT HORIZONTAL ST AB L/E PANEL 341AB CRACK REPAIRED IAW FEDEX EA 6-5510-12159. 2 L 7 2 4F RT A35EU 20080529 EU 2008 5 29 08FDEA01876 1 20080517 A 5753 A57960017206 PLATE AIRBUS 300 A300F4605R 3930327 EU LT WING TE FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 LT WING INBD FLAP UPPER SURFACE OUTBD EDGE RUB STRIP HAS 1.25 IN WEAR MARK REPAIRED WEAR STRIP ON LT INBD FLAP UPPER OUT BD EDGE IAW FEDEX EA 6-5750- 121269, RELEASE DATE 14 MAY, 2008. 2 L 7 2 4F RT A35EU 20080529 NM 2008 5 29 UIEA200800217 1 20080520 A 2612 FIRE WARNING BOEING 747 74747UF 1384812 NM APU BAY FALSE ACTIVATION A UIEA O OTHER N FALSE WARNING CR CRUISE 1 EA 15 498MC 29259 EICAS MESSAGE "APU" PULLED APU FIRE SWITCH IAW QRH. INSPECTED APU COMPARTMENT. NO DEFECTS NOTED. RESET FIRE HANDLE AP U, OPS NORMAL PER MM 49-11-00. OK FOR CONTINUED SERVICE. 2 L 7 4 4F RT A20WE 20080521 EU 2008 5 21 2008UALA02732 1 20080509 A 3350 D9239003500060 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 463UA 1282 EPSU INT LOAD EMER R MESSAGE AT CIDS DURING OPERATIONAL TEST OF EMERGENCY CABIN LIGHTS AND SIGN CK. FOUND EPSU FAILED. REPLACED RT O/W EPSU, CHECKS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080521 NM 2008 5 21 2008UALA02734 1 20080509 A 3350 1619 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 313UA 23674 LT EXTERNAL FUSELAGE EEL LIGHT INOP AFT OF INBOARD AFT FLAP. SUSPECT FAULTY LAMP. REPLACED LAMP OP CHECKED GOOD. AC O K FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 20080521 EU 2008 5 21 2008UALA02757 1 20080512 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 497UA 1847 DURING TAKEOFF, THE EMERGENCY LIGHTS IN THE CABIN CAME ON FOR ABOUT 4 MINUTES. 2 L 7 2 4F 4 F RT A28NM E40NE 20080521 NM 2008 5 21 2008UALA02766 1 20080513 A 3830 TANK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAVATORY FULL A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 572UA 26682 MID LAV FULL PER CREW. FLT DIVERTED. SERVICED LAVS, OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 NM 2008 5 21 AALA200801013 1 20080418 A 3350 LIGHT BOEING 767 767323 1385205 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 347AN 33086 DFW - EXTERIOR EMERGENCY LIGHT AT FORWARD RIGHT OVERWING INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT FOR WARD RIGHT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080521 WP 2008 5 21 AALA200801018 1 20080420 A 3350 LENS DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 428AA 49340 LGA - EMERGENCY LIGHT AT SEAT 15D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F A6WE 20080521 EU 2008 5 21 AALA200801020 1 20080420 A 3350 82400 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 JFK - EMERGENCY LIGHT AT OVERHEAD LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20080521 WP 2008 5 21 AALA200801016 1 20080419 A 3350 8039001 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9677W 53627 SFO - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 23 TO 28 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHE AD SEAT ROWS 23 TO 28. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080521 NM 2008 5 21 BEFA200800004 1 20080410 A 5320 SHEAR WEB BOEING 757 757200 1384950 NM PWA 2037 PW2040 NE ZONE 100 CORRODED A BEFA K NONE O OTHER IN INSP/MAINT 1 WP 19 741PA 55899 24737 MAIN CABIN SHEAR WEB AT BS 1681 BETWEEN LBL 12 INCH AND RBL 24 INCH AT FLOOR ATTACHMENT HOLES, CORRODED. CUT OUT CORROD ED AREA AND PERFORMED SRM REQUIRED INSPECTION FOR CRACKS. NO CRACKS FOUND. INSTALLED DOUBLER REPAIR AS CALLED OUT BY S RM TREATED AND PRIMED AREA. 2 L 7 2 4F 4 F RT A2NM E17NE 20080521 NM 2008 5 21 AALA200801031 1 20080421 A 3350 BR964814 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 609AA 27447 LAX - EMERGENCY LIGHTS AT SEAT ROWS 17D TO 27D INOPERATIVE. FOUND SEAT 18D SHORTED. REPLACED LIGHT ASSEMBLY FOR EMERGE NCY LIGHTS AT SEAT ROWS 17D TO 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080521 NM 2008 5 21 08FDEA01850 1 20080515 A 5320 65575686 ANGLE BOEING 727 727233 138408A NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 220FE 20934 RT Z- ANGLE UNDER AUX TANK HAS SEVERAL LOOSE/MISSING NUT PLATES WITH AREAS OF LIGHT CORROSION ON LOWER SIDE OF PANEL VER IFIED MATERIAL THICKNESS, BLENDED OUT CORROSION, VERIFIED Z ANGLE THICKNESS WAS OUT OF LIMITS AFTER BLEND OUT ORIGINAL T HICKNESS WAS .056", AFTER BLEND OUT .036, LOSS OF .020". VERIFIED MATERIAL ID, FABRICATED REPAIR PARTS, TREATED AND P RIMED REPAIR ANGLES, INSTALLED REPAIR ANGLE, REPLACED NUT PLATES. REF DWG 65-57568-6, SRM 53-10-1 PG 1-2, SRM 51-40-4 PG 14-17. TOL ID IN 17-0236 CAL DUE DATE 1-8-09. THIS IS CLASSIFIED AS A MINOR REPAIR, LEVEL 1 CORROSION. 2 L 7 3 4F RT A3WE 20080521 EU 2008 5 21 08FDEA01855 1 20080515 A 5347 R5307008820400 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 MAIN DECK CARGO SEAT TRACK NR 2 RT HAS 6 AREAS OF CORROSION BETWEEN FR 30 TO FR 38.1 REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SECTION OF SEAT TRACK NR 2 RT AND INSTALLED SPLICE REPAIR AT SEAT TRACK NR 2 RT BETWEEN FR 30 AND FR 33 IAW A30 0-600 SRM 53-10-16, FIG 208. 2 L 7 2 4F RT A35EU 20080521 EA 2008 5 21 MASA200800400 1 20080514 A 5210 60031902300 SEAL CNDAIR CL600 CL6002B19 1900309 EA CABIN DOOR LEAKING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 FLT 2721, PHX-SBA - FRONT CABIN DOOR HAS AIR LEAK. REPLACED DOOR SEAL, OP AND PRESSURE CHECKS GOOD. 2 L 7 2 4F RT A21EA 20080521 EA 2008 5 21 MASA200800403 1 20080515 A 3040 FILLER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MELTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17358 7358 ASH FLT 2818 DSM (RON) - ELECTRICAL ODOR AND THE RT WINDSHIELD TERMINAL COVER WAS MELTED. MX FOUND COVER WAS OKAY BUY F ILLER AROUND THE PHENOLIC AREA OF THE CONTACTS WAS MELTED, CLEANED FILLER MATERIAL AND PERFORMED OPS CHECKS OF THE HEAT SYSTEM NORMAL. NO HEATING OF THE TERMINAL BLOCK NOTED. 2 L 7 2 4F RT A21EA 20080521 CE 2008 5 21 GLBA20061096 1 20080501 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BS 451 S10R CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 154GL UE154 FUSELAGE FRAME AT FS 451 CRACKED ON THE TOP SIDEOF STRINGER 10R. CRACK APPROXIMATELY 1.1 INCH LENGTH. MAINT REPAIRED FU SELAGE FRAME FLANGE AT FS 451 STRINGER 10R IAW SRM 51-70. REPAIR APPROXIMATELY 6 INCH BY 2 INCH. 2024-T3 .071. RII INSPE CTIONS COMPLIED WITH IAW TASKCARD 8.2.1. 2 L 7 2 4T 3 T RT A24CE E2NE 20080521 NM 2008 5 21 2008UALA02714 1 20080509 A 5754 DOUBLER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE L/E SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 23674 NR 2 SLAT INBOARD OF EXISTING REPAIR DOUBLER IS CRACKED AT AFT ROW OF FASTENERS. REMOVED THE EXISTING DOUBLER AND THE D AMAGED AREA. INSTALLED REPAIR SPLICE AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 20080521 NM 2008 5 21 2008UALA02735 1 20080510 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY LIGHT ROW 3A AFT INOP. SUSPECT FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR S ERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080521 NM 2008 5 21 AALA200801094 1 20080426 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 962AN 30858 DFW - EMERGENCY LIGHT AT BULLNOSE OVERHEAD SEAT ROW 22ABC INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT BUL LNOSE OVERHEAD SEAT ROW 22ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 NM 2008 5 21 AALA200801054 1 20080422 A 3397 WIRE BOEING 777 777223 1385213 NM CABIN EXPOSED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT WIRING AT SEAT 41D NOT STOWED. STOWED WIRING FOR EMERGENCY LIGHT AT SEAT 41D. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 EU 2008 5 21 AALA200801045 1 20080422 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 JFK - EMERGENCY LIGHTS AT SEAT ROWS 7C TO 18C INOPERATIVE. REPLACED BATTERY PACK AT SEAT 8G FOR EMERGENCY LIGHTS AT SEA T ROWS 7C TO 18C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20080521 NM 2008 5 21 AALA200801097 1 20080426 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 962AN 30858 DFW - EMERGENCY EXIT LIGHT AT AFT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT LIGHT AT AFT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 WP 2008 5 21 AALA200801064 1 20080423 A 3350 SHROUD DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 495AA 49733 LGA - EMERGENCY LIGHT AT SEAT 7D SHROUD BROKEN. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080521 NM 2008 5 21 KCSA081247 1 20080518 A 5311 STRAP BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 FUSELAGE FRAME STABILIZATION STRAP CRACKED AT B.S.2230 ABOVE STR-42L 2 L 7 4 4F RT A20WE 20080522 NM 2008 5 22 DU4R2008193 1 20080505 A 5330 SKIN BOEING 737 737448 13844BU NM CFMINT CFM56 CFM563C 13802 EU BS 795-846 DENTED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 742VA 24773 S/O 312001 OPS NR 24422 - AFT CARGO EXT DOOR SKIN HAS OUT OF LIMIT DENTS BETWEEN 2 EA EXISTING REPAIRS. 2 L 7 2 4F 4 F RT A16WE E21EU 20080522 NM 2008 5 22 DU4R2008195 1 20080505 A 5311 FRAME BOEING 737 737448 13844BU NM CFMINT CFM56 CFM563C 13802 EU BS 188 CRACKED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 742VA 24773 S/O 312001 OPS NR 24727 - CRACK AT MAIN FRAME OB CHORD STA. 188 RT SIDE FLOOR LEVEL (CRACK IN RADIUS). 2 L 7 2 4F 4 F RT A16WE E21EU 20080522 EA 2008 5 22 HNAA0800149 1 20080506 A 5100 8681CLEAR TAPE DHAV DHC8 DHC8311 1386006 EA NACELLE LOOSE A HNAA E D ENGINE SHUTDOWN RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 07 328EN 281 PAX AND F/A REPORTED SMALL FIRE COMING FROM NR 1 NACELLE , CENTER GEAR DOOR AREA. CREW PULLED FUEL OFF HANDLE, NO INDICA TION ON FIRE LOOP. F/A POINTED OUT TO MX WHERE FIRE WAS REPORTED, MX FOUND A 4 INCH PIECE OF EROSION TAPE LOOSE ON STRUT , WHICH WAS A YELLOW COLOR AND WAS FLAPPING AROUND. MX INSPECTED GEAR AREA AND AREA; NO EVIDENCE OF SMOKE OR FIRE, OPENE D UP ENGINE COMPARTMENT, NO DEFECTS NOTED. MX REMOVED TAPE, PERFORMED ENGINE FIRE TEST AND GROUND RAN AIRCRAFT, NO DEFEC TS NOTED. 2 H 7 2 4T RT A13NM 20080522 NE 2008 5 22 2562 1 20080423 A 6210 7615009100051A BLADE SKRSKY S76 S76B 8143007 NE PWA PT6 PT6B36 52043 EA MAIN ROTOR CRACKED E Q2HA K NONE O OTHER IN INSP/MAINT 1 EA 25 19HF 7575 391 760315 DURING INDUCTION, INSPECTION INTO A ROTOR BLADE REPAIR FACILITY, MAIN ROTOR BLADE SPAR WAS FOUND CRACKED (INTERNAL ROOT END). CRACK ORIGINATES FROM LEADING EDGE, OB LOWER ATTACHMENT BOLT HOLE. PHENOLIC BLOCK WAS REMOVED AND DYE PENETRANT IN SPECTION WAS PERFORMED TO CONFIRM PRESENCE OF CRACK. 1 G 7 2 4U 4 U H1NE E4EA 20080522 CE 2008 5 22 DXTA200803066 1 20080518 A 2701 SLZ80712 COMPUTER CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C 03047 GL FALSE ACTIVATION E DXTA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 07 950QS 318 318 7500050 AT CRUISE ALTITUDE FL410 A PULSATING THUMP COULD BE FELT IN BOTH CONTROL COLUMNS. INSPECTED, ALL PANELS, FLT CONTROLS D OORS ETC. NO DEFECTS NOTED. REMOVED AND REPLACED RT AOA COMPUTER IAW MM 34-14-01 C/W FT OF AOA SYSTEM PER SAME OPS CHECK GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080522 SO 2008 5 22 C2XA08CL056 1 20080506 A 3411 CS50006004A SENSOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL COCKPIT BURNED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13913 145438 FLIGHT NR 2706 THE CREW REPORTED A ELECTRICAL ODOR IN THE COCKPIT. MAINT INSPECTED AND REPLACED THE NR 1 PITOT CURRENT S ENSOR AND SOCKET. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080522 SO 2008 5 22 C2XA08IA121 1 20080506 A 2810 UNKNOWN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL FUEL SYSTEM LEAKING A C2XA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 15572 145636 FLIGHT 3140, DURING PREFLIGHT INSP THE CREW REPORTED A FUEL SMELL IN THE COCKPIT. MAINT INSPECTED THE AIRCRAFT WITH NO DEFECTS / SMELL NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080529 WP 2008 5 29 08FDEA01880 1 20080519 A 5542 AMC71141 SKIN DOUG DC10 DC1030 3023501 WP RUDDER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 307FE 48291 DURING RIGGING RUDDER MECHANICAL CTRL ACCIDENTAL DAMAGED ON LOWER AFT RUDDER LT SIDE. REPAIRED SKIN & PAINT AREA IAW SR M 55-10-00 FIG 2 VOL I & DWG D10-11-014. 2 L 7 3 4F A22WE 20080529 NM 2008 5 29 08FDEA01996 1 20080527 A 5320 65C8067691 COVER BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 C-2 PIT RT THRESHOLD COVER AT STA 950E IS CRACKED AT BOLT HOLE WITH LIGHT CORROSION ON BOTTOM SIDE OF PANEL TRANSFERRED HOLES, INSTALLED NUTPLATES, TREATED, PRIMED AND PAINTED NEW PANEL. REF; SRM 51-30-2 PG 1 - 3, FX 727 200 MM 51-20-15 1-7, AND FX727-200 MM 51-20-21-7 PG 1-3, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 EU 2008 5 29 08FDEA01919 1 20080520 A 5321 A532B388300100 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 815FD 638 THERE IS A BROKEN FLOOR PANEL FOR THE MAIN CARGO DECK FROM FRAME 66 TO FRAME 67, RBL 57 TO RBL 71. MATERIAL ID IS A402H 35039-003, PO 604814.1 IAW FEDEX DWG SRZ 25-005, REV F. FABRICATED A NEW FLOOR PANEL FOR THE MAIN CARGO DECK FROM FRAME 66TO 67 USING THE OLD FLOOR PANEL AS A TEMPLATE IAW FEDEX DWG SRZ 25-005, REV F. MARKED PANEL NR 252 BH IAW FEDEX DWG SRZ 25-005, REV F AND GMM 7-0-1000. PANEL PART ID IS FDX532B388300100. 2 L 7 2 4F RT A35EU 20080529 NM 2008 5 29 08FDEA01921 1 20080520 A 5320 6582623 ANGLE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 FWD PANEL RACK, FWD PIT FRAME BS 720 CORROSION AROUND NUTPLATES REMOVED CORROSION IAW SRM 51-10-6, ORIGINAL "T'' .040 IN CH, MAT. REMOVED IS .012. MAT REMAINING .028 INCH IS OUT OF LIMITS IAW SRM 53-1031. FABRICATED NEW LINER SUPPORT AN GLE FROM 7075-0 .050' AND HEAT TREATED TO T-6. LOCATED NEW ANGLE, TREATED AND PRIMED IAW SRM 51-20-2 AND INSTALLED NUT PLATES IAW SRM 51-30-02 THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA02014 1 20080528 A 5315 652083817 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 AFT CABIN, AT BS 1130 FLOORBEAM LOWER FLANGE, UPPER SURFACE CORRODED, BETWEEN LBL 22 AND LBL 35. REMOVED LOWER LT EXIST ING T-CAP REPAIR, REF SRM 51-30-2. FABRICATED NEW T-CAP AND SPLICE ANGLES AND STRAP, REF SRM 53-10-8 FIG 10. INSTALLED REPAIR PARTS, REF SRM 53-10-8 FIG 10. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01960 1 20080522 A 5330 SKIN BOEING 757 75723A 1384967 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 EXTERNAL PATCH REPAIR ON FUSELAGE FROM BS 1520 TO BS 1540, BETWEEN S-28L AND S-29L TO BE EVALUATED. EXISTING REPAIR EVA LUATED AS PER EO F-1500-7-5001 PT1 ATTACHMENT B, AND FOUND TO HAVE BEEN ACCOMPLISHED IAW B757 SRM 53-00-01 FIG 204. EXI STING REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 2 4F RT A2NM 20080529 2008 5 29 HALA0800584 4 20080515 A 3421 6227998003 ADI BOEING 767 767332 1382001 NM COCKPIT INTERMITTENT A HALA O OTHER O OTHER CR CRUISE 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, F/O'S ADI IS INTERMITTENT. REPLACED F/O ADI OPS CHECK OK PER M/M 34-22-03. PERFORMED MCDP TE ST 30 TO RETAIN LAND 3 LMP STATUS. TEST PASSED. 2 L 7 2 4F RT A1NM 20080529 NM 2008 5 29 08FDEA01927 1 20080521 A 5313 A6A7003501 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 CRACK INDICATION FOUND DURING X-RAY INSPECTION AT STA 6-100, LONGERON 2L, FORWARD SECTION EDGE, CRACK LENGTH APPROX 1 INCH. REPAIRED AS PER SRM 53-10-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 CALA0800470 1 20080519 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM BS 867 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17640 28901 FRAME CRACKED AT STATION 867 BETWEEN S8L AND S9L. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS PER EA 5310-04489. 2 L 7 2 4F RT A16WE 20080529 NM 2008 5 29 CALA0800476 1 20080521 A 5347 146A75012 CARGO TRACK BOEING 737 737724 13844BY NM BS 787-827 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23708 28769 AFT CARGO RIGHTHAND TIE DOWN RAIL HAS SURFACE CORROSION AT FASTENER HOLES BETWEEN STATION 787 AND 827. REMOVED TIE DOWN RAIL, FABRICATED AND INSTALLED REPAIR STRAP PER ECRA 5321-01550 AND REINSTALLED TIE DOWN RAIL. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800488 1 20080527 A 5340 65C16121 BRACKET BOEING 737 737524 1384721 NM L1 GIRT BAR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 CORROSION ON L1 DOOR GIRT BAR ATTACH PLATES (2EA). REMOVED L1 DOOR GIRT BAR ATTACH FITTINGS, CORROSION DETERMINED TO BE OUT OF LIMITS PER 737-500 SRM 53-10-15 FIG 101. FABRICATED NEW GIRT BAR ATTACH FITTINGS REF BAC DWG 65C16121, AND INST ALLED NEW GIRT BAR FITTINGS REF 737-500 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800478 1 20080521 A 5322 6546563 SHEAR TIE BOEING 737 7373T0 1384582 NM BS 967 S27L/R CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 39343 23581 STATION 967 BETWEEN S27L AND S27R FRAME CORRODED. REPAIRED SHEAR TIE AT SKIN ATTACHMENTS REF SRM 53-00-07 FIG 201, REPA IR 1. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800479 1 20080520 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM BS 440 S8L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 STATION 440 AT S8L AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED FRAME AT STATION 440 S8L BRACKET INBOARD MOUNT HOLE IAW EA 5310-04498. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800481 1 20080501 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 STATION 360 INBOARD AIR CONDITIONING (A/C) BRACKET MOUNT HOLE CRACKED. REPAIRED FRAME PER PACE EA620-53-001 AND CO EC/R A 5310-04772. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800471 1 20080519 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM BS 907 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17640 28901 FUSELAGE FRAME CRACKED AT STATION 907 BETWEEN S8R AND S9R. REMOVED DAMAGE, FABRICATED AND INSTALLED 2EA REPAIR ANGLES P ER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800473 1 20080519 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM BS 440 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17640 28901 FRAME CRACKED AT STATION 440 BETWEEN S8L AND S9L. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES PER EA 35310-0 4498. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800496 1 20080528 A 5311 6546525 FRAME BOEING 737 737524 1384721 NM BS 380 S8R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 RIGHT-HAND STATION 380 AT S8R AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED CRACKED FRAME RIGHT-H AND STATION 380 S8R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800498 1 20080528 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM BS 440 S8R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 RIGHT-HAND STATION 440 AT S8R AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED CRACKED FRAME RIGHT-H AND STATION 440 S8R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800500 1 20080528 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM BS 827 S8R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 RIGHT-HAND STATION 827 AT S-8 AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED CRACKED FRAME RIGHT-H AND STATION 827 S8R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800487 1 20080525 A 5330 65C35794 SKIN BOEING 737 7373T0 1384582 NM BS 727E S23R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17329 23459 APPROXIMATELY .75 INCH SKIN CRACK NOTED RT FUSELAGE 2.5 INCH BELOW AND 15 INCH AFT OF EMERGENCY EXIT LIGHT, JUST AFT OF WHEEL WELL STATION 727E STRINGER 23R. REPAIRED IAW SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 HALA0800590 1 20080516 A 5730 SKIN BOEING 767 76733A 1385209 NM RT WING DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 RIVETS SHEARED ON RIGHT WING FIXED T/E UPPER SURFACE (9). REMOVED AND REPLACED SHEARED RIVETS ON RIGHT WING FIXED T/E U PPER SURFACE PANEL IAW SRM 51-40-04-OG-O. 2 L 7 2 4F RT A1NM 20080530 NM 2008 5 30 HALA0800592 1 20080517 A 5700 STIFFENER BOEING 767 76733A 1385209 NM RT WING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 CRACK ON RIGHT WING FIXED T/E, JUST FORWARD OF O/B AILERON LENGTH WISE STIFFENER. REPAIRED RIGHT WING T/E, JUST FWD OF O/B AILERON STIFFENER PER SRM 51-20-11-OG-0, AND SRM 51-01-OG-0. 2 L 7 2 4F RT A1NM 20080530 NM 2008 5 30 HALA0800602 1 20080524 A 2120 UNKNOWN BOEING 767 76733A 1385209 NM CABIN ODOR A HALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 13 581HA 28141 ELECTRICAL ODOR IN COCKPIT AND MID GALLEY. TURNED OFF UTILITY BUSSES ODOR DISIPATED. ATB TO SEA. PERFORMED THE FOLLOW ING TEST WITH APU, ENGINES 1 AND 2 PACKS AND RECIRC FANS ON AND RUNNING. IFE OPS CHECK (23-34-00-715-001)GALLEY OPS TES T (25-31-03-764-020) DOOR HEATERS OPS TEST WITH AIR/GROUND ACTIVATED (21-45-00) FOUND A1 CHILLER (AFTRH 267-100) AND F1 CHILLER (F/C P/N 267-100 SN 7600) TO FAIL; OVERHEATS WITHIN 5-15 MIN. CHILLERS DID NOT SHUT OFF. ALSO, CHECKED ALL LAV HEATERS FOR ODOR, NO PROBLEMS FOUND. NO ODOR DETECTED IN COCKPIT OR CABIN. WATER HEATERS AMM REF 38-13-01-404-013. O K FOR SERVICE A1 AND F1 CHILLERS. ALSO, CHECKED ALL LAV HEATERS FOR ODOR, NO PROBLEMS FOUND. NO ODOR DETECTED IN COCKP 2 L 7 2 4F RT A1NM 20080530 NM 2008 5 30 HALA0800598 1 20080522 A 3241 ANTI-SKID SYS BOEING 717 717200 1383700 NM FAILED A HALA O OTHER J WARNING INDICATION LD LANDING 1 WP 13 481HA 55126 RT ANTI-SKID FAIL. ACCOMPLISH FIM 32-45-00, RESET ANTI-SKID SYS POWER SWI, BCU RTS PASSED. FAULT MSG CLEARED. OK TO CO NTINUE. 2 L 7 2 4F TR A6WE 20080530 NM 2008 5 30 CALA0800460 1 20080514 A 5311 6573743 FRAME BOEING 737 737524 1384721 NM BS 616 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 LAST FASTENER AT FRAME AT STATION 616 RBL 64 IN MID CABIN IS CRACKED. FABRICATED REPAIR PARTS, CAD PLATED, PRIMED AND I NSTALLED REPAIR PARTS PER ECRA 5310-01158. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082719 1 20080518 A 5315 6545810 FLOORBEAM BOEING 737 7373Q8 1384670 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 15. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 20080528 2008 5 28 SWAA082700 4 20080516 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 710SW 27844 DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080528 2008 5 28 SWAA082701 4 20080516 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 725SW 27857 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 NWAA082165803 1 20080514 A 3350 BATTERY PACK BOEING 757 757351 1384991 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 583NW 32983 BATTERY PACK ASSOCIATED WITH THE ESCAPE PATH LIGHTING AT ROWS 40 THROUGH 44 FAILED DURING EMERGENCY LIGHT BATTERY PACK C HECK DURING SCHEDULED OVERNIGHT MAINTENANCE. MAINTENANCE REPLACED THE BATTERY PACK AND ALL OPERATIONS CHECKED GOOD. 2 L 7 2 4F RT A2NM 20080528 WP 2008 5 28 IXXA08SMN093S 1 20080313 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1421 L36 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND DOUBLER, AFT LOWER FUSELAGE BELLY BELOW D-PIT DOOR RIVET SPACING EXCEEDED AT FS 1421 LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, FILLER SKIN, INTERNAL FINGER DOUBLER, AND FILLER INTERNAL DOUBLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC 8 SRM 51-1-11, 51-1-12, 51-3-1, FAA FORM 8110-3 NUMBER 08205 DATED 04/29/08, SEMAN DRAWING NUMBER ED-4735 DATED03/24/08, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 20080528 NM 2008 5 28 KNNA20080011 1 20080515 A 5347 SEAT TRACK BOEING 737 7372L9 1384497 NM BS 940-947 CORRODED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 464AT 21278 REMOVED GALLEY AND THEN FOUND THAT A SEAT TRACK WAS CORRODED. REMOVED AND THEN REPLACED SEAT TRACK. 2 L 7 2 4F RT A16WE 20080528 NE 2008 5 28 UIEA200800210 2 20080514 A 7320 665038062835 MEC BOEING 747 7472D3B 1384805 NM GE CF6 CF650E2 30018 NE FAILED A UIEA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 EA 15 506MC 21252 517579 AT FL 320 ON DESCENT, NR 1 ENGINE N1, N2 AND EGT ROLLED BACK WITH NO THROTTLE RESPONSE. RESTART NO HELP. SHUT DOWN FOR LANDING. REPLACED NR 1 MEC PER AMM 73-21-01 ACCOMPLISHED VSV RIG PER 75-30-00 CHECKED OK. LEAK CHECKED OK, ACCOMPLISHE D ENGINE RUN TEST PER AMM 71-00-00 TEST 3 ,4 , AND 5 ALL PARAMETERS NORMAL. 2 L 7 4 4F 4 F RT A20WE E23EA 20080529 NM 2008 5 29 08FDEA01889 1 20080520 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 MAIN DECK CARGO DOOR SPOOL FITTING NR 1 FOUND 3RD LAYER CRACK INDICATION AT FITTING BOLT HOLES 'C' AND 'D'. FITTING REM OVED AND REPLACED AS PER SRM 51-31-01 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 WP 2008 5 29 08FDEA01898 1 20080520 A 5330 NGA6013 SKIN DOUG DC10 DC1010 3022110 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 EXT FUSELAGE LWR SURFACE FOUND DENT 1 INCH BY 0.85 INCH DEEP .080 INCH ON SKIN DOUBLER (SEE NRC N00072). REPAIRED AREA IAW SRM 53-20-00 FIG 13 SHEET 2 A & SHT 5 VOL I. 2 L 7 3 4F A22WE 20080529 NM 2008 5 29 08FDEA01991 1 20080527 A 5320 6557568U26 ANGLE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 C-2 PIT Z - ANGLE FROM STA 960 TO 1036, RT SIDE, HAS SEVERAL LOOSE/MISSING NUT PLATES WITH AREAS OF LIGHT CORROSION ON PANEL REMOVED CORROSION, ORIGINAL THICKNESS, .062 INCH, REMOVED .037 INCH, REMAINING THICKNESS .025 INCH. OUT OF LIMITS . VERIFIED NEW PART 65-57568U26. TRANSFERRED HOLES TO NEW PART. TREATED AND PRIMED. ATTACHED SUPPORT TO NEW Z ANGLE REF SRM 53-10-1 PG 2 - 2A, SRM 51-30-5 PG 1, SRM 51-10-2 PG 7 AND 8, AND BOEING DWG 65-57567. 2 L 7 3 4F RT A3WE 20080529 EU 2008 5 29 08FDEA01997 1 20080523 A 5330 A53772518202 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 815FD 638 FWD CARGO DOOR CUT OUT FUSELAGE SKIN EDGE IS GOUGED AT THE UPPER FWD CORNER. COMPLIED WITH EA 6-5310-118494 FUSELAGE SK IN AT FRAME 20 AND STRINGER 28 R REPAIR. 2 L 7 2 4F RT A35EU 20080529 NM 2008 5 29 08FDEA01910 1 20080520 A 5330 6554574 SKIN BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 CORROSION ON AFT SKIN IN C-1 PIT AT FS 683 LBL 11, WL 148 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. ORIINAL "T" IS .045" REMAINING 'T' IS .024. MATERIAL LOSS OF .021 REF SRM 53-30-1 FIG 1. FABRICATED DOUBLER AND FILLER, TREATED AND PRIMED, INSTALLED DOUBLER AND FILLER REF SRM 53-30-3 FIG A AND SRM 51-10-2 THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 EU 2008 5 29 08FDEA02016 1 20080528 A 7830 SKIN AIRBUS 310 A310324 3930206 EU THRUST REVERSER GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 815FD 638 NR 2 ENG LT T/R AFT LATCH INNER CUTOUT CHAFED BY LATCH HANDLE. COMPLIED WITH EA 6-7830-118504 THRUST REVERSER, NR 2 ENG INE LT T/R LWR BIFURCATION DECK ASSY, OUTER SKIN GOUGE. 2 L 7 2 4F RT A35EU 20080529 WP 2008 5 29 08FDEA02017 1 20080528 A 5310 STRUCTURE DOUG DC10 DC1010F 3022111 WP BS 1250-1256 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 68059 46907 DURING REPAIR ASSESSMENT WAS FOUND AN EXISTING REPAIR AT CENTER FUSELAGE DOOR JAMB LT SIDE REPAIR HAS BEEN REPLACED BECA USE IT FOUND NOT IN CONFORMITY WITH APPROVED DATA. 2 L 7 3 4F A22WE 20080529 NE 2008 5 29 HNAA0800154 2 20080508 A 7250 TURBINE BLADES DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 2 ENGINE DAMAGED A HNAA O OTHER E VIBRATION/BUFFET CR CRUISE 1 EA 07 331EN 279 124243 BAD VIBRATION FELT THROUGH NR 2 CONDITION LEVER WHEN NR 2 PROP RPM IS TRANSIENT. INSPECTION FOUND THAT TURBINE ASSEMBLY HAD EXCESSIVE RUBBING AGAINST CASING. 2 H 7 2 4T 4 T RT A13NM E20NE 20080529 SO 2008 5 29 C2XA08RI070 1 20080512 A 3250 3085701007 MODULE EMB 135 EMB135ER 3260203 SO HYD SYSTEM INACCURATE A C2XA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 27 16502 15227 145166 FLIGHT 1202 - EWR - FLIGHT CREW REPORTED STEERING PULLED TO LEFT AND SHAKING LEFT & RIGHT. CREW RETURNED AIRCRAFT TO GA TE. EWR MX REMOVED AND REPLACED HYDRAULIC MODULE (STEERING MANIFOLD) AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. AI RCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20080529 2008 5 29 HNAA0800152 4 20080508 A 3417 7000700976 DADC DHAV DHC8 DHC8102 2809003 NM FAULTY A HNAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 07 931HA 12433 12433 132 TWO MINUTES AFTER ROTATION, BOTH YAW DAMPERS DISENGAGED AND RECEIVED AHARS DATA INVALID MESSAGE. BOTH 802 PANELS WENT B LANK AND ALTITUDE PRE-SELECT WENT TO ALL DASHES. BOTH FLIGHT DIRECTORS FAILED MULTIPLE TIMES. 2 H 7 2 4T RT A13NM 20080529 NE 2008 5 29 08FDEA01955 2 20080522 A 7200 ENGINE AIRBUS 310 A310203 3930313 EU GE CF6 CF680A 30025 NE NR 1 FAILED A FDEA E C ENGINE SHUTDOWN ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 21 432FE 28022 326 585118 ON TAKEOFF ROLL SERIES OF POPS OR BANGS, SPEED LESS THAN 40 KTS, EXPERIENCED LEFT SWERVE, LOW SPEED REJECT. SOUNDED LIK E POSSIBLE COMPRESSOR STALL. GVI OF NR 1 ENG SHOWS VERY SMALL METAL PARTICLES APX 1MM SIZE IN TAILPIPE. ALSO SLIGHT I NTERMITTENT SQUEAL W/ENGINE WIND MILLING IN GATE. REMOVED AND REPLACED THE NR 1 ENG IAW WORK CARD 44T0101-1 AND 44T0701 -1 LEAK AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A35EU E13NE 20080529 NM 2008 5 29 HALA0800583 1 20080515 A 3600 PRECOOLER BOEING 767 767332 1382001 NM NR 1 ENGINE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 596HA 23277 ETOPS SIGNIFICANT SYSTEM, DURING ENG CHANGE FOUND CRACK APPROX 1 IN LONG IN FWD INBD CORNER OF NR 1 ENG PRECOOLER. ACCO MPLISHED PROCEDURE WELDMENT IAW H/S MANUAL 36-12-12 PG 601. TASK ACCOMPLISHED BY UAL. 2 L 7 2 4F RT A1NM 20080529 NM 2008 5 29 ZZDA2008106 1 20080510 A 3260 49397141 SPRING BOEING 717 717200 1383700 NM MLG UPLATCH BROKEN A ZZDA O OTHER J WARNING INDICATION CL CLIMB 1 SO 37 934AT 55070 UNSAFE GEAR INDICATION (LEFT MAIN) AFTER GEAR RETRACTION, 3 GREEN LIGHTS WHEN EXTENDED. REMOVED AND REPLACED LEFT MLG U PLATCH PROXIMITY SENSOR CRANK ASSEMBLY SPRING. CYCLED GEAR NUMEROUS TIMES, ALL LIGHTS NORMAL. NO FAULT NOTED. OK FOR SERVICE AT THIS TIME REF 32-61 AMM. 2 L 7 2 4F TR A6WE 20080530 NM 2008 5 30 CALA0800497 1 20080528 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM BS 400 S8R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 RIGHT-HAND STATION 400 AT S8R AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED CRACKED FRAME RIGHT-H AND STATION 400 S8R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080530 EU 2008 5 30 YENA2008045 1 20080511 A 2910 D2901010200100 LINE AIRBUS 320 A320232 3930326 EU HYD SYSTEM BROKEN A YENA O OTHER K FLUID LOSS DE DESCENT 1 EA 15 661JB 2607 2607 3228 FLT 766, BQN-MCO, GREEN HYDRAULIC FLUID DEPLETED IN FLIGHT. GEAR MANUALLY EXTENDED. FLUID LOSS ECAM OCCURRED DURING DE SCENT INTO MCO. APPROXIMATELY BELOW 30,000 FT ENGINES AT IDLE. REMOVED CASE DRAIN LINE (HYDRAULIC) FROM NR 1 ENGINE PY LON AND DISCONNECTED HYDRAULIC PRESSURE LINE FROM NR 1 ENGINE PYLON. REF IPC 29-11-06-02D ITEM 240 AND 220. HYDRAULIC CASE DRAIN LINE FOUND BROKEN AT CLAMP. INSTALLED CASE DRAIN LINE REF IPC 29-11-06-02D ITEM 240 & 220 AND TORQUED REF AM M 20-00-00. LEAK CHECK OK. RETORQUED HYD PRESS LINE IAW AMM 20-00-00. OPS CHECK OK. 2 L 7 2 4F RT A28NM 20080530 NM 2008 5 30 HALA0800600 1 20080522 A 2150 A/C PACK BOEING 767 76733A 1385209 NM LEFT MALFUNCTIONED A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM, PACK INOP LIGHT ILL EICAS MESSAGE L PACK TEMP DISPLAYED. OPERATED NORMAL AFTER STBY SELECTED. BITE CHECK LEFT PACK, NO FAULTS NOTED. RESET LEFT PACK GND, OPS CHECK OK. 2 L 7 2 4F RT A1NM 20080602 NM 2008 6 2 CALA0800462 1 20080511 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM BS 747 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 RIGHT SIDE BS 747 INBOARD ATTACH FASTENER HOLE ON AIR CONDITIONING (A/C) BRACKET CRACKED. REPAIRED FRAME AT STA 747RT P ER EA 5310-04498 2 L 7 2 4F RT A16WE 20080602 NM 2008 6 2 CALA0800468 1 20080517 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM BS 867 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17640 28901 FUSELAGE FRAME CRACKED AT STATION 867 BETWEEN S8R AND S9R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES PER E A 5310-04498. 2 L 7 2 4F RT A16WE 20080603 CE 2008 6 3 GUUA05200801 1 20080520 A 3260 SQUAT SWITCH BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT MLG LOOSE A GUUA O OTHER S AFFECT SYSTEMS CL CLIMB 1 SO 29 17541 UE203 FLIGHT: 9140 AFTER TAKEOFF, LANDING GEAR WILL NOT RETRACT. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT RESECURED RT LANDING GEAR SQUAT SWITCH. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A24CE E26NE 20080603 NM 2008 6 3 ASMF200805002 1 20080520 A 2781 106122629 SENSOR BOEING 737 73776Q 13845AA NM L/E SLAT FAILED W ASMF D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 23 997AM 30283 AIRCRAFT RETURNED TO PLATFORM, DUE TO LE FLAPS TRANSIT LIGHT TURNED ON AND TAKEOFF WARNING ACTIVATED. MAINT PERFORMED BI TE TO PSEU AND FSEU IAW FIM 32-09 TASK 801 AND FIM 27-51 TASK 801 INDICATING FAIL OF SLAT NR1 SENSOR. FSEU WAS REPLACED BUT FAIL CONTINUED, SO SLAT NR1 SENSOR WAS REPLACED IAW MM 27-88-11, TESTED CORRECT. DURING OVERNIGHT CHECK, LEADING EDG E FLAP/SLAT POSITION INDICATION SYS AND LEADING EDGE FLAP/SLAT PROXIMITY SENSOR WERE TESTED IAW MM 27-88-00-710-801 AND 27-88-11-700-801; CONDITION AND ADJUSTMENT OF SLAT NR1 SENSOR S995 WAS PERFORMED IAW MM 27-88-11 PAGES 413 AND 414, ALL CORRECT. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 DU4R2008207 1 20080518 A 5340 STRINGER CLIP BOEING 737 737448 13844BU NM FUSELAGE CRACKED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 742VA 24773 S/O 312001 OPS NR 24792 - CABIN BS 400 STR. 2L HAS CRACKED STRINGER CLIP. 2 L 7 2 4F RT A16WE 20080603 EA 2008 6 3 N6WA0080506 1 20080522 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 155GJ 10225 EMERGENCY LIGHT NOT WORKING. PERFORMED OPS CHECK ON EMERGENCY LIGHTS IAW AMM 33-51-17. 2 L 7 2 4F RT A21EA 20080603 CE 2008 6 3 GUUA05080805 1 20080508 A 5511 1016200144 SPAR CAP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HORIZ STAB CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81536 25881 UE152 DURING SCHEDULED ROUTINE MAINT DISCOVERED RT HORIZONTAL STABILIZER UPPER SPAR CAP EXFOLIATED. REPLACED RT HORIZONTAL ST ABILIZER UPPER SPAR CAP. 2 L 7 2 4T 4 T RT A24CE E26NE 20080603 CE 2008 6 3 DXTA200803078 1 20080526 A 3233 281723 ACTUATOR CESSNA 680 680CE 2076811 CE PWA JT15 JT15D5 52112 NE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 313QS 955 6800140 AFTER TAKE-OFF, LANDING GEAR WOULD NOT RETRACT. 2 L 7 2 4F 4 F RC T00012WI E25EA 20080603 CE 2008 6 3 AMWA188150 1 20080520 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE LT MLG MALFUNCTIONED A AMWA O OTHER P NO WARNING INDICATION AP APPROACH 1 CE 07 143YV 23387 15728 UE143 ON APPROACH FOR LANDING, WHEN GEAR WAS EXTENDED, LT MAIN GEAR HAD NO DOWN AND LOCKED INDICATION. CREW COMPLETED EMERGENC Y CHECKLIST AND DECLARED EMERGENCY. CREW AND TOWER CONFIRMED GEAR DOWN BUT UNABLE TO TELL IF IT WAS LOCKED. FLIGHT LANDE D SAFELY AND TAXIED CLEAR OF RUNWAY. MAINT REMOVED AND REPLACED LT MAIN LANDING GEAR ACTUATOR AND CLEARED DISCREPANCY. 2 L 7 2 4T RT A24CE 20080603 EA 2008 6 3 N6WA0080508 1 20080525 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A N6WA K NONE O OTHER NR NOT REPORTED 1 CE 03 164GJ 10256 5385- IAD. CEILING EMERGENCY LIGHT INOP. DEFERRED ITEM ON DMI 2488 IAW MEL 33-51-01-2A CAT C. 2 L 7 2 4F RT A21EA 20080603 EU 2008 6 3 MALA080108 1 20080525 A 3350 CIRCUIT BREAKER SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS TRIPPED A MALA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 15 425XJ 340B425 DURING TAXI OUT WITH BOTH ENGINES RUNNING, CIRCUIT BREAKER L8 POPPED. REMOVED AND REPLACED THE L8 BREAKER ON THE RT SID E. 2 L 7 2 4T RT A52EU 20080603 CE 2008 6 3 DJFA2008046 1 20080527 A 2150 73838433 ACM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL A/C BAY SEIZED E DJFA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 23 707LX 3091 7500078 WITH APU ONLY, OPERATING, SMOKE ENTERED COCKPIT/CABIN WEMAC VENTS HOT TO TOUCH. MAINT TROUBLESHOT SYS TO SEIZED AIR CYCL E MACHINE (FORWARD). REMOVED ACM, INSTALLED REPAIRED ACM, AND NEW COALESCER SOCK. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080603 EA 2008 6 3 SWIA200819636 1 20080304 A 5743 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT MLG CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 457SW 7773 LEFT MAIN GEAR BRAKE TRANSDUCER BRACKET IS CRACKED, FOUND AT C-CHECK. REPLACED TRANSDUCER BRACKET PER CRJ200 AMM 51-80- 00-400-802. 2 L 7 2 4F RT A21EA 20080603 SO 2008 6 3 SWIA200819694 1 20080406 A 5320 SUPPORT EMB 120 EMB120ER 3260203 SO BS 4992-5100 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 561SW 120335 LEFT FLOOR AND SIDEWALL SUPPORT IS CORRODED AT FS 4992 TO FS 5100, FOUND AT C-CHECK. COMPLIED WITH REPLACEMENT AND REPA IR PER EMB 120 SRM 51-30-10 AND 51-40-02. 2 L 7 2 4T RT A31SO 20080603 NM 2008 6 3 LYNX00015 1 20080520 A 3260 LIGHT BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA COCKPIT INOPERATIVE A 3LYA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 NM 21 506LX 4176 DURING FINAL APPROACH, ON FLIGHT 3391, WE HAD NO GREEN INDICATION OF THE NOSE LANDING GEAR, AFTER SELECTING THE GEAR TO THE DOWN POSITION. THE CREW DISCONTINUED THE APPROACH. THE TOWER ADVISED THE ALL (3) GEARS APPEARED DOWN AND THE NOSE L ANDING LIGHT WAS ILLUMINATED. THE CREW LEFT THE GEAR DOWN THE ENTIRE TIME SINCE THEY COULD FEEL THE NOSE GEAR HAD LOWER ED AND THERE WHERE NO OTHER CAUTION LIGHTS. WHILE IN CONTACT WITH MOC AND DISPATCH, THE CREW TESTED THE ADVISORY LIGHTS AND THE GREEN "DOWN" LIGHT WOULD NOT ILLUMINATE INDICATING THE BULB HAS BURNED OUT. THE CREW THEN RAN THE QRH AND THE B ACKUP INDICATORS, INDICATED THAT ALL 3 GREEN LIGHTS ILLUMINATED PROPERLY. THE CREW THEN DECLARED AN EMERGENCY APPROACH W 2 H 7 2 4T 4 T RT A13NM E00062EN 20080522 SO 2008 5 22 C2XA08IA122 1 20080506 A 3350 78241 INVERTER EMB 145 EMB145EP 3260221 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16927 145006 FLIGHT 3029, DURING POST FLIGHT INSPECTION THE CREW REPORTED AN EMERGENCY EXIT IDENTIFIER AT AN OVERWING TO BE INOPERATI VE. MAINT INSPECTED THE AC, AND REMOVED AND REPLACED THE NR (3) INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080522 NM 2008 5 22 R61A200800005 1 20080506 A 3260 8001901 UPLOCK SENSOR EMB ERJ170 ERJ170100SU 3260403 NM GE CF34 CF348E5 30061 NE MLG FAILED A R61A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 803MD 10841 17000015 CREW REPORTS THUMPING NOISE UNDER FEET DURING CLIMB OUT. NO EICAS MESSAGES NOTED. CREW FOLLOWED QRH, DIVERTED AND LANDED WITHOUT INCIDENT. MAINT TROUBLESHOT AIRCRAFT AND FOUND RT NR1 MLG UPLOCK SENSOR AND NR1 PSEM MODULE FAILED. REMOVED AND REPLACED UPLOCK SENSOR AND PSEM MODULE. SYSTEM OPERATIONAL CHECK GOOD AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT A56NM E00063EN 20080522 SO 2008 5 22 C2XA08RI058 1 20080502 A 3320 BR90002 BALLAST EMB 145 EMB145EP 3260221 SO LAV LIGHT INOPERATIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14940 145033 FLIGHT 2674 - FLIGHT CREW REPORTED BURNING SMELL IN LAVATORY. MX REMOVED AND REPLACED LIGHT BALLAST OVER LAVATORY MIRRO R AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20080522 CE 2008 5 22 DXTA200803054 1 20080511 A 3260 6839 BULB RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE731* 01518 WP MLG BURNED OUT E DXTA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 07 880QS 258570 PRIMARY NOSE GEAR GREEN DOWN ANNUNCIATOR DID NOT ILLUMINATE PRIOR TO LANDING. REMOVED 2 EA UNSERVICEABLE LIGHT BULBS. I NSTALLED 2 EA NEW LIGHT BULBS. OPERATIONAL CHECK WAS FOUND TO BE SATISFACTORY. ACCOMPLISHED IAW MM 33-10-00. 2 L 7 2 4F 4 F RT A3EU E6WE 20080522 CE 2008 5 22 DXTA200803055 1 20080511 A 3240 215672 BRAKE ASSY CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C 03047 GL MLG LEAKING E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 964QS 2025 2025 7500164 RT BRAKE GRABS WITH MINIMAL PRESSURE APPLIED TO BRAKE PEDAL AND JERKS AIRPLANE IN SAME DIRECTION. REMOVED AND REPLACED NR 3 MAIN BRAKE ASSY. IAW MM 32-42-01 AND BRAKE BEEDING IAW MM 32-42-00 OPS CHECK LEAK CHECKS GOOD. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080522 GL 2008 5 22 U0GA119634 2 20080509 A 7200 250C20B ENGINE BOLKMS 105 BO105CBS 5626008 EU ALLSN 250C 250C20 03013 GL NR 2 INOPERATIVE E U0GA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 SW 03 290EH S850 DURING APPROACH, ENGINE 2 MADE EXPLOSIVE SOUND, NG WENT TO 0 TORQUE WENT TO 0. FUEL SUPPLY WAS CUT OFF, ENGINE 1 WAS IN CREASED TO MAX AND A RUN ON LANDING WAS MADE WITHOUT EVENT. TO RUNWAY 17. 1 G 7 2 3U 3 U NC H3EU E4CE 20080522 NM 2008 5 22 DU4R2008192 1 20080504 A 5315 FLOORBEAM BOEING 737 737 UTILSYS NM CFMINT CFM56 CFM567B27 13046 NE BS 986-987 CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 321TZ 29249 S/O 245007 OPS NR 25007 - STA 986.5 FLOORBEAM HAS CORROSION ON UPPER T-CAP SURFACE BL 32L TO BL 32R. CORROSION OUT OF LI MITS. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080522 SO 2008 5 22 BKE2008F00003 1 20080314 A 5610 1159SCB31024 WINDSHIELD GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU COCKPIT CRACKED E BKEA O OTHER O OTHER CR CRUISE 1 WP 01 297GB 1208 PILOT REPORTED, IN FLIGHT, THAT THE CO-PILOTS WINDSHIELD OUTER PANE CRACKED AND SHATTERED. THE INNER PANE HELD. PILOT DIVERTED AND REPAIRS ARE IN PROGRESS. SUSPECT THE THE WINDSHIELD HEAT FAILED. (K) 2 L 7 2 4F 4 F RT A12EA E25NE 20080522 CE 2008 5 22 GLBA20061098 1 20080501 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA BS 177 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 154GL UE154 FUSELAGE FRAME AT FS 177.3 CRACKED AT STRINGER 9R CUTOUT. CRACK APPROXIMATELY .6 INCH IN LENGTH. MAINTENANCE REPAIRED FU SELAGE FRAME AT FS 177.3 AT STRINGER 9R RELIEF HOL IAW. SRM 51-70. REPAIR APPROXIMATELY 5 INCH BY 2.5 INCH. 2024-T3 .07 1. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1. 2 L 7 2 4T 3 T RT A24CE E2NE 20080522 NE 2008 5 22 2008003 2 20080514 A 7200 ENGINE BOEING 727 727212 138407G NM PWA JT8 JT8D17 52049 NE VIBRATION INOPERATIVE A I5PA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 86425 21459 688039 ON TAKEOFF, CREW EXPERIENCED A SLIGHT VIBRATION ON NR 3 ENGINE, VERIFIED ALL PARAMETERS NORMAL, CONTINUED WITH TAKEOFF C REW THEN NOTICED A LOSS OF OIL ON NR 3 ENGINE. SHUTDOWN ENGINE AND RETURN TO DEPARTURE. ON INSPECTION, FOUND BLADE DAMA GE, 2ND STAGE FAN BLADE. 2 L 7 3 4F 4 F A3WE E2EA 20080522 NM 2008 5 22 DU4R2008198 1 20080505 A 5311 FRAME BOEING 737 737448 13844BU NM CFMINT CFM56 CFM563B2 13802 EU BS 188-196 CRACKED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 742VA 24773 S/O 312001 OPS NR 27955 - FLIGHT COMPARTMENT HAS CRACK AT SHEAR WEB FRAME BS 188 - 196 LT FLOOR LEVEL (CRACK EMANATING A T EDGE CUT OUT). 2 L 7 2 4F 4 F RT A16WE E21EU 20080522 CE 2008 5 22 DXTA200803057 1 20080513 A 2710 FEEL SENSOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C 03047 GL AILERONS BINDING E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 989QS 7500089 IN FLIGHT, AILERON FLIGHT CONTROLS ARE BINDING WHILE TURNING BOTH LT AND RT. REMOVED AND REPLACED ARTIFICIAL FEEL BUNGE E. PERFORMED OPS CHECKS AND ADJUSTMENTS ALL OK. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080522 NM 2008 5 22 ASMF200805001 1 20080504 A 5341 STRUCTURE BOEING 737 737* NM GALLEY DOOR DENTED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 904AM 28262 CAPTAIN REPORTED A DENT IN RT FWD GALLEY DOOR. MAINT PERFORMED INSPECTION FOUNDING A DENT OF .2500 INCH DIAMETER AND .12 50 INCH DEPTH, BETWEEN BS 309 AND 323 AND LONGERONS 17 AND 21 IN RT FWD GALLEY DOOR, WITHIN LIMITS IAW SRM 53-00-01, FI GURE 103. 2 L 7 2 4F RT A16WE 20080522 NM 2008 5 22 DU4R2008202 1 20080502 A 5330 SKIN BOEING 737 737 UTILSYS NM CFMINT CFM56 CFM567B27 13046 NE BS 440-460 DENTED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 321TZ 28249 S/O 245007 OPS NR 24892 - FUSELAGE EXT. SKIN, BETWEEN S-19L AND S-20L BS 440 TO BS 460 HAS DENT OUT OF LIMITS. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080522 NM 2008 5 22 DU4R2008200 1 20080502 A 5315 FLOORBEAM BOEING 737 737448 13844BU NM CFMINT CFM56 CFM563B2 13802 EU BS 312 CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 742VA 24773 S/O 312001 N/R 24703 - CORROSION ON TOP OF FLOORBOARD IN GOUGE BS 312 LBL 52 TO LBL 8, AND NUMEROUS PLACES AT RBL 0 TO R BL-54. 2 L 7 2 4F 4 F RT A16WE E21EU 20080522 CE 2008 5 22 GUUA05110804 1 20080511 A 5524 1016200131 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 178YV 27822 UE178 DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED RT CTR ELEVATOR HINGE BRACKET HAS CORROSION. REPLACED RT CTR ELEVATOR HINGE BRACKET. 2 L 7 2 4T 3 T RT A24CE E2NE 20080522 CE 2008 5 22 DXTA200803069 1 20080519 A 3241 GPP125052 PRESSURE SWITCH CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE ANTI SKID SYS INOPERATIVE E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 814QS 306 5600776 WHILE TAKING THE RUNWAY FOR DEPARTURE THE LOW BRAKE PRESSURE - ANTI-SKID ANNUNCIATOR LIGHT ILLUMINATED. REMOVED DEFECTI VE PUMP MOTOR PRESSURE SWITCH AND INSTALLED REPAIRED SWITCH. SYSTEM CHECKS GOOD REF MM 32-20-00. TAXI CHECKED GOOD I AW PILOTS HANDBOOK. 2 L 7 2 4F 4 F RT A22CE E00053EN 20080522 CE 2008 5 22 GUUA05130801 1 20080513 A 5540 10164001415 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RUDDER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87557 UE246 DURING SCHEDULED ROUTINE MAINT, DISCOVERED UPPER RUDDER HINGE BRACKET EXFOLIATED. REPLACED UPPER RUDDER HINGE BRACKET. 2 L 7 2 4T 3 T RT A24CE E2NE 20080522 CE 2008 5 22 GUUA05070801 1 20080507 A 5210 CABLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA CABIN DOOR OUT OF ADJUST A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 190YV UE190 PILOT REPORTED CABIN DOOR CAMS DO NOT ALIGN WITH BOLTS AND IS HARD TO CLOSE. ADJUSTED AIRSTAIR DOOR STRUT CABLE. 2 L 7 2 4T 3 T RT A24CE E2NE 20080522 CE 2008 5 22 DJFA2008044 1 20080504 A 2133 OUTFLOW VALVE BEECH MU300 400A 1155402 CE CABIN PRESSURE OBSTRUCTED E DJFA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 23 470LX RK478 CREW REPORTED WHILE CLIMBING THROUGH FL200 THE CABIN LOW PRESSURE LIGHT ILLUMINATED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED. MAINT FOUND A TY-WRAP LODGED IN THE OUTFLOW VALVE. THE DEBRIS WAS REMOVED AND SUBSEQUENT OPERATIONA L CHECKS WERE SUCCESSFUL. 2 H 7 2 4F RT A16SW 20080522 2008 5 22 DXTA200803013 4 20080423 A 2210 LMP5001P RELAY CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE AUTO PILOT INOPERATIVE E DXTA O OTHER O OTHER CR CRUISE 1 GL 07 686QS 1531 5605661 UNCOMMANDED EMERGENCY DESCENT WITH AUTOPILOT ENGAGED AT FL400. REPLACED RELAY KC009 AND CONNECTOR. IAW MFG WIRING DIAGRA M MAN 20-10-04. OPS CHECK GOOD. RELAY P/N LMP5001P S/N NSN/CONNECTOR LMS01T-TL S/N NSN / CONNECTOR P/N LMP4001S S/N NSN. 2 L 7 2 4F 4 F RT A22CE E00059EN 20080522 CE 2008 5 22 GUUA04290802 1 20080429 A 5524 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87551 24897 UE206 DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED RT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT OB ELEVATOR HINGE BRACKET 2 L 7 2 4T 3 T RT A24CE E2NE 20080522 CE 2008 5 22 DXTA200803067 1 20080519 A 3297 CONNECTOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C 03047 GL MLG LOOSE E DXTA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 07 941QS 7500141 GEAR BUMP HEARD AND FELT 3 TIMES DURING CLIMB. FOUND RT MLG DOOR LOOSE & RT UPLOCK SWITCH CONNECTOR LOOSE. TIGHTENED R T UPLOCK SWITCH CONNECTOR & ADJUSTED RT MLG DOOR. OPERATIONAL CHECKS GOOD ON GEAR SWING, ALSO, ACCOMPLISHED GEAR BUMP TR OUBLESHOOTING IAW MM CHAPTERS 32-30-00 &32-30-05. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080522 NM 2008 5 22 DXTA200803068 1 20080519 A 2720 C18009AA YAW DAMPER AMD FALC50 FALCON2000 2730170 NM CFE CFE73811B NE INOPERATIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 280QS 1065 1065 181 DURING LEVEL FLIGHT, ACCELERATING THROUGH 250KT AT 10,000 FT, THE AC EXPERIENCED A SUDDEN YAW TO THE RT WITH THE TRIM IN DICATOR AT ZERO. INSTALLED A NEW YAW DAMPER SVL-86A OPS CHECKED GOOD. ALL WORK DONE IAW F-2000 MM 22-105 22-104 2 L 7 2 4F 4 F RT A50NM E44NE 20080522 CE 2008 5 22 DXTA200803071 1 20080519 A 3260 BULB CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007A 03030 GL LT MLG INDICATOR INOPERATIVE E DXTA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 07 932QS 7500032 LT MAIN GEAR INDICATOR LIGHT NOT ILLUMINATED WHEN GEAR HANDLE IS DOWN. RELAMPED LT MLG LIGHT IAW MM 33-10-00. CYCLED LA NDING GEARS SEVERAL TIMES, ALL ANNUNCIATORS FUNCTIONED NORMALLY AS PER MM 32-10-00. OPS CHECK OK. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080521 NM 2008 5 21 2008UALA02767 1 20080512 A 2120 AIR FILTER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE DIRTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 209UA 30215 EQUIPMENT COOLING HORN ON AND EQUIP COOLING EICAS. FOUND DIRTY AIR FILTER. REPLACED AIR FILTER PER MM -21-27-02. OP C HECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080523 WP 2008 5 23 UPS08852194 1 20080420 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 DOUBLER LOOSE, WORN AND NUMEROUS SCREWS PULLING THROUGH ALONG BOTTOM EDGE OF LEFT OUTBOARD FLAP L/E B ETWEEN 219 AND 340. REPAIRED BOTTOM EDGE OF OUTBOARD FLAP L/E AT STA 219 AND 340 IAW SRM 57-07 -01-0, SRM 57-02-00-0 FI G 002, SRM 57-01-08 AND SRM 51-01-21. 2 L 7 4 4F RT 4A25 20080521 SO 2008 5 21 LR7A08069 1 20080513 A 3010 351783 MOUNT BRACKET LKHEED 382 382G 526414U SO RT WING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5712, FOUND RT OW LEADING EDGE DIFFUSER MOUNTING BRACKET P/N 351783 CRACKED OW S205-255R. WELD REPAIR ACCOMPLISHED IAW LAC MEA 382-30-08-029. 2 H 7 4 4T A1SO 20080521 NM 2008 5 21 F3LA200800264 1 20080425 A 5311 D53571554202 FRAME AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 DURING C2 C CHECK INSPECTION NOTED FRAME 75 DAMAGED STRINGER 26 LEFT AND STRINGER 26 RIGHT. MAINTENANCE REPLACED FRAME 75 AND ALL ATTACHING SHEAR TIES IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30262. UPON COMPLETION OF THE REPAIR I T WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080521 NM 2008 5 21 AALA200801025 1 20080420 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 DFW - EMERGENCY LIGHT AT SEAT 36G INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 36G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 EA 2008 5 21 MASA200800369 1 20080505 A 2620 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 7264V 7264 ASH FLT 2922 COS - FIRE BOTTLE WARNING MESSAGE. OPS CHECKED THE FIRE BOTTLE WARNING SYSTEM, NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 20080521 EU 2008 5 21 2008UALA02513 1 20080429 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN ODOR A UALA A UNSCHED LANDING W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 425UA 508 UNIDENTIFIED PLASTIC BURNING SMELL FROM ROW 24. SMELL INTENSIFIED. FLIGHT DIVERTED. NO SMELL NOTICED ON AC ARRIVAL. TURNED RECIRC FANS BACK ON, RAN PACKS. TURNED ALL CABIN LIGHTS ON. RAN VIDEO SYS, NO SMELL NOTICED. CKD GALLEY AREA, NO SMELLS NOTICED. TURNED ON COFFEEMAKERS, OVENS, HOT PLATES AND NO SMELL. LOWERED OVERHEAD CEILING PANEL AND VISUAL C K OK. CHECKED CARGO PITS AND NO SMELLS. AC OK FOR CONTINUED SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080521 EU 2008 5 21 2008UALA02528 1 20080430 A 3251 GA712823 CONTROL SERVO AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG STEERING FAILED A UALA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 29 413UA 470 PER CREW, AIRCRAFT PULLS TO LEFT AT TAXI SPEED, REQUIRES 2 DEGREES OF TILLER DEFLECTION. SUPPLEMENTAL DATA UPDATE, NOSE WHEEL STEERING CONTROL SERVO FAILING. REPLACED NOSE WHEEL STEERING CONTROL SERVO, TAXI TEST GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080521 CE 2008 5 21 GLBA20061099 1 20080502 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA FUSELAGE DAMAGED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 154GL UE154 RT UPPER ICE SHIELD DIVIDED INTO (2) PIECES AT APPROXIMATE LOCATION OF STRINGER 8R FROM F.S. 183.25 TO F.S. 220.75. MAIN T REPLACED THE RT UPPER ICE SHILED IAW. SRM 51-40. RII INSP COMPLIED WITH IAW TASKCARD 8.2.1. 2 L 7 2 4T 3 T RT A24CE E2NE 20080521 SO 2008 5 21 GUUA05090802 1 20080509 A 2710 SHROUD EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AILERON BROKEN A GUUA O OTHER O OTHER AP APPROACH 1 SO 29 282AS 120226 FLIGHT: 9144, DURING FINAL APPROACH AILERONS JAM WITH AUTO PILOT OFF.INSPECTED, FOUND LT AILERON IB BALANCE WEIGHT TAB S BROKEN AND NOT ATTACHED. INSTALLED NEW LT BALANCE WEIGHT ASSY SHROUD. OPS CHECK, AILERONS NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 20080521 CE 2008 5 21 GUUA04280801 1 20080428 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA CABIN ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 81536 UE152 DURING FLIGHT, STRONG FUEL SMELL IN THE CABIN WITH BLOWERS ON HIGH. RAN BOTH ENGINES COULD NOT DETECT ODOR TREATED CARP ET AS NEEDED. 2 L 7 2 4T 3 T RT A24CE E2NE 20080521 NM 2008 5 21 AALA200801091 1 20080426 A 3350 LENS BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 962AN 30858 DFW - EMERGENCY LIGHT AT SEAT ROW 16DEF MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 16DEF. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080521 NM 2008 5 21 AALA200801081 1 20080424 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 DFW - EMERGENCY LIGHT AT SEAT 40C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 40C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 NM 2008 5 21 AALA200801053 1 20080422 A 3397 WIRE BOEING 777 777223 1385213 NM CABIN EXPOSED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 DFW - EMERGENCY LIGHT WIRING AT SEAT 36D NOT STOWED. STOWED WIRING FOR EMERGENCY LIGHT AT SEAT 36D. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080521 EU 2008 5 21 AALA200801066 1 20080423 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7055A 462 JFK - EMERGENCY LIGHTS AT RIGHT AISLE FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT AISL E FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20080522 NM 2008 5 22 F3LA200800273 1 20080425 A 5330 SR531990A01201 SKIN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 938FR 5588 2406 REFERENCE NON ROUTINE C043440. DURING C2 C-CHECK INSPECTION NOTED: WHILE JACKING THE AIRCRAFT, THE TAIL JACK STAND WAS N OT REMOVED FROM THE TAIL JACK PAD WHICH CAUSED DAMAGE TO THE AIRCRAFT SKIN, STRINGERS, FRAMES 72 TO 75 AND BETWEEN STRIN GERS 26 LT AND 26 RT. MAINT PERFORMED REPAIR TO AC SKIN AND STRUCTURE IAW THE REQUIREMENTS OF EA A9-53R-30262. UPON COMP LETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080522 EA 2008 5 22 N6WA0080503 1 20080505 A 3397 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE EMERGENCY LIGHTS LOOSE A N6WA K NONE L NO TEST IN INSP/MAINT 1 CE 03 156GJ 10227 RT ROW 12 LOWER EMERGENCY EXIT LIGHT INOPERATIVE. INSPECTED AND FOUND CONNECTOR LOOSE ON NR 4 EMERGENCY BATTERY. RECON NECTED AND OPS CHECKED GOOD IAW AMM 33-51-17. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080522 EA 2008 5 22 N6WA0080502 1 20080505 A 3397 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE EMERGENCY LIGHT LOOSE A N6WA K NONE L NO TEST IN INSP/MAINT 1 CE 03 156GJ 10227 RT AFT OVERWING EMERGENCY LIGHT INOP. INSPECTED AND FOUND CONNECTOR LOOSE ON NR 4 EMERGENCY BATTERY. RESECURED CONNECT OR IAW AMM 33-51-17, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080522 NM 2008 5 22 200805071 1 20080505 A 2780 FLAP SYSTEM EMB ERJ170 ERJ170100SE 3260406 NM GE CF34 CF348E5 30061 NE LE FLAPS MALFUNCTIONED A UHLA O OTHER O OTHER DE DESCENT 1 GL 11 636RW 17000052 FLIGHT 7533, ON DESCENT, CREW SELECTED FLAPS (1) AND GOT SLAT FAIL MESSAGE FOLLOWED BY SPOILER FAULT AND SHAKER ANTICIPA TED. RECYCLED TO ZERO AND MESSAGES WENT AWAY. ON SECOND RECYCLE SLAT FAIL MESSAGE REMAINED. CREW DECLARED AN EMERGENCY A ND LANDED WITHOUT INCIDENT. ON-CALL MAINTENANCE CLEARED SF-ACE INHIBITS AND RELEASED MOTOR BRAKE. HAS NOT REPEATED THIS DATE 05/07/2008. 2 L 7 2 4F 4 F RT A56NM E00063EN 20080522 CE 2008 5 22 HSYA20080430 1 20080430 A 2731 TRIM SYSTEM BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA HARTZL HCB4M HCB4MP3 GL ELEVATOR STUCK E HSYA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 NM 05 319BH UB36 DURING A TRAINING FLIGHT 25 MILES EAST OF AIRPORT, AT 5000 FT, THE ELEVATOR TRIM CONTROL BOUND AND JAMMED UP. AFTER ATTE MPTS TO FREE UP THE TRIM WERE UNSUCCESSFUL, THE CREW DECLARED AN EMERGENCY WITH CONTROL AND LANDED ON WITHOUT INCIDENT. MX PERFORMED A VISUAL INSPECTION OF THE ELEVATOR TRIM CONTROL CABLES ROUTING, NO DEFECTS WERE NOTED. MX LUBRICATED THE ELEVATOR TRIM ACTUATOR AND VERIFIED PROPER CABLE TENSIONS. NO DEFECTS WERE NOTED AFTER PERFORMING OPERATIONAL AND FUNCTI ONAL CHECKS OF THE ELEVATOR TRIM SYSTEM. THE AC WAS RELEASED FOR THE PURPOSES OF A TEST FLIGHT. MANUAL AND ELECTRICAL OP ERATION OF THE ELEVATOR TRIM DURING THE TEST FLIGHT WAS FOUND TO BE NORMAL WITH NO FURTHER DISCREPANCIES NOTED. THE AC W 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P56GL 20080522 CE 2008 5 22 DXTA200803061 1 20080514 A 2720 RUDDER CONTROL CESSNA 750 750 2076810 CE MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 918QS 7500223 DURING CLIMBOUT, PASSING THROUGH FL300, FELT A/C TAIL OSCILLATING RAPIDLY L/R. OBSERVED UPPER RUDDER CARAT ON FLT CTL P AGE MOVING RAPIDLY L/R WITH ABT .2500 OF ITS DISPLACEMENT. REMOVED AND REPLACED "B" CHANNEL YSAC IAW MM 27-24-01. OPERA TIONAL CHECKS GOOD. 2 L 7 2 4J RT T00007WI 20080522 NE 2008 5 22 A8OA200800001 2 20080422 A 7200 JT15D5 ENGINE BEECH MU300 400BEECH CE PWA JT15 JT15D5 52112 NE ZONE 400 SEIZED E A8OA E A ENGINE SHUTDOWN UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SO 11 913MC 1046 RJ22 PCE100136 UPON VR DEPARTING, RT ENGINE FAILED. DETECTED BY THE FLIGHT CREW AFTER HEARING (2) LOUD POPS FOLLOWED BY INCREASE OF IT T AND FUEL FLOW. ENGINE WAS SHUTDOWN AND AC RETURNED TO DEPARTURE UNEVENTFULLY. ENGINE REMOVED AND CURRENTLY IN TEARDO WN. A SUPPLEMENT WILL BE SUBMITTED, INCLUDING DETAILS IN SECTION 6, UPON DISCOVERY OF CAUSE OF FAILURE. SUPPLEMENTAL: ENGINE TEARDOWN REPORT RECEIVED. UNDER THE SUMMARY AND CONCLUSION, THEIR STATEMENT OF PROBABLE CAUSE OF DISTRESS IS AS FOLLOWS: HIGH TURBINE BLADE FAILURE: DAMAGE TO THE HOT SECTION OF THE ENGINE IS BELIEVED TO BE RELATED TO THE LIBERATIO N OF ONE HIGH TURBINE BLADE NEAR OR AT THE ROOT OF THE BLADE. DOWN STREAM DAMAGE OF THE TURBINE IS DUE TO LIBERATION OF 2 H 7 2 4F 4 F RT A16SW E25EA 20080522 SO 2008 5 22 C2XA08RI062 1 20080506 A 3350 66903 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 19966 145131 DURING ROUTINE MAINT, MX FOUND EMERGENCY LIGHT FLOOR STRIP AT ROWS 1 AND 2 INOPERATIVE. MX REMOVED AND REPLACED LIGHT ST RIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080522 SW 2008 5 22 MD0519081 1 20080510 A 6510 206040369101 DRIVE SHAFT BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL TAIL ROTOR SCORED E EVCA K NONE O OTHER IN INSP/MAINT 1 CE 03 28AE 51077 CAE900070 COAX CABLE FROM ANTENNA MOUNTED ON OIL RESERVOIR COWLING SCORED THE (NR 3) TAIL ROTOR DRIVESHAFT SEGMENT. 1 G 7 1 3U 3 U H2SW E1GL 20080522 CE 2008 5 22 BKE2008F00002 1 20080314 A 5310 5410600008 DOOR FRAME LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP PAX DOORWAY UNSERVICEABLE E BKEA K NONE O OTHER IN INSP/MAINT 1 WP 01 125LR 11097 032 85172C DURING PREFLIGHT, PILOT NOTED THE MAIN ENTRY DOOR WAS HARD TO CLOSE, ON INSPECTION BY MAINT, FRAME 15 IS THE FRAME THAT BORDERS THE AFT SIDE OF THE MAIN ENTRY DOOR TO HAVE CORROSION THAT HAD PROGRESSED TO THE POINT OF EXFOLLIATION AND START ED INTERFERING WITH THE DOOR SNUBBER OPERATION. THE AC WAS EVALUATED, PHOTOS AND REPORTS SENT TO MFG ENGINEERING FOR EV ALUATION AND WITH RECOMMENDATION, A SPECIAL FLIGHT PERMIT WAS OBTAINED TO RELOCATE THE AC FOR REPAIRS. (K) 2 L 7 2 4F 4 F A10CE E6WE 20080522 2008 5 22 4911905172008 4 20080517 A 3413 060002600 VERTICAL GYRO BELL 430 430 1182150 SW ALLSN 250C 250C40B 03032 NE COCKPIT FAULTY E QMLA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 557UH 49119 DURING CRUISE FLIGHT, PILOT FELT A VIBRATION IN THE AC FOLLOWED BY ATTITUDE EXCURSIONS IN THE PITCH AXIS. THIS OCCURRED OVER A PERIOD OF APPROXIMATELY (2) MINUTES AND FELT SIMILAR TO GOING OVER A SERIES OF SPEED BUMPS. THE PILOT ELECTED TO MAKE A PRECAUTIONARY LANDING AND NOTIFIED MAINTENANCE. TROUBLESHOOTING INDICATES THE VERTICAL GYRO AT FAULT. 1 G 7 2 3U 3 U RT H9SW E1GL 20080522 SW 2008 5 22 408UT051308 1 20080513 A 2140 407H201203 HEATER BELL 407 407 1182206 SW ALLSN 250C 250C47B GL CABIN FUMES E M3XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 07 408UT 30 53808 CAE848108 FUMES AND SMOKE IN THE COCKPIT, DURING FLIGHT, RESULTING IN A UNSCHEDULED LANDING. 1 G 7 1 3U 3 U O H2SW E1GL 20080522 CE 2008 5 22 CWQR200802 1 20080417 A 5320 661503517 SUPPORT BRACKET CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE FUSELAGE CRACKED B DXTA K NONE O OTHER IN INSP/MAINT 1 GL 05 677QS 5605367 DURING A PHASE 1-4 INSPECTION FOUND A CRACKED ECU SUPPORT BRACKET. THE CRACK STARTED AT THE EDGE OF THE BRACKET AND EXTE NDED 2.25 INCH. AND WAS ALMOST TO A RIVET THAT SECURES THE OTHER PART OF THE BRACKET ASSY. AN SCR AND PHOTO HAS BEEN SUB MITTED TO MFG UNDER NR 354883. 2 L 7 2 4F 4 F RT A22CE E00059EN 20080522 SO 2008 5 22 FDKA200805187 1 20080504 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHTS LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6042, EMERGENCY LIGHT ABOVE ROW 12 WAS INOPERATIVE. MX RESECURED CONNECTORS. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080522 EU 2008 5 22 401104242008 1 20080424 A 2121 050143 BLOWER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE EVAPORATOR BURNED E QMLA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 129LN 4011 WHILE IN CRUISE FLIGHT, RETURNING TO BASE (WITH NO PATIENT ON BOARD) THE MED CREW REPORTED A SMELL OF BURNING RUBBER COM ING OUT OF THE AIR CONDITIONING VENTS. PILOT PERFORMED A PRECAUTIONARY LANDING WITHOUT INCIDENT IN A FIELD. MAINT INSPEC TED THE A/C SYSTEM AND FOUND NO EVIDENCE OF A/C SYS FAILURE. SUSPECTED INTERNAL FAILURE OF UPPER EVAPORATOR BLOWER. SYST EM DEACTIVATED AND DEFERRED IAW MEL. AIRCRAFT RETURNED TO BASE WITH NO FURTHER (SMELL). LATER, CHANGED UPPER EVAPORATOR BLOWER. 1 G 7 1 3U 3 U H9EU E19EU 20080522 EU 2008 5 22 7211051508 1 20080515 A 5302 1053025151 FRAME BOLKMS BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE TAILBOOM CRACKED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 117VU 8104 7211 DURING SCHEDULED INSP, A 1 INCH LONG CRACK WAS DISCOVERED ON TAILBOOM FRAME 10L AT THE 3:00 POSITION. 1 G 7 2 3U 3 U H13EU E5NE10 20080522 NM 2008 5 22 F3LA200800275 1 20080518 A 2530 4110010105 COFFEEMAKER AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE GALLEY ODOR A F3LA H J DEACTIVATE SYST/CIRCUITS DUMP FUEL B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 935FR 17 2400 REFERENCE LOG PAGES 369125 AND 369126. DURING FLIGHT THE FA REPORTED A STRONG ODOR AND HEAT. MAINT RAN APU AND ENGINE (1 ) AND (2) AT IDLE WITH BOTH PACKS ON. MAINT VISUALLY INSPECTED CARGO PITS, FWD AVIONICS COMPARTMENTS AND FUSELAGE, AFT OF PRESSURE BULKHEAD NO UNUSUAL ODERS NOTED. MAINT INSPECTED CABIN AND FOUND AND UNUSUAL ODOR COMING FROM AFT COFFEE MAK ERS WHILE BREWING. PLACED NR (2) AFT COFFEE MAKER ON NEF 25-99-30AD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080522 SO 2008 5 22 GUUA05120801 1 20080512 A 3350 12021299001 LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN INOPERATIVE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 280AS 120231 DURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED LT AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LT AFT EMERGENCY LIGHT AS SY. 2 L 7 2 4T 4 T RT A31SO E20NE 20080522 EA 2008 5 22 N6WA0080504 1 20080517 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE CABIN INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 151GJ 10216 AFT EMERGENCY CEILING LIGHT INOP. DEFERRED LIGHT IAW MEL 33-51-01-2A. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080522 NM 2008 5 22 QXEA200800496 1 20080515 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM LT AFT UNKNOWN A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 417QX 4086 GEG - FLIGHT 2395 - FA COULD NOT CLOSE THE LEFT REAR PASSENGER DOOR. MAINTENANCE RESET THE DOOR. OPERATIONAL CHECKS GOO D. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080522 NM 2008 5 22 QXEA200800497 1 20080518 A 5270 401020101 PROXIMITY SENSOR BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR MALFUNCTIONED A QXEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 418QX 4143 IDA0 FLIGHT 2269 - AFT PASSENGER DOOR INDICATES NOT CLOSED ON THE MFD DOOR PAGE, EVEN THOUGH IT IS CONFIRMED TO BE CLOSE D. MAINTENANCE REPLACED THE PROX SENSOR FOR THE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080522 NM 2008 5 22 QXEA200800498 1 20080517 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM AFT PAX UNKNOWN A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 404QX 4046 SEA - FLIGHT 2257 - AFT PASSENGER DOOR HARD TO CLOSE. MAINTENANCE CLEANED DEBRIS FROM THE DOOR. DOOR OPERATIONAL CHECK S GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080522 EU 2008 5 22 MALA080096 1 20080509 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 236-258 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 452XJ 340B452 RAIL CORRODED AT STA 236 TO STA 258 BL 18.3. REPLACED RAIL P/N 7253710-131 IAW SRM 51-40-27. 2 L 7 2 4T RT A52EU 20080522 NM 2008 5 22 QXEA200800454 1 20080507 A 6123 POTENTIOMETER DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS OUT OF ADJUST A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 345PH 476 SEA - AUTOFEATHER SLOW TO ARM. ARMS ABOUT 90 PERCENT TORQUE. MAINTENANCE PLACED ON MEL 61-2. AIRCRAFT RETURNED TO SER VICE. MEL CLEARED BY RIGGING THE ARMING POTS IAW 76-10-15-820-802. NOW ARMS AT 78-80 PERCENT. AIRCRAFT RETURNED TO SE RVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080522 NM 2008 5 22 QXEA200800455 1 20080507 A 5210 85217555003 SEAL BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR DAMAGED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 400QX 4030 SEA - LEFT AFT PASSENGER DOOR IS HARD TO CLOSE. REPLACED THE DOOR SEAL. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080523 NM 2008 5 23 USAA920081031 1 20080508 A 5320 CHANNEL BOEING 757 7572B7 1384964 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 930UW 27145 CLT - MAJOR REPAIR - DROP IN - CRACKED CHANNEL, BS 845, LBL 2.90. REPAIRED CHANNEL, BS 845, LBL 2.90 IAW EA 100458. 2 L 7 2 4F RT A2NM 20080523 2008 5 23 USAA920081042 4 20080511 A 2565 HOSE BOEING 767 7672B7ER 1385107 NM ESCAPE SLIDE COLLAPSED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 C4 CHECK - RT WING ESCAPE SLIDE INFLATION HOSE AT SLIDE COMPARTMENT IS COLLAPSED. REMOVED AND REPLACED RIGHT WING ESCAP E SLIDE INFLATION HOSE AT SLIDE COMPARTMENT IAW AMM 25-65-02. 2 L 7 2 4F RT A1NM 20080523 SO 2008 5 23 FDKA200805196 1 20080507 A 5700 BONDING STRAP EMB 145 EMB145LR 3260212 SO WING CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 837MJ 145367 BONDING STRAP IS CORRODED ON PANEL 5731. THE CORRODED STRAPS HAVE BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 20080523 NM 2008 5 23 USAA920081024 1 20080422 A 5311 FRAME BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 440, S8L. REPAIRED FRAME, BS 440, S8L IAW TASK CARD MIC53002. 2 L 7 2 4F RT A16WE 20080523 NM 2008 5 23 USAA920081026 1 20080506 A 5320 907822 STRAP BOEING 737 7373S3 1384711 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - CRACKED STRAP L1 DOOR CUTOUT, BS 312, S8L. REPAIRED STRAP L1 DOOR CUTOUT, BS 312, S8L IAW BOEING DRAWING 90-7822. 2 L 7 2 4F RT A16WE 20080523 EU 2008 5 23 USAA920081029 1 20080506 A 5347 SEAT TRACK AIRBUS 320 A320214 3930316 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 105UW 868 PIT - MAJOR REPAIR - C11 CHECK - CORROSION ON SEAT TRACK, BS 808/ FR 20, -Y765. REPAIRED SEAT TRACK, BS 808/ FR 20, -Y 765 IAW A320 SRM 53-11-15. 2 L 7 2 4F RT A28NM 2008041500171 20080415 00171 EU 2008 4 15 F3LA200800152 1 20080407 A 5320 D53480019222 PLATE AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 C CHECK, INSPECTION REPORTED A CRACK WAS FOUND IN THE MOULLION PLATE LOCATED AFT OF THE L2 DOOR FRAME AT TH E JOINT SHEET ATTACH POINT. MAINTENANCE REMOVED AND REPLACED THE MOULLION PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPH 6. UPON COMPLETION OF THE INSTALLATION OF THE NEW MOULLION PLATE, IT WAS INSPECTED AND FOU ND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041500184 20080415 00184 NM 2008 4 15 08FDEA01392 1 20080414 A 5311 AFA00283 FRAME DOUG MD11 MD11F 3023600 NM BS 1681 L12R DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 525FE 48565 MAIN DECK, RIGHT FUSELAGE FRAME AT STATION 1681, LONGERON 12 RIGHT FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYC LES TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041500186 20080415 00186 NM 2008 4 15 08FDEA01394 1 20080414 A 5311 AFA00203 FRAME DOUG MD11 MD11F 3023600 NM BS 1701 L12L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 525FE 48565 MAIN DECK, LEFT FUSELAGE FRAME AT STATION 1701, LONGERON 12 LEFT FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041500187 20080415 00187 NM 2008 4 15 08FDEA01395 1 20080414 A 5311 AFA00193 FRAME DOUG MD11 MD11F 3023600 NM BS 1721 L12L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 525FE 48565 MAIN DECK, LEFT FUSELAGE FRAME AT STATION 1721, LONGERON 12 LEFT FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080603 SO 2008 6 3 SWIA200819695 1 20080406 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 561SW 120335 STRINGER NR 10 ON RIGHT WING BETWEEN RIBS NR 8 AND NR 9 IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH MAJOR REPAIR ON RIG HT WING PER SRM 57-20-03. 2 L 7 2 4T RT A31SO 20080603 EU 2008 6 3 CPCP20080028 1 20080502 A 5320 THRESHOLD AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 499AT 499 RT FR 36-39 THRESHOLD CORRODED. RT THRESHOLD AT FR 36-39 REPLACED IAW SRM NR 51-25-01/03. THRESHOLD FABRICATED ON NRWC NR 207385. 2 H 7 2 4T RT A53EU 20080603 EA 2008 6 3 SWIA200819672 1 20080228 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910SW 7566 FS 484 BRACKET AT LBL27 IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 20080603 CE 2008 6 3 DXTA200803030 1 20080428 A 2913 5117102 PUMP CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE HYDRAULIC SYS MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 364QS 2044 6800062 GEAR WOULD NOT EXTEND NORMALLY.TROUBLESHOT SYSTEM. SYSTEM OPS CHECK GOOD. SUSPECT LT HYDRAULIC PUMP WAS CAUSE OF DISCRE PANCY. REMOVED AND REPLACED LT HYDRAULIC PUMP. OP/LEAK CHECK GOOD. IAW MM. CH 29-10-04. 2 L 7 2 4F 4 F RC T00012WI E35NE 20080603 EU 2008 6 3 MALA080113 1 20080531 A 2750 CONTROL VALVE SAAB SF340 340B 7860101 EU TE FLAPS FAILED A MALA O OTHER O OTHER AP APPROACH 1 GL 15 434XJ 340B434 FLAPS WOULD NOT EXTEND, PERFORMED ZERO FLAP LANDING. REMOVED AND REPLACED FLAP CONTROL VALVE. 2 L 7 2 4T RT A52EU 20080603 CE 2008 6 3 DXTA200803039 1 20080501 A 3250 714878 STEERING SYS CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL NLG INOPERATIVE E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 970QS 5111 5111 7500070 AFTER TAKEOFF NOSE GEAR DID NOT RETRACT. FOUND NOSE STEERING UNIT WOULD NOT CENTER PROPERLY, NOT ALLOWING NOSE GEAR TO R ETRACT. REMOVED AND REPLACED STEERING UNIT, OPS AND LEAK CHECK GOOD IAW MM 32-50-00. LANDING GEAR EXTEND AND RETRACT NOR MALLY. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080603 NM 2008 6 3 CALA0800451 1 20080511 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 RIGHT SIDE BS 400 INBOARD ATTACH FASTENER HOLE ON AIR CONDITIONING (A/C) BRACKET CRACKED. REPAIRED CRACKED FRAME ATTACH FASTENER HOLE AT RIGHT SIDE BS400 PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 ASAA0842951 1 20080429 A 5755 MA5428 SKIN BOEING 737 7374Q8 138447Q NM NR 4 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 NR 4 SPOILER LOWER SURFACE IS DENTED ON DOUBLER AFT OF I/B ACTUATOR. PREPPED DAMAGED AREA, REMOVED DELAMINATED SKIN, FA BRICATED AND INSTALLED REPAIR FILLER AND SKIN IAW B737 40 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080603 EA 2008 6 3 SWIA200819628 1 20080508 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG UNDERSERVICED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 460SW 7803 RECEIVED A "GEAR DISAGREE" WARNING MESSAGE AFTER TAKE-OFF, FLIGHT NR 3917. INSPECTED AND SERVICED NOSE STRUT. OPS CHEC K GOOD. 2 L 7 2 4F RT A21EA 20080603 SO 2008 6 3 SWIA200819630 1 20080515 A 5210 HANDLE EMB 120 EMB120ER 3260203 SO PAX DOOR BINDING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 224SW 120294 MAIN CABIN DOOR HANDLE IS DIFFICULT TO CLOSE AND OPEN, FLIGHT NR 3614. INSPECTED, CLEANED AND OPERATED CABIN DOOR FROM INSIDE AND OUTSIDE WITH NO DISCREPANCIES NOTED. 2 L 7 2 4T RT A31SO 20080603 SO 2008 6 3 SWIA200819631 1 20080515 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 234SW 120308 EXIT SIGN AT ROW 6 IS BROKEN. REPLACED EXIT SIGN ASSEMBLY WITH A SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080603 SO 2008 6 3 SWIA200819684 1 20080519 A 3242 21661 BRAKE DISC EMB 120 EMB120ER 3260203 SO MLG DRAGGING A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 251YV 3876 1084 120251 FLT 5718 - ON TAKEOFF ROLL, THE AIRCRAFT VEERED TO THE LEFT. REPLACED NR 2 BRAKE ASSEMBLY IAW AMM 32-41-05. 2 L 7 2 4T RT A31SO 20080603 EA 2008 6 3 SWIA200819687 1 20080523 A 3040 HEATER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT WINDOW FAILED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 928SW 7701 FLT 5992 - RIGHT WINDOW HEAT CAUTION MESSAGE APPEARED. REPLACED RIGHT SIDE WINDOW PER AMM 56-12-01. OPS CHECK GOOD, P/ N NP-139322-12, S/N OFF 03042H9718. 2 L 7 2 4F RT A21EA 20080603 EU 2008 6 3 TRBA2008052 1 20080516 A 3320 37172 BALLAST AEROSP ATR72 ATR72212A 8680902 EU CABIN LIGHTS FAILED A TRBA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 29 494AE 494 F/A REPORTS BURNING ODOR OVER PAX SEATS 13AB AND 6CD. POSSIBLE FLUORESCENT TUBES. REMOVED AND REPLACED FLUORESCENT TUB ES AND BALLASTS AT 4AB AND 14AB IAW JIC NR 33-21-23-RAI-10000-009 AND JIC NR 33-21-21-RAI-10000-007. 2 H 7 2 4T RT A53EU 20080529 EU 2008 5 29 08FDEA01913 1 20080520 A 5321 A532B382400200 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 815FD 638 THERE IS A BROKEN FLOOR PANEL FOR THE MAIN CARGO DECK FROM FRAME 62 TO FRAME 65, LBL-57 TO LBL-72. MATERIAL ID IS A402H 35039-003, PO 604814.1 IAW FEDEX DWG SRZ 25-005, REV F. FABRICATED A NEW FLOOR PANEL FOR THE MAIN CARGO DECK FROM FRAME 62 TO FRAME 65 USING THE OLD PANEL AS A TEMPLATE IAW FEDEX DWG SRZ 25-005, REV F. MARKED PANEL NR 251YG IAW FEDEX DWG SRZ 25-005, REV F AND GMM 7-0-1000. PANEL PART 9ID IS FXR532B382400200. 2 L 7 2 4F RT A35EU 20080529 NM 2008 5 29 08FDEA01989 1 20080527 A 5340 69445598 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 AFT PIT BILGE BODY FRAME STR CLIP IS CORRODED BS 950F FWD, STR 29 R, O/B WL 139. REMOVED AND REPLACED STRINGER CLIP/CH ANNEL REF SRM 51-30-2 PG 2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01944 1 20080521 A 5320 652954832 PAN BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 AFT MAIN DECK FLOOR DITCHING PAN ASSY IS CRACKED BS 1176 - 1183, LBL 27 - 37, WL 208 REPLACED DITCHING PAN AT STA 1176 - 1183, LBL 27 - 37, WL 208 REF BOEING DWG 65-29548 AND SRM 51-30-2 AND 51-30-2 PG 1-10. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01945 1 20080521 A 5320 652954823 PAN BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 DITCHING PAN FWD ATTACH ANGLE BS 1166, RBL 38 - 47, IS CRACKED AT RBL 45 - 4. REMOVED DAMAGED PART (ANGLE) FABRICATED N EW, TREATED AND PRIMED AND INSTALLED IAW SRM 51-10-02 PG 1, 51-30-02, PG 1 AND DWG 65-29548. THIS IS CLASSIFIED AS A MI NOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 SO 2008 5 29 C2XA08IA124 1 20080512 A 3297 D3899926FA98SN CONNECTOR EMB 145 EMB145LR 3260212 SO MLG DIRTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13914 145430 IAH - FLIGHT 2331, THE CREW REPORTED A LANDING GEAR AIR GROUND FAILURE MESSAGE ON EICAS ON INITIAL TAKEOFF. THE AIRCRAF T RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED, CLEANED, AND REINSTALL ED THE CONNECTORS ON THE RIGHT MAIN LANDING GEAR FORWARD PROXIMITY SENSORS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20080529 SO 2008 5 29 C2XA08RI071 1 20080412 A 3320 BR90002 BALLAST EMB 145 EMB145LR 3260212 SO CABIN LIGHTS SHORTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14998 145302 FLIGHT 2224 - EWR - CREW REPORTED BURNING SMELL IN THE AREA OF SEAT 1A. EWR MX REMOVED AND REPLACED BALLAST AND PERFORM ED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20080529 SO 2008 5 29 C2XA08RI066 1 20080510 A 3350 2013BR BATTERY EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS DEFECTIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12160 11720 992 145799 RIC - DURING ROUTINE MAINTENANCE, MX FOUND MULTIPLE EMERGENCY LIGHT DIMMED. MX REMOVED AND REPLACED NR 1 EMERGENCY LIGH T BATTERY IAW EMB145 AMM 33-50-04 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERV ICE. 2 L 7 2 4F RT 20080529 SO 2008 5 29 C2XA08SHO76 1 20080414 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13968 145138 SHV - DURING C-CHECK LEFT OMEGA BEAM REPAIR AT FR 20 IS CORRODED. MX REMOVED AND REPLACED PREVIOUS REPAIR ON LEFT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 20080529 NM 2008 5 29 HALA0800585 1 20080518 A 7931 41801104 TRANSMITTER BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE OIL PRESSURE INOPERATIVE A HALA O OTHER P NO WARNING INDICATION CR CRUISE 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM , RT OIL PRESSURE NO DIGITAL READING ON MONITOR. REMOVED AND REPLACED RT ENG OIL PRESS XMTR PE R AMM 79-32-01 OPS AND LEAK CHECKED GOOD. 2 L 7 2 4F 4 F RT A1NM E13NE 20080529 WP 2008 5 29 08FDEA01954 1 20080522 A 5730 ARC07952 PANEL DOUG MD10 MD1010F 3022112 WP RT WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 367FE 46605 RIGHT WING PANEL 635 BL HAS DELAMINATION AND A PUNCTURE. REPAIRED PANEL BY FABRICATING A NEW INNER SKIN IAW E.A. 8-5720 -118490 & TPS 1001, REV E. DURING POST CURE CLEAN UP FOUND 4 CRACKS IN THE PANEL. HEAT TREATED IAW TPS 1003, REV A. FABBED REPAIR DOUBLERS IAW DWG ARC0795 & TPS 1001, REV E. PREPPED REPAIR AREAS ; LAYED UP THE REPAIR; VACUUM BAGGED & CURED REPAIR IAW SRM 51-71-00; VOL II. 2 L 7 3 4F RT A22WE 20080529 WP 2008 5 29 08FDEA01931 1 20080521 A 5730 ARB087244 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 567FE 46994 RIGHT WING FUEL TANK PLATE/PANEL 633 AT, INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION, NICKS AND GOUGES. FABRICATED NEW FUEL PANEL IAW DAC DWG ARB0872, REV "AV". 2 L 7 3 4F RT A22WE 20080529 WP 2008 5 29 08FDEA01936 1 20080521 A 5730 ARB087241 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 567FE 46994 RIGHT WING RUEL TANK TANK PLATE/PANEL 634 BT, INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION, NICKS AND GOUGES. REMOVE D CORROSION FROM THE FLANGE AND FOUND PANEL TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00, VOL I; PG 217. MACHINED A NE W 634 BT PANEL IAW DAC DWG ARB0872, REV "AV". ALODINED, PRIMED AND PAINTED 634 BT DC/MD-10 SRM 51-21-01, VOL II AND SR M 51-21- 02, VOL II. PART MARKED IAW FEDEX GMM 7-0-1001. FPI IAW DPS 4.707 AND DAC DWG ARB 0872, REV "AV", NO CRACKS NOTED. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 CALA0800458 1 20080515 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM BS 400 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17640 28901 FRAME CRACKED AT STA 400 BETWEEN S8R AND S9L. FABRICATED AND INSTALLED REPAIR ANGLES PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800480 1 20080520 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM BS 400 S8L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 STATION 400 AT S8L AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED FRAME AT STATION 400 S8L BRACKET INBOARD MOUNT HOLE IAW EA 5310-04498. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 YENA2008046 1 20080513 A 3250 WARNING MESSAGE EMB ERJ190 ERJ190100IGW 3260408 NM NLG STEERING FALSE ACTIVATION A YENA O OTHER N FALSE WARNING AP APPROACH 1 EA 15 216JB 19000026 FLT 426, PBI-BOS, ON APPROACH AFTER SELECTING LDG GEAR DOWN, RECEIVED A STEER FAIL EICAS.INTERROGATED STEER FAIL MESSAGE IN CMC. NO CORRELATED FAULTS FOUND. COMPLIED WITH FIM TASK 32-53-00-810-806A. ALL FAULTS CLEARED. PERFORMED CHECK O F STEERING SYSTEM PER AMM 32-52-00-720. ALL CHECK GOOD. TAXIED AIRCRAFT AND STEERING SYSTEM OPERATES NORMALLY. NO DEF ECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A57NM 20080530 NM 2008 5 30 CALA0800501 1 20080528 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM BS 867 S8R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 RIGHT-HAND STATION 867 AT S-8 AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED CRACKED FRAME AT RIGH T-HAND STATION 867 S8R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 HALA0800593 1 20080517 A 5712 RIB BOEING 767 76733A 1385209 NM RT WING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 CRACK, JUST INBOARD OF VENT BOX, RIGHT WING FIXED T/E FORE AND AFT RIB. REPAIRED RIGHT WING FIXED T/E RIB I/B OF VENT B OX. ALL WORK ACCOMPLISHED PER SRM 51-20-11-OG-0 AND SRM 51-40-01-OG-0. 2 L 7 2 4F RT A1NM 20080530 NM 2008 5 30 HALA0800603 1 20080526 A 2697 89873200 LOGIC CARD BOEING 767 7673G5 1385126 NM FIRE OVERHEAT FAILED A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM, LEFT ENG FIRE LOOP 2 EICAS MESSAGE ILLUMINATED. REMOVED AND REPLACED FIRE OVERHEAT DETECTION CARD, OPS CHECK GOOD AMM 26-11-02-012-001. 2 L 7 2 4F RT A1NM 20080530 2008 5 30 HALA0800601 4 20080522 A 3442 20414440402 ANTENNA BOEING 767 76733A 1385209 NM WX RADAR SYS FAILED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM, WXR FAIL DISP ON HSI (CAPT AND F/O) WITH BOTH SYS 1 AND SYS 2 SELECTED WXR TEST NOT ATTEMPTED. REPLACED WXR ANT DRIVE. GND OPS CHK OK 34-43-05. 2 L 7 2 4F RT A1NM 20080602 NM 2008 6 2 CALA0800463 1 20080430 A 5320 INTERCOSTAL BOEING 737 737524 1384721 NM BS 787 BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 INTERCOSTAL IS BENT AT STATION 787+4", S23L. REMOVED BENT INTERCOSTAL AND REPLACED WITH NEW INTERCOSTAL PER BAC DRAWING 65C34362 AND B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 200805142 1 20080511 A 2120 UNKNOWN EMB ERJ170 ERJ170100SE 3260406 NM CABIN SMOKE A UHLA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 641RW 17000062 FLIGHT 7548 DEN TO CID CREW REPORTED WHILE DEPLANING, RECEIVED A LAV SMOKE EICAS MESSAGE AND THE AFT CABIN HAD A SLIGHT HAZE TO IT. CREW TURNED OFF THE RECIRC FAN AND SHUT DOWN THE APU. MAINTENANCE INSPECTED LAV AND CABIN AREA, RAN APU, P ACKS AND RECIRC FAN AND COULD NOT INDUCE SMOKE OR SMOKE INDICATION. HAS NOT DUPLICATED THIS DATE. 2 L 7 2 4F RT A56NM 20080603 NM 2008 6 3 BB08087 1 20080511 A 2782 5006397R ROTARY ACTUATOR BOEING 757 7572S7 1384962 NM L/E SLAT OVERTORQUED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 906AW 67265 20222 23568 PHX FLT 146 PHX TO LIH. ON DEPARTURE FROM PHX, THE CREW RECEIVED A 'LE SLAT DISAGREE' EICAS MESSAGE WITH A LEADING ED GE LIGHT ILLUMINATED. THE FLAPS INDICATOR REMAINED BETWEEN FLAPS UP AND FLAPS ONE POSITIONS. THE FLIGHT RETURNED TO FI ELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMBER 12 SLAT ROTARY ACTUATOR DUE TO AN OVERTORQUED INDICATION. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 20080603 EA 2008 6 3 SWIA200819645 1 20080319 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 952SW 7805 FS 280 AT RBL9 LOWER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 20080603 WP 2008 6 3 UPS08852232 1 20080411 A 5347 DC853B007002 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 SEAT TRACK LBL 45 DAMAGED IN SEVERAL AREAS AT MCD BALL MAT AREA. REMOVED AND REPLACED 3 EACH SEAT TR ACK PLUGS IAW, SRM 53-2-3 FIG 6D, 51 -1-8. 2 L 7 4 4F RT 4A25 20080603 EA 2008 6 3 SWIA200819651 1 20080326 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 948SW 7789 FS 621 LEFT SIDE FLOOR SUPPORT ANGLE IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER REO 601R-53-61-117 NOTES 4 -7. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819652 1 20080326 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 948SW 7789 LBL9 AND RBL9 UPPER FLOOR SUPPORT AT FS 280 IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS TO UPPER FLOOR SUPPORT PER REO 601R-53-11-136 REV A. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819653 1 20080326 A 7120 BUSHING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 948SW 7789 RIGHT ENGINE FORWARD MOUNT BOLT LINK AND BUSHING IS CORRODED, FOUND AT C-CHECK. REPLACED BOLT AND BUSHINGS IAW CRJ200 A MM 71-21-01-000-801 AND 71-21-01-400-801. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819659 1 20080516 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS LOOSE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 965SW 7871 FLOOR LEVEL EMERGENCY LIGHTS ARE INOP AT ROW 5. RESECURED WIRING LIGHTING TERMINAL. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 20080603 SO 2008 6 3 SWIA200819662 1 20080518 A 2710 AILERON EMB 120 EMB120ER 3260203 SO MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 566SW 120341 FLT 5721 - THERE IS A SLIGHT BIND WHEN THE AILERONS ARE MOVED LEFT TO RIGHT. INSPECTED AILERON CABLES, FITTINGS AND PUL LEYS IAW MM 27-11-00. COULD NOT DUPLICATE THE DISCREPENCY. AILERONS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080603 SO 2008 6 3 SWIA200819663 1 20080516 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 270YV 120270 FLT 5446 - EMERGENCY EXIT SIGN AT ROW 9 IS INOP. REPLACED EMERGENCY EXIT LIGHT FIXTURE AT ROW 9. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080603 EU 2008 6 3 MALA080103 1 20080516 A 5510 COUNTERWEIGHT SAAB SF340 340B 7860101 EU HORIZONTAL STAB LOOSE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 442XJ 340B442 RT HORIZONTAL STAB FOUND ANTI-OSCILLATION FIXTURE LOOSE AND END RIB MOUNTING HOLE FIXTURE DAMAGED. THE RT HORIZONTAL ST AB OUTBD RIB AT HS 174.95 WAS FOUND TO HAVE FRETTING DAMAGE ON THE INBD AND OUTBD FACES DUE TO THE COUNTERWEIGHT BOX WOR KING LOOSE. THE COUNTERWEIGHT BOX ALSO HAS FRETTING DAMAGE AND ELONGATED MOUNTING HOLES. CHAFING IS BEYOND SRM 51-10-1 0 PARA 21 ALLOWABLE LIMITS. REMOVED ANTI-OSCILLATION WEIGHT FROM RT HORIZONTAL STAB (HOLES ELONGATED) P/N 7255154-502, COMPLIED WITH EOS55145 AND SAAB REPAIR STATEMENT 340SDS015023 FOR FRETTING CORROSION, BLENDED CHAFES ON HORIZ STAB RIB, INSPECTED FOR CRACKS WITH NO DEFECTS NOTED, AND RESTORED PROTECTIVE FINISH. INSTALLED SERVICEABLE OSCILLATION WEIGHT IA 2 L 7 2 4T RT A52EU 20080603 EU 2008 6 3 CPCP20080029 1 20080502 A 5320 THRESHOLD AEROSP ATR72 ATR72212A 8680902 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 499AT 499 LT FR 36-39 THRESHOLD CORRODED. LT THRESHOLD AT FR 36-39 REPLACED IAW SRM 51-25-01/03. THRESHOLD FABRICATED ON NRWC NR 207386. 2 H 7 2 4T RT A53EU 20080603 EA 2008 6 3 SWIA200819640 1 20080316 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 459SW 7782 CRACK FOUND ON UPPER SUPPORT FRAME AT FS280.0 AND RBL9.0, FOUND AT C-CHECK. INSTALLED REPAIR PARTS FOR UPPER SUPPORT FR AME PER REO 601R-53-111-137. 2 L 7 2 4F RT A21EA 20080603 NM 2008 6 3 QXEA200800472 1 20080509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 425QX 4039 PDX - C4 CHECK, SEAT TRACK NR 1 IS CORRODED AT X20.5, X38 AND X70.5. FOUND TO BE OUTSIDE LIMITS AFTER BLENDING. REPLAC ED SEAT TRACK. 2 H 7 2 4T RT A13NM 2008041500204 20080415 00204 NM 2008 4 15 SWAA081924 1 20080410 A 5311 6546534 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500212 20080415 00212 NM 2008 4 15 SWAA081917 1 20080410 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510D, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008041500221 20080415 00221 NM 2008 4 15 USAA920080751 1 20080317 A 5310 6545855538 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - LEVEL 2 CORROSION ON THE R2 DOOR CUTOUT LOWER SILL CREASE BEAM INNER CHORD, BS 990 - BS 996, RBL 48 - RBL 51, WL 208. REPLACED THE R2 DOOR CUTOUT LOWER SILL CREASE BEAM INNER CHORD, BS 990 - BS 996, RBL 48 - RBL 51, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041500226 20080415 00226 NM 2008 4 15 USAA920080685 1 20080311 A 5320 507946118 ATTACH ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR-C18- CABIN - FUSELAGE FRAME TO INTERCOSTAL ATTACH CHANNEL IS CRACKED BS 294.5 STR 13L WL 237 (NDT VER IFIED). INSTALLED NEW CHANNEL IAW SRM 51-40-02-OG PAR 4B, FIG 3, 8 & 12. 2 L 7 2 4F RT A16WE 2008041500237 20080415 00237 EU 2008 4 15 USAA920080753 1 20080404 A 2910 41010029 PTU AIRBUS 320 A320231 3930325 EU HYDRAULIC SYSTEM DEFECTIVE A USAA O OTHER K FLUID LOSS CR CRUISE 1 EA 19 636AW 48285 41173 98 FLT 625 - PHX-OAK - RTF - CREW REPORTED TOTAL LOSS OF YELLOW SYSTEM HYDRAULIC FLUID. DESELECTED PTU AND ENG NR 2 YELLOW PUMP PER ECAM, HOWEVER BOTH RAN WITHOUT FLUID FOR SHORT PERIOD. ELECTRIC YELLOW PUMP WAS NOT ACTIVATED. CREW DECLARED AN EMERGENCY AND RETURNED TO PHX. MAINTENANCE REMOVED AND REPLACED THE POWER TRANSFER UNIT. ALSO REMOVED AND REPLACED THE YELLOW SYSTEM NR 2 ENGINE DRIVEN PUMP FOR PRECAUTIONARY MAINTENANCE. OPERATIONAL CHECK GOOD. HYDRAULIC PUMP ASSEM BLY / MFGR EATON / MFG P/N 887673 / MFG S/N MX607895 / PART CONDITION UNKN / PART LOCATION ZONE 400 NACELLES/PYLONS / TO TAL TIME 28608 / TOTAL CYCLES 11272 / TIME SINCE REPAIR 1462. 2 L 7 2 4F RT A28NM 2008041600015 20080416 00015 NM 2008 4 16 UIEA200800110 1 20080406 A 2611 2156646 SMOKE DETECTOR BOEING 747 7472D3B 1384805 NM ZONE 200 MALFUNCTIONED A UIEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 15 506MC 21252 DIVERSION TO YJT DUE TO "MAIN DECK CARGO SMOKE DET ZONE 4 LIGHT ILLUMINATED WITH CARGO AND MASTER FIRE ANNUNCIATOR LIGHT S ILLUMINATED. AFTER LANDING RETESTED OKAY (NORMAL). AIRCRAFT ALSO SUSTAINED AN OVERWEIGHT LANDING. SWAPPED ZONE 3 AN D 4 SMOKE DETECTORS A/B PER AMM 26-14-00. ZONE 4 SYSTEM A P/N ON 2156-646 S/N 393 SYSTEM B P/N ON 2156-10C S/N 869. SY STEMS CHECKED NORMAL. PERFORMED OVERWEIGHT LANDING PHASE 1 INSPECTION IAW AMM 5-51-39. NO DAMAGE NOTED. 2 L 7 4 4F RT A20WE 2008041600017 20080416 00017 GL 2008 4 16 UIEA200800112 2 20080406 A 7230 FAN BLADE BOEING 747 74747UF 1384812 NM GE CF6 CF680C2* GL NR 4 ENGINE DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492MC 29253 704882 NR 4 ENGINE 2 EACH FAN BLADES WITH DAMAGE WITH DENT. DYE PENETRANT CHECK OF BLADES FOUND DENTS WITHIN LIMITS OF TASK 72 -31-02-206-001-J00. NO CRACKS FOUND. 2 L 7 4 4F 4 F RT A20WE E23EA 2008041600018 20080416 00018 NM 2008 4 16 UIEA200800113 1 20080407 A 5755 SKIN BOEING 747 7472D7B 1384803 NM SPOILER DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 528MC 22472 RIGHT WING INBOARD SPOILER UPPER SURFACE HAS DELAMINATION WBL 235.150. REMOVED NR 7 GROUND SPOILER IAW MM 27-62-01. RE PAIRED DELAMINATION IAW SRM 51-40-20. INSTALLED SPOILER AND OPS CHECKED OKAY PER 27-62-01. 2 L 7 4 4F RT A20WE 2008041600030 20080416 00030 NM 2008 4 16 AALA200800786 1 20080401 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT FIRST CLASS CART COMPARTMENT BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FIRST CLAS S CART COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041600083 20080416 00083 NM 2008 4 16 UIEA200800122 1 20080404 A 5320 T07A1615687 WEB BOEING 747 747243B 1384830 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK STA 434 STR 26R FLOOR WEB CRACKED. FLOOR WEB REPLACED SRM 51-10-01. 2 L 7 4 4F RT A20WE 2008041600090 20080416 00090 NM 2008 4 16 UIEA200800125 1 20080404 A 5730 SKIN BOEING 747 747243B 1384830 NM ZONE 500 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 LEFT WING FROM WBL 150 TO 470 UPPER SKIN CORROSION EVIDENT BETWEEN NR 1 BEAM TO THE REAR SPAR. BLENDED OUT CORROSION P ER SRM 51-10-01, REPROTECTED PER SRM 51-10-02. 2 L 7 4 4F RT A20WE 2008041600095 20080416 00095 NM 2008 4 16 AALA200800715 1 20080324 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EXTERNAL EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER F OUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041600102 20080416 00102 NM 2008 4 16 AALA200800757 1 20080330 A 3350 PBS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 678AN 29428 JFK - EMERGENCY LIGHT AT OVERHEAD CENTER AISLE JUST AFT OF FIRST CLASS LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD CENTER AISLE JUST AFT OF FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041600119 20080416 00119 EA 2008 4 16 A6WA200840187 1 20080305 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 CRACK FOUND ON THE FLOOR SUPPORT STRUCTURE AT FS 621, RBL 41 AND WL 73. FLOOR SUPPORT STRUCTURE AT FS 621, RBL 41 AND W L 73 REPAIRED IAW CRJ 200 REO 601R-53-61-117 REV. (M) 2 L 7 2 4F RT A21EA 2008041600130 20080416 00130 NM 2008 4 16 UIEA200800132 1 20080403 A 5730 SKIN BOEING 747 747243B 1384830 NM RWS 470-510 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 RIGHT WING WBL 470 TO WS 510 FROM FRONT SPAR TO REAR SPAR UPPER SKIN FOUND LIGHT CORROSION. BLENDED OUT CORROSION PER S RM 51-10-01, REPROTECTED PER SRM 51-10-02. 2 L 7 4 4F RT A20WE 20080603 NM 2008 6 3 QXEA200800535 1 20080531 A 6123 954215B653323 SWITCH DHAV DHC8 DHC8202 2809007 NM AUTOFEATHER SYS MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 349PH 486 PDX - FLIGHT 2193, AUTOFEATHER ARM LIGHT FLICKERING AND SHOWING AS "ARM" WITHOUT THE BUTTON BEING SELECTED. DURING CLIM B AND CRUISE. MAINTENANCE REPLACED THE AUTOFEATHER SELECT SWITCH. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVI CE. 2 H 7 2 4T RT A13NM 20080603 NM 2008 6 3 EIA2008020 1 20080515 A 3350 MODULE BOEING 747 747212B 1384886 NM EMERGENCY LIGHTS NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486EV 20888 UPPER DECK CEILING EMERGENCY LIGHT DOES NOT TEST. REPLACED U/D AFT CEILING EMERGENCY LIGHT MODULE PER B747 MM 33-51-00. SYSTEM OPS CHECKED NORMAL PER B747 MM 33-51-00 PAGE 501. 2 L 7 4 4F RT A20WE 20080603 NM 2008 6 3 UPS08M52247 1 20080411 A 5320 WEB DOUG MD11 MD11 3023602 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C CTR CARGO COMPT AT STA 1841, X=-02 & X=-10, WEB FOUND DENTED AS MARKED. DENTED WEB AT STA 1841, RT & ATTACHING FASTENERS REMOVED. NEW WEB FAB USING MAT'L 7075T6 0.050" PER BOEING DWG ACA7170. HOLES PICKED UP & PAINTING DONE ON NEW WEB. NEW WEB INSTALLED PER SRM 51-33-01VIIR35 & FASTENERS RE-INSTALLED PER SRM 51-33-01VIIR35. 2 L 7 3 4F RT A22WE 20080603 NM 2008 6 3 USAA920081069 1 20080513 A 5755 654645262A HINGE BOEING 737 7374B7 1384702 NM SPOILER CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 453UW 25797 1626 24980 PIT - MAJOR REPAIR - WEEKLY CHECK - RIGHT WING INBOARD GROUND SPOILER HINGE CRACKED. REMOVED AND REPLACED RIGHT WING INBOARD GROUND SPOILER IAW 737 AMM 27-62-12-4. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 USAA920081070 1 20080419 A 5313 143N3110 STRINGER BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - LEVEL 2 CORROSION ON STRINGER, BS 760, S21R. REPAIRED STRINGER, BS 760, S21R IAW B757 SRM 53-00-03-2R1, FIGURE 201. 2 L 7 2 4F RT A2NM 20080603 NM 2008 6 3 QXEA200800515 1 20080527 A 2120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 412QX 4059 SEA - FLIGHT 2399 - FAINT EXHAUST ODOR COMING FROM THE VENTS. SMELLED THE SAME WHEN THE BLEEDS ARE TURNED ON TOO SOON A FTER ENGINE START. FLIGHT CREW SUFFERING FROM HEADACHES AFTER OPERATING AIRCRAFT. NO VISIBLE SMOKE. MAINTENANCE LOOKE D AT THE CDS FOR FAULTS AND FOUND NONE. CHECKED THE OIL LEVEL, NO DEFECTS. RAN ENGINES ONE BLEED AT A TIME, THEN BOTH ON AND NOTED NO ODORS. CHECKED WITH ONCOMING FLIGHT CREW THAT NO ABNORMAL ODOR WAS NOTED. AIRCRAFT RETURNED TO SERVICE . NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080603 NM 2008 6 3 QXEA200800522 1 20080525 A 2721 SWITCH DHAV DHC8 DHC8202 2809007 NM RUDDER TRIM BROKEN A QXEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 09 353PH 496 SEA - FLIGHT 2090 - JUST AFTER TAKEOFF, AND GEAR SELECTED UP, THE FIRST OFFICER USED THE RUDDER TRIM SWITCH, AND IN DOIN G SO, THE SWITCH BROKE TO THE RIGHT POSITION. RUDDER TRIM MOVED 3/4 TO THE RIGHT. CAPTAIN HELD THE TRIM SWITCH TO THE LEFT AND TRIM MOVEMENT STOPPED. CREW HELD SWITCH TO THE LEFT FOR THE REMAINDER OF THE FLIGHT. CALLED CFR AS A PRECAUTI ON. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING ON 16L. MAINTENANCE REPLACED THE TRIM PANEL. OPERATION AL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080603 NM 2008 6 3 ASAA0842959 1 20080429 A 5320 BEAM BOEING 737 7374Q8 138447Q NM FUSELAGE UNKNOWN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 ACCOMPLISH EO 5310 02528 SECTION 4 ON STA 616 STUB BEAM LEFT SIDE, FABRICATED AND INSTALLED STIFFENING ANGLE IAW ASA EO 5310 02528 SECTION 4. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 ASAA0872960 1 20080430 A 5320 141A512010 WEB BOEING 737 737790 13844CN NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 611AS 29753 GOUGES FOUND AT FLIGHT COMPARTMENT FLOOR WEB AT BS 250 AND LBL 6. REPAIRED IAW B737 700 SRM 53 10 51. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 ASAA0892956 1 20080504 A 5730 116A3010 SKIN BOEING 737 737990 NM LT WING DAMAGED A ASAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 NM 02 319AS 33679 BIRD STRIKE TO LT WING JUST INBOARD OF NR 1 ENGINE. REPAIRED PER SRM 57 41 01 REPAIR NR 5. 2 L 7 4 4F RT A16WE 20080603 NM 2008 6 3 ASAA0842957 1 20080430 A 5752 654645528L TAB BOEING 737 7374Q8 138447Q NM AILERON GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 RIGHT AILERON TAB T/E IS GOUGED. REMOVED DAMAGE. PREPARED AND INSTALLED REPAIR PLIES IAW B737 400 SRM 51 70 06 REPAIR 7. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 AALA200801120 1 20080428 A 2910 HOSE BOEING 737 737823 13844BZ NM HYD SYSTEM CRACKED A AALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 21 910AN 29512 YYZ INFLIGHT T1586/28APR - DURING APPROACH CREW REPORTED A SYSTEM HYDRAULIC QUANTITY LOSS AND ENGINE DRIVEN PUMP LOW PR ESSURE INDICATION. LANDED YYZ WITHOUT INCIDENT. FOUND CRACKED HYDRAULIC LINE IN LEFT ENGINE PYLON. REPLACED HYDRAULIC LINE IN LEFT ENGINE PYLON AND REPLACED BOTH LEFT AND RIGHT ENGINE DRIVEN PUMPS AND CASE DRAIN FILTERS. SYSTEM GROUND C HECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 AALA200801122 1 20080428 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 940AN 30598 DFW - EMERGENCY LIGHT AT SEAT 10D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080603 EU 2008 6 3 AALA200801106 1 20080427 A 2130 GCU AIRBUS 300 A300B4605R 3930308 EU NR 1 INOPERATIVE A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 21 33069 512 SJU INFLIGHT T935/27APR MIA CSS - CREW REPORTED CABIN PRESSURE LOSS. OXYGEN MASKS DEPLOYED AT 10000 FEET. LANDED SJU W ITHOUT INCIDENT. REPLACED NUMBER ONE GENERATOR CONTROL UNIT AND CABIN PRESSURE CONTROL UNIT. REPLACED FORWARD OUTFLOW VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20080603 NM 2008 6 3 P5CA0801565 1 20080525 A 5730 PANEL BOEING 747 74746NF 13848BT NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 451PA 30809 LEFT WING INBOARD FIXED PANEL FORWARD OF THE INBOARD FUELING PANEL CRACKED 3 INCHES LONG. ACCOMPLISHED PART 1 OF EO 445 7A142. STOP DRILLED CRACK AND APPLIED SPEED TAPE OVER AFFECTED AREA. 2 L 7 4 4F RT A20WE 20080603 NM 2008 6 3 QXEA200800524 1 20080528 A 4910 4502052A NOZZLE BOMBDR DHC8 DHC8402 1390042 NM STARTER FAILED A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 418QX 4143 YYJ - FLIGHT 2375 - APU STARTED BLOWING SMOKE DURING A START AND PERFORMED A AUTO SHUTDOWN, FOR ABOUT 5 MINUTES IT LEAKE D FUEL. MAINTENANCE FOUND FUEL LEAK TO BE FROM COMBUSTION CAN DRAIN LINE AND PLACED ON MEL 49-00-1. MEL CLEARED 5/28 IN BOI BY REPLACING EXCITER BOX WITH NO HELP, THEN REPLACED RT START NOZZLE. OPERATIONAL CHECKS GOOD MEL CLEARED AND AIRC RAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080603 2008 6 3 P5CA0801566 4 20080529 A 3100 DISPLAY BOEING 747 74746NF 13848BT NM INOPERATIVE A P5CA D RETURN TO BLOCK G MULTIPLE FAILURE TX TAXI/GRND HDL 1 EA 15 454PA 30812 CAPTAIN'S PFD WENT BLANK DURING A POWER INTERRUPTION AT PUSHBACK. CYCLED EIU LEFT, CENTER, RIGHT CIRCUIT BREAKERS. OPE RATION NORMAL AFTERWARDS IAW MM 31-61-00." 2 L 7 4 4F RT A20WE 20080603 NM 2008 6 3 AALA200801110 1 20080427 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 958AN 30091 DFW - EMERGENCY LIGHT AT SEAT 13D MISSING LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 13D. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 AALA200801119 1 20080427 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 652AA 24610 MIA - EMERGENCY LIGHT AT OVERHEAD CABIN MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD CABIN. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080603 2008 6 3 EIA2008021 2 20080516 A 7532 8925982 BOOT BOEING 747 747212B 1384886 NM BLEED VALVE TORN A EIAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 486EV 20888 DURING CLIMB-OUT, APU FIRE WARNING LIGHT AND BELL CAME ON. FIRE SWITCH PULLED AND BOTTLE DISCHARGED. FIRE WARNING INDI CATIONS CONTINUED AFTER APU SHUTDOWN AND EMERGENCY ACTION ITEMS COMPLETED. REPLACED SURGE BLEED VALVE BOOT PER B747 MM 49-53-01. OPS CHECK PER B747 MM 49-53-01. BOTH FIRE CARDS CHANGED PER B747 MM 26-10-000 PAGE 401. OPS CHECKED PER MM 26-15-00. 2 L 7 4 4F RT A20WE 20080603 NM 2008 6 3 QXEA200800470 1 20080509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 425QX 4039 PDX - C4 CHECK, SEAT TRACK NR 2 IS CORRODED AT X279, X292, X326, X373, X558, AND X540. BLENDED AND FOUND TO BE OUT OF L IMITS. REPLACED SEAT TRACK. 2 H 7 2 4T RT A13NM 20080604 WP 2008 6 4 UPS08852257 1 20080501 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 130 RBL 30 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 CORROSION, MISSING BOLTS ON SEAT TRACK SPLICE IN A-PIT CEILING,STA 130, RBL 30. FABBED AND REPLACED SEAT TRACK SPLICE AT STA 130 AND RBL 30 IAW SRM 51 -03-00, SRM 53-02-00 FIG 1F, SRM 53-02-03 FIG 6A. 2 L 7 4 4F RT 4A25 20080604 NM 2008 6 4 NOCA03808 1 20080514 A 5320 4013066 INTERCOSTAL BOEING 767 76739H 1385311 NM FUSELAGE CRACKED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 760NA 26257 INTERCOSTAL ANGLE AT CEILING IS CRACKED AT 2EA AREAS AROUND FASTENERS BETWEEN STA 566-588 AT LBL 40. INSTALLED NEW INTE RCOSTAL PER SRM 53-30-51. 2 L 7 2 4F RT A1NM 20080701 NM 2008 7 1 AALA200801504 1 20080603 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 761AJ 31478 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE GALLEY CLOSET BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LEFT NUMB ER ONE GALLEY CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 20080701 NM 2008 7 1 AALA200801505 1 20080603 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 761AJ 31478 DFW - EMERGENCY LIGHT AT SEAT 26C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED N ORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 20080701 EA 2008 7 1 SWIA200819769 1 20080609 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA FLOODLIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 948SW 7789 NR 1 CEILING LEVEL EMERGENCY FLOODLIGHT IS INOP. (FLT 4266) INSTALLED SERVICEABLE LAMP. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 20080701 SO 2008 7 1 SWIA200819778 1 20080615 A 3240 BRAKE SYS EMB 120 EMB120ER 3260203 SO MLG MALFUNCTIONED A SWIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 07 221SW 120290 BRAKES FAILED TO STOP AIRCRAFT WHILE TAXIING. (FLT 5515) PERFORMED BRAKE VALVE PRESSURE TEST ON BOTH BRAKE SYSTEMS AND PERFORMED TAXI CHECK WITH ANTI-SKID ON AND OFF. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080701 EA 2008 7 1 SWIA200819779 1 20080617 A 7830 NP13932110 O-RING CNDAIR CL600 CL6002C10 1390015 EA NR 1 HYD SYSTEM LEAKING A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 340CA 10062 HYDRAULIC SYSTEM NR 1 QUANTITY INDICATION DECREASED TO 0% WITH AN EDP NR 1 CAUTION MESSAGE. (FLT 3898) REPLACED O-RING ON THE QUICK CONNECT COUPLING IN THE PYLON FOR THE LT THRUST REVERSER. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819724 1 20080530 A 5330 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA BS 1031-1051 DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 715SK 10179 DAMAGE ON AFT RIGHT FUSELAGE BETWEEN FS 1031 AND 1051.3 BETWEEN STRINGERS 19R AND 20R.INSTALLED PERMANENT REPAIR PER REO 670-53-61-372. 2 L 7 2 4F RT A21EA 20080701 SO 2008 7 1 SWIA200819780 1 20080618 A 4930 38827302 FUEL CONTROL EMB 120 EMB120ER 3260203 SO APU ODOR A SWIA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 07 579SW 13772 13772 120347 FUEL SMELL REPORTED IN THE CABIN WHEN APU BLEED IS ON. REPLACED APU FUEL CONTROL UNIT WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080701 EA 2008 7 1 SWIA200819782 1 20080615 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 763SK 10228 LAST OVERHEAD EMERGENCY LIGHT ON CEILING IS INOP. (FLT 6502) RELAMPED AFT EMERGENCY DOME LIGHT IAW AMM 33-51-00. OPS C HECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819783 1 20080619 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS LOOSE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 454SW 7749 LAST HALF OF FLOOR EMERGENCY LIGHTS DO NOT WORK. (FLT 3857) RESECURED WIRE CONNECTORS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008041600152 20080416 00152 NM 2008 4 16 AALA200800744 1 20080329 A 2530 OVEN DOUG MD80 MD83 3023681 NM GALLEY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 951TW 53470 EWR INFLIGHT T1905/29MAR - DURING CLIMB FLIGHT ATTENDANT REPORTED OUTBOARD GALLEY OVEN SMOKING AND OVERHEATING. RETURNE D TO EWR AND LANDED WITHOUT INCIDENT. FOUND PLASTIC WRAP MELTED ON RACK IN OVEN. REMOVED OVEN RACK AND COLLARED CIRCUI T BREAKER AND PLACARDED OVEN. REPLACED OUTBOARD GALLEY OVEN AT DFW. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 2008041600177 20080416 00177 EU 2008 4 16 08FDEA01412 1 20080415 A 5411 A54611750 SPAR AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND CRACK ON PYLON LOWER SPAR CENTER STIFFENER RIB 10 REPAIR PERFORMED IAW, DRAWING R546-10340 AND SB 54-6019, APPROVE D BY RAS/AS/0029/2008 ISS A AND EA 6-5450-117165. 2 L 7 2 4F RT A35EU 2008041600179 20080416 00179 NM 2008 4 16 UIEA200800092 1 20080324 A 5610 60B1002812 WINDSHIELD BOEING 747 7472D7B 1384803 NM COCKPIT CRACKED A UIEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 524MC 21784 AIR TURN BACK ON CLIMB TO FL 320 AT FL 250 THE FIRST OFFICERS WINDSHIELD STARTED ARCING, CAUGHT FIRE AND CRACKED. FOLLO WED FHB PROCEDURES. REPLACED R1 WINDSHIELD IAW AMM 56-11-01. 2 L 7 4 4F RT A20WE 2008041600181 20080416 00181 NM 2008 4 16 UIEA200800094 1 20080326 A 5720 RUB STRIP BOEING 747 74747UF 1384812 NM RT WING WORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 498MC 29259 RT WING INBOARD AILERON UPPER SURFACE HAS RUB STRIP WORN THROUGH. REPAIRED RUB STRIP IAW ATLAS EO 4457A136 AND SRM 57-6 0-01 FIG 201 AND SRM 51-70-09 AND 51-70-10. 2 L 7 4 4F RT A20WE 2008041600191 20080416 00191 NM 2008 4 16 AALA200800779 1 20080314 A 5330 143T35204 SKIN BOEING 767 767223 1385123 NM BS 437 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 321AA 22322 AFW - FUSELAGE SKIN AT STATION 437 STRINGER 32 RIGHT HAD DAMAGE. AREA OF DISCREPANCY WAS 13.2 INCHES BY 2.2 INCHES. RE PAIRED PER SRM 53 00 01 2R AND MRB 767 3160. 2 L 7 2 4F RT A1NM 2008041600196 20080416 00196 EU 2008 4 16 AALA200800776 1 20080331 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 40064 507 MIA - EMERGENCY LIGHT AT SEAT 5C INOPERATIVE. SECURED LAMP FOR EMERGENCY LIGHT AT SEAT 5C. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A35EU 2008041600197 20080416 00197 NM 2008 4 16 2008UALA02092 1 20080410 A 5210 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PAX DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD ENTRY DOOR FUSELAGE CUTOUT STRUCTURE AT BS 294.5 INTERCOSTAL WEB CRACKED AT FWD END AROUND INNER MOST FASTENER HOLE AT STR 16L. MAJOR REPAIR ACCOMPLISHED, REPLACED INTERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041600198 20080416 00198 NM 2008 4 16 F3LA200800164 1 20080403 A 5320 D5347646100000 STRAP AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO FLOOR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 44 1841 DURING C4 S1 CHECK INSPECTION REPORTED SURFACE CORROSION ON CARGO BAY FLOOR STRAP 2403 TO 2456 STRINGER 38R. MAINTENANC E REMOVED AND REPLACED FLOOR STRAP IN ACCORDANCE WITH SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008041700001 20080417 00001 NM 2008 4 17 2008UALA02094 1 20080410 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD ENTRY DOOR LOWER HINGE CUTOUT HAS 2 CRACK INDICATIONS AT FASTENER HOLES AT FWD END OF CUTOUT. MAJOR REPAIR ACCOMPLIS HED, CUTOUT THE DAMAGES COMMON THE THE BEAR STRAP. INSTALLED REPAIR DOUBLER WITH FILLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700006 20080417 00006 NM 2008 4 17 UPS08551976 1 20080405 A 3150 FIRE WARNING BOEING 757 75724APF 1384969 NM COCKPIT FALSE ACTIVATION A IPXA O OTHER N FALSE WARNING LD LANDING 1 SO 01 402UP 23724 AURAL FIRE WARNING ON TOUCH DOWN. RESET WEU BITE MODULE PER FIM 31-51-00. SYSTEM CHECKS NORMAL. OK TO CONTINUE. 2 L 7 2 4F RT A2NM 2008041700014 20080417 00014 NM 2008 4 17 2008UALA02102 1 20080410 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 669 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 CABIN LONGITUDINAL FLOORBEAM HAS A CRACK AT LIGHTENING HOLE JUST BELOW SEAT TRACK, RBL 25" BS 669. MAJOR REPAIR ACCOMPLI SHED: STOP DRILLED CRACK & VERIFIED CRACK TERMINATION WITH HFEC. INSTALLED REPAIR CHANNEL. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700016 20080417 00016 NM 2008 4 17 2008UALA02104 1 20080410 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 384 S15L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 UPPER LT FUSELAGE SKIN HAS DENT BS 384 1" ABOVE STR 15L. MAJOR REPAIR ACCOMPLISHED: RMV'D THE DAMAGE. VERIFIED DAMAGE RM VL WITH HFEC. INSTALLED REPAIR DOUBLER, TRIPLER & FILLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700017 20080417 00017 NM 2008 4 17 2008UALA02105 1 20080410 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 386 S16L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 UPPER LT FUSELAGE SKIN HAS SHARP DENT BS 386 STR 16L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND VERIFIED DAMAGE REM OVAL WITH HFEC. INSTALLED REPAIR DOUBLER, TRIPLER AND FILLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700035 20080417 00035 2008 4 17 UPS08851952 4 20080401 A 2565 BRACKET DOUG DC8 DC873F 302199F WP SLIDE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 FWD LT CREW ENTRY DOOR BOTTOM BRACKET ON SLIDE CASE IS BROKEN CASE SLIDE WILL NOT CLOSE AND SECURE. DEFERRED PER MEL 34 -7-4, M 372532. INSTALLED, INSTALLED EMER EVAC SLIDE PACK IAW 25-60-01-2. THIS CLEARS M-372532. 2 L 7 4 4F RT 4A25 2008041700038 20080417 00038 NM 2008 4 17 MWEA080054 1 20080412 A 5553 591214186 ATTACH ANGLE DOUG MD88 MD88 3023688 NM BS 1474-1485 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 823ME 49766 RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE IS CRACKED IN THE RADIUS BETWEEN CANTED FRAMES 1474 AND 1485. FABRIC ATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 20080701 EA 2008 7 1 SWIA200819785 1 20080620 A 2421 820465 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA ADG AUTO DEPLOY FAULTY A SWIA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 07 953SW ADG DEPLOYED AFTER TAKE OFF. (FLT 6769) RESTOWED ADG IAW MM 24-23-01 AND REPLACED ADG AUTO DEPLOYMENT CONTROL UNIT IAW MM 24-23-15. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080701 SO 2008 7 1 SWIA200819717 1 20080602 A 2150 1945463 HEAT EXCHANGER EMB 120 EMB120ER 3260203 SO RT A/C PACK SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 07 290SW 17242 1322 120317 DURING DESCENT, THE FLIGHT ATTENDANT SMELLED SMOKE IN THE CABIN. (FLT 5702) REPLACED RIGHT PACK HEAT EXCHANGER PER IAW EMB 120 MM 21-50-03. 2 L 7 2 4T RT A31SO 20080701 NM 2008 7 1 SWAA083179 1 20080610 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULE 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080701 SO 2008 7 1 SWIA200819770 1 20080614 A 5210 DOOR EMB 120 EMB120ER 3260203 SO MAIN PAX BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 562SW 120336 CABIN DOOR IS OCCASIONALLY DIFFICULT TO OPEN. (FLT 5441) INSPECTED, CLEANED AND PERFORMED OPS CHECK ON MAIN CABIN DOOR SEVERAL TIMES. NO DISCREPANCIES NOTED. 2 L 7 2 4T RT A31SO 20080701 EA 2008 7 1 SWIA200819727 1 20080531 A 2621 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA FIRE BOTTLE FALSE INDICATION A SWIA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 NM 07 479CA 7675 CARGO BOTTLE LOW CAUTION MESSAGE WHILE AT CRUISE. (FLT 2803) INSPECTED CARGO FIRE BOTTLES FOUND PRESSURES TO BE WITHIN LIMITS PER AMM 26-25-01. ALL INDICATIONS NORMAL. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819729 1 20080529 A 2760 601R906073 CONTROL LEVER CNDAIR CL600 CL6002B19 1900309 EA SPOILERS MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 441SW 7602 "R FLT SPOILER" CAUTION MESSAGE ILLUMINATED DURING DESCENT AND AIRCRAFT ROLLED TO THE RIGHT AFTER FLIGHT SPOILERS WERE D EPLOYED. (FLT 3801) INSTALLED SERVICEABLE CONTROL LEVER HANDLE ASSEMBLY. OPS CHECK GOOD IAW 27-60-00. 2 L 7 2 4F RT A21EA 20080701 SO 2008 7 1 SWIA200819734 1 20080527 A 3350 BATTERY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS INOPERATIVE A SWIA O OTHER L NO TEST NR NOT REPORTED 1 NM 07 299SW 120329 ROW 6 EMERGENCY LIGHTS ARE INOP. (FLT 5785) REPLACED EMERGENCY LIGHT BATTERY. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080530 NM 2008 5 30 CALA0800489 1 20080528 A 3244 419K623 TIRE BOEING 737 737524 1384721 NM MLG FAILED A CALA O OTHER O OTHER LD LANDING 1 SW 27 62631 27535 LEFT INBOARD TIRE BLEW ON LANDING. REMOVED AND REPLACED NR 1 AND NR 2 MAIN TIRES PER MM 32-45-11. NR 1 MAIN S/N ON 906 9, S/N OFF 3490, NR 2 MAIN S/N ON 9253 S/N OFF 3114.  2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800491 1 20080528 A 3350 D71701100 CHARGER BOEING 737 737724 13844BY NM EMERGENCY LIGHTS INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27722 28789 EMERGENCY LIGHTS ON BULLNOSE IN 1ST CLASS AND ABOVE R-1 DOOR ARE INOPERATIVE. INSTALLED NEW BATTERY CHARGER AND BATTERY PACK, OPERATIONAL CHECK OK PER AMM 33-51-00 AND 33-51-06. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800499 1 20080528 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM BS 747 S8R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 RIGHT-HAND STATION 747 AT S8R AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED CRACKED FRAME RIGHT-H AND STATION 747 S8R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800486 1 20080523 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM BS 827 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17640 28901 FUSELAGE FRAME IS CRACKED AT STATION 827 BETWEEN S8L AND S9L. INSTALLED FRAME REPAIR PER ECRA 5310-04774. 2 L 7 2 4F RT A16WE 20080603 EU 2008 6 3 147SL51808 1 20080518 A 2121 EM6751 BLOWER MOTOR PIAGIO P180 P180 6960204 EU PWA PT6 PT6* 52043 EA SEIZED E V2JA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 15 147SL 264 1083 PILOT DESCRIBED A BURNING SMELL AND SAW SOME LIGHT SMOKE IN THE CABIN. 1 H 7 2 3O 3 T RT A59EU E2NE 20080603 CE 2008 6 3 DXTA200803019 1 20080424 A 3260 387 LIGHT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C GL COCKPIT INOPERATIVE E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 997QS 5509 7500208 NOSE GEAR DOWN INDICATION LIGHT FAILED TO ILLUMINATED UPON GEAR EXTENSION. PERFORMED EMERGENCY PROCEDURE LANDING GEAR BL OWDOWN AND PULLED NOSE GEAR UPLOCK. REPLACED BOTH NOSE GEAR DOWN INDICATOR LIGHT BULBS IAW MM 33-00-00. JACKED AC C/W RE TRACTION AND EXTENSION CHECKS BLEED SYS ALL WORK C/W IAW MM 32-30-00 SERVICED BLOWDOWN BOTTLE IAW MM 32-30-00. SERVICED BLOWDOWN BOTTLE IAW MM 12-10-36. BULBS FROM KIT. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080603 EA 2008 6 3 SWIA200819673 1 20080228 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910SW 7566 PAX DOOR EXTERNAL HANDLE IS CRACKED, FOUND AT C-CHECK. INSTALLED NEW PAX DOOR OUTER HANDLE IAW AMM 52-11-03-400-802. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819674 1 20080228 A 5210 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910SW 7566 PAX DOOR LOWER FRAME IS CRACKING IN LOWER RADIUS, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ200 REO 601R-52-11-513 (REV A). 2 L 7 2 4F RT A21EA 20080603 CE 2008 6 3 GUUA05230801 1 20080523 A 5520 1016200111BW HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81535 UE147 DURING SCHEDULED ROUTINE MAINT, DISCOVERED LT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED LT OB ELEVATOR HINGE BRACKE T. 2 L 7 2 4T 4 T RT A24CE E26NE 2008041700040 20080417 00040 NM 2008 4 17 F3LA200800166 1 20080403 A 5320 D5397496800400 STRAP AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 44 1841 DURING C4 S1 C CHECK INSPECTION REPORTED CORROSION ON AFT CARGO BAY FLOOR FRAME STRAP UPPER SURFACE FLOOR STRAP 2350 FRA ME 58. MAINTENANCE REMOVED AND REPLACED FLOOR STRAP 2350 AT FRAME 58 IN ACCORDANCE WITH SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008041700041 20080417 00041 NM 2008 4 17 F3LA200800167 1 20080403 A 5347 D5311281300051 SEAT TRACK AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 44 1841 DURING C4 S1 C CHECK INSPECTION REPORTED DEEP CORROSION CABIN FLOOR STRUCTURE SEAT TRACK AT FRAME 21, Y1292 FLOOR STRAP 810. MAINTENANCE REMOVED AND REPLACED NEW SEAT TRACK AND ONE SPLICE IN ACCORDANCE WITH SRM 51-72-11. UPON COMPLETION O F THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008041700050 20080417 00050 EU 2008 4 17 2008UALA01872 1 20080402 A 5520 SEAL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELEVATOR LOOSE A UALA O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 29 448UA 842 VIBRATION WITH VERTICAL BOUNCE NOTICEABLE ABOVE 320KTS. WHEN ELEVATOR LOADED UP IN DESCENT, VIBRATION STARTED AND WHEN LOADED FOR CLIMB VIBRATION STOPPED. FIRST OFFICER NOTICED RIGHT ELEVATOR INDICATION HAD SLIGHT FLUCTUATION WHEN VIBRAT ION PRESENT. CAUSE: LOOSE SEALS ON ELEVATOR PANELS. REPLACED SEALS WITH NEW. A/C HASN'T REPEATED SINCE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041700051 20080417 00051 NM 2008 4 17 MWEA080052 1 20080405 A 3350 6011779 BATTERY PACK BOEING 717 717200 1383700 NM EMERGENCY LIGHTS INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 927ME 55193 THE OVERWING EMERGENCY LIGHTS ARE ILLUMINATED WHEN THE EMERGENCY LIGHT SWITCH IS IN THE OFF POSITION. REMOVED AND REPLA CED BATTERY PACK. 2 L 7 2 4F TR A6WE 2008041700053 20080417 00053 NM 2008 4 17 2008UALA01934 1 20080405 A 2612 WARNING LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE APU FIRE FALSE INDICATION A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 932UA 26658 RTFL DUE TO APU FIRE WARNING. NO SIGNS OF FIRE FOUND. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700060 20080417 00060 WP 2008 4 17 UPS08851978 1 20080408 A 3350 LIMITER DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 EMERGENCY LIGHTS DISARM LIGHT WAS NOT ILLUMINATED. FOUND BATTERY BUS 30 AMP CURRENT LIMITER BAD. REPLACED SAME AND PER FORMED EMERGENCY LIGHT TEST IAW DC8 AMM 33-50-01-2. SYS OPS CKS NORMAL. 2 L 7 4 4F RT 4A25 2008041700061 20080417 00061 WP 2008 4 17 UPS08851981 1 20080301 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1690-1766 L28 MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 L28R STA 1690-1766 HAS TWO EXISTING DOUBLER NOT CONFORMED TO DWG NR SRO8 5300032 NEED APPX E TO REPAI R. REMOVED DOUBLERS, FABBED AND INSTALLED REPAIR DOUBLERS IAW SRM 51-1-8, SRO 8530032, 51-3-1. 2 L 7 4 4F RT 4A25 2008041700069 20080417 00069 NM 2008 4 17 2008UALA02084 1 20080410 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 540 S24L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 DENTED FUSELAGE FRAME, INBOARD FLANGE AT BS 540 BETWEEN STR 24L AND 25L. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGED FRAM E FLANGE. FABRICATED & INSTALLED A REPAIR ANGLE J-SECTION, STRINGER CLIP (P/N 140N2001-80) & SHEAR TIE (P/N 140N2002-664 ). 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700076 20080417 00076 NM 2008 4 17 2008UALA01944 1 20080404 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 500A S10L GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 EXTERNAL FUSELAGE SKIN GOUGED BS 500A ABOVE STR 10L. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED, FABRICATED A ND INSTALLED EXTERNAL FUSELAGE DOUBLER/TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700078 20080417 00078 NM 2008 4 17 2008UALA01946 1 20080404 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 616 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 OVERWING FRAME BS 616 RT IS CRACKED AT INNER CHORD BTWN WING BOX AND FLOOR LEVEL. SUPPLEMENTAL DATA UPDATE, MAJOR REPAI R ACCOMPLISHED, FABRICATED AND INSTALLED STIFFENER ANGLE REPAIR AND ONCE SECTION OF WEB WITH SPLICE DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700079 20080417 00079 NM 2008 4 17 2008UALA01947 1 20080404 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 827 S25L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 BS 827 STR 25L STRINGER CLIP CRACKED. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED, REPLACED STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700084 20080417 00084 CE 2008 4 17 220CM04 1 20080401 A 2760 240805 VALVE CESSNA 650 650 2076802 CE NR 8 SPOILER FAILED E DBCA K NONE O OTHER IN INSP/MAINT 1 GL 13 220CM 6457 6500160 DURING PREFLIGHT, THE CREW NOTED THE RIGHT ROLL SPOILER DID NOT STOW WHEN SPOILER HOLD DOWN WAS SELECTED. MAINTENANCE V ERIFIED SQUAWK AND TRIP WAS MOVED TO ANOTHER AIRCRAFT. TROUBLESHOT AND FOUND THE NR 8 SPOILER HOLD DOWN RELEASE VALVE H AD FAILED IN THE RELEASE POSITION. MAINTENANCE REPLACED NR 8 SPOILER HOLD DOWN RELEASE VALVE WITH OVERHAULED UNIT. OPS CHECK GOOD. 2 L 7 2 4F A9NM 2008041700090 20080417 00090 NM 2008 4 17 2008UALA01956 1 20080405 A 5310 DOOR FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CARGO DOORWAY GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 AFT BULK PIT ACCESS DOOR BOTTOM FRAME HAS GOUGE ON REPAIR DOUBLER. MAJOR REPAIR ACCOMPLISHED, REMOVED DENTED DOUBLER. FABRICATED AND INSTALLED NEW DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041700091 20080417 00091 NM 2008 4 17 2008UALA01957 1 20080405 A 5310 DOOR FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CARGO DOORWAY CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 AFT BULK PIT LOWER BILGE, FUSE FRAME HAS CORROSION ON LOWER AFT SIDE AT BS 1540 BETWEEN STR 38L-39L. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGED SHEAR TIE. FABRICATED AND INSTALLED NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041600025 20080416 00025 NM 2008 4 16 AALA200800771 1 20080330 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 772AN 29580 DFW - EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041600027 20080416 00027 NM 2008 4 16 AALA200800780 1 20080325 A 2497 WIRE BOEING 757 757223 1384957 NM CHAFED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 694AN 26974 TUL - WIRE BUNDLE W4104 CHAFED AGAINST BRACKET JUST OUTBOARD OF RIGHT RECIRCULATION FAN AT THE AFT END OF FORWARD CARGO AREA. THREE EACH WIRES WERE BURNED IN HALF. THE BRACKET WAS DAMAGED AND THE INSULATION AROUND AREA WAS BURNED. REPLAC ED THREE FOOT SECTION OF WIRING, REPLACED INSULATION AND REPAIRED BRACKET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041600036 20080416 00036 EU 2008 4 16 08FDEA01402 1 20080414 A 5754 A57865200175 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 3 SLAT DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND DENTS ON SLAT NR 3 RT ON LEADING EDGE, RIB 34-35. REPAIR PERFORMED BY INSTALLATION OF A FLUSH DOUBLER IAW RAS/FOK /022/2008 ISS A, APPROVED BY EA 6-5744-115245. 2 L 7 2 4F RT A35EU 2008041600046 20080416 00046 WP 2008 4 16 AALA200800783 1 20080326 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 443AA 49469 TUL - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD BIN SEAT 20D FAILED OPERATIONAL CHECK. REPLACED BATTERY PACK AT OVERHEAD SEAT 20D FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008041600048 20080416 00048 EU 2008 4 16 F3LA200800154 1 20080404 A 5321 D5367175604800 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM56 CFM565B6P 13018 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION WAS FOUND ON THREE INSERTS ON FLOOR PANEL 261PF. MAINTENANCE REMOVE D THE CORRODED PANEL. THE NEW PANEL WAS INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF TASK CARD CP 753-36. FOLLOWIN G THE INSTALLATION OF THE NEW PANEL, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041600051 20080416 00051 EA 2008 4 16 A6WA200840202 1 20080305 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 PAX DOOR EDGE MEMBER AFT SIDE FOUND CRACKED. DOOR EDGE MEMBER REPAIRED IAW REO 601R-52-11-279. (M) 2 L 7 2 4F RT A21EA 2008041600063 20080416 00063 NM 2008 4 16 UIEA200800104 1 20080331 A 5315 FLOORBEAM BOEING 747 747243B 1384830 NM BS 1200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK STA 1200 RBL 110 FLOORBEAM WEB FOUND CRACKED. FLOORBEAM WEB REPAIRED PER SRM 51-40-02. 2 L 7 4 4F RT A20WE 2008041600073 20080416 00073 SW 2008 4 16 WGEA200800053 1 20080410 A 3411 10043539 PITOT TUBE ECLIPS EA500 ECLIPSEEA500 3350000 SW LEFT DEFECTIVE E WGEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 158DJ 112 000074 DURING T/O, RECEIVED AIRSPEED DISAGREE AND STICK PUSHER FAIL MESSAGE. CPT AIRSPEED INDICATED 74 KTS ON TAXI IN AND 63 K TS STOPPED ON THE RAMP. RESOLVED ON W/O:1834 TASKCARD: NR-00001. REPLACED LT PITOT/AOA PROBE WITH NEW PROBE IAW AMM 34 -10-10. PERFORMED ADJUSTMENT/TEST IAW AMM 34-10-00. TESTED AIR DATA SYSTEM IAW AMM 34-10-00, NO AIRSPEED DISAGREE, SYS TEM CHECKS GOOD, NO DEFECTS NOTED. 1 L 7 2 4J RT A00002AC 2008041600076 20080416 00076 EA 2008 4 16 A6WA200840194 1 20080305 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 PAX DOOR STAIRS FORWARD WEB FOUND CRACK IN FIRST STEP CORNER AREA. PAX DOOR STAIRS FORWARD WEB REPAIRED IAW REO 601R-52 -11-702 REV A. (M) 2 L 7 2 4F RT A21EA 2008041600092 20080416 00092 NM 2008 4 16 AALA200800734 1 20080327 A 3350 6832AS25 LAMP DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 951TW 53470 PHX - EMERGENCY LIGHT AT SEAT 7D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT 2008041600098 20080416 00098 NM 2008 4 16 AALA200800718 1 20080325 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN WRONG PART A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 385AM 27059 DFW - EMERGENCY LIGHT AT SEAT 5B HAS WRONG LIGHT. REPLACED LED LIGHT FOR EMERGENCY LIGHT AT SEAT 5B. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008041600114 20080416 00114 NM 2008 4 16 HALA0800525 1 20080410 A 2840 INDICATION SYS BOEING 767 76733A 1385209 NM FUEL MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM CENTER FUEL TANK AND FUEL QUANTITY INDICATORS BLANK INTERMITTENT. DEFERRED PER MEL 28-41-1-2. 2 L 7 2 4F RT A1NM 2008041600116 20080416 00116 NM 2008 4 16 HALA0800522 1 20080408 A 3610 2780539103 ISOLATION VALVE BOEING 767 767332 1382001 NM MALFUNCTIONED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM DURING TAXI RIGHT BLEED ISOLATION VALVE EICAS MESSAGE RECEIVED. UNABLE TO RESET. REPLACED RIG HT ISOLATION VALVE PER AMMM 36-11-04, OPS CHECK LEAK CHECK OK. 2 L 7 2 4F RT A1NM 2008041600132 20080416 00132 NM 2008 4 16 UIEA200800134 1 20080403 A 5730 SKIN BOEING 747 747243B 1384830 NM RWS 1196-1392 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 RIGHT WING WS 1196 TO WS 1392 FROM MID SPAR SURROUND AREA TO REAR SPAR HAS 15 AREAS OF CORROSION. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02. 2 L 7 4 4F RT A20WE 2008041600141 20080416 00141 SO 2008 4 16 SIMA200810502 1 20080411 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 646AE 145213 ON FLIGHT 301H, CREW REPORTED WHILE CLIMBING THRU FL 280, BOTH CREW MEMBERS DETECTED AN ELECTRICAL BURNING ODOR. AIR CO MING FROM GASPER VENTS WAS CLEAN WITH NO ODOR. AIRCRAFT DIVERTED TO EVV. AIRCRAFT REMOVED FROM SERVICE. PERFORMED NUM EROUS CHECKS IN THE FLIGHT DECK AND OVERHEAD PANELS AND IN THE CABIN. RAN AIRCRAFT. NO FURTHER BURN ODOR NOTED. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008041600182 20080416 00182 NM 2008 4 16 UIEA200800095 1 20080326 A 5753 SKIN BOEING 747 74747UF 1384812 NM LT TE FLAP DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 498MC 29259 LT OUTBOARD T/E FORE FLAP SURFACE DAMAGE ON BULLNOSE AREA AT OUT BOARD END. REPAIRED PER SRM 51-70-07 AND ATLAS EO 4457 A135. 2 L 7 4 4F RT A20WE 2008041600183 20080416 00183 NM 2008 4 16 GTIA0800053 1 20080411 A 4920 4500001B APU AIRBUS A319 A319132 3930340 NM FIRE A GTIA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 GL 23 515NK 2698 VISIBLE FLAMES FROM APU. SHUT DOWN APU/DISCHARGED FIRE BOTTLE. INSPECTED APU INTAKE, EXHAUST, AND COMPARTMENT NO PHYSI CAL DAMAGE NOTED. APU DEACTIVATED AND DEFERRED IAW MEL49-10-01. APU REMOVED AND REPLACED, DMI CLEARED. 2 L 7 2 4F RT A28NM 2008041600185 20080416 00185 EU 2008 4 16 08FDEA01414 1 20080415 A 5330 A53812189 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 COROSION FOUND ON SKIN PANEL, C39-40, P28-29 RT REPAIR PERFORMED IAW DRAWING R538-10690, APPROVED BY RAS 70503475/004/20 08 AND EA 6-5315-115270. 2 L 7 2 4F RT A35EU 2008041600190 20080416 00190 EU 2008 4 16 AALA200800766 1 20080330 A 5610 WINDOW AIRBUS 300 A300B4605R 3930308 EU COCKPIT CRACKED A AALA B EMER. DESCENT O OTHER CR CRUISE 1 SW 21 41063 506 SJU INFLIGHT T647/30MAR - CREW REPORTED FIRST OFFICERS RIGHT NUMBER ONE WINDOW CRACKED. DESCENDED TO FLIGHT LEVEL 250. LANDED SJU WITHOUT INCIDENT. REPLACED FIRST OFFICERS RIGHT NUMBER ONE WINDOW AND HEAT CONTROLLER. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008041700002 20080417 00002 NM 2008 4 17 2008UALA02095 1 20080410 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 626 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 BS 616 LT OVERWING FRAME IS CRACKED AT INNER CHORD. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE AND VERIFIED REMOVAL WITH HFEC. INSTALLED REPAIR ANGLE AND FILLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700028 20080417 00028 NM 2008 4 17 2008UALA02115 1 20080410 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 440 S14-16R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 RT FUSELAGE FRAME BS 440 HAS MISDRILLED HOLES AT STR'S 14-15-16. MAJOR REPAIR ACCOMPLISHED: REPLACED FWD FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700045 20080417 00045 2008 4 17 UPS08851961 4 20080402 A 2565 GAUGE DOUG DC8 DC871F 302199D WP ESCAPE SLIDE UNSERVICEABLE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 ESCAPE SLIDE TO BE REPACKED. PRESSURE GAUGE IS UNREADABLE. REPACKED ESCAPE SLIDE PER DC8 MM 25-60-01-2. OK FOR SERVIC E. 2 L 7 4 4F RT 4A25 2008041700054 20080417 00054 NE 2008 4 17 2008UALA01935 2 20080405 A 7230 COMPRESSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 654UA 25392 727698 R ENG HPSOV EICAS. FOUND HIGH PRESSURE SHUT OFF VALVE AND HIGH PRESSURE CONTROLLER TO BE FAULTY. REPLACED NR 2 ENG HPSO V PER MM 36- 11-07 PG 401, NO HELP. BITE CHECK AIR SUPPLY CONTROLLER. REPLACED NR 2 ENG HPC PER MM 36-11-08. RAN ENGIN ES PER JRH. NR 2 BLEED AIR SYSYTEM OPS CHECK SATISFACTORY. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041700059 20080417 00059 WP 2008 4 17 UPS08851977 1 20080221 A 5313 564932754 LONGERON DOUG DC8 DC873F 302199F WP BS 1755 L14L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 AFT CABIN L14L CRACKED AT CANTED FRAME STA 1755. REPAIRED L14L STA 1755 CANTED FRAME IAW SRM 51-3-0, 53-2-2 FIG 10 AND AND 51-1-8, EO 008-5320-28843A AND EA 008-5320-01-A1314. 2 L 7 4 4F RT 4A25 2008041700062 20080417 00062 WP 2008 4 17 UPS08851982 1 20080301 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1690-1766 L28 MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 L28L STA 1690-1766 HAS 3 EXISTING DOUBLERS, 1 INTERNAL AND 2 EXTERNAL NOT CONFORM DWG NR SRO8530032 N EED APX D TO REPAIR. REMOVED DOUBLER, FABBED AND INSTALLED REPAIR DOUBLERS IAW SRM 51-1-8, SRO 8530032, 51-1-26 2 L 7 4 4F RT 4A25 2008041700065 20080417 00065 NM 2008 4 17 2008UALA01988 1 20080406 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 UPPER DECK CEILING 2 EMERGENCY LIGHTS IS INOP. SUPPLEMENTAL DATA UPDATE, RELAMPED. CHECKS NO. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700067 20080417 00067 NM 2008 4 17 2008UALA02082 1 20080410 A 5230 TEE FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 AFT CARGO DOOR LOWER AFT TEE CHORD CRACKED AT FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW TEE CHORD (PN 65 -47952U363) 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700070 20080417 00070 NM 2008 4 17 2008UALA02085 1 20080411 A 5753 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT WING TE FLAP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 306UA 23667 LT INBD FLAP TRAILING EDGE HAS DAMAGE. REPLACED FLAP ASSEMBLY. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700088 20080417 00088 NM 2008 4 17 2008UALA01954 1 20080404 A 3597 CABLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE OXY MASK MIC FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 370UA 24539 CREW REPORT, FO O2 MASK MIC INOP. REPLACED OXYGEN MASK. SHOP FOUND MIC CABLE BAD AND RUBBER BANDS DETERIORATED. REPLACE D CHORD AND RUBBER BANDS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700094 20080417 00094 NM 2008 4 17 2008UALA01960 1 20080405 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1153 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 AFT CARGO COMPARTMENT AT BS 1153 AND LBL 8 -16, FRAME T-CAP IS CORRODED ON UNDERSIDE AND AROUND NUTPLATE. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGED SECTION OF CARGO FLOOR "T" CAP. SPLICED IN NEW SECTION. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041700095 20080417 00095 NM 2008 4 17 2008UALA01961 1 20080405 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1400 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 AFT PIT FRAME DENTED STA 1400 S25L TO 26L. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAI R. 2 L 7 2 4F 4 F RT A2NM E17NE 20080603 EU 2008 6 3 MALA080109 1 20080526 A 3350 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS DISCHARGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425XJ 340B425 EMERGENCY LIGHTS ARE INOP, FOUND CB TRIPPED AND BATTERY PACKS WERE DRAINED. REPLACED EMERGENCY POWER SUPPLIES 20LN, 21L N, 23LN, AND 24LN. 2 L 7 2 4T RT A52EU 20080603 NM 2008 6 3 CALA0800452 1 20080511 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 LEFT SIDE BS 907 INBOARD ATTACH FASTENER HOLE ON AIR CONDITIONING (A/C) BRACKET CRACKED. REPAIRED CRACKED FRAME ATTACH FASTENER HOLE AT LT SIDE BS 907 PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080603 EA 2008 6 3 SWIA200819664 1 20080319 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 FS 280 LOWER BEAM AT RBL 9 LOWER BEAM IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ200 REO601R-53-11-171. 2 L 7 2 4F RT A21EA 20080603 EU 2008 6 3 MALA080112 1 20080601 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 803 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 340B408 WHILE INSPECTING ZONE 314, FOUND A DENT ON RIGHT SKIN AT STA 803 IN ZONE 318 BETWEEN RIGHT HORIZONTAL STABILIZER AND THE RUDDER. REPAIRED. 2 L 7 2 4T RT A52EU 20080603 EA 2008 6 3 SWIA200819650 1 20080326 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 948SW 7789 FS 280 AT RBL 9 LOWER SUPPORT FLOOR ANGLE IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REO 601R-53-11-171 REV D TO REPAI R FS 280 LOWER BEAM RBL9. 2 L 7 2 4F RT A21EA 20080603 NM 2008 6 3 QXEA200800525 1 20080529 A 5210 ROLLER BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 419QX 4145 SEA - AFT PASSENGER DOOR APPEARS TO BE OUT OF RIG. DOOR JAMS IN THE PART OPEN POSITION WITH THE UPPER LEFT CAMLOCK STUC K IN THE LOCK POSITION. AIRCRAFT FERRIED TO PDX FOR REPAIRS. IN PDX, MAINTENANCE ADJUSTED THE FORWARD TOP GUIDE ROLLER AND STABILIZER ROD ASSEMBLY IAW 52-00-00-802-801 STEPS 4D 17-18 E AND F PARAGRAPH 5 A-D. PERFORMED FUNCTIONAL TEST WIT H NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080603 WP 2008 6 3 UPS08852248 1 20080506 A 5720 97532977 ANGLE DOUG DC8 DC873F 302199F WP NR 1 STUBWING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 NR 1 STUBWING INBOARD WEB "L" ANGLE CRACKED IN LOWER RADIUS. FABRICATED AND REPLACED NR 1 STUBWING I NBOARD WEB L-ANGLE IAW SRM 51- 01-20D, SRM 51-03-00 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 20080603 NM 2008 6 3 QXEA200800518 1 20080526 A 6123 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 413QX 4060 SEA - FLIGHT 2299 - ABORTED TAKEOFF AT 60 KNOTS FOR THE AUTOFEATHER WOULD NOT ARM. RETURNED TO THE GATE. MAINTENANCE F OUND FAULT CODE 64. PERFORMED FIM 61-20-02-810-834. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080603 NM 2008 6 3 CALA0800508 1 20080531 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 RIGHT FRAME IS CRACKED AT S8R STATION 907. REPAIRED FRAME AT S8R STATION 907 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080603 2008 6 3 AALA200801103 4 20080427 A 3442 INDICATOR BOEING 767 767323 1385205 NM WX RADAR UNIT CLOGGED A AALA A UNSCHED LANDING C J F.O.D. WARNING INDICATION CR CRUISE 1 SW 21 393AN 29430 MIA INFLIGHT T203/27APR - CREW REPORTED WEATHER RADAR INOPERATIVE. FLIGHT REPORTEDLY HEADING INTO THUNDERSTORMS. RETU RNED TO MIA AND LANDED WITHOUT INCIDENT. FOUND DAMAGE TO ANTENNA AND LINT ON CAPTAINS ELECTRONIC HORIZONTAL SITUATION I NDICATOR VENT HOLES. REPLACED CAPTAINS ELECTRONIC HORIZONTAL SITUATION INDICATOR AND CLEANED VENT HOLES. REPLACED WEAT HER TRANSCEIVER AND ANTENNA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080603 NM 2008 6 3 QXEA200800510 1 20080521 A 3397 WIRE BOMBDR DHC8 DHC8402 1390042 NM SWITCH DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 416QX 4083 SEA - AFTER ENGINE SHUTDOWN EMERGENCY LIGHTS CAME ON AND REMAINED ON EVEN AFTER SWITCH WAS MOVED TO "OFF". MAINTENANCE REPAIRED WIRE 3351-11C-20-2. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080603 NM 2008 6 3 QXEA200800512 1 20080520 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM MAIN PAX MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 414QX 4061 SEA - FLIGHT 2340 - UNABLE TO CLOSE THE AFT PASSENGER DOOR. MAINTENANCE RECENTERED THE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080603 NM 2008 6 3 QXEA200800471 1 20080509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 425QX 4039 PDX - C4 CHECK- SEAT TRACK 9 IS CORRODED AT X174. REPLACED SEAT TRACK. 2 H 7 2 4T RT A13NM 20080603 NM 2008 6 3 CALA0800511 1 20080531 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 FRAME AT STATION 360 BELOW S11L, HAS A HOLE IN IT. REPAIRED FRAME AT STATION 360 BELOW S11L PER EC/RA 5310-04780 AND PA CE EA644-53-005CAL. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 USAA920081183 1 20080606 A 3350 BPS73 BATTERY PACK BOEING 737 7373S3 1384711 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 315AW 23734 FLT 199 SJC-LAS, EEL - FIRST SIX ROWS OF SEAT MOUNTED EMERGENCY LIGHTS VERY DIM. MAINTENANCE REMOVED AND REPLACED THE L EFT FORWARD CABIN EMERGENCY BATTERY PACK. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 20080701 2008 7 1 SWIA200819736 4 20080602 A 3417 8220372445 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA AIR DATA MALFUNCTIONED A SWIA O OTHER N FALSE WARNING DE DESCENT 1 NM 07 948SW 11455 11455 7789 RECEIVED AN EFIS COMP MON FOR AIRSPEED SPLIT. (FLT 6043) REPLACED NR 1 ADC IAW AMM 34-13-01 AND PURGED MOISTURE FROM T HE SYSTEM. 2 L 7 2 4F RT A21EA 2008041700100 20080417 00100 NM 2008 4 17 2008UALA01966 1 20080406 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE OUT OF TOLERANCE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 DOOR R2 UPPER HINGE ARM CUTOUT REQUIRES DOUBLER TO BE INSTALLED. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED, P ERFORMED INSURANCE CUT. LOCATED AND INSTALLED DOUBLER AS PREVENTATIVE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700101 20080417 00101 NM 2008 4 17 2008UALA01967 1 20080406 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE OUT OF TOLERANCE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 DOOR 2L UPPER HINGE CUTOUT REQUIRES DOUBLER TO BE INSTALLED. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED, REMOV ED DAMAGE AND PERFORMED A .040" INSURANCE CUT. LOCATED AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700102 20080417 00102 NM 2008 4 17 2008UALA01968 1 20080406 A 5210 146N61341 CAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 535UA 25130 L-1 DOOR EMERGENCY POWER ACTUATOR CABLE FAILS TRAVEL CHECK. FOUND ACTUATOR CAM FAILED. REPLACED EMERGENCY POWER A CTU ATING CAM 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700103 20080417 00103 NM 2008 4 17 2008UALA01969 1 20080406 A 2520 COFFEEMAKER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FWD GALLEY FAULTY A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 906UA 25006 FLIGHT ATTENDANT NOTICED HOT SMELL AT FWD GALLEY. SMELL WAS ELECTRIC. THEN SPARK OCCURRED FROM COFFEE MARKER GRILL (HOT PLATE) THEN ARC AND PUFF OF SMOKE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700111 20080417 00111 NM 2008 4 17 2008UALA01977 1 20080406 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 4A AFT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 SEAT 4A AFT EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE, RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700113 20080417 00113 NM 2008 4 17 2008UALA01979 1 20080404 A 5240 HOUSING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR HANDLE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 DOOR 4L HANDLE BOX CORRODED AROUND INSERTS AND INTERNAL AREA FOR HANDLE ASSY GOUGED. REPLACED HANDLE BOX. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700114 20080417 00114 NM 2008 4 17 2008UALA01980 1 20080406 A 3520 OXYGEN BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 O2 BOTTLE OVERHEAD 15ABC NEEDS WORK. REPLACED O2 BOTTLE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700122 20080417 00122 NM 2008 4 17 2008UALA01989 1 20080406 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 DOOR 5R SILL EMERGENCY LIGHT IS INOP. REPLACED LAMP. CHECKS NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700128 20080417 00128 NM 2008 4 17 2008UALA01993 1 20080407 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 ZONE C CEILING EMERGENCY LIGHT 2 LEFT SIDE IS INOP. SUPPLEMENTAL DATA UPDATE RELAMPED, CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700133 20080417 00133 NM 2008 4 17 2008UALA01998 1 20080405 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EEL LIGHT INOP AT SEAT 58 ABC. SUPPLEMENTAL DATA UPDATE, RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700138 20080417 00138 EU 2008 4 17 2008UALA02006 1 20080407 A 3243 C202162282223 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE BSCU 2 INTERMITTENT A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 416UA 479 ACFT PULLS STRONGLY TO THE RIGHT. REQUIRES LEFT TILLER AND OR LEFT BRAKE INPUT. REPLACED NOSE WHEEL STEERING CONTROL V ALVE,REPLACING BSCU AND CAPT'S TILLER TRANSMITTER- ALL MTC SEEMS TO HAVE FIXED ISSUES WITH STEERING, A/C TAXI TEST PERF ORMED AND PASSES- A/C TRACKS STRAIGHT WITH NO TILLER. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041700140 20080417 00140 NM 2008 4 17 2008UALA02009 1 20080407 A 2530 COFFEEMAKER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GALLEY SHORTED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 220UA 30223 FLIGHT DIVERTED DUE TO ELECTRICAL/BURNING ODOR AND SMOKE IN AFT GALLEY. COFFEEMAKER WIRING TO TANK CONNECTION DAMAGED. REPLACED COFFEEMAKER. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008041700148 20080417 00148 NM 2008 4 17 2008UALA02016 1 20080407 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 760-780 S17L GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 CABIN BETWEEN BS 760-780 LT AT STR 17L, CREASE BEAM OUTER SPLICE IS GOUGED. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGED SPLICE FITTING. MACHINED AND INSTALLED A NEW SPLICE (P/N 143N5548-7). 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700150 20080417 00150 NM 2008 4 17 2008UALA02021 1 20080407 A 2760 CONTROL MODULE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SPOILERS MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 596UA 28749 EICAS SPOILERS MSG ON UPPER EICAS AND ON OVERHEAD PANEL. REPLACED SPOILER CONTROL MODULE- M535 WAS FAULTING GROUND TEST . 2 L 7 2 4F 4 F RT A2NM E17NE 20080701 NM 2008 7 1 SWAA083180 1 20080610 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULE 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080701 2008 7 1 SWAA083161 4 20080610 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST.` ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080701 EA 2008 7 1 SWIA200819707 1 20080410 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 954SW 7815 FS 280 FLOORBEAM IS CRACKED AT LBL9 AND RBL9. (FOUND AT C-CHECK) INSTALLED REPAIR PARTS PER REO 601R-53-11-136. 2 L 7 2 4F RT A21EA 20080701 NM 2008 7 1 BJNA080403 1 20080417 A 3350 LAMP BOEING 737 7378Q8 13844BX NM EMERGENCY LIGHTS INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 01 GXLAB 28218 LEFT AFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EXTERNAL EMERGENCY LIGHT LAMP, OPERATIONAL CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 SWAA083408 1 20080619 A 5315 6545834 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 16Y CHECK, FOUND FLOOR BEAM UPPER CHORD CORRODED AT BS 328, RBL 12 TO RBL 48. R&R CHORD PER SRM. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 SWAA083398 1 20080619 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER TEE CHORD CRACKED BETWEEN BS 655 AND BS 675, LBL 25. R&R CHORD PER SRM. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 SWAA083397 1 20080619 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 525, BL 0. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 DL757080866 1 20080612 A 5320 FLOOR SUPPORT BOEING 757 757232 1384965 NM FS 377.7 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 MAIN CABIN FS 377.7 LBL 3-10 HAS CORROSION WHERE FLOOR PANEL SITS. REPLACED ANGLE IAW SRM 53-10-51. 2 L 7 2 4F RT A2NM 20080701 NM 2008 7 1 SWAA083392 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 SWAA083391 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 SWAA083373 1 20080619 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083375 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 2008 7 2 SWAA083160 4 20080610 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 USAA920081207 1 20080505 A 5712 RIB BOEING 737 7374B7 1384702 NM LT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 Q6 CHECK - NR 03C30557003/2, CRACK ON LEFT WING TANK RIB AT WING STATION 135.5. REPAIRED DAMAGE AND INSTALLED REPAIR PAR TRS IAW EA 100473. (K) 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 2008UALA03573 1 20080624 A 3397 80541 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY LIGHT ON MID GALLEY WALL LT SIDE INOP. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03560 1 20080623 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 FOUND CORROSION ON FLOOR BEAM UPPER FLANGE IN SEVERAL SPOTS BETWEEN BL0 TO RBL 64 AT BS 365, MAIN DECK FLOOR. REMOVED D AMAGE FABRICATED T-CAP AND INSTALLED IAW SRM 53-00-98 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700153 20080417 00153 NM 2008 4 17 2008UALA02026 1 20080408 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY EXIT EEL LIGHT INOP, TO THE RIGHT OF LAV 110 WALL EEL. FOUND EMERGENCY EXIT LIGHT SHORTED. REPLACED LIGHT ASSE MBLY OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700157 20080417 00157 NM 2008 4 17 2008UALA02030 1 20080408 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY EXIT EEL LIGHT INOP, ACROSS LAV 100 LOWER WALL EEL. FOUND SHORTED LIGHT ASSEMBLY BY LAV 110. REPLACED LIGHT ASSEMBLY OPS CHECKS NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700158 20080417 00158 NM 2008 4 17 2008UALA02031 1 20080408 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY EXIT EEL LIGHT INOP, ACROSS LAV 104 LOWER WALL EEL. FOUND SHORTED LIGHT ASSEMBLY. REPLACED LIGHT ASSEMB LY OPS CHECKS NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700161 20080417 00161 NM 2008 4 17 UIEA200800085 1 20080312 A 2612 FIRE WARNING BOEING 747 747271C 1384869 NM APU BAY FALSE ACTIVATION A UIEA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 EA 15 537MC 22403 APU FIRE WARNING LIGHT ILLUMINATED AND FIRE WARNING BELL ACTIVATED DURING MAIN ENGINE START. ENGINE START TERMINATED, A PU SHUT DOWN. FIRE BOTTLE DISCHARGED. INVESTIGATION/INSPECTION OF APU AND COMPARTMENT REVEALED NO FIRE, PNEUMATIC AIR LEAK OR EVIDENCE OF ELECTRICAL ARCING. APU INOP DUE NO FIRE PROTECTION, EXTINGUISHER DISCHARGED AND APU FIRE WARNING DE TECTION SYSTEM INOP. DISPATCH NOTIFIED. ITEMS DEFERRED. NO CORRECTIVE ACTION TO ABOVE ITEMS SINCE A/C IS IN SHORT-TER M STORAGE AT ROW. 2 L 7 4 4F RT A20WE 2008041700167 20080417 00167 NM 2008 4 17 UIEA200800147 1 20080330 A 5730 SKIN BOEING 747 747243B 1384830 NM ZONE 600 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 RIGHT WING REAR SPAR UPPER SKIN AT WS 1490 FOUND EXISTING EXCESSIVE BLEND OUT AS MARKED. CHECKED THE BLENDOUT AREA AND FOUND AS PER ATLAS EO 4757A338 THE BLENDOUT IS PERMITTED. 2 L 7 4 4F RT A20WE 2008041700176 20080417 00176 WP 2008 4 17 IXXA080013O 1 20080416 A 2697 CONNECTOR DOUG DC8 DC871F 302199D WP FIRE LOOP DAMAGED A IXXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SW 11 820BX 90391 1312 46065 DURING CRUISE FROM KLAX TO KTOL THE CREW HAD A FIRE WARNING INDICATION ON NUMBER ONE ENGINE, ALL PARAMETERS WERE WITHIN NORMAL LIMITS. NUMBER ONE ENGINE WAS SHUTDOWN IAW THE QRH AND THE INBOARD FIRE BOTTLE WAS DISCHARGED. THE FIRE WARNING INDICATION EXTINGUISHED AND THE CREW CONTINUED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE FIRE WAR NING SYSTEM AND FOUND A BAD CONNECTOR AT NR 1 ENG PYLON FIRE LOOP. MAINTENANCE REPLACED THE CONNECTOR AND REPLACED NR 1 ENG PYLON FIRE LOOP IAW MM 26-10-1. ALSO IAW MM 20-50-1. MAINTENANCE RAN NR 1 ENG AND TESTED FIRE WARNING, NO DEFECT S NOTED IAW ATI ERH 70.01. C/W ATI GMM 3.116 NR 1 ENG FIRE WARNING OP'S NORMAL AT THIS TIME. THE AIRCRAFT WAS RETURNED 2 L 7 4 4F RT 4A25 2008041700177 20080417 00177 NM 2008 4 17 QXEA200800377 1 20080412 A 5200 DOOR DHAV DHC8 DHC8202 2809007 NM OPEN A QXEA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 NM 09 355PH 500 SEA - AFTER TAKEOFF, TRIED TO RAISE THE GEAR AND THE GEAR DOOR LIGHTS WERE STILL ILLUMINATED ALONG WITH THE LEFT AND RIG HT UNSAFE LIGHTS. A LOUD FLAPPING SOUND WAS HEARD. VISUAL INSPECTION SHOWED THE GEAR TO STILL BE DOWN. CYCLED THE GEA R AND PROBLEM REMAINED. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. FERRIED THE AIRCRAFT TO PDX FOR R EPAIRS. TRASH BAGS AROUND THE ALTERNATE EXTENSION RELEASE DOOR CAUSED INTERFERENCE. ENSURED THAT THE ALTERNATE EXTENSI ON DOOR WAS COMPLETELY CLOSED. OPERATIONAL CHECKS GOOD NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008041700182 20080417 00182 NM 2008 4 17 QXEA200800374 1 20080412 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM MAIN PAX OUT OF ADJUST A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 405QX 4047 BOI - FLIGHT 2391, AFT PASSENGER DOOR WILL NOT CLOSE AFTER PASSENGERS BOARDED. RESET THE DOOR IAW SIL 52-003A. AIRCRAF T RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008041700184 20080417 00184 NM 2008 4 17 DL76G080577 1 20080410 A 5330 146T35313 SKIN BOEING 767 767332 1382001 NM FS 1373 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1613B 32776 DURING MTC VISIT AT GSO, THE FUSELAGE SKIN WAS FOUND TO HAVE ONE DENTED AREA OUT OF LIMITS PER B767-300 SRM 53-00-01 AT FS 1373, BETWEEN S-28R AND S-29R. THE SRM REPAIR IS NOT APPLICABLE DUE TO PROXIMITY TO THE CARGO DOOR CUTOUT. AS SUCH, BOEING WAS CONTACT FOR REPAIR APPROVAL, AND IS DOCUMENTED IN ER/A 467423-14. 2 L 7 2 4F RT A1NM 2008041700189 20080417 00189 SO 2008 4 17 SWIA200819473 1 20080412 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 562SW 120336 FLT 5477 - FLOOR LEVEL EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED MIDDLE ELBP IAW AMM 33-59-02. OPS CHECK GOOD, PN D36 6-04-001, SN OFF 975/05-91. 2 L 7 2 4T RT A31SO 2008041700194 20080417 00194 NM 2008 4 17 DL757080581 1 20080410 A 3350 LAMP BOEING 757 757232 1384965 NM EMERGENCY LIGHTS INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 699DL 29970 EMERGENCY LIGHT OUT AFT OF LEFT WING. RELAMPED SAME, CKS OK. 2 L 7 2 4F RT A2NM 2008041700199 20080417 00199 EU 2008 4 17 08FDEA01417 1 20080415 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 658FE 752 CROSSBEAM AT FR 60 HAS 1 IN CRACK ON VERTICAL FLANGE, O/B OF SEAT TRACK 3 RT, - Y1456. ON AFT FACE REMOVED CRACK AND A CCOMPLISHED FLOORBEAM REPAIR IAW A300-600 SRM 53-10-15, FIG 211. 2 L 7 2 4F RT A35EU 2008041800003 20080418 00003 NM 2008 4 18 HNAA0800123 1 20080402 A 3350 6038443LB POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 936HA 49572 49572 145 DURING RON MAINTENANCE, THE LEFT FORWARD FUSELAGE EMERGENCY EGRESS LIGHT WAS DIM AND THE 2 MOST FORWARD EMERGENCY FLOOR PATH LIGHTS WERE INOPERATIVE. POWER SUPPLY 3351-PS3 WAS REPLACED ALONG WITH THE BULB IN THE FORWARD FUSELAGE POSITION. SYSTEM OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2008041800006 20080418 00006 NM 2008 4 18 WRLA2008041 1 20080314 A 5322 ANB71745 SHEAR TIE DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 48407 DURING C-CHECK INSPECTION FOUND LT INTERNAL FLAP SUPPORT SHEAR CLIP CRACKED AT STA Y=1521. FABRICATE SHEAR CLIP IAW ENG INEERING INSTRUCTION W2008P53B-226 REV 00. REF EGAT NR U05012. 2 L 7 3 4F 4 F RT A22WE E24NE 2008041800008 20080418 00008 EU 2008 4 18 USAA920080756 1 20080404 A 5210 FE240004 CYLINDER AIRBUS 320 A320214 3930316 EU L1 DOOR BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 109UW 28332 1471 1065 FLT 1550 - PHX-CLT - EMERGENCY EQUIP - FOUND L-1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER WITH BROKEN SPRING AT TRIG GER ASSEMBLY. MAINTENANCE REMOVED AND REPLACED L-1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 2008041800011 20080418 00011 SO 2008 4 18 FDKA200803141 1 20080331 A 4930 FUEL FILTER EMB 145 EMB145LR 3260212 SO APU DEFECTIVE A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 860MJ 145773 FDM 6028 HSV-MCO (1757 PHX LCL). FUEL ODOR IN CABIN ON APU START. MX REMOVED AND REPLACED FUEL FILTER. 2 L 7 2 4T RT T00011AT 2008041800012 20080418 00012 SO 2008 4 18 FDKA200803143 1 20080331 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN BURNED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 837MJ 145367 FDM 5998 MCO-SDF (1546 PHX LCL). SMOKE IN CABIN. MX FOUND 13A SIDEWALL LIGHT BURNT. MX INSPECTED SYSTEM AND COULD NOT DUPLICATE. 2 L 7 2 4T RT T00011AT 2008041800014 20080418 00014 SO 2008 4 18 FDKA200804145 1 20080404 A 5270 SWITCH EMB 145 EMB145LR 3260212 SO CARGO BAY LACK OF LUBE A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 842MJ 145457 FDM 6179 JFK-BWI (0557 PHX LCL). BAGGAGE DOOR WARNING WITH DOOR VERIFIED CLOSED AND LOCKED. MX CLEANED AND LUBED DOOR MICRO SWITCH. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008041800015 20080418 00015 WP 2008 4 18 WRLA2008043 1 20080406 A 2530 OVEN DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE GALLEY MALFUNCTIONED A WRLA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 14075 46922 EDDP/KBGR OVEN 609 AFT GALLEY ON FOR 5 MIN. THEN GRAY AND WHITE SMOKE BILLOWED OUT, SHUT OFF OVEN. ITEM PLACED ON DMI PER MEL 25-29-01 CAT C DUE 04/17/08. REMOVED AND REPLACED OVEN 609, DMI CLEARED 04/10/08. 2 L 7 3 4F 4 F A22WE E23EA 2008041800017 20080418 00017 SO 2008 4 18 C2XA08CL041 1 20080404 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT SMOKE A C2XA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 17146 145746 CLE FLIGHT 2846 THE CREW REPORTED SMOKE IN THE COCKPIT. EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED IN CLE WITHOUT FUR THER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED HIGH POWER ENGINE RUNS WITH BLEEDS, PACKS, AND ANTI ICE SYSTEMS ON. ALSO RAN ALL A/C ELECTRICAL SYSTEMS AND NO SMOKE OR BURNING SMELLS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT 2008041800023 20080418 00023 SO 2008 4 18 C2XA08CL044 1 20080405 A 3350 66369 LIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 25504 145186 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT STRIP AT ROW 3 & 4 FAILED OPERATIONAL CHECK. MAINTENANCE INSPECTED AND R EPLACED THE FLOOR PROXIMITY LIGHT STRIP AT ROW 3 & 4. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT T00011AT 2008041800036 20080418 00036 SO 2008 4 18 FDKA200802151 1 20080405 A 5210 LATCH EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 145568 FDM RON CLT (1535 PHX LCL). PAX DOOR HARD TO OPEN FROM INSIDE. MX LUBED PAX DOOR LATCHES AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2008041600180 20080416 00180 NM 2008 4 16 UIEA200800093 1 20080324 A 7603 7428026 CONTROL CABLE BOEING 747 7472D7B 1384803 NM THROTTLE BINDING A UIEA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 15 522MC 21783 AIR TURN BACK, NR 4 ENGINE THROTTLE ON REDUCED TAKEOFF, THRUST LEVER WAS BINDING AND HAD TO PUSH THROTTLE LEVER 1.5 KNOB S ABOVE THE OTHER THROTTLES TO SET POWER AND STILL COULD NOT REACH CLIMB THRUST. REMOVED AND REPLACED THROTTLE PUSH PUL L CABLE AND PLA SENSOR IAW AMM 76-11-05 AND OPS CHECKED IAW 76-11-00. ALSO, PERFORMED TEST 4 PER AMM 71-00-00, OPS CHEC KED NORMAL. 2 L 7 4 4F RT A20WE 2008041600186 20080416 00186 EU 2008 4 16 08FDEA01415 1 20080415 A 5230 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU CARGO DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND DENT AND CORROSION SPOTS ON BULK CARGO DOOR, NEAR C 67, BEAM 5 REPAIR PERFORMED BY REWORK OF CORROSION IAW SRM 51- 74-10 AND LET THE DENT AS IT IS, APPROVED BY RAS/DAHAM/4024431/2008 ISS B AND EA 6-5234-117140. 2 L 7 2 4F RT A35EU 2008041600187 20080416 00187 EA 2008 4 16 A6WA200840203 1 20080313 A 5320 ACCESS PANEL CNDAIR CL600 CL6002B19 1900309 EA DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 TWO ELONGATED HOLES FOUND ON SURROUND DOUBLER OF FORWARD ACCESS PANEL 132AL FS 228, 4 O`CLOCK AND 7 O`CLOCK. TWO ELONGA TED HOLES OPENED TO .299 TO CLEAR DAMAGE IAW CRJ 200 SRM 51-40-11. FREEZE PLUG INSTALLED IAW CRJ 200 REO 601R-53-11-162 REV B. (M) 2 L 7 2 4F RT A21EA 2008041600194 20080416 00194 NE 2008 4 16 AALA200800774 2 20080331 A 7200 ENGINE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE NR 1 FAILED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 188AN 32382 31585 FLL INFLIGHT T2083/31MAR CAPTAIN REPORTED NUMBER ONE ENGINE OIL PRESSURE WENT TO ZERO AND THE NUMBER ONE ENGINE SPOOLED DOWN. CREW SHUT NUMBER ONE ENGINE DOWN. RETURNED TO FLL AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE ON 0 1 APR AT FLL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 2008041600199 20080416 00199 NM 2008 4 16 2008UALA02093 1 20080410 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD ENTRY DOOR UPPER HINGE CUTOUT HAS 2 FASTENER HOLES WITH CRACK INDICATIONS, FWD END OF CUTOUT. MAJOR REPAIR ACCOMPLI SHED, CUTOUT DAMAGED SECTIONS COMMON TO THE BEAR STRAP. INSTALLED REPAIR DOUBLER WITH FILLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700004 20080417 00004 NM 2008 4 17 2008UALA02097 1 20080410 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD ENTRY DOOR, INNER SKIN AND FRAME CRACKED AT AFT SIDE STOP PIN JUST BELOW CENTERING FITTING. MAJOR REPAIR ACCOMPLISH ED: REMOVED DAMAGE & INSTALLED REPAIR DOUBLERS AT AFT SIDE STOP PIN JUST BELOW CENTERING FITTING. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700009 20080417 00009 NM 2008 4 17 F3LA200800165 1 20080403 A 5321 D5397497200200 STRAP AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 44 1841 DURING C4 S1 C CHECK INSPECTION REPORTED SURFACE CORROSION ON AFT CARGO BAY FLOOR FRAME STRAP UPPER SURFACE AT FLOOR STR AP 2243 FRAME 56. MAINTENANCE REMOVED AND REPLACED FLOOR STRAP IN ACCORDANCE WITH SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008050500089 20080505 00089 EA 2008 5 5 HNAA0800148 1 20080501 A 6123 M390166105L RELAY DHAV DHC8 DHC8311 1386006 EA AUTOFEATHER SYS FAULTY A HNAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 07 330EN 274 AUTO FX WILL NOT ARM ON TAKEOFF ROLL STATIC TEST. 2 H 7 2 4T RT A13NM 2008041700019 20080417 00019 NM 2008 4 17 2008UALA02107 1 20080410 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 420 S6R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 UPPER RT FUSELAGE SKIN BS 420 STR 6R, EXISTING REPAIR DOUBLER HAS DEGRADED SEALANT CAUSING PRESSURE LEAK. MAJOR REPAIR ACCOMPLISHED: REPLACED THE REPAIR WITH DOUBLER AND A TRIPLER. 2 L 7 2 4F 4 F RT A16WE E2GL 20080523 NM 2008 5 23 SB08029 1 20080512 A 2560 P4010021 BATTERY BOEING 737 7374B7 1384702 NM FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 450UW 24933 CLT - MAINTENANCE REPORTED THE AFT EMERGENCY FLASHLIGHT NOT WORKING. MAINTENANCE REPLACED THE BATTERY FOR THE AFT TOP E MERGENCY FLASHLIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20080523 NM 2008 5 23 UPS08M52207 1 20080331 A 5347 S492915012000 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 495 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:2C RCB LEFT FLOOR PANEL SUPPORT AT STA 495 CRACKED AND BUCKLING ON INBOARD SUPPORT AS WELL (EXFOLIATED C ORROSION). REMOVED, FABRICATED, AND REPLACED SEAT TRACK PER DWB WSP0826 SAA TRAVELER 79598410001, AND SRM 51-33-01, 51- 21-00. 2 L 7 3 4F RT A22WE 20080523 NM 2008 5 23 UPS08M52208 1 20080331 A 5347 S49291501200 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 475 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:4C AT STA 475 FROM 0 BUTTLINE TO OUTBOARD AFT OF R1 DOOR AREA SEAT TRACK FOR RCB PANEL IS CRACKED (EXFOL IATED CORROSION). REMOVED, FABRICATED, AND REPLACED SEAT TRACK PER DWG WSP0826, SAA TRAVELER 79598420001, AND SRM 51-31 -01. 2 L 7 3 4F RT A22WE 20080523 NM 2008 5 23 USAA920081044 1 20080509 A 5512 65C25727 SKIN BOEING 737 7374B7 1384702 NM HORIZONTAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 443US 24842 CLT - MAJOR REPAIR - LEFT HORIZONTAL STAB LOWER SKIN CRACKED, ELEVATOR STA 80.5 TO 82.5 AT FWD EDGE OF REAR SPAR . 2 L 7 2 4F RT A16WE 20080523 NM 2008 5 23 USAA920081038 1 20080506 A 5311 FRAME BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED FRAME, BS 727F, S8R - S9R. REPAIRED FRAME, BS 727F, S8R - S9R IAW USAIRWAYS TYP ICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 20080523 NM 2008 5 23 USAA920081039 1 20080507 A 5754 65C26602224 SKIN BOEING 737 7374B7 1384702 NM NR 5 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - DELAMINATION ON RIGHT WING NR 5 SLAT OUTBOARD END. REPAIRED RIGHT WING NR 5 SLAT OUTBOA RD END IAW B737 SRM 57-43-02 AND 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080523 SO 2008 5 23 FDKA200805197 1 20080508 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 FDM 6040 RDU-CVG. FLOOR PROXIMITY LIGHTING OUT BETWEEN ROWS 9-14. MX RESET AND OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080523 SO 2008 5 23 FDKA200805189 1 20080504 A 3350 1317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 FDM RON MCO - COCKPIT EMERGENCY LIGHT INOP. MX RELAMPED, OPS GOOD. 2 L 7 2 4T RT T00011AT 20080523 WP 2008 5 23 UPS08852201 1 20080422 A 5313 47723981 LONGERON DOUG DC8 DC873F 302199F WP BS 1766 L26L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 MAIN CABIN AT STA 1766 LONGERON 26L END FITTING HAS AREA OF MODERATE C CORROSION. REPLACED LONGERON 26L END FITTING AT STA 1766 IAW SRM 51-01-21-0. 2 L 7 4 4F RT 4A25 20080523 EU 2008 5 23 USAA920081045 1 20080509 A 5320 D53472193200 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650AW 856 SAL - MAJOR REPAIR - C4 CHECK - CORROSION ON CABIN BEAM, BS 3257 / FR 68, -Y765. REPLACED CABIN BEAM, BS 3158 / FR 66 - BS 3366 / FR 70, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20080523 NM 2008 5 23 USAA920081054 1 20080508 A 5753 SKIN BOEING BOEING 737 737401 1384701 NM LT WING TE FLAP DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US BN654 23879 CLT - MAJOR REPAIR - C4 CHECK - LEFT WING AFT FLAP TRAILING EDGE HAS AREA OF DISBOND. REPLACED LEFT WING AFT FLAP IAW A MM 27-51-39. 2 L 7 2 4F RT A16WE 20080523 EU 2008 5 23 USAA920081064 1 20080512 A 2560 P4010021 BATTERY AIRBUS 320 A320231 3930325 EU FLASHLIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 621AW 53 FLT 647 CMH-PHX - EMERG EQUIP - AFT LEFT F/A EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BAT TERY IN THE AFT LEFT F/A EMERGENCY FLASHLIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 20080523 EU 2008 5 23 USAA920081046 1 20080509 A 5320 D53472190203 FLOOR SUPPORT AIRBUS 320 A320232 3930326 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650AW 856 SAL - MAJOR REPAIR - C4 CHECK - CORROSION ON CABIN BEAM, BS 3158 / FR 66, -Y765. REPLACED CABIN BEAM, BS 3043 / FR 64 - BS 3158 / FR 66, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20080523 NM 2008 5 23 UPS08652203 1 20080430 A 5240 SKIN BOEING 767 76734AF 1385212 NM DOOR MEC CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 329UP 27755 INSPECTION TYPE:C FX MEC DOOR EXTERIOR SURFACE FOUND CHAFING MARK. MEC DOOR SKIN REPAIRED AS PER SRM 52-40-01-2R5 FIG 2 01. 2 L 7 2 4F RT A1NM 20080523 WP 2008 5 23 UPS08852217 1 20080423 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 FLOOR PANEL F80B HAS DENTS AND CRACKS AS MARKED. REPAIRED FLOOR PANEL F80B IAW SRM 53-02-03-0 FIG 10 AND SRM 53-02-03-0. 2 L 7 4 4F RT 4A25 20080702 NM 2008 7 2 2008UALA03537 1 20080621 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERG LT INOP:CEILING BETWEEN MID LAVS. SUSPECT BATTERY ASSEMBLY. REPLACED BATTERY ASSEMBLY OP CHECKED GOOD. AC OK FO R SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03526 1 20080620 A 3350 767 LAMP BOEING 737 737322 1384676 NM EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 370UA 24539 LEFT EMERGENCY EXIT WING LIGHT IS INOP. FOUND BURNED OUT LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800557 1 20080601 A 5743 115A5211 BUSHING BOEING 737 737724 13844BY NM RT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 RIGHT MAIN LANDING GEAR FWD TRUNNION SUPPORT (OUTBOARD UPPER BUSHING FACE) HAS CORROSION. COMPLETED ECRA 5741-01106 REV D. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800590 1 20080528 A 5320 655484221 ANGLE BOEING 737 737524 1384721 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 VERTICAL STABILIZER PANELS 9501L, 9505L 9503L ARE FRETTING FUSELAGE ATTACH ANGLE, WEAR ON ANGLE AND PANELS. REMOVED DAM AGED ANGLES BEHIND VERTICAL STABILIZER PANELS 9501L, 9505L, 9503L. FABRICATED REPAIR ANGLES AND INSTALLED ANGLES IAW TY PICAL REPAIR 5380-10113. RESTORED PROTECTIVE FINISH ON PANELS IAW SRM 51-20-01. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800563 1 20080601 A 5743 115A5211 BUSHING BOEING 737 737724 13844BY NM LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 LEFT MAIN LANDING GEAR FWD TRUNNION SUPPORT (INBOARD LOWER BUSHING FACE) HAS CORROSION. REWORKED INBOARD LOWER BUSHING FACE PER ECRA 5741-01106. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800591 1 20080528 A 5320 6554842 ANGLE BOEING 737 737524 1384721 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 VERTICAL STABILIZER PANELS 9504R, 9506R 9508R ARE FRETTING FUSELAGE ATTACH ANGLE, WEAR ON ANGLE AND PANELS. REMOVED DAM AGED ANGLES BEHIND VERTICAL STABILIZER PANELS 9504R, 9506R, 9508R. FABRICATED REPAIR ANGLES AND INSTALLED IAW TYPICAL R EPAIR 5380-10113. RESTORED PROTECTIVE FINISH ON PANELS IAW SRM 51-20-01. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800633 1 20080623 A 5311 654656627 FRAME BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16646 28907 FUSELAGE FRAME HAS CORROSION STATION 992 RBL-48 AT FLOORLINE. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER AN D FILLER REF SRM 51-70-11. 2 L 7 2 4F RT A16WE 20080702 2008 7 2 SWAA083060 4 20080608 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 223WN 32492 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082811 1 20080524 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 23 DEF. REMOVED AND REPLACED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082826 1 20080524 A 7933 21SN04211 BULB BOEING 737 7375H4 138449D NM NR 1 ENGINE FAULTY A SWAA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SW 29 511SW 24188 NR 1 ENGINE OIL TEMP CLIMBED INTO RED BAND. NR 1 ENGINE WAS SHUTDOWN PER QRH. REMOVED AND REPLACED OIL TEMP BULB PER M M. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082852 1 20080526 A 5310 6546956 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 400 TO BS 420, LBL 68. REMOVED AND REPLACED WEB PER SR M. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 CALA0800526 1 20080530 A 3233 65448106 ACTUATOR BOEING 737 7373T0 1384582 NM MLG WW DEFECTIVE A CALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 27 76354 23592 LEFT MAIN GEAR DID NOT SHOW DOWN AND LOCKED (GREEN LIGHT) UPON MANUAL GEAR EXTENSION GOT NORMAL GEAR INDICATION, BUT AUT O BRAKE AND ANTI-SKID BREAKERS POPPED. LUBRICATED LEFT GEAR ASSEMBLY REPLACED LEFT MAIN GEAR UPLOCK ACTUATOR. PERFORME D NORMAL AND MANUAL GEAR EXTENSION, OPERATES NORMAL PER AMM 32-32-41. PERFORMED OPERATIONAL CHECK OF ANTI-SKID SYSTEM A ND AUTO BRAKE SYSTEM, BOTH NORMAL PER AMM 32-42-00 AND 32-43-01. ROTABLE PARTS CHANGE WAS INDICATED - ACTUATOR, MLG PAR T NUMBER 65-44810-6. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 CALA0800527 1 20080531 A 2612 6937307300 MODULE BOEING 737 737824 13844BZ NM FIRE DETECTION MALFUNCTIONED A CALA B EMER. DESCENT O OTHER CR CRUISE 1 SW 27 35260 30855 LEVELING OFF AT FLT 380 CABIN ALTITUDE HORN WENT OFF. CABIN ALT WAS ABOVE 1000FT. COULD NOT RE-ESTABLISH PRESSURE. EX ECUTED AN EMERGENCY DESCENT TO 9000FT. ON CREW DEBRIEF, NR 2 ENGINE BLEED WAS INSUFICIENT. TROUBLESHOT TO FAILED S9 ON FIRE CONTROL PNL (P8-1) NOT OPENING PRESSURE OUTFLOW VALVE. PERFORMED HEALTH CHECK IAW 36-11-00. REPLACED HI STAGE RE GULATOR FOR OUTFLOW VALVE PX FAULT. REF 26-00- 01 AND 36-11-07. OPS CHECKED BLEED SYSTEM OK. ROTABLE PARTS CHANGE WAS INDICATED - FIRE DECTION MODULE PART NUMBER 69-37307-300, AND HIGH-STAGE REGULATOR PART NUMBER 107484-7. 2 L 7 2 4F RT A16WE 20080707 SO 2008 7 7 C2XA08SH077 1 20080516 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12175 14500878 SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 20 MX REMOVED AND REPLACED CENTER OMEGA BEAM AT FR 20 IAW EM B 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE 2 L 7 2 4F RT 20080707 WP 2008 7 7 UPS08852233 1 20080509 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 A/C IS OOS DUE TO FUSELAGE DAMAGE CAUSED BY OTHER CARRIER'S BAGGAGE CART. REPAIRED PER UPS EO DC8-5330-29309-A. 2 L 7 4 4F RT 4A25 20080707 NM 2008 7 7 2008UALA02736 1 20080510 A 3350 60B4005715 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY LIGHT DR 4L SLIDE LIGHT INOP. SUSPECT LIGHT ASSEMBLY FAULTY. REPLACED LIGHT ASSEMBLY, OP CHECKED GOOD. AC O K FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 2008UALA02740 1 20080511 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY CEILING LIGHT ROW 15 INOP. FOUND LAMP FAULTY. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 2008UALA02759 1 20080513 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY CEILING LIGHT ABOVE ROW 17 INOP. SUSPECT FAULTY LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 2008UALA02786 1 20080514 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY EXIT EEL LIGHT INOP, AT SEAT 2A AFT LIGHT ASSY. REPLACED LIGHT ASSY. OP CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 EU 2008 7 7 2008UALA02794 1 20080515 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 446UA 834 DOOR SILL 2R CORRODED AROUND FLOOR PANEL ATTACH NUTPLATE HOLES IN AREA OF FR66. 2 L 7 2 4F 4 F RT A28NM E40NE 20080707 EU 2008 7 7 2008UALA02797 1 20080515 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 446UA 834 FOUND CORROSION ON FLOORBEAM NR 250. 2 L 7 2 4F 4 F RT A28NM E40NE 20080707 NM 2008 7 7 2008UALA02804 1 20080515 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 DOOR 3 LEFT FWD SILL EMERGENCY LIGHT IS INOP. SUSPECT FAULTY LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 USAA920081084 1 20080514 A 2560 P4010021 BATTERY BOEING 767 7672B7ER 1385107 NM FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 MIA - EEL - C4 CHECK - FORWARD FLIGHT ATTENDANT POSITION 4 FLASHLIGHT BATTERY WEAK. REPLACED FORWARD FLIGHT ATTENDANT P OSITION 4 FLASHLIGHT BATTERY IAW B767 AMM 25-60-00. 2 L 7 2 4F RT A1NM 20080707 NM 2008 7 7 USAA920081087 1 20080514 A 2560 P4010021 BATTERY BOEING 767 7672B7ER 1385107 NM FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 MIA - EEL - C4 CHECK - AFT FLIGHT ATTENDANT POSITION 2 FLASHLIGHT BATTERY WEAK. REPLACED AFT FLIGHT ATTENDANT POSITION 2 FLASHLIGHT BATTERY IAW B767 AMM 25-60-00. 2 L 7 2 4F RT A1NM 20080707 EU 2008 7 7 UPS08152291 1 20080517 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 125UP 0809 INSPECTION TYPE:N/A GLARESHIELD EMERGENCY LIGHT CAPTAIN'S PANEL INOP. RELAMPED EMERGENCY LIGHT, CHECKS OK IAW TC 050000 -01-1. 2 L 7 2 4F RT A35EU 20080707 NM 2008 7 7 UPS08652292 1 20080517 A 3350 BRACKET BOEING 767 76734AF 1385212 NM L1 DOOR LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 323UP 27749 INSPECTION TYPE:N/A L1 DOOR EMERGENCY EXIT LIGHT HOLDING BRACKET NEEDS RE-SECURED. RE-SECURED LIGHT ASSY USING STANDARD MX PRACTICES, CHAP 20. 2 L 7 2 4F RT A1NM 20080915 EU 2008 9 15 08FDEA03172 1 20080730 A 5753 A57960306200 SKIN AIRBUS 300 A300F4605R 3930327 EU RT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 686FE 804 RT WING CENTER FLAP UPPER SURFACE APPROX RIB 16, 7 EA WEAR MARKS FROM BUTTON HEAD RIVETS CHAFING REMOVED DAMAGED SECTION AND INSTALLED FLAP SKIN PATCH REPAIR IAW SRM 57-50-00, FIG 205, PG 219. 2 L 7 2 4F RT A35EU 20080915 WP 2008 9 15 08FDEA03078 1 20080725 A 5755 SKIN DOUG MD10 MD1010F 3022112 WP RT WING SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 THE RIGHT WING NR 3 SPOILER IS DELAMINATED ON THE LOWER SURFACE AT THE OUTBD CORNER. REPLACED THE LOWER SKIN, DOUBLER A ND PARTIAL CORE THEN BONDED IT IAW DC/MD-10 SRM 57-10-00, VOL I AND SRM 51-71-00, VOL II. PRIMED AND SEALED IAW DC/MD-1 0 SRM 51-21-01, VOL II. ACCOMPLISHED ALL WORK ON W/O 3283309 AND NON-ROUTINE NR N00270. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 CALA0800796 1 20080819 A 5320 6935367 INTERCOSTAL BOEING 737 737524 1384721 NM BS 380 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 STATION 380 + 7 INCHES LBL 25 INTERCOSTAL DENTED AT FASTENER ON VERTICAL LEG. REMOVED CRACKED PORTION ON WEB, FABRICATE D FILLER AND DOUBLER AND INSTALLED IAW SRM 51-70-13. 2 L 7 2 4F RT A16WE 20080915 WP 2008 9 15 UPS08853081 1 20080730 A 5753 DOUBLER DOUG DC8 DC871F 302199D WP RT WING TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 RT WING O/B FLAP STA XF 228 HAS A ROUND DOUBLER GOUGED AT UPPER SKIN, NEXT TO L/E AREA. REMOVED EXIS TING DOUBLER IAW SRM 51-1-21A. FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW SRM 57-07-01 FIG 004, 57-02-0 FI G 002A, AND SRM 51-1-21A. 2 L 7 4 4F RT 4A25 20080915 EA 2008 9 15 SWIA200819997 1 20080829 A 2621 34600271 SWITCH CNDAIR CL600 CL6002B19 1900309 EA FIRE BOTTLE FAULTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 913SW 7597 RECEIVED A "CARGO BTL LO" CAUTION MESSAGE. RETURNED TO FIELD. FLIGHT 5802. REPLACED LARGE CARGO BOTTLE DUE TO FAULTY BOTTLE PRESSURE SWITCH PER AMM 26-25-01. OPS CHECK GOOD AT THIS TIME. P/N 3460037-1, S/N OFF 229NBFI. 2 L 7 2 4F RT A21EA 20080915 WP 2008 9 15 UPS08853083 1 20080730 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FS 680-780 CRUSHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 MAIN CABIN FLOORBOARD AT STA 680-780 LBL 25.44 IS CRUSHED AT FWD & AFT ENDS. FABRICATED REPLACEMENT FLOOR PANEL IAW EO DC8-5320-9691. 2 L 7 4 4F RT 4A25 20080915 WP 2008 9 15 UPS08853089 1 20080730 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FS 880-1000 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 MAIN CABIN FLOORBOARD AT STA 880-1000 LBL 44.60 HAS 3EA MISSING & 1 EA DAMAGED INSERT. REPLACED 4EA INSERTS IAW DPS 1.9023 REPAIR 4.3-1 PAGE 4. 2 L 7 4 4F RT 4A25 20080915 WP 2008 9 15 UPS08853090 1 20080729 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 1360 L31R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 D PIT STA 1360 LONGERON 31R FLOORBOARD SUPPORT CRACKED. REPAIRED FLOORBOARD SUPPORT AT STA 1360 L31R IAW EO DC8-5320-6176. 2 L 7 4 4F RT 4A25 20080915 NM 2008 9 15 UPS08M53103 1 20080802 A 5712 RIB DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:C RT WING LOWER WINGLET FWD RIB FOUND CRACKED AS MARKED. CRACKED RIB REMOVED PER SRM 51-31-01 V2 R40. NEW RIB FAB PER BOEING DRWG ARB7774 USING MATL 7075-0-0.040". RIB HEAT TREATED TO T6 PER DPS7.00-1 HARDNESS VALUE OBTAI NED HRB80.1 PER DPS1.053. NEW RIB HOLES P/UP&NEW RIB PROTECTED PER SRM 51-21-01 V2 R40. NEW RIB INSTALLED PER SRM 51-3 1-01 V2 R40. PAINT TOUCH UP ON REPAIRED AREA PER SRM 51-21-02 V2 R40. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 UPS08553113 1 20080815 A 5320 SUPPORT BOEING 757 75724APF 1384969 NM BS 1200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 BULKHEAD SUPPORT WEB IS CORRODED AT PREVIOUS REPAIR BS 1200 LBL 14 WL 150. REPAIRED PER SRM 51-70-11 -0G. 2 L 7 2 4F RT A2NM 20080915 NM 2008 9 15 UPS08553138 1 20080809 A 5210 LATCH BOEING 757 75724APF 1384969 NM PAX DOOR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 UPPER CAM LATCH ON CREW ENTRY DOOR FWD FRAME IS GOUGED. BLENDED GOUGED ON CREW ENTRY DOOR UPPER LATCH CAM IAW SRM 51-10 -02. 2 L 7 2 4F RT A2NM 20080915 NM 2008 9 15 UPS08M53139 1 20080807 A 5754 STRAP DOUG MD11 MD11F 3023600 NM RT WING SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:C RT WING L/E LOWER ACCESS AT 13 INCHES O/B OF SLAT NR 12 FOUND STRAP SUSPECT CRACK. HFEC CARRIED OUT I AW DAC NDT SPM REV 13 PART 06-10-01.001 AND CRACK CO CONFIRM APPROX 4.75 INCHES LONG. DAMAGE STRAP AND ATTACH FORMER RE MOVED, STRAP FABRICATED AND INSTALLED AS PER SRM 51-31-01 VOL II REV 40. 2 L 7 3 4F RT A22WE 20080915 NM 2008 9 15 SWAA084787 1 20080828 A 5340 65C27314 STRINGER CLIP BOEING 737 7373T0 1384582 NM BS 360 S13L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 08FDEA03083 1 20080725 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 577FE 48469 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES A, B, C AND D BUSHING. REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL I. SUPPORT FITTING REMOVED AND REPLACED AS PER 51-33-01 VOL II. R EPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080916 EU 2008 9 16 08FDEA03271 1 20080805 A 5753 A5796608420300 RUB STRIP AIRBUS 300 A300B4622R 3930312 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 RIGHT INBD FLAP L/E NOSE SKIN STRAPS HAVE ELONGATED HOLES, (2 STRAPS) MATERIAL ID IAW A300-600 SRM 51-31-00. FABRICATE D, LOCATED AND DRILLED IAW A300-600 SRM 51-40-44. ALODINED AND PRIMED IAW A300-600 SRM 51-21-10. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03296 1 20080807 A 5420 A54515328 FAIRING AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CHAFING MARKS ON PYLON NR 2 UPPER AFT FAIRING RIB 19 REPAIR PERFORMED BY REWORK OF CHAFING MARK, NDT FOR CRACK FRE E CONDITION AND INSTALLING A STRIP TO LIMIT NEW CHAFING IAW RAS /70511364/010/2008 ISS A , APPROVED BY EA 6-5454-12008 4. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03240 1 20080804 A 5330 A53973192207 DOUBLER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION AT DOUBLER C 71-72, P 54-56 RT. REPAIR PERFORMED BY REMOVAL OF CORROSION AND FLAP PEENING IAW RAS /EFW/ 9000070/2008 ISS A, APPROVED BY EA 6-5317-123027. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03243 1 20080804 A 5330 A53974417202 DOUBLER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION AND SMALL NICK AT ANTENNA DOUBLER C 63-65, P 55 -56 LT REPAIR PERFORMED BY REWORK OF BOTH DAMAGES, NDT F OR CORROSION FREE CONDITION AND FLAP PEENING IAW RAS/EFW/9000072/2008 ISS A, APPROVED BY EA 6-5317-123038. 2 L 7 2 4F RT A35EU 20080917 NM 2008 9 17 2008UALA04350 1 20080819 A 2421 745329F IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEFT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 662UA 27159 LH GENERATOR WILL NOT COME ON LINE, WITH "FIELD OFF" LIGHT ILLUMINATED. SUPPLEMENTAL DATA UPDATE FOUND FAULTY IDG.REPL ACED #1 IDG. TESTS OKAY. OK FOR SVC. 2 L 7 2 4F 4 F RT A1NM E24NE 20080917 NM 2008 9 17 ASAA0843389 1 20080820 A 2751 2061141 INDICATOR BOEING 737 737490 1384715 NM TE FLAPS MALFUNCTIONED A ASAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NM 02 799AS 34808 29270 ON APPROACH WHEN CONFIGURING WITH FLAP 1 AT YAK FLAP INDICATOR STAYED UP AND LED "LED FLAP EXT" LIGHT WAS GREEN. ACFT D IVERTED TO ANC PER MX AND DISPATCH. AT ANC SAME CONDITION ALTERNATE FLAP OPERATION DID NOT WORK. LANDED WITH ZERO T/E FLAPS. FOUND T/E POSITION C/B OUT. RESET C/B PER RESET PROCEDURE. L/E & T/E FLAP OPERATION AND INDICATION OPS CKS NOR MAL. SUSPECT DURING F/O'S SHOULDER HARNESS RELEASE BELT CLIP TRIPPED C/B. 2 L 7 2 4F RT A16WE 20080917 2008 9 17 ASAA0853397 4 20080821 A 3442 6225132633 TRANSCEIVER BOEING 737 737890 1384527 NM WX RADAR MALFUNCTIONED A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 579AS 5745 35187 LOUD STATIC NOISE IN COCKPIT AFTER SHUTDOWN AT GATE. FOUND WX RADAR TO TURN ITSELF ON WHEN TURNED OFF AND STAY IN TEST MODE. PULLED RT C/B AND LOUD STATIC NOISE WENT AWAY. REMOVED AND REPLACED WXR RDR RT PER MM 34 43 41. WXR RADAR OPS N ORMAL PER MM 34 43 00. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082632 1 20080514 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 947 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947 S25R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080527 EU 2008 5 27 USAA920081065 1 20080509 A 5347 D5311278220201 SEAT TRACK AIRBUS A319 A319112 3930323 EU BS 8070 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 715UW 1051 PIT - MAJOR REPAIR - C9 CHECK - CORROSION ON CABIN SEAT TRACK, BS 870 / FR 22, -Y1292. REPLACED CABIN SEAT TRACK, BS 87 0 / FR 22, -Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20080527 EA 2008 5 27 VNAA0804019 1 20080426 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE EMERGENCY EXIT FALSE ACTIVATION A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 05 237PS 7906 CREW REPORTED ON CLIMBOUT A LEFT EMERGENCY DOOR MESSAGE. CREW ELECTED TO RETURN TO DAY AND LANDED WITHOUT INCIDENT. MA INTENANCE INSPECTED THE LEFT HAND EMERGENCY DOOR AND FOUND NO DEFECTS. MAINTENANCE DEFERRED THE DOOR INDICATION ONLY PE R MEL 52-70-03. MAINTENANCE COMPLIED WITH AN OPS CHECK OF THE EMERGENCY EXIT DOOR INDICATION IN ACCORDANCE WITH THE AIR CRAFT MAINTENANCE MANUAL. OPS CHECK WAS GOOD, MEL WAS CLEARED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080527 EA 2008 5 27 VNAA0804023 1 20080430 A 2740 706010 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PITCH TRIM FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 223JS 2447 7892 CREW REPORTED AN AMBER PITCH TRIM, MACH TRIM AND AUTO PILOT PITCH TRIM CAS MESSAGES ON CLIMB TO CRUISE OUT OF CLT. CRE W ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT WHERE EMERGENCY EQUIPMENT DID RESPOND. MAINTENANCE REMOVED AND R EPLACED THE HSTCU IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080527 EA 2008 5 27 VNAA0805006 1 20080505 A 2750 860D10018 FCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS FAILED A VNAA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 GL 05 259PS 9090 7945 CREW REPORTED ON APPROACH A FLAPS FAIL AT ZERO INDICATION. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAI NTENANCE REMOVED AND REPLACED THE FECU IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE GOOD . AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080527 NE 2008 5 27 ASAA0852932 2 20080511 A 7261 CFM567B27 ENGINE BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE NR 1 OIL CONSUMPTION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 587AS 2148 35684 895977 NR 1 ENGINE OIL CONSUMPTION AT .62 PER SEAMC. AIRCRAFT RESTRICTED FROM ETOPS SERVICE UNTIL EXCESSIVE OIL CONSUMPTION IS CORRECTED. PER SEAMC, AFTER LAST OIL ADD LP 6415958 NR 1 ENG OIL CONSUMPTION IS NOW .12 AC IS NOW ETOPS QUALIFIED. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080527 NM 2008 5 27 USAA920081056 1 20080511 A 5754 114N407639 SKIN BOEING 757 7572S7 1384962 NM NR 2 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - LEFT WING NR 2 SLAT COVE PANEL CRACKED, SS 607. REPLACED LEFT WING NR 2 SLAT COVE PANE L CRACKED, SS 607 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A2NM 20080527 NM 2008 5 27 USAA920081057 1 20080421 A 5320 146N54125 ANGLE BOEING 757 7572S7 1384962 NM BS 1375-1380 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - CORROSION ON ANGLE, BS 1375 - BS 1380, RBL 23. REPLACED ANGLE, BS 1375 - BS 1380, RBL 23 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 20080527 NM 2008 5 27 SWAA082645 1 20080514 A 5320 6554892 STIFFENER BOEING 737 7373H4 1384600 NM BS 320 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 320, STR 21L. REMOVED AND REPLACED STIFFENER PER BO EING DRAWING. 2 L 7 2 4F RT A16WE 20080527 EU 2008 5 27 SA08033 1 20080509 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 725UW 16291 16291 1135 TPA - FWD EMERGENCY LIGHT POWER UNIT FAILED. MAINTENANCE REPLACED FWD POWER SUPPLY, OPS OK. 2 L 7 2 4F RT A28NM 20080527 WP 2008 5 27 UPS08852224 1 20080416 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 BOTH FLOOR SEAT TRACKS WORN FOR F/E'S SEAT. REPLACED FWD AND AFT SEAT TRACKS IAW SRM 51-01-24 AND 51 -03-00. 2 L 7 4 4F RT 4A25 20080527 2008 5 27 SWAA082631 4 20080514 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080521 NM 2008 5 21 2008UALA02650 1 20080506 A 5411 311T3110 SPAR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 NR 2 PYLON UPPER SPAR WEB IS CRACKED AT OTBD DRAIN HOLE, NAC STA 156. MAJOR REPAIR ACCOMPLISHED, ACCOMPLISHED HFEC AND FOUND 2 CRACKS APPROX .5 INCH LONG. STOP DRILLED CRACKS. FABRICATED AND INSTALLED A REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 20080521 CE 2008 5 21 051108N425CS0 1 20080511 A 2611 47359717 SMOKE DETECTOR CESSNA 525 525A 2076615 CE WILINT FJ44 FJ44 66000 GL CARGO BAY CONTAMINATED E Z5FA O OTHER N FALSE WARNING AP APPROACH 1 EA 63 425CS 525B0132 BAGGAGE SMOKE LIGHT INDICATION ON APPROACH. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MAINT PERSONNEL FOUND PAINT OVERSPRAY ON BAGGAGE SMOKE DETECTOR AND REPLACED WITH REPAIRED UNIT. AIRCRAFT RETURNED TO SERVICE. 1 L 7 1 4F 4 F RT A1WI E3GL 20080522 CE 2008 5 22 DXTA200803074 1 20080520 A 5280 DOOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG OUT OF ADJUST E DXTA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 07 656QS 5605732 THUMPING /VIBRATION FELT IN COCKPIT FLOOR YOKE AND PEDALS WHEN SPEEDBRAKES ARE DEPLOYED. ADJUSTED LT MLG DOOR FIT IAW M M 32-10-00. GEAR SWINGS GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A22CE E00059EN 20080522 SO 2008 5 22 GLBA20061104 1 20080515 A 3260 922AA2YA6P2722 PROXIMITY SENSOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE MLG MALFUNCTIONED A GLBA O OTHER S AFFECT SYSTEMS AP APPROACH 1 NM 03 108UX 120108 FLIGHT NR 5161 ENROUTE, PILOTS REPORTED THAT THE GEAR WOULD NOT EXTEND. PILOTS USED ELECTRICAL EXENTENSION PROCEDURES T O LOWER THE GEAR. MAINT REMOVED AND REPLACED THE (A) SYSTEM DOWLOCK PROXIMITY SENSOR IAW. MM 32-61. OPERATIONAL CHECK WA S GOOD. RII INSPECTION COMPLIED WITH IAW TASKCARD 4.3.8. PN OFF 922AA2Y-A6P-2722A. 2 L 7 2 4T 4 T RT A31SO E20NE 20080522 SO 2008 5 22 C2XA08CL057 1 20080506 A 3240 4131 SHUTOFF VALVE EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL BRAKES FAULTY A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 14905 145476 FLIGHT NR 2691, THE CREW REPORTED A IB BRAKE INOP MESSAGE ON THE ECIAS AFTER LOWERING GEAR. REPORTED BRAKES WERE NOT NE ARLY AS EFFECTIVE ON LANDING. MAINTENANCE INSPECTED AND REPLACED THE IB BRAKE SHUTOFF VALVE. OPERATIONAL CHECKS WERE G OOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080522 SO 2008 5 22 GUUA05110802 1 20080511 A 3233 2060500005 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE NLG INOPERATIVE A GUUA O OTHER O OTHER AP APPROACH 1 SO 29 285AS 120265 DURING APPROACH, NOSE GEAR TAKES APPROXIMATELY 15 SECONDS TO LOWER AND FULLY EXTEND. REPLACED NOSE GEAR ACTUATOR. 2 L 7 2 4T 4 T RT A31SO E20NE 20080522 SO 2008 5 22 C2XA08SH073 1 20080509 A 5210 ROLLER EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL PAX DOOR OUT OF ADJUST A C2XA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 27 12136 145719 FLT 4920 (FERRY FLIGHT) CABIN DOOR FAIL TO CLOSE. MX ADJUSTED STABILIZER ARMS AND ROLLERS ON CABIN DOOR OPS CHECK GOOD, FORCE APPLIED CHECK 40 LBS IAW AMM 52-18-00. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F 4 F RT TE6CH 20080522 SO 2008 5 22 C2XA08RI063 1 20080428 A 3350 1317 BULB EMB 145 EMB145XR 3260214 SO ALLSN AE300 AE3007A GL EMERGENCY LIGHTS BURNED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 23139 145731 DURING ROUTINE MAINT, MX FOUND MAIN ENTRANCE DOOR EMERGENCY LIGHT (CEILING PANEL) INOPERATIVE. MX REMOVED AND REPLACED T HE BULB AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 20080522 NM 2008 5 22 DU4R2008203 1 20080511 A 5315 FLOORBEAM BOEING 737 737448 13844BU NM CFMINT CFM56 CFM563B2 13802 EU BS 360 CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 742VA 24773 S/O 312001 N/R 28019, CORROSION AT CABIN FLOORBEAM UPPER CHORD UPPER SURFACE BS 360 LBL 15 TO RBL 15 W/L 201. 2 L 7 2 4F 4 F RT A16WE E21EU 20080522 NM 2008 5 22 F3LA200800274 1 20080514 A 3397 WIRE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE EMERGENCY LIGHT MISINSTALLED A F3LA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 03 925FR 12 2103 REFERENCE LOG PAGE 321828. DURING PRE FLIGHT INSP, THE CREW NOTED EMERGENCY EXIT LIGHT OVER L2 DOOR WAS ILLUMINATED. THE CREW WAS UNABLE TO EXTINGUISH WITH EMERGENCY EXIT LIGHT SWITCH IN THE COCKPIT. MAINT SWAPPED WIRES AND TESTED EMERGENCY EXIT LIGHTS IAW THE REQUIREMENTS OF AMM 33-51-00-710-001. MAINT OPERATION CHECKED GOOD AND RETURNED THE AC TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080522 WP 2008 5 22 ABXA080150 1 20080430 A 5330 59114015 SKIN DOUG DC9 DC932F 3022067 WP BS 160 L20-21L CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 FUSELAGE SKIN CRACKED AT STA 160, LONGERON 20 - 21 LEFT AT AIRSTAIR HINGE FORWARD SIDE. REPAIRED FUSELAGE SKIN CRACK IA W DC9 SRM. 2 L 7 2 4F A6WE 20080522 WP 2008 5 22 ABXA080152 1 20080501 A 5210 49559481 PAN DOUG DC9 DC932F 3022067 WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 MAIN ENTRY DOOR PAN CRACKED FORWARD SIDE (BOTTOM HINGE) SECOND STOP FROM BOTTOM. REMOVED AND REPAIRED DOOR IAW DC9 SRM. 2 L 7 2 4F A6WE 20080522 EU 2008 5 22 MALA080098 1 20080516 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 236-251 DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 452XJ 340B452 ON THE RIGHT FUSELAGE, STA 236.5-251.5 AND EXTENDING 8.3 INCHES FROM SL1636, THERE IS AN EXISTING RT FUSELAGE SKIN DOUBL ER REPAIR THAT IS NOT LISTED ON THE MRAL. MAP THIS REPAIR AND SEND IT TO MESABA ENGINEERING. INSPECTED THIS REPAIR AND FOUND IT AS PER EO NR S53574. REPAIR ACCEPTED AS IS, PROVIDED IT COMPLIES WITH SAAB REPAIR STATEMENT 340SDS015017. 2 L 7 2 4T RT A52EU 20080523 EA 2008 5 23 MASA200800406 1 20080516 A 2697 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA SMOKE DETECTOR UNSECURE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17337 7337 ASH 2781 PHX-BFL. LAV SMOKE DETECTOR WILL NOT TEST. MX REPORTED THE DETECTOR DOES NOT TEST. MX RE-SECURED CONNECTOR. 2 L 7 2 4F RT A21EA 20080523 NM 2008 5 23 UPS08M52193 1 20080407 A 5313 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C CTR CARGO COMPT BILGE AREA BETWEEN STA 5-113 & STA 1541 LEFT LONGERON 44 FOUND SUSPECTED CRACK WITH ST ICKER NR 5190. HFEC INSP C/O & FOUND CRACK APPROX 1 INCH. CRACKED LONGERON SPLICE BETWEEN STA 5-113 & 1541 LT L-44 REM OVED. SPLICE HOLES PICKED UP & PROTECTED. NEW SPLICE INSTALLED PER SRM 51-33-01VII R35. 2 L 7 3 4F RT A22WE 20080523 NM 2008 5 23 USAA920081055 1 20080508 A 5754 SKIN BOEING BOEING 737 737401 1384701 NM NR 2 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 53289 23879 CLT - MAJOR REPAIR - C4 CHECK - LEFT WING NR 2 SLAT LOWER SKIN REPAIR DOUBLER CRACKED. REPAIRED LEFT WING NR 2 SLAT LOW ER SKIN REPAIR IAW SRM 57-43-01 REPAIR 6. 2 L 7 2 4F RT A16WE 20080523 EA 2008 5 23 MASA200800408 1 20080518 A 5250 STRIP CNDAIR CL600 CL6002B19 1900309 EA COCKPIT DOOR LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17231 7231 ASH 2825 PHX - REPORTED HAVING TROUBLE CLOSING THE COCKPIT DOOR. MX RE-SECURED A LOOSE TRIM STRIP THAT WAS OBSTRUCTING THE DOOR. 2 L 7 2 4F RT A21EA 20080527 WP 2008 5 27 UPS08852215 1 20080418 A 5347 3657503501 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 COCKPIT STA 32 OBSERVERS SEAT FWD SEAT TRACK HAS ELONGATED HOLES. REPLACED 2ND OBSERVERS FWD SEAT TR ACK IAW SRM 51-01-02 AND SRM 51-03-00. 2 L 7 4 4F RT 4A25 20080527 EA 2008 5 27 VNAA0804018 1 20080426 A 2421 IDG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 1 UNDERSERVICED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 259PS 7945 CREW REPORTED A NR 1 IDG AND NR 1 GENERATOR INOP CAS MESSAGES ON TAKEOFF ROLL. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PROPERLY SERVICED THE NR 1 IDG OIL LEVEL. NO LEAKS NOTED, OPS CH ECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080527 EA 2008 5 27 VNAA0804022 1 20080429 A 5200 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE GROUND POWER OPEN A VNAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 05 703PS 10137 CREW REPORTED A WHISTLING NOISE IN THE NOSE AREA ON CLIMBOUT OF CLT. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT I NCIDENT. MAINTENANCE INSPECTED AND FOUND THE GROUND POWER DOOR OPEN. MAINTENANCE SECURELY CLOSED THE DOOR. NO DEFECTS OR DAMAGE NOTED AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080527 WP 2008 5 27 UPS08852218 1 20080421 A 5740 37702921 FITTING DOUG DC8 DC873F 302199F WP STUB WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3, 2 CRACKED REINFORCEMENT PLATES IN NR 2 STUB WING AT SLOT ACTUATOR. REPLACED LEFT WING INBOARD SLOT ACTUATOR ATTACH FITTING IAW MM 27-80-01-2 AND SRM 51-03-00-0. 2 L 7 4 4F RT 4A25 20080527 NM 2008 5 27 SA08034 1 20080510 A 4990 OIL SYSTEM AIRBUS A319 A319132 3930340 NM APU LOW A USAA O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 829AW 1563 DCA FLT 44 EN ROUTE DCA-PHX. APU AUTO SHUTDOWN WITH NR 1 GENERATOR BECOMING INOP EN ROUTE. MAINTENANCE SERVICED APU OI L TO CORRECT LEVEL AND RESET NR 1 GENERATOR CIRCUIT BREAKER. OPS CHECKS OK. 2 L 7 2 4F RT A28NM 20080527 EA 2008 5 27 VNAA0805001 1 20080501 A 5200 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE GROUND POWER OPEN A VNAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 05 706PS 10150 CREW REPORTED ON CLIMBOUT A WHISTLING SOUND COMING FROM THE NOSE AREA. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE GROUND POWER DOOR OPEN. MAINTENANCE SECURED THE DOOR CLOSED. NO DEFECT S OR DAMAGE NOTED AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080527 EA 2008 5 27 VNAA0805008 1 20080505 A 2780 SLAT SYSTEM CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE MALFUNCTIONED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 720PS 10178 CREW REPORTED A SLAT FAIL CAUTION MESSAGE ON TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINT ENANCE INTERROGATED THE MDC AND FOUND NO FAULTS. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE SLATS IN ACCORDANCE WI TH THE AIRCRAFT MAINTENANCE MANUAL. OPS CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080527 EA 2008 5 27 VNAA0805010 1 20080507 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE CABIN ODOR A VNAA B A EMER. DESCENT UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 05 705PS 10144 CREW REPORTED A FORWARD SMOKE IN LAV WARNING MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO DAY AND LANDED WITHOUT IN CIDENT. MAINTENANCE INSPECTED AND FOUND NO SIGNS OF A FIRE IN THE LAVATORY. MAINTENANCE SUSPECTS ENGINE WASH SOLUTION FOR THE CAUSE OF THE ODOR. MAINTENANCE GROUND RAN ENGINE AND BURNED OFF ALL REMNANTS OF THE SOLUTION IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE GOOD, NO LEAKS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080527 NM 2008 5 27 SWAA082643 1 20080514 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 500B S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CRACKED AT BS 500B, STR 10R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082668 1 20080515 A 5754 SKIN BOEING 737 7373A4 1384585 NM RT WING LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082669 1 20080515 A 5753 113A3943201 FLAP TRACK BOEING 737 7377H4 1384404 NM LT WING LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED 10Y CHECK, FOUND LT WING OUTBOARD T/E AFT, NR 2 FLAP TRACK LOOSE. REMOVED AND REPLACED FLAP TRACK PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082661 1 20080515 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 467WN 33830 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082663 1 20080515 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM BS 787 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND KEEL BEAM CHORD CORRODED AT BS 787, RBL 6.5. REMOVED AND REPLACED CHORD PER EA. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082637 1 20080514 A 3350 20121 CHARGER BOEING 737 7375H4 138449D NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082639 1 20080514 A 3350 311500 LENS BOEING 737 7375H4 138449D NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082664 1 20080515 A 5330 6545777 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 23252 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT UPPER AFT CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080917 2008 9 17 ASAA0853396 4 20080820 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM FLT MANAGE FAULTED A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 558AS 8309 35177 AFTER ENGINE START FMC DISAGREE ILLUMINATED. PERFORMED QRH PROCEDURE RESET OK, PER PROCEDURE. 2 L 7 2 4F RT A16WE 20080917 NM 2008 9 17 ASAA0853399 1 20080821 A 4990 38810521 INDICATOR BOEING 737 737890 1384527 NM APU ACTIVATED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 577AS 35186 WHILE ACCOMPLISHING TASKCARD 78349013 FOUND APU DELTA P POPPED ACCOMPLISHED APU OIL FILTER INDICATOR SERVICING PER MM 49 91 13. 2 L 7 2 4F RT A16WE 20080917 NM 2008 9 17 ASAA0843379 1 20080803 A 5240 654587548 DOUBLER BOEING 737 7374Q8 138447Q NM R1 DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 R1 INNER CHORD DOUBLER CORRODED AT FORWARD SIDE OF DOOR CUTOUT STA 293 TO STA 298. REMOVED, FABBED AND INSTALLED NEW R1 DOOR INNER CHORD DOUBLER IAW SRM 51-40-02 AND 51-30-01. 2 L 7 2 4F RT A16WE 20080917 NM 2008 9 17 ASAA0843380 1 20080719 A 5320 655287897 SILL BOEING 737 7374Q8 138447Q NM BS 948-1006 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 L2 DOOR MOP SILL IS CORRODED FROM STA 948 TO 1006. REMOVED AND REPLACED MOP SILL IAW B7373 400 SRM 51 40 02 AND 51 40 0 5. 2 L 7 2 4F RT A16WE 20080917 NM 2008 9 17 ASAA0843382 1 20080721 A 5320 652072629 THRESHOLD BOEING 737 7374Q8 138447Q NM BS 447-485 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 FWD CARGO DOOR CUTOUT THRESHOLD WEB CORRODED ON LWR SIDE AROUND NUT PLATES STA 447 TO STA 485 RBL 30 TO RBL 32 WL 156. REMOVED DAMAGED THRESHOLD WEB LOCATED DRILLED AND INSTALLED A REPLACEMENT WEB IAW SRM 51-40-02 FIG 9. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 2008UALA04358 1 20080820 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU BS 277 S24R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 333UA 24228 DAMAGE AT FRAME 277 AND STR 24R. *S/D* MAJOR REPAIR ACCOMPLISHED: MFG & INSTALLED REPAIR FILLERS, DOUBLER & TRIPLER. 2 L 7 2 4F 4 F RT A16WE E21EU 20080918 NM 2008 9 18 2008UALA04374 1 20080822 A 3350 20131A POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INTERMITTENT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT AND PATH LIGHTS AT DOORS 2L-2R IN BUSINESS CLASS COME ON INTERMITTENTLY. *S/D* REPLACED POWER SUPPLY M6 002 AT DOOR 2R. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 NM 2008 9 18 2008UALA04096 1 20080801 A 5315 STIFFENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FLOORBEAM CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 STA 246 FLOORBEAM VERT STIFFENER CRACKED 2ND HOLE FROM BOTTOM RBL 26 FWD SIDE OF FLOORBEAM. *S/D* MAJOR REPAIR ACCOMPL ISHED. INSTALLED NEW STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 20080918 EU 2008 9 18 UPS08153223 1 20080822 A 5321 B5327077700000 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 138UP 0821 INSPECTION TYPE:C1 MAIN CARGO FLOOR BOARD PANEL 252WJ HAS A FIELD REPAIR. REPAIRED MAIN CARGO FLOOR PANEL 252WJ REF SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20080918 WP 2008 9 18 ASAA0883402 1 20080822 A 5210 5910081167 DOOR DOUG DC9 DC983 3022083 WP L1 STIFF A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 968AS 54172 53016 F/A REPORTS L1 DOOR DIFFICULT TO OPEN AND CLOSE. CHECK DOOR ADJUSTMENT, FOUND TO BE WITHIN LIMITS PER MM 52 11 00. 2 L 7 2 4F RT A6WE 20080918 NM 2008 9 18 ASAA0853403 1 20080822 A 7714 3205490040 SENSOR BOEING 737 737890 1384527 NM NR 2 ENGINE N2 FAULTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 559AS 7600 35178 AIRCRAFT DISPLAYS DOWNGRADED SHOWS NO N2 ON EITHER ENGINE. REGULAR METHODS TO RESTORE FAILED. VERIFIED PROBLEM CW MM F IM 73 00 00 810 801 F100 NO RECENT FAULTS, NO FAULT HISTORY AND NO MAINT HISTORY. DISPLAY RESET TO NORMAL. RAN BOTH EN GINES, ALL CHECKS NORMAL. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 SWAA084799 1 20080831 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 232WN 32500 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 SWAA084800 1 20080830 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 252WN 34973 EEPLS END CAP MISSING AT ROW 1 ABC. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 UPS08553203 1 20080813 A 5420 ANGLE BOEING 757 75724APF 1384969 NM ZONE 445 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 NR 2 ENGINE STRUT FWD MOUNTING SURFACE FOR PANEL 445BL STRUCTURE IS DAMAGED. REMOVED, FABRICATED AND INSTALLED PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20080918 NM 2008 9 18 SWAA084803 1 20080901 A 3350 20311A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 RIGHT AFT CABIN EMERGENCY EXIT LIGHT WILL NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 SWAA084809 1 20080829 A 3350 1619 LAMP BOEING 737 7373A4 1384585 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 2008UALA04299 1 20080816 A 3397 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY LIGHT LT FROM ROW 45 TO 53 INOP. *S/D* REPLACED EEL CABLE. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 NM 2008 9 18 2008UALA04300 1 20080816 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY LIGHT AFT GALLEY LOWER WALL LT INOP. *S/D* REPLACED EEL CABLE. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 NM 2008 9 18 ASAA0843415 1 20080812 A 5311 654653970 FRAME BOEING 737 7374Q8 138447Q NM BS 616 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 FRAME INNER CHORD BS 616 RT BELOW FLOOR IS CRACKED FROM BOTTOM TIP TO THE LWR HOLE. REPAIRED IAW ERO 8605 AND EA 5310 0 28114 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 ASAA0843420 1 20080825 A 5753 6546486 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 DENT 1 AND 2 (WBL 87.5 AND WBL 87.8) FOUND BEYOND ALLOWABLE LIMITS IAW B737 400 SRM 57 53 02. TRANSFERRED FROM MIG5 NR 5106400 LT INBOARD MID FLAP T/E WEDGE. LT INBOARD MID FLAP T/E WEDGE REPAIRED IAW B737 400 SRM CH 51 70 10. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 SWAA084811 1 20080901 A 5311 6546526 FRAME BOEING 737 7373T0 1384582 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 ASAA0843422 1 20080812 A 5330 65C337569 SKIN BOEING 737 7374Q8 138447Q NM BS 331 S20-21R DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 DENT IN EXTERIOR SKIN OF FUSELAGE AT BS 331.5 BETWEEN STR 20R AND 21R. REPAIRED IAW CASCADE ERO 8620 AND EA 5330 02384. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 SWAA084813 1 20080830 A 5315 6546811 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, LBL 12. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 20080918 2008 9 18 SWAA084814 4 20080830 A 2565 63500 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 736SA 27868 L2 DOOR EMERGENCY EVAC SLIDEOUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 UPS08553207 1 20080813 A 5320 SUPPORT BRACKET BOEING 757 75724APF 1384969 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 RIGHT MLG BODY DOOR TANG CUTOUT SEAL RETAINER SUPPORT BRACKET IS CRACKED AT LOWER CORNER. REMOVED, F ABRICATED AND INSTALLED PER SRM 51-20-02-G SRM 51-40-02. 2 L 7 2 4F RT A2NM 20080918 WP 2008 9 18 UPS08853210 1 20080812 A 5340 BRACKET DOUG DC8 DC871F 302199D WP BS 880 LBL60 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 CRACK ON ANGLE BRACKET MAIN CABIN WING BOX ST 880 LBL 60. REMOVE AND REPLACE BRACKET IAW SRM, 51-1-2 1, 51-1-8, 51-3-2. 2 L 7 4 4F RT 4A25 20080918 WP 2008 9 18 UPS08853211 1 20080810 A 5340 4597643U1 FITTING DOUG DC8 DC871F 302199D WP BS 25 L21R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 CORRODED FUSELAGE FRAME FITTING ON THE UPPER SURFACE OF INTERIOR CUSP EXTRUSION SRA 25 L21R. REMOVED AND REPLACED FITTING IAW SRM, 51-3-1, 51-1-8. 2 L 7 4 4F RT 4A25 20080918 NM 2008 9 18 SWAA084820 1 20080901 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 520 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 SWAA084822 1 20080901 A 5330 6545800 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA . 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 2008UALA04151 1 20080802 A 3397 BR963165 CONNECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SEAT 23 ABC UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 837UA 1474 EEL LIGHT AT SEAT 23ABC INOP. *S/D* SECURED CONNECTOR. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080918 WP 2008 9 18 UPS08853196 1 20080810 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP BS 200 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 TOOL MARK ON INNER SKIN INSIDE FWD RT SERVICE DOOR AFT DOOR JAMB BOX LOWER CORNER STA 200. REMOVED D AMAGE AND INSTALLED REPAIR DOUBLER IAW, SRM, 51-1-8, 53-2-0, 51-1-21. 2 L 7 4 4F RT 4A25 20080918 NM 2008 9 18 UPS08M53169 1 20080804 A 5310 DOOR FRAME DOUG MD11 MD11F 3023600 NM LT MLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:C LT MLG DOOR AROUND CTR HINGE FOUND FRAME CRACKED. CRACKED FRAME REMOVED, REPAIR FRAME PART, FILLER & DOUBLER FABRICATED AND INSTALLED AS PER EN1338-08 AND SRM 51-31-011 VOL II REV 40. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53170 1 20080807 A 5754 SKIN DOUG MD11 MD11F 3023600 NM NR 6 SLAT DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:C LT WING NR 6 SLAT EXTERIOR SURFACE FOUND QTY 04EA DENTED AREA AT 20 TO 27 INCHES FROM B/B END AND 26 I NCHES FROM T/E. DENTED AREAS MEASURED DEPTH: 0.039 INCH AND FOUND EXCEED LIMIT AS PER SRM 57-10-00 FIG 16 VOL I REV 40. DENTED AREA TRIMMED OFF PER EN1340-08 & HFEC INSP NO CRACK EVIDENT. REPAIR PARTS FABRICATED AND INSTALLED AS PER EN13 40-08 AND SRM 51-31-01 VOL II REV 40. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53171 1 20080806 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 1561-1601 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:C CTR CARGO STA 1561 TO 1601 BILGE AREA LONGERON 48 RT FOUND CORRODED. LONGERON CORR CLEANED, FOUND EXC EED LIMIT AT STA 1571-1591 L48R AS PER SRM 53-00-01 FIG 4 VOL I REV 40. THICKNESS REMAINED 0.034 INCH, ORIG THICKNESS 0 .100", MATERIAL REMOVED 0.066". CORR LONG I BEAM SPLICE CUT AT STA 1571 & 1591 L48R & HFEC INSP NO CRACK EVIDENT. REPA IR PART FAB & INSTALLED PER SRM 53-10-00 FIG 2 VOL I REV 40. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53217 1 20080822 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 13 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53218 1 20080820 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 27 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 2008UALA04317 1 20080816 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1480 S26-27L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 AFT PIT STA 1480 BETWEEN STR 27L AND 26L FRAME IS DENTED. *S/D* MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NM 2008 9 18 UPS08M53176 1 20080817 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 9 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAI R BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53178 1 20080819 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 15 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 2008UALA04318 1 20080816 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 580 S23-24L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 FWD CARGO PIT, DENT ON FUSELAGE FRAME UPPER FLANGE AT STA 580, STR 23L TO 24L. *S/D* MAJOR REPAIR ACCOMPLISHED: CUT O UT DAMAGE ON FRAME & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NM 2008 9 18 2008UALA04319 1 20080816 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1520 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 AFT PIT STA 1520, STR 25L, FRAME IS DENTED. *S/D* MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & INSTALLED DOUBLER REPAI R. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NM 2008 9 18 UPS08M53185 1 20080822 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 7 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53187 1 20080819 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 15 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53188 1 20080822 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 16 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 2008 9 18 2008UALA04330 4 20080818 A 2565 EA81020401 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR SLIDE INTERMITTENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 DOOR 1L ARM LIGHT IS INTERMITTENT. REPLACED SWITCHS S10214 & S10215. OP CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NM 2008 9 18 2008UALA04136 1 20080805 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 52 ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY LIGHT INOP: SEAT 52 ABC. 2 L 7 4 4F 4 F RT A20WE E24NE 20080527 NM 2008 5 27 SWAA082644 1 20080514 A 3397 W116010920 WIRE BOEING 737 7373Q8 1384670 NM EMERGENCY LIGHTS BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. FOUND BROKEN WIRE. REPAIRED WIRE PER WDM. 2 L 7 2 4F RT A16WE 20080527 2008 5 27 SWAA082642 4 20080514 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 787SA 29812 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082672 1 20080515 A 5311 6545812 FRAME BOEING 737 7373H4 1384600 NM BS 328 S20R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082653 1 20080515 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727C S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082654 1 20080515 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 747 S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082656 1 20080515 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 767 S24R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 24R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 ASAA0842952 1 20080429 A 5755 SKIN BOEING 737 7374Q8 138447Q NM NR 6 SPOILER DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 NR 6 SPOILER HAS A BULGE ON THE TOP SIDE WITH DELAMINATION. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLE R AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082686 1 20080517 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082687 1 20080517 A 5753 6546434370 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD T/E AFT FLAP OUTBOARD END DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082691 1 20080516 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 520 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082713 1 20080518 A 5330 6545777 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERVICE DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082698 1 20080518 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 485WN 32473 EEPLS LENS LOOSE AT ROW 21 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082674 1 20080518 A 2121 215201 FAN BOEING 737 7373H4 1384600 NM E&E BAY FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 304SW 22944 GASPER FAN CIRCUIT BREAKER OPENED AND CABIN HAD A SMOKE ODOR. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082722 1 20080518 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 663 S2L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 2L CRACKED AT BS 663. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082723 1 20080518 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 663 S3L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 3L CRACKED AT BS 663. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080527 2008 5 27 SWAA082696 4 20080518 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 456WN 32463 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 2008UALA04384 1 20080821 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ROWS 1-2AB UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 641UA 25091 EEL LIGHTS LEFT SIDE FC ROWS 1AB & 2AB INOP. SECURED EMERGENCY LIGHTS TO POWER SUPPLY RIBBON. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20080918 NM 2008 9 18 2008UALA04387 1 20080821 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE SEAT 2F MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 794UA 26953 ESCAPE PATH LIGHTING BAR MISSING ALONG SIDE SEAT 2F. LIGHT BAR OUT OF POSITION. REPLACED BAR. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080918 NM 2008 9 18 2008UALA04115 1 20080803 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EEL INOP: 56 RT. *S/D* REPLACED LAMP, OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 NM 2008 9 18 2008UALA03857 1 20080713 A 5311 FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 196 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 FUSELAGE FRAME 196.5 CRACKED AND BUCKLED FROM DAMAGE FROM TOW TRACTOR. *S/D* MAJOR REPAIR. REPLACED UPPER AND LOWER F RAME CAPS AND WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 20080918 NE 2008 9 18 2008UALA05394 2 20080822 A 7200 51B156 BEARING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 127UA 38395 18019 28813 FOUND METAL DEPOSIT ON NR 1, 1.5 AND 2 BEARING CHIP DETECTORS AND MAIN OIL FILTER. WILL REQUIRE NR 4 ENG REPLACEMENT. ENGINE WAS REPLACED AT LAX PRIOR TO FURTHER FLIGHT. SHOP TEARDOWN FOUND THE NR 1 BEARING WITH A BALL COMPLETELY MISSIN G. THE BALL HAD FAILED, AND PIECES WERE FOUND IN THE FORWARD SUMP. THE CAGE POCKET WAS DAMAGED, BUT THE INNER AND OUTE R RACES, AND THE REMAINING BALLS SHOWED VERY LITTLE DAMAGE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080602 NM 2008 6 2 CALA0800461 1 20080511 A 5311 65C34356 FRAME BOEING 737 737524 1384721 NM BS 482A CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 RIGHT SIDE BS 482A INBOARD ATTACH FASTENER HOLE ON AIR CONDITIONING (A/C) BRACKET CRACKED. REPAIRED FRAME BS 482A RIGHT AT A/C RAIL BRACKET PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080602 NM 2008 6 2 CALA0800469 1 20080519 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM BS 747 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17640 28901 FUSELAGE FRAME CRACKED AT STATION 747 BETWEEN S8R AND S9R. REMOVED DAMAGE, FABRICATED ANGLES, TREATED, PRIMED AND INSTA LLED PER EA 5310-04498 OP NR 2. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 AALA200801502 1 20080603 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 198AA 32392 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NR 1 DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 20080701 NM 2008 7 1 AALA200801503 1 20080603 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 198AA 32392 DFW - EMERGENCY LIGHT AT SEAT 31D DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 31D. SYSTEM GROUND CHEC KED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 20080701 2008 7 1 TRAX200800684 4 20080523 A 3140 DCU CNDAIR CL600 CL6002B19 1900309 EA NR 1 & 2 MALFUNCTIONED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 927EV 7844 ON APP INTO ATL FUEL TOTALIZER WENT TO -0- RIGHT MFD PANEL SHOWED NO FUEL IN LEFT TANK AND THE AUTO INHIBIT INDICATOR CA ME ON. RIGHT TANK READ 1920 LBS. ALL INDICATIONS RETURNED TO NORMAL ON LANDING. FLT 4801 DEL 42 MINS. REMOVED AND RE PLACED DCU 1 AND DCU 2 IAW CRJ AMM 31041-04. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819726 1 20080530 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA NOSE MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 464SW 7827 NOSE GEAR WOULD NOT EXTEND ON FIRST ATTEMPT. SECOND ATTEMPT WAS SUCCESFULL. (FLT 3836) INSPECTED ASSOCIATED COMPONENTS AND SWUNG GEAR SEVERAL TIMES AND PERFORMED MANUAL GEAR RELEASE. ALL OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 20080701 SO 2008 7 1 SWIA200819737 1 20080603 A 2150 A/C PACK EMB 120 EMB120ER 3260203 SO LEFT ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 236SW 120312 THE LT PACK FAILED AND A BURNING SMELL WAS NOTED. (FLT 5476) INSPECTED AND WASHED LT PACK HEAT EXCHANGER ASSEMBLY. OP S CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 20080701 EA 2008 7 1 SWIA200819768 1 20080612 A 3230 555406 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 411SW 7067 WHILE SELECTING GEAR DOWN, RECEIVED A TRIPLE CHIME "GEAR DISAGREE" AND "NOSE GEAR DOOR" AURAL WARNING. (FLT 3812) REP LACED NOSE GEAR SELECTOR VALVE IAW AMM 32-33-01. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819712 1 20080404 A 2620 SWITCH CNDAIR CL600 CL6002B19 1900309 EA FIRE BOTTLE STICKS A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 433SW 7550 NR 2 ENGINE FIRE BOTTLE DISCHARGE SWITCH LIGHT STICKS CLOSED. (FOUND AT C-CHECK) REPLACED INNER SWITCH CONTACTS PER AMM 26-21-01-000-802. 2 L 7 2 4F RT A21EA 20080701 NM 2008 7 1 SWAA083403 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 26L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 2008UALA03575 1 20080624 A 3397 P10225027003 WIRE HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY LIGHT FROM ROW 45 TO 53 LT INOP. FOUND FAULTY POWER CABLE. REPLACED POWER CABLE OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 WP 2008 7 7 UPS08852280 1 20080421 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LOWER FLOOR SUPPORT FRAME FITTING STA 200, RT TUNNEL PIT IS CORRODED. FABRICATED AND INSTALLED FITTI NG IAW DWG 3772922, SRM 51-01-20D, SRM 51-01-21. 2 L 7 4 4F RT 4A25 20080707 NM 2008 7 7 UPS08M52285 1 20080401 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C CABIN - CORROSION ON SEAT TRACK CROWN, CHANNEL & FLANGE AT STA 808-839 X=107. CORROSION ON AFFECTED A REAS REMOVED. MAT'L THK:0.080" (FLANGE), MAT'L REMOVED: 0.040" (STA 808-824), MAT'L REMN:0.040" FOUND OUT OF LIMIT. DI SCREPANT SEAT TRACK ON EXIST SPLICE HAT SECT FROM STA 765-889 X=107 REMOVED. HFEC INSP C/O ON TRIM OFF AREA, NO CRACK E VIDENT. NEW SEAT TRACK FROM STA 765-889 X=10 7 REWORKED, HOLES PICK-UP, REPROTECTED, PAINTED AND FINALLY, INSTALLED. 2 L 7 3 4F RT A22WE 20080707 NM 2008 7 7 UPS08M52287 1 20080411 A 5730 SKIN DOUG MD11 MD11 3023602 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C RIGHT WING L/E LWR SURFACE ACCESS PANEL CUTOUT FWD APPROX STA XORS 813 FOUND CRACKED. ATTACH DOOR, FA STENERS & BRACKET REMOVED FROM CRACKED ACCESS PANEL CUTOUT. REPAIR DOUBLER FAB & FASTENER HOLES PICK-UP & PAINTED. REP AIR DOUBLER & ATTACHED BRACKET INSTALLED. RIGHT WING L/E PANEL 626FB INSTALLED AS PER AMM20-50-02R53. 2 L 7 3 4F RT A22WE 20080707 NM 2008 7 7 DHL2008760001 1 20080519 A 5320 WEB BOEING 727 7272B7 138407L NM AFT AIRSTAIRS CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 AFT AIRSTAIRS WELL AREA, RT LWR TORQUE BOX AT STA 1223 PREVIOUS REPAIR ON WORK PLATFORM WEB IS CRACKED BEYOND STOP DRILL ED HOLES. CUT-OUT DAMAGED AREA APPROX DIM 5 1/2 INCH BY 6 INCH. FAB REPAIR DOUBLER FROM 7075-T6 .0.40 INCH PO NR 90066 39 APPROX DIM 10 INCH BY 9 1/2 INCH AND INSTALLED REPAIR DOUBLER AT AFT AIRSTAIRS BS 1223 IAW B727 SRM 51-40-2 FIG 1 AND SRM 53-10-2 FIG 6 AND SRM 51-30-2. 2 L 7 3 4F A3WE 20080707 2008 7 7 2008UALA02675 4 20080507 A 2565 SPRING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L1 DOOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 656UA 25394 DEPLOYMENT BAR SNUBBER DOES NOT RETRACT BAR ON L1 DOOR. SUPPLEMENTAL DATA UPDATE, REPLACED GAS SPRING. OPS CHECKS GOOD . 2 L 7 2 4F 4 F RT A1NM E24NE 20080707 EU 2008 7 7 2008UALA02814 1 20080516 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 446UA 834 FOUND CORROSION ON FLOOR BEAM NR 215. 2 L 7 2 4F 4 F RT A28NM E40NE 20080707 NM 2008 7 7 2008UALA02815 1 20080516 A 5322 140T21021076 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 CORROSION ON SHEARTIE AT STA 1219, STR 37L TO 38L. MAJOR REPAIR ACCOMPLISHED: REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080707 NM 2008 7 7 2008UALA02824 1 20080515 A 3350 BR964421 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 838UA 1477 EMERGENCY LIGHTING ON SEATS 1A AND 1B IS BROKEN. REPLACED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A28NM E40NE 20080707 NM 2008 7 7 2008UALA02837 1 20080516 A 3350 767 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 550UA 25398 EXTERIOR EMERGENCY LIGHT INOP AT DOOR 4R. RELAMPED. OPS CHK'D GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080707 2008 7 7 NOCA03708 4 20080511 A 3417 4040800911 ADC BOEING 767 76736N 1385152 NM NR 2 MALFUNCTIONED A NOCA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 768NA 29898 F/O AIR DATA INSTRUMENTS PROCESSED RAPIDLY AND ADC FLAGS CAME INTO VIEW ALONG WITH L/R EEC WENT TO ALTERNATE MODE AILERO N LOCKOUT AND RUDDER RATIO EICAS MESSAGES. REMOVED AND REPLACED NR 2 DADC, CHECKED NR 2 DADC IAW MM CHAPTER 34-12-01 AL L EICAS MESSAGE CLEARED OBSERVED PROPER AILERON RESPONSE, AND RVSM GEN GMM 3.33.63, 34-11-00 AS REQUIRED. 2 L 7 2 4F RT A1NM 20080707 NM 2008 7 7 NOCA04108 1 20080518 A 2697 WIRE HARNESS BOEING 757 75728A 1384976 NM OVERHEAT WARNING OUT OF POSITION A NOCA K NONE N FALSE WARNING UK UNKNOWN 1 EA 15 750NA 26277 RIGHT ENGINE O/H LP 1 STATUS MSG DISPLAYED. CHECKED OVERHEAT SENSORS RESISTANCE AND CHECKED OK. REPOSITIONED HARNESS A ND CLEARED CONNECTOR PER MM 26-11-00 AND OPS CHECK OK. 2 L 7 2 4F RT A2NM 20080707 2008 7 7 R61A200800004 4 20080505 A 3140 70244401901 POWER SUPPLY EMB ERJ170 ERJ170100SU 3260403 NM MALFUNCTIONED A R61A A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 802MD 10561 17000013 CREW REPORTED MAU 3 FAIL MESSAGE IN FLIGHT AND CIRCUIT BREAKER POPPED ELECTRICAL BURNING SMELL WAS PRESENT. CREW DECLAR ED EMERGENCY LANDED IN GREENSBORO WITH OUT INCIDENT AND TAXIED TO THE GATE. MAINTENANCE WAS DISPATCHED AND FOUND MAU PO WER SUPPLY 2 TO HAVE A BURNT SMELL. 2 L 7 2 4F RT A56NM 20080707 SO 2008 7 7 RAIA00805019 1 20080516 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 813HK 145044 PRE FLT 5511 - STL - VARIOUS EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 3 POWER INVERTER. S YSTEM CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080707 NM 2008 7 7 ZZDA2008107 1 20080515 A 5320 J0602289 PAN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 986AT 55089 AFT CARGO COMPARTMENT LOWER PAN CORRODED BEYOND LIMITS. FABRICATED 4 EACH SPLICE 7075 0.040 HEAT TREATED TO 7075 T6 AND INSTALLED AFT CARGO DOOR JAMB LOWER PAN CORROSION REPAIR PER SRM 53-20-15. 2 L 7 2 4F TR A6WE 20080527 NM 2008 5 27 SWAA082697 1 20080518 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 457WN 33856 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082685 1 20080518 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 767 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 18L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082680 1 20080518 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 787 S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082740 1 20080520 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 276WN 32530 EEPLS LENS MISSING AT ROW 3 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082750 1 20080520 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 483WN 32472 EEPLS ASSY LOOSE AT ROW 1 ABC. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082776 1 20080522 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM BS 188 S17L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 188, STR 17L. REMOVED AND REPLACED CHORD PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082765 1 20080521 A 2560 P2070001 FLASHLIGHT BOEING 737 7373Q8 1384670 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 22Y CHECK, FOUND AFT CABIN EMERGENCY FLASHLIGHT LENS CRACKED. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082766 1 20080521 A 3350 101114 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 700GS 27835 FWD CABIN EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080528 SO 2008 5 28 RAIA00805004 1 20080504 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 818HK 145059 PRE FLT 5515 - STL - EMERGENCY LIGHT INOPERATIVE AT RIGHT OVERWING EXIT. MAINTENANCE CLEANED THE CONNECTOR TO THE LIGHT ASSEMBLY. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080528 NM 2008 5 28 SWAA082791 1 20080522 A 5754 STRUCTURE BOEING 737 7373T5 1384608 NM NR 2 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED AT LOWER INBOARD END. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082783 1 20080522 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 704SW 27838 DURING SCHEDULED HC1 CHECK, FWD LT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082788 1 20080522 A 2170 1808494 COALESCER BAG BOEING 737 7377H4 1384404 NM A/C BAY CLOGGED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 29 910WN 36618 ON CLIMBOUT OF TPA FLIGHT DECK FILLED WITH STRONG ELECTRICAL BURNING ODOR. INSPECTED AIRCRAFT, RAN ENGINES AND GASPER F AN. NO ODOR DETECTED. REMOVED AND REPLACED COALESCER BAGS PER MM. 2 L 7 2 4F RT A16WE 20080528 SO 2008 5 28 C2XA08IA123 1 20080512 A 3297 D3899926FA98SN CONNECTOR EMB 145 EMB145LR 3260212 SO LANDING GEAR DIRTY A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 13914 145430 IAH - FLIGHT 2331, THE CREW REPORTED A LANDING GEAR AIR GROUND FAILURE MESSAGE ON EICAS ON INITIAL TAKEOFF. THE AIRCRAF T RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED, CLEANED, AND REINSTALL ED THE CONNECTORS ON THE LEFT MAIN LANDING GEAR FORWARD PROXIMITY SENSORS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20080528 NM 2008 5 28 SWAA082751 1 20080520 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM BS 895-930 WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED BRDG CHECK, FOUND UPPER FUSELAGE SKIN WORN BETWEEN BS 895 AND BS 930 BELOW DORSAL FIN. REPAIRED SKIN P ER EA. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082724 1 20080519 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 947 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080522 EU 2008 5 22 MALA080097 1 20080512 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 284 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 452XJ 340B452 LEFT AND RIGHT SEAT TRACK CORRODED AT STA 284 BL0 AND BL18.3. REPAIRED SEAT TRACK. 2 L 7 2 4T RT A52EU 20080522 NM 2008 5 22 QXEA200800466 1 20080509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 706-712 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 425QX 4039 PDX- C4 CHECK - LT CENTER SEAT TRACK NR 9 AT STATION 706-712 HAS CORROSION PITTING ON THE INSIDE SURFACE IN MULTIPLE PLA CES. REPLACED THE SEAT TRACK. 2 H 7 2 4T RT A13NM 20080522 NM 2008 5 22 QXEA200800467 1 20080509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM BS 114-140 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 425QX 4039 PDX - C4 CHECK- NR 12 SEAT TRACK IS CORRODED ON THE OUTBOARD FLANGE AT STATIONS 114-140. BLENDED CORROSION AND HFEC NO CRACKS FOUND. ACID ETCH AND ALODINED. 2 H 7 2 4T RT A13NM 20080522 NM 2008 5 22 QXEA200800461 1 20080509 A 5320 INTERCOSTAL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 425QX 4039 PDX - C4 CHECK - RT ELEVATOR CONTROL QUADRANT HAS CORROSION AT LOWER FLANGE INTERCOSTAL X -57 TO X -59.5 STRINGER 28R. REMOVED RIVETS TO AID IN CORROSION REMOVAL. REMOVED CORROSION BY HAND. MATERIAL REMOVED .004 INCH. WITHIN LIMITS OF S RM. INSTALLED RIVETS, PRIMED AND PAINTED AREA. 2 H 7 2 4T RT A13NM 20080522 NM 2008 5 22 QXEA200800464 1 20080509 A 5320 STRUCTURE BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 425QX 4039 PDX - C4 CHECK- NUTPLATE AND MATING SURFACE CORRODED AT LOWER ANGLE OF CARGO PIT STEP STA X 783. REPLACED ANGLE AT STATI ON X 783. 2 H 7 2 4T RT A13NM 20080523 NM 2008 5 23 USAA920081027 1 20080413 A 5347 BAC15222193 SEAT TRACK BOEING 767 7672B7ER 1385107 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 MIA - MAJOR REPAIR - C4 CHECK - LEVEL 2 CORROSION ON CABIN SEAT TRACK, BS 764 - BS 820, RBL 86. REPLACED CABIN SEAT TRA CK, BS 764 - BS 820, RBL 86. 2 L 7 2 4F RT A1NM 20080523 NM 2008 5 23 USAA920081036 1 20080503 A 5340 66235743 STRINGER CLIP BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED STRINGER TIE CLIP, BS 727C, S8R. REPLACED STRINGER TIE CLIP, BS 727C, S8R IAW B 737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20080523 EU 2008 5 23 SB08033 1 20080509 A 3350 32145410 EPSU AIRBUS A319 A319112 3930323 EU ZONE 200 FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 725UW 16291 16291 1135 TPA - FWD EMERGENCY LIGHT POWER UNIT FAILED. MAINTENANCE REPLACED FWD POWER SUPPLY, OPS OK. 2 L 7 2 4F RT A28NM 20080523 NM 2008 5 23 USAA920081037 1 20080507 A 5311 FRAME BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED FRAME, BS 727B, S8L - S9L. REPAIRED FRAME, BS 727B, S8L - S9L IAW USAIRWAYS TYP ICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 20080523 SO 2008 5 23 FDKA200805194 1 20080506 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 837MJ 145367 THE RIGHT FORWARD FUSELAGE SKIN IS DENTED UNDER THE PITOT STATIC TUBE. THE DAMAGE HAS BEEN FILLED. 2 L 7 2 4T RT T00011AT 20080523 EA 2008 5 23 FDKA200805188 1 20080504 A 5210 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR UNKNOWN A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 600LR 15142 FDM FLT 6208 JFK-DCA. PASSENGER DOOR FREEFALLS TOO FAST WHEN OPENING. MX OPERATED DOOR SEVERAL TIMES AND DOOR OPS NORM AL. 2 L 7 2 4F RT A21EA 20080523 NM 2008 5 23 UPS08652231 1 20080507 A 3350 GUARD BOEING 767 76734AF 1385212 NM LIGHT SWITCH CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 304UP 27242 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT SWITCH GUARD IS CRACKED IN THE CENTER. REMOVED AND REPLACED SWITCH GUARD IAW A MM 33-51-08-4. 2 L 7 2 4F RT A1NM 20080527 NM 2008 5 27 ASAA0852935 1 20080510 A 3610 BELLOWS BOEING 737 737890 1384527 NM PRSOV LEAKING A ASAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 02 587AS 2137 35684 ON CLIMBOUT DUCT PRESS SPLIT WITH RT DUCT CYCLING APPROX 60 CYCLES PER MIN. 10 000 N1 91.6 LT DUCT 40 PSI N2 94.7 RT DUC T40 50 PSI. 18 000 N1 96.7 LT DUCT 42 DUCT N2 96.7 RT DUCT 42 45 PSI 39 000 N1 90.7 LT DUCT 40 PSI. N2 93.8 RT DUCT 40 P SI. CYCLING STOPPED APPROX FL230 ACCOMP LEAK CHECK OF BLEED AIR SYS FOUND BELLOWS OF PRSOV LEAKING AND B-NUTS FOR BLEED REG LOOSE. TIGHTENED BLEED REG B-NUTS AND REMOVED AND REPLACED PRSOV 401 406 STEP G STEP 4. NEEDS TO BE ACCOMP ROTABLE PART NUMBER VERIFIED THRU SEAMC M. JACK PRSOV INSTALLED TEST ACCOMP REF MM 36 1104 STEP H, NO LEAKS NOTED. ACCOMP ENG BLEED AIR OPS TEST OPS NORMAL. 2 L 7 2 4F RT A16WE 20080527 NE 2008 5 27 VNAA0805002 2 20080501 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 2 OVERTEMP A VNAA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 GL 05 241PS 7909 CREW REPORTED AT 125KTS, RECEIVED AN ITT INDICATION ON THE NR 2 ENGINE. CREW ELECTED TO ABORT THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE MDC AND FOUND THE OVERTEMP TO BE 902 FOR 3.2 SECONDS IN AREA A ON THE RIGHT HAND ENGINE. MAINTENANCE COMPLIED WITH THE REJECTED TAKEOFF INSPECTION. OPERATIONAL CHECKS WERE GOOD A ND NO DEFECTS NOTED AT THIS TIME IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080527 2008 5 27 SWAA082630 4 20080514 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 206WN 34011 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082638 1 20080514 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 847 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 ASAA0842953 1 20080501 A 5755 SKIN BOEING 737 7374Q8 138447Q NM NR 7 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 NR 7 SPOILER UPPER SURFACE HAS A PROTRUDING DENT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082688 1 20080517 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 821 S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 821, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082690 1 20080516 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727A S25L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082721 1 20080518 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 663 S2R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 2R CRACKED AT BS 663. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082703 1 20080516 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 784SW 29810 EEPLS LENS LOOSE AT ROW 9 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082746 1 20080520 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM BS 188 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 188, STR 17R. REPAIRED FRAME CHORD PER SRM. 2 L 7 2 4F RT A16WE 20080528 2008 5 28 SWAA082747 4 20080520 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080528 2008 5 28 SWAA082748 4 20080520 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082775 1 20080522 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM BS 188 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 188, STR 17R. REMOVED AND REPLACED CHORD PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082777 1 20080522 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 491WN 33867 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082704 1 20080517 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080528 2008 5 28 SWAA082781 4 20080522 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082780 1 20080522 A 5330 6545777 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERVICE DOOR CUTOUT UPPER HINGE CUTOUT. REPAIRED SKIN PE R SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082739 1 20080519 A 5310 6545874 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FWD SERVICE DOOR CUTOUT UPPER FWD CORNER STUB FRAME CRACKED AT UPPER STOP FITTING. R EMOVED AND REPLACED STUB FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082732 1 20080519 A 5315 6545810 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 312, LBL 13 TO RBL 13. REMOVED AND REPLACED CHORD PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082734 1 20080519 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 360 S14L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082729 1 20080519 A 5755 SKIN BOEING 737 7377H4 1384404 NM NR 6 SPOILER WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 710SW 27844 DURING SCHEDULED 10Y CHECK, FOUND LT WING NR 6 SPOILER LOWER SURFACE WORN. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 20080707 SO 2008 7 7 C2XA08ON124 1 20080519 A 2620 4800105 SWITCH EMB 145 EMB145XR 3260214 SO FIRE EXTINGUISH INOPERATIVE A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 27 17169 10397 10397 14500844 FLT 7653 - LAX - FLIGHT CREW REPORTED LAV FIRE EXTINGUISHER NO TEST. MX REMOVED AND REPLACED EXTINGUISHER FIRE SWITCH O PERATIONALLY CHECKED SATISFACTORY, AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 20080707 NM 2008 7 7 Q2SA758002 1 20080515 A 5420 65B9082842 ACCESS PANEL BOEING 747 747281F 13848AB NM NR 1 NACELLE CRACKED A Q2SA K NONE O OTHER IN INSP/MAINT 1 EA 63 758SA 23138 POST FLIGHT WALK-AROUND, FOUND HYDRAULIC ACCESS PANEL ON NR 1 ENGINE SAIL BOAT FAIRING OPEN. FOUND CRACK AT NR 1 ENGINE INBOARD SAIL BOAT DOOR, AT THE FORWARD HINGE. HYDRAULIC ACCESS PANEL OPENED IN FLIGHT. 2 L 7 4 4F RT A20WE 20080707 NM 2008 7 7 HNAA0800164 1 20080513 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A HNAA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 07 981HA 378 FIRST TWO RED EMERGENCY LIGHTS INOP FROM FLIGHT ATTENDANT PANEL, OKAY FROM COCKPIT. PLASTIC COVER OVER LIGHTS IS DAMAGE D. REPAIRED BROKEN WIRE AND RE-POSITIONED PLASTIC COVER, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 20080707 NM 2008 7 7 HNAA0800165 1 20080515 A 2120 UNKNOWN DHAV DHC8 DHC8102 2809003 NM CABIN ODOR A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 845EX 344 FLIGHT ATTENDANT REPORTED TO CREW STRONG BURNING SMELL IN CABIN. CREW POWER AIRCRAFT DOWN. AFTER INSPECTING A/C WITH A PU BLEED ON AND OFF, SMELL HAD GONE AWAY. MNT AND CREW SUSPECT APU EXHAUST HAD BLOWN INTO CABIN AREA. MNT INSPECTED AP U COMPARTMENT. NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 20080707 NM 2008 7 7 EMB08004 1 20080518 A 3243 14209114 CONTROL MODULE EMB ERJ190 ERJ190100IGW 3260408 NM BRAKE SYSTEM MALFUNCTIONED A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 954UW 115 19000139 PHL ORD-PHL FLT 856. DURING DESCENT TO PHL THE CAPTAIN DECLARED AN EMERGENCY WITH ATC, RECEIVED A FAULT MESSAGE ON EICA S THAT THE OUTBOARD BRAKES ARE COLD AND THE INBOARD BRAKES ARE AMBER. THE FLIGHT DID A GO-AROUND AND THE CAPTAIN AND FI RST OFFICER RAN THROUGH THE PROCEDURES IN THE HANDBOOK. THE FLIGHT THEN MADE THE APPROACH AND LANDED WITHOUT INCIDENT. THE BRAKES FUNCTIONED PROPERLY. MAINTENANCE REPLACED BRAKE CONTROL MODULE NR 2. CHECKS OK. 2 L 7 2 4F RT A57NM 20080707 EA 2008 7 7 HNAA0800167 1 20080514 A 3350 6013211X BATTERY DHAV DHC8 DHC8311 1386006 EA CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 329EN 16755 260 290 NR 3 AND NR 4 RED EMERGENCY LIGHTS INOP, ON CABIN AISLE FLOOR. REMOVED AND REPLACED BATTERY AT LOCATION PS5 AT CEILING IN CABIN. 2 H 7 2 4T RT A13NM 20080707 EA 2008 7 7 REXA200800013 1 20080507 A 5210 6003188715 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A REXA K NONE O OTHER IN INSP/MAINT 1 SO 25 8771A 12323 7771 PASSENGER DOOR INTERNAL HANDLE CRACKED AT ROLL PIN, FOUND DURING MAINTENANCE. REMOVED CRACKED PAX DOOR INNER HANDLE AND INSTALLED NEW HANDLE IAW CRJ 200 SRM 51-43-00. 2 L 7 2 4F RT A21EA 20080707 EU 2008 7 7 U2RA290LP024 1 20080519 A 2510 TRIM PANEL BAG JETSTM JETSTM3201 1500217 EU COCKPIT LOOSE A U2RA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 290MA 800 SMOKE IN THE F/O'S AREA OF THE FLIGHT DECK. FLT CREW PERFORMED QRH CHECKLIST IMMEDIATE ITEMS AND LANDED AIRCRAFT AT YIP . FOUND LOOSE VINYL FROM GLARE SHIELD ON FLOOD LIGHT. SECURED VINYL AND REPLACED BULB. OPS CHECKS GOOD IAW J/S3200 MM 33-10-00. 2 L 7 2 4T RT A56EU 20080707 NM 2008 7 7 2008UALA02841 1 20080517 A 2910 CONTROL UNIT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE HYDRAULIC SYS FAULTED A UALA K NONE M OVER TEMP IN INSP/MAINT 1 WP 29 799UA 26926 HYDRAULIC PUMP DEM C1 LOW CENTER HYDRAULIC DEMAND PUMP NR 1 PRESSURE WHEN COMMANDED ON, OR CENTER DEMAND PUMP NR 1 OVERH EATED. STATUS MSG-2910420 LATCHD DC MODE MSG-2910420 LATCHED DC MODE MSG-2910450 LATCHED AP MODE. FOUND LOGIC SPEED CONTROL UNIT FAULTY. REPLACED AIR DRIVEN LOGIC SPEED CONTROL UNIT PER 29-11-15. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080707 NE 2008 7 7 2008UALA02849 2 20080518 A 7532 BLEED VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT ENGINE MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 773UA 26929 BLEED OFF ENG L LEFT ENGINE BLEED VALVE CLOSED FOR SYSTEM FAULT OR SWITCH OFF, AND THE ENGINE IS NOT SHUTDOWN. ADVISORY MSG-3610500 LATCHED ER MODE MSG-3610500 LATCHED ER MODE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080707 EU 2008 7 7 2008UALA02860 1 20080518 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 494UA 1840 DENT IN FWD LOWER FUSELAGE JUST LEFT OF GROUND COMMUNICATION ACCESS DOOR FWD OF E/E DOOR. MAJOR REPAIR ACCOMPLISHED, IN STALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 20080707 EU 2008 7 7 2008UALA02861 1 20080518 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 494UA 1840 FOUND DENT ON BOTTOM OF FUSELAGE JUST FWD OF THE FRONT E-E DOOR. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 20080708 WP 2008 7 8 UPS08852296 1 20080422 A 5347 DC853B007002 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 SEAT TRACK WORN LBL 61 STA 930 MAIN CABIN. REPAIRED MAIN CABIN SEAT TRACK AT STA 930 AND LBL 61 IAW SRM 51-1-8 AND SRM 53-02-03-0 FIG 006D. 2 L 7 4 4F RT 4A25 20080708 CE 2008 7 8 N87SFGEAR 1 20080515 A 3260 65080755 PRINTED CKT BOAR CESSNA 500 550 2076604 CE COCKPIT FAULTY E SFOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 23 87SF 7139 5500402 AFTER TAKEOFF CREW WENT TO SELECT GEAR UP & NOTICED THAT THE GEAR DOWNLOCK LIGHTS WERE INOPERATIVE. CREW CYCLED GEAR WI TH NO AFFECT AND NOTED THE GEAR UNLOCK LIGHT ILLUMINATED AND EXTINGUISHED AS THOUGH A NORMAL CYCLE HAD BEEN COMPLETED. GEAR ALSO FELT NORMAL DURING THE RETRACT/EXTEND CYCLE. CREW PERFORMED A LIGHT TEST AND LIGHTS STILL WOULD NOT ILLUMINAT E. AFTER A FLY BY CONFIRMING GEAR APPEARED TO BE FULLY DOWN, AND A REVIEW OF THE GEAR SCHEMATIC DIAGRAMS, IT WAS DETERM INED THAT ONLY AN INDICATION FAULT WAS OCCURRING AND A SAFE LANDING COULD BE MADE. THE EMERGENCY GEAR SYSTEM WAS ACTUAT ED AND A SAFE LANDING WAS MADE AT DEPARTURE AIRPORT. TROUBLESHOOTING REVEALED A FAULT IN THE LIGHT DIMMING CIRCUITRY (C 1 L 7 2 4F A22CE 20080708 NM 2008 7 8 08FDEA01939 1 20080521 A 5320 652454863 PAN BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 AFT MAIN DECK FLOOR DITCHING PAN ASSY IS CRACKED WITH INTERIM COMPOSITE REPAIR BS 1176-1183, RBL 37-47 WL 208 (MKD). FA BRICATED NEW DITCHING PAN, HEAT TREATED, ALODINED AND PRIMED, INSTALLED IAW SRM 51-10-2, PG 1, 51-30-2, PG 1, 51-30-5 PG 1. BOEING DWD: 65-29548. HEAT TREATED, TRACKING NR: 2008-05-068. THIS IS CLASSIFIED AS A MINOR REPAIR. REF: GMM 6-2-100 PG 2 AND 3. 2 L 7 3 4F RT A3WE 20080528 NM 2008 5 28 SWAA082715 1 20080515 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING DUCT CUTOUT AFT END. REPAIRED SKIN PER SRM . 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082756 1 20080521 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 1140 22942 DURING SCHEDULED SPV CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP P ER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082757 1 20080521 A 5330 65C337568 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082758 1 20080521 A 3397 W0130000120 WIRE BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 448WN 33721 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT LT MID CABIN. FOUND LOOSE WIRE AT LIGHT ASSY. SECURED WIRE PER WDM. 2 L 7 2 4F RT A16WE 20080528 WP 2008 5 28 IXXA08SMN091S 1 20080313 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT FUSELAGE SKIN FORWARD OF FLAT AFT PRESSURE BULKHEAD AT LONGE RON 28. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLERS. REMOVED DAMAGED AREA. PERFO RMED NDT INSPECTION. NO CRACK AND CORROSION FOUND. FABRICATED EXTERNAL REPAIR DOUBLERS, FILLERS, FINGER DOUBLERS. CLE ANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW S/B 53A-080 DATED 06-22-04 , AD 2007-02-02, ASB DC8-53-080 DATED JUNE 22 2004, FAA FORM 8100-9 DATED 04-02-08, DOUGLAS DRAWING SR08530032, BOEING MESSAGE 1-791406133-7 DATED 04-02-08, SEMAN DRAWING ED-4734 DATED 04-22-08, DC8 SRM 51-1-21, 51-3-0, 51-1-20D, DC8 NDT 2 L 7 4 4F RT 4A25 20080528 WP 2008 5 28 IXXA08SMN096S 1 20080314 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1150 L21R MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND DOUBLER REPAIR RIGHT AFT FUSELAGE ABOVE AND FWD OF C-PIT DOOR RIVET SPACING EXC EEDED AT FS 1150 LONGERON 21.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXITING REPAIR. PERFORME D NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER. CLEANED, TREATED AND PRIME D AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8100-9 DATED 04-25-08, AD 2005-18-07, S/ B DC8 53-078, DRAWING DOUGLAS NUMBER SR08530019, 5750776, BOEING MESSAGE 1-792473913-9 DATED 04/25/08, BOEING SKETCH 1-7 92473913, SEMAN DRAWING ED-4736, DC8 SRM 51-1-21, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 53-2-0 FIGURE 22, DC8 SRM 51-1- 2 L 7 4 4F RT 4A25 20080528 NM 2008 5 28 NWAA082185514 1 20080512 A 5730 PANEL BOEING 757 757251 1384970 NM RT WING INFLT SEPARATION A NWAA A UNSCHED LANDING D K J INFLIGHT SEPARATION FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 514US 23202 CLIMBING THROUGH FL 230 PANEL 651, ON THE UPPER SURFACE OF THE RIGHT WING ABOVE THE RIGHT LANDING GEAR RETRACT CYLINDER, DEPARTED FROM THE AIRCRAFT. WHEN THE PANEL DEPARTED THE AIRCRAFT IT TORE TWO HYDRAULIC LINES FOR THE RETRACT CYLINDER AND DRAINED THE LEFT HYDRAULIC SYSTEM. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED TO LAS. ALTERNATE LANDING GEA R AND FLAP EXTENSION WAS USED, THE LANDING WAS OTHERWISE UNEVENTFUL. AT THE TIME OF THIS WRITING, TECHNICIANS ARE ON SI TE REPLACING THE DAMAGED LINE FOR THE RETRACT CYLINDER ALONG WITH THE ASSOCIATED SYSTEM PUMPS AND FILTERS. THIS WILL BE UPDATED WITH THE FINAL CORRECTIVE ACTION ONCE THE LOG PAGE HAS BEEN CLOSED. 2 L 7 2 4F RT A2NM 20080528 WP 2008 5 28 IXXA08SMN174S 1 20080419 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT HAND INBOARD FLAP UPPER SKIN HAS DENTS BETWEEN STATION XW 104.000 TO STATI ON XW 115.000.REMOVED FASTNERS AS NEEDED TO PERFORM REPAIR.REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, AND BONDED DOUBLE R. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTNERS AND REPA IR PARTS IAW DC8 SRM 57-7-1 FIGURE 1 ITEM "A" AND "L", DC8 SRM 57-1-0 PAGE 1, 51-1-21, DC8 SRM 51-1-9 TR NUMBER 51-142 , 51-1-9A TR NUMBER 51-141, DC8 SRM 51-1-8B, AND DC8 SRM 51-1-11. 2 L 7 4 4F RT 4A25 20080528 EA 2008 5 28 CHQA200800095 1 20080515 A 2751 855D1009 POSITION SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS DEFECTIVE A CHQA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 454 181 147 7313 GEE872507 FLIGHT 5569 IAH TO LBB - WHILE ON A VISUAL APPROACH INTO LBB THE CREW RECEIVED A FLAPS FAIL CAUTION MSG ON THE EICAS. T HE CREW RAN THEIR QRH, RAN APPROPRIATE CHECK LISTS, DECLARED AN EMERGENCY WITH LBB TOWER AND LANDED WITH OUT INCIDENT. REMOVED AND REPLACED THE LT BPSU IAW 27-51-10-400-801. 2 L 7 2 4F 4 F RT A21EA E15NE 20080528 NM 2008 5 28 KNNA200816 1 20080515 A 5347 SEAT TRACK BOEING 737 7372L9 1384497 NM BS 927-947 CORRODED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 464AT 21278 REMOVED GALLEY AND FOUND THAT THE SEAT TRACK HAD EXFOLIATION CORROSION ON THE UPPER SURFACE AT STA 938 TO 947.5. RBL 24. 5. REMOVED AND REPLACED SEAT TRACK FROM STA 927 TO STA 947, RBL 24.5. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 UIEA200800212 1 20080518 A 5311 FRAME BOEING 747 7472D7B 1384803 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK STA 1740 STRINGER 13R - 14R FRAME FOUND CRACKED. FRAME CRACKED AREA REPAIRED PER EO NR 4753B152. 2 L 7 4 4F RT A20WE 20080528 NM 2008 5 28 NWAA082146310 1 20080516 A 3350 CHARGER BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING OVERNIGHT CHECK, FOUND EMERGENCY PATH LIGHT AT ZONE D INOP. MAINTENANCE REMOVED AND REPLACED BATTERY CHARGER. O PERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20080528 EA 2008 5 28 CHQA200800094 1 20080514 A 2751 855D1009 POSITION SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS FAULTED A CHQA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 11 639BR 159 124 7313 GEE872507 FLIGHT 5569, IAH TO LBB. ON APPROACH, THE FLAP HANDLE WAS SELECTED TO 8 DEGREES AND THE CREW RECEIVED A FLAP FAIL MESSA GE ON EICAS WITH NO FLAP MOVEMENT. THE FLIGHT CREW ABORTED THE APPROACH TO RUN THROUGH THE APPROPRIATE QRH CHECKLISTS. AFTER RUNNING THROUGH THE PROPER CHECK LISTS, THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAULT ACCORDING TO THE APPROPRIATE FIM TASKS AND RECORDED THE FECU FAULT LOG CONTENTS AND APPLICABLE INFORMATION. THE FLAP SY STEM WAS RESET PER THE FIM AND THE FLAP SYSTEM OPERATED NORMALLY. ENGINEERING RELEASED DOCUMENTATION TO TROUBLESHOOT THE LEFT HAND BRAKE POSITION SENSING UNIT DUE TO STORED CODES IN THE FECU AT THE NEXT MAINTENANCE VISIT. 2 L 7 2 4F 4 F RT A21EA E15NE 20080528 WP 2008 5 28 IXXA08SMN092S 1 20080313 A 5730 SB085700863 SKIN DOUG DC8 DC873F 302199F WP ZONE 500 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT LEFT WING UPPER AFT SKIN PANEL. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-1-11, 51 -1-20D, 51-3-1, AD 90-16-05, DC8 S/B 57-86, DOUGLAS DRAWING J060104, SERVICE SKETCH NUMBER 3313, BOEING MESSAGE 1-780888 417-2 DATED 03-03-08, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 20080528 WP 2008 5 28 IXXA08SMN162S 1 20080419 A 5340 FITTING DOUG DC8 DC871F 302199D WP BS 960 L19R CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT UPPER SURFACE OF CUSP EXTRUSION FT FITTING WITH CRACK AT STATION 960.000 LONGERON 19 RIGHT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSIO N FOUND. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-3-1 DC8 SRM 51-1-20D, DPS 4.707, DC8 SRM 51-1-8B, ATI REPAIR SPECIFICATION NUMBER 2003-05, AND DOUGLAS DRAWING 3779874. 2 L 7 4 4F RT 4A25 20080528 WP 2008 5 28 IXXA08SMN163S 1 20080419 A 5340 FITTING DOUG DC8 DC871F 302199D WP BS 798 L20R CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT CUSP EXTRUSION UPPER SURFACE AFT FITTING WITH CRACK AT STATION 798.000 LO NGERON 20 RIGHT. REMOVED AFT CRACKED FITTING. FABRICATED FITIING. PERFORMED NDT INSPECTION. CLEANED TREATED AND PRIM ED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-3-1, SRM 51-1-20D, DACO DPS 4.707, DC8 SRM 51-1-8B, ATI REPAI R SPECIFICATION NUMBER 2003-05, AND DOUGLAS DRAWING 3779874. 2 L 7 4 4F RT 4A25 20080528 NE 2008 5 28 NSVA2008028 2 20080519 A 7200 CT79B ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT FAILED A NSVA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 27 352CJ 340B352 785518 LEFT ENGINE FAILED AFTER TAKEOFF, AT APPROX 300 FT, ITT WAS NOTED AT 1030 DEG. ENGINE LIGHT ON, BLEED VALVES WERE OPEN C TOT POWER WAS SET AT 90 PERCENT CONDITIONS AT CLL CALM 10S - 1 7/15, 29.83, PAC AND FA NOTED FIREBALL AND LOUD BANG IMME DIATELY PRECEDING ENGINE PROBLEM. FDR CONFIRMED OVERTEMP EVENT, ENGINE CHANGE REQUIRED. 2 L 7 2 4T 4 T RT A52EU E8NE 20080528 WP 2008 5 28 IXXA08SMN169S 1 20080419 A 5340 FITTING DOUG DC8 DC871F 302199D WP BS 781 L18L CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION; FOUND LEFT HAND CUSP EXTRUSION UPPER SURFACE FORWARD FITTING CRACKED AT STATION 781.5 00 LONGERON 18LEFT.REMOVED CRACKED FITTING.FABRICATED FITTING.PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND.CLE ANED TREATED AND PRIMED FITTING AND AREA.INSTALLED NEW FITTING IAW DC8 SRM 51-3-1, DC8 SRM 51-1-20D, DACO DPS 4.707, DC8 SRM 51-1-8B, ATI REPAIR SPECIFICATION NUMBER 2003-05, AND DOUGLAS DRAWING 3779978. 2 L 7 4 4F RT 4A25 20080528 NM 2008 5 28 08FDEA01863 1 20080516 A 5330 655457235 SKIN BOEING 727 727233 138408A NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 274FE 22039 DENT RT FUSELAGE STA 540 STR 24R (RVSM AREA). REPAIRED DENT IAW EA 7-5330-116983. 2 L 7 3 4F RT A3WE 20080528 NM 2008 5 28 08FDEA01885 1 20080520 A 5330 AJC70602 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 AFT FUSELAGE RT SKIN, LOWER MOUNTING AREA OF FIXED FAIRING (347DF) FOUND EXFOLIATION CORROSION. REPAIRED AS PER SRM 53-20-00 FIGURE 13 VOLUME I. CLASSIFIED AS MINOR REPAIR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080528 NM 2008 5 28 08FDEA01887 1 20080520 A 5753 ARC27362 SKIN DOUG MD11 MD11F 3023600 NM RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 RT WING INBD FLAP LOWER SURFACE FOUND WITH 2 DENT MARKS. 2 L 7 3 4F RT A22WE 20080529 EU 2008 5 29 08FDEA01872 1 20080517 A 5315 A53781966200 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 MAIN CABIN FLOORBEAM AT FR 32 HAS .250 IN CRACK BETWEEN SEAT TRACKS NR 4 LT AND NR 5 LT REMOVED CRACK AND INSTALLED FLOO RBEAM REPAIR ON FLOORBEAM FR 32, BETWEEN SEAT TRACKS NR 4 LT AND NR 5 LT IAW A300-600 SRM 53-10-15, FIG 212. 2 L 7 2 4F RT A35EU 20080529 EU 2008 5 29 08FDEA01873 1 20080517 A 7830 1477M42P01 STIFFENER AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 NR 2 ENGINE INBD THRUST REVERSER UPPER FWD SPAR HAS 1.5 IN CRACK AT FASTENER REPAIRED CRACK ON NR 2 ENG INBD T/R UPPER F WD SPAR IAW FEDEX EA 6-7830-121260, RELEASE DATE 30 APRIL,2008. 2 L 7 2 4F RT A35EU 20080529 NM 2008 5 29 08FDEA01902 1 20080520 A 5320 6944884 ANGLE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 AFT PIT BILGE BODY FRAME INTERCOSTAL UPPER CHORD IS CORRODED BS 1050 - 1070 STR 27L OB, WL 149. REMOVED ATTACHED UPPER CHORD ANGLE. FABRICATED NEW ANGLE REF DWG 69-44884 PG 1. TREATED AND PRIMED UPPER CHORD ANGLE. INSTALLED REF SRM 51-30 -20 PG 1-10. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01905 1 20080520 A 5313 BAC1498143 STRINGER BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 CORROSION ON I/B SIDE OF STR 28L AT FS 661, LBL6, WL 149 REPAIRED STRINGER AT 292 AT FS 661 LBL 6, WL 149. REF SRM 53- 10-3, PG 3 -4, FIG 1, DETAIL 1, THIS IS CLASSIFIED AS MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080522 CE 2008 5 22 DXTA200803052 1 20080510 A 3233 99124913 ACTUATOR CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE MLG FALSE INDICATION E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 640QS 5409 5605240 LANDING GEAR GREEN (NO) NOSE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. REPLACED NOSE GEAR ACTUATOR WITH NEW IAW MM 32-30-03. OPERATION & LEAK CHECK NORMAL. 2 L 7 2 4F 4 F RT A22CE E00059EN 20080522 NM 2008 5 22 DU4R2008201 1 20080502 A 5315 FLOORBEAM BOEING 737 737448 13844BU NM CFMINT CFM56 CFM563B2 13802 EU BS 328 CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 742VA 24773 S/O 312001 N/R 24738 - CORROSION ON UPPER SURFACE OF FLOOR SUPPORT BEAM BS 328 RBL 16 - RBL 60. 2 L 7 2 4F 4 F RT A16WE E21EU 20080522 WP 2008 5 22 RRXA001532 1 20080121 A 5311 DOUGLAS FRAME DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE FS 1340 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 994CF 45956 DURING A MAINT VISIT, FOUND MISDRILLED HOLES IN THE UPPER CARGO COMPT. FS 1340 AND L21R TO L21L, DAMAGE EXCEEDED LIMITAT IONS IAW SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW SRM 51-1-8. PLUGGED HOLES, FABRICATED DOUBLERS FROM 7075-T6 AND INSTALLED IAW EO NR 99-236 WITH APPROVED 8110-3, DATED 12-06-99. 2 L 7 4 4F 4 F 4A25 1E8 20080522 WP 2008 5 22 BKE2008F00001 2 20080317 A 7200 ENGINE RAYTHN DH125 HAWKER800 7450004 CE GARRTT TFE731 TFE731* 01518 WP LEFT MALFUNCTIONED E BKEA B A EMER. DESCENT UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 WP 01 752CS 4047 258323 P107179 ON SATURDAY, MARCH 15, 2008, AT FL 39,000 FT, THE PILOT NOTICED SMOKE COMING INTO CABIN. THE PILOT DECLARED AN EMERGENC Y AND STARTED DESCENT. DURING DESCENT PILOT NOTICED THAT THE LT ENGINE`S FUEL COMPUTER ANNUNCIATOR LIGHT CAME "ON", THE POWER LEVER WAS RETARDED TO MAINTAIN PROPER EGT ON THAT LT ENGINE. COPILOT NOTICED THE LT ENGINE`S OIL PRESSURE ANNUNC IATOR LIGHT CAME ON AND THEN NOTICED THE LT ENGINE`S OIL PRESSURE DROPPING VERY QUICKLY; AT THIS POINT THE PILOT PROCEED ED TO SHUTDOWN THAT LT ENGINE. SHORTLY AFTER ENGINE SHUTDOWN THE LT ENGINE SMOKE CEASED AND THE CABIN CLEARED. THE PIL OTS COMPLETED EMERGENCY PROCEDURES AND KEPT DESCENDING AND GETTING VECTORED TO AIRPORT WHERE THE AC FINALLY LANDED WITHO 2 L 7 2 4F 4 F RT A3EU E6WE 20080523 SO 2008 5 23 FDKA200805191 1 20080505 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO GALLEY INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 854MJ 145490 FDM FLT 6166 JFK-PHL. GALLEY WALL EXIT LOCATOR LIGHT INOP. MX RESET, OPS GOOD. 2 L 7 2 4T RT T00011AT 20080708 NM 2008 7 8 2008UALA02882 1 20080519 A 5753 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT WING TE FLAP DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 RT WING INBD FLAP T/E IS DENTED. REPAIRED IAW GN-6-0-2-19. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080708 NM 2008 7 8 2008UALA02889 1 20080519 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 SEAT 51 ABC EMERGENCY LIGHT IS INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 2008UALA02896 1 20080519 A 5512 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HORIZ STAB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 213UA 30219 LIGHTNING STRIKES LT HORIZ STAB UPPER SURFACE, INBOARD END. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080708 NM 2008 7 8 2008UALA02911 1 20080520 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY EXIT LIGHT INOP AT ROW 42 RIGHT CEILING. RELAMPED EMERGENCY LIGHT, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 2008UALA02913 1 20080520 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 5E FWD LIGHT ASSY. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 2008UALA02919 1 20080520 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY EXIT EEL LIGHT INOP AT ROW 56 LEFT. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 SO 2008 7 8 C2AO8SH079 1 20080522 A 5320 14525480603 BEAM EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 SHV - DURING C-CHECK CARGO DOOR LOWER BEAM HAS CORROSION. MX REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER BEAM IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 20080708 NM 2008 7 8 MWEA080073 1 20080520 A 5230 591014193 SKIN DOUG MD88 MD88 3023688 NM FWD CARGO DOOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 823ME 49766 FORWARD CARGO DOOR OUTER SKIN HAS SEVERAL DENTS. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 20080708 NM 2008 7 8 ASAA0852974 1 20080520 A 4990 38809381 OIL FILTER BOEING 737 737890 1384527 NM APU DIRTY A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 558AS P7229 35177 APU OIL FILTER DELTA P INDICATOR EXTENDED REQUIRES MAINT REF: T C 78349013. REPLACED APU OIL FILTER AND RESET DELTA P INDICATOR, OPERATED APU FOR 30 MIN AND RE-CHECKED DELTA P INDICATOR. INDICATOR REMAINS RESET AMM 49 91 13 & 49 91 12. 2 L 7 2 4F RT A16WE 20080603 CE 2008 6 3 GUUA05190802 1 20080519 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 190YV 23110 UE190 DURING SCHEDULED ROUTINE MAINT, DISCOVERED RT OB ELEVATOR HINGE BRACKET HAS CORROSION. REPLACED RT OB ELEVATOR HINGE BR ACKET. 2 L 7 2 4T 4 T RT A24CE E26NE 20080603 CE 2008 6 3 DXTA200803075 1 20080521 A 3260 387 BULB CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C 03047 GL MLG INDICATOR INTERMITTENT E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 916QS 7500116 ON FINAL LT MLG DOWN INDICATOR LIGHT DID NOT ILLUMINATE. REMOVED INTERMITTENT LT MLG DOWNLOCK. INDICATOR BULBS & INSTAL LED NEW BULBS IAW MM 32-60-00. OPERATED NORMAL NO DEFECTS. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080603 NM 2008 6 3 CALA0800450 1 20080511 A 5340 6546596 BRACKET BOEING 737 737524 1384721 NM BS 727B CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 LT SIDE BS 727B INBOARD ATTACH FASTENER HOLE ON AIR-CONDITIONING (A/C) BRACKET CRACKED. REPAIRED CRACKED FRAME ATTACH F ASTENER HOLE AT LT SIDE BS 727B PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080603 SO 2008 6 3 SWIA200819692 1 20080521 A 2611 SMOKE DETECTOR EMB 120 EMB120ER 3260203 SO CARGO BAY NO TEST A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 581SW 120349 THE NR 2 CARGO SMOKE DETECTOR WILL NOT TEST. REPLACED NR 2 CARGO SMOKE DETECTOR. SYSTEM TESTS GOOD, P/N 473597-13, S/N OFF 1500. 2 L 7 2 4T RT A31SO 20080603 CE 2008 6 3 DXTA200803082 1 20080528 A 3210 BOLT CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C 03047 GL MLG LINK MISSING E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 903QS 7500162 GEAR UNLOCK LIGHT REMAINED ON AFTER GEAR RETRACTION. FOUND RT MLG TRAILING LINK THROUGH BOLT MISSING. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080603 SO 2008 6 3 SWIA200819697 1 20080406 A 2497 WIRE EMB 120 EMB120ER 3260203 SO BUSS BAR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 561SW 120335 WIRE TERMINAL CONNECTED TO BUSS BAR IN RIGHT AFT CONSOLE IS CORRODED, FOUND AT C-CHECK. REPLACED TERMINAL ON WIRE. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 20080523 WP 2008 5 23 UPS08852195 1 20080423 A 5310 3755856501 BELTFRAME DOUG DC8 DC873F 302199F WP BS 1140 L21R GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 BELTFRAME END FITTING GOUGED IN MAIN CABIN STA 1140 AND L21R. FABRICATED AND REPLACED BELTFRAME END FITTING AT STA 1140 AND L21R IAW DWG 3755856, SRM 51-03-02-0, SRM 51-01-08 AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 20080523 NM 2008 5 23 SB08034 1 20080510 A 4990 OIL SYSTEM AIRBUS A319 A319132 3930340 NM APU LOW A USAA O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 829AW 1563 DCA FLT 44 EN ROUTE DCA-PHX. APU AUTO SHUTDOWN WITH NR 1 GENERATOR BECOMING INOP EN ROUTE. MAINTENANCE SERVICED APU OI L TO CORRECT LEVEL AND RESET NR 1 GENERATOR CIRCUIT BREAKER. OPS CHECKS OK. 2 L 7 2 4F RT A28NM 20080523 SO 2008 5 23 FDKA200805199 1 20080512 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 839MJ 145416 FDM RON IAD. GALLEY EMERGENCY EXIT LIGHTS INOP. MX SECURED ELECTRICAL CONNECTOR ON EMERGENCY LIGHT STRIP, OPS CHECK GO OD. 2 L 7 2 4T RT T00011AT 20080523 WP 2008 5 23 UPS08852184 1 20080421 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LEFT WING CENTER L/E UPPER RIB CRACKED AT XFS 398. REPAIRED LEFT WING CENTER L/E UPPER RIB AT XFS 39 8 IAW SRM 57-02-00-0 FIG 002 AND SRM 57-03-03-0 FIG 005. 2 L 7 4 4F RT 4A25 20080527 NE 2008 5 27 ASAA0852933 2 20080511 A 7261 CFM567B27 ENGINE BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE NR 2 OIL CONSUMPTION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 587AS 2148 35684 895978 NR 2 ENGINE OIL CONSUMPTION AT .62 PER SEAMC. AIRCRAFT RESTRICTED FROM ETOPS SERVICE UNTIL EXCESSIVE OIL CONSUMPTION IS CORRECTED. PER SEAMC AFTER LAST OIL ADD LP 6415958 NR 2 ENG OIL CONSUMPTION IS NOW .12 AC IS NOW ETOPS QUALIFIED. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080527 WP 2008 5 27 UPS08852216 1 20080424 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP BS 1680 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 MAIN CABIN AT STA 1680 AFT FLOORBOARD F213 HAT CHANNEL IS DAMAGED AT EDGE. FABRICATED AND REPLACED H AT CHANNEL ON FLOORBOARD F213 IAW SRM 51-02-0 FIG 52 AND 53-02-00 FIG 002. 2 L 7 4 4F RT 4A25 20080527 EA 2008 5 27 VNAA0804020 1 20080427 A 4997 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE APU LOW A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 05 254PS 7935 CREW REPORTED AN APU OIL CAUTION MESSAGE IN FLIGHT. CREW ELECTED TO DIVERT TO BNA AND LANDED WITHOUT INCIDENT. MAINTEN ANCE INSPECTED AND VISUALLY CHECKED THE APU OIL LEVEL AND APU OIL SYSTEM IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MAN UAL. OIL LEVEL CHECKED GOOD, NO VISUAL DEFECTS NOTED AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080527 EA 2008 5 27 VNAA0805003 1 20080501 A 5200 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE COMMS OPEN A VNAA A UNSCHED LANDING W E INADEQUATE Q C VIBRATION/BUFFET CL CLIMB 1 GL 05 725PS 10186 CREW REPORTED AFTER TAKEOFF A LOUD WHINING NOISE COMING FROM THE NOSE OF THE AIRCRAFT. CREW ELECTED TO RETURN TO CLT AN D LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE EXTERNAL COMM DOOR OPEN. MAINTENANCE SECURED THE DOOR C LOSED. NO DEFECTS OR DAMAGE NOTED AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080527 NM 2008 5 27 USAA920081062 1 20080508 A 5311 143N8313U38 FRAME BOEING 757 757225 1384959 NM BS 690 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924UW 22204 PIT - MAJOR REPAIR - C2 CHECK - R2 DOOR CUTOUT FRAME WEB CRACKED, BS 690.40 UNDER THE NR 1 STOP. REPAIRED THE R2 DOOR C UTOUT FRAME WEB CRACKED, BS 690.40 UNDER THE NR 1 STOP IAW USAIRWAYS EA 97407A. 2 L 7 2 4F RT A2NM 20080527 EU 2008 5 27 USAA920081063 1 20080508 A 5320 D534721722000 FLOOR SUPPORT AIRBUS 320 A320214 3930316 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 105UW 868 PIT - MAJOR REPAIR - C11 CHECK - CORROSION ON FLOORBEAM, BS 2835 / FR 67 - BS 2884 / FR 68, +Y1160. REPLACED FLOORBEAM, BS 2835 / FR 67 - BS 2884 / FR 68, +Y1160 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20080527 NM 2008 5 27 ASAA0842942 1 20080429 A 5753 FAIRING BOEING 737 7374Q8 138447Q NM LT FLAP TRACK CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 LEFT O/B MID FLAP CHAFED ON LOWER SURFACE O/B OF NR 2 FLAP TRACK. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10, REPAIR GENERAL. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082662 1 20080515 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 468WN 33858 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082655 1 20080515 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 787 S22R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082705 1 20080515 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 930 S23-24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 930, BETWEEN STR 24L AND STR 23L. REPAIRED SKIN PER SWA E A. 2 L 7 2 4F RT A16WE 20080527 2008 5 27 SWAA082695 4 20080517 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 425LV 29829 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082774 1 20080522 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM BS 907 S6R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 6R. REMOVED AND REPLACED STRINGER SPLICE PER S RM. 2 L 7 2 4F RT A16WE 20080528 SO 2008 5 28 RAIA00805006 1 20080504 A 3297 PIN EMB 145 EMB145LR 3260212 SO RELAY LOOSE A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 838HK 145321 FLT 7887 - ROC - LANDING GEAR AIR/GROUND FAILURE ON THE EICAS. MAINTENANCE INSPECTED THE SYSTEM AND FOUND PIN X1 ON REL AY K1202 RECESSED. THE PIN WAS RESET AND THE SYSTEM CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080528 NM 2008 5 28 SWAA082767 1 20080521 A 3397 W2114001320 WIRE BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED 10Y CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. FOUND LOOSE WIRE AT TB505YA1. SECURED WIRE PER WDM. 2 L 7 2 4F RT A16WE 20080528 SO 2008 5 28 RAIA00805005 1 20080504 A 3240 38793500 SHUTOFF VALVE EMB 145 EMB145LR 3260212 SO BRAKE ASSY INOPERATIVE A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 811HK 145256 FLT 5503 - JAX - ABORTED TAKEOFF DUE TO INBOARD BRAKE INOPERATIVE MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACE D THE BRAKE SHUTOFF VALVE. 2 L 7 2 4T RT T00011AT 20080528 NM 2008 5 28 SWAA082735 1 20080519 A 5315 6545833 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 188 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 188, RBL 10. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080528 2008 5 28 SIMA200813701 4 20080514 A 3425 6226190113 AHRS SAAB SF340 340B 7860101 EU NR 1 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 232AE 20720 340B232 ON FLIGHT 3347 CREW REPORTED AFTER TAKEOFF BOTH TUBES EADI, EHSI BLANKED OUT SEVERAL TIMES, PITCH AND ROLL AMBER INDICA TIONS, ADI SHOWED +40 DEGREES NOSE UP AND 5 DEGREE ROLL TO THE LEFT. CREW RETURNED TO THE FIELD AND TAXI SAFELY TO THE GATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 AHRS. OPERATIONAL CHECK GOOD AT THIS TIME WHILE ON GRO UND PER SAAB AMM 34-21-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 20080528 WP 2008 5 28 IXXA08SMN160S 1 20080418 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 CRACKED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XRS 74.000, STRINGER 7. REMOVED FASTE NERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABR ICATED NEW SKIN, AND FILLER. TAPERED BOTH SIDE OF DOUBLER. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. INSTAL LED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08188 DATED 04-23-08, SEMAN DRAWING NUMBER ED-4769 DATE 04 -22-08, DC8 SRM 51-1-20D, 51-3-0, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-10-0, FIGURE 1 PAGE 20, DC8 SRM 51-1-12, DC8 SRM 51-1-11, 51-1-21, AND 51-3-1. 2 L 7 4 4F RT 4A25 20080528 NM 2008 5 28 NWAA082245505 1 20080517 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS NO TEST A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 505US 23194 DURING EMERGENCY LIGHT BATTERY PACK CHECK, BATTERY PACK M737 FAILED THE CHECK OUT. MAINTENANCE REPLACED BATTERY PACK M7 37, OPERATION CHECKED GOOD. 2 L 7 2 4F RT A2NM 20080528 NM 2008 5 28 NWAA082346308 1 20080524 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHTS DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 668US 24223 DURING LINE CHECK, FOUND RT UPPER DECK DOOR BATTERY INOPERATIVE. LINE MAINTENANCE TESTED AND FOUND BATTERY DISCHARGED. REPLACED BATTERY PACK PER AMM 52-23-14 AND TESTED OK. AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20080528 EU 2008 5 28 NSVA2008030 1 20080520 A 2613 SEAL SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE TAILPIPE SENSOR LEAKING A NSVA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 350CJ 340B350 785169 AIR RETURN FOR RT TAILPIPE HOT ON CLIMB-OUT FROM LGA. EMERGENCY DECLARED, LIGHT WENT OUT ON IT'S OWN SHORTLY AFTER. WE ATHER ON THE GROUND WAS HEAVY RAIN PRIOR TO DEPARTURE. CW WORKCARD FOR TAILPIPE SENSOR SEALING. ONCE DONE, OPS CHECKED GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 20080528 SO 2008 5 28 CHQA200800097 1 20080519 A 2720 3603001001 ACTUATOR EMB 145 EMB145 3260210 SO ALLSN AE300 AE3007A GL RUDDER INOPERATIVE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 261SK 20190 20190 145144 CAE312650 FLIGHT 5914 CLE TO GRB, SHORTLY AFTER TAKEOFF THE CREW RECEIVED A RUDDER OVERBOOST MESSAGE ON THEIR EICAS. THE CREW THE N RAN THEIR QRH AND DECIDED TO RETURN TO FIELD AND LANDED WITH OUT INCIDENT. MAINTENANCE ARRIVED AND FOUND THE RUDDER P OWER CONTROL UNIT INOPERATIVE. MAINTENANCE REPLACED THE RUDDER PCU IAW EMB-145 MM 27-22-03 AS WELL AS CONDUCTED A FUNCT IONAL CHECK OF THE RUDDER SYSTEM WITH NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080528 EU 2008 5 28 NSVA2008027 1 20080518 A 2435 23080031 STARTER GEN SAAB SF340 340B 7860101 EU RIGHT SMOKE A NSVA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 184CJ 340B184 STARTED RT ENGINE, PILOT SAW SMOKE, SHUTDOWN ENGINE. PILOT EXTINGUISHED RT ENGINE FIRE BOTTLE. REMOVED AND REPLACED RT ENG DC GEN IAW AMM 24-31-05. 2 L 7 2 4T RT A52EU 20080528 NM 2008 5 28 08FDEA01886 1 20080520 A 5753 ARC24441 SKIN DOUG MD11 MD11F 3023600 NM LT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 LT WING INBD FLAP UNDER SURFACE FOUND WITH MULTIPLE DENT MARKS. DENT AREA MEASURED AND FOUND WITHIN LIMIT AS PER SRM 57- 10-00 FIGURE 17 VOLUME I AT LEFT HAND WING INBOARD FLAP UNDER SURFACE AT XIFH 249. HFEC INSPECTION CARRIED OUT AS PER DAC NDT SPM REVISION 13 PART 6 06-10-01.001 ON DENTED AREA AND FOUND NO CRACK EVIDENT. REPAIR CLASSIFIED AS MI NOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 WP 2008 5 29 08FDEA01897 1 20080520 A 5542 NMC6017519 SKIN DOUG DC10 DC1010 3022110 WP RUDDER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 40061 46973 VERTICAL STABILIZER, RUDDER CRACK AND SUSPECT INTERNAL CORROSION ON SKIN UPPER FWD RUDDER. REPAIRED AREA IAW SRM 55-1 0-00 FIG 3 VOL I. 2 L 7 3 4F A22WE 20080529 NM 2008 5 29 08FDEA01906 1 20080520 A 5320 STRUCTURE BOEING 727 727233 138408A NM LAVATORY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 FWD LAV SINK CABINET WASTE DISPOSAL FIBERGLASS SHOOT IS CRACKED. REPAIRED LAV SINK CABINET WASTE DISPOSAL CHUTE REF SRM 51-40-9 PAR 7, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 EU 2008 5 29 08FDEA01914 1 20080520 A 5321 A532B38300200 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 815FD 638 THERE IS A BROKEN FLOOR PANEL FOR THE MAIN CARGO DECK AT FRAME 65 TO FRAME 66, LBL-57 TO LBL-71. MATERIAL ID IS A402H35 039-003, PO 604814.1 IAW FEDEX DWG SRZ 25-005, REV F. FABRICATED NEW FLOOR PANEL FOR THE MAIN CARGO DECK FROM FRAME 65 TO FRAME 66 USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ 25-005, REV F. MARKED PANEL NR 251 BH IAW FEDEX DWG NR SRZ 25-005, REV F AND GMM 7-0-1000. PANEL PART ID IS FXR532B38300200. 2 L 7 2 4F RT A35EU 20080529 NM 2008 5 29 UIEA200800213 1 20080518 A 5315 FLOORBEAM BOEING 747 7472D7B 1384803 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK FLOORBEAM WEB FOUND CRACKED AT STA 1180 LBL 120. MAIN DECK FLOOR WEB CRACKED AREA REPAIRED PER EO 4753B153. 2 L 7 4 4F RT A20WE 20080603 EA 2008 6 3 SWIA200819665 1 20080319 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 FS 280 LOWER BEAM AT LBL 9 IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ200 REO601R-53-11-171. 2 L 7 2 4F RT A21EA 20080603 EU 2008 6 3 MALA080110 1 20080531 A 5347 7253001029 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 420XJ 340B420 CORROSION AT CENTER AISLE SEAT TRACK TO FLOOR INTERSECTIONS STA 297 LEFT AND RIGHT. REPAIRED CORRODED SEAT TRACK INTERS ECTIONS AT STA 297 IAW EO NR S53342. 2 L 7 2 4T RT A52EU 20080603 EU 2008 6 3 MALA080111 1 20080601 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 288-339 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 340B408 AT STA 288 TO 339, SEAT TRACKS ARE CORRODED AS DETAILED ON THE ATTACHED CONTINUATION CARDS. REPAIRED THE SEAT TRACKS. 2 L 7 2 4T RT A52EU 20080603 SO 2008 6 3 SWIA200819685 1 20080522 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DAMAGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 298SW 120328 FLT 3619 - EMERGENCY EXIT SIGN AT ROW 9 IS INTERMITTENT. REPAIRED WIRING ON EMERGENCY LIGHT AT ROW 9. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080603 EA 2008 6 3 SWIA200819643 1 20080317 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 613SK 10038 COCKPIT FLOOR SUPPORT IS CORRODED, FOUND AT C-CHECK. REPLACED COCKPIT FLOOR SUPPORT PER CRJ7/9 SRM 51-42-06. 2 L 7 2 4F RT A21EA 20080603 SO 2008 6 3 SWIA200819658 1 20080517 A 5210 ROD END EMB 120 EMB120ER 3260203 SO PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 297SW 120327 FLT 3569 - CABIN DOOR IS HARD TO OPEN FROM THE INSIDE. REPLACED CORRODED TORQUE TUBE ROD ENDS AND BEARINGS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080603 EA 2008 6 3 SWIA200819639 1 20080316 A 7120 BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 459SW 7782 UPPER FORWARD ENGINE BEAM IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS ON ENGINE BEAM WEB PER REO 601R-53-61-870 REV C AND REO 601R-53-61-2554. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 REXA200800018 1 20080530 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA ILLUMINATED A REXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 8932C 7932 FLIGHT SPOILERS SPOILERON CAUTION IN FLIGHT. FOLLOWED QRH MANUAL. EMERGENCY DECLARED AND LANDED WITHOUT INCIDENT. MAIN TENANCE RESET PER CRJ FIM, MESSAGE CLEARED. OK FOR SERVICE. 2 L 7 2 4F RT A21EA 20080603 WP 2008 6 3 UPS08852241 1 20080423 A 5320 GUSSET DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 MAIN CABIN GOUGE/CRACK IN BELTFRAME GUSSET STA 1460 AND L21R. FABRICATED AND REPLACED BELTFRAME GUSS ET AT STA 1460 AND L21R IAW SRM 51-21-24, DWG 5773480, SRM 51-1-8 AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 20080603 WP 2008 6 3 UPS08852242 1 20080423 A 5313 4619670 LONGERON SPLICE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 A PIT STA 390, LONGERON 36 SPLICE HAS EVIDENCE OF CRACK. REPLACED LONGERON 36 SPLICE AT STA 390 IAW SRM 51-01-20. 2 L 7 4 4F RT 4A25 20080603 NM 2008 6 3 USAA920081071 1 20080418 A 5315 143N501413 FLOORBEAM BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - CRACKED FLOORBEAM UPPER CHORD, BS 700, RBL 24.75 AND RBL 45.5, WL 207. REPLACED FLOORB EAM UPPER CHORD, BS 700, RBL 16.25 - RBL 53.5, WL 207 IAW USAIRWAYS EA 130014. 2 L 7 2 4F RT A2NM 20080603 NM 2008 6 3 CALA0800506 1 20080530 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 LEFT-HAND STATION 360 AT S8L AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED CRACK AT STATION 360 S 8L PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 CALA0800510 1 20080531 A 5730 65C267025 SKIN BOEING 737 737524 1384721 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 LEFT WING LEADING EDGE SKIN UPPER SURFACE CRACKED AT THE NUMBER 3 SLAT ACTUATOR. REPAIRED CRACK AT LEFT WING LEADING ED GE AT NUMBER 3 SLAT ACTUATOR CUT OUT PER CONTINENTAL EC/RA 5720-02060 AND PACE EA644-57-001 CAL. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 AALA200801123 1 20080428 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 940AN 30598 DFW - EMERGENCY LIGHT AT SEAT 10D HAS BROKEN LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080603 EA 2008 6 3 REXA200800019 1 20080531 A 3244 TIRE CNDAIR CL600 CL6002B19 1900309 EA MLG FAILED A REXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 25 8698A 7698 UPON ROTATION DEPARTING KJAN CREW NOTICED SUDDEN AND SHARP ROLLING MOTION AND TUG TO THE LEFT. SUSPECTED TO BE BLOWN TI RE. NO OTHER INDICATIONS NOTED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. NO DAMAGE OR DEFECTS NOTED AND A/C HA NDLED NORMALLY. MAINTENANCE FOUND NO DAMAGE OF DEFECTS NOTED. 2 L 7 2 4F RT A21EA 20080603 WP 2008 6 3 AALA200801108 1 20080427 A 3350 0202226001 SHROUD DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 975TW 53625 LGA - SEAT MOUNTED EMERGENCY LIGHT IN CABIN HAD DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT IN CABIN. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080603 CE 2008 6 3 A8OA200800002 1 20080430 A 2910 SA7670024001 HOSE RAYTHN DH125 HAWKER800XP 7150012 CE HYD SYSTEM RUPTURED E A8OA O OTHER K FLUID LOSS LD LANDING 1 SO 11 33NL 258643 ON SHORT FINAL TO KPDK, THE PLANNED DESTINATION, THE FLIGHT CREW DETECTED THAT THE HYDRAULIC FLUID LEVEL WAS DECREASING RAPIDLY. THE CREW DID NOT HAVE TIME TO DECLARE AN EMERGENCY AND LANDED. AS THE HYDRAULIC SYSTEM DEPLETED, THEY HAD RES IDUAL HYDRAULICS TO APPLY INITIAL BRAKING AND WERE ABLE TO STEER THE AIRCRAFT FROM THE ACTIVE BEFORE THE SYSTEM TOTALLY DEPLETED. AFTER DEPARTING THE ACTIVE, THEY DEPLOYED THE EMERGENCY BRAKING SYSTEM AND CAME TO REST WITHOUT FURTHER INCID ENT. MAINTENANCE DISCOVERED A RUPTURED HYDRAULIC HOSE FOR THE LT MAIN LANDING GEAR INBOARD DOOR ACTUATOR ON THE CLOSE P ORT. THE HOSE WAS REPLACED, SYSTEM SERVICED AND BLED AND ALL OPERATIONAL CHECKS REQUIRED ACCOMPLISHED. THE AIRCRAFT WA 2 L 7 2 4F RT A3EU 20080603 NM 2008 6 3 05212008001 1 20080507 A 3600 2703550 CLAMP BOEING 767 767238 1385114 NM PWA JT9 JT9D7R4E 52054 NE DUCT FAILED A L43A O OTHER M OVER TEMP CR CRUISE 1 EA 27 250MY 23306 P716915 THE CREW REPORTED THAT AFTER A NORMAL TAKEOFF AND CLIMB, AND AFTER GOING INTO CRUISE THE LEFT ENGINE WOULD NOT PRODUCE G REATER THAN 70 PERCENT N1, 80 PERCENT N2 AND 1.00 EPR. THEY ALSO REPORTED THAT EICAS REPORTED A LEFT ENGINE OVERTEMP OF 451 DEGREES. THE CREW FOLLOWED THE QRH WHICH INSTRUCTED THEM TO SHUTOFF THE BLEED, AFTER THIS ACTION THEY REGAINED NOR MAL OPERATION OF THE ENGINE. UPON ARRIVAL AND FURTHER INVESTIGATION BY MAINTENANCE IN MZJ, MAINTENANCE DISCOVERED THE 8 TH STAGE BLEED AIR DUCT V BAND CLAMP LAYING IN THE COWLING FOR THE INBOARD THRUST REVERSER. THE BLEED LEAK THAT WAS CAU SED BY THE FAILURE OF THE V BAND CLAMP HAD ALSO DAMAGED THE FAN AIR MODULATING VALVE. THE INVESTIGATION REVEALED THAT T 2 L 7 2 4F 4 F RT A1NM E3NE 20080603 2008 6 3 QXEA200800513 4 20080521 A 2210 C18117AA SERVO BOMBDR DHC8 DHC8402 1390042 NM AUTOPILOT MALFUNCTIONED A QXEA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 09 425QX 4370 4039 PDX - FLIGHT 2332 - AFTER TAKEOFF WITH THE GEAR UP AND THE FLAPS AT ZERO ON FLAP RETRACT (STILL MOVING), THE FIRST OFFIC ER WAS UNABLE TO TURN THE AIRCRAFT TO THE LEFT FOR ABOUT 4-5 SECONDS. AFTER THE FLAPS WERE FULL UP CONTROL WAS RETURNED . ON LANDING IN PDX, FLAPS 5 DEGREES, NO PROBLEMS. AS THE LANDING GEAR WAS LOWERED, CONTROLS LOCKED AGAIN FOR 10-15 SE CONDS. AFTER GEAR WAS FULLY DOWN, CONTROL RETURNED. IN BOTH CASES THE AUTOPILOT WAS OFF. MAINTENANCE REPLACED THE AUT OPILOT ROLL SERVO AND CAPSTAN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080603 NM 2008 6 3 QXEA200800537 1 20080602 A 2611 47359715 SMOKE DETECTOR BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY NO TEST A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 408QX 4050 PDX - NR 1 AFT BAGGAGE BAY SMOKE DETECTOR WILL NOT TEST. MAINTENANCE REPLACED THE SMOKE DETECTOR. OPERATIONAL CHECKS G OOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080702 NM 2008 7 2 SWAA083381 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 USAA920081204 1 20080605 A 5320 143N52601 ANGLE BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 905AW 23567 C12/ NR 6109923 - INTERCOSTAL UPPER ANGLE CRACKED BS 440 TO 460, WL 208.1, BL0 (HFEC VERIFIED). REPLACED INTERCOSTAL UPP ER ANGLE CRACKED BS 440 TO 460, WL 208.1, BL 0 IAW SRM 51-40-02-0G. (K) 2 L 7 2 4F RT A2NM 20080702 EU 2008 7 2 USAA920081199 1 20080528 A 5540 D5537131800200 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 640AW 448 C3 CHECK, NR6105677, NR 4 RUDDER HINGE FITTING HAS EXCESSIVE PLAY. VERTICAL STABILIZER STATION 2632 / RIB 6. REPLACED NR 4 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 2632/ RIB 6 IAW AMM 55-36-41. (K) 2 L 7 2 4F RT A28NM 20080702 NM 2008 7 2 2008UALA03549 1 20080622 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 OVERWING EMERGENCY LIGHT RT TOP FWD INOP. FOUND BURNED OUT LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03548 1 20080622 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 OVERWING EMERGENCY LIGHT LT SECOND FROM TOP FWD INOP. FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY OP CHECKED OK. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03517 1 20080622 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM AFT GALLEY LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 311UA 23672 EXIT PATH LIGHTING AT REAR OF CABIN HAS COME LOOSE. LIGHT ASSEMBLY BROKEN AND LOOSE. REPLACED LIGHT ASSEMBLY OP CHECKE D GOOD. AC OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800630 1 20080622 A 5320 141A5410U23 FLOOR SUPPORT BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 15712 28783 MAIN DECK FLOOR SUPPORT CRACKED AT STATION 344 TO 360 BL 0. REMOVED AND REPLACED FLOOR SUPPORT AT BODY STATION 344-360 BL 0 REF SRM 51-40-02, APPLIED CIC REF SRM 51-20-01. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800631 1 20080622 A 5320 141A5410U12 FLOOR SUPPORT BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 15712 28783 MAIN DECK FLOOR SUPPORT CRACKED AT STATION 312 TO 328 RBL 28. REMOVED AND REPLACED FLOOR SUPPORT AT BODY STATION 312 TO 328 RBL 28 REF SRM 51-40-02, APPLIED CIC REF SRM 51-20-01. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800592 1 20080612 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 BODY STATION 827 RIGHT BETWEEN S-8R AND S-9R IS CRACKED. INSTALLED INTERIM REPAIR AT CABIN FRAME BODY STATION 827 RIGHT BETWEEN S-8R AND S-9R PER ECRA 5310-04783 DIP CONTROL NUMBER 88782 FOR FRAME REPAIR AT BODY STATION 827 S-8R AND S-9R A T PASSENGER SERVICE UNIT (PSU) BRACKET ACCOMPLISH A PERMANENT REPAIR BEFORE 09 JUNE 09 PER ECRA 5310-04783 PART 3. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083322 1 20080618 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 440, STR 13R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082794 1 20080522 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 253WN 32511 FWD CABIN EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080703 2008 7 3 SWAA082796 4 20080522 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 287WN 32537 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082805 1 20080524 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082868 1 20080527 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 235WN 34630 EEPLS ASSY LOOSE AT ROW 5 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080703 2008 7 3 SWAA082859 4 20080527 A 2565 D3135443 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED MV1 CHECK, L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED E VAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082851 1 20080526 A 5310 6546958 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 480 TO BS 500, LBL 68. REMOVED AND REPLACED WEB PER SR M. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082861 1 20080527 A 3397 8100022608 CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 464WN 32468 DURING SCHEDULED MV2 CHECK, FOUND RT FWD CABIN EEPLS INOP. FOUND LOOSE CONNECTOR AT LIGHT ASSY. SECURED CONNECTOR ON L IGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 CALA0800528 1 20080601 A 3397 W03600120 WIRE BOEING 737 7373T0 1384582 NM COCKPIT SHORTED A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 27 16310 23361 ON TOUCHDOWN SPARKS FELL FROM THE OVERHEAD PANEL, BOTH PILOTS SMELLED ELECTRICAL SMOKE. FOUND WIRE W036-01-20 SHORTED T O HOUSING OF RIGHT START SWITCH. REPAIRED IAW SWP 20-10-13 REPOSITIONED WIRE BUNDLE FOR PROPER CLEARANCE. WIRE SHORTED DUE TO IMPROPER CLEARANCE FROM RIGHT START VALVE SWITCH. 2 L 7 2 4F RT A16WE 20080703 NE 2008 7 3 2008UALA03521 2 20080622 A 7261 ENGINE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 OIL CONSUMPTION A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 219UA 30551 222053 NR 2 ENGINE OIL CONSUMPTION EXCEEDS LIMIT. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080703 SO 2008 7 3 RAIA00805013 1 20080513 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO AIRSTAIRS INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 835MJ 145353 PRE FLT 7900 - ORD - EMERGENCY LIGHT ON AIRSTAIRS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB. SYSTEM CHECK ED GOOD. 2 L 7 2 4T RT T00011AT 20080707 NM 2008 7 7 2008UALA02805 1 20080515 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 DOOR 4 LEFT CEILING ENTRY EMERGENCY LIGHT IS INOP. RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 USAA920081086 1 20080514 A 2560 P4010021 BATTERY BOEING 767 7672B7ER 1385107 NM FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 MIA - EEL - C4 CHECK - AFT FLIGHT ATTENDANT POSITION 3 FLASHLIGHT BATTERY WEAK. REPLACED AFT FLIGHT ATTENDANT POSITION 3 FLASHLIGHT BATTERY IAW B767 AMM 25-60-00. 2 L 7 2 4F RT A1NM 20080707 NM 2008 7 7 ASAA0842967 1 20080516 A 5512 SKIN BOEING 737 737490 1384715 NM HORIZ STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 795AS 28890 DENT FOUND IN RIGHTHAND HORIZONTAL STABILIZER LEADING EDGE. INSTALLED EXTERNAL DOULBER PER ALK EA 5510 01322. 2 L 7 2 4F RT A16WE 20080707 NM 2008 7 7 UPS08652290 1 20080518 A 3350 LIGHT BOEING 767 76734AF 1385212 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 324UP 27750 INSPECTION TYPE:ETOP ENTRY DOOR EMERGENCY LIGHT IS OUT. REMOVED AND REPLACED EMERGENCY DOOR LIGHT PER MM 33-51-03-2. 2 L 7 2 4F RT A1NM 20080707 NE 2008 7 7 NOCA03508 2 20080508 A 7200 RB211535E4 ENGINE BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE LEFT MALFUNCTIONED A NOCA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 15 752NA 28174 31331 JUST AFTER ROTATION LEFT ENGINE COMPRESSOR STALLED REPEATEDLY ALL INSTRUMENTS IN RED, EGT AT 896. SECURED ENGINE AND RE TURNED TO "STATION" TCM. PILOT REPORTED ENGINE SEEMED TO STABILIZE ONLY AFTER THE THRUST LEVER WAS RETARDED TO JUST ABO VE IDLE. CREW PERFORMED ENGINE SHUT DOWN PROCEDURE. DFDR READOUT IS TO BE ACCOMPLISHED AND ENGINE IS SCHEDULED TO BE C HANGED IN ACCORDANCE WITH FIM TASK PROCEDURE. LEFT ENGINE WAS REMOVED AND REPLACED ON 5-13-08 ON PL 752-0805-03 IN STAT ION TCM AS REQUIRED. 2 L 7 2 4F 4 F RT A2NM E12EU 20080707 EU 2008 7 7 2008UALA02813 1 20080516 A 5320 SHEAR PLATE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 446UA 834 FOUND SHEAR PLATE NR 15 CORRODED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080707 NM 2008 7 7 2008UALA02832 1 20080516 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 SEAT 4E EMERGENCY LIGHT INOP. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 KCSA081253 1 20080519 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 FUSELAGE FRAME DAMAGED AT BS 1120, STR 13L. 2 L 7 4 4F RT A20WE 20080707 EU 2008 7 7 UPS08152299 1 20080520 A 3040 4237084 MOTOR AIRBUS A300 A300F4622R 3930360 EU WINDSHIELD WIPER MALFUNCTIONED A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 01 139UP 0822 INSPECTION TYPE:N/A STRONG SMELL OF ELECTRICAL FIRE IN COCKPIT WITH PACKS OFF AFTER LANDING. REMOVED AND REPLACED CAPTA IN`S WINDSHIELD WIPER MOTOR, OPS CHECKS GOOD IAW MM 30-45-1 1-04, OK TO CONTINUE. 2 L 7 2 4F RT A35EU 20080708 SO 2008 7 8 C2XA08IA131 1 20080516 A 3397 M3902931229 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18557 145596 AUS - DURING MAINTENANCE INSPECTION THE SERVICE DOOR EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE LIGHT ON MEL 33-50-00/1 CAT-C CTL NR 146110, AND THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. ON 05/17/08 THE AIRCRAFT LANDED AT MCI WHERE MAINTENANCE REPAIRED A BROKEN WIRE NEAR THE DOOR HINGE, OP ERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20080708 NM 2008 7 8 2008UALA02888 1 20080519 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 SEAT 3J FWD EMERGENCY LIGHT IS INOP. REPLACED LAMPS. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 2008UALA02890 1 20080519 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 CEILING EMERGENCY LIGHT NEAR SEAT ROW 37 ABC IS INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 2008UALA02893 1 20080517 A 2530 191AC3 MOTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY FAULTY A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 174UA 24381 CART LIFT INOP WITH ACRID ELECTRICAL ODOR. NOTE CHRONIC HISTORY. MOTOR AND LIMIT SWITCH TO BE FAULTY. REPLACED SWITCH S10 OPS NORMAL PER MM 25-38-00. REPLACED MOTOR PER 25-38-02 OPS NORMAL. ACFT OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 2008UALA02921 1 20080519 A 3350 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 197UA 26901 FC EMERGENCY LIGHTS FLASH ON AND OFF. AFTER A HISTORY OF EXTENSIVE TROUBLE SHOOTING REPLACED POWER SUPPLY M6000 AT DOOR 1R LIGHTS TESTED OK. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 EU 2008 7 8 2008UALA02923 2 20080520 A 7320 8063215 MEC BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 FAILED A UALA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 WP 29 329UA 17858 17858 24149 860242 NR 1 ENGINE FLAMED OUT. FOLLOWED CHECKLIST WITH ENG RESTART. NORMAL LANDING. NO EMERGENCY DECLARED. THE ENGINE WAS B ORESCOPED AND VISUALLY EXAMINED. NO UNUSUAL FINDINGS. REPLACED NR 1 MEC AND FUEL PUMP (PRECUATIONARY). ACCOMPLISHED ALL RUNS ON NR 1 ENGINE. ALL PARAMETERS NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20080708 NM 2008 7 8 HNAA0800175 1 20080515 A 3350 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN EXPOSED A HNAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 07 807EX 292 RIGHT EMERGENCY FLOOR LIGHT COVER HAS WIRES STICKING OUT AT ROW 4 D+F. RE-SECURED WIRES AS NEEDED OK FOR SERVICE. 2 H 7 2 4T RT A13NM 20080708 SO 2008 7 8 RAIA0805021 1 20080518 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 811HK 145256 PRE FLT 5574 - STL - EMERGENCY LIGHT SIGN AT ROW 3 AND ROW 12 INOPERATIVE. MAINTENANCE CLEANED THE CONNECTORS TO THE EM ERGENCY LIGHT ASSEMBLIES. LIGHTS OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080708 SO 2008 7 8 RAIA00805023 1 20080519 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 816HK 145055 DURING MAINTENANCE INSPECTION, EMERGENCY LIGHTS ON THE CABIN FLOOR WERE FOUND TO BE INOPERATIVE. MAINTENANCE CLEANED AN D REPAIRED A BROKEN WIRE ON THE CONNECTOR. LIGHTS OPS CHECKED GOOD AFTERWARDS. 2 L 7 2 4T RT T00011AT 20080708 NM 2008 7 8 DHL2008764501 1 20080519 A 5311 FRAME BOEING 727 727264 138408M NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C CHECK REF N/R 098173, DENT AT RT MAIN CABIN FRAME BS 480 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40 -3 FIG1 AND 53-10-2 FIG3 MATERIAL DOUBLER 7075-T6 .050 INCH DIM 7 1/4 INCH BY 5 3/4 INCH PO NR 9006742. 2 L 7 3 4F A3WE 20080708 NM 2008 7 8 DHL2008764504 1 20080519 A 5311 FRAME BOEING 727 727264 138408M NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C CHECK REF N/R 098180, DENT AT MAIN CABIN FRAME BS 680 BETWEEN STR 16 AND 17R. FABRICATED REPAIR IAW B727 SRM 51-40-3 FIG1 AND 53-10-2 FIG3 MATERIAL 7075-T6 .050 INCH DIM 7 1/8 INCH BY 5 1/4 INCH PO NR 9006742. 2 L 7 3 4F A3WE 20080603 CE 2008 6 3 GUUA05080804 1 20080508 A 5540 10164001415 HINGE BRACKET BEECH 1900 1900D 1154162 CE RUDDER CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81536 25881 UE152 DURING SCHEDULED ROUTINE MAINT DISCOVERED UPPER RUDDER HINGE BRACKET EXFOLIATED. REPLACED UPPER RUDDER HINGE BRACKET. 2 L 7 2 4T RT A24CE 20080603 EA 2008 6 3 N6WA0080507 1 20080521 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT MALFUNCTIONED A N6WA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 151GJ 10216 5373-ORD. RT EMERGENCY EXIT DOOR CAUTION MESSAGE CAME ON AND OFF A FEW TIMES DURING TAXI FROM RUNWAY. PERFORMED OPS CH ECK OF THE RT OVERWING EMERGENCY EXIT DOOR IAW AMM 52-21-00, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819675 1 20080228 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910SW 7566 RIGHT ENGINE THRUST FITTING IS CORRODED, FOUND AT C-CHECK. REPLACED THRUST FITTING PER AMM 71-22-01-400-801. 2 L 7 2 4F RT A21EA 20080603 CE 2008 6 3 GUUA05240801 1 20080524 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 81536 UE152 FLIGHT: 5200, DURING FLIGHT CABIN SMELLS LIKE JET FUEL FUEL. INSPECTED UNDER CABIN FLOORBOARD NO LEAK NOTED CLEANED UND ER FLOOR AS NEEDED. 2 L 7 2 4T 4 T RT A24CE E26NE 20080603 NM 2008 6 3 CALA0800453 1 20080514 A 5315 65C33950 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17640 28901 FLOORBEAM 986.5 LBL 43 HAS CORROSION. BURNISHED CORROSION AND INSTALLED STRAP REPAIR PER SRM 53-00-51, FIG 201. 2 L 7 2 4F RT A16WE 20080603 EA 2008 6 3 SWIA200819629 1 20080512 A 7830 1267588 PDU CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 909SW 16782 16782 7558 RECEIVED A "R REV UNLOCKED" CAUTION MESSAGE, FLIGHT NR 6370. REPLACED THE NR 2 THRUST REVERSER PDU IAW MM 78-32-03. OP S CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819638 1 20080304 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 457SW 7773 FS 280 UPPER FLOOR SUPPORT IS CRACKED AT LBL9 AND RBL9, FOUND AT C-CHECK. COMPLIED WITH REPAIRS AT STA 280 PER REO601R 53-11-136. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819686 1 20080521 A 5240 LINKAGE CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR LOOSE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 745SK 10201 FLT 6390 - SERVICE DOOR WILL NOT OPEN AND CLOSE PROPERLY. INSPECTED AND RESECURED LINKAGE ON SERVICE DOOR. OPS CHECK G OOD. 2 L 7 2 4F RT A21EA 20080603 NM 2008 6 3 BB08085 1 20080511 A 2782 5006398N ROTARY ACTUATOR BOEING 757 7572S7 1384962 NM L/E SLAT OVERTORQUED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 906AW 81119 20198 23568 PHX FLT 146 - PHX TO LIH. ON DEPARTURE FROM PHX, THE CREW RECEIVED A 'LE SLAT DISAGREE' EICAS MESSAGE WITH A LEADING E DGE LIGHT ILLUMINATED. THE FLAPS INDICATOR REMAINED BETWEEN FLAPS UP AND FLAPS ONE POSITIONS. THE FLIGHT RETURNED TO F IELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMBER ONE SLAT ROTARY ACTUATOR DUE TO AN OVERTORQUE D INDICATION. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 20080603 NM 2008 6 3 UPS08M52260 1 20080514 A 2560 ESCAPE ROPE DOUG MD11 MD11F 3023600 NM COCKPIT TANGLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP 48745 INSPECTION TYPE:N/A F/O'S EMERGENCY ESCAPE LINE TANGLED BEHIND PANELING NEAR ANCHOR POINT, COULD NOT FREE LINE. UNTANGL ED AND STOWED PROPERLY F/O'S EMERGENCY LINE IAW MM 25-60-00. 2 L 7 3 4F RT A22WE 20080603 NM 2008 6 3 ASAA0892955 1 20080504 A 5730 116A3010 SKIN BOEING 737 737990 NM RT WING DAMAGED A ASAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 NM 02 319AS 33679 BIRD STRIKE TO RT WING LEADING EDGE ROOT. REMOVED & REPLACED RT LEADING EDGE SKIN. 2 L 7 4 4F RT A16WE 20080603 NM 2008 6 3 CALA0800503 1 20080528 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 LEFT-HAND STATION 867 AT S8L AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED CRACK AT STATION 867 S 8L PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 CALA0800509 1 20080531 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 RIGHT FRAME IS CRACKED AT S8R STATION 787. REPAIRED FRAME AT S8R STATION 787 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 AALA200801121 1 20080428 A 3350 SHROUD BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 342AN 33081 DFW - EMERGENCY LIGHT AT SEAT 38H SHROUD DAMAGED. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 38H. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080603 WP 2008 6 3 AALA200801109 1 20080427 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7546A 53028 DFW - EMERGENCY LIGHT AT FORWARD TAIL COMPARTMENT WALL LENS BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORW ARD TAIL COMPARTMENT WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080603 NM 2008 6 3 QXEA200800468 1 20080509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 425QX 4039 PDX - C4 CHECK, SEAT TRACK NR 5 IS CORRODED AT X30 AND X70. BLENDED CORROSION AND FOUND TO BE WITHIN LIMITS, HFEC FOUND NO CRACKS, ALODINE AND PRIMED AREA IAW RD 8/4-53-884. 2 H 7 2 4T RT A13NM 20080701 NE 2008 7 1 SWIA200819776 2 20080611 A 7261 ENGINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE NR 2 LEAKING A SWIA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 771SK 10244 OIL IS LEAKING OUT OF NR 2 ENGINE. (FLT 6084) REPLACED LEAKING SUCTION LINE ON NR 2 ENGINE DRIVEN HYDRAULIC PUMP. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080701 NM 2008 7 1 SWAA083163 1 20080610 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. R&R FITTING PER SRM. 2 L 7 2 4F RT A16WE 20080701 NE 2008 7 1 SWIA200819771 2 20080616 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RIGHT SMOKE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 290SW 120317 115691 SMOKE REPORTED IN CABIN ALONG WITH BAGGAGE COMPARTMENT SMOKE INDICATIONS. ACTIVATED BAGGAGE COMPARTMENT EXTINGUISHER. (FLT 5769) REPLACED RT ENGINE WITH SERVICEABLE UNIT. ALSO REPLACED THE NR 1 AND 2 CARGO FIRE BOTTLES IAW MM 26-21-00. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 20080701 EA 2008 7 1 SWIA200819773 1 20080616 A 3040 601R3303312 HEATER CNDAIR CL600 CL6002B19 1900309 EA WINDSHIELD INOPERATIVE A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 506CA 7793 RT WINDOW HEAT CAUTION MESSAGE DISPLAYED. REPLACED SIDE WINDOW ASSEMBLY IAW AMM 56-12-01. 2 L 7 2 4F RT A21EA 20080701 SO 2008 7 1 SWIA200819735 1 20080603 A 2460 ELECTRICAL SYS EMB 120 EMB120ER 3260203 SO MALFUNCTIONED A SWIA O OTHER J H WARNING INDICATION ELECT. POWER LOSS-50 PC AP APPROACH 1 NM 07 284YV 120284 AFTER SELECTING THE GEAR DOWN, THE ELECTRICAL SYSTEM TRANSFERRED TO EMERGENCY MODE. (FLIGHT #5719)INSPECTED AND OPERATE D THE AUXILLARY GENERATOR TRANSFERRING AND ELECTRICAL EMERGENCY SYSTEMS. SWUNG GEAR MULTIPLE TIMES. NO DISCREPENCIES NO TED. 2 L 7 2 4T RT A31SO 20080701 EA 2008 7 1 SWIA200819721 1 20080602 A 5610 NP13932212 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 710BR 7852 FIRST OFFICER SIDE WINDOW IS CRACKED. (FLIGHT 2724) REPLACED SIDE WINDOW IAW AMM 56-11-01. 2 L 7 2 4F RT A21EA 20080701 NM 2008 7 1 SWAA083401 1 20080619 A 5315 6545834 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 294, BL 0 TO RBL 4. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 SWAA083387 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 4L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080701 2008 7 1 DL757080883 4 20080617 A 2565 SLIDE BOEING 757 757232 1384965 NM LT OFF WING FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 647DL 24218 LT OFF WING ESCAPE FAILED PNEUMATIC DEPLOYMENT OPS CHECK. REPLACED LT OFF WING ESCAPE SLIDE ACTUATOR IAW AMM 25-65-05. LEAK AND OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 20080701 NM 2008 7 1 SWAA083380 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 DHL2008764514 1 20080521 A 5753 FLAP BOEING 727 727264 138408M NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 L/WING I/B MIDFLAP T/E CHORD CRACKED AT I/B CABLE DRUM, 2 PLACES. REMOVED DAMAGED AREA AT T/E CHORD ABOUT 51 INCHES. F ABRICATED NEW SECTION WITH P/N 604754 7075-T6 DIM 51 INCH AND PO 815986 IAW B727 SRM 57-50-2 FIG 5 AND 51-40-1 FIG 1. 2 L 7 3 4F A3WE 20080708 EA 2008 7 8 COMA0860248 1 20080521 A 5312 601R3114627 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 32939 7050 WHILE PERFORMING TASK CARD CRJ-2-162011, PRESSURE FLOOR SKIN DETAILED INSPECTION FOUND 2 CRACKS IN THE PRESSURE FLOOR SK IN BETWEEN RBL 9 AND LBL 9. CRACKS MEASURED 2.50" IN LENGTH. THE FLOOR SKIN WAS REPAIRED IAW BOMBARDIER REO 601R-53-41 -103 REV D. 2 L 7 2 4F RT A21EA 20080708 EA 2008 7 8 COMA0860249 1 20080521 A 5312 601R32026 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 32939 7050 TEMP REPAIR PREVIOUSLY APPLIED TO FS 559.0 BULKHEAD. REMOVED TEMP REPAIR AND PERFORMED PERMANENT REPAIR IAW COMAIR SR10 -53-41-0001 REV A SECTION II. 2 L 7 2 4F RT A21EA 20080708 EA 2008 7 8 COMA0860250 1 20080521 A 5311 601R3602629 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 32939 7050 CARGO COMPARTMENT UNDERFLOOR FRAME SECTOR AT FS 605 IS CRACKED. REMOVED AND REPLACED WITH SERV FRAME IAW CRJ SRM 51-42- 06 AND COMAIR SR99-5140-0001. 2 L 7 2 4F RT A21EA 20080708 EA 2008 7 8 COMA0860251 1 20080521 A 5210 601R319025 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 32939 7050 PAX DOOR FRAME FS 338.9 IS CRACKED AT UPPER END. REPAIRED IAW REO 601R-52-11-402. 2 L 7 2 4F RT A21EA 20080708 EA 2008 7 8 COMA0860253 1 20080521 A 5320 601R3401225 STRAP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 7014 STRAP BENEATH WINDSHIELD LOWER SIDE POST FITTINGS CRACKED. REMOVED AND REPLACED STRAP BENEATH LOWER POST IAW SRM 51-42- 21. 2 L 7 2 4F RT A21EA 20080708 WP 2008 7 8 ARWA20080505 1 20080518 A 7830 9791861 SHUTOFF VALVE DOUG DC10 DC1030F 3023504 WP THRUST REVERSER FAULTY A ARWA O OTHER J WARNING INDICATION DE DESCENT 1 SO 29 450ML 47831 NR 1 REVERSER PRESSURE LIGHT CAME ON DURING CRUISE, WENT OUT WHEN THROTTLES RETARDED FOR DESCENT. AS PER TAFI M/M 78-30 -00 FOUND OVERPRESSURE INLET SHUTOFF VALVE BAD. REMOVED AND REPLACED VALVE IN ACCORDANCE WITH M/M 78-31-09, CHECK SYSTE MS NORMAL. 2 L 7 3 4F RT A22WE 20080708 NM 2008 7 8 SWAA082867 1 20080527 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 765SW 29805 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080529 NM 2008 5 29 UIEA200800214 1 20080518 A 5315 FLOORBEAM BOEING 747 7472D7B 1384803 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK FLOORBEAM WEB FOUND CRACKED AT STA 1200 LBL 120. MAIN DECK FLOOR WEB CRACKED AREA REPAIRED PER EO 4753B154. 2 L 7 4 4F RT A20WE 20080529 NM 2008 5 29 08FDEA01868 1 20080516 A 5230 141N6243 SKIN BOEING 757 757236 1384971 NM ZONE 800 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 915FD 24120 R1 DOOR SKIN DENTED. REMOVED DAMAGE AND INSTALLED A DOUBLER REPAIR ON R1 DOOR SKIN IAW SRM 52-10-01 REPAIR NR 2, FIGURE 202. THIS REPAIR IS CLASSIFIED AS A "MAJOR" REPAIR, CATEGORY A, WITH NO FOLLOW UP TRACKING REQUIRED. 2 L 7 2 4F RT A2NM 20080529 NM 2008 5 29 08FDEA02008 1 20080528 A 5311 AFA00203 FRAME DOUG MD11 MD11F 3023600 NM BS 1701 L12R DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 529FE 48624 AFT CABIN AT APPROXIMATELY STATION 1701 RIGHT SIDE LONGERON 12 RIGHT TO LONGERON 13 RIGHT FOUND FRAME DENTED. AFT BS 17 01 FRAME RT LONGERON 12 TO 13 RT CARRIED OUT REPAIR AS PER SRM 53-30-00, FIG.1, VOL.I. DUE TO CAT B REPAIR, INITIAL I NSPECTION TO BE CARRIED OUT AT 14,500 CYCLE WITH REPETITIVE INSPECTIONS AT EVERY 9,500 CYCLE AS PER SRM 53-30-00, FIG. 1, VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA01981 1 20080524 A 5322 53FX14402 SHEAR TIE BOEING 727 727233 138408A NM BS 640 S27L DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 274FE 22039 FWD CARGO COMPARTMENT FRAME STA 640 SHEAR TIE LOWER FLANGE HAS A HOLE DRILLED THRU ABOVE STR 27L. FABRICATED 2 EACH FRE EZE PLUGS, 2 RETAINING PLATES. INSTALLED FREEZE PLUGS AND RETAINING PLATES IAW EA 7-5310-116985, SRM 51-30-2 AND 51-10- 7. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01982 1 20080525 A 5310 AGA72023 DOOR FRAME DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 AFT CARGO COMPARTMENT, AFTER REMOVAL OF DAMAGED DOOR CUT-OUT AFT LOWER SCUFF PLATE FOUND DOOR JAMB STRUCTURE WITH CORROS ION. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-122464, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 EU 2008 5 29 08FDEA01983 1 20080525 A 5347 R532H1414201 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 MAIN CARGO DECK SEAT TRACK NR 3 RT HAS BROKEN SCALLOPS AT FR 54.2 REMOVED DAMAGED SECTION AND INSTALLED REPAIR ON NR 3 R T SEAT TRACK BETWEEN FR 54.2 AND FR 55 IAW A310-200 SRM 53-10-16, FIG 202, PAGE 209/210. 2 L 7 2 4F RT A35EU 20080529 NM 2008 5 29 08FDEA01985 1 20080527 A 5347 BAC1520720 SEAT TRACK BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 AFT CABIN, LBL 25 , SEAT TRACK IB AND OB UPPER FLANGES CORRODED ON LOWER SURFACE AT 1130. REMOVED AND REPLACED SEAT TRA CK AT STA 1130, LBL 25, FOUND OLD SEAT TRACK OUT OF LIMITS. FABRICATED NEW AND INSTALLED REF BOEING DWG. 65-19606. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01861 1 20080516 A 5330 65139131 SKIN BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 274FE 22039 STA 660 AT PREVIOUS REPAIR STR 28L TO 28R EXTERIOR SKIN BULGED AND CRACKED NEAR L/E OF REPAIR, BULGING NEAR T/E. MANY F ASTENERS SHOW EVIDENCE OF WORKING AND CORROSION. REMOVED PREVIOUS DOUBLER IAW B727 SRM 51-30-2, CUTOUT DAMAGED AREA DIM 17 INCH BY 11 INCH AND FABRICATED REPAIR DOUBLER FROM 2024-T3 .080 PO NR 9005551 DIM 25 3/4 INCH BY 21 3/4 INCH AND 2 F ILLERS FROM 2024-T3 .071 PO NR 9007126 DIM 10 INCH BY 1 INCH EACH IAW B727 SRM 53-30-3 FIG 1 AND 53-30-2 FIG 2. TREATED AND PRIMED PARTS IAW B727 SRM 51-10-2 AND INSTALLED REPAIR DOUBLER AND FILLERS IAW B727 SRM 51-30-2 AND 53-30-3 FIG 1. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01988 1 20080527 A 5311 651634447 FRAME BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 AFT PIT BILGE BODY FRAME UPPER FLG IS BUCKLED, BS 1070, STR 25R - 27R DAMAGE ON FRAME FLANGE FOUND TO BE OUT OF LIMITS P ER SRM 53-10-1 PG 1-3 DETAIL 4 NOTE 5. REMOVED DAMAGE, NDT VERIFIED DAMAGE REMOVAL. VERIFIED MATERIAL FOR REPAIR DOU BLER, 7075 - O - .063" .A 03916 / PO 1035912. FABRICATED REPAIR DOUBLER ITEM 14. REPAIR DOUBLER FABRICATED IN ITEM NR 6 NOT USED. HEAT TREATED TO T-6. TREATED AND PRIMED AND INSTALLED REPAIR DOUBLER, REF SRM 53-10-1 PG 1-3, DETAIL 4, S RM 51-40-3 FIG 1 SRM 51-30-2 FIG 7 BOEING DWG 65-16344. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01992 1 20080527 A 5320 53FX14511 CHANNEL BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 FWD PIT STA 620 ABOVE STR 27L " U " CHANNEL SUPPORT ON FWD SIDE OF FRAME HAS 2 MISDRILLED HOLES AT LBL 26. REMOVED DAMA GE, FABRICATED 2 REPAIR ANGLES, HEAT TREATED TO T-6 CONDITION. FABRICATED FILLER. ALODINED AND PRIMED ALL REPAIR PARTS , INSTALLED REPAIR PARTS, REF FED EX EA NR 7-5310-118270. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01994 1 20080527 A 5322 69208134 SHEAR TIE BOEING 727 727233 138408A NM ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 AFT PIT BILGE BODY FRAME SHEAR TIE ASSY HAS DISBONDED LEVELING COMPOUND/CORROSION BS 1130 AFT, STR 29R - 30, WL 148. BL ENDED CORROSION ON SHEAR TIE, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW PIECE. REF SRM 51-30-02 AND DWG NR 69-20813. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA02000 1 20080527 A 5330 141N3215* SKIN BOEING 757 7572B7 1384964 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 903FD 27124 EXTERNAL FUSELAGE LOWER SKIN, APPROX BS 255, STR 27L, DENT WITH GOUGE. ACCOMPLISHED A MAJOR REPAIR IAW EA F-5330-110861 , WITH A RELEASE DATE OF 5/9/08. THERE IS NO FOLLOW UP TRACKING OR REPETITIVE INSPECTIONS REQUIRED FROM THIS REPAIR. 2 L 7 2 4F RT A2NM 20080529 EU 2008 5 29 08FDEA02001 1 20080527 A 5315 A53774571204 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 423FE 281 1/4 INCH CRACK IN FLOORBEAM C25 BETWEEN SEAT TRACK 2R AND 3R AT UPPER RADIUS IN FRONT FACE STIFFENER. REMOVED CRACK AND INSTALLED FLOORBEAM REPAIR ON FLOORBEAM FR C25, BETWEEN SEAT TRACKS 2RT AND 3RT IAW A310-200 SRM 53-10-15 FIG, 206. 2 L 7 2 4F RT A35EU 20080529 WP 2008 5 29 08FDEA01882 1 20080519 A 7160 NSL6012509 COWLING DOUG MD10 MD1010F 3022112 WP ZONE 400 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 567FE 46994 NR 3 ENGINE INBD FAN COWL HAS A SMALL PUNCTURE. REPAIRED DAMAGED AREA BY FABRICATING AND BONDING A FILLER AND DOUBLER I AW DC/MD-10 SRM 54-00-01, FIG 4, VOL I. RESTORED THE SURFACE FINISH IAW DC/MD-10 SRM 51-21-01, VOL II, 51-21-01; VOL I I AND 51-41-01, VOL II. 2 L 7 3 4F RT A22WE 20080529 EU 2008 5 29 08FDEA01884 1 20080519 A 5720 A5724105900100 STIFFENER AIRBUS 300 A300F4605R 3930327 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 661FE 760 LEFT WING SPAR AREA, TOP SKIN STIFFENER AT WIAX 13-9 HAS A CRACK. MATERIAL ID FOR THE REPAIR IS 7075-T6 0.110 60-7018 E XTRUSION PO 566980.6 IAW A300-600 SRM 57-51-11, FIG 207 AND DWG NR A57241059. FABBED REPAIR ANGLE IAW A300-600 SRM 57-5 1-11, FIG 207. ALODINED AND PRIMED IAW A300-600 SRM 1-21-10, PG 3, AND 51-23-10, PG 24. INSTALLED REPAIR IAW A300-600 SRM 57-51-11, FIG 207 AND SRM 51-40-21, PG 7. 2 L 7 2 4F RT A35EU 20080529 NM 2008 5 29 08FDEA02009 1 20080528 A 5311 FRAME DOUG MD11 MD11F 3023600 NM BS 1761 L12L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 529FE 48624 AFT CABIN AT APPROXIMATELY STATION 1761 LEFT SIDE LONGERON 12 LEFT FOUND FRAME DENTED. BS 1761 LT LONGERON 12 LT FRAME CARRIED OUT REPAIR AS PER SRM 53-30-00, FIG.1, VOL.I. DUE TO CAT B REPAIR, INITIAL INSPECTION TO BE CARRIED OUT AT 14,5 00 CYCLE, WITH REPETITIVE INSPECTIONS AT EVERY 9,500 CYCLE AS PER SRM 53-30-00, FIG.1, VOL.I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA02010 1 20080528 A 5311 AFA00193 FRAME DOUG MD11 MD11F 3023600 NM BS 1721 L12L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 529FE 48624 AFT CABIN AT APPROXIMATELY STATION 1721 LEFT SIDE LONGERON 12 LEFT FOUND FRAME DENTED. CARRIED OUT REPAIR AS PER SRM 53-30-00, REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA01907 1 20080520 A 5511 6933174 RIB BOEING 727 727233 138408A NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 LT HORIZ STAB TRAILING EDGE ELEVATOR HINGE SUPPORT RIB CRACKED 2 AREAS AT ELEVATOR STA 99.79 AFT INBOARD SIDE. REPAIR ED LT HORIZONTAL TRAILING EDGE HINGE SUPPORT RIB AT STA 99.79 REF SRM 55-10-4. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01917 1 20080520 A 5320 6529548 PAN BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 AFT MAIN DECK FLOOR DITCHING PAN ASSY HAS 2 CRACKS AND A MISSING FASTENER COLLER, BS 1176 - 1183,LBL 18 - 27, WL 208. REPLACED DITCHING PAN AT STA 1176 - 1183, LBL 18 - 27 REF BOEING DWG 65-29548 AND SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 EU 2008 5 29 08FDEA01922 1 20080520 A 5321 A532B384800400 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 815FD 638 THERE IS A BROKEN FLOOR PANEL FOR THE MAIN CARGO DECK FROM FRAME 77 TO FRAME 80/82, LBL 45 TO LBL 63. MATERIAL ID IS A4 02H35039-003, PO 604814.1 IAW FEDEX DWG SRZ 25-005, REV F. FABRICATED A NEW FLOOR PANEL FOR THE MAIN CARGO DECK FROM FR AME 77 TO FRAME 80/82 USING THE OLD FLOOR PANEL AS A TEMPLATE IAW FEDEX DWG SRZ 25-005, REV F. MARKED PANEL NR 251 ZF I AW FEDEX DWG SRZ 25-005, REV F AND GMM 7-0-1000. PANEL PART ID IS FDX532B384800400. 2 L 7 2 4F RT A35EU 20080529 NM 2008 5 29 08FDEA01923 1 20080520 A 5720 651626941 ANGLE BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 LEFT WING INBD LE CAVITY NR 2 FLAP ACTUATOR AFT MOUNT, UPPER CORNER ANGLE IS CRACKED REMOVED AND REPLACED WEB REF SRM 51 -30-2. OPS CHECKED ACCOMPLISHED ON W/C 70C003-00 THIS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA02006 1 20080528 A 5730 ARB2886503 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 529FE 48624 LEFT WING ANTI-ICE TELESCOPIC DUCT DOOR CUT OUT CORNER FOUND CRACKED AT STATION XOS 464 AND XOS 470. REPAIR CARRIED O UT AS PER SRM 57-10-00, FIG.43, VOL.I AND EA 1-5710-122715, REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA01946 1 20080521 A 5753 65217953 FAIRING BOEING 727 727233 138408A NM FLAP TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 NR 4 T/E FLAP TRACK FWD FAIRING, HAS CRACK AT FWD END CUTOUT REMOVED EXISTING DOUBLER, CUT OUT DAMAGE, NDT CHECKED FAIRI NG AND FOUND CRACK TO BE TERMINATED. MADE ADDITIONAL CUT FINALE CUT. FABRICATED REPAIR DOUBLER AND FILLER. TREATED AN D PRIMED. INSTALLED REPAIR PARTS. PAINTED IN REF TO SRM 57-20-4 PG 5-12, SRM 57-20-2 PG 4, SRM 51-10-2 PG 1-7, MM 51 -20-151-7, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 EU 2008 5 29 08FDEA01947 1 20080522 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU RT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND OLD REPAIR ON RT INNER FLAP UPPER SKIN, RIB 11-12 WITH NEW DAMAGES, (2 NICKS ON DOUBLER). REPAIR RENEWED IAW SRM 57-50-00 FIG 205. 2 L 7 2 4F RT A35EU 20080529 EU 2008 5 29 08FDEA01948 1 20080522 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU RT WING TE FLAP DAMAGED A FDEA O OTHER O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND OLD DOUBLER REPAIR ON RT INNER FLAP LOWER SKIN, RIB 1C-3 WITHOUT ANY OLD DOCUMENTATION AVAILABLE. REPAIR RENEWED (PATCH REPAIR) IAW RAS RAS/FOK/086/2008 ISS A, APPROVED BY EA 6-5752-120047. 2 L 7 2 4F RT A35EU 20080529 SO 2008 5 29 C2XA08RI065 1 20080509 A 2611 LIGHT EMB 145 EMB145LR 3260212 SO SMOKE DETECTOR INOPERATIVE A C2XA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 27 12567 145623 FLIGHT 2648 - EWR - FLIGHT CREW REPORTED BAG SMOKE DETECT WOULD NOT ILLUMINATED ON TEST. EWR MX RESET THE SYSTEM AND PE RFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20080529 SO 2008 5 29 C2XA08TY050 1 20080513 A 5751 14569009409SD BRACKET EMB 145 EMB145LR 3260212 SO LT AILERON DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13970 145146 TYS - DURING A CURRENT C-CHECK INSPECTION THE LT AILERON I/B PCA ACTUATOR ROD ATTACHMENT FITTING WAS FOUND DAMAGED. MAI NTENANCE REMOVED AND REPLACED THE PCA BRACKET IAW EC 5750-01177. A/C WILL BE RELEASED UPON COMPLETION OF THE C-CHECK IN SPECTION. 2 L 7 2 4T RT T00011AT 20080529 EA 2008 5 29 HNAA0800151 1 20080511 A 3150 WARNING HORN DHAV DHC8 DHC8311 1386006 EA FALSE ACTIVATION A HNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 07 328EN 281 TAKEOFF WARNING HORN SOUNDED ON TAKEOFF ROLL. COMPLIED WITH WORK CARD 31-50-03Q. NO DEFECTS OR DISCREPANCIES FOUND. O PERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 20080529 NM 2008 5 29 HALA0800586 1 20080508 A 5740 BRACKET BOEING 767 7673CB 1385187 NM CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 590HA 33467 CRACK FROM FASTENER HOLE ON BRACKET, WHICH ATTACHES TO SLAT CONTROL ROD, AND SUPPORTS FILLER PANEL, WHICH CONTROLS ROTAR Y ACTUATOR, WHEN SLAT RETRACTED. LOCATION, L/WING, NR 3 L/E SLAT, INBD CONTROL ROD, FWD BRACKET. REPLACED BRACKET. 2 L 7 2 4F RT A1NM 20080529 NE 2008 5 29 HALA0800587 2 20080516 A 7320 EEC BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE LT ENGINE INOPERATIVE A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 596HA 23276 ATB - ETOPS SIGNIFICANT SYSTEM, EICAS L ENG EEC INOP. REMOVED AND REPLACED THE EEC IAW 73-21-07 ACCOMPLISHED EEC PMC TE ST. NEED TO ACCOMPLISH TASK 71-00-00-735-202-G00 (CONT. BELOW). ACCOMPLISHED TEST 11 EEC (PMC)/MAIN ENGINE CONTROL (ME C) TEST, TESTED GOOD OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E13NE 20080529 WP 2008 5 29 08FDEA01949 1 20080522 A 5347 601096418 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 301FE 46800 MAIN CARGO COMPARTMENT SEAT TRACK HAS GOUGED AREA AT F/S 1380-1400 LBL 75 REMOVED DAMAGE AREA IAW SRM 53-70-00. FABRICA TED SPLICE HAT AND PLATE ON TRAVELER NR T8/740011. SEAT TRACK ON TRAVELER NR T8/740012. INSTALLED NEW SEAT TRACK, SPLI CE HAT AND PLATE IAW SRM 53-70-00. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA01956 1 20080522 A 5343 ACA7017501 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 NLG LT TRUNNION FITTING FWD EDGE FOUND WITH CRACK. REPAIRED AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1,500 LANDING INTERVALS IN REFERENCE T O WITH SRM 53-40-00 FIGURE 23 VOLUME I. 2 L 7 3 4F RT A22WE 20080722 2008 7 22 2008UALA02904 4 20080519 A 2565 D31591478U1 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU R1 DOOR MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 339UA 24243 DOOR 1R SLIDE PRESSURE GAUGE MISALIGNED. SUSPECT SLIDE IMPROPERLY INSTALLED. REPOSITIONED DOOR 1R SLIDE PACK. AC OK F OR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080529 NM 2008 5 29 HALA0800579 1 20080514 A 7700 DISPLAY BOEING 767 76733A 1385209 NM COCKPIT INOPERATIVE A HALA O OTHER P NO WARNING INDICATION CR CRUISE 1 WP 13 582HA 28139 ETOPS SIGNIFICANT SYSTEM, STAND-BY ENGINE INSTRUMENTS BLANK WHEN SELECTED ON. PERFORMED OPS CK PER AMM77-41-01, OPS CK GOOD OK TO CONTINUE. 2 L 7 2 4F RT A1NM 20080529 NM 2008 5 29 HALA0800581 1 20080514 A 7500 7732899 CONTROLLER BOEING 767 76733A 1385209 NM BLEED AIR SYS MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, LT ENGINE HPSOV EICAS CAME ON WHEN POWER REDUCED. TROUBLESHOT PER FIM 36-10-00. REPLACED HP CONTROLLER PER AMM 36-11-08-004-005-003 ENG RUN CHECKS GOOD, NO FAULTS/MSG. 2 L 7 2 4F RT A1NM 20080529 NM 2008 5 29 08FDEA01933 1 20080521 A 5312 655717227 ANGLE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 AFT PIT BS 950E BULKHEAD RIGHT FWD BLOW OUT PANEL FRAME HAS CORROSION AROUND NUTPLATES. REMOVED DAMAGED Z-ANGLE, REPLAC ED WITH FABRICATED Z-ANGLE. INSTALLED ON BULKHEAD PANEL STA 950E IAW DWG 65-57172 AND SRM 51-40-02. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 WP 2008 5 29 08FDEA01935 1 20080521 A 5730 ARB087241 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 567FE 46994 RIGHT WING FUEL PLATE/PANEL 635 AT, INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION, NICKS AND GOUGES. REMOVED DAMAGE AND FOUND PANEL TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00, VOL II, PG 217. MACHINED A NEW 635 AT PANEL IAW DAC DWG ARB0872, REV "AV". APPLIED ALODINE, PRIMER AND PAINT IAW ARB0872, REV "AV" AND DC/MD-10 SRM 51-21-01, VOL II. PART M ARKED IAW FEDEX GMM 7-0-1001. FPI PER DPS 4.707 AND DAC DWG ARB0872, REV "AV", NO CRACKS NOTED. 2 L 7 3 4F RT A22WE 20080527 NM 2008 5 27 SWAA082673 1 20080515 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM BS 360 S20R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 ASAA0842944 1 20080511 A 5753 SKIN BOEING 737 7374Q8 138447Q NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 LEFT INBOARD AFT FLAP LWR SURFACE DENTED 2.5 FEET OUTBOARD & AT INCHES UP. REPAIRED INBOARD AFT FLAP IAW B737 400 SRM 5 1 70 10 REPAIR 2 PG 201. 2 L 7 2 4F RT A16WE 20080527 NM 2008 5 27 SWAA082679 1 20080518 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727E S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082745 1 20080520 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 867-887 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 867 TO BS 887, LBL 65. REMOVED AND REPLACED WEB PER SR M. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082792 1 20080522 A 5312 6517853 STIFFENER BOEING 737 7373H4 1384600 NM BS 178 BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178, RBL 5.7, WL 185. REPAIRED STIFFENER PER SWA EA . 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082790 1 20080522 A 5311 6546564 FRAME BOEING 737 7375H4 138449D NM BS 986 S2L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 986.5, STR 2L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082789 1 20080522 A 5311 6546564 FRAME BOEING 737 7375H4 138449D NM BS 986 S3L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 986.5, STR 3L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080528 SO 2008 5 28 RAIA00805007 1 20080505 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DIRTY A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 829HK 145281 PRE FLT 8018 - STL - EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE CLEANED THE CONNECTOR TO THE AFFECTED LIGHT. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080528 NM 2008 5 28 SWAA082764 1 20080521 A 3350 ANNUNCIATOR BOEING 737 7373G7 1384595 NM EMERGENCY LIGHTS FALSE INDICATION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 EMERGENCY LIGHTS ILLUMINATED WITH ALL SWITCHES IN NORMAL POSITION. THE ANNUNCIATOR LIGHT DID NOT ILLUMINATE WHEN COVERE D SWITCH WAS PLACED OFF. RESET CIRCUIT BREAKER PER MM. OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082714 1 20080518 A 5340 6557463 FITTING BOEING 737 7375H4 138449D NM L1 DOOR GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082782 1 20080522 A 2560 PL22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM ROW 12 DEF LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 704SW 27838 DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 12 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082733 1 20080519 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 380 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND STRINGER 15L CRACKED AT BS 380. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 SWAA082716 1 20080515 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 500A S27R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 500A, STR 27R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080528 2008 5 28 SWAA082702 4 20080516 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 760SW 27874 L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080528 NM 2008 5 28 NWAA082135803 1 20080514 A 3350 BATTERY PACK BOEING 757 757351 1384991 NM EMERGENCY LIGHTS DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 583NW 32983 BATTERY PACK ASSOCIATED WITH THE ESCAPE PATH LIGHTING AT ROWS 14 THROUGH 20 FAILED DURING EMERGENCY LIGHT BATTERY PACK C HECK DURING SCHEDULED OVERNIGHT MAINTENANCE. MAINTENANCE REPLACED THE BATTERY PACK AND ALL OPERATIONS CHECKED GOOD. 2 L 7 2 4F RT A2NM 20080528 SO 2008 5 28 SIMA200814301 1 20080520 A 3350 20131A POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 626AE 145117 ON FLIGHT 3942, DURING TAXI CREW REPORTS EMERGENCY FLOOR LIGHTING SYSTEM FROM EXIT ROW BACK INOPERATIVE. AIRCRAFT REMOV ED FROM SERVICE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY NR 4 IAW EMB 145 AMM 33-50-04. OPERATIONAL CHECK GO OD. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4T RT T00011AT 20080528 GL 2008 5 28 SIMA200814303 2 20080520 A 7200 ENGINE EMB 135 EMB135KL 3260302 SO ALLSN AE300 AE3007A GL NR 2 MALFUNCTIONED A SIMA O OTHER E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 839AE 145653 ON FLIGHT 3882, DURING TAKEOFF CREW REPORTED THERE WAS A VERY PRONOUNCED EXCESSIVE VIBRATION DURING TAKEOFF ROLL AND DUR ING GEAR RETRACTION FROM NOSE GEAR. DURING TAKEOFF DEADHEAD EMJ CAPTAIN REPORTED 3 LOUD BANGS SIMILAR TO A COMPRESSOR S TALL ON TAKEOFF. MOMENTARY LOSS OF NR 2 ENGINE INDICATIONS N1 N2 AND ITT INDICATED DASHED LINES ON LIFTOFF WITH APU RUN NING RELAYS BEHIND F/O SEAT KEPT CLICKING AND CABIN LIGHTS FLICKERED. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080528 WP 2008 5 28 NWAA082329855 1 20080524 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 764NC 47717 DURING LINE CHECK, MAINTENANCE FOUND THAT THE RIGHT SIDE EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE RE PLACED THE EMERGENCY LIGHT POWER SUPPLY AND OPERATIONALLY CHECKED THE SYSTEM. 2 L 7 2 4F RT A6WE 20080528 WP 2008 5 28 IXXA08SMN095S 1 20080314 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1395 L36 MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND DOUBLER AFT LOWER FUSELAGE BELLY SKIN BELOW AND FWD D-PIT DOOR ALUMINUM RIVETS IN FRAMES AT FS 1395, LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED INS PECTION NDT. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, FILLER SKIN, INTERNAL FINGER DOU BLER, AND FILLER INTERNAL DOUBLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REP AIR PARTS IAW DC8 SRM 51-1-11, 51-1-12, 51-3-1, FAA FORM 8110-3 NUMBER 08205 DATED 04/29/08, SEMAN DRAWING NUMBER ED-473 5 DATED 03/24/08, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 20080528 WP 2008 5 28 IXXA080022S 1 20080313 A 5730 SB085700865 SKIN DOUG DC8 DC873F 302199F WP ZONE 600` MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RIGHT WING UPPER AFT SKIN PANEL. REMOVED FASTENERS AS NEEDE D TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-1-11, 5 1-1-20D, 51-3-1, AD 90-16-05, DC8 S/B 57-86, DOUGLAS DRAWING J060104, SERVICE SKETCH NUMBER 3313, BOEING MESSAGE 1-78088 8417-2 DATED 03-03-08, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 20080528 EU 2008 5 28 08FDEA01871 1 20080517 A 5315 A53781966200 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 MAIN CABIN FLOORBEAM AT FR 31 HAS .250 IN CRACK, BETWEEN SEAT TRACKS NR 4 LT AND NR 5 LT REMOVED CRACK AND INSTALLED FLO ORBEAM REPAIR ON FLOORBEAM FR 31, BETWEEN SEAT TRACKS NR 4 LT AND NR 5 LT IAW A300-600 SRM 53-10-15, FIG 212. 2 L 7 2 4F RT A35EU 20080529 NM 2008 5 29 08FDEA01894 1 20080520 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 MAIN DECK CARGO DOOR SPOOL FITTING NR 6 FOUND 3RD LAYER CRACK INDICATION AT FITTING BOLT HOLES 'A' AND 'D'. FITTING REM OVED AND REPLACED AS PER SRM 51- 31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA01895 1 20080520 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 MAIN DECK CARGO DOOR SPOOL FITTING NR 7 FOUND 3RD LAYER CRACK INDICATION AT FITTING BOLT HOLES 'A', 'B', 'C' AND 'D'. F ITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA01896 1 20080520 A 5330 ADA70301 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 590FE 48505 EXISTING DOUBLER REPAIR AT FWD CARGO DOOR AFT CUT-OUT AT APPROX STR 39-42 NOT IAW SRM STANDARDS. EXISTING REPAIR AND FO UND NOT IAW. SRM 53-50-00 FIG 17 VOL. I. REPAIR CARRIED-OUT AS PER SRM 53-50-00 FIG. 17 VOL. I. REPAIR CLASSIFIED AS M AJOR AS PER GMM 6-2-100. EO 1-5100-7-5001 A3 PT 1. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA01904 1 20080520 A 5311 6556132 FRAME BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 AFT PIT, BILGE BODY FRAME, HAS A DRILL START ON UPPER FLANGE AND CORRODED WEB BS 1143, FWD AND AFT SIDE, STR 26R - 27R, WL 153 - 156 LEVEL 1 CORROSION BLENDED AREA, FLAP PEENED AREA, APPLIED ALODINE AND PRIMER TO AREA APPLIED CORROSION INHI BITOR TO AREA, REF EA 7-5310-118267. ORIGINAL T .080 INCH REMOVED .055 INCH, .025 INCH REMAINING. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 UIEA200800215 1 20080518 A 5210 PANEL BOEING 747 7472D7B 1384803 NM BS 800 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 522MC 21783 MAIN DECK L-2 DOOR FWD UPPER INNER REVEAL PANEL FOUND CRACKED. CRACKED AREA REPAIRED IAW EO NR 4753B148. 2 L 7 4 4F RT A20WE 20080529 NM 2008 5 29 08FDEA01878 1 20080518 A 5730 ARB74024 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 08 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN ST A XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-122452, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-10 0. 2 L 7 3 4F RT A22WE 20080708 NM 2008 7 8 SWAA082843 1 20080523 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 SWAA082901 1 20080529 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 467WN 33830 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 CALA0800517 1 20080602 A 5320 65528942 FLOOR SUPPORT BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 MAIN DECK FLOOR SUPPORT AT STATION 540 LBL 2 IS CRACKED. REMOVED AND REPLACED MAIN DECK FLOOR SUPPORT AT STATION 540 LB L 2 PER EC/RA 5321-01551. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 CALA0800521 1 20080602 A 5311 143A1113 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 FRAME CRACKED AT STATION 440 BETWEEN S8R AND S9R. REPAIRED FRAME AT STATION 440 S8R AND S9R PER EC/RA 5310-04777. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 DL757080858 1 20080612 A 5320 WEB BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 RT SIDE MAIN CABIN FLOOR STRUCTURE IS CORRODED AT FS 1420-1440 LOWER WEB FWD END. REPLACED DAMAGED WEB IAW SRM 51-40-02 . 2 L 7 2 4F RT A2NM 20080708 NM 2008 7 8 DL757080870 1 20080613 A 5310 DOOR FRAME BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 CABIN L4 DOOR CUTOUT, FWD FRAME AT FLOOR LEVEL 5 IN FWD OF DOOR FRAME CORRODED. REPAIRED DAMAGED SECTION IAW SRM'S 53-6 0-15, 51-10-02 AND ERA 468357-14. 2 L 7 2 4F RT A2NM 20080708 NM 2008 7 8 DL764080796 1 20080530 A 2120 WARNING SYSTEM BOEING 767 767432ER 1385134 NM COCKPIT ACTIVATED A DALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SO 27 826MH 29697 ATB DUE TO FWD EQUIPT COOLING EICAS AND OVHT LIGHT. C/W QRH PROCEDURES LIGHT WENT OUT. NTF AT GATE. OPS CHECK OF EQUI PT COOLING PASSED. 2 L 7 2 4F RT A1NM 20080708 NM 2008 7 8 DL76G080815 1 20080601 A 5270 S283T0067 SENSOR BOEING 767 767332 1382001 NM BULK CARGO DOOR MALFUNCTIONED A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 172DZ 29691 ABORTED DUE TO BULK CARGO DOOR LIGHT, JUST BELOW 80 KNTS. OPENED DOOR CHECKED SENSORS AND LINKAGES AND OK. CLOSED DOOR . NOW BULK CARGO DOOR LIGHT EXT IN COCKPIT FWD TO MCO AND PLAC PER MEL 52-71-01. C/W REP CHECK BE VERIFYING DOOR IS CL OSED AND LOCKED. HANDLE FAIRED AND FLUSH WITH FUSELAGE. 2 L 7 2 4F RT A1NM 20080708 NM 2008 7 8 DL76G080832 1 20080604 A 3350 BPS73 POWER SUPPLY BOEING 767 7673P6 1385105 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1501P 24983 FOUND EMERGENCY PATH LIGHTS OUT LEFT SIDE AT L1 DOOR. REPLACED CHARGER AND BATTERY PACK AND K371 RELAY AND RELAMP AT L1 DOOR. CHECKS GOOD PER AMM. CHARGER AT 1084. 2 L 7 2 4F RT A1NM 20080708 SO 2008 7 8 RAIA00805011 1 20080514 A 3240 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT ACTIVATED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 835HK 145670 FLT 8006 - RIC - BRAKE OVERHEAT INDICATION ON THE EICAS DURING CLIMB. MAINTENANCE DEFERRED THE BRAKE TEMPERATURE INDICA TION IAW MEL PROCEDURES. 2 L 7 2 4T RT T00011AT 20080708 SO 2008 7 8 RAIA00805024 1 20080520 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 842HK 14500830 PRE FLT 8027 - TYS - EMERGENCY LIGHTS INOPERATIVE THROUGHOUT THE CABIN. MAINTENANCE RESECURED THE CONNECTOR TO THE NR 3 BATTERY. LIGHTS OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080708 NM 2008 7 8 2008UALA02686 1 20080508 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 CORROSION ON SHEAR TIE IN BILGE AT STA 1197.66, BETWEEN STR 39L AND 39R. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW SHEA R TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080708 NM 2008 7 8 HNAA0800177 1 20080516 A 2432 5224871 WARNING SYSTEM DHAV DHC8 DHC8102 2809003 NM MAIN BATTERY FAULTY A HNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 07 807EX 36588 1357 292 MAIN BATTERY HOT WARNING LIGHT ILLUMINATED DURING TAXI, BATTERY TEMP MONITOR PANEL READS NORMAL TEMP. INSPECTED WIRES A T MAIN BATTERY, NO DEFECTS NOTED. REMOVED AND REPLACED MAIN BATTERY GROUND RAN A/C, NO DEFECTS NOTED IAW 24-32-00. 2 H 7 2 4T RT A13NM 20080710 NM 2008 7 10 DL75A080726 1 20080514 A 5330 141N32311 SKIN BOEING 757 757212 1384951 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 750AT 23126 FUSELAGE SKIN FOUND CORRODED AT STA 440 BELOW STR 28L. DAMAGE WAS CUT OUT, AREA WAS INSPECTED AND A REPAIR DOUBLER WAS INSTALLED. 2 L 7 2 4F RT A2NM 20080710 NM 2008 7 10 DLM90080734 1 20080423 A 5311 SR095300572 FRAME DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 AFT CARGO BAY FRAME AFT SIDE CORRODED STA 1328 FROM LONGERON 29L TO 28R. REPAIRED FRAME AT STA 1328, IAW MD90 SRM 53-10 -02 FIG 2. 2 L 7 2 4F RT A6WE 20080710 NE 2008 7 10 DL76G080736 2 20080516 A 7310 AC922F1740 FILTER BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 ENGINE DIRTY A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 177DZ 29698 706131 AFTER TAKEOFF GOT L ENG FUEL FILT EICAS MSG AND STATUS MSG. REPLACED LEFT ENG MAIN FUEL FILTER OPN AND LEAK CHECK GOOD. FILTER P/N AC922F1740. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK. 2 L 7 2 4F 4 F RT A1NM E13NE 20080710 NM 2008 7 10 DL76L080748 1 20080418 A 3397 CONNECTOR BOEING 767 767332 1382001 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 EEL SEAT FEEDER AT STA 434 RIGHT MISSING MOLEX CONNECTOR. EMERGENCY LIGHT SEAT FEEDER CONNECTOR WAS REMOVED AND REPLACE D, OPS CHECKS GOOD IAW B767-300 MM 33-51-10. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 DL76L080749 1 20080418 A 3397 CONNECTOR BOEING 767 767332 1382001 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 EEL SEAT FEEDER AT STA 550 RIGHT MISSING MOLEX CONNECTOR. REMOVED AND REPLACED MOLEX CONNECTOR AT STA 550 RIGHT, OPS CH ECKS GOOD IAW B767-300 MM 33-51-10. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 DL76L080751 1 20080505 A 3597 CONNECTOR BOEING 767 767332 1382001 NM PSU BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 SEAT 41FG O2 CONNECTOR BROKEN. RE-TERMINATED IAW B767 WIRING DIAGRAM 35-21-13 AND BSWPM 20-10-13. OPS CHECK DONE ON OP N 6841. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 DL76L080754 1 20080507 A 3350 RECEPTACLE BOEING 767 767332 1382001 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 EEL RECEPTACLES ON SEATS 1A/B AND 1E/F ARE DAMAGED. REPLACED RECEPTACLES ON SEAT 1A/B AND 1E/F IAW DAL B767 SWPM 20-64- 17. OPS CHECKED GOOD IAW DAL B767 MM 33-51-00-715-200. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 DL76L080760 1 20080421 A 3397 CONNECTOR BOEING 767 767332 1382001 NM CABIN BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 EMERGENCY SEAT LIGHT CONNECTOR BROKEN AT SEAT 31 LEFT. REPLACED CONNECTOR AT SEAT 31 L IAW DAL B767 SWPM 20-64-17. OPS CHECKS GOOD IAW B767-300 MM 33-51-00. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 DL76L080761 1 20080421 A 3397 CONNECTOR BOEING 767 767332 1382001 NM CABIN BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 EMERGENCY SEAT LIGHT CONNECTION BROKEN AT SEAT 41 LT. REPLACED CONNECTOR IAW DAL B767 SWPM 20-64-17. OPS CHECKED GOOD IAW DAL B767 MM 33-51-00. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 DLM88080762 1 20080510 A 2432 203BC1021 CHARGER DOUG MD88 MD88 3023688 NM E&E BAY FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 976DL 53257 BATTERY CHARGER FAILED - UPON SHOP EXAMINATION, FOUND C9 DAMAGED BY HEAT FROM R6. NOTE: THIS CHARGER HAS HAD SB 203BC1 02-24-06 COMPLIED WITH (MOVED R6 TO BASE OF C9 ASSEMBLY). THE DAMAGE TO C9 APPEARED TO BE ALMOST TO THE POINT OF CAUSIN G C9 TO IGNITE AND CAUSE A BATTERY CHARGER FIRE. 2 L 7 2 4F RT A6WE 20080710 EU 2008 7 10 USAA920081096 1 20080430 A 5315 D53472094008 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650AW 856 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN BEAM, BS 2786 / FR 66, +Y510. REPAIRED CABIN BEAM, BS 2786 / FR 66, +Y510 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20080710 EU 2008 7 10 USAA920081097 1 20080430 A 5320 D53480043204 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650AW 856 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON L2 DOOR CUTOUT LOWER SILL, BS 2786 / FR 66 - BS 2884 / FR 68, +Y1430. REPA IRED L2 DOOR CUTOUT LOWER SILL, BS 2786 / FR 66 - BS 2884 / FR 68, +Y1430 IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 20080710 NM 2008 7 10 AALA200801118 1 20080427 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 794AN 30256 JFK - EMERGENCY LIGHTS IN COACH CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN COACH CABIN. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080710 GL 2008 7 10 3657 1 20080522 A 2434 645843 ALTERNATOR CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO HARTZL HCJ3Y PHCJ3YF1 GL ENGINE FAILED E J4PA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 13 134AJ 1511 917726 FP3800R AIRCRAFT DEPARTED KCLT AT 0825 FOR DESTINATION KJAX. DURING CRUISE, ALTERNATOR 1 ANNUNCIATOR LIGHT ILLUMINATED INDICATI NG A FAILURE. THE PILOT DIVERTED TO KGMU WITH AN UNEVENTFUL LANDING. THE ALT 1 FIELD WIRE WAS FOUND TO BE BROKEN. FIE LD WIRE WAS REPAIRED BY SATSAIR MAINTENANCE AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 1 3O 3 O NT A00009CH E3SO 5 C P36EA 20080710 2008 7 10 SA08037 4 20080523 A 2565 SLIDE AIRBUS A319 A319112 3930323 EU CABIN LOW PRESSURE A USAA K NONE J WARNING INDICATION NR NOT REPORTED 1 EA 19 766US 1378 CLT - FLIGHT 1684, CLT-PHL, CAUTION LIGHT ILLUMINATED ON CIDS PANEL. MAINTENANCE REPORTED THE SLIDE EMER R PRESSURE LOW , SERVICED TO GREEN BAND. CIDS CAUTION OUT, OK FOR FLIGHT. 2 L 7 2 4F RT A28NM 20080710 NM 2008 7 10 R61A200800006 1 20080513 A 3240 142071141 CONTROL MODULE EMB ERJ170 ERJ170200LR 3260121 NM FAULTY A R61A K NONE J WARNING INDICATION DE DESCENT 1 GL 11 127HQ 208 17000206 RIGHT AND LEFT HAND FAULT MESSAGE ON ECAS. MADE NORMAL LANDING TAXI TO THE GATE NO PROBLEMS. 2 L 7 2 4F RT A56NM 20080710 NM 2008 7 10 2008UALA02834 1 20080515 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 539UA 25223 EEL INOP ON EXTERIOR OF DOOR 2 LEFT. BULB IN EEL ASSY INOP. RELAMPED EEL ASSY, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080710 NM 2008 7 10 2008UALA02931 1 20080520 A 3350 58674 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 348UA 24252 EMERGENCY FLOOR EEL LIGHTS INOP FROM SEAT 15ABC TO AFT LEFT GALLEY. AFTER EXTENSIVE TROUBLE SHOOTING FOUND POWER INVERT ER TO BE FAULTY. REPLACED POWER INVERTER OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080710 NM 2008 7 10 2008UALA02933 1 20080521 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 5E FWD LIGHT ASSY. REPLACED LIGHT ASSY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080710 NM 2008 7 10 2008UALA02938 1 20080521 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EXIT EEL LIGHT INOP AT SEAT ROW 55 LEFT. REPLACED LIGHT ASSY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080710 NM 2008 7 10 R61A200800009 1 20080513 A 2797 WIRE HARNESS EMB ERJ170 ERJ170200LR 3260121 NM L/E SLAT DEFECTIVE A R61A O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 101HQ 17000156 CREW REPORTED SLAT FAIL MESSAGE ON APPROACH. CREW FOLLOWED QRH PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE TRO UBLESHOT AND FOUND SLAT 3/4 HARNESS TO BE BAD. REMOVED AND REPLACED SLAT SKEW SENSOR WIRING HARNESS OPERATIONAL CHECK G OOD. 2 L 7 2 4F RT A56NM 20080710 EU 2008 7 10 UPS08152281 1 20080516 A 5230 SEAL AIRBUS A300 A300F4622R 3930360 EU FWD CARGO DOOR DAMAGED A IPXA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 SO 01 128UP 0812 INSPECTION TYPE:N/A DIVERSION - DIVERTED TO OMA FOR AN UNIDENTIFIED AIRFRAME VIBRATION AND AUDIBLE HUM. THE VIBRATION B EGAN CHANGING AND CAUSED CONCERN SO THE CREW DIVERTED. ACCOMPLISHED SPLICE REPAIR REF 52-30-18-08 OF FWD CARGO AFT DOOR SEAL. CURE CHECK AND LEAK CHECKS PER MM 52-39-18 AND 05-53-00-00. NO LEAKS. OK TO CONTINUE. 2 L 7 2 4F RT A35EU 20080603 EA 2008 6 3 SWIA200819648 1 20080319 A 7120 BEARING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT ENGINE YOKE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 952SW 7805 LEFT ENGINE YOKE LINK BEARING IS CORRODED, FOUND AT C-CHECK. REPLACED LINK ASSEMBLY PER CRJ200 AMM TASK 71-21-01-420-00 1 SECTION A. 2 L 7 2 4F 4 F RT A21EA E15NE 20080603 EU 2008 6 3 TRBA2008053 1 20080515 A 3350 3071BPEGPC LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 LOWER LEFT EMERGENCY LIGHT BY THE MAIN PAX DOOR HAS TWO BULBS INOPERATIVE. REMOVED AND REPLACED BULBS AND PERFORMED OPT CK IAW JIC NR 33-50-00. 2 H 7 2 4T RT A53EU 20080603 NM 2008 6 3 USAA920081073 1 20080418 A 5320 143N8333 INTERCOSTAL BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - CRACKED INTERCOSTAL AT THE L2 DOOR CUTOUT, BS 660, S11L. REPAIRED INTERCOSTAL AT THE L 2 DOOR CUTOUT, BS 660, S11L IAW USAIRWAYS TASK CARD M1C53604. 2 L 7 2 4F RT A2NM 20080603 NM 2008 6 3 ASAA0872958 1 20080426 A 5320 141A85123 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 611AS 29753 GOUGES FOUND AT THE INTERCOSTAL WEB AT THE E&E COMPARTMENT DOOR CUTOUT AT BS 338 AND RBL 11. REPLACED WITH FABBED REPAI R PART IAW B737 700 SRM. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 ASAA0872963 1 20080430 A 5320 141A512010 WEB BOEING 737 737790 13844CN NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 611AS 29753 GOUGES FOUND AT FLIGHT DECK FLOOR WEB AT BS 254 AND RBL 3 TO LBL 8. GOUGES REPAIRED IAW B737 700 SRM 53 10 51. 2 L 7 2 4F RT A16WE 20080603 NE 2008 6 3 EIA2008019 2 20080423 A 7200 ENGINE BOEING 747 747132 1384882 NM PWA JT9 JT9D7F 52054 NE NR 3 FAILED A EIAA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 NM 09 481EV 19896 662349 NUMBER 3 ENGINE FAILED AT 35,000 FEET DESCENT TO FL 32.0 NORMAL INFLIGHT RESTART ALL ENGINE PARAMETERS WERE NORMAL. PER FORMED ENG WINDMILL INSPECTION PER B747MM 72-00-00 CONFIG 1 PAGE 684(O), NO DEFECTS NOTED. PERFORMED ENGINE IDLE GROUND RUN PER B747 MM 71-00-00 PAGE 518 TEST NR 3 OPS CHECKED NORMAL. INSPECTED EVC PRESSURE FILTER PER B747 MM 73-21-07 PAG E 401. NO DEFECTS NOTED. 2 L 7 4 4F 4 F RT A20WE E20EA 20080603 NM 2008 6 3 QXEA200800473 1 20080509 A 5320 FLOOR SUPPORT BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 425QX 4039 PDX - C4 CHECK. LEFT OUTBOARD FLOOR SUPPORT HAS LIGHT CORROSION AROUND NUTPLATE HOLES X-9. REMOVED CORROSION. .003 INC H REMOVED WITHIN LIMITS. PRIMED AND TREATED AREA AND INSTALLED NUTPLATES. 2 H 7 2 4T RT A13NM 20080702 NM 2008 7 2 SWAA083376 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083388 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 EU 2008 7 2 USAA920081198 1 20080610 A 5540 D5537131800200 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 640AW 448 C3-CHECK, NR 6105675, NR 3 RUDDER HINGE FITTING HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 2279/ RIB 5. REPLACED NR 3 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 2279/ RIB 5 IAW AMM 55-36-41. 2 L 7 2 4F RT A28NM 20080702 NM 2008 7 2 2008UALA03570 1 20080624 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY LIGHT ON MID GALLEY FWD WALL INOP. FOUND LIGHT ASSEMBLY FAULTY. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03540 1 20080621 A 3350 80541 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT INOP, FWD GALLEY RT WALL. SECURED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03538 1 20080621 A 3350 362624 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT INOP, SEAT 48 LT. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD.AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03514 1 20080621 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LEFT MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 779UA 26941 ELEC GEN DRIVE L LEFT IDG FAULT (LOW INTERNAL OIL PRESSURE). REPLACED IDG PER MM 24-11- 01 OPS AND LEAK CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080702 NM 2008 7 2 CALA0800613 1 20080619 A 5315 143N54321 FLOORBEAM BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14118 27560 FLOORBEAM AT STATION 698 HAS CORROSION AROUND FASTENER HOLE. REMOVED CORRODED FLOOR, SUPPORT FITTING, FABRICATED AND IN STALLED NEW FITTING REF GMM 10-900-01, SRM 51-40-02 AND BOEING DRAWING 143N5432-1. 2 L 7 2 4F RT A2NM 20080702 NM 2008 7 2 CALA0800582 1 20080610 A 5511 186A2000678 RIB BOEING 737 737724 13844BY NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 RIGHT-HAND HORIZONTAL STABILIZER OUTBOARD CLOSURE RIB HAS SURFACE CORROSION AT SCREW HOLES - 3 EA AT UPPER SURFACE AND 2 EA AT LOWER SURFACE AREA. BLENDED OUT ALL CORROSION, PERFORMED HFEC OF BLENDED AREAS AND REFINISHED PER ECRA 5510-0193 3 MIN REMAINING THICKNESS IS .060 INCH. 2 L 7 2 4F RT A16WE 20080702 2008 7 2 SWAA083445 4 20080620 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 200WN 32482 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080702 2008 7 2 SWAA083061 4 20080608 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 223WN 32492 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083066 1 20080608 A 3350 417A5600 LIGHT BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 245WN 32506 FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT ASSY MISSING. INSTALLED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082810 1 20080524 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 6 ABC. REMOVED AND REPLACED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082849 1 20080526 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080707 WP 2008 7 7 UPS08852251 1 20080422 A 5320 5773846107 SUPPORT DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 MAIN CABIN SURFACE CORROSION ON VERTICAL FLOORBEAM SUPPORT (AFT SIDE) STA 1746 AT C/L. REPAIRED VERT ICAL FLOORBEAM SUPPORT AT STA 1746 AND BL-0 BY FABRICATION AND REPLACEMENT IAW SRM 51-01-21, DWG 5773846 AND SRM 51-01-2 0D. 2 L 7 4 4F RT 4A25 20080707 WP 2008 7 7 UPS08852270 1 20080420 A 5244 DOOR DOUG DC8 DC873F 302199F WP ACCESSORY BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 AFT ACCESSORY COMPT DOOR (STA 1540) HAS CRACK ON CENTER AREA. REPAIRED AFT ACC COMPT DOOR IAW EO DC8 -5350-7876-A. 2 L 7 4 4F RT 4A25 20080707 NM 2008 7 7 2008UALA02785 1 20080514 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 1J AFT LIGHT ASSY. REPLACED LIGHT ASSY. OP CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 2008 7 7 2008UALA02792 4 20080514 A 2565 680149916 O-RING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 653UA PA2694 25391 LOW BOTTLE PRESSURE. BOTTLE TO VALVE O-RING LEAKING. REPLACED O-RING. 2 L 7 2 4F 4 F RT A1NM E24NE 20080707 NM 2008 7 7 2008UALA02807 1 20080515 A 3350 20131A CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 LEFT OVERWING FWD TWO EMERGENCY LIGHT IS INOP. REPLACED EMERGENCY LIGHT BATTERY CHARGER. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 USAA920081078 1 20080514 A 2560 P4010021 BATTERY BOEING 767 7672B7ER 1385107 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 251AY 24764 MIA - EEL - C4 CHECK - FORWARD FLIGHT ATTENDANT POSITION 1 FLASHLIGHT BATTERY WEAK. REPLACED FORWARD FLIGHT ATTENDANT P OSITION 1 FLASHLIGHT BATTERY IAW B767 AMM 25-60-00. 2 L 7 2 4F RT A1NM 20080529 NM 2008 5 29 08FDEA01995 1 20080527 A 5347 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 MAIN CABIN SEAT TRACK CORRODED STA 1148 - 1170, RBL 45 WL 208 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, ORIGINAL THI CKNESS .070 INCH, MATERIAL LOSS OF .030", REMAINING MATERIAL .040". REMOVED SEAT TRACK, REF SRM 53-10-1 PAGE 16 DET 5 . SEAT TRACK FABRICATED ON N/R N00584. TREATED AND PRIMED REF SRM 51-10-2 PG 1. INSTALLED SEAT TRACK REF SRM 51-30-2 PG 1-10. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 WP 2008 5 29 08FDEA02013 1 20080528 A 5230 NFA6066575 SKIN DOUG DC10 DC1010 3022110 WP ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 40061 46973 CENTER CARGO DOOR FOUND CRACK ON LOWER FWD SIDE EXT SKIN DOOR. REPAIRED SKIN IAW SRM 52-10-00 FIG 17 VOL I. 2 L 7 3 4F A22WE 20080529 EA 2008 5 29 HNAA0800150 1 20080513 A 6123 M390166105L RELAY DHAV DHC8 DHC8311 1386006 EA PROPELLER FAILED A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 330EN 33908 274 AUTO FX WOULD NOT ARM DURING TAKEOFF. 2 H 7 2 4T RT A13NM 20080529 2008 5 29 HNAA0800153 4 20080509 A 3420 7001182913 ADI DHAV DHC8 DHC8102 2809003 NM COCKPIT FALSE INDICATION A HNAA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 EA 07 846EX 43282 307 326 CAPT'S ADI DURING CLIMB TWITCHED OFF AND ON WITH ROLL MISMATCH AND ATT FLAG. AFTER LEVELING OFF, ADI INDICATED 15 DEG L EFT AND 2 DEG NOSE DOWN. 2 H 7 2 4T RT A13NM 20080529 SO 2008 5 29 C2XA08RI064 1 20080509 A 2611 LIGHT EMB 145 EMB145LR 3260212 SO SMOKE DETECTOR INOPERATIVE A C2XA O OTHER L NO TEST TX TAXI/GRND HDL 1 SW 27 13956 145078 FLIGHT 3098 - EWR - FLIGHT CREW REPORTED BAG SMOKE DETECT TEST LIGHT WAS INOPERATIVE. EWR MX RESET THE SYSTEM AND PERFO RMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20080529 NM 2008 5 29 08FDEA01950 1 20080522 A 5280 65175631 DOOR BOEING 727 727233 138408A NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 NOSE LANDING GEAR LEFT DOOR, CRACK AT AFT END EDGE SKIN AT B-STOP ANGLE SUPPORT REMOVED DAMAGE, NDT FOR CRACKS REMOVAL, FABRICATED FILLER AND DOUBLER REPAIR PARTS. INSTALLED FILLER AND DOUBLER REF SRM 51-30-2 PG 1, SRM 51-40-3 PG 1-3, SRM 52-80-1 ITEM 3, SRM 51-10-2, PG 7-15. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 NE 2008 5 29 HALA0800578 2 20080514 A 7230 BLADES BOEING 767 76733A 1385209 NM PWA 4060 PW4060 52119 NE LT COMPRESSOR DAMAGED A HALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 WP 13 591HA 33423 OPEN - ATB: FL 350 SMOOTH AIR L ENGINE EXPERIENCED LOUD BANG, MODERATE VIBRATION AND LOUD GRINDING SOUNDS. SHUT DOWN EN GINE AND RETURNED TO OGG. INITIAL FINDINGS DURING LT ENG HPC BORESCOPE. FOUND 5TH AND 6TH STAGE COMPRESSOR BLADES AND STATOR DAMAGED. ENGINE CHANGE IN WORK. 2 L 7 2 4F 4 F RT A1NM E24NE 20080529 WP 2008 5 29 08FDEA02018 1 20080528 A 5310 AEA01121 DOOR FRAME DOUG DC10 DC1010F 3022111 WP ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 68059 46907 DURING REPAIR ASSESSMENT WAS FOUND AN EXISTING REPAIR AT CTR CARGO FUSELAGE DOOR JAMB REPAIR HAS BEEN REPLACED BECAUSE I T FOUND NOT IN CONFORMITY WITH APPROVED DATA. 2 L 7 3 4F A22WE 20080529 NM 2008 5 29 CALA0800459 1 20080514 A 5311 6573743 FRAME BOEING 737 737524 1384721 NM BS 616 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 LAST FASTENER IN FRAME AT STA 616 LBL 64 IN MID-CABIN IS CRACKED. FABRICATED REPAIR PARTS SENT OUT FOR CAD PLATING TRIM MED AND INSTALLED REPAIR PER ECRA 5311-01158. 2 L 7 2 4F RT A16WE 20080529 NM 2008 5 29 CALA0800475 1 20080520 A 5311 BAC15171472 FRAME BOEING 737 737524 1384721 NM BS 787 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17640 28901 FRAME CRACKED AT STATION 787 BETWEEN S8L AND S9L. CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLES AND INSTALLED PER EA53 10-04498. 2 L 7 2 4F RT A16WE 20080530 EU 2008 5 30 YENA2008050 1 20080525 A 3150 CONTROLLER AIRBUS 320 A320232 3930326 EU A/C PACK MALFUNCTIONED A YENA B EMER. DESCENT B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 15 524JB 27923 1528 INFLIGHT ECAM "FWS SDAC 2 FAULT" FOLLOWED BY STRONG ELECTRICAL TYPE ODOR IN THE COCKPIT. REMOVED & REPLACED NR 2 SDAC & OPS OK PER MM 31-55-34. CIRCUIT BREAKERS Y18 AND Y19 TRIPPED IN FLT. PACK NR 1 INDICATION LOST DESCENDED TO FL 300. REMOVED & REPLACED NR 1 PACK CONTROLLER & OPS OK PER MM 21-61-34. PERFORMED TSM TASKS 24-00-00-810-823 & 24-00-00-810-8 03, FOUND SMELL FROM SDAC NR 2 AND PACK CONT NR 1 CAUSING FAULTS & ODOR, REMOVED AND REPLACED SDAC NR 2 & PACK CONT NR 1 . SEE SDR YENA2008051 FOR NR 1 PACK CONTROLLER REPLACEMENT. 2 L 7 2 4F RT A28NM 20080530 NM 2008 5 30 CALA0800490 1 20080528 A 3233 65448105 ACTUATOR BOEING 737 7373T0 1384582 NM MLG MALFUNCTIONED A CALA O OTHER O OTHER AP APPROACH 1 SW 27 18350 51755 35304 23588 RIGHT-HAND MAIN GEAR INDICATION DID NOT INDICATE GREEN WITH LANDING GEAR HANDLE DOWN. COMPLIED WITH MANUAL EXTENSION AN D INDICATION WAS NORMAL. RIGHT-HAND MAIN GEAR HANGING UP DURING MAINTENANCE SWING REF NR 4263137 FOR UPLOCK ACTUATOR RE MOVE AND REPLACE AND NR 4263138 FOR LEAK AND OPS CHECK. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800482 1 20080520 A 5312 0502024T42 BULKHEAD BOEING 737 7373T0 1384582 NM MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 39343 23581 LEFT-HAND MLG WHEEL WELL PRESSURE DECK CRACKED AT UPPER FWD SKIN LOCATED APPROXIMATELY LBL 40. REPAIRED IAW SRM 53-60-5 1 REPAIR 4. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800483 1 20080521 A 5330 6545769 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 CRACK AT AFT END OF E&E COOLING EXHAUST PORT AT CENTER OF FUSELAGE. INSTALLED REPAIR PER EC/RA 5330-03806, STEPS 1-19. PLACED ON DIP FOR PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 12 MONTHS. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800484 1 20080522 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM BS 360 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17640 28901 FRAME CRACKED STATION 360 ABOVE S9L. REPAIRED FRAME AT STATION 360 S9L PER ECRA 5310-04775. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800502 1 20080528 A 5311 6546596 FRAME BOEING 737 737524 1384721 NM BS 727B S8L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 LEFT-HAND STATION 727B AT S8L AIR CONDITIONING (A/C) BRACKET MOUNT HOLE CRACKED. REPAIRED CRACKED FRAME AT LEFT-HAND ST ATION 727B S8L PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800485 1 20080503 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM BS 827 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17640 28901 FUSELAGE FRAME IS CRACKED AT STATION 827 BETWEEN S8R AND S9R. INSTALLED FRAME REPAIR PER ECRA 5310-04774. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 YENA2008052 1 20080523 A 3350 340022 POWER SUPPLY EMB ERJ190 ERJ190100IGW 3260408 NM EMERGENCY LIGHTS FAILED A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 187JB 6935 6935 19000009 FWD DOOR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT, OPS TEST GOOD IAW AMM 33-50-01. 2 L 7 2 4F RT A57NM 20080530 EU 2008 5 30 YENA2008047 1 20080511 A 3610 VALVE AIRBUS 320 A320232 3930326 EU BLEED AIR LEAKING A YENA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 546JB 1827 FLT NR 303, IAD-FLL, AIR ENG 1 BLEED ABNORMAL PRESSURE (SUBSEQUENT PACK 1/PACK 2-FAULT). FOUND AIR LEAK ON PRESSURE REG VALVE CLAMP JOINT. CLAMP WAS REMOVED AND JOINT RE-ALIGNED WITH VALVE. NO FURTHER AIR LEAK NOTED FAN AIR VALVE THERMOS TAT SEAL WAS REPLACED TO CORRECT AIR LEAKAGE AS PER AMM REF 36-11-43. NO FURTHER LEAKS NOTED. POWER ASSURANCE TEST ACC OMPLISHED AT 1.25 EPR. ENG NR 1 & 2 BLEED AND NACELLE TEMP PARAMETERS EXAMINED. NO DEFECTS NOTED. PARAMETERS WITHIN L IMITS. BLEED SYS 1 & 2 CHECKED BY ALTERNATE SYSTEMS. BLEED NR 1 NR 2 SYSTEMS OPERATE AS DESIGNED PER AMM REF 71-00-00- 710-013A & REF 36-11-00-710-001. 2 L 7 2 4F RT A28NM 20080530 EU 2008 5 30 YENA2008048 1 20080519 A 3231 114079016 SELECTOR VALVE AIRBUS 320 A320232 3930326 EU MLG DOOR MALFUNCTIONED A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 505JB 20210 805 1173 FLT 119, JFK-MSY, UPON LANDING GEAR RETRACTION, RECEIVED "L/G DOORS NOT CLOSED" ECAM. LANDING GEAR WHEELS IND NORMAL, B UT GEAR DOOR IND OPEN. DID NOT CLEAR UPON RECYCLE. RETURNED TO DEPARTURE AIRFIELD. REMOVED AND REPLACED L/G DOOR SELE CTOR VALVE (41GA) IAW AMM 32-31-34, OPS CHECK OK, LEAK CHECK OK. 2 L 7 2 4F RT A28NM 20080530 NM 2008 5 30 HALA0800589 1 20080516 A 5730 PANEL BOEING 767 76733A 1385209 NM RT WING LOOSE A HALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 13 581HA 28141 ATB - ON CLIMB APPROX 16,000, A BANG SOUND WAS HEARD AND A/C AIRFRAME VIBRATION OCCURRED. SLOWED A/C FROM 330 KTS TO 27 0 KTS VIB DECREASED. ALL OTHER INDICATIONS NORMAL. RETURNED TO SEA. REDUCED SPEED TO 250 KTS IN DESCENT. F/A CONFIRM ED BANG AND VIBRATION FROM MID-GALLEY. PERFORMED AIRFRAME VIBRATION CONDITIONAL INSPECTION AND FOUND 9 RIVET HEADS BROK EN ON RT WING UPPER PANEL T/E, JUST FWD OF O/B AILERON. INSTALLED 7 OF 9 WITH STEEL SCREWS FOR SECURITY. FERRY FLIGHT REQUIRED. THIS ACFT HAS BEEN INSPECTED THIS DATE AND IS SAFE FOR THE INTENDED FLIGHT. RT WING FIXED UPPER SURFACE PANE L RIVETS SHEARED(9). REMOVED AND REPLACED SHEARED RIVETS ON RT WING FIXED T/E UPPER SURFACE PANEL IAW 51-40-04-OG-0. R 2 L 7 2 4F RT A1NM 20080530 NM 2008 5 30 HALA0800594 1 20080508 A 5710 STRUCTURE BOEING 767 7673CB 1385187 NM LT WING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 590HA 33467 LT WING HAS CRACKED STRUCTURE ON FIXED L/E ABOVE FUELING PANEL. REPAIRED PER SRM 57-41-13 FIG 201 REPAIR 3. 2 L 7 2 4F RT A1NM 20080530 NE 2008 5 30 HALA0800596 2 20080519 A 7320 EEC BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE RT ENGINE INOPERATIVE A HALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 13 596HA 23276 ETOPS SIGNIFICANT SYSTEM, RT ENGINE HAD A 945 EGT EXCEEDENCE FOR 8 SECONDS. EGT OVERTEMP CAUSED BY OPERATION WITH EEC I NOP/OFF. REF DMI NR 78256 PERFORMED INSP PER MM 71-00-00. NO FAULTS NOTED A/C OK FOR CONTINUED SERVICE. 2 L 7 2 4F 4 F RT A1NM E13NE 20080530 NM 2008 5 30 HALA0800588 1 20080519 A 3610 BLEED AIR SYS BOEING 717 717200 1383700 NM RIGHT WARNING LIGHT A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 479HA 55124 ATB - RT AIR SYS FAULT DURING CLIMB AND INTERMITTENT LT AIR SYS PRESSURE LOW. REPAIR IN WORK. 2 L 7 2 4F TR A6WE 20080530 NM 2008 5 30 HALA0800599 1 20080522 A 2600 285T003511 WARN PANEL BOEING 767 767332 1382001 NM COCKPIT MALFUNCTIONED A HALA O OTHER N FALSE WARNING CR CRUISE 1 WP 13 596HA 23278 ETOPS SIGNIFICANT SYSTEM - "WARN ELEX" ANNUNCIATED ON STATUS PAGE. REMOVED AND REPLACED WARN ELEX OPS CHECK GOOD, IAW R EF AMM31-51-04. 2 L 7 2 4F RT A1NM 20080528 NE 2008 5 28 NSVA2008026 2 20080515 A 7200 CT79B ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT OVERTEMP A NSVA E ENGINE SHUTDOWN M R J OVER TEMP PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 27 356CJ 340B356 DURING CLIMB AT APPROX 1000 FT, LT ENGINE MADE POPPING NOISES, CHECKED GAUGES SHOWED NO LEFT SIDE TORQUE, NP, OR OIL PRE SSURE. NG WAS WITHIN GREEN ARC AND NORMAL. NEITHER LEFT SIDE BLEED WAS ON CTOT AND AOR WERE OFF. BEFORE REDUCING POWE R ON PLS IS WHEN POPPING BEGAN ITT SHOWED 1010 WHEN SEEN, AND ACCOMPLISHED SHUTDOWN. PERFORMED DFDR DOWNLOAD TO DETERMI NE TEMPERATURE EXCEEDANCE AND THRESHOLD. FDR CONFIRMED OVERTEMP EVENT REQUIRES ENGINE REPLACEMENT. 2 L 7 2 4T 4 T RT A52EU E8NE 20080528 NM 2008 5 28 KNNA20080014 1 20080515 A 5347 SEAT TRACK BOEING 737 7372L9 1384497 NM BS 270-294 CORRODED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 464AT 21278 REMOVED GALLEY AND THEN FOUND CORROSION ON UPPER SURFACE OF SEAT TRACK AT STA 270 TO STA 294 AND RBL 16. REMOVED SECTIO N OF SEAT AND REPLACED WITH NEW SECTION. 2 L 7 2 4F RT A16WE 20080528 WP 2008 5 28 NWAA082269926 1 20080516 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 926NW 47425 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 10-21 OF THE CABIN WERE INOPERATIVE. M AINTENANCE REPLACED THE BATTERIES. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F A6WE 20080528 NM 2008 5 28 NWAA082315533 1 20080516 A 5330 SKIN BOEING 757 757251 1384970 NM BS 630 S24-25R DENTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 533US 24264 DURING "L" CHECK, FOUND DENT AND GOUGE IN FUSELAGE SKIN AT BS 630 BETWEEN S24R TO S25R. REPAIRED PER EA 55-212820 SECTI ON I, SECTION II REQUIRES FOLLOW UP INSPECTIONS BEGINNING NO LATER THAN 37,500 TOTAL AIRCRAFT FLIGHT CYCLES. SECTION II I REQUIRES REPEAT INSPECTIONS AT 6000 CYCLES INTERVALS AFTER SECTION II ACCOMPLISHMENT. 2 L 7 2 4F RT A2NM 20080528 WP 2008 5 28 IXXA08SMN097S 1 20080314 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1660 L19L MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 602AL 99983 2870 45991 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT AFT FUSELAGE L-2 DOOR AFT EDGE HAS IMPROPER REPAIR AT FS-1660 LONGERON 19. 5. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRAC K, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REP AIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW AD 2000-20-08, S/B DC8-53-075, DRAWING DOUGLAS SR08530021, 5750 776, BOEING MESSAGE 1-792473688-12 DATED 04/23/08, BOEING SKETCH 1-792473688-9, SEMAN DRAWING ED-4737 DATED 04/18/08, DC 8 SRM 51-1-21, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 53-2-0 FIGURE 18, DC8 SRM 51-1-8B, 51-1-11, 51-1-21, AND 51-3-1. 2 L 7 4 4F RT 4A25 20080528 SO 2008 5 28 LR7A08076 1 20080513 A 5230 STRIKER LKHEED 382 382G 526414U SO CARGO DOOR CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 403LC 2602 4590 DURING SCHEDULED C-8 CHECK PER JOB CARD HC5211, FOUND RAMP DOOR FWD LEADING EDGE SEAL STRIKER EXFOLIATION CORROSION RS0, LBL50 TO RBL50. REPAIR ACCOMPLISHED BY FABRICATING AND REPLACING STRIKER IAW LAC MEA 382-52-08-034 AND DWG 353607. 2 H 7 4 4T A1SO 20080528 NM 2008 5 28 08FDEA01860 1 20080516 A 5330 6554583157 SKIN BOEING 727 727233 138408A NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 274FE 22039 EXISTING DOUBLER REPAIR TO THE FUSELAGE SKIN AT BS 1140 AND STR 20L DOES NOT CONFORM TO FAA APPROVED DATA. REMOVED PREV IOUS REPAIR IAW SRM 51-30-2, FABRICATED NEW DOUBLER. INSTALLED NEW REPAIR DOUBLER IAW SRM 53-30-2 FIG 3 AND SRM 53-30-3 FIG 14 AND SRM 51-30-2. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01869 1 20080516 A 5730 ARB2886503 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 LT WING LEADING EDGE TELESCOPIC DUCT CUT OUT OUTBOARD UPPER CORNER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 43 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA01879 1 20080519 A 5730 ARB74023 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 590FE 48505 FOURTEEN FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND STA XORS 700. REPAIR CARRIED OUT AS EA 1-5710-122451, REPAIR CLASSIFIED AS MINOR AS PER FED EX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA02011 1 20080528 A 5730 ARB2886504 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 529FE 48624 RT WING LEADING EDGE ANTI-ICE TELESCOPIC DUCT CUT-OUT TOP INBOARD AND OUTBOARD CORNER FOUND CRACKED. REPAIR CARRIED O UT AS PER SRM 57-10-00, REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 HNAA0800156 1 20080509 A 7120 87110047001 MOUNT DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE WORN A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 825EX 7311 388 NR 1 INBOARD AFT VERTICAL MOUNT STRUT BEARING WORN. INSP GENERATED BY RII CARD 71-20-03. 2 H 7 2 4T RT A13NM 20080529 SO 2008 5 29 C2XA08SH075 1 20080514 A 5210 14533996401 SUPPORT EMB 145 EMB145LR 3260212 SO DOOR HANDLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13968 145138 SHV - DURING C-CHECK PAX DOOR INTERNAL HANDLE SUPPORT CRACKED. MX REMOVED AND REPLACED PAX DOOR INTERNAL HANDLE SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 20080529 NM 2008 5 29 08FDEA01959 1 20080522 A 5330 2024T30063 SKIN BOEING 757 75723A 1384967 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 EXTERNAL SMALL HOLE FLUSH REPAIR AT FUSELAGE BS740, S-18L, TO BE EVALUATED. EXISTING REPAIR EVALUATED AS PER EO F-5100- 7-5001 PT1 ATTACHMENT B AND FOUND TO BE PREVIOUSLY ACCOMPLISHED IAW B757-200 SRM 53-00-01 FIG 208. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080529 WP 2008 5 29 08FDEA01934 1 20080521 A 5730 ARB087241 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 567FE 46994 LEFT WING FUEL TANK PLATE/PANEL 535 AT, INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION, NICKS, GOUGES AND TWO FASTENER HOLES. REMOVED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00, VOL I, PG 217. MACHINED A NEW PANEL IAW DAC DWG ARB0872, REV "AV". APPLIED ALODINE, PRIMER AND PAINT IAW DAC DWG ARB0872, REV "AV" AND DC/MD-10 SRM 51-21-01, VOL II. PART MARKED IAW FEDEX GMM 7-0-1001. FPI IAW DPS 4.707AND DAC DWG ARB0872, REV "AV", NO CRACKS NOTED. 2 L 7 3 4F RT A22WE 20080530 NM 2008 5 30 CALA0800492 1 20080510 A 5230 146A61101 SKIN BOEING 737 737824 13844BZ NM AFT CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24212 28772 AFT CARGO DOOR STATION 837 AT LOWER INNER SKIN HAS CORROSION. REPAIRED NOTED DAMAGED AREA IAW EC/RA 5232-01101. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800495 1 20080528 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 787 S8R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 RIGHT-HAND STATION 787 AT S8R AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED CRACKED FRAME RIGHT-H AND STATION 787 S8R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 YENA2008049 1 20080520 A 2913 5116404 PUMP EMB ERJ190 ERJ190100IGW 3260408 NM HYD SYSTEM LEAKING A YENA O OTHER K FLUID LOSS AP APPROACH 1 EA 15 190JB 5146 689 19000011 FLT 907, JFK-ORD, COMPLETE LOSS OF HYDRAULICS SYSTEM NR 2. ACCOMPLISHED MANUAL GEAR EXTENSION PER QRH. FOUND NR 2 EDP LEAKING. REMOVED AND REPLACED NR 2 EDP IAW AMM 29-11-01, OPS CHECK AND LEAK CHECK GOOD. SERVICED HYD RESERVOIR IAW AMM 12-12-01. CHECK OK. 2 L 7 2 4F RT A57NM 20080530 NM 2008 5 30 HALA0800605 1 20080523 A 2131 211738815 CONTROLLER BOEING 767 7673G5 1385126 NM CABIN PRESSURE FAILED A HALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEMS, CABIN PRESSURE CONTROLLER 1 AND 2 UNABLE TO DESCEND CABIN AT IDLE THRUST IN DESCENT. PERFORM ED FIM 21-33-00. REMOVED AND REPLACED CABIN PRESS GAUGE PWR PER AMM 21-33-01/401. PRECAUTIONARY REPLACED NR 2 AUTO PRE SS CONTROLLER PER AMM 21-31-02-404-005 (FAILED LAMP TEST). BITE CHECK GOOD PN 2117388-15 SN ON 18-1326 OFF 27-1101. BIT E CHECK BOTH SYSTEMS NO FAULTS NOTED, OK FOR SERVICE, PN SET LOC40M SN ON 1255DAE OFF 209E 2 L 7 2 4F RT A1NM 20080530 NM 2008 5 30 HALA0800604 1 20080527 A 5751 SKIN BOEING 767 7673G5 1385126 NM RT AILERON DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 586HA 24259 RT UPPER OUTBOARD AILERON UPPER OUTBOARD SKIN HAS A PIECE MISSING FROM THE FORWARD AND OUTBOARD SIDE. THE MIDDLE PIECE OF SKIN IS PEELED BACK. REPAIRED UPPER SURFACE RIGHT AILERON CONDUCTIVE FRAME PER SRM 57-60-02-1A-1, NOTE:O (O FOR SERV ICE). AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A1NM 20080602 NM 2008 6 2 CALA0800464 1 20080516 A 5311 146A1143 FRAME BOEING 737 737724 13844BY NM BS 867 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23708 28769 FRAME CRACKED AT STATION 867 ABOVE S9R. INSTALLED REPAIR PARTS PER EC/RA 5310-04763, REPAIRED FRAME PER EC/RA 5310-0476 3. 2 L 7 2 4F RT A16WE 20080602 NM 2008 6 2 CALA0800449 1 20080511 A 5311 65C34355 FRAME BOEING 737 737524 1384721 NM BS 400 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17620 27333 LEFT SIDE BS 400 INBOARD ATTACH FASTENER HOLE ON AIR CONDITIONING (A/C) BRACKET CRACKED. REPAIRED CRACKED FRAME ATTACH FASTENER HOLE AT LEFT SIDE BS 400 PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080603 GL 2008 6 3 HEEA119671 2 20080512 A 7200 23063392 ENGINE BELL 407 407 1182206 SW ALLSN 250C 250C47B GL MALFUNCTIONED B HEEA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 03 724PH 53327 LOST ENGINE OIL PRESSURE, ENGINE TORQUE, AND THE ENGINE CHIP LIGHT ILLUMINATED. 1 G 7 1 3U 3 U O H2SW E1GL 20080603 NM 2008 6 3 DU4R2008208 1 20080521 A 5420 311A151911 SUPPORT BOEING 737 737448 13844BU NM NR 1 PYLON GOUGED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 742VA 24773 S/O NR312001 NR 24376, NR1 ENGINE PYLON FAN COWL SUPPORT UPPER CHORD FWD HORIZ END FLANGE NAC 166-175 APPROX IS GOUGED. 2 L 7 2 4F RT A16WE 20080707 NM 2008 7 7 SB08030 1 20080518 A 2750 CIRCUIT BREAKER BOEING 737 7374B7 1384702 NM COCKPIT TRIPPED A USAA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 EA 19 440US 24811 FLL - FLT 1723 ON APPROACH TO FLL, WHEN FLAP HANDLE WAS SELECTED TO FLAPS 10 POSITION, THE FLAP INDICATOR SHOWED ONLY F LAPS 5 WITH L/E FLAPS EXTEND LIGHT. SELECTING FLAPS 15 POSITION, INDICATOR REMAINED AT FLAPS 5. CREW ACCOMPLISHED A GO -AROUND AND ACCOMPLISHED ALTERNATE FLAP EXTEND/OPS CHECK LIST. FLAP INDICATOR REMAINED AT FLAPS 5. FLIGHT LANDED WITHO UT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FLAP INDICATOR T/E CIRCUIT BREAKER OUT. RESET BREAKER A ND OPERATED FLAPS SEVERAL TIMES. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20080707 WP 2008 7 7 MWEA080071 1 20080517 A 2130 39613011 CONTROL VALVE DOUG DC9 DC982 3022082 WP LT PACK FAULTY A MWEA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 GL 13 810ME 48072 LEFT AIRCRAFT SYSTEM UNABLE TO HOLD CABIN PRESSURE AT 24,000 FEET, FLOW LIGHT WAS ON WITH OUTFLOW VALVE CLOSED. REMOVED AND REPLACED LEFT PACK FLOW CONTROL VALVE. 2 L 7 2 4F A6WE 20080707 EU 2008 7 7 UPS08152288 1 20080516 A 2170 COALESCER BAG AIRBUS A300 A300F4622R 3930360 EU A/C BAY DEFECTIVE A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 159UP 0848 INSPECTION TYPE:N/A HYDRAULIC MIST COMING FROM A/C VENTS. REMOVED AND REPLACED BOTH LEFT AND RIGHT WATER SEPARATOR COAL ESCERS WITH REFERENCE TO A300 MM 21-51-16-03. OPS CHECK NORMAL. 2 L 7 2 4F RT A35EU 20080707 NM 2008 7 7 UPS08M52286 1 20080402 A 5313 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C CTR CARGO - BILGE AREA AT BS 1701 TO BS 1710 LONGERON 52 FOUND CRACKED AS MARKED. EXISTING SPLICE AT STA 1701 - 1710 LONGERON 52 REMOVED, CRACKED LONGERON TRIMMED. HFEC INSP C/O ON REWORKED AREA, FOUND NO CRACK EVIDENT. REPAIR LONGERON FABRICATED. FPI C/O ON FAB LONGERON, FOUND NO CRACK EVIDENT. REPAIR SPLICE FAB & FPI C/O, FOUND NO CR ACK EVIDENT. HOLES PICK-UP ON LONGERON & SPLICE. NEW LONGERON & SPLICE PAINTED & INSTALLED PER SRM 51-33-01VII R35. 2 L 7 3 4F RT A22WE 20080707 SO 2008 7 7 C2XA08ON125 1 20080515 A 2820 UNKNOWN EMB 145 EMB145XR 3260214 SO LT WING LEAKING A C2XA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 27 17196 14500945 FLT 0074, FLIGHT CREW REPORTED LEFT WING FUEL LEAK IN FLIGHT. SEALED CLEAR ICE DETECTOR WIRE CONDUIT. OPERATIONALLY A ND LEAK CHECK SATISFACTORY. ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4F RT 20080707 SO 2008 7 7 RAIA00805018 1 20080516 A 3610 BLEED AIR SYS EMB 145 EMB145LR 3260212 SO NR 2 LEAKING A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 836HK 145695 FLT 8068 - IAD - BLEED NR 2 LEAK MESSAGE ON THE EICAS. MAINTENANCE DEFERRED THE NR 2 BLEED SYSTEM IAW MEL PROCEDURES. 2 L 7 2 4T RT T00011AT 20080708 NM 2008 7 8 HNAA0800174 1 20080520 A 3230 DIODE DHAV DHC8 DHC8102 2809003 NM LANDING GEAR MALFUNCTIONED A HNAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 07 911HA 034 LANDING GEAR WOULD NOT RETRACT WHEN SELECTED. REPLACED DIODES 3261-CR 3, 4, 5 AND 7. INSPECTED RELAY BASE K9 AND K11 A ND CONNECTOR 9811-P94. GEAR SWING AND OPS CHECK GOOD. CHECKED DOOR SOLENOID SEQUENCE VALVE GROUNDS. UNABLE TO DUPLICA TE PROBLEM ON JACKS. SYSTEM OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 20080708 NM 2008 7 8 USAA920081091 1 20080517 A 5330 143N35212 SKIN BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 924UW 22204 PIT - MAJOR REPAIR - C2 CHECK - CRACKED FUSELAGE SKIN, BS 730, BL 0 AT THE VHF ANTENNA MOUNT AREA. REPAIRED FUSELAGE SK IN, BS 730, BL 0 AT THE VHF ANTENNA MOUNT AREA IAW USAIRWAYS EA 111060. 2 L 7 2 4F RT A2NM 20080708 NM 2008 7 8 2008UALA02883 1 20080518 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERG EXIT LT INOP, DR3L MONITOR EXIT SIGN. FOUND LOOSE CONNECTION. SECURED CONNECTION. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 2008UALA02891 1 20080519 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 CEILING EMERGENCY LIGHT LEFT AISLE NEAR DOOR 1L AND FWD GALLEY IS INOP. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 2008UALA02778 1 20080513 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAVATORY NICKED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 536UA 25156 PAX REPORTED RECEIVING A ELECTRIC SHOCK IN MID LAV. FOUND VERY TINY NICK ON DOOR SWITCH WIRE, GROUNDING TO LAV STRUCTUR E. REPAIRED WIRE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080708 NM 2008 7 8 2008UALA02898 1 20080519 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 R-2 DOOR UPPER HINGE ARM CUTOUT REQUIRES DOUBLER. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080708 NM 2008 7 8 2008UALA02916 1 20080520 A 3350 FU305 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 RIGHT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP, TWO MOST AFT LIGHT ASSY'S. FOUND OPEN FUSE. REPLACED FUSE OP CHECKE D GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 2008UALA02920 1 20080520 A 2560 65B090944 GIRT BAR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L5 DOOR DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 196UA 28715 DOOR 5L, AFT LOWER GIRT BAR MECH CRANK ASSY IS SHEARED OFF. SUSPECT FAULTY GIRT BAR CRANK ASSY. REPLACED GIRT BAR CRANK ASSY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NE 2008 7 8 2008UALA02922 2 20080520 A 7230 STATOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 ENGINE CRACKED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 229UA 30557 222253 NR 1 ENG FOUND 1EA 9TH STG COMPRESSOR VANE CRACKED COMPLETELY THRU VIEWED FROM CONVEX SIDE. PER THE RECOMMENDATIONS OF MANUFACTURER ALL OPERATORS WIRE PW4000/72-35-25/CTS:ERC:08-5-08-1, PERFORMED A BORESCOPE INSPECTION OF THE SUBJECT ENGIN E TO CHECK FOR HP COMPRESSOR, STAGE-9 STATOR AIRFOIL CRACKING. ONE VANE WAS FOUND CRACKED COMPLETELY THROUGH THE AIRFOI L. THE ENGINE WAS REPLACED PRIOR TO FURTHER FLT, AND AS THIS ENGINE WAS LEASED FROM MANUFACTURER IT WAS RETURNED TO THEM IN AN UNSERVICEABLE CONDITION. THE ISSUE OF STAGE-9 STATOR CRACKING IS THE SUBJECT OF A PROPOSED MANUFACTURER`S FLEET M ANAGEMENT PLAN. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080708 NM 2008 7 8 HNAA0800176 1 20080516 A 3260 M390166105L RELAY DHAV DHC8 DHC8102 2809003 NM LANDING GEAR DEFECTIVE A HNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 07 940HA 156 ON FOLLOW UP INOP FOR LOG BOOK WRITE UP 267083 ITEM 1 LEFT MAIN FWD GEAR DOOR AMBER LIGHT CAME ON AFTER GEAR SELECTED UP . CHECKED FUNCTION OF LEFT FWD MAIN GEAR DOOR ACTUATOR, CHECKED FOR LEAKES, CYCLED GEAR MULTIPLE TIMES, C/N/D. CHANGED 6121-K5 AS PRECAUTIONARY MEASURE. CYCLED GEAR MULTIPLE TIMES. GEAR OPS CHECK GOOD REF 32-30. 2 H 7 2 4T RT A13NM 20080708 NM 2008 7 8 DHL2008764509 1 20080520 A 5315 FLOORBEAM BOEING 727 727264 138408M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 CORROSION ON BS 1110 FLOORBEAM LBL 24 - LBL 45. CORROSION ON FLOORBEAM LBL 24-LBL 45 BS 111O FOUND OUT OF LIMITS AT LBL 33 IAW B727 SRM 51-10-6 AND 53-10-1 FIG 5. CUT OUT DAMAGED AREA, FAB ONE FILLER WITH 7075-T6 .125 INCH DIM 2 INCH BY 1 INCH PO 7371263. TWO SUPPORT ANGLES ONE WITH BAC1490-2785-7075-T6 DIM 13 BY 2 1/4 PO 9006027 AND 2) BAC1490-2831-7075T 6 DIM 9 1/2 INCH BY 2 1/4 INCH PO 7283322 IAW B727 SRM 53-10-8 FIG 8 AND 51-30-5. 2 L 7 3 4F A3WE 20080708 EA 2008 7 8 COMA0860246 1 20080520 A 5320 6013600129 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 487CA 13628 7729 CRACK ON REINFORCEMENT ANGLE OF LEFT FS 640 FRAME BETWEEN STR 9 AND STR 12. REPAIRED IAW SB 601R-53-061. 2 L 7 2 4F RT A21EA 20080708 EA 2008 7 8 COMA0860247 1 20080521 A 5311 60034017595 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 32939 7050 DURING A 72/48 MO INSPECTION, TASK CRJ-2-142005, FOUND FUSELAGE FRAME CORRODED ON TOP EDGE AND CRACKED ON LOWER EDGE. P ERFORMED PERMANENT REPAIR IAW REO 601R-53-11-136. 2 L 7 2 4F RT A21EA 20080708 NM 2008 7 8 CALA0800518 1 20080602 A 5320 65528941 FLOOR SUPPORT BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 MAIN DECK FLOOR SUPPORT AT STATION 540 RBL 2 IS CRACKED. REMOVED AND REPLACED MAIN DECK FLOOR SUPPORT AT STATION 540 RB L 2 PER EC/RA 5321-01551. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 CALA0800524 1 20080602 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 STATION 400 LT BETWEEN S8L AND S9L IS CRACKED. REMOVED AND INSTALLED NEW REPAIR ANGLES A AND B PER EA 5310-04498 OP2. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 DLM88080879 1 20080617 A 5313 STINGER DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 947DL 49878 UPON REMOVAL OF DOME NUT PLATE, FOUND EXFOLIATING CORROSION IN CHANNEL OF S-20R STA 758. REPLACED DAMAGED SECTION OF ST RINGER IAW SRM 53-00-03. 2 L 7 2 4F RT A6WE 20080708 NM 2008 7 8 DL76G080829 1 20080604 A 3350 20121 CHARGER BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1605 30198 FOUND ON PDC/DRC MISC L SIDE EXTERIOR EMERGENCY LIGHTS INOP. 2 L 7 2 4F RT A1NM 20080708 NM 2008 7 8 ASAA0852975 1 20080521 A 2161 6228145 CONTROLLER BOEING 737 737890 1384527 NM LT PACK MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 579AS 4887 35187 LEFT PACK LIGHT ILLUMINATED ON RECALL AFTER ENG START. RESETS WITH M C DEF PER MEL 21 32 LEFT PACK TEMP CONTROLLER INOP . PERFORMED BITE TEST PER FIM 21 62 801, CLEARED TCV FAULT AND RAN TEST PASS "GO". NO RECENT HISTORY. AC GOOD FOR SER VICE. FAULT DUPLICATED ON NR 1 PACK TEMP CONTROLLER, CLEARED PASS GO. 2 L 7 2 4F RT A16WE 20080710 NM 2008 7 10 DL76L080730 1 20080513 A 7997 WIRE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE CHAFED A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 173DN 48337 21381 24800 724165 WHEN THROTTLES ADVANCED FOR TAKEOFF RT ENG OIL PSI LIGHT ILLUMINATED AND RT ENG OIL PSI EICAS MSG ANNUNCIATED, LIGHT EXT WITH THROTTLES AT IDLE, RE-ILLUMINATED EACH TIME THROTTLE IS ADVANCE OIL PSI INDICATES NORMAL. INSP MAIN ENG OIL FILTE R CHIP DETECTORS NO DISCREPANCIES NOTED. REPLACED MAIN ENG OIL FILTER PRECAUTION. FOUND WIRE W3510-027-18 CHAFING CLAM P AT PREVIOUSLY. REPAIRED SPLICE. REPLACED CLAMP AND REPOSITIONED TO PREVENT CHAFING. AFTER WIRE REPAIR RT ENG OIL LI GHT ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS. 2 L 7 2 4F 4 F RT A1NM E24NE 20080710 NM 2008 7 10 DL76L080753 1 20080410 A 3397 CONNECTOR BOEING 767 767332 1382001 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 EMERGENCY LIGHT CONNECTOR AT SEAT 36 RT IS DAMAGED. REPLACED CONNECTOR IAW DAL B767-300 SWPM 20-64-17. OPS CHECKED GOO D IAW B767 MM 33-51-00-715-200. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 DL76L080759 1 20080507 A 3597 CONNECTOR BOEING 767 767332 1382001 NM CABIN WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 THE PSU O2 CONNECTORS AT 37FG, 18AB, 23AB, 26AB, 33AB AND 35AB ARE WORN. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 USAA920081101 1 20080516 A 5230 6546921225 DOOR BOEING 737 7374B7 1384702 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 444US 24862 CLT - MAJOR REPAIR - C2 CHECK - CRACKED FORWARD CARGO DOOR AT DOOR HANDLE CUTOUT. REPLACED FORWARD CARGO DOOR IAW B737 AMM 52-31-00. 2 L 7 2 4F RT A16WE 20080710 2008 7 10 2008UALA02878 4 20080516 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE LOOSE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 512UA 24809 CREW REPORTED LANYARD LOOSE AT DOOR 1R. SECURED LANYARD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080710 NM 2008 7 10 2008UALA02932 1 20080521 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 1J FWD LIGHT ASSY. REPLACED LIGHT ASSY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080710 WP 2008 7 10 070199 1 20080519 A 3350 408822101 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 887GA 49932 IT HAS BEEN REPORTED BY THE FLIGHT CREW THE EMERGENCY EVACUATION LIGHTING SYSTEM HAS BEEN FOUND TO BE DEFECTIVE. MAINTE NANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPE RATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00, SYSTEM OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT HAS BEEN RETURNED T O SERVICE. 2 L 7 2 4F A6WE 20080711 NM 2008 7 11 UPS08M52311 1 20080505 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C MAIN CABIN SEAT TRACK LOCATED AT LBL 8.5 HAS EXTENSIVE EXFOLIATION CORROSION AT STA 490. REMOVED, FA BRICATED, AND INSTALLED SEAT TRACK IAW DWB WSP0826 DWB S4929150 MD-11 SRM 51-31-01 AND 51-21-01. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 UPS08M52316 1 20080515 A 5730 STRAP DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C RT LEADING EDGE FIXED SKIN SPLICE STRAP STA XORS 562 CRACKED. REMOVED, FABRICATED, AND INSTALLED SKI N SPLICE STRAP IAW MD-11 SRM 51-33-01, 51-21-01, AND DWG ARB3954-1. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 UPS08M52318 1 20080510 A 5712 DOUBLER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C LEFT WING FIXED L/E RIB DOUBLER AT XORS 562 FOUND CRACKED. REMOVED, FABRICATED, AND INSTALLED RIB DO UBLER IAW MD-11 SRM 51-21-01, 51-33-01, AND DWG ARB3954. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 UPS08M52325 1 20080516 A 5321 WSP0785501 PANEL DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C MAIN CARGO RCB PANEL NR 6 HAS CORROSION DAMAGE ON TOP FACE. LOCATED AND DRILLED REPLACEMENT PANEL AN D INSTALLED ON EO MD11-5330-27218-B. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 UPS08M52326 1 20080508 A 5320 SWP075056 MOUNT DOUG MD11 MD11F 3023600 NM MAIN CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C RIGID BARRIER NR 10 FLOOR MOUNT P/N WSP0750-5-6 IS CRACKED. RECEIVED RIGID BARRIER PANEL NR 10 AND I NSTALLED ON EO MD11-5330-27218-B. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 UPS08M52327 1 20080504 A 5321 WSP0789501 PANEL DOUG MD11 MD11F 3023600 NM MAIN CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C MAIN CARGO RCB PNL NR 3 HAS CORROSION DAMAGE 4 PLACES ON TOP FACE. LOCATED AND DRILLED REPLACEMENT P ANEL AND INSTALLED PANEL ON EO MD11-5330-27218-B. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 UPS08M52328 1 20080504 A 5321 WSP0788502 PANEL DOUG MD11 MD11F 3023600 NM MAIN CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C MAIN CARGO RCB PNL NR 13 HAS CORROSION DAMAGE ON 2 PLACES, TOP FACE. LOCATED AND DRILLED NEW PANEL I AW MD-11 SRM 51-31-01 AND INSTALLED ON EO MD11-5330-27218-B. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 UPS08M52334 1 20080503 A 5321 SWP0791Y501 PANEL DOUG MD11 MD11F 3023600 NM MAIN CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C MAIN CARGO RCB PNL NR 1 HAS CORROSION DAMAGE 7 PLACES ON TOP FACE. LOCATED AND DRILLED REPLACEMENT P ANEL IAW MD-11 SRM 51-31-01 AND INSTALLED ON EO MD11-5330-27218-B. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 BB08094 1 20080523 A 3350 036000570010 FUSE BOEING 757 7572B7 1384964 NM POWER SUPPLY BLOWN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 929UW 27144 CLT - THE EXTERIOR EMERGENCY LIGHTS AT L2, L3 & R3 WERE FOUND INOPERATIVE. MAINTENANCE REPLACED A BLOWN FUSE AT POWER S UPPLY UNIT M733. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 AALA200801162 1 20080430 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 623AA 24581 DFW - EMERGENCY LIGHTS AT SEAT ROWS 9D TO 16D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 9D T O 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080707 NM 2008 7 7 2008UALA02846 1 20080517 A 2611 SMOKE WARNING BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE FALSE ACTIVATION A UALA O OTHER N FALSE WARNING CR CRUISE 1 WP 29 105UA 26473 'SMOKE DR 5 REST' EICAS CAUTION MESSAGE DISPLAYED. ACCOMPLISHED CREW REST SMOKE DETECTION SYSTEM TEST PER MM 26-14-20 A LL 4 DETECTORS CHECK NORMAL ALSO ACCOMPLISHED GROUND TEST OF RECIRCULATION FANS TEST PASSED.TRIED TO DUPLICATE PROBLEM SYSTEM ALL TEST PASSED. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 2008 7 8 2008UALA02810 4 20080514 A 2565 416N28209 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT OVERWING UNSECURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 539UA 25223 LEFT OVERWING SLIDE PACK FOUND UNLEASHED. REMOVED AND REPLACED OFF WING SLIDE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080708 EU 2008 7 8 2008UALA02812 1 20080516 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 446UA 834 FOUND CORROSION ON FLOORBEAM 205. MAJOR REPAIR ACCOMPLISHED: REPLACED BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20080708 NM 2008 7 8 2008UALA02918 1 20080520 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY EXIT EEL LIGHT INOP AT ROW 48 LEFT. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 EA 2008 7 8 SWIA200819642 1 20080317 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 613SK 10038 INNER PAX DOOR HANDLE IS CRACKED AT LOWER ATTACH POINT, FOUND AT C-CHECK. INSTALLED NEW PAX DOOR INNER HANDLE ASSEMBLY PER CRJ700 AMM 52-11-02-400-809-A01. 2 L 7 2 4F RT A21EA 20080708 EA 2008 7 8 COMA0870019 1 20080516 A 3610 SHUTOFF VALVE CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A COMA O OTHER O OTHER DE DESCENT 1 SO 01 625CA 10113 FLIGHT 5249 - LEFT AND RIGHT PRSOV'S AS WELL AS ISOLATED VALVE BEGAN CYCLING OPEN AND CLOSED. RAPID PRESSURIZATION LOSS OCCURRED. DECLARED EMERGENCY, FOLLOWED QRH, ISOLATION FAULT MESSAGE DISPLAYED. LANDED WITHOUT INCIDENT. OPS CHECKED PRSOV'S BOTH SIDES, PERFORMED CRJ700/900-SL-36-014. NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 20080708 EA 2008 7 8 COMA0860240 1 20080509 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 739CA 7273 SEVERE CORROSION WAS FOUND ON LEFT FLOOR SILL BETWEEN FS 349.00 AND FS 364.00. REMOVED AND SPLICED SECTION OF FLOOR SIL L IAW ES 10-5320-02208. 2 L 7 2 4F RT A21EA 20080708 EA 2008 7 8 COMA0860241 1 20080511 A 5311 6013600130 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 868CA 19698 7427 CRACK ON AFT SIDE FS 640 FRAME JUST BELOW STR 9. REPLACED RIGHT SIDE FRAME AT 640 AND PERFORMED REPAIR IAW SB601R-53-06 1 PART C. 2 L 7 2 4F RT A21EA 20080708 NM 2008 7 8 SWAA082841 1 20080524 A 3350 MS155721 LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 CALA0800519 1 20080602 A 5311 146A1143 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 FRAME CRACKED AT STATION 867 BETWEEN S8R AND S9R. REPAIRED FRAME AT STATION 867 BETWEEN S8R AND S9R PER EC/RA 5310-0477 7. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 DL757080875 1 20080606 A 2597 GROUND WIRE BOEING 757 757232 1384965 NM EVAC SLIDE LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 727230 SQUIB AND SWITCH TEST P61 PANEL FAILS TEST 1. TROUBLESHOT L EMERGENCY ESCAPE SLIDE SQUIB AND NR 1 TEST SWITCH ON P61 PA NEL IAW WDM 25-65-01. FOUND LOOSE GROUNDS ON CONNECTOR D5544. RECONNECTED LOOSE GROUND WIRES ON CONNECTOR D5544 IAW SW PM 20-20-00. PERFORMED OPS CHECK OF LEFT EMERGENCY ESCAPE SLIDE SQUIB TEST IAW AMM 25-65-00. OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 20080708 NM 2008 7 8 DLM88080855 1 20080612 A 3260 387 LIGHT DOUG MD88 MD88 3023688 NM COCKPIT INOPERATIVE A DALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 27 900DE 53372 RIGHT MAIN GEAR GREEN LIGHTS FAIL TO ILLUMINATE ON LANDING. FLIGHT CREW RELAMPED ON GO AROUND. OPERATION NORMAL FOR LA NDING. MAINTENANCE RECORDED INFORMATION AND PERFORMED ANNUN/DIGITAL LIGHT TEST. LANDING GEAR INDICATOR LIGHTS CHECK NO RMAL. 2 L 7 2 4F RT A6WE 20080708 NM 2008 7 8 2008UALA02689 1 20080508 A 5753 113T172099G FAIRING BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE T/E FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 670UA 29240 LEFT WING FLAP MOST INBOARD FAIRING ON MID FLAP HAS TWO EACH CRACKS. SUSPECT GROUND EQUIPMENT DAMAGE REMOVED FAIRINGS S ENT TO SHOP 272 FOR REPAIR. REINSTALLED FAIRINGS. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080710 NM 2008 7 10 AALA200801117 1 20080427 A 3350 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 191AN 32385 DFW - EMERGENCY LIGHT IN FRONT OF SEAT 18F HAS DAMAGED DECAL. REPLACED DECAL ON LENS FOR EMERGENCY LIGHT IN FRONT OF SE AT 18F. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080710 NM 2008 7 10 2008UALA02835 1 20080515 A 2611 BLOWER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FWD CARGO BAY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 541UA 25253 FWD CARGO SMOKE BLOWER 2 INOP. REPLACED FWD CARGO SMOKE DETECTOR BLOWER NR 2, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080710 NM 2008 7 10 2008UALA02942 1 20080519 A 2910 HYDRAULIC SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU B-SYSTEM MALFUNCTIONED A UALA O OTHER K FLUID LOSS CR CRUISE 1 WP 29 385UA 24660 THE B-SYSTEM HYDRAULIC PRESSURE DECREASING. 2 L 7 2 4F 4 F RT A16WE E21EU 20080710 NM 2008 7 10 USAA920081104 1 20080415 A 5315 BAC1520 FLOORBEAM BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 MIA - MAJOR REPAIR - C4 CHECK - CORROSION ON CABIN FLOORBEAM, BS 1480, RBL 40. REPAIRED CABIN FLOORBEAM, BS 1480, RBL 4 0 IAW B767 SRM 53-00-52 REPAIR 2. 2 L 7 2 4F RT A1NM 20080711 NM 2008 7 11 UPS08M52310 1 20080517 A 5712 DOUBLER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C LEFT WING FIXED L/E RIB DOUBLER BETWEEN SLAT TRACK 9 AND 10 FOUND CRACKED. REMOVED, FABRICATED, AND INSTALLED RIB DOUBLER IAW DWB ARB2931 MD-11 SRM 51-21-01, 51-33-01, AND 51-31-01. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 MWEA080079 1 20080522 A 2560 50002401 GROMMET BOEING 717 717200 1383700 NM TAILCONE MISSING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 909ME 55173 TAIL CONE INNER RELEASE HANDLE CABLE GROMMET IS MISSING CAUSING THE HANDLE TO NOT PULL WHEN TESTED. INSTALLED GROMMET. 2 L 7 2 4F TR A6WE 20080711 NM 2008 7 11 AALA200801185 1 20080503 A 1100 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 648AA 24606 DFW - EMERGENCY LIGHT EXIT PLACARD AT RIGHT FORWARD OVERWING DAMAGED. REPLACED PLACARD FOR EMERGENCY LIGHT EXIT PLACARD AT RIGHT FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 AALA200801214 1 20080505 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 DFW - EMERGENCY LIGHT AT SEAT 26C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801128 1 20080428 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 678AN 29428 MIA - EMERGENCY SLIDE ARMING LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY SLIDE ARMING LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080603 CE 2008 6 3 DXTA200803076 1 20080522 A 2720 99145586 ACTUATOR CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C 03047 GL RUDDER LIMITER INOPERATIVE E DXTA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 07 903QS 6928 7500162 DURING CLIMBOUT THROUGH APPROX 7000 FT AGL IN GUSTY WINDS A RUD LIMIT FAIL A ILLUMINATED WITH RUDDER LIMIT AT 27 PERCENT . 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080603 CE 2008 6 3 GUUA05080801 1 20080508 A 5520 1016200131 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81536 25881 UE152 DURING SCHEDULED ROUTINE MAINT, DISCOVERED LT CENTER ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED LT CTR ELEVATOR HINGE BRACKET. 2 L 7 2 4T 3 T RT A24CE E2NE 20080603 CE 2008 6 3 GUUA05080802 1 20080508 A 5520 1016200131 HINGE BRACKET BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81536 25881 UE152 DURING SCHEDULED ROUTINE MAINT DISCOVERED RT CTR ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT CTR ELEVATOR HINGE BRAC KET. 2 L 7 2 4T 3 T RT A24CE E2NE 20080603 CE 2008 6 3 GUUA05080803 1 20080508 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE RT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81536 25881 UE152 DURING SCHEDULED ROUTINE MAINT DISCOVERED RT OB ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT OB ELEVATOR HINGE BRACKE T. 2 L 7 2 4T RT A24CE 20080603 NE 2008 6 3 HEEA119764 1 20080520 A 7921 9560156790 SHAFT SKRSKY S76 S76C 8143008 NE TMECA ARRIEL ARRIEL2S2 60036 NE OIL COOLER SHEARED B HEEA E ENGINE SHUTDOWN O OTHER NR NOT REPORTED 1 SW 03 769P 760671 NR 1 ENGINE OIL TEMPERATURE WENT TO 120 DEGREES C, IN THE RED ZONE. COMPLIED WITH CHECKLIST AND SHUTDOWN NR1 ENGINE AND PERFORMED RUN-ON LANDING. FOUND OIL COOLER BLOWER SHAFT SHEARED. 1 G 7 2 3U 4 U NC H1NE E00054EN 20080603 CE 2008 6 3 GLBA20061106 1 20080523 A 3230 LANDING GEAR BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MALFUNCTIONED A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 211GL UE211 AIR RETURN - FLIGHT 5031 ENROUTE, PILOTS REPORTED THAT THE GEAR WOULD NOT RETRACT PROPERLY. AIRCRAFT WAS FOUND SAFE FOR INTENDED FERRY FLIGHT TO WHERE MAINTENANCE PERFORMED NUMEROUS EXTENSIONS AND RETRACTIONS WITH NO DEFECTS NOTED IAW. MM 3 2-00. SUBSEQUENT OPERTIONAL CHECK FLIGHT WAS PERFORMED WITH NO ABNORMALITIES NOTED. 2 L 7 2 4T 3 T RT A24CE E2NE 20080603 SO 2008 6 3 SWIA200819690 1 20080526 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO CABIN SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 07 290SW 120317 FLT 5556 - THE CABIN FILLED WITH SMOKE ON DESCENT. BLEEDS AND PACKS SELECTED TO LOW AND SMOKE CLEARED. INSPECTED AND R AN BOTH PACKS IN MULTIPLE CONFIGURATIONS AND COULD NOT DUPLICATE DISCREPANCY. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080603 EA 2008 6 3 SWIA200819691 1 20080522 A 5610 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 703SK 10139 FLT 6716 - COPILOT SIDE WINDOW IS CRACKED. REPLACED COPILOT'S SIDE WINDOW IAW MM 56-11-01. ALL OPS CHECKS GOOD, P/N OF F 601R33033-18, S/N OFF 03321H8789. 2 L 7 2 4F RT A21EA 20080603 NE 2008 6 3 SBAA200800002 2 20080510 A 7200 99105791 ENGINE CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE MCAULY 3AF34C 3GFR34C703 GL SHUTDOWN E SBAA A UNSCHED LANDING Y ENGINE STOPPAGE AP APPROACH 1 GL 09 893FE 8836 674 208B0223 17219 900932 PILOT REPORTED THAT ENGINE SHUTDOWN IN FLIGHT. 1 H 7 1 3T 3 T A37CE E4EA 5 C P60GL 20080603 SO 2008 6 3 SWIA200819693 1 20080406 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO BS 5118-6653 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 561SW 120335 FLOOR SUPPORT RAIL AND WEB ON THE LEFT SIDE OF FS 5118 TO FS 6653 IS CORRODED. FOUND AT C-CHECK. REPLACED CORRODED PART S PER EMB 120 SRM 51-40-02. 2 L 7 2 4T RT A31SO 20080603 SO 2008 6 3 SWIA200819696 1 20080406 A 2497 WIRE EMB 120 EMB120ER 3260203 SO DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 561SW 120335 WIRE AT TB0122 IN LEFT, FORWARD CONSOLE SHOWS SIGNS OF OVERHEATING, FOUND AT C-CHECK. REPLACED WIRE AT TB0122 AS REQUIR ED. 2 L 7 2 4T RT A31SO 20080603 EU 2008 6 3 TRBA2008054 1 20080517 A 3350 7012210 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHTS FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 447AM 447 THE EMERGENCY LIGHT ON THE CABIN STAIRS MAIN DOOR IS INOPERATIVE. REMOVED AND REPLACED LIGHT BULB AND PERFORMED OPERATI ONAL CHECK IAW JIC NR 33-50-00-OPT-10000-001. 2 H 7 2 4T RT A53EU 20080603 EA 2008 6 3 SWIA200819669 1 20080319 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 615 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 CORROSION FOUND ON FLOOBEAM ATTACH FITTING AT FS 615, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R53-61 -2562. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819671 1 20080228 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910SW 7566 FS 280 LOWER FLOOR SUPPPORT IS CRACKED AT RBL9, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER REO601R-53-11-171 REV D DAT ED 02-13-07. 2 L 7 2 4F RT A21EA 20080603 SO 2008 6 3 SWIA200819679 1 20080522 A 5410 BEAM EMB 120 EMB120ER 3260203 SO NACELLE DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 576SW 120345 FLT 3613 - DAMAGE TO KEELSON BEAM FOUND NEAR INBOARD SIDE OF GEAR AT NACELLE. REPLACED DAMAGED SECTION OF KEELSON BEAM IAW EMB SRM 51-40-02. 2 L 7 2 4T RT A31SO 20080603 EA 2008 6 3 SWIA200819680 1 20080518 A 2421 ADG CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 935SW 7725 FLT 6644 - THE ADG DEPLOYED AFTER TAKEOFF. RESET ADG SENSE C/B AND RESTOWED ADG. OPS CHECK GOOD PER MM 24-23-01. 2 L 7 2 4F RT A21EA 20080603 CE 2008 6 3 DXTA200803047 1 20080507 A 2722 666061311 ACTUATOR CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE RUDDER DEFECTIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 656QS 574 5605732 RUDDER CONTROL REQUIRES EXCESSIVE CONTROL INPUTS TO GET DESIRED RESULTS. REMOVED AND REPLACED ACTUATOR IAW MM 27-30-05. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A22CE E00059EN 20080603 CE 2008 6 3 GUUA05220801 1 20080522 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 81536 UE152 FLIGHT: 9150, DURING FLIGHT, FUEL SMELL IN THE CABIN. INSPECTED FOR FUEL AROUND ACM NO FUEL FOUND, RAN ENGINES NO FUEL SMELL NOTED. 2 L 7 2 4T 4 T RT A24CE E26NE 20080603 CE 2008 6 3 GUUA05220802 1 20080522 A 2150 INLET BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE ACM CONTAMINATED A GUUA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 29 81536 UE152 FLIGHT: 9254, DURING APPROACH, AIRCRAFT CABIN SMELLS OF FUEL. CLEANED RESIDUAL FUEL AT ACM AIR INLET. RAN ENGINES NO FU EL SMELL NOTED. 2 L 7 2 4T 4 T RT A24CE E26NE 20080603 EA 2008 6 3 S9BA20080020 1 20080523 A 5514 C6TPM102529 ADAPTER DHAV DHC6 DHC6300 2802606 EA HORIZ STAB CRACKED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 533SW 533 (CLOSE) LT AFT HORIZONTAL WEB ADAPTER CRACKED FOUND DURING SB 454 PART AEMERGENCY MEASURES EXECUTED. AIRCRAFT GROUNDED , REMOVED AND REPLACED LT AFT WEB ADAPTOR. 1 H 7 2 3T RT A9EA 20080603 EA 2008 6 3 SWIA200819637 1 20080304 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 457SW 7773 LOWER FLOOR SUPPORT IS CRACKED AT FS 280 AND RBL9, FOUND AT C-CHECK. COMPLIED WITH REPAIRS OF SUPPORT PER REO 601R-53-1 1-171. 2 L 7 2 4F RT A21EA 20080603 CE 2008 6 3 DXTA200803083 1 20080528 A 3243 LINE RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP MASTER CYLINDER LOOSE E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 872QS 258472 LT FOOT BRAKE ON CAPTS SIDE INOP. TIGHTENED LINE ON PILOTS BRAKE MASTER CYLINDER AND SERVICED AND BLED PILOTS BRAKE MAS TER CYLINDER. 2 L 7 2 4F 4 F RT A3EU E6WE 20080603 EA 2008 6 3 SWIA200819625 1 20080507 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 403SW 7028 PAX DOOR EMERGENCY FLOODLIGHT LENS COVER AND BASE IS BROKEN. REPLACED EMERGENCY LIGHT FLOODLIGHT ASSEMBLY. OPS CHECK G OOD. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819667 1 20080319 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 FS 280 FORWARD FLOOR SUPPORT ON LEFT SIDE IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ200 SRM 51-2-06 PG 14-18. 2 L 7 2 4F RT A21EA 20080603 EU 2008 6 3 MALA080104 1 20080516 A 5523 TRIM TAB SAAB SF340 340B 7860101 EU LT ELEVATOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 442XJ 340B442 LT ELEVATOR TRIM TAB HAS TWO SMALL DENTS, FOUND TO BE DISBONDED, ON THE BOTTOM SURFACE. REMOVED LT ELEVATOR TRIM TAB, R EPAIRED DENTS THAT WERE FOUND TO BE DISBONDED. CUT OUT DAMAGED SKIN, FILLED CORE, INSTALLED REPAIR PLIES AND RESTORED P ROTECTIVE FINISH IAW SAAB 340 SRM 51-70 AND EONR S51031. REINSTALLED TRIM TAB AND PERFORMED STATIC BALANCE CHECK IAW SR M 51-60, CHECK TO BE WITHIN LIMITS. 2 L 7 2 4T RT A52EU 20080603 SO 2008 6 3 SWIA200819681 1 20080525 A 5230 SEAL EMB 120 EMB120ER 3260203 SO CARGO DOOR DAMAGED A SWIA G O2 MASK DEPLOYED J WARNING INDICATION DE DESCENT 1 NM 07 567SW 120342 FLT 3597 - CABIN ALTITUDE CLIMBED ON DESCENT AND O2 MASKS DEPLOYED. INSPECTED SYSTEM AND REPLACED DAMAGED CARGO DOOR SE AL IAW MM 52-30-01. 2 L 7 2 4T RT A31SO 20080603 SO 2008 6 3 SWIA200819682 1 20080525 A 3520 OXYGEN MASK EMB 120 EMB120ER 3260203 SO CABIN UNWANTED DEPLOY A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 567SW 120342 FOUND ALL CABIN OXYGEN MASKS DROPPED. INSPECTED AND RESTOWED ALL OXYGEN MASKS AS REQUIRED. 2 L 7 2 4T RT A31SO 20080603 EA 2008 6 3 SWIA200819688 1 20080524 A 3397 CIRCUIT BOARD CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 756SK 10221 FLT 5879 - LOWER LEVEL EMERGENCY LIGHTS ARE INOP. REPLACED PRINTED CIRCUIT BOARD IAW AMM 33-51-11. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080603 EU 2008 6 3 MALA080105 1 20080516 A 5260 TRACK SAAB SF340 340B 7860101 EU AIRSTAIR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 442XJ 340B442 FLOOR PANELS, ENTRANCE STAIR SLIDE TRACK SEVERELY CORRODED, APPROX STA 236-288. REMOVED CORRODED SLIDE TRACK AND REPLAC ED WITH NEW SLIDE TRACK, P/N 7253710-871 IAW SAAB 340 SRM 51-20 AND 51-40. 2 L 7 2 4T RT A52EU 20080603 NE 2008 6 3 200805141 2 20080511 A 7321 4120T01P01 FMU EMB ERJ170 ERJ170100SE 3260406 NM GE CF34 CF348E5 30061 NE NR 2 ENGINE FAULTY A UHLA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 11 634RW 9534 17000055 GEE193232 FLIGHT 7544 DEN TO IND CREW REPORTED E2 HAD LP VIBE TO 4.0 (IN AMBER) ON CLIMBOUT, PROCEEDED TO PULL POWER BACK UNTIL VI BE STABILIZED. ABOUT 15 MINS LATER IN CRUISE N1 DROPPED TO 25% AND RECEIVED AN E2 CNTRL FAULT. COULD NOT REGAIN CONTRO L OF ENGINE AND PERFORMED PRECAUTIONARY SHUT DOWN. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE FMU AND GEAE FADEC P/N: 4120T00P48, S/N: LMDL0503, TT: 3979, TC: 2402. 2 L 7 2 4F 4 F RT A56NM E00063EN 20080529 NM 2008 5 29 08FDEA01915 1 20080520 A 5320 6529548 PAN BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 AFT MAIN DECK FLOOR DITCHING PANS PAN ASSY IS CRACKED BS 1176 - 1183, LBL 37-47, WL 208. REMOVED DITCHING PAN, FABRICAT ED, HEAT TREATED TO T-6 CONDITION, ALODINED AND PRIMED AND INSTALLED NEW PAN, REF SRM 51-30-2 PG 1, CWG 65-29549, MM 51- 30-05 PG1, SRM 51-10-2 PG 7, MM 51-20-151-07 PG 1, SRM 51-20-04 PG1-4. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 EU 2008 5 29 08FDEA01916 1 20080520 A 5321 A532B385600500 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 815FD 638 THERE IS A BROKEN FLOOR PANEL FOR THE MAIN CARGO DECK FROM FRAME 54.2 TO FRAME 55/58, RBL-17 TO RBL-37. MATERIAL ID IS A402H35039-003, PO 604814.1 IAW FEDEX DWG SRZ 25-005, REV F. FABRICATED A NEW FLOOR PANEL FOR THE MAIN CARGO DECK FROM FRAME 54.2 TO FRAME 55/58 USING THE OLD FLOOR PANEL AS A TEMPLATE IAW FEDEX DWG SRZ 25-005, REV F. MARKED PANEL NR 252 GF IAW FEDEX DWG SRZ 25-005, REV F AND GMM 7-0-1000. PANEL PART ID IS FXR532B385600500. 2 L 7 2 4F RT A35EU 20080529 EU 2008 5 29 08FDEA01870 1 20080517 A 5347 R5307008820400 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 672FE 779 MAIN DECK CARGO SEAT TRACK NR 3 RT HAS 4 AREAS OF CORROSION BETWEEN FR 55 AND FR 57.3, APPROX 14 SQ IN REMOVED LEVEL 1 C ORROSION AND INSTALLED SEAT TRACK REPAIR AT TRACK NR 3 RT BETWEEN FR 57 AND FR 57.3 IAW A300-600 SRM 53-10-16, FIG 208. 2 L 7 2 4F RT A35EU 20080529 NM 2008 5 29 08FDEA01990 1 20080527 A 5230 6559948502 SEAL BOEING 727 727233 138408A NM ZONE 800 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 LOWER NR 2 CARGO DOOR S/N BNW 506, AFT LWR CORNER, OF SEAL DEPRESSOR HAS NICKS. NR 2 CARGO DOOR SEAL DEPRESSOR, AFT COR NER FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED AFT CORNER SEAL DEPRESSOR PN NR 65-59948-502, REF 51-40-02 AND DWG 65-60234 THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01993 1 20080527 A 5230 65571467 SEAL BOEING 727 727233 138408A NM ZONE 800 DIRTY A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 LOWER FWD CARGO COMPARTMENT DOOR, UPPER AFT CORNER CRACKED FABRICATED PER BOEING DWG 65-57146 CARGO DOOR AFT UPPER CORNE R REF SRM 51-30-2. INSTALLED NEW SEAL DEPRESSOR CORNER REF 51-30-2, RESTORED LEVELING COMPOUND TO AREA. REF AMM 51-40- 000-0. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01998 1 20080527 A 5347 BAC15201466 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 MAIN DECK FLOOR, SEAT TRACK EXTRUSION IS CORRODED, BS 850 - 870, LBL 45, WL 208. REMOVED AND REPLACED TRACK WITH NEW TR ACK. FABRICATED FROM BAC 1520-1466 EXTRUSION REF SRM 51-30-2 PG 2, SRM 51-10-2 PG -3, GMM7-0-1001, AMM 51-20-014. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 EA 2008 5 29 HNAA0800158 1 20080505 A 6123 30005000051 TSCU DHAV DHC8 DHC8311 1386006 EA AUTOFEATHER SYS FAULTED A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 330EN 11037 274 AUTO FEATHER WOULD NOT ARM DURING TAKEOFF ROLL. 2 H 7 2 4T RT A13NM 20080529 SO 2008 5 29 C2XA08SH074 1 20080513 A 5320 14525599001 SUPPORT BRACKET EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13968 145138 SHV - DURING C-CHECK WASTE DRAIN SUPPORT CORRODED INSIDE AIRCRAFT. MX REMOVED AND REPLACED WASTE DRAIN DUMP VALVE SUPPO RT ASSY IAW EMB 145SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 20080529 NM 2008 5 29 08FDEA01951 1 20080522 A 5320 65295984 PAN BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 AFT MAIN DECK FLOOR DITCHING PAN ASSY IS CRACKED WITH INTERIM COMPOSITE REPAIR BS 1176 - 1183, RBL 18-27, WL 208 REMOVED OLD DITCHING PAN. FABRICATED NEW DITCHING PAN OUT OF 6061-O, HEAT TREATED TO T-6, DRILLED TRIMMED, TREATED PRIMED AND INSTALLED. REF BAC DWG 65- 29548, FED EX GMM 7-0-1001, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080529 NM 2008 5 29 08FDEA01924 1 20080521 A 5311 AFA00203 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 MAIN DECK TRANSVERSE FRAME REPAIR AT STA 1701 L=12R FOUND DENTED. REPAIRED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. INI TIAL INSPECTION REQUIRED AT 14,500 CYCLES AND REPETITIVE INSPECTION AT EVERY 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 5 3-30-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 08FDEA01925 1 20080521 A 5313 AEA74761 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 CRACK INDICATION FOUND DURING X-RAY INSPECTION AT STA 6-100, LONGERON 1R AFT SECTION EDGE, CRACK LENGTH APPROX 0.5 INCH. REPAIRED AS PER SRM 53-10-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080529 WP 2008 5 29 08FDEA01932 1 20080521 A 5730 ARB087244 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 567FE 46994 LEFT WING FUEL TANK PLATE/PANEL 531 AT, INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION, NICKS AND GOUGES. FABRICATED N EW FUEL PANEL IAW DAC DWG ARB0872, REV "AV". 2 L 7 3 4F RT A22WE 20080529 NM 2008 5 29 CALA0800457 1 20080515 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM BS 400 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17640 28901 FUSELAGE FRAME STA 400 HAS A CRACK BETWEEN S8R AND S9R. FABRICATED AND INSTALLED REPAIR ANGLES PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080529 NM 2008 5 29 YENA2008053 1 20080526 A 2120 UNKNOWN EMB ERJ190 ERJ190100IGW 3260408 NM CABIN SMOKE A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 198JB 19000021 FLT 931, ORD-LGB, STRONG ODOR OF ELECTRICAL SMOKE FROM ROW 6 OR 7 DURING FLIGHT. FLIGHT ATTENDANTS DID NOT SEE ANY SMOK E. INSPECTED SEAT ROWS 3 THRU 10 L & R, LTV SEBS ARE OK. PERFORMED FIM PROCEDURES PER TSM E190 21-20-00-810-801-A. NO PRESENCE OF ELECTRICAL SMOKE OR SMELL. FOUND OK. 2 L 7 2 4F RT A57NM 20080530 NM 2008 5 30 CALA0800472 1 20080519 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM BS 787 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17640 28901 FUSELAGE FRAME CRACKED AT STATION 787 BETWEEN S8R AND S9R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES PER E A 5310-04498. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 CALA0800493 1 20080510 A 5230 146A61101 SKIN BOEING 737 737824 13844BZ NM AFT CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24212 28772 AFT CARGO DOOR STATION 815 AT LOWER INNER SKIN HAS CORROSION. REPAIRED NOTED DAMAGED AREA IAW EC/RA 5232-01101. 2 L 7 2 4F RT A16WE 20080603 EA 2008 6 3 SWIA200819644 1 20080319 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 952SW 7805 FS 280 AT RBL9 UPPER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-536-11-137. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819647 1 20080319 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 952SW 7805 PAX DOOR HANDLE CRACKED ON AFT SIDE, FOUND AT C-CHECK. REPLACED PAX DOOR LATCH LOCK BOX ASSEMBLY AS PER CRJ200 AMM 52-1 1-25-400-801. 2 L 7 2 4F RT A21EA 20080603 NM 2008 6 3 UPS08652240 1 20080512 A 3260 CIRCUIT CARD BOEING 767 76734AF 1385212 NM NLG FAULTY A IPXA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 310UP 27762 INSPECTION TYPE:N/A ON APPROACH, GEAR TO DOWN POSITION, INITIALLY 3 GREEN LEFT, NOSE, RIGHT "ILLUMINATED" LOUD BANG, "GE AR DISAGREE" MSG NOSE AND GEAR LIGHT, FOLLOWED BY TRANSIT "GEAR DISAGREE" MSG AND LIGHT EXTINGUISHING NOSE GEAR LIGHT. REMOVED AND REPLACED PSEU A5 DRIVER CARD (SEE LP 660092/2). ALSO REMOVED AND REPLACED NOSE GEAR ANNUNCIATOR DIODE FUSE CARD & LAMPS IAW AMM 33-16-02-2 & AMM 32-09-06-4 FOR A5 CARD. NOSE JACKED A/C & CYCLED GEAR NUMEROUS TIMES WITH NO DEFE CTS OR FAULTS NOTED. OK FOR A/C TO CONTINUE. 2 L 7 2 4F RT A1NM 20080603 2008 6 3 SWIA200819655 4 20080518 A 3417 8220372445 ADC CNDAIR CL600 CL6002B19 1900309 EA NR 2 MALFUNCTIONED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 403SW 10514 10514 7028 FLT 2805 - RIGHT SIDE ALTIMETER SETTING WILL CHANGE RANDOMLY WHILE SETTING SPEEDS. REPLACED FLIGHT CONTROL PANEL IAW AM M 22-11-07 AND NR 2 ADC IAW MM 34-11-00. OPS CHECK GOOD, P/N 822-0044-001, S/N OFF 2FX8T. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819657 1 20080518 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX OUT OF RIG A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 427SW 7497 FLT 3912 - PASSENGER DOOR IS VERY HARD TO OPEN. RESHIMMED AND RIGGED THE FORWARD LATCH CAMS IAW CRJ MM 52-11-23. OPS C HECK GOOD. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819660 1 20080515 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 716SK 10180 FLT 6149 - SERVICE DOOR EMERGENCY FLOOD LIGHT IS BROKEN. REPLACED EMERGENCY FLOOD LIGHT ASSEMBLY IAW CRJ AMM CHAP 33-51 -11. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819661 1 20080517 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 701SK 10133 FLT 6050 - EMERGENCY LIGHT NEAR SERVICE DOOR IS DAMAGED. REPLACED EMERGENCY EXIT FLOOD LIGHT ASSEMBLY PER CRJ MM 33-51- 11. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080603 NM 2008 6 3 QXEA200800475 1 20080509 A 5310 DOOR FRAME BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 425QX 4039 PDX - C4 CHECK, FRAME AT X1 FORWARD MAIN CABIN DOOR FRAME IS CHAFED INBOARD OF STRINGER 32L. BLENDED OUT AREA .020 INCH REMOVED, WITHIN LIMITS. ALODINED AREA, HFEC FOR CRACKS, NONE FOUND. 2 H 7 2 4T RT A13NM 20080603 WP 2008 6 3 UPS08852237 1 20080512 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK IN REF TO DC8 MM 33-51-01. EMER GENCY POWER OPS NORMAL. 2 L 7 4 4F RT 4A25 20080603 WP 2008 6 3 UPS08852244 1 20080423 A 3260 STRUCTURE DOUG DC8 DC873F 302199F WP RT MLG WW DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 RIGHT GEAR DOOR SWITCH MOUNT HOLES ARE ELONGATED. REPAIRED RIGHT GEAR DOOR SWITCH HOLES IAW EO DC8-3 260-16914-A AND DWG 56 53490. 2 L 7 4 4F RT 4A25 20080603 2008 6 3 UPS08M52236 4 20080512 A 2565 COVER DOUG MD11 MD11F 3023600 NM EVAC SLIDE UNSECURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:N/A L1 DOOR EMERGENCY ESCAPE SLIDE COVER NOT SECURED FLUSH AND RUBBING WHEN DOOR OPENED. RESECURED L1 D OOR SLIDE COVER IAW MM 25-23-07-4-1. 2 L 7 3 4F RT A22WE 20080603 NM 2008 6 3 UPS08M52246 1 20080325 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C CABIN - SEAT TRACK AT STA 791 - 909 X=+75.25 FOUND CORROSION. CORR ON AFFECTED AREA REMOVED MAT'L THK :0.145"(CROWN), MAT'L REMOVED: 0.045"(STA.869-896), MAT'L REMN:0.100". FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK ON EX ISTING SPLICE HAT SECT FROM STA 765 TO STA 909 X=+75.25" REMOVED. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT . NEW SEAT TRACK FROM STA 765-909 X=+75.25" REWORKED & INSTALLED. 2 L 7 3 4F RT A22WE 20080603 NM 2008 6 3 QXEA200800521 1 20080525 A 2611 SMOKE DETECTOR BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY FAILED A QXEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 09 425QX 4039 SEA - FLIGHT 2392 - DURING PILOT DAILY CHECK, DISCOVERED NR 1 AFT BAGGAGE SMOKE DETECTOR FAILED. MAINTENANCE PLACED ON MEL 26-10-2A. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080603 NM 2008 6 3 ASAA0842965 1 20080427 A 5330 65C3578513 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 DOUBLE DRILLED FASTENER HOLE REPAIRED IAW ASA EA 5330 02264. REMOVED REPAIR FASTENER, TRIMMED OUT DAMAGED AREA, FABRICA TED AND INSTALLED REPAIR DOUBLER TRIPLER AND FILLER IAW ASA EA 5330 02337. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 CALA0800474 1 20080519 A 2612 233N6204301 CONTROL PANEL BOEING 757 757224 1384958 NM COCKPIT DEFECTIVE A CALA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 57111 55615 27301 AT 23,000 FT, RT ENG FIRE AND OVERHEAT WARNING CAME ON. ACCOMPLISHED ENGINE FIRE / SHUTDOWN CHECKLIST. FIRE LIGHTS STA YED ON. BLEW BOTH BOTTLES. POSITIVE OIL PRESSURE ON SHUTDOWN, 15 MINUTE WINDMILL ON ENGINE. TROUBLESHOT PER FIM 26-11 -00. FOUND NR 2 ENG TEST CIRCUIT STUCK IN TEST MODE. REPLACED FIRE/OVERHEAT TEST PANEL PER MM 26-11-02. OPS CHECK GOO D. REF LOG PAGES 7992436 AND 7992437 FOR FIRE BOTTLE REPLACEMENT. WINDMILL TIME WITH OIL PRESSURE WITHIN LIMITS OF MM 71-00-00 P605. A/C OK TO CONTINUE. ROTABLE PARTS CHANGE WAS INDICATED - TT 1200263 SN OFF 00392 PANEL, TEST, FI OFF 19 -3111-9-9002 0392 ON 19-3111-9-9002 0504. 2 L 7 2 4F RT A2NM 20080603 NM 2008 6 3 CALA0800505 1 20080424 A 5320 6517785 FASTENER BOEING 737 737524 1384721 NM FUSELAGE MISSING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 INTERCOSTAL INBOARD FRAME TO STIFFENER BRACKET AT STATION 354 S8L IS MISSING (4) FASTENERS. INSTALLED MISSING FASTENERS AT STATION 354 S8L PER EA639-6003CAL AND EC/RA 5310-04753. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 CALA0800507 1 20080531 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 RIGHT FRAME IS CRACKED AT S8R STATION 867. REPAIRED FRAME AT S8R STATION 867 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080603 EA 2008 6 3 REXA200800016 1 20080527 A 7500 34H80150 COUPLING CNDAIR CL600 CL6002B19 1900309 EA BLEED VALVE LEAKING A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 8458A 7458 ON CLIMB-OUT AFTER TAKEOFF FROM KMSP, THE "R 14TH DUCT" WARNING MESSAGE ILLUMINATED FOLLOWED BY THE "BLEED AIR DUCT" AUR AL WARNING. THE FLIGHT CREW RAN THE QRH, DECLARED AN EMERGENCY AND RETURNED TO KMSP. RIGHT ENGINE POWER WAS REDUCED TO IDLE AND AN OTHERWISE NORMAL APPROACH AND LANDING WERE COMPLETED. CFR FOUND NO DAMAGE TO THE ENGINE AND THE AIRCRAFT W AS RELEASED TO THE GATE. MAINTENANCE FOUND THE AFT COUPLING OF THE 14TH STAGE BLEED VALVE TO BE LEAKING. THE COUPLING AND THE PYLON SENSING LOOP WERE REPLACED. MAINTENANCE ALSO COMPLIED WITH AN OVERWEIGHT LANDING INSPECTION ON THE AIRCRA FT. 2 L 7 2 4F RT A21EA 20080603 NM 2008 6 3 QXEA200800519 1 20080527 A 3260 327 LAMP BOMBDR DHC8 DHC8402 1390042 NM MLG INDICATOR INOPERATIVE A QXEA O OTHER P NO WARNING INDICATION AP APPROACH 1 NM 09 403QX 4037 GEG - FLIGHT 2392 - RIGHT MAIN GEAR DID NOT INDICATE DOWN. ALTERNATE INDICATION SHOWED 3 GREEN LIGHTS. CFR CALLED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO PSEU FAULTS. FOUND THE RIGHT GEAR DOWN LAMPS INOP. REPLACED LAMPS. OPE RATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080603 NM 2008 6 3 AALA200801107 1 20080427 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971AN 29547 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 16DEF INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 16DEF. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 AALA200801104 1 20080427 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 751AN 30798 MIA - EMERGENCY LIGHT AT SEAT 21G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080603 NM 2008 6 3 AALA200801105 1 20080427 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 751AN 30798 MIA - EMERGENCY LIGHT AT SEAT 31G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080603 EA 2008 6 3 QXEA200800509 1 20080519 A 3150 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA ILLUMINATED A QXEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 09 602QX 10010 SMF - FLIGHT 2506 - ELEVATOR SPLIT CAUTION MESSAGE. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. C/W F IM 27-31-00-810-A01. MESSAGE CLEARED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 20080701 NM 2008 7 1 AALA200801501 1 20080603 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 780AN 29956 DFW - EMERGENCY LIGHT AT SEAT ROW 31 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 31. SYSTEM GROUND CHE CKED NORMAL OPERATION. (M) 2 L 7 2 4F RT T00001SE 20080701 SO 2008 7 1 LR7A08078 1 20080603 A 5330 SKIN LKHEED 382 382G 526414U SO FS 947 NICKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 4606 FLT 703 - DURING SCHEDULED A CHECK PER JOB CARD HA1200, FOUND FUSELAGE EXTERIOR SKIN NICKED AT FS 947, WL 203, RBL 60.5. REPAIR ACCOMPLISHED IAW SMP583 51-140-12 ON LOG PAGE 27956, ITEM 2. (M) 2 H 7 4 4T A1SO 20080701 EA 2008 7 1 SWIA200819777 1 20080615 A 5610 NP13932113 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 732SK 10194 CAPTAINS FRONT WINDSHIELD CRACKED AT THE GATE. (FLT 5903) REPLACED CAPTAINS WINDSHIELD IAW MM 56-11-01. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819781 1 20080617 A 2622 BA232171 EXTINGUISHER CNDAIR CL600 CL6002B19 1900309 EA LAVATORY DISCHARGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 417SW 21746 21746 7400 LAVATORY TRASH FIRE EXTINGUISHING BOTTLE IS DISCHARGED. (FLT 2778) REMOVED AND REPLACED THE LAVATORY TRASH FIRE BOTTLE AS NEEDED PER MM 26-26-01. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819784 1 20080620 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA NOSE MALFUNCTIONED A SWIA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 07 454SW SELECTED GEAR DOWN AND THE NOSE GEAR WOULD NOT EXTEND AND RECEIVED GEAR DISAGREE WARNING MESSAGE. GEAR THEN EXTENDED NO RMALLY. (FLT 3845) INSPECTED AND PERFORMED OPERATIONAL CHECKS OF NOSE GEAR EXTENSION AND RETRACTION IAW MM 32-33-00 AND 32-32-00. ALL CHECKS GOOD. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819786 1 20080618 A 3230 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAULTY A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 916SW 16299 16299 7634 MAIN LANDING GEAR WOULD NOT EXTEND ON APPROACH. MANUALLY EXTENDED GEAR TO GET THREE GREEN INDICATIONS. (FLT 5985) REP LACED MAIN LANDING GEAR SELECTOR VALVE IAW AMM 32-32-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080701 NM 2008 7 1 SWAA083164 1 20080610 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 921WN 36626 LT FWD FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. R&R LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 SWAA083183 1 20080610 A 5315 6546811 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULE 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 44. REPAIRED FLOOR BEAM PER ER. 2 L 7 2 4F RT A16WE 20080701 NM 2008 7 1 SWAA083182 1 20080610 A 3350 65C27093 LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULE 22Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. R&R LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080711 NM 2008 7 11 AALA200801165 1 20080430 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 623AA 24581 DFW - SEAT EMERGENCY LIGHT EXIT MARKERS AT LEFT AND RIGHT NUMBER FOUR DOOR AND AFT GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT EXIT MARKERS AT LEFT AND RIGHT NUMBER FOUR DOOR AND AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 AALA200801231 1 20080506 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 684AA 25341 DFW - EMERGENCY LIGHT AT SEAT 16D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 AALA200801143 1 20080428 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801139 1 20080428 A 3397 CONNECTOR BOEING 777 777223 1385213 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 753AN 30261 DFW EMERGENCY LIGHTS AT FORWARD AND AFT SEAT 9D INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY LIGHTS AT FORWARD AND AF T SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 WP 2008 7 11 AALA200801242 1 20080507 A 2120 5953625521 DUCT DOUG DC9 DC983 3022083 WP A/C BAY BLOWN A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 978TW 53628 ORD INFLIGHT T2079/07MAY - TAIL COMPARTMENT TEMPERATURE HIGH INDICATION ILLUMINATED DURING CLIMB. LIGHT EXTINGUISHED IN ABOUT FIVE MINUTES. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND WATER SEPARATOR DUCT AT FORWARD RIGHT SIDE OF AFT TAIL COMPARTMENT BLOWN. REPLACED BLOWN DUCT ON FORWARD RIGHT SIDE OF AFT TAIL COMPARTMENT. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080711 EU 2008 7 11 AALA200801243 1 20080507 A 2824 2790475102 TRANSFER VALVE AIRBUS 300 A300B4605R 3930308 EU LT FUEL TANK INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 SW 21 70054 461 BDA INFLIGHT T1692/07MAY SJU TO JFK - CREW REPORTED FUEL IMBALANCE. LANDED BDA WITHOUT INCIDENT. REPLACED LEFT OUTER T ANK VALVE WITH LEFT AFT TRANSFER VALVE AND PLACARDED LEFT AFT TRANSFER VALVE INOPERATIVE. REPLACED LEFT AFT TRANSFER VA LVE AT TUL ON 09 MAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20080711 NM 2008 7 11 AALA200801297 1 20080513 A 2842 HG1057LR02 PROCESSING UNIT BOEING 767 767323 1385205 NM FUEL SYSTEM MALFUNCTIONED A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 362AA 24043 LHR INFLIGHT T049/13MAY CDG TO DFW - CREW REPORTED RIGHT QUANTITY AND TOTAL QUANTITY BLANKED OUT WITH FUEL IMBALANCE IND ICATION. LANDED LHR WITHOUT INCIDENT. REPLACED FUEL QUANTITY PROCESSOR UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080711 NM 2008 7 11 AALA200801305 1 20080514 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW - EMERGENCY LIGHT AT SEAT 31C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 EU 2008 7 11 AALA200801206 1 20080504 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 11060 470 MIA - EMERGENCY LIGHT AT SEAT 12G INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 12G. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20080711 EU 2008 7 11 AALA200801200 1 20080504 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 11060 470 MIA - EMERGENCY LIGHT AT SEAT 6C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 6C. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A35EU 20080711 WP 2008 7 11 AALA200801209 1 20080504 A 3350 TERMINAL DOUG DC9 DC983 3022083 WP CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 984TW 53634 SFO - EMERGENCY LIGHT AT OVERHEAD FROM AFT FIRST CLASS TO SEAT ROW 18 INOPERATIVE. CLEANED BATTERY PACK TERMINAL FOR EM ERGENCY LIGHTS AT OVERHEAD FROM AFT FIRST CLASS TO SEAT ROW 18. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080711 EU 2008 7 11 AALA200801197 1 20080504 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 11060 470 MIA - EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. FOUND PIN PUSHED BACK AT CONNECTOR. SECURED CONNECTOR FOR EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20080711 WP 2008 7 11 AALA200801145 1 20080428 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 588AA 53251 TUL - LOWER WEB AT AFT LAVATORY SERVICE COMPARTMENT AFT END AFT CARGO HAS CORROSION AT STATION 1300 TO 1320. REPLACED F OUR INSIDE DOUBLERS IN ACCORDANCE WITH ENGINEERING SPECIFICATION ORDER 80559 DATED 23 APR 2008. 2 L 7 2 4F RT A6WE 20080711 WP 2008 7 11 AALA200801208 1 20080504 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 433AA 49451 SFO - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 21D TO 32D INOPERATIVE. REPLACED BATTERY PACK AT AB53 FOR SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 21D TO 32D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080711 NM 2008 7 11 AALA200801186 1 20080503 A 1100 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 648AA 24606 DFW - EMERGENCY LIGHT EXIT PLACARD AT LEFT FORWARD OVERWING DAMAGED. REPLACED PLACARD FOR EMERGENCY LIGHT EXIT PLACARD AT LEFT FORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 AALA200801236 1 20080506 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 755AN 30263 DFW - EMERGENCY LIGHT AT SEAT 21C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 WP 2008 7 11 AALA200801155 1 20080430 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 485AA 49678 BOS - EMERGENCY LIGHTS FROM SEAT ROW 21 TO AFT OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FROM SE AT ROW 21 TO AFT OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080711 NM 2008 7 11 AALA200801129 1 20080428 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801164 1 20080430 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 623AA 24581 DFW EMERGENCY LIGHTS AT SEAT ROWS 26D TO 36D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 26D TO 36D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 EU 2008 7 11 AALA200801239 1 20080506 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 18066 509 MIA - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20080711 NM 2008 7 11 AALA200801303 1 20080514 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW - EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801308 1 20080514 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW - EMERGENCY LIGHT AT SEAT 23G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 WP 2008 7 11 AALA200801252 1 20080508 A 2120 DUCT DOUG DC9 DC983 3022083 WP A/C BAY LEAKING A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 9617R 53564 MCI INFLIGHT T1964/08MAY - CREW REPORTED ACCESSORY COMPARTMENT OVERHEAT INDICATION. RETURNED TO MCI AND LANDED WITHOUT INCIDENT. FOUND RIGHT TEMPERATURE CONTROL VALVE DUCT BOOT LEAKING. REPLACED BOOT AND CLAMPS FOR RIGHT TEMPERATURE CON TROL VALVE DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080711 NM 2008 7 11 AALA200801173 1 20080501 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT EXIT MARKER AT AFT BULKHEAD RIGHT SIDE MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT EXIT MARKE R AT AFT BULKHEAD RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801229 1 20080506 A 3350 LENS BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 935AN 30081 DFW - EMERGENCY LIGHT AT SEAT ROW 22 HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 22. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080711 NM 2008 7 11 AALA200801131 1 20080428 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT SEAT 26C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801217 1 20080505 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN MALFUNCTIONED A AALA K NONE O OTHER UK UNKNOWN 1 SW 21 945AN 30085 MIA INFLIGHT T1409/05MAY - CREW REPORTED EMERGENCY LIGHTS IN THE ARMED POSITION. EMERGENCY LIGHTS STAYED ON IN THE MAI N CABIN IN FLIGHT. RESET EMERGENCY LIGHT CIRCUIT BREAKER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080711 WP 2008 7 11 AALA200801240 1 20080506 A 2810 FUEL CAP DOUG DC9 DC982 3022082 WP RT WING DEPARTED A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 SW 21 493AA 49731 DAY INFLIGHT T1237/06MAY - CREW REPORTED RIGHT OVERWING FUEL CAP CAME OFF WITH LOSS OF FUEL. REPLACED RIGHT FUEL CAP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080711 NM 2008 7 11 AALA200801175 1 20080501 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 901AN 29503 MIA - EMERGENCY LIGHT AT WING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT WING. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A16WE 20080711 NM 2008 7 11 AALA200801216 1 20080505 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 DFW - EMERGENCY LIGHT AT SEAT 22G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801196 1 20080504 A 3350 LIGHT BOEING 757 757223 1384957 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 194AA 32388 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 AALA200801172 1 20080501 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 754AN 30262 DFW - EMERGENCY LIGHT EXIT MARKER AT FORWARD LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT EXI T MARKER AT FORWARD LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801138 1 20080428 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT SEAT 23G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801152 1 20080429 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 654A 24612 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 25D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 08FDEA01938 1 20080521 A 5313 BAC1498143 STRINGER BOEING 727 727233 138408A NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 274FE 22039 FWD CARGO COMPT STR 28R LEVELING COMPOUND IS CRACKED AND BULGING AT SPLICE STA 680 PLUS 10 INCHES CUT OUT DAMAGED AREA A PPROX DIM 6 3/8 INCH LENGTH, FABRICATED REPAIR SPLICE FROM BAC1498-132 PO NR 8177148 DIM 19 1/2 INCH LENGTH AND FILLER F ROM BAC1498-143 PO NR 8177148 DIM 6 3/8 INCH LENGTH. INSTALLED REPAIR PARTS AT BS 680 10 INCH STR 28R IAW B727 SRM 53- 10-3 FIG 1 SRM 53-10-2 FIG 9 AND SRM 51-30-2. 2 L 7 3 4F RT A3WE 20080711 NM 2008 7 11 08FDEA01972 1 20080523 A 5330 155PH SKIN BOEING 757 75723A 1384967 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 EXTERNAL PATCH REPAIR ON NR 2 RT DOOR UPPER HINGE CUT-OUT TO BE EVALUATED. REPAIR CARRIED OUT AS PER EA F-5240-118832. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA.B 2 L 7 2 4F RT A2NM 20080707 NM 2008 7 7 UPS08M52284 1 20080329 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C CABIN - CORROSION ON SEAT TRACK CROWN & CHANNEL AT STA 893 X=107. CORROSION ON AFFECTED AREA REMOVED. MAT'L THK:0.145" (CROWN), MAT'L REMOVED:0. 045", MAT'L REMN:0.100" FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK ON EXIST SPLICE HAT SECT FROM STA 889 TO STA 969, X=107 REMOVED. HFEC INSP C/O ON TRIM OFF AREA, FOUND NO CRACK EVIDENT. NEW S EAT TRACK FROM STA 889-969 X=107 REWORKED. NEW SEAT TRACK HOLES PICK-UP, RE-PROTECTED, PAINTED & INSTALLED. 2 L 7 3 4F RT A22WE 20080707 NM 2008 7 7 2008UALA02825 1 20080515 A 2120 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN ODOR A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 815UA 867 AFTER START GOT AN ACRID SMELL THROUGHOUT ENTIRE AIRCRAFT. 2 L 7 2 4F 4 F RT A28NM E40NE 20080707 NM 2008 7 7 USAA920081089 1 20080517 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 308AW 24710 FLT 490/PHX - EMERGENCY EQUIPMENT - ONE OF THE AFT GALLEY FLASHLIGHTS IS NOT WORKING. MAINTENANCE REPLACED THE AFT FLAS HLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 20080707 EA 2008 7 7 SWIA200819633 1 20080128 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 988CA 7204 STA 280 FLOOR SUPPORT IS CRACKED JUST OUTBOARD OF LBL 9, FOUND AT C-CHECK. COMPLETED REPAIR IAW BOMBARDIER REO 601R-53- 11-136A. 2 L 7 2 4F RT A21EA 20080707 NM 2008 7 7 MWEA080072 1 20080519 A 5753 9935942502 SKIN DOUG MD88 MD88 3023688 NM T/E FLAP DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 823ME 49766 RIGHT WING SMALL DENT ON LOWER SURFACE OF INBOARD TRAILING EDGE FLAP 17' FORWARD OF AFT TRAILING EDGE AT APPROXIMATELY X FLS117.0. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 20080708 NM 2008 7 8 2008UALA02866 1 20080518 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 305UA 23666 STA 294.5 FRAME AT STR 11L HAS TOOLING MARK. 2 L 7 2 4F 4 F RT A16WE E2GL 20080708 2008 7 8 2008UALA02871 4 20080518 A 2350 MICROPHONE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT INOPERATIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 848UA 1647 FO'S OXYGEN MASK MICROPHONE IS INOPERATIVE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080708 NM 2008 7 8 2008UALA02876 1 20080517 A 3350 1619 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 315UA 23947 EMERGENCY SLIDE LIGHT INOP DOOR 2R. RELAMPED. 2 L 7 2 4F 4 F RT A16WE E2GL 20080708 NM 2008 7 8 2008UALA02903 1 20080519 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 EXT FUSELAGE SKIN CRACKED AT CHEM MILLED STEP BS 727E +2" AND STRINGER S-18L. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACK DAMAGE. ACCMP'D NDT FOR CRACK CONTAINMENT & ACCMP INSURANCE CUT. ACCMP NDT OF OPEN HOLES COMMON TO REPAIR. FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 20080708 SO 2008 7 8 C2XA08SH078 1 20080522 A 5751 14569384001 ATTACH BRACKET EMB 145 EMB145LR 3260212 SO AILERON DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14920 145380 LEFT DAMPER ATTACHMENT BRACKET ON AILERON SPAR O/B HAT BUSHING IS MIGRATED. MX REMOVED AND REPLACED LEFT AILERON DAMPER ATTACH BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 20080708 NM 2008 7 8 AALA200801111 1 20080427 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 958AN 30091 DFW - EMERGENCY LIGHT AT SEAT 11D MISSING LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 11D. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 DHL2008764502 1 20080519 A 5311 FRAME BOEING 727 727264 138408M NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C CHECK REF N/R 098174, DENT AT MAIN CABIN FRAME AT BS 520 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40 -3 FIG 1 AND 53-10-2 FIG 3 MAT, 7075-T6 .050" DIM 5 1/8 INCH BY 8 1/4 INCH PO NR 9006742. 2 L 7 3 4F A3WE 20080708 NM 2008 7 8 DHL2008764503 1 20080519 A 5311 FRAME BOEING 727 727264 138408M NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C CHECK REF N/R098179, DENT AT MAIN CABIN FRAME BS 660 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 F IG 1 AND 53-10-2 FIG 3 DOUBLER MATERIAL 7075-T6 .050 DIM 7 1/8 INCH BY 5 1/4 INCH PO NR 9006742. 2 L 7 3 4F A3WE 20080708 NM 2008 7 8 DHL2008764512 1 20080520 A 5347 SEAT TRACK BOEING 727 727264 138408M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 CORRODED SEAT TRACK RBL 24 BS 1110-1135. SEAT TRACK CORRODED FROM RBL 24 FROM BS 1070 TO 1136 IAW B727 SRM 51-30-2 AND 53-10-1 FIG 3. FAB NEW SECTION WITH BAC 1520-792-7178-T6 DIM 5'6" AND PO 9006020 IAW B727 SRM 53-10-5 FIG 1. 2 L 7 3 4F A3WE 20080708 NM 2008 7 8 DHL2008765513 1 20080521 A 5347 SEAT TRACK BOEING 727 727264 138408M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 CORRODED SEAT TRACK RBL 45 BS 1110-1135. SEAT TRACK AT RBL 45 BS 950 TO 1183 CORRODED OUT OF LIMITS IAW B727 SRM 53-10- 1 FIG 3. FAB NEW SECTION OF SEAT TRACK WITH BAC 1520-792-7178-T6 DIM 15'7 INCH AND PO 9006864 AND TWO ANGLES FOR SPLICE S WITH BAC 1503-100122-7178-4381. DIM 13 INCH EACH AND ONE STRAP WITH .250 INCH 7075-T6 DIM 7 INCH AND PO 9005865 IAW B 727 SRM 53-10-5 FIG 1. 2 L 7 3 4F A3WE 20080708 NM 2008 7 8 P5CA0801564 1 20080522 A 5522 SKIN BOEING 747 74746NF 13848BT NM RT ELEVATOR DAMAGED A P5CA K NONE O OTHER TX TAXI/GRND HDL 1 EA 15 452PA 30810 DURING MAINTENANCE, THE RIGHT INBOARD ELEVATOR'S TRAILING EDGE APPROXIMATELY 5 INCHES FROM INBOARD EDGE OF THE ELEVATOR WAS STRUCK AND DAMAGED BY THE CHERRY PICKER. INSPECTED AREA AND ACCOMPLISHED INTERIM REPAIR IAW EO 4455A025. 2 L 7 4 4F RT A20WE 20080708 WP 2008 7 8 ARWA20080504 1 20080517 A 3697 WIRE DOUG DC10 DC1030 3023501 WP REGULATOR VALVE BROKEN A ARWA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 526MD 46998 NR 3 ENGINE PNEUMATIC PRESSURE GAUGE INDICATING 40 PSI W/PNEUMATIC SUPPLY SWITCH IN THE OFF POSITION. REPAIRED BROKEN W IRE AT ELECTRICAL CONNECTOR ON NR 3 ENGINE PNEUMATIC PRESSURE REGULATOR VALVE IN ACCORDANCE WITH DC10 M/M 36-12-01 AND O PERATIONAL CHECK FOUND NORMAL IN ACCORDANCE WITH DC10 M/M 36-12-01. 2 L 7 3 4F A22WE 20080708 NM 2008 7 8 SWAA082840 1 20080525 A 3350 101073 LENS BOEING 737 7373G7 1384595 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 AFT CABIN EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 CALA0800516 1 20080602 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 STATION 747 BETWEEN S8R & S9R IS CRACKED. INSTALLED REPAIR DOUBLERS AND COLD WORKED 6 EA HOLES PER EA 5310-04498 OP 02. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 DL757080859 1 20080612 A 5347 SEAT TRACK BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 MAIN CABIN SEAT TRACK STARTING AT FS 630 LBL 45 TO FS 790 HAS NUMEROUS AREAS OF CORROSION DAMAGE. REPAIRED SEAT TRACK I AW SRM 53-30-52. 2 L 7 2 4F RT A2NM 20080708 NE 2008 7 8 2008UALA02696 2 20080509 A 7240 COMBUST CHAMBER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 ENGINE DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 204UA 28713 222174 NR 1 ENGINE COMBUSTION CHAMBER DAMAGE BEYOND LIMITS. FOUND COMBUSTION CHAMBER CLAMP PROTRUDING INTO THE GASPATH. ENGINE REPLACED PRIOR TO FURTHER FLIGHT. TEARDOWN REVEALED THAT THE COMBUSTION CHAMBER CLAMP (C/C CLAMP) HAD BROKEN AT THE 3 O 'CLOCK POSITION. ROOT CAUSE WAS THAT THE INNER BURNER LINER HAD NOT BEEN INSTALLED PROPERLY. CONSEQUENTLY, A 12-INCH SEC TION OF THE CLAMP WAS NOT FULLY SEATED IN THE OUTER BURNER LINER. THIS RESULTED IN COOLING AIR LEAKING FROM THE O.D. OF THE COMBUSTOR. THIS CAUSED EXCESSIVE CLAMP RUB AND SUBSEQUENT BREAKAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080708 NM 2008 7 8 2008UALA02697 1 20080507 A 2160 CONTROL SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN TEMP MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 547UA 25368 CAN'T CONTROL COCKPIT OR CABIN TEMP WITH OR WITHOUT TRIM AIR EITHER TO HOT OR TO COLD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080710 2008 7 10 R61A200800007 4 20080523 A 3160 DISPLAY EMB ERJ170 ERJ170100SU 3260403 NM COCKPIT MALFUNCTIONED A R61A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 826MD 17000046 CREW REPORTED F/O'S MFD FLICKERED AND THEN WENT BLANK, MOMENTS LATER HAD AN ELECTRICAL SMELL IN THE COCKPIT. THERE WERE NO EICAS MSGS PRESENTED AND NO C/B'S TRIPPED. 2 L 7 2 4F RT A56NM 20080710 NM 2008 7 10 2008UALA02925 1 20080521 A 2997 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HYD SYSTEM DIRTY A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 661UA 27158 RIGHT HYDRAULIC SYSTEM PRESSURE FAILURE. RT HYD SYS PRESS LIGHT & RT HYD SYS ELEC DEMAND PUMP PRESS LIGHT ALONG WITH B RAKE SOURCE LIGHT ALL. VERBAL REPORT FROM FLT CREW. EVERYTHING NORMAL ON REST OF FLT. MOTORED RT ENG & OPERATED RT ELEC HYD PUMP. UNABLE TO DUPLICATE ITEM. MX CLEANED CONNECTOR AT PRESS TRANSMITTER & RAN ENGINE PER JRH2-6-1 AND TEST HYD P ER JRH2-6 -8. ALL TEST PASSED. ALSO TEST HYD PRESS INDICATION IAW AMM 29-31-0 0 ALL TEST PASSED. 2 L 7 2 4F 4 F RT A1NM E24NE 20080710 NM 2008 7 10 2008UALA02950 1 20080521 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 INTERCOSTAL CRACKED AT BS 680 BETWEEN STR 11R AND STR 12R. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW INTERCOSTAL (P/N 1 43N8338U26). 2 L 7 2 4F 4 F RT A2NM E17NE 20080710 NM 2008 7 10 2008UALA02954 1 20080521 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 AFT PIT STA 1540 BETWEEN STR 25R AND 26R FRAME DENTED. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE. INSTALLED ANGLE REP AIR. INSTALLED NEW SPLICE PLATE & 2EA STR CLIPS (P/N 140N2001). 2 L 7 2 4F 4 F RT A2NM E17NE 20080710 NM 2008 7 10 USAA920081106 1 20080510 A 5314 BAC15202167 KEELBEAM BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 MIA - MAJOR REPAIR - C4 CHECK - CORROSION ON KEEL BEAM LOWER CHORD, BS 961 - BS 1006.75, RBL 9.5. REPAIRED KEEL BEAM LO WER CHORD, BS 961 - BS 1006.75, RBL 9.5. IAW SRM 53-50-12. 2 L 7 2 4F RT A1NM 20080529 NM 2008 5 29 CALA0800456 1 20080515 A 5320 65C3397337 INTERCOSTAL BOEING 737 737524 1384721 NM BS 328-344 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17640 28901 FLOOR SUPPORT STA 328 TO 344 LBL 45 CRACKED. REMOVED AND REPLACED CRACKED FLOOR SUPPORT REF SRM 51-40-02 PAGE 1 FIG 3. 2 L 7 2 4F RT A16WE 20080529 NM 2008 5 29 CALA0800477 1 20080521 A 5312 148A22881 BULKHEAD BOEING 737 737724 13844BY NM DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 29717 28936 DENT IN AFT PRESSURE BULKHEAD STR 12 C, WATERLINE 246. REPAIRED DAMAGE TO AFT PRESSURE BULKHEAD AT STRINGER 12L, WATERL INE 246 IN COMPLIANCE WITH SRM 53-80-08 REPAIR 1, ECRA 5344-01001. 2 L 7 2 4F RT A16WE 20080530 EU 2008 5 30 YENA2008051 1 20080525 A 2150 759D000002 CONTROLLER AIRBUS 320 A320232 3930326 EU A/C PACK MALFUNCTIONED A YENA B EMER. DESCENT B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 15 524JB 15924 2074 1528 INFLIGHT ECAM "FWS SDAC 2 FAULT" FOLLOWED BY STRONG ELECTRICAL TYPE SMELL IN THE COCKPIT. REMOVED & REPLACED NR 2 SDAC & OPS OK PER MM 31-55-34. CIRCUIT BREAKERS Y18 AND Y19 TRIPPED IN FLT PACK NR 1 INDICATION LOST DESCENDED TO FL 300. R EMOVED & REPLACED NR 1 PACK CONTROLLER & OPS OK PER MM 21-61-34. PERFORMED TSM TASKS 24-00-00-810-823 & 24-00-00-810-80 3, FOUND SMELL FROM SDAC NR 2 AND PACK CONT NR 1 CAUSING FAULTS & SMELL. REMOVED AND REPLACED SDAC NR 2 & PACK CONT NR 1. SEE SDR YENA2008050 FOR NR 2 SDAC REPLACEMENT. 2 L 7 2 4F RT A28NM 20080530 NM 2008 5 30 CALA0800494 1 20080528 A 5311 6546557 FRAME BOEING 737 737524 1384721 NM BS 787 S8L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 LEFT-HAND STATION 787 AT S8L AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED CRACKED FRAME AT LEFT- HAND STATION 787 S8L PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080530 NM 2008 5 30 HALA0800591 1 20080517 A 5720 SEAL BOEING 767 76733A 1385209 NM RT WING TORN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 BLADE SEAL TORN ON RIGHT WING O/B AILERON UPPER BLADE. REPLACED UPPER BLADE SEAL ON RIGHT WING O/B AILERON AT TORN AREA IAW SRM 51-40-02-OG-0. 2 L 7 2 4F RT A1NM 20080603 EA 2008 6 3 N6WA0080505 1 20080522 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 155GJ 10225 CEILING EMERGENCY LIGHT 5 BACK IS INOP. DEFERRED IAW MEL 33-51-01-2. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819678 1 20080521 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 411SW 7067 FLT 3757 - RIGHT WING FORWARD EMERGENCY EXIT LIGHT IS INOP. REPLACED EMERGENCY BULB. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819626 1 20080513 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 932SW 7714 FLT 6139 - CAPTAINS SIDE WINDOW IS CRACKED. REPLACED SIDE WINDOW IAW MM 56-12-01, P/N: NP139322-11, S/N OFF: 02211H2546 . 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819627 1 20080511 A 3230 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 405SW 7029 FLT 6377 - WHEN EXTENDING GEAR ON APPROACH, RECEIVED A "GEAR DISAGREE" MESSAGE. MANUALLY EXTENDED THE GEAR. REPLACED M AIN GEAR SELECTOR VALVE IAW 32-32-10. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819683 1 20080524 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 952SW 7805 FLT 6065 - MAIN GEAR DID NOT EXTEND ON APPROACH. COMPLIED WITH MANUAL EXTENSION AND LANDED NORMALLY. INSPECTED AND OPE RATED LANDING GEAR SYSTEM THROUGH SEVERAL CYCLES WITH NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A21EA 20080603 EU 2008 6 3 MALA080106 1 20080515 A 5311 FRAME SAAB SF340 340B 7860101 EU BS 360 TORN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 442XJ 340B442 DENT AND TEAR IN FRAME FLANGE FS 630.112 RIGHT SIDE JUST ABOVE SEAT TRACK. COMPLIED WITH MESABA EOS53152 AND APPLICABLE SECTIONS OF 340 SRM CHS 51-20, 51-40 AND 51-70 FOR THE DENT IN THE RT SIDE FLANGE AT FS 630.112. CUT OUT DAMAGED FRAME FLANGE SECTION, FABRICATED FILLER AND INNER FRAME SPLICE AND INSTALLED. NO FURTHER ACTION REQUIRED. 2 L 7 2 4T RT A52EU 20080603 NM 2008 6 3 UPS08652238 1 20080512 A 3243 SHUTTLE VALVE BOEING 767 76734AF 1385212 NM RT BRAKE MALFUNCTIONED A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 315UP 27743 INSPECTION TYPE:N/A A/C PULLED LEFT USING AUTOBRAKES. RIGHT BRAKES INOP. REMOVED AND REPLACED AUTOBRAKE SHUTTLE VALVE PER MM 32-42-10-4, NO HELP. REMOVED AND REPLACED NORMAL AUTO SKID MODULE PER MM 32-42-02-4. GROUND OPS CHECKS GOOD AND LEAK CHECKS GOOD, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20080603 EA 2008 6 3 QXEA200800516 1 20080525 A 2730 8221310104 DCU CNDAIR CL600 CL6002C10 1390015 EA ELEVATOR SYS MALFUNCTIONED A QXEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 09 602QX 12727 479 10010 PDX - FLIGHT 2521 - RETURNED TO THE FIELD FOR ELEVATOR SPLIT CAUTION MESSAGE. MAINTENANCE REPLACED THE NR 1 AND NR 2 D CU'S AS A PRECAUTION. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 20080603 NM 2008 6 3 USAA920081074 1 20080421 A 5310 146N852247 DOOR FRAME BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - CORROSION ON AFT CARGO COMPARTMENT DOOR CUTOUT OUTBOARD CHORD, BS 1374 - BS 1376, S27R. REPAIRED AFT CARGO COMPARTMENT DOOR CUTOUT OUTBOARD CHORD, BS 1374 - BS 1376, S27R IAW USAIRWAYS EA 130016. 2 L 7 2 4F RT A2NM 20080603 NM 2008 6 3 QXEA200800511 1 20080520 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM MAIN PAX LACK OF LUBE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 400QX 4030 PDX - FLIGHT ATTENDANT REPORTS THAT THE AFT PASSENGER DOOR IS HARD TO MOVE. MAINTENANCE CLEANED AND LUBED THE DOOR. OP ERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080603 NM 2008 6 3 QXEA200800514 1 20080523 A 5210 SEAL BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR DIRTY A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 400QX 4030 SEA - FLIGHT 2215 - AFT CABIN DOOR DIFFICULT TO OPEN. MAINTENANCE CLEANED THE SEAL. OPERATIONAL CHECKS GOOD, AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080711 NM 2008 7 11 UPS08M52335 1 20080506 A 5321 WSP0790501 PANEL DOUG MD11 MD11F 3023600 NM MAIN CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C MAIN CARGO RCB PNL NR 2 HAS CORROSION DAMAGE 3 PLACES ON TOP FACE. LOCATED AND DRILLED REPLACEMENT PANEL IAW MD-11 SRM 51-31-01 AND INSTALLED ON E0 MD11-5330-27218-B. 2 L 7 3 4F RT A22WE 20080711 EU 2008 7 11 AALA200801201 1 20080504 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 11060 470 MIA - EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A35EU 20080711 WP 2008 7 11 AALA200801223 1 20080506 A 3350 LENS DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 575AM 53152 ORD EMERGENCY EXIT SIGN LIGHT AT RIGHT AFT LAVATORY MISSING LENS. REPLACED LENS FOR EMERGENCY EXIT SIGN LIGHT AT RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080711 WP 2008 7 11 AALA200801264 1 20080509 A 8012 9794104 START VALVE DOUG DC9 DC983 3022083 WP LT ENGINE INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 9624T 53594 LAX INFLIGHT T1928/09MAY - NUMBER ONE ENGINE START VALVE INDICATION ILLUMINATED. RETURNED TO LAX AND LANDED WITHOUT INC IDENT. REPLACED START VALVE FOR NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080711 WP 2008 7 11 AALA200801207 1 20080504 A 3350 P4010051111 MODULE DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 433AA 49451 SFO - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROWS 21D TO 32D INOPERATIVE. REPLACED MODULE FOR SEAT MOUNTED EMERGENCY LIG HT AT SEAT ROWS 21D TO 32D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20080711 NM 2008 7 11 AALA200801219 1 20080505 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 781AN 29586 MIA - MOUNTED EMERGENCY LIGHT AT FIRST CLASS GALLEY CLOSET BROKEN. REPLACED LIGHT FOR MOUNTED EMERGENCY LIGHT AT FIRST CLASS GALLEY CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801228 1 20080506 A 3350 LENS BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 935AN 30081 DFW - EMERGENCY LIGHT AT SEAT ROW 17 HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 17. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080711 2008 7 11 AALA200801194 4 20080504 A 3418 COMPUTER DOUG DC9 DC982 3022082 WP STALL WARNING FAILED A AALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 21 407AA 49318 DFW INFLIGHT T1487/04MAY - ON FINAL APPROACH AUTO SLAT FAIL INDICATION WHILE EXTENDING SLATS FROM 11 TO 15. FAIL LIGHT EXTINGUISHED WHEN SLAT BACK TO 11 AND ILLUMINATED WHEN SLATS TO 15. INDICATION WHEN OUT THREE TO FOUR MINUTES LATER. CREW ABORTED LANDING AND ACCOMPLISHED A GO AROUND TO ENSURE AIRCRAFT WAS CONFIGURED PROPERLY. LANDED DFW WITHOUT INCIDE NT. REPLACED NUMBER TWO STALL WARNING COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080711 WP 2008 7 11 AALA200801150 1 20080429 A 7931 1163P0041 PRESSURE SWITCH DOUG DC9 DC982 3022082 WP NR 1 ENGINE DEFECTIVE A AALA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 464AA 49594 SFO INFLIGHT T2426/29APR SJC TO DFW - NUMBER ONE ENGINE OIL CLOG LIGHT ILLUMINATED ON CLIMB-OUT. PER CHECKLIST SHUT DOW N NUMBER ONE ENGINE. OIL TEMPERATURE AT IDLE WAS 110 DEGREES. SINGLE ENGINE TIME 30 MINUTES. LANDED SFO WITHOUT INCID ENT. REPLACED OIL SYSTEM DIFFERENTIAL PRESSURE SWITCH AND OIL FILTER. DOWNLOADED FLIGHT DATA RECORDER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080711 NM 2008 7 11 DHL2008764520 1 20080522 A 2782 BRACKET BOEING 727 727264 138408M NM KRUEGER FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 NR 2 K-FLAP ACTUATOR, TRUNNION MOUNTING BRACKETS CRACK INDICATION (WS 235 APPROX). REMOVED NR 2 K-FLAP TRUNNION MOUNTIN G BRACKETS FROM ACTUATOR WS 235 IAW B727 SRM 51-30-2. FAB NEW BRACKETS WITH 2024-T3 .063" DIM 9" X 6.5 AND PO 9006773 I AW BOEING ENGINEERING DWG 65-16269. 2 L 7 3 4F A3WE 20080711 NM 2008 7 11 DHL2008764521 1 20080522 A 5311 FRAME BOEING 727 727264 138408M NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 DENTS ON MAIN CABIN FRAME BS 640 BETWEEN STR 16 AND 17R. CUT OUT DAMAGED AREA AT FRAME BS 640 BETWEEN STR 16 & 17 RT AP PROX 7/8" X 1", FAB DOUBLER REPAIR WITH 7075-T6 .050", DIM 7" X 5" AND PO 9006742 IAW B727 SRM 53-10-2 FIG 3 AND 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20080711 NM 2008 7 11 DHL2008764522 1 20080522 A 2782 MOUNT BRACKET BOEING 727 727264 138408M NM KRUEGER FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 NR 1 K-FLAP ACTUATOR TRUNNION MOUNTING BRACKETS CRACK INDICATION WS 305. REMOVED NR 1 K-FLAP MOUNTING BRACKETS WS 305 I AW B727 SRM 51-30-2. FAB NEW BRACKETS WITH 2024-T3 .063", DIM 7.5" X 4" AND PO 9006027 IAW BOEING ENGINEERING DWG 65-16 275. 2 L 7 3 4F A3WE 20080711 NM 2008 7 11 KCSA081258 1 20080526 A 5347 SEAT TRACK BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 FIRST OFFICERS FWD O/B SEAT TRACK CRACKED AT FWD STOP BS 320, RBL-36. 2 L 7 4 4F RT A20WE 20080711 EA 2008 7 11 MASA200800412 1 20080521 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27173 7173 ASH FLT 7236, ORD-MSN - PAX DOOR PRESSURE FLAP HARD TO CLOSE. LUBED HANDLE AND PERFORMED OP CHECKS WITH NO DEFECTS. 2 L 7 2 4F RT A21EA 20080711 EA 2008 7 11 MASA200800414 1 20080523 A 5297 WIRE CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR DAMAGED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 915FJ 15015 ASH FLT 2774 DEN-PHX - MAIN DOOR CAUTION MESSAGE WITH DOOR CLOSED AND LOCKED. REPAIRED WIRES ON PX107, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080711 EA 2008 7 11 MASA200800424 1 20080526 A 5240 601R383055 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37178 7178 ASH 2823 PHX - SERVICE DOOR ASSIST HANDLE BROKEN. MX REPLACED THE DOOR HANDLE. 2 L 7 2 4F RT A21EA 20080711 NM 2008 7 11 ASAA0842992 1 20080518 A 5755 SKIN BOEING 737 737490 1384715 NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 NR 5 SPOILER DENTED AT UPPER OTBD SURFACE. PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLERS IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080711 NM 2008 7 11 08FDEA02051 1 20080530 A 5315 BAC1505100617 FLOORBEAM BOEING 757 75723A 1384967 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 UNRECORDED EXISTING REPAIR FOUND ON FLOORBEAM AT BS 1640, BETWEEN LBL 4 AND RBL 4 TO EVALUATE EXISTING REPAIR. EXISTING REPAIR FOUND ACCOMPLISHED IAW B757-200 SRM 53-00-51 FIG 201, REPAIR 3, BASED ON EXTERNAL VISUAL EVALUATION ON THE SHAPE , LOCATION, SIZE, MATERIAL THICKNESS, TYPE AND GENERAL WORKMANSHIP OF THE REPAIR. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 DL76S080838 1 20080607 A 2740 TRIM SYSTEM BOEING 767 767332 1382001 NM STAB MALFUNCTIONED A DALA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 27 138DL 25409 UNSCHEDULED STAB TRIM 3X DURING T/O ROLL. RTO AND RTN GATE. NO HIST, T/S PER FIM 27-09-00 FIG 106A. SAMS AND FSPM BIT E CHK GOOD. RAN STAB FROM BOTH COLUMNS AND CTR PEDESTAL FULL TRAVEL NO EICAS MSGS. ALL CHKS OK. A/C OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20080714 NE 2008 7 14 DL76G080839 2 20080607 A 7320 EEC BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1608 30573 704871 AFTER 35 MINUTES OF TAXI, LEFT THROTTLE WAS ADVANCED AND THERE WAS NO ENGINE RESPONSE. LEFT ENGINE REMAINED AT IDLE REG ARDLESS OF THROTTLE POSITION. NO EICAS MESSAGE OR EEC LIGHTS DISPLAYED. ONCE APU WAS STARTED AND ELEC PWR SWAPPED CONT ROL RETURNED TO LEFT THROTTLE AND ENGINE. REMOVED AND REPLACED LT ENG EEC IAW MM, OPS CKS OK. ETOPS CATEGORY 'D': INAB ILITY TO CTRL ENG OR GET DESIRED PWR. 2 L 7 2 4F 4 F RT A1NM E13NE 20080714 NM 2008 7 14 DL757080846 1 20080609 A 5330 SKIN BOEING 757 757232 1384965 NM BS 330 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 689DL 27172 FUSELAGE SKIN LIGHTNING DAMAGE AT FS 330, S-26R. DAMAGE CUT OUT AND REPAIRED WITH DOUBLERS. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 DLM88080848 1 20080610 A 2910 HYDRAULIC SYSTEM DOUG MD88 MD88 3023688 NM LEFT UNKNOWN A DALA O OTHER K FLUID LOSS DE DESCENT 1 SO 27 928DL 49715 LEFT HYD SYSTEM FAILED IN FLIGHT. LEFT HYD PRESS WENT TO ZERO WITH INCREASING QTY. QTY BEFORE EVENT 11, AFTER 19. ALT ITUDE FL330 AUX PUMP OFF WHEN SPEEDBRAKE APPLIED. RAN ELECTRIC PUMPS, BLEED ALL AIR AND FOAM. RAN ENGINES, BLED ALL AI R AND FOAM AGAIN. SERVICED LEFT AND RIGHT SYSTEMS TO FULL PER M/M. SYSTEM HAS GOOD PRESSURE. 2 L 7 2 4F RT A6WE 20080714 EU 2008 7 14 USAA920081107 1 20080522 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 3930316 EU CABIN DISCHARGED A USAA K NONE L L NO TEST NO TEST IN INSP/MAINT 1 EA 19 121UW 36817 1863 1294 FLT 769 BOS - EEL - AFT LEFT EMERGENCY POWER SUPPLY UNIT FAULT LIGHT IS ON. MAINTENANCE REMOVED AND REPLACED THE AFT LE FT EPSU PER AMM 33-51-38-400-002. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 20080714 EU 2008 7 14 UPS08152347 1 20080523 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 144UP 0827 INSPECTION TYPE:N/A GLARESHIELD EMERGENCY LIGHT 91LE INOP. RELAMPED, OPS CK GOOD PER MM 33-12-23. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 UPS08652341 1 20080524 A 5720 114T2300271 WEB BOEING 767 76734AF 1385212 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 302UP 27240 INSPECTION TYPE:N/A LEFT WING LES 675 FWD OF REFUEL PANEL LOWER CHORD FOUND CRACK. LEFT WING FWD D-NOSE FAIRING SUPPORT WEB REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02, JUST BETWEEN OSS648 AND 694 REFER NRC50623 FOR WORK ING DETAIL. 2 L 7 2 4F RT A1NM 20080714 EU 2008 7 14 08FDEA02421 1 20080624 A 5753 A5796011120200 SKIN AIRBUS 300 A300F4605R 3930327 EU ZONE 600 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 RT INBD FLAP UPPER SURFACE MIDSPAN GOUGED AT 3 PLACES. BLENDED GOUGED AREAS IAW SRM 57-50-00. ALL AREAS ARE BEYOND LIM ITS IAW SRM 57-50-00 FIG 101 SHEET 5. TRIMMED OUT DAMAGED AREAS OF THE SKIN & STRINGER IAW SRM 57-50-00; FIGS 205 & 206 . REPAIRED AREAS IAW SRM 57-50-00; FIG 206. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 08FDEA01962 1 20080522 A 5330 SKIN BOEING 757 75723A 1384967 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 EXTERNAL PATCH REPAIR ON FUSELAGE FROM BS 1701 TO BS 1720, BETWEEN S-14L AND S-17L TO BE EVALUATED. EXISTING REPAIR FOU ND PREVIOUSLY ACCOMPLISHED IAW BOEING TELEX NR GUE-MAN-03-00062H, WITH FAA FORM 8110-3. LFEC REPEAT INSPECTION AT EVERY 3,000 FC INTERVAL AFTER AIRFRAME ACCUMULATES 31,000FC. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 DLM90080786 1 20080520 A 5310 DOOR FRAME DOUG MD90 MD9030 3023690 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 MIDPIT DOOR JAMB LWR SURFACE HAS CORROSION ON LWR SURFACE AT FASTENER HOLES. REPAIRED MIDPIT DOOR JAMB, IAW DELTA ER/A 468150-14, REV ORIG DATE ISSUED 05MAY08 VIA AAR EA 12661 REV I/R DATE ISSUED 05/05/08. 2 L 7 2 4F RT A6WE 20080714 NM 2008 7 14 UPS08M52345 1 20080429 A 5347 SEAT TRACK BOEING 737 7377BD 1384511 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 34861 INSPECTION TYPE:C CABIN-STA 6-10 SEAT TRACK CROWN AND BASE AREA, X=8.50 FOUND CORROSION AS MARKED. STA 6-10 SEAT TRACK BASE AREA X=8.5 CORROSION REMOVED PER SRM 51-21-01 VII R35. CABIN EXCEED LIMIT SEAT TRACK FROM STA 6-10 TO STA 6-100 X= 8. 50 EXISTING SPLICE REMOVED PER SRM 51-31-01 VII R35. HFEC C/O ON TRIMMED OFF AREA FOUND NO CRACK EVIDENT. NEW SEAT TRACK REWORKED PER SRM 51-70 -00 VI R35. NEW SEAT TRACK INSTALLED PER SRM 51-31-01 VII REV 35. 2 L 7 2 4F RT A16WE 20080714 2008 7 14 DL76L080792 4 20080530 A 3460 4077880908 DISPLAY BOEING 767 767332 1382001 NM COCKPIT FAILED A DALA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 SO 27 190DN 28447 AN HOUR AFTER DEPARTURE FROM MXP THE RIGHT FMS MCDU FAILED. RESET C/B SEVERAL TIMES, NO HELP. DIVERTED TO CDG AND REPL ACED RT MCDU. CKS OK. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 F3LA200800277 1 20080526 A 5280 D52880165004 HINGE FITTING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE LT MLG DOOR WORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 28 1583 DURING C5 C CHECK INSPECTION NOTED THE LEFT HAND FORWARD MAIN LANDING GEAR DOOR HINGE FITTING HAS OBLONG HOLES IN FITTIN G ATTACHED TO DOOR. MAINTENANCE INSTALLED A NEW FITTING ASSEMBLY IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-52R-30327 AND AMM 20-21-11 PAGE BREAK 201. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080714 NM 2008 7 14 F3LA200800278 1 20080517 A 3350 321431 BATTERY AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CABIN FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 925FR 28 1583 DURING C5 C CHECK INSPECTION NOTED ALL FOUR EPSU BATTERY PACKS FAILED EMERGENCY LIGHTS CAPACITY TEST. MAINTENANCE REMOV ED AND REPLACED EPSU BATTERIES 10WL, 11WL, 12WL AND 13WL IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 33-51-38-400-002. U PON COMPLETION OF THE REPAIR THE BATTERIES OPERATIONAL CHECKED GOOD AND WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080714 CE 2008 7 14 BSYA2008011 1 20080527 A 5270 LIGHT LEAR 35 35A 5170602 CE COCKPIT SHORTED E BSYA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 15WH 085 AFTER TAKEOFF OUT OF PHX CREW NOTICED CABIN DOOR LIGHT ON, CREW TRIED TAPPING WARNING LIGHT CAPSULE, NOTICED SOME SMOKE COMING FROM THE DOOR LIGHT CAPSULE. RETURNED TO PHX WITH NO PROBLEMS. MAINTENANCE FOUND DOOR WARNING LIGHT CAPSULE SHO RTED. DISCONNECTED WIRE, MEL'D DOOR WARNING LIGHT AND RETURNED TO LCK. RECONFIGURED WARNING LIGHT PANEL TO USE A SPARE CAPSULE FOR THE DOOR WARNING LIGHT. 2 L 7 2 4F A10CE 20080714 NM 2008 7 14 KCSA081259 1 20080527 A 5412 BULKHEAD BOEING 747 7472B4B 138481B NM NR 4 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 4 ENG FWD MOUNT HANGER CHORD CHAFED ON I/B SIDE NAC STA 128.95. 2 L 7 4 4F RT A20WE 20080714 2008 7 14 ZZDA2008109 4 20080524 A 2565 D29982225 SLIDE BOEING 717 717200 1383700 NM GALLEY DOOR UNSERVICEABLE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 955AT 55017 GALLEY DOOR PACK SLIDE PRESSURE GAUGE INDICATING IN THE RED. REMOVED AND REPLACED GALLEY DOOR SLIDE PER MM 25-61. 2 L 7 2 4F TR A6WE 20080714 NM 2008 7 14 ZZDA2008110 1 20080525 A 2560 GIRT BAR BOEING 717 717200 1383700 NM SERVICE DOOR OUT OF POSITION A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 986AT 55089 SERVICE DOOR PACK SLIDE FOLDS HANGING LOW. REPOSITIONED GIRT BAR AND REINSTALLED LANYARD ASSY REF MM 25-61. 2 L 7 2 4F TR A6WE 20080714 NM 2008 7 14 2008UALA02962 1 20080522 A 2930 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT ACTIVATED A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 WP 29 641UA 25091 DURING GEAR RETRACTION, HAD A C-HYD SYS PRESSURE AND AIR DEMAND PUMP EICAS ALONG WITH A C-HYD SYS. 2 L 7 2 4F 4 F RT A1NM E24NE 20080714 NE 2008 7 14 2008UALA02972 2 20080522 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 CONTAMINATED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 224UA 30225 222183 EVIDENCE OF METAL CONTAMINATION FOUND ON NR 1 ENG. METAL ON THE FORWARD MAGNETIC CHIP DETECTOR (MCD. ENGINE REMOVED PRI OR TO FURTHER FLIGHT. TEARDOWN FOUND THAT THE NR 2 BEARING HAD 3 BALLS WITH SPALLATION APPROXIMATELY 1/4-INCH TO 1/2-IN CH IN SIZE. THE OUTER RACE ALSO HAD EXTENSIVE PITTING WHERE LIBERATED SPALL MATERIAL HAD GOTTEN BETWEEN THE BALLS AND TH E RACE. THERE WAS NO COLLATERAL DAMAGE TO ANY OTHER NEARBY PARTS. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080708 NM 2008 7 8 DHL2008764515 1 20080521 A 5754 RIB BOEING 727 727264 138408M NM L/E SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 NR 6 K-FLAP ACTUATOR SUPPORT SIDE I/B AND O/B RIBS CRACKED WS 304. REMOVED INBOARD AND OUTBOARD RIBS AND FAB NEW RIBS W ITH 2024-T3-.063 INCH DIM 7 1/2 INCH BY 4 INCH AND PO 9006773 IAW BOEING ENGINEER DWG NR 65-16275. 2 L 7 3 4F A3WE 20080708 EA 2008 7 8 COMA0870020 1 20080517 A 2130 GG43610087 ISOLATION VALVE CNDAIR CL600 CL6002C10 1390015 EA AFT EQUIP BAY FAULTY A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 625CA 4833 10113 FLIGHT 5307 - CABIN PSI ROSE RAPIDLY, AT 10000 FT CABIN PRESSURE ALTITUDE WAS 8800. NO MESSAGES RECEIVED. RETURNED TO ATL, LANDED WITHOUT INCIDENT. PERFORMED BITE CHECK OF ACSC, PASSED. REPLACED ISOLATION VALVE. GROUND PRESSURIZED A/C. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 20080708 NM 2008 7 8 SWAA082842 1 20080524 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 768SW 30587 DURING SCHEDULED MV2 CHECK, FOUND RT MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 DL757080857 1 20080612 A 5313 STRINGER BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 UPON REMOVAL OF DOME NUT PLATE, FOUND EXFOLIATION CORROSION IN CHANNEL OF S 20R STA 758. REPLACED DAMAGED SECTION OF ST RINGER IAW SRM 53-30-03 FIG 201. 2 L 7 2 4F RT A2NM 20080708 SO 2008 7 8 RAIA00805022 1 20080519 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 835HK 145670 PRE FLT 7892 - STL - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A DEFECTIVE BULB. 2 L 7 2 4T RT T00011AT 20080710 NM 2008 7 10 DL76L080743 1 20080518 A 3397 CONNECTOR BOEING 767 767332 1382001 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 EEL SEAT FEEDER AT STA 434 LEFT MISSING MOLEX CONNECTOR. REMOVED AND REPLACED RED EEL CONNECTOR AT STA 434 LEFT. OPS C HECKS GOOD IAW B767-300 MM 33-51-10. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 DL76L080752 1 20080430 A 3397 CONNECTOR BOEING 767 767332 1382001 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 EMERGENCY LIGHT CONNECTOR AT SEAT 20 LT DAMAGED. REMOVED AND REPLACED MULER CONNECTOR FOR EMERGENCY LIGHTS. OPS CHECKS GOOD IAW B767-300 MM 33-51-10. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 DL76S080764 1 20080520 A 5753 113T220112A SPAR BOEING 767 767332 1382001 NM T/E FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 121DE 23435 DURING SHOP VISIT, CORROSION WAS FOUND ON THE REAR SPAR OF THE RT INBOARD MAIN FLAP. THE DAMAGE WAS CUT OUT AND A REPLA CEMENT SECTION WAS SPLICED IN. REPAIR WAS COMPLETED PER ERA 467064-14. 2 L 7 2 4F RT A1NM 20080710 EU 2008 7 10 USAA920081098 1 20080430 A 5320 D53480019216 STRUCTURE AIRBUS 320 A320232 3930326 EU FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650AW 856 SAL - MAJOR REPAIR - C7 CHECK - CRACKED COVER SHEET, BS 2884 / FR 68 - BS 2936 / FR 69, +Y1732. REPLACED COVER SHEET, B S 2884 / FR 68 - BS 2936 / FR 69, +Y1732 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20080710 NM 2008 7 10 USAA920081099 1 20080513 A 5330 6545774 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 444US 24862 CLT - MAJOR REPAIR - C2 CHECK - CRACKED FUSELAGE SKIN, BS 727F, S24L. REPAIRED FUSELAGE SKIN, BS 727F, S24L IAW B737 SR M 53-00-01. 2 L 7 2 4F RT A16WE 20080701 EA 2008 7 1 SWIA200819787 1 20080620 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 471CA 7655 REAR CEILING EMERGENCY LIGHT IS INOP. (FLT 2874) REPLACED AFT CEILING EMERGENCY LIGHT PER AMM CH 33-51-16. OPS CHECK G OOD. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819774 1 20080614 A 2697 WIRE CNDAIR CL600 CL6002B19 1900309 EA FIRE LOOP LOOSE A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 986CA 7174 ON CLIMB OUT, RECEIVED A "LEFT JET OVHT FAIL" MESSAGE. MESSAGE CLEARED ON GROUND. (FLT 2701) INSPECTED LOOP A WIRING ON LEFT ENGINE AND REPLACED LOOSE TERMINAL END PER AMM 26-11-04. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080701 2008 7 1 SWIA200819767 4 20080610 A 3417 6229819104 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA NR 1 ADC FAILED A SWIA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 NM 07 939SW 8847 8847 7742 NR 1 ADC PANEL FAILED. (FLT 6587) REPLACED NR 1 AIR DATA REFERENCE PANEL. OPS CHECKS GOOD IAW CRJ 200 MM 34-13-04. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819722 1 20080528 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA FALSE ACTIVATION A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 934SW 7722 RECEIVED A "SMOKE TOILET" CAUTION MESSAGE AFTER TAKE OFF. (FLIGHT #6647)INSPECTED AND OPERATED THE LEFT AND RIGHT ACM I AW AMM 21-51-13. NO DISCREPENCIES NOTED. 2 L 7 2 4F RT A21EA 20080701 NM 2008 7 1 SWAA083404 1 20080619 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 913WN 29840 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. R&R LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080701 EA 2008 7 1 SWIA200819711 1 20080410 A 7120 BUSHING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 954SW RT ENGINE MOUNT BUSHINGS ARE CORRODED. (FOUND AT C-CHECK) REPLACED BUSHINGS AS REQUIRED. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819775 1 20080613 A 5240 O-RING CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR LEAKING A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 730SK 10193 SERVICE DOOR MAKES LOUD NOISE INFLIGHT.INSTALLED NEW O-RING ON SERVICE DOOR OUTER HANDLE ASSEMBLY IAW AMM 52-41-03. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819708 1 20080410 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 954SW RBL 9 LOWER FLOORBEAM IS CRACKED AT FS 280. (FOUND AT C-CHECK) COMPLIED WITH REPAIRS PER REO 601R-53-11-1377. 2 L 7 2 4F RT A21EA 20080701 NM 2008 7 1 2008UALA02737 1 20080510 A 3350 90085 BATTERY PACK BOEING 747 747422 1384935 NM EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY CEILING LIGHTS ROW 16-17 INOPERATIVE. SUPPLEMENTAL DATA UPDATE, SUSPECT FAULTY POWER SUPPLY. REPLACED POWER SUPPLY ASSEMBLY, OPS CHECKES NORMAL. A/C OK FOR SERVICE. 2 L 7 4 4F RT A20WE 20080701 NM 2008 7 1 SWAA083394 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083379 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083383 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083378 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 USA2008F00002 1 20080616 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 458UW 25022 MAINTENANCE REPORTED THE AFT TWO EMERGENCY LIGHT BATTERY PACKS HAD LOW CAPACITY. MAINTENANCE REMOVED AND REPLACED THE AF T TWO EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 2008UALA03569 1 20080623 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 196UA 28715 SEAT 4J EMERGENCY LIGHT BROKEN. FOUND BROKEN LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVI CE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03554 1 20080623 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 AFT PIT FRAME AT FS 1460 STR 26L HAS DENT. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR IAW 53-00-07 REPAIR 5 THIS IS A CAT B REPAIR IN ZONE 1 AND REQUIRES S UPPLEMENTAL INSPECTIONS STARTING AT 50000FC AND 12000FC THERE AF TER. INSPS CO NSISTS OF BOTH DETAILED VISUAL AND NDT PER SRM 53-0 0-07 RPR 5 TABLE II. CURRENT PTC IS 14404C. 2 L 7 2 4F 4 F RT A2NM E17NE 20080702 NM 2008 7 2 2008UALA03527 1 20080620 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 514UA 24839 LEFT AFT OVERWING EXIT EMERGENCY LIGHT FWD AND ABOVE HATCH INOP WHEN LIGHTS SELECTED ON. RELAMPED BULB, OPS CHECKED GOO D. 2 L 7 2 4F 4 F RT A2NM E17NE 20080702 NM 2008 7 2 CALA0800559 1 20080601 A 5743 115A5211 BUSHING BOEING 737 737724 13844BY NM RT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 RIGHT MAIN LANDING GEAR FWD TRUNNION SUPPORT (INBOARD UPPER BUSHING FACE) HAS CORROSION. COMPLETED ECRA 5741-01106 REV D. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800570 1 20080606 A 5330 65C35772 SKIN BOEING 737 737524 1384721 NM FUSELAGE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 FUSELAGE UPPER SKIN IS WORN AT STATION 874-882 RBL-3 TO RBL-4 FROM DORSIL FIN SEAL. BLENDED OUT AREA AND INSTALLED DOUB LER, TRIPLER AND WEAR STRIPS REFINISHED AREA PER SRM 53-60-01, REPAIR 10, PROCEDURE III. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800616 1 20080620 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16646 28907 FRAME STATION 400 LEFT CRACKED BETWEEN S8 AND S9 AFT SIDE OF AIR CONDITIONING (A/C) OUTLET ASSEMBLY SUPPORT BRACKET. IN STALLED REPAIR ANGLES PER EA 5310-04498 OP 02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800551 1 20080528 A 5311 6545829 FRAME BOEING 737 737524 1384721 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 E&E ACCESS BAY LEFT-HAND FRAME IS GOUGED. TRIMMED OUT DAMAGE AT E&E ACCESS BAY LEFT-HAND FRAME AND REPAIRED SAME PER SRM 51-70-13 FIG 1. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083367 1 20080618 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 480, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083223 1 20080612 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 751SW 29803 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083063 1 20080608 A 2731 251A2420 CONTROL VALVE BOEING 737 7377H4 1384404 NM ELEVATOR TAB FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 223WN 32492 DURING SCHEDULED HC1 CHECK, LT ELEVATOR TAB FAILED CONTROL CHECK. REMOVED AND REPLACED TAB CONTROL VALVE PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082855 1 20080526 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 447, RBL 1. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20080703 SO 2008 7 3 RAIA00805014 1 20080513 A 3260 801571 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NR 2 MLG MALFUNCTIONED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 838HK 145321 FLT 7989 - IAD - LANDING GEAR AIR/GROUND FAILURE MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE LEFT NR 2 A ND RIGHT NR 2 MAIN LANDING GEAR WOW SWITCHES. MAINTENANCE GEAR SWING OPERATION CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080707 NM 2008 7 7 USAA920081080 1 20080505 A 5320 65C334191 SHEAR WEB BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 157AW 23779 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON SHEAR WEB, BS 1016 - BS 1025, LBL 10 - LBL 15, WL 208. REPLACED SHEAR WEB , BS 1016 - BS 1025, LBL 10 - LBL 15, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080707 EA 2008 7 7 HNAA0800159 1 20080505 A 6123 82410401001 POTENTIOMETER DHAV DHC8 DHC8311 1386006 EA AUTOFEATHER SYS MISRIGGED A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 330EN 274 AUTOFEATHER DID NOT ARM DURING TAKEOFF ROLL. 2 H 7 2 4T RT A13NM 20080707 EU 2008 7 7 UPS08152265 1 20080514 A 3350 SWITCH AIRBUS A300 A300F4622R 3930360 EU COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 160UP 0005 EMERGENCY LIGHTS WILL NOT SHUTOFF IN "SHUT OFF" POSITION. REMOVED AND REPLACED EMERGENCY LIGHT TOGGLE S/W E0062 PER CH 20. OPS CKS OK. 2 L 7 2 4F RT A35EU 20080707 NM 2008 7 7 UPS08552279 1 20080515 A 3350 GUARD BOEING 757 75724APF 1384969 NM COCKPIT LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 428UP 25459 EMERGENCY EXIT LIGHT SWITCH COVER ON OVERHEAD PANEL LOOSE. REPLACED GUARD REF MM CHAPTER 20. OPS CHECKED NORMAL. 2 L 7 2 4F RT A2NM 20080707 WP 2008 7 7 UPS08852272 1 20080423 A 5311 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 D-PIT STA 1420 LONGERON 35L, FRAME SECTION HAS CRACK PAST THE TERMINATION HOLE AT PREVIOUS REPAIR. R EPAIRED FLOOR SUPPORT FRAME AT STA 1420 AND 35L IAW DC8 EO-5320-6176- C. 2 L 7 4 4F RT 4A25 20080707 WP 2008 7 7 UPS08852274 1 20080415 A 5230 WEB DOUG DC8 DC873F 302199F WP CARGO DOOR DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 PIT 31 DOOR DENTED IN AREA OF UPPER HANDHOLD. REPAIRED PIT 31 DOOR IAW SRM 51-1-21, SRM 52-02-0 FIG 002 AND SRM 52-4-02 FIG 1A. 2 L 7 4 4F RT 4A25 20080707 2008 7 7 200805161 4 20080513 A 3497 2015G2H2H8 CONNECTOR EMB ERJ170 ERJ170100SE 3260406 NM TAT PROBE DAMAGED A UHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 11 638RW 17000053 FLIGHT 7653 ABQ TO ORD - CREW REPORTED A LOUD NOISE LIKE AN "EXPLOSION" FOLLOWED BY AN ELECTRICAL SMELL. MAINTENANCE FO UND THE CONNECTOR FOR THE TAT 2 PROBE SEPARATED FROM THE SHELL WITH EVIDENCE OF BURN MARKS. MAINTENANCE REMOVED AND REP LACED THE CONNECTOR, ROSEMONT AEROSPACE TAT 2 SENSOR P/N: 102AW1AF S/N: A58435. 2 L 7 2 4F RT A56NM 20080707 NM 2008 7 7 P5CA0801561 1 20080518 A 2782 1267629 PDU BOEING 747 74746NF 13848BT NM L/E SLAT MALFUNCTIONED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 450PA 30808 LEADING EDGE DRIVE, LEADING EDGE MULTI DRIVE STATUS MESSAGES RECEIVED. REPLACED NR 2 RT LEADING EDGE PDU PER MM 27-81-0 3. OPERATIONAL CHECK NORMAL. 2 L 7 4 4F RT A20WE 20080707 NM 2008 7 7 USAA920081081 1 20080515 A 3350 BPS73R BATTERY PACK BOEING 767 7672B7ER 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 251AY 24764 MIA - EEL - C4 CHECK - EXTERIOR EMERGENCY LIGHTS BATTERY PACK M 736 IS INOPERATIVE. REPLACED EXTERIOR EMERGENCY LIGHTS BATTERY PACK M 736 IAW B767 AMM 33-51-07. 2 L 7 2 4F RT A1NM 20080707 NM 2008 7 7 USAA920081082 1 20080514 A 2560 P4010021 BATTERY BOEING 767 7672B7ER 1385107 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 251AY 24764 MIA - EEL - C4 CHECK - FORWARD FLIGHT ATTENDANT POSITION 2 FLASHLIGHT BATTERY WEAK. REPLACED FORWARD FLIGHT ATTENDANT P OSITION 2 FLASHLIGHT BATTERY IAW B767 AMM 25-60-00. 2 L 7 2 4F RT A1NM 20080707 NM 2008 7 7 USAA920081085 1 20080514 A 2560 P4010021 BATTERY BOEING 767 7672B7ER 1385107 NM FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 MIA - EEL - C4 CHECK - AFT FLIGHT ATTENDANT POSITION 4 FLASHLIGHT BATTERY WEAK. REPLACED AFT FLIGHT ATTENDANT POSITION 4 FLASHLIGHT BATTERY IAW B767 AMM 25-60-00. 2 L 7 2 4F RT A1NM 20080707 NM 2008 7 7 USAA920081088 1 20080514 A 2560 P4010021 BATTERY BOEING 767 7672B7ER 1385107 NM FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 MIA - EEL - C4 CHECK - AFT FLIGHT ATTENDANT POSITION 1 FLASHLIGHT BATTERY WEAK. REPLACED AFT FLIGHT ATTENDANT POSITION 1 FLASHLIGHT BATTERY IAW B767 AMM 25-60-00. 2 L 7 2 4F RT A1NM 20080707 NM 2008 7 7 NOCA04008 1 20080519 A 5411 313T3380244 FRAME BOEING 767 76739H 1385311 NM CRACKED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 760NA 26257 AFT A FRAME LOWER CHANNEL CRACKED AT RIVET I/B FWD SIDE OF A FRAME BELOW DIAG BRACE AFT FITTING. REPLACED CRACKED C-CHA NNEL IAW SRM 51-10-02. 2 L 7 2 4F RT A1NM 20080707 GL 2008 7 7 C2XA08IA130 2 20080517 A 7200 AE3007A13 ENGINE EMB 135 EMB135LR 3260305 SO ALLSN AE3007 AE3007A 03030 GL LEFT FAILED A C2XA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SW 27 16520 17349 5016 145372 CAE310104 IAH - FLIGHT 2804, THE CREW REPORTED A NUMBER ONE ENGINE FAILURE ON CLIMBOUT AT APPROXIMATELY 5500'. THE AIRCRAFT RETUR NED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY CHEC KED WITHOUT DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080707 EU 2008 7 7 UPS08152293 1 20080508 A 2170 WATER SEPARATOR AIRBUS A300 A300F4622R 3930360 EU A/C BAY DEFECTIVE A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 01 168UP 0005 INSPECTION TYPE:N/A UPON LANDING, ONCE IN REVERSE, STRONG ODOR FROM BOTH A/C VENTS. ODOR WAS NOT ELECTRICAL. REMOVED, CLEANED AND REPLACED WATER SEPARATOR IAW AMM 21-51-16-03. CHECKS NORMAL. NO ODOR NOTED. 2 L 7 2 4F RT A35EU 20080915 EU 2008 9 15 08FDEA03136 1 20080729 A 5753 A5796030620000 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING TE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 THE LEFT WING CENTER FLAP UPPER SKIN IS GOUGED. AREA IS OUT OF LIMITS IAW SRM 57-50-00; FIG 102; SHEET 5. FABRICATED I AW SRM 57-50-00; PG 219. ALODINED AND PRIMED IAW AMM 51-22-00-0, PG 1. INSTALLED IAW SRM 57-50-00, PG 219. 2 L 7 2 4F RT A35EU 20080915 WP 2008 9 15 UPS08853088 1 20080730 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FS 680-780 RBL44 CRUSHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 MAIN CABIN FLOORBOARD AT STA 680-780 RBL 44.60 HAS 2 EA CRUSHED AREAS. FABRICATED REPLACEMENT FLOOR PANEL IAW EO DC8-5320-9691. 2 L 7 4 4F RT 4A25 20080915 NM 2008 9 15 UPS08M53096 1 20080805 A 5710 STRUCTURE DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 281UP 48538 INSPECTION TYPE:2C LT WING FIXED L/E TELESCOPIC DOOR CUTOUT FOUND CRACKED ON ONE SIDE. REMOVED CRACK, FABRICATED, AND I NSTALLED FILLER AND DOUBLER IAW MD-11 SRM 57-10-00 FIG 43, 51-21-01, 51-35-01, 51-33-01. 2 L 7 3 4F RT A22WE 20080915 WP 2008 9 15 UPS08853129 1 20080729 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FS 857 RBL 23 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 MAIN CABIN SUBFLOOR "L" ANGLE CUTOFF THROUGH BOLT HOLE RADIUS BOLT INSTALLED (HALF ON AND HALF OFF CU T) STA 857 RBL 23, AT BOTTOM OF PRESSURE PNL. REMOVED AND REPLACED "L" ANGLE IAW SRM 51-1-24, 51-3-0, 51-1-20D, 51-1-21 . 2 L 7 4 4F RT 4A25 20080915 WP 2008 9 15 UPS08853130 1 20080811 A 5753 SKIN DOUG DC8 DC871F 302199D WP RT WING TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 2 EA GOUGES IN UPPER SKIN OF RT WING O/B FLAP, ON I/B & O/B SIDE OF FLAP STA 219. FABRICATED AND INS TALLED 2 EA REPAIR DOUBLERS IAW SRM 57-07-01 FIG 004, 57-02-00, AND 51-1-21A. 2 L 7 4 4F RT 4A25 20080915 SO 2008 9 15 SWIA200819968 1 20080817 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 233SW 120307 EMERGENCY EXIT SIGN AT ROW 6 IS BROKEN. FLIGHT 5576. REPLACED EXIT SIGN AT ROW 6. 2 L 7 2 4T RT A31SO 20080915 NM 2008 9 15 SWAA084785 1 20080828 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 767 S27L/R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27R TO STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080915 NM 2008 9 15 08FDEA03590 1 20080826 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 574FE 48499 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTI NG AT HOLES B AND D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080915 EU 2008 9 15 08FDEA03142 1 20080729 A 5321 B5327047602000 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CABIN FLOOR BOARD AT FRAME 30; LBL 30 INCH IS CRUSHED. FABRICATED NEW FLOORBOARD NR 231 YG IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080916 NM 2008 9 16 08FDEA03449 1 20080816 A 5753 6521795 FAIRING BOEING 727 7272S2F 1384O81 NM NR 5 FLAP TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 NR 5 FLAP TRACK MIDDLE FAIRING, AFT SKIN BENT/CRACKED. REMOVED DAMAGED SKIN, REF 51-30-2, PG 1-7. ORIGINAL SKIN AND RE PLACEMENT BOTH IDENTIFIED AS 7075-T6, .040 REF 65-21795, REV E, PG 35 AND DWG 65-21795, AND A-TAG NR A27927. FABRICATED NEW SKIN, REF SRM 51-20-01, P 1-7. TREATED AND PRIMED REF SRM 51-10-2 P 1-27. INSTALLED SKIN REF 51-30-2, P 1-7. TOP COATED SKIN REF MM 51-20-151-PG 7. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080916 WP 2008 9 16 08FDEA03075 1 20080725 A 5755 SKIN DOUG MD10 MD1010F 3022112 WP NR 5 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 THE LEFT WING NR 5 SPOILER IS DELAMINATED ON THE LOWER SURFACE AT THE INBD CORNER. REMOVED LEFT NR 5 SPOILER IAW MD-1 0 AMM 27-60-01-4. REPAIRED THE LEFT NR 5 SPOILER BY REMOVING THE DELAMINATED LOWER SKIN DOUBLER, CORE SECTION AND END R IB. FABRICATED AND BONDED A NEW CORE SECTION, LOWER SKIN; DOUBLER AND END RIB IAW DC/MD-10 SRM57-10-00; VOL I AND DAC D WG ACA 1347. INSTALLED SEALS AND HARDWARE IAW DC/MD-10 SRM 51-31-01, VOL II. PAINTED SPOILER IAW DC/MD-10 SRM 51-21-01 ; VOL II. 2 L 7 3 4F RT A22WE 20080916 NM 2008 9 16 08FDEA03086 1 20080725 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 577FE 48469 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES A, B, C AND D BUSHING. REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL 1. SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080917 NE 2008 9 17 ASAA0883400 2 20080816 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217C 52053 NE NR 2 FAILED A ASAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 02 972AS 48514 53448 P725845D DEPARTURE OUT OF SMF AS GEAR RETRACTED LOUD BANG AND SHUDDER NR 2 MOTOR INDICATION OF FAILURE THROTTLE PULLED TO IDLE NO FIRE WARNING NO SECONDARY LIGHTS ENGINE SHUTDOWN ON GROUND. NR 2 ENGINE REMOVED PER TC 28771002 ASA NR 8-7200-9-8201 S /N 725845 TT NR 36712, INSTALLED NR 2 ENGINE S/N 728062 PER TC 28771004 ASA NR 8-7200-9-8201 TT NR 35180. 2 L 7 2 4F 4 F RT A6WE E9NE 20080917 2008 9 17 ASAA0853398 4 20080821 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM FLT MANAGE FAULTED A ASAA O OTHER N FALSE WARNING CR CRUISE 1 NM 02 583AS 4378 35681 AT LIM ILLUMINATED IN FLIGHT ABOVE N1'S. AFTER LANDING DASHES ABOVE N1'S CURRENT STATUS & BITE CHECKS GOOD REF FIM 22 3 1 710 801 FMS CHECKS GOOD REF FIM 34 61 00 810 807 & FIM 73 00 00 810 801 F00, NO PREVIOUS HISTORY. GROUND VERIFICATION SUCCESSFUL. 2 L 7 2 4F RT A16WE 20080917 NM 2008 9 17 ASAA0843371 1 20080719 A 5320 6545855103 SILL BOEING 737 7374Q8 138447Q NM BS 948-1006 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 CABIN R2 DOOR INNER CHORD (MOP SILL) CORRODED. REMOVED DAMAGED INNER CHORD, LOCATE, DRILLED AND INSTALLED A REPLACEMENT INNER CHORD IAW SRM 51 40 02 PAGES 2 AND 6. 2 L 7 2 4F RT A16WE 20080917 NM 2008 9 17 ASAA0843384 1 20080719 A 5320 654587545 SILL BOEING 737 7374Q8 138447Q NM BS 259-360 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 R1 DOOR THRESHOLD INNER CHORD (MOP SILL) CORRODED. REMOVED DAMAGED INNER CHORD. LOCATED, DRILLED AND INSTALLED A REPLA CEMENT INNER CHORD IAW B737 400 SRM 51 40 02 PAGE 2 AND 4. 2 L 7 2 4F RT A16WE 20080917 NM 2008 9 17 ASAA0843385 1 20080719 A 5320 654587547 THRESHOLD BOEING 737 7374Q8 138447Q NM BS 298-328 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 R1 DOOR THRESHOLD WEB CORRODED BETWEEN STA 298 TO 328 AREA. REMOVED DAMAGED WEB, FABRICATED LOCATED DRILLED AND INSTALL ED NEW WEB IAW B737 400 SRM 51 30 01 PG 7 AND 51 40 02 PAGES 2 AND 4. 2 L 7 2 4F RT A16WE 20080917 NM 2008 9 17 ASAA0843386 1 20080803 A 5320 654587527 STRAP BOEING 737 7374Q8 138447Q NM BS 275-298 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 R1 DOOR INNER CHORD STRAP CORRODED STA 275 TO STA 298.5 RBL 54 WL 208. REMOVED DAMAGED STRAP, FABRICATED, LOCATED, DRIL LED AND INSTALLED IAW B737 400 SRM 51 40 02 PGS 3 & 4. 2 L 7 2 4F RT A16WE 20080917 NM 2008 9 17 ASAA0843347 1 20080721 A 5340 BRACKET BOEING 737 7374Q8 138447Q NM BS 291 S11-12R CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 INTERIOR FUSELAGE STIFFENER BRACKET CRACKED 1 INCH LENGTH FWD OF STA 291 BETWEEN STRINGERS 11R AND 12R. REMOVED DAMAGED ANGLE, LOCATED DRILLED AND INSTALLED A REPLACEMENT STIFFENER IAW SRM 51-40-02 PG 3 DETAIL 1. 2 L 7 2 4F RT A16WE 20080917 NM 2008 9 17 ASAA0843348 1 20080721 A 5340 BRACKET BOEING 737 7374Q8 138447Q NM BS 291 S12-13R CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 INTERIOR FUSELAGE STIFFENER BRACKET CRACKED 4.5 INCH LENGTH FWD OF STA 291 BETWEEN STRINGERS 12R AND 13R. REMOVED DAMAG ED ANGLE, LOCATED DRILLED AND INSTALLED A REPLACEMENT STIFFENER IAW SRM 51-40-02 PG 30 DETAIL 1. 2 L 7 2 4F RT A16WE 20080917 NM 2008 9 17 ASAA0843349 1 20080721 A 5340 BRACKET BOEING 737 7374Q8 138447Q NM BS 291 S10-11R CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 INTERIOR FUSELAGE STIFFENER BRACKET CRACKED 1.5 INCHES IN LENGTH FWD OF STA 291 BETWEEN STRINGERS 10R AND 11R. REMOVED DAMAGED ANGLE, LOCATED, DRILLED AND INSTALLED A REPLACEMENT STIFFENER IAW SRM 51-40-02 PG 30 DETAIL 1. 2 L 7 2 4F RT A16WE 20080918 2008 9 18 2008UALA04369 4 20080820 A 2565 69B528083 HOUSING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT OWING SLIDE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 LT OVERWING DISCONNECT HOUSING CRACKED. REMOVED & REPLACED DISCONNECT HOUSING. 2 L 7 2 4F 4 F RT A1NM E24NE 20080918 NM 2008 9 18 2008UALA04376 1 20080821 A 3397 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 540UA 25252 EMERGENCY LIGHT STRIP INOP AT DOOR 2L. FOUND SUPPLY CABLE PINCHED/SHORTED. REPLACED SUPPLY CABLE, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 EU 2008 9 18 UPS08153222 1 20080820 A 5321 B5327077600000 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 138UP 0821 INSPECTION TYPE:C1 MAIN CARGO FLOOR PANEL 251MJ FWD HAS FIELD REPAIR. REPAIRED MAIN CARGO FLOOR PANEL 251MJ REF SRM 53- 10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20080918 NM 2008 9 18 ASAA0853404 1 20080824 A 3040 8300005604 CONTROLLER BOEING 737 737890 1384527 NM WINDOW HEAT INOPERATIVE A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 583AS 4413 35681 LT FWD WINDOW OVERHEAT LIGHT ILLUMINATED FOUND LEFT FRONT HEAT POWER C/B ON P6 11 OUT. RESET C/B REF PROCEDURE MM 20 60 01. BITE CHECK ON WHCU OPS NORMAL REF MM FIM 30 41 00 TASK 801. GROUND VERIFICATION CHECKS GOOD. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 UPS08553198 1 20080814 A 5210 CAM BOEING 757 75724APF 1384969 NM PAX DOOR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 CREW ENTRY DOOR UPPER LATCH CAM GOUGED ON FACE. BLENDED PER B757-5210-14721. 2 L 7 2 4F RT A2NM 20080918 NM 2008 9 18 SWAA084805 1 20080828 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 504C S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 504C, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 SWAA084806 1 20080829 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 EEPLS LENS LOOSE AT ROW 5 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 SWAA084807 1 20080828 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED SPV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 SWAA084810 1 20080830 A 3350 1619 LAMP BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 ASAA0843421 1 20080820 A 5330 65C32661 SKIN BOEING 737 7374Q8 138447Q NM BS 727F DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 DENT FOUND AT A C, SKIN AT BS 727F BETWEEN STR 25L AND 26L. REPAIRED IAW ERO 8620 AND EA 5330 02385. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 SWAA084815 1 20080830 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 10 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 SWAA084816 1 20080901 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 909WN 32458 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 SWAA084818 1 20080901 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 5 TO RBL 43. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 UPS08M53214 1 20080819 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 12 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 2008UALA04304 1 20080814 A 2612 473760 FIRE DETECTOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE RT ENGINE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 788UA 26942 FIRE LOOP 1 ENG R RIGHT ENGINE FIRE DETECTION SYSTEM LOOP 1 FAILURE. *S/D* REPLACED RIGHT ENGINE UPPER FIRE LOOP. FIR E TEST PASSED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080918 NM 2008 9 18 2008UALA04135 1 20080805 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 46 ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY LIGHT INOP: SEAT 46 ABC. *S/D* REPLACED LIGHT ASSY. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 NM 2008 9 18 2008UALA04176 1 20080808 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 814UA 862 FLOORBEAM 175 CORRODED. *S/D* REMOVED BEAM AND AFT 2 PROFILES. BEAM PARTIALLY INSTALLED AND IN PLACE. INSTALLED BEAM , AFT FASTENERS AND FWD TOP FASTENERS. 2 L 7 2 4F 4 F RT A28NM E40NE 20080918 NM 2008 9 18 2008UALA04177 1 20080807 A 3510 QUICK DISCONNECT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU OXYGEN MASK LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 COCKPIT O2 STILL LEAKING, LOST 200 LBS IN 2 LEGS. *S/D* FOUND 1ST OFFICER'S MASK LEAKING AT QUICK DISCONNECT FITTING I N O2 BOX. REPLACED 1ST OFFICER'S MASK. NO LEAKS DETECTED. CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 20080918 NM 2008 9 18 UPS08M53216 1 20080822 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 10 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53225 1 20080820 A 5330 SKIN DOUG MD11 MD11F 3023600 NM BS 1761-1781 MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C EXISTING DOUBLER AT FS 1761-1781 BETWEEN LONGERON L-1 AND R-1 IS NOT IN COMPLIANCE WITH THE SRM 53-20 -00 FIG 2. REMOVED DOUBLER, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND FINGER DOUBLER IAW MD-11 SRM 53-20-00 FIG 2 PAGE 2. 2 L 7 3 4F RT A22WE 20080918 2008 9 18 UPS08M53226 4 20080825 A 2565 LEVER DOUG MD11 MD11F 3023600 NM SLIDE ARM INOPERATIVE A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 286UP 48453 L1 DOOR ARM LEVER WILL NOT ARM. ADJUSTED LOWER DOOR INTERIOR COVER. OPS CHECK NORMAL. DOOR LIGHT EXTINGUISHED. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53174 1 20080820 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 2 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAI R BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53175 1 20080820 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 7 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAI R BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53182 1 20080819 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 24 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53183 1 20080813 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 26 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53184 1 20080817 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSIOIN IN NR 6 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53191 1 20080821 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 22 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 2008UALA04112 1 20080803 A 2612 CGAB140001 FIRE LOOP BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NR 4 NACELLE FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 933UA 26659 CREW REPORTS ALL 4 CARGO FIRE SUPPRESSION LOOP FAIL LIGHTS ARE ON. *S/D* IN THE AFT CARGO COMP, FOUND THE A LOOP NR 1 AND B LOOP NR 2 & 3 DETECTORS INOP. SWAPPED NR 1 DETECTORS. NOW AFT CARGO A LOOP IS OPERATIONAL, AFT CARGO B LOOP IS INOP. REPLACED 'A' AND 'B' LOOP DETECTORS, CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20080918 NM 2008 9 18 ZZDA2008154 1 20080816 A 5330 SKIN BOEING 717 717200 1383700 NM BS 1087 L10L DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 932AT 55073 FOUND HOLE IN FUSELAGE UNPRESSURIZED AREA AT STATION 1087 LONGERON 10L HOLE SIZE 5 IN X 1.5. REPAIRED FUSELAGE AT STA 1 087 LONGERON 10 L REF AAR W/O 28330 PER SRM 53-00-00 REPAIR 2. 2 L 7 2 4F TR A6WE 20080918 NM 2008 9 18 2008UALA04332 1 20080817 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE SEAT 31B MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 EMERGENCY LIGHT STRIP ON RIGHT SIDE SEAT 31B MISSING. *S/D* REPLACED EEL LIGHT. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20080918 NM 2008 9 18 2008UALA04334 1 20080819 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY LIGHT ROW 4F INOP. *S/D* RELAMPED, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 2008 9 18 2008UALA04145 4 20080806 A 3442 5819310 RADAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WX SYSTEM INTERMITTENT A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 508UA 24744 WEATHER RADAR FAILURE. FLIGHT DIVERTED. *S/D* WX RADAR AUTO TILT INOP MANUAL TILT OK. CHRONIC PROBLEM, NEED NEW SCAN NER. REPLACED SCANNER, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NM 2008 9 18 2008UALA04146 1 20080805 A 3350 58791 POWER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 330UA 24191 LAST 7 ROWS OF EMERGENCY ROW FLOOR LIGHTING INOP. *S/D* REPLACED POWER CABLE. EEL LIGHTING, OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 20080918 NM 2008 9 18 2008UALA04336 1 20080819 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY LIGHT ROW 4A INOP. *S/D* REPLACED LAMP, OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 NM 2008 9 18 UPS08M53192 1 20080820 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 16 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 EU 2008 9 18 2008UALA04154 1 20080805 A 2560 D30665109 GIRT LACING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT DOOR SLIDE INADEQUATE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 411UA 464 LT AFT DOOR SLIDE GIRT LACING. *S/D* SLIDE GIRT LACING INADEQUATE. NEW SLIDE INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080918 NM 2008 9 18 UPS08M53193 1 20080820 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 22 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 2008UALA04166 1 20080806 A 3350 55 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 369UA 24538 LEFT OVERWING HATCH ILLUMINATION EMERGENCY LIGHTS INOP. *S/D* RELAMPED WITH 2EA LAMPS. 2 L 7 2 4F 4 F RT A16WE E21EU 20080918 NM 2008 9 18 2008UALA04167 1 20080806 A 2197 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE F BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 IN P36 PANEL AT RIGHT-FWD CORNER - SIGNS OF ELECTRICAL ARCING AT WIRE BUNDLE W1260. *S/D* IN P36 PANEL AT RIGHT-FWD CO RNER - SIGNS OF ELECTRICAL ARCING AT WIRE BUNDLE W1260. REMOVED CLAMPS FROM WIRE BUNDLES AND INSPECTED WIRE BUNDLES PER BSWPM 20-10-06. FOUND TWO WIRES W1260-5589-18 AND W1260-5589 DAMAGED AND BURNED. REPLACED DAMAGED WIRES PER BSWPM 20- 10-11 AND OPS CHECKED AFT EQUIPMENT FAN SYSTEM GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NM 2008 9 18 2008UALA04388 1 20080820 A 2421 GENERATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEFT MALFUNCTIONED A UALA D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 655UA 25393 LEFT GEN DID NOT STAY ONLINE AFTER ENG START. 2 L 7 2 4F 4 F RT A1NM E24NE 20080918 NM 2008 9 18 2008UALA04389 1 20080821 A 7921 2810193111 BYPASS VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE ENG OIL COOLER LEAKING A UALA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 29 664UA 29236 OIL LEAKAGE FROM LT ENG OIL COOLER BYPASS VALVE. FOUND LEAK FOUND COMING FROM AIR-OIL HEAT EXCHANGER VALVE. REPLACED NR 1 ENG AIR OIL HEAT EXCHANGER. NO LEAKS ON GROUND TEST. 2 L 7 2 4F 4 F RT A1NM E24NE 20080918 NM 2008 9 18 2008UALA04390 1 20080822 A 3510 OXYGEN MASK BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE 1ST OFFICER'S LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 673UA 29241 F/O OXYGEN MASK HAS LEAK. 2 L 7 2 4F 4 F RT A1NM E24NE 20080918 NM 2008 9 18 2008UALA05393 1 20080822 A 2611 SMOKE DETECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW REST AREA MALFUNCTIONED A UALA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 29 107UA 26900 SMOKE ALARM IN FLT ATT CREW REST AREA WENT OFF TWICE ON TAXI IN. ALSO LOUD NOISE HEARD BENEATH 5L- :DOOR 5 SMOKE DETECT C/B CYCLED, SYS RESET, ALL OPS NORMAL. UNABLE TO REPRODUCE LOUD NOISE UNDER 5 L. 2 L 7 4 4F 4 F RT A20WE E24NE 20080602 NM 2008 6 2 CALA0800465 1 20080516 A 5311 146A1141 FRAME BOEING 737 737724 13844BY NM BS 827 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23708 28769 FRAME CRACKED AT STATION 827 ABOVE S9R. INSTALLED REPAIR PARTS PER EC/RA 5310-04763, REPAIRED FRAME PER EC/RA 5310-0476 3. 2 L 7 2 4F RT A16WE 20080602 NM 2008 6 2 CALA0800466 1 20080516 A 5311 146A1133 FRAME BOEING 737 737724 13844BY NM BS 787 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23708 28769 FRAME CRACKED AT STATION 787 ABOVE S9R. INSTALLED REPAIR PARTS PER EC/RA 5310-04763, REPAIRED FRAME PER EC/RA 5310-0476 3. 2 L 7 2 4F RT A16WE 20080602 NM 2008 6 2 CALA0800467 1 20080514 A 5330 146A3230 SKIN BOEING 737 737724 13844BY NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27733 28800 CORROSION AROUND FUSELAGE DRAIN PLUG 8" AFT OF NR 1 VHF COMMUNICATION ANTENNA. REPAIRED IAW ECRA 5330-03805 PART 1, INI TIATED A DIP TO ACCOMPLISH INSPECTION OF THE REPAIR PER PART 2 PRIOR TO THE ACCOMPLISHMENT OF 50,000 TOTAL AIRFRAME FLIG HT CYCLES AND REPEAT INSPECTION AT INTERVALS NOT TO EXCEED 18,000 FLIGHT CYCLES THERE AFTER. 2 L 7 2 4F RT A16WE 20080602 NM 2008 6 2 CALA0800454 1 20080514 A 5320 65C3397053 FLOOR SUPPORT BOEING 737 737524 1384721 NM BS 344-360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17640 28901 FLOOR SUPPORT STA 344 TO 360 BL 0 CRACKED. REMOVED AND REPLACED DAMAGED WEB ASSEMBLY P/N 65C33970-53 PER SRM 51-10-2. 2 L 7 2 4F RT A16WE 20080602 NM 2008 6 2 CALA0800455 1 20080514 A 5320 65C333672 INTERCOSTAL BOEING 737 737524 1384721 NM BS 947-967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17640 28901 FLOOR SUPPORT STA 947.5 TO 967 RBL 51 HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT STA 947.5 TO 967 RBL 51 PER SRM 51-40-12. 2 L 7 2 4F RT A16WE 20080710 NM 2008 7 10 AALA200801116 1 20080427 A 3350 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 191AN 32385 DFW - EMERGENCY LIGHT IN FRONT OF SEAT 18A HAS DAMAGED DECAL. REPLACED DECAL ON LENS FOR EMERGENCY LIGHT IN FRONT OF SE AT 18A. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080710 WP 2008 7 10 ASAA0882977 1 20080521 A 5330 59360215 DOUBLER DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 958AS 53024 FWD LAV SERVICE PANEL DOUBLER IS CORRODED AT FORWARD LOWER LATCH CUTOUT DAMAGED SECTION. FABRICATED LOCATED DRILLED AND INSTALLED REPAIR STRAP AND FILLER IAW ALASKA EA 5330 02339 AND AAR EA12687. 2 L 7 2 4F RT A6WE 20080710 NM 2008 7 10 2008UALA02795 1 20080514 A 5412 BULKHEAD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 PYLON DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 NR 1 PYLON AFT BULKHEAD, LWR FLANGE AFT SIDE, FASTENER HOLES GOUGED & ELONGATED, INCLUDES EXISTING REPAIR. ACCOMPLISHED MAJOR REPAIR AT GSO- RPR PER REO G12334 AND EVA 71554 BY MECH 5561 AND INSP BY QC 254 ON NR 47928. THIS ITEM HAS 1ST S TAGE APPROVAL ONLY. THE COMPLIANCE FINDINGS FOR 14 CFR 25 .571 AND 26.43D IS DEFERRED FOR A PERIOD OF NO LATER THAN 12 MONTHS FROM 12MAY08. ON OR BEFORE 12MAY09 BOEING 118031 MUST ISSUE A NEW FAA FORM 8100-9 TO SHOW COMPLIANCE WITH 14 CFR 25.571 AND 26.43D. AIRCRAFT MUST BE REMOVED FROM SERVICE ON 12 MAY 2009 UNLESS A NEW 8100-9 IS RECEIVED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080711 NM 2008 7 11 UPS08M52317 1 20080510 A 5720 DOUBLER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C LEFT WING FIXED L/E BEADED DOUBLER BETWEEN SLAT TRACK 10 AND 11 FOUND CRACKED. CUT OUT DAMAGE, FABRI CATED FILLER, ANGLES, AND DOUBLER, AND INSTALLED IAW MD-11 SRM 57-10-00 FIG 27, 51-33-01, 51-31-01, AND 51-21-01. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 AALA200801195 1 20080504 A 3350 OL3071BPEGPL LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 967AN 29545 LGA - EMERGENCY LIGHT AT SEAT 22B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22B. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A16WE 20080711 NM 2008 7 11 AALA200801302 1 20080514 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801184 1 20080503 A 3350 LENS BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 648AA 24606 DFW - EMERGENCY LIGHT ADJACENT TO RIGHT AFT LAVATORY MISSING LENS. REPLACED LENS COVER FOR EMERGENCY LIGHT ADJACENT TO RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 AALA200801220 1 20080505 A 2752 ACTUATOR BOEING 757 757223 1384957 NM T/E FLAP FAILED A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 623AA 24581 ORD INFLIGHT T1624/05MAY - CREW REPORTED LEADING EDGE SLAT ASYMMETRY AND LIGHT INDICATION. FLAP INDICATION STOPPED AT . 05. TRAILING EDGE LIGHT ALSO ILLUMINATED. TRAILING EDGE FLAPS OPERATED WITH ALTERNATE SWITCH. LANDED ORD WITHOUT INCID ENT. FOUND NUMBER 12 RIGHT WING ROTARY ACTUATOR OVERLOADED. REPLACED NUMBER 12 ROTARY ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 AALA200801167 1 20080430 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHTS AT SEAT ROWS 30 TO 45 INOPERATIVE. RECHARGED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 30 T O 45. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801218 1 20080505 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN FAULTY A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 950AN 30087 MIA - EMERGENCY LIGHT CIRCUIT BREAKER POPPED LEFT AFT EMERGENCY CHARGER. REPLACED BATTERY PACK M1673 AND RESET CIRCUIT BREAKER FOR EMERGENCY LIGHT LEFT AFT CHARGER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080711 NM 2008 7 11 AALA200801158 1 20080430 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 666A 25300 DFW - EMERGENCY LIGHTS AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT NUMBER T WO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 AALA200801238 1 20080506 A 3397 PIN BOEING 777 777223 1385213 NM CONNECTOR BACKED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW - SEAT MOUNTED EMERGENCY LIGHT AT AFT SEAT 3G INOPERATIVE. FOUND PUSHED BACK PIN AT CONNECTOR. RESEATED PIN FOR EM ERGENCY LIGHT AT AFT SEAT 3G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801144 1 20080428 A 3397 WIRE BOEING 777 777223 1385213 NM CABIN EXPOSED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT SEAT 33D HAS WIRING EXPOSED. STOWED WIRING UNDER COVER FOR EMERGENCY LIGHT AT SEAT 33D SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 WP 2008 7 11 AALA200801174 1 20080501 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7544A 53026 LGA - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD SEAT ROW 6 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVE RHEAD SEAT ROW 6. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008041600080 20080416 00080 NM 2008 4 16 UIEA200800119 1 20080403 A 5347 SEAT TRACK BOEING 747 747243B 1384830 NM ZONE 200 CHAFED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK STA 1595 TO 1600 RBL 11 SEAT TRACK CHAFED, SEAT TRACK REPAIRED PER SRM 53-10-05 FIG 14. 2 L 7 4 4F RT A20WE 2008041600081 20080416 00081 NM 2008 4 16 UIEA200800120 1 20080410 A 5347 SEAT TRACK BOEING 747 747243B 1384830 NM ZONE 200 WORN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK STA 1625 TO 1680 RBL 11 SEAT TRACK FOUND WORN. SEAT TRACK REPAIRED PER SRM 53-10-05. 2 L 7 4 4F RT A20WE 2008041600084 20080416 00084 NM 2008 4 16 UIEA200800123 1 20080404 A 5710 T08A007504 BEAM BOEING 747 747243B 1384830 NM RT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 RIGHT WING LEADING EDGE CAVITY INBOARD OF NR 4 PYLON AT ABOUT WBL 830 FOUND WEB OF D-BEAM CRACKED. DAMAGED WEB REPLACED IAW SRM 57-20-03. 2 L 7 4 4F RT A20WE 2008041600100 20080416 00100 NM 2008 4 16 AALA200800738 1 20080327 A 3350 SIGN BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AA 27054 DFW - EMERGENCY EXIT LIGHT ARROW AT SEAT 17F IS PEELING OFF. REPLACED EXIT ARROW FOR EMERGENCY LIGHT AT SEAT 17F. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041600105 20080416 00105 NM 2008 4 16 AALA200800729 1 20080326 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 752AN 30260 DFW - EMERGENCY LIGHT AT SEAT 31C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041600107 20080416 00107 NM 2008 4 16 AALA200800737 1 20080327 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AA 27054 DFW - EMERGENCY LIGHT AT AFT SEAT 3E MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT AFT SEAT 3E. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041600109 20080416 00109 EU 2008 4 16 AALA200800741 1 20080328 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14077 612 MIA - EMERGENCY LIGHTS AT SEATS 2D AND 2G INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHTS AT SEATS 2D AND 2G. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008041600112 20080416 00112 NM 2008 4 16 F3LA200800148 1 20080402 A 5321 D5367175604800 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE 261PF CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 5380 1841 DURING C4 S1 C CHECK, INSPECTION REPORTED CORROSION AND DAMAGE WAS FOUND ON FLOOR PANEL 261PF, UNDER THE RIGHT CORNER OF THE AFT GALLEY. MAINTENANCE REPAIRED THE CORROSION AND DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-12-00 . UPON COMPLETION OF THE REPAIRS, THE PANEL WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041600122 20080416 00122 EA 2008 4 16 A6WA200840274 1 20080330 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 401AW 7280 CRACKS FOUND ON BRACKETS ON INTERCOSTALS FS 621 TO FS 625.30 STRINGER 14 RT AND LT SIDE. (M) REPLACED BRACKET ON INTER COSTAL FS 621.00 STR 14 RT & IAW REO 601R-53-61-100. 2 L 7 2 4F RT A21EA 2008041600126 20080416 00126 NM 2008 4 16 UIEA200800128 1 20080403 A 5730 SKIN BOEING 747 747243B 1384830 NM LWS 640-1120 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 LEFT WING FROM WS 1120 TO 640 UPPER SKIN CORROSION EVIDENT BETWEEN FRONT SPAR AND MID SPAR. BLENDED OUT CORROSION PER S RM 51-10-01, REPROTECTED PER SRM 51-10-02. 2 L 7 4 4F RT A20WE 2008041600131 20080416 00131 NM 2008 4 16 UIEA200800133 1 20080403 A 5711 SPAR BOEING 747 747243B 1384830 NM RWS 1250-1392 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 RIGHT WING WS 1250 TO WS 1392 FROM NR 23,AND 24 LEADING EDGE FLAP AREA, FRONT SPAR AREA SURROUNDING FOUND 7 AREAS OF COR ROSION. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTECTED PER SRM 51-10-02. 2 L 7 4 4F RT A20WE 2008041600138 20080416 00138 EA 2008 4 16 SIMA200810501 1 20080410 A 5610 NP1393114 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A SIMA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 513AE 10114 ON FLIGHT 3593, CREW REPORTED FRONT FIRST OFFICERS WINDSHIELD SHATTERED WHILE CRUISING AT FL390. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND INSTALLED FIRST OFFICERS WINDSHIELD IAW 56-11-01. PERFORMED OPERATION CHECK OF WIPER, HEAT AND PR ESSURIZATION IAW CRJ 700 AMM 30-41-00 AND 21-31-00. ALL OPERATIONAL CHECKS GOOD AT THIS TIME. AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4F RT A21EA 2008041600144 20080416 00144 NM 2008 4 16 AALA200800749 1 20080329 A 3350 O9L1098BPEGPL LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 678AN 29428 JFK - EMERGENCY LIGHT AT SEAT 36D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 36D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041600146 20080416 00146 WP 2008 4 16 AALA200800751 1 20080329 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 553AA 53083 LGA - EMERGENCY LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD GALLEY. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008041600155 20080416 00155 NM 2008 4 16 UIEA200800138 1 20080404 A 5730 SKIN BOEING 747 747243B 1384830 NM ZONE 600 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 RT WING WBL 470 TO WS 917 WING UPPER SKIN FROM FRONT SPAR TO REAR SPAR FOUND CORRODED. BLENDED OUT CORROSION PER SRM 51 -10-01, REPROTECTED PER SRM 51-10-02. 2 L 7 4 4F RT A20WE 2008041600157 20080416 00157 EA 2008 4 16 A6WA200840190 1 20080311 A 7830 BRACKET CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 LT ENGINE THRUST REVERSER STOW SWITCH BRACKET CRACKED. LT ENGINE THRUST REVERSER STOW SWITCH BRACKE FABRICATED IAW SRM 51-24-26 AND INSTALLED IAW SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2008041600158 20080416 00158 NM 2008 4 16 NWAA081586310 1 20080304 A 5330 SKIN BOEING 747 747451 1384940 NM BS 460 DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 670US 24225 DURING "M" CHECK, FOUND SHORT EDGE MARGIN ON FUSELAGE SKIN FASTENER HOLES ABOVE DOOR 1 RT AT BS 460. REPAIRED PER EA 63 -212524. 2 L 7 4 4F RT A20WE 2008041600176 20080416 00176 NM 2008 4 16 08FDEA01411 1 20080415 A 5730 ARB2886503 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 619FE 48770 LT WING, ANTI-ICE TELESCOPE TUBE CUT-OUT AT L/E FIXED COMPARTMENT FOUND OUTBD CORNER CRACKED. TRIMMED OFF AND REPAIR CA RRIED OUT AS PER SRM 57-10-00 FIG. 43 VOL.I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041600178 20080416 00178 NM 2008 4 16 UIEA200800091 1 20080319 A 5410 ACCESS PANEL BOEING 747 74747UF 1384812 NM NR 3 PYLON CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 408MC 29261 NR 3 PYLON ACCESS PANEL 472FL BOTH SIDES SKINS ADJACENT TO LATCH AREA HAVE CRACKED. REPAIRED PANEL PER EO 4454A055 AND RE-INSTALLED PER 54-62-02. 2 L 7 4 4F RT A20WE 2008041600189 20080416 00189 WP 2008 4 16 AALA200800765 1 20080330 A 4990 5940405503 APU DOUG DC9 DC982 3022082 WP LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 293AA 49305 DFW INFLIGHT T2034/30MAR - CREW REPORTED SMOKE IN CABIN DURING CLIMB. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REP LACED AUXILLIARY POWER UNIT ON 04 APR AT DWH DUE TO OIL LEAK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008041600192 20080416 00192 NM 2008 4 16 AALA200800778 1 20080331 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 938AN 29533 DFW - EXTERIOR EMERGENCY LIGHT AT AFT LEFT OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 44G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 2008041600193 20080416 00193 NM 2008 4 16 AALA200800773 1 20080331 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 361AA 24042 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 10H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 10H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 2008041600195 20080416 00195 EU 2008 4 16 AALA200800775 1 20080331 A 2560 BATTERY AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7083A 645 MIA - EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT LEFT NUMBE R ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 2008041700003 20080417 00003 NM 2008 4 17 2008UALA02096 1 20080410 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD ENTRY DOOR, LOWER FWD FRAME CRACKED NEAR INNER RADIUS. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGE & INSTALLED EXTERNA L FRAME DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700007 20080417 00007 NM 2008 4 17 UPS08M51975 1 20080406 A 3397 WIRE DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHTS BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 EMERGENCY LIGHTS INOP. BROKEN WIRE AT BATTERY CONNECTOR. REPAIRED WIRING IAW SWPM 20-41. OPS CHECKED NORMAL. 2 L 7 3 4F RT A22WE 2008041700011 20080417 00011 NM 2008 4 17 2008UALA02099 1 20080410 A 5312 PRESSURE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE WING BOX CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 CABIN WING BOX UPPER PRESS DECK IS CRACKED BS 664 LBL 31". FABRICATED & INSTALLED REPAIR DOUBLER ON UPPER SURFACE OF PR ESSURE DECK REF MM53-21-98 PG 801 & SRM51-40-02 PG 1-3. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700018 20080417 00018 NM 2008 4 17 2008UALA02106 1 20080410 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 288 S2L GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 UPPER FUSELAGE CROWN SKIN HAS DEEP GOUGE BS 288 STR 2L. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND INSTALLED EXTERNAL FU SELAGE SKIN DOUBLER-TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700020 20080417 00020 NM 2008 4 17 2008UALA02108 1 20080410 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 952-986 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 AFT ENTRY DOOR INNER CREASE BEAM UPPER SURFACE CORRODED AT STA 952-986. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700021 20080417 00021 NM 2008 4 17 2008UALA02109 1 20080410 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 986 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 AFT FLOORBEAM CORRODED AT FLOOR BOARD HOLES STA 986.5 RBL 20-32 UPPER AND LOWER SURFACE. MAJOR REPAIR ACCOMPLISHED: FAB RICATED & INSTALLED FLOORBEAM UPPER "T" CAP SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700023 20080417 00023 NM 2008 4 17 2008UALA02111 1 20080410 A 5340 ATTACH FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD ENTRY DOOR FUSELAGE CUTOUT AT BS 294.5 UPPER INTERCOSTAL CLIP CRACKED IN RADIUS STRINGER 11L. MAJOR REPAIR ACCOMPLIS HED: REPLACED THE CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700029 20080417 00029 NM 2008 4 17 2008UALA02116 1 20080410 A 7797 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE DAMAGED A UALA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 29 544UA 25322 726555 EICAS MSG 'R ENG SEC CONT' DISPLAYED. FOUND CONNECTOR FAILED. REPLACED CONNECTOR AND BACKSHELL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700031 20080417 00031 NM 2008 4 17 2008UALA02119 1 20080409 A 3510 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CREW OXYGEN LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 597UA 28750 CREW OXYGEN LOW, INDICATES 1100. SERVICED CREW O2, NO LEAKS WERE NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700033 20080417 00033 NM 2008 4 17 MWEA080053 1 20080409 A 2781 892101 SENSOR BOEING 717 717200 1383700 NM SLATS FAILED A MWEA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 GL 13 913ME 55176 AFTER EXTENDING SLATS DOWN ARROW STAYED ON AND PSEU FAIL ILLUMINATED. REMOVED AND REPLACED FLAP POSITION SENSOR. 2 L 7 2 4F TR A6WE 2008041700034 20080417 00034 EU 2008 4 17 2008UALA02121 1 20080411 A 2730 SC47003 SERVO VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT ELEVATOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 407UA 456 DURING A CHECK, RIGHT ELEVATOR WILL NOT PASS FLIGHT TEST. 34CE1 SERVO FAULTY. REPLACED ELEV SERVO CONTROL, INBD GREEN (34CE1), OPS CHECKED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041700042 20080417 00042 WP 2008 4 17 MWEA080051 1 20080401 A 2520 SEAT FRAME DOUG DC9 DC982 3022082 WP FLT ATTENDENT DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 809ME 48071 FORWARD FLIGHT ATTENDANT SEAT HAS THE TOP HINGE HARDWARE PULLED THROUGH THE STRUCTURE OF THE SEAT FRAME. REMOVED AND RE PLACED SEAT ASSEMBLY. 2 L 7 2 4F A6WE 2008041700052 20080417 00052 NM 2008 4 17 2008UALA01933 1 20080405 A 5230 STRIKER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CARGO DOOR LOOSE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 914UA 25381 RTFL FOR A REPORTED AFT CARGO DOOR WARNING. FOUND LOOSE STRIKER ON CARGO DOOR. TIGHTENED. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700055 20080417 00055 NM 2008 4 17 2008UALA01936 1 20080404 A 2910 7321870019 MODULE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FLAP/SLAT CRACKED A UALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 654UA 25392 AC ARRIVED CENTER HYD LOW, 68 PERCENT. FOUND FLAP SLAT HYD SHUTOFF MOD CRACKED AND LEAKING, RT WHEEL WELL. REPLACED HYD RAULIC SHUTOFF MODULE LEAK CHECKED OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041700057 20080417 00057 NM 2008 4 17 2008UALA01938 1 20080405 A 3150 873602 POWER SUPPLY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 775UA 26947 STATUS MESSAGE FLIGHT CONTROL SYSTEM. REPLACED LT PSA. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008041700066 20080417 00066 NM 2008 4 17 2008UALA02081 1 20080411 A 3150 WARNING MESSAGE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 217UA 30550 FLIGHT DIVERTED DUE A TEMP CONTROL VALVE STATUS MESSAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008041700068 20080417 00068 NM 2008 4 17 2008UALA02083 1 20080410 A 5230 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 AFT CARGO DOOR EXTERIOR SKIN HAS 7 DENTS IN VARIOUS LOCATIONS. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGED AREAS. FABRICA TED & INSTALLED EXTERNAL DOOR SKIN DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700071 20080417 00071 EU 2008 4 17 2008UALA02086 1 20080411 A 3350 32145410 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 424UA 506 EMERGENCY LIGHTS FAILS TEST. REPLACED 12WL POWER SUPPLY AND ASSOC BATTERY PACK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041700073 20080417 00073 NM 2008 4 17 2008UALA02088 1 20080410 A 5551 LUG BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 RT HORIZONTAL STABILIZER AFT SPAR UPPER LUG HAS EVIDENCE OF CORROSION. MAJOR REPAIR: REMOVED CORROSION. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700074 20080417 00074 NM 2008 4 17 2008UALA02089 1 20080409 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 1008 S13-14L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 DURING AIRCRAFT MAINTENANCE A DENT WAS FOUND AT BS 1008 BETWEEN STRINGERS 13L AND 14L. MAJOR REPAIR ACCOMPLISHED, REPLA CED SKIN PANEL ASSY BTWN BS 986.5 AND BS 1016, S10L - S14L. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700075 20080417 00075 NM 2008 4 17 2008UALA02090 1 20080410 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 ESCAPE PATH LIGHTING STRIP IN AFT GALLEY LOOSE. SECURED ELL STRIP END CAP. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700080 20080417 00080 NM 2008 4 17 2008UALA01948 1 20080404 A 5330 SERVICE PANEL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 THE FUSELAGE ABOVE THE AFT LAV SERVICE PANEL HAS A CREASE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED, FABRICAT ED AND INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER, TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700083 20080417 00083 CE 2008 4 17 220CM04A 1 20080401 A 2760 240805 VALVE CESSNA 650 650 2076802 CE NR 8 SPOILER FAILED E DBCA K NONE O OTHER IN INSP/MAINT 1 GL 13 220CM 6457 6500160 DURING PREFLIGHT, THE CREW NOTED THE RIGHT ROLL SPOILER DID NOT STOW WHEN SPOILER HOLD DOWN WAS SELECTED. MAINTENANCE V ERIFIED SQUAWK AND TRIP WAS MOVED TO ANOTHER AIRCRAFT. TROUBLESHOT AND FOUND THE NR 8 SPOILER HOLD DOWN RELEASE VALVE H AD FAILED IN THE RELEASE POSITION. STERLING MAINTENANCE REPLACED NR 8 SPOILER HOLD DOWN RELEASE VALVE WITH OVERHAULED U NIT. OPS CHECK GOOD. 2 L 7 2 4F A9NM 20080701 SO 2008 7 1 LR7A08080 1 20080605 A 5330 SKIN LKHEED 382 382G 526414U SO BS 99 DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 4676 DURING SCHEDULED A CHECK PER JOB CARD HA1200, FOUND FUSELAGE EXTERIOR SKIN DENT AT FS 99.0, WL 156, LBL 63. REPAIR ACCO MPLISHED IAW SMP 583 51-140-12 ON LOG PAGE 27239, ITEM M6. 2 H 7 4 4T A1SO 20080701 2008 7 1 USAA920081184 4 20080608 A 2565 POWER SUPPLY AIRCRUISERS AIRBUS 320 A320231 3930325 EU EVAC SLIDE FAULTED A USAA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 19 634AW 46457 A6650 091 FLT 193 LAS-PHX, EMERGENCY EQUIPMENT - AFT LEFT EMERGENCY POWER SUPPLY UNIT SHOWS INTERNAL FAULT. MAINTENANCE REMOVED A ND REPLACED THE R2 DOOR SLIDE RAFT ASSEMBLY. OPERATIONAL TEST GOOD, NO FAULTS. 2 L 7 2 4F RT A28NM 20080701 EA 2008 7 1 SWIA200819725 1 20080531 A 7603 THROTTLE CNDAIR CL600 CL6002B19 1900309 EA LEFT BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 439SW 7578 LEFT THROTTLE OCCASSIONALLY BINDS AND IS STIFF. (FLT 3801) REPLACED ENGINE THROTTLE CABLE ON LEFT SIDE IAW AMM 76-11-0 9. ENGINE RUN CHECK GOOD. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819718 1 20080527 A 2612 FIRE LOOP CNDAIR CL600 CL6002C10 1390015 EA RT NACELLE DISLODGED A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 754SK 10215 FIRE SYSTEM FAULT MESSAGE APPEARED INTERMITTENTLY INFLIGHT. (FLT 6131) REPOSITIONED FIRE LOOPS ON RIGHT ENGINE IAW AMM 26-11-01. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A21EA 20080701 SO 2008 7 1 SWIA200819719 1 20080601 A 2697 CONNECTOR EMB 120 EMB120ER 3260203 SO FIRE WARNING DIRTY A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 298SW 120328 CARGO FIRE "WARN" LIGHT STAYS ON AND WILL NOT TEST CORRECTLY. INSPECTED AND CLEANED CONNECTORS ON BOTH LEFT AND RIGHT CA RGO FIRE BOTTLES. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080701 EA 2008 7 1 SWIA200819709 1 20080410 A 7120 BUSHING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 954SW LEFT ENGINE FORWARD MOUNT BUSHINGS ARE CORRODED. (FOUND AT C-CHECK) REPLACED BUSHINGS ON MOUNT. 2 L 7 2 4F RT A21EA 20080707 WP 2008 7 7 UPS08852282 1 20080421 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LT WING CENTER L/E LOWER OUTBOARD. EXTERIOR SKIN GOUGED AND CORRODED AT CORNER SCREW HOLES. REPAIRE D LT WING CENTER L/E LOWER OUTBOARD. EXTERIOR SKIN IAW EO DC8-5720- -A AND SRM 57-03-03-0 FIG 005. 2 L 7 4 4F RT 4A25 20080707 NM 2008 7 7 2008UALA02816 1 20080515 A 5320 TORQUE TUBE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 CORROSION ON TORQUE TUBE BETWEEN STA 1263 AND STA 1285 AND STA 1285 AT LBL 6 TO RBL 16 IN AFT PIT. MAJOR REPAIR ACCOMPL ISHED: REPLACED WEB. 2 L 7 2 4F 4 F RT A1NM E24NE 20080707 NM 2008 7 7 2008UALA02817 1 20080515 A 2740 RUDDER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 RUDDER DAMAGED ON TRAILING EDGE BY MANLIFT OPERATION, APPROX .25 INCH DEEP BY 6 INCH LONG. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED AREA. INSTALLED LAY-UP REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20080707 NM 2008 7 7 2008UALA02818 1 20080515 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 AFT PIT FS 1414 STR 29R STRINGER CORRODED. MAJOR REPAIR ACCOMPLISHED, INSTALLED RIB, STRINGER AND STRINGER SPLICE AND W EB. 2 L 7 2 4F 4 F RT A2NM E17NE 20080707 NM 2008 7 7 2008UALA02828 1 20080516 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 SEAT 33 ABC EMERGENCY LIGHT INOP. RELAMPED. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 2008UALA02830 1 20080516 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 SEAT 5E EMERGENCY LIGHT INOP. FOUND LOOSE LIGHT CONNECTION. SECURED LIGHT ASSEMBLY. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 2008UALA02831 1 20080516 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 SEAT 4A EMERGENCY LIGHT INOP. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 BB08090 1 20080517 A 2560 P4010021 BATTERY BOEING 757 757225 1384959 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 920UW 22199 FLL - THE FLASHLIGHT AT THE FORWARD FLIGHT ATTENDANT STATION WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY TO THE F ORWARD FLIGHT ATTENDANT FLASHLIGHT. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 20080707 EA 2008 7 7 SWIA200819634 1 20080128 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 988CA 7204 FS 484 AT RBL 36 IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIR IAW BOMBARDIER REO 601R-53-41-059, STEPS 11-14. 2 L 7 2 4F RT A21EA 2008041700085 20080417 00085 EU 2008 4 17 2008UALA01951 1 20080404 A 2611 RAI2800M0706 CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SMOKE DETECTION ILLUMINATED A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 449UA 851 DISCH AGENT 2 LIGHT ILLUMINATED ON CARGO SMOKE PANEL. CAUSE, SCDU FAILURE, UNKNOWN CAUSE. REPLACED SCDU, GROUND TESTS WERE NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041700086 20080417 00086 EU 2008 4 17 2008UALA01952 1 20080404 A 2621 DISK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE APU FIRE BOTTLE DISLODGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 411UA 464 APU FIRE BOTTLE DISK DISLODGED. SUPPLEMENTAL DATA UPDATE, CAUSE, DISK WAS DETERIORATED. REPLACED FIRE BOTTLE DISK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041700092 20080417 00092 NM 2008 4 17 2008UALA01958 1 20080405 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1395 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 AFT PIT FRAME SHEAR TIES HAVE CORROSION BS 1395 RBL 1 AND LBL 8. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED, R EMOVED DAMAGED SHEAR TIE. FABRICATED AND INSTALLED NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041600016 20080416 00016 NM 2008 4 16 UIEA200800111 1 20080406 A 3150 WARNING MESSAGE BOEING 747 74747UF 1384812 NM THRUST REVERSER ILLUMINATED A UIEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 499MC 29260 ABORTED TAKEOFF DUE TO ENGINE 4 REVERSER EICAS MESSAGE APPEARED AT 70 KNOTS ON TAKEOFF ROLL. REJECTED TAKEOFF EICAS MES SAGE REPLACED WITH STATUS MESSAGE. DEACTIVATED THE REVERSER AND PLACED ON DMI PER MEL 78-31-01. 2 L 7 4 4F RT A20WE 2008041600026 20080416 00026 NM 2008 4 16 AALA200800772 1 20080330 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 772AN 29580 DFW - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041600034 20080416 00034 WP 2008 4 16 08FDEA01400 1 20080414 A 5315 AGA384717 FLOORBEAM DOUG DC10 DC1010F 3022111 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 MODIFICATION ACF FOUND IN AFT CARGO COMPT STA 1857 AT X 30 BEAM FLOOR WITH DOUBLE HOLE. REPAIRED FOR SRM 53-60-01 FIG 3 VOL I. 2 L 7 3 4F A22WE 2008041600045 20080416 00045 NM 2008 4 16 AALA200800787 1 20080401 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 782AN 30003 DFW - EMERGENCY LIGHT AT SEAT 21G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041600047 20080416 00047 WP 2008 4 16 AALA200800782 1 20080326 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 443AA 49469 TUL - EMERGENCY LIGHT BATTERY PACK AT OVERHEAD BIN AT STATION 243 FAILED OPERATIONAL CHECK. REPLACED BATTERY PACK AT OV ERHEAD STATION 243 FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008041600060 20080416 00060 NM 2008 4 16 UIEA200800101 1 20080402 A 7830 AMS55180063IN LOCK PLATE BOEING 747 747243B 1384830 NM THRUST REVERSER BROKEN A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 NR 4 ENGINE LEFT SIDE THRUST REVERSER FORWARD EDGE LOWER THRUST REVERSER LOCK PLATE POSITION TWO LOCK BOLTS HOLES BROKEN . REPAIRED PER CF6-50 ENGINE MANUAL 78-32-03. 2 L 7 4 4F RT A20WE 2008041600064 20080416 00064 NM 2008 4 16 EIA2008007 1 20080109 A 2612 BAC5308P11 SWITCH BOEING 747 747273C 1384896 NM FIRE DETECTION MALFUNCTIONED A EIAA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 471EV 20651 APU FIRE WARNING INDICATION AT 9500 MSL. ACCOMPLISHED IMMEDIATE ACTION ITEM (FIRE BOTTLE DISCHARGED). LIGHT AND BELL W ENT OUT IMMEDIATELY. DUMPED FUEL AND RETURNED TO JFK. INSPECTED APU COMPARTMENT FOR EVIDENCE OF FIRE NONE FOUND FIRE W ARNING SYSTEM AND APU DIFFERED. REPLACED SWITCH S4 IN M176 APU CONTROL MODULE PER 20-83-11 SWPM, ACCOMPLISHED OPS CHECK IAW 26-15-02 AND 26-15-00. 2 L 7 4 4F RT A20WE 2008041600065 20080416 00065 NM 2008 4 16 EIA2008013 1 20080307 A 3350 900835AB BATTERY PACK BOEING 747 747212B 1384886 NM EMERGENCY LIGHT DISCHARGED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 485EV 20712 UPPER DECK EXIT DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED UPPER EXIT DOOR EMERGENCY LIGHT BATTERY PACK IAW B747 M M 33-51-00, OPS CHECK NORMAL. 2 L 7 4 4F RT A20WE 2008041600078 20080416 00078 NM 2008 4 16 UIEA200800117 1 20080410 A 5313 T08A044741 STRINGER BOEING 747 747243B 1384830 NM BS 2357 S51R CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 AFT PRESSURE BULKHEAD STRINGER END FITTING CORROSION AT STA 2357 STR 51R, STRINGER AND FITTING REPLACED PER SRM 51-30-02 . 2 L 7 4 4F RT A20WE 2008041600088 20080416 00088 NM 2008 4 16 QXEA200800371 1 20080408 A 2611 SMOKE DETECTOR BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY NO TEST A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 405QX 4047 SEA- FLIGHT 2391- AFT BAGGAGE SMOKE DETECTOR NR 1 WON'T TEST. MAINTENANCE PLACED ON MEL 26-10-2A. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008041600101 20080416 00101 NM 2008 4 16 AALA200800739 1 20080327 A 3350 SIGN BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 603AA 27054 DFW - EMERGENCY EXIT LIGHT ARROW AT SEAT 17A IS PEELING OFF. REPLACED EXIT ARROW FOR EMERGENCY LIGHT AT SEAT 17A. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041600103 20080416 00103 NM 2008 4 16 AALA200800758 1 20080330 A 3350 767 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 678AN 29428 JFK - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. RESEATED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 2008041600108 20080416 00108 NM 2008 4 16 AALA200800743 1 20080328 A 3244 TIRE BOEING 777 777223 1385213 NM MLG PUNCTURED A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 763AN 31480 EZE INFLIGHT T943/28MAR - NUMBER ELEVEN TIRE PRESSURE DROPPED IN FLIGHT. LANDED EZE WITHOUT INCIDENT. FOUND NUMBER 11 TIRE PUNCTURED. REPLACED NUMBER 11 AND 12 TIRE/WHEEL ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041600111 20080416 00111 NM 2008 4 16 F3LA200800146 1 20080404 A 5321 D5361067400000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE 221EF DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 5380 1841 DURING C4 S1 C CHECK, INSPECTION REPORTED FLOOR PANEL 221EF HAD PUNCTURE DAMAGE. MAINTENANCE REPAIRED THE PUNCTURE IN T HE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-12-00. UPON COMPLETION OF THE REPAIR, THE PANEL WAS INSPECT ED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM 2008041600124 20080416 00124 NM 2008 4 16 QXEA200800340 1 20080328 A 6123 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 09 430QX 4163 SEA- FLIGHT 2289 (SEA-EUG) - ABORTED TAKEOFF AT 85 TO 90 KNOTS AND RETURNED TO THE GATE FOR AUTOFEATHER SYSTEM NOT ARMIN G. MAINTENANCE FOUND FAULT CODE 494 AND PERFORMED FIM TASK 61-20-10-810-826. AIRCRAFT RETURNED TO SERVICE. NO PARTS R EPLACED. 2 H 7 2 4T RT A13NM 2008041600128 20080416 00128 NM 2008 4 16 UIEA200800130 1 20080403 A 5730 SKIN BOEING 747 747243B 1384830 NM LWS 150-470 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 LEFT WBL 150 TO 470 HAS CORROSION EVIDENT BETWEEN MIDSPAR TO NR 1 BEAM. BLENDED OUT CORROSION PER SRM 51-10-01, REPROTE CTED PER SRM 51-10-02. 2 L 7 4 4F RT A20WE 2008041600136 20080416 00136 EA 2008 4 16 A6WA200840191 1 20080311 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 436AW 7734 CRACK FOUND ON THE FLOOR SUPPORT STRUCTURE AT FS 621 LBL 41 WL 73. REPAIR TO FLOOR ANGLE FS 621 CARRIED OUT IAW CRJ 200 REO 601R-53-61-117 REV C. (M) 2 L 7 2 4F RT A21EA 2008041600140 20080416 00140 WP 2008 4 16 AALA200800742 1 20080328 A 2560 P4010021000 BATTERY DOUG DC9 DC982 3022082 WP FLASHLIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 499AA 49737 LGA - EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED BATTERIES FOR EMERGENCY FLASHLIGHT AT AFT FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 2008041600163 20080416 00163 NM 2008 4 16 AALA200800760 1 20080330 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 767AJ 33539 JFK - EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 2008041600173 20080416 00173 WP 2008 4 16 NWAA081489921 1 20080411 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 943N 47647 DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY IN THE TAIL CONE AND OPERATIONALLY CHECKED THE SYSTEM. 2 L 7 2 4F A6WE 2008041600184 20080416 00184 EU 2008 4 16 08FDEA01413 1 20080415 A 5310 A52374351204 DOOR FRAME AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 745FD 668 FOUND CRACK IN FRAME HEAD C61A OF AFT CARGO DOOR. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080516 NM 2008 5 16 SWAA082624 1 20080513 A 5322 6546534 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 10R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008041700013 20080417 00013 NM 2008 4 17 2008UALA02101 1 20080410 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 665 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 CABIN LONGITUDINAL FLOORBEAM HAS A CRACK AT LIGHTENING HOLE JUST BELOW SEAT TRACK, LBL 25" BS 665. MAJOR REPAIR ACCOMPLI SHED: STOP DRILLED THE CRACKS AND VERIFIED CRACK TERMINATION WITH HFEC. INSTALLED REPAIR CHANNELS AT LBL & RBL 24.5. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700015 20080417 00015 NM 2008 4 17 2008UALA02103 1 20080410 A 5320 STRAP BOEING 737 737322 1384676 NM FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 'H' STRAP AT STR 13L HINGE LOCATION BTWN BS 294-303, STRINGER SPLICE CHANNEL CRACKED AT AFT EDGE. MAJOR REPAIR ACCOMPLI SHED: REPLACED THE INBD 'H' STRAP, INTERCOSTAL WEB, CLIPS AND ANGLE. INSTALLED FRAME WEB REPAIR DOUBLER. 2 L 7 2 4F RT A16WE 2008041700032 20080417 00032 NM 2008 4 17 2008UALA02120 1 20080411 A 2560 SMOKE GOGGLES BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 1ST OFFICER'S CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 F/O SMOKE GOGGLES ARE CRACKED. REPLACED GOGGLES. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700043 20080417 00043 WP 2008 4 17 MWEA080050 1 20080401 A 5311 9912243241 FRAME DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 809ME 48071 AFT CARGO COMPARTMENT HAS CORROSION ON UPPER SURFACE OF FRAME LOWER LEG BETWEEN LONGERON 29 LEFT AND 29 RIGHT AT FRAME S TATION 1309. REMOVED CORROSION WAITING FOR MORE INFORMATION ON FIX 2 L 7 2 4F A6WE 2008041700048 20080417 00048 WP 2008 4 17 UPS08851964 1 20080228 A 5740 3344046501 FITTING DOUG DC8 DC873F 302199F WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 NR 1 ALT THRU 560A BETWEEN XRS 428 AND XRS 463 STRINGER TO FRONT SPAR FITTING CRACKED. REPLACED NR 1 ALT FRONT SPAR FITTING BETWEEN XRS 428 AND XRS 463 IAW DWG 3644046, SRM 51-03-02, SRM 51-01-08, SRM 51-01-20D AND SRM 5 1- 01-12. 2 L 7 4 4F RT 4A25 20080707 EA 2008 7 7 HNAA0800161 1 20080514 A 6123 M390166141P RELAY DHAV DHC8 DHC8311 1386006 EA AUTOFEATHER SYS FAULTY A HNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 07 329EN 290 ON TAKEOFF ROLL, AUTO FEATHER ARM LIGHT EXTINGUISHED. 2 H 7 2 4T RT A13NM 20080707 2008 7 7 HNAA0800160 4 20080508 A 3442 MI5853505 RADAR DHAV DHC8 DHC8102 2809003 NM WEATHER RADAR FAULTY A HNAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 07 837EX 974 138 217 WHILE EN ROUTE TO ROA AT 9,000 FT, THE WX RADAR WENT INOP. 2 H 7 2 4T RT A13NM 20080707 SO 2008 7 7 RAIA00805020 1 20080517 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 825HK 145510 PRE FLT 5545 - STL - EMERGENCY LIGHTING FLOOR STRIPS INOPERATIVE. MAINTENANCE RESEATED A LOOSE CONNECTOR TO THE LIGHT S TRIP. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080707 SO 2008 7 7 RAIA00805017 1 20080514 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 829HK 145281 PRE FLT 8033 - MDT - OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AT THE LIGHT ASSEMBLY. O PERATIONAL CHECK OF THE LIGHT PROVED GOOD. 2 L 7 2 4T RT T00011AT 20080707 NM 2008 7 7 DHL2008764508 1 20080520 A 5347 SEAT TRACK BOEING 727 727264 138408M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 CORROSION ON MAIN CABIN SEAT TRACK BS 480-620 RBL 45. SEAT TRACK CORRODED OUT OF LIMITS IAW B727 SRM 51-20-2 FIG 21 AND 53-10-1 FIG 3. FAB NEW SECTION WITH BAC 1520-792-7178T6 DIM 12'6 3/8 INCH AND PO 9006020 IAW B727 SRM 53-10-5 FIG 1 AN D VENTURA AEROSPACE DWG 2902. 2 L 7 3 4F A3WE 20080707 SO 2008 7 7 C2XA08CL060 1 20080519 A 2133 2097K011100 OUTFLOW VALVE EMB 145 EMB145LR 3260212 SO CABIN PRESSURE FAULTY A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 14972 17749 145151 CLE FLIGHT 2039 THE CREW REPORTED ON TAKEOFF FROM CLE THE AIRCRAFT WOULD NOT PRESSURIZE. TRIED MANUAL MODE WITHOUT SUCC ESS. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE ELECTRO PNEUMATIC OUTFLOW VALVE AND REMOVED DEBRIS FROM MANUAL CONTROLLER VENT SCREEN. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20080707 NM 2008 7 7 HNAA0800163 1 20080513 A 3297 WIRE DHAV DHC8 DHC8102 2809003 NM LOOSE A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 911HA 034 AFTER GEAR WAS RETRACTED VIA NORMAL PROCEDURES, THE GEAR DOORS REMAINED OPEN WITH THE LANDING GEAR DOOR LIGHTS ILLUMINAT ED. THE GEAR WAS CYCLED AND THEN RETRACTED AGAIN. THE DOORS DID NOT CLOSE AND THE DOOR LIGHTS REMAINED ILLUMINATED. F OUND INHIBIT SWITCH, NR 25 TERMINAL TO HAVE TWO LOOSE WIRES. SECURED WIRING. EVAL FLIGHT, SATISFACTORY. OPERATIONAL C HECK GOOD. 2 H 7 2 4T RT A13NM 20080707 GL 2008 7 7 C2XA08TY051 2 20080518 A 7261 SEAL EMB 145 EMB145XR 3260214 SO ALLSN AE3007 AE3007A 03030 GL NR 1 ENGINE LEAKING A C2XA K NONE K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SW 27 14116 145672 LAV SMOKE DETECTOR WENT OFF ON SHORT FINAL AND WENT AWAY AFTER LANDING/IDLE SET. FOUND ENGINE NR 1 ZERO BEARING SEAL LE AKING. AIRCRAFT STILL IN MAINTENANCE. 2 L 7 2 4F 4 F RT TE6CH 20080707 NM 2008 7 7 KCSA081254 1 20080520 A 3350 LIGHT BOEING 747 747221F 1384868 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 747CK 21743 EMERGENCY LIGHT ON RIGHT UPPER DECK SLIDE HAS ONE BULB BURNED OUT. 2 L 7 4 4F RT A20WE 20080707 NE 2008 7 7 ASAA0852971 2 20080517 A 7261 CFM567B27 ENGINE BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE NR 2 OIL CONSUMPTION A ASAA O OTHER O OTHER IN INSP/MAINT 1 NM 02 587AS 2210 35684 895978 NR 2 ENG OIL CONSUMTION AT .61 NR 2 ENG OIL CONSUMTION AT ALERT. AIRCRAFT RESTRICTED FROM ETOPSSERVICE UNTIL OIL CONS UMPTION WITHIN LIMITS. INSPECTED INLET EXHAUST AND DRAINS. REF MM 71 71 00 PG 602, NOSIGNS OF LEAKAGE. OIL CONSUMPT ION RATE IS NOW .20 BELOW ETOPS MAX CONSUMPTION RATE OF .60 ACFT IS NOW ETOPS CERTIFIED. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080707 NM 2008 7 7 NOCA04208 1 20080521 A 5320 140T25409 INTERCOSTAL BOEING 767 76739H 1385311 NM FUSELAGE CRACKED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 760NA 26257 INTERCOSTAL ANGLE CRACKED AT CABIN FLOOR SUPPORT STA 1395-1417 AT LBL 40 AROUND NUT PLATE. REPLACED INTERCOSTAL AS PER SRM 51-70-13. 2 L 7 2 4F RT A1NM 20080707 NM 2008 7 7 UPS08652300 1 20080515 A 5720 114T02212 ANGLE BOEING 767 76734AF 1385212 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 302UP 27240 INSPECTION TYPE:C RIGHT WING LES 679 FRONT SPAR SUPPORT ANGLE FOUND CRACK. CRACK LENGTH .375 INCH APPROX. RIGHT WING L ES 679 FRONT SPAR SUPPORT ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20080707 NM 2008 7 7 UPS08652301 1 20080513 A 5320 140T0130U39 BRACKET BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 302UP 27240 INSPECTION TYPE:C AFT CARGO COMPT STA 1087 LBL 25" END WALL SUPPORT LOWER BRACKET CRACK. CRACK LENGTH .875 INCH APPROX. AFT CARGO COMPT STA 1087 LBL 25" LOWER SUPPORT BRACKET REPLACED PER SRM 51-10-02 AND INSTALLED PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 20080707 NM 2008 7 7 UPS08652302 1 20080513 A 5320 140T0130U38 BRACKET BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 302UP 27240 INSPECTION TYPE:C AFT CARGO COMPT STA 1087 RBL 25" END WALL SUPPORT LOWER BRACKET CRACK. CRACK LENGTH .75 INCH APPROX. AFT CARGO COMPT STA 1087 RBL 25" LOWER SUPPORT BRACKET REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20080707 NM 2008 7 7 2008UALA02839 1 20080516 A 5310 CREASE BEAM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 910UA 25254 FUSELAGE STR 17R CREASE BEAM NEEDS CUT AT BS 400. MAJOR REPAIR ACCOMPLISHED, FABRICATED REPAIR ANGLES AND INSTALLED NES TED ANGLE DOUBLER/TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 20080707 NM 2008 7 7 2008UALA02840 1 20080516 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 AFT PIT STA 1500, STR 25L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGE. INSTALLED "J" ANGLE REPAIR. HFEC IN SPECTION VERIFIED DAMAGE REMOVED. NO CRACKS NOTED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080708 NM 2008 7 8 ABXA080153 1 20080517 A 2613 233T620411 CONTROL PANEL BOEING 767 767200 1385120 NM GE CF6 CF680A 30025 NE COCKPIT DEFECTIVE A ABXA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 799AX 23432 580343 AFTER TAKEOFF FROM STA JFK, RIGHT ENGINE OVERHEAT LIGHT AND EICAS MESSAGE. PERFORMED NON NORMAL - SECURED RIGHT ENGINE. LIGHT DID NOT GO OUT AFTER THRUST LEVER RETARDED. AN EMERGENCY WAS DECLARED AND AN AIR TURNBACK TO JFK WAS PERFORMED. TROUBLESHOT PER FIM 26-11-00, PERFORMED ENGINE FIRE/OVERHEAT TEST AND "RIGHT ENGINE OVERHEAT" LIGHT AND EICAS MESSAGE STAYED ILLUMINATED AFTER TEST WITH ENGINE SHUT DOWN AND NO OVERHEAT CONDITION. RIGHT ENGINE OVERHEAT INDICATION SYSTEM AT FAULT. REMOVED AND REPLACED FIRE/OVERHEAT TEST PANEL IAW AMM 26-11-01. FIRE/OVERHEAT TEST CHECKED GOOD PER AMM 26-1 1-01. (PART REMOVED WAS 'F' CLASS). 2 L 7 2 4F 4 F RT A1NM E13NE 20080708 NM 2008 7 8 HNAA0800170 1 20080515 A 3260 858601 PSEU DHAV DHC8 DHC8102 2809003 NM LANDING GEAR MALFUNCTIONED A HNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 07 911HA 31636 31636 034 AFTER DEPARTURE CYCLED GEAR UP AND GEAR DOORS DID NOT CLOSE. RETURNED TO FIELD SELECTED GEAR DOWN. UPON GEAR DOWN SELE CTION ALL GEAR DOORS CLOSED. REMOVED AND REPLACED PSEU AND TESTED IAW 32-61-50, CYCLED GEAR IN NORMAL AND ALT OPS SATIS FACTORY. 2 H 7 2 4T RT A13NM 20080708 NM 2008 7 8 HNAA0800171 1 20080515 A 3231 DOOR DHAV DHC8 DHC8102 2809003 NM LANDING GEAR OPEN A HNAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 07 911HA 034 ACFT RELEASED FOR EVAL FLT DUE TO GEAR DOOR REMAINS OPEN AFTER GEAR RETRACTION. MX ACTION COMPLETE SUBJECT SATISFACTORY EVAL FLT. 2 H 7 2 4T RT A13NM 20080708 NM 2008 7 8 BB08092 1 20080520 A 2560 P4010021 BATTERY BOEING 767 7672B7 1385107 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 251AY 24764 PHL - THE RED LIGHT DOES NOT BLINK ON THE RIGHT, AFT FLASHLIGHT. MAINTENANCE REPLACED THE BATTERY ON THE RIGHT, AFT FLA SHLIGHT. 2 L 7 2 4F RT A1NM 20080708 NM 2008 7 8 HNAA0800172 1 20080515 A 3231 DOOR DHAV DHC8 DHC8102 2809003 NM LANDING GEAR CLOSED A HNAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 07 911HA 034 ACFT RELEASED FOR EVAL FLT DUE TO GEAR DOORS WOULD NOT OPEN AND GEAR WOULD NOT RETRACT. MX ACTION COMPLETE SUBJECT SATI SFACTORY EVAL FLT. EVAL FLT UNSATISFACTORY. 2 H 7 2 4T RT A13NM 20080708 NM 2008 7 8 USAA920081094 1 20080419 A 5320 143N5158 STRAP BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - CRACKED FLOORBEAM STABILIZER STRAP, BS 377.7 - 395, LBL 24.75. REPLACED FLOORBEAM STAB ILIZER STRAP, BS 377.7 - 395, LBL 24.75 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 20080708 NM 2008 7 8 2008UALA02864 1 20080518 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 FWD CARGO PIT STRINGER CLIP CRACKED AT BS 380 AND STRINGER S-21L. MAJOR REPAIR ACCOMPLISHED, REMOVED AND REPLACED DAMAG ED STRINGER CLIP WITH NEW. 2 L 7 2 4F 4 F RT A16WE E2GL 20080708 NM 2008 7 8 2008UALA02867 1 20080518 A 3510 OXYGEN SYSTEM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CREW O2 LOW A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 386UA 24661 CREW O2 INDICATES 1000PSI. 2 L 7 2 4F 4 F RT A16WE E2GL 20080708 EU 2008 7 8 2008UALA02873 1 20080518 A 2730 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MALFUNCTIONED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 477UA 1514 ELAC 2 PITCH FAULT AFTER FIRST ENG START ON GROUND SWITCH CYCLE. RESET ECAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20080708 NM 2008 7 8 2008UALA02875 1 20080517 A 3350 1619 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 315UA 23947 EMERGENCY SLIDE LIGHT INOP DOOR 1L. RELAMPED. 2 L 7 2 4F 4 F RT A16WE E2GL 20080708 NM 2008 7 8 2008UALA02892 1 20080519 A 3350 582233 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 ALL RIGHT SEAT EEL LIGHTS INOP, 'D' ZONE. REPLACED BATTERY PACK ABOVE DOOR 3R. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 2008UALA02894 1 20080518 A 2697 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 SQUIB DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 ENGINE NR 2 SQUIB, NR 2 TEST FAILS. FOUND DIRTY CONNECTION. CLEANED CONNECTION OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 2008UALA02779 1 20080514 A 2560 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GIRT BAR SHORTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 581UA 26701 NR 1 RT GALLEY DOOR SLIDE ARM LIGHT ONLY FUNCTIONS ON DIM. *S/D* GIRT BAR SWITCH HAS ELECTRICAL SHORT. REPLACED GIRT BAR SWITCH IN FWD POSITION, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080708 EU 2008 7 8 2008UALA02798 1 20080515 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 446UA 834 FOUND CORROSION ON FLOORBEAM NR 165. MAJOR REPAIR ACCOMPLISHED: REPLACED BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041700049 20080417 00049 WP 2008 4 17 UPS08851965 1 20080228 A 5340 3755028504 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:C2 NR 2 MAIN THRU 560F AT XRS 23 1ST CLIP FROM R/S CRACKED. FABRICATED AND REPLACED NR 2 MAIN TANK CLIP AT XRS 23 IAW DWG 3755028, SRM 51-01-08, SRM 51-01-20D, SRM 51-03-01. 2 L 7 4 4F RT 4A25 2008041700058 20080417 00058 EU 2008 4 17 2008UALA01940 1 20080404 A 3350 32145410 BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 473UA 1469 EMERGENCY LIGHTS REQUIRE BATTERY CAPACITY TEST PER A CHK. SUPPLEMENTAL DATA UPDATE, REPLACED EPSU BATTERIES. OPS CHK N ORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041700063 20080417 00063 WP 2008 4 17 UPS08851983 1 20080409 A 7830 THRUST REVERSER DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 2 MALFUNCTIONED A IPXA O OTHER J WARNING INDICATION DE DESCENT 1 SO 01 818UP 46108 DURING DESCENT NR 2 THRUST REVERSER W/NOT STOW IN FWD THRUST INDICATION BLINKED ON AND OFF. DEFERRED NR 2 ENGINE T/R, I N FWD THRUST POSITION. PLACARD INSTALLED. T/S PER MM 78-00-00-1 FIG 190 SHEETS 1-3. NO DEFECTS NOTED. THIS CLEARS M373 174. PLACARD REMOVED. OPS CHECK GOOD ON GROUND. 2 L 7 4 4F 4 F RT 4A25 E2GL 2008041700064 20080417 00064 EU 2008 4 17 2008UALA01941 1 20080404 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 442UA 780 FUSELAGE DENT APPROX 14 INCHES FORWARD OF L-1 ENTRY DOOR ON NEAR CENTER LINE OF AIRCRAFT. MAJOR REPAIR ACCOMPLISHED, FA BRICATED AND INSTALLED PATCH AND DOUBLER. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041700093 20080417 00093 NM 2008 4 17 2008UALA01959 1 20080405 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1197 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 AFT CARGO COMPT AT BS 1197 AND LBL 20-25, FRAME T-CAP IS CORRODED AROUND NUT PLATE FASTENER HOLES. MAJOR REPAIR ACCOMPL ISHED, REMOVED DAMAGED SECTION OF PIT FLOOR T-CAP. SPLICED IN NEW SECTION. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041700096 20080417 00096 NM 2008 4 17 2008UALA01962 1 20080405 A 3350 20131A LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FWD GALLEY FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 669UA 30025 EMERGENCY PATH LIGHTING FLICKERS ON AND OFF IN FORWARD GALLEY AND FIRST CLASS ONLY. SUPPLEMENTAL DATA UPDATE, REPLACED POWER SUPPLY BATTERY M1577. CHECKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041700097 20080417 00097 NM 2008 4 17 2008UALA01963 1 20080405 A 3150 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE ILLUMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 PACK "OFF" LIGHT AND "PACK OFF" EICAS MESSAGE DISPLAYED WITH PACK SELECTED TO AUTO. NO "PACK TEMP" OR "INOP" LIGHT DISP LAYED. RECURRED ON FLT 0059-07. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041700098 20080417 00098 NM 2008 4 17 2008UALA01964 1 20080407 A 5230 65B043081 DOOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FWD CARGO OUT OF TOLERANCE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 70823 24322 FWD CARGO DOOR AFT LOWER CORNER FAIR TOLERANCE OUT OF LIMIT. MAJOR REPAIR ACCOMPLISHED IAW SRM52-30-01 FIG 201. FAIR TOLERANCE CHECKED GOOD ACTUAL:0.020" PER MM52-34-00. NO FURTHER ACTION REQUIRED.AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700104 20080417 00104 NM 2008 4 17 2008UALA01970 1 20080407 A 3510 3686500 OXYGEN MASK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE OXYGEN SYSTEM OBSTRUCTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 CREW O2 READS LOW. SUPPLEMENTAL DATA UPDATE, ISOLATED O2 LEAK TO FIRST OBSERVER'S O2 MASK. WITH MASK PLUGGED INTO FITT ING MASK LEAKS. WITH MASK UNPLUGGED FROM FITTING NO LEAKS FROM FITTING. NEEDS NEW FITTING ASSY. REPLACED 1ST OBSERVER 'S OXYGEN FITTING. LEAK CHECKED SYS CKS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700106 20080417 00106 NM 2008 4 17 2008UALA01972 1 20080407 A 2121 FAN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 793UA 26946 F/A'S REPORTED SCREECHING SOUND AND SMOKE ODOR IN 1ST CLASS. CMC INDICATED AN OVERHEAT OF THE EQUIP COOLING VENT FAN. REPLACED COOLING VENT FAN PER MM21-27-20 AND OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008041700108 20080417 00108 NM 2008 4 17 2008UALA01974 1 20080405 A 3350 1619 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 364UA 24533 OUTSIDE EMERGENCY EXIT LIGHT AFT OF LEFT WING ON BODY FAIRING IS INOPERATIVE. SUSPECT BURNED OUT BULB. REPLACED LIGHT OP S CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700116 20080417 00116 NM 2008 4 17 2008UALA01982 1 20080404 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 560UA 26660 EMERGENCY LIGHT INOP AT DOOR 1R. FOUND BULB INOP. RELAMPED BULB. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700118 20080417 00118 NM 2008 4 17 2008UALA01984 1 20080404 A 2530 COFFEEMAKER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE GALLEY FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 666UA 29238 FA SHOCKED WHEN GRABBING BOTH HANDLES OF THE COFFEE POTS AT 2R. REPLACED M51 & M52 COFFEE MAKER - OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041700119 20080417 00119 NM 2008 4 17 2008UALA01985 1 20080406 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 2J AFT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 SEAT 2J AFT EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE, RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700120 20080417 00120 NM 2008 4 17 2008UALA01986 1 20080406 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 4F AFT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 SEAT 4F AFT EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE, RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700127 20080417 00127 NM 2008 4 17 2008UALA01992 1 20080407 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 SEAT 56 ABC EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700136 20080417 00136 NM 2008 4 17 2008UALA02004 1 20080407 A 5753 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE RT WING TE FLAP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 829UA 1211 FOUND RIGHT OTBD FLAP HAS A HOLE AND A DENT AT THE MIDDLE AFT SECTION. REPAIRED DAMAGED AREA OF FLAP. (POTTED COMPOSIT E REPAIR) 2 L 7 2 4F 4 F RT A28NM E40NE 2008041700141 20080417 00141 NM 2008 4 17 KCSA08023 1 20080330 A 5312 PRESSURE PANEL BOEING 747 747123 1384873 NM FUSELAGE LEAKING A KCSA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 GL 23 717CK 20325 UNABLE TO MAINTAIN CABIN ABOVE FL 260. COMPLETED ALL CHECK LISTS BUT STILL UNABLE TO MAINTAIN ALT. FOUND 8 INCH DIAMET ER HOLE IN PRESSURE PAN ASSY. INSTALLED NEW PRESSURE PANEL ASSY PER SRM 51-30-02, 51-10-01 AND 51-10-06. PRESSURIZATIO N LEAK CHECK GOOD PER MM 21-31-00. 2 L 7 4 4F RT A20WE 2008041700145 20080417 00145 NM 2008 4 17 2008UALA02012 1 20080407 A 5210 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PAX DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 FWD ENTRY DOOR FRAME AND INNER SKIN CRACKED AT STOP PIN LOCATED AT AFT SIDE UNDER CENTERING FITTING. MAJOR REPAIR ACCOM PLISHED, FABRICATED AND INSTALLED INNER SKIN AND FRAME REPAIR DOUBLERS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700151 20080417 00151 NM 2008 4 17 2008UALA02022 1 20080408 A 2121 5649029 FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT RECIRCULATION SMOKE A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 586UA 26710 THERE IS SMOKE IN THE COCKPIT, PACKS WERE OFF AND GROUND AIR WAS ON. TURNED OFF UTILITY BUSS AND RECIRCULATION FANS. S MOKE WENT AWAY. FOUND BAD PART OUT OF STOCK (INSTALLATION OF CABIN AIR RECIRCULATION FAN (LEFT) ) BEARING FAILURE. REINSTALLED CABIN AIR RECIRCULATION FAN (LEFT) 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700152 20080417 00152 NM 2008 4 17 2008UALA02025 1 20080408 A 3350 417U51231 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY EXIT LIGHT INOP AT STAIRS LEADING TO UPPER DECK. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700164 20080417 00164 NM 2008 4 17 UIEA200800141 1 20080408 A 5311 FRAME BOEING 747 747243B 1384830 NM BS 1780 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK STA 1780 STRINGER 11R FRAME FOUND CRACKED. FRAME REPAIRED PER ATLAS EO NR 4753A141. 2 L 7 4 4F RT A20WE 2008041700168 20080417 00168 NM 2008 4 17 UIEA200800148 1 20080407 A 5754 FAIRING BOEING 747 747243B 1384830 NM LE FLAP CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 LEFT WING VARIABLE CAMBER FLAP BULLNOSE FAIRING OUTBOARD FORWARD CORNER CRACKED. REPAIRED BULLNOSE PER SRM 57-50-03. 2 L 7 4 4F RT A20WE 2008041700172 20080417 00172 NM 2008 4 17 UIEA200800152 1 20080409 A 5730 SKIN PANEL BOEING 747 747243B 1384830 NM LT WING CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 LEFT WING LEADING EDGE NOSE CAP UPPER CHORD FOUND CRACK JUST INBOARD OF NR 6 VARIABLE CAMBER FLAP UPPER STOP FITTING. F ABRICATED AND REPAIRED DAMAGED AREA IAW SRM 57-20-03. 2 L 7 4 4F RT A20WE 2008041700173 20080417 00173 SO 2008 4 17 CHQA200800077 1 20080412 A 2121 4611028900 FAN EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL CABIN INOPERATIVE A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 259JQ 13898 4590 145763 CAE311619 FLIGHT 3019, GSO TO CLT, DURING INITIAL CLIMB AT APPROXIMATELY 2,000 FT THE FLIGHT ATTENDANT REPORTED VISIBLE SMOKE IN T HE CABIN EMANATING FROM THE GASPER VENTS. THE FLIGHT CREW CONTACTED DEPARTURE TO RETURN TO FIELD AND FOLLOWED APPROPRIA TE QRH CHECKLISTS. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RAN ENGINES AND TRACED T HE SOURCE OF THE SMOKE TO THE AFT CABIN RECIRCULATION FAN. THE RECIRCULATION FAN WAS REPLACED AND THERE WERE NO FURTHER SIGNS OF SMOKE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008041700175 20080417 00175 NM 2008 4 17 NWAA081563162 1 20080415 A 2530 351005301 COFFEEMAKER AIRBUS A319 A319114 3930350 NM GALLEY SMOKE A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 362NB 1982 FIRST CLASS COFFEEMAKER MADE A LOUD POP WITH SMOKE, LANDING UNEVENTFUL. FOUND COFFEEMAKER BOTTOM DAMAGED AND CIRCUIT BR EAKER ON BACK OF COFFEEMAKER POPPED. REPLACED COFFEEMAKER AND CHECKS OK. 2 L 7 2 4F RT A28NM 2008041700178 20080417 00178 NM 2008 4 17 QXEA200800376 1 20080413 A 3231 ROD END BOMBDR DHC8 DHC8402 1390042 NM NR 2 MLG DOOR OUT OF ADJUST A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 408QX 4050 SEA - FLIGHT 2233 - AFTER TAKEOFF, THE RIGHT MAIN GEAR DOOR ADVISORY LIGHT REMAIN ILLUMINATED FOR ABOUT 1.5 MINUTES. AI RSPEED WAS ABOUT 180 KNOTS WHEN THE LIGHT WENT OUT. FERRIED THE AIRCRAFT TO PDX. ADJUSTED THE NR 2 MLG RETRACT ACTUATO R ROD END 1 FULL TURN IN IAW RD 8/4-32-059. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008041700179 20080417 00179 NM 2008 4 17 QXEA200800378 1 20080413 A 2120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 424QX 4006 AFT FLIGHT ATTENDANT REPORTED A STRONG POTENT ODOR LIKE ROTTEN EGGS DURING THE CLIMB AND DESCENT. MAINTENANCE PERFORMED GROUND RUNS FOR 25 MINUTES WITH NO DEFECTS OR SMELL NOTED. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008041700183 20080417 00183 NM 2008 4 17 DL76S080574 1 20080409 A 2530 COFFEEMAKER BOEING 767 767332 1382001 NM AFT 4 GALLEY INOPERATIVE A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 132DN 24981 AFT GALLEY NR 4 COFFEEMAKER INOP. HEATING ELEMENT FOR POT WARMER BROKEN CAUSING IT TO SMOKE. REMOVED AND REPLACED COFF EEMAKER. 2 L 7 2 4F RT A1NM 2008041700185 20080417 00185 NM 2008 4 17 DL757080578 1 20080410 A 3397 CONNECTOR BOEING 757 757232 1384965 NM EMERGENCY LIGHT BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 699DL NA 29970 EMERGENCY LIGHT OUT AT SEAT 4D, DEF PER MEL 33-51-03. FOUND WIRE BROKEN BETWEEN SEAT LEG CONNECTOR AND WALL CONNECTOR. REPLACED SAME. OPS CKS GOOD. MCO AND PLACARD REMOVED. 2 L 7 2 4F RT A2NM 2008041700192 20080417 00192 EA 2008 4 17 SWIA200819476 1 20080409 A 3350 SIGN CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS LOOSE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 812SK 15098 FLT 1994 - EXIT SIGN ABOVE GALLEY SERVICE DOOR IS INOP. RESECURED EXIT SIGN. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 2008041800004 20080418 00004 NM 2008 4 18 HNAA0800124 1 20080402 A 3350 OL3071BPEGPL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 936HA 49572 49572 145 DURING RON MAINTENANCE, THE EMERGENCY LIGHT LOCATED UNDER THE LEFT EMERGENCY EXIT DOOR WAS FOUND TO BE DIM. SEVERAL BUL BS IN THE LIGHT PANEL WERE FOUND TO BE INOPERATIVE. THE BULBS WERE REPLACED AND OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 2008041800007 20080418 00007 2008 4 18 ZZDA2008087 4 20080405 A 2565 D29982225 SLIDE BOEING 717 717200 1383700 NM L1 DOOR UNSERVICEABLE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 948AT 55011 L1 DOOR SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED L1 DOOR SLIDE REF B717 M/M 25-61-01. 2 L 7 2 4F TR A6WE 2008041800009 20080418 00009 NM 2008 4 18 USAA920080754 1 20080406 A 3397 BR963180 WIRE HARNESS BOEING 737 73733A 1384673 NM CABIN DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 168AW 23629 FLT 525 - RNO-PHX - EEL - ROW 10 EMERGENCY EXIT LIGHT INOP, WIRE PULLED OUT OF BAYONET. MAINTENANCE REPLACED THE SEAT E LECTRICAL HARNESS. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2008041800018 20080418 00018 NM 2008 4 18 USAA920080772 1 20080314 A 5322 6948204 SHEAR TIE BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED SHEAR TIE, BS 360, S14L - S15L. REPLACED SHEAR TIE, BS 360, S14L - S15L IAW B7 37 SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041800021 20080418 00021 SO 2008 4 18 C2XA08CL042 1 20080404 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13992 145284 DURING ROUTINE MAINTENANCE THE AISLE PATH EMERGENCY LIGHTS STRIP 4 AND 5 WERE INOPERATIVE ALONG WITH BOTH OVERWING EMERG ENCY EXIT IDENTIFIER SIGNS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED EMERGENCY LIGHT INVERTER NR 5. OPERATI ONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008041800029 20080418 00029 SO 2008 4 18 FDKA200804147 1 20080405 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6118 IAD-CVG (0355 PHX LCL). EMERGENCY LIGHTS ABOVE ROW 12 WERE INOPERATIVE. MX SECURED LOOSE CONNECTOR AND OPS CH ECKED. 2 L 7 2 4T RT T00011AT 2008041800030 20080418 00030 SO 2008 4 18 FDKA200804148 1 20080405 A 5210 DOOR EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 845MJ 145502 FDM 6181 CVG-LIT (0612 PHX LCL). MAIN CABIN DOOR DIFFICULT TO OPEN FROM THE INSIDE. MX CLEANED AND LUBED, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008041800034 20080418 00034 WP 2008 4 18 ABXA080121 1 20080408 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 946AX 47003 FLIGHT COMPARTMENT EMERGENCY FLOODLIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53- 00-4. 2 L 7 2 4F A6WE 2008041800039 20080418 00039 NM 2008 4 18 BB08054 1 20080406 A 2780 WARNING SYSTEM BOEING 767 7672B7 1385107 NM L/E SLAT FALSE ACTIVATION A USAA O OTHER N S FALSE WARNING AFFECT SYSTEMS AP APPROACH 1 EA 19 253AY 24894 MAD - FLT 730 PHL TO MAD. DURING APPROACH, THE FLAPS AUTOMATICALLY LOCKED AT 20 DEGREES DUE TO A LEADING EDGE SLAT ASY MMETRY WARNING. THE CREW DECLARED AN EMERGENCY, ACCOMPLISHED QRH PROCEDURES, AND LANDED WITHOUT FURTHER INCIDENT. MAIN TENANCE PERFORMED A BITE CHECK OF THE FSEU, AND OPERATED THE SLATS/FLAPS OVER A FULL RANGE. NO DEFECTS WERE NOTED. ALS O, THE PHYSICAL INSPECTION OF THE SLATS IN THE DEPLOYED POSITION REVEALED NO DEFECTS. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 2008041800040 20080418 00040 2008 4 18 BB08055 4 20080407 A 3497 PIN BOEING 767 7672B7 1385107 NM TRANSPONDER BACKED OUT A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 255AY 25257 MXP - FLT 717 EN ROUTE MXP TO PHL. AFTER TAKEOFF, EICAS MESSAGE 'ATC FAULT', AND ATC FAULT LIGHT ILLUMINATED WITH THE TRANSPONDER SELECTED IN LEFT AND RIGHT. THE FLIGHT RETURNED TO MXP AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE IN SERTED A PIN IN THE CONTROL PANEL CONNECTOR. BITE CHECKED OK. 2 L 7 2 4F RT A1NM 2008041600174 20080416 00174 EU 2008 4 16 EPUA040808 1 20080408 A 5330 SKIN REIMS 406 F406 7535723 EU BS 154-175 CRACKED E EPUA K NONE O OTHER IN INSP/MAINT 1 AL 03 406GV F4060049 DURING A ROUTINE INSPECTION A LARGE STRESS CRACK WAS DISCOVERED EMANATING FROM THE BASE OF THE UPPER VHS COMM ANTENNA BA SE AT FS 154.80 RIGHT OF CENTERLINE. THE DAMAGED SKIN WAS REMOVED AND REPLACED, WITH NEW DOUBLER AND ANTENNA. AIRCRAFT WAS RETURNED TO SERVICE. 1 L 7 2 3T RT A54EU 2008041600175 20080416 00175 EU 2008 4 16 08FDEA01410 1 20080415 A 5754 A57865200175 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 3 SLAT DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 FOUND DENTS ON LEADING EDGE SLAT NR 3 RT FLUSH DOUBLER REPAIR PERFORMED IAW RAS/FOK/022/2008, APPROVED BY EA 6-5744-1152 45. 2 L 7 2 4F RT A35EU 2008041600188 20080416 00188 EU 2008 4 16 TRBA2008040 1 20080412 A 3350 LP1670 LAMP AEROSP ATR72 ATR72212 8680945 EU EMERGENCY LIGHT FAILED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 29 448AM 448 ONE OF THE FLOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED FLOOR EMERGENCY LAMP IAW JIC NR 33-50-00. 2 H 7 2 4T RT A53EU 20080708 EU 2008 7 8 2008UALA02811 1 20080516 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 446UA 834 FOUND CORROSION ON FLOORBEAM 200. MAJOR REPAIR ACCOMPLISHED: REPLACED BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20080708 NM 2008 7 8 2008UALA02902 1 20080519 A 3350 58791 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 903UA 25003 EMERGENCY EXIT LIGHTS INOP ON FLOOR FROM ROW 15 TO AFT GALLEY. REPLACED RIBBON CABLE IN EEL TRACK & AFT GALLEY FLOOR LI GHT. 2 L 7 2 4F 4 F RT A16WE E21EU 20080708 NM 2008 7 8 2008UALA02905 1 20080520 A 2130 5639005 MODULE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 598UA 28751 CABIN PRESSURIZATION PROBLEM CAUSED DIVERSION. MAIN PWR SUPPLY T1 AND FLEX CABLE BAD. A1 CARD (CPU) FAILS LRU TEST 1407 60. REPLACED CABIN PRESSURIZATION MODULE., OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080708 NM 2008 7 8 2008UALA02912 1 20080520 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY EXIT LIGHT INOP AT ROW 44 RIGHT CEILING. RELAMPED EMERGENCY LIGHT, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 2008UALA02914 1 20080520 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 2J AFT LIGHT ASSY. REPLACED LIGHT ASSY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 2008UALA02915 1 20080520 A 3350 256005 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE OVERWING LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP, TWO MOST FWD LIGHT ASSY'S. FOUND OPEN FUSE. REPLACED FUSE OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 MWEA080075 1 20080521 A 5210 9935942502 STRUCTURE DOUG MD88 MD88 3023688 NM PAX DOOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 823ME 49766 FORWARD PASSENGER DOOR, AFT LOWER AREA HAS A DENT. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 20080708 WP 2008 7 8 MWEA080077 1 20080521 A 2460 ASH7341 INVERTER DOUG DC9 DC981 3022081 WP COCKPIT INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 814ME 48010 WHEN EMERGENCY POWER SWITCH TURNED ON, CAPTAIN'S PFD AND ND WENT BLANK AND REMAINED BLANK. REMOVED AND REPLACED NR 1 EF IS SYMBOL GENERATOR NO FIX. REMOVED AND REPLACED PFD NO FIX. REMOVED AND REPLACED EMERGENCY INVERTER OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 20080603 EU 2008 6 3 BA08019 1 20080510 A 2560 P2070001214 FLASHLIGHT AIRBUS 330 A330323 3930335 EU ZONE 200 INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 270AY 0315 CLT - THE CAPTAIN'S SIDE FLASHLIGHT, JUST FORWARD OF FLIGHT KIT STORAGE SPACE IS INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT. 2 L 7 2 4F RT A46NM 20080603 2008 6 3 DXTA200803077 4 20080522 A 2211 701730031444 WARNING SYSTEM CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007C 03047 GL COCKPIT ACTIVATED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 936QS 7500036 "FGC- B FAIL" CAS MESSAGE CAME ON 45 MIN INTO FLIGHT. DID NOT RESET. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080603 NM 2008 6 3 ERKR200800311 1 20080526 A 5330 SKIN BOEING 767 767231 1385131 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 606TW 22569 ECRA 606TW-53-767-001 REPAIR OF CORROSION DAMAGE AT STA 285 STR 36L: TRIMMED OUT CORROSION DAMAGED AREA AND PERFORMED A HFEC SKIN AND OPEN HOLE INSPECTION REPAIR FILLERS, DOUBLER AND TRIPLER PER THIS ENGINEERING CHANGE/REPAIR AUTHORIZATION ( ECRA ). APPROVAL SOURCE FAA FORM 8100-9, AR-635582-OB, DATED APRIL 28, 2008. 2 L 7 2 4F 4 F RT A1NM E3NE 20080603 NE 2008 6 3 HEEA119779 1 20080524 A 2170 85022051 BLOWER SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL A/C BAY MALFUNCTIONED B HEEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 03 911MJ 760231 IN CRUISE FLIGHT BOTH PILOTS NOTICED STRONG SMELL OF SOMETHING BURNING. BOTH FLIGHT NURSES SMELLED SMOKE. ONE SAID SHE SAW SMOKE COME FROM ABOVE HER HEAD. AIRCRAFT WAS TURNED TOWARD LAKE FRONT. LANDED IMMEDIATELY. AIRCRAFT HAD NO FAILU RES OR WARNING LIGHTS. MAINTENANCE REPLACED THE AIR CONDITIONING EVAPORATOR BLOWER MOTOR ASSY. 1 G 7 2 3U 3 U H1NE E1GL 20080603 EA 2008 6 3 SWIA200819635 1 20080128 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 988CA 7204 FS 280 FLOOR SUPPORT BETWEEN LBL 9 AND RBL 9 IS CORRODED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS IAW CRJ 200 SRM 57-42 -06 AND 51-40-11. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 S9BA2008021 1 20080527 A 7120 735125672 MOUNT DHAV DHC6 DHC6300 2802606 EA RT ENGINE FAILED A S9BA K NONE O OTHER TX TAXI/GRND HDL 1 SO 29 573SA 30 573 RT SPINNER NOTED MISALIGNED. REMOVED AND REPLACED TOP ENGINE MOUNT INSPECTED ALL RIGGING AND WIRING. EMERGENCY MEASURES EXECUTED, RETURNED TO DOCK. AIRCRAFT GROUNDED, RETURNED TO SERVICE NEXT DAY. FLIGHT NR 189 1 H 7 2 3T RT A9EA 20080603 EA 2008 6 3 SWIA200819666 1 20080319 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 FS 280 AT RBL 9 AND LBL 9 FLOOR SUPPORT ANGLE IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO601R 5 3-11-136. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819668 1 20080319 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 PAX DOOR EXTERNAL HANDLE IS CRACKED, FOUND AT C-CHECK. REPLACED PAX DOOR HANDLE IAW CRJ200 SRM 51-41-04, 51-42-06 AND 5 1-42-21. 2 L 7 2 4F RT A21EA 20080603 NM 2008 6 3 ASAA0842945 1 20080427 A 5753 SKIN BOEING 737 7374Q8 138447Q NM T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 782AS 25113 RIGHT WING TRAILING EDGE I/B AFT FLAP LOWER SURFACE IS DENTED AT WBL 82.25. PREPPED DAMAGED AREA, CUT TO FIT AND INSTAL LED PREPREG GLASS IAW B737 400 SRM 51 70 02 REPAIR 2. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 BB08088 1 20080511 A 2782 5006397R ROTARY ACTUATOR BOEING 757 7572S7 1384962 NM L/E SLAT OVERTORQUED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 906AW 20222 23568 PHX FLT 146 - PHX TO LIH. ON DEPARTURE FROM PHX, THE CREW RECEIVED A 'LE SLAT DISAGREE' EICAS MESSAGE WITH A LEADING E DGE LIGHT ILLUMINATED. THE FLAPS INDICATOR REMAINED BETWEEN FLAPS UP AND FLAPS ONE POSITIONS. THE FLIGHT RETURNED TO F IELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NUMBER 13 SLAT ROTARY ACTUATOR DUE TO AN OVERTORQUED INDICATION. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 20080603 NM 2008 6 3 UPS08552234 1 20080512 A 3350 POWER SUPPLY BOEING 757 75724APF 1384969 NM CABIN DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 471UP 28842 INSPECTION TYPE:N/A CREW EXIT LIGHTS DIM. REMOVED AND REPLACED EXIT LIGHT POWER SUPPLY PER MM 33-51-007-2. 2 L 7 2 4F RT A2NM 20080603 SO 2008 6 3 SWIA200819656 1 20080517 A 1100 PLACARD EMB 120 EMB120ER 3260203 SO EMERGENCY EXIT MISSING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 298SW 120328 FLT 3592 - EMERGENCY EXIT PLACARD MISSING FROM PAX DOOR AREA. REPLACED EMERGENCY EXIT SIGN. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080603 NM 2008 6 3 QXEA200800474 1 20080509 A 5320 SILL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 425QX 4039 PDX - C4 CHECK, FLANGE UNDER MAIN CABIN DOOR SILL IS CORRODED AROUND NUT PLATES. REMOVED NUTPLATES AND BLENDED DAMAGE. WITHIN LIMITS. HFEC AREA AND NO CRACKS FOUND. ALODINED AND PRIMED AREA. RE-INSTALLED NUT PLATES. 2 H 7 2 4T RT A13NM 20080603 WP 2008 6 3 UPS08852243 1 20080422 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 MAIN CABIN COURIER AREA STA 55 AND RBL 12 FLOORBOARD SKIN CORRODED. REPAIRED FLOORBOARD AT STA 55 AN D RBL 12 IAW SRM 53-02-03 FIG 10 AND DWG 5892154. 2 L 7 4 4F RT 4A25 20080603 NM 2008 6 3 QXEA200800523 1 20080526 A 2430 400SG163Q GENERATOR BOMBDR DHC8 DHC8402 1390042 NM NR 2 FAILED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 426QX 13235 838 4154 GTF - DURING ENGINE START NR 2 WAS SLOW TO START. AFTER STARTER CUT-OFF RPM, INDICATIONS FROM THE RAMP OF A NR 2 ENGINE FIRE. NO FIRE INDICATIONS IN THE COCKPIT. RAMP NOTICED JUST SMOKE. MAINTENANCE FOUND THE STARTER/GENERATOR NR 2 TO B E FAILED. REPLACED STARTER GENERATOR. OPERATIONAL CHECKS GOOD. NO EVIDENCE OF FIRE, BUT COWLING DOOR HAS SOME SMOKE D AMAGE TO PAINT. ALSO REPLACED GCU AS A PRECAUTION. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080603 NM 2008 6 3 QXEA200800469 1 20080509 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 425QX 4039 PDX - C4 CHECK, SEAT TRACK NR 1 IS CORRODED AT X170, X155, X132 AND X119. BLENDED AND POLISHED CORRODED AREAS. AMOUNT REMOVED WAS 0.013 INCH AND FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-884. HFEC FOUND NO CRACKS AND ALODINED AREA. 2 H 7 2 4T RT A13NM 20080702 NM 2008 7 2 SWAA083385 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083369 1 20080619 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 USA2008F00003 1 20080610 A 3350 20121 POWER SUPPLY BOEING 737 737401 1384701 NM CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 418US 23985 MAINTENANCE REPORTED THE AFT EMERGENCY LIGHTS REMAINING ON AT RIGHT HAND OVERHEAD AND EXTERIOR. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY IN AFT CEILING IAW MM 33-51-51. OPERATIONAL TEST GOOD AS LIGHTS ARE NOW EXTINGUISHED. (K) 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 USAA920081185 1 20080528 A 5330 6545766 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 REPETITIVE UPPER LAP SEAM INSPECTION. NR 4417266, CRACKED FUSELAGE SKIN, BS 520, S10R, REPAIRED FUSELAGE SKIN, BS 500D, S10R IAW EA120783. 2 L 7 2 4F RT A16WE 20080702 EU 2008 7 2 USAA920081197 1 20080609 A 5540 D5537131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 640AW 448 MAJOR REPAIR: C3 CHECK- NR 6105676, NR 5 RUDDER HINGE FITTING HAS EXCESSIVE PLAY. VERTICAL STABILIZER STATION 2985/ RIB 7. REPLACED NR 5 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 2985 / RIB 7 IAW AMM 55-36-41. (K) 2 L 7 2 4F RT A28NM 20080702 NM 2008 7 2 2008UALA03576 1 20080624 A 3350 GE209 BULB BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY SILL LIGHT ON L5 DOOR AFT INOP. FOUND BURNED OUT BULB. REPLACED BULB OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03561 1 20080623 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 MAIN CABIN FLOOR BEAM AT STA 1640, BL0 TO RBL 57, CORROSION ON TOP AND BOTTOM SIDES OF T-CAP. REMOVED DAMAGE FABRICATED T-CAP AND INSTALLED IAW SRM 53-00-98. 2 L 7 2 4F 4 F RT A2NM E17NE 20080702 NM 2008 7 2 2008UALA03547 1 20080622 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 OVERWING EMERGENCY LIGHT NOT WORKING. LOCATION: LEFT SIDE 2ND FROM TOP. FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT AS SEMBLY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03544 1 20080621 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHTS INOP, ALL D ZONE RT SEATS. FOUND FAULTY BATTERY PACK. REPLACED BATTERY PACK OP CHECKED GOOD. AC OK FO R SAERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03535 1 20080621 A 3350 78961 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHTS INOP, SEAT 5A AFT SECTION. FOUND FAULTY LIGHT ASSY. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK F OR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03533 1 20080621 A 3397 7956327 FEEDER CABLE BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 WALL EEL INOP:LWR WALL BETWEEN MID LAVS. FOUND LIGHT ASSEMBLY AND FEEDER CABLE DAMAGED. REPLACED LIGHT ASSEMBLY AND FEE DER CABLE OP CHECKED GOOD.AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03523 1 20080623 A 3350 362624 LAMP BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 29H EEL LIGHT INOP. SUSPECT FAULTY LAMP. REPLACED LAMP OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080702 NM 2008 7 2 CALA0800542 1 20080604 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 BODY STATION 907 LEFT CRACKED AT AIR GRILL MOUNT. INSTALLED REPAIR ANGLES AND COLD WORKED 6EA HOLES PER EA 5310-04498 O P 02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800619 1 20080620 A 5320 6547690 ANGLE BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 AFT CARGO STATION 767 TO 787 RIGHT TRANSITION ANGLE TOP AND BOTTOM SURFACES ARE CORRODED. REMOVED CORRODED TRANSITION A NGLE FROM AFT CARGO STATION 767 TO 787 AND INSTALLED NEW TRANSITION ANGLE IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800558 1 20080601 A 5743 115A5211 BUSHING BOEING 737 737724 13844BY NM RT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 RIGHT MAIN LANDING GEAR FWD TRUNNION SUPPORT (OUTBOARD LOWER BUSHING FACE) HAS CORROSION. COMPLETED ECRA 5741-01106 REV D. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800571 1 20080606 A 5330 65C35772 SKIN BOEING 737 737524 1384721 NM FUSELAGE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 UPPER FUSELAGE SKIN IS WORN AT STATION 864-882 LBL-1 TO LBL-4 FROM DORSAL FIN SEAL. BLENDED OUT AREA AND INSTALLED DOUB LER, TRIPLER AND WEAR STRIPS REFINISHED AREA PER SRM 53-60-01 REPAIR 10, PROCEDURE III. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800578 1 20080608 A 5330 65C3579237 SKIN BOEING 737 737524 1384721 NM FUSELAGE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59630 27534 UPPER FUSELAGE SKIN IS WORN AT STATION 875 - 880 CAUSED FROM DORSAL FIN SEAL CHAFING. INSTALLED PERMANENT REPAIR PER EC RA 5331-01408 REV B. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800581 1 20080531 A 5315 65C33947 FLOORBEAM BOEING 737 737524 1384721 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 MAIN CABIN FLOORBEAM GOUGED AT STATION 927 AT B-0. REPAIRED DAMAGED FLOORBEAM FORWARD FLANGE AT BODY STATION 927 AT BL 0 PER B737-500 SRM 53-60-51, REPAIR 3. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800548 1 20080530 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 BODY STATION 400 LEFT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8L AND S-9L. REPAIRED CRACKED FRAME AT STATION 400 AT A/C BRACKET BETWEEN S-8L AND S-9L PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800549 1 20080530 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 BODY STATION 440 RIGHT-HAND SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED CRACKED FRAME AT STATION 440 AT A/C BRACKET BETWEEN S-8R AND S-9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800540 1 20080604 A 5230 65C36231 SKIN BOEING 737 737524 1384721 NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 NUMBER 2 CARGO DOOR EXTERIOR SKIN DENTED 12 INCHES FROM AFT EDGE AND 15 INCHES FROM THE TOP. CUT OUT DENT, FABRICATED A ND INSTALLED REPAIR DOUBLER PER SRM 52-00-01 FIGURE 201 REPAIR 3. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083368 1 20080618 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 420, STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082809 1 20080524 A 5343 6546543 FITTING BOEING 737 7373H4 1384600 NM RT MLG W/W CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED MV2 CHECK, FOUND RT MLG SIDE SUPPORT FITTING LUG CORRODED AT BS 685. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082812 1 20080523 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED HC2 CHECK, FOUND AFT SERVICE DOOR LOWER HINGE CUTOUT CRACKED AT LOWER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082822 1 20080523 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082857 1 20080524 A 2530 41600019 COFFEEMAKER BOEING 737 7377H4 1384404 NM CABIN FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 29 438WN 29833 DECLARED EMERGENCY - FLIGHT CREW REPORTED BURNING SMELL AT FL 190. INSPECTED AIRCRAFT FOUND FWD COFFEEMAKER HOT AFTER B EING SHUTDOWN OVER HALF AN HOUR. REMOVED AND REPLACED COFFEEMAKER PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082863 1 20080527 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 491WN 33867 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 CALA0800513 1 20080601 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 STATION 400 BETWEEN S8R & S9R IS CRACKED. REPAIRED CRACK AT STATION 400 BETWEEN S8R AND S9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080707 NM 2008 7 7 NOCA03608 1 20080511 A 3350 1317 LIGHT BOEING 767 76736N 1385152 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 768NA 29898 EMERGENCY PATH LIGHT AT 8B AND 16G INOP. RELAMPED PER MM 33-51-10. 2 L 7 2 4F RT A1NM 20080707 EA 2008 7 7 COMA0860236 1 20080501 A 5230 ROLLER CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR OUT OF POSITION A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 938CA 7046 FLIGHT 5247- ON CLIMB-OUT FROM JAN TO CVG A/C FAILED TO PRESSURIZE. EMERGENCY DECLARED, A/C RETURNED TO JAN AND LANDED SAFELY. INSPECTED A/C AND FOUND FWD TOP ROLLER ON CARGO DOOR OUT OF TRACK. REINSTALLED ROLLER IN TRACK. OPS CHECK GOO D. 2 L 7 2 4F RT A21EA 20080707 NM 2008 7 7 2008UALA02781 1 20080514 A 2197 W09001824 WIRE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN SHORTED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 935UA 44698 26663 BURNING ODOR NOTED THROUGHOUT THE ACFT. ODOR DISSIPATED WHEN RECIC FAN WAS TURNED OFF. AFTER EXTENSIVE TROUBLE SHOOTIN G AND PART REPLACEMENT REPAIRED WIRE W090-018-24 REF WD21-61-01 BETWEEN CABIN TEMP CONTROLLER AND CABIN TEMP SELECTOR. F OUND WIRE SHORTED TO GROUND. REF GNMM 2-0-15-1. LEFT PACK AUTO TEMP CONTROL OPS CHECKS NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 20080707 NM 2008 7 7 2008UALA02783 1 20080514 A 3350 60B4005715 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY EXIT LIGHT INOP, AT DOOR 4 LEFT SLIDE LIGHT. SUSPECT LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY. OPS CHECKS NO RMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 NOCA03908 1 20080519 A 5420 4057546 FITTING BOEING 767 76739H 1385311 NM LT FAN COWL CRACKED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 760NA 26257 FAN COWL SUPPORT BEAM FITTING ASSY IS CRACKED IN TWO PLACES LT SIDE. REPLACED COWL SUPPORT BEAM FITTING AND SHIMMED AS PER SRM 51-10-02. 2 L 7 2 4F RT A1NM 20080707 SO 2008 7 7 C2XA08RI075 1 20080516 A 3320 BR90002 BALLAST EMB 145 EMB145EP 3260221 SO CABIN DEFECTIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 14945 145049 FLIGHT 2404 - EWR - FLIGHT CREW REPORTED SIDE LIGHTS AT 2A AND 3A INOPERATIVE WITH BURNING SMELL COMING FROM BALLAST. E WR MX REMOVED AND REPLACED BALLAST IAW WMB 145 AMM 33-21-03 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20080707 NM 2008 7 7 ARWA20080502 1 20080517 A 7722 8DJ260WAF1 INDICATOR DOUG DC10 DC1040F 3023507 NM NR 2 FAULTY A ARWA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 29 140WE 46920 IN FLIGHT NR 2 ENGINE EGT INDICATOR FLUCTUATING 20 TO 30 DEGREES BOTH POINTER AND COUNTER ALL OTHER PARAMETERS NORMAL. REMOVED AND REPLACED NR 2 EGT INDICATOR CHECK GOOD IN ACCORDANCE WITH M/M 77-21-00 AND M/M 71-00-00. 2 L 7 3 4F RT A22WE 20080707 NM 2008 7 7 UPS08552303 1 20080520 A 3350 GUARD BOEING 757 75724APF 1384969 NM COCKPIT BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 445UP 27390 INSPECTION TYPE:N/A EMERGENCY LIGHT SWITCH GUARD BROKEN. REMOVED AND REPLACED SWITCH GUARD. TESTED LIGHT ADJ/TEST PER 33-51-0804. CHECKS OK. IPC REF 33-51-08. 2 L 7 2 4F RT A2NM 20080707 NM 2008 7 7 2008UALA02842 1 20080516 A 2760 B435428 PCU BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE SPOILER SYSTEM MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 221UA 30552 EICAS ADV MSG DISPLAYED SPOILERS INTERMITTENTLY, MSG 27-11503 FIM TASK 27-61 TASK 821. SUSPECT FAULTY POWER CONTROL UNI T. REPLACED NR 4 SPOILER PCU PER MM 27-61-09. OPS CHECK NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080707 NM 2008 7 7 2008UALA02843 1 20080517 A 2740 STABILIZER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 210UA 30216 "STAB AUTO SHUTDOWN" STATUS MSG IS DISPLAYED ON EICAS. STAB SYSTEM GND TEST FAILS. EXISTING FAULTS MAINT MSG 27-10007, 27-10010. UNABLE TO CONTROL STAB TRIM USING RIGHT STAB TRIM CUTOUT SWITCH, STAB CONTINUES TO MOVE WITH SWITCH IN CUTOU T. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008041700005 20080417 00005 NM 2008 4 17 2008UALA02098 1 20080410 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 284 S4L GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 UPPER FUSELAGE CROWN SKIN GOUGED AT BS 284 STR 4L. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR DOUBLER/TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700008 20080417 00008 EU 2008 4 17 F3LA200800163 1 20080411 A 5321 261CG FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE CABIN DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 7217 1876 DURING C4 S1 C CHECK INSPECTION REPORTED FLOOR PANEL 261CG HAD DELAMINATION FROM ONE SCREW HOLE. MAINTENANCE REPAIRED F LOOR PANEL 261CG IN ACCORDANCE WITH SRM 53-08-00 STEP 8J, SRM 51-77-11 PARAGRAPH A11 AND SRM 51-44-21 PARAGRAPH 3A. UPO N COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008041700022 20080417 00022 NM 2008 4 17 2008UALA02110 1 20080410 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD ENTRY DOOR FUSELAGE CUTOUT BS 294.5 L-ANGLE CRACKED AT AFT END BELOW THE RADIUS AT S10L. MAJOR REPAIR ACCOMPLISHED: REPLACED I-B 'H' STRAP, AUX INTERCOSTAL ANGLE, INTERCOSTAL WEB & CLIPS & INSTALLED FRAME WEB REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E2GL 20080711 NM 2008 7 11 MWEA080078 1 20080520 A 5311 3956151505 FRAME BOEING 717 717200 1383700 NM FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 918ME 55180 LIGHT CORROSION EVIDENT AT LOWER FLANGE OF FUSELAGE FRAME STATION AT 908, AT ATTACH POINT WITH LONGERON 30 RIGHT. FLANG E IN AFT CARGO COMPARTMENT. REMOVED DAMAGE SECTION OF FLANGE, FABRICATED AND INSTALLED FLANGE. 2 L 7 2 4F TR A6WE 20080711 EA 2008 7 11 MASA200800415 1 20080523 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR MALFUNCTIONED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 513MJ 10111 ASH FLT 7277 PWM-IAD - MAIN PAX DOOR CAUTION. MX INSPECTED AND OPERATED DOOR ASSY WITH NO DEFECTS NOTED. WARNING OPS G OOD. 2 L 7 2 4F RT A21EA 20080711 NM 2008 7 11 ASAA0843092 1 20080507 A 5311 90526913 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 LT SIDE FRAME AT STA 727F CRACK AT PSU RAIL BRACKET. FRAME REPAIRED IAW ASA EA5310 02797. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 USAA920081109 1 20080523 A 2560 BRACKET BOEING 737 7373B7 1384580 NM FLASHLIGHT BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 23380 FLT 1575 - DCA - EMERGENCY FLASHLIGHT FWD GALLEY HAS BROKEN BASE/BRACKET. REPLACED EMERGENCY FLASHLIGHT AT FORWARD GALL EY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 ASAA0843093 1 20080507 A 5311 90526911 FRAME BOEING 737 7374Q8 138447Q NM BS 787 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 LT FRAME AT STA 787 CRACKED AT PSU RAIL BRACKET. FRAME REPAIRED IAW ASA EA5310 02797. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083413 1 20080622 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083485 1 20080623 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083444 1 20080622 A 5311 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 433, RBL 3. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083455 1 20080623 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083454 1 20080623 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083461 1 20080623 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 403WN 29815 DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 133. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083464 1 20080623 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083463 1 20080623 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 DURING SCHEDULED HC2 CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 2008 7 14 SWAA083462 4 20080623 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083427 1 20080620 A 2560 6557463 FITTING BOEING 737 7375H4 138449D NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED GIRT BAR FITTING PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083428 1 20080621 A 3350 PH22300L LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 EEPLS STRIP LOOSE AT ROW 7 DEF. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083429 1 20080622 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500C, LBL 18 TO RBL 19. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083430 1 20080621 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 6 ABC. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083431 1 20080620 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083473 1 20080623 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083472 1 20080623 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083486 1 20080623 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083438 1 20080620 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 133. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083355 1 20080618 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 15L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083357 1 20080618 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 13R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083173 1 20080610 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083186 1 20080610 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 847, RBL 17. REPAIRED SHEAR TIE PER ACO. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083187 1 20080610 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 460, BL 0. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 DLM88080798 1 20080530 A 5523 TAB DOUG MD88 MD88 3023688 NM ELEVATOR DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 963DL 49982 DURING HMV3 DELAMINATION WAS FOUND ON LOWER SURFACE OF LT ELEVATOR GEARED TAB. DELAMINATION WAS REPAIRED IAW DRD 55-04D PARA 3A FIG 2. 2 L 7 2 4F RT A6WE 20080714 NM 2008 7 14 DLM88080800 1 20080530 A 5523 TAB DOUG MD88 MD88 3023688 NM LT ELEVATOR DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 963DL 49982 DURING HMV3 DENTS WERE FOUND ON UPPER SURFACE OF LT ELEVATOR GEARED TAB. DENTS WERE REPAIRED IAW DRD 55-04D PARA 2A 2 F IG1 AND PARA 3A FIG 2. 2 L 7 2 4F RT A6WE 20080714 NM 2008 7 14 DLM88080803 1 20080531 A 2910 HYDRAULIC SYSTEM DOUG MD88 MD88 3023688 NM LEFT MALFUNCTIONED A DALA O OTHER J WARNING INDICATION LD LANDING 1 SO 27 950DL 15087 49881 ON DESCENT 27000 FT, THE LEFT HYD PRESS LOW ANNUC CAME ON, DROPPED TO ZERO PSI AND QUANT INCREASED LEFT REV WOULD NOT S TOW AFTER LANDING. FOUND LT SYSTEM RESERVOIR ACCUMMULATOR FULL OF AIR BLED AIR FROM RESERVOIR. OPS CHK GOOD QTY, NO LE AKS NOTED. CYCLED FLT CONTROLS PRESS NORMAL. NO LEAKS NOTED PRESS NML. NO HISTORY. 2 L 7 2 4F RT A6WE 20080714 NM 2008 7 14 DL757080805 1 20080531 A 5313 STRINGER BOEING 757 757232 1384965 NM BS 1710 S24L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 AFT OF AFT CARGO BAY CORROSION AT STR 24L STA 1710/SPLICED STR HAT SECTION FROM STA 1690 TO 1720 PER SRM 53-00-03 FIG 20 1 AND 51-20-01 ON SAA N/R 78980240001. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 DL757080807 1 20080531 A 5313 STRINGER BOEING 757 757232 1384965 NM BS 1710 S27L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 STA 1710 STR 27L HAS EXFOLIATING CORROSION AFT CARGO BAY. REPLACED STR SECTION PER SRM 53-00-03 FIG 201 REF NR 78981650 001. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 DL757080808 1 20080530 A 5330 SKIN BOEING 757 757232 1384965 NM BS 192 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 DENT ON STR BETWEEN STR 28R AND 29R AT STA 192. REPAIRED DENT PER SRM 53-00-01 REF SAA N/R 78986200001. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 DL764080816 1 20080531 A 3150 WARNING MESSAGE BOEING 767 767432ER 1385134 NM COCKPIT ILLUMINATED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 843MH 29716 L AIR DATA CAUTION MSG ON TAXI OUT FWD TO MCO/PLAC PER MEL 34-26-01A. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 DL76L080824 1 20080521 A 5315 143T51143 FLOORBEAM BOEING 767 767332 1382001 NM BS 720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 193DN 51895 28450 DURING B ZONE MOD, FOUND CORROSION ON FLOORBEAM AT BS 720 LBL 26 UPPER CHORD REMOVED CORROSION ON FLOORBEAM, FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-51 FIG 201 DWG NR 06T083N032 DDN NR 55. INSTALLED IAW SRM 53-00-21, 51-40-02 DW G NR 06T083N032 DDN NR 35. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 DL76L080825 1 20080516 A 5315 143T51143 FLOORBEAM BOEING 767 767332 1382001 NM BS 720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 193DN 51895 28450 CORROSION ON FLOORBEAM BS 720 RBL 26 UPPER CHORD. REPAIRED FLOORBEAM PER SRM 53-00-01 FIG 201. 2 L 7 2 4F RT A1NM 20080711 NM 2008 7 11 AALA200801130 1 20080428 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801142 1 20080428 A 3350 COVER BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR GALLEY COMPARTMENT STORAGE AREA WIRING EXPOSED. REPLACED COVER FOR EMERG ENCY LIGHT AT RIGHT NUMBER ONE DOOR GALLEY COMPARTMENT STORAGE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801133 1 20080428 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT SEAT 35G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 35G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801140 1 20080428 A 3350 HOUSING BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET AREA DAMAGED. REPLACED HOUSING FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801221 1 20080506 A 3397 CONNECTOR BOEING 767 767323 1385205 NM CABIN NOT SEATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 351AA 24032 DFW - EMERGENCY LIGHT AT SEATS 10H AND 11H INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHTS AT SEATS 10H AND 11H. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080711 NM 2008 7 11 AALA200801211 1 20080505 A 3350 LIGHT BOEING 777 777223 1385213 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR IN OPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LEF T NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801248 1 20080507 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 21C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801230 1 20080506 A 3350 LENS BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 935AN 30081 DFW - EMERGENCY LIGHT AT SEAT ROW 25 HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 25. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 HNAA0800169 1 20080515 A 8097 HA11981 CABLE DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE BURNED A HNAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 942HA 163 NR 2 ENG WOULD NOT START, NO ROTATION. MT INSPECTED AND FOUND LEAD CABLE FROM GEN TO BULKHEAD BURNED. REMOVED AND REPL ACED LEAD CABLE, GROUND RAN AC AND OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 20080708 NM 2008 7 8 BB08091 1 20080520 A 2560 P4010021 BATTERY BOEING 767 7672B7 1385107 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 251AY 24764 PHL - THE RED LIGHT DOES NOT BLINK ON THE LEFT, AFT FLASHLIGHT. MAINTENANCE REPLACED THE BATTERY IN THE LEFT, AFT FLASH LIGHT. 2 L 7 2 4F RT A1NM 20080708 NM 2008 7 8 2008UALA02886 1 20080516 A 2560 GIRT BAR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L5 DOOR FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 122UA 29168 DOOR 5L HARD TO ARM AND DISARM. FOUND FLOOR FITTING LOOSE. SECURED FITTING DOOR OPERATES GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 2008UALA02776 1 20080514 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 MAIN CABIN FLOORBEAM CORRODED STA 324, RBL 40 TO RBL 54. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW MM 53-00-98 RPR XXV FIG 824. 2 L 7 2 4F 4 F RT A2NM E17NE 20080708 NM 2008 7 8 MWEA080074 1 20080521 A 5210 5910081155 STRUCTURE DOUG MD88 MD88 3023688 NM PAX DOOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 823ME 49766 FORWARD PASSENGER DOOR, FORWARD LOWER AREA HAS A DENT. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 20080708 SO 2008 7 8 RAIA00805015 1 20080514 A 3244 TIRE EMB 145 EMB145LR 3260212 SO NLG LOW A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 815HK 145048 FLT 5488 - IAD - NOSE STEERING UNCONTROLLABLE. ABORTED TAKEOFF. STEERING WAS PULLING LEFT. MAINTENANCE SERVICED THE N OSE LANDING GEAR TIRES AND CLEANED THE FEEDBACK UNIT CONNECTORS. OPERATIONAL CHECK OF THE SYSTEM PROVED GOOD. 2 L 7 2 4T RT T00011AT 20080708 NM 2008 7 8 AALA200801113 1 20080427 A 1100 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 611AM 24487 DFW - EMERGENCY EXIT MARKER DECAL AT LEFT NUMBER TWO DOOR DAMAGED. REPLACED DECAL FOR EMERGENCY EXIT MARKER AT LEFT NUM BER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080708 NE 2008 7 8 REXA200800014 2 20080522 A 7200 ENGINE CNDAIR CL600 CL6002D24 1390016 EA GE CF34 CF348C5 30050 NE CONTAMINATED A REXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 153PQ 15153 194640 DURING CLIMB-OUT FROM KMEM, THE COCKPIT AND CABIN FILLED WITH SMOKE. THE FLIGHT CREW DONNED O2 MASKS, COMPLIED WITH THE QRH AND DECLARED AN EMERGENCY WITH ATC. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE. THE AIRCRAFT WAS STOPPED O N THE TAXIWAY AND CFR INSPECTED THE AIRCRAFT. THE PASSENGERS WERE REMOVED AND TRANSPORTED TO THE TERMINAL ON BUSES. MA INTENANCE DETERMINED THAT THE CAUSE OF THE SMOKE WAS RESIDUAL FLUID FROM THE PREVIOUS NIGHT'S COMPRESSOR WASH. THE AIRC RAFT WAS RUN UP TO TOGA POWER WITH THE BLEEDS ON. NO FURTHER SMOKE, FUMES OR VAPORS WERE DETECTED. THE AIRCRAFT WAS RE LEASED FOR SERVICE. PINNACLE AIRLINES IS REVIEWING THE COMPRESSOR WASH PROCEDURE TO DETERMINE IF THE PROCESS SHOULD BE 2 L 7 2 4F 4 F RT A21EA E00063EN 20080708 NM 2008 7 8 DHL2008764500 1 20080519 A 5753 SKIN BOEING 727 727264 138408M NM T/E FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C CHECK REF N/R 097599, RT I/B AFT FLAP LOWER SKIN WBL 203 CRACKED AT MOUNTING FITTING. REPAIRED IAW B727 SRM 57-50-4 FIG 11, SPLICE 2024T3 .050 DIM 5.5 INCH BY 11 INCH PO NR 9006742. FABBED FILLER 2024T3 .040 DIM 9 INCH BY 14 IN CH PO NR 9006587. 2 L 7 3 4F A3WE 20080603 EA 2008 6 3 S9BA20080019 1 20080519 A 5413 C6W1512S142 LONGERON DHAV DHC6 DHC6300 2802606 EA RT NACELLE CRACKED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 573 RT ENGINE, OB NACELLE LONGERON CRACKED. REPLACED WITH FACTORY NEW PART IAW AC43.13-1B SECTION 4 PARA 4-57 FIG 4-6 AND 4- 9. (PN C6W1512-S142) NO EMERGENCY MEASURES EXECUTED , AIRCRAFT GROUNDED. 1 H 7 2 3T RT A9EA 20080603 EA 2008 6 3 MALA080082 1 20080424 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 833AY 8033 2 EXTERNAL EMERGENCY LIGHTS FOUND INOPERATIVE DURING LINE CHECK. REMOVED AND REPLACED BATTERY, IAW TASKCARD 33-900-701. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819670 1 20080228 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910SW 7566 FS 280 FLOORBEAM AT LBL 9 AND RBL 9 IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO601R-53-11-136 REV A DA TED NOV 01-07. 2 L 7 2 4F RT A21EA 20080603 CE 2008 6 3 DXTA200803081 1 20080527 A 2842 WARNING SYSTEM CESSNA 560 560XL 2076702 CE PWA 545 PW545A NE COCKPIT ACTIVATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 627QS 5605227 BOTH L/R FUEL GAUGE ANNUNCIATORS ILLUMINATED ON TAKEOFF. TAKEOFF WAS ABORTED. FUEL QTY GAUGES BOTH READ ZERO. GAINED ACCESS TO LT/RT WING ROOT ELECTRICAL CONNECTORS FOR MOISTURE NONE FOUND. INSPECTED FUEL SIGNAL CONDITIONER FOR FAULT BI TES NONE FOUND. 2 L 7 2 4F 4 F RT A22CE E00059EN 20080603 EA 2008 6 3 SWIA200819676 1 20080228 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910SW 7566 LEFT ENGINE THRUST FITTING IS CORRODED, FOUND AT C-CHECK. REPLACED THRUST FITTING PER CRJ200 AMM TASK 21-22-01-400-801. 2 L 7 2 4F RT A21EA 20080603 2008 6 3 SWIA200819677 4 20080521 A 3417 8220372445 ADC CNDAIR CL600 CL6002B19 1900309 EA NR 2 MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 441SW 10561 10561 7602 FLT 3936 - AIRSPEED INDICATION SLOWLY DECREASED ALONG WITH ASSOCIATED MESSAGES. PURGED MOISTURE FROM NR 2 PITOT SYSTEM AND REPLACED THE NR 2 ADC PER AMM 34-13-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080603 CE 2008 6 3 DXTA200803045 1 20080505 A 2131 52770116 CONTROLLER CESSNA 500 560CESSNA 2076750 CE PWA 530 PW535A NE CABIN PRESSURE FAILED E DXTA G B O2 MASK DEPLOYED EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 07 825QS 2063 5600655 AT FL300 THE CABIN RATE STARTED CLIMBING ABNORMALLY TILL IT REACHED 6000 FT IAW MINT THE 10,000 FT CABIN ENUNCIATORS ILL UMINATED AND THE EMER PRESS CAME ON. OXYGEN MASKS DROPPED IN THE CABIN. DECLARED AN EMERGENCY AND STARTED AN EMERGENCY DESCENT TO 10,000. REPLACED FAILED CABIN ALT. CONTROLLER, INSTALLED A SERVICEABLE UNIT, OPS CK GOOD IAW MM CH 21-31-0 0. 2 L 7 2 4F 4 F RT A22CE E00053EN 20080711 NM 2008 7 11 AALA200801153 1 20080430 A 3350 BEZEL BOEING 767 767323 1385205 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 39364 24045 MIA - EMERGENCY AISLE LIGHT AT SEAT 40C MISSING LENS BEZEL. REPLACED LENS BEZEL FOR EMERGENCY AISLE LIGHT AT SEAT 40C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080711 NM 2008 7 11 AALA200801187 1 20080503 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 648AA 24606 DFW - EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 AALA200801245 1 20080507 A 3350 OL3071BPEGPL LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 23C MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801233 1 20080506 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 DFW - EMERGENCY LIGHT AT SEAT 26G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 ZZDA2008108 1 20080518 A 3350 8039251 POWER SUPPLY BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 928AT 55076 FIRST CLASS EMERGENCY LIGHT PATH LIGHTING INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY. 2 L 7 2 4F TR A6WE 20080711 NM 2008 7 11 DHL2008760002 1 20080522 A 5312 ANGLE BOEING 727 7272B7 138407L NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 760AT 21954 LWR FUSELAGE AFT BULKHEAD IN FWD CARGO PIT AT STA 740 RBL 10-20 LOWER CHORD ANGLE IN BILGE AREA HAS CORROSION. REMOVED AND FAB NEW ANGLE SKIN SUPPORT MATERIAL USED 7075-0 .190" PO 7220256 DIM 10.25" X 11.75" IAW B727 DWG 69-64841 IAW EC-00 958-001. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 DHL2008764528 1 20080527 A 5314 KEELBEAM BOEING 727 727264 138408M NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C-CHECK, CRACK AT BS 874 RIGHT KEEL BEAM LWR CHORD IN APU BAY. REPAIRED IAW S/B 727 53-02-08 MATERIAL 4130 STE EL .071" PO 610176. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 USAA920081110 1 20080523 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 308AW 24710 FLT 137 - PHX - FWD CABIN FLASHLIGHT INOP. MX REPLACED THE FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 20080714 EU 2008 7 14 UPS08152350 1 20080524 A 5610 BELLCRANK AIRBUS 300 A300B4622R 3930312 EU COCKIPT WINDOW LACK OF LUBE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 163UP 0805 INSPECTION TYPE:N/A CAPTAIN'S WINDOW HANDLE RED TAB WILL NOT RETRACT INTO HANDLE COMPLETELY. LUBRICATED BELLCRANK PIVOT PIN IN CAPTAIN'S SLIDING WINDOW HANDLE. OPS CHECK GOOD. REF MM 56-12-00-04. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 UPS08552343 1 20080509 A 5320 STRUCTURE BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 410UP 23732 INSPECTION TYPE:C1 TAIL COMPARTMENT APU CUTOUT, FWD SIDE OF BS 1825 CHORD HAS CORROSION AROUND AREAS OF NUT PLATES 7 INC HES O/B OF STR 3R. REMOVED, FABRICATED AND INSTALLED STRAP. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 UPS08652342 1 20080524 A 5720 14T2300271 WEB BOEING 767 76734AF 1385212 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 302UP 27240 INSPECTION TYPE:N/A LEFT WING LES 694 FWD D-NOSE FAIRING SUPPORT WEB LOWER AREA FOUND CRACKED. CRACK LENGTH 2.5 INCHES APPROX. LEFT WING FWD D-NOSE FAIRING SUPPORT WEB REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02, JUST BETWEEN OSS648 AND 694 AREA. 2 L 7 2 4F RT A1NM 20080714 2008 7 14 DHLA200800049 4 20080524 A 3414 WARNING SYSTEM BOEING 727 727227 1384078 NM COCKPIT MALFUNCTIONED A DHLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 05 784DH 22001 FLT NR 589 MACH AIRSPEED WARNING ACTIVATED AT 70 KNT. PUMPED UP MACH AIRSPEED SYSTEM PER MM 34-14-00, SYSTEM OP'S CK NO RMAL. NO DEFECTS NOTED AND 34-11-00 PITOT TEST. AIRCRAFT WAS GROUNDED. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 SWAA083419 1 20080622 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083421 1 20080622 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083426 1 20080622 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 449WN 32469 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083469 1 20080623 A 5753 6546435335 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW 28331 DURING SCHEDULED MV1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20080603 CE 2008 6 3 GUUA05230802 1 20080523 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CABIN & COCKPIT ODOR A GUUA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 81536 UE152 FLIGHT: 9184, DURING FLIGHT, CABIN AND COCKPIT SMELLS OF FUEL ON THE GROUND AND IN FLIGHT, SMELL OF FUEL OUT OF VENTS AS WELL. INSPECTED FOR FUEL AROUND ACM AND INLET NO FUEL NOTED ALSO INSPECTED VENT BLOWERS AND AIR VENTS NO FUEL NOTED. 2 L 7 2 4T 4 T RT A24CE E26NE 20080603 EA 2008 6 3 MALA080107 1 20080424 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 833AY 8033 2 EXTERNAL EMERGENCY LIGHTS FOUND INOPERATIVE DURING LINE CHECK. EMERGENCY BATTERY PACK DEAD. REMOVED AND REPLACED BAT TERY, PS4LF, PS4LF P/N ON: 2013-1A, P/N OFF: 2013-BR, S/N ON: 101367, S/N OFF: B0298 IAW CRJ200 TASKCARD 33-900-701. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819646 1 20080319 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 952SW 7805 LBL9 AT FS 280 LOWER FLOOR SUPPORT IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 20080603 NE 2008 6 3 UPS08852235 2 20080513 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE NR 4 FLAMED OUT A IPXA O OTHER X ENGINE FLAMEOUT CL CLIMB 1 SO 01 805UP 46117 INSPECTION TYPE:N/A CLIMBING THROUGH FL360 THE NR 4 ENGINE FLAMED OUT. DESCENDED TO FL220 AFTER ACCOMPLISHING THE IN FL IGHT ENGINE FLAMEOUT CHECKLIST TO ATTEMPT A RESTART. FOLLOWED THE IN FLIGHT ENGINE START CHECKLIST AND ATTEMPTED 1 REST ART. AFTER DRY MOTORING ENG FOR SEVERAL MINS OPS CHECK OF IGNITION SYS COMPLETED WITH NO FAULTS NOTED. ENG WAS RUN SEV ERAL TIMES USING A AND B IGNITION SEPARATELY WITH NO FAULTS NOTED. AFTER FURTHER REVIEW OF EVENT REPORT 18355, IT WAS N OTED THE NR 4 BOOST PUMP WAS OFF. UNABLE TO DUPLICATE. 2 L 7 4 4F 4 F RT 4A25 E2GL 20080603 EA 2008 6 3 REXA200800017 1 20080527 A 7500 34H80150 COUPLING CNDAIR CL600 CL6002B19 1900309 EA BLEED VALVE LEAKING A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 8458A 7458 ON CLIMB-OUT AFTER TAKEOFF FROM KMSP, THE "R 14TH DUCT" WARNING MESSAGE ILLUMINATED FOLLOWED BY THE "BLEED AIR DUCT" AUR AL WARNING. THE FLIGHT CREW RAN THE QRH, DECLARED AN EMERGENCY AND RETURNED TO KMSP. RIGHT ENGINE POWER WAS REDUCED TO IDLE AND AN OTHERWISE NORMAL APPROACH AND LANDING WERE COMPLETED. CFR FOUND NO DAMAGE TO THE ENGINE AND THE AIRCRAFT WA S RELEASED TO THE GATE. MAINTENANCE FOUND THE AFT COUPLING OF THE 14TH STAGE BLEED VALVE TO BE LEAKING. THE COUPLING AN D THE PYLON SENSING LOOP WERE REPLACED. MAINTENANCE ALSO COMPLIED WITH AN OVERWEIGHT LANDING INSPECTION ON THE AIRCRAFT . 2 L 7 2 4F RT A21EA 20080603 NM 2008 6 3 QXEA200800536 1 20080601 A 5240 DOOR BOMBDR DHC8 DHC8402 1390042 NM MAIN PAX STUCK A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 400QX 4030 SEA - FLIGHT 2429 - AFT PASSENGER DOOR FOUND TO BE STUCK. MAINTENANCE CLEANED AND LUBED DOOR MECHANISMS. OPERATIONAL C HECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080603 NM 2008 6 3 USAA920081072 1 20080429 A 5320 143N51292 STIFFENER BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - CRACKED VERTICAL STIFFENER ANGLE, BS 700, RBL 24.75. REPLACED VERTICAL STIFFENER ANGLE , BS 700, RBL 24.75 IAW USAIRWAYS EA 130014. 2 L 7 2 4F RT A2NM 20080603 NM 2008 6 3 QXEA200800517 1 20080526 A 3230 860TS09Y00 CONTROL PANEL BOMBDR DHC8 DHC8402 1390042 NM MLG MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 425QX 1291 4039 GTF - FERRY FLIGHT 9800 - AFTER TAKEOFF FOR FERRY FLIGHT GEAR DID NOT RETRACT. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. MAINTENANCE REPLACED THE LANDING GEAR CONTROL PANEL AND THE PSCU (PN 30145-0301, SN 0172). AIRCRA FT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080603 NM 2008 6 3 USAA920081075 1 20080419 A 5320 141N516078 FLOOR SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 902AW 23322 MCN - MAJOR REPAIR - C12 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 348 - BS 358, RBL 55. REPLACED CABIN FLO OR SUPPORT, BS 348 - BS 358, RBL 55 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 20080603 NM 2008 6 3 P5CA0801563 1 20080522 A 2910 0690001981 GASKET BOEING 747 74746NF 13848BT NM HYD SYSTEM LEAKING A P5CA O OTHER K FLUID LOSS CL CLIMB 1 EA 15 452PA 30810 ON CLIMB-OUT OF NRT, NR 3 HYDRAULIC SYSTEM WAS LOST. QUANTITY AND PRESSURE DROPPED TO ZERO. FOUND UPPER RUDDER ACTUATO R LEAKING FROM MATING SURFACE OF PROPORTIONAL VALVE AND ACTUATOR. REPLACED GASKET PLATE. NO LEAKS NOTED. 2 L 7 4 4F RT A20WE 20080701 EA 2008 7 1 SWIA200819713 1 20080404 A 2620 TUBE CNDAIR CL600 CL6002B19 1900309 EA EXTINGUISHER DEFORMED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 433SW BAGGAGE FIRE EXTINGUISHER TUBE IS KINKED. (FOUND AT C-CHECK) REPLACED KINKED DISCHARGER TUBE PER CRJ200 AMM 26-25-07-40 0-801. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819723 1 20080604 A 5210 SPRING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STIFF A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 464SW PAX DOOR IS HARD TO OPEN FROM THE GROUND. ADJUSTED PAX DOOR SPRING CABLES IAW 52-11-17. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080701 EA 2008 7 1 SWIA200819716 1 20080529 A 3411 0856KV9 PROBE CNDAIR CL600 CL6002C10 1390015 EA PITOT STATIC MALFUNCTIONED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 730SK 581 581 10193 CAPTAINS AND FIRST OFFICERS ALTIMETERS ARE SPLIT INFLIGHT. (FLT 5929) REPLACED LEFT PITOT HEAD IAW AMM 34-11-01. 2 L 7 2 4F RT A21EA 20080701 NE 2008 7 1 SWIA200819731 2 20080601 A 7261 INDICATOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE ENGINE OIL POPPED A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 755SK 10220 RIGHT ENGINE OIL PRESSURE INDICATED 0. (FLIGHT #6117)RESET INDICATION C/B AND RAN ENGINES WITH NO DEFECTS NOTED PER AMM 79-00-00. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080701 SO 2008 7 1 SWIA200819728 1 20080529 A 5610 NP1513111 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT LEAKING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 563SW 120338 AUTO PRESSURIZATION WILL NOT HOLD PRESSURE CORRECTLY. (FLT 5460) REPLACED LEFT WINDSHIELD AS REQUIRED PER MM 56-10-01. 2 L 7 2 4T RT A31SO 20080701 2008 7 1 SWIA200819772 4 20080609 A 3454 6226137001 RADIO EMB 120 EMB120ER 3260203 SO NAVIGATION MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 296SW 120325 BOTH NAV RADIOS WENT INOP. REPLACED FIRST OFFICERS VIR32 AND VOR ANTENNA COUPLER. OPERATIONAL CHECKS ARE GOOD. 2 L 7 2 4T RT A31SO 20080714 2008 7 14 SWAA083439 4 20080620 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080714 2008 7 14 SWAA083480 4 20080623 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 918WN 29843 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083070 1 20080606 A 5753 6546435278 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED SPV CHECK, FOUND RIGHT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD CORNER. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083185 1 20080610 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 DL757080811 1 20080530 A 5313 STRINGER BOEING 757 757232 1384965 NM BS 1720 S22L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 STR 22L AT STA 1710, FOUND CORROSION. REPAIRED PER SRM 53-00-03 FIG 201. 2 L 7 2 4F RT A2NM 20080714 NE 2008 7 14 DLM88080820 2 20080603 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 POWER LOSS A DALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 27 946DL 51356 49819 716800 AT CRUISE HAD LT ENG EPR 1.40 AND RT ENG EPR 1.88 WITH BOTH N1'S AT 75. COULD ONLY CLIMB AT 500 FPM AT 300 KIAS. PRESS URE CHECKED PT2 AND PT7 LINES NR 1 AND NR 2 ENGS. FOUND P FLEX LINE THRU PYLON LEAKING ON NR 2 ENG. REPLACED LINE. PU M EPR SYSTEM UP WITH TEST BOX PER M/M. ALL TEST CHECK GOOD. RAN ENG PER M/M. ALL CKS GOOD. 2 L 7 2 4F 4 F RT A6WE E9NE 20080714 NM 2008 7 14 DLM90080822 1 20080601 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FS 998 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 916DN 53396 LEFT CABIN CUSP WEB FS 998 CORRODED AT LIGHTNING HOLE. REMOVED CORROSION IAW MD90 SRM 53-00-01 FIG 3. MATERIAL LOSS 10 0 PERCENT OUT OF LIMITS IAW MD90 SRM 53-00-01 FIG 3. INSTALLED REPAIR DOUBLER IAW MD 80 SRM 53-05D FIG 827D. 2 L 7 2 4F RT A6WE 20080714 EU 2008 7 14 08FDEA02398 1 20080624 A 5320 A53773644202 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON CORNER FITTING C32 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080714 EU 2008 7 14 08FDEA02399 1 20080624 A 5320 A53773644203 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON CORNER FITTING C27 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 08FDEA02400 1 20080624 A 5340 BRACKET BOEING 727 727227 1384078 NM BS 305 S3-4R CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 STATION 305 BETWEEN STR'S 3R AND 4R WHERE COCKPIT BULKHEAD ATTACHES TO INTERCOSTAL, BRACKET CHAFFING THROUGH INTERCOSTAL . REMOVED INTERCOASTAL WEB IAW SRM 51-30-2. FABRICATED WEB IAW B727 SRM 51-10-3, 51-30-5, AND 53-10-2. TREATED AND P RIMED IAW SRM 51-10-2. INSTALLED NEW INTERCOASTAL IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20080714 EU 2008 7 14 08FDEA02401 1 20080624 A 5347 A53832100208 SEAT TRACK AIRBUS 300 A300B4622 3930401 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CRACKS IN WEB AT TRACKS 1-2 LT/RT AT C 47 REPAIR PERFORMED BY CRACK STOP HOLE AND INSTALLING A DOUBLER IAW RAS 705 11471/005/2008 ISS A, APPROVED BY EA 6-5315-120074. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 08FDEA02403 1 20080624 A 5313 BAC1498143 STRINGER BOEING 727 727227 1384078 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 STATION 344 STR 11R STRINGER TIE MIS-DRILLED AND HAS A FASTENER WITH ZERO EDGE DISTANCE. INSTALLED FRAME REPAIR, FILLER AND STRINGER CLIP IAW SRM 51-30-2, 53-10-4 FIG 1, 53-10-2 FIG 3 AND 51-20-1. 2 L 7 3 4F A3WE 20080714 EU 2008 7 14 USAA920081111 1 20080516 A 5540 D5537131800000 HINGE AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 602AW 565 SAL - MAJOR REPAIR - C1 CHECK - RUDDER HINGE NR 1 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 780 / RIB 2. REPLACED RUDDER HINGE NR 1, VERTICAL STABILIZER STATION 780 / RIB 2 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 20080714 NM 2008 7 14 08FDEA02409 1 20080624 A 5311 6516314 FRAME BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 FWD LAV BS 312 FRAME CRACKED FROM O/B WEB FASTENER TO O/B RADIUS JUST BELOW S-13 R. FABRICATED 3 REPAIR PARTS FOR FWD L AV BS 312 FRAME, REF SRM 53-10-4 FIG 1, HEAT TREATED, TRACKING NR 2008-06-068, 2008-06-064, AND 2008-06-065, TREATED AND PRIMED AND INSTALLED REF SRM 51-10-2 PG 1-7, 51-30-2 PG-2, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 08FDEA02411 1 20080624 A 5313 BAC1498140 STRINGER BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 STRINGER 6L, MIS-DRILLED HOLE, BS 950D, UPPER WEB. REMOVED DAMAGE SECTION OF STRG 6L, BS 950D 10. FABRICATED REPAIR PA RTS REF SRM 53-10-3 PG 5-9. TREATED AND PRIMED REPAIR PARTS REF SOPM 20-43-03 PG 3. INSTALLED REPAIR PARTS REF SRM 53- 10-02 PG 1-8 AND SRM 51-30-02 PG 1-11. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080714 EU 2008 7 14 08FDEA02412 1 20080624 A 5740 A572413790000 SUPPORT AIRBUS 300 A300F4605R 3930327 EU RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 THE RIGHT WING LOWER SKIN, UPPER SURFACE AFT OF THE REAR SPAR; STRAP IS CRACKED; ACCESS FROM PANEL 675 FB. COMPLIED WIT H EA 6-5730-118516. 2 L 7 2 4F RT A35EU 20080701 NM 2008 7 1 SWAA083406 1 20080619 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND RH WING #6 L/E SLAT INBOARD END DISBONDED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 DHL2008764505 1 20080520 A 5311 FRAME BOEING 727 727264 138408M NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C CHECK REF N/R 098175, DENT ON MAIN CABIN FRAME BS 540 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 MATERIAL 7075-T6 .050 INCH DIM 7 1/8 INCH BY 6 INCH PO NR 9006742. 2 L 7 3 4F A3WE 20080708 NM 2008 7 8 DHL2008764511 1 20080520 A 5347 SEAT TRACK BOEING 727 727264 138408M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 CORROSION ON MAIN CABIN SEAT TRACK BS 480-600 LBL 45. SEAT TRACK CORRODED OUT OF LIMITS STA 480-590 IAW B727 SRM 51-20- 2 FIG 21 AND 53-10-1 FIG 3. FAB NEW SECTION OF SEAT TRACK WITH BAC 1520-792-7178-T6511 DIM 9'2 INCH PO 9006020 IAW B727 SRM 53-10-2 FIG 1 AND VENTURA AEROSPACE DWG 2902. 2 L 7 3 4F A3WE 20080708 EA 2008 7 8 COMA0860242 1 20080511 A 5340 60034017 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 868CA 7427 DURING HMV4 INSPECTION THE STRINGER 3L TO FRAME FS 280 ATTACH CLIP WAS FOUND CRACKED. REMOVED AND REPLACED STRINGER CLI P IAW 51-42-21. 2 L 7 2 4F RT A21EA 20080708 EA 2008 7 8 COMA0860244 1 20080514 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 7050 SEVERE CORROSION FOUND ON LEFT FLOOR SILL BETWEEN FS 349.00 AND FS 364.00. REMOVED AND SPLICED SECTION OF FLOOR SILL IA W EA 10-5320-02217. 2 L 7 2 4F RT A21EA 20080708 EA 2008 7 8 COMA0860245 1 20080515 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 811CA 7380 FLIGHT 4988 - EN ROUTE FROM JAX TO LGA RECEIVED FLAPS FAIL CAUTION MESSAGE. EMERGENCY DECLARED, AIRCRAFT DIVERTED TO JF K AND LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 20080708 EA 2008 7 8 COMA0860254 1 20080526 A 5320 601R332371 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 588SW 7069 LEFT HAND LOWER POST BRACKET CRACKED CENTER WINDSHIELD. REMOVED AND REPLACED LEFT LOWER CENTER POST WINDSHIELD BRACKET. 2 L 7 2 4F RT A21EA 20080708 EA 2008 7 8 COMA0860255 1 20080516 A 2133 VP1257C00 EXHAUST VALVE CNDAIR CL600 CL6002B19 1900309 EA E&E BAY FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 916CA 32331 7014 FLIGHT 5246 - DURING CLIMBOUT FROM JFK RECEIVED CABIN ALT MESSAGE AT 8000 FT, COULD NOT CONTROL IN AUTO OR MANUAL. EMER GENCY DECLARED AND A/C RETURNED BACK TO JFK AND LANDED SAFELY. REMOVED AND REPLACED OVERBOARD EXHAUST VALVE. 2 L 7 2 4F RT A21EA 20080708 NM 2008 7 8 CALA0800522 1 20080602 A 5311 143A1110 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 FRAME CRACKED AT STATION 380 BETWEEN S8R AND S9R. REPAIRED FRAME AT STATION 380 S8R AND S9R PER EC/RA 5310-04777. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 CALA0800525 1 20080602 A 5311 146A1141 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 FRAME CRACKED AT STATION 827 BETWEEN S8R AND S9R. REPAIRED FRAME STATION 827 S8R AND S9R PER EC/RA 5310-04777. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 DL757080882 1 20080617 A 5320 STRUCTURE BOEING 757 757232 1384965 NM COCKPIT DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 COCKPIT FLOOR HAS DEEP DENT AT ENTRY. DOUBLER REPAIRED DAMAGE IAW SRM 51-20-01. 2 L 7 2 4F RT A2NM 20080708 NM 2008 7 8 DL757080860 1 20080612 A 5320 DOUBLER BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 MAIN CABIN FLOOR STRUCTURE DECK PLATE REPAIR DOUBLER HAS CORROSION STA 1715 LBL 12. REPLACED DOUBLER IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 20080708 NM 2008 7 8 DL757080863 1 20080612 A 5311 FRAME BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 AFT CARGO PIT STA 1540 LT FRAME AT STR 23L HAS A DENT. REPAIRED DENT IAW SRM 53-00-07. 2 L 7 2 4F RT A2NM 20080708 NM 2008 7 8 DL757080869 1 20080613 A 5347 SEAT TRACK BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 MAIN CABIN STA 365 SEAT TRACK AT RBL 45 HAS SEVERE CORROSION, EXFOLIATED. REPLACED DAMAGED SEAT TRACK IAW SRM'S 51-40-0 2 AND 53-10-52. 2 L 7 2 4F RT A2NM 20080708 NM 2008 7 8 DL757080873 1 20080615 A 5230 SKIN BOEING 757 757232 1384965 NM AFT CARGO DOOR DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 RAMP REPORTS 2 MINOR DENTS IN AFT CARGO DOOR. 1ST APPROX 8 IN BELOW HANDLE AFT EDGE. 2ND APPROX 7 IN AFT AND 4 IN UP F ROM FWD CORNER OF DOOR. DENT AT FWD CORNER OF DOOR FOUND TO BE OUT OF LIMITS. REPLACED REPAIR DOUBLER IAW SRM 51-40-01 . 2 L 7 2 4F RT A2NM 20080708 NM 2008 7 8 DLM8K080856 1 20080612 A 2910 B-NUT DOUG MD88 MD88 3023688 NM HYDRAULIC SYSTEM LOOSE A DALA A UNSCHED LANDING K FLUID LOSS DE DESCENT 1 SO 27 908DE 53417 ON DESCENT AFTER TURNING ON AUX AND TRANS PUMPS, HYD QTY LOW LIGHT ILLUM AND QTY INDICATED 2 QTS. C/W QRH. FOUND LOOSE B NUT ON ELBOW FITTING TO FILTER MODULE ASSY LEFT TAIL COMPT. SECURED SAME AND REPLACED BOTH FILTERS ON MODULE ASSY. LEAK CKS OK. 2 L 7 2 4F RT A6WE 20080714 EU 2008 7 14 08FDEA02413 1 20080624 A 5320 A5361221420001 FLOOR SUPPORT AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 MDCC FLOOR SUPPORT HAS CORROSION BETWEEN FRAME 13 AND FRAME 13A, LBL 73.66 CM. REMOVED AND REPLACED THE FLOOR SUPPORT I AW A300 SRM 51-40-21, PARA 6. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 USAA920081116 1 20080508 A 5312 651758243 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 157AW 23779 MCN - MAJOR REPAIR - C21 CHECK - CRACKED BULKHEAD WEB, BS 178, LBL 17, WL 225. REPAIRED BULKHEAD WEB, BS 178, LBL 17, W L 225 IAW B737 SRM 53-10-08 2R 12 FIGURE 201. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 USAA920081119 1 20080505 A 5310 655287846 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 157AW 23779 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON THE L2 DOOR CUTOUT CREASE BEAM INNER CHORD, BS 967 - 986, LBL 52. REPLACE D, THE L2 DOOR CUTOUT CREASE BEAM INNER CHORD, BS 967 - 986, LBL 52 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080714 EU 2008 7 14 08FDEA02420 1 20080624 A 5753 A579600050100 SKIN AIRBUS 300 A300F4605R 3930327 EU ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 L/W INBD FLAP LOWER SURFACE HAS NUMEROUS DENTS BETWEEN INBD END AND OUTBD END. REMOVED THE TOP COAT AT THE DENT AREAS I AW AMM 51-75-2-7. REPAIRED THE OUT OF LIMITS AREA IAW SRM 57-50-00. TOP COATED REPAIR & FILLED AREAS IAW SRM 51-23-1 0. 2 L 7 2 4F RT A35EU 20080714 EU 2008 7 14 08FDEA02041 1 20080530 A 5315 A53778807202 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON TOP CAP BEAM C 35 RT BETWEEN OUTER STRUT AND CORNER FITTING TOP CAP BEAM REPAIR PERFORMED IAW SRM 5 3-10-15 FIG 207. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 ASAA0843102 1 20080610 A 5320 65C335831 WEB BOEING 737 7374Q8 138447Q NM BS 986-1015 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 SHEAR WEB AT BS 986 TO BS 1015 RT IS CRACKED. SHEAR WEB REPLACED WITH FABRICATED PART IAW B737 400 SRM 52 60 51 SRM 51 40 05 AND 51 21 00. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 ASAA0843105 1 20080509 A 5320 657374143 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 303 S4L CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 CRACKED INTERCOSTAL COMMON TO UPPER SILL BEAM STRAP STA 303 STR4L. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 08FDEA02080 1 20080602 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 624FE 48443 DURING HFEC OPEN HOLE INSPECTION ON LOWER JAMB SUPPORT FITTING BOLT BORE HOLE, 01 EA CRACK WAS FOUND ON THE FWD SIDE OF 3RD LAYER ON THE AFT I/B BOLT HOLE AT NR 7 LOWER JAMB SUPPORT FITTING. CRACKED LOWER JAMB NR 7 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080714 NM 2008 7 14 08FDEA02081 1 20080602 A 5730 ARB74023 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 624FE 48443 CRACK FOUND QUANTITY 3 FASTENER HOLES ON LT SIDE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUTOUT BETWEEN STA XORS=683.4 A ND XORS=713.6. LT SIDE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUTOUT BETWEEN STA XORS=683.4 AND XORS=713.6 03 FASTENER HOLES CRACKED. AREA REPAIRED AS PER FEDEX EA 1-5710-122470- AD 2007-07-04- WINGS - LT LOWER SKIN PLANK CUT OUT AT 536AB . THREE ACCESS DOOR ATTACHMENT BORES WITH CRACK INDICATIONS PSE 57.23.01 ALI-REPAIR. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100. REPETITIVE INSPECTION, TO BE ACCOMPLISHED NLT EVERY 2000 FLIGHT CYCLES, STARTING FROM 13,324 CSN. 2 L 7 3 4F RT A22WE 20080714 2008 7 14 BB08095 4 20080522 A 2565 140N28231 LINK BOEING 757 7572B7 1384964 NM EVAC SLIDE BINDING A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 933UW 27199 CLT - DURING THE R2 DOOR EMERGENCY EVACUATION SLIDE OPERATIONAL TEST, THE R2 DOOR DID NOT OPEN, AND THE DOOR ASSIST BOTT LE DID NOT DISCHARGE DUE TO A BINDING LINK. MAINTENANCE REPLACED DOOR ASSIST BOTTLE LINK. SYSTEM OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 BB08096 1 20080524 A 2560 P4010021 BATTERY BOEING 767 7672B7 1385107 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 253AY 24894 PHL - THE FLASHLIGHT AT D POSITION WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AT D POSITION. OK FOR SERVI CE. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 08FDEA02426 1 20080624 A 5340 6545313Y2 STRINGER CLIP BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 STRINGER CLIP ON STR 8L, AT FS HAS AREAS OF SURFACE CORROSION REMOVED AND REPLACED STR CLIP, STA 720B, STR 8L REF SRM 51 -30-2 PGS 8-9 AND 32. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 08FDEA02428 1 20080624 A 5711 6526797 SPAR BOEING 727 727225 1384077 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 PANEL JUST AFT OF RT WING AFT SPAR LOWER CHORD IS CORRODED FABRICATED NEW PANEL FROM JUST AFT OF RT WING SPAR LOWER CHOR D REF. BOEING DWG 65-26797-3, TREATED AND PRIMED AND PAINTED REF SRM 51-10-2 PG 1-7, MM 51-20-151-7. THIS IS CLASSIF IED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 08FDEA02429 1 20080624 A 5340 6545313Y2 STRINGER CLIP BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 STRINGER CLIP CRACKED, BS 950 E, STRINGER 6L. REPLACED STRINGER CLIP REF SRM 51-30-2 PG 1-7. THIS IS CLASSIFIED AS A M AJOR REPAIR. 2 L 7 3 4F A3WE 20080714 WP 2008 7 14 08FDEA02064 1 20080530 A 5720 ANB720335 STIFFENER DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 LEFT MLG WHEEL WELL LEFT WING INBD WEB AFT OF THE MLG GEAR CUTOUT; THE FIRST ANGLE IS CRACKED AT THE BOTTOM. REMOVED CO VERS IAW DC/MD-10 SRM 51-31-01; VOL II AND STIFFENER IAW DC/MD-10 SRM 51-31-01 AND 51-33-01 VOL II. MATERIAL ID FOR ST IFFENER 7075-0, 0.063 PO 613534.3. FABRICATED STIFFENER IAW DAC DWG ANB7203, REV "BA". ALODINED; PRIMED AND PAINTED IA W DC/MD-10 SRM 51-21-01; PGS 21-24 AND 51-21-02; VOL II. INSTALLED STIFFENER IAW DC/MD-10 SRM 51-33-01; VOL II AND 51-2 1-02; VOL II. 2 L 7 3 4F RT A22WE 20080714 WP 2008 7 14 08FDEA02067 1 20080530 A 5720 ANB720311 STIFFENER DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 LEFT MLG WHEEL WELL; LEFT WING INBD WEB; 4TH ANGLE AFT OF THE MLG CUTOUT IS CRACKED. THIS SDR WAS GENERATED IN ERROR. FOR DETAILS OF THIS DISCREPANCY SEE NON-ROUTINE NR N00205 AND SDR TRACKING NUMBER 08-2066. 2 L 7 3 4F RT A22WE 20080714 EU 2008 7 14 08FDEA02442 1 20080625 A 5320 ANGLE AIRBUS 310 A310222 3930315 EU FUSELAGE UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 FR 54-Y450 THE UPPER ANGLE FOR MOUNTING OF BULKHEAD LINING OF AFT CARGO COMPARTMENT. REMOVED THE RELATIVE FASTENERS F OR ACCESS PER SRM 51-40-21. REMOVED THE CORROSION PER SRM 51-74-10/201. APPLIED AN ALODINE COATING PER SRM 51-74-10/00 1. NDT MEASURED THE REMAINING THICKNESS PER NTM 51-10-04. THE ORIGINAL THICKNESS IS 0.098 INCH PER SRM 53-15-18/001 AL LOWABLE DAMAGE IS 10% PER SRM 53-10-00/101, IT IS NOT WITHIN THE LIMIT. MAKE THE REPAIR PART PER DWG: A53410767200. IN STALLED THE REPAIR PART PER SRM 51-40-21. RESTORED FINISH PER AMM51-75-10. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 08FDEA02443 1 20080625 A 5713 ARB29323 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 LEFT WING LEADING EDGE STRINGER AT STATION XOS 672 FOUND CRACKED OFF. REPAIR CARRIED OUT AS PER EA 1-5720-122504, REPA IR CLASSIFIED MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080714 EU 2008 7 14 08FDEA02444 1 20080625 A 5415 A54610926000 ATTACH FITTING AIRBUS 310 A310222 3930315 EU PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 PYLON TO ENGINE AFT ATTACHMENT BEAM CORROSION ON MATING FACE. CLEAN THE BEAM CAREFULLY PER AMM 12-21-12. PERFORMED DVI FOR CORROSION (FOUND CORROSION). REMOVED CORROSION USING ABRASION BY HAND AS PER SRM 51-74-10,PARAGRAPH 7.B. MEASURED THE REWORKED AREA AND THE REMOVAL THICKNESS OF MATERIAL. PERFORMED MANTENANCE ACTIONS IAW EA 6-5450-117357. 2 L 7 2 4F RT A35EU 20080714 EU 2008 7 14 08FDEA02445 1 20080625 A 5320 STRAP AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 FWD CARGO COMPT BELOW FLOOR LEVEL BETWEEN FR38.2 - FR39, STR 56L-STR 57(CTR) SKIN STRAP WITH LIGHT CORROSION. REMOVED T HE RELATIVE FASTENERS FOR ACCESS PER SRM 51-40-21. REMOVED THE CORROSION PER SRM 51-74-10/201. APPLIED AN ALODINE COAT ING PER SRM 51-21-10/001. THE REMAINING THICKNESS IS 0.049 INCH (EXCEEDED LIMIT) PER NTM 51-10-04. REPAIR PER EA 6-53 10-117360. 2 L 7 2 4F RT A35EU 20080714 WP 2008 7 14 08FDEA02447 1 20080625 A 5542 AMC71121 SKIN DOUG DC10 DC1010 3022110 WP RUDDER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 UPPER AFT RUDDER FOUND CORROSION MODERATE ABOVE SKIN AND SUSPECT INNER SKIN. REPAIRED AREA IAW SRM 55-10-00 VOL I FIG 2 . 2 L 7 3 4F A22WE 20080714 EU 2008 7 14 08FDEA02076 1 20080601 A 3230 A252791 SEQUENCE VALVE AIRBUS 300 A300F4605R 3930327 EU MLG FAILED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 CE 21 668FE 18487 18487 772 ON FINAL APPROCH DURING LANDING GEAR EXTENSION, LEFT MAIN GEAR WOULD NOT EXTEND. RED GEAR NOT DOWN INDICATION ON BOTH P OSITION 1 AND 2 AND OVERHEAD PANEL. PROCEEDED WITH LANDING GEAR GRAVITY EXTENSION PROCEDURE. ALL GEAR DOORS OPENED BUT LEFT MAIN GEAR STILL NOT DOWN AND LOCKED. A STEADY STATE SIDE LOAD WAS APPLIED AND LEFT MAIN GEAR EXTENDED AND INDICA TED GREEN LIGHT. ALL HYDRAULIC INDICATIONS NORMAL. SEQUENCING VALVE APPEARED TO BE BYPASSING. REMOVED AND REPLACED M LG LT SEQUENCING VALVE IAW A300 MM 32-31-37-4. CYCLED MLG 25 TIMES. OPS AND LEAK CK GOOD. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 DLM88080876 1 20080616 A 3040 3080800 BLANKET DOUG MD88 MD88 3023688 NM RT WING SHORTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 935DL 49722 727230 WHILE INSTALLING RT WING HEATER BLANKET MTC DRILLED AFT HOLES PRIOR TO VACUUM BAGGING AS CALLED FOR IN AMM. ER/A ISSUED TO AUTHORIZE DRILLING THE HOLES PRIOR TO BAGGING. 2 L 7 2 4F RT A6WE 20080714 WP 2008 7 14 08FDEA02034 1 20080529 A 5230 ADA37991 SKIN DOUG MD10 MD1010F 3022112 WP CARGO DOOR BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 FWD LOWER CARGO DOOR EXTERIOR IS BENT ON THE LEFT SIDE OF THE DOOR. CUTOUT DAMAGE AND FABRICATED REPAIR DOUBLER, FILLER AND REPAIR ANGLE PER DC/MD-10 SRM 52-10-00, FIG 17; SHEET 1; VOL I. ALODINED AND PRIMED PER DC/MD-10 SRM 51-21-01; PG S 21 AND 25; VOL II. INSTALLED REPAIR DOUBLER, FILLER AND REPAIR ANGLE PER DC/MD-10 SRM 52-10-00, FIG 17, SHEET 1, VOL I. 2 L 7 3 4F RT A22WE 20080714 WP 2008 7 14 08FDEA02093 1 20080602 A 5730 ARC0619501 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 LEFT WING LOWER TRAILING EDGE PANEL NR 551 BB INBD UPPER EDGE IS WORN FROM FRETTING. REPAIRED LEFT WING T/E PANEL NR 55 1 BB BY REMOVING THE DAMAGED AREA, FABRICATING A NEW FILLER AND DOUBLER. PERFORMED BONDING, CURE AND SEALING IAW DC/MD- 10 SRM 51-71-00; VOL II. PAINTED AND RESTORED FINISH IAW DC/MD-10 SRM 51-21-01; VOL II. 2 L 7 3 4F RT A22WE 20080714 NM 2008 7 14 08FDEA02454 1 20080625 A 5730 PANEL BOEING 727 727225 1384077 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 RT LOWER SIDE T/E PANEL FOWARD OF I/B AILERON HAS CRACK IN O/B EDGE SUPPORT ANGLE 1 3/4 INCH FORWARD FROM AFT EDGE. REM OVED DAMAGED PART PER REF SRM 51-30-2 PG 1-3. FABRICATED NEW PART PER DWG 65-19281-107. TREATED AND PRIMED NEW PART PE R REF SRM 51-10-02. INSTALLED NEW PART, PER REF 51-30-02 PG 1-3. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080714 EU 2008 7 14 08FDEA02456 1 20080625 A 5347 A53279239200 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 660FE 759 MDCC SEAT TRACK NR 1 FR 71 TO FR 78 HAS 4 AREAS OF CORROSION REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SECTION OF TRAC K AND INSTALLED SEAT TRACK SPLICE REPAIR AT TRACK NR 1 BETWEEN FR 71 AND FR 80 IAW A300-600 SRM 53-10-16, FIG 208. 2 L 7 2 4F RT A35EU 20080714 EU 2008 7 14 08FDEA02457 1 20080625 A 5347 A5361252420002 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 660FE 759 MDCC SEAT TRACK NR 3 LT HAS CORROSION BETWEEN FR 15 AND FR 17 REMOVED LEVEL 1 CORROSION. REMOVED AND REPLACED SEAT TRAC K WITH NEW PART AT TRACK NR 3 LT BETWEEN FR 15 AND FR 17 IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 08FDEA02462 1 20080625 A 5320 656725572 STRAP BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 FWD CARGO COMPARTMENT RT STRIP AT STA 620 - 660, CORRODED ON BACK SIDE AND CRACKED FABRICATED NEW STRIP USING .063" 2024 T-3, A93206 REF BAC DWG 65-67255 1498-288 SRM 51-20-1 FIG 7. TREATED AND PRIMED REF 51-10-2 PART MARKED REF FED EX GMM 7-0-1001. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080714 WP 2008 7 14 08FDEA02164 1 20080605 A 5414 PANEL DOUG MD10 MD1010F 3022112 WP NR 3 PYLON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 NR 3 PYLON PANEL 488 GL IS CHAFED ON THE INNER SKIN. 2 L 7 3 4F RT A22WE 20080714 WP 2008 7 14 08FDEA02279 1 20080615 A 2170 COALESCER BAG DOUG MD10 MD1010F 3022112 WP NR 2 ODOR A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 21 568FE 47827 MEM TO LAS NR 2 MANIFOLD FAIL AT FL 380 ACCOMPANIED BY BURNING ODOR. EMERGENCY DIVERT TO KDFW AS PER QRH. PERFORMED DE CAY CK NR 2 SYS; CK PASSED, NOTICED NR 2 PACK BURNED SMELL. REMOVED AND REPLACED THE NR 2 PACK COALESCER SOCK; NO FURTH ER BURNED SMELL NOTICED. ACN RELEASED FOR SERVICE PER MEL 36-23-01-02. FOUND D1-29 LOOP BAD REMOVED AND REPLACED LOOP. OPS CHECK GOOD. RETURNED TO SERVICE. 2 L 7 3 4F RT A22WE 20080714 NM 2008 7 14 08FDEA02305 1 20080618 A 5315 143N534640 FLOORBEAM BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 CORROSION FOUND ON FLOOR SUPPORT AT BS750, LBL 8. CORROSION FOUND EXCEED ALLOWABLE DAMAGE LIMITS IN SRM 51-10-02. REMO VED AND REPLACED FLOOR SUPPORT STRINGER IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINO R PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080708 NM 2008 7 8 DLM88080826 1 20080604 A 5751 5955401502 SKIN DOUG MD88 MD88 3023688 NM AILERON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 917DL 49573 DISBOND IN SKIN AND CRACK FOUND IN SPAR ON AILERON DURING SHOP VISIT. REPAIRED PER DELTA ERA 467537-14, REV A. 2 L 7 2 4F RT A6WE 20080708 NM 2008 7 8 DLM88080834 1 20080604 A 3250 BOLT DOUG MD88 MD88 3023688 NM NLG STEERING MISSING A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 960DL 49979 ON TAXI OUT NOSE WHEEL STEERING TO THE LEFT GAVE OUT. A/C BROUGHT BACK TO GATE BY SUPERTUG NO STEERING WORKING. FOUND BOLT MISSING FROM STEERING CONTROL VALVE ROD END. FOUND MISSING HARDWARE IN TUNNEL BELOW VALVE. 2 L 7 2 4F RT A6WE 20080708 EU 2008 7 8 2008UALA02687 1 20080507 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT ODOR A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 420UA 489 ODOR IN COCKPIT SMELLED ELECTRICALLY HOT TURNED BLOWER FAN TO OVRD, SMELL DISSIPATED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080708 2008 7 8 ASAA0852976 4 20080521 A 3160 1741010201 CDU BOEING 737 737890 1384527 NM COCKPIT MALFUNCTIONED A ASAA O OTHER O OTHER CR CRUISE 1 NM 02 579AS 4887 35187 LEFT CDU BLANKED OUT FOR A MOMENT EN ROUTE. ABOUT 5 SECONDS IT WENT THROUGH A SERIES OF BIT TEST THEN CAME BACK TO A NO RMAL SCREEN. CHECKED FMC INFLIGHT FAULT LEFT FMC CDU FAULTED. PERFORMED FIM34 61 TASK 804 FAULT RESET CDU TEST GOOD REF FIM 34 61 TASK 804. 2 L 7 2 4F RT A16WE 20080710 NM 2008 7 10 DLM90080733 1 20080514 A 5753 5910042609 SKIN DOUG MD90 MD9030 3023690 NM FLAP VANE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 LEFT WING O/B FLAP CENTER FIXED VANE UPPER SURFACE IS CRACKED. REMOVED & REPLACED LT O/B CENTER FIXED VANE, IAW MD90 AM M 27-50-02. 2 L 7 2 4F RT A6WE 20080710 NM 2008 7 10 DL76L080744 1 20080418 A 3397 CONNECTOR BOEING 767 767332 1382001 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 EEL SEAT FEEDER AT STA 478 LEFT MISSING MOLEX CONNECTOR. REMOVED AND REPLACED EEL CONNECTOR AT STA 478 LEFT, EELS LIGHT OPS CHECKS GOOD IAW B767-300 MM 33-51-10. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 DL76L080755 1 20080507 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 188DN 27583 EMERGENCY LIGHTS INOP AT SEATS 6A. REMOVED AND REPLACED POWER SUPPLY AND OPS CHECK GOOD IAW DAL B767-300 MM 33-51-07. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 DL76L080757 1 20080515 A 3350 LIGHT BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 188DN 27583 L-1 DOOR LOWER FWD EMERGENCY LIGHT INOP. RELAMPED L-1 DOOR FWD EMERGENCY LIGHT IAW B767 MM 33-51-01-962-001. OPS CHECK GOOD IAW B767 MM 33-51-01. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 DLM88080763 1 20080519 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 963DL 49982 DURING HMV A CRACK WAS FOUND ON FUSELAGE SKIN AT STA Y=1437 BETWEEN LONG 3 AND 4LT. CRACK WAS REPAIRED IAW SRM 53-04D F IG 27. 2 L 7 2 4F RT A6WE 20080710 NM 2008 7 10 USAA920081102 1 20080515 A 5755 654645170A SKIN BOEING 737 7374B7 1384702 NM NR 2 SPOILER DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 444US 24862 CLT - MAJOR REPAIR - C2 CHECK - LEFT WING NR 2 SPOILER TRAILING EDGE SURFACE IS DEBONDED. REPAIRED THE LEFT WING NR 2 S POILER TRAILING EDGE SURFACE IAW B737 SRM 51-70-10. 2 L 7 2 4F RT A16WE 20080710 2008 7 10 HNAA0800178 4 20080518 A 2300 526011 ELECTRONIC UNIT DHAV DHC8 DHC8102 2809003 NM COMM SYSTEM FAULTY A HNAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 07 814EX 32320 983 318 BOTH COMMS ARE UNREADABLE DUE TO CHIRPING SOUNDS AND UNABLE TO TRANSMIT DUE TO SAME. REMOVED AND REPLACED REU, OPS CHEC K GOOD, IAW -8 MM 23-30-06. 2 H 7 2 4T RT A13NM 20080710 NM 2008 7 10 2008UALA02819 1 20080515 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 AFT PIT STA 1560 AT STRL FRAME DENTED. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED DAMAGE, FABRICATED AND INSTALLED RPR IAW SRM 53-00-07 FIG 201 RPR 5. THIS IS A CAT B RPR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSP STARTING AT 50,0 00 TOTAL FC AND 12,000FC THERE AFTER. INSP TO BE ACP PER SRM 53- 00-07 RPR 5 TABLE II ZONE 1. INSP ARE BOTH VISUAL AND NDT. CURRENT PTC IS 20417 WORK ACP BY MECH 111457 AND INSP BY QC 071 ON NR 20301 RII INSP ACP BY QC 071, SEE CF 9058 FOR SUPP LEMENTAL INSP REQUIRMENTS. 2 L 7 2 4F 4 F RT A2NM E17NE 20080710 NM 2008 7 10 2008UALA02833 1 20080515 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCONNECTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 507UA 24743 EEL LIGHT AT ROW 13ABC IS DISCONNECTED AND CLEAR COVER IS MISSING FOR A 10 INCH SECTION. RECONNECTED WIRE AND REPLACED MISSING OR IMPROPER LENGTH COVERS. SYSTEM TEST OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080710 NM 2008 7 10 2008UALA02936 1 20080521 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EXIT EEL LIGHT INOP AT SEAT ROW 43 LEFT. REPLACED LIGHT ASSY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080710 NM 2008 7 10 2008UALA02937 1 20080521 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EXIT EEL LIGHT INOP AT LOWER WALL EMERGENCY LIGHT ACROSS DOOR 4 LEFT. FOUND LOOSE CONNECTION. SECURED CONNEC TION OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080710 NM 2008 7 10 2008UALA02946 1 20080521 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 FUSELAGE SKIN CRACKED AT STR 12 RIGHT, STA 520. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 20080710 NM 2008 7 10 2008UALA02947 1 20080522 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY LIGHT ROW 49 RIGHT INOP. FOUND FAULTY LIGHT STRIP. REPLACED LIGHT STRIP OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080710 NM 2008 7 10 2008UALA02956 1 20080520 A 2424 756603E GCU BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RIGHT FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 217UA 30550 ELEC GEN OFF R RIGHT GENERATOR CONTROL BREAKER (GCB) OPEN OR GENERATOR CONTROL SWITCH OFF, AND ENGINE NOT SHUT DOWN. AD VISORY MSG01- NOT ACTIVE DESCENT MODE DEPENDENT; INTEGRATED DRIVE GENERATOR (R) FREQUENCY IS LOW. DB- GENERATOR CONTROL UNIT (R) MSG02- LATCHED DESCENT MODE DEPENDENT; INTEGRATED DRIVE GENERATOR (R) WAS MANUALLY DISCONNECTED. DB- GENERATO R CONTROL UNIT (R) MSG-2431632 INACTV DC MODE MSG-2431562 LATCHD DC MODE. FOUND FAULTY GENERATOR AND INTEGRATED DRIVE U NIT. REPLACED RT GCU PER MM24-22-02, OPS CHECKS NORMAL. INSTALLED NEW IDG PER AMM 24-11-01-401. OP AND LEAK CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080710 WP 2008 7 10 070198 1 20080511 A 3350 57761 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 877GA 53467 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 20080710 NM 2008 7 10 USAA920081105 1 20080513 A 5315 BAC15063116 FLOORBEAM BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 MIA - MAJOR REPAIR - C4 CHECK - CORROSION ON CABIN FLOORBEAM, BS 1518, LBL 6 - RBL 6. REPAIRED CABIN FLOORBEAM, BS 1518 , LBL 6 - RBL 6 IAW B767 SRM 53-00-51 REPAIR 1. 2 L 7 2 4F RT A1NM 20080603 EA 2008 6 3 SWIA200819649 1 20080319 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 952SW 7805 LEFT ENGINE THRUST FITTING IS CORRODED, FOUND AT C-CHECK. REPLACED LEFT ENGINE AFT MOUNT THRUST FITTING PER CRJ200 AMM TASK 71-22-01-400-801. 2 L 7 2 4F RT A21EA 20080603 EA 2008 6 3 SWIA200819654 1 20080326 A 7120 BUSHING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 948SW 7789 LEFT ENGINE FORWARD MOUNT BOLT AND BUSHINGS ARE CORRODED, FOUND AT C-CHECK. REPLACED BOLT AND BUSHINGS IAW CRJ200 AMM 7 1-21-01-000-801 AND 71-21-01-400-801. 2 L 7 2 4F RT A21EA 20080603 NM 2008 6 3 QXEA200800520 1 20080525 A 2610 WIRE BOMBDR DHC8 DHC8402 1390042 NM FIRE SUPPRESSION BROKEN A QXEA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 09 424QX 4006 LAX - WHEN PERFORMING FIRE WARNING TEST, FOUND NR 1 ENGINE PRESS TO RESET LIGHT INOP. RESET SWITCH WORKS GOOD WHEN PERF ORMING FIRE TEST FOR NR 1 ENGINE, AURAL CHIME RESETS WHEN THE RESET SWITCH IS PRESSED. BOTH T HANDLES INDICATE NORMALLY . MAINTENANCE FERRIED THE AIRCRAFT TO PDX. IN PDX, FOUND WIRE ON TERMINAL A ON BACK OF CAPTAIN'S ENGINE FIRE RESET LIG HT SWITCH SOLDER BROKEN. SOLDERED WIRE TO TERMINAL A. CHECKS GOOD. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080603 NM 2008 6 3 CALA0800504 1 20080528 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 LEFT-HAND STATION 827 AT S8L AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED CRACK AT STATION 827 S 8L PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080603 NM 2008 6 3 AALA200801124 1 20080428 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHT AT SEAT 26C LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080603 NM 2008 6 3 P5CA0801562 1 20080520 A 7810 NOZZLE BOEING 747 74746NF 13848BT NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 EA 15 450PA 30808 ON WALK AROUND AFTER ARRIVAL FOUND A CRACK AT 2 O'CLOCK POSITION ON NR 3 ENGINE EXHAUST NOZZLE. PERFORMED INTERIM REPA IR IAW EO 4478A070 WITH DVI EVERY 3 FLIGHT CYCLES. 2 L 7 4 4F RT A20WE 20080603 EA 2008 6 3 REXA200800015 1 20080527 A 7500 34H80150 COUPLING CNDAIR CL600 CL6002B19 1900309 EA BLEED AIR LEAKING A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 8458A 7458 ON CLIMB-OUT AFTER TAKEOFF FROM KMSP, THE "R 14TH DUCT" WARNING MESSAGE ILLUMINATED FOLLOWED BY THE "BLEED AIR DUCT" AUR AL WARNING. THE FLIGHT CREW RAN THE QRH, DECLARED AN EMERGENCY AND RETURNED TO KMSP. RIGHT ENGINE POWER WAS REDUCED TO IDLE AND AN OTHERWISE NORMAL APPROACH AND LANDING WERE COMPLETED. CFR FOUND NO DAMAGE TO THE ENGINE AND THE AIRCRAFT W AS RELEASED TO THE GATE. MAINTENANCE FOUND THE AFT COUPLING OF THE 14TH STAGE BLEED VALVE TO BE LEAKING. THE COUPLING AND THE PYLON SENSING LOOP WERE REPLACED. MAINTENANCE ALSO COMPLIED WITH AN OVERWEIGHT LANDING INSPECTION ON THE AIRCRA FT. 2 L 7 2 4F RT A21EA 20080702 NM 2008 7 2 SWAA083384 1 20080619 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 2008UALA03577 1 20080624 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY LIGHT ON AFT GALLEY LT WALL INOP AT L5 DOOR. FOUND BURNED OUT LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080702 NM 2008 7 2 2008UALA03512 1 20080620 A 5320 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 811UA 847 BEAM NR 130 FOUND CORRODED. REMOVED CORROSION. 2 L 7 2 4F 4 F RT A28NM E40NE 20080702 NM 2008 7 2 CALA0800625 1 20080620 A 5320 65C33582 PAN BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 CORROSION FOUND ON UNDERSIDE OF FLOORBEAM PAN AT BODY STATION 1016 LBL 37. FABRICATED NEW FLOOR PAN IAW BAC DWG 65C3358 2, FABRICATED T-CAP REPAIR STRAP IAW SRM 53-00-51, ALODINED AND PRIMED IAW SRM 51-20-01, INSTALLED FLOOR PAN DRIP PAN GA LLEY MOUNTS T-ANGLE AND REPAIR STRAP IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 CALA0800584 1 20080610 A 5754 65C26794 SKIN BOEING 737 737524 1384721 NM L/E SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 NUMBER 2 SLAT HAS CRACKS ON THE LOWER TRAILING EDGE AT AFT RIVETS FSS 424 AND 426. TRIMMED OUT CRACKED SKIN AND INSTALL ED REPAIR DOUBLER AND FILLER PER SRM 57-43-01 FIG 201 AND REINSTALLED INNER PANEL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080702 2008 7 2 SWAA083319 4 20080618 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083325 1 20080618 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER TEE CHORD CRACKED BETWEEN BS 655 AND BS 675, RBL 25. REM OVED AND REPLACED TEE CHORD PER SRM. 2 L 7 2 4F RT A16WE 20080702 NM 2008 7 2 SWAA083062 1 20080608 A 2731 251A2420 CONTROL VALVE BOEING 737 7377H4 1384404 NM ELEVATOR TAB FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 223WN 32492 DURING SCHEDULED HC1 CHECK, RT ELEVATOR TAB FAILED CONTROL CHECK. REMOVED AND REPLACED TAB CONTROL VALVE PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082802 1 20080524 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082847 1 20080526 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082856 1 20080526 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080703 2008 7 3 SWAA082831 4 20080523 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082873 1 20080527 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080703 NM 2008 7 3 SWAA082838 1 20080523 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED MV3 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080703 2008 7 3 2008UALA03513 4 20080621 A 8300 GEARBOX BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 ENGINE MAKING METAL A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 798UA 26928 222003 FOUND METAL ON NR 2 ENGINE MAIN GEAR BOX CHIP DETECTOR. ENGINE REMOVED. SHOP TEARDOWN REVEALED THAT MAIN GEARBOX MB7 B EARING HAD FAILED. ALL RELEVANT HARDWARE WAS RETURNED TO MANUFACTURER FOR FURTHER ANALYSIS. THIS IS AN ONGOING PROBLEM THAT MANUFACTURER IS ACTIVELY INVESTIGATING. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080707 NM 2008 7 7 BB08089 1 20080514 A 2560 P4010021 BATTERY BOEING 767 7672B7 1385107 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 252AU 24765 PHL - THE FLASHLIGHT AT DOOR L-2 NEEDS A NEW BATTERY. MAINTENANCE REPLACED BATTERY IN FLASHLIGHT AT DOOR L-2. 2 L 7 2 4F RT A1NM 20080707 2008 7 7 USAA920081077 4 20080514 A 2565 60592101 RESERVOIR AIRBUS 320 A320214 3930316 EU EVAC SLIDE BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 105UW 868 PIT - EES - C11 CHECK - LEFT WING SLIDE INFLATION RESERVOIR CABLE ASSEMBLY BROKEN. REPLACED LEFT WING SLIDE INFLATION R ESERVOIR IAW A320 AMM 25-62-46. 2 L 7 2 4F RT A28NM 20080707 NM 2008 7 7 UPS08M52263 1 20080428 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C CABIN-BETWEEN STA 879-899, SEAT TRACK CROWN AREA, X=75.25 FOUND SURFACE CORROSION AS MARKED CORROSION AT CABIN BETWEEN STA 879-899 X=75.25 ON SEAT TRACK CROWN SURFACE AREA REMOVED PER SRM51-21-01 V.II R35. EXISTING SEAT T RACK REPAIR SPLICES AT STA 869 AND STA 929 REMOVED PER SRM 51-31-01 V.II R35. HFEC INSP C/O PER DAC NDTSPM R13 06-10-01 .001 ON EXISTING TRIMMED OFF FOUND NO CRACK. NEW SEAT TRACK REPAIR SECT AND SPLICE INSTALLED PER SRM51-31-01 V.II R35 2 L 7 3 4F RT A22WE 20080707 2008 7 7 2008UALA02749 4 20080509 A 2565 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR OBSTRUCTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 597UA 28750 DOOR 1R WILL NOT ARM. DEBRIS UNDER GIRT BAR. CLEANED DEBRIS, STOWED LANYARD AND DOOR ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080707 NM 2008 7 7 2008UALA02806 1 20080515 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 SEAT 5J AFT EMERGENCY LIGHT IS INOPERATIVE. RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080707 NM 2008 7 7 2008UALA02808 1 20080515 A 3350 2012120131A CHARGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 533UA 25073 EMERGENCY EXIT LIGHTS OUT AT DOOR 2L (3EA) AND 1 EA FWD OF DOOR 2R. REPLACED BATTERY PACK AND CHARGER AT DOOR 2L. OP C HK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080707 NM 2008 7 7 USAA920081083 1 20080514 A 2560 P4010021 BATTERY BOEING 767 7672B7ER 1385107 NM FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 MIA - EEL - C4 CHECK - FORWARD FLIGHT ATTENDANT POSITION 3 FLASHLIGHT BATTERY WEAK. REPLACED FORWARD FLIGHT ATTENDANT P OSITION 3 FLASHLIGHT BATTERY IAW B767 AMM 25-60-00. 2 L 7 2 4F RT A1NM 20080707 NM 2008 7 7 SB08031 1 20080519 A 3350 1012721 LIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 450UW 24933 CLT - MAINTENANCE REPORTED THE SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 11D INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 11D. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20080707 SO 2008 7 7 C2XA08RI074 1 20080516 A 2530 500064001 COFFEEMAKER EMB 145 EMB145EP 3260221 SO GALLEY MALFUNCTIONED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 14945 145049 FLIGHT 2404 - EWR - FLIGHT CREW REPORTED COFFEEMAKERS EMITTING BURNING SMELL WHEN TURNED ON. EWR MX PERFORMED OPERATION AL CHECK OF BOTH COFFEEMAKERS IAW EMB 145 VCMM 25-30-39 SUCCESSFULLY AND COULD NOT DUPLICATE BURNING SMELL. NO ABNORMAL ITIES WERE FOUND. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20080707 NM 2008 7 7 HNAA0800166 1 20080513 A 3350 OL3071BPEGPL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 942HA 163 EMERGENCY EXIT SIGN OVER MAIN CABIN DOOR HAS SEVERAL LAMPS INOP. REMOVED INOP LAMPS AND REPLACED WITH NEW. OPS CHECK G OOD. 2 H 7 2 4T RT A13NM 20080707 NM 2008 7 7 ASAA0852970 1 20080517 A 4990 38007021 APU BOEING 737 737890 1384527 NM OIL CONSUMPTION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 584AS 21337 35682 APU OIL COMSUMPTION INDICATE ALERT. STRIP AC FROM ETOPS SERVICES INSP, APU INTAKE EXHAUST AND APU AREA, NO OIL LEAKS NO TED AT THIS TIME. AC RESTRICTED FROM ETOPS UNTIL NEW APU OIL COMSUMPTION RATE IS CALULATED. INSPECTED APU, APU OIL LEV EL FULL CONSUMPTION FOR APU .0, THIS REMOVES TOP DEFFERAL FOR APU OIL USED. 2 L 7 2 4F RT A16WE 20080707 NM 2008 7 7 ASAA0842972 1 20080501 A 5755 SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 RIGHT WING NR 7 SPOILER HAS SEVERAL DENTS ON UPPER SURFACE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER & BONDED I AW B737 499 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080707 EU 2008 7 7 2008UALA02838 1 20080516 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 446UA 834 FOUND CORROSION ON FLOORBEAM ITEM 235. MAJOR REPAIR ACCOMPLISHED, REPLACED FLOORBEAM 235. 2 L 7 2 4F 4 F RT A28NM E40NE 20080707 NM 2008 7 7 2008UALA02848 1 20080517 A 5310 6520722076 DOOR FRAME BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 910UA 25254 FWD CARGO PIT DOOR CUTOUT FWD FRAME HAS DAMAGE UNDER LOWER STOP FITTING. MAJOR REPAIR ACCOMPLISHED: REPLACED FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 20080707 NM 2008 7 7 2008UALA02851 1 20080518 A 3397 WIRE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS MISINSTALLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 365UA 24534 WHEN EMERGENCY EXIT LIGHT SW IS SELECTED ' ON' THE 'ANTI-ICE' MASTER CAUTION IS ILLUMINATED INSTEAD OF 'OVERHEAD'. FOUN D WIRES SWAPPED ON RIGHT SIX PACK. CORRECTED PER WDM33-18-21. SYSTEM OPS CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 20080707 EU 2008 7 7 2008UALA02859 1 20080518 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 494UA 1840 GOUGE FOUND JUST BELOW AND FWD OF O2 SVC ACCESS DOOR ON LEFT SIDE OF FUSELAGE AT FRAME 13, BETWEEN STRINGERS 21 AND 27, 3 INCHES LONG AND .015 INCH DEEP. MAJOR REPAIR ACCOMPLISHED, INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 20080708 NM 2008 7 8 08FDEA01940 1 20080521 A 5320 652954863 PAN BOEING 727 727200 138407E NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 AFT MAIN DECK FLOOR DITCHING PAN ASSY IS CRACKED WITH INTERIM / DISBONDED. COMPOSITE REPAIR, BS 1176 - 1183, RBL 27-37, WL 208. REMOVED CRACKED DITCHING PAN. FABRICATED NEW DITCHING PAN, HEAT TREATED TO T-6 CONDITION, TREATED AND PRIMED, AND INSTALLED. REF SRM 51-30-2 PG 5, 51-20-021 PG 7 AND DWG 65-29548 THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080708 NM 2008 7 8 2008UALA02865 1 20080518 A 5320 STRAP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 305UA 23666 THE FOLLOWING CRACKS WERE AT VERTICAL STRAP STA 348 STR 16L, INTERCOSTAL CLIP STA 360 STR 11L, INTERCOSTAL CLIP STA 294. 5 STR 11L AND INTERCOSTAL WEB STA 294.5 STR 11L. 2 L 7 2 4F 4 F RT A16WE E2GL 20080708 2008 7 8 2008UALA02895 4 20080519 A 2565 7A146913 BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EVAC SLIDE LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 193UA 26890 LOW BOTTLE. REPLACED SLIDE OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 2008UALA02917 1 20080520 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 4J FWD LIGHT ASSY. FOUND LOOSE CONNECTION. SECURED LIGHT ASSEMBLY OP CHECKED GOO D. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 MWEA080076 1 20080521 A 2612 473465 CONTROL UNIT BOEING 717 717200 1383700 NM RT ENGINE MALFUNCTIONED A MWEA K NONE N FALSE WARNING CR CRUISE 1 GL 13 910ME 55174 AT 35,000 FEET RIGHT FIRE DETECTOR FAIL CAME ON INTERMITTENTLY. LIGHT WOULD COME ON FOR NO LONGER THAN 2 SECONDS, THEN GO OFF. REMOVED AND REPLACED FDCU FOR RIGHT ENGINE. 2 L 7 2 4F TR A6WE 20080708 NM 2008 7 8 DHL2008764510 1 20080520 A 5320 SHEAR WEB BOEING 727 727264 138408M NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 DENT AND PUNCTURE HOLE ON MAIN CABIN SHEAR WEB BS 1140 RBL 24. CUT OUT DAMAGED AREA AT SHEAR WEB RBL 24 BS 1140 (2 EACH ) 3/4 INCH BY 3/4 INCH AND 1 INCH BY 1 INCH IAW B727 SRM 51-40-2 FIG 1. FAB DOUBLER REPAIR WITH 7075-T6 .071 INCH SIZE : 9 INCH BY 7 INCH AND PO 9006522 IAW B727 SRM 57-10-2 FIG 7 AND 51-40-2. 2 L 7 3 4F A3WE 20080708 NM 2008 7 8 DHL2008764516 1 20080521 A 5347 SEAT TRACK BOEING 727 727264 138408M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 CORROSION ON MAIN CABIN SEAT TRACK BS 1110-1130 LBL 45. REMOVED CORRODED SEAT TRACK FROM BS1110 TO 1137 LBL 45 FOUND O UT OF LIMITS IAW B727 SRM 51-30-2 ZND 53-10-1 FIG 3. FAB NEW SECTION WITH BAC 1520-792-7178-T6 DIM. 2'3" AND P.O. 62951 13 IAW B727 SRM 53-10-5 FIG 1. 2 L 7 3 4F A3WE 20080708 EA 2008 7 8 COMA0860243 1 20080512 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 868CA 7427 DURING HMV 4 CHECK, NDT INSPECTION FOUND THE REAR PRESSURE BULKHEAD CRACKED AROUND LINTEL FITTING. DAMAGED PORTION OF W EB CUT OUT AND REPAIRED DOUBLER PER REO 601R-53-61-1230. 2 L 7 2 4F RT A21EA 20080708 EA 2008 7 8 COMA0860252 1 20080521 A 5320 601R332372 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 32939 7050 WHILE PERFORMING TASK CARD CRJ-2-122006, SPECIAL DETAILED INSP OF THE WINDSHIELD CENTER POST AND BULKHEAD AFT POST AT FS 202.75, FOUND LOWER RT POST FITTING TO BE CRACKED. REPLACED FITTING IAW CRJ SRM 51-42-21 PGS 1-21. 2 L 7 2 4F RT A21EA 20080708 WP 2008 7 8 ARWA20080501 1 20080516 A 7110 COWLING DOUG DC10 DC1030F 3023504 WP NR 3 ENGINE DENTED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 29 478CT 47819 NR 3 ENGINE NOSE COWL LIP HAS A DENT AT 5 O'CLOCK POSITION. TRANSFERRED TO CARRY-OVER ITEM NR 7584 IN ACCORDANCE WITH A RROW CARGO GMM 5-08-1 AND EO NR AS11722 FOR TRACKING OF DENT. 2 L 7 3 4F RT A22WE 20080708 NM 2008 7 8 DL757080862 1 20080612 A 5320 ANGLE BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 AFT CARGO PIT STA 1360-1380 WEB "L" ANGLE BETWEEN S 27R AND 26R CORRODED. REPLACED "L" ANGLE IAW SRM 51-10-01 AND 53-60 -04. 2 L 7 2 4F RT A2NM 20080708 NM 2008 7 8 DL757080833 1 20080504 A 3610 212N30706 DUCT BOEING 757 757232 1384965 NM WING CRACKED A DALA B EMER. DESCENT G MULTIPLE FAILURE CL CLIMB 1 SO 27 610DL 22817 AT FLT LVL 240 WITH ENGINE AND WING ANTI-ICE ON LEFT ENG BLEED LIGHT ILLUMINATED. FOLLOWED QRH SHUT BLEED SW OFF. OPEN ED ISOLATION VLV AT FLT LVL 260 RIGHT ENGINE BLEED LIGHT ILLUM. CABIN PRESSURE CLIMBED THROUGH 10K DEPLOYED MASKS. DEC LARED EMERGENCY INTO ORF. MTC FOUND SEAT ROWS 26 AND 27 DEF MASKS DID NOT DEPLOY. ALSO FOUND AFT RT LAV MASK DID NOT D EPLOY. MX HAS FOUND A DUCT IN THE UNDERWING SECTION CRACKED. 2 L 7 2 4F RT A2NM 20080708 EU 2008 7 8 2008UALA02695 1 20080508 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 451UA 865 SEAT 8A EMERGENCY LIGHT INOP. 2 L 7 2 4F 4 F RT A28NM E40NE 20080708 NM 2008 7 8 200805221 1 20080521 A 2120 UNKNOWN EMB ERJ170 ERJ170100SE 3260406 NM CABIN ODOR A UHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 11 657RW 17000115 FLIGHT 7553 DEN TO YEG CREW REPORTS STRONG SMELL OF ELECTRICAL SMOKE AT PUSH TIME. PASSENGERS WERE DEPLANED. MAINTENAN CE COULD NOT DUPLICATE SMOKE SMELL. ANOTHER AC CART WAS HOOKED UP TO THE AIRCRAFT AND NO FURTHER DISCREPANCIES WERE NOT ED. 2 L 7 2 4F RT A56NM 20080710 NM 2008 7 10 DLM90080735 1 20080419 A 5310 5912494501 DOOR FRAME DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 FWD CARGO DOOR CUTOUT LOWER JAMB CORRODED FS 370 TO 427. REPAIRED FWD CARGO DOOR JAMB, IAW MD80 SRM. 2 L 7 2 4F RT A6WE 20080710 NM 2008 7 10 AALA200801115 1 20080427 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 191AN 32385 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080710 NM 2008 7 10 R61A200800008 1 20080521 A 2750 FLAP EMB ERJ170 ERJ170200LR 3260121 NM WING MALFUNCTIONED A R61A O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 125HQ 17000202 CREW REPORTED FLAP FAIL MESSAGE ON EICAS DURING DESCENT. CREW DECLARED EMERGENCY FOLLOWED QRH PROCEDURE AND LANDED WITH OUT INCIDENT. MAINTENANCE WAS DISPATCHED TO AIRCRAFT. RESET THE SF. ACE AND CLEARED INHIBITS. SYSTEM OPERATIONAL CHE CK GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A56NM 20080710 NM 2008 7 10 2008UALA02809 1 20080514 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 539UA 25223 EEL EXIT SIGN ON LAV-A WIRES DAMAGED & CRACKED. UNKNOWN DAMAGE TO WIRING. REPAIRED WIRES ON EEL EXIT SIGN ON LAV A, OP S CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080710 NM 2008 7 10 UPS08652308 1 20080521 A 2761 1542615 CAP BOEING 767 76734AF 1385212 NM SPOILER ACTUATOR CRACKED A IPXA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 01 319UP 27758 INSPECTION TYPE:N/A ATB - AFTER TAKEOFF RECEIVED CTR HYD QTY LIGHT FOLLOWED BY LOSS OF CENTER HYD PRESSURE. QTY INDICAT ED .08 IN CENTER SYSTEM. FOUND NR 3 SPOILER ACT LEAKING FROM FILTER CAP. REPLACED NR 3 SPOILER PCA FILTER CAP AND PACK ING. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 BB08097 1 20080525 A 2750 TRANSMISSION BOEING 757 757225 1384959 NM T/E FLAP MALFUNCTIONED A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 917UW 22193 CLT FLT 1075 EN-ROUTE PHL TO CLT. ON APPROACH, A TRAILING EDGE FLAP DISAGREE EICAS MESSAGE WAS INDICATED. ALSO, THE TRAILING EDGE FLAPS STAYED AT 20 DEGREES WITH THE FLAPS SELECTED TO 25 DEGREES. THE CREW PERFORMED A GO-AROUND, AND THE N COMPLETED THE QRH CHECKLIST. AN ALTERNATE EXTENSION OF THE FLAPS TO 30 DEGREES WAS ACCOMPLISHED, WITH NO ROLL FELT. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. THE FLAPS RETRACTED NORMALLY AFTER LANDING. MAINTENANCE RESET TRIPPED OVER LOAD INDICATOR ON THE NUMBER SIX, RIGHT HAND OUTBOARD FLAP TRANSMISSION. FLAPS OPERATIONALLY CHECKED OK. ALSO, BITE CH ECKED THE FSEU. NO FAULTS FOUND. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 20080714 EU 2008 7 14 SA08038 1 20080526 A 5200 SEAL AIRBUS A319 A319112 3930323 EU DETERIORATED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 702UW 0896 MSY, FLIGHT 1888, MSY-PHL - THE FLIGHT RETURNED TO MSY DUE TO HEAVY AIRCRAFT MAINFRAME VIBRATION. THE CAPTAIN ADVISED T HAT ON TRANSITION FROM FLIGHT LEVEL 24000 TO 25000 THE AIRCRAFT BEGAN TO VIBRATE AND DECIDED TO RETURN TO MSY FOR INSPEC TION. MAINTENANCE REPLACED FIVE DOOR SEALS IN WING/BODY FAIRING AND TIGHTENED LOOSE FAIRING SCREWS. 2 L 7 2 4F RT A28NM 20080714 EU 2008 7 14 08FDEA02314 1 20080618 A 5730 A5797130000100 SKIN AIRBUS 310 A310203 3930313 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING O/B FLAP UPPER MAIN SKIN UNDER RUB STRIP AT FLAP TRACK NR 4 MEASUR ING 4 INCH BY 5.7 INCH. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT REPAIR ON LEF T WING O/B FLAP UPPER MAIN SKIN UNDER RUB STRIP AT FLAP TRACK NR 4 IAW FEDEX EA6-5750-121291. THIS IS AN APPROVED REPAI R AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080714 EU 2008 7 14 08FDEA02317 1 20080618 A 5730 A5797130100100 SKIN AIRBUS 310 A310203 3930313 EU ZONE 600 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RIGHT WING O/B FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN FLAP TRACK NR 5 TO RIB 11 AND 1.4 INCH FWD OF REAR SPAR MEASURING 13.6" BY 4.3". REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REP AIR AND INSTALLED AN APPROVED REPAIR ON RIGHT WING O/B FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN FLAP TRACK NR 5 TO R IB 11 AND 1.4 INCH FWD OF REAR SPAR IAW FED EX EA6-5750-121299. THIS IS AN APPROVED REPAIR AND IS A RESULT OF AGING AIR CRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080714 WP 2008 7 14 08FDEA02066 1 20080530 A 5720 ANB720311 STIFFENER DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 LEFT MLG WHEEL WELL; LEFT WING INBD WEB; 4TH ANGLE AFT OF THE MLG CUTOUT IS CRACKED. REMOVED STIFFENER IAW DC/MD-10 S RM 51-35-01 AND 51-33-01; VOL II. MATERIAL ID FOR THE STIFFENER 7075-0, 0.040 PO 606256.4. FABRICATED STIFFENER IAW D AC DWG ANB 7203, REV "BA". ALODINED; PRIMER AND PAINTED IAW DC/MD-10 SRM 51-21-01, PGS 21-24 AND 51-21-02; VOL II. INS TALLED STIFFENER IAE DC/MD-10 SRM 51-35-01; AND 51-33-01; VOL II. 2 L 7 3 4F RT A22WE 20080714 2008 7 14 08FDEA02376 4 20080622 A 3418 2566A30 AOA BOEING 727 727227 1384078 NM DAMAGED A FDEA C ABORTED TAKEOFF N FALSE WARNING AP APPROACH 1 CE 21 240FE 1 1 20978 STALL WARNING ACTIVATED AT ROTATION. AIRCRAFT FLYING NORMALLY. STAYED ON UNTIL CIRCUIT BREAKER PULLED. AMBER WINDSHE AR LIGHT CAME ON. REMOVED AND REPLACED AOA VANE AND SYSTEM OPS CKS NORMAL IAW 727 M/M 34-18-051-4 AND REINSTALLED S/OS HAND MIKE AND BOOM MIKE AND COAT HANGERS AND LIFE VEST PREVIOUSLY FOM, ALL ASSOCIATED ITEMS OPS CKS NORMAL 727 M/M 23-10 -00. OK TO CONTINUE. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 08FDEA02377 1 20080623 A 5315 149N713094 FLOORBEAM BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 LT FUSELAGE FWD OF BS900 SUPPORT ANGLE HAS SURFACE CORROSION. CHORD REMOVED AND REPLACED IAW B757-200 SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 08FDEA02381 1 20080623 A 5713 ARB29323 STRINGER DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 RIGHT WING LEADING EDGE STRINGER AT XOS 672 FOUND CRACKED OFF. REPAIR CARRIED OUT AS PER EA 1-5720-122505, REPAIR CLASS IFIED MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080714 NM 2008 7 14 DL757080781 1 20080527 A 5411 012N804237 FITTING BOEING 757 757232 1384965 NM NR 2 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 DURING ACCOMPLISHMENT OF THE SIP MOD PER S/B 757-54-0034 REV 1, THE NR 2 PYLON MID SPAR FITTING UPPER HORIZONTAL TANGE W AS MISDRILLED IN A FORWARD MOST HOLE LOCATION. THE FINAL CLEANUP SIZE HOLE WAS 0.704". A BUSHING AND RETENTION WASHER WERE INSTALLED AS A REPAIR. AD 2003-18-05 APPLIES. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 DHL2008764519 1 20080522 A 5730 SKIN BOEING 727 727264 138408M NM LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 SKIN DAMAGE ON LT WING T/E AT NR 2 SPOILER NR 3 HINGE CUTOUT. ROUTER OUT SKIN AT LT WING T/E NR 2 SPOILER NR 3 HINGE CU TOUT FOUND OUT OF LIMITS IAW B727 SRM 51-10-1 AND 57-20-1 FIG 2. FAB DOUBLER REPAIR WITH 7075-T6. DIMENSION: 4" X 7" AN D PO 9006522 IAW B727 SRM 57-30-04 FIG 10. 2 L 7 3 4F A3WE 20080711 NM 2008 7 11 DHL2008764523 1 20080525 A 5230 HINGE BOEING 727 727264 138408M NM CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C-CHECK, EXTERNAL FUSELAGE BS 650 MCD AFT HINGE SEGMENT HAS AFT 2 LOBES WITH SMALL CRACKS. REMOVED AND REPLACE D MCD STA 650 AFT HINGE SEGMENT IAW AEI B727 M/M CH 52 PGS 17-20 P/N MS20001-16-7200 PO 9006913. 2 L 7 3 4F A3WE 20080714 EA 2008 7 14 HNAA0800180 1 20080524 A 2720 XD4N RELAY DHAV DHC8 DHC8311 1386006 EA RUDDER INOPERATIVE A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 331EN 279 FIVE SECS AFTER TAKEOFF RUDDER FULL PRESSURE, NR 2 RUDDER HYD CAUTION LIGHT ILLUMINATED. BOTH NR 1 AND 2 HYD PRESSURE A ND QTY REMAINED NORMAL. AIRCRAFT RETURNED TO FIELD. REMOVED AND REPLACED RELAY 2721-K1. 2 H 7 2 4T RT A13NM 20080714 NM 2008 7 14 NOCA04308 1 20080526 A 5315 5565025 FLOORBEAM BOEING 767 76739H 1385311 NM FUSELAGE CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 760NA 26257 STA 1480 FLOORBEAM IS CORRODED THRU AT APPROXIMATELY RBL 54-60 AND VARIOUS SPOTS TO RBL 81. ACCOMPLISHED STA 1480 RIGHT O/B FLOORBEAM REPAIR IN ACCORDANCE WITH SRM 53-00-51. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 UPS08652339 1 20080513 A 5330 SKIN BOEING 767 76734AF 1385212 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 302UP 27240 INSPECTION TYPE:N/A CUSTOMER REQUEST - CLARIFY PREVIOUS REPAIR AND C/OUT PERMANENT REPAIR ON FX SKIN BETWEEN BS 654+100 AND BS 654+121 AT STR 19L AS PER UPS EO B767-5330-28779-A AND BOEING MSG 1-781623252. FX STA 654+97 TO STA 654+131.5 BE TWEEN STR 18L-20L AREA SKIN REPAIRED STA 654+110 AND STA 654+121 AT STR 19L TEAR STRAP REPAIRED AS PER RS R53-30-36014. 4EA SHEAR TIE AND 2EA TIE CLIP REPLACED AND INSTALLED AS PER RS R53-30-36014. THIS REPAIR WILL BE CLASSIFIED AS CAT B. REPEAT INSP IS REQUIRED AS PER UPS EO B767-5330-28779-B. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 DL75E080874 1 20080612 A 2913 291702437 PUMP BOEING 757 7572Q8 1384972 NM HYD SYSTEM FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 712TW 27624 EICAS - L HYD ENG PUMP- WHEN LEFT ELEC PUMP IS TURNED OFF THE LEFT HYD SYSTEM LOSES PRESSURE. RUDDER RATIO EICAS MSG AF TER ABOUT 15 MINUTES. LT HYD SYSTEM OVERHEAT. SHUT DOWN LEFT ENGINE. LEFT ENG EMERGENCY HANDLE PULLED/ENG HYD PUMP SW ITCH OFF/CTR RESERVOIR HEAD PRESS BLEED HYD SERVICE DOOR OPEN. PRESS FILTER AND CASE DRAIN REMOVED FOR INSPECTION LT EN G PUMP REMOVED. CHECKED MAIN PRESSURE FILTER FOR METAL, NO METAL FOUND. REPLACED FILTER AND SAFETIED. REPLACED NR 1 EDP PRESSURE AND CASE DRAIN FILTERS AFTER FLUSHING SYSTEM. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 ASAA0843099 1 20080609 A 5310 65C327747 BEAM BOEING 737 7374Q8 138447Q NM BS 616 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 LT SIDE BS616 STUB BEAM CHORD CRACKED AT FASTENER HOLE. REPAIRED IAW EO5310 02528 SECTION 5. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 DLM90080787 1 20080520 A 5310 5936038501 DOOR FRAME DOUG MD90 MD9030 3023690 NM AFT CARGO CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 AFT CARGO BAY LOWER DOOR JAMB BEAM CORRODED BETWEEN STA 1212 AND 1269 LONGERON 28R. REPAIRED AFT CARGO LOWER JAMB BEAM, IAW DELTA ER/A 468149-14, REV ORIG DATED 05MAY08. 2 L 7 2 4F RT A6WE 20080714 NM 2008 7 14 F3LA200800279 1 20080523 A 3397 BR8164005 CONNECTOR AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CABIN DISCONNECTED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 905FR 28 1583 DURING C5 C CHECK INSPECTION NOTED SEAT ROWS 9 ABC AND 10 ABC EMERGENCY PATH LIGHTS ARE INOPERATIVE. MAINTENANCE TROUBL ESHOT EMERGENCY LIGHTS AND FOUND CONNECTOR DISCONNECTED ON SIDEWALL. MAINTENANCE RE-CONNECTED CONNECTOR AND OPERATIONAL CHECKED GOOD. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080714 NM 2008 7 14 KCSA081261 1 20080527 A 5412 BULKHEAD BOEING 747 7472B4B 138481B NM NR 1 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 1 ENG FWD MOUNT HANGER CHORD CHAFED ON O/B SIDE NAC STA 128.95. 2 L 7 4 4F RT A20WE 20080714 NM 2008 7 14 SWAA083418 1 20080622 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083412 1 20080622 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083420 1 20080622 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 330, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083443 1 20080622 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 21L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083422 1 20080621 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083474 1 20080623 A 5320 6517582 BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083432 1 20080622 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SKIN P ER EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083437 1 20080620 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 DURING SCHEDULED HC2 CHECK, FOUND LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 133. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083363 1 20080618 A 5330 6518420 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083356 1 20080618 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 13R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083071 1 20080606 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 300, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083174 1 20080610 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 DL757080806 1 20080531 A 5320 CHANNEL BOEING 757 757232 1384965 NM BS 1720 S21L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 AFT CARGO STA 1720 STR 21L IS CORRODED/SPLICED IN NEW HAT CHANNEL PER SRM 53-00-03 FIG 201 REF NR78980200001. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 DL757080810 1 20080530 A 5313 STRINGER BOEING 757 757232 1384965 NM BS1710 S26L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 STR 26L AT STA 1710 WAS FOUND TO HAVE CORROSION UNDER STRINGER. REPAIRED PER SRM 53-80-08 FIG 201. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 08FDEA02415 1 20080624 A 5311 6516525 FRAME BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 FIGURE "8" HOLE ON STA 760 FRAME I/B OF STR 5L. FABRICATED REPAIR PART (CHANNEL) FOR FRAME STA 760, STRINGER 5L, REF SR M 51-40-03. HEAT TREATED, TRACKING NR 208-06-060, TREATED AND PRIMED AND INSTALLED REF SRM 51-10-2 PG 1-7, 51-30-2 PG 2 , 51-40-03 FIG 1, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080714 EU 2008 7 14 08FDEA02392 1 20080623 A 5330 A53978152200100 SKIN AIRBUS 300 A300F4605R 3930327 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 FUSELAGE SKIN HAS GOUGES AT THE AFT CARGO DOOR FRAME 64 BETWEEN STRINGER 27R AND 28 R. BLENDED GOUGES AT THE AFT CARGO DOOR FRAME 64 BETWEEN STRINGER 27R AND 28R. ORIGINAL THICKNESS ARE 0.236 AND 0.315 IAW A300-600 SRM 53-17-12. REMAININ G THICKNESS IS 0.214 AND 0.214 AND 0.285. FOUND TO BE IN LIMITS IAW A300-600 SRM 53-10-12. ALODINED AND PRIMED IAW A30 0-600 51-40-10. PAINTED IAW A300-600 SRM 51-40-12. 2 L 7 2 4F RT A35EU 20080714 WP 2008 7 14 08FDEA02128 1 20080603 A 5347 NFA602215 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 UPPER CARGO COMP SEAT TRACK HAS PITTING CORROSION IN THE BOTTOM OF THE TRACK LOCATED AT FS 760; LBL 9. REMOVED AND REPL ACED THE SEAT TRACK IAW DC/MD-10 SRM 51-31-01. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01; VOL II. FABRICATED NEW S EAT TRACK IAW DC/MD-10 SRM 53-70-00, VOL I; FIG 2; SHEET 2. 2 L 7 3 4F RT A22WE 20080714 NM 2008 7 14 08FDEA02082 1 20080602 A 5730 ARB74024 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 624FE 48443 CRACK FOUND QUANTITY 13 FASTENER HOLES ON RT SIDE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUT-OUT BETWEEN STA XORS=683.4 AND XORS=713.6 RT SIDE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUT-OUT BETWEEN STA XORS=683.4 AND XORS=713.6 13 FASTENE R HOLES CRACKED. AREA REPAIRED AS PER FEDEX EA 1-5710-122471- AD 2007-07-4- WINGS- RT LOWER SKIN PLANK CUT OUT AT 636AB , THIRTEEN ACCESS DOOR ATTACHMENT BORES WITH CRACK INDICATIONS PSE 57.23.01 ALI- REPAIR. REPAIR CLASSIFIED AS MINOR PER FEDEX GMM 6-2-100. REPETITIVE INSPECTION TO BE ACCOMPLISHED NLT EVERY 2000 FLIGHT CYCLES, STARTING FROM 13,324 CSN. 2 L 7 3 4F RT A22WE 20080714 EU 2008 7 14 08FDEA02095 1 20080602 A 5320 C2311819 BRACKET AIRBUS 300 A300F4605R 3930327 EU MLG FAILED A FDEA O OTHER J WARNING INDICATION LD LANDING 1 CE 21 668FE 772 REPEAT WRITE-UP- DURING FINAL APPROACH PHASE, LEFT LANDING GEAR WOULD NOT INDICATE DOWN AND LOCKED AFTER GEAR SELECTED DOWN. RECYCLED GEAR HANDLE WITH SAME RESULT, COMPLIED WITH ALL ECAM AND QRH ITEMS. TRIED SIDE SLIPS AFTER MANUALLY LOW ERING GEAR. NO HELP AFTER 20 MIN IN PATTERN TRYING TO TROUBLESHOOT INDICATION CHANGED TO DOWN AND LOCKED ON ITS OWN. O RDERED DOWN LOCK (SIDE BRACE ACTUATOR) DUE TO FAT STARTED AFTER CHANGING FOR LEAKING ACTUATOR. REMOVED AND REPLACED LT GEAR BRACE STRUT CYLINDER IAW A300 AMM 32-31-55-4. OPS AND LEAK CHECKS GOOD. PERFORMED EXT AND RETRACTION IAW A300 AMM 32-31-00. OPS CHECKS GOOD PERFORMED MANUAL EXT AND RETRACTION. OPS CHECKS GOOD RESET MANUAL EXT IAW. 2 L 7 2 4F RT A35EU 20080714 EU 2008 7 14 08FDEA02438 1 20080625 A 5313 A53610792731 LONGERON AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 FR12-FR12A Y1456 LONGERON FOR SUPPORTING OF MAIN DECK FLOOR CORRODED. REPAIR THE DAMAGE PER EA 6-5310-117358. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 MWEA080080 1 20080526 A 5210 HOOK BOEING 717 717200 1383700 NM PAX DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 914ME 55177 FORWARD PASSENGER DOOR HAS DRILLED TOOLING MARK DAMAGE IN THE RADIUS ON THE AFT SIDE OF THE DOOR HOLD OPEN HOOK. FABRIC ATED AND INSTALLED DOUBLER. 2 L 7 2 4F TR A6WE 20080714 EU 2008 7 14 08FDEA02315 1 20080618 A 5730 A5797130100000 SKIN AIRBUS 310 A310203 3930313 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING O/B FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB 3 AND FLAP TR ACK NR 3 MEASURING 4" BY 6". REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED APPROVED REPAIR ON LEFT WING O/B FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB 3 AND FLAP TRACK NR 3 IAW FEDEX EA6-5750-121298. THIS I S AN APPROVED REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 08FDEA02380 1 20080623 A 5313 A6A7003501 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 CRACK INDICATION FOUND DURING X-RAY INSPECTION AT STATION 6-100, LONGERON-3 RIGHT FORWARD SECTION EDGE. CRACK LENGTH AP PROXIMATELY 0.3 INCH. REPAIR CARRIED OUT AS PER EA 1-5310-122735, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080714 NM 2008 7 14 DL757080779 1 20080528 A 5412 311N32701 BULKHEAD BOEING 757 757232 1384965 NM NR 1 PYLON WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 THE NR 1 PYLON AFT BULKHEAD O/B VERTICAL FLANGE AT NAC STA 203 WAS FOUND WITH WEAR. THIS WEAR WAS CAUSED BY THE RUBBING OF THE PYLON AFT FAIRING UPPER SPAR FLANGE. THIS WEAR WAS FOUND DURING ACCOMPLISHMENT OF THE SIP MOD, S/B B757-54-0034 . REPAIR WAS ACCOMPLISHED WITH INSTALLATION OF A GUSSET AND FILLER. AFTER BLENDOUT THE MAXIMUM WEAR DIMENSIONS WERE 1. 7" X 1.25" X 0.140" DEEP. AD 2003-18-05 APPLIES. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 DL764080778 1 20080527 A 3250 STEERING SYS BOEING 767 767432ER 1385134 NM NLG NOISY A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 845MH 29719 LOUD NOISE FROM E/E COMPARTMENT UNDER 1L F/A SEAT. FOUND NOSE LANDING GEAR STEERING METERING VALVE BYPASSING IN FULL RT TURN POSITION. DEPRESSURIZED CTR HYD SYSTEM AND RE-PRESSURIZED. EXERCISED NOSE GEAR STEERING SEVERAL TIMES AND NOISE WENT AWAY. NOSE GEAR STEERING OPERATION NORMAL PER AMM 32-51-00. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ET OPS. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 DLM90080777 1 20080526 A 3260 PROXIMITY SENSOR DOUG MD90 MD9030 3023690 NM RT MLG W/W MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 915DN 53395 AFTER T/O RAISED GEAR HANDLE AND RT GEAR UNSAFE LIGHT STAYED ILLUMINATED. REPLACED RT MAIN UP LATCH PROX SENSOR D1-25. PERFORMED GEAR SWING 3 TO 4 TIMES. ALL INDICATIONS CHECKED NORMAL. PROX SENSOR ALWAYS SHOWED FAR WITH ORIGINAL AND NE W PSEU. 2 L 7 2 4F RT A6WE 20080715 EU 2008 7 15 USAA920081224 1 20080603 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 652AW 25767 12887 0953 SAL-EEL-C7 CHECK - NR 6107582, SEAT ROWS 1R AND 2R EMERGENCY POWER SUPPLY UNIT IS INOPERATIVE. REPLACED AND FUNCTIONAL C HECKED THE EMERGENCY POWER SUPPLY UNIT AT SEAT ROWS 1R AND 2R IAW A320 AMM 33-51-38. (K) 2 L 7 2 4F RT A28NM 20080715 NM 2008 7 15 08FDEA02388 1 20080623 A 5311 FRAME BOEING 757 7572B7 1384964 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 906FD 27148 AFT CARGO COMPARTMENT LT STA 1460 S-26L, FRAME IS DENTED. CUT OUT DAMAGED AREA IAW SRM 53-00-01, FIG 201. NDT, HFEC IA W NTM 51-00-00, FIG 6, OF CUT OUT AREA. FABRICATED SPLICE ANGLE IAW SRM 53-00-07, MAT. 7075T6, .071 INCH C, BATCH NR 53 2681, PO NR MST 0023621 ON MAE TRAVELER NR T8/743564. COLD WORKED HOLES IAW SRM 51-40-00 AND 53-00-07. INSTALLED ALL R EPAIRS PARTS IAW SRM 51-40-02 AND 53-00-07. THIS REPAIR IS CLASSIFIED AS A CATEGORY "B" MAJOR REPAIR. INITIAL INSP OF REPAIR AT 37,500 FC AND REPEAT INSP. THEREAFTER AT 12,000 FC. 2 L 7 2 4F RT A2NM 20080715 EU 2008 7 15 08FDEA02390 1 20080623 A 5320 A5378193720200 FLOOR SUPPORT AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 THE CABIN CROSS S-TRACK IS DAMAGED AT FRAME 31; LBL 70". EVALUATED THE GOUGE; FOUND IT TO BE OUT OF LIMITS IAW FEDEX SR M 53-10-16; FIG 101. REMOVED ADAPTER TRACK IAW FEDEX SRM 51-40-21. LOCATED AND DRILLED THE NEW ADAPTER TRACK IAW FEDEX A300-600 SRM 51-40-47 P/N A5378193720200. INSTALLED THE NEW ADAPTER TRACK IAW FEDEX SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080711 NM 2008 7 11 UPS08652309 1 20080522 A 3242 26124121A BRAKE ASSY BOEING 767 76734AF 1385212 NM NR 8 BROKEN A IPXA D RETURN TO BLOCK K A FLUID LOSS FLAME/FIRE UK UNKNOWN 1 SO 01 304UP 27242 INSPECTION TYPE:N/A BTB - HYDRAULIC FLUID LEAK AND SMALL FIRE FROM BROKEN NR 8 BRAKE ASSY. REPLACED NR 8 BRAKE ASSY PER AMM 32-41-08-4. REMOVED BRAKE IS COMPLETELY BROKEN. NEW BRAKE OPERATION CHECKS GOOD. NR 8 MAIN WHEEL AXLE CONDITION IS GOOD. 2 L 7 2 4F RT A1NM 20080711 NM 2008 7 11 UPS08652319 1 20080515 A 5320 141T514622 STIFFENER BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 302UP 27240 INSPECTION TYPE:N/A MEC STA 246 RBL 10 FLOORBEAM STIFFENER CRACK. CRACK LENGTH .375 INCH. MEC STA 246 RBL 10 FLOORBEAM ATTACHED STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20080711 NM 2008 7 11 UPS08652320 1 20080513 A 5320 146T56515 SUPPORT BRACKET BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 302UP 27240 INSPECTION TYPE:C BULK CARGO STA 1580 LBL 75 FLOOR PANEL SUPPORT BRACKET CRACKED (1.375 INCH APPROX). BULK CARGO STA 15 80 LBL 75 FLOOR SUPPORT BRACKET ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20080711 NM 2008 7 11 UPS08M52312 1 20080513 A 5712 RIB DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C LEFT FIXED LEADING EDGE RIB STA XORS 917 CRACKED ON LWR FLANGE VIEWED WITH MIRROR. STOP DRILLED CRAC K, FABRICATED SHIM AND REPAIR ANGLE IAW MD-11 SRM 57-00-01, 51-21-01, AND DWG ARB2920. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 UPS08M52314 1 20080513 A 5730 STRAP DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C LEFT FIXED LEADING EDGE SKIN SPLICE STRAP CRACKED STA XORS 683. REMOVED, FABRICATED, AND INSTALLED S KIN SPLICE STRAP IAW MD-11 SRM 51-31-01, 51-33-01, AND DWG ARB3954. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 UPS08M52329 1 20080504 A 5321 SWP0785502 PANEL DOUG MD11 MD11F 3023600 NM MAIN CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C MAIN CARGO RCB PNL NR 5 HAS CORROSION 3 PLACES ON TOP FACE. LOCATED AND DRILLED REPLACEMENT PANEL IA W MD-11 SRM 51-31-01 AND INSTALLED ON EO MD11-5330-27218-B. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 UPS08M52331 1 20080507 A 5321 SWP0788501 PANEL DOUG MD11 MD11F 3023600 NM MAIN CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C MAIN CARGO RCB PNL NR 4 HAS CORROSION DAMAGE ON TOP FACE. LOCATED AND DRILLED REPLACEMENT PANEL IAW MD-11 SRM 51-31-01 AND INSTALLED ON EO MD11-5330-27218-B. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 UPS08M52332 1 20080505 A 5321 PANEL DOUG MD11 MD11F 3023600 NM MAIN CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C MAIN CARGO RCB PNL NR 12 HAS CORROSION ON TOP FACE. LOCATED AND DRILLED REPLACEMENT PANEL IAW MD-11 SRM 51-31-01 AND INSTALLED ON EO MD11-5330-27218-B. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 UPS08M52333 1 20080507 A 5321 SWP0786501 PANEL DOUG MD11 MD11F 3023600 NM MAIN CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C MAIN CARGO RCB NR 7 HAS CORROSION DAMAGE ON TOP FACE. LOCATED AND DRILLED REPLACEMENT PANEL IAW MD-1 1 SRM 51-31-01 AND INSTALLED ON EO MD11-5330-27218-B. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 AALA200801126 1 20080428 A 3397 WIRE BOEING 777 777223 1385213 NM CABIN EXPOSED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 792AN 30253 DFW - EMERGENCY LIGHT AT FORWARD GALLEY CLOSET BY LEFT NUMBER ONE DOOR HAS WIRES EXPOSED. RESECURED WIRE FOR EMERGENCY LIGHT AT FORWARD GALLEY CLOSET BY LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 WP 2008 7 11 AALA200801146 1 20080428 A 5312 5910130285 BULKHEAD DOUG DC9 DC983 3022083 WP FUSELAGE DEFORMED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 588AA 53251 TUL - AFT PRESSURE BULKHEAD WEB DEFORMED AT STATION 1338. AREA OF DISCREPANCY IS 45 INCHES BY 28.5 INCHES. REPAIRED BU LKHEAD DOME PER SRM 53 03 FIGURE 33 VIEW C ON BOTH SIDES OF AIRCRAFT PER ESO 80559. 2 L 7 2 4F RT A6WE 20080707 NM 2008 7 7 WRLA2008049 1 20080518 A 2530 CHILLER DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE CABIN MALFUNCTIONED A WRLA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 273WA 48519 KDFW/KATL: FORWARD CHILLER POPS C/B IN FLIGHT WITH ASSOCIATED ODOR OF ELECTRICAL SMOKE. REMOVED AND REPLACED FWD GALLE Y CHILLER, OPS CHECK SATISFACTORY PER MD-11 25-37-82. (A) 2 L 7 3 4F 4 F RT A22WE E24NE 20080707 SO 2008 7 7 C2XA08IA129 1 20080514 A 3397 7287580501 WIRE EMB 145 EMB145EP 3260221 SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14930 145011 IAH - DURING MAINTENANCE INSPECTION THE 2ND AISLE PATH LIGHT STRIP ON THE FLOOR WAS FOUND TO HAVE A BROKEN WIRE. MAINTE NANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20080707 NM 2008 7 7 HNAA0800162 1 20080502 A 3397 PIN DHAV DHC8 DHC8102 2809003 NM CONNECTOR LOOSE A HNAA O OTHER O OTHER LD LANDING 1 EA 07 336EN 336 WHILE APPLYING POWER ON T/O AND UPON LANDING ROLL EMERGENCY LIGHTS ILLUMINATED FOR ABOUT 5 SECONDS EACH TIME. FOUND PIN ON 3351-J1 CONNECTOR NOT LOCKED IN PLACE. LOCKED PIN IN PROPER POSITION. NO OTHER DEFECTS NOTED. 2 H 7 2 4T RT A13NM 20080707 NM 2008 7 7 2008UALA02850 1 20080518 A 2797 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE PFC DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 773UA 26929 THE PFC FAILS THE OPERATIONAL TEST. AFTER TROUBLE SHOOTING FOUND BAD CONNECTION. CLEANED NR 11 SPOILER ACTUATOR CONN. TEST PASSED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080708 WP 2008 7 8 UPS08852297 1 20080421 A 5720 3769968501 FITTING DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 LEFT WING CENTER L/E SLOT STRESS PANEL TO ROD END FITTING HAS 8 INCH CRACK AT OUTBOARD END. REMOVED AND REPLACED LT CENTER L/E FITTING IAW SRM 51-3-0 AND SRM 51-1- 24. 2 L 7 4 4F RT 4A25 20080708 WP 2008 7 8 UPS08852298 1 20080415 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 RIGHT FUSELAGE DENT IN SKIN FS 176.5 AND L26R. REPAIRED RIGHT FUSELAGE DENT AT FS 176.5 AND L26R IAW EO DC8-5330-26529D. 2 L 7 4 4F RT 4A25 20080708 NM 2008 7 8 HNAA0800168 1 20080513 A 3234 574205A SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM MLG MALFUNCTIONED A HNAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 07 911HA 17413 5425 034 AFTER DEPARTURE CYCLED GEAR UP, GEAR RETRACTED NORMALLY BUT ALL DOORS STAYED OPEN. CYCLED GEAR DOWN DOORS CLOSED NORMAL LY, RETRACTED GEAR AGAIN DOORS, REMAINED OPEN AGAIN. REMOVED AND REPLACED MAIN LANDING GEAR SELECTOR VALVE, OPS CHECKS GOOD IAW -8 MM 32-30-10. 2 H 7 2 4T RT A13NM 20080708 NM 2008 7 8 HNAA0800173 1 20080515 A 3230 692101 SEQUENCE VALVE DHAV DHC8 DHC8102 2809003 NM NR 1 MALFUNCTIONED A HNAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 07 911HA 57441 57441 034 UPON GEAR UP SELECTION NOSE AND MAIN GEAR STAYED LOCKED DOWN DUE TO THE FACT THAT THE GEAR DOORS WOULD NOT OPEN. REMOVE D AND REPLACED NR 1 MECHANICAL SEQUENCE VALVE IAW MM 32-10-41. 2 H 7 2 4T RT A13NM 20080708 WP 2008 7 8 08FDEA01937 1 20080521 A 5730 ARB087241 PANEL DOUG DC10 DC1010F 3022111 WP LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 567FE 46994 LEFT WING FUEL TANK PLATE / PANEL 534 CT; INTERIOR FLANGE HAS NUMEROUS AREAS OF CORROSION; NICKS & GOUGES. REMOVED DAM AGE FROM THE PANEL & FOUND IT TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00; VOL I; PG 217. MACHINED A NEW 534 CT PANEL IAW DAC DWG ARB0872, REV "AV". APPLIED ALODINE; PRIMER & PAINT IAW DAC DWG ARB0872, REV "AV" & DC/MD-10 SRM 51-21-02 ; VOL II. PART MARKED IAW FEDEX GMM 7-0-1001. FPI PER DPS 4.707 & DAC DWG ARB0872, REV "AV". NO CRACKS NOTED. 2 L 7 3 4F A22WE 20080708 NM 2008 7 8 08FDEA01941 1 20080521 A 7110 B277101704 DOUBLER BOEING 727 727200 138407E NM COWLING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 NR 3 ENG LOWER COWL, I/B SIDE EDGE, 3RD LATCH CUTOUT FROM FWD END, LOWER CUTOUT AREA, DOUBLER CRACKED OUT. REMOVED AND REPLACED DOUBLER, REF SRM 51-30-2 PG 2, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080708 NM 2008 7 8 2008UALA02863 1 20080518 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 FWD CARGO PIT STRINGER CLIP CRACKED AT BS 380 AND STRINGER S-22L. MAJOR REPAIR ACCOMPLISHED, REMOVED AND REPLACED DAMAG ED STRINGER CLIP WITH NEW. 2 L 7 2 4F 4 F RT A16WE E2GL 20080708 EU 2008 7 8 2008UALA02872 1 20080517 A 3530 9F4027507 OXYGEN BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 469UA 1409 FOUND PORTABLE OXYGEN BOTTLE LOW AT SEAT ROW 26 ABC. REPLACED O2 BOTTLE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080708 NM 2008 7 8 2008UALA02789 1 20080513 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 566UA 26670 EXTERIOR EMERGENCY LIGHT AT DOOR 2L INOP. LAMP INOP. RELAMPED LIGHT AT DOOR 2L. 2 L 7 2 4F 4 F RT A2NM E17NE 20080708 NM 2008 7 8 KCSA081255 1 20080522 A 5412 BULKHEAD BOEING 747 747246F 1384850 NM NR 1 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 NR 1 PYLON BULKHEAD NAC STA 221.90 "B" NUT HYDRAULIC PRESSURE LINE CHAFING ON BULKHEAD. 2 L 7 4 4F RT A20WE 20080708 NM 2008 7 8 DHL2008764507 1 20080520 A 5311 FRAME BOEING 727 727264 138408M NM FUSELAGE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C CHECK REF N/R 097896, 4 EACH TOOLING MARKS/GOUGES ON MAIN CABIN FRAME BS 700 BETWEEN S7-8L. REPAIRED IAW B72 7 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 MATERIAL 7075-O PO NR 9006027 HEAT TREATED FROM 7075-O TO 7075-T6 IAW FAS ENGINEER ING REPORT NR 2-37153 REV A DIMENSION 10 1/4 INCH BY 3 3/4 INCH. 2 L 7 3 4F A3WE 20080708 NM 2008 7 8 CALA0800515 1 20080602 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 STATION 440 BETWEEN S8R & S9R IS CRACKED. REPAIRED CRACK AT STATION 440 BETWEEN S8R AND S9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 CALA0800520 1 20080602 A 5311 146A1111 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 FRAME CRACKED AT STATION 727D BETWEEN S8L AND S9L. REPAIRED FRAME AT STATION 727D BETWEEN S8L AND S9L PER EC/RA 5310-04 777. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 CALA0800523 1 20080602 A 5311 143A1120 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 FRAME CRACKED AT STATION 480 BETWEEN S8R AND S9R. REPAIRED FRAME AT STATION 480 S8R AND S9R PER EC/RA 5310-04777. 2 L 7 2 4F RT A16WE 20080708 2008 7 8 DL76G080830 4 20080604 A 2565 101656306 SLIDE BOEING 767 7673P6 1385105 NM RT WING MISSING A DALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 27 154DL 25241 PASSING THRU FL210 AND LIGHT TURB GOT R WING SLIDE LIGHT. F/A AND PAX`S HEARD AIR NOISE AND ALSO SOMETHING HIT ACFT. ALL FLIGHT CONTROLS NORMAL. RETURNED TO ATL AND PERFORMED FLY-BY TO VERIFY NO SLIDE OR OTHER DAMAGE. UNEVENTFUL LDG. MTC IN PROGRESS. DAMAGE TO R INBD AFT FLAP, SLIDE COMPARTMENT AND SLIDE BOTTLE COMPARTMENT. INSTALLED PNL 196ER AND S LIDE PACK. BEGAN INST OF SLIDE BOTT AND DOOR LATCH CABLE ALSO MIDDLE AND AFT DOOR LATCH RODS. COMPLETED INSTALLATION O F SLIDE DOOR AND COMPONENTS ON RTN 7838 AD AND NRC 1-5. 2 L 7 2 4F RT A1NM 20080708 NM 2008 7 8 DL76G080831 1 20080604 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1605 30198 FOUND ON PDC/DRC, MISC LT SIDE EXTERNAL EMERGENCY ESCAPE PATH LIGHTS INOP. REPLACED M731 AND M733. L SIDE EXTERNAL EME RGENCY ESCAPE PATH LIGHTS OKAY. 2 L 7 2 4F RT A1NM 20080708 NM 2008 7 8 KCSA081256 1 20080522 A 5412 BULKHEAD BOEING 747 747246F 1384850 NM NR 3 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 NR 3 PYLON BULKHEAD NAC STA 221.90 B-NUT HYDRAULIC PRESSURE LINE CHAFING ON BULKHEAD. 2 L 7 4 4F RT A20WE 20080715 EU 2008 7 15 08FDEA02391 1 20080623 A 5347 A5378193620200 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 THECABIN CROSS SEAT TRACK IS GOUGED AT FRAME 32; LBL 70 INCH. EVALUATED GOUGE; FOUND IT TO BE OUT OF LIMITS IAW FEDEX A300-600 SRM 53-10-16; FIG 101. REMOVED ADAPTER TRACK IAW FEDEX A300-600 SRM 51-40-21. LOCATED AND DRILLED THE NEW AD APTER P/N A5378193620200 IAW FEDEX A300-600 SRM 51-40-47. INSTALLED THE NEW ADAPTER IAW FEDEX A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080715 WP 2008 7 15 08FDEA02143 1 20080604 A 5347 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 1481-1884 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 ON THE MAIN CARGO DECK FLOOR, THE SEAT TRACK FROM BS 1481 TO BS 1884; LBL 48L HAS MINOR NICKS AND SCRATCHES. 2 L 7 3 4F RT A22WE 20080715 WP 2008 7 15 08FDEA02278 1 20080614 A 2611 SMOKE DETECTOR DOUG MD10 MD1010F 3022112 WP CABIN FALSE ACTIVATION A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 570FE 47829 GOT CABIN SMOKE LVL 3 AND ASSOCIATED TONE ON CLIMB-OUT. LIGHT STAYED ON ABOUT 5 MINUTES. NR 7 SMOKE DETECTOR ILLUMINAT ED AT SAME TIME. DECLARED EMERGENCY AND RETURNED TO MEM. CREW STATED AT GATE THAT THEY HAD NO SMOKE INDICATION LIGHT ON OVERHEAD CARGO FIRE TEST PANEL. ONLY THE NR 7 SMOKE DETECTOR WAS ILLUMINATED. DEPINNED PLUGS AND INSP CRIMPS, CK'D GOOD. ALSO CK'D CONTINUITY OF ASSOC WIRING FROM MSC TO SMOKE DET'S NR 7 AND NR 9 (REF WDM 26-15-01 AND 26-14-02), ALL CK'D GOOD. OHMED DIODES R7-570 AND R7-572, BOTH CK'D GOOD. FOUND LOOSE SCREW INSIDE NR 7 SMOKE DET LAYING ON CIRCUIT CARD, COULD BE POSSIBLE CAUSE OF FAULT. 2 L 7 3 4F RT A22WE 20080715 EU 2008 7 15 08FDEA02320 1 20080619 A 5320 A53973085208 SILL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON AFT CARGO DOOR SILL BEAM REPAIR PERFORMED BY CUT OUT OF DAMAGED SILL BEAM AND REPAIR IAW SRM 53-17-18 PB 201, APPROVED BY RAS/DAHAM/4024836/2008 ISS A AND EA 6-5317-120050. 2 L 7 2 4F RT A35EU 20080715 EU 2008 7 15 08FDEA02322 1 20080619 A 5711 A57110431200 SPAR AIRBUS 300 A300B4622R 3930312 EU WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CRACKED FASTENER HOLE IN CENTER SPAR WEB C 44. REPAIR PERFORMED BY CUT OUT THE DOUBLER, ROTOTEST FOR CRACK FREE C ONDITION AND REAM UP UNTIL CRACK REMOVAL IAW RAS 70507029/021/2008 ISS A, APPROVED BY EA 6-5710-120043. 2 L 7 2 4F RT A35EU 20080715 NM 2008 7 15 08FDEA02328 1 20080619 A 5320 453N16069 ANGLE BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 SIDEWALL SUPPORT ANGLE FROM BS 1600 TO 1640, STR 23R HAS CORROSION. REMOVED AND REPLACED SIDEWALL SUPPORT ANGLE ASSY IA W B757-200 SRM 51-10-02 AND 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 08FDEA02332 1 20080619 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATIONS AT HOLE NR C (THIRD LAYER). REMOVED AND R EPLACED AS PER SRM 51-31-01, VOL.II. NEW FITTING FABRICATED AS PER EA 1-5300-122494, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 08FDEA02338 1 20080619 A 5343 ACA7017501 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 NOSE LANDING GEAR LEFT TRUNNION FITTING FOUND CRACKED. AREA TRIMMED OUT AND REPAIRED AS PER SRM 53-40-00, FIG.23, VOL.I . PER SRM 53-40-00, FIG.23, VOL.I, OPTION 2: REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1,500 LANDING INTERV ALS. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 08FDEA02346 1 20080619 A 5100 NONE BOEING 757 7572B7 1384964 NM NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 903FD 27124 ACCOMPLISHED BOEING SB 757-54-0035, R2, PARA. 3, PART 3, STRUCTURE CHANGES FOR THE NR 2 STRUT, EXCEPT STEO Q, PANEL 5, P ER FEDEX EA F-5450-108907, DATED 11 OCT 2007. COMPLIED WITH FEDEX EA F-5450-108907A, DATED 28 MAY 2008 ON W/C T F-5450- 108907A, WRI 54500172 AND BOEING SB 757-54-0035, PARA 3, PART 3, EXCEPT STEP Q, PANEL 5. ALSO COMPLIED WITH FEDEX EA F- 5450-110825, DATED 01/11/2007, WHICH IS A DEVIATION TO EA F-5450-108907A. SCHEDULE EO F-5450-7-5006 WIC PARTS 3 AND 4, AT 9000 FC OR 54 MONTHS, WHICHEVER OCCURS FIRST. 2 L 7 2 4F RT A2NM 20080715 EU 2008 7 15 08FDEA02347 1 20080619 A 5230 A2557381120200 ANGLE AIRBUS 300 A300F4605R 3930327 EU CARGO DOOR DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 675FE 789 AFT CARGO DOOR CUTOUT UPPER CLOSE OUT PANEL FWD END IS DAMAGED. REMOVED DAMAGED ANGLE IAW SRM 51-40-21. REMOVED DAMAGED AREA OF SEAL PLATE IAW SRM 51-71-30. REPAIRED THE SEAL PLATE IAW SRM 51-71-31. INSTALLED THE NAS ANGLE. 2 L 7 2 4F RT A35EU 20080715 NM 2008 7 15 08FDEA02304 1 20080618 A 5340 149N712436 TEE FITTING BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 SURFACE CORROSION FOUND ON LT FUSELAGE WING-TO-BODY FAIRING ATTACHMENT HOLES AT BS 820. CORROSION FOUND EXCEED LIMITS I N SRM 53-00-71 FIG 101 DETAIL VIII. REMOVED AND REPLACED LOWER TEE FITTING IAW SRM 51-40-02 REV 93. REPAIR IS CLASSIFI ED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 08FDEA02282 1 20080617 A 5230 6557204520 SKIN BOEING 727 727225 1384077 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 AFT CARGO DOOR LOWER FWD SKIN CRACKED CRACK ON EDGE OF SKIN (OUT OF LIMITS). REMOVED DAMAGED SKIN INSTALLED FILLER AND DOUBLER REPAIR REF SRM 52-00-3 PG 7-13, REPAIR CLASSIFIED AS A MAJOR. 2 L 7 3 4F A3WE 20080715 NM 2008 7 15 08FDEA02284 1 20080617 A 5340 65453135 STRINGER CLIP BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 CABIN, BS 720B AT 7L STRINGER CLIP HAS CORROSION REMOVED CLIP REF SRM 51-30-02 DRILLED UP NEW CLIP. INSTALLED NEW CLIP REF 51-30-02 PG 1-17, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080715 NM 2008 7 15 08FDEA02285 1 20080617 A 5340 65453132 STRINGER CLIP BOEING 727 727225 1384077 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 STRINGER CLIP CRACKED, BS 950D, STRINGER 5L REMOVED CRACKED STRINGER CLIP FROM BS 950D, STRINGER 5L, AND INSTALLED A NEW STRINGER CLIP AT SAME LOCATION, REF SRM 51-30-02 P 1-32. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080715 WP 2008 7 15 08FDEA02287 1 20080617 A 5730 ARB09831 SKIN DOUG DC10 DC1010 3022110 WP ZONE 500 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 40061 46973 LT WING LOWER SURFACE FOUND EXISTING REPAIR ON BEAVER TAIL NOT IN COMPLIANCE WITH SRM 57-00-01 VOL I FIG 8. ACCOMPLISHE D EA 8-5710-120488. 2 L 7 3 4F A22WE 20080715 NM 2008 7 15 USAA920081189 1 20080601 A 5320 INTERCOSTAL BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 905AW 23567 MCN - C12 - MAJOR REPAIR - NR 6109944 - INTERCOSTAL UPPER ANGLE CRACKED B/S 660 TO 680, W/L 208.1, BL 0 (HFEC VERIFIED). REPLACED INTERCOSTAL UPPER ANGLE B/S 660 TO 680, W/L 208.1, BL 0 IAW SRM 51-40-02-0G. (K) 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 USAA920081190 1 20080530 A 5320 ANGLE BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 905AW 23567 MCN - C12 - MAJOR REPAIR - NR 6108587 - L-ANGLE CLIP CRACKED B/S 350 S6L JUST ABOVE L-1 DOOR SURROUND (HFEC VERIFIED). REPAIRED L-ANGLE CLIP B/S 350 S6L JUST ABOVE L-1 DOOR SURROUND IAW SRM 51-40-02-0G. (K) 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 USAA920081217 1 20080613 A 5753 SKIN BOEING 737 7374B7 1384702 NM T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT - C3 - MAJOR REPAIR - NR 04-9557-8-0055/001 - LEFT WING OB AFT FLAP DELAMINATED ON TOP SIDE. REPLACED LEFT WING OB A FT FLAP IAW B737, AMM 27-51-39. (K) 2 L 7 2 4F RT A16WE 20080715 EU 2008 7 15 USAA920081219 1 20080524 A 5315 D53472793200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 652AW 0953 SAL - C7 - MAJOR REPAIR - NR 6107518 - CORROSION ON FLOORBEAM AT FR 66 TO FR 70 AT BL-Y-65. REPAIRED CORROSION ON FLOORB EAM AT FR 66 TO FR 70 AT BL Y-765 IAW SRM 51-72-11. (K) 2 L 7 2 4F RT A28NM 20080715 NM 2008 7 15 USAA920081214 1 20080606 A 5754 SKIN BOEING 757 7572B7 1384964 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 929UW 27144 BFM - C2-MAJOR REPAIR - TAXK CARD NR JL-900-09000 - RIGHT WING NR 6 SLAT HAS AREA OF DELAMINATION. REPAIRED RIGHT WING N R 6 SLAT IAW SRM 57-43-01 AND 51-70-10. (K) 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 USAA920081216 1 20080612 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT - C3 - MAJOR REPAIR - NR O3C10000004/001 - FUSELAGE SKIN CRACKED AT BS 727F, STRINGER 22R, REPAIRED FUSELAGE SKIN AT BS 727F, STRINGER 22R IAW SRM 53-00-01. (K) 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 08FDEA02292 1 20080617 A 5720 6521656224 STIFFENER BOEING 727 727227 1384078 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 SEAL RETAINER STIFFENER RT WING AFT LWR SPAR WS 181-220 IS CORRODED REMOVED CORROSION FROM STIFFENER AT STA 181-220 RT W ING ORIGINAL MATERIAL .040 MATERIAL LOSS .010 REMAINING MATERIAL .030 OUT OF LIMITS. REMOVED STIFFENER AND FABRICATED N EW STIFFENER MATERIAL 2024-T3-.040 AND INSTALLED. TREATED AND PRIMED. REF DWR 65-21656 AND SRM 51-10-2. THIS IS CLASSI FIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080715 EU 2008 7 15 08FDEA02154 1 20080604 A 5730 SKIN AIRBUS 310 A310203 3930313 EU ZONE 500 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LT WING OUTBD FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB NR 2 AND RIB NR 3, MEASURING 4.0 IN BY 4.7 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT OUTER S KIN REPAIR ON RT WING OUTBD FLAP UPPER SKIN BETWEEN RIB NR 2 AND RIB NR 3 IAW A310-200 SRM 57-53-10, FIG 210. THIS IS A N AIRBUS REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080715 NM 2008 7 15 08FDEA02156 1 20080604 A 5534 6517506 WEB BOEING 727 727227 1384078 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 AIR STAIR COMPARTMENT ABOVE "S" DUCT AT STA 1303, LT SIDE OF YELLOW VERTICAL WEB WHERE STIFFENER PASSES THROUGH CUT OUT, CRACKED. DOT ON AFT SIDE OF WEB AND ACCESS THROUGH VERT STAB PANEL 9504 REMOVED DAMAGE, FABRICATED, TREATED, PRIMED AN D INSTALLED REPAIR PARTS. REF SRM'S 51-30-02 PG 32, 51-40-02 PG 1-6, MM'S 51-20-021-7, 51-20-031 PGS 1-3, NAD BOEING D OC 65-17506 ITEM 31. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080715 EU 2008 7 15 08FDEA02157 1 20080604 A 5753 SKIN AIRBUS 310 A310203 3930313 EU ZONE 500 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LT WING OUTBD FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB NR 6 AND RIB NR 7, MEASURING 3.9 IN BY 4.1 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT OUTER S KIN REPAIR ON RT WING OUTBD FLAP UPPER SKIN BETWEEN RIB NR 6 AND RIB NR 7 IAW A310-200 SRM 57-53-10, FIG 210. THIS IS A N AIRBUS REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080715 NM 2008 7 15 USAA920081243 1 20080613 A 5312 651758243 BULKHEAD BOEING 737 7373B7 138447F NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 531AU 24478 PIT - FPBH - MAJOR REPAIR - E1A53032 - TWO EACH CRACKS AT WEB OF VERTICAL BEAM BS 178, RBL 17 JUST BELOW WL 234. REPAIR ED WEB OF VERTICAL BEAM BS 178, RBL 17 JUST BELOW WL 234. (K) 2 L 7 2 4F RT A16WE 20080715 EA 2008 7 15 A6WA200840405 1 20080508 A 5320 SEPARATOR CNDAIR CL600 CL6002B19 1900309 EA ACCESS PANEL WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 442AW 7778 FIREWALL SEPARATOR WORN ON ACCESS PANEL 412DB. (K) FIREWALL SEPARATOR REPLACED IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 20080715 CE 2008 7 15 MT9A00000033 1 20080513 A 3240 06111800 HOUSING CESSNA 208 208B 2073701 CE LT MLG BRAKE DAMAGED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9623B 208B0138 LT BRAKE CYLINDER HSG WORN AT THE ANCHOR BOLT PASS THROUGH HOLE ALLOWING THE ANCHOR BOLT TO BE PRESSED OUT BY HAND. THIS IS NORMALLY A CLOSE TOLERANCE FIT. THIS CONDITION IN THE PAST HAS CAUSED THE ANCHOR BOLT TO SHEER OFF CAUSING CATASTROF IC DAMAGE TO THE CALIPER ASSY, TORQUE PLATE AND/OR TIRE ON THREE AC. 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000039 1 20080516 A 7921 FLANGE CESSNA 208 208B 2073701 CE OIL COOLER CRACKED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 UPPER MOUNTING FLANGE HAS A 2 INCH CRACK AGAINST OIL COOLER BODY. (K) 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000038 1 20080516 A 7921 FLANGE CESSNA 208 208B 2073701 CE OIL COOLER CRACKED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 222 UPPER MOUNTING FLANGE HAS A 2.25 INCH CRACK AGAINST OIL COOLER BODY. (K) 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000031 1 20080512 A 2750 MS276404 BEARING CESSNA 208 208B 2073701 CE T/E FLAP CORRODED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 1037N 208B0334 THE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K) 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000030 1 20080512 A 2750 MS276404 BEARING CESSNA 208 208B 2073701 CE T/E FLAP CORRODED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 1041L 208B0337 THE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K) 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000029 1 20080512 A 2750 MS276404 BEARING CESSNA 208 208B 2073701 CE T/E FLAP CORRODED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 1041L 208B0337 THE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K) 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000028 1 20080505 A 2750 BEARING CESSNA 208 208B 2073701 CE T/E FLAP CORRODED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 1041L 208B0337 THE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K) 1 H 7 1 3T A37CE 20080715 EU 2008 7 15 08FDEA02175 1 20080606 A 5320 A53978105200 COUPLING AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND A GAP BETWEEN COUPLING AND FRAME 65 RT, P21 REPAIR PERFORMED BY REMOVING THE COUPLING AND REPLACE IAW SRM 51-72-1 0. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 SWAA083453 1 20080623 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, RBL 32 TO RBL 41. REMOVED AND REPLACED CHOR D PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083456 1 20080623 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 729D, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083475 1 20080623 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 348, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083184 1 20080610 A 5315 6545808 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 294.5, LBL 10. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 2008UALA02975 1 20080522 A 5313 STRINGER SPLICE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 914UA 25381 E&E COMPARTMENT STRINGER SPLICE CORRODED BS 380 & STRINGER S-27L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED STRINGER SPLICE. REPLACED WITH NEW SPLICE P/N 65-59664-501. 2 L 7 2 4F 4 F RT A16WE E21EU 20080714 EU 2008 7 14 08FDEA02402 1 20080624 A 5347 A53832103206 SEAT TRACK AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CRACKS IN WEB AT TRACKS 3-4 RT AT C 47. REPAIR PERFORMED BY CRACK STOP HOLE AND INSTALLING A DOUBLER IAW RAS 7051 1471/005/2008 ISS A, APPROVED BY EA 6-5315-120074. 2 L 7 2 4F RT A35EU 20080714 EU 2008 7 14 08FDEA02408 1 20080624 A 5320 A53612213209 FLOOR SUPPORT AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 719FD 388 MAIN CARGO FLOOR SUPPORT AT RBL 77 HAS CORROSION AROUND FASTENER HOLES FOR FLOORBOARD FROM FR 13A TO FR 16A. REMOVED AN D REPLACED FLOORBOARD SUPPORT IAW SRM 51-73-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 08FDEA02410 1 20080624 A 5311 651632710 FRAME BOEING 727 727227 1384078 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 FRAME CRACKED AT LOCK FASTENER, STA 800 STRINGER 14R. REMOVED DAMAGED PORTION OF FRAME ANGLE, FABRICATED REPAIR ANGLE A ND FRAME FILLER. HEAT TREATED, ALODINED AND PRIMED AND INSTALLED. REF SRM 51-40-2 FIG 1, 51-30-2 PG 2, THIS IS CLASSIF IED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 DLM88080853 1 20080610 A 5330 59360665 DOUBLER DOUG MD88 MD88 3023688 NM BS 693 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 964DL 49983 CORROSION ON THE BELLY INTERNAL DOUBLER AT FS 693 BETWEEN LONGERONS 29R AND 30R. 1 INCH BY 1.5 INCH CUTOUT DID NOT AFF ECT THE SKIN. EXTERNAL REPAIR DOUBLER AND TRIPLER DUE TO PRESENCE OF THE C-2 DOOR EXTERNAL SURROUND DOUBLER. DTA SCHE DULED AT 24 MONTHS. 2 L 7 2 4F RT A6WE 20080714 NM 2008 7 14 08FDEA02430 1 20080624 A 5315 65255896 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 PASS CABIN AT STA 760 CARGO FLOOR SUPPORT NUT PLATE IS MIS-DRILLED AT RBL 4, WL 208. REMOVED FLOOR SUPPORT CHANNEL, LOC ATED, DRILLED, AND INSTALLED NEW FLOOR SUPPORT P/N 65-25589-6, A18848, PO NR 1038952 REF SRM 51-30-5 PG 6, 51-30-2 PG 4. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 DL757080780 1 20080527 A 5420 311N373022 BRACE BOEING 757 757232 1384965 NM NR 1 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 DURING ACCOMPLISHMENT OF THE SIP MOD, S/B 757-54-0034 REV 1, THE DIAGONAL BRACE LOWER/FWD I/B LUG WAS INADVERTENTLY OVER SIZED TO 2.003" INSTEAD OF THE REQUIRED 2.000" MAXIMUM. AN OVERSIZED BUSHING WAS INSTALLED. AD 2003-18-05 APPLIES. 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 08FDEA02389 1 20080623 A 5311 FRAME BOEING 757 7572B7 1384964 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 906FD 27148 AFT CARGO COMPARTMENT, LT SIDE, STA 1340, S026L, FRAME IS DENTED. REPAIRED DENTED FRAME BY INSTALLING A FABRICATED DOUB LER REPAIR, ON MAE TRAVELER NR T8/741854, IAW SRM 53-00-07, REPAIR NR 5. THIS REPAIR IS CLASSIFIED AS A CATAGORY "A" MAJOR REPAIR, WITH NO FOLLOW UP TRACKING REQUIREMENTS. 2 L 7 2 4F RT A2NM 20080715 WP 2008 7 15 08FDEA02226 1 20080611 A 5343 ARB06341 ANGLE DOUG MD10 MD1010F 3022112 WP MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 368FE 76008 46606 LT MLG, AUX SPLICE ANGLE FOR THE MLG ATTACH FITTING, P/N ARB0634-1, OUTBOARD OF THE LT MLG FITTING ON THE FWD SIDE OF TH E LOWER AUX. SPAR HAS SEVERE EXFOLIATION CORROSION FROM APPROX WING STA XW222.000 TO WING STA XW231.000 RESULTING IN AN APPROX 8 INCH CRACK. REMOVED FITTING ARB0634-1. INSTALLED NEW SPLICE ANGLE ARB0634-1 REF SRM 51-31-01. 2 L 7 3 4F RT A22WE 20080710 NM 2008 7 10 DLM90080732 1 20080514 A 5753 5930492501 SKIN DOUG MD90 MD9030 3023690 NM FLAP VANE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 LEFT WING I/B FIXED VANE LOWER SURFACE HAS SEVERAL SMALL DINGS. REPAIRED DENT DAMAGE TO LOWER SURFACE OF LT WING I/B FI XED VANE, IAW MD90 SRM 57-20-05D, PARA 14, FIG 21. 2 L 7 2 4F RT A6WE 20080710 NM 2008 7 10 DL76L080750 1 20080418 A 3397 CONNECTOR BOEING 767 767332 1382001 NM CABIN INCORRECT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 EEL SEAT FEEDER AT STA 1263 RIGHT HAS WRONG CONNECTORS. EEL CONNECTOR WAS REPLACED AT STA 1263 RIGHT, EELS LIGHT OPS CH ECKS GOOD IAW B767-300 MM 33-51-10. 2 L 7 2 4F RT A1NM 20080710 NE 2008 7 10 DL76L080766 2 20080520 A 7532 80217010 BLEED VALVE BOEING 767 767332 1382001 NM PWA 4090 PW4090 52119 NE NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 196DN 28453 724655 RT ENG HPSOV MSG. FWD TO MCO PLAC PER MEL 36-11-02 RT ENG HP BLEED VALVE LOCKED OUT. NOTE: AIRCRAFT FLOWN TO ATL FOR EQUIP SUB DUE TO ADDITIONAL PROBLEM WITH THE LT ENG BLEED. CVG REPLACED LT HP CONTROLLER AND LOCK RT HP BLEED VALVE CLO SED. ATL MTC REPLACED RT ENG HP BLEED VALVE. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS. 2 L 7 2 4F 4 F RT A1NM E46NE 20080710 NM 2008 7 10 2008UALA02820 1 20080515 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 AFT PIT STA 1340 BETWEEN STR 26R AND 27R, FRAME DENTED. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED DAMAGE FAB AN D INSTALL RPR IAW SRM 53-00-07. THIS IS A CAT B RPR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSP STARTING AT 50000 TOTAL FC AND 12000FC THEREAFTER. INSP PER SRM 53-00-07 RPR 5 TABLE II. INSP CONSISTS OF BOTH VISUAL AND NDT. CURRENT PTC IS 20 417. -INF- :MF2631 OPENED TO CHECK AT MAX PTC 62000 & EVERY 12000C THEREAFTER. 2 L 7 2 4F 4 F RT A2NM E17NE 20080710 NM 2008 7 10 2008UALA02821 1 20080515 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 AFT PIT STA 1340, STR 26L, FRAME DENTED. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED DAMAGE FAB AND INSTALL RPR IAW SRM 53-00-07. THIS IS A CAT B RPR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSP STARTING AT 50000 TOTAL FC AND 12000FC THEREAFTE R. INSP PER SRM 53-00-07 RPR 5 TABLE II. INSP CONSISTS OF BOTH VISUAL AND NDT. CURRENT PTC IS 20417. -INF- :MF2633 OPENED TO CHECK AT MAX PTC 62000 & EVERY 12000 THEREAFTER. 2 L 7 2 4F 4 F RT A2NM E17NE 20080710 NM 2008 7 10 2008UALA02929 1 20080519 A 2560 65B09094 GIRT BAR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L5 DOOR FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 196UA 28715 DOOR 5L WILL NOT ARM. REPLACED AFT GIRT BAR LATCH MECHANISM CONTROL ROD BELL CRANK OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080710 NM 2008 7 10 2008UALA02934 1 20080521 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 5A FWD LIGHT ASSY. REPLACED LIGHT ASSY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080710 NM 2008 7 10 2008UALA02951 1 20080521 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 FWD OF L-2 DOOR AT STA 680 AND STR 12L, INTERCOSTAL CRACKED. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW INTERCOSTAL (P/N 143N8334U27). 2 L 7 2 4F 4 F RT A2NM E17NE 20080710 2008 7 10 BB08093 4 20080522 A 2565 D30655123 SLIDE BOEING 757 7572B7 1384964 NM EVAC SLIDE LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 929UW 41280 592 27144 MCO - THE R-2 DOOR EMERGENCY ESCAPE SLIDE PRESSURE WAS FOUND LOW. MAINTENANCE REPLACED THE R-2 DOOR EMERGENCY ESCAPE SL IDE. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 UPS08M52324 1 20080509 A 5321 WSP0785501 FLOOR PANEL DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C MAIN CARGO, RCB NR 10 HAS CORROSION DAMAGE 2 PLACES ON TOP FACE. REPLACED PANEL AND INSTALLED ON E0 MD11-5330-27218. 2 L 7 3 4F RT A22WE 20080711 2008 7 11 SA08036 4 20080522 A 2565 60592201 RESERVOIR AIRBUS A319 A319112 3930323 EU EVAC SLIDE LOW PRESSURE A USAA K NONE J WARNING INDICATION CR CRUISE 1 EA 19 742PS 1275 DEN, FLIGHT 1553, PHL-DEN - CIDS CAUTION EMR L LOW PRESSURE. MAINTENANCE REPLACED THE L/OFFWING ESCAPE SLIDE RESERVOIR. 2 L 7 2 4F RT A28NM 20080711 NM 2008 7 11 AALA200801127 1 20080428 A 2822 PUMP BOEING 767 767323 1385205 NM FUEL SYSTEM MALFUNCTIONED A AALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC UK UNKNOWN 1 SW 21 357AA 24038 JFK INFLIGHT T92/28APR ORD TO DUB - CREW REPORTED LEFT AFT FUEL BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED AND CIRCUIT BR EAKER POPPED. LANDED JFK WITHOUT INCIDENT. REPLACED LEFT AFT FUEL BOOST PUMP. 2 L 7 2 4F RT A1NM 20080711 NM 2008 7 11 AALA200801147 1 20080428 A 2700 113W12114 FITTING BOEING 777 777223 1385213 NM DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 793AN 30255 AFW - DRIVE ARM FITTING ASSEMBLY JOINT 2A HAS BEEN BORED TO 1.714 INCH. BEYOND ALLOWABLE DIMENSION OF CMM 27 57 97 REPA IR 2.2. REPAIRED PER ENGINEERING INSTRUCTIONS. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801171 1 20080430 A 3350 LENS BOEING 777 777223 1385213 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHT AT OVERHEAD FIRST CLASS GALLEY HAS LOOSE LENS. SECURED LENS FOR EMERGENCY LIGHT AT OVERHEAD FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801234 1 20080506 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 DFW - EMERGENCY LIGHT AT SEAT 26G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080715 NM 2008 7 15 08FDEA02325 1 20080619 A 5320 144N8140Y46 SUPPORT BOEING 757 75723A 1384967 NM BS 960 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 LWR FUSELAGE KEEL BEAM AREA, CORROSION ON CENTER SUPPORT FRAME AT BS 960. CORROSION FOUND EXCEED ALLOWABLE LIMITS IN B7 57-200 SRM 53-00-71. REMOVED AND REPLACED TEE SUPPORT IAW B757-200 SRM 51-40-02 REV.93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 08FDEA02330 1 20080619 A 5320 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATIONS AT HOLES NR C AND NR D (THIRD LAYER). REMO VED AND REPLACED AS PER SRM 51-31-01 VOL.II. NEW FITTING FABRICATED AS PER EA1-5300-122494, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 08FDEA02335 1 20080619 A 5320 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D (THIRD L AYER). MAIN CARGO DOOR LOWER JAMB, CRACKED NR 7 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. NEW F ITTING FABRICATED AS PER EA 1-5300-122494, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080715 WP 2008 7 15 08FDEA02303 1 20080618 A 5320 AEA034423 SILL DOUG DC10 DC1010 3022110 WP BS 1701 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 CTR CARGO COMPT DOOR SILL AREA FOUND CORROSION WITH EXFOLIATION ON TEE CAP OF JAMB. 2 L 7 3 4F A22WE 20080715 NM 2008 7 15 08FDEA02283 1 20080617 A 5340 6545313Y2 STRINGER CLIP BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 CABIN, BS 520 S 3R CLIP CRACKED (STR CLIP) REMOVED CLIP REF SRM 51-30-02, DRILLED UP NEW CLIP. INSTALLED CLIP REF SRM 5 1-30-2 PG 1-17. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080715 NM 2008 7 15 USAA920081206 1 20080601 A 5320 INTERCOSTAL BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 905AW 23567 MCN - C12 - MAJOR REPAIR - NR 6109924 - INTERCOSTAL UPPER ANGLE CRACKED B/S 540 TO 560 B/LO W/L 208.1. (HFEC VERIFIED). REMOVED AND REPLACED INTERCOSTAL UPPER ANGLE B/S 540 TO 560 B/LO W/L 208.1 IAW SRM 51-40-02-0G. (K) 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 USAA920081211 1 20080614 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 307AW 24634 PHX - ROW 20 EMERGENCY PATH LIGHT INOPERATIVE. MX REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD. (K) 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 USAA920081235 1 20080531 A 5320 907822 STRAP BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW 23713 CLT - C22 - MAJOR REPAIR - NR 11A52001/004 - FORWARD ENTRY DOOR CUTOUT STRAP CRACKED AT BS-312, S-13L. REPLACED FORWARD ENTRY DOOR CUTOUT STRAP AT BS 312, S-13L IAW DRAWING NR 65-17684. (K) 2 L 7 2 4F RT A16WE 20080715 WP 2008 7 15 08FDEA02295 1 20080617 A 5347 6010965 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 395FE 46629 MAIN CARGO COMPT SEAT TRACK HAS DAMAGED AREAS AT F/S 735-755 LBL8 EVALUATED AND FOUND OUT OF LIMITS. REMOVED FLOOR PANE LS AND SEAT TRACK. FABED NEW TRACK AND SPLICE ON TRAVELERS T8/744729,T8/744769, T8/744782. INSTALLED NEW TRACK AND SPL ICES AND REINSTALLED FLOOR PANELS ALL IAW SRM 51-31-01, 53-70-00 FIG 5. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A22WE 20080715 EU 2008 7 15 08FDEA02144 1 20080604 A 5411 RIB AIRBUS 300 A300F4605R 3930327 EU NR 2 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 NR 2 PYLON RIB 8A; STA 726 OUTBD SIDE SHIM HAS A .75 INCH CRACK. 2 L 7 2 4F RT A35EU 20080715 CE 2008 7 15 MT9A00000036 1 20080515 A 2750 MS276404 BEARING CESSNA 208 208B 2073701 CE BELLCRANK CORRODED E MT9A O OTHER O OTHER NR NOT REPORTED 1 SW 05 9623B 208B0138 THE SEALED BEARING WERE CORRODED. (K) 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000032 1 20080512 A 2750 MS276404 BEARING CESSNA 208 208B 2073701 CE T/E FLAP CORRODED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 1037N 208B0334 THE SEALED BEARING WAS CORRODED AND FROZEN, ALSO THE BEARING WAS CORRODED TO THE BOLT. (K) 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000003 1 20080311 A 2750 26220911 BELLCRANK CESSNA 208 208B 2073701 CE T/E FLAP CORRODED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9525B 208B0087 DURING AN INSPECTION OFTHE LEFT WING ON AC, REGISTRATION NUMBER 9525B, SN 208B0087, MAINTENANCE PERSONNEL FOUND THE MOST OB FLAP BELLCRANK (PN 26220911) FROZEN. THE BOLT WAS FROZEN TO THE BUSHING (PN 82614410ON). THIS PREVENTED THE BOLT FR OM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET ( PN 26221013). THIS GAVE ENOUG H PLAY THAT THE FLAP CABLE, WHEN SELECTED UP, WOULD WRAP AROUND THE BELLCRANK CAUSING THE CABLE TENSION TO INCREASE AND ALSO PUSHED THE CABLE INTO THE TRAILING EDGE RIB IB OF THE MIDDLE FLAP TRACK AT WS 118.00 WHICH FRAYED AND STRETCHED THE CABLE REQUIRING REPLACEMENT. CORROSION WAS SO SEVERE THAT DURING THE PROCESS TO REMOVE THE BELLCRANK, THE BOLT HEAD BRO 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000009 1 20080410 A 2750 BEARING CESSNA 208 208B 2073701 CE CORRODED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9505B 208B0085 THE SEALED BEARING WAS CORRODED AND FROZEN ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K) 1 H 7 1 3T A37CE 20080715 WP 2008 7 15 08FDEA02186 1 20080606 A 5420 AUB70795 STIFFENER DOUG MD10 MD1010F 3022112 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 NR 3 PYLON PANEL NR 487 EL HAS A CRACKED STIFFENER. REMOVED AND REPLACED THE CRACKED STIFFENER IAW DC/MD-10 SRM 51-31-0 1; VOL II ON PANEL 487 EL ON THE NR 3 PYLON. 2 L 7 3 4F RT A22WE 20080715 EU 2008 7 15 08FDEA02187 1 20080606 A 5753 A57971445200 SKIN AIRBUS 310 A310203 3930313 EU ZONE 600 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RT WING OUTBD FLAP LOWER SKIN AFT OF FWD SPAR BETWEEN RIB NR 3 AND RIB NR 4, MEASURING 6.9 IN BY 8.6 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED OUTER SKIN REPAIR ON RT WING OUTBD FLAP LOWER SKIN BETWEEN RIB NR 3 AND RIB NR 4 IAW A310-200 SRM 57-53-12,FIG 210. THIS IS AN AIRBUS REPAI R AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080715 CE 2008 7 15 MT9A00000010 1 20080423 A 2750 MS276404 BEARING CESSNA 208 208 2073702 CE BELLCRANK CORRODED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9653F 20800114 THE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K) 1 H 7 1 3T NT A37CE 20080715 CE 2008 7 15 MT9A00000013 1 20080423 A 2750 26220919 BELLCRANK CESSNA 208 208 2073702 CE T/E FLAP DAMAGED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9653F 20800114 THE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE B OLT HOLE THROUGH THE MOUNTING BRACKET. (K) 1 H 7 1 3T NT A37CE 20080715 CE 2008 7 15 MT9A00000018 1 20080508 A 2750 26220919 BELLCRANK CESSNA 208 208B 2073701 CE T/E FLAP DAMAGED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9760B 208B0102 THE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE B OLT HOLE THROUGH THE MOUNTING BRACKET. ALSO, THE SLEEVE CORRODED TO THE BELLCRANK. (K) 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000019 1 20080512 A 3240 06111800 HOUSING CESSNA 208 208B 2073701 CE LT MLG BRAKE WORN D MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9505B 208B0085 LT BRAKE CYLINDER HOUSING WORN AT THE ANCHOR BOLT PASS THROUGH HOLE ALLOWING THE ANCHOR BOLT TO BE PRESSED OUT BY HAND. THIS IS NORMALLY A CLOSE TOLERANCE FIT. THIS CONDITION IN THE PAST HAS CAUSED THE ANCHOR BOLT TO SHEER OFF CAUSING CATAS TROPHIC DAMAGE TO THE CALIPER ASSEMBLY, TORQUE PLATE AND/OR TIRE ON THREE OF OUR AC. (K) 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000021 1 20080512 A 3240 06111800 HOUSING CESSNA 208 208 2073702 CE RT MLG BRAKE WORN E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9653F 20800114 RT BRAKE CYLINDER HOUSING WORN AT THE ANCHOR BOLT PASS THROUGH HOLE ALLOWING THE ANCHOR BOLT TO BE PRESSED OUT BY HAND. THIS IS NORMALLY A CLOSE TOLERANCE FIT. THIS CONDITION IN THE PAST HAS CAUSED THE ANCHOR BOLT TO SHEER OFF CAUSING CATAS TROPHIC DAMAGE TO THE CALIPER ASSEMBLY, TORQUE PLATE AND/OR TIRE ON THREE AC. (K) 1 H 7 1 3T NT A37CE 20080715 EU 2008 7 15 08FDEA02196 1 20080607 A 5540 A550485000465 ARM AIRBUS 310 A310222 3930315 EU RUDDER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 NR 6 RUDDER HINGE ARM EXFOLIATED AT RUDDER ATTACH FITTING, WILL REPLACE. REPLACED NR 6 RUDDER HINGE ARM P/N A5507853000 466 2 L 7 2 4F RT A35EU 20080715 NM 2008 7 15 08FDEA02197 1 20080608 A 5313 6523535 STRINGER BOEING 727 727227 1384078 NM BS 576-584 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 STR-3R HAS CORROSION, BS 576-584 REMOVED CORROSION REF SRM 53-10-1. AREA FOUND TO BE OUT OF LIMITS. REMOVED STRINGER S ECTION REF SRM 51-30-02 P 6-7. FABRICATED NEW SECTION REF SRM 53-10-2 FIG 9. INSTALLED NEW SECTION REF SRM 51-30-02. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080715 NM 2008 7 15 08FDEA02201 1 20080609 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 624FE 48443 CABIN RT TRANSVERSE FRAME AT STA 1661 FOUND DENTED AT LONGERON 12. 2 L 7 3 4F RT A22WE 20080715 EU 2008 7 15 08FDEA02206 1 20080609 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 THE BULK CARGO COMPARTMENT CEILING AREA MAIN DECK FLOOR SUPPORT ANGLE IS CRACKED AT THE FWD FACE OF FRAME 69 AND LBL 60. 2 L 7 2 4F RT A35EU 20080715 WP 2008 7 15 08FDEA02207 1 20080609 A 5414 AJC741595 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 ON THE NR 2 ENGINE ABOUT 7 O'CLOCK POSITION THE COWL RING COVERING THE NR 2 ENGINE ADAPTER RING IS CHAFED BY THE LEFT FA N COWL. REMOVED COWL RING PANEL FROM THE NR 2 ENGINE IAW DC/MD-10 SRM 51-31-01; VOL II. MATERIAL ID FOR THE NEW PANEL IS CLAD 2024-T6, 0.063 IAW DC/MD-10 SRM 55-31-01; VOL I; PGS 49 AND 50. FABRICATED A NEW PANEL IAW DC/MD-10 SRM 55-31- 01; VOL I; PGS 49 AND 50. ALODINED AND PRIMED THE NEW PANEL IAW DC/MD-10 SRM 51-21-01; VOL II. PART MARKED THE NEW PAN EL FX-AJC-7415-95 IAW FEDEX GMM 7-0-1000. INSTALLED THE NEW PANEL IAW DC/MD-10 SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 20080715 WP 2008 7 15 08FDEA02189 1 20080606 A 5414 AUB7108180 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 NR 3 PYLON PANEL 487 FL IS CHAFFED IN THE INNER SURFACE. BLENDED AREA AND FOUND A CRACK ON THE OUTBD ATTACH FLANGE. BL ENDED THE AREA AND FOUND A CRACK ON THE ATTACH FLANGE. ORIGINAL MATERIAL THICKNESS 0.071 IAW DC/MD-10 SRM 54-51-01; VOL III. MATERIAL REMAINING 0.064 USING UT GAUGE T8225P. FOUND TO BE WITHIN LIMITS IAW DC/MD-10 SRM 54-00-01; VOL I; FIG 1-A; SHEET 3. MATERIAL ID 2024-T30.071, PO 618569.1 IAW DC/MD-10 SRM 54-00-01; VOL I; FIG 2-B, SHEET 2 AND DC/MD-10 SR M 54-51-01; VOL III. FABRICATED REPAIR PARTS IAW DC/MD-10 SRM 54- 00-01; VOL I; FIG 2-B; SHEET 2. ALODINED AND PRIME D IAW DC/MD-10 SRM 51-21-01; VOL II. INSTALLED DOUBLER IAW DC/MD-10 SRM 51-35-01; VOL II. 2 L 7 3 4F RT A22WE 20080715 EU 2008 7 15 S8A2008F00001 1 20080418 A 7931 642512001 TRANSDUCER BRAERO DH125 HS125700A 4230170 EU GARRTT TFE731 TFE7313R1H 29001 WP NR 1 ENGINE FAILED E S8AA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 39 110EJ 11062 NA0273 P84238 AT 15,000 ENROUTE, AIRCRAFT LOST INDICATION OF OIL PRESSURE ON THE NR ONE (LEFT) ENGINE AND THE FLIGHT CREW ACCOMPLISHED A PRECAUTIONARY SHUTDOWN OF THE NR ONE ENGINE. AFTER A REVIEW BY THE FLIGHT CREW OF ALL INDICATING ENGINE INSTRUMENTATI ON THE FLIGHT CREW DETERMINED THAT IT WAS SAFE TO ACOMMPLISH A RESTART OF THE NR ONE ENGINE FOR LANDING. THE LOW OIL PR ESSURE LIGHT NEVER ELIMINATED BUT OIL PRESSURE GAGE STILL READ ZERO. THE LANDING WAS UNEVENTFUL. FLIGHT CREW DID NOT DEC LARE AN EMERGENCY BUT DID REQUEST PRIORITY HANDLING. 2 L 7 2 4F 4 F A3EU E6WE 20080715 CE 2008 7 15 MT9A00000026 1 20080512 A 3240 06111800 HOUSING CESSNA 208 208B 2073701 CE CALIPER DAMAGED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9525B 208B0087 BRAKE CYLINDER HOUSING WORN AT THE ANCHOR BOLT PASS THROUGH HOLE ALLOWING THE ANCHOR BOLT TO BE PRESSED OUT BY HAND. THI S IS NORMALLY A CLOSE TOLERANCE FIT. THIS CONDITION IN THE PAST HAS CAUSED THE ANCHOR BOLT TO SHEER OFF CAUSING CATASTRO PHIC DAMAGE TO THE CALIPER ASSEMBLY, TORQUE PLATE AND/OR TIRE ON THREE OF OUR AC. (K) 1 H 7 1 3T A37CE 20080715 SO 2008 7 15 ODR2008F00000 2 20080424 A 8550 SEAL CESSNA 402 402B 207590P CE CONT O520 TSIO520EB 17040 SO ENG OIL PUMP LEAKING E ODRA E ENGINE SHUTDOWN K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 01 87193 402B1019 1457259B DURING A PART 91 FLIGHT, THE RIGHT ENGINE BEGAN LEAKING OIL. WITHIN 15 MINUTES THE OIL LEAK GOT PROGRESSIVELY WORSE. SMA LL PUFFS OF SMOKE CAME OUT OF THE TOP OF THE ENGINE. THE ENGINE WAS THEN SHUTDOWN AND FEATHERED. THE RESULT OF THE OIL LEAK WAS A BAD SEAL BETWEEN THE OIL PUMP AND COVER. (K) 1 L 7 2 3O 3 O A7CE E8CE 20080715 NE 2008 7 15 VQI2008F00001 2 20080514 A 7297 642W9810505 WIRE HARNESS AIRBUS A319 A319111 3930336 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE DAMAGED A VQIA A UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 WP 15 527VA 170 3417 IN NORMAL CRUISE, THE AIRCRAFT EXPERIENCED AN UNCOMMANDED SHUTDOWN OF THE NR 1 ENGINE. ECAM ENG1 FADEC A FAULT OCCURRED WITH ASSOCIATED MESSAGES. THE CREW RESTARTED THE ENGINE AFTER FOLLOWING QRH PROCEDURES . A/C DIVERTED INTO PDX WITH NO F URTHER FAULTS NOTED. CIRCUIT BREAKER A-4 (ENGINE 1 FADEC A AND EIU1) ON THE 49VU OVERHEAD PANEL WAS FOUND OPEN. UPON INS PECTION OF THE NR 1 ENGINE, CONDUCTED IAE TSM 73-25-00-810-843, THE J1 CONNECTOR PIN 13 (28V POWER SUPPLY) WAS FOUND WIT H A RECESSED CONTACTOR DEEP WITHIN THE CONNECTOR. NO ARCING WAS NOTED ON EITHER THE ECU OR CONNECTOR. WITH THE CONNECTOR INSTALLED, CB A-4 WOULD NOT STAY CLOSED. WITH THE CONNECTOR REMOVED, THE CB WOULD REMAIN CLOSED. THESE PARTS WERE SENT 2 L 7 2 4F 4 F RT A28NM E2GL 20080711 NM 2008 7 11 AALA200801134 1 20080428 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT SEAT 34G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 34G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801141 1 20080428 A 3350 CAP BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET AREA HAS WIRING EXPOSED. REPLACED END CAP ON WIRE COVER FOR EMERGE NCY LIGHT AT LEFT NUMBER ONE DOOR CLOSET AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 WP 2008 7 11 AALA200801125 1 20080428 A 2120 CLAMP DOUG DC9 DC982 3022082 WP A/C BAY LOOSE A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION UK UNKNOWN 1 SW 21 70529 49921 DFW INFLIGHT T1578/28APR - CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE INDICATION. LIGHT FLICKERED ON AND OFF FOR THREE TO FOUR MINUTES BEFORE EXTINGUISHING. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND RIGHT PACK CLAMP ON BOO T LOOSE ON DUCT. FOUND P SEALS AT HEAT EXCHANGER LEAKING. REPLACED P SEALS. REPLACED CLAMPS AND REINSTALLED BOOT ON A PU SURGE BLEED VALVE TEMPERATURE TABS IN AFT COMPARTMENT. 2 L 7 2 4F A6WE 20080711 NM 2008 7 11 AALA200801235 1 20080506 A 3350 OL3071BPEGPL LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801222 1 20080506 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 688AA 25730 JFK - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 16D INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 AALA200801213 1 20080505 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 DFW - EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 EU 2008 7 11 AALA200801203 1 20080504 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 11060 470 MIA - EMERGENCY LIGHT AT SEAT 22G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A35EU 20080711 NM 2008 7 11 AALA200801288 1 20080512 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 758AN 32637 DFW - EMERGENCY LIGHT AT SEAT 40G INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 40G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801232 1 20080506 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 684AA 25341 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 3B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 3B. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 AALA200801193 1 20080504 A 2782 18196914 TRANSMITTER BOEING 757 757223 1384957 NM L/E SLAT INOPERATIVE A AALA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 SW 21 623AA 24581 LAX INFLIGHT T1913/04MAY - CREW REPORTED LEADING EDGE SLAT DISAGREE INDICATION ON APPROACH. REPLACED LEADING EDGE DRIVE TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 WP 2008 7 11 AALA200801190 1 20080503 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 400AA 49311 DFW - EMERGENCY LIGHT AT SEAT ROW 23 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 23. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080711 WP 2008 7 11 AALA200801154 1 20080430 A 2120 5953625521 DUCT DOUG DC9 DC982 3022082 WP A/C BAY DEFECTIVE A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 460AA 49565 DFW INFLIGHT T318/30APR - CREW REPORTED TAIL COMPARTMENT TEMPERATURE HIGH INDICATION. RETURNED TO DFW AND LANDED WITHO UT INCIDENT. REPLACED DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080711 NM 2008 7 11 AALA200801163 1 20080430 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 623AA 24581 DFW - EMERGENCY LIGHT EXIT MARKERS AT LEFT AND RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY L IGHT EXIT MARKERS AT LEFT AND RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 AALA200801168 1 20080430 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 36C TO 42C INOPERATIVE. RECHARGED BATTERY PACKS FOR EMERGENCY LIGHTS AT OV ERHEAD SEAT ROWS 36C TO 42C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801237 1 20080506 A 3350 OL3071BPEGPL LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW - EMERGENCY LIGHT AT SEAT 37C INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 37C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801304 1 20080514 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW - EMERGENCY LIGHT AT SEAT 13G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 13G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801276 1 20080511 A 3397 WIRE BOEING 777 777223 1385213 NM CABIN EXPOSED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 795AN 30257 DFW - EMERGENCY LIGHT WIRES ARE EXPOSED IN MAIN DECK CREW CABIN FORWARD CLOSET. STOWED EMERGENCY LIGHT WIRES IN MAIN DE CK CREW CABIN FORWARD CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801309 1 20080514 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW - EMERGENCY LIGHT AT SEAT 26G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801307 1 20080514 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 755AN 30263 DFW - EMERGENCY LIGHT AT FORWARD GALLEY BY LEFT NUMBER ONE DOOR BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD GALLEY BY LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801188 1 20080503 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 604AA 27055 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 WP 2008 7 11 AALA200801179 1 20080502 A 3230 59403375511 RELAY DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 291AA 49303 LAX INFLIGHT T1716/02MAY - NOSE GEAR WOULD NOT RETRACT. NOSE GEAR UNSAFE INDICATION AFTER TAKEOFF AND CREW REPORTED NO ISE. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR INTERIOR RELAY R 262. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080711 NE 2008 7 11 AALA200801180 2 20080502 A 7261 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE RIGHT LEAKING A AALA E A ENGINE SHUTDOWN UNSCHED LANDING K R M FLUID LOSS PARTIAL RPM/PWR LOSS OVER TEMP CR CRUISE 1 SW 21 564AA 49346 725739 COS INFLIGHT T656/02MAY SAN TO ORD - NUMBER TWO ENGINE COMPRESSOR STALLED. HIGH ENGINE GAS TEMPERATURE NOTED. CREW SHU T NUMBER TWO ENGINE DOWN. LANDED COS WITHOUT INCIDENT. SINGLE ENGINE TIME TWENTY FIVE MINUTES. REPLACED NUMBER TWO EN GINE DUE TO OIL QUANTITY LOSS ON 04 MAY AT COS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A6WE E9NE 20080711 NM 2008 7 11 AALA200801191 1 20080503 A 2910 271N61191 HYDRAULIC LINE BOEING 757 757223 1384957 NM MLG LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SW 21 629AA 24587 CCS INFLIGHT T2133/03MAY - CREW REPORTED LEFT HYDRAULIC SYSTEM FAILED AFTER LOWERING LANDING GEAR. LANDED WITHOUT INCID ENT AND AIRCRAFT WAS TOWED TO GATE. FOUND A HOSE ASSEMBLY AT MAIN LANDING GEAR DOWNLOCK AT LEFT MAIL LANDING GEAR LEAKI NG. REPLACED HOSE FOR LEFT MAIN LANDING GEAR DOWNLOCK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 EU 2008 7 11 AALA200801204 1 20080504 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 11060 470 MIA - EMERGENCY LIGHT AT SEAT 26G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A35EU 20080711 NM 2008 7 11 AALA200801192 1 20080504 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW - EMERGENCY EXIT IDENTIFER AT LEFT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT IDENTIFER AT LEF T NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 EU 2008 7 11 AALA200801241 1 20080507 A 3260 DSB11021 DOWNLOCK SENSOR AIRBUS 300 A300B4605R 3930308 EU LT MLG MALFUNCTIONED A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 70074 517 SJU INFLIGHT T1635/07MAY - UPON GEAR EXTENSION CREW REPORTED AN INTERMITTENT UNSAFE INDICATION ON CENTER PANEL FOR NUMBE R ONE SYSTEM FOR LEFT MAIN LANDING GEAR. LANDED SJU WITHOUT INCIDENT. REPLACED THE LEFT MAIN GEAR DOWN LOCK SENSOR AND RELAY FOR LEFT MAIN LANDING GEAR DOWN LOCK SYSTEM ONE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20080711 NM 2008 7 11 AALA200801160 1 20080430 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 666A 25300 DFW - EMERGENCY LIGHT AT SEAT 12ABC BULLNOSE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 12ABC BULLNOSE. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 AALA200801161 1 20080430 A 3350 MODULE BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 666A 25300 DFW - EMERGENCY EXIT SIGN LIGHT AT FORWARD LAVATORY SIDEWALL INOPERATIVE. REPLACED MODULE FOR EMERGENCY EXIT SIGN LIGHT AT FORWARD LAVATORY SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 WP 2008 7 11 AALA200801149 1 20080429 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7546A 53028 DFW - EMERGENCY LIGHT AT LEFT STAIRWELL HAS BROKEN WIRE. REPLACED QUICK DISCONNECT TERMINAL FOR EMERGENCY LIGHT AT LEFT STAIRWELL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080711 NM 2008 7 11 AALA200801169 1 20080430 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHT AT OVERHEAD FORWARD SEAT 9D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD FORWARD SE AT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801215 1 20080505 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 DFW - EMERGENCY LIGHT AT SEAT 31C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 2008 7 11 AALA200801181 4 20080502 A 2213 285T0015117MODD CONTROL MODULE BOEING 757 757223 1384957 NM AUTOPILOT SYS INOPERATIVE A AALA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SW 21 603AA 27054 SJU INFLIGHT T660/02MAY SXM TO JFK - WITH CENTER AUTO PILOT ON CREW REPORTED A PITCH UP. FOLLOWED BY EICAS MESSAGE AND MASTER CAUTION LIGHT. AUTO PILOT WENT OFF. REPLACED CENTER FLIGHT CONTROL COMPUTER AND LEFT AND RIGHT STABILIZER TRIM AILERON CONTROL MODULES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 WP 2008 7 11 AALA200801182 1 20080502 A 4920 5940405503 APU DOUG DC9 DC982 3022082 WP LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 21 581AA 3204 53158 JFK INFLIGHT T2275/02MAY LGA TO BNA - CREW REPORTED SMOKE IN CABIN AND COCKPIT. DIVERTED TO JFK AND LANDED WITHOUT INC IDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION AND REPAIR. FOUND AUXILLIARY POWER UNIT (APU) LEAKING OIL. REPLAC ED APU ON 04 MAY AT JFK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080711 NM 2008 7 11 AALA200801226 1 20080506 A 3350 LENS BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 935AN 30081 DFW - EMERGENCY LIGHT AT SEAT ROW 10 HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 10. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080711 NM 2008 7 11 AALA200801135 1 20080428 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT SEAT 32G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 EU 2008 7 11 AALA200801198 1 20080504 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 11060 470 MIA - EMERGENCY LIGHT AT SEAT ROWS 6G TO 18G INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROWS 6G TO 18G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20080711 NM 2008 7 11 AALA200801136 1 20080428 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT SEAT 31G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801137 1 20080428 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT SEAT 25G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801151 1 20080429 A 3350 LENS BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 654A 24612 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 3B MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD SEAT 3B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 NE 2008 7 11 AALA200801178 2 20080502 A 7230 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LT ENGINE DAMAGED A AALA A UNSCHED LANDING R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CL CLIMB 1 SW 21 406A 49317 709998 DFW INFLIGHT T2452/02MAY - NUMBER ONE ENGINE COMPRESSOR STALL AND VIBRATIONS ON TAKEOFF AND CLIMB. REDUCED ENGINE TO IDLE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND ONE FAN BLADE DAMAGED. REPLACED TWO SETS OF FAN BLADES. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F A6WE E9NE 20080711 EU 2008 7 11 EGRR119748 1 20080520 A 5302 DOUBLER AEROSP SA365 SA365N 8680669 EU TAILBOOM CORRODED B EGRR K NONE O OTHER AA AIR AMBULANCE 1 EA 17 906LL 6018 DURING 600 HR INSPECTION FOUND CORROSION ON LT AND RT DOUBLERS AT FITTINGS IN TAILBOOM AT AIRCRAFT STATION 7951 MM. RE MOVED DOUBLER INSPECTED AND REPAIRED IAW AMERICAN EUROCOPTER REPORT AERS-08-1014. 1 G 7 2 3U H10EU 20080711 EU 2008 7 11 EGRR119766 1 20080522 A 5310 365A25300525 WINDOW FRAME AEROSP SA365 SA365N 8680669 EU CRACKED B EGRR K NONE O OTHER NR NOT REPORTED 1 EA 17 906LL 6018 DURING 600 HR INSPECTION TECHNICIAN FOUND LT AND RT UPPER WINDSHEILD FRAMES CRACKED. REPAIRS TO LT AND RT UPPER WINDSHI ELD FRAMES WILL BE PERFORMED IN ACCORDANCE WITH AMERICAN EUROCOPTER REPORT AE2007-55 AND AE2007-018. 1 G 7 2 3U H10EU 20080711 NM 2008 7 11 08FDEA01976 1 20080523 A 5414 311N504634 SKIN BOEING 757 75727B 1384921 NM NR 1 PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 916FD 24137 CORROSION FOUND ON PYLON NUMBER ONE INNER STRUT SKIN NEAR ACCESS PANEL 433JR CUTOUT, PPS 162.8. EVALUATE AND RECTIFY. PYLON NUMBER ONE RIGHT SIDE PANEL SKIN NEAR ACCESS PANEL 433JR CUTOUT REPLACED IN ACCORDANCE WITH BOEING DRAWING 311N500 2 ID 0014 REVISION E, 311N5046 ID0002 REVISION A AND B757-200 SRM 51-10-02 REVISION 93. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100. 2 L 7 2 4F RT A2NM 20080707 EU 2008 7 7 2008UALA02796 1 20080514 A 5320 BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 446UA 834 LT AFT PASSENGER-CREW DOOR SILL BEAM HAS CORROSION AROUND FLOOR PANEL ATTACH NUTPLATE HOLE LOCATED AT INBD MOST FLANGE A PPROX 4 INCHES FWD OF FR68. MAJOR REPAIR ACCOMPLISHED: MFG AND INSTALLED ANGLE REPAIR WET. 2 L 7 2 4F 4 F RT A28NM E40NE 20080707 SO 2008 7 7 RAIA00805016 1 20080514 A 3213 STRUT EMB 145 EMB145LR 3260212 SO MLG LOW A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 838HK 145321 FLT 7950 - IAD - LANDING GEAR AIR GROUND FAILURE MESSAGE AFTER GEAR RETRACTION. MAINTENANCE SERVICED THE MLG STRUTS AND PERFORMED AN OPERATIONAL CHECK OF THE LANDING GEAR SYSTEM. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080707 NM 2008 7 7 ASAA0842973 1 20080501 A 5755 SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 25114 RIGHT WING NR 6 SPOILER HAS SEVERAL DENTS ON UPPER SURFACE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER & INSTALLE D IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080707 NM 2008 7 7 USAA920081093 1 20080521 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 529AU 24411 FLT 945 - PHL - EMERGENCY EXIT LIGHTING - FLIGHT ATTENDANT REPORTED EMERGENCY ESCAPE PATH LIGHTING FROM ROWS 12-16 INOP. MX REPLACED THE BATTERY PACK FOR M1136 POWER SUPPLY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 20080708 EU 2008 7 8 USAA920081090 1 20080519 A 3232 114087005 BYPASS VALVE AIRBUS 320 A320232 3930326 EU LANDING GEAR LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 647AW 39125 39115 762 FLT 598 - PHL-LAS - EMERGENCY LANDING - CREW REPORTED LOSS OF GREEN HYDRAULIC SYSTEM ON CLIMB AT ABOUT 7000'. CREW DECL ARED AN EMERGENCY AND RETURNED TO PHL. MAINTENANCE REMOVED AND REPLACED THE DOOR BYPASS VALVE PER AMM 32-31-13. OPERAT IONAL AND LEAK CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 20080708 NM 2008 7 8 USAA920081092 1 20080516 A 5230 6547952524A STRUCTURE BOEING 737 7373G7 1384595 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 PHX - MAJOR REPAIR - RON - 4300672, AFT CARGO DOOR HANDLE CUTOUT CRACKED. REPAIRED AFT CARGO DOOR IAW B737 SRM 52-00-01 -2R3. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 2008UALA02862 1 20080518 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 FWD CARGO PIT STRINGER CLIP BENT AT BS 400 AND STRINGER S-24R. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED STRINGER CLI P AND REPLACED IT WITH NEW CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 20080708 NM 2008 7 8 2008UALA02884 1 20080518 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EEL INOP, ROW 36H. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 NM 2008 7 8 2008UALA02885 1 20080518 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHT INOP, LT OVERWING 2ND ASSY AFT. REPLACED LAMPS. 2 L 7 4 4F 4 F RT A20WE E24NE 20080708 2008 7 8 2008UALA02887 4 20080519 A 2397 BACC63BN0835 CONNECTOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU OXYGEN MASK MIC DETERIORATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 936UA 26667 F/O'S O2 MASK MIC INOP. CREW TO SWAP WITH 1ST OBSERVER O2 MASK & ADVISE. WHEN TROUBLE SHOOTING FOUND FAULTY CONNECTOR. REPLACED CONNECTOR OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080708 NM 2008 7 8 AALA200801112 1 20080427 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 958AN 30091 DFW - EMERGENCY LIGHT AT SEAT 23D MISSING LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 23D. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 ARWA20080503 1 20080517 A 7722 744471B THERMOCOUPLE DOUG DC10 DC1040F 3023507 NM NR 2 ENGINE SHORTED A ARWA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 29 140WE 46920 IN FLIGHT NR 2 ENGINE EGT INDICATOR FLUCTUATING 20 TO 30 DEGREES BOTH POINTER AND COUNTER, ALL OTHER PARAMETERS NORMAL. TROUBLE SHOT IN ACCORDANCE WITH TAFY MANUAL 77-21-00, FOUND THERMO COUPLE SHORTED AT 6 O'CLOCK POSITION AND HARNESS ISO LATION HIGH, REMOVED AND REPLACED HARNESS IN ACCORDANCE WITH M/M 77-21-05. INSTALLED PROBE IN ACCORDANCE WITH M/M 77-21 -00. SAFETY WIRED EGT PROBE IN ACCORDANCE WITH M/M 70-00-00. PERFORMED OPERATIONAL CHECK ON ENGINE RUN-UP IN ACCORDANC E WITH M/M 71-00-00, FOUND NORMAL, NO FLUCTUATION NOTED AT THIS TIME. 2 L 7 3 4F RT A22WE 20080708 NM 2008 7 8 DL757080881 1 20080617 A 5311 FRAME BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 AFT CARGO PIT STA 1540 LT FRAME AT STR 23L HAS A DENT. REPLACED DAMAGED FRAME FLANGE IAW SRM 53-00-07. 2 L 7 2 4F RT A2NM 20080708 NM 2008 7 8 DL738080890 1 20080619 A 5270 SWITCH BOEING 737 737832 13844CF NM R2 DOOR STICKS A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 3750D 32375 AFT SERVICE DOOR LIGHT ILLUMINATED ON T/O ROLL (WITH ASSOCIATED M/C LIGHT) DISCONNECTED T/O AT 50KTS. CLEANED PLUNGER O N AFT SERVICE DOOR SWITCH OPERATED SEVERAL TIMES DOOR CLOSED AND SECURED VERIFIED SWITCH TURNS LIGHT OFF. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 DL76L080854 1 20080610 A 5330 146T32311 SKIN BOEING 767 767332 1382001 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 176DN 25061 DURING PSV, MTC FOUND A GOUGE ALONG THE FUESLAGE SKIN FORWARD EDGE OF THE BULK CARGO DOOR CUTOUT AT FS 1417 AND S-30L. DAMAGE REMOVAL RESULTED IN A ROUTOUT APPROX 0.225 INCH WIDE BY 1.2 INCH LONG. THE UNDERLYING STRUCTURE WAS NOT DAMAGED OR CUT OUT. BOEING APPROVED A PERMANENT REPAIR FOR 12 MONTHS PENDING A DAMAGE TOLERANCE ANALYSIS. 2 L 7 2 4F RT A1NM 20080708 NM 2008 7 8 DL757080812 1 20080530 A 5313 STRINGER BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 STR 20L AT 1680 AND STA 1700 FOUND CRACKED AND CORRODED. REMOVED DAMAGE, FABRICATED STRINGER, SPLICED, TREATED, IAW 757 SRM 51-40-05 F 201, 2 L 7 2 4F RT A2NM 20080708 NM 2008 7 8 2008UALA02694 1 20080508 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 813UA 858 AFT CABIN EMERGENCY ESCAPE LIGHTS ON WITH SWITCH OFF. LIGHTS EXTINGUISHED WITH SWITCH ARMED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080710 NM 2008 7 10 DL76L080740 1 20080517 A 3412 102LA2AG PROBE BOEING 767 767332 1382001 NM TAT INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 178DN 25143 TAT LIGHT AFTER TAKEOFF. REPAIRS IN PROGRESS. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 DL76L080745 1 20080418 A 3397 CONNECTOR BOEING 767 767332 1382001 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 EEL SEAT FEEDER AT STA 654 LEFT MISSING MOLEX CONNECTOR. REMOVED AND REPLACED CONNECTOR AT STA 654 LEFT, EELS LIGHT OPS CHECK GOOD IAW B767-300 MM 33-51-10. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 DL76L080747 1 20080418 A 3397 CONNECTOR BOEING 767 767332 1382001 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 EEL SEAT FEEDER AT STA 1439 LEFT CUT/MISSING MOLEX CONNECTOR. REMOVED AND REPLACED CONNECTOR AT STA 1439 LEFT, EELS LIG HT OPS CHECKS GOOD IAW B767-300 MM 33-51-10. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 DL76L080756 1 20080511 A 3350 LIGHT BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 188DN 27583 EMERGENCY LIGHTS AT LT SEAT ROWS 16-20 INOP. C/W EA 01-468450-14 DATED 5-16-08, OPS CHECKS GOOD IAW B767-300 MM 33-51-0 0. 2 L 7 2 4F RT A1NM 20080710 EU 2008 7 10 USAA920081100 1 20080521 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 651AW 866 FLT 250 - SNA - EMERGENCY EQUIPMENT - FORWARD CABIN FLIGHT ATTENDANT FLASHLIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT BATTERY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 20080710 EU 2008 7 10 USAA920081095 1 20080430 A 5320 D53480043 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650AW 856 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON R2 DOOR CUTOUT LOWER SILL, BS 2786 / FR 66, -Y1430. REPAIRED THE R2 DOOR C UT OUT LOWER SILL, BS 2786 / FR 66, -Y1430 IAW USAIRWAYS EA 120744. 2 L 7 2 4F RT A28NM 20080710 NM 2008 7 10 SB08032 1 20080523 A 2560 P2070003001 FLASHLIGHT BOEING 737 7374B7 1384702 NM AFT CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 451UW 24934 CLT - MAINTENANCE REPORTED THE AFT LEFT TOP EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT TOP EMERGENCY FLASHLIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20080710 NE 2008 7 10 2008UALA02836 2 20080515 A 7261 BEARING IAE V2527A5 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 574UA 717964 26686 717964 BAD SMELL ON TAKEOFF LIKE BURNT OIL IN PACK. BAD IN COCKPIT & MID TO AFT CABIN. BEARING FAILURE IN NR 2 ENG. REPLACED NR 2 ENG. 2 L 7 2 4F 4 F RT A2NM E17NE 20080710 NM 2008 7 10 2008UALA02926 1 20080520 A 5311 FRAME SPLICE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 AFT PIT STA 1520 FRAME SPLICE GOUGED 3 EA PLACES STR 24R TO 25R. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE SPLICE. FA BRICATED AND INSTALLED NEW SPLICE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080710 NM 2008 7 10 2008UALA02948 1 20080522 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 EMERGENCY LIGHT WALL RIGHT AFT GALLEY INOP. FOUND LIGHT FAULTY. REPLACED LIGHT OP CHECKED GOOD. AC OK FOR SERVICE, . 2 L 7 4 4F 4 F RT A20WE E24NE 20080710 NM 2008 7 10 2008UALA02957 1 20080520 A 2750 ELECTRONIC UNIT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FLAP SYSTEM ACTIVATED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 787UA 26939 PRIMARY CHANNEL MESSAGE ON MAINTENANCE PAGE WHEN LOWERING FLAPS AND FLAPS ARE SLOW. SUSPECT FAULTY FSEU. REPLACED NR 2 FSEU REF. MM 21-51-01. OP CHECKS GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080711 NM 2008 7 11 UPS08M52313 1 20080513 A 5720 STRUCTURE DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C LEFT WING L/E SLAT TRACK NR 14 CUTOUT CRACKED. TRIMMED OUT CRACK, FABRICATED REPAIR DOUBLER AND FILL ER AND INSTALL DOUBLER AND FILLER IAW MD-11 SRM 57-10-00 VOLUME 1 FIG 21. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 UPS08M52315 1 20080513 A 5730 ANGLE DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C RT WING LEADING EDGE SKIN SPLICE STRAP ANGLE CRACK XOS 475. REMOVED CRACKED ANGLE, FABRICATED ANGLE, AND INSTALLED IAW DWG ARM2931, MD-11 SRM 51-33-01, 51-21-01, AND 51-21-00. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 UPS08M52322 1 20080511 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C LEFT WING FIXED L/E STRINGER AT XORS 506 FOUND CRACKED. REMOVED, FABRICATED, AND INSTALLED DOUBLER I AW MD-11 SRM 51-35-01, 51-33-01, 51-10-00, AND DWG ARB2933. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 UPS08M52323 1 20080506 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C RIGHT WING LEADING EDGE ACCESS PNL LANDING CRACKED XOS 550. FABRICATED AND INSTALLED STIFFENER IAW D WG ARB 2918 AND MD-11 SRM 51-31-01. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 AALA200801244 1 20080507 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT FORWARD GALLEY NEAR LEFT NUMBER ONE DOOR BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT A T FORWARD GALLEY NEAR LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801212 1 20080505 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 21C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801246 1 20080507 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 23C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 WP 2008 7 11 AALA200801156 1 20080430 A 3350 8039001 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7544A 53026 LGA - EMERGENCY LIGHT BATTERY PACK AT SEAT ROW 6 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080711 NM 2008 7 11 AALA200801157 1 20080430 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 666A 25300 DFW - EMERGENCY LIGHTS AT SEAT ROWS 7DEF TO 15DEF INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 7DEF TO 15DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 KCSA081267 1 20080530 A 5313 STRINGER BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 STA-495 STR-39L STRINGER CRACKED .5 INCH. 2 L 7 4 4F RT A20WE 20080715 NM 2008 7 15 KCSA081268 1 20080530 A 3350 LIGHT BOEING 747 747236B 1384804 NM CABIN INOPERATIVE A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 EMERGENCY EXIT LIGHT INOPERATIVE ON UPPER DECK STA-840. 2 L 7 4 4F RT A20WE 20080715 NM 2008 7 15 AALA200801286 1 20080512 A 3397 WIRE BOEING 777 777223 1385213 NM EMERGENCY LIGHTS EXPOSED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 758AN 32637 DFW - EMERGENCY LIGHT WIRING AT MAIN DECK CREW REST FORWARD CLOSET EXPOSED. REPLACED COVER FOR EMERGENCY LIGHT WIRING A T MAIN DECK CREW REST FORWARD CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080715 SW 2008 7 15 MT9A0000001 1 20080619 A 7603 NAS13513H16 SCREW SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MISSING E MT9A E ENGINE SHUTDOWN O OTHER NR NOT REPORTED 1 SW 05 26932 AC660 P44414C IN FLIGHT THE PPC INPUT LEVER TO THE PPC SHAFT CAME OFF AND PREVENTED THE CREW FROM BEING ABLE TO RETARD THE POWER TO TH E LEFT ENGINE. THIS FORCED THEM TO DO AN IN-FLIGHT SHUTDOWN OF THAT ENGINE. THE INVESTIGATION FOUND THAT THE SCREW AND S PACER THAT SECURES THE ARM TO THE SHAFT WAS NOT INSTALLED. FURTHER INVESTIGATION SHOWED A DISCREPANCY BETWEEN THE MM AN D THE IPC MANUAL FOR INSTALLING THESE PARTS ACCORDING TO AIRCRAFT SERIAL NR. THE OLDER SERIAL NR AC BELOW (AC 664) ARE N OT INSTRUCTED TO INSTALL THEM (71-00-15 (5) (D)). ALSO THE IPC CONTRADICTS ITSELF 76-10-40 FIG 7 CALLS FOR THE INSTALL ATION OF THESE PARTS FOR SN 420683 HOWEVER 76-10-50 LIMITS INSTALLATION OF THESE PARTS TO SN 664-683. 2 L 7 2 4T 4 T RT A8SW E4WE 20080715 NM 2008 7 15 AALA200801251 1 20080508 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 960AN 29542 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 ASAA0853015 1 20080530 A 3150 WARNING LIGHT BOEING 737 737890 1384527 NM APU ILLUMINATED A ASAA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 02 585AS 2950 35683 APU MAINT LIGHT ON. ACCOMPLISHED BITE CHECK FOUND MAINT MESSAGE 49 41244 START CONVERTER UNIT SHOWS FAILED GEN DIODE. ACCOMPLISHED TASK 49 40 00 810 806. FAULT LIGHT WENT OUT ON RESTART AND DID NOT RETURN. NO MAINT MESSAGES. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 ASAA0843007 1 20080519 A 5320 65479573 SILL BOEING 737 737490 1384715 NM BS 800-827 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 AFT CARGO DOOR CUTOUT SILL WEB IS CORRODED. REMOVED CORRODED WEB AND INSTALLED NEW WEB IAW SRM 51 40 02 PG 3. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 ASAA0843010 1 20080517 A 5330 65C357873 SKIN BOEING 737 737490 1384715 NM BS 380 S16-17L DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 DENT ON FUSELAGE SKIN AT STA 380 STR 16L 17L. REMOVED DAMAGED SECTION OF SKIN FABRICATED AND INSTALLED REPAIR FILLER DO UBLER AND TRIPLER IAW ASA EA5330 02346. 2 L 7 2 4F RT A16WE 2008041700030 20080417 00030 NM 2008 4 17 2008UALA02118 1 20080410 A 2160 285T00958 CIRCUIT CARD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN TEMP MALFUNCTIONED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 648UA 25285 UNABLE TO CONTROL TEMPERATURE IN ANY PART OF ACFT USING AUTO, TRIM AIR OFF, OR STANDBY SYSTEM. AFTER EXTENSIVE TROUBLE SHOOTING FOUND FAULTY COOLING CARD. REPLACED EQUIPMENT COOLING CARD M867 RAN ENGINES OP CHECKED GOOD. AC OK FOR SERVIC E. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041700036 20080417 00036 NM 2008 4 17 F3LA200800170 1 20080405 A 5320 151TG PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 44 1841 DURING C4 S1 C CHECK INSPECTION REPORTED PANEL 151TG AFT CARGO SLANT PANEL HAS HOLE. MAINTENANCE FABRICATED DOUBLER AND APPLIED REPAIR IN ACCORDANCE WITH SRM 53-02-00 AND AMM 25-00-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FO UND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008041700037 20080417 00037 NM 2008 4 17 F3LA200800168 1 20080403 A 5320 D534766000000 STRAP AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 44 1841 DURING C4 S1 C CHECK INSPECTION REPORTED SURFACE CORROSION ON AFT CARGO BAY FLOOR STRAP FROM FLOOR STRAP 2216 TO 2030 ST RINGER 38 RIGHT. MAINTENANCE REMOVED AND REPLACED DAMAGED FLOOR STRAP IN ACCORDANCE WITH SRM 53-41-14 FIGURE 2 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008041700077 20080417 00077 NM 2008 4 17 2008UALA01945 1 20080404 A 5311 FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 348 S16L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 FUSELAGE FRAME HAS DRILL START DAMAGE BS 348 STR 16L ADJACENT TO FASTENER HOLE FOR STOP FITTING. SUPPLEMENTAL DATA UPDA TE, MAJOR REPAIR ACCOMPLISHED, REAMED HOLE AND INSTALLED FREEZE PLUG REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700082 20080417 00082 NE 2008 4 17 2008UALA01950 2 20080404 A 7320 SHUTOFF VALVE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUEL SYSTEM MALFUNCTIONED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 783UA 26950 222223 ENG FUEL VALVE L LEFT HIGH PRESSURE (HP) FUEL SHUTOFF VALVE POSITION DISAGREES WITH COMMANDED POSITION. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008041700087 20080417 00087 NM 2008 4 17 2008UALA01953 1 20080404 A 3510 BOTTLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE OXYGEN SYSTEM READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED OXYGEN SYSTEM. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700099 20080417 00099 NM 2008 4 17 2008UALA01965 1 20080405 A 3150 WARNING MESSAGE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 772UA 26930 FOUND "FLIGHT CONTROL SYSTEM STATUS MESSAGE" LATCHED WITH NO CORRELATED MESSAGES. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008041700107 20080417 00107 NM 2008 4 17 2008UALA01973 1 20080406 A 2611 SMOKE DETECTOR BOEING 737 737322 1384676 NM FWD LAVATORY FALSE ACTIVATION A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 318UA 23950 FWD LAVATORY SMOKE DETECTOR WARNING, UNEXPLAINED. REPLACED SMOKE DETECTOR. 2 L 7 2 4F RT A16WE 2008041700109 20080417 00109 NM 2008 4 17 2008UALA01975 1 20080406 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY DOOR MOUNT LIGHT INOP AT 4R DOOR. REPLACED EMERGENCY DOOR MOUNT LIGHT OP CHECKS GOOD PER AMM 33-51-00 PB500. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700135 20080417 00135 NM 2008 4 17 2008UALA02000 1 20080406 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE SEAT 31AB & 37AB INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 EEL LIGHT AT SEAT 31AB, AND 37AB INOP. SUPPLEMENTAL DATA UPDATE, REPLACED EEL STRIPS. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041700137 20080417 00137 NM 2008 4 17 2008UALA02005 1 20080407 A 7830 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE THRUST REVERSER DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 521UA 24891 NR 2 ENG OB REV UPPER BIFURCATION PANEL INNER SKIN DELAMINATED. REPLACED REVERSER HALF. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700142 20080417 00142 NM 2008 4 17 2008UALA02091 1 20080410 A 3150 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 668UA 30024 LEFT PACK "OFF" LIGHT WITH ASSOCIATED "L PACK OFF" DISPLAYED IN CRUISE WITH PACK SELECTED TO "STBY" (REF DF583) DUCT PRE SSURE AND PRESSURIZATION NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041700146 20080417 00146 NM 2008 4 17 2008UALA02013 1 20080407 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 311UA 23672 FWD PIT DOORWAY AFT SIDE FRAME IS CRACKED AT INBD SIDE OF LOWER DOOR STOP FITTING. MAJOR REPAIR ACCOMPLISHED, INSTALLED A DOUBLER/TRIPLER AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700147 20080417 00147 NM 2008 4 17 2008UALA02015 1 20080407 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1241 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 AFT PIT LOWER FUSE FRAME SHEAR TIES HAVE CORROSION AT BS 1241 FROM STR 39R-35L. MAJOR REPAIR ACCOMPLISHED, REMOVED CORR OSION AND REPLACED SHEAR TIES. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041700154 20080417 00154 NM 2008 4 17 2008UALA02027 1 20080408 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY EXIT EEL LIGHTS INOP. ALL LEFT SIDE B ZONE SEATS, SEATS 6, 7 AND 8. FOUND SHORTED WALL EEL LIGHT ASSY BY LAV 110. REPLACED LIGHT ASSEMBLY. OPS. CHECKS. NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700163 20080417 00163 NM 2008 4 17 UIEA200800140 1 20080408 A 5343 084836250100 BOLT BOEING 747 747243B 1384830 NM MLG FITTING SHEARED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 RIGHT WING GEAR WHEEL WELL CENTER WING REAR SPAR RIGHT BULKHEAD FITTING ONE BOLT SUSPECTED SHEARED. BOLT REPLACED IAW B OEING MESSAGE NUMBER 1-801292679-4. 2 L 7 4 4F RT A20WE 2008041700165 20080417 00165 NM 2008 4 17 UIEA200800145 1 20080408 A 5311 FRAME BOEING 747 747243B 1384830 NM ZONE 200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK STA 1980 STRINGER 11R FRAME FOUND CRACKED. FRAME REPAIRED PER ATLAS EO NR 4753A141. 2 L 7 4 4F RT A20WE 2008041700170 20080417 00170 NM 2008 4 17 UIEA200800150 1 20080415 A 5730 PANEL BOEING 747 7472D3B 1384805 NM NR 8 SPOILER DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 RT WING UPPER FIXED TRAILING EDGE PANEL, OUTBOARD OF NR 8 SPOILER HAS AN AREA OF 5.0 INCH BY 2.0 INCH OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 2, SHEETS 1, 2 AND 5. PREPREG LAYUP 250 DEGREES F CURE P ER SRM 51-40-12. REFERENCE ATLAS AIR EO NR 4757A433. 2 L 7 4 4F RT A20WE 2008041700181 20080417 00181 NM 2008 4 17 QXEA200800373 1 20080411 A 3231 ROD END BOMBDR DHC8 DHC8402 1390042 NM MLG DOOR OUT OF RIG A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 409QX 4051 BOI - FLIGHT 2391 (BOI-SEA) - AFTER SELECTING GEAR UP THE LEFT GEAR DOOR LIGHT REMAINED ON. VISUAL INSPECTION CONFIRMED BOTH GEAR DOORS OPEN. USED ALTERNATE GEAR EXTENSION. FOUND THE LT ROD END OUT OF RIG ON THE LT MLG. REPLACED THE RET RACT ACTUATOR AND UPGRADED THE UPLOCK ACTUATOR TO 46500-9 STATUS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVIC E. 2 H 7 2 4T RT A13NM 2008041700190 20080417 00190 EA 2008 4 17 SWIA200819474 1 20080410 A 3244 TIRE CNDAIR CL600 CL6002B19 1900309 EA MLG FAILED A SWIA O OTHER O OTHER LD LANDING 1 NM 07 442SW 7609 FLT 3751 - NR 3 AND NR 4 MAIN TIRES FOUND DEFLATED AFTER LANDING. REPLACED NR 3 AND NR 4 MAIN WHEEL ASSEMBLYS IAW AMM 3 2-41-01, PN 5010571-1, SN OFF AUG04-6585, PN 5010571-1, SN OFF JULY01-4192. 2 L 7 2 4F RT A21EA 2008041700200 20080417 00200 EU 2008 4 17 08FDEA01418 1 20080415 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 658FE 752 CROSSBEAM AT FR 60 HAS 1 IN CRACK ON VERTICAL FLANGE, O/B OF SEAT TRACK 3 RT, - Y1456, ON AFT FACE REMOVED CRACK AND AC COMPLISHED FLOORBEAM REPAIR IAW A300-600 SRM 53-10-15, FIG 211. 2 L 7 2 4F RT A35EU 2008041800002 20080418 00002 NM 2008 4 18 ZZDA2008086 1 20080403 A 3350 8039251 POWER SUPPLY BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 932AT 55073 EPL LIGHTING IS OUT FROM SEATS 1D - 10D. REMOVED AND REPLACED BATTER PACK POWER SUPPLY ASSY B5-118. OPS CHECK GOOD REF AMM 33-51. 2 L 7 2 4F TR A6WE 20080711 EU 2008 7 11 AALA200801281 1 20080512 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 41063 506 MIA - EMERGENCY LIGHTS AT RIGHT SIDE AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT SIDE AF T CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20080711 NM 2008 7 11 AALA200801148 1 20080429 A 2612 FIRE DETECTOR BOEING 767 767323 1385205 NM NR 2 INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 361AA 24042 DFW INFLIGHT T2421/29APR - CREW REPORTED RIGHT NUMBER TWO FIRE LOOP INDICATION ON CLIMB-OUT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND LOWER FORWARD FIRE DETECTOR OPEN. REPLACED LOWER FORWARD FIRE DETECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080711 EU 2008 7 11 AALA200801224 1 20080506 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7083A 645 JFK - EMERGENCY LIGHT AT SEAT 21G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A35EU 20080711 EU 2008 7 11 AALA200801225 1 20080506 A 3350 PR010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 18066 509 JFK - EMERGENCY CABIN AISLE LIGHTS AT LEFT AFT DOOR INOPERATIVE FROM COCKPIT SWITCH 29C TO 37C. REPLACED BATTERY PACK FOR EMERGENCY CABIN AISLE LIGHTS AT LEFT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20080711 EU 2008 7 11 AALA200801199 1 20080504 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 11060 470 MIA - EMERGENCY LIGHT AT SEAT 10G LIGHT BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 10G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20080711 NM 2008 7 11 AALA200801247 1 20080507 A 3350 OL3071BPEGPL LAMP BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHT AT SEAT 21C MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 WP 2008 7 11 08FDEA01979 1 20080523 A 5350 ANB71064 PANEL DOUG MD10 MD1010F 3022112 WP FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 567FE 46994 FILLET PANEL NR 152 LT IS DENTED. REPAIRED DAMAGED AREAS (2 EACH) BY REPLACING THE CORE AND APPLYING WET FIBERGLASS OVE RLAYS IAW DC/MD-10 SRM 51-62-01; VOL II AND SRM 51-43-01; VOL II; PARA 16. RESTORED SURFACE FINISH IAW DC/MD-10 SRM 51- 21-02; VOL II. REMOVED AND REINSTALLED THE PANEL IAW DC/MD-10 SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 20080711 NM 2008 7 11 KCSA081257 1 20080526 A 5311 STIFFENER BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 FUSELAGE FRAME STIFFENERS (2EA) AND STRINGER CLIP DAMAGED AT BS 2280, STR-12R. 2 L 7 4 4F RT A20WE 20080711 EU 2008 7 11 DATA200800000 1 20080523 A 7722 UNKNOWN STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA UNKNOWN E DATA D RETURN TO BLOCK M OVER TEMP CL CLIMB 1 GL 13 936MA SH3036 PCE84302 FLIGHT CREW STARTED THE RIGHT ENGINE FIRST BECAUSE IT USUALLY STARTS COOLER. THE ITT PEAKED AT 780 DEGREES AND STABILIZ ED AT 630. THE GS GENERATOR GAUGE WAS SLOW TO RISE. THE PROBLEM OCCURRED NOTICEABLE AT V2, 90KTS, IT WAS AT 830 DEGEES ITT. TAKEOFF WAS CONTINUED AND AT CLIMB OUT THE ITT HAD RISEN TO 900 DEGREES. IT WOULD HAVE CONTINUED TO RISE IF PILO T HAD NOT REDUCED THE TORQUE. FLIGHT CREW CLIMBED TO 4000' AND THERE WAS A 200 DEGREE SPLIT BETWEEN LEFT AND RIGHT. RE DUCED THE TORQUE TO 1500 LBS AND THE GAUGE READ 740 DEGREES. CREW DECIDED TO RETURN TO MYR. 2 H 7 2 4T 4 T A41EU E4EA 20080711 EA 2008 7 11 MASA200800410 1 20080520 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR OUT OF ADJUST A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 518LR 10259 ASH 7276 AUS-IAD - SERVICE DOOR CAUTION MESSAGE IN FLIGHT. ADJUSTED DOOR PROX SENSOR, OPS GOOD. 2 L 7 2 4F RT A21EA 20080711 NM 2008 7 11 MASA200800416 1 20080524 A 3350 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN OUT OF POSITION A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 445YV 445 ASH FLT 7336 DEN-ASE. MAIN CABIN DOOR LOWER EMERGENCY EXIT LIGHT PUSHED IN. RE-SECURED, OPS GOOD. 2 H 7 2 4T RT A13NM 20080711 EA 2008 7 11 MASA200800418 1 20080524 A 3040 SCREW CNDAIR CL600 CL6002B19 1900309 EA RT WINDSHIELD LOOSE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 17358 7358 ASH FLT 2923, PHX-ICT. RT WINDSHIELD LOWER TERMINAL SMOKING/ARCING. MX FOUND TERMINAL SCREW NOT SECURED. MX SECURED S CREW AND SYSTEM OP GOOD. 2 L 7 2 4F RT A21EA 20080711 EA 2008 7 11 MASA200800419 1 20080524 A 4950 M832481154 PACKING CNDAIR CL600 CL6002B19 1900309 EA APU DEFECTIVE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 7305V 7305 ASH FLT 2781 BFL- OVERNIGHT. FUEL ODOR IN CABIN WITH PACKS ON APU BLEED. REMOVED AND REPLACED PACKING AND FUEL FEED WI GGINS FITTING. 2 L 7 2 4F RT A21EA 20080711 EA 2008 7 11 MASA200800420 1 20080525 A 3810 LINE CNDAIR CL600 CL6002B19 1900309 EA POTABLE WATER LEAKING A MASA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 07 570ML 7206 ASH FLT 7290 ROA-IAD. CREW REPORTED AN ELECTRICAL ODOR AND WATER LEAKING AT THE FWD POTABLE DRAIN AND THE AVIONICS DOOR . REPLACED SUCTION LINE. 2 L 7 2 4F RT A21EA 20080711 EA 2008 7 11 MASA200800423 1 20080526 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77195 7195 ASH 7172 ORD - AFT CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20080711 NM 2008 7 11 DHL2008764526 1 20080527 A 5313 STRINGER BOEING 727 727264 138408M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C-CHECK, PILLOWING AT FASTENERS AT RIGHT LWR FUSELAGE AT BS 350, 4 INCHES FWD OF NOSE JACK PAD. REPAIRED IAW S RM 53-10-3 FIG 1 DETAIL 2. MATERIAL USED P/N 95-24786-10 GUSSET / CHANNEL, REPAIR FOR 21R BAC 1496-138 DIM 11" PO 81598 7, CHANNEL SPLICE FROM BAC1493-412 9 .5 INCH PO 815987 2EA J-ANGLES FROM BAC 1493-513 7 .25 INCH PO 815987 AND 2EA FILLE RS FROM 7075T6 .050" PO 90063742 MIM 7" X .5 INCH. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 DHL2008764527 1 20080527 A 5311 FRAME BOEING 727 727264 138408M NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C-CHECK, DENT AT MAIN FRAME BS 580 BETWEEN STR 16 AND 17R. REPAIRED IAW SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3, 7 075T6 .050 DIM 7.125" X 6.25" PO 9006742. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 08FDEA02134 1 20080603 A 5753 BAC1503100046 ANGLE BOEING 727 727233 138408A NM RT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 274FE 22039 RT WING INBOARD MID FLAP LOWER AFT CHORD ANGLE IS CRACKED AT WBL 110. CUT OUT DAMAGED SECTION DIM 47 1/4 INCH IAW B727 SRM 51-10-1, FABRICATED FILLER REPAIR USING BAC1503-100046 7075-T6 PO NR 8177105 DIM 47 1/4 INCH BY 2 INCH AND SPLICE US ING BAC1503-100046 7075-T6 PO NR 8177105 IAW B727 SRM 51-30-5 AND 57-50-2 FIG 5. ALODINED AND PRIMED REPAIR PARTS IAW B 727 SRM 51-10-2. INSTALLED REPAIR ANGLES IAW B727 SRM 51-30-2 AND 51-40-4 FIG 1. 2 L 7 3 4F RT A3WE 20080714 NE 2008 7 14 DL76S080845 2 20080609 A 7200 CF680A2 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 FAILED A DALA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 27 131DN 56207 24852 580358 DURING CRUISE FLT FELT VIBS AND HEARD UNUSUAL NOISE VIBS AT5.0. WHILE PERFORMING WALKAROUND CHECK FOUND METAL IN TAILPI PE OF THE NR 2 ENG. ENG CHG IN PROGRESS. 2 L 7 2 4F 4 F RT A1NM E13NE 20080714 NM 2008 7 14 UPS08652337 1 20080515 A 5711 112T22524 STIFFENER BOEING 767 76734AF 1385212 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 302UP 27240 INSPECTION TYPE:N/A LEFT WING LES 665 FRONT SPAR STIFFENER UPPER AREA FOUND CRACK. CRACK LENGTH .5 INCH APPROX . LEFT WING LES 665 FRONT SPAR STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20080714 2008 7 14 DL764080774 4 20080524 A 3160 COMPUTER BOEING 767 767432ER 1385134 NM MALFUNCTIONED A DALA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 842MH 29715 RTB DUE TO NO OIL PRESS INDICATION ON RT ENG. FOUND RT DPC FAILED FWD TO MCO AND PLAC PER MEL 31-63-04 OIL PRESS INDICA TION WAS BLANK. MAINTENANCE RAN ENG AFTER IFSD OPN AND OPS OK THEN. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 UPS08652338 1 20080514 A 5720 1142300272 WEB BOEING 767 76734AF 1385212 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 302UP 27240 INSPECTION TYPE:N/A RIGHT WING LES 679 FWD D-NOSE SUPPORT WEB FOUND CRACK AT LOWER AREA. CRACK LENGTH 2 INCHES TO 2.5 I NCHES APPROX. RIGHT WING FWD D-NOSE SUPPORT WEB REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 JUST BETWEEN OS S648 AN 694 AREA. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 08FDEA02422 1 20080624 A 5310 655612571 DOOR FRAME BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 AFT PIT DOOR OPENING AFT FRAME STA 990 IS CORRODED ON LOWER SURFACE OF FRAME, UPPER ANGLE BETWEEN STR 26R AND STR 27R RE MOVED CORROSION, FORMED REPAIR ANGLE, HEAT TREATED AND CAD PLATED REPAIR ANGLE. INSTALLED REPAIR ANGLE. REFERENCE EA N R 75310-113992. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 08FDEA02423 1 20080624 A 5340 6545313Y2 STRINGER CLIP BOEING 727 727225 1384077 NM BS 760 S5R CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 STRINGER CLIP CRACKED AT LOWER O/B RADIUS STR 5R STA 760 REPLACED STRINGER CLIP TO STR 5, STA 760 REF SRM 51-30-2 PG 10. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 08FDEA02424 1 20080624 A 5340 69690852 STRINGER CLIP BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 FWD LWR PIT BILGE, CORROSION ON INBD SIDE OF STR CLIP AT FWD SIDE OF FRAME AT STA 480 STR 26R. REMOVED AND REPLACED STR CLIP AT FWD LWR, PIT BILGE STA 480, STR 26R, FWD SIDE REF SRM 51-30-02 PG 1-5. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 DLM90080789 1 20080520 A 5320 INTERCOSTAL DOUG MD90 MD9030 3023690 NM BS 1360 BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 INTERCOSTAL AT FS 1360 BLO TO HAVE A SECTION OF UPPER FLANGE BROKEN OFF. REPAIRED INTERCOSTAL, IAW DELTA ER/A 12670 DAT E 5/19/08 REV I/R. 2 L 7 2 4F RT A6WE 20080714 NE 2008 7 14 DL75E080790 2 20080527 A 7321 FCU BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE NR 1 ENGINE MALFUNCTIONED A DALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 718TW 25876 28486 728712 MAINTENANCE ATTEMPTING TO REPOSITION A/C STARTED NR 1 ENG AND TRIED TO ADVANCE THE THROTTLES WHEN THE ENGINE ROLLED BACK AND THEY HAD A TAIL PIPE FIRE WHICH THEY BLEW OUT. PERFORMED BORO, NO DAMAGE FOUND. REPLACED FCU AS PRECAUTIONARY. N O EPCS MESSAGES WERE FOUND. FOUND IGVS OUT OF RIG, ADJUSTED IGV'S AND VSV'S. DUE TO HISTORY MAINTENANCE FERRIED TO ATL FOR ENGINE REPLACEMENT. 2 L 7 2 4F 4 F RT A2NM E17NE 20080714 NM 2008 7 14 DL757080793 1 20080530 A 5312 148N2332 STRUCTURE BOEING 757 757232 1384965 NM BS 1720 S19L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 DURING HMV AT SAA, CORROSION WAS FOUND ON THE HORIZONTAL AFT CHORD OF THE AFT PRESSURE BULKHEAD, FORWARD SIDE AT STA 172 0, S-19L. THE CORROSION WAS REPAIRED PER BOEING INSTRUCTIONS AS DOCUMENTED IN ER/A 06-468363-14. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 DLM88080794 1 20080524 A 5230 STRUCTURE DOUG MD88 MD88 3023688 NM CARGO DOOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 963DL 49982 TRANSFERRED FROM OMI C/N C12317161 DUE ERA 465882-14 REV A CODE 9-53-31-20 ACTL 2300 FWD CARGO DOOR CUTOUT FORWARD EDGE DAMAGE. ACCOMPLISHED PERMANENT REPAIR IAW ERA 465882-14 REV A. 2 L 7 2 4F RT A6WE 20080714 EU 2008 7 14 WRNA20080039 1 20080526 A 3230 A2519903 CONTROL VALVE AIRBUS 300 A300B4203 3930306 EU LANDING GEAR FAULTY A WRNA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 05 504TA 216 DURING APPROACH TO BQN, LANDING GEAR FAILED TO EXTEND WITH SYSTEM 1 OR 2, RETURNED TO 2,000 FEET TO HOLD WHILE LOWERING GEAR MANUALLY. AFTER SUCCESSFUL EXTENSION OF GEAR, A SAFE LANDING WAS MADE. FIM 32-30-00 /107 INDICATED A FAULTY LANDI NG GEAR ELECTROVALVE. REPLACED LANDING GEAR ELECTROVALVE IAW MM 32-31-12 PAGE 401. PERFORMED SYSTEM OPS TEST PER 32-31 -12 PAGE 501, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 KCSA081260 1 20080527 A 5412 BULKHEAD BOEING 747 7472B4B 138481B NM NR 4 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 4 ENG FWD MOUNT HANGER CHORD CHAFED ON O/B SIDE NAC STA 128.95. 2 L 7 4 4F RT A20WE 20080714 NM 2008 7 14 2008UALA02963 1 20080522 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 821UA 944 RIGHT EXT FUSE SKIN DENTED AND GOUGED AT FRAME 20 PLUS 6 INCHES AT STR 29R. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAI R DOUBLER. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041800005 20080418 00005 2008 4 18 HNAA0800125 4 20080402 A 3425 7003360941 AHRS DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 940HA 29290 41 156 DURING FLIGHT, THE CAPTAINS AHRS FAILED CAUSING THE ADI AND HSI TO TUMBLE. BOTH F/DS BECAME INOPERATIVE. SAHS WAS SELE CTED AND A SLIGHT MISMATCH WAS NOTED. AN AIR TURNBACK WAS PERFORMED BUT NO EMERGENCY WAS DECLARED. UPON RETURN TO FIEL D, MAINTENANCE REPLACED THE NR 1 AHRS COMPUTER. OPS CHECKS WERE GOOD AT THAT TIME AND THE AIRCRAFT WAS RETURNED TO SERV ICE. 2 H 7 2 4T RT A13NM 2008041800010 20080418 00010 NM 2008 4 18 USAA920080755 1 20080406 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 512AU 23595 FLT 1452 - TPA-DCA - EEL - 19C EMERGENCY EXIT LIGHT INOP. MAINTENANCE REPAIRED BROKEN WIRE AND RELAMPED. OPERATIONAL C HECK WAS GOOD. 2 L 7 2 4F RT A16WE 2008041800016 20080418 00016 NM 2008 4 18 WRLA2008042 1 20080407 A 5753 HINGE FITTING DOUG MD11 MD11F 3023600 NM PWA 4060 PW4060 52119 NE T/E FLAP CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 48407 LEFT OUTBOARD FLAP CENTER BOX INBOARD AFT HINGE SUPPORT CRACKED. R&R LT OUTBOARD FLAP IAW AMM 27-60-30. 2 L 7 3 4F 4 F RT A22WE E24NE 2008041800019 20080418 00019 NM 2008 4 18 USAA920080773 1 20080312 A 5311 6546552 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN - MAJOR REPAIR - C18 CHECK - CRACKED FRAME, BS 827, S8L - S9L. REPAIRED FRAME, BS 827, S8L - S9L IAW USAIRWAYS EO 5 311-01019. 2 L 7 2 4F RT A16WE 2008041800022 20080418 00022 SO 2008 4 18 C2XA08CL043 1 20080404 A 2742 3833001009 ACTUATOR EMB 145 EMB145LR 3260212 SO STABILIZER FAULTY A C2XA B EMER. DESCENT F FLT CONT AFFECTED CR CRUISE 1 SW 27 13914 16782 145430 CLE FLIGHT 2898 THE CREW REPORTED A YAW TRIM RUNAWAY IN FLIGHT. QRH WAS FOLLOWED AND FOUND BOTH SYSTEMS TO BE INOPERATI VE. EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE YA W TRIM SWITCH AND ACTUATOR. OPERATIONAL CHECKS WERE GOOD. SWITCH P/N 79-2257. 2 L 7 2 4T RT T00011AT 2008041800031 20080418 00031 SO 2008 4 18 FDKA200804149 1 20080405 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN NOT SEATED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 FDM 6073 JFK-ORF (0855 PHX LCL). SERVICE DOOR EMERGENCY LIGHT OUT. MX RESEATED THE CONNECTOR AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 2008041800035 20080418 00035 WP 2008 4 18 ABXA080119 1 20080405 A 2433 6RW176YN3 TRANSFORMER DOUG DC9 DC932 3022066 WP E/E BAY DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 900AX 3758 47380 ELECTRICAL SMELL IN COCKPIT, WORSE WITH EMERGENCY POWER SELECTED ON. FOUND SMELL TO BE WORSE IN FORWARD ACCESSORY COMPA RTMENT. NO SIGNS OF OVERHEATED OR BURNING EQUIPMENT WITH POWER ON. DETERMINED ODOR TO BE RESIDUAL FROM RIGHT TRANSFORM ER RECTIFIER THAT WAS REPLACED ON PREVIOUS FLIGHT. 2 L 7 2 4F A6WE 2008041800038 20080418 00038 NM 2008 4 18 BB08053 1 20080406 A 2560 P4010021 BATTERY BOEING 757 7572S7 1384962 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 906AW 23568 OGG - THE 2L DOOR FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN THE FLASHLIGHT AT DOOR 2L. OPERATION ALLY CHECKS OK. 2 L 7 2 4F RT A2NM 2008041800043 20080418 00043 NM 2008 4 18 USAA920080760 1 20080405 A 5330 148T3121 SKIN BOEING 767 767201 1385125 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246AY 23898 MIA - MAJOR REPAIR - C3 CHECK - CRACKED FUSELAGE, BS 1654.5, S3R - S8R. REPAIRED FUSELAGE, BS 1654.5, S3R - S8R IAW B7 67 SRM 53-80-01. 2 L 7 2 4F RT A1NM 2008041800045 20080418 00045 EU 2008 4 18 USAA920080762 1 20080401 A 5210 FE240221001 DIAPHRAGM AIRBUS 330 A330323 3930335 EU L4 DOOR LEAKING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AY 337 BFM - EES - C2 CHECK - THE L4 DOOR ASSIST BOTTLE CANNOT BE SERVICED. REPLACED THE L4 DOOR DAMPER DIAPHRAGM AND SERVICED DAMPER IAW A330 AMM 52-10-00. 2 L 7 2 4F RT A46NM 2008041800046 20080418 00046 NM 2008 4 18 USAA920080763 1 20080324 A 5320 D53480079276 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802AW 924 SAL - MAJOR REPAIR - C7 CHECK - CRACK ON CABIN SHEAR PLATE, BS 3257 / FR 68 - BS 3310 / 69, +Y1732. REPLACED CABIN SHEA R PLATE, BS 3257 / FR 68 - BS 3310 / 69, +Y1732 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008041800051 20080418 00051 NM 2008 4 18 USAA920080768 1 20080324 A 5320 D53471124201 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802AW 924 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / 70, -Y1732. REPLACED CABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / 70, -Y1732 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008041800053 20080418 00053 NM 2008 4 18 USAA920080770 1 20080324 A 5315 D53472189204 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802AW 924 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3207 / FR 67 - BS 3310 / 69, -Y1292. REPLACED CABIN FL OORBEAM, BS 3207 / FR 67 - BS 3310 / 69, -Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008041800054 20080418 00054 NM 2008 4 18 USAA920080775 1 20080403 A 5315 FLOORBEAM BOEING 767 767201 1385125 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246AY 23898 MIA - MAJOR REPAIR - C3 CHECK - CORROSION ON CABIN FLOORBEAM, BS 347, RBL 45. REPLACED CABIN FLOORBEAM, BS 347, RBL 45 IAW USAIRWAYS EA 110628. 2 L 7 2 4F RT A1NM 2008041800057 20080418 00057 SO 2008 4 18 RAIA00804004 1 20080402 A 3260 PROXIMITY SENSOR EMB 145 EMB145EP 3260221 SO NLG FAULTY A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 827HK 145021 FLT 5489 -STL- CREW RECEIVED A LG AIR/GND FAIL MESSAGE ON THE EICAS SHORTLY AFTER T/O. GEAR WOULD NOT RETRACT. MAINTEN ANCE REMOVED AND REPLACED THE NOSE WOW SWITCH AND RT MAIN AFT DOWNLOCK PROXIMITY SWITCH. 2 L 7 2 4F RT T00011AT 20080714 NM 2008 7 14 2008UALA02973 1 20080523 A 2820 LINE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FUEL SYSTEM BROKEN A UALA O OTHER W INADEQUATE Q C CL CLIMB 1 WP 29 217UA 30550 UNWANTED FUEL TRANSFER TO RIGHT MAIN JUST AFTER TAKEOFF. LINE WAS BROKEN AT RIGHT MAIN TANK SHUT OFF VALVE. REPLACED RT TANK FLOAT SHUTOFF VALVES AND MADE NEW LINE TO RT TANK OUTLET FLOAT SHUT OFF VALVE REPLACED FUEL CONTROL UNIT. OP CHKS & LEAK CHKS GOOD. FOUND RT FWD BOOST PUMP DISCHARGE CHECK VALVE LEAKING. REPLACED RT FWD BOOST PUMP DISCHARGE CHECK VALV E. REPLACED FUEL QTY PROCESSOR. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080714 NM 2008 7 14 SWAA083416 1 20080622 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 DHL2008764506 1 20080520 A 5311 FRAME BOEING 727 727264 138408M NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C CHECK REF N/R 098177, DENT ON MAIN CABIN FRAME BS 600 BETWEEN STR 16 AND 17R. REPAIRED IAW B727 SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3 MATERIAL 7075-T6 .050 INCH DIMENSION 7 INCH BY 5 1/4 INCH PO NR 9006153. 2 L 7 3 4F A3WE 20080708 EA 2008 7 8 COMA0880008 1 20080517 A 3230 LANDING GEAR CNDAIR CL600 CL6002D24 1390016 EA NLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 678CA 15125 FLIGHT 5099 - GEAR DISAGREE MESSAGE RECEIVED ON CLIMB. NOSE GEAR NOT RETRACTING. DECLARED EMERGENCY, FOLLOWED QRH, RET URNED TO CVG, ALL GEAR SHOWED GREEN, LANDED WITHOUT INCIDENT. VISUALLY INSPECTED NOSE GEAR, PERFORMED EXTENSION AND RET RACTION CHECKS. NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 20080708 NM 2008 7 8 CALA0800512 1 20080531 A 5320 69487472 ATTACH ANGLE BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17644 28905 INTERCOSTAL WEB ATTACH ANGLE IS CRACKED AT STATION 360 S4L. REPAIRED INTERCOSTAL WEB ATTACHMENT AT STATION 360 S4L PER EC/RA 5310-04778 AND PACE EA 644-53-003 CAL. 2 L 7 2 4F RT A16WE 20080708 NM 2008 7 8 DL757080880 1 20080617 A 5320 WEB BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 RT SIDE MAIN CABIN FLOOR STRUCTURE IS CORRODED AT FS 1420-1440 LOWER WEB FWD END. REPLACED DAMAGED WEB IAW SRM'S 51-20- 02 AND 51-40-02. 2 L 7 2 4F RT A2NM 20080708 NM 2008 7 8 DL757080861 1 20080612 A 5330 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 647DL 24218 DENT ON LT SIDE FUSELAGE STA 408 GOES ACROSS STR 16L AND 2 BAYS. REPAIRED DAMAGE IAW SRM 53-00-01. 2 L 7 2 4F RT A2NM 20080710 NM 2008 7 10 DL777080725 1 20080513 A 2530 72077500 OVEN BOEING 777 777232 1385232 NM MID GALLEY DEFECTIVE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 860DA 29951 ELEC SMELL IN MID GALLEY NR 1 OVEN SHUTDOWN TURNED OFF SMELL DISSIPATED. REMOVED NR 1 OVEN AND INSP WIRING BEHIND OVEN AND OVEN ELEC CONNECTOR. NO TROUBLE FOUND. REMOVED AND STOWED OVEN ELEC CONNECTOR. PULLED AND COLLARD OVEN NR 1 C/BS FWD TO NEF USING FRC 253.30. REPLACED OVEN, CKS GOOD, REMOVED MCO. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS. 2 L 7 2 4F RT T00001SE 20080710 NM 2008 7 10 DL76L080746 1 20080418 A 3397 CONNECTOR BOEING 767 767332 1382001 NM CABIN INCORRECT A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 188DN 27583 EEL SEAT FEEDERS AT STA 900 LEFT HAS WRONG CONNECTORS. REMOVED AND REPLACED EELS CONNECTOR AT STA 900, EELS AISLE LIGHT ING OPS CHECK GOOD IAW B767-300 MM 33-51-10. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 DL76L080758 1 20080508 A 3397 CONNECTOR BOEING 767 767332 1382001 NM COCKPIT NOT SEATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 WITH COCKPIT P-5 EMERGENCY LIGHTS SWITCH OFF, WHEN ACFT POWER IS REMOVED, EMERGENCY LIGHTS COME ON AND WHEN SWITCH PLACE D IN ARMED, LIGHTS GO OFF. RESEATED CONNECTOR D1650P AT P22 PANEL IAW BSWPM 20-60-06 AND OPS CHECK GOOD IAW DAL B767-30 0 MM 33-51-00 AND WDM 33-51-11. 2 L 7 2 4F RT A1NM 20080710 NM 2008 7 10 USAA920081103 1 20080515 A 5754 65C26602224 SKIN BOEING 737 7374B7 1384702 NM L/E SLAT DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 444US 24862 CLT - MAJOR REPAIR - C2 CHECK - RIGHT WING NR 5 SLAT UPPER SURFACE TRAILING EDGE IS DISBONDED. REPAIRED THE RIGHT WING NR 5 SLAT UPPER SURFACE TRAILING EDGE IAW USAIRWAYS TYPICAL REPAIR 57-42-02. 2 L 7 2 4F RT A16WE 20080710 NM 2008 7 10 AALA200801114 1 20080427 A 3350 LAMP BOEING 757 757223 1384957 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 611AM 24487 DFW - EXTERNAL EMERGENCY LIGHT AT LEFT HAND FORWARD OVERWING AFT INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIG HT AT LEFT HAND FORWARD OVERWING AFT POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080710 NM 2008 7 10 2008UALA02822 1 20080515 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 AFT PIT STA 1560, STR 26L, FRAME DENTED. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED DAMAGE FAB AND INSTALL RPR IAW SRM 53-00-07. THIS IS A CAT B RPR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSP STARTING AT 50000 TOTAL FC AND 12000FC THEREAFTE R. INSP PER SRM 53-00-07 RPR 5 TABLE II. INSP CONSISTS OF BOTH VISUAL AND NDT. CURRENT PTC IS 20417. -INF- :MF2632 OPENED TO CHECK AT MAX PTC 62000 & EVERY 12000C THEREAFTER. 2 L 7 2 4F 4 F RT A2NM E17NE 20080710 NM 2008 7 10 2008UALA02823 1 20080515 A 5210 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 DOOR 2L HAS A SKIN DENT. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 52- 10-01. 2 L 7 2 4F 4 F RT A2NM E17NE 20080710 NM 2008 7 10 2008UALA02935 1 20080521 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EXIT EEL LIGHT INOP AT SEAT ROW 32 LEFT. REPLACED LIGHT ASSY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080711 NM 2008 7 11 UPS08652321 1 20080513 A 5320 146T56516 SUPPORT BRACKET BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 302UP 27240 INSPECTION TYPE:C BULK CARGO STA 1580 RBL 75 FLOOR PANEL SUPPORT BRACKET CRACKED. CRACK THROUGH 2 INCH APPROX. BULK CA RGO STA 1580 RBL 75 FLOOR SUPPORT BRACKET ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20080711 NM 2008 7 11 AALA200801210 1 20080504 A 2781 PSEU BOEING 767 767323 1385205 NM L/E SLAT FAULTY A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 381AN 25450 MIA INFLIGHT T381/04MAY - CREW REPORTED ALERT TWO LEADING EDGE ASYMMETRY MESSAGE. LANDED MIA WITHOUT INCIDENT. FOUND N UMBER FIVE SLAT INBOARD PROXIMITY SWITCH ELECTRONIC UNIT FAULTING. REPLACED PROXIMITY SWITCH ELECTRONIC UNIT. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080711 EU 2008 7 11 AALA200801205 1 20080504 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 11060 470 MIA - EMERGENCY LIGHT AT SEAT 24G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A35EU 20080711 EU 2008 7 11 AALA200801202 1 20080504 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 11060 470 MIA - EMERGENCY LIGHT AT SEAT 33G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 33G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A35EU 20080711 WP 2008 7 11 AALA200801183 1 20080502 A 2560 5961568501 CAM DOUG DC9 DC983 3022083 WP TAILCONE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 565AA 49347 TUL - TAILCONE RELEASE MECHANISM CAM IS WORN. REPLACED TAILCONE MECHANISM CAM ASSEMBLY. SYSTEM GROUND CHECKED NORMAL O PERATION. 2 L 7 2 4F RT A6WE 20080711 WP 2008 7 11 AALA200801189 1 20080503 A 3350 0201804001 LENS DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 400AA 49311 LGA - EMERGENCY LIGHT AT SEAT ROW 23 HAS LENS LOOSE. REPLACED LENS COVER FOR EMERGENCY LIGHT AT SEAT ROW 23. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080711 WP 2008 7 11 AALA200801298 1 20080513 A 2560 1001191 LIGHT DOUG DC9 DC982 3022082 WP FLASHLIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7532A 49924 DFW - FORWARD CHARGEABLE EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED LIGHT UNIT FOR FORWARD CHARGEABLE EMERGENCY FLASHLI GHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080711 NM 2008 7 11 AALA200801227 1 20080506 A 3350 LENS BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 935AN 30081 DFW - EMERGENCY LIGHT AT SEAT ROW 14 HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 14. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080711 WP 2008 7 11 AALA200801176 1 20080501 A 2530 OVEN DOUG DC9 DC982 3022082 WP GALLEY DIRTY A AALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 274AA 49271 STL INFLIGHT T311/274 - FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL AND SMOKE EVIDENCE. TURNED OFF GALLEY POWER AND CAB IN LIGHTS. SMOKE WAS LOCALIZED TO FORWARD GALLEY AND FORWARD SECTION OF FIRST CLASS. SMOKE DISSIPATED DURING APPROACH. RETURNED TO STL AND LANDED WITHOUT INCIDENT. AIRCRAFT OUT OF SERVICE FOR EVALUATION. REMOVED LARGE AMOUNT OF BURNED FOOD FROM UNDER OVEN INTERIOR. REPLACED OVEN ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080711 NM 2008 7 11 AALA200801177 1 20080502 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT AT SEAT 25G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080728 EA 2008 7 28 TRAX200800675 1 20080520 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 POSSIBLE CRACK AT LBL 27 UNDER LT SIDE COCKPIT ATTACHES TO FLOOR AND FRAME 280 STRUCTURE AREA IS MARKED. REPAIRED COCKPI T FLOOR INTERCOSTAL AT FS 280 AND LBL 33.0 IAW REO 670-53-11-304. REFER TO ATTACHED M-234 FOR WORK PERFORMED. EC/TC REO 670-53-11-304 COMPLIED WITH. JOB COMPLETE. 2 L 7 2 4F RT A21EA 20080711 NM 2008 7 11 08FDEA01977 1 20080523 A 5414 311N504633 SKIN PANEL BOEING 757 75727B 1384921 NM NR 2 PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 916FD 24137 SURFACE CORROSION ON PYLON NUMBER TWO LEFT SIDE PANEL INNER SKIN FORWARD OF ACCESS PANEL 443HL, PPS 124 TO PPS 200. EVALUATE AND RECTIFY. PYLON NUMBER TWO LEFT SIDE SKIN PANEL LOCATED FORWARD OF ACCESS PANEL 443HL REPLACED IN ACCORDA NCE WITH BOEING DRAWING 311N5046 SHEET 2, 311N5002 AND B757-200 SRM 51-10-02 REVISION 93. REPAIR CLASSIFIED AS MAJOR AS PEF FEDEX GMM 6-2-100. 2 L 7 2 4F RT A2NM 20080711 EA 2008 7 11 MASA200800409 1 20080519 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 916FJ 15016 ASH 2812 PHX-OKC - PILOT REPORTED THAT THE EMERGENCY CEILING LEVEL FLOOD LIGHT 3RD FROM FRONT IS INOP. MX RELAMPED AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20080711 EU 2008 7 11 AALA200801280 1 20080512 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 41063 506 MIA - EMERGENCY LIGHTS AT RIGHT SIDE MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT SIDE M ID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 DL76L080783 1 20080529 A 5411 311T311020 SPAR BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 176DN 25061 CRACKS AT PASSTHROUGHS IN NR 2 PYLON UPPER SPAR WEB. CRACKS WERE CUT OUT AND DOUBLERS INSTALLED. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 DL76L080795 1 20080528 A 5414 SKIN BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 194DN 28451 NR 2 PYLON I/B SIDE TRAPEZOIDAL CUTOUT UPPER FWD CORNER PYLON SKIN HAS CRACK. REPAIRED I/B STRUT SIDE SKIN AT AFT TRAPE ZOIDAL ACCESS DOOR NR 2 PYLON PER SRM 54-53-01 REPAIR 7 FIG 201 SHTS 1-4. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 SWAA083417 1 20080622 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008041800058 20080418 00058 SO 2008 4 18 RAIA00804005 1 20080404 A 3222 STRUT EMB 145 EMB145EP 3260221 SO NLG LOW A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 827HK 145021 FLT 5549 -STL- CREW RECEIVED A LG AIR/GRN FAIL MESSAGE ON THE EICAS. GEAR HANDLE WOULD NOT MOVE. MAINTENANCE SERVICED THE NLG STRUT AND PERFORMED SEVERAL SUCCESSFUL LANDING GEAR OPERATIONAL CHECKS WITH NO ADDITIONAL DEFECTS NOTED. 2 L 7 2 4F RT T00011AT 2008041800071 20080418 00071 SO 2008 4 18 C2XA08IA105 1 20080403 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11544 145557 IAH - DURING MAINTENANCE INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008041800075 20080418 00075 SO 2008 4 18 C2XA08IA107 1 20080408 A 2560 P2070009520 FLASHLIGHT EMB 135 EMB135LR 3260305 SO CABIN SHORTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 14516 145323 IAH - FLIGHT 2856, THE CREW REPORTED AN ELECTRICAL SMELL COMING FROM THE FWD FLIGHT ATTENDANT FLASHLIGHT THAT GOES AWAY WHEN DISCONNECTED FROM THE BASE. MAINTENANCE REMOVED AND REPLACED THE FWD LIGHT ATTENDANT FLASH LIGHT ASSY INCLUDING TH E HOLDER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008041800077 20080418 00077 SO 2008 4 18 FDKA200804154 1 20080408 A 5210 SEAL EMB 145 EMB145LR 3260212 SO PAX DOOR DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FDM 5994 BNA-BOS (1910 PHX LCL). MAIN CABIN DOOR DIFFICULT TO CLOSE. MX CLEANED AND LUBED DOOR SEAL OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 2008041800084 20080418 00084 SO 2008 4 18 C2XA08ON112 1 20080407 A 2810 2770138101 FLAPPER VALVE EMB 145 EMB145XR 3260214 SO RT WING WORN A C2XA D RETURN TO BLOCK K FLUID LOSS TO TAKEOFF 1 SW 27 27190 7102 7102 14500934 FLT 220 - ABQ - FLIGHT CREW REPORTED FUEL LEAKING FROM RIGHT WING / OVERWEIGHT LANDING TOUCH DOWN 46,600, 100FPM. THE C REW RETURNED TO BLOCK AND DECLARED AN EMERGENCY AND LANDED SAFELY WITHOUT INCIDENT. MX REMOVED AND REPLACED RT WING MOS T OUTBOARD FLAPPER VLV, OPERATIONALLY CHECKED SATISFACTORY. OVERWEIGHT LANDING IS PERMITTED AT SINK RATE INCODE IAW EMB 145 EC0550-01004. 2 L 7 2 4F RT 2008041800101 20080418 00101 NM 2008 4 18 USAA920080791 1 20080308 A 5320 146N52407 ANGLE BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 908AW 24233 MCN - MAJOR REPAIR - C3 CHECK - LEVEL 2 CORROSION ON ANGLE, BS 1715, RBL 33 - RBL 39, WL 208. REPLACED ANGLE, BS 1715, RBL 33 - RBL 39 IAW B757 SRM 51-30-01. 2 L 7 2 4F RT A2NM 2008041800102 20080418 00102 NM 2008 4 18 USAA920080792 1 20080308 A 5330 148N3770 SKIN BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 908AW 24233 MCN - MAJOR REPAIR - C3 CHECK - LEVEL 2 CORROSION ON FUSELAGE SKIN, BS 1941 - BS 1992.8, S26L - S26R. REPAIRED FUSELAGE SKIN, BS 1941 - BS 1992.8, S26L - S26R IAW B757 SRM 51-70-10-2R4. 2 L 7 2 4F RT A2NM 2008041800104 20080418 00104 EU 2008 4 18 08FDEA01421 1 20080416 A 5230 A5237407820000 DOOR FRAME AIRBUS 310 A310 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT DOOR, LWR FWD CORNER, GOUGED. FOUND GOUGE TO BE OUT OF LIMITS IAW SRM 51-10-00. REMOVED AND REPLACED EDGE SECTIO N IAW SRM 51-40-21. FOR ADJUSTMENT AND CHECK SEE WC 41X5114ALI. 2 L 7 2 4F RT A35EU 2008041800105 20080418 00105 NM 2008 4 18 USAA920080795 1 20080308 A 5754 114N407639 PANEL BOEING 757 7572G7 1384963 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 908AW 24233 MCN - MAJOR REPAIR - C3 CHECK - RIGHT WING NR 10 SLAT COVE PANEL CRACKED, WS 707 - WS 736. REPLACED RIGHT WING NR 10 SL AT COVE PANEL IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008041800109 20080418 00109 NM 2008 4 18 SA08027 1 20080410 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 825AW 1527 PIT - THE FLASHLIGHT UNDER THE AFT FLIGHT ATTENDANT JUMPSEAT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. OPERATI ONALLY CHECKS GOOD. 2 L 7 2 4F RT A28NM 2008041800113 20080418 00113 SO 2008 4 18 C2XA08RI051 1 20080330 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 18982 145223 FLIGHT 3132 - EWR - THE FLIGHT CREW REPORTED AFT GALLEY WALL EMERGENCY LIGHT NOT ILLUMINATING. EWR MX REMOVED AND REPLA CED AFT GALLEY WALL EMERGENCY LIGHT INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RET URN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008041800120 20080418 00120 EA 2008 4 18 A6WA200840174 1 20080308 A 5710 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA LT WING DAMAGED A A6WA O OTHER O OTHER LD LANDING 1 GL 31 462AW 7875 WINDSHEAR DURING LANDING LEFT WING PUSHED UP AND RIGHT WINGSTRIP SCRAPED RUNWAY. (M) 2 L 7 2 4F RT A21EA 2008041800126 20080418 00126 EA 2008 4 18 A6WA200840221 1 20080314 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 PAX DOOR AFT SIDE PANEL, QTY TWO CRACKS EXIST AT 4 AND 5 STEP. PAX DOOR AFT SIDE PANEL REPAIRED IAW 601R-52-11-702 REV A. (M) 2 L 7 2 4F RT A21EA 2008041800128 20080418 00128 SO 2008 4 18 C2XA08TY044 1 20080412 A 3350 20133A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13989 145271 TYS - DURING A SERVICE ROUTINE, THE AFT CABIN EMERGENCY LIGHTS WERE FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE AF T CABIN EMERGENCY BATTERY NR 4 IAW EMB 145 MM 33-50-04. OPS CHECK GOOD. A/C RELEASED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008041800129 20080418 00129 NM 2008 4 18 08FDEA01429 1 20080416 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 619FE 48770 UPPER CARGO DOOR CUT OUT, NR 1 LOWER JAMB SUPPORT FITTING CRACKED. REMOVED & REPLACED AS PER SRM 51-33-01 VOL.II. MOUNT ING HOLES ON NR 1 JAMB BEAM REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG. 10 VOL.I. CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041800130 20080418 00130 NM 2008 4 18 08FDEA01430 1 20080416 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 619FE 48770 UPPER CARGO DOOR CUT OUT, NR 2 LOWER JAMB SUPPORT FITTING CRACKED. REMOVED & REPLACED PER SRM 51-33-01 VOL.II. MOUNTING HOLES ON NR 2 JAMB BEAM REPAIR CARRIED OUT PER SRM 53-50-00 FIG. 10 VOL I. CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-10 0. 2 L 7 3 4F RT A22WE 2008041800131 20080418 00131 NM 2008 4 18 08FDEA01431 1 20080416 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 619FE 48770 UPPER CARGO DOOR CUT OUT, NR 3 LOWER JAMB SUPPORT FITTING CRACKED. REMOVED & REPLACED PER SRM 51-33-01 VOL.II. MOUNTING HOLES ON NR 3 JAMB BEAM REPAIR CARRIED OUT PER SRM 53-50-00 FIG 10 VOL.I. CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-10 0. 2 L 7 3 4F RT A22WE 2008041700121 20080417 00121 NM 2008 4 17 2008UALA01987 1 20080406 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 32HJK INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 SEAT 32 HJK EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE, RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700125 20080417 00125 NM 2008 4 17 KCSA081221 1 20080409 A 5311 FRAME BOEING 747 747SR46 1384816 NM BS 1760 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 BS 1760 FUSELAGE FRAME LOWER CHORD DAMAGED BETWEEN STR-39R AND STR-40R. 2 L 7 4 4F RT A20WE 2008041700129 20080417 00129 NM 2008 4 17 2008UALA01994 1 20080407 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 DOOR 1 LEFT FWD SILL EMERGENCY LIGHT IS INOP. FOUND FAULTY LAMP. REPLACED LAMP OP CHECKED NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700130 20080417 00130 NM 2008 4 17 2008UALA01995 1 20080407 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 LEFT OVERWING AFT EMERGENCY LIGHT ASSY FWD LAMP IS INOP. REPLACED BULB OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700132 20080417 00132 NM 2008 4 17 2008UALA01997 1 20080405 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 3A INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EEL LIGHT INOP AT SEAT 3A. SUPPLEMENTAL DATA UPDATE, REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700143 20080417 00143 NM 2008 4 17 2008UALA02010 1 20080408 A 2611 80600031600U8446 FIRE DETECTOR BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE APU BAY INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 932UA 26658 APU FIRE SUPPRESSION SYS INOP. REPLACED APU FIRE EXTINGUISHER BOTTLE ASSY. ENGINE & APU FIREX BOTTLE RUPTURE DISC ASSY & ENG/APU FIRE CONTROL P8-1 MODULE PRINTED CIRCUIT.TROUBLESHOOT AND REPAIRED "APU FIRE DET LIGHT". 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700159 20080417 00159 NM 2008 4 17 UIEA200800153 1 20080409 A 5347 SEAT TRACK BOEING 747 747243B 1384830 NM BS 1760-1890 CHAFED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK STA 1760 TO 1890 LBL 11 SEAT TRACK FOUND CHAFED. SEAT TRACK SMOOTHED OUT PER SRM 51-10-01 AND REPROTECTED PER 51-10-02. 2 L 7 4 4F RT A20WE 2008041700171 20080417 00171 NM 2008 4 17 UIEA200800151 1 20080415 A 5730 PANEL BOEING 747 7472D3B 1384805 NM LT WING DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 LT WING UPPER SURFACE NR 5 SPOILER CENTER HINGE GAP PANEL DAMAGED, ALSO, INBOARD, OUTBOARD AND CENTER HINGE CUT-OUT AND FORWARD PANEL OF CENTER HINGE DAMAGED, SKIN PULLED AND CRACKED. PERMANENT REPAIRS ACCOMPLISHED AS PER B747-200 SRM 51-4 0-09 FIG. 2, SHEETS 1, 2, AND 5, PREPREG LAYUP 250 DEGREES F CURE PER SRM 51-40-12. ALSO, HINGE GAP PANEL, FABRICATED P ER SAMPLE FROM 2024-T3 0.063 PER B747-200 SRM 51-30-02. ALSO, REFERENCE ATLAS AIR EO NR 4757A434. 2 L 7 4 4F RT A20WE 2008041700186 20080417 00186 NM 2008 4 17 DL757080579 1 20080410 A 3350 LAMP BOEING 757 757232 1384965 NM EMERGENCY LIGHT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 699DL 29970 EMERGENCY LIGHT OUT AT R4 DOOR EXTERIOR, RELAMPED CKS OK. 2 L 7 2 4F RT A2NM 2008041700191 20080417 00191 2008 4 17 SWIA200819475 4 20080409 A 3416 ALTIMETER EMB 120 EMB120ER 3260203 SO COCKPIT INACCURATE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 560SW 120334 FLT 5574 - CAPTAINS ALTIMETER INDICATES BELOW FIELD ELEVATION. REPLACED ALTIMETER. OPS CHECK GOOD, PN 28704-E2101, SN/ OFF 1248. 2 L 7 2 4T RT A31SO 2008041700193 20080417 00193 EA 2008 4 17 SWIA200819477 1 20080406 A 2913 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 FLT 6377 - NR 1 HYDRAULIC SYSTEM QUANTITY SHOWS 0 PERCENT. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP IAW MM 29-11-01, P/N 887055, S/N OFF MX555744A. 2 L 7 2 4F RT A21EA 2008041700197 20080417 00197 NM 2008 4 17 DL777080588 1 20080411 A 2120 UNKNOWN BOEING 777 777232 1385232 NM AFT GALLEY ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 861DA 29952 GALLEY 401 STRONG ELECTRICAL SMELL ON START. GALLEY 401 ELEC CONTROL PNL REMOVED AND DETAILED INSPECTED BACKSIDE ELEC C ONNECTION AS PER AMM 25-30-00. NO ABNORMAL FOUND ELEC CONTROL PNL INSTALLED. GALLEY POWER ON TEST ON GND. NO ELEC SME LL EXISTING. 2 L 7 2 4F RT T00001SE 2008041700201 20080417 00201 NE 2008 4 17 08FDEA01419 2 20080415 A 7230 COMPRESSOR DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 3 ENGINE STALLED A FDEA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 25 315FE 55457 48313 455239 NR 3 ENGINE COMPRESSOR STALL IN CRUISE SHAKING. AIRCRAFT FLUCTUATION OF N1,-THROTTLE AT IDLE N137 PERCENT EGT 600-700 D EG INFLIGHT ENGINE SHUTDOWN, RESIDUAL FUEL FLOW AFTER SHUTDOWN 800 LBS FF. REMOVED AND REPLACED THE #3 ENGINE. PERFORM ED IDLE AND FLT IDLE RUNS. ALSO PERFORMED A MAX POWER ASSURANCE RUN. ALL ENGINE PARAMITERS WERE NORMAL AND A/C OK FOR SERVICE. FUEL FLOW DISCR. WAS ALSO CLEARED WITH ENGINE R & R. 2 L 7 3 4F 4 F RT A22WE E23EA 2008041800024 20080418 00024 SO 2008 4 18 C2XA08CL045 1 20080406 A 2612 902081 CONTROL MODULE EMB 145 EMB145XR 3260214 SO COCKPIT FAULTY A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 14153 12751 145761 CLE FLIGHT 2285 THE CREW REPORTED A ENGINE 2 FIRE DETECT FAIL TWICE IN FLIGHT FOR 1-2 MINUTES EACH TIME. THE AIRCRAFT L ANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE FIRE CONTROL MODULE. OPERATIONAL CH ECKS WERE GOOD. 2 L 7 2 4F RT 2008041800025 20080418 00025 SO 2008 4 18 FDKA200804146 1 20080405 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 848MJ 145530 FDM 6069 TYS-MCO (0305 PHX LCL). RIGHT OVERWING EMERGENCY EXIT SIGN OUT. MX RECONNECTED LOOSE CONNECTOR. OPS GOOD. 2 L 7 2 4T RT T00011AT 2008041800037 20080418 00037 NM 2008 4 18 BB08052 1 20080406 A 2560 P4010021 BATTERY BOEING 757 7572S7 1384962 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 906AW 23568 OGG - THE FLASHLIGHT WAS INOPERATIVE AT THE 1L DOOR. MAINTENANCE REPLACED THE BATTERY IN THE FLASHLIGHT AT THE 1L DOOR. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 2008041800055 20080418 00055 SW 2008 4 18 EVCA200804108 1 20080410 A 6330 206033554101 LINK BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL TRANMISSION BROKEN E EVCA R AUTOROTATION E VIBRATION/BUFFET AA AIR AMBULANCE 1 CE 03 89AE 8 45433 FAILURE OF THE LT REAR TRANSMISSION LINK IN FLIGHT. HEARD NOISE AUTOROTATION TO A SAFE LANDING IN FIELD. INVESTIGATION SHOWED THE LINK HAD SEPARATED, TRANS UP STOP HELD. 1 G 7 1 3U 3 U H2SW E1GL 2008041800097 20080418 00097 NM 2008 4 18 USAA920080788 1 20080314 A 5320 146N524023 ANGLE BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 908AW 24233 MCN - MAJOR REPAIR - C3 CHECK - LEVEL 2 CORROSION ON ANGLE, BS 1715, RBL 20.5 - RBL 25, WL 208. REPLACED ANGLE, BS 1715 , RBL 20.5 - RBL 25, WL 208 IAW B757 SRM 51-30-01. 2 L 7 2 4F RT A2NM 2008041800098 20080418 00098 NM 2008 4 18 USAA920080789 1 20080314 A 5320 146N524020 ANGLE BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 908AW 24233 MCN - MAJOR REPAIR - C3 CHECK - LEVEL 2 CORROSION ON ANGLE, BS 1715, LBL 10.5 - LBL 14.5, WL 208. REPLACED ANGLE, BS 17 15, LBL 10.5 - LBL 14.5, WL 208 IAW B757 SRM 51-30-01. 2 L 7 2 4F RT A2NM 2008041800100 20080418 00100 NM 2008 4 18 USAA920080790 1 20080314 A 5320 146N524022 ANGLE BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 908AW 24233 MCN - MAJOR REPAIR - C3 CHECK - LEVEL 2 CORROSION ON ANGLE, BS 1701 - BS 1712, LBL 50, WL 208. REPLACED ANGLE, BS 1701 - BS 1712, LBL 50, WL 208 IAW B757 SRM 51-30-01. 2 L 7 2 4F RT A2NM 2008041800114 20080418 00114 NM 2008 4 18 BB08051 1 20080406 A 3350 PROXIMITY SENSOR BOEING 757 7572S7 1384962 NM L2 DOOR FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 906AW 23568 OGG - THE EMERGENCY SLIDE LIGHT AT DOOR 2L WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE GIRT BAR PROXIMITY SENSOR. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 2008041800137 20080418 00137 SO 2008 4 18 C2XA08SH064 1 20080413 A 5311 14523115415 FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV - DURING C-CHECK FR 15 DAMAGE AT STR 2R FROM COCKPIT DOOR HINGE PIN. MX REPAIRED FR 15 AT STR 2R IAW EMB 145 SRM 53 -00-04 FIG 206. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008041800142 20080418 00142 NM 2008 4 18 F3LA200800179 1 20080417 A 3350 BULB AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE EMERGENCY LIGHT INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 905FR 10 1583 DURING PRE FLIGHT INSPECTION THE FLIGHT CREW REPORTED SEAT ROWS 9 AND 22 HAD ONE SEGMENT OF LIGHTS FOUND BURNED OUT DURI NG PRE FLIGHT TEST. MAINTENANCE REMOVED AND REPLACED ONE BULB FROM ROW 22 IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 31 -51-00 AND DEFERRED EMERGENCY LIGHT IN ACCORDANCE WITH THE REQUIREMENTS OF MEL 33-50-03A. 2 L 7 2 4F 4 F RT A28NM E37NE 2008041800143 20080418 00143 EA 2008 4 18 A6WA200840220 1 20080313 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 CRACKS ON FORWARD AND AFT ON PAX DOOR UNDER STEP PLATE. REPAIRED IAW REO 601R-52-11-279. (M) 2 L 7 2 4F RT A21EA 2008041800148 20080418 00148 EA 2008 4 18 A6WA200840245 1 20080318 A 5340 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 439AW 7753 CRACK FOUND ON HYDRAULIC SUPPORT BRACKET ON MLG BAY RT FORWARD. NEW SUPPORT BRACKET ON MLG BAY INSTALLED IAW SRM 51-42- 06. (M) 2 L 7 2 4F RT A21EA 2008041800149 20080418 00149 EA 2008 4 18 A6WA200840207 1 20080314 A 5347 CARGO TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 567 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 ONE CARGO TRACK CORRODED IN CARGO BAY AT FS 567 LBL 9. CORROSION REMOVED IAW CRJ 200 SRM 51-21-06 OUT OF LIMITS IAW CRJ 200 SRM 53-61-49 THEREFORE SEAT RAIL AT FS 567 RBL 9. REPLACED IAW CRJ 200 SRM 51-40-11 AND 51-41-02. (M) 2 L 7 2 4F RT A21EA 2008041800150 20080418 00150 EA 2008 4 18 A6WA200840208 1 20080317 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 CLIPS CRACKED ON INTERCOSTALS AT FS 484, RBL 27 AND RBL 36. INBOARD CLIP REPLACED IAW SRM 51-42-21, OUTBOARD CLIP, REPL ACED IAW REO 601R-53-41-059. (M) 2 L 7 2 4F RT A21EA 2008041800151 20080418 00151 EA 2008 4 18 A6WA200840209 1 20080314 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 559-621 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 BTW FS 621 TO FS 559 PLUS 112, WL 73, FLOOR SILL IS CORRODED AT NUT PLATES LOCATION. CORROSION BETWEEN FS 559 PLUS 112 TO 621 WL 73 FLOOR SILL REMOVED IAW CRJ200 SRM 51-21-06 AND WITHIN LIMITS IAW SRM 53-61-23. (M) 2 L 7 2 4F RT A21EA 2008041800152 20080418 00152 EU 2008 4 18 08FDEA01436 1 20080417 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 SEVERAL HOLES ELONGATED ON LT WING BOTTOM SKIN AND SUPPORT BRACKET. REPAIR PERFORMED BY DRAWING R571-50532 (REAM UP AND BUSHING INSTALLATION) IAW RAS/BAE/1006453/2008 ISS A, APPROVED BY EA 6-2910-115254. 2 L 7 2 4F RT A35EU 2008041800153 20080418 00153 EA 2008 4 18 A6WA200840176 1 20080309 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WINGLET DELAMINATED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 458AW 7861 REQUEST INSPECTION RIGHT WINGLET TRAILING EDGE DELAMINATED/PILOT FOUND ON WALK AROUND. (M) 2 L 7 2 4F RT A21EA 2008041800162 20080418 00162 EA 2008 4 18 A6WA200840243 1 20080318 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 439AW 7753 CRACK EXISTS ON INTERCOSTAL FS 484 LBL 27. ATTACH FITTING ON INTERCOSTAL AT FS 484 LBL 27 REMOVED AND REPLACED IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (M) 2 L 7 2 4F RT A21EA 2008041800163 20080418 00163 EU 2008 4 18 08FDEA01437 1 20080417 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 730FD 659 HYDRAULIC LINES IN WING WORN OUT. REPAIR PERFORMED IAW SB 29-6057 (INSTALLATION OF ANTI-ROTATING DEVICES) ON BOTH WINGS , RIB 8-9. 2 L 7 2 4F RT A35EU 2008041800164 20080418 00164 WP 2008 4 18 08FDEA01438 1 20080417 A 5712 ARB1666502 RIB DOUG DC10 DC1010F 3022111 WP ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION ON SLAT NR 3 RT WING FOUND RIB P/N ARB1666-502 WITH HOLE OVALIZED REPLACED RIB FOR SRM 51-3 5-01 VOL II AND DWG NRB6027. 2 L 7 3 4F A22WE 2008041800165 20080418 00165 WP 2008 4 18 08FDEA01439 1 20080417 A 5347 NEA602223 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1341 X = -75.250 FOUND SEAT TRACK WITH CRACK .5" LONG REPAIRED FO R SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F A22WE 2008041800166 20080418 00166 WP 2008 4 18 08FDEA01440 1 20080417 A 5347 ADA7321503 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE FROM STA 1099 TO STA 1159 ON SEAT TRACK FOUND HOLES OVALIZED REPAIRED FRO M SRM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F A22WE 2008041800168 20080418 00168 NM 2008 4 18 08FDEA01442 1 20080417 A 5320 655850521 PANEL BOEING 727 727232 1384082 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 LOWER PANEL 3456 RT IS CRACKED WITH ERODED AREA FLAME SPRAY. REPLACED CRACK AND FLAME SPRAY ON PANEL 3456 REF SRM 51-40 -9 PARAGRAPHS 3D, 4E, 4F AND AMM 51-20-051-7. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008041800171 20080418 00171 EA 2008 4 18 A6WA200840217 1 20080312 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 CRACK FOUND ON FS 280 LBL 9 ON FLOOR STRUCTURE. REPAIRED IAW CRJ200 REO 601-53-11-171 REV D ON FS 280 LBL 9. (M) 2 L 7 2 4F RT A21EA 2008041800172 20080418 00172 EA 2008 4 18 A6WA200840108 1 20080222 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA LAVATORY SMOKE A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 31 468AW 7916 SMOKE TOILET CAUTION MESSAGE ON SHORT FINAL. FLIGHT ATTENDANT REPORTS PHYSICAL SMOKE COMING FROM AREA OF LAV CEILING. REMOVED SMOKE DETECTOR AND LAV SPEAKER AND INSPECTED AREA BEHIND BOTH. REINSTALLED AND PERFORMED OPS TEST OF DETECTOR P ER AMM 26-16-01. NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A21EA 2008041800175 20080418 00175 EU 2008 4 18 F3LA200800178 1 20080406 A 5320 D5347047720800 PROFILE AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AROUND NUT PLATES AFT CARGO PIT LEFT FLOOR PROFILE AT C 58. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 PARAGRAPH 5 AND 6 AND AIRBUS DRAWING D 53476318. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008041800178 20080418 00178 NM 2008 4 18 08FDEA01443 1 20080417 A 5340 66118094 STRINGER CLIP BOEING 727 727232 1384082 NM BS 950A S27L DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 STRINGER CLIP CRACKED ON STR 27L FS 950A REMOVED DAMAGED CLIP, REPLACED CLIP, REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008041800180 20080418 00180 EU 2008 4 18 08FDEA01445 1 20080417 A 5740 A5724329200000 ATTACH ANGLE AIRBUS 310 A310203 3930313 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 LEFT WING ATTACHING ANGLE FOR L/E PANEL 523 HB IS CRACKED. FABRICATED A NEW REINFORCING PLATE IAW AIRBUS DWG 23-A-572-4 3292 ISSUE F. PRIMED IAW A310 SRM 51-21-10 AND 51-23-10. REPLACED REINFORCING PLATE IAW A310 SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008041800183 20080418 00183 NM 2008 4 18 08FDEA01448 1 20080417 A 5322 69436835 SHEAR TIE BOEING 727 727232 1384082 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 FWD PIT SHEAR TIE CORRODED, STA 660 BETWEEN STR 27R - 26R REMOVED CORROSION ON FWD SHEAR TIE STA 660 STR 27R - 26R REF S RM 51-10-6 PG 12 ORIGINAL MATERIAL .050". MATERIAL REMAINING .035", MATERIAL LOSS .015". FOUND OUT OF LIMITS REF SRM 53-10-1 PG 1-2. FABRICATED NEW SHEAR TIE NOTE ID 60-4493, 7075 T-6 EXTRUSION REF BOEING DWG 69-43683. TREATED AND PRI MED AND INSTALLED SHEAR TIE, REF SRM 51-10-2, 51-30-2. THIS IS CLASSIFIED A MAJOR REPAIR. 2 L 7 3 4F A3WE 2008041800186 20080418 00186 EA 2008 4 18 A6WA200840222 1 20080319 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOORWAY CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 SERVICE DOOR SILL PLATE CORRODED. SERVICE DOOR SILL PLATE REPLACED IAW CRJ 200 SRM 51-41-04. (M) 2 L 7 2 4F RT A21EA 2008041800187 20080418 00187 NM 2008 4 18 USAA920080840 1 20080327 A 5753 113N3003 SKIN BOEING 757 757225 1384959 NM T/E FLAP CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT- MAJOR REPAIR - C4 CHECK - A 5" CRACK ON RIGHT O/B FLAP BOTTOM SKIN AT O/B EDGE. REPAIRED IAW SRM 57-53-01 FIG 201, REPAIR 4. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 SWAA083415 1 20080622 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083414 1 20080622 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083450 1 20080623 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 330, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083441 1 20080622 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 824, STR 26R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083442 1 20080622 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 27R CORRODED BETWEEN BS 500B AND BS 500C. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083481 1 20080623 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083482 1 20080623 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 414, LBL 1.5. REPAIRED SK IN PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083451 1 20080623 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083452 1 20080623 A 3350 100031 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083424 1 20080622 A 5310 6546818 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 947 TO BS 1006, RBL 50. REMOVED AND REPLACED WEB PER S RM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083423 1 20080622 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083458 1 20080623 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED MV2 CHECK, FOUND BEADED PRESSURE DECK WEB CRACKED AT BS 540, LBL 25. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083459 1 20080623 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083460 1 20080623 A 3350 6574550 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 LEFT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT ASSY LOOSE. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083425 1 20080622 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 403WN 29815 DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 133. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083465 1 20080623 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 DURING SCHEDULED HC2 CHECK, LEFT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083470 1 20080623 A 5754 65C26602 SLAT BOEING 737 7373G7 1384595 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND RIGHT WING NR 4 L/E SLAT INBOARD UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083476 1 20080623 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SKIN P ER EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083433 1 20080620 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 731SA 27863 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083479 1 20080623 A 5743 115A5211 FITTING BOEING 737 7377H4 1384404 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 743SW 29279 DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083435 1 20080621 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 743SW 29279 DURING SCHEDULED MV2 CHECK, FOUND LEFT MLG TRUNNION LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083434 1 20080621 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 743SW 29279 DURING SCHEDULED MV2 CHECK, FOUND RIGHT MLG TRUNNION LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083436 1 20080620 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 744SW 29490 L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083358 1 20080618 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083360 1 20080618 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083361 1 20080618 A 5312 6546568 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER CRACKED AT BS 1016, NR 16 POSITION. REMOVED AN D REPLACED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083362 1 20080618 A 5312 6546568 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER CRACKED AT BS 1016, NR 19 POSITION. REMOVED AN D REPLACED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083352 1 20080618 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083353 1 20080618 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083069 1 20080607 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 484, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083072 1 20080606 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506D, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083073 1 20080606 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED C1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008041800188 20080418 00188 EA 2008 4 18 A6WA200840231 1 20080321 A 5420 RETAINER CNDAIR CL600 CL6002B19 1900309 EA PANEL SEAL CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 776 RIGHT ENGINE, PYLON PANEL 422 DB SEAL RETAINER IS CRACKED. REPLACED IAW CRJ 200 SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2008041800190 20080418 00190 EA 2008 4 18 A6WA200840238 1 20080319 A 5310 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 439AW 7753 CRACK FOUND ON PAX DOOR STAIR AFT DRAG ANGLE. AFT DRAG ANGLE REPAIRED IAW REO 601R-52-11-513 REV A. (M) 2 L 7 2 4F RT A21EA 2008041800201 20080418 00201 EU 2008 4 18 USAA920080852 1 20080402 A 5347 D5307008920600 SEAT TRACK AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 187US 1704 PIT - MAJOR REPAIR - S3 CHECK - CORROSION RIGHT O/B SEAT TRACK FR24, -Y1292. INSTALLED SEAT TRACK SPLICE REPAIR IAW SRM 53-00-15 FIG 202. 2 L 7 2 4F RT A28NM 2008041800202 20080418 00202 NM 2008 4 18 USAA920080853 1 20080403 A 5320 FLOOR SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT - MAJOR REPAIR - C4 CHECK - CORROSION ON FLOOR SUPPORT ANGLE AT BS 1635, WL 208.1, LBL 64. REPLACED SUPPORT ANGLE I AW 51-40-02 AND 53-60-13. 2 L 7 2 4F RT A2NM 2008041800203 20080418 00203 NM 2008 4 18 USAA920080854 1 20080403 A 5320 FLOOR SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT - MAJOR REPAIR - C4 CHECK - CORROSION ON FLOOR SUPPORT CHANNEL AT BS 345, WL, 208.1, LBL 36. REPLACED CHANNEL IAW S RM 53-00-51. 2 L 7 2 4F RT A2NM 2008041800204 20080418 00204 NM 2008 4 18 USAA920080855 1 20080331 A 5754 SLAT BOEING 757 757225 1384959 NM RT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT - MAJOR REPAIR - C4 CHECK - NR 9 SLAT HAS DELAMINATION AT I/B TRAILING EDGE CORNER (2.5" X 9.5") AND O/B TRAILING ED GE CORNER (4" X 15.75"). INSTALLED REPAIR IAW SRM 51-70-10. 2 L 7 2 4F RT A2NM 2008041800206 20080418 00206 NM 2008 4 18 USAA920080857 1 20080409 A 5347 143N50901 SEAT TRACK BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT - MAJOR REPAIR - C4 CHECK - A 2" CORNER OF SEAT TRACK CRACKED AT BS 780. REPLACED SEAT TRACK (BS 680-790) IAW SRM 5 1-40-00. 2 L 7 2 4F RT A2NM 2008041800231 20080418 00231 NM 2008 4 18 USAA920080860 1 20080409 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT - MAJOR REPAIR - C4 CHECK - A .3" CRACK ON FUSELAGE SKIN AT BS 1708, STR 4L. INSTALLED DOUBLER / TRIPLER REPAIR IAW EA 110816. 2 L 7 2 4F RT A2NM 2008041800232 20080418 00232 EU 2008 4 18 TRBA2008042 1 20080416 A 3230 E024428AO RELAY AEROSP ATR72 ATR72212 8680945 EU LT MLG FAILED A TRBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 426AT 426 LT MLG UNSAFE INDICATION IN FWD AND UPPER PANELS. EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO SJU WITHOUT FURTHER I NCIDENT. REPLACED LT MLG UPLOCK BOX AND RELAY FIN NR 9GB AT 91VU. PERFORMED FUNCTIONAL CHECK OF EXTENSION AND RETRACTI ON. ALSO PERFORMED EMERGENCY EXTENSION FUNCTIONAL TEST. BOTH TEST FOUND SATISFACTORY IAW AMM NR 32-31-00 AND NR 32-33- 00. 2 H 7 2 4T RT A53EU 2008041800234 20080418 00234 NM 2008 4 18 2008UALA02037 1 20080409 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 809UA 825 FOUND BEAM 150 CORRODED WHILE ACCOMPLISHING EQ3700 CALLOUT. REMOVED BEAM. INSTALLED BEAM 150 AND 105 AS A UNIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041800242 20080418 00242 NM 2008 4 18 USAA920080861 1 20080410 A 5320 BRACKET BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT - MAJOR REPAIR - C4 CHECK - A .5" CRACK ON BRACKET AT BS 310.5. REPLACED BRACKET IAW SRM 510-10-00. 2 L 7 2 4F RT A2NM 2008041800249 20080418 00249 NM 2008 4 18 USAA920080870 1 20080405 A 5320 312A13221 FITTING BOEING 737 737401 1384701 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 CLT - MAJOR REPAIR-C3- A .25" X .5" HOLE IN AFT PRESSURE BULKHEAD FITTING ON THE INBOARD SIDE (AROUND THE APU BLEED DUCT ) AT BS 1016. REPLACED FITTING IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041800285 20080418 00285 2008 4 18 BB08063 4 20080413 A 2310 7926140001 COUPLER BOEING 757 7572B7 1384964 NM HF ANTENNA INOPERATIVE A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 202UW 43211 1286 27811 DUB - FLT 723 EN ROUTE DUB TO PHL. BOTH HF RADIOS BECAME INOPERATIVE DURING THE FLIGHT. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT HF ANTENNA COUPLER. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 2008041800287 20080418 00287 EU 2008 4 18 USAA920080873 1 20080414 A 3350 COVER AIRBUS 320 A320214 3930316 EU CABIN OUT OF POSITION A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 117UW 1224 FLT 1196 CLT - EEL - POWER SUPPLY SEAT 11C INOP. MAINTENANCE FOUND COVER POPPED OUT. REINSTALLED COVER. POWER SUPPLY SEAT 11C OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A28NM 2008041800288 20080418 00288 NM 2008 4 18 USAA920080799 1 20080316 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A .25" CRACK ON FRAME AT BS 500F BETWEEN STR 8L AND STR 9L. INSTALLED REPAIR IAW SRM TR 53-10-20E. 2 L 7 2 4F RT A16WE 2008041800293 20080418 00293 NM 2008 4 18 USAA920080804 1 20080327 A 5754 65C26602224TR WEDGE BOEING 737 7374B7 1384702 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A 5" X 2.5" DISBOND ON NR 5 SLAT TRAILING EDGE WEDGE. INSTALLED REPAIR IAW SRM 57-43-02 , 51-70-00, 57-70-10 R4 AND AMM 51-21-99. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083074 1 20080608 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083178 1 20080610 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083157 1 20080610 A 2761 693667310 ACTUATOR BOEING 737 7373H4 1384600 NM NR 4 SPOILER FROZEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND LT WING NR 4 SPOILER ACTUATOR ROD END FROZEN. REMOVED AND REPLACED ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 2008UALA02978 1 20080522 A 2612 233U42039 MODULE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE APU EXTINGUISHER FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 BEFORE DEPARTURE FOUND APU FIRE EXTINGUISHER SQUIB TEST INOP. SUSPECT SQUIB TEST MODULE SWITCH FAULTY. LUBRICATED SQU IB TEST SWITCHES AND OP CHECKED SQUIB TEST MODULE PER MM 26-21-02 PG.405. OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080714 NM 2008 7 14 DLM88080797 1 20080530 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 963DL 49982 DURING HMV 3 FIVE CRACKS WERE FOUND ON FUSELAGE AT STATIONS:Y=189 OF .093",Y=190 OF .031",Y=191 OF .093",Y=193 OF.078" A ND Y=196 OF .062"; AND THE LONGERON 22 LT CRACKS WERE REPAIRED IAW EA 09-069085-12AD REV D. 2 L 7 2 4F RT A6WE 20080714 NM 2008 7 14 DLM88080799 1 20080530 A 2730 TAB DOUG MD88 MD88 3023688 NM ELEVATOR WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 963DL 49982 DURING HMV3 WEAR WAS FOUND ON TRAILING EDGE OF LT ELEVATOR GEARED TAB. WEAR WAS REPAIRED IAW DRD 55-04D PARA 3D FIG 2. 2 L 7 2 4F RT A6WE 20080714 NM 2008 7 14 DLM88080801 1 20080530 A 5753 VANE DOUG MD88 MD88 3023688 NM LT WING TE FLAP ERODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 963DL 49982 DURING HMV3 ERODED LOWER SURFACE OF INBD FIXED VANE LT INBD FLAP WAS FOUND. EROSION WAS REPAIRED IAW SRM 57-03 PARA 8D FIG 9A. 2 L 7 2 4F RT A6WE 20080714 NM 2008 7 14 DL757080809 1 20080530 A 5313 STRINGER BOEING 757 757232 1384965 NM BS 1460-1480 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 STR 28 L HAS 2 AREAS OF CORROSION BETWEEN STA 1460 AND 1480/SRM 51-40-05. REPAIR REPORTED PER SRM 53-00-03. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 DL76L080814 1 20080601 A 3150 WARNING MESSAGE BOEING 767 767332 1382001 NM COCKPIT ILLUMINATED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 175DN 24803 MULTIPLE STATUS MSGS AND RT EEC ALTN LIGHT. FOUND C/B ON P6-3 PANEL 115 VAC RT XFR BUS PULLED. RESET BREAKER AND ALL M SGS CLEARED. RAN RT ENG AS PRECAUTIONARY. NO EEC MSGS. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 DL76G080818 1 20080602 A 3610 80217010 VALVE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 ENGINE MALFUNCTIONED A DALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 27 1605 30198 704696 ABORTED TAKEOFF FOR L ENG PRV LT AT 60 KTS FWD TO MCO PER MEL 36-11-08C. TESTED LT ENG PRVC PER HEALTH CK JIC 6119. TE STED BAD. REPLACED WITH FLEX MUSCLE LINE. TESTED PRV VALVE. NOTED LEAKAGE REPLACED PER AMM. ALL TESTS NOW OK PER AJI C 6119 HEALTH CK. ACTIVATED FAN AIR VALVE/HPV/AND PRESS SWITCHES. RAN ENG, CKS NML. 2 L 7 2 4F 4 F RT A1NM E13NE 20080714 NM 2008 7 14 USAA920081108 1 20080521 A 5420 311T31561 STRAP BOEING 767 767201 1385125 NM NR 2 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 250AY 23902 BFM - MAJOR REPAIR - C3 CHECK - CRACKED CHORD STRAP ON NR 2 PYLON. REPLACED CHORD STRAP ON NR 2 PYLON IAW USAIRWAYS EA 100416. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 DLM90080823 1 20080602 A 5347 593054767 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 1300-1364 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 916DN 53396 CABIN SEAT TRACK RBL 22 STA 1310 OUT OF LIMITS. REMOVED AND INSTALLED NEW SEAT TRACK IAW MD90 SRM 53-40-01. 2 L 7 2 4F RT A6WE 20080714 EU 2008 7 14 08FDEA02397 1 20080624 A 5414 A54612478 PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CRACK ON PYLON NR 2 RIB 8A SIDE PANELS INBOARD/OUTBOARD SIDE DOUBLER REPAIR PERFORMED IAW SRM 54-51-31 PB201. 2 L 7 2 4F RT A35EU 20080711 NM 2008 7 11 AALA200801166 1 20080430 A 3397 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 665AA 25299 MIA - EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 AALA200801306 1 20080514 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW - EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801170 1 20080430 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 33G TO 41G INOPERATIVE. RECHARGED BATTERY PACK FOR EMERGENCY LIGHTS AT OVE RHEAD SEAT ROWS 33G TO 41G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 AALA200801159 1 20080430 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 666A 25300 DFW - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080711 NM 2008 7 11 AALA200801132 1 20080428 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 753AN 30261 DFW - EMERGENCY LIGHT AT SEAT 38C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 38C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080711 NM 2008 7 11 DHL2008764517 1 20080521 A 5347 SEAT TRACK BOEING 727 727264 138408M NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 CORROSION ON MAIN CABIN SEAT TRACK BS 1110-1130 LBL 24. REMOVED SEAT TRACK FROM MAIN CABIN BS 1110-1137 LBL 24 FOUND OU T OF LIMITS IAW B727 SRM 53-10-1 FIG 3 AND SRM 51-30-2. FAB NEW SEAT TRACK WITH BAC1520-792-7178-T6 DIM, 2'3" AND PO 90 03797 IAW B727 SRM 53-10-5 FIG 1. 2 L 7 3 4F A3WE 20080711 EA 2008 7 11 MASA200800411 1 20080521 A 3350 BATTERY CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 506MJ 10073 ASH FLT 7220 ORF-ORD. MULTIPLE EMERGENCY LIGHTS INTERIOR & EXTERIOR INOP. CHARGED EMERGENCY LIGHT BATTERIES, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008041700025 20080417 00025 NM 2008 4 17 2008UALA02112 1 20080410 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 947-986 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 AFT GALLEY DOOR INNER CREASE BEAM UPPER SURFACE CORRODED AT STA 947-986. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW CREAS E BEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700026 20080417 00026 NM 2008 4 17 2008UALA02113 1 20080410 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 S9L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD ENTRY DOOR FUSELAGE CUTOUT, STRINGER 9L INTERCOSTAL CRACKED IN UPPER RADIUS FWD END ON THE AFT SIDE OF FRAME BS 294. 5. MAJOR REPAIR ACCOMPLISHED: REPLACED INTERCOSTAL AT S9L. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700027 20080417 00027 NM 2008 4 17 2008UALA02114 1 20080410 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 294 S7L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 398UA 24673 FWD ENTRY DOOR FUSELAGE CUTOUT, S7L INTERCOSTAL CRACKED IN RADIUS FWD END ON THE AFT SIDE OF FRAME AT BS 294.5. MAJOR R EPAIR ACCOMPLISHED: REPLACED INTERCOSTAL AT S7L. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700039 20080417 00039 NM 2008 4 17 MWEA080055 1 20080415 A 3350 2232 LIGHT BOEING 717 717200 1383700 NM LT EXTERNAL INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 922ME 55184 LEFT EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT. 2 L 7 2 4F TR A6WE 2008041700044 20080417 00044 NM 2008 4 17 UPS08651966 1 20080403 A 3510 80316311 REGULATOR BOEING 767 76734AF 1385212 NM CREW O2 LEAKING A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 328UP 27754 UPON BLOCKING IN, CREW O2 ON EICAS READS 250PSI AND FALLING. FOUND UPPER O2 REGULATOR LEAKING. REPLACED BOTH O2 REGULA TORS AS PRECAUTIONARY. 2 L 7 2 4F RT A1NM 2008041700046 20080417 00046 WP 2008 4 17 UPS08851962 1 20080402 A 3350 LAMP DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 EMERGENCY LIGHTS DISARM CHECK LIGHT INOP. RELAMPED, CHECKS GOOD. 2 L 7 4 4F RT 4A25 2008041700047 20080417 00047 WP 2008 4 17 UPS08851963 1 20080402 A 3350 BATTERY DOUG DC8 DC873F 302199F WP INST PNL LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 PREFLIGHT, EMERGENCY INSTRUMENT LIGHTS DID NOT ILLUMINATE AND C/P DOME LIGHT SAME. DISARM CHECKS OK. REMOVED AND REPLA CED BATTERY AND RELAY UNIT IAW MM 33-50-01-2. SYSTEM OK FOR CONTINUED SERVICE. 2 L 7 4 4F RT 4A25 2008041700056 20080417 00056 NM 2008 4 17 2008UALA01937 1 20080405 A 3150 745329D IDG BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE RT ENGINE FAULTY A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 671UA 30026 EICAS MSG R GEN DRIVE DISPLAYED.GEN DRIVE LGT ILLUM. GEN DRIVE DISCONNECTED. REPLACED RT ENGINE IDG PER MM 24-11-01-401 RAN ENGINE OPS GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041700072 20080417 00072 EU 2008 4 17 2008UALA02087 1 20080410 A 2560 GIRT BAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R1 DOOR DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 405UA 452 DOOR 1R SLIDE ARM LEVER BINDS ON ARMING AND DOES NOT STAY FLUSH. FOUND DEBRIS UNDER GIRT BAR FITTING. REMOVED DEBRIS FR OM GIRT BAR FITTING. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041700081 20080417 00081 NM 2008 4 17 2008UALA01949 1 20080404 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 947-1006 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 AFT GALLEY DOOR WAY FLOOR CREASE BEAM UPPER SURFACE CORRODED BS 1006-947 WL 208 RBL 51". SUPPLEMENTAL DATA UPDATE, MAJ OR REPAIR ACCOMPLISHED, REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041700089 20080417 00089 NM 2008 4 17 2008UALA01955 1 20080406 A 5414 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE RT PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 171UA 24322 RT WING TO NR 4 PYLON ATTACH AREA "D" L/E NOSE INTERNAL SKIN CRACKED (5") AND UPPER AND LOWER CHORD CRACKED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041800296 20080418 00296 NM 2008 4 18 USAA920080807 1 20080328 A 5311 SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A 2" CRACK ON FRAME SUPPORT AT BS 927 - 947, BL 0. INSTALLED REPAIR IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041800305 20080418 00305 NM 2008 4 18 USAA920080816 1 20080403 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - CORROSION ON FLOORBEAM T-CAP AT BS 312, RBL 21 - 45. INSTALLED REPAIR IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2008041800308 20080418 00308 NM 2008 4 18 USAA920080819 1 20080403 A 5754 65C26601197 SKIN BOEING 737 7374B7 1384702 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - NR 1 SLAT HAS 4" AREA OF DELAMINATION ON O/B END UPPER SURFACE. REPLACED SLAT IAW JOB C ARD O3C30227005. 2 L 7 2 4F RT A16WE 2008041800311 20080418 00311 NM 2008 4 18 USAA920080824 1 20080407 A 5310 DOOR FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A .1875" CRACK ON FUSELAGE DOOR FRAME AT BS 294.5, STR 17R. INSTALLED DOUBLER REPAIR IA W SRM 51-70-11 FIG 1. 2 L 7 2 4F RT A16WE 2008041800315 20080418 00315 NM 2008 4 18 USAA920080832 1 20080328 A 5312 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 23634 CLT - MAJOR REPAIR - C22 CHECK - TWO EACH 1" CRACKS ON WEB AT BS 178, WL 213, RBL 5.5 - 6.5. INSTALLED REPAIR IAW SRM 5 3-10-08. 2 L 7 2 4F RT A16WE 2008041800317 20080418 00317 NM 2008 4 18 USAA920080834 1 20080331 A 5312 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 23634 CLT - MAJOR REPAIR - C22 CHECK - A .125" CRACK ON WEB AT BS 178, WL 225, LBL 17. INSTALLED DOUBLER REPAIR IAW SRM 51-70 -13. 2 L 7 2 4F RT A16WE 2008041800318 20080418 00318 NM 2008 4 18 USAA920080835 1 20080403 A 5320 WEB BOEING 737 73733A 1384673 NM FUSELAGE DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 23634 CLT - MAJOR REPAIR - C22 CHECK - VERTICAL BEAM AND WEB AT BS 184, WL 233, RBL 17 HAS 2 RIVETS WITH CRACKS, DAMAGE TO WEB . INSTALLED REPAIR IAW SRM 51-70-13. 2 L 7 2 4F RT A16WE 2008041800321 20080418 00321 NM 2008 4 18 USAA920080862 1 20080410 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - CORROSION ON ANGLE (TRANSITION) AT BS 500F - 500G, STR 26L. INSTALLED REPAIR IAW SRM 53 -30-53. 2 L 7 2 4F RT A16WE 2008042100002 20080421 00002 NM 2008 4 21 2008UALA02122 1 20080412 A 3233 ACTUATOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MLG MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 175UA 24382 RTFL DUE TO GEAR TILT MESSAGE AND INABILITY TO RETRACT LANDING GEAR. REPLACED RT BODY GEAR TILT ACTUATOR. NO ROOT CAUSE DETERMINED FOR ACTUATOR. OSV SHOP - NO SHOP DATA FOR ROOT CAUSE. THIS SAME ACTUATOR WAS REPLACED ON THIS AIRCRAFT ON 2/18/2008. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042100007 20080421 00007 NM 2008 4 21 2008UALA02128 1 20080413 A 2121 732591F FAN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE E/E BAY FAILED A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 646UA 25283 EQUIPMENT COOLING FAN FAILURE. REPLACED FWD EQUIPMENT COOLING FAN OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041800042 20080418 00042 NM 2008 4 18 USAA920080724 1 20080403 A 5754 SKIN BOEING 767 767201 1385125 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246AY 23898 MIA - MAJOR REPAIR - C3 CHECK - LEFT WING NR 4 SLAT UPPER SURFACE HAS AREA OF DELAMINATION. REPAIRED LEFT WING NR 4 SLA T UPPER SURFACE IAW B767 SRM 51-70-10. 2 L 7 2 4F RT A1NM 2008041800048 20080418 00048 NM 2008 4 18 USAA920080765 1 20080324 A 5315 D53472172204 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802AW 924 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3158 / FR 66 - BS 3257 / 68, +Y1292. REPLACED CABIN SH EAR PLATE, BS 3158 / FR 66 - BS 3257 / 68, +Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008041800081 20080418 00081 SO 2008 4 18 FDKA200803103 1 20080311 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO A/C BAY MALFUNCTIONED A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 852MJ 13689 145567 FDM 6069 MCO-MIA (0609 PHX LCL). BURNING SMELL FROM NR 2 PACK. MX REPLACED AIR CYCLE MACHINE. 2 L 7 2 4T RT T00011AT 2008041800083 20080418 00083 EU 2008 4 18 USAA920080793 1 20080409 A 3397 CONNECTOR AIRBUS 320 A320231 3930325 EU CABIN NOT SEATED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 626AW 65 FLT 258 - PHX - EEL - OPERATIONAL TEST OF EMERGENCY LIGHTS ON WEEKLY CHECK - FAILED TEST. MAINTENANCE RESEATED CONNECTO RS AT PSEU FORWARD LEFT, AFT LEFT AND MID LEFT & RIGHT. OPERATIONAL TEST GOOD. 2 L 7 2 4F RT A28NM 2008041800090 20080418 00090 EU 2008 4 18 USAA920080780 1 20080326 A 5320 D5347218820400 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 187US 1704 PIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 3851 / FR 66 - BS 3950 / FR 68, +Y1162. RE PLACED CABIN FLOOR SUPPORT, BS 3851 / FR 66 - BS 3950 / FR 68, +Y1162 IAW A321 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008041700105 20080417 00105 NM 2008 4 17 2008UALA01971 1 20080406 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 641 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 DAMAGE FOUND ON CROWN AREA OF FUSELAGE ON RT SIDE AT STA 641 AND ONE INCH RT OF STRINGER S3R. REMOVED DAMAGE AREA THAT WAS OUT OF LIMITS. EDDY CURRENT ACP NO CRACKS NOTED. REPAIRED WITH SOLID FASTENER PER SRM 53-00-01 REPAIR 6 115824 THIS IS A PERMANENT REPAIR. DEEPEST PART OF DENT WAS REMOVED WITH REMOVAL OF GOUGE. NEW DENT MEASUREMENTS WITHIN LIMITS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700110 20080417 00110 NM 2008 4 17 2008UALA01976 1 20080407 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 171UA 24322 EMERGENCY DOOR MOUNT LIGHT INOP AT DOOR 5R. REPLACED EMERGENCY DOOR MOUNT LIGHT OP CHECKED GOOD PER AMM 33-51-00 PB 500. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700112 20080417 00112 NM 2008 4 17 2008UALA01978 1 20080406 A 5240 CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 R4 DOOR FAILS EMERGENCY POWER CABLE TRAVEL CHECK. FOUND CABLE OUT OF ADJUSTMENT. REMOVED DOOR LINER AND ADJUSTED SET SCREW PER MM 52-11-32 AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700115 20080417 00115 2008 4 17 2008UALA01981 4 20080404 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R 1 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 FLIGHT ATTENDANT COULD NOT ARM DOOR ONE RIGHT BEFORE PUSHBACK. FOUND LANYARD OUT OF POSITION, INTERFERING WITH MECHANSI M. RESTOWED LANYARD ROPE. DOOR 1R ARMS DISARMS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700123 20080417 00123 NM 2008 4 17 2008UALA01990 1 20080407 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 DOOR 4 RIGHT EXIT SIGN EMERGENCY LIGHT IS INOP. REPLACED LAMP OP CHECKED NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700124 20080417 00124 NM 2008 4 17 KCSA081220 1 20080409 A 5315 FLOORBEAM BOEING 747 747SR46 1384816 NM BS 360 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 719CK 20923 UPPER DECK FLOORBEAM UPPER CHORD CRACKED AT BS 360, 18TH HOLE FROM LT SIDE 2 L 7 4 4F RT A20WE 2008041700126 20080417 00126 NM 2008 4 17 2008UALA01991 1 20080407 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 SEAT 1A FWD EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE, RELAMPED, CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700134 20080417 00134 NM 2008 4 17 2008UALA01999 1 20080405 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EEL LIGHT INOP AT SEAT 48 ABC. SUPPLEMENTAL DATA UPDATE, RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700155 20080417 00155 NM 2008 4 17 2008UALA02028 1 20080408 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY EXIT EEL LIGHT INOP, AT LEFT SIDE COAT CLOSET JUST FWD OF LAV 104 WALL EEL. FOUND SHORTED LIGHT ASSEMBLY BY LA V 110. REPLACED LIGHT ASSEMBLY OPS. CHECKS NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700156 20080417 00156 NM 2008 4 17 2008UALA02029 1 20080408 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY EXIT EEL LIGHT INOP, JUST AFT OF DOOR 1 LEFT WALL EEL. FOUND SHORTED LIGHT ASSEMBLY BY LAVATORY 110. REPLACED LIGHT ASSEMBLY OPS CHECKS NORMAL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700160 20080417 00160 NM 2008 4 17 UIEA200800154 1 20080403 A 5347 SEAT TRACK BOEING 747 747243B 1384830 NM ZONE 200 CHAFED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK STA 1595 TO 1600 RBL 11 SEAT TRACK FOUND CHAFED. SEAT TRACK SMOOTHED OUT PER SRM 51-10-01. 2 L 7 4 4F RT A20WE 2008041700162 20080417 00162 NM 2008 4 17 UIEA200800105 1 20080331 A 5347 SEAT TRACK BOEING 747 747243B 1384830 NM ZONE 200 CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK BS 1700 TO 1740 RBL 75 SEAT TRACK FOUND CORRODED AND WORN. SEAT TRACK AREA CORROSION REMOVED AND SMOOTHED OUT IAW SRM 51-10-01. 2 L 7 4 4F RT A20WE 2008041700166 20080417 00166 NM 2008 4 17 UIEA200800146 1 20080330 A 5730 SKIN BOEING 747 747243B 1384830 NM RWS 1390 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 RIGHT WING REAR SPAR UPPER SKIN AT WS 1390 FOUND EXISTING EXCESSIVE BLEND OUT AS MARKED. CHECKED THE BLENDOUT AREA AND FOUND AS PER ATLAS EO 4757A338 THE BLENDOUT IS PERMITTED. 2 L 7 4 4F RT A20WE 2008041700169 20080417 00169 NM 2008 4 17 UIEA200800149 1 20080415 A 5210 SKIN BOEING 747 7472D3B 1384805 NM PAX DOOR CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 505MC 21251 MAIN ENTRY DOOR L-1 EXTERIOR SKIN, UPPER HINGE CUT-OUT PREVIOUS DOUBLER REPAIR, LOWER RADIUS CORNER IS CRACKED. VERIFIE D CRACK WITH HFEC AS PER B747-200 NDT MANUAL PART 6, 51-00-00 FIG 23. STOPPED DRILLED CRACK AND ACCOMPLISHED PERMANENT REPAIRS AS PER B747 SERVICE BULLETIN 747-52-2144. ALSO, REFERENCE ATLAS AIR EO NR 4752A143. 2 L 7 4 4F RT A20WE 2008041700174 20080417 00174 NM 2008 4 17 EIA2008017 1 20080416 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM ZONE 200 INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 485EV 20712 EMERGENCY LIGHT AT AFT UPPER DECK DOOR INOP. AFT U/D EMERGENCY EXIT LIGHT ASSEMBLY REPLACED AS PER B747MM 33-51-00 PAGE 10. OPS CHECKED NORMAL. 2 L 7 4 4F RT A20WE 2008041700195 20080417 00195 NM 2008 4 17 DL738080582 1 20080411 A 5511 182A15024 SPAR BOEING 737 737832 13844CF NM HORIZONTAL STAB DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 389DA 30376 RT HORIZONTAL STABILIZER REAR SPAR WAS SEVERED AT STATION 321.67. THE SPAR UPPER CHORD REQUIRED A MATERIAL SUBSTITUTION TO FABRICATE A NEW OUTBOARD SECTION. THE MATERIAL REMAINED 2024-T3511 EXTRUSION. BUT THE PROFILE WAS MADE PER THIS ER /A FROM BAC1505-100450, INSTEAD OF THE ORIGINAL BAC1506-4318. SEE COLLECTOR ER/A 467287-14 FOR MORE DETAILS OF THE OVERALL REPAIR. 2 L 7 2 4F RT A16WE 2008041700196 20080417 00196 NE 2008 4 17 DL76G080587 2 20080411 A 7200 CF680C2B6F ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1613B 31203 32776 706113 BEARING MATERIAL FOUND ON MCD, C/W NUMBER 1 ENGINE CHANGE PER TRANS 1T160. 2 L 7 2 4F 4 F RT A1NM E13NE 2008041800001 20080418 00001 NM 2008 4 18 WRLA2008040 1 20080402 A 5753 ARB0029507 HINGE FITTING DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE T/E FLAP CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 48407 DURING C-CHECK INSPECTION FOUND LEFT OUTBOARD FLAP CENTER BOX INBOARD AFT HINGE SUPPORT FITTING CRACKED. REMOVED AND RE PLACED HINGE WITH NEW PARTS IAW MD11 SRM VOL.II 51-33-01 REV.40 2 L 7 3 4F 4 F RT A22WE E24NE 2008041800013 20080418 00013 SO 2008 4 18 FDKA200804144 1 20080403 A 2611 SMOKE WARNING EMB 145 EMB145LR 3260212 SO CARGO BAY ACTIVATED A FDKA F ACTIVATE FIRE EXT. J WARNING INDICATION NR NOT REPORTED 1 SW 07 831MJ 145273 FDM 6001 GSO-MCO (0704 PHX LCL). BAG SMOKE WARNING AFTER TAKEOFF. MX REMOVED AND REPLACED BOTH FIRE BOTTLES. 2 L 7 2 4T RT T00011AT 2008041800026 20080418 00026 2008 4 18 SB08019 4 20080406 A 3416 2057011 ALTIMETER BOEING 737 7374B7 1384702 NM COCKPIT FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 433US 41426 372 24555 PHL - FLT 1833 - ON CLIMBOUT FROM PHL, EN ROUTE TO NAS, THE NR 2 ALTIMETER FAILED IN FLIGHT WITH FLAG IN VIEW. STANDBY ALTIMETER INDICATED 300 FEET LOW AT 30,000 FEET AND 200 FEET LOW AT 20,000 FEET. FLIGHT RETURNED TO FIELD AT PHL AND LA NDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. ONCE ON GROUND, WITH POWER CHANGE AND APU ON LINE, NR 2 ALTI METER BEGAN TO WORK AGAIN. MAINTENANCE REPLACED THE NR 2 ALTIMETER PER MM 34-12-21. PERFORMED SATISFACTORY PITOT STATI C SYSTEM CHECK PER MM 34-11-00. ALL ALTIMETERS CHECK GOOD. 2 L 7 2 4F RT A16WE 2008041800027 20080418 00027 SO 2008 4 18 C2XA08CL047 1 20080407 A 2612 36011335002309 FIRE LOOP EMB 145 EMB145LR 3260212 SO NR 1 ENGINE FAULTY A C2XA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 27 11539 14454 145536 CLE FLIGHT 2600 THE CREW REPORTED A ENGINE 1 FIRE DETECT FAIL ON TAXI. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHE R INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FIRE DETECT LOOP. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 2008041800028 20080418 00028 SO 2008 4 18 C2XA08RI048 1 20080405 A 3040 381D2MODA CONTROLLER EMB 145 EMB145XR 3260214 SO COCKPIT DEFECTIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 26141 14042 145733 FLIGHT 2784 - EWR - FLIGHT CREW REPORTED STRONG ELECTRICAL SMELL IN COCKPIT DURING CRUISE FLIGHT. THEN SMELL WENT AWAY WHEN WINDSHIELD HEAT WAS TURNED OFF. EWR MX REMOVED AND REPLACED WINDSHIELD CONTROLLER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2008041800032 20080418 00032 SO 2008 4 18 FDKA200804150 1 20080405 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 838MJ 145384 FDM 6139 PNS (1000 PHX LCL). EN ROUTE TO MSY AIRCRAFT DIVERTED INTO PNS DUE TO ELECTRICAL BURN SMELL IN COCKPIT. MX IN SPECTED ALL AVIONICS AND GROUND RAN AC WITH CREW AND FOUND NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008041800041 20080418 00041 NM 2008 4 18 USAA920080723 1 20080323 A 5540 D553713180000 HINGE FITTING AIRBUS A319 A319132 3930340 NM RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802AW 924 SAL - MAJOR REPAIR - C7 CHECK - RUDDER HINGE FITTING NR 2 HAS PLAY, VERTICAL STABILIZER STATION 1926 / RIB 4. REPLACED RUDDER HINGE FITTING NR 2, VERTICAL STABILIZER STATION 1926 / RIB 4 IAW A319 AMM 55-36-00. 2 L 7 2 4F RT A28NM 2008041800044 20080418 00044 EU 2008 4 18 USAA920080761 1 20080402 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 677AW 2430 SAL - EEL - C3 CHECK - LEFT HAND AFT FLIGHT ATTENDANTS FLASHLIGHT HAS A LOW BATTERY. REMOVED AND REPLACED THE LEFT HAN D AFT FLIGHT ATTENDANTS FLASHLIGHT BATTERY. 2 L 7 2 4F RT A28NM 2008041800047 20080418 00047 NM 2008 4 18 USAA920080764 1 20080324 A 5315 D53472188204 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802AW 924 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3257 / FR 68 - BS 3310 / 69, +Y1292. REPLACED CABIN SH EAR PLATE, BS 3257 / FR 68 - BS 3310 / 69, +Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008041800049 20080418 00049 NM 2008 4 18 USAA920080766 1 20080324 A 5315 D53472190203 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802AW 924 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3043 / FR. 64 - BS 3101 / 65, -Y765. REPLACED CABIN FL OORBEAM, BS 3043 / FR 64 - BS 3101 / 65, -Y765 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008041800050 20080418 00050 NM 2008 4 18 USAA920080767 1 20080324 A 5315 D53472190205 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802AW 924 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN FLOORBEAM, BS 3043 / FR 64 - BS 3101 / 65, -Y1292. REPLACED CABIN FL OORBEAM, BS 3043 / FR 64 - BS 3101 / 65, -Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008041800063 20080418 00063 NM 2008 4 18 ASAA0852807 1 20080404 A 5610 5893543130 WINDOW BOEING 737 737890 1384527 NM COCKPIT FAULTY A ASAA K NONE O OTHER NR NOT REPORTED 1 NM 02 577AS 35186 R1 FOGS UP & FORMS FROST ON THE LOWER INNER CORNER ABOUT 10" UP & 4" FROM THE CORNER. VERIFIED RT FRONT INBOARD SIDE OF WINDOW HAS ICED OVER. CHECKED WINDOW SENSOR READINGS. FRONT RT=326 OHMS AT PIN 13 TO 26. SENSOR READS 396 OHMS. REP LACED R1 WINDOW. OP CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2008041800064 20080418 00064 NM 2008 4 18 ASAA0852809 1 20080405 A 4920 38007021 APU BOEING 737 737890 1384527 NM APU BAY SHUTDOWN A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 557AS 6979 35176 APU QUIT AT GATE. FOUND METAL SILVER PARTICLES ON MAGNETIC DRAIN PLUG. REPLACED APU. 2 L 7 2 4F RT A16WE 2008041800093 20080418 00093 EU 2008 4 18 USAA920080783 1 20080329 A 5320 D5348004320501 THRESHOLD AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 187US 1704 PIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON R2 DOOR CUTOUT LOWER SILL THRESHOLD, BS 3851 / FR 66, S23R. REPAIR ED R2 DOOR CUTOUT LOWER SILL THRESHOLD, BS 3851 / FR 66, S23R IAW A321 SRM 53-41-14. 2 L 7 2 4F RT A28NM 2008041800121 20080418 00121 NM 2008 4 18 USAA920080798 1 20080404 A 5320 140N250532 ATTACH FITTING BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 913AW 22207 MCN - MAJOR REPAIR - C1 CHECK - CRACKED FLOOR SUPPORT INTERCOSTAL ATTACH CLIP, BS 1520-1540, BL 0, WL 208. REPLACED FLO OR SUPPORT INTERCOSTAL ATTACH CLIP, BS 1520-1540, BL 0, WL 208 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008041800123 20080418 00123 NM 2008 4 18 USAA920080863 1 20080407 A 5330 6545769 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 529AU 24411 CLT - MAJOR REPAIR - C6 CHECK - CRACKED FUSELAGE SKIN AT THE E/E COOLING DUCT EXHAUST CUTOUT, BS 380, S28L - S28R, BL 0. REPAIRED FUSELAGE SKIN AT THE E/E COOLING DUCT EXHAUST CUTOUT, BS 380, S28L - S28R, BL 0 IAW USAIRWAYS EA 100406. 2 L 7 2 4F RT A16WE 2008041800139 20080418 00139 SO 2008 4 18 C2XA08SH066 1 20080413 A 5320 14521200007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV - DURING C-CHECK LT OMEGA BEAM CORRODED UNDER LOWER LT RAMP ANGLE FR 20. MX REPAIRED LT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00-10. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008041800191 20080418 00191 NM 2008 4 18 USAA920080842 1 20080401 A 5320 146N524U7 FLOOR SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT- MAJOR REPAIR - C4 CHECK - A 1" X 1" AREA OF CORROSION ON FLOOR SUPPORT AT BS 1640 - 1661, LBL 54. REPLACED SUPPORT IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008041800192 20080418 00192 NM 2008 4 18 USAA920080843 1 20080407 A 5320 143N8328U53 ANGLE BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT - MAJOR REPAIR - C4 CHECK - Z-ANGLE CORRODED BENEATH L2 DOOR SILL PLATE AT BS 686 - 760. REPLACED Z-ANGLE IAW SRM 5 1-40-02. 2 L 7 2 4F RT A2NM 2008041800247 20080418 00247 NM 2008 4 18 USAA920080868 1 20080411 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 529AU 24411 CLT - MAJOR REPAIR-C6- .4 INCH CRACK ON FUESLAGE SKIN AT BS 380, BL 0. INSTALLED DOUBLER REPAIR IAW EA 100406. 2 L 7 2 4F RT A16WE 2008042100022 20080421 00022 NM 2008 4 21 2008UALA02068 1 20080409 A 5753 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT WING TE FLAP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 LT WING INBD FLAP UPPER MID SURFACE OTBD DEPTH WEAR LINE IN PREVIOUS REPAIR. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED NEW METAL DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042100025 20080421 00025 2008 4 21 2008UALA02071 4 20080409 A 2330 VIDEO UNIT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 575UA 26689 F/A REPORTS ACRID ODOR AND HAZE FROM VIDEO SYSTEM PROG. VIDEO SYSTEM WAS CLEANED AND RETESTED WITH NO SMELL, NO REPEATS . 2 L 7 2 4F 4 F RT A2NM E17NE 2008042100038 20080421 00038 2008 4 21 2008UALA02139 4 20080413 A 2565 D31591478U1 SLIDE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE R1 DOOR OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 305UA 23666 1R DOOR ESCAPE SLIDE SLID OUT OF CONTAINER. ACCOMPLISHED INSPECTION OF DOOR SLIDE INSTALLATION DOOR 1R SLIDE CHECKED N ORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042100043 20080421 00043 EA 2008 4 21 A6WA200840223 1 20080320 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 FLOOR SUPPORT ANGLES AT FS 621, WL 73, LBL 40 AND RBL 40 ARE CRACKED. REPAIRED IAW REO 601R-53-61-117 REV C. (M) 2 L 7 2 4F RT A21EA 2008042100051 20080421 00051 NM 2008 4 21 2008UALA02035 1 20080409 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 809UA 825 FOUND BEAM 140 CORRODED WHILE ACCOMPLISHING EQ3700 CALLOUT. REMOVED BEAM. BEAMS 140,145 AND 90 INSTALLED AS UNIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042100059 20080421 00059 EU 2008 4 21 2008UALA02024 1 20080407 A 2611 PAI280001 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO BAY DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 485UA 1617 SMOKE DETECTOR 3WH IN AFT PIT, CASE IS DAMAGED. SUPPLEMENTAL DATA UPDATE CAUSE, UNKNOWN DAMAGE. REPLACED AFT CARGO SMO KE DETECTOR 3WH. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042100068 20080421 00068 NM 2008 4 21 CALA0800320 1 20080412 A 3350 252005 FUSE BOEING 737 7373T0 1384582 NM BATTERY CHARGER BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 69351 23589 LAST ROW OF FLOOR PROXIMITY EMERGENCY LIGHTS INOP. REPLACED FUSES IN BATTERY CHARGER. OPS CHECK'S GOOD. 2 L 7 2 4F RT A16WE 2008042100069 20080421 00069 EA 2008 4 21 COMA0860215 1 20080407 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 957CA 7109 DURING HMV - NR 6 INSPECTION, NDT INSPECTION FOUND CRACKS ON THE FS 559 RBL 18, LBL 18 LOWER CAP ANGLES. CUT OUT DAMAGE AND INSTALLED DOUBLERS IAW REO 601R-53-41-260. 2 L 7 2 4F RT A21EA 2008041800066 20080418 00066 NM 2008 4 18 UPS08M51971 1 20080131 A 5313 LONGERON DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP INSPECTION TYPE:C CAC: BETWEEN STA 6-70 AND STA 6-90, LONGERON 52L FOUND CORROSION CRACK. EXISTING LONG END SPLICE & L ONG FASTENERS REMOVED AT STA 6.50-6.90 L52 PER SRM 51-31-01 V.2R.40. CORRODED LONG CUT OUT AT STA 6-60L52 PER SRM 53-10 00 FIG 1V.1R.40. HFEC CUT OUT PER DACNDTSPM06-10-01.001R.13 FOUND NO CRACK EVIDENT. NEW LONG 52 & LONG SPLICE REWORK C/OUT FR MATL 1D0540X7150T6511&1 D1104-7150T6511 PER SRM51-21-01V.2 & SRM 53-10-00FIG 2V.1 R40. 2 L 7 3 4F RT A22WE 2008041800073 20080418 00073 SO 2008 4 18 C2XA08IA103 1 20080406 A 3230 23092900001 UPLOCK EMB 145 EMB145EP 3260221 SO RT MLG MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14939 18941 18941 145030 IAH - FLIGHT 2106, THE CREW REPORTED A LOUD BANGING NOISE UNDER THE FLIGHT COMPARTMENT FLOOR, AND THAT THE RIGHT MAIN LA NDING GEAR INDICATION CYCLING BETWEEN UP AND AMBER. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAI NTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK BOX, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008041800076 20080418 00076 SO 2008 4 18 FDKA200804152 1 20080407 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM 6018 MCO-TLH (0913 PHX LCL). ROW 12 OVERHEAD EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED LAMP, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008041800078 20080418 00078 SO 2008 4 18 FDKA200804153 1 20080409 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6044 JFK-ALB (1633 PHX LCL). TWO EMERGENCY LIGHTS INOP AT ROW 12C AND OVERHEAD CENTER. MX RESECURED THE CONNECTOR. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008041800082 20080418 00082 EU 2008 4 18 USAA920080784 1 20080409 A 3397 E0053R8B3ASNE CONNECTOR AIRBUS 320 A320232 3930326 EU CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 676AW 2422 P-9 CHECK PHX - EEL - ROW 19 AISLE EMERGENCY EXIT LIGHT INOPERATIVE LED LIGHT. REPLACED BROKEN CONNECTOR AT WALL. OPER ATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 2008041800085 20080418 00085 NM 2008 4 18 USAA920080771 1 20080324 A 2560 PUSHROD BOEING 757 7572G7 1384963 NM R4 DOOR STUCK A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 908AW 24233 MCN - EES - C3 CHECK - THE R4 DOOR EMERGENCY MECHANISM MANUAL SELECT HANDLE STUCK IN THE ARMED POSITION. ADJUSTED AND O PERATIONAL CHECKED THE R4 DOOR GIRT BAR CRANK PUSHRODS IAW B757 AMM 52-11-25-5. 2 L 7 2 4F RT A2NM 2008041800092 20080418 00092 EU 2008 4 18 USAA920080782 1 20080326 A 5320 D5347112420000 SHEAR PLATE AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 187US 1704 PIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON SHEAR PLATE, BS 3523 / FR 60 - BS 4059 / FR 70, S23L. REPLACED SHE AR PLATE, BS 3523 / FR 60 - BS 4059 / FR 70, S23L IAW A321 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008041800094 20080418 00094 NM 2008 4 18 USAA920080785 1 20080316 A 5320 143N52601 ANGLE BOEING 757 7572G7 1384963 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 908AW 24233 MCN - MAJOR REPAIR - C3 CHECK - CRACKED INTERCOSTAL ANGLE, BS 780 - BS 800, BL 0, 208. REPLACED INTERCOSTAL ANGLE, BS 7 80 - BS 800, BL 0, 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008041800095 20080418 00095 NM 2008 4 18 USAA920080786 1 20080406 A 2560 P4010021 BATTERY BOEING 757 7572G7 1384963 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 908AW 24233 MCN - EMERGENCY EQUIPMENT - C3 CHECK - FORWARD INBOARD FLIGHT ATTENDANTS FLASHLIGHT INOPERATIVE. REPLACED FORWARD INBOA RD FLIGHT ATTENDANTS FLASHLIGHT BATTERY. 2 L 7 2 4F RT A2NM 2008041800096 20080418 00096 NM 2008 4 18 USAA920080787 1 20080310 A 5315 146N51091 FLOORBEAM BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 908AW 24233 MCN - MAJOR REPAIR - C3 CHECK - LEVEL 2 CORROSION ON FLOORBEAM, BS 1640, BL 0 - RBL 55, WL 208. REPAIRED FLOORBEAM, BS 1640, BL 0 - RBL 55, WL 208 IAW USAIRWAYS TYPICAL REPAIR 53-15-01. 2 L 7 2 4F RT A2NM 2008041800099 20080418 00099 EU 2008 4 18 08FDEA01420 1 20080416 A 5230 A5237407820000 STRUCTURE AIRBUS 310 A310 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 AFT PIT DOOR, NEAR AFT HOOK, STRUCTURE DENTED. NO DENTS ALLOWED IAW SRM 51-10-00. REMOVED AND REPLACED EDGE SECTION IAW SRM 51-40-21. FOR ADJUSTMENT AND CHECK SEE WC 41X5114ALI. 2 L 7 2 4F RT A35EU 2008041800107 20080418 00107 NM 2008 4 18 HNAA040708001 1 20080407 A 3350 6013211X BATTERY PACK DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 975HA 18690 149 176 OVERHEAD CENTER AISLE E-EXIT SIGN ROW 4 INOP ON FORWARD SIDE. REMOVED AND REPLACED BATTERY PACK NR 6, OPS CHECK GOOD I.A .W. 33-51-01. 2 H 7 2 4T RT A13NM 2008041800108 20080418 00108 SO 2008 4 18 C2XA08SH063 1 20080411 A 5320 14525480603 BEAM EMB 145 EMB145XR 3260214 SO CARGO BAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12136 145719 SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 65 THROUGH 68. MAINTENANC E REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008041800111 20080418 00111 SO 2008 4 18 C2XA08RI050 1 20080329 A 5220 14525737403 ESCAPE HATCH EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT DIRTY A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29917 16798 145414 RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND LEFT EMERGENCY OVERWING EXIT HATCH HARD TO OPEN. MX CLEANED AND LEFT EME RGENCY OVERWING EXIT HATCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008041800112 20080418 00112 NM 2008 4 18 BB08056 1 20080408 A 2560 P2070001214 FLASHLIGHT BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 200UU 27809 PHL - THE R3 DOOR EMERGENCY FLASHLIGHT BATTERY HAD A LOW CHARGE. MAINTENANCE PLACED THE FLASHLIGHT ON MEL. MAINTENANCE REPLACED THE R3 DOOR FLASHLIGHT. 2 L 7 2 4F RT A2NM 2008042100074 20080421 00074 NM 2008 4 21 YENA2008030 1 20080408 A 7500 10012463 SHUTOFF VALVE EMB ERJ190 ERJ190100IGW 3260408 NM BLEED SYSTEM FAILED A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 238JB 5601 3035 19000039 FLT 1060, AUS-JFK, DIVERTED TO MCO, BLEED 2 FAIL EICAS MESSAGE AT 4000 FT, PERFORMED QRH AND PROBLEM RESOLVED. BLEED 2 FAIL MESSAGE RETURNED AT 14000 AND PERFORMED QRH, PROBLEM RESOLVED BUT RETURNED AND DESCENT INITIATED. PSI FLUCTUATION OF <10 TO >70. REMOVED AND REPLACED NR 2 BLEED NAC PRSOV, REF AMM 36-1-03, ITEM 2, OPS CHECK OK. 2 L 7 2 4F RT A57NM 2008042100093 20080421 00093 NM 2008 4 21 ZZDA2008808 1 20080406 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 960AT 55022 AFT BAG BIN THRESHOLD STRUCK BY BELT LOADER. FABRICATED DOUBLER REPAIR. MAT USED -071-2024-T3 X 34 " X 29". TRIPLER R EPAIR .080-7075-T6 X 32 " X 33 1/2". QUADRUPLEX REPAIR .100-2024-T3 X 22" X 30 1/2" IAW EA 17-53-01078A SECTION 2. 2 L 7 2 4F TR A6WE 2008042100098 20080421 00098 EA 2008 4 21 COMA0860225 1 20080413 A 2840 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA FUEL INDICATION MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 957CA 7109 FLIGHT 5404 - ON CLIMBOUT FROM BWI LOST ALL FUEL INDICATIONS. A/C RETURNED BACK TO BWI AND LANDED SAFELY. UPON ARRIVAL AT BWI ALL FUEL INDICATION OPS NORMAL. RESET FUEL COMPUTER, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008042100113 20080421 00113 EA 2008 4 21 COMA0870012 1 20080404 A 3080 GG670804061 ELEMENT CNDAIR CL600 CL6002C10 1390015 EA LT WING FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 391CA 10108 FLIGHT 5100 - EN ROUTE PIT-CVG RECEIVED AN ANTI-ICE DUCT WARNING MESSAGE, CREW DECLARED EMERGENCY AND FLIGHT LANDED WITH OUT INCIDENT. REPLACED THE LEFT WING CENTER LEADING EDGE WING SENSING ELEMENT. 2 L 7 2 4F RT A21EA 2008042100114 20080421 00114 SO 2008 4 21 C2XA08TY045 1 20080414 A 3350 3104404 FUSE EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHTS BURNED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27506 145206 TYS - DURING AN OVERNIGHT INSPECTION THE OVERWING EMERGENCY LIGHTS WERE FOUND INOP. MX REMOVED AND REPLACED THE NR 4 BA TTERY POWER SUPPLY FUSE AND OPS CHECKED GOOD IAW EMB AMM 33-21-70. A/C WAS RELEASED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008042100126 20080421 00126 NM 2008 4 21 08FDEA01454 1 20080418 A 3230 ARG7331501 TORQUE LINK DOUG MD11 MD11F 3023600 NM LT MLG SHEARED A FDEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 574FE 48499 LEFT MAIN LANDING GEAR TORQUE LINK SHEARED DURING PUSH-BACK. COMPLETED TORQUE LINK INSTALLATION IAW MD-11 MM 32-11-12-4 2 L 7 3 4F RT A22WE 2008042100149 20080421 00149 EA 2008 4 21 SWIA200819487 1 20080415 A 2120 DUCT CNDAIR CL600 CL6002B19 1900309 EA HEAT EXCHANGER LOOSE A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 971SW 7947 FLT 5849 - "CABIN ALT" WARNING MESSAGE APPEARED. INSPECTED AND SECURED DUCT TO PRIMARY HEAT EXCHANGER ASSEMBLY. OPS CH ECK GOOD. 2 L 7 2 4F RT A21EA 2008042100150 20080421 00150 SO 2008 4 21 SWIA200819488 1 20080414 A 5413 STRINGER EMB 120 EMB120ER 3260203 SO LT NACELLE DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 LEFT NACELLE OUTBOARD STRINGER IN WHEEL WELL REQUIRES REPLACEMENT. REPAIRED STRINGER IAW EMB-IC2008-120/03069. 2 L 7 2 4T RT A31SO 2008042100151 20080421 00151 EA 2008 4 21 SWIA200819489 1 20080414 A 3520 OXYGEN MASK CNDAIR CL600 CL6002D24 1390016 EA CABIN UNWANTED DEPLOY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 805SK 15069 FLT 4033 - OXYGEN MASKS DEPLOYED WHILE SITTING AT GATE. STOWED ALL OXYGEN MASKS AS REQUIRED. 2 L 7 2 4F RT A21EA 2008042300001 20080423 00001 NM 2008 4 23 UPS08M51974 1 20080127 A 5751 SKIN DOUG MD11 MD11 3023602 NM LT AILERON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C LEFT I/B AILERON FOUND CHAFE MARKS ALONG L/E LOWER SKIN I/B SIDE. CHAFED SKIN REMOVED PER SRM 51-35-0 1 V.2R40. HOLES ON NEW SKIN PICKED UP PER SRM 51-31-01 V.2 REV.40. NEW SKIN INSTALLED PER SRM 51-35-01 V.2 REV.40. 2 L 7 3 4F RT A22WE 2008042300010 20080423 00010 NM 2008 4 23 2008UALA02204 1 20080415 A 3510 FITTING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CREW O2 BOTTLE STRIPPED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 FOUND ACFT CREW O2 SERVICE FITTING STRIPPED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042300015 20080423 00015 NM 2008 4 23 2008UALA02207 1 20080417 A 2120 UNKNOWN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 339UA 24243 HEAVY "WET SOCKS" ODOR DURING TAKEOFF AND CLIMB. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042300022 20080423 00022 WP 2008 4 23 UPS08852045 1 20080407 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 STOP HOLES WORN IN F/E'S AFT SEAT TRACK. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-3-0, 51-1-24, 51 -1-8. 2 L 7 4 4F RT 4A25 2008042300024 20080423 00024 NM 2008 4 23 UPS08M52028 1 20080203 A 5753 SKIN DOUG MD11 MD11 3023602 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C RT I/B TE FLAP LOWER SEGMENT BOTTOM SKIN TO BE REPLACED DUE TO MULTIPLE DENTS AND CORROSION. NEW SKIN FABRICATED PER BOEING DRAWING ARC2736 USING 2024T3-0.040" MATL NEW SKIN HOLE PICKED UP PER SRM 51-31-01 V.2R.40. NEW S KIN PROTECTED PER SRM 51-21-01 V.2R.40. NEW SKIN PAINTED PER SRM 51-21-01 V.2R.40 . NEW SKIN INSTALLED PER SRM 51-31-0 1 V.2R.40. RHW I/B FLAP ASSY I/B SEGMENT INSTALLED PER CMM 57-52-03 R.60. 2 L 7 3 4F RT A22WE 2008042300029 20080423 00029 WP 2008 4 23 NWAA081669853 1 20080419 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 762NC 47710 DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 2 L 7 2 4F RT A6WE 2008042300032 20080423 00032 NM 2008 4 23 SA08030 1 20080418 A 3350 SWITCH AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 804AW 1043 LAS - EMERGENCY LIGHTS FLICKER ON AND OFF IN CABIN WITH EMERGENCY EXIT LIGHT SWITCH IN ARMED POSITION. MAINTENANCE REPL ACED EMERGENCY LIGHT SWITCH (4WL). OPERATIONAL CHECK IS GOOD. 2 L 7 2 4F RT A28NM 2008042300038 20080423 00038 NM 2008 4 23 2008UALA02212 1 20080416 A 5240 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 R2 DOOR UPPER HINGE ARM CUT-OUT REQUIRES DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED: PERFORMED INSURANCE CUT & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300040 20080423 00040 NM 2008 4 23 2008UALA02214 1 20080416 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1540 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 AFT PIT BS 1540, FRAME INBOARD FLANGE DENTED AT STR 24R. REMOVED DAMAGED FABRICATED RPR AND INSTALLED IAW SRM 53-00-07 RPR 5 TABLE II THIS IS A CAT B RPR IN ZONE 1 AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS STARTING AT 50,000 TOT AL FLIGHT CYCLES AND 12,000FC THERE AFTER PER SRM 53-00-07 RPR 5 TABLE II. CURRENT PTC= 14,767 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300048 20080423 00048 EA 2008 4 23 MASA200800308 1 20080409 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 77302 7302 PAX DOOR UPPER INNER SKIN CRACKED. REPAIRED SKIN. 2 L 7 2 4F RT A21EA 2008042300064 20080423 00064 NM 2008 4 23 2008UALA02229 1 20080417 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EMERGENCY EXIT EEL LIGHT INOP AT ROW 33 LEFT. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SER VICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300072 20080423 00072 NM 2008 4 23 2008UALA02237 1 20080416 A 5730 114W411011 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 779UA 26941 NR 1 SLAT, OUTBOARD TRACK HAS CRACK ON WING CUTOUT, ABOUT 1.25 INCH LONG. REMOVED 3 RIVETS AND 1 LOCK FASTENER. REMOVED DAMAGE LAID UP REPAIR AND STARTED CURE CYCLE. REF SRM 57-41-01. CURED THEN CLOSED UP. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042300078 20080423 00078 EU 2008 4 23 F3LA200800182 1 20080410 A 5320 D5347047720800 PLATE AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AT NUT PLATES AFT PIT LEFT COVER PROFILE AT FRAME 58 LOCATED FROM STRING ER 38 LEFT TO 38 RIGHT. MAINTENANCE INSTALLED NEW PROFILE PLATE IN ACCORDANCE TO THE REQUIREMENTS OF SRM 51-42-1 PAGE 7 . UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042300101 20080423 00101 NM 2008 4 23 UPS08M51984 1 20080317 A 5754 ARB2850505 FITTING DOUG MD11 MD11F 3023600 NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 256UP 48405 INSPECTION TYPE:2C LEFT SLAT NR 16 FITTING CRACKED. REMOVED AND REPLACED LEFT SLAT NR 16 FITTING IAW MD-11 SRM 51-31-01 & 51-33-01. 2 L 7 3 4F RT A22WE 2008042300102 20080423 00102 EU 2008 4 23 F3LA200800188 1 20080413 A 5340 FITTING AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSLEAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED GIRT BAR FITTING WAS REMOVED ON R1 DOOR DUE TO CORROSION UNDER SPACERS. MAINTENAN CE FABRICATED NEW NUT CLIP PLATES IN ACCORDANCE WITH THE REQUIREMENTS OF AIRBUS DRAWING D53112534. MAINTENANCE INSTALLE D NEW DRAIN PANS AND NEW NUT PLATES AND GIRTH BAR FITTINGS IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11. UPON CO MPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042300110 20080423 00110 NM 2008 4 23 UPS08M51993 1 20080319 A 5730 ARB3954502 SPLICE DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 256UP 48405 INSPECTION TYPE:2C RIGHT WING L/E SPLICE STRAP XFS 669 CRACKED. REMOVED CRACKED SPLICE STRAP, FABRICATED REPLACEMENT SP LICE STRAP AND INSTALLED IAW DWG3954 & MD-11 SRM 51-33-01. 2 L 7 3 4F RT A22WE 2008042300122 20080423 00122 NM 2008 4 23 USAA920080825 1 20080403 A 5347 SEAT TRACK BOEING 737 7374B7 1384702 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT- MAJOR REPAIR - Q6 CHECK - 3 INCH LENGTH CORROSION ON SEAT TRACK AT BS 943, LBL17.2. INSTALLED SPLICE REPAIR IAW SR M 53-00-53 FIG 201. 2 L 7 2 4F RT A16WE 2008042300124 20080423 00124 NM 2008 4 23 USAA920080827 1 20080408 A 5310 507945264 DOOR FRAME BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT- MAJOR REPAIR - Q6 CHECK - .25 INCH CRACK ON L1 DOOR FRAME AT NR 7 STOP. INSTALLED REPAIR IAW EA100332. 2 L 7 2 4F RT A16WE 2008042300129 20080423 00129 NM 2008 4 23 USAA920080889 1 20080411 A 5312 65175827 BULKHEAD BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 MCM - MAJOR REPAIR - C21 - NR 6046444, .5 INCH CRACK ON WEB AT BS 178, WL 230, RBL17.1. INSTALLED REPAIR IAW SRM 53-10- 08-2R 12 FIG 201. 2 L 7 2 4F RT A16WE 2008042300145 20080423 00145 NM 2008 4 23 UPS08M52037 1 20080326 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:4C RT WING LE ACCESS PNL LANDING XOS 550 STRINGER DOUBLER CRACKED. FABRICATED AND INSTALLED REPAIR DOUB LER IAW MD-11 SRM 57-10-00 FIG 18 AND 51-33-01. 2 L 7 3 4F RT A22WE 2008042300146 20080423 00146 NM 2008 4 23 UPS08M52038 1 20080326 A 5730 ARB118010 SKIN DOUG MD11 MD11F 3023600 NM RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:4C RT WING LE ACCESS PNL LANDING AT SLAT TRACK FITTING 9 STRINGER CRACKED. REMOVED CRACKED STRINGER DOU BLER. FABRICATED AND INSTALLED REPLACEMENT STRINGER DOUBLER IAW DWG ARB1180 AND MD-11 SRM 51-33-01. 2 L 7 3 4F RT A22WE 2008041800116 20080418 00116 NM 2008 4 18 BB08057 1 20080411 A 3350 LIGHT BOEING 757 757225 1384959 NM CABIN BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 914AW 22208 PHX - THE EMERGENCY PATH LIGHT AT ROW 5L WAS FOUND BROKEN. MAINTENANCE REPLACED THE EMERGENCY PATH LIGHT ASSEMBLY AT RO W 5L. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 2008041800117 20080418 00117 NM 2008 4 18 USAA920080796 1 20080404 A 5320 140N250532 ATTACH FITTING BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 913AW 22207 MCN - MAJOR REPAIR - C1 CHECK - FLOOR SUPPORT INTERCOSTAL ATTACH CLIP, BS 1320-1340, BL 0, WL 208. REPLACED FLOOR SUPPO RT INTERCOSTAL ATTACH CLIP, BS 1320-1340, BL 0, WL 208 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008041800118 20080418 00118 NM 2008 4 18 USAA920080797 1 20080404 A 5320 140N250532 ATTACH FITTING BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 913AW 22207 MCN - MAJOR REPAIR - C1 CHECK, CRACKED FLOOR SUPPORT INTERCOSTAL ATTACH CLIP BS 1420-1440, BL 0, WL 208. REPLACED FLOOR SUPPORT INTERCOSTAL ATTACH CLIP, BS 1420-1440, BL 0, WL 208 IAW B757-200 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008041800119 20080418 00119 EA 2008 4 18 A6WA200840205 1 20080314 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 RIGHT WING LE, 620AT, AT WS 140 EDGING IS CRACKED IN RADIUS. RIGHT WING INBOARD L/E (620AT) WS 140 SHROUD CRACK REMOVED IAW REO 601R-57-41-502. (M) 2 L 7 2 4F RT A21EA 2008041800122 20080418 00122 EA 2008 4 18 A6WA200840246 1 20080318 A 5340 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 439AW 7753 CRACK FOUND ON HYDRAULIC SUPPORT BRACKET ON MLG BAY RT. SUPPORT BRACKET ON RT MLG BAY FABRICATED AND INSTALLED IAW REO 601R-83-42-007 REV A. (M) 2 L 7 2 4F RT A21EA 2008041800124 20080418 00124 EA 2008 4 18 A6WA200840213 1 20080313 A 2910 MANIFOLD CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 NR 2 HYDRAULIC MANIFOLD CRACKED ON AFT LOWER CORNER P/N 600-75221-130. NR 2 HYDRAULIC MANIFOLD SUPPORT BRACKET REPAIRED . (M) 2 L 7 2 4F RT A21EA 2008041800125 20080418 00125 EA 2008 4 18 A6WA200840210 1 20080314 A 5320 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA BS 574 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 AT FS 574 WL 73 QTY ONE CHANNEL OF CARGO DOOR SURROUND STRUCTURE IS CRACKED. CHANNEL AT FS 574, WL 73, REMOVED IAW CRJ SRM 51-42-06 CHANNEL FABRICATED AND TREATED IAW CRJ SRM 51-24-16 AND 51-21-11, 51-25-06 CHANNEL INSTALLED IAW CRJ SRM 51 -42-06. (M) 2 L 7 2 4F RT A21EA 2008041800127 20080418 00127 EA 2008 4 18 A6WA200840173 1 20080308 A 2121 FAN CNDAIR CL600 CL6002B19 1900309 EA TRU INOPERATIVE A A6WA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 GL 31 420AW 7640 TRU 1 FAN INOPERATIVE. (M) 2 L 7 2 4F RT A21EA 2008041800132 20080418 00132 NM 2008 4 18 08FDEA01432 1 20080416 A 5320 ACA72241 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 619FE 48770 UPPER CARGO DOOR CUT OUT, NR 4 LOWER JAMB SUPPORT FITTING CRACKED. REMOVED & REPLACED PER SRM 51-33-01 VOL II. MOUNTING HOLES ON NR 4 JAMB BEAM REPAIR CARRIED OUT PER EA 1-5310-112624, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041800133 20080418 00133 NM 2008 4 18 08FDEA01433 1 20080416 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 619FE 48770 UPPER CARGO DOOR CUT OUT, NR 5 LOWER JAMB SUPPORT FITTING CRACKED. FITTING REMOVED & REPLACED PER SRM 51-33-01 VOL II. MOUNTING HOLES ON NR 5 JAMB BEAM REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL I. CLASSIFIED AS MINOR REPAIR AS PE R GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041800134 20080418 00134 NM 2008 4 18 08FDEA01434 1 20080416 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 619FE 48770 UPPER CARGO DOOR CUT OUT, NR 6 LOWER JAMB SUPPORT FITTING MOUNTING HOLE CRACKED. MOUNTING HOLES REAMED PER SRM 53-50- 00 FIG. 10 VOL.I. AND BUSHING REPAIR CARRIED OUT PER SRM 53-50-00 FIG. 10. VOL.I. BUSHING FABRICATED PER SRM 53-50-00 FI G. 10 VOL.I. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 2008041700117 20080417 00117 NM 2008 4 17 2008UALA01983 1 20080404 A 2560 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FLASHLIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 663UA 27160 STATUS LIGHT ON FLASHLIGHT AT BUSINESS GALLEY NOT ON. REPLACED BATTERY OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041700131 20080417 00131 NM 2008 4 17 2008UALA01996 1 20080407 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 FWD GALLEY CEILING EMERGENCY LIGHT IS INOP. SUPPLEMENTAL DATA UPDATE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700139 20080417 00139 NM 2008 4 17 2008UALA02007 1 20080407 A 3150 CIRCUIT CARD BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE MALFUNCTIONED A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 776UA 26937 EICAS STATUS MESSAGE "ELEC STANDBY SYS" DISPLAYED, UNABLE TO CLEAR. EXISTING FAULT FOUND ON MAT ALSO. REPLACED M24406A1 2 CARD. RESEATED RELAY K24013. SYSTEM OP CHECK OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008041700144 20080417 00144 NE 2008 4 17 2008UALA02011 2 20080408 A 7200 ENGINE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 3 FLAMED OUT A UALA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 WP 29 119UA 28812 727883 PER THE CREW, WHILE IN CRUISE THE NR 3 ENGINE FLAMED OUT AND WAS FOLLOWED BY AN ENGINE FAIL MESSAGE. METAL IN THE 2.5 B LEED DUCT. REPLACED ENGINE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041700149 20080417 00149 NM 2008 4 17 2008UALA02017 1 20080407 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1420 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 AFT PIT FRAME DENTED STA 1420 S25L TO 26L. REPAIRED FRAME IAW SRM 53- 00-07 DETAIL III PG 8 FRAME FALLS UNDER THE INSPE CTION REQUIRMENTS OF SRM 53-00-07 RPR 5 TABLE II ZONE 3. INSPECTIONS TO BEGIN 1 2000 FLIGHT CYCLES AFTER INSTALLATION AN D 11000 FLIGHT CYCLES T HERE AFTER. INSPECTIONS ARE BOTH VISUAL AND NDT. PTC CURRENTLY 2 L 7 2 4F 4 F RT A2NM E17NE 2008041700180 20080417 00180 NM 2008 4 17 QXEA200800372 1 20080410 A 3231 4686011 LINKAGE BOMBDR DHC8 DHC8402 1390042 NM RT MLG DOOR DISCONNECTED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 404QX 4046 BTM - RIGHT MAIN GEAR DOOR LINKAGE DISCONNECTED. FERRIED AIRCRAFT TO PDX FOR REPAIRS. REPLACED THE LINKAGE. OPERATION AL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 2008041700187 20080417 00187 NM 2008 4 17 DL757080580 1 20080410 A 3350 LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 699DL 29970 EMERGENCY LIGHT OUT RT AFT OVERWING POSITION. RELAMPED SAME. 2 L 7 2 4F RT A2NM 2008041700188 20080417 00188 EA 2008 4 17 SWIA200819472 1 20080411 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 924SW 7681 FLT 6634 - PILOT'S WINDSHIELD CRACKED. REPLACED CAPTAIN'S WINDSHIELD IAW MM 56-11-01. OPS CHECKS GOOD,PN NP139321-13, SN OFF 02091H2986. 2 L 7 2 4F RT A21EA 2008041700198 20080417 00198 NM 2008 4 17 DL738080593 1 20080413 A 2613 356462255 OVERHEAT LOOP BOEING 737 737832 13844CF NM CARGO BAY INOPERATIVE A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 3730B 30538 AFTER TAKEOFF CLIMBING THROUGH 300 FT AGL LT WING-BODY OVERHEAT LIGHT ILLUM. DID QRH PROCEDURE. LIGHT STILL ILLUM, RET URNED TO LAND SLC. LANDED OVERWEIGHT. AT GATE, LIGHT STILL ILLUM. REPLACED DETECTORS M347 AND M1147. TESTS OK. 2 L 7 2 4F RT A16WE 2008041800020 20080418 00020 NM 2008 4 18 SA08026 1 20080407 A 3397 WIRE AIRBUS A319 A319132 3930340 NM CABIN DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 801AW 0889 LAS - ROW TWENTY-TWO AIRCRAFT LEFT EMERGENCY ESCAPE FLOOD PATH LIGHT IS INOPERATIVE. MAINTENANCE REPAIRED AND REPLACED BROKEN WIRE. OPERATIONALLY CHECKS OKAY. 2 L 7 2 4F RT A28NM 2008041800033 20080418 00033 WP 2008 4 18 ABXA080117 1 20080402 A 2130 UNKNOWN DOUG DC9 DC941 302207N WP CABIN PRESSURE MALFUNCTIONED A ABXA G O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 GL 23 956AX 47620 CABIN PRESSURIZATION WAS NORMAL OUT OF 10,000 MSL. APPROX 14,000 MSL, CABIN PRESSURIZATION ANNUNCIATOR & MASTER WARNING CAME ON. CHECKED CABIN PRESSURIZATION AND IT WAS APPROX 11K. DONNED OXYGEN MASKS AND PROCEEDED WITH ABNORMAL CHECKLIS T. DURING THE ABNORMAL CHECKLIST, THE PRESSURIZATION STARTED WORKING NORMAL. CHECKED PACKS IAW DC9 AMM 21-20-00-5, SYS TEM CHECKED GOOD. CHECKED AUTO PRESSURIZATION CONTROL SYSTEM IAW DC9 AMM 21-32-00-2. SYSTEM CHECKED GOOD. 2 L 7 2 4F A6WE 2008041800052 20080418 00052 NM 2008 4 18 USAA920080769 1 20080324 A 5320 D5347112420000 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 802AW 924 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / 70, +Y1732. REPLACED CABIN SHEAR PLATE, BS 3310 / FR 69 - BS 3366 / 70, +Y1732 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008041800059 20080418 00059 SO 2008 4 18 C2XA08CL046 1 20080407 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145XR 3260214 SO RUDDER FAULTY A C2XA K NONE F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 27 11137 145721 CLE FLIGHT 2285 CLE-MHT - THE CREW REPORTED RUDDER SYSTEM NR 1 AND NR 2 INOP, AND RUDDER YAW DAMP INOP MESSAGES ILLUMINA TED ON THE ECIAS DISPLAY. AN EMERGENCY WAS DECLARED AND THE A/C LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 AND NR 2 RUDDER PRESSURE SWITCHES. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2008041800065 20080418 00065 NM 2008 4 18 ASAA0852810 1 20080408 A 2162 WARNING SYSTEM BOEING 737 737890 1384527 NM TEMP CONTROL MALFUNCTIONED A ASAA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 NM 02 557AS 35176 FLIGHT DECK PRIMARY TEMPERATURE CONTROL INOPERATIVE WITH TRIM VALVE FAULT INDICATION. RESET FAULT INDICATION. OP CHECK ED OK. 2 L 7 2 4F RT A16WE 2008041800079 20080418 00079 SO 2008 4 18 FDKA200804155 1 20080409 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6044 JFK (1506 PHX LCL). TWO EMERGENCY LIGHTS INOP AT ROW 12C AND OVERHEAD CENTER. MX RESECURED THE CONNECTOR. OP S CHECK GOOD. 2 L 7 2 4T RT T00011AT 2008041800080 20080418 00080 SO 2008 4 18 FDKA200803129 1 20080324 A 5320 14526437001 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 BUTT STRAP AT Y=479 AND FRAME 61 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED BUTT STRAP. 2 L 7 2 4T RT T00011AT 2008041800110 20080418 00110 SO 2008 4 18 C2XA08RI049 1 20080411 A 3350 1317 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18101 145590 RIC - DURING ROUTINE MAINTENANCE, RIC MX FOUND LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED LIGHT BULB AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 2008041800136 20080418 00136 SO 2008 4 18 C2XA08TY043 1 20080412 A 3350 375911 SIGN EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16918 145397 TYS - DURING A SERVICE ROUTINE THE EMERGENCY EXIT SIGN AT ROW 12 WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE E MERGENCY EXIT SIGN AT ROW 12 IAW AMM 33-50-15. OPS CHECK GOOD. A/C RELEASED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008041800138 20080418 00138 SO 2008 4 18 C2XA08SH065 1 20080413 A 5230 14524610003 DOOR FRAME EMB 145 EMB145LR 3260212 SO CARGO DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12552 145583 SHV - DURING C-CHECK MINOR CRACK AT FWD LOWER CORNER OF CARGO DOOR. MX REMOVED AND REPLACED FWD FRAME ON CARGO DOOR IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 2008042300148 20080423 00148 NM 2008 4 23 UPS08M52040 1 20080326 A 5730 ARB39545 SKIN DOUG MD11 MD11F 3023600 NM LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:4C LEFT WING LE SKIN SPLICE STRAP XFS 669 CRACKED. REMOVED CRACKED SKIN SPLICE STRAP. FABRICATED AND I NSTALLED REPLACEMENT SKIN SPLICE STRAP IAW DWG ARB3954 AND 51-33-01. 2 L 7 3 4F RT A22WE 2008042300160 20080423 00160 EU 2008 4 23 F3LA200800190 1 20080410 A 5315 D53476476200000 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED CORROSION AT NUT PLATES AFT PIT LEFT FLOORBEAM UNDER COVER PROFILE AT FRAME 56 LOC ATED FROM STRINGER 38 LEFT TO 38 RIGHT. MAINTENANCE FABRICATED REPLACEMENT PART IN ACCORDANCE WITH THE REQUIREMENTS OF AIRBUS DRAWING D53476476200 AND MATERIAL SPECIFICATION DAN26H35. INSTALLED NEW SUPPORT ANGLE IN ACCORDANCE WITH THE REQ UIREMENTS OF SRM 51-42-11 PARAGRAPH 6. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042300163 20080423 00163 NM 2008 4 23 F3LA200800193 1 20080417 A 5210 D5211021420200 FITTING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE PAX DOOR FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 45 1841 DURING C4 S1 C CHECK INSPECTION NOTED THE FORWARD ENTRY DOOR FAILED RIG CHECK AT THE TORSION BAR BELL CRANK AND REDUCER SHAFT. MAINTENANCE REMOVED AND REPLACED THE LEFT FITTING FOR RIG PIN AND ADJUSTED DOOR RODS IN ACCORDANCE WITH THE REQU IREMENTS OF AMM 52-11-400-001. MAINTENANCE CHECKED THE RIG PINS IN ACCORDANCE WITH THE REQUIREMENTS OF WORK CARD C52800 2-2 STEP 4B. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042300165 20080423 00165 EU 2008 4 23 2008UALA02174 1 20080415 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 494UA 1840 FOUND CREW O2 LOW 1430 PSI. SERVICED CREW O2, NO LEAKS WERE NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042300182 20080423 00182 NM 2008 4 23 UPS08M52048 1 20080324 A 5754 ARB2850505 FITTING DOUG MD11 MD11F 3023600 NM LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:4C LEFT WING NR 16 SLAT TRACK IB FITTING CRACKED. REMOVED AND REPLACED NR 16 SLAT TRACK IB RIB FITTING IAW MD-11 SRM 51-31-01 AND 51-33-01. 2 L 7 3 4F RT A22WE 2008042300190 20080423 00190 EA 2008 4 23 A6WA200840242 1 20080318 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 439AW 7753 CRACKS EXISTS ON FRAME FS 280 LBL 9. REPAIR ON FLOORBEAM AT FS 280 LBL 9. PERFORMED IAW REO 601R-53-11-171 REV D. (M) 2 L 7 2 4F RT A21EA 2008042300206 20080423 00206 EA 2008 4 23 MASA200800311 1 20080412 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 654BR 7454 FLT 1950, HNL - ITO. LEFT MID EXTERIOR EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 2008042300212 20080423 00212 EA 2008 4 23 SWIA200819491 1 20080416 A 2730 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA ELEVATORS FAILED A SWIA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 07 969SW 7876 FLT 6126 - ELEVATOR IS VERY STIFF. REPLACED NR 2 LINEAR ACTUATOR IAW CRJ AMM 27-31-23. OPS CHECKS GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 2008041800056 20080418 00056 CE 2008 4 18 BSYA2008010 1 20080408 A 3200 UNKNOWN BEECH 58 58 1152740 CE LANDING GEAR MALFUNCTIONED E BSYA O OTHER O OTHER LD LANDING 1 GL 07 6650D TH1375 ON LANDING INTO HKS PILOT REPORTED, HAD GEAR DOWN AND LOCK INDICATION, BUT WHEN AIRCRAFT TOUCHED DOWN THE NOSE GEAR COLL APSED THEN THE MAINS COLLAPSED. CAUSE IS UNKNOWN AT THIS TIME AS TO WHY ALL THREE GEAR COLLAPSED. 1 L 7 2 3O 3A16 2008041800061 20080418 00061 2008 4 18 ASAA0852805 4 20080404 A 2210 721101A1 SWITCH BOEING 737 737890 1384527 NM AUTOPILOT SYS FAULTY A ASAA K NONE O OTHER NR NOT REPORTED 1 NM 02 583AS 35681 AUTOPILOT "A" WILL NOT ENGAGE. COULD NOT GET AUTOPILOT "A" TO ENGAGE. PERFORMED DFCS BITE SHOWED MULTIPLE DISCONNECT F AILURES. FOUND F/O'S DISCONNECT SWITCH BAD. THE "A" SIDE OF SWITCH STICKS OPEN REQUIRES NUMEROUS PRESSES OF SWITCH TO CLOSE AND ENGAGE AUTOPILOT. REPLACED F/O'S AUTOPILOT DISCONNECT SWITCH. OPS NORMAL. 2 L 7 2 4F RT A16WE 2008041800070 20080418 00070 WP 2008 4 18 ABXA080118 1 20080404 A 3310 LIGHT DOUG DC9 DC941 302207N WP COCKPIT OUT OF POSITION A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 23 954AX 47612 MAP & BRIEFCASE CIRCUIT BREAKER TRIPPED, SMOKE EXITING FROM FIRST OFFICER'S MAP LIGHT ON FIRST OFFICER'S CONTROL COLUMN. REPOSITIONED LIGHT ASSEMBLY. SYSTEM CHECKS GOOD IAW DC9 AMM 33-13-00. 2 L 7 2 4F A6WE 2008041800072 20080418 00072 SO 2008 4 18 C2XA08IA104 1 20080406 A 4900 UNKNOWN EMB 145 EMB145LR 3260212 SO APU ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 16918 145397 IAH - FLIGHT 3144, DURING PRE-FLIGHT INSPECTION THE CREW REPORTED A FUEL SMELL COMING FROM THE APU. MAINTENANCE INSPECT ED THE AIRCRAFT, AND PLACED THE APU ON MEL 49-00-00 CTL#143170 CAT C, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. ON 04/09/08, IAH MAINTENANCE OPERATIONALLY CHECKED THE APU WITH NO SMELL OR DEFECTS NOTED, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 2008041800091 20080418 00091 EU 2008 4 18 USAA920080781 1 20080327 A 5320 D5347112420100 SHEAR PLATE AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 187US 1704 PIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON SHEAR PLATE, BS 3523 / FR 60 - BS 4059 / FR 70, S23R. REPLACED SHE AR PLATE, BS 3523 / FR 60 - BS 4059 / FR 70, S23R IAW A321 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008041800106 20080418 00106 NM 2008 4 18 USAA920080774 1 20080407 A 5210 DOOR BOEING 737 737301 1384611 NM L1 OUT OF ADJUST A USAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 19 591US 23936 FLT 1580 - CLT - PIT - CAPTAIN ABORTED TAKEOFF DUE TO L1 ENTRY DOOR LIGHT ILLUMINATED. MX ADJUSTED FORWARD ENTRY DOOR. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A16WE 2008041800147 20080418 00147 SO 2008 4 18 RAIA00804013 1 20080411 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 833HK 145240 PRE FLT 7884 -ORD- EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RESECURED THE CONNECTION TO THE AFFECTED LIGHT STRIP. 2 L 7 2 4T RT T00011AT 2008041800194 20080418 00194 NM 2008 4 18 USAA920080845 1 20080401 A 5345 SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT- MAJOR REPAIR - C4 CHECK - CORROSION ON GALLEY SUPPORT AT BS 1710 - 1720, WL 208.1, RBL 6. REPLACED SUPPORT IAW SRM 51-10-00, 51-40-02 AND DRAWING 146N5300. 2 L 7 2 4F RT A2NM 2008041800251 20080418 00251 EU 2008 4 18 2008UALA02044 1 20080408 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS MISINSTALLED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 492UA 1755 TEST FLIGHT, EMERGENCY EXIT LIGHTS CAN NOT TURN ON FROM AFT FLIGHT ATTENDANT PANEL WITH COCKPIT SWITCH IN ARM POSITION. FOUND WIRES 1032 AND 1033 SWAPPED AT TB7222VT AND 13WLA. PROPERLY WIRED SYSTEM PER AWM 33- 51-01. OPS CHECKED GOOD PER MM 33-51-00. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041800253 20080418 00253 2008 4 18 2008UALA02046 4 20080408 A 2565 HOSE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SLIDE BOTTLE KINKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 LT OVERWING SLIDE-BOTTLE PRESSURE HOSE IS KINKED SEVERAL SPOTS. SUSPECT HOSE MIS- STOWED DURING MAINTENANCE. REPLACED H OSE IAW SB 767-25-022. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041800254 20080418 00254 NE 2008 4 18 2008UALA02047 2 20080408 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE NR 1 MALFUNCTIONED A UALA O OTHER O OTHER LD LANDING 1 WP 29 668UA 30024 724634 RIGHT ENG NO N1 READING ON TOUCHDOWN. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041800263 20080418 00263 SO 2008 4 18 SWIA200819480 1 20080412 A 3244 TIRE EMB 120 EMB120ER 3260203 SO MLG FAILED A SWIA O OTHER O OTHER LD LANDING 1 NM 07 584SW 120352 FLT 5780 - NR 1 MAIN TIRE FOUND FLAT AFTER LANDING. REPLACED NR 1 AND NR 2 MAIN WHEEL ASSEMBLIES PN 3-1446-1, SN/OFF 06 95, PN 3-1446-1, SN/OFF 1267. 2 L 7 2 4T RT A31SO 2008041800264 20080418 00264 NM 2008 4 18 F3LA200800176 1 20080415 A 5321 D53470477208 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 45 1841 DURING C4 S1 C CHECK INSPECTION NOTED PANEL 251RF HAS TWO PUNCTURES. MAINTENANCE CLEANED AREA OF DAMAGE, PREPPED AND AP PLIED REPAIR IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FO UND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008041800265 20080418 00265 NM 2008 4 18 2008UALA02054 1 20080409 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 805UA 783 FLOORBEAM CORRODED AT FWD GALLEY. MAJOR REPAIR. REPLACED OR REWORK OF CORROSION ACOMP ON SFOOV, BEAM INSTL, INSTG NUT P LATES AND PREPPING FLOOR BOARDS. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041800275 20080418 00275 SO 2008 4 18 C2XA08CL049 1 20080414 A 3232 21180100401 ACTUATOR EMB 145 EMB145XR 3260214 SO NLG MALFUNCTIONED A C2XA K NONE J WARNING INDICATION AP APPROACH 1 SW 27 11106 15649 145650 CLE FLIGHT 2879 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL WHEN GEAR WAS SELECTED DOWN. MAINTENANCE INSPECTED AND REPLACED THE RIGHT NOSE GEAR DOOR ACTUATOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2008041800284 20080418 00284 2008 4 18 BB08062 4 20080413 A 2310 7926140001 COUPLER BOEING 757 7572B7 1384964 NM HF ANTENNA INOPERATIVE A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 202UW 3112 2747 27811 DUB - FLT 723 EN ROUTE DUB TO PHL. BOTH HF RADIOS BECAME INOPERATIVE DURING THE FLIGHT. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT HF ANTENNA COUPLER. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 2008041800295 20080418 00295 NM 2008 4 18 USAA920080806 1 20080326 A 5320 SHEAR WEB BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A 5" X 7" AREA OF CORROSION ON SHEAR WEB AT BS 988 - 989, LBL 30 - 31. INSTALLED REPAIR IAW SRM 51-70-13 PG 1-3. 2 L 7 2 4F RT A16WE 2008041800300 20080418 00300 NM 2008 4 18 USAA920080811 1 20080406 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A .25" CRACK ON FLOORBEAM ANGLE AT BS 328, LBL 26. INSTALLED REPAIR IAW SRM 53-10-51 FI G 201. 2 L 7 2 4F RT A16WE 2008041800303 20080418 00303 NM 2008 4 18 USAA920080814 1 20080409 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - CORROSION ON ANGLE AT BS 300 - 328, RBL 59. INSTALLED REPAIR IAW SRM 53-10-15 FIG 101, 51-10-02. 2 L 7 2 4F RT A16WE 2008041800306 20080418 00306 NM 2008 4 18 USAA920080817 1 20080403 A 5320 6545834312 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - CORROSION ON CHORD ANGLE AT BS 294 - 312, RBL 16. REPLACED ANGLE IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008041800322 20080418 00322 NM 2008 4 18 USAA920080872 1 20080328 A 5312 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 23634 CLT - MAJOR REPAIR-C22 CHECK - A 3 EACH 1" CRACKS ON WEB AT BS 178, WL 213, RBL 5.5. INSTALLED DOUBLER REPAIR IAW SRM 5 3-10-08 REPAIR 9 FIG 201. 2 L 7 2 4F RT A16WE 2008042100009 20080421 00009 NM 2008 4 21 2008UALA02130 1 20080411 A 5320 RETAINER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GALLEY DOORWAY MISINSTALLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 FWD GALLEY DOOR, FRAME UNDER SEAL RETAINER, AFT SIDE HAS PRE-DRILLED HOLES WITH INSUFFICIENT SPACING JUST ABOVE NEW FRAM E. MAJOR REPAIR ACCOMPLISHED: REPLACED AFT FRAME. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041800141 20080418 00141 NM 2008 4 18 F3LA200800197 1 20080417 A 3350 BULB AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE EMERGENCY LIGHT INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 905FR 10 1583 DURING PRE FLIGHT INSPECTION, THE FLIGHT CREW REPORTED SEAT ROWS 9 AND 22 HAD ONE SEGMENT OF LIGHTS FOUND BURNED OUT DUR ING PRE FLIGHT TEST. MAINTENANCE REMOVED AND REPLACED ONE BULB FROM ROW 22 IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 3 1-51-00 AND DEFERRED EMERGENCY LIGHT IN ACCORDANCE WITH THE REQUIREMNTS OF MEL 33-50-03A. 2 L 7 2 4F 4 F RT A28NM E37NE 2008041800146 20080418 00146 SO 2008 4 18 RAIA00804007 1 20080408 A 3150 80069425 COMPUTER EMB 145 EMB145LR 3260212 SO COCKPIT FAULTY A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 815HK 145048 FLT 5468 -STL- TAKEOFF CONFIGURATION WARNING AFTER WHEELS OFF DURING CLIMB. MAINTENANCE REMOVED AND REPLACED THE AURAL WARNING COMPUTER AND PERFORMED ASSOCIATED FOLLOW-ON MAINTENANCE WITH NO ADDITIONAL DISCREPANCIES. 2 L 7 2 4T RT T00011AT 2008041800158 20080418 00158 SO 2008 4 18 RAIA00804011 1 20080409 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DAMAGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 813HK 145044 FLT 5452 -IND- VARIOUS CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED THE CONNECTOR TO THESE FLOOR STRIP LIGH TS. PERFORMED AN OPERATIONAL CHECK WITH NO ADDITIONAL DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008041800160 20080418 00160 SO 2008 4 18 C2XA08IA108 1 20080409 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 34110 145658 IAH - FLIGHT 2496, THE CREW REPORTED A FUEL SMELL IN THE COCKPIT AFTER T/O WHEN BLEEDS SWITCHED TO ENGINE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THAT AIRCRAFT, OPERATIONALLY CHECKED THE APU AND BLEED SYSTE MS WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008041800161 20080418 00161 NM 2008 4 18 USAA920080839 1 20080330 A 5315 141N51626 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT - MAJOR REPAIR - C4 CHECK - A 1" X 3" AND 4" X 6" CORROSION AREAS ON FLOOR RAIL AT BS 365-395, RBL 10. MANUFACTURE D AND REPLACED RAIL IAW BOEING DRAWING 141N5162-6. 2 L 7 2 4F RT A2NM 2008041800167 20080418 00167 WP 2008 4 18 08FDEA01441 1 20080417 A 5347 NEA602241 SEAT TRACK DOUG DC10 DC1010F 3022111 WP ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION IN UPPER FUSELAGE AT STA 1209 X= 47.250 SEAT TRACK WITH MISSING MATERIAL. REPAIRED FOR S RM 53-70-00 FIG 1 VOL I. 2 L 7 3 4F A22WE 2008041800169 20080418 00169 EA 2008 4 18 A6WA200840184 1 20080306 A 5340 HINGE CNDAIR CL600 CL6002B19 1900309 EA DOOR STEP CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 410AW 7490 PAX DOOR FOLDING STEP UPPER HINGE, REF P/N 601R31980-41, AND LOWER HINGE , REF P/N 601R31980-63 FOUND CRACKED. (M) 2 L 7 2 4F RT A21EA 2008041800170 20080418 00170 EA 2008 4 18 A6WA200840212 1 20080318 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 PAX DOOR AFT WEB DRAG ANGLE IS CRACKED. REPAIRED IAW REO 601R-52-11-513 REV A. (M) 2 L 7 2 4F RT A21EA 2008041800173 20080418 00173 EA 2008 4 18 A6WA200840247 1 20080319 A 5340 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 439AW 7753 CRACK FOUND ON HYDRAULIC SUPPORT BRACKET ON MLG BAY LEFT. NEW SUPPORT BRACKET ON MLG BAY INSTALLED IAW SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2008041800174 20080418 00174 EA 2008 4 18 A6WA200840204 1 20080313 A 5210 HINGE CNDAIR CL600 CL6002B19 1900309 EA DOOR STEP CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 PAX DOOR FOLDING STEP UPPER HINGE FOUND CORRODED. PAX DOOR FOLDING STEP UPPER HINGE REPLACED WITH SERVICEABLE ITEM IAW CRJ 200 SRM 51-40-11 AND 51-41-04. (M) 2 L 7 2 4F RT A21EA 2008041800176 20080418 00176 EA 2008 4 18 A6WA200840214 1 20080314 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR PUNCTURED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 TOP STAIR ASSY IS PUNCTURED IN THE TREAD AREA. TOP STAIR ASSY PUNCTURED AREA REPAIRED IAW REO 601R-52-11-1457. (M) 2 L 7 2 4F RT A21EA 2008041800177 20080418 00177 EA 2008 4 18 A6WA200840215 1 20080313 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 CARGO POST NET BRACKET COMMON TO FORWARD FACE CRACKED, LOWER BRACKET. BRACKET REMOVED IAW SRM 51-42-06, BRACKET FABRICA TED IAW SRM 51-24-21 AND FABRICATED BRACKET INSTALL IAW SRM 51-42-06. (M) 2 L 7 2 4F RT A21EA 2008041800179 20080418 00179 WP 2008 4 18 08FDEA01444 1 20080417 A 5420 9071M78P001A BRACKET DOUG MD10 MD1010F 3022112 WP NR 3 NACELLE BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 NR 3 ENGINE INBD AND OUTBD CENTER T/R ALIGNMENT PADS ARE BENT. REMOVED AND REPLACED IAW SRM 51-35-02; VOL II AND EM-78 -32-03; REPAIR 17. VERIFIED GAP AND LATCH CHECKS GOOD AT THE NR 3 T/R IAW AMM 78-32-11-2. 2 L 7 3 4F RT A22WE 2008041800181 20080418 00181 NM 2008 4 18 08FDEA01446 1 20080417 A 2613 675530144 HOSE BOEING 727 727233 138408A NM NR 1 OVERHEAT LEAKING A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 257FE 20939 ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT COMPLIED WITH QRH. AIRCRAFT INCURRED A MAINTENANCE FLIGHT DIVERS ION INTO ATL. FLIGHT CREW ADVISED, THAT, THE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED AT APPROXIMATELY 10,000 FT, DURING C LIMB-OUT WITH AN EPR 1.95 INDICATION DISPLAYED, ENGINE NR 1 STRUT OVERHEAT LIGHT 'EXTINGUISHED' WHEN THROTTLE WAS RETA RDED. R&R MODULATING SHUTOFF VALVE SENSE LINE. NR 1 ENGINE REQUIRES LEAK CHECK RUN OF SENSE LINES AND INSTALLATION OF S TRUT PANELS. RAN NR 1 ENGINE AT 75% N1 FOR A DURATION OF 40+ MINS - RAN WITH BLEEDS OPEN. ALL CHECKED GOOD - NO LEAKS FOUND - A/C RETURNED TO SERVICE. 2 L 7 3 4F RT A3WE 2008041800182 20080418 00182 EU 2008 4 18 08FDEA01447 1 20080401 A 5420 A5461177650200 STIFFENER AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 724FD 530 PYLON NR 1 STIFFENER AT RIB 9 WITH CORROSION. THE STIFFENER WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 2008041800184 20080418 00184 NM 2008 4 18 08FDEA01449 1 20080417 A 5340 65496525 ATTACH BRACKET BOEING 727 727232 1384082 NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 MAIN ENTRY DOOR 1-L, S/N 261, UPPER AFT LINER ATTACH BRACKET IS CRACKED REMOVED BRACKET IN REF TO SRM 51-30-2 PG 2, VERI FIED MAT'L AS 2024 T3 .040" IN REF TO DWG 65-49652-5 FABRICATED NEW ANGLE IN REF TO DWG 65-49652-5. TREATED AND PRIMED ANGLE IN REF TO SRM 51-10-2 PG 2, APPLIED FX P/N FX65-49652-5 IN REF TO GMM 7-0-1001. INSTALLED NEW ANGLE IN REF TO 51 -30-2 PG 2. CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 2008041800185 20080418 00185 EU 2008 4 18 08FDEA01450 1 20080417 A 3230 MS28775015 PITCH LINK AIRBUS 310 A310222 3930315 EU MLG DAMAGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 455FE 331 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF WITH BOTH SELECTOR. GEAR HANDLE WOULD NOT COME PASSED THE NORMAL POSITION. PRESSURE INDICATOR POP OUT. T/S IN PROGRAM. NEED PART. T/S FOUND PITCH DAMPER AIR CHARGE VALVE PACKING DAMAGED. RE MOVED AND REPLACED PACKING AND SERVICING PITCH DAMPER WITH NITROGEN PER AMM 12-12-30-0. INSPECTED NOT LEAK FOUND. A/C OK FOR SERVICE. 2 L 7 2 4F RT A35EU 2008041800189 20080418 00189 NM 2008 4 18 USAA920080841 1 20080403 A 5313 BAC148236 STRINGER BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT- MAJOR REPAIR - C4 CHECK - A 1" CRACK ON STRINGER 3R BETWEEN BS 1020 AND BS 1040. INSTALLED REPAIR IAW SRM 53-00-03 FIG 201. 2 L 7 2 4F RT A2NM 2008041800196 20080418 00196 NM 2008 4 18 USAA920080847 1 20080401 A 5320 146N5246U8 FLOOR SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT- MAJOR REPAIR - C4 CHECK - CORROSION ON FLOOR SUPPORT AT BS 1640 - 1661, RBL 54. REPLACED SUPPORT IAW SRM 51-40-02 . 2 L 7 2 4F RT A2NM 2008041800199 20080418 00199 NM 2008 4 18 USAA920080850 1 20080402 A 5320 FLOOR SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT- MAJOR REPAIR - C4 CHECK - A 1" CRACK ON FLOOR SUPPORT WEB AT BS 1681, WL 208.1, RBL 10. REPLACED WEB IAW SRM 51-40 -02. 2 L 7 2 4F RT A2NM 2008041800205 20080418 00205 EU 2008 4 18 USAA920080856 1 20080331 A 5320 BEAM AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 187US 1704 PIT - MAJOR REPAIR - S3 CHECK - CORROSION ON SILL BEAM AT FR66 (AFT SERVICE ENTRY DOOR THRESHOLD). INSTALLED REPAIR IAW SRM 53-41-14. 2 L 7 2 4F RT A28NM 2008041800230 20080418 00230 NM 2008 4 18 USAA920080859 1 20080409 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT - MAJOR REPAIR - C4 CHECK - A .2" CRACK ON FUSELAGE SKIN AT BS 1630, STR 4R. INSTALLED DOUBLER / TRIPLER REPAIR IAW EA 110817/. 2 L 7 2 4F RT A2NM 2008041800233 20080418 00233 NM 2008 4 18 QXEA200800375 1 20080411 A 5240 HANDLE BOMBDR DHC8 DHC8402 1390042 NM SERVICE DOOR CONTAMINATED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 420QX 4147 SEA - AFT GALLEY SERVICE DOOR HARD TO OPEN AND CLOSE. REMOVED DEBRIS FROM THE DOOR HANDLE AREA. OPERATIONAL CHECKS GOO D. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008041800235 20080418 00235 NM 2008 4 18 2008UALA02038 1 20080409 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 809UA 825 FOUND BEAM 105 CORRODED WHILE ACCOMPLISHING EQ3700 CALLOUT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED AT LCQ. REMOVED BEAM. BEAM 105 AND 150 INSTALLED AS A UNIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041800236 20080418 00236 NM 2008 4 18 2008UALA02039 1 20080408 A 5414 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 NR 2 PYLON UPPER WEB FUEL LINE CUTOUT SKIN CRACKED AT NAC STA 178. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR, ACCOMPLISHED REMOVED EXISTING REPAIR DOUBLER FROM NAC STA 172 TO 178. STOP DRILLED CRACK AND ACCMP'D HFEC TO VERIFY DAMAGE REMOVED. FABRICATED AND INSTALLED A REPAIR DOUBLER AND SPLICE TO INCORPORATE ENTIRE AREA. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041800237 20080418 00237 NM 2008 4 18 2008UALA02040 1 20080408 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 540 S24L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 DENTED FUSELAGE FRAME, INBOARD FLANGE AT BS 540 BETWEEN STR 24L AND 25L. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLI SHED, CUTOUT DAMAGED FRAME FLANGE. FABRICATED AND INSTALLED A REPAIR ANGLE J-SECTION, STRINGER CLIP (P/N 140N2001-80) A ND SHEAR TIE (P/N 140N2002-664). 2 L 7 2 4F 4 F RT A2NM E17NE 2008041800238 20080418 00238 NM 2008 4 18 2008UALA02041 1 20080408 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1400 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 535UA 25130 AFT PIT LT SIDE, FRAME INBOARD FLANGE DENTED AT BS 1400 ABOVE STR 25L. REPAIRED IAW REO G12301 REV B AND EVA 71401 BY M ECH 7762 AND INSP BY QC 177 ON NR 27640. THIS RPR HAS RECEIVED ONLY 1ST STAGE APPROVAL PENDING FATIGUE AND DTA EVALUATIO N BY BOEING TO SHOW COMPLIANCE WITH 14 CFR 25.571 AND 26.43D. ACFT MUST BE REMOVED FROM SERVICE ON 08APR09 UNLESS A NEW 8100-9 IS ISSUED PRIOR TO THAT DATE SHOWING COMPLIANCE. 2 L 7 2 4F 4 F RT A2NM E17NE 2008041800239 20080418 00239 EU 2008 4 18 2008UALA02042 1 20080408 A 2597 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DOOR 1L SHORTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 428UA 523 3 SVC EMERGENCY LIGHT TEST FAILS. MED 1L SLIDE LIGHT NOT TESTING. FOUND SHORTED WIRE INSIDE ASSY SLIDE AT 1L. REPLACE D DOOR SLIDE 1L. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041800240 20080418 00240 EU 2008 4 18 F3LA200800177 1 20080406 A 5315 D5397497200200 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION REPORTED NUT PLATE CORRODED OUTBOARD OF CENTER FLOORBEAM AFT CARGO PIT C 56 1. MAINTENA NCE REMOVED AND REPLACED NEW C 56 PROFILE PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 PARAGRAPH 6 AND AIRB US DRAWING 17D53974965. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008041800241 20080418 00241 2008 4 18 2008UALA02043 4 20080408 A 2397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OXYGEN MASK SHORTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 411UA 464 F/O'S OXYGEN MASK MICROPHONE IS INOPERATIVE. FOUND INTERNAL SHORT. REPLACED FO MASK. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041800246 20080418 00246 NM 2008 4 18 USAA920080867 1 20080330 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 A .3125 INCH CRACK IN FUSELAGE SKIN AT CORNER OF LWR AFT SERVICE DOOR. REPAIRED IAW EA 100368. 2 L 7 2 4F RT A16WE 2008041800250 20080418 00250 NM 2008 4 18 USAA920080871 1 20080414 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 445US 24863 A 1.125" CRACK ON FUSELAGE SKIN AT BS 1088 (AFT JACK PAD), S24R-S25R. INSTALLED DOUBLER REPAIR IAW SRM 53-80-01, REPAIR 04, FIG 201. 2 L 7 2 4F RT A16WE 2008041800278 20080418 00278 SO 2008 4 18 C2XA08IA110 1 20080413 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 14116 145672 IAH - FLIGHT 2121, ON TAKEOFF THE CREW REPORTED A FUEL ODOR THAT GOES AWAY WHEN SWITCHING FROM APU BLEED TO ENGINE BLEED . THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE OPERATIONALLY CHECKED THE BLEED SYSTEM WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008041800280 20080418 00280 2008 4 18 BB08058 4 20080412 A 2565 D31041147 SLIDE BOEING 757 7572B7 1384964 NM R3 DOOR LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 938UW 39003 593 27246 PHL - THE EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE AT DOOR R3 WAS LOW. MAINTENANCE REPLACED THE R3 DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2008041800282 20080418 00282 2008 4 18 BB08060 4 20080413 A 2310 6225272001 TRANSCEIVER BOEING 757 7572B7 1384964 NM HF COMM INOPERATIVE A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 202UW 3112 2747 27811 DUB - FLT 723 EN ROUTE DUB TO PHL. BOTH HF RADIOS BECAME INOPERATIVE DURING THE FLIGHT. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT HF RADIO TRANSCEIVER. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 2008041800283 20080418 00283 2008 4 18 BB008061 4 20080413 A 2310 6225272001 TRANSCEIVER BOEING 757 7572B7 1384964 NM HF COMM INOPERATIVE A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 202UW 44871 1428 27811 DUB - FLT 723 EN ROUTE DUB TO PHL. BOTH HF RADIOS BECAME INOPERATIVE DURING THE FLIGHT. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT HF RADIO TRANSCEIVER. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 2008041800289 20080418 00289 NM 2008 4 18 USAA920080800 1 20080327 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A .125" CRACK ON FRAME AT BS 727B, STR 8R AND STR 9R. INSTALLED REPAIR IAW SRM TR 53-10 -20. 2 L 7 2 4F RT A16WE 2008041800290 20080418 00290 NM 2008 4 18 USAA920080801 1 20080319 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A .5" CRACK ON FRAME AT BS 727D BETWEEN STR 8R AND STR 9R. INSTALLED REPAIR IAW SRM TR 53-10-20E. 2 L 7 2 4F RT A16WE 20080711 EA 2008 7 11 MASA200800417 1 20080524 A 3350 BATTERY CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 515MJ 10117 ASH FLT 7099 SAT- DEN. AC EMERGENCY LIGHTS WILL NOT ILLUMINATE. CHARGED BATTERIES, EMERGENCY LIGHTING SYSTEM OPS GOOD. 2 L 7 2 4F RT A21EA 20080711 NM 2008 7 11 DHL2008764524 1 20080525 A 5752 SKIN BOEING 727 727264 138408M NM AILERON TAB DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C-CHECK, LT WING O/B AILERON TAB LWR I/B SURFACE DELAM WBL 492. CUT OUT DELAMINATED AREA 1 INCH DIA AND APPLIE D POTTING COMPOUND. FABRICATED DOUBLER 3 INCH DIA FROM.010" 2024-T3 PO 9003621. BONDED DOUBLER, CLEANED PRIMED AND SEA LED IAW B727 SRM 51-40-22 AND 57-50-02. 2 L 7 3 4F A3WE 20080711 NM 2008 7 11 ASAA0843095 1 20080507 A 5311 65465588 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 RT FRAME AT STA 907 CRACKED AT PSU RAIL BRACKET. FRAME REPAIRED IAW ASA EA5310 02797. 2 L 7 2 4F RT A16WE 20080711 EU 2008 7 11 08FDEA02040 1 20080530 A 5320 A53832103206 WEB AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CRACKS ON INTERNAL WEB BETWEEN BEAM 3 AND 4 LT/RT. REPAIR PERFORMED BY CRACK STOP HOLE AND DOUBLER INSTALLATION I AW RAS 70507081/004/2008, APPROVED BY EA 6-5315-120051. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 DL764080843 1 20080609 A 2121 4100941B FAN BOEING 767 767432ER 1385134 NM COCKPIT ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 833MH 29706 MILD ODOR IN COCKPIT AND CABIN 6 HOURS INTO FLT WHILE CRUISING AT FL330. ODOR SEEMED ELECTRICAL. DISSIPATED THEN RETU RNED 15 MINS LATER WITH R RECIR FAN EICAS MESSAGE. UNLATCHED RIGHT RECIRC FAN SWITCH IAW MCC DIRECTION. NDS MFN 410094 1B NIS ATL, REPLACED RT RECIRC FAN OPS CK OK NO SMELL PRESENT MCO AND PLACARD REMOVED. ETOPS CATEGORY 'E': PROBLEMS WIT H SYSTEMS CRITICAL TO ETOPS. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 UPS08652336 1 20080515 A 5711 112T2252Y4 STIFFENER BOEING 767 76734AF 1385212 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 302UP 27240 INSPECTION TYPE:N/A RIGHT WING LES 665 FRONT SPAR STIFFENER UPPER AREA FOUND CRACK. CRACK LENGTH .5 INCH APPROX. RIGHT WING LES 665 FRONT SPAR STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 UPS08652348 1 20080525 A 2613 THERMAL SWITCH BOEING 767 76734AF 1385212 NM LT BLEED DUCT INOPERATIVE A IPXA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 319UP 27758 INSPECTION TYPE:ETOP ATB - DUCT LEAK LIGHT ILLUM. EICAS MSG: LEFT BLEED DUCT LEAK DISPLAYED. FUEL DUMPED. REPLACED M 691 CONTROL CARD PER MM 26-10-01-4. REPLACED S236 THERMAL SWITCH PER MM 26-18-01-4. REMOVED AND REPLACED S237 THERMAL SWITCH PER MM 26-18-01-4. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 ASAA0843094 1 20080507 A 5311 65465588 FRAME BOEING 737 7374Q8 138447Q NM BS 907 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 LT FRAME AT STA 907 CRACKED AT PSU RAIL BRACKET. FRAME REPAIRED IAW ASA EA5310 02797. 2 L 7 2 4F RT A16WE 2008042100032 20080421 00032 2008 4 21 2008UALA02077 4 20080409 A 2565 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR SLIDE MISINSTALLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 487UA 1669 DOOR 2L SLIDE COVER MIS-INSTALLED. REMOVED SLIDE AND REPLACED IT WITH CORRECT SLIDE FOR THAT POSITION. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042100035 20080421 00035 2008 4 21 2008UALA02080 4 20080408 A 2397 WIRE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE O2 MASK MIC DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 824UA 965 CAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. FOUND WIRE PULLED OUT OF CONNECTOR THAT CONNECTS INSIDE THE BOX. REPLA CED THE O2 MASK STOWAGE BOX, OPS CHECKED NORMAL, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042100095 20080421 00095 EA 2008 4 21 COMA0860223 1 20080413 A 2731 706010 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA ELEVATOR TRIM FAULTY A COMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 01 587SW 980 7062 FLIGHT 5665 - MOMENTARY ELEVATOR DOWN TRIM ON TAKEOFF. ABORTED TAKEOFF SAFELY. REMOVED AND REPLACED HSTCU. 2 L 7 2 4F RT A21EA 2008042100120 20080421 00120 NM 2008 4 21 YENA2008033 1 20080412 A 3230 17071000407 ACTUATOR EMB ERJ190 ERJ190100IGW 3260408 NM RT MLG UPLOCK FAILED A YENA O OTHER S AFFECT SYSTEMS AP APPROACH 1 EA 15 206JB 5563 5563 19000025 FLT 620, JFK-BUF, WHEN LG LEVER WAS SELECTED TO DOWN RT MAIN INDICATED UP AND LG DISAGREE EICAS ILLUMINATED. ACCOMPLISH ED LG DISAGREE CHECKLIST. GEAR REMAINED RETRACTED. PERFORMED ABNORMAL GEAR EXT AND RT MAIN EXTENDED AND INDICATED NORM AL WHEN ALT GEAR EXT LEVER WAS PULLED. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM 32-31-03, OPS CHECK AND LEAK CHECK OK. OPERATED GEAR SEVERAL TIMES AND NO DEFECTS NOTED. 2 L 7 2 4F RT A57NM 2008042100125 20080421 00125 EU 2008 4 21 08FDEA01453 1 20080418 A 3230 MS28775010 PACKING AIRBUS 310 A310222 3930315 EU CHARGE VALVE DAMAGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 455FE 331 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF WITH BOTH SELECTOR. GEAR HANDLE WOULD NOT COME PASSED THE NORMAL POSITION. T/S FOUND PITCH DAMPER AIR CHARGE VALVE PACKING DAMAGED. REMOVED AND REPLACED PACKING AND SERVICING PITCH DAMPER WITH NITROGEN PER AMM 12-12-30-0. INSPECTED NOT LEAK, FOUND. A/C OK FOR SERVICE, NO FUTHER REPORTS. 2 L 7 2 4F RT A35EU 2008042100137 20080421 00137 NM 2008 4 21 QXEA200800383 1 20080416 A 5210 SEAL BOMBDR DHC8 DHC8402 1390042 NM AFT PAX DOOR DIRTY A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 400QX 4030 SEA - REAR PASSENGER DOOR IS HARD TO OPEN AND CLOSE. MAINTENANCE CLEANED AND LUBRICATED THE SEAL. OPERATIONAL CHECKS G OOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008042100152 20080421 00152 NM 2008 4 21 F3LA200800180 1 20080417 A 5210 D5211021420200 FITTING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE PAX DOOR FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 45 1841 DURING C4 S1 C CHECK INSPECTION REPORTED THE FORWARD ENTRY DOOR FAILED RIG CHECK AT TORSION BAR BELL CRANK AND REDUCER S HAFT BELLCRANK. MAINTENANCE REMOVED AND REPLACED LEFT FITTING FOR RIG PIN AND ADJUSTED DOOR RODS IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 52-11-21-400-001 AND CHECKED RIG PINS IN ACCORDANCE WITH THE REQUIREMENTS OF WORK CARD C528002-2 ST EP 4B. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042300013 20080423 00013 EA 2008 4 23 MASA200800299 1 20080408 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75987 7405 ASH FLT 7337 IAD. PAX DOOR HARD TO OPEN. LUBED PAX DOOR HANDLE. 2 L 7 2 4F RT A21EA 2008042300034 20080423 00034 NM 2008 4 23 USAA920080900 1 20080408 A 5330 6545775 SKIN BOEING 737 73733A 1384673 NM BS 873-895 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 164AW 23625 CLT - MAJOR REPAIR-C21- THREE 3 CRACKS ON FUSELAGE SKIN AT BS 873-895, STR 24R-STR 25R. INCORPORATED INTO 1. REPAIR IA W SRM 53-00-01-2R31 FIG 201. 2 L 7 2 4F RT A16WE 2008042300060 20080423 00060 NM 2008 4 23 2008UALA02226 1 20080416 A 3397 FEEDER CABLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS CUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 347UA 24251 FLOOR EMERGENCY LIGHTS INOP FROM SEAT 15ABC TO AFT GALLEY CARPET. REPLACED EEL LIGHT RIBBON CABLE, REF 33-50-00 OP CHEC KED OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042300061 20080423 00061 EU 2008 4 23 UPS08151997 1 20080324 A 5753 A57960000007 SKIN AIRBUS A300 A300F4622R 3930360 EU T/E FLAP DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 150UP 0833 INSPECTION TYPE:5YR RIGHT I/B FLAP LOWER SKIN I/B OF NR 2 FLAP TRACK DENT. MEASURED DENT AND FOUND OUT OF LIMITS IAW A3 00 SRM 57-50-00 FIG 101. CUT OUT DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SAA EA 300-5730-01-A1334. 2 L 7 2 4F RT A35EU 2008042300077 20080423 00077 NM 2008 4 23 UPS08551999 1 20080411 A 5610 CRANK ASSY BOEING 757 75724APF 1384969 NM COCKPIT WINDOW OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 471UP 28842 INSPECTION TYPE:N/A CAPTAIN UNLOCK LEVER REQUIRES EXCESSIVE FORCE TO OPEN. IF WINDOW CRANK IS MOVED, THEN PRESSURE RELE ASED FROM UNLOCK LEVER. FOUND OPERATING CRANK AFT AND ABOVE CRANK HORIZONTAL CENTER LINE. REPOSITIONED CRANK TO FWD AN D BELOW CRANK HORIZONTAL CENTER LINE. WINDOW CKS SATISFACTORY W/REF TO AMM 56-11-02-5 PARA 3.B (2). 2 L 7 2 4F RT A2NM 2008042300097 20080423 00097 WP 2008 4 23 UPS08852001 1 20080409 A 3530 SEAL DOUG DC8 DC873F 302199F WP PBE MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:N/A CREW PBE MISSING THE UPPER GREEN LOCKED SEAL. REPLACED LOCK SEAL. 2 L 7 4 4F RT 4A25 2008042300161 20080423 00161 EA 2008 4 23 A6WA200840103 1 20080219 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 438AW 7748 FLAPS FAIL AT ZERO ON APPROACH. C/W RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4, FLAP SYSTEM RESET OK. RES ET NOTED BY MAINTENANCE. (M) 2 L 7 2 4F RT A21EA 2008042300164 20080423 00164 EU 2008 4 23 F3LA200800173 1 20080410 A 5340 D5348015800700 FITTING AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED R2 FORWARD GIRT BAR FITTING PLATE CORODDED IN SEVERAL PLACES. MAINTENANCE REMOVED AND REPLACED FITTING PLATE. OKAY TO INSTALL AND INSTALL WILL BE ACCOMPLISHED ON WORK CARD CP753-36. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042300215 20080423 00215 NM 2008 4 23 2008UALA02249 1 20080418 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY LIGHT ROW 5A INOP. RESPLICED EEL CABLE. OP CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300218 20080423 00218 NM 2008 4 23 2008UALA02251 1 20080418 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 DOOR 4 LT EMERGENCY LIGHT BATTERY CHARGE IS LOW. REPLACED LIGHT ASSEMBLY OP CHECKS GOOD PER AMM33-51-12 PB200. AC OK FO R SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300220 20080423 00220 WP 2008 4 23 CLCA040801 1 20080409 A 5270 H2024B PROXIMITY SWITCH DOUG DC10 DC1030F 3023504 WP CARGO DOOR DEFECTIVE A CLCA J A DUMP FUEL UNSCHED LANDING P NO WARNING INDICATION TO TAKEOFF 1 SO 29 612GC 47840 AIRCRAFT WOULD NOT PRESSURIZE. FOUND FWD MAIN CARGO DOOR VENT OPEN. 2 L 7 3 4F RT A22WE 2008042300223 20080423 00223 SO 2008 4 23 SIMA200810902 1 20080410 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO CARGO DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 632AE 19993 5000 145143 DURING A MBV INSP, THE BAGGAGE DOOR CUTOUT LOWER SILL WAS FOUND CORRODED. REMOVED THE DAMAGED SILL AND CLEANED THE AREA . POSITIONED NEW SILL AND MARKED AND DRILLED, COUNTERSUNK AND ALODINED PART. INSTALLED NEW PART. REPAIR DONE IAW EMBR AER 145 SRM (SRM EMB 145/1142 REV. 39) CHAPTERS 51-20-01, 03, 51-40-02, 04 AND 51-40-06. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008042300230 20080423 00230 SO 2008 4 23 CHQA200800079 1 20080414 A 2810 14569688903 GASKET EMB 145 EMB145LR 3260212 SO ALLSN AE300 AE3007A GL TANK PANEL 6 MISSING A CHQA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 11 566RP 145691 CAE311768 FLIGHT 6239, BOS TO SAV, DURING CRUISE, THE FLIGHT ATTENDANT NOTIFIED THE FLIGHT CREW OF A FLUID LEAK COMING FROM THE LE FT WING. THE FLIGHT CREW VERIFIED THE FLUID LEAK AND DIVERTED TO IAD. THE FLIGHT LANDED WITHOUT INCIDENT IN IAD. MAIN TENANCE INSPECTED THE LEFT WING AND TRACED THE SOURCE OF THE LEAK TO THE NR 6 FUEL TANK ACCESS PANEL. THE PANEL GASKET WAS REPLACED, THE TANK LEAK CHECKED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 2008042300231 20080423 00231 EA 2008 4 23 A6WA200840239 1 20080319 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 625 S14R CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 439AW 7753 CRACK FOUND ON BRACKET OF INTERCOSTAL FS 625 STRINGER 14RT. BRACKET ON INTERCOSTAL FS 625 STRINGER 14 RT REMOVED AND RE PLACED IAW CRJ 200 SRM 51-42-21. (M) 2 L 7 2 4F RT A21EA 2008042300243 20080423 00243 NM 2008 4 23 SWAA081939 1 20080412 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 512, BETWEEN STR 16L AND STR 17L. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 2008042300253 20080423 00253 NM 2008 4 23 SWAA081945 1 20080413 A 5753 6573731 SKIN BOEING 737 7373H4 1384600 NM MIDFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND RT WING INBOARD MIDFLAP LOWER SURFACE DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 2008042300259 20080423 00259 EU 2008 4 23 2008UALA02143 1 20080413 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SEAT 22A INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 416UA 479 EMERGENCY LIGHT INOP AT SEAT 22A. REPLACED LIGHT AND HARNESS. CHECKS OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042300260 20080423 00260 NM 2008 4 23 SWAA081963 1 20080413 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300264 20080423 00264 NM 2008 4 23 UPS08M52010 1 20080214 A 5313 LONGERON DOUG MD11 MD11 3023602 NM BS 1721 L46L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C CENTER CARGO BILGE LT 46 STA 1721 FOUND CORROSION AS MARKED ON LONGERON STA 1721 L46 LT CORROSION REMO VED, REMOVED THK0.027" ORIG THK:0.072 INCH FOUND EXCEEDED LIMIT PER SRM 53-10-00 FIG 2A V.1R.40. CORRODED LONG SPLICE C UT C/OUT AT STA 1691 L46 LT PER SRM 53-10-00 FIG 1V.1R.40. NEW LONG REWORK C/OUT FR MATL S2922456X7075T6511 PER DWG AFA 7753 S2931860-7075T6511 PER SRM 53-10-00 FIG 2 V.1R.40. FPI C/OUT PER DAC NDT SPM, FOUND NO CRACK. 2 L 7 3 4F RT A22WE 2008042300265 20080423 00265 NM 2008 4 23 SWAA081964 1 20080413 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300266 20080423 00266 NM 2008 4 23 SWAA081965 1 20080413 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300267 20080423 00267 NM 2008 4 23 UPS08M52011 1 20080115 A 5710 STRUCTURE DOUG MD11 MD11 3023602 NM LT WING LE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C LT WING OUTBOARD FIXED L/E AT NR 8 SLAT 13 INCHES LONG GROOVE WORN FROM CONTACT WITH SEAL RETAINER, OU T OF LIMITS. GROOVE MARK REWORKED PER SRM 51-21-01V.2R35 ORIG THK:0.040", MAT`L REMVD :0.007", MATL REM:0.033" FOUND EX CEED LIMIT PER SRM 57-10-00 FIG 12 V.1 R.35. REWORKED AREA PROTECTED PER SRM 51-21-01V.2R.35. HFEC INSP C/OUT PER DAC NDTSPM R.13,06-10-01.001 FOUND NO CRACK EVIDENT. PAINT TOUCH UP ON REWORKED AREA PER SRM 51-21-01 V.2R.40. 2 L 7 3 4F RT A22WE 2008042300269 20080423 00269 NM 2008 4 23 UPS08M52012 1 20080214 A 5313 LONGERON DOUG MD11 MD11 3023602 NM BS 1721 L44L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C CENTER CARGO BILGE LH44 STA 1721 FOUND CORROSION AS MARKED ON LONGERON UNDERSIDE. LONGERON CORROSION REMOVED AND FOUND EXCEEDED LIMIT PER SRM 53-10-00 FIG 2A V.1R.40. MATL REMOVED:0.044", ORIG THK:0.071". CORRODED LONG SPLICE CUT C/OUT AT STA 1671 L44 LT PER SRM 53-10-00 FIG 1V.1R.40. NEW LONG REWORK C/OUT FR MATL S2931952X7075T6511 PER DWG AFA7792 AND SPLICE REWORKED C/OUT FR MATL S293180-7075T6511 PER SRM 53-10-00 FIG.2V.1R.40. 2 L 7 3 4F RT A22WE 20080714 NM 2008 7 14 DL76L080785 1 20080528 A 4920 APU BOEING 767 767332 1382001 NM SHUTDOWN A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 186DN 16466 27962 APU SHUTDOWN ON PUSHBACK. BITE CKD ECU, SHOWS REVERSE FLOW. CLEARED AND RESTARTED APU. OPS CKS GOOD. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 DLM90080788 1 20080520 A 5310 591746311 DOOR FRAME DOUG MD90 MD9030 3023690 NM AIRSTAIR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 AFTER REMOVAL OF WEATHER SEAL, FOUND VENTRAL STAIRWAY DOOR JAMB CORRODED OUT OF LIMITS, LOWER SECTION AT FLOOR LEVEL. REPAIRED STAIRWAY DOOR JAMB, IAW DELTA ER/A 468148-14 REV ORIG. 2 L 7 2 4F RT A6WE 20080714 NM 2008 7 14 SWAA083483 1 20080623 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, LBL 2.5 TO LBL 3.5. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083466 1 20080623 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 449WN 32469 EEPLS LENS MISSING AT ROW 3 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083468 1 20080623 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 6 DEF. SECURED STRIP PER SRM. 2 L 7 2 4F RT A16WE 20080714 2008 7 14 SWAA083440 4 20080620 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083175 1 20080610 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 DL757080804 1 20080530 A 5312 STRUCTURE BOEING 757 757232 1384965 NM BULKHEAD CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 UNKNN DURING HMV FOUND AFT CHORD CORRODED AROUND SEVERAL HOLES AFTER STR STR 27L TO 20L. REPLACED A SECTION OF THE CHORD PER SMR 53-80-08D REF SAA N/R 78986090001. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 08FDEA02404 1 20080624 A 5311 6516348137 FRAME BOEING 727 727227 1384078 NM ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 ORIGINAL DISCREPANCY STILL EXISTS. AFT PIT LT SIDE WALL BODY FRAME IB FLANGE CHAFED, 1148, STR 21L - L CHECKED WEAR A REA FOR MATERIAL LOSS, ORIGINAL THICKNESS "T' .065' MATERIAL LOSS MEASURE .017', REMAINING MATERIAL .048' AND IS OUT OF LIMITS REF SRM 53-10-1 FIG 1. FABRICATED REPAIR MATERIAL REF SRM 51-40-3, INSTALL REPAIR, REF SRM 51-40-3. THIS IS CL ASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 08FDEA02407 1 20080624 A 5311 6516325 FRAME BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 FUSELAGE FORMER FRAME DOUBLE DRILLED ON VERT FLANGE WITH LESS THEN 1/4 D DISTANCE BETWEEN HOLES AT FS 760 BETWEEN STR 3R AND 4R REPAIR DOUBLE DRILLED HOLE ON FRAME STA 760 BETWEEN STR 3R AND 4R REF SRM 53-10-4 FIG 1. THIS IS CLASSIFIED A S A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080714 EU 2008 7 14 USAA920081112 1 20080516 A 5540 D5537131800200 HINGE AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 602AW 565 SAL - MAJOR REPAIR - C1 CHECK - RUDDER HINGE NR 3 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 2279 / RIB 5. REPLACE D RUDDER HINGE NR 3, VERTICAL STABILIZER STATION 2279 / RIB 5 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 20080714 NM 2008 7 14 08FDEA02414 1 20080624 A 5532 65174614 SKIN BOEING 727 727225 1384077 NM ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 DRILL START NEXT TO RIVET, UNDER PANEL 9702, VERTICAL STABILIZER UPPER SKIN, DEPTH OUT OF LIMITS. FOUND WHILE ACCOMPLIS HING N/R N00752, FOUND DAMAGE TO BE OUT OF LIMITS. VERIFIED REPAIR MATERIAL TO 2024-T-3 .080". FABRICATED REPAIR DOUBL ER AND INSTALLED DOUBLER IN REF TO SRM 55-30-3 PG 1-2. TREATED AND PRIMED DOUBLER, IN REF TO SRM 51-10-2 PG 1-7, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080714 WP 2008 7 14 08FDEA02416 1 20080624 A 5521 ALC73912 RIB DOUG MD10 MD1010F 3022112 WP ZONE 300 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 RIGHT STABILIZER INBD ELEVATOR UPPER SURFACE IS GOUGED IN 2 PLACES. REPAIRED 2 EA GOUGES IAW DC/MD-10 SRM 55-10-00; VOL I; FIG 8 AND DC/MD-10 SRM 55-00-01; VOL I; FIG 3; SHEET 2. REPAIRED THE DAMAGED RIB CAP IAW DC/MD-10 SRM 55-00-01; VOL I; FIG 6. WEIGHT AND BALANCE NOT REQUIRED IAW DC/MD-SRM 55-10-00; VOL I; FIG 8; NOTE II. 2 L 7 3 4F RT A22WE 20080714 NM 2008 7 14 08FDEA02419 1 20080624 A 5523 657279972 TAB BOEING 727 727225 1384077 NM ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 RT HORIZONTAL STAB ELEVATOR TRIM TAB IS DISBONDED ON LE UPPER SURFACE 29 INCHES OUT FROM INBD EDGE AT NR 3 HINGE. REMOV ED AND INSTALLED NEW SERVICABLE TAB REF MM 27-30-011-2, OPERATIONAL AND FUNCTIONAL CHECK ACP ON W/C 73C022-00 THIS IS CL ASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 USAA920081120 1 20080504 A 5730 65C2704421 SKIN PANEL BOEING 737 7373G7 1384595 NM LT WING CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 157AW 23779 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON THE LEFT WING LOWER SURFACE INNER SPAR SKIN, WBL 583, STRINGER 6. REPAIRE D THE LEFT WING LOWER SURFACE INNER SPAR SKIN, WBL 583, STRINGER 6 IAW USAIRWAYS EA 130024. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 USAA920081121 1 20080522 A 3397 1721601 CONNECTOR BOEING 737 7373G7 1384595 NM CABIN DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 157AW 23779 MCN - EEL - C21 CHECK - EMERGENCY ESCAPE PATH LIGHT WIRING HARNESS HAS SEVERAL DAMAGED CONNECTORS. REPLACED EMERGENCY E SCAPE PATH LIGHT WIRING HARNESS CONNECTORS IAW BSWPM 20-42-01. 2 L 7 2 4F RT A16WE 2008042300275 20080423 00275 NM 2008 4 23 SWAA081946 1 20080412 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 415WN 29836 EEPLS LENS LOOSE AT ROW 5 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008042300285 20080423 00285 NM 2008 4 23 SWAA081988 1 20080413 A 5311 6546534 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300287 20080423 00287 NM 2008 4 23 SWAA081982 1 20080413 A 5311 6546555 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041800145 20080418 00145 SO 2008 4 18 C2XA08CL048 1 20080411 A 5730 SKIN EMB 145 EMB145EP 3260221 SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12934 145019 WING SKIN CRACK ON RIGHT WING AT I/B SPOILER CENTER HINGE CUTOUT. REPAIRED CRACK IAW IC 2008-145/02561. AIRCRAFT RELEA SED FOR SERVICE. 2 L 7 2 4F RT T00011AT 2008041800154 20080418 00154 SO 2008 4 18 RAIA00804010 1 20080409 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 849HK 145002 PRE FLT 7923 -STL- EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR TO THE AFFECTED LIGHT. NO ADDITION AL DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 2008041800193 20080418 00193 NM 2008 4 18 USAA920080844 1 20080401 A 5345 SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT- MAJOR REPAIR - C4 CHECK - CORROSION ON GALLEY SUPPORT AT BS 1700-1720, WL 208.1, LBL 6. REPLACED SUPPORT IAW SRM 5 1-10-00, 51-40-02 AND DRAWING 146N5300. 2 L 7 2 4F RT A2NM 2008041800207 20080418 00207 NM 2008 4 18 ANCF200800008 1 20080413 A 2750 WARNING LIGHT BOEING 757 7572T7 1384914 NM SLATS ILLUMINATED W ANCF A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 23 513NA 23895 FLAP LEVER UP, FLAP POINTERS UP, EICAS MSG LE SLAT ASYM, LEADING EDGE LIGHT ON DURING CLIMB, RUDDER TRIM 3-4 UNITS TO TH E RIGHT TO CENTER COLUMN. FIM PROCEDURE 27-81-00 FIG 105 WAS ACCOMPLISHED. IN ACCORDANCE AMM 27-51-01/201 FLAP SLAT EL ECTRONIC UNIT NR 1 AND NR 3 WERE REPLACED, OPERATIONAL TEST SATISFACTORY. AS PER FIM27-81-00 FIG.105 SHEET 1 BLOCK 1 AND 40 WAS PERFORMED AND FIM 27-51-0. IAW AMM 27-81-41 AT SLAT LOSS SW LEVER ARM WAS REPLACED, IAW AMM 27-81-41. TEST WAS P ERFORMED AND THE SYSTEM IS OK. 2 L 7 2 4F RT A2NM 2008041800211 20080418 00211 WP 2008 4 18 08FDEA01424 1 20080416 A 5330 ADA3139501 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION ON LOWER FUSELAGE EXTERNAL FOUND DENT 0.047" BY 2" BY 1.5 INCH LONG ON EXTERNAL SKIN STA 10 49 RT SIDE LONGERON 46 TO LONGERON 47. REPAIRED FOR SRM 53-20-00 FIG 6 VOL I. 2 L 7 3 4F A22WE 2008041800213 20080418 00213 EU 2008 4 18 08FDEA01426 1 20080416 A 5330 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 445FE 297 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT LOWER CENTER FUSELAGE SKIN MANHOLE FITTING CUTOUT AT FRAMES 23 TO 24 AND B ETWEEN STRINGERS 48 RT TO 52 RT MEASURES 24.4 IN BY 15 IN WITH 4 INTERNAL POCKET REPAIRS BETWEEN STRINGERS 54 LT TO 49 R T REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT REPAIR IAW FED EX EA 6-5310-118095 THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080715 NM 2008 7 15 ASAA0843014 1 20080517 A 5330 6545800602 SKIN BOEING 737 737490 1384715 NM BS 322-334 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 DENT FOUND ON FUSELAGE BELOW R1 DOOR. REMOVED DAMAGED AREA OF SKIN FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER IAW ASA EA5330 02347. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 NWAA082396623 1 20080520 A 5311 FRAME BOEING 747 747251B 1384892 NM BS 800 S16R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 623US 21705 DURING "M" CHECK, FOUND CRACK IN FRAME INNER CHORD STRAP HOLE AT BS 800 S16R. REPAIRED PER EA 66-212931. 2 L 7 4 4F RT A20WE 20080715 2008 7 15 X7P2008F00000 4 20080425 A 3417 271010101 AIR DATA MODULE CESSNA 500 560CESSNA 2076750 CE COCKPIT MALFUNCTIONED E X7PA O OTHER O OTHER NR NOT REPORTED 1 WP 25 41VP 5600626 AIRCRAFT HAS EXPERIENCED "OFF" FLAGGING OF AIRSPEED AND ALTITUDE ON STANDBY FLIGHT DISPLAY THREE TIMES IN THE LAST 7 MON THS. STANDBY AIR DATA UNIT HAS BEEN REPLACED WITH AN OVERHAULED UNIT EACH TIME, WHICH HAS RECTIFIED THE ISSUE. (K) 2 L 7 2 4F RT A22CE 20080715 2008 7 15 USAA920081154 4 20080524 A 2565 101630305 SLIDE BOEING 767 767201 1385125 NM LT OVERWING FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 250AY 23902 BFM - C3 CHECK - NR 6040422, LEFT OVERWING SLIDE PARTALLY DEPLOYED ELECTRICALLY BATTERY POWER. REMOVED AND REPLACED THE LEFT OVERWING SLIDE IAW B767 AMM 25-05-11. 2 L 7 2 4F RT A1NM 20080715 EU 2008 7 15 USAA920081155 1 20080513 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 678AW 2482 SAL - EMERGENCY EQUIPMENT - BC2 CHECK - NR 6103162, AFT FLIGHT ATTENDANT SEAT LEFT OUTBOARD FLASHLIGHT CHARGE INDICATOR NOT BLINKING. REPLACED AFT FLIGHT ATTENDANT SEAT LEFT OUTBOARD FLASHLIGHT BATTERY. 2 L 7 2 4F RT A28NM 20080715 EU 2008 7 15 USAA920081157 1 20080513 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 678AW 2482 SAL - EMERGENCY EQUIPMENT - BC2 CHECK - NR 6101927, FORWARD FLIGHT ATTENDANT SEAT LEFT FLASHLIGHT CHARGE INDICATOR NOT B LINKING. REPLACED FORWARD FLIGHT ATTENDANT SEAT LEFT FLASHLIGHT BATTERY. 2 L 7 2 4F RT A28NM 20080715 NM 2008 7 15 ASAA0842985 1 20080520 A 5230 65C361831 SKIN BOEING 737 737490 1384715 NM CARGO DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 FWD CARGO DOOR EXTERNAL SKIN HAS CREASE. REMOVED DAMAGED AREA OF SKIN FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 52 00 01 REPAIR 2. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 USAA920081117 1 20080508 A 5330 65C30803 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 157AW 23779 MCN - MAJOR REPAIR - C21 CHECK - CRACKED FUSELAGE SKIN, BS 727E, S21R. REPAIRED FUSELAGE SKIN, BS 727E, S21R IAW B737 S RM 53-00-01- 2R 31, FIGURE 201. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 08FDEA02418 1 20080624 A 5340 6545313Y STRINGER CLIP BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 STRINGER CLIP CRACKED, BS 950D, STRINGER 6L. REPLACED STRINGER CLIP AT BS 950D STRINGER 6L REF SRM 51-30-2 PG 1-11. T HIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 USAA920081118 1 20080505 A 5315 6546811 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 157AW 23779 MCN - MAJOR REPAIR - C21 CHECK - CORROSION ON FLOORBEAM UPPER CHORD, BS 986, RBL 15 - RBL 45. REPAIRED FLOORBEAM UPPER CHORD, BS 986, RBL 15 - RBL 45 IAW USAIRWAYS EA 130026 AND TYPICAL REPAIR 53-15-01B. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 08FDEA02374 1 20080621 A 5314 KEELBEAM BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 LEFT MAIN LANDING GEAR WHEEL WELL KEEL BEAM CHORD CRACKED AT STA 872. 2 L 7 3 4F A3WE 20080714 WP 2008 7 14 08FDEA02065 1 20080530 A 5720 ANB720315 STIFFENER DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 LEFT MLG WHEEL WELL; LEFT WING INBD WEB 2ND AFT ANGLE AFT OF THE MLG CUTOUT IS CRACKED. REMOVED STIFFENER IAW DC/MD-10 SRM 51-35-01 AND 51-33-01; VOL II. MATERIAL ID FOR THE STIFFENER 7075-0, 0.040. FABRICATED STIFFENER IAW DAC DWG ANB 7208, REV "AB". ALODINED; PRIMED AND PAINTED IAW DC/MD-10 SRM 51-21-01; PGS 21-24 AND 51-21-02; VOL II. INSTALLED THE STIFFENER IAW DC/MD-10 SRM 51-35-01 AND 51-33-01; VOL II. 2 L 7 3 4F RT A22WE 20080714 NM 2008 7 14 08FDEA02079 1 20080602 A 5330 SKIN BOEING 757 75723A 1384967 NM ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 919FD 24636 PATCH REPAIR FOUND ON PRESSURE PANEL AT BS1720, RBL16 TO EVALUATE UNRECORDED REPAIR. EXISTING REPAIR FOUND ACCOMPLISHED IAW B757 -200 SRM 53-60-51 FIG 201 REPAIR 2, BASED ON EXTERNAL VISUAL EVALUATION ON THE SHAPE, LOCATION, SIZE, MATERIAL THICKNESS, TYPE AND GENERAL WORKMANSHIP OF THE REPAIR. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 08FDEA02431 1 20080624 A 5315 FLOORBEAM BOEING 757 757236 1384971 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 STA 377.7, BL0 TO LBL 45 HAS CORROSION AROUND NUT PLATE HOLES. REMOVED DAMAGED AREA, LBL 13 TO LBL 70, BS 377.7 IAW SRM 53-00-51, FIG 201, REPAIR NR 3. FABRICATED T-CHORD AND SHIM IAW SRM 53-00-51, REPAIR NR 3. FABRICATED STRAP NR 4 AND NR 5 ON TRAVELER NR T8/744935. FABRICATED ANGLE NR 2 AND NR 3 ON TRAVELER NR T8/744935. INSTALLED ALL REPAIR PARTS IAW SRM 53-00-51, FIG 201, REPAIR NR 3. THIS IS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING. 2 L 7 2 4F RT A2NM 20080714 EU 2008 7 14 08FDEA02433 1 20080624 A 5347 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 FR 15A-FR 15C Y50 MAIN DECK SEAT TRACK CORRODED. REMOVED THE RELATIVE RASTENERS FOR ACCESS PER SRM 51-40-21. REMOVED T HE CORROSION PER SRM 51-74-10/201. APPLIED AN ALODINE COATING PER SRM 51-21-10/001. NDT MEASURED THE REMAINING THICKNE SS PER NTM 51-10-04. THE ORIGINAL THICKNESS IS 0.078 INCH, IT IS NOT WITHIN 0.012 IN ALLOWABLE CLEANUP LIMIT PER SRM 53 -10-16/101. MAKE THE SEAT TRACK PER DWG: A53611640200. DRILLED FASTENER HOLES IN THE NEW PART PER SRM 51-40-21. APPLIED ALODINE PER SRM 51-21-10. APPLIED PAINT PER AMM 51-75-10. REPLACED AND INSTALLED THE SEAT TRACK PER SRM 51-40-21. RES TORED FINISH PER AMM 51-75-10. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 08FDEA02439 1 20080625 A 5320 A6A709417 STANCHION DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 FORWARD CARGO COMPARTMENT, FOUND COMPARTMENT AFT BULKHEAD LINER SUPPORTING STANCHION CORRODED AT STATION 6-73.5, X = -9" . FORWARD CARGO COMPARTMENT AFT BULKHEAD LINER SUPPORTING STANCHION AT STATION 6-73.5, X = -9" CORROSION REMOVED AS P ER SRM 51-21-01, VOL.II. MATERIAL REMOVED 0.092", ORIGINAL THICKNESS 0.100", REMAINED THICKNESS 0.008", AND FOUND EXCEED ED LIMIT AS PER SRM 53-00-01, FIG.2, VOL.I. STANCHION REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. NEW STANCHION R EWORKED AS PER DRAWING A6A7094. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080714 NM 2008 7 14 ASAA0853089 1 20080625 A 2131 8243921003 CONTROLLER BOEING 737 737890 1384527 NM CABIN PRESSURE FAULTED A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 558AS 7691 35177 DURING PREFLIGHT "AUTO FAIL" AND "ALTN" ILLUMINATED ON PRESSURIZATION CONTROLLER. CYCLED AUTO PRESSURE CONTROL SW IN MA N AND DROVE OF VLV DOOR CLEARED FAIL LT, PERFORMED AUTO PRESS PNL CONTROLLER BITE NR 1 PASS NR 2 LOGGED CABIN PRESS CONT FAULT CLEARED ALL AND PERFORMED BITE TO CONFIRM INTERMITTENT FAULT PER AMM 21 31 00. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 DLM88080850 1 20080611 A 2150 ACM DOUG MD88 MD88 3023688 NM PWA 4060 PW4060 52119 NE NR 1 LEAKING A DALA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SO 27 938DL 49811 724147 FLOW LIGHT ON CLIMB-OUT PASSING FL280. BOTH AC PACKS ON. NO AUTO PRESS INOP LIGHTS ON. C/W QRH PROCEDURES NO HELP. C LOSED OUTFLOW VALVE, NO HELP. BOTH PNEU X FEED VALVES CLOSED. FOUND 1 LEAK AT RT ACM 1 LEAK FROM HEAT EXCHANGE ON LEF T SIDE ON 1 OPEN DUCT ON HOT AIR SUPPLY LINE THE SPIDER DUCT FIXED ALL 3 LEAKS LEAK CHECK OK. 2 L 7 2 4F 4 F RT A6WE E24NE 20080714 EU 2008 7 14 08FDEA02455 1 20080625 A 5315 A53974222202 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 719FD 388 BULK CARGO BAY UNDER FLOOR AREA STA FR 66, AND BETWEEN LBL 26 TO LBL43, FLOOR SUPPORT AND "T" CHANNEL HAS CORROSION. RE MOVED AND REPLACED "T" CHANNEL/FLOOR SUPPORT ASSEMBLY IAW SRM 51-40-44 AND 51-40-21. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 ZZDA2008111 1 20080528 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 921AT 55082 DAMAGE TO RIGHT FUSELAGE JUST AFT OF RIGHT AOA VANE. CUT OUT DAMAGED SECTION AT RIGHT HAND FUSELAGE, FABRICATED DOUBLER REPAIR AND REPAIRED SKIN PER AIRTRAN EA17-53-01150IR. 2 L 7 2 4F TR A6WE 20080714 NM 2008 7 14 UPS08652358 1 20080514 A 5720 1142300272 WEB BOEING 767 76734AF 1385212 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 302UP 27240 INSPECTION TYPE:N/A RIGHT WING LES664 FWD D-NOSE WEB FOUND CRACKED AT LWR AREA. CRACK LENGTH 2 TO 2.5 INCHES APPROX. R IGHT WING FWD D-NOSE SUPPORT WEB REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02, JUST BETWEEN OSS648 AND 694. REFER NRC50622 FOR WORKING DETAIL. 2 L 7 2 4F RT A1NM 20080714 EU 2008 7 14 08FDEA02312 1 20080618 A 5330 A53978155200 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER AND TRIPLER LOCATED FWD OF BULK CARGO DOOR ON RIGHT SIDE FUSELAGE SKIN AT FRAME 67 AND BETWEEN STRINGERS 37 TO 39 RT, THE REPAIR DOUBLER MEASURES 8.7 INCH BY 6.2 INCH AND THE TRIPLER MEASURES 6.7 INCH BY 4 .5 INCH. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED APPROVED REPAIR IAW FEDEX EA6-5310-121 293 "FUSELAGE - FR67 SKIN. REPLACE PREVIOUS REPAIR AT FWD EDGE OF BULK CARGO DOOR". THIS IS AN AIRBUS REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080715 NM 2008 7 15 08FDEA02323 1 20080619 A 5314 144N818048 KEELBEAM BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 LWR FUSELAGE KEEL BEAM AREA AT BS 1040 RT SIDE, SUPPORT FRAME HAS SURFACE CORROSION. CORROSION FOUND EXCEED ALLOWABLE LIMITS IN B757 SRM 51-10-02. REMOVED AND REPLACED TEE SUPPORT IAW B757-200 SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 08FDEA02334 1 20080619 A 5320 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CRACK INDICATIONS AT HOLES NR A , NR B , NR C AND NR D (THIRD LAYER). MAIN CARGO DOOR LOWER JAMB, CRACKED NR 6 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. NEW FITTING FABRICATED AS PER EA 1-5300-122494, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 USAA920081227 1 20080602 A 5320 143N80216 INTERCOSTAL BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 905AW 23567 MCN - C112 - MAJOR REPAIR - NR 6109932 - INTERCOSTAL WEB CRACKED B/S 550 RBL 54 W/L 208.1 (HFEC VERIFIED). REPLACED INTE RCOSTAL WEB B/S 550 RBL 54 W/L 208.1 IAW SRM 51-40-02-0G. (K) 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 08FDEA02294 1 20080617 A 5720 6521656 STIFFENER BOEING 727 727227 1384078 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 RT MLG STRUT WELL LWR FIXED PNL SEAL RETAINER ASSY IS CRACKED/CORRODED ALONG WING SPAR CHORD WS 190-220 REMOVED 4 HYD ST ANDOFFS AND 2 SEAL DEPRESSORS FROM STA 180-220. REMOVED DRAIN TUBE, TE FAIRING PANEL, TE FIXED PANEL RT. FABRICATED 2 NEW SEAL RETAINERS OUT OF LIMITS. MATERIAL 2024-T3 INSTALLED NEW SEAL AND SEAL RETAINERS. INSTALLED OLD 1 EA STIFFENER S. TREATED AND PRIMED REF DWG 65-21656 AND SRM 51-10-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080715 NM 2008 7 15 USAA920081240 1 20080610 A 5312 6516300 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN - C-21 - MAJOR REPAIR - NR 6110583 - 178 BULKHEAD WEB CRACKED AT WL 218, LBL 10. REPAIRED 178 BULKHEAD WEB AT WL 21 8, LBL 10 IAW SRM 53-10-08-2R9. (K) 2 L 7 2 4F RT A16WE 20080715 EU 2008 7 15 08FDEA02155 1 20080604 A 5753 SKIN AIRBUS 310 A310203 3930313 EU ZONE 500 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LT WING OUTBD FLAP UPPER SKIN UNDER RUB STRIP BETWEEN RIB NR 3 AND RIB NR 4, MEASURING 4.1 IN BY 11.9 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT OUTER SKI N REPAIR ON RT WING OUTBD FLAP UPPER SKIN BETWEEN RIB NR 3 AND RIB NR 4 IAW A310-200 SRM 57-53-10, FIG 210. THIS IS AN AIRBUS REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080715 EU 2008 7 15 08FDEA02168 1 20080605 A 2612 CGAB200100 FIRE DETECTOR AIRBUS 300 A300F4605R 3930327 EU CARGO BAY MALFUNCTIONED A FDEA F B ACTIVATE FIRE EXT. EMER. DESCENT N FALSE WARNING DE DESCENT 1 CE 21 685FE 504 504 803 ABOUT 80 MILES OUT OF KEWR HAD A LOWER CARGO FIRE INDICATION AND FOLLOWED PROCEDURES AND FIRE BOTH FWD CARGO BOTTLES, FO LLOWED ON GROUND EVACUATION CHECKLIST, L1 DOOR SLIDE DEPLOYED NORMAL STOP AND ROLLOUT. REMOVED AND REPLACED BOTH FWD CA RGO COMPT SMOKE DET PER AMM 26-16-11-4. OPS TEST OK PER AMM 26-16-00-5-01. NO DISCREPANCIES NOTED DURING REPLACEMENT O F DETECTORS. REMOVED AND REPLACED NR 2 FIRE EXTINGUISHER BOTTLES IAW MM 26-23-11-4. 2 L 7 2 4F RT A35EU 20080715 EU 2008 7 15 08FDEA02173 1 20080606 A 5313 A53974202482 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION AT STRINGER P55, C 64-65. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 20080715 EU 2008 7 15 08FDEA02174 1 20080606 A 5320 A53810767200 STIFFENER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CHAFING MARK AT VERTICAL MEMBER Y-1456, Z-1870 REPAIR PERFORMED BY REWORK TO SMOOTH CONTOUR, NDT FOR CRACK FREE CO NDITION IAW RAS 70510754/009/2008 ISS A, APPROVED BY EA 6-5315-120112. 2 L 7 2 4F RT A35EU 20080715 CE 2008 7 15 MT9A00000020 1 20080512 A 3240 06111800 HOUSING CESSNA 208 208B 2073701 CE RT MLG BRAKE WORN E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9505B 208B0085 RT BRAKE CYLINDER HOUSING WORN AT THE ANCHOR BOLT PASS THROUGH HOLE ALLOWING THE ANCHOR BOLT TO BE PRESSED OUT BY HAND. THIS IS NORMALLY A CLOSE TOLERANCE FIT. THIS CONDITION IN THE PAST HAS CAUSED THE ANCHOR BOLT TO SHEER OFF CAUSING CATA STROPHIC DAMAGE TO THE CALIPER ASSEMBLY, TORQUE PLATE AND/OR TIRE ON THREE OF OUR AC. (K) 1 H 7 1 3T A37CE 20080715 NE 2008 7 15 E0X2008F00002 2 20080518 A 7200 ENGINE BRAERO 1000 BAE1251000A 1500104 EU PWA 305 PW305 NE NR 1 FAILED E E0XA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 EA 39 539LR 259039 NR 1 ENGINE QUIT AS AC WAS CLIMBING THROUGH FL370 WITH NO WARNING. FIRST INDICATION WAS LOSS OF OIL PRESSURE AS ENGINE S POOLED DOWN. DIVERTED AND DECLARED AN EMERGENCY. THEIR WAS NOT AN ATTEMPT MADE TO AIRSTART THE FAILED ENGINE. SINGLE EN GINE LANDING WAS UNEVENTFUL, NO PASSENGERS WERE ON BOARD AND CREW WAS NOT INJURED. INSPECTION AND MAINTENANCE OF AIRCRAF T, FINDING TO DATE ARE AS FOLLOWS; NO OVERTEMP, ASSESSMENT THAT THE ENGINE FLAMED OUT EITHER DUE TO LACK OF FUEL CONTAMI NATION/ ICING. MFG ENGINEERING IS DOING AN EVALUATION OF THIS EVENT TO DETERMINE ANY FURTHER ACTION THAT MAY BE RECOMME NDED FOR THIS ENGINE. (K) 2 L 7 2 4F 4 F RT A3EU E35NE 20080715 NM 2008 7 15 KCSA081266 1 20080530 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 740 S27L DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 STA-740 STR-27L SKIN DENTED APROX .75 INCH. 2 L 7 4 4F RT A20WE 20080715 NM 2008 7 15 AALA200801258 1 20080508 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 42G INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 42G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080715 NM 2008 7 15 AALA200801259 1 20080508 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 44C INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 44C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080715 NM 2008 7 15 AALA200801250 1 20080508 A 3397 PIN BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 386AA 27060 MIA - EMERGENCY LIGHT AT SEAT 4AB DAMAGED. REPLACED PIN FOR EMERGENCY LIGHT AT SEAT 4AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080715 NE 2008 7 15 705805272008 2 20080527 A 7200 430110209 ACTUATOR BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE NR 1 ENGINE FAILED E QMLA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NM 03 158BK 621 7058 LE45273 AFTER DROPPING A PATIENT OFF AT THE HOSPITAL, ON THE RETURN LEG TO THE AIRCRAFT HOME BASE, IN CRUISE FLT, THE NR 1 ENGIN E FAILED TO FOLLOW COLLECTIVE MOVEMENTS AND STAYED FIXED AT 60 PERCENT TORQUE. THE NR 2 ENGINE RESPONDED APPROPRIATELY, CAUSING LARGE TORQUE SPLITS. ATTEMPTED TO TRIM THE NR 1 ENGINE, BUT THE NR 1 ENGINE FAILED TO RESPOND TO ELECTRONIC TR IM INPUTS. WITH THE NR 1 ENGINE STUCK AT A FIXED CRUISE POWER SETTING, DECLARED AN EMERGENCY WITH TAMPA INTERNATIONAL ( KTPA) TOWER AND PERFORMED A SINGLE-ENGINE (OEI) PROFILED APPROACH AND LANDING TO THE AIRPORT'S PARALLEL TAXIWAY WITH THE AIRPORT'S EMERGENCY CRASH CREW STANDING BY. AIRCRAFT WAS LANDED WITHOUT INCIDENT AND MOVED THE ADJACENT FBO RAMP, CLEA 1 G 7 2 3U 3 U H13EU E5NE 20080715 NM 2008 7 15 ASAA0892984 1 20080517 A 5330 146A320116 SKIN BOEING 737 737990 NM BS 827-867 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 307AS 30015 AIRCRAFT SKIN AT BS 827 TO BS 867 BETWEEN STR14L TO 17L HAS MULTIPLE BLENDS (127 PREVIOUS BLENDS). AREA REPAIRED IAW ER O8387 AND ASA EA5330 02341. 2 L 7 4 4F RT A16WE 20080715 NM 2008 7 15 ASAA0842987 1 20080518 A 5755 SKIN BOEING 737 737490 1384715 NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 NR 7 SPOILER UPPER SURFACE DENTED OTBD OF INBD HINGE. PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 08FDEA02071 1 20080531 A 5320 655851312 PANEL BOEING 727 727233 138408A NM ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 RT A/C BAY PANEL 3456 R DELAMINATED REMOVED AND REPLACED PANEL 3456R WITH SERVICEABLE PANEL REF SRM 51-30-2 PG 13. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080715 NM 2008 7 15 UPS08B52392 1 20080417 A 5340 TENSION TIE BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 BS 1180 TENSION TIE LT FWD SIDE CRACKED, BS 1180 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201. 2 L 7 4 4F RT A20WE 20080715 WP 2008 7 15 ASMF200805005 1 20080528 A 2420 696233B CSD DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE LEFT DAMAGED W ASMF O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 23 205AM 40053 13226 49405 718133 DURING PUSH BACK, CAPTAIN REPORTED THAT AFTER STARTED THE LEFT ENGINE, THE CSD LIGHT TURNED ON AND TEMPERATURE REACHED 1 50 DEGREES CELSIUS, SO ABNORMAL PROCEDURE WAS ACCOMPLISHED. MAINTENANCE PERSONNEL DETECTED THE LEFT CSD OIL LEVEL IN RE D RANGE, SO THE EXCESSIVE OIL WAS DRAINED UNTIL YELLOW RANGE. DURING TRANSIT CHECK AT MEX, THE LEFT CSD AND OIL EXCHANG ER WERE REPLACED IAW MM 24-13-01 AND 24-14-01, TESTED CORRECT. 2 L 7 2 4F 4 F RT A6WE E9NE 20080715 SO 2008 7 15 CHQA200800099 1 20080526 A 2120 UNKNOWN EMB 135 EMB135LR 3260305 SO ALLSN AE3007 AE3007A 03030 GL CABIN ODOR A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 841RP 145737 CAE311599 FLIGHT 6426, CMH TO JFK - DURING CLIMB AT 500FT AGL, THE FLIGHT ATTENDANT CONTACTED THE FLIGHT DECK WITH A CABIN EMERGEN CY. THE FLIGHT ATTENDANT REPORTED SMOKE ENTERING THE CABIN. THE FLIGHT CREW REPORTED THAT THERE WAS NO SMOKE AT ANY TI ME IN THE COCKPIT. THE FLIGHT RETURNED TO LAND AT CMH WITHOUT INCIDENT. MAINTENANCE PERFORMED A VISUAL INSPECTION OF B OTH ENGINES WITH NO PRESENCE OF OIL LEAKAGE, RAN BOTH ENGINES WITH NO OIL OR SMOKE SMELL IN CABIN, AND INSPECTED BOTH PA CKS AND DUCTING WITH NO DEFECTS NOTED IN ACCORDANCE WITH FIM 21-20-00-810-803-A AND AMM 72-00-00. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080715 NM 2008 7 15 AALA200801274 1 20080511 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 965AN 29544 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR HAS BROKEN LENS. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LEFT NUMB ER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 AALA200801263 1 20080509 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM GALLEY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 NRT - EMERGENCY LIGHT AT GALLEY NEAR RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT GALLEY NEAR RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080715 NM 2008 7 15 AALA200801270 1 20080510 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 355AA 24036 DFW - EMERGENCY LIGHTS AT SEAT ROWS 20AB TO 24AB INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 2 0AB TO 24AB. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080715 2008 7 15 SWAA082895 4 20080529 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082896 1 20080529 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082900 1 20080529 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 456WN 32463 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082908 1 20080529 A 5743 69378777 FITTING BOEING 737 7373Q8 1384670 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED A1 CHECK, FOUND LT WALKING BEAM ACTUATOR FITTING CRACKED AT AFT SPAR. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082909 1 20080529 A 3350 20131A BATTERY PACK BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED A1 CHECK, AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082913 1 20080529 A 2560 6557463 FITTING BOEING 737 7373Q8 1384670 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 20080715 2008 7 15 SWAA082910 4 20080529 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 781WN 30601 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080714 WP 2008 7 14 08FDEA02087 1 20080602 A 5320 AEA0161289A CHANNEL DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 CENTER LANDING GEAR WELL/SPACE INTERIOR; HYDRAULIC MODULE UPPER CHANNEL HAS A CRACK STARTING AT THE MOUNT BOLT HOLE JUST FWD OF THE HYDRAULIC PUMPS. REMOVED SUPPORT CHANNEL IAW DC/MD-10 SRM 51-31-10; VOL II. MATERIAL ID 7275-0, 0.040 IAW DAC DWG AEA 0161, REV CR. FABRICATED THE SUPPORT CHANNEL IAW DAC DWG AEA 0161, REV CR. HEAT TREATED 7075-0 TO T6 IAW T PS 1003, REV A. HT 0603081 USED. ALODINED AND PRIMED THE SUPPORT CHANNEL IAW DC/MD-10 SRM 51-21-01; VOL II. PART MAR KED THE SUPPORT CHANNEL FX AEA-016-289A IAW FEDEX GMM 7-0-1000. INSTALLED THE SUPPORT CHANNEL IAW DC/MD-10 SRM 51-35-01 ; VOL II 2 L 7 3 4F RT A22WE 20080714 EU 2008 7 14 08FDEA02446 1 20080625 A 5320 STRAP AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 FWD CARGO COMP BELOW FLOOR LEVEL BETWEEN FR 38.2 - FR 39, STGR 55R - STGR 56R SKIN STRAP WITH LIGHT CORROSION. REMOVED THE RELATIVE FASTENERS FOR ACCESS PER SRM 51-40-21. REMOVED THE CORROSION PER SRM 51-74-10/201. APPLIED AN ALODINE COA TING PER SRM 51-21-10/001. THE REMAINING THICKNESS IS 0.049 INCH (EXCEEDED LIMIT) PER NTM 51-10-04. REPAIR PER EA6-531 0-117360. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 08FDEA02449 1 20080625 A 5280 6517563160 RIB BOEING 727 727225 1384077 NM NLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 NLG RIGHT FWD DOOR, CRACK IN AFT SIDE FRAME AT O/B STOP FITTING LOWER 2 FASTENERS FOR INNER STRUCTURE. REMOVED AND RE PLACED DOOR FOR ACCESS, REPAIRED DOOR REF MM 32-22-001-4 AND SRM 51-40-3 FIG 1. ADJUSTED AND OPS CHECK OF DOOR ACCOMPLI SHED ON W/C 71C130-00. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 08FDEA02453 1 20080625 A 5340 6545313Y2 STRINGER CLIP BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 STRINGER CLIP CRACKED BS 950C, STRINGER 5L REPLACED STRINGER CLIP REF SRM 51-30-2 PG 1-10. THIS IS CLASSIFIED AS A MAJO R REPAIR. 2 L 7 3 4F A3WE 20080714 EU 2008 7 14 08FDEA02075 1 20080601 A 2133 88005B0306 REGULATOR AIRBUS 310 A310222 3930315 EU CABIN PRESSURE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 21 454FE 6027 6027 278 DURING CLIMB-OUT WITH NR 1 REG DEFERRED, LOST NR 2 REG. USED MANUAL PRESSURIZATION FOR THE REST OF FLIGHT. ACN RELEASE D FOR SERVICE PER MEL/CDL: 21-31-04-01-A. DEACTIVATED IN CLOSED POSITION. ENSURE CAB DIF PRESS IS ZERO PRIOR TO OPENI NG ANY DOOR." SWAPPED FWD TO AFT CABIN PRESSURE OUTFLOW VALVE AS PER WRI 21-30/7595. REMOVED AND REPLACED AFT OUTFLOW VALVE PER AMM 21-31-12-4 02. OPS TEST GOOD PER AMM 21-31-00-5 02. MEL CLEARED AND PLACARD REMOVED. A/C OK TO CONTINU E. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 08FDEA02078 1 20080602 A 5330 2024T3 SKIN BOEING 757 75723A 1384967 NM ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 919FD 24636 PATCH REPAIR FOUND ON PRESSURE PANEL AT BS1720, RBL4, TO EVALUATE UNRECORDED REPAIR. EXISTING REPAIR FOUND ACCOMPLISHED IAW B757-200 SRM 53-60-51 FIG 201 REPAIR 2, BASED ON EXTERNAL VISUAL EVALUATION ON THE SHAPE, LOCATION, SIZE, MATERIAL THICKNESS, TYPE AND GENERAL WORKMANSHIP OF THE REPAIR. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 08FDEA02432 1 20080624 A 5315 FLOORBEAM BOEING 757 757236 1384971 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 MAIN CABIN FLOORBEAM STA 1640 RBL 47-51 HAS CORROSION BLENDED AREA IAW SRM 51-10-02, ORIG MAT. .125 AFTER 0.90 FOUND OUT LIMITS, IAW SRM 53-00-51 PAGE 103, CUT OUT DAMAGED AREA STA 1640 BET RBL36.5 TO RBL 68.5, IAW SRM 53-00-51 PAGE 201. R ECEIVED REPAIR PARTS NR 1 TEE CHORD, NR 2 ANGLE FAB`D. ON TRAV NR T8/746064 PART NR 3 REPAIR ANGLE FAB`D. ON TRAV NR T 8/746065, AND STRAP NR 4 AND 5 FAB`D IAW SRM 53-00-51 PAGE 203 FIG 201. LOCATED AND DRILLED FASTENERS HOLES REPAIR PART S DEBURRED, TRIMED AND TREATED AND PRIMED IAW SRM 51-20-01 AND SRM 51-40-05. INSTALLED REPAIR PARTS IAW SRM 53-00-51 IA W SRM 51-40-02. CATEGORY A REPAIR NO FOLLOW UP TRACKING REQUIRED. 2 L 7 2 4F RT A2NM 20080714 EU 2008 7 14 08FDEA02434 1 20080624 A 5330 A53778669206 SKIN AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 BETWEEN C23 AND C24, S-50R FUSELAGE SKIN INTERNAL SURFACE CORRODED AROUND THE RIVET BUCKING HEAD. REMOVED CORROSION COM PLETELY PER SRM51-74-10. REPAIRED PER SRM 53-13-12 REPAIR SOLUTION NR 6, FIGURE 202. 2 L 7 2 4F RT A35EU 20080714 EU 2008 7 14 08FDEA02435 1 20080624 A 5320 A53610995205 STIFFENER AIRBUS 310 A310222 3930315 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 HFEC FOUND ONE CRACK ABOUT 17MM AT ZONE B OF FRAME 12A STIFFENER FITTING LT. ACCOMPLISH EO6-5340-7-5002 PART 2 AND PART 3. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 08FDEA02436 1 20080625 A 5330 AJC70602 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 SKIN UNDER RIGHT BODY FAIRING NR 347DF, 01 EACH SURFACE CORROSION FOUND NEAR FASTENER HOLE AT STATION 2155. CORROSION REMOVED AS PER SRM 51-21-01 VOL.II. EXCEEDED LIMITS AS PER SRM 53-00-01, FIG. 2, VOL.I. REPAIR CARRIED OUT AS PER SRM 53-20-00, FIG.13, VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080714 EU 2008 7 14 08FDEA02437 1 20080625 A 5347 A53611640200 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 FR15C-FR17-Y953 MAIN DECK SEAT TRACK CORRODED. REMOVED THE RELATIVE FASTENERS FOR ACCESS PER SRM 51-40-21. REMOVED THE CORROSION PER SRM 51-74-10/201. APPLIED ALODINE COATING PER SRM 51-21-10/001. NDT MEASURED THE REMAINING THICKNESS PER NTM 51-10-04. THE ORIGINAL THICKNESS OF THE REWORKED FLANGE IS 0.079 INCH, OUT OF THE ALLOWABLE LIMITS PER SRM 53-12-16 & 53-10-00. REMOVED THE DAMAGED SEAT TRACK PER SRM 51-40-21. FABRICATED A NEW SEAT TRACK PER DWG: A53611640. DRILLED FASTENER HOLES IN THE NEW PART PER SRM 51-40. APPLIED ALODINE PER SRM 51-21-10. INSTALLED THE NEW PARTS PER SRM 51-40 -21. RESTORED FINISH PER AMM 51-75-10. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 08FDEA02084 1 20080602 A 5330 AGA3102501 SKIN DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 624FE 48443 UPON AFT FUSELAGE RT LOWER WASTE VACUUM EXHAUST PLUG REMOVED AT STA 1959 BETWEEN LONGERON 39R TO 40R, FOUND EXISTING DOU BLER CORRODED. AFT FUSELAGE RT LOWER, AT STA 1959 BETWEEN LONGERON 39R TO 40R REPAIR CARRIED OUT AS PER SRM 53-20-00 VOL 1 FIG 2. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080714 EU 2008 7 14 08FDEA02348 1 20080619 A 5730 PANEL AIRBUS 300 A300F4605R 3930327 EU RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 RIGHT WING L/E PANEL 613 AB CUTOUT FWD OUTBD FASTENER HOLE IS CRACKED. MATERIAL ID FOR THE REPAIR IS 2024-T3, 0.056, PO 609852.1 IAW A300-600 SRM 53-52-00; FIG 703. FABRICATED THE REPAIR IAW A300-600 SRM 53-52-00; FIG N703. ALODINED IAW A300-600 SRM 51-21-10;PG 3. PRIMED IAW A300-600 SRM 51-23-10; PG 24. INSTALLED THE REPAIR IAW A300-600 SRM 53-52-00; FIG 703 AND 51-40-21; PG 7. 2 L 7 2 4F RT A35EU 20080714 WP 2008 7 14 08FDEA02140 1 20080603 A 5414 AUB703627 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 NR 1 PYLON PANEL 438 GL HOLE IS CHAFED. FABRICATED A NEW AUB 7036-27 SKIN IN REF TO FEDEX EA 8-5480-116987 AND REASSEMB LED THE PANEL IN REF TO FEDEX EA 8-5480-116987 "NACELLES/PYLONS - NR 1 PYLON AFT "V" FAIRING PANEL DAMAGED - REPAIR". 2 L 7 3 4F RT A22WE 20080714 WP 2008 7 14 08FDEA02141 1 20080603 A 5730 ARB25103 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 LEFT WING INBD LOWER L/E PANEL 516 HB IS CHAFED. BLENDED AREA IAW DC/MD-10 SRM 57-00-01; VOL I; FIG 1-A. ORIGINAL MAT ERIAL THICKNESS IS 0.090 IAW DC/MD-10 SRM 57-31-01; VOL III; FIG 1. MATERIAL LOSS IS 0.028. REMAINING THICKNESS IS 0.0 62. FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-00-01; VOL I; FIG 1- A. USED UT GAUGE T8225P. MATERIAL ID IS 7075-T 6, .100; PO 342278.3. FOR THE FILLER 7075-T6, 0.090, PO 603413.5 IAW DC/MD-10 SRM 57-00-01 AND 57-31-01; VOL III. FABR ICATED DOUBLER AND FILLER IAW DC/MD-10 SRM 57-00-01; VOL I; FIG 4; VOL I. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-0 1; VOL II; PGS 21-26. INSTALLED DOUBLER 7 FILLER IAE DC/MD-10 SRM 51-35-01; VOL II. 2 L 7 3 4F RT A22WE 20080714 NM 2008 7 14 ASAA0843097 1 20080507 A 5347 65554849 CARGO TRACK BOEING 737 7374Q8 138447Q NM BS 450-500 BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 FWD CARGO PIT TIE DOWN TRACK TIE DOWN POINT BROKEN OUT. TIE DOWN POINT REPAIRED IAW SRM 53 00 53 REPAIR 2 FIG 201. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 08FDEA02459 1 20080625 A 5312 BULKHEAD BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 CRACK IN RIGHT WHEEL WELL 870 BULKHEAD BOTTOM SIDE OF APU BLEED VALVE DUCT CUTOUT. FABRICATED REPAIR DOUBLER IAW SRM 53 -10-9, & FILLER, INSTALLED REPAIR PARTS IAW SRM 53-10-9 FIG 5. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 08FDEA02300 1 20080618 A 2130 CABIN PRESSURE BOEING 727 727225 1384077 NM MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 21 468FE 21452 FL270 AND .80 MACH, UPON COMP OF THROTTLE ALIGN CK AND RECYCLING OF NR 1 AND NR 2 ENG BLEED S CABIN PRESS BEGAN TO CLIMB AT 500-1000' FPM. COULD NOT STOP CLIMB AND APPROACHING 10K CAB PRESS WE WERE FORCED TO DESCEND TO 10K' AND DIVERT INTO DSM. IAW QRH ATTEMPTED TO STAB CABIN PRESS IN BOTH STANDBY AND MANUAL MODES 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 08FDEA02306 1 20080618 A 5315 143N534640 FLOORBEAM BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 CORROSION FOUND ON FLOOR SUPPORT AT BS 750, LBL4. CORROSION FOUND EXCEED ALLOWABLE LIMITS IN B757-200 SRM 51-10-02. RE MOVED AND REPLACED FLOOR SUPPORT STRINGER IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV.93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 08FDEA02307 1 20080618 A 5315 143N534640 FLOORBEAM BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 CORROSION FOUND ON FLOOR SUPPORT AT BS 748, RBL 12. CORROSION FOUND EXCEED ALLOWABLE LIMITS IN B757-200 SRM 51-10-02. REMOVED AND REPLACED FLOOR SUPPORT STRINGER IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080714 EU 2008 7 14 08FDEA02308 1 20080618 A 5710 A57310021202 PANEL AIRBUS 310 A310203 3930313 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 CENTER WING TANK LT BOOST PUMP AREA HAS 4 FASTENERS DAMAGED AT REINFORCEMENT BETWEEN FR 46 AND FR 47 REPAIRED DAMAGED FASTENER HOLES AT CENTER TANK LT BOOST PUMP INNER REINFORCEMENT PANEL BETWEEN FR 46 AND FR 47 IAW FEDEX EA 6-5710-121292 , RELEASE DATE 6 JUNE,2008 2 L 7 2 4F RT A35EU 20080714 EU 2008 7 14 08FDEA02311 1 20080618 A 5330 A255720310100 PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 BULK CARGO COMPARTMENT LEFT TRANSITION PANEL IS GOUGED FROM FRAME 63 TO FRAME 64; LBL 53 TO LBL 62. CHECKED LIMITS AND FOUND OUT OF LIMITS IAW A300-600 SRM 53-10-00. REMOVED TRANSITION PANEL IAW A300-600 SRM 51-40-21. MATERIAL ID 2024-T 3, 0.063, PO 619567.2 IAW AIRBUS DWG A25572031. ALODINED IAW A300-600 SRM 51-21-10. PRIMED AND PAINTED IAW A300- 600 S RM 51-23-10. LOCATED AND DRILLED IAW A300-600 SRM 51-40-44. PART MARKED IAW FEDEX GMM 7-0-1000. INSTALLED IAW A300-60 0 SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080714 EU 2008 7 14 08FDEA02369 1 20080620 A 5321 A5351014320500 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 MAIN CABIN FLOOR PANEL 262 VF IS CRACKED AND DAMAGED. MATERIAL ID FOR THE REPAIR IS 2024-T3, 056; PO 609852.1 IAW A300- 600 SRM 53-52-00; FIG 703. FABRICATED REPAIR IAW A300-600 SRM 53-52-00; FIG 7003. ALODINED IAW A300-600 SRM 51-21-10; PG 3. PRIMED IAW A300-600 SRM 51-23-10; PG 24. INSTALLED REPAIR IAW A300-600 SRM 53-52-00; FIG 703 AND 51-40-21; PG 7. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 08FDEA02370 1 20080621 A 5330 6545800Y218 DOUBLER BOEING 727 727227 1384078 NM ZONE 200 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 FUSELAGE SKIN DOUBLER IN FRONT OF L1/R1 WINDSHIELDS TORN AWAY AT L/E, BODY STA 178 AT TOP OF NOSE RADOME. REMOVED AND R EPLACED TORN SKIN DOUBLER AT BS 178 IN FRONT OF L1 AND R1 WINDOWS. NEW SKIN PART NUMBER 65-45800Y218 PO 819342 IAW SRM 51-30-5 AND SRM 51-30-5. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 08FDEA02371 1 20080621 A 5330 65184203 SKIN BOEING 727 727227 1384078 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 EXTERIOR FUSELAGE STA 300 JUST FWD OF L1 DOOR HAS A BULGE IN SKIN STR 9L. 9L REWORKED DENT TO ORIGINAL CONTOUR IAW SRM 51-40-1. HFEC INSPECTED DENT IAW NDTM 51-00-00 FIG 23 PART 6. NO DEFECTS NOTED. TREATED AND PRIMED AREA IAW SRM 51-10 -2. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 08FDEA02373 1 20080621 A 5314 65182333 KEELBEAM BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 LT MAIN LANDING GEAR WHEEL WELL KEEL BEAM CHORD CRACKED AT STA 872. TRIMMED OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER , INSTALLED DOUBLER IAW SB727-53-0208 AND EA 7-5310-116992. 2 L 7 3 4F A3WE 20080711 NM 2008 7 11 DHL2008764518 1 20080522 A 5753 FLAP BOEING 727 727264 138408M NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 LEFT INBOARD FORE FLAP CRACK INDICATIONS AT L/E FWD OF SEQUENCE CAR ATTACH POINTS (FITTING) WBL 124/203. STOP DRILLED A T THE END OF CRACKS AT LEFT INBOARD FORE FLAP L/E WBL 124/203 IAW B727 SRM 51-10-1. FAB DOUBLER REPAIR WITH 2024-T3 .05 0" AND PO 9006457 I/B DOUBLER 5.75" X 3.75" AND O/B 5" X 3.25" IAW B727 SRM 57-50-2 FIG 3 AND 57-50-4 FIG 1. C/W HFEC I AW B727 NDTM PT. 6 51-00-00 FIG 23, CRACK TERMINATES IN STOP DRILL HOLES. 2 L 7 3 4F A3WE 20080711 2008 7 11 MASA200800422 2 20080525 A 7310 FUEL CNDAIR CL600 CL6002B19 1900309 EA AFT COMPARTMENT DETECTED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 7305V 7305 ASH FLT 2821 BFL-PHX. FUEL ODOR IN COCKPIT LEFT PACK IN FLIGHT. MX CLEANED RESIDUAL FUEL FROM AFT COMPARTMENT. 2 L 7 2 4F RT A21EA 20080714 2008 7 14 DL76G080835 4 20080604 A 2565 SLIDE BOEING 767 7673P6 1385105 NM RIGHT OVERWING DEPARTED A DALA A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 SO 27 154DL 25241 FLT 116 RETURNED TO ATL AFTER A REPORTED LOUD NOISE AND THE RT OVERWING ESCAPE SLIDE DOOR LIGHT INDICATION. UPON ARRIVA L IT WAS FOUND THAT THE RIGHT SIDE OFF WING ESCAPE SLIDE HAD DEPARTED THE A/C AND THE DOOR WAS OPENED AND SEVERAL COMPON ENTS INSIDE THE SLIDE COMPARTMENT WERE DAMAGED. 2 L 7 2 4F RT A1NM 20080714 NM 2008 7 14 DLM88080844 1 20080610 A 5311 9953015115 FRAME DOUG MD88 MD88 3023688 NM BS 1463 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 971DL 53214 FUSELAGE STA 1463 CANTED FRAME OUTER CHORD FOUND CRACKED OUTBOARD OF L2L AND L2R AND BETWEEN L13R AND 14R. INNER SKIN D OUBLERS ALSO FOUND CRACKED ON BOTH SIDES OF BULKHEAD. INNER SKIN PANEL WEB FOUND CRACKED. INNER SKIN PANEL WEB AND BOT H SKIN DOUBLERS WERE REPLACED. CRACKED CHORD SECTIONS WERE CUTOUT AND REPAIR STRAPS WERE INSTALLED. 2 L 7 2 4F RT A6WE 20080714 NM 2008 7 14 DL757080782 1 20080528 A 5414 311N3153 FITTING BOEING 757 757232 1384965 NM NR 2 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 DURING HMV AT SAA, A HOLE WAS MISDRILLED COMMON TO THE NR 2 PYLON MIDSPAR FITTING, WEB, CHORD AND DOUBLER. THE HOLE WA S REAMED, BUSHED, AND REDRILLED PER BOEING INSTRUCTIONS. 2 L 7 2 4F RT A2NM 20080714 WP 2008 7 14 08FDEA02289 1 20080617 A 5751 ARC10589 STRUCTURE DOUG MD10 MD1010F 3022112 WP LT WING AILERON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 LEFT WING OUTBD AILERON T/E IS CRACKED AND DETERIORATING. REMOVED T/E SECTION IAW DC/MD-10 SRM 51-35-01; VOL II. MATER IAL ID FOR T/E SECTION IS 3913181-72, PO 621834.1 AND "Z" CHANNELS 2024-T3, 0.032, PO 473755.1. FABRICATED IAW DC/MD-10 SRM 57-20-01; FIG 10; VOL I. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01; PGS 21 - 24; VOL II. INSTALLED IAW DC/MD- 10 SRM 51-35-02; VOL II. 2 L 7 3 4F RT A22WE 20080715 EU 2008 7 15 E0X2008F00003 1 20080519 A 3040 ND00752011 CONTROLLER LUCAS BRAERO 1000 BAE1251000A 1500104 EU COCKPIT DEFECTIVE E E0XA A UNSCHED LANDING M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 39 541LR L240377 259041 ON CLIMBOUT, FLIGHT CREW ELECTED TO TURN ON WINDSHIELD HEAT, SOMETIME AFTER THAT AND BEFORE REACHING CRUISE ALT. THE FLI GHTCREW NOTED THE FO`S RT REAR WINDSHIELD DELAMINATING, LITERALLY COOKED, STATED BY CAPTAIN. FLIGHT CREW LEVELED AT 12,0 00 FT, DECLARED AN EMERGENCY AND DIVERTED. LANDIND WAS UNEVENTFUL WITH NO INJURIES TO THE PASSENGERS OR CREW, PILOT NOT ED NO UNUSUAL INDICATIONS OR SCREEN OVERHEAT. INSPECTED RT WINDSHIELD AND FOUND OVERHEATED. REPLACED WINDSHIELD RT SIDE AND THERMAL CONTROL UNIT. FUNCTIONAL CHECK WAS ACCOMPLISHED WITH NO DESCREPANCIES NOTED FOR THE RT WINDSHIELD OR WINDSH IELD HEAT. (K) 2 L 7 2 4F RT A3EU 20080715 NM 2008 7 15 08FDEA02138 1 20080603 A 5230 65691457 SUPPORT ANGLE BOEING 727 727227 1384078 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 FWD LOWER CARGO DOOR, FWD FRAME HAS CRACK IN SUPPORT ANGLE AT 3RD STOP FITTING UP FROM BOTTOM REMOVED DAMAGE PARTS. FAB RICATED NEW TEE CLIP AND GUSSET. INSTALLED NEW PARTS. REF SRM 51-30-02, 51-30-05 P 1-34 DWG NR 65-69145. TREATED AND PRIMED (GUSSET AND TEE) REF SRM 51-10-2 PG 1-27. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080715 NM 2008 7 15 08FDEA02083 1 20080602 A 5311 FRAME DOUG MD11 MD11F 3023600 NM BS 1139 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 624FE 48443 CAC COMPARTMENT AT STA 1139 LONGERON 29L TO 30L FRAME SPLICE FOUND CRACKED. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 ASAA0842997 1 20080515 A 5753 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 LT WING INBOARD FORE FLAP UPPER SURFACE HAS 4 EACH DENTS 15 INCHES FROM O BEND PREPARED DAMAGED AREA. FABRICATED DOUBLE R AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 ASAA0843001 1 20080514 A 5753 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 LT WING INBD FORE FLAP HAS 8 EA SMALL DENTS ON LOWER SURFACE NEAR 2ND TRACK OTBD. PREPARED DAMAGED AREA FABRICATED DOUB LER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 ASAA0843006 1 20080514 A 5753 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 LEFT WING OUTBOARD AFT FLAP DENTED ON LOWER SURFACE 46 INCHES FROM OUTBOARD END AND 4 INCHES FROM TRAILING EDGE. PREPAR ED DAMAGED AREA FABRICATED DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 ASAA0843008 1 20080525 A 5753 SKIN BOEING 737 737490 1384715 NM RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 RT OTBD AFT FLAP HAS A DENT 23 INCHES FROM INBD END ON UPPER SURFACE. REMOVED DAMAGED SKIN FABBED FILLER SKIN AND EXTER NAL DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 PARA'S 20 22 PGS 254 257. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 ASAA0843000 1 20080514 A 5755 SKIN BOEING 737 737490 1384715 NM NR 4 SPOILER LT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 LT WING NR 4 SPOILER LOWER SURFACE ABOVE INBD ACTUATOR HAS 8 EACH SMALL DENTS NEAR TRAILING EDGE. PREPARED DAMAGED AREA , FABRICATED DOUBLER FILLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080715 2008 7 15 IXXA080025O 4 20080529 A 3423 1428302001 COMPASS DOUG DC8 DC862F 3021972 WP COCKPIT DEFECTIVE A IXXA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 11 71CX 71916 1913 45961 DURING CRUISE FROM KBWI, THE CREW PERFORMED COMPASS RATING CHECK, BOTH COMPASS SYSTEM HAD EXCESSIVE DRIFT (20 DEGREE IN 30 MIN). THE CREW LANDED IN CYYR WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FOG GYRO COMPASS SYS TEM. OPERATIONAL CHECK GOOD IAW DC8 MAINTENANCE MANUAL 34-11-1. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 20080715 NM 2008 7 15 SB08037 1 20080529 A 3350 20131ASMI BATTERY PACK BOEING 737 737401 1384701 NM AFT CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 421US 23988 BDL MAINTENANCE REPORTED THE EMERGENCY LIGHT BATTERY PACK WAS DISCHARGED AT THE AFT RIGHT-HAND POSITION OF AFT GALLEY CEILING, RIGHT-HAND SIDE OF CENTERLINE OVERHEAD LIGHT. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK PER MM 33-51-51 -2. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20080714 EU 2008 7 14 08FDEA02383 1 20080623 A 5720 A57244250006 CHANNEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND A DOUBLE HOLE IN LT WING TIP END RIB CHANNEL. REPAIR PERFORMED BY OVERSIZING, PLUGGED THE HOLE AND FASTENER INSTA LLATION AT ORIGINAL LOCATION IAW RAS /BAE/1007232/2008 ISS A, APPROVED BY EA 6-5730-120058. 2 L 7 2 4F RT A35EU 20080715 EU 2008 7 15 08FDEA02261 1 20080613 A 2910 LINE AIRBUS 310 A310324 3930206 EU HYD SYSTEM LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 21 810FD 452 HYD GREEN SYSTEM LOW LEVEL IN FLIGHT. ECAM WARNING, MANUAL EXTENTION OF L/G. FOUND UPPER HYD LINE TO RT AILERON DROOP ACTUATOR LEAKING. REPAIRED SAME HYD LINE IAW AMM 20-23-11-0, LEAK CHECK GOOD. REPLENISHED GREEN HYDRAULIC SYSTEM IAW AMM 29-10-00-3. CREW SHUT HYD SYS DWN, NO PUMP CAVITATION/DAMAGE. FOUND UPPER HYD LINE TO RT AILERON DROOP ACTUATOR LEAKING. REPAIRED SAME HYD LINE IAW AMM 20-23-11-0. LEAK CHECK GOOD. REPLENISHED GREEN HYDRAULIC SYSTEM IAW AMM 29-1 0-00-3. 2 L 7 2 4F RT A35EU 20080715 EU 2008 7 15 08FDEA02321 1 20080619 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND 2 CHAFING MARKS AT LT OUTER FLAP TOP SKIN, RIB 3A-4 AND 14A-15A REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR, N DT FOR CRACK FREE CONDITION AND INSTALLING NEW CHAFING PLATES IAW RAS/FOK/131/2008 ISS A, APPROVED BY EA 6-5754-120125. 2 L 7 2 4F RT A35EU 20080715 NM 2008 7 15 08FDEA02333 1 20080619 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 FOUND WITH CRACK INDICATIONS AT HOLES NR B, NR C AND NR D (THIRD LAYER). REMOVED AND REPLACED AS PER SRM 51-31-01, VOL.II. NEW FITTING FABRICATED AS PER EA 1-5300-122494, REPAIR CLASSIFIED A S MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 08FDEA02341 1 20080619 A 5320 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 4 O'CL OCK POSITION) AT HOLE NR C. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 08FDEA02344 1 20080619 A 5320 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 10 O'C LOCK POSITION) AT HOLE NR C. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PE R GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080714 NM 2008 7 14 SWAA083484 1 20080623 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083457 1 20080623 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730E, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083477 1 20080623 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 16R. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083359 1 20080618 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083176 1 20080610 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083188 1 20080610 A 3234 65542191 HANDLE BOEING 737 7373H4 1384600 NM COCKPIT DIRTY A SWAA K NONE J WARNING INDICATION AP APPROACH 1 SW 29 355SW 25250 WITH LANDING GEAR HANDLE IN DOWN POSITION HAD THREE GREEN AND THREE RED LIGHTS ILLUMINATED. CYCLED GEAR UP AND DOWN, AL L INDICATIONS NORMAL. CLEANED AND LUBED GEAR HANDLE PER MM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 2008UALA02979 1 20080523 A 2150 CONTROLLER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE AIR CON SYS MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C CL CLIMB 1 WP 29 218UA 30222 RIGHT ENG BLEED SYSTEM HAS LARGE PRESSURE FLUCTUATIONS WITH ASSOCIATED ENG PARAMETER FLUCTUATIONS IN CLIMB AND IN CRUISE . WITH RIGHT PACK SELECTED -OFF- THE PRESSURE AND ENG PARAMETERS ARE STABLE. REPLACED ASCPC FOR RT AIR SUPPLY. ASCPC I NSTALLED AND CABIN PRESS CONTROL SYSTEM TEST PASSED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080714 NM 2008 7 14 DLM90080821 1 20080601 A 5320 WEB DOUG MD90 MD9030 3023690 NM FS 588-586 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 916DN 53396 LEFT CABIN CUSP WEB FS 588-586 CORRODED. INSTALLED REPAIR DOUBLER IAW MD 80 SRM 53-05D FIG 827D. 2 L 7 2 4F RT A6WE 20080714 NM 2008 7 14 08FDEA02396 1 20080624 A 7603 NUT BOEING 727 727227 1384078 NM THROTTLE MISSING A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 MISSING NUT ON BOLT SECURING NR 3 ENGINE THROTTLE CONTROL ROD INBD OF ENGINE. REMOVED AND REPLACED NUT, BOLT AND LOCK I AW FX B727 76-12-000-5. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 08FDEA02405 1 20080624 A 5753 6521795 FAIRING BOEING 727 727225 1384077 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 NR 4 FLAP TRACK MID FAIRING, CRACK ON INNER SIDE OF MLG FLYING DOOR FWD HINGE CUT OUT ON FAIRING. FABRICATED NEW DOUBLE R, REF 727 51-20-1 PG 4, MATERIAL VERIFIED AS 7075-76 .050" REF BAC DWG 65-21795. REPLACEMENT MATERIAL VERIFIED AS 7075 -76 .050" BY A-TAG NR A03906. TREATED AND PRIMED NEW DOUBLER. REF 727-51-2, PG 1. INSTALLED DOUBLER REF 727 SRM 51-30 -2 PG1, TOP COATED REPAIR AREA OF NEW DOUBLER REF MM 51-20-013 PG -7. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 USAA920081115 1 20080509 A 5313 6552988 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 23700 MCN - MAJOR REPAIR - B1 CHECK - CRACKED STRINGER, BS 927, S22L. REPAIRED STRINGER, BS 927, S22L IAW B737 SRM 53-00-03 F IGURE 201. 2 L 7 2 4F RT A16WE 20080714 WP 2008 7 14 08FDEA02448 1 20080625 A 5312 AEA01613 BULKHEAD DOUG DC10 DC1010 3022110 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 LT MLG WW FOUND CRACK ON VERTICAL BULKHEAD. 2 L 7 3 4F A22WE 20080714 NM 2008 7 14 ASAA0843100 1 20080609 A 5320 69353654 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM BS 380-400 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 PASSENGER CABIN FLOOR STRUCTURE AT BS380 400 BL0 UPPER ANGLE IS CRACKED AT 3 FASTENER HOLES. REPLACED CABIN FLOOR UPPER ANGLE WITH NEW PART IAW B737 400 SRM 51 40 05 AND 51 40 02. 2 L 7 2 4F RT A16WE 20080714 WP 2008 7 14 08FDEA02309 1 20080618 A 5313 ADA3064507 LONGERON DOUG DC10 DC1010 3022110 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 FWD CARGO COMPT BILGE AREA FOUND ELONGATED HOLE. 2 L 7 3 4F A22WE 20080714 WP 2008 7 14 08FDEA02384 1 20080623 A 5712 ARB13354 RIB DOUG DC10 DC1010 3022110 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 RT WING L/E DROOPED FOUND NR 3 BROKEN ANGLES INT DROOPED. REPAIRED AREA IAW SRM 57-00-01 FIG 1,3,4 VOL I. 2 L 7 3 4F A22WE 20080715 NM 2008 7 15 USAA920081221 1 20080601 A 5310 143N832853 CREASE BEAM BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 905AW 23567 NR 6109913 - LEVEL 2 CORROSION ON CREASE BEAM INNER CHORD AT BS 734, WL 208, BL64L. REPLACED CREASE BEAM INNER CHORD AT BS 734, WL208, BL 64L IAW SRM 51-40-02-0G. (K) 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 USAA920081223 1 20080601 A 5310 140N0504 CREASE BEAM BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 905AW 23567 NR 6110496 - LEVEL 2 CORROSION ON CREASE BEAM CHORD AT BS 443, WL 208, BL 64L. REMOVED AND REPLACED CREASE BAM CHORD AT BS 443, LW 208, BL 64I, IAW SRM 51-40-02-0G. (K) 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 USAA920081226 1 20080601 A 5320 284N102039 INTERCOSTAL BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 905AW 23567 MCN-C12-MAJOR REPAIR - NR 6109932 - INTERCOSTAL WEB CRACKED B/S 480 LBL 38 W/L 201.1 (HFEC VERIFIED). REPAIRED INTERCOST AL WEB B/S 480 LBL 38 W/L 201.1 IAW SRM 51-40-02-0G. (K) 2 L 7 2 4F RT A2NM 20080715 WP 2008 7 15 08FDEA02387 1 20080623 A 5340 AGA38052 STRUT DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 AFT CARGO COMPT TUNNEL AREA FOUND MODERATE CORROSION ON STRUT. 2 L 7 3 4F A22WE 20080715 WP 2008 7 15 08FDEA02290 1 20080617 A 5410 AUB70375 SEAL DOUG MD10 MD1010F 3022112 WP NR 3 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 NR 3 PYLON LEFT SKIRT FAIRING METAL SEALS ARE WORN. REMOVED AND REPLACED P/N AUB 7078-17 SEAL AND AUB 7037-17 SEAL IAW DC/MD-10 SRM 51-35-01; VOL II. MATERIAL ID GAL-4V063 TITANIUM, 0.063 IAW DC/MD-10 SRM 54-00-01; FIG 2B; VOL I. FABRICA TED A DOUBLER AND DRILLED HOLES IAW DC/MD-10 SRM 54-00-01, FIG 2B; VOL I. 2 L 7 3 4F RT A22WE 20080715 WP 2008 7 15 08FDEA02299 1 20080617 A 5230 ACA74477 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 MAIN CARGO DOOR LOWER JAMB NR 5 SPOOL FITTING LOWER JAMB SUPPORT FITTING IS CORRODED AND CRACKED. PERFORMED HFEC INSPEC TION PER STSPM 6-10-01-00 ON THE LOWER JAMB FITTING FOR THE MCD AT SPOOL FITTING AT THE NR 5 LOCATION AND VERIFIED THAT NO CRACK WAS NOTED AT THIS TIME. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 08FDEA02301 1 20080618 A 5330 SKIN BOEING 757 75723A 1384967 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 LIGHTNING STRIKE REPAIR FOUND AT BS 550 BETWEEN S-26L AND S-27L TO EVALUATE REPAIR. EXISTING LIGHTNING STRIKE REPAIR EVALUATED AS PER EO F-5100-7-5001 PT 1 ATTACHMENT B, FOUND PREVIOUSLY ACCOMPLISHED IAW B757-200 SRM 53-00-01 FIG 201, RE PAIR 6 SECTION 1. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 08FDEA02327 1 20080619 A 5320 453N180140 ANGLE BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 BS 1560, STR 22R TO 26R SIDEWALL SUPPORT ANGLE HAS CORROSION. REMOVED AND REPLACED SUPPORT ANGLE IAW B757-200 SRM 51-40 -02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 08FDEA02329 1 20080619 A 5320 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATIONS AT HOLES NR A AND NR C (THIRD LAYER). REM OVED AND REPLACED AS PER SRM 51-31-01 VOL. II. NEW FITTING FABRICATED AS PER EA 1-5300-122494, REPAIR CLASSIFIED AS MAJ OR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 08FDEA02337 1 20080619 A 5730 ARB74024 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 03 EACH FASTENER HOLES FOUND CRACK INDICATIONS DURING OPEN-HOLE HFEC INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR C UTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. CARRIED OUT REPAIR AS PER EA 1-5710-122497 PART 1. THIS REP AIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 08FDEA02339 1 20080619 A 5320 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 2 O'CL OCK POSITION) AT HOLE NR C. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 08FDEA02340 1 20080619 A 5320 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 8 O'C LOCK POSITION) AT HOLE NR C. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PE R GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 08FDEA02345 1 20080619 A 5100 NONE BOEING 757 7572B7 1384964 NM NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 903FD 27124 ACCOMPLISH SB 757-54-0035, R2, PARA 3, PART 2; WING STRUCTURE CHANGES FOR THE NR 2 STRUT AND RT WING PER EA F-5450-10890 7, DATED 11 OCT 2007. ACCOMPLISHED SB 757-54-0035, PART 2, ON NR 2 STRUT, AS PER EA F-5450-108907A, DATED 28 MAY 2008. PER EA, SCHEDULE EO F-5450-7-5006 WIC PARTS 3 AND 4, EVERY 9000 FC OR 54 MONTHS, WHICHEVER OCCURS FIRST. 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 08FDEA02281 1 20080616 A 5313 655623620 STRINGER BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 490FE 21493 FWD CARGO COMPARTMENT, STRINGER 27R CORRODED BETWEEN STA 720A AND 720C REMOVED BODY FAIRINGS NR 3420 AND 3437 IAW SRM 51 -30-2, REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. CUT OUT DAMAGE AREA (DIM 47 INCHES LONG ) AND FABRICATED NEW STRINGER F ROM BAC1498-145 AND NEW SPLICE FROM BAC1498-131 IAW SRM 53-10-3, FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INST ALLED PARTS AND REINSTALLED BODY FAIRINGS IAW SRM 53-10-3 FIG AND 51-30-2. FOR REFERENCE SEE N/R N00861. 2 L 7 3 4F A3WE 20080715 EU 2008 7 15 08FDEA02395 1 20080624 A 5330 A53973278202 SKIN AIRBUS 310 A310222 3930315 EU FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 LOWER FUSE STA 3461/FR64-STA 3514/FR65, S31R-S34R 1 DENT ON EXTERNAL SKIN (13 INCH BY 0.5 INCH BY 0.007 INCH) SEE DETA ILED EA6-5330-117353. 2 L 7 2 4F RT A35EU 20080715 EU 2008 7 15 08FDEA02318 1 20080618 A 5753 A5797130100100 SKIN AIRBUS 310 A310203 3930313 EU ZONE 600 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RIGHT WING O/B FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB 3 AND FLAP T RACK NR 3 AND 5.7 INCH FWD OF REAR SPAR MEASURING 11.3 INCH BY 3.9 INCH. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREV IOUS REPAIR AND INSTALLED AN APPROVED REPAIR ON RIGHT WING O/B FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB 3 AND FL AP TRACK NR 3 AND 5.7 INCH FWD OF REAR SPAR IAW FEDEX EA6-5750-121299. THIS IS AN APPROVED REPAIR AND IS A RESULT OF AG ING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080715 NM 2008 7 15 08FDEA02288 1 20080617 A 5414 311N504633 SKIN BOEING 757 7572B7 1384964 NM NR 2 STRUT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 906FD 27148 STRUT NR 2 INBOARD SIDE OF SKIN AT APPROX PPS 200.50 HAS EXFOLIATED CORROSION (APPEARS TO BE TRAVELING UNDER FRAME/CORD ALSO). REMOVED SKIN IAW SRM 51-40-02. REMOVED CORROSION AT STA 157, ORIGINAL MATERIAL THICKNESS .090 INCH, REMAINING T HICKNESS .062 INCH, OUT OF LIMITS PER SRM 54-50-01. REMOVED AND RE-INSTALLED I/B SUPPORT FITTING AND PLATE, 3 ACCESS DO ORS, 2 BULB SEALS, HEAT SHIELD, AND I/B FAIRING IAW ARM 51-40-02 TO FACILITATE SKIN REMOVAL AND INSTALLATION. INSTALLED REPAIR SKIN IAW DWG 311N5002 AND SRM 51-40-02. THIS IS A MAJOR REPAIR CATEGORY A, NO FOLLOW UP TRACKING REQUIRED. 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 08FDEA02291 1 20080617 A 5330 65562502 SKIN BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 AFT PIT BILGE SKIN HAS CORROSION AT STATION 1008 OB OF STRINGER 28L REMOVED CORROSION REF SRM 51-10-1 ORIG T .082 REMAIN ING .047, .035 LOSS USING TOOL IN22-0028, OUT OF LIMITS. REF SRM 53-10-1 FIG 1. FABRICATED REPAIR DOUBLER REF EA 7-53 30-113 990. INSTALLED NEW STRINGER SPLICE REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080715 NM 2008 7 15 USAA920081231 1 20080604 A 5320 143N832854 STRUCTURE BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 905AW 23567 MCN - C12 - MAJOR REPAIR - NR 6061159 - R2 DOOR CUTOUT HAS CORROSION ON INNER STRUCTURE AT BS 686 TO 729.6, WL 208.1. RE PLACED R2 DOOR CUTOUT INNER STRUCTURE AT BS 686 TO 729.6, WL 208.1 IAW SRM 51-40-02-0G. (K) 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 USAA920081230 1 20080602 A 5315 143N50637 FLOORBEAM BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 905AW 23567 MCN - C12 - MAJOR REPAIR - NR 6111603 - FLOORBEAM CRACKED UPPER T-CAP AFT RADIOS B/S 700 RBL 45 W/L 208.1. REPAIRED FLOO RBEAM UPPER T-CAP AFT B/S 700 RBL 45 W/L 208.1 IAW B757 SRM 53-00-51-2R1. (K) 2 L 7 2 4F RT A2NM 20080715 NE 2008 7 15 USA2008F00004 2 20080615 A 7200 ENGINE BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE RIGHT OVERHEATED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 19 937UW 27245 CUN FLT 808, ENROUTE CUN TO CLT. ON CLIMB-OUT, AT FL290, THE RIGHT ENGINE INDICATED AN OVERHEAT CONDITION. THE CREW REDU CED THE THRUST SETTING HOWEVER, THE INIDCATION DID NOT GO OUT. THE CREW SHUTDOWN THE RIGHT ENGINE AS REQURIED IAW PROCED URES, AND RETURNED TO CUN. MAINTENANCE ACTION PENDING. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 20080715 NM 2008 7 15 USAA920081209 1 20080607 A 5330 6545778 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 445US 24863 GLT - MAJOR REPAIR - NR 7028999, CRACKED FUSELAGE SKIN, BS 960, WL 208 AT THE R2 DOOR CUT OUT. REPAIRED FUSELAGE SKIN, B S 960, WL 208 AT THE R2 DOOR CUT OUT IAW EA 111178. (K) 2 L 7 2 4F RT A16WE 20080715 EU 2008 7 15 USAA920081220 1 20080524 A 5347 D53472090004 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 652AW 0953 SAL - C7 - MAJOR REPAIR - NR 61075158 - CORROSION ON SEAT RAIL ASSEMBLY BEAM AT FR 64 TO FR 66, BL Y1292. REPAIRED CORRO SION ON SEAT RAIL ASSY BEAM AT FR 64 TO FR 66, BL Y1292 IAW SRM 51-72-11. (K) 2 L 7 2 4F RT A28NM 20080715 NM 2008 7 15 USAA920081213 1 20080604 A 5315 STRAP BOEING 757 7572B7 1384964 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 929UW 27144 BFM - C-2 - MAJOR REPAIR - NR 6051543 - FLOORBEAM STRAP CRACKED AT BS 1300 RBL 25. REPAIRED FLOORBEAM STRAP AT BS 1300 RBL25 IAW SRM 51-70-11. (K) 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 USAA910081236 1 20080531 A 5320 907822 STRAP BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW 23713 CLT - C22 - MAJOR REPAIR - NR 11A52001/003 - FORWARD ENTRY DOOR HINGE CUTOUT AT BS-312, S-10L IAW DWG NR 65-17684. (K) 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 USAA920081232 1 20080604 A 5312 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW 23713 CLT - C22 - MAJOR REPAIR - NR 03-0553-8-0105/006- WEB CRACKED AT BS 178 1.5, LBL 17.1. REPAIRED WEB AT BS 178 1.5, LBL 17.1 IAW 51-70-13G. (K) 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 USAA920081233 1 20080603 A 5312 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW 23713 CLT - C22 - MAJOR REPAIR - NR 03-0553-8-0105/007 - CRACK IN WEB AT BS 178 1.5, RBL 5.7. REPAIRED WEB AT BS 178 1.5, RBL 5.7 IAW SRM 51-70-13. (K) 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 USAA920081239 1 20080604 A 5312 6547952524A BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW 23713 CLT - C22 - MAJOR REPAIR - NR 03-0553-8-0005/002 - PRESSURE WEB CRACKED BS 178, WL 212, LBL 4.5. REPAIRED PRESSURE WEB BS 178, WL 212, LBL 4.5 IAW SRM 53-10-08, REPAIR 11. (K) 2 L 7 2 4F RT A16WE 20080715 EU 2008 7 15 08FDEA02293 1 20080617 A 5720 A5724019420100 SUPPORT AIRBUS 300 A300F4605R 3930327 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 LEFT WING T/E SPAR AREA; NR 4 SPOILER OUTBD HINGE INNER WEB HAS A REPAIR INSTALLED THAT IS CRACKED IN THE RADIUS. THE N R 4 SPOILER IS REALLY THE NR 2 OUTBD. REMOVED SKIN SUPPORT IAW A300-600 SRM 51-40-21; PG 7. LOCATED; DRILLED AND DEBUR RED SKIN SUPPORT P/N A5724019420100, PO 592540.6 IAE BA DWG A57240194. INSTALLED SKIN SUPPORT IAW A300-600 SRM 51-40-2 1; PG 7. 2 L 7 2 4F RT A35EU 20080715 WP 2008 7 15 08FDEA02296 1 20080617 A 5313 AEA04721 LONGERON DOUG MD10 MD1010F 3022112 WP BS 1500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 LEFT MLG WHEEL WELL UNDER UPPERWING TO BODY FAIRING AT FS 1500 LONGERON IS CRACKED. REMOVED & RE-ISTALLED THE LT GILL L INER PANEL FROM BS 1521-1561 FOR ACCESS IAW SRM 51-31-01; VOL II. REMOVED LONGERON. FABRICATED & INSTALLED IAW DWG AEA 0472, REV NC SRM 51-33-14, VOL II; & 51-35-01, VOL II. ALODINED & PRIMED IAW SRM 51-21-01, VOL II. 2 L 7 3 4F RT A22WE 20080715 WP 2008 7 15 08FDEA02298 1 20080617 A 5320 FITTING DOUG MD10 MD1010F 3022112 WP DOOR FRAME CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 MAIN CARGO DOOR LOWER JAMB NR 7 SPOOL FITTING LOWER JAMB FITTING IS CORRODED AND CRACKED. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 08FDEA02153 1 20080604 A 5320 651750631 WEB BOEING 727 727227 1384078 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 AIR STAIR COMPARTMENT ABOVE "S" DUCT AT STA 1303, RT SIDE OF YELLOW VERTICAL WEB WHERE STIFFENER PASSES THROUGH CUTOUT , CRACKED. DOTS ARE ON AFT SIDE ACCESING THROUGH VERT STAB PANEL. REMOVED DAMAGED, FABRICATED, TREATED, PRIMED, AND IN STALLED. REPAIR REF SRM'S 51-30-02 PG 32, 51-40-02 PG 1-6, AMM`S 51-20-021-7 PG 1-3, 51-20-031, PG 1-3, AND DOC PL 65-1 7506 ITEM 31. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080715 EU 2008 7 15 08FDEA02158 1 20080604 A 5753 SKIN AIRBUS 310 A310203 3930313 EU TE FLAP MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RT WING OUTBD FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB NR 2 AND RIB NR 3 AND 9.6 IN FWD OF REAR SPAR MEASURING 7.5 IN BY 7.1 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AN D INSTALLED CORRECT OUTER SKIN REPAIR ON RT WING OUTBD FLAP UPPER SKIN BETWEEN RIB NR 2 AND RIB NR 3 IAW A310-200 SRM 57 -53-10, FIG 210. THIS IS AN AIRBUS REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080715 EU 2008 7 15 08FDEA02349 1 20080619 A 5753 A5796001120000 SKIN AIRBUS 300 A300F4605R 3930327 EU RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 THE RIGHT INBD FLAP LOWER SURFACE HAS DENTS. LIMITS CHECKED AND THE DENTS WERE FOUND TO BE WITHIN LIMITS AT DOTS C528, 0 .029 AND P745, 0.029 IAW A300-600 SRM 57-50-00 PGS 104; 105 AND 106; FIGURE D USING DEPTH GAUGE T8410B. DOT NR C527 WAS FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 57-50-00. REPAIR ACCOMPLISHED IAW A300-600 SRM 57-50-00; FIG 205. DOT NR P745 IS .018 BY .086 AND DOT NR C528 .022 BY .084 FOUND TO BE WITHIN LIMITS IAW A300-600 SRM 57-50-00 USING DEPTH GAUGE TT8401B. 2 L 7 2 4F RT A35EU 20080715 WP 2008 7 15 08FDEA02165 1 20080605 A 5720 BRACKET DOUG MD10 MD1010F 3022112 WP SLAT TRACK BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 RIGHT WING NR 7 SLAT TRACK CLOSE OUT PANEL HAS A BROKEN BRACKET. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 USAA920081242 1 20080605 A 5330 65457742 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN - C-21 - MAJOR REPAIR - NR 6110423- FUSELAGE SKIN CRACKED BS 754 JUST ABOVE S20L. REPAIRED FUSELAGE SKIN BS 754 JUS T ABOVE S20L IAW SRM 53-00-01 & TEMP REVISION 53-33. (K) 2 L 7 2 4F RT A16WE 20080715 CE 2008 7 15 MT9A00000027 1 20080512 A 3240 06111800 HOUSING CESSNA 208 208B 2073701 CE MLG BRAKE DAMAGED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 4602B 208B0140 BRAKE CYLINDER HOUSING WORN AT THE ANCHOR BOLT PASS THROUGH HOLE ALLOWING THE ANCHOR BOLT TO BE PRESSED OUT BY HAND. THI S IS NORMALLY A CLOSE TOLERANCE FIT. THIS CONEIDION IN THE PAST HAS CAUSED THE ANCHOR BOLT TO SHEER OFF CAUSING CATASTRO PHIC DAMAGE TO THE CALIPER ASSEMBLY, TORQUE PLATE AND/OR TIRE ON THREE OF OUR AC. (K) 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000008 1 20080410 A 2750 MS276404 BEARING CESSNA 208 208B 2073701 CE BELLCRANK FROZEN E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9505B 208B0085 THE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS. (K) 1 H 7 1 3T A37CE 20080715 NM 2008 7 15 08FDEA02191 1 20080607 A 5313 651821041 STRINGER BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 CORROSION ON INSIDE OF STRINGER S-3R AT STA 520 REMOVED .008' CORROSION FROM ORIGINAL STRINGER. THICKNESS OF .036'. RE MAINING THICKNESS IS .028" AND STRINGER WHERE DAMAGE IS OUT OF LIMITS. REMOVED DAMAGE SECTION OF STRINGER, FABRICATED R EPAIR PARTS, TREATED, PRIMED AND INSTALLED, REFERENCE SRM 53-10-1/FIG NR 1 AND SRM 53-10-3/FIG NR 3, CLASSIFIED AS A M AJOR REPAIR. 2 L 7 3 4F A3WE 20080715 CE 2008 7 15 MT9A00000023 1 20080512 A 3240 06111800 HOUSING CESSNA 208 208A 2073703 CE BRAKE ASSY DAMAGED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 BRAKE CYLINDER HOUSING WORN AT THE ANCHOR BOLT PASS THROUGH HOLE ALLOWING THE ANCHOR BOLT TO BE PRESSED OUT BY HAND. THI S IS NORMALLY A CLOSE TOLERANCE FIT. THIS CONDITION IN THE PAST HAS CAUSED THE ANCHOR BOLT TO SHEER OFF CAUSING CATASTRO PHIC DAMAGE TO THE CALIPER ASSEMBY, TORQUE PLATE AND/OR TIRE ON THREE OF OUR AC. (K) 1 H 7 1 3T NT A37CE 20080715 NM 2008 7 15 UPS08B52375 1 20080327 A 5311 FRAME BOEING 747 747400 13848AT NM BS 1120 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:C LT BS 1120 TENSION TIE FRAME WEB CRACKED ABOUT 0.500 INCH LT BS 1120 TENSION TIE FRAME WEB REPLACED PE R SRM 53-40-07 REPAIR 1. 2 L 7 4 4F RT A20WE 20080715 NM 2008 7 15 ASAA0843009 1 20080528 A 5320 651960351 CUSP WEB BOEING 737 737490 1384715 NM BS 380 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 CUSP WEB IS CREASED AT STA 380 LT SIDE. REMOVED DAMAGED AREA FABBED AND INSTALLED REPAIR IAW SRM 51 70 13 FIG 1. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 ASAA0843011 1 20080518 A 5512 657378252 SKIN BOEING 737 737490 1384715 NM HORIZONTAL STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 RT HORIZONTAL STABILIZER LEADING EDGE IS DENTED. REMOVED DAMAGED AREA OF SKIN FABRICATED AND INSTALLED REPAIR SKIN AND SPLICE PLATES IAW B737 400 SRM 55 10 01 REPAIR 12. 2 L 7 2 4F RT A16WE 20080715 NE 2008 7 15 ASAA0853017 2 20080601 A 7261 OIL SYSTEM BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE LOW A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 587AS 2372 35684 895977 NR 1 ENGINE OIL IS AT 13 QTS SERVICED ENGINE OILS NR 1 ADDED 3 QTS, NR 2 ADDED 3.5 QTS APU ADDED 0. 2 L 7 2 4F 4 F RT A16WE E2GL 20080715 NM 2008 7 15 SWAA082902 1 20080529 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 468WN 33858 EEPLS ASSY LOOSE AT ROW 5 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 AALA200801275 1 20080511 A 3350 HOUSING BOEING 777 777223 1385213 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 795AN 30257 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR GALLEY CLOSET HAS BROKEN HOUSING. REPLACED LIGHT ASSEMBLY HOUSING FOR EME RGENCY LIGHT AT LEFT NUMBER ONE DOOR GALLEY CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080715 WP 2008 7 15 AALA200801253 1 20080508 A 7830 221EN502R SWITCH DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE THRUST REVERSER WORN A AALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 584AA 53247 709899 STL INFLIGHT T863/08MAY PHL TO DFW - CREW REPORTED NUMBER ONE ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. NO YAW ASSOCIA TED WITH INDICATION. CREW SHUT DOWN NUMBER ONE ENGINE. LANDED STL WITHOUT INCIDENT. SINGLE ENGINE TIME 31 MINUTES. F OUND BOTH UPPER AND LOWER SWITCHES WORN. REPLACED BOTH UPPER AND LOWER SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATIO N. 2 L 7 2 4F 4 F A6WE E9NE 20080715 NM 2008 7 15 SWAA083825 1 20080713 A 5315 147A5505 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 773SA 27881 DURING SCHEDULED 8Y CHECK, FOUND FLOOR BEAM CORRODED AT BS 986.5, RBL 14.5. REPAIRED FLOOR BEAM PER SRM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083824 1 20080713 A 5310 65479769 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 847 TO BS 867, LBL 70. REPAIRED WEB PER SRM AND BOEING DRAWING. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083822 1 20080713 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMEMRGECY EXIT SIGN BROKEN. R&R EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 20080715 2008 7 15 SWAA083851 4 20080709 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080715 2008 7 15 SWAA083850 4 20080709 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080715 2008 7 15 SWAA083849 4 20080711 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083847 1 20080712 A 3397 W4142001220 WIRE BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 485WN 32473 DURING SCHEDULED MV3 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. FOUND LOOSE WIRE. SECURED WIRE PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083846 1 20080711 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 480WN 33998 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. R&R BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083840 1 20080706 A 5315 BAC15201397 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 423WN 29827 DURING SCHEDULED 6Y CHECK, FOUND FLOOR BEAM CORRODED AT BS 772, LBL 12 TO RBL 13. REPAIRED FLOOR BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083834 1 20080710 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT RH FWD CABIN. R&R EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083836 1 20080710 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT LT AFT CABIN. R&R EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 08FDEA02129 1 20080603 A 5310 65235557 BEAM BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 CORROSION INSIDE DELTA BEAM STA740, LBL 3, WL 148 CUT AWAY LWR WEB SECTION OF DELTA BOX TO FOM. REMOVED CORROSION FROM DELTA BEAM STA 740, LBL 3, WL 148. VERIFIED MATERIAL LOSS BY NDT, AND FOUND TO BE OUT OF LIMITS REF DWG 65-23555. REPL ACED INTERCOSTAL REF DWG-23555. FABRICATED NEW WEB SECTION, VERIFIED MATERIAL FOR NEW WEB REF DWG .080. FABRICATED AN D INSTALLED WEB. REF DWG 65-23555-7, SRM 51-4-02 PG 1-6, SRM 51-30-2 PG 1-6. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080716 NM 2008 7 16 NWAA082366623 1 20080525 A 5411 FRAME BOEING 747 747251B 1384892 NM NR 4 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 623US 21705 DURING M-CHECK FOUND CRACK IN NR 4 PYLON NACELLE BULKHEAD FRAME AT NAC STA 221.90 LT. REPAIRED PER EA 66-212663. 2 L 7 4 4F RT A20WE 20080716 EU 2008 7 16 08FDEA02056 1 20080514 A 5310 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 FWD CARGO COMPT, SCRATCHES AND DEFORMATIONS AT FRAME 20A BETWEEN STGR 39-41 RT. 2 L 7 2 4F RT A35EU 20080716 NM 2008 7 16 DHL2008764533 1 20080529 A 5753 ATTACH ANGLE BOEING 727 727264 138408M NM TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C CHECK, LT O/B MID FLAP I/B LOWER END CAP AND ATTACHMENT ANGLE CRACKED. REPAIRED IAW B727 SRM 51-40-2, 51-20- 1, 51-30-5 AND 57-50-2 FIG 6. REPAIR ANGLE MAT.7075 T6 .071" PO NR 9006522 DIM 4 INCH BY 4 INCH AND 3 INCH BY 2 INCH. 2 L 7 3 4F A3WE 20080716 WP 2008 7 16 DHL2008807534 1 20080507 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 "D" CARGO DOOR JAMB FWD LWR CORNERS CRACKED (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2005-18-07, S/B DC8 53-078, DO UGLAS DWG SR08530019, 5750776. REMOVED PARTS TO GIVE ACCESS IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED EDDY CURRENT INSPE CTION OF EXT SKIN, INTERNAL DOUBLER, INTERNAL SKIN AND PRESSURE SEAL IAW BOEING DC8 NDT SPM PART 06-10-01-001 AND PERFOR MED X-RAY INSPECTION OF "D" CARGO DOOR JAMB. NO CRACK FOUND IAW BOEING DC8 NDT SPM PART 02. ENCLOSED SMN FORM 242-1, 2 42-2. FABRICATED EXT REPAIR DOUBLER (AL7075T6 0.090") AND EXT REPAIR TRIPLER (AL7075T6 0.125") IAW DOUGLAS DWG NR SR085 30019, SRM 51-1-11, SRM 51-1-21, SRM 51-1-26, SRM 51-1-20D, SRM 51-3-1 (TORQUE) WITHIN 17,000 LANDING CYCLES. PERFORM N 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 08FDEA02020 1 20080529 A 5310 507945152 DOOR FRAME BOEING 727 727233 138408A NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 REF SNRM N00174 JPF ITEM NR 1. MAIN DECK, 1L DOOR FRAME IS CRACKED UNDER REMOVED STOP FITTING, AT BOTTOM CROSS BEAM AF T END. REMOVED DAMAGED MATERIAL REF SRM 51-40-02. VERIFIED CRACK REMOVED REF. 727 NDT MAN. PT. 6 51.00-00 FIG 23. NO DEFECTS FOUND. INSTALLED FILLER AND DOUBLER REF SRM 51-40-02 PG. 1 & 2 2 L 7 3 4F RT A3WE 20080716 EA 2008 7 16 COMA0860257 1 20080523 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 7050 FUSELAGE SKIN HAS DAMAGE FROM DOOR PIN AT FWD LOWER POSITION AT FS 310.00. TRIMMED OUT DAMAGE AND INSTALLED REPAIR PART S PER REO 601R53-21-180 AND SR 99-5140-0001. 2 L 7 2 4F RT A21EA 20080715 EU 2008 7 15 08FDEA02159 1 20080604 A 5753 SKIN AIRBUS 310 A310203 3930313 EU TE FLAP MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RT WING OUTBD FLAP UPPER SKIN UNDER RUB STRIP BETWEEN RIB NR 3 AND RIB NR 4 AND 3.6 IN FWD OF REAR SPAR MEASURING 4.4 IN BY 14.2 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND IN STALLED CORRECT OUTER SKIN REPAIR ON RT WING OUTBD FLAP UPPER SKIN BETWEEN RIB NR 3 AND RIB NR 4 IAW A310-200 SRM 57-53- 10, FIG 210. THIS IS AN AIRBUS REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080715 WP 2008 7 15 08FDEA02167 1 20080605 A 5100 NONE DOUG MD10 MD1010F 3022112 WP NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 366FE 46602 REJECTED TAKEOFF FOR WINDSHEAR AURAL ALERT 80 KTS,34 DEG C ,386K FACT 05 JUN08 21:47 AFW U CHECKED PER AMM 05-56-00 AND 05-57-00, ACFT OK FOR SERVICE CHECKED PER AMM 05-56-00 AND 05-57-00, ACFT OK FOR SERVICE. 2 L 7 3 4F RT A22WE 20080715 CE 2008 7 15 MT9A00000034 1 20080513 A 3240 061118000 HOUSING CESSNA 208 208B 2073701 CE RT MLG BRAKE DAMAGED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9623B 208B0138 RT BRAKE CYLINDER HSG WORN AT THE ANCHOR BOLT PASS THROUGH HOLE ALLOWING THE ANCHOR BOLT TO BE PRESSED OUT BY HAND. THIS IS NORMALLY A CLOSE TOLERANCE FIT. THIS CONDITION IN THE PAST HAS CAUSED THE ANCHOR BOLT TO SHEER OFF CAUSING CATASTROF IC DAMAGE TO THE CALIPER ASSY, TORQUE PLATE AND /OR TIRE ON THREE OF OUR AC. (K) 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000017 1 20080508 A 2750 26220919 BELLCRANK CESSNA 208 208B 2073701 CE T/E FLAP CORRODED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9760B 208B0102 THE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE B OLT HOLE THROUGH THE MOUNTING BRACKET, ALSO, THE SLEEVE HAD CORRODED TO THE BELLCRANK. (K) 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000037 1 20080516 A 7921 FLANGE CESSNA 208 208B 2073701 CE OIL COOLER CRACKED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9956B 11668 969 173 208B0119 UPPER MOUNTING FLANGE HAS A 1.5 INCH CRACK AGAINST OIL COOLER BODY. (K) 1 H 7 1 3T A37CE 20080715 NM 2008 7 15 08FDEA02169 1 20080605 A 2910 HYDRAULIC SYSTEM BOEING 727 727233 138408A NM MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION DE DESCENT 1 CE 21 283FE 22350 DURING DESCENT LOST ALL OF SYS A HYD QUANITY PRESSURE WAS NORMAL - 3000 PSI AND NO A.R.E. OR ENG PUMP LOW PRESSURE LIGH TS WERE ILLUMINATED AFTER TEN MINUTES BOTH ENG 1 AND ENG 2 LOW PRESSURE LIGHTS STARTED TO FLASH. TURNED BOTH SYSTEM OF F AT THE PUMP SWITCHES. QUANTITY ZERO, PRESSURE ZERO. REMOVED AND INSPECTED BOTH HYDRAULIC SYSTEM A PRESSURE FILTERS. NO CONTAMINATION FOUND. INSTALLED NEW ELEMENTS. NO LEAKS NOTED. REF AMM 29-11-062-3. ALSO REMOVED AND INSPECTED N R 1 AND NR 2 ENGINE CASE DRAIN FILTERS. NO CONTAMINATION NOTED. INSTALLED NEW ELEMENTS. GROUND RAN ENGINES. NO LEAK S NOTED. 2 L 7 3 4F RT A3WE 20080715 EU 2008 7 15 08FDEA02171 1 20080606 A 5315 A53978267208 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON CROSS BEAM PROFILE C 67RHS. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080715 NM 2008 7 15 08FDEA02176 1 20080606 A 5340 6545313 STRINGER CLIP BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 CORROSION ON STRINGER CLIP AT BS 660, STRINGER, S-1R INSTALLED 1 EA CLIP, NEW CLIP AT STR 1, F/S 660 PER REF SRM 51-30-0 2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 SWAA083467 1 20080623 A 2560 6557463 FITTING BOEING 737 7375H4 138449D NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083471 1 20080623 A 5210 507945 DOOR FRAME BOEING 737 7373G7 1384595 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR LOWER FWD FRAME CRACKED AT FWD CORNER. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083478 1 20080623 A 5743 115A5211 FITTING BOEING 737 7377H4 1384404 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 743SW 29279 DURING SCHEDULED MV2 CHECK, FOUND RIGHT MLG TRUNNION FITTING LUG CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083354 1 20080618 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS740E, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083177 1 20080610 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 SWAA083170 1 20080610 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 DL757080813 1 20080530 A 5313 STRINGER BOEING 757 757232 1384965 NM BS 1700 S23L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 641DL 23995 STR 23L AT STA 1700, FOUND CORROSION. REPAIRED PER SRM 53-00-03 FIG 201. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 08FDEA02406 1 20080624 A 4910 65585417 PANEL BOEING 727 727225 1384077 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 PANEL RACK, UPPER APU PANEL CUTOUT FASTENER HOLE CRACKED/GOUGE FABRICATED NEW PANEL FROM 2024 T-3 .040", APPLIED ALODINE , PRIMER AND PAINT REF DWG 65-58541, SRM 51-10-02 PG 7 AND MM 51-20-151-7 PG 1/2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080716 NE 2008 7 16 COMA0860258 2 20080526 A 7261 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT ENGINE LOW A COMA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 01 451CA 7562 FLIGHT 5531 - RIGHT ENGINE OIL PRESSURE ERRATIC IN FLIGHT AT NORMAL T/O THRUST SETTING. AIRCRAFT RETURNED BACK TO CVG L ANDED SAFELY. FOUND RIGHT ENGINE OIL SERVICED. SERVICED RIGHT ENGINE, GROUND RAN A/C, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 20080716 EU 2008 7 16 08FDEA02049 1 20080530 A 5320 PROFILE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON LONGITUDINAL PROFILE C 67-69,P 45 RT, BCD CUT OUT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 5 1-72-10. 2 L 7 2 4F RT A35EU 20080716 NM 2008 7 16 NWAA082473142 1 20080601 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 342NB 16849 16849 1746 EMERGENCY ESCAPE LIGHTING EPSU LEFT EXIT INOP. REPLACED LEFT EXIT EPSU, CHECKS GOOD. 2 L 7 2 4F RT A28NM 20080716 NM 2008 7 16 ASAA0873019 1 20080516 A 5720 111A11414 WEB BOEING 737 737790 13844CN NM BS 663 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 613AS 30163 BS 663.75 WING CENTER SECTION REAR SPAR LOWER RIGHT WEB (COMPOSITE PANEL) CRACKED. WING CENTER SECTION REAR SPAR AT BS 663.75 LOWER RIGHT WEB CRACK REPAIRED IAW B737 700 SRM 51 70 04 REPAIR NR 10. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 08FDEA02074 1 20080601 A 5312 6582623 BULKHEAD BOEING 727 727233 138408A NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 FWD PANEL RACK: BULKHEAD BS 720 FWD PIT FRAME CORROSION AROUND NUT PLATES (MKD) FABRICATED NEW FRAME ANGLE REF DAD DWG 6 5-82623. TREATED PRIMED RES AMM 51-20-021-7 PG 1-7 51-20-031-7 PG 1-7. MARKED PART REF FEDEX GMM 7-0-1001. THIS IS CL ASSIFIED AS AMINOR REPAIR. 2 L 7 3 4F RT A3WE 20080716 NM 2008 7 16 08FDEA02077 1 20080601 A 5730 113N3500Y28 SKIN PANEL BOEING 757 7572B7 1384964 NM ZONE 600 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 903FD 27124 RIGHT WING T/E O/B FLAP NOSE SKIN TOP SIDE HAS GOUGE. REMOVED RIGHT WING T/E FLAP NOSE SKIN IAW SRM 51-40-02. RECEIVED NEW PART P/N 113N3500Y28. INSTALLED NEW SKIN IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 20080716 EU 2008 7 16 08FDEA02092 1 20080528 A 5730 A57350103201 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 LT WING, WING TOP SKIN FOUND WITH CORROSION NEXT TO REAR SPAR, BETWEEN RIBS 27 AND 28. REPAIRED AS PER EA 6-5710-121647 . 2 L 7 2 4F RT A35EU 20080716 EU 2008 7 16 08FDEA02046 1 20080530 A 5310 A53973057202 DOOR FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON BULK CARGO DOOR CUT OUT C 67 -69, P 44-48 RT ON SECTION BEAM. REPAIR PERFORMED BY REPLACEMENT OF PAR T IAW SRM 51-72-10 2 L 7 2 4F RT A35EU 20080716 EU 2008 7 16 08FDEA02047 1 20080530 A 5310 A53973264202 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU DOOR SEAL CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON BULK CARGO DOOR CUT OUT C 67-69, P 44-48 RT ON SEALING SECTION REPAIR PERFORMED BY REPLACEMENT OF PAR T IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080716 WP 2008 7 16 UPS08852364 1 20080526 A 3350 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. EMERGENCY LIGHT SYSTEM OPS CKS GOOD PER MM 33-50-02-2. 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 UPS08M52355 1 20080410 A 5730 SKIN DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C LEFT WING L/E FIXED WING AFT SKIN APPROX STA XORS 522 FOUND CRACKED (2478). ATTACHED RIBS 2 EA REMOVE D. INNER SKIN BEADED SKIN TRIM OFF. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. THREE EA REPAIR ANGLES, R EPAIR DOUBLERS & FILLER FAB, 3 EA ANGLES HEAT TREATED. REPAIR PARTS HOLES PICKED UP AND PAINTED. REPAIR ANGLES 3 EA, D OUBLER, FILLER & ATTACHED PARTS INSTALLED AS PER SRM 57-10-00VI FIG 27 R40. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 UPS08M52356 1 20080404 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C LEFT WING FUEL TANK LOWER NR 41 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 8.5 IN CH. LEFT WING NR 41 STRINGER END SPLICE REMOVED, ATTACHED CLIP & FASTENERS REMOVED. SLOT OUT CRACKED AREA C/O. HFEC I NSP C/O ON REWK AREA, FOUND NO CRACK EVIDENT. REPAIR ARROW HEAD FITTING FAB, FPI C/O & FOUND NO CRACK EVIDENT. REPAIR ARROWHEAD FITTING & ATTACH CLIP INSTALLED. SEALANT APPLIED ON STR 41 REPAIR AREA. LEAK CHECK OK. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 AALA200801294 1 20080512 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 758AN 32637 DFW - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080716 NM 2008 7 16 UPS08M52365 1 20080524 A 3350 LIGHT DOUG MD11 MD11F 3023600 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 292UP 48475 INSPECTION TYPE:N/A 2 BULBS NOT ILLUMINATED OVER LT ENTRANCE DOOR DURING EMERGENCY LIGHT TEST. RELAMPED EMERGENCY LIGHT S, OPS CHECK NORMAL. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 2008UALA02981 1 20080525 A 7500 CONTROLLER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT ENGINE BLEED FAULTY A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 785UA 26954 LEFT ENGINE BLEED INOP IN FLIGHT. SUSPECT FAULTY HIGH PRESSURE FAN AIR CONTROLLER. REPLACED LT HPFAC RAN BOTH ENGINES . OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080716 NM 2008 7 16 2008UALA02987 1 20080524 A 5320 FITTING BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 FOUND CRACKED CLIP AT STA 301.5 AND STRINGER 10L. MAJOR REPAIR ACCOMPLISHED: REPLACED CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 20080714 NM 2008 7 14 ASAA0843101 1 20080610 A 5310 65C327748 BEAM BOEING 737 7374Q8 138447Q NM BS 616 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 RT SIDE BS 616 STUB BEAM CHORD CRACKED AT FASTENER HOLE. REPAIRED STUB BEAM CHORD IAW EO5310 02528 SECTION 6. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 08FDEA02450 1 20080625 A 5280 6517563159 RIB BOEING 727 727225 1384077 NM NLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 NLG LEFT FWD LEFT DOOR, CRACK IN AFT SIDE FRAME AT O/B STOP FITTING LOWER 2 FASTENERS FOR INNER SUPPORT. REPAIRED NLG DOOR REF SRM 51-40-3 PG 1-6. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080714 EU 2008 7 14 08FDEA02451 1 20080620 A 5340 A5361076120495 ATTACH FITTING AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 BS 1091, RT OUTBD FRAME TO FLOORBEAM AFT ATTACH LINK CRACKED UPPER SURFACE. LINK WAS REPLACED ON E.O. 6-5340-7-5002 PT 5. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 ASAA0843103 1 20080521 A 5330 65C323592 SKIN BOEING 737 7374Q8 138447Q NM BS 500 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 DENTS AT LT LOWER EXTERIOR AT BS 500 STR 26 TO 27L. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 20080714 NM 2008 7 14 08FDEA02458 1 20080625 A 2750 BCREF0074 CONTROL CABLE BOEING 727 727227 1384078 NM ZONE 500 TWISTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 OUTBOARD FLAP TRANSMITTER CABLE TWISTED AROUND (2 EACH) LT WING SPOILER CABLES. RE-ROUTED LT O/B FLAP TRANSMITTER CABLE WHICH WAS WRAPPED AROUND 2 EACH SPOILER CABLES IAW MM 27-52-013-4. NO DEFECTS NOTED TO SPOILER OR FLAP TRANSMITTER CAB LE. OPS CHECK GOOD IAW MM 27-51-000-5 AND 27-61-000-5. 2 L 7 3 4F A3WE 20080714 NE 2008 7 14 DL76L080849 2 20080610 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 FIRE A DALA E ENGINE SHUTDOWN B A SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 185DN 64883 27961 724147 ON TAXI IN RIGHT ENG WAS SHUTDOWN, GRND TOLD US SMOKE AND MECHANIC CONFIRMED SMOKE AND FLAMES FROM LEFT ENG TAILPIPE. S ECURED LEFT ENG AND MOTORED ENG FOR TWO MINUTES. NO COCKPIT INDICATIONS OR HIGH EGT NOTED PRIOR TO SMOKE ANNOUNCEMENT. PERFORMED FIM PROCEDURES 71-08-00 FIG 117, ALL OK. PERFORMED AMM 70-11-11-912-018-N00, NO ABNORMALTIES FOUND ALLOK. P ERFORMED TEST RUN ON LT ENGINE TWICE ALL OK. ALL PARAMETERS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20080714 EU 2008 7 14 08FDEA02316 1 20080618 A 5730 A5797130100000 SKIN AIRBUS 310 A310203 3930313 EU ZONE 500 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING O/B FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB 2 AND FLAP TR ACK NR 3 MEASURING 6 INCH BY 5 INCH. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED AN APPROVE D REPAIR ON LEFT WING O/B FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB 2 AND FLAP TRACK NR 3 IAW FEDEX EA6-5750-1212 98. THIS IS AN APPROVED REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 NOCA04408 1 20080528 A 5320 146T353416 MOUNT FITTING BOEING 767 76739H 1385311 NM FUSELAGE CORRODED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 760NA 26257 INSIDE BULK CARGO BELOW FLOOR AT HEATED DRAIN LINE BOX AREA BETWEEN STR 36R-35R AT STA 1417-1395 HAS LEVEL 2 CORROSION. REPLACED DRAIN MOUNT PLATES AND BRACKETS IAW 51-10-02. 2 L 7 2 4F RT A1NM 20080715 NM 2008 7 15 08FDEA02324 1 20080619 A 5314 144N8140Y45 KEELBEAM BOEING 757 75723A 1384967 NM BS 1000 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 LWR FUSELAGE KEEL BEAM AREA, CORROSION ON CENTER SUPPORT FRAME AT BS1000. CORROSION FOUND EXCEED ALLOWABLE LIMITS IN B7 57-200 SRM 53-0071 FIG 101 DETAIL VII. REMOVED AND REPLACED TEE CHORD IAW B757-200 SRM 51-40-02 REV.93. REPAIR IS CL ASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 08FDEA02336 1 20080619 A 5730 ARB74023 SKIN DOUG MD11 MD11F 3023600 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 02 EACH FASTENER HOLES FOUND CRACK INDICATIONS DURING OPEN-HOLE HFEC INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CU TOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. CARRIED OUT REPAIR AS PER EA 1-5710-122496 PART 1. THIS REPA IR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 08FDEA01967 1 20080523 A 5330 2024T30090 SKIN BOEING 757 75723A 1384967 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 EXTERNAL PATCH REPAIR ON FUSELAGE FROM BS 1416 TO BS 1446, BETWEEN S-26R AND S-28R (REAR LOWER CORNER OF AFT CARGO DOOR CUTOUT), TO BE EVALUATED. EXISTING REPAIR EVALUATED AS PER EO F-5100-7-5001 PT 1 ATTACHMENT B, AND FOUND PREVIOUSLY ACCO MPLISHED IAW BOEING TELEX NO: GUE-MAN-03-00089H WITH FAA FORM 8110-3. LFEC INSPECTION REQUIRED AT EVERY 3,000 FC INTERV AL AFTER AIRFRAME ACCUMULATED 50,000 FC. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080715 WP 2008 7 15 08FDEA02286 1 20080617 A 5347 NFA6022 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 MAIN CABIN DAMAGED HOLES ON SEAT TRACK. 2 L 7 3 4F A22WE 20080715 2008 7 15 USA2008F00005 4 20080615 A 2565 D30656126 SLIDE BOEING 757 7572B7 1384964 NM R4 DOOR LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 37537 507 27809 PHL - THE R4 DOOR EMERGENCY ESCAPE SLIDE PRESSURE WAS IN THE RED ZONE. MAINTENANCE REPLACED THE R4 DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. (K) 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 USAA920081208 1 20080611 A 5330 6552988 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 458UW 25022 CLT - MAJOR REPAIR - RON - NR 4391327, FUSELAGE SKIN CRACKED, BS 942 ABOVE S24L. REPAIRED FUSELAGE SKIN AT BS 942 ABOVE S24L IAW EA 100522 AND SRM 51-10-01. (K) 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 USAA920081215 1 20080529 A 5320 STRAP BOEING 757 7572B7 1384964 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 929UW 27144 BFM - C2 - MAJOR REPAIR - TASK CARD 19C11053005 -FLOOR SUPPORT STABILIZER STRAP CRACKED AT BS 365.25 - 377.7, LBL 25. R EPAIRED FLOOR SUPPORT STABILIZER STRAP AT BS 365.25 - BS 377.7, LBL 25 IAW SRM 51-40-02 AND 53-35-01. (K) 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 USAA920081241 1 20080609 A 5312 6517583112 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN - C-21 - MAJOR REPAIR - NR 6110566 - CRACK ON VERTICAL BEAM WEB AT LINING RETAINER HOLE BS 178, WL 177, RBL 5.7. RE PAIRED VERTICAL BEAM WEB AT LINING RETAINER HOLE BS 178, WL 177, IAW SRM 53-10-08-2R 12. (K) 2 L 7 2 4F RT A16WE 20080715 EU 2008 7 15 08FDEA02170 1 20080606 A 5320 A53974220216 WEB AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON WEB C 64, P56-56`. REPAIR PERFROMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080715 WP 2008 7 15 08FDEA02177 1 20080606 A 5720 ARB1066 ANGLE DOUG DC10 DC1010 3022110 WP LT WING TIP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 LT WING L/E, FOUND 1 CRACK 1" LONG ON ANGLE INT WING TIP. REPAIR ANGLE IAW SRM 57-00-01 VOL.1 FIG.10 SHT 1. 2 L 7 3 4F A22WE 20080715 WP 2008 7 15 08FDEA02178 1 20080606 A 5512 NLC6025 PANEL DOUG DC10 DC1010 3022110 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 40061 46973 LT HORIZONTAL STABILIZER 1 DENT AND 1 CRACK, LONG .25 INCH ON UPPER SKIN PANEL, FROM STA XE 67 TO STA XE 73. REPAIR PAN EL IAW SRM 55-00-01 VOL 1 FIG 3 SHEET 2. 2 L 7 3 4F A22WE 20080715 WP 2008 7 15 08FDEA02179 1 20080606 A 5330 AEA01121 SKIN DOUG DC10 DC1010 3022110 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 MAIN CABIN, CRACK 1.5 INCH LONG ON WEB ON AFT L3 JAMB AT STA 1306 BETWEEN L23 AND L27 LT SIDE. REPAIR JAMB IAW SRM 53-5 0-00 FIG 19 SHEET 2, 3 AND 6 VOL 1. 2 L 7 3 4F A22WE 20080715 CE 2008 7 15 MT9A00000004 1 20080404 A 2750 26220911 BELLCRANK CESSNA 208 208B 2073701 CE T/E FLAP DAMAGED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9331B 208B0055 THE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE B OLT HOLE THROUGH THE MOUNTING BRACKET. (K) 1 H 7 1 3T A37CE 20080715 WP 2008 7 15 08FDEA02183 1 20080606 A 5320 AYK701415 SUPPORT DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 THE CENTER LANDING GEAR WELL/SPACE INTERIOR, FWD BULKHEAD RIGHT UPPER CORNER AREA HAS A HYDRAULIC LINE SUPPORT BRACKET THAT IS CRACKED. REMOVED THE SUPPORT BRACKET IAW DC/MD-10 SRM 51-35-01; VOL II. MATERIAL ID 6061-T6, 0.063 IAW DC/MD- 10 DWG AYK7014, REV BF. FABRICATED A NEW SUPPORT BRACKET IAW DC/MD-10 DWG AK7014, REV BF. ALODINED AND PRIMED IAW DC/M D-10 SRM 51-21-01; VOL II. INSTALLED THE SUPPORT BRACKET IAW DC/MD-10 SRM 51-33-01; VOL II. 2 L 7 3 4F RT A22WE 20080715 CE 2008 7 15 MT9A00000005 1 20080508 A 2750 MS276404 BEARING CESSNA 208 208B 2073701 CE BELLCRANK CORRODED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9331B 208B0055 THE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K) 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000006 1 20080409 A 2750 BEARING CESSNA 208 208B 2073701 CE CORRODED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9331B 208B0055 THE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K) 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000011 1 20080423 A 2750 262208315 BELLCRANK CESSNA 208 208 2073702 CE T/E FLAP DAMAGED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9653F 20800114 THE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET. (K) 1 H 7 1 3T NT A37CE 20080715 EU 2008 7 15 08FDEA02146 1 20080604 A 5753 SKIN AIRBUS 310 A310203 3930313 EU ZONE 500 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING OUTBOARD FLAP UPPER MAIN RUB STRIP BETWEEN RIB 4 AND RIB 5, MEASUR ING 6.9 IN BY 13.0 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT OUTER SKIN REPAI R ON LT WING OUTBD FLAP UPPER RUB STRIP IAW A310-200 SRM 57-53-12, FIG 210, BETWEEN RIB NR 4 AND RIB NR 5. THIS IS AN A IRBUS REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080715 CE 2008 7 15 MT9A00000014 1 20080505 A 2750 MS276404 BEARING CESSNA 208 208B 2073701 CE T/E FLAP CORRODED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 4602B 208B0140 THE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K) 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000015 1 20080505 A 2750 26220831 BELLCRANK CESSNA 208 208B 2073701 CE T/E FLAP CORRODED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 4602B 208B0140 THE SEALED BEARING WAS CORRODED AND FROZEN. ALSO, THE BEARING WAS CORRODED TO THE BOLT. (K) 1 H 7 1 3T A37CE 20080715 EU 2008 7 15 08FDEA02192 1 20080607 A 5313 A5381136920200 STRINGER AIRBUS 300 A300B4622 3930401 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 719FD 388 AIRCON BAY AT BILGE AREA BETWEEN FR 41 AND 42 STR 51R HAS CORROSION, BELOW WATER SEPARATOR. REMOVED AND REPLACED STR 51R IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080715 CE 2008 7 15 MT9A00000025 1 20080512 A 3240 06111800 HOUSING CESSNA 208 208B 2073701 CE BRAKE DAMAGED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9331B 208B0055 BRAKE CYLINDER HOUSING WORN AT THE ANCHOR BOLT PASS THROUGH HOLE ALLOWING THE ANCHOR BOLT TO BE PRESSED OUT BY HAND. THI S IS NORMALLY A CLOSE TOLERANCE FIT. THIS CONDITION IN THE PAST HAS CAUSED THE ANCHOR BOLT TO SHEER OFF CAUSING CASTASTR OPHIC DAMAGE TO THE CALIPER ASSEMBLY, TORQUE PLATE AND/OR TIRE ON THREE OF OUR AC. (K) 1 H 7 1 3T A37CE 20080715 NM 2008 7 15 08FDEA02195 1 20080607 A 5320 65585684 THRESHOLD BOEING 727 727227 1384078 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 RIGHT AFT SERVICE DOOR THRESHOLD CRACKED NEAR STOP PAD. SENT TO SHOP FOR WELD ON NR N00707, THRESHOLD WILL GET INSTALLE D ON CLOSE CARD 72C201-01. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080715 NM 2008 7 15 08FDEA02202 1 20080609 A 5311 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 624FE 48443 CABIN RT TRANSVERSE FRAME AT STA 1681 FOUND DENTED AT LONGERON 12. 2 L 7 3 4F RT A22WE 2008041800214 20080418 00214 EU 2008 4 18 08FDEA01427 1 20080416 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 445FE 297 PREVIOUS REPAIR LOCATED ON MAIN CABIN SEAT TRACK NR 4 RT -Y1456 BETWEEN FRAMES 62 TO 63, HAS 2 EACH REPAIR SPLICES MEASU RING 7 IN LONG BY 3 IN TALL AND 1 REPAIR SECTION 52 IN LONG FROM FRAME 65 TO BETWEEN FRAMES 62 AND 63. REPAIR NOT IAW S RM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT REPAIR IAW A310 SRM SUPPLEMENT 53-10-16, FIG 202, PG 209 /210. THIS IS AN AIRBUS REPAIR WITH NO ASSIGNED PART NUMBER AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 2008041800218 20080418 00218 NM 2008 4 18 F3LA2008179 1 20080417 A 3350 BULB AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE EMERGENCY LIGHT INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 905FR 10 1583 DURING PRE FLIGHT INSPECTION, THE FLIGHT CREW REPORTED SEAT ROWS 9 AND 22 HAD ONE SEGMENT OF LIGHTS FOUND BURNED OUT DUR ING PRE FLIGHT TEST. MAINTENANCE REMOVED AND REPLACED ONE BULB FROM ROW 22 IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 3 1-51-00 AND DEFERRED EMERGENCY LIGHT IN ACCORDANCE WITH THE REQUIREMNTS OF MEL 33-50-03A. 2 L 7 2 4F 4 F RT A28NM E37NE 2008041800221 20080418 00221 NM 2008 4 18 HALA08000527 1 20080413 A 2130 1305027 SELECTOR PANEL BOEING 767 7673CB 1385187 NM CABIN PRESSURE FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 588HA 33466 ATB - BOTH CABIN PRESS AUTO SYSTEMS FAILED, MANUAL MODE OPERATED OK. PERFORMED FIM 21-31-00. REPLACED CABIN PRESSURE S ELECTOR PANEL PER AMM21-31-01. CHECKED OK, NO DEFECTS NOTED. 2 L 7 2 4F RT A1NM 2008041800222 20080418 00222 NM 2008 4 18 UIEA200800142 1 20080408 A 5311 FRAME BOEING 747 747243B 1384830 NM ZONE 200 DEFORMED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK STA 1840 STRINGER 12R - 13R FRAME FOUND DEFORMED. FRAME REPAIRED PER ATLAS EO NR 4753A141. 2 L 7 4 4F RT A20WE 2008041800223 20080418 00223 NM 2008 4 18 UIEA200800143 1 20080408 A 5311 FRAME BOEING 747 747243B 1384830 NM ZONE 200 DEFORMED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK STA 1860 STRINGER 12R FRAME FOUND DEFORMED. FRAME REPAIRED PER ATLAS EO NR 4753B141. 2 L 7 4 4F RT A20WE 2008041800228 20080418 00228 NM 2008 4 18 UIEA200800158 1 20080414 A 5755 SKIN BOEING 747 7472D7B 1384803 NM SPOILER DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 RIGHT WING NR 7 GROUND SPOILER HAS SIGNS OF DELAMINATION. REPAIRED IAW SRM 57-40-24 AND 51-40-20, AND EO NR 4757A429. 2 L 7 4 4F RT A20WE 2008041800248 20080418 00248 NM 2008 4 18 USAA920080869 1 20080412 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 23379 A 1.25 INCH CRACK ON FUSELAGE SKIN AT BS 727D + 17" - 18", S23R. INSTALLED DOUBLER REPAIR IAW SRM 53-00-01 REPAIR 3 FIG 201. 2 L 7 2 4F RT A16WE 2008041800266 20080418 00266 EA 2008 4 18 A6WA200840216 1 20080312 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 440AW 7766 CRACKS FOUND ON FS 280 RBL 9 ON FLOOR STRUCTURE. REPAIRED IAW REO 601R-53-11-1366 REV A. (M) 2 L 7 2 4F RT A21EA 2008041800267 20080418 00267 NM 2008 4 18 2008UALA02055 1 20080410 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 809UA 825 FOUND BEAM 160 CORRODED WHILE ACCOMPLISHING EQ3700 CALLOUT. REPLACED BEAM 160 WITH NEW BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041800268 20080418 00268 EU 2008 4 18 2008UALA02056 1 20080409 A 3350 F100034200 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 446UA 834 EMERGENCY EXIT ROW LIGHT COVER MISSING AT MID CABIN, ROW SIDE ABC. REPLACED LENS COVER. 2 L 7 2 4F 4 F RT A28NM E40NE 2008041800269 20080418 00269 NM 2008 4 18 2008UALA02057 1 20080409 A 5340 ATTACH FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 348 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 FUSELAGE LT SIDE AT BS 348 AND STRINGER 16L INTERCOSTAL CLIP IS MISDRILLED. MAJOR REPAIR ACCOMPLISHED, REMOVED AND REPL ACED INTERCOSTAL CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041800276 20080418 00276 SO 2008 4 18 C2XA08CL050 1 20080412 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14972 6726 145151 DURING ROUTINE MAINTENANCE THE NR 3 EMERGENCY LIGHT BATTERY WOULD NOT HOLD A CHARGE. MAINTENANCE INSPECTED AND REPLACED THE NR 3 EMERGENCY LIGHT BATTERY. 2 L 7 2 4T RT T00011AT 2008041800319 20080418 00319 NM 2008 4 18 USAA920080836 1 20080331 A 5753 6546431286 SKIN BOEING 737 73733A 1384673 NM FOREFLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 23634 CLT - MAJOR REPAIR - C22 CHECK - A 2.25" X 1.75" AREA OF DELAMINATION ON RIGHT O/B TRAILING EDGE FOREFLAP ON TOP SURFACE . INSTALLED REPAIR IAW SRM 51-70-10 REPAIR 3 AND 4. 2 L 7 2 4F RT A16WE 2008041800320 20080418 00320 NM 2008 4 18 USAA920080837 1 20080402 A 5754 65C2660399A SKIN BOEING 737 73733A 1384673 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 23634 CLT - MAJOR REPAIR - C22 CHECK - NR 3 SLAT HAS 3 EACH CRACKS STARTING FROM RIVET HEADS ON LOWER SURFACE TRAILING EDGE. INSTALLED REPAIR IAW SRM 57-43-01-2 R6 AND 51-40-02. 2 L 7 2 4F RT A16WE 2008042300294 20080423 00294 NM 2008 4 23 2008UALA02152 1 20080413 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 198UA 28716 AT SEAT 32C, WIRES TO SEAT EMERGENCY PATH LIGHT BROKEN. FOUND BROKEN WIRES TO LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY. A C OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300295 20080423 00295 NM 2008 4 23 2008UALA02153 1 20080411 A 2697 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SMOKE DETECTOR DETERIORATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 "R" LAV SMOKE DETECTOR WIRE DETERIORATED. REPLACED BOTH WIRES FOR SMOKE DETECTOR IN "R" LAV. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300297 20080423 00297 NM 2008 4 23 2008UALA02155 1 20080411 A 5210 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 DOOR 2L UPPER HINGE ARM CUT OUT REQUIRES DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. ACCMP'D H FEC. PERFORMED INSURANCE CUT. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300298 20080423 00298 NE 2008 4 23 BB08064 2 20080417 A 7310 FUEL FILTER BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE ZONE 400 CLOGGED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 201UU 27810 31306 BFM - FLT 9244 BFM TO PHL - RECEIVED "RT FUEL FILTER" EICAS MESSAGE ON TAKEOFF. FLIGHT RETURNED TO FIELD AND LANDED WI THOUT FURTHER INCIDENT. MAINTENANCE REPLACED RIGHT ENGINE FUEL FILTER. OPERATIONALLY AND LEAK CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E12EU 2008042300300 20080423 00300 NM 2008 4 23 SWAA081987 1 20080413 A 5311 6546596 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300301 20080423 00301 NM 2008 4 23 SWAA081980 1 20080413 A 5311 6546525 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300310 20080423 00310 NM 2008 4 23 SWAA081954 1 20080410 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED MV2 CHECK, FOUND RIGHT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008042300311 20080423 00311 NM 2008 4 23 SWAA081955 1 20080410 A 5330 65C357781 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300312 20080423 00312 2008 4 23 SWAA081956 4 20080410 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042300315 20080423 00315 NM 2008 4 23 SWAA081974 1 20080413 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042300324 20080423 00324 NM 2008 4 23 RYNA200800002 1 20080329 A 5610 5893543139 WINDSHIELD BOEING 737 73786N 13844CD NM COCKPIT CRACKED A RYNA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 07 DJT 28592 CAPTAIN'S WINDSHIELD (L1 WINDSHIELD) CRACKED ON THE OUTER LAYER. REPLACED CAPTAIN'S WINDSHIELD AND HEAT CONTROLLER IAW AMM 56-11-11 & AMM 30-41-11, OPS CHECKED NORMAL. 2 L 7 2 4F RT A16WE 2008042300325 20080423 00325 EU 2008 4 23 MAC040802 1 20080409 A 5751 S5761006000200 FITTING AEROSP ATR42 ATR42300 8680920 EU RT AILERON CORRODED A MTNA K NONE O OTHER IN INSP/MAINT 1 EA 68 909FX 275 DURING INSPECTION LEVEL 2 EXFOLIATION CORROSION WAS FOUND ALONG EDGE OF BEARING OUTER FITTING I/B ON THE RT AILERON OUTB OARD HINGE/SHACKLE ASSEMBLY. THE BEARING OUTER HINGE WAS REPLACED. INSPECTION REASON: MRB 576108-01REFERENCE ATR 42 SRM 57-61-10 P115-116 FIG 1. 2 H 7 2 4T RT A53EU 2008042300326 20080423 00326 EU 2008 4 23 MAC040803 1 20080409 A 5751 TEE FITTING AEROSP AEROSP ATR42 ATR42300 8680920 EU LT AILERON CORRODED A MTNA K NONE O OTHER IN INSP/MAINT 1 EA 68 909FX NT1235 275 DURING INSPECTION LEVEL 2 CORROSION WAS FOUND ON THE AILERON "TEE PICKUPS" (TEE CLIPS) ON THE LEFT AILERON ASSEMBLY. TH E EXFOLIATION CORROSION WAS ALONG THE EDGES AND SIDES OF THE FITTINGS. REFERENCE: ATR 42 SRM 57-61-10 P 115/116 FIG 1. REASON FOR INSPECTION MRB 576108-01. 2 H 7 2 4T RT A53EU 2008042300328 20080423 00328 NM 2008 4 23 SWAA081990 1 20080414 A 5753 6546430100 SKIN BOEING 737 7373K2 13844BA NM FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED MV2 CHECK, FOUND RIGHT WING INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 2008042300334 20080423 00334 NM 2008 4 23 SWAA081999 1 20080414 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300335 20080423 00335 NM 2008 4 23 SWAA082001 1 20080414 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300336 20080423 00336 NM 2008 4 23 SWAA082000 1 20080414 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300338 20080423 00338 NM 2008 4 23 SWAA082008 1 20080414 A 5753 6549456 FITTING BOEING 737 7373H4 1384600 NM FLAP TRACK CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED BRDG CHECK, FOUND LEFT WING NR 2 FLAP TRACK AFT SPAR FITTING CORRODED. REMOVED AND REPLACED FITTING PE R SRM. 2 L 7 2 4F RT A16WE 2008042300350 20080423 00350 NM 2008 4 23 SWAA082006 1 20080414 A 5743 115A5211 FITTING BOEING 737 7377AD 1384502 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 798SW 28436 DURING SCHEDULED MV2 CHECK, FOUND LEFT MLG FWD TRUNNION LUG FITTING CORRODED. REMOVED AND REPLACED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300365 20080423 00365 NM 2008 4 23 SWAA082016 1 20080415 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED MV1 CHECK, FOUND AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 2008042300366 20080423 00366 2008 4 23 SWAA082017 4 20080415 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 2008042300367 20080423 00367 NM 2008 4 23 SWAA082018 1 20080415 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 482A, RBL 5 TO LBL 5. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008042300370 20080423 00370 NM 2008 4 23 SWAA082024 1 20080415 A 5330 6545776 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 979, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042300374 20080423 00374 EU 2008 4 23 MAC040801 1 20080411 A 2913 8210181 PUMP PWA AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE NR 2 ENGINE CRACKED A MTNA E B ENGINE SHUTDOWN EMER. DESCENT K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 68 811FX 2679 124438 283 PCE124519 DURING FLT (MIA-KIN) 5NM FROM KIN THE NR 2 ENG OIL PRESSURE DROPPED TO ZERO WITH CAP WARNING "ENG OIL" AND CRC. THE ENG WAS SHUTDOWN AND THE PIC DECLARED AN EMERGENCY. UPON INSP AFTER LANDING, THE COWLING WAS COVERED WITH OIL. AN OVERSPE ED HYDRAULIC PUMP HAS BEEN DETERMINED TO BE THE CAUSE FOR THE LOSS OF ENG OIL. 2 H 7 2 4T 4 T RT A53EU E2ONE 2008042300375 20080423 00375 NM 2008 4 23 CALA0800333 1 20080407 A 5320 65C333671 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 CORROSION ON INTERCOSTAL BETWEEN BS 947.5 TO BS 967 AT LBL 52", DRAIN GOES THROUGH THIS INTERCOSTAL. REMOVED AND REPLAC ED INTERCOSTAL REF 737-500 SRM 51-40-02; LOCATED BETWEEN BS 947.5 & 967 AT LBL 52. 2 L 7 2 4F RT A16WE 2008042300378 20080423 00378 NM 2008 4 23 SWAA082030 1 20080416 A 5330 65C381921 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 501C, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300392 20080423 00392 NM 2008 4 23 2008UALA02257 1 20080416 A 5320 SILL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE AFT CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 AFT CARGO DOOR SILL PLATE HAS 2 CRACKS FIRST CRACK IS ONE INCH LONG, 28 INCHES FROM FWD EDGE. SECOND CRACK IS .750 LONG FOUR INCHES BEHIND FIRST CRACK. REMOVED CRACKED SILL BULLNOSE AND REPAIRED. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042300394 20080423 00394 NM 2008 4 23 SWAA082041 1 20080416 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 739GB 29275 DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 11 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 2008042300395 20080423 00395 NM 2008 4 23 SWAA082042 1 20080416 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 739GB 29275 DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042300397 20080423 00397 NM 2008 4 23 SWAA082060 1 20080417 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 2008042300399 20080423 00399 NM 2008 4 23 SWAA082062 1 20080417 A 5514 65C25170 FITTING BOEING 737 7373H4 1384600 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND LEFT HORIZONTAL STABILIZER CENTER SECTION FITTING BEARING HOUSING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300403 20080423 00403 NM 2008 4 23 SWAA082048 1 20080417 A 5311 6516302 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008042300406 20080423 00406 NM 2008 4 23 SWAA082052 1 20080417 A 5311 6546560 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947, STR 18R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008042400002 20080424 00002 EU 2008 4 24 08FDEA01470 1 20080422 A 4900 A5247133600200 DRAIN MAST AIRBUS 300 A300F4605R 3930327 EU APU BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 APU DRAIN MAST RIGHT UPPER FLANGE IS BENT AND THE MAST IS DENTED AND BENT. REMOVED AND REPLACED THE DRAIN MAST IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008042400004 20080424 00004 EU 2008 4 24 08FDEA01472 1 20080422 A 5230 A5397822420051 RETAINER AIRBUS 300 A300F4605R 3930327 EU CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 661FE 760 AFT CARGO DOOR AFT CUTOUT; PRESSURE SEAL DEPRESSOR IS GOUGED FROM TOP TO BOTTOM. REMOVED AND REPLACED THE DAMAGED SEAL DEPRESSOR IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008042400011 20080424 00011 WP 2008 4 24 DHLA200800040 1 20080417 A 2697 CONNECTOR DOUG DC8 DC873 302199C WP NR 2 ENGINE CONTAMINATED A DHLA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 05 873SJ 46091 FLIGHT 445, NR 2 FIRE LIGHT ILLUMINATED ADHERED TO THE ENGINE FIRE EMERGENCY PROCEDURE FIRE LIGHT STILL REMAIN ILLUMINAT ED. FOUND OIL IN CONNECTOR FIRELOOP AT FAN SECTION RT. CLEANED LA 26195. FOUND INDICATION ONLY NO OTHER CAUSE, FIRELO OP SYSTEM CKD NORMAL IAW MM 26-10-0. AIRCRAFT WAS GROUNDED. 2 L 7 4 4F RT 4A25 2008042400024 20080424 00024 NM 2008 4 24 2008UALA02164 1 20080414 A 5710 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT WING LE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 CRACK INDICATION UNDER FLAKING TEFLON PAINT ON UPPER SURFACE OF THE RT WING FIXED LEADING EDGE BELOW NR 10 SLAT. REMOVE D DAMAGED AREA APPLIED A PRE-PREG FIBERGLASS REPAIR IAW SRM 57-41-01 AND 51-70-07 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400025 20080424 00025 NM 2008 4 24 2008UALA02165 1 20080414 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1480 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 AFT PIT STA 1480, STR 26L FRAME DENTED. AFT PIT STA 1480, STR 26L FRAME DENTED. REPAIRED FRAME DENTS IAW S RM 53-00-07 RPR 5 TABLE II ZONE 1.THIS REPAIR MUST BE REINSPECT ED STARTING AT 50000 TOTAL FLIGHT CYCLES AND 12000FC THERE AFTER . 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400027 20080424 00027 NM 2008 4 24 2008UALA02167 1 20080415 A 2121 6454051 FAN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN FAILED A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 307UA 23668 SMOKE COCKPIT CABIN, ELECTRICAL BURNING ODOR, RIGHT PACK TRIP OFF LIGHT ALL DURING ENGINE STARTS. FOUND CABIN RE-CIRCULA TION FAN FAILED. REPLACED CABIN RE-CIRCULATION FAN. BEARINGS DRY AND UNIT DIRTY. CLEANED UNIT AND REPLACED BEARINGS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042400031 20080424 00031 NM 2008 4 24 2008UALA02172 1 20080414 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EXTERIOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 851UA 1664 EMERGENCY EXIT LIGHT ON EXTERIOR OF FIRST CLASS CLOSET IS LOOSE. SECURED EXIT LIGHT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042400032 20080424 00032 NM 2008 4 24 2008UALA02173 1 20080414 A 4900 380029817 APU BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE SHUTDOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 671UA 30026 APU SHUT DOWN ON ITS OWN AT THE GATE. FOUND METAL IN OIL FILTER AND CHIP DETECTOR. REPLACED APU. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042400033 20080424 00033 NM 2008 4 24 UPS08552036 1 20080412 A 5330 SKIN BOEING 757 75724APF 1384969 NM BS 261 S24 PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 467UP 25483 LARGE PUNCTURE AND GOUGE 13.75 BY 3.75 AT LT NOSE BS 261 STRINGER 24L/STR 21 LAP SEAM. DEEP GOUGE CONTINUES FORWARD TO BS 253. 1.25 INCH DIAMETER PUNCTURE AND 3.25 GOUGE 5 INCHES ABOVE STR 24L BETWEEN BS 239L AND 247L. CUT OUT DAMAGED SKI N PER SRM 53-00-01. HFEC PERFORMED. C/W EO B757-5330-29012 PG 2, STEPS 2,4,5. FABBED DOUBLER BELOW LAP. INSTALLED FA STENERS. ALODINED, SEALED AND PRIMED DOUBLER EXTERIOR IAW EO B757-5330-29012. FINAL TOP COAT APPLIED PER EO B757-5330- 29012. 2 L 7 2 4F RT A2NM 2008042400035 20080424 00035 WP 2008 4 24 UPS08852020 1 20080408 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING TIP DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C1 3 SCREWS PULLING THRU SKIN BOTTOM OF RT WING TIP. REMOVED SCREWS, FABBED AND INSTALLED REPAIR DOUBLE R. REINSTALLED SCREWS IAW SRM 51-3-0, 57-3-3 FIG 23, 51-1-8,51-1-21A, 51-1-11. 2 L 7 4 4F RT 4A25 2008042400039 20080424 00039 SW 2008 4 24 WGEA200800055 1 20080415 A 2721 271127521004 ACTUATOR ECLIPS EA500 ECLIPSEEA500 3350000 SW RUDDER TRIM MALFUNCTIONED E WGEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 EA 27 150DJ 193 000062 MOMENTARY APPLICATION OF RIGHT RUDDER TRIM RESULTED IN TRIM RUNNING AWAY FULL RIGHT. UNABLE TO GET ANY FURTHER TRIM MOV EMENT. REMOVED AND INSTALLED NEW RUDDER TRIM ACTUATOR IAW EA500 AMM 27-23-16. RIGGED AND OP'S CHECKED RUDDER IAW EA500 AMM 27-00-01 AND 27-00-00. NO DEFECTS NOTED. 1 L 7 2 4J RT A00002AC 2008042400040 20080424 00040 WP 2008 4 24 070193 1 20080414 A 2170 COALESCER BAG DOUG DC9 DC987 3022087 WP DIRTY A WX0A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 19 952MA 49673 FLIGHT ATTENDANT PERSONNEL REPORTED SMOKE IN THE CABIN. THE AIRCRAFT RETURNED TO THE ORIGINAL POINT OF DEPARTURE (RFD). MAINTENANCE PERSONNEL WERE DISPATCHED AND FOUND THE COALESCER BAGS EXCESSIVELY DIRTY. REPLACED THE RIGHT AND LEFT AIR CONDITIONING PACK COALESCER BAGS IAW AMM 21-20-02. RETURN TO SERVICE OPERATIONAL CHECK WAS PERFORMED AND ALL SYSTEMS O PS CHECK NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 2008042400046 20080424 00046 NM 2008 4 24 2008UALA02185 1 20080415 A 3350 58807 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 312UA 23673 EMERGENCY EXIT LIGHT INOP ON FLOOR ADJACENT TO GALLEY G-7. FOUND LIGHT INOPERATIVE. REPLACED BURNED OUT EEL LAMP REF M M33-51-90 PG 401. OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 20080715 EA 2008 7 15 A6WA200840364 1 20080427 A 2720 RUDDER PEDAL CNDAIR CL600 CL6002B19 1900309 EA INOPERATIVE A A6WA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 31 411ZW 7569 NO DIRECTIONAL CONTROL ON TAKEOFF WITH RUDDER PEDALS. ABORTED TAKEOFF. AIRSPEED NOT REGISTERED. BRAKE TEMPS 4,3,2,4. PER FORMED TAXI TEST WITH CREW ASSISTANCE IAW 09-20-00 AT 60 KNOTS. NO DEFECTS NOTED. A/C GOOD FOR SERVICE. (K) 2 L 7 2 4F RT A21EA 20080715 CE 2008 7 15 G1I2008F00000 1 20080207 A 3040 FED2000 DEFOG SYSTEM LEAR 35 35A 5170602 CE WINDSHIELD BURNED E G1IA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AL 01 60WL 382 AFTER DEPARTING, THE FLIGHT CREW EXPERIENCED SMOKE IN THE CABIN. THE FLIGHT CREW TURNED BACK TO DEPARTURE. MAINTENANCE W AS CONTRACTED TO FIND THE PROBLEM AND DISCOVERED THE COPILOT AUX WINDSHIELD DEFOGGER OVERHEATED. MX INSPECTED THE WIRING , SWITCH, AND REMOVED THE DEFOGGER UNIT AND SECURED THE WIRING, THE AUX DEFOGGER WAS DEFERED AND THE AC RETURNED TO SERV ICE. (K) 2 L 7 2 4F A10CE 20080715 EA 2008 7 15 A6WA200840301 1 20080407 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA MLG OUT OF ADJUST A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 417AW 7610 GEAR DISAGREE WARNING MESSAGE ILLUMINATED AFTER RETRACTION. REF WO 122814 ADJUSTED NLG OLEO CENTERED/EXTENDED PROX SENSO R IAW AMM 32-61-05. OPS CHECK GOOD. (K) 2 L 7 2 4F RT A21EA 20080715 EU 2008 7 15 08FDEA02069 1 20080530 A 5313 A53980668220 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS STRINGER REPAIR LOCATED IN AFT CABIN UNDER FLOOR BEHIND BULK CARGO ON STRINGER 41 RT BETWEEN FR 72 TO FR 73, HA S 1 EA REPAIR L-ANGLE MEASURING 9.9 INCHES LONG AND 1 REPAIR SECTION MEASURING 10.3 INCHES LONG REPAIR NOT IAW SRM REQUI REMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT STRINGER SPLICE REPAIR AT STRINGER 41 RT BETWEEN FR 72 AND FR 73 IAW A310 -200 SRM 53-10-14, FIG 201. THIS IS AN AIRBUS REPAIR WITH AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080812 EA 2008 8 12 A6WA200840365 1 20080426 A 2710 NUT CNDAIR CL600 CL6002B19 1900309 EA CONTROL WHEEL LOOSE A A6WA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 31 469AW 7917 DURING AILERON CHECK, BONDING OF CONTROLS FROM LEFT TO RIGHT FROM NEUTRAL AND BACK TO NEUTRAL FROM RIGHT ON BOTH YOKES. TORQUED PILOTS AND CO-PILOTS CONTROL WHEEL LATCHING NUT IAW AMM 27-11-01. OPS CHECK GOOD. OK FOR FURTHER SERVICE. (K) 2 L 7 2 4F RT A21EA 20080715 NM 2008 7 15 AALA200801256 1 20080508 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 39G INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 39G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080715 WP 2008 7 15 AALA200801261 1 20080508 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 459AA 49564 DFW - EMERGENCY LIGHT AT SEAT 17D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F A6WE 20080715 NM 2008 7 15 AALA200801254 1 20080508 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 194AA 32388 DFW - EMERGENCY LIGHT AT SEAT 16C BULLNOSE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 16C BULLNOSE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 A102008F00000 1 20080506 A 7997 1122514 CONNECTOR BOEING 737 737317 138447P NM NR 1 ENGINE CORRODED I A10B J DUMP FUEL E A VIBRATION/BUFFET FLAME/FIRE CR CRUISE 1 SO 29 253DV 23800 ON MAY 6, 2008 DURING A FLIGHT, THE FLIGHT CREW HAD A NR 1 (SN 721787) ENGINE HI OIL TEMP. THE CREW FOLLOWING THERE MANU ALS COULD NOT GET THE TEMP BELOW THE YELLOW BAND SO THEY DID AN INFLIGHT SHUTDOWNIAW THERE MANUALS. THE PLANE WAS DIVERT ED. TROUBLESHOOTING WAS PERFORMED BY MAINTENANCE PERSONAL ALONG WITH MCA PERSONAL IAW MM. THE CONNECTOR TO THE OIL TEMP BULB HAD CORRODED PINS. THE CORROSION WAS REMOVED SYSTEM TESTED , ENGINES RAN AT LOW AND HI POWER SETTING AND ALL INDIC ATION WERE NORMAL. LOG PAGES WERE COMPLETED AND PREFLIGHT SIGNED OFF. AIRCRAFT IS RETURNING TODAY FROM AT 1300. (K) 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 ASAA0843005 1 20080513 A 5230 65C362311 SKIN BOEING 737 7374Q8 138447Q NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 AFT CARGO DOOR DENTS WITH SCRATCHES AND DENTS WITH CREASES IN 3 AREAS. REMOVED AFT CARGO DOOR EXTERNAL SKIN. FABRICATE D LOCATED DRILLED AND INSTALLED A REPLACEMENT SKIN IAW B737 400 SRM 52 30 01 FIG 201. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 ASAA0842996 1 20080531 A 5754 SKIN BOEING 737 737490 1384715 NM KRUEGER FLAP CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 RT WING NR 3 K FLAP LEADING EDGE GOUGED ON EXTERIOR 5.5 INCHES FROM LEADING EDGE AND 13.2 INCHES FROM IB END VERIFIED CR ACK IN GOUGE STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER IAW B737 400 SRM 57 43 02 FIG 201 REPAIR 2. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 NWAA082386623 1 20080526 A 5330 SKIN BOEING 747 747251B 1384892 NM BS 340 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 623US 21705 DURING "M" CHECK, FOUND CRACK IN FUSELAGE SKIN AT BS 340 BETWEEN S7L AND S8L. REPAIRED PER EA 66-213141. 2 L 7 4 4F RT A20WE 20080715 CE 2008 7 15 BB17205222008 1 20080522 A 2121 MOTOR BEECH 200 200BEECH 1152920 CE VENT BLOWER FAILED E QMLA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 94KC BB172 SHORTLY AFTER DEPARTURE, CLIMBING THRU 8,000 (MSL), THE CREW NOTICED AN ODOR COMING FROM THE CABIN. APPROXIMATELY FIVE MINUTES AFTER THAT THE CREW NOTICED A HAZE BEGINNING TO FORM IN THE REAR OF THE CABIN. THAT IS WHEN THEY DECIDED TO MAK E A PRECAUTIONARY LANDING AT THE NEAREST SUITABLE AIRPORT. AT THAT TIME THE FLIGHT WAS AT 17,000 (MSL). THE HAZE AN OD OR WAS NOT BAD ENOUGH IN THE PILOT’S OPINION TO DECLARE AN EMERGENCY. THROUGH OUT THE PROCESS WE STARTED TO ELIMINATE P OWER SOURCES, SUCH AS OVERHEAD LIGHTING, AND LIFE PORT INVERTERS. THE AIRCRAFT WAS ON THE GROUND IN ABOUT TEN MINUTES A FTER THE HAZE FIRST STARTED. BETWEEN THE TIME WE LANDED TO THE TIME WE TAXIED TO THE FBO, THE HAZE AND SMELL HAD BECOME 1 L 7 2 4T A24CE 20080715 WP 2008 7 15 ASMF200805006 1 20080529 A 5260 H201 SWITCH DOUG DC9 DC981 3022081 WP AFT DOOR DAMAGED W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 501AM 49188 BEFORE PUSH BACK, CAPTAIN REPORTED THAT AFT STAIR LIGHT TURNED ON. MAINTENANCE PERSONNEL DETECTED SWITCH S1-277 DAMAGED , SO IT WAS REPLACED IAW MM 52-70-10, TESTED CORRECT. AFTER THAT, MAINTENANCE PERSONNEL DETECTED A FUEL LEAK IN BOTH WI NGS, SO AIRCRAFT WAS SENT TO THE HANGAR AND THE FUEL TANKS WERE OPENED, DETECTING DAMAGED SEAL IN THE LT WING FUEL TANK AND A NUT MISSING IN THE RIGHT WING FUEL TANK, SO SEAL WAS REPLACED AND NUT INSTALLED IAW MM 57-30-03 AND SRM 51-30-0, T ESTED CORRECT. 2 L 7 2 4F A6WE 20080715 EU 2008 7 15 USAA920081156 1 20080513 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 678AW 2482 SAL - EMERGENCY EQUIPMENT - BC2 CHECK - NR 6103162, AFT FLIGHT ATTENDANT SEAT LEFT INBOARD FLASHLIGHT CHARGE INDICATOR N OT BLINKING. REPLACED AFT FLIGHT ATTENDANT SEAT LEFT INBOARD FLASHLIGHT BATTERY. 2 L 7 2 4F RT A28NM 20080715 NM 2008 7 15 ASAA0842986 1 20080518 A 5753 SKIN BOEING 737 737490 1384715 NM FORE FLAP DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 LT INBD FORE FLAP HAS NUMEROUS DENTS ON LOWER SURFACE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR GENERAL. 2 L 7 2 4F RT A16WE 2008042400047 20080424 00047 NM 2008 4 24 2008UALA02186 1 20080415 A 3350 CM387 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 312UA 23673 EMERGENCY EXIT LIGHT INOP AT STOWBIN BULLNOSE ABOVE SEAT ROW 2L. FOUND BURNED OUT BULB. REPLACED LAMP OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042400054 20080424 00054 NM 2008 4 24 2008UALA02195 1 20080415 A 5240 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR LOWER CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 R2 DOOR LOWER GATE HAS CORROSION AROUND LUG FTG HOLES. REPLACED GATE PER SRM 51-40 -02. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400064 20080424 00064 NM 2008 4 24 USAA920080898 1 20080417 A 5320 ANGLE BOEING 737 7374B7 1384702 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 - NR 03C10753060/13, CORROSION ON Z-ANGLE AT BS 320-340, LBL61. INSTALLED REPAIR IAW EA100404. 2 L 7 2 4F RT A16WE 20081103 SO 2008 11 3 C2XA08TY1242 1 20081009 A 5610 163500116 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT MALFUNCTIONED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 27 16999 19679 19679 145307 AC WAS ON APPROACH INTO BNA WHEN SMOKE WAS SEEN COMING OUT FROM UNDERNEATH THE FO DASH. MX R&R THE RT WINDSHIELD IAW EM B 145 AMM 56-10-01. PRESSURIZATION CHECK/LEAK CHECK IAW EMB AMM 21-31-00. AC RELEASED, AFTER ALL CHECKS, BACK TO SERVI CE. 2 L 7 2 4T RT T00011AT 2008042400070 20080424 00070 NM 2008 4 24 2008UALA02262 1 20080417 A 2120 UNKNOWN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 29 902UA 25002 VERY STRONG BURNING RUBBER TYPE ODOR IN FWD CABIN AREA OCCURRED SHORTLY AFTER LANDING GEAR LOWERED, STILL NOTICEABLE AT GATE. 2 L 7 2 4F 4 F RT A16WE E2GL 20080919 NM 2008 9 19 SWAA084854 1 20080903 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM BS 426 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 426, RBL 2. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20080919 2008 9 19 ASAA0853447 4 20080831 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM FLT MANAGE MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 583AS 4492 35681 FMC DISAGREE LIGHT ILLUMINATED. ACCOMPLISHED FMC DISAGREE QRH ON THE GROUND. PERFORMED "FMC DISAGREE MESSAGE ON CDU" F IM TASK 34 61 00 810 835. GROUND VERIFCATION SUCCESSFUL. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0843433 1 20080819 A 5754 65C26603202A SKIN BOEING 737 737490 1384715 NM NR 4 SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 INBOARD TRAILING EDGE OF NR 4 SLAT CHAFED. REMOVED DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 51-70-10. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0843438 1 20080902 A 5753 6546430189 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 LT WING I/B FOR FLAP REPAIR ON UPPER SURFACE 34 INCHES FROM O/B AND CHAFED AND DELAMINATED. REPAIRED DAMAGE TO LT WING I/B FORE FLAP UPPER SURFACE IAW B737 400 SRM 51-70-10 PARA 96 PG 217 REPAIR 4. 2 L 7 2 4F RT A16WE 20080919 2008 9 19 ASAA0853430 4 20080829 A 3442 6225129105 CONTROL PANEL BOEING 737 737890 1384527 NM WX RADAR SYS MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 570AS 6102 35185 THE "PWS FAIL" "WXR FAIL" AMBER ANNUNCIATOR ON BOTH NAV DISPLAYS DURING COCKPIT SET UP WITH WXR SELECTED ON EFIS CONTROL PNL. PROBLEM VERIFIED 'PWS FAIL' C W FIM 344-010-00-34-43 TASK 810 WXR SYSTEM OPS TEST AMM TASK 34-43-00-710-802 001, ALL CHECKS NORMAL AFTER ENGAGING 'STAB' BUTTON ON THE WXR CONT PNL. 2 L 7 2 4F RT A16WE 20080919 EA 2008 9 19 COMA086374 1 20080829 A 5315 60035031563 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 420CA 7451 LT FLOOR SUPPORT ANGLE AT STA 621 LBL 45 IS CRACKED. PERFORMED REPAIR IAW REO 601R-53-61-117 REV A. 2 L 7 2 4F RT A21EA 20080919 NM 2008 9 19 UPS08M53247 1 20080824 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 3 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAI R BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080919 NM 2008 9 19 UPS08M53248 1 20080825 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 4 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAI R BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080919 NM 2008 9 19 UPS08M53250 1 20080824 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 25 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080919 NM 2008 9 19 UPS08M53255 1 20080824 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 3 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080919 NM 2008 9 19 UPS08M53256 1 20080825 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 2 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080919 NM 2008 9 19 UPS08M53257 1 20080825 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 34 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080919 NM 2008 9 19 UPS08M53258 1 20080826 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 4 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080919 NM 2008 9 19 CALA0800839 1 20080829 A 5315 146A7501 FLOORBEAM BOEING 737 737724 13844BY NM BS 773 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27722 28789 AFT CARGO STATION 773 RBL 13.84 FLOOR SUPPORT HAS MILD CORROSION. FABRICATED AND INSTALLED REPAIR PER ECRA 5321-01562. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 CALA0800841 1 20080829 A 3350 276005 FUSE BOEING 737 737524 1384721 NM EMERGENCY LIGHT BLOWN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 R2 DOOR EMERGENCY EXIT LIGHTS INOPERATIVE OUTSIDE AND LOWER INSIDE. FOUND FUSE'S BAD AT POWER SUPPLY, REPLACED FUSES IA W AMM33-51-51, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 CALA0800844 1 20080831 A 5343 BUSHING BOEING 737 737824 13844BZ NM NLG TRUNNION CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18223 28932 NLG RT TRUNNION BUSHING HAS LIGHT PITTING CORROSION. REMOVED AND REPLACED RIGHTHAND INBOARD TRUNNION FITTING IAW BOEING DRAWING 141A7500 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080919 EA 2008 9 19 A6WA200840584 1 20080828 A 2613 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA LT NACELLE MALFUNCTIONED A A6WA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 31 448AW 7814 LT 14TH DUCT WARNING MESSAGE EN ROUTE. COMPLIED WITH QRH. R&R LT PYLON 14TH STAGE SENSE ELEMENT IAW 36-21-00. OPS CHE CK GOOD. 2 L 7 2 4F RT A21EA 20080919 EA 2008 9 19 HNAA0800253 1 20080612 A 5210 BRACKET DHAV DHC8 DHC8311 1386006 EA PAX DOOR CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 335EN 32270 375 CORROSION PAX DOOR BOTTOM BRACKET ZED SUPPORT FWD AND AFT FOUND CORRODED. REPLACED PAX DOOR BOTTOM BRACKET. 2 H 7 2 4T RT A13NM 20080919 NM 2008 9 19 CALA0800846 1 20080901 A 3350 ADD71701100 BATTERY PACK BOEING 737 737824 13844BZ NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12238 28808 EMERGENCY EXIT LIGHT BATTERY PACKS FAILED TEST AT SEAT ROWS 12, 20, RIGHT FORWARD GALLEY, AND RIGHT AFT GALLEY. REMOVED AND REPLACED BATTERY PACKS AT ROW 12, 20, FWD GALLEY, AND AFT GALLEY REF MM 33-51-06. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084880 1 20080904 A 5320 6517582 VERTICAL BEAM BOEING 737 7373H4 1384600 NM BS 178 BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080922 2008 9 22 SWAA084881 4 20080904 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 407WN 29817 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084886 1 20080904 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM BS 370 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 370, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084933 1 20080908 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727C S22R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080922 EA 2008 9 22 COMA086380 1 20080902 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 966CA 30219 7132 CRACK ON AFT PRESSURE BULKHEAD ABOVE CARGO DOOR TRACK AT LBL 27.50. REPAIRED AFT PRESSURE BULKHEAD AT LBL 27.50 IAW REO 601R-53-61-1541. 2 L 7 2 4F RT A21EA 20080922 NM 2008 9 22 HNAA0800281 1 20080907 A 3040 NP15790114 WINDSCREEN DHAV DHC8 DHC8102 2809003 NM COCKPIT ARCED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 814EX 128 318 EN ROUTE TO DESTINATION AT 16000 FEET THE FLIGHT CREW NOTED A PUFF OF SMOKE COMING FROM UNDERNEATH THE MASTER CAUTION PA NEL. THE SMOKE DISSIPATED WITH NO OTHER SIGNS OF DIFFICULTY. THE CAPTAIN DECLARED AN EMERGENCY AND NOTIFIED THE PASSEN GERS OF AN AVIONICS PROBLEM THEN TOLD THEM TO FOLLOW THE DIRECTS OF THE FLIGHT ATTENDANT. THE ACFT THEN LANDED WITHOUT INCIDENT. UPON INSPECTION IT WAS DISCOVERED THAT THE CO-PILOTS WINDSCREEN CONTACTS HAD ARCED AND ONE WAS LOOSE. THE WI NDSCREEN WAS THEN CHANGED. OPS CHECKS WERE GOOD AND THE ACFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 20080922 NM 2008 9 22 SWAA084914 1 20080907 A 5311 69432332 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND AFT CARGO DOOR CUTOUT AFT FRAME CORRODED AT LOWER END. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084915 1 20080906 A 5743 115A5211 TRUNNION BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 744SW 29490 DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION FITTING LUG CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084916 1 20080906 A 5743 115A5211 TRUNNION BOEING 737 7377H4 1384404 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 744SW 29490 DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION FITTING LUG CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084917 1 20080907 A 5753 6546434 SKIN BOEING 737 7377AD 1384502 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 798SW 28436 DURING SCHEDULED 10Y CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084922 1 20080907 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 277 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084923 1 20080907 A 5311 6558280 FRAME BOEING 737 7373T0 1384582 NM BS 360 S20R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084924 1 20080907 A 5322 6546569 SHEAR TIE BOEING 737 7373T0 1384582 NM BS 967 S27R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084838 1 20080903 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 877 S24L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER 24L CORRODED AT BS 877. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084839 1 20080903 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 540 S26L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER 26L CORRODED AT BS 540. REPAIRED STRINGER PER ACO. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843360 1 20080724 A 5320 654769010 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM BS 820-874 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 AFT CARGO PIT FLOOR SUPPORT HAS DOUBLE DRILLED HOLES AT STA 860 LBL 19. CUT OUT DAMAGED AREA, LOCATED DRILLED AND INSTA LLED A REPLACEMENT FLOOR SUPPORT (SPLICE REPAIR) IAW B737 400. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843372 1 20080724 A 5315 654659268 FLOORBEAM BOEING 737 7374Q8 138447Q NM BS 857 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 AFT CARGO PIT FLOOR SUPPORT CORRODED STA 857 LBL 6. CUT OUT DAMAGE AREA OF FLOOR SUPPORT, FABRICATED REPAIR ANGLES, REP AIR PARTS LOCATED DRILLED AND INSTALLED IAW AAR EA 12811 AWE ASA EA 5310 02810. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843381 1 20080719 A 5315 FLOORBEAM BOEING 737 7374Q8 138447Q NM BS 294 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 CABIN FLOORBEAM UPPER CHORD CORRODED LBL 20 TO RBL 60 STA 294.5. REMOVED DAMAGED UPPER CHORD, FABRICATED REPAIR PARTS, LOCATED DRILLED AND INSTALLED SPLICE ANGLE AND UPPER BEAM CHORD IAW B737 400 SRM 53 10 51 FIG 201. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843370 1 20080718 A 5330 BEAR STRAP BOEING 737 7374Q8 138447Q NM BS 483-496 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 FWD CARGO PIT BILGE AREA BEAR STRAP EXFOILATED STA 490 RBL 10.5 TO RBL 13. REMOVED DAMAGED AREA, HFEC INSPECTED IAW NDT M PT6 FIG 23 AND FIG 16, NO DEFECTS NOTED. FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR PARTS AND EXT DOUBLER AND TRIPLER IAW ASA EA 5330 02377. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843365 1 20080723 A 5322 654653175 SHEAR TIE BOEING 737 7374Q8 138447Q NM BS 500E CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 SHEAR TIE AT STA 500E IS CORRODED BETWEEN STRINGERS 28L TO 26R. CORROSION FOUND TO BE ON PREVIOUS REPAIR, REMOVED AND R EPLACED SHEAR TIE IAW B737 400 SRM 53 00 07. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843354 1 20080717 A 5753 6546435317 SKIN BOEING 737 7374Q8 138447Q NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 LT WING O/B TRAILING EDGE AFT FLAP 3 EACH DENTS ON LOWER SURFACE. PREPARED DAMAGED AREAS, FABRICATED DOUBLERS AND BONDE D IN ACCORDANCE WITH B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843355 1 20080731 A 5751 65C259261 HINGE FITTING BOEING 737 7374Q8 138447Q NM RT AILERON CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 UPON REMOVAL OF RT AILERON TAB FOUND 2ND FROM O/B HINGE FITTING ON AILERON CRACKED AT FWD UPPER CENTER. AREA APPROX .20 0 LENGTH. RECEIVED A REPLACEMENT FITTING, INSTALLED NEW FITTING IAW B737 400 SOPM 20 50 01 PG 2 STEP 3 AND CMM 57 50 25 PG 701 STEP 2E FIG 56 INITIATED. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843363 1 20080717 A 5755 654645170 SKIN BOEING 737 7374Q8 138447Q NM NR 3 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 LEFT WING NR 3 SPOILER UPPER SURFACE HAS AREA OF SEVERAL DENTS. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 20080714 EU 2008 7 14 USAA920081113 1 20080516 A 5540 D5537131800200 HINGE AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 602AW 565 SAL - MAJOR REPAIR - C1 CHECK - RUDDER HINGE NR 4 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 2632 / RIB 6. REPLACE D RUDDER HINGE NR 4, VERTICAL STABILIZER STATION 2632 / RIB 6 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 20080714 EU 2008 7 14 USAA920081114 1 20080524 A 5522 D55281225001 SKIN AIRBUS 320 A320232 3930326 EU RT ELEVATOR DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 602AW 565 SAL - MAJOR REPAIR - C1 CHECK - WATER TRAPPED IN THE RIGHT ELEVATOR UPPER SURFACE SKIN AT RIB 1 AND RIB 5. REPAIRED THE RIGHT ELEVATOR UPPER SURFACE SKIN AT RIB 1 AND RIB 5 IAW A320 SRM 55-21-11 AND 51-77-13. 2 L 7 2 4F RT A28NM 20080714 NM 2008 7 14 08FDEA02417 1 20080624 A 5330 6554582 SKIN BOEING 727 727225 1384077 NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 DURING INSPECTION OF NR 2 ENG INLET, RAN JLG INTO FUSELAGE AT STATION 1030 STRINGER 1R TO 3R, LIGHT SCRATCH AND GOUGE RE MOVED DAMAGE PER REF SRM 53-30-3 FIG 3. NDT DAMAGE REMOVAL AND MATERIAL LOSS. PER REF 727 NDT MAN PART 6, 51-00-00 FIG 23. TOOL IDM-0065. NO DEFECTS NOTED MAT. LOSS .003 INCH, ORIGINAL MAT. .040 INCH THICK. .037 INCH REMAIN. PER 727 NDT MAN. PART 4 51-00-00 FIG 2 TOOL ID IN-22-0029. FABRICATED AND INSTALLED REPAIR DOUBLER PER REF SRM 53-30-3 FIG 3, SRM 51-10-2 AND 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080714 EU 2008 7 14 08FDEA02042 1 20080530 A 5315 A53778807202 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON OLD TOP CAP BEAM C 32 LT, TOP CAP BEAM REPAIR RENEWED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 08FDEA02096 1 20080602 A 5330 2024T3 SKIN BOEING 757 75723A 1384967 NM ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 919FD 24636 EXISTING PATCH REPAIR FOUND ON AFT PRESSURE PANEL AT BS 1720, LBL24 TO EVALUATE UNRECORDED REPAIR. EXISTING REPAIR FOUN T TO BE ACCOMPLISHED IAW B757-200 SRM 53-60-51 FIG 201 REPAIR 2, BASED ON EXTERNAL VISUAL EVALUATION ON THE SHAPE, LOCAT ION, SIZE, MATERIAL THICKNESS, TYPE AND GENERAL WORKMANSHIP OF THE REPAIR. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-10 0 CRITERIA. 2 L 7 2 4F RT A2NM 20080714 EU 2008 7 14 08FDEA02440 1 20080625 A 5312 A53610571200 BULKHEAD AIRBUS 310 A310222 3930315 EU MLG WW CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 NOSE WHEEL WELL-STA 1090/FR11, LIGHT SURFACE CORROSION FOUND ON W/W FWD WALL, LOCATED RBL8.0 BETWEEN STIFFENERS 5/6. RE MOVED THE LIGHT CORROSION PER SRM 51-74-10. APPLIED ALODINE PER SRM 51-21-10. NO CRACK FOUND PER NTM 51-10-08. THE RE MAINING THICKNESS IS 0.087 INCH PER NTM 51-10-04. REPAIR PER EA 6-5310-117363. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 08FDEA02441 1 20080625 A 5347 AFA7082502 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 MID CABIN AFTER REMOVAL OF FLOOR PANELS AT APPROXIMATELY STATION 5-33, X = - 75.5 FOUND SEAT TRACK FLANGE STRUCTURE COR ROSION. SEAT TRACK REPAIRED AS PER SRM 53-70-00, FIG.1, VOL.1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080714 WP 2008 7 14 08FDEA02310 1 20080618 A 5320 ADA1089 SKIN DOUG MD10 MD1010F 3022112 WP BS 913-933 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 FWD PIT, IN THE DOOR SILL AREA BETWEEN STRINGER L43R AND STRINGER L44R 36 INCH AFT OF THE FWD EDGE OF THE DOOR CUTOUT, T HE WEB SKIN IS CRACKED. ACCOMPLISHED EA 3 8-5310-118513, FUSEALGE FWD CARGO COMPT JAMB INNER TORQUE BOX SKIN AND DOUBL ER REPAIR. REPAIR WAS ACCOMPLISHED BETWEEN L43-44R FROM BS 913-933. 2 L 7 3 4F RT A22WE 20080714 EU 2008 7 14 08FDEA02313 1 20080618 A 5320 A255720310100 PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 THE BULK CARGO COMPARTMENT LEFT TRANSITION PANEL IS CORRODED AROUND THE FASTENER RECEPTICALS FROM FRAME 67 TO FRAME 69. REMOVED THE CORROSION; FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-00. REMOVED TRANSITION PANEL. FABRIATED A NEW TRANSITION PANEL IAW AIRBUS DWG 17A25572031. ALODINED PANEL IAW A300-600 51-21-10. PRIMED AND PAINTED THE NEW PANEL IAW A300-600 SRM 51-23-10. LOCATED AND DRILLED PANEL IAW A300-600 SRM 51-40-44. INSTALLED THE NEW PANEL IAW A300-600 SRM 51-40-21. PART MARKED NEW PANEL IAW FEDEX GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080714 NM 2008 7 14 08FDEA01971 1 20080523 A 5330 2024T30063 SKIN BOEING 757 75723A 1384967 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 919FD 24636 EXTERNAL PATCH REPAIR ON FUSELAGE AT BS365, S-21R TO BE EVALUATED. EXISTING REPAIR FOUND ACCOMPLISHED IAW SRM 53-00-01 FIG 203, BASED ON EXTERNAL VISUAL EVALUATION OF THE SHAPE, LOCATION, SIZE, MATERIAL THICKNESS, TYPE AND GENERAL WORKMANS HIP OF THE REPAIR. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080714 NM 2008 7 14 08FDEA02372 1 20080621 A 5720 65162169 WEB BOEING 727 727227 1384078 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 CRACK ON LEFT WING TRAILING EDGE WEB JUST OUTBOARD OF NR 7 SPOILER FITTING. CUT-OUT DAMAGED AREA, FABRICATED NEW DOUBLE R, FABRICATED WEB, & INSTALLED REPAIR PARTS IAW SRM 51-30-2, AND DRAWING SR27-57-038. 2 L 7 3 4F A3WE 20080714 NM 2008 7 14 08FDEA02378 1 20080623 A 5312 AEA05261 BULKHEAD DOUG MD11 MD11F 3023600 NM MLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 CENTER LANDING GEAR WHEEL WELL STATION 1391 LEFT WEB CORNER DOUBLER FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-3 1-01 VOL.II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080714 NM 2008 7 14 08FDEA02379 1 20080623 A 5313 ACA37961 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 DURING HFEC INSPECTION, MULTIPLE CRACKS (05 EACH, TOTAL LENGTH APPROX 1.2 INCH) FOUND AT FASTENER HOLE OF LONGERON ADJAC ENT TO NOSE LANDING GEAR LEFT TRUNNION FITTING. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080714 NM 2008 7 14 DL764080775 1 20080525 A 3240 MS250081 SWITCH BOEING 767 767432ER 1385134 NM PARKING BRAKE STICKING A DALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 27 827MH 29698 728712 RTO AND RTB DUE TO PARKING BRAKE TAKEOFF WARING AURAL AND EICAS MSG. T/S PER FIM. FOUND SWITCH S459 STICKING. REPLACE D PARKING BRAKE SWITCH PER M/M. CHECKS GOOD. 2 L 7 2 4F RT A1NM 20080714 WP 2008 7 14 08FDEA02385 1 20080623 A 5310 NFA6024 BEAM DOUG DC10 DC1030F 3023504 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 307FE 48291 WHILE PERFORMING J/C 8-2550-7-2354 PT 2 CTR CARGO HANDLING SYSTEM FOUND CRACK ON LOWER FLANGE OF BEAM. REPAIRED AREA IA W SRM 53-00-01 FIG 9 SHT 7 VOL I. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 USAA920081205 1 20080601 A 5320 143N52601 INTERCOSTAL BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 905AW 23567 NR 6109926, INTERCOSTAL UPPER ANGLE CRACKED B/S 480 TO 500 RBL 10 W/L 208.1. REPLACED INTERCOSTAL UPPER ANGLE B/S 480 TO 500 RBL 10 W/L 208.1 IAW SRM 51-40-02-0G. (K) 2 L 7 2 4F RT A2NM 20080922 NM 2008 9 22 ASAA0843368 1 20080717 A 5755 MA14910 SKIN BOEING 737 7374Q8 138447Q NM NR 8 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 RT WING NR 8 SPOILER DENTED ON LOWER SURFACE CENTER AREA. PREPARED DAMAGED AREA, FABRICATE REPAIR DOUBLER AND BONDED IA W B737 400 SRM 51 70 10 PAGES 201 203 REPAIR 2. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843423 1 20080812 A 5330 65C277997 SKIN BOEING 737 7374Q8 138447Q NM BS 178 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 LOWER FUSELAGE SKIN DAMAGED AT BS 178 BETWEEN STR 27R AND 28R. REPAIRED IAW CASCADE ERO 8610 AND ASA EA 5330 02383. 2 L 7 2 4F RT A16WE 20080924 NM 2008 9 24 08FDEA03113 1 20080729 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCHES HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB CRACKED NR 7 SUPPORT FITTING REMOVED AND REPLACED AS PER SR M 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 08FDEA03082 1 20080725 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 577FE 48469 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FITTING AT HOLES A, B, C AND D. MAI. REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL 1. REPAIR CLASSIFIED A S MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 2008 9 24 DL738081137 4 20080901 A 2397 WIRE HARNESS BOEING 737 737832 13844CF NM ENTERTAIN SYS CHAFED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 3760C 30816 IN FLIGHT ENTERTAINMENT SYSTEM INOP DUE TO CHAFING HARNESS AT BACK OF SEAT 2D RUNNING DOWN LT SIDE ARCING TO FRAME. C/B FOR ENT SYSTEM PULLED AND COLLARED. CONFIRMED FAULT, REPLACED HARNESS PN RD KM6391 1717 FOR LCD MONITORS AT 3CD, OPS C HECK OK PER MM. ALSO, REPLACED VSEB AT 3CD PN RD KA3303 05, OPS CHECK OK PER MM SN ON D630690 SN OFF D739233. 2 L 7 2 4F RT A16WE 20080924 NM 2008 9 24 DL757081138 1 20080902 A 2120 UNKNOWN BOEING 757 757232 1384965 NM CABIN ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 645DL 24216 AT 40K FEET FLT NOTIFIED FLT CREW OF RUBBERY/SULFUR ODOR AROUND ROWS 23-27 IN PASSENGER CABIN. THE ODOR WAS EMANATING F ROM THE FLOOR AREA. CREW DECIDED TO DIVERT TO IAD, DECLARED AN EMERGENCY. AT APPROX 20K FT ODOR WAS DISSIPATING, ON LAN DING ODOR WAS GONE. INSPECTED A/C INCLUDING ENG 1 AND INSPECTED LT AND RT PACK BAY, APU AND BOTH PACKS FOR 90 MINUTES, RECIRC FAN AREA. INSPECTED PAX CA ELECTRONIC BOXES. INSPECTED OVHD PSUS IN AFFECTED AREA. NO TROUBLE. 2 L 7 2 4F RT A2NM 20080924 NM 2008 9 24 DL76G081140 1 20080902 A 2730 ELEVATOR SYSTEM BOEING 767 767332 1382001 NM MALFUNCTIONED A DALA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 27 169DZ 29689 RT ELEVATOR IND NOT RESPONDING TO CONTROL INPUTS. VERIFIED ELEVATOR MOVEMENT PER MEL FWD TO MCO/PLAC PER MEL 27-08-01 Y ELLOW PLAC INSTALLED. 2 L 7 2 4F RT A1NM 20080924 NM 2008 9 24 DLM88081141 1 20080901 A 2910 7952170567 LINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE HYD SYSTEM LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 918DL 49583 725837 LT ENG HYD FLUID DEPLETED IN FLT, LT ENG HYD PUMP PRESS LINE LEAK IN TAIL OF A/C. REPLACED ENG DRIVEN PUMP AND INSTALLE D TEMP FLEX LINE PER M/M. 2 L 7 2 4F 4 F RT A6WE E9NE 20080924 NM 2008 9 24 DL76L081148 1 20080430 A 3350 SIGN BOEING 767 767332 1382001 NM LEFT OVERWING BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 KICK PANEL 411T1262-61 LEFT OVERWING AFT EXIT SIGN BROKEN, BASE AND LENS MISSING. REMOVED AND REPLACED EXIT SIGN AT OVE RWING HATCH ON LT SIDE. OPS CHECKS GOOD IAW B767-300 MM 33-51-01. 2 L 7 2 4F RT A1NM 20080924 WP 2008 9 24 08FDEA03100 1 20080728 A 5320 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 MAIN CARGO DOOR JAMB SPOOL FITTING NR 7 HAS A CRACK INDICATION IN THE BACK UP FITTING AT HOLE "A". HOLE "A" HOLE DIS IS 0.519". REMOVED SUBSTRUCTURE AND WEB TO GAIN ACCESS TO THE NR 7 SPOOL BACK UP FITTING IAW SRM 51-33-01; VOL II. LOCAT ED AND DRILLED NEW BACK UP FITTING IAW 51-33-01; VOL II. INSTALLED NEW BACK UP FITTING AFA 7132-1 IAW SRM 51-33-01; VO L II. RE-INSTALLED SUB STRUCTURE AND WEB IAW SRM 51-33-01; VOL II. INSTALLED BUSHING IAW SRM 53-50-11; VOL I. 2 L 7 3 4F RT A22WE 20080924 EU 2008 9 24 08FDEA03526 1 20080819 A 3230 A2519903 SELECTOR VALVE AIRBUS 300 A300B4622R 3930312 EU MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 725FD 2863 2863 572 LANDING GEAR FAILED TO RETRACT, FOLLOWED ECAM AND QRH GEAR HANDLE DOWN AND RETURNED TO LAND. SYSTEM B WAS USED AND SYS A DID NOT WORK EITHER. REMOVED AND REPLACED LANDING GEAR ELECTRO HYDRAULIC SELECTOR VALVE 3GA PRECAUTIONARY. PERFORMED LEAK CHECK SATISFACTORY. WORK PERFORMED IAW AMM 32-31-12-4. 2 L 7 2 4F RT A35EU 20080924 WP 2008 9 24 08FDEA03527 1 20080821 A 5313 AYB70201 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 LONGERON 51 L LEFT END FITTING AT STA 1521 IS CORRODED. FABRICATED 1 LONGERON END FITTING P/N AYB 7020-2 IAW BAC DWG NR AYB7020. 2 L 7 3 4F RT A22WE 20080924 EA 2008 9 24 SWIA200820044 1 20080912 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 912SW 7595 FLT 6553-12, AFT EMERGENCY FLOOD LIGHT INOP. REPLACED AFT OVERHEAD EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20080924 EA 2008 9 24 SWIA200820045 1 20080908 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 944SW 7764 FLT 6504-8, EMERGENCY PATH LIGHT STRIP SECTION BURNED OUT. RECONNECTED LOOSE CONNECTOR. 2 L 7 2 4F RT A21EA 20080924 NM 2008 9 24 DL76L081151 1 20080516 A 3350 LIGHT BOEING 767 767332 1382001 NM OVRWING SLIDE NO TEST A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 188DN 27583 RT OFF WING SLIDE LIGHT DOES NOT ILLUMINATE FOR TEST 1. PERFORMED SQUIB TEST IAW MM 25-65-00. OPS CHECKS GOOD REF 25-6 0-00. 2 L 7 2 4F RT A1NM 20080924 NM 2008 9 24 DL764081152 1 20080903 A 2121 73259F FAN BOEING 767 767432ER 1385134 NM OVERHEATED A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 837MH 29710 ATB DUE TO FWD EQUIPT OVERHEAT MESSAGE. REMOVED AND REPLACED FWD EQUIPT FAN AND MONITOR. 2 L 7 2 4F RT A1NM 20080715 NM 2008 7 15 08FDEA02326 1 20080619 A 5320 453N1801Y58 CHANNEL BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 SIDE WALL SUPPORT ANGLE AT BS 1300, STR 27R TO 30R FOUND CORRODED. CORROSION FOUND EXCEED SRM 53-00-71 LIMITS. REMOVED A ND REPLACED SIDEWALL SUPPORT ANGLE IAW SRM 51-10-02 AND SRM 51-40-02 REV.93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2- 100 CRITERIA. 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 USAA920081228 1 20080531 A 5753 SKIN BOEING 757 7572S7 1384962 NM T/E FLAP DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 905AW 23567 MCN - C12 - MAJOR REPAIR - NR 6108532 - I/B TRAILING EDGE DISBONDED, RIGHT WING I/B AFT FLAP. REPAIRED I/B TRAILING EDGE RIGHT WING I/B AFT FLAP DISBONDED IAW SRM 51-70-04-0G. (K) 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 USAA920081203 1 20080605 A 5330 65C3080327 SKIN BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN - C-21 - MAJOR REPAIR - NR 6110424 - FUSELAGE SKIN CRACKED B/S 727E+6 S21R IAW SRM 53-00-01-2R-31. (K) 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 USAA920081201 1 20080605 A 5754 SKIN BOEING BOEING 737 73733A 1384673 NM L/E SLAT DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 192 23627 MCN - C-21 - MAJOR REPAIR - NR 6061316 - DISBOND TOP NR 5 SLAT STA 254. REPAIRED DISBOND TOP NR 5 SLAT WEDGE, SLAT STA 254 IAW B737, SRM 51-70-10-2R4 REPAIR 4. (K) 2 L 7 2 4F RT A16WE 20080715 WP 2008 7 15 08FDEA02166 1 20080605 A 5100 NONE DOUG MD10 MD1010F 3022112 WP NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 377FE 47965 REJECTED TAKEOFF AT IND AT 100 KTS OAT 31C WEIGHT 386,200. REJECTED FOR PREDICITIVE WINDSHEAR ALERT. NO OBSERVED OR RE PORTED WINDSHEAR. PERFORMED BRAKE INSPECTION PER AMM 32-57-00-6. NO DEFECTS NOTED. ACN RELEASED FOR SERVICE PER MEL/C DL: 34-41-01-01-A CATEGORY: C EXPIRATION: 15JUN08 "MEL 34-41-01-01-A: PREDICTIVE WINDSHEAR INOP. WAGS WINDSHEAR IS AVAI LABLE." PERFORMED BRAKE INSPECTION PER AMM 32-57-00-6. NO DEFECTS NOTED. 2 L 7 3 4F RT A22WE 20080715 CE 2008 7 15 MT9A00000035 1 20080515 A 2750 MS276404 BEARING CESSNA 208 208B 2073701 CE T/E FLAP CORRODED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9623B 208B0138 THE SEALED BEARING WAS CORRODED AND FROZEN. ALSO THE BEARING WAS CORRODED TO THE BOLT. (K) 1 H 7 1 3T A37CE 20080715 CE 2008 7 15 MT9A00000016 1 20080505 A 2750 26220919 BELLCRANK CESSNA 208 208B 2073701 CE T/E FLAP DAMAGED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9760B 208B0102 THE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE B OLT HOLE THROUGH THE MOUNTING BRACKET. (K) 1 H 7 1 3T A37CE 20080715 WP 2008 7 15 08FDEA02180 1 20080606 A 5330 AEA01122 SKIN DOUG DC10 DC1010 3022110 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 MAIN CABIN, 2 CRACK 1.5 INCH LONG ON WEB ON AFT R3 JAMB AT STA 1306 BTWN L26 AND L27 RT SIDE. REPAIR JAMB IAW SRM 53-50 -00 FIG 19 SHEET 2, 3 AND 6 VOL 1. 2 L 7 3 4F A22WE 20080715 CE 2008 7 15 MT9A00000007 1 20080509 A 2750 26220911 BELLCRANK CESSNA 208 208B 2073701 CE T/E FLAP FROZEN E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9505B 208B0085 THE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS. (K) 1 H 7 1 3T A37CE 20080715 EA 2008 7 15 OVF2008F00001 2 20080508 A 7414 M3056 BRUSHES SLICK GIPPLD GA8 GA8 3900102 EU LYC O540 IO540K1A5 41532 EA MAGNETO WORN E OVFA K NONE O OTHER IN INSP/MAINT 1 WP 13 7508M GA805094 L3095348A AIRCRAFT EXPERIENCED AN ENGINE FAILURE. ATTEMPTS TO RESTART ENGINE FAILED AND SAFE LANDING WAS ACCOMPLISHED. CAUSE OF FA ILURE REMAINS UNKNOWN AT THIS TIME. MAGNETOS FUEL PUMP, AND FUEL INJECTOR SERVO WERE SENT TO THE RESPECTIVE OEM`S. THE MAGNETOS WERE SENT TO THE MFG FOR ANALYSIS. THEY WERE SENT AS REMOVED TO PRECLUDE ANY FIELD CONTAMINATION. I WAS TOLD T HEY WERE NOT PRODUCING SPARK DUE TO LARGE AMOUNTS OF CARBON DUST FROM THE ABNORMAL WEAR AS THE FIRST. THE DUST CREATES A PATHWAY TO GROUND EFFECTIVELY SHUTTING DOWN THE MAGNETOS. SINCE THE AIRCRAFT/ ENGINES/ MAGNETOS WERE MANUFACTURED WITHI N THE YEAR OF EACH OTHER, AND ALL EXHIBITED THE SAME WEAR AT THE SAME HOURS IN SERVICE, I WOULD THINK AN EXAMINATION OF 1 H 7 1 3O 3 O NT 1E4 20080715 EA 2008 7 15 UH02008F00001 1 20080220 A 7921 269D45031 SCROLL SCWZER 269 269D 8059501 EA OIL COOLER FAN CRACKED E UH0A K NONE O OTHER IN INSP/MAINT 1 SW 03 411HU 1541 0040 UPON INSPECTION OF OIL COOLER FAN ASSY FOUND MANY CRACKS AROUND THE TOP MOUNT OF SCROLL ASSY. (K) 1 G 7 1 3U 0 4H12 20080715 EA 2008 7 15 A6WA200840300 1 20080407 A 2133 1314022 REGULATOR CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 407AW 674 7424 AIRCRAFT DID NOT PRESSURIZE AFTER TAKEOFF, CABIN RATE OF CLIMB MATCHED AIRCRAFT RATE OF CLIMB. NO EICAS MESSAGE RECEIVED . PLACED BOTH AUTOPRESSURE CONTROLLERS ON MEL. REMOVED AND REPLACED AUTOPRESSURE REGULATOR IAW AMM21-31-07. (K) 2 L 7 2 4F RT A21EA 20080715 NM 2008 7 15 AALA200801257 1 20080508 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 779AN 29955 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 40G INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 40G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080715 NM 2008 7 15 AALA200801249 1 20080508 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 772AN 29580 DFW - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080715 NM 2008 7 15 AALA200801255 1 20080508 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 325AA 22326 JFK - EMERGENCY LIGHT AT SEAT 30H INOPERATIVE. REPLACED EMERGENCY LIGHT AT SEAT 30H. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A1NM 20080715 NE 2008 7 15 ASAA0853013 2 20080529 A 7261 ENGINE BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE NR 2 OIL CONSUMPTION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 587AS 2341 35684 895978 NR 2 ENGINE HAS A HISTORY OF ABOVE NORMAL OIL CONSUMPTION PERFORM MM 71-71-00-200-801 VENTS AND DRAIN INSPECTION, PART P OWER ENGINE RUN REQUIRED. ACCOMPLISHED TSR AND AMM 71 71 00. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 20080715 NM 2008 7 15 08FDEA02070 1 20080530 A 5347 BAC1520742 SEAT TRACK BOEING 757 7572B7 1384964 NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 906FD 27148 STA 440-640 RBL 24 SEAT TRACK HAS HOLE AND GOUGES AROUND CLIPNUTS HOLE. REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02. F ABRICATED NEW SEAT TRACK ON MAE TRAVELER T8/741234 MAT BAC1520-792-7178-T6511. INSTALLED NEW SEAT TRACK AND SPLICE REPA IR ON STA 440-530 IAW SRM 53-00-52, 51-40-02. MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 AALA200801290 1 20080512 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 758AN 32637 DFW - EMERGENCY LIGHT AT SEAT 24G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080715 NM 2008 7 15 AALA200801291 1 20080512 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 758AN 32637 DFW - EMERGENCY LIGHT AT SEAT 22G LAMP MISSING. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080715 NM 2008 7 15 AALA200801299 1 20080513 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 198AA 32392 DFW - EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RIGH T NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20080715 CE 2008 7 15 K5LA050908001 1 20080505 A 5210 5043003117 BELLCRANK BEECH 200 A200 1152921 CE PWA PT6 PT6A41 52043 EA CABIN DOOR TWISTED E K5LA K NONE O OTHER IN INSP/MAINT 1 EA 05 636B BC61 DRUING A ROUTINE PHASE 3 INSPECTION, IT WAS FOUND THAT THE MAIN CABIN DOOR AFT UPLOCK BELLCRANK WAS TWISTED ABOUT 10 DEG REES FROM WHAT A NEW ONE IS.. ALSO THE BOLT PN NAS110321D THAT THE UPLOCK BRACKET PIVOTS ON WAS DEFORMED SLIGHTLY. THIS WAS PROBABLY CAUSED BY THE UPLOCK HOOK BEING MISRIGGED. ALL AFFECTED PARTS WERE REPLACED AND THE UPLOCK HOOKS WERE ABLE TO BE RIGGED PROPERLY. (K) 1 L 7 2 4T 4 T A24CE E4EA 20080715 NM 2008 7 15 UPS08B52388 1 20080417 A 5340 TENSION TIE BOEING 747 747400 13848AT NM BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:C BS 1180 TENSION TIE FOUND CRACK AT RT AFT SIDE. BS 1180 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201 . 2 L 7 4 4F RT A20WE 20080715 NM 2008 7 15 UPS08B52389 1 20080417 A 5340 TENSION TIE BOEING 747 747400 13848AT NM BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:C BS 1180 TENSION TIE RT FWD SIDE CRACKED. BS 1180 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201. 2 L 7 4 4F RT A20WE 20080715 NM 2008 7 15 UPS08B52390 1 20080417 A 5340 TENSION TIE BOEING 747 747400 13848AT NM BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:C BS 1180 TENSION TIE LT AFT SIDE CRACKED. BS 1180 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201. 2 L 7 4 4F RT A20WE 20080715 EU 2008 7 15 08FDEA02044 1 20080530 A 5315 A53778807202 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND OLD TOP CAP BEAM REPAIR WITH NEW CORROSION TOP CAP REPAIR RENEWED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 20080715 WP 2008 7 15 AALA200801271 1 20080510 A 3397 CONTACT DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 463AA 49593 LGA - EMERGENCY LIGHTS AT SEAT ROWS 7 TO 11 INOPERATIVE. ADJUSTED CONTACTS FOR EMERGENCY LIGHTS AT SEAT ROWS 7 TO 11. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080715 NM 2008 7 15 AALA200801277 1 20080512 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 972AN 30097 LGA - EMERGENCY LIGHT AT SEAT 17D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 AALA200801269 1 20080510 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 355AA 24036 MIA - EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RI GHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080715 NM 2008 7 15 SWAA082889 1 20080529 A 3350 767 LIGHT BOEING 737 737705 13844SC NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 270WN 29089 DURING SCHEDULED 10Y CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082897 1 20080529 A 5753 6546430130 SKIN BOEING 737 7373H4 1384600 NM FORE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD FORE FLAP OUTBOARD UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FL AP PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082898 1 20080529 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 431WN 29845 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082899 1 20080529 A 3350 417N56014 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 438WN 29833 AFT CABIN EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082906 1 20080529 A 5753 6546435 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP UPPER INBOARD SURFACE DELAMINATED. REPAIRED FLAP PER SR M. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082907 1 20080529 A 5330 6545768 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 315, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080715 CE 2008 7 15 T652008F00000 1 20080522 A 7120 265102319 MOUNT CESSNA 208 208 2073702 CE PWA PT6 PT6A114A 52043 NE ENGINE DAMAGED E T65A K NONE O OTHER IN INSP/MAINT 1 SO 19 208JS 575 20800400 DURING AIRCRAFT CORROSION INSPECTION IT WAS NOTICED THAT THE AIR CONDITIONING CONDENSER DUCT CLAMP WAS CUTTING INTO THE ENGINE MOUNT ON THE LT TRUSS. THE TRUSS WAS ALSO RUBBING AGAINST THE CONDENSER DUCT. THERE ARE (4) CUTS MEASURING AS F OLLOWS: ( LENGTH 9/32- .020 DEEP) (LENGTH 9/32 - .020 DEEP) (LENGTH 7/32 - .010 DEEP) (LENGTH 9/16 - .032) IT WAS DETER MINED THA THE CLAMP WAS CORRECTLY INSTALLED, AND THE PN ARE IAW THE CURRENT IPC. THE CLAMP, WHEN INSTALLED ON THE ENGIN E MOUNT, RUBS AGAINST THE TRUSS AND CREATES DAMAGE. MFG WAS NOTIFIED BY E-MAIL AND RECOMMENDS USING ALUMINUM "SPEED TAP E" UNDER THE CLAMP TO REDUCE DAMAGE TO THE TRUSS. MFG HAS NOT PROVIDED AN OFFICIAL ENGINEERING ANALYSIS, AND THE RECOMM 1 H 7 1 3T 3 T NT A37CE E4EA 20080715 NM 2008 7 15 AALA200801266 1 20080509 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 758AN 32637 DFW - EMERGENCY LIGHT AT SEAT 20C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080715 NM 2008 7 15 08FDEA02135 1 20080603 A 5730 6521664 PANEL BOEING 727 727227 1384078 NM ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 LEFT WING L/E PANEL 6220, CORNER SKIN DISBONDED REPAIRED PANEL 6620 REF SRM 51-20-9 PAR 3D AND 7 PG 3-11 AND AMM 51-20- 051-7 PG 1 AND 51-20-151-7 PG1, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080715 NM 2008 7 15 08FDEA02136 1 20080603 A 5753 6521631 SKIN BOEING 727 727227 1384078 NM LT WING TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21489 LT WING O/B FLAP I/B END BY END FITTING IS DELAMED (TOP SKIN ) OF FORE FLAP REPAIRED LT WING OUTBOARD FORE FLAP REF SRM 51-40-20 PAR'S 7,14,15,18,20,21 PGS 12-62 SRM 57-50-02 FIG 4 PG 7, AND AMM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080715 NM 2008 7 15 AALA200801267 1 20080509 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 758AN 32637 DFW - EMERGENCY LIGHT AT SEAT 35G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 35G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080715 NM 2008 7 15 ASAA0842999 1 20080515 A 5753 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 LT WING UPPER OTBD FORE FLAP DENT WITH DELAMINATION ON UPPER SURFACE 63 INCHES FROM INBD SIDE. PREPARED DAMAGED AREA FA BRICATED DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 ASAA0843004 1 20080515 A 5753 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 LEFT WING INBOARD AFT FLAP OUTBOARD LOWER CORNER DELAMINATED. REMOVED DAMAGED AREA. PREPARED FABRICATED FILLER SKIN DO UBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 ASAA0843002 1 20080514 A 5755 SKIN BOEING 737 737490 1384715 NM NR 4 SPOILER LT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 LT WING NR 4 SPOILER LOWER SURFACE HAS 8 EACH SMALL DENTS AT INBOARD END. PREPARED DAMAGED AREA, FABRICATED DOUBLER FIL LER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 ASAA0842993 1 20080518 A 5755 SKIN BOEING 737 737490 1384715 NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 NR 5 SPOILER DENTED ON UPPER SURFACE CENTER TRAILING EDGE. PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B73 7 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080714 EU 2008 7 14 08FDEA02382 1 20080521 A 5542 A5547150001600 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 300 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 721FD 477 PREVIOUS REPAIR FOUND LOCATED ON RUDDER RT STA 270-869 RIB BR 2-7, OUTER SKIN. REPAIR REQUIRES EVALUATION FOR MAJOR MIN OR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR WAS FOUND IAW FEDEX EA-6-1 18158R. 2 L 7 2 4F RT A35EU 20080714 WP 2008 7 14 08FDEA02386 1 20080623 A 5310 AGA38052 STRUT DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 AFT CARGO COMPT TUNNEL AREA FOUND MODERATE CORROSION ON STRUT. 2 L 7 3 4F A22WE 20080715 NM 2008 7 15 08FDEA02331 1 20080619 A 5320 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLE NR D (THIRD LAYER). REMOVED AND RE PLACED AS PER SRM 51-31-01, VOL.II. NEW FITTING FABRICATED AS PER EA 1-5300-122494, REPAIR CLASSIFIED AS MAJOR AS PER G MM 6-2-100. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 08FDEA02342 1 20080619 A 5320 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 1 O'CL OCK POSITION) AT HOLE NR D. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 08FDEA02343 1 20080619 A 5320 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 UPPER WEB SECOND LAYER FOUND WITH CRACK INDICATION (APPROXIMATELY 4 O'CL OCK POSITION) AT HOLE NR D. CARRIED OUT REPAIR AS PER EA 1-5310-122506, PART 1. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 USAA920081229 1 20080601 A 5340 143N51578200 ATTACH FITTING BOEING 757 7572S7 1384962 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 905AW 23567 MCN - C12 - MAJOR REPAIR - NR 6109942 - INTERCOSTAL UPPER CLIP CRACKED B/S 860 TO 879 B/L 208.1 (HFEC VERIFIED). REPLACE D INTERCOSTAL UPPER CLIP B/S 860 TO 879 B/L 208. IAW SRM 51-40-02-0G. (K) 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 USAA920081218 1 20080613 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 531AU 24478 PIT - FORWARD PRESSURE BULKHEAD - MAJOR REPAIR - EA 53032 - FORWARD PRESSURE BULKHEAD SKIN HAS 2 CRACKS AT BS 178, WL 23 4, LBL 17. REPAIRED FORWARD PRESSURE BULKHEAD SKIN CRACKS AT BS 178, WL 234, LBL 17 IAW SRM 53-10-08. (K) 2 L 7 2 4F RT A16WE 20080715 NE 2008 7 15 USAA920081212 2 20080615 A 7310 3364014020 MANIFOLD AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4P NE NR 1 ENGINE FAILED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 118US 1264 FLT NR 973. CREW REPORTED HIGH ENGINE VIBRATION ON CLIMB OUT. DECLARED AN EMERGENCY & RTF MAKING AN OVERWEIGHT LANDING. PILOT REPORTED SMOKE COMING FROM NR 1 ENGINE ON SHUTDOWN, WHICH STOPPED AFTER FIRE BUTTON RELEASE. R&R LPT ACTIVE CLEAR ANCE CONTROL SYS FUEL MANIFOLD IAW MM 75-22-10-400-002. INSPECTED NR 1 ENGINE & FOUND BLADES 18 AND 17 SHINGLING, UNSHI NGLED BLADES. BLADES PLACED ON A 50 CYCLE MONITOR. COMPLIED WITH VIBRATION CHK IAW MM 71-00-00-05-210-009. PERFORMED OV ERWEIGHT LANDING INSPECTION IAW MM 05-51-11-210-090 & 31-37-00-991-003. OPS CHK GOOD. ACFT RETURNED TO SERVICE. R&R BL ADES 17, 18, 35, & 36. VIBRATION CHKS OK IAW MM 71-00-00-05-210-009. 2 L 7 2 4F 4 F RT A28NM E38NE 20080715 WP 2008 7 15 08FDEA02182 1 20080606 A 5330 AEA01151 SKIN DOUG DC10 DC1010 3022110 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 MAIN CABIN, 2 CRACKS 2 INCH AND 1.5 INCH LONG ON WEB ON FWD L3 JAMB AT STA 1254 BTWN L26 AND L27 LT SIDE. REPAIR JAMB I AW SRM 53-50-00 FIG 19 SHEET 1, 3 AND 6 VOL 1. 2 L 7 3 4F A22WE 20080715 NM 2008 7 15 08FDEA02184 1 20080606 A 5311 FRAME BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 LT WHEEL WELL STA 913.5 FRAME IS CRACKED OUT OF UPPER FILLER, END. CRACK IS WITHIN THE SHADED AREA OF JOB CARD FIGURE 1 A REPAIRED LT WHEEL WELL FRAME AT STA 913.5, PER EO 7-5310-7-4329 PART 3, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080715 EU 2008 7 15 08FDEA02185 1 20080606 A 5753 SKIN AIRBUS 310 A310203 3930313 EU ZONE 600 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RT WING O/B FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB NR 6 AND RIB NR 7 AND 2.6 IN FWD OF REAR SPAR MEASURING 4.0 IN BY 4.0 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED OUTER SKIN REPAIR ON RT WING OUTBD FLAP UPPER SKIN BETWEEN RIB NR 6 AND RIB NR 7 IAW A310-200 SRM 57-53-12, FI G 210. 2 L 7 2 4F RT A35EU 20080715 NM 2008 7 15 08FDEA02188 1 20080606 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM ZONE 200 UNKNOWN A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 906FD 27148 STA 377.7 - 440, LBL 24, SEAT TRACK REQUIRES REPLACEMENT PER CUSTOMER REQUEST. REMOVED SEAT TRACK, BS 377.7 - 440, LBL 24, IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK ASSY FROM MAT BAC 1520-792, BATCH NR 0001370089, IAW SRM 51-10-02. TRE ATED AND PRIMED THEN INSTALLED NEWLY FABRICATED SEAT TRACK ASSY, BS 377.7 - 40, LBL 24, IAW SRM 51-20-01 AND 51-40-02. THIS IS CLASSIFIED AS A MAJOR REPAIR, CATEGORY A REPAIR. THERE ARE NO FOLLOW UP TRACKING REQUIREMENTS WITH THIS REPAIR. 2 L 7 2 4F RT A2NM 20080715 NM 2008 7 15 08FDEA02193 1 20080607 A 5340 6545313 STRINGER CLIP BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 CORROSION ON STRINGER CLIPS, BS 520 STRINGER, S-4R AND S-3R REMOVED STR 3R CLIP AT STA 520 AND REMOVED CORROSION ORIG T HICKNESS .032' LOSS .005 REMAINING .027. FOUND OUT OF LIMITS. REMOVED STR 4R AND REMOVED CORROSION FOUND TO BE CRACK ED. INSTALLED 2 NEW STR CLIPS REF SRM 53-10-1 PG 2 AND 51-30-2 PG 1-3. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080715 CE 2008 7 15 MT9A00000022 1 20080512 A 3240 06111800 HOUSING CESSNA 208 208B 2073701 CE BRAKE DAMAGED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 BRAKE CYLINDER HOUSING WORN AT THE ANCHOR BOLT PASS THROUGH HOLE ALLOWING THE ANCHOR BOLT TO BE PRESSED OUT BY HAND. TH IS IS A CLOSE TOLERANCE FIT. THIS CONDITION IN THE PAST HAS CAUSED THE ANCHOR BOLT TO SHEER OFF CAUSING CATASTROPHIC DAM AGE TO THE CALIPER ASSEMBLY. TORQUE PLATE AND/OR TIRE ON THREE OF OUR AC. (K) 1 H 7 1 3T A37CE 20080715 NM 2008 7 15 USAA920081153 1 20080524 A 5712 RIB BOEING 737 7374B7 1384702 NM ZONE 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - NR 03C30557003/2, LEFT WING TANK RIB CRACKED, WS 135.5. REPAIRED LEFT WING TANK RIB, BS 135.5 IAW US AIRWAYS EA 100473. 2 L 7 2 4F RT A16WE 20080715 WP 2008 7 15 AALA200801260 1 20080508 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 459AA 49564 DFW - EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F A6WE 20080715 NM 2008 7 15 ASAA0842988 1 20080518 A 5755 SKIN BOEING 737 737490 1384715 NM SPOILERS DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 NR 6 SPOILER UPPER SURFACE HAS PROTRUDING DENTS ABOVE BLADE SEAL. PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 2008041800292 20080418 00292 NM 2008 4 18 USAA920080803 1 20080327 A 5754 65C26603102 WEDGE BOEING 737 7374B7 1384702 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A 5" X 7" DISBOND AREA ON NR 4 SLAT TRAILING EDGE WEDGE. INSTALLED REPAIR IAW SRM 51-70 -10. 2 L 7 2 4F RT A16WE 2008041800294 20080418 00294 NM 2008 4 18 USAA920080805 1 20080324 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A .7" CRACK ON FRAME AT BS 727F BETWEEN STR 8R AND STR 9R. INSTALLED REPAIR IAW SRM TR 53-10-20. 2 L 7 2 4F RT A16WE 2008041800297 20080418 00297 NM 2008 4 18 USAA920080808 1 20080328 A 5311 SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A 1" CRACK ON FRAME SUPPORT AT BS 947, STR 22L. INSTALLED REPAIR IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 2008041800301 20080418 00301 NM 2008 4 18 USAA920080812 1 20080408 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - CORROSION ON FLOORBEAM T-CAP AT BS 328, RBL 9. INSTALLED REPAIR IAW SRM 53-10-51 AND DW G 65-45812. 2 L 7 2 4F RT A16WE 20080924 EU 2008 9 24 08FDEA03334 1 20080808 A 5321 R532B363300000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 241 BF IS DAMAGED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080716 NM 2008 7 16 UPS08M52373 1 20080523 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C CENTER CARGO COMP BILGE AREA FOUND CORROSION AT STA 5-53 TO 5-123 LONGERON 47RH AS MARKED. REMOVED C ORRODED LONGERON AND SPLICE, FABRICATED LONGERON AND SPLICE AND INSTALLED IAW SAA TRAVELER 79724800001, 797244810001, AN D DWG ASA 7031 AND MD-11 SRM 53-10-00 FIG 2, 51-31-01, AND 51-21-01. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 USAA920081137 1 20080521 A 5313 DWG65C25709 STRINGER SPLICE BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - NR O3C10853043/6, CRACKED STRINGER SPLICE, BS 907, S4R. REPLACED STRINGER SPLICE, BS 90 7, S4R IAW BOEING SRM 51-10-07 AND DWG 65C25709. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 2008UALA02995 1 20080523 A 2597 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE AFT GALLEY DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 120UA 29166 AFT GALLEY CART STATION 504 HAD SMOKE - SPARKS FROM PIGTAIL, 503-505 402 ALSO GOT HOT. FOUND BENT PIN IN PIG TAIL AND F AULTY SPRING REEL. REPLACED PIGTAIL ELECTRIC CABLE CHECK GOOD. REPLACED SPRING REEL OP CHECKED GOOD. ACFT OK FOR SERVI CE 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 NE 2008 7 16 2008UALA03005 2 20080526 A 7250 TURBINE WHEEL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DAMAGED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 642UA 24424 25092 724188 NR 1 ENGINE SLOW TO IDLE. REPLACEMENT OF STARTER, IDG, FMU, AND 2.95 BV SOLENOID WERE NO HELP. ENGINE REPLACED. SHOP T EARDOWN REVEALED HEAVY HOT SECTION DISTRESS, ESPECIALLY IN THE HP TURBINE STAGE-1 AND STAGE-2 NOZZLE GUIDE VANES. THE ST AGE-1 VANES WERE ON REDUCED BORESCOPE INSPECTION INTERVAL DUE TO LE EROSION. THIS DISTRESS WAS CONSISTENT WITH THE HIGH TIME SINCE LAST ENGINE SHOP REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20080715 WP 2008 7 15 08FDEA02181 1 20080606 A 5330 AEA01151 SKIN DOUG DC10 DC1010 3022110 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 MAIN CABIN, 2 CRACKS 2 INCHES AND 1.5 INCHES LONG ON WEB ON FWD R3 JAMB AT STA 1254 BTWN L26 AND L27 RT SIDE. REPAIR JA MB IAW SRM 53-50-00 FIG 19 SHEET 1, 3, AND 6 VOL 1. 2 L 7 3 4F A22WE 20080715 EU 2008 7 15 08FDEA02142 1 20080604 A 5330 A53981600 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND SCRATCHES AND NICKS ON FUSELAGE SKIN C 79-80, BELOW P 26 LHS. REPAIR PERFORMED BY REWORK OF DAMAGED AREA IAW SRM 51-73-10, NDT FOR CRACK FREE, APPROVED BY RAS/DAHAM/4024994/2008 ISS A AND EA 6-5318-120119. 2 L 7 2 4F RT A35EU 20080715 CE 2008 7 15 MT9A00000012 1 20080423 A 2750 26220919 BELLCRANK CESSNA 208 208 2073702 CE T/E FLAP DAMAGED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 9653F 20800114 THE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE B OLT HOLE THROUGH THE MOUNTING BRACKET. (K) 1 H 7 1 3T NT A37CE 20080715 EU 2008 7 15 08FDEA02145 1 20080604 A 5753 SKIN AIRBUS 310 A310203 3930313 EU ZONE 500 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING OUTBOARD FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB NR 3 AND NR 4, MEASURING 3.9 IN BY 13.8 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT OUTER SKIN REPAIR ON LT WING OUTBD FLAP UPPER SKIN IAW A310-200 SRM 57-53-12, FIG 210, BETWEEN RIB NR 3 AND RIB NR 4. THIS I S AN AIRBUS REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080715 NM 2008 7 15 08FDEA02198 1 20080608 A 5340 654531315 STRINGER CLIP BOEING 727 727227 1384078 NM BS 660 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 CORROSION ON STRINGER CLIP AT BS 660 STRINGER S-2R REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-02 PG-2-8. THIS IS CLASSIFIED AS A MAJOR REPAIR IAW, GMM 6-2-100 PG 2 AND 3. 2 L 7 3 4F A3WE 20080715 EU 2008 7 15 S8A2008F00000 1 20080416 A 2170 1710195 BYPASS VALVE BRAERO 1000 HAWKER1000 7450005 EU WATER SEPARATOR STUCK E S8AA O OTHER O OTHER NR NOT REPORTED 1 EA 39 547LR 9377 259047 ENROUTE, AIRCRAFT N547LR AT 22,000 FT EXPERIENCED A UNCOMMANDED LOSS OF PRESSURIZATION FROM 16,000 TO 6,000 FT. THE AIRC RAFT MADE A DIVERSION, WITH AN UNEVENTFUL APPROACH AND LANDING. THIS WAS REPOSITIONING FLIGHT WITH ON PASSENGERS ON AIRC RAFT AND TWO FLIGHT CREW. MFG WAS CONTRACTED AS AGENT FOR INSPECTION AND MAINTENANCE. INSPECTED AND FOUND BYPASS VALVE S TUCK OPEN. INSTALLED NEW VALVE ASSY BYPASS VALVE ON WATER SEPARATOR. A PRESSURIZATION SYSTEM FUNCTIONAL CHECK IAW AMM 21 -30-00 WAS ACCOMPLISHED, NO OTHER DISCREPANCIES NOTED. (K) 2 L 7 2 4F RT A3EU 20080715 CE 2008 7 15 WX52008F00000 1 20080516 A 3220 50820218 SHAFT BEECH 80 65A80 1152808 CE LYC O540 IGO540* 41532 EA NLG ACTUATOR WORN E WX5A O OTHER J WARNING INDICATION LD LANDING 1 SW 13 6AQ 4383 LD214 NLG WOULD NOT DEPLOY ON APP TO LANDING. AFTER NLG REMOVAL IT WAS DISCOVERED THA THE NLG ACTUATOR DRIVE SHAFT (PN 50-820 218) INTERNAL SPLINE WAS WORN AND SHEARED. LUBE POINTS ON DRIVE SHAFT TO LUBE SPLINES TO REDUCE WEAR. (K) 1 L 7 2 3O 3 O 3A20 1E11 20080715 WP 2008 7 15 AALA200801262 1 20080508 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 459AA 49564 DFW - EMERGENCY LIGHT AT SEAT 27D HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F A6WE 20080715 NM 2008 7 15 SWAA082903 1 20080529 A 2560 P4010021 BATTERY BOEING 737 7375H4 138449D NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 AALA200801287 1 20080512 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 758AN 32637 DFW - EMERGENCY LIGHT AT SEAT 44G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 44G. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080715 NM 2008 7 15 SWAA082893 1 20080529 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 4 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER EA. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082894 1 20080529 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER EA. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082911 1 20080529 A 3350 20131A BATTERY PACK BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED A1 CHECK, MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082912 1 20080529 A 3350 20131A BATTERY PACK BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 672SW 23406 DURING SCHEDULED A1 CHECK, FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080715 EU 2008 7 15 08FDEA02115 1 20080603 A 5315 A53778807202 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON UPPER FLANGE C 27 RT BETWEEN OUTER STRUT AND CORNER FITTING. SPLICE REPAIR PERFORMED IAW SRM 53-10-1 5 FIG 207. 2 L 7 2 4F RT A35EU 20080715 NM 2008 7 15 SWAA083848 1 20080711 A 5210 6552873567 DOOR BOEING 737 7375H4 138449D NM L2 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED OTS CHECK, FOUND L2 DOOR FWD LOWER SNUBBER CUTOUT CRACKED. R&R DOOR PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083814 1 20080709 A 5753 65C30462 FLAP BOEING 737 7373H4 1384600 NM LT WING DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED SPV CHECK, FOUND LH WING INBOARD FORE FLAP DISBONDED AT INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083835 1 20080710 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED C3 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT RT MID CABIN. R&R EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 NWAA082356623 1 20080523 A 5322 SHEAR TIE BOEING 747 747251B 1384892 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 624US 21706 DURING M-CHECK FOUND CRACKS IN FLOOR TO SKIN SHEAR TIE BETWEEN BS 340-360 LT SIDE. REPAIRED PER EA 66-212930. 2 L 7 4 4F RT A20WE 20080716 SO 2008 7 16 C2XA08CL062 1 20080522 A 3350 110049 POWER SUPPLY EMB 145 EMB145XR 3260214 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11107 145654 DURING ROUTINE MAINTENANCE BOTH AFT EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 BAT TERY POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 20080716 NM 2008 7 16 ASAA0873020 1 20080522 A 5312 148A22816 BULKHEAD BOEING 737 737790 13844CN NM BS 1016 CANNING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 613AS 30163 OIL CANNING CONDITION FOUND AT WEB OF AFT PRESSURE BULKHEAD AT BS 1016 WL300 LBL7 AND S2-3L. REPAIRED IAW B737 700 SRM 53 80 08 REPAIR 2 AND EA5310 02796. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 AALA200801285 1 20080512 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 758AN 32637 DFW - EMERGENCY LIGHT AT SEAT 45G LAMP MISSING. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 45G. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080716 WP 2008 7 16 AALA200801272 1 20080510 A 3350 SWITCH DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS TRIPPED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 463AA 49593 LGA - EMERGENCY LIGHT AT OVERHEAD BETWEEN AFT LAVATORIES INOPERATIVE. CYCLED SWITCH FOR EMERGENCY LIGHT AT OVERHEAD BET WEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080716 NM 2008 7 16 2008UALA03015 1 20080526 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 EMERGENCY EXIT ROW LIGHT ON SEAT 12B LOOSE. FOUND LIGHT ASSEMBLY LOOSE. SECURED LIGHT ASSEMBLY. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080716 NM 2008 7 16 2008UALA03017 1 20080523 A 3350 79411 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE SEAT 1H INOPERATIVE A UALA O OTHER W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 EMERGENCY LIGHT INOP 1H. FOUND LIGHT ASSEMBLY LOOSE. SECURED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080716 NM 2008 7 16 2008UALA03024 1 20080525 A 3350 STRIP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 105UA 26473 AFT EMERGENCY LIGHT STRIP BROKEN OFF HALF AT SEAT 5F. 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 SO 2008 7 16 RAIA00805025 1 20080522 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 811HK 145256 PRE FLT 5461 - CID - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPAIRED THE AFFECTED LIGHT ASSEMBLY WIRING. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080716 NM 2008 7 16 ASAA0842995 1 20080518 A 5753 SKIN BOEING 737 737490 1384715 NM LT WING FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 DENT ON LT INBD FORE FLAP LOWER SKIN. SKIN IS PUNCTURED. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR DOUBLER IAW B7 37 400 SRM 51 70 10 REPAIR GENERAL. 2 L 7 2 4F RT A16WE 20080716 EU 2008 7 16 SIMA200814904 1 20080522 A 6100 UNKNOWN SAAB SF340 340B 7860101 EU MALFUNCTIONED A SIMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 21 307AE 340B307 ON FLIGHT 3229 ON TAKEOFF CREW REPORTED LEFT ENGINE PROP OIL TEMP AT 100FT AT BEGINNING OF TAKEOFF ROLL. LEFT PROP RPM WOULD NOT GO BELOW 1200 RPM AFTER ABORT TAKEOFF WHEN CONDITION LEVER AT "MIN". ALL OTHER INDICATIONS NORMAL. AIRCRAFT REMOVED FROM SERVICE. PERFORMED ENGINE RUNS FOR 20 MINUTES AT DIFFERENT POWER SETTINGS IAW GE CT7 ENGINE MM OIL TEMP ON BOTH ENGINES THE SAME AND WITHIN LIMITS PROP RPM WAS NORMAL ON BOTH ENGINES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4T RT A52EU 20080716 NM 2008 7 16 USAA920081124 1 20080514 A 5340 6545812 ATTACH ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED ATTACH ANGLE, BS 328, LBL 45. REPLACED ATTACH ANGLE, BS 328, LBL 45 IAW BOEING SRM 51-10-02 AND DWG 65-45812. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 USAA920081126 1 20080517 A 5315 SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED FLOORBEAM SUPPORT, BS 540, BL 0 - RBL 24. REPLACED CRACKED FLOORBEAM SUPPORT, B S 540, BL 0 - RBL 24 IAW BOEING SRM 51-10-20 & 51-00-00. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 USAA920081134 1 20080430 A 5320 65457835 SUPPORT ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - CRACKED VERTICAL SUPPORT ANGLE, BS 500, LBL 3. REPLACED CRACKED VERTICAL SUPPORT ANGLE, BS 500, LB L 3 IAW BOEING SRM 51-10-02. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 UPS08B52383 1 20080417 A 5311 FRAME BOEING 747 747400 13848AT NM BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:C RT BS 1180 TENSION TIE FRAME CRACKED ABOUT 0.040 INCH. RT BS 1180 TENSION TIE FRAMED REPLACED PER SRM 53-40-07, REPAIR 4. 2 L 7 4 4F RT A20WE 20080716 NM 2008 7 16 UPS08M52374 1 20080523 A 5740 FITTING DOUG MD11 MD11F 3023600 NM RT WING TE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C RT WING L/E FITTING HAS CRACKED APPROX 1 INCH BETWEEN NR 1 AND NR 2 L/E SLAT. REMOVED, FABRICATED, A ND INSTALLED FITTING IAW DWG ARB1602, MD-11 SRM 51-31-01. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 USAA920081143 1 20080520 A 5311 6547959 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 795, S22R. REPAIRED FRAME, BS 795, S22R IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 USAA920081144 1 20080517 A 5754 65C26603100 SLAT BOEING 737 7373S3 1384711 NM RT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - RIGHT WING NR 4 SLAT INBOARD END HAS DELAMINATION. REPAIRED RIGHT WING NR 4 SLAT INBOA RD END IAW US AIRWAYS EA 100445. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 NWAA082425816 1 20080529 A 3350 BATTERY PACK BOEING 757 757351 1384991 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 596NW 32996 DURING A CHECK OF THE EMERGENCY LIGHT BATTERY PACKS AS A PART OF AN OVERNIGHT WORK PACKAGE 15 EMERGENCY LIGHT BATTERY PA CKS FAILED THE CHECK OUT. MAINTENANCE FERRIED THE AIRCRAFT TO MSP WHERE THE BATTERY PACKS WERE EITHER REPLACED OR RESTO RED TO SERVICEABLE CONDITION. 2 L 7 2 4F RT A2NM 20080716 SO 2008 7 16 C2XA08TY054 1 20080528 A 5751 14569382609 BRACKET EMB 145 EMB145LR 3260212 SO LT AILERON DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16918 145397 TYS - DURING C-CHECK, THE LEFT AILERON DAMPNER BRACKET WAS FOUND DAMAGED. THE BRACKET WAS REMOVED AND REPLACED IAW EMB 145 SRM 51-40-02. THE A/C IS CURRENTLY STILL IN C-CHECK. 2 L 7 2 4T RT T00011AT 20080716 NM 2008 7 16 UPS08M52393 1 20080518 A 5754 STRUCTURE DOUG MD11 MD11F 3023600 NM RT WING SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 275UP 48774 INSPECTION TYPE:C RT WING DROOP L/E UPPER SURFACE FOUND CRACKED FROM O/B END TO I/B ABOUT 2 INCHES LONG AS MARKED. CRAC K STOP DRILLED PER SRM 57-10-00 FIG30 V.1R.40. HFEC INSP C/OUT PER D AC NDT SPM R.13 PART06-10-01-001 AT STOP DRILL HOL E FOUND NO CRACK EVIDENT. REPAIR DOUBLER FABRICATED AND HOLES PICK UP PER SRM 57-10-00 FIG 30 V.1.R40. REPAIR DOUBLER EDGE TAPERING C/OUT BY MACHINING PER SRM 57-10-0 0 FIG 30 V.1R.40. RHW DROOP L/E INSTALLED PER AMM27-80-10 REV.61. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 200805301 1 20080527 A 3251 1855A000004 STEERING SYS EMB ERJ170 ERJ170100SE 3260406 NM NLG MALFUNCTIONED A UHLA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 648RW 17000068 FLIGHT 7658 MCI TO ORD CREW REPORTS NWS FAIL ON APPROACH THEY CYCLED CB B25 ON TAXI IN AND FAULT CLEARED. MAINTENANCE R EPLACED THE NWS MODULE FOR PREVENTATIVE MAINTENANCE. 2 L 7 2 4F RT A56NM 20080716 EU 2008 7 16 08FDEA02048 1 20080530 A 5310 A53973100200 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON BEAM 10 C 67-69,P 45 RT, BCD CUT OUT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080716 SO 2008 7 16 C2XA08RI078 1 20080526 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 27962 145110 FLIGHT 2623 - YOW - FLIGHT CREW REPORTED STRANGE FUEL SMELL IN CABIN ROWS 8/9. CONTRACTED MAINTENANCE PERFORMED EVALUAT ION AND COULD NOT DUPLICATE ANY ODOR. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20080716 EU 2008 7 16 08FDEA02059 1 20080528 A 5347 SEAT TRACK AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 CABIN FLOOR, SEAT-TRACK Y-1959 DAMAGED AT FR 29. 2 L 7 2 4F RT A35EU 20080716 NM 2008 7 16 08FDEA01978 1 20080523 A 5414 311N504651 SKIN PANEL BOEING 757 75727B 1384921 NM ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 916FD 24137 CORROSION ON PYLON NUMBER ONE LT INNER STRUT SKIN NEAR ACCESS PANEL 433BL CUTOUT, PPS 124.76. EVALUATE AND RECTIFY. RE PLACED PYLON NUMBER ONE LT INNER STRUT SKIN NEAR ACCESS PANEL 433BL CUTOUT IN ACCORDANCE WITH BOEING DRAWING 311N5002 ID 0013 REVISION E, 311N5046 ID 00002 REVISION A AND B757-200 SRM 51-10-02 REVISION 93. REPAIR CLASSIFIED AS MAJOR PER F EDEX GMM 6-2-100. 2 L 7 2 4F RT A2NM 20080716 NM 2008 7 16 GTIA0800067 1 20080425 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 505NK 2485 FOUND CORROSION ON AFT FUSELAGE FLOORBEAM Y765 BETWEEN FR64 AND FR66. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 20080716 NM 2008 7 16 08FDEA02133 1 20080603 A 5310 652355530 BEAM BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 KEEL BEAM END TOP ATTACH ANGLE ON BACK OF BULKHEAD AT FS 740 HAS CORROSION ON TOP SIDE OF ANGLE AT RBL 4, ABOVE CONTROL CABLE PULLEY WHEELS. REMOVED AND REPLACED ANGLE REF SRM 51-30-02. FABRICATED REPLACEMENT ANGLE ON N/R N00726. FLAP P EENED, ALODINED, PRIMED AND INSTALLED. REF SRM 51-10-2, SOPM 20-10-03. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080716 EU 2008 7 16 08FDEA02260 1 20080612 A 7830 10AT4731 SWITCH AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4E1 52054 NE THRUST REVERSER WORN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 452FE 313 715438 ON TAKEOFF FROM CDG GOT REVERSE UNLOCK LIGHT ON ECAM ALSO MATCHED WENT TO NR 2 ENG REVERSE. LIGHT WENT OUT THEN CAME BA CK ON WITH POWER ADVANCE. LEFT NR 2 AT IDLE AND CAME BACK TO LAND ASAP CDG. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-3 0-01-C CATEGORY: C EXPIRATION: 22JUN08 (NO BUFFETING REPORTED). PERFORMED SEVERAL TIMES EXTENSION/RETRACTION OF THE THR UST REVERSER. INSPECTED CABLES FOR NO STRESS. CHECKED SWITCHES S303 AND S307: FOUND S3 07 INSIDE SPRING WEAK RD AND RD S307 AS PER MM78-3 1-18-4 03. TRIED SEVERAL TIMES THRUST REVERSER, NO ABNORMALITIES FOUND. MEL CLOSED/STICKER REMO VED. 2 L 7 2 4F 4 F RT A35EU E3NE 20080716 NM 2008 7 16 08FDEA02302 1 20080618 A 5330 APB74451 SKIN DOUG MD11 MD11F 3023600 NM BS 1371 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 598FE 48597 AFTER REMOVAL OF LEFT OVERWING FLOOR PANELS FOR WIRING INSPECTION ACCESS FOUND CENTER WING TANK LEFT UPPER TORQUE BOX SK IN APPROXIMATELY AT STA Y1371, XCW113 WITH EXFOLIATION CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA NR 15710-122479, T ITLE: WINGS CENTER WING AFT UPPER SKIN CORROSION REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 DHL2008764529 1 20080527 A 5210 SKIN BOEING 727 727264 138408M NM BS 344 BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C CHECK, L1 DOOR INNER SKIN BENT FWD LOWER CORNER. REPAIRED IAW B727 SRM 51-40-2 AND ASTAR EVA B52-00073 REV1. 2 L 7 3 4F A3WE 20080716 NM 2008 7 16 DHL2008764530 1 20080527 A 5754 RIB BOEING 727 727264 138408M NM KRUEGER FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C CHECK, NR 5 K-FLAP ACTUATOR SIDE MOUNTING RIBS I/B AND O/B CRACKED. REPAIRED RIBS IAW BOEING DWG 65-16269 RE VC MATERIAL 2024T3 .063" DIM 7" BY 6 1/8 INCH PO NR 9006773. 2 L 7 3 4F A3WE 20080716 EU 2008 7 16 08FDEA02121 1 20080603 A 5210 A53980210206 WEB AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORRODED WEB AT PAX DOOR 4 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080716 WP 2008 7 16 DHL2008807522 1 20080501 A 5100 NONE DOUG DC8 DC873F 302199F WP NONE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 REMOVE AND REPLACE EXISTING REPAIR AT FUSELAGE STA 1260 LONGERON 31L TO 29L WITH A PERMANENT TYPE REPAIR PER SRM OR APPR OVED DATA. INDICATE TYPE OF REPAIR, REINSPECTION INTERVAL AND NEXT REQUIRED INSPECTION (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1,4,5. REMOVED EXISTING REPAIR NOT ACCORDING TO SRM IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL7075T6 0.125") FILLER (AL7075T6 0.100") AND (2EA) INTERNAL FING ER DOUBLER (AL7075T6 0.050") IAW SRM 53-2-1 FIG 7 SHEET 1, 4, 5, SRM 53-4-1 FIG 17A SHEET 1 ITEM "C". CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIG 7 SHEET 1, 4, 5, SRM 51-1-2 2 L 7 4 4F RT 4A25 20080716 WP 2008 7 16 DHL2008807515 1 20080505 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP BS 880 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 LT MLG DOOR JAMB ZEE CRACKED STA 880.000. REMOVED CRACKED JAMB ZEE IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA I AW SRM 51-1-8B. INSTALLED NEW JAMB ZEE IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 20080716 WP 2008 7 16 DHL2008807514 1 20080506 A 5740 FITTING DOUG DC8 DC873F 302199F WP RWS 421 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 RT WING T/E FITTING CRACKED AT STA XRS 421.000. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 2008UALA02877 1 20080517 A 2611 SQUIB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 571UA 26681 L ENG NUMBER 2 SQUIB TEST FAIL. SUPPLEMENTAL DATA UPDATE CAUSE, SWITCH S2 WAS DIRTY. CLEANED SWITCH S2 ON M32 PANEL, R ESET CIRCUIT BREAKER C786 ON P6 PANEL, SQUIB TEST OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080716 SO 2008 7 16 SIMA200815104 1 20080525 A 5320 SILL EMB 135 EMB135KL 3260302 SO SERVICE DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 828AE 5000 145604 DURING A MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED DAMAGED SILL. CLEANED AND ALODINED N EW SLLL AND INSTALLED IAW EMB 145 SRM (SRM EMB-14511142 REV 39) CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20080716 NM 2008 7 16 SB08035 1 20080529 A 3350 20121 POWER SUPPLY BOEING 737 737401 1384701 NM EMERGENCY LIGHTS INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 421US 23988 BDL - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT THE LAST TWO ROWS OF LEFT SEATS, L2 DOOR OVERHEAD, R2 DOOR EXTERIOR L IGHT AND RIGHT AFT BULLNOSE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT RIGHT EMERGENCY LIGHT BATTERY CHARGER /POWER SUPPLY PER MM 33-51-51-2. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20080716 SO 2008 7 16 C2XA08CL064 1 20080530 A 3260 8005701 SENSOR EMB 145 EMB145LR 3260212 SO LT MLG FAULTY A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 11539 145536 CLE FLIGHT NR 2356, THE CREW REPORTED A LANDING GEAR AIR/GND FAIL MESSAGE AFTER TAKEOFF AND GEAR RETRACTION. THE AIRCRA FT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT GEAR WOW PROXIMITY SENSOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20080716 NM 2008 7 16 UPS08M52545 1 20080520 A 5313 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM BS 1676 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C CTR CARGO AT STATION 1676 LONGERON 46 RT LONGERON SPLICE DOUBLER FOUND CRACKED AS MARKED. CRACK SPLIC E REMOVED PER SRM 51-33-01 VII REV 35. REPAIR LONGERON SPLICE FAB PER SRM 53-10-00 FIG 2 VI REV 35. NEW SPLICE REWORKE D SMOOTH AND REPROTECTED PER SRM 51-21-01 VII REV 35. FPI C/O PER DPS 4.707 REV AW ON NEW SPLICE AND FOUND NO CRACK EVI DENT. SPLICE REPROTECTED PER SRM 51-21-01 V II R35. NEW SPLICE INSTALLED PER SRM 51-33-01 VII REV 35. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 UPS08B52376 1 20080327 A 5311 FRAME BOEING 747 747400 13848AT NM BS 1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:C LT BS 1160 TENSION TIE FRAME WEB CRACKED ABOUT 0.400 INCH. LT BS 1160 TENSION TIE FRAME WEB REPLACED PER SRM 53-40-07 REPAIR 3. 2 L 7 4 4F RT A20WE 20080715 WP 2008 7 15 AALA200801265 1 20080509 A 7312 VALVE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE FUEL HEAT INOPERATIVE A AALA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 494AA 49732 709948 IAD INFLIGHT T1097/09MAY - CREW REPORTED NUMBER TWO ENGINE OIL TEMPERATURE LIGHT AND FUEL TEMPERATURE LIGHT ILLUMINATED IN FLIGHT. CREW SHUT NUMBER TWO ENGINE DOWN. RETURNED TO IAD AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME APPROXIM ATELY 15 MINUTES. REPLACED RIGHT ENGINE FUEL HEAT VALVE. CHANGED OIL AND OIL FILTER. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F 4 F A6WE E9NE 20080715 2008 7 15 SWAA083852 4 20080709 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083815 1 20080710 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 469WN 33859 DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. R&R BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20080715 2008 7 15 SWAA083841 4 20080710 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080716 WP 2008 7 16 DHL2008807533 1 20080506 A 5230 STRUCTURE DOUG DC8 DC873F 302199F WP CARGO DOOR MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 807DH 91019 45990 "A" CARGO DOOR FWD LWR JAMB CORNER REPAIR NOT IN ACCORDANCE WITH DRAWING NR SR08530019 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2005-18-07, S/B DC8 53-078, DOUGLAS DWG SR08530019 S750776. REMOVED REPAIR NOT ACCORDING TO DOUGLAS DWG SR 08530019 IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK, NO CORROSION F OUND. ENCLOSED SMN FORM 242-2. FABRICATED REPAIR DOUBLER (AL7075T6 0.090") REPAIR TRIPLER (AL7075T6 0.125") AND FILLER (AL7075T6 0.071") IAW DOUGLAS DWG NR SR08530019. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. I NSTALLED REPAIR PARTS IAW DOUGLAS DWG SR08530019, SRM 51-1-11, SRM 51-1-126, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQ 2 L 7 4 4F RT 4A25 20080716 WP 2008 7 16 DHL2008807532 1 20080508 A 5410 COWL DOOR DOUG DC8 DC873F 302199F WP NR 3 NACELLE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 NR 3 ENG RT COWL DOORS EXTERIOR SHOWS TWO DENTS AT 5 O'CLOCK POS STA YN 160.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-2-8 PAR 17 FIG 8, TR NR 71-44 DATED 11-20-07. CUT OUT DAMAGED SECTION IAW SRM 71-2-8 PAR 17 PG 29 FIG 8 TR N R 71-44. FABRICATED NEW EXTERNAL SKIN SEGMENT, (2EA) INTERNAL SPLICE DOUBLERS AND SPLICE DOUBLER ALL FROM AL2024T3 0.03 2 INCH AND NEW CORE SEGMENT P/N 5056-1000 IAW SRM 71-2-8 PAR 17 FIG 8, TR NR 71-44. HEAT TREATED FROM 2024-T3 TO 2024-T 62 IAW SRM 51-1-1 PG 1-13-17. INSTALLED AND BONDED REPAIR PARTS WITH RIVETS MS20426AD4 AND ADHESIVE FM300-2 IAW SRM 71- 2-8 PAR 17 TR NR 71-44, SRM 51-1-21. 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 USAA920081152 1 20080516 A 5340 6935352U14 STRINGER CLIP BOEING 737 7374B7 1384702 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - NR 03C10753045/7, CRACKED STRINGER TIE CLIP, BS 807, S4R. REPLACED STRINGER TIE CLIP, B S 807, S4R IAW B737 SRM 51-20-10 AND 51-00-00. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 ASAA0842994 1 20080518 A 5753 SKIN BOEING 737 737490 1384715 NM RT WING FLAP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 SEVERAL DENTS ON RT INBD FORE FLAP SKIN PUNCTURED. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR GENERAL. 2 L 7 2 4F RT A16WE 20080716 EU 2008 7 16 08FDEA02035 1 20080530 A 5340 A53773644 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORRODED CORNER FITTING AT C 27 LT AND RT IN FWD CARGO COMPARTMENT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW S RM 51-72-10. 2 L 7 2 4F RT A35EU 20080716 NM 2008 7 16 AALA200801300 1 20080514 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 781AN 29586 MIA - EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080716 NM 2008 7 16 AALA200801273 1 20080511 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 965AN 29544 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR HAS BROKEN LENS. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RIGHT NU MBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 AALA200801295 1 20080513 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 773AN 29583 DFW - EMERGENCY LIGHT AT OVERHEAD LAVATORY AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OV ERHEAD LAVATORY AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080716 NM 2008 7 16 08FDEA02023 1 20080529 A 5330 655456945 SKIN BOEING 727 727227 1384078 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 490FE 21493 RT FUSELGE EXTERNAL 2 EA OLD REPAIRS AT STA 416 BETWEEN STR 21R AND STR 22R HAVE DENTS. 2 L 7 3 4F A3WE 20080716 NM 2008 7 16 2008UALA02986 1 20080524 A 5311 ATTACH FITTING BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 FUSELAGE FRAME 360 LEFT AFT SIDE OUTBOARD ATTACH CLIP CRACKED AT STR 13L. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACE D CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 20080716 EU 2008 7 16 08FDEA02118 1 20080603 A 5330 A53985240204 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND OLD BUSHING REPAIR ON FUSELAGE SKIN C 83, P 5 LT WITHOUT ANY OLD DOCUMENTATION. REPAIR PERFORMED BY REMOVING OF BUSHING, CHECK THE HOLE AND INSTALL BUSH IAW SRM 53-10-12 FIG 221. 2 L 7 2 4F RT A35EU 2008041800302 20080418 00302 NM 2008 4 18 USAA920080813 1 20080331 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - CORROSION ON FLOORBEAM AT BS 344, RBL 12 - LBL 12. INSTALLED REPAIR IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2008041800313 20080418 00313 NM 2008 4 18 USAA920080830 1 20080403 A 5312 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 23634 CLT - MAJOR REPAIR - C22 CHECK - A 1" CRACK ON WEB AT BS 178, WL 187, BL 0. INSTALLED DOUBLER REPAIR IAW SRM 53-10-08 R EPAIR 2. 2 L 7 2 4F RT A16WE 2008041800314 20080418 00314 NM 2008 4 18 USAA920080831 1 20080402 A 5312 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 23634 CLT - MAJOR REPAIR - C22 CHECK - TWO EACH CRACKS (.25") ON WEB EXTENDING FROM FASTENER HOLES AT BS 178, WL 234, RBL 9.5. INSTALLED DOUBLER REPAIR IAW SRM 53-10-08 R2 FIG 201. 2 L 7 2 4F RT A16WE 2008041800316 20080418 00316 NM 2008 4 18 USAA920080833 1 20080328 A 5312 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 23634 CLT - MAJOR REPAIR - C22 CHECK - TWO EACH 1" CRACKS ON WEB AT BS 178, WL 213, LBL 5.5. INSTALLED DOUBLER REPAIR IAW SRM 53-10-08 FIG 201. 2 L 7 2 4F RT A16WE 2008042100014 20080421 00014 NM 2008 4 21 2008UALA02135 1 20080411 A 5311 FRAME AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 854UA 1731 AFT CABIN FRAME 69 GOUGED RT SIDE AT -Y1162. MAJOR REPAIR ACCOMPLISHED: INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042100018 20080421 00018 NM 2008 4 21 2008UALA02064 1 20080409 A 3350 60B4005715 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 RIGHT SIDE EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP. TWO MOST FWD ASSY'S. REPLACED LIGHT ASSEMBLY OPS CHECK NORMAL . AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041800060 20080418 00060 NM 2008 4 18 ASAA0852806 1 20080405 A 2131 8243921002 CONTROLLER BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA K NONE J WARNING INDICATION NR NOT REPORTED 1 NM 02 557AS 35176 DURING APU SHUTDOWN PRESSURIZATION "AUTO" FAIL LIGHT ILLUMINATED. VERIFIED FAULT LIGHT. C/W BITE ON NR 2 PRESSURE CONT ROLLER. FAULTED FOR POWER LOSS. RESET, CHECKS NORMAL. 2 L 7 2 4F RT A16WE 2008041800067 20080418 00067 SO 2008 4 18 C2XA08SH06208 1 20080408 A 2560 P2070005120 CHARGER EMB 135 EMB135LR 3260305 SO CABIN DEFECTIVE A C2XA L ABORTED APPROACH B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14516 145323 SHV - FLIGHT 2148 - PILOT REPORTS ELECTRICAL SMELL COMING FROM AFT AREA OF AIRCRAFT CABIN WHEN PERFORMING POST FLIGHT IN SPECTION. MAINTENANCE REMOVED & REPLACED AFT FLIGHT ATTENDANT FLASHLIGHT CHARGER IAW EMB 135 AMM 33-50-16. OPS CHECK G OOD. 2 L 7 2 4F RT T00011AT 2008041800069 20080418 00069 WP 2008 4 18 ABXA080120 1 20080405 A 2740 920710296 RELAY DOUG DC9 DC932F 3022067 WP E&E BAY DEFECTIVE A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 23 909AX 1105 47148 PRIMARY TRIM CIRCUIT BREAKER TRIPPED WHILE SETTING TAKEOFF TRIM. WHILE MECHANIC WAS TROUBLESHOOTING PRIMARY TRIM, HEAVY SMOKE PRODUCED THROUGHOUT FRONT & REAR CABIN. CREW CONDUCTED EMERGENCY SHUT DOWN & EVACUATED AIRCRAFT. FOUND RELAY R2 0-15 BURNT. REPLACED RELAY R20-15 IAW DC9 AMM 27.40.04. 2 L 7 2 4F A6WE 2008041800103 20080418 00103 NM 2008 4 18 USAA920080794 1 20080310 A 5320 146N53181 PLATE BOEING 757 7572G7 1384963 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 908AW 24233 MCN - MAJOR REPAIR - C3 CHECK - LEVEL 2 CORROSION ON AFT GALLEY FLOOR PLATE, BS 1680 - BS 1720, LBL 50 - RBL 50, WL 208. REPLACED AFT GALLEY FLOOR PLATE, BS 1680 - BS 1720, LBL 50 - RBL 50, WL 208 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008041800140 20080418 00140 NM 2008 4 18 HNAA0800126 1 20080406 A 2435 230088008 STARTER GEN DHAV DHC8 DHC8102 2809003 NM NR 2 DEFECTIVE A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 940HA 8157 62 156 IN FLIGHT ON CLIMBOUT NR 2 DC BUSS FAULTED, RESET BUSS AND RETURNED TO FIELD. REMOVED AND REPLACED NR 2 STARTER GEN PER WC 24-30-02. 2 H 7 2 4T RT A13NM 2008041800144 20080418 00144 NM 2008 4 18 ABXA080122 1 20080407 A 3350 20131A BATTERY PACK BOEING 767 767281 1385109 NM CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 789AX 23022 AT STA RNO, MAINTENANCE FOUND EMERGENCY LIGHTS INOP. BOTH PRIMARY AND SPARE BATTERY PACK DEAD. REMOVED AND REPLACED PR IMARY AND SPARE BATTERY PACKS AND BATTERY CHARGERS IAW B767 AMM 33-51-07-02. EMERGENCY LIGHTS OPS CHECKED GOOD. ALL PA RTS REMOVED WERE 'F' CLASS. 2 L 7 2 4F RT A1NM 2008041800159 20080418 00159 SO 2008 4 18 C2XA08IA109 1 20080409 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17108 145655 IAH - FLIGHT 2832 DURING POST FLIGHT INSPECTION THE CREW REPORTED THE MID CABIN CEILING EMERGENCY LIGHT TO BE INOPERATIV E. MAINTENANCE REMOVED AND REPLACED THE NUMBER SIX EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 2008041800200 20080418 00200 NM 2008 4 18 USAA920080851 1 20080403 A 5320 FLOOR SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT - MAJOR REPAIR - C4 CHECK - CORROSION ON FLOOR SUPPORT AT BS 1640 - 1661, WL 208.1, BL 0. REPLACED SUPPORT IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 2008041800229 20080418 00229 NM 2008 4 18 USAA920080858 1 20080408 A 5754 SLAT BOEING 757 757225 1384959 NM RT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT - MAJOR REPAIR - C4 CHECK - NR 6 L/E SLAT HAS 4" DELAMINATION. INSTALLED DOUBLER REPAIR IAW SRM 51-70-10. 2 L 7 2 4F RT A2NM 2008041800244 20080418 00244 NM 2008 4 18 USAA920080865 1 20080412 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 A 3 INCH SKIN CRACK ON LEFT SIDE OF FUSELAGE AT BS 927, BELOW S25L. REPAIRED IAW SRM 53-00-01 REPAIR 31, PG 244. 2 L 7 2 4F RT A16WE 2008041800279 20080418 00279 SO 2008 4 18 C2XA08IA111 1 20080414 A 3350 78241 INVERTER EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15926 145005 OKC, FLIGHT 2033, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE EMERGENCY LIGHT ON THE LEFT CABIN EXIT DOOR AT SEAT 12A WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 4 EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008041800281 20080418 00281 2008 4 18 BB08059 4 20080412 A 2565 D31041147 SLIDE BOEING 757 7572B7 1384964 NM R3 DOOR LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 938UW 38113 8 27246 PHL - THE R3 DOOR EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE WAS LOW. MAINTENANCE REPLACED THE EMERGENCY ESCAPE SLIDE AT DO OR R3. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 2008041800312 20080418 00312 NM 2008 4 18 USAA920080828 1 20080408 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A 1" CRACK ON ANGLE AT BS 500C, STR 22L. REPLACED ANGLE IAW SRM 51-70-11. 2 L 7 2 4F RT A16WE 2008042100006 20080421 00006 NE 2008 4 21 2008UALA02127 2 20080413 A 7261 OIL SYSTEM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT ENGINE LEAKING A UALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 775UA 26947 AT SHUTDOWN OF THE RIGHT ENGINE ABOUT A PINT OF OIL CAME FROM THE BACKUP GEN-MAIN GEARBOX DRAIN MAST. EICAS SHOWS RT BU G SVC. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042100013 20080421 00013 NM 2008 4 21 2008UALA02134 1 20080411 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 854UA 1731 FUSELAGE SKIN GOUGED FWD OF FRAME 24 BETWEEN STR 43L AND 42L. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042100026 20080421 00026 NM 2008 4 21 2008UALA02072 1 20080409 A 5311 146T1209 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1263 S39L/R PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 AFT PIT STA 1263 FRAME WEB HAS A PUNCTURE ABOVE STR 39L AND 39R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SR M 51-70-13 AND SRM 51-40-02. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042100028 20080421 00028 2008 4 21 2008UALA02136 4 20080412 A 2565 SQUIB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE NONE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 571UA 26681 RIGHT NUMBER ONE EMERGENCY ESCAPE SLIDE DOES NOT TEST ON SQUIB PANEL. TESTED SQUIB 20 TIMES, OPS CHECKS GOOD EVERY TIME. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042100045 20080421 00045 NM 2008 4 21 2008UALA02001 1 20080406 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE SEATS 16HJ & 23H INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 EEL LIGHTS AT SEATS 16HJ, AND 23HJ ARE IN-OP. SUPPLEMENTAL DATA UPDATE REPLACED STRIPS. CHECKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042100052 20080421 00052 NM 2008 4 21 2008UALA02036 1 20080409 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 809UA 825 FOUND BEAM 90 CORRODED WHILE ACCOMPLISHING EQ3700 CALLOUT. REMOVED BEAM. 7 BEAMS 90,140 AND 145 INSTALLED AS A UNIT. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042100053 20080421 00053 EU 2008 4 21 2008UALA02008 1 20080406 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 416UA 479 CREW O2 LOW, NEEDS SERVICE (1520PSI). SUPPLEMENTAL DATA UPDATE CAUSE, UNKNOWN. SERVICED CREW O2, NO LEAKS WERE NOTED A T THE TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042100054 20080421 00054 2008 4 21 IXXA080012O 4 20080411 A 3414 INDICATOR DOUG DC8 DC871F 302199D WP AIRSPEED FAILED A IXXA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 11 820BX 90374 1295 46065 DURING CLIMB-OUT FROM KTOL, THE CREW NOTICE V1=134 NOTICE HESITATION IN AIR SPEED INCREASE AT VR AT 151 AIRSPEED FAILED TO INCREASE IN EXTERNAL MODE. WHEN SWITCH TO STANDBY AIRSPEED INDICATE 220KTS WHICH MATCHED TO FMS SPEEDS. THE CREW RE TURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND PITOT STATIC LINE AT DRAIN BROKEN. REPLACE D PITOT LINE OPERATIONAL CHECK GOOD IAW DACO DC-8 MAINTENANCE MANUAL 34-12-0, AND ATI JOB CARD 34.12.1. AIRCRAFT WAS R ETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2008042100077 20080421 00077 NM 2008 4 21 CALA0800324 1 20080411 A 5340 65C161215 BRACKET BOEING 737 737524 1384721 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 BRACKET AT STA 312 LBL 54" FOUND CORRODED. REMOVED & REPLACED 65C16121-5 GIRT BAR FITTING BRACKET REF SRM 51-10-02 & 51 -40-02 (STA 312, LBL 54"). 2 L 7 2 4F RT A16WE 2008042100078 20080421 00078 NM 2008 4 21 CALA0800316 1 20080410 A 5210 50794530 INTERCOSTAL BOEING 737 737524 1384721 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 46625 27529 L1 DOOR WEB CRACKED I/B OF TORQUE UPPER END (ONE BAY ABOVE TORQUE BOX). REMOVED AND INSTALLED NEW INTERCOSTAL AND CLOSE D INNER SKIN REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 2008042100084 20080421 00084 EA 2008 4 21 COMA0860208 1 20080404 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 597SW 7293 CABIN ROW 2 EMERGENCY CEILING LIGHT FAILED TO ILLUMINATE. DEFERRED PER MEL 33-51-01-2. 2 L 7 2 4F RT A21EA 2008042100103 20080421 00103 EA 2008 4 21 COMA0860219 1 20080410 A 5730 601R100461 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 958CA 30170 7111 LEFT WING PLANK CRACKED ON BOTTOM SIDE JUST O/N OF JACK PAD. PERMANENT REPAIR OF THE LOWER WING PLANK WS 148.019 LEFT I AW REO 601R-57-21-130. 2 L 7 2 4F RT A21EA 2008042100108 20080421 00108 EA 2008 4 21 COMA0860218 1 20080409 A 3230 17051101 UPLOCK CNDAIR CL600 CL6002B19 1900309 EA LT MLG FAILED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 973CA 29294 7146 FLIGHT 5175 - DURING APPROACH INTO MSP SELECTED GEAR DOWN AND RECEIVED LEFT MLG DISAGREE MESSAGE. DURING GO-AROUND AFTE R APPROX 1 MIN THE LEFT MLG SHOWED DOWN AND LOCKED GIVING 3 GREEN INDICATION. AIRCRAFT LANDED SAFELY. REMOVED AND REPL ACED LEFT MLG UPLOCK ASSEMBLY. 2 L 7 2 4F RT A21EA 2008042100122 20080421 00122 NM 2008 4 21 CALA0800315 1 20080409 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM EMERGENCY LIGHT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 77066 29461 BUSINESS FIRST EMERGENCY AISLE LIGHTS INOP. REMOVED & REPLACED POWER SUPPLY UNIT & BATTERY PER AMM 33-51-07-022-005. 2 L 7 2 4F RT A1NM 2008042100123 20080421 00123 NM 2008 4 21 08FDEA01451 1 20080415 A 2697 221W5148509 WIRE HARNESS DOUG MD11 MD11F 3023600 NM FIRE DETECTION SHORTED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 527FE 48601 ON CLIMB-OUT, "FIRE DETECT 2 FAIL" WHICH GAVE US NOT DETECTION CAPABILITY ON ENG NR 2. AIR-TURN-BACK TO LAX, EXTINGUISH ED ON TURN BACK TO LAX. FOUND WIRES CHAFING ON LEFT T/R LOOP. SPLICED LEFT LOOP A AND B WIRES. LOOP A CHECKS NORMAL, FDCU FAULTS LOOP B LEFT SIDE. REMOVED LT A/B LOOP HARNESS FROM RESPONDERS AND FOUND THAT EVEN WITH THE NEW SPLICES, THE HARNESS SHOWED SHORT TO SHIELD/GROUND ON BOTH A/B. DECIDED TO REMOVE AND REPLACE ENTIRE HARNESS. REMOVED OLD HARNES S. PARTIALLY INSTALLED NEW HARNESS. INSTALLED NEW LT FIRE LOOP HARNESS. PERFORMED FIRE DETECTION BITE TEST. ALL TE STS PASSED. 2 L 7 3 4F RT A22WE 2008042100138 20080421 00138 NE 2008 4 21 TRBA2008043 2 20080418 A 7200 ENGINE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE NR 2 MALFUNCTIONED A TRBA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 29 407AT 407 AFTER TAKEOFF LEVEL AT 6000 FT, NR 2 ENG INTERMITTENT OVERTORQUE. SHUT DOWN THE ENGINE AS PER AOM VOL 2. PERFORMED SEV ERAL ENGINE RUNS (RT) AT ALL POWER SETTINGS AND NO TORQUE SURGE OR OVERTORQUE NOTICED. ALSO VERIFIED RT ENGINE INTERCOM PRESSOR BLEED VALVE AND FOUND OK. ALSO PERFORMED ENGINE GROUND OPERATIONAL CHECK AS PER WORK CARD NR 055007-CS-20000-00 1 AND FOUND ALL PARAMETERS WITHIN LIMITS. MANUALS USED JIC NR 72-00-00 AND PWC MM NR 72-00-03. FCF PASSED OK. 2 H 7 2 4T 4 T RT A53EU E20NE 2008042100146 20080421 00146 SO 2008 4 21 SWIA200819484 1 20080228 A 5310 WINDOW POST EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 251YV 120251 RIGHT SIDE WINDOW FORWARD POST IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIRS ON WINDOW POST IAW SB 120-63-0072. 2 L 7 2 4T RT A31SO 2008042300002 20080423 00002 NM 2008 4 23 2008UALA02203 1 20080414 A 2432 CHARGER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE MASTER BATTERY INOPERATIVE A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 226UA 30226 BATTERY CHARGER MESSAGE ON EICAS. FOUND FAULTY BATTERY CHARGER AND BATTERY. REPLACED BATTERY AND BATTERY CHARGER. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042300007 20080423 00007 NM 2008 4 23 2008UALA02177 1 20080415 A 5710 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT WING DAMAGED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 202UA 24717 BIRD STRIKE LEFT WING. DAMAGE TO THE LEFT HAND WING OUTBOARD FIXED FLAP FAIRING ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042300020 20080423 00020 EA 2008 4 23 MASA200800302 1 20080409 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77286 7286 ASH 2728 PHX - SEVERAL STRIPS OF FLOOR PATH LIGHTING INOP. MX RESECURED A LOOSE CONNECTOR TO THE FLOOR PATH LIGHTING. 2 L 7 2 4F RT A21EA 2008042300030 20080423 00030 EA 2008 4 23 MASA200800305 1 20080404 A 2910 750006000D HYDRAULIC LINE CNDAIR CL600 CL6002B19 1900309 EA NLG WW LEAKING A MASA O OTHER K FLUID LOSS CR CRUISE 1 SW 07 77286 17781 7286 FLT 2761 SLC-PHX. HYD 3 LOW PRESSURE WARNING FOLLOWED BY TOTAL LOSS OF HYDRAULIC FLUID. AC DECLARED EMERGENCY. CONTRA CT MX FOUND HYD LINE LEAKING IN NOSE WHEEL AREA. REMOVED AND REPLACED SELECTOR VALVE AND BLED HYDRAULICS, OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2008042300036 20080423 00036 NM 2008 4 23 2008UALA02211 1 20080416 A 5551 LUG BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZONTAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 LT HORIZONTAL STABILIZER FWD SPAR UPPER LUG HAS EVIDENCE OF CORROSION. MAJOR REPAIR ACCOMPLISHED: HONED LUG BORE TO DIM ENSION OF 1.2537". SPOT FACED FWD AND AFT FACES TO FINAL DIMENSION OF 1.042". ACP'D REPAIR AND INSTALLED OVERSIZED SLEE VE AND BUSHINGS. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042300039 20080423 00039 NM 2008 4 23 2008UALA02213 1 20080416 A 5210 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 L2 DOOR UPPER ARM CUT-OUT REQUIRES DOUBLER TO BE INSTALLED. MAJOR REPAIR ACCOMPLISHED: PERFORMED INSURANCE CUT & INSTAL LED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300042 20080423 00042 NM 2008 4 23 2008UALA02216 1 20080416 A 5311 FRAME SPLICE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1520 GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 AFT PIT STA 1520 FRAME SPLICE GOUGED BETWEEN STR 22R AND 24R. REMOVED DAMAGE FABRICATED AND INSTALLED RPR PER SRM 53-00 -07 RPR 5 TABLE II ZONE 1. RPR IS A CAT B RPR AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS STARTING AT 50,000 TO TAL FLIGHT CYCLES AND 12,000 FC THERE AFTER. CURRENT FC= 14767 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300052 20080423 00052 NM 2008 4 23 2008UALA02218 1 20080416 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1500 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 AFT PIT STA 1500 STR 26L FRAME HAS 1 DENT. REMOVED DAMAGE FABRICATED AND INSTALLED RPR PER SRM 53-00-07 RPR 5 TABLE II ZONE 1. RPR IS A CAT B RPR AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS STARTING AT 50,000 TOTAL FLIGHT CYCLES AND 12,000FC THERE AFTE R. CURRENT FC= 14767. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300057 20080423 00057 NM 2008 4 23 2008UALA02222 1 20080416 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS1400 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 592UA 28143 AFT PIT STA 1400 STR 26L IS DENTED ON FRAME. REMOVED DAMAGE FABRICATED AND INSTALLED RPR PER SRM 53-00-07 RPR 5 TABLE I I ZONE 2. RPR IS A CAT B RPR AND REQUIRES SUPPLEMENTAL VISUAL AND NDT INSPECTIONS STARTING IN 25,000 FLIGHT CYCLES AND 1 1,000FC THERE AFTER. CURRENT FC= 14767. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300063 20080423 00063 NM 2008 4 23 2008UALA02228 1 20080417 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EMERGENCY EXIT LIGHT INOP, AT AISLE CEILING BESIDE LAV 104. RELAMPED. OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300070 20080423 00070 NE 2008 4 23 2008UALA02235 2 20080416 A 7321 78360018072 EEC BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE ERRATIC A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 589UA 28707 NR 1 ENG EICAS MSG ENG SEC CONT DISPLAYED. REPLACED LEFT ENGINE EEC PER FIM 71-EPCS MSG INDEX S274-24. AND MM73-21-04. C HECKED ALL CONNECTORS ON EEC AND FIREWALL, FOUND OK. RAN ENGINE NO FAULTS. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300080 20080423 00080 EU 2008 4 23 F3LA200800184 1 20080410 A 5340 MOUNT AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE WINDSCREEN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED RIGHT WIND SCREEN LOWER ATTACH MOUNTS WERE CORRODED. MAINTENANCE REMOVED AND REPL ACED RIGHT WINDSCREEN LOWER ATTACH MOUNTS IN ACCORDANCE WITH THE REQUIRMENTS OF WORK CARD CP725-18. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042300085 20080423 00085 NM 2008 4 23 2008UALA02242 1 20080415 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHTS BY DOOR 1R KEEP FLICKERING ON AND OFF. REPLACED BATTERY POWER SUPPLY ASSEMBLY. OP CHECKED GOOD. AC OK F OR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300087 20080423 00087 NM 2008 4 23 2008UALA02244 1 20080417 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 517UA 24861 DOOR 4R EMERGENCY LIGHT INOP BY 107639, RESEATED CONNECTOR. OPS CHK'D OK. RESECURED/RESEATED CONNECTOR, OPS CHECKED NOR MAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300092 20080423 00092 NM 2008 4 23 UPS08552003 1 20080410 A 5610 BRACKET BOEING 757 75724APF 1384969 NM R2 WINDOW DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 474UP 28844 INSPECTION TYPE:N/A F/O R2 WINDOW DIFFICULT TO UNLATCH, HAD TO DEPRESS BUTTON TO UNLATCH. REWORKED THE FORWARD LATCH ST RIKER BRACKET IAW EO B757-5610-5738 PAR 2, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 2008042300093 20080423 00093 NM 2008 4 23 USAA920080895 1 20080328 A 5312 BULKHEAD BOEING 737 73733A 1384673 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 175AW 23634 CLT - MAJOR REPAIR- TWO EACH .25 INCH CRACKS ON WEB AT BS 178, WL234, RBL9.5. INSTALLED REPAIR IAW SRM 53-10-08-R2 FIG 201. 2 L 7 2 4F RT A16WE 2008042300095 20080423 00095 WP 2008 4 23 UPS08851996 1 20080301 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE:C3 UPPER RIB CRACKED AT END IN LEFT WING O/B LEADING EDGE NEAR STA XFS 809. FABBED AND INSTALLED REPAIR DOUBLERS IAW SRM 51-1-8, 57-2-00, 57-3-0 FIG 19. 2 L 7 4 4F RT 4A25 2008042300103 20080423 00103 EU 2008 4 23 F3LA200800189 1 20080415 A 5321 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE CABIN DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1539 1876 DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 232MF HAS HOLE IN FACE 1/4 INCH DIAMETER, 3 INCHES FROM INBOARD EDGE A ND 3 FEET FROM FORWARD EDGE. MAINTENANCE REPAIRED DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PAGE 205 F IGURE 201. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008042300105 20080423 00105 NM 2008 4 23 UPS08M51988 1 20080319 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 256UP 48405 INSPECTION TYPE:2C RIGHT WING L/E SLAT TRACK NR 12 CUTOUT CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUB LER & FILLER IAW MD-11 SRM 57-10-00 FIG 21. 2 L 7 3 4F RT A22WE 2008042300120 20080423 00120 NM 2008 4 23 USAA920080821 1 20080315 A 5310 6545871132 DOOR FRAME BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT- MAJOR REPAIR - Q6 CHECK - .1875 INCH CRACK ON R2 DOOR AFT FRAME, 3RD FROM BOTTOM DOOR STOP. INSTALLED REPAIR IAW S RM 52-10-11. 2 L 7 2 4F RT A16WE 2008042300123 20080423 00123 NM 2008 4 23 USAA920080826 1 20080408 A 5310 507945264 DOOR FRAME BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT- MAJOR REPAIR - Q6 CHECK - .25 INCH CRACK ON L1 DOOR FRAME AT NR 6 STOP. INSTALLED REPAIR IAW EA100332. 2 L 7 2 4F RT A16WE 2008042300125 20080423 00125 NM 2008 4 23 USAA920080829 1 20080317 A 5320 ANGLE BOEING 737 7374B7 1384702 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT- MAJOR REPAIR - Q6 CHECK - 1 INCH CRACK ON ANGLE AT BS 500F, STR 21L. REPLACED ANGLE IAW DWG 65C32055. 2 L 7 2 4F RT A16WE 2008042300126 20080423 00126 EU 2008 4 23 USAA920080879 1 20080408 A 2560 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 642AW 584 FORWARD F/A FLASHLIGHT, INDICATOR DOES NOT BLINK. REPLACED FLASHLIGHT BATTERY, OPS OK. 2 L 7 2 4F RT A28NM 2008042300143 20080423 00143 NM 2008 4 23 UPS08M52034 1 20080326 A 5730 ARB39548 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE:4C RIGHT WING LE SKIN SPLICE STRAP XFS791 CRACKED. REMOVED CRACKED SKIN SPLICE. FABRICATED AND INSTALL ED REPLACEMENT SKIN SPLICE IAW DWG ARB3954 AND MD-11 SRM 51-33-01. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 2008UALA03026 1 20080526 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 SEAT 4E FWD SEAT EMERGENCY LIGHT INOP. 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 NM 2008 7 16 USAA920081127 1 20080517 A 5313 66516989 STRINGER SPLICE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED STRINGER SPLICE, BS 907, S4L. REPLACED CRACKED STRINGER SPLICE, BS 907, S4L IAW BOEING SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080716 EU 2008 7 16 08FDEA02130 1 20080603 A 5310 A53810967 DIAPHRAGM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND TOOLING MARKS ON DIAPHRAGM C47-54, TRACK 5 LT-5 RT. REPAIR PERFORMED BY BLEND OUT THE TOOLING MARKS, NDT FOR CRAC K FREE. INSTALLING A DOUBLER AT C53-54, BEAM 1-2 RT IAW RAS 70510882/020/2008, APPROVED BY EA 6-5315-120114. 2 L 7 2 4F RT A35EU 20080716 NM 2008 7 16 NWAA082435528 1 20080529 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 528US 23843 DURING OVERNIGHT MAINTENANCE IT WAS FOUND THAT THE EMERGENCY LIGHTS AT DOOR 4L AND THE AFT LEFT BULLNOSE WERE INOPERATIV E. MAINTENANCE REPLACED BATTERY PACK M737, ALL OPERATIONS CHECKED GOOD. 2 L 7 2 4F RT A2NM 20080716 SO 2008 7 16 C2XA08RI076 1 20080520 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11121 145683 RIC - DURING ROUTINE MAINTENANCE, MX FOUND RIGHT SIDE EMERGENCY EXIT LOWER SIGN NOT ILLUMINATING. MX REMOVED AND REPLAC ED NR 3 INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20080716 2008 7 16 ZZDA2008113 4 20080528 A 2565 64210103 SLIDE BOEING 717 717200 1383700 NM TAIL CONE UNSERVICEABLE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 987AT 55088 TAIL CONE EVACUATION SLIDE PRESSURE GAUGE FELL DOWN INSIDE OF CONTAINER. REMOVED AND REPLACED TAIL CONE SLIDE ASSEMBLY IAW B717 MM 25-61-02. 2 L 7 2 4F TR A6WE 20080716 NM 2008 7 16 UPS08B52384 1 20080417 A 5311 FAILSAFE BOEING 747 747400 13848AT NM RH BS 1140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:C RT BS 1140 TENSION TIE FAIL SAFE CHORD CRACKED ABOUT O.030 INCH. RT BS 1140 TENSION TIE FAIL SAFE CHO RD REPLACED PER SRM 51-70-11. 2 L 7 4 4F RT A20WE 20080716 EU 2008 7 16 08FDEA02131 1 20080603 A 5730 A57111225200 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND 2 NICKS ON TOP SKIN C 46-47, TRACK 4-5 RT REPAIR PEFORMED BY SMOOTH BLEND OUT, SPOTFACING AND NDT FOR CRACK FREE C ONDITION IAW RAS 70507169/004/2008, APPROVED BY EA 6-5710-120053. 2 L 7 2 4F RT A35EU 20080716 NM 2008 7 16 USAA920081142 1 20080521 A 5313 BAC1498152 STRINGER BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - NR O3C10753045/28, CRACKED STRINGER, BS 578, S6L. REPAIRED CRACKED STRINGER, BS 578, S6 L IAW B737 SRM 53-00-03 AND DWG BAC 1498-152. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 2008UALA03079 1 20080529 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT LIGHTS INOP. UPPER DECK DOORS FWD AND AFT CEILING LIGHTS. 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 WP 2008 7 16 IXXA08SMN134S 1 20080411 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 653 L26L MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIRS LOCATED AT STATION FS 653 LONGERON 26.5 LEFT. REMOVED FASTENE RS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. PERFORMED NDT INSPECTION. NO CRACK AND CORROSION FOUND. FAB RICATED REPAIR DOUBLER, TRIPLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08198 DATED 04/25/08, SEMAN DRAWING NUMBER ED-4761 DATED 04/24/08, DC8 SRM 51-1-21, 51 -1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND 51-3-1. 2 L 7 4 4F RT 4A25 20080716 CE 2008 7 16 DJFA2008047 1 20080529 A 3243 CONTROL VALVE RAYTHN DH125 HAWKER800XP 7150012 CE BRAKE ASSY MALFUNCTIONED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 843CW 258543 AFTER LANDING THE CREW REPORTED THE BRAKES WERE MUSHY AND COULD ONLY ACHIEVE 200-300 PSI WITH BRAKES FULLY DEPRESSED. T HE CREW WAS ABLE TO PUMP THE BRAKES UP AFTER ENGINE SHUT DOWN. MAINTENANCE GAINED ACCESS TO THE BRAKE CONTROL VALVE AND BLED THE PILOT AND COPILOT MASTER CYLINDERS. MX DID FIND AIR IN THE SYSTEM. THEY PERFORMED A GOOD OPS AND TAXI CHECK. 2 L 7 2 4F RT A3EU 20080716 SO 2008 7 16 C2XA08RI079 1 20080529 A 5100 NONE EMB 145 EMB145XR 3260214 SO NONE A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 11113 145662 FLIGHT 1245 - EWR - FLIGHT CREW REPORTED SPS FAIL DURING PRE-FLIGHT TEST AND SMELLED SMOKE AFTER TEST. EWR MX PERFORMED OPERATIONAL CHECK OF SPS SYSTEM AND NO ABNORMALITIES WERE FOUND. FURTHER TROUBLESHOOTING FOUND EXTERNAL AIR CONDITIONI NG CART BAD. MX THEN PERFORMED OPERATIONAL CHECK OF AIR CONDITIONING SYSTEM SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RET URN TO SERVICE. 2 L 7 2 4F RT 20080716 NM 2008 7 16 KCSA08038 1 20080525 A 5310 STRUCTURE BOEING 747 747209F 1384800 NM FUSLEAGE DAMAGED A KCSA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 23 704CK 22299 AIRCRAFT 704CK WAS INVOLVED IN A RUNWAY EXCURSION WHICH RESULTED IN SUBSTANTIAL DAMAGE TO THE AIRCRAFT. 2 L 7 4 4F RT A20WE 20080716 2008 7 16 LR7A08084 2 20080612 A 7320 6821493 VALVE LKHEED 382 382G 526414U SO SPEED SENSE INTERMITTENT A LR7A O OTHER Y J ENGINE STOPPAGE WARNING INDICATION TX TAXI/GRND HDL 1 AL 03 406LC 37 4676 ON LANDING ROLL OUT, NR 2 ENGINE FLAMED OUT WHEN SELECTED INTO REVERSE. REPLACED NR 2 SPEED SENSE VALVE IAW ALLISON 501 D MM 75-10-1, INSPECTED NR 4 MISC CONNECTOR, NO DEFECTS NOTED, INSPECTED FUEL CONTROL INLET SENSE LINE, NO DEFECTS NOTED . INSPECTED ANTI ROTATION BRACKET, NO DEFECTS NOTED. PERFORMED REVERSE CHECK NUMEROUS TIMES PER LAS JOB CARD HN7101 AN D OPS CHECKED NORMAL, LOG PAGE 27341 ITEM M1. 2 H 7 4 4T A1SO 20080716 EU 2008 7 16 109RX5202008 1 20080520 A 6420 NUT AGUSTA AGUSTA A109 A109A2 0260120 EU TMECA ARRIEL ARRIEL1K1 60030 NE TAIL ROTOR LOOSE E I7LA K NONE O OTHER IN INSP/MAINT 1 NM 07 109RX G50693 10016 DURING PREFLIGHT INSPECTION, PILOT NOTED THE TAIL ROTOR BALANCE WHEEL HAD SLIGHT ROTATIONAL MOVEMENT. MAINTENANCE WAS D ISPATCHED TO INSPECT THE TAIL ROTOR ATTACHMENT. TAIL ROTOR RETENTION NUT 109-0130-85-1 WAS LOOSE CAUSING SLIGHT WEAR TO THE TAIL ROTOR GEARBOX OUTPUT SHAFT(SPLINES) AND TRUNNION 109-8131-33-101 SERIAL NUMBER M127. REPLACED TAIL ROTOR GEAR BOX 109-0440-01-119 SERIAL NUMBER H103596 TSO 2520.2 TSI 376.0. REPLACED TRUNNION 109-8131-33-101 SERIAL NUMBER M127 TS N 644.8. REPLACED TAIL ROTOR RETENTION NUT 109-0130-85-1. REPLACED SLIDER SLEEVE 109-0130-90-117 SERIAL NUMBER A2-0327 TSN 112.4. THE SLIDER SLEEVE SHOWS ABNORMAL WEAR AT THE AREA THE SLIDER SLEEVE MATES WITH THE TAIL ROTOR GEARBOX OUTPU 1 G 7 2 3U 3 U H7EU E19EU 20080716 NM 2008 7 16 2008UALA03041 1 20080527 A 5542 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RUDDER DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 RUDDER SN 100, LT LE SKIN HAS AREA OF DAMAGE 1 INCH ABOVE LOWER EDGE. MAJOR REPAIR ACCOMPLISHED, TAPER SANDED DAMAGED A REA. INSTALLED MULTIPLE LAYER COMPOSITE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 20080716 NM 2008 7 16 UPS08M52546 1 20080404 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48474 INSPECTION TYPE:C RT WING FUEL TANK UPPER NR 13 STRINGER END SUSPECT CRACK. HFEC INSP C/O AND FOUND CRACK APPROX 8 INCH . NR 13 STR END SPLICE REMOVED. STR CRACKED AREA CUT-OFF AND REMOVED. HFEC C/O ON TRIMMED EDGE AND FOUND NO CRACK EVI DENT. REPAIR STR, STRAP AND 02EA ANGLES FAB. FPI C/O ON FAB STRAP AND ANGLES, FOUND NO CRACK EVIDENT. REPAIR STR, STR AP AND 02EA ANGLES AND ATTACH CLIP INSTALLED. REWORKED AREA PAINTED. LEAK CHK SATIS. 2 L 7 3 4F RT A22WE 20080716 WP 2008 7 16 IXXA08SMN148S 1 20080418 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 118 L27R MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR LOCATED AT STATION FS 118 LONGERON 27 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, INTERNAL FING ER DOUBLER, FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC 8 SRM 53-2-1 FIGURE 7 SHEET 1 AND 4, DC8 SRM 51-9-0 FIGURE 68A, DC8 SRM 53-4-1 FIGURE 1 ITEM D, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 2008UALA03078 1 20080528 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 SEAT 1H SIDE MOUNTED EEL LIGHT INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20080716 NM 2008 7 16 2008UALA03080 1 20080529 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT EEL LIGHT INOP, AT SEAT 41 RIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 NM 2008 7 16 USAA920081147 1 20080520 A 5313 STRINGER BOEING 737 7373S3 1384711 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - NR I2D53012/1, LEVEL 2 CORROSION ON AFT CARGO COMPARTMENT STRINGER, BS 967, S27L. REPA IRED AFT CARGO COMPARTMENT STRINGER, BS 967, S27L IAW B737 SRM 51-20-01 AND 53-00-03. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 2008UALA03085 1 20080529 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EEL LIGHT INOP, MAIN DECK C ZONE RT AFT AREA. SUSPECT FAULTY BATTERY PACK. REPLACED BATTERY PACK, OP CHECK OK REF MM 3 3-51-04. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 NM 2008 7 16 2008UALA03088 1 20080529 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EEL INOP SEAT 42ABC. 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 WP 2008 7 16 DHL2008807529 1 20080506 A 5200 DOUBLER DOUG DC8 DC873F 302199F WP ACCESS DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 FUS NOSE SECTION ACCESS DOOR NR 2 INTERNAL DOUBLER CRACKED AND BROKEN (STA -156.000 - -165.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-29-08, EVA D853-00071 REV IR DATED 05-02-08. REMOVED CRACKED INTERNAL DOUBLE R IAW SRM 51-1-21. FABRICATED INTERNAL DOUBLER (AL7075T6 0.050") AND (2EA) INTERNAL STRAPS (AL7075T6 0.050") IAW DWG AF 56-53-102. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED STRAPS AND INTERNAL DOUBLER IA W EVA D853-00071, DWG AF56-53-102, SRM 51-1-11, SRM 51-1-21. 2 L 7 4 4F RT 4A25 20080716 WP 2008 7 16 DHL2008807535 1 20080507 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 "D" CARGO DOOR AFT LWR JAMB CORNER WITH CRACKS ON IT (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW AD2005-18-07, S/B DC8 5 3-078, DOUGLAS DWG SR08530019, 5750776. REMOVED PARTS TO GAIN ACCESS IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED EDDY CU RRENT INSP OF EXT SKIN, INTERNAL DOUBLER, INTERNAL SKIN AND PRESSURE SEAL AND X-RAY INSPECTED 'D" CARGO DOOR LWR JAMB CO RNER IAW BOEING DC8 NDT SPM PART 02 AND PART 06-10-001-01. NO CRACK FOUND. ENCLOSED SMN FORM 242-1, 242-2. FABRICATED EXT REPAIR DOUBLER (AL7075T6 0.090") AND EXTERNAL REPAIR TRIPLER (AL7075T6 0.125") IAW DOUGLAS DWG SR08530019. CLEANED , TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW DOUGLAS DWG SR08530019, SRM 51-1 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 KCSA081270 1 20080601 A 5414 SKIN BOEING 747 747212B 1384886 NM NR 4 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 NR 4 PYLON I/B SKIN CRACKED AT FWD LOWER ACCESS PANEL CUTOUT. 2 L 7 4 4F RT A20WE 20080716 2008 7 16 DXTA200803084 4 20080530 A 3160 7014300901 DISPLAY CESSNA 560 560XL 2076702 CE COCKPIT MALFUNCTIONED E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 664QS 5605264 NR 2 COPILOTS PFD WENT BLANK FOR 20 SECONDS, RED X FOR ABOUT 10 SECONDS, THEN PFD CAME ON. MASTER CAUTION CAME ON & WEN T OUT. ODOR OF SMOKE OR OF BURNING PLASTIC OR WIRES. 2 L 7 2 4F RT A22CE 20080716 CE 2008 7 16 DXTA200803085 1 20080531 A 2720 99145586 ACTUATOR CESSNA 750 750 2076810 CE RUDDER FAILED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED DE DESCENT 1 GL 07 943QS 7500043 DESCENDING OUT OF FL410 "RUDDER LIMIT FAIL A" CAS MESSAGE ILLUMINATED. RUDDER LIMITER FAILED AT 23 PERCENT. R&R "UPPER LIMITER ACTUATOR A" WITH NEW. 2 L 7 2 4J RT T00007WI 20080716 CE 2008 7 16 DXTA200803087 1 20080601 A 3260 LIGHT CESSNA 560 560XL 2076702 CE COCKPIT UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 07 641QS 5605295 WHEN GEAR SELECTED DOWN THE RT SIDE GREEN LIGHT DIDN'T ILLUMINATE. 2 L 7 2 4F RT A22CE 20080716 NM 2008 7 16 SWAA082884 1 20080528 A 5320 6517582 STIFFENER BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED 16Y CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178, LBL 17. REPAIRED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2008042300187 20080423 00187 EA 2008 4 23 A6WA200840241 1 20080318 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 439AW 7753 CRACK FOUND ON FRAME FS 280 RBL 9 AND BRACKET INBOARD. FLOOR STRUCTURE REPAIRED IAW REO 601R-53-11-171 REV D. (M) 2 L 7 2 4F RT A21EA 2008042300207 20080423 00207 EA 2008 4 23 A6WA200840104 1 20080219 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION DE DESCENT 1 GL 31 421ZW 7346 FLAPS FAIL INDICATION ON APPROACH, DIVERTED TO ORD, FLAPS AT 5 DEGREES. COMPLIED WITH RESET PROCEDURES, IAW AWAC SUPP 9 8-018B, STEPS 1.3 AND 1.4, FLAPS SYSTEM RESET OK. (M) 2 L 7 2 4F RT A21EA 2008042300211 20080423 00211 NM 2008 4 23 MASA200800312 1 20080413 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM NR 1 & 2 FAULTY A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 989HA 15152 427 ASH FLIGHT 2851 PHX-YUM. INTERMITTENT SMOKE WARNING LIGHT IN FLIGHT. REMOVED AND REPLACED NR 1 & NR 2 SMOKE DETECTORS. 2 H 7 2 4T RT A13NM 2008042300214 20080423 00214 EA 2008 4 23 MASA200800313 1 20080411 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 77302 7302 LOWER ENGINE SUPPORT BEAM IS CRACKED AT LBL 7.2. REPAIRED BEAM. 2 L 7 2 4F RT A21EA 2008041800062 20080418 00062 2008 4 18 ASAA0852808 4 20080403 A 2210 4082499903 AUTOPILOT SYS BOEING 737 737890 1384527 NM COCKPIT MALFUNCTIONED A ASAA K NONE O OTHER NR NOT REPORTED 1 NM 02 583AS 35681 THE "A" AUTOPILOT WILL NOT ENGAGE. UNABLE TO DUPLICATE. RAN LAND VERIFY TEST WITH NO FAILURES. 2 L 7 2 4F RT A16WE 2008041800068 20080418 00068 SO 2008 4 18 C2XA08SH062 1 20080408 A 2560 P2070005120 CHARGER EMB 135 EMB135LR 3260305 SO CABIN DEFECTIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14516 145323 SHV - FLIGHT 2148 - PILOT REPORTS ELECTRICAL SMELL COMING FROM AFT AREA OF AIRCRAFT CABIN WHEN PERFORMING POST FLIGHT IN SPECTION. MAINTENANCE REMOVED & REPLACED AFT FLIGHT ATTENDANT FLASHLIGHT CHARGER IAW EMB 135 AMM 33-50-16. OPS CHECK G OOD. 2 L 7 2 4F RT T00011AT 2008041800074 20080418 00074 SO 2008 4 18 C2XA08IA106 1 20080408 A 3397 66366 CONNECTOR EMB 135 EMB135LR 3260305 SO CABIN DIRTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14514 145303 IAH - FLIGHT 2791, DURING PREFLIGHT INSPECTION THE CREW REPORTED THE SECOND AND THIRD SECTION OF AISLE PATH LIGHTING TO BE INOPERATIVE. MAINTENANCE CLEANED THE CONNECTOR ON THE AISLE PATH LIGHTING, OPERATIONALLY CHECKED WITH NO DEFECTS, AN D THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 2008041800086 20080418 00086 EU 2008 4 18 USAA920080776 1 20080327 A 5320 D5311281820401 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 187US 1704 PIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 709 / FR 16, +Y254. REPLACED CABIN FLOOR S UPPORT, BS 709 / FR 16, +Y254 IAW A321 SRM 53-11-14. 2 L 7 2 4F RT A28NM 2008041800087 20080418 00087 EU 2008 4 18 USAA920080777 1 20080326 A 5320 D5347218920400 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 187US 1704 PIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 3950 / FR 68 - BS 4059 / FR 70, -Y1050 TO - Y1162. REPLACED CABIN FLOOR SUPPORT, BS 3950 / FR 68 - BS 4059 / FR 70, -Y1050 TO -Y1162 IAW A321 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008041800089 20080418 00089 EU 2008 4 18 USAA920080779 1 20080325 A 5320 D5347218820400 FLOOR SUPPORT AIRBUS A321 A321211 3930370 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 187US 1704 PIT - MAJOR REPAIR - S3 CHECK - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 3950 / FR 68 - BS 4003 / FR 69, +Y1050. RE PLACED CABIN FLOOR SUPPORT, BS 3950 / FR 68 - BS 4003 / FR 69, +Y1050 IAW A321 SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008041800115 20080418 00115 SO 2008 4 18 C2XA08RI052 1 20080330 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 16918 145397 FLIGHT 4930 - EWR - THE FLIGHT CREW REPORTED AISLE EMERGENCY LOCATOR EXIT LIGHT INOPERATIVE. EWR MX REMOVED AND REPLACE D EMERGENCY LIGHT BATTERY INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SER VICE. 2 L 7 2 4T RT T00011AT 2008041800155 20080418 00155 2008 4 18 RAIA00804008 4 20080409 A 3442 3031450801 TRANSCEIVER EMB 145 EMB145LR 3260212 SO WEATHER RADAR MALFUNCTIONED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 829HK 145281 FLT 7903 -STL- WEATHER RADAR FAILED. MAINTENANCE REMOVED AND REPLACED THE WEATHER RT AND ACCOMPLISHED THE ASSOCIATED FO LLOW ON MAINTENANCE. 2 L 7 2 4T RT T00011AT 2008041800245 20080418 00245 NM 2008 4 18 USAA920080866 1 20080329 A 5320 WEB BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 PRESSURE DECK WEB HAS 1.5" CRACK AT BS 663.75, WL 208.1, LBL 30. INSTALLED DOUBLER REPAIR IAW SRM 56-60-51. 2 L 7 2 4F RT A16WE 2008041800252 20080418 00252 NM 2008 4 18 2008UALA02045 1 20080409 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY EXIT EEL LIGHTS INOP. ALL RIGHT "E" ZONE SEATS. SUPPLEMENTAL DATA UPDATE REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041800255 20080418 00255 NM 2008 4 18 2008UALA02048 1 20080408 A 3150 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LT ENGINE FALSE ACTIVATION A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 667UA 29239 727816 LEFT ENGINE FUEL FILTER LIGHT ON MOMENTARILY IN DESCENT. GOT STATUS LIGHT, CLEARED IT. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041800256 20080418 00256 NM 2008 4 18 2008UALA02049 1 20080409 A 3150 COOLER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUEL/OIL FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 669UA 30025 EICAS MSG L GEN DRIVE DISPLAYED. GEN DRIVE LGT ILLUM. GENERATOR DRIVE DISCONNECTED. FOUND OIL COMING FROM IDG FUEL OI L HEAT EXCHANGER. REPLACED FUEL-OIL COOLER & FUEL-OIL COOLER BYPASS VALVE ASSEMBLY PER MM79-21-01. VERIFICATION FLT CON FIRMS NORMAL OPERATION OF THE SUBJECT SYSTEM. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041800257 20080418 00257 NE 2008 4 18 2008UALA02050 2 20080409 A 7230 BLADE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COMPRESSOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 641UA 25091 727882 CRACK FOUND IN THE 5TH STAGE COMPRESSOR BLADE ROOT OF THE NR 1 ENGINE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 2008041800258 20080418 00258 EU 2008 4 18 2008UALA02051 1 20080408 A 3350 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 425UA 508 2R EMERGENCY EXIT LIGHT COVER IS MISSING. RESECURED COVER 2 L 7 2 4F 4 F RT A28NM E40NE 2008041800259 20080418 00259 NM 2008 4 18 2008UALA02052 1 20080408 A 3510 HOSE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE OXYGEN SYSTEM FRAYED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 837UA 1474 F/O O2 MASK GREEN HOSE FRAYED. SWAPPED WITH 1ST OBS POSTION AND LATER REPLACED ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 2008043000189 20080430 00189 NM 2008 4 30 CALA0800390 1 20080428 A 5311 143A1121 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24706 28767 CABIN STATION 500 AT S9R PASSENGER SERVICE UNIT RAIL BRACKET TO FRAME CRACKED. REPAIRED FRAME REF EA 5310-04498. 2 L 7 2 4F RT A16WE 2008041800260 20080418 00260 NE 2008 4 18 C1HA200881001 2 20080411 A 7200 ENGINE BOEING 727 7272S7 138407Z NM PWA JT8 JT8D* NE NR 1 ERRATIC A C1HA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 681CA 22020 688835 NR 1 ENGINE ENGINE CONTINUOUS ERRATIC AT ALT EPR - N1 - N2 TEMP DECREASING AND SURGING. RETURNED FOR LANDING HOUSTON. REPLACED NR 1 ENG FUEL FILTER AND DID FIND CONTAMINATION. REPLACED 2 AND 3 ENG FILTERS PRECAUTIONARY PER 73-11-01, 405. PERFORMED ENG RUN PER 71-00-501, CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 2008041800261 20080418 00261 EA 2008 4 18 SWIA200819478 1 20080407 A 5220 SPRING CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 RIGHT EMERGENCY DOOR SPRINGS ARE CORRODED. REPLACED RIGHT EMERGENCY EXIT DOOR HANDLE SPRINGS IAW 52-21-02. 2 L 7 2 4F RT A21EA 2008041800262 20080418 00262 EA 2008 4 18 SWIA200819479 1 20080413 A 2913 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 NM 07 937SW 7735 FLT 6085 - NR 3 HYDRAULIC SYSTEM QUANTITY SHOWED 0 PERCENT ON DESCENT. REPLACED 3A HYDRAULIC PUMP IAW AMM 29-12-03. AL L OPS CHECKS GOOD, PN 848847, SN OFF MX661284. 2 L 7 2 4F RT A21EA 2008041800286 20080418 00286 NM 2008 4 18 HNAA0800128 1 20080410 A 4990 OIL SYSTEM DHAV DHC8 DHC8102 2809003 NM APU LOW A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 809EX 18829 15293 302 OIL SMELL IN CABIN. APU BLEED AIR ON. APU WAS FOUND TO BE LOW ON OIL. 2 H 7 2 4T RT A13NM 2008041800291 20080418 00291 NM 2008 4 18 USAA920080802 1 20080327 A 5754 65C26602224TR WEDGE BOEING 737 7374B7 1384702 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A 14.5" X 6.5" DISBONDED AREA ON NR 5 SLAT T/E WEDGE. INSTALLED REPAIR IAW SRM 57-43-02 , TR 57-42-02, 51-70-10 AND AMM 51-21-99. 2 L 7 2 4F RT A16WE 2008041800299 20080418 00299 NM 2008 4 18 USAA920080810 1 20080331 A 5311 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A .5" CRACK ON FRAME AT BS 907 BETWEEN STR 8R AND STR 9R. INSTALLED REPAIR IAW SRM TR 5 3-10-20E. 2 L 7 2 4F RT A16WE 2008041800307 20080418 00307 NM 2008 4 18 USAA920080818 1 20080404 A 5320 FITTING BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A 1" CRACK ON CLIP AT BS 344, LBL 12. INSTALLED REPAIR IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 2008041800309 20080418 00309 NM 2008 4 18 USAA920080820 1 20080402 A 5754 SKIN BOEING 737 7374B7 1384702 NM L//E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A .125" CRACK ON NR 6 SLAT SKIN JUST I/B OF AUX TRACK. INSTALLED DOUBLER REPAIR IAW SRM 57-43-01 REPAIR 6. 2 L 7 2 4F RT A16WE 2008041800310 20080418 00310 NM 2008 4 18 USAA920080823 1 20080401 A 5321 FLOOR PANEL BOEING 737 7374B7 1384702 NM COCKPIT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A 1" CRACK ON COCKPIT FLOOR AT BS 257, LBL 3. INSTALLED DOUBLER REPAIR IAW SRM 53-10-51 . 2 L 7 2 4F RT A16WE 2008042100003 20080421 00003 NM 2008 4 21 2008UALA02124 1 20080413 A 3150 WARNING LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE FALSE INDICATION A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 668UA 30024 RTFL DUE TO LANDING GEAR DOOR AND TAILSKID INDICATIONS. NO FAULT FOUND. 2 L 7 2 4F 4 F RT A1NM E24NE 2008042100016 20080421 00016 NM 2008 4 21 2008UALA02062 1 20080409 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY EXIT EEL LIGHTS INOP, AT MAIN STAIRS LEADING TO UPPER DECK. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042100017 20080421 00017 NM 2008 4 21 2008UALA02063 1 20080409 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY EXIT EEL LIGHTS INOP. JUST AFT OF UPPER DECK ROW 17 LOWER WALL EEL, BOTH LIGHT ASSY'S. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042100027 20080421 00027 NE 2008 4 21 2008UALA02073 2 20080409 A 7320 MR7320537 FMU BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 ENGINE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 773UA 26929 777009 CREW REPORTED NR 1 ENG FAILED TO SHUT DOWN ON INITIAL MOVEMENT OF FUEL CUT-OFF SWITCH. ENGINE SHUT DOWN AFTER APPROX 2 MINS STATUS ENG FUEL VALVE L, MSG 73-60211. REPLACED FUEL MANAGEMENT UNIT (FMU). 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042100065 20080421 00065 NM 2008 4 21 CALA0800119 1 20080212 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM BS 867 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19621 27334 FRAME CRACKED AT STA 867 ABOVE STRINGER 9L. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04714. 2 L 7 2 4F RT A16WE 2008042100085 20080421 00085 EA 2008 4 21 COMA0860209 1 20080404 A 3040 SENSOR CNDAIR CL600 CL6002B19 1900309 EA WINDSHIELD HEAT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 797CA 7344 FLIGHT 5129 - EN ROUTE BUF-CVG RECEIVED A RIGHT WINDSHIELD HEAT CAUTION, FLIGHT RETURNED TO BUF. SWAPPED THE SPARE TEMP ERATURE SENSOR ON THE RIGHT WINDSHIELD TO THE SPARE TERMINALS. 2 L 7 2 4F RT A21EA 2008042100094 20080421 00094 EA 2008 4 21 COMA0880005 1 20080411 A 3250 ECU CNDAIR CL600 CL6002D24 1390016 EA NLG STEERING MALFUNCTIONED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 678CA 15125 FLIGHT 5210 - ON APPROACH INTO CVG RECEIVED NOSE WHEEL STEERING INOP CAUTION MESSAGE. EMERGENCY DECLARED, AIRCRAFT LAND ED SAFELY. RESET NOSE WHEEL STEERING SYSTEM C/B'S AND ECU. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008042100101 20080421 00101 EA 2008 4 21 COMA0860211 1 20080406 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 640 S9 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 938CA 32500 7046 CRACK AT FUSELAGE FRAME 640 STR 9 CUTOUT. INSTALLED REPAIR TO STA 640 FRAME AT STR 9 PER CRJ REO 601R-53-61-557 REV A. 2 L 7 2 4F RT A21EA 2008042100116 20080421 00116 NM 2008 4 21 CALA0800325 1 20080411 A 5340 65C16121 BRACKET BOEING 737 737524 1384721 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14639 28900 BRACKET AT STA 344, LBL 58" FOUND CORRODED. REMOVED & REPLACED 65C16121-6 GIRT BAR MOUNT BRACKET REF 51-10-02 & 51-40-0 2 (STA 344, LBL 58"). 2 L 7 2 4F RT A16WE 2008042100130 20080421 00130 NM 2008 4 21 QXEA200800384 1 20080414 A 5210 HANDLE BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR BROKEN A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 405QX 4047 PDX- FLIGHT 2429 - AFT PASSENGER DOOR INSIDE HANDLE BROKEN. MAINTENANCE SECURED THE HANDLE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED SO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 2008042100133 20080421 00133 EA 2008 4 21 QXEA200800381 1 20080417 A 5210 LATCH CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR STIFF A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 09 609QX 10031 PDX - FLIGHT 2562 - MAIN CABIN DOOR REPORTED AS DIFFICULT TO LATCH SHUT. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 2008042300008 20080423 00008 2008 4 23 2008UALA02178 4 20080411 A 2565 B14056906 O-RING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE SLIDE BOTTLE UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 202UA 24717 LOW BOTTLE. FOUND FAULTY O-RING. REPLACED O-RING. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042300009 20080423 00009 NM 2008 4 23 R61A200800003 1 20080405 A 3150 WARNING SYSTEM EMB ERJ170 ERJ170200LR 3260121 NM COCKPIT MALFUNCTIONED A R61A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 109HQ 17000168 CREW REPORTED ON CLIMBOUT HAD THE FOLLOWING EICAS MESSAGES, ADSP1 FAIL TAT1 FAIL, AOA LIMIT FAIL GROUND SPOILER FAIL AND ENGINE 2 NI AN ITT INDICATIONS FLASHING ALONG WITH THE CAPTAIN’S PFD WAS FLASHING. CREW DECLARED AN EMERGENCY AND DIVE RTED TO WINDSOR LOCK CT. LANDED WITHOUT INCIDENCE. MAINTENANCE WAS DISPATCHED TO A/C AND CYCLED POWER, ALL FAULTS CLEA RED AND INDICATIONS RETURNED TO NORMAL. A/C WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A56NM 2008042300019 20080423 00019 EU 2008 4 23 UPS08152044 1 20080415 A 3150 WARNING LIGHT AIRBUS A300 A300F4622R 3930360 EU FLIGHT DECK INOPERATIVE A IPXA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 01 127UP 0811 EVAC SLIDE WARNING LIGHT INOP, BUZZER OK. PLACED ON MEL 52-73-01-1. CONTROL NR M373730. RESET ELEC. CONNECTOR ON ASPS U (7OWN) WITH REF TO AMM 52-73-18-04 PARA C(6). TESTED ASPSU IAW AMM 52-73-00-05. NO FAULTS NOTED. TESTED EVAC SLIDE WAR NING LIGHT WITH REF TO AMM 52-73-11-04 PARA 1. OPS CK GOOD. THIS CLEARS M 373730. 2 L 7 2 4F RT A35EU 2008042300028 20080423 00028 EU 2008 4 23 2008UALA02210 1 20080416 A 5210 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 493UA 1821 SMALL DENT AFT OF DOOR NR 2 LEFT PAINT MISSING. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042300031 20080423 00031 EA 2008 4 23 A6WA200840160 1 20080317 A 2613 ELEMENT CNDAIR CL600 CL6002B19 1900309 EA LT ANTI ICE SYS MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 31 412AW 7582 FOUND LT WING ANTI-ICE DUCT WARNING MESSAGE. REMOVED AND REPLACED HEAT SENSE ELEMENT A41WK REF AMM 36-21-04, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 2008042300045 20080423 00045 EU 2008 4 23 USAA920080902 1 20080417 A 5311 29534130003 FRAME AIRBUS A321 A321211 3930370 EU ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 188US 1724 PIT-MAJOR REPAIR - CORROSION ON SHEAR PLATE SUPPORT FRAME AT FR 70, STR 23R. REPLACED FRAME IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 2008042300065 20080423 00065 NM 2008 4 23 2008UALA02230 1 20080417 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EMERGENCY EXIT EEL LIGHT INOP, AT ROW 43 LEFT. FOUND LOOSE CONNECTION. SECURED CONNECTION OP CHECKED GOOD. AC OK FOR SER VICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300066 20080423 00066 NM 2008 4 23 2008UALA02231 1 20080417 A 3350 256005 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP, AT LEFT SIDE AFT TWO LIGHT ASSY'S. FOUND POWER SUPPLY FUSE FAULTY. REPLACED FUSE OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300067 20080423 00067 NM 2008 4 23 2008UALA02232 1 20080416 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 46H MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 118UA 28811 FOUND SEAT 46H EEL LIGHT STRIP IS MISSING. REPLACED EEL. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300068 20080423 00068 NM 2008 4 23 2008UALA02233 1 20080416 A 3350 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 592UA 28143 DOOR L2 EXTERIOR EMERGENCY LIGHT INOP. FOUND BATTERY CHARGER INOP. REPLACED BATTTERY CHARGER, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300073 20080423 00073 NM 2008 4 23 2008UALA02238 1 20080416 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 1E UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 779UA 26941 SEAT 1E EEL LIGHTING MOUNTED ON THE SEAT NEEDS TO BE SECURED. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042300086 20080423 00086 NM 2008 4 23 2008UALA02243 1 20080417 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 517UA 24861 EEL STRIP LIGHTS ON SIDE OF COACH SEATS 18C, 22C ARE INOP. FOUND A SHORT IN ASSY WIRING/FIXTURE. REPLACED LIGHT STRIP S, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042300088 20080423 00088 NM 2008 4 23 2008UALA02247 1 20080417 A 3350 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 211UA 30217 EXTERIOR EMERGENCY LIGHTS AT DOORS 1L, 2R, AND 4R INOP. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042300115 20080423 00115 NM 2008 4 23 ASAA0852811 1 20080409 A 3150 WARNING SYSTEM BOEING 737 737890 1384527 NM COCKPIT MALFUNCTIONED A ASAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 02 557AS 35176 FMC - DISAGREE ANNUNCIATION OCCURRED FOLLOWING ENGINE START. ACCOMPLISHED FIM 34 61 TASK 835 WITH NO FAULT FOUND. VERI FIED BOTH FMC UNITS WERE OPERATING PROPERLY. 2 L 7 2 4F RT A16WE 2008042300210 20080423 00210 EA 2008 4 23 SWIA200819490 1 20080414 A 2910 DRAIN LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 07 460SW 7803 FLT 5450 - HYDRAULIC SYSTEM NR 2 QUANTITY SHOWED 0 PERCENT. REPAIRED LEAK IN CASE DRAIN LINE IAW 20-22-00. LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 2008042300224 20080423 00224 NM 2008 4 23 UPS08652008 1 20080412 A 2130 1305026 CONTROL PANEL BOEING 767 76734AF 1385212 NM COCKPIT DEFECTIVE A IPXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 320UP 27747 INSPECTION TYPE:ETOP DIVERSION - UNABLE TO MAINTAIN CABIN PRESSURIZATION. REPLACED CABIN PRESSURE SELECTOR PANEL PER AM M 21-31-01-4. AUTO TEST AND MANUAL TEST NORMAL, NO FAULTS AT PRESSURE CONTROLLERS WITH REFERENCE TO FIM 21-31-00. 2 L 7 2 4F RT A1NM 2008042300225 20080423 00225 SO 2008 4 23 SIMA200810903 1 20080414 A 2612 FIRE LOOP EMB 145 EMB145LR 3260212 SO NR 2 MALFUNCTIONED A SIMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 922AE 14500906 ON FLIGHT 3609, CREW REPORTED DURING TAXING OUT FOR TAKEOFF THEY GOT ENGINE NR 2 FIRE WARNING ON EICAS (ENGINE NOT RUNNI NG) FIRE BELL AND NR 2 FIRE HANDLE RED. COMPLIED WITH ENGINE FIRE FAILURE EPC CHECKLIST. AIRCRAFT REMOVED FROM SERVICE . REMOVED AND REPLACED ENGINE NR 2 FIRE DETECTION LOOP IAW EMB 145 AMM 26-11-09. OPERATIONAL CHECKED GOOD. AIRCRAF T RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 2008042300226 20080423 00226 2008 4 23 UPS08652019 4 20080413 A 2564 600307FRBM LIFE RAFT BOEING 767 76734AF 1385212 NM COCKPIT UNSERVICEABLE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 312UP 27763 INSPECTION TYPE:N/A DURING PS CHECK, FOUND LIFE RAFT UNSERVICEABLE. REMOVED AND REPLACED LIFE RAFT PER MM 25-62-00-0. 2 L 7 2 4F RT A1NM 2008042300236 20080423 00236 NM 2008 4 23 SWAA081936 1 20080411 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 2008042300244 20080423 00244 NM 2008 4 23 SWAA081940 1 20080413 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 2008042300246 20080423 00246 NM 2008 4 23 SWAA081941 1 20080412 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 779, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042300249 20080423 00249 NM 2008 4 23 2008UALA02252 1 20080418 A 3350 60B4005715 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 LT OW AREA EMERGENCY LIGHT 2 INOP. REPLACED EMERGENCY LIGHT OP CHECKS GOOD PER AMM 33-51-03 P 201. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042300251 20080423 00251 NM 2008 4 23 SWAA081942 1 20080413 A 5310 6546956 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 410, LBL 62 TO LBL 70. REMOVED AND REPLACED WEB PER SR M. 2 L 7 2 4F RT A16WE 2008042300255 20080423 00255 NM 2008 4 23 SWAA081968 1 20080413 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300258 20080423 00258 NM 2008 4 23 SWAA081962 1 20080413 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300262 20080423 00262 NM 2008 4 23 UPS08652017 1 20080414 A 2421 IDG BOEING 767 76734AF 1385212 NM NR 1 GENERATOR LOW A IPXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 323UP 27749 INSPECTION TYPE:ETOP ATB - EICAS MSG R GEN DRIVE DISPL, GEN DRIVE LIGHT ILLUMINATED, GEN DRIVE DISCONNECTED. SERVICED O IL TO PROPER LEVEL, RECONNECTED NR 2, IDG RAN ENGINE. OPS CHECKS GOOD. 2 L 7 2 4F RT A1NM 2008042300270 20080423 00270 NM 2008 4 23 SWAA081966 1 20080413 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300271 20080423 00271 NM 2008 4 23 SWAA081967 1 20080413 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300276 20080423 00276 NM 2008 4 23 SWAA081978 1 20080413 A 5753 6549456 FITTING BOEING 737 7375H4 138449D NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND RIGHT WING NR 8 FLAP TRACK OUTBOARD FITTING CORRODED. REMOVED AND REPLACED FITTING P ER SWA EA. 2 L 7 2 4F RT A16WE 2008042300278 20080423 00278 NM 2008 4 23 UPS08M52013 1 20080212 A 5311 FRAME DOUG MD11 MD11 3023602 NM BS 449 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 294UP 48472 INSPECTION TYPE:C FAC AFT COMPARTMENT AT STA 449.250 FOUND CRACKED FRAME STRUCTURE JUST BELOW NR 1 RAM AIR INLET SCOOP A FT SECTION AS MARKED. DAMAGE AT RETURN FLANGE TRIM OFF PER EN1071-08. HFEC INSP C/OUT PER DAC NDTSPM R.13 PART06.10.01 .001 FOUND NO CRACK EVIDENT. REPAIR DOUBLER AND CLIP FAB PER EN1071-08 AND HEAT TREATED PER DPS 7.00-1. REPAIR DOUBLER HARDNES HRB82 CLIP HARDNESS HRB81.6 ACCEPTABLE PER DPS1.05.3. REP DOUBLER AND CLIP PROTECTED PER SRM 51-21-01V.2R.40. REPAIR DOUBLER AND CLIP INSTALLED PER EN1071-08. 2 L 7 3 4F RT A22WE 2008042300279 20080423 00279 2008 4 23 UPS08M52016 2 20080414 A 7532 33990462 BLEED VALVE DOUG MD11 MD11F 3023600 NM BLEED SYSTEM ILLUMINATED A IPXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 293UP 48473 DIVERSION NR 1 AND NR 3 ENGINE BLEED OFF MESSAGES (ICING RESTRICTED). PERF PSC-1 & PSC-2 COMMENT FAULT REVIEW FOUND. MA NUALLY OPEN/CLOSE ENG NR 1 & 3 HI STAGE VALVES FOR BINDING. ALL FOUND NORMAL. REF EO 3610-18062D. TRIPPED & COLLARD C/B' S PERF LEAK. SECURITY CK OF ALL SENSE LINES FROM NR 1 & 3 HI STG PILOT VALVES HI STG BLEED VALVES. ALL NORMAL & NO LEAKS . REF LP 430512, 430513. 2 L 7 3 4F RT A22WE 2008042300280 20080423 00280 NM 2008 4 23 2008UALA02146 1 20080411 A 3350 LAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 301UA 23642 LT OVERWING EXIT LIGHT INOP. RELAMPED. OPS CHKS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042300281 20080423 00281 NM 2008 4 23 2008UALA02147 1 20080413 A 5313 STRINGER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE 14 LT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 STRINGER SPLICE CHANNEL CRACKED AFT OF FWD ENTRY DOOR AT STRINGER 14 LT. MAJOR REPAIR ACCOMPLISHED: REPLACED CHANNEL. 2 L 7 2 4F 4 F RT A16WE E2GL 2008042300282 20080423 00282 NM 2008 4 23 2008UALA02148 1 20080413 A 5210 INTERCOSTAL BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE L1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 L1 DOOR INTERCOSTAL WEBS CRACKED AT STA 294.5 STR 12 LT AND STR 7 LT AND CLIP AT STA 360 AT STR 10 LT. MAJOR REPAIR AC COMPLISHED: REPLACED WEBS AND CLIP. 2 L 7 2 4F 4 F RT A16WE E2GL 2008041800135 20080418 00135 NM 2008 4 18 08FDEA01435 1 20080416 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 619FE 48770 UPPER CARGO DOOR CUT OUT, NR 7 LOWER JAMB SUPPORT FITTING MOUNTING HOLE CRACKED. MOUNTING HOLES REAMED PER SRM 53-50 -00 FIG. 10 VOL.I. AND BUSHING REPAIR CARRIED OUT PER SRM 53-50-00 FIG. 10. VOL.I. BUSHING FABRICATED PER SRM 53-50-00 FIG. 10 VOL.I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080716 WP 2008 7 16 UPS08852536 1 20080525 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP BS 45 RBL47 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 MAIN CABIN FLOORBOARD CRACKED, STA 45 RBL 47. FABBED AND INSTALLED REPAIR DOUBLER IAW, SRM. 53-2-00, 53-2-3, 510108, 51-1-26, 51-1-21. 2 L 7 4 4F RT 4A25 20080716 WP 2008 7 16 UPS08852541 1 20080612 A 5320 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP BS 420 L30L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 SUPPORT FLOOR BRACKET CRACKED AT STA 420 AND L30L. REPAIRED FLOOR SUPPORT BRACKET AT STA 420 AND L30 L IAW EO DC8-5320- 6176-C. 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 2008UALA03099 1 20080530 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 119UA 28812 SEAT 3J EEL LIGHT LOOSE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 NM 2008 7 16 2008UALA03100 1 20080530 A 3510 89151114 OXYGEN BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW O2 LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 127UA 28813 CREW OXYGEN BOTTLE PRESSURE LOW. REPLACED WITH SERVICEABLE CREW OXYGEN CYLINDER AND THEN LEAK CHECKED GOOD PER AMM 12-1 5-08 P 301. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 NM 2008 7 16 ZZDA2008124 1 20080618 A 5532 SKIN BOEING 717 717200 1383700 NM VERTICAL STAB CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 937AT 55091 VERTICAL STAB RT SKIN CRACKED JUST BELOW HORIZONTAL STAB CUTOUT. COMPLIED WITH EA 17-55-01183A. MAJOR REPAIR, FORM 337 SUBMITTED. 2 L 7 2 4F TR A6WE 20080716 NM 2008 7 16 ZZDA2008118 1 20080609 A 7331 QA07995 PRESSURE SWITCH BOEING 737 7377BD 1384511 NM LEFT ENGINE DEFECTIVE A ZZDA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SO 37 292AT 33926 LEFT ENGINE FILTER BYPASS ILLUMINATED IN FLIGHT. REMOVED AND REPLACED LEFT ENGINE DIFFERENTIAL PRESSURE SWITCH AND FUEL FILTER. 2 L 7 2 4F RT A16WE 20080716 EU 2008 7 16 SA08039 1 20080531 A 2611 SMOKE WARNING AIRBUS A319 A319112 3930323 EU COCKPIT MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 700UW 0885 FLIGHT 1130, BGI-CLT - JUST AFTER TAKEOFF THE FLIGHT CREW RECEIVED AN AVIONICS SMOKE WARNING AND RETURNED TO BGI. MAINT ENANCE PERFORMED AN INSPECTION OF THE AVIONICS COMPARTMENTS WITH NO EVIDENCE OF SMOKE NOTED. A SATISFACTORY OPERATIONAL CHECK OF THE EQUIPMENT COOLING WAS ALSO PERFORMED. 2 L 7 2 4F RT A28NM 20080716 NM 2008 7 16 2008UALA03048 1 20080527 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 360 S13L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 FWD ENTRY DOOR CUTOUT AFT SIDE SHEAR TIE IS CRACKED ON AFT SIDE AT BS 360 JUST BELOW STRINGER S-13L. MAJOR REPAIR ACCOM PLISHED, REPLACED SHEAR TIE WITH P/N 69-48204U505. 2 L 7 2 4F 4 F RT A16WE E2GL 20080716 NM 2008 7 16 SWAA082885 1 20080528 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 UPS08M52538 1 20080509 A 5753 HINGE DOUG MD11 MD11 3023602 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C RHW O/B FLAP I/B HINGE (FLAP MOUNTED) UPPER FWD MOUNTING SPOT FACE FOUND CORRODED. CORROSION REMOVED PER BSOPM20-11-02REV60 ORIG THK 0.751" REMAIN THK 0.746" MAT`L REMOVED 0.005". FPI C/OUT PER DAC NDTSPMREV13PT8 NO CORR OSION EVIDENT. RHW AFT OB FLAP INBD HINGE UPPER FWD MOUNTING SPOTFACE THK OF 0.746" ACCEPTED PER EN1182-08. RWK AREA E TCH INSP SATIS, C/OUT FLAP PEENING, CAD PLATE AND PAINT PER EN1182-08. REF MD016812 FOR BUSHING REPAIR AND WASHER INSTL . 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 UPS08M52539 1 20080612 A 5330 NDA6712 SKIN DOUG MD11 MD11F 3023600 NM FS 879 L28L DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 286UP 48453 INSPECTION TYPE:1C EVALUATE EXISTING REPAIR DOUBLER AT FS 879 AND LONGERON 28L ON EXTERNAL SKIN. EXISTING REPAIR AT FS 879 AND LONG 28L DOES NOT MEET SRM CRITERIA. REMOVED EXISTING REPAIR, CUT OUT DAMAGED SKIN, FABRICATED REPAIR DOUBLER, TRIPLER, AND FINGER DOUBLER AND INSTALLED IAW MD-11 SRM 53-20-00 FIG. 2. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 SWAA082883 1 20080528 A 2121 215201 FAN BOEING 737 7377H4 1384404 NM E&E BAY FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 717SA 27851 FLIGHT CREW REPORTED A BURNING ELECTRICAL ODOR. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 2008UALA03090 1 20080529 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 LT OVERWING EMERGENCY EXIT LIGHTS INOP, 1ST AND 2ND FROM FWD POSITION. FOUND FAULTY LAMPS AND FUSE'S. REPLACED FUSE'S AND LAMPS OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 SO 2008 7 16 GLBA20061108 1 20080527 A 5330 SKIN EMB 120 EMB120ER 3260203 SO BS 1017 CHAFED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 299UX 120299 MAJOR REPAIR, RT FUSELAGE EXTERNAL PATCH AT FS 10172 STRINGER 17R AND 18R AT FRAME 30 CHAFED. MAINTENANCE REMOVED AND R EPLACED THE PATCH PER EMB-120 SRM 51-70. REPAIR AREA APPROXIMATELY 3 BY 7. .050 2024 T-3. RII INSPECTION COMPLIED PER TASKCARD 8.2.1. 2 L 7 2 4T RT A31SO 20080716 EA 2008 7 16 MASA200800427 1 20080527 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 521LR 8298 10261 ASH 7221 IAD. ALL EMERGENCY LIGHTS WILL NOT TURN ON. REPLACED BATTERIES. 2 L 7 2 4F RT A21EA 20080715 NM 2008 7 15 SWAA083823 1 20080713 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083817 1 20080713 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083816 1 20080713 A 3350 65C27028 LIGHT BOEING 737 7375H4 138449D NM CABIN DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED 18Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ASSY DISBONDED AT ROW 14 DEF. REPAIRED LIGHT ASSY PER M M. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083833 1 20080710 A 5330 65C257921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 737A, STR 4L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080716 WP 2008 7 16 08FDEA02139 1 20080603 A 5230 INTERCOSTAL DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 CENTER LOWER CARGO DOOR INTERIOR INTERCOSTAL JUST FWD OF THE UNLOCK ACTUATOR IS CORRODED. REMOVED THE INTERCOSTAL AND C RACKED BRACKET PER MD-10 SRM 51-35-01; VOL II. REMOVED THE DAMAGE FROM THE INTERCOSTAL. ORIGINAL MATERIAL 0.040; MATE RIAL REMOVED .005; REMAINING MATERIAL .035. FOUND TO BE WITHIN LIMITS PER MD-10 SRM 57-00-01; PG 5; VOL I. VERIFIED C RACKED BRACKET TO BE OUT OF LIMITS PER MD-10 SRM 52-00-01; FIG 2; VOL I. MATERIAL ID 7075-T6, .050 FOR THE BRACKET PER DAC DWG ADA3791; REV M. FABBED A NEW BRACKET PER DAC DWG ADA3791; REV M. ALODINED AND PRIMED THE INTERCOSTAL AND NEW BRACKET PER MD-10 SRM 51-21-01; VOL II. INSTALLED BRACKET. 2 L 7 3 4F RT A22WE 20080716 SO 2008 7 16 C2XA08ON127 1 20080526 A 4930 NUT EMB 145 EMB145XR 3260214 SO APU FUEL SYSTEM LOOSE A C2XA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 27 12163 14500811 FLT 0318 - ABQ - FLIGHT CREW REPORTED APU LEAKING FUEL WHILE ON THE GROUND. MX TIGHTEN APU FUEL VLV JAM NUT. OPERATION ALLY AND LEAK CHECK SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 20080716 SO 2008 7 16 C2XA08SH080 1 20080528 A 2910 1452342640 HYDRAULIC LINE EMB 145 EMB145LR 3260212 SO HYDRAULIC SYS CHAFED A C2XA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 27 19966 145131 SHV - AIRCRAFT 966, FLIGHT NUMBER 2504, EN ROUTE FROM IAH TO BIRMINGHAM HAD A NR 1 HYD SYSTEM FAILURE AT CRUISE ALTITUDE AND MADE AN EMERGENCY LANDING AT SHV. MAINTENANCE FOUND A CHAFED HYDRAULIC LINE AT FRAME 49-50 LT AND REPAIRED THE DIS CREPANCY IAW EMB 145 AMM 20-10-03. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 20080716 NM 2008 7 16 ASAA0873021 1 20080520 A 5753 113A214312 SKIN BOEING 737 737790 13844CN NM RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 613AS 30163 RT WING INBD MAIN FLAP UPPER AFT ACCESS PANEL HAS DENT AT OTBD SIDE. RT WING INBD MAIN FLAP UPPER AFT ACCESS PANEL DENT REPAIRED IAW B737 700 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080716 WP 2008 7 16 UPS08852354 1 20080423 A 5320 46198151 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 D-PIT STA 1380 LONG 23L HAS 1 EA WEB WITH CRACK AT AFT EDGE. FABRICATED AND REPLACED STA 1380/LONGER ON 23L WEB IAW DWG 4619815, SRM 51-01-08-0, SRM 51-01-21A AND SRM 51-01-21. 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 AALA200801284 1 20080512 A 3350 LENS BOEING 767 767223 1385123 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 321AA 22322 JFK - EMERGENCY LIGHT AT LEFT SIDE MID GALLEY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT SIDE MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080716 NM 2008 7 16 AALA200801292 1 20080512 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 758AN 32637 DFW - EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080716 NM 2008 7 16 UPS08M52372 1 20080524 A 5730 DOUBLER DOUG MD11 MD11F 3023600 NM RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C HAIRLINE CRACK 2 PLACES ON RT WING TOP OF ANTI-ICE TELESCOPIC DUCT CUT OUT CORNER. REMOVED DAMAGE IN 2 PLACES, FABRICATED FILLERS AND DOUBLER AND INSTALLED IAW MD-11 SRM 57-10-00, 51-31-01, AND 51-21-01F. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 USAA920081139 1 20080516 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - NR O3C10753638/1, CRACKED FLOORBEAM SUPPORT STRUCTURE, BS 540, BL 0 - LBL 24. REPAIRED CRACKED FLOORBEAM SUPPORT STRUCTURE, BS 540, BL 0 - LBL 24 IAW BOEING SRM 51-10-20 AND 51-00-00. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 2008UALA02989 1 20080524 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 CABIN FLOOR INTERCOSTAL AT STA 344 WL 208 IS CRACKED IN RADIUS AT THE FWD END. MAJOR REPAIR ACCOMPLISHED: REPLACED INT ERCOSTAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20080716 NM 2008 7 16 USAA920081125 1 20080513 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - CRACKED SEAT TRACK, BS 727B, LBL 25. REPAIRED SEAT TRACK BS 727B, LBL 25 IAW B737 SRM 53-00-52. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 GTIA0800065 1 20080425 A 5315 D53472193200 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 505NK 10470 10470 2485 FOUND CORROSION AT FLOORBEAM Y765 FR66 TO FR70. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 20080716 NM 2008 7 16 GTIA0800064 1 20080425 A 5315 D53472189202 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 505NK 2485 FOUND FLOORBEAM CORROSION AT Y1292 BETWEEN FR66 AND FR68. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 20080716 WP 2008 7 16 08FDEA01942 1 20080521 A 2750 4C9572 CHECK VALVE DOUG MD10 MD1010F 3022112 WP TE FLAPS FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 68052 47806 AFTER TAKEOFF, FLAPS UP GOT LEVEL 2 "FLAP DISAG". FLAPS INDICATED 8/7 (LEFT) AND 5/4 RIGHT WING. FLAP HANDLE BACK TO L AST POSITION AND FLAPS WOULD NOT MOVE. HANDLE BACK TO UP NO CHANGE, WHILE MANEUVERING TO LAND FLAPS INDICATED 3/1 AND U P. RETURNED TO MEM. FLAP HINGES, ACTUATORS, CARRIAGES, TRACKS, FLAP VANES, RIG POSITIONS AND IND POSITIONS ALL OKAY. FOUND LT O/B FLAP SPEED SLOWER THAN RT O/B CAUSING A SPLIT. REMOVED RESTRICTOR AND CHECK VALVES ON LT O/B FLAP CONTROL VALVE. FOUND FOD IN CHECK VALVES FILTERS. RESTRICTORS WERE CLEAN. INSPECTED NR 1 AND NR 2 HYDRAULIC ENGINE AND SYSTEM MANIFOLD FILTERS. NO EVIDENCE OF DEBRIS FOUND. REPLACED CHECK VALVES. EXTEND AND RETRACT SPEED NOW MATCH. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 DHL2008764531 1 20080529 A 5711 SPAR BOEING 727 727264 138408M NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C CHECK, LT WING REAR SPAR J BEAM CRACKED INDICATION WBL126. FABRICATED AND REMOVED AND REPLACED IAW BOEING DW G 65-21655 AND ASTAR EC-00910-001 MATERIAL BAC 1506-860 7075T6 DIM 81 INCH BY 5 1/2 INCH PO NR 815922. 2 L 7 3 4F A3WE 20080716 SO 2008 7 16 200805210001 2 20080521 A 8530 EC636397 CYLINDER CONT IO550C BEECH 58 58 1152740 CE CONT O550 IO550C SO NR 4 FAILED E N58A E ENGINE SHUTDOWN E VIBRATION/BUFFET TX TAXI/GRND HDL 1 GL 09 58GE 734 287391R TH1480 287391R BURN THROUGH HOLE FOUND ON TOP OF NUMBER 4 CYLINDER BETWEEN SPARK PLUG HOLE AND EXHAUST VALVE. 1 L 7 2 3O 3 O 3A16 E3SO 20080716 WP 2008 7 16 DHL2008807521 1 20080509 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 857 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 MAIN CARGO COMPT FRAME FITTING CRACKED 3 INCHES STA 857.125 L-19R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITT ING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 20080716 SO 2008 7 16 FDKA200805202 1 20080517 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 833MJ 145327 FDM 6031 JFK-IAD, ROW 12 EMERG LIGHT INOP. MX RESET SYSTEM. 2 L 7 2 4T RT T00011AT 20080716 WP 2008 7 16 DHL2008807523 1 20080509 A 5540 SKIN DOUG DC8 DC873F 302199F WP RUDDER CANNING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 RT RUDDER SKIN OIL CANNING (STA ZR 136.000 - 125.000) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 55-6-1 FIG 1. REMOV ED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING AND BONDED DOUBLER BOTH FROM AL2024T3 0.0 16" IAW SRM 55-6-1 FIG 1 ITEM "A". BONDED BOTH PARTS WITH HYSOL IAW SRM 51-1-9, TR NR 51-142, SRM 51-1-9A, TR NR 51-141 . CLEANED, TREATED AND PRIMED AREA AND PANEL PLATING IAW SRM 51-1-8B. INSTALLED PANEL PLATING IAW SRM 51-1-11, SRM 51- 1-21, SRM 51-1-21A. REFER TO NR 107097 FOR BALANCING. 2 L 7 4 4F RT 4A25 20080716 EA 2008 7 16 MASA200800435 1 20080530 A 5220 SEAL CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT DIRTY A MASA O OTHER O OTHER CR CRUISE 1 SW 07 930LR 15030 ASH FLT 2708 FAT-PHX. EMERGENCY EXIT DOOR AT ROW 16 HAD A LOUD SQUEAL IN FLIGHT. CLEANED DEBRIS FROM SEAL. 2 L 7 2 4F RT A21EA 20080716 EA 2008 7 16 MASA200800437 1 20080530 A 5270 SWITCH CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT DIRTY A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 926LR 15026 ASH FLT 2917 LAS-COS. LEFT FORWARD OVERWING EMERGENCY DOOR CAUTION MESSAGE. MX CLEANED DOOR SWITCHES, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080716 EA 2008 7 16 MASA200800413 1 20080521 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT OUT OF ADJUST A MASA O OTHER N FALSE WARNING LD LANDING 1 SW 07 923FJ 15023 ASH FLT 2741 OKC-PHX. AFT EMERGENCY DOOR CAUTION AFTER LANDING. ADJUSTED PROX SENSOR. 2 L 7 2 4F RT A21EA 20080716 NM 2008 7 16 SWAA082918 1 20080601 A 5753 65464257 FLAP TRACK BOEING 737 7373H4 1384600 NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND LT WING NR 2 FLAP TRACK CORRODED AT AFT MOUNT PAD. REMOVED AND REPLACED FLAP TRACK PE R MM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SWAA082919 1 20080601 A 5330 65C381921 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 932, STR 25R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SWAA082920 1 20080601 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505D, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SWAA082927 1 20080531 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 736SA 27868 DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SWAA082930 1 20080530 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 767SW 29807 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 45. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20080716 SO 2008 7 16 C2XAA08TY056 1 20080602 A 5720 PANEL EMB 145 EMB145XR 3260214 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12142 145735 TYS - DURING A CURRENT 3C INSPECTION PANEL 197 CL WAS FOUND CORRODED AT THE BONDING STRAP. MAINTENANCE REPAIRED THE PAN EL IAW EMB 135/145 EC 5750-01315 AND PAINTED IAW EMB 145XR AMM 51-21-02. ALL WORK WAS ACCOMPLISHED AND AIRCRAFT WILL BE RELEASED AT THE END OF THE CHECK. 2 L 7 2 4F RT 20080716 EA 2008 7 16 SWIA200819705 1 20080526 A 3520 OXYGEN MASK CNDAIR CL600 CL6002C10 1390015 EA CABIN UNLATCHED A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 614SK 10051 OXYGEN MASK IN FORWARD LAVATORY FELL OUT. FLIGHT 4004 - RESTOWED O2 MASKS AS REQUIRED. 2 L 7 2 4F RT A21EA 20080716 CE 2008 7 16 GLBA20061109 1 20080602 A 5730 SKIN BEECH 1900 1900D 1154162 CE WING DAMAGED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 220GL UE220 MAJOR REPAIR - DURING ROUTINE MX INSPECTION A REPORT OF A FUEL LEAK WAS REPORTED ON THE LEFT LEADING EDGE NEAR THE FUEL BARRIER BOX AT WS 194.8 WING SKIN. ALSO REMOVED TO FACILITATE REPAIR AT WS 177.8 - WS 226.8. **SUPPLEMENTAL INFORMATIO N WILL BE PROVIDED UPON COMPLETION OF THE REPAIR ** 2 L 7 2 4T RT A24CE 20080717 WP 2008 7 17 UPS08852566 1 20080530 A 5340 37799191N FITTING DOUG DC8 DC873F 302199F WP BS 1360 L35L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 D PIT STA 1360 L35L SPLICE FITTING CRACKED AND CORRODED. REMOVED AND REPLACED SPLICE FITTING IAW DC8 SRM 51-03-01 AND 51-01-20D. 2 L 7 4 4F RT 4A25 20080717 WP 2008 7 17 UPS08852567 1 20080530 A 5340 ATTACH FITTING DOUG DC8 DC873F 302199F WP BS 1230 L27L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 C PIT STA 1230 L27L ATTACH FITTING HAS CORROSION. REMOVED AND REPLACED LONGERON ATTACH FITTING IAW D C8 SRM 51-01-20D. 2 L 7 4 4F RT 4A25 20080717 NM 2008 7 17 UPS08B52551 1 20080327 A 5311 65B0175128 FRAME BOEING 747 747400 13848AT NM BS 1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:BCF RT BS 1160 TENSION TIE FRAME WEB CRACKED ABOUT 0.250 INCH. RT BS 1160 TENSION TIE FRAME WEB REPLACE D PER SRM 53-40-07 REPAIR 3. 2 L 7 4 4F RT A20WE 20080717 NM 2008 7 17 UPS08B52556 1 20080417 A 5311 65B01750802 FRAME BOEING 747 747400 13848AT NM BS 1140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:BCF RT BS1140 TENSION TIE FRAME CRACKED MORN THAN 0.060 INCH. RT BS 1140 TENSION TIE FRAME REPLACED PER SRM 53-40-07. 2 L 7 4 4F RT A20WE 20080717 NM 2008 7 17 UPS08B52558 1 20080417 A 5311 65B01750357 FAILSAFE BOEING 747 747400 13848AT NM BS 1140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:BCF LT BS 1140 TENSION TIE FRAME FAIL/SAFE CHORD CRACKED. LT BS 1140 TENSION TIE FRAME FAIL/SAFE CHORD REPLACED PER SRM 51-70-11. 2 L 7 4 4F RT A20WE 20080717 WP 2008 7 17 IXXA080024O 1 20080528 A 2612 FIRE LOOP DOUG DC8 DC871F 302199D WP NR ENGINE INTERMITTENT A IXXA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 11 820BX 90489 1410 46065 DURING CRUISE FROM KSJC TO KRFD NUMBER ONE ENGINE FIRE INDICATION AT FL 350 WITH FIRE WARNING LIGHT ON. AFTER SILENCING THE BELL THE CREW DISCHARGED THE FIRE AGENT, AFTER THIRTY SECONDS THE FIRE LIGHT REMAINED ON AND THE CREW DISCHARGED TH E SECOND BOTTLE AND THE FIRE LIGHT WENT OUT. THE FIRE LIGHT CAME BACK ON AT FL 096 AND REMAINED ILLUMINATED. THE CREW LANDED AT KRNO WITHOUT INCIDENT. MAINTENANCE INSPECTED NUMBER ONE ENGINE AND FOUND NO EVIDENCE OF FIRE, MAINTENANCE DID FIND RIGHT FAN CASE LOOP WOULD DROP FROM 2.M OHMS INTO K OHMS INTERMITTENTLY CENTER PIN TO GROUND. MAINTENANCE REPLACE D RIGHT FAN CASE LOOP, LEFT FAN CASE LOOP, UPPER PYLON LOOP, AND NUMBER ONE ENGINE FIRE DETECTOR. OPERATIONAL CHECK GOO 2 L 7 4 4F RT 4A25 20080717 NM 2008 7 17 UPS08M52502 1 20080508 A 5313 STRINGER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C LHW:UPPER FUEL TANK ACCESS NR 534CT INTERIOR COMPT, STRINGER NR 44 END SUSPECT CRACK. HFEC INSP C/O P ER DAC NDTSPM R13 06-10-01.001 AND FOUND CRACK APPROX 1/2 INCH. CRACKED AREA AT LHW STRINGER NR 44 END AREA SLOTTED PER SRM 57-2 0-00 V1 FIG 10 R35. NEW REPAIR SPLICE FAB PER SRM 57-20-00 VI FIG 10 R35. NEW FAB REPAIR SPLICE INSTALLED AT LHW ACCESS NR 534CT STRINGER NR 44 END AREA PER SRM 57-20-00 VI FIG 10 R35 AND SRM 51-33-01 VII R35. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 UPS08M52547 1 20080416 A 5740 FITTING DOUG MD11 MD11 3023602 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C RHW LOWER WINGLET (WING MOUNTED) FOUND ATTACH FITTING CRACKED. RHW LOWER WINGLET ATTACH FITTING REMOV ED. NEW FITTING FAB WITH FPI C/O, FOUND NO CRACK EVIDENT. NEW FITTING HOLES PICKED UP, PROTECTED AND PAINTED. NEW FIT TING INSTALLED AS PER SRM 51-33-01 VOL II, REV 35. 2 L 7 3 4F RT A22WE 20080717 WP 2008 7 17 UPS08852564 1 20080527 A 5347 365702U509 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 COPILOT REAR LT AND RT SEAT TRACKS SHOWS ELONGATION. REMOVED AND REPLACED SEAT TRACKS IAW SRM, 51-1- 20D, 51-3-1, 51-1-24 AN D 25-11-1. 2 L 7 4 4F RT 4A25 20080717 NM 2008 7 17 ASAA0843104 1 20080510 A 5330 65C323591 SKIN BOEING 737 7374Q8 138447Q NM BS 480-500 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 DENTS AT BS 480 500 STR 25L 26L. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843098 1 20080510 A 5330 65C323591 SKIN BOEING 737 7374Q8 138447Q NM BS 500E-500F DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 LT LOWER FUSELAGE EXTERIOR DENTED AT STA 500E TO 500F STR 26 TO 27. REPAIRED DENT IAW B737 400 SRM TR53 27 REPAIR 31 FI G 201. 2 L 7 2 4F RT A16WE 20080717 NE 2008 7 17 ASAA0853090 2 20080625 A 7261 QA07320ISS1 FILTER BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE NR 1 ENG OIL SUP DIRTY A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 570AS 35185 894536 LT ENG OIL FILTER POP OUT INDICATOR EXTENDED. REMOVED AND REPLACED LT ENG OIL SUPPLY FILTER PER MM79 21 03 000 802 F00. OPS AND LK CK GOOD. POP OUT IND CKS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 20080717 NE 2008 7 17 ASAA0853091 2 20080625 A 7261 QA07320ISS1 FILTER BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE NR 2 ENG OIL SUP DIRTY A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 570AS 35185 894523 RT ENG OIL FILTER POP OUT INDICATOR EXTENDED. DRAINED ENG OIL AND AGB PER 737 AMM 12 13 11. REMOVED AND REPLACED RT EN GINE OIL SUPPLY FILTER PER MM 79 21 00 802 FOO. OPS AND LEAK CHECK GOOD, POP OUT INDICATOR CKS GOOD. NO CONTAMINATION IN FILTER. 2 L 7 2 4F 4 F RT A16WE E2GL 20080717 NM 2008 7 17 ASAA0853069 1 20080618 A 2131 2193301AC CONTROLLER BOEING 737 737890 1384527 NM A/C PACK FAILED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 559AS 6918 35178 AUTO FAIL PRESSURE LIGHT IS ON WITH ALTN LIGHT NR 2 (FWD) CONTROLLER LOGGED THE FOLLOWING FAULTS: (1) CADC NR 1 INV (2) ALT NR 1 INV (3) AS NR 1 INV (4) CORALT NR 1 INV (5) GROUND MODE. DUE HISTORY IF THE NR 1 CPC AND FMC'S 1 2 DO NOT HAVE THE SAME AIRDATA FAULTS WHICH ARE ON THE SAME DATA BUS THEN REF WDM21 31 24 PG 2 SUGGEST CHECK WIRING TO NR 2 CPC FROM TB1111 YA1 ANDYB1 LOOK FOR INTERMITTENT CONTACT PROBLEMS. UNABLE TO DUPLICATE OPS CHECK GOOD AT BOTH CABIN PRESSURE CON TROLLERS. REMOVED AND REPLACED NR 1 CABIN PRESSURE CONTROLLER IAW BOEING AMM21 31 01. OPS CHECK GOOD. PRECAUTIONARY A ND RANG OUT WIRING FROM CPC NR 2 TO TB1111 YA1 ANDYB1, NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 20080717 SO 2008 7 17 CHQA200800100 1 20080530 A 2434 M832481113 O-RING EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL NR 3 GENERATOR BROKEN A CHQA E ENGINE SHUTDOWN K FLUID LOSS CL CLIMB 1 GL 11 283SK 145424 CAE312071 FLIGHT 5981, STL TO IAH. WHILE CLIMBING THROUGH FL190, THE CREW NOTICED THE OIL PRESSURE FOR E1 DECREASING BELOW 50 PSI . THE QUANTITY WAS THEN CHECKED AND IT INDICATED 2 QUARTS OF OIL. THE ENGINE WAS SHUTDOWN PER QRH PROCEDURES AND THE A IRCRAFT RETURNED TO STL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE SHAFT O-RING ON THE NR 3 GENERATOR WAS BROKEN AND ALLOWING OIL TO LEAK OUT. THE O-RING WAS REPLACED ACCORDING TO AMM 24-31-01 AND THE ENGI NE WAS OPS AND LEAK CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080717 EA 2008 7 17 CHQA200800103 1 20080530 A 7830 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE THRUST REVERSER ACTIVATED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 645BR 7383 GEE807232C FLIGHT 5640, IAH TO LIT. WHILE CLIMBING THROUGH 23,000FT THE FLIGHT CREW RECEIVED A R REV UNLOCKED EICAS MESSAGE. THE EMERGENCY ACTION ITEMS WERE RUN AND THE RELEVANT CHECKLISTS WERE COMPLETED. THE REVERSER WAS THEN STOWED, BUT THE R REV UNLOCKED MESSAGE REMAINED ON EICAS. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE COMPLIED WI TH THE MEL PROCEDURES FOR THE REVERSER AND RELEASED THE AIRCRAFT TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080717 NM 2008 7 17 ASAA0873041 1 20080605 A 5321 141A5810175 FLOOR PANEL BOEING 737 737790 13844CN NM LAVATORY BROKEN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 644AS 30795 FLOORBOARD UNDER FWD LAV BROKEN ALONG OUTBOARD EDGE STA 297 TO STA 309 LBL 54 TO LBL 57. PREPARED DAMAGED AREA. FILLED DAMAGED AREA WITH BMS 5 28 TYPE 19 AND BONDED 4 EACH LAYERS OF BMS 9 3 FABRIC IAW B737 700 SRM 53 00 53 REPAIR 1. 2 L 7 2 4F RT A16WE 20080717 NE 2008 7 17 ASAA0853034 2 20080604 A 7261 OIL SYSTEM BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE LOW A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 583AS 3476 35681 894763 NR 1 ENG QTY AT 13 NR 2 ENG QTY AT 15 SERVICED NR 1 ENG OIL TO FULL 5.5 QTS SERVICED NR 2 ENG TO FULL. 2 L 7 2 4F 4 F RT A16WE E2GL 20080717 NM 2008 7 17 CALA0800529 1 20080602 A 3244 Y07YS134 TIRE BOEING 737 737824 13844BZ NM MLG BLOWN A CALA K NONE O OTHER LD LANDING 1 SW 27 26210 28770 NORMAL LANDING AND ROLLOUT UNTIL 80-100 KTS. AIRCRAFT VEERED LEFT WITH AN ASSOCIATED LOUD POP. TOWER AND AIR CREW VERI FIED RIGHT MAIN OUTBOARD TIRE SEPARATION. NUMBER 3 AND 4 TIRES REMOVED AND REPLACED. PER AMM 05-51-54-210-801, TIRE BU RST INSPECTION OK PER AMM 05-51-16-210-801, FLAT SPOTTED TIRE INSPECTION FAILED TRANSDUCER OPS CHECK PORTION. FOUND NUM BER 3 TRANSDUCER HARNESS ON NUMBER 4 AND NUMBER 4 ON NUMBER 3. UNCROSSED HARNESS IN AXLE, TRANSDUCER OPS CHECK PASSED. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843055 1 20080610 A 5755 SKIN BOEING 737 7374Q8 138447Q NM NR 6 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 NR 6 SPOILER HAS SEVERAL DENTS ON THE LOWER SURFACE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR DOUBLERS IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 CALA0800536 1 20080603 A 5315 147A5506 FLOORBEAM BOEING 737 737724 13844BY NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 STATION 986.5 FLOORBEAM UPPER CHORD AFT FLANGE HAS CORROSION LBL 26. REPAIRED PER EC/RA 5321-01330 REVISION A. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843072 1 20080607 A 5755 SKIN BOEING 737 7374Q8 138447Q NM NR 4 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 LT WING INBD NR 4 GROUND SPOILER LOWER SURFACE HAS MULTIPLE DENTS AND A PUNCTURE HOLE. REMOVED DAMAGED AREA FABRICATED REPAIR PARTS AND BONDED REPAIR IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080717 2008 7 17 ASAA0853086 4 20080624 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM E/E BAY FAULTED A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 583AS 3711 35681 FMC DISAGREE FLAG DISPLAYED ON TAXI OUT CONFIRMED FAULT FMC DISAGREES MONITORING PARAMETERS. RESET BOTH FMC'S AND TEST NML PER FIM 34 61 00 810 807. INSPECTION ACCOMPLISHED FOR SIMULTANEOUS MAINTENANCE. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 USAA920081136 1 20080511 A 5320 WEB BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED WEB, BS 180, WL 230, BL 17.5 RIGHT. REPAIRED CRACKED WEB, BS 180, WL 230, BL 17 .5 RIGHT IAW BOEING SRM 53-10-08. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 USAA920081145 1 20080516 A 5751 65C2591118A AILERON BOEING 737 7373S3 1384711 NM RT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - RIGHT WING AILERON LEADING EDGE HAS DELAMINATION, WS 417. REPLACED RIGHT WING AILERON IAW US AIRWAYS TASK CARD JCR3M27015. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 UPS08B52385 1 20080417 A 5311 FAILSAFE BOEING 747 747400 13848AT NM BS 1140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:C LT BS 1140 TENSION TIE FRAME FAIL SAFE CHORD CRACKED. LT BS 1140 TENSION TIE FRAME FAIL SAFE CHORD RE PLACED PER SRM 51-70-11. 2 L 7 4 4F RT A20WE 20080716 WP 2008 7 16 08FDEA02120 1 20080603 A 5330 ADA3139501 SKIN DOUG DC10 DC1010F 3022111 WP ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 68059 46907 DURING REPAIR ASSESSMENT AN EXISTING REPAIR WAS FOUND AT FUSELAGE SKIN REPLACED EXISTING REPAIR IAW SRM53-50-00 FIG 9 BE CAUSE IT IS NOT IN COMPLIANCE WITH APPROVED DATA. 2 L 7 3 4F A22WE 20080716 NM 2008 7 16 2008UALA03066 1 20080528 A 5320 ANGLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 291.5 S12R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 BODY STATION 291.5 STRINGER S-12R WEB ANGLE CRACKED. MAJOR REPAIR ACCOMPLISHED, REMOVED AND REPLACED CRACKED ANGLE. 2 L 7 2 4F 4 F RT A16WE E2GL 20080716 NM 2008 7 16 2008UALA02854 1 20080518 A 3350 LENS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 EMERGENCY AISLE LIGHT BELOW STOW BIN AT SEATS 23DEF MISSING LENS COVER. SUPPLEMENTAL DATA UPDATE CAUSE, UNKNOWN. INSTA LLED MISSING LENS COVER. 2 L 7 2 4F 4 F RT A2NM E17NE 20080716 WP 2008 7 16 DHL2008807516 1 20080507 A 5320 ANGLE DOUG DC8 DC873F 302199F WP MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 RT MLG W/W ZEE ANGLE CRACKED 1 INCH STA XCW -3.000. REMOVED CRACKED ZEE ANGLE IAW SRM 51-1-21. CLEANED, TREATED AND PR IMED AREA IAW SRM 51-1-8B. INSTALLED NEW ZEE ANGLE IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 2008041800156 20080418 00156 SO 2008 4 18 RAIA00804009 1 20080409 A 2120 UNKNOWN EMB 145 EMB145 3260210 SO CABIN SMOKE A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 809HK 145187 FLT 8061 -ORD- SMOKE IN THE CABIN. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE AIRCRAFT LIGHTING AND THE BLEED AI R SYSTEM WITH NO DEFECTS NOTED. 2 L 7 2 4F RT T00011AT 2008041800157 20080418 00157 SO 2008 4 18 RAIA00804006 1 20080407 A 5210 COVER EMB 145 EMB145LR 3260212 SO PAX DOOR DAMAGED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 831HK 145232 FLT 7923 -STL- PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE INSPECTED THE DOOR AND FOUND THE AFT HINGE COVER STOPPING THE DOOR. THE COVER WAS REMOVED FOR REPAIR IAW GMM AND AMM PROCEDURES. 2 L 7 2 4T RT T00011AT 2008041800195 20080418 00195 NM 2008 4 18 USAA920080846 1 20080408 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT- MAJOR REPAIR - C4 CHECK - CORROSION ON FLOORBEAM AT BS 1680, WL 208.1, LBL 54 - RBL 54. REPAIRED FLOORBEAM IAW SRM 51-10-00, 51-21-02 AND 53-00-51 REPAIR 3. 2 L 7 2 4F RT A2NM 2008041800197 20080418 00197 NM 2008 4 18 USAA920080848 1 20080330 A 5320 146N5246U6 SUPPORT BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT- MAJOR REPAIR - C4 CHECK - CORROSION ON R4 DOOR DRAIN PAN SUPPORT AT BS 1661 - 1681. REPLACED SUPPORT IAW SRM 51-40 -02. 2 L 7 2 4F RT A2NM 2008041800198 20080418 00198 NM 2008 4 18 USAA920080849 1 20080331 A 5320 146N876948 ANGLE BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 22202 PIT - MAJOR REPAIR - C4 CHECK - CORROSION ON Z-ANGLE R4 DOOR SILL PLATE MOUNT AT BS 1640. REPLACED Z-ANGLE MOUNT IAW SR M 51-40-02. 2 L 7 2 4F RT A2NM 2008041800208 20080418 00208 EA 2008 4 18 REXA200800007 1 20080415 A 3520 OXYGEN MASK CNDAIR CL600 CL6002B19 1900309 EA CABIN UNWANTED DEPLOY A REXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 8718E 7718 IN CRUISE, PASSENGER OXYGEN MASKS DEPLOYED. SYSTEM INVESTIGATED, MASKS REPACKED AND AMM 35-21-09. OPERATIONAL CHECKS P ERFORMED WITH NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 2008041800209 20080418 00209 EU 2008 4 18 08FDEA01422 1 20080416 A 5320 A5397425920000 FLOOR SUPPORT AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 425FE 264 BULK PIT FLOOR SUPPORT AT FRAME 65 - 66 LBL 36 IS CORRODED. REPLACED IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 2008041800210 20080418 00210 WP 2008 4 18 08FDEA01423 1 20080416 A 5712 ARB1666501 RIB DOUG DC10 DC1010F 3022111 WP ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 68059 46907 DURING MD10 ACF MODIFICATION ON WING LT SIDE OUTBOARD SLAT NR 3 FOUND RIB P/N ARB1666-501 WITH EA 7 HOLES OVALIZED. R EPLACED RIB FOR SRM 51-35-01 VOL II AND DWG ARB1666. 2 L 7 3 4F A22WE 2008041800212 20080418 00212 WP 2008 4 18 08FDEA01425 1 20080416 A 5753 ARC1652 SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 40061 46973 RT WING OUTBD FLAP NR 80 FASTENERS LOOSE ON LOWER SKIN. REPAIR AREA IAW SRM 57-20-00 FIG.11 VOL.I. 2 L 7 3 4F A22WE 2008041800215 20080418 00215 EU 2008 4 18 08FDEA01428 1 20080416 A 5712 RIB AIRBUS 310 A310203 3930313 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 445FE 297 THE RIB 5 FWD BORE ON THE LT MLG IS CORRODED ON THE INSIDE, FOUND AFTER BUSHING WAS REMOVED. THE MAX DIAMETER OF 4.8405 HAS BEEN REACHED REMOVED LEVEL 1 CORROSION, AND REPAIRED LT MLG RIB 5 IAW FED EX EA 6-5710-118108. THIS IS AN AIRBUS R EPAIR WITH NO ASSIGNED PART NUMBER. 2 L 7 2 4F RT A35EU 2008041800216 20080418 00216 EU 2008 4 18 F3LA200800174 1 20080406 A 5315 NOTLISTED FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 916FR 1458 1876 DURING C4 S1 C CHECK INSPECTION REPORTED FLOORBEAM Y1292 SHOWS SIGNS OF CORROSION AT FRAME 16. MAINTENANCE REPLACED ON E SECTION OF THE BEAM IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 AND BLENDED OTHER AREA LOCATED AT 62.875" AFT OF FWD END OF BEAM IN ACCORDANCE WITH SRM 51-74-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE . 2 L 7 2 4F 4 F RT A28NM E37NE 2008041800217 20080418 00217 NM 2008 4 18 F3LA200800175 1 20080415 A 5320 D53470477208 STRAP AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 914FR 45 1841 DURING C4 S1 C CHECK INSPECTION REPORTED SURFACE CORROSION ON AFT CARGO BAY FLOOR STRAP FROM FLOOR STRAP 2350-2030 STRIN GER 38 LEFT. MAINTENANCE FABRICATED NEW STRAP OUT OF 2024-T3 .040 IN ACCORDANCE WITH THE REQUIREMENTS OF AIRBUS A319 DR AWING D53470477. PART WAS TREATED, PRIMED AND PAINTED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-21-11 AND SRM 51-42- 11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 2008041800219 20080418 00219 NM 2008 4 18 HALA08000528 1 20080414 A 5540 2915873501 BALANCE WEIGHT BOEING 717 717200 1383700 NM RUDDER BROKEN A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 HA479 55124 FOUND RUDDER THROW LIMITER BALANCE WEIGHT ARM BROKEN. REMOVED AND REPLACED RUDDER THROW LIMITER BALANCE WEIGHT AND ARM PER O/H MANUAL 27-20-6. ACCOMPLISHED FUNCTION TEST RUDDER THROW LIMITER ACTUATOR ASSY AMM27-26-01-820-802. 2 L 7 2 4F TR A6WE 2008041800220 20080418 00220 2008 4 18 HALA08000529 4 20080414 A 3420 3103455 CONTROL PANEL BOEING 767 7673CB 1385187 NM EFIS FAILED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 592HA 33468 ETOPS SIGNIFICANT SYSTEMS, F/O HSI RANGE SELECTOR WILL NOT GO INTO 320 RANGE, ALL OTHERS WORK OK. REMOVED AND REPLACED F/O EFIS CONTROL PANEL IAW AMM 34-22-02-201. ACCOMPLISHED MCDP TEST 40 TEST CHKS OK. LMP STATUS REMAINS IN LAND 3. 2 L 7 2 4F RT A1NM 2008041800224 20080418 00224 NM 2008 4 18 UIEA200800144 1 20080408 A 5311 FRAME BOEING 747 747243B 1384830 NM ZONE 200 DEFORMED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 517MC 23300 MAIN DECK STA 1780 STRINGER 15R FRAME FOUND DEFORMED. FRAME REPAIRED PER ATLAS EO NR 4753B141. 2 L 7 4 4F RT A20WE 20080716 SO 2008 7 16 C2XA08TY055 1 20080601 A 2810 14538951401 BRACKET EMB 145 EMB145XR 3260214 SO FUEL TANK CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12142 145735 TYS - DURING A CURRENT 2C INSPECTION THE VENTRAL TANK FWD CENTER BRACKET WAS FOUND CORRODED. MAINTENANCE CUT OUT THE DA MAGE AREA, FAB A FILLER, SHIM AND EXTERNAL DOUBLER. APPLIED SEALANT AND ANTI-BACTERIAL COMPOUND PLUS A FUEL BARRIER SEA LANT. LEAK CHECK GOOD. WORK WAS ACCOMPLISHED IAW EC 2810-01032. AIRCRAFT WILL BE RELEASED AT THE END OF THE CHECK. 2 L 7 2 4F RT 20080716 CE 2008 7 16 DJFA2008048 1 20080528 A 5511 45A21146006 RIB BEECH MU300 400A 1155402 CE HORIZ STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 468LX 1692 RK468 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER INBOARD RIB AND BRACKET ASSEMBLIES, THE RIGHT HORIZONTAL INBOARD RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRU CTIONS OF THIS AREA ARE OUTLINED IN BEECHJET COMMUNIQUE' NUMBER 70. SDR WILL BE UPDATED UPON COMPLETION OF CORRECTIVE A CTION. 2 H 7 2 4F RT A16SW 20080716 SO 2008 7 16 SWIA200819702 1 20080526 A 4930 B-NUT EMB 120 EMB120ER 3260203 SO APU LOOSE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 07 298SW 120328 WITH APU BLEED ON, THE CABIN SMELLS LIKE FUEL. TIGHTENED FUEL NOZZLE MANIFOLD B-NUT. NO LEAKS NOTED. 2 L 7 2 4T RT A31SO 20080717 WP 2008 7 17 ASAA0883085 1 20080624 A 5210 4916044502 FITTING DOUG DC9 DC983 3022083 WP L1 DOOR WORN A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 961AS 53075 F/A REPORTS L 1 DOOR DIFFICULT TO CLOSE FOUND BAYONET FITTING WORN. REMOVED LINER, REMOVED SLIDE, REMOVED REPLACED BAYO NET FITTING. FUNCTION CKD L 1 DOOR AS REQUIRED PER MM 52 11 00. REINSTALLED LINER. REINSTALLED SLIDE, OPS CKD DOOR, O PS CKD GOOD PER MM 25 62 00 52 11 01. 2 L 7 2 4F RT A6WE 20080717 NM 2008 7 17 MWEA080082 1 20080603 A 5330 5911410347 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 601ME 49762 FUSELAGE SKIN IS DAMAGED FROM STATION 275 TO STATION 313, BETWEEN LONGERON 24 LEFT & LONGERON 25 LEFT. CUT OUT DAMAGE. FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 20080717 NM 2008 7 17 ASAA0843080 1 20080606 A 5311 65C2523054 FRAME BOEING 737 7374Q8 138447Q NM BS 727E S22-23L DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 AFT CARGO PIT BS 727E BETWEEN STR 22L AND 23L TOP FLANGE OF FRAME DENTED. FRAME REPAIRED WITH REPAIR PART IAW B737 400 SRM 51 70 11. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843082 1 20080506 A 5311 65465262 FRAME BOEING 737 7374Q8 138447Q NM BS 400 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 LT FRAME AT STA 400 CRACKED AT PSU RAIL BRACKET. REPAIRED IAW ASA EA5310 02797. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843083 1 20080507 A 5311 65582802 FRAME BOEING 737 7374Q8 138447Q NM BS 360 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 LT FRAME AT STA 360 CRACKED AT PSU RAIL BRACKET. REPAIRED IAW EA5310 02797. 2 L 7 2 4F RT A16WE 20080717 SO 2008 7 17 SIMA200815102 1 20080527 A 2611 FDS765A2 SMOKE DETECTOR EMB 135 EMB135LR 3260305 SO LAVATORY FALSE ACTIVATION A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 713AE 145249 ON FLIGHT 3456 ON CLIMB-OUT, CREW REPORTED LAV SMOKE WARNING. CREW RETURNED TO FIELD. AIRCRAFT REMOVED FROM SERVICE. REMOVED LAV SMOKE DETECTOR IAW AMM 26-14-01. OPERATIONAL CHECK GOOD IAW EMB AMM 26-14-00. NO FURTHER DEFECT NOTED. PE RFORMED BOROSCOPE INSPECTION OF LEFT AND RIGHT ENGINES INLET AREA NO.0 CARBON SEAL AND FOUND NO EVIDENCE OF ANY LEAKS AS PER RRMM 72-00-00. PERFORMED ETN NR EM-72-034 R4. NO DEFECT NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20080717 EU 2008 7 17 BA08020 1 20080529 A 7711 71N211401 SENSE LINE AIRBUS 330 A330323 3930335 EU P4.95 BROKEN A USAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 19 270AY 0315 MAN FLT 735 EN ROUTE MAN TO PHL. DURING TAKEOFF ROLL, ECAM MESSAGE 'L ENG EPR MODE FAULT' WAS GENERATED. THE FLIGHT REJECTED THE TAKEOFF AT APPROXIMATELY 100 KNOTS AND MADE A HIGH ENERGY STOP. THE REJECTED TAKEOFF RESULTED IN A BLOWN N UMBER ONE TIRE. THE AIRCRAFT REQUIRED TO BE TOWED BACK TO THE GATE. MAINTENANCE FOUND THE P4.95 SENSE LINE BROKEN AT C LAMP. MAINTENANCE REPLACED THE P4.95 SENSE LINE. 2 L 7 2 4F RT A46NM 20080717 NM 2008 7 17 HALA0800610 1 20080531 A 2910 HYDRAULIC SYSTEM BOEING 767 767300 1385204 NM LEFT MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM - LEFT SYS ELECT HYD PUMP NO PRESSURE PRIOR TO PUSHBACK. RESET LEFT SYS ELECT. HYD PUMP C/B. PUMP OPS CHECK GOOD. NO FAULTS NOTED. PRESSURE AT 3040 PSI. OK TO CONTINUE. 2 L 7 2 4F RT A1NM 20080717 NM 2008 7 17 HALA0800608 1 20080530 A 3412 CIRCUIT CARD BOEING 767 767300 1385204 NM TAT SYSTEM MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM - "TAT" OVERHEAD TEST LIGHT PANEL LIGHT DOES NOT ILLUMINATE ON GROUND. PROBE IS POWERED ON GRO UND CONSTANTLY. RERACKED NR 1 AND NR 2 SPEED CARDS PER MM 77-12-01. GND CHECK OK. 2 L 7 2 4F RT A1NM 20080717 NM 2008 7 17 SWAA083321 1 20080618 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 460, STR 13R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0853035 1 20080602 A 5320 143A9403188 INTERCOSTAL BOEING 737 737890 1384527 NM BS 495 S19-25R CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 566AS 35181 CRACK IN FWD PIT RT SIDE STRAP AFT OF CARGO PIT DOOR 8 INCHES UP SIDEWALL FROM CARGO NET FLOOR ATTACH POINT. STOP DRILL ED CRACK. REPLACED STRAP (INTERCOSTAL WEB) WITH FABRICATED REPAIR PART IAW BOEING DWG NR 143A9403 AND SRM 51 30 01 51 4 0 05 AND 53 30 15.5.0 QTS APU 0 QTS ADDED LIMITS. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843027 1 20080514 A 5753 SKIN BOEING 737 737490 1384715 NM RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 RIGHT INBOARD FORE FLAP LOWER SURFACE 3 EACH SMALL PUNCTURES AT CENTER TRACK AREA PREPARED DAMAGED AREA. FABRICATED FIL LER AND REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR NR 2. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083331 1 20080618 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 444WN 29839 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT LENS MISSING AT ROW 18 DEF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 DHL2008764532 1 20080529 A 5711 SPAR BOEING 727 727264 138408M NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 WHILE AT C CHECK, RT WING REAR SPAR J BEAM CRACKED WBL 126. FABRICATED AND REMOVED AND REPLACED IAW BOEING DWG 65-21655 AND ASTAR EC-00911-001. 2 L 7 3 4F A3WE 20080717 NM 2008 7 17 SWAA083333 1 20080618 A 3350 417A5601 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 456WN 32463 DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083338 1 20080618 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULE 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 SW 2008 7 17 L412008F00000 1 20080703 A 2140 2199017 ACTUATOR ECLIPS EA500 ECLIPSEEA500 3350000 SW CABIN HEATER OUT OF ADJUST E L41A O OTHER O OTHER NR NOT REPORTED 1 EA 61 568EA 000168 PILOT REPORTED A BLEED AIR TEMP OVERHEAT CAS MESSAGE DURING NORMAL FLIGHT. DURING GROUND TESTING, FOUND THE VORE WOULD NOT ACTUATE. THE ACTUATOR APPEARED TO BE MISADJUSTED. A POSSIBLE CAUSE WAS A MISADJUSTED VORE DOOR ACTUATOR. VERIFYING PROPER CALIBRATION OF ACTUATOR COULD PROLONG LONGEVITY. THERE WAS ALSO MOISTURE COLLECTING IN FAIRING BELOW THE ACTUAT OR MOTOR. THIS COULD CONTRIBUTE TO MOISTURE COLLECTING IN THE ACTURATOR. IT APPEARED THAT SOME MOISTURE HAD COLLECTED AROUND THE END SHAFT OF THE ACTUATOR AND THE LOWER MOTOR BODY SCREWS. RECOMMEND HAVING A METHOD OF DRAINING MOISTURE FR O COLLECTING IN FAIRING. (K) 1 L 7 2 4J RT A00002AC 20080717 EU 2008 7 17 PNS2008F00000 1 20080519 A 3350 BULB SAAB SF340 340B 7860101 EU GE CT7TS CT71 30030 NE EMERGENCY LIGHTS BURNED OUT A PNSA O OTHER O OTHER NR NOT REPORTED 1 AL 03 679PA 340B345 DURING CABIN CREW TRAINING THE EMERGENCY LIGHTS WERE ACTIVATED AND THE ARM LIGHT FAILED TO ILUMINATE. MAINTENANCE REPLA CED THE BULB AND THE SYSTEM TESTED, OK. NO EMERGENCY ACTION WAS TAKEN AS THIS WAS AN ON GROUND TRAINING. AIRCRAFT WAS RELEASED FOR SERVICE. (K) 2 L 7 2 4T 4 U RT A52EU E8NE 20080717 NM 2008 7 17 SWAA083344 1 20080618 A 5743 115A5211 FITTING BOEING 737 7377H4 1384404 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 739GB 29275 DURING SCHEDULED MV2 CHECK, FOUND RIGHT MLG FWD TRUNNION FITTING LUG CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NE 2008 7 17 M7K2008F00007 2 20080512 A 7200 790081 MAGNETIC SEAL UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE LEAKING E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 812MH 109 3956 SHORTLY AFTER ENGINE OVERHAUL WAS COMPLETED AND ENGINE RETURNED TO FLIGHT STATUS THE POWERSHAFT SEAL BEGAN TO WEEP AND P ROGRESSIVELY THE WEEP BECAME A LEAK. A NEW SEAL WAS INSTALLED AND NO FURTHER LEAKAGE WAS NOTED. SUGGEST IMPROVED QUALI TY CONTROL FOR THESE SEALS BEFORE INSTALLATION MAY BE REQUIRED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080717 EU 2008 7 17 M7K2008F00010 1 20080512 A 6220 350A31182703 FREQ ADAPTER UROCOP UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE MAIN ROTOR HUB CRACKED A M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 821MH 1294 M2877 4134 23319 (REF 0429084134) DURING ROUTINE INSPECTION, THE ELASTOMER ON (1) FREQUENCY ADAPTER WAS FOUND CRACKED. A NEW SET OF (3) ADAPTERS WAS INSTALLED. THIS IS A VERY COMMON DEFECT FOR THIS PART. SUGGEST A DIFFERENT ELASTOMER FORMULATION BE UTILIZ ED. AN OLDER PN FREQUENCY ADAPTER HAD A FORMULATION THAT RARELY FAILED. THE MFG IS HAVING DIFFICULTY PRODUCING ENOUGH O F THESE FAILURE PRONE PART TO MEET DEMAND. RETURNING TO THE OLDER FORMULATION HAS BEEN SUGGESTED TO THE AC MFG FOR YEAR S WITH O ACTION TAKEN. 1 G 7 2 3U 3 U H9EU E00054EN 20080717 NM 2008 7 17 SWAA083346 1 20080618 A 5753 6573731 FLAP BOEING 737 7377Q8 1384418 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 799SW 28209 DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20080717 WP 2008 7 17 A8O2008F00000 2 20080614 A 7314 307085057 PUMP BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE731* 01518 WP FUEL SYSTEM FAILED E A8OA O OTHER O OTHER NR NOT REPORTED 1 SO 11 24JG 258170 EMERGENCY ACTION TAKEN DURING FLIGHT DUE TO A COMPONENT OR SYSTEM MALFUNCTION. AFTER DUAL ENGINE REPLACEMENT DUE TO MPI , ON TEST FLIGHT, CREW DISCOVERED DUAL FUEL OVERTEMP ANNUNCIATOR LIGHTS CAME ON. CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE WHERE THEY MADE AN UNEVENTFUL LANDING. FOUND BOTH ENGINES FUEL PUMPS BD. PN 307085057. NR 1 ENGINE FUEL P UMP; SN OFF MX378833, SN ON MX413446. NR 2 ENGINE FUEL PUMP; SN OFF MX445829, SN ON MX429061. ENGINE MODEL; TFE 731. NO VISIBLE DEFECTS WERE NOTED. FUEL PUMPS REMOVED WERE EXPECTED TO BE RETURNED TO MFG FOR TEARDOWN ANALYSIS. BOTH ENGINE FUEL PUMPS WERE REPLACED WITH OVERHAULED UNITS. NEW FUEL FILTERS INSTALLED. MAINTENANCE PROVIDER ACCOMPLISHED GROUND R 2 L 7 2 4F 4 F RT A3EU E6WE 20080717 CE 2008 7 17 GLB2008F00000 1 20080627 A 3230 1013830083 VALVE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA MLG WORN A GLBA O OTHER O OTHER NR NOT REPORTED 1 NM 21 211GL 2315 UE211 AC 211GL, AIR RETURN FLT NR 5066 "GBD" 06/27/08. PILOTS REPORTED THAT AFTER GEAR RETRACTION, THE GEAR WOULD NOT RETRACT. APPROXIMATE SPEED AT THE TIME WAS 106 KTS. "3" GREEN LIGHTS, NO RED GEAR UNSAFE LIGHTS. MAINTENANCE REMOVED AND REPLA CED SERVICE VALVE IAW MM32-30. MAINTENANCE ALSO REPLACED THE RT MLG SQUAT SWITCH AND RIGGED IAW MM 32-60. OPS CHECK OF GEAR WAS GOOD. (K) 2 L 7 2 4T 3 T RT A24CE E2NE 20080717 SO 2008 7 17 JIK2008F00001 1 20080701 A 2140 TUBE PIPER PA31 PA31350 7103110 SO COMBUST HEATER MALFUNCTIONED A JIKA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 WP 01 29UM 5008228 317652127 THE PILOT REPORTED THAT THE CO2 DETECTOR TURNED BLACK AND DETECTED EXHAUST DURING THE FLIGHT. MX PERFORMED A DECAY TEST ON THE HEATER AND IT FAILED. FIRST POST OVH DECAY TEST WAS DUE IN 139 HOURS TT ON THE CERAMIC COMBUSTION TUBE. TUBE WAS 1121. MFG RECOMMENDED TBO FOR THIS UNIT IS 1500 HOURS. THIS UNIT WAS OVERHAULED AT 900 HOURS. THE COMBUSTION TUBES AR E OK TO REINSTALL AFTER DETAILED VISUAL INSPECTION, WHICH THIS TUBE PASSED. IT IS SUGGESTED THAT THE IMPROVED CERAMIC C OATED COMBUSTION TUBES BE REPLACED AT OVERHAUL, AND THAT THE OVERHAUL PERIOD BE REDUCED, AS THIS TUBE WOULD NOT HAVE MAD E IT TO A "NORMAL" OVERHAUL. (K) 1 L 7 2 3O A20SO 20080717 NM 2008 7 17 SWAA083218 1 20080612 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083082 1 20080608 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083076 1 20080608 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008041800225 20080418 00225 NM 2008 4 18 UIEA200800155 1 20080413 A 5753 ACCESS PANEL BOEING 747 7472D7B 1384803 NM RT WING TE FLAP CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 RIGHT WING TRAILING EDGE INBOARD MIDFLAP LOWER SURFACE ACCESS PANEL WBL 240.00 HAS SIGNS OF CORROSION. REMOVED AND REPA IRED CORROSION AT WBL 240.00 PER SRM 57-40-20. 2 L 7 4 4F RT A20WE 2008041800226 20080418 00226 NM 2008 4 18 UIEA200800156 1 20080416 A 5753 PANEL BOEING 747 7472D7B 1384803 NM TE FLAP DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 NR 1 KNEE CAP PANEL UNDER SURFACE DELAMINATED. REPAIRED PER EO NR 4757A431 AND SRM 51-40-14 AND 51-40-15. 2 L 7 4 4F RT A20WE 2008041800227 20080418 00227 NM 2008 4 18 UIEA200800157 1 20080414 A 5753 FLAP BOEING 747 7472D7B 1384803 NM LT TE FLAP PERFORATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 LEFT INBOARD FOREFLAP PERFORATED APPROX 12 INCH INBOARD FROM IT'S OUTBOARD EDGE APPROX WS 1178. REPAIR CARRIED OUT IAW EO NR 4757A432. 2 L 7 4 4F RT A20WE 2008041800243 20080418 00243 NM 2008 4 18 USAA920080864 1 20080407 A 5320 SUPPORT ANGLE BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 529AU 24411 CLT - MAJOR REPAIR-C6 - SUPPORT ANGLE AT BS 350, BL 0 HAS 1" X 5" AREA OF CORROSION. REMOVED ANGLE, INSTALLED REPAIR PA RT IAW EA 100408. 2 L 7 2 4F RT A16WE 2008041800270 20080418 00270 NM 2008 4 18 2008UALA02058 1 20080409 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY EXIT EEL LIGHT INOP, AT DOOR 5 RIGHT AFT CROSS AISLE AFT LOWER WALL. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041800271 20080418 00271 NM 2008 4 18 2008UALA02059 1 20080409 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY EXIT EEL LIGHT INOP ACROSS DOOR 4 RIGHT AISLE WALL EEL. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041800272 20080418 00272 NM 2008 4 18 2008UALA02060 1 20080409 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY EXIT EEL SIGN INOP, AT DOOR 4 RIGHT FWD SIGN. REPLACED BATTERY. 2 L 7 4 4F 4 F RT A20WE E24NE 2008041800273 20080418 00273 WP 2008 4 18 IXXA080014O 1 20080417 A 2997 WIRE DOUG DC8 DC873F 302199F WP HYD PUMP BROKEN A IXXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 11 605AL 98793 2232 46106 DURING CRUISE FROM KLRD TO KDFW ,THE CREW OBSERVED ONE OF THE MAIN HYDRAULIC PUMPS WOULD NOT BYPASS. THE CREW DIVERTED TO KIAH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE MAIN HYDRAULIC PUMP SYSTEM AND FOUND A BROKEN WIRE ON TH E NUMBER TWO MAIN HYDRAULIC PUMP BYPASS SOLENOID. MAINTENANCE REPAIRED THE BROKEN WIRE ON THE NR 2 HYDRAULIC PUMP BYPAS S SOLENOID IAW DOUGLAS DC-8 MM 20-50-1. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 2008041800274 20080418 00274 WP 2008 4 18 NWAA081619860 1 20080416 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 769NC 47757 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE TAILCONE AND FOR THE VENTRAL STAIRWAY WE RE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK (B5-28) AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 2 L 7 2 4F RT A6WE 2008041800277 20080418 00277 SO 2008 4 18 C2XA08CL051 1 20080413 A 3397 78241 CONNECTOR EMB 145 EMB145XR 3260214 SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 24128 145700 DURING ROUTINE MAINTENANCE THE EMERGENCY EXIT SIGN AT COCKPIT DOOR AND THE FORWARD OVERHEAD EMERGENCY EXIT SIGN WERE FOU ND INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR OF THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 2008041800298 20080418 00298 NM 2008 4 18 USAA920080809 1 20080328 A 5751 AILERON BOEING 737 7374B7 1384702 NM LT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A 1" AREA OF DELAMINATION ON LEFT AILERON AT MIDDLE HINGE AREA. REPLACED AILERON IAW JO B CARD O3L30627001. 2 L 7 2 4F RT A16WE 2008041800304 20080418 00304 NM 2008 4 18 USAA920080815 1 20080407 A 5315 ATTACH ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT - MAJOR REPAIR - Q6 CHECK - A .125" CRACK ON FLOORBEAM ATTACH ANGLE AT BS 328, RBL 32. INSTALLED REPAIR IAW SRM 51- 10-02 AND DWG 65-45839. 2 L 7 2 4F RT A16WE 2008042300288 20080423 00288 NM 2008 4 23 SWAA081983 1 20080413 A 5311 6546558 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300291 20080423 00291 NM 2008 4 23 SWAA081986 1 20080413 A 5311 6546548 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300299 20080423 00299 NM 2008 4 23 2008UALA02253 1 20080416 A 3510 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE OXYGEN MASK LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 305UA 23666 CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. FOUND FIRST OBSERVERS O2 MASK LEAKING AT QUICK DISCONNECT FITTING, REPLACED MASK AND STOWED PER AMM 35-12-85 FOUND B-NUT LEAKING ON EXTERNAL FILL VLV. (B-NUT LOCATED INSIDE BOTTL E ACCESS PANEL) SECURED B-NUT LEAK CHECKED PER MM 35-12-00 501. SERVICED OXYGEN TO 1850 PSI. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E2GL 20080717 NM 2008 7 17 SWAA083077 1 20080608 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083079 1 20080608 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083100 1 20080607 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 438WN 29833 EEPLS INOP AT ROW 6 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083101 1 20080607 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 452WN 29846 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083094 1 20080608 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083084 1 20080608 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083296 1 20080617 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 258WN 32516 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083284 1 20080616 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 283WN 36610 EEPLS END CAP LOOSE AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083297 1 20080617 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 283WN 36610 EEPLS LIGHT ASSY LOOSE AT ROW 3 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083286 1 20080617 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 27R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083301 1 20080617 A 2730 6545187 TORQUE TUBE BOEING 737 7373H4 1384600 NM LT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED 20Y CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083309 1 20080617 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 425LV 29829 EEPLS LIGHT INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080717 2008 7 17 WAI2008F00001 4 20080617 A 8300 30721167 PLANETARY GEAR ISRAEL 1124 1124 4500102 EU GARRTT TFE731 TFE73131G 29003 NE ACCESSORY G/B BROKEN E WAIA O OTHER O OTHER NR NOT REPORTED 1 SW 09 211ST 303 DURING A PREFLIGHT INSPECTION, DISCOVERED NR 2 ENGINE FAN WOULD NOT ROTATE. DISCOVERED PLANETARY GEARSHAFT HAD A MISSING TOOTH. PERFORMED A 4200 HR. FAN SUPPORT INSPECTION; REPLACED PLANETARY GEARSHAFT; BALANCED FAN ASSY; DRAINED OIL SYSTEM AND REPLACE OIL FILTER; RESERVICED OIL SYTEM WITH 254 TURBINE OIL. PERFORMED VIBRATION SURVEY AND ACCESSORY GEARBOX PRE SSURE CHECK. NO DEFECTS NOTED. PERFORMED ENGINE GROUND PERFORMANCE CHECK; PERFORMED OPS CHECK FLIGHT; NO DEFECTS NOTED. (K) 2 M 7 2 4F 4 F A2SW E6WE 20080717 NM 2008 7 17 SWAA083312 1 20080617 A 3211 65633789 LINK BOEING 737 7375H4 138449D NM RT MLG TRUNNION CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED SPV CHECK, FOUND RT MLG TRUNNION LINK CORRODED. REMOVED AND REPLACED LINK PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083259 1 20080613 A 3350 3034321 LIGHT BOEING 737 7375H4 138449D NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083260 1 20080614 A 3350 65C27093 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 506SW 24183 L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 2008042300306 20080423 00306 NM 2008 4 23 SWAA081949 1 20080413 A 5311 6546539 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT RIGHT BS 616 INBOARD LOWER END. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008042300308 20080423 00308 NM 2008 4 23 SWAA081971 1 20080413 A 5330 6545776 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CHAFED AT BS 860 TO BS 862 STR 1. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042300313 20080423 00313 NM 2008 4 23 SWAA081972 1 20080410 A 5330 65C357781 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 607SW 27927 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300320 20080423 00320 NM 2008 4 23 SWAA081959 1 20080410 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 759GS 30544 DURING SCHEDULED MV2 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 2008042300333 20080423 00333 NM 2008 4 23 SWAA082002 1 20080414 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300339 20080423 00339 NM 2008 4 23 SWAA082009 1 20080414 A 5311 6546529 BELTFRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED BRDG CHECK, FOUND BELT FRAME CRACKED AT BS 277, STR 16R. REPAIRED BELT FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300344 20080423 00344 NM 2008 4 23 SWAA082012 1 20080414 A 5311 6516301 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 15R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 2008042300345 20080423 00345 NM 2008 4 23 SWAA082003 1 20080414 A 5310 6546956 CREASE BEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 440 TO BS 460, LBL 65. REMOVED AND REPLACED WEB PER SR M. 2 L 7 2 4F RT A16WE 2008042300346 20080423 00346 NM 2008 4 23 SWAA081994 1 20080414 A 5340 6936600 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 278, RBL 60. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300347 20080423 00347 NM 2008 4 23 SWAA081993 1 20080414 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 460, STR 18L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008042300348 20080423 00348 NM 2008 4 23 SWAA082004 1 20080414 A 5320 BAC14902738 STIFFENER BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 277, LBL 12, WL 208. REPAIRED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 2008042300353 20080423 00353 EA 2008 4 23 MASA200800318 1 20080414 A 5270 PROXIMITY SWITCH CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT OUT OF ADJUST A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 905J 15005 ASH FLT 2732 PHX-LGB. RIGHT AFT EMERGENCY DOOR CAUTION INTERMITTENT. MX ADJUSTED PROX SWITCH. 2 L 7 2 4F RT A21EA 2008042300356 20080423 00356 EA 2008 4 23 MASA200800322 1 20080415 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCONNECTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37178 7178 ASH FLT 2728 PHX-LGB. RIGHT EMERGENCY DOOR LIGHT INOP. MX RECONNECTED THE POWER STRIP, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 2008042300358 20080423 00358 NM 2008 4 23 SWAA082029 1 20080415 A 5322 6546536 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 540, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 2008042300359 20080423 00359 NM 2008 4 23 SWAA082014 1 20080415 A 5310 6545875 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 277 TO BS 360, STR 17L. REMOVED AND REPLACED WEB PER S RM. 2 L 7 2 4F RT A16WE 2008042300361 20080423 00361 NM 2008 4 23 SWAA082023 1 20080415 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300369 20080423 00369 NM 2008 4 23 SWAA082020 1 20080415 A 5330 6545800 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 275 TO BS 279, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 2008042300376 20080423 00376 NM 2008 4 23 CALA0800334 1 20080417 A 3350 D71702030 CHARGER BOEING 737 737824 13844BZ NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 35260 30855 RIGHT AFT EXTERIOR OVERWING EXIT LIGHT INOP. RELAMPED RIGHT AFT EXTERIOR OVERWING LIGHT PER AMM 33-51-04, NO HELP. FOU ND M1671 EMERGENCY PWR SUPPLY BAD. REMOVED & REPLACED M1671 EMERGENCY PWR SUPPLY (CHARGER & BATTERY PACK) PER AMM 33-51 -06. LIGHT OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 2008042300377 20080423 00377 NM 2008 4 23 SWAA082031 1 20080416 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042300381 20080423 00381 NM 2008 4 23 SWAA082033 1 20080416 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 973, 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 2008042300383 20080423 00383 NM 2008 4 23 SWAA082044 1 20080416 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042300396 20080423 00396 NM 2008 4 23 SWAA082046 1 20080417 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 219WN 32490 EEPLS LIGHT LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 2008042300405 20080423 00405 NM 2008 4 23 SWAA082050 1 20080417 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 2008042400006 20080424 00006 WP 2008 4 24 08FDEA01474 1 20080422 A 5315 AEA03611 FLOORBEAM DOUG MD10 MD1010F 3022112 WP BS 1295 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 367FE 46605 CABIN OVERWING FLOORBEAM IS CRACKED AT STA 1295 RBL 107 AT THE R-3 DOOR THRESHOLD. REPAIRED CRACKED BEAM AT STA 1295 BY SPLICING IN A NEW SECTION IN REF TO EA 8-5310-118482. 2 L 7 3 4F RT A22WE 2008042400012 20080424 00012 EU 2008 4 24 08FDEA01459 1 20080420 A 5330 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 445FE 297 LT MLG WHEEL WELL BETWEEN FRAME 48 AND 49 INTERIOR OF SKIN AT STRINGER 38 HAS CORROSION APPROX 1 SQ IN. REMOVED LEVEL 1 CORROSION AND INSTALLED REPAIR DOUBLER BETWEEN FRAMES 49 AND 50 AND STRINGERS 37 AND 38 LT IAW FEDEX EA 6-5310-118099, RELEASE DATE 17 MARCH, 2008. 2 L 7 2 4F RT A35EU 2008042400016 20080424 00016 NM 2008 4 24 UPS08452007 1 20080410 A 2170 COALESCER BAG BOEING 747 747212B 1384886 NM NR 3 A/C PACK ODOR A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 522UP 21936 CLIMBING THROUGH FL 220 A VIBRATION WAS FELT ACCOMPANIED BY A BURNING ODOR. SECURED NR 3 PACK AND VIBRATION AND ODOR WEN T AWAY. ON NR 3 PACK REPLACED COALESCER BAG AND RETAINING RING MM 21-51-05 LP 935157/1. REPLACED COMP DISCH TEMP BULB MM 21-51-02 LP 935158/1. ACCOMPLISHED AIR CYCLE PACK SYSTEM TEST PER MM 21-51-00. COULD NOT DUPLICATE VIBE/SMELL. RAN PACK 55 MINUTES. 2 L 7 4 4F RT A20WE 2008042400020 20080424 00020 NM 2008 4 24 2008UALA02160 1 20080413 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 774UA 26936 EMERGENCY LIGHTS ON SEATS 31 TO 43 BOTH SIDES ARE NOT WORKING. FOUND SHORTED LIGHT ASSEMBLY SEAT 33A. REPLACED LIGHT A SSY,POWER SUPPLY ASSEMBLY OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042400023 20080424 00023 NM 2008 4 24 2008UALA02163 1 20080414 A 2701 BOLT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CONTROL COLUMN OUT OF RIG A UALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 WP 29 517UA 24861 CAPTAIN'S ELEVATOR CONTROLS FEEL HEAVY. CREW COMMENTS: EXCESSIVE BACK PRESS REQUIRED ON TO. 3.3 SET OVER 6 UNITS REQUIR ED TO TRIM OUT PRESSURE. OK IN FLT. FOUND CAPTAINS AFT QUADRANT STOP BOLT OUT OF RIG. REMOVED ONE WASHER AT STOP BOLT . RECHECKED AFTER RIG AND FOUND NEUTRAL COLUMN TO FWD POSITION AT 9 DEG. AND AFT AT 13 DEG. RIGGED AND OK. TWO TEST FLIG HTS WERE SATISFACTORY PER EG. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400028 20080424 00028 NM 2008 4 24 2008UALA02168 1 20080414 A 3510 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CAPTAIN'S FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 574UA 26686 CAPTAIN'S OXYGEN RESET SWITCH STICKY. REPLACED CAPTS WITH OBSERVERS O2 MASK ASSY CHECKS OK 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400029 20080424 00029 NM 2008 4 24 2008UALA02169 1 20080413 A 4900 263BA1011 BATTERY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU DISCHARGED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 215UA 30221 10 MINUTES PRIOR TO DEPARTURE CREW CALL EICAS MSG 'APU BATTERY. FOUND FAULTY BATTERY. REPLACED APU BATTERY. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 2008042400045 20080424 00045 EU 2008 4 24 2008UALA02182 1 20080414 A 3150 WARNING LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 401UA 435 L AILERON FAULT DISPLAYED ON UPPER ECAM SCREEN. 2 L 7 2 4F 4 F RT A28NM E40NE 2008042400050 20080424 00050 NM 2008 4 24 2008UALA02190 1 20080416 A 3350 SOCKET BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 121UA 29167 EEL LIGHT CABLE SOCKET CUT AT SEAT 37C. FOUND LIGHT ASSEMBLY DAMAGED. REPAIRED CABLE SOCKET CONTACT OP CHECKS GOOD PE R MM 33-51-12 PB 200 CONFIGURE 2 PARA 2. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 2008042400072 20080424 00072 NM 2008 4 24 2008UALA02264 1 20080418 A 3397 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 514UA 24839 A ZONE EEL INOP. FOUND POWER FEEDER WAS LOOSE. RECONNECTED POWER FEEDER AND OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 2008042400073 20080424 00073 NM 2008 4 24 2008UALA02265 1 20080418 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 514UA 24839 EXTERIOR EMERGENCY LIGHTS HAS 2 INOP LIGHTS, ONE AT THE DPP R R2 AND ONE AT THE LEFT WING. FOUND BULBS OUT/INOP. RELAMP ED BULBS, ALL OPS CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080919 NM 2008 9 19 SWAA084841 1 20080903 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 350 S25R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER 25R CORRODED AT BS 350. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084849 1 20080903 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0843434 1 20080819 A 5755 654645170A SKIN BOEING 737 737490 1384715 NM NR 1 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 DENT IN UPPER INBOARD SURFACE OF NR 1 SPOILER. PREPPED AREA, FABRICATED DOUBLER BONDED REPAIR IAW B737 400 SRM 51-70-10 . 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0843435 1 20080819 A 5755 654645170A SKIN BOEING 737 737490 1384715 NM NR 1 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 DENT IN UPPER OUTBOARD SURFACE OF NR 1 SPOILER. PREPPED AREA, FABRICATED DOUBLER AND BONDED REPAIR IAW B737 400 SRM 51- 70-10. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0843436 1 20080825 A 5755 654645170A SKIN BOEING 737 737490 1384715 NM NR 3 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 DENT IN LOWER SURFACE OF NR 3 SPOILER. PREPPED AREA, FABBED DOUBLER AND BONDED IAW B737 400 SRM 51-70-10. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0843437 1 20080902 A 5754 654645170A SKIN BOEING 737 737490 1384715 NM NR 6 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 NR 6 SPOILER IS DENTED ON UPPER SURFACE FROM SEAL SCREWS ON LOWER SURFACE. REPAIRED NR 6 SPOILER IAW B737 400 SRM 51-70 -10 REPAIR 4 PG 201. 2 L 7 2 4F RT A16WE 20080919 2008 9 19 ASAA0853432 4 20080819 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM FLT MANAGE MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 579AS 5821 35187 THE "INFO ONLY" "FMC DISAGREE" QRH RESET PERFORMED INFO NOTED PERFORMED FMC BITE TEST REF FIM 34 61 TASK 801 WITH NO FAI LED MESSAGES. AIRCRAFT OKAY FOR ETOPS FLIGHT. 2 L 7 2 4F RT A16WE 20080919 EA 2008 9 19 A6WA200840579 1 20080813 A 2751 855D10011 SENSOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 31 429AW 12322 7711 FLAP FAIL CAUTION MESSAGE. FLAPS AT ZERO. DIVERTED TO BWI. FOUND LT BPSU CODES CONTINUITY CHECK AND MEGGED LT WING WI RING PER WM AND FIM CHAP 27. NO FAULTS FOUND. CURRENT BPSU INSTALLED HAS REPEAT HISTORY OF FAULTS IN OTHER ACFT. SUSP ECT BAD PART. REPLACED BPSU PER AMM CHAP 27. FLAP OPS CHECK GOOD. S/N OFF 2243, S/N ON 1995 2 L 7 2 4F RT A21EA 20080919 WP 2008 9 19 UPS08853263 1 20080813 A 5320 WEB DOUG DC8 DC871F 302199D WP BS -80, L21L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 STA -80 WEB EXFOLIATED ON FORE AND AFT SIDES IN COCKPIT SUBFLOOR, AT FUSE SKIN, LT SIDE BELOW SIDE BE LOW SIDE CONSOLE. REMOVED AND REPLACED -80 WEB IAW SRM 51-1-20D, 51-3-0, 51-1-24. 2 L 7 4 4F RT 4A25 20080919 NM 2008 9 19 UPS08M53249 1 20080824 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM BHORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 28 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080919 NM 2008 9 19 UPS08M53251 1 20080826 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 33 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080919 NM 2008 9 19 UPS08M53252 1 20080824 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 13 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080919 NM 2008 9 19 UPS08M53253 1 20080825 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 36 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080919 NM 2008 9 19 UPS08M53254 1 20080825 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 34 LEFT BARREL NUT BOREHOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAI R BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080919 NM 2008 9 19 UPS08M53259 1 20080828 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 36 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080919 NM 2008 9 19 UPS08M53260 1 20080827 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 33 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080919 NM 2008 9 19 CALA0800840 1 20080829 A 5320 6553A4424 FLOOR SUPPORT BOEING 737 737524 1384721 NM BS 807 S26R CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14628 27532 CORROSION ON FLOOR TRACK AT STATION 807 STRINGER 26R. INSTALLED REPAIR SPLICES AND NEW SECTION OF TIE DOWN RAIL REF SRM 53-00-03 / 53-60-53. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 CALA0800842 1 20080830 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM BS 360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 BODY STATION 360 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REPAIRED FRAME AT BODY S TATION 360 BETWEEN S8L AND 9L AND REPLACED INTERCOSTAL CLIP AT BS 360 AND S8L PER EA5310-04498 AND EC/RA 5310-04830. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 CALA0800843 1 20080831 A 3397 WIRE BOEING 737 7373T0 1384582 NM EMERGENCY LIGHT PINCHED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14325 23455 EMERGENCY PATH LIGHTING AT ROW 24 FOUND WIRE PINCHED BETWEEN SEAT TRACK COVER AND TRACK. REMOVED AND REPLACED SEAT HARN ESS EMERGENCY SEAT LIGHTS ROW 24. ALL LIGHTS OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 USAA920081593 1 20080828 A 3397 WIRE BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - CORROSION EEL - EMERGENCY LIGHT AT SEAT 10 LT IS INOP. REPAIRED BROKEN WIRE AT SEAT 10 LT EMERGENCY LIGHT IAW B73 7 BSWPM 20-15-02-5 & B737 AMM 33-51-02-5. 2 L 7 2 4F RT A16WE 20080919 EA 2008 9 19 COMA086379 1 20080901 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 966CA 7132 DURING HMV6 INSPECTION, FOUND FRAME DOUBLER CRACKED AT FS 718, BETWEEN STRINGERS 10 LT AND 11 LT. CUT OUT DAMAGED SECTI ON OF FRAME/DOUBLER AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-193. 2 L 7 2 4F RT A21EA 20080919 NM 2008 9 19 CALA0800845 1 20080831 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM BS 747 S26L/R CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14628 27532 CORROSION ON FRAME AT STATION 747 STRINGER 26R TO 26L. BURNISHED CORROSION FROM S-26R TO S-26L, FROM 27R TO 26R FOUND T O BE OUT OF LIMITS AND REPAIRED PER SRM 53-00-07 REPAIR 3. ALL OTHER AREAS FOUND TO BE WITHIN ALLOWABLE LIMITS, TREATED AND PRIMED REF SRM 53-60-07. 2 L 7 2 4F RT A16WE 20080919 EA 2008 9 19 A6WA200840581 1 20080820 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA STUCK A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 433AW 7289 CREW REPORTS PASSENGER DOOR UNABLE TO OPEN FROM OUTSIDE. INSPECTED PASSENGER DOOR LATCH MECHANISM, INNER AND OUTER HAND LES PER AMM 52-11-02, 52-11-03. REMOVED PUSH-PULL RODS AND CLEANED AND LUBED ROD ENDS. REMOVED, CLEANED AND LUBED INNE R AND OUTER HANDLES REF 12-20-52. NO DEFECTS FOUND, DOOR OPERATES SMOOTHLY. PASSENGER DOOR OPS CHECK GOOD. REF 52-11- 23. 2 L 7 2 4F RT A21EA 20080919 NM 2008 9 19 USAA920081589 1 20080819 A 5315 65498852 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - CORROSION MAJOR REPAIR - CORROSION ON FLOORBEAM AT FASTENER HOLES AT BS 986, RBL 15, BL 0, LBL 16. REPLACED FLOOR BEAM AT BS 986, LBL 60 TO RBL 60 IAW US AIRWAYS EA NR 130099. 2 L 7 2 4F RT A16WE 20080919 EA 2008 9 19 COMA086378 1 20080901 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 966CA 7132 DURING HMV6 INSPECTION, FOUND FRAME DOUBLER CRACKED AT FS 718, BETWEEN STRINGERS 10 RT AND 11 RT. CUT OUT DAMAGED SECTI ON OF FRAME/DOUBLER AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-193. 2 L 7 2 4F RT A21EA 20080922 NM 2008 9 22 SWAA084866 1 20080903 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 747 S26R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CORRODEED AT BS 747, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084867 1 20080903 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM BS 505D S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 505D, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084868 1 20080903 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM BS 506D S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 16L CRACKED AT BS 506D. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080717 WP 2008 7 17 08FDEA02025 1 20080529 A 5321 AGA74287 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 AFT PIT FLOOR PANEL 187 BF REQUIRES FAB NEW. FABRICATED NEW FLOOR PANEL 187 BF; POTTED EDGES; COMPLETED CURE AND SANDE D EDGE POTTING; INSTALLED INSERTS; FABRICATED TOP SHEET; LAYED-UP TOP SHEET UNDER A VAC BAG; COMPLETED CURE; BACK DRIL LED AND COUNTERSUNK HOLES; APPLIED NON-SKID AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005, REV F AND 25-011, REV C. 2 L 7 3 4F RT A22WE 20080717 EA 2008 7 17 SWIA200819812 1 20080625 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR WORN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 498CA 7792 FLT 2555 - MAIN CABIN DOOR WOULD NOT OPEN. REPLACED MAIN CABIN DOOR OUTER HANDLE IAW AMM 52-11-03. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080717 EU 2008 7 17 08FDEA02227 1 20080611 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 MAIN DECK FLOOR; FRAME 64; RIGHT 46 INCH FROM CENTERLINE; THE FLOORBEAM IS CRACKED. 2 L 7 2 4F RT A35EU 20080717 EU 2008 7 17 08FDEA02222 1 20080611 A 5420 SHIM AIRBUS 300 A300F4605R 3930327 EU NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 NR 1 PYLON RIB 3-A STA 615 INBD SIDE SHIM HAS A .75 INCH CRACK. 2 L 7 2 4F RT A35EU 20080717 NM 2008 7 17 ASAA0843062 1 20080606 A 5330 65C357984 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 SIX DENTS AFT OF R2 DOOR JUST ABOVE LAP. REMOVED DENTED SKIN PANEL, FABRICATED AND INSTALLED REPLACEMENT SKIN PANEL IAW B737 400 SRM 51 40 02 51 30 01. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 08FDEA02100 1 20080602 A 5100 NONE DOUG MD11 MD11F 3023600 NM NO DAMAGE NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 EXISTING DOUBLER REPAIR AT CENTER CARGO DOOR AFT CUT-OUT APPROX STRINGER 38 TO 42. EXISTING DOUBLER REPAIR AT CENTER CA RGO DOOR AFT CUT-OUT APPROX STRINGER 38 TO 42 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-50-00 FIGURE 17 VOLUME I FEDEX EO NR 1-5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG - MD11 - REPAIR CATALOG AND TRACKING REQUIREMENTS, H AS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 08FDEA02005 1 20080528 A 5320 AGA70945 STANCHION DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 FORWARD CARGO COMPARTMENT: AFTER REMOVAL OF STA 6-73 AFT BULKHEAD PANEL FOR WIRING INSPECTION ACCESS FOUND X = 57 STANCH ION WITH CORROSION. CORRODED STANCHION AT STA 6-73, X = 57 AFT BULKHEAD PANEL REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. STANCHION FABRICATED AS PER DOUGLAS DRAWING AGA7094. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080717 WP 2008 7 17 08FDEA02211 1 20080610 A 5415 MOUNT DOUG MD10 MD1010F 3022112 WP NR 1 PYLON LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 NR 1 PYLON LOWER AFT END (AT THE PYLON MOUNT) BRACKET IS LOOSE AND CRACKED AT THE BOTTOM, (FASTENERS ARE WORKING). 2 L 7 3 4F RT A22WE 20080717 2008 7 17 SWAA083261 4 20080614 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080717 2008 7 17 SWAA083290 4 20080615 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083313 1 20080617 A 3350 311500 LENS BOEING 737 7375H4 138449D NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 BULLNOSE EMERGENCY EXIT LIGHT LENS FELL OFF AT ROW 21 DEF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083263 1 20080613 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT AFT UPPER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080924 NM 2008 9 24 08FDEA03780 1 20080909 A 5320 RETAINER BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 906FD 27148 CORROSION ON NUT PLATE RETAINER OF APU INTAKE DOOR CUT-OUT BESIDES STA 1787.45 UPPER RT BULKHEAD. REMOVED AND REPLACED FWD SKIN STRAP, AFT SKIN DOUBLER, BOTTOM ANGLE SUPPORT IAW SRM 51-40-02 AND BLUEPRINT 148N3138. THIS IS CLASIFIED MAJOR REPAIR NO FOLLOW-UP TRACKING REQUIRED . 2 L 7 2 4F RT A2NM 20080924 EU 2008 9 24 08FDEA03781 1 20080909 A 5321 A5328524100000 FLOOR PANEL AIRBUS 310 A310222 3930315 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 MAIN CABIN FLOOR PANEL CF AT FRAME C 11 A, LOWER SURFACE IS CRACKED. REPAIRED AS REQUIRED IAW ARM 53-10-20; FIG 202. 2 L 7 2 4F RT A35EU 20080922 NM 2008 9 22 ASAA0843378 1 20080719 A 5315 65C339483 FLOORBEAM BOEING 737 7374Q8 138447Q NM BS 947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 FUSELAGE STA 947.5 CENTER OF FRAME HAS CORROSION ON UPPER CAP. REPAIRED FLOORBEAM IAW ASA EA 5310-02812, REMOVED AND RE PLACED T-CAP WITH SPLICE ANGLES AND STRAPS. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843383 1 20080721 A 5322 65465348 SHEAR TIE BOEING 737 7374Q8 138447Q NM BS 520 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 FWD CARGO PIT SHEAR TIE CORRODED STA 520 RBL 110. REMOVED DAMAGED SHEAR TIE, LOCATED DRILLED AND INSTALLED A REPLACEMEN T SHEAR TIE IAW SRM 51-40-02 PAGE 4. 2 L 7 2 4F RT A16WE 20080923 NM 2008 9 23 DL757081180 1 20080909 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1550 S25-26L DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 FOUND SKIN DAMAGE AT STA 1550 STRINGER 25L TO 26L. REPAIRED PER SRM 53-00-01. 2 L 7 2 4F RT A2NM 20080923 NM 2008 9 23 2008UALA05441 1 20080823 A 2612 MOTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BLOWER FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 IN AFT CARGO PIT, FIRE DETECTION BLOWER M1 0464 NEEDS TO BE REPLACED. (WHITE LIQUID OOZING FROM MOTOR HOUSING) INSTALLE D NEW FIRE DETECTION MOTOR M10464. 2 L 7 2 4F 4 F RT A2NM E17NE 20080924 EU 2008 9 24 08FDEA03347 1 20080808 A 5321 R532B371500000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 242 AJ IS DAMAGED. REPAIRED CABIN FLOOR PANEL 242 AJ BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARK ED AND APPLIED NON-SKID TAPE IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03755 1 20080908 A 5315 A5397455400 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 CORROSION FOUND IN AFT CARGO COMPARTMENT AT CROSSBEAM C 60. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03756 1 20080908 A 5322 A53810743200 SHEAR TIE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND ELONGATED HOLES AT FRAME FOOT C 43 RT. REPAIR PERFORMED BY OVERSIZING THE HOLE AND INSTALLING FASTENER EN6115V4 W ITH COLLAR NAS172604 IAW RAS /70513306/009/2008 ISS A, APPROVED BY EA 6-5315-123136. 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03757 1 20080907 A 3260 WARNING LIGHT DOUG MD11 MD11F 3023600 NM MLG FALSE ACTIVATION A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 598FE 48597 AFTER T/O R MAIN GEAR SHOWED UNSAFE RAN LIST RECYCLED GEAR NO HELP, INCREASE SPEED AFTER FLAP RETRACT AND AT 225 LIGHT W ENT OUT. 2 L 7 3 4F RT A22WE 20080925 EU 2008 9 25 08FDEA03884 1 20080915 A 3231 SEQUENCE VALVE AIRBUS 300 A300F4605R 3930327 EU NGL DOOR MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 678FE 792 ON DEPARTURE AND GEAR RETRACTION THE NOSE GEAR DOOR SHOWED IT DID NOT CLOSE. RAN ECAM AND QRH AND LIGHT STAYED. DUPLIC ATED PROBLEM ON GROUND WITH LEFT NOSE DOOR NOT FULLY CLOSING. ADJUSTED LT GEAR DOOR UPLOCK ASSY PER AMM 32-22-11-5. PE RFORMED NOSE GEAR EXTENSION AND RETRACTION TEST SEVERAL TIMES PER AMM 32-31-00-5. 2 L 7 2 4F RT A35EU 20080925 WP 2008 9 25 08FDEA03885 1 20080915 A 2910 LINE DOUG DC10 DC1030F 3023504 WP HYD SYSTEM LEAKING A FDEA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CE 21 314FE 19854 19854 AP004 48312 CENTER GEAR FAILED TO EXTEND WITH GEAR HANDLE. RAN CHECK LIST, CENTER GEAR EXTENDED WHEN THE CENTER GEAR ALTERNATE EXTE NSION HANDLE WAS PULLED. ON LANDING ROLLOUT HYD QUE ILLUMINATED, HYD SYS 3 ELEV ILLUMINATED. FOUND HYD LINE TO CENTER GEAR UNLOCK CYLINDER LEAKING, AND UPPER LOCK LINK LUGS FOR UNLOCK CYLINDER ROD DAMAGED. REPLACED LEAKING UNLOCK CYLIND ER HYD LINE, UPPER LOCK LINK, AND UNLOCK CYLINDER AND TESTED CENTER GEAR PER M/M 32-38-02-2, 32-16-01-4, AND 32-10-01-5. CENTER GEAR OPERATION TESTED NORMAL. NR 3 HYD RESERVOIR SERVICED TO 7.5 GAL. CENTER GEAR STRUT SERVICED PER STRUT S ERVICE PLACARD. 2 L 7 3 4F RT A22WE 20080925 EU 2008 9 25 08FDEA03887 1 20080916 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND OLD REPAIR AFT OF REAR SPAR AT RIB 9 (RAS/BAE/0081/2002 ISS C, UNREPAIRED CRACK WITH CRACK STOP HOLE IN BOTTOM SKI N). REPAIR PERFORMED BY NDT FOR CRACK FREE CONDITION (NO CRACK FOUND AFTER REMOVAL OF REPAIR PLATES) FOR EVERY HOLE AFF ECTED BY THE REPAIR PLATE AND REINSTALLING REPAIR PLATE IAW DRAWING R573-40199 WITH DEVIATION OF OVERSIZING EACH HOLE TO SECOND OVERSIZE, APPROVED BY RAS/BAE/1007820/2008 ISS A AND EA 6-5720-123096. 2 L 7 2 4F RT A35EU 20080925 EA 2008 9 25 QXEA200800436 1 20080421 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 612QX 10042 PDX C4 CHECK - 280 BEAM HAS 2 CRACKS AT APPROX LBL 9 AND RBL 9. REMOVED 280 BEAM IAW CRJ 700 SRM 51-40-11. HFEC AT CUT OUT AREA IAW NDTM PT 1, 51-20-006 NO CRACKS NOTED. INSTALLED 280 BEAM IAW CRJ 700 SRM 51-42-06 AND 51-42-21. 2 L 7 2 4F RT A21EA 20080925 EU 2008 9 25 08FDEA03849 1 20080911 A 3230 LANDING GEAR AIRBUS 310 A310203 3930313 EU NR 1 MALFUNCTIONED A FDEA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 CE 21 423FE 281 DURING GEAR EXTENSION ON SYSTEM NR 1 GEAR DID NOT EXTEND (THREE RED INDICATIONS) WENT AROUND CYCLED GEAR HANDLE UP AND T HEN BACK DOWN AND GEAR EXTENDED NORMALLY (ALL ON SYSTEM NR 1). 2 L 7 2 4F RT A35EU 20080925 NM 2008 9 25 08FDEA03850 1 20080912 A 3010 ARM007812 DOOR DOUG MD11 MD11F 3023600 NM TELESCOPIC DUCT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 623FE 48794 RIGHT WING, NR 3 LEADING EDGE SLAT TELESCOPIC DUCT LOWER DOOR FWD SECTION FOUND CHAFED. REMOVED AND REPLACED WITH A FAB RICATED DOOR AS PER AMM 27-80-30-4. DOOR FABRICATED AS PER EA 1-5740-122550, THIS REPAIR CLASSIFIED AS MINOR PER GMM 6- 2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03851 1 20080912 A 5340 AEA7053502 ATTACH BRACKET DOUG MD11 MD11F 3023600 NM BS 1259 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 623FE 48794 MAIN DECK CABIN, 1 OFF FRAME ATTACHMENT BRACKET AT APPROX FRAME STA 1259 LONGERON 15 FOUND CRACKED. NEW FRAME ATTACHM ENT BRACKET FABRICATED AS PER EA 1-5740-122552, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03852 1 20080912 A 5720 65162161 SUPPORT BEAM BOEING 727 727227 1384078 NM SPOILER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 LWR SIDE OF I/B SPOILER FITTING HAS MISSING AND LOOSE FASTENERS EVALUATED AND FOUND CRACK ON SPOILER SUPPORT BEAM. REPA IRED I/B SPOILER SUPPORT BEAM CRACK AT SPOILER FITTING AREA IAW FEDEX DRAWING NR: SR27-57-038 REV "C". 2 L 7 3 4F A3WE 20080925 NM 2008 9 25 08FDEA03930 1 20080917 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 DURING OPEN HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D. MAIN DECK CARGO DOOR LOWER JAMB NR 7 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR ON FITTING CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. R EPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 EU 2008 9 25 08FDEA03869 1 20080915 A 5753 A579600050000 SKIN AIRBUS 300 A300F4605R 3930327 EU LT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 LEFT WING INBD FLAP TOP SKIN IS CHAFED AT APPROX 13 INCHES AFT OF THE FRONT SPAR AND 79 INCHES FROM THE INBD EDGE. BLEN DED CHAFED AREA REF SRM SRM 51-73-10. ORIGINAL MATERIAL THICKNESS 0.031 REF SRM 57-52-12. REMOVED MATERIAL 0.003. MAT ERIAL REMAINING 0.028, FOUND TO BE BEYOND LIMITS REF SRM 57-50-00. CUT OUT DAMAGED SKIN REF SRM 57-50-00; FIG 205. FAB RICATED A REPAIR DOUBLER REF SRM 57-50-00; FIG 205. ALODINED REPAIR DOUBLER REF SRM 51-21-10. PRIMED REPAIR DOUBLER RE F SRM 51-23-10. INSTALLED REPAIR DOUBLER REF SRM 57-50-00; FIG 205. PAINTED REPAIR DOUBLER REF SRM 51-23-10. 2 L 7 2 4F RT A35EU 20080922 NM 2008 9 22 SWAA084877 1 20080904 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 637 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 637, RBL 70. REMOVED AND REPLACED WEB PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084882 1 20080904 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 451WN 32495 R2 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084870 1 20080904 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 360 S14L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND STRINGER 14L CRACKED AT BS 360. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084871 1 20080904 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 260 S12L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 260, STR 12L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080922 EA 2008 9 22 COMA086373 1 20080829 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 310 S16-17L DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 420CA 7451 PAX DOOR CUTOUT AIRFRAME SIDE FWD LOWER CORNER SKIN DAMAGED. PERFORMED REPAIR AT STA 310 STR 16 AND 17 IAW CRJ REO 601R -53-21-180 REV A. 2 L 7 2 4F RT A21EA 20080922 EA 2008 9 22 HNAA0800257 1 20080612 A 5347 SEAT TRACK DHAV DHC8 DHC8311 1386006 EA BS 593-626 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 335EN 32270 375 CORROSION LIGHT SURFACE. SPOTS FOUND ON I/B SEAT RAILS BETWEEN FS 593 AND 626. HFEC DONE - NO CRACKS. SEAT RAIL REPAI RED BY SPLICE RD8-53-3886 AND FSR 07-3003. 2 H 7 2 4T RT A13NM 20080922 EA 2008 9 22 HNAA0800279 1 20080907 A 3350 L235A01711 LAMP DHAV DHC8 DHC8311 1386006 EA EMERGENCY LIGHT BURNED OUT A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 329EN 34317 290 THE EMERGENCY SWITCH LIGHT ON THE FLIGHT ATTENDANTS AUDIO CONTROL PANEL WAS FOUND TO BE BURNT OUT. LINE MX CHANGED THE LAMP AND OPS CHECKS WERE GOOD. ACFT CONTINUED IN SERVICE. 2 H 7 2 4T RT A13NM 20080922 2008 9 22 SWAA084895 4 20080906 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084907 1 20080907 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 500 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084908 1 20080907 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 380 S21L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 21L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084909 1 20080905 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM BS 779 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 779, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084910 1 20080907 A 5311 6546543 FRAME BOEING 737 7373T0 1384582 NM BS 706 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084911 1 20080907 A 5311 6546552 FRAME BOEING 737 7373T0 1384582 NM BS 827 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084840 1 20080903 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 887 S25R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 887, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 ASAA0842989 1 20080518 A 5755 SKIN BOEING 737 737490 1384715 NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 NR 7 SPOILER UPPER SURFACE HAS PROTRUDING DENTS. PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM REPAIR 4. 2 L 7 2 4F RT A16WE 20080715 NE 2008 7 15 ASAA0853016 2 20080530 A 7261 OIL SYSTEM BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE LOW A ASAA O OTHER O OTHER DE DESCENT 1 NM 02 570AS 5126 35185 894536 NR ONE ENGINE OIL AT 13 QTS TOP OF DESCENT. NR TWO ENGINE OIL AT 14 QTS TOP OF DESCENT VERIFIED NR 1 AND NR 2 ENG OIL S ERVICED TO 16 AND 17 QTSRESPECTIVELY. TOPPED OFF BOTH ENG OILS TO FULL. NR 1 ENG OIL ADDED 2.5 QTS, NR 2 ENG OIL ADDE D 2.5 QTS, APU OIL ADDED 0 QTS. 2 L 7 2 4F 4 F RT A16WE E2GL 20080715 NM 2008 7 15 SWAA082905 1 20080529 A 5311 65C25230 FRAME BOEING 737 7373H4 1384600 NM BS 727E S27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727E, STR 27R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 UPS08B52391 1 20080417 A 5340 TENSION TIE BOEING 747 747400 13848AT NM BS 1140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 BS 1140 TENSION TIE RT AFT SIDE FOUND CRACK, BS 1140 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201. 2 L 7 4 4F RT A20WE 20080715 EU 2008 7 15 08FDEA02043 1 20080530 A 5311 A53771283201 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CHAFING MARKS ON FRAME C 22 RT, P 14-15 OUT OF LIMIT. FRAME REPAIR PERFORMED IAW SRM 53-10-13 FIG 202. 2 L 7 2 4F RT A35EU 20080715 NM 2008 7 15 ASAA0842980 1 20080526 A 5210 507945154 DOOR BOEING 737 7374Q8 138447Q NM FORWARD ENTRY STUCK A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 765AS 25102 FLIGHT ATTENDANT REPORTS L1 DOOR HARD TO CLOSE. OPENS EASILY NO SQUEALING DURING FLIGHT. LIGHT INDICATION NORMAL. INS PECTED L1 DOOR FOR PROPER OPERATION. FOUND OK REF 52 11 00, LUBED DOOR HINGES. 2 L 7 2 4F RT A16WE 20080715 EU 2008 7 15 AALA200801279 1 20080512 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 41063 506 MIA - EMERGENCY LIGHTS AT RIGHT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20080715 2008 7 15 C2XA08ON129 4 20080529 A 3160 7014300901 DISPLAY EMB 145 EMB145XR 3260214 SO COCKPIT BURNED OUT A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 11176 9738 9738 14500881 FLT 7693 - ONT - FLIGHT CREW REPORTED EICAS SCREEN FAILED, EICAS DISPLAY CIRCUIT BREAKER POPPED AND LOTS OF SMOKE EMITTE D FROM ABOVE EICAS UNIT, SWAPPED MFD W/EICAS PLACED FO'S MFD. MX REMOVED AND REPLACED EICAS DISPLAY UNIT OPERATIONALLY CHECK SATISFACTORY. AIRCRAFT WAS RELEASE TO RETURN FOR SERVICE. 2 L 7 2 4F RT 20080715 NM 2008 7 15 AALA200801278 1 20080512 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 972AN 30097 LGA - EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20080715 2008 7 15 SWAA083862 4 20080711 A 2565 63550 SLIDE BOEING 737 7377AD 1384502 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 798SW 28436 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083861 1 20080711 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 788SA 30603 DURING SCHEDULED HC1 CHECK, FWD CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. R&R BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20080715 2008 7 15 SWAA083864 4 20080711 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083818 1 20080713 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083821 1 20080713 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083819 1 20080713 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083844 1 20080710 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. R&R BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083845 1 20080710 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083839 1 20080706 A 5315 BAC15201397 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 423WN 29827 DURING SCHEDULED 6Y CHECK, FOUND FLOORBEAM CORRODED AT BS 727D, RBL 7. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20080925 EU 2008 9 25 08FDEA03870 1 20080915 A 5320 A53771417206 SILL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSION AT FWD CARGO DOOR SILL BEAM, C 20-25 REPAIR PERFORMED BY CORROSION REWORK, NDT FOR CORROSION FREE CONDIT ION, UPPER FLANGE REPAIR BETWEEN C 24-26 PER DRAWING R537-06913 AND INSTALLING OF BUSHES IAW SRM 53-13-18 FIG 202, APPRO VED BY RAS/EFW/9000102/2008 ISS A AND EA 6-5313-123140. 2 L 7 2 4F RT A35EU 20080925 SO 2008 9 25 SWIA200820064 1 20080808 A 5411 FRAME EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 299SW 120329 C-CHECK, RIGHT INBOARD NACELLE FRAME CRACKED. REPLACED FRAME. 2 L 7 2 4T RT A31SO 20080925 SO 2008 9 25 SWIA200820065 1 20080808 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 299SW 120329 C-CHECK, CRACK IN FRAME IN FRONT OF RIGHT HEAT EXCHANGER. INSTALLED DOUBLER REPAIR ON FRAME. 2 L 7 2 4T RT A31SO 20080925 SO 2008 9 25 SWIA200820067 1 20080805 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT LOOSE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 299SW 120329 FLT 3563 - EMERGENCY EXIT LIGHT AT 6 A INOP. CONNECTED LOOSE WIRE. 2 L 7 2 4T RT A31SO 20080925 EU 2008 9 25 08FDEA03871 1 20080915 A 5321 A5322060000200 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 650FE 726 UPPER CARGO FLOORBOARD IS BULGED AT THE TRACK FITTING (251 QH) REMOVED DAMAGED FLOOR PANEL 251 QH IAW SRM 51-40-21. MAT ERIAL ID FOR THE NEW PANEL A402H144 IAW DWG SRZ 25-005; REV "G". FABBED A NEW FLOOR PANEL 251 QH IAW DWG 25-005; REV "G ". INSTALLED PANEL IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080925 WP 2008 9 25 08FDEA03912 1 20080917 A 5347 607155 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 1638-1631 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 571FE 47830 UPPER CARGO COMPARTMENT SEAT TRACK 75L, FS 1638L TO 1631L, HAS 3 WORN LOBES BLEND AREA IAW 53-70-00 FIG 5, SHEET 1 OF 2 ORIGINAL .145 AFTER REWORK .118 OUT OF LIMITS. REMOVED AND REPLACED FLOOR PANELS IAW AMM 53-21-08-2 STA 1561-1661 LBL 48-75 AND 1561-1661 LBL 75-108. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1. FABRICATED SEAT TRACK, SPLICE HAT AND PLATE ON TR NR T8/ 758025 AND T8/758026. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03913 1 20080917 A 5347 6045007075 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 571FE 47830 UPPER CARGO COMPARTMENT SEAT TRACK 1072, FS 1053 LOBE 1/2 MISSING. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 1(SHEET 1). FABRICATED NEW SEAT TRACK UNDER MAE TRAVELER NR T8/758248. BLENDED AREA (LOBE) IAW SRM 53-70-00. O RIGINAL .420, AFTER REWORK .230, OUT OF LIMITS. REMOVED AND REPLACED SIDEWALL GRILLS AND SIDEWALL GRILL ANGLES IAW SRM 51-31-01. 2 L 7 3 4F RT A22WE 20080925 EU 2008 9 25 08FDEA03873 1 20080915 A 5411 2240083501 LONGERON AIRBUS 300 A300B4622R 3930312 EU NR 1 PYLON WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND ELONGATED HOLE ON AFT FAIRING ADAPTER LONGERON, PYLON NR 1. REPAIR PERFORMED BY WELDING THE LONGERON OVERSIZE FAS TENER HOLE AND REDRILL THE FASTENER HOLE SAME AS ORIGINAL IAW RAS/ROHR/0776/2008 ISS A, APPROVED BY EA 6-5455-123139. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03876 1 20080915 A 5330 A5377608020200 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 EXTERIOR FUSELAGE UPPER SKIN HAS STATIC DISCHARGE BETWEEN FRAME 69 AND FRAME 70; STR 2 L AND 3 L REMOVED DAMAGE BY WAY O F DRILLING A 5/32 HOLE IAW A310-200 SRM 53-10-12, FIG 220. ACCOMPLISHED A BHEC INSPECTION IAW NTM 51-10-01. INSTALLED A RIVET IAW A310-200 SRM 53-10-12, FIG 220. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03878 1 20080915 A 5330 A5377601720200 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 EXTERIOR FUSELAGE UPPER SKIN HAS STATIC DISCHARGE AT FRAME 66 BETWEEN STRINGER 2 L AND 3 L. REMOVED AND REPLACED FASTEN ER IAW A310-200 SRM 53-10-12; FIG 220. ACCOMPLISHED A BHEC INSPECTION IAW NTM 51-10-01. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03879 1 20080915 A 5330 A5377608020200 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 EXTERIOR FUSELAGE SKIN HAS STATIC DISCHARGE BETWEEN FRAME 69 AND FRAME 70 FROM STRINGER 5L AND 6L REMOVED DAMAGE BY WAY OF DRILLING A 5/32 HOLE IAW A310-200 SRM 53-10-12; FIG 220. ACCOMPLISHED A BHEC INSPECTION IAW NTM 51-10-01. INSTALLED A RIVET IAW A310-200 SRM 53-10-12, FIG 220. 2 L 7 2 4F RT A35EU 20080925 WP 2008 9 25 08FDEA03747 1 20080905 A 7797 WIRE DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL NR 2 ENGINE CHAFED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 399FE 50742 48262 NR 2 ENGINE SHUTDOWN IN FLIGHT. ON CLIMB-OUT PASSING FL 250 HAD A LEVEL 1 NR 2 ENGINE EGT EXCEEDANCE. PER CHECKLIST BR OUGHT POWER BACK. TEMP CAME DOWN WITHIN LIMITS BUT SHORTLY CLIMBED BACK ABOVE REDLINE AND HAD A NR 2 EGT HIGH LEVEL 2. SHUT ENGINE DOWN AND RETURNED TO LAND PER CHECKLIST. FOUND WIRES J011-229-20GR AND J011-229-20WH CHAFED THRU SHIELDING AND INTO CONDUCTORS INSIDE OF J BOX , APPROX 6 INCHES BACK FROM PLUG R5-8216. AFTER EA 8-7720-123490, RETERMINATED NR 2 ENG EGT WIRES PER WDM 77-21-01. CONTINUITY CHECK 'OK'. ENG AT MAX. ASSURANCE POWER PER JRH ALL PARAMETERS GOOD OP S CK GOOD. 2 L 7 3 4F 4 F RT A22WE E23EA 20080925 SO 2008 9 25 LR7A08095 1 20080819 A 5321 FLOORBOARD LKHEED 382 382G 526414U SO FS737E-817E WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HC5314 FOUND CABIN CENTER FLOOR BOARD WARPED AT FS 737E TO 817E, WL146, LBL15 T O RBL15. REPAIRED BY FABRICATING AND INSTALLING FLOORBOARD IAW SMP583 CHAP 51-60 AND 51-70 AND FIG 53-40-05 PG 37 AND S MP581-25-50 FIG 25-50-06. 2 H 7 4 4T A1SO 20080925 SO 2008 9 25 LR7A08096 1 20080819 A 5321 FLOORBOARD LKHEED 382 382G 526414U SO FS 737E-817E WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HC5314 FOUND LT CABIN FLOORBOARD WARPED AT FS 737E TO 817E, WL146, LBL15 TO 50. REPAIRED BY FABRICATING AND INSTALLING FLOORBOARD IAW SMP583 FIG 53-40-05 PG 37, CHAP 51-60 AND 51-70 AND SMP 581-25-5 0 FIG 25-50-06. 2 H 7 4 4T A1SO 20080925 NM 2008 9 25 08FDEA03351 1 20080809 A 5330 651842011 SKIN BOEING 727 727233 138408A NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 275FE 22040 FUSELAGE SKIN BELOW L1 DOOR CUTOUT HAS 2 SMALL DENTS BETWEEN STA 320 - 316 AND BETWEEN STR 19 - 20L. EVALUATED 2 DENTS BELOW L1 DOOR USING MECHANICAL MEANS DENT NR 1 A: 1.9 Y: .031 A/Y: 61.2 AND DENT NR 2 A: 1.2 Y: .007 A/Y: 171.4. A/Y MEASUREMENTS ARE WITHIN LIMITS BUT DENTS ARE LESS THAN 10 INCHES FROM LAP SEAM IAW SRM 53-30-1 FIG 1. HFEC INSPECTED D ENTS AND NO DEFECTS NOTED AND FOUND DENTS ACCEPTABLE "AS IS" IAW EA 7-5330-122389. 2 L 7 3 4F RT A3WE 20080925 NM 2008 9 25 08FDEA03366 1 20080810 A 5347 A5A70821 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 587FE 48489 MAIN DECK CARGO AT APPROXIMATELY STATION 5-73 TO 5-93, X = -27.5 FOUND SEAT TRACK CORROSION. CABIN MAIN DECK CARGO S EAT TRACK REPAIRED FROM STA 5-00 TO STA 5-123, X = -27.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MA JOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080715 NM 2008 7 15 SWAA083826 1 20080709 A 2121 215201 GASPER FAN BOEING 737 7373H4 1384600 NM E&E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 29 385SW 26600 FLIGHT CREW REPORTED ELECTRICAL SMOKE SMELL. R&R GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 20080716 EU 2008 7 16 08FDEA02116 1 20080603 A 5210 A53611658 FAILSAFE AIRBUS 300 A300B4622R 3930312 EU PAX DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON LT FWD PAX DOOR FAIL/SAFE RING IN TWO AREAS (C 14 AND C16 LOWER CORNER). REPAIR PERFORMED BY BLEND O UT THE CORROSION IAW SRM 51-74-10, NDT FOR CRACK FREE CONDITION AND INSTALLING 1ST OVERSIZED FASTENER IAW RAS 70507043/0 09/2008 ISS A, APPROVED BY EA 6-5312-120045. 2 L 7 2 4F RT A35EU 20080716 NM 2008 7 16 ZZDA2008112 1 20080522 A 2560 BATTERY BOEING 717 717200 1383700 NM FLASHLIGHT DISCHARGED A ZZDA K NONE L NO TEST CR CRUISE 1 SO 37 961AT 55023 AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED AFT FLASHLIGHT BATTERY AND SECURITY STRAP, OK FOR SERVICE PER MM 25 -60. 2 L 7 2 4F TR A6WE 20080716 NM 2008 7 16 KCSA081263 1 20080528 A 5412 BULKHEAD BOEING 747 7472B4B 138481B NM NR 1 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 1 PYLON REAR ENG MOUNT BULKHEAD AT NAC STA 221.9 HAS TWO CRACKS AT FWD I/B WEB. 2 L 7 4 4F RT A20WE 20080716 NM 2008 7 16 UPS08B52378 1 20080327 A 5311 FRAME BOEING 747 747400 13848AT NM BS 1120 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:C RT BS 1120 TENSION TIE FRAME WEB CRACKED ABOUT 0.250 INCH. RT BS 1120 TENSION TIE FRAME WEB REPLACED PER SRM 53-40-07, REPAIR 1. 2 L 7 4 4F RT A20WE 20080716 NM 2008 7 16 UPS08M52371 1 20080523 A 5330 DOUBLER DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C DOUBLER IS PEELED BACK AFT OF RADOME ON TOP. REMOVED DOUBLER, CUTOUT CRACK, FABRICATED FILLER AND DO UBLER AND INSTALLED IAW MD-11 SRM 51-31-01, 53-00-01, 53-35-01 NS 51-21-02. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 USAA920081159 1 20080528 A 5330 6545774 SKIN BOEING 737 737401 1384701 NM ZONE 100 CANNING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 23987 CLT - MAJOR REPAIR - C4 CHECK - NR 6094947 AND 03C10053006/003, FUSELAGE SKIN OIL CANNING AT BS 727D AND BS 727E, S21L - S24L. REPAIRED FUSELAGE SKIN OIL CANNING AT BS 727D AND BS 727E, S21L - S24L IAW B737 SRM 53-00-01 REPAIR 31, AND US A IRWAYS TR 53-27 DETAIL VIII. 2 L 7 2 4F RT A16WE 20080716 EU 2008 7 16 08FDEA02045 1 20080530 A 5315 A53974322214 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND ON CROSS BEAM C 63 LT HEAVY CORROSION, CROSS BEAM REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 20080716 WP 2008 7 16 DHL2008807518 1 20080429 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 180 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 FWD CARGO COMPT FLOOR SUPPORT CRACKED 1/2 INCH STA 180.000 L-31L. REMOVED FASTENERS IAW SRM 51-1-20D. PERFORMED STOP H OLE AND FABRICATED ANGLE DOUBLER (STEEL 301 1/2H 0.040") IAW SRM 53-2-0 PG 2E/2F. INSTALLED ANGLE DOUBLER IAW SRM 51-1- 20D, SRM 51-3-1 PG 2A. 2 L 7 4 4F RT 4A25 20080716 WP 2008 7 16 DHL2008807519 1 20080501 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 759 L18L CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 MAIN CARGO COMPT FRAME FITTING CRACKED 2 INCH STA 759.000 L-18L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 P G 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED FITTING IA W SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 20080716 EU 2008 7 16 08FDEA02061 1 20080530 A 5347 A53611040212 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 MAIN DECK CARGO FLOOR SEAT TRACK NR 5 LT HAS CORROSION, BETWEEN FR 16 TO FR 17, 10 SQ INCHES REMOVED LEVEL 1 CORROSION. REMOVED AND REPLACED SEAT TRACK SECTION AT TRACK NR 5 LT BETWEEN FR 16 AND FR 17 IAW A310-200 SRM 53-12-16, FIG 1, PG 4 C. 2 L 7 2 4F RT A35EU 20080716 SW 2008 7 16 WGEA200800058 1 20080528 A 3243 1094 MASTER CYLINDER ECLIPS EA500 ECLIPSEEA500 3350000 SW NR 1 STICKS E WGEA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 27 153DJ 000072 NR 1-COPILOT RIGHT BRAKE PEDAL STICKY. SUPPLEMENTAL INFORMATION - REMOVED AND REPLACED COPILOTS RIGHT BRAKE MASTER CYLI NDER WITH NEW IAW EA500 M/M 32-41-11. BLEED BRAKES IAW EA500 M/M 32-40-00. OP'S CHECK GOOD. 1 L 7 2 4J RT A00002AC 20080716 SO 2008 7 16 C2XA08ON128 1 20080526 A 5210 LOCK EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF ADJUST A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 27 14558 145598 FLT 522 - RDU - FLIGHT CREW REPORTED PAX DOOR HARD TO OPEN. MX FERRY FLIGHT TO TYS. MX ADJUSTED HANDLE LOCKING MECHANI SM OPERATIONALLY CHECK SATISFACTORY AIRCRAFT WAS RELEASE TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 20080716 EU 2008 7 16 NWAA082413354 1 20080528 A 3350 EPSU AIRBUS A330 A330223 3940031 EU EMERGENCY LIGHTS FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 854NW 0620 DOOR 1 EPSU TEST FAULTED THE ESCAPE SLIDE LIGHT SW/EPSU (11WL). REPLACED SLIDE AND TESTED GOOD. 2 L 7 2 4F RT A46NM 20080716 NE 2008 7 16 ASAA0852978 2 20080516 A 7230 COMPRESSOR BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE DIRTY A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 570AS 4970 35185 894523 GE REMOTE DIAGNOSTICS NR 2 ENGINE TREND DATA CONTINUES TOSHOW A GREATER THAN NORMAL EGT MARGIN LOSS. ACCOMPLISH NR 2 ENGINE SINGLE ENGINE COMPRESSOR CLEANING IAW AMM SUPPLEMEMT 72-00-00 P710. ACCOMPLISHED COMPRESSOR WASH ON NR 2 ENG REF MM SUPP 72-00-00 PGS 710-713 STEP F(1) (26). COMPLETED STEPS (27) THROUGH (70) PGS 713 715. 2 L 7 2 4F 4 F RT A16WE E2GL 20080716 NM 2008 7 16 KCSA081265 1 20080530 A 5330 SKIN BOEING 747 747212B 1384886 NM BS 1700 S43-44L DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 STA-1700 BETWEEN STR-43L AND STR-44L SKIN DAMAGED .5 INCH. 2 L 7 4 4F RT A20WE 20080925 EU 2008 9 25 08FDEA03379 1 20080811 A 5321 B5327060901500 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO FLOORBOARD 242 ZJ IS CRACKED. FABRICATED NEW FLOORBOARD NR 242 ZJ IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080925 WP 2008 9 25 08FDEA03951 1 20080919 A 5320 7075T6100ALR SUPPORT FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 571FE 47830 MCD LWR JAMB SUPPORT NR 5 FITTING HOLE NR C (FWD OUTBOARD) HAS CORROSION. REAMED HOLE, FABRICATED BUSHING, NDT HOLE, IN STALLED BUSHING AND REAMED NEW BUSHING IAW MAE TRAVELER T8/757301, NTSPN 06-10-01 AND SRM 53-50-00 FIG 17. MAJOR REPAIR , RII, RDR AND SDR. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03762 1 20080908 A 2820 LINE DOUG MD10 MD1010F 3022112 WP ZONE 600 CRACKED A FDEA K NONE K FLUID LOSS IN INSP/MAINT 1 CE 21 550FE 46521 RIGHT WING OUTBD FUEL TANK OPENING 635 AT, FWD MOST FUEL LINE HAS A CRACKED, CLAMP ATTACH BRACKET. XORS 593 OUTBD AND FWD OF THE OPENING. REMOVED THE BRACKET. FABRICATED A NEW BRACKET AND INSTALLED THE NEW BRACKET IAW DWG ARL 0500, REV "BM" AND SRM 51-31-01, VOL II. ALODINED IAW SRM 51-21-01; VOL II. PART MARKED IAW GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03763 1 20080908 A 5740 ARL0501200 ATTACH BRACKET DOUG MD10 MD1010F 3022112 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 RIGHT WING OUTBD FUEL TANK OPENING 634 BT, FWD MOST FUEL LINE HAS A CRACKED CLAMP ATTACH BRACKET. XORS 480 OUTBD AND FW D OF THE OPENING. REMOVED THE BRACKET. FABRICATED A NEW BRACKET AND INSTALLED THE NEW BRACKET IAW DAC DWG ARL 0501; REV "AU" AND DC/MD-10 SRM 51-31-01; VOL II. ALODINED IAW DC/MD-10 SRM 51-21-01; VOL II. PART MARKED IAW FEDEX GMM 7-0- 1001. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03764 1 20080908 A 5740 ARL0501200 ATTACH BRACKET DOUG MD10 MD1010F 3022112 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 RIGHT WING UPPER FUEL TANK OPENING 634 BT, AT XORS 455 HAS A FUEL LINE CLAMP ATTACH BRACKET CRACKED INBD AND FWD OF TH E OPENING. REMOVED THE BRACKET. FABRICATED A NEW BRACKET AND INSTALLED THE NEW BRACKET IAW DWG ARL 0501; REV "AU" AND SRM 51-31-01; VOL II. ALODINED IAW SRM 51-21-01;VOL II. PART MARKED IAW GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03765 1 20080908 A 5740 ARL053141 ATTACH BRACKET DOUG MD10 MD1010F 3022112 WP ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING UPPER FUEL TANK ACCESS 533 AT, FUEL LINE ATTACH BRACKET WORN AND LOOSE AFT AND OUTBD OF THE OPENING AT THE RIB (XORS 316.9). REMOVED BRACKET ASSEMBLY -41 AND -37. FABRICATED A NEW BRACKET ASSEMBLY -41 AND -37. INSTALLED THE N EW BRACKET ASSEMBLIES -41 AND -37 IAW DAC DWG ARL 0531, REV "AA" AND DC/MD-10 SRM 51-31-01; VOL II. ALODINED IAW DC/MD -10 SRM 51-21-01, VOL II. PART MARKED IAW FEDEX GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03772 1 20080908 A 5730 ARB0903501 DOUBLER DOUG MD10 MD1010F 3022112 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LT WING NR 2 TANK INBD COMP PROBE PANEL LAND HAS A CRACK AT THE ATTACH BOLT HOLE. REMOVED & REPLACED NR 8 STRINGER IN R EF TO EA 8-5720-117035 LEAK CHECK COMPLIED WITH ON NON-ROUTINE N00534 / 41534. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03956 1 20080921 A 2613 ENGINE BOEING 757 75727B 1384921 NM OVERHEAT FALSE INDICATION A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 916FD 24137 DURING CLIMB PASSING FL180 EICAS MESSAGE DISPLAYS L ENG OVHT ALL OTHER ENG INDICATIONS WERE NORMAL. RETARDED L THROTTLE AND TURNED OFF L BLEED AIR. AFTER APPROXIMATELY 2 MIN THE EICAS MESSAGE WENT AWAY. DECLARED EMERGENCY AND LANDED WITH L ENG AT IDLE. COMPLIED WITH QRH. REPLACED HP2 DUCT ASSY AS PER MM36-11-01-4. 2 L 7 2 4F RT A2NM 20080925 NM 2008 9 25 08FDEA03957 1 20080921 A 2910 BACH8A08NN0360T HOSE BOEING 727 727227 1384078 NM HYD SYSTEM LEAKING A FDEA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CE 21 492FE 21530 TEST FLIGHT, LOST ALL HYD SYS A FLUID UPON RAISING LANDING GEAR. REMOVED AND REPLACED LMLG ACTUATOR LOWER HYDRAULIC HOS E IAW MM 32-32-000-4. LEAK CHECK GOOD IAW MM 32-32-000-5. 2 L 7 3 4F A3WE 20080925 NM 2008 9 25 08FDEA03615 1 20080828 A 5313 AFA7762501 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 574FE 48499 CENTER CARGO STA 1541 TO STA 1561 LONGERON 52 FOUND CORRODED. CENTER CARGO STA 1541 TO STA 1561 LONGERON 52 REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03777 1 20080908 A 5246 ARB23695 HINGE DOUG MD10 MD1010F 3022112 WP FUEL DOOR WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING FUEL TANK FUEL FLAPPER VALVE AT XORS 402; 534 AT ACCESS OPENING; HAD ELONGATED MOUNT HOLES (A/C SIDE) AT THE ATTACH BRACKET. REMOVED THE FLAPPER DOOR AND HINGE ASSEMBLY IAW SRM 51-31-01, VOL II. FABRICATED A NEW HINGE ASSEMBLY AND INSTALLED THE NEW HINGE ASSEMBLY IAW DWG ARB 2369; REV "C" AND SRM 51-33-01;VOL II. ALODINED AND PRIMED IAW SRM 5 1-21-01; VOL II. RE-INSTALLED THE FLAPPER DOOR IAW SRM 51-31-01; VOL II. PART MARKED HINGE ASSEMBLY IAW GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03616 1 20080828 A 5753 65246001 SPAR BOEING 727 727227 1384078 NM RT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 RT WING O/B MID FLAP AFT SPAR, UPPER CHORD IS CRACKED AT WBL 332 REMOVED AND REPLACED RT O/B MIDFLAP ASSY IAW FX B727-20 0 MM 27-51-011-4. OPS CHECK GOOD IAW FX B727-200 MM 27-51-011-4 AND 27-51-000-5. 2 L 7 3 4F A3WE 20080925 NM 2008 9 25 08FDEA03617 1 20080828 A 5753 652163113 SKIN BOEING 727 727227 1384078 NM RT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 LT WING O/B FORE FLAP L/E REPAIR DOUBLER IS CHAFED (DAMAGED) AT WS 440 REMOVED PREVIOUS REPAIR DOUBLER IAW SRM 51-30-2. FABRICATED NEW DOUBLER IAW SRM 57-50-2 FIG 4 AND SRM 57-50-4 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REP AIR DOUBLER IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20080925 NM 2008 9 25 08FDEA03369 1 20080810 A 5347 AFA7795507 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 587FE 48489 MAIN DECK CARGO COMPARTMENT AT APPROXIMATELY STATION 1541, X = -8.5 FOUND SEAT TRACK FLANGE CORROSION. CABIN MAIN DEC K CARGO COMPARTMENT SEAT TRACK REPAIRED FROM STA 1531 TO STA 1551, X = -8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPA IR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03371 1 20080810 A 5730 ARB74024 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 587FE 48489 05 EACH FASTENER HOLES FOUND CRACK INDICATION AS MARKED DURING OPEN-HOLE HFEC INSPECTION AT RT WING LOWER SKIN ACCESS DO OR CUTOUT BETWEEN STATION XORS = 683.400 AND STATION XORS = 713.600. REPAIR CARRIED OUT AT RT WING FUEL TANK LOWER SKIN CUTOUT AT STA XORS = 683.400 AND STA 713.600 AS PER FEDEX EA NR 1-5710-122417, THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 QXEA200800958 1 20080907 A 2611 47359715 SMOKE DETECTOR BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 19 413QX 1442 4060 SEA FLIGHT 2216. NUMEROUS MOMENTARY MASTER WARNING SMOKE ILLUMINATIONS DURING FLIGHT. ASSOCIATED AFT BAGGAGE SMOKE LIG HT ALSO ILLUMINATED. THE ILLUMINATION OF THESE LIGHTS WAS FOR ABOUT 1 SECOND. NO SMOKE DETECTED IN THE CABIN. MX REPL ACED BOTH AFT CARGO COMPARTMENT SMOKE DETECTORS. CHECKS GOOD. ACFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080716 NM 2008 7 16 DL75E080772 1 20080523 A 3350 LIGHT BOEING 767 7672Q8 1385157 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 710TW 28169 728712 THE 36C EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT, OPS OK. 2 L 7 2 4F RT A1NM 20080716 NM 2008 7 16 08FDEA02073 1 20080531 A 5320 6550290 BEAM BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 RT A/C EQUIP BAY PANEL 3455 HAS CORROSION UNDER FWD HINGE PLATE ON FRAME REMOVED PNL NR 3453, 3358, 3465. SPLICED IN NE W BEAM ASSY P/N NR 65-58502-90. FABRICATED 4. REPAIR ANGLES, TREATED AND PRIMED AND INSTALLED. RE-INSTALLED A/C PANEL S. REF SRM 51-30-02 PG5, 51-40-4 PG 14-17, 51-30-4 PG 1-2, RESTORED CIC REF SRM 51-10-2. THIS IS CLASSIFIED AS A MINO R REPAIR. 2 L 7 3 4F RT A3WE 20080716 NE 2008 7 16 DL75E080773 2 20080523 A 7321 736001006 FUEL CONTROL BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE NR 1 ENGINE MALFUNCTIONED A DALA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 718TW 28098 28486 728712 AFTER LEFT ENGINE START THROTTLES ADV BUT ENGINE UNRESPONSIVE. LEFT ENG BLEED VALVE WOULD NOT OPEN. FIRE REPORTED TO B E FROM LEFT ENG TO ABOVE WING AND ENG SMOKING. FUEL CONTROL SW TO OFF AND NR 1 ENGINE FIRE BOTTLE DISCHARGED. NO ENG E XCEEDANCES ON MTC PAGE. EPCS MSG P AOX ON FCU/EEC. REPLACED FCU PER AMM. INSPECTED PYLON AND AFT OF ENG WING AREA FOR POSSIBLE DAMAGE. NO TROUBLE FOUND. PERFORMED FUEL CONTROL REPLACEMENT TEST PER 71-00-00-735-328-P00. ENGINE CKS NORMA L. ETOPS CATEGORY 'D': INABILITY TO CTRL ENG OR GET DESIRED PWR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080716 WP 2008 7 16 UPS08852352 1 20080513 A 5320 9754055U1 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 STA 280, L36 FLANGE IS CRACKED ON FITTING. REMOVED AND REPLACED STA 280/L 36 FITTING IAW SRM 51-01-2 4-0 AND SRM 51-03-00-0. 2 L 7 4 4F RT 4A25 20080716 EU 2008 7 16 08FDEA02036 1 20080530 A 5313 A53811360200 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON STRINGER P50, C39-41. CORROSION REWORKED AND NDT FPR CRACK FREE CONDITION PERFORMED IAW RAS 70507182 /009/2008, APPROVED BY EA 6-5315-120102. 2 L 7 2 4F RT A35EU 20080716 SO 2008 7 16 C2XA08ON126 1 20080525 A 5240 ROD EMB 145 EMB145LR 3260212 SO SERVICE DOOR LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14558 145598 FLT 0543 - MCI - FLIGHT CREW REPORTED SERVICE DOOR WILL NOT OPEN FROM INSIDE. MX SECURED LOOSE HARDWARE AT DOOR OPEN RO D. OPERATIONALLY CHECK SATISFACTORY AIRCRAFT RELEASED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20080716 2008 7 16 AALA200801283 4 20080512 A 3460 COMPUTER DOUG DC9 DC982 3022082 WP FLT GUIDANCE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 477AA 49652 SDF INFLIGHT T1485/12MAY DCA TO DFW - DIGITAL FLIGHT GUIDANCE COMPUTER CIRCUIT BREAKER POPPED. AIRCRAFT BANKED TO RIGHT WHEN AUTOPILOT REENGAGED. LANDED SDF WITHOUT INCIDENT. REPLACED SWITCH A CIRCUIT BREAKER, NUMBER TWO DIGITAL FLIGHT G UIDANCE COMPUTER AND DIGITAL FLIGHT GUIDANCE MODE PANEL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080716 NM 2008 7 16 NWAA082445649 1 20080516 A 5330 SKIN BOEING 757 757251 1384970 NM BS 360-378 DENTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 549US 26496 DURING "M" CHECK, FOUND DENT IN FUSELAGE SKIN AT BS 360-378 S17R-S18R. REPAIRED PER EA 56-210592. 2 L 7 2 4F RT A2NM 20080716 NM 2008 7 16 UPS08M52360 1 20080404 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C LEFT WING FUEL TANK UPPER 14 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 0.5 INCH. STR 14 END SPLICE REMOVED. ATTACH CLIP & FASTENERS REMOVED. SLOT OUT CRACKED AREA C/O. HFEC INSP C/O ON REWORK AREA & FOUND NO CRACK EVIDENT. TWO EA REPAIR ANGLES FAB & HEAT- TREATED. CLIP FAB WITH FPI C/O. FOUND NO CRACK EVIDENT. REPAIR ANGLES, STR END SPLICE & CLIP INSTALLED, WITH SEALANT APPLIED. LEAK CHECK SATIS. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 NWAA082486309 1 20080531 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING OVERNIGHT CHECK, FOUND ZONE B RIGHT SIDE FLOOR PATH LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY A ND BATTERY PACK. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20080716 NM 2008 7 16 UPS08M52361 1 20080406 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C LEFT WING FUEL TANK LOWER 43 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 8 INCH. STR 43 END SPLICE REMOVED. ATTACHED CLIP & FASTENERS REMOVED. SLOT OUT CRACKED AREA C/O. HFEC INSP C/O ON REWK AREA, FOUND NO CRACK EVIDENT. REPAIR ARROWHEAD FITTING FAB WITH FRI C/O & FOUND NO CRACK EVIDENNT. REPAIR ARROWHEAD FITTING & CLIP INSTALLED. SEALANT ON REPAIR AREA APPLIED & LEAK CHECK SATISFACTORY. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 UPS08M52362 1 20080406 A 5713 STRINGER DOUG MD11 MD11 3023602 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C RIGHT WING FUEL TANK LOWER 44 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 0.5 INCH . STR 44 END ARROWHEAD FITTING REMOVED. ATTACHED CLIP & FASTENERS REMOVED. CRACKED AREA TRIMMED OFF. HFEC C/O ON TRI M EDGE, FOUND NO CRACK EVIDENT. REPAIR ARROWHEAD FITTING FAB WITH FPI C/O, FOUND NO CRACK EVIDENT. REPAIR ARROWHEAD FI TTING & ATTACHED CLIP INSTALL. REWORK AREA PAINTED. LEAK CHECK SATIS. 2 L 7 3 4F RT A22WE 20080716 WP 2008 7 16 UPS08852386 1 20080422 A 5315 561215257 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 MAIN CABIN FLOORBEAM HAS INTERGRANULAR CORROSION, LOWER SURFACE OF UPPER AFT FLANGE STA1700 RBL 20 TO 28. REPAIRED MAIN CABIN FLOORBEAM AT STA 1700 RBL 20 TO 28 IAW EA 008- 5310-01-A1369, EO DC8-5310-29405-AAND DWG 57550 32. 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 UPS08B52380 1 20080329 A 5311 FRAME BOEING 747 747400 13848AT NM BS 1140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:C LT BS 1140 TENSION TIE FRAME CRACKED. LT BS 1140 TENSION TIE FRAME REPAIRED PER SRM 53-40-07. 2 L 7 4 4F RT A20WE 20080716 NM 2008 7 16 2008UALA02988 1 20080524 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 AFT PIT STA 727A S-25L STRINGER ATTACH CLIP TO FRAME IS CRACKED. MAJOR REPAIR ACCOMPLISHED: REPLACED STRINGER ATTACH C LIP. 2 L 7 2 4F 4 F RT A16WE E21EU 20080716 NM 2008 7 16 UPS08B52381 1 20080417 A 5311 FRAME BOEING 747 747400 13848AT NM BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 LT BS 1180 TENSION TIE FOUND CRACKED AT FRAME MORE THAN O.200 INCH. LT BS 1180 TENSION TIE FRAME REPLACED PER SRM 53-40 -07. 2 L 7 4 4F RT A20WE 20080716 NM 2008 7 16 USAA920081138 1 20080521 A 5320 651768465 INTERCOSTAL BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - NR 3 O3C10753007/19, CRACKED INTERCOSTAL ANGLE, BS 303.9, S10L. REPLACED CRACKED INTERC OSTAL ANGLE, BS 303.9, S10L IAW BOEING SRM 51-10-02. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 USAA920081140 1 20080521 A 5310 06545871132 DOOR FRAME BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR SERVICE - Q6 CHECK - NR O3C10652003/12 AND O3C10652003/13, CRACKED FWD SERVICE DOOR FRAME. REPAIRED CRACKED FWD SERVICE DOOR FRAME IAW US AIRWAYS TYPICAL REPAIR NR 52-10-11. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 2008UALA02990 1 20080524 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 CREASE BEAM CORRODED IN SEVERAL PLACES FROM STA 290 TO STA 344 AT DOOR 1R. MAJOR REPAIR ACCOMPLISHED: REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E21EU 20080716 EU 2008 7 16 08FDEA02117 1 20080603 A 5315 A53974343200 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION SPOTS ON CROSS BEAM C 72, C 46-46`. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080716 NM 2008 7 16 2008UALA02991 1 20080524 A 5320 FLOOR SUPPORT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 CABIN FLOORBOARD SUPPORT CORRODED AT STA 335 RBL 50. MAJOR REPAIR ACCOMPLISHED: REPLACED FLOOR SUPPORT AT STA 328 TO S TA 344. 2 L 7 2 4F 4 F RT A16WE E21EU 20080715 CE 2008 7 15 MT9A00000024 1 20080512 A 3240 06111800 HOUSING CESSNA 208 208B 2073701 CE BRAKE ASSY DAMAGED E MT9A K NONE O OTHER IN INSP/MAINT 1 SW 05 4655B 208B0160 BRAKE CYLINDER HOUSING WORN AT THE ANCHOR BOLT PASS THROUGH HOLE ALLOWING THE ANCHOR BOLT TO BE PRESSED OUT BY HAND. THI S IS NORMALLY A CLOSE TOLERANCE FIT. THIS CONDITION IN THE PAST HAS CAUSED THE ANCHOR BOLT TO SHEER OFF CAUSING CATASTRO PHIC DAMAGE TO THE CALIPER ASSEMBLY, TORQUE PLATE AND/OR TIRE OR THREE AC. (K) 1 H 7 1 3T A37CE 20080715 NM 2008 7 15 08FDEA02194 1 20080607 A 5320 65585684 THRESHOLD BOEING 727 727227 1384078 NM BS 1070-1090 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 R2 DOOR OPENING, THRESHOLD CRACKED 2 PLACES SENT TO SHOP FOR WELD REPAIR ON NR N00707. THRESHOLD WILL BE INSTALLED ON C LOSE CARD 72C201-01 THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080715 EU 2008 7 15 08FDEA02114 1 20080603 A 5720 A57111251200 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND TOOLING MARKS ON PICK UP FITTING GANTRY 5 LT, C 47 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080715 NM 2008 7 15 UPS08B52387 1 20080417 A 5340 TENSION TIE BOEING 747 747400 13848AT NM BS 1140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:C BS 1140 TENSION TIE LT AFT SIDE CRACKED. BS 1140 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201. 2 L 7 4 4F RT A20WE 20080715 NM 2008 7 15 ASAA0843012 1 20080520 A 5230 65C362311 SKIN BOEING 737 737490 1384715 NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 AFT CARGO DOOR HAS 10 EA DENTS. REMOVED CARGO DOOR SKIN FABRICATED AND INSTALLED REPLACEMENT SKIN IAW B737 400 SRM 52 3 0 01 PG 201. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082904 1 20080529 A 5311 65C25228 FRAME BOEING 737 7373H4 1384600 NM BS 727C S27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727C, STR 27R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082890 1 20080529 A 3350 3071BPEGPL LIGHT BOEING 737 737705 13844SC NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 270WN 29089 DURING SCHEDULED 10Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 8 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082891 1 20080529 A 3350 767 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082892 1 20080529 A 5753 65C30462 SKIN BOEING 737 7373H4 1384600 NM FORE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED SPV CHECK, FOUND LT WING INBOARD FORE FLAP UPPER INBOARD SURFACE DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA082914 1 20080529 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 22Y CHECK, FOUND STRINGER 27L CORRODED AT BS 1006. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080715 SW 2008 7 15 EHA2008F00001 1 20080627 A 5100 CHIP DETECTOR BELL 206 206L3 1182108 SW ACTIVATED E EHAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 AL 03 33AZ 51110 CHIP LIGHT ILLUMINATED, PILOT LANDED AIRCRAFT IMMEDIATELY. INSPECTION FOUND TINY SLIVER ON CHIP PLUG, NO FURTHER FINDIN GS. FOLLOWED MANY PROCEDURES. NO FURTHER PORBLEMS NOTED. (K) 1 G 7 1 3U H2SW 20080925 EA 2008 9 25 SWIA200820042 1 20080909 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 925SW CEILING EMERGENCY LIGHT ROW 5 INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20080925 NM 2008 9 25 08FDEA03358 1 20080810 A 5311 6516318108 FRAME BOEING 727 727233 138408A NM ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 FRAME DAMAGED STA 360 STR 2R. CUTOUT DAMAGED AREA DIMS 1 1/8 INCH BY 1 INCH, FABRICATED REPAIR ANGLE FROM 7075-0 .063 P O NR 9007470 DIMS 9 INCH BY 3 INCH BY 1 INCH. INSTALLED REPAIR ANGLE AT BS 360 STR 2R IAW B727 SRM 53-10-4 FIG 2 AND S RM 53-10-2 FIG 3. 2 L 7 3 4F RT A3WE 20080925 EU 2008 9 25 08FDEA03278 1 20080806 A 5321 B5327031800400 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DOOR PANEL NR 261 UF, LOWER SURFACE IS CRACKED AND PUNCTURED. FABRICATED PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03279 1 20080806 A 5321 B5327028600400 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DOOR PANEL NR 251 AH; UPPER AND LOWER SURFACE IS CRACKED AND PUNCTURED. FABRICATED PANEL IAW SRM 53-10-20 AN D DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080925 WP 2008 9 25 08FDEA03816 1 20080911 A 5753 NRC6060 SKIN DOUG DC10 DC1030F 3023504 WP RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 RT WING INBD FLAP FOUND DEEP DENT ON LOWER SKIN 0.25 INCH BY 0.25 INCH DEEP .074 INCH (SUSPECT CRACK ). REPAIRED DENT I AW SRM 57-00-01 FIG 4 SHT 2 VOL I. 2 L 7 3 4F RT A22WE 20080925 EU 2008 9 25 08FDEA03817 1 20080911 A 5730 A5735000220000 SKIN AIRBUS 310 A310222 3930315 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 LEFT WING FUEL TANK DOOR CUT OUT BETWEEN RIB 25 AND RIB 26 IS CORRODED. REMOVED CORROSION AND CHECKED LIMITS. ORIGINAL THICKNESS 0.276. REMOVED MATERIAL 0.003. REMAINING THICKNESS 0.273 AND IS FOUND TO BE WITHIN LIMITS IAW SRM 57-20-12, PG 68, FIG 7A AND SRM 57-20-12, PARA A-1 (G), FIG 201. ACCOMPLISHED PFPI IAW A310 NTM 51-90-11. ALODINED AND PRIMED I AW SRM 51-20-10 AND SRM 57-20-12; PG 201B; PARA 3(A). 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03325 1 20080808 A 5321 R532B362100000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOORBOARD IS CRACKED AT BS 1711, LBL 60. REPAIRED CABIN FLOOR PANEL 231 VG DOT C389 BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED T HE INSERTS. PART MARKED AND APPLIED NON-SKID TAPE IAW DWG SRZ 25-005, REV "G". 2 L 7 2 4F RT A35EU 20080925 NM 2008 9 25 08FDEA03302 1 20080807 A 5753 6526787 FAIRING BOEING 727 7272S2F 1384O81 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 LEFT WING INBD TE NR 3 FLAP TRANSMISSION JACKSCREW FAIRING ON O/B END OF MID FLAP IS CRACKED OUT OF FWD UPPER HOLE REMOV ED FAIRING. NDT VERIFIED CRACK LOCATION. REMOVED DAMAGE AND INSTALLED REPAIR. REINSTALLED FAIRING TO MID FLAP REF SRM 51-30-2 PG 13/ NDT MAN PART 6 51-00-00, FIG 23/ SRM 57-20-4, FIG 1/SRM 51-30-4, FIG 1. THIS IS CLASSIFIED AS A MINOR R EPAIR. 2 L 7 3 4F A3WE 20080925 EA 2008 9 25 SWIA200820043 1 20080908 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 367CA 10069 CEILING EMERGENCY FLOOD LIGHT FORWARD OF AFT LAV INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20080926 WP 2008 9 26 08FDEA03989 1 20080922 A 5321 ABA72033 FLOOR SKIN DOUG DC10 DC1030F 3023504 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 AFTER REMOVAL FLOOR PANEL ON COCKPIT AREA WITH OAN J/C 0600C210-1JR FOUND SEVERE CORROSION ON MEMBRANE. REPAIRED WEB IAW SRM 53-00-01 FIG 4 SHT 2 VOL I. 2 L 7 3 4F RT A22WE 20080926 EU 2008 9 26 08FDEA03998 1 20080923 A 5415 A54611051200 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 400 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOR A REPAIR THE NEW PYLON SPIGOT FITTING FOR PYLON NR 2 HAVE BEEN DELIVERED WITHOUT ATTACHMENT HOLES AND SURFACE PROTEC TION. REPAIR PERFORMED BY DRILL SPIGOT FITTING BY COPY OF OLD PART, PERFORM SPRAYING SURFACE PROTECTION AND INSTALL F ITTING PER DRAWING R546-10351 IAW RAS/70513739/016/2008 ISS A, APPROVED BY EA 6-5451-123142. 2 L 7 2 4F RT A35EU 20080926 WP 2008 9 26 08FDEA03999 1 20080923 A 5411 AUB710739 RIB DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 1 PYLON PANEL 439 AL FWD RIB IS CHAFED THROUGH. REMOVED RIB IAW ARM 51-35-01; VOL II. LOCATED AND DRILLED THE NEW R IB P/N AUB 7107-39, PO 631193.2 IAW DWG AUB 7107; REV "P". INSTALLED NEW RIB IAW SRM 51-35-01; VOL II. 2 L 7 3 4F RT A22WE 20080926 EU 2008 9 26 08FDEA04001 1 20080923 A 5230 SKIN AIRBUS 300 A300B4622R 3930312 EU CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD UH1625 664 FOUND ON AFT CARGO DOOR CORROSION ON SKIN PLATES (P/N A523-74263-212, A523-74263-214, A523-74160-208) REPAIR PERFORMED B Y CORROSION REWORK, NDT FOR CORROSION FREE CONDITION IAW RAS/DAHAM/4025425/2008 ISS A, APPROVED BY EA 6-5232-123072. 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 08FDEA03991 1 20080922 A 5330 143N3691 SKIN BOEING 757 757236 1384971 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 915FD 24120 EXISTING RT FUSELAGE SKIN EXTERNAL DOUBLER REPAIR AT BS 670, S-20R-S-21R, COMPLY WITH ATTACHMENT "B" OF EO F-5100-7-5001 , PART 1. DURING EVALUATION OF ABOVE NOTED REPAIR PER ATTACHMENT "B" OF EO F-5100-7-5001, PART 1, IT WAS DISCOVERED THA T PREVIOUS REPAIR WAS NOT PER ANY APPROVED DATA. REMOVED EXISTING REPAIR AND INSTALLED A NEW DOUBLER REPAIR PER SRM 53 -00-01, FIGURE 201, REPAIR NR 16. NEWLY INSTALLED DOUBLER REPAIR AT BS 670, S-20R - S-21R, EXTERNAL, IS CLASSIFIED AS A CATEGORY "B" MAJOR REPAIR WITH THE FOLLOWING REPETITIVE INSPECTION: INSPECTION THRESHOLD; 25,000 FC; REPEAT INTERVA LS OF 3,000 FC (LFEC). 2 L 7 2 4F RT A2NM 20080926 NM 2008 9 26 08FDEA03992 1 20080922 A 5310 CREASE BEAM BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 MAIN CABIN, BS 1180 - 1200, RT SIDE, I/B CREASE BEAM CHORD HAS CORROSION UNDERNEATH FWD AND AFT NUT PLATES. REMOVED C ORROSION ON WEB CHORD AT BS 1180-1200, AND FOUND TO BE OUT-OF-LIMITS IAW SRM 53-60-13, FIG 101, DETAIL 3. REMOVED AND R EPLACED CREASE BEAM WEB CHORD PER MAE TRAVELER NR T8/760030 AND SRM 51-40-02, 51-10-02 AND 53-60-13. THIS REPAIR IS CLA SSIFIED AS A "MAJOR" REPAIR, CATEGORY "A". NO FOLLOW UP TRACKING IS REQUIRED. 2 L 7 2 4F RT A2NM 20080926 NM 2008 9 26 08FDEA03993 1 20080922 A 5320 CUSP WEB BOEING 757 75723A 1384967 NM BS 1000-1020 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 CENTER WING, INTERNAL, BS 1000-1020, RBL 68, CUSP WEB CORRODED. REMOVED CORROSION ON CTR WING, INTERNAL, SHEAR WEB, BS 1000-1020, RBL 68, PER SRM 51-21-01, 51-40-02. FOUND CORROSION OUT-OF-LIMITS PER SRM 53-40-13, FIG 101, DETAIL 3. R EMOVED AND REPLACED SHEAR WEB, CTR WING INTERNAL, BS 1000-1020, RBL 68 PER MAE TRAVELER NR T8/753665 AND SRM 51-40-02, 5 1-20-01 AND 53-40-13, FIG 101, DETAIL 3. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRA CKING REQUIREMENTS. 2 L 7 2 4F RT A2NM 20080926 NM 2008 9 26 2008UALA05784 1 20080917 A 2421 734285E GENERATOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE RIGHT FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 675UA 29243 EICAS MSG R GEN OFF DISPLAYED. GEN OFF LGT ILLUM AND FAILED TO RESET. REPLACED GCU AND REPLACED IDG, NO HELP. ALSO SWA PPED BUSS POWER CONTROL UNIT, NO HELP. REINSTALLED OLD BPCU. WIRE HARNESS REPAIRED. ACP 'D GROUND ENGINE RUN. GEN OPS CH ECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20080926 NM 2008 9 26 2008UALA05785 1 20080918 A 5753 WEDGE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT TE FLAP DEBONDED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 FOUND LEFT INBD MID FLAP TRAILING EDGE WEDGE DISBONDED BETWEEN THE WEDGE AND ATTACH CHANNEL. GAP BETWEEN TRAILING EDGE WEDGE OF MID FLAP AND LEADING EDGE OF AFT FLAP IS OUT OF LIMITS. REMOVED T/E WEDGE & ADJUSTED GAP. REPLACED MID FLAP WED GE. REPLACED INBD TE FLAP SLAVE ATTACH FITTING. 2 L 7 2 4F 4 F RT A16WE E2GL 20080922 NM 2008 9 22 ASAA0843418 1 20080825 A 5751 6546455270 SKIN BOEING 737 7374Q8 138447Q NM LT WING AILERON DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 LT WING AILERON TRIM TAB HAS DELAM. LT WING AILERON TRIM TAB REPAIRED IAW B737 400 SRM CH 51 70 16. 2 L 7 2 4F RT A16WE 20080923 NM 2008 9 23 DL764081161 1 20080907 A 5414 81205331T10 PANEL BOEING 767 767432ER 1385134 NM LT NACELLE MISSING A DALA O OTHER D INFLIGHT SEPARATION CL CLIMB 1 SO 27 832MH 29704 NR 1 ENGINE NACELLE STRUT ACCESS DOOR MISSING. 2 L 7 2 4F RT A1NM 20080923 2008 9 23 DL76G081167 2 20080908 A 7532 SWITCH BOEING 767 767332 1382001 NM BLEED VALVE BROKEN A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 171DZ 29690 RTB DUE TO R ENG BLEED VALVE SWITCH WILL NOT STAY LATCHED IN. FOUND BLEED VLV SWITCH LIGHT BROKEN INTERNALLY. REPLACED SWITCH LIGHT ASSY. 2 L 7 2 4F RT A1NM 20080923 EA 2008 9 23 SWIA200820013 1 20080902 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 915SW 7615 EMERGENCY FLOODLIGHT ON BULKHEAD NEAR AIRSTAIR BROKEN. REPLACED FLOOD LIGHT ASSEMBLY AT PAX DOOR ENTRANCE. 2 L 7 2 4F RT A21EA 20080923 NM 2008 9 23 2008UALA05421 1 20080823 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 117UA 28810 DOOR 2 RIGHT SILL EMERGENCY LIGHT IS INOP. RELAMPED. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080923 NM 2008 9 23 2008UALA05428 1 20080823 A 3397 58791 FEEDER CABLE BOEING 737 737322 1384676 NM EMERGENCY LIGHTS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 AFT GALLEY EEL STRIP INOP. FOUND FEEDER CABLE DAMAGED. REPAIRED FEEDER CABLE. AC OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20080923 NE 2008 9 23 DL76L081101 2 20080821 A 7532 80217010 BLEED VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 176DN 25061 724638 DURING CLIMB-OUT HAD LEFT HPSOV EICAS MESSAGE WOULD NOT CLEAR FOLLOWED QRH PROCEDURES LEFT BLEED NOW SECURED. DIVERTING TO ATL FOR REPAIRS. 2 L 7 2 4F 4 F RT A1NM E24NE 20080923 NM 2008 9 23 DLM90081102 1 20080731 A 5320 ANGLE DOUG MD90 MD9030 3023690 NM BS 1250-1265 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DN 53395 FOUND CORROSION FROM STA 1250 TO 1265. REPLACED ANGLE PER SRM 51-30-03 AND 51-30-05. 2 L 7 2 4F RT A6WE 20080923 NM 2008 9 23 DLM90081103 1 20080805 A 5320 FITTING DOUG MD90 MD9030 3023690 NM BS 1395 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DN 53395 FOUND FITTING CORRODED. REPLACED FITTING REF SRM`S 51-30-02, 51-30-05, 53-10-01, & 53-10-02D. 2 L 7 2 4F RT A6WE 20080923 NM 2008 9 23 08FDEA03561 1 20080822 A 5711 112N1005 SPAR BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 LT AFT MAIN TANK BOOST PUMP HEAVY CORROSION ON SPAR. CORROSION REMOVED AND AREA TREATED IAW FEDEX EA NR F-5710-124306. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080923 EU 2008 9 23 08FDEA03486 1 20080818 A 5330 A5377873620800 SKIN AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 652FE 735 FUSELAGE EXTERION SKIN IS CORRODED AT FRAME 30 AND FRAME 31, STRINGER 52. DME ANTENNA, REFERENCE SNRM N00375. REMOVED CORROSION PER SRM 51-74-10. FOUND TO BE WITHIN LIMITS PER SRM 53-10-12. ALODINED AND PRIMED PER SRM 51-21-10. PAINTED PER SRM 51-21-10. 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 2008UALA05792 1 20080919 A 3397 WIRE HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHT INOP, DR1R AFT EXIT SIGN. REPAIRED HARNESS. OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080926 NM 2008 9 26 2008UALA05793 1 20080919 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 WALL EEL INOP, LWR WALL ACROSS FROM DR 1R. REPLACED LIGHT. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080715 NM 2008 7 15 ASAA0842998 1 20080514 A 5755 SKIN BOEING 737 737490 1384715 NM NR 1 SPOILER LT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 LT WING NR 1 SPOILER UPPER SURFACE DENTED 12 INCHES FROM T/E AND 10 INCHES FROM OUTBOARD END. PREPARED DAMAGED AREA, FA BRICATED DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083843 1 20080710 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 DURING SCHEDULED HC2 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. R&R BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083838 1 20080711 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 411WN 29821 EEPLS LENS LOOSE AT ROW 4 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 ASAA0852981 1 20080526 A 7720 TC29604 PROBE BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE NR 1 ENG EGT DIRTY A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 570AS 35185 894536 NR 1 ENGINE EGT HOT DAY MARGIN HAS NOT RECOVERED TO EXPECTEDLEVELS AFTER LAST COMPRESSOR WASH. ALL OTHER PARAMETERS A RENORMAL. COMPLETED T C 78273000, NO FAULTS LOGGED. PRE CLEAN T49.5 S1 S4 106 61 67 128. AFTER CLEANED 62 32 35 78. DURING ENG RUN AFTER3 MIN IDLE STAB 396 416 415 407. NO FAULT LOGGED EEC BITE PASS. TSR CLEARED REF LP 6434027 FOR PLT 20 CYCLE RECHECK PER MMS 77 21 00. 2 L 7 2 4F 4 F RT A16WE E2GL 20080716 NM 2008 7 16 KCSA081262 1 20080528 A 5412 BULKHEAD BOEING 747 7472B4B 138481B NM NR 4 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 4 PYLON REAR ENG MOUNT BULKHEAD AT NAC STA 221.9 CRACKED AT AFT O/B WEB. 2 L 7 4 4F RT A20WE 20080716 WP 2008 7 16 DHL2008807537 1 20080506 A 5410 COWL DOOR DOUG DC8 DC873F 302199F WP NR 3 NACELLE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 NR 3 ENG RT COWL DOORS EXTERIOR SHOW 2 DENTS AT 5 O'CLOCK POS STA YN 192.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-2-8 PAR 16 FIG 6, TR NR 71-44 DATED 11-20-07. CUT OUT CORE AND DAMAGED EXTERNAL SKIN IAW SRM 71-2-8 PAR 16 FIG 6, TR NR 71-44. FABRICATED EXTERNAL DOUBLER (AL2024T3 0.032") IAW SRM 71-2-8 PAR 16 FIG 6, TR NR 71-44 AND NEW CORE SEG MENT P/N 5056-1000 IAW DC8 SRM 71-2-8 PAR 16 FIG 6, TR NR 71-44. HEAT TREATED FROM 2024T3 TO 2024T62 IAW SRM 51-1-1 PG 1-13-17. PREPARED NEW CORE SEGMENT AND EXT DOUBLER IAW SRM 71-2-8 FIG 6, TR NR 71-44. BONDED CORE SEGMENT AND DOUBLER WITH ADHESIVE FM300-2 IAW SRM 71-2-8 PAR 16 ITEM J. INSTALLED REPAIR PARTS (BONDED) IAW SRM 71-2-8 PAR 16 FIG 6, TR NR 2 L 7 4 4F RT 4A25 20080716 WP 2008 7 16 08FDEA02021 1 20080529 A 5315 7075T6511 FLOORBEAM DOUG DC10 DC1010F 3022111 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 301FE 46800 AFT LOWER PIT STA 1841 FLOORBEAM IS CORRODED FROM LBL 20 TO RBL 20. AFTER CORROSION REMOVAL, FOUND OUT OF REPAIR LIMIT IAW SRM 53-00-01, REMOVED FLOORBEAM AND REPLACED NEW FLOORBEAM IAW SRM 51-31-01, CLASSIFIED AS MAJOR REPAIR. 2 L 7 3 4F A22WE 20080716 WP 2008 7 16 NWAA082459927 1 20080529 A 2150 WARNING LIGHT DOUG DC9 DC931 3022065 WP COCKPIT ILLUMINATED A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 8920E 45835 AT FL310 THE RED CABIN PRESS WARNING LIGHT ILLUMINATED. BOTH ENGINE & AIRFOIL ICE PROTECTION SYS OPERATING. ATTEMPT T O REGAIN CONTROL OF CABIN PRESSURE COMPLIED WITH, CABIN CONTINUED CLIMB. DECLARED EMERG & INITIATED EMERG DESCENT. CAB IN PRESS FOLLOWED CONTROLLER COMMANDS AT ABOUT 3.5 PSI DURING DESCENT. LANDED SAFELY. BITE CHKED BOTH CONTROLLERS & N O FAULTS. TAIL BAY INSPECTED FOR LOOSE OR BLOWN DUCTS WITH BOTH APU & EACH PACK INDIVIDUALLY. NO LEAKS FOUND & VESSEL PRESSURIZED NORMAL. FOUND ACFT WOULD NOT PASS CABIN PRESSURE DECAY CHK. FOUND LEAKS IN CABIN & LT PACK THE CAUSE. LEAKS REPAIRED & PRESSURE SYS OPS NORMAL. (A) 2 L 7 2 4F A6WE 20080716 NM 2008 7 16 ASAA0843018 1 20080601 A 5210 507945178 DOOR BOEING 737 7374Q8 138447Q NM L1 STIFF A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 50957 25102 FLIGHT ATTENDANT REPORTS THAT THE L1 DOOR HANDLE IS DIFFICULTTO MOVE TOWARDS THE CLOSED POSITION THE LAST FEW INCHES O FTRAVEL. ADJ FWD ENTRY DOOR GUIDE ARM REF MM 52 11 00, NO HELP. 76732. ADJ GUIDE ARM 1 FLAT IN76732. CONT WITH FWD ENTRY DOOR ADJ MIG 2 C 211789 INIT. SEE MIG 2C 211789 FOR WORK ACCP. RIGGED L1DOOR REF MM 52 11 00 705 007 B00. PE RFORMED FWD DOOR ENTRY DOOR TEST. REF MM 52 11 00 755 051 B00. MIG 2C 211789 CLOSED. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 AALA200801301 1 20080514 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 755AN 30263 DFW - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080716 NM 2008 7 16 AALA200801268 1 20080510 A 3350 3017684 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 355AA 24036 MIA - EMERGENCY LIGHT AT RIGHT NUMBER FOUR AFT SLIDE INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR AFT SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080716 NM 2008 7 16 UPS08M52357 1 20080404 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C LEFT WING FUEL TANK UPPER NR 12 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 11.5 I NCH. STR 12 END SPLICE REMOVED. STR 12 ATTACH CLIP & FASTENERS REMOVED. SLOT OUT CRACKED AREA C/O. HFEC INSP C/O ON RWK AREA, FOUND NO CRACK EVIDENT. TWO EA REPAIR ANGLES FAB & HEAT TREATED. REPAIR ANGLES, ATTACHED CLIP & SPLICE END I NSTALLED. SEALANT ON STR 12 REPAIR AREA APPLIED. LEAK CHECK SATIS. 2 L 7 3 4F RT A22WE 20080716 WP 2008 7 16 08FDEA02094 1 20080602 A 5414 AUB710812 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 NR 3 PYLON PANEL NR 487 HR IS CHAFED AT THE INNER SURFACE. BLENDED CHAFED AREA AND FOUND TO BE OUT OF LIMITS REF DC/MD- 10 SRM 54-00-01; VOL I. FABRICATED A NEW PANEL REF DAC DWG NR AUB7108; REV J. ALODINED AND PRIMED REF DC/MD-10 SRM 51 -21-01; VOL II. INSTALLED THE SEALS REF DC/MD-10 SRM 51-31-01; VOL II. PARTS MARKED REF FEDEX GMM 7-0-1000. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 AALA200801289 1 20080512 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 758AN 32637 DFW - EMERGENCY LIGHT AT SEAT 36G HAS LAMP MISSING. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 36G. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080716 NM 2008 7 16 2008UALA03008 1 20080523 A 5512 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 914UA 25381 RIGHT HORIZONTAL STABILIZER STA 120 LOWER SKIN CRACKED JUST FORWARD OF AFT SPAR. MAJOR REPAIR ACCOMPLISHED: REMOVED DA MAGE. VERIFIED DAMAGE RMVL WITH HFEC. INSTALLED A REPAIR DOUBLER & FILLER. ALSO INSTALLED TWO ACCESS PANELS. 2 L 7 2 4F 4 F RT A16WE E21EU 20080716 NM 2008 7 16 2008UALA03016 1 20080525 A 3350 79411 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE SEAT 2H UNSECURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 672UA 30027 EMERGENCY PATH LIGHTS DANGLING FROM AISLE ARM REST 02H. FOUND LOOSE LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY OP CHECKE D GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080926 NM 2008 9 26 2008UALA05794 1 20080919 A 3350 FU305 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHTS INOP, LT OVERWING 2 FWD MOST ASSY. REPLACED FUSE ON EPSU. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080926 NM 2008 9 26 2008UALA05795 1 20080919 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHTS INOP, CEILING BEHIND ROW 18 BY- 104896. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 20080926 WP 2008 9 26 08FDEA03252 1 20080805 A 5310 NDA6024 BEAM DOUG DC10 DC1030F 3023504 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 FWD CARGO COMPT SEVERE CORROSION WITH EXFOLIATION ON BEAM LOWER SIDE. 2 L 7 3 4F RT A22WE 20080926 WP 2008 9 26 08FDEA03253 1 20080805 A 5321 ABA720323 FLOOR PANEL DOUG DC10 DC1030 3023501 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 AFTER REMOVAL FLOOR PANEL ON COCKPIT AREA WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE. 2 L 7 3 4F A22WE 20080926 WP 2008 9 26 08FDEA03819 1 20080911 A 5713 ARB08232 STRINGER DOUG MD10 MD1010F 3022112 WP ZONE 600 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 RIGHT WING OUTER FUEL TANK UPPER STRINGER 3 - 4 AT XORS 965 (639 BB ACCESS OPENING) HAS A GOUGED EDGE. TRIMMED THE ED GE OF THE STRINGER. ORIGINAL THICKNESS OF THE LEG IS 1.080. MATERIAL REMOVED 0.020. REMAINING WIDTH OF THE LEG IA 1.0 60 AND FOUND TO BE WITHIN LIMITS IAW DC/MD-10 SRM 57-00-01, FIG 1-A,VOL II. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21- 01, VOL II. 2 L 7 3 4F RT A22WE 20080926 EU 2008 9 26 08FDEA03824 1 20080911 A 5321 A5327997800200 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 FWD LOWER CARGO COMPARTMENT FLOOR PANEL 132 MG IS BROKEN AND PUNCTURED. FABBED NEW PANEL 132 MG IAW DWG SRZ 25-005; REV "G". PART MARKED IAW GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03825 1 20080911 A 5321 A532102100000 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 AVIONICS COMPARTMENT FLOOR PANEL 121 JF HAS EDGE DAMAGE. FABBED A NEW PANEL IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080926 WP 2008 9 26 08FDEA02867 1 20080714 A 5330 SM105300015 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 FUSELAGE EXTERNAL SKIN HAS 2 DENTS BETWEEN LONGERONS 41R AND 42R AT FS 1821. INSPECTED THE AREA AND FOUND IT TO BE GOOD IAW EA 8-5330-123604; TITLED "FUSELAGE - SKIN AT STA 1825 AND L-40R - DENTS". 2 L 7 3 4F RT A22WE 20080926 NM 2008 9 26 08FDEA03632 1 20080829 A 5313 655458346 STRINGER BOEING 727 727227 1384078 NM BS 1010-1039 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 CORROSION INSIDE CHANNEL AND AT ATTACHING RIVETS STR 27L STA 1010 TO STA 1039 CUT OUT DAMAGED SECTION IAW SRM 53-10-31 F IG 1. FABRICATED 2 STRINGER SECTIONS AND 3 SPLICE SECTIONS IAW SRM 53-10-3 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED 2 STRINGERS AND 3 SPLICES IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20080926 WP 2008 9 26 08FDEA03634 1 20080829 A 5347 ADA73491 SEAT TRACK DOUG DC10 DC1030F 3023504 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 MAIN DECK, FROM STA 808 TO STA 879 AT X=-75, CORROSION WITH EXFOLIATION ON SEAT TRACK. REPAIR PER SRM 53-70-00 VOL.1 F IG.1 SHEET 1. 2 L 7 3 4F RT A22WE 20080926 WP 2008 9 26 08FDEA03635 1 20080829 A 5730 ARB3029514 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 RT WING L/E, FOUND DEEP WEAR ON SKIN AND PANEL LOWER SIDE L/E AT STA XORS 264. REPAIR IAW SRM 57-10-00 VOL 1 FIG 15 . 2 L 7 3 4F RT A22WE 20080926 WP 2008 9 26 08FDEA03304 1 20080807 A 3231 ARC2859506 DOOR DOUG MD10 MD1010F 3022112 WP MLG OUT OF ALIGNMENT A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 CE 21 395FE 77546 46629 AFTER GEAR RETRACTION RT MAIN INDICATION REFLECTED UNSAFE (RED) INTERMITTANLY CYCLED GEAR REF QRG AND UNSAFE GEAR INDICA TION REMAINED OUT ON SLOW DOWN FOR LANDING UNSAFE RT MAIN GEAR AT 200 KNOTS UNSAFE INDICATION ON PRI AND SEC SOURCES, SW UNG GEAR. FOUND WING DOOR NOT FAIRED (DN .25 INCH). ADJ WING DOOR TO FAIRED. REF MD10MM 32-14-01-2. CK'D GEAR DOOR G APS. GAPS OK. CK'D HOOK AND ROLLER CLEARANCE. CLEARANCE OK. FOUND PROX SENSOR GAP AT .230 INCH RESHIMMED TO .180 INC H. SWUNG GEAR ALL IND AND CLEARANCES OK. REF MD10MM 32-34-03-2. 2 L 7 3 4F RT A22WE 20080926 NM 2008 9 26 08FDEA03305 1 20080807 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM BS 440-680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 906FD 27148 SEAT TRACK LBL 45 STA 440-680 CORRODED AND SCALLOPS DAMAGED IN NUMEROUS LOCATIONS. FABRICATED SEAT TRACK FROM STA 440 TO 680 LBL 45.5 PER MAE TRAV NR T8/739184 AND IAW SRM 53-00-52. INSTALLED SEAT TRACK IAW SRM 51-40-02, MAYOR REPAIR. 2 L 7 2 4F RT A2NM 20080926 NM 2008 9 26 08FDEA03306 1 20080807 A 5320 WEB BOEING 757 757236 1384971 NM BS 1681-1720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 MAIN CABIN FIXED FLOOR STRUCTURE BETWEEN STA 1681.8-1720 HAS SEVERAL AREAS OF CORROSION. BLEND CORROSION IAW SRM 51-10- 02, AREAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51 PG FIG. FABRICATED REPAIR DOUBLERS IAW SRM 53-60-51. INSTALLED RE PAIR DOUBLERS IAW SRM 53-60-51 REPAIR 2 ALT 1, MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20080926 NM 2008 9 26 08FDEA03307 1 20080807 A 5310 CREASE BEAM BOEING 757 757236 1384971 NM BS 324-395 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 MAIN CABIN, CREASE BEAM INBD CHORD BS 395-BS 418 LBL 65 HAS CORROSION ALSO SEE BS 331 AT FASTENER HOLE FOR CORROSION. R EMOVED CORROSION IAW SRM 51-10-02, L=VARIOUS AREAS TOTAL 6.5'', W=1.5'', D=0.035. FOUND TO BE OUT OF LIMITS NO SRM REFE RENCE. REMOVED CREASE BEAM IAW SRM 51-40- 02, FABRICATED NEW CREASE BEAM FROM MAE TRAVELER T/8 748853. LOCATED AND DR ILLED HOLES IAW SRM 51-40-05. TREATED AND PRIMED IAW SRM 51-20-01, PAINTED IAW MM 51-20-00-7. INSTALLED CREASE BEAM IA W SRM 51-40-02, STA 324-395, (CREASE BEAM FROM BS 395-418 DELETED BY P TO F MOD, MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20080926 EU 2008 9 26 08FDEA03848 1 20080911 A 5330 A5377601720200 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 EXTERIOR UPPER FUSELAGE SPLICE DOUBLER HAS STATIC DISCHARGE AT FRAME 33 BETWEEN STRINGER 1 R AND 2 R. REMOVED AND REP LACED RIVET IAW SRM 53-10-12; FIG 220. ACCOMPLISHED A BHEC INSPECTION OF THE FASTENER HOLE IAW NTM PT6 51-10-01. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03337 1 20080808 A 5321 R532B373400000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 242 DK IS DAMAGED. REPAIRED CABIN FLOOR PANEL 241 QH BY FABRICATING A NEW PANEL USING THE OLD PANEL A S A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SKID TAPE IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03340 1 20080808 A 5321 R532B3724000100 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 242 RJ IS DAMAGED. REPAIRED CABIN FLOOR PANEL 242 RJ BY FABRICATING A NEW PANEL USING THE OLD PANEL A S A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SKID TAPE IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03341 1 20080808 A 5321 R532B360600000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 231 EF IS DAMAGED. REPAIRED CABIN FLOOR PANEL 231 EF BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MAR KED AND APPLIED NON-SKID TAPE IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 08FDEA03388 1 20080812 A 5350 6527172 FAIRING BOEING 727 7272S2F 1384O81 NM WING TO BODY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 PANEL RACK, WING BODY FAIRING 3517 AFT CORNER EXISTING COMPOSITE REPAIR IS CRACKED. REPAIRED PANEL 3517 REF SRM 51-40-9 STEP 7B(1)-7B(12) AND AMM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20080926 NM 2008 9 26 08FDEA03390 1 20080812 A 7500 65801551 DUCT BOEING 727 7272S2F 1384O81 NM BLEED AIR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 BLEED AIR EXH DUCT ON FUSELAGE ABOVE NR 1 ENG PYLON CRACKED AT AFT EDGE OF OPENING. REMOVED AND REPLACED BLEED AIR EXH DUCT ON FUSELAGE ABOVE NR 1 ENG PYLON. REF IPC 36-10-00-10 FIG 10, SRM 51-30-2 PG 13. THIS IS CLASSIFIED AS A MINOR RE PAIR. 2 L 7 3 4F A3WE 20080926 WP 2008 9 26 08FDEA03070 1 20080725 A 5730 ARC0280503 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 PANEL, LEFT WING LOWER SURFACE, FWD OF THE MLG WELL IS DELAMINATED. REMOVED AND REPLACED THE LEFT WING T/E PANEL P/N AR C 0280-503, PO 627171.3 IAW DWG ARC 0448, REV "BG" AND SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 20080926 WP 2008 9 26 08FDEA03071 1 20080725 A 5420 AUB703815 RUB STRIP DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 NR 3 PYLON PANEL 487 CL HAS BOTH FLANGES WORN. BLENDED RUB STRIPS. ORIGINAL MATERIAL 0.063. MATERIAL REMOVED 0.040. MATERIAL REMAINING 0.023. FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01; VOL I AND 54-31-01; VOL II. PRIMED RUB STRIPE IAW SRM 51-21-01; VOL II. INSTALLED RUB STRIPS IAW SRM 51-31-01; VOL II AND DWG AUB 7038, REV AC. FABRICATED RUB STRI PS IAW DWG AUB 7038, REV AC. 2 L 7 3 4F RT A22WE 20080926 EU 2008 9 26 08FDEA03529 1 20080821 A 3230 A2519903 SELECTOR VALVE AIRBUS 310 A310324 3930206 EU MLG FAILED A FDEA O OTHER J WARNING INDICATION LD LANDING 1 CE 21 804FD 4069 549 LDG GEAR DID NOT EXTEND WITH GEAR HANDLE, GRAVITY EXTENSION OK PER CREW DEBRIEF, WHEN GEAR HANDLE CYCLED THERE WAS NO AS SOCIATED AUDIABLE SOUND NORMALLY HEARD DURING GEAR EXTENSION. CREW DID NOT TRY SELECTING LDG GEAR POSITON DET SYSTEM T O "2" DURING ATTEMPTS TO EXTEND GEAR. FOUND THE LANDING GEAR SELECTOR VALVE BAD GND. REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE PER MM 32-31-12-4. ALL OPS AND LEAK CHECKS WERE NORMAL OK FOR SERVICE. 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 08FDEA03531 1 20080821 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 587FE 48489 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATIONS AT HOLES A, B, C AND D. REPAIR CARRIED OUT AT MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080926 EU 2008 9 26 08FDEA03543 1 20080822 A 5730 A5724053500339 PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 RIGHT WING LOWER T/E PANEL NR 675 CB INNER SKIN OF THE PANEL AND PANEL LAND ON THE AIRFRAME SIDE IS CHAFED WITH BARE MET AL. REPAIRED AREAS BY BLENDING CHAFFED AREAS AND BONDING A REPAIR DOUBLER IAW EA NR 6-5720-123622. ALODINED, PRIMED AN D PAINTED PER A033-600 AMM 51-23-10-0. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03286 1 20080806 A 5321 B5327027800400 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DOOR PANEL NR 252 WH, IS CRACKED AND HAS A HOLE IN THE LOWER SURFACE. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 08FDEA03932 1 20080917 A 5347 A5A7082501 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 MAIN DECK, SEAT TRACK BETWEEN STA 1521 - 5-73 LBL, 65 FOUND CORRODED. MAIN DECK CORRODED SEAT TRACK BETWEEN STA 5-0 TO 5-73 LBL 65 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS M AJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080926 NM 2008 9 26 2008UALA05691 1 20080915 A 2421 1701768 GENERATOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 1 FAULTED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 791UA 26933 LEFT BACK UP GENERATOR BLOCKED FILTER MSG ON SYNOPTIC PAGE. *S/D* FOUND GENERATOR FAULTY. REPLACED NR 1 ENGINE BACK UP GENERATOR. ALL OPS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080926 NM 2008 9 26 SWAA085001 1 20080911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727A S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085002 1 20080911 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 440 S1 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 1. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085003 1 20080911 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP P ER MM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 2008UALA03025 1 20080525 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 EMERGENCY LIGHT UPPER DECK CEILING 12AB INOP. 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 NM 2008 7 16 2008UALA03029 1 20080526 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 SEATS 6GH, 7GH, 8GH EMERGENCY LIGHTS INOP. 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 NM 2008 7 16 2008UALA03033 1 20080527 A 2797 W83931YEL22 GROUND WIRE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CONTROL UNIT SHORTED A UALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 222UA 28161 30553 SPOILERS EICAS MESSAGE DISPLAYED. OUTBOARD SPOILERS INOP. MAINT MESSAGE 27-10500 SPOILER POWER CONTROL UNIT NR 1. AFT ER EXTENSIVE TROUBLE SHOOTING AND PART REPLACEMENT. FOUND HIGH RESISTANCE SHORT TO SHIELD-GROUND. REF WDM 27-61-15 PG2 IN AREA AT RECEPTACLE D2139J. REPLACED NR 1 SPOILER CONTROL HARNESS OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080716 NE 2008 7 16 BB08098 2 20080526 A 7310 FUEL FILTER BOEING 757 7572G7 1384963 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE LEAKING A USAA A UNSCHED LANDING K W FLUID LOSS INADEQUATE Q C CL CLIMB 1 EA 19 908AW 24233 111111 PHX - FLT 432 - EN ROUTE PHX TO OGG. DURING TAKEOFF, COMPANY WITNESSES SAW FUEL MISTING FROM THE LEFT ENGINE. THE FLIG HT WAS CONTACTED AND WAS DIRECTED TO RETURN TO FIELD IN PHX. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE R EPLACED A HIGH PRESSURE FUEL FILTER ASSEMBLY ON THE LEFT ENGINE. ENGINE LEAK CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E12EU 20080716 NM 2008 7 16 SWAA082844 1 20080523 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SWAA082846 1 20080523 A 3350 D71701100 BATTERY BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 774SW 27882 DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20080716 SO 2008 7 16 RAIA00805027 1 20080525 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN OUT OF ADJUST A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 816HK 145055 PRE FLT 5584 - RIC - EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RE-ADJUSTED THE BULB. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080716 SO 2008 7 16 RAIA00805026 1 20080524 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 811HK 145256 PRE FLT 5461 - STL - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RESEATED THE CONNECTOR TO THE AFFECTED LIGHT. OPS CHECKE D GOOD. 2 L 7 2 4T RT T00011AT 20080716 NE 2008 7 16 SIMA200814903 2 20080522 A 7321 4120Y01P02 FMU GE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE NR 2 ENGINE MALFUNCTIONED A SIMA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 21 522AE 13423 1722 GEE965242 10147 GEE965242 ON FLIGHT 3689 AFTER TAKEOFF CREW REPORTED LOSS OF POWER ON ENGINE 2. CREW REPORTED THAT ENGINE 2 LOST 50 PERCENT POWER DURING CLIMB. EMERGENCY WAS DECLARED AND AIRCRAFT RETURNED TO FIELD. NO OVERWEIGHT LANDING WAS NOTED. AIRCRAFT REMOV ED FROM SERVICE. REMOVED AND REPLACED RIGHT FUEL METERING UNIT IAW CRJ-700 AMM 73-21-03. OPERATIONAL CHECK GOOD. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080716 NM 2008 7 16 USAA920081123 1 20080513 A 5320 6545834U551 INTERCOSTAL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED INTERCOSTAL, BS 328, LBL 45. REPLACED CRACKED INTERCOSTAL, BS 328, LBL 45 IAW B OEING SRM 51-10-02 & 51-40-02. 2 L 7 2 4F RT A16WE 20080716 WP 2008 7 16 DHL2008807526 1 20080514 A 5320 STIFFENER DOUG DC8 DC873F 302199F WP BS 896 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 KEEL BEAM TEE STIFFENER (EXTRUSION) HAS TWO CRACKS OF 0.250 INCH STA 896.000. REMOVED CRACKED TEE STIFFENER IAW SRM 51- 1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW STIFFENER IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE) . 2 L 7 4 4F RT 4A25 20080716 EU 2008 7 16 08FDEA02119 1 20080603 A 5330 A53980666204 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND OLD DENT ON FUSELAGE C 73-74, P 45-46 LT OUT OF LIMIT IAW SRM 53-10-12. DOUBLER REPAIR PERFORMED SRM 53-10-12 FIG 225. 2 L 7 2 4F RT A35EU 20080716 NM 2008 7 16 USAA920081135 1 20080504 A 5320 69353663 ATTACH ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK, CRACKED INTERCOSTAL UPPER ATTACH ANGLE, BS 520, BL 24 RIGHT. REPLACED CRACKED INTERCOSTA L UPPER ATTACH ANGLE, BS 520, BL 24 RIGHT IAW BOEING SRM 51-10-02. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 USAA920081131 1 20080514 A 5311 90526911 FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FRAME, BS 480, S8R - S9R. REPAIRED FRAME BS 480, S8R - S9R IAW US AIRWAYS EA 1 00441 AND 100447. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 ASAA0842990 1 20080518 A 5755 SKIN BOEING 737 737490 1384715 NM NR 6 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 NR 6 SPOILER UPPER SURFACE DENTED ABOVE INBD HINGE. PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 S RM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 USAA920081132 1 20080520 A 5330 6545778 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - CRACKED FUSELAGE SKIN, BS 927, S24L. REPAIRED FUSELAGE SKIN, BS 927, S24L IAW US AIRWA YS EA 100450. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 ASAA0842991 1 20080518 A 5753 6546486149 WEDGE BOEING 737 737490 1384715 NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 LT INBD MID FLAP TRAILING EDGE HAS NUMEROUS DENTS. PREPPED DAMAGED AREA FABRICATED AND INSTALLED REPAIR DOUBLERS IAW B7 37 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080716 WP 2008 7 16 NWAA082409858 1 20080527 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 767NC 47724 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN LIGHT FOR THE FWD LEFT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AT ROW 14 AND THE TRANSFORMER AT ROW 14-15. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A6WE 20080716 EU 2008 7 16 08FDEA02038 1 20080530 A 5210 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU PAX DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON PAX DOOR 4 LT BOTTOM SEALING SECTION REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080716 EU 2008 7 16 08FDEA02057 1 20080519 A 5347 SEAT TRACK AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DEFORMED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 CABIN FLOOR, DEFORMATION ON SEAT-TRACK Y1959 BETWEEN FR 20 AND 21. 2 L 7 2 4F RT A35EU 20080716 NM 2008 7 16 UPS08552370 1 20080518 A 5330 707576511125 SKIN BOEING 757 75724APF 1384969 NM BS 1280 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 436UP 25467 INSPECTION TYPE:C LIGHTNING STRIKE AT FUSELAGE EXTERNAL SURFACE APPROX STA 1280, S2R. REMOVED 1EA RIVET IAW SRM 51-40-0 1 F 2. ENLARGED HOLE 0 UP TO .250 IAW SRM 53-00-01-2R6 SECTION II PARAGRAPH 3 3. HFEC IAW NTM 51-00-00 PT.6 FIG23. FO UND CRACK INDICATION RADIATING FROM HOLE MARKED END. 2 L 7 2 4F RT A2NM 20080716 NM 2008 7 16 GTIA0800066 1 20080425 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 505NK 2485 AFT FUSELAGE FLOORBEAM CORRODED AT Y254 BETWEEN FR66 AND FR68. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 20080716 NM 2008 7 16 GTIA0800068 1 20080425 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 505NK 2485 FOUND CORROSION ON FLOORBEAM AT Y765 BETWEEN FR66 AND FR70. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 20080716 NM 2008 7 16 GTIA0800069 1 20080425 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 505NK 2485 FOUND CORROSION ON FLOORBEAM AT Y1292 BETWEEN FR66 AND FR68. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 20080716 EU 2008 7 16 08FDEA02039 1 20080530 A 5320 A53832100208 WEB AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CRACKS ON INTERNAL WEB BETWEEN BEAM 1 AND 2 LT/RT. REPAIR PERFORMED BY CRACK STOP HOLE AND DOUBLER INSTALLATION I AW RAS 70507081/004/2008, APPROVED BY EA 6-5315-120051 2 L 7 2 4F RT A35EU 20080716 NM 2008 7 16 08FDEA02132 1 20080603 A 5310 69471112 BEAM BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 DELTA BEAM INTERIOR RT LOWER CHORD AT BS 747 - 749, RBL 5, IS CORRODED ON INNER SURFACE AT AND AROUND SPLICE. BLENDED C ORROSION AT LOWER, FWD CHORD. FOUND TO BE OUT OF LIMITS, REF DWG 69-47111. REPLACED CHORD REF DWG 65-47111. THIS IS C LASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080716 NM 2008 7 16 USAA920081149 1 20080515 A 5754 65C26603101 SKIN BOEING 737 7374B7 1384702 NM NR 3 SLAT LT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - NR 03C30257009/ 9, LEFT WING NR 3 SLAT UPPER SURFACE INBOARD END HAS DELAMINATION. REPA IRED LEFT WING NR 3 SLAT UPPER SURFACE INBOARD END IAW B737 SRM 57-43-02 AND 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 USAA920081150 1 20080523 A 5210 SKIN BOEING 737 7374B7 1384702 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - NR O3C10552004/1, O3C10552004/2 AND O3C10552004/3, FORWARD ENTRY DOOR INNER SKIN CRACKED AT THE NR 5, NR 6 AND NR 7 DOOR STOP CUT OUT AREA. REPAIRED THE FORWARD ENTRY DOOR INNER SKIN CRACKED AT THE NR 5, NR 6 AND NR 7 DOOR STOP CUT OUT AREA IAW US AIRWAYS EA 100459. 2 L 7 2 4F RT A16WE 20080716 WP 2008 7 16 DHL2008807525 1 20080519 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 300 L26L CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 FWD CARGO COMPT FITTING CRACKED STA 300.000 L-26L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1 -11, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 2008UALA02853 1 20080518 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 513UA 24810 EMERGENCY AISLE LIGHT BELOW STOW BIN AT SEATS 11 ABC INOP. SUPPLEMENTAL DATA UPDATE CAUSE, LAMP INOP. RELAMPED, OPS CH ECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080716 NM 2008 7 16 2008UALA03042 1 20080527 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1219 S37-38L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 656UA 25394 FRAME WEB AT STA 1219 BETWEEN STR 37 TO 38L HAS AN ELONGATED FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED, CUTOUT DAMAGE. INSTALLED NEW SHEARTIE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080716 NM 2008 7 16 DHL2008764535 1 20080522 A 5312 BULKHEAD BOEING 727 727264 138408M NM BS 870 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 CRACK INDICATION AT BS 870 IN RT W/WELL AT APU LOAD CONTROL VALVE CUT-OUT. TRIMMED OUT CRACKED MATERIAL, FABRICATED REP AIR PARTS, AND INSTALLED REPAIR AT BS 870 BULKHEAD PER B727 SRM 53-10-9 FIG 5, 51-10-6, 51-10-1, AND NDTM PT6, 51-00-00 FIG 23. 2 L 7 3 4F A3WE 20080716 WP 2008 7 16 IXXA08SMN130S 1 20080411 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 167 L21R MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIRS LOCATED AT STATION FS 167 LONGERON 21.5 RIGHT. REMOVED FASTEN ERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, INTERNAL D OUBLER, AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC 8 SRM 53-2-1 FIGURE 7 SHEETS 1 AND 5, DC8 SRM 51-1-21, 51-1-20D, DC8 SRM 53-4-1 FIGURE 1 ITEM "D", DC8 SRM 51-1-8B, 51-1 -11, AND 51-3-1. 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 2008UALA02870 1 20080518 A 5210 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 3R NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 535UA 25130 DOOR 3R ARM LIGHT WILL NOT ILLUMINATE. SUPPLEMENTAL DATA UPDATE CAUSE, DEBRIS UNDER GIRT BAR. REMOVED DEBRIS AND CLEAN ED SWITCHES, OPS CHECKS OK, ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080716 WP 2008 7 16 IXXA08SMN158S 1 20080418 A 5753 SKIN DOUG DC8 DC871F 302199D WP LT WING TE FLAP WORN B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION; FOUND LEFT INBOARD FLAP UPPER SKIN WORN AT STATION XW 104.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART S. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 1 ITEM "D", DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-2 1, DC8 SRM 51-1-8B, AND DC8 SRM 51-1-11. 2 L 7 4 4F RT 4A25 20080716 2008 7 16 SIMA200815101 3 20080528 A 6110 PROPELLER SAAB SF340 340B 7860101 EU NR 1 MALFUNCTIONED A SIMA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 21 263AE 340B263 ON FLIGHT 3204 ON ABORTED TAKEOFF AT 100 KTS, NR 1 ENGINE PROP RPM GAUGE WENT TO 1440 RPM, DURING ABORT POWER LEVERS TO FLIGHT IDLE NR 1 PROP RPM STAYED ABOVE 1300 RPM FOR AT LEAST 3 SECONDS. 2 L 7 2 4T RT A52EU 20080716 SO 2008 7 16 LR7A08083 1 20080611 A 3243 23410 VALVE LKHEED 382 382G 526414U SO LT BRAKE FAILED A LR7A D RETURN TO BLOCK A FLAME/FIRE TX TAXI/GRND HDL 1 AL 03 406LC 6399 4676 RETURNING TO BLOCK AFTER TAXI FOR ENGINE MAINTENANCE GROUND RUNS, LT FWD AND AFT BRAKES NOTED AS VERY HOT, SUBSEQUENTLY LT FWD BRAKE CAUGHT FIRE AND WAS QUICKLY EXTINGUISHED BY GROUND CREW. C/W LAC JOB CARD HN32144, REPLACED LT BRAKE CONTR OL VALVE (SUSPECTED DISCREPANT PART), LT FWD AND AFT BRAKES, WHEELS AND TIRES. ALSO REPLACED LT NORMAL AND EMERGENCY BR AKE HOSES, SHUTTLE VALVES, BRAKE FUSES AND SWIVELS PRECAUTIONARY. BRAKE BLEED AND LEAK CHECK IAW SMP581 29-00 LOG PAGE 27338 ITEM M3 THR M19 BRAKE CONTROL VALVE SENT TO VENDOR FOR TEAR-DOWN AND INSPECTION. 2 H 7 4 4T A1SO 20080716 SO 2008 7 16 LR7A08081 1 20080608 A 2897 CONNECTOR LKHEED 382 382G 526414U SO CROSSFEED VALVE CORRODED A LR7A O OTHER J WARNING INDICATION CR CRUISE 1 AL 03 403LC 4590 DURING CRUISE FLIGHT, NR 2 CROSSFEED VALVE FAILED IN THE CLOSED POSITION. NR 2 CROSSFEED VALVE SUBSEQUENTLY DEFERRED IA W MEL 28-4 CAT "C" DEFERRAL SP NR 2 COMPLIED WITH. CROSSFEED VALVE ELECTRICAL PLUG REMOVED AND BAGGED. VALVE OPENED MA NUALLY AND LOCKWIRED IN THE OPEN POSITION ON LOG PAGE 27022, ITEM 2. WILL UPDATE COMPONENT INFORMATION WHEN IT BECOMES AVAILABLE. UPDATED INFORMATION IS AS FOLLOWS, FOUND CORRODED WIRE EYE TERMINAL AT POSITION "9" TB42B. REPAIR AND OPS C HECK IAW SMP581 28-22, LOG PAGE 28526 ITEM M1. 2 H 7 4 4T A1SO 20080715 NM 2008 7 15 UPS08B52377 1 20080327 A 5311 FRAME BOEING 747 747400 13848AT NM BS 1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 747400 INSPECTION TYPE:C RT BS 1160 TENSION TIE FRAME WEB CRACKED ABOUT .250 INCH. RT BS1160 TENSION TIE FRAME WEB REPLACED PE R SRM 53-40-07. REPAIR 3. 2 L 7 4 4F RT A20WE 20080715 NM 2008 7 15 AALA200801282 1 20080512 A 3350 1000679 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 329AA 22329 LAX - EMERGENCY LIGHT IN COCKPIT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT IN COCKPIT. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20080922 NM 2008 9 22 SWAA084912 1 20080907 A 5311 65C22909 FRAME BOEING 737 7373T0 1384582 NM BS 500C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084913 1 20080907 A 5311 6546595 FRAME BOEING 737 7373T0 1384582 NM BS 727A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084918 1 20080907 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 360 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084919 1 20080907 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 291.5 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 291.5, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER S RM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084920 1 20080907 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 360 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084921 1 20080907 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 360 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084837 1 20080903 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 727E S23L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER 23L CORRODED AT BS 727E. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085008 1 20080911 A 5322 69353656 SHEAR TIE BOEING 737 7373Y0 1384671 NM BS 360 S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CORRODED AT BS 360, STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085009 1 20080911 A 3350 3071BPEGPL LAMP BOEING 737 7373A4 1384585 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 2 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085010 1 20080911 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085055 1 20080914 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 767 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080926 EU 2008 9 26 2008UALA05694 1 20080913 A 5753 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT WING TE FLAP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 471UA 1432 LEFT OUTBOARD FLAP 12 INCHES LONG BY 5 INCHES WIDTH BY THREE EIGHTS INCH DEEP. APPROXIMATELY 13FT 3 INCHES FROM O/B EDG E OF O/B END OF FLAP. REPLACED LT OTBD FLAP. COMPLETED INSP OF FLAP INSTALLATION, ADJUSTMENT AND OPS. 2 L 7 2 4F 4 F RT A28NM E40NE 20080926 NM 2008 9 26 2008UALA05697 1 20080914 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 324 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 MAIN CABIN T-CAP AT BS 324, RBL 58, IS CORRODED BEYOND LIMITS. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTI ON OF T-CAP. FABRICATED & INSTALLED A NEW REPAIR SECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 20080926 NM 2008 9 26 SWAA085056 1 20080914 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 500A S24R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 24R. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085061 1 20080914 A 5311 65C25228 FRAME BOEING 737 7373H4 1384600 NM BS 727B S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085062 1 20080914 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM BS 500C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083270 1 20080617 A 5320 6517852 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17, WL 226. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083271 1 20080617 A 5320 6517852 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17, WL 226. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080716 WP 2008 7 16 IXXA08SMN149S 1 20080418 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 310 L22L MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR LOCATED AT STATION FS 310 LONGERON 22 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXITING REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, INTERNAL FINGER DOUBLER, AND FILLER. CLEANED TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW D C8 SRM 53-2-1 FIGURE 7 SHEETS 1 AND 5, 51-9-0 FIGURE 68A, 53-4-1 FIGURE ITEM "B", 51-1-11, 51-3-1, DC8 SRM 51-1-21, 51-1 -20D, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 2008UALA02900 1 20080519 A 2121 FILTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COOLING FAN DIRTY A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 547UA 25368 EQUIP COOLING OVHT LT ON OVH PANEL AND FWD EICAS ILLUM INTERMITTENT. SUPPLEMENTAL DATA UPDATE CAUSE, EQ COOLING FAN FIL TER DIRTY. REPLACED EQ COOLING FAN FILTER, OPS ARE NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080716 NM 2008 7 16 F3LA200800280 1 20080528 A 5754 D5757420200000 SKIN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE LT LE FLAP PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 921FR 2010 DURING WALK AROUND MAINTENANCE NOTED A BIRD STRIKE ON THE LEFT OUTBOARD LEADING EDGE FLAP APPROXIMATELY SIX FEET FROM OU TBOARD END OF FLAP. ENGINE PARAMETERS WERE REPORTED NORMAL BY THE PILOT. MAINTENANCE REPAIRED THE LEFT OUTBOARD FLAP L EADING EDGE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 57-53-00 FIGURE 202. UPON COMPLETION OF THE REPAIR IT WAS INSPEC TED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080716 NM 2008 7 16 2008UALA03068 1 20080529 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 992 S14L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 FUSELAGE SKIN KINKED JUST BELOW STR 14L LAP JOINT, AFT OF STA 992. MAJOR REPAIR ACCOMPLISHED, REPLACED FUSELAGE SKIN. 2 L 7 2 4F 4 F RT A16WE E2GL 20080716 WP 2008 7 16 DHL2008807524 1 20080504 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 420 MISREPAIRED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 807DH 91019 45990 REMOVED AND REPLACED EXISTING REPAIR AT FUSELAGE STA 420 LT SIDE L-27L TO L-28L WITH PERMANENT TYPE REPAIR PER SRM, INDI CATE TYPE OF REPAIR REINSPECTION INTERVAL AND NEXT REQUIRED INSPECTION (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 5 3-2-1 FIG 7 SHEET 1-4. REMOVED EXISTING REPAIR NOT ACCORDING TO SRM IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SEC TION AND FABRICATED REPAIR DOUBLER (AL7075T6 0.090") FILLER (AL7075T6 0.080") AND (2EA) INTERNAL FINGER DOUBLER (AL7075T 6 0.050") IAW SRM 53-2-1 FIG 7 SHEET 1, 4, SRM 53-4-1 FIG 4 ITEM "F". CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIG 7 SHEET 1, 4, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE 2 L 7 4 4F RT 4A25 20080716 WP 2008 7 16 IXXA080023O 1 20080528 A 2697 TERMINAL DOUG DC8 DC871F 302199D WP FIRE LOOP DEFECTIVE A IXXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 11 820BX 90488 1409 46065 DURING CLIMB FROM KSJC TO KRFD NUMBER ONE ENGINE FIRE WARNING LIGHT AND BELL CAME ON INTERMITTENTLY. ALL ENGINE INSTRUM ENT INDICATIONS WERE NORMAL. WHEN THROTTLE WAS REDUCED TO IDLE FIRE INDICATION CAME BACK AND SILENCED ON IT'S OWN. THE CREW RAN THE QRH CHECKLIST WITH NO OTHER INDICATION. THE CREW RETURNED TO KSJC AND LANDED WITHOUT INCIDENT. MAINTENAN CE INSPECTED THE FIRE WARNING SYSTEM AND FOUND THE FORWARD LEFT HAND LOWER FIRE LOOP GROUND CONNECTION BAD. MAINTENANCE SPLICED ON A NEW GROUND TERMINAL AND CLEANED THE FIRE LOOP CONNECTOR. MAINTENANCE PERFORMED A SHAKEDOWN TEST OF ALL FI RE LOOPS AND CONNECTORS, NO FURTHER DEFECTS WERE NOTED IAW UAL MAINTENANCE MANUAL 26-11-02 AND 26-11-07. AIRCRAFT WAS R 2 L 7 4 4F RT 4A25 20080716 SO 2008 7 16 C2XA08CL065 1 20080601 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN SMOKE A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14972 145151 YQB FLIGHT 2128 - THE CREW REPORTED PACK 2 PRODUCES SMOKE IN CABIN WHEN TURNED ON. THE AIRCRAFT RETURNED TO THE GATE WI THOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE PACK SYSTEM IN BOTH MANUAL AND AU TO USING THE APU AND ENGINE BLEED. NO SMOKE WAS DETECTED AND ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEAS ED FOR SERVICE. 2 L 7 2 4T RT T00011AT 20080716 NM 2008 7 16 ZZDA2008119 1 20080611 A 3260 SENSOR BOEING 717 717200 1383700 NM MLG UNKNOWN A ZZDA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 37 952AT 55014 DURING TAKEOFF ROLL AT ROTATION, FELT RIGHT SIDE SHIMMY. AFTER LIFT OFF, GOT A RIGHT GEAR UNSAFE INDICATION RED LIGHT O N COCKPIT AND CONFIG SYNOPTIC ALONG WITH PSEU FAIL ALERT. RIGHT ENGINE N1 VIBRATION ALERT AT 5.0. DECLARED EMERGENCY A ND AIR RETURNED TO TPA. FOUND NR 3 TIRE BLOWN. REMOVED AND REPLACED NR 3 AND 4 TIRES. BOROSCOPED NR 2 ENGINE AND PERF ORMED ENGINE RUN. NO DEFECTS FOUND. ALL INDICATIONS NORMAL. REMOVED AND REPLACED RIGHT MLG DOWN AND LOCK SENSORS AND CONDUITS. PERFORMED GEAR SWINGS. ALL FUNCTIONS CHECK GOOD. REF NRWC'S N072076 AND N066367 FOR ALL WORK PERFORMED AND SIGNATURES. 2 L 7 2 4F TR A6WE 20080716 NM 2008 7 16 ZZDA2008116 1 20080602 A 5311 FRAME BOEING 717 717200 1383700 NM BS 1178 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 892AT 55044 AFT FUSELAGE INT TAIL AREA FOUND CRACK AT CANTED FRAME RT AREA STA 1178.225 BETWEEN STA 16R AND 17R. INSTALLED FORMER A NGLE REPAIR PER SRM 51-70-11 FIG 201. 2 L 7 2 4F TR A6WE 20080716 NM 2008 7 16 UPS08B52400 1 20080417 A 5320 65B09631344 FILLER BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:BCF BS 1140 LT TENSION TIE UPPER & LWR CLIP FILLER CRACKED. BS 1140 LT TENSION TIE UPPER & LWR CLIP FIL LER REPLACED PER SRM 53-40-30 F FIG 201. 2 L 7 4 4F RT A20WE 20080716 SO 2008 7 16 C2XA08CL063 1 20080529 A 3320 BR90002 BALLAST EMB 145 EMB145EP 3260221 SO LAVATORY LIGHT FAULTY A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 17928 145007 CLE FLIGHT NR 2401, THE CREW REPORTED A STRONG BURNING SMELL COMING FROM THE LAVATORY. MAINTENANCE INSPECTED AND REPLAC ED THE LAV LIGHT BALLAST. 2 L 7 2 4F RT T00011AT 20080716 EA 2008 7 16 MASA200800434 1 20080530 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37342 7342 ASH FLT 1019, HNL-ITO. PAX DOOR OUTER HANDLE WILL NOT STOW IN. PERFORMED OP CHECKS, OP CHECKS ARE NORMAL. 2 L 7 2 4F RT A21EA 20080716 EA 2008 7 16 MASA200800441 1 20080531 A 2520 72710223 LATCH CNDAIR CL600 CL6002B19 1900309 EA FWD WARDROBE BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 649BR 7414 ASH FLT 7175 ATL-OVERNIGHT. FWD WARDROBE DOOR WOULD NOT OPEN AND A FIRE EXTINGUISHER AND A PBE ARE INSIDE. FOUND LATCH BROKEN. REPLACED LATCH. 2 L 7 2 4F RT A21EA 20080716 NM 2008 7 16 SWAA082921 1 20080601 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 15L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SWAA082922 1 20080530 A 5755 654645165A SKIN BOEING 737 737317 138447P NM NR 6 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED C2 CHECK, FOUND RT WING NR 6 SPOILER UPPER SURFACE DELAMINATED AT INBOARD END. REMOVED AND REPLACED SP OILER PER MM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SWAA082931 1 20080530 A 5313 BAC1498 STRINGER BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 767SW 29807 DURING SCHEDULED 8Y CHECK, FOUND STRINGER 5R CRACKED AT BS 332. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 2008UALA03474 1 20080619 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY EEL LIGHT BROKEN OFF SEAT 55C. REPLACED EEL LIGHT ASSY. OP CHECKED OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080718 NM 2008 7 18 SWAA083547 1 20080626 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083548 1 20080626 A 5330 6518420 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259.5, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083551 1 20080626 A 5310 6546818 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 950 TO BS 955, RBL 50. REMOVED AND REPLACED WEB PER S RM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843361 1 20080803 A 5320 65C334951 WEB BOEING 737 7374Q8 138447Q NM BS 1025-1029 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 AFT CABIN FLOOR WEB UNDER G4 GALLEY CORRODED STA 1025 TO STA 1029 LBL 10 TO LBL 17 AREA. CUT OUT DAMAGED AREA, FABRICAT ED FILLER AND DOUBLER, LOCATED, DRILLED AND INSTALLED IAW B737 400 SRM 51 70 13 FIG 1. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843369 1 20080722 A 5315 6545833212 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM BS 270 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 FLIGHT DECK FLOOR SUPPORT CORRODED AT STA 270 LBL 11 INCHES TO RBL 11 INCHES. REMOVED CORRODED FLOOR SUPPORT, FABRICATE D, LOCATED, DRILLED AND INSTALLED A NEW FLOOR SUPPORT IAW B737 400 SRM 51 40 05 FIG 6. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843359 1 20080716 A 5330 65C3235719 SKIN BOEING 737 7374Q8 138447Q NM BS 363-375 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 EXTERNAL FUSELAGE STA 368 DENTED WITHIN 3 INCHES OF LAP SPLICE BETWEEN STR 18R AND 19R. CUT OUT DAMAGED AREA OF SKIN, H FEC AND MFEC INSPECTED AREA, NO DEFECTS NOTED, FABRICATED FILLERS AND DOUBLER, LOCATED, DRILLED & INSTALLED IAW B737 400 SRM 53 00 01 DETAIL XXIX . 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843364 1 20080723 A 5322 SHEAR TIE BOEING 737 7374Q8 138447Q NM BS 727G S25-26L CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 SHEAR TIE CORRODED AT STA 727G FROM STRINGER 25L TO 26L. REMOVED CORRODED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE IAW B737 400 SRM 53 00 07. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843357 1 20080717 A 5753 65C26603101A SKIN BOEING 737 7374Q8 138447Q NM LT WING TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 LT WING NR 3 L/E SLAT I/B LWR SURFACE OF T/E WEDGE CHAFED. REMOVED DAMAGED AREA OF SKIN, FABRICATED REPAIR PARTS AND DO UBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843351 1 20080717 A 5753 6546430130 SKIN BOEING 737 7374Q8 138447Q NM RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 RT WING I/B TRAILING EDGE FOREFLAP HAS MULTIPLE DENTS ON LOWER SURFACE I/B AREA. PREPARED DAMAGED AREA, APPLIED ADHESIV E FILLER, FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843366 1 20080717 A 5753 6546430131 SKIN BOEING 737 7374Q8 138447Q NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 LT WING TRAILING EDGE I/B FORE FLAP SEVERAL DENTS ON LOWER SURFACE CENTER I/B AREAS. REMOVED DAMAGED DOUBLERS AND SKINS , FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843367 1 20080717 A 5755 654645262A SKIN BOEING 737 7374Q8 138447Q NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 RT WING NR 5 SPOILER UPPER SURFACE DENTED AT 8 INCHES FROM TRAILING EDGE AND 2.5 FROM O/B EDGE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BONDED IAW B747 400 SRM 51 70 10 PAGES 201 203 REPAIR 2. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843376 1 20080717 A 5753 65C263108 WEDGE BOEING 737 7374Q8 138447Q NM RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 RIGHT I/B MID FLAP LOWER SURFACE OF TRAILING EDGE WEDGE DENTED JUST O/B OF NR 3 TRACK. PREPARED DAMAGED AREA, FABRICATE D REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51 70 10. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843394 1 20080717 A 5754 65C26603192A SKIN BOEING 737 7374Q8 138447Q NM NR 4 SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 RT WING NR 4 2 E SLAT LOWER TRAILING EDGE WEDGE CHAFED. PREPARED DAMAGED AREA, FABRICATED FILLERS AND DOUBLERS AND BOND ED IAW SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080923 NM 2008 9 23 2008UALA05510 1 20080828 A 2520 SEAT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROW 13 UNSECURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 579UA 26697 F/A REPORTS ROW 13 SEATS D, E, F ARE NOT SECURE TO FLOOR. SECURED SEAT TO TRACK. NO RECENT MTX ACTIVITY IN THIS AREA F OR THIS A/C. 2 L 7 2 4F 4 F RT A2NM E17NE 20080923 NM 2008 9 23 2008UALA05481 1 20080825 A 2432 284N14098 CHARGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MAIN BATTERY FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 549UA 25397 STATUS MESSAGE MAIN BATTERY CHARGER ON. FOUND MAIN BATTERY CHARGER FAILING. REPLACED MAIN SHIPS BATTERY CHARGER. 2 L 7 2 4F 4 F RT A2NM E17NE 20080923 NM 2008 9 23 08FDEA03396 1 20080813 A 5330 65545754 LAP JOINT BOEING 727 727233 138408A NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 SKIN GOUGED RIGHT FUSELAGE LAP SEAM FWD OF STA 720E AT STR 19R. CUTOUT DAMAGED AREA DIMS 3 INCH BY 4 1/2 INCH IAW SRM 5 3-30-3. FABRICATED DOUBLER, FABRICATED REPAIR FILLER IAW SRM 53-30-3 FIG 14. TREATED AND PRIMED REPAIR PARTS IAW SRM 5 1-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 20080923 EU 2008 9 23 08FDEA03397 1 20080813 A 5712 A5796005920100 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 RIGHT WING INBD FLAP NOSE RIB NR 5 IS CRACKED AT RIVET HOLE. FABRICATED REPAIR DOUBLER REF SRM 57-50-00; PG 204. ALODI NED AND PRIMED REF AMM 51-22-00-0; PG 1. INSTALLED REF SRM 51-40-21; PG 7. 2 L 7 2 4F RT A35EU 20080923 WP 2008 9 23 08FDEA03398 1 20080813 A 5312 BULKHEAD DOUG MD10 MD1010F 3022112 WP MLG WW CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 THE CENTER WHEEL WELL SKIN HAS VARIOUS AREAS OF CORROSION FROM STA 1521 THRU 1380; BETWEEN LONGERON 51L TO LONGERON 51R. REPAIRED THE CENTER WHEEL WELL SKIN IAW FEDEX EA 8-5330-117008 " FUSELAGE, UNDER WING BARREL BELLY SKIN CORROSION, REP AIR". REMOVED AND REPLACED LONGERONS L-52 AND L-51L; INTERCOSTALS AT STA 1501 - 1521 AND THE LONGERON END FITTINGS IAW DC/MD-10 SRM 51-31-01; VOL II AND SRM 51-33-01; VOL II. ALODINED; PRIMED AND PAINTED IAW DC/MD-10 SRM 51-21-01; VOL II. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 08FDEA03088 1 20080725 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 577FE 48469 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON EXISTING 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES B, C AND D. MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES B, C, AND D BUSHING REPAI R CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL 1. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 DL76G081139 1 20080902 A 2751 TRANSMITTER BOEING 767 767332 1382001 NM TE FLAP POSITION MALFUNCTIONED A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 16065 30199 TRAILING EDGE FLAPS SHUTDOWN. REMOVED AND REPLACED NR 4 FLAP POSITION TRANSMITTER PER AMM. 2 L 7 2 4F RT A1NM 20080924 NM 2008 9 24 DL76P081142 1 20080903 A 5343 TRUNNION BOEING 767 767332 1382001 NM NLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 143DA 25991 RT NLG TRUNNION FITTING BORE CORRODED. BORE MACHINED OVERSIZED TO REMOVE CORROSION AND AN OVERSIZED REPAIR BUSHING WAS INSTALLED. 2 L 7 2 4F RT A1NM 20080924 NM 2008 9 24 DL76G081144 1 20080903 A 5270 WARNING LIGHT BOEING 767 767332 1382001 NM L1 DOOR FALSE ACTIVATION A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 1605 30198 1L DOOR SLIDE FLASHING. UNABLE TO RESET, NTF CYCLED DOOR SEVERAL TIMES. DOOR SLIDE LIGHT STAYED ON STEADY, INSP DOOR P ROX SENSOR. NO DAMAGE. DOOR SLIDE ARMED LIGHT CK GOOD. 2 L 7 2 4F RT A1NM 20080924 NM 2008 9 24 DL76L081145 1 20080416 A 3350 SIGN BOEING 767 767332 1382001 NM EMERGENCY LIGHT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 EMERGENCY EXIT LIGHT FWD OR R1 DOOR IS CRACKED. REMOVED AND REPLACED EMERGENCY EXIT SIGN AT R1 DOOR. OPERATIONALLY CHE CKS GOOD IAW B767-300 MM 33-51-01-402-026. 2 L 7 2 4F RT A1NM 20080924 NM 2008 9 24 DL76L081146 1 20080416 A 3350 SIGN BOEING 767 767332 1382001 NM EMERGENCY LIGHT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 L2 DOOR UPPER EXIT SIGN AND L2 EXIT THRESHOLD EXIT SIGN HAS BROKEN HOUSING AND LENS. REMOVED AND REPLACED L2 DOOR UPPER EXIT SIGN, OPS CHECKS GOOD IN ACCORDANCE WITH B767-300 MM 33-51-01. 2 L 7 2 4F RT A1NM 20080924 NM 2008 9 24 DL76L081147 1 20080821 A 3397 CONNECTOR BOEING 767 767332 1382001 NM EMERGENCY LIGHT BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 EMERGENCY SEAT LIGHT CONNECTOR BROKEN AT SEAT 28 RIGHT. REMOVED AND REPLACED CONNECTOR AT SEAT 28 RIGHT, EELS LIGHT OPE RATIONALLY CHECKS GOOD IAW B767-300 MM 33-51-10. 2 L 7 2 4F RT A1NM 20080924 WP 2008 9 24 08FDEA03528 1 20080821 A 5313 AYB70202 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 LONGERON 51 L RIGHT END FITTING AT STA 1521 IS CORRODED. FABRICATED 1 LONGERON 51 L END FITTING P/N AYB 7020-2 IAW DWG NR AYB 7020. 2 L 7 3 4F RT A22WE 20080924 EA 2008 9 24 SWIA200820046 1 20080908 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 944SW 7764 FLT 6504-8, LEFT SIDE EXIT ROW, GREEN EMERGENCY EXIT LIGHT BURNED OUT. RECONNECTED LOOSE CONNECTOR. 2 L 7 2 4F RT A21EA 20080924 NM 2008 9 24 DLM8K081153 1 20080902 A 5330 59114065 SKIN DOUG MD88 MD88 3023688 NM FS 206 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DE 53419 FUSELAGE SKIN GOUGED NEAR FS 206 AND L-6L. DAMAGE CUT OUT AND REPAIR DOUBLER INSTALLED PER ERA 470387-14 AND SRM 53-04 FIG 12B. 2 L 7 2 4F RT A6WE 20080922 NM 2008 9 22 ASAA0843377 1 20080719 A 5315 65C3394311 FLOORBEAM BOEING 737 7374Q8 138447Q NM BS 344 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 FLOORBEAM UPPER CHORD CORRODED STA 344 CENTER AREA TO LBL 35. REMOVED DAMAGED CHORD, FABRICATED UPPER CHORD AND REPAIR PARTS, LOCATED DRILLED AND INSTALLED IAW ASA EA 5310 02811 AND AAR EA 12804. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843350 1 20080719 A 5315 65C3394116 FLOORBEAM BOEING 737 7374Q8 138447Q NM BS 312 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 CABIN FLOORBEAM STA 312 SEVERAL AREAS OF CORROSION ON CAP RBL 32 TO LBL 27. REMOVED DAMAGED UPPER CHORD, FABRICATED UPP ER CHORD AND REPAIR SPLICES, LOCATED DRILLED AND INSTALLED IAW B737 400 SRM 53 10 51 REPAIR 5 PAGE 203 FIG 201. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843358 1 20080724 A 5320 654769012 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM BS 727G-767 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 AFT CARGO PIT FLOOR SUPPORT CORRODED STA 727G TO STA 767. REMOVED DAMAGED ZEE ANGLE, LOCATED DRILLED AND INSTALLED A RE PLACEMENT ANGLE IAW B737 400 SRM 51 40 02 PG 2 AND 51 40 05 PG 3. 2 L 7 2 4F RT A16WE 20080923 NM 2008 9 23 DL757081182 1 20080908 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1700 S15L DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 FOUND SKIN DAMAGED AT STATION 1700 STRINGER 15L. REPAIR INSTALLED PER SRM 53-00-01. 2 L 7 2 4F RT A2NM 20080923 NM 2008 9 23 DL757081184 1 20080907 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 1640 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 CABIN FLOOR BEAM UPPER CAP REQUIRES REPLACEMENT AT STA 1640 REPLACED CABIN FLOOR BEAM 2 L 7 2 4F RT A2NM 20080923 NM 2008 9 23 2008UALA05525 1 20080828 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CABIN INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 EEL LIGHT STRIP FOR SEAT ROWS 1 AND 2 IS INOP. FOUND FAULTY LAMP STRIP. REPLACED EEL STRIP BETWEEN ROW 1 AND 2. OP CK S GOOD. AC OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20080923 NM 2008 9 23 2008UALA05523 1 20080828 A 2497 GROUND WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HEATER TAPE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 BARE WIRE EXPOSED AT TOP LEFT BURNDY BLOCK CONNECTION, HEATER TAPE GROUND, APPROX LOCATION AFT SIDE OF FLOORBEAM STA 266 .5, LBL 68. REPLACED B97 HEATER TAPE GROUND WIRE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080718 NM 2008 7 18 SWAA083605 1 20080629 A 5311 6546533 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 08FDEA02356 1 20080620 A 5312 A53981860208 BULKHEAD AIRBUS 310 A310203 3930313 EU ZONE 100 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS REPAIR LOCATED AT FRAME 80/82 AFT PRESSURE BULKHEAD FORWARD SIDE CIRCUMFERENTIAL STRAP AND FRAME WEB REPAIR BET WEEN STR 48 LT AND 48 RT WITH 2 EA FRAME WEB REPAIR PLATES, 2 CIRCUMFERENTIAL REPAIR SPLICE STRAPS AND 1 CIRCUMFERENTIAL REPAIR SECTION REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS INSTALLED LOCK FASTENER COLLARS ON REPAIR AT FR 80/ 82 BETWEEN STR 48 LT TO STR 48 RT CIRCUMFERENTIAL STRAP AND INSTALLED CORRECT COLLARS IAW FEDEX EA 6-5310-121308, RELE ASE DATE 18 JUNE, 2008. THIS IS AN AIRBUS REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080718 EU 2008 7 18 08FDEA02152 1 20080604 A 5753 SKIN AIRBUS 310 A310203 3930313 EU ZONE 600 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RT WING OUTBD FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB 10 AND RIB 11 AND 1.1 IN FWD OF REAR SPAR MEASURING 4.8 INCH BY 10.5 INCH REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR A ND INSTALLED CORRECT OUTER SKIN REPAIR ON RT WING OUTBD FLAP UPPER SKIN BETWEEN RIB NR 10 AND RIB NR 11 IAW A310-200 SRM 57-53-10, FIG 210. THIS IS AN AIRBUS REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 08FDEA02112 1 20080603 A 5100 NONE DOUG MD11 MD11F 3023600 NM IAW SDR NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 LEFT WING LEADING EDGE AT APPROX STA XOS 484 TO XOS 549 FOUND EXISTING REPAIR. LEFT WING LEADING EDGE AT APPROX STA X OS 484 TO XOS 549 EXISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 7 VOLUME I FEDE X EO NR 1- 5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG - MD11, REPAIR CATALOG AND TRACKING REQUIREMENTS 14 CFR 121.707, HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 SWAA083614 1 20080629 A 5754 65C26601 SLAT BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083613 1 20080629 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 18L CRACKED AT BS 787. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083577 1 20080629 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT FWD END. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083576 1 20080629 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663, BL 0. REPAIRED BEAM PER ER. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083556 1 20080626 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083580 1 20080628 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 EEPLS LENS MISSING AT ROW 12 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080718 2008 7 18 SWAA083581 4 20080629 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 444WN 29839 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080718 2008 7 18 SWAA083582 4 20080627 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 469WN 33859 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083557 1 20080626 A 3350 100031 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 475WN 32474 DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM . 2 L 7 2 4F RT A16WE 20080718 2008 7 18 SWAA083583 4 20080629 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 491WN 33867 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083588 1 20080629 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 482, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083559 1 20080626 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080923 NM 2008 9 23 2008UALA05522 1 20080829 A 3350 60243 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAVATORY INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 558UA 26654 AFT LAV FLOOR EEL LIGHT INOP. REPLACED LIGHT ASSY. CHECKED OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080923 NM 2008 9 23 2008UALA05456 1 20080825 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 EEL LIGHT INOP AT 'K' LAV. FOUND BULB INOP. REPLACED FLOOR MOUNTED LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 20080923 NM 2008 9 23 2008UALA05457 1 20080825 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 519UA 24872 EXTERIOR EEL LIGHT AT DOOR 1L IS INOP. RELAMPED, OP CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080924 2008 9 24 08FDEA03782 2 20080909 A 7261 OIL SYSTEM DOUG MD10 MD1010F 3022112 WP NR 2 ENGINE LOW A FDEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 21 366FE 46602 35 MINUTES INTO FLT ENG NR 2 OIL QTY DROPPED TO ZERO. TEMP 7 PRESSURE NORMAL. PRESSURE FLUCTUATED CONSTANTLY DECREASIN G TO APPROX (15 PSI) FLUCTUATING /- 5 PSI WHEN ENGINE WAS SHUT DOWN IN ACCORDANCE W/QRH. WINDMILLING PRESSURE GREATER THAN 2 PSI. 2 L 7 3 4F RT A22WE 20080924 EU 2008 9 24 08FDEA03344 1 20080808 A 5321 R532B371400000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 241 CK IS DAMAGED. REPAIRED CABIN FLOOR PANEL 241 QH BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MAR KED AND APPLIED NON-SKID TAPE IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03752 1 20080906 A 3244 Z3200203 TIRE AIRBUS 310 A310324 3930206 EU MLG FAILED A FDEA O OTHER O OTHER TO TAKEOFF 1 CE 21 801FD 539 ON DEPT TLV, ATC ADVISED COMPANY THAT RUBBER WAS FOUND ON RWY AFTER T/O. FRA CONFIRMED THAT A STARBOARD SIDE WAS DAMAGE D. FOUND NR 8 TIRE LOST COMPLETE REINFORCED PLY, NO DAMAGE ON FLAPS OR GEAR FOUND. REMOVED AND REPLACED NR 7 TIRE FOR OVERLOAD. 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03301 1 20080807 A 5753 65281311 FAIRING BOEING 727 7272S2F 1384O81 NM LT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 LEFT WING OB TE NR 2 FLAP TRANSMISSION JACKSCREW FAIRING ON INBD END OF MID FLAP HAS CRACK IN SIDE WEB 19 INCH AFT OF FW D END REMOVED CRACKED WEB. FABRICATED NEW WEB, P/N 65-28131-1. TREATED, PRIMED, AND PAINTED WEB. INSTALLED WEB REF SR M 51-30-2 PG 2-4/SRM 57-20-2 PG 15-17/SRM 51-20-1 PG 13/BOEING DWR NR 65-28131-1/SRM 51-10-2 PG 1-2/MM 51-20-151 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080924 EU 2008 9 24 08FDEA03758 1 20080908 A 5320 A53870064200 SUPPORT ANGLE AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 426FE 245 FUSELAGE CENTER SECTION ZONE 240 LT/SIDE EMERGENCY EXIT LOWER JAMB, AT FRAME 43 TOP ANGLE SUPPORT HAS CRACK. REMOVED AN D INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03759 1 20080908 A 5320 A53870064200 SUPPORT ANGLE AIRBUS 310 A310203 3930313 EU CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 426FE 245 FUSELAGE CENTER SECTION ZONE 240 RT/SIDE EMERGENCY EXIT LOWER JAMB AT FRAME 43,TOP ANGLE SUPPORT HAS CRACK. REMOVED AND INSTALLED NEW SUPPORT ANGLE IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080925 NM 2008 9 25 QXEA200800959 1 20080907 A 3297 473901 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM NLG MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 19 404QX 4046 PDX FLIGHT 2157. DEPARTING SEATTLE, RETRACTED THE GEAR AND GOT A NOSE GEAR UNSAFE LIGHT AND GEAR HANDLE LIGHT. AFTER A BOUT 60 SECONDS THE LIGHTS WENT OUT. BOTH LIGHTS CYCLED TWICE IN THE NEXT 3 MINUTES. THEN STAYED OUT FOR THE REST OF T HE FLIGHT. MX REPLACED THE NOSE GEAR PRIMARY LOCK HARNESS ASSEMBLY. OPS CHECKS GOOD. ACFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20080925 GL 2008 9 25 08FDEA03784 2 20080909 A 7230 COMPRESSOR DOUG MD11 MD11F 3023600 NM GE CF6 CF680C GL NR 1 ENGINE STALLED A FDEA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CE 21 607FE 37365 48547 704389 NR 1 ENG COMPRESSOR STALLED ON CLIMB AT ABOUT 8000 FT TWO EVENTS OCCURRED ABOUT 3 MINUTES APART. PRECAUTIONARY ENGINE S HUTDOWN ACCOMPLISHED. PLACED IN WORK. NR 1 ENGINE CHANGE APPROVED. PLANT ENGINEERING. REMOVED AND REPLACED NR 1 ENG INE IAW WORKCARD 71T0901- MANUFACTURER PERFORMED GROUND RUNS ENG CHECKS GOOD. 2 L 7 3 4F 4 F RT A22WE E23EA 20080925 EU 2008 9 25 08FDEA03797 1 20080910 A 5347 A5327842420800 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 MAIN DECK CARGO COMPARTMENT SEAT TRACK IS GOUGED BETWEEN FRAME 63 AND FRAME 64, RBL 18. BLENDED AREA AND FOUND THE REMA INING MATERIAL TO BE BEYOND ALLOWABLE LIMITS IAW A300-600 SRM 53-10-16, FIG 102, TOOL NR T8878G. REPAIRED THE SEAT TRAC K IAW A300-600 SRM 53-10-16, PGS 207/208. REMOVED AND RE-INSTALLED ELECTRICAL BRACKETS AND GROUND WIRES AS REQUIRED IA W A300-600 SRM 51-40-21; PARA 5. 2 L 7 2 4F RT A35EU 20080925 NM 2008 9 25 08FDEA03929 1 20080917 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 DURING OPEN HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH C RACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D. MAIN DECK DOOR LOWER JAMB NR 4 SUPPORT FITTING REMOVED AND REPLACE D AS PER SRM 51-33-01 VOLUME II. FITTING HOLES CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 SO 2008 9 25 SWIA200820063 1 20080921 A 6120 78249046 PCU EMB 120 EMB120ER 3260203 SO LEFT MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 07 284YV 24366 4825 120284 FLT 5415 - AFTER ROLLOUT LEFT PROP WOULD GO TO FEATHER. REPLACED LEFT PCU, P/N 782490, S/N ON: 960232, S/N OFF: 861240. 2 L 7 2 4T RT A31SO 20080925 SO 2008 9 25 SWIA200820066 1 20080808 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 299SW 120329 C-CHECK, CRACK IN FRAME IN FRONT OF LEFT HEAT EXCHANGER. INSTALLED DOUBLER. 2 L 7 2 4T RT A31SO 20080925 NM 2008 9 25 08FDEA03906 1 20080916 A 7830 THRUST REVERSER BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION CR CRUISE 1 CE 21 903FD 30545 27124 30898 L REV AMBER LIGHT ON RAN QRH NO YAW OR ADVERSE CONDITIONS. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-36-01 CATEGORY: C E XPIRATION: 26SEP08 MEL 78-36-01: LEFT ENGINE REVERSER UNLOCK INDICATION INOP. REVERSER DEACTIVATED IN FORWARD THRUST PO SITION." "A/C CAT A" C/0374246. REMOVED AND REPLACED RELAYS K26 AND K10108. 2 L 7 2 4F 4 F RT A2NM E12EU 20080925 NM 2008 9 25 08FDEA03907 1 20080916 A 3297 CONNECTOR BOEING 727 727233 138408A NM LT MLG DAMAGED A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CE 21 276FE 22041 LEFT GEAR (RED AND GREEN) INDICATOR LIGHTS ILLUMINATED IN FLIGHT. ON APPROACH WHEN LANDING GEAR LEVER PLACED DOWN, UNSA FE LIGHT REMAIN ON. RAN QRH AND CHECKED MANUAL MAIN GEAR EXTENSION DOWNLOCKS. FOUND PIN 31 IN CONNECTOR D4658P PUSHED BACK AND LOCK BROKEN. REPLACED CONNECTOR D4658P, REF WDM 32-64-01 AND ALSO WDM 27-22-01. COMPLETED OPS CHECK OF GEAR I NDICATION PER REF AMM 727-32-61-001-5. ALL LIGHTS CHECKED GOOD. COMPLETED GEAR SWING PER MOCC REQUEST, STILL CHECKS GO OD, ALL GEAR INDICATION LIGHTS WORK GOOD, GEAR UP LIGHTS OUT AND GEAR DOWN LIGHTS GREEN. 2 L 7 3 4F RT A3WE 20080925 NM 2008 9 25 08FDEA03908 1 20080916 A 5343 ACA70171 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 NOSE LANDING GEAR LEFT TRUNNION FITTING FOUND CRACKED. NOSE LANDING GEAR LT TRUNNION FITTING REPAIRED AS PER SRM 53-40- 00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEE D 1,500 LANDING INTERVALS. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03909 1 20080916 A 5343 ACA70172 TRUNNION DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 NOSE LANDING GEAR RIGHT TRUNNION FITTING FOUND CRACKED. NOSE LANDING GEAR RT TRUNNION FITTING REPAIRED AS PER SRM 53-40 -00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REPETITIVELY INSPECT FOR CRACK GROWTH AT NOT TO EXCEED 1,500 LANDING INTERVALS. 2 L 7 3 4F RT A22WE 20080925 EU 2008 9 25 08FDEA03910 1 20080917 A 5347 A53274787204 SEAT TRACK AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 808FD 439 MAIN DECK CARGO SEAT TRACK NR 4LT BETWEEN FR 59.2 AND FR 59.3 HAS 2 AREAS OF DAMAGED SCALLOPS REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED REPLACEMENT TRACK AT NR 4 LT BETWEEN FR 58 AND FR 60.5 IAW A310-300 SRM 51-40-210AND 53-17-1 6 2 L 7 2 4F RT A35EU 20080925 NM 2008 9 25 08FDEA03911 1 20080917 A 5310 CREASE BEAM BOEING 757 757236 1384971 NM BS 1360-1340 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 AFT PIT, CREASE BEAM WEB, LOWER SURFACE BS 1360 BS 1340 RBL 67 INCH HAS CORROSION REMOVED CORROSION FOUND TO BE OUT OF L IMITS IAW SRM 53-60-13. FABRICATED NEW WEB ON TRAVELER T8/753327. INSTALLED NEW WEB IAW SRM 51-40-02 AND REINSTALLED CREASE BEAM IAW SRM 51-40-02, MAJOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED. 2 L 7 2 4F RT A2NM 20080925 WP 2008 9 25 08FDEA03872 1 20080915 A 5522 SKIN DOUG MD10 MD1010F 3022112 WP RT ELEVATOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 RIGHT STABILIZER INBD ELEVATOR UPPER SKIN IS DENTED. CHECKED LIMITS ON THE DENT DEEPEST POINT 0.095 WITH DEPTH GAUGE T8 492C DUE 10/25/08. FOUND TO BE OUT OF LIMITS IAW SRM 51-80-01; VOL II; PG 2; NOTE "K". CUT OUT DAMAGE IAW SRM 55-10-0 0; VOL I; FIG 8. ALODINED AND PRIMED IAW SRM 51-21-01; VOL II. INSTALLED REPAIR DOUBLER IAW SRM 55-10-00; VOL I; FI G 8. PAINTED IAW SRM 51-21-01; VOL II. 2 L 7 3 4F RT A22WE 20080925 EU 2008 9 25 08FDEA03874 1 20080915 A 5411 A54611750 SPAR AIRBUS 300 A300B4622R 3930312 EU NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND ON LOWER SPAR OF PYLON NR 1 UPPER SURFACE CRACK IN CENTER STIFFENER AT RIB 10A. REPAIR PERFORMED BY CUT OUT THE C RACKED AREA AND INSTALLING A DOUBLER IAW DRAWING R546-10349, APPROVED BY RAS/70512822/010/2008 ISS A, APPROVED BY EA 6-5 451-123098. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03875 1 20080915 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND OLD REPAIR AFT OF REAR SPAR AT RIB 9 RAS/BAE/0081/2002 ISS C, UNREPAIRED CRACK WITH CRACK STOP HOLE IN BOTTOM SKIN . REPAIR PERFORMED BY DRILLING CRACK STOP HOLE, INSTALLING A CRACK STOP PLUG AND REPAIR PLATE IAW DRAWING R573-40199, A PPROVED BY RAS/BAE/1007820/2008 ISS A AND EA 6-5720-123096. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03877 1 20080915 A 5330 A5377608020200 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 EXTERIOR FUSELAGE SKIN HAS STATIC DISCHARGE BETWEEN FRAME 68 AND FRAME 69, STRINGER 1 L AND 2 L. REMOVED DAMAGE BY WAY OF DRILLING A 5/32 HOLE IAW SRM 53-10-12, FIG 220. ACCOMPLISHED A BHEC INSPECTION IAW NTM 51-10-01. INSTALLED A RIVET IAW A310-200 SRM 53-10-12, FIG 220. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03880 1 20080915 A 5330 A5377601720200 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 EXTERIOR FUSELAGE UPPER SPLICE DOUBLER HAS STATIC DISCHARGE AT FRAME 33 BETWEEN STRINGER 5 L AND 6 L. REMOVED AND REP LACED FASTENER IAW A310-200 SRM 53-10-12; FIG 220. ACCOMPLISHED A BHEC INSPECTION IAW A310 NTM 51-10-01. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03881 1 20080915 A 5533 A55371397203 ANGLE AIRBUS 310 A310203 3930313 EU VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 426FE 245 VERTICAL STABILIZER FWD RT LOWER CHORD ANGLE HAS A 6.5 INCH CRACK. REMOVED AND REPLACED CHORD ANGLE IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080925 NM 2008 9 25 08FDEA03941 1 20080918 A 5313 STRINGER BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 STRINGER 11R, BS 1500, HAS CORROSION ON ANGLE FITTING ATTACHMENT TO FRAME. REMOVED AND REPLACED STRINGER 11R, BS 1460-1 640, IAW SRM 51-40-02 AND SRM 53-00-03, FIGURE 101, DETAIL 2. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING. 2 L 7 2 4F RT A2NM 20080925 WP 2008 9 25 08FDEA03942 1 20080918 A 5753 ARC27443 WEDGE DOUG MD10 MD1010F 3022112 WP LT TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT INBD FLAP, INBD TRAILING EDGE IS CRACKED. REMOVED TRAILING EDGE SECTION IAW SRM 51-35-02. FABRICATED IAW SRM 57-2 0-00. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED IAW SRM 51-35-02. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03943 1 20080919 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK INDICATIONS AT HOLES A, B AND C. MAIN DECK CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 SO 2008 9 25 LR7A08097 1 20080819 A 5321 FLOORBOARD LKHEED 382 382G 526414U SO FS 737E-817E WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HC5314 FOUND RT CABIN FLOORBOARD WARPED AT FS 737E TO 817E WL146, RBL15 TO 50. REPAIRED BY FABRICATING AND INSTALLING FLOORBOARD IAW SMP583 FIG 53-40-05 PG 37, CHAP 51-60, 51-70, AND SMP 581-25-50 FIG 25-50-06. 2 H 7 4 4T A1SO 20080718 NM 2008 7 18 SWAA083591 1 20080625 A 5752 654645522C TAB BOEING 737 7373H4 1384600 NM RT AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED HC1 CHECK, FOUND RT WING AILERON TAB DELAMINATED. REMOVED AND REPLACED TAB PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083592 1 20080629 A 3350 65C27093 LIGHT BOEING 737 7373G7 1384595 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 M7K2008F00025 1 20080512 A 6710 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE FAILED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 813MH 3967 23183 A FAULT CODE WAS GENERATED ON SHUTDOWN INDICATING A DEFECT OF COLLECTIVE POTENTIOMETER. A NEW PART WAS INSTALLED, NO FU RTHER FAULT WAS DETECTED. THIS IS RECURRING FAILURE FOR THIS PART WHICH HAS EFFECTED DISPATCH RELIABILITY FOR THIS MODE L HELICOPTER. SUGGEST AN ALTERATION OF FAULT SENSING SOFTWARE TO REDUCE FAULT SENSITIVITY TO PERHAPS A SIGNAL LOSS OF 0 .5 SECOND RATHER THAN 1/20TH OF A SECOND. AN OPTIC RATHER THAN A RESISTANCE BASED SENSOR SHOULD BE CONSIDERED AS CONTAC T POINT IS DAMAGED BY AC VIBRATION WHEN AC POWER SETTINGS ARE SET FOR CRUISE FLIGHT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 EU 2008 7 18 M7K2008F00036 1 20080612 A 6220 704A33640088 FREQ ADAPTER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE M/R HUB ASSY CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 818MH 1498 M2880 4131 DURING ROUTINE INSPECTION A CRACK WAS FOUND IN ONE FREQUENCY ADAPTERS ELASTOMER SURFACE WHICH EXCEEDS THE MM LIMITATIONS OF 10MM. A NEW KIN OF (3) ADAPTER HAS BEEN INSTALLED IAW OEM RECOMMENDATIONS. THIS IS A VERY COMMON FAILURE FOR THIS ASSEMBLY. SUGGEST THAT THE MFG RETURN TO THE ORIGINAL ELASTOMER FOUND ON THE OLDER PN FREQUENCY ADAPTERS WHICH VERY RAR ELY FAILED. THE RECENT EXTENSION OF THE SERVICE LIFE LIMITS ON THIS PART TO 20,000 HOURS IS RATHER SILLY AS NONE HAVE L ASTED TO EVEN 2500 HOURS DUE TO ELASTOMER FAILURES. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 EU 2008 7 18 M7K2008F00037 1 20080612 A 7410 9550178070 IGNITER BOX UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE MALFUNCTIONED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 807MH 1951 3912 23130 DURING ROUTINE INSPECTION AN OPERATIONAL CHECK REVEALED VERY SLOW FUNCTION ON (1) OF THE (2) IGNITERS POWER CIRCUITS. A NEW IGNITER BOX WAS INSTALLED AND OPERATIONAL CHECK WAS NORMAL. THIS PARTIAL LOSS OF A CIRCUIT IS TYPICAL FOR THIS ASSE MBLY. USUALLY THIS UNIT IS TROUBLE FREE. 1 G 7 2 3U 3 U H9EU E00054EN 20080718 NM 2008 7 18 SWAA083565 1 20080626 A 5311 6546566 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 992, STR 17R. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 M7K2008F00019 1 20080523 A 6320 1130021089 PRESSURE SENSOR UROCOP UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE RGB FAILED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 809MH 1335 3927 46047 LOW MGB OIL PRESSURE WARNING LIGHT ILLUMINATES DURING GROUND IDLE OF THE AC. SWITCH WAS FOUND OUT OF TOLERANCE. SWITCH WAS REPLACED WITH A SERVICEABLE PART WITH NO FURTHER DISCREPANCY NOTED. THIS IS NOT AN UNCOMMON FAULT FOR THIS PART. SUG GEST IMPROVED DESIGN OR BETTER QC FOR INTERNAL PARTS AS PERHAPS ON A THIRD OF THESE SWITCHES FAIL IN SERVICE. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 EU 2008 7 18 M7K2008F00027 1 20080512 A 6710 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE FAILED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 847MH 143 4266 23416 A FAULT CODE WAS GENERATED ON SHUTDOWN INDICATING A DEFECT OF COLLECTIVE POTENTIOMETER. A NEW PART WAS INSTALLED, NO FU RTHER FAULT WAS DETECTED. THIS IS RECURRING FAILURE FOR THIS PART WHICH HAS EFFECTED DISPATCH RELIABILITY FOR THIS MODE L HELICOPTER. SUGGEST AN ALTERATION OF FAULT SENSING SOFTWARE TO REDUCE FAULT SENSITIVITY TO PERHAPS A SIGNAL LOSS OF 0 .5 SECOND RATHER THAN 1/20TH OF A SECOND. AN OPTIC RATHER THAN A RESISTANCE BASED SENSOR SHOULD BE CONSIDERED AS CONTAC T POINT IS DAMAGED BY AC VIBRATION WHEN AC POWER SETTINGS ARE SET FOR CRUISE FLIGHT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 NM 2008 7 18 SWAA083615 1 20080629 A 5310 141A1120 DOOR FRAME BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 772SW 27880 DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR FRAME CUTOUT FWD FRAME CRACKED AT LOWER END. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083599 1 20080627 A 2121 215201 GASPER FAN BOEING 737 7377H4 1384404 NM E&E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 796SW 27889 AT FL 360 CREW REPORTED AN ELECTRICAL ODOR IN CABIN. TURNED OFF GASPER FAN ODOR DISSIPATED. REMOVED AND REPLACED GASPE R FAN PER MM. 2 L 7 2 4F RT A16WE 20080718 2008 7 18 SWAA083488 4 20080625 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 251WN 32510 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083499 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083496 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083514 1 20080625 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 13R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083515 1 20080625 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 14R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080925 SO 2008 9 25 LR7A08098 1 20080819 A 5312 3562517 BULKHEAD LKHEED 382 382G 526414U SO FS 817 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HC5321, FOUND BULKHEAD SKIN CRACKED AT FS 817E, WL138, LBL9. REPAIRED IAW SMP 583 FIG 51-140-17. 2 H 7 4 4T A1SO 20080925 SO 2008 9 25 LR7A08099 1 20080819 A 5350 33873518R SKIN LKHEED 382 382G 526414U SO FAIRING WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HST5301 FOUND RT WW BOTTOM FAIRING SKIN WARPED AT FS 507, WL130, RBL 50. REPAI RED IAW SMP583 CHAP 51-60, 51-70 AND DWG 338735. 2 H 7 4 4T A1SO 20080925 SO 2008 9 25 LR7A08100 1 20080819 A 5330 36201410 SKIN LKHEED 382 382G 526414U SO FS 497-537 WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HST5301, FOUND BELLY SKIN WARPED AT FS 497 TO 537, WL128 TO 141, LBL 50 TO RBL 50. REPAIRED IAW SMP583 CHAP 51-60, 51-70 AND DWG 362014. 2 H 7 4 4T A1SO 20080925 NM 2008 9 25 08FDEA03760 1 20080908 A 5230 65569271 SKIN BOEING 727 727233 138408A NM CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 C-3 DOOR EXTERIOR SKIN HAS NUMEROUS DENTS AND GOUGES. FABRICATED NEW EXTERIOR SKIN IAW EA NR 7-5230-123319 AND BOEING D WG NR 65-56927 EA 7-5230-123319. 2 L 7 3 4F RT A3WE 20080925 WP 2008 9 25 08FDEA03766 1 20080908 A 5740 ARL0501199 ATTACH BRACKET DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING FUEL TANK UPPER ACCESS 534 BT FWD MOST FUEL LINE CLAMP ATTACH BRACKET IS CRACKED AT XORS 455. REMOVED THE BRA CKET. FABRICATED A NEW BRACKET AND INSTALLED THE NEW BRACKET IAW DAC DWG ARL 0501; REV "AU" AND DC/MD-10 SRM 51-31-01; VOL II. ALODINED IAW DC/MD-10 SRM 51-21-01; VOL II. PART MARKED IAW FEDEX GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03776 1 20080908 A 5740 ARB23696 BRACKET DOUG MD10 MD1010F 3022112 WP ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 RIGHT WING UPPER FUEL TANK AT ACCESS OPENING 634 AT HAS A MOUNT BRACKET (A/C SIDE) WITH ELONGATED HOLES AT THE FUEL CHEC K FLAPPER VALVE, WING STA XORS 402, AFT AND INBD OF THE OPENING. REMOVED THE HINGE ASSEMBLY. FABRICATED A NEW HINGE AS SEMBLY AND INSTALLED THE NEW HINGE ASSEMBLY IAW DWG ARB 2369; REV "C" AND SRM 51-33-01; VOL II. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II. PART MARKED HINGE ASSEMBLY IAW GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03985 1 20080922 A 5347 NFA60229 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION BEWTEEN STA 1800 AND STA 1860, LBL 105. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS IAW SRM 53-70-00. FABRICATED CHANNEL IAW SRM 53-70-00. ALODINED & PRIMED IAW SRM 51-21-01. INSTAL LED CHANNEL REPAIR IAW SRM 53-70-00. REMOVED & REPLACED FLOOR PANEL IAW AMM 53-21-01-8. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03986 1 20080922 A 5347 NEA60225 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION BETWEEN BS 1330-1341, LBL 27. REMOVED CORROSION, FOUND OUT OF LIM ITS IAW SRM 53-70-00 VOL I FIG SHEETS 1&2 NOTE 5. FABBED A NEW SECTION IAW SRM 53-42-01 & SRM 53-70-00. ALODINED & PR IMED SECTION IAW SRM 51-21-01. INSTALLED NEW SEAT TRACK SECTION AT BS 1311-1371 LBL 27 IAW SRM 53-70-00 & SRM 51-31-01 . REMOVED & RE-INSTALLED FLOOR PANELS IAW AMM 53-21-01-8. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03987 1 20080922 A 5347 NEA60225 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION BEWTEEN STA 1361 AND STA 1391, LBL 27. REMOVED CORROSION, FOUND OU T OF LIMITS IAW SRM 53-70-00. FABBED A NEW SECTION IAW SRM 53-42-01 AND SRM 53-70-00. ALODINED & PRIMED SECTION IAW SR M 51-21-01. INSTALLED NEW SECTION IAW SRM 53-70-11 & SRM 51-31-01. REMOVED & RE-INSTALLED FLOOR PANELS IAW AMM 53-21- 01-08. 2 L 7 3 4F RT A22WE 20080925 GL 2008 9 25 08FDEA03603 2 20080827 A 7200 ENGINE AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2* GL NR 1 UNSTABLE A FDEA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CE 21 661FE 760 705234 NR 1 ENGINE N1 INDICATION BECAME UNSTABLE DURING CLIMB. REPEAT WRITE-UP, THEN EGT EXCEEDED LIMITS AT 952 DEG. THEN FUE L FLOW INDICATION BECAME UNSTABLE WITH SURGING AND YAW. PULLED TO IDLE N-1 AND FF INDICATION REMAINED UNSTABLE BUT SURG ING STOPPED. R&R N1 SENSOR, FUEL CONTROL, C.I.T. SENSOR AND BORESCOPED. 2 L 7 2 4F 4 F RT A35EU E23EA 20080925 WP 2008 9 25 08FDEA03778 1 20080908 A 5730 ARB0903502 DOUBLER DOUG MD10 MD1010F 3022112 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 RIGHT WING COMP PROBE PANEL LAND IS CRACKED; NR 2 TANK. REMOVED & REPLACED NR 8 STRINGER IN REF TO EA 8-5720-117035. L EAK CHECK COMPLIED WITH ON NON-ROUTINE N00533 / 41533. 2 L 7 3 4F RT A22WE 20080925 EU 2008 9 25 08FDEA03618 1 20080828 A 5753 A579420920000 FLAP TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 650FE 726 RIGHT WING FLAP FAIL SAFE BOLT PIN PLATING IS WORN, (FWD BOLT). REMOVED AND REPLACED THE RIGHT WING INBD FLAP FAIL SAFE BOLT REF AMM 57-20-24-4. 2 L 7 2 4F RT A35EU 20080925 NM 2008 9 25 08FDEA03620 1 20080828 A 5330 65545835 SKIN BOEING 727 727233 138408A NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 DENT LT AFT FUSELAGE STA 1070 S18-20L. EVALUATED DENT AT STA 1070 STR 18L TO 20L AND FOUND WITHIN LIMITS IAW SRM 53-30- 01 FIG1 BUT DENT CROSSES OVER STR 19L EA 7-5330-117024 "SKIN PANEL DENT AT STA 1074 S18-20L" ISSUED TO ADDRESS DENT CROS SING S19L. PER EA 7-5330-117024 SUBJECT AREA REMAINS CAPABLE OF CARRYING DESIGN LOADS AND WILL HAVE NO ADVERSE AFFECT O N SKIN FATIGUE LIFE. HFEC INSPECTED AREA AND FOUND NO CRACKS IN THE DENT LOCATIONS. 2 L 7 3 4F RT A3WE 20080925 NM 2008 9 25 08FDEA03802 1 20080910 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 623FE 48794 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIA HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRA CK INDICATION AT HOLES B, C AND D. MAIN CARGO DOOR LOWER JAMB, FOR CRACKED BOLT HOLES B, C AND D AT NR 1 SUPPORT FITTIN G REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL 1. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03372 1 20080811 A 5320 7075T6 FLOOR SUPPORT BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 MAIN CABIN RT FLOOR SUPPORT ANGLE FROM BS 630 TO BS 640, RBL 64 HAS CORROSION. CORROSION FOUND EXCEEDED SRM LIMITS. RE MOVED AND REPLACED FLOOR SUPPORT ANGLE IAW B757-200 SRM 51-70-12 DETAIL VI. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-1 00 CRITERIA. 2 L 7 2 4F RT A2NM 20080925 EU 2008 9 25 08FDEA03277 1 20080806 A 5321 B5327031600600 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DOOR PANEL NR 261 RF, FWD OUTBD LOWER SURFACE IS PUNCTURED. FABRICATED PANEL IAW A300-600 SRM 53-10-20 AND F EDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080718 EA 2008 7 18 A6WA200840435 1 20080520 A 5310 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 CORROSION ON BOTH CLEATS OF PAX DOOR SURROUND STRUCTURE LOWER SILL BETWEEN FS 310 TO FS 349. CORROSION REMOVED IAW SRM 51-21-06. (A) 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840444 1 20080523 A 5753 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 LEFT OUTBOARD FLAP, OUTBOARD FLAP HINGE ARM FOUND GOUGED ON BEARING ATTACHMENT PLATE, FWD FACE. GOUGE ON BEARING ATTACH MENT PLATE FWD FACE REMOVED IAW REO 601R-57-54-112. (A) 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840447 1 20080516 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 PAX DOOR EDGE MEMBER CRACKED AT FS 338. REPAIRED IAW REO 601R-52-11-279. (A) 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840452 1 20080527 A 5240 SKIN CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 CORROSION ON SKIN AROUND SCREW HOLES UNDER PROTECTIVE PLATE OF SERVICE DOOR. CORROSION ON SKIN AROUND SCREW HOLES REMOV ED IAW SRM 51-41-06. (A) 2 L 7 2 4F RT A21EA 20080718 CE 2008 7 18 E812008F00001 1 20080626 A 3020 5188001 VALVE RAYTHN 390 390 7150030 CE ANTI ICE SYSTEM STUCK B E81R K NONE O OTHER NR NOT REPORTED 1 GL 03 404JM 444 RB167 INVESTIGATED PILOT REPORT OF UNCOMMANDED RT ENGINE ANTI-ICE OPERATION DURING TAKEOFF AND CRUISE FLIGHT. FOUND RT ENGINE ANTI-ICE VALVE STICKING OPEN. REPLACED VALVE WITH SERVICEABLE O/H VALVE, FUNCTIONS NORMAL. HAVE NOTED SEVERAL FAILURE S OF ANTI-ICE VALVES AFTER LOW TIME IN SERVICE. RECOMMEND MFG INVESTIGATE WHETHER VALVE DESIGN OR INSTALLATION CAUSING PREMATURE FAILURES. (K) 1 L 7 2 3F RT A00010WI 20080718 WP 2008 7 18 MWE2008F00004 1 20080623 A 3350 WIRE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D* NE EMERGENCY LIGHTS BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 FLOOR TRACK LIGHTS INOPERATIVE ROWS 9 TO 18. REPAIRED 2 EACH BROKEN WIRES ON FLOOR TRACK FWD OVERWING EXITS. (K) 2 L 7 2 4F 4 F A6WE E2EA 20080718 EA 2008 7 18 A6WA200840411 1 20080510 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 442AW 7778 CRACK EXISTS ON INTERCOSTAL FS 484 RBL 36 AND RBL 27. DAMAGED ATTACHMENT FLANGE CUTOUT, EDDY CURRENT PERFORMED AND NEW SERVICEABLE ANGLE INSTALLED IAW REO 601R-53-41-059 REV A. 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840412 1 20080509 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 442AW 7778 LEFT FS 280, LBL 8 & 10, ANGLE ON BEAM FOUND CRACKED. LT FS 280, LBL 8 & 10, ANGLE ON BEAM REPLACED IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 20080718 EU 2008 7 18 M7K2008F00031 1 20080523 A 5551 350A23422221 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE HORIZONTAL STAB CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 808MH 3914 23072 DURING ROUTINE INSP THE FITTING WAS FOUND CRACKED FROM AN OB ATTACHMENT SCREW BORE TO THE FLANGE EDGE. A NEW FITTING WAS INSTALLED. THIS IS A COMMON FAILURE FOR THIS PART. PART MAY HAVE BEEN SHIMMED INCORRECTLY OR BORE HOLE NOT ALIGNED PER FECTLY. SUGGEST A MORE DURABLE MATERIAL BE USED IN THIS PARTS MFG SUCH AS TITANIUM OR SS AS ALUMINUM ALLOY FAILS ROUTIN ELY UNDER THE NORMAL STRESS APPLIED TO THIS PART. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 NM 2008 7 18 KCSA081269 1 20080531 A 5412 BULKHEAD BOEING 747 747259B 1384804 NM NR 2 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 NR 2 PYLON HYDRAULIC PRESSURE LINE BULKHEAD FITTING CHAFING AFT SIDE OF NAC STA 221.9 BULKHEAD. 2 L 7 4 4F RT A20WE 20080718 EA 2008 7 18 A6WA200840413 1 20080510 A 5420 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT NACELLE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 442AW 7778 LEFT TAIL PIPE STANDOFF BRACKET FOR FIRE DETECTION LOOP CRACKED. REPLACED IAW SRM 51-42-06. (S) 2 L 7 2 4F RT A21EA 20080718 EU 2008 7 18 UPS08152445 1 20080610 A 5753 FLAP AIRBUS A300 A300F4622R 3930360 EU LT WING DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 159UP 0848 INSPECTION TYPE:N/A LT INBOARD T/E FLAP DENT OUT OF LIMITS. 2 L 7 2 4F RT A35EU 20080718 EU 2008 7 18 LV62008F00000 1 20080407 A 6300 850A37128901 SPACER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE MAIN ROTOR SHAFT DAMAGED E LV6A O OTHER O OTHER NR NOT REPORTED 1 WP 19 46CD M5488 1878 RETAINING RING "SPACER" APPARENTLY BROKE AND AS IT SPUN AROUND, CAUGHT M/R SHAFT CHIP DETECTOR AND BROKE THE END OF IT O FF THUS TURNING ON "CHIP LIGHT" IN COCKPIT. AC TURNED AROUND AND LANDED AT BASE. FOUND CHIP DETECTOR BROKEN, TRANSMI SSION APART AND SUBSEQUENTLY FOUND SOURCE OF PROBLEM. (K) 1 G 7 1 3U 3 U H9EU E19EU 20080718 NM 2008 7 18 UPS08552447 1 20080527 A 5330 STRUCTURE BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 411UP 23851 INSPECTION TYPE:C-1 BS 1787 TO 1825 APU INLET CUTOUT IS CORRODED AT NUT PLATE CONTACT AREAS. REMOVED, FABRICATED AND IN STALLED STRAP PER ER 08-2091. 2 L 7 2 4F RT A2NM 20080718 NM 2008 7 18 UPS08552467 1 20080612 A 5610 LATCH BOEING 757 75724APF 1384969 NM COCKPIT WINDOW STIFF A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 442UP 27387 INSPECTION TYPE:N/A CAPTAIN'S DV WINDOW LATCH/UNLATCH HANDLE VERY STIFF TO MOVE TO UNLATCH POSITION. REF AMM 56-11-02-5 . HANDLE EXCEEDS 50PDS PULL FORCE. CAPTAIN'S L WINDOW REPLACED PER M/M 56-11-02-4. PRESSURIZATION & WINDOW HEAT CHECK GOOD. WINDOW OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 20080718 NM 2008 7 18 UPS08652440 1 20080609 A 5753 CAP BOEING 767 76734AF 1385212 NM T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE:N/A RIGHT WING O/B FLAP LEADING EDGE CAP CRACKED. 2 L 7 2 4F RT A1NM 20080718 WP 2008 7 18 UPS08852461 1 20080522 A 5340 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 MAIN CARGO COMP STA 980, L22R ATTACHING FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51- 1-20, 51-1-20D, 51-1-8. 2 L 7 4 4F RT 4A25 20080718 WP 2008 7 18 UPS08852462 1 20080524 A 5347 3657504501 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 COCKPIT SECOND OBSERVER SEAT TRACKS SHOWS ELONGATIONS. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-1 -8, 51-3-0, 51-1-24. 2 L 7 4 4F RT 4A25 20080718 WP 2008 7 18 UPS08852463 1 20080523 A 5411 FRAME DOUG DC8 DC873F 302199F WP NR 2 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 NR 2 PYLON UPPER PANEL FRAME, WORN BEYOND LIMITS, DEEP CHAFED DAMAGE BETWEEN PANELS 293A/B AND 294A/B . FABBED AND INSTALLED NEW PANEL FRAME IAW SRM, 51-1-8, 51-1-20D, 51-1-2 1, 54-3-3 FIG 7. 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 F3LA200800281 1 20080531 A 5311 D5347112320300 FRAME AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 DURING C4 S1 C-CHECK INSPECTION NOTED SUPPORT FRAME FOR SHEAR PLATE CORRODED ON BOTTOM SURFACE AT NUT CLIP HOLE. MAINTE NANCE REMOVED OLD SUPPORT FRAME AND INSTALLED A NEW SUPPORT FRAME IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11 PA RAGRAPH 6 AND 7. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F 4 F RT A28NM E37NE 20080718 EU 2008 7 18 M7K2008F00020 1 20080523 A 5551 350A23422221 FITTING UROCOP UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE HORIZONTAL STAB CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 821MH 4134 DURING ROUTINE INSP FITTING WAS FOUND CRACKED IN (2) PIECES. NEW FITTING WAS INSTALLED. THIS IS A COMMON FAILURE FOR THI S PART. PART MAY HAVE BEEN SHIMMED INCORRECTLY OR BORE HOLE NOT ALIGNED PERFECTLY. SUGGEST A MORE DURABLE MATERIAL BE U SED IN THIS PARTS MFG SUCH AS TITANIUM OR SS AS ALUMINUM ALLOY FAILS ROUTINELY UNDER NORMAL STRESS APPLIED TO THIS PART. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 EU 2008 7 18 M7K2008F00040 1 20080612 A 6720 116SF2C502W00253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE FAILED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 807MH 124 3912 3912 23130 UPON SHUTDOWN A FAULT CODE WAS GENERATED THAT INDICATED A FAULT WITH COLLECTIVE POTENTIOMETER. A NEW POTENTIOMETER WAS I NSTALLED AND NO FURTHER DEFECT NOTED. THIS HAS BEEN A VERY COMMON FAULT FOR THIS PART. RECENTLY IT WAS DETERMINED THAT ELECTRICAL HARNESS FOR THIS SIGNAL WAS LACKING SHIELDING, ADJACENT WIRING MAY HAVE BEEN INDUCING SOME SPURIOUS INPUTS T O FADEC THAT WERE INTERPRETED AS A FAULT. RE-ROUTED OUR AIR CONDITIONING WIRE HARNESS TO INCLUDE SPACERS SO AS TO REDUCE CHANCE OF SIGNAL CORRUPTION, OCCURRENCES OF THIS FAILURE TYPE HAVE BEEN SIGNIFICANTLY REDUCED. THIS MAY BE A COINCIDEN CE BUT A CASE IS BUILDING TO USE SHIELDED HARNESS TO CARRY THIS RESISTANCE SIGNAL TO FADEC. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 EU 2008 7 18 M7K2008F00047 1 20080623 A 6220 704A33640088 FREQ ADAPTER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE M/R HUB ASSY CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 823MH 1304 4158 DURING ROUTINE INSP A CRACK WAS FOUND IN ELASTOMER SURFACE OF BLUE CODED FREQUENCY ADAPTER THAT HAD REACHED MM LIMITATIO N OF 10MM. ALL (3) ADAPTERS WERE REPLACED AS A KIT IAE MFG RECOMMENDATIONS. SUGGEST MFG ALTER ELASTOMER FORMULATION TO IMPROVE SERVICE LIFE FOR THIS PART AS THIS HAS BECOME A VERY COMMON FAILURE FOR THIS PART WITH A 20,000 HR SERVICE LIFE . (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 NM 2008 7 18 UPS08M52448 1 20080520 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 280UP 48634 INSPECTION TYPE:2C RIGHT WING OUTER ACCESS PNL LANDING HAS CRACK. CRACK BETWEEN UPPER AND LOWER HINGE. VIEWED WITH MIR ROR. FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD11 SRM 57-10-00 FIG 18. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 UPS08M52449 1 20080521 A 5720 STRAP DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 280UP 48634 INSPECTION TYPE:2C RIGHT WING L/E SPLICE STRAP XFS 669 CRACKED. REMOVED, FABRICATED, AND INSTALLED SPLICE STRAP IAW MD1 1 SRM 51-21-01, 51-33-01, AND DWG ARB3954. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 UPS08M52450 1 20080521 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 280UP 48634 INSPECTION TYPE:2C LT WING L/E FIXED PANEL SUPPORT LOWER STRINGER FOUND CRACKED AT WING STA YORS AS MARKED, JUST O/B OF SLAT DRIVE MECHANISM. FABRICATED AND INSTALLED DOUBLER IAW MD11 SRM 57-10-00 FIG 18, 51-31-01, AND 51-21-01. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 UPS08M52451 1 20080522 A 5730 STRUCTURE DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 280UP 48634 INSPECTION TYPE:2C LT WING OUTBOARD L/E FIXED PANEL, SLAT ANTI-ICE DUCT ACCESS CUTOUT AREA FOUND UPPER CORNER CRACKED. CUT OUT TWO EACH AREAS, FABRICATED 2 EA DOUBLERS AND FILLERS, AND INSTALLED IAW MD11 SRM 57-10-00, 51-35-01, 51-21-01, A ND 51-21-02. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 UPS08552441 1 20080609 A 2560 TAPE BOEING 757 75724APF 1384969 NM COCKPIT MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 434UP 25465 INSPECTION TYPE:N/A 2 DESCENT INERTIAL REELS MISSING TAMPER PROOF TAPE. REMOVED & REPLACED BOTH DESCENT DEVICES PER MM 25-61-02-2. 2 L 7 2 4F RT A2NM 20080718 NM 2008 7 18 UPS08552452 1 20080610 A 8010 7902905 STARTER BOEING 757 75724APF 1384969 NM NR 1 ENGINE MALFUNCTIONED A IPXA F D ACTIVATE FIRE EXT. RETURN TO BLOCK A FLAME/FIRE NR NOT REPORTED 1 SO 01 446UP 27735 INSPECTION TYPE:N/A NR 1 ENGINE WOULD NOT ROTATE. GROUND ADVISED "ENGINE ON FIRE". FIRE HANDLE PULLED AND DISCHARGED. REMOVED AND REPLACED STARTER ON ENGINE. REF AMM 80-11-01-4. OPS TEST OK, EO M-8010-1558. 2 L 7 2 4F RT A2NM 20080721 EU 2008 7 21 UPS08152418 1 20080522 A 5753 SKIN AIRBUS A300 A300F4622R 3930360 EU T/E FLAP CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 137UP 0820 INSPECTION TYPE:3C LEFT WING CENTER FLAP UPPER SKIN MID SECTION HAS 6 CHAFE MARKS. CUT OUT DAMAGE AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300-600 SRM 57-50-00 FIG 206, 51-40-21 AND EO M-5100-19814-D. 2 L 7 2 4F RT A35EU 20080721 NM 2008 7 21 UPS08552423 1 20080603 A 3350 BATTERY PACK BOEING 757 75724APF 1384969 NM COCKPIT FAULTY A IPXA K NONE O OTHER NR NOT REPORTED 1 SO 01 428UP 25459 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT FLICKERS ON/OFF WHILE EN ROUTE. REMOVED AND REPLACED EMERGENCY BATTERY PACK AS SY, CHECKS GOOD PER MM 33-51-00-5. 2 L 7 2 4F RT A2NM 20080721 NM 2008 7 21 SWAA083631 1 20080701 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083633 1 20080701 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED BRDG CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083736 1 20080706 A 5330 6545753 BEAR STRAP BOEING 737 7373H4 1384600 NM CORRODED CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN AFT CARGO DOOR CUTOUT BEAR STRAP CORRODED AT BS 797, RBL 18. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080721 2008 7 21 2008UALA02688 4 20080508 A 2565 D31591478U1 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU R1 DOOR FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 338UA 24242 DOOR 1R GIRT BAR NOT SECURING PROPERLY. SUSPECT FAULTY DOOR SLIDE ASSEMBLY. REPLACED DOOR SLIDE ASSEMBLY IAW MM 25-61- 35. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080721 EU 2008 7 21 2008UALA02717 1 20080510 A 2420 E0175B01E00 RELAY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELECTRICAL SYS FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 421UA 500 EMERGENCY GENERATOR DOES NOT COME ON WHEN EMER GEN SW IS SELECTED. TRIED RELAY 12XE AND CONTROL UNIT 1XE, NO HELP. CK' D FOR VOLTAGE AT HYD FLOW SOLENOID ON TOP OF EMER GEN 8XE, NO VOLTAGE PRESENT. *S/D* RAT EXT INHIB COND RELAY BAD. RE PLACED RAT EXT INHIB CONDITION RELAY 20XE, CKS GOOD PER MM. 2 L 7 2 4F 4 F RT A28NM E40NE 20080721 2008 7 21 2008UALA02827 4 20080515 A 2565 D31591478U1 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FWD GALLEY DOOR OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 910UA 25254 FWD GALLEY DOOR 1R SLIDE PACK GIRT NEEDS REPACK - GIRT DRAGGING ON FLOOR AND DOOR FRAME WHEN DOOR IS OPERATED. SUSPECT SLIDE IMPROPERLY INSTALLED. REPOSITIONED GIRT PER MM 25-61-35 PG 208, AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080721 NM 2008 7 21 SWAA083490 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083498 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083506 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083505 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8L AND STR 5L. REMOVED AND REPLACED STRINGER CL IP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083521 1 20080625 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER TEE CHORD CRACKED AT BS 724, LBL 25. REMOVED AND REPLACE D TEE CHORD PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083523 1 20080625 A 5315 6545834 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED BETWEEN BS 326 AND BS 329, LBL 45. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 20080721 2008 7 21 SWAA083529 4 20080625 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083533 1 20080625 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503D, STR 16R. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20080721 2008 7 21 SWAA083534 4 20080625 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 30544 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPL ACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 PID2008F00000 1 20080620 A 3350 20131A BATTERY PACK BOEING 767 767277 1385128 NM EMERGENCY LIGHTS INOPERATIVE A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 767MW 22694 RT EMERGENCY ESCAPE SPOILER SQUIB DOES NOT TEST PROPERLY. REPLACED RT EMERGENCY ESCAPE SPOILER SQUIB BATTERY ASSY. OPS CHECK GOOD IAW AMM 25-65-17. (K) 2 L 7 2 4F RT A1NM 20080925 NM 2008 9 25 08FDEA03803 1 20080910 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 623FE 48794 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIA HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRA CK INDICATIONS AT HOLE A. MAIN CARGO DOOR LOWER JAMB, FOR CRACKED BOLT HOLE NR A AT NR 2 SUPPORT FITTING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL 1. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 EU 2008 9 25 08FDEA03813 1 20080911 A 5347 A25775039204 TRACK AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 CORROSION FOUND ON ROLLERTRACK C54-56 LT. A REPAIR IAW SRM 53-10-15 FIG 202 IS NOT POSSIBLE. REPAIR PERFORMED BY CUTTI NG THE ROLLER TRACK AT C 55, INSTALLING TWO SEPARATE L- PROFILES ON CROSSBEAM IAW RAS/EFW/900089/2008 ISS A, APPROVED BY EA 6-5316-123087. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03814 1 20080911 A 5347 A25775049204 TRACK AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 CORROSION FOUND ON ROLLERTRACK C54-56 RT. A REPAIR IAW SRM 53-10-15 FIG 202 IS NOT POSSIBLE. REPAIR PERFORMED BY CUTT ING THE ROLLER TRACK AT C 55, INSTALLING TWO SEPARATE L- PROFILES ON CROSS BEAM IAW RAS/EFW/900090/2008 ISS A, APPROVED BY EA 6-5316-123089. 2 L 7 2 4F RT A35EU 20080925 WP 2008 9 25 08FDEA03355 1 20080809 A 3260 PROXIMITY SENSOR DOUG MD10 MD1010F 3022112 WP MLG OUT OF ADJUST A FDEA O OTHER N FALSE WARNING DE DESCENT 1 CE 21 395FE 46629 DURING DESCENT WHEN SPEED BRAKE DEPLOYED RIGHT MAIN GEAR UNSAFE LT, RED LT DISPLAYED. RED SHOWING ON SD TOO. NO ABNORM AL YAW FELT. GEAR EXT NORMAL ALL GREEN. SWUNG GEAR. FOUND WING DOOR NOT FAIRED (DN .25"). ADJ WING DOOR TO FAIRED. REF MM 32-14-01-2. CHECKED GEAR DOOR GAPS. GAPS OK. CHECKED HOOK AND ROLLER CLEARANCE. CLEARANCE OK. FOUND PROX SEN SOR GAP AT .230 INCH RESHIMMED TO .180 INCH. SWUNG GEAR ALL IND AND CLEARANCES OK MD10 MM 32-34-03-2. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03303 1 20080807 A 5311 ACA00503 FRAME DOUG DC10 DC1030F 3023504 WP ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 LT AIR COND COMPT FOUND DEEP WEAR ON FRAME. REPAIRED AREA IAW SRM 53-00-00 FIG 4A VOL I. 2 L 7 3 4F RT A22WE 20080926 EU 2008 9 26 08FDEA03997 1 20080923 A 5415 A54611051200 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 400 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOR A REPAIR THE NEW PYLON SPIGOT FITTING FOR PYLON NR 1 HAVE BEEN DELIVERED WITHOUT ATTACHMENT HOLES AND SURFACE PROTEC TION. REPAIR PERFORMED BY DRILL SPIGOT FITTING BY COPY OF OLD PART, PERFORM SPRAYING SURFACE PROTECTION AND INSTALL F ITTING PER DRAWING R546-10351 IAW RAS/70513739/015/2008 ISS A, APPROVED BY EA 6-5451-123142. 2 L 7 2 4F RT A35EU 20080926 WP 2008 9 26 08FDEA04000 1 20080923 A 5411 AUB710740 RIB DOUG MD10 MD1010F 3022112 WP NR 3 PYLON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 3 PYLON PANEL 489 AL FWD RIB IS CHAFED. REMOVED & REPLACED RIB IAW DWG AUB 7107 & SRM 51-35-01. 2 L 7 3 4F RT A22WE 20080926 EU 2008 9 26 08FDEA04002 1 20080923 A 5415 A54612546 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSION ON PYLON NR 1 UPPER AND LOWER SPIGOT FITTING AROUND BEARING SEAT. REPAIR PERFORMED BY INSTALLATION OF C ORROSION RESISTENT FITTING IAW SB A300-54-6017, APPROVED BY EA 6-5451-123011. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA04003 1 20080923 A 5415 A54612546 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSION ON PYLON NR 2 UPPER AND LOWER SPIGOT FITTING AROUND BEARING SEAT. REPAIR PERFORMED BY INSTALLATION OF C ORROSION RESISTENT FITTING IAW SB A300-54-6017, APPROVED BY EA 6-5451-123011. 2 L 7 2 4F RT A35EU 20080926 WP 2008 9 26 08FDEA03994 1 20080922 A 5340 AJC7236517 FITTING DOUG MD10 MD1010F 3022112 WP BS 1997 L50L GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 FOUND WASTE COMPARTMENT BS 1997, LONGERON 50L, INBD AND OUTBD SIDES ARE GOUGED. REMOVED LONGEROON END FITTING IN REF T O SRM 51-33-01. SMOOTHED OUT THE GOUGES IN REF TO SRM 53-00-01. AREA IS OUT OF LIMITS IN REF TO SRM 53-00-01. LOCATED ; DRILLED & DEBURRED NEW AJC 7236-517 LONGERON END FITTING IN REF TO SRM 51-33-01. APPLIED TOP COAT IN REF TO SRM 51-21 -01. INSTALLED LONGERON END FITTING IN REF TO SRM 51-33-01. 2 L 7 3 4F RT A22WE 20080926 WP 2008 9 26 08FDEA03995 1 20080922 A 5313 AEA04511 LONGERON DOUG MD10 MD1010F 3022112 WP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 CENTER PIT LONGERON 50R OUTBD SIDE HAS CORROSION ON THE INNER FLANGE. REMOVED LT & RT AFT ADF PANELS IAW SRM 51-31-01. REMOVED 2 FRAME SECTIONS; 4 EA SPLICES AND 4 EA SUPPORTS IAW SRM 51-33-01 & SRM 51-35-01. REMOVED DAMAGED LONGERON FIT TING 50R IAW SRM 51-35-01. LOCATED AND DRILLED NEW LONGERON FITTING & INSTALLED FITTING & SUBSTRUCTURE IAW SRM 51-35-01 . INSTALLED ADF PANELS IAW SRM 51-31-01. 2 L 7 3 4F RT A22WE 20080926 EU 2008 9 26 08FDEA03996 1 20080922 A 7120 A5461092600000 MOUNT AIRBUS 310 A310222 3930315 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 NR 1 PYLON, ENGINE AFT ATTACHMENT BEAM LOWER SURFACE INBD AND OUTBD FAYING SURFACES HAVE CORROSION. ABRASIVE BLASTED EN GINE MOUNT IAW AIRBUS A310-200 SRM 51-74-10; PG 208. CONTINUED BLENDING TO REMOVE CORROSION IAW AIRBUS A310-200 SRM 51- 74-10. FOUND TO BE OUT OF LIMITS IAW AIRBUS A310-200 AMM 54-51-00. MAX ALLOWABLE , 0.020. AMOUNT REMOVED, 0.080. ORD ERED AND RECEIVED A NEW ENGINE MOUNT. REMOVAL AND INSTALLATION OF THE MOUNT IS ACCOMPLISHED ON NON-ROUTINE N01193. NO FURTHER ACTION IS REQUIRED. 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 2008UALA05786 1 20080916 A 2841 INDICATION SYS BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FUEL QTY MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 785UA 26954 GOT UNBALANCED FUEL EICAS TWICE WITH FAULTY R FUEL QUANTITY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080926 EU 2008 9 26 2008UALA05788 1 20080918 A 2612 FIRE LOOP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 NACELLE FAULTED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 435UA 613 FIRE LOOP A FAULT DISPLAYED ON UPPER ECAM SCREEN, ENG 2. FOUND FIRE DETECTOR UNIT FAULTY. REPLACED UNIT. TESTS OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080926 NE 2008 9 26 2008UALA05789 2 20080918 A 7261 SEAL BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE GEN DRIVE LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 216UA 30549 NR 2 ENG HAS EVIDENCE OF OIL LEAK ON CORE COWL. RAN ENG AND FOUND BACK UP GEN DRIVE DRAIN TUBE LEAKING. REPLACED BACK UP GEN DRIVE SEAL. REPLACED BUG. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080923 EU 2008 9 23 08FDEA03143 1 20080729 A 5321 B5327046101800 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN DECK FLOORBOARD, RIGHT SIDE NR 252 CF IS DAMAGED. FABRICATED NEW FLOORBOARD NR 232 CF IAW FEDEX DWG SRZ 25-005; RE V "G". 2 L 7 2 4F RT A35EU 20080721 EU 2008 7 21 V2J2008F00002 1 20080703 A 2612 M3901622007 RELAY PIAGIO P180 P180 6960204 EU PWA PT6 PT6A66 52043 NE FIRE DETECTION LOCKED E V2JA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 15 102SL 5152 1052 RT ENGINE FIRE INDICATION AFTER TAKEOFF. (K) 1 H 7 2 3O 4 T RT A59EU E26NE 20080721 2008 7 21 SWAA083621 4 20080630 A 2565 63550 SLIDE BOEING 737 73776Q 13845AA NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 551WN 30280 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SIDE PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083622 1 20080630 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 L1 DOOR EMERGENCY EXIT LIGHT ASSY FELL OFF. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083804 1 20080713 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 14L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083859 1 20080713 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND NLG W/W LT CEILING PANEL WEB CRACKED. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080721 EA 2008 7 21 A6WA200840351 1 20080420 A 4930 O-RING CNDAIR CL600 CL6002B19 1900309 EA APU FUEL LINE LEAKING A A6WA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 13 433AW 7289 STRONG FUEL ODOR THROUGHOUT CABIN AND COCKPIT SOMETIME AFTER APU STARTED ON ARRIVAL. FOUND APU FUEL LINE LEAKING. WITH APU OFF, FUEL LEAK STOPS. REF 201527/4 FOR MEL. R&R LOWER SOV ELBOW & O-RING IAW AMM 49-31-01. OPS AND LEAK CHECK GOOD . 2 L 7 2 4F RT A21EA 20080721 NM 2008 7 21 SWAA083795 1 20080708 A 3350 101073 LENS BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED SPV CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080721 EA 2008 7 21 A6WA200840358 1 20080419 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 13 443AW 7781 REAR PRESSURE BULKHEAD WEB CRACK FS 621 LBL 45 BTWN WL 106.17 AND WL (LINTEL ATTACHMENT FITTING). REAR PRESSURE BULKHE AD WEB FS 621 LBL 45 BTWN WL 106.17 AND WL 113.33 REPAIRED IAW REO 601R-53-61-1230 REV D. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840383 1 20080506 A 5420 STRIP CNDAIR CL600 CL6002B19 1900309 EA LT NACELLE GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 LT ENGINE UPPER NOSE ACCESS COWL AFT EDGE STRIP GOUGE. LT UPPER ENGINE COWL, AFT EDGE STRIP REPLACED IAW CMM 71-14-01-3 00-814-A01. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840418 1 20080512 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 442AW 7778 PAX DOOR TOP STEP AFT LOWER CORNER IS CRACKED. PAX DOOR TOP STEP AFT LOWER CORNER REPAIRED IAW REO 601R-52-11-702 REV A . 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840392 1 20080502 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 CRACK EXISTS ON INTERCOSTAL FS 621 TO 625 STR R14. REPLACED IAW SRM 51-42-06. (A) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840373 1 20080430 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 INTERCOSTAL FS 484 CRACK AT LBL 27 AND LBL 36. INTERCOSTAL FS 484 AT LBL 27 AND 36 ANGLE INSTALLED IAW REO 601R-53-41-0 59 REV A. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840376 1 20080430 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 574-621 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 CORROSION EXISTS ON LOWER SILL OF CARGO DOOR FS 574 TO FS 621 LBL 45. CORROSION REMOVED ON LOWER SILL OF CARGO DOOR FS 574 TO FS 621 LBL 45 IAW SRM 51-21-06. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840393 1 20080429 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 CRACK EXISTS ON PILOT BULKHEAD FRAME FS 280 LBL 9. REPAIRED IAW REO 601R-53-11-171 REV D. (A) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840399 1 20080505 A 2620 365000183 EXTINGUISHER CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY DISCHARGED A A6WA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 440AW 7766 CARGO BOTTLE LOWER MESSAGE IN FLIGHT. COMPLIED WITH QRH. R&R LT CARGO FIRE BOTTLE IAW AMM 26-25-01. CHECKS GOOD. NO AIR LEAKS FOUND AND NO SMOKE PRESENT IN CARGO BAY. OK FOR SERVICE. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840314 1 20080404 A 5340 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 718 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 AT FS 718 RT SIDE, NR2 HYDRAULIC MANIFOLD SUPPORT BRACKET FOUND CRACKED IN AFT LOWER CORNER. PERFORMED REPAIR AT FS 71 8.00 RT SIDE NR2 HYDRAULIC MANIFOLD SUPPORT BRACKET IAW REO 601R-53-62-031 REV A. (A) 2 L 7 2 4F RT A21EA 20080923 EU 2008 9 23 08FDEA03483 1 20080818 A 5711 A57140885104 SPAR AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON LT MLG FWD PICK UP FITTING AREA ON REAR SPAR (HOLE NR 8, NR 13). REPAIR PERFORMED BY BLEND OUT THE C ORROSION IAW RAS/BAE/1006539/2008 ISS A, APPROVED BY EA 6-5751-1210094. 2 L 7 2 4F RT A35EU 20080923 EU 2008 9 23 08FDEA03484 1 20080818 A 5743 A57242391 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON LT MLG FWD PICK UP FITTING HOLE NR 8 AND NR 13. REPAIR PERFORMED BY BLEND OUT THE CORROSION, OVERSIZ E THE HOLES IAW DRAWING R572-40266 AND INSTALLING BOLTS A228S32X IAW RAS/BAE/1006539/2008 ISS A , APPROVED BY EA 6-57 51-1210094. 2 L 7 2 4F RT A35EU 20080923 EU 2008 9 23 08FDEA03485 1 20080818 A 5230 STRUCTURE AIRBUS 300 A300F4605R 3930327 EU CARGO DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 650FE 726 AFT CARGO DOOR BETWEEN LOCKING HOOKS NR 4 AND 35 WEB IS PUNCTURED. REMOVED DAMAGE PER A300-600 SRM 52-32-11. ACCOMPLIS HED BHEC INSPECTION OF THE DAMAGED AREA PER NTM 51-10-01. NO DEFECTS NOTED. GENERATED RFTS NR N650FE -1-31253. RECEIV ED FINAL RFTS N650FE-1-31253. INSTALLED FASTENER PER A300-600 SRM 51-40-21. ALODINED; PRIMED AND PAINTED PER A300-600 SRM 51-21-10. 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 2008UALA05790 1 20080919 A 3397 P10225027001 WIRE HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EEL INOP, ALL SEATS 1J THRU 5J. REPAIRED HARNESS AT 1J. 2 L 7 4 4F 4 F RT A20WE E24NE 20080926 NM 2008 9 26 2008UALA05791 1 20080919 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 1A INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY EXIT EEL LIGHT INOP, AT SEAT 1A AFT LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080926 NM 2008 9 26 2008UALA05796 1 20080919 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHTS INOP, SEAT 2A AFT SECTION. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 20080926 NM 2008 9 26 2008UALA05797 1 20080919 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHTS INOP, SEAT 5F BOTH SECTIONS. 2 L 7 4 4F 4 F RT A20WE E24NE 20080926 NM 2008 9 26 2008UALA05798 1 20080919 A 4920 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU SPARKS A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 549UA 25397 SEVERAL LARGE SPARKS SHOOTING OUT OF THE APU TAIL PIPE. FOUND INTERNAL TURBINE FAILURE. REPLACED APU 2 L 7 2 4F 4 F RT A2NM E17NE 20080926 NM 2008 9 26 2008UALA05799 1 20080919 A 3350 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 937UA 26668 EMERGENCY LIGHTS IN FRONT OF THE AFT GALLEY IS IN OP. FOUND PINS GOING TO EEL STRIP BROKEN. REPLACED EMERGENCY LIGHT STRIP AND REPLACED TWO SIDED TAPE FOR MERGENCY LIGHT STRIP. OP CHECKED OK. 2 L 7 2 4F 4 F RT A16WE E2GL 20080926 WP 2008 9 26 08FDEA03251 1 20080805 A 5312 NCA624625 BULKHEAD DOUG DC10 DC1030F 3023504 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 RT AIR COND COMPT FOUND CRACK ON VERTICAL WEB. 2 L 7 3 4F RT A22WE 20080926 EU 2008 9 26 08FDEA03823 1 20080911 A 5321 A5327996300200 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 BULK CARGO PIT FLOOR PANEL 161 GF HAS NUMEROUS AREAS OF DELAMINATION AND DENTS. FABBED NEW FLOOR PANEL IAW DWG SRZ 25-0 05; REV "G". MATERIAL ID A402H35039-003 IAW DWG SRZ 25-005; REV "G". PART MARKED IAW GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 08FDEA03631 1 20080829 A 5330 655457719 SKIN BOEING 727 727227 1384078 NM BS 720C-720D CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 CRACK AT FUSELAGE SKIN FWD OF STA 720D AND O/B OF STR 27R ABOVE RT RAM AIR DUCT REMOVED CTR FAIRING AT STA 720D, AIR DUC T AND 2 SUPPORT BRACKETS FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGED AREA DIM 4" PER 3". FABRICATED REPAIR DOUBLER AN D 2 REPAIR FILLERS IAW SRM 53-30-3 FIG 1 AND 53-30-2 FIG 3. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-30-1 FIG 1. REINSTALLED REMOVED PARTS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20080926 NM 2008 9 26 08FDEA03633 1 20080828 A 2782 269002916P ACTUATOR BOEING 727 727233 138408A NM SLAT SYSTEM FAILED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 CE 21 281FE 22348 NR 8 SLAT FAILED TO RETRACT NORMALLY. LED AMBER ON FRONT PANEL AND S/O PANEL. REMOVED PANELS ON EACH SIDE OF ACTUATOR. FOUND WIRING CLAMPS LOOSE TIGHTENED. WILL CHANGE ACTUATOR OR SWITCH FOR MOCC. REPLACED NR 8 SLAT ACTUATOR REF MM 27- 81-032-4. OPS AND LEAK CK GOOD, NO LEAKS NOTED AT THIS TIME. HYD QTY STILL CKS GOOD AT THIS TIME. INSTALLED CLOSE OU T PANELS REF SMP. ACFT OK FOR SERVICE. 2 L 7 3 4F RT A3WE 20080926 WP 2008 9 26 08FDEA03636 1 20080829 A 5347 AGA7551504 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 40061 46973 FOUND SEVERE EXFOLIATION CORROSION ON SEAT TRACK AT STA 1923 X=-57, Z=-19. REPAIR IAW SRM 53-70-00 VOL 1 FIG 13 SHEET 1 -2. 2 L 7 3 4F A22WE 20080926 EU 2008 9 26 08FDEA03281 1 20080806 A 5230 B7327028100200 PANEL AIRBUS 300 A300F4605R 3930327 EU CARGO DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DOOR PANEL NR 251 YG; LOWER SURFACE IS CRACKED AND THE UPPER SURFACE IS PUNCTURED. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 08FDEA03308 1 20080807 A 5310 CREASE BEAM BOEING 757 757236 1384971 NM CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 MAIN CABIN, CREASE BEAM INBD CHORD BS 395-BS 418 LBL 65 HAS CORROSION ALSO SEE BS 331 AT FASTENER HOLE FOR CORROSION. R EMOVED CORROSION IAW SRM 51-10-02, L=VARIOUS AREAS TOTAL 6.5'', W=1.5'', D=0.035. FOUND TO BE OUT OF LIMITS NO SRM REFE RENCE. REMOVED CREASE BEAM IAW SRM 51-40-02, FABRICATED NEW CREASE BEAM FROM MAE TRAVELER T/8 748853. LOCATED AND DRIL LED HOLES IAW SRM 51-40-05. TREATED AND PRIMED IAW SRM 51-20-01, PAINTED IAW MM 51-20-00-7. INSTALLED CREASE BEAM IAW SRM 51-40-02, STA 324-395, CREASE BEAM FROM BS 395-418. DELETED BY P TO F MOD, MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20080926 EU 2008 9 26 08FDEA03326 1 20080808 A 5321 R532B361800000 FLOORBOARD AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOORBOARD IS CRACKED AT BS 1552, LBL 40. REPAIRED CABIN FLOOR PANEL 231 HG BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SKID TAPE IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03845 1 20080911 A 5330 A5377601720200 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 EXTERIOR UPPER FUSELAGE SKIN HAS STATIC DISCHARGE BETWEEN FRAME 36 AND FRAME 37; STRINGER 1 R STRINGER 2 R. REMOVED D AMAGE BY WAY OF DRILLING A 5/32 HOLE IAW SRM 53-10-12; FIG 220. ACCOMPLISHED A BHEC INSPECTION OF THE DRILLED HOLE IAW NTM PT 6 51-10-01. INSTALLED RIVET IAW SRM 53-10-12; FIG 220. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03846 1 20080911 A 5330 A5377601720200 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 EXTERIOR UPPER FUSELAGE SKIN HAS STATIC DISCHARGE BETWEEN FRAME 35 AND FRAME 36; STRINGER 1R AND STRINGER 2 R. REMOVED DAMAGE BY WAY OF DRILLING A 5/32 HOLE IAW SRM 53-10-12; FIG 220. ACCOMPLISHED A BHEC INSPECTION OF THE DRILLED HOLE IAW NTM PT 6 51-10-01. INSTALLED RIVET IAW SRM 53-10-12; FIG 220. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03847 1 20080911 A 5330 A5377608020200 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 EXTERIOR UPPER FUSELAGE SKIN HAS STATIC DISCHARGE AT FRAMES 26/32; STRINGER 1 R AND 2 R. REMOVED AND REPLACED RIVET IA W SRM 53-10-12; FIG 220. ACCOMPLISHED A BHEC INSPECTION OF THE FASTENER HOLE IAW NTM PT6 51-10-01. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03327 1 20080808 A 5321 R532B371900000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 242 AK IS DAMAGED. REPAIRED CABIN FLOOR PANEL 242 AK BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARK ED AND APPLIED NON-SKID TAPE IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 08FDEA03889 1 20080916 A 5210 SKIN BOEING 727 727227 1384078 NM L1 DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 DOOR L-1, INTERIOR AFT SKIN CRACKED AT 2 STOP PIN LOCATIONS (MKD). REPAIRED 2 DAMAGE AREA'S AT DOOR L-1 INTERIOR AFT SK IN STOP PIN LOCATIONS. HFEC IAW NDT MANUAL PART 6 51-00-00 FIG 23. TOOLING ID NR 0065 19 SEP 08. FOUND CRACKED. REMO VED DAMAGE AND REPAIR 2 AREA WITH DOUBLERS REF SRM 51-40-2 PG 1-6 FIG 1 AND REF SRM 52-10-1 PG 1 FIG 1 ITEM 15. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080715 NM 2008 7 15 08FDEA02127 1 20080603 A 5350 652557965 FRAME BOEING 727 727233 138408A NM WING TO BODY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 CORROSION ON TOP OF WING TO BODY FAIRING FRAME WORK AT TWO FWD ADF ANTENNA LEAD POSITION CLAMP ATTACH AT FS 730F, RBL 10 , INBOARD OF RT RAM AIR DUCT REMOVED PANELS REF SRM 51-30-2, REMOVED CORROSION REF SRM 53-10-01. FOUND TO BE OUT OF LIM ITS REF SRM 51-20-01. FABRICATED NEW Z-ANGLE REF SRM 53-10-1. REPLACED Z-ANGLE REF 51-30-02. REPLACED PANELS REF 51-3 0-02. THIS IS CLASSIFIED AS A MINOR. 2 L 7 3 4F RT A3WE 20080715 NM 2008 7 15 ASAA0843003 1 20080514 A 5753 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 LT WING INBD FORE FLAP LOWER SURFACE HAS NUMEROUS SMALL DENTS BETWEEN 1ST AND 2ND TRACK. PREPARED DAMAGED AREA FABRICAT ED DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083853 1 20080709 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083842 1 20080710 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 DURING SCHEDULED HC2 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080715 2008 7 15 SWAA083837 4 20080713 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083813 1 20080709 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. R&R LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080716 WP 2008 7 16 DHL2008807520 1 20080501 A 5340 FITTING DOUG DC8 DC873F 302199F WP BS 834.5 L18R CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 MAIN CARGO COMPT FRAME FITTING CRACKED 1.250 INCH STA 834.500 L-18R (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1 -0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FI TTING IAW SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 20080716 SO 2008 7 16 C2XA08TY052 1 20080523 A 5730 SKIN EMB 145 EMB145LR 3260212 SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 26545 145558 LEFT WING SKIN CENTER CUTOUT AT I/B SPOILER HAS A CRACK. CUT OUT DAMAGE AREA, FABRICATED FILLER, DOUBLER AND TRIPLER. ALODINED, PRIMED AND PAINTED IAW EC 5740-01158. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20080716 SO 2008 7 16 C2XA08TY053 1 20080523 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11536 145520 NR 4 EMERGENCY BATTERY INOP. REMOVED AND REPLACED BATTERY IAW EMB 145 MM 33-50-04, OPS CHECK GOOD. AIRCRAFT RELEASED A ND RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20080721 EU 2008 7 21 08FDEA02540 1 20080627 A 5321 B5327060401500 FLOOR PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 242 ZJ IS CRACKED & CRUSHED. FABBED A NEW FLOOR PANEL; POTTED EDGES; CURED; SANDED; POTT ED INSERTS; APPLIED NON-SKID & PART MARKED IAW DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080721 NM 2008 7 21 SWAA083794 1 20080709 A 3350 079123 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 EEPLS AFT COVER MISSING. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 20080721 WP 2008 7 21 08FDEA02928 1 20080716 A 5712 RIB DOUG MD10 MD1010F 3022112 WP LT WING LE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING L/E INTERIOR RIB IS CRACKED AT THE STOP DRILL AT APPROX WING STA 683 (INBD OF THE NR 5 SLAT CENTER TRACK). 2 L 7 3 4F RT A22WE 20080721 NM 2008 7 21 SWAA083793 1 20080709 A 2560 PL2230LH00 STRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULE HC2 CHECK, FOUND EEPLS STRIP WORN AT 13C. CLEANED EEPLS STRIP PER MM. 2 L 7 2 4F RT A16WE 20080721 EU 2008 7 21 08FDEA02947 1 20080717 A 3240 C20101610003 CONTROL UNIT AIRBUS 310 A310 EU MLG BRAKES MALFUNCTIONED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 21 407FE 2724 2724 254 NORMAL BEFORE T/O CHCK LIST, CLEARED FOR T/O RWY 77C DFW PASSING 40 KIAS GOT RED ECAM PARKING BRAKE SET. ABORTED T/O. PARKING BRAKE HANDLE CHECKED STOWED, BUT MOVED FURTHER DOWN 1/8 INCH /- NO DRAGGING BRAKI NG FELT ON INITIAL ROLL . HO WEVER CLEAR OF RWY BRAKES 4/7/8 WENT UP TO 330 (NR 3 STAYED AT 65) BRAKES 1/2/ 5/6 UP TO <100. RR'D BRAKE SYSTEM CONT ROL UNIT PER AMM 32-42-72-4. PREMATURE REMOVAL/INSTALLATION OFF MFG C20101610-003. 2 L 7 2 4F RT A35EU 20080721 EU 2008 7 21 08FDEA02879 1 20080715 A 5315 A53974322200 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON CROSSBEAM C 61 SPLICE REPAIR PERFORMED IAW. SRM 53-10-15 FIG.205 2 L 7 2 4F RT A35EU 20080721 NM 2008 7 21 SWAA083768 1 20080708 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 8R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083779 1 20080708 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085063 1 20080914 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085011 1 20080911 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 DURING SCHEDULED HC2 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 CALA0800882 1 20080916 A 5320 101391107 STIFFENER BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 Z-ANGLE STIFFENER FROM LBL 3.54 TO LBL 18.32 ADJACENT TO AFT PRESSURE BULKHEAD HAS OVERHEAT DAMAGE. REMOVED DAMAGED Z-A NGLE STIFFENER IAW SRM 51-A01-02. FABRICATED NEW STIFFENER IAW DWG 65-46812 INSTALLED NEW Z-ANGLE STIFF IAW SRM 51-40-0 2 AT LBL 3.54-LBL 18.32 AT AFT PRESSURE BULKHEAD. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 CALA0800883 1 20080916 A 5320 6976736U1 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 1016 OVERHEATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INTERCOSTAL AT LBL 18.32 FROM 1016 TO AFT PRESS BULKHEAD HAS OVERHEAT DAMAGE. REMOVED INTERCOSTAL IAW B737 SRM 51-40-02 . FABRICATED INTERCOSTAL IAW BAC DWG 65C32677. INSTALLED INTERCOSTAL IAW B737 SRM 51-40-02 AT LBL 18.32 AFT PRESS BULK HEAD. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 CALA0800884 1 20080916 A 5320 6546568559 STIFFENER BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 STIFFENER ON AFT PRESS BULKHEAD JUST I/B OF APU BLEED DUCT HAS OVERHEAT DAMAGE FROM FLOOR LEVEL DOWN TO Y-CORD. REMOVED STIFFENER ON AFT PRESSURE BULKHEAD JUST INBOARD OF APU BLEED DUCT AND INSTALLED NEW STIFFENER PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 CALA0800885 1 20080916 A 5320 6546568U551 STIFFENER BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 STIFFENER ON AFT PRESS BULKHEAD JUST O/B OF APU BLEED DUCT HAS OVERHEAT DAMAGE FROM FLOOR LEVEL DOWN TO Y-CORD. REMOVED STIFFENER FROM AFT PRESSURE BULKHEAD JUST OUTBOARD OF APU BLEED DUCT AND INSTALLED NEW STIFFENER PER 13-737-300 SRM 51- 40-02. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085012 1 20080911 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 DURING SCHEDULED HC2 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085013 1 20080911 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 DURING SCHEDULED HC2 CHECK, RT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085018 1 20080911 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085019 1 20080911 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085020 1 20080911 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 303 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 303, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085021 1 20080911 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 1010 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 4L CRACKED AT BS 1010. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080929 NM 2008 9 29 UPS08553304 1 20080815 A 5347 CARGO TRACK BOEING 757 75724APF 1384969 NM BS 335-440 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 MAIN CARGO SEAT TRACK IS CORRODED, BS 335-440, WL 208 AT O/B FLANGE AND RADIUS. REPAIRED PER ER 08-2 777. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 UPS08553305 1 20080815 A 5347 CARGO TRACK BOEING 757 75724APF 1384969 NM BS 351-416 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 MAIN CARGO FLOOR SEAT TRACK IS CORRODED BS 351-416, RBL 25, WL 208 ON O/B FLANGE AND RADUIS. REPAIRE D PER ER 08-2775. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 SWAA085069 1 20080914 A 5330 6549274 SKIN BOEING 737 7373A4 1384585 NM BS 492 S27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 492, STR 27R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080929 NM 2008 9 29 2008UALA05706 1 20080913 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT LIGHT INOP AT DOOR 2 LEFT CEILING ENTRY LIGHT. FOUND BATTERY INOP. REPLACED BATTERY. OPS CHECKS NORMAL . 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 EU 2008 9 29 2008UALA05709 1 20080913 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 454UA 1104 EMERGENCY LIGHTS FAILED CAPACITY TEST, TEST FAULTS EPSU EXT EMERGENCY LEFT. POWER SUPPLY FAILED TEST. REPLACED EPSU LE FT OVERWING UNIT. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080929 NM 2008 9 29 2008UALA05714 1 20080913 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1520 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 AFT PIT FRAME AT STA 1520 (LEFT SIDE) IS DENTED AND HAS GOUGES AT LOWER SECTION. MAJOR REPAIR ACCOMPLISHED. REMOVED PR ODUCTION SPLICE AND DAMAGED SECTION OF FRAME. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080929 NM 2008 9 29 2008UALA05720 1 20080913 A 2620 G718505342004051 CONTROL PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE DETECTOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 372UA 24637 AFTER REPLACEMENT OF NR 2 CARGO FIRE BOTTLE, SQUIB ACTIVATED WHEN CIRCUIT BREAKER PUSHED BACK IN. FIRE BOTTLE AND SQUIB WILL REQUIRE REPLACEMENT. CONSTANT .5 VOLTS AT SQUIB CONNECTOR D9497 BETWEEN PIN 1 AND PIN 2. REPLACED CARGO FIRE CON TROL PANEL, NR 2 FIRE BOTTLE, DIVERTER VALVE, METERING VALVE, SQUIBS AND INLINE FILTERS. WIRING CHECKED NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20080716 NM 2008 7 16 SWAA082882 1 20080528 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 6 ABC. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 ZZDA2008117 1 20080604 A 3397 CONNECTOR BOEING 717 717200 1383700 NM EMERGENCY LIGHT MALFUNCTIONED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 946AT 55009 L-1 DOOR EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. REF CARD NR 339. FAILED TO OP CHECK. REINSTALLED CONNECTOR FOR L-1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY, REF CH 33-51-18 BOEING 717 MM. 2 L 7 2 4F TR A6WE 20080716 NM 2008 7 16 EMB08005 1 20080530 A 2560 P4010030 BATTERY EMB ERJ190 ERJ190100IGW 3260408 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 959UW 19000166 PHL - THE FORWARD FLIGHT ATTENDANT FLASHLIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY IN THE FLASHLIGHT. 2 L 7 2 4F RT A57NM 20080716 NM 2008 7 16 2008UALA03049 1 20080527 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1000 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 MAIN CABIN CREASE BEAM AT STA 1000 LBL 71 IS CORRODED. MAJOR REPAIR ACCOMPLISHED, REMOVED AND REPLACED WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 20080716 WP 2008 7 16 UPS08852353 1 20080424 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 PNEUMATIC DUCT CHAFING AT RIGHT L/E INBOARD OF SLAT DOOR STA XFS 404.000. REPAIRED RIGHT L/E INBOAR D RIB AT XFS 404.000 IAW SRM 57-02-00-0, SRM 51- 01-08 AND SRM 51-03-03-01. 2 L 7 4 4F RT 4A25 20080716 EU 2008 7 16 08FDEA02037 1 20080530 A 5100 NONE AIRBUS 300 A300B4622R 3930312 EU NONE NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND OLD DOUBLER REPAIR ON FUSELAGE C 73, P45-46 RT DOUBLER REPAIR RENEWED IAW SRM 53-10-12 FIG 228. 2 L 7 2 4F RT A35EU 20080716 WP 2008 7 16 AALA200801296 1 20080513 A 2133 1036311 OUTFLOW VALVE DOUG DC9 DC982 3022082 WP CABIN PRESSURE INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 462AA 49592 DFW INFLIGHT T682/13MAY AUS TO ORD - CREW REPORTED CABIN PRESSURE LOSS. NO MASKS DEPLOYED. LANDED DFW WITHOUT INCIDENT . REPLACED BOTH CABIN SAFETY RELIEF VALVES. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20080716 NM 2008 7 16 UPS08652394 1 20080530 A 2810 FUEL SYS BOEING 767 76734AF 1385212 NM LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 01 311UP 27741 INSPECTION TYPE:ETOP DIVERSION, FUEL DISCREPANCY WITH ASSOCIATED INSUFFICIENT FUEL LEAK. 2 L 7 2 4F RT A1NM 20080716 NM 2008 7 16 2008UALA02983 1 20080525 A 2824 32C171 CHECK VALVE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUEL TANK MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 217UA 30550 FUEL TRANSFER PROBLEM FROM CENTER TO THE RIGHT TANK. WITH CENTER TANK FEEDING ENGINES, THE CENTER TANK PUMPED ENOUGH FU EL INTO THE RIGHT TANK TO CAUSE RIGHT FUEL TANK TO OVER FILL AND CAUSE FUEL, APPROX 3000FT TO DUMP OVERBOARD THRU FUEL V ENT. REPLACED RT FWD BOOST PUMP DISCHARGE CHECK VALVE, FUEL QTY PROCESSOR & FUEL CONTROL UNIT. OPS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080716 NM 2008 7 16 UPS08B52382 1 20080417 A 5311 FRAME BOEING 747 747400 13848AT NM BS 1140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:C RT BS 1140 TENSION TIE FRAME CRACKED MORE THAN 0.060". RT BS 1140 TENSION TIE FRAME REPLACED PER SRM 53-40-07. 2 L 7 4 4F RT A20WE 20080716 NM 2008 7 16 USAA920081141 1 20080524 A 5311 6546525 FRAME BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - NR O3C10753045/14, CRACKED FUSELAGE FRAME, BS 360, S16R. REPAIRED CRACKED FUSELAGE FRAM E, BS 360, S16R IAW US AIRWAYS EA 100485. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 2008UALA03030 1 20080526 A 5753 65B1553227 FAIRING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LT WING TE FLAP DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 179UA 25158 ON WALK AROUND FOUND DAMAGE TO OUTBOARD SIDE OF OUTBOARD FLAP CANOE FAIRING ON INBOARD LEFT FLAP. DAMAGE APPROX 8 INCHE S LONG BY 2 INCHES AT WIDEST POINT, ALSO TWO GRAZE MARKS BELOW DAMAGE 3 INCHES AND 4 INCHES LONG. ACCOMPLISHED PERMANE NT REPAIR REF SRM 57-53-70. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 NM 2008 7 16 SWAA082845 1 20080523 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080716 SO 2008 7 16 SIMA200814901 1 20080522 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER UK UNKNOWN 1 SW 21 687JS 14500846 DURING CPCP INSPECTION FOUND AFT BAGGAGE DOOR SILL CORRODED UNDER STAINLESS STEEL CUTOUT RETAINERS. MAINTENANCE REPLACE D BAGGAGE DOOR SILL IAW EMB SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20080716 NM 2008 7 16 USAA920081129 1 20080517 A 5310 65207270 DOOR FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - FORWARD CARGO DOOR CUTOUT FORWARD FRAME CRACKED, BS 440, S19R - S20R. REPAIRED FORWARD CARGO DOOR CUTOUT FORWARD FRAME, BS 440, S19R - S20R IAW US AIRWAYS EA 100440. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 UPS08M52379 1 20080519 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 1581 L52 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:2C CENTER CARGO COMP BILGE AREA FOUND CORROSION AT STA 1581 LONGERON 52 AS MARKED. REMOVED END FITTING, FABRICATED AND INSTALLED END FITTING IAW MD-11 SRM 51-31-01, 51-35-01, 53-00-01, AND 51-21-01. 2 L 7 3 4F RT A22WE 20080909 NM 2008 9 9 2008UALA04035 1 20080728 A 5310 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 813UA 858 BEAM 175 CORRODED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080716 NM 2008 7 16 GTIA0800070 1 20080425 A 5315 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 505NK 2485 AFT FUSELAGE FLOORBEAM AT Y254 BETWEEN FR68 AND FR70. REPLACED FLOORBEAM. 2 L 7 2 4F RT A28NM 20080716 EA 2008 7 16 SIMA200815103 2 20080525 A 7240 LINER RROYCE EMB 135 EMB135LR 3260305 SO RROYCE AE3007 AE3007A13 54166 EA COMBUSTOR CRACKED A SIMA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 738NR CAE311821 145401 CAE311821 ON FLIGHT 4599 IN CLIMB CREW EXPERIENCED A MOMENTARY HIGH ITT ON ENGINE NUMBER 1 GOING THRU 3000 FEET FOR 3600 FEET. C REW REDUCED THRUST AND ITT REMAINED IN NORMAL GREEN LIMITS. FADEC A WAS IN CONTROL OF ENGINE NUMBER ONE. FOUND NUMBER ONE ENGINE COMBUSTOR LINER HAS MISSING PIECES. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ENGINE NUMBER 1 IA W WORK CARD NR 71-00-00. ALL LEAK CHECKS AND RUN UP CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080716 SO 2008 7 16 FDKA200805209 1 20080523 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM FLT 5991 JFK-BWI, MAIN DOOR HARD TO CLOSE. MX LUBED DOOR ROLLERS, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 20080716 NM 2008 7 16 UPS08M52544 1 20080512 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM BS 1894 L40R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C AFT CARGO AT STATION 1894 LONGERON 40 RT CORROSION FOUND ON LONGERON AREA AS MARKED. CORROSION LONGER ON REMOVED PER SRM 53-10-00 FIG 1 VI REV35. HFEC C/O IAW NDTSPM R13 PT 06.10-01.001 ON TRIMMED EDGE AND FOUND NO CRACK EVIDENT. REPAIR LONGERON AND REPAIR SPLICE FAB PER SRM 53-10-00 FIG 2 VI REV 35 FPI C/O PER DPS 4.707 REV AW ON FABRICA TED REPAIR PART AND FOUND NO CRACK EVIDENT. NEW REPAIR SPLICE INSTALLED PER SRM 51-31-01 VII REV 35. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 2008UALA03040 1 20080527 A 5315 FLOORBEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 986 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 CABIN FLOOR FRAME CAP CORRODED AROUND FASTENER HOLES BS 986 WL208 RBL 24"-37". MAJOR REPAIR ACCOMPLISHED, REMOVED UPPE R "T" CAP. INSTALLED FLOORBEAM UPPER CAP SPLICE REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 20080716 SO 2008 7 16 FDKA200805208 1 20080523 A 2620 WARNING LIGHT EMB 145 EMB145LR 3260212 SO EXTINGUISHER MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 FDM FLT 6101 ROC - BAG EXTINGUISHING LIGHT STAYS ON AFTER TEST. MX RE-TESTED SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 20080716 WP 2008 7 16 IXXA08SMN146S 1 20080418 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 260 L22R MISREPAIRED B IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR LOCATED AT STATION FS 260 LONGERON 22.5 RIGHT. REMOVED FASTENE RS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, INTERNAL FI NGER DOUBLER, FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 53-2-1 FIGURE 7 SHEETS 1, 4 AND 5, 51-9-0 FIGURE 68A, 53-4-1 FIGURE 1 ITEM B, 51-1-11, 51-3-1, DC8 SRM 51-1-21, 51-1-20D, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 20080716 WP 2008 7 16 IXXA08SMN151S 1 20080415 A 5710 745897501 STRUCTURE DOUG DC8 DC871F 302199D WP ZONE 700 MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT XRS 74 EXTERNAL DOUBLER LEFT WHEEL WELL AFT OF MAIN LANDING GEAR TRUNNION. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICA TED EXTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PART IAW A D 90-16-05, DACO SB 57-58 DATED 01-19-08, DOUGLAS DRAWING 5758978 AND 5643410, DACO SRM 51-1-11, 51-1-21, 51-1-20D AND 5 1-3-1, DC8 SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 20080716 WP 2008 7 16 IXXA08SMN152S 1 20080418 A 5753 SKIN DOUG DC8 DC871F 302199D WP LT WING TE FLAP DENTED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP UPPER SKIN DENTED AT STATION XW 104.000 TO 115.000. REM OVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, BONDED DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC 8 SRM 51-1-11, 51-1-21, DC8 SRM 57-7-1 FIGURE 1 ITEM "A" AND "L", DC8 SRM 57-1-0 PAGE 1, 51-1-21, DC8 SRM 51-1-8B, DC8 S RM 51-1-9 TR NUMBER 51-142, AND 51-1-9A TR NUMBER 51-141. 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 2008UALA03065 1 20080528 A 5310 CREASE BEAM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 967-986 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 AFT GALLEY DOOR CUTOUT CREASE BEAM AT STR S- 17R CORRODED ON UPPER SURFACE FROM BS 967-986.5. MAJOR REPAIR ACCOMPLISHED : BLENDED CORROSION & FOUND BLEND OUT OF LIMITS. REMOVED AND REPLACED CREASE BEAM. 2 L 7 2 4F 4 F RT A16WE E2GL 20080716 NM 2008 7 16 2008UALA03067 1 20080528 A 5330 SKIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 904 S14L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 UPPER LT FUSELAGE SKIN STA 904 S-14L IS DENTED. MAJOR REPAIR ACCOMPLISHED, FABRICATED AND INSTALLED EXTERNAL DOUBLER, T RIPLER AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E2GL 20080716 NM 2008 7 16 2008UALA02897 1 20080519 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1420 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 AFT PIT STA 1420, STR 25L AND STR 26L, FRAME DENTED. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVE D DAMAGE, FABRICATED RPR AND INSTALLED IAW SRM 53-00-07. RPR 5 BY MECH 110694 AND INSP BY QC 409 ON NR 20299. THIS IS A CAT B RPR IN ZONE 2 REQUIRING SUPPLEMENTAL INSPECTIONS STARTING AT 25,000 FLT CYCLES AFTER INSTALLATION AND 11,000C TH ERE AFTER. THESE INSPS ARE BOTH VISUAL AND NDT PER SRM 53-00-07 RPR5 TABLE II CURRENT PTC IS 20417. 2 L 7 2 4F 4 F RT A2NM E17NE 20080716 NM 2008 7 16 2008UALA03044 1 20080527 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 DOOR R4 DOUBLER AFT AND BELOW HANDLE BOX CHAFED. MAJOR REPAIR ACCOMPLISHED, REMOVED DAMAGE. FABRICATED AND INSTALLED D OUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080716 EA 2008 7 16 S9BA2008022 1 20080529 A 3246 13000 FLOAT DHAV DHC6 DHC6300 2802606 EA MLG LEAKING A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 573SA 298 573 "OPEN" LEFT FLOAT BAY NR 6 LEAKING. REMOVED AND REPLACED FLOAT. WILL UPDATE AFTER FLOAT INSPECTION, EMERGENCY MEASURE EXECUTED NO. AIRCRAFT GROUNDED. FLIGHT NA. 1 H 7 2 3T RT A9EA 20080716 SO 2008 7 16 SIMA200814902 1 20080527 A 2810 2810051104 VALVE EMB 145 EMB145LR 3260212 SO FUEL VENT LEAKING A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 691AE 14500860 ON FLIGHT 3456 AFTER TAKEOFF, TOWER REPORTED A FUEL LEAK COMING FROM ONE OF THE WINGS. CREW DID NOT NOTICED ANY ABNORMA LITY. AT FL130 HE DID NOTICED A NORMAL FUEL BURN AND NO FUEL QUANTITY CHANGES. CREW ELECTED TO RETURN TO THE BLOCK. A IRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT WING FUEL VENT VALVE. LEAK CHECKED GOOD AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20080716 NM 2008 7 16 2008UALA02941 1 20080520 A 3350 68AT341 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 541UA 25253 EMERGENCY LIGHT SWITCH (TEST) AT L1 DOOR DOES NOT WORK. SUPPLEMENTAL DATA UPDATE CAUSE, SWITCH AT L1 INOP. REMOVED AND REPLACED SWITCH, CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080716 SO 2008 7 16 C2XA08IA0132 1 20080527 A 3320 7281000501 CONTROL MODULE EMB 145 EMB145XR 3260214 SO CABIN LIGHTS INOPERATIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 11109 145657 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT HALF OF THE CABIN LIGHTS WERE INOP, AND A BURNING SMELL WAS PR ESENT. MAINTENANCE REMOVED AND REPLACED THE CABIN LIGHT CONTROLLER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20080716 SO 2008 7 16 RAIA00805030 1 20080528 A 5210 MECHANISM EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 822HK 145069 POST FLT NR 5594 - STL - PASSENGER DOOR HARD TO OPEN. MAINTENANCE LUBED THE DOOR ROLLERS, LATCH MECHANISM AND PIVOTS. DOOR OPERATION CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080716 NM 2008 7 16 SWAA082932 1 20080530 A 2121 215301 GASPER FAN BOEING 737 7377H4 1384404 NM E&E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 792SW 27887 DECLARED EMERGENCY. FLIGHT CREW REPORTED SMELL OF SMOKE IN AFT CABIN. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 UPS08B52557 1 20080417 A 5311 65B0175224 FRAME BOEING 747 747400 13848AT NM BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:BCF RT BS 1180 TENSION TIE FRAME CRACKED ABOUT 0.040 INCH. RT BS 1180 TENSION TIE FRAME REPLACED PER SR M 53-40-07 REPAIR 4. 2 L 7 4 4F RT A20WE 20080717 NM 2008 7 17 UPS08552507 1 20080617 A 3350 COVER BOEING 757 75724APF 1384969 NM EEL SWITCH MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 428UP 25459 WITH OVERHEAD PANEL SWITCH IN ARMED POSITION, UNARMED LIGHT ILLUMINATED AND MESSAGE DISPLAYED. REPLACED SWITCH COVER A SSEMBLY. OPS CHECK NORMAL PER MM 33-51-00-05. 2 L 7 2 4F RT A2NM 20080717 NM 2008 7 17 UPS08M52500 1 20080430 A 5313 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C RT WING FUEL TANK UPPER STRINGER NR 10 END SUSPECT CRACK, HFEC INSP C/O PER DAC NDTSPM R13 06-10-01.00 1 AND FOUND CRACK APPROX 9 INCH CRACK AREA AT RT WING FUEL TANK UPPER STRINGER NR 10 END SLOTTED OUT PER SRM 57-20-00 FI G 10 VI R35. REPAIR ANGLES 02EA FAB PER SRM 57-20-00 FIG 10 VI R35. NEW FAB 02 EA ANGLES/ATTACHED SPLICE INSTALLED RT WING NR 10 STRINGER NR 10 PER SRM 57-20-00 FIG 10 VI R35 AND SRM 51-33-01 VII R35. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 UPS08M52501 1 20080430 A 5313 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C RT WING FUEL TANK UPPER STRINGER NR 12 END SUSPECT CRACK, HFEC INSP C/O PER DAC NDTSPM R13 06-10-01.0 01 AND FOUND CRACK APPROX 10 1/2 INCH. CRACK AREA AT RT WING STRINGER NR 12 END SLOTTED PER SRM 57-20-00 FIG 10 VI R35. NEW REPAIR ANGLES 02 EA FAB PER SRM 57-20-00 FIG 10 VI R35. NEW FAB 02EA REPAIR ANGLES/ATTACHED SP AND SRM 51-33-01 V II R35. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 HNAA0800182 1 20080523 A 3350 3351PS3 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 826EX 12097 65 389 EMERGENCY LIGHT AT ROW 4 OVERHEAD INOP. INSPECTED & FOUND 3351-PS3 BATTERY BAD. REMOVED AND REPLACED BATTERY. OPS CHE CK GOOD. 2 H 7 2 4T RT A13NM 20080717 WP 2008 7 17 IXXA08SMN133S 1 20080411 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 290 L35R MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIRS LOCATED AT STATION FS 290 LONGERON 35.5 RIGHT. REMOVED FASTEN ERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR.REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND CORROSION FOUND. FABRICATED REPAIR DOUBLER, TRIPLER, AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. I NSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08188 DATED 04/23/08, SEMAN DRAWING NUMBER ED-4756 DA TED 04/21/08, DC8 SRM 51-1-21, 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, 51-1-21, AND 5 1-3-1. 2 L 7 4 4F RT 4A25 20080717 EA 2008 7 17 CHQA200800098 1 20080525 A 2751 855D1009 POSITION SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT WING TE FLAPS FAULTY A CHQA O OTHER N FALSE WARNING DE DESCENT 1 GL 11 642BR 18037 12136 7356 GEE873284 FLIGHT 5621, CMH TO IAH, WHILE DESCENDING THROUGH 10,000 FT, FLAPS FAIL APPEARED ON EICAS WITHOUT THE FLAPS BEING ACTUAT ED. THE FLIGHT CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAULT TO THE LEFT BRAKE POSITION SENSING UNIT. THE SENSING UNIT WAS REPLACED AND THE FLAP SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 20080717 NM 2008 7 17 ASMF200805003 1 20080523 A 3230 1FA011342 SELECTOR VALVE BOEING 737 73776Q 13845AA NM MLG FAILED W ASMF O OTHER J WARNING INDICATION CR CRUISE 1 SW 23 997AM 18442 18442 30283 CAPTAIN REPORTED THAT DURING CRUISE AT 39,000 FEET, THE MAIN LANDING GEAR RED LIGHT TURNED ON AND MAIN LANDING GEAR GO D OWN WITH LEVER IN OFF POSITION, THEN LEVER WAS POSITIONED ON UP POSITION AND LIGHT TURNED OFF. MAINTENANCE PERSONNEL RE PLACED THE LANDING GEAR SELECTOR VALVE AND RT MAIN GEAR LOCK UP ASSY IAW MM 32-31-51 AND 32-32-31, OPERATIONAL TEST WAS CORRECT IAW MM 32-32-00, ALL CORRECT. 2 L 7 2 4F RT A16WE 20080717 SO 2008 7 17 FDKA200805212 1 20080530 A 3350 SIGN EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM FLT 6077 IAD-JFK. RIGHT EMERGENCY EXIT SIGN INOP. MX PERFORMED OPS CHECKS, NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 20080717 NM 2008 7 17 ASAA0853022 1 20080603 A 2432 893003 CHARGER BOEING 737 737890 1384527 NM E/E BAY MALFUNCTIONED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 583AS 3465 35681 AUX BATTERY SHOWS A 2 AMP CHARGE AND HAS NOT DECREASED TO ZERO. DC VOLTS SHOWS 27 CKD AUX BATT AND AUX BATT CHGR REF 24 31 31, OPS CKS OK WITHIN. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 CALA0800534 1 20080603 A 5315 147A5506 FLOORBEAM BOEING 737 737724 13844BY NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 STATION 986.5 FLOORBEAM UPPER CHORD HAS CORROSION AT LBL 38. REPAIRED PER EC/RA 5321-01330. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843054 1 20080609 A 5755 SKIN BOEING 737 7374Q8 138447Q NM NR 4 SPOILER GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 NR 4 SPOILER IS GOUGED ON THE LOWER SURFACE. PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 7 0 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843073 1 20080504 A 5320 654583444 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 306-312 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 CORROSION ON SUPPORT "T" AT RBL 12 WL 208 STA306. FLOOR SUPPORT "T" REPLACED WITH NEW PART IAW B737 400 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843088 1 20080507 A 5311 90526913 FRAME BOEING 737 7374Q8 138447Q NM BS 727D S8-9L CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 LT SIDE FRAME AT STA 727D CRACKED AT PSU RAIL BRACKET. FRAME REPAIRED IAW ASA EA5310 02797. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 2008UALA03086 1 20080529 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW REST AREA FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 AFT CREW REST AREA, CEILING EMERGENCY EXIT LIGHT TURNS OFF AFTER A FEW SECONDS OF OPERATION. 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 NM 2008 7 16 2008UALA03087 1 20080529 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EEL INOP SEAT 4A. 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 NM 2008 7 16 SWAA082880 1 20080528 A 3350 MS155721 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 311SW 23333 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 NOCA04508 1 20080531 A 3350 58791 LIGHT BOEING 767 767304 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 769NA 28039 EMERGENCY LIGHTS INOP ON LEFT HAND SIDE A/C ROWS 1ABC THROUGH 2ABC. T/S SYSTEM REMOVED AND REPLACED LEAD ASSY AND E-PAT H STRIP ASSY AS PER MM 33-51-10, OPS CHECK OK. 2 L 7 2 4F RT A1NM 20080716 NM 2008 7 16 BB08101 1 20080528 A 2560 P4010021 BATTERY BOEING 767 767201 1385125 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 250AY 23902 PHL - THE AFT RIGHT FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY ON THE AFT RIGHT FLASHLIGHT. 2 L 7 2 4F RT A1NM 20080716 2008 7 16 MAC060801 4 20080520 A 3414 7002860909 INDICATOR AEROSP ATR72 ATR72202 8680940 EU COCKPIT INOPERATIVE A MTNA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 68 810FX 220 ON TAKEOFF ROLL, THE ANNUNCIATOR ILLUMINATED. ON CROSS CHECK THE F/O`S AIRSPEED INDICATOR INDICATED ZERO. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE F/O`S AIRSPEED INDICATOR WAS REPLACED AND OPS CHECK NORMAL. RET URNED AIRCRAFT TO SERVICE. 2 H 7 2 4T RT A53EU 20080716 EU 2008 7 16 MAC060802 1 20080520 A 3411 0851JA PITOT TUBE AEROSP ATR72 ATR72202 8680940 EU PITOT STATIC SYS OBSTRUCTED A MTNA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 68 810FX 220 ON TAKEOFF ROLL, THE ANNUNCIATOR ILLUMINATED. ON CROSS CHECK THE F/O`S AIRSPEED INDICATOR INDICATED ZERO. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. THE NR 2 PITOT TUBE WAS REMOVED AND REPLACED THE SYSTEM CHECKED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 20080716 CE 2008 7 16 DXTA200803086 1 20080531 A 2710 UNKNOWN RAYTHN DH125 HAWKER800XP 7150012 CE AILERON MALFUNCTIONED E DXTA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 07 862QS 258362 DURING FLIGHT THE AILRON TRIM LIGHT CAME ON. TRIED TO MOVE AILERON TRIM KNOB, BUT IT WOULD NOT MOVE WITH AUTOPILOT OFF. 2 L 7 2 4F RT A3EU 20080716 CE 2008 7 16 DXTA200803088 1 20080601 A 2120 UNKNOWN CESSNA 750 750 2076810 CE ODOR E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 905QS 7500105 IN CRUISE AFTER A WARMER TEMP WAS SELECTED ON THE COCKPIT PAC, JET FUEL SMELL STARTED COMING THROUGH THE WEMACS. 2 L 7 2 4J RT T00007WI 20080716 EU 2008 7 16 DXTA200803089 1 20080601 A 3610 BLEED AIR SYS ISRAEL GALAXY GALAXY 4500307 EU MALFUNCTIONED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 700QS 052 UPON FULL POWER APPLICATION AT APPROX 40KTS, RED BLEED PRESS / TEMP HI WARNING LIGHTCAME ON. ABORTED TAKEOFF. 2 L 7 2 4F RT A53NM 20080716 NM 2008 7 16 SWAA082887 1 20080528 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 2008UALA03097 1 20080529 A 2810 VALVE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUEL SYSTEM INOPERATIVE A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 218UA 30222 LEFT OUTBOARD REFUEL VLV INOP. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080716 NM 2008 7 16 ZZDA2008123 1 20080615 A 5100 NONE BOEING 717 717200 1383700 NM NONE A ZZDA O OTHER O OTHER NR NOT REPORTED 1 SO 37 982AT 55041 EMERGENCY LIGHT SYSTEM INOPERATIVE. FOUND ON F/A PANEL SWITCH IN ON POSITION. RESET SWITCH, SYSTEM OPS NORMAL AS REQUI RED. 2 L 7 2 4F TR A6WE 20080716 NM 2008 7 16 ZZDA2008122 1 20080616 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM EMERGENCY LIGHTS INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 928AT 55076 EMERGENCY PATH LIGHTING AT ROWS 1-10 ARE INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY ASSEMBLY AND BATTERY IAW B717 M M 33-51. OPS CHECK NORMAL. 2 L 7 2 4F TR A6WE 20080716 NM 2008 7 16 ZZDA2008114 1 20080528 A 5347 5971207503 SEAT TRACK BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 952AT 55014 F/O AFT I/B SEAT TRACK CORRODED BEYOND LIMITS. REPLACED SEAT TRACK. 2 L 7 2 4F TR A6WE 20080716 CE 2008 7 16 DJFA2008050 1 20080530 A 5610 991438012 WINDSHIELD CESSNA 750 750 2076810 CE COCKPIT CRACKED E DJFA B EMER. DESCENT O OTHER CR CRUISE 1 EA 23 706LX 2398 7500073 CREW REPORTED WHILE AT FL470 IN CRUISE CONFIGURATION, THE CO-PILOTS WINDSHIELD SHATTERED. 2 L 7 2 4J RT T00007WI 20080717 SO 2008 7 17 FDKA200805213 1 20080530 A 2612 BOTTLE EMB 145 EMB145LR 3260212 SO CARGO BAY DEFECTIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 828MJ 145218 FDM FLT 6085 JFK - BAGGAGE EXTINGUISH LIGHT WILL NOT ILLUMINATE. MX REMOVED AND REPLACED BOTTLES. 2 L 7 2 4T RT T00011AT 20080717 NM 2008 7 17 HALA0800609 1 20080531 A 8012 START VALVE BOEING 767 767300 1385204 NM PWA 4090 PW4090 52119 NE RT ENGINE MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM - AFTER STARTING R ENGINE, EICAS MSG OF R STARTER CUTOUT. OPERATED STARTER VAL MANUALLY SEVERA L TIMES. ACCMP NORMAL START. STARTER CUTOUT LT OPERATED NORMAL. 2 L 7 2 4F 4 F RT A1NM E46NE 20080717 NM 2008 7 17 SWAA083364 1 20080618 A 5315 6545834 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 11 TO LBL 19. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 20080717 SO 2008 7 17 FDKA200805210 1 20080525 A 2913 971808MODA PUMP EMB 145 EMB145LR 3260212 SO NR 2 HYD SYSTEM FAILED A FDKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 827MJ 15098 145217 FDM FLT 6190 BNA-JFK, NR 2 HYD EDP FAIL IN FLIGHT. MX CHANGED NR 2 EDP. 2 L 7 2 4T RT T00011AT 20080717 NM 2008 7 17 SWAA083332 1 20080618 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 451WN 32495 R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 MWE2008F00003 1 20080630 A 7830 ANGLE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE THRUST REVERSER CRACKED A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 907ME 55171 RT UPPER BUCKET, FWD IB Z FRAME IS CRACKED AT STA 26 APPROXIMATELY .75 LONG. FABRICATED AND INSTALLED ANGLE. (K) 2 L 7 2 4F 4 F TR A6WE E00061EN 20080717 EU 2008 7 17 M7K2008F00006 1 20080512 A 6510 800301 MAGNETIC SEAL UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE T/R INPUT SHAFT LEAKING E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 810MH 3949 (REF 0421083949) THE TAIL ROTOR DRIVE FREE WHEEL ASSEMBLY OUTPUT SHAFT SEAL OF MODULE 5 BEGAN TO WEEP AND PROGRESSIVELY THE WEEP BECAME A LEAK. A NEW SEAL WAS INSTALLED AND NO FURTHER LEAKAGE WAS NOTED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080717 SW 2008 7 17 MT92008F00001 1 20080606 A 3230 2752018003 SPRING SWRNGN SA227 SA227* SW MLG HOOK BROKEN E MT9A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 05 26932 AC660 AN INTERRUPTION OF FLIGHT OCCURRED . AIRCRAFT ROLLED OUT AT 0546 AND TOOK OFF AT O552 FOR FLIGHT 602 ON ROUTE WITH 7225 LBS OF CARGO ON BOARD. AFTER A NORMAL TAKEOFF THE CREW SELECTED GEAR UP AND SOON NOTICED THAT THE NOSE GEAR WOULD NOT LOCK IN THE UP POSITION. THE CREW CYCLED THE GEAR SEVERAL TIMES IN LEVEL FLIGHT BUT WAS UNABLE TO LOCK THE NOSE GEAR IN THE UP AND LOCKED POSITION. THE PILOT THEN NOTIFIED THE TOWER THAT HE WAS HAVING LANDING GEAR TROUBLE AND NEEDED TO RET URN TO DEPARTURE. THE AIRCRAFT LANDED SAFELY BACK AT DEPARTURE AT 0605 WHERE FIRE AND RESCUE VEHICLES ESCORTED THE AIRC RAFT BACK TO THE BASE FACILITY AND THE AIRCRAFT SHUTDOWN ENGINES AT 0608. UPON INSPECTION OF THE NOSE GEAR ASSY BY THE 2 L 7 2 4T RT A5SW 20080717 NM 2008 7 17 SWAA083219 1 20080612 A 5312 6517582 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 178, RBL 17. REPAIRED STIFFENER PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083083 1 20080608 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083095 1 20080608 A 5340 6546837 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE LUG FITTING CORRODED AT BS RT 685. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 WP 2008 7 17 08FDEA02024 1 20080529 A 5321 AGA386311 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 AFT PIT FLOOR PANEL 187 AF REQUIRES FAB NEW. FABRICATED A NEW FLOOR PANEL 187 AF; POTTED EDGES; COMPLETED CURE AND SAN DED EDGES; INSTALLED INSERTS; FABBED TOP SHEET; LAYED UP UNDER A VAC BAG; COMPLETED CURE; BACK DRILLED AND COUNTERSU NK HOLES; APPLIED NON-SKID AND PART MARKED THE PANEL IAW FEDEX DWG SRZ 25-005, REV F AND 25-011, REV C. 2 L 7 3 4F RT A22WE 20080717 SO 2008 7 17 SWIA200819806 1 20080616 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 234SW 120308 EMERGENCY EXIT LIGHT AT ENTRY DOOR IS BROKEN. REPLACED EMERGENCY LIGHT AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080717 EA 2008 7 17 SWIA200819807 1 20080623 A 3350 COVER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 865AS 7507 FLT 3832 - FORWARD LOWER EMERGENCY LIGHT COVER IS BROKEN. REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080717 2008 7 17 ASAA0853043 4 20080608 A 2230 305RAA1 SERVO BOEING 737 737890 1384527 NM AUTOTHROTTLES FAULTED A ASAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 02 579AS 5092 35187 AT 360 CLIMBING 380 AND 380 CLIMBING 400 IN VERT SPEED (500 800FM) AUTO THROTTLES WOULD NOT FOLLOW THE N1 CHEVRON (GREEN ) ON N1 GAGE. (OAT 58C TAS 444 KT AT 400) USING VNAV AUTOTHROTTLES FUNCTION CORRECTLY PERFORMED FIM TASK 22 31 00 710 80 1 AND 22 31 00 710 802 ON AUTOTHROTTLES AND PERFORMED LAND. VERIFY TEST PER MM 22 11 00. OPS CHECK NORMAL. NO FAULTS LOGGED ON FFR. OK FOR CONTINUE SERVICE. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 08FDEA02101 1 20080602 A 5100 NONE DOUG MD11 MD11F 3023600 NM NO DAMAGE NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 EXISTING DOUBLER REPAIR AT CENTER CARGO DOOR FORWARD CUT-OUT APPROX STRINGER 37 TO 40. EXISTING DOUBLER REPAIR AT CENTE R CARGO DOOR FORWARD CUT-OUT APPROX STRINGER 37 TO 40. EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-50-00 FIGURE 17, VOLUME I. FEDEX EO NR 1-5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG - MD11 - REPAIR CATALOG AND TRACKING REQUIREMENTS, HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 08FDEA02002 1 20080528 A 5320 AGA70949 STANCHION DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 AFTER REMOVAL OF FORWARD CARGO AFT BULKHEAD STA 6-70 PANEL FOR WIRING INSPECTION FOUND PANEL SUPPORT LEFT 10 INCH FROM CENTER FOUND CORRODED. FORWARD CARGO AFT BULKHEAD STA 6-70 LEFT X = 9.05 STANCHION REMOVED AND REPLACED AS PER SRM 5 1-31-01 VOLUME II. STANCHION FABRICATED AS PER DOUGLAS DRAWING AGA7094. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 08FDEA02160 1 20080605 A 5313 655623620 STRINGER BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 490FE 21493 FWD CARGO COMPARTMENT HAS STRINGER 27 RT CORRODED BETWEEN STA 720E AND 720F CUT OUT DAMAGED AREA (DIM 17" LONG) AND FABR ICATED NEW FILLER FROM BAC 1498-147, 0.090 PO NR 8150104 (DIMENSION 17 INCH LONG) AND SPLICE FROM BAC-1498-131 7075-T6 PO NR 9006222 (DIMENSION 13 INCHES LONG ) IAW B-727 SRM 53-10-3 FIGURE 1 AND 53-10-2 FIGURE 9. TREATED AND PRIMED PARTS IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR PARTS AT FWD CARGO COMPARTMENT STRINGER 27 RT BETWEEN STA 720E-720F IAW B-72 7 SRM 51-30-2 AND 53-10-3 FIGURE 1. 2 L 7 3 4F A3WE 20080717 NM 2008 7 17 SWAA083269 1 20080617 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 08FDEA02216 1 20080611 A 5322 6516340 SHEAR TIE BOEING 727 727227 1384078 NM BS 990 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 DOT 114-010 AFT PIT BILGE SHEAR TIE IS CORRODED AT STATION 990 FRAME, STRINGER 29 RIGHT TO STR 30. MANUFACTURED AND INS TALLED NEW SHEAR TIE AT STA 990 STR 29 TO 30. FOUND OLD SHEAR TIE OUT OF LIMITS. ORIGINAL T .063 AFTER REMOVAL .051 RE F SRM 53-10-1. INSTALL REF SRM 53-10-4 PG 1 - 4. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080717 NM 2008 7 17 08FDEA02219 1 20080611 A 5313 6523535 STRINGER BOEING 727 727227 1384078 NM BS 620-624 S2R CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 STR-2R HAS CORROSION, BS: 620-624 REMOVED CORROSION REF SRM 51-10-6 P 12-14, VERIFIED MATERIAL LOSS WITHIN LIMITS REF SR M 53-10-1. ORIGINAL "T" .036", MATERIAL REMOVED .002" REMAINING "T" = .034. TREATED AND PRIMED REF SRM 51-10-2 P. 1-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080717 EU 2008 7 17 08FDEA02242 1 20080612 A 5347 A53611640200 SEAT TRACK AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 719FD 388 MAIN CARGO SEAT TRACK CORRODED FROM FR 14 C TO FR 19, RBL 37 (-YD). REMOVED SEAT TRACK IAW SRM 51-40-21 LOCATED HOLES A ND DRILLED IAW SRM 51-40-44. INSTALLED NEW SEAT TRACK IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080717 EU 2008 7 17 08FDEA02243 1 20080612 A 5330 A5361165420000 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT SIDE FUSELAGE BETWEEN FRAME 17 TO 18 AND BETWEEN STRINGERS 33 TO 36 LT AT FWD SIDE OF SKIN BUTTSEAM, THE REPAIR MEASURES 7.8" BY 7". REPAIR NOT IAW SRM AND DWG 922269 REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT REPAIR DOUBLER ON LT SIDE FUSELAGE BETWEEN FRAME 17 TO 18 AND STRINGERS 33 TO 36 I AW A310-200 SRM 53-10-12 FIG 216 SHEETS 1 AND 2. THIS IS AN AIRBUS REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080717 NM 2008 7 17 SWAA083153 1 20080610 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 266WN 32523 DURING SCHEDULED HC2 CHECK, FOUND EEPLS END CAP LOOSE AT ROW 1 ABC. SECURED END CAP PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083541 1 20080626 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 288WN 36611 EEPLS LIGHT INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 08FDEA02552 1 20080628 A 5311 65208391 FRAME BOEING 727 727225 1384077 NM ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 DOT 5, AFT PIT, STA 1148, FRAME WORN FROM HYDRAULIC LINES CHAFING, LOCATED BETWEEN STR 21L TO STR 22L. REPAIRED FRAME AT STA 1148 BETWEEN STR 21L TO STR22L. REF SRM 51-40-3 FIG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR. INSTALLED DOUBLE R ON FRAME AT STA 1148 BETWEEN STR 21L TO STR 22L. 2 L 7 3 4F A3WE 20080718 NM 2008 7 18 08FDEA02108 1 20080603 A 5100 NONE DOUG MD11 MD11F 3023600 NM IAW SRM NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 EXISTING REPAIR, RIGHT WING INBOARD FLAP UPPER SURFACE AT XIFH 186 FOUND REPAIR DOUBLER. EXISTING REPAIR AT RIGHT WING INBOARD FLAP UPPER SURFACE AT XIFH 186 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. FEDEX EO NR 1-5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG - MD11, REPAIR CATALOG AND TRACKING REQUIREMENTS 14 CFR 12 1.707, HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 08FDEA02111 1 20080603 A 5100 NONE DOUG MD11 MD11F 3023600 NM IAW SRM NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 590FE 48505 LEFT WING LEADING EDGE AT APPROX STA XIS 247 FOUND EXISTING REPAIR. LEFT WING LEADING EDGE AT APPROX STA XIS 247 EXISTI NG REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 24 VOLUME I. FEDEX EO NR1-5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG MD11, REPAIR CATALOG AND TRACKING REQUIREMENTS 14 CFR 121.707, HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 08FDEA02240 1 20080612 A 5340 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 598FE 48597 MAIN DECK CARGO DOOR SPOOL FITTING NR 7 FOUND 3RD LAYER CRACK INDICATIONS AT ALL FITTING MOUNTING BOLT HOLES. MAIN DECK CARGO DOOR SPOOL FITTING NR 7 REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHIN G REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 08FDEA02258 1 20080613 A 3233 ACTUATOR BOEING 727 727233 138408A NM MLG OUT OF ADJUST A FDEA L ABORTED APPROACH F FLT CONT AFFECTED LD LANDING 1 CE 21 274FE 22039 TEST FLIGHT, RMG SHOWED UNSAFE IND ON THIRD EXTENSION. NO GREEN DOWN AND LOCKED LIGHT, RED DOOR OPEN LIGHT ON. VISUAL INSPECTION BY TOWER AND OTHER A/C CONFIRMED RIGHT MAIN GEAR WAS STILL UP. CYCLED IAW RED TABS AND GOT SAFE DOWN AND LOC KED INDICATION. ADJUSTED RT MLG DOOR AND ACTUATOR AS REQUIRED IAW FX 727-200 MM 32-12-001-5. PERFORMED GEAR SWING AND OPS CHECK GOOD IAW FX 727-200 MM 32-32-000-5. ALSO PERFORMED MANUAL EXTENSION CHECKS ON MLG, OPS CHECK GOOD IAW FX 727- 200 MM 32-34-000-0. NO FURTHER DISCREPANCIES AT THIS TIME. 2 L 7 3 4F RT A3WE 20080718 NM 2008 7 18 2008UALA03438 1 20080617 A 2761 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 6 SPOILER MALFUNCTIONED A UALA O OTHER K FLUID LOSS LD LANDING 1 WP 29 661UA 27158 ON LANDING LOST ALL HYDRAULIC FLUID LEFT SIDE. FOUND FAULTY ACTUATOR. REPLACED NR 6 SPOILER IN BOARD ACTUATOR PER MM27 -61-01 OP AND PRESS CHECK NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080718 NM 2008 7 18 2008UALA03452 1 20080618 A 2611 473760 FIRE LOOP BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RT ENGINE FAILED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 216UA 30549 FIRE LOOP 2 ENG R RIGHT ENGINE FIRE DETECTION SYSTEM LOOP 2 FAILURE. STATUS MSG-2610232 ACTIVE DC HARD. SUSPECT IMPROP ERLY INSTALLED. REPLACED WIRE HARNESS FROM M26OO5 TO M26006, REF WD26-11-21. FOUND LOOP M26006 DAMAGED. REPLACED M26006 PER MM26-11-01. TESTED PER MM26-11-00. TESTED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080716 GL 2008 7 16 LR7A08082 2 20080611 A 7320 4409701 FUEL CONTROL LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL NR 2 ENGINE INTERMITTENT A LR7A O OTHER X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 AL 03 406LC 4139 4676 ON LANDING ROLL OUT, NR 2 ENGINE FLAMED OUT WHEN SELECTED INTO REVERSE. REMOVED AND REPLACED FUEL CONTROL, COORDINATOR AND GENEVA LOC ACTUATOR IAW AMM 73-1-4 PG 201-203, LOG PAGE 27338 ITEM 11. 2 H 7 4 4T 4 T A1SO E282 20080716 WP 2008 7 16 UPS08852397 1 20080422 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 A PIT CARGO COMP FLOORBEAM AT STA 70, LBL 50 IS CORRODED. CUT OUT DAMAGE, FABBED AND INSTALLED REPAI R ANGLE AND FILLER IAW, SRM 51-1-8, 51-3-0, 53-2-0 FIG 1F. 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 UPS08M52396 1 20080531 A 2913 887673 PUMP DOUG MD11 MD11F 3023600 NM HYDRAULIC SYS LEAKING A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 294UP 48472 INSPECTION TYPE:N/A ATB - NR 2 HYDRAULIC FAIL ALERT MESSAGE. EMERGENCY DECLARED. FOUND NR 2 ENGINE L FWD HYD PUMP LEAK ING FROM CASE DRAIN. REMOVED AND REPLACED NR 2 ENG LT & RT HYDRAULIC PUMPS AND FILTERS. 2 L 7 3 4F RT A22WE 20080716 EU 2008 7 16 USAA920081148 1 20080529 A 3260 664700500A4D CONTROL UNIT AIRBUS 320 A320232 3930326 EU MLG FAULTY A USAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 19 660AW 24874 651 1234 FLT NR 640 PHX-ONT - EMERGENCY LANDING, AFTER LANDING GEAR WAS SELECTED DOWN, GEAR INDICATION INTERMITTENTLY SHOWED NOSE GEAR NOT DOWN AND LOCKED. RECYCLED GEAR WITH NO CHANGE. CREW DECLARED AN EMERGENCY. GEAR UNSAFE INDICATION EXTINGUIS HED, THE AIRCRAFT LANDED UNVENTFULLY AND TAXIED TO THE GATE NORMALLY. MAINTENANCE REMOVED AND REPLACED THE NR 2 LANDING GEAR CONTROL INTERFACE UNIT IAW AMM 32-31-71. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20080716 NM 2008 7 16 UPS08M52533 1 20080519 A 5740 SB115700635 FITTING DOUG MD11 MD11F 3023600 NM RH WINGLET CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 280UP 48634 INSPECTION TYPE:2C RT WING LWR WINGLET FWD ATTACH FITTING ANGLED CLIP CRACKED AND AFT ATTACH FITTING CRACKED. REMOVED A ND REPLACED FWD ATTACH FITTING ANGLED CLIP AND AFT ATTACH FITTING IAW UPS EO MD11-5720-27680-A APPENDIX E. 2 L 7 3 4F RT A22WE 20080716 EA 2008 7 16 FDKA200805201 1 20080515 A 2120 UNKNOWN CNDAIR CL600 CL6002D24 1390016 EA CABIN ODOR A FDKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 602LR 15151 FDM 6050 IAD-ATL, AFTER TAKEOFF CABIN FILLED WITH SMOKE AND AN ODD ODOR WAS SMELLED. MX PERFORMED ENGINE GROUND RUN. N O DEFECTS NOTED. 2 L 7 2 4F RT A21EA 20080716 EA 2008 7 16 MASA200800428 1 20080527 A 3397 2060441 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DEFECTIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17337 7337 ASH 2982 PHX - LT SIDE FLOOR LEVEL EXIT LIGHT INOP. MX REPLACED A BAD CONNECTOR ON THE LIGHT ASSEMBLY. 2 L 7 2 4F RT A21EA 20080716 SO 2008 7 16 RAIA00805031 1 20080528 A 2430 32248001 BATTERY EMB 145 EMB145LR 3260212 SO NR 1 MALFUNCTIONED A RAIA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 844HK 14938 14500838 FLT 5506 - ATL - CREW RECEIVED A BATTERY NR 1 OVERHEAT MESSAGE ON THE EICAS DURING FLIGHT. MAINTENANCE REMOVED AND REPL ACED THE NR 1 MAIN BATTERY ASSEMBLY. NO OTHER DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 20080716 2008 7 16 RAIA00805028 4 20080526 A 3425 26006881102 AHRS EMB 145 EMB145EP 3260221 SO NR 2 MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 827HK 20073 20073 145021 FLT 5454 - STL - AHRS 2 OVERHEAT MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 2 AHRS. SYSTEM OPS CHEC KED GOOD. 2 L 7 2 4F RT T00011AT 20080716 EA 2008 7 16 MASA200800430 1 20080529 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 917FJ 15017 ASH FLT 2682 CLT - IAD. EMERGENCY LIGHTS OUTS AT ROW 15 AND 16. MX RELAMPED LIGHTS, OPS GOOD. 2 L 7 2 4F RT A21EA 20080716 EA 2008 7 16 MASA200800433 1 20080530 A 2612 FIRE WARNING CNDAIR CL600 CL6002D24 1390016 EA COCKPIT MALFUNCTIONED A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 931LR 15031 ASH FLT 2712 CMH-CLT, FIRE SYSTEM FAULT STATUS MESSAGE IN FLIGHT. MESSAGE ILLUMINATED, THEN EXTINGUISHED SHORTLY AFTER APPEARING. MX PERFORMED FIRE SYSTEM OPS CHECK, SYSTEM OPS GOOD. 2 L 7 2 4F RT A21EA 20080715 NM 2008 7 15 SWAA083863 1 20080711 A 3350 20131A BATTERY PACK BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED MV1 CHECK, AFT LT CABIN EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080715 NM 2008 7 15 SWAA083820 1 20080713 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080715 2008 7 15 SWAA083832 4 20080709 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080716 EU 2008 7 16 NWAA082373359 1 20080527 A 3240 BRAKE ASSY AIRBUS A330 A330223 3940031 EU NR 1 FIRE A NWAA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 GL 01 859NW 0722 ON ARRIVAL AT GATE, FOUND NR 1 BRAKE ON FIRE, A GROUND FIRE EXTINGUISHER WAS USED TO PUT OUT THE FIRE. THE BRAKE AND WH EEL WERE REPLACED AND CHECK OK. 2 L 7 2 4F RT A46NM 20080716 WP 2008 7 16 DHL2008807517 1 20080506 A 5740 BRACKET DOUG DC8 DC873F 302199F WP RWS 415 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 NR 4 ALT TANK BOOSTER PUMP BRACKET CRACKED STA XW 415.000 S-59. REMOVED AND REPLACED CRACKED BOOSTER PUMP BRACKET AT NR 4 ALT TANK STA XW 415.000 S-59 IAW SRM 51-1-20D. REFER TO JC BZ5R28338 FOR LEAK CHECK. 2 L 7 4 4F RT 4A25 20080716 WP 2008 7 16 DHL2008807530 1 20080513 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 FUSELAGE NOSE SECTION, MODIFICATION DOUBLER AT AFT UPPER CORNER OF RT PRIMARY HEAT EXCHANGER, STA -12.000 L-24R (0.500" SKIN CRACKED) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 04-30-08, EVA D853-00056 REV IR DATED 04-1 6-08, ASTAR DWG NR ESD853-00056-001-D REV IR DATED 04-15-08. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTIO N IAW ASTAR DWG NR ESD85300056-001-D. PERFORMED NDT INSPECTION IAW EVA D853-00056 ITEM 3, BOEING DC8 NDT SPM PART 06-10 -01-001. NO CRACK FOUND. ENCLOSED SMN FORM 242-2. FABRICATED REPAIR DOUBLER (AL2024T3 0.050") REPAIR TRIPLER (AL2024T 3 0.063") AND FILLER (AL2024T3 0.100") IAW ASTAR DWG NR ES D85300056-001-D. CLEANED, TREATED AND PRIMED AREA AND REPAIR 2 L 7 4 4F RT 4A25 20080716 2008 7 16 ASAA0852979 4 20080525 A 2210 8221567102AS CONTROL PANEL BOEING 737 737890 1384527 NM COCKPIT FAULTED A ASAA O OTHER O OTHER CL CLIMB 1 NM 02 579AS 4931 35187 ON CLIMB-OUT SELECTED VNAV AND NOTICIED 209 IMMEDIATELY REPLACED250 ON TOP OF THE AIRSPEED TAPE THE FLIGHT DIRECTOR ST ARTEDPITCHING FOR 209 KNOTS. THE CLIMB PAGE ON THE FMC SHOWED"CLIMB ACT 209" 7 COULD NOT BE MANIPULATED ALSO LOST B ESTANGLE AND BEST RATE PROMPTS AMONG OTHER MISSING INFO USED "LVL FFR SHOWS NUMEROUS FMC DATA AND MCP DATA INVALID MSG . ACCOMPLISHED BOTH DFCS LAND VERIFY AND EXTENDED MAINT TESTS PER MM 22-11-00 AND HGS SENSORS TESTS PER MM 34-36-00. O P'S CK NORMAL. SEAMC NOTIFIED "PAT" ACFT LWMP STATUS REMAINS UPGRADED AT CAT 111A AUTOLAND AND HGS. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 NWAA082465528 1 20080530 A 3350 CONTROL PANEL BOEING 757 757251 1384970 NM EMERGENCY LIGHTS FAULTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 528US 23843 DURING PREFLIGHT CHECK THE EMERGENCY LIGHTS AT ROWS 23 THROUGH 32 EXTINGUISHED WHEN THE EMERGENCY LIGHTS WERE SELECTED O N. WHEN THE EMERGENCY LIGHTS WERE SELECTED OFF THE EMERGENCY ESCAPE PATH LIGHTING CAME ON INTERMITTENTLY. MAINTENANCE REPLACED THE EMERGENCY LIGHT CONTROL PANEL ON THE OVER HEAD PANEL AND THE EMERGENCY LIGHT POWER SUPPLY, ALL OPERATIONS C HECKED GOOD. 2 L 7 2 4F RT A2NM 20080716 NE 2008 7 16 DL764080769 2 20080522 A 7260 COVER BOEING 767 767432ER 1385134 NM GE CF6 CF680 30025 NE NR 1 ENGINE MISSING A DALA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 27 827MH 706151 29698 706151 LEFT ENG SHUTDOWN AT 15000 FT DUE TO LOW OIL PRESSURE AND QUNTITY DURING CLIMBOUT. INFO DURING CHECKLIST AND SUBSEQUENT SHUTDOWN ENG WAS RUN AT 8 PSI FOR LESS THAN 30 SEC AT CRUISE POWER AND APPROX 3-4 MIN AT IDLE, PLS CHECK FOR TIME ACCUR ACY. OPENED LT ENG COWLING TO CHECK FOR OIL LEAK. FOUND DRIVE PAD COVER ON GEARBOX MISSING. ENG OIL PRESS RED AT 1245 . 24 GMT. FDR BEING READ TO FIND OUT ENG S/D TIME. CLOSED BUT DID NOT LATCH COWLING FOR A/C MOVEMENT. PERFORMED ENGIN E INSP FOR LOW OIL PRESS PER AMM. PERFOMRED EA INSP 48-468580-14. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK. 2 L 7 2 4F 4 F RT A1NM E13NE 20080716 NM 2008 7 16 08FDEA02072 1 20080531 A 5340 655784811 MOUNT BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 220FE 20934 CORROSION ON CARGO TIE DOWN MOUNT ON BOTTOM INBOARD FWD CORNER AT FS 720, LBL 22, WL 156. REMOVED AND REPLACED DAMAGED FITTING, REF SRM 51-30-02 PG 1-3. FITTING FOUND TO BE OUT F LIMITS, REF BOEING DWG 65-57848 ITEM NR 1, ORIG THK IS .11 0 INCH, MAT LOSS IS .035", MAT. REMAINING IS. 075 INCH, CAL TOOL NR IN 17-0213, DUE DATE 4/7/09. REINSTALLED ALL, REMO VED FASTENERS TO F.O.M. REF SRM 51-30-02 PG 1-3. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080716 NM 2008 7 16 UPS08M52359 1 20080404 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C LEFT WING FUEL TANK UPPER NR 11 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 11.5 I NCH. STR 11 SPLICE REMOVED. ATTACHED CLIP & FASTENERS REMOVED. SLOT OUT CRACKED AREA C/O. HFEC INSP C/O ON SLOT OUT AREA, FOUND NO CRACK EVIDENT. TWO EA REPAIR ANGLE FAB & HEAT TREATED. TWO EA REPAIR ANGLES, ATTACHED CLIP & SPLICE END INSTALLED. SEALANT ON STR 11 REPAIR AREA APPLIED. REWORK AREA PAINTED. LEAK CHECK SATIS. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 AALA200801293 1 20080512 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 758AN 32637 DFW - EMERGENCY LIGHT AT SEAT 22C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20080716 NM 2008 7 16 2008UALA03018 1 20080523 A 3350 79411 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 EMERGENCY LIGHT INOP 5B. FOUND LOOSE LIGHT ASSEMBLY. SECURED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080716 NM 2008 7 16 2008UALA03020 1 20080525 A 3350 3071BPEGPL LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 771UA 26932 EMERGENCY LIGHTS ON SIDES OF SEATS 21C AND 24C INOP. SUSPECT FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY 21C REPLA CED LAMP 24C OP CHECKED GOOD.AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080716 NM 2008 7 16 2008UALA03022 1 20080524 A 2421 1317 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT BURNED OUT A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 773UA 26929 NR 1 GENERATOR DRIVE LIGHT NOT ILLUMINATED WITH ENGINE SHUTDOWN. SUSPECT FAULTY LAMP. REPLACED ROLS SWITCH DRIVE LIGHT , OPS NORMALLY PER MM 24-11-15. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080716 NM 2008 7 16 2008UALA03023 1 20080526 A 2497 W3951016 WIRE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GENERATOR SHORTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 792UA 26934 RIGHT GENERATOR FAILED WOULD NOT RESET. RIGHT GEN INOP. AFTER EXTENSIVE TROUBLE SHOOTING AND PART REPLACEMENT. FOUND W3951O-16 CHAFING & SHORTED TO GROUND. REPAIRED AND SECURED WIRING. REPAIRED CHAFFED WIRE AND OPS CHECK OK. AC OK FOR S ERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080716 NM 2008 7 16 USAA920081128 1 20080516 A 5340 693535U14 STRINGER CLIP BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6, CRACKED STRINGER TIE CLIP, BS 727C, S4L. REPLACED CRACKED STRINGER TIE CLIP BS 727C, S4L IAW B OEING SRM 51-10-20 & 51-00-00. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 UPS08552369 1 20080517 A 5311 70750071C FRAME BOEING 757 75724APF 1384969 NM BS 1340 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 436UP 25467 DENTS IN AFT CARGO FUSELAGE FRAME STA 1340 APPROX BET S25L AND S26L (2EA). DENT SIZE NR 1 L=1.3 INCH, W=.75 INCH, D=.02 2 INCH. DENT SIZE NR 2 L=1.35 INCH, W=.8 INCH, D=.028 INCH. DENTS LOCATION IS 2.7 INCH FROM PRODUCTION SPLICE, 8.1 FRO M TRANS PNL. CUTOUT DAMAGE AREAS DIM NR 1 L=1.2 INCH, W=1.4 INCH; NR 2, L=1.260 INCH, W=1.300 INCH. MPI NR P19726. 2 L 7 2 4F RT A2NM 20080716 NM 2008 7 16 USAA920081130 1 20080520 A 5310 652072328 DOOR FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 315AW 23734 CLT - MAJOR REPAIR - C20 CHECK - FORWARD CARGO DOOR CUTOUT AFT FRAME CRACKED, BS 490, S20R - S21R. REPAIRED FORWARD CAR GO DOOR CUTOUT AFT FRAME, BS 490, S20R - S21R IAW US AIRWAYS EA 100439. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 UPS08552368 1 20080517 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 1320 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 436UP 25467 DENT IN AFT CARGO FUSELAGE FRAME STA 1320, BETWEEN S25R AND S26R. DENT SIZE L = 1.5", W=.80", D= .030" DENT LOCATION: 6 .10" FROM PRODUCTION SPLICES 7.15" FROM TRANS PNL 2. CUT OUT DAMAGE AREA DIMENSIONS L=1.51 INCH, W=1.40 INCH, IAW SRM 5 3-07-2R5 STEP NR 1 DETAIL I 3. PERFORMED HFEC IAW NTM 51-00-00 PT 6 ON CUTOUT AREA, NO CRACK INDICATIONS NOTED. MPI N R P19734. 2 L 7 2 4F RT A2NM 20080718 NM 2008 7 18 SWAA083603 1 20080629 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 08FDEA02358 1 20080620 A 5315 A53275336200 FLOORBEAM AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 AFT CARGO COMPARTMENT FRAME 54.3 FLOORBEAM AFT SIDE BETWEEN SEAT TRACKS 2 RT AND 3 RT VERTICLE STIFFENER HAS 2 CRACKS .2 50 IN LONG EACH REMOVED DAMAGED SECTION AND INSTALLED CROSSBEAM CRACK REPAIR AT FR 54.3, BETWEEN SEAT TRACKS 2 RT AND 3 RT IAW FDEDEX EA 6-5310-121286, RELEASE DATE 3 JUNE, 2008. 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 SWAA083575 1 20080629 A 5311 6545808 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294, STR 2L. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083564 1 20080626 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 22Y CHECK, FOUND STRINGER 25L CORRODED BETWEEN BS 343 AND BS 355. REPAIRED STRINGER PER ER. 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 M7K2008F00011 1 20080512 A 6220 350A31191700 STARFLEX UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE M/R HUB ASSY CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 823MH M2902 4158 23336 (REF 1212074158) DURING ROUTINE INSP, THE ADHESIVE BEAD FOR A STAR ARM END BUSHING WAS FOUND CRACKED. FURTHER EXAMINATI ON UTILIZING A SOAP WATER DETECTION METHOD REVEALED RELATIVE MOTION BETWEEN BUSHING & STAR ARM END. WITH ROTOR HUB SLEEV ES REMOVED BUSHING COULD BE MOVED MANUALLY. A SERVICEABLE REPLACEMENT STARFLEX WAS INSTALLED. THIS IS A DEFECT THAT REC ENTLY HAS BECOME MORE COMMON THAN IN THE PAST. SUGGEST A DIFFERENT ADHESIVE BE UTILIZED OR STAR ARM ENDS AND BUSHINGS B E DESIGNED TO HAVE A LARGER ADHESIVE BONDING SURFACE SUCH AS ADDING INNER BUSHING AND OUTER STAR ARM END SPLINING. THER E WAS NO EVIDENCE OF ANY IMMINENT FAILURE FOR PART OR EXCESSIVE PLAY DEVELOPMENT OF BUSHING. SUGGEST THAT APPLICATION O 1 G 7 2 3U 3 U H9EU E00054EN 20080718 EU 2008 7 18 M7K2008F00026 1 20080512 A 6710 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE FAILED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 816MH 425 4038 23096 A FAULT CODE WAS GENERATED ON SHUTDOWN INDICATING A DEFECT OF COLLECTIVE POTENTIOMETER. A NEW PART WAS INSTALLED, NO FU RTHER FAULT WAS DETECTED. THIS IS RECURRING FAILURE FOR THIS PART WHICH HAS EFFECTED DISPATCH RELIABILITY FOR THIS MODE L HELICOPTER. SUGGEST AN ALTERATION OF FAULT SENSING SOFTWARE TO REDUCE FAULT SENSITIVITY TO PERHAPS A SIGNAL LOSS OF 0 .5 SECOND RATHER THAN 1/20TH OF A SECOND. AN OPTIC RATHER THAN A RESISTANCE BASED SENSOR SHOULD BE CONSIDERED AS CONTAC T POINT IS DAMAGED BY AC VIBRATION WHEN AC POWER SETTINGS ARE SET FOR CRUISE FLIGHT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 2008 7 18 SWAA083487 4 20080625 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 230WN 34592 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080718 EA 2008 7 18 A6WA200840433 1 20080520 A 5420 PLATE CNDAIR CL600 CL6002B19 1900309 EA LT PYLON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 LEFT PYLON TRAINING EDGE, INBOARD UPPER BONDING PLATE CORRODED. REMOVED CORROSION ON UPPER BONDING PLATE LT PYLON TRAIL ING EDGE INBOARD SIDE IAW CRJ 200 SRM 51-21-06 AND WITHIN LIMITS IAW SRM 54-00-00. (A) 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840445 1 20080523 A 5753 PLATE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 GOUGE FOUND ON AFT HINGE LOG PLATE OF RT INBOARD FLAP. GOUGE ON AFT HINGE LUG PLATE OF RT INDB FLAP REMOVED IAW REO 601 R-57-52-1341. (A) 2 L 7 2 4F RT A21EA 20080718 SW 2008 7 18 JIK2008F00002 1 20080703 A 2910 223002 ACCUMULATOR SWRNGN SA227 SA227AC 8780603 SW HYD SYSTEM FAILED E JIKA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 01 423MA 26613 AC636 FOLLOWING TAKEOFF, BOTH HYDR PRESSURE LIGHTS CAME ON RIGHT AFTER GEAR RETRACTION. PILOT DECLARED AN EMERGENCY, CONDUCTE D AN EMERGENCY GEAR EXTENSION PROCEDURE, MADE A LANDING WITHOUT FURTHER INCIDENT. UPON EXAMINATION, IT WAS DISCOVERED TH AT HYDR ACCUMULATOR END CAP ON HYDR SIDE HAD EXPERIENCED A CATASTROPHIC METALLURGICAL FAILURE, RESULTING IN SIGNIFICANT LOSS OF HYDR FLUID AND THEREFORE PRESSURE. THIS ACCUMULATOR IS AN "ON CONDITION" PART, WITH NO O/H REQUIREMENTS. THIS C OMPANY HAS EXPERIENCED (2) SIMILAR FAILURES IN 2005 AND 2003 ON THIS MAKE AND MODEL OF AC, AND AN ADDITIONAL FAILURE OF THIS TYPE ON ANOTHER AC WHICH HAS AN ACCUMULATOR PN 22300-3. IT WOULD SEEM PRUDENT TO INSTITUTE SOME SORT OF NDI SCHEDU 2 L 7 2 4T RT A8SW 20080718 EA 2008 7 18 A6WA200840455 1 20080528 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 CRACK FOUND ON INTERCOSTAL FS 484 LBL 27 AND LBL 36. DAMAGE REMOVED, NEW ANGLE FABRICATED, HFEC PERFORMED AND FABRICATE D ANGLE INSTALLED IAW REO 601R-53-41-059 REV A. AT FS 484 LBL 27 NEW ANGLE INSTALLED IAW REO 601R-53-41-059 REV A. (A) 2 L 7 2 4F RT A21EA 20080718 SO 2008 7 18 FDK2008F00000 1 20080623 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL EMERGENCY LIGHT UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 FDM 6202 PVD-JFK. RT OVERWING EMERGENCY LIGHT INOP. MX RESECURED CONNECTOR AND OPS CHECKED. (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080716 WP 2008 7 16 UPS08852540 1 20080612 A 5340 4751643U2 FITTING DOUG DC8 DC871F 302199D WP BS 720 L13R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 UPPER FITTING CRACKED AT STA 720 AND LONG 13R AT MAIN CABIN. REPLACED FITTING AT STA 720 AND L13R IN MAIN CABIN IAW SRM 51-01-21D, AND SRM 51-01-24-0. 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 2008UALA03098 1 20080530 A 3397 CONNECTOR BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT STRIP ON STAIRWELL AND AISLE IN UPPER DECK COMES ON AND OFF. FOUND LOOSE CONNECTION. SECURED CONNECTIO N OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 2008 7 16 2008UALA03103 4 20080529 A 2565 B142681 DISC BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE EVAC SLIDE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 797UA 0817 26924 LOW BOTTLE. RUPTURE DISC LEAKING. REMOVED AND REPLACED RUPTURE DISC. REPLACED RUPTURE DISC AND SLIDE BOTTLE. AC OK F OR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080716 SO 2008 7 16 C2XA08RI077 1 20080519 A 2611 SMOKE WARNING EMB 145 EMB145XR 3260214 SO COCKPIT MALFUNCTIONED A C2XA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SW 27 18101 145590 FLIGHT 2059 - EWR - DURING PREFLIGHT PROCEDURES, FLIGHT CREW REPORTED BAG SMOKE WARNING LIGHT ON. EWR MX RESET THE SYST EM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20080716 WP 2008 7 16 08FDEA01980 1 20080523 A 5743 ARB06341 ANGLE DOUG MD10 MD1010F 3022112 WP ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 68049 47803 LT MLG- SPLICE ANGLE FOR THE MLG ATTACH FITTING, P/N ARB0634-1, AT WING STATION XW231.160 OUTBOARD OF LT MLG FITTING AT LOWER FORWARD AUX SPAR HAS SEVERE EXFOLIATION CORROSION ON THE LOWER LEG OF THE ANGLE RESULTING IN AN APPROX 1 INCH CRAC K. ACCESS THRU PANEL 541BB, SNRM 769 REMOVED CORRODED FITTING ARB0634-1, LOCATED AND REAMED NEW FITTING AND SHIM REF DR AWING ARB0621. INSTALLED FITTING AND SHIM PER DRAWING ARB0621. 2 L 7 3 4F RT A22WE 20080716 SO 2008 7 16 C2XA08CL061 1 20080527 A 2824 2930003102 SHUTOFF VALVE EMB 145 EMB145XR 3260214 SO FUEL SYSTEM MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 13118 15574 145675 IAH - FLT 2187 - THE CREW REPORTED A VENTRAL TANK TRANSFER FAIL MESSAGE ON THE EICAS. THE AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS INSPECTED AND RELEASED IAW MEL 28-45-14. SUPPLEMENT TO FOLLOW: MAIN TENANCE REPLACED THE VENTRAL TANK TRANSFER SHUT-OFF VALVE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 20080716 WP 2008 7 16 DHL2008807528 1 20080511 A 5522 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 LT ELEV UPPER SKIN CRACKED 2 INCHES AND SEVERAL FASTENERS LOOSE (STA XE 79.531) MAJOR REPAIR. PERFORMED MAJOR REPAIR IA W SRM 55-4-1 FIG 1 SHEET 1-2. REMOVED DAMAGED PANEL PLATING IAW SRM 55-1-0 PG 1, SRM 51-1-21. FABRICATED PLATING AND F INGER DOUBLER BOTH FROM AL2024T3 0.016" IAW SRM 55-4-1 FIG 1 SHEET 1-2 ITEM "E", "F". BONDED BOTH PARTS WITH HYSOL IAW SRM 51-1-9, TR NR 51-142, SRM 51-1-9A, TR NR 51-141. CLEANED, TREATED AND PRIMED AREA AND PANEL PLATING INNER FACE IAW SRM 51-1-8B. INSTALLED NEW PANEL PLATING IAW SRM 51-1-21. PERFORMED LT ELEVATOR BALANCING IAW SRM 51-4-4- PG 1-2. INS TALLED (1EA) WEIGHT P/N 5701580-501 AND (1EA) RETAINER P/N 5701581-13 AT STA XE 99. FOUND WITHIN TOLERANCE (MOMENT: 145 2 L 7 4 4F RT 4A25 20080716 WP 2008 7 16 DHL2008807527 1 20080508 A 5100 NONE DOUG DC8 DC873F 302199F WP NONE A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 807DH 45990 REMOVED AND REPLACED EXISTING REPAIR AT FUSELAGE STA 320 LT SIDE L-28L WITH PERMANENT TYPE REPAIR PER SRM. INDICATE TYP E OF REPAIR, RE-INSPECTION INTERVAL AND NEXT REQUIRED INSPECTION (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-2-1 FIG 7 SHEET 1,4. REMOVED REPAIR NOT IN ACCORDANCE WITH SRM IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER (AL7075T6 0.090") FILLER (AL7075T6 0.080") AND (4EA) INTERNAL FINGER DOUBLER (AL7075T6 0.050") IAW SRM 53-2-1 FIG. 7 SHEET 1, 4, SRM 53-4-1 FIG 4 ITEM "F". CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SR M 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIG 7 SHEET 1-4 (THIS IS A CLASS 1 PERMANENT TYPE REPAIR, INITIAL INSP 2 L 7 4 4F RT 4A25 20080716 WP 2008 7 16 DHL2008807536 1 20080508 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 665-680 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 FUSELAGE EXTERNAL SKIN CORRODED (STA 665.000 - 680.000, L-35L - L-36) MAJOR REPAIR. PERFORMED MAJOR REPAIR IAW SRM 53-2 -1 FIG 7 SHEET 1-4. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. FABRICATED R EPAIR DOUBLER (AL7075T6 0.125") AND (2EA) INTERNAL FINGER (AL7075T6 0.050") IAW SRM 53-2-1 FIG 7 SHEET 1-4, SRM 53-4-1 F IG 15B ITEM "A". CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SRM 53- 2-1 FIG 7, SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1 (TORQUE). THIS IS A PERMANENT CLASS I REPAIR, INITIAL INS P AT 4.000 LANDING CYCLES, REPETITIVE AT 4.000 LANDING CYCLES, REPLACEMENT N/A, EXTERNAL VISUAL METHOD, NEXT REINSPECTIO 2 L 7 4 4F RT 4A25 20080716 SO 2008 7 16 C2XA08IA133 1 20080525 A 2530 COFFEEMAKER EMB 145 EMB145LR 3260212 SO GALLEY ODOR A C2XA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 18982 145223 JAN - FLIGHT 2461 DURING TAXI THE CREW REPORTED AN ELECTRIC SMELL IN GALLEY AREA. CONTRACT MAINTENANCE, "FOUND COFFEE M AKER NR 1 MAKING SMELL PLACED ON NEF-6L01 CAT D CONTROL NR 146579", AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED IN IAH WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE COFFEE MAKER ALL WITH N O DEFECTS/SMELL NOTED. REMOVED THE NEF, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20080716 WP 2008 7 16 DHL2008807512 1 20080509 A 5540 STIFFENER DOUG DC8 DC873F 302199F WP RUDDER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 RUDDER INTERNAL STRUCTURE STIFFENER CRACKED 1.500 INCH STA ZR 105.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21. CLEA NED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW STIFFENER IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 20080716 EA 2008 7 16 SIMA200815401 2 20080530 A 7321 FADEC EMB 145 EMB145LR 3260212 SO RROYCE AE3007 AE3007A1 54165 EA ENGINE UNKNOWN A SIMA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION DE DESCENT 1 SW 21 625AE 1438 145115 CAE312798 ON FLIGHT 3936 DURING DESCENT CREW REPORTED AT FL190 AIR SPEED 290KTS IT EXPERIENCED A LIGHTNING STRIKE. SHORTLY AFTER ENGINE 1 ITT BEGAN TO RISE UP INTO THE RED. ALL OTHER ENGINE INDICATION READINGS NORMAL. PERFORMED PRECAUTIONARY SHUT DOWN OF ENGINE 1. DECLARED EMERGENCY. LANDED IN ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. COMPLETED LIGHT NING STRIKE INSPECTION AND REMOVED AND REPLACED BOTH FADECS PER ROLLS ROYCE SUGGESTION. NO ENGINE PROBLEMS FOUND. AIRC RAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080716 WP 2008 7 16 UPS08852543 1 20080613 A 5230 56453573 WEB DOUG DC8 DC871F 302199D WP CARGO DOOR PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 B-PIT DOOR INTERIOR WEB IS PUNCTURED AT FWD UPPER LIGHTENING HOLE. REPAIRED B-PIT DOOR INTERIOR WEB IAW DWG 5645357 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 20080716 EA 2008 7 16 MASA200800439 1 20080531 A 3350 58351 STRIP CNDAIR CL600 CL6002D24 1390016 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 942LR 15042 ASH FLT 2829 PHX-TUS. SEAT 14C YELLOW EMERGENCY STRIPS MISSING AND INTERMITTENT MASTER CAUTION RT AFT OVERWING EMERGENC Y DOOR. MX FOUND YELLOW STRIP AND RE-INSTALLED. MX CLEANED EMERGENCY DOOR SEAL, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080716 EA 2008 7 16 MASA200800440 1 20080531 A 3530 17696531 OXYGEN BOTTLE CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27314 10381 7314 ASH FLT 1906 HNL-LIH. PORTABLE O2 BOTTLE AT ZERO PSI. MX REPLACED THE PORTABLE O2 BOTTLE ASSEMBLY. 2 L 7 2 4F RT A21EA 20080716 EA 2008 7 16 MASA200800421 1 20080525 A 2150 GG670950095 ACM CNDAIR CL600 CL6002D24 1390016 EA NR 2 MALFUNCTIONED A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 07 935LR 15035 ASH FLT 2698 BNA-CLT. SMOKE IN CABIN ON LANDING. REMOVED AND REPLACED NR 2 ACM. 2 L 7 2 4F RT A21EA 20080716 NM 2008 7 16 SWAA082935 1 20080601 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SWAA082916 1 20080530 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SWAA082917 1 20080530 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, STR 13L. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SWAA082923 1 20080601 A 2560 PH22300L GLOWSTRIP BOEING 737 7373G7 1384595 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 EEPLS LENS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SWAA082925 1 20080601 A 3350 3071BPEGPL LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 22Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 21 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SWAA082933 1 20080529 A 5610 141A484108 WINDOW BOEING 737 7377H4 1384404 NM COCKPIT CRACKED A SWAA K NONE O OTHER CR CRUISE 1 SW 29 772SW 27880 CREW REPORTED AT FL 400, FLIGHT DECK R2 WINDOW ARCED AND CRACKED. REMOVED AND REPLACED R2 WINDOW PER MM. 2 L 7 2 4F RT A16WE 20080716 NE 2008 7 16 EGRR119825 1 20080602 A 2620 9231004050043 LINE SKRSKY S92 S92A NE EXTINGUISH SYS CHAFED B EGRR K NONE O OTHER NR NOT REPORTED 1 EA 17 252DV 752 920009 DURING THE 250 HR AIRFRAME INSPECTION TECHNICAN FOUND NR 1 ENGINE FIRE BOTTLE DISCHARGE LINE P/N 92310-04050-043 CHAFED THE APU GENERATOR DUCT P/N 92550-04803-104. REPOSITION APU GENERATOR DUCT ASSY AND REPLACED NR 1 FIRE BOTTLE DISCHARGE LIME WITH NEW. 2 G 7 2 4U R00024BO 20080716 SO 2008 7 16 C2XAA08TY057 1 20080602 A 5720 PANEL EMB 145 EMB145XR 3260214 SO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12142 145735 TYS - DURING A CURRENT 3C INSPECTION THE BONDIND STRIP ON PANEL 197CL WAS FOUND CORRODED. MAINTENANCE REPAIRED THE PANE L IAW EMB 135/145 EC 5750-01315 AND PAINTED IAW EMB 145 XR AMM 2 51-21-02. ALL WORK WAS ACCOMPLISHED AND AIRCRAFT WILL BE RELEASED AT THE END OF THE CHECK. 2 L 7 2 4F RT 20080716 NM 2008 7 16 DXTA200803090 1 20080602 A 2612 FIRE WARNING GULSTM 200 200 4500308 NM NR 1 ENGINE ACTIVATED E DXTA F ACTIVATE FIRE EXT. J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 711QS 129 DURING THE START OF ENGINE NR 1 RECEIVED AN "APU FIRE" WARNING WITH THE FIRE BELL. FIRED THE APU FIRE BOTTLE. 2 L 7 2 4F RT A53NM 20080716 CE 2008 7 16 DXTA200803091 1 20080602 A 2120 UNKNOWN CESSNA 750 750 2076810 CE COCKPIT & CABIN SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 960QS 7500160 ON THE GROUND OUT OF THE RAMP WITH APU AND PACS ON, COCKPIT AND CABIN FILLED UP WITH SMOKE VERY RAPIDLY. 2 L 7 2 4J RT T00007WI 20080716 EA 2008 7 16 SWIA200819699 1 20080526 A 3397 POWER CABLE CNDAIR CL600 CL6002B19 1900309 EA CABIN DEFECTIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 466SW 7856 EMERGENCY LIGHTS INOP. FLIGHT 6616 - REPLACED POWER CABLE BETWEEN ROW 2 AND ROW 5. OPS CHECK GOOD IAW 33-51-00. 2 L 7 2 4F RT A21EA 20080716 EA 2008 7 16 SWIA200819700 1 20080528 A 3010 GG690800123 CONTROLLER CNDAIR CL600 CL6002C10 1390015 EA ANTI-ICE SYS MALFUNCTIONED A SWIA G A O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 728SK 2100 2100 10192 RECEIVED A LEFT ENGINE BLEED WARNING, FOLLOWED BY AN INCREASE IN CABIN PRESSURE AND DEPLOYMENT OF THE CABIN OXYGEN MASKS . FLIGHT 5825 - REPLACED AILC IAW AMM 30-12-12. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080716 SO 2008 7 16 SWIA200819701 1 20080527 A 2163 SENSOR EMB 120 EMB120ER 3260203 SO A/C PACK FAILED A SWIA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 NM 07 232SW 120306 DURING CRUISE, FLIGHT ATTENDANT REPORTED A BURNING SMELL IN THE CABIN FOLLOWED BY AN INTERMITTENT RIGHT "DUCT OVERHEAT" LIGHT ON OVERHEAD PANEL. FLIGHT 3628 - REPLACED RIGHT PACK TEMP SENSOR FOR AUTO CONTROL. OPS CHECK GOOD IAW 21-60-04. 2 L 7 2 4T RT A31SO 20080716 SO 2008 7 16 SWIA200819703 1 20080525 A 2130 UNKNOWN EMB 120 EMB120ER 3260203 SO CABIN PRESSURE MALFUNCTIONED A SWIA O OTHER N FALSE WARNING UK UNKNOWN 1 NM 07 308SW 120326 ON DESCENT, THE CABIN PRESSURE BEGAN TO INCREASE FOLLOWED BY A "CABIN PRESS WARNING" MESSAGE. FLIGHT 3616 - PRESSURIZED AIRCRAFT SEVERAL TIMES. COULD NOT DUPLICATE. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4T RT A31SO 20080716 SW 2008 7 16 WGEA200800059 1 20080602 A 3244 M16901 TIRE ECLIPS EA500 ECLIPSEEA500 3350000 SW MLG BLOWN E WGEA O OTHER O OTHER LD LANDING 1 EA 27 162DJ 16 000079 LEFT TIRE BLEW ON ROLL OUT AFTER LANDING ON PANAMA CITY. *SUPPLEMENTAL* REMOVED AND REPLACED LEFT MAIN LANDING GEAR WH EEL ASSY WITH SERVICEABLE ASSY IAW EA 500 MM CH 32-42-00. NO VISIBLE DAMAGE NOTED TO BRAKE OR MLG ASSY. 1 L 7 2 4J RT A00002AC 20080716 SO 2008 7 16 LR7A08077 1 20080531 A 5330 SKIN LKHEED 382 382G 526414U SO FUSELAGE DENTED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 17 4676 DURING SCHEDULED A CHECK PER JOB CARD HA1200, FOUND FUSELAGE EXTERIOR SKIN DENT 1.5 IN LONG X 0.0100 AT RIGHT FS 757, WL 161. REPAIR ACCOMPLISHED IAW LAC MEA 382-53-08-038 ON LOG PAGE 28220, ITEM M2. 2 H 7 4 4T A1SO 20080716 EU 2008 7 16 TRBA2008055 1 20080602 A 3240 BRAKE AEROSP ATR72 ATR72212 8680945 EU MLG MALFUNCTIONED A TRBA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 447AM 447 DURING TAXI A/C LOST BRAKES. AWAITING FOR AML FOR FURTHER DETAILS. 2 H 7 2 4T RT A53EU 20080717 WP 2008 7 17 UPS08852568 1 20080528 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 RUDDER RT SIDE EXTERIOR SKIN HAS CORROSION, POPPED RIVETS AND BEADED SKIN IS SEPARATED. REMOVED AND REPLACED 2 RUDDER SKINS IAW DC8 SRM 51-1-21, 51-1-21A , AND51-01-22. 2 L 7 4 4F RT 4A25 20080717 WP 2008 7 17 UPS08852570 1 20080605 A 5720 SUPPORT ANGLE DOUG DC8 DC873F 302199F WP RT WING CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 RT WING INBD SLOT VANE HAS A DEEP CHAFING MARK AT SUPPORT ANGLE AT OTBD SIDE. REMOVED AND REPLACED S UPPORT ANGLE IAW AMM, 51-1-24, 27-80-00. 2 L 7 4 4F RT 4A25 20080716 2008 7 16 UPS08852550 4 20080619 A 2565 SLIDE DOUG DC8 DC871F 302199D WP PAX DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 701UP 45938 MAIN ENTRY DOOR SLIDE INOP 378344. REMOVED MAIN ENTRY DOOR SLIDE AND ROUTED TO S/M. RIVET INSTALLED ON LOOSE BRACKET S RM 51-1-21 AND FWD ENTRY SLIDE REINSTALLED IAW MM 25- 60-01-2. THIS CLEARS M378344. 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 ZZDA2008125 1 20080623 A 2612 FIRE WARNING BOEING 737 7377BD 1384511 NM MLG WW FALSE ACTIVATION A ZZDA O OTHER N FALSE WARNING CR CRUISE 1 SO 37 336AT 36716 WHEEL WELL FIRE LIGHT ILLUMINATED IN FLIGHT WITH FIRE BELL FOR 2 SECONDS THEN EXTINGUISHED ON OWN. TESTED NORMAL. INSP ECTED MAIN WHEEL WELL LOOP AND FAULT DETECTOR UNIT. ACCOMPLISHED FIM 26-18-801 AND 26-18-802. GROUND TEST NORMAL AT TH IS TIME. 2 L 7 2 4F RT A16WE 20080716 NE 2008 7 16 SA08040 2 20080531 A 7320 UNKNOWN AIRBUS A319 A319132 3930340 NM IAE V2524 V2524A5 NE MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 19 810AW 1116 V11020 FLIGHT 132, SNA-PHX - THE CAPTAIN RECEIVED AN ECAM MESSAGE OF FUEL CONTROL FAULT. THEY PROCEEDED WITH THE TAKEOFF AND T HE ECAM STATED TO BRING THE ENGINE BACK TO IDLE. DECLARED AN EMERGENCY AND LANDED IN LAX WITHOUT FURTHER INCIDENT. MAI NTENANCE ACTION IS PENDING. 2 L 7 2 4F 4 F RT A28NM E40NE 20080716 NM 2008 7 16 UPS08B52405 1 20080417 A 5320 65B09631612 TENSION TIE BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:BCF BS 1180 TENSION TIE RT FWD SIDE CRACKED. BS 1180 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201. 2 L 7 4 4F RT A20WE 20080716 SO 2008 7 16 FDKA200805203 1 20080521 A 3234 7455503 CONTROL LEVER EMB 145 EMB145LR 3260212 SO MLG MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 847MJ 24102 145517 FDM 6008 SYR-JFK MLG DISAGREE. THE GEAR WOULD NOT RETRACT. MX REMOVED AND REPLACED LDG CONTROL LEVER. 2 L 7 2 4T RT T00011AT 20080716 2008 7 16 C8GA20080015 4 20080528 A 3425 6560214106 ACCESSORY UNIT BOEING 727 727223 1384074 NM COCKPIT MALFUNCTIONED A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 713AA 22469 FLT 245 FROM EWR TO BDA. DURING CRUISE OPERATION CAPTAIN'S RMI CARD AND F/O'S HSI CARD STOPPED TURNING IN FLIGHT, BOTH RMI NEEDLES FROZE IN POSITION. AIRCRAFT RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEA LED THE FLIGHT INSTRUMENT ACCY. UNIT AT FAULT. REMOVED AND REPLACED FLIGHT INSTRUMENT ACCY. UNIT, OPS CHECK GOOD. NO O THER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20080716 EA 2008 7 16 MASA200800432 1 20080530 A 3350 505802 COVER CNDAIR CL600 CL6002D24 1390016 EA CABIN MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 928LR 15028 ASH 2691 MYR-CLT. EMERGENCY LIGHT COVER MISSING AT AFT F/A STATION. INSTALLED COVER ASSEMBLY. 2 L 7 2 4F RT A21EA 20080716 NM 2008 7 16 SWAA082926 1 20080601 A 3350 3071BPEGPL LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 22Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 23 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SWAA082928 1 20080530 A 2560 33500003 GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 767SW 29807 DURING SCHEDULED 8Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP MISSING AT ROW 9 ABC. INSTALLED STRIP PER MM. 2 L 7 2 4F RT A16WE 20080721 EU 2008 7 21 UPS08152434 1 20080528 A 5321 B5327077600000 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 137UP 0820 INSPECTION TYPE:3C MCD FLOOR PANEL NR 251WJ HAS A LARGE FIELD REPAIR WITH A LARGE DENT. REMOVED FIELD REPAIR AND REPAIR ED FLOOR PANEL NR 251WJ IAW A300-600 SRM 53-10-20 FIG 203. 2 L 7 2 4F RT A35EU 20080721 NM 2008 7 21 SWAA083632 1 20080701 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 24L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 2008UALA01930 1 20080403 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 ENGINE FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 786UA 26938 ELEC GEN SYSTEM L IDG HAS DISCONNECTED OR A PROTECTIVE TRIP OF THE GENERATOR CONTROL BREAKER HAS OCCURRED OR A PROTECTIV E TRIP OF THE BTB HAS OCCURRED. AFTER EXTENSIVE TROUBLESHOOTING FOUND IDG TO BE FAULTY. SUSPECT FAULTY BEARING. REPLA CED LEFT IDG PER AMM24-11-01. GROUND RUN CHECKED NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080721 NM 2008 7 21 2008UALA02700 1 20080508 A 2432 263BC1012 CHARGER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU BATTERY FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 772UA 26930 APU BATTERY CHARGE MESSAGE DISPLAYED ON EICAS. SUSPECT FAULTY BATTERY CHARGER. REPLACED BATTERY CHARGER PER MM 24-31-0 6. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080721 EA 2008 7 21 A6WA200840434 1 20080520 A 5410 PLATE CNDAIR CL600 CL6002B19 1900309 EA RT NACELLE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 RIGHT PYLON TRAILING EDGE, OUTBOARD UPPER BONDING CORRODED. CORROSION REMOVED IAW 51-21-06 AND WITHIN LIMITS IAW SRM 54 -00-00. (A) 2 L 7 2 4F RT A21EA 20080721 2008 7 21 2008UALA02826 4 20080515 A 2565 D31591478U1 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FWD ENTRY DOOR CRACKED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 910UA 25254 FWD ENTRY DOOR FWD SLIDE COVER CRACKED AT GIRT BAR HANGER. FOUND MAIN ENTRY DOOR SLIDE DAMAGED. REPLACED SLIDE ASSEMBL Y IAW MM 25-61-35. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080721 NM 2008 7 21 SWAA083504 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 6L AND STR 4L. REMOVED AND REPLACED STRINGER CLI P PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083503 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 9L AND STR 4L. REMOVED AND REPLACED STRINGER CLI P PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083532 1 20080625 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 410, BL 0. REPAIRED SKIN P ER EA. 2 L 7 2 4F RT A16WE 20080721 CE 2008 7 21 DVI2008F00000 1 20080625 A 3230 LANDING GEAR BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA RIGHT FAILED E DVIA E ENGINE SHUTDOWN F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 CE 19 311AV BB336 85436 CREW EXTENDED THE LANDING GEAR IN PREP FOR LANDING. AFTER EXTENDING THE GEAR, RT MAIN GEAR STUCK IN A POSITION APPROX 1 2 INCHES FWD OF "DOWN AND LOCKED" POSITION. WHEN THE LANDING GEAR WAS RECYCLED, RT MAIN GEAR DID NOT MOVE, IT REMAINTED IN THE SAME POSITION. AN ATTEMPT TO MANUALLY CRANK THE GEAR WAS UNSUCCESSFUL, AS EXPECTED. A LOW PASS WAS INITIATED T O CONTACT THE RIGHT MAIN WHEEL TO THE RUNWAY. CONTACT WAS MADE, BUT THE GEAR WOULD NOT LOCK IN PLACE. RT ENGINE WAS SH UTDOWN PRIOR TO LANDING TO REDUCE RISK OF FIRE. UPON LANDING, RT GEAR COLLAPSED BUT NO FIRE EXISTED AND RELATIVELY MINO R DAMAGE TO AIRCRAFT. NTSB STILL INVESTIGATING. (K) 1 L 7 2 4T 4 T A24CE E4EA 20080721 EA 2008 7 21 A6WA200840368 1 20080421 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 13 441ZW 7777 CRACK FOUND ON WEB STRUCTURE FS 280 RBL 9. REPAIRED IAW REO 601R-53-11-171 REV D. (S) 2 L 7 2 4F RT A21EA 20080721 NM 2008 7 21 SWAA083783 1 20080708 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 9L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083772 1 20080709 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 EU 2008 7 21 08FDEA02882 1 20080715 A 5340 A53970710203 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORRODED CORNER FITTING C 58 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080721 NM 2008 7 21 SWAA083639 1 20080701 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083640 1 20080701 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 LEFT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083645 1 20080701 A 5310 143A0345 CREASE BEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 769SW 30588 DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM CORRODED AT BS 312, STR 17R. REMOVED AND REPLACED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083655 1 20080702 A 5753 65C30462 FLAP BOEING 737 7373H4 1384600 NM RT WING DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND RT WING INBOARD FORE FLAP DISBONDED AT OUTBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083665 1 20080702 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 21R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083666 1 20080702 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083682 1 20080702 A 5315 6546816 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 727, RBL 10.7 TO LBL 1.5. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 20080721 2008 7 21 2008UALA02944 4 20080520 A 2565 101655305 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 663UA 27160 ASPIRATOR LEAKING. SUSPECT FAULTY O-RING. REPLACED ASPIRATOR. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080721 2008 7 21 2008UALA02945 4 20080521 A 2565 D31354437 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU R2 DOOR OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 309UA 23670 DOOR 2R SLIDE GIRT IS PARTIALLY OUT OF THE CONTAINER. SUSPECT IMPROPERLY INSTALLED. REPOSITION THE CABLE. AC OK FOR S ERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080717 WP 2008 7 17 UPS08852571 1 20080528 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1746 L15L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 MAIN CABIN, L-15L CRACKED AT CANT FRAME STA 1746. REMOVED, FABBED AND INSTALLED LONGERON SLICE IAW S RM, 51-1-8, 53-2-2 FIG 10, 53-5-1 FIG 7, 51-1-20D. 2 L 7 4 4F RT 4A25 20080717 WP 2008 7 17 UPS08852572 1 20080604 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 84 L21L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 INTERCOSTAL CRACKED AT STA -84 L21L BELOW SUB-FLOOR. REMOVED AND REPLACED INTERCOSTAL IAW, SRM, 51-1 -20D ,51-1-8, 51-1-21 2 L 7 4 4F RT 4A25 20080717 NM 2008 7 17 UPS08B52552 1 20080327 A 5311 65B0174922 FRAME BOEING 747 747400 13848AT NM BS 1120 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:BCF RT BS 1120 TENSION TIE FRAME WEB CRACKED ABOUT 0.250 INCH. RT BS 1120 TENSION TIE FRAME WEB REPLACE D PER SRM 53-40-07 REPAIR 1. 2 L 7 4 4F RT A20WE 20080717 NM 2008 7 17 UPS08B52553 1 20080329 A 5311 65B2583735 DOUBLER BOEING 747 747400 13848AT NM BS 1120 FRAME CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:BCF LT BS1120 TENSION TIE FRAME DOUBLER CRACKED ABOUT 0.030 INCH. LT BS 1120 TENSION TIE FRAME DOUBLER REPLACED PER 65B25837 PL AND DWG. 2 L 7 4 4F RT A20WE 20080717 NM 2008 7 17 UPS08B52562 1 20080401 A 5347 CARGO TRACK BOEING 747 747400 13848AT NM CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:BCF AFT CARGO TRACK SECTION CORRODED. CORRODED TRACK SECTION CUT AND REPLACED PER SRM 53-00-52. 2 L 7 4 4F RT A20WE 20080717 NM 2008 7 17 UPS08M52569 1 20080424 A 5740 FITTING DOUG MD11 MD11 3023602 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C RHW LOWER WINGLET ASSY AFT FITTING FOUND CRACKED. RHW LOWER WINGLET ASSY ATTACHED BRACKET AND WINGLET FITTING REMOVED. NEW WINGLET FITTING FASTENER HOLES PICKED UP PER SRM 51-31-01VIIR 35. NEW WINGLET INSTALLED PER SRM 51-31-01VIIR35. ATTACH BRACKET INSTALLED PER SRM 51-31-01VIIR35. 2 L 7 3 4F RT A22WE 20080717 NE 2008 7 17 UPS08M52499 2 20080614 A 7261 OIL SYSTEM DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE NR 2 ENGINE OVERTEMP A IPXA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 01 290UP 48456 ATB - NR 2 ENGINE OIL TEMP WENT TO 175C AFTER TAKEOFF. RAN CHECKLIST WITH NR 2 ENGINE AT IDLE, OIL TEMP WAS 122C (ENG O IL TEMP HI MSG). OIL TEMP WAS IN CAUTION ZONE FOR APPROXIMATELY 3 MINUTES. REFER FIM 79-00-03-02 FIG 105 NO FAULT MSG FOUND. OIL TEMP PEAK AT 175 DEG FOR 3 MINS. NO MAINTENANCE ACTION REQ, PER MM 72-00-04-280- 357 OIL QTY INDICATED 24 Q TS ON ARRIVAL. SAME AS OTHER ENGINE. INSP OIL CAP CHK NO OVER SERVICE, NO FUEL SMELL, RPL MGB OIL TEMP PROBE PER MM 79 -32-01. ENG RUN CHK, OIL TEMP OK PER MM 71-02-03-700-870. 2 L 7 3 4F 4 F RT A22WE E24NE 20080717 NM 2008 7 17 UPS08M52504 1 20080326 A 5753 HINGE DOUG MD11 MD11 3023602 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C RHW O/B FLAP O/B HINGE CENTER CAVITY HOLE FOUND CORRODED AS MARKED. RHW AFT O/B FLAP O/B HINGE FWD MO UNTING CENTER CAVITY HOLE CORROSION. REMOVED ORG DIA EVIDENT FLAP HINGE CENTER CAVITY HOLE OF DIA 1.788 INCH EVAL AND FOUND ACCEPTED PER EN1181-08. REWORK AREA ETCH INSP AND FOUND SATIS. FLAP PEENING, CADMIUM PLATING AND PAINTING C/O AS PER EN1181-08. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 UPS08M52505 1 20080416 A 5740 BRACKET DOUG MD11 MD11 3023602 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C RHW L/E TOP PANEL NR 616ET INTERNAL SUPPORT BRACKET FOUND CRACKED. INTERNAL SUPPORT BRACKET REMOVED. REPAIR BRACKET FAB 2EA SUPPORT BRACKET HEAT-TREATED AND FASTENER HOLES PICKED UP. REPAIR BRACKETS REPROTECTED AND PAI NTED AS PER SRM 51-21-01 VIIR35 2EA REPAIR BRACKETS INSTALLED AS PER SRM 57-10-00VI FIG31 R35. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 UPS08652574 1 20080625 A 5230 STRUCTURE BOEING 767 767300 1385204 NM CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 320UP 27747 FWD PIT DOOR AFT EDGE DAMAGE. 2 L 7 2 4F RT A1NM 20080717 NM 2008 7 17 ASAA0843096 1 20080602 A 5330 65C3235720 SKIN BOEING 737 7374Q8 138447Q NM BS 373-377 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 DENTS AT BS 374, 5 INCHES BELOW STR 32L AND BS 377.5 2 INCHES BELOW STR 24L. DENTS REPAIRED IAW B737 400 SRM 53 00 01 R EPAIR 31 FIG 201 TR 53 27. 2 L 7 2 4F RT A16WE 20080717 EU 2008 7 17 MAC060803 1 20080603 A 7722 56785538012 INDICATOR AEROSP ATR42 ATR42300 8680920 EU ITT DEFECTIVE A MTNA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 68 916FX 314 UPON APPLICATION OF TAKE OFF POWER, NUMBER 2 ITT RED LIGHT (816 DEGREES) ILLUMINATED. ABORTED TAKEOFF. THE ITT INDICAT OR WAS DETERMINED TO BE AT FAULT AND WAS REPLACED AND OPS CHECKED OK. 2 H 7 2 4T RT A53EU 20080717 SO 2008 7 17 FDKA200805211 1 20080529 A 3240 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO BRAKE SYS MALFUNCTIONED A FDKA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 07 840MJ 145429 FDM 5990 JFK-RIC. BRAKES DEGRADED CAUTION ABORTED TAKEOFF. FLIGHT CREW WAS IN HOLD POSITION ON RUNWAY WHEN MESSAGE OCC URRED. WHEN CREW TAXIED OFF RUNWAY, FAULT CLEARED. SIGNED OFF WITH FLIGHT CREW AS NO FURTHER ACTION REQUIRED. 2 L 7 2 4T RT T00011AT 20080717 NM 2008 7 17 ASAA0843071 1 20080606 A 5330 65C3578517 SKIN BOEING 737 7374Q8 138447Q NM BS 500 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 DENT IN FUSELAGE STA 500+6 5 INCHES BELOW STRINGER 7L. CUTOUT DENTS FABRICATED REPAIR DOUBLER AND INSTALLED IAW B737 40 0 SRM TR 53 27 UPDATED FIG 201 REPAIR 31 AND EA'S 5330 02354 5330 02355. 2 L 7 2 4F RT A16WE 20080717 SO 2008 7 17 FDKA200805204 1 20080522 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6180 IAD-JFK RT SIDEWALL EXIT LOCATOR LIGHT INOP. MX RESET LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 20080717 SO 2008 7 17 FDKA200805206 1 20080522 A 5320 14529495004 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 THE FWD FLOOR PANEL FLANGE (SILL) IS CORRODED UNDER FLOOR PANEL 262CF. THE CORRODED PART HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 20080722 NM 2008 7 22 2008UALA02880 1 20080517 A 3350 20131A POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 656UA 25394 RIGHT AFT OVERWING EXTERIOR EMERGENCY LIGHT IS INOP. SUSPECT POWER SUPPLY. REPLACED POWER SUPPLY. OPS CHECKS GOOD, AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 WP 2008 7 22 08FDEA02259 1 20080613 A 5310 AGA31021 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 THE FUSELAGE SKIN IS BULGING AT FS 1943 STRINGER 46 L. REMOVED DOUBLER IN REF TO SRM 51-33-01; VOL II. REMOVED CORROSI ON IN REF TO SRM 51-21-01; VOL II. ORIGINAL THICKNESS 0.068 IN REF TO SRM 53-36-01; VOL III. REMOVED 0.015, MATERIAL R EMAINING IS 0.053. AREA IS OUT OF LIMITS IN REF TO SRM53-00-01; FIG 1A; VOL I. REPAIRED AREA IN REF TO SRM 53-20-00; VOL I. MATERIAL ID FOR THE REPAIR PARTS DOUBLER AND TRIPLER IS 0.050 2024-T3, PO 610199.1 AND FINGER DOUBLERS ARE 0.040 2024-T3, PO 614599.2. 2 L 7 3 4F RT A22WE 20080722 2008 7 22 2008UALA02899 4 20080519 A 2350 MICROPHONE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU O2 MASK INOPERATIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 306UA 23667 F/O O2 MASK MIC DOES NOT WORK. SUSPECT FAULTY OXYGEN MASK. REPLACED MASK IAW MM35-12-86. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA02908 1 20080519 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 664UA 29236 SEAT 1H, ONE SEAT MOUNTED ELECTROLUMINESCENT LIGHT HANGING OUT OF SEAT. LIGHT ALSO INOP. FOUND BROKEN LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY AT SEAT 1H. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 NM 2008 7 22 2008UALA02909 1 20080519 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN MISSING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 672UA 30027 EMERGENCY LIGHT ON 3H MISSING. FOUND LIGHT ASSEMBLY BROKEN. REPLACED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVI CE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080721 NM 2008 7 21 SWAA083761 1 20080705 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 EEPLS LOOSE AT ROW 8. SECURED EEPLS TRACK PER MM. 2 L 7 2 4F RT A16WE 20080721 2008 7 21 SWAA083726 4 20080705 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 L2 DOOR EVAC SLIDE FELL OUT OF CONTAINER. DID NOT DEPLOY. INSTALLED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083725 1 20080705 A 3350 300432 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 401WN 29813 DURING SCHEDULED MV2 CHECK, FOUND LT FWD EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080721 2008 7 21 SWAA083724 4 20080705 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EVAC SLIDE PRESS INDICATION LOW. REMOVED AND REPLACED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 20080721 EU 2008 7 21 2008UALA02857 1 20080519 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 446UA 834 FOUND CORROSION ON FLOORBEAM ITEM 210. ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED FLOORBEAM, FLOOR BEAM INSTALLED. NEE D TO SECURE AFT OUTBOARD BOLT, AND WIRE CLAMPS. 2 L 7 2 4F 4 F RT A28NM E40NE 20080721 NM 2008 7 21 2008UALA02844 1 20080518 A 2611 80600031600U FIRE BOTTLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU APU BAY LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 385UA 24660 APU FIRE BOTTLE BELOW PRESS LIMITS. SUSPECT LEAKING AT DISCHARGE OUTLET LINE. REPLACED APU FIRE BOTTLE PER MM 26-22-11 . AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080721 NM 2008 7 21 2008UALA02868 1 20080518 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 655UA 25393 EMERGENCY FLOOR LIGHTING INOP WHEN ACTUATED FROM CABIN. CARRIED OUT TROUBLESHOOTING PER MM AND ACTIONED OPS TEST OF EME RGENCY ESCAPE PATH LIGHTING EEL SYSTEM PER MM 33-51-00 PAGE 503-504, SATIS. AC RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080916 WP 2008 9 16 08FDEA03732 1 20080905 A 5710 ARB1066504 SKIN DOUG MD10 MD1010F 3022112 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 A CRACK IS PROPAGATING FROM UNDER THE REPAIR DOUBLER AT THE RIGHT WING L/E SLAT DRIVE MECHANISM INBD CORNER. WORK WAS A CCOMPLISHED ON NON-ROUTINE N00802. 2 L 7 3 4F RT A22WE 20080916 EU 2008 9 16 08FDEA03147 1 20080729 A 5321 B5327048401400 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 CABIN FLOOR BOARD HAS A DENT FROM FRAME 26 TO 28 AND RBL 47 INCHES TO 67 INCHES. FABRICATED NEW FLOORBOARD NR 232 VH IA W FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03552 1 20080822 A 5230 F5257043020000 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 800 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 650FE 726 BULK CARGO DOOR, LOWER SECTION, FRAME IS GOUGED. REMOVED AND REPLACED THE BULK CARGO DOOR LOWER FRAME SECTION IAW SRM 5 1-72-10 AND SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080717 NM 2008 7 17 QXEA200800539 1 20080602 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR BINDING A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 414QX 4061 SEA - AFT PASSENGER DOOR HARD TO CLOSE. MAINTENANCE RESET THE DOOR BY DHC-8-400 SERVICE LETTER 52-001. OPERATIONAL CHE CKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080717 NM 2008 7 17 2008UALA03052 1 20080527 A 5330 SKIN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE AFT OF E&E DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 905UA 25005 SHEARED RIVET HEAD AFT OF E/E DOOR. 2 L 7 2 4F 4 F RT A16WE E2GL 20080717 NE 2008 7 17 USAA920081146 2 20080526 A 7230 COMPRESSOR AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B32P 13008 NE NR 1 ENGINE STALLED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 19 173US 23709 23709 1481 FLT NR 732 SFO-CLT - EMERGENCY LANDING, LEAVING CRUISE, NR 1 ENGINE HAD POSSIBLE COMPRESSOR STALL OR OTHER VIBRATION. C OULD NOT MAINTAIN POWER. OPERATED AT REDUCED THRUST WITH NO INDICATION OF VIBRATION. MAINTENANCE FOUND THE NR 1 ENGINE BEYOND LIMITS DURING BOROSCOPE. REMOVED AND REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A28NM 20080717 EA 2008 7 17 CHQA200800102 1 20080530 A 2621 TRANSDUCER PACIFICSCIEN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FIRE BOTTLE INTERMITTENT A CHQA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 11 639BR 9 9 36979D1 7313 GEE872507 FLIGHT 5552, IAH TO MGM. EN ROUTE TO MGM THE FLIGHT CREW RECEIVED A CARGO BOTTLE LOW EICAS MESSAGE. THE QRH WAS FOLLOW ED AND IT WAS DECIDED TO DIVERT TO BTR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE TRANSDUCER ON THE CARGO FIRE BOTTLE INTERMITTENT AND REPLACED THE BOTTLE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080717 NM 2008 7 17 ASAA0893066 1 20080620 A 5230 143A61121 SKIN BOEING 737 737990 NM CARGO DOOR CRACKED A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 305AS 30013 GOUGE CRACK IN FORWARD CARGO DOOR SKIN. REPAIRED PER SRM 52 00 01. 2 L 7 4 4F RT A16WE 20080717 NM 2008 7 17 ASAA0853038 1 20080607 A 2131 71211997101AC CONTROLLER BOEING 737 737890 1384527 NM CABIN PRESSURE FAILED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 559AS 6732 35178 "AUTO FAIL" AND ALTN LIGHT ON "AUTO FAIL" LIGHT GOES OFF WHEN PRESSURIZATION MODE SELECTOR SWITCH MOVED TO ALTN. VERIFI ED NR 2 CABIN PRESSURE CONTROLLER SHOWED CONTROLLER FAILURE. REPLACED NR 2 CABIN PRESS CONTROLLER. REF MM 21 31 00. O PS CHECK GOOD. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0853039 1 20080607 A 2130 8243921003 CONTROL MODULE BOEING 737 737890 1384527 NM CABIN PRESSURE FAULTY A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 559AS 35178 "AUTO FAIL" LIGHT AT FL 390 (REPEAT) ALTN=NORM PRESS CABIN CONTROL UNABLE TO DUPLICATE. ACCOMPLISHED FAULT HISTORY PRES ENT STATUS AND GROUND TESTS BOTH 1 AND 2 DCPS OPS CHECK NORMAL. REMOVED AND REPLACED P5 6 CABIN PRESSURE CONTROL MODULE AS PRECAUTION PER MM 21 31 02. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 CALA0800532 1 20080602 A 5311 141N12043 FRAME BOEING 757 757224 1384958 NM FUSELAGE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17139 30352 BULKHEAD GOUGED FROM FWD ACCESSORY DOOR (113AL) LATCH HITTING PART STATION 231 BL 0. PERFORMED REPAIR TO FRAME AT STATI ON 231 BL 0 PER EC/RA 5311-01407. 2 L 7 2 4F RT A2NM 20080717 NM 2008 7 17 CALA0800533 1 20080603 A 5315 147A5506 FLOORBEAM BOEING 737 737724 13844BY NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 STATION 986.5 FLOORBEAM UPPER CHORD HAS CORROSION AT LBL 44. REPAIRED PER EC/RA 5321-01330 REVISION A. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843070 1 20080606 A 5755 SKIN BOEING 737 7374Q8 138447Q NM LT WING FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 LT OTBD FORE FLAP EXTERNAL SKIN IS CHAFED AT INBD UPPER CORNER. REMOVED DAMAGE FABRICATED FILLER AND DOUBLER AND INSTAL LED IAW B737 400 SRM 57 53 01 REPAIR 8 AND EA5750 02461. 2 L 7 2 4F RT A16WE 20080717 NE 2008 7 17 BB08099 2 20080527 A 7530 C8E3812 CONTROL UNIT BOEING 757 7572G7 1384963 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE FAULTY A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 908AW 51865 1728 24233 HNL FLT 125 EN ROUTE HNL TO PHX. DURING CLIMB OUT FROM HNL, THE CABIN CREW REPORTED A LOUD NOISE, POSSIBLY COMING FROM THE DOOR. THE FLIGHT CREW REPORTED THAT THE AIRCRAFT WAS UNABLE TO PRESSURIZE, ALTHOUGH THERE NO EICAS MESSAGES OR OTH ER INDICATIONS FROM THE AIRCRAFT TO INDICATE WHAT THE PROBLEM WAS. FLIGHT RETURNED TO HNL AND LANDED WITHOUT FURTHER IN CIDENT. MAINTENANCE REPLACED THE LEFT ENGINE BVCU. OPERATIONALLY CHECKED THE PACKS AND INSPECTED THE L2 DOOR SEAL WHIL E THE CABIN WAS PRESSURIZED. NO FAULTS WERE FOUND. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 20080716 NM 2008 7 16 2008UALA03032 1 20080523 A 2611 2156556HS SMOKE DETECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW REST INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 DOOR 5R CREW REST SMOKE DETECTOR ZONE 1A INOP. FOUND FAULTY SMOKE DETECTOR. REPLACED SMOKE DETECTOR OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 NM 2008 7 16 USAA920081122 1 20080511 A 5743 65C3271610 ATTACH FITTING BOEING 737 7374B7 1384702 NM RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED RIGHT WING LANDING GEAR BEAM ATTACH FITTING, RSS 224.14. REPAIRED RIGHT WING LA NDING GEAR BEAM ATTACH FITTING, RSS 224.14 IAW US AIRWAYS EO 5702V54. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 USAA920081133 1 20080501 A 5313 BAC14902508707 STRINGER BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - CRACKED STRINGER, BS 500, S23 RIGHT. REPLACED CRACKED STRINGER, BS 500, S23 RIGHT IAW B OEING SRM 53-00-03. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083703 1 20080704 A 5322 6546528 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 380, LBL 5. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080916 EU 2008 9 16 08FDEA03553 1 20080822 A 5321 B5327048401200 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 650FE 726 MAIN CABIN FLOORBOARD 241 DF IS DAMAGED ON THE UPPER SURFACE. FABRICATED NEW FLOOR PANEL 241DF, POTTED EDGES, COMPLETED CURE AND LIGHTLY SANDED EDGE POTTING, INSTALLED INSERTS. APPLIED NON-SKID AND PART PARKED THE PANEL IAW DWG SRZ 25-0 05; REV "G". 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03554 1 20080822 A 5321 B5327048401600 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 650FE 726 MAIN CABIN FLOORBOARD 241 BF HAS DAMAGE ON THE FWD CORNER. FABRICATED NEW FLOOR PANEL 241BF, POTTED EDGES, COMPLETED CU RE AND LIGHTLY SANDED EDGE POTTING. INSTALLED INSERTS, APPLIED NON-SKID AND PART MARKED THE PANEL IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080916 NM 2008 9 16 08FDEA03183 1 20080730 A 5347 AEA753223 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 MAIN DECK SEAT TRACK AT STA 1421, X = -8 FOUND CORROSION. MAIN DECK CORRODED SEAT TRACK AT STA 1421, X = -8 REPAIRED BY SECTIONAL SEAT TRACK. REPLACEMENT FROM STA 1411 TO STA 1431, X = -8 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLA SSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 CALA0800799 1 20080822 A 5320 143A812210 THRESHOLD BOEING 737 737800* NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 79279 31597 FORWARD CARGO DOOR CUTOUT THRESHOLD PLATE LIFTING DUE TO CORROSION AT TOP CENTER SURFACE. REMOVED THRESHOLD PLATE AND C ORNERS, REMOVED CORRODED WEB SECTION TRANSFER HOLES TO NEW WEB P/N 143A8122-10, INSTALLED WEB, RECEIVED OK TO INSTALL TH RESHOLD PLATES. INSTALLED ALL THRESHOLDS AND REPLACED WEB PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 2008UALA04289 1 20080811 A 3350 SIGN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT OVERWING DISLODGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 582UA 26702 RIGHT OVERWING EXIT SIGN FELL OFF. *S/D* REPLACED RT WING EXT COVER. SYSTEM IS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NM 2008 9 18 2008UALA04367 1 20080810 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 37 BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 SEAT 37C EMERGENCY LIGHT BROKEN. *S/D* REPLACED LIGHT & OP CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 NM 2008 9 18 2008UALA04291 1 20080811 A 3350 20131A LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE SEAT 7C INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 805UA 783 EMERGENCY LIGHT AT SEAT 7C INOP. *S/D* REPLACED LIGHT ASSY, OKAY FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080918 NM 2008 9 18 2008UALA04298 1 20080816 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE ROW 56 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY LIGHT ROW 56 RT INOP. *S/D* RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 NM 2008 9 18 2008UALA04303 1 20080817 A 3350 D71702001 CHARGER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 776UA 26937 EMERGENCY LIGHT BATTERY ASSEMBLY M33424 AT DOOR L1 IS DRAINED. FOUND EMERGENCY LIGHT POWER SUPPLY M33424 BAD. REMOVED & REPLACED BATTERY CHARGER. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080918 NM 2008 9 18 SWAA084821 1 20080901 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 500D S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 15L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 2008UALA04137 1 20080805 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 1J INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EEL INOP: SEAT 1J FWD AND AFT SECTIONS. *S/D* REPLACED FWD & AFT LIGHT ASSEMBLIES. OPS CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080919 NM 2008 9 19 SWAA084960 1 20080908 A 2560 35500003 GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED 8Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIPS WORN IN RT AFT CABIN. REMOVED AND REPLACED STRIPS PER MM . 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084843 1 20080903 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 933-944 S22R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND STRINGER 22R CORRODED BETWEEN BS 933 AND BS 944. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084844 1 20080903 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED MV1 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084846 1 20080903 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 867 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 USAA920081151 1 20080524 A 5313 STRINGER BOEING 737 7374B7 1384702 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - NR 03C10753045/7, CRACKED STRINGER, BS 578, S6R. REPAIRED STRINGER, BS 578, S6R IAW US AIRWAYS EA 100482. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 2008UALA02855 1 20080517 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1R CLOGGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 509UA 24763 1R DOOR WILL NOT ARM. SUPPLEMENTAL DATA UPDATE CAUSE, DEBRIS UNDER GIRT BAR. REMOVED DEBRIS AND CLEANED SWITCHES, OPS CHECKS OK, ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080716 WP 2008 7 16 DHL2008807531 1 20080506 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 980 DAMAGED A DHLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 807DH 91019 45990 MAIN CARGO COMPT FLOORBEAM HAS A MISDRILLED HOLE, STA 980.000 RBL 32 1/4 INCHES (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 045-29-08, EVA D853-00070 REV IR DATED 05-01-08, DWG AF56-53-101 REV IR DATED 04-28-08. REMOV ED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED FILLER AND REPAIR ANGLE (BOTH FROM AL7075T6S1 0.12 5:) IAW DWG AF56-53-101. PERFORMED NDT INSPECTION OF REPAIR PARTS IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK, NO COR ROSION FOUND. ENCLOSED SMN FORM 242-2. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. INSTALLED R EPAIR PARTS IAW DWG AF56-53-101, SRM 51-1-20D, SRM 51-3-1 (TORQUE). 2 L 7 4 4F RT 4A25 20080717 EU 2008 7 17 USAA920081164 1 20080602 A 2560 P4010021 BATTERY AIRBUS A321 A321211 3930370 EU FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 184US 1651 FLT 881 CLT - 2R FLASHLIGHT BATTERY WEAK. MAINTENANCE REMOVED AND REPLACED FLASHLIGHT BATTERY AT 2R DOOR. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20080717 NM 2008 7 17 ASAA0843074 1 20080507 A 5311 654655211 FRAME BOEING 737 7374Q8 138447Q NM BS 827 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 RT FRAME AT STA827 CRACKED AT PSU RAIL BRACKET. FRAME REPAIRED IAW ASA EA5310 02797. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 BB08102 1 20080528 A 3350 BPS73 CHARGER BOEING 757 7572G7 1384963 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 910AW 24523 PHX - THE EMERGENCY SEAT LIGHTING WAS FOUND INOPERATIVE FROM ROWS 1 - 8. MAINTENANCE REPLACED THE BATTERY CHARGER FOR S EATS AT ROWS 1 - 8. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 20080717 NM 2008 7 17 MWEA080081 1 20080601 A 7830 ANGLE BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 916ME 55178 THRUST REVERSER STATION 26 Z FRAME REPAIR ANGLE IS CRACKED APPROXIMATELY .75 INCH IN RADIUS ON INBOARD END, LEFT REVERSE R UPPER BUCKET. FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F TR A6WE 20080717 NM 2008 7 17 ASAA0843079 1 20080606 A 5311 65C25228129 FRAME BOEING 737 7374Q8 138447Q NM BS 727C S24-25R DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 AFT CARGO PIT BS 727C BETWEEN STR 24R AND 25R TOP FLANGE OF FRAME DENTED. FRAME REPAIRED WITH REPAIR PART IAW B737 400 SRM 51 70 11. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843084 1 20080507 A 5311 65465292 FRAME BOEING 737 7374Q8 138447Q NM BS 440 S8-9L CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 LT SIDE FRAME AT STA 440 CRACKED AT PSU RAIL BRACKET. REPAIRED FRAME IAW ASA EA5310 02797. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843087 1 20080507 A 5311 90526913 FRAME BOEING 737 7374Q8 138447Q NM BS 500A S8-9L CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 LT SIDE FRAME AT STA 500A CRACKED AT PSU RAIL BRACKET. FRAME REPAIRED IAW ASA EA5310 02797. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843081 1 20080508 A 5320 65317876 SUPPORT CHANNEL BOEING 737 7374Q8 138447Q NM BS 303-325 S17L CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 L1 DOOR SILL INNER SUPPORT CORRODED ON SURFACE AND CRACKED. INSTALLED NEW CHANNEL IAW B737 400 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 HALA0800607 1 20080530 A 3244 3910797513 TIRE BOEING 717 717200 1383700 NM NR 4 SEPARATED A HALA K NONE O OTHER LD LANDING 1 WP 13 487HA 55123 NR 4 TIRE RECAP SEAM SEPARATING. REMOVED AND REPLACED NR 4 MLG TIRE ASSY PER AMM 32-41-01. SECURITY CHECK OKAY. 2 L 7 2 4F TR A6WE 20080717 NM 2008 7 17 ASAA0853067 1 20080622 A 2421 7588429101 FILTER BOEING 737 737890 1384527 NM NR 1 IDG DIRTY A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 579AS AAAH004890 35187 WHILE PERFORMING S C FOUND NR 1 ENG DELTA "P" BUTTON POPPED ACCOMPLISHED FIM TASK 24 11 00 801 803 NO NR 1 ENG ACCOMPLIS HED ASA T C 78273000 78424000 DRAINED NR 1 ENG OIL CHECKED FILTER RESERVICED LEAK CKD GOOD. OPD CKD GOOD PER MM 24 11 4 1 200 800 24 11 41 200 801. NO DEBRIS IN OIL, OIL NOT BURNED. RESET DELTA P 1. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0873068 1 20080622 A 5210 141A60752 ARM BOEING 737 737790 13844CN NM L1 DOOR OUT OF ADJUST A ASAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 02 609AS NG000295 29752 FA REPORTS FWD ENTRY DOOR DIFFICULT TO CLOSE AND LOCK ADJUSTED GUIDE ARM REF MM 52 11 00 820 801 "H". OPS CKS NML. OK FOR CONT SVC. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083327 1 20080618 A 5512 6573782 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED SPV CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 125. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 2008UALA02845 1 20080516 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 3R SLIDE OBSTRUCTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 DOOR 3R SLIDE LIGHT NOT WORKING. SUPPLEMENTAL DATA UPDATE CAUSE, BOTTLE CAP LODGED IN GIRT BAR FITTING. CLEANED DEBRIS , OPS CHKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080919 NM 2008 9 19 SWAA084855 1 20080903 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM BS 454 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BS 454, BL 0. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0843459 1 20080824 A 5311 65C4653969 FRAME BOEING 737 7374Q8 138447Q NM BS 616 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 778AS 25110 BODY STA 616 FRAME LT SIDE INNER CHORD IS CRACKED BELOW FLOOR WL 202. REMOVED DAMAGED AREA, FABBED FILLER AND STIFFENIN G ANGLES AND INSTALLED REPAIR PARTS IAW ASA EO 5310 02528. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0843448 1 20080823 A 5330 65C3375730 SKIN BOEING 737 7374Q8 138447Q NM BS 390 S18L DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 778AS 25110 FUSELAGE SKIN HAS A DENT LT SIDE STA 390 STR 18L. REMOVED DAMAGED AREA, FABBED DOUBLER AND INSTALLED REPAIR IAW AAREA 1 2887. 2 L 7 2 4F RT A16WE 20080919 EU 2008 9 19 USAA920081623 1 20080828 A 5540 D5537131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 660AW 1234 SAL - BC6 MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 5. REPLACED RUDDER HINGE FITTING NR 5 IAW A320 AMM 5 5-36-41. 2 L 7 2 4F RT A28NM 20080919 EU 2008 9 19 UPS08153244 1 20080818 A 5330 A53986202200 SKIN AIRBUS A300 A300F4622R 3930360 EU FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 138UP 0821 INSPECTION TYPE:1C GOUGE 24 INCHES FWD AND 18 INCHES LEFT OF TAIL STAND BALL. FABRICATED & INSTALLED PERMANENT REPAIR I N FUSELAGE SKIN 24 INCHES FWD & 18 INCHES LEFT OF TAIL STAND BALL REF SRM 53-10-12 FIG 216, SRM 53-19-12 FIG 2, EO A300- 5100-20876-B AND EO M-5100-21238-B. 2 L 7 2 4F RT A35EU 20080919 EU 2008 9 19 UPS08153267 1 20080831 A 3350 LENS AIRBUS A300 A300F4622R 3930360 EU EMERGENCY LIGHT MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 151UP 0834 EMERGENCY EXIT LIGHT ABOVE ELT STORAGE COMPARTMENT LENS MISSING. REPLACED EMERGENCY EXIT WALL MOUNTED LIGHT. EMERGENCY LIGHT OPS NORMAL PER A300 MM 33-50-00-00. 2 L 7 2 4F RT A35EU 20080919 NM 2008 9 19 UPS08553240 1 20080815 A 5320 FLOOR SUPPORT BOEING 757 75724APF 1384969 NM BS 565-580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 CORRODED FLOOR SUPPORT. BLENDED & TREATED TO SRM 53-00-53-1A. 2 L 7 2 4F RT A2NM 20080919 NM 2008 9 19 UPS08653243 1 20080821 A 5340 141T514616 STIFFENER BOEING 767 76734AF 1385212 NM BS 246 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 320UP 27747 INSPECTION TYPE:C FX- INTERNAL AREA STA 246 LBL 50 CABIN FLOORBEAM ATTACHMENT STIFFENER FOUND CRACK. CRACK LENGTH 0.75 INCH. FX- STA 246 LBL 50 CABIN FLOORBEAM ATTACHMENT STIFFENER REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51- 40-02. 2 L 7 2 4F RT A1NM 20080919 NM 2008 9 19 UPS08653245 1 20080824 A 5347 SEAT TRACK BOEING 767 76734AF 1385212 NM BS 754 WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 320UP 27747 INSPECTION TYPE:C M/D STA 754 RBL 11 SEAT TRACK CROWN WORN. M/D - CARGO TRACK SECTIONAL REPLACED FROM STA 709 TO STA 78 5 RBL 11 AND REPAIRED AS PER SRM 53-00-52-2R REPAIR 9 FIG 201. 2 L 7 2 4F RT A1NM 20080919 2008 9 19 ASAA0853431 4 20080829 A 3460 1741010201 CONTROL UNIT BOEING 737 737890 1384527 NM FLIGHT DECK MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 558AS 8409 35177 THE LEFT MCDU BLANKED OUT TWICE WITHIN 10 MINUTES THE FAIL LIGHT ILLUMINATED ON THE LEFT VERTICAL SIDE OF THE NUMBER KEY PAD. THE CENTER SCRENE MESSAGE INDICATED BIT TEST BIT PASS NORMAL OPERATION WAS AUTOMATICALLY RESTORED BOTH TIMES WITH IN 10 SECONDS. UNABLE TO DUPLICATE MCDU FAIL LIGHT ON OR A BLANK DISPLAY. REMOVED MCDU AND ACCOMPLISHED COOLING VENT C LEANING PER AMM 34 61 01 100 801. REINSTALLED MCDU AND ACCOMPLISHED INSTALLATION TEST PER AMM 34 61 01 401. GROUND VER IFICATION SUCCESSFUL DUE TO ALL TEST NORMAL. SINCE THE DISCREPANCY WAS NOT DUPLICATED ON THE GROUND VERIFICATION OF COR RECTIVE ACTION IS DEFERRED FOR THE FIRST 60 MINUTES OF ETOPS FLIGHT. VERIFICATION FLIGHT SATISFACTORY. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0873424 1 20080824 A 5210 69202314 GUIDE ARM BOEING 737 737790 13844CN NM R1 DOOR LOOSE A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 618AS 30543 FWD SERVICE DOOR LIGHT REMAINED ILLUMINATED AFTER DOOR CLOSED, FOUND JAMNUT LOOSE ON GUIDE ARM AND TIGHTENED REF 52 41 2 1. NOTED UPPER HINGE LOWER CAMPLATE LOOSE IN FUSELAGE. TIGHTENED UPPER HINGE LOWER CAMPLATE REPLACED DOOR SNUBBER AND ADJUSTED THE GUIDE ARM PER MM'S 52 41 21 52 41 51 AND 52 41 00. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0843439 1 20080902 A 5753 6546430189 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 LT WING I/B FORE FLAP UPPER SURFACE HAS A SMALL DENT 53 INCHES O/B FROM I/B END AND .75 INCHES UP FROM TRAILING EDGE. R EPAIRED LT WING I/B FORE FLAP UPPER SUFRACE IAW B737 400 SRM 51-70-10 REP 2 PG 201. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0843440 1 20080902 A 5753 6546430182 SKIN BOEING 737 737490 1384715 NM RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 RIGHT I/B FORE FLAP LOWER SURFACE ABOVE NR 4 TIRE IS PUNCTURED AT ONE DENT IN THE MIDDLE OF A GROUP OF DENTS. REPAIR RI GHT I/B FORE FLAP LOWER SURFACE IAW B737 400 SRM 51-70-10. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0843441 1 20080902 A 5753 65C2631025 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 LT WING I/B MID FLAP TRAILING EDGE WEDGE HAS 3 EA SHARP DENTS ON LOWER SURFACE 46 INCHES FROM I/B END. REPAIRED LT WING TRAILING EDGE WEDGE MID FLAP IAW B737 400 SPM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0843443 1 20080902 A 5753 65370611 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 LT WING I/B UPPER TRAILING EDGE PANEL DELAMINATED 2 EA PLACES AS MARKED 53 AND 70 INCHES O/B OF I/B END. REPAIRED LT WI NG I/B UPPER TRAILING EDGE PNL IAW B737 400 SRM 51 70 10 REPAIR 2 PG 201. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0843474 1 20080902 A 5330 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 DENT FWD LAV RT SIDE BS 310 316 BETWEEN STR 23 AND 26R. DIMENSION OF DENT ARE DEPTH .148 WIDTH 6.1" HEIGHT 5.4" AND FOU ND TO BE OUT OF LIMITS PER SRM 53-00-01. REPAIRED STRINGER IAW SRM 53-00-03. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0843446 1 20080903 A 5753 6546430182 SKIN BOEING 737 737490 1384715 NM RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 RIGHT I/B FOREFLAP LOWER SURFACE ABOVE NR 3 TIRE IS DENTED ON A REPAIR DOUBLER. REPAIRED THE DAMAGED AREA OF THE LOWER SURFACE OF I/B FORE FLAP IAW B737 400 SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080919 EA 2008 9 19 COMA086376 1 20080829 A 5320 60034017595 WEB CNDAIR CL600 CL6002B19 1900309 EA FS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 420CA 7451 UNDERFLOOR AFT WEB OUTBOARD OF RBL 9 AT STA 280 LOWER EDGE CRACKED. REPAIRED PER REO 601R-53-11-171 REV D. 2 L 7 2 4F RT A21EA 20080919 EA 2008 9 19 COMA086377 1 20080829 A 5315 601R35031239 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 420CA 7451 RT FLOOR SUPPORT ANGLE AT STA 621 RBL 5 IS CRACKED. REPAIRED PER CRJ SRM 51-42-21 PG 1-21, SRM 51-42-06 PG 1-20 AND REO 601R-53-61-117 REV A. 2 L 7 2 4F RT A21EA 20080919 NM 2008 9 19 SWAA084857 1 20080903 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 360 S13R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 13R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084862 1 20080903 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084863 1 20080903 A 5311 6546547 FRAME BOEING 737 7373H4 1384600 NM BS 663 S2L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663.75, STR 2L, STR 2R AND STR 3R. REPAIRED FRAME PER S RM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084864 1 20080903 A 5320 6546568 ANGLE BOEING 737 7373H4 1384600 NM BS 178 BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND FWD BULKHEAD ANGLE CRACKED AT BS 178, LBL 28. REMOVED AND REPLACED ANGLE PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084865 1 20080903 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 663 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084874 1 20080904 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 277 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084875 1 20080904 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500D S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084869 1 20080904 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 202WN 33999 DURING SCHEDULED CV CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084934 1 20080908 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727C S21R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080922 WP 2008 9 22 UPS08853149 1 20080802 A 5720 FITTING DOUG DC8 DC871F 302199D WP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 NR 4 ALT Z-FITTING CRACKED. REMOVED CRACKED FITTING IAW SRM 51-01-20D. FABRICATED AND INSTALLED REP LACEMENT FITTING IAW DWG 3644046, SRM 51-01-24, AND 51-01-20D. 2 L 7 4 4F RT 4A25 20080922 WP 2008 9 22 UPS08853152 1 20080805 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FS 660 RBL 24 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 FLOOR PANEL FROM STA 660 TO STA 760 RBL 24 TO 44 HAS 14 INCH GOUGE PENETRATING OUTER SKIN. FABRICATE D AND REPLACED FLOOR PANEL IAW EO DC8-5320-9691C. 2 L 7 4 4F RT 4A25 20080922 NM 2008 9 22 2008UALA05408 1 20080821 A 3260 SWITCH BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RT MLG MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 669UA 30025 RIGHT MAIN GEAR INDICATOR LIGHT INOP WILL ILLUMINATE WHEN WIGGLED. REPLACED RIGHT GEAR DOWN INDICATOR LIGHT KORRY SWITC H, CONDITION NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20080922 2008 9 22 2008UALA05409 4 20080822 A 2565 SELECTOR SWITCH BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE DOOR SLIDE NO TEST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 DOOR 4L SLIDE PACK ARM MODE SELECTOR SWITCH FAILED TEST PER JC 283507211. NO CONTINUITY ON DOOR ARMING CONDUIT. REPLAC ED DOOR OPEN SWITCH, REF 52-11-28-201. ACP EPAS BATTERY OPERATIONAL TEST, TEST IS OK. WORK IS ACP ON AMECO GFS112973. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080717 NM 2008 7 17 2008UALA02852 1 20080518 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 513UA 24810 EEL STRIP INOP OUTSIDE OF LAV FWD OF DOOR 4L LOOSE. SUPPLEMENTAL DATA UPDATE CAUSE, UNKNOWN. SECURED LOOSE CONNECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 20080717 CE 2008 7 17 FIS2008F00000 1 20080604 A 2730 50350053 FITTING CESSNA 421 421C 2076016 CE CONT O520 GTSIO520* 17032 SO ELEVATOR CRACKED E FISA O OTHER O OTHER NR NOT REPORTED 1 SO 19 934HD 7100 421C1032 THE COLLAR HAS A CRACK WHERE THE TAPER PIN GOES THROUGH. POSSIBLE SOMEONE OVER TORQUED THE TAPER PIN. (K) 1 L 7 2 3O 3 O A7CE E7CE 20080717 NM 2008 7 17 SWAA083348 1 20080618 A 3297 65557975 TERMINAL BOEING 737 737317 138447P NM RT MLG CRACKED A SWAA K NONE N FALSE WARNING CL CLIMB 1 SW 29 693SW 23174 ON CLIMBOUT, RIGHT MLG UNSAFE LIGHT AND GEAR DOWN LIGHT ILLUMINATED. CYCLED GEAR, ALL INDICATIONS NORMAL. INSPECTED GE AR, FOUND RIGHT MLG UPLOCK SENSOR TERMINAL CRACKED. REMOVED AND REPLACED TERMINAL END PER MM. 2 L 7 2 4F RT A16WE 20080717 2008 7 17 SWAA083340 4 20080618 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 709SW 27843 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083343 1 20080618 A 5743 115A5211 FITTING BOEING 737 7377H4 1384404 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 739GB 29275 DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION FITTING LUG CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 CE 2008 7 17 JBG2008F00001 1 20080630 A 2910 605700311 HOSE PARKER LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE HYD PUMP FAILED E JBGA O OTHER O OTHER NR NOT REPORTED 1 SW 11 260AN KO265AB 124 PILOT REPORTED A LOSS OF HYDRAULICS DURING FLIGHT AT CRUISE FL400. INSPECTION REVEALED THAT THE RT ENGINE DRIVEN HYDRAU LIC PUMP, PRESSURE SIDE HYDRAULIC LINE WAS LEAKING, AND ALLOWED THE AIRCRAFT`S HYDRAULIC SYSTEM FLUID TOBE DEPLETED. FU RTHER INSPECTION REVEALED THAT THE LINE HAD FAILED INTERNALLY AND WHEN PRESSURE WAS APPLIED THE HOSE WOULD SWELL AND BEG IN TO LEAK. THE PROBABLE CAUSE OF THE FAILURE IS AGE AND POSSIBLE EMBRITTLEMENT OF THE HOSE. TO POSSIBLY PREVENT RECURR ENCE OF SUCH FAILURES AT A TIME INTERVAL FOR REPLACEMENT OF AGEING TEFLON HOSES MAY BE NEEDED. (K) 2 L 7 2 4F 4 F RT A10CE E35NE 20080717 EU 2008 7 17 IJA2008F00000 1 20080517 A 3340 BULB SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE SEARCH LIGHT BROKEN E IJAA O OTHER O OTHER NR NOT REPORTED 1 CE 07 911EM 3603 ON MAY 17, 2008, THE PILOT REPORTED ELECTRIC SYSTEM FAILURE AND MADE A PRECAUTIONARY LANDING DUE TO THE FAILURE, IN A FI ELD. ON INSPECTION OF THE AIRCRAFT, MAINTENANCE FOUND THE AC BATTERY DEAD, INSTALLED NEW/ SERVICEABLE BATTERY. GROUND RAN AIRCRAFT TO TEST SYSTEM. ON START GENERATOR CAME ON LINE NORMALLY WITH NORMAL OUTPUT. AT WHICH TIME THE AIRCRAFT W AS REPOSITIONED TO ITS BASE. THE REPOSITION FLIGHT, FOUND THE ELECTRIC SYSTEM WORKING WITHOUT DEFECTS. UPON ARRIVAL, TH E MECHANIC NOTED THE SEARCH LIGHT WAS INOPERATIVE, REMOVAL OF THE SEARCH LIGHT BULB FOUND THE BULB HAD BROKEN IN HALF AN D THE WIRING HAD SORTED TO THE SEARCH LIGHT HOUSING. THIS CAUSED THE GENERATOR TO TRIP OFF LINE (ELECTRIC SYSTEM FAILUR 1 G 7 1 3U 3 U H9EU E19EU 20080717 NM 2008 7 17 SWAA083075 1 20080608 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083081 1 20080608 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083097 1 20080607 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR LOWER FWD CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080717 2008 7 17 SWAA083098 4 20080605 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083298 1 20080617 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 950, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083305 1 20080617 A 5330 65C337568 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 294.5, STR 14R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083308 1 20080617 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 425LV 29829 EEPLS LIGHT ASSY LOOSE AT ROW 1 ABC. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080717 EU 2008 7 17 M7K2008F00004 1 20080506 A 5300 350A58004523 HINGE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE CRACKED A M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 817MH 203 4125 23292 DURING ROUTINE INSPECTION, HINGE WAS FOUND CRACKED THROUGH A SCREW MOUNTING BORE TO THE METALS EDGE. THIS IS A VERY COM MON FAILURE FOR THIS PART. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080922 NM 2008 9 22 2008UALA05411 1 20080821 A 3240 3415251 SHUTOFF VALVE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU PARKING BRAKE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 914UA 25381 ANTI-SKID INOP LIGHT ON WITH SWITCH ON -CONSTANTLY. LIGHT ON WHEN PARK BRAKE ON, HOWEVER LIGHT GOES OFF AFTER PARK BRAK E RELEASED, PROG TEXT PARKING BRAKE SHUTOFF VALVE, OPS CHECKED NORMAL. AC OK FOR SERVICE 2 L 7 2 4F 4 F RT A16WE E21EU 20080922 NM 2008 9 22 CALA0800834 1 20080826 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 907 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14628 27532 LEFT FRAME IS CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STA 907 BETWEEN STRINGERS 8 AND 9. TRIMME D OUT CRACKED AREA AND INSTALLED REPAIR DOUBLERS PER EA 5310-04498 OP 2. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 CALA0800836 1 20080826 A 5311 65C27021 FRAME BOEING 737 737524 1384721 NM BS 440 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14628 27532 RIGHT FRAME IS CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 440 BETWEEN STRINGERS 8 AND 9. R EPAIRED FRAME AT STATION 440 RIGHT BETWEEN STRINGERS 8 AND 9 RIGHT PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 CALA0800837 1 20080826 A 5311 65C27021 FRAME BOEING 737 737524 1384721 NM BS 400 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14628 27532 RIGHT FRAME IS CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 400 BETWEEN STRINGERS 8 AND 9. R EMOVED DAMAGED AREA, AND INSTALLED REPAIR DOUBLERS A AND B PER EA 5310-04498 OPS-2. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 CALA0800838 1 20080826 A 5311 65C27021 FRAME BOEING 737 737524 1384721 NM BS 380 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14628 27532 RIGHT FRAME IS CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 380 BETWEEN STRINGERS 8 AND 9. R EPAIRED FRAME AT STATION 380 RIGHT BETWEEN STRINGERS 8 AND 9 RIGHT PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080922 NE 2008 9 22 2008UALA05527 2 20080830 A 7261 O-RING BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE ENGINE OIL SYS LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 793UA 26946 SIGNS OF OIL LEAK FROM NR 1 ENGINE. FOUND LEAK FROM FUEL SERVO HEATER TRANSFER TUBES AT BASEPLATE. REPLACED TRANSFER T UBES O-RING SEALS AND REFITTED FUEL SERVO HEATER. ACP'D DRY MOTOR AND NO LEAKS APPARENT. ACP'D IDLE RUN AND ALL OPS G OOD. NO LEAKS APPARENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080922 EU 2008 9 22 2008UALA05532 1 20080829 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 451UA 865 FLOORBEAM 250 CORRODED (MARKED). ALSO HAS 8 EA SHEARED FASTENERS ON OUTBOARD SIDE OF BEAM (MARKED). MAJOR REPAIR ACCOM PLISHED. BEAM REMOVED, TRANSFERRED FASTENER HOLES TO NEW BEAM. BEGAN INSTALLING FLOORBEAM 250 IN AC. COMPLETED INSTAL LATION OF FLOORBEAM 250. 2 L 7 2 4F 4 F RT A28NM E40NE 20080922 NM 2008 9 22 2008UALA05537 1 20080830 A 3350 COVER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 839UA 1507 EXIT PATH LIGHT COVER MISSING ON SEAT 1B. 2 L 7 2 4F 4 F RT A28NM E40NE 20080922 NM 2008 9 22 2008UALA05541 1 20080830 A 3350 80172424 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 3F INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 779UA 26941 SEAT 3F HAS BOTH FWD AND AFT EEL PROXS LIGHTS INOP. FOUND FAULTY HARNESS. REPLACED SEAT EEL LIGHT HARNESS. OP CHKS O KAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080918 EU 2008 9 18 2008UALA04352 1 20080819 A 3510 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OXYGEN SYS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 422UA 503 LARGE O2 BOTTLE AT 2R PRESS IS LOW. 2 L 7 2 4F 4 F RT A28NM E40NE 20080918 NM 2008 9 18 SWAA084798 1 20080828 A 5330 6545800 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 2008UALA04257 1 20080811 A 3320 78942 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE ROW 1F & 4F FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 LIGHT ASSEMBLY FOUND IN COCKPIT. *S/D* REPLACED LIGHT ASSY & SECURED ROW 1F & 4F. 2 L 7 2 4F 4 F RT A1NM E24NE 20080918 EU 2008 9 18 2008UALA05475 1 20080826 A 5320 SHEAR PLATE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 451UA 865 RIGHT SHEAR PLATE CORRODED. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED RT SHEAR PLATE. INSTALLED NEW RT SHEAR PLATE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080918 NM 2008 9 18 CALA0800801 1 20080819 A 5311 6546525 FRAME BOEING 737 7373T0 1384582 NM BS 380 S20-21R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 BODYSTATION 380 FRAME CRACK BETWEEN S20R AND 21R. REPAIRED FRAME AT BODYSTATION 380 IAW B737 SRM 51-70-11. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 ASAA0853401 1 20080816 A 3040 CIRCUIT BREAKER BOEING 737 737890 1384527 NM WINDOW HEAT TRIPPED A ASAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 02 579AS 5791 35187 LT FWD WINDOW HEAT OVERHEAT LIGHT ILLUMINATED INFLIGHT AT FL 330 43 SAT AND REMAINED ILLUMINATED AT COMPLETION OF OVERHE AT CHECKLIST. FOUND THE P63B C/B OPEN RESET C/B. C/B STAYS SET, PERFORMED BITE CHK REF FIM 30 41 00 SYS CHK'S GOOD, AC FT OK FOR SVC. 2 L 7 2 4F RT A16WE 20080717 NE 2008 7 17 E0X2008F00004 2 20080606 A 7200 31B4892 ENGINE BRAERO 1000 BAE1251000 1500287 EU PWA 305 PW305 NE RIGHT DAMAGED E E0XA O OTHER O OTHER NR NOT REPORTED 1 EA 39 513LR 4848 NA1004 PCE305005 AC DEPARTED AND SHORTLY AFTER DEPARTURE, SMOKE WAS NOTED IN CABIN WITH BAGGAGE SMOKE DETECTOR INDICATING SMOKE IN BAGGAG E COMPARTMENT. FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE, APPROACH AND LANDING WERE UNEVENTFUL WITH N O OTHER INDICATION OF FIRE. UPON LANDING, FIRE DEPT CHECKED FOR HEAT SOURCES WITH NONE FOUND. CONTRACTED FOR INSPECTIO N AND MAINT, FOUND THAT THE RT (NR 2) ENGINE WAS MAKING SMOKE THROUGH THE ENGINE BLEEDS AND INJECTING SMOKE INTO THE CAB IN. THIS ENGINE WAS A LOANER ENGINE FROM MFG AND AS SUCH MFG WAS CONTACTED. SERV REP WAS ON SITE AND DETERMINED THAT O IL WAS LEAKING INTERNALY AND ENGINE IS BEING REMOVED AND SERVICEABLE ENGINE INSTALLED. NOT KNOW AT THIS TIME WHAT PART F 2 L 7 2 4F 4 F RT A3EU E35NE 20080717 NM 2008 7 17 SWAA083310 1 20080617 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 EEPLS LIGHT LENS MISSING AT ROW 5 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080717 WP 2008 7 17 08FDEA02029 1 20080529 A 5321 AGA387715 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 AFT PIT FLOOR PANEL 187 FF REQUIRES FAB NEW. FABRICATED NEW FLOOR PANEL 187 FF; POTTED EDGES; COMPLETED CURE AND SAND ED EDGE POTTING; INSTALLED INSERTS; FABRICATED TOP SHEET; LAYED UP UNDER A VAC BAG; BACK DRILLED AND COUNTERSUNK HOLES; APPLIED NON-SKID AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005, REV F AND 25-011, REV C. 2 L 7 3 4F RT A22WE 20080717 WP 2008 7 17 08FDEA02062 1 20080530 A 5280 ANB72163 SKIN DOUG MD10 MD1010F 3022112 WP MLG DOOR WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 LEFT MLG DOOR SKIN A THE OUTBD T/E IS WORN AND BENT. BLENDED OUT DAMAGE. ORIGINAL MATERIAL 0.063 IAW DC/MD-10 SRM 52-8 0-01; VOL III. MATERIAL REMOVED 0.013. MATERIAL REMAINING 0.050. FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 52-00-0 1; VOL I; VOL I. WTG NR T8225P DOUBLER REPAIR IAW DC/MD-10 SRM 52-10-00; VOL I. LOCATED AND DRILLED DOUBLER IAW DC/MD -10 SRM 51-31-01; VOL II. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01; PGS 24 AND 21; VOL II. INSTALLED DOUBLER REP AIR IAW DC/MD-10 ARM 51-31-01; VOL II. PAINTED IAW DC/MD-10 SRM 51-21-02; VOL II AND DOUBLER REPAIR SR1052000-3-15, PO 621189.1. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 SWAA083257 1 20080613 A 3397 W4142001220 WIRE BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 486WN 33852 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 10 ABC. FOUND BROKEN WIRE AT LIGHT ASSY. REPAIRED WIRE PER WDM AND MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083311 1 20080617 A 3211 69416335 PIN BOEING 737 7375H4 138449D NM RT MLG TRUNNION CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED SPV CHECK, FOUND RT MLG TRUNNION PIN CORRODED. REMOVED AND REPLACED PIN PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 08FDEA02054 1 20080530 A 5313 655623620 STRINGER BOEING 727 727227 1384078 NM BS 735-740 S27R CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 490FE 21493 FWD CARGO COMPARTMENT, STR 27R IS CORRODED FWD OF STA 740 REMOVED FASTENERS IAW B-727 SRM 51-30-2, CUT-OUT DAMAGED AREA (DIM 9 1/4 INCH LONG) AND FABRICATED FILLER FROM BAC1498-147 0.090" PO NR 8150104 ( DIM 9 1/4" LONG ) AND STRINGER SPLIC E FROM BAC1498-131 7075-T6 PO NR 9006522 (DIM 11 INCH LONG) IAW B-727 SRM 53-10-3 FIG 1 AND 53-10-2 FIGURE 9. TREATED A ND PRIMED PARTS IAW B-727 SRM 51-10-2 AND INSTALLED REPAIR PARTS AT FWD CARGO COMPT STR 27 RT FWD OF STA 740 IAW B-727 S RM 53-10-3 FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 20080717 NM 2008 7 17 08FDEA02055 1 20080530 A 5313 65564225 STRINGER BOEING 727 727227 1384078 NM BS 735-740 S28L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 490FE 21493 FWD CARGO COMPARTMENT, STR 28L HAS BULGING SEAL ON O/B SIDE JUST FWD OF STA 740 EVIDENCE OF CORROSION REMOVED SEALANT AN D CLEANED AREA. NO CORROSION NOTED IAW BSOPM 20-30-03. TREATED AND PRIMED AREA IAW B727 SRM 51-10-2. RESEALED AREA IA W FX 727-200 51-31-000-2. 2 L 7 3 4F A3WE 20080717 WP 2008 7 17 08FDEA02085 1 20080602 A 5753 ARC0212504 PANEL DOUG MD10 MD1010F 3022112 WP TE FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 RIGHT WING INBD FLAP HINGE PANEL 641 BR IS WORN. REPAIRED RIGHT WING INBD FLAP HINGE PANEL 641 BR BY REMOVING DAMAGED A REA AND BONDING A FILLER AND DOUBLER REPAIR IAW DC/MD-10 SRM 51-71-00; VOL II. ALODINED AND PRIMED IAW DC/MD-10 SRM 51- 2-01; VOL II AND SEALED IAW DC/MD-10 SRM 51-41-01; VOL II. 2 L 7 3 4F RT A22WE 20080717 SO 2008 7 17 SWIA200819813 1 20080625 A 4930 LINE EMB 120 EMB120ER 3260203 SO APU FUEL SYS LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 NM 07 581SW 120349 FLT 5799 - APU IS DRIPPING FUEL. REPLACED AFT LINE ON APU FUEL MANIFOLD IAW EMB MM 49-30-17. NO LEAKS NOTED. 2 L 7 2 4T RT A31SO 20080717 NE 2008 7 17 ASAA0853107 2 20080623 A 7320 1853M56P12 HYDROMECH UNIT BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAULTY A ASAA L ABORTED APPROACH J WARNING INDICATION NR NOT REPORTED 1 NM 02 584AS 3436 35682 894832 ENG NR 2 SHORT TERM FAULT MSG NO. FAULT CODE NR 73 20342. THE FMVPOSITION SIGNAL OUT OF RANGE. PERFORMED TEST 12 AC TUATORS TEST CONFIRMED FAULT. VERIFIED ROTABLE COMPONENT MFG NR 442369 S/N NR 3219 REF IPC 73 21 10 01 ITEM 25T. REPLA CED HMU REF MM 73 21 10 400 801 FOO AND 000 801 F00. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 20080717 NE 2008 7 17 ASAA0853109 2 20080628 A 7261 OIL SYSTEM BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE LOW A ASAA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 02 577AS 5186 35186 894540 BOTH ENGINE OIL QUANTITIES LOW NR 1 AT 13 NR 2 AT 14. SERVICED NR 1 ENG WITH 5QT OF OIL. SERVICED NR 2 ENG WITH 5 QT O FOIL. 2 L 7 2 4F 4 F RT A16WE E2GL 20080717 SO 2008 7 17 SWIA200819809 1 20080618 A 2611 47359713 SMOKE DETECTOR EMB 120 EMB120ER 3260203 SO CARGO BAY FAULTY A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 298SW 14418 14418 120328 RECEIVED CARGO SMOKE MESSAGE UPON APU START UP. REPLACED FORWARD CARGO SMOKE DETECTOR IAW EMB 120 MM 26-15-01. OPS CHE CK GOOD. 2 L 7 2 4T RT A31SO 20080717 2008 7 17 SWIA200819811 4 20080625 A 3497 CONNECTOR EMB 120 EMB120ER 3260203 SO DISPLAY BURNED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 227SW 120304 FLT 5574 - DISPLAY SCREEN WENT BLANK. REPLACED TWO DAMAGED PINS AT J2 CONNECTOR. DISPLAY OPERATES NORMALLY. 2 L 7 2 4T RT A31SO 20080717 WP 2008 7 17 08FDEA02228 1 20080612 A 5310 AFA00433 BEAM DOUG DC10 DC1010 3022110 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 CTR CARGO COMPT SUMP AREA FOUND CRACK ON BEAM. REPAIRED AREA IAW SRM 53-00-01 FIG 9 SHT 9 VOL I. 2 L 7 3 4F A22WE 20080918 NM 2008 9 18 UPS08553201 1 20080815 A 5340 STRINGER CLIP BOEING 757 75724APF 1384969 NM BS 1060 S6L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 STRINGER CLIP CRACKED AT FASTENER HOLE BS 1060 STR 6L. REMOVED, FABRICATED AND INSTALLED PER SRM 51- 40-02 DWG 140W2001. 2 L 7 2 4F RT A2NM 20080918 NM 2008 9 18 SWAA084801 1 20080831 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LGIHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 289CT 36633 DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 SWAA084802 1 20080829 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 BULLNOSE EMERGENCY EXIT LIGHT LENS MISSING AT ROW 13 DEF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080918 WP 2008 9 18 UPS08853209 1 20080812 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 880 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 DEEP SCRATCH ABOUT 16 INCHES LONG MAIN CABIN WING BOX FLOORBEAM UPPER SURFACE STA 880 LBL 25-45. FAB BED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-8, 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 20080918 WP 2008 9 18 UPS08853212 1 20080810 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1770 L19R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 CRACKED LONGERON END FITTING ON L19R AT STA 1770 INSIDE DOOR PANEL 60 COMPARTMENT. REMOVED AND REPLA CED FITTING IAW SRM, 51-1-8, 51-1-21, 51-3-1. 2 L 7 4 4F RT 4A25 20080918 WP 2008 9 18 UPS08853195 1 20080810 A 5340 ATTACH FITTING DOUG DC8 DC871F 302199D WP BS 1666 L21R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 CORRODED FRAME LWR CLIP ON THE UPPER SURFACE OF INTERIOR CUSP EXTRUSION STA 1666 L21R. REMOVED AND R EPLACED LOWER CLIP IAW SRM 51-1-8, 51-3-2, 51-1-20D. 2 L 7 4 4F RT 4A25 20080918 NM 2008 9 18 UPS08M53219 1 20080817 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 9 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53172 1 20080821 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 10 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53177 1 20080819 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 12 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53179 1 20080822 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 25 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 2008 9 18 2008UALA04322 4 20080815 A 2350 MICROPHONE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OXYGEN MASK FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 FIRST SEAT O2 MASK MIC INOP. *S/D* REPLACED O2 MASK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NM 2008 9 18 UPS08M53186 1 20080821 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 19 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53189 1 20080814 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 26 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 ZZDA2008153 1 20080823 A 5248 49344691 SPRING BOEING 717 717200 1383700 NM TAIL CONE MISSING A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 989AT 55152 A 1EA TAIL CONE RELEASE MECHANISM TENSION SPRING MISSING. INSTALLED 1EA TAIL CONE MECHANISM TENSION SPRING PER EA 17-53 -01195IR. 2 L 7 2 4F TR A6WE 20080918 NM 2008 9 18 2008UALA04339 1 20080817 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE SEAT 31B MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 EMERGENCY LIGHT STRIP ON RIGHT SIDE SEAT 31B MISSING. *S/D* REPLACED EEL LIGHT,OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20080918 NM 2008 9 18 2008UALA04386 1 20080821 A 7500 79027013 SHUTOFF VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BLEED SYSTEM ILLUMINATED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 662UA 27159 IN POWER REDUCTIONS ON DESCENT, RECEIVED L ENG HPSOV AND ASSOC BLEED LIGHT. WENT OUT AFTER 1 MINUTE. FOUND FAULTY HIGH PRESSURE SHUTOFF VALVE. HPSOV AND CONTROLLER REPLACED. OPS CK GOOD ON ENG. 2 L 7 2 4F 4 F RT A1NM E24NE 20080918 NM 2008 9 18 2008UALA03870 1 20080714 A 2500 TUBE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU LOOSE A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 930UA 26655 LOUD HISSING NOISE COMING FROM F/O WINDOW. RTFL. *S/D* CREW COMMENT: TUBE WAS STUCK IN SLIDING WINDOW. AFTER LANDIN G, CREW OPENED WINDOW & RECONNECTED. INSPECTED TUBE, AND FOUND NO ABNORMALITIES. RECONNECTED DRAIN TUBE. OKAY FOR SERVIC E. 2 L 7 2 4F 4 F RT A16WE E21EU 20080919 NM 2008 9 19 SWAA084856 1 20080903 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM BS 968 S26L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 26L CORRODED AT BS 968. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080919 NE 2008 9 19 2008UALA05396 2 20080822 A 7532 BLEED VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 ENGINE MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 223UA 30224 NR 2 ENGINE LT LOWER TURBINE VANE AND BLADE COOLING AIR VALVE WAS FOUND IN THE CLOSED POSITION. BEGAN REMOVAL OF NR 2 E NGINE LT LOWER TVBC VALVE UP TO BUT NOT INCLUDING STEP 7 PER MM 75-25- 01 CONFIG 2 PAGE 414. CONT OF AMIS ITEM 6602011: VALVE IN POSITION ON ENG WITH NEW FLANGE AND LARGE DUCT GASKET INSTALLED, 3 BOLTS LOOSELY INSTALLED ON FLANGE, AWAITING BOLTS TO CONTINUE INSTALLATION FROM 75-25-01 PAGE 419 ITEM 7.A. CONT OF AMIS ITEM 6602014 (PARTIAL) CONT OF AMIS ITEM 6 602015: COMPLETED INSTALLATION OF LOWER LT TVBC VALVE ON THE NR 2 ENGINE REF MM 75-25-01 PG 401. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080919 2008 9 19 2008UALA05397 4 20080822 A 2300 CONTROLLER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 408UA 457 CABIN EMERGENCY CALL GOES OFF BY ITSELF. REPLACED NR 1 CIDS DIRECTOR PER MM 23-73-00, TESTS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20080919 NM 2008 9 19 2008UALA05399 1 20080822 A 3110 CONTROL PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MALFUNCTIONED A UALA O OTHER O OTHER LD LANDING 1 WP 29 509UA 24763 ON APPROACH NO LIGHTS ON RIGHT SIDE OF ANY SELECTED MCP BUTTONS AND FLIGHT DIR WOULD NOT CAPTU. *S/D* MCP FAILED. REP LACED MCP. ALL L-C-R AUTOFLIGHT LAND CAT III TESTS PASSED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080919 NM 2008 9 19 2008UALA05400 1 20080822 A 5210 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR SEPARATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 531UA 25042 CREW REPORT: RUBBER DOOR SEAL 1L SEPARATED FROM DOOR. *S/D* SECURED SEAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080922 NM 2008 9 22 SWAA084872 1 20080904 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 277 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084873 1 20080904 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 277 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084935 1 20080908 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 767 S22R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084888 1 20080906 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 288WN 36611 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084890 1 20080907 A 5315 6545808 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 294.5, LBL 10.5. REPAIRED FLOORBEAM CHORD PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084891 1 20080907 A 5340 57463 FITTING BOEING 737 7373H4 1384600 NM L1 DOOR GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084896 1 20080905 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 489WN 33855 DURING SCHEDULED HC2 CHECK, LT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084897 1 20080905 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 621SW 28037 RT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084898 1 20080907 A 3350 3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 DURING SCHEDULED MV2 CHECK, FOUND BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 13 ABC. REMOVED AND REPLACED LIGHT BULB PE R MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084899 1 20080907 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 FWD CABIN EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084903 1 20080902 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 747 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 24L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080922 2008 9 22 SWAA084904 4 20080906 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084905 1 20080907 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 500C S24R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 24R. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084906 1 20080907 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 500D S20R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084925 1 20080907 A 5311 6545853 FRAME BOEING 737 7373A4 1384585 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 947, RBL 16. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084940 1 20080908 A 5311 6546538 FRAME BOEING 737 7373H4 1384600 NM BS 597 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084941 1 20080908 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 967 S27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER 27R CORRODED AT BS 967. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084946 1 20080908 A 5311 6546525 FRAME BOEING 737 737301 1384611 NM BS 380 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084947 1 20080908 A 5311 6546555 FRAME BOEING 737 737301 1384611 NM BS 867 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084948 1 20080908 A 5311 6546543 FRAME BOEING 737 737301 1384611 NM BS 787 S22R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 22R AND STR 21R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084949 1 20080908 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 787 S22R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 22R AND STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084950 1 20080908 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 767 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 18L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084827 1 20080902 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 FWD CABIN EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084828 1 20080902 A 5755 654645165A SKIN BOEING 737 7373H4 1384600 NM NR 1 SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED MV1 CHECK, FOUND LT WING NR 1 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084829 1 20080902 A 3350 10107451 SIGN BOEING 737 7377H4 1384404 NM R1 DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 R1 DOOR EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 08FDEA02060 1 20080530 A 5710 6521655440 BEAM BOEING 727 727227 1384078 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 490FE 21493 RT WING UPPER TRAILING EDGE "J " BEAM IS CRACKED AT WBL 118, WS 155 - WS 160 REMOVED NR 8 SPOILER FITTING FOR ACCESS IAW B727 SRM 51-30-2. TRIMMED OUT CRACK (DIMENSION 0.280 INCH IN LENGTH ) IAW B727 SRM 51-10-1 AND FEDEX DRAWING SR 27-57- 025 REV A. TREATED AND PRIMED AREA IAW FEDEX DRAWING SR 27-57-025 AND 51-10-2 AND REINSTALLED NR 8 SPOILER FITTING AT R T WING UPPER T/E AREA WBL 118 IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 20080717 EU 2008 7 17 08FDEA02221 1 20080611 A 5420 SHIM AIRBUS 300 A300F4605R 3930327 EU NR 1 PYON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 NR 1 PYLON RIB 3-A; STA 615, THE OUTBD SIDE SHIM HAS A 3/4 INCH CRACK. 2 L 7 2 4F RT A35EU 20080717 NM 2008 7 17 ASAA0843031 1 20080514 A 5753 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 LEFT WING INBOARD MID FLAP UPPER SKIN CHAFED AT INBOARD END CUT OUT DAMAGED AREA. FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 57 53 01 FIG 201 REPAIR 3. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843032 1 20080514 A 5753 SKIN BOEING 737 737490 1384715 NM RT WING TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 RIGHT WING INBOARD MID FLAP UPPER SKIN CHAFED AT INBOARD END WITH A DENT CUT OUT DAMAGED AREA. FABRICATED REPAIR PARTS AND INSTALLED IAW B737 400 SRM 57 53 01 FIG 201 SHEET 2 OF 3 REPAIR 2. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 08FDEA02003 1 20080528 A 5320 AGA70947 STANCHION DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 AFTER REMOVAL OF FORWARD CARGO AFT BULKHEAD STA 6-70 PANEL FOR WIRING INSPECTION FOUND PANEL SUPPORT APPROXIMATELY 10 INCH RIGHT FROM CENTER FOUND CORRODED. CORRODED STANCHION AT FORWARD CARGO AFT BULKHEAD STA 6-70 10 INCH RIGHT FROM CEN TER REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. STANCHION FABRICATED AS PER DOUGLAS DRAWING AGA7094. REPAIR CL ASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 ASAA0843042 1 20080609 A 5210 60440611 TORQUE TUBE BOEING 737 7374Q8 138447Q NM L2 DOOR CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 002219 25101 L2 MAIN ENTRY PASSENGER DOOR LOWER DOOR HINGE CHAFING ON HARDWARE MIG2C 222915 INT REMOVED AND REPLACED TORQUE TUBE RADI US LING ASSY AND TORQUE TUBE SPLINED END REF AMM 52 13 11. VERIFIED ALL MIG2C 222915. ITEMS CLEARED. 2 L 7 2 4F RT A16WE 20080717 EU 2008 7 17 08FDEA02247 1 20080612 A 7830 WARNING LIGHT AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7 52054 NE THRUST REVERSER ILLUMINATED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 452FE 313 715438 ON TAKEOFF FROM CDG GOT REVERSE UNLOCK LIGHT ON ECAM ALSO MATCHED WENT TO NR 2 ENG REVERSE. LIGHT WENT OUT THEN CAME BA CK ON WITH POWER ADVANCE. LEFT NR 2 AT IDLE AND CAME BACK TO LAND ASAP CDG. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01 -C CATEGORY: C EXPIRATION: 22JUN08 "MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2) NR 2 THRUST REVERSER, INOP. THRUST REVERSE R IS DEACTIVATED IN FORWARD THRUST POSITION. 2 L 7 2 4F 4 F RT A35EU E20EA 20080717 NM 2008 7 17 08FDEA02200 1 20080608 A 5313 655623664 STRINGER BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 490FE 21493 INTERNAL FUSELAGE FWD CARGO COMPARTMENT, STRINGER 28R CORRODED AT BS 500. REMOVED INTERCOSTAL AT BS 480-500 STR 28 RT I AW B-727 51-30-2, CUT-OUT DAMAGE STRINGER, (DIM 23 1/2 INCH LONG). FABRICATED STRINGER FILLERS FROM BAC1498-205 PO NR 6 42842 (DIM 13 INCH LONG AND 10 5/8 INCH LONG) IAW B-727 SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9, CUT-OUT DAMAGED SKIN (DIM 8 INCH BY 3 1/4 INCH) AND FABRICATED SKIN DOUBLER FROM 2024-T3 0.090 INCH PO NR 9006027 (DIM 19 1/4" BY 11") AND REPAIR F ILLER FROM 2024-T3 0.080 INCH PO NR 9006377 (DIM. 8" BY 3 1/4") IAW B-727 SRM 53-30-3 FIG 3 AND 53-30-2 FIG 2, INSTALLED REPAIR PARTS AND REINSTALLED INTERCOSTAL IAW B-727 SRM 51-30-2. 2 L 7 3 4F A3WE 20080717 EU 2008 7 17 08FDEA02203 1 20080609 A 2930 INDICATION SYS AIRBUS 300 A300B4622R 3930312 EU HYD SYSTEM MALFUNCTIONED A FDEA R AUTOROTATION J WARNING INDICATION DE DESCENT 1 CE 21 748FD 633 LEFT ECAM INDICATED GREEN SYS HYD RESVR LO LEVEL ON DESCENT. GREEN SYS HYD OVERHEAD PANEL GAUGE INDICATED BOTTOM OF YEL LOW ARC. RT ECAM HYD POINTER INDICATED BOTTOM OF YELLOW ARC. AFTER COMPLETING HYD RSVR LO LEVEL PROC AND L/G GRAVITY E XT PROC, GREEN SYS QUANTITY RETURNED TO NORMAL. SERVICED GREEN SYSTEM HYDRAULICS PER FEDEX A300-600 M/M 12-12-29-0. PR ESSURIZED SYSTEM NO LEAKS NOTED. RAN ENGINES PER FEDEX A300 JRH CHAP 5. DURING RUN EXERCISED ALL FLT CONTROLS NO LEAKS FOUND, HYD QTY AND PRESS OPS CHECKED GOOD. RESTORED LANDING GEAR TO NORMAL OPERATING CONDITION PER A300-600 M/M 32-33 -00-5 AND EA 6-3231-71640. 2 L 7 2 4F RT A35EU 20080717 NM 2008 7 17 SWAA083266 1 20080617 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 DHL2008764534 1 20080521 A 5523 TAB BOEING 727 727264 138408M NM LT ELEVATOR BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 764AT 22984 LT ELEV TAB INBD CORNER DAMAGED, REMOVED DAMAGED AREA, FABRICATED REPAIR, AND INSTALLED BY BONDING IAW B727 SRM 51-40-20 PGS 12 THROUGH 62 AND SRM 51-80 FIG 2. NO FURTHER ACTION REQUIRED. 2 L 7 3 4F A3WE 20080716 NM 2008 7 16 2008UALA03089 1 20080529 A 3350 209 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 DOOR 5L DOOR MOUNTED EMERG EXIT LIGHT TURNS OFF AFTER A FEW SECONDS OF OPERATION. FOUND FAULTY LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080716 WP 2008 7 16 DHL2008807513 1 20080509 A 5540 STIFFENER DOUG DC8 DC873F 302199F WP RUDDER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 91019 45990 RUDDER INTERNAL STRUCTURE STIFFENER CRACKED 1.500 INCH STA ZR 162.000. REMOVED CRACKED STIFFENER IAW SRM 51-1-21. CLEA NED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW STIFFENER IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 BB08100 1 20080528 A 2560 P4010021 BATTERY BOEING 767 767201 1385125 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 250AY 23902 PHL - THE AFT LEFT FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE AFT LEFT FLASHLIGHT BATTERY. 2 L 7 2 4F RT A1NM 20080716 CE 2008 7 16 DJFA2008049 1 20080531 A 5514 45A21086004 BRACKET BEECH MU300 400A 1155402 CE HORIZ STAB CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 452LX 776 RK317 DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABIL IZER INBOARD RIB AND BRACKET ASSEMBLIES, THE RIGHT AFT ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIO NS OF THIS AREA ARE OUTLINED IN BEECHJET COMMUNIQUE' NUMBER 70. SDR WILL BE UPDATED UPON COMPLETION OF CORRECTIVE ACTIO N. 2 H 7 2 4F RT A16SW 20080716 NM 2008 7 16 DHLA200800050 1 20080601 A 2782 1U1110 ACTUATOR BOEING 727 727200 138407E NM KRUEGER FLAP LEAKING A DHLA C ABORTED TAKEOFF K FLUID LOSS TO TAKEOFF 1 GL 05 752DH 209 22466 FLIGHT 1612 ON TAKEOFF ROLL, A/C SUSTAINED HYD A-SYSTEM FAILURE PRIOR TO 60 KIAS. FOUND NR 5 KRUEGER FLAP LEAKING. REM OVED AND REPLACED NR 5 KRUEGER FLAP ACTUATOR. SERVICED A-SYS. INSP NR 1 & 2 CASE DRAIN FILTERS. OPS CHECK GOOD. NO F URTHER LEAKS NOTED. HYD PRESSURE NORMAL IAW AMM 27-81 22, 29-11-41, 12-12-00. AIRCRAFT WAS GROUNDED. 2 L 7 3 4F RT A3WE 20080716 WP 2008 7 16 UPS08852535 1 20080524 A 5347 3657502U507 SEAT TRACK DOUG DC8 DC873F 302199F WP FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 PILOT REAR LT AND RT SEAT TRACKS SHOW ELONGATIONS REMOVED AND REPLACED 2 EACH SEAT TRACKS IAW SRM , 51-1-20D, 51-1-24. 2 L 7 4 4F RT 4A25 20080716 WP 2008 7 16 UPS08852542 1 20080613 A 5321 5777814 FLOOR PANEL DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 COURIER AREA FLOOR PNL F25 SKIN CORRODED. REPAIRED CABIN FLOOR PNL F25 IAW SRM 53-1-21, SRM 53-02-00 FIG 1F, AND DWG 5777814. 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 ZZDA2008120 1 20080612 A 2120 UNKNOWN BOEING 737 7377BD 1384511 NM CABIN ODOR A ZZDA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 37 318AT 33931 SHORTLY AFTER TAKEOFF THE FLIGHT ATTENDANTS REPORTED A BURNING SMELL AROUND THE GALLEY AREA. RETURNED TO ATL, LANDING W EIGHT 110,000. UPON ARRIVAL, NO UNUSUAL SMELL OR BURNING SMELL NOTED, NO CIRCUIT BREAKERS POPPED. INSPECTED GALLEY ARE A, CABIN, LAVS, OVERHEAD BINS, CARGO BINS, AFT EQUIPMENT BAY, AND FORWARD E/E BAY. OPERATED COFFEEMAKERS, CREDIT CARD R EADERS AND LIGHTS. RAN BOTH ENGINES AND APU WITH PACKS ON AND PRESSURIZED A/C. NO EVIDENCE OF SMELL OR SMOKE NOTED. R EF FIM 21-50. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SWAA082886 1 20080528 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM BS 500C S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 KCSA081264 1 20080529 A 5347 CARGO TRACK BOEING 747 747212B 1384886 NM BS 560 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 FWD PIT CARGO PALLET RESTRAINT BRACKET CRACKED AT FWD LOWER CORNER OF THE FWD PIT DOOR BS 560, RBL-67. 2 L 7 4 4F RT A20WE 20080716 NM 2008 7 16 SWAA082934 1 20080531 A 3213 654610222 LINK BOEING 737 7373Q8 1384670 NM RT MLG BROKEN A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 685SW 23401 RIGHT MLG LOWER TORSION LINK BROKEN. REMOVED AND REPLACED TORSION LINK PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083549 1 20080626 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER 23R CRACKED AT BS 359. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083572 1 20080629 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 371, STR 26L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083600 1 20080629 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083601 1 20080629 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 08FDEA02352 1 20080620 A 5320 A53988524204 STRUT AIRBUS 300 A300B4622R 3930312 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION SPOTS AT AFT FACE OF LT CROSS STRUT C85 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-00. 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 08FDEA02354 1 20080620 A 5414 311N51931 PANEL BOEING 757 75727B 1384921 NM ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 916FD 24137 PYLON NUMBER TWO RIGHT SIDE STRUT SKIN CUTOUT AT ACCESS PANEL 443AR FOUND CORROSION, FROM PPS100 TO PPS126. EVALUATE AND RECTIFY. REPLACED PYLON NUMBER TWO STRUT SKIN CUTOUT PANEL 443AR IN ACCORDANCE WITH BOEING DRAWING 311N5002 ID001 4, SRM 51-10-02 REV 93. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080718 NM 2008 7 18 08FDEA02122 1 20080603 A 5100 NONE DOUG MD11 MD11F 3023600 NM IAW SRM NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 590FE 48505 EXISTING REPAIR, MAIN DECK EXISTING TRANSVERSE FRAME REPAIR FOUND AT STA 1761 LONGERON 12L. EXISTING REPAIR AT MAIN DEC K EXISTING TRANSVERSE FRAME STA 1761 LONGERON 12L EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-30-00 FIGURE 1 VOLUME I FEDEX EO NR 1-5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG, MD11 REPAIR CATALOG AND TRACKING REQUIREMENTS, H AS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 SWAA083553 1 20080626 A 3350 101073 LENS BOEING 737 7373K2 13844BA NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083574 1 20080629 A 5755 654645170A SPOILER BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND LT WING NR 3 FLIGHT SPOILER DELAMINATED AT INBOARD END. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083555 1 20080626 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 28R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080718 2008 7 18 SWAA083578 4 20080625 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083563 1 20080626 A 5755 654645168A SKIN BOEING 737 7373L9 1384470 NM SPOILER DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 7 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083562 1 20080626 A 5230 6552873 SKIN BOEING 737 7373L9 1384470 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 DURING SCHEDULED HC2 CHECK, FOUND FWD CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 M7K2008F00024 1 20080512 A 6710 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE FAILED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 823MH 1073 4158 A FAULT CODE WAS GENERATED ON SHUTDOWN INDICATING A DEFECT OF COLLECTIVE POTENTIOMETER. A NEW PART WAS INSTALLED, NO FU RTHER FAULT WAS DETECTED. THIS IS RECURRING FAILURE FOR THIS PART WHICH HAS EFFECTED DISPATCH RELIABILITY FOR THIS MODE L HELICOPTER. SUGGEST AN ALTERATION OF FAULT SENSING SOFTWARE TO REDUCE FAULT SENSITIVITY TO PERHAPS A SIGNAL LOSS OF 0 .5 SECOND RATHER THAN 1/20TH OF A SECOND. AN OPTIC RATHER THAN A RESISTANCE BASED SENSOR SHOULD BE CONSIDERED AS CONTAC T POINT IS DAMAGED BY AC VIBRATION WHEN AC POWER SETTINGS ARE SET FOR CRUISE FLIGHT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 NE 2008 7 18 M7K2008F00034 2 20080612 A 7261 800301 MAGNETIC SEAL UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE LEAKING E M7KA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 810MH 1047 3949 23318 DURING ROUTINE INSPECTION EXCESSIVE OIL LEAKAGE WAS NOTED AT THE MODULE 5 OUTPUT MAGNETIC SEAL. CLOSE INSPECTION OF THE REMOVED SEAL REVEALED NO OBVIOUS DEFECT. A NEW SEAL WAS INSTALLED WITH NO FURTHER LEAKAGE NOTED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 EU 2008 7 18 M7K2008F00022 1 20080612 A 2612 9550177130 FIRE DETECTOR UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE INTERMITTENT E M7KA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 19 809MH 572 3927 46047 DURING FLIGHT, PILOT REPORTED THAT THE FIRE LIGHT ILLUMINATED IN A FLICKERING FASHION, FLIGHT WAS ABORTED. NO EVIDENCE O F FIRE OR HEAT WAS FOUND AND TROUBLESHOOTING PROCEDURES OF THE MM WERE FOUND INEFFECTIVE AT DISCOVERING WHICH OF (3) DE TECTORS WAS FAULTY. RETORQING THE TERMINAL CONNECTIONS HAD RESOLVED A SIMILAR PROBLEM WITH THIS ENGINE SEVERAL WEEKS PR EVIOUSLY. IN THIS CASE PROBLEM REMAINED INTERMITTENTLY DURING SUBSEQUENT SYSTEM CHECKS. ALL (3) DETECTORS WERE REPLACED WITH NO FURTHER DEFECT NOTED. SUGGEST A DIFFERENT DESIGN DETECTOR OR QC IMPROVEMENTS BE MADE WITH THIS PART AS SEVERAL INSTANCES OF FALSE FIRE INDICATIONS HAVE SHAKEN CONFIDENCE IN SYS. IT IS QUESTIONABLE WHY THERE IS EVEN SUCH A SYS ON A 1 G 7 2 3U 3 U H9EU E00054EN 20080718 NM 2008 7 18 SWAA083537 1 20080625 A 3233 273A12012 ACTUATOR BOEING 737 7377H4 1384404 NM NLG FAULTY A SWAA K NONE J WARNING INDICATION AP APPROACH 1 SW 29 740SW 29276 EXTENDED LANDING GEAR ON APPROACH TO MHT, THE NLG RED LIGHT ILLUMINATED, NO GREEN LIGHT. OVERHEAD INDICATIONS GREEN FOR MLG BLANK FOR NLG. CYCLED GEAR INDICATED NORMAL. REMOVED AND REPLACED NLG LOCKING ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083595 1 20080629 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 743SW 29279 DURING SCHEDULED MV2 CHECK, FOUND RT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 M7K2008F00021 1 20080612 A 2612 9550177160 FIRE DETECTOR UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE INTERMITTENT E M7KA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 19 809MH 572 3927 DURING FLIGHT, PILOT REPORTED THAT FIRE LIGHT ILLUMINATED IN A FLICKERING FASHION AND FLIGHT WAS ABORTED. NO EVIDENCE OF FIRE OR HEAT WAS FOUND AND TROUBLESHOOTING PROCEDURES OF THE MM WERE FOUND INEFFECTIVE AT DISCOVERING WHICH OF (3) DET ECTORS WAS FAULTY. RETORQING THE TERMINAL CONNECTIONS HAD RESOLVED A SIMILAR PROBLEM WITH THIS ENGINE SEVERAL WEEKS PRE VIOUSLY. IN THIS CASE PROBLEM REMAINED INTERMITTENTLY DURING SUBSEQUENT SYSTEM CHECKS. ALL (3) DETECTORS WERE REPLACED W ITH NO FURTHER DEFECT NOTED. SUGGEST A DIFFERENT DESIGN DETECTOR OR QC IMPROVEMENTS BE MADE WITH THIS PART AS SEVERAL I NSTANCES OF FALSE FIRE INDICATIONS HAVE SHAKEN CONFIDENCE IN SYS. IT IS QUESTIONABLE WHY THERE IS EVEN SUCH A SYS ON A 1 G 7 2 3U 3 U H9EU E00054EN 20080718 EU 2008 7 18 M7K2008F00032 1 20080523 A 5551 350A23422320 FITTING UROCOP UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE HORIZONTAL STAB CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 808MH 3914 23072 DURING ROUTINE INSPECTION, THE FITTING WAS FOUND CRACKED FROM AN OB ATTACHMENT SCREW BORE TO FLANGE EDGE. NEW FITTING WA S INSTALLED. THIS ISA COMMON FAILURE FOR THIS PART. BORE HOLES MUST BE MATCH DRILLED AND ALIGNED PERFECTLY. SUGGEST A MORE DURABLE MATERIAL BE USED IN THIS PARTS MFG SUCH AS TITANIUM OR SS AS ALUMINUM ALLOY FAILS ROUTINELY UNDER NORMAL S TRESS APPLIED TO THIS PART. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 NM 2008 7 18 SWAA083597 1 20080629 A 5310 147A5503 CREASE BEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 947 AND BS 986.5, RBL 65. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083598 1 20080629 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 DURING SCHEDULED 8Y CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083618 1 20080629 A 5340 BAC1503 STRINGER CLIP BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 772SW 27880 DURING SCHEDULED 8Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 M7K2008F00015 1 20080512 A 6220 350A31191701 STARFLEX UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE M/R HUB ASSY CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 846MH 498 M3001 4248 DURING ROUTINE INSP ADHESIVE BEAD FOR A STAR ARM END BUSHING WAS FOUND CRACKED. FURTHER EXAMINATION UTILIZING A SOAP WA TER DETECTION METHOD REVEALED RELATIVE MOTION BETWEEN BUSHING AND STAR ARM END. WITH ROTOR HUB SLEEVES REMOVED, BUSHING COULD BE MOVED MANUALLY. A SECOND BUSHING WAS ALSO FOUND LOOSE. A SERVICEABLE REPLACEMENT STARFLEX WAS INSTALLED. THIS IS A DEFECT THAT RECENTLY HAS BECOME MORE COMMON THAN IN THE PAST. SUGGEST A DIFFERENT ADHESIVE BE UTILIZED OR THE STAR ARM ENDS AND BUSHINGS BE DESIGNED TO HAVE A LARGER ADHESIVE BONDING SURFACE SUCH AS ADDING INNER BUSHING AND OUTER STAR ARM END SPLINING. THERE WAS NO EVIDENCE OF ANY IMMINENT FAILURE FOR THE PART OR EXCESSIVE PLAY DEVELOPMENT OF THE BUSHI 1 G 7 2 3U 3 U H9EU E00054EN 20080718 EU 2008 7 18 M7K2008F00016 1 20080512 A 6220 350A31191701 STARFLEX UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE M/R HUB ASSY CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 849MH 203 4313 23458 DURING ROUTINE INSP, ADHESIVE BEAD FOR A STAR ARM END BUSHING FOUND CRACKED. FURTHER EXAMINATION UTILIZING A SOAP WATER DETECTION METHOD REVEALED RELATIVE MOTION BETWEEN BUSHING & STAR ARM END. WITH ROTOR HUB SLEEVES REMOVED, BUSHING COULD BE MOVED MANUALLY. A SERVICEABLE REPLACEMENT STARFLEX WAS INSTALLED. THIS IS A DEFECT THAT RECENTLY HAS BECOME MORE COM MON THAN IN THE PAST. SUGGEST A DIFFERENT ADHESIVE BE UTILIZED OR THE STAR ARM ENDS AND BUSHING BE DESIGNED TO HAVE A LA RGER ADHESIVE BONDING SURFACE SUCH AS ADDING INNER BUSHING AND OUTER STAR ARM END SPLINING. NO EVIDENCE OF ANY IMMINENT FAILURE FOR PART OR EXCESSIVE PLAY DEVELOPMENT OF BUSHING. SUGGEST THAT APPLICATION OF A SLIPPAGE MARK BETWEEN STAR ARM 1 G 7 2 3U 3 U H9EU E00054EN 20080718 NM 2008 7 18 SWAA083617 1 20080629 A 5340 BAC1503 STRINGER CLIP BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 772SW 27880 DURING SCHEDULED 8Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294.5, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080718 NE 2008 7 18 SWAA083538 2 20080624 A 7230 COMPRESSOR BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE NR 1 ENGINE STALLED A SWAA K NONE R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET NR NOT REPORTED 1 SW 29 794SW 30605 874108 COMPRESSOR STALL ON NR 1 ENGINE, FLIGHT CREW REPORTED VIBRATION FOR THREE SECONDS AFTER STALL. REMOVED AND REPLACED NR 1 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080718 NM 2008 7 18 SWAA083489 1 20080625 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 257WN 32515 R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083493 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 M7K2008F00014 1 20080512 A 6220 350A31191700 STARFLEX UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE M/R HUB ASSY CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 806MH 1299 M2528 3833 23220 (REF 0501083833) DURING ROUTINE INSP, ADHESIVE BEAD FOR A STAR ARM END BUSHING WAS FOUND CRACKED. FURTHER EXAMINATION U TILIZING A SOAP WATER DETECTION METHOD REVEALED RELATIVE MOTION BETWEEN THE BUSHING AND STAR ARM END. WITH ROTOR HUB SLE EVES REMOVED BUSHING COULD BE MOVE MANUALLY. A SERVICEABLE REPLACEMENT STARTFLEX WAS INSTALLED. THIS IS A DEFECT THAT RECENTLY HAS BECOME MORE COMMON THAN IN THE PAST. SUGGEST A DIFFERENT ADHESIVE BE UTILIZED OR THE STAR ARM ENDS AND BUS HING BE DESIGNED TO HAVE A LARGER ADHESIVE BONDING SURFACE SUCH AS ADDING INNER BUSHING AND OUTER STAR ARM END SPLINING. THERE WAS NO EVIDENCE OF ANY IMMINENT FAILURE FOR THE PART OR EXCESSIVE PLAY DEVELOPMENT OF THE BUSHING. SUGGEST THAT 1 G 7 2 3U 3 U H9EU E00054EN 20080926 EU 2008 9 26 08FDEA03338 1 20080808 A 5321 R532B362200000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 231 AH IS DAMAGED. REPAIRED CABIN FLOOR PANEL 231 AH BY FABRICATING A NEW PANEL USING THE OLD PANEL A S A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SKID TAPE IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 08FDEA03931 1 20080917 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 DURING OPEN HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D. MAIN DECK CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARRIED OUT ON FITTING HOLES A, B, C AND D AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080926 EU 2008 9 26 08FDEA03339 1 20080808 A 5321 R532B361600000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 231 QG IS DAMAGED. REPAIRED CABIN FLOOR PANEL 231 QG BY FABRICATING A NEW PANEL USING THE OLD PANEL A S A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SKID TAPE IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03386 1 20080812 A 5321 B7327032200300 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DECK PANEL 262 AH HAS AN INSERT PULLING LOOSE ON THE AFT LOWER SURFACE. FABRICATED NEW PANEL IAW SRM 53-10 -20 AND DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1001. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03387 1 20080812 A 5321 B7327031200100 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DECK PANEL 262 AH HAS A CRACK ON THE LOWER SURFACE. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005 ; REV "G". PART MARKED PANEL IAW GMM 7-0-1001. 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 08FDEA03389 1 20080812 A 5210 69202005 BRACKET BOEING 727 7272S2F 1384O81 NM L1 DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 L-1 GRAB ASSIST HANDLE MOUNT BRACKET CRACKED ON DOOR REPLACED FWD ENTRY DOOR ASSIST BRACKET REF: SRM 51-30-2 PG 13. THI S IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080926 EU 2008 9 26 08FDEA03328 1 20080808 A 5321 R532B385400200 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 241 KJ IS DAMAGED. REPAIRED CABIN FLOOR PANEL 241 KG BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARK ED AND APPLIED NON-SKID TAPE IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 08FDEA03530 1 20080821 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 587FE 48489 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK INDICATIONS AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FITTING HOLES A, B, C AND D CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080926 NM 2008 9 26 08FDEA03544 1 20080822 A 5330 SKIN BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 EXTERIOR SKIN PILLOWING AND BULGED WITH BROKEN AND PULLED RIVETS STA 309 TO 312 STR 24L. FABRICATED REPAIR DOUBLER FROM 2024-T3 .071 PO NR 9007561 DIMS 12 INCH BY 7 INCH. FABRICATED STRUCTURAL FILLER FROM 2024-T3 .063 PO NR 9007007 DIMS 1 2 INCH BY 5 INCH AND INSTALLED REPAIR PARTS AT BS 309-312 STR 24L IAW B727 SRM 53-30-3 FIG 14, SRM 53-30-2 FIG 2 AND SRM 51-30-2. 2 L 7 3 4F RT A3WE 20080926 EU 2008 9 26 08FDEA03280 1 20080806 A 5321 B5327028700200 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DOOR PANEL NR 251 BH, CENTER CUT-OUT IS CRACKED. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; R EV "G". 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03282 1 20080806 A 5321 B5327028000600 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DOOR PANEL NR 251 VF; FWD END IS CRACKED AND HAS SEVERAL PUNCTURES. FABRICATED NEW PANEL IAW SRM 53-10-20 A ND DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080926 2008 9 26 SWAA085004 4 20080911 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085005 1 20080911 A 5311 6546557 FRAME BOEING 737 737301 1384611 NM BS 887 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085006 1 20080911 A 5315 BAC15091000146 FLOORBEAM BOEING 737 737301 1384611 NM BS 773 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CHANNEL CRACKED AT BS 773, LBL 12. REPAIRED FLOORBEAM CHANNEL PER SWA EA. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085007 1 20080911 A 5330 6545776 SKIN BOEING 737 7373Y0 1384671 NM BS 927 S25R DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CREASED AT BS 927, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 2008UALA05692 1 20080914 A 2910 FITTING BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RT HYD SYSTEM DAMAGED A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 676UA 30028 RIGHT HYDRAULIC SYSTEM RF IN EICAS. HYDRAULIC LEAK IN LT WHEEL WELL COMING FROM UPPER AFT HYDRAULIC MOD. IT LEAKS WITH CENTER ADP RUNNING. TRACED LEAK TO PRESSURE INLET LINE OF ADP FILTER MODULE, UNION O-RING REPLACED, NO LEAKS NOTED. ARE A CLEANED AS REQUIRED. 2 L 7 2 4F 4 F RT A1NM E24NE 20080926 NM 2008 9 26 2008UALA05693 1 20080915 A 2780 3930007102 CONTROL VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 SLAT FAILED A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 771UA 26932 NR 1 SLATS PRIMARY FAIL UPPER EICAS. *S/D* SLAT PRIMARY CONTROL VALVE FAILURE. REPLACED SLAT PRIMARY CONTROL VALVE & SVC'D CENTER HYD RESERVOIR. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080926 2008 9 26 2008UALA05695 4 20080912 A 2565 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R1 DOOR SLIDE LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 449UA 851 SLIDE 1R DOOR PRESSURE LOW READS 1550. SERVICED DOOR ASSIST BOTTLE PRESSURE TO WITHIN LIMITS. 2 L 7 2 4F 4 F RT A28NM E40NE 20080926 NM 2008 9 26 2008UALA05698 1 20080912 A 2697 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 3 FIRE DETECT DAMAGED A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 107UA 26900 NR 3 ENG FIRE LP B-STATUS MSG CLEARS WITH FIRE TEST, BUT COMES BACK. TS681 AND TS682 READING LOW RESISTANCE AT 1.5KOHMS . ORDERED LOWER AFT LOOP. REPLACED NR 3 ENG LWR-AFT FIRE DETECTOR LOOP (TS682), NO HELP. EICAS SHOWS "ENG 3 - FIRE LP B " STATUS MSG. FIRE TEST FAILS WITH CMC MSG 26025. SUSPECT WIRING PROBLEM ON ACCNT AFTER ENGINE SHOP REPLACED OIL TANK & REROUTED WIRES IN THE VICINITY OF AFT-LWR FIRE LOOP AREA - 9 O'CLOCK POS LOOKING AFT BY THE OIL TANK. ENGINE REPLACED DU E TO FAILURE. AFTER ENGINE CHANGE ACCOMPLISHED FIRE TEST NUMEROUS TIMES. ALL TESTS PASS. NO FIRE LOOP STATUS MESSAGE DI SPLAYED. 2 L 7 4 4F 4 F RT A20WE E24NE 20080926 NM 2008 9 26 SWAA085057 1 20080914 A 5311 6546593 FRAME BOEING 737 7373A4 1384585 NM BS 500A S20R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085058 1 20080911 A 2560 P4010021 BATTERY BOEING 737 737317 138447P NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 AFT CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085059 1 20080914 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085060 1 20080914 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 747 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 CALA0800880 1 20080916 A 5320 6546812 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 1016 OVERHEATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INTERCOSTAL AT LBL 3.54 FROM BS 1016 TO AFT PRESS BULKHEAD HAS OVERHEAT DAMAGE. REMOVED DAMAGED INTERCOSTAL IAW SRM 51- 40-02. FABRICATED NEW INTERCOSTAL IAW DWG 65-46812. INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02 AT LBL 3.54 AFT PRESS B ULKHEAD. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 CALA0800881 1 20080916 A 5320 101391107 STIFFENER BOEING 737 7373T0 1384582 NM FUSELAGE OVERHEATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 Z-ANGLE STIFFENER FROM LBL 18.32 TO 27.95 ADJACENT TO AFT PRESSURE BULKHEAD HAS OVERHEAT DAMAGE. REMOVED DAMAGED Z-ANGLE STIFFENER IAW SRM51-40-02. FABRICATED NEW STIFFENER IAW BAC DWG 65-46812, INSTALLED NEW Z-ANGLE STIFFENER AT LBL 18-32 -27.95 AT AFT PRESSURE BULKHEAD IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 CALA0800886 1 20080916 A 5320 65528941 INTERCOSTAL BOEING 737 737524 1384721 NM BS 540 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 INTERCOSTAL AT STA 540 FROM BL 0 TO LBL 24.0 IS CRACKED (VIEWED FROM FWD SIDE). REMOVED DAMAGED INTERCOSTAL, LOCATED AN D DRILLED NEW INTERCOSTAL AND RE-INSTALLED IAW B737 SRM 51-40-05, 51-40-02. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084830 1 20080902 A 3230 655825029 CIRCUIT CARD BOEING 737 7373H4 1384600 NM MLG FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 616SW 27699 AIRTURN BACK, DURING CLIMB LT MLG RED LIGHT ILLUMINATED. CYCLED GEAR, NO CHANGE. FOUND CIRCUIT CARD BAD. REMOVED AND REPLACED CARD PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084831 1 20080902 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 927WN 36889 R2 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084832 1 20080903 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 219WN 32490 DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084833 1 20080903 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM BS 503C S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 503C, STR 16L. REPAIRED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084951 1 20080908 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 360 S26R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084952 1 20080908 A 3350 65C27093 LIGHT BOEING 737 7373T0 1384582 NM R2 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084957 1 20080908 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM BS 492-500 S28R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 28R CORRODED AT BS 492 TO BS 500. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084958 1 20080908 A 5322 6546546 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 767 S25L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 25L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084959 1 20080908 A 5330 6545877 SKIN BOEING 737 7373A4 1384585 NM BS 967 S26R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT BS 967, STR 26R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843388 1 20080720 A 5311 654653969 FRAME BOEING 737 7374Q8 138447Q NM BS 616 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 CRACK FOUND ON LT BS 616 FRAME INNER CHORD WL 201 TO WL 200 AREA DURING ACCOMPLISHMENT OF EO 5310 02528. REMOVED DAMAGE D FRAME INNER CHORD, CUT OUT AREA, FABRICATED FILLER SHIM AND STIFFENING ANGLE AND INSTALLED IAW EO 5310 02528 SECTION 5 . 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843390 1 20080719 A 5315 65C3394225 FLOORBEAM BOEING 737 7374Q8 138447Q NM BS 328 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 CABIN FLOORBEAM STA 328 CORRODED IN SEVERAL AREAS ON UPPER SURFACE. REMOVED DAMAGED UPPER CHORD, FABRICATED, LOCATED, D RILLED INSTALLED REPAIR PARTS AND UPPER CHORD IAW AAR EA 12802 AND ASA EA 5310 02813 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843391 1 20080727 A 5311 654653141 FRAME BOEING 737 7374Q8 138447Q NM BS 500G DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 FWD CARGO COMPT FRAME 500 G DENTED JUST ABOVE STR 24L. CUT OUT DAMAGED AREA OF FRAME, FABRICATED REPAIR DOUBLER, LOCATE D, DRILLED AND INSTALLED IAW B737 400 SRM 51 70 11 PAGES 1 THRU 5. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843392 1 20080729 A 5315 69774771 FLOORBEAM BOEING 737 7374Q8 138447Q NM BS 993 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 AFT CABIN FLOOR SUPPORT CORRODED STA 993 FROM LBL 32 TO LBL 44.5. REMOVED CORRODED SUPPORT, FABRICATED, LOCATED, DRILLE D TRUSTED PRIMED AND TOP COATED AND INSTALLED NEW SUPPORT IAW B737 400 SRM 51 40 02 PG 2. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843393 1 20080810 A 5320 6545834260 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM BS 312-328 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 CABIN FLOOR SUPPORT CORRODED STA 312 TO STA 328 LBL 11. REMOVED DAMAGED FLOOR SUPPORT, LOCATED DRILLED AND INSTALLED A REPLACEMENT FLOOR SUPPORT IAW B737 400 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843428 1 20080819 A 5755 654645170A SKIN BOEING 737 737490 1384715 NM NR 7 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 RT WING NR 7 SPOILER UPPER SURFACE MULTIPLE PROTRUDING DENTS. REMOVED DAMAGED AREA, FABRICATED REPAIR FILLER AND DOUBLE R BONDED IAW B737 400 SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843429 1 20080819 A 5753 65C3570340 SKIN BOEING 737 737490 1384715 NM RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 RIGHT WING O/B FOREFLAP DENTED 24 INCHES FROM I/B END 4 INCHES FROM T/E. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBL ER AND BONDED IAW B737 400 SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085014 1 20080911 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085015 1 20080911 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 782SA 29808 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085016 1 20080911 A 5754 STRUCTURE BOEING 737 7377AD 1384502 NM NR 5 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 798SW 28436 DURING SCHEDULED 6Y CHECK, FOUND RT WING NR 5 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER EA. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085017 1 20080911 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 909WN 32458 EEPLS LENS MISSING AT ROW 3 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085022 1 20080911 A 5311 6545812 FRAME BOEING 737 7373A4 1384585 NM BS 328 S20R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 328, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080926 NM 2008 9 26 SWAA085023 1 20080911 A 5754 SKIN BOEING 737 7373A4 1384585 NM NR 1 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20080929 NM 2008 9 29 UPS08553310 1 20080815 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 365 S5-14L DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 MAIN CARGO HAS 8 EA AREAS OF MECH DAMAGE ON FRAME BS 365 STR 5L-14L WL 263 OUT OF LIMITS. INSTALLED DOUBLER IAW EO. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 UPS08553311 1 20080817 A 5320 FLOOR SUPPORT BOEING 757 75724APF 1384969 NM BS 879-894 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 THE FLOOR SUPPORT IS CORRODED BS 879-894 RBL 65 WL 208. CUT OUT CORRODED AREA, SPLICED IN NEW SECTIO N OF CREASE BEAM. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 2008UALA05703 1 20080913 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT LIGHT INOP UPPER DECK CEILING ROW 12. FOUND DEFECTIVE LAMP. REPLACED LAMP. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 NM 2008 9 29 2008UALA05705 1 20080913 A 3350 582240 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT SIGN INOP ABOVE DOOR 2 LEFT. FOUND BATTERY INOP. REPLACED BATTERY. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 EU 2008 9 29 2008UALA05708 1 20080913 A 3350 582240 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS NO TEST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 454UA 1104 EMERGENCY LIGHTS BATTERY CAPACITY TEST REQUIRED. CONDUCTED CAPACITY TEST. REPLACED EPSU BATTERIES AS ALTERNATE PROCEDU RE. TEST OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080929 NM 2008 9 29 2008UALA05711 1 20080913 A 2130 SHUTOFF VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RIGHT MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 510UA 24780 PRESSURIZATION PROBLEMS. FLIGHT DIVERTED. FOUND RT ENGINE HPSOV FAILED. REPLACED RT HPSOV. OPS AND LEAK CHECKED. NO DISCREPANCIES NOTED. BLEED SHIFT OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080929 NM 2008 9 29 2008UALA05712 1 20080913 A 3350 20131A POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INTERMITTENT A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 119UA 28812 UPPER DECK EMERGENCY CABIN LIGHTS FLASHING IN FLIGHT. FOUND FAULTY POWER PACK. REPLACED POWER PACK. POSITIONED EMERGE NCY LIGHT SWITCH IN ARMED POSITION. OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 NM 2008 9 29 UPS08553319 1 20080817 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM BS 608.5 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 SEAT TRACK HAS ELONGATED HOLE AT 608.5 LBL 45 WL 208. REPAIRED SEAT TRACK BS 608.5 LBL 45 WL 208 IAW ER 08-2795, SRM 53-00-2R5 REPAIR 201. 2 L 7 2 4F RT A2NM 20080716 EA 2008 7 16 N6WA0080509 1 20080530 A 7722 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA LEFT MALFUNCTIONED A N6WA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 162GJ 10254 ORD - LEFT ENGINE HOT ICON DISPLAYED DURING START. NO MESSAGE IN MDC ENGINE EXCEEDANCE HISTORY. RETURNED TO SERVICE IA W CRJ700 AMM 72-00-00. 2 L 7 2 4F RT A21EA 20080716 NM 2008 7 16 SWAA082881 1 20080528 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080716 NE 2008 7 16 2008UALA03096 2 20080529 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEFT MALFUNCTIONED A UALA O OTHER W R INADEQUATE Q C PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 WP 29 642UA 25092 724188 LEFT ENGINE STARTED UP WITHIN 95 SECONDS BUT STOPPED ACCELERATING AT 50 PERCENT FOR 10 SECONDS. 2 L 7 2 4F 4 F RT A1NM E24NE 20080716 WP 2008 7 16 UPS08852395 1 20080422 A 5321 5277265815300 CHANNEL DOUG DC8 DC873F 302199F WP FLOORBOARD CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C3 MAIN CABIN LAV AREA SAT 66-RBL 30, FLOORBOARD BOTTOM U-CHANNEL IS BLOWN OUT. REMOVED AND REPLACED U- CHANNEL ON FLOORBOARD IAW SRM, 53-2-3, 51-3-0, 51-1-8. 2 L 7 4 4F RT 4A25 20080716 NM 2008 7 16 WRLA2008050 1 20080524 A 5330 ABA87124 DOUBLER DOUG MD11 MD11F 3023600 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 381WA 48523 FOUND FUSELAGE WASTE SERVICE PANEL EXTERNAL DOUBLER CORRODED STA Y392.00 TO STA Y421.507 CENTER LINE. DOUBLER REPLACED PER SRM 51-30-00 VOL 2 REV 40. 2 L 7 3 4F 4 F RT A22WE E24NE 20080716 NM 2008 7 16 UPS08M52532 1 20080517 A 5740 ARB7774U6 FITTING DOUG MD11 MD11F 3023600 NM RH WINGLET CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 280UP 48634 INSPECTION TYPE:2C FOUND CRACK AROUND SMALL HOLE ON RT WING LWR WINGLET. REMOVED CRACKED WEB (BOX FITTING) AND REPLACED IAW MD-11 SRM 51-31-01. 2 L 7 3 4F RT A22WE 20080716 NM 2008 7 16 UPS08552367 1 20080518 A 5311 70750063C FRAME BOEING 757 75724APF 1384969 NM BS 1480 S25-26R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 436UP 25467 DENT IN BULK CARGO COMPARTMENT FUSELAGE FRAME STA 1480 BETWEEN S25R AND S26R. DENT SIZE L:=.085", W=.059", D=.030". DE NT LOCATION, FROM PRODUCTION SPLICE 4.5", FROM TRANSITION PANEL 10". REMOVED CLIP AT STA 1480 AND S25R AND LINER SUPPOR T IAW SRM 51-40-02. TRIMMED OUT DAMAGE L = 1.065, W=1.4 IAW SRM 53-00-07 2R STEP NR 1; DETAIL III. 2 L 7 2 4F RT A2NM 20080716 NM 2008 7 16 DU4R2008209 1 20080602 A 5330 SKIN BOEING 737 737448 13844BU NM FUSELAGE DENTED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 742VA 24773 DENT ON FUSELAGE SKIN AFT BS 947 AT S-23R. 2 L 7 2 4F RT A16WE 20080716 CE 2008 7 16 CWQR200805 1 20080602 A 3610 66140831 AIR DUCT CESSNA 560 560XL 2076702 CE BLEED AIR SYS CRACKED B DXTA K NONE O OTHER IN INSP/MAINT 1 GL 05 634QS 5605558 DURING A PHASE 1-4 INSPECTION THE PRECOOLER EXHAUST DUCT WELD ASSEMBLIES WERE FOUND TO BE CRACKED IN THE LEFT AND RIGHT PYLON. THE LEFT HAD TWO CRACKS AND THE RIGHT HAD THREE CRACKS. A SERVICE CONDITION REPORT HAS BEEN SENT TO CESSNA UNDE R #362539 FOR THE LEFT AND #362553 FOR THE RIGHT. 2 L 7 2 4F RT A22CE 20080716 SO 2008 7 16 SWIA200819698 1 20080526 A 3350 D36604001 BATTERY PACK EMB 120 EMB120ER 3260203 SO CABIN DISCHARGED A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 584SW 12048 12048 120352 FLIGHT ATTENDANT REPORTS THAT SEVERAL EMERGENCY EXIT SIGNS ARE INOP. FLIGHT 5408 - REPLACED THE MIDDLE ELBP. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080717 NM 2008 7 17 UPS08B52554 1 20080417 A 5311 65B01750801 FRAME BOEING 747 747400 13848AT NM BS 1140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:BCF LT BS 1140 TENSION TIE FRAME CRACKED. LT BS 1140 TENSION TIE FRAME REPAIRED PER SRM 53-40-07. 2 L 7 4 4F RT A20WE 20080717 NM 2008 7 17 CALA0800530 1 20080603 A 3350 767 LIGHT BOEING 737 737924ER 13848A3 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 38417 31665 AFT RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT, OPS CHECK GOOD PER AMM 33-51-04. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843059 1 20080610 A 5755 SKIN BOEING 737 7374Q8 138447Q NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 NR 5 SPOILER HAS DENTS ON THE LOWER SURFACE. PREPPED DENTED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 S RM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 CALA0800535 1 20080603 A 5315 147A5506 FLOORBEAM BOEING 737 737724 13844BY NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 STATION 986.5 FLOORBEAM UPPER CHORD FORWARD FLANGE LBL 26 CORROSION ON PREVIOUS REPAIR. REMOVED AND REPLACED REPAIR FIL LER PER SRM 53-00-51 REPAIR 1. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843056 1 20080611 A 5755 SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 RT WING INBD GROUND SPOILER HAS SEVERAL DENTS ON TOP SURFACE. PREPPED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2. OPS CHECK NORMAL PER MM 21 31 00. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0853064 1 20080618 A 2140 32149721 VALVE BOEING 737 737890 1384527 NM CABIN HEATER INOPERATIVE A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 587AS 2568 35684 UNABLE TO HEAT PASSENGER CABIN TO PASSENGER COMFORT RANGE. TROUBLESHOT AND FOUND NO HEAT LEAVING TRIM AIR PRSOV. VERIF IED PRSOV NOT OPENING AND GOOD POWER AND GROUND. REQUIRES REPLACEMENT. REMOVED AND REPLACED TRIM AIR PRSOV PER MM 21 6 2 01. GROUND VERIFICATION SUCCESSFUL. SYSTEM OPS NML PER MM 21 62 01. 2 L 7 2 4F RT A16WE 20080717 SO 2008 7 17 FDKA200805214 1 20080531 A 7930 LINE EMB 145 EMB145LR 3260212 SO OIL SYSTEM DEFECTIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 FDM FLT 9963 MCO-BUF. EMERGENCY DECLARED DUE TO NR 2 ENGINE LOW OIL QUANTITY AND PRESSURE. ENGINE WAS SHUT DOWN IN FLI GHT AND ANTI ICE ACTIVATED IN NON ICING CONDITIONS. REMOVED AND REPLACED OIL LINE, LEAK CHECK GOOD. 2 L 7 2 4T RT T00011AT 20080922 NM 2008 9 22 ASAA0843413 1 20080816 A 5512 657378351 SKIN BOEING 737 7374Q8 138447Q NM HORIZONTAL STAB DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 LEFT HORIZONTAL STAB LEADING EDGE PREVIOUS BLEND OUT AT APPROX STAB STA 98.70 HAS NICK IN THE BLEND OUT. NICK BLENDED O UT AND FOUND TO BE BEYOND ALLOWABLE LIMITS. REPLACE LEADING EDGE IAW SRM 55 10 01. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843405 1 20080819 A 5753 6546434369 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 LT WING I/B AFT FLAP DENTED ON LOWER LEADING EDGE SURFACE 46 INCHES FROM I/B END. REMOVED DAMAGED SECTION OF FLAP LEADI NG EDGE FABRICATED, LOCATED, DRILLED AND INSTALLED NEW LEADING EDGE SECTION IAW B737 400 SRM 57 53 01 DETAIL IV PG 4 AND B DWG 65 4634. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843451 1 20080822 A 5330 65C3579511 SKIN BOEING 737 7374Q8 138447Q NM BS 727A-727C DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 778AS 25110 DENT ON FUSELAGE SKIN AT BS 727C JUST BELOW STR 16R, GOES OVER STRINGER AND FRAME. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, INSTALLED REPAIR PARTS IAW AAREA 12889. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843457 1 20080823 A 5330 65C323591 SKIN BOEING 737 7374Q8 138447Q NM BS 500B DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 778AS 25110 FUSELAGE SKIN HAS A DENT AT STA 500B STR 29L A=.160 Y=.039 AY=4.10. AY MUST NOT BE LESS THAN 30. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, INSTALLED REPAIR PARTS IAW. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843466 1 20080904 A 5330 65C357986 SKIN BOEING 737 737490 1384715 NM BS 1010 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 BS 1010 UPPER SIDE OF STR 15 RT SKIN HAS DENTS 2 EA. REPAIR SKIN STA 1010 BETWEEN STR 14R AND 15R IAW ASA EA 5330 02387 . 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843467 1 20080904 A 5330 65C357885 SKIN BOEING 737 737490 1384715 NM BS 388 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 DENT 2 INCHES AFT OF D2 BLOWOUT DISC. DENT WITHIN 10 INCHES OF CUTOUT. REPAIRED SKIN DENT STA 388.5 AND STR 21R IAW AS A EA 5330 02388. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843449 1 20080823 A 5755 654645258 SKIN BOEING 737 7374Q8 138447Q NM NR 5 SPOILER CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 778AS 25110 NR 5 SPOILER LOWER SURFACE CHAFED ON I/B 8D END. PREPPED DAMAGED AREA, FABBED FILLER AND DOUBLER, INSTALLED REPAIR IAW B737 400 SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843450 1 20080823 A 5753 6546430190 SKIN BOEING 737 7374Q8 138447Q NM RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 778AS 25110 RIGHT INBOARD FOREFLAP LOWER SURFACE HAS SEVERAL DENTS OUTBOARD OF INBOARD TRACK. REMOVED DAMAGED AREA, FABBED DOUBLER AND BONDED REPAIR IAW B737 400 SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 UPS08553197 1 20080815 A 5320 COVER BOEING 757 75724APF 1384969 NM BS 900 RBL25-45 BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 FUSELAGE INTERIOR, BS 900, RBL 25 TO RBL 45, WL 208, FLOOR SUPPORT UPPER COVER IS BROKEN. REMOVED, F ABRICATED, INSTALLED PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20080918 NM 2008 9 18 2008UALA04120 1 20080802 A 3397 794640 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 FWD LT AFT GALLEY EMERGENCY LIGHT BOTTOM OF SIDEWALL INOP. *S/D* RESECURED CONNECTOR. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 NM 2008 9 18 UPS08553200 1 20080816 A 5330 FLOOR PANEL BOEING 757 75724APF 1384969 NM BS 900-1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 CLEAN AND TREAT ALL DOOR FASTENERS AT FLOOR PANEL NUT PLATE LOCATIONS WL 208 BS 900-1180 RBL 0-LB L0 AND BBL 0- RBL 60 AS NEEDED TO REMOVE CORROSION FROM DOOR FASTENERS. REMOVED AND REPLACED DISCONNECT FASTENERS PER SRM 51-40-02 2 L 7 2 4F RT A2NM 20080918 NM 2008 9 18 UPS08553202 1 20080817 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM BS 615 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 THE SEAT TRACK HAS ELONGATED HOLE AT BS 615.5 LBL 45 WL 208. REPAIRING SECTION OF SEAT TRACK FROM BS 590-680 PER SRM 53-00-52-2R REPAIR 5. 2 L 7 2 4F RT A2NM 20080918 NM 2008 9 18 SWAA084808 1 20080831 A 3350 20131A BATTERY BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHTS INOP BETWEEN ROW 2 DEF AND ROW 6 DEF. REMOVED AND REPL ACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 SWAA084812 1 20080830 A 5740 655223533 FITTING BOEING 737 7373Y0 1384671 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED 22Y CHECK, FOUND LT WING STABILIZER LINK LUG CORRODED. REMOVED AND REPLACED FITTING PER MM. 2 L 7 2 4F RT A16WE 20080918 WP 2008 9 18 UPS08853208 1 20080812 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP BS 55 LBL 17 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 CORROSION ON SUBFLOOR COURIER AREA SAT 55 LBL 17. REMOVED CORROSION, FABBED AND INSTALLED REPAIR DOU BLER IAW SRM 51-1- 2-1, 51-1-8, 52-3-2. 2 L 7 4 4F RT 4A25 20080918 NM 2008 9 18 UPS08M53213 1 20080812 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 17 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 SWAA084819 1 20080901 A 3397 D12464 CONNECTOR BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED 8Y CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT CONNECTOR CRACKED. REPAIRED CONNECTOR PER WDM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 2008UALA04311 1 20080815 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 3L MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 116UA 26908 SEAT 3J EEL MARKER MISSING. *S/D* REPLACED EEL LIGHT ASSY, CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 NM 2008 9 18 2008UALA04316 1 20080816 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1440 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 AFT PIT STA 1440 STR 25L, FRAME DENTED. *S/D* MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NM 2008 9 18 UPS08M53180 1 20080819 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 27 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 UPS08M53181 1 20080822 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 28 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 EU 2008 9 18 2008UALA04323 1 20080816 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 484UA 1609 FAILURE OF THE EMERGENCY LIGHT TEST. *S/D* REPLACED POWER SUPPLY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080918 NM 2008 9 18 UPS08M53190 1 20080817 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 21 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 2008UALA04331 1 20080815 A 3350 LENS BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 LT AISLE OVERHEAD EXIT SIGN AT FWD ECONOMY CABIN MISSING LENSE. *S/D* REPLACED CALL LIGHT HOUSING. ALL OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20080918 NM 2008 9 18 2008UALA04385 1 20080821 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 641UA 25091 FWD GALLEY X-AISLE EEL LIGHT INOP. SECURED EEL STRIP TO PWR SUPPLY, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20080919 NM 2008 9 19 SWAA084845 1 20080903 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 827 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084887 1 20080904 A 3350 20131 BATTERY PACK BOEING 737 737317 138447P NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843453 1 20080823 A 5753 654645262A SKIN BOEING 737 7374Q8 138447Q NM NR 4 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 778AS 25110 NR 4 SPOILER LOWER SURFACE HAS MULTIPLE DENTS IN 6 LOCATIONS. PREPPED 6 AREAS FOR REPAIRS FABBED 6 DOUBLERS AND BONDED REPAIRS IAW B737 400 SRM 51-70-10 REPAIR 2. NOTE THE 2 REPAIRS ON THE INBOAR END HAVE THE SAME DIMENSIONS WBL 87.75 92. 25 ABOVE AND BELOW THE BULB SEAL. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843410 1 20080819 A 5755 654645170A SKIN BOEING 737 737490 1384715 NM NR 8 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 RT WING NR 8 SPOILER DENTED ON UPPER SURFACE MIDDLE NEAR T/E. PREPARED DAMAGED AREA, FABRICATED FILLER AND DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843412 1 20080819 A 5755 654645268A SKIN BOEING 737 737490 1384715 NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 RIGHT I/B SPOILER LOWER SURFACE MULTIPLE SMALL DENTS. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BONDED IAW B 737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080923 NE 2008 9 23 DL76G081164 2 20080906 A 7532 ISOLATION VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE RT BLEED MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1603 29695 724372 RT BLEED ISOLATION VALVE LIGHT CAME ON DURING TAXI. RETURNED TO GATE PER MAINTENANCE REQUEST. REMOVED AND REPLACED RIG HT ISOLATION VALVE PER AMM. OPS CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20080923 NM 2008 9 23 DL757081179 1 20080910 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1390 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 FOUND SKIN DAMAGE AT STA 1390 STRINGER 24L - 25L. REPAIR INSTALLED PER SRM 53-00-01. 2 L 7 2 4F RT A2NM 20080923 NM 2008 9 23 DL757081169 1 20080910 A 5411 311N300025A SPAR BOEING 757 757232 1384965 NM NR 1 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 DURING CURRENT HMV, AN OVERSIZED HOLE WAS FOUND ON THE SPAR CHORD, NR 1 PYLON, DURING ACCOMPLISHMENT OF PYLON MOD. SUBJ ECT HOLE IS COMMON TO SIDE STRUT SKIN. BOEING WAS CONTACTED CONCERNING OVERSIZING SUBJECT HOLE, INSPECTING, AND INSTALL ATION OF OVERSIZED FASTENER. DOCUMENTED IN ERA 469688-14. 2 L 7 2 4F RT A2NM 20080923 NM 2008 9 23 DL757081170 1 20080911 A 5330 SKIN BOEING 757 757232 1384965 NM BS 324 S23-24L DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 FUSELAGE DAMAGE STA 324 STRINGER 23 -24 LEFT. 2 L 7 2 4F RT A2NM 20080923 NM 2008 9 23 DL757081172 1 20080911 A 5330 SKIN BOEING 757 757232 1384965 NM BS 410-430 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 SKIN DAMAGE AT STA 410-430 STRINGER 21 LEFT TO 22 LEFT. 2 L 7 2 4F RT A2NM 20080923 NM 2008 9 23 2008UALA04345 1 20080819 A 2612 G718505 CONTROL PANEL BOEING 737 737322 1384676 NM FIRE DETECTION INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 302UA 23643 CREW REPORT: CARGO FIRE DETECTION SYSTEM INOP. SUPPLEMENTAL DATA UPDATE FOUND FIRE CONTROL PANEL TO BE FAULTY. REPLACED CARGO FIRE CONTROL PANEL PER MM 26-00-02. OPS TEST NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20080923 2008 9 23 2008UALA05417 4 20080822 A 2565 H2052K3833 LATCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT O/W SLIDE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 RIGHT OVERWING SLIDE COMPT DOOR LATCH NR 1 SLIDER GOUGED. FOUND NR 1 LATCH GOUGED. REPLACED LATCH. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20080923 2008 9 23 2008UALA05462 4 20080823 A 3400 S10563 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE INTERMITTENT A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 572UA 26682 TRANSPONDERS FAILED. RTFL. COAX SWITCH S10563 SHORTING/INTERMITTENT. REPLACED COAX SWITCH S10563 AND ALSO REPLACED C ABLE AS PRECAUTIONARY. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080923 NM 2008 9 23 2008UALA05472 1 20080823 A 3397 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT DISLODGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 EMERGENCY LIGHT SECTION INOPERATIVE ROW 9 THRU 12. FOUND FEEDER CABLE DISLODGED FROM CONNECTOR. RE-SECURED FEEDER CA BLE, ALL OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080923 NM 2008 9 23 2008UALA05478 1 20080825 A 3510 REGULATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OXYGEN SYSTEM LEAKING A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 532UA 25072 CREW O2 BELOW LIMITS - RTFL. FOUND LEAK AT REGULATOR AND INDICATION ISSUE. REPLACED PRESSURE TRANSDUCER AND REPLACED PR ESSURE REGULATOR OPS OK, NO REPEATS. 2 L 7 2 4F 4 F RT A2NM E17NE 20080923 2008 9 23 2008UALA05515 4 20080828 A 2565 5A32957 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L1 DOOR LOW A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 653UA 25391 DOOR 1L ESCAPE SLIDE PRESSURE LOW. FOUND SLIDE PRESSURE LOW. REPLACED 1R ESCAPE SLIDE PACK. OKAY FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080923 NM 2008 9 23 2008UALA05514 1 20080828 A 3350 362624 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 364UA 24533 EMERGENCY LIGHT STRIP FOR SEAT ROWS 1 AND 2 IS INOPERATIVE. FOUND FAULTY LAMP STRIP. REPLACED LAMP STRIP OP CHECK GOO D. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080923 NM 2008 9 23 2008UALA05513 1 20080828 A 3350 58673 INVERTER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 364UA 24533 EMERGENCY PATH LIGHTING DOES NOT ILLUMINATE THE ENTIRE AIRCRAFT WITH SWITCH IN THE ON POSITION. SUSPECT INVERTER FAULTY. REPLACED INVERTER M1389 REFERENCE AMM 33-51-93. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080923 2008 9 23 2008UALA05507 4 20080827 A 2565 CONTACT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR SLIDE DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 560UA 26660 THE R2 DOOR SLIDE IND LIGHT INOP, STAYS DIM. CONTACT AT INDICATOR LIGHT 2R DOOR IS DIRTY. CLEANED CONTACT AT DOOR 2R I NDICATOR LIGHT, ALL OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080923 EA 2008 9 23 SWIA200820016 1 20080905 A 3260 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 403SW 7028 "NOSE GEAR DOOR" WARNING MESSAGE AFTER TAKEOFF, RETURNED TO FIELD. REPLACED PROX SWITCH PS18GA. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080923 SO 2008 9 23 SWIA200820018 1 20080907 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 288SW 120316 RIGHT BLEED OVERHEAT WARNING LIGHTS CAME ON ALONG WITH A BURNING ODOR AND VISUAL SMOKE IN THE MAIN CABIN. PERFORM OPS CHECK OF RT ENG BLEED, COULDN'T DUPLICATE AT THIS TIME. 2 L 7 2 4T RT A31SO 20080717 NM 2008 7 17 2008UALA02940 1 20080520 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 541UA 25253 L2 DOOR EMERGENCY LIGHT SWITCH INOP. SUPPLEMENTAL DATA UPDATE CAUSE, LAMP INOP AT DOOR L2. REMOVED AND REPLACED L2 DO OR EMERGENCY LIGHT, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080717 SW 2008 7 17 RMX2008F00000 1 20080617 A 5302 206032409001 FITTING BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL TAILBOOM CRACKED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 154MW 52154 CAE695833 DURING ROUTINE INSPECTION TECHNICIAN DISCOVERED UPPER LEFT TAILBOOM ATTACH FITTING CRACKED. (K) 1 G 7 1 3U 3 U NC H2SW E1GL 20080717 NM 2008 7 17 SWAA083337 1 20080618 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080717 EU 2008 7 17 M7K2008F00003 1 20080512 A 5302 350A23422220 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 812MH 311 3956 23036 CRACK DISCOVERED DURING ROUTINE INSPECTION ON FITTING FLANGE AND GOING THROUGH AN ATTACHMENT BORE. A NEW FITTING WAS MA TCH DRILLED AND INSTALLED. THIS IS A VERY COMMON PROBLEM FOR THIS PART. SUGGEST THIS PART BE MANUFACTURED FROM A MORE DURABLE MATERIAL SUCH AS TITANIUM OR STAINLESS STEEL. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080717 NM 2008 7 17 MWE2008F00002 1 20080625 A 2133 OUTFLOW VALVE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE CABIN PRESSURE OBSTRUCTED A MWEA O OTHER J C WARNING INDICATION F.O.D. NR NOT REPORTED 1 GL 13 822ME 49759 UNABLE TO CONTROL CABIN WITH NR 1 PRESSURE SYSTEM CABIN, SWITCHED OVER NR 2 PRESSURE SYSTEM FLOW LIGHT ON. FOUND INSTAL LATION BAG WAS STUCK IN AFT PRESSURE RELIEF VALVE. REMOVED OBSTRUCTION. (K) 2 L 7 2 4F 4 F RT A6WE E9NE 20080717 NM 2008 7 17 SWAA083221 1 20080612 A 5315 6546809 FLOORBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 947.5, RBL 48. REMOVED AND REPLACED CHORD PER SR M. 2 L 7 2 4F RT A16WE 20080717 2008 7 17 SWAA083099 4 20080605 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 420WN 29825 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083086 1 20080608 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083299 1 20080617 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 27L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083307 1 20080617 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 375SW 26583 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080717 WP 2008 7 17 08FDEA02030 1 20080529 A 5321 AGA38622 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 AFT PIT FLOOR PANEL 187 GF REQUIRES FAB NEW. FABRICATED NEW FLOOR PANEL 187 GF; POTTED EDGES; COMPLETED CURE AND SANDED EDGE POTTING; INSTALLED INSERTS; FABRICATED TOP SHEET; LAYED UP UNDER A VAC BAG; COMPLETED CURE; BACK DRILLED AND COUN TERSUNK HOLES; APPLIED NON-SKID AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005, REV F AND 25-011, REV C. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 SWAA083289 1 20080615 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS MISSING AT ROW 21 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843111 1 20080628 A 2913 371380 PUMP BOEING 737 7374Q8 138447Q NM HYD SYSTEM FAILED A ASAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 02 763AS 35976 25100 DURING CLIMB-OUT RIGHT HYDRAULIC QTY SHOWED 44 PERCENT DURING LANDING ROLLOUT NR 2 ENG LOW PRESSURE LIGHT ILLUMINATED AN D REMAINED ON LOUD METAL GRINDING NOISE NOTED BY PILOT RIDING IN BACK DURING TAXI IN SERVICED RT HYD SYSTEM TO FULL REF MM 12-12-00 (91541). OPERATED NR 2 ENG W NO ENG HYD PRESSURE NOTED (91541). REPLACED NR 2 ENG HYD PUMP REF ASA 29 15 1 1(13287). STILL REQ FILTERSCHANGED. OPS CK AND LEAK CHECK. FLUSH B HYD SYSTEM NO FILTERSCONTAINED. LEAK CHECK GO OD. OPS NORMAL REF AMM 29-15-00-172-037. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 08FDEA02052 1 20080530 A 5754 65192831 SKIN BOEING 727 727227 1384078 NM NR 4 SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 490FE 21493 NR 4 SLAT UPPER SURFACE ON AFT HOOK ATTACHMENT SCREW HAS SKIN CRACKED REMOVED HOOK AS REQ IAW B727 SRM 51-10-2. FAB REP AIR PLATE MAT USED 2024T3-.125 PO NR 810563. DIM (5" BY 4") IAW B727 SRM 57-50-3 FIG 10, TREATED AND PRIMED IAW B727 SR M 51-10-2, C/W HFEC IAW B727 NDTM PT 6. 51-00-00 FIG 23. CRACK TERMINATES IN FASTENER HOLES. INSTALLED REPAIR PART IAW B727 SRM 51-30-2. INSTALLED HOOK WITH BOLTS IAW B727 SRM 51-30-2. 2 L 7 3 4F A3WE 20080717 NM 2008 7 17 SWAA083258 1 20080613 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 420 AND BS 440, STR 1. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20080717 WP 2008 7 17 08FDEA02027 1 20080529 A 5321 AGA38753 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 AFT PIT FLOOR PANEL 187 DF REQUIRES FAB NEW. FABRICATED NEW FLOOR PANEL 187 DF; POTTED EDGES; COMPLETED CURE AND SANDED THE EDGE POTTING; INSTALLED INSERTS; FABRICATED TOP SHEET; LAYED UP UNDER VAC BAG; COMPLETED CURE; BACK DRILLED AND COUNTERSUNK HOLES; APPLIED NON-SKID AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005, REV F AND 25-011, REV C. 2 L 7 3 4F RT A22WE 20080717 WP 2008 7 17 08FDEA02026 1 20080529 A 5321 AGA74289 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 AFT PIT FLOOR PANEL 187 CF REQUIRES FAB NEW. FABRICATED NEW FLOOR PANEL 187 CF; 187 CF; POTTED EDGES; COMPLETED CURE; I NSTALLED INSERTS; FABRICATED TOP SHEET; LAYED UP UNDER VAC BAG; COMPLETED CURE; BACK DRILLED AND COUNTERSUNK HOLES; APPL IED NON-SKID AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005, REV F AND 25-011, REV C. 2 L 7 3 4F RT A22WE 20080717 EA 2008 7 17 SWIA200819810 1 20080622 A 5200 PANEL CNDAIR CL600 CL6002B19 1900309 EA OXYGEN SYS UNLATCHED A SWIA G O2 MASK DEPLOYED O OTHER NR NOT REPORTED 1 NM 07 403SW 7028 FLT 2825 - OXYGEN PANEL AT ROW 5 DROPPED OPEN IN FLIGHT. RESECURED PANEL FOR PSU IAW 25-28-01. 2 L 7 2 4F RT A21EA 20080717 WP 2008 7 17 08FDEA02229 1 20080612 A 5710 ARB07432 CAP DOUG DC10 DC1010 3022110 WP BULKHEAD CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 40061 46973 THE LOWER BULKHEAD CAP IS CRACKED IN 3 PLACES. LOWER LUG AT STR NR 43 FWD AND AFT, STR NR 44 AFT RT WING. REPAIRED ARE A IAW SRM 57-20-00 FIG 27 SHT 3 VOL I. 2 L 7 3 4F A22WE 20080717 WP 2008 7 17 08FDEA02231 1 20080612 A 5712 ARB1136 RIB DOUG DC10 DC1010 3022110 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 LT WING L/E FOUND CRACK ON INT RIB L/E . REPAIRED RIB IAW SRM 57-00-01 VOL I FIG 10 SHEET 1. 2 L 7 3 4F A22WE 20080717 NM 2008 7 17 ASAA0843028 1 20080514 A 5753 SKIN BOEING 737 737490 1384715 NM RT WING TE FLAP DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 RIGHT OUTBOARD AFT FLAP UPPER SURFACE TRAILING EDGE DAMAGED 47.5 INCHES FROM OUTBOARD END PREPARED DAMAGED AREA. FABRIC ATED FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083274 1 20080612 A 3350 20131SWA BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 08FDEA02215 1 20080611 A 5311 6516347 FRAME BOEING 727 727227 1384078 NM BS 1130 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 AFT CARGO PIT FUSELAGE FRAME 1130 HAS GOUGES AND CORROSION ON UPPER FLANGE, RBL: 22-23, UNDER Z ANGLE. REMOVED CORROSIO N AND GOUGES, ORG MATERIAL THICKNESS .071" REMOVED .030", REMAINING .041". FOUND TO BE OUT OF LIMITS, FABRICATED REPAIR PART, TREATED AND PRIMED REPAIR AND INSTALLED, REF SRM 51-10-2 PG 7, SRM 51-30-2 PG 2, SRM 53-10-1, SRM 53-10-2 FIG 5, SRM 51-40-3 FIG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080718 EU 2008 7 18 08FDEA02361 1 20080620 A 5321 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU CABIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 MAIN CABIN FLOOR PANEL 232 UG IS CRACKED AND DAMAGED. FABBED A NEW FLOOR PANEL 232 UG BY USING THE OLD PANEL AS A TEMPL ATE; POTTED; CURED AND SANDED EDGES; POTTED AND CURED INSERTS; APPLIED NON-SKID TAPE AND PART MARKED THE PANEL IAW FED EX DWG SRZ 25-005, REV F. 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 08FDEA02104 1 20080603 A 5100 NONE DOUG MD11 MD11F 3023600 NM IAW SRM NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 EXISTING REPAIR, RIGHT WING NR 3 LEADING EDGE SLAT UPPER SURFACE LEADING EDGE FOUND REPAIR DOUBLER. EXISTING REPAIR AT RIGHT WING NR 3 LEADING EDGE SLAT UPPER SURFACE LEADING EDGE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-1 0-00 FIGURE 5 VOLUME I FEDEX EO NR 1-5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG - MD11 - REPAIR CATALOG AND TRACKING REQUIREMENTS 14 CFR 121.707, HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 WP 2008 7 18 08FDEA02150 1 20080604 A 5415 BRACKET DOUG MD10 MD1010F 3022112 WP NR 1 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 NR 1 PYLON THRU PANEL 438 AR; STAND OFF BRACKET FOR THE FIREX LINE IS CRACKED. 2 L 7 3 4F RT A22WE 20080718 WP 2008 7 18 08FDEA02151 1 20080604 A 5410 STRUCTURE DOUG MD10 MD1010F 3022112 WP NR 1 NACELLE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 NR 1 ENGINE RIGHT FAN COWL INTERIOR IS GOUGED JUST FWD OF THE GENERATOR EXHAUST DUCT. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 08FDEA02238 1 20080612 A 5340 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 598FE 48597 MAIN DECK CARGO DOOR SPOOL FITTING NR 5 FOUND 3RD LAYER CRACK INDICATION AT FITTING MOUNTING BOLT HOLE D. MAIN DECK CAR GO DOOR SPOOL FITTING NR 5 REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING RE PAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 2008UALA03350 1 20080612 A 5320 ANGLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 MAIN CABIN UNDER FLOOR, INTERCOSTAL UPPER ANGLE CRACKED BETWEEN BS 742 AND BS 764, AND RBL 40. MAJOR REPAIR ACCOMPLISHE D: INSTALLED NEW ANGLE (P/N OA00002UD). 2 L 7 2 4F 4 F RT A1NM E24NE 20080718 EU 2008 7 18 2008UALA03434 1 20080617 A 3350 321454 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 420UA 489 MESSAGE "ATA 33-51-38 INT LOADS AFT L" SHOWS AFTER THE TEST. POWER SUPPLY FAILURE. REPLACED POWER SUPPLY AND BATTERY. OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080718 NM 2008 7 18 2008UALA03437 1 20080615 A 2931 211C223534 SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HYDRAULIC SYS FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 661UA 27158 PRESS LIGHT DO NOT COME ON WHEN RIGHT ELECTRIC DEMAND PUMP IS TURNED OFF. FOUND FAULTY SWITCH. REPLACED S30 SWITCH OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080923 SO 2008 9 23 SWIA200820019 1 20080907 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DISCHARGED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 582SW 120350 AFT EMERGENCY LIGHTS INOP. REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK, PN D366-04-001, SN ON 1195, SN OFF 551. 2 L 7 2 4T RT A31SO 20080923 EA 2008 9 23 SWIA200820020 1 20080906 A 5210 LATCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 943SW 7762 MAIN CABIN DOOR LATCH STICKS. INSPECTED AND LUBED DOOR, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080923 NM 2008 9 23 08FDEA03186 1 20080730 A 5347 AEA73256 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 MAIN DECK SEAT TRACK AT STA 1259, X = -27 FOUND CORROSION. MAIN DECK CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRA CK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080923 NM 2008 9 23 08FDEA03392 1 20080812 A 5347 7178T6511 SEAT TRACK BOEING 757 75723A 1384967 NM BS 377-440 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 SEAT TRACK REPLACE STA 377-440, REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK IAW SRM 51-10-02. INSTALLED SEAT TRACK IAW SRM 51-40-02. MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20080923 NM 2008 9 23 08FDEA03393 1 20080812 A 5755 65249661 FITTING BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 LT WING, EVALUATE PREVIOUS REPAIR AT INBD LOWER CORNER OF NR 7 SPOILER FITTING AT FALSE SPAR. REMOVED IMPROPER REPAIR I AW SRM 51-30-2 AND FEDEX DRAWING SR-27-57-038 REV C. REMOVED NR 7 SPOILER FITTING AND DOUBLER, TRIMMED OUT WEB, FABRIC ATED NEW DOUBLER USING 7075T6 .032 PO NR 9006612 DIMS 12 INCH BY 8 1/2 INCH, FABRICATED NEW INBD LOWER CHORD FROM BAC151 4-1437 PO NR 8195260 DIMS 20 3/4 INCH BY 4 7/8 INCH, 2 EACH ANGLES FROM 7075- O .071 PO NR 9007470, 1 EACH STRAP FROM 7 075T6 .090 PO NR 9006152 AND INSTALLED REPAIR PARTS IAW FEDEX DRAWING SR-27-57-038 REV C. 2 L 7 3 4F RT A3WE 20080923 NM 2008 9 23 08FDEA03394 1 20080812 A 5347 BAC1520792 SEAT TRACK BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 CORROSION ON SEAT TRACK FLANGES AND ATTACHING HARDWARE, STA 1010 10 INCH TO STA 1050, LBL 45 FOUND CORROSION OUT OF LIMI TS IAW B727 SRM 53-10-1. REMOVED (3) EA SECTIONS OF SEAT TRACK FROM BS 1010 TO 1130 IAW B727 SRM 51-30-2. FABRICATED N EW SECTION OF SEAT TRACK FROM BS 1010 TO 1130 LBL 45 USING BAC1520-792 7178T6511, DIM 114 INCH IAW B727 SRM 51-30-5 AND 53-10-5 FIG 1. ALODINE AND PRIME SEAT TRACK IAW B727 SRM 51-10-2. INSTALLED SEAT TRACK IAW B727SRM 51-30-2 AND 53-10-5 FIGURE 1. 2 L 7 3 4F RT A3WE 20080923 EU 2008 9 23 08FDEA03395 1 20080813 A 5753 A5796005920700 RIB AIRBUS 300 A300B4622R 3930312 EU RT WING FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 RIGHT WING INBD FLAP NOSE RIB NR 9 IS CRACKED AT A RIVET HOLE. FABRICATED A REPAIR DOUBLER REF SRM 57-50-00; PG 204. A LODINED AND PRIMED REF AMM 51-22-00-0; PG 1. INSTALLED REF SRM 51-40-21; PG 7. 2 L 7 2 4F RT A35EU 20080923 EU 2008 9 23 08FDEA03476 1 20080818 A 5754 A57840120203 PAN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 LT SLAT NR 1 FOLDING NOSE INNER PAN WITH CRACK FINDING REPAIR PERFORMED BY INSTALLING SB A300-6067 WITH INNER PAN REPLAC EMENT, APPROVED BY EA 6-5742-120064. 2 L 7 2 4F RT A35EU 20080923 EU 2008 9 23 08FDEA03477 1 20080818 A 5330 A53973277208 SKIN AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON INNER SKIN AT BULK CARGO DOOR CUT OUT C 67-69, P 45-46 RT. REPAIR PERFORMED BY CORROSION REWORK, NDT FOR CORROSION FREE CONDITION AND FLAP PEENING IAW RAS/EFW/9000073/2008 ISS A, APPROVED BY EA 6-5317-123021. 2 L 7 2 4F RT A35EU 20080923 EU 2008 9 23 08FDEA03555 1 20080822 A 7830 WEB AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 650FE 726 NR 1 ENGINE INBD T/R FWD UPPER WEB IS CRACKED. STOP DRILLED CRACK; NDT'D AREA FOR CRACK PROPAGATION AT THE CRACK END IA W A300 NTM 51-90-00 PT 9. FABBED A NEW DOUBLER IAW MRA CMM 78-32-01. TREATED DOUBLER AND AREA IAW A30-600 SRM 51-1-23 AND MRA CMM 78-32-01. INSTALLED THE REPAIR DOUBLER IAW A300-600 SRM 51-41-21 AND MRA CMM 78-32-01. 2 L 7 2 4F RT A35EU 20080923 SO 2008 9 23 SWIA200820021 1 20080505 A 5310 WINDOW FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 562SW 120336 PILOT'S SIDE AFT OF DV WINDOW AREA FRAME 12 EAR SUPPORT CLIP, AFT, IS CRACKED. INSTALLED DOUBLER IN PLACE WITH RIVETS P ER SRM 51-30-01 AND 51-40-02. 2 L 7 2 4T RT A31SO 20080923 NM 2008 9 23 08FDEA03481 1 20080818 A 5330 65184204 SKIN BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 INTERNAL FUSELAGE SKIN AT BS 355 BELOW STRINGER 7RT HAS A DRILL START. DRILLED A .161 DIA HOLE AND INSTALLED A NAS1097A D5 RIVET IAW EA NR 7-5330-117006 AND SRM 51-30-2. 2 L 7 3 4F RT A3WE 20080923 NM 2008 9 23 08FDEA03560 1 20080822 A 5330 146N8630 STRAP BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 AFT CARGO CORROSION ON SKIN STRAP AT BS 1400, RBL 20 BETWEEN S27R AND S28R. MINOR CORROSION ON STRAP REMOVED AND AREA T REATED IAW SRM 51-10-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 2 4F RT A2NM 20080924 NM 2008 9 24 08FDEA03562 1 20080823 A 5210 ROLLER CAM BOEING 727 727233 138408A NM PAX DOOR BROKEN A FDEA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 21 264FE 21626 AFTER TAKEOFF CREW REPORTS 2 LOUD BANGS OR POPS. NO ENG INDICATION FLUCTUATIONS OR PRESSURIZATION CHANGES. CREW REPOR TS ENTRY DOOR WAS HARD TO CLOSE, BUT NO LIGHTS EVER CAME ON. OCCURED APPROXIMATELY AROUND 14,000 FT. INSPECT CABIN EN TRY DOOR AND FOUND TOP, AFT, CRANK ROLLER CAM BROKEN. THE TIP AND ROLLER STILL ATTACHED BROKE OFF. TALKING WITH MOCC O N PARTS. REMOVED AND REPLACED UPPER AFT CRANK ASSY AND ROLLER. REMOVED AND REPLACED THE LOWER AFT ROLLER REF MM 51-11- 022-4. 2 L 7 3 4F RT A3WE 20080924 NM 2008 9 24 08FDEA03563 1 20080823 A 5320 AFA71321 FITTING DOUG MD10 MD1030F 3024020 NM DOOR FRAME CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 304FE 46992 MCD HOLES NR 3 FITTING LWR JAMB SUPPORT 1 AFT OUTBD HOLE HAVE CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-50-00 PAGE 81 FIG 17. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR AND IS RII. 2 L 7 3 4F RT A22WE 20080924 EU 2008 9 24 08FDEA03346 1 20080808 A 5321 R532B371500000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 241 AJ IS DAMAGED. REPAIRED CABIN FLOOR PANEL 241 AJ BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MAR KED AND APPLIED NON-SKID TAPE IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 2008UALA03443 1 20080617 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 STA 303, RBL 88.5, CRACK ON FLOORBEAM. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED T-CHORD, REPAIR SPLICE & STRA P. 2 L 7 2 4F 4 F RT A1NM E24NE 20080718 EU 2008 7 18 2008UALA03460 1 20080618 A 3350 SIGN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INADEQUATE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 402UA 439 EMERGENCY LIGHT WILL NOT PASS TEST AT 1L. FOUND EXIT SIGN AT 1R OVER DOOR VERY DIM. REPLACED SIGN ASSY, OPS CHECKED NO RMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080718 NM 2008 7 18 SWAA083607 1 20080629 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L AND STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083608 1 20080629 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083573 1 20080629 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 807, STR 23L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083587 1 20080629 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 2008 7 18 SWAA083590 4 20080629 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 27698 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083560 1 20080626 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515B, STR 26L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083494 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083517 1 20080625 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER 23R CRACKED AT BS 540. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080718 EA 2008 7 18 A6WA200840448 1 20080522 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 DENTS ON PASSENGER DOOR FWD AND AFT UPPER CORNER COVERS. ON FURTHER INVESTIGATION, CRACKS FOUND ON PARTS (CORNERS) ON PAX DOOR FWD AND AFT REMOVED AND REPLACED IAW SRM 51-42-06 AND SRM 51-42-13. (A) 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840406 1 20080510 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 442AW 7778 CORROSION EXISTS UNDER FLOOR FS 576, FS 605, FS 618 LBL 40. CORROSION REMOVED UNDER FLOOR FS 576, FS 605, FS 618 LBL 40 IAW SRM 51-21-06. 2 L 7 2 4F RT A21EA 20080718 EU 2008 7 18 M7K2008F00033 1 20080528 A 5302 350A23422220 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 823MH 1100 4158 DURING ROUTINE INSP, FITTING WAS FOUND CRACKED FROM AN OB ATTACHMENT SCREW BORE TO FLANGE EDGE. NEW FITTING WAS INSTALLE D. THIS ISA COMMON FAILURE FOR THIS PART. BORE HOLES MUST BE MATCH DRILLED AND ALIGNED PERFECTLY. SUGGEST A MORE DURA BLE MATERIAL BE USED IN THIS PARTS MFG SUCH AS TITANIUM OR SS AS ALUMINUM ALLOY FAILS ROUTINELY UNDER NORMAL STRESS APPL IED TO THIS PART. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 WP 2008 7 18 UPS08852444 1 20080525 A 5320 STRUCTURE DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 MAIN CABIN, FLOORBOARD TIEDOWN BULGED AND FASTENERS PULLING STA 350 LBL 35. REMOVED, DAMAGED RECEPTI CLE, FABBED AND INSTALLED REPAIR DOUBLER ON FLOOR PANEL, INSTALLED NEW RECEPTICLE IAW SRM 51-1-8, 53-2-3 FIG 1F, 51-1 -2 1A, 51-1-11. 2 L 7 4 4F RT 4A25 20080718 EU 2008 7 18 UPS08152415 1 20080512 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU LAVATORY INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 151UP 0834 INSPECTION TYPE:N/A LAVATORY EMERGENCY LIGHT IS INOP. RELAMPED EMERGENCY LIGHT, CHECKS GOOD. 2 L 7 2 4F RT A35EU 20080716 NM 2008 7 16 SWAA082888 1 20080528 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080924 NM 2008 9 24 08FDEA03361 1 20080810 A 5314 6518636155 KEELBEAM BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 LEFT KEEL BEAM CHORD IS CRACKED AT STA 880. REMOVED AND DISCARDED EXISTING GUSSET PLATE AND FASTENERS COMMON TO THE KEE L BEAM CHORD IAW FEDEX EA 7-5310-117026. VERIFIED END OF CRACK USING HFEC IAW B727 NDTM 51-00-00 FIG 1. TRIMMED UPPER FLANGE OF KEEL BEAM CHORD, FABRICATED REPAIR DOUBLER, AND INSTALLED REPAIR DOUBLER IAW FEDEX EA 7-5310-117026, MLG WHEEL WELL KEEL BEAM CRACK AT BS 872 - REPAIR. 2 L 7 3 4F RT A3WE 20080924 EU 2008 9 24 08FDEA03488 1 20080818 A 5340 A5381026720001 ATTACH FITTING AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 650FE 726 MAIN CARGO FLOOR SUPPORT WEB, LOWER OUTBD ATTACH FITTING IS CRACKED AT FRAME 49; FLOOR LOCATION -Y 145.6. REMOVED AND R EPLACED ATTACH FITTING IAW A300-600 SRM 51-40-21; PARA 10-B. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03316 1 20080729 A 5330 A53989437200 SKIN AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 727FD 579 TAIL CONE, FUSELAGE UPPER AREA WITH DENTS BETWEEN FR 100 AND 103 AND BETWEEN STGR 2 LT AND 2 RT. DENTED SKIN BETWEEN FR 100 AND FR 103 WAS REPAIRED AS PER FEDEX EA 6-5330-123347. FRAME SECTIONS OF FR 101 AND FR 102 WERE REPLACED AS PER SR M 51-72-10. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03796 1 20080910 A 5315 A5361303320000 FLOOR SUPPORT AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 DAMAGED FLOOR CAP AT FRAME 13 AND FWD; BL 0. REPAIRED DAMAGED FLOOR CAP IN REF TO SRM 51-71-50 & DWG A53612213.0 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03239 1 20080804 A 5753 SKIN AIRBUS 300 A300F4605R 3930327 EU RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 RIGHT WING INBD FLAP UPPER SKIN IS DENTED 5' FROM THE INBD END. SMOOTHED AREA AROUND THE DENT IAW A300-600 SRM 51-73-10 . ORIGINAL MATERIAL 0.031 IAW SRM 57-52-12; ITEM 45. MATERIAL REMOVED 0.002. MATERIAL REMAINING 0.029, FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 57-50-00; FIG 101; SHEET 5. REPAIRED IAW A300-600 SRM 57-50-00. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03242 1 20080804 A 5753 A5751101000000 SKIN AIRBUS 300 A300F4605R 3930327 EU RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 RIGHT WING INBD FLAP LOWER SKIN HAS SEVERAL DENTS. SMOOTHED DENTS IAW SRM 51-73-10. ALL DENTS EXCEPT RIB 7. ORIGINAL MATERIAL IS 0.028. MATERIAL REMOVED 0.015. MATERIAL REMAINING 0.013; FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00. RIB 7 DENT 0.049 DEPTH. NO MATERIAL LOSS; FOUND TO BE IN LIMITS IAW SRM 57-50-00. REPAIRED ALL DENTS IAW SRM 57-50-00, 1 LARGE DOUBLER; 1 SMALL DOUBLER AND APPLIED FILLER AT RIB 7. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03607 1 20080828 A 5720 FXA93540675201 SUPPORT BRACKET AIRBUS 310 A310222 3930315 EU RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 455FE 331 RT WING, REAR SPAR RIB 1-RIB-4, HYD TUBE SUPPORT BRACKET WITH INNER-GRANULAR CORROSION. REMOVED THE CORRODED TUBE SUPPO RT BRACKET. FABRICATED A NEW BRACKET PER AIRCRAFT DRAWING 25 A935-40675. INSTALLED THE NEW BRACKET AND HYD TUBES PER A MM 20-21-12-0 AND AMM 20-23-11-0. PERFORMED LEAK CHECK PER AMM 29-00-00-6. NO LEAK FOUND. 2 L 7 2 4F RT A35EU 20080924 WP 2008 9 24 08FDEA02981 1 20080716 A 5512 74391 SKIN PANEL DOUG MD10 MD1010F 3022112 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 381FE 46615 THE HORIZONTAL STABILIZER, LT OUTER SECTION SKIN PANEL NR 7439-1, TOP SIDE JUST OUTBOARD OF FAIRING AND FORWARD OF REAR SPAR IS A 1.750 INCH CRACK. VERIFIED BY HFEC EDGES MARKED. APPROXIMATE LOCATION XE 67.333 STRINGER NR 1 INSTALLED REPA IR PER EA 8-5510-121560. 2 L 7 3 4F RT A22WE 20080924 WP 2008 9 24 08FDEA02866 1 20080714 A 5313 AFA30441 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 CENTER CARGO PIT, LONGERON 30 L END FITTING IS CRACKED IN THE UPPER LEG AT STA 1756. MACHINED LONGERON END FITTING P/N AFA 3044-1. MATERIAL ID 7075-T651, PO 626147.1 IAW DAC DWG AFA 3044. HEAT TREATED TO T-73. LOAD NR HT092208-1 AND PE RFORMED DIMENSIONAL CHECK IAW EA 8-5310-116996 "FUSELAGE - LONGERON SPLICE FITTING HEAT TREAT REQUIREMENTS". PART MARK ED IAW FEDEX GMM 7-0-1000. REMOVED OLD FITTING AND INSTALLED NEW FITTING IAW DC/MD-10 SRM 51-31-01; PG 1; VOL II. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 DLM90081116 1 20080824 A 5330 SKIN DOUG MD90 MD9030 3023690 NM FS 795-885 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DN 53395 DURING CURRENT HMV, DAMAGE (CORROSION) WAS FOUND ON FUSELAGE SKIN AT WING TO BODY FAIRING. REPAIR WAS ACCOMPLISHED PER SRM 53-04 FIGURE 53. MANUFACTURER APPROVED USE OF SUBJECT SRM ON 9215 PROVIDED THERE WERE NO DEVIATIONS. ADDRESSED ON ERA 470199-14. 2 L 7 2 4F RT A6WE 20080924 NM 2008 9 24 DLM90081118 1 20080825 A 3320 D73311001 BALLAST DOUG MD90 MD9030 3023690 NM CABIN LIGHTS INOPERATIVE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 909DA 53389 BURNING ODOR AFT CABIN NEAR ROW 39 CDE. FOUND 2 EA SIDEWALL LIGHTS INOP AND INOP BALLAST BAD AFT OF O/H BAG BIB 39 CDE. REPLACED BALLEST AND LIGHTS OPS GOOD. 2 L 7 2 4F RT A6WE 20080728 EU 2008 7 28 2008UALA03071 1 20080528 A 5320 SHEAR PLATE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 447UA 836 RIGHT SHEAR PLATE BETWEEN FRAMES 69 AND 70 HAS EVIDENCE OF SURFACE CORROSION ON UPPER SURFACE AND FASTENER HOLES. ACCOM PLISHED MAJOR REPAIR AT DEN. REMOVED SHEAR PLATE, DRILLED NEW PLATE AND INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 EA 2008 7 28 TRAX200800853 1 20080630 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 409-559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 NUMEROUS AREAS OF MINOR CORROSION ON PRESSURE FLOOR SILL FROM FS 409.0+128 TO FS 559.0, LBL 36.0 TO LBL 47.0, WL 73.0. REMOVED MINOR CORROSION ON PRESSURE FLOOR SILL IAW SRM 51-21-06. RUBATEX TAPE REQUIRES INSTALLATION. INSTALLED RUBATEX TAPE IAW MM 53-01-01-400-802. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAC200800612 1 20080507 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 928EV 8006 THE AFT PAX DOOR ANCHOR FITTING IS CRACKED AND SWIVEL FITTING HOLE ELONGATED. REMOVED AND REPLACED PAX DOOR AFT ANCHOR FITTING ASSY WITH A NEW SERVICEABLE ANCHOR FITTING ASSY IAW CRJ 200 MM 52-11-17-400-804 STEP 2A-2B (3) CRJ 200 MM 52-11 -17-400-804 CLOSEOUT DUE. COMPLIED WITH CLOSEOUT (STEP 3) IAW CRJ 200 AMM 52-11-17-400-804. [SUPPLEMENTAL SDR CLOSED 6 /24/08] (A) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 KCSA081305 1 20080702 A 3350 LIGHT BOEING 747 747212B 1384886 NM L1 DOOR INOPERATIVE A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 EMERGENCY LIGHTS ARE OUT AT FORWARD AND AFT OF L1 DOOR (B) 2 L 7 4 4F RT A20WE 20080728 EA 2008 7 28 TRAX200800751 1 20080604 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 477-693 CORRODED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 708EV 10060 RT CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE FS 477.00 TO FS 693.00. REMOVED SEAT RAIL ASSY INSPECTED AND FOUND CORR OSION UNDER SEAT RAIL. PREPPED, PRIMED AND PAINTED AREA ON FUSELAGE SKIN IAW SRM 53-00-49. REPLACED SEAT RAILS AT FLOOR STATION 477.00 TO 693.00 IAW AMM 53-00-49. 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 KCSA081297 1 20080623 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2050 S34L CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 EXTERNAL SKIN AT STA-2050 AT STR-34L HAS MATERIAL LOSS EXCEDING SRM LIMITS (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 USAA920081195 1 20080514 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - LEVEL 2 CORROSION ON CABIN FLOORBEAM, BS 312, LBL 62 - RBL 24. REPAIRED CABIN FLOORBEAM , BS 312, LBL 62 - RBL 24 IAW B737 SRM 53-10-51, FIGURE 201. (S) 2 L 7 2 4F RT A16WE 20080728 NM 2008 7 28 USAA920081260 1 20080621 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 530AU 24412 PIT - FORWARD PRESSURE BULKHEAD - MAJOR REPAIR - VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17 JUST BELOW WL 234. REPAIRE D VERTICAL BEAM WEB AT BS 178, LBL 17 JUST BELOW WL 234 IAW B737 SRM 53-10-08. (S) 2 L 7 2 4F RT A16WE 20080728 SO 2008 7 28 RAIA00806001 1 20080606 A 3350 RPS113 POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 850HK 145003 MX-PHL - ALL EMERGENCY LIGHTS NOT STAYING ON. MAINTENANCE REMOVED AND REPLACED NR 1, 2, 3 AND 4 BATTERY POWER SUPPLY. (S) 2 L 7 2 4T RT T00011AT 20080728 NM 2008 7 28 2008UALA03349 1 20080612 A 2597 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SMOKE DETECTOR DEFECTIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 538UA 25222 LOCK MISSING FOR S LAV SMOKE DETECTOR CONNECTOR (P15). REPLACED P15 CONNECTOR ON S LAV SMOKE DETECTOR, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 EA 2008 7 29 REX2008F00015 1 20080709 A 2423 756652 ADG CNDAIR CL600 CL6002B19 1900309 EA UNWANTED DEPLOY A REXA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 21 8933B 10076 7933 ON A REPOSITIONING FLIGHT, AT FL310, THE AIR DRIVEN GENERATOR (ADG) DEPLOYED WITHOUT WARNING. THE FLIGHT CREW VERIFIED THAT ALL AIRCRAFT GENERATORS WERE ON LINE AT THE TIME OF DEPLOYMENT. THE FLIGHT CREW NOTIFIED ATC, DECLARED AN EMERGENC Y AND REQUESTED THE CLOSEST SUITABLE AIRFIELD. THE AIRCRAFT WAS ROUTED TO ANOTHER AIRPORT WHERE AN OTHERWISE NORMAL AP PROACH AND LANDING WERE MADE. MAINTENANCE MET THE AIRCRAFT AT THE GATE. MAINT STOWED THE ADG AND PERFORMED AN AUTO DEP LOY TEST IAW AMM. THE TEST WAS NORMAL. MAINTENANCE THEN PERFORMED THE DYE PENETRANT INSPECTION REQUIRED BY SB A601R-24- 120. AND THE NDT MANUAL. NO DEFECTS WERE NOTED AND THE AC WAS RELEASED FOR SERVICE. (K) 2 L 7 2 4F RT A21EA 20080729 NE 2008 7 29 UIE2008F00009 2 20080607 A 7200 CF650E2 ENGINE BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE DAMAGED A UIEA A UNSCHED LANDING E M J VIBRATION/BUFFET OVER TEMP WARNING INDICATION CL CLIMB 1 EA 15 524MC 21784 617858 SHORTLY AFTER TAKING OFF, HEARD AND FELT 2 LOUD BANGS (18 SECONDS AFTER TAKEOFF) EGT WENT TO 962 FOR 3 SECONDS ACCOMPLIS HED ENGINE FAILURE AND SEVERE DAMAGE CHECKS. ENGINE WAS LOCKED AND PERFORMED 3 ENGINE FERRY. ENGINE WAS REPLACED. (K) 2 L 7 4 4F 4 F RT A20WE E23EA 20080729 NM 2008 7 29 HNA2008F00006 1 20080309 A 5714 85350270101 BRACKET DHAV DHC8 DHC8102 2809003 NM UPPER WING BOX CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 846EX 36658 326 IN WING BOX, UNDER ACCESS PANEL 261 FT BRACKET ANGLE BETWEEN LT STRINGER 2 AND WING BOX FRAME AT FS 369.511 FOUND CRACKE D. REPLACED WITH NEW PN 85350270-101 IAW SRM 51-40-00 CRACK MINOR IN NATURE, NON STRUCTURAL IN TYPE. (K) 2 H 7 2 4T RT A13NM 20080729 NM 2008 7 29 2008UALA03432 1 20080616 A 2797 GROUND WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER TRIM DAMAGED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 545UA 25323 RUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. WIRING SHORT AT S3 SWITCH. REPAIRED GROUND TO S3 SWITCH ON M74 PANEL, SYSTEM CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 NM 2008 7 29 2008UALA03584 1 20080624 A 5320 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 FWD PIT STA 540 STR 24L-25L HAS 1 EA DENT. ACCOMPLISHED MAJOR REPAIR AT GSO. REPAIRED IAW REO G12368 AN D EVA 71698 AN D SRM 51-00-06. THIS IS A CAT B REPAIR AND REQUIRES SUPPLEMENTAL INSPECTIONS TO BEGIN AT 50000C AND 12000C THEREAFTER. THIS CONSISTS OF BOTH DETAILED VISUAL INSP AND NDT PER EVA 71698 CURRENT PTC IS 14404. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 NM 2008 7 29 2008UALA03587 1 20080624 A 3350 362624 BULB BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 776UA 26937 AFT PORTION OF FLOOR LIGHTING AT SEAT 2E HAS ONE BULB OUT. REPLACED LAMP OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080729 EA 2008 7 29 TRAX200800767 1 20080606 A 5310 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 684BR 7708 CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED .3" IN LENGTH. REMOVED CRACKED SUPPORT BEAM. INSTALLED NEW SERVICEABLE IA W SRM 51-42-21. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 ASAA0843176 1 20080629 A 5755 654645170A SKIN BOEING 737 737490 1384715 NM NR 8 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 RIGHT WING NR 8 SPOILER HAS DENT ON LOWER SURFACE 5 INCHES FROM O/B END. PREPARED DAMAGED AREA. FABRICATED REPAIR DOUB LER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080729 NE 2008 7 29 ASAA0853174 2 20080710 A 7261 OIL SYSTEM BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE NR 1 ENGINE LOW A ASAA O OTHER K FLUID LOSS DE DESCENT 1 NM 02 558AS 7871 35177 894148 ENGINE OIL NR 1 = 12 QTS, NR 2 = 13 QTS AT TOP OF DESCENT SERVICED BOTH ENGINE OIL LEVELS TO FULL PER MM 12 13 11. NR 1 ENGINE ADDED 4.5 QTS, NR 2 ENGINE ADDED 4.0 QTS AND APU 0 ENGINE OIL ADDED INFO ENTERED INTO WEB BASED OIL MONITORING D ATA BASE. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080729 EU 2008 7 29 USAA920081160 1 20080601 A 3230 664700500A4D CONTROL UNIT AIRBUS A321 A321211 3930370 EU LANDING GEAR FAULTY A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 173US 25534 2205 1481 FLT 41437 - CLT-LAX - AIR TURNBACK - THE FLIGHT CREW EXPERIENCED A LOUD, CONSTANT NOISE WITH EXCESSIVE VIBRATION AFTER T AKEOFF. THE AIRCRAFT WAS UNABLE TO CLIMB MORE THAN 500 FEET PER MINUTE AND UNABLE TO REACH SPEEDS BEYOND 280 KTS. AFTE R A FLY-BY, IT WAS DETERMINED THAT THE NOSE GEAR DOORS HAD NOT RETRACTED. THE CREW DECLARED AN EMERGENCY AND RETURNED T O CLT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL INTERFACE UNIT. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080716 NM 2008 7 16 2008UALA03094 1 20080529 A 5330 SKIN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 914UA 25381 FUSELAGE LOWER SKIN AFT FASTENER HOLE OF E&E COMPARTMENT EXHAUST DUCT CUTOUT CRACKED AT BS 378-380 STRINGER S-28L TO S-2 8R. 2 L 7 2 4F 4 F RT A16WE E21EU 20080716 NM 2008 7 16 UPS08B52401 1 20080417 A 5320 65B09631344 FILLER BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:BCF BS 1140 RT TENSION TIE UPPER & LWR CLIP FILLER CRACKED. BS 1140 RT TENSION TIE UPPER & LWR CLIP FIL LER REPLACED PER SRM 53-40-30 I FIG 201. 2 L 7 4 4F RT A20WE 20080716 CE 2008 7 16 GUUA05290801 1 20080529 A 3260 WARNING SYSTEM BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A GUUA O OTHER N FALSE WARNING CL CLIMB 1 SO 29 87554 UE227 FLIGHT: 9131 TPA/TLH AFTER TAKEOFF DURING LANDING GEAR RETRACTION THE LANDING GEAR HORN CAME ON WITH GEAR HANDLE LIGHT I LLUMINATED. RECYCLED THE LANDING GEAR EVERTHING EXTINGUISHED LATER GEAR HANDLE LIGHT ILLUMINATED. RETURNED TO TPA. LA NDED WITHOUT INCIDENT. INSPECTED LANDING GEAR SYSTEM, NO DEFECTS NOTED. LANDING GEAR, OPERATIONAL CHECKS OK. 2 L 7 2 4T RT A24CE 20080716 SO 2008 7 16 RAIA00805029 1 20080526 A 3350 744436 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 840HK 145341 PRE FLIGHT INSPECTION BY FLIGHT ATTENDANT -ORD- SEVERAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE RIGHT HA ND OVERWING EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20080716 EA 2008 7 16 MASA200800429 1 20080527 A 5240 601R3189015 LOCK CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR FAULTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37178 7178 ASH 2785 PHX - SERVICE DOOR WILL NOT STAY OPEN. MX REPLACED THE LOCK ASSEMBLY. 2 L 7 2 4F RT A21EA 20080716 NM 2008 7 16 C8GA20080014 1 20080529 A 2150 2040751 ACM BOEING 727 727223 1384074 NM LEFT FAILED A C8GA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 29 715AA 22470 FLT 711 FOR DEN TO TOL. DURING CLIMB OPERATION FROM DEN THE AIRCRAFT WAS UNABLE TO MAINTAIN CABIN ALTITUDE BELOW 10000 F EET WITH ONE PACK OPERATION. AIRCRAFT RETURNED TO DEN WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALE D LEFT ACM INOP. REMOVED AND REPLACED LEFT ACM AND LEFT PACK SHUTOFF VALVE, OPS CHECK GOOD. NO OTHER DEFECTS NOTED. A IRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20080716 EA 2008 7 16 MASA200800443 1 20080601 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002D24 1390016 EA LAVATORY ACTIVATED A MASA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 07 912FJ 15012 ASH FLT 2821 BFL-PHX. SMOKE DETECTOR WENT OFF IN FORWARD LAVATORY. MX PERFORMED INSPECTION AND TEST OF FORWARD LAVATOR Y SMOKE DETECTOR, NO FAULT FOUND. AIR START CART RUNNING NEXT TO AIRCRAFT IS DETERMINED SOURCE OF SMOKE FUMES. 2 L 7 2 4F RT A21EA 20080716 NM 2008 7 16 SWAA082936 1 20080529 A 3350 20121 CHARGER BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED MV1 CHECK, FOUND LT AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SWAA082915 1 20080601 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED MV2 CHECK, FOUND RT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SWAA082924 1 20080601 A 3350 3071BPEGPL LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 22Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 12 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 USAA920081158 1 20080527 A 5330 65457742 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 PHX - MAJOR REPAIR - CRACKED FUSELAGE SKIN, BS 727D, S22L - S24L, WL 154 - WL 172. REPAIRED FUSELAGE SKIN, BS 727D, S2 2L - S24L, WL 154 - WL 172 IAW US AIRWAYS TR 53-33 AND B737 SRM 53-00-01-2R31 FIGURE 201. RECEIVED AND REVIEWED THE ME- 0308 STRUCTURAL DEFECT ALERT FORM FOR THIS DISCREPANCY AND HAVE ADDED THE CORRECTIVE ACTION AND LOCATION OF THE DISCREPA NCY AS REQUIRED. 2 L 7 2 4F RT A16WE 20080718 EA 2008 7 18 VNA2008F00000 1 20080705 A 5100 NONE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NO DEFECTS NONE A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 250PS 7929 CREW REPORTED MULTIPLE BIRD STRIKES ON TAKEOFF. MAINT INSPECTED AND FOUND NO DEFECTS. AC WAS RELEASED FOR SERVICE. (K ) 2 L 7 2 4F 4 F RT A21EA E15NE 20080718 SO 2008 7 18 A3W2008F00000 2 20080527 A 8520 SA631475 PISTON CESSNA 185 A185F 2072821 CE CONT O520 IO520D 17032 SO ENGINE BROKEN E A3WC O OTHER O OTHER NR NOT REPORTED 1 AL 03 121EE 1185 18503765 282624R AT OIL CHANGE, FOUND ALUMINUM CONTAMINATION IN OIL FILTER ELEMENT. INVESTIGATION FOUND BROKEN PISTON SKIRT AND RING PAR TS IN OIL PAN FROM NR 4 CYLINDER. NR 4 PISTON SKIRT WAS BROKEN AT LOWEST RING, AT BOTTOM OF PISTON HALF, TOTAL SKIRT WA S BROKEN OFF THIS PISTON , FOUND 5/27/2008. (K) 1 H 7 1 3O 3 O 3A24 E5CE 20080721 NM 2008 7 21 UPS08M52411 1 20080415 A 5730 DOUBLER DOUG MD11 MD11 3023602 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C RIGHT WING FIXED WING L/E AFT SKIN DOUBLER APPROX STA XORS 556 FOUND CRACKED (2522). RIGHT FIXED WING L/E AFT SKIN DBLR ATTACH PARTS & FASTENERS REMOVED. CRACKED BEADED DOUBLER TRIM OFF. HFEC INSP C/O ON TRIM OFF AREA, FOUND NO CRACK EVIDENT. TWO EA REPAIR ANGLES, FILLER & DOUBLER FABRICATED. REPAIR PARTS HOLES PICKED UP, PROTECTED/PAI NTED. TWO EA REPAIR ANGLES, FILLER, DOUBLER & ATTACH PARTS INSTALLED. REWORKED AREA PAINTED. 2 L 7 3 4F RT A22WE 20080721 NM 2008 7 21 SWAA083649 1 20080701 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083739 1 20080707 A 5320 6545410 BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND CENTER CABIN LONGITUDINAL BEAM CRACKED AT BS 665, RBL 24.75. REPAIRED BEAM PER SWA E A. 2 L 7 2 4F RT A16WE 20080721 2008 7 21 2008UALA02424 4 20080424 A 3431 8220298001 RECEIVER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE ILS FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 786UA 26938 PRE-DEPARTURE CHECK FOUND NO LAND 3 ILS C ON STATUS PAGE. FOUND CENTER INSTRUMENT LANDING SYSTEM RECEIVER FAULTY. REPL ACED CENTER ILS RECEIVER PER AMM 34-31-01. CAT III CHECK OKAY PER AMM 22-11-00. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080721 NM 2008 7 21 2008UALA02690 1 20080509 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 195UA 26899 EEL LIGHT ASSY AT SEAT 34C TORN OFF. FOUND LIGHT ASSEMBLY DISLODGED. REPLACED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080721 NM 2008 7 21 SWAA083509 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083510 1 20080625 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER 8R CRACKED AT BS 400. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083500 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083511 1 20080625 A 3210 6546140 FITTING BOEING 737 7373H4 1384600 NM RT MLG WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED BRDG CHECK, FOUND RT MLG UNIVERSAL FITTING WORN. REMOVED AND REPLACED FITTING PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083512 1 20080625 A 2910 41630A FUSE BOEING 737 7373H4 1384600 NM HYDRAULIC SYS FAULTY A SWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 29 335SW 23939 ON APPROACH INTO AUS T/E FLAPS INDICATED 30 DEGREES, NO L/E DEVICES DEPLOYED. CYCLED FLAPS, ON SECOND APPROACH NO L/E D EVICES. REMOVED AND REPLACED L/E HYDRAULIC FUSES PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083513 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 EA 2008 7 18 A6WA200840436 1 20080520 A 5420 PLATE CNDAIR CL600 CL6002B19 1900309 EA LT PYLON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 LEFT PYLON TRAILING EDGE, OUTBOARD UPPER BONDING PLATE CORRODED. REPLACED BECAUSE OF MATERIAL OUT OF LIMITS TOLERANCE I AW ARM 54-00-00. FORMED AND INSTALLED NEW BONDING PLATE IAW SRM 51-24-21 AND SRM 51-42-10. (A) 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840438 1 20080516 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 CRACK EXIST ON BRACKET INTERCOSTAL FS 621 TO 625 ADJACENT TO STR 14 LEFT. BRACKET OF INTERCOSTAL FS 621 TO 625 ADJACENT TO STR 14 LT REPLACED IAW SRM 51-42-21. (A) 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840439 1 20080520 A 5347 CARGO TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 CORROSION FOUND ON CARGO TRACK RBL 9 BETWEEN FS 559 + 110 AND FS 568. CARGO TRACK REPLACED IAW AMM 53-01-11-400-802. ( A) 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840440 1 20080520 A 5347 CARGO TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 CORROSION ON CARGO TRACK AT LBL 9 BTW FS 559 + 110 AND FS 570. CARGO TRACK REPLACED IAW AMM 53-01-11-400-802. (A) 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840442 1 20080518 A 5320 CROSSBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 PILOT`S BULKHEAD, CROSSBEAM CRACKED AT FS 280, LBL 9. BULKHEAD CROSSBEAM REPAIRED IAW REO 601R-53-11-171 REV D SCHEME B . (A) 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840443 1 20080518 A 5320 CROSSBEAM CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 PILOT`S BULKHEAD, CROSSBEAM CRACKED AT FS 280, RBL 9. BULKHEAD REPAIRED IAW REO 601R-53-11-171 REV D SCHEME B. (A) 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840449 1 20080522 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 CORROSION ON FLOOR SILL LEFT SIDE BETWEEN FS 574 AND FS 621. CORROSION ON FLOOR SILL LT SIDE BETWEEN FS 574 AND FS 621. REMOVED AND TREATED IAW SRM 51-21-06. (A) 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840450 1 20080522 A 5347 FITTING CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 CORROSION ON THREE TIE DOWN CARGO DOOR NET AROUND FLOOR SCREW. CORROSION ON THREE TIE DOWNS OF CARGO DOOR NET REMOVED A ND TREATED IAW SRM 51-21-06. (A) 2 L 7 2 4F RT A21EA 20080729 EU 2008 7 29 USAA920081174 1 20080603 A 3350 E0062B1A4AD0A SWITCH AIRBUS 320 A320232 3930326 EU CABIN INTERMITTENT A USAA O OTHER O OTHER CR CRUISE 1 EA 19 604AW 1196 FLT 570 YVR - PHX, EMERGENCY EXIT LIGHTS FLICKER ON AND OFF ON GROUND AND DURING FLIGHT. MAINTENANCE REMOVED AND REPLAC ED THE OVERHEAD EMERGENCY EXIT LIGHT SWITCH. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080729 EU 2008 7 29 USAA920081182 1 20080524 A 5320 D53471124200 SHEAR PLATE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 652AW 0953 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SHEAR PLATE BS 3310 FR 69 - BS 3366 FR 70, S23 -24R. REPLACED CABIN SHEAR PLATE BS 3310 FR 69 - BS 3366 FR 70, S23 -24R IAW SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080729 EU 2008 7 29 USAA920081181 1 20080524 A 5540 D5537131800200 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 652AW 0953 SAL - MAJOR REPAIR - C7 CHECK - NR 3 RUDDER HINGE FITTING HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 2279 RIB 5. R EPLACED NR 4 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 2279 RIB 5 IAW A320 AMM 55-36-41. (S) 2 L 7 2 4F RT A28NM 20080729 NM 2008 7 29 USAA920081191 1 20080609 A 3397 WIRE BOEING 737 73733A 1384673 NM EMERGENCY LIGHTS DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 164AW 23625 FLT 550 - PHX - EMERGENCY PATH LIGHT AT AFT GALLEY INOP. MX RECONNECTED WIRES TO CONNECTOR. OPERATIONAL CHECK WAS GOOD . (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081192 1 20080609 A 3397 WIRE AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 806AW 1056 FLT 688 - PHX - ROW 22 LT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT INOP. MX REPAIRED BROKEN WIRE. OPERATIONAL CHECK WA S GOOD. (S) 2 L 7 2 4F RT A28NM 20080729 NM 2008 7 29 USAABB08108 1 20080617 A 3397 CONNECTOR BOEING 757 757225 1384959 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 914AW 22208 PHX - THE EMERGENCY LIGHT ON SEAT 6C WAS FOUND INOPERATIVE. MAINTENANCE RECONNECTED THE SEAT EMERGENCY LIGHT CONNECTOR AT SEAT 6C AND SECURED THE CABLE. OPERATIONAL CHECKS OK. (S) 2 L 7 2 4F RT A2NM 20080729 NM 2008 7 29 USAA920081237 1 20080617 A 3350 20131A BATTERY PACK BOEING 737 7373S3 1384711 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 315AW 23734 FLT 088 - PHX - EEL - EMERGENCY LIGHTS INOP FROM ROW 6 FWD, INCLUDING L1 AND R1 EXIT LIGHTS. MX REPLACED THE BATTERY PA CK. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A16WE 20080729 CE 2008 7 29 DXTA200803092 1 20080603 A 3246 WHEEL CESSNA 750 750 2076810 CE NLG VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 913QS 7500113 TAKE OFF ABORTED DUE TO SEVERE NOSE WHEEL SHIMMY AND VIBRATION. (B) 2 L 7 2 4J RT T00007WI 20080729 CE 2008 7 29 DXTA200803101 1 20080607 A 3150 WARNING MESSAGE CESSNA 750 750 2076810 CE ILLUMINATED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 906QS 7500206 AFTER TAKEOFF THE FOLLOWING MESSAGE ILLUMINATED YAW DAMPER OFF BOTH YAW DAMPERS WERE OFF LINE. (B) 2 L 7 2 4J RT T00007WI 20080729 NM 2008 7 29 USAA080722001 1 20080618 A 2780 4911711 COMPUTER AIRBUS A319 A319132 3930340 NM E&E BAY FAILED A USAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 19 832AW 23617 805 1643 FLT 04 - PHX - LAS - FX - CREW REPORTED AFTER TAKEOFF RECEIVED AN ACARS MESSAGE THAT THE SLATS WERE LOCKED IN THE UP POS ITION. CREW CONTINUED ON TO LAS. CREW DECLARED AN EMERGENCY ON APPROACH INTO LAS. EMERGENCY EQUIPMENT WAS CALLED OUT. THE CABIN WAS NOT PREPPED. CREW MADE A ZERO SLAT FLAPS 3 LANDING. THE LANDING WAS UNEVENTFUL. THE ACFT TAXIED TO TH E GATE. MX REPLACED THE SLAT AND FLAP CONTROL COMPUTER IN THE NR1 AND NR2 POSITIONS. MX PERFORMED A BITE TEST PER AMM 27-81-00-740-002. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080729 EA 2008 7 29 TRAX200800798 1 20080616 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 820AS 7188 FORWARD OVER HEAD EMERGENCY EXIT FLOOD LIGHT INOPERATIVE. REMOVED AND REPLACED FWD OVERHEAD EMERGENCY FLOOD LIGHT BULB. OPS CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAA920081244 1 20080619 A 5754 SKIN BOEING 757 7572B7 1384964 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 929UW 27144 BFM - C2 - MAJOR REPAIR - LT WING LEADING SLAT NR 2 COVE PANEL SKIN ALONG OUTBOARD TRACK HINGE FITTING HAS A CRACK. REP AIRED LT WING LEADING EDGE SLAT NR 1 COVE PANEL SKIN ALONG OUTBOARD TRACK HINGE FITTING IAW B737 SRM 51-20-05. (S) 2 L 7 2 4F RT A2NM 20080729 CE 2008 7 29 DXTA200803108 1 20080608 A 2120 UNKNOWN CESSNA 500 560CESSNA 2076750 CE CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 327QS 5600327 BURNING ODOR IN CABIN. (B) 2 L 7 2 4F RT A22CE 20080729 EU 2008 7 29 USAA920081257 1 20080623 A 2560 321430 BATTERY AIRBUS A321 A321211 3930370 EU FLASHLIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 172US 1472 FLT 728 SFO - PHL - EMERGENCY EQUIPMENT - AFT GALLEY FLASHLIGHT NEEDS NEW BATTERY. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080729 CE 2008 7 29 DXTA200803125 1 20080615 A 3150 WARNING MESSAGE CESSNA 750 750 2076810 CE ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 978QS 7500187 AMBER CAS "FADEC FAIL L A" ILLUMINATED PRIOR TO TAKEOFF. ABORTED T/O. (B) 2 L 7 2 4J RT T00007WI 20080729 NM 2008 7 29 USAA920081252 1 20080620 A 2761 31077111 ACTUATOR AIRBUS A319 A319132 3930340 NM NR 3 SPOILER FAILED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 827AW 25340 25340 1547 FLT 687 - PHX - EWR - RETF - DURING CLIMB THE LT SPOILER REMAINED DEPLOYED 2 INCHES CAUSING EXCESSIVE VIBRATION. CABIN VERIFIED CONDITION. CAPTAIN RETURNED TO THE FIELD. MX REPLACED THE NR3 SPOILER ACTUATOR IAW WITH AIRCRAFT MAINTENANCE MANUAL 27-64-51. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080718 EA 2008 7 18 A6WA200840451 1 20080520 A 5240 601R3895719 PLATE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 SERVICE DOOR LOWER PROTECTIVE PLATE P/N 601R38957-19, FOUND CORRODED OVER LIMITS. SERVICE DOOR LOWER PROTECTIVE PLATE REPLACED IAW SRM 51-41-04. (A) 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840453 1 20080528 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 CORROSION FOUND ON PAX DOOR LOWER SILL FS 315 AND FS 344 LBL 43. CORROSION REMOVED IAW SRM 51-21-06. (A) 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840456 1 20080528 A 5210 PANEL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 REPAIR CRACKS IN PASSENGER DOOR PANELS. CRACKS ON PASSENGER DOOR PANELS REPAIRED IAW CRJ 200 REO 601R-52-11-279. (A) 2 L 7 2 4F RT A21EA 20080718 EU 2008 7 18 M7K2008F00042 1 20080512 A 2150 5300273 TENSIONER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE A/C COMPRESSOR CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 815MH 2209 4022 DURING ROUTINE MAINT (1) OF (2) BELT TENSIONING ARMS FOUND CRACKED IN (2) PIECES. FAILURE ORIGINATED AT WELDMENT. SEVE RAL HAVE FAILED IN THIS MANNER. SUGGEST POST WELD, HEAT TREATMENT TO RELIEVE WELD STRESS. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 EA 2008 7 18 A6WA200840409 1 20080510 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 442AW 7778 CORROSION EXISTS ON LOWER SILL OF CARGO DOOR FS 574 TO FS 621 LBL 45. CORROSION REMOVED IAW SRM 51-21-06. 2 L 7 2 4F RT A21EA 20080718 EU 2008 7 18 M7K2008F00029 1 20080512 A 6720 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE FAILED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 814MH 565 4020 23100 A FAULT CODE WAS GENERATED ON SHUTDOWN INDICATING A DEFECT OF COLLECTIVE POTENTIOMETER. A NEW PART WAS INSTALLED, NO FU RTHER FAULT WAS DETECTED. THIS IS RECURRING FAILURE FOR THIS PART WHICH HAS EFFECTED DISPATCH RELIABILITY FOR THIS MODE L HELICOPTER. SUGGEST AN ALTERATION OF FAULT SENSING SOFTWARE TO REDUCE FAULT SENSITIVITY TO PERHAPS A SIGNAL LOSS OF 0 .5 SECOND RATHER THAN 1/20TH OF A SECOND. AN OPTIC RATHER THAN A RESISTANCE BASED SENSOR SHOULD BE CONSIDERED AS CONTAC T POINT IS DAMAGED BY AC VIBRATION WHEN AC POWER SETTINGS ARE SET FOR CRUISE FLIGHT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 SO 2008 7 18 C2XA08SH081 1 20080601 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14177 14500888 SHV - DURING C-CHECK, LT OMEGA BEAM LOWER FLANGE HAS CORROSION BETWEEN FRAME 19-24. MX REPAIRED LT OMEGA BEAM AT FR 19- 24 BY INSTALLING NEW SECTION IAW EC 5320-01229. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 20080718 NM 2008 7 18 UPS08M52506 1 20080416 A 5720 SUPPORT BRACKET DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C LEFT WING L/E TOP PANEL 516ET INTERNAL SUPPORT BRACKETS 03 EA FOUND CRACKED. NR 516ET PANEL INTERNAL (3EA) SUPPORT BRACKETS REMOVED. REPAIR BRACKETS 6EA FAB & HEAT-TREATED. FASTENER HOLES PICK-UP ON 6EA REPAIR SUPPORT B RACKETS. SIX EA REPAIR SUPPORT BRACKETS REPROTECTED, PAINTED & INSTALLED AS PER SRM 57-10-00 VOLI FIG 31 REV 35. 2 L 7 3 4F RT A22WE 20080718 CE 2008 7 18 VQ82008F00000 1 20080522 A 2760 2607003375 TUBE LEAR 35 35A 5170602 CE LT SPOILER CORRODED E VQ8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 19 135WE 240 DURING TAXI FOR DEPARTURE, PILOT NOTICED REDUCED BRAKING ABILITY OF THE AC. UPON RETURNING TO THE TERMINAL IT WAS NOTIC ED THAT A LARGE AMOUNT OF HYDR FLUID WAS COMING FROM LT WHEEL WELL FURTHER INVESTIGATION BY MFG REVEALED A RUPTURE IN A SPOILER RETRACT LINE. MFG HAS BEEN CONTACTED FOR REPAIR AND RETURN TO SERVICE OF THE AC. (K) 2 L 7 2 4F A10CE 20080718 WP 2008 7 18 UPS08852457 1 20080608 A 5321 FLOORBOARD DOUG DC8 DC873F 302199F WP CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 FLOORBOARD F81 HAS ONE EACH SCREW HOLE BROKEN OUT. CUT OUT DAMAGE, FABBED AND INSTALLED REPAIR DOUBL ER IAW SRM 53-2-3 FIG 10, 51-1-8, 51-1-21, 51-1-16. 2 L 7 4 4F RT 4A25 20080718 WP 2008 7 18 UPS08852464 1 20080611 A 3350 6012235 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY DISCHARGED. EMERGENCY LIGHT BATTERY PACK AND RELAY UNIT REPLACED AND TESTED SERV IAW DC8 AMM 33-50-01-2-4. 2 L 7 4 4F RT 4A25 20080718 WP 2008 7 18 UPS08852466 1 20080612 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED & REPLACED BATTERY PACK REF DC-8 MM 33-50-01. OPS CHECKS NORMAL. 2 L 7 4 4F RT 4A25 20080718 NM 2008 7 18 UPS08B52465 1 20080610 A 3350 POWER SUPPLY BOEING 747 747400 13848AT NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 579UP 26062 INSPECTION TYPE:N/A FWD RT OVERWING EXTERNAL EMERGENCY EXIT LIGHT INOP. NOTE: TROUBLESHOT TO DEFECTIVE PWR SUPPLY. DEF ERRAL M377738 ISSUED. REF MEL 33- 51-2-2. EMERGENCY LIGHTS DEACTIVATED PER SR 747-00-2117. TRANSFERRED TO NR ASL7612 2 L 7 4 4F RT A20WE 20080718 EU 2008 7 18 E0X2008F00005 1 20080603 A 2435 23091002 STARTER GEN BRAERO 1000 BAE1251000 1500287 EU PWA 306 PW306B NE NR 1 ENGINE FAILED E E0XA O OTHER O OTHER NR NOT REPORTED 1 EA 39 542LR 598 259042 IN CRUISE FLIGHT AT FL380, CREW FELT A VIBRATION, IT CONTINUED TO GET STRONGER. CREW REQUESTED ATC TO LAND AT NEAREST S UITABLE AIRPORT BUT DID NOT DECLARE AN EMERGENCY. FLIGHT CREW DETERMINED THAT NR 1 GENERATOR WAS GONG BAD AND DIVERTED THE AC. APPROACH WAS MADE WITH THE LT ENG IN IDLE, AC MADE AN UNEVENTFUL LANDING WITH NO INJURIES TO PASSENGERS OR CREW . CONTACTED INSP AND MAINT OF LT ENGINE AND STARTER/GEN. ON INSP, FOUND THAT LT STARTER/GEN HAD FAILED, BRGS WERE WORN . REMOVED AND REPLACED LT STARTER/GEN, RT SERVICEABLE STARTER/GEN AS WELL AS FOR TIME. PERFORMED AN OPS CHECK OF BOTH STARTER/GENS WITH NO DISCREPANCIES NOTED. (K) 2 L 7 2 4F 4 F RT A3EU E35NE 20080718 CE 2008 7 18 E0X2008F00006 1 20080613 A 3260 SWITCH BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE MLG FAULTY A E0XA O OTHER O OTHER NR NOT REPORTED 1 SW 99 311GL RK311 ON DEPARTURE, ON A MAINT/ REPOSITION FLIGHT, FLIGHT CREW NOTED NR 2 T/R STOW LIGHT ON. FLIGHT CREW ELECTED TO RETURN TO DEPARTURE. CREW NOTED ON SELECTING GEAR DOWN THAT THE NR 1 GEAR DOWN LIGHT WAS NOT ILLUMINATED. CREW ELECTED TO DO A FLY BY TO VISUALLY VERIFY GEAR DOWN AND LOCKED. GEAR WAS VERIFIED BY TOWER, AC MADE AN UNEVENTFUL LANDING. CONTRACT FO R INSP AND MAINT, ON INSP FOUND THAT NR 2 OB T/R STOW SWITCH WAS FAULTY, SWITCH WAS REPLACED, OPERATIONALLY CHECKED. FO UND THAT NR 1 MAIN GEAR DOWN LIGHT WAS BURNED OUT. LAMP WAS REPLACED WITH A NEW LAMP (PN AS327) AND OPERATIONALLY CHECK ED. AC WAS RELEASED FOR MAINT/REPOSITION TEST FLIGHT. (K) 2 H 7 2 4F 4 F RT A16SW E25EA 20080718 NM 2008 7 18 UPS08552453 1 20080610 A 3350 LIGHT BOEING 757 75724APF 1384969 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 475UP 28845 INSPECTION TYPE:N/A DURING CHECK EMERGENCY LIGHTS FOUND EMERGENCY EXIT EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED E MERGENCY EXIT EGRESS LIGHT LAMP PER B757 AMM TASK 33-51-06-962- 001 PAGE 1 AND 2 STEP 8, OPERATIONAL TEST OK. 2 L 7 2 4F RT A2NM 20080729 NM 2008 7 29 USAABB08110 1 20080619 A 3350 20121 CHARGER BOEING 767 767201 1385125 NM CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 245AY 23897 PHL - THE EXTERIOR EMERGENCY LIGHT, AFT OF CARGO DOOR WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK CHAR GER. OPERATIONAL CHECKS OK. (S) 2 L 7 2 4F RT A1NM 20080729 2008 7 29 USAABA08020 4 20080620 A 3441 ADIRU AIRBUS 330 A330323 3930335 EU NR 3 MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 275AY 0370 MAN FLT 735 EN ROUTE MAN TO PHL. THE FLIGHT HAD AN ADIRU 3 FAILURE PRIOR TO ETOPS AIRSPACE, PREVENTING ETOPS OPERATIONS . THE FLIGHT RETURNED TO FIELD MAN, AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SWAPPED ADIRU 3 WITH ADIRU 2, AND PLACED ADIRU 2 ON MEL. (S) 2 L 7 2 4F RT A46NM 20080729 NM 2008 7 29 USAA920081255 1 20080601 A 5320 149N7130 INTERCOSTAL BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 905AW 23567 CMN - C12 - MAJOR REPAIR - LEVEL 2 CORROSION AT INTERCOSTAL OUTER CHORD 4"X1" AREA AT BS 900 WL 133 BL 0. REPAIRED LEVE L 2 CORROSION AT INTERCOSTAL OUTER CHORD 4"X1" AREA AT BS 900 WL 133 BL 0 IAW B757-200 SRM 51-70-12-0G. (S) 2 L 7 2 4F RT A2NM 20080729 CE 2008 7 29 DXTA200803102 1 20080607 A 3210 LANDING GEAR CESSNA 680 680CE 2076811 CE UNKNOWN E DXTA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 07 313QS 6800140 DEPARTED PDX RAISED GEAR FOLLOWED BY LOUD BANG, VIOLENT SHAKING. INDICATIONS WERE RED UNLOCK LT AND NOSE WHEEL GREEN LT . (B) 2 L 7 2 4F RC T00012WI 20080722 NM 2008 7 22 2008UALA02964 1 20080522 A 3510 6350A33XA OXYGEN SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW O2 LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 386UA 24661 CREW REPORT: CREW OXYGEN READS 1050 PSI. SUSPECT PRE FLIGHT CHECKS. SERVICED OXYGEN SYSTEM TO FULL 1650 PSI. AC OK F OR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 2008 7 22 2008UALA02967 4 20080522 A 2565 D31591478U1 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 378UA 24653 CREW REPORT: MATERIAL LOOPING THAT HOLDS GIRT BAR AT 1L HAS MIGRATED OVER COLLAR AND NEEDS ADJUSTMENT. IMPROPERLY INST ALLED SLIDE ASSEMBLY. CENTERED BAR IN LOOPING MATERIAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA02974 1 20080522 A 5753 654643661SP FLAP BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU LT WING DELAMINATED A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 941UA 43735 26676 LEFT WING AFT INBOARD FLAP OUTBOARD EDGE APPEARS TO BE DELAMINATED. SUSPECT MOISTURE CONTAMINATION. REPAIRED BY SHOP M ECHANIC PER GNMM 01-0-01-024. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA03004 1 20080526 A 3350 1619 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 921UA 25388 LIGHT ON LEFT UPPER AFT OF EMERGENCY EXIT INOP. SUSPECT FAULTY LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVIC E. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA02930 1 20080521 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 548UA 25396 FWD END GRIT BAR FALLING OFF WHEN DOOR 4R OPENS. ARM AND DISARM FEELS STIFF AND BINDING. REMOVED LINER & SLIDE & LUBED ARM-DISARM MECHANISM, ADJUST FWD & AFT LIFTER WITH SLIDE INSTALLED, ALL OPS ARE NOW NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080722 NM 2008 7 22 2008UALA03013 1 20080523 A 3350 60121 COVER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN UNSECURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 655UA 25393 BUSINESS EMERGENCY LIGHTING COMING OUT AGAIN. FOUND LIGHT ASSEMBLY LOOSE RE-ATTACHED EMERGENCY LIGHT STRIP COVER. AC O K FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 NM 2008 7 22 2008UALA03014 1 20080523 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN LOOSE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 661UA 27158 EMERGENCY PATH LIGHTS FROM ROW 15 TO 21 FLICKERING SWITCH ARMED. LOOSE CONNECTION. SECURED LOOSE EEL TRACK ASSEMBLY, O PS GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 NM 2008 7 22 2008UALA03108 1 20080530 A 2560 65659733 FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU GIRT BAR STRIPPED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 334UA 24229 DOOR 1R AFT GIRT BAR FITTING STRIPPED OUT. FOUND GIRT BAR FITTING DAMAGED. REPLACED GIRT BAR FITTING. AC OK FOR SERVI CE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA03174 1 20080603 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 FWD ENTRY DOOR CUTOUT AFT SIDE INTERCOSTAL WEB BETWEEN BS 348.2 & 360 AT STRINGER S-16L IS CORRODED. MAJOR REPAIR ACCOM PLISHED: FABRICATED & INSTALLED REPLACEMENT INTERCOSTAL ASSY. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA03216 1 20080605 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHT ROW 50 ABC INOP. RELAMPED EMERGENCY LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080722 NM 2008 7 22 2008UALA02939 1 20080520 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 541UA 25253 EXTERIOR EMERGENCY LIGHT AT AFT CARGO PIT DOOR INOP. INOP LAMP. RELAMPED LIGHT, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080718 EU 2008 7 18 M7K2008F00044 1 20080623 A 5302 350A23422221 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 806MH 999 3833 23220 DURING ROUTINE INSP, FITTING WAS FOUND CRACKED IN EXCESS OF 2 INCHES FROM MOUNTING FLANGE EDGE THROUGH ONE SCREW BORE HO LE. THIS IS A COMMON FAILURE FOR THIS PART. SUGGEST THIS PART BE MFG FROM MORE ROBUST MATERIAL SUCH AS SS OR TITANIUM. CAREFUL MATCH DRILLING AND SHIMMING IS REQUIRED DURING REPLACEMENT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 NM 2008 7 18 UPS08552454 1 20080611 A 3350 SWITCH BOEING 757 75724APF 1384969 NM EMERGENCY LIGHTS BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 435UP 25466 INSPECTION TYPE:N/A EMERGENCY LIGHTS SWITCH GUARD HAS PIECE BROKE OFF. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH GUAR D. OPS CHECK NORMAL IAW 757 M/M 33- 51-00. 2 L 7 2 4F RT A2NM 20080718 NM 2008 7 18 UPS08652424 1 20080604 A 3242 BRAKE BOEING 767 76734AF 1385212 NM NR 1 FIRE A IPXA K NONE A FLAME/FIRE LD LANDING 1 SO 01 323UP 27749 INSPECTION TYPE:N/A, NR 1 BRAKE FIRE ON ARRIVAL, FUSE PLUGS MELTED. CFR WAS CALLED DUE TO FIRE. 2 L 7 2 4F RT A1NM 20080718 WP 2008 7 18 UPS08852438 1 20080529 A 5320 47723981 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 END FITTING BLOWN OUT, L30L, STA 1759 DIFFICULT ACCESS. REMOVED AND REPLACED CORRODED FITTING IAW SR M 51-1-21, 51-1-8, 51-1-24 , 51-3-0. 2 L 7 4 4F RT 4A25 20080718 EU 2008 7 18 BIG2008F00000 1 20080714 A 6120 8954817 PITCH CONTROL CASA C212 C212CC 2410204 EU GARRTT TPE331 TPE33110R 0517 WP LT ENGINE MALFUNCTIONED E BIGA O OTHER J WARNING INDICATION CR CRUISE 1 NM 04 107BH 4497 165 P37018 ON THE LT ENG WITH THE SPEED LEVERS EET AT 100 PERCENT AND YOU TRY TO BRING THE POWER LEVER BACK TO CRUISE, AT ABOUT 70 PERCENT TO 80 PERCENT TORQUE THE RPM DROPS TO 93 PERCENT. TORQUE TEMP AND FUEL FLOW WILL INCREASE TO A HIGHER SETTING O N ITS OWN MAKING CONTROL OF THE PROP DIFFICULT. PILOT PERFORMED OF A COMMANDED ENG SHUTDOWN ON THE LT ENG AND LANDED NO RMALLY. (K) 2 H 7 2 4T 4 T A43EU E4WE 20080718 EU 2008 7 18 EHA2008F00002 1 20080708 A 5730 SKIN CASA C212 C212CC 2410204 EU GARRTT TPE331 TPE331* 01514 WP RT WING CRACKED E EHAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 423CA 240 DURING A ROUTINE INSP, FOUND AND DOCUMENTED CRACKS IN THE UPPER WING SKINS AT APPROX STA 6700 TO 7100 ON BOTH THE LT AND RT WINGS. (K) 2 H 7 2 4T 3 T A43EU E2WE 20080718 NM 2008 7 18 UIE2008F00000 1 20080712 A 2612 FIRE WARNING BOEING 747 74747UF 1384812 NM GE CF6 CF680C2* GL FALSE ACTIVATION A UIEA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 15 415MC 32837 REF: LOG PAGE 362049; TWICE DURING CRUISE, MOMENTARY ILLUMINATION OF MASTER WARNING LIGHTS WITH ASSOCIATED FIRE WARNING BELL. NO EICAS MESSAGE. ACCOMPLISHED CMC GROUND TEST FIRE PROTECTION SYSTEM. (TEST PASS) NO FAULTS IN CMC FAULT HISTO RY, MM26-10-00. (K) 2 L 7 4 4F 4 F RT A20WE E23EA 20080721 WP 2008 7 21 UPS08852419 1 20080602 A 3350 6012235 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. EMERGENCY LIGHTING BATTERY PACK REPLACED IAW DC8 AMM 33-50-01-2-4. 2 L 7 4 4F RT 4A25 20080721 NM 2008 7 21 UPS08M52409 1 20080317 A 5350 SKIN DOUG MD11 MD11 3023602 NM TAILCONE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C, RIGHT TAIL CONE DOOR ASSY INTERIOR BELOW BARRIER KEEPER SKIN CHAFED. KEEPER SKIN CHAFE MARK REMOVED & REPROTECTED. MAT'L REMOVED 0.008" ORG THK 0.032", REMN THK 0.024" FOUND OUT OF LIMIT. EXCEEDED LIMIT SKIN TRIMMED OF F. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. REPAIR DOUBLER FAB, HOLES PICKED UP, REPROTECTED & PAINTED. NEW REPAIR DOUBLER INSTALLED & REWORKED AREA PAINTED. 2 L 7 3 4F RT A22WE 20080721 NM 2008 7 21 UPS08M52410 1 20080410 A 5730 SKIN DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C, LEFT WING L/E FIXED WING AFT SKIN APPROX STA XORS 538 FOUND CRACKED (2477). LEFT WING NR 4 SLAT CABL E PULLEY REMOVED & L/E FIX WING AFT SKIN FASTENERS REMOVED. INNER SKIN BEADED DOUBLER TRIM OFF. HFEC INSP C/O ON TRIM OFF AREA, FOUND NO CRACK EVIDENT. THREE EA REPAIR ANGLES, DOUBLER & FILLER FAB REPAIR PARTS HOLES PICK-UP, REPROTECTED & PAINTED. THREE EA REPAIR ANGLES, DOUBLERS & FILLER ATTACH PARTS INSTALLED. NR 4 SLAT CABLE PULLEY INSTALLED. 2 L 7 3 4F RT A22WE 20080721 WP 2008 7 21 UPS08852428 1 20080605 A 2150 FLUID DOUG DC8 DC871F 302199D WP ACM LOW A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 755UP 46055 INSPECTION TYPE:N/A ON STARTING LEFT PACK, GRINDING NOISE FELT AND ODOR ENTERED COCKPIT COMPRESSOR OUT TEMP REACHED 100 DEG C DEF PER MEL 21-38-1, M 377306 ASSIGNED. FOUND CLAMP OFF OF ACM OUTLET AND OIL LEVEL LOW. RAN PACKS AND PRESSURIZ ED A/C IAW MM 21-31-00-2. ALL CHECKS NORMAL. THIS CLEARS M377306. 2 L 7 4 4F RT 4A25 20080721 NM 2008 7 21 UPS08M52430 1 20080408 A 3211 BUSHING DOUG MD11 MD11 3023602 NM RT MLG DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C CLG RT TRUNNION FITTING AFT HOLE FOUND SCORING MARK ON EXISTING BUSHING. CLG RT TRUNNION FITTING AFT HOLE BUSHING REMOVED. FPI C/O ON REWK AREA AND FOUND NO CORROSION EVIDENT. AFT BOLT HOLE DIA: 1.4380" & FOUND EXCEED L IMIT MAX ALLOWABLE DIA:1.385". TRUNNION FITTING AFT BOLT HOLE DIA 1.4380" EVAL & FOUND ACCEPTED PER EN1153-08. NEW BUS HING FAB & CADMIUM PLATED. NEW BUSHING INSTALLED AT CLG RT TRUNNION FITTING AFT BOLT HOLE. 2 L 7 3 4F RT A22WE 20080721 2008 7 21 SWAA083630 4 20080701 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 265WN 32522 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083652 1 20080701 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083722 1 20080705 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER 17L DAMAGED AT BS 360 TO BS 380. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 20080721 2008 7 21 2008UALA02693 4 20080509 A 2565 720129101 HOSE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE COLLAPSED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 653UA 25391 RIGHT OVERWING SLIDE INFLATION HOSE COLLAPSED. SUSPECT AC MAINTENANCE. REPLACED HOSE ASSEMBLY. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 EA 2008 7 22 A6WA200840461 1 20080530 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 CRACK EXIST ON FLOOR WEB FS 280 LBL 9. REWORK PERFORMED IAW REO 601R-53-11-1402. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840425 1 20080521 A 2931 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYSTEM MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION CR CRUISE 1 GL 31 442ZW 11725 7788 HYDRAULIC NR 2 LOW PRESSURE CAS MESSAGE IN FLIGHT. COMPLIED WITH QRH, QUANTITY INDICATED DASHES, PRESSURE INDIDCATED O PSI. ENGINE DRIVEN PUMP NR 2 RAN FOR APPROXIMANTELY 35 MINUTES AT 0 PSI. ACMP RAN FOR APPROXIMATELY 2 MINUTES AT 0 PSI . RAN FOR APPROXIMATELY 2 MINUTES AT O PSI. R&R EDP NR 2, EDP NR 2 RETURN LINE AND ALL FILTERS FOR NR 2 HYD SYSTEM IAW CRJ 200 AMM 29-10-00 OPS CHECK GOOD, NO LEAKS NOTED. 2 L 7 2 4F RT A21EA 20080722 WP 2008 7 22 ABXR080172 1 20080507 A 5313 27779223 LONGERON DOUG DC9 DC915F 3022037 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 783TW 47010 LONGERON 3 LEFT CRACKED AT FRAME TO LONGERON ATTCH POINT STA 930. REMOVED LONGERON SECTION, SPLICED NEW LONGERON IAW DC 9 SRM 53-02, FIG 18. (A) 2 L 7 2 4F A6WE 20080722 WP 2008 7 22 ABXA080176 1 20080616 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC933F 302207A WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 933AX 47291 COCKPIT EMERGENCY LIGHTS WOULD NOT COME ON DURING TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33- 53-00. (A) 2 L 7 2 4F A6WE 20080722 NM 2008 7 22 SWAA083912 1 20080715 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 258WN 32516 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080722 NM 2008 7 22 SWAA083962 1 20080716 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 10L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SWAA082929 1 20080530 A 5315 BAC1509100144 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 767SW 29807 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 733D, LBL 12 TO RBL 8. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20080716 NM 2008 7 16 SB08038 1 20080601 A 3350 20121 POWER SUPPLY BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 419US 23986 DFW - MAINTENANCE REPORTED THE EMERGENCY LIGHTS ON SEAT ROWS 21, 22, 23 AND 24 INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE BATTERY PACK/CHARGER ASSEMBLY LOCATED IN THE AFT GALLEY CEILING, LEFT-HAND SIDE, PER MM 33-51-51. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 UPS08M52503 1 20080516 A 5313 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM BS 869 L33L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C FWD CARGO AT STATION 869 LONGERON 33 LT LONGERON SPLICE DOUBLER FOUND CRACKED. CRACK SPLICE REMOVED P ER SRM 51-33-01 VII R35. NEW SPLICE REWORKED SMOOTH AND REPROTECTED PER SRM 51-21-01VII R35. FPI C/O PER DPS 4.707 REV AW ON NEW SPLICE AND FOUND NO CRACK EVIDENT. NEW SPLICE ADA8423-501 INSTALLED PER SRM 51-33-01 VII REV 35 AND BOEING D WG ADA8423. 2 L 7 3 4F RT A22WE 20080717 WP 2008 7 17 UPS08852565 1 20080527 A 5347 DC853B007002 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1460 WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK STA 1460, 0BL 2 EACH HOLES ELONGATED. REMOVED AND REPLACED SEAT TRACK PLUG IAW SRM, 51-3-00. 2 L 7 4 4F RT 4A25 20080717 EA 2008 7 17 CHQA200800101 1 20080530 A 2913 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 2 ENGINE LEAKING A CHQA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 11 469SM 18248 18248 7650 GEE873397 FLIGHT 5998, AMA TO SDF. AFTER TAKEOFF, THE CREW NOTICED THE HYDRAULIC QUANTITY DECREASING. WHILE RETURNING TO AMA, LO W HYDRAULIC 2 WAS DISPLAYED ON EICAS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE HYDRAULIC SYSTEM AND FOUND THE E2 HYDRAULIC PUMP LEAKING AT THE CASE LINE. THE PUMP WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080717 NM 2008 7 17 HNAA0800183 1 20080527 A 3350 0L3071BPRGL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 809EX 302 EMERGENCY LIGHT AT 4DF ON SIDEWALL IS BROKE. REPLACED EMERGENCY EXIT LIGHT, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 20080717 NM 2008 7 17 BB08104 1 20080602 A 2560 ACREM1A MEGAPHONE BOEING 757 7572B7 1384964 NM CABIN DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 939UW 27303 MCO - THE AFT MEGAPHONE WAS FOUND DAMAGED AND INOPERATIVE. MAINTENANCE REPLACED THE AFT MEGAPHONE. OPERATIONALLY CHECK S OK. 2 L 7 2 4F RT A2NM 20080717 EU 2008 7 17 USAA920081162 1 20080516 A 5540 D5537131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 602AW 565 SAL - MAJOR REPAIR - C1 CHECK - RUDDER HINGE FITTING NR 5 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 2985 / RIB 7. REPLACED RUDDER HINGE FITTING NR 5, VERTICAL STABILIZER STATION 2985 / RIB 7 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 20080717 NE 2008 7 17 ASMF200806001 2 20080601 A 7320 0154GF7 SENSOR BOEING 777 7772Q8 1385238 NM GE GE90 GE9094B 30045 NE RT ENGINE FAILED W ASMF A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 23 745AM 10004 10004 32718 900476 AIRCRAFT RETURNED OF FLIGHT DUE TO RIGHT ENGINE STALLED. MAINTENANCE PERSONNEL PERFORMED FIM 75-21 TASK 822 AND STALL I NSPECTION IN 1ST, 5TH AND 9TH HPC STAGES, NO DAMAGES WERE DETECTED IAW MM 71-00-00. RIGHT PT25 SENSOR WAS REPLACED IAW MM 73-21-63, TESTED CORRECT. THE OVERWEIGHT INSPECTION WAS NOT NECESSARY DUE TO AIRCRAFT LANDED WITH 211,400 KGS AND MA XIMUM LANDING WEIGHT IS 213,188 KGS. 2 L 7 2 4F 4 F RT T00001SE E00049EN 20080717 NM 2008 7 17 HALA0800611 1 20080602 A 3830 FLUSH MOTOR BOEING 767 767300 1385204 NM LAVATORY INOPERATIVE A HALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 585HA 24257 AIRCRAFT DIVERTED INTO LAX - ALL LAVATORY FLUSH MOTORS INOP. AIRPLANE WAS 16000 FEET OR ABOVE. FOUND TANKS LIGHTS ILLU MINATED AT AFT ATTENDED PNL. SERVICED AND RESERVICE IAW AMM 12-17-01. OPS CHECK NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20080717 NM 2008 7 17 SWAA083320 1 20080618 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 13L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843026 1 20080514 A 5753 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 LEFT OUTBOARD AFT FLAP LOWER SURFACE CHAFED 58 INCHES FROM OUTBOARD END PREPARED DAMAGED AREA. FABRICATED DOUBLER AND B ONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083339 1 20080618 A 5312 6546568 BULKHEAD BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 22Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED WEB PER ER. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083209 1 20080612 A 5340 6935364 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 987, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080717 NE 2008 7 17 ML62008F00000 2 20080620 A 7310 70BM021080 FILTER SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE CLOGGED E ML6A O OTHER O OTHER NR NOT REPORTED 1 WP 11 5793P 1476 A REDUCED FUEL FLOW CONDITION DEVELOPED AS THE ELECTRIC FUEL BOOST PUMP BEGAN TO DISINTEGRATE AS IT NEARED IT TBO (APPRO X 70 HRS TO REPLACEMENT). INTRODUCING METAL AND CONTAMINATING THE AIRFRAME FUEL FILTER, THIS IS A BYPASS CONDITION AND PROVIDED UNFILTERED FUEL TO THE FUEL CONTROL UNIT. THE BYPASS (F. FILTER) LIGHT APPARENTLY HAD AN ELECTRICAL FAULT IN THE TEST CIRCUIT AND THE CONDITION WAS NOT DETECTED ON RUN UP OR INFLIGHT. THE CONTAMINATED FUEL STATE EVENTUALLY LED T O A LARGE DROP IN THE FUEL FLOW RATE AND RESULTED IN THE GOVERNOR FAILING TO THE LOW SIDE, AS THE GOVERNOR WAS UNABLE TO MAINTAIN ENGINE AND ROTOR RPM. UPON INSPECTION OF THE ENGINE AFTER THE INCIDENT, THE AXIAL COMPRESSOR (MOD 03) FAILED 1 G 7 1 3U 3 U NC H9EU E19EU 20080717 NM 2008 7 17 SWAA083217 1 20080612 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083085 1 20080608 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083093 1 20080608 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083295 1 20080617 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 206WN 34011 EEPLS LENS MISSING AT RT OVERWING EXIT. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083303 1 20080617 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STR 24R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083302 1 20080617 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083304 1 20080617 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 WP 2008 7 17 S8A2008F00002 2 20080706 A 7261 M632481117 O-RING LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP LT ENG DIP STICK BROKEN E S8AA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 39 29NW 029 ON INITIAL DECENT, FLIGHT CREW NOTED A LOW INDICATION ON THE OIL PRESSURE GAGE FOLLOWED BY A LOW OIL PRESSURE LIGHT ON N R 1 ENGINE. THE FLIGHT CREW ELECTED TO SHUTDOWN THE LT ENGINE AND AN UNEVENTFUL LANDING WAS MADE WITH NO INJURIES TO PA SSENGERS. CARRIER CONTRACT FOR INSPECTION AND MAINTENANCE, FOUND A DEFECTIVE O-RING ON LT ENGINE OIL DIP STICK. REMOVE D AND REPLACED O-RING, SERVICED OIL AND PERFORMED A GROUND ENGINE RUN WITH NO DISCREPANCIES OR LEAKS NOTED. RETURNED AC TO SERVICE WITH NO ISSUES NOTED, REF NR 1 ENGINE OIL PRESSURE. (K) 2 L 7 2 4F 4 F A10CE E6WE 20080717 WP 2008 7 17 08FDEA02089 1 20080602 A 5720 ARB12613 ANGLE DOUG MD10 MD1010F 3022112 WP ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 LEFT WING INBD UPPER L/E PANEL 516 DT HAS A BROKEN ANGLE. REMOVED THE BROKEN ANGLE ON THE LEFT WING L/E PANEL 516 DT IA W DC/MD-10 SRM 51-31-01; VOL II. RECEIVE MATERIAL ID 7075-0, 0.050, PO 606256.5 IAW DAC DWG ARB 1261, REV IFOR THE FAB OF A NEW ANGLE. HEAT TREATED ANGLE IAW TPS 1003, REV A. ALODINED AND PRIMED THE NEW ANGLE IAW DC/MD-10 SRM 51-21-01; V OL II. PART MARKED THE ANGLE IAW DAC DWG ARB 1261, REV I AND FEDEX GMM 7-0-1000. INSTALLED THE NEW ANGLE IAW DC/MD-10 SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 20080717 WP 2008 7 17 08FDEA02033 1 20080529 A 5321 AGA386315 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 AFT PIT FLOOR PANEL 187 KF REQUIRES FAB NEW. FABRICATED A NEW PANEL 187 KF; POTTED EDGES; COMPLETED CURE AND SANDED EDG E POTTING; INSTALLED INSERTS; FABRICATED THE TOP SHEET; LAYED UP TOP SHEET UNDER A VAC BAG AND COMPLETED CURE; BACK DRI LLED AND COUNTER SUNK HOLES; APPLIED NON-SKID AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005 REV F AND 25-011 REC C. 2 L 7 3 4F RT A22WE 20080717 2008 7 17 ASAA0853061 4 20080619 A 2310 8220990004 TRANSCEIVER BOEING 737 737890 1384527 NM HF SYSTEM INOPERATIVE A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 559AS 5633 35178 HF2 COMM CIRCUIT BREAKER POPPED. NR 2 HF C/B REST BUT NR 2 HF TRANSCEIVER INOP. REMOVED AND REPLACED NR 2 HF TRANS PER MM 23 11 21 AND CONTACTED SFO RADIO, OPS CHECKS OK PER MM 23 11 00. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 08FDEA02004 1 20080528 A 5320 AGA70947 STANCHION DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 FORWARD CARGO COMPARTMENT: AFTER REMOVAL OF STA 6-73 AFT BULKHEAD PANEL FOR WIRING INSPECTION ACCESS FOUND X = 30 STANCH ION WITH CORROSION. CORRODED STANCHION AT FWD CARGO COMPARTMENT AFT BULKHEAD STA 6-73; X=30. REMOVED AS PER SRM 51-31- 01 VOL II. NEW STANCHION REWORKED AS PER DOUGLAS DWG AGA 7094 AND INSTALLED AS PER SRM 51-31-01 VOL II. REPAIR CLASSIF IED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 SWAA083262 1 20080613 A 3350 20131A BATTERY BOEING 737 7375H4 138449D NM CABIN FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT STAYS ON ALL THE TIME. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 08FDEA02209 1 20080610 A 5313 6518444 STRINGER BOEING 727 727227 1384078 NM BS 540-560 S28L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 FWD LOWER CARGO PIT, CORROSION ON STRINGER L28 BETWEEN FS 540 AND FS 560 CORROSION FOUND ON LOWER CARGO PIT STRINGER L28 BETWEEN FS 540 AND 560 WAS OUT OF LIMITS (EXFOLIATION). REMOVED DAMAGED SECTION OF STRINGER FROM 551-575 FS. FABRICAT ED, TREATED PRIMED PAINTED AND INSTALLED STRINGER SPLICE REPAIR REF SRM 53-10-3 FIG 1. THIS REPAIR IS CLASSIFIED AS A M AJOR REPAIR. 2 L 7 3 4F A3WE 20080717 EU 2008 7 17 08FDEA02217 1 20080611 A 5347 A53274005 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 MAIN DECK CARGO SEAT TRACK NR 6LT BETWEEN FR 21 AND FR 22 HAS 1 GOUGE ON SCALLOP, .25 IN DIA BY .020 IN DEEP REMOVED D AMAGED SECTION AND INSTALLED SEAT TRACK SPLICE REPAIR AT SEAT TRACK NR 6. LT BETWEEN FR 21 AND FR 22 IAW A310-200 SRM 5 3-10-16, FIG 208, SHT 2 2 L 7 2 4F RT A35EU 20080717 2008 7 17 SWAA083278 4 20080612 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080717 EU 2008 7 17 08FDEA02224 1 20080611 A 5347 A5381067620000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 THE CABIN SEAT TRACK HAS CORROSION AT FRAME 39; LBL 18. REMOVED THE CORROSION AND FOUND TO BE WITHIN LIMITS IAW A300-60 0 SRM 53-10-16; FIG 101. ORIGINAL MATERIAL 0.134. MATERIAL LOSS 0.020. MATERIAL REMAINING 0.114. ALODINED; PRIMED AN D TOPCOATED THE AREA IAW A300-600 SRM 51-23-10. 2 L 7 2 4F RT A35EU 20080717 NM 2008 7 17 SWAA083567 1 20080629 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 202WN 33999 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 08FDEA02364 1 20080620 A 5321 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU CABIN DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 MAIN CABIN FLOOR PANEL 251 BH IS DAMAGED. FABBED A NEW FLOOR PANEL 251 BH USING THE OLD PANEL AS A TEMPLATE; POTTED; CU RED AND SANDED EDGES; POTTED AND CURED INSERTS; APPLIED NON-SKID TAPE AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005, RE V F. 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 08FDEA02103 1 20080602 A 5100 NONE DOUG MD11 MD11F 3023600 NM IAW SRM NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 EXISTING DOUBLER REPAIR AT LEFT FUSELAGE APPROX STA 999 TO STA 979, STRINGER 41 TO 43. EXISTING DOUBLER REPAIR AT LEF T FUSELAGE APPROX STA 999 TO STA 979, STRINGER 41 TO 43 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-50-00 FIGURE 17 VOLUME I. FEDEX EO NR 1-5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG - MD11 - REPAIR CATALOG AND TRACKING RE QUIREMENTS, HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 EU 2008 7 18 08FDEA02172 1 20080606 A 5320 A53974279202 PROFILE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON LONGITUDINAL PROFILE C 63-64, Y140. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080718 WP 2008 7 18 08FDEA02248 1 20080612 A 2710 19697 PULLEY DOUG DC10 DC1030F 3023504 WP LT AILERONS CORRODED A FDEA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CE 21 301FE 46800 INTERMITTENTLY, THE LEFT OUTBOARD AILERON WILL NOT GO FULL DEFLECTION WHEN UNLOCKED. REMOVED AND REPLACED OB AILERON PU LLEY AT WRAP AROUND FOR CABLE RUNS 7G AND 8G AND PERFORMED ADJUSTMENT/TEST IAW AMM 27-10-00-5. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 08FDEA02251 1 20080613 A 5340 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 598FE 48597 MAIN DECK CARGO DOOR SPOOL FITTING NR 4 MOUNTING BOLT HOLES "B" AND "C" FOUND WITH CRACK FREE CONDITION AFTER REAMED TO MAXIMUM ALLOWABLE DIAMETER 0.52". MAIN DECK CARGO DOOR SPOOL FITTING NR 4 MOUNTING BOLT HOLES CARRIED OUT BUSHING REPAI R AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 EU 2008 7 18 2008UALA03344 1 20080612 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 432UA 587 EMERGENCY LIGHTS BITE TEST FAILS 3 RED SEAT PATHWAY LIGHTS AND LOWER EMERGENCY EXIT LIGHTED SIGN ON OPPOSITE SIDE DO NOT LIGHT UP. EPSU ON RT MID CABIN BENEATH EMERGENCY EXIT INDICATES UNIT FAULT. FOUND WIRE SHORTED UNDER SEAT 9ABC. WIRE STRANDS NOT DAMAGED. REPAIRED WIRE INSULATION, AND REPLACED 12WL POWER SUPPLY BLOWN BY SHORT. SYSTEM OP CHECK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20080718 EU 2008 7 18 08FDEA02147 1 20080604 A 5347 A53612518200 SEAT TRACK AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 719FD 388 MAIN CARGO SEAT TRACK EXFOLIATED FROM FR 14C TO FR 19 LBL 17 (YE). REMOVED AND REPLACED SEAT TRACK P/N A53612518200 IAW SRM 51-40-21 AND SRM 51-40-40. 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 2008UALA03454 1 20080618 A 2621 WARNING LIGHT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE COCKPIT ILLUMINATED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 224UA 30225 APU FIRE BOTTLE ARM AND BOTTLE DISCHARGE AMBER LIGHTS ON P40 PANEL INOP. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080718 NM 2008 7 18 SWAA083550 1 20080626 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 779, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 CALA0800514 1 20080601 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 BS 380 BETWEEN S8R & S9R IS CRACKED. REPAIRED CRACK PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 2008UALA02777 1 20080513 A 2560 D31591478U1 GIRT BAR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR LOOSE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 913UA 25291 DOOR 1L GIRT BAR LOOSE. *S/D* FOUND GIRT BAR LOOSE IN STOWED POS ON DOOR WHEN SLIDE UNARMED. ADJUSTED HOLDER FOR GIRT BAR ON DOOR. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080721 NM 2008 7 21 2008UALA02790 1 20080513 A 2120 285T00958 CIRCUIT CARD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE E&E BAY FAULTY A UALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 648UA 25285 FWD EQUIPMENT VAL EICAS MSG ON WHILE TAXIING OUT. SUSPECT EQUIPMENT COOLING CARD. REPLACED EQUIP COOL CARD IN P50 PNL M867, RAN ENGINES OPS NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080721 NM 2008 7 21 SWAA083495 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083507 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083525 1 20080625 A 5730 112A0002700 SKIN BOEING 737 7377H4 1384404 NM RT WING WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 DURING SCHEDULED 6Y CHECK, FOUND RT WING LOWER SKIN WORN OUTBOARD OF PYLON AFT END. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083526 1 20080625 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 465WN 33829 R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083536 1 20080625 A 5315 147A5504 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 771SA 27879 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 951, BL 0. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083651 1 20080701 A 5311 6546595 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED BS 727A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083653 1 20080701 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083802 1 20080713 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 460, STR 14L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080721 WP 2008 7 21 IXX2008F00000 1 20080712 A 2612 FIRE WARNING DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE NR 4 NACELLE FALSE ACTIVATION A IXXA O OTHER O OTHER NR NOT REPORTED 1 SW 11 830BX 45973 FLIGHT NR: ATN 229/ TAT 81724.7/ TAC 32713 - DURING CRUISE, NR 4 ENGINE FIRE WARNING CAME ON, THE CREW ACCOMPISHED CHEC K LIST AND RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. CORRECTIVE ACTION IN WORK. (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 20080721 CE 2008 7 21 GLB2008F00001 1 20080715 A 5320 1144300027179 ANGLE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA FS 288 CRACKED A GLBA O OTHER O OTHER NR NOT REPORTED 1 NM 21 192GL UE192 LT HEAVY ANGLE DOUBLER AT FS 288.0 CRACKED FWD OF BEND RADIUS APPROX 1.75 INCH IN LENGTH. MAINT REPAIRED LT HEAVY ANGLE DOUBLER AT FS 288 IAW SRM 53-90. REPAIR AREA APPROXIMATELY 13.5 INCHES LONG. RII INSPECTION COMPLIED WITH IAW TASKCAR D 8.2.1. (K) 2 L 7 2 4T 3 T RT A24CE E2NE 20080721 EA 2008 7 21 A6WA200840342 1 20080416 A 5344 HINGE CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 443AW 7781 CARGO DOOR STEP PLATE ONE HINGE CRACKED (FWD). CARGO DOOR STEP PLATE ONE HINGE (FWD) REPLACED IAW SRM 51-42-06. . 2 L 7 2 4F RT A21EA 20080721 NM 2008 7 21 SWAA083828 1 20080710 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 225WN 34333 DURING SCHEDULED HC2 CHECK, LT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080721 EA 2008 7 21 A6WA200840353 1 20080415 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA BS 325-334 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 13 443AW 7781 CRACK EXIST ON PASSENGER DOOR EDGE MEMBER. PAX DOOR CRACKS REPAIRED IAW REO 601R-52-11-279. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840367 1 20080421 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 13 441ZW 7777 BRACKET CRACK ON FS 280 LBL 9 ON FLOOR STRUCTURE. ON FS 280 LBL 9 ON FLOOR STRUCTURE (2) BRACKET REPLACED IAW SRM 51-4 2-21 AND SRM 51-42-06. (S) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840355 1 20080416 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 13 443AW 7781 BRACKET CRACKED ON BULKHEAD AT FS 621 WL 107 (CRACK LENGTH .500") BRACKET FABRICATED AS PER SAMPLE AND REPLACED AT FS 6 21 WL 107 IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA20840317 1 20080410 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 REPAIR CRACK IN PAX DOOR AT AFT EDGE MEMBER. PAX DOOR AT AFT EDGE MEMBER REPAIRED IAW CRJ 200 REO 601R-52-11-279. (A) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840414 1 20080510 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 442AW 7778 PAX DOOR MID STEP, AFT CORNER EDGE IS CRACKED. OPEN. (S) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840419 1 20080513 A 5420 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT NACELLE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 442AW 7778 CRACKED BRACKET ON RT NOSE INLET COWL APPROX 4 O`CLOCK POSITION. BRACKET FABRICATED IAW SRM 51-24-16 AND REPLACED IAW S RM 51-42-13. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840375 1 20080430 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 315-343 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 LOWER SILL ON PAX DOOR FS 315 AND 343 LBL 40 IS CORRODED. CORROSION REMOVED ON LOWER SILL OF PAX DOOR FS 315 ANDF FS 34 3 LBL 40 IAW SRM 51-21-06. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840421 1 20080514 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 324-349 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 442AW 7778 SERVICE DOOR LOWER SILL PLATE CORRODED. SILL PLATE ON SERVICE DOOR LOWER REPLACED IAW SRM 51-41-02. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840309 1 20080404 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 605 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 CARGO DOOR SILL CRACK AROUND RIVET FS 605 LBL 45. OPEN. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840310 1 20080408 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 FLOOR ANGLE CRACKED ON COCKPIT TO CABIN AT FS 280 LBL 9 TO RBL 9. - - FLOOR ANGLE AT FS 280.00 LBL 9 TO RBL 9 REPLACED IAW SRM 51-42-06 . . (A) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840387 1 20080501 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 REPAIR CRACK ON AFT OF PAX DOOR. REPAIR ON AFT SIDE OF PAX DOOR IAW REO 601R-52-11-279. (A) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840384 1 20080506 A 5710 PICCOLO TUBE CNDAIR CL600 CL6002B19 1900309 EA RT WING DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 RT WING INTERNAL OUTBOARD LEADING EDGE AT W/S 252, PICCOLLO TUBE DENTED (.300 X .200 X .040 DEEP). PICCOLLO TUBE REPLACE D IAW AMM TASK 30-11-41-400-801. (A) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840389 1 20080429 A 5320 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 523.60 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 HYD SUPPORT BRACKET CRACK IN RT MLG BAY AT FS 523 AND BTWN RBL 18 TO RBL 27. REPLACED IAW SRM 51-42-06. (A) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840397 1 20080504 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 317-349 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 SERVICE DOOR LOWER SILL PLATE CORRODED OVER LIMITS. SERVICE DOOR LOWER SILL PLATE REPLACED IAW SRM 51-41-02. (A) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840311 1 20080407 A 5344 HINGE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 PAX DOOR UPPER FOLDING STEP BOTTOM HINGE FOUND CRACKED FOUND NEAR FWD END. - - PAX DOOR FLODING STEP BOTTEM HINGE REPLA CED IAW SRM 51-41-02. .(A) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840395 1 20080429 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 574 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 CRACK EXISTS ON LOWER SILL OF CARGO DOOR FS 574 LBL 45 UNDER BRACKET. REPAIRED IAW REO 601R-53-61-1741. (A) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840394 1 20080428 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 REAR PRESSURE BULKHEAD CRACK AT LINTEL ATTACHMENT POINT. AFT PRESSURE BULKHEAD IN LINTEL FITTING AREA REPAIRED IAW REO 601R-53-61-1230 REV D. (A) 2 L 7 2 4F RT A21EA 20080721 EU 2008 7 21 08FDEA02862 1 20080714 A 3210 A5381077100195 FITTING AIRBUS 300 A300B4605R 3930308 EU ZONE 700 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 RIGHT MLG DOOR UPPER ACTUATOR ATTACH FITTING BRACKET IS GOUGE BY THE SEQUENCE VALVE. REMOVED DAMAGED FITTING IAW SRM 51- 41-21. LOCATED & DRILLED NEW FITTING P/N A5381077100195, PO 624364.1 IAW DWG A53810906. INSTALLED IAW DWG A53810906. LANDING GEAR FUNCTIONAL CHECK TO BE ACCOMPLISHED ON SNRM N00753. 2 L 7 2 4F RT A35EU 20080721 EU 2008 7 21 08FDEA02542 1 20080627 A 5310 B5327060401300 FLOOR PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 242 UJ IS CRACKED & CRUSHED. FABBED A NEW FLOOR PANEL; POTTED EDGES; CURED; SANDED; POTT ED INSERTS; APPLIED NON-SKID & PART MARKED IAW DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080721 NM 2008 7 21 SWAA083800 1 20080709 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED 18Y CHECK, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED AT OUTBOARD AUX TRACK CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 08FDEA02949 1 20080717 A 5754 651622198 WEB BOEING 727 727200 138407E NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 RIGHT WING O.B. L.E. NR 5 SLAT BN 279, CRACKED LWR. AFT INTERNAL WEB ANGLE AT INBD. SIDE OF ACTUATOR RAM ATACH STRUCTURE REMOVED ACCESS PANEL, INSPECTED FOR CRACKS, VERIFIED MATERIAL, FABRICATED, LOCATED AND DRILLED REPAIR PART. INSTALLED REPAIR, INSTALLED ACESS PANEL. REF SRM 51-30-2 PG 1-10. REF NDT MAN PART 6. 51-00-00 FIG 23, REF SRM 51-40-3 PG 1, REF SRM 51-10- 2 PG 1-10, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080721 EU 2008 7 21 08FDEA02950 1 20080717 A 4910 A5398939523400 ANGLE AIRBUS 300 A300B4622R 3930312 EU APU BULKHEAD CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 APU COMPARTMENT AFT BULKHEAD LOWER ANGLE IS CRACKED & BENT. REMOVED CRACKED ANGLE IAW SRM 51-40-21. LOCATED & DRILLED NEW ANGLE IAW SRM 51-72-10. INSTALLED THE ANGLE IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080721 NM 2008 7 21 SWAA083788 1 20080708 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 EU 2008 7 21 08FDEA02881 1 20080715 A 5730 A57111225200 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND TOOLMARK ON CENTER TANK TOP SKIN C 46, TRACK 1-2 LT REPAIR PERFROMED BY SMOOTH BLEND OUT AND NDT FOR CRACK FREE CO NDITION IAW. RAS 70507169/2008 ISS.A , APPROVED BY EA 6-5710-120053 2 L 7 2 4F RT A35EU 20080721 NM 2008 7 21 SWAA083774 1 20080709 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083781 1 20080708 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083730 1 20080706 A 3350 65C27093 SIGN BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 742SW 29278 R2 DOOR EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN ASSY PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083728 1 20080705 A 5754 6573714 SKIN BOEING 737 7373Q8 1384670 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED 22Y CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED AT AUX TRACK CUTOUT. REMOVED AND REPLACED SLAT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080916 EU 2008 9 16 08FDEA03169 1 20080730 A 5321 B5327060700400 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CABIN FLOOR PANEL NR 242 HK IS CRACKED. FABRICATED NEW FLOORBOARD NR 242 HK IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080916 NM 2008 9 16 08FDEA03460 1 20080817 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 DURING OPEN HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WIT H CRACK INDICATIONS AT HOLE A. MAIN CARGO DOOR LOWER JAMB CRACKED SUPPORT FITTING NR 3 REPAIRED AS PER SRM 53-50-00 FIG 10 VOL I . REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080916 NM 2008 9 16 08FDEA03461 1 20080817 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 DURING OPEN HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CR ACK INDICATIONS AT HOLES A, AND C. MAIN CARGO DOOR LOWER JAMB CRACKED SUPPORT FITTING NR 4 REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080916 NM 2008 9 16 08FDEA03182 1 20080730 A 5347 AEA7104521 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 MAIN DECK SEAT TRACK AT STA 755, X = 47.5 FOUND DAMAGED. MAIN DECK DAMAGED SEAT TRACK AT STA 755, X = 47.5 REPAIRED BY SECTIONAL SEAT TRACK. REPLACEMENT FROM STA 725 TO STA 765, X = 47.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLAS SIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 SWAA083604 1 20080629 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083616 1 20080629 A 5311 146A1133 FRAME BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 772SW 27880 DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 25L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 M7K2008F00009 1 20080512 A 5320 SUPPORT UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE FUSELAGE CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 818MH 1497 4131 23322 DURING ROUTINE INSPECTION OF THE DRIVE FLANGE A CAST PLASTIC SUPPORT BUTRESS WAS FOUND CRACKED. A NEW DRIVE FLANGE WAS INSTALLED. SUGGEST THAT THE ALTERNATE METAL DRIVE FLANGE BE USED INSTEAD OF THE PLASTIC DESIGN AS ONLY THE PLASTIC DRIV ES FAIL. THE WEIGHT OF THE PART SEEMS TO BE THE MFG PRIMARY CONSIDERATION IN THE SELECTION FOR THIS PARTS MATERIAL. (K ) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 EU 2008 7 18 M7K2008F00012 1 20080512 A 6220 350A31191700 STARFLEX UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE M/R HUB ASSY CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 815MH 1307 M2754 4022 23091 (REF 0213084022) DURING ROUTINE INSP, ADHESIVE BEAD FOR A STAR ARM END BUSHING WAS FOUND CRACKED. FURTHER EXAMINATION U TILIZING A SOAP WATER DETECTION METHOD REVEALED RELATIVE MOTION BETWEEN BUSHING & STAR ARM END. WITH ROTOR HUB SLEEVES R EMOVED BUSHING COULD BE MOVED MANUALLY. A SERVICEABLE REPLACEMENT STARFLEX WAS INSTALLED. THIS IS A DEFECT THAT RECENTL Y HAS BECOME MORE COMMON THAN IN THE PAST. SUGGEST A DIFFERENT ADHESIVE BE UTILIZED OR THE STAR ARM ENDS AND BUSHINGS BE DESIGNED TO HAVE A LARGER ADHESIVE BONDING SURFACE SUCH AS ADDING INNER BUSHING AND OUTER STAR ARM END SPLINING. THERE WAS NO EVIDENCE OF ANY IMMINENT FAILURE FOR THE PART OR EXCESSIVE PLAY DEVELOPMENT OF THE BUSHING. SUGGEST THAT THE APP 1 G 7 2 3U 3 U H9EU E00054EN 20080718 NM 2008 7 18 SWAA083491 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083497 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 EA 2008 7 18 A6WA200840446 1 20080523 A 5753 PLATE CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 GOUGE FOUND ON AFT HINGE LOG PLATE OF LT INBOARD FLAP. GOUGE REMOVED IAW REO 601R-57-1343. (A) 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840408 1 20080509 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 442AW 7778 RT FS 280 RBL 8 & 10 ANGLE ON BEAM FOUND CRACKED. RT FS 280 RBL 8 & 10 ANGLE ON BEAM REPLACED IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840410 1 20080510 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 442AW 7778 CRACK EXISTS ON INTERCOSTAL FS 484 LBL 36. DAMAGED ATTACHMENT FLANGE CUTOUT, EDDY CURRENT PERFORMED AND NEW SERVICEABLE ANGLE INSTALLED IAW REO 601R-53-41-059 REV A. 2 L 7 2 4F RT A21EA 20080718 EU 2008 7 18 M7K2008F00030 1 20080512 A 6720 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE FAILED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 806MH 385 3833 23220 A FAULT CODE WAS GENERATED ON SHUTDOWN INDICATING A DEFECT OF COLLECTIVE POTENTIOMETER. A NEW PART WAS INSTALLED, NO FU RTHER FAULT WAS DETECTED. THIS IS RECURRING FAILURE FOR THIS PART WHICH HAS EFFECTED DISPATCH RELIABILITY FOR THIS MODE L HELICOPTER. SUGGEST AN ALTERATION OF FAULT SENSING SOFTWARE TO REDUCE FAULT SENSITIVITY TO PERHAPS A SIGNAL LOSS OF 0 .5 SECOND RATHER THAN 1/20TH OF A SECOND. AN OPTIC RATHER THAN A RESISTANCE BASED SENSOR SHOULD BE CONSIDERED AS CONTAC T POINT IS DAMAGED BY AC VIBRATION WHEN AC POWER SETTINGS ARE SET FOR CRUISE FLIGHT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080721 WP 2008 7 21 UPS08852414 1 20080529 A 5322 SHEAR TIE DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 LARGE SHEAR TIE CRACKED IN RADIUS, 60 COMARTMENT CEILING, STA 1800 L4R. STOP DRILLED, FABBED AND INS TALLED REPAIR ANGLE IAW, SRM 51-1-21, 53-2 -0, 51-1-8, 53-5-03, 51-1-20D. 2 L 7 4 4F RT 4A25 20080721 NE 2008 7 21 UPS08852422 2 20080603 A 7314 PUMP DOUG DC8 DC873F 302199F WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE MALFUNCTIONED A IPXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 SO 01 894UP 46094 692196 INSPECTION TYPE:N/A AT FLT F/L 36.0 WITH BOOST OFF NR 2 ENGINE FLAMED OUT WHEN THROTTLE WAS MOVED TO IDLE. THIS WAS DUR ING A CONDITION FLT WITH A NEW PROCEDURE THAT THE FLT CREWS ARE FOLLOWING. A/C WAS NOT IN NORMAL FLT CONDITION WHEN THE FLAME OUT OCCURRED. REMOVED NR 2 ENG FUEL BOOST PUMP IAW MM 73-10-01-2. INSTALLED NR 2 ENG FUEL BOOST PUMP IAW MM 73- 10-01-2. REQUIRES LEAK AND OPS CHECK VERIFIED VSV STATIC RIG. CHECKS GOOD. PERFORMED ENGINE RUN REF MM 71-00-00-1 AND 71-00-00-5. ENG RUN OPS GOOD. 2 L 7 4 4F 4 F RT 4A25 1E8 20080721 WP 2008 7 21 UPS08852432 1 20080531 A 5230 SKIN DOUG DC8 DC873F 302199F WP CARGO DOOR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 C-PIT CROSS SLIDE DOOR INTERIOR SKIN IS GOUGED, FWD LWR AREA. FABBED AND INSTALLED REPAIR DOUBLER IA W SRM, 51-1-8, 51-1-21, 52-2-0 FIG 2. 2 L 7 4 4F RT 4A25 20080721 NM 2008 7 21 SWAA083650 1 20080701 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED BS 706, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083734 1 20080706 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 2008UALA02691 1 20080509 A 3510 MC1025154 OXYGEN MASK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 374UA 24639 F/O O2 MASK HAS BROKEN LEVER ON FRONT OF MASK. SUSPECT PRE FLIGHT CHECKS. REPLACED FIRST OFFICERS OXYGEN MASK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080721 NM 2008 7 21 SWAA083524 1 20080625 A 3350 65C27093 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 387SW 26602 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083646 1 20080701 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080721 EA 2008 7 21 A6WA200840340 1 20080416 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 443AW 7781 CRACK FOUND AT FS 484 RBL 36 WL 72. - - INTERCOSTAL REPAIRED AT FS 484, RBL 36, WL 72 IAW REO 601R-53-41-059 REV A. (S) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840369 1 20080421 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 13 441ZW 7777 REAR PRESSURE BULKHEAD CRACKED AROUND LINTER FITTING ATTACHMENT POINT. REPAIRED IAW CRJ 200 REO 601R-53-61-1230 REV D. (S) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840360 1 20080423 A 5210 SEAL CNDAIR CL600 CL6002B19 1900309 EA PAX SEAL LEAKING A A6WA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 13 450AW 7823 AT 8,000 FT HIGH PITCH WHISTLE FROM PASSENGER DOOR, FLIGHT ATTENDANT REPORTS CURTAIN SUCKED TO THE DOOR, PRESSURIZATION INDICATED 3,000 FT CLIMB, RETURNED TO MHT. R&R PAX DOOR SEAL IAW 52-11-10. OPS CHECK GOOD. PRESSURIZATION CHECK GOOD. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840312 1 20080409 A 5753 SKIN CNDAIR CL600 CL6002B19 1900309 EA TE FLAP DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 DENT ON RT OUTBOARD WING FLAP. RT OUTBOARD WING FLAP REPAIRED IAW SRM 57-53-00 FIG 202 SHEET 2 REPAIR 3. (A) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840388 1 20080429 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 202.75 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 CRACK EXISTS ON FS 202 AT LBL 23 PRESSURE BULKHEAD AROUND PARKING BRAKE CABLE. REPAIR PERFORMED ON FS 202.75 LBL 23.72 P RESSURE BULKHEAD AROUND PARKING BRAKE IAW REO 601R-53-11-563. (A) 2 L 7 2 4F RT A21EA 20080716 NM 2008 7 16 SB08036 1 20080528 A 7797 CA14900 HARNESS BOEING 737 737401 1384701 NM NR 2 ENGINE FAULTY A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 405US 23885 BWI - FLT 956 - EN ROUTE FROM CLT TO BOS, AT FL350, CREW RECEIVED A NR 2 ENGINE EGT INDICATION OF 1,200 DEGREES CELCIUS FOR APPROXIMATELY 3 SECONDS. CREW THROTTLED BACK NR 2 ENGINE TO IDLE AND EGT RETURNED TO NORMAL, MATCHING THE OTHER ENG INE AT IDLE. ALL OTHER PARAMETERS WERE NORMAL AT TIME OF INCIDENT. HIGH EGT RED LIGHT CAME ON AND WENT OUT AT APPROPRI ATE EGT. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE REMOVED A ND REPLACED THE THERMOCOUPLE INTERFACE HARNESS AND CLEANED CONNECTORS IN THERMOCOUPLE CIRCUIT ON ENGINE AND PYLON. ACCO MPLISHED ENGINE RUN. ALL PARAMETERS NORMAL. 2 L 7 2 4F RT A16WE 20080716 EA 2008 7 16 SWIA200819704 1 20080529 A 3350 PRINTED CKT BOAR CNDAIR CL600 CL6002C10 1390015 EA CABIN DEFECTIVE A SWIA O OTHER O OTHER UK UNKNOWN 1 NM 07 758SK 10222 EMERGENCY LIGHTS CYCLE ON AND OFF INTERMITTENTLY. REPLACED PRINTED CIRCUIT CARD IN JB11 IAW CRJ 700 MM 24-06-11. OPS C HECK GOOD. 2 L 7 2 4F RT A21EA 20080716 NM 2008 7 16 KCSA081271 1 20080603 A 5411 FRAME BOEING 747 747212B 1384886 NM NR 1 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 NR 1 PYLON REAR ENG MOUNT BULKHEAD AFT I/B FRAME EDGE CRACKED AT NAC STA 221.9. 2 L 7 4 4F RT A20WE 20080716 NM 2008 7 16 DHLA200800051 1 20080603 A 3350 LIGHT BOEING 727 727200 138407E NM CABIN INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 GL 05 749DH 22013 FLT 119 - DURING PREFLIGHT STBY POWER CHECK, L1 EXIT DOOR EMERGENCY LIGHT FAILED TO ILLUMINATE. CLEANED & RESEATED EMER GENCY FWD ENTRY LIGHT ASSY & PERF OPS CK IAW AOM 1.3, PG 7, SYS OPS CHECK GOOD. AIRCRAFT WAS GROUNDED. 2 L 7 3 4F RT A3WE 20080717 NM 2008 7 17 UPS08B52559 1 20080417 A 5311 65B09631612 TENSION TIE BOEING 747 747400 13848AT NM BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:BCF BS1180 TENSION TIE LT AFT SIDE CRACKED. BS 1180 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201. 2 L 7 4 4F RT A20WE 20080717 NM 2008 7 17 UPS08B52560 1 20080417 A 5311 65B09631610 TENSION TIE BOEING 747 747400 13848AT NM BS 1140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:BCF BS 1140 TENSION TIE RT AFT SIDE FOUND CRACK. BS 1140 TENSION TIE REPAIRED PER SRM 53-40-30 FIG 201. 2 L 7 4 4F RT A20WE 20080717 NM 2008 7 17 UPS08B52561 1 20080417 A 5311 65B09631612 TENSION TIE BOEING 747 747400 13848AT NM BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:BCF BS1180 TENSION TIE LT FWD SIDE CRACKED. BS 1180 TENSION TIE REPAIRED PER SRM 53-40-31 FIG 201. 2 L 7 4 4F RT A20WE 20080717 SO 2008 7 17 FDKA200805205 1 20080522 A 5320 14525480603 THRESHOLD EMB 145 EMB145LR 3260212 SO CARGO DOORWAY CORRODED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 THE CARGO DOOR THRESHOLD IS CORRODED OUT OF LIMITS. THE CORRODED PART HAS BEEN REMOVED AND REPLACED. 2 L 7 2 4T RT T00011AT 20080717 NM 2008 7 17 CALA0800537 1 20080603 A 5315 147A5506 FLOORBEAM BOEING 737 737724 13844BY NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13716 28787 STATION 986.5 FLOORBEAM HAS CORROSION ON UPPER CHORD RBL 23 FWD FLANGE AT PREVIOUS REPAIR. REMOVED AND REPLACED REPAIR FILLER PER SRM 53-00-51 REPAIR 1. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 USAA920081163 1 20080424 A 5311 652072354 FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 514AU 23700 MCN - MAJOR REPAIR - LEASE RETURN - CRACKED FRAME, BS 492, S24R. REPLACED FRAME, BS 492, S24R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080717 SO 2008 7 17 FDKA200806215 1 20080602 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 833MJ 145327 FDM 6181 JFK-CVG. ROW 12 FWD OVERHEAD LIGHT INOP. MX REMOVED AND REPLACED THE LIGHT. 2 L 7 2 4T RT T00011AT 20080717 NM 2008 7 17 SWAA083365 1 20080618 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 16 TO RBL 37. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843036 1 20080607 A 5344 3030301 HINGE BOEING 737 7374Q8 138447Q NM L1 DOOR WORN A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 769AS 647 25103 FA REPORTS L1 IS DIFFICULT TO MOVE OPEN AND CLOSED OPERATED L 1 DOOR AND HEARD AND FELT GRINDING POPPING EMANATING FROM UPPER END OF FUSE TORQUE TUBE INITIATED MIG 2C 224114. WITH FURTHER TROUBLESHOOTING REMOVED L1 DOOR CAM PLATE AND FOUND WORM AREA ON PLATE. ALSO FOUND CRANK ASSEMBLY ROLLER BAD. REMOVED AND REPLACED CRANK ASSEMBLY ROLLER AND CAM PLATE IA W OHM 52 16 01. ASSEMBLED L 1 DOOR IAW AMM 52 11 31. ACCOMPLISHED L 1 FORWARD DOOR OPERATIONAL TEST IAW AMM 52 11 00. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083329 1 20080618 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843029 1 20080514 A 5754 WEDGE BOEING 737 737490 1384715 NM NR 4 SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 RIGHT WING NR 4 SLAT TRAILING EDGE WEDGE LOWER SURFACE CHAFED THROUGH IN TWO PLACES ON AFT EDGE ONE EACH AT INBOARD AREA AND 1 EACH AT ACTUATOR AREA. PREPARED DAMAGED AREA. FABRICATED FILLERS AND DOUBLERS AND BONDED IAW B737 400 SRM 51 70 10 REPAIR NR 4. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843024 1 20080514 A 5753 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 LEFT WING OUTBOARD AFT FLAP HAS 3 EACH DENTS ON LOWER SURFACE 9 INCHES FROM INBOARD END AND 4 INCHES FROM TRAILING EDGE. PREPARED DAMAGED AREA FABRICATED DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083347 1 20080618 A 5311 6545815 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 689SW 23387 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 344, STR 22L. REPAIRED FRAME PER EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083345 1 20080618 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 795SW 30606 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083211 1 20080612 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083212 1 20080612 A 5322 6546536 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 540, STR 18L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083220 1 20080612 A 5330 655298871 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 976, STR 22L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083078 1 20080608 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083102 1 20080607 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 473WN 33832 DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS CRACKED AT ROW 4 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083089 1 20080608 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080916 NM 2008 9 16 08FDEA03184 1 20080730 A 5347 AEA75321 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 MAIN DECK SEAT TRACK AT STA 1481, X = 8 FOUND CORROSION. MAIN DECK CORRODED SEAT TRACK AT STA 1481, X = 8 REPAIRED BY S ECTIONAL SEAT TRACK REPLACEMENT FROM STA 1471 TO STA 1531, X = 8 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFI ED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080916 WP 2008 9 16 08FDEA02863 1 20080714 A 5730 ARB1231503 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING FIXED L/E IS CRACKED AT THE INBD OF SLAT DRIVE MECHANISM ACCESS PANEL. CUT OUT CRACKED AREA AND FABRICATED A DOUBLER AND FILLER IAW SRM 57-10-00; FIG 68; VOL I. ALODINED AND PRIMED THE DOUBLER AND FILLER IAW SRM 51-21-01; VOL II ; PGS 21-24. INSTALLED THE DOUBLER AND FILLER IAW SRM 51-33-01; VOL II. 2 L 7 3 4F RT A22WE 20080916 EU 2008 9 16 08FDEA03470 1 20080818 A 5712 A57240457 RIB AIRBUS 300 A300B4622R 3930312 EU LT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CHAFING MARKS ON LT WING TRAILING EDGE STRUCTURE RIB 6A-6B. REPAIR PERFORMED BY REWORK OF CHAFING MARK AT RIB 6A AND NDT FOR CRACK FREE CONDITION AND REWORK CHAFING MARK AT INTERMEDIATE RIB WITH INSTALLING A NEW RUBBING PLATE IAW R AS/BAE/1007587/2008 ISS A, APPROVED BY EA 6-5751-123012. 2 L 7 2 4F RT A35EU 20080916 EU 2008 9 16 08FDEA03471 1 20080818 A 5311 A53970868201 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CRACK IN FRAME C 56 RT AT STRINGER P 22 RT. REPAIR PERFORMED IAW R539-71112 AND INSTALLING A REPAIR T-PROFILE IAW . RAS/EFW/9000062/2008 ISS C, APPROVED BY EA 6-5316-123030 A. 2 L 7 2 4F RT A35EU 20080916 WP 2008 9 16 08FDEA03030 1 20080723 A 5414 AUB70543 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 NR 1 PYLON PANEL 437 DOOR SKIN IS CRACKED AT A FASTENER HOLE. 3 1 PYLON PANEL 437 DOOR WAS REPLACED ON N/R N00808. SEE SDR TRACKING NR 08-3031 FOR THE DETAILED INFORMATION. 2 L 7 3 4F RT A22WE 20080916 WP 2008 9 16 08FDEA03711 1 20080902 A 5710 ARC072419 CAP DOUG MD10 MD1010F 3022112 WP LT WING WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING LOWER T/E STRUCTURE IS WORN APPROXIMATELY 48" INBD OF THE OUTBD AILERON ACTUATOR. UPON FURTHER INVESTIGATIO NDAC DWG ARC 0824; REV "H" ALLOWS THE TRIMMING OF THE FLANGE IN THE WORN ARE. TRIMMED AREA FLANGE IAW DWG ARC 0724; REV "H"; E.O. SHEET 2. ALODINED, PRIMED, & PAINTED AREA IAW DC/MD-10 SRM 51-21-01; VOL II. 2 L 7 3 4F RT A22WE 20080917 NM 2008 9 17 08FDEA03512 1 20080820 A 5730 ARB74024 SKIN DOUG MD11 MD11 3023602 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 11 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWE EN STA XORS= 690 AND STA XORS= 700. 11 EACH FASTENER HOLES CRACK AT RT WING LOWER SKIN ACCESS. REPAIR CARRIED OUT AS PER EA 1-5710-122425A, THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 SWAA084797 1 20080828 A 5330 6545800 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 2008UALA04356 1 20080820 A 3350 2012120131A POWER SUPPLY BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 202UA 24717 EMERGENCY EXIT LIGHT OVER DOOR 2L STAY ON WITH LIGHTS OFF. *S/D* REPLACED POWER SUPPLY & BATTERY. CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20080918 NM 2008 9 18 2008UALA04175 1 20080808 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 814UA 862 FLOORBEAM 80 CORRODED (MARKED). *S/D* REMOVED FASTENERS FROM FWD SPLICE. ASSEMBLED BEAM 80. INSTALLED FASTENERS IN S PLICE AND LATERAL BEAM CONNECTIONS. BEAM COMPLETED & INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080918 NM 2008 9 18 2008UALA04108 1 20080803 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU ROW 16 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 327UA 24147 EEL LIGHTS ARE INOP FROM ROW 16 AFT. *S/D* REMOVED & REPLACED EEL LIGHTS FROM ROW 16 AFT. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20080918 NM 2008 9 18 2008UALA04119 1 20080801 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 4E MISSING A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 AFT EMERGENCY LIGHT PLATE IS MISSING AT SEAT 4E. *S/D* REPLACED LIGHT ASSEMBLY. OPS CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 NM 2008 9 18 UPS08553204 1 20080813 A 5410 SUPPORT BOEING 757 75724APF 1384969 NM NR 2 NACELLE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 NR 2 ENGINE STRUT LT NAC STA 136 WL 161.70 O/B SUPPORT FOR PANEL 441AT IS CHAFED. REMOVED, FABRICATE D AND INSTALLED SPLICE PLATE PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20080918 NM 2008 9 18 ASAA0843417 1 20080811 A 5414 314A10206 SKIN BOEING 737 7374Q8 138447Q NM RT NACELLE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 RT ENGINE INLET COWL LIP SKIN AT 6 O'CLOCK POSITION MULTIPLE SCRATCHES. REPAIRED IAW GRO8617 AND EA. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 SWAA084817 1 20080901 A 5315 149A5504 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 11 TO RBL 36.5. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083285 1 20080614 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 FWD CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080717 WP 2008 7 17 08FDEA02032 1 20080529 A 5321 AGA38643 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 AFT PIT FLOOR PANEL 187 JF REQUIRES FAB NEW. FABRICATED NEW FLOOR PANEL 187 JF; POTTED EDGES; COMPLETED CURE AND SANDED EDGES; INSTALLED INSERTS; FABRICATED TOP SHEET; LAYED UP UNDER VAC BAG; COMPLETED CURE; BACK DRILLED AND COUNTERSUNK H OLES; APPLIED NON-SKID AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005, REV F AND 25-011, REV C. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 ASAA0853110 1 20080629 A 3040 8300005604 CONTROLLER BOEING 737 737890 1384527 NM WINDOW HEAT FAULTED A ASAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 02 558AS 7734 35177 RT SIDE WINDOW HT OVERHEAT LT ILLUMINATED COMPLETED QRHPROCEDURE OPS NORMAL REMAINDER OF FLT PERFORMED WINDOW HEAT SYS OPS TEST PER MM 30 41 00 SYSTEM CHECK GOOD. 2 L 7 2 4F RT A16WE 20080717 SO 2008 7 17 SWIA200819805 1 20080620 A 5210 DOOR EMB 120 EMB120ER 3260203 SO MAIN PAX BINDING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 291SW 120318 FLT 5423 - FLIGHT ATTENDANT REPORTS THAT THE CABIN DOOR IS VERY DIFFICULT TO OPEN AND CLOSE. ADJUSTED LOWER AFT SHIM ST ACK. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080717 NM 2008 7 17 ASAA0843063 1 20080607 A 5521 SPAR BOEING 737 7374Q8 138447Q NM RT ELEVATOR PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 RIGHT ELEVATOR HAS PUNCTURE HOLE IN FORWARD SPAR. REMOVED DAMAGED ELEVATOR. INSTALLED REPLACEMENT ELEVATOR IAW B737 AM M 27 31 11 004 027 27 31 11 404 025. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 08FDEA02098 1 20080602 A 5100 NONE DOUG MD11 MD11F 3023600 NM REPAIRED PER SRM NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 EXISTING DOUBLER REPAIR AT RIGHT FUSELAGE APPROX STA 1019 TO STA 1039, STRINGER 40 TO 43. EXISTING DOUBLER REPAIR AT RI GHT FUSELAGE APPROX STA 1019 TO STA 1039, STRINGER 40 TO 43 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-20 -00 FIGURE 10 VOLUME I. FEDEX EO NR 1-5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG - MD11 - REPAIR CATALOG AND TRACKING REQUIREMENTS, HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 SWAA083268 1 20080617 A 5320 6517853 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7, WL 180. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083272 1 20080614 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 637SW 27710 R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080717 EU 2008 7 17 08FDEA02204 1 20080609 A 5310 A5398111320051 SHEAR WEB AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 LEFT FLOOR STRINGER SHEAR WEB IS CRACKED JUST AFT OF FRAME 79 A; AT THE MAIN CARGO DECK FLOOR LEVEL REMOVED AND REPLACED WITH A NEW WEB IAW SRM 51-40-21; PG 7. 2 L 7 2 4F RT A35EU 20080717 NM 2008 7 17 SWAA083273 1 20080612 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 649SW 27719 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT CRACKED AT INBOARD END. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 2008 7 17 SWAA083314 4 20080617 A 2565 D31354433 SLIDE BOEING 737 7373Q8 1384670 NM R2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPL ACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 08FDEA02218 1 20080611 A 5320 6519606 FLOOR SUPPORT BOEING 727 727227 1384078 NM BS 1140-1146 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 MAIN DECK BS 1140-1146 RBL 11-12 WL 208 FLOOR SUPPORT "T" HAS CORROSION ON UPPER AND LOWER SURFACES OF I/B FLANGE. REMO VED CORROSION, ORIGINAL "T" .080, REMOVED .025, REMAINING .055 - OUT OF LIMITS REF SRM 51-10-1. REMOVED OLD SUPPORT BEA M, FABRICATED, HEAT TREATED, TREATED AND PRIMED, INSTALLED ON AIRCRAFT REF GMM 7-0-1001, SRM 51-10-2 AND SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080717 EU 2008 7 17 08FDEA02225 1 20080611 A 5347 A5381067620000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 THE CABIN SEAT TRACK HAS CORROSION AT FRAME 39; LBL 18. THIS SDR WAS GENERATED IN ERROR. FOR DETAILED INFORMATION SEE SDR TRACKING NUMBER 08-2224. REMOVED THE CORROSION AND FOUND TO BE WITHIN LIMITS IAW A300-600 SRM 53-10-16; FIG 101. O RIGINAL MATERIAL 0.134. MATERIAL LOSS 0.020. MATERIAL REMAINING 0.114. ALODINED; PRIMED AND TOPCOATED THE AREA IAW A3 00-600 SRM 51-23-10. 2 L 7 2 4F RT A35EU 20080717 2008 7 17 SWAA083294 4 20080616 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 918WN 29843 L2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080717 2008 7 17 SWAA083154 4 20080610 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 286WN 32471 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083155 1 20080610 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 14L CRACKED AT BS 727B. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 2008UALA04315 1 20080816 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1400 S26-27L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 AFT PIT STA 1400 BETWEEN STR 27L AND 26L, FRAME IS DENTED. *S/D* MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & INSTALLE D DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NM 2008 9 18 2008UALA04144 1 20080805 A 5320 WEB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 246 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 CABIN STA 246, RBL 26, WEB CRACKED. *S/D* MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF WEB. FABRICATED & IN STALLED A REPLACEMENT WEB SECTION, 2EA DOUBLERS, TAPERED FILLER & A STIFFENER. 2 L 7 2 4F 4 F RT A1NM E24NE 20080918 NM 2008 9 18 2008UALA04147 1 20080805 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 588UA 26717 NR 3 LEFT MAIN ENTRY DOOR EXT EVACUATION LIGHT INOP. *S/D* BULBS INOP. REPLACED BULBS, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NE 2008 9 18 2008UALA05395 2 20080822 A 7261 CARBON SEAL BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE LT ENGINE LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 218UA 30222 LT ENG LEAKING OIL. FOUND DRAIN LINE 10 LEAKING PAST LIMITS. REPLACED LEFT ENG IDG AND CARBON SEAL MM 24-11-11-01 AND 72-61-04. ACP ENG RUN AND LEAK CHECK, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080919 NM 2008 9 19 SWAA084848 1 20080903 A 5310 6547980 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 817 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 817, LBL 67. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084850 1 20080903 A 3320 412A1150 LIGHT BOEING 737 7377H4 1384404 NM ROW 18 DEF OVERHEATED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 433LV 33716 DIVERSION, FLIGHT CREW REPORTED STRONG ELECTRICAL BURNING ODOR. INSPECTED AND FOUND OVERHEATED LIGHT ASSY AT ROW 18 DEF . REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084851 1 20080903 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 807 S25-26R DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 610WN 27696 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CREASED AT BS 807, BETWEEN STR 25R AND STR 26R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084961 1 20080908 A 2560 35500003 GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED 8Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIPS WORN IN LT MID CABIN. REMOVED AND REPLACED STRIPS PER MM . 2 L 7 2 4F RT A16WE 20080919 EA 2008 9 19 COMA086370 1 20080829 A 3231 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 915CA 29622 7013 AFTER T/O FROM JFK RECEIVED NOSE WHEEL DOOR OPEN MSG. EMERGENCY DECLARED. ACFT RETURNED BACK TO JFK AND LANDED SAFELY. R&R NLG DOOR SELECTOR VALVE. 2 L 7 2 4F RT A21EA 20080919 EA 2008 9 19 COMA086371 1 20080829 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 349 S16-17L DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 420CA 7451 PAX DOOR CUTOUT AIRFRAME SIDE AFT LOWER CORNER SKIN DAMAGED. PERFORMED REPAIR AT STA 349 STR 16L AND 17L PER CRJ REO 60 1R-53-00-030 REV D. 2 L 7 2 4F RT A21EA 20080919 NM 2008 9 19 SWAA084824 1 20080901 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 289CT 36633 DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084825 1 20080902 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 520 S12L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 12L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084826 1 20080902 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 440-500 S26L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER 26L CORRODED AT BS 440 TO BS 500. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084853 1 20080903 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM BS 380 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0853469 1 20080901 A 4990 41310203 OIL FILTER BOEING 737 737890 1384527 NM APU MALFUNCTIONED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 559AS P7222 35178 WHILE ACCOMPLISHING TC 78349013 FOUND APU OIL FILTER DELTA P INDICATOR POPPED. REMOVED AND REPLACED APU OIL FILTER ELEM ENT NO CONTAMINATION NOTED. RESET DELTA P INDICATOR. INSPECTED MAGNETIC DRAIN PLUG NO CONTAMINATION NOTED. REF AMM'S 49 91 13 & 49 91 81. LEAK CHECK GOOD. RAN APU FIVE MINUTES, OPS CHECK GOOD REF AMM 49 91 13. 2 L 7 2 4F RT A16WE 20080919 EU 2008 9 19 USAA920081622 1 20080827 A 5540 D5537131800000 FITTING AIRBUS 320 A320232 3930326 EU RUDDER HINGE WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 660AW 1234 SAL - BC6 MAJOR REPAIR EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 2. REPLACED RUDDER HINGE FITTING NR 2 IAW A320 AMM 55- 36-41. 2 L 7 2 4F RT A28NM 20080721 NM 2008 7 21 SWAA083508 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083519 1 20080625 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER 11R CRACKED AT BS 355. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083527 1 20080625 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083531 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083648 1 20080701 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083619 1 20080630 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20080721 WP 2008 7 21 I5H2008F00000 1 20080405 A 3250 10150 ACTUATOR CVAC 340 34031 2422704 WP ALLSN 501D 501D13 03004 GL NLG STEERING DAMAGED A I5HA O OTHER O OTHER NR NOT REPORTED 1 GL 25 581P 29 DURING A STORM, ON APR 6,2008, A CARGO CAN (ULB) WAS THROWN INTO THE RT SIDE. THE RT PROP WAS ALSO STRUCK A GLANCING BL OW. THERE WAS SIGNIFICANT DAMAGE TO THE SKIN AND SUPPORT STRUCTURE BENEATH THE SKIN. THERE WAS DAMAGE TO WIRING IN THE AREA. THE NOSE STEERING ACTUATOR WAS ALSO DAMAGED. DAMAGE AREA WAS BETWEEN FUSELAGE STA 72 TO 125 AT APPROXIMATELY BET WEEN STRINGERS 11 AND 3. THE PROPELLER AND REDUCTION GEARBOX WERE REMOVED AND INSPECTED. NO DAMAGE TO EITHER. AC WAS REPAIRED AND THE AC TEST FLOWN ON JULY 3, 2008. THE AC WAS RETURNED TO SERVICE JULY 8, 2008. SDR IS OPEN PENDING RECEI PT OF ADDITIONAL PN. (K) 2 L 7 2 4R 4 T 6A6 E282 20080721 NM 2008 7 21 SWAA083733 1 20080706 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 305, WL 257.88, L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083803 1 20080713 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727D, STR 14R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083829 1 20080711 A 3350 8210248801 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 251WN 32510 AFT CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080721 EA 2008 7 21 A6WA200840344 1 20080412 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 443AW 7781 CRACK FOUND ON FRAME FS 280 RBL 9 WL 73. FRAME AT FS 280, RBL 9, WL 73 REPAIRED IAW RWO 601R-53-11-171 REV "D" SCHEME " B". . 2 L 7 2 4F RT A21EA 20080721 NM 2008 7 21 SWAA083827 1 20080710 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 225WN 34333 DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20080721 EA 2008 7 21 A6WA200840299 1 20080407 A 2697 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA FIRE LOOP LOOSE A A6WA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 31 462AW 7875 INTERMITTENT MLG BAY OVERHEAT FAULT THEN MLG BAY OVER HEAT INDICATION DIVERTED TO SCE. BRAKE TEMPS INDICATED NORMAL AT A LL TIMES (01 ON ALL FOUR). SECURED LOOSE CONNECTION ON RT MLG BAY FIRELOOP. REPAIRED BROKEN CONNECTION ON LT MLG FIRELO OP. COMPLIED WITH FUNCTION TEST IAW AMM 26-14-00 PARA B (1) AND (2) FAULTS. (A) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840313 1 20080402 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA BS 625 GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 GOUGE FOUND ON VERTICAL Z MEMBER AT FS 625 BL 0 WL 136. - - VERTICAL 2 MEMBER AT FS 625 BL O WL 136 REPAIRED IAW REO 601 R-53-61-2573. . (A) 2 L 7 2 4F RT A21EA 20080721 EU 2008 7 21 08FDEA02911 1 20080716 A 5310 A53974267202 STRINGER AIRBUS A300 A300F4622R 3930360 EU ZONE 100 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON STRINGER P 56 LT, C59-62 STRINGER REPAIR PERFORMED IAW. SRM 53-10-14 FIG. 201A. 2 L 7 2 4F RT A35EU 20080717 NM 2008 7 17 SWAA083168 1 20080610 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083169 1 20080610 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080729 EU 2008 7 29 USAA920081254 1 20080616 A 5321 D5367527700400 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 679AW 2613 SAL - BC-02 - MAJOR REPAIR - FLOOR PANEL HAS 14 INCH AREA DELAMINATED AT FR 52 - 56, BL Y765 TO Y-165. REPLACED FLOOR P ANEL AT FR 52 - 56, BL Y765 TO Y-765. (S) 2 L 7 2 4F RT A28NM 20080729 NM 2008 7 29 USAA920081265 1 20080624 A 3397 SPLICE BOEING 737 7373G7 1384595 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 306AW 24633 FLT 550 - PHX - EEL - EMERGENCY EXIT LIGHTS AT SEAT ROW 2 ARE INOP. MAINTENANCE REPLACED WIRE SPLICE. OPERATIONAL CHEC K WAS GOOD. (S) 2 L 7 2 4F RT A16WE 20080729 EU 2008 7 29 USAA920081268 1 20080624 A 2560 P070003001 FLASHLIGHT AIRBUS 320 A320232 3930326 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 669AW 1792 FLT 376 SMF - PHL - EMERGENCY EQUIPMENT - AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT F/A FLASHLIGHT. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080729 NM 2008 7 29 USAASB08045 1 20080629 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 440US 24811 CLT MAINTENANCE REPORTED SEVERAL EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK M1103 . OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800896 1 20080708 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 873AS 7549 LT EMERGENCY OVERWING EXTERIOR AFT LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM 33-51-21. OPS CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800802 1 20080618 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 2ND FROM THE FRONT EMERGENCY CEILING LIGHT INOP. REMOVED AND REPLACED LAMP IAW AMM 33-51-16 OPS CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800803 1 20080619 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 930EV 8014 BOTTOM STEP CRACKED AT SIDE ARM ATTACH POINT. (B) REMOVED AND REPLACED ASD BOTTOM STEP IAW AMM 52-11-00. (S) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800718 1 20080521 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 924EV 7830 LIGHTED EXIT SIGN ON WARDROBE HAS BROKEN ELECTRICAL CONNECTION CIRCUIT P9LY/J9LY. INSTALLED NEW P9LY/J9LY WARDROBE EME RGENCY LIGHT CONNECTORS IAW EESPM 20-17-10 AND WDM 33-51-00. WARDROBE EMERGENCY LIGHTS OP TEST REQUIRED. OPS TEST GOOD AT THIS TIME IAW AMM 33-51-00-710-801. (B) 2 L 7 2 4F RT A21EA 20080729 NE 2008 7 29 DXTA200803132 2 20080618 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LEFT SHUTDOWN E DXTA O OTHER Y J ENGINE STOPPAGE WARNING INDICATION NR NOT REPORTED 1 GL 07 361QS 5600361 PCEJC0268 LT ENGINE SHUT DOWN IN FLIGHT WHEN THROTTLE WAS BROUGHT BACK TO IDLE FIRMLY. (B) 2 L 7 2 4F 4 F RT A22CE E25EA 20080729 EU 2008 7 29 USAA920081275 1 20080629 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 654AW 1050 FLT 484 CLT - DEN - EMERGENCY EQUIPMENT - FLIGHT ATTENDANT JUMPSET FLASHLIGHT DOES NOT BLINK RED. MAINTENANCE REMOVED A ND REPLACED THE FLASHLIGHT BATTERY. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A28NM 20080729 EA 2008 7 29 TRAX200800842 1 20080626 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 977EV FS 484.0 RBL 36.0 INTERCOSTAL CRACKED AT UPPER FASTENER HOLE APPROX .3" LONG. NOT PREVIOUSLY REPAIRED. REPAIRED RBL 36. 0 INTERCOSTAL IAW REO 601R-53-41-059, REV. A. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAA920081308 1 20080529 A 5320 FLOOR SUPPORT BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW 23713 CLT - C22 - MAJOR REPAIR - CRACKED FLOORBOARD SUPPORT CHANNEL, BS 540 BL 0 WL 208, 1 LT AND RT SIDES. REPLACED FLOORBOA RD SUPPORT CHANNEL, BS 540 BL 0 WL 208,1 LT AND RT SIDES IAW B737 SRM 51-10-02. (S) 2 L 7 2 4F RT A16WE 20080729 2008 7 29 USAA920081311 4 20080702 A 2565 62158101 STUD AIRBUS A319 A319112 3930323 EU EVAC SLIDE BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 1019 PIT - NR 2 ENG - EMERGENCY EQUIPMENT - MOUNT STUD ASSEMBLY FOR SLIDE RAFT WIRE END BROKE OFF CAUSING STREAMER PULL HANDL E TO COME LOOSE ON THE L1 DOOR. REPLACED MOUNT STUD ASSEMBLY FOR SLIDE RAFT L-1 DOOR IAW TASK CARD 26L0025011 AND JA-90 0-09000-016. (S) 2 L 7 2 4F RT A28NM 20080729 NM 2008 7 29 KCSA081312 1 20080705 A 5315 FLOORBEAM BOEING 747 747122 1384872 NM BS 520 RBL 16 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 UPPER DECK FLOORBEAM WEB IS CRACKED AT STA. 520, RBL 16.(B) 2 L 7 4 4F RT A20WE 20080729 NM 2008 7 29 USAA920081312 1 20080530 A 5753 RIVET BOEING BOEING 737 7373S3 1384711 NM T/E FLAP LOOSE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW BN1458 23713 CLT - C22 - MAJOR REPAIR - LT OUTBOARD FOREFLAP HAS SEVERAL SMOKING RIVETS. REPLACED FOREFLAP IAW B737 AMM 27-51-37. ( S) 2 L 7 2 4F RT A16WE 20080729 SO 2008 7 29 MAS2008F00001 1 20080616 A 3350 BA50933901 CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FLT 6151 JFK ROW 3 EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED CHARGER OPS CHECKED GOOD. (B) 2 L 7 2 4T RT T00011AT 20080729 NM 2008 7 29 USAA920081293 1 20080706 A 5320 6935352U14 TIE CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT - Q3 - MAJOR REPAIR - TIE CLIP CRACKED AT 867 S-4L. REPLACED THE CLIP AT BS 867 S-4L IAW B737 SRM 51-10-02 AND SRM 51-40-02. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081326 1 20080705 A 2752 791C000001 ACTUATOR AIRBUS A319 A319132 3930340 NM T/E FLAP FAILED A USAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 19 834AW 14390 14390 2302 PHX - ANC - FLT 140 - DURING DESCENT AT 3,000 FT, CREW SELECTED FLAPS 3, CREW RECEIVED ECAM MESSAGE OF "FLAP FAULT." CR EW DECLARED AN EMERGENCY AND THE CABIN WAS PREPPED. LANDING WAS UNEVENTFUL AND THE ACFT TAXIED TO THE GATE. MAINTENANC E REPLACED THE RT NR 1 FLAP TRACK ACTUATOR PER AMM 27-54-49. OPERATIONAL CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERV ICE. (S) 2 L 7 2 4F RT A28NM 20080729 NM 2008 7 29 USAA920081289 1 20080629 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT - Q3 - MAJOR REPAIR - CRACK IN FRAME AT BS 400, S8-9R. REPAIRED FRAME AT BS 400, S8-9R IAW TYPICAL REPAIR 53-10-20. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081288 1 20080630 A 5340 65516982 STRINGER CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT - Q3 - MAJOR REPAIR - CRACK IN STRINGER TIE CLIP AT BS 908, SR4. REPLACED STRINGER TIE CLIP AT BS 908, SR4 IAW B737 SRM 51-40-02. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 DXTA200803142 1 20080625 A 3260 WARNING LIGHT AMD FALC50 FALCON2000 2730170 NM MLG ILLUMINATED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 218QS 118 UPON GEAR RETRACTION WE HAD A LEFT GEAR RED LIGHT. (B) 2 L 7 2 4F RT A50NM 20080729 EA 2008 7 29 TRAX200800814 1 20080621 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 RBL 9 CLIPS CRACKED INBD AND OUTBD AT FS 280. REMOVED AND REPLACED CLIPS IAW SRM 51-42-21 AND AMM 51-23-00. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAA920081318 1 20080628 A 5532 SKIN BOEING 757 757225 1384959 NM VERTICAL STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925UW 22205 BFM - MAJOR REPAIR - C3 CHECK - VERTICAL STABILIZER RT SIDE REAR SPAR WEB EXTERNAL SKIN CRACKED, VERTICAL STABILIZER STA TION 116.20. REPAIRED VERTICAL STABILIZER RT SIDE REAR SPAR WEB SKIN, VERTICAL STABILIZER STATION 116.20 IAW B757 SRM 5 1-70-06. (S) 2 L 7 2 4F RT A2NM 20080729 EA 2008 7 29 MASA200800477 1 20080617 A 5210 MS171536 ROLL PIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75996 7357 RON IN ORD PAX DOOR HANDLE WILL NOT STOW. REPLACED DOOR LINKAGE ROLL PIN. (B) 2 L 7 2 4F RT A21EA 20080729 EU 2008 7 29 USAABA08023 1 20080703 A 2750 FLAP SYSTEM AIRBUS 330 A330323 3930335 EU WING MALFUNCTIONED A USAA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 EA 19 277AY 0380 MAD - FLT 740 EN ROUTE PHL TO MAD. DURING APPROACH, THE TRAILING EDGE FLAPS WOULD NOT EXTEND. THE LEADING EDGE FLAPS O PERATED NORMALLY. THE FLIGHT MADE A MISSED APPROACH AND THEN LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AN D FOUND NO TORQUE LIMITER INDICATORS TRIPPED. PERFORMED OPERATIONAL CHECKS AND FOUND OK. OK FOR CONTINUED SERVICE. (S ) 2 L 7 2 4F RT A46NM 20080729 EU 2008 7 29 USAA920081320 1 20080705 A 3397 POWER CABLE AIRBUS A321 A321211 3930370 EU CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 171US 1465 FLT 1021 PIT - EMERGENCY EXIT LIGHT - SEAT EMERGENCY LIGHT 31 INOP. MAINTENANCE RECONNECTED SEAT 31 EMERGENCY LIGHT POW ER FEED CABLE. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080729 NM 2008 7 29 USAA920081321 1 20080630 A 5330 654576Y SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 PHX - MAJOR REPAIR - CRACK ON FUSELAGE SKIN BS 500C BELOW S14R, FORWARD AND ABOVE THE RT ENG ANTI-ICE SCAN LIGHT. REPA IRED FUSELAGE SKIN BS 500C BELOW S14R, FORWARD AND ABOVE THE RT ENG ANTI-ICE SCAN LIGHT IAW EA 120803 (S) 2 L 7 2 4F RT A16WE 20080729 CE 2008 7 29 DXTA200803133 1 20080618 A 3240 BRAKE SYS CESSNA 500 560CESSNA 2076750 CE MLG WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 361QS 5600361 BRAKES VERY INEFFECTIVE ON LANDING ROLL-OUT. (B) 2 L 7 2 4F RT A22CE 20080729 EU 2008 7 29 TRAX200800895 1 20080708 A 5250 PIN AEROSP ATR72 ATR72212 8680945 EU COCKPIT DOOR MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 634AS 370 COCKPIT DOOR MISSING RED PIN ON LT DOOR INSTALLED NEW COCKPIT DOOR PIN. OPS CK GOOD. REF CMM 25-13-14 (B) 2 H 7 2 4T RT A53EU 20080729 NM 2008 7 29 USAA920081280 1 20080626 A 5340 STRINGER CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT - Q3 - MAJOR REPAIR - CRACK IN STRINGER CLIP AT BS 520 S16L. REPLACED STRINGER CLIP AT BS 520 S16L IAW B737 SRM 51- 10-02. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081281 1 20080628 A 5752 WEDGE BOEING 737 737401 1384701 NM LT AILERON DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT - Q3 - MAJOR REPAIR - LT AILERON TAB OUTBOARD TRAILING EDGE CORNER DELAMINATED. REPAIRED LT AILERON TAB OUTBOARD TR AILING EDGE CORNER IAW B737 SRM 51-70-16. (S) 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800673 1 20080519 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA CABIN PEELING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 755EV 10185 EMERGENCY MEDICAL KIT PLACARD PEELING REMOVED AND REPLACED EMERGENCY MEDICAL KIT PLACARD IAW AMM 11-30-02. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAA920081269 1 20080625 A 5230 6547962524M WEB BOEING 737 7373B7 1384580 NM AFT CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 23379 CLT - C-5 - MAJOR REPAIR - AFT CARGO DOOR LOWER WEB FWD END IS CRACKED APPROX 4TH FASTENER AFT AND ANGLE IS CRACKED AT 3 FASTENER LOCATIONS. REMOVED DEFECTIVE DOOR AND INSTALLED SERVICEABLE DOOR FROM STOCK IAW B737 AMM 52-31-00-4. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081270 1 20080625 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CANNING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 23379 CLT - C5 - MAJOR REPAIR - FUSELAGE SKIN OIL CANNING AT BS 727E TO BS 740, S18-19R. REPAIRED FUSELAGE SKIN, BS 727E TO B S 740, S18-19R IAW B737 SRM 53-00-01 REPAIR 31. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081272 1 20080612 A 5310 652072354 DOOR FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 531AU 24478 PIT - RON - MAJOR REPAIR - A .75" INCH CRACK AT FORWARD CARGO DOOR AFT FRAME AT BS 495 S24R. REPAIRED FORWARD CARGO DOO R AFT FRAME AT BS 495 S24R IAW EA 111206. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081278 1 20080626 A 5753 SKIN BOEING 757 757225 1384959 NM T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925UW 22205 BFM - C3 - MAJOR REPAIR - LT WING INBOARD FLAP UPPER SURFACE HAS DELAMINATION APPROX 12 INCHES FROM INBOARD SIDE OF WEDG E EDGE. REPAIRED LT WING INBOARD FLAP UPPER SURFACE APPROX 12 INCHES FROM INBOARD SIDE OF WEDGE EDGE IAW B757 SRM 51-70 -10 AND SRM 57-53-01. (S) 2 L 7 2 4F RT A2NM 20080729 NM 2008 7 29 USAA920081283 1 20080630 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 PHX - MAJOR REPAIR - CABIN FLOORBEAM AT SEAT ROW 8 CROSSBEAM HAS CRACK IN (VERIFIED BY HFEC) RADIUS OF PREVIOUS REPAIR J UST TO THE LT OF CENTER BEAM. REPLACED CABIN FLOORBEAM AT SEAT ROW 8 CROSSBEAM AT BS 540 IAW BOEING DRAWING 65-52894. (S) 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800754 1 20080605 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 290-559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 SEAT RAIL AT RBL 9 F.S. 290 TO 559 HAS AREAS OF CORROSION. OPEN (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAA920081303 1 20080702 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 23380 CLT - MAJOR REPAIR - FUSELAGE SKIN CRACKED, BS 303.5, S13L AT THE FORWARD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED FUSEL AGE SKIN, BS 303.5, S13L AT THE FORWARD ENTRY DOOR LOWER HINGE CUTOUT IAW US AIRWAYS EA 100550. (S) 2 L 7 2 4F RT A16WE 20080728 EA 2008 7 28 A6WA200840315 1 20080402 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 403AW 7288 CRACK EXISTS ON LOWER SILL OF CARGO DOOR FS 574 LBL 45. NEW SILL CARGO DOOR FS 574 LBL 45 INSTALLED IAW REO 601R-53-61- 690 REV D. (A) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 2008UALA03595 1 20080626 A 5311 65B07374 FRAME BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 1600 PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 AFT CARGO PIT LWR LOBE FRAME WEB PUNCTURED AT BS 1600 LBL 15. FOUND WEB PUNCTURED. INSTALLED REPAIR DOUBLER REF KAL FR R UAL-744-0417 AND FAA FORM 8100-9. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080729 EA 2008 7 29 VNA2008F00003 1 20080630 A 5240 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE EXTERNAL POWER OPEN A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 712PS 10168 CREW REPORTED AN EXTERNAL SERVICE DOOR LEFT OPEN AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDE NT. MAINT INSPECTED AND FOUND THE EXTERNAL POWER DOOR OPEN. NO DEFECTS OR DAMAGE FOUND. MAINTENANCE SECURED THE DOOR CLOSED. AIRCRAFT WAS RELEASED FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A21EA E00063EN 20080729 NM 2008 7 29 HNA2008F00007 1 20080304 A 5347 85320890 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 846EX 36658 326 SEAT TRACK CORRODED IN AREA OF LAV AND GALLEY, SEAT TRACK REPAIRED IAW EA08-53-08-3097. (K) 2 H 7 2 4T RT A13NM 20080729 NM 2008 7 29 WRL2008F00003 1 20080706 A 5100 NONE DOUG MD11 MD11F 3023600 NM RT WING NONE A WRLA O OTHER O OTHER NR NOT REPORTED 1 SO 11 274WA 48633 DURING 1C + 12A CHECK REQUIRED UPGRADE EXISTING REPAIR DOUBLER ON RT WING FIXED L/E UPPER SKIN AT WING STA XS 261. PERF ORM EJ NR W2008A578-613 REV 00. REPAIR ON RT WING FIXED L/E UPPER SKIN AT XIS 261, COND CHECK NML AND JOB COMPLETED. ( K) 2 L 7 3 4F RT A22WE 20080729 NM 2008 7 29 UIE2008F00020 1 20080629 A 5320 REVEAL BOEING 747 747243B 1384830 NM 5R DOOR CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 540MC 22508 MAINE DECK R5 MAIN ENTRY DOOR CUTOUT FWD MIDDLE POSITION, DOOR OPENING LOCK RELEASE HANDLE CUTOUT REVEAL PANEL FOUND CRA CKED. CRACKED AREA TRIMMED OUT AND REPAIRED IAW SRM 51-10-01. (K) 2 L 7 4 4F RT A20WE 20080729 NM 2008 7 29 UIE2008F00021 1 20080607 A 5313 STRINGER BOEING 747 747243B 1384830 NM BS 300 S25R CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 540MC 22508 UPPER DECK STA 300 STRINGER 25R HAS FATIGUE CRACK. REPAIRED STRINGER CLIPS STRAP AND FRAME SPLICE FABRICATED IAW SRM 53 -10-04 AND INSTALLED IAW SRM 51-30-02. (K) 2 L 7 4 4F RT A20WE 20080721 NM 2008 7 21 SWAA083798 1 20080709 A 5330 6546767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELLY SKIN TEAR STRAP CRACKED AT BS 379, LBL 4. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083797 1 20080705 A 3260 273A3312 HANDLE BOEING 737 7377H4 1384404 NM COCKPIT DIRTY A SWAA K NONE N FALSE WARNING LD LANDING 1 SW 29 201LV 29854 MLG & NLG UNSAFE LIGHTS INDICATION. RECYCLED GEAR HANDLE AND GOT 3 GREEN LIGHTS. C/W BITE CK AND CLEANED GEAR HANDLE. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 2008UALA02829 1 20080516 A 3397 362624 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 SEAT 5A EMERGENCY LIGHT INOPERATIVE. FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECKED OK. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080721 NM 2008 7 21 SWAA083731 1 20080706 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT, BS 291.5, WL 256.5. REPAIRED SKI N PER SWA EA. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083638 1 20080701 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 632SW 27707 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083624 1 20080630 A 5753 65C30462 FLAP BOEING 737 7373Q8 1384670 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED 22Y CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083625 1 20080630 A 5752 6546455 TAB BOEING 737 7373Q8 1384670 NM LT AILERON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED 22Y CHECK, FOUND LT WING AILERON TAB CRACKED AT INBOARD END. REMOVED AND REPLACED TAB PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083627 1 20080630 A 3350 3071BPEGPL LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 691WN 23781 DURING SCHEDULED MV2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083643 1 20080701 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 706SW 27840 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083659 1 20080702 A 5311 6546559 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 927, STR 23L TO STR 23R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083670 1 20080702 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER 22R CRACKED AT BS 496. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083694 1 20080704 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 13R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083695 1 20080704 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 25L. REPAIRED FRAME PER SRM.. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083830 1 20080711 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 258WN 32516 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083668 1 20080702 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083663 1 20080702 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 927, STR 24R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083672 1 20080702 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS BS 616, STR 17L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083671 1 20080702 A 5753 65C30462 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD FORE FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20080722 NM 2008 7 22 2008UALA02959 1 20080521 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 655UA 25393 EMERGENCY LIGHT STRIP IN BUSINESS GALLEY LOOSE. FOUND LIGHT ASSEMBLY LOOSE. SECURED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 NM 2008 7 22 2008UALA03021 1 20080525 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 771UA 26932 EMERGENCY LIGHT AT SIDE OF SEAT 14C IS INOP. SUSPECT FAULTY LAMP. REPLACED LAMP, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080722 NM 2008 7 22 2008UALA03028 1 20080526 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 SEAT 41C, 43C EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT, CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20080722 WP 2008 7 22 08FDEA02213 1 20080610 A 3213 39140165501 CYLINDER DOUG MD10 MD1010F 3022112 WP RT MLG DAMAGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 363FE 48263 UPON GEAR RETRACTION HAD RED LIGHT IN PRIMARY RT MAIN INDICATOR. CONFIRMED IN SECONDARY. RAN" GEAR PRIMARY OR SECONDA RY LT(S) ILLUMINATE WITH GEAR HANDLE UP" CHECKLIST. RETURN TO KMEM. NO PROBLEMS ON ROLLOUT. REMOVED AND REPLACED RT MLG BUNGEE CYLINDER, ROD END BROKE IN HALF. 2 L 7 3 4F RT A22WE 20080722 NM 2008 7 22 2008UALA02985 1 20080526 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 ENGINE LOW A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 217UA 30550 NR 2 ENGINE IDG TOOK APPROXIMATELY 40 STROKES TO GET TO FULL. SUSPECT FAULTY O-RING. INSTALLED NEW IDG PER AMM 24-11-0 1-401. LEAK AND OP CHECK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080722 NM 2008 7 22 2008UALA02906 1 20080519 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 656UA 25394 LEFT MID LAV EEL LIGHT BAR IS INOP. SUSPECT BROKEN LIGHT ASSEMBLY. REPAIRED LT MID LAV EEL LIGHT BAR IAW GNMM 2-0-15-0 05 OPS CHECKED GOOD IAW MM 33-51-00. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 NM 2008 7 22 2008UALA02971 1 20080523 A 5753 FLAP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 590UA 28708 CRACK HAS MIGRATED THRU THE RT INBOARD T/E FLAP. ALSO HAVE DELAM ON BOTH SIDES OF CRACK. COMPOSITE DELAMINATION. ACP INTERIM REPAIR PER SRM 57-53-01, PERMANENT REPAIR ACCOMPLISHED PER EVA-71598. 2 L 7 2 4F 4 F RT A2NM E17NE 20080722 NM 2008 7 22 2008UALA03001 1 20080527 A 5610 141N00031 WINDOW BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT OVERHEATED A UALA O OTHER W M B INADEQUATE Q C OVER TEMP SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 524UA 24977 STRONG ELECTRICAL ODOR IN FLT DECK, GOT WORSE DURING DESCENT. ODOR WAS COMING FROM NR 1 LT WINDSHIELD. WINDOW HEAT TER MINAL BLOCK MELTED. REPLACED NR 1 LT WINDOW, REPLACED WIND HEAT CONTROL UNIT FOR WINDOW 1L AS PRECAUTION. 2 L 7 2 4F 4 F RT A2NM E17NE 20080722 NM 2008 7 22 2008UALA03003 1 20080526 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN CONTAMINATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 337UA 24241 EMERGENCY EXIT LIGHTS STRIP INOP. FOUND MOISTURE CONTAMINATION. REMOVED MOISTURE, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 2008 7 22 2008UALA02924 4 20080520 A 2565 B14056916 O-RING AIRCRUISERS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE LEAKING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 568UA 0496 26674 DOOR 2 SLIDE LOW BOTTLE. BOTTLE TO VALVE O-RING LEAKING. REPLACED BOTTLE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080722 NM 2008 7 22 2008UALA03074 1 20080528 A 2560 MXP21000 SMOKE GOGGLES BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT CRACKED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 921UA 25388 F/O GOGGLES CRACKED. SUSPECT PRE FLIGHT CHECKS. REPLACED SMOKE GOGGLES. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA03075 1 20080528 A 2612 655449915 MODULE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT FAULTY A UALA K NONE W L INADEQUATE Q C NO TEST CL CLIMB 1 WP 29 925UA 26646 BELL TO FIRE TEST DOES NOT WORK. SUSPECT FAULTY AURAL WARNING MODULE. REPLACED AURAL WARNING MODULE REF MM 31-26-41 PG 401, ALL TEST OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA03011 1 20080523 A 5344 141N83782 HINGE FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 CRACK AT FWD UPPER L-1 DOOR CUTOUT AREA, INNER UPPER DOOR HINGE FITTING AT BS 337 AND STR 12L. REMOVED DAMAGED AREA REF R EO G-12344-3 AND SRM 51-20-01. THIS IS A TIME LIMITED REPAIR. FITTING P/N 141N8378-2 MUST BE REPLACED AT NEXT CK, N O LATER THAN 05-16-201 0, NOT TO EXCEED 3,000 CYC. CURRENT PTC 18048. 2 L 7 2 4F 4 F RT A2NM E17NE 20080722 NM 2008 7 22 2008UALA03136 1 20080530 A 3350 3024711 LIGHT BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 914UA 25381 EXTERIOR EMERGENCY LIGHT AT LT OVERWING EXIT INOP. SUSPECT FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA03173 1 20080603 A 3510 6350A33XA BOTTLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW O2 LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 203UA 24718 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. SUSPECT PRE FLIGHT CHECKS. SERVICED OXYGEN SYSTEM TO FULL 1850 PSI. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA03183 1 20080603 A 5210 SLEEVE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FWD ENTRY DOOR WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 FWD ENTRY DOOR CUTOUT, BODY TORQUE TUBE SLEEVES WORN & BOLT HOLES CORRODED. INSTALLED OVERHAULED BODY TORQUE TUBE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA03212 1 20080604 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 AFT CARGO FRAME DENTED STA 1520, STR 26L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080722 NM 2008 7 22 2008UALA03213 1 20080604 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU R2 SLIDE INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 340UA 24244 THE 2R SLIDE LIGHT INOP. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA03215 1 20080605 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHT ROW 4A AFT INOP. RELAMPED EMERGENCY LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080722 NM 2008 7 22 2008UALA03019 1 20080523 A 3350 20131A POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 675UA 29243 EMERGENCY ESCAPE PATH LIGHTS ON RIGHT SIDE OF A/C BETWEEN ROWS 25 & 35 CAME ON & STAYED ON FOR 2HR. SUSPECT POWER SUPPL Y. REPLACED POWER SUPPLY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 EA 2008 7 22 A6WA200840471 1 20080507 A 5340 BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 438AW 7748 AFT BRACKET OF HYDRAULIC RESERVOIR (SYSTEM 3) CRACK IN MLG BAY BL 0. AFT BRACKET OF HYDRAULIC RESERVOIR (SYSTEM 3) IN ML G BAY BL 0 REPLACED IAW SRM 51-42-13. (A) 2 L 7 2 4F RT A21EA 20080722 NM 2008 7 22 SWAA083880 1 20080714 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPV CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. R&R LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080722 NM 2008 7 22 SWAA083958 1 20080716 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080722 NM 2008 7 22 SWAA083964 1 20080716 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 16R. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080722 NM 2008 7 22 SWAA083686 1 20080702 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR CUTOUT UPPER HINGE. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 DU4R2008210 1 20080602 A 5330 SKIN BOEING 737 737448 13844BU NM FUSELAGE DENTED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 742VA 24773 DENT ON FUSELAGE SKIN AFT BS 910 AT S-21R. 2 L 7 2 4F RT A16WE 20080717 EU 2008 7 17 UPS08152573 1 20080624 A 5100 NONE AIRBUS A300 A300F4622R 3930360 EU WITHIN LIMITS NONE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 172UP 0005 CRACK MAIN CARGO PIT DOOR. EVALUATED DAMAGE TO BE WITHIN LIMITS OF A300 SRM CH 53-10-20 FIG 104. C/W TEMPORARY AND OPE N DEFERRAL FOR PERMANENT REPAIR WITHIN 350 FLIGHT HRS. 2 L 7 2 4F RT A35EU 20080729 EA 2008 7 29 TRAX200800716 1 20080531 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 LINTEL SUPPORT ANGLE PN 601R35050-109 CRACKED AT PRESSURE BULKHEAD WEB BS 621 . REMOVED LINTEL SUPPORT ANGLE. FABRICATED NEW LINTEL SUPPORT ANGLE PER EO 600-53-0346. INSTALLED FABRICATED LINTEL SUPPORT ANGLE IAW SRM 51-42-20. AWAITING EC/ TC 7025126. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 2008UALA03433 1 20080616 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 515UA 24840 ESCAPE LIGHTING ON FLOOR BETWEEN ROWS 12 & 13 IS NEEDING REPAIR. REPAIRED LENS STRIP. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 EU 2008 7 29 2008UALA03582 1 20080625 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN ODOR A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 423UA 504 F/A REPORTS VERY STRONG ODOR POSSIBLE CHEMICAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080729 EA 2008 7 29 TRAX200800669 1 20080519 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 929EV 8007 PAX DOOR AFT DRAG ANGLE IS CRACKED JUST ABOVE ASSIST MOTOR PULLEY. CUT AWAY DAMAGED PROTION OF DRAG ANGLE IAW REO 601R5 211513 REV.A, STEP 1-2. COMPLIED WITH HFEC IAW REO 601R-52-11-513, STEP 3 AND NDTM PT 1 51-20-06. NO INDICATIONS NOTED AT THIS TIME. INSTALLED REPAIR PARTS FOR AFT DRAG ANGLE IAW REO 601R-52-11-513 REV A, STEPS 4-12. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800906 1 20080712 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 461 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 FLOORBEAM FITTING AT FS 461 ON O/B SIDE OF RBL 9 CRACKED REMOVED FITTING AND DRILLED NEW SUPPORT FITTING. OK TO INSTA LL FLOORBEAM FITTING. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800725 1 20080602 A 5242 HANDLE CNDAIR CL600 CL6002C10 1390015 EA E/E BAY DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 AVIONICS SERVICE DOOR HANDLE CRACKED. REMOVED AND REPLACED AVIONIC SERVICE DOOR HANDLE IAW SRM 51-42-02. FOR PRESSURIZ ATION LEAK CHECK REFER TO W/O 92203 N/R-00065 ITEM 2. (S) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800727 1 20080602 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 202 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 684BR 7708 FS 202.75 BULKHEAD HAS A .50 INCH CRACK WHERE PARKING BRAKE CABLE GOES THROUGH. REPAIRED FS 202 BULKHEAD IAW ASA EO 600 -53-217 IN ITS ENTIRETY. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 ASAA0843124 1 20080507 A 5311 65465302 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 RIGHT FRAME AT STA 440 CRACKED AT PSU RAIL BRACKET. REPAIRED PER EA 5310 02797. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ZZDA2008127 1 20080702 A 3350 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 930AT 55072 LT AND RT EXTERIOR EMERGENCY LIGHTS WILL NOT EXTINGUISH. REPLACED EXTERIOR EMERGENCY LIGHTS BATTERY PACK AND RELAY R2-2 73, ALL OPS CHECK OK PER MM 33-51. 2 L 7 2 4F TR A6WE 20080729 NM 2008 7 29 USAA920081234 1 20080604 A 5312 BULKHEAD BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW 23713 CLT - C22 - MAJOR REPAIR - CRACK IN WEB AT BS 178, RBL 17. REPAIRED WEB AT BS 178, RBL 17 IAW B737 SRM 51-70-13G. (S) 2 L 7 2 4F RT A16WE 20080729 EU 2008 7 29 USAA920081253 1 20080616 A 5321 D5367520400000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU AFT CARGO BAY DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 679AW 2613 SAL - BC - 02 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 151VG IN AFT CARGO COMPARTMENT FR 24 - 28, BL Y765 TO Y-765. REPLACED FLOOR PANEL 151VG IN AFT CARGO COMPARTMENT IAW AIRBUS A319 SRM 53-02-00. (S) 2 L 7 2 4F RT A28NM 20080729 NM 2008 7 29 USAASB08044 1 20080627 A 2560 MV10 MEGAPHONE BOEING 737 737401 1384701 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 420US 23987 MCO - MAINTENANCE REPORTED THE AFT MEGAPHONE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT MEGAPHONE. OPERATIO NAL CHECK GOOD. (S) 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800833 1 20080624 A 5310 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 977EV CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.5" IN LENGTH. REMOVED AND REPLACED CARGO DOOR SUPPORT BEAM LOW ER ANGLE WITH NEW PART IAW SRM 51-42-21 AND 51-40-11. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAA920081309 1 20080702 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT - MAJOR REPAIR - Q3 CHECK - CRACKED FRAME, BS 440, S8L-S9L. REPAIRED FRAME, BS 440, S8L-S9L IAW US AIRWAYS TYPICAL REPAIR 53-10-20F. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081310 1 20080702 A 3350 2013A1 BATTERY BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 526AU 23861 MCN - B01 - EEL - SEVERAL EMERGENCY LIGHTS OUT IN CABIN. REPLACED CENTER EMERGENCY BATTERY IAW B737 AMM 33-51-51-2. (S ) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081290 1 20080630 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT - Q3 - MAJOR REPAIR - CRACK IN FRAME AT BS 440 S8-9R. REPAIRED FRAME AT BS 440 S8-9R IAW TYPICAL REPAIR 53-10-20E. (S) 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 QXEA200800540 1 20080531 A 5250 HINGE BOMBDR DHC8 DHC8402 1390042 NM COCKPIT OUT OF ADJUST A QXEA K NONE O OTHER NR NOT REPORTED 1 NM 09 425QX 4039 SEA - COCKPIT DOOR VERY HARD TO OPEN OR CLOSE (BINDS). MAINTENANCE ADJUSTED THE HINGES. DOOR OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080717 NM 2008 7 17 QXEA200800538 1 20080603 A 5210 TRACK BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR DIRTY A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 406QX 4048 SEA - FLIGHT 2257. AFT PASSENGER DOOR HARD TO CLOSE. MAINTENANCE CLEANED THE TRACKS AND LUBED THE DOOR. OPERATIONAL C HECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20080717 WP 2008 7 17 ASMF200805004 1 20080523 A 3222 59516395001 STRUT DOUG DC9 DC987 3022087 WP NLG FAILED W ASMF A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 23 216AM 10493 10493 49586 AIRCRAFT RETURNED OF FLIGHT DUE TO NOSE LANDING GEAR FAILURE. MAINTENANCE PERSONNEL REPLACED THE NOSE GEAR SHOCK STRUT O-RINGS, NOSE GEAR ACTUATOR CYLINDER AND NOSE GEAR BUNGEE CYLINDER IAW MM 32-21-02, 32-32-06 AND 32-32-07, TESTED IAW MM 32-30-00, ALL CORRECT. THE OVERWEIGHT INSPECTION WAS PERFORMED IAW MM 05-51-04, NO DAMAGES WERE FOUND. 2 L 7 2 4F RT A6WE 20080717 NM 2008 7 17 ASAA0843060 1 20080611 A 5754 SKIN BOEING 737 7374Q8 138447Q NM NR 6 SLAT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 NR 6 SLAT HAS 3 DENTS ON TOP SURFACE. PREPPED DAMAGED AREA FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 CALA0800538 1 20080603 A 5311 BAC15171147 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14645 28906 STATION 727B LEFT BETWEEN S8L AND S9L IS CRACKED. REPAIRED CRACK PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843076 1 20080511 A 5330 65C3235720 SKIN BOEING 737 7374Q8 138447Q NM BS 500A-500B DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 DENT OF LT LOWER FUSELAGE EXTERIOR BS 500A TO BS 500B STR25 TO STR26. DAMAGE REPAIRED IAW B737 400 SRM 53 00 01. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843077 1 20080501 A 5330 65C3235720 SKIN BOEING 737 7374Q8 138447Q NM BS 373-377 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 4 DENTS IN SKIN 2 INCHES BELOW STR 24L FROM BS 373.5 TO BS 377.5. REPAIR WORK ACCOMPLISHED IAW B737 400 SRM 53 00 01. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0853065 1 20080621 A 2140 3989083 VALVE BOEING 737 737890 1384527 NM CABIN HEATER FAILED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 585AS 3218 35683 FWD CAB ZONE TEMP LIGHT ILLUMINATES ON RECALL ACCOMPLISHED FIM TASK 21 62 00 810 848 ZONE TEMP LIGHTS COME ON INTERMITTE NTLY DURING MASTER CAUTION RECALL VERIFIED FWD CAB ZONE TEMP LIGHT ILLUMINATED DURING RECALL. ACCOMPLISHED FAULT ISOLAT ION PROCEDURE PACK ZONE TEMP CONTROLLER BITE REF 21 62 TASK 801. NR 2 CONTROLLER FAULTED ZONE TRIM VALVE. ACCOMPLISHED FIMTASK 21 62 00 810 834 FORWARD CABIN TRIM AIR VALVE FAULT ISOLATION. VERIFIED P/N OF FORWARD CABIN TRIM AIR VALVE WI TH SEAM MARK. REMOVED AND REPLACED VALVE REF MM21 61 21. OPS CHKS LEAK CHKS GOOD. GROUND VERIFICATION CHKD GOOD WITH MASTER CAUTION RECALL AND TEMP CONTROLLER BITE CHK OK. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843023 1 20080517 A 5330 65C277995 SKIN BOEING 737 737490 1384715 NM BS 322-334 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 703AS 28893 CORRECTION TO MFR'S PART NUMBER. DENT FOUND IN FUSELAGE BELOW R1 DOOR. REMOVED DAMAGED AREA OF SKIN FABRICATED AND INST ALLED REPAIR FILLERS AND DOUBLER IAW ASA EA5330 02347. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083334 1 20080618 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 456WN 32463 DURING SCHEDULED MV3 CHECK, FOUND EEPLS LENS MISSING AT ROW 15 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 MWE2008F00001 1 20080626 A 5330 591022819 SKIN BOEING 717 717200 1383700 NM BS 1189-1200 DAMAGED A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 903ME 55167 LOWER SKIN DAMAGED AT STA 1189 TO 1200, 21 INCHES LEFT OF CENTER. FABRICATED AND INSTALLED DOUBLER. (K) 2 L 7 2 4F TR A6WE 20080717 NM 2008 7 17 SWAA083341 1 20080618 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 709SW 27843 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083342 1 20080618 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 723SW 27855 L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083349 1 20080618 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 764SW 27878 DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083213 1 20080612 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083216 1 20080612 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 410WN 27897 DURING SCHEDULED HC2 CHECK, FWD LT CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PAC K PER MM. 2 L 7 2 4F RT A16WE 20080717 2008 7 17 SWAA083215 4 20080612 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 410WN 27897 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083283 1 20080615 A 3350 101073 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 258WN 32516 FWD CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083300 1 20080617 A 2720 6545187 TORQUE TUBE BOEING 737 7373H4 1384600 NM RUDDER WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 DURING SCHEDULED 20Y CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED TORQUE TUBE PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083288 1 20080617 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 401WN 29813 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 08FDEA02053 1 20080530 A 5330 656044747 SKIN BOEING 727 727227 1384078 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 490FE 21493 LOWER FUSELAGE, SEVERAL DENTS WITH BULGING SKIN BETWEEN STA 1050 AND 1070, BETWEEN STR 28R AND 26R LOWER FUSELAGE SEVERA L DENTS WITH BULGING BTW STA 1015 TO 1070 STR 28R - 26R; CUT OUT 2 EA DAMAGE AREA DIM (12 INCH BY 6 1/2 INCH), (2 1/2 BY 1 1/2) IAW SRM 53-30-3 FIG 3. FAB DOUBLER REPAIR MAT USED 2024T3.071" PO NR 9001282 DIM (24 1/2 INCH BY 17 1/2 INCH) AND 2 EA FILLER MAT USED 2024T3.063" PO NR 9006767 DIM (8" BY 3"), (6 1/2" BY 2") IAW SRM 53-30-3 FIG 3 AND 53-30-2 FI G. REMOVED 2EA INTERNATIONAL AND ANTENNA SUPPORT IAW SRM 51-30-2. TREATED AND PRIMED PARTS IAW SRM 51-10-2, INSTALLED COUNTER SINK WASHER IAW SRM 51-30-8. INSTALLED DOUBLER REPAIR AND PARTS," INTERCOSTAL 2 EA, AND ANTENNA SUPPORT. 2 L 7 3 4F A3WE 20080717 WP 2008 7 17 08FDEA02063 1 20080530 A 5310 AFA3871117 DOOR FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 THE CENTER CARGO DOOR AFT JAMB HAS A 2 INCH DENT AT THE LOWER AFT CORNER. REMOVED BULKHEAD PANEL 183 GA TO FOM PER MD-1 0-10 AMM 25-52-36-2; REMOVED DAMAGED ANGLE P/N AFA 3871-117 PER DC/MD-10 SRM 51-35-01; VOL II; PG 1. CUT OUT DAMAG E AND FABBED A REPAIR ANGLE AND FILLER PER DC/MD-10 SRM 53-00-01; FIG 8; SHEET 1; VOL I. INSTALLED REPAIR ANGLE; FILL ER AND AFA 3871-117 ANGLE PER DC/MD-10 SRM 53-00- 01; FIG 8; SHEET 1; VOL I. INSTALLED AFA 3871-117 ANGLE PER DC/MD-10 SRM 51-35-01; VOL II AND DC/MD-10 SRM 51-33-01; VOL II. INSTALLED BULKHEAD PANEL 183 GA PER DC-10-10 AMM 25-52-36-02. 2 L 7 3 4F RT A22WE 20080717 WP 2008 7 17 08FDEA02214 1 20080610 A 5410 STRUCTURE DOUG MD10 MD1010F 3022112 WP NR 1 PYLON LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 NR 1 PYLON, AFT LOWER RIGHT SIDE HAS NUMEROUS RIVETS LOOSE. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 08FDEA02161 1 20080605 A 5330 6554577 SKIN BOEING 727 727227 1384078 NM BS 566-572 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 FWD PIT FUSELAGE SKIN HAS CORROSION, BS 566 - 572, STR 28L REMOVED CORROSION FROM FWD PIT FUSELAGE SKIN, BS 566 - 572 ST R 28L. NDT FOR MATERIAL REMOVAL. FOUND TO BE OUT OF LIMITS. .035 INCH REMOVED AT DEEPEST POINT. ORIGINAL .100 INCH R EMOVED DAMAGE/PREVIOUS REPAIR NEAR CUT OUT. FABRICATED, TREATED AND PRIMED AND INSTALLED DOUBLER REF SRM 53-30-3 FIG 3. THIS REPAIR IS A CATAGORY "B'' REPAIR THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080717 NM 2008 7 17 08FDEA02097 1 20080602 A 5100 NONE DOUG MD11 MD11F 3023600 NM REPAIRED PER SRM NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 EXISTING DOUBLER REPAIR AT RIGHT FUSELAGE APPROX STA 2003 TO STA 2004, STRINGER 38 TO 41. EXISTING DOUBLER REPAIR AT RIGHT FUSELAGE APPROX STA 2003 TO STA 2004, STRINGER 38 TO 41 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED PER SRM 53-20- 00 FIGURE 2 VOLUME I. FEDEX EO NR 1-5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG - MD11. REPAIR CATALOG AND TRACKING R EQUIREMENTS, HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 SWAA083264 1 20080613 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT KEEL BEAM BS 714, LBL 6.5. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 EU 2008 7 17 08FDEA02244 1 20080612 A 5347 A53611640200 SEAT TRACK AIRBUS 300 A300B4622 3930401 EU ZONE 800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 719FD 388 MAIN CARGO SEAT TRACK EXFOLIATED FROM FR14 C TO FR 19 LBL 37 (YD). REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-21 AND 51-40-44. 2 L 7 2 4F RT A35EU 20080717 NM 2008 7 17 SWAA083539 1 20080626 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 203WN 32483 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083542 1 20080626 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 295WN 32541 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080718 WP 2008 7 18 08FDEA02554 1 20080629 A 3620 356632255 ELEMENT DOUG MD10 MD1010F 3022112 WP FAILED A FDEA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 CE 21 570FE 47829 DURING CRUISE FLIGHT AT FL320 GOT A LEVEL 3 ALERT AIR MAINF 2 FAIL REDUCED POWER TO IDLE AIR MAINF 2 FAIL ALERT STAYED O N FOLLOWED BY A LEVEL 1 ALERT AIR SYS 2 OFF MANF AIR LIGHT WAS ILLUMINATED ON OVERHEAD AIR SYS CONTROL PANEL NO INDICAT IONS OF SMOKE OR FUMES NOTED DIVERTED TO NEAREST SUITABLE AIRFIELD NO INDICATIONS OF FIRE NOTED BY FIRETRUCKS AFTER LAND ING. MEL 29JUN08. ACN RELEASED FOR SERVICE PER MEL/CDL: 36-23-01-02. REMOVED AND REPLACED MANIFOLD FAILURE SENSING EL EMENT D1-28C RECONNECTED SENSING ELEMENT CONNECTOR C5-76,C5-27,C5-18 AND C5-20 OP'S CHECKED GOOD. 2 L 7 3 4F RT A22WE 20080718 EU 2008 7 18 08FDEA02360 1 20080620 A 5321 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU CABIN DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 MAIN CABIN FLOOR PANEL 251 UH IS DAMAGED. FABBED A NEW FLOOR PANEL 251 UH BY USING THE OLD PANEL AS A TEMPLATE; POTTED ; CURED; SANDED EDGES; POTTED AND CURED INSERTS; APPLIED NON-SKID TAPE AND PART MARKED THE PANEL IAW FEDEX DWG SRZ 25-00 5 REV F. 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 08FDEA02137 1 20080603 A 2120 UNKNOWN BOEING 727 727227 1384078 NM COCKPIT SMOKE A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CE 21 492FE 21530 ON SHORT FINAL AT EWR ALL 3 CREW MEMBERS COULD SEE AND SMELL SMOKE IN COCKPIT. ONLY LEFT PACK WAS ON AT THE TIME, WITH NR 1 AND NR 3 BLEEDS OPEN. RAN LT PACK WITH APU BLEED, NO SMELL OR SMOKE PRESENT. RAN NR 1 WITH LT PACK, NO SMELL. IN SPECTED LEFT ACM FOR PROPER OIL LEVEL AND FOUND ALL INDICATIONS OF LT PACK TO BE NORMAL. WHILE T/S NOTICED WEATHER IND C/B POPPED, C/B WILL NOT RESET. 2 L 7 3 4F A3WE 20080729 NM 2008 7 29 USAA920081291 1 20080720 A 5311 FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT - Q3 - MAJOR REPAIR - FRAME CRACKED AT BS 616, S-17L. REPAIRED FRAME AT BS 616, S-17L IAW TYPICAL REPAIR 53-62-01. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAASB08046 1 20080702 A 3397 WIRE BOEING 737 7374B7 1384702 NM EMERGENCY LIGHTS BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 442US 24841 PIT MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 20 AND 21 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRES AT SPLICE. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800714 1 20080530 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 878AS 7590 ASD BOTTOM STEP IS BROKEN AND ATTACHMENT LINKAGE IS BENT. REMOVED AND REPLACED BOTTOM STEP AND ATTACHMENT LINKAGE IAW A MM 52-11-04. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 ASAA0843132 1 20080505 A 5311 65C329621 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 AFT CARGO COMPARTMENT FRAME AT BS 727G IS CORRODED BETWEEN STRINGER 25R AND 26R. REPAIRED WITH REPAIR PART IAW B737 400 SRM. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800735 1 20080603 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA BS 409 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 FS 409.0+128 BULKHEAD VERTICAL STIFFENER BEAM AT LBL 18 CRACKED AT OUTBOARD SIDE LOWER RADIUS APPROX 1/2" LONG. (B) RE PAIRED BULKHEAD VERTICAL STIFFENER IAW REO 601R-53-41-056 & REO 601R-53-41-056. (A) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 ASAA0843140 1 20080516 A 5711 111A11414 SPAR BOEING 737 7374Q8 138447Q NM CENTER WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 BS 663.75 WING CENTER SECTION REAR SPAR LOWER RIGHT WEB (COMPOSITE PANEL) CRACKED. WING CENTER SECTION REAR SPAR AT BS 663.75 LOWER RIGHT WEB CRACK REPAIRED PER SRM 51 70 04 REPAIR NR 10. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843149 1 20080506 A 5311 65C25229100 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 AFT CARGO PIT BS 727E AT STR 24R FRAME DENTED ON TOP FLANGE. AFT CARGO PIT BS 727E AT STR 24R FRAME REPAIRED IAW B737 4 00 SRM 51 70 11. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843150 1 20080506 A 5311 654659673 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 AFT CARGO PIT BS 727C BW STR 24R 25R TOP FLANGE OF FRAME DENTED. AFT CARGO PIT FRAME BS 727C STR 24R 25R REPAIRED IAW B 737 400 SRM 51 70 11. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843151 1 20080506 A 5320 654655055 ATTACH ANGLE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 FRAME TO SKIN ATTACH ANGLE CORRODED IN AFT BILGE AREA. REPAIRED PER SRM 53 00 07. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 DXTA200803122 1 20080614 A 3260 UNKNOWN GULSTM 200 200 4500308 NM MLG MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 724QS 100 AFTER TAKEOFF WHEN GEAR SELECTOR HANDLE WAS MOVED UP BOTH L & R GEAR INDICATORS INDICATED RED HASH MARKS. (B) 2 L 7 2 4F RT A53NM 20080729 NM 2008 7 29 ASAA0843158 1 20080604 A 5310 DOOR FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 AFT CARGO PIT DOORWAY LWR AFT CORNER BS 847 MISDRILLED HOLE. AFT CARGO PIT DOORWAY LWR AFT CORNER BS 847 REPAIRED IAW R O 8463 AND ASA EA 5330 02356. ACCOMPLISHED INITIAL INSPECTION OF THE SUBJECT AREA AT 50 000 TOTAL FLIGHT CYCLES. CONTA CT ENGINEERING FOR DEFINITION OF INSPECTION METHODS REPEAT INTERVAL. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800600 1 20080505 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 920EV 7810 I/B AND O/B CLIPS AT FS 280.0 LBL 9.0 CRACKED IN RADIUS. REMOVED 2 EA CAMLOC RECEPTACLES IAW SRM 51-42-06. REMOVED INB D AND OTBD CLIPS IAW SRM 51-42-06 AND 51-42-21. CAMLOC RECEPTACLES AT FS 280.0, 2 TOTAL AND INBD AND OTBD CLIPS REQUIRE INSTALLATION. INSTALLED INBD AND OTBD CLIPS AT FS 280.0 LBL 9.0 NEW SERVICEABLE IAW SRM 51-42-06 AND 51-42-21. 2 EA C AMLOC RECEPTACLES REQUIRE INSTALLATION. INSTALLED 2 EA SAME CAMLOC RECEPTACLES IAW SRM 51-42-06. REPAIR COMPLETE. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 DXTA200803123 1 20080614 A 2120 UNKNOWN GULSTM 200 200 4500308 NM CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 07 706QS 131 DURING APPROACH INTO SAN JUAN BEGAN TO SMELL A STRONG ODOR WHICH APPEAR TO BE COMING FROM AN ELECTRICAL UNIT. (B) 2 L 7 2 4F RT A53NM 20080729 NM 2008 7 29 ASAA0843161 1 20080506 A 5311 6549596111 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 AFT CARGO PIT BS 727E BETWEEN STRINGER 22L & 23L TOP FLANGE OF FRAME DENTED. AFT CARGO PIT FRAME REPAIRED AT BS 727E ST RINGER 22L TO 23L IAW B737 400 SRM 51 70 11 FIG 1. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843163 1 20080507 A 5311 90526911 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 LEFT SIDE FRAME AT STA 747 CRACKED AT PSU RAIL BRACKET. LEFT SIDE FRAME AT STA 747 AT PSU RAIL BRACKET REPAIRED IAW ERO 8337 & ASA EA 5310 02797 REF CERT 11678. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843166 1 20080507 A 5311 654655211 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 LEFT FRAME AT STA 827 CRACKED AT PSU RAIL BRACKET. LEFT FRAME AT STA 827 AT PSU BRACKET REPAIRED IAW CASCADE ERO 8337 & ASA EA 5310 02797. 2 L 7 2 4F RT A16WE 20080729 CE 2008 7 29 DXTA200803119 1 20080613 A 3241 WARNING LIGHT CESSNA 560 560XL 2076702 CE ANTI SKID SYSTEM ILLUMINATED E DXTA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 07 664QS 5605264 ON TAKEOFF ROLL AT APPROX 65 KIAS THE ANTI-SKID INOP WARNING LIGHT ILLUMINATED. TAKEOFF ABORTED. (B) 2 L 7 2 4F RT A22CE 20080729 NM 2008 7 29 ASAA0843138 1 20080502 A 5330 6545775102 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE NICKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 FUSELAGE SKIN NICKED. REPAIRED PER SRM 53 00 01 AND EA 5300 01080. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800812 1 20080621 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 750EV 10161 ENTRYWAY/GALLEY EMERGENCY LIGHTS HAVE SEVERAL INOP BULBS. RELAMPED ENTRYWAY/GALLEY EMERGENCY LIGHTS IAW AMM 33-51-00. (B) 2 L 7 2 4F RT A21EA 20080729 EU 2008 7 29 ASAA0853169 2 20080701 A 7220 3370051180 INLET BULLET BOEING 737 737890 1384527 NM CFMINT CFM56 CFM562AFR 13802 EU NR 1 ENGINE ERODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 570AS 894536 35185 894536 NR 1 ENGINE FWD SPINNER (CONE) HAS EXCESSIVE ERROSION OF BLACK AND WHITE COATING. REMOVED AND REPLACED SPINNER (CONE) P ER TC 78472002. 2 L 7 2 4F 4 F RT A16WE E21EU 20080729 NM 2008 7 29 ASAA0843142 1 20080612 A 5320 654795710 SILL BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 AFT CARGO BAY DOOR LOWER SILL CHANNEL HAS TWO DRILL MARKS. REPLACED SILL PER SRM 51 40 05 AND 51 40 02. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843152 1 20080506 A 5330 65479551 BEAR STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 BEAR STRAP CORRODED IN AFT CARGO BAY AREA. REPAIR STRAP PER EA 5330 02357. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800860 1 20080701 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 MAIN CABIN DOOR COULD NOT BE OPENED FROM OUTSIDE. COMPLIED WITH INSP OF PAX DOOR HANDLE CLEARED AND LUBE HANDLE OPS CHE CK GOOD OK FOR SERVICE PER CRJ200AMM52-10.--[SDR CLOSED](B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800800 1 20080617 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 EMERGCY LIGHT AT GALLEY SERVI CE DOOR, AFT SIDE 2 LIGHTS OUT REMOVED AND REPLACED LAMPS, OPS CK GOOD. REF 33-50-01. ( B) 2 L 7 2 4F RT A21EA 20080729 CE 2008 7 29 DXTA200803110 1 20080611 A 3240 WARNING MESSAGE CESSNA 500 560CESSNA 2076750 CE BRAKE SYSTEM ILLUMINATED E DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 830QS 5600784 "LO BRK PRESS AND ANTISKID INOP" ANNUNCIATOR ILLUMINATED IN FLIGHT. STOPPED AIRCRAFT WITH EMER BRAKE. (B) 2 L 7 2 4F RT A22CE 20080729 CE 2008 7 29 DXTA200803103 1 20080607 A 3240 BRAKE SYS CESSNA 500 560CESSNA 2076750 CE MLG WEAK E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 302QS 5600402 CAPTAIN AND COPILOT RIGHT BRAKE PEDALS ARE LESS EFFECTIVE THEN THE LEFT PEDALS. (B) 2 L 7 2 4F RT A22CE 20080729 CE 2008 7 29 DXTA200803094 1 20080603 A 3240 BRAKE SYS BEECH MU300 400A 1155402 CE MLG WEAK E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 123QS RK486 LEFT BRAKE PEDAL WILL GO ALL THE WAY TO THE FLOOR ON BOTH SIDES OF COCKPIT. (B) 2 H 7 2 4F RT A16SW 20080729 EA 2008 7 29 TRAX200800648 1 20080516 A 2170 DRAIN LINE CNDAIR CL600 CL6002B19 1900309 EA WATER SEPARATOR CLOGGED A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 846AS 7328 AFTER T/O WHILE RAISING THE GEAR, THERE WAS A SEVERE RANCID ELECTRICAL SMOKE SMELL WITH A HAZY SMOKE IN THE COCKPIT. AI RCRAFT RETURNED TO ATL AFTER T/O, EMERGENCY DECLARED. UNCLOGGED DRAIN LINES FOR LT WATER SEPERATOR IAW AMM 21-51-13-100 -802 AND REPLACED COALESCER IAW AMM 21-51-13-140-801 REPLACED MISSING INSULATION BLANKETS ON WATER SEPERATORS PERFORMED FULL GEAR SWING IAW AMM 32-30-00-710-802 AND ENGINE RUNS IAW AMM 71-00-00-710-808 PER REQUEST OF DIRECTOR OF MTC. 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800868 1 20080703 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 CEILING EMERGENCY LIGHTS NR 4 AND 5 INOPERATIVE. REMOVED AND REPLACED CEILING EMERGENCY LIGHTS NR 4 AND 5 LIGHT BULBS. OPS CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800652 1 20080517 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 904EV 7628 EMERGENCY FLOOR FLOOD LIGHT ON WARDROBE WILL NOT ILLUMINATE FOUND BROKEN WIRE NEAR CONNECTORS. SPLICED ON NEW CONNECTOR ON WIRE 39LY IAW WSPM 20-29-11. OPS CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080730 EA 2008 7 30 VNAA0806006 1 20080609 A 2460 B080474001 RELAY CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE AC BUSS FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 237PS 7906 CREW REPORTED AN AC ESSENTIAL BUSS CAUTION MESSAGE AFTER TAKEOFF. THE CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AUTO TRANSFER RELAY IN ACCORDANCE WITH THE ACFT MAINTENANCE MANUAL. OPE RATIONAL CHECKS WERE GOOD. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080730 NM 2008 7 30 CALA0800687 1 20080707 A 5311 6546596 FRAME BOEING 737 737524 1384721 NM BS 727B S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 RIGHT STATION 727B FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. CUT OUT DAMAGE AT STATION 727B BETWEEN S-8 AND S-9, REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080730 EA 2008 7 30 COMA0860309 1 20080626 A 3230 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG BAY FAILED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 917CA 15410 7017 ON APPROACH INTO SYR SELECTED GEAR DOWN AND RECEIVED GEAR DISAGREE WARNING MSG. PERFORMED QRH, MANUALLY EXTENDED GEAR, EMERGENCY DECLARED, ACFT LANDED SAFELY. REMOVED AND REPLACED MLG SELECTOR VALVE. (S) 2 L 7 2 4F RT A21EA 20080730 EA 2008 7 30 COMA0860313 1 20080629 A 3350 59257 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS FAULTY A COMA O OTHER L NO TEST TX TAXI/GRND HDL 1 SO 01 798CA 7348 TWO GREEN AND ONE ORANGE EMERGENCY PATH LIGHTS FAILED TO ILLUMINATE AT ROWS 6, 7 AND 8 DURING TEST. REPLACED INVERTER. (S) 2 L 7 2 4F RT A21EA 20080730 EA 2008 7 30 REX2008F00007 1 20080705 A 2421 755469E IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 FAILED A REXA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 8907A 5186 7907 ON CLIMBOUT RECEIVED NR 2 IDG FAILED, APU FAILED TO START QRH FOLLOWED DECLARED EMERGENCY RETURNED TO FIELD WITH UNEVENT FUL LANDING. OUTSTATION MAINTENANCE PERFORMED OPERATIONAL CHECKS FOR BOTH THE NR 2 IDG AND THE APU PER BOMBARDIER MAINT ENANCE MANUAL AND RETURNED ACFT TO SERVICE. APU PART NUMBER 3800488-3 TSN 6881 CSN 13944 TSI 2047 CSI 3897. (S) 2 L 7 2 4F RT A21EA 20080730 SO 2008 7 30 CHQA200800111 1 20080613 A 3240 429515 CONTROL UNIT EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL BRAKE SYSTEM MALFUNCTIONED A CHQA O OTHER O OTHER NR NOT REPORTED 1 GL 11 281SK 16969 498 145391 CAE311900 FLIGHT 7783, IAD TO PIT. UPON LANDING THE FLIGHT CREW APPLIED BRAKE PRESSURE ALONG WITH DEPLOYING REVERSERS TO SLOW THE ACFT, AND NOTICED DEGRADED BRAKE PERFROMANCE. FULL BRAKING WAS APPLIED WITH LOWERED EFFECTIVENESS UNTIL AT A SLOW TAXI . THE ACFT TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAULT TO THE BRAKE CONTROL UNIT NOT OPERAT ING THE OUTSIDE BRAKE ASSEMBLIES. AFTER REPLACING THE BCU THE AIRCRAFT TAXIED NORMALLY. (S) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080730 EA 2008 7 30 CHQA200800116 1 20080616 A 4990 OIL SYSTEM HONEYWELL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE APU UNDERSERVICED A CHQA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 GL 11 667BR P596 7535 E873066 FLIGHT 5681, IAH TO ELP. WHILE AT CRUISE WITH THE NR2 IDG ON DEFERRAL, THE FLIGHT CREW RECEIVED AN APU OIL TEMP MESSAGE . THE QRH WAS FOLLOWED AND THE FLIGHT DIVERTED TO MAF. WHILE IN MAF MAINTENANCE FOUND THE APU OIL LEVEL WAS LOW AND SE RVICED IT PROPERLY. THE HIGH OIL TEMP BULB WAS ALSO REMOVED, CLEANED AND REINSTALLED. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080730 EU 2008 7 30 COEA0811911 1 20080529 A 5751 S5761006000200 HINGE AEROSP ATR42 ATR42300 8680920 EU RT AILERON CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 911FX 045 FOUND DURING HEAVY CHECK AT COE. FOUND LEVEL 2 CORROSION ON RT AILERON O/B HINGE FITTING ON THE AILERON HAS EXFOLIATING CORROSION. REMOVED AND REPLACED RT AILERON ASSY. (S) 2 H 7 2 4T RT A53EU 20080730 EU 2008 7 30 COEA0801742 1 20080521 A 3411 F2710GE1091A COVER FOKKER F27 F27MK600 4990706 EU RT PITOT TUBE TORN A COEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 13 742FE 10349 ABORTED TAKEOFF. FLT 8777 GEG TO YKM. DURING THE TAKEOFF ROLL THE COPILOT`S AIRSPEED SHOWED NO INDICATIONS. TAKEOFF W AS ABORTED AND THE ACFT TAXIED BACK TO THE RAMP SAFELY. MAINTENANCE FOUND THE PITOT STATIC TUBE HEAD TO BE OBSTRUCTED W ITH A SMALL PIECE OF MATERIAL FROM THE PITOT STATIC TUBE COVER. REMOVED OBSTRUCTION FROM THE END OF CO-PILOT`S PITOT ST ATIC TUBE HEAD AND A PITOT STATIC SYSTEM CHECK WAS PERFORMED. NOTE: THE PITOT STATIC TUBE COVER WAS ALSO REPLACED WITH A NEW COVER AND PLACED WITH THE ACFT`S OTHER PARKING COVERS. (S) 2 H 7 2 4T A817 20080730 WP 2008 7 30 MWEA080083 1 20080606 A 3397 WIRE DOUG DC9 DC981 3022081 WP EMERGENCY LIGHT DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 EMERGENCY FLOOR TRACK RED LIGHTS AT AFT GALLEY ARE INOPERATIVE. INSTALLED WIRE SPLICE. (S) 2 L 7 2 4F A6WE 20080730 EA 2008 7 30 COMA0860288 1 20080615 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 30545 7117 REAR PRESSURE BULKHEAD CRACKED AT THE TOP OF LINTEL FITTING. REPAIRED REAR PRESSURE BULKHEAD AROUND LINTEL FITTING IAW REO 601R-53-61-1230. (S) 2 L 7 2 4F RT A21EA 20080730 EA 2008 7 30 VNAA0804014 1 20080417 A 7500 GG670800053 SENSOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE BLEED TEMP FAILED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 05 705PS 4107 10144 CREW REPORTED AN AFT AND FORWARD LAVATORY RED WARNING MESSAGE DURING TAKEOFF. THE CREW ELECTED TO RETURN TO DAY WHERE T HE ACFT LANDED AND TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE PERFORMED GROUND RUNS AND OPERATIONAL CHECKS. MAIN TENANCE REMOVED AND REPLACED THE RT ACM BLEED TEMP SENSOR IN ACCORDANCE WITH THE ACFT MAINTENANCE MANUAL. OPERATIONAL C HECKS WERE GOOD. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E00063EN 20080730 NM 2008 7 30 SWAA084002 1 20080717 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 778SW 27883 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080730 2008 7 30 SWAA084003 4 20080715 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 786SW 29811 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800692 1 20080708 A 5311 6546525 FRAME BOEING 737 737524 1384721 NM BS 380 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14629 27533 FRAME CRACKED STATION 380 AT S-9 RIGHT. REPAIRED FRAME PER EA 5310-04498 OP2. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800744 1 20080604 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 349-669 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 LT CABIN SIDE SEAT RAILS HAVE CORROSION DAMAGE FS 349.00 TO 669.40. REPAIRED DAMAGED AREAS OF CABIN SIDE WALL SEAT RAILS IAW SRM 53-21-49 AND SRM 53-31-49. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800724 1 20080601 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 COCKPIT FLOORBEAM AFT LAND CORRODED. FWD SIDE OF FS 280 LBL9-RBL9. (B) ALL WORK DONE IAW SRM 51-40-06. (A) 2 L 7 2 4F RT A21EA 20080718 EU 2008 7 18 08FDEA02363 1 20080620 A 5321 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU CABIN DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 MAIN CABIN FLOOR PANEL 251 AH IS DAMAGED. FABBED A NEW FLOOR PANEL 251 AH USING THE OLD PANEL AS A TEMPLATE; POTTED; CU RED AND SANDED EDGES; POTTED AND CURED INSERTS; APPLIED NON-SKID TAPE AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005, R EV F. 2 L 7 2 4F RT A35EU 20080718 EU 2008 7 18 08FDEA02557 1 20080629 A 5415 A5461175400200 FITTING AIRBUS 310 A310203 3930313 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 423FE 281 RT PYLON LOWER LUG FITTING, RIB 18, HAS 4 EA HOLES WITH CORROSION REMOVED LEVEL 1 CORROSION AND REPAIRED RIB 18 FITTING IAW FED EX EA 6-5450-121280, RELEASE DATE 29 MAY, 2008 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 2008UALA03448 1 20080617 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 672UA 30027 EEL LIGHT AT SEAT 33H INOPERATIVE. FOUND LOOSE CONNECTION. SECURED CONNECTION. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080718 NM 2008 7 18 2008UALA03468 1 20080619 A 5610 SEAL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT WINDOW NOISY A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 653UA 25391 WINDOW SEAL BEGAN TO SQUEAL LOUDLY. CAPTAIN REPORTED, NOISE IS TOO LOUD TO OPERATE SAFELY, RTFL. REPLACED SEAL. APPLIE D SEALANT AROUND FILLET. PERFORMED PRESSURE CHECK. ALL CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20080718 NM 2008 7 18 2008UALA03471 1 20080618 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW O2 LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 849UA 1649 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED CREW O2 TO FULL, NO LEAKS WERE NOTED AT TIME OF S ERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080718 NM 2008 7 18 SWAA083552 1 20080626 A 5311 6545805 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083609 1 20080629 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083610 1 20080629 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083606 1 20080629 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 27R CORRODED AT BS 538. REMOVED AND REPLACED STRINGER SECTION PER SRM. 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 08FDEA02355 1 20080620 A 5330 SKIN AIRBUS 300 A300B4622 3930401 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 719FD 388 RT LOWER FUSELAGE AFT OF FR 16A ABOVE STRINGER 40R HAS A 1 INCH GOUGE. INSTALLED DOUBLER REPAIR IAW SRM 53-12-12 FIG 20 1, PAINTED IAW SRM 53-23-10. STRUCTURAL REPAIR INSPECTION INTERVALS IAW SRI 53-12-12-2-003-0. 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 SWAA083612 1 20080629 A 5310 6546818 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 907 TO BS 927, LBL 65. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083554 1 20080626 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500C, STR 26R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083579 1 20080627 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 EEPLS END CAP LOOSE AT ROW 1 ABC. SECURED END CAP PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083584 1 20080629 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083585 1 20080629 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 M7K2008F00023 1 20080612 A 2612 9550177130 FIRE DETECTOR UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE INTERMITTENT E M7KA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 19 809MH 572 3927 46047 DURING FLIGHT, PILOT REPORTED THAT THE FIRE LIGHT ILLUMINATED IN A FLICKERING FASHION, FLIGHT WAS ABORTED. NO EVIDENCE O F FIRE OR HEAT WAS FOUND AND TROUBLESHOOTING PROCEDURES OF THE MM WERE FOUND INEFFECTIVE AT DISCOVERING WHICH OF (3) DE TECTORS WAS FAULTY. RETORQING THE TERMINAL CONNECTIONS HAD RESOLVED A SIMILAR PROBLEM WITH THIS ENGINE SEVERAL WEEKS PR EVIOUSLY. IN THIS CASE PROBLEM REMAINED INTERMITTENTLY DURING SUBSEQUENT SYSTEM CHECKS. ALL (3) DETECTORS WERE REPLACED WITH NO FURTHER DEFECT NOTED. SUGGEST A DIFFERENT DESIGN DETECTOR OR QC IMPROVEMENTS BE MADE WITH THIS PART AS SEVERAL INSTANCES OF FALSE FIRE INDICATIONS HAVE SHAKEN CONFIDENCE IN SYS. IT IS QUESTIONABLE WHY THERE IS EVEN SUCH A SYS ON A 1 G 7 2 3U 3 U H9EU E00054EN 20080718 2008 7 18 SWAA083561 4 20080626 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083596 1 20080629 A 5315 147A5504 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 769SW 30588 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, RBL 4 TO LBL 0. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 M7K2008F00013 1 20080512 A 6220 350A31191700 STARFLEX UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE M/R HUB ASSY CRACKED A M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 847MH 499 4266 23416 (REF 0505084266) DURING ROUTINE INSP, ADHESIVE BEAD FOR A STAR ARM END BUSHING WAS FOUND CRACKED. FURTHER EXAMINATION UT ILIZING A SOAP WATER DETECTION METHOD REVEALED RELATIVE MOTION BETWEEN BUSHING AND STAR ARM END. WITH ROTOR HUB SLEEVES REMOVED, BUSHING COULD BE MOVED MANUALLY. A SECOND BUSHING WAS FOUND LOOSE. A SERVICEABLE REPLACEMENT STARFLEX WAS INS TALLED. THIS IS A DEFECT THAT RECENTLY HAS BECOME MORE COMMON THAN IN THE PAST. SUFFGEST A DIFFERENT ADHESIVE BE UTILI ZED OR STAR ARM ENDS AND BUSHINGS BE DESIGNED TO HAVE A LARGER ADHESIVE BONDING SURFACE SUCH AS ADDING INNER BUSHING AND OUTER STAR ARM END SPLINING. THERE WAS NO EVIDENCE OF ANY IMMINENT FAILURE FOR THE PART OR EXCESSIVE PLAY DEVELOPMENT 1 G 7 2 3U 3 U H9EU E00054EN 20080718 NM 2008 7 18 SWAA083492 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 EA 2008 7 18 A6WA200840437 1 20080520 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 319-349 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 CORROSION ON ANGLE OF PAX DOOR LOWER SILL BETWEEN FS 319 TO FS 349, WL 72. CORROSION ON ANGLE REMOVED IAW SRM 51-21-06. (A) 2 L 7 2 4F RT A21EA 20080718 EA 2008 7 18 A6WA200840441 1 20080523 A 4910 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA APU BAY CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 APU ENCLOSURE CRACKED. APU ENCLOSURE REPAIR DONE IAW REO 601R-49-11-071. (A) 2 L 7 2 4F RT A21EA 20080718 EU 2008 7 18 M7K2008F00045 1 20080623 A 6220 704A33640021 SPACER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE SCISSOR LINK WORN E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 821MH 1499 4134 23319 DURING ROUTINE INSP, SPACER WAS FOUND WITH EXCESSIVE WEAR AT ENDS WHERE IT MAKES SCISSOR LINK BUSHING CONTACT. POSSIBLE DIRT ACCUMULATION IN THE GREASE WAS A FACTOR IN THE WEAR. THIS IS A COMMON FAILURE FOR THIS PART. SUGGEST THIS PART B E KEPT CLEAN IN SANDY ENVIRONMENTS. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080721 WP 2008 7 21 UPS08852427 1 20080528 A 5522 SKIN DOUG DC8 DC873F 302199F WP RT ELEVATOR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 RIGHT ELEVATOR UPPER SKIN IS DENTED AND GOUGED, FWD OF GEARED TAB. REMOVED DAMAGE, FABBED AND INSTAL LED REPAIR DOUBLER IAW SRM 55-2-0, 55 51-1-8, 53-1-8, 55-2-0 FIG 10. 2 L 7 4 4F RT 4A25 20080721 NM 2008 7 21 UPS08M52437 1 20080606 A 3350 LIGHT DOUG MD11 MD11F 3023600 NM L1 DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 276UP 48579 INSPECTION TYPE:PS3 EMERGENCY LIGHT ON L1 DOOR INOP. RELAMPED IN REF TO 33-50-00, OP CHECK GOOD. 2 L 7 3 4F RT A22WE 20080721 NM 2008 7 21 SWAA083518 1 20080625 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND STRINGER 22R CRACKED AT BS 540. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 2008UALA02692 1 20080506 A 3510 6350A33XA BOTTLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CREW O2 LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 941UA 26676 CREW OXYGEN SYSTEM LOW. CREW COMMENTS: CREW O2 READS 1250. SUSPECT PRE FLIGHT CHECKS. SERVICED OXYGEN SYSTEM. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080721 NM 2008 7 21 2008UALA02702 1 20080508 A 2721 658D1005 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RUDDER TRIM FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 647UA 25284 RUDDER TRIM FAILED TO TRIM IN EITHER DIRECTION. SUSPECT FAULTY ACTUATOR. REPLACED RUDDER TRIM ACTUATOR IAW MM 27-21-11 . AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080721 NM 2008 7 21 SWAA083520 1 20080625 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083530 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080721 CE 2008 7 21 GLB2008F00002 1 20080714 A 5311 FRAME BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA FS 164 S9AR CRACKED A GLBA O OTHER O OTHER NR NOT REPORTED 1 NM 21 192GL UE192 FRAME CRACKED AT STRINGER CUTOUT AT FS 164 STRINGER 9AR APPROXIMATELY 1.25 INCH IN LENGTH. MAINT REPAIRED CRACK AT STRI NGER RELIEF HOLE FS 164, STRINGER 9R, REPAIR APPROXIMATELY 5.5 INCH X 2.5 INCH. 2024-T3, .071. RII INSPECTION COMPLIED WITH IAW TASKCARD 8.2.1. (K) 2 L 7 2 4T 3 T RT A24CE E2NE 20080721 NM 2008 7 21 SWAA083738 1 20080707 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE STRINGER 13L CRACKED AT BS 301. REPAIRED STRINGER PER SRM & BAC DRAWING. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 USAA920081626 1 20080822 A 5320 6546812 FLOOR SUPPORT BOEING 737 7373G7 1384595 NM BS 986-1006 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 SAL - C19 MAJOR REPAIR GALVANIC CORROSION ON CABIN FLOORBEAM BETWEEN BS 986.5 AND BS 1006, LBL 15. REPAIRED CABIN FLOOR BEAM BETWEEN BS 986.5 AND BS 1006, LBL 15 IAW SRM 51-70-12. 2 L 7 2 4F RT A16WE 20080919 EU 2008 9 19 USAA920081635 1 20080906 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 669AW 1792 FLT 380 - PHX - LAX EMERGENCY EQUIPMENT FORWARD JUMPSEAT FLIGHT ATTENDANT FLASHLIGHT NOT BLINKING FOR RECHARGE. FLASHLI GHT WORKS WHEN PULLED OUT. MX R&R THE FLASHLIGHT BATTERY. OPS CHECK WAS NORMAL. 2 L 7 2 4F RT A28NM 20080919 EU 2008 9 19 USAA920081609 1 20080902 A 3350 SWITCH AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AW 076 FLT 352, LT SIDE OVERWING EMERGENCY LIGHTS WILL NOT TEST. MX RESET OVERWING DOOR EMERGENCY CUT OUT SWITCH. OPS CHEC K GOOD. 2 L 7 2 4F RT A28NM 20080919 NM 2008 9 19 USAA920081627 1 20080822 A 5320 6977019 WEB BOEING 737 7373G7 1384595 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 SAL - C19 MAJOR REPAIR - GALVANIC CORROSION ON WEB AT BS 1016, RBL 3, WL 208. REPAIRED WEB AT BS 1016, RBL 3, WL 208 IA W B737 SRM TYPICAL REPAIR 51-70-03. 2 L 7 2 4F RT A16WE 20080919 EU 2008 9 19 USAA920081624 1 20080827 A 5540 D5537131800200 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 660AW 1234 SAL - BC6 MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 4. REPLACED RUDDER HINGE FITTING NR 4 IAW A320 SRM 5 1-72-17. 2 L 7 2 4F RT A28NM 20080919 EU 2008 9 19 UPS08153237 1 20080820 A 5321 B5327078100100 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 138UP 0821 INSPECTION TYPE:1C MAIN CARGO FLOOR PNL 252SJ HAS FIELD REPAIRS. REPAIRED MAIN CARGO FLOOR PNL 252SJ REF A300-600 SRM 5 3-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20080919 EU 2008 9 19 UPS08153238 1 20080820 A 5321 B5327077400200 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 138UP 0821 INSPECTION TYPE:C1 MAIN CARGO FLOOR PNL 251XJ AFT HAS FIELD REPAIRS. REPAIRED MAIN CARGO FLOOR PNL 251XJ REF A300-600 S RM 51-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20080919 EA 2008 9 19 A6WA200840561 1 20080810 A 2751 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A A6WA O OTHER N FALSE WARNING AP APPROACH 1 GL 31 448AW 7814 FLAPS FAIL AT 20 DEGREES ON APPROACH. R&R FLAP PDU PER AMM 27-53-01, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080919 EA 2008 9 19 A6WA200840580 1 20080821 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 465AW 7893 FLAPS FAILED AT 20 DEGREES WITH FLAPS FAIL CAUTION AFTER TAKEOFF. LANDED AT FLAPS 20 AFTER COMPLYING WITH QRH. COMPLIE D WITH AWAC SUPP 98-018B RESET, FLAPS RESET OK. RESET. 2 L 7 2 4F RT A21EA 20080919 NM 2008 9 19 ASAA0843442 1 20080902 A 5753 65C2631026 SKIN BOEING 737 737490 1384715 NM RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 RIGHT I/B MID FLAP LOWER SURFACE T/E WEDGE HAS MULTIPLE SMALL DENTS BETWEEN MIDDLE TRACKS. REPAIRED RIGHT I/B MID FLAP WEDGE LOWER SURFACE DENTS IAW B737 400 SRM 51-30-01 PG 13. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0843472 1 20080902 A 5330 6518420726 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 DENT FWD LAV RT SIDE BS 310-316 BETWEEN STR 23 AND 26R. DIMENSIONS OF DENT AER DEPTH .148 WIDTH 6.1" HEIGHT 5.4" AND FO UND TO BE OUT OF LIMITS PER SRM 53-00-01. REPAIRED UPPER SKIN PANEL IAW SRM 53-00-31 REPAIR 31. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0843444 1 20080902 A 5753 65370611 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 LT WING I/B UPPER TRAILING EDGE PANEL HAS A SMALL DENT 85 INCHES O/B OF I/B END 9 INCHES FWD OF TRAILING EDGE. REPAIRED LT WING I/B UPPER TRAILING EDGE PANEL IAW B737 400 SRM 51-70-10 REPAIR. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0843445 1 20080902 A 5753 654645170A SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 LT WING NR 3 SPOILER UPPER SURFACE HAS 2 EA INVERTED DENTS. REPAIRED NR 3 SPOILER UPPER SURFACE IAW B737 400 SRM 51-70- 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080919 EA 2008 9 19 COMA086372 1 20080829 A 5320 601R350313 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 589-605 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 420CA 7451 UNDERFLOOR CAP BEAM AT LBL 9 AMD LBL 27 BETWEEN FS 589 AND FS 605 HAS CORROSION AROUND NUT PLATES HOLE. PERFORMED REPAI R TO LBL 27 BEAM PER CRJ SRM 53-00-43 PG 201 TO 208 AND COMAR SR99-5140-0001. 2 L 7 2 4F RT A21EA 20080919 NM 2008 9 19 ASAA0853471 1 20080902 A 2421 7588429101 OIL FILTER BOEING 737 737890 1384527 NM IDG ACTIVATED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 583AS AAAH005134 35681 NR 1 ENG IDG DPI FOUND EXTENDED ARCTIC VERIFIED 1ST OCCURRENCE LAST 365 DAYS. ACCOMP FIM 24 11 TASK 803. REMOVED INSP & REPLACED CHG & SCAVENGE FILTERS REF MM 24-11-41. RESET DPI LK & OPS NORMAL REF MM 24-11-41. GROUND VERIFICATION SUCC ESSFUL. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAASB08039 1 20080602 A 2782 65C3805914 ACTUATOR BOEING 737 7374B7 1384702 NM L/E SLAT LEAKING A USAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 19 442US 48232 48232 24841 CLT FLT 1457 - ON CLIMBOUT FROM CTL, EN ROUTE TO FLL, CREW RECEIVED A LEADING EDGE SLAT INDICATION LIGHT. UNSURE OF WHI CH SLAT GAVE THE INDICATION, CAPTAIN DECIDED TO RETURN TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EME RGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 4 SLAT ACTUATOR AND ROD END PER MM 27-81-41-4. LEAK CHECK AND OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 MASA200800463 1 20080611 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75993 7372 FLT 7104 ORD-CWA AFT CABIN CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAA920081245 1 20080617 A 5754 SKIN BOEING 757 7572B7 1384964 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 929UW 27144 BFM - C2 - MAJOR REPAIR - LT WING LEADING EDGE SLAT NR 3 AFT WEDGE UPPER AND LOWER SKIN APPROX 28 INCHES FROM INBOARD AN D 8 INCHES FROM AFT EDGE HAS DELAMINATION. REPAIRED LT WING LEADING EDGE SLAT NR 3 AFT WEDGE UPPER AND LOWER SKIN IAW B 757 SRM 57-43-02 & 51-70-10. (S) 2 L 7 2 4F RT A2NM 20080729 NM 2008 7 29 USAA920081273 1 20080625 A 5310 652072354 DOOR FRAME BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 530AU 24412 PIT - FORWARD PRESSURE BULKHEAD - MAJOR REPAIR - FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT LOWER DOOR STOP. ST 492, S- 24R, CRACK MEASURES .5 INCH, FOUND WITH HPEC MARKED ENDS. REPAIRED FWD CARGO DOOR CUTOUT AFT FRAME AT LOWER DOOR STOP S T 492, S-24R IAW EA 111238. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 KCSA081303 1 20080628 A 5315 FLOORBEAM BOEING 747 747122 1384872 NM BS 440 CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 UPPER DECK FLOORBEAM WEB HAS A CHAFED AREA AT STA. 440, LBL 36. (B) 2 L 7 4 4F RT A20WE 20080729 EA 2008 7 29 TRAX200800869 1 20080703 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 861AS 7445 LT SIDE FS 621 FLOORBEAM ON FWD SIDE OF AFT PRESSURE BULKHEAD IS CRACKED. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800900 1 20080710 A 2560 GLOWSTRIP CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 717EV 10088 PHOTOLUMINESCENT FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING MISSING AT ROW 14.REPLACED AND SECURED GLOWSTRIP, DEFERRE D CLEAR OK FOR SERVICE. 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800788 1 20080614 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA BS 319 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 CABIN FLOOR SILL FS 319.70 AT RBL 45 HAS CORROSION DAMAGE. BLENDED CORRODED AREAS ON CABIN FLOOR SILL FS319.70 AT RBL 45 . PER SRM SRM51-21-06. KR17389 PERFORMED UT THICKNESS MEASUREMENT OF THE REWORKED AREA OF THE FLOOR SILL PER NDTM 51-20- 004. MINIMUM THICKNESS IS .030" 061408. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 ASAA0843148 1 20080612 A 5313 65465548 STRINGER BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 DOUBLE DRILLED HOLE FOUND ON STRINGER FLANGE. REPAIRED PER SRM 53 00 01. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800897 1 20080709 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 922EV 7822 FS 280.00 CLIP AT LBL 9 O/B SIDE IS CRACKED 1/2" LONG IN UPPER RADIUS. OPEN (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 ASAA0843159 1 20080506 A 5330 65479551 BEAR STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 AFT PIT BILGE STA 787 TO STA 793 RBL 23R BEAR STRAP HAS TWO AREAS OF CORROSION. REFER TO NIR 5097068 FOR REPAIR OF BEAR STRAP BS 787 TO BS 793 RBL 23. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843160 1 20080501 A 5754 65C26603192 SLAT BOEING 737 7374Q8 138447Q NM NR 4 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 NR 4 SLAT OUTBOARD END DELAMINATED. REPAIRED SLAT PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800684 1 20080707 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM BS 827 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 RIGHTHAND STATION 827 FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. CUT OUT DAMAGE AT STATION 827 BETWEEN S-8 AND S-9, REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080730 EU 2008 7 30 COEA0801902 1 20080702 A 2121 EVAC2423FD FAN AEROSP ATR42 ATR42320 8680930 EU NR 1 A/C PACK FAILED A COEA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 NM 13 902FX 175 SMOKE IN ACFT FLT 8783 GTF TO GPI. DURING TAXI TO PARKING AFTER THE FLIGHT, ELECT SMOKE LIGHT ILLUMINATED AND THE CREW SMELLED SMOKE. SHUT DOWN AND TURNED OFF ALL POWER. CONTINUED TO TAXI TO PARKING AREA WITHOUT INCIDENT. REMOVED & REPL ACED NR 1 GROUND COOLING FAN. (S) 2 H 7 2 4T RT A53EU 20080730 EA 2008 7 30 REX2008F00005 1 20080707 A 7830 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER FALSE ACTIVATION A REXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 8788A 7877 L REV CAUTION IN FLIGHT AT FL250. COMPLETED QRH. LANDED AT KIND, THE NEAREST SUITABLE AIRPORT. DECLARED EMERGENCY AND LANDED UNEVENTFULLY. MAINTENANCE FOUND THRUST REVERSER TO BE STOWED PROPERLY. DEFERRED THE THRUST REVERSER FOR GIVING FALSE UNLOCKED INDICATION. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F RT A21EA 20080717 NM 2008 7 17 SWAA083171 1 20080610 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083540 1 20080626 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 281WN 36528 EEPLS LENS LOOSE AT ROW 3 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083546 1 20080626 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 08FDEA02551 1 20080628 A 5343 69650451 ANGLE BOEING 727 727225 1384077 NM RT MLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 RT MLG STA 940 UPPER BEAM ANGLE CRACKED IN RADIUS. FABRICATED NEW ANGLE. REF BOEING DWG 69-65045. MATCH DRILLED REF D WG 69-65045. INSTALLED ANGLE. REF SRM 51-30-2. THIS IS CLASSFIED A MINOR REPAIR. 2 L 7 3 4F A3WE 20080718 NM 2008 7 18 08FDEA02553 1 20080628 A 2612 656020916 CONTROL UNIT BOEING 727 7272S2F 1384O81 NM FIRE PROTECTION INOPERATIVE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 215FE 22936 IMMEDIATELY AFTER ROTATION, FIRE BELL ACTIVATED AND FIRE WARN LIGHTS ILLUMINATED. COULD NOT CANCEL BELL. FINALLY PULLE D "FIRE BELL" CIRCUIT BREAKER. RAN FIRE TEST ON ENGINES AND MAIN CARGO COMPARTMENT. TESTED OK. REMOVED AND REPLACED E NGINE FIRE PROTECTION CONTROL UNIT IAW B727 26-11-000-4. OPS CHECKS NORMAL AT THIS TIME. A/C OK FOR CONT SERVICE. REM OVAL/INSTALLATION OFF MFG 65-60209-16, POS ONL SRL D00032 TAG B25254. 2 L 7 3 4F A3WE 20080718 NM 2008 7 18 08FDEA02126 1 20080603 A 5100 NONE DOUG MD11 MD11F 3023600 NM IAW SRM NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 CENTER CARGO, STA 1791 LEFT LONGERON 37 FOUND WITH EXISTING SPLICE REPAIR. CENTER CARGO STA 1791 LEFT LONGERON 37 FOUND WITH EXISTING SPLICE REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-10-00 FIGURE 2 VOLUME I FEDEX EO NR 1-5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG, MD11, REPAIR CATALOG AND TRACKING REQUIREMENTS, HAS BEEN ACCOMPLISHED . REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 WP 2008 7 18 08FDEA02088 1 20080602 A 5730 ARB126823R PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 LEFT WING INBD LOWER L/E PANEL 518 FB IS CHAFING AROUND THE CONTACT SURFACE. REPAIRED LEFT WING INBD LOWER PANEL ARB 12 68-23 BY FABRICATING AND BONDING THE PAN DOUBLER IAW FEDEX EA 8-5720-116990; TIMCO TPS - 1001, REV E, AND DAC DWG ARB 12 68. FEDEX EA 8-5720-116990 TITLED " WINGS - LT WING LEADING EDGE LOWER ACCESS PANEL 518 FB - REPAIR". 2 L 7 3 4F RT A22WE 20080718 EU 2008 7 18 08FDEA02362 1 20080620 A 5321 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU CABIN DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 MAIN CABIN FLOOR PANEL 232 HG IS DAMAGED. FABBED A NEW FLOOR PANEL 232 HG USING THE OLD PANEL AS A TEMPLATE; POTTED; CU RED AND SANDED EDGES; POTTED AND CURED INSERTS; APPLIED NON-SKID TAPE AND PART MARKED THE PANEL IAW FEDEX DWG SRZ 25-00 5, REV F. 2 L 7 2 4F RT A35EU 20080718 EU 2008 7 18 08FDEA02365 1 20080620 A 5321 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU CABIN DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 MAIN CABIN FLOOR PANEL 251 XG IS DAMAGED. FABBED A NEW PANEL 251 XG BY USING THE OLD PANEL AS A TEMPLATE; POTTED; CURE D AND SANDED EDGES; POTTED AND CURED INSERTS; APPLIED NON-SKID TAPE AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005, REV F. 2 L 7 2 4F RT A35EU 20080718 EU 2008 7 18 08FDEA02366 1 20080620 A 5321 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU CABIN DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 MAIN CABIN FLOOR PANEL 232 NG IS DAMAGED. FABBED A NEW FLOOR PANEL 232 NG USING THE OLD PANEL AS A TEMPLATE; POTTED; CU RED AND SANDED EDGES; POTTED AND CURED INSERTS; APPLIED NON-SKID TAPE AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005, RE V F. 2 L 7 2 4F RT A35EU 20080718 EU 2008 7 18 08FDEA02555 1 20080629 A 5511 A5517713620000 RIB AIRBUS 310 A310203 3930313 EU HORIZONTAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 423FE 281 RT HORIZONTAL TRAILING EDGE SUPPORT RIB AT RIB 11 HAS CORROSION AROUND FASTENER HOLES ON LOWER AND UPPER FLANGES REMOV ED LEVEL 1 CORROSION AND INSTALLED FORMED SECTION REPAIR ON RT HORIZONTAL TRAILING EDGE BETWEEN RIB 11 AND RIB 12 IAW A3 10-200 SRM 55-13-11, FIG 1 AND 51-71-40, FIG 201. 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 2008UALA03035 1 20080527 A 2130 91252ZC7C4001 RELAY BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE FAULTY A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 364UA 24533 PRESSURIZATION LOSS, RTFL. FAULTY R3 RELAY. REPLACED R3 RELAY. 2 L 7 2 4F 4 F RT A16WE E21EU 20080718 EU 2008 7 18 2008UALA03063 2 20080528 A 7310 219946TYP FUEL FILTER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 ENGINE UNKNOWN A UALA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION TO TAKEOFF 1 WP 29 383UA 24658 FUEL FILTER BYPASS NR 2 ON TAKEOFF, LIGHT WENT OUT WHEN POWER REDUCED, RTFL. FUEL FILTER. REPLACED FUEL FILTER. 2 L 7 2 4F 4 F RT A16WE E21EU 20080718 EU 2008 7 18 08FDEA02558 1 20080629 A 5415 A5461175400200 FITTING AIRBUS 310 A310203 3930313 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 423FE 281 LT PYLON LOWER LUG FITTING, RIB 18, HAS PITTING CORROSION ON 4 FASTENER HOLES REMOVED LEVEL 1 CORROSION AND REPAIRED LT PYLON RIB 18 LUG FITTING IAW FED EX EA 6-5450-121279, RELEASE DATE 29 MAY, 2008 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 08FDEA02110 1 20080603 A 5100 NONE DOUG MD11 MD11F 3023600 NM IAW SRM NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 590FE 48505 EXISTING REPAIR, MAIN DECK EXISTING SEAT TRACK SPLICE REPAIR FOUND AT STA 1235, X = - 47.5. EXISTING REPAIR AT MAIN DEC K SEAT TRACK SPLICE REPAIR AT STA 1235, X = -47.5 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-70-00 FIGURE 1 VOLUME I FEDEX EO NR 1- 5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG - MD11 - REPAIR CATALOG AND TRACKING REQUIREMENT S 14 CFR 121.707, HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 WP 2008 7 18 08FDEA02162 1 20080605 A 5330 NCA63123 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 FUSELAGE EXTERNAL SKIN HAS A DENT ON THE LEFT SIDE AT APPROX FS 632 BETWEEN STRINGERS 39L AND 40L. REPAIRED DAMAGE AT T HE LEFT SIDE FUSELAGE APPROX STA 632 BETWEEN L39L AND L40L IAW DC/MD-10 SRM 53-20-00; VOL I; FIG 6; SHEET 3. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 08FDEA02237 1 20080612 A 5340 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 598FE 48597 MAIN DECK CARGO DOOR SPOOL FITTING NR 3 FOUND 3RD LAYER CRACK INDICATIONS AT ALL FITTING MOUNTING BOLT HOLES. MAIN DECK CARGO DOOR SPOOL FITTING NR 3. REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSH ING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080919 NM 2008 9 19 SWAA084858 1 20080903 A 5311 6546543 FRAME BOEING 737 7373T0 1384582 NM BS 706 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084859 1 20080903 A 5315 6546812 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, LBL 12. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084860 1 20080903 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084861 1 20080903 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 DURING SCHEDULED HC1 CHECK, RT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084876 1 20080904 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 637 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 637, LBL 70. REMOVED AND REPLACED WEB PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084883 1 20080904 A 5311 6546558 FRAME BOEING 737 7375H4 138449D NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084884 1 20080904 A 3233 65448106 ACTUATOR BOEING 737 7373H4 1384600 NM LT MLG FAULTY A SWAA O OTHER J WARNING INDICATION CL CLIMB 1 SW 29 616SW 27699 UPON LANDING GEAR RETRACTION LT MLG RED LIGHT REMAINED ILLUMINATED WITH GEAR RETRACTED. RED AND GREEN LIGHTS ON WITH GE AR IN OFF POSITION. REMOVED AND REPLACED LT MLG UPLOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084885 1 20080904 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 R2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084931 1 20080908 A 3350 6104789 BATTERY PACK BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED MV2 CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS STAY ILLUMINATED. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084936 1 20080908 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 767 S21R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080922 WP 2008 9 22 UPS08853155 1 20080727 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FS 1120 RBL 14 CRUSHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 MAIN CABIN, FLOOR PNL HAS CRUSHED HONEYCOMB STA 1120 RBL 14. FABRICATED AND REPLACED FLOOR PNL IAW E O DC8-5320-9691C. 2 L 7 4 4F RT 4A25 20080922 NM 2008 9 22 2008UALA05405 1 20080821 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 L-4 DOOR LOWER GATE LOWER EDGE HAS MATERIA L LOSS AND GOUGES. UNKNOWN DAMAGE. REMOVED DAMAGED LWR GATE AND INSTALLED N EW GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080922 NM 2008 9 22 2008UALA05410 1 20080821 A 5414 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 NACELLE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 822UA 948 21AUG ORD CF -T : NR 2 ENG RIGHT SIDE FAN COWL GOUGED APPROX 3 INCHES FROM REAR ABOUT 3 O'CLOCK POSITION. ACCOMPLISHED INTERIM REPAIR PER UA-EVA-71852, NO DELAMINATION PRESENT & APPLIED SPEED TAPE. RECHECK REPAIR AT NEXT A01 CHECK, REPAIR WITHIN 500 FLIGHT HOURS NOT TO EXCEED PTT 34736. 2 L 7 2 4F 4 F RT A28NM E40NE 20080922 2008 9 22 ZZDA2008155 4 20080826 A 2565 D29982225 SLIDE BOEING 717 717200 1383700 NM R1 DOOR DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 958AT 55020 R1 SLIDE PACK COVER LOOSE AND COVER RIPPED BY CATERING. SLIDE COVER DAMAGED AND SLIDE PIN PULLED OUT OF R1 SLIDE. REMO VED AND REPLACED R1 SLIDE ASSY AND SLIDE COVER ASSY REF MM 25 61. 2 L 7 2 4F TR A6WE 20080922 NM 2008 9 22 CALA0800832 1 20080825 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM BS 827 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14628 27532 LEFT FRAME IS CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 827 BETWEEN STRINGERS 8 AND 9. AC COMPLISHED AIR CONDITIONING (A/C) FUSELAGE CRACK INTERIM REPAIR AT STATION 827 PASSENGER SERVICE UNIT ATTACH BRACKETS BE TWEEN S-8 TO S-9 PER ECRA 5310-04827. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 CALA0800833 1 20080826 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM BS 867 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14628 27532 LEFT FRAME IS CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 867 BETWEEN STRINGERS 8 AND 9. AC COMPLISHED LEFT FRAME REPAIR AT STATION 867 BETWEEN STRINGER 8 AND 9 PER EA5310-04498 OP 2. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 08FDEA02241 1 20080612 A 5340 ACA72241 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 598FE 48597 AFTER REAMED TO MAXIMUM ALLOWABLE DIAMETER 0.52 INCH ON MAIN DECK CARGO DOOR SPOOL FITTING NR 2 MOUNTING BOLT HOLE "D" F OUND 2ND LAYER OF DOOR JAMB WITH CRACK INDICATION. REPAIR CARRIED OUT AS PER FEDEX EA NR 1-5310-122486, TITLE: FUSELAGE MAIN CARGO DOOR LOWER JAMB BORE HOLE AT STA = 645 - REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 WP 2008 7 18 08FDEA02250 1 20080612 A 5410 AJC74154 RING DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 ON THE NR 2 ENGINE AT THE 5 O'CLOCK POSITION; THE COWL RING COVERING THE NR 2 ENGINE ADAPTER RING IS CHAFED THROUGH BY T HE RIGHT FAN COWL. REMOVED COWL RING PANEL IAW DC/MD-10 SRM 51-35-01; VOL II. MATERIAL ID FOR A NEW COWL RING PANEL IS 2024-T3, 0.063 IAW DC/MD-10 SRM 55-35-01; PGS 49 AND 50. ALODINED AND PRIMED THE NEW COWL RING PANEL IAW DC/MD-10 SRM 51-21-01; VOL II. PART MARKED THE NEW COWL RING PANEL IAW FEDEX GMM 7-0-1001. INSTALLED THE NEW COWL RING PANEL IAW DC /MD-10 SRM 51-35-01; VOL II. PAINTED THE NEW COWL RING PANEL IAW DC/MD-10 SRM 51-21-02; VOL II. 2 L 7 3 4F RT A22WE 20080718 EU 2008 7 18 08FDEA02252 1 20080613 A 7120 MOUNT AIRBUS 310 A310203 3930313 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 NR 2 ENGINE FORWARD MOUNT SPIGOT HOLE CORRODED REMOVED LEVEL 1 CORROSION. ACCOMPLISHED BUSHING REPAIR ON NR 2 ENGINE FO RWARD MOUNT SPIGOT HOLE PER FED EX EA6-5450-121268. 2 L 7 2 4F RT A35EU 20080718 EU 2008 7 18 08FDEA02255 1 20080613 A 5330 A53611658200 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT SIDE FUSELAGE SKIN BETWEEN FRAME 17 TO 18 AND BETWEEN STRINGERS 28 TO 3 1 LT AT FWD SIDE OF SKIN BUTT SEAM, THE REPAIR DOUBLER MEASURES 9.2 INCH BY 7.5 INCH. REPAIR NOT IAW DWG 912188 AND AIR BUS RAS AS.128/93 ISSUE B. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT REPAIR ON LEFT SIDE FUSELAGE SKIN BETWEEN FRAM E 17 TO 18 AND BETWEEN STRINGERS 28 TO 31 LT AT FWD SIDE OF SKIN BUTT SEAM IAW FED EX EA6-5310-121274. THIS IS AN AIR BUS REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080718 EU 2008 7 18 2008UALA03435 1 20080617 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 411UA 464 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. CREW COMMENTS: O2 IS 1480 PSI. SERVICED CREW O2 TO FULL, NO LEAKS WERE NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080718 NM 2008 7 18 2008UALA03442 1 20080617 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 DENT TO LOWER FUSELAGE AT STA 1720 JUST BELOW EMPENNAGE ACCESS DOOR. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE. INSTA LLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080718 NM 2008 7 18 2008UALA03444 1 20080617 A 5315 111T5007 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 CABIN FLOORBEAM AT BS 805, RBL 11 IS CORRODED. REMOVED DAMAGE, FABRICATED NEW REPAIR AND INSTALLED IAW SRM 53-00-51 AND SRM 51-40-02. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080718 NM 2008 7 18 2008UALA03447 1 20080617 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 672UA 30027 EEL LIGHT AT SEAT 25H INOP. FOUND LOOSE CONNECTION. SECURED CONNECTION. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080718 NM 2008 7 18 2008UALA03453 1 20080618 A 2160 8102003 CONTROLLER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CABIN TEMP FAILED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 221UA 30552 PACK MODE L LEFT PACK AIR CYCLE MACHINE HAS FAILED, OR LEFT ECONOMY COOLING VALVE FAILED OPEN, OR BOTH LEFT CONDENSOR IN LET TEMP SENSORS FAILED. LEFT PACK IS OPERATING IN A NON-NORMAL MODE (HEAT EXCHANGER ONLY COOLING MODE). ADVISORY CREW COMMENTS: PACK MODE LEFT. SUSPECT FAULTY CABIN TEMPERATURE CONTROLLER SOFTWARE. REPLACED LT CABIN TEMPERATURE CONTRO LLER SOFTWARE IAW 21-61-01 OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080718 NM 2008 7 18 2008UALA03465 1 20080618 A 5315 141T52821 STIFFENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 E&E COMPARTMENT AT STA 246 FLOORBEAM AND LBL 40 HAS CRACKED VERTICAL STIFFENER. REPLACED CRACKED STIFFENER. FABRICATED & INSTALLED NEW REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20080718 EU 2008 7 18 2008UALA03467 1 20080619 A 2910 HYDRAULIC LINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE LEAKING A UALA A UNSCHED LANDING W K INADEQUATE Q C FLUID LOSS CR CRUISE 1 WP 29 411UA 464 YELLOW SYSTEM PRESSURE & QTY LOSS IN CRUISE. FLIGHT DIVERTED. LEAK ON HYD LINE ON NR 2 ENGINE. FOUND HYDRAULIC LINE O N ENGINE LEAKING. REPLACED LINE. ALSO, REPLACED NR 2 ENGINE HYDRAULIC PUMP, CHECKED HYDRAULIC CONTROL UNIT FILTER, CAS E DRAIN FILTRT AND HP FILTER. ALL HAD NO PARTICLES. REPLACED FILTERS PRECAUTIONARY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080718 NM 2008 7 18 2008UALA03472 1 20080615 A 3350 BR964421 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 853UA 1688 SEAT 10L EMERGENCY LIGHT INOP. RELAMPED SEAT 10L EMERGENCY LIGHT. OP CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080717 SO 2008 7 17 SIMA200815105 1 20080527 A 5320 14525480603 SILL EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 829AE 5000 145609 DURING A MBV INSPECTION, FOUND CARGO DOOR SLLL CORRODED BEYOND SRM LIMITS. REMOVED CORRODED SILL, DRILLED AND ALODINED NEW PART. INSTALLED NEW SLLL IAW EMB SRM (SRM145/1142 REV. 39) CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20080717 NM 2008 7 17 ASAA0843075 1 20080501 A 5330 65C3235720 SKIN BOEING 737 7374Q8 138447Q NM BS 374 S23-24L DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 DENT IN SKIN AT BS 374 5 INCHES BELOW STR 23L. DAMAGE REPAIRED ON MIG 5 NR 5097180 IAW B737 400 SRM 53 00 01. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843078 1 20080510 A 5330 65C3235720 SKIN BOEING 737 7374Q8 138447Q NM BS 500-500A DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 DENT ON LT LOWER FUSEALGE AT BS 500 TO 500A STR 25 TO 26. REPAIR WORK ACCOMPLISHED IAW B737 400 SRM 53 00 01. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083328 1 20080618 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND STRINGER 28R CRACKED AT BS 436. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 ASAA0843025 1 20080514 A 5753 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 LEFT WING OUTBOARD AFT FLAP LOWER SURFACE HAS 2 EACH DENTS 20 INCHES FROM INBOARD END AND 6 INCHES FROM TRAILING END PRE PARED DAMAGED AREA. FABRICATED DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080717 WP 2008 7 17 IXXA08SMN150S 1 20080418 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 400 L29R MISREPAIRED B IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR LOCATED AT STATION FS 400 LONGERON 29 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED EXTERNAL REPAIR DOUBLER, INTE RNAL FINGER DOUBLER, AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR S PARTS IAW DC8 SRM 53-2-1 FIGURE 7 SHEETS 1 AND 4, 51-9-0 FIGURE 68A, 53-4-1 FIGURE 1 ITEM "B", 51-1-11, 51-3-1, DC8 SR M 51-1-21, 51-1-20D, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 20080717 NM 2008 7 17 2008UALA02847 1 20080518 A 3810 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE POTABLE WATER OPEN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 515UA 24840 POTABLE WATER INDICATION CAUSED FLIGHT DIVERSION. SUPPLEMENTAL DATA UPDATE CAUSE, LAV DRAIN VALVE IN LAV 2L WAS OPEN. CLOSED DRAIN VALVE IN LAV 2L, SERVICED LAVS, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080717 NM 2008 7 17 SWAA083208 1 20080612 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 583, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083210 1 20080612 A 5340 6935364 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 1006, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083092 1 20080608 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083287 1 20080617 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500A, BETWEEN BL 0 AND RBL 3. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080717 CE 2008 7 17 W1X2008F00000 1 20080523 A 3220 084300117 BELLCRANK CESSNA 310 310R 2074245 CE CONT O520 IO520* 17032 SO NLG BROKEN E W1XA O OTHER O OTHER NR NOT REPORTED 1 GL 13 5338C 310R1544 FAILURE OF NOSE GEAR TO EXTEND, FOUND BELLCRANK ON GEAR BOX BROKEN. (K) 1 L 7 2 3O 3 O 3A10 E5CE 20080717 2008 7 17 ASAA0853108 4 20080627 A 3442 6225132633 TRANSCEIVER BOEING 737 737890 1384527 NM WX RADAR SYS FAULTY A ASAA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 02 587AS 2671 35684 WX RADAR, SHOWS STROBES AND FILLS DISPLAY WITH A GRAINY RETURN. DISPLAYS APPARENT GROUND RETURNS FROM WELL OVER HORIZON . THETEST "TEST" IS OK. COULD NOT DUPLICATE MALFUNCTION REPLACED WX RDR R T PRECAUTIONARY PER MM 34 43 41 FUNCTIONS NML. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 08FDEA02190 1 20080607 A 7500 652244420 DUCT BOEING 727 727233 138408A NM BLEED AIR LEAKING A FDEA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 CE 21 275FE 22040 AFTER TAKEOFF IN CLIMB-OUT NR 3 ENG STRUT OVERHEAT ILLUM. RAN QRH WHICH DETERMINED POSSIBLE LEAK ON FUSELAGE SIDE. WIT H LIGHT EXTINGUSHED CONT CLIMB AND CABIN PRESSURE WOULD NOT HOLD AT FL 320 WITH ONE PACK OPERATION. REQ DESCENT TO 10,0 00 FT TO CONTROL CABIN PRESSURE. REMOVED AND REPLACED DUCT CONNECTING 8TH STAGE CHECK VALVE TO ENGINE BLEED SYS AS PER M/M 36-00-001 2 LEAK CHECKS GOOD. 2 L 7 3 4F RT A3WE 20080717 NM 2008 7 17 SWAA083315 1 20080617 A 5340 65C27314 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083279 1 20080614 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 901WN 32545 DURING SCHEDULED MV1 CHECK, LT MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083172 1 20080610 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 2008 7 17 SWAA083566 4 20080629 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 202WN 33999 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083545 1 20080626 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6R AND STR 6L. REMOVED AND REPLACED STRINGER CL IP PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 CALA0800835 1 20080826 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM BS 827 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14628 27532 RIGHT FRAME IS CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 827 BETWEEN STRINGERS 8 AND 9. R EPAIRED RIGHT FRAME AT FASTENERS FOR AIR GRILL SUPPORT RAIL MOUNT AT STATION 827 BETWEEN S-9R AND S-9R PER EC/RA 5310-04 827. 2 L 7 2 4F RT A16WE 20080922 2008 9 22 2008UALA05528 4 20080902 A 2310 490S1 COUPLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT HF SYS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 589UA 28707 RIGHT HF WILL NOT TRANSMIT. FOUND FAULTY HF. SUSPECT COUPLER. REPLACED RT HF COUPLER AND RT HF TRANSCEIVER. 2 L 7 2 4F 4 F RT A2NM E17NE 20080922 NM 2008 9 22 2008UALA05529 1 20080902 A 2897 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUEL QTY IND DAMAGED A UALA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 WP 29 549UA 25397 RT FUEL QTY IND NOT WORKING. RTFL. FOUND FQIS PROCESSOR INTERMITTANT. SPLICE IS BAD AT HI Z WIRE GOING TO TANK UNIT 9, NEEDS RESPLICED. REPLACED SPLICE. FUEL QTY INDICATOR CHECKS GOOD. REPLACED FUEL QTY INDICATOR. OPS CHECK OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080922 NM 2008 9 22 2008UALA05530 1 20080901 A 2910 HYDRAULIC SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LOW A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 827UA 1022 LANDED UNDER AMBER ALERT DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. AIRCRAFT TOWED TO GATE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080922 EU 2008 9 22 2008UALA05531 1 20080829 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOORWAY CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 451UA 865 DOOR SILL 2R HAS CORROSION (MARKED). DOOR SILL 2R HAS CORROSION (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED DOOR SIL L. PICKED UP HOLES IN NEW SILL PAN. STARTED INSTALLING HI-LOKS THRU EXTERNAL SKIN COMMON TO DOOR 2R SILL BEAM ONLY. CO NTINUED INSTALLING FASTENERS THRU FWD SPLICES ONLY. COMPLETED FASTENER INSTALLATION. INSPECTED DOOR 2R SILL PLATE INST ALLATION FOR SECURITY AND FOUND SECURE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080922 NE 2008 9 22 2008UALA05533 2 20080901 A 7261 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE LEAKING A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 598UA 28751 NR 1 ENG HIGH OIL CONSUMPTION EXCEEDS LIMITS. REPLACED NR 1 ENG DEOILER SEAL. RAN ENGINE. NO LEAKS. NO LEAKS EVIDENT FR OM SHAFT SEAL DRAINS. 2 L 7 2 4F 4 F RT A2NM E17NE 20080922 NE 2008 9 22 2008UALA04088 2 20080803 A 7261 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE LEAKING A UALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 590UA 28708 717964 STRONG OIL SMELL IN COCKPIT. *S/D* INTERNAL BEARING SEAL LEAKAGE. REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080922 NE 2008 9 22 2008UALA04090 2 20080803 A 7261 6159009 SCAVENGE PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE LEAKING A UALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 567UA 26673 726664 OIL PRESSURE PROBLEM. FLIGHT DIVERTED. *S/D* LUBE & SCAVENGE PUMP FAILING. CHANGED LUBE & SCAVENGE PUMP-HIGH POWER R UNS ACCOMPLISHED WITH LEAK CHECKS, ALL NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080922 NM 2008 9 22 2008UALA05540 1 20080830 A 3350 58673 INVERTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 596UA 28749 EEL LIGHTS IN AISLE LAST SECTION ARE INOP FOUND BAD INVERTER. FOUND AFTER BATTERY HAD TIME TO CHARGE LIGHTS OPS CK GOO D. 2 L 7 2 4F 4 F RT A2NM E17NE 20080922 NM 2008 9 22 2008UALA05542 1 20080830 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 8F INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 779UA 26941 SEAT 8F AFT EEL PROX LIGHT INOP. FOUND LIGHT INOP. REPLACED LIGHT ASSY. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080917 NM 2008 9 17 2008UALA04219 1 20080809 A 3397 90085 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY LIGHT RH SEAT 35 THRU 44 INOP. FOUND LOOSE CONNECTOR. SECURED BATTERY CONNECTOR. EXIT SIGN OPS CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080917 NM 2008 9 17 2008UALA04240 1 20080810 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS MISWIRED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT LIGHT INOP. AT DOOR 2 GALLEY CEILING. FOUND SOCKET MISWIRED. INSTALLED WIRES CORRECTLY. OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080917 NM 2008 9 17 2008UALA04349 1 20080818 A 8011 35054367 STARTER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 NR 1 ENGINE STARTER FAILED DURING ENGINE START. STARTER FAILURE. REPLACED ENGINE STARTER. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20080918 NM 2008 9 18 2008UALA04295 1 20080817 A 3350 362624 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 EEL LIGHT AT 5A FOUND BROKEN. *S/D* FOUND LIGHT BROKEN. REPLACED EEL ASSY, OPS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 NM 2008 9 18 2008UALA04164 1 20080806 A 3350 1317 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 369UA 24538 FLIGHT DECK EMERGENCY LIGHT INOP. *S/D* RELAMPED, OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 20080918 NM 2008 9 18 UPS08M53224 1 20080820 A 5730 SKIN DOUG MD11 MD11F 3023600 NM LT WING LE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C LT WING L/E PANEL TOP SURFACE FOUND WITH GOUGE JUST TOP SURFACE OF NR 18 SLAT TRACK COMP. REMOVED SK IN, FABRICATED AND INSTALLED SKIN IAW DWG ARB2891, MD-11 SRM 51-33-01, 51-21-01, AND 51-35-01. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 2008UALA04169 1 20080806 A 3150 MR31600 COMPUTER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EICAS FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 667UA 29239 EICAS "R EICAS CMPTR" DISPLAYED. *S/D* FOUND FAULTY COMPUTER. REPLACED RT EICAS COMPUTER PER MM 31-41-00, RELOADED CO RRECT SOFTWARE, OPS CHECKS GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080918 NM 2008 9 18 2008UALA04314 1 20080816 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1420 S26-27L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 AFT PIT STA 1420 BETWEEN STR 27L AND 26L FRAME IS DENTED. *S/D* MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NM 2008 9 18 UPS08M53173 1 20080821 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 13 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NM 2008 9 18 2008UALA04335 1 20080819 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY CEILING LIGHT ABOVE ROW 32 RT INOP. *S/D* RELAMPED, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 NM 2008 9 18 ZZDA2008152 1 20080823 A 3350 1703651 SOCKET BOEING 717 717200 1383700 NM ROW 26 DEF MISSING A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 989AT 55152 EMERGENCY PATH LIGHT AT SEAT ROW 26 DEF DOES NOT ILLUMINATE. ELECTRICAL CONNECTOR AT BASE OF SEAT WAS TORN OFF/MISSING. FOUND DURING SERVICE CHECK. REPLACED AIRCRAFT SIDE ELECTRICAL CONNECTOR AT SEAT ROW 26 DEF PER SWPM 20-20, WDM 33-51- 14. OPS CHECK GOOD PER AMM 33-51-00. 2 L 7 2 4F TR A6WE 20080919 NM 2008 9 19 SWAA084842 1 20080903 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM BS 908 S25R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 25R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084847 1 20080903 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 380 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084823 1 20080902 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 231WN 32499 DURING SCHEDULED HC2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 19 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 SWAA084852 1 20080903 A 5330 6545774 SKIN BOEING 737 7373L9 1384470 NM BS 847 S27L/R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 FUSELAGE SKIN CORRODED AT BS 847, BETWEEN STR 27R AND STR 27L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080919 NM 2008 9 19 ASAA0853468 1 20080830 A 2131 71211997101AC CONTROLLER BOEING 737 737890 1384527 NM CABIN PRESSURE FAILED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 559AS 25338 35178 AUTO FAIL LIGHT ILLUMINATED. VERIFIED DISCREP PRESS CNTL AUTO 2 C/B RESET AUTO AND ALT ANN'S ILL'D. NR 2 CNTLR SHOWS " FAULT" PER FIM 21 31 TASK 801 EXSIST FAULT LAST FLT SHOWS 2 CNTLR LRU FAILS CODES 050 AND 049. REF TABLE 201 DCPCS FAUL T NR LIST CODES 049 AND 050 REFER TO PRESS SENSOR. PERFORMED FIM 21 31 TASK 824 GND SYSTEM TEST PASS. REMOVED AND INST ALLED NR 2 DCPC REF 21 31 01. OPS NORMAL REF SAME. GND SYSTEM TESTS PASS. 2 L 7 2 4F RT A16WE 20080919 EU 2008 9 19 2008UALA05398 1 20080822 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 29 476UA 1508 F/A AND CPT CREW SMELLED AN ELECTRIC ODOR UPON LANDING ALSO ON APPROACH. ACCOMPLISHED POWER RUNS ON BOTH ENGINES, COMPA RING BLEEDS FOR ODOR AT POWER AND AT IDLE, CHECKING COMBINATIONS OF BLEEDS AND PACKS. NO UNUSUAL ODORS NOTED, NO ELECTR ICAL ODORS NOTED. POWERED VIRTUALLY ALL CABIN ELECTRICAL COMPONENTS. NO ODORS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080919 NM 2008 9 19 UPS08553163 1 20080821 A 7931 OIL SYSTEM BOEING 757 75724APF 1384969 NM RIGHT ENGINE LOW PRESSURE A IPXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 01 412UP 23852 INSPECTION TYPE:N/A IFSD - LOSS OF RIGHT ENGINE OIL PRESSURE IN FLIGHT. CREW DECLARED EMERGENCY. *SUPPLEMENTAL SDR* R EMOVED AND REPLACED RIGHT ENGINE PER TC 5001. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A2NM 20080919 NM 2008 9 19 UPS08553164 1 20080815 A 3350 LAMP BOEING 757 75724APF 1384969 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 474UP 28844 INSPECTION TYPE:N/A EMERGENCY EGRESS LIGHT ON FUSELAGE INOP. RELAMPED EMERGENCY EGRESS LIGHT, OPS CHECKED GOOD. 2 L 7 2 4F RT A2NM 20080718 EU 2008 7 18 08FDEA02359 1 20080620 A 5321 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU CABIN DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 MAIN CABIN FLOOR PANEL 241 NF IS DAMAGED. FABRICATED NEW FLOORBOARD; POTTED EDGES; LOCATED HOLES; INSTALLED INSERTS; CU RED; APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005, REV F. 2 L 7 2 4F RT A35EU 20080718 EU 2008 7 18 2008UALA02517 2 20080430 A 7261 OIL SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 ENGINE OBSTRUCTED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 202UA 24717 722282 RTFL DUE TO LOW OIL QTY/PRESSURE INDICATIONS FOR NR 2 ENGINE. FOUND RAG BLOCKING THE FRONT COMPARTMENT SUMP AS WELL AS A RAG IN THE SCAVENGE TUBE. REPLACED THE ENGINE. SHOP FINDINGS: RAGS IN OIL SCAVENGE SYSTEM. ENGINE MADE SERVICEABLE . 2 L 7 2 4F 4 F RT A16WE E21EU 20080718 NM 2008 7 18 08FDEA02102 1 20080602 A 5100 NONE DOUG MD11 MD11F 3023600 NM IAW SRM NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 EXISTING DOUBLER REPAIR AT CENTER CARGO FORWARD CUT-OUT APPROX STRINGER 40 TO 42. EXISTING DOUBLER REPAIR AT CENTER CAR GO FORWARD CUT-OUT APPROX STRINGER 40 TO 42 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-50-00 FIGURE 17 VO LUME I FEDEX EO NR 1-5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG - MD11 - REPAIR CATALOG AND TRACKING REQUIREMENTS, HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 EU 2008 7 18 08FDEA02367 1 20080620 A 5321 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU CABIN DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 MAIN CABIN FLOOR PANEL 232 YG IS DAMAGED. FABBED A NEW FLOOR PANEL 232 YG BY USING THE OLD PANEL AS A TEMPLATE; POTTED; CURED AND SANDED EDGES; POTTED AND CURED INSERTS; APPLIED NON-SKID TAPE AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005, REV F. 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 08FDEA02109 1 20080603 A 5100 NONE DOUG MD11 MD11F 3023600 NM IAW SRM NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 590FE 48505 EXISTING REPAIR, MAIN DECK EXISTING SEAT TRACK SPLICE REPAIR FOUND AT STA 1235, X = - 27.5. EXISTING REPAIR AT MAIN DEC K SEAT TRACK SPLICE REPAIR AT STA 1235, X = -27.5 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. FEDEX EO NR 1- 5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG - MD11 - REPAIR CATALOG AND TRACKING REQUIREME NTS 14 CFR 121.707, HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 08FDEA02236 1 20080612 A 5340 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 598FE 48597 MAIN DECK CARGO DOOR SPOOL FITTING NR 2 FOUND 3RD LAYER CRACK INDICATIONS AT FITTING MOUNTING BOLT HOLES A, C, AND D. M AIN DECK CARGO DOOR SPOOL FITTING NR 2 REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 WP 2008 7 18 08FDEA02249 1 20080612 A 5410 ATL0022503 RUB STRIP DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 THE NR 2 ENGINE RIGHT FAN COWL; THE RUB STRIP IS WORN. RUB STRIP WAS FOUND TO BE OUT OF LIMITS IAW MD-10-10 AMM 71-13-0 2-2. REMOVED THE RUB STRIP AND FWD LOWER FIRE SHIELD IAW DC/MD-10 SRM 51-35-01; VOL II. LOCATED; DRILLED AND DEBURRED RUB STRIP IAW DAC DWG ATL0022. INSTALLED NEW RUB STRIP AND FWD LOWER FIRE SHIELD IAW DC/MD-10 SRM 51-35-01; VOL II. 2 L 7 3 4F RT A22WE 20080718 EU 2008 7 18 08FDEA02253 1 20080613 A 5330 A53610317201 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT SIDE FUSELAGE SKIN AT FRAME 14 CENTER OF SKIN PANEL BETWEEN STRINGERS 3 4 TO 35 LT UNDER THE L-1 DOOR AREA, THE REPAIR DOUBLER MEASURES 5.3 NCH BY 4.5 INCH. REPAIR IAW SRM AND SWISSAIR DWG 91 2189 REQUIREMENTS. REMOVED PREVIOUS REPAIR AND RE-INSTALLED REPAIR ON LT SIDE FUSELAGE SKIN AT FRAME 14 CENTER OF SKIN PANEL BETWEEN STRINGERS 34 AND 35 LT UNDER THE L-1 DOOR AREA IAW FED EX EA6-5310-121277 AND A310-200 SRM 53-10-12 FIG 22 4 SHEET 3. THIS IS AN AIRBUS REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 SWAA083570 1 20080627 A 3233 654482517 ACTUATOR BOEING 737 7373H4 1384600 NM RT MLG FAULTY A SWAA K NONE J WARNING INDICATION CL CLIMB 1 SW 29 312SW 23334 DURING CLIMB RT MLG UNSAFE LIGHT ILLUMINATED. AFTER MOVING GEAR HANDLE TO OFF POSITION RT GEAR FELL OUT OF W/W. CYCLED GEAR, GEAR RETRACTED NORMAL INDICATIONS. REMOVED AND REPLACED RT MLG UPLOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083602 1 20080629 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 08FDEA02357 1 20080620 A 5753 A57970100002 SKIN AIRBUS 310 A310203 3930313 EU LT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 LEFT INBOARD FLAP LOWER SKIN HAS REPAIR MISSING, BETWEEN FLAP RIB 2 AND FLAP RIB 4 REMOVED DAMAGED SKIN AND CORE, FABRIC ATED AND INSTALLED FLAP REPAIR DOUBLER AT LT INBD LOWER SKIN BETWEEN FLAP RIB 2 AND FLAP RIB 4 IAW FEDEX EA 6-5750-12128 1, RELEASE DATE 29 MAY, 2008. 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 08FDEA02113 1 20080603 A 5100 NONE DOUG MD11 MD11F 3023600 NM IAW SRM NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 590FE 48505 LEFT WING LEADING EDGE NR 3 SLAT UNDER SURFACE INBOARD FOUND EXISTING REPAIR. LEFT WING LEADING EDGE NR 3 SLAT UNDER SURFACE INBOARD EXISTING REPAIR EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 10 VOLUME I FEDEX EO NR 1-5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG - MD11, REPAIR CATALOG AND TRACKING REQUIREMENTS, HAS BEEN ACCOMPL ISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 SWAA083558 1 20080626 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, BL 0. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080718 2008 7 18 SWAA083589 4 20080626 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 520SW 25319 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083593 1 20080629 A 5310 6547580 CREASE BEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 827 AND BS 847, LBL 70. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083594 1 20080629 A 5330 6545800 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084878 1 20080904 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 947 S25L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 947, STR 25L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084932 1 20080908 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 787 S25L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 2008UALA05402 1 20080821 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 L-1 HANDLE BOX GOUGED AT FASTENER POINTS. UNKNOWN DAMAGE/WEAR. REMOVED DAMAGED BOX ASSY, INSTALLED NEW BOX ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080922 NM 2008 9 22 2008UALA05403 1 20080821 A 5240 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 DOOR 2R HAS HANDLE BOX CRACKED AT INSERT HOLE. *S/D* UNKNOWN DAMAGE/WEAR. REMOVED DAMAGED HANDLE BOX AND INSTALLED NE W BOX. 2 L 7 2 4F 4 F RT A2NM E17NE 20080922 NM 2008 9 22 2008UALA05404 1 20080821 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 L-2 DOOR HANDLE BOX ASSY HAS SEVERAL CRACKS AT THE FASTENER HOLES, VIEWED EXTERNALLY. *S/D* UNKNOWN DAMAGE/WEAR. REMO VED DAMAGED BOX, ASSEMBLED AND INSTALLED NEW BOX. 2 L 7 2 4F 4 F RT A2NM E17NE 20080922 NM 2008 9 22 2008UALA05543 1 20080830 A 3350 3071BPEGPL LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 94 INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 779UA 26941 SEAT 9F FWD EEL PROX LIGHT INOP. LIGHT FOUND DEFECTIVE. REPLACED LAMP. OPS CHK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080922 2008 9 22 SWAA084889 4 20080907 A 2565 63550101 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084892 1 20080907 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM BS 787 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084893 1 20080907 A 5311 6546595 FRAME BOEING 737 7373H4 1384600 NM BS 727A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084894 1 20080907 A 5330 6547955 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084900 1 20080904 A 5330 6545766 SKIN BOEING 737 7373Q8 1384670 NM BS 581 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 581, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084901 1 20080904 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM BS 773 S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 773, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084902 1 20080904 A 5330 6545777 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR CUTOUT AFT UPPER CORNER. REPAIRED SKIN PER SR M. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084926 1 20080907 A 5330 6545800 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA . 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084927 1 20080907 A 5322 6546569 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 967 S27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 967, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084928 1 20080907 A 5311 141A1120 FRAME BOEING 737 7377H4 1384404 NM BS 295 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 295, RBL 54. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 M7K2008F00041 1 20080612 A 6220 M3199 STARFLEX UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE MAIN ROTOR DEFECTIVE E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 810MH 3949 2331B DURING ROUTINE INSPECTION WITH ROTOR HEAD SLEEVE ASSY REMOVED ONE OF THE STAR ARM END BUSHINGS WAS FOUND TO TURN SLIGHTL Y WITH HAND PRESSURE APPLIED. THE STARFLEX WAS REMOVED FOR REPAIR OF BONDING DEFECT. THIS IS A COMMON FAILURE FOR THIS PART. THE MFG CLAIMS TO HAVE A REPAIR FOR THIS DEFECT BUT OFFERS ONLY AN EXCHANGE ASSY. SUGGEST A NEW ADHESIVE SYS OR P ART DESIGN BE TRIED TO REDUCE THIS TYPE OF DEFECT FOR AN EXPENSIVE PART. A SLIPPAGE MARK PAINTED ACROSS THE EDGE OF THE BUSHING AND ONTO THE STAR ADHESIVE BEAD HELPS IN DETECTION OF THIS DEFECT WHILE IN SERVICE BY INDICATING THE BUSHING HA S TURNED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 EU 2008 7 18 M7K2008F00008 1 20080512 A 6710 116F2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE DEFECTIVE E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 808MH 998 3914 (REF 0423083914) A FAULT CODE WAS GENERATED ON SHUTDOWN INDICATING A DEFECT OF THE YAW POTENTIOMETER. A NEW PART WAS INS TALLED AND NO FURTHER FAULT WAS DETECTED. THIS IS A RECURRING FAILURE FOR THIS PART WHICH HAS EFFECTED THE DISPATCH REL IABILITY FOR THIS MODEL HELICOPTER. SUGGEST AN OPTIC RATHER THAN A RESISTANCE BASED SENSOR SHOULD BE CONSIDERED AS THE CONTACT POINT IS DAMAGED BY AIRCRAFT VIBRATION WHEN THE AIRCRAFT PEDAL SETTINGS ARE SET FOR CRUISE FLIGHT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 EU 2008 7 18 M7K2008F00018 1 20080523 A 6320 PRESSURE SENSOR UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE RGB FAILED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 851MH 143 4340 23479 LOW MGB OIL PRESSURE WARNING LIGHT FLICKERED IN FLIGHT WITH NO AUDIBLE WARNING. SWITCH WAS REPLACED WITH A SERVICEABLE P AR AND WITH NO FURTHER DISCREPANCY NOTED. THIS IS NOT AN UNCOMMON FAULT FOR THIS PART. SUGGEST IMPROVED DESIGN OR BETTE R QC FOR INTERNAL PARTS AS PERHAPS ONLY A THIRD OF THESE SWITCHES FAIL IN SERVICE. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 EU 2008 7 18 M7K2008F00017 1 20080523 A 6320 1130021089 PRESSURE SENSOR UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE RGB INOPERATIVE E M7KA O OTHER O OTHER CR CRUISE 1 WP 19 807MH 997 3912 23130 LOW MGB OIL PRESSURE WARNING LIGHT FLICKERED IN FLIGHT WITH NO AUDIBLE WARNING. SWITCH WAS REPLACED WITH A SERVICEABLE P AR AND WITH NO FURTHER DISCREPANCY NOTED. THIS IS TO AN UNCOMMON FAULT FOR THIS PART. SUGGEST IMPROVED DESIGN OR BETTER QC FOR INTERNAL PARTS AS PERHAPS ONLY A THIRD OF THESE SWITCHES FAIL IN SERVICE. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 NM 2008 7 18 SWAA083516 1 20080625 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 540, STR 23R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080718 EA 2008 7 18 A6WA200840454 1 20080528 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 CRACK FOUND ON INTERCOSTAL FS 484 RBL 27 AND RBL 36. DAMAGE REMOVED NEW ANGLE FABRICATED, HFEC PERFORMED AND FABRICATED ANGLE INSTALLED IAW REO 601R53-41-059 REV A AT FS 484 RBL 27 NEW ANGLE INSTALLED IAW REO 601R-53-41-059 REV A. (A) 2 L 7 2 4F RT A21EA 20080718 CE 2008 7 18 060808N622CS1 1 20080608 A 2611 SMOKE DETECTOR CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE CARGO BAY CONTAMINATED E Z5FA O OTHER J WARNING INDICATION CR CRUISE 1 EA 63 622CS 6800124 DURING CRUISE, BAGGAGE SMOKE LIGHT ILLUMINATED. CREW FOLLOWED AFM PROCEDURES, FIRED BAGGAGE FIRE EXTINGUISHERS, DECLARE D AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINT NOTICED BAGGAGE CONTAINING CAKE MIX HAD BURST OPEN AND THE POWDER MIX WAS SCATTERED ABOUT BAGGAGE COMPARTMENT. (SMOKE DETECTORS WERE COVERED WITH THIS CAKE MIX POWDER CAUSING SMOKE WARNING ). FIRE BOTTLES REPLACED, SENSORS CLEANED AND AC RETURNED TO SERVICE. SMOKE DETECTION SYS WORKING PROPERLY, NO DEFECTIV E PARTS. (K) 2 L 7 2 4F 4 F RC T00012WI E35NE 20080718 EU 2008 7 18 M7K2008F00038 1 20080612 A 3150 0676 WARNING SYSTEM UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE CENTRAL WARNING FAILED E M7KA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 19 822MH 1158 4142 23069 WHEN AC POWER WAS TURNED ON ALL WARNING LIGHTS OF CENTRAL WARNING PANEL ILLUMINATED AS IF WARNING LIGHT TEST SWITCH WAS ACTIVATED. A NEW ASSY WAS INSTALLED AND NO FURTHER DEFECT NOTED. PREVIOUS EXPERIENCE AN INTERNAL SHORT WAS FOUND THAT CAUSED THIS PROBLEM, THIS IS A RARE FAILURE OF THIS PART. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 NE 2008 7 18 M7K2008F00035 2 20080612 A 7261 800301 MAGNETIC SEAL UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE LEAKING E M7KA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 805MH 2804 3799 23167 DURING ROUTINE INSP EXCESSIVE OIL LEAKAGE WAS NOTED AT THE MODULE 5 OUTPUT MAGNETIC SEAL. CLOSE INSP OF REMOVED SEAL RE VEALED NO OBVIOUS DEFECT. A NEW SEAL WAS INSTALLED WITH NO FURTHER LEAKAGE NOTED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 EU 2008 7 18 M7K2008F00046 1 20080623 A 3150 024803AA CONTROL PANEL UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE CENTERAL WARNING FAILED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 821MH 1720 4134 23322 POSITION LIGHTS FAILED TO ILLUMINATE WITH CB NOT POPPED AND NO APPARENT SHORTS FOUND. INVESTIGATION REVEALED CIRCUIT TR ACE ON THE PCB SUPPLYING POWER TO THE POSITION LIGHT SWITCH HAD MELTED/BLOWN LIKE A FUSE. THIS A COMMON PROBLEM FOR THI S PART. SUGGEST MORE ROBUST TRACE BE APPLIED TO PCB CIRCUIT. REDUCTION OF CB AMPERAGE PROTECTION VALUE OR A REDESIGN OF CIRCUIT WHICH MAY BE FAULTY. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 NM 2008 7 18 UPS08B52442 1 20080329 A 5320 DOUBLER BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:N/A LEFT BS 1120 TENSION TIE FRAME DOUBLER CRACKED ABOUT 0.030 INCH. LEFT BS 1120 TENSION TIE FRAME DOU BLER REPLACED. 2 L 7 4 4F RT A20WE 20080718 CE 2008 7 18 JGB2008F00000 1 20080630 A 2910 605700311 HOSE LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE HYDRAULIC SYS FAILED E JGBA O OTHER O OTHER NR NOT REPORTED 1 SW 11 260AN 124 PILOT REPORTED A LOSS OF HYDRAULICS DURING FLIGHT AT CRUISE FL400. INSP REVEALED THAT RT ENG DRIV HYD PUMP, PRESSURE SI DE HYDR LINE WAS LEAKING, AND ALLOWED THE AC HYDR SYS FLUID TO BE DEPLETED. FURTHER INSP REVEALED THAT LINE HAD FAILED INTERNALLY AND WHEN PRESSURE WAS APPLIED, HOSE WOULD SWELL AND BEGIN TO LEAK. THE PROBABLE CAUSE OF THE FAILURE IS AGE A ND POSSIBLE EMBRITTLEMENT OF THE HOSE. TO POSSIBLY PREVENT RECURRENCE OF SUCH FAILURES, A TIME INTERVAL FOR REPLACEMENT OF AGEING TEFLON HOSES MAY BE NEEDED. (K) 2 L 7 2 4F 4 F RT A10CE E35NE 20080721 WP 2008 7 21 UPS08852433 1 20080524 A 5347 3657503501 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 COCKPIT, SECOND OBSERVER SEAT TRACKS SHOW ELONGATIONS. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-3 -0, 51-1-2, 51-1-8. 2 L 7 4 4F RT 4A25 20080721 NM 2008 7 21 SWAA083735 1 20080706 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 754, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083522 1 20080625 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 23L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084929 1 20080907 A 5315 141A5504 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 32.5 TO RBL 11. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084930 1 20080907 A 5311 6545808 FRAME BOEING 737 7373H4 1384600 NM BS 294.5 S13R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294.5, STR 13R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084937 1 20080908 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 747 S23R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084938 1 20080908 A 5315 6546810 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 967, RBL 30. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084939 1 20080908 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 867 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084942 1 20080908 A 3350 1619 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 390SW 26593 L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084943 1 20080908 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084944 1 20080907 A 3233 65446104 ACTUATOR BOEING 737 7373H4 1384600 NM NLG FAULTY A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 29 631SW 27706 RAISED GEAR HANDLE TO UP POSITION, NLG WARNING LIGHT ILLUMINATED. LANDING GEAR HANDLE PLACED TO OFF POSITION NLG FELL O UT. REMOVED AND REPLACED NLG RETRACT ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084945 1 20080908 A 3350 OL3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 651SW 27721 BULL NOSE EMERGENCY EXIT LIGHT INOP AT ROW 13 DEF. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084834 1 20080903 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 360-372 S22R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER 22R CORRODED BETWEEN BS 360 AND BS 372. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084835 1 20080903 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 360-365 S23R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER 23R CORRODED BETWEEN BS 360 AND BS 365. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084836 1 20080903 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 400 S19R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 400, STR 19R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084953 1 20080908 A 5313 BAC1498 STRINGER BOEING 737 7373Y0 1384671 NM BS 324 S24R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED 22Y CHECK, FOUND STRINGER 24R CORRODED AT BS 324. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084954 1 20080908 A 5330 148A3320 SKIN BOEING 737 7377H4 1384404 NM BS 1028 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 723SW 27855 FUSELAGE SKIN CRACKED AT BS 1028, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 SWAA084955 1 20080908 A 2560 PL22300LH GLOWSTRIP BOEING 737 7377H4 1384404 NM ROW 8 ABC LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 778SW 27883 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 ABC. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 20080922 2008 9 22 SWAA084956 4 20080908 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 912WN 36621 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080922 2008 9 22 ASAA0853425 4 20080828 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 02 583AS 4454 35681 DURING CLIMB SPEED BUG DROPPED TO CLEAN SPEED WITH V NAV ENGAGED FMC READS GOOD FOR CLIMB SPEED. AT CRUISE V NAV AND BU G APPEAR TO BE WORKING OKAY. PERFORMED FMC BITE TEST PER MM 34-61-00. PERFORMED DFGS BITE TEST PER MM 22-11-00. NO FA ULTS NOTED. NO HISTORY NOTED. GROUND VERIFICATION SUCCESFUL. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843426 1 20080820 A 5754 65C26603201A SKIN BOEING 737 737490 1384715 NM NR 3 SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 LEFT WING NR 3 SLAT LOWER T/E WEDGE CHAFED ON I/B SIDE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLER AND BONDED IAW B737 400 SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843427 1 20080819 A 5753 6546430186 SKIN BOEING 737 737490 1384715 NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 LEFT WING I/B FORE FLAP UPPER SURFACE DENTED AND CHAFED 47 INCHES FROM I/B END AND 9 INCHES FROM T/E. PREPARED DAMAGED AREA, FABRICATED DOUBLER AND BONDED IAW B737 400 SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843395 1 20080818 A 5311 65465479 FRAME BOEING 737 7374Q8 138447Q NM BS 727 S12-16L CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 754AS 25095 BODY STA 727 FRAME IS CRACKED 2 EA PLACES AT STR 14L AND 15L. REPAIRED FRAME IAW EA 5330 02380 BY INSTALLING TWO REPAIR ANGLES AND TWO CLIPS. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843414 1 20080822 A 5340 STRINGER CLIP BOEING 737 7374Q8 138447Q NM BS 727F S26L DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 AFT CARGO PIT BS 727F STR 26L TIE CLIP DAMAGE. TIE CLIP REPLACED WITH MADE REPAIR PART IAW B737 400 SRM 51 40 02 AND B DRAWG SPECS 69 35350. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843406 1 20080819 A 5755 654645268A SKIN BOEING 737 737490 1384715 NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 RIGHT I/B GROUND SPOILER LOWER SURFACE 12 EA SMALL DENTS AT I/B AREA. REMOVED DAMAGED AREA, FABRICATED FILLER AND EXTER NAL DOUBLER PREPARED AREA AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843407 1 20080819 A 5755 654645268A SKIN BOEING 737 737490 1384715 NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 RIGHT WING NR 5 SPOILER CLUSTER OF DENTS ON UPPER SURFACE 12 INCHES FROM O/B END. REMOVED DAMAGED AREA, FABRICATED SKIN FILLER AND DOUBLER PREPARED AREA AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080918 WP 2008 9 18 UPS08853194 1 20080802 A 5313 STRINGER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 FOUND CRACK ON STRINGER 53 AT O/B DRAG ANGLE NR 4 ALT. REMOVED AND REPLACED STRINGER IAW SRM 51-1-8, 57-2-2 FIG 3D, 57-4-0 FIG 11. 2 L 7 4 4F RT 4A25 20080918 NM 2008 9 18 UPS08553199 1 20080814 A 5210 CAM BOEING 757 75724APF 1384969 NM PAX DOOR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 CREW ENTRY DOOR LWR LATCH CAM GOUGED ON FACE. BLENDED PER B757-5210-14721. 2 L 7 2 4F RT A2NM 20080918 NM 2008 9 18 SWAA084804 1 20080828 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 506B S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506B, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 ASAA0843416 1 20080812 A 5330 65C277932 SKIN BOEING 737 7374Q8 138447Q NM BS 178 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 LWR FUSELAGE SKIN DAMAGED AT FS 178 BETWEEN STR 27R AND 28R. REPAIRED IAW ERO 8610 AND EA 5330 02383. 2 L 7 2 4F RT A16WE 20080918 NM 2008 9 18 UPS08553205 1 20080813 A 5410 SPLICE PLATE BOEING 757 75724APF 1384969 NM LT NACELLE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 NR 2 ENGINE STRUT, LT NAC STA 136, WL 161.70, I/B SUPPORT FOR PNL 441AT IS CHAFED. REMOVED, FABRICAT ED AND INSTALLED SPLICE PLATE PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20080918 NM 2008 9 18 UPS08M53215 1 20080820 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 30 LEFT BARREL NUT BORE HOLE. REMOVED CORROSIOIN, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080918 NE 2008 9 18 2008UALA04122 2 20080805 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT MAKING METAL A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 504UA 24625 717940 LEFT ENGINE STALLED. RTFL. *S/D* INTERNAL ENGINE DAMAGE, INITIAL INSPECTION OF ENGINE SHOW PIECES OF METAL IN TAIL PI PE. REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080918 NM 2008 9 18 2008UALA04138 1 20080805 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY LIGHT INOP: CEILING AT 35 RT. *S/D* RELAMPED, OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080918 NM 2008 9 18 2008UALA04152 1 20080802 A 3397 BR963165 CONNECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 839UA 1507 CABIN EMERGENCY LIGHT OUT AT SEAT 23C. *S/D* SECURED CONNECTOR TO LIGHT, OPS OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080918 NM 2008 9 18 2008UALA04382 1 20080821 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 641UA 25091 EMERGENCY LIGHT ADJACENT DOOR 1R INOP. SECURED LOOSE CONNECTOR. OPS CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20080918 NM 2008 9 18 2008UALA04383 1 20080821 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LAVATORY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 641UA 25091 EEL LIGHT ADJACENT TO LAV AT DOOR 1L INOP. SPLICED EEL LIGHT STRIP TO CKT PWR. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20080919 WP 2008 9 19 UPS08853261 1 20080811 A 5280 5646310506508 HINGE DOUG DC8 DC871F 302199D WP MLG DOOR WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 RIGHT I/B GEAR DOOR LOOSE ON HINGE PINS. REMOVED AND REPLACED HINGE ON MAIN GEAR DOOR IAW SRM 51-1-8 , 51-1-20D, 51-1-3, 51-1-21, 51-1-21A, 51-3-1. 2 L 7 4 4F RT 4A25 20080919 WP 2008 9 19 UPS08853262 1 20080812 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 CRACKED EXISTING REPAIR DOUBLER AT STA 3 ON FLAP WELL SUPPORT FRAME. REMOVED AND INSTALLED REPAIR DO UBLER IAW SRM 51-1-21, 51-1-8, 57-2-00 FIG 2A, 51-1-21. 2 L 7 4 4F RT 4A25 20080922 NM 2008 9 22 SWAA084879 1 20080904 A 5320 6517582 VERTICAL BEAM BOEING 737 7373H4 1384600 NM BS 178 BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.1. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843452 1 20080823 A 5754 65C26603202A SKIN BOEING 737 7374Q8 138447Q NM NR 4 SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 778AS 25110 NR 4 SLAT INBOARD T/E IS DELAMINATED ON THE TOP INBOARD END. PREPPED DAMAGED AREA, FABBED CORE PLUG AND DOUBLER, INSTAL LED REPAIR IAW B737 400 SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843408 1 20080819 A 5755 654645268A SKIN BOEING 737 737490 1384715 NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 RIGHT WING NR 5 SPOILER UPPER SURFACE DENTED 5 INCHES FWD OF T/E AND 24 FROM O/B EDGE. PREPARED DAMAGED AREA, FABRICATE D REPAIR DOUBLER AND BOUNDED IAW B737 4 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843409 1 20080819 A 5755 654645268A SKIN BOEING 737 737490 1384715 NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 RIGHT WING NR 5 SPOILER LOWER SURFACE SEVERAL DENTS WITH PUNCTURES 24 INCHES FROM I/B END AND 6 INCHES FROM L/E. REMOVE D DAMAGED AREA, FABRICATED TWO FILLER SKINS AND ONE EXTERNAL DOUBLER PREPARED AREA AND BONDED IAW B737 400 SRM REPAIR 4. 2 L 7 2 4F RT A16WE 20080922 NM 2008 9 22 ASAA0843411 1 20080819 A 5755 654645170A SKIN BOEING 737 737490 1384715 NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 LT WING NR 0 SPOILER UPPER SURFACE PROTRUDING DENT 6 INCHES FROM O/B AND 7 INCHES FROM T/E. REMOVED DAMAGED AREA, FABRI CATED FILLER AND EXTERNAL DOUBLER AND BONDED IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080923 NM 2008 9 23 DLM88081160 1 20080905 A 5330 9958156505 SKIN DOUG MD88 MD88 3023688 NM BS 1022-1041 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 908DL 49539 FUSELAGE WINDOW BELT HAD LIGHTNING DAMAGE AT STA 1022-1041 ON THE RT SIDE OF THE AIRCRAFT. REMOVED DAMAGE PER MD88 SRM 53-05, FIGURE 111 AND SUBMITTED FINAL DIMENSIONS TO BOEING FOR APPROVAL. 8100-9 APPROVAL WAS RECEIVED FROM BOEING FOR T HE REWORK AS TIME LIMITED UNTIL THE PANEL IS REPLACED. 2 L 7 2 4F RT A6WE 20080923 NM 2008 9 23 DL76P081162 1 20080907 A 5410 311T3065125 DOOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 NACELLE MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 140LL 25988 724372 FOUND NR 2 ENG INBD AFT NACELLE STRUT ACCESS DOOR MISSING. FORWARD TO MCO PER CDL 54-53-02. 2 L 7 2 4F 4 F RT A1NM E24NE 20080923 NM 2008 9 23 DL738081163 1 20080907 A 3246 39353 VALVE BOEING 737 737832 13844CF NM PWA 4060 PW4060 52119 NE LEFT OUT OF TOLERANCE A DALA O OTHER O OTHER LD LANDING 1 SO 27 387DA 19900 30374 724372 LEFT OUTBD TIRE BURST AFTER LANDING. TROUBLESHOOT ANTI-SKID SYSTEM FOUND LEFT OUTBD ANTI-SKID NORMAL VALVE RESISTANCE O UT OF RANGE PER FIM 32-42-00-810-804. BITE A/S BOX FOUND VLV1 WITH SP-CO-VI. T/S PER FIM 32-42-00-810-804 FO UND NR 1 NORMAL A/S VALVE RESIS OUT OF RANGE. REPLACED NR 1 NORMAL A/S VALVE PER AMM. CKS GOOD LEAK CHECK GOOD 2 L 7 2 4F 4 F RT A16WE E24NE 20080923 NM 2008 9 23 DL757081177 1 20080911 A 5330 SKIN BOEING 757 757232 1384965 NM BS 620 S16L DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 SKIN DAMAGE STATION 620 STRINGER 16 LEFT. REPAIR INSTALLED PER SRM 53-00-01. 2 L 7 2 4F RT A2NM 20080923 NM 2008 9 23 DL757081185 1 20080906 A 5315 STRAP BOEING 757 757232 1384965 NM BS 1390 RBL 48 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 CABIN FLOORBEAM LOWER TORSION STRAP REQUIRES REPLACENT AT STA 1390 RBL 48 2 L 7 2 4F RT A2NM 20080923 2008 9 23 2008UALA05418 4 20080822 A 2565 H2052K3833 LATCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT O/W SLIDE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 RIGHT OVERWING SLIDE COMPARTMENT DOOR LATCH NR 3 SLIDER GOUGED. FOUND NR 3 LATCH GOUGED. REPLACED LATCH. OPS CHECKS G OOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20080923 NM 2008 9 23 2008UALA05545 1 20080831 A 2432 018550000 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU SMOKE A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 509UA 24763 SMOKE DETECTED IN AFT GALLEY BY OUTBD FA GATE. MECH IN COCKPIT TURNED OFF PWR TO AC. FOUND APU BATTERY SMOLDERED. REPL ACED APU BATTERY & APU BATTERY CHARGER. ALL CHKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080923 NM 2008 9 23 2008UALA05466 1 20080825 A 2920 BLADE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RAM AIR TURBINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 RAM AIR TURBINE BLADES DAMAGED. REPLACED AND OPS CHECKED THE RAM AIR TURBINE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080923 EU 2008 9 23 2008UALA05477 1 20080823 A 2611 PPA120300 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LAVATORY FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 491UA 1741 SMOKE LAVATORY DETECTOR FAULT AT FL350. FOUND DEFECTIVE SMOKE DETECTOR. REPLACED SMOKE DETECTOR. TESTS OKAY ON CFDS TE ST & CIDS. 2 L 7 2 4F 4 F RT A28NM E40NE 20080923 NM 2008 9 23 2008UALA05479 1 20080827 A 4920 211734219 CONTROLLER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE APU FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 675UA 29243 APU WILL NOT START. HANGS BETWEEN 0-10% RPM. SHUTS DOWN WITH APU FAULT LIGHT ON. REPLACED APU CONTROLLER, APU BATTERY, BATTERY CHARGER, AND APU STARTER. OPS CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20080923 NM 2008 9 23 2008UALA05480 1 20080825 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR OBSTRUCTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 DOOR 2L WILL NOT ARM. FOUND LANYARD CAUGHT IN GIRT BAR. STOWED LANYARD. DOOR OPERATES NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080923 NM 2008 9 23 2008UALA05490 1 20080825 A 5754 WEDGE BOEING 737 737322 1384676 NM NR 3 SLAT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 302UA 23643 LT NR 3 SLAT WEDGE HAS DAMAGE. REMOVED NR 3 SLAT, R&R R425 60 TO SHOP AND RE-INSTALLED. INSPECTED INSTALLATION, FOUND OK AY. 2 L 7 2 4F RT A16WE 20080923 NM 2008 9 23 2008UALA05496 1 20080827 A 7160 NOSE COWL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 NR 1 ENG NOSE COWL HAS DAMAGE AT THE 5 OCLOCK POSITION. REPLACED NR 1 ENG NOSE COWL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080923 SO 2008 9 23 SWIA200820014 1 20080903 A 3010 VALVE EMB 120 EMB120ER 3260203 SO DE ICE BOOTS MALFUNCTIONED A SWIA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 NM 07 216SW 120285 AFTER TAKEOFF, "DUCT LEAK" AURAL AND "DUCT LEAKAGE" ON LEFT ENGINE ILLUMINATED. PERFORMED PRECAUTIONARY SHUTDOWN OF LT ENGINE. CHECKED ALL POSSIBLE SOURCES FOR WARNING. SUSPECT LT DEICE NOT REGULATING PRESSURE CORRECTLY, REPLACED VALVE. RAN LEFT ENGINE AT VARIOUS POWER SETTINGS AND BLEED CONFIGURATIONS AND DEICE BOOTS FOR REGULATING VALVE; ALL CKS GOOD. PN 38E96-6A, SN ON RR-1894, SN OFF 99-047. 2 L 7 2 4T RT A31SO 20080923 EA 2008 9 23 SWIA200820015 1 20080903 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 936SW 7726 LT WING FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED, CHECKS GOOD. 2 L 7 2 4F RT A21EA 20080923 EA 2008 9 23 SWIA200820017 1 20080906 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA LEFT ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 07 464SW FAINT RUBBER BURNING ODOR ON SHORT FINAL WITH APU OFF. NO VISIBLE SMOKE. FOUND LEFT ACM BAD. REPLACED LEFT ACM. 2 L 7 2 4F RT A21EA 20080923 NM 2008 9 23 DL764081124 1 20080827 A 2730 COMPUTER BOEING 767 767432ER 1385134 NM ELEVATOR FEEL MALFUNCTIONED A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 829MH 29700 ELEVATOR FEEL EICAS MESSAGE DURING CLIMB-OUT. REPLACED ELEV FEEL COMPUTER PER AMM. LEAK CK OK. ADJ AND TEST CK OK PER 767-400 AMM. MFG NR 162900-100. 2 L 7 2 4F RT A1NM 20080923 NM 2008 9 23 08FDEA03116 1 20080729 A 5230 ACA72251 BEAM DOUG MD11 MD11F 3023600 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 CRACK INDICATION FOUND SECOND LAYER DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 7 LOWER JA MB AT HOLE C. MAIN CARGO DOOR NR 7 LOWER JAMB AT HOLE C, CRACKED SECOND LAYER REPAIRED AS PER FEDEX EA NR 1-5310-124330 , TITLE: FUSELAGE, MAINFRAME, MAIN CARGO DOOR LOWER JAMB BORE HOLES AT STA 757.708. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080923 NM 2008 9 23 08FDEA03185 1 20080730 A 5347 AFA779513 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 MAIN DECK SEAT TRACK AT STA 1887 TO STA 1853, X = 8 FOUND CORROSION. MAIN DECK CORRODED SEAT TRACK REPAIRED BY SECTIONA L SEAT TRACK REPLACEMENT AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080923 EU 2008 9 23 08FDEA03126 1 20080729 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 CABIN SEAT TRACK HAS CORROSION BETWEEN FRAME 30 AND FRAME 31; RBL 37 INCHES. REMOVED CORROSION IAW AMM 51-74-10-8; PGS 1-2. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED DAMAGED SEAT TRACK, DRILLED IAW SRM 51-40-21 PARA 7 AND SRM 53-10-16 FIG 201/201A. ALODINED IAW SRM 51-21-10. PRIMED IAW SRM 51-23-10. RESTORED CIC IAW SRM 51-22-00. 2 L 7 2 4F RT A35EU 20080923 EU 2008 9 23 08FDEA03478 1 20080818 A 5330 A53973402200 DOUBLER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON DOUBLER AT BULK CARGO DOOR CUT OUT C 67-69, P 45-46 RT. REPAIR PERFORMED BY CORROSION REWORK, NDT FO R CORROSION FREE CONDITION AND FLAP PEENING IAW RAS/EFW/9000073/2008 ISS A, APPROVED BY EA 6-5317-123021. 2 L 7 2 4F RT A35EU 20080721 NM 2008 7 21 SWAA083535 1 20080625 A 5315 141A5160 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 769SW 30588 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 344, RBL 2. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083634 1 20080701 A 5315 6546809 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 947.5, LBL 55. REPAIRED CHORD PER ER. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083858 1 20080713 A 5310 6545808 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FWD SERVICE DOOR CUOUT FWD FRAME CRACKED AT BS 294.5, STR 7R. REPAIRED FRAME PER SRM . 2 L 7 2 4F RT A16WE 20080721 EA 2008 7 21 A6WA200840341 1 20080414 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA BS 605 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 443AW 7781 FLOOR LANDING PLATE CRACKED AT FS 605, LBL 42. - - DAMAGE CUTOUT, NDT PERFORMED ON CUTOUT, REDUNDANT HOLE PLUGGED IAW R EO 601R-53-61-433. . 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840359 1 20080422 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LACK OF LUBE A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 13 454AW 7842 CANNOT OPEN SERVICE DOOR FROM OUTSIDE. CLEANED AND LUBED SERVICE DOOR HANDLE AS REQUIRED IAW AMM 52-40-00. OPS CHECK G OOD. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840354 1 20080419 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA BS 574-621 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 13 443AW 7781 CORROSION ON FLOOR LANDING PLATE AROUND NUT PLATES HOLES BTWN FS 574 TO FS 621 AND AT LBL 44. CORROSION REMOVED ON FLO OR LANDING PLATE AROUND NUT PLATES HOLES BTWN FS 574 TO FS 621 AND AT LBL 44 IAW SRM 51-21-06. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840356 1 20080418 A 5320 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA BS 574 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 13 443AW 7781 CHANNEL CRACK AT FS 574 FWD TRACK OF CARGO DOOR. CRACKED CHANNEL REPLACED IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840371 1 20080430 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 INTERCOSTAL FS 484 CRACK AT RBL 29 AND RBL 36. INTERCOSTAL FS 484 AT RBL 27 AND RBL 36 ANGLE INSTALLED IAW REO 601R-53- 41-059 REV A. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840378 1 20080501 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 PAX DOOR AFT DRAG ANGLE FOUND CRACKED. PAX DOOR DRAG ANGLE REPAIRED IAW REO 601R-52-11-513. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840390 1 20080429 A 5320 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 531.75 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 HYD SUPPORT BRACKET CRACK IN LT MLG BAY AT FS 531 AND BTWN LBL 18 - 27. REPLACED IAW SRM 51-42-06. (A) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840382 1 20080506 A 5420 STRIP CNDAIR CL600 CL6002B19 1900309 EA RT NACELLE CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 RT ENGINE NOSE ACCESS COWL (LOWER) TRAILING EDGE STRIP CHAFED BEYOND LIMIT. RT ENGINE NOSE ACCESS COWL (LOWER), NEW TRA ILING EDGE STRIP INSTALLED IAW CMM 71-14-01-300-815-A01. 2 L 7 2 4F RT A21EA 20080721 EU 2008 7 21 08FDEA02877 1 20080715 A 5730 A57340085206 SKIN AIRBUS A300 A300F4622R 3930360 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON LT TOP SKIN AT FRONT SPAR AREA BETWEEN RIB 24-28 REPAIR PERFORMD BY CORROSION REWORK , NDT FOR CRACK FREE CONDITION AND INSTALLING FIRST OVERSIZED FASTENER IAW. RAS/BAE/1007273/2008 ISS.A, APPROVED BY EA 6-5720-120110. 2 L 7 2 4F RT A35EU 20080721 EU 2008 7 21 08FDEA02535 1 20080627 A 5321 B5327027600400 FLOOR PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 252 RT IS CRACKED. FABRICATED A NEW FLOOR PANEL; LOCATED HOLES FROM THE OLD PANEL AS A TEMP LATE; POTTED INSERTS; POTTED; CURED; SANDED EDGES SMOOTH; APPLIED NON-SKID & PART MARKED IAW DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080721 EU 2008 7 21 08FDEA02543 1 20080627 A 5321 B5327060001300 FLOOR PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 242 QJ IS CRACKED & CRUSHED. FABBED A NEW FLOOR PANEL; POTTED EDGES; CURED; SANDED; POTT ED INSERTS; APPLIED NON-SKID & PART MARKED IAW DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080721 EU 2008 7 21 08FDEA02878 1 20080715 A 5315 A53974268200 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON CROSSBEAM C 56 AND C 58 SPLICE REPAIR PERFORMED IAW. SRM 53-10-15 FIG. 205. 2 L 7 2 4F RT A35EU 20080721 EU 2008 7 21 08FDEA02880 1 20080715 A 5320 A53974275202 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON CORNER FITTING C58 REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080718 WP 2008 7 18 MWE2008F00005 1 20080711 A 5270 PROXIMITY SWITCH DOUG DC9 DC981 3022081 WP PWA JT8 JT8D* NE CARGO DOOR FAILED A MWEA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 13 803ME 48029 MID CARGO DOOR LIGHT CAME ON. REMOVE AND REPLACED PROXIMITY SWITCH. (K) 2 L 7 2 4F 4 F A6WE E2EA 20080718 CE 2008 7 18 EHA2008F00000 1 20080624 A 2133 PRESSURE VALVE LEAR 35 35A 5170602 CE CABIN PRESSURE STUCK E EHAA O OTHER O OTHER NR NOT REPORTED 1 AL 03 405PC 35A651 EMERGENCY PRESSURIZATION ACTIVATED. T/S FOUND LT EMERGENCY PRESSURE VALVE STUCK IN EMERGENCY. SUSPECT BURNED SOLENOID. (K) 2 L 7 2 4F A10CE 20080718 EU 2008 7 18 UPS08152416 1 20080521 A 5753 SKIN AIRBUS A300 A300F4622R 3930360 EU T/E FLAP CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 137UP 0820 INSPECTION TYPE:3C LEFT I/B FLAP UPPER L/E SKIN CHAFED 8 INCH HORIZONTALLY. REMOVED DAMAGED AREA, FABRICATED AND INSTAL LED REPAIR DOUBLER IAW A300-600 SRM 57-50-00. 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 ANC2008F00000 1 20080712 A 5100 UNKNOWN BOEING 757 757236 1384971 NM RROYCE RB211 RB211535E4 54555 NE UNKNOWN W ANCF O OTHER O OTHER NR NOT REPORTED 1 SO 23 521NA 25592 PILOT REPORT 4274013-1: DURING SINGLE ENG TAXI WHILE APPLYING THRUST RT ENGINE STALLED THEN AFTER THE LT ENG WAS STARTED , IT ALSO STALLED LT ENG LIMITER COME ON AT THE EICAS. LT BVCU SHOWS CODE 07, IAW FIM 75-32-00 TABLE 102 GEN DEDICATED CONTROL UNIT "B" WAS REPLACED IAW AMM. THE RT BVCU SHOWS CODE 12, IAW FIM 75-32-00 TABLE 102 WAS CHECKED RESISTANCE BET WEEN D1364 TO D1388/D1484 AND RT IP BLEED VALVE SOLENOID D1352 AND THESE VALUES ARE INTO THE ACCEPTANCE LIMITS. ACCORDI NG TO FIM 71-06-00/FIG 104, BLOCKS 12-3-12 AND 25. C/A WAS ACCOMPLISHED. THE RUNNING TEST AMM 71-00-00/ TEST NR 3 AND N R 13 ARE SATISFACTORY. AC IS ON GROUND IN TROUBLESHOOTING PROCESS. (K) 2 L 7 2 4F 4 F RT A2NM E12EU 20080721 EU 2008 7 21 UPS08152417 1 20080521 A 5753 SKIN AIRBUS A300 A300F4622R 3930360 EU T/E FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 137UP 0820 INSPECTION TYPE:3C LEFT I/B FLAP UPPER SKIN MID SECTION 6 INCH LONG GOUGE. REMOVED DAMAGED AREA, FABRICATED AND INSTALL ED REPAIR DOUBLER IAW A300-600 SRM 57-50-00. 2 L 7 2 4F RT A35EU 20080721 NM 2008 7 21 UPS08M52431 1 20080415 A 5730 DOUBLER DOUG MD11 MD11 3023602 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C RT WING FIXED WING L/E AFT SKIN DOUBLER APPROX STA XORS 550 FOUND CRACKED (2522). AFFECTED SKIN DOUBL ER ATTACH PARTS & FASTENERS REMOVED. CRACKED BEADED DOUBLER TRIM OFF. HFEC INSP C/O ON TRIM OFF AREA & FOUND NO CRACK. THREE EACH A REPAIR ANGLES, FILLER & DOUBLER FAB (REF TO EARN: N295UP-0030). THREE EA ANGLES HEAT TREATED. REPAIR PA RTS HOLES PICKED-UP, PROTECTED & PAINTED. THREE EA REPAIR ANGLES, FILLER, DOUBLER & ATTACH PARTS INSTALLED. 2 L 7 3 4F RT A22WE 20080721 NM 2008 7 21 SWAA083737 1 20080707 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 380, LBL 2.5. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083647 1 20080701 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 19L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083796 1 20080709 A 3350 101114 HOUSING BOEING 737 7373G7 1384595 NM EXIT LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND AFT GALLEY EMERGENCY EXIT LIGHT HOUSING BROKEN. REMOVED AND REPLACED LIGHT ASSY PER M M. 2 L 7 2 4F RT A16WE 20080721 EA 2008 7 21 A6WA200840357 1 20080412 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 202 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 13 443AW 7781 CRACK FOUND ON PRESSURE BULKHEAD FS 202.75 LBL 23.71 AROUND PARKING BRAKE. CRACK PRESSURE BULKHEAD REPAIRED IAW REO 601 R-53-11-563. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840370 1 20080422 A 5415 BRACKET CNDAIR CL600 CL6002B19 1900309 EA LT NACELLE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 13 441ZW 7777 LT ENGINE INLET, QTY (2) BRACKETS CRACKED AT 4 & 5 O`CLOCK POSITION NEAR LOWER OUTBOARD T/R ACTUATOR (LOOKING AFT). QT Y (2) BRACKETS AT 4 & 5 O`CLOCK POSITION NEAR THE LOWER OUTBOARD T/R ACTUATOR OF THE LT ENGINE INLET REPLACED IAW CRJ 20 0 SRM 51-42-06. (S) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840385 1 20080429 A 5210 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 STIFFENER CRACK INSIDE PAX DOOR ON FIXED STAIR AFT PANEL. STIFFENER INSIDE PAX DOOR ON FIXED STAIR AFT PANEL REPLACED IA W SRM 51-42-06. (A) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840391 1 20080502 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 CRACK EXISTS ON INTERCOSTAL FS 621 TO 625 LT. REPLACED IAW SRM 51-42-06. (A) 2 L 7 2 4F RT A21EA 20080721 EU 2008 7 21 08FDEA02534 1 20080627 A 5321 B5327048101400 FLOOR PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 241 JF IS CRACKED & BROKEN. FABBED NEW PANEL 241 JF; POTTED INSERTS; POTTED; CURED; SAND ED EDGES; APPLIED NON-SKID TAPE & PART MARKED IAW DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080721 EU 2008 7 21 08FDEA02541 1 20080627 A 5321 B5327060401400 FLOOR PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 242 EK IS CRACKED & CRUSHED. FABBED A NEW FLOOR PANEL; POTTED EDGES; CURED; SANDED; POTT ED INSERTS; APPLIED NON-SKID & PART MARKED IAW DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080721 NM 2008 7 21 SWAA083771 1 20080709 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083785 1 20080708 A 5322 6546530 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 460, STR 16R TO STR 17R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083782 1 20080708 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 10L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083777 1 20080708 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083778 1 20080708 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083727 1 20080705 A 2560 6557463 HOOK BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 R1 DOOR EVAC SLIDE GIRT BAR RETAINING HOOKS LOOSE. SECURED HOOKS PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 2008UALA02856 1 20080518 A 2920 5652535 SWITCH AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE RAT FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 840UA 1522 RAT FAULT DISPLAYED ON UPPER ECAM SCREEN. *S/D* FOUND SWITCH 1GE-E BAD. REPLACED SWITCH. OPS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080721 NM 2008 7 21 2008UALA02701 1 20080508 A 2421 1701768 SHAFT BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE GENERATOR SHEARED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 787UA 26939 ELEC BACKUP GEN L LEFT BACKUP GENERATOR IS OFF OR HAS FAILED. ADVISORY MSG01- LATCHED CRUISE MODE DEPENDENT; BACKUP GE NERATOR (L) OIL PRESSURE IS LOW. DB- BACKUP CONVERTER MSG02- ACTIVE CRUISE MODE DEPENDENT; BACKUP GENERATOR (L) HAS A S HEARED SHAFT. DB- BACKUP CONVERTER MSG03- NOT ACTIVE CRUISE MODE DEPENDENT; BACKUP GENERATOR (L) SPEED IS OUT OF RANGE. DB- BACKUP CONVERTER MSG04- NOT ACTIVE CRUISE MODE DEPENDENT; BACKUP GENERATOR (L) SPEED IS OUT OF RANGE. MSG-2446080 LATCHD ER MODE MSG-2446000 ACTIVE ER MODE MSG-2447000 INACTV ER MODE MSG-2447000 INACTV ER MODE. FOUND SHEARED SHAFT O N BACKUP GENERATOR. REPLACED NR 1 ENG BACK UP GENERATOR REF 24 -25-01. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080721 NM 2008 7 21 SWAA083623 1 20080630 A 2121 6454051 FAN BOEING 737 7373H4 1384600 NM E&E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 618WN 28034 FLIGHT CREW REPORTED AN ELECTRICAL ODOR IN CABIN. TURNED OFF RECIRC FAN ODOR DISSIPATED. REMOVED AND REPLACED RECIRC F AN PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083628 1 20080701 A 5315 147A5504 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 769SW 30588 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, LBL 22 TO RBL 4. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083658 1 20080702 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 19L. REMOVED AND REPAIRED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083657 1 20080702 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 8L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083664 1 20080702 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 21L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083687 1 20080703 A 2560 6557463 HOOK BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 228WN 32496 R1 DOOR EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER MM. 2 L 7 2 4F RT A16WE 20080721 2008 7 21 SWAA083688 4 20080703 A 2565 416A2200 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 237WN 34632 R1 DOOR EVAC SLIDE FELL OUT OF CONTAINER. INSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083690 1 20080704 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 380, STR 15R. REPAIRED STR PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083693 1 20080704 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 500B, STR 16L. REMOVED AND REPLACED CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080923 EU 2008 9 23 08FDEA03479 1 20080818 A 5542 A55471556256 PANEL AIRBUS 300 A300B4622R 3930312 EU RUDDER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON RUDDER SIDE PANEL AT BR NR 1, LT. REPAIR PERFORMED BY REPLACEMENT OF LIGHTNING STRIKE PROTECTION PLA TE AND LAMINATING IAW RAS/DAHAM/4025191/2008 ISS B, APPROVED BY EA 6-5541-120083. 2 L 7 2 4F RT A35EU 20080923 EU 2008 9 23 08FDEA03482 1 20080818 A 5740 A57240048200 NUT AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON LT FWD PICK UP SPHERICAL BEARING NUT. REPAIR PERFORMED BY REPLACEMENT OF NUT IAW AMM 321124/401. 2 L 7 2 4F RT A35EU 20080923 EU 2008 9 23 08FDEA03556 1 20080822 A 7830 WEB AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 650FE 726 NR 1 ENGINE OUTBD T/R FWD UPPER WEB IS CRACKED. FABBED DOUBLER IAW A300-600 MRA CMM 78-32-02. MATERIAL ID 2024-T3, 0. 063. LOCATED HOLES IAW A300-600 MRA CMM 78-32-02. ALODINED, PRIMED AND INSTALLED DOUBLER IAW A30-600 MRA CMM 78-32-02. MATERIAL PO NR 614899.3. 2 L 7 2 4F RT A35EU 20080923 NM 2008 9 23 08FDEA03557 1 20080822 A 5330 SKIN BOEING 757 75723A 1384967 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 TWO DENTS FOUND ON FUSELAGE SKIN AT RT STA 395, WL208.10. REPAIR CARRIED OUT IAW FEDEX EA NR F-5330-111008. REPEAT INS PECTION REQUIRED WHEN AIRFRAME ACCUMULATES 37,500 FC AND THEREAFTER AT 12,000 FC INTERVAL. REPAIR IS CLASSIFIED AS MA JOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080923 NM 2008 9 23 08FDEA03558 1 20080822 A 5315 141N5113 FLOORBEAM BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 MAIN CARGO FLOORBEAM AT BS 377, LBL 22 HAS CORROSION. MINOR CORROSION ON FLOORBEAM REMOVED, TREATED, AND IS WITHIN ALLO WABLE DAMAGE LIMITS IAW SRM 53-00-51 REV 93, FIG 101. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080923 NM 2008 9 23 08FDEA03559 1 20080822 A 5315 141N5111 FLOORBEAM BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 MAIN CARGO FLOORBEAM HAS CORROSION AT BS 345, LBL 21 TO 34. MINOR CORROSION REMOVED, TREATED AND IS WITHIN ALLOWABLE DA MAGE LIMIT IAW SRM 53-00-51 REV. 93, FIG. 101. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080923 NM 2008 9 23 DLM88081099 1 20080821 A 5320 5912494501 PAN DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 917DE 49958 CORROSION WAS FOUND AT C1 LOWER THRESHOLD JAMB PAN AND REPAIRED PER SRM 53-05D FIG 804D. 2 L 7 2 4F RT A6WE 20080923 2008 9 23 DL757081100 4 20080821 A 2330 VIDEO UNIT BOEING 757 757232 1384965 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 618DL 22908 IFE REPORTED BY FA THAT IT SMELLED AS IF IT WERE OVERHEATING. SECURED IFE. AFTER SECURING IFE ODOR IS SLOWLY GOING AWA Y. F/A REPORTED ODOR COMING FROM NR 1 VIDEO UNIT. REPLACED NR 1 VIDEO UNIT OPS CHECKS GOOD. 2 L 7 2 4F RT A2NM 20080924 EU 2008 9 24 08FDEA03331 1 20080808 A 5321 R532B382400000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 251 YG IS DAMAGED. REPAIRED CABIN FLOOR PANEL 251 YG BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARK ED AND APPLIED NON-SKID TAPE IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03564 1 20080823 A 5320 AFA71321 FITTING DOUG MD10 MD1030F 3024020 NM DOOR FRAME CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 304FE 46992 MCD HOLES NR 5 FITTING LWR JAMB SUPPORT 2 EA AFT HOLES HAVE CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-50-00 PA GE 81 FIG 17. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR AND IS RII. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 08FDEA03565 1 20080823 A 5320 AFA71321 FITTING DOUG MD10 MD1030F 3024020 NM DOOR FRAME CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 304FE 46992 MCD HOLES NR 7 FITTING LWR JAMB SUPPORT 2 EA INBD HOLES HAVE CORROSION REMOVED AND REPLACED FITTING IAW SRM 53-50-00 PAG E 81 FIG 17. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR AND IS RII. 2 L 7 3 4F RT A22WE 20080924 EU 2008 9 24 08FDEA03343 1 20080808 A 5321 R532B364200100 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 242 MF IS DAMAGED. REPAIRED CABIN FLOOR PANEL 242 MF BY FABBING A NEW PANEL USING THE OLD PANEL AS A T EMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKE D AND APPLIED NON-SKID TAPE IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03345 1 20080808 A 5321 R532B370900000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 241 WH IS DAMAGED. REPAIRED CABIN FLOOR PANEL 241 QH BY FABRICATING A NEW PANEL USING THE OLD PANEL A S A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SKID TAPE IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03360 1 20080810 A 5314 6518636156 KEELBEAM BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 RIGHT KEEL BEAM CHORD IS CRACKED AT STA 872. ACCOMPLISHED REPAIR ON RIGHT KEEL BEAM CHORD AT STA 872 IAW FEDEX EZ 7-531 0-117026, MLG WHEEL WELL KEEL BEAM CRACK AT BS 872 REPAIR. 2 L 7 3 4F RT A3WE 20080924 WP 2008 9 24 08FDEA03576 1 20080825 A 5245 SKIN DOUG MD10 MD1010F 3022112 WP NR 1 PACK DOOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 DENTS JUST BELOW THE NR 1 PACK DOOR HANDLE, FOUND DURING INCOMING INSPECTION. REMOVED THE DAMAGED AREA BELOW THE NR 1 P ACK DOOR HANDLE PER DC/MD-10 SRM 52-10-00; FIG 2; VOL I. FABBED, LOCATED AND DRILLED THE FILLER; INTERNAL AND EXTERNAL DOUBLERS PER DC/MD-10 SRM 52-10-00; FIG 2; VOL 1. ALODINED PER DC/MD-10 SRM 51-21-01; PARA 31; VOL II. PRIMED PER DC/ MD-10 SRM 51-21-01; PARA 24; VOL II. INSTALLED PER DC/MD-10 SRM; FIG 2; VOL I. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 08FDEA03577 1 20080825 A 5711 65162322 SPAR BOEING 727 727233 138408A NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 CORROSION ON RIGHT WING FRONT LOWER SPAR CHORD AT FSS 514. REMOVED CORROSION, VERIFIED REMAINING MATERIAL TO BE 0.123", HFEC INSPECTED ALL OPEN HOLES WITH NO DEFECTS NOTED, PERFORMED ULTRASONIC INSPECTION OF BLENDED AREAS, NO DEFECTS NOTED , SPOT FACED FASTENER HOLES, FLAP PEENED AREA AND REFINISHED AREA IAW EZ 7-5710-117014, WINGS, AD 2005-05-19 - EO 7-5740 -7-5000, RT WING LOWER FORWARD SPAR CORROSION AT FSS 514, REPAIR. 2 L 7 3 4F RT A3WE 20080721 NM 2008 7 21 SWAA083681 1 20080702 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 665, LBL 24.5. REPAIRED CHORD PER SWA EA. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083683 1 20080702 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 27R CORRODED AT BS 538. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 2008UALA02952 1 20080521 A 3350 POWER SUPPLY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 541UA 25253 EXTERIOR EMERG LIGHT AT DOOR R1 IS INOP. POWER SUPPLY FAILURE. REPLACED POWER SUPPLY M730. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080721 NM 2008 7 21 2008UALA02953 1 20080521 A 3350 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 541UA 25253 EMERGENCY LIGHT TEST SWITCH AT DOOR 4L IS BROKEN. REPLACED SWITCH, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080722 NM 2008 7 22 2008UALA02881 1 20080517 A 3510 MF20003 OXYGEN MASK BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CREW O2 DEFECTIVE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 773UA 26929 CREW COMMENTS: F/O O2 MASK STRAPS WILL NOT TIGHTEN. SUSPECT PRE FLIGHT CHECKS. REPLACED FIRST OFFICERS OXYGEN MASK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080722 NM 2008 7 22 2008UALA03036 1 20080528 A 5753 113W30034 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE T/E FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 780UA 47315 26944 RIGHT O/B FLAP UPPER SURFACES ARE WORN. SUSPECT NORMAL AC OPERATION. ACP RPR FROM AMECO 777EN 57-0040-01. THE REPAIR IS APPROVED BY BAC 8100-9. THE REPAIR IS PERMANENT REPAIR. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080722 NM 2008 7 22 2008UALA03037 1 20080528 A 5753 113W21009 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE T/E FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 780UA 47315 26944 LEFT WING I/B TRAILING EDGE MAIN FLAP UPPER SURFACE HAS CRACK AT LOCATION AT 82 INCHES FROM I/B END. SUSPECT NORMAL AC OPERATION. ACP REPAIR PER AMECO 777EN -57-0044-01. THE REPAIR IS APPROVED BY BAC 8100-9 THE REPAIR IS A PERMANENT REPA IR. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080722 2008 7 22 2008UALA02910 4 20080520 A 2565 62772221 SLIDE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L2 DOOR MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 213UA 30219 ENTRY DOOR 2L ESCAPE SLIDE SAFETY PIN HOLE IS OBSTRUCTED. SUSPECT IMPROPERLY INSTALLED. REPLACED SLIDE PER MM 25-6 6-0 1-401. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080722 NM 2008 7 22 2008UALA02994 1 20080524 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR DIRTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 536UA 25156 THE 3R WILL NOT ARM. CLEANED AND LUBED 3R GIRT BAR FITTING, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080722 NM 2008 7 22 2008UALA03034 1 20080526 A 3510 80404415 OXYGEN BOTTLE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE CREW O2 READS LOW A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 792UA 26934 CREW O2 READING 1350 PSI. SUSPECT FAULTY OXYGEN BOTTLE. REPLACED O2 BOTTLE, LEAK CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080722 NM 2008 7 22 2008UALA03047 1 20080527 A 2721 233T620121 CONTROL PANEL BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE COCKPIT FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 668UA 30024 RUDDER TRIM INTERMITTANT NO RESPONSE IN POSITION GAUGE OR IN RUDDER POSITION MAINT TEXT: DEBRIEF INBOARD CREW: RUDDER T RIM SWITCH ON THE PANEL WAS INTERMITTANT. SUSPECT FAULTY TRIM CONTROL PANEL. REPLACED RUDDER TRIM CONTROL PANEL PER MM 27-28-05 P401 AND OPS CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 NM 2008 7 22 2008UALA03069 1 20080529 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 ENGINE MALFUNCTIONED A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 217UA 30550 CREW REPORTED RT ENG IDG DRIVE LIGHT ILLUMINATED. SUSPECT FAULTY BEARING. REPLACED RT IDG PER MM 24-11-01. OPS CHECK ED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080722 2008 7 22 2008UALA03002 4 20080526 A 2565 D31591478U1 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 927UA 26649 SLIDE PACK AT DOOR 1L NOT SECURE. SUSPECT IMPROPERLY INSTALLED SLIDE ASSEMBLY. RE-ATTACHED SLIDE ASSEMBLY. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA02928 1 20080520 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 MAIN CABIN FLOORBEAM STA 324 CORRODED. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED DAMAGE, FABRICATED AND INSTALLED REPA IR IAW SRM 53-00-98 PG 842 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E17NE 20080722 NM 2008 7 22 2008UALA03051 1 20080527 A 3350 20131A POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 656UA 25394 FWD LT OVERHEAD EXIT SIGN IS INOP. SUSPECT POWER SUPPLY. REPLACED POWER SUPPLY PER MM 33-51-07. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080924 EU 2008 9 24 08FDEA03139 1 20080729 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CABIN SEAT TRACK BETWEEN FRAMES 49 AND 47 AT RBL 57 INCH HAS WORN SCALLOPS. SEAT TRACK FOUND TO BE OUT OF LIMITS I AW A300-600 SRM 53-10-16. REMOVED SEAT TRACK IAW A300-600 SRM 51-40-21. RECEIVED NEW SEAT TRACK P/N A5327400500053, PO 617932.1 IAW A300-600 SRM 53-14-16. CUT AND DRILLED NEW SEAT TRACK IAW A300-600 SRM 53-10-16. INSTALLED NEW SEAT TRAC K IAW A300-600 SRM 53-10-16 AND AIRBUS DWG A53812914. APPLIED CIC TO THE SEAT TRACK IAW A300-600 AMM 51-22-00-0. 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03580 1 20080825 A 2432 400704 RECTIFIER DOUG MD11 MD11F 3023600 NM MALFUNCTIONED A FDEA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 CE 21 595FE 48553 EMERGENCY PWR ON ALERT INFLIGHT. WHEN SELECTED OFF, DC3 DID NOT APPEAR POWERED. EMERGENCY PWR ARM AND ALERT STAYED ON . ADG DEPLOYED. ON SHORT FINAL DC3 UNPOWERED WITH LOSS OF ADG POWER RESULTING IN LOSS OF ASSOCIATED SYSTEMS. FLIGHT DIVERTED DFW AND LANDED WITHOUT INCIDENT. INTEREGATED EPCU FOUND TR-3/INTFC FAULT. WORK ACCOMPLISHED PER AMM &TSM 24- 30-00/24-31-01-2. REMOVED & REPLACED NR 3 TR PER AMM 24-31-01. ACFT RELEASED FOR SERVICE. 2 L 7 3 4F RT A22WE 20080924 WP 2008 9 24 08FDEA03581 1 20080825 A 3241 142109 CONTROL UNIT DOUG MD10 MD1010F 3022112 WP ANTI-SKID SYS INOPERATIVE A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 CE 21 375FE 46613 ANTI-SKID FAIL ALERT ON SHORT FINAL WENT AROUND RAN RED TABS WHICH HAD US DO ANTI-SKID TEST, ALERT WENT OUT. ALERT REAP PEARED ON NEXT GEAR EXTENSION. A/C C/W GO AROUND AND LANDED WITHOUT INCIDENT. T/S ANTI SKID FAULT CODES PER FIM 32-45- 20. REMOVED AND REPLACED ANTISKID CONTROL UNIT PER MM 32-45-01-5. ALL TESTS PASSED. ACFT OK FOR SERVICE. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 08FDEA03793 1 20080910 A 5330 6554581 SKIN BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 LOWER FUSELAGE STATION 1010 STRINGER 30 HAS AREA OF CORROSION ON EXTERIOR. REMOVED CORROSION AREA DAMAGED BEYOND LIMITS. NDT VERIFIED ORIG MATERIAL THICKNESS TO BE .071 "MATERIAL LOSS IS .009" REMAINING MATERIAL IS .062". FABRICATED REPAI R DOUBLER AND FILLER REF SRM 53-30-3, FIG 3A/NDT MAN PART 6, 51-00-00, FIG 23, SRM 51-10-2 PG 2-7. THIS IS CLASSIFIED A S A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080924 WP 2008 9 24 08FDEA03794 1 20080910 A 5754 ARC050469 RETAINER DOUG MD10 MD1010F 3022112 WP TE FLAP FAIRING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING OUTBD FLAP INBD FAIRING OUTBD SIDE PANEL 535 DL HAS A CRACK SEAL RETAINER. REMOVED SEAL RETAINER IAW SRM 51 -31-01. FORMED A NEW SEAL RETAINER IAW SRM 51-10-00. ALODINED & PRIMED THE SEAL RETAINER IAW SRM 51-31-01. DRILLED UP THE NEW SEAL RETAINER & INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F RT A22WE 20080924 EU 2008 9 24 08FDEA03795 1 20080910 A 5220 A5227107320000 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 LEFT OVERWING EMERGENCY EXIT; INBD UPPER FWD & AFT CORNER CHAFE STRIPS ARE MISSING WITH SKIN CHAFED. REMOVED COVER PL ATE IAW SRM 51-40-21. LOCATED & DRILLED COVER PLATE IAW SRM 51-40-21. ALODINED COVER PLATE IAW SRM 51-21-10. INSTALLE D 3 EA CHAFE STRIPS IAW CMM 52-23-11. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03241 1 20080804 A 5753 A5796000720000 SKIN AIRBUS 300 A300F4605R 3930327 EU RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 RIGHT WING INBD FLAP UPPER SKIN IS CREASED 3' FROM THE OUTBD END. SMOOTHED DENT IAW SRM 51-73-10. DENT DEPTH 0.049. O RIGINAL MATERIAL THICKNESS IS 0.031. NO MATERIAL LOSS NOTED, FOUND TO BE WITHIN LIMITS IAW SRM 57-50-00, FIG 101. DENT DIAMETER 1.25 INCH, ALODINED AND PRIMED IAW SRM51-21-10. APPLIED FILLER IAW A300-600 SRM 51-73-10 3-B. TOPCOATED IAW SRM 51-23-10. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03244 1 20080804 A 5753 A5796000720000 SKIN AIRBUS 300 A300F4605R 3930327 EU RT WING TE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 RIGHT WING INBD FLAP LOWER T/E SKIN IS GOUGED 7' FROM THE INBD END. REMOVED GOUGE IAW SRM 51-73-10. ORIGINAL MATERIAL 0.028 IAW SRM 57-50-00. MATERIAL REMOVED 0.015. MATERIAL REMAINING 0.013. FOUND TO BE OUT OF LIMITS IAW SRM 57-50-0 0. REPAIRED AREA IAW SRM 57-50-00. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03608 1 20080828 A 5720 FXA93540675200 SUPPORT BRACKET AIRBUS 310 A310222 3930315 EU LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 455FE 331 LT WING, REAR SPAR SURFACE 1, RIB 4, HYD TUBE SUPPORT BRACKET WITH INNER- GRANULAR CORROSION (DELAMINATED). REMOVED TH E CORRODED TUBE SUPPORT BRACKET. FABRICATED A NEW BRACKET PER AIRCRAFT DRAWING 25 A935-40675. INSTALLED THE NEW BRACKE T AND HYD TUBES PER AMM 20-21-12-0 AND AMM 20-23-11-0. PERFORMED LEAK CHECK PER AMM 29-00-00-6. NO LEAK FOUND. 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03610 1 20080828 A 5330 6554583153 SKIN BOEING 727 727227 1384078 NM BS 1130 S21-22L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 FUSELAGE LT SIDE DENT AT FWD OF STA 1130 STR 22L AND STR 21L CUTOUT DAMAGE AREA DIM CUTOUT 4 3/4 INCH PER 2 7/8 IAW SRM 53-30-3 FIG 3. FABRICATED DOUBLER REPAIR & FILLER IAW SRM 53-30-2 FIG 2, 53-30-3 FIG 3. TREATED AND PRIMED IAW SRM 51 -10-2. INSTALLED REPAIR WASHERS IAW SRM 51-30-8. INSTALLED REPAIR PARTS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20080924 NM 2008 9 24 08FDEA03612 1 20080828 A 5330 65545772 SKIN BOEING 727 727227 1384078 NM BS 720D S30L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 FUSELAGE SKIN HAS CORROSION BY CARGO HEAT OUTFLOW VALVE FLANGE AT STA 720D AND STR 30 REMOVED CENTER FAIRING AT STA 720D AIR DUCT AND 02 EA SUPPORT BRACKETS FOR ACCESS IAW SRM 51-30-2. CUTOUT DAMAGED AREA DIM 4 INCH PER 3 INCH. FABRICATED REPAIR DOUBLER AND 2 REPAIR FILLERS IAW SRM 53-30-3 FIG 1, AND 53-30-2 FIG 3. TREATED AND PRIMED PARTS AND AREA IAW SR M 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-30-1 FIG 1. REINSTALLED REMOVED PARTS FOR ACCESS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20080924 NM 2008 9 24 DLM90081114 1 20080721 A 5320 CUSP WEB DOUG MD90 MD9030 3023690 NM FS 360 LBL 54 PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DN 53395 CABIN CUSP WEB PUNCTURED ON I/B SIDE OF SEAT TRACK AT FS 360 CBL 54/CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IA W SRM 51-11-01 VOL 1. 2 L 7 2 4F RT A6WE 20080924 NM 2008 9 24 DLM90081115 1 20080730 A 5330 SKIN DOUG MD90 MD9030 3023690 NM BS 795-885 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DN 53395 CORROSION ON FUSELAGE SKIN STA 795-885 AT ATTACH POINTS FOR LOWER WING TO BODY FAIRING. REPAIRED DAMAGED SKIN IAW SRM 5 3-04 FIG 53. 2 L 7 2 4F RT A6WE 20080924 WP 2008 9 24 08FDEA03171 1 20080730 A 5415 AVB7091501 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 NR 2 ENGINE BEAVER TAIL LEFT SIDE SKIN IS CHAFED UNDER NR 2 AND 3 RIBS. REMOVED DAMAGE IAW DC/MD-10 SRM 54-20-00; VOL I , FIG 9. FABRICATED REPAIR IAW DC/MD-10 SRM 54-20-00; VOL I; FIG 9. INSTALLED IAW DC/MD-10 SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 DL764081117 1 20080825 A 2131 CONTROLLER BOEING 767 767432ER 1385134 NM CABIN PRESSURE MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 827MH 29698 FCP AFT CABIN CONTROL STATUS MSG WITH MEL 21-61-01A. CREW DOING PROCEDURE 2 SET SEVERAL INOP MSGS AND FAULTS. RTB - AB LE TO RESET BOTH CTC'S. ORIGINAL MSG CLEARED NOW HAVE MID B TEMP CONTROL STATUS MSG (ONE PREV) WILL FCP PER MEL 21-61-0 4B. 2 L 7 2 4F RT A1NM 20080924 NM 2008 9 24 08FDEA03015 1 20080722 A 5730 ARB23122 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 577FE 48469 RT WING DROOP LEADING EDGE TOP SURFACE FOUND CRACKED. REPAIR CARRIED OUT AT RT WING DROOP LEADING EDGE TOP SURFACE AS P ER SRM 57-10-00 FIG 30 VOL I. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080728 EA 2008 7 28 TRAX200800891 1 20080707 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 PAX DOOR NOT CLOSING PROPERLY. GREEN ALIGNMENT MARKS WILL NOT ALIGN WITHOUT MOVING HANDLE WITH GREAT FORCE LUBE DOOR HA NDLE IAW AMM 52-00 AC OK FOR SERVICE. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800806 1 20080620 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 930EV LT FS 621 SUPPORT ANGLE CRACKED. REPAIRED ITEM BY ACCOMPLISHMENT OF REO 601R-53-61-117. RII REQUIREMENTS MET PER SP 6 07. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800691 1 20080526 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 924EV 7830 FS 484 ANGLE IS CRACKED AT THE INBOARD SIDE OF LBL 36. REMOVED CABLE GUIDE BRACKETS FOR ACCESS TO REPAIR BY REMOVING B OLTS, NUTS, WASHERS AND COTTERPINS. REMOVED CRACKED ANGLE AND INSTALLED NEW SERVICEABLE ANGLE IAW REO 601R-53-41-059 AN D REO 601R-53-41-734. INSTALLED SAME SERVICEABLE CABLE GUIDE BRACKETS IAW SRM 51-41-04. COMPLIED WITH REO 601R-53-41-05 9. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800738 1 20080603 A 5312 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA BS 409 BULKHEAD CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 824AS 7203 FS 409.0+128 BULKHEAD VERTICAL STIFFENER BEAM AT RBL 27 CRACKED AT INBOARD SIDE AT BOTTOM RADIUS APPROX 1/4" LONG. COMP LIED WITH REPAIR OF BULKHEAD VERTICAL STIFFENER AT RBL 27 IAW REO 601R-53-41-056 AND REO 601R-53-41-056. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800634 1 20080514 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 978EV 7723 AFT FLOOR SUPPORT ANGLE CRACKED AT STA 280 BULKHEAD LBL9. JOB COMPLETE, REPAIRED AFT FLOOR SUPPORT ANGLE AT STA 280 BU LKHEAD LBL 9 IAW REO 601R-53-11-138. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800797 1 20080616 A 5210 STRIKER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR GOUGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 ASD HARD TO OPEN FOUND ASD FORWARD TOP ROLLER STRIKER PLATE GOUGED. UPON INSPECTION OF DOOR FOUND UPPER FORWARD ROLLER DRAGING ON CAM. CHECKED RIGGING ON CONTROL RODS IAW AMM 52-11-21. ADJUSTED UPPER LINK TO CAM AND ADJUSTED SHIMS AT FWD U PPER CAM IAW AMM 52-11-21. DOOR STILL NEEDS CHECKED FOR RIGGING OF THE CAM ASSY AND THE ICE BREAKER (B) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800624 1 20080513 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 835AS 7258 EMERGENCY LIGHTS DO NOT WORK. FLT 4691 DEL 36 MINS REMOVED AND REPLACED BATTERY PACKS, IAW AMM 33-51-01. OPS CHECKED G OOD. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 MASA200800462 1 20080611 A 3397 CONNECTOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 921FJ 15021 ASH FLT 2934 FAT-PHX. SERVICE DOOR EXIT LIGHT INOP. MX CLEANED CONNECTORS--LIGHT OPS GOOD. (B) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800864 1 20080701 A 5310 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.5". REMOVED SUPPORT BEAM LOWER AFT BRACKET AND INSTALLED NEW SER VICEABLE BRACKET IAW SRM 51-42-21. LEAK CHECK DUE. PRESSURIZED ACFT IAW AMM 21-32-00-863-801. LEAK CHECK GOOD. (S) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 AALA200801351 1 20080519 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 385AM 27059 DFW EMERGENCY LIGHT AT SEAT 21B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21B. SYSTEM GROUND CHECKED NORM AL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A1NM 20080728 NM 2008 7 28 USAA920081307 1 20080617 A 3350 BR964411 LIGHT BOEING 737 7373S3 1384711 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 316AW 23713 CLT - C22 - MAJOR REPAIR - SEAT ROW 20ABC EMERGENCY ESCAPE PATH LIGHT IS NOT WORKING. REPLACED AND OPERATIONAL CHECKED SEAT ROW 20ABC EMERGENCY ESCAPE PATH LIGHT ASSEMBLY. (S) 2 L 7 2 4F RT A16WE 20080728 EU 2008 7 28 USAA920081196 1 20080609 A 5540 D5587131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 640AW 448 SAL - MAJOR REPAIR - C3 CHECK - NR 2 RUDDER HINGE FITTING HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 1926 RIB 4. R EPLACED NR 2 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 1926 RIB 5 IAW AMM 55-36-41. (S) 2 L 7 2 4F RT A28NM 20080728 NM 2008 7 28 USAA920081256 1 20080601 A 5320 149N77015 SUPPORT BOEING 757 7572S7 1384962 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 905AW 23567 MCN - C12 - MAJOR REPAIR - LEVEL 2 CORROSION ON CHANNEL SUPPORT AT BS 1200 - 1220, WL 133, BL 10R. REPLACED CHANNEL SUP PORT AT BS 1200 - 1220, WL 133, BL 10R IAW B757-200 SRM 51-40-02-0G. (S) 2 L 7 2 4F RT A2NM 20080728 NM 2008 7 28 2008UALA03353 1 20080612 A 2781 TRANSMITTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L/E SLAT OUT OF ADJUST A UALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 29 597UA 28750 FLAP SLAT ELEC MESSAGE ON TAXI OUT. OUT OF ADJUSTMENT (TRANSMITTER). ADJUSTED RIGHT L/E SLAT POSITION TRANSMITTER - RE PLACED LEFT L/E SLAT POSITION TRANSMITTER PER MM 27-88-01-401. ADJUSTED RIGHT L/E SLAT POSITION TRANSMITTER - ELECTRICA L ANGLE FOR FLAP LEVER UP ADJUSTED TO 8.71 BOTH L AND R TRANSMITTERS. 2 L 7 2 4F 4 F RT A2NM E17NE 20080728 NM 2008 7 28 2008UALA03348 1 20080612 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 522UA 24931 EMERGENCY EXIT IDENTIFIER LIGHTS AT 15F AND 16A INOP. LIGHT ASSY HAS A SHORT INTERNAL. REPLACED 16A EMERGENCY EXIT ID ENTIFIER LIGHT ASSY & CLEANED 15F CONNECTOR. OPS CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 SO 2008 7 29 SIM2008F00002 1 20080711 A 3230 LANDING GEAR EMB 135 EMB135KL 3260302 SO MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 840AE 145656 ON FLIGHT 3394, CREW REPORTED ON CLIMBOUT THAT THE GEAR WOULD NOT RETRACT WITH A GEAR LEVER DISAGREE MSG ON EICAS NO CMC MESSAGES. AIRCRAFT LANDED WITHIN WEIGHT LIMITS AND NO EMERGENCY WAS DECLARED. ACFT REMOVED FROM SERVICE. OPS CHECK FO R LG/LEVER DISAGREEMENT MESSAGE- COULD NOT DUPLICATE IAW FRM 32-32-00-810-803-A STEP 1, STEP 2, STEP 9, AND STEP 22. AI RCRAFT RETURNED TO SERVICE. (K) 2 L 7 2 4F RT T00011AT 20080729 EA 2008 7 29 HNA2008F00015 1 20080626 A 6123 AUTOFEATHER SYS DHAV DHC8 DHC8311 1386006 EA FAILED A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 329EN 290 ABORTED TAKEOFF, RETURNED TO GATE. MX GROUND RAN AIRCRAFT AUTOFEATHER ARMED AT APPROX 80 PERCENT, TORQUE AT 40 DEGREES, PLA OK FOR SERVICE. AUTOFEATHER HAD FAILED TO ARM AT 85 PERCENT TORQUE ON TAKEOFF ROLL. (K) 2 H 7 2 4T RT A13NM 20080729 NE 2008 7 29 UIE2008F00010 2 20080625 A 7200 ENGINE BOEING 747 74747UF 1384812 NM GE CF6 CF680 30025 NE NR 2 POWER LOSS A UIEA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 EA 15 492MC 29253 ON TAKEOFF ROLL POWER WAS ADVANCED TO 70 PERCENT. N1 ENGINE 1,3, AND 4 ADVANCED NR 2 LAGGED SIGNIFICANTLY BEHIND, TAKEO FF ROLL ABORTED AT 40 KNOTS, AIRCRAFT TAXIED TO RUNUP AREA WHERE ENGINE RUN UP WAS PERFORMED AND NR 2 WAS NOW NORMAL. ( K) 2 L 7 4 4F 4 F RT A20WE E13NE 20080729 EA 2008 7 29 TRAX200800768 1 20080606 A 5297 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA DOOR ASSIST ACT DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 931EV 8015 DOOR ASSIT ON PASSENGER DOOR NOT CLOSING DOOR FULLY. GOES UP APPOX 1/3 TO 1/2 WAY UP AND STOP. (PASSENGER DOOR POWER ASS IST SYSTEM). REMOVED AND REPLACED PAX DOOR ELECTRICAL HARNESS ASSY IAW CRJ 200 AMM 52-70-04. OPS CHECK GOOD. DML CLEARED PLACARD REMOVED. (A) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800760 1 20080605 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 873AS 7549 FORWARD EMERGENCY STRIP BROKEN NEXT TO SEAT 1C. REMOVED AND REPLACED FWD 20 FOOT SECTION OF FLOOR TRACK EMERGENCY LIGHT LENS IAW AMM 33-51-01. OPS CHECK OF FLOOR EMERGENCY LIGHT GOOD. (A) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800904 1 20080711 A 5210 CAM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE. FLT 4251 DEL 37 MINS LUBED MAIN CABIN DOOR CAMS IAW AMM 12-20-52 OPS CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800730 1 20080603 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 RT BS 280 WEB CORRODED OUT OF LIMITS. WEB REPLACEMENT. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 2008UALA03586 1 20080624 A 3350 362624 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 775UA 26947 CREW REPORT EEL LIGHTING LOOSE. FOUND LOOSE LIGHT ASSEMBLY. SECURED LIGHT ASSEMBLY. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080729 NM 2008 7 29 USAA920081167 1 20080601 A 5754 65C26602217 WEDGE BOEING 737 73733A 1384673 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 PHX - MAJOR REPAIR - B CHECK - LT WING NR 2 SLAT TRAILING EDGE WEDGE DELAMINATED. REPLACED THE LT WING NR 2 SLAT TRAILI NG EDGE WEDGE IAW DRAWING 65C26602. (S) 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800866 1 20080703 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 837AS 7271 PAX DOOR LOWER STEP CRACKED. REMOVED AND REPLACED LOWER PAX DOOR STEP IAW AMM 52-11-04. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800849 1 20080628 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 753EV 10169 EMERGENCY LIGHT IN GALLEY NEAR SERVICE DOOR HAS A COUPLE LIGHTS BURNT OUT. RELAMPED EMERGENCY LIGHT IAW CRJ 700 AMM 33- 51-05. (B) 2 L 7 2 4F RT A21EA 20080729 EU 2008 7 29 TRAX200800654 1 20080518 A 2697 CONNECTOR AEROSP ATR72 ATR72212 8680945 EU SMOKE DETECTOR DAMAGED A ASOA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 27 634AS 370 ELECTRIC SMOKE WARNING ASSOCIATED WITH ELECTRICAL SMELL (NO ACTUAL SMOKE NOTED) TURING FINAL IN MGM, EMERGENCY DECLARED. FLT 4224. REMOVED AND REPLACED RELAY 151WW AND 17WW, INSPECTED ALL CONTRACTORS RELAYS BEHIND F/O`S SEAT AND ALL AVIONI CS RACKS. FOUND BENT PIN ON AVIONICS SMOKE DETECTOR, STRAIGHTEN PIN, ALSO FOUND DUST INSIDE DETECTOR, CLEANED, PERFORME D GROUND ENG RUN WITH FULL LOADED ALL SYSTEMS OPS CHECK GOOD IAW AMM 26-15-00. (B) 2 H 7 2 4T RT A53EU 20080729 NM 2008 7 29 USAA920081250 1 20080615 A 5321 D5367520800200 FLOOR PANEL AIRBUS A319 A319132 3930340 NM AFT CARGO BAY DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 837AW 2595 SAL - BC-02 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 151VG IN AFT CARGO COMPARTMENT. REPLACED FLOOR PANEL 151VG IN AFT CARGO COMPARTMENT IAW AIRBUS A319 SRM 53-02-00. (S) 2 L 7 2 4F RT A28NM 20080729 EA 2008 7 29 TRAX200800656 1 20080518 A 5240 ROLL PIN CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 SERVICE DOOR DIFFICULT TO CLOSE REMOVED AND REPLACED ROLL PIN ON SERVICE DOOR RELEASE HANDLE OPS CHECK GOOD IAW AMM 52- 41-02. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAA920081247 1 20080609 A 5312 651758365 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN - C21 - MAJOR REPAIR - 5 CRACKS ON WEB AT BS 178, WL 226 TO 222, LBL 17. REPAIRED 5 CRACKS ON WEB AT BS 178, WL 226 TO 222, LBL 17 IAW B737 SRM 53-10-08-2R 12. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081248 1 20080609 A 5312 651758365 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN - C21 - MAJOR REPAIR - CRACK ON VERTICAL BEAM WEB AT LINING RETAINER HOLE AT BS 178, WL 178, LBL 5. REPAIRED CRACK ON VERTICAL BEAM WEB LINING RETAINER HOLE AT BS 178, WL 178, LBL 5 IAW B737 SRM 53-10-08-2R 12. (S) 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800877 1 20080704 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 846AS 7328 ESCAPE PATH LIGHTING FWD OF AFT LAV IS CRACKED AND BROKEN REMOVED AND REPLACED EMERGENCY LIGHTING TRACK IAW AMM 33-51-0 1. OPS CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAA920081258 1 20080623 A 3397 BMS13311122 WIRE BOEING 737 7373G7 1384595 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 308AW 24710 FLT 493 - DEN - EEL - CABIN SIDEWALL LIGHTING INOP AT ROW 7 THRU 11 LT SIDE. EMERGENCY SIDEWALL LIGHT INOP. MX REPAIRE D BROKEN WIRE ON CONNECTOR. OPERATIONAL TEST WAS GOOD. (S) 2 L 7 2 4F RT A16WE 20080729 2008 7 29 UASSBA08020 4 20080620 A 3441 46502003030316 ADIRU AIRBUS 330 A330323 3930335 EU NR 3 FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 275AY 4078 0370 MAN FLT 735 EN ROUTE MAN TO PHL. THE FLIGHT HAD AN ADIRU 3 FAILURE PRIOR TO ETOPS AIRSPACE, PREVENTING ETOPS OPERATIONS . THE FLIGHT RETURNED TO FIELD MAN, AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SWAPPED ADIRU 3 WITH ADIRU 2, AND PLACED ADIRU 2 ON MEL. SUBSEQUENT INFO: MAINTENANCE REPLACED ADIRU 2. OPERATIONAL CHECKS OK. (S) 2 L 7 2 4F RT A46NM 20080729 CE 2008 7 29 DXTA200803096 1 20080603 A 2120 UNKNOWN CESSNA 750 750 2076810 CE CABIN ODOR E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 916QS 7500116 MUSTY ODOR IN CABIN WHEN OPERATING THE ACM. (B) 2 L 7 2 4J RT T00007WI 20080729 NM 2008 7 29 USAA920081266 1 20080624 A 2560 P2070001214 FLASHLIGHT AIRBUS A319 A319132 3930340 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 810AW 1116 FLT 662 - PHX - EEL - FORWARD MAIN CABIN EMERGENCY FLASHLIGHT INOP. MAINTENANCE REPLACED THE FLASHLIGHT. (S) 2 L 7 2 4F RT A28NM 20080729 NM 2008 7 29 USAA920081267 1 20080615 A 5210 654587545 STRUCTURE BOEING 737 73733A 1384673 NM R1 DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN - C-21 - MAJOR REPAIR - R-1 DOOR INNER CHORD HAS AREA OF CORROSION AROUND DOME HUT HOLES AT BS 295, STRINGER 17R, WL 208, BL 52R. REPLACED R-1 DOOR INNER CHORD AT BS 295, STRINGER 17R, WL 208, BL 52R IAW B737 SRM 51-40-02-0G. (S) 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800693 1 20080527 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 PAX DOOR HARD TO OPEN. HANDLE OPERATES OK, DOOR REQUIRES HARD PUSH TO OPEN. PERFORMED OPS CHECK OF PAX DOOR PER AMM 52- 10-00. NO DEFECT NOTED. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAASB08043 1 20080624 A 3610 32144464 VALVE BOEING 737 7374B7 1384702 NM LT ENGINE FAULTY A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 444US 52297 52297 24862 FLT 1835 - DURING CRUISE AT FL270, A PRESSURIZATION FAILURE AS CABIN ALTITUDE WARNING HORN SOUNDED. DECLARED AN EMERGE NCY & DESCENDED TO 10,000 FT. ACCOMPLISHED QUICK REFERENCE PROCEDURES & REGAINED CABIN PRESSURE. FLT CONTINUED & LANDE D AT RSW WITHOUT FURTHER INCIDENT. ACCOMPLISHED PRESSURIZATION TROUBLESHOOTING & CARD & FOUND LT PACK SYS LOW FLOW MODE & CABIN PRESSURE LEAK TEST FAILED. R&R LT ENGINE HIGH STAGE VALVE PER MM 36-11-85. CHKD LT PACK LOW FLOW MODE & PRESS URE LEAK TEST. CHECK PASSED. R&R CABIN PRESSURE CONTROLLER. 2 L 7 2 4F RT A16WE 20080729 EU 2008 7 29 USAA920081276 1 20080629 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 660AW 1234 FLT 685 SAN - PHX - EMERGENCY EQUIPMENT - FWD FLIGHT ATTENDANT FLASHLIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE FW D FLIGHT ATTENDANT FLASHLIGHT BATTERY. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A28NM 20080729 SO 2008 7 29 MAS2008F00004 1 20080606 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 FDM 6172 JFK-ALB. RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. MX CLEANED CONNECTION AND OPS CHECKED. (B) 2 L 7 2 4T RT T00011AT 20080729 NM 2008 7 29 USAA920081292 1 20080707 A 5330 6547955533 BEAR STRAP BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 24893 CLT - C2 - MAJOR REPAIR - CORROSION AFT OF CARGO DOOR OPENING LOWER CORNER BS 847 TO 887, S-25R. REPAIRED AREA AFT OF C ARGO DOOR OPENING LOWER CORNER BS 847 TO 887, S-25R IAW EA 100556. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081287 1 20080630 A 5754 65C26661197 SLAT BOEING 737 7374B7 1384702 NM NR 1 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 24893 CLT - C2 - MAJOR REPAIR - FIVE CRACKS IN NR 1 LEADING EDGE SLAT. REPAIRED NR 1 LEADING EDGE SLAT IAW B737 SRM 57-43-01 REPAIR 6. (S) 2 L 7 2 4F RT A16WE 20080729 CE 2008 7 29 DXTA200803141 1 20080624 A 2700 UNKNOWN CESSNA 500 560CESSNA 2076750 CE FLT ATTITUDE UNKNOWN E DXTA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 07 325QS 5600425 THE AIRCRAFT HAS AN AGGRESSIVE ROLL LEFT WITH THE ASSOCIATED TRIM TAB CENTERED. (B) 2 L 7 2 4F RT A22CE 20080729 EU 2008 7 29 USAA920081323 1 20080625 A 5540 D5537131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AW 1196 SAL - BC-06 - MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE NR5, VERTICAL STABILIZER STATION 2985 RIB NR 7. REPLACED RU DDER HINGE FITTING NR 5, VERTICAL STABILIZER STATION 2985 RIB NR 7 IAW AIRBUS A320 AMM 55-36-41. (S) 2 L 7 2 4F RT A28NM 20080729 NM 2008 7 29 USAA920081316 1 20080628 A 5322 SHEAR TIE BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925UW 22205 BFM - MAJOR REPAIR - C3 CHECK - LEVEL 2 CORROSION ON SHEAR TIE, BS 1280, S28-29L. REPLACED SHEAR TIRE, BS 1280, S28-29L IAW B757 SRM 51-40-02. (S) 2 L 7 2 4F RT A2NM 20080729 NM 2008 7 29 USAA920081315 1 20080626 A 5322 SHEAR TIE BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925UW 22205 BFM - MAJOR REPAIR - C3 CHECK - LEVEL 2 CORROSION ON SHEAR TIE, BS 1320, S28-29R. REPLACED SHEAR TIE, BS 1320, S28-29R IAW B757 SRM 51-40-02. (S) 2 L 7 2 4F RT A2NM 20080729 NM 2008 7 29 USAA920081274 1 20080626 A 2560 P4010021 BATTERY BOEING 737 7373S3 1384711 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 313AW 23712 FLT 282 - CREW REPORTED FWD F/A FLASHLIGHT INOP. MX REPLACED FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A16WE 20080729 CE 2008 7 29 DXTA200803134 1 20080619 A 3210 LANDING GEAR CESSNA 750 750 2076810 CE UNKNOWN E DXTA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 GL 07 943QS 7500043 DURING FLIGHT THE LANDING GEAR UNLOCK LIGHT ILLUMINATED SEVERAL TIME IN QUICK SECESSION ACCOMPANIED BY A LOUD THUMPING S OUND. (B) 2 L 7 2 4J RT T00007WI 20080729 EA 2008 7 29 TRAX200800844 1 20080626 A 3250 RVDT CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING OUT OF RIG A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 920EV STEERING INOP CAUTION MSG ON CLIMB OUT AFTER GEAR RETRACTION. ENROUTE TO FNT A/C DIVERTED TO CVG DUE TO MTC--EMERGENCY DECLARED. FLT 4901. UPON INSPECTION FOUND LT AND RT FEEDBACK RVDT`S OUT OF RIG. RIGGED RVDT`S, OPS CHECK GOOD DONE IAW AMM 32-51-20. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAA920081279 1 20080626 A 5330 SKIN BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 917UW 22193 PIT - PYLON SHIM - MAJOR REPAIR - CORROSION ON FUSELAGE SKIN AT BS 1340 S29L. REPAIRED FUSELAGE SKIN AT BS 1340 S29L I AW B757 SRM 53-00-01. (S) 2 L 7 2 4F RT A2NM 20080729 NM 2008 7 29 USAA920081271 1 20080625 A 5330 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 23379 CLT - C5 - MAJOR REPAIR - FUSELAGE SKIN CRACKED AT FORWARD ENTRY DOOR LOWER FORWARD HINGE CUTOUT BETWEEN BS 294-312, BET WEEN S12-14L. REPAIRED FUSELAGE SKIN AT FORWARD ENTRY DOOR LOWER FORWARD HINGE CUTOUT BETWEEN BS 294-312, BETWEEN S12-1 4L IAW B737 SRM 53-10-01 REPAIR 5. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081285 1 20080612 A 5313 BAC1498162 STRINGER BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN - C21 - MAJOR REPAIR - CORROSION ON LOWER SURFACE OF STRINGER 27L BETWEEN BS 947.5 TO 967. REPAIRED STRINGER 27L BE TWEEN BS 947.5 TO 967 IAW B737 SRM 53-00-03-2R1. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081302 1 20080531 A 5315 STIFFENER BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW 23713 CLT - C22 - MAJOR REPAIR - LOWER END OF VERTICAL STIFFENER CRACKED ON FORWARD FACE OF BS 328 FLOORBEAM AT RBL 32. REPAI RED LOWER END OF VERTICAL STIFFENER ON FORWARD FACE OF BS 328 FLOORBEAM AT RBL 32 IAW BOEING DRAWING 65-45812. (S) 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800898 1 20080709 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 922EV 7822 FS 621.00 FLOORBEAM IS CRACKED 1/2 IN LONG ON O/B RADIUS. REMOVED DAMAGED SECTION OF FLOORBEAM AND REPAIRED IAW REO 601 R-53-61-117. NEEDS PAINT AND DINITROL. NEEDS LEAK CHECK. LEAK CHECK GOOD IAW CRJ 200 MM 21-32-00-863-801. TOUCH UP F LOOR SUPPORT ANGLE AT RT FS 621 IAW CRJ SRM 51-21-16. NEEDS DINITROL IAW MM 51-25-56-390-802. C/W ECTC REO 601R-53-61- 117. RII C/W 5300005. (S) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAA920081306 1 20080529 A 5711 6545402 STIFFENER BOEING 737 7373S3 1384711 NM CENTER WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW 23713 CLT - C22 - MAJOR REPAIR - CENTER WING REAR SPAR VERTICAL STIFFENER CRACKED. REPLACED CENTER WING REAR SPAR VERTICAL ST IFFENER IAW B737 SRM 51-40-03. (S) 2 L 7 2 4F RT A16WE 20080728 EU 2008 7 28 USAA920081259 1 20080616 A 5321 D53675210002000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FWD CARGO BAY DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 679AW 2613 SAL - BC-2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 131HF IN FORWARD CARGO COMPARTMENT AT FR 30 - 34, BL Y765 TO Y-7 65. REPLACED FLOOR PANEL 131HF IN FORWARD CARGO COMPARTMENT AT FR 30 - 34, BL Y765 TO Y-765 IAW A320 SRM 53-02-00. (S) 2 L 7 2 4F RT A28NM 20080728 EU 2008 7 28 USAA920081179 1 20080524 A 5540 D5537131800200 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 652AW 0953 SAL - MAJOR REPAIR - C7 CHECK - NR 4 RUDDER HINGE FITTING HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 2632 RIB 6. R EPLACED NR 4 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 2632 RIB 6 IAW AMM 55-36-41. (S) 2 L 7 2 4F RT A28NM 20080728 EA 2008 7 28 A6WA200840417 1 20080514 A 2913 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS FAILED A A6WA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 GL 31 449AW 7818 IN FLIGHT RECEIVED SPOILERONS FAULT STATUS MESSAGE AND INBOARD GROUND SPOILER FAULT STATUS MESSAGE. AFTER HYDRAULIC PUM P 2B REPLACEMENT REF MEL 182321/3 OPS TESTED SPOILER SYS PER AMM 27-60-00 NO DEFECTS NOTED. PERFORMED SYSTEM BITE ON SE CU NR 1 AND NR 2 ALL SYSTEM PASS REF FIM 27-60-00. (S) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 REX2008F00011 1 20080617 A 3230 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR MALFUNCTIONED A REXA O OTHER O OTHER AP APPROACH 1 SO 25 8623A 7623 GEAR DISAGREE ON APPROACH WITH NOSE NOT SHOWING DOWN AND LOCKED, EMERGENCY DECLARED, QRH FOLLOWED WITH UNEVENTFUL LANDIN G. COMPLIED WITH PINNACLE AIRLINES TROUBLESHOOTING PA (PROJECT AUTHORIZATION) AND PERFORMED GEAR SWINGS PER BOMBARDIER AMM 32-30-00 WITH NO DEFECTS NOTED. (S) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 2008UALA03601 1 20080625 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 DENT IN EXTERNAL SKIN AT BS 424, 2 INCHES BELOW STR 19L. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 NM 2008 7 29 HNA2008F00014 1 20080607 A 4990 OIL SYSTEM DHAV DHC8 DHC8102 2809003 NM APU LEAKING A HNAA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 930HA 870500 126 APU BLEED ON, VAPOR VISIBLE IN CABIN. INSPECTED AND FOUND APU HAS AN OIL LEAK, NO VAPOR VISIBLE OFF ENGINE BLEEDS. REM OVED AND REPLACED APU. (K) 2 H 7 2 4T RT A13NM 20080729 NM 2008 7 29 UIE2008F00018 1 20080630 A 7830 STRUCTURE BOEING 747 747243B 1384830 NM THRUST REVERSER DENTED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 540MC 22508 NR 1 ENGINE LT "C" DUCT (REVERSER) EXTERIOR FOUND WITH 1 EACH DENT AT 7 O`CLOCK POSITION. NR 1 REVERSER EXTERIOR SURFAC E DENT REPAIRED IAW ENGINE MANUAL 78-32-01, REPAIR NR 4. (K) 2 L 7 4 4F RT A20WE 20080729 NM 2008 7 29 2008UALA03395 1 20080615 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 542UA 25276 DOOR 4R EMERGENCY LIGHT INOP, EXTERIOR. LAMP INOP. RELAMPED EMERGENCY LIGHT, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 SO 2008 7 29 SIM2008F00004 1 20080712 A 3297 14521495403 WIRE HARNESS EMB 135 EMB135KL 3260302 SO NLG WOW CORRODED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 834AE 145631 CREW REPORTED ON CLIMB OUT THAT THEY RECEIVED LDG AIR/ GROUND FAIL MESSAGE AFTER THEY RETRACTED GEAR. GOT 3-GREEN LIGHT S. LND/AIR GROUND MESSAGE DID NOT GO AWAY WHEN GEAR LEVER WAS RETRACTED. T/R DISAGREE MESSAGE ON EICAS BUT MESSAGE WEN T AWAY WHEN GEAR WAS LOWERED. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. C/A - REMOVED AND REPLACED RT MLG WOW 1 AND 2 PROX SWITCH. FOUND NLG WOW PROX HARNESS CONNECTOR CORRODED. REMOVED AND REP LACED PROX HARNESS REF ERJ AMM 32-63-01. AIRCRAFT RETURNED TO SERVICE. (K) 2 L 7 2 4F RT T00011AT 20080729 NE 2008 7 29 2008UALA03397 2 20080614 A 7311 471111171 OIL COOLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 548UA 25396 RIGHT IDG DRIVE LIGHT CAME ON JUST AFTER T/O. FUEL OIL COOLER FAILURE CAUSING LOW OIL QTY IN IDG. IDG SHUTDOWN. REPLA CED NR 2 ENG FUEL/OIL COOLER AND REPLACED BYPASS VALVE ON COOLER. ALL LEAK CHECKS PERFORMED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 EA 2008 7 29 TRAX200800741 1 20080603 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 290-559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 SEAT RAIL AT RBL 9 FS 290 TO 559 HAS AREAS OF CORROSION. BLENDED CORROSION TO REMOVAL IAW SRM 51-21-06. DEPTH OF BLEND R ANGED FROM 0.001" TO 0.008". 390 AND 406+128 AREAS STILL NEED CORROSION REMOVED. REMOVED CORROSION FROM FS 390 TO 406+1 28. DEPTH RANGED FROM .007 TO .008 WHICH IS WITHIN REPAIRABLE LIMITS IAW SRM 53-21-49. DAMAGE WAS REMOVED IAW 51-21-06 A ND UPON INVESTIGATION FOUND TO BE WITHIN REPAIRBALE LIMITS OF SRM 53-21-49. 4. NEEDS ALODINE. APPLIED ALODINE IAW CRJ 200 SRM 53-21-49. (A) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800753 1 20080604 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 693-977 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 RT CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE FS 693.00 TO FS977.00. REMOVED SEAT RAIL ASSY, INSPECTED AND FOUND CORR OSION UNDER SEAT RAIL. PREPPED, PRIMED AND PAINTED AREA ON FUSELAGE SKIN IAW SRM 53-00-49. REPLACED SEAT RAIL IAW AMM 53 -00-49. BLENDED AREAS ON SEAT RAIL IAW SRM 53-41-49. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 2008UALA03623 1 20080629 A 7931 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT INOPERATIVE A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 652UA 25390 THE L ENG OIL PRESS LIGHT IS NOT ILLUMINATED ON FORWARD 1ST PANEL. 2 L 7 2 4F 4 F RT A1NM E24NE 20080729 EA 2008 7 29 TRAX200800867 1 20080703 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 EMERGENCY LIGHT FWD OF RT OVERWING EMERGENCY EXIT HAS SEVERAL INOP BULBS. REMOVED AND REPLACED RT OVERWING EMERGENCY EX IT FWD FLOOR LEVEL EMERGENCY FLOOD LIGHT BULBS. OPS CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 ASAA0843117 1 20080627 A 5240 AN2532160 COTTER PIN BOEING 737 7374Q8 138447Q NM R1 DOOR MISSING A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 775AS 002020 25108 R1 DOOR WILL NOT CLOSE FOUND LOWER AFT DOOR LATCH BEARING MISSING COTTER PIN AND NUT BACKING OFF. SECURED LOOSE NUT AND INSTALLED COTTER PIN OPS CHECK GOOD REF MM 52 41 00. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843116 1 20080513 A 5340 654656922 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 STRINGER TIE CLIP GOUGED. REPLACED CLIP PER SRM 51 40 02 51 30 01 AND DWG 65 46569. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843118 1 20080511 A 5340 693535214 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 STRINGER TIE CLIP CRACKED. REPLACED CLIP PER SRM 51 40 02. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843119 1 20080507 A 5311 65465262 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 RIGHT FRAME AT PSU RAIL BRACKET CRACKED REPAIR PER EA 5310 02747. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ZZDA2008128 1 20080702 A 3233 59713305001 ACTUATOR BOEING 717 717200 1383700 NM LT MLG FAILED A ZZDA O OTHER J WARNING INDICATION AP APPROACH 1 SO 37 934AT 55070 FELT SMALL THUMP IN FLOOR FOLLOWED BY LEVEL 2 ALERT, "RIGHT HYD QUANTITY LOW." COMPLETED NON-NORMAL CHECK LIST AND EXTE NDED EMERGENCY GEAR EXTENSION LEVER (ALSO STOWED GEAR LEVER AS PER MX). REMOVED AND REPLACED LEFT MLG RETRACT ACTUATOR CYLINDER. 2 L 7 2 4F TR A6WE 20080729 NM 2008 7 29 USAA920081194 1 20080513 A 5320 654534259 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 328-344, LBL 10. REPLACED CABIN FLOOR SUPPOR T, BS 328-344, LBL 10 IAW SRM 51-10-02 AND 51-40-02. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081251 1 20080621 A 5210 143N610018 ANGLE BOEING 757 7572B7 1384964 NM R2 DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 922UW 27303 CLT - RON - MAJOR REPAIR - CORROSION FOUND ON ANGLE IN BOTTOM OF R2 DOOR AT BS 710. REPAIRED CORROSION FOUND ON ANGLE I N BOTTOM OF R2 DOOR AT BS 710 IAW BOEING B757 DRAWING 143N6100. (S) 2 L 7 2 4F RT A2NM 20080729 NM 2008 7 29 USAA920081246 1 20080618 A 2780 4911710 COMPUTER AIRBUS A319 A319132 3930340 NM E&E BAY FAILED A USAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 19 832AW 41222 1361 1643 FLT 04 - PHX - LAS - FX - CREW REPORTED AFTER TAKEOFF RECEIVED AN ACARS MESSAGE THAT THE SLATS WERE LOCKED IN THE UP POS ITION. CREW CONTINUED ON TO LAS. CREW DECLARED AN EMERGENCY ON APPROACH INTO LAS. EMERGENCY EQUIPMENT WAS CALLED OUT. THE CABIN WAS NOT PREPPED. CREW MADE A ZERO SLAT FLAPS 3 LANDING. THE LANDING WAS UNEVENTFUL. THE ACFT TAXIED TO TH E GATE. MX REPLACED THE SLAT AND FLAP CONTROL COMPUTER IN THE NR 1 AND NR 2 POSITIONS. MX PERFORMED A BITE TEST PER AM M 27-81-00-740-002. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080721 SW 2008 7 21 WGE2008F00000 1 20080625 A 2110 2188571 COMPRESSOR ECLIPS EA500 ECLIPSEEA500 3350000 SW A/C PACK FAILED E WGEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 27 162DJ 232 000079 MX LOG PAGE NR 1832 DISCREPANCY 3 "BURNING SMELL COMING FROM A/C CONDENSER COOLING FAN" WO 2349 NR 00001 REMOVED REPLACE D INTEGRAGED TWIN PACK COMPRESSOR PALLET IAW EA500 AMM 21-10-11. SERVICED A/C SYSTEM IAW EA500 AMM 21-00-00. PERFORMED A/C SYSTEM ADJ./TEST IAW EA500 AMM 21-00-00. OPS AND LEAK CHECKED GOOD. (K) 1 L 7 2 4J RT A00002AC 20080721 EA 2008 7 21 A6WA200840416 1 20080512 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 442AW 7778 PAX DOOR TOP STEP FWD LOWER CORNER IS CRACKED. PAX DOOR TOP STEP FWD LOWER CORNER REPAIRED IAW REO 601R-52-11-702 REV A. 2 L 7 2 4F RT A21EA 20080722 NM 2008 7 22 2008UALA03012 1 20080523 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 510UA 24780 EXIT IDENTIFIER SIGNS - VERTICLE EXIT LIGHTS INOP DOOR 2L AND 2R, POSSIBLE BAD INVERTER. CONNECTOR WAS LOOSE RESEATED C ONNECTOR. ALL LIGHTS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080722 NM 2008 7 22 2008UALA03123 1 20080531 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 309UA 23670 LAST 10 FEET OF EMERGENCY EXIT LIGHTS INOP. SUSPECT FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY ROW 17 THRU 21. O P CHECKS GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA03176 1 20080603 A 3510 MXP4023 OXYGEN MASK BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE COCKPIT FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 224UA 30225 OXYGEN MASK PROBLEM. SUSPECT FAULTY MASK BOX ASSEMBLY. REPLACED MASK BOX ASSEMBLY PER MM 35-11-18. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080722 NM 2008 7 22 2008UALA03189 1 20080604 A 3200 UNKNOWN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU UNKNOWN A UALA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 29 910UA 25254 AIRCRAFT PULLS TO LEFT. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA03201 1 20080602 A 2721 TRIM SYSTEM BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE RUDDER FAILED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 668UA 30024 RUDDER TRIM FAILED TO TRIM IN POS 988 (01=L, 02=R) DIRECTION. CREW COMMENTS: RUDDER TRIM WOULD ONLY MOVE LEFT AFTER FI RST MOVING TRIM TO RIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 NM 2008 7 22 2008UALA03204 1 20080603 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 SEAT EEL ON 25R INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 NM 2008 7 22 2008UALA03214 1 20080604 A 3350 BATTERY BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 340UA 24244 TWO EA EMERGENCY STOW BIN LIGHTS INOP. REPLACED BATTERY & POWER SUPPLY FOR M1135. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA03219 1 20080604 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 665UA 29237 BAG CART HIT AIRCRAFT BELLY JUST AFT OF MAIN LANDING GEAR. MAJOR REPAIR ACCOMPLISHED: ROUTED OUT DAMAGED SKIN AT BS 11 71-1175 AND 1197+22-1197+29 BETWEEN STR 36L-38R. FABRICATED & INSTALLED DOUBLERS, TRIPLERS AND FILLERS. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 EA 2008 7 22 A6WA200840366 1 20080428 A 5610 NP13932114 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A A6WA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 449AW 2601 7818 FIRST OFFICERS WINDSHIELD SHATTERED (OUTER PANE) ON CLIMBOUT AT 9000 FT COMPLIED WITH QRH AND LANDED WITHOUT INCIDENT IN RDU. REMOVED AND REPLACED FIRST OFFICER`S WINDSHIELD IAW 56-11-01, OPS CHECK GOOD, LEAK CHECK GOOD. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840403 1 20080513 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FALSE ACTIVATION A A6WA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 31 452AW 7835 UPON ENGINE START GROUND SPOILER DEPLOY ADVISORY MESSAGE. ALL SPOLERS CONFIRMED UP VISUALLY AND ON FLIGHT CONTROL PAGE. INTERROGATED LT AND RT SECU`S FOR FAULTS, NO FAULTS FOUND. CHECKED MDC FOR FAULTS/DIAGNOSTICS, NO FAULTS FOUND GROUND RA N AIRCRAFT, RE CHECKED MDC NO FAULTS FOUND OPS CHECK NORMALLY IAW AMM 27-60-00. (A) 2 L 7 2 4F RT A21EA 20080722 WP 2008 7 22 ABXA080175 1 20080612 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 944AX 47550 COCKPIT EMERGENCY LIGHT IMOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00. (A) 2 L 7 2 4F A6WE 20080722 2008 7 22 SWAA083877 4 20080714 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 215WN 32487 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080722 NM 2008 7 22 SWAA083955 1 20080716 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 9L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080722 NM 2008 7 22 SWAA083961 1 20080716 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 8L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080722 NM 2008 7 22 SWAA083960 1 20080716 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 7L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080716 NE 2008 7 16 HEEA119824 2 20080530 A 7310 AS3209009 O-RING BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE FUEL MANIFOLD LEAKING B HEEA K NONE K FLUID LOSS NR NOT REPORTED 1 EA 17 412UM 33023 AT ABOUT 5 MINUTES FROM LANDING A STRONG FUEL SMELL ENTERED THE CABIN. NO ABNORMAL INDICATIONS. LANDED AT THE TRAUMA C ENTER AND SHUT DOWN. FOUND SMALL PUDDLE OF FUEL ON GROUND. MECHANIC FOUND A LEAKY FUEL MANIFOLD ON NR 1 ENGINE AT THE NR 8 FUEL NOZZLE POSITION ON THE ENGINE. REPLACED O-RINGS ON THE FUEL MANIFOLD TRANSFER TUBE PART 3020030. 1 G 7 2 4U 4 U H4SW E22EA 20080716 EA 2008 7 16 SWIA200819706 1 20080529 A 2420 ADG CNDAIR CL600 CL6002B19 1900309 EA DEPLOYED A SWIA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 NM 07 918SW 7645 ADG DEPLOYED DURING FLIGHT. RESTOWED ADG AS REQUIRED. 2 L 7 2 4F RT A21EA 20080717 NM 2008 7 17 UPS08B52555 1 20080417 A 5311 65B0175223 FRAME BOEING 747 747400 13848AT NM BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:BCF LT BS1180 TENSION TIE FOUND CRACKED AT FRAME MORN THAN 0.200 INCH. LT BS 1180 TENSION TIE FRAME REP LACED PER SRM 53-40-07. 2 L 7 4 4F RT A20WE 20080717 NM 2008 7 17 UPS08M52563 1 20080429 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1961 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C CABIN-STA 1961 CURVE SEAT TRACK CROWN AREA, X=-107.25 FOUND CORROSION AS MARKED. CURVE SEAT TRACK COR ROSION REMOVED PER SRM 51-21-01VII R35. CORRODED SEAT TRACK REMOVED FROM STA 1831-2007 PER SRM 51-31-01 VII R35. CORRO DED SEAT TRACK TRIMMED OFF AT STA 1831-2007 PER SRM 53-70-00 VI FIG R35. HFEC INSP C/O PER DAC NDTSPM 06-10-01.001 R13 ON TRIMMED OUT AREA FOUND NO CRACK EVIDENT. REWORKED SEA TRACK, SPLICE, PLATE INSTALLED PER SRM 51-31-01 VI. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 DU4R2008211 1 20080602 A 5311 FRAME BOEING 737 737448 13844BU NM FUSELAGE DRILLED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 742VA 24773 DOUBLED DRILLED HOLE IN FUSELAGE FRAME AT BS 986L.5 AT WL 208. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 CALA0800531 1 20080603 A 2560 ACREM1A MEGAPHONE BOEING 767 767224 1385170 NM CABIN WEAK A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 68155 30434 MEGAPHONE IN GALLEY G8 VERY WEAK. REPLACED MEGAPHONE IN GALLEY G8, OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 20080717 NE 2008 7 17 HALA0800606 2 20080527 A 7250 BRH10305 TURBINE BLADES BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE LT ENGINE FAILED A HALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 479HA 13301 425 55124 13301 HEARD A LOUD BANG ON TAKEOFF. N1 & N2 SEIZED ON NR 1 ENGINE. NR 1 ENGINE WAS REMOVED AND REPLACED. LPT 3 BLADE EXHIB ITED SIGNS OF FATIGUE IN THE SHANK NECK AND RELEASED BELOW PLATFORM RESULTING IN THE FAILURE OF THE REMAINING LPT3 TURBI NE BLADES. (S) 2 L 7 2 4F 4 F TR A6WE E00061EN 20080717 NM 2008 7 17 ASAA0853044 1 20080612 A 2160 3989083 VALVE BOEING 737 737890 1384527 NM CABIN TEMP FAULTED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 587AS 2474 35684 UNABLE TO ADJUST FWD OR AFT CABIN TEMP USING CONTROL KNOBS. CONT CABIN WORKS NORMAL. POSTIONED TRIM AIR SWITCH TO OFF POSITION ABLE TO CONTROL CABIN TEMPS. TEMP CONTROLLER (ZONE 2): FAULTED THE TRIM AIR MOD VALVE FOR THE FWD PASS CABIN. REMOVED AND REPLACED MOD VALVE PER: M M21 61 21. TEMP CONTROLLER FAULTS CLEARED (CONFIRM FIX). 2 L 7 2 4F RT A16WE 20080717 2008 7 17 ASAA0853040 4 20080607 A 2397 CONNECTOR BOEING 737 737890 1384527 NM COM RADIO PANEL LOOSE A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 587AS 2426 35684 NR 2 COM RADIO SHOWS FAIL IN ACTIVE AND STANDBY WINDOWS HAPPENED JUST AFTER GRD POWER DIED AND SWITCH TO APU. RE SEATED CONNECTOR NR 2 VHF COMM CONTROL PANEL. OPS CHECK GOOD REF MM 23 12 31. VERIFIED NR 2 VHF COMM CONTROL PANEL DISPLAYED FAIL IN LT AND RT WINDOWS. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083335 1 20080618 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 456WN 32463 DURING SCHEDULED MV3 CHECK, FOUND EEPLS LENS MISSING AT ROW 11 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083336 1 20080618 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 456WN 32463 DURING SCHEDULED MV3 CHECK, FOUND EEPLS LENS MISSING AT ROW 2 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 MWE2008F00000 1 20080628 A 3350 B5116 BATTERY PACK BOEING 717 717200 1383700 NM RROYCE BR700 BR700710A110 NE EMERGENCY LIGHTS INOPERATIVE A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 910ME 55174 TWO LIGHT INOPERATIVE ON TAILCONE SLIDE EMERGENCY LIGHT. REPLACED BATTERY PACK ASSEMBLY. (K) 2 L 7 2 4F 4 F TR A6WE E00057EN 20080717 NM 2008 7 17 SWAA083214 1 20080612 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 7L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083103 1 20080607 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 798, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083088 1 20080608 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083087 1 20080608 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 CE 2008 7 17 2008F00017 1 20080612 A 3610 66002023 VALVE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP RT ENGINE MALFUNCTIONED E XUPA O OTHER O OTHER NR NOT REPORTED 1 GL 21 35AX 280 AT FL400 ENROUTE, RAT ABOUT -38 C AND NOT IN ICING CONDITIONS. DURING DESCENT, NOTED ABNORMALLY HIGH N1 AND ITT INDICATI ONS FOR DESCENDING FLT AT IDLE. FOUND COULD ADD POWER, BUT NOT REDUCE IT. ACTIVATED NAC HEAT ON BOTH ENGINES IN AN ATTEM PT TO RESTORE NORMAL OPERATIONS, SUSPECTING ICE MAY HAVE FORMED IN THE PT2/TT2 PROBES. RESULTING IN NO CHANGE TO THE SIT UATION. ELECTED TO RUN ABNORMAL ENGINE OPS CHECKLIST. LT THRUST LEVER RETARDED TO IDLE AND LT FUEL COMPUTER SWITCHED TO THE OFF POSITION. ENGINE DID IN FACT SPOOL DOWN TO ABOUT 35 PERCENT N1, BUT WE ALSO INSTANTANEOUSLY LOST CABIN PRESSUR E. OBSERVED THE CABIN CLIMB/DESCENT GAUGE "PEGGED" ON CLIMB. THEN INITIATED AND EMERGENCY DESCENT AND NOTIFIED ATC OF O 2 L 7 2 4F 4 F A10CE E6WE 20080717 SO 2008 7 17 UG82008F00000 1 20080604 A 3800 SHAFT GULSTM GVSP GVSP 3980101 SO RROYCE BR700 BR700710A220 09500 NE DRAIN VALVE FAILED E UG8A O OTHER O OTHER NR NOT REPORTED 1 GL 23 551KF 273 0248 5148 DUMP HANDLE SLIPS ON SHAFT. THE SHAFT SEEMS TO BE UNDER SIZE. (K) 2 L 7 2 4F 4 F RT A12EA E00061EN 20080717 EU 2008 7 17 M7K2008F00005 1 20080512 A 5300 350A58004523 HINGE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 821MH 195 4134 23319 (REF 0429084134) DURING ROUTINE INSPECTION, HINGE WAS FOUND CRACKED THROUGH TO SCREW MOUNTING BORES TO THE METALS EDGE. THIS IS A VERY COMMON FAILURE FOR THIS PART. SUGGEST PART BE MFG OF MORE DURABLE MATERIAL SUCH AS STAINLESS STEEL. (K ) 1 G 7 2 3U 3 U H9EU E00054EN 20080717 WP 2008 7 17 08FDEA02031 1 20080529 A 5321 AGA3869502 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 AFT PIT FLOOR PANEL 187 HF REQUIRES FAB NEW. FABRICATED NEW FLOOR PANEL 187 HF; POTTED EDGES; COMPLETED CURE AND SANDE D EDGES; INSTALLED INSERTS; FABRICATED TOP SHEET; LAYED UP UNDER VAC BAG; COMPLETED CURE; BACK DRILLED AND COUNTERSUNK HOLES; APPLIED NON-SKID AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005, REV F AND 25-011, REV C. 2 L 7 3 4F RT A22WE 20080717 WP 2008 7 17 08FDEA02068 1 20080530 A 5720 ANB717559 STIFFENER DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 LEFT MLG WHEEL WELL; AFT OUTBD CORNER HORIZONTAL FRAME SUPPORT, INBD ANGLE IS CRACKED AT THE BOTTOM. REMOVED ACCESS PAN ELS IAW DC/MD-10 SRM 51-31-01; VOL II AND ANGLE IAW DC/MD-10 SRM 51-35-01; 51-33-01; VOL II. MATERIAL ID FOR THE ANGLE IS 7075-0, 0.063; PO 609289.3 IAW ASTME 1476. FABRICATED ANGLE IAW AS THE 1476; SRM 51-10-00 AND 51-33-01; VOL II. ALO DINED; PRIMED AND PAINTED IAW SRM 51-21-01; PGS 21-24; 51-21-02; VOL II. INSTALLED IAW SRM 51-33-01; VOL II. INSTALL ED PANELS IAW DC/MD-10 SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 20080717 NE 2008 7 17 ASAA0853106 2 20080627 A 7261 OIL SYSTEM BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE LOW A ASAA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 NM 02 583AS 3740 35681 894763 NR 1 OIL AT 13 ADDED 4QTS OIL TO NR 1 AND 4QTS OIL TO NR 2. 2 L 7 2 4F 4 F RT A16WE E2GL 20080717 WP 2008 7 17 08FDEA02230 1 20080612 A 5710 ARB07431 CAP DOUG DC10 DC1010 3022110 WP BULKHEAD CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 40061 46973 LOWER BULKHEAD CAP LUG IS CRACKED FWD SIDE. REPAIRED AREA IAW SRM 57-20-00 FIG 27 SHEET 2-3-4 VOL I. 2 L 7 3 4F A22WE 20080717 NM 2008 7 17 SWAA083265 1 20080613 A 2560 PH22300L STRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 6 DEF. REMOVED AND REPLACED STRIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 EU 2008 7 17 08FDEA02205 1 20080609 A 5310 A5398111320100 SHEAR WEB AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 RIGHT FLOOR STRINGER SHEAR WEB IS CRACKED JUST AFT OF FRAME 79 AT THE MAIN CARGO DECK FLOOR LEVEL. REMOVED AND REPLACED WITH A NEW WEB P/N A5398111320100; PO 616322.4 IAW SRM 51-40-21; PGS 6 AND 7. RESTORED CIC IAW SRM 51-22-00. 2 L 7 2 4F RT A35EU 20080717 GL 2008 7 17 SWAA083281 2 20080614 A 7397 CONNECTOR BOEING 737 7373H4 1384600 NM CFMINT CFM56 CFM563B1US GL CROSSFEED VALVE CORRODED A SWAA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SW 29 637SW 18623 27710 INFLIGHT SHUTDOWN/DECLARED EMERGENCY/DIVERSION. NR 1 ENGINE FAILED AT FL 350, EGT FLUCTUATED. RESTARTED ENGINE AT FL 2 00. INSPECTED ENGINE FOUND CORRODED CONNECTOR ON CROSSFEED VALVE. REMOVED AND REPLACED VALVE PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 20080717 NM 2008 7 17 08FDEA02208 1 20080609 A 5753 SKIN BOEING 727 727227 1384078 NM ZONE 500 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 490FE 21493 LT OB FORE FLAP WBL 478 ON T/E IS DELAMINATED CUT OUT DELAMINATED AREA 4 1/2 BY 9 INCH ON LT O/B FOREFLAP WBL 478. FABR ICATED FILLER 4 1/2 BY 9 INCH AND DOUBLER 6 INCH BY 12 INCH FROM 0.016" 2024-T3 PO NR 9004174 IAW B727 SRM 57-50-2. BON DED FILLER AND DOUBLER, CLEANED, SEALED AND PRIMED IAW B727 SRM 51-40-20. 2 L 7 3 4F A3WE 20080717 EU 2008 7 17 08FDEA02212 1 20080610 A 5753 A5797010003600 SKIN AIRBUS 310 A310324 3930206 EU ZONE 400 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 815FD 638 LEFT WING INBD FLAP T/E AREA IS DENTED AND DELAMINATED APPROX 18 INCHES FROM THE OUTBD EDGE. REPAIRED THE LEFT INBD FLA P BY REMOVING THE DAMAGED AREA ; FABRICATING; AND BONDING A NEW CORE AND DOUBLERS IAW A310 SRM 57-52-12 AND FEDEX EA 6- 5750-118501 TITLED "WING - LEFT WING FLAP T/E UPPER AND LOWER SKIN". 2 L 7 2 4F RT A35EU 20080717 NM 2008 7 17 SWAA083275 1 20080612 A 3350 101114 LENS BOEING 737 7373A4 1384585 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080717 2008 7 17 SWAA083277 4 20080612 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 08FDEA02220 1 20080611 A 5322 651634994 SHEAR TIE BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 490FE 21493 AFT CARGO COMPARTMENT, SHEAR TIE CORRODED AND FASTENERS PULLING THROUGH AT BS 116 BETWEEN STRINGER 30 AND 29R AFT SIDE. 2 L 7 3 4F A3WE 20080717 EU 2008 7 17 08FDEA02223 1 20080611 A 5347 A5377986220000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 THE CABIN SEAT TRACK HAS CORROSION BETWEEN FRAME 32 AND FRAME 33; LBL 58. REMOVED CORROSION AND FOUND TO BE WITHIN LIMI TS IAW A300-600 SRM 53-10-16; FIG 101. ORIGINAL MATERIAL 0.134. MATERIAL LOSS 0.025. MATERIAL REMAINING IS 0.109. DE PTH GAUGE USED WAS T8492G. ALODINED; PRIMED AND TOPCOATED AREA IAW A300-600 SRM 51-23-10. 2 L 7 2 4F RT A35EU 20080717 EU 2008 7 17 08FDEA02245 1 20080612 A 5753 SKIN AIRBUS 310 A310203 3930313 EU TE FLAP MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RT WING O/B FLAP UPPER MAIN SKIN UNDER RUBSTRIP BETWEEN FLAP TRACK NR 4 TO R IB 7 AND 10 INCH FWD OF REAR SPAR MEASURING 4.7 INCH BY 5.9 INCH. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS RE PAIR AND INSTALLED CORRECT REPAIR ON RT WING O/B FLAP UPPER MAIN SKIN UNDER RUBSTRIP BETWEEN FLAP TRACK NR 4 TO RIB 7 AN D 10 INCH FWD OF REAR SPAR IAW A310-200 SRM 57-53-12 FIG 210. THIS IS AN AIRBUS REPAIR AND IS A RESULT OF AGING AIRCRAF T INSPECTION. 2 L 7 2 4F RT A35EU 20080717 NM 2008 7 17 SWAA083291 1 20080616 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 716SW 27850 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083293 1 20080614 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 719SW 27853 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083280 1 20080614 A 3397 W3142025020 WIRE BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 916WN 36623 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT 5 ABC TO ROW 10 ABC. FOUND LOOSE WIRE AT LIGHT ASSY. SECURED LOOSE WIR E PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083166 1 20080610 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083167 1 20080610 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083569 1 20080626 A 2560 6557463 FITTING BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 245WN 32506 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK FITTING LOOSE. SECURED FITTING PER SRM . 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083543 1 20080626 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083544 1 20080626 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R AND STR 6L. REMOVED AND REPLACED STRINGER CL IP PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 08FDEA02125 1 20080603 A 5100 NONE DOUG MD11 MD11F 3023600 NM IAW WITH SRM NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 LOWER AFT FUSELAGE BELLY AT STA 1711 TO STA 1751 FOUND WITH EXISTING REPAIR. EXISTING SKIN SPLICE REPAIR AT LOWER AFT F USELAGE BELLY STA 1711 TO STA 1751 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-20-00 FIGURE 10 VOLUME I FE DEX EO NR 1-5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG, MD11, REPAIR CATALOG AND TRACKING REQUIREMENTS, HAS BEEN ACCOM PLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 EU 2008 7 18 08FDEA02556 1 20080629 A 5753 SKIN AIRBUS 310 A310203 3930313 EU TE FLAP FAILED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 423FE 281 PREVIOUS REPAIR BONDED REPAIR DOUBLER LOCATED ON LT WING INBD FLAP TRAILING EDGE LOWER SKIN BETWEEN TRACK 1 TO TRACK 2 A ND AT THE AFT EDGE MEASURES 38.3 INCH BY 10.2 INCH WITH A TRIPLER MEASURING 3.3 INCH BY 10.2 INCH ON TOP BETWEEN RIB 4 A ND RIB 5 REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED NEW REPAIR AT LT INBD FLAP TRAILING EDG E BETWEEN TRACK 1 AND TRACK 2 IAW FED EX EA 6-5750-121311 RELEASE DATE 19 JUNE,2008. THIS IS AN AIRBUS REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080718 2008 7 18 2008UALA02998 4 20080526 A 2210 TRANSFORMER HONEYWELL 4051601937 BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AUTOPILOT BURNED A UALA A UNSCHED LANDING W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 378UA 92041899 24653 STRONG ACRID ODOR DETECTED AFTER DEPARTURE, RTFL. *S/D* BAD AUTO PILOT FLIGHT CONTROL PANEL. REPLACED CONTROL PANEL. SHOP FINDINGS: FOUND TRANSFORMER A10T1 PRIMARY BURNED. TRANSISTORS A10Q1/Q2 PARTIALLY SHORTED. REPLACED PARTS. 2 L 7 2 4F 4 F RT A16WE E21EU 20080718 NM 2008 7 18 08FDEA02106 1 20080603 A 5100 NONE DOUG MD11 MD11F 3023600 NM IAW SRM NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 EXISTING REPAIR, RIGHT WING FIXED LEADING EDGE UPPER SURFACE BETWEEN NR 1 AND NR 2 LEADING EDGE SLATS FOUND REPAIR DOUBL ER. EXISTING REPAIR AT RIGHT WING FIXED LEADING EDGE UPPER SURFACE BETWEEN NR 1 AND NR 2 LEADING EDGE SLATS EVALUATED A ND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 24 VOLUME I FEDEX EO NR 1-5100-7-5001 A3 PART 1, TITLE: REPA IR CATALOG - MD11, REPAIR CATALOG AND TRACKING REQUIREMENTS 14 CFR 121.707, HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 08FDEA02107 1 20080603 A 5100 NONE DOUG MD11 MD11F 3023600 NM IAW SRM NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 EXISTING REPAIR, RIGHT WING INBOARD FLAP UPPER SURFACE AT XIFH 225 FOUND REPAIR DOUBLER. EXISTING REPAIR AT RIGHT WING INBOARD FLAP UPPER SURFACE AT XIFH 225 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 38 VOLUME I. FEDEX EO NR 1-5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG - MD11, REPAIR CATALOG AND TRACKING REQUIREMENTS 14 CFR 12 1.707, HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 08FDEA02235 1 20080612 A 5340 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 598FE 48597 MAIN DECK CARGO DOOR SPOOL FITTING NR 1 FOUND 3RD LAYER CRACK INDICATIONS AT ALL FITTING MOUNTING BOLT HOLES. MAIN DECK CARGO DOOR SPOOL FITTING NR 1 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. BUSHING REPAIR CARRIED OUT AS PER SR M 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 2008 7 18 2008UALA03112 4 20080601 A 3445 806002 SWITCH BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 364UA 24533 RTFL DUE TO GROUND MODE INDICATION. FAULTY SENSOR SWITCH AND GROUND SENSOR. REPLACED SENSOR SWITCH M990 AND GROUND SEN SOR S105. 2 L 7 2 4F 4 F RT A16WE E21EU 20080718 EU 2008 7 18 08FDEA02350 1 20080619 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 MDCC SEAT TRACK HAS CORROSION ON THE UPPER SURFACE BETWEEN FRAME 14C AND FRAME 17; LML 99.06 CM. 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 08FDEA02353 1 20080620 A 5414 311N51932 PANEL BOEING 757 75727B 1384921 NM ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 916FD 24137 PYLON NUMBER ONE RIGHT SIDE SKIN CUTOUT AT ACCESS PANEL 433GR FOUND CORROSION, FROM PPS 100 TO PPS 120. EVALUATE AND RE CTIFY. REPLACED PYLON NUMBER ONE SKIN CUTOUT PANEL 433GR IN ACCORDANCE WITH BOEING DRAWING 311N5002 AND SRM 51-10-02 RE V 93. 2 L 7 2 4F RT A2NM 20080718 NM 2008 7 18 08FDEA02239 1 20080612 A 5340 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 598FE 48597 MAIN DECK CARGO DOOR SPOOL FITTING NR 6 FOUND 3RD LAYER CRACK INDICATION AT FITTING MOUNTING BOLT HOLE C. MAIN DECK CAR GO DOOR SPOOL FITTING NR 6 REMOVED AS PER SRM 51-31-01 VOLUME II AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING RE PAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 EU 2008 7 18 08FDEA02256 1 20080613 A 5330 A53610263200 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON THE LEFT SIDE FUSELAGE NOSE SKIN BETWEEN FRAMES 1 TO 4 AND BETWEEN STRINGERS 28 TO 30 LT, AT AND ABOVE THE SKIN LAP SEAM, THE REPAIR DOUBLER MEASURES 12.2 INCHES BY 5.9 INCHES. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT REPAIR ON LEFT SIDE FUSELAGE NOSE SKIN BETWEEN FRAMES 1 TO 4 AND BETWEEN STRINGERS 28 TO 30 LT, AT AND ABOVE THE SKIN LAP SEAM, IAW FED EX EA 6-5310-121278. THIS IS AN AIRBUS RE PAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080718 WP 2008 7 18 08FDEA02257 1 20080613 A 5520 S391804473 WEDGE DOUG MD10 MD1010F 3022112 WP ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 RIGHT STABILIZER; OUTBD ELEVATOR, INBD SIDE T/E AREA IS DELAMINATED. REMOVED AND REPLACED WEDGE IAW DC/MD-10 SRM 51-35- 01; VOL II. 2 L 7 3 4F RT A22WE 20080718 EU 2008 7 18 2008UALA03345 1 20080612 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN SHORTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 455UA 1105 F/A SMELLED BURNING AT FWD DOOR 1L AND PAX LIGHTS FLASHING ON AND OFF. FWD ENTRY LIGHT BULB SHORTING. RELAMPED FWD ENT RY LIGHT. LIGHT SOCKETS OKAY. NO ARCING NOTED. NO ABNORMAL SMELLS NOTED UPON ARRIVAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080718 EU 2008 7 18 08FDEA02149 1 20080604 A 5710 A5797149920090 RUB STRIP AIRBUS 310 A310203 3930313 EU ZONE 600 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 283 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RT WING OUTBD FLAP MAIN SKIN UNDER RUB STRIP BETWEEN RIB NR 2 AND RIB NR 3 , 4.4 IN FWD OF REAR SPAR MEASURING 13 IN BY 11.8 IN REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTA LLED CORRECT OUTER SKIN REPAIR ON RT WING OUTBD FLAP UPPER SKIN BETWEEN RIB NR 2 AND RIB NR 3 IAW A310-200 SRM 57-53-10, FIG 210. THIS IS AN AIRBUS REPAIR AND IS A RESULT OF AGING AIRCRAFT INSPECTION. 2 L 7 2 4F RT A35EU 20080718 2008 7 18 2008UALA03436 4 20080617 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN CRACKED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 496UA 1845 RIGHT OVERWING EVACUATION SLIDE IS CRACKED AT AFT SIDE. COMPOSITE CRACK. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080718 EU 2008 7 18 2008UALA03439 2 20080618 A 7200 ENGINE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 MAKING METAL A UALA C ABORTED TAKEOFF A FLAME/FIRE TO TAKEOFF 1 WP 29 338UA 24242 725210 ENGINE 2 COMPRESSOR STALL ON TAKEOFF 95 PERCENT N1 TARGET, SERIES OF LOUD BANGS, ASSOCIATED YAW, EGT THRU 725 DEGS. RET ARDED THROTTLES. THE ACFT BEHIND REPORTED FLAMES FROM ENGINE EXHAUST. FOUND METAL FOUND IN TAILPIPE. CHANGED ENGINES. 2 L 7 2 4F 4 F RT A16WE E21EU 20080718 NM 2008 7 18 2008UALA03440 1 20080617 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 AFT PIT FRAME AT FS 1360 STR 26L HAS 1EA DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080718 NM 2008 7 18 2008UALA03441 1 20080617 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 FWD CARGO PIT STA 620 STR 24L FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080718 NM 2008 7 18 2008UALA03446 1 20080617 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 672UA 30027 EEL LIGHT AT SEAT 32A INOP. FOUND LOOSE CONNECTION. SECURED CONNECTION. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080718 NE 2008 7 18 2008UALA03456 2 20080616 A 7321 EEC BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE LT ENGINE MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 229UA 30557 222139 ENGINE EEC C1 L LEFT ENGINE CONTROL IS IN A TIME LIMITED DISPATCH CONDITION. ENGINE CONTROL SYSTEM IS OPERATING WITH RE DUCED REDUNDANCY. STATUS MSG-7361081 INACTV ER INTER, MAINT MESSAGE 73-61081 PRESENT T-3 THERMOCOUPLE PROBE. MSG NOT A CTIVE, INTERMITTENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080718 EU 2008 7 18 2008UALA03458 1 20080615 A 3411 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE UNKNOWN A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 429UA 539 ALL 3 PITOT PROBES INOP AFTER TAKEOFF. ALL RESET ATTEMPTS NO HELP, LGCIU'S, FWC'S, SDAC'S, AND CYCLE OF THE GEAR NO HEL P. SUSPECT AIR GROUND MODE PROBLEM. REPLACED LGCIU 2, ALL SYSTEMS WERE CHECKED AND FOUND TO FUNCTIONING NORMALLY. NO REPEATS AFTER THIS INCIDENT. 2 L 7 2 4F 4 F RT A28NM E40NE 20080722 NM 2008 7 22 SWAA083675 1 20080702 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080722 NM 2008 7 22 SWAA083676 1 20080702 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 485WN 32473 EEPLS INOP AT ROW 2 ABC. R&R LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080722 NM 2008 7 22 SWAA083677 1 20080702 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11R. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080722 NM 2008 7 22 SWAA083680 1 20080702 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 745SW 29491 DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. R&R LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080722 EA 2008 7 22 A6WA200840464 1 20080530 A 5420 ANGLE CNDAIR CL600 CL6002B19 1900309 EA RT PYLON CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 ANGLE CRACKED ON RT PYLON ACCESS PANEL 422 BT. ANGLE REPLACED IAW SRM 51-42-06. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840466 1 20080502 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 438AW 7748 BOTH CLIPS CRACKED AT FS 280 AND LBL 9 ON CROSSBEAM. BOTH CLIPS REPLACED AT FS 280 AND LBL 9 ON CROSSBEAM IAW CRJ 200 S RM 51-42-06 AND SRM 51-42-21. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840469 1 20080505 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 438AW 7748 CLIP CRACKED AT FS 484 RBL 27 UNDER FLOOR. CLIP AT FS 484, RBL 27 UNDER FLOOR REPLACED IAW SRM 51-42-06 AND SRM 51-42-2 1. (A) 2 L 7 2 4F RT A21EA 20080721 NM 2008 7 21 2008UALA02869 1 20080519 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 655UA 25393 EMERGENCY LIGHTS IN FLOOR LOOSE RIGHT SIDE ACROSS FROM BUSINESS GALLEY. FOUND DAMAGED LIGHT ASSEMBLY. REPLACED LIGHT A SSEMBLY. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080721 NM 2008 7 21 SWAA083656 1 20080702 A 5315 6545834 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 2. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083689 1 20080704 A 3350 101114 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 299WN 36614 FWD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 2008UALA02955 1 20080521 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 649UA 25286 REF SMC001 ON EEL STRIP BROKEN, NEW STRIP IS IN PLACE AND WILL REQUIRE SPLICING AND RE-ASSEMBLY OF EEL STRIP CABLE PROTE CTIVE COVERS AND CARPET. FOUND LIGHT ASSEMBLY BROKEN. SPLICED IN SECTION OF EEL LIGHT ASSEMBLY, OP CHECKED GOOD. AC O K FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 NM 2008 7 22 2008UALA02879 1 20080517 A 3350 20131A BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN MISSING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 656UA 25394 EMERGENCY POWER SUPPLY MISSING (M1209) FOR RT FWD WING EXIT DOOR (VERTICALLY MOUNTED). SUSPECT BATTERY PACK IMPROPERLY INSTALLED. REPLACED BATTERY PACK PER MM 33-51-07. OPS CHECKS GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 NM 2008 7 22 2008UALA02965 1 20080522 A 2611 824PTY SMOKE DETECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT LAVATORY FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 376UA 24641 AFT LAV SMOKE DETECTOR INTERMITTENTLY GOES OFF FOR APPROX FIFTEEN SECONDS THEN STOPS. SUSPECT FAULTY SMOKE DETECTOR. R EPLACED AFT LAVATORY SMOKE DETECTOR. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA03175 1 20080603 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 AFT PIT FRAME TOP CHORD BENT OVER STA 1440, STR 27L. MAJOR REPAIR ACCOMPLISHED: CUTOUT DAMAGE. INSTALLED FRAME REPAIR . 2 L 7 2 4F 4 F RT A2NM E17NE 20080722 WP 2008 7 22 ABXA080165 1 20080520 A 5315 99234847 FLOORBEAM DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944TW 47550 FLOOR BEAM CRACKED AT STA 180, LEFT BUTT LINE 2 VISIBLE ON AFT SIDE OF FLOOR BEAM. REPAIRED FLOOR BEAM IAR DC9 SSRM K051 95. (A) 2 L 7 2 4F A6WE 20080722 NM 2008 7 22 SWAA083878 1 20080714 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 297WN 32542 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080722 EA 2008 7 22 A6WA200840474 1 20080507 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 438AW 7748 FWD BRACKET OF CARGO STEP PLATE AT FS 575.00, WL 73.50. LBL 40 IS CRACKED. FWD BRACKET OF CARGO STEP PLATE AT FS 575, WL 73.5, LBL 40 REPLACED IAW SRM 51-42-21. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840475 1 20080507 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 438AW 7748 CARGO FLOOR LANDING PLATE AT FS 605, WL 73.5, LBL 39 IS CRACKED. CARGO FLOOR LANDING PLATE AT FS 605, WL 73.5, LBL 39 R EPAIRED IAW REO 601R-53-61-433. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840477 1 20080507 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 438AW 7748 CARGO BAY FLOOR SILL AT FS 574.00, WL 73.5, LBL 39 IS CRACKED. CARGO BAY FLOOR SILL AT FS 574, WL 73.5, LBL 39 REPAIRED IAW REO 601R-53-61-1741. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840423 1 20080515 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 437AW 7744 FLAPS FAILED AFTER TAKEOFF AT 12 DEGREES, PERFORMED QRH, RETURNED TO CMH. OPEN (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840424 1 20080515 A 3310 HOLDER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT SPARKS A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 438AW 7748 FIRST OFFICERS CHART HOLDER SPARKED WHEN MOVED-POPPED CIRCUIT BREAKER ON CBP2 UG. SUFFICIENT LIGHTING EXISTS FOR DUTIES. PLACARDED AND PLACED ON MEL. OPEN (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840380 1 20080503 A 2450 BUSS CNDAIR CL600 CL6002B19 1900309 EA COCKPIT SHORTED A A6WA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 31 449AW 7818 RECIEVED MASTER CAUTIOIN AC SERVICE BUSS, RAN QRH AND CONTINUED IN ARI AND ON GROUND, MESSAGE IS INTERMITTENT, POSSIBLE ELECTRICAL ODOR IN COCKPIT, PULLED CIRCUIT BREAKER PANEL 2, S2. R&R ACFT SERVICE BUS SENSE RELAY K5XD REF WDM 24-50-00. OPS CHECK GOOD IAW 24-51-20. 2 L 7 2 4F RT A21EA 20080722 WP 2008 7 22 ABXR080174 1 20080508 A 5340 995823869 SHEAR TIE DOUG DC9 DC915F 3022037 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 783TW 47010 SHEAR TIE CRACKED BELOW LONGERON 14 LEFT AT FRAME STA 801 REPAIRED SHEAR TIE IAW DWG K050159. (A) 2 L 7 2 4F A6WE 20080722 NM 2008 7 22 ABXA080159 1 20080508 A 5330 141T83208 SKIN BOEING 767 767281 1385109 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 783AX 23016 DEEP PITTING CORROSION ON LT DOOR FRAME FORWARD LOWER CORNER INTERIOR SKIN AT FS 300 AND STRINGER 19 LEFT. BLENDED OUT AREAS, WITHIN LIMITS IAW B767-200 SRM 53-10-01 & 53-00-15. 1 EA PITTED AREA REPAIRED IAW B767 REA B653-573-69. (A) 2 L 7 2 4F RT A1NM 20080722 WP 2008 7 22 ABXA080164 1 20080520 A 5315 99234847 FLOORBEAM DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 STIFFENER AND FLOORBEAM CRACKED AT STA 180, RBL 26. REPAIRED FLOORBEAM, REPLACED STIFFENER IAW DC9 SRM 51-30-2 AND DWG K05011. (A) 2 L 7 2 4F A6WE 20080722 WP 2008 7 22 ABXA080167 1 20080520 A 5320 991050313 CUSP WEB DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 CUSP WEB CRACKED PAST STOP DRILL FS 958, RBL 54. INSTALLED -3 DOUBLE IAW DC9 SRM 51-31-2 AND DWG K07259. (A) 2 L 7 2 4F A6WE 20080722 WP 2008 7 22 ABXA080154 1 20080524 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 975AX 47512 COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00. (A) 2 L 7 2 4F A6WE 20080722 NM 2008 7 22 ABXA080156 1 20080610 A 5220 DOOR BOEING 767 767281 1385109 NM EMERGENCY EXIT UNSECURE A ABXA O OTHER J WARNING INDICATION DE DESCENT 1 GL 23 783AX 23016 STA ILN, LEFT EMERGENCY EICAS MESSAGE DISPLAYED. EICAS MESSAGE EXTINGUISHED DESCENDING THROUGH 10,000/PSI DIFF APPROXIM ATELY 1.5 FOUND LEFT EMERGENCY WING DOOR NOT SECURLY LATCHED. INSPECTED PROX SWITCH 5,192 AND SECURED DOOR. OPS CHECKE D GOOD IAW B767 AMM 52-70-00 AND WDM 52-71-11. 2 L 7 2 4F RT A1NM 20080722 WP 2008 7 22 ABXA080177 1 20080617 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 978AX 47628 EMERGENCY EXIT PLANE EXIT LIGHTS FOUND INOPERATIVE ON PRE-FLIGHT. REPLACED EMERGENCY POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00. (A) 2 L 7 2 4F A6WE 20080722 EA 2008 7 22 A6WA200840509 1 20080612 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 444ZW 7788 INTERCOSTAL AT FS 484 LBL 36, WL 72 IS CRACKED. NTERCOSTAL AT FS 484.0 LBL 36.0 REPAIRED IAW REO 601R-53-41-059. (A) 2 L 7 2 4F RT A21EA 20080723 EA 2008 7 23 TRAX200800649 1 20080516 A 2750 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OUT OF RIG A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 844AS 7317 FLAPS FAILED IN FLIGHT AT 20. BOTH FLAPS INDICATED 20 ON THE SYNOPTIC PAGE, BOTH FLAPS OUTLINED IN YELLOW ON SYNOPTIC PA GE. FLAPS WERE LOWERED AT AIRSPEED OF 180KNOTS. COMPLIED WITH QRH, NO UNUSUAL CONTROL FEEL---[EMERGENCY DECLARED] REMOVE D & REPLACED PDU AND RIGGED LT BPSU. OPS CHECK GOOD REMOVED AND REPLACED PDU IAW AMM 27-52-01, OPS CHECK GOOD 2 L 7 2 4F RT A21EA 20080724 NM 2008 7 24 SWAA083706 1 20080704 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 344, STR 9R. REMOVED AND REPLACED STR CLIP PER S RM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083707 1 20080704 A 5311 6546569 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 986.5, STR 2L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080724 2008 7 24 2008UALA02943 4 20080521 A 2564 D31517121 HOSE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE RAFT BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 837UA 1474 AIRBUS RAFT DOOR BROKEN HOSE. UNKNOWN DAMAGE. REPLACED HOSE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 EU 2008 7 24 2008UALA02997 1 20080526 A 3222 SEAL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG DAMAGED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 441UA 751 LANDING GEAR FAILED TO RETRACT. RTFL. FOUND NOSE STRUT SEALS DAMAGED. REPLACED NOSE STRUT SEALS, SERVICED STRUT. NO REPEATS. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 EU 2008 7 24 2008UALA03007 1 20080526 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN UNSECURE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 417UA 483 NR 3 SERVICE CABIN EMER LIGHT CHECK FAILED. INT LOADS EMER R AND EXT LOADS AFT L. REMOVED AFT LT SLIDE AND RESET CONNE CTOR AND RE-INSTALLED AND TEST NOW OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03046 1 20080527 A 5320 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 CABIN RT BETWEEN STA 1400 AND 1420 AT STR 17R CORROSION. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED AND REPLACED WEB IA W SRM 53-60-13. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03070 1 20080529 A 3213 BUSHING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT MLG CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 555UA 26647 AFT LT MLG AXLE HAS CORROSION ON AXLE SLEEVES. BUSHING FAILURE ON LT AFT TRUCK. TRUCK REMOVED AND BUSHINGS REPLACED, R EINSTALLED AND ALL TESTS WERE GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 2008 7 24 2008UALA03241 4 20080607 A 3442 066500080408 RADAR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WEATHER SYSTEM FAILED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 307UA 23668 WX FAILED IN FLIGHT. RTFL. REPLACED WEATHER RADAR TRANSCEIVER. SHOP FOUND ANTENNA AZ FAULT IN F.M.. INSTALLED S.B RTA -4B-34-113 ON ANT. DRIVE MODULE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 2008 7 24 2008UALA03242 4 20080607 A 3497 CABLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU WEATHER RADAR BROKEN A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 937UA 26668 WEATHER RADAR FAILED. RTFL. FOUND BROKEN RIBBON CABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03248 1 20080607 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE LT ENGINE INOPERATIVE A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 225UA 30554 A/C REPORTED LEFT GENERATOR DRIVE INOP. APU IN USE. HOWEVER APU CNTRL STATUS LIGHT HAS ILLUMINATED. SUSPECT FAULTY BE ARING. REPLACED IDG OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080724 NM 2008 7 24 2008UALA03249 1 20080606 A 5340 ATTACH FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 FWD ENTRY DOOR CUTOUT FWD SIDE INTERCOSTAL WEB OUTBOARD ATTACH CLIP CRACKED ON AFT SIDE AT BS 302 AND STRINGER S-10L. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 2008 7 24 2008UALA03263 4 20080606 A 2350 MICROPHONE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU OXYGEN MASK INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 F/O'S OXYGEN MASK MIC INOP. REPLACED FIRST OFFICERS OXYGEN MASK OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03268 1 20080606 A 5210 BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOOR LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 852UA 1671 CREW REPORT: DOOR 2R DOOR ASSIST BOTTLE PRESSURE LOW. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03270 1 20080609 A 5320 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 810UA 843 DOOR 2R SILL PAN NEEDS TO BE REPLACED DUE TO CORROSION. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03273 1 20080608 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 810UA 843 FLOORBEAMS 145 AND 140 REMOVED FROM FR 64 TO 69 FOR CORROSION. 2 L 7 2 4F 4 F RT A28NM E40NE 20080718 EU 2008 7 18 2008UALA03470 1 20080618 A 7932 D7931158000060 TRANSMITTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 422UA 503 NR 2 ENG OIL QUANTITY LOW INDICATION, RTFL. INCORRECT INDICATION ISSUE. REPLACED NR 2 ENGINE OIL QUANTITY TRANSMITTER, ACCOMPLISHED ENGINE RUN. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080718 EU 2008 7 18 2008UALA03473 1 20080619 A 3350 D92 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 419UA 487 CIDS BIT BATTERY FWD L. EPSU FAILURE. REPLACED EPSU. 2 L 7 2 4F 4 F RT A28NM E40NE 20080717 NM 2008 7 17 BB08103 1 20080530 A 3350 BPS73 POWER SUPPLY BOEING 757 7572B7 1384964 NM CABIN NO TEST A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 941UW 27806 CLT - THE EMERGENCY LIGHT POWER SUPPLY OVER L3 DOOR WILL NOT TEST. MAINTENANCE REPLACED THE POWER SUPPLY UNIT FOR THE L 3 DOOR. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 20080717 EU 2008 7 17 USAA920081161 1 20080516 A 5540 D5537131800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 602AW 565 SAL - MAJOR REPAIR - C1 CHECK - RUDDER HINGE FITTING NR 2 HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 1926 / RIB 4. REPLACED RUDDER HINGE FITTING NR 2, VERTICAL STABILIZER STATION 1926 / RIB 4 IAW A320 AMM 55-36-41. 2 L 7 2 4F RT A28NM 20080717 SO 2008 7 17 FDKA200806216 1 20080602 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM RON JFK. GALLEY OVERHEAD EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED LIGHT. 2 L 7 2 4T RT T00011AT 20080717 NM 2008 7 17 ASAA0853037 1 20080607 A 2435 28B5457 STARTER GEN BOEING 737 737890 1384527 NM APU FAULTY A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 557AS P5681 35176 BLUE MAINT LIGHT APU ILLUMINATED ON TAXI IN JUST AFTER STARTED. INSPECTED FOUND APU START GENERATOR FAULT. REMOVED AND REPLACED STARTER GENERATOR PER: MM 49 41 21 400 801 PP 1 13. PART NR VERIFIED. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083330 1 20080618 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 SW 2008 7 17 RMX2008F00001 1 20080617 A 5302 206032409001 FITTING ECLIPS EA500 ECLIPSEEA500 3350000 SW ALLSN 250C 250C30P 03013 GL TAILBOOM CRACKED E RMXA O OTHER O OTHER NR NOT REPORTED 1 SW 05 164MW 000122 DURING ROUTINE INSPECTIO TECHNICIAN DISCOVERED UPPER LEFT TAILBOOM ATTACH FITTING CRACKED. (K) 1 L 7 2 4J 3 U RT A00002AC E1GL 20080717 NM 2008 7 17 SWAA083080 1 20080608 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083096 1 20080608 A 5743 6582764 FITTING BOEING 737 7373H4 1384600 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED MV2 CHECK, FOUND LT MLG BEAM CORRODED AT INBOARD FITTING. REMOVED AND REPLACED FITTING PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083091 1 20080608 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 1. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083090 1 20080608 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 SO 2008 7 17 UG82008F00001 1 20080604 A 3800 SHAFT GULSTM GVSP GVSPG550 3980203 SO RROYCE BR700 BR700710A220 09500 NE DRAIN VALVE FAILED E UG8A O OTHER O OTHER NR NOT REPORTED 1 GL 23 940DC 787 5128 DUMP HANDLE SLIPS ON SHAFT. THE SHAFT SEEMS TO BE UNDERSIZE. (K) 2 L 7 2 4F 4 F RT A12EA E00061EN 20080717 WP 2008 7 17 08FDEA02091 1 20080602 A 5753 ARC074415 ANGLE DOUG MD10 MD1010F 3022112 WP TE FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 LEFT WING LOWER TRAILING EDGE OUTBD FLAP; AT THE OUTBD SIDE OF THE HINGE FAIRING (XORS 500) ANGLE IS FRETTING FROM CONT ACT WITH THE INBD SIDE OF PANEL NR 551 BB. CHECKED ANGLE AND FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-00-01; VOL I ; FIG 1- A. ORIGINAL THICKNESS 0.080. MATERIAL REMAINING 0.042. MATERIAL REMOVED 0.039. UT GAUGE USED E2579A IAW DC /MD-10 SRM 51-31-01; VOL II. REMOVED ARC0744-15 ANGLE IAW DC/MD-10 SRM 51-31-01; VOL II. FABRICATED A NEW ANGLE IAW D AC DWG ARC0744, REV P. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01; VOL II. PART MARKED IAW FEDX GMM 7-0-1000. INST ALLED NEW ANGLE IAW DC/MD-10 SRM 51-31-01; VOL II. INSTALLED PANEL 536 BL IAW DC/MD-10 SRM 51-31-01; 2 L 7 3 4F RT A22WE 20080717 WP 2008 7 17 08FDEA02028 1 20080529 A 5321 AGA38763 FLOOR PANEL DOUG MD10 MD1010F 3022112 WP ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 AFT PIT FLOOR PANEL 187 EF REQUIRES FAB NEW. FABRICATED NEW FLOOR PANEL 187 EF; POTTED EDGES; COMPLETED CURE AND SANDED EDGES; INSTALLED INSERTS; FABRICATED TOP SHEET; LAYED UP UNDER VAC BAG; COMPLETED CURE; BACK DRILLED AND COUNTERSUNK HOLES; APPLIED NON-SKID AND PART MARKED PANEL IAW FEDEX DWG SRX 25-005, REV F AND 25-011, REV C. 2 L 7 3 4F RT A22WE 20080724 NM 2008 7 24 2008UALA03275 1 20080608 A 2150 UNKNOWN BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE A/C PACK FAILED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 206UA 30212 PACK MODE R RIGHT PACK AIR CYCLE MACHINE HAS FAILED, OR RIGHT ECONOMY COOLING VALVE FAILED OPEN, OR BOTH RIGHT CONDENSOR INLET TEMP SENSORS FAILED. RIGHT PACK IS OPERATING IN A NON-NORMAL MODE (HEAT EXCHANGER ONLY COOLING MODE). ADVISORY CREW COMMENTS: PACK MODE R. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080724 NM 2008 7 24 2008UALA03283 1 20080607 A 2133 OUTFLOW VALVE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN PRESSURE INOPERATIVE A UALA D RETURN TO BLOCK W INADEQUATE Q C IN INSP/MAINT 1 WP 29 672UA 30027 AIRCRAFT RETURN TO GATE, DUE OUTFLOW VLV INOP IN AUTO & MANUAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20080724 NM 2008 7 24 2008UALA03295 1 20080609 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 AFT CARGO FRAME DENTED STA 1420, STR 27L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED AREA OF FRAME INBOARD FLANGE. FO RMED AND INSTALLED A REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 EU 2008 7 24 2008UALA03054 1 20080527 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 447UA 836 FLOORBEAM ITEM 250 HAS CORROSION. ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED BEAM, BEAM ON WORK TABLE. CONT OF AMIS IT EM 0912010: PICKED UP HOLES FOR BARREL NUT FITTINGS AND SPLICE ANGLES ON NEW BEAM. CONT OF AMIS ITEM 0912017: CONTINU ED WORKING BEAM PART ON WORK TABLE. CONT OF AMIS ITEM 0912024: INSTALLED BEAM 250- NEEDS RIVETS FOR SHEAR PLATE INSTAL LED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 EU 2008 7 24 2008UALA03057 1 20080527 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 447UA 836 FLOORBEAM ITEM 200 HAS CORROSION. UPDATE ACCOMPLISHED MAJOR REPAIR AT DEN. REF SRM 53-41-14 FIG 1 ITEM 200. BEAM REMO VED CONT OF AMIS ITEM 0912013. REPLACED BEAM, REF SRM 53-41-14. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 EU 2008 7 24 2008UALA03059 1 20080527 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 447UA 836 FLOORBEAM ITEM 205 HAS CORROSION. ACCOMPLISHED MAJOR REPAIR AT DEN. BEAM REMOVED. REPLACED BEAM, REF SRM 53-41-14. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03124 1 20080601 A 2421 729825G IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE FAILED A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 548UA 25396 RIGHT GENERATOR TRIPPED DURING CRUISE TWICE. NO SHOP DATA EXISTS FOR REPAIR. REPLACED IDG. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03144 1 20080530 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 L2 DOOR UPPER HINGE ARM CUTOUT HAS A CRACK. ACCOMPLISHED MAJOR REPAIR AT GSO. REPAIRED PER MM 52-11-87 AND SRM 51-40-0 2. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 UPS08M52458 1 20080429 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C CABIN STA 1961 CURVE SEAT TRACK CROWN AREA, X=107.25 FOUND CORROSION AS MARKED. CURVE SEAT TRACK CORR OSION REMOVED PER SRM 51-21-01 VII R35. ORIGINAL THICKNESS REMOVED AND FOUND EXCEEDED LIMIT PER SRM 53-70-00 VI R35. C ORRODED SEAT TRACK TRIMMED OFF FR STA 1831-2007 PER SRM 53-70-00 FIG 7 VI R35. SEAT TRACK SPLICE & SPLICE PLATE FAB PER SRM 53-70-00 VI FIG R35. SEAT TRACK, SEAT TRACK SPLICE & SPLICE PLATE INSTALLED PER SRM 51-31-01 VII R35. 2 L 7 3 4F RT A22WE 20080724 NM 2008 7 24 UPS08M52459 1 20080429 A 5720 DOUBLER DOUG MD11 MD11 3023602 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C RT WING FIXED L/E COMPT AT STA XORS 538 APPROX FOUND UPPER DOUBLER CRACKED AS MARKED. DAMAGED AREA AT RT WING FIXED L/E COMPT STA 538 UPPER DOUBLER AREA TRIMMED OFF AS PER SRM 57-10-00 VI FIG 27 R40. NEW REPAIR DOUBLER, REPAIR FILLER & 03EA REPAIR ANGLES FAB PER SRM57-10-00 VI FIG 27 R40. NEW FAB REPAIR DOUBLER, REPAIR FILLER & 3EA REPAI R ANGLES INSTALLED AT RT WING FIXED L/E COMPT STA XORS 538 INTERIOR AREA PER SRM 57-10-00 VI FIG 27 REV 40. 2 L 7 3 4F RT A22WE 20080724 NM 2008 7 24 UPS08M52460 1 20080526 A 5315 AFA00395N FLOORBEAM DOUG MD11 MD11 3023602 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C CTR CARGO COMPT - UPON REMOVING OF PHENOLIC SPACER AT STATION 5-73,X-33 FOUND FLOORBEAM CRACKED. CRAC K BEAM REMOVED AND NEW BEAM P/N AFA0039-5N INSTALLED AS PER SRM 51-31-01 VOL II REV 35. 2 L 7 3 4F RT A22WE 20080724 NM 2008 7 24 2008UALA03186 1 20080603 A 5210 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 R2 DOOR UPPER HINGE CUTOUT CRACKED. MAJOR REPAIR ACCOMPLISHED: INSTALLED FRAME REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03187 1 20080603 A 2611 22179374 FAN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SMOKE DETECTOR FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 775UA 26947 DET FAN 2 CARGO AFT CARGO COMPARTMENT SMOKE DETECTOR FAN NR 2 FAILURE. FOUND AFT SMOKE DETECTOR FAN FAULTY. REPLACED A FT CARGO SMOKE DETECTOR NR 2 FAN ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080724 NM 2008 7 24 2008UALA03197 1 20080604 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 545UA 25323 SLIDE ARMED LIGHT INOP 4R. FOUND AFT END OF GIRT BAR NOT IN THE FLOOR CLEET WHEN IN THE ARMED POSITION. POSITIONED GIR T BAR AND CYCLED SEVERAL TIMES AND LIGHT OP CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03217 1 20080604 A 5270 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 525UA 24978 SLIDE ARMED INDICATOR LIGHT DOOR 3R BULB NOT LIT AFTER ARMING. DOOR SENSOR/SLIDER TARGET DIRTY. CLEANED DOOR SLIDER TA RGET SENSOR, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03251 1 20080606 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 FWD ENTRY DOOR CUTOUT AFT SIDE AT BS 360 STRINGER 16L END PIECE CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED WITH NEW STRINGER CLIP. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03253 1 20080606 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 INTERCOSTAL WEB CRACKED AT STRINGER S-16L BETWEEN BS 294.5 AND 303.9 FWD OF 1L ENTRY DOOR. MAJOR REPAIR ACCOMPLISHED: REPLACED INTERCOSTAL WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03258 1 20080606 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 UPPER LT FUSELAGE STA 948 S-14 IS DENTED. MAJOR REPAIR ACCOMPLISHED: REMOVED DENT DAMAGE. VERIFIED DAMAGE RMVLD WITH HFEC. INSTALLED TRIPLER/DOUBLER/FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 2008 7 24 2008UALA03265 4 20080607 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 546UA 25367 SLIDE PACK DOOR 3L HAS LANYARD PROTRUDING. RE-INSTALLED LANYARD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03305 1 20080609 A 2931 MODULE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT MALFUNCTIONED A UALA O OTHER W N INADEQUATE Q C FALSE WARNING NR NOT REPORTED 1 WP 29 549UA 25397 RIGHT HYD ENGINE LOW PRESSURE LIGHT FLICKERS. OVERHEAD LIGHT MASTER MODULE SHORTING. REPLACED OVERHEAD LIGHT MASTER MO DULE, REPLACED ENGINE LOW PRESSURE SWITCH AS PRECAUTIONARY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03310 1 20080611 A 5315 FLOORBEAM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 181UA 25278 UPPER DECK FLOORBEAM UPPER CHORD AT BS 860 & 880, LBL 7 1.5, TOTAL OF 3 FASTENER HOLES MISDRILLED. PLUGGED FASTENER HOL ES REF SRM 51-40-02. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080724 NM 2008 7 24 2008UALA03322 1 20080611 A 5753 6546481149 CARRIAGE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU T/E FLAP CORRODED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 914UA 25381 LEFT OUTBOARD FLAP SPINDLE DUE TO CORROSION IN THE EXPOSED PORTION OF SPINDLE. REMOVED LT OTBD FLAP OUTBD SPINDLE. REPL ACED LT OTBD MIDFLAP CARRIAGE 355 LT. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03325 1 20080611 A 5753 WEDGE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU MID FLAP DELAMINATED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 329UA 24149 MID FLAP T/E WEDGE IS DELAMINATED 47.5 INCHES OUTBOARD FROM INBOARD EDGE AND IS DENTED ON LOWER SURFACE DUE TO BIRD STRI KE. FOUND DAMAGE TO BE OUT OF LIMITS. REPLACED LT I-B MID FLAP WEDGE REF MM 27-51-11 PG 406, ALL GAPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03337 1 20080612 A 2840 0092 PUMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUEL BOOST FAULTY A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION IN INSP/MAINT 1 WP 29 775UA 26947 THE 'FUEL PUMP LT AFT' EICAS MSG DISPLAYED AND LOW PRESS LIGHT ON THE SW. FOUND NO POWER AT PUMP CONNECTOR ON PIN 4 (PH ASE B1) SUSPECT RELAY K28123 INOP. REPLACED RELAY K28123 NO HELP. FOUND C PHASE SHORTED TO GROUND, SUSPECT WIRING OR PUM P. T-S BY REMOVING K28123 & CK DK28123 PIN B1 TO PUMP(DM28102) PIN 4 FOR OPEN OR SHORT. POSS BAD CONN DM28102. CHECKED F OR 115 VAC AT DM2 8102 PINS 2,4,6. FOUND NO DISCREPANCIES, SUSPECT L AFT FUEL BOOST PUMP. REPLACED LT MAIN TANK FUEL BOO ST PUMP HOUSING. AFTER LEAK AND OPERATIONAL CHECK, NO LEAKS NOTED, OPS GOOD, NO EICAS MESSAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080724 NM 2008 7 24 2008UALA03226 1 20080605 A 5230 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 AFT CARGO DOOR EXTERNAL SKIN HAS 9 DENTS AT SCATTERED LOCATIONS. MAJOR REPAIR ACCOMPLISHED: REMOVED OLD DOUBLER. FABR ICATED AND INSTALLED NEW REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03228 1 20080605 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 652UA 25390 DEEP GOUGE ON FUSE SKIN AT STA 256.25 TO 276 AND STR 31R, JUST AFT OF CREW O2 DISCHARGE. MAJOR REPAIR ACCOMPLISHED: RE MOV'D DAMAGED SKIN, INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20080724 NM 2008 7 24 SWAA083805 1 20080713 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 480, STR 15L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083917 1 20080715 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 13R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083919 1 20080715 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, STR 13R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083881 1 20080714 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 13R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083883 1 20080714 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727B, STR 13L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083882 1 20080714 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, STR 13R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083942 1 20080715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083944 1 20080715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080722 NM 2008 7 22 SWAA083674 1 20080702 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083708 1 20080702 A 5312 6545409 PRESSURE PANEL BOEING 737 7373H4 1384600 NM LT MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED HC1 CHECK, FOUND LT MLG WHEEL WELL CEILING CRACKED AT BS 664, LBL 31. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 2008UALA02901 1 20080519 A 2730 6449014 SERVO AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ELEVATOR FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 805UA 783 ELEV SERVO FAULT DISPLAYED ON UPPER ECAM SCREEN. - F -CTL ELEV SERVO FAILURE. REPLACED 3EC1 LT INBOARD SERVO CONTROL, ALL OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 2008 7 24 2008UALA02966 4 20080522 A 2565 D31516113 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 425UA 508 DOOR 1L SLIDE OUT OF PACK. UNKNOWN. REMOVED SLIDE AND REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03271 1 20080609 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 810UA 843 FLOORBEAM 175 NEEDS REPLACEMENT FROM FR68 TO FR70. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03282 1 20080609 A 7921 WARNING MESSAGE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 643UA 25093 PER CREW, R ENG A-O VALVE MESSAGE AFTER START. 2 L 7 2 4F 4 F RT A1NM E24NE 20080724 NM 2008 7 24 2008UALA02977 1 20080523 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EEL INOP SEAT 55C. RELAMPED EMERGENCY LIGHT, OP CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080724 NM 2008 7 24 2008UALA03250 1 20080606 A 5340 ATTACH FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 INTERCOSTAL WEB AFT LWR ATTACH CLIP CRACKED AT INBOARD CORNER OF STRINGER S-11L BETWEEN BS 351.2 AND 360 AT 1L ENTRY DOO R. MAJOR REPAIR ACCOMPLISHED: REMOVED & REPLACED CLIP (P/N 69-48985U6). 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 EU 2008 7 24 2008UALA03313 1 20080610 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 465UA 1341 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. CREW COMMENTS: SYSTEM READS 0. SAMC TEXT: PRESSURE IS LES S THAN 10 PSI. PURGE SYSTEM FIRST AND THEN SERVICE TO FULL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 SWAA083857 1 20080713 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND LT KEEL BEAM WEB CORRODED AT BS 540, RBL 6.5. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080730 EA 2008 7 30 REX2008F00010 1 20080616 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA SPOILERS FALSE ACTIVATION A REXA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SO 25 8932C 7932 FLIGHT SPOILER AND SPOILERON FAIL MESSAGE IN FLIGHT, QRH FOLLOWED, EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. SYSTEM INSPECTED AND RESET PER FAULT ISOLATION MANUAL (FIM). (S) 2 L 7 2 4F RT A21EA 20080717 SO 2008 7 17 SWIA200819808 1 20080618 A 2121 AE1711AA0 FAN EMB 120 EMB120ER 3260203 SO LT PACK SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 07 290SW 120317 FLT 5672 - LEFT PACK SMOKES ON DESCENT AND SETS OFF LAV SMOKE DETECTOR. REPLACED LEFT PACK GROUND COOLING FAN. OPS CHE CK GOOD, P/N AE1711AA0, S/N OFF 744. 2 L 7 2 4T RT A31SO 20080717 NM 2008 7 17 ASAA0843033 1 20080514 A 5753 SKIN BOEING 737 737490 1384715 NM RT WING TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 799AS 29270 RIGHT OUTBOARD AFT FLAP FORE FLAP OUTBOARD LEADING EDGE CHAFED PREPARED DAMAGED AREA BY BLENDING. FABRICATED REPAIR DOU BLER AND INSTALLED IAW B737 400 SRM 57 53 01 FIG 201 REPAIR 1. 2 L 7 2 4F RT A16WE 20080717 WP 2008 7 17 08FDEA02086 1 20080602 A 5730 ARC01555 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 LEFT WING INBD FLAP HINGE PANEL 541 BR HAS A WORN AREA. REPAIRED BLENDED AREA BY REMOVING FINISH ON INNER SKIN AREA OF LEFT WING INBD FLAP HINGE PANEL 541 BR; FABBING A DOUBLER; HOT BONDING THE DOUBLER IN PLACE AND REFINISHING IAW DC/MD- 10 SRM 51-71-00; VOL II AND DAC DWG ARC0166. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 08FDEA02099 1 20080602 A 5100 NONE DOUG MD11 MD11F 3023600 NM NO DAMAGE NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 EXISTING DOUBLER REPAIR AT FORWARD CARGO DOOR FORWARD CUT-OUT APPROX STRINGER 38 TO 42. EXISTING DOUBLER REPAIR AT FORW ARD CARGO DOOR FORWARD CUT-OUT APPROX. STRINGER 38 TO 42 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-50-0 0 FIGURE 17 VOLUME I. FEDEX EON NR 1-5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG - MD11 - REPAIR CATALOG AND TRACKING REQUIREMENTS, HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GEM 6-2-100. 2 L 7 3 4F RT A22WE 20080717 NM 2008 7 17 SWAA083267 1 20080617 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 08FDEA02210 1 20080610 A 5313 6518444 STRINGER BOEING 727 727227 1384078 NM BS 520-540 S28L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 FWD LOWER CARGO PIT, CORROSION ON STRINGER L28 BETWEEN FS 520 AND FS 540 REMOVED CORROSION ON STRINGER L28 FWD LOWER CAR GO PIT FS 520-540. FOUND CORROSION AREA TO BE OUT OF LIMITS WITH A .020 MATERIAL LOSS FROM ORIGINAL "T" = .063. REMO VED DAMAGE SECTION OF STRINGER, FABRICATED, TREATED, PRIMED, PAINTED AND INSTALLED STRINGER SPLICE REPAIR REF SRM 53-10- 3 PG 1B DETAIL I. CORROSION ON SKIN REPAIRED ON N/R 00635, 00636, 00637. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080717 NM 2008 7 17 SWAA083316 1 20080617 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083276 1 20080612 A 5330 6552988 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 976, STR 22L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083292 1 20080616 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 716SW 27850 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083282 1 20080615 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 757LV 29850 BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 16 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083165 1 20080610 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER 7L CRACKED AT BS 1013. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083156 1 20080610 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080717 NM 2008 7 17 SWAA083568 1 20080627 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 225WN 34333 EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 08FDEA02105 1 20080603 A 5100 NONE DOUG MD11 MD11F 3023600 NM IAW SRM NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 EXISTING REPAIR, RIGHT WING NR 3 LEADING EDGE SLAT LOWER SURFACE FOUND REPAIR DOUBLER. EXISTING REPAIR AT RIGHT WING NR 3 LEADING EDGE SLAT LOWER SURFACE EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 57-10-00 FIGURE 10 VOLUME I FE DEX EO NR 1-5100-7-5001 A3 PART 1, TITLE: REPAIR CATALOG - MD11, REPAIR CATALOG AND TRACKING REQUIREMENTS 14 CFR 121.707 , HAS BEEN ACCOMPLISHED. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 08FDEA02124 1 20080603 A 5100 NONE DOUG MD11 MD11F 3023600 NM IAW SRM NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 590FE 48505 MAIN DECK, EXISTING TRANSVERSE FRAME REPAIR AT STA 1681 LONGERON 12L. EXISTING TRANSVERSE FRAME REPAIR AT STA 1681 LONG ERON 12L EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. FEDEX EO NR 1-5100-7-5001 A 3 PART 1, TITLE: REPAIR CATALOG, MD11. REPAIR CATALOG AND TRACKING REQUIREMENTS, HAS BEEN ACCOMPLISHED. REPAIR CLASSIF IED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 EU 2008 7 18 2008UALA03343 1 20080613 A 2160 5650079 SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE A/C BAY FAILED A UALA A UNSCHED LANDING W M INADEQUATE Q C OVER TEMP CL CLIMB 1 WP 29 413UA 470 PRESSURIZATION PROBLEM, RTFL. PACK 2 OVERHEATED AND WOULD NOT RESET FULLY, AND PACK 1 WAS ON DEFFERAL. RTFL, UNABLE TO PRESSURIZE AC. REPLACED ACM DISCHARGE TEMP SENSOR NR 2 PACK, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080718 EU 2008 7 18 08FDEA02254 1 20080613 A 5753 SKIN AIRBUS 310 A310203 3930313 EU ZONE 600 MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 443FE 01024 283 PREVIOUS EXTERNAL BONDED REPAIR DOUBLER LOCATED ON RIGHT WING I/B FLAP TRAILING EDGE LOWER SKIN BETWEEN TRACK 1 TO RIB 1 0 AND AT THE AFT EDGE MEASURING 59 INCH BY 11.6 INCH. REPAIR NOT IAW EA6-5750-62865. REMOVED PREVIOUS REPAIR AND INST ALLED CORRECT REPAIR AT RT WING I/B FLAP TRAILING EDGE LOWER SKIN BETWEEN TRACK 1 TO RIB 10 AT THE AFT EDGE IAW FED EX E A6-5750-121270. 2 L 7 2 4F RT A35EU 20080718 EU 2008 7 18 08FDEA02148 1 20080604 A 5230 A5237204320000 SKIN AIRBUS 310 A310324 3930206 EU CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 815FD 638 FWD CARGO PIT DOOR LOWER INTERNAL SKIN PLATE IS CORRODED IN NUMEROUS PLACES. REMOVED AND REPLACED THE FWD CARGO DOOR IN TERNAL SKIN PLATE IAW A310 SRM 51-40-21. MATERIAL ID IAW A310 SRM 52-31-00; PG 4; SHEET 2; ITEM 20, P/N A52372043200. THIS SDR WAS GENERATED TO CORRECT THE VERBIAGE IN THE DISCREPANCY AND IN THE CORRECTIVE ACTION OF SDR TRACKING NR 08-18 05 AND NON-ROUTINE NR N00434. THE VERBIAGE "EXTERNAL SKIN PLATE" WAS CORRECTED TO READ "INTERNAL SKIN PLATE". 2 L 7 2 4F RT A35EU 20080718 NM 2008 7 18 2008UALA03482 1 20080619 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 RAMP REPORTED DENT AFT OF DOOR 2 LEFT. FOUND DENT TO BE IN SKIN LAP, LOCATED BETWEEN STATIONS 986 AND 1006. REMOVED & REPLACED DAMAGED STRINGER SECTION JUST AFT OF DOOR 2L BETWEEN STR'S 986 AND 1006. NEW STRINGER INSTALLED CLOSING SKIN LA P. WORKING FASTENER INSTALLATION. COMPLETED INSTALLATION OF ALL FASTENERS IN REPAIR AREA. 2 L 7 2 4F 4 F RT A16WE E21EU 20080718 2008 7 18 SWAA083571 4 20080629 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 08FDEA02123 1 20080603 A 5100 NONE DOUG MD11 MD11F 3023600 NM IAW SRM NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 590FE 48505 MAIN DECK, EXISTING TRANSVERSE FRAME REPAIR AT STA 1641 LONGERON 12L. EXISTING REPAIR AT MAIN DECK TRANSVERSE FRAME STA 1641 LONGERON 12L EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED AS PER SRM 53-30-00 FIGURE 1 VOLUME I. FEDEX EO NR 1-510 0-7-5001 A3 PART 1, TITLE: REPAIR CATALOG, MD11, REPAIR CATALOG AND TRACKING REQUIREMENTS, HAS BEEN ACCOMPLISHED. REPAI R CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080718 NM 2008 7 18 SWAA083611 1 20080629 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 749.5, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080718 NM 2008 7 18 SWAA083586 1 20080629 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080718 EU 2008 7 18 M7K2008F00039 1 20080612 A 3340 M128834802 RELAY UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE LANDING LIGHT FAILED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 806MH 3788 3833 23220 DURING ROUTINE OPERATIONS THE LANDING LIGHT WOULD INTERMITTENTLY NOT STOP WORKING WITH THE SELECTOR SWITCH IN THE OFF PO SITION. CYCLING THE SWITCH SEVERAL TIME RAPIDLY WOULD USUALLY CORRECT THE PROBLEM. AN OBVIOUS STICKING RELAY. A NEW REL AY WAS INSTALLED AND NO FURTHER DEFECT WAS NOTED. THIS IS A REAR FAILURE FOR THIS PART. ONE FAILURE HAS BEEN NOTED IN E VERY 20,000 FLIGHT HOURS FOR OUR FLEET. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 EU 2008 7 18 M7K2008F00028 1 20080512 A 6710 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE FAILED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 807MH 258 3912 23130 A FAULT CODE WAS GENERATED ON SHUTDOWN INDICATING A DEFECT OF COLLECTIVE POTENTIOMETER. A NEW PART WAS INSTALLED, NO FU RTHER FAULT WAS DETECTED. THIS IS RECURRING FAILURE FOR THIS PART WHICH HAS EFFECTED DISPATCH RELIABILITY FOR THIS MODE L HELICOPTER. SUGGEST AN ALTERATION OF FAULT SENSING SOFTWARE TO REDUCE FAULT SENSITIVITY TO PERHAPS A SIGNAL LOSS OF 0 .5 SECOND RATHER THAN 1/20TH OF A SECOND. AN OPTIC RATHER THAN A RESISTANCE BASED SENSOR SHOULD BE CONSIDERED AS CONTAC T POINT IS DAMAGED BY AC VIBRATION WHEN AC POWER SETTINGS ARE SET FOR CRUISE FLIGHT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080718 NM 2008 7 18 SWAA083501 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 EA 2008 7 18 A6WA200840407 1 20080506 A 5340 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 442AW 7778 NR 2 HYDRAULIC SUPPORT MANIFOLD BRACKET CRACKED. HYDRAULIC SUPPORT BRACKET REPAIRED IAW REO 601R-53-62-031 REV A. 2 L 7 2 4F RT A21EA 20080718 NE 2008 7 18 AWH2008F00000 2 20080625 A 7230 BLADES CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE COMPRESSOR DAMAGED E AWHA A UNSCHED LANDING E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 17 984FE 208B0115 PCE19155 AT ABOUT 2800 FT, THE PILOT REPORTED A LOUD BANG FROM ENGINE COMPARTMENT AND SUBSEQUENT ENGINE POWER LOSS. AN EMERGENCY WAS DECLARED, PILOT LANDED SAFELY. POST INCIDENT INSP REVEALED DAMAGE TO COMPRESSOR TURBINE BLADES, COMPRESSOR TURBINE V ANE RING., POWER TURBINE BLADES AND POWER TURBINE GUIDE VANE. THE ENGINE WAS REMOVED FROM THE AC AND SENT FOR TEAR DOWN ANALYSIS. (K) 1 H 7 1 3T 3 T A37CE E4EA 20080718 EA 2008 7 18 UH02008F00000 1 20080226 A 5302 269A332511 SUPPORT BRACKET SCWZER 269 269D 8059501 EA TAILBOOM CRACKED E UH0A K NONE O OTHER IN INSP/MAINT 1 SW 03 411HU 1557 0040 UPON INSP OF TAIL ROTOR DAMPER ASSY, CRACK WAS FOUND IN SUPPORT BRACKET ASSY. (PN 269A332511) STOPPED DRILLED CRACK AND REPAIRED WITH A DOUBLER USING 2024T3 .025 FOR REINFORCEMENT PRO SEALED AND RIVETED IN PLACE. (K) 1 G 7 1 3U 0 4H12 20080718 NE 2008 7 18 MWR2008F00000 2 20080513 A 8530 399359 CYLINDER SCWZER G164 G164A 3952704 EA PWA R1340 R1340AN1 52016 NE ENGINE CRACKED P MWRG A UNSCHED LANDING R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 EA 17 48399 1573 P328717 MADE AN EMERGENCY LANDING FOLLOWING AN IN-FLIGHT LOSS OF ENG PWR. LANDED IN A FIELD APPROX .7500 MILE FROM APPROACH END OF AIRPORT. POST INCIDENT INSP REVEALED THAT NR 8 ENG CYLINDER HAD FAILED. CYLINDER CRACKED AT UPPER OIL DRAIN FITTING ON EXHAUST ROCKER HSG, EXTENDING TO LOWER OIL DRAIN FITTING. ENG MAINT RECORDS NOTED THAT ENGINE WAS OVERHAULED IN MARC H OF 2004. ENG HAD ACCUMULATED APPROX 8,115 HOURS TT AND 357 HOURS SINCE O/H. AD 99-11-02 WAS COMPLIED WITH BY FLUORESC ENT PENTRANT INSP. LAST REPETITIVE VISUAL INSP REQUIRED BY AD 99-11-02 WAS ACCOMPLISHED AT ANNUAL INSP ON FEBRUARY 7, 2 008, APPROX22 HOURS AGO. (K) 1 Q 7 1 3R 3 R 1A16 5E2 20080721 NM 2008 7 21 UPS08M52429 1 20080407 A 5713 STRINGER DOUG MD11 MD11 3023602 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C LEFT WING FUEL TANK LOWER NR 40 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 6.5 IN CH. LEFT WING NR 40 STRINGER END SPLICE REMOVED. ATTACH CLIP & FASTENERS REMOVED. SLOT OUT CRACK AREA C/O & HFEC INSP C/O ON REWK AREA & FOUND NO CRACK EVIDENT. REPAIR ARROWHEAD FITTING AND NEW CLIP FAB WITH FPI C/O, FOUND NO CRACK EVID ENT. NEW ARROWHEAD FITTING & CLIP INSTALLED. SEALANT APPLIED. FUEL LEAK CHECK SATIS. 2 L 7 3 4F RT A22WE 20080721 NM 2008 7 21 SWAA083787 1 20080708 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083723 1 20080705 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED BRDG CHECK, FOUND FWD LAV AFT WALL EXIT LIGHT BULBS INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 20080721 EA 2008 7 21 A6WA200840352 1 20080419 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 280 DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 13 443AW 7781 DENT EXIST ON FLIGHT COMPARTMENT BULKHEAD FS 280 RBL 9 WL 93.0 FLIGHT COMPARTMENT BULKHEAD REPAIRED IAW REO 601R-53-11- 1376. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840377 1 20080430 A 3340 LENS CNDAIR CL600 CL6002B19 1900309 EA LT WING ERODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 ERROSION OF THE LT WING TIP POSITION LIGHT LENS. REPLACED LT WINGTIP POSITION LIGHT LENS IAW AMM 57-30-39-400-801 SUPP NR 07-009. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840386 1 20080501 A 5320 SEPARATOR CNDAIR CL600 CL6002B19 1900309 EA ACCESS PANEL CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 SEPARATOR CRACK ON ACCESS PANEL 422DB. NEW SEPARATOR INSTALL ON ACCESS PANEL 422DB IAW CRJ200 SRM 51-42-06. (A) 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840374 1 20080429 A 5340 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 529 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 HYD SUPPORT BRACKET CRACK IN RT MLG BAY AT FS 529 AND BTWN RBL 18 TO RBL 27. REPLACED HYD SUPPORT BRACKET IN RT MLG BAY AT FS 529 RBL 18 TO RBL 27 REPLACED IAW SRM 51-42-06 AND 51-23-00. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840381 1 20080505 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 ANGLE CRACK ON ACCESS PANEL 422 BT. CRACKED ANGLE REPLACED ON ACCESS PANEL 422BT IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 20080721 EU 2008 7 21 08FDEA02523 1 20080627 A 5321 B5327046200400 FLOOR PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOE PANEL 231 GG IS CRUSHED & HAD MULTIPLE PUNCTURES & WORN AREAS. FABBED A NEW PANEL; POTTE EDGES; CURED; SANDED; POTTED INSERTS; APPLIED NON- SKID & PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080721 NM 2008 7 21 08FDEA02839 1 20080712 A 5713 65185702 STRINGER BOEING 727 727200 138407E NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 RT WING, STR 10, CRACKED AT W.S. 686.5, ITEM IS AD DRIVEN, IF CRACKS EXCEED LIMITS IN SECTION II, FIG 12, CONTACT STRUCT URES ENGINEERING FOR REPAIR INSTRUCTIONS PER WORK CARD E7-5710-7-4322. STOP DRILLED CRACK. NDT TO VERIFY TERMINATION O F CRACK AT STOP DRILL. LOCATED HOLES IN REPAIR ANGLES AND INSTALLED. REF E.O. 7-5710-7-4322 / FIGURE 18. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080721 NM 2008 7 21 08FDEA02852 1 20080714 A 5730 ARB2889501 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 597FE 48596 LEFT HAND WING NR 14 SLAT TRACK LOWER CUT OUT FOUND CRACKED. SKIN REPAIRED AS PER SRM 57-10-00, FIG 21 VOL.I. REPAIR C LASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080721 EU 2008 7 21 08FDEA02948 1 20080717 A 5347 A53832211204 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 686FE 804 MAIN DECK LT SIDE SEAT TRACK NR 2 AT FRAME 52 HAS 1 ELONGATED SCALLOP REMOVED DAMAGED SECTION AND INSTALLED REPAIR ON NR 2 LT SEAT TRACK AT FRAMES 52-54 IAW SRM 53-10-16 FIG 203 SHEET 5. 2 L 7 2 4F RT A35EU 20080721 EU 2008 7 21 08FDEA02951 1 20080717 A 5320 A53970875201 COVER AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CHAFING MARKS ON CROSS SHEET C56-57A, RT NEAR EMERGENCY EXIT. REPAIR PERFORMED BY SMOOTH REWORK , NDT FOR CRACK FREE CONDITION AND FLAP PEENING IAW. RAS /EFW/9000061/2008 ISS.A , APPROVED BY EA 6-5316-123049. 2 L 7 2 4F RT A35EU 20080721 NM 2008 7 21 SWAA083790 1 20080709 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED MV2 CHECK, FOUND AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083799 1 20080709 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800769 1 20080607 A 5210 MOTOR CNDAIR CL600 CL6002B19 1900309 EA DOOR ASSIST INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 844AS 7317 ASD WILL NOT OPEN. (PASSENGER DOOR POWER ASSIST SYSTEM). REMOVED AND REPLACED CABIN DOOR ASSIST MOTOR IAW AMM 52-11-00 . DEFER CLEARED, PLACARD REMOVED. (S) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAABB08109 1 20080618 A 3232 274647 DOOR ACTUATOR BOEING 757 757225 1384959 NM NLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 917UW 74831 2 22193 CLT FLT 1121 EN ROUTE CLT TO MCO. AFTER TAKEOFF, THE NOSE LANDING DOORS DID NOT INDICATE CLOSED. THE QRH PROCEDURES DI D NOT HAVE ANY EFFECT. THE FLIGHT RETURNED TO FIELD CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NLG DOOR ACTUATOR. OPERATIONAL, LEAK AND GEAR SWING CHECKS OK. (S) 2 L 7 2 4F RT A2NM 20080730 EU 2008 7 30 COEA0805911 1 20080611 A 5330 S53371208200 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 911FX 33406 045 FOUND DURING HEAVY CHECK AT COE. MAJOR REPAIR: LEVEL 2 CORROSION: SRAS: FOUND CORROSION ON EXTERNAL SURFACE OF FUSEL AGE SKIN UNDER THE CARGO DOOR THRESHOLD PROTECTION PLATE. PROTECTION PLATE INSTALLED BY M7 AEROSPACE STC ST01189WI. BL ENDED-OUT AREAS OF CORROSION ON EXTERNAL FUSELAGE SKIN PER SRAS DO/TS-2668...4699, DO/TS-2668-08-10359, JUSTIFICATION DO CUMENTS REF: NOTE DO/TS-2717/08. SKIN THICKNESS LEFT AS-IS AFTER BLENDING. (S) 2 H 7 2 4T RT A53EU 20080730 EU 2008 7 30 COEA0808911 1 20080528 A 5315 S53372411210 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 911FX 33406 045 FOUND DURING HEAVY CHECK AT COE. MAJOR REPAIR: LEVEL 2 CORROSION: FLOORBEAM 13, BL 0 HAS 5 EACH FLOORBOARD SCREW HOLE S EXFOLIATING ON TOP AND BOTTOM OF FLOORBEAM UPPER FLANGES. FLOORBEAM 13 REPLACED WITH AN ADDED SPLICE TO THE BEAM AT B L 0. (S) 2 H 7 2 4T RT A53EU 20080730 EU 2008 7 30 MAL2008F00005 1 20080607 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 288-339 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 STA 288 TO STA 339 SEAT TRACK CORRODED, BL 0 AND BL 18.3. REPAIRED SEAT TRACK IAW EOS53060. SUPPORT FRAME CORRODED AT STA 294 RT SIDE. REPLACED SUPPORT FRAME P/N 7253710-243 IAW SRM 51-40-21. SUPPORT FRAME CORRODED AT STA 294 ON LT SIDE . REPLACED SUPPORT FRAME P/N 7253711-245 IAW SRM 51-40-21. (S) 2 L 7 2 4T RT A52EU 20080730 EU 2008 7 30 MAL2008F00006 1 20080509 A 3350 HOUSING SAAB SF340 340B 7860101 EU EMERGENCY LIGHT DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 423XJ 340B423 DURING OPS CHECK OF EMERGENCY LIGHTING, NOTED EMERGENCY LIGHT ABOVE SEAT 8A INOP; WIRE WAS BROKEN OFF HOUSING. REPLACED EMERGENCY LIGHT HOUSING AT SEAT 8A WITH SERVICEABLE IAW SAAB AMM 33-50. (S) 2 L 7 2 4T RT A52EU 20080730 EU 2008 7 30 COEA0810911 1 20080528 A 5753 RIB AEROSP ATR42 ATR42300 8680920 EU TE FLAP CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 911FX 045 FOUND DURING HEAVY CHECK AT COE. LEVEL 2 CORROSION ON RT WING OUTBOARD FLAP, FLAP RIB 18 FWD PICK UP IS EXFOLIATING INS IDE OF FLAP. REPLACED OUTBOARD FLAP ASSEMBLY. (S) 2 H 7 2 4T RT A53EU 20080730 NM 2008 7 30 USAA920081313 1 20080702 A 5743 654610821 BEAM BOEING 737 7374B7 1384702 NM ZONE 600 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 457UW 25021 CTO - FORWARD PRESSURE BULKHEAD - MAJOR REPAIR - WALKING BEAM ON RT MAIN LANDING GEAR RETRACT ACTUATOR HAS HEAVY CORROSI ON PITTING UNDER TEFLON RUB BLOCKS, AND ROLLED BEARING IS VERY LOOSE. REPLACED WALKING BEAM ON RT MAIN LANDING GEAR RET RACT ACTUATOR IAW BOEING AMM 32-32-11. (S) 2 L 7 2 4F RT A16WE 20080730 2008 7 30 USAA920081299 4 20080702 A 2320 80555154501 PRINTER AIRBUS 320 A320232 3930326 EU COCKPIT DEFECTIVE A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 663AW 25105 12949 1419 FLT 189 FLL - PHX - DIVERSION - CREW REPORTED SMOKE FROM THE ACARS PRINTER AND WIRE UNDER PRINTER APPEARED BURNED. THE CREW PULLED THE CIRCUIT BREAKER AND PLANNED TO CONTINUE ON TO PHX, HOWEVER THE SMELL IN THE COCKPIT WOULD NOT DISSIPATE. AS A PRECAUTION, AN EMERGENCY WAS DECLARED AND THE ACFT DIVERTED TO MSY. THE PRINTER WAS DISCONNECTED AND THE ACFT RE TURNED TO PHX WHERE MAINTENANCE REMOVED AND REPLACED THE PRINTER. MAINTENANCE ALSO REPORTED SLIGHT DISCOLORATION UNDER PRINTER PAPER REFILL COVER BUT NO INDICATION OF FIRE. (S) 2 L 7 2 4F RT A28NM 20080730 EU 2008 7 30 USAA920081300 1 20080701 A 2560 P2070001214 FLASHLIGHT AIRBUS A319 A319112 3930323 EU CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 703UW 0904 DCA- FLT1880 - LT AFT F/A`S FLASHLIGHT WAS NOT CHARGING. MX REPLACED THE F/A`S FLASHLIGHT. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080730 NM 2008 7 30 2008UALA03594 1 20080627 A 2120 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN/COCKPIT ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 810UA 843 FUMES SMELLED IN CABIN & COCKPIT. RTFL. OIL IN RECIRC PATH ACCOMPLISH PACK BURN OUTS AND CHANGED FILTERS (RECIR) CHECK OF GENERATOR FEEDER PINS ALSO REPLACED FILTERS RECIRC. CHECKED CABIN INTERCOM. RUN CREW REPORTED THE ODOR CAME FROM V ENTS UNTILL PACK BURN OUT WAS COMPLETE. ACCOMPLISHED HIGH POWER RUNS 4 SEPARATE TIMES. FIRST TIME RAN BOTH ENGINES TO TOGA, THE ODOR WAS NOT SMOKE BUT AN ODOR OF HOT OIL THROUGH PACKS. NO VISIBLE SIGN OF SMOKE IN CABIN BUT SMELL THROUGHO UT ENTIRE CABIN. SET ENGINES TO IDLE FOR 5 MINUTES 74045 TO CLEAR CABIN FUMES. ENGINES WERE RUN AGAIN TO TOGA ONE AT A TIME. NO ODOR PRESENT. RAN ONLY NR 2 ENG TO TOGA & SWITHCHED BETWEEN NR 2 PACK AND NR 1 PACK TO ISOLATE. DID THE SAM 2 L 7 2 4F 4 F RT A28NM E40NE 20080730 NM 2008 7 30 2008UALA03603 1 20080626 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROWS 8 - 13 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 551UA 25399 EMERGENCY EXIT LIGHT ROW 8-13 INOP. EEL STRIP DAMAGED. REPLACED EEL STRIP AT ROWS 12 AND 13, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080730 NM 2008 7 30 SWAA084062 1 20080721 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 727 S21R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727, STR 21R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 USAA920081301 1 20080701 A 2560 P2070001214 FLASHLIGHT BOEING 737 7373B7 1384580 NM MAIN CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 504AU 23379 CLT - FLT 923 - FWD FLT ATTENDANT LOWER FLASHLIGHT INOP. MX REPLACED FWD F/A FLASHLIGHT. OPERATIONAL TEST WAS GOOD. ( S) 2 L 7 2 4F RT A16WE 20080730 EA 2008 7 30 VNAA0804012 1 20080414 A 3250 STEERING SYS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NLG MALFUNCTIONED A VNAA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 GL 05 246PS 7920 CREW REPORTED A LOSS OF DIRECTIONAL CONTROL ON TAKEOFF. THE ACFT PULLED LEFT AND WAS UNCONTROLLABLE WITH THE RUDDER. C REW ELECTED TO ABORT THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NOSE LANDING GEAR AND FOUND NO DEFECTS. MAINTENANCE ALSO CHECKED THE RIGGING AND FOUND TO BE WITHIN LIMITS AT THIS TIME IN ACCORANCE WIT H THE ACFT MAINTENANCE MANUAL. MAINTENANCE AND THE CREW COMPLIED WITH A HIGH SPEED TAXI CHECK AND RESULTS WERE SATISFAC TORY. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080730 NE 2008 7 30 Y2PA080015 2 20080604 A 7200 ENGINE AMD FALC20 FALCOND 2720304 EU GE CF700 CF700* 30010 NE NR 2 FLAMED OUT A Y2PA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 23 823AA 228 CREW REPORTED, DIVERTED AROUND WEATHER AT FL350 WITH ENGINE ANTI-ICE ON. WHEN ACFT CLEARED WEATHER STILL AT FL360 CRUIS ING M .68 TEMP ON RAT -25, TURNED NR2 ENG ANTI-ICE OFF AND NR 2 ENG FLAMED OUT. ACFT BEGAN DESCENT TO FL220, WHEN IN RE LIGHT ENVELOPE TRIED TO RELIGHT ENG. ENG DID NOT RELIGHT, INFORMED ATC - DIVERT TO SDF AND DECLARED AN EMERGENCY. LAND ED AT SDF UNEVENTFULLY AND CONTACTED USA JET IN YIP. MECHANIC PERFORMED FOD INSPECTION IAW MM, RAN AIRCRAFT IAW MM 72- 00 WITH NO DEFECTS NOTED AT THIS TIME. ACFT WAS RESTRICTED TO 33,000 IAW GMM V-3. ACFT RETURNED TO YIP AND MAINTENANCE INSPECT AIRFRAME, FUEL CONTROL AND FUEL PUMP FILTERS IAW DA-20 MM WITH NO DEFECTS NOTED. INSPECTED PT2 LINE, P3 LINE C 2 L 7 2 4F 4 F A7EU E7EA 20080730 NM 2008 7 30 SWAA084013 1 20080720 A 5240 507945 SKIN BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPV CHECK, FOUND FWD SERVICE DOOR SKIN CRACKED AT LOWER FWD CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800875 1 20080704 A 5210 STEP CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 ASD LOWER STEP CRACKED. REMOVED AND REPLACED ASD LOWER STEP IAW AMM 52-11-04. (S) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 KCSA081288 1 20080618 A 5340 ATTACH ANGLE BOEING 747 747122 1384872 NM BS 2231 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FRAME ATTACH ANGLE IS CRACKED, FORWARD SIDE OF R/H BS 2231 FRAME AT WL 200 LOWER MAIN SILL. (B) 2 L 7 4 4F RT A20WE 20080729 EA 2008 7 29 TRAX200800857 1 20080701 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA BS 559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 861AS 7445 RIGHT SIDE FLOOR SEAT TRACK FORWARD OF LAV AT FS559+112 HAS SEVERE CORROSION. REMOVED DAMAGE BY BLENDING PER SRM 51-12 -00, REMOVED DAMAGE FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS PER SRM 53-51-49 AND 51-21-49 FIG 101, APPLIED FINISH PER SRM 51-21-16 SG7021421 JOB COMPLETE. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAA920081314 1 20080704 A 3350 1103213 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 322AW 25400 PHX - FLT 412 - ROW 6 EMERGENCY LIGHT INOP. RELAMP, NO HELP. MX REPLACED LIGHT HOUSING. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A16WE 20080729 2008 7 29 USAABA08021 4 20080620 A 3441 46502003030316 ADIRU AIRBUS 330 A330323 3930335 EU NR 3 FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 275AY 4078 0370 MAN FLT 735 EN ROUTE MAN TO PHL. THE FLIGHT HAD AN ADIRU 3 FAILURE PRIOR TO ETOPS AIRSPACE, PREVENTING ETOPS OPERATIONS . THE FLIGHT RETURNED TO FIELD MAN, AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SWAPPED ADIRU 3 WITH ADIRU 2, AND PLACED ADIRU 2 ON MEL. MAINTENANCE REPLACED ADIRU 2. OPERATIONAL CHECKS OK. (S) 2 L 7 2 4F RT A46NM 20080729 NM 2008 7 29 USAA920081277 1 20080619 A 5310 654795944 DOOR FRAME BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW 23713 CLT - C22 - MAJOR REPAIR - AFT CARGO DOOR CUTOUT FORWARD FRAME HAS A .500 INCH CRACK AT LOWER DOOR STOP BS 827 BETWEEN S 23-24R. REPAIRED AFT CARGO DOOR CUTOUT FORWARD FRAME AT LOWER DOOR STOP BS 827 BETWEEN S23-24R IAW BOEING 737 DRAWING 6 9-42945 AND SRM 51-40-02. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081305 1 20080529 A 5753 6546430100 FLAP BOEING 737 7373S3 1384711 NM RT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW 23713 CLT - C22 - MAJOR REPAIR - RT WING INBOARD FOREFLAP HAS AREA OF DELAMINATION. REPLACED RT WING INBOARD FOREFLAP IAW B73 7 AMM 27-51-07. (S) 2 L 7 2 4F RT A16WE 20080729 CE 2008 7 29 DXTA200803139 1 20080623 A 3230 LANDING GEAR CESSNA 500 560CESSNA 2076750 CE MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 818QS 5600778 AFTER TAKE OFF THE LANDING GEAR WOULD NOT RETRACT. (B) 2 L 7 2 4F RT A22CE 20080729 NM 2008 7 29 ASAA0843137 1 20080612 A 5313 654655418 STRINGER BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 DOUBLE DRILLED HOLE ON STRINGER FLANGE. REPAIRED HOLE PER SRM 51 70 11. 2 L 7 2 4F RT A16WE 20080729 CE 2008 7 29 DXTA200803143 1 20080625 A 2730 ELEVATOR SYSTEM RAYTHN DH125 HAWKER800XP 7150012 CE INOPERATIVE E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 858QS 258691 ABORTED TAKEOFF AT APPROXIMATELY 130 KIAS DUE TO NO ELEVATOR AUTHORITY. (B) 2 L 7 2 4F RT A3EU 20080729 NM 2008 7 29 ASAA0843139 1 20080507 A 5311 654654965 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 AFT CARGO PIT BS 767 BETWEEN 25R AND 26R LOWER FLANGE OF FRAME (AFT SIDE) HAS CORROSION. AFT CARGO PIT B767 BETWEEN STR INGER 25R 26R LOWER FLANGE REPAIRED IAW B737 400 SRM 51 70 11. REPAIRED WITH REPAIR PART. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800785 1 20080613 A 5210 MOTOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR ASSIST INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 844AS 7317 AIRSTAIR DOOR WILL NOT OPEN REMOVED AND REPLACED CABIN DOOR ASSIST MOTOR IAW AMM 52-11-00, DEFER CLEARED, PLACARD REMOV ED. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 ASAA0843146 1 20080508 A 5320 69353521 TIE CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 E&E COMPARTMENT BS 380 STR 22L TIE CLIP CRACKED. E&E COMPARTMENT BS 380 STR 22L TIE CLIP REPLACED IAW B737 400 SRM 51 4 0 02. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843147 1 20080506 A 5311 654659673 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 AFT CARGO PIT BS 727C AT STR 25L TOP FLANGE OF FRAME DENTED. REPAIRED WITH REPAIR PART IAW B737 400 SRM. 2 L 7 2 4F RT A16WE 20080729 CE 2008 7 29 DXTA200803121 1 20080614 A 2150 A/C PACK CESSNA 750 750 2076810 CE ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 913QS 7500113 AT FL390 SMELLED SMOKE AND PERFORMED AND EMERGENCY DECENT AND DIVERTED TO OMA. NO VISIBLE SMOKE UNTIL PACKS OFF. A HAZ E DEVELOPED. KASE-KOMA (B) 2 L 7 2 4J RT T00007WI 20080729 NM 2008 7 29 ASAA0843157 1 20080507 A 5311 90526913 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 FRAME CRACKED. REPAIRED FRAME PER EA 5310 02797. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800899 1 20080710 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 VARIOUS EMERGENCY LIGHTS IN CABIN. REMOVED AND REPLACED NR 4 POWER SUPPLY UNIT AND BATTERY PACK ASSY IAW CRJ200 AMM33-5 0. OPS GOOD. NO OTHER DEFECTS NOTED AT THIS TIME. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800779 1 20080611 A 5320 INTERCOSTAL CNDAIR CL600 CL6002C10 1390015 EA BS 364 S27L CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 LT SIDE INTERCOSTAL CORRODED AT STA 364 STR 27. BLENDED CORROSION WITH LIMITS TO SRM 52-22-55. ALODINE, PRIME, PAINT AN D DYNOTROL IAW SRM 51-25-00. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 ASAA0843167 1 20080507 A 5311 65465252 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 RIGHT FRAME AT STA 380 CRACKED AT PSU RAIL BRACKET. RIGHT FRAME AT STA 380 PSU RAIL BRACKET REPAIRED IAW CASCADE ERO 83 37 AND ASA EA 5310 02797. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843141 1 20080610 A 5347 6546815154 SEAT TRACK BOEING 737 7374Q8 138447Q NM CABIN WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 SEAT TRACK WORN. REPLACED TRACK PER SRM 53 00 52. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0853168 1 20080701 A 2430 115195214 CONTROL UNIT BOEING 737 737890 1384527 NM COCKPIT MALFUNCTIONED A ASAA O OTHER O OTHER UK UNKNOWN 1 NM 02 585AS 3331 35683 SPCU STBY C/B OUT RESET SPCU STBY PWR C/B REF 20 60 01. CLEARED ELEC FAULT ON GENERATOR PANEL STBY POWER SYSTEM, OPS CH ECK NORMAL PER MM 24 34 00. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843154 1 20080512 A 5330 65479551 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 FUSELAGE SKIN DENT. REPAIRED PER SRM 53 00 01 AND EA 5330 02357. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 MASA200800472 1 20080616 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27185 7185 ASH FLT 7000, IAD-ORD. FLOOR LEVEL EMERGENCY LIGHTS AFT ROW 8 INOP. RE-SECURED CONNECTOR. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800787 1 20080614 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 929EV 8007 AFT EMER CEILING LIGHT INOP RELAMPED AFT EMER CEILING LIGHT IAW AMM 33-51-16. OPS CK GOOD. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800811 1 20080620 A 5320 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR TRACK CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 930EV 8014 CARGO DOOR FWD TRACK SUPPORT LOWER U CHANNEL IS CRACKED REMOVED AND REPLACED CARGO DOOR FWD TRACK SUPPORT LOWER U CHAN NEL PER SRM 51-42-06. (B) 2 L 7 2 4F RT A21EA 20080729 CE 2008 7 29 DXTA200803127 1 20080616 A 2120 UNKNOWN CESSNA 750 750 2076810 CE CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 926QS 7500026 STRONG OILY SMELL IN CABIN AFTER APU START. (B) 2 L 7 2 4J RT T00007WI 20080729 EA 2008 7 29 TRAX200800770 1 20080607 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 ASD LOWER STEP CRACKED. REMOVED AND REPLACED ASD LOWER STEP IAW AMM 52-11-00. OPS CHECKED GOOD. REMOVED AND REPLACED AS D LOWER STEP IAW AMM 52-11-00. OPS CHECKED GOOD. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 ASAA0843155 1 20080603 A 5755 654645262 SKIN BOEING 737 7374Q8 138447Q NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 NR 5 SPOILER LOWER SURFACE IS DENTED. REPAIRED PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800646 1 20080514 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 978EV 7723 ATTACH CLIP CRACKED AT BS 280 BULKHEAD WEB RBL 9. REMOVED 280 RBL 9 ATTACH CLIP IAW SRM 51-42-21. INSTALLED 280RBL 9 AT TACH CLIP IAW SRM 51-42-21. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800881 1 20080705 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 LT FS280 WEB CORRODED. (B) REMOVED MINOR CORROSION ON LT 280 WEB, LOWER INBD CORNER (1X.8X.004 REMOVED). BLEND IS WIT HIN LIMITS PER SRM 53-11-10. (S) 2 L 7 2 4F RT A21EA 20080730 WP 2008 7 30 WRLA2008051 1 20080607 A 5740 APB73511 FITTING DOUG DC10 DC1030 3023501 WP CENTER FUEL TANK CRACKED A WRLA O OTHER O OTHER NR NOT REPORTED 1 SO 11 14075 46922 DURING INSPECTION, MAINTENANCE FOUND FITTING CRACKED IN CENTER FUEL TANK I/B CORNER ABOVE ACCESS DOOR 141AZ. REMOVED AN D REPLACED FITTING. (S) 2 L 7 3 4F A22WE 20080730 EU 2008 7 30 MAL2008F00004 1 20080604 A 5753 SKIN SAAB SF340 340B 7860101 EU LT TE FLAP PUNCTURED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 449XJ 340B449 PUNCTURE IN UPPER SKIN OF LT FLAP BELOW EXHAUST SHROUD 454AT. DID WET LAYUP COMPOSITE REPAIR ON LT FLAP BELOW EXHAUST S HROUD 454AT IAW EO S51031. (S) 2 L 7 2 4T RT A52EU 20080730 EA 2008 7 30 CHQA200800121 1 20080630 A 5240 600332801001 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE OXYGEN SERVICE OPEN A CHQA O OTHER O OTHER NR NOT REPORTED 1 GL 11 483CA 7689 E873434 FLIGHT 5544, SRQ TO IAH. AT 1,000 FT AFTER TAKEOFF, THE FLIGHT CREW RECEIVED A STALL FAIL MESSAGE ON EICAS. THE ACFT W AS LEVELED OFF AT 3,000 FT AND THE CREW HEARD A LOUD BUZZING SOUND. THE ACFT RETURNED TO SRQ AND LANDED WITHOUT INCIDEN T. MAINTENANCE INSPECTED THE ACFT AND FOUND THE OXYGEN SERVICE DOOR OPEN. THE DOOR WAS INSPECTED AND CLOSED WITH NO FU RTHER DEFECTS. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080730 NM 2008 7 30 CALA0800689 1 20080708 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM BS 867 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14629 27533 FRAME CRACKED STATION 867 AT S9L. REPAIRED FRAME PER EA 5310-04498 OP2. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800690 1 20080708 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM BS 867 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14629 27533 FRAME CRACKED STATION 867 AT S-9 RIGHT. REPAIRED FRAME PER EA 5310-04498 OP2. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083991 1 20080720 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 967 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 MWEA080086 1 20080618 A 2611 110001 SMOKE DETECTOR BOEING 717 717200 1383700 NM LT LAVATORY INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 917ME 55179 LT LAVATORY SMOKE DETECTOR FAILED TO TEST. REMOVED AND REPLACED LAVATORY SMOKE DETECTOR. (S) 2 L 7 2 4F TR A6WE 20080730 EU 2008 7 30 MAL2008F00002 1 20080617 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 288-363 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422XJ 340B422 SEAT TRACK CORRODED AT STA 288 TO STA 363 BL 0 & BL 18.3. SEAT TRACKS AT STA 288 AND STA 363 REPLACED IAW EO S53060 AND INSTALLED WITH SOLID RIVETS IAW SRM 51-40-21 AT BL 0 AND BL 18.3. (S) 2 L 7 2 4T RT A52EU 20080730 NM 2008 7 30 SWAA084058 1 20080719 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 520 S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 22L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080730 SO 2008 7 30 RAIA0080606 1 20080610 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 831HK 145232 MX - DTW - EMERGENCY LIGHT 16D INOP. MAINTENANCE RE-LAMPED LIGHT ASSEMBLY. (S) 2 L 7 2 4T RT T00011AT 20080730 EU 2008 7 30 COEA0809911 1 20080530 A 5531 S55371301200 SPAR AEROSP ATR42 ATR42300 8680920 EU VERTICAL STAB CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 911FX 045 FOUND DURING HEAVY CHECK AT COE. AFT SURFACE OF VERTICAL STAB REAR SPAR HAS AREAS OF SURFACE CORROSION BETWEEN LOWER & UPPER RUDDER ATTACH FITTINGS. REPAIRED PER SRAS DO/TS-2656/08-4694, NOTE DO/TS-2665/08-10353. CORROSION REMOVED FROM T HE RIVET HOLE AREA PER THE SRM. A REPAIR DOUBLER WAS MADE & INSTALLED ON THE STABILIZER SPAR. (S) 2 H 7 2 4T RT A53EU 20080730 EU 2008 7 30 MAL2008F00003 1 20080607 A 5311 FRAME SAAB SF340 340B 7860101 EU BS 630 DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 443XJ 340B443 AT STA 630 ON RT SIDE, FRAME DAMAGED BETWEEN STRINGER SL1614 AND SL1620. REPAIRED IAW EOS53476. THIS EO ACCOMPLISHES A REPAIR AS NEEDED TO THE RT FUSELAGE FRAME`S INNER FLANGE FROM 30.112-725.5 IAW SRM 53-80-30 SPECIAL REPAIR PARAGRAPH 2. (S) 2 L 7 2 4T RT A52EU 20080730 EU 2008 7 30 COEA0812911 1 20080529 A 5751 S5761002520440 FITTING AEROSP ATR42 ATR42300 8680920 EU RT AILERON CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 911FX 045 FOUND DURING HEAVY CHECK AT COE. RT AILERON CENTER TEE PICKUP FITTING I/B SIDE HAS EXFOLIATING CORROSION. REMOVED AND REPLACED RT AILERON ASSY. (S) 2 H 7 2 4T RT A53EU 20080730 NM 2008 7 30 CALA0800702 1 20080714 A 2910 271N61192 HOSE BOEING 757 757224 1384958 NM HYD SYSTEM RUPTURED A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 17105 27295 LOST LEFT HYDRAULIC QUANTITY INFLIGHT LANDED AT 227,440 POUNDS VERTICAL SPEED - 264. FOUND DOWNLOCK ACTUATOR HYDRAULIC LINE RUPTURED ON RIGHT-HAND SIDE. REMOVED AND REPLACED RIGHT-HAND DOWNLOCK ACTUATOR, PRESSURE AND RETURN LINES REF AMM 20-10-10. LEAK CHECK GOOD. PERFORMED CONDITIONAL 1 REF AMM 29-11-00. NO DEFECTS NOTED. PERFORMED PHASE 1 OVERWEIGHT INSPECTION REF AMM 05-51-35. NO DEFECTS NOTED, A/C OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A2NM 20080729 EA 2008 7 29 TRAX200800742 1 20080603 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 684BR 7708 PASSENGER DOOR STAIR AFT DRAG ANGLE IS CRACKED 1/2" REPAIRED PAX DOOR STAIR AFT DRAG ANGLE IAW REO 601R-52-11-513 AND E T/CT 601R-52-11-513. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 2008UALA03450 1 20080617 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN UNSECURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 583UA 26705 THE 13C EXIT PATH LIGHTING IS WARPED. SECURED EEL STRIP TO FLOOR, OPS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 NM 2008 7 29 2008UALA03580 1 20080624 A 2751 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION LD LANDING 1 WP 29 646UA 25283 EICAS MESSAGES T/E FLAP DISAGREE & T/E FLAP SHUTDOWN DISPLAYED. 2 L 7 2 4F 4 F RT A1NM E24NE 20080729 EA 2008 7 29 TRAX200800752 1 20080604 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 693-977 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 LT CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE FS 693.00 TO FS 977.00. REMOVED SEAT RAIL ASSY, INSPECTED AND FOUND COR ROSION UNDER SEAT RAIL. PREPPED, PRIMED, AND PAINTED AREA ON FUSELAGE SKIN IAW SRM 53-00-49. REPLACED SEAT RAILS AT FLOO R BS 693.00 TO 977.00 IAW AMM 53-00-49. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800883 1 20080705 A 5320 ANGLE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 COCKPIT ENTRANCE PANEL 221ALF AFT ANGLE CORRODED. REMOVED ANGLE IAW SRM 51-42-06. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 2008UALA03631 1 20080627 A 2540 UNKNOWN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LAVATORY SMOKE A UALA F ACTIVATE FIRE EXT. A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 768UA 26919 LAV COMPARTMENT DOOR DAMAGED AND LAV WASTE CONTAINER DAMAGED DUE TO SUSPECT LAV SMOKE IN LAV WASTE CONTAINER. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080729 NM 2008 7 29 ZZDA2008130 1 20080715 A 2170 1808494 COALESCER BAG BOEING 737 7377BD 1384511 NM A/C BAY CONTAMINATED A ZZDA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 37 166AT 33917 AIR CONDITIONING SMOKE IN COCKPIT. RIGHT PACK OFF, RECIRCULATION FAN OFF AND SMOKE DISSIPATED. NO FUMES NOTED WHEN AIR CRAFT PULLED INTO GATE. RAN APU AND NOTED FUMES FROM BOTH LEFT AND RIGHT PACKS. PERFORMED FIM 49-55 TASK 802 - FUMES A PPEAR WITH APU AND PACK OPERATION. PERFORMED AIR CONDITIONING SYSTEM OIL CONTAMINATION REMOVAL IAW MM 21-00-01. REMOVE D AND REPLACED LEFT AND RIGHT COALESCER BAGS IAW MM 21-51-05. RAN ENGINES WITH NO FUMES NOTED. 2 L 7 2 4F RT A16WE 20080729 EU 2008 7 29 USAA920081176 1 20080603 A 3350 321454 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 603AW 15940 3125 661 FLT 460 PHX - IND, AFT DOORS EXIT LIGHTS ARE BLINKING. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT EMERGENCY POWER SU PPLY UNIT AND BATTERY. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080729 EU 2008 7 29 USAA920081169 1 20080528 A 5320 D53472189204 BEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 652AW 0953 AL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN BEAM, BS 3257 FR 68, -Y1180. REPLACED CABIN BEAM, BS 3257 FR 68, -Y11 80 IAW SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080729 NM 2008 7 29 USAA920081177 1 20080605 A 3350 1011143 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 306AW 24633 FLT 79 - PHX, SEAT ROW 1 LT, AFT EMERGENCY AISLE LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT ROW 1. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAAEMB0008006 1 20080603 A 5210 FASTENER EMB ERJ190 ERJ190100IGW 3260408 NM PAX DOOR MISSING A USAA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 19 945UW 19000062 CLT - UNABLE TO OPEN CABIN DOOR. MAINTENANCE FOUND THE PIN FOR DOOR HANDLE MISSING CIRCLIP. THE PIN HAD MOVED FORWARD AND WAS HITTING THE DOOR STRUCTURE PREVENTING THE DOOR HANDLE FROM OPERATING. THE PIN WAS PUT BACK IN ITS PLACE, REPLAC ED THE WASHER AND CIRCLIP. THE DOOR OPENS AND SHUTS NORMALLY. (S) 2 L 7 2 4F RT A57NM 20080729 NM 2008 7 29 USAA920081187 1 20080529 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - LEVEL 2 CORROSION ON THE AFT PRESSURE BULKHEAD, BS 1016, RBL 5. REPAIRED THE AFT PRESS URE BULKHEAD, BS 1016, RBL 5 IAW EA 100475. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081238 1 20080606 A 5230 6547952524A SKIN BOEING 737 7373S3 1384711 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW 23713 CLT - C22 - MAJOR REPAIR - CARGO DOOR INNER SKIN CRACKED. REPAIRED CARGO DOOR INNER SKIN IAW US AIRWAYS EA NR100513. ( S) 2 L 7 2 4F RT A16WE 20080729 EU 2008 7 29 TRAX200800874 1 20080704 A 2913 PUMP AEROSP ATR72 ATR72 EU HYD SYSTEM INOPERATIVE A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 641AS 387 AFTER T/O FLAPS REMAINED AT 15 DEG. WHEN SELECTED TO 0 DEG. AIRCRAFT RETURNED TO ATL AFTER T/O, EMERGENCY DECLARED. F LT4232. REMOVED AND REPLACED BLUE HYD PUMP OPS CHECK GOOD IAW ATR-72 AMM 29-10-00. (B) 2 H 7 2 4T RT 20080729 CE 2008 7 29 DXTA200803136 1 20080622 A 3220 UNKNOWN CESSNA 750 750 2076810 CE NLG UNKNOWN E DXTA O OTHER O OTHER CL CLIMB 1 GL 07 955QS 7500055 NOSE GEAR "BUMP" OCCURED MULTIPLE TIMES DURING CLIMBOUT. (B) 2 L 7 2 4J RT T00007WI 20080729 NM 2008 7 29 USAA920081324 1 20080703 A 5313 BAC1498139 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 302AW 24009 PHX - SKIN REPAIR - MAJOR REPAIR - STRINGER CRACKED BS 500C S16R. REPAIRED STRINGER AT BS 500C S16R IAW B737 SRM 53-00- 05-2R1. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081322 1 20080704 A 5330 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 23885 CLT - RON - MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT BS 881 - 883, S25R. REPAIRED FUSELAGE SKIN AT BS 881 - BS 883, S25 R IAW B737 SRM 53-00-01 AND TYPICAL REPAIR 53-27. (S) 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800816 1 20080621 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 874AS 7551 ADS ENTRYWAY EMERGENCY EXIT LIGHT IS BROKEN. REMOVED AND REPLACED ASD ENTRYWAY EMERGENCY EXIT LIGHT IAW AMM 33-51-19. O PS CHECK NORMAL. (B) 2 L 7 2 4F RT A21EA 20080729 CE 2008 7 29 DXTA200803126 1 20080615 A 3150 WARNING MESSAGE CESSNA 500 560CESSNA 2076750 CE ILLUMINATED E DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 830QS 5600784 WHILE TAXIING FOR DEPARTURE, POWER BRAKE CIRCUIT BREAKER POPPED FOLLOWED BY A "LO BRAKE PRESS/ANTISKID INOP" CAUTION LIG HT AND LOSS OF BRAKING PRESSURE. (B) 2 L 7 2 4F RT A22CE 20080730 NM 2008 7 30 SWAA084014 1 20080720 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 360 S23R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER 23R CORRODED AT BS 360. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080730 2008 7 30 SWAA084015 4 20080720 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800666 1 20080702 A 5320 651758243 STIFFENER BOEING 737 737524 1384721 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 STATION 178 VERTICAL BEAM WEB AT LBL 17 AND WL 234 CRACKED. REMOVED, FABRICATED AND INSTALLED UPPER WEB AT LBL 17 IAW E CRA 5310-04794. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800667 1 20080702 A 5312 6516300291 BULKHEAD BOEING 737 737524 1384721 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 STATION 178 BULKHEAD WL 207 LBL 4.5 FASTENER HOLE SHOWS CRACK INDICATION. REAMED HOLE TO .214 IAW ECRA 5310-04794 HFEC IAW B737 NDT MANUAL PT6-51-00-00 SIG.16 OF OPEN HOLE NO CRACKS NOTED. REAMED HOLE TO.246 FOR INSURANCE CUT IAW ECRA 531 0-04794 INSTALLED FASTENER IAW ECRA 5310-04794. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800668 1 20080623 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM BS 440 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 STATION 440 RIGHT-HAND FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. REPAIRED CRACK ED FRAME AT BODY STATION 440 AT A/C BRACKET BETWEEN S-8 AND S-9R PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800669 1 20080628 A 5320 65479573 THRESHOLD BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 AFT CARGO DOOR SILL THRESHOLD WEB CORRODED ON LOWER SIDE AT NUT PLATES. FABRICATED AND INSTALLED NEW DOOR SILL THRESHOL D WEB IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083892 1 20080714 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM BS 340 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 340, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083895 1 20080714 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083930 1 20080714 A 5610 57176429 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 29 383SW 26589 FLIGHT DECK R4 WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 20080730 EA 2008 7 30 VNAA0806010 1 20080615 A 5100 NONE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NO DAMAGE NONE A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 206PS 7860 CREW REPORTED A BIRD STRIKE TO THE CAPTAIN`S WINDSHIELD. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080730 NM 2008 7 30 CALA0800694 1 20080710 A 5320 694147374 INTERCOSTAL BOEING 737 737524 1384721 NM BS 420-440 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 WEB AT STATION 420 TO 440 LBL 27 IS CRACKED IN FORWARD CARGO HOLD. REMOVED WEB AND INSTALLED NEW WEB AT STATION 420 TO 440 LBL 27 PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800696 1 20080710 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM BS 907 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14629 27533 FRAME CRACKED STATION 907 AT S-9L. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED REPAIR DOUBLERS PER EA 5310-04498 OP 2. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083899 1 20080714 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 452WN 29846 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083900 1 20080714 A 5754 SKIN BOEING 737 7375H4 138449D NM NR 3 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED 18Y CHECK, FOUND LT WING NR 3 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083867 1 20080714 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 578 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 WRLA2008054 1 20080624 A 5343 ACA7051 TRUNNION DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 48407 DURING LANDING GEAR REPLACEMENT MAINTENANCE FOUND CORROSION ON CENTER LANDING GEAR LT PILLOW BLOCK AFT UPPER SURFACE OF PILLOW BLOCK AFT BOLT HOLE CORRODED. (S) 2 L 7 3 4F RT A22WE 20080730 NM 2008 7 30 SWAA083902 1 20080714 A 5754 SKIN BOEING 737 7373H4 1384600 NM NR 2 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083925 1 20080715 A 3350 100031 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 LEFT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 20080730 2008 7 30 SWAA083906 4 20080711 A 2565 D31354 SLIDE BOEING 737 7373L9 1384470 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083984 1 20080718 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM BS 274 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 274, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083986 1 20080718 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED MV4 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083987 1 20080718 A 5240 6969854 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED 18Y CHECK, FOUND FWD SERVICE DOOR AFT FRAME CRACKED AT LOWER CORNER. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083994 1 20080716 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 503C S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083871 1 20080711 A 5330 6545766 SKIN BOEING 737 737301 1384611 NM BS 510 S12R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 12R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083926 1 20080715 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM EMERGENCY LIGHT FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED MV2 CHECK, RT AFT CABIN EMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PACK P ER MM. 2 L 7 2 4F RT A16WE 20080730 2008 7 30 SWAA083927 4 20080715 A 2565 D31354 SLIDE BOEING 737 7373G7 1384595 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080730 2008 7 30 SWAA083907 4 20080712 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 693SW 23174 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083928 1 20080715 A 5343 275A1104 TRUNNION BOEING 737 7377H4 1384404 NM NLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 706SW 27840 DURING SCHEDULED 10Y CHECK, FOUND NLG TRUNNION CORRODED. REPAIRED TRUNNION PER EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083909 1 20080712 A 5743 115A5211 TRUNNION BOEING 737 7377H4 1384404 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 723SW 27855 DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083908 1 20080712 A 5743 115A5211 TRUNNION BOEING 737 7377H4 1384404 NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 723SW 27855 DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083910 1 20080713 A 2560 P207001 FLASHLIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 745SW 29491 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083876 1 20080714 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 773SA 27881 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, RBL 36. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 2008UALA03607 1 20080627 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 DOOR 4R AFT SILL EMERGENCY LIGHT IS INOP. EMERGENCY LIGHT ASSY. FOUND FAULTY LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080730 NM 2008 7 30 SWAA083875 1 20080714 A 5315 149A5510 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 773SA 27881 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER TEE CAP CORRODED AT BS 328, RBL 20. REPAIRED TEE CAP PER SRM. 2 L 7 2 4F RT A16WE 20080730 EA 2008 7 30 VNAA0806011 1 20080620 A 5100 NONE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NO DAMAGE TO A/C NONE A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 245PS 7919 CREW REPORTED A BIRD STRIKE TO THE RT WINDSHIELD. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. ACFT WAS RELEASED FOR SE RVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080730 NM 2008 7 30 SWAA083996 1 20080715 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM BS 390 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 390, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 2008UALA03583 1 20080624 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 564UA 26666 DOOR 4 LEFT OUTSIDE EMERGENCY LIGHT INOP. *S/D* LAMP INOP. RELAMPED LIGHT BULB AND OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080730 2008 7 30 2008UALA03592 4 20080625 A 2565 D31517121 ASPIRATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ESCAPE SLIDE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 457UA A6537 1146 CROSS THREADED ASPIRATOR FITTING. IMPROPER INSTALLATION. REPLACED ASPIRATOR. 2 L 7 2 4F 4 F RT A28NM E40NE 20080729 EA 2008 7 29 TRAX200800887 1 20080705 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 933EV 8022 RT FWD EXTERIOR EMERGENCY LIGHT BURNED OUT REPLACED RT FWD EXTERIOR EMERGENCY LIGHT BULB IAW CRJ 200 AMM 33-51-21. OPS CK GOOD. --[SDR CLOSED](B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAA920081175 1 20080601 A 5754 SKIN BOEING BOEING 757 7572B7 1384964 NM L/E SLAT DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 942UW P20732 27807 MCN - MAJOR REPAIR - A CHECK WINGLET MOD - RT WING NR 10 SLAT TRAILING EDGE HAS 2 AREAS THAT ARE DEBONDED, SS 790 AND SS 802. REPAIRED RT WING NR 10 SLAT TRAILING EDGE, SS 790 AND SS 802 IAW B757 SRM 51-70-10 REPAIR 2 AND 4. (S) 2 L 7 2 4F RT A2NM 20080729 EA 2008 7 29 TRAX200800692 1 20080526 A 5310 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 924EV 7830 CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX .5" LONG. REMOVED AND REPLACED CARGO DOOR SUPPORT BEAM LOWER ANGLE WITH A NEW SERVICEABLE ANGLE IAW SRM 51-42-21. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAA920081262 1 20080621 A 5753 FLAP BOEING 757 7572B7 1384964 NM LT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 939UW 27303 CLT - C-22 - MAJOR REPAIR - FOUND DELAMINATION ON LEFT OUTBOARD AFT FLAP MEASURES 4"X4.5", 5.5" FORWARD OF TRAILING EDGE . REPAIRED DELAMINATION ON LEFT OUTBOARD AFT FLAP 4"X4.5" AREA., 5.5" FORWARD OF TRAILING EDGE IAW B757 SRM 57-53-01. (S) 2 L 7 2 4F RT A2NM 20080729 NM 2008 7 29 KCSA081299 1 20080625 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 2260 S1L CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STA-2260 STRINGER 1-L IS CORRODED. (B) 2 L 7 4 4F RT A20WE 20080729 EA 2008 7 29 TRAX200800719 1 20080601 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 908EV 7654 F/A REPORTS MAIN CABIN DOOR DIFFICULT TO CLOSE. NO FAULT FOUND OPS CHECK GOOD IAW AMM 52-11-00. (B) 2 L 7 2 4F RT A21EA 20080729 EU 2008 7 29 USAABA08022 1 20080627 A 5610 NP1752014 WINDSHIELD AIRBUS 330 A330323 3930335 EU COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 275AY 35966 0370 YHZ - FLT 700 EN ROUTE PHL TO FRA. THE FLIGHT REPORTED A CRACKED WINDSHIELD DURING CRUISE FLIGHT. PROCEDURES REQUIRED DESCENDING TO FL 230. THE FLIGHT DIVERTED TO YHZ SINCE THE FUEL BURN AT FL 230 WOULD BECOME EXCESSIVE. THE FLIGHT LAND ED WTIHOUT FURTHER INCIDENT. (S) MAINTENANCE REPLACED THE FIRST OFFICER`S WINDSHIELD. OPERATIONALLY CHECKS OK. (B) 2 L 7 2 4F RT A46NM 20080729 NM 2008 7 29 DXTA200803130 1 20080617 A 3230 LANDING GEAR GULSTM 200 200 4500308 NM MALFUNCTIONED E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 724QS 100 MAIN LANDING GEAR FAILS TO FULLY RETRACT. (B) 2 L 7 2 4F RT A53NM 20080729 EA 2008 7 29 TRAX200800813 1 20080621 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 LBL 9 CLIPS CRACKED INBD AND OUTBD AT FS 280. REMOVED AND REPLACED CLIPS IAW CRJ 200 SRM 51-42-21 AND AMM 51-23-00. (B ) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 DXTA200803095 1 20080603 A 3260 INDICATION SYS AMD FALC50 FALCON2000 2730170 NM MLG MALFUNCTIONED E DXTA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 07 265QS 165 UPON GEAR RETRACTION AFTER TAKEOFF THE THREE GREEN LIGHTS WENT OUT; HOWEVER THE THREE RED LIGHTS REMAINED ON AND THE GEA R HANDLE WAS FLASHING. (B) 2 L 7 2 4F RT A50NM 20080729 NM 2008 7 29 ASAA0843135 1 20080508 A 5315 654681179 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 FLOORBEAM UPPER FLANGE IS CORRODED. REPLACED BEAM PER EA 5310 02800. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843143 1 20080501 A 5754 65C26602301 SLAT BOEING 737 7374Q8 138447Q NM NR 2 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 NR 2 SLAT INBOARD END FOUND DELAMINATED. NR 2 SLAT REPAIRED PER SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 2008UALA03501 1 20080620 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR OBSTRUCTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 551UA 25399 THE 2L WILL NOT ARM. DEBRIS UNDER GIRT BAR. CLEANED DEBRIS FROM UNDER GIRT BAR. DOOR ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080730 NM 2008 7 30 SWAA084001 1 20080720 A 5330 6545800 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND FWD ENTRY DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800685 1 20080707 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM BS 747 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 RIGHT STATION 747 FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. CUT OUT DAMAGE AT S TATION 747 BETWEEN S-8 AND S-9, REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800686 1 20080707 A 5311 6546595 FRAME BOEING 737 737524 1384721 NM BS 727A S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 RIGHT STATION 727A FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. CUT OUT CRACKED AR EA OF BODY STATION 727A FRAME BETWEEN S-8 AND S-9, INSTALLED REPAIR ANGLES A AND B IAW EA 5310-098. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 MWEA080085 1 20080614 A 5330 5936002 SKIN DOUG MD88 MD88 3023688 NM BS 655-674 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 701ME 49760 LT FUSELAGE EXTERIOR SKIN REPAIR AT FRAME STATION 655 TO 674, LONGERON 22-23L. FABRICATED AND INSTALLED SKIN PLATE. (S ) 2 L 7 2 4F RT A6WE 20080730 NM 2008 7 30 SWAA084012 1 20080719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500B S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080730 EU 2008 7 30 COEA0804911 1 20080611 A 5531 S55371301200 SPAR AEROSP ATR42 ATR42300 8680920 EU VERTICAL STAB CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 911FX 33406 045 FOUND DURING HEAVY CHECK AT COE. FOUND LEVEL 2 CORROSION AROUND THE RIVET FILLED TOOLING HOLE ON THE AFT SURFACE OF VER TICAL STAB REAR SPAR. LOCATED IN THE CENTERLINE OF THE SHEAR WEB BETWEEN STIFFENERS (P/N`S S55371300230 AND S5537130022 5). REPAIRED PER SRAS DO/TS-2656/08-4694, NOTE DO/TS-2665/08-10353. CORROSION REMOVED FROM THE RIVET HOLE AREA PER THE SRM. A REPAIR DOUBLER WAS MADE & INSTALLED ON THE STABILIZER SPAR. (S) 2 H 7 2 4T RT A53EU 20080730 NM 2008 7 30 CALA0800671 1 20080707 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 787 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 LEFT BS 787 FRAME CRACKED AT AIR CONDTIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. CUT OUT CRACKED SECTION OF BS 787 FRAME BETWEEN STR 8 LEFT AND STR 9 LEFT AND INSTALLED REPAIR ANGLES IAW EA 5310-04498. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA084057 1 20080719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 787 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA084054 1 20080719 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM BS 559 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083985 1 20080718 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM BS 340 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 340, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083866 1 20080714 A 5220 65C367341SP HANDLE BOEING 737 7373H4 1384600 NM OVERWING DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED BRDG CHECK, FOUND LT OVERWING EMERGENCY EXIT DOOR HANDLE BROKEN. REMOVED AND REPLACED DOOR HANDLE PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083995 1 20080717 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 425LV 29829 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083997 1 20080715 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM BS 460 S17L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 460, STR 17L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 NE 2008 7 30 SWAA083911 2 20080713 A 7200 CFM567B24G22 ENGINE BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE NR 1 FAILED A SWAA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SW 29 789SW 29816 876462 INFLIGHT SHUTDOWN, CLIMBING OUT OF SNA AT FL270 NR 1 ENGINE FAILED. REMOVED AND REPLACED NR 1 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080730 NM 2008 7 30 SWAA083954 1 20080716 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727B S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083953 1 20080716 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727A S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083952 1 20080716 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 685 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083949 1 20080716 A 5315 6546809 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 947, LBL 54. REPAIRED CHORD PER ER. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083691 1 20080704 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 847 S13L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 13L. REPAIRED FRAME PER ACO & EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083699 1 20080704 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM BS 303 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR FUSELAGE SKIN CUTOUT CRACKED AT BS 303.90, WL 236.68. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083700 1 20080704 A 5311 6546542 FRAME BOEING 737 7373H4 1384600 NM BS 616 S17L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 616, STR 17L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083705 1 20080704 A 5320 6545866 SUPPORT FITTING BOEING 737 7373H4 1384600 NM KEELBEAM CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM SUPPORT FITTING CRACKED AT BS 727, RBL 5. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083963 1 20080716 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 400 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 16R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083969 1 20080716 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 767 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 767, STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080731 EA 2008 7 31 COMA0860311 1 20080628 A 2997 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM TRIPPED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 918CA 7018 RECEIVED A GEAR DISAGREE AND HYDRAULIC PUMP 3B WARNING DURING CLIMBOUT OF JFK, CREW DECLARED AN EMERGENCY AND RETURNED T O THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. RESET CIRCUIT BREAKER FOR HYDRAULIC PUMP 3B AND PERFORMED GEAR SWINGS, NO DEFECTS NOTED. (S) 2 L 7 2 4F RT A21EA 20080731 SO 2008 7 31 C2XA08ON132 1 20080606 A 5210 HANDLE EMB 145 EMB145XR 3260214 SO PAX DOOR LOOSE A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 12195 14500943 FLT 0022 - ONT - FLIGHT CREW REPORTED MAIN CABIN DOOR HARD TO OPEN. MX PERSONNEL RESECURED LOOSE BOLT AT THE BASE OF HA NDLE ON MAIN CABIN DOOR. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4F RT 20080731 EA 2008 7 31 COMA0860316 1 20080707 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA BS 559 RBL 18 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 963CA 7127 DURING 559 INSPECTION FOUND OUTBOARD SIDE, LOWER END OF VERTICAL POST AT RBL 18 CRACKED. CUT OUT DAMAGE AND INSTALLED D OUBLER PER BOMBARDIER REO 601R-53-41-067. (S) 2 L 7 2 4F RT A21EA 20080731 NM 2008 7 31 HNAA0800198 1 20080607 A 3350 1013073 LAMP DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHT BURNED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 911HA 034 SECOND FLOOR EMERGENCY LIGHT IS INOPERATIVE (FLOOR PROX EMERGENCY ESCAPE PATH RED LIGHTS). REMOVED AND REPLACED BULB, W ORK COMPLETE. OPS CHECK GOOD. (S) 2 H 7 2 4T RT A13NM 20080731 EA 2008 7 31 CHQA200800110 1 20080611 A 2751 855D10011 POSITION SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT WING TE FLAPS FAULTY A CHQA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 465SM 15441 13530 7612 E873561 FLIGHT 5512, CRP TO IAH. WHILE ON APPROACH TO LAND, THE FLAPS WERE SELECTED TO 45 DEGREES, AND THE CREW RECEIVED A FLAP FAIL MESSAGE WITH THE FLAPS AT 40 DEGREES. THE CREW ABORTED THE APPROACH AND PERFORMED THE CHECKLISTS IN THE QRH AND L ANDED WITHOUT INCIDENT. MAINTENANCE PULLED CODES FROM THE FECU POINTING TO THE RT BRAKE POSITION SENSOR UNIT. THE BPSU WAS REPLACED AND RIGGED AND THE FLAPS OPERATED NORMALLY. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080731 SO 2008 7 31 C2X2008F00001 1 20080604 A 3350 110049 MOUNT EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT INOPERATIVE A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 16112 145660 COCKPIT OVERHEAD EMERGENCY LIGHT AND NR 1 OVERHEAD EMERGENCY LIGHT AND FWD LT OVERWING EMERGENCY LIGHT INOPERATIVE. REM OVED AND REPLACED NR 1 EMERGENCY BATTERY BASE IAW EMB145XR AMM 33-50-00. OPS CHECK GOOD. REMOVED AND REPLACED LT OVERW ING LAMP IAW EMB145XR AMM 33-50-07. OPS CHECK GOOD. (S) 2 L 7 2 4F RT 20080731 2008 7 31 HNAA0800189 4 20080530 A 2210 AUTOPILOT SYS DHAV DHC8 DHC8102 2809003 NM MALFUNCTIONED A HNAA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 EA 07 940HA 49134 156 WHEN AUTO PILOT SELECTED OFF F/O REPORTED POSSIBLE PITCH JAM, F/O REQUESTED HELP. CAPTAIN TOOK CONTROL, FELT NO JAM, NO TED ACFT FLEW NORMALLY. RIGGED ELEVATOR CONTROL CABLES IAW DASH 8 MM 27-32-00. MEL 30MAY08 16:52 ABE B15119 22-1 AUTOP ILOT DFRL 30MAY08 16:54 ABE. MX INSPECTED ELEVATOR CONTROL CABLES AND AUTOPILOT SERVO IN APU HOLE, NO DEFECTS NOTED. C YCLED ELEVATOR FULL TRAVEL SEVERAL TIMES, NO DEFECTS NOTED. RAN GMT ON ELEVATOR SERVO AND ENGAGED AND DISENGAGED A/P SE VERAL TIMES WITH NO FAULTS. REF 8 M/M 2 2-10-01. TRANSCRIBED TO HA 300 30MAY 08 SEQ 2 FOR FURTHER ACTION 940 22-00 265 9021 30MAY08 ABE CLOSE POSSIBLE PITCH JAM. MAINTENANCE ACTION COMPLETE SUBJECT TO SATISFACTORY EVAL FLIGHT. 67360 00 R 2 H 7 2 4T RT A13NM 20080731 EA 2008 7 31 COMA0860293 1 20080617 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FS 621 LBL 36 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 30545 7117 CRACK ON REAR PRESSURE BULKHEAD AT LBL 36.20 WL 80. REPAIRED REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1285. (S) 2 L 7 2 4F RT A21EA 20080731 2008 7 31 COMA0860277 4 20080609 A 8300 388700320153 CHECK VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30068 NE RT AGB FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 785CA 7326 DURING CLIMBOUT FROM CVG RT ENG HIGH OIL TEMP. EMERGENCY DECLARED, ACFT RETURNED BACK TO CVG AND LANDED SAFELY. FOUND RT ENG AGB OVER SERVICED WITH OIL. REMOVED AND REPLACED RT ENG BYPASS CHECK VALVE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080731 EA 2008 7 31 CHQA200800119 1 20080620 A 7500 356024310 SENSING ELEMENT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BLEED SYSTEM INTERMITTENT A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 473CA 7668 E873451 FLIGHT 5716, IAH TO JAX. ON CLIMB CREW RECEIVED A RT 14TH STAGE BLEED OVERTEMP MESSAGE. THE QRH WAS FOLLOWED, BUT THE M ESSAGE REMAINED. THE FLIGHT THEN LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE RT 14TH STA GE LOOP BAD. AFTER REPLACING THE LOOP THE SYSTEM OPERATED NORMALLY. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080731 GL 2008 7 31 COEA0802960 3 20080512 A 6111 A106GA0 BLADE CESSNA 208 208B 2073701 CE MCAULY 3AF34C 3GFR34C703 GL PROPELLER STRIPPED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 960FE 5442 208B0075 971903 STRIPPED OUT THREADS FOUND DURING MINI CHECK IN GEG: WHILE CHECKING FOR PROPER TORQUE ON THE PROPELLER BLADE ACTUATOR P IN (P/N B5072-1) ATTACHING SCREWS (P/N A-1635-159) ONE SCREW WAS UNABLE TO ACHIEVE PROPER TORQUE DUE TO STRIPPED OUT THR EADS IN THE BLADE BUTT. REMOVED SCREW AND FOUND AN UNUSUAL WEAR PATTERN ON SCREW AND THREADED PORTION OF THE ALUMINUM B LADE BUTT. REPLACED PROPELLER ASSEMBLY. (S) 1 H 7 1 3T A37CE 5 C P60GL 20080731 EA 2008 7 31 COMA0860282 1 20080610 A 5320 60034017724 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 7117 DURING HMV-6, EDDY CURRENT INSPECTION FOUND VERTICAL WEB STIFFENER CRACKED ON FWD SIDE OF FS 280, RBL 12, AT AND ABOVE C ABIN FLOOR LINE. REMOVED AND REPLACED DAMAGED ANGLE IN ACCORDANCE WITH SRM 51-42-06 AND 51-42-13. (S) 2 L 7 2 4F RT A21EA 20080731 SO 2008 7 31 CHQA200800118 1 20080619 A 3397 860CC01 CONTACTOR EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL EMERGENCY LIGHTS FAULTY A CHQA O OTHER O OTHER CL CLIMB 1 GL 11 272SK 145306 CAE311940 FLIGHT 6312, CVG TO FWA. WHILE CLIMBING THROUGH 1,000 FT, AN EMERGENCY LIGHTS NOT ARMED WAS DISPLAYED. THE EMERGENCY L IGHTS WERE RESET AND LIGHTS CAME BACK ON ALONG WITH AN ELECTRICAL EMERGENCY ABNORMAL MESSAGE. THE ELECTRICAL PAGE ON TH E MFD SHOWED NORMAL LOADS AND VOLTAGE. THE QRH WAS COMPLIED WITH AND THE ACFT RETURNED TO CVG. MAINTENANCE FOUND NO ME SSAGES ON THE CMC AND TROUBLESHOT THE FAULT TO THE ESSENTIAL BUSS CONTACTORS. BOTH K0079 AND K0080 WERE REPLACED. (S) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080731 EA 2008 7 31 COMA0860308 1 20080626 A 2750 601R93106107 DRIVE SHAFT CNDAIR CL600 CL6002B19 1900309 EA LT WING TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 514CA 7809 RECEIVED FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LT WING NR 1 FLAP FLEX S HAFT. NO FURTHER DEFECTS. (S) 2 L 7 2 4F RT A21EA 20080731 SO 2008 7 31 C2XA08SH083 1 20080611 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 SHV - DURING C-CHECK IT WAS FOUND THAT THE LT OMEGA SHAPE WAS CORRODED AT FRAME 20. MAINTENANCE REMOVED THE CORROSION A ND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080731 EA 2008 7 31 COMA0860276 1 20080609 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 713CA 20957 7245 ON APPROACH INTO CVG DURING GEAR DOWN SELECTION RECEIVED GEAR DISAGREE MSG, EXECUTED MISAPPROACH. RAN QRH SECOND GEAR D OWN SELECTION WAS SUCCESSFUL. ACFT LANDED SAFELY IN CVG. REMOVED AND REPLACED NLG PRIORITY VALVE. (S) 2 L 7 2 4F RT A21EA 20080731 SO 2008 7 31 C2XA08RI083 1 20080612 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14143 145739 FLIGHT 2484 - EWR - FLIGHT CREW REPORTED ELECTRICAL ODOR IN CABIN. EWR MAINTENANCE PERFORMED OPERATIONAL CHECK OF ELECT RICAL SYSTEM AND COULD NOT DUPLICATE THE DISCREPANCY, SYSTEM WORKING PROPERLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080731 SO 2008 7 31 C2X2008F00002 1 20080608 A 3350 AD20131A BATTERY EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS DISCHARGED A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 16944 145045 EMERGENCY LIGHTING OVERHEAD AND FLOOR BY EMERGENCY EXITS ARE DIM. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY IAW EMB14 5 AMM 33-50-04. OPS CHECK GOOD. (S) 2 L 7 2 4F RT T00011AT 20080731 NM 2008 7 31 SAJ2008F00000 1 20080612 A 5313 STRINGER BOEING 747 747400 13848AT NM PWA 4056 PW4056 NE BS 1840-1920 CORRODED W SAJF K NONE O OTHER IN INSP/MAINT 1 WP 03 168CL 29906 DURING 8C CHECK, N168CL AFT CARGO BAY BILGE AREA STRINGER S50R WAS FOUND CORRODED, AT STA 1840, STA 1860, STA 1880, STA 1920. (S) 2 L 7 4 4F 4 F RT A20WE E24NE 20080731 SO 2008 7 31 C2XA08ON134 1 20080609 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 14907 16347 12471 145468 FLT 7668 - ONT - FLIGHT CREW REPORTED RT EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED RT LOWER EMERGENCY LIGHT BULB. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080729 NE 2008 7 29 USAABB08111 2 20080628 A 7310 PRESSURE SWITCH BOEING 767 7672B7ER 1385107 NM GE CF6 CF680C2B2 30025 NE RT ENGINE FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 256AY 26847 PHL FLT 710 EN ROUTE PHL TO ZRH. THE FLIGHT RETURNED TO FIELD DUE TO A NR 2 ENGINE FUEL FILTER MESSAGE. THE FLIGHT LAN DED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENG FUEL PRESSURE SWITCH. OPERATIONAL AND LEAK CHECKS OK. (S) 2 L 7 2 4F 4 F RT A1NM E13NE 20080729 NM 2008 7 29 USAA920081282 1 20080628 A 5712 RIB BOEING 737 737401 1384701 NM RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT - Q3- MAJOR REPAIR - CRACK RT WING TANK RIB AT WBL 135 WING ROOT. REPAIRED RT WING TANK RIB AT WBL 135 IAW EA 10054 6. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081304 1 20080529 A 5210 BOLT BOEING 737 7373S3 1384711 NM PAX DOOR WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW 23713 CLT - C22 - EES - FORWARD ENTRY DOOR POPS AND BINDS DURING OPERATION. REMOVED AND REPLACED WORN UPPER AND LOWER HINGE B OLTS. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843131 1 20080507 A 5311 90526911 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 RIGHT FRAME AT STA 787 CRACKED AT PSU RAIL BRACKET. REPAIRED PER EA 5310 02797. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800625 1 20080513 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 836AS 7263 LT MIDDLE EXTERIOR EMERGENCY LIGHT INOP RELAMPED LT MIDDLE EXTERIOR EMERGENCY LIGHT PER CRJ 200 AMM 33-51-21. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 ASAA0843162 1 20080506 A 5320 652072629 SILL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 FORWARD CARGO BAY DOOR SILL PLATE CORRODED. REPLACED SILL PLATE PER SRM 51 40 05. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843129 1 20080501 A 5754 65C26602302 SLAT BOEING 737 7374Q8 138447Q NM NR 5 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 NR 5 SLAT INBOARD END FOUND DELAMINATION. NR 5 SLAT INBOARDD END REPAIRED IAW B737 400 SRM CH 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20080730 EA 2008 7 30 REX2008F00003 1 20080701 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA LEFT SMOKE A REXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 25 8409N 8577 1607 7409 CAPTAIN REPORTS WHEN LEFT AIR CYCLE MACHINE (ACM) IS TURNED ON COCKPIT STARTED TO FILL WITH SMOKE. MAINTENANCE DISPATCH , PERFORMED ENG RUNS AND VERIFIED LT ACM FAILURE CAUSING SMOKE. LT ACM DEFERRED PER MEL 21-51-11. (S) 2 L 7 2 4F RT A21EA 20080730 NE 2008 7 30 COEA0802816 2 20080617 A 7200 3247600 ENGINE AEROSP ATR72 ATR72212 8680945 EU PWA PW120 PW127 NE RIGHT FAILED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 816FX 21765 347 127010 ENG FAILURE: DURING WALK AROUND BETWEEN FLIGHTS, THE FLIGHT CREW NOTICED THAT THE RT PROP WAS HARD TO SPIN. A CLOSER L OOK AT THE ENGINE DISCOVERED FINE PIECES OF METAL IN THE TAIL PIPE. REMOVED AND REPLACED THE RT ENG. (S) 2 H 7 2 4T 4 T RT A53EU E20NE 20080730 EU 2008 7 30 COEA0801919 1 20080604 A 2460 1050032 BPCU AEROSP ATR42 ATR42300 8680920 EU INTERMITTENT A COEA O OTHER H ELECT. POWER LOSS-50 PC CL CLIMB 1 NM 13 919FX 1026 266 AIR TURNBACK, FLT 7202 SEA TO JUN. UPON ROTATION AND DURING INITIAL CLIMBOUT THE AIRCRAFT APPEARED TO SHED AND REGAIN M ULTIPLE DC BUSSES. LOUD RELAY ACTION COULD BE HEARD FROM THE ELECTRICAL PANEL. THIS LASTED FOR 30 TO 45 SECONDS THEN A LL SYSTEMS RETURNED TO NORMAL. REMOVED AND REPLACED THE DC BUSS POWER CONTROL UNIT (BPCU). (S) 2 H 7 2 4T RT A53EU 20080730 EA 2008 7 30 COMA0860304 1 20080621 A 5297 601R578951 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 810CA 7370 EN ROUTE FROM DCA TO CVG ACFT WOULD NOT PRESSURIZE, ALSO RECEIVED OVBD COOL CAUTION MSG. EMERGENCY DECLARED, ACFT DIVER TED TO IAD AND LANDED SAFELY. REMOVED AND REPLACED PAX DOOR WIRE HARNESS. (S) 2 L 7 2 4F RT A21EA 20080730 NM 2008 7 30 CALA0800700 1 20080703 A 5330 65C27755 SKIN BOEING 737 7373T0 1384582 NM BS 967 S27L CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69348 23586 GENERATED DIP DUE TO HEAVY CORROSION AT STATION 967, STR 27LT TO STR 27RT, PERFORM A PERMANET REPAIR PER EC/RA 5331-0124 4 WITHIN 6,000 FLIGHT CYCLES OR 24 MONTHS, WHICHEVER OCCURS FIRST. DURING OPEN-UP FOUND MORE CORROSION, REMOVED EXISTIN G REPAIRS AND REPAIRED PER EC/RA 5330-03827. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800688 1 20080707 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 787 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 RIGHT STATION 787 FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. CUT OUT DAMAGE AT S TATION 787 BETWEEN S-8 AND S-9, REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080730 WP 2008 7 30 WRLA2008052 1 20080606 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 1967 CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 14075 46922 DURING INSPECTION, MAINTENANCE FOUND AFT FUSELAGE WASTE TANK COMPARTMENT CORROSION ON FRAME LOWER LEG 1967 LBL 6-10. RE PAIRED IAW SRM 63-30-00 FIG 9 & 10 VOL 1. (S) 2 L 7 3 4F A22WE 20080730 EU 2008 7 30 COEA0806911 1 20080529 A 5340 S53172218213 ANGLE AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 911FX 33406 045 FOUND DURING HEAVY CHECK AT COE. FOUND LEVEL 2 CORROSION ON FLOORBEAM 12 REINFORCEMENT ANGLE FOR ENGINE CABLE QUADRANT ABOVE STRINGER 20R HAS EXFOLIATION. REMOVED CORRODED ANGLE, MADE AND INSTALLED REPLACEMENT ANGLE. (S) 2 H 7 2 4T RT A53EU 20080730 EA 2008 7 30 REX2008F00008 1 20080705 A 2421 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 MALFUNCTIONED A REXA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 25 8458A 7458 ON CLIMBOUT OF KDSM, IDG2 CAUTION MESSAGE ILLUMINATED, FOLLOWED ONE MINUTE LATER BY THE GEN 2 CAUTION MESSAGE. THE FLIG HT CREW PERFORMED THE QRH AND REQUESTED TO LAND AT MSP. PERMISSION WAS GRANTED TO DIVERT TO KMSP. EN ROUTE TO KMSP THE APU OIL TEMP CAUTION ILLUMINATED. DUE TO THE FACT THE AIRCRAFT WAS DOWN TO TWO GENERATORS AND HAD AN APU OIL TEMP CAUT ION, THE FLIGHT CREW DECLARED AN EMERGENCY AND REQUESTED CFR ASSISTANCE. AN OTHERWISE NORMAL APPROACH AND LANDING WAS M ADE AT KMSP. THE F/O SECURED THE APU ON LANDING ROLL OUT. MAINTENANCE REPLACED IDG 2 AND FOUND THE APU OIL LEVEL LOW. THE APU OIL WAS SERVICED AND THE ACFT WAS GROUND RUN AND RELEASED FOR SERVICE. (S) 2 L 7 2 4F RT A21EA 20080730 NM 2008 7 30 SWAA083989 1 20080720 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 400 S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA084000 1 20080717 A 5330 6545777 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080730 SO 2008 7 30 SIM2008F00008 1 20080702 A 3260 852701 PROXIMITY SENSOR EMB 135 EMB135LR 3260305 SO LT MLG MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 701MH 145162 ON FLIGHT 4834 CREW REPORTED ON TAKEOFF THAT THE LT LANDING GEAR WOULD NOT RETRACT. CAPTAIN ELECTED TO RETURN TO FIELD. ACFT REMOVED FROM SERVICE. PERFORMED CMC DOWNLOAD REMOVED AND REPLACED LANDING GEAR NR1 DOWN LOCK (A) PROXIMITY SWITC H IAW EMB AMM 32-61-02. OPERATIONAL CHECK GOOD. ACFT RETURNED TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080730 EA 2008 7 30 REX2008F00012 1 20080626 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OPEN A REXA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SO 25 8554A 7554 PASSENGER DOOR MASTER WARNING DURING CLIMB. FOLLOWED QRH AND DECLARED AN EMERGENCY. NO LOSS IN CABIN PRESSURE AND DOOR REMAINED CLOSED. LANDING WAS UNEVENTFUL. EXTERIOR HANDLE APPEARED TO BE OPEN SLIGHTLY AS STATED BY EMERGENCY PERSONNE L (CFR). MAINTENANCE INSPECTED DOOR, SEAL AND STRIKER WITH NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK OF DOOR AND B OTH INNER AND OUTER DOOR HANDLES WITH NO DEFECTS NOTED. (S) 2 L 7 2 4F RT A21EA 20080730 EA 2008 7 30 REX2008F00009 1 20080617 A 2750 860D10018AB2D FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 8694A 7694 FLAP FAILURE MESSAGE ON TAKEOFF, QRH FOLLOWED, DECLARED EMERGENCY AND RETURNED TO THE AIRPORT. MAINTENANCE INSPECTED FL AP CONTROL SYSTEM AND FOUND A FAILURE WITH THE FLAP ELECTRONIC CONTROL UNIT (FECU). FECU REPLACED PER BOMBARDIER AMM 27 -50-00. (S) 2 L 7 2 4F RT A21EA 20080730 NM 2008 7 30 SWAA084011 1 20080719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 520 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080730 EA 2008 7 30 VNAA0804010 1 20080412 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE FUSELAGE DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 709PS 10165 CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE PERFORMED AN EN ROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. MAINTE NANCE FOUND DAMAGE TO THE NR 2 VHF ANTENNA AND SEVERAL RIVETS. MAINTENANCE REPAIRED ALL DAMAGE IN ACCORDANCE WITH THE S TRUCTURAL REPAIR MANUAL. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E00063EN 20080730 NM 2008 7 30 SWAA084060 1 20080719 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 282WN 32534 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA084061 1 20080721 A 3350 MS157721 LAMP BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 MWEA080084 1 20080608 A 5330 2024T3 SKIN DOUG MD88 MD88 3023688 NM BS 392-453 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 701ME 49760 ACFT HAS EXTERIOR SKIN DAMAGE AND POSSIBLE FRAME AND LONGERON AT STATION 392-453, 3 INCHES ABOVE LONGERON 26L. FABRICAT ED AND INSTALLED DOUBLER. (S) 2 L 7 2 4F RT A6WE 20080730 NM 2008 7 30 SWAA083993 1 20080720 A 5311 6545874 FRAME BOEING 737 7373H4 1384600 NM BS 291 S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STUB FRAME CRACKED AT BS 291, STR 18R. REMOVED AND REPLACED STUB FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083983 1 20080716 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 510 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA084016 1 20080719 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM EMERGENCY EXIT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 AFT CABIN EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA084018 1 20080720 A 3350 1619 LAMP BOEING 737 7373K2 13844BA NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800663 1 20080702 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM BS 360 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 LEFT SIDE STATION 360 FRAME BETWEEN S-8 AND S-9 AIR CONDITIONING (A/C) BRACKET MOUNT HOLE CRACKED. REPAIRED FRAME AT BO DY STATION 360 BETWEEN S-8 AND S-9 PER EA 624-53-002CAL AND EC/RA 5310-04793. 2 L 7 2 4F RT A16WE 20080730 EA 2008 7 30 VNAA0806007 1 20080611 A 3234 7455025 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE MLG FAILED A VNAA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 GL 05 246PS 113 7920 CREW REPORTED THE LANDING GEAR DID NOT EXTEND WITH THE LANDING GEAR HANDLE. CREW MANUALLY EXTENDED THE GEAR. THE CREW DECLARED AN EMERGENCY AND LANDED IN CAK WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL HAN DLE IN ACCORDANCE WITH THE ACFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE GOOD AT THIS TIME. ACFT WAS RELEASED FOR S ERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080730 NM 2008 7 30 SWAA083891 1 20080714 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM BS 291 S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 291, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083890 1 20080714 A 5340 65C27314 STRINGER CLIP BOEING 737 7373K2 13844BA NM BS 274 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 274, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083897 1 20080714 A 3397 L1065 TERMINAL BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 DEF. FOUND LOOSE TERMINAL. SECURED TERMI NAL PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083896 1 20080714 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 360 S28L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 28L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080730 2008 7 30 SWAA083921 4 20080715 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083898 1 20080714 A 3397 W4142001220 WIRE BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 2 ABC. FOUND LOOSE WIRE. SECURED WIRE PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083903 1 20080714 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083869 1 20080712 A 3350 65C32046 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 L1 DOOR EMERGENCY EXIT LOWER LIGHT LOOSE. SECURED LIGHT PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083905 1 20080710 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW BN838 28401 DURING SCHEDULED MV1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP P ER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA084017 1 20080720 A 3350 1619 LAMP BOEING 737 7373K2 13844BA NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083874 1 20080712 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 728SW 27860 R2 DOOR EMERGENCY EXIT LIGHT CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080730 2008 7 30 SWAA083929 4 20080714 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 916WN 36623 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 2008UALA03579 1 20080625 A 2421 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT MALFUNCTIONED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 597UA 28750 THE L GEN DRIVE LT ILLUMINATED AT APPLICATION OF TAKEOFF THRUST. PROBLEM IDG (CHRONIC) UNIT WAS INSTALLED ON A/C ON 6/ 17/08, FAILED AGAIN ON 6/25. LAST SHOP VISIT WAS NFF, BUT REPLACED LOG, C/P SWITCH, AND INPUT SEAL AND FILTER. IDG REM OVED AND TAGGED AND SENT TO SHOP FOR T/S AND REBUILD. NEW IDG INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080730 NM 2008 7 30 2008UALA03589 1 20080625 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 429-434 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 DENT IN EXTERNAL SKIN STA 429 - 434, 6 INCHES BELOW STR 17L. ACCOMPLISHED MAJOR REPAIR AT GSO. EVALUATED DENT AND FOUN D TO BE OUT OF LIMITS PER SRM 53-00-01, DETAIL III - OIL CANNED. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER AND FILLER , INSTALLED PER TIMCO REO-G12367, REV B AND EVA 71697 ON NON ROUTINE 21325. INSP KPAKPO-5189. THIS REPAIR IS AN INTE RNAL DOUBLER AND PER EVA 71697, THIS REPAIR HAS RECEIVED ONLY FIRST STAGE APPROVAL FOR STATIC STRENGTH, 85625 PENDING DA TA ANALYSIS BY BACO PRIOR TO 19JUN09. THE AIRCRAFT WILL BECOME UNAIRWORTHY UNLESS A NEW 8100-9 IS ISSUED PRIOR TO 19J U N09, REF 14 CFR 25.571. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 EU 2008 7 29 USAA920081171 1 20080528 A 5320 D5347172705 BEAM AIRBUS 320 A320232 3930326 EU CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 652AW 0953 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN BEAM, BS 3158 FR 66 - BS 3207 FR 67, -Y1292. REPLACED CABIN BEAM, BS 3158 FR 66 - BS 3207 FR 67, -Y1292 IAW SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080729 EA 2008 7 29 TRAX200800715 1 20080530 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LACK OF LUBE A ASOA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 916EV 7757 EXTERNAL HANDLE ON SERVICE DOOR REQUIRE EXCESSIVE FORCE TO OPEN LUBE SERVICE DOOR HANDLE OPS CHECK GOOD PER 52-40-02. (B) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 COMA0860279 1 20080610 A 2760 SPOILER SYS CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 917CA 7017 EN ROUTE FROM CVG TO YUL RECEIVED SPOILERON, FLT SPOILER CAUTION MSG AND O/B SPOILER FAULT, O/B GROUND SPOILER FAULT MSG . FOLLOWED QRH PROCEDURE MSGS PERSISTED. ACFT LANDED SAFELY IN YUL. RESET SPOILER SYSTEM PER FIM. OPS CHECK GOOD, NO DEFECTS NOTED. (S) 2 L 7 2 4F RT A21EA 20080731 NM 2008 7 31 C8GA200800 1 20080611 A 5415 FITTING BOEING 727 727223 1384074 NM BYPASS SWITCH DAMAGED A C8GA O OTHER O OTHER CL CLIMB 1 SO 29 708AA 22465 FLT 720 FROM TOL TO MCO. DURING CLIMB OPERATION OUT OF TOL THE NR 2 ENG LOW OIL PSI LIGHT ILLUMINATED AND OIL QUANTITY WENT TO EMPTY. THE NR 2 ENGINE WAS SHUT DOWN, AN EMERGENCY WAS DECLARED AND THE ACFT LANDED IN TOL WITHOUT INCIDENT. P OST FLIGHT INSPECTION FOUND OIL FILTER BYPASS SWITCH GEARBOX FITTING AT FAULT. REPAIRED GEARBOX PERFORMED OPS AND LEAK CHECKS GOOD. NO OTHER DEFECTS. ACFT WAS RETURNED TO SERVICE. (S) 2 L 7 3 4F A3WE 20080731 SO 2008 7 31 C2XA08RI082 1 20080604 A 3350 375901 SIGN EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 10156 145786 FLIGHT 2058 - EWR - FLIGHT CREW REPORTED SERVICE DOOR EMERGENCY SIGN INOPERATIVE. EWR MX REMOVED AND REPLACED SERVICE D OOR EMERGENCY EXIT SIGN IAW EMB145 AMM 33-50-09 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETU RN TO SERVICE. (S) 2 L 7 2 4F RT 20080731 SO 2008 7 31 C2XA08ON137 1 20080614 A 2810 FUEL EMB 145 EMB145XR 3260214 SO RIGHT WING LEAKING A C2XA O OTHER K FLUID LOSS CR CRUISE 1 SW 27 12166 11575 6182 14500831 FLT 0222 - TUL - FLIGHT CREW REPORTED RT WING FUEL LEAK. MX PERSONNEL REMOVED AND REPLACED RT WING CONDUIT LINE. OPS A ND LEAK CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4F RT 20080731 NM 2008 7 31 SWAA083972 1 20080717 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 747 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 SWAA083973 1 20080717 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM BS 480 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 SWAA083990 1 20080720 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 CALA0800656 1 20080630 A 5320 65479769 PAN BOEING 737 737524 1384721 NM BS 847-867 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 CORROSION ON FLOOR-PAN AND WEB BETWEEN STATION 847 TO 867 LBL 62.5. REMOVED FLOOR-PAN CORROSION AND WEB BETWEEN STATION 847 TO 867 LBL 62.5 IAW B737 SRM 53-60-13, FIG 1. LOCATED, DRILLED AND INSTALLED NEW WEB IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800786 1 20080613 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 878AS 7590 EMERGENCY LIGHT ON FLIGHT ATTENDANT CLOSET DAMAGED. REMOVED AND REPLACED FLOOR LEVEL EMERGENCY FLOOD LIGHT ASSY ON WARD ROBE IAW AMM 33-51-19. OPS CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080729 CE 2008 7 29 DXTA200803138 1 20080623 A 2400 UNKNOWN CESSNA 560 560XL 2076702 CE CABIN SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 603QS 5605203 FOUND HT030 BREAKER POPPED IN THE "HELL HOLE" WE RESET IT. UPON TURNING ON THE AVIONICS/BATTERY THE FLIGHT DECK FILLED W ITH SMOKE. (B) 2 L 7 2 4F RT A22CE 20080729 EA 2008 7 29 TRAX200800618 1 20080510 A 7930 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA OIL PRESSURE MALFUNCTIONED A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 680BR 7679 OIL PRESSURE INDICATING 156 PSI IN ALL PHASES FROM CLIMB TO SHUTDOWN AT GATE. AIRCRAFT RETURNED TO ATL AFTER T/O---EMER GENCY DECLARED. FLT 4531 DEL 156 MINS REMOVED AND REPLACED RT ENG OIL PRESSURE TRANSDUCER IAW AMM 79-31-03, LEAK AND OP S CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080729 CE 2008 7 29 DXTA200803120 1 20080614 A 3260 INDICATION SYS CESSNA 500 560CESSNA 2076750 CE MLG INOPERATIVE E DXTA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 07 395QS 5600496 LEFT MAIN GEAR LIGHT FAILED TO ILLUMINATE WITH GEAR HANDLE SELECTED DOWN ON LANDING. (B) 2 L 7 2 4F RT A22CE 20080729 NM 2008 7 29 ASAA0843153 1 20080610 A 5755 654645170 PANEL BOEING 737 7374Q8 138447Q NM NR 2 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 NR 2 SPOILER EVIDENCE OF DENT AT I/B LOWER AREA OF ACTUATOR LUG ATTACHMENT. NR 2 SPOILER PANEL REPLACED WITH NEW SERVIC EABLE FLIGHT SPOILER PANEL IAW B737 400 AMM TASK 27 61 11 404 010 PARA F STEPS 1 16. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800653 1 20080516 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS INOPERATIVE A ASOA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 844AS 7317 FLAPS FAILED AT 20 DEGREES DURING APPROACH INTO FSM. REMOVED AND REPLACED RT BPSU IAW AMM 27-51-10 COMPLIED WITH PER SP 607 AND AMM 27-51-10 WORK SATISFACTORY. PERFORMED RIGGING OF SYSTEM. OPS CHECK GOOD ON FLAP SYSTEM AT THIS TIME. (B) 2 L 7 2 4F RT A21EA 20080730 EU 2008 7 30 MAL2008F00008 1 20080618 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 560-686 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422XJ 340B422 CORROSION ON LT INBOARD SEAT TRACK AT STA 560 TO STA 686 AT BL 18.3. BL 18.3 SEAT TRACK AT STA 560 TO STA 686 REPAIRED IAW EO S53077. (S) 2 L 7 2 4T RT A52EU 20080730 NM 2008 7 30 SWAA084004 1 20080718 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 213WN 34217 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA084009 1 20080719 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 286WN 32471 EEPLS LENS CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080730 EA 2008 7 30 REX2008F00006 1 20080705 A 3260 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA NLG FALSE ACTIVATION A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8907A 7907 GEAR DISAGREE MESSAGE (NOSE NOT DOWN AND LOCKED) ON APPROACH, QRH FOLLOWED GEAR LOCKED DOWN. EMERGENCY DECLARED WITH UN EVENTFUL LANDING. TROUBLESHOT SYSTEM IAW MM, GEAR SWINGS PERFORMED WITH NO DEFECTS FOUND. (S) 2 L 7 2 4F RT A21EA 20080730 NM 2008 7 30 CALA0800704 1 20080714 A 5320 BAC1496364 ANGLE BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 FORWARD CARGO LT TRANSITION ANGLE HAS MULTIPLE SPOTS WITH SURFACE CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED S PLICE AND REPAIR PARTS AT FORWARD CARGO TRANSITION ANGLE LEFTHAND SIDE PER SRM 53-30-53. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA084055 1 20080719 A 5311 6546541 FRAME BOEING 737 7373H4 1384600 NM BS 663 S2L-3R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 2L AND STR 3R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080730 EA 2008 7 30 SIM2008F00005 2 20080701 A 7261 23073567 CARBON SEAL EMB 145 EMB145 3260210 SO RROYCE AE3007 AE3007A1 54165 EA LT ENGINE LEAKING A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 611AE 145074 CAE311906 ON FLIGHT 3748, CREW REPORTED ON TAKEOFF GOT AN OIL BURN OR DIRTY SOCK ODOR IN COCKPIT. ODOR DISSIPATED ON CLIMBOUT BET WEEN 10,000 FEET AND 15,000 FEET. NO EMERGENCY DECLARED. ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. ACFT REM OVED FROM SERVICE. ACCOMPLISHED ETN EM 72-034R4 AND REPLACED ZERO CARBON SEAL ON LT ENG. OPERATIONAL CHECK GOOD. NO O DOR IN COCKPIT OR CABIN. ACFT RETURNED TO SERVICE. (S) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080730 NM 2008 7 30 SWAA083894 1 20080714 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800695 1 20080710 A 5320 694147374 INTERCOSTAL BOEING 737 737524 1384721 NM BS 400-420 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 WEB AT STATION 400 TO 420 LBL 27 IS CRACKED IN FORWARD CARGO HOLD. REMOVED WEB AND INSTALLED NEW WEB AT STATION 400 TO 420 LBL 27 PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800697 1 20080710 A 2913 731966 PUMP BOEING 777 777224 1385225 NM HYD SYSTEM LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 77019 7134 583 35547 HYD QUANTITY LOW-C AND RESERVE BRAKES/STRG FOUND C1 ELECTRIC PUMP LEAKING. REMOVED AND REPLACED C1 AS PER 29-11-002-401 . ALSO REMOVED AND REPLACED CASE DRAIN FILTERS AS PER 29-11-41-000-801 ALL OPS CHECKS NORMAL. ROTABLE PARTS CHANGE WAS INDICATED - TT 1312506 S/N OFF 05581 PUMP, HYD ELECT OFF 64-2910-9-0001 5581 ON 64-2910-9-0001 1111. 2 L 7 2 4F RT T00001SE 20080730 NM 2008 7 30 SWAA083868 1 20080714 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 616 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080730 2008 7 30 SWAA083870 4 20080712 A 2565 D31354 SLIDE BOEING 737 7373L9 1384470 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083968 1 20080716 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM BS 887 S21R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 21R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083978 1 20080717 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM BS 907 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080731 EA 2008 7 31 COM2008F00002 1 20080708 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 640 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 7018 DURING FS 640 FRAME INSPECTION FOUND 640 FRAME CRACKED ON LT SIDE AT STRINGER 9 CUTOUT. CUT OUT DAMAGED SECTION OF FRAM E AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH REO 601R-53-61-557. (S) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 COMA0860310 1 20080627 A 3230 750005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 920CA 11947 7022 DURING ORD APPROACH RECEIVED A LANDING GEAR DISAGREE WARNING, CREW DECLARED AN EMERGENCY AND PERFORMED MANUAL EXTENSION. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE MLG SELECTOR VALVE. (S) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 COMA0860292 1 20080616 A 5310 POST CNDAIR CL600 CL6002B19 1900309 EA FS 409 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 7117 DURING HMV-6, EDDY CURRENT INSPECTION FOUND CRACK ON LOWER POST, FS 409+128, LBL 18, OUTBOARD SIDE. CUT OUT DAMAGE AND INSTALLED A DOUBLER IN ACCORDANCE WITH REO 601R-53-41-056 REV E. (S) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 COMA0860306 1 20080626 A 2752 853D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA LT WING TE FLAP BINDING A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 514CA 13270 7809 RECEIVED FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LT WING NR 3 FLAP ACTUAT OR. NO FURTHER DEFECTS. (S) 2 L 7 2 4F RT A21EA 20080731 SO 2008 7 31 C2XA08RI084 1 20080613 A 5210 14533413401 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR UNSECURE A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 14953 24003 17819 145071 FLIGHT 2807 - EWR - FLIGHT CREW REPORTED MAIN CABIN DOOR WOULD NOT OPEN OR CLOSE FROM INSIDE. EWR MAINTENANCE SECURED M AIN CABIN DOOR HANDLE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080731 SO 2008 7 31 CHQA200800122 1 20080623 A 2131 22250N030301 CONTROLLER EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CABIN PRESSURE MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 278SK 7221 7221 145370 CAE311143 FLIGHT 5723, SDF TO IAH. ACFT WOULD NOT PRESSURIZE PROPERLY DURING CLIMB. CABIN ALTITUDE CLIMBED EXCESSIVELY AND CREW RECEIVED CABIN MESSAGE. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAULT TO THE AUTO PRESSURE CONTROLLER. AFTER REPLACEMENT THE PRESSURIZATION SYSTEM OPERATED NORMALLY. (S) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080731 NM 2008 7 31 BJNA080402 1 20080402 A 2730 654997025 ACTUATOR BOEING 737 737400 138449A NM ELEVATOR MALFUNCTIONED A BJNA O OTHER F FLT CONT AFFECTED DE DESCENT 1 WP 11 43XA 10794 24796 STABILIZER TRIM WOULD NOT KEEP UP WITH THE COMMANDED POSITION, ASSOCIATED WITH A STAB OUT OF TRIM ANNUNCIATION. STABILI ZER TRIMMED "UP" OK. REMOVED AND REPLACED STABILIZER JACK SCREW ASSEMBLY. OVERHAUL FOUND - P/N 54032-006 SCREW ASSEMBL Y WORN; P/N 65C34615-1 SLEEVE OUT OF TOLERANCE; P/N 69-44011-8 GEAR OUT OF TOLERANCE; BEARINGS WORN REQUIRED REPLACEMENT ; SPRING OUT OF TOLERANCE. (S) 2 L 7 2 4F RT A16WE 20080731 2008 7 31 SWAA083970 4 20080717 A 2565 65C27093 LIGHT BOEING 737 7373H4 1384600 NM R1 DOOR SLIDE INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED MV4 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 CALA0800657 1 20080630 A 5320 6549573503 SUPPORT ANGLE BOEING 737 737524 1384721 NM BS 559 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 LEFT-HAND RAM AIR DUCT SUPPORT ANGLE IS CRACKED AT STATION 559 + 14". REMOVED CRACKED ANGLE, FABRICATED REPAIR PER DRAW ING 65-49573-504 AND SRM 51-70-13, INSTALLED REPAIR PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 CALA0800658 1 20080701 A 5553 65538343 FITTING BOEING 737 737524 1384721 NM VERTICAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16646 28907 AFT LEFT-HAND OUTBOARD VERTICAL STABILIZER FORWARD FAIL-SAFE LUG INSIDE DIAMETER HAS CORROSION. OVERSIZED BORE TO REMOV E ALL CORROSION DAMAGE, INSPECTED REWORKED AREA, INSTALLED REPAIR BUSHING AND REINSTALLED DRAG ANGLE PER ECRA 5342-01054 . 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 CALA0800661 1 20080624 A 5210 6517688U175 ANGLE BOEING 737 737524 1384721 NM L1 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 SURFACE CORROSION FOUND ON Z-ANGLE AT L1 DOOR. ATTEMPTED TO BLEND CORROSION, BUT DAMAGE FOUND TO BE BEYOND LIMITS OF 73 7-500 SRM 53-10-15, FIGURE 101. REMOVED AND REPLACED L-1 DOOR Z-ANGLE PER 737-500 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080731 SO 2008 7 31 SIM2008F00007 1 20080703 A 5320 14525480 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 689EC 14500853 DURING MBV INSPECTION FOUND CARGO DOOR SILL BETWEEN FRAMES 65-68 TO BE CORRODED. REMOVED AND REPLACED CARGO DOOR SILL I AW EMB SRM 51-40-02. ACFT WAS RETURNED TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080731 EA 2008 7 31 TRAX200800711 1 20080530 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 AFT PRESSURE BULKHEAD, AFT FACE LEFT SIDE CLIP IS CRACKED. JOB COMPLETE REMOVED AND REPLACED LT 625 CLIP IAW SRM 51-42 -21. JOB COMPLETE. DB7020877. (B) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 TRAX200800707 1 20080530 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 473 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 CORROSION DAMAGE ON LT PRESSURE FLOOR SILL FS 473.15 AT RBL 43 (MARKED). REMOVED MINOR SURFACE CORROSION DAMAGE ON PRES SURE FLOOR SILL ASSEMBLY REINFORCING ANGLE AT FS 473.15 AT RBL 43. BLENDED AREA DIMENSIONS ARE 1"X1.5"X.004"MAX DEPTH. MAXIMUM MATERIAL REMOVAL ALLOWED IS .008". BLENDED AREA IS WITHIN LIMITS PER CRJ 200 SRM 53-41-45 FIGURE 101. WORK CO MPLETED. (B) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 TRAX200800709 1 20080530 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 574-589 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 AFT CARGO COMP FLOOR SILL CORRODED LT SIDE BETWEEN FS 574 AND 589 AT LBL 45 (MARKED). REMOVED LIGHT SURFACE CORROSION O N CARGO FLOOR SILL AT FS 574 AND 589 IAW SRM 51-21-06. REMOVED .002 MATERIAL WITHIN LIMITS. ALODINE, PRIMED, AND PAINT ED IAW CRJ 200 SRM 51.00.00. (B) 2 L 7 2 4F RT A21EA 20080731 SO 2008 7 31 C2XA08IA137 1 20080606 A 2530 500064001 COFFEEMAKER EMB 145 EMB145LR 3260212 SO GALLEY BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 13566 9335 9335 145622 IAH - FLIGHT 2504, THE CREW REPORTED A BURNING SMELL IN FRONT OF CABIN. MAINTENANCE INSPECTED THE ACFT AND FOUND THE NR 1 COFFEE BREWER TO BE BURNED UP. MAINTENANCE REMOVED AND REPLACED THE COFFEE BREWER. OPERATIONALLY CHECKED WITH NO DEF ECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080731 NM 2008 7 31 BJNA080501 1 20080526 A 2560 P4010021 BATTERY BOEING 737 737400 138449A NM FLASHLIGHT DISCHARGED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 42XA 25729 FORWARD RT EMERGENCY FLASHLIGHT HAS DEAD BATTERY. REPLACED BATTERY IN THE FORWARD RT EMERGENCY FLASHLIGHT. (S) 2 L 7 2 4F RT A16WE 20080731 EA 2008 7 31 COMA0860307 1 20080626 A 2752 854D10019 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA LT WING TE FLAPS BINDING A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 514CA 13270 7809 RECEIVED FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED LT WING NR 4 FLAP ACTUAT OR. NO FURTHER DEFECTS. (S) 2 L 7 2 4F RT A21EA 20080731 SO 2008 7 31 C2XA08XL069 1 20080612 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 13956 145078 CLE FLIGHT 3060, THE CREW REPORTED THE FORWARD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPAIRED WIRE TO SERVICE DOOR EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4T RT T00011AT 20080731 EA 2008 7 31 COMA0860283 1 20080610 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 640 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 30545 7117 LT FUSELAGE FRAME CRACKED AT FS 640 BETWEEN STRINGERS 9 & 10. PERFORMED MODIFICATION K601R36009-3 AS PER PART C OF SB 6 01R-53-061E. (S) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 CHQA200800113 1 20080615 A 3260 INDICATION SYS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE MLG MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 638BR 7311 E872506 FLIGHT 5534, IAH TO CRP. ON INITIAL CLIMBOUT THE FLIGHT CREW SELECTED THE LANDING GEAR TO THE UP POSITION AND THE NOSE AND RT LANDING GEAR INDICATED UP, BUT THE LT MAIN SHOWED A RED UNSAFE INDICATION. THIS WAS PRECEDED BY A RED DISAGREE M ESSAGE. THE CREW FOLLOWED THE QRH CHECKLISTS, BUT THE INDICATION REMAINED. THE LANDING GEAR WAS THEN SELECTED DOWN AND THE CREW RECEIVED A 3 GREEN INDICATION. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE GEAR AND PERFOR MED SEVERAL SWINGS, BUT COULD NOT DUPLICATE THE FAULT. THE ACFT WAS RETURNED TO SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080731 NM 2008 7 31 2008UALA03612 1 20080626 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 543UA 25698 DOOR 1R & 2R EXTERIOR EMERGENCY LIGHTS INOP. *S/D* LAMPS ARE INOP. REPLACED LAMPS, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080731 NM 2008 7 31 2008UALA03614 1 20080626 A 5420 BUSHING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 PYLON OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NR 1 PYLON INBOARD MID SPAR FITTING BUSHING MIGRATED .035 NO CORROSION OR ROTATION. 2 L 7 2 4F 4 F RT A1NM E24NE 20080731 NM 2008 7 31 2008UALA03622 1 20080627 A 2751 SRDLOC12H TRANSMITTER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE TE FLAPS MALFUNCTIONED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 659UA 27114 FLIGHT CREW REPORT SLIGHT SPLIT BETWEEN LEFT AND RIGHT T/E FLAP INDICATOR NEEDLES NORMAL AT 1 AND 25 BUT SLIGHT SPLIT AT UNITS 5, 10 & 15. REPLACED LEFT FLAP POSITION TRANSMITTER NR 1 PER AMM CH 27-51-45 OP CHECK NORMAL. AC OK FOR SERVICE . 2 L 7 2 4F 4 F RT A1NM E24NE 20080731 NE 2008 7 31 2008UALA03625 2 20080630 A 7261 SCAVENGE PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE OIL SYS MALFUNCTIONED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 29 540UA 25252 726600 NR 2 ENG HIGH OIL TEMPERATURE INDICATION. RTFL. REPLACED LUBE SCAVENGE PUMP AS WELL AS CHECKED ALL WIRING FROM PYLON D OWN ENG. ALSO REPLACED EEC AS PRECUATIONARY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080731 NE 2008 7 31 2008UALA03627 2 20080629 A 7320 EEC BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 29 513UA 24810 726527 NR 2 ENG UNCOMMANDED ROLLBACK FOR 30 SECONDS. RTFL. POSSIBLE INTERNAL EEC ISSUE. REPLACED EEC AND PMA STATOR AS PRECA UTIONARY, NO REPEATS. 2 L 7 2 4F 4 F RT A2NM E17NE 20080731 EU 2008 7 31 COEA0802911 1 20080602 A 5310 S53671259201 CREASE BEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 911FX 045 FOUND DURING HEAVY CHECK AT COE. MAJOR REPAIR: LEVEL 2 CORROSION: THE RT CREASE BEAM BETWEEN FRAMES 35R & 36R HAS ARE AS OF MISSING PAINT & SURFACE CORROSION. FOUND CORROSION BETWEEN WEB DOUBLER PLATE AND CREASE BEAM WEB. REMOVED CORROS ION FROM WEB AND REMOVED & REPLACED WEB DOUBLER ON CREASE BEAM WEB BETWEEN FRAMES 35R & 36R. (S) 2 H 7 2 4T RT A53EU 20080731 EA 2008 7 31 COMA0860298 1 20080622 A 5311 601R3500733 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 640 S9R CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 DURING FS 640 FRAME INSPECTION FOUND 640 FRAME CRACKED ON RT AT STRINGER 9 CUTOUT. REMOVED DAMAGED SECTION OF FRAME FRO M STRINGER 6-20 AND REPLACED WITH SPLICED IN REPAIR FRAME AND BONDED DOUBLER PER, S/B 601R-53-061E PART C. (S) 2 L 7 2 4F RT A21EA 20080731 NM 2008 7 31 CALA0800674 1 20080707 A 5311 6546538 FRAME BOEING 737 737524 1384721 NM BS 597 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 LEFT STATION 597 FRAME CRACKED AT AIR CONDTIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. REMOVED DAMAGE, FABRI CATED AND INSTALLED REPAIR ANGLES AT STATION 597 BETWEEN S-8 AND S-9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080731 EA 2008 7 31 COMA0860300 1 20080620 A 2621 365000183 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA E/E BAY INTERMITTENT A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 713CA 6172 7245 EN ROUTE FROM CLE TO SYR RECEIVED CARGO BOTTLE LOW CAUTION MSG AT 28500, STAYED ON FOR 3 MIN THEN WENT OUT. EMERGENCY D ECLARED, ACFT RETURNED BACK TO CLE AND LANDED SAFELY. REMOVED AND REPLACED CARGO FIRE BOTTLE. (S) 2 L 7 2 4F RT A21EA 20080731 NM 2008 7 31 CALA0800677 1 20080707 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM BS 907 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 LEFT STATION 907 FRAME CRACKED AT AIR CONDTIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. CUT OUT DAMAGE AT FRA ME STATION 907 LEFTHAND BETWEEN S-8 AND S-9, REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 CALA0800679 1 20080707 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM BS 827 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 LEFT STATION 827 L FRAME CRACKED AT AIR CONDTIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. CUT OUT CRACKED SEC TION OF BS 827 FRAME BETWEEN STR 8 LEFT AND STR 9 LEFT AND INSTALLED REPAIR ANGLES IAW EA 5310-04498. 2 L 7 2 4F RT A16WE 20080731 EA 2008 7 31 COMA0860301 1 20080620 A 4990 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA APU LOW A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 430CA 7461 EN ROUTE FROM CVG TO JAX RECEIVED APU OIL TEMP CAUTION MSG. EMERGENCY DECLARED, ACFT DIVERTED TO ATL AND LANDED SAFELY. FOUND APU OIL LEVEL LOW. SERVICED APU OIL TO PROPER LEVEL. NO FURTHER DEFECTS. (S) 2 L 7 2 4F RT A21EA 20080731 NM 2008 7 31 SWAA083784 1 20080708 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500C S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 9L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080731 2008 7 31 YEN2008F00006 4 20080603 A 2330 LSEBUTK1400101 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU ENTERTAIN SYS ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 15 510JB 5276 1280 F/A REPORTED BURNING ODOR AROUND ROW 3, REDUCED AFTER TVS WERE SHUT OFF, TS IAW TSM 24-00-00-810-823 AND NO TROUBLE FOUN D. REMOVED AND REPLACED 3DEF SEB IAW MM 44-20-17, OPS CHECKS GOOD, INSPECTED LIVE TV SYS IAW TSM 23-39-00-810-801, NO F AULTS FOUND. 2 L 7 2 4F RT A28NM 20080729 NE 2008 7 29 DXTA200803107 2 20080608 A 7200 ENGINE CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE RIGHT FLAMED OUT E DXTA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION NR NOT REPORTED 1 GL 07 380QS 6800089 WHILE ADDING POWER AND SIMULTANEOUSLY TURNING FUEL X-FEED OFF, RIGHT ENG FLAMED OUT. ENGINE RELIT VERY FAST. (B) 2 L 7 2 4F 4 F RC T00012WI E35NE 20080729 EA 2008 7 29 TRAX200800645 1 20080515 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 979EV 7737 FWD AND AFT CEILING EMERG. LIGHT OUT RELAMPED FWD AFT CEILING EMERGENCY LIGHT IAW 33-51-16. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAA920081202 1 20080609 A 2560 P207003001 FLASHLIGHT BOEING 737 73733A 1384673 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 166AW 23627 MCN - C21 - EMERGENCY EQUIPMENT - AFT LAV WALL, (IEA) EMERGENCY FLASHLIGHT INOP (BLACK WIRE BROKEN). REPLACED EMERGENCY FLASHLIGHT AND POWER UNIT. OPS CHECK GOOD. (S) 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 MASA200800464 1 20080611 A 5270 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR INTERMITTENT A MASA O OTHER N FALSE WARNING DE DESCENT 1 SW 07 503MJ 10058 ASH 7154 IAH-ORD. SERVICE DOOR CAUTION INTERMITTENT ON DECENT. MX PERFORMED OPS CHECKS AND IT CHECKED GOOD. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 USAA920081264 1 20080615 A 5320 654587547 CUSP WEB BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 MCN - C-21 - MAJOR REPAIR - CORROSION ON LOWER SURFACE OF CUSP WEB AROUND DOME NUT HOLE R1 DOOR SURROUND BS 295 RT. REM OVED CORROSION ON LOWER SURFACE OF CUSP WEB AROUND DOME NUT HOLE; FOUND WEB TO BE CRACKED. REPLACED WEB AT R1 DOOR SURR OUND BS 295 IAW B737 SRM 51-10-02-0G & SRM 51-40-02-0G. (S) 2 L 7 2 4F RT A16WE 20080729 CE 2008 7 29 DXTA200803140 1 20080623 A 3230 LANDING GEAR CESSNA 560 560XL 2076702 CE SLOW E DXTA O OTHER O OTHER AP APPROACH 1 GL 07 687QS 5605187 GEAR HANDLE PLACED IN THE DOWN POSITION ON FINAL APPROACH AND NOTHING HAPPENED FOR 3-5 SECONDS THEN THE GEAR EXTENDED NO RMALLY. (B) 2 L 7 2 4F RT A22CE 20080729 NM 2008 7 29 KCSA081300 1 20080625 A 5311 FRAME BOEING 747 747122 1384872 NM LT WING DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FRAME WEB DAMAGED APPROX 20" FWD OF I/B AILERON AT WBL-445 (B) 2 L 7 4 4F RT A20WE 20080729 NM 2008 7 29 KCSA081311 1 20080705 A 5310 DOOR FRAME BOEING 747 747122 1384872 NM BS 2236 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 RT SIDE FUSELAGE CLOSURE FRAME IS CRACKED 3" AT LOWER FORWARD CORNER OF THE R5 DOOR CUTOUT AT BS 2236, WL 208 (B) 2 L 7 4 4F RT A20WE 20080729 NM 2008 7 29 KCSA081293 1 20080619 A 5315 FLOORBEAM BOEING 747 747122 1384872 NM BS 1265 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 MAIN DECK FLOORBEAM INTERCOSTAL UPPER CHORD CORRODED B.S. 1265, LBL-108 (B) 2 L 7 4 4F RT A20WE 20080729 NM 2008 7 29 USAA920081325 1 20080707 A 5312 BULKHEAD BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 457UW 25021 CLT - FORWARD PRESSURE BULKHEAD - MAJOR REPAIR - CRACK ON WEB AT 178 BULKHEAD WL 226, LBL 17. REPAIRED WEB AT 178 BULKH EAD WL 226, LBL 17 IAW B737 SRM 53-10-08. (S) 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081284 1 20080626 A 5310 143N85111 DOOR FRAME BOEING 757 757225 1384959 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 917UW 22193 PIT - PYLON SHIM - MAJOR REPAIR - FORWARD CARGO DOOR SURROUND STRUCTURE - FWD FRAME WEB CRACKED AT BS 560 S23R. REPAIRE D FORWARD CARGO DOOR SURROUND STRUCTURE - FWD FRAME WEB AT BS 560 S23R IAW EA111264. (S) 2 L 7 2 4F RT A2NM 20080721 NM 2008 7 21 SWAA083789 1 20080709 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 334SW 23938 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 933, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083786 1 20080708 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080718 EA 2008 7 18 OVF2008F00000 2 20080508 A 7414 M3056 BRUSHES SLICK GIPPLD GA8 GA8 3900102 EU LYC O540 IO540K1A5 41532 EA MAGNETO WORN E OVFA O OTHER O OTHER NR NOT REPORTED 1 WP 13 7058M GA805094 THIS IS AN UPDATE OF A SDR FILED 15 APRIL, 2008. MAGNETOS, FUEL PUMP, AND FUEL INJECTOR SERVO WERE SENT TO THE RESPECTIV E OEM`S. MAGNETOS WERE SENT TO MFG FOR ANALYSIS. THEY WERE SENT AS REMOVED TO PRECLUDE ANY FIELD CONTAMINATION. THEY WE RE NOT PRODUCING SPARK DUE TO LARGE AMOUNTS OF CARBON DUST FROM ABNORMAL WEAR AS THE FIRST. DUST CREATES A PATHWAY TO GR OUND EFFECTIVELY SHUTTING DOWN MAGNETOS. SINCE AC/ENGINES/MAGNETOS WERE MFG WITHIN YEAR OF EACH OTHER, AND ALL EXHIBITE D THE SAME WEAR AT SAME HOURS IN SERVICE, WOULD THINK AN EXAMINATION OF MATERIALS/ PROCESS USED TO MFG CARBON BRUSHES DU RING THAT PERIOD WOULD BE APPROPRIATE. (K) 1 H 7 1 3O 3 O NT 1E4 20080718 EU 2008 7 18 M7K2008F00043 1 20080512 A 5302 350A23422220 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 816MH 245 4038 4038 23096 CRACK DISCOVERED DURING ROUTINE INSP ON FITTING FLANGE AND GOING THROUGH AN ATTACHMENT BORE. A NEW FITTING WAS MATCH DR ILLED AND INSTALLED. THIS IS A VERY COMMON PROBLEM FOR THIS PART. SUGGEST THIS PART BE MFG FROM A MORE DURABLE MATERIAL SUCH AS TITANIUM OR SS. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080721 NM 2008 7 21 SWAA083502 1 20080625 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 YEN2008F00000 1 20080630 A 2752 C1558151 ACTUATOR EMB ERJ190 ERJ190100IGW 3260408 NM TE FLAPS TRIPPED A YENA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 15 203JB 6470 19000023 ON APPROACH, AT 210KIAS FLAPS PLACED TO FLAP 1, FLAP FAIL EICAS MSG, FOLLOWED QRH PROCEDURES FINAL FLAP CONFIGURATION, 0 SLAT 0 FLAP, ORIGINALLY SLATS 3 ONLY AND FLAPS 0. REMOVED AND REPLACED RT IB FLAP OB ACTUATOR IAW MM 27-51-01. OPS CHE CK OK. 2 L 7 2 4F RT A57NM 20080731 NM 2008 7 31 YEN2008F00001 1 20080630 A 2752 C155815 ACTUATOR EMB ERJ190 ERJ190100IGW 3260408 NM TE FLAPS TRIPPED A YENA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 15 203JB 6470 19000023 ON APPROACH, FLAPS PLACED TO FLAP 1, FLAP FAIL EICAS MSG. FOLLOWED QRH PROCEDURES, FINAL FLAP CONFIGURATION, 0 SLAT, 0 FLAP, ORIGINALLY SLATS 3 ONL AND FLAPS 0. REMOVED AND REPLACED RT IB FLAP OB ACTUATOR (NR 2 RT)IAW MM 27-51-01. OPS C HECK OK. (K) 2 L 7 2 4F RT A57NM 20080731 EU 2008 7 31 YEN2008F00007 1 20080604 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 621JB 2491 IN CRUISE, BURNING RUBBER TYPE ODOR IN AREA OF ROWS 18 TO 21, AFTER TURNING OFF LTV ODOR WENT AWAY, C/W TSM 23-39-810-80 1. NO LTV DISCREPANCIES NOTED, OP CHECK OF LTV SYS NML IAW MM 23-39-00. (K) 2 L 7 2 4F RT A28NM 20080731 SO 2008 7 31 GLB2008F00006 1 20080611 A 5730 PANEL EMB 120 EMB120ER 3260203 SO LT WING LOOSE A GLBA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 21 71GL 120071 ENROUTE, THE PILOTS REPORTED THAT A LARGE FUEL LEAK WAS OBSERVED IN FLIGHT FROM THE LT FUEL TANK. 300 POUNDS OF FUEL LO ST IN ONE HOUR OF FLIGHT. MAINTENANCE RETORQUED SCREW ON AFFECTED WING PANELS IAW MM 28-10-00. LEAK CHECK WAS GOOD. ( K) 2 L 7 2 4T RT A31SO 20080731 EU 2008 7 31 YEN2008F00011 1 20080623 A 3350 321431 BATTERY PACK AIRBUS 320 A320232 3930326 EU EMERGENCY LIGHT DISCHARGED A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 556JB 1904 ON MAINTENANCE INSP LT EMERGENCY EXIT EPSU BATTERY FAIL TEST, REMOVED AND REPLACED LT EMERGENCY EXIT EPSU BATTERY OPS CH ECK NORMAL IAW 33-51-00. (K) 2 L 7 2 4F RT A28NM 20080731 CE 2008 7 31 MTN2008F00003 1 20080617 A 3411 PITOT TUBE CESSNA 208 208B 2073701 CE CONTAMINATED E MTNA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 EA 68 874FE 208B0205 ON TAKEOFF, THE PILOTS AIRSPEED INDICATOR SHOWED ZERO KNOTS. THE TAKEOFF WAS ABORTED AND THE AC RETURNED TO THE RAMP. AFTER TROUBLESHOOTING, MAINT REMOVED INSECT DEBRIS FROM THE PITOT TUBE THE SYSTEM CHECKED GOOD AND THE AC WAS RETURNED T O SERVICE. (K) 1 H 7 1 3T A37CE 20080731 EU 2008 7 31 SIM2008F00011 1 20080711 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 219AE 340B219 ON FLIGHT 3846 CREW NOTED A BURNING ODOR IN COCKPIT AND FWD PART OF CABIN. AC REMOVED FROM SERVICE. PERFORMED INSP OF AV IONICS RACK DOOR. RUN ENGINES TURN ON AIR CONDITIONING SYS, NO BURNING ODOR NOTED IAW AMM 05-50-00. AC RETURNED TO SER VICE. (K) 2 L 7 2 4T RT A52EU 20080731 NM 2008 7 31 C8G2008F00002 1 20080611 A 7722 152BL801E INDICATOR BOEING 727 727225 1384077 NM NR 2 ENG EGT INOPERATIVE A C8GA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 29 801EA 22432 DURING TAKEOFF ROLL, THE NR 2 EGT INDICATOR WENT TO ZERO INDICATION. THE TAKEOFF WAS ABORTED AND THE AC RETURNED TO THE BLOCKS WITHOUT INCIDENT. POST FLIGHT INSP REVEALED THE NR 2 ENGINE EGT INDICATOR WAS AT FAULT. THE NR 2 EGT INDICATOR WAS REMOVED AND REPLACED, OPS CHECK GOOD. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F A3WE 20080801 NM 2008 8 1 2008UALA03101 1 20080529 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN INTERMITTENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 669UA 30025 EMERGENCY EXIT PATH LIGHTS & EXIT SIGNS IN LEFT SIDE OF 1ST CLASS ILLUMINATED INTERMITTENLY. AFTER TROUBLE SHOOTING COU LD NOT DUPLICATE PROBLEM. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080801 NM 2008 8 1 2008UALA03102 1 20080529 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ROW 23 AFT INTERMITTENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 EXIT LIGHTS 23-AFT ON OFF UNCOMMANDED. AFTER TROUBLE SHOOTING UNABLE TO DUPLICATE PROBLEM. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080801 NM 2008 8 1 08FDEA01888 1 20080520 A 5753 ARC24442 SKIN DOUG MD11 MD11F 3023600 NM RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 590FE 48505 RT WING INBD FLAP LOWER SURFACE FOUND WITH 3 DENT MARKS AT XIFH 249. DENTS ON RIGHT HAND WING INBD FLAP LOWER SURFACE AT XIFH 249 MEASURED AND FOUND OUT OF LIMITS AS PER SRM 57-10-00 FIGURE 17 VOLUME I. REPAIR CARRIED OUT AS PER SRM 57- 10-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080801 NM 2008 8 1 08FDEA02375 1 20080622 A 5343 AEA7051501 TRUNNION DOUG MD11 MD11 3023602 NM ZONE 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 598FE 48597 DURING CENTER LANDING GEAR REMOVAL FOR REPLACEMENT, THE RIGHT TRUNNION FITTING AFT ATTACHMENT BOLT HOLE FOUND CORRODED . REPAIR CARRIED OUT AS PER EA 1-5310-122488, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080801 NM 2008 8 1 08FDEA02050 1 20080530 A 5100 NONE BOEING 757 75723A 1384967 NM IAW SRM NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 919FD 24636 UNRECORDED PREVIOUS REPAIR FOUND ON RT APU COWLING LOCATED AT MIDDLE HINGE. REPAIR TO BE EVALUATED. EXISTING REPAIR FO UND TO BE IAW B757-200 SRM 52-40-01 FIG 201, REPAIR 5, BASED ON EXTERNAL VISUAL EVALUATION ON THE SHAPE, LOCATION, SIZE, MATERIAL THICKNESS, TYPE AND GENERAL WORKMANSHIP OF THE REPAIR. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA . NOT AN SDR. 2 L 7 2 4F RT A2NM 20080801 NE 2008 8 1 08FDEA02452 2 20080625 A 7321 NAS110412 BOLT BOEING 727 727227 1384078 NM PWA JT8 JT8D15 52051 NE FUEL CONTROL DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 NR 3 ENGINE STARTER CONTROL ROD INBD OF ENGINE, NUT HAS NO THREADS SHOWING AND SPRING CLIP NOT BENT OVER BOLT HEAD. PROP ERLY INSTALLED NR 3 ENG START CONTROL ROD (UPPER) BOLT AND ATTACHING HARDWARE IAW FX MM 76-11-021-2. 2 L 7 3 4F 4 F A3WE E2EA 20080801 EU 2008 8 1 08FDEA02058 1 20080521 A 5347 A5361252420000 SEAT TRACK AIRBUS 300 A300B4622R 3930312 EU N/A CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 CABIN - FLOOR - SEAT-TRACK Y953 WITH CORROSION NEXT TO FRAME 15A. REPLACED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080801 NM 2008 8 1 CALA08FA001 1 20080620 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 787 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16646 28907 FRAME STATION 787 LEFT CRACKED BETWEEN S8 AND S9 AFT SIDE OF AIRCONDITIONING (A/C) OUTLET ASSEMBLY SUPPORT BRACKET. REPA IRED FRAME PER EA 5310-04498 OP 2. 2 L 7 2 4F RT A16WE 20080721 2008 7 21 SWAA083528 4 20080625 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED RON CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083620 1 20080630 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 372SW 26599 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083635 1 20080701 A 3230 654623014 DRAG BRACE BOEING 737 7375H4 138449D NM NLG VIBRATION A SWAA K NONE E VIBRATION/BUFFET CL CLIMB 1 SW 29 522SW 26564 DURING CLIMB WHEN RAISING NLG EXCESSIVE VIBRATION FELT. REMOVED AND REPLACED LOWER DRAG BRACE PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083636 1 20080701 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 764, STR 25L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083808 1 20080713 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 EA 2008 7 21 A6WA200840343 1 20080412 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 443AW 7781 CRACK FOUND ON FRAME 280, LBL 9 WL 73.00. - - FRAME AT FS 280 LBL 9 WL 73.00 REPAIRED IAW REO 601R-53-11-171 REV "D" SC HEME B. . 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA20840275 1 20080331 A 3240 BRAKE CNDAIR CL600 CL6002B19 1900309 EA MLG CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 13 401AW 7280 CRACK FOUND AROUND PARKING BRAKE AT FS 202.75. - - PARKING BRAKE AT FS 202.75 REPAIRED IAW REO 601R-53-11-563. . 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840420 1 20080514 A 5320 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA BS 574 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 442AW 7778 CHANNEL ON CARGO DOOR SUPPORT STRUCTURE CRACKED AT FS 574. CHANNEL ON CARGO DOOR SUPPORT STRUCTURE AT FS 574 REPLACED I AW SRM 51-42-06. 2 L 7 2 4F RT A21EA 20080721 EA 2008 7 21 A6WA200840372 1 20080430 A 5313 LONGERON CNDAIR CL600 CL6002B19 1900309 EA BS 319-345 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 CORROSION EXISTS ON LOWER SILL LONGERON OF PAX DOOR FS 319 TO 345. CORROSION REMOVED ON LOWER SILL LONGERON OF PAX DOOR FS 319 TO 345 IAW SRM 51-21-06. 2 L 7 2 4F RT A21EA 20080721 EU 2008 7 21 08FDEA02544 1 20080627 A 5321 B5327028000200 FLOOR PANEL AIRBUS 300 A300B4605R 3930308 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 251 XG IS CRACKED & CRUSHED. FABBED A NEW FLOOR PANEL; POTTED EDGES; CURED; SANDED; POTT ED INSERTS; APPLIED NON-SKID & PART MARKED IAW DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080721 2008 7 21 SWAA083792 4 20080709 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULE HC2 CHECK, FOUND L1 DOOR EVAC SLIDE OUT OF POSITION. ADJUSTED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 20080721 EU 2008 7 21 08FDEA02952 1 20080717 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD FH1126 630 DURING ACCOMPLISHMENT OF EO 6-5750-7-5000 PT.3 FOUND DAMAGED HOLE ON LT INBOARD FLAP TOP SKIN NEAR RIB 7. REPAIR PERFORM ED BY REAM UP THE HOLE TO DIAMETER 0.1865 -0.1895 INCH , INSPECT THE HOLE BY NDT AND INSTALL HL11VF-6 IAW RAS /FOK/165/2 008 ISS.A, APPROVED BY EA 6-5752-123015. 2 L 7 2 4F RT A35EU 20080721 NM 2008 7 21 SWAA083773 1 20080709 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 9R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083776 1 20080708 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083780 1 20080708 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 9L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 2008 7 21 SWAA083791 4 20080708 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 256WN 32514 R2 DOOR EVAC SLIDE LOOSE. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 20080804 WP 2008 8 4 08FDEA02550 1 20080627 A 5347 ACA73993 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 MAIN CABIN SEAT TRACK LOBE IS BROKEN OUT AT FS 755; LBL 48. REPLACED THE MAIN CABIN SEAT TRACK FROM STATIONS 675 TO 760 ; LBL 48 IAW SRM 53-70-00; VOL I; PG 3. INSTALLED 4 FLOORBOARDS AT STATIONS 675-765; LBL 27-48; STATIONS 675-835; LBL 48-76 IAW SRM 51-31-01; VOL II; PG 1. 2 L 7 3 4F RT A22WE 20080804 NM 2008 8 4 08FDEA02570 1 20080630 A 5310 655853631 CREASE BEAM BOEING 727 727225 1384077 NM BS 640-660 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 FUSELAGE CREASE BEAM WEB CRACKED, STR17L, BS-640-660 FABRICATED NEW CREASE BEAM WEB PER SAMPLE AND BOEING DWG NR 65-5853 6. TRANSFERED NEW FASTENER HOLES REF, SRM 51-30-2, PG 1-10. TREATED AND PRIMED WEB, REF: SRM 51-10-2, PG 1-2. WEB BE INSTALLED ON NR N00796, JPF LINE ITEM 2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080804 SO 2008 8 4 LR7A08086 1 20080701 A 5312 3425828R BULKHEAD LKHEED 382 382G 526414U SO FS 880 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 636 4763 DURING SCHEDULED B-2 CHECK, PER JOB CARD HB5302, FOUND RT AFT FUSELAGE INTERIOR LOWER BULKHEAD WEB CRACKED THROUGH FASTE NER HOLE AT FS 880R, WL 200. REPAIR IAW DRAWING 342582 BY FABRICATING AND INSTALLING WEB. 2 H 7 4 4T A1SO 20080730 EU 2008 7 30 MAL2008F00007 1 20080618 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 622-658 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422XJ 340B422 CORROSION ON CENTER SEAT TRACK AT STA 622 TO STA 658 AT BL 0. BL 0 SEAT TRACK AT STA 622 TO STA 658 REPAIRED IAW EO S53 342. (S) 2 L 7 2 4T RT A52EU 20080730 NM 2008 7 30 SWAA084056 1 20080719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 787 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080730 EU 2008 7 30 MAL2008F00000 1 20080613 A 5311 FRAME SAAB SF340 340B 7860101 EU BS 272 DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422XJ 340B422 REPAIR AT STA 272 ON RT UPPER FRAME IN ACCORDANCE WITH EO S53108 & SRM 53-70-30. REPAIRED THE DAMAGE IAW EO S53108. (S ) 2 L 7 2 4T RT A52EU 20080730 NM 2008 7 30 SWAA083893 1 20080714 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 352SW 24888 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083901 1 20080714 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 277 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083865 1 20080714 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 EA 2008 7 30 VNAA0806008 1 20080613 A 5710 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT WING DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 226JS 7895 CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE COMPLIED WITH AN EN ROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. MA INTENANCE FOUND DAMAGE TO THE LT AND RT WINGTIPS. MAINTENANCE REPAIRED THE DAMAGE UNDER REO 601R-57-30-001 AND THE STRU CTURAL REPAIR MANUAL. NO OTHER DEFECTS NOTED AT THIS TIME. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080730 NM 2008 7 30 SWAA083698 1 20080704 A 5330 6545877 SKIN BOEING 737 7373H4 1384600 NM BS 291 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR FUSELAGE SKIN CUTOUT CRACKED AT BS 291.50, WL 233.50. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083971 1 20080717 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 500C S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 HNAA0800193 1 20080610 A 3350 6104789 BATTERY DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS DISCHARGED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 935HA 50562 142 RT EGRESS LIGHT IN INOPERATIVE FORWARD. REMOVED AND REPLACED EMERGENCY BATTERY IAW W/C 33-50-05R. (S) 2 H 7 2 4T RT A13NM 20080731 NM 2008 7 31 HNAA0800192 1 20080610 A 3350 6104789 BATTERY DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS DISCHARGED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 935HA 50562 142 RT EGRESS LIGHT IS INOPERATIVE FORWARD. REMOVED AND REPLACED EMERGENCY BATTERY IAW W/C 33-50-05R. P/N OFF 61-0478-9, P /N ON 60-1721-1XC S/N OFF 138, S/N ON JAX12. (S) 2 H 7 2 4T RT A13NM 20080731 SO 2008 7 31 CHQA200800109 1 20080611 A 3297 14521493401 WIRE HARNESS EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL NLG SHORTED A CHQA O OTHER O OTHER NR NOT REPORTED 1 GL 11 275SK 145345 CAE312704 FLIGHT 5800, CLE TO ATL. THE CREW REPORTED THE NOSE LANDING GEAR DOORS DID NOT CLOSE ON GEAR RETRACTION. MAINTENANCE I NSPECTED THE HARNESSES AND FOUND THE WO17 HARNESS WITH TWO WIRES SHORTING TOGETHER. THE HARNESS WAS REPLACED AND THE DO ORS OPERATED NORMALLY. (S) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080731 EA 2008 7 31 COMA0860271 1 20080608 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 30545 7117 FS 280 FLOORBEAM (GALLEY SIDE) CRACKED. REPAIRED FS 280 FLOORBEAM IAW REO 601R-53-11-136. (S) 2 L 7 2 4F RT A21EA 20080731 SO 2008 7 31 C2XA08IA134 1 20080531 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13553 145585 AUS - DURING MAINTENANCE INSPECTION THE FORWARD SIDE OF THE CEILING EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MA INTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT INVERTER. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AC FT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080731 NM 2008 7 31 HNAA0800186 1 20080601 A 3150 WARNING LIGHT DHAV DHC8 DHC8102 2809003 NM HYD SYSTEM ILLUMINATED A HNAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 07 808EX 40551 299 NR 1 HYDRAULIC ISO C/L AND INBOARDD SPOILER C/L ILLUMINATED IN FLIGHT, QTY STABILIZED AT 1 QT. INSPECTED ACFT, NO LEAKS NOTED, SERVICED AS REQ. GROUND RAN ACFT, HYDRAULIC QTY`S REMAINED THE SAME, DRAINED EPA, OK FOR SERVICE. (S) 2 H 7 2 4T RT A13NM 20080731 SW 2008 7 31 WGEA200800061 1 20080605 A 2621 FIRE BOTTLE ECLIPS EA500 ECLIPSEEA500 3350000 SW NR 1 NACELLE LEAKING A WGEA O OTHER O OTHER NR NOT REPORTED 1 EA 27 130DJ 000023 NR 1 ENG FIRE EXTINGUISHING AGENT LEAKING OUT OF COWLING AND GAUGE SHOWS 0. (S) 1 L 7 2 4J RT A00002AC 20080731 SO 2008 7 31 C2XA08CL072 1 20080617 A 3350 66369 LIGHT EMB 135 EMB135ER 3260203 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14505 145192 DURING ROUTINE MAINTENANCE THE NR 2 EMERGENCY AISLE PATH LIGHT STRIP WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4F RT T00011AT 20080731 SO 2008 7 31 SIM2008F00010 1 20080706 A 3297 CONNECTOR EMB 145 EMB145LR 3260212 SO MLG LOOSE A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 675AE 14500806 ON FLIGHT 4402, CREW REPORTED ON TAKEOFF RECEIVED A LANDING GEAR AIR/GND FAIL CAUTION MESSAGE. LANDING GEAR WOULD NOT R ETRACT. CREW ELECTED TO RETURN TO FIELD. ACFT REMOVED FROM SERVICE. FOUND CONNECTOR J0775 LOOSE. RE-TIGHTENED, OPERA TIONAL CHECKED GOOD IAW AMM 32-30-00 AND AMM 32-34-00. ACFT RETURNED TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080731 NM 2008 7 31 SWAA083979 1 20080717 A 5754 SKIN BOEING 737 7373H4 1384600 NM LT WING SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED 18Y CHECK, FOUND L/E WING NR 5 L/E SLAT DELAMINATED AT INBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20080731 EA 2008 7 31 VNAA0806009 1 20080613 A 2840 73664320 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUEL QTY FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 220PS 10345 7887 CREW REPORTED THE RT FUEL QUANTITY AND TOTAL FUEL QUANTITY SHOWED DASHED LINES ON CLIMBOUT. THE CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FUEL QUANTITY GAUGE COMPUTER IN ACCORDANCE WIT H THE ACFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE GOOD. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080731 SO 2008 7 31 C2XA08IA139 1 20080608 A 3230 355022002MOD3 ELECTRONIC UNIT EMB 145 EMB145XR 3260214 SO MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 31131 15256 15256 145705 DGO - FLIGHT 2036. DURING CLIMBOUT THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS, AND THE LANDING G EAR WOULD NOT RETRACT. THE ACFT RETURNED TO DGO WHERE IT LANDED WITHOUT INCIDENT. THE ACFT WAS FERRIED TO IAH WHERE MA INTENANCE INSPECTED THE ACFT, AND REMOVED AND REPLACED THE LGEU. OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE A CFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080731 EA 2008 7 31 COMA0860289 1 20080615 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 420CA 19470 7451 RECEIVED FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED PDU. NO FURTHER DEFECTS . (S) 2 L 7 2 4F RT A21EA 20080731 2008 7 31 2008UALA03593 4 20080625 A 2565 D31517121 ASPIRATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SLIDE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 430UA A6154 568 LEAKING ASPIRATOR FLAPPER VALVES. DAMAGE DUE TO EXCESSIVE USE. REPLACED ASPIRATOR, OPS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20080731 NM 2008 7 31 2008UALA03615 1 20080627 A 3510 MXP1472 OXYGEN MASK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CAPTAIN'S FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 CAPTAIN'S OXYGEN MASK DOOR LATCH DOES NOT WORK PROPERLY. SUSPECT PRE FLIGHT CHECKS. REPLACED OXYGEN MASK BOX ASSEMBLY O P CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080731 EU 2008 7 31 COEA0803914 1 20080510 A 3297 WIRE HARNESS AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NLG SHORTED A COEA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 NM 13 914FX 293 RETURN TO BLOCKS, FLIGHT 7826 GPI TO GTF: AFTER TAXIING TO THE RUNWAY AND COMPLETION OF THE TAXI CHECKLIST ITEMS. THE CREW NOTICED A RAPID INCREASE IN TAT TEMP (TURBINE AIR TEMP) AND THE AFCS (AUTOMATIC FLIGHT CONTROL SYSTEM) SHOWED "DADC (DIGITAL AIR DATA COMPUTER) INVALID." BOTH ENGINE TORQUE BUGS INDICATED 20% AND WERE ERRONEOUS. AFTER A SYSTEM RE-BOO T FAILED TO CORRECT THE PROBLEM, A DECISION TO RETURN TO BLOCKS FOR MAINTENANCE WAS MADE. TROUBLESHOOTING IS STILL ONGO ING, CORRECTIVE ACTION TO FOLLOW. FOUND NLG WIRE HARNESS CONNECTOR RECEPTACLE AT 5044 VC INTERNALLY SHORTED TO GROUND. REPLACED NLG WIRE HARNESS CONNECTOR RECEPTACLE 5004 VC. (S) 2 H 7 2 4T 4 T RT A53EU E20NE 20080731 NM 2008 7 31 YEN2008F00012 1 20080706 A 2120 UNKNOWN EMB ERJ190 ERJ190100IGW 3260408 NM CABIN ODOR A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 239JB 19000040 AIR RETURN TO DEPARTURE, AFTER TAKEOFF THE ODOR OF SMOKE WAS NOTICED WAS 2 L 7 2 4F RT A57NM 20080731 NE 2008 7 31 PID2008F00006 2 20080713 A 7261 SWITCH BOEING 737 7372K5 138448X NM PWA JT8 JT8D15A 52051 NE OIL BYPASS DIRTY A PIDA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 39 250TR 22597 OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. SHUTDOWN RT ENGINE IAW QRH. DIVERTED FLT, INSPECTED NR 2 MAIN ENGINE OI L FILTER AND CLEANED BYPASS CONNECTOR SWITCH. RAN NR 2 ENGINE, BYPASS LIGHT DID NOT ILLUMINATE. PERFORMED OPS CK IAW M M 79-02. RELEASED ON MEL 79-02. 2 L 7 2 4F 4 F RT A16WE E2EA 20080731 CE 2008 7 31 GLB2008F00005 1 20080618 A 5320 1144300027179 ANGLE BEECH 1900 1900D 1154162 CE BS 288 CRACKED A GLBA O OTHER O OTHER NR NOT REPORTED 1 NM 21 195GL UE195 LT HEAVY ANGLE CRACKED APPROX 1.125 INCH IN LENGTH AT FORWARD BEND RADIUS AT FS 288.0. REPAIRED LT HEAVY ANGLE AT FS 288 IAW SRM 53.90. REPAIR AREA APPROX 13.125 INCH LONG. RII INSPECTION CP,[;OED WOTJ OAW TASKCARD NR 8.2.1. (K) 2 L 7 2 4T RT A24CE 20080721 NM 2008 7 21 SWAA083729 1 20080705 A 3350 65C27093 SIGN BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 719SW 27853 AFT GALLEY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN ASSY PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 2008UALA02874 1 20080517 A 2560 P4010021 BATTERY BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FLASHLIGHT DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 932UA 26658 AFT EMERGENCY FLASHLIGHT INOPERATIVE. SUSPECT FAULTY BATTERY. REPLACED BATTERY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080721 EU 2008 7 21 2008UALA02858 1 20080519 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 446UA 834 FOUND CORROSION ON FLOORBEAM ITEM 175. ACCOMPLISHED MAJOR REPAIR AT DEN. INSTALLED FLOORBEAM. REQUIRES INSTALLATION O F WIRE CLAMPS AND BLOWER FAN BOLTS. HARDWARE IS ATTACHED TO FLOORBEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20080721 NM 2008 7 21 SWAA083637 1 20080701 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 632SW 27707 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083626 1 20080630 A 3350 311500 LENS BOEING 737 7373Q8 1384670 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 BULLNOSE EMERGENCY EXIT LIGHT LENS LOOSE AT ROW 22 ABC. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083642 1 20080701 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 700GS 27835 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 138. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083641 1 20080701 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 700GS 27835 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 120. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083644 1 20080701 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 716SW 27850 DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083654 1 20080702 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 206WN 34011 DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083667 1 20080702 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083684 1 20080702 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 8R CRACKED AT BS 500B. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083673 1 20080702 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED C2 CHECK, FOUND STRINGER 16L CRACKED AT BS 517. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 2008UALA02958 1 20080521 A 3510 6350A33XA OXYGEN SYSTEM BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CREW O2 LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 941UA 26676 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. SUSPECT PRE FLIGHT CHECKS. SERVICED OXYGEN SYSTEM TO FULL . AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA02960 1 20080521 A 2432 18550000 BATTERY BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE AFT CARGO BAY DISCHARGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 666UA 29238 APU WILL NOT START. SUSPECT FAULTY BATTERY. REPLACED BATTERY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 NM 2008 7 22 2008UALA02961 1 20080521 A 2697 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENG FIRE LOOP LOOSE A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 547UA 25368 EICAS MSG - FIRE OVHT SYS-. FIRE OVHT TEST PANEL SYS FAIL LIGHT ON: EICAS MSG - L ENG FIRE LP 1 -. CREW COMMENTS: EIC AS STATUS MESSAGE LENG FIRE LP 1. LOOSE CONNECTOR IN HOT SECTION. SECURED LOOSE CONNECTOR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080804 SW 2008 8 4 WGEA2008000061 1 20080610 A 2621 FX002002 CARTRIDGE ECLIPS EA500 ECLIPSEEA500 3350000 SW FIRE EXTING FAILED A WGEA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 27 130DJ 137 000023 NR 1 ENGINE FIRE EXTINGUISHING AGENT LEAKING OUT OF COWLING AND GAUGE READS ZERO. REPLACED FIREX CARTRIDGE WITH SERVICE ABLE UNIT. (A) 1 L 7 2 4J RT A00002AC 20080804 NM 2008 8 4 08FDEA02571 1 20080630 A 5320 65463422 CHANNEL BOEING 727 727225 1384077 NM BS 1070 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 DOT 7 AFT PIT, FLOOR SUPPORT ATTACH ANGLE MISDRILLED AND CRACKED ON LOWER SURFACE AS MARKED, LOCATED AT STA 1070 5 INCH , LBL 18 INCH. REPLACED ATTACH ANGLE REF SRM 51-30-02 PG 2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080804 SW 2008 8 4 WGEA2008000062 1 20080608 A 2621 FX002002 CARTRIDGE ECLIPS EA500 ECLIPSEEA500 3350000 SW FIRE EXTING FAILED A WGEA O OTHER O OTHER NR NOT REPORTED 1 EA 27 139DJ 150 000054 NR 1 ENGINE FIRE EXTINGUISHING AGENT LEAKING. REPLACED FIREX CARTRIDGE WITH NEW UNIT. (A) 1 L 7 2 4J RT A00002AC 20080804 NM 2008 8 4 08FDEA02465 1 20080625 A 5344 66168497 HINGE BOEING 727 727225 1384077 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 GROUND POWER ACCESS PANEL. TOP HINGE BRACKET CRACKED REMOVED DAMAGED PART PER REF SRM 51-30-02 PG 1-3, FABRICATED NEW P ART PER REF DWG NR 66-16849-7. TREATED AND PRIMED NEW PART PER REF SRM 51-10-02. INSTALLED NEW PART PER REF SRM 51-30- 02 PG 1-3. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080804 NM 2008 8 4 08FDEA02468 1 20080625 A 5340 654531313 STRINGER CLIP BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 STRINGER CLIP ON STR 9L AT FS 720B HAS CORROSION ON SIDES REMOVED STRINGER CLIP REF SRM 51-30-02. DRILLED UP NEW CLIP. INSTALLED NEW CLIP REF SRM 51-30-02, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080804 WP 2008 8 4 08FDEA02472 1 20080625 A 5313 AEA04511 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 FOUND L 52 AT STA 1575 CRACKED. REMOVED DAMAGED L 52 AND INSTALLED A NEW LONGERON P/N AEA 0451-1 IAW DAC DWG NEA 6076; REV AK. 2 L 7 3 4F RT A22WE 20080804 EU 2008 8 4 08FDEA02474 1 20080625 A 5347 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN DECK FLOOR SEAT TRACK HAS CORROSION AT C73-C74; RBL 62. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02475 1 20080625 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN DECK FLOOR SEAT TRACK HAS CORROSION; C75-C76; RBL 44. BLENDED CORROSION AND FOUND SEAT TRACK TO BE OUT OF LIMITS P ER SRM 53-10-16. REMOVED CORRODED SEAT TRACK PER SRM 51-41-21. RECEIVED NEW SEAT TRACK P/N A5327400500053, PER SRM 53- 18-16. LOCATED AND DRILLED NEW SEAT TRACK PER SRM 53-10-16 AND DWG A53278295. INSTALLED SEAT TRACK PER SRM 51-41-21 AN D DWG A53278295. APPLIED CIC PER AMM 51-22-00-0. PART MARKED PER GMM 7-0-1001. 2 L 7 2 4F RT A35EU 20080804 NM 2008 8 4 08FDEA02486 1 20080625 A 5347 SEAT TRACK BOEING 757 7572B7 1384964 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 906FD 27148 BS 440-640, LBL 24, SEAT TRACK HAS DOUBLE DRILLED HOLES AND GOUGES AROUND CLIPNUT HOLES. REMOVED DAMAGE SEAT TRACK IA W SRM 51-40-02. ALL DAMAGE TO SEAT TRACK IS OUT OF LIMITS PER SRM 53-00-52. FABRICATED A NEW SEAT TRACK, ON TRAVELER N R T8/741233, AND INSTALLED IAW SRM 51-40-02 AND 53-00-52. ALSO FABRICATED 2 ANGLES, 1 PLATE AS PART OF REPAIR FOR SEAT TRACK. THIS IS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING. 2 L 7 2 4F RT A2NM 20080804 EU 2008 8 4 08FDEA02497 1 20080626 A 5315 A53778807202 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND OLD UPPER FLANGE SPLICE REPAIR AT FWD CARGO FLOOR STRUCTURE C 32 LT/RT WITHOUT ANY DOCUMENTATION REPAIR RENEWED IA W SRM SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02501 1 20080626 A 5347 A53274005 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 423FE 281 PREVIOUS REPAIR LOCATED ON MAIN CABIN SEAT TRACK NR 6 RT - Y2462 BETWEEN FRAMES 34 TO 36, HAS 4 EACH REPAIR SPLICES, THE AFT INBD AND OTBD REPAIR SPLICES MEASURE 8.4 INCHES LONG BY 3 INCHES TALL, THE FWD INBOARD AND OUTBOARD REPAIR SPLICES MEASURE 8.4 INCHES LONG BY 3 INCHES TALL AND 1 EACH SEAT TRACK REPAIR SECTION MEASURING 21 INCHES LONG. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT SEAT TRACK REPAIR AT MAIN CABIN SEAT TRACK NR 6 RT - Y2 462 BETWEEN FRAMES 34 TO 36 IAW A310-200 SRM 53-10-16 FIG 208. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02561 1 20080630 A 5315 A25313792202 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON FLANGE C12A-13A, Y - 730. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02822 1 20080711 A 5754 A57840120200 PAN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND OLD DOUBLER REPAIR ON LT SLAT NR 1 FOLDING NOSE INNER PAN REPAIR PERFORMED IAW SB A300-57-6067 (REPLACEMENT OF I NNER PAN), APPROVED BY EA 6-5742-120037. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02592 1 20080701 A 5313 A53974203228 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION SPOTS AT STRINGER P 56, C65-72 LT OUT OF LIMIT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 . 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02824 1 20080711 A 5754 A57863251163 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND ON RT SLAT NR 1 TRAILING EDGE LOWER SKIN WEAR DAMAGE AT FOLDING NOSE CUTOUT. REPAIR PERFORMED BY BLENDOUT THE DAM AGE TO SMOOTH CONTOUR IAW. RAS/FOK/097/2008 ISS A, APPROVED BY EA 6-5742-120057. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02559 1 20080630 A 5320 A53612214201 SUPPORT AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON SUPPORT C11-14, Y-730 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080722 NM 2008 7 22 2008UALA03038 1 20080528 A 5753 113W30033 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE T/E FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 780UA 47315 26944 LEFT WING O/B FLAP UPPER SURFACE ARE WORN AT LOCATIONS: 1" TO 9", 62" TO 71", 147" TO 168", AND 220" TO 240". DAMAGED L OCATION IS MEASURED FROM I/B END. MAX DAMAGE DEPTH IS .080". SUSPECT NORMAL AC OPERATION. ACP REPAIR PER AMECO, 777E N-57-0041-01. THE REPAIR IS APPROVED BY BAC, AND 8100-9 THE REPAIR IS A PERMANENT REPAIR. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080722 NM 2008 7 22 2008UALA03039 1 20080528 A 5753 113W210010 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE T/E FLAP DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 780UA 47315 26944 RIGHT WING I/B MAIN FLAP UPPER SURFACE OUTBOARD SIDE ATTACHED SCREW HOLES HAVE 3 DENTS. SUSPECT TOOLING MARKS. ACP REP AIR PER AMECO 777EN -57-0045-01. THE REPAIR IS APPROVED BY BAC, AND 8100-9 THE REPAIR IS A PERMANENT REPAIR. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080722 NM 2008 7 22 2008UALA02907 1 20080519 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 656UA 25394 RIGHT AFT LAV EEL LIGHT BAR IS INOP. SUSPECT BROKEN LIGHT ASSEMBLY. REPAIRED RT AFT LAV EEL LIGHT BAR IAW GNMM 20-51-0 05 AND OPS CHECKED GOOD IAW MM 33-51-10. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 NM 2008 7 22 2008UALA02992 1 20080524 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 655UA 25393 EMERGENCY ESCAPE LIGHT STRIP IN FRONT OF RT MID LAV IS INOP. FOUND LIGHT ASSEMBLY BROKEN. REPAIRED LIGHT ASSEMBLY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 NM 2008 7 22 2008UALA03000 1 20080526 A 3020 6439002 ANTI-ICE VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE LOCKED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 595UA 28748 LEFT ENG ANTI-ICE EICAS, LEFT ENG ANTI-ICE SWITCH OFF WITH VALVE LIGHT. NR 1 ENG ANTI ICE VALVE LOCKED IN THE OPEN POSI TION. REPLACED NR 1 ENG AI VALVE, OPS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080722 2008 7 22 2008UALA02968 4 20080523 A 2565 D31591478U1 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR DEPLOYED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 903UA 25003 PARTIAL SLIDE DEPLOYMENT 1L. SUSPECT IMPROPERLY INSTALLED SLIDE ASSEMBLY. REPLACED 1L SLIDE PER MM 25-61-35. AC OK FO R SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NE 2008 7 22 2008UALA02969 2 20080522 A 7530 7732887810 REGULATOR VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 649UA 25286 LEFT ENG BLEED AIR VALVE WILL NOT OPEN. DUCT PRESSURE ON LEFT SIDE IS ZERO. ADVANCED ENG POWER AND STILL NO HELP. FOU ND PRESSURE REGULATING VALVE TO BE FAULTY. REPLACED PRV, RAN ENGINE OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 2008 7 22 2008UALA02970 4 20080520 A 3140 S243W0011401 MODULE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LEFT FAULTY A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION IN INSP/MAINT 1 WP 29 778UA 26940 AIMS LRM MESSAGE DISPLAYED. FOUND M11 IN LEFT AIMS CABINET FAULTY. REPLACED LEFT AIMS M11 REF MM 31-41-02. SOFTWARE L OADED AND TEST OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080722 NM 2008 7 22 2008UALA02976 1 20080522 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 337UA 24241 EMERGENCY EEL FLOOR LIGHTS INOP FROM 12ABC TO 16ABC, ALSO GALLEY STRIP. SUSPECT FAULTY LIGHT SECTION. REPAIRED LIGHT S ECTION, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA02980 1 20080522 A 5320 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 536UA 25156 BS 1440 STR 26L HAS DAMAGE. ACCOMPLISHED MAJOR REPAIR AT GSO--RPR WAS RPL ON PTT#8002108 PER SRM 53 -00-07 RPR 5. THIS IS A RPR IN ZONE 1 AND IS CAT B RPR AND REQUIRES SUPPLEMENTAL INSPECTIONS STARTING AT 50,000 TOTAL FLIGHT CYCLES AND 12 ,000 FC THERE AFTER. INSPS ARE BOTH VISUAL AND NDT PER SRM 53-00-07 RPR 5 TABLE II. CURRENT PTC IS 20477. ON NR 46109 -INF- : REPAIR ACCMPLSHED PER SRM 50-00-07 TABLE II ZONE 1. REQUIRING REINSPECTION AT 50,000 CYCLES & REPEAT AT 12,000 CYCLES. THIS IS CAT B REPAIR. EC 50-5330-036SA -A CREATED TO ACCMPLSH INSP'S. DTA 03-184 WILL TRACK REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080722 2008 7 22 2008UALA03050 4 20080527 A 2564 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE RAFT BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 544UA 25322 AFT FWD LOWER CEILING SLIDE RAFT ELT SEAL IS BROKEN. UNKNOWN DAMAGE. REPLACED ELT. 2 L 7 2 4F 4 F RT A2NM E17NE 20080722 NM 2008 7 22 2008UALA02927 1 20080520 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 541UA 25253 AFT FUSELAGE SKIN AT BS 1414 AND STR 29R, SKIN IS DENTED. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED DAMAGE FAB RPR AND INSTALLED IAW SRM 53-00-01 ON NR 20950 THIS RPR REQUIRES SUPPLEMENTAL INSPS STARTING IN 37,50 0C PER SRM 53-00-01 RPR 2 TABLE V. CURRENT PTC=20417 INSPS CONSISTS OF EITHER LFEC OR HFEC AND REINSPECTION IS BASED ON WHAT METHOD IS USED AT T IME OF INSP. 2 L 7 2 4F 4 F RT A2NM E17NE 20080722 NM 2008 7 22 2008UALA03009 1 20080524 A 3350 58721 COVER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 374UA 24639 FIRST CLASS FLOOR LIGHTING COVER LOOSE - PORTSIDE. FOUND LOOSE LIGHT COVER. SECURED LIGHT COVER. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA03010 1 20080525 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR OBSTRUCTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 540UA 25252 SLIDE LIGHT 2L ON W-DOOR DISARMED. DEBRIS UNDER GIRT BAR. REMOVED DEBRIS, PERFORMED OPS CHECKS, ALL NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080804 EU 2008 8 4 08FDEA02560 1 20080630 A 5320 A53612214200 SUPPORT AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON SUPPORT C11-14, Y 730. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080804 NM 2008 8 4 08FDEA02578 1 20080630 A 5322 69459473 SHEAR TIE BOEING 727 727225 1384077 NM CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 LOWER FUSELAGE, CORROSION ON TIE FITTING STA 337 EXTERIOR, LBL17 INCH. BELOW LANDING GEAR SUPPORT BEAM TO DRAG BRACE FI TTING. REMOVED AND REPLACED TIE FITTING STA 337 LBL17 BELOW NOSE LANDING GEAR DRAG BRACE FITTING SUPPORT BEAM REF SRM 5 1-30-2 PG'S 8-9 AND 13-14. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080804 NM 2008 8 4 08FDEA02568 1 20080630 A 5720 6922894 SUPPORT ANGLE BOEING 727 727225 1384077 NM FLAP TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 RT WING LWR FIXED T/E PANEL BELOW NR 14 SPOILER ACTUATOR. FLAP TRACK SUPPORT ANGLE CRACKED. REMOVED AND MANUFACTURED N EW O/B ANGLE FOR NR 8 FLAP TRACK SUPPORT BRACKET REF BOEING DRAWING 69-22894-9 AND SRM 51-20-1. INSTALLED NEW MANUFACTU RED ANGLE ON BRACKET REF SRM 51-30-2 1-4 AND BOEING DRAWING 69-22894. INSTALLED SUPPORT BRACKET ON NR 8 FLAP TRACK REF SRM 51-30-2 PG 13. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080804 NM 2008 8 4 KCSA081284 1 20080615 A 5315 FLOORBEAM BOEING 747 747122 1384872 NM BS 1560 S46L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 AFT PIT FLOORBEAM WEB CRACKED AT BS 1560 ABOVE STR-46L. (B) 2 L 7 4 4F RT A20WE 20080804 EU 2008 8 4 08FDEA02511 1 20080627 A 5315 A5327534720000 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 660FE 759 THRU AFT CARGO COMPT CEILING, FR 62 CABIN FLOORBEAM BETWEEN SEAT TRACKS NR 3 RT AND NR 4RT, AFT FACE VERTICLE STIFFENER CRACKED, .250 IN LONG REMOVED CRACK AND INSTALLED CROSSBEAM REPAIR AT CRACKED STIFFENER AT FR 62 FLOORBEAM BETWEEN SEA T TRACK NR 3RT AND NR 4RT IAW A300-600 SRM 53-10-15, FIG 212, SHT 1. 2 L 7 2 4F RT A35EU 20080804 SO 2008 8 4 SIMA200816504 1 20080609 A 5315 FLOORBEAM EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 836AE 145635 DURING A MBV INSP, THE GALLEY FLOOR CENTER BEAM AT FR 20 WAS FOUND CORRODED WITH LEVEL TWO CORROSION. PERFORMED CUT OUT OF THE CENTER BEAM TO REMOVE THE DAMAGE. FAB A DOUBLER, DRILLED, APPLIED PREVENTIVE AND INSTALLED. WORK DONE IAW EMB 145 SRM (SRM EMB-14511142 REV 40) CHAPTER 53-21-10. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080804 NM 2008 8 4 NWAA082605514 1 20080602 A 5532 SKIN BOEING 757 757251 1384970 NM VERTICAL STAB DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 514US 23202 DURING INSPECTION FOUND DAMAGE CAUSED TO VERTICAL STABILIZER RT LOWER LOWER SIDE SKIN PANEL. DAMAGE WAS CAUSED BY THE D EPARTURE OF RT WING TRAILING EDGE PANEL. REPAIRED PER EA 55-213280 SECT1 SECTION 2 REQUIRES REPETITIVE INSPECTIONS NOT TO EXCEED 24 MONTH INTERVALS AFTER SECTION 1 ACCOMPLISHMENT. (A) 2 L 7 2 4F RT A2NM 20080804 EA 2008 8 4 A6WA200840500 1 20080609 A 5210 PANEL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STAIR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 PAX DOOR STAIR FWD SIDE PANEL IS CRACKED BETWEEN STEP NR 1 AND STEP NR 2. REPAIRED IAW REO 601R-52-11-702 REV A. (A) 2 L 7 2 4F RT A21EA 20080804 EA 2008 8 4 A6WA200840457 1 20080530 A 3260 TARGET CNDAIR CL600 CL6002B19 1900309 EA MLG UPLOCK OUT OF ADJUST A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 431AW 7256 GEAR DISAGREE LT MLG SHOWS HATCHED. COMPLIED WITH QRH, RETURNED TO PHL. SECURED LT MLG UPLOCK TARGET REF AMM 32-32-05, OPS CHECK AND GEAR SWINGS GOOD. 2 L 7 2 4F RT A21EA 20080804 EU 2008 8 4 AALA200801381 1 20080524 A 2560 FLASHLIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 19059 469 MIA - EMERGENCY FLASHLIGHT AT LT NR TWO DOOR INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT AT LT NR TWO DOOR. SYSTEM GROU ND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080804 NM 2008 8 4 AALA200801696 1 20080624 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 788AN 30011 DFW - EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080804 WP 2008 8 4 ARWA20080604 1 20080625 A 7797 CONNECTOR DOUG DC10 DC1030 3023501 WP EGT INDICATOR LOOSE A ARWA O OTHER N FALSE WARNING LD LANDING 1 SO 29 524MD 46999 NR 3 ENGINE EGT ERRATIC DURING LANDING ROLLS. FOUND LOOSE CONNECTOR PI-8036. RE-SECURED IT IN ACCORDANCE WITH MM 20-30 -02. OPERATIONAL CHECK SYSTEM FOUND NORMAL IAW MM 71-00-00. (A) 2 L 7 3 4F A22WE 20080804 EU 2008 8 4 AALA200801380 1 20080524 A 3530 OXYGEN BOTTLE AIRBUS 300 A300B4605R 3930308 EU PORTABLE LOW A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 19059 469 MIA - EMERGENCY OXYGEN BOTTLE AT LT NR TWO DOOR PRESSURE LOW. REPLACED OXYGEN BOTTLE AT LT NR TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080804 NM 2008 8 4 F3LA200800323 1 20080610 A 5315 D54380043204 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 REFERENCE NON ROUTIN C044731. DURING C4 S1 C-CHECK INSPECTION NOTED CORROSION ON OUTBOARD NUT CLIP HOLE 2 INCHES FORWAR D OF FRAME 66 ON FLOORBEAM Y1732 LT. MAINTENANCE REPAIRED FLOORBEAM Y1732 LT IN ACCORDANCE WITH THE REQUIREMENTS OF EA A9-53R-30354, SRM 51-44-12, SRM 51-42-11 AND SRM 53-41-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACC EPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080804 EA 2008 8 4 SIMA200818202 1 20080628 A 3000 CONTROLLER CNDAIR CL600 CL6002C10 1390015 EA ADS HEATER ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 507AE 10059 ON FLIGHT 3468 - MAINTENANCE REPORTED AN ELECTRICAL BURNING SMELL WHILE DOING ANTI ICE CHECKS FOR A PIREP. AIRCRAFT REM OVED FROM SERVICE. REMOVED AND REPLACED RT AIR DATA SENSOR HEATER CONTROLLER IAW AMM 30-31-15, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A21EA 20080804 NM 2008 8 4 F3LA200800329 1 20080611 A 5321 D5367320100000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 REFERENCE NON ROUTINE 34615. DURING C3 S1 C-CHECK INSPECTION NOTED FORWARD CARGO FLOOR PANEL 131AF HAS A HOLE. MAINTEN ANCE REPAIRED HOLE ON PANEL 131AF IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080722 NM 2008 7 22 2008UALA03148 1 20080531 A 2750 3910015103600U SOLENOID VALVE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE T/E FLAP FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 799UA 26926 FLAPS PRIMARY FAIL PRIMARY (HYDRAULIC) FLAPS DRIVE FAILURE. FLAPS OPERATING IN SECONDARY (ELECTRIC) MODE. CAUTION MSG- 2720372 LATCHD DC MODE. FAILED HIGH LIFT CONTROLS TEST. FOUND FLAPS PRIMARY LOW SPEED SOLENOID VALVE AT FAULT AND REPL ACED REF MM 27-51-05, ALL OPS CHECKS SATISFIED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080722 NM 2008 7 22 2008UALA03160 1 20080602 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN UNSECURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 398UA 24673 FLOOR EMERGENCY LIGHTING STRIP PULLED UP AT 1B. FOUND LIGHT ASSEMBLY LOOSE. SECURED LIGHT ASSEMBLY. AC OK FOR SERVICE . 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA03161 1 20080602 A 3397 362624 CONNECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN CONTAMINATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 342UA 24246 EEL LIGHTS INOP FROM SEAT 15 TO BACK OF AIRCRAFT. SUSPECT MOISTURE CONTAMINATION. CLEANED ELECTRICAL CONNECTION POINTS ALONG EEL ON THE AFT END. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 NM 2008 7 22 2008UALA03185 1 20080603 A 5210 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 L2 DOOR REQUIRES REPAIR DOUBLER AT UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080722 NM 2008 7 22 2008UALA03203 1 20080603 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 SEAT 20R TO 26R, SEAT EEL INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 NM 2008 7 22 2008UALA03205 1 20080603 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 SEAT EEL ON 39R INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 NM 2008 7 22 2008UALA03208 1 20080604 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 774UA 26936 LIGHT AT 3B MISSING. RELAMPED LIGHT, OPS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080722 EA 2008 7 22 A6WA200840463 1 20080601 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 CORROSION FOUND ON FLOOR STRUCTURE FS 574 TO 605 LBL 27. FLOORBEAM REPLACED IAW SRM 51-42-06, SRM 51-42-21, SRM 51-42-3 6. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840362 1 20080327 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CORRODED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 401AW 7280 CREW ESCAPE HATCH OUTER HANDLE SHAFT CORRODED. REPLACED HANDLE ASSEMBY AND LUBED INTERIOR WITH DC33. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840462 1 20080526 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 SERVICE DOOR LOWER SILL PLATE ASSY CORRODED. SERVICE DOOR LOWER SILL PLATE REMOVED AND REPLACED IAW SRM 51-41-02 AND 51- 41-04. (A) 2 L 7 2 4F RT A21EA 20080722 WP 2008 7 22 ABXR080171 1 20080503 A 2740 59109623 JACKSCREW DOUG DC9 DC915F 3022037 WP HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 783TW 47010 HORZ, STAB JACK SCREW THREADS PITTED/CORRODED. REMOVED AND REPLACED JACK SCREW IAW DC9 MM 27-40-1. (A) 2 L 7 2 4F A6WE 20080722 WP 2008 7 22 ABXA080178 1 20080607 A 3397 L2G2H20N WIRE DOUG DC9 DC941 302207N WP LT WING BURNED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 951AX 47616 WHILE TROUBLE SHOOTING THE INOP LT INBO TAIL LIGHT AND THIS LT AFT WING TIP LIGHT FOUND WIRE L 26AH20N BURNT FROM R5-105 1D TO GROUND STUD 713 IAW WDM 33-42-02. (A) 2 L 7 2 4F A6WE 20080722 NM 2008 7 22 SWAA083913 1 20080715 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 268WN 32524 R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080722 NM 2008 7 22 SWAA083948 1 20080716 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 227WN 34450 R1 DOOR EMERGENCY EXIT LIGHTS INOP. FOUND LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080722 NM 2008 7 22 SWAA083959 1 20080716 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 8L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080804 WP 2008 8 4 WXOA070211 1 20080604 A 3350 AD4002 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 884GA 49401 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETUR NED TO SERVICE. (A) 2 L 7 2 4F RT A6WE 20080804 NM 2008 8 4 2008UALA03668 1 20080701 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 DOOR CLOGGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 532UA 25072 DOOR 3L WILL NOT ARM PROPERLY. *S/D* FOUND DEBRIS STUCK UNDER GIRT BAR. REMOVED DEBRIS, DOOR ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080804 NM 2008 8 4 2008UALA03680 1 20080701 A 2910 HYDRAULIC SYSTEM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT NACELLE FIRE A UALA K NONE A FLAME/FIRE IN INSP/MAINT 1 WP 29 771UA 26932 WHILE PERFORMING OPERATIONAL CHECK ON RT HYD ACMP FLASH FIRE OCCURRED IN PYLON. FLASH FIRE WAS ON FOR A FEW SECONDS AND WAS CONTAINED. NO FIRE EXTINGUISH AGENT WAS NEEDED OR USED BY FIRE DEPT. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080804 NM 2008 8 4 2008UALA03683 1 20080702 A 3697 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SHUTOFF VALVE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NR 1 PYLON PRSOV VALVE WIRES W306-68-18 AND W306-71-18 DAMAGED. REPLACED WIRES W306-68-18 ANSD W306-71-18 PER B767 WDM 36-11-51 AND BSWPM 20-30-12. REPLACED CONNECTOR D22 PER WDM 36-11-51. OPS CHECKS GOOD. AC OK FOR SERVCICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080730 NM 2008 7 30 SWAA083692 1 20080704 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 500C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME SWA EA. 2 L 7 2 4F RT A16WE 20080731 SO 2008 7 31 C2X2008F00000 1 20080603 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS OVERHEATED A C2XA O OTHER M OVER TEMP NR NOT REPORTED 1 SW 27 16918 145397 NR 4 EMERGENCY BATTERY INVERTER IS REAL HOT WHEN EMERGENCY LIGHT IS NOT ON. REMOVED AND REPLACED NR 4 INVERTER IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD. (S) 2 L 7 2 4T RT T00011AT 20080731 EA 2008 7 31 COMA0860274 1 20080608 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FS 718 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 30545 7117 RT FS 718.00 FRAME DOUBLER CRACKED ON THE AFT SIDE AT STRINGERS 10 AND 11. REMOVED AND REPLACED FRAME DOUBLER IAW BOMBA RDIER REO 601R-53-61-243. (S) 2 L 7 2 4F RT A21EA 20080731 SO 2008 7 31 CHQA200800108 1 20080610 A 3610 40303925SD O-RING EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL BLEED AIR LEAKING A CHQA O OTHER O OTHER NR NOT REPORTED 1 GL 11 278SK 145370 CAE311143 FLIGHT 7803, IAD TO IND. WHILE CLIMBING THROUGH 8,000 FT THE FLIGHT CREW RECEIVED A BLEED 1 LEAK MESSAGE, RETURNED TO I AD, AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DURING INSPECTION THAT THE BAGGAGE COMPARTMENT FLOOR WAS WARM, AND A FTER REMOVING THE FLOOR BOARDS FOUND JOINT 17 TO BE LEAKING. THE O-RINGS WERE REPLACED AND THE BLEED SYSTEM OPERATED NO RMALLY. (S) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080731 NM 2008 7 31 HNAA0800188 1 20080520 A 5246 85410618053 DOOR DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE UNSECURE A HNAA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 EA 07 838EX 37685 220 REFUEL DOOR APPEARED OPEN IN FLIGHT. UPON ARRIVAL VERIFIED BOTH DOOR LATCHES WERE NOT SECURED. INSPECTED AREA, NO DAMA GE NOTED. LATCHES AND DOOR OPERATE NORMALLY. (S) 2 H 7 2 4T RT A13NM 20080731 EA 2008 7 31 COMA0860290 1 20080616 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 915CA 7013 RECEIVED FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH SI-2-27I0001 FLAP C AUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION. FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. (S) 2 L 7 2 4F RT A21EA 20080731 SO 2008 7 31 C2XA08IA136 1 20080608 A 3350 78241 INVERTER EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14516 145323 IAH - DURING A-CK INSPECTION THE EMERGENCY LIGHT AT THE RT EXIT ROW WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE EMERGENCY LIGHT INVERTER. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080731 EA 2008 7 31 COMA0860295 1 20080619 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA RT WING TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 514CA 5 7809 RECEIVED FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY, RAN QRH, LANDED WITHOUT INCIDENT. REPLACED RT BPSU. NO FU RTHER DEFECTS. (S) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 COMA0860280 1 20080610 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 30545 7117 CRACK ON REAR PRESSURE BULKHEAD ABOVE CARGO DOOR TRACK. REPAIRED REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1541. (S) 2 L 7 2 4F RT A21EA 20080731 NM 2008 7 31 CALA0800659 1 20080701 A 5553 6549559 LUG BOEING 737 737524 1384721 NM VERTICAL STAB GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16646 28907 AFT RIGHT-HAND OUTBOARD VERTICAL STABILIZER FORWARD FUSELAGE FITTING BUSHING IS GOUGED. REMOVED BUSHING, REWORKED LUG A ND INSTALLED OVERSIZED REPAIR BUSHING PER ECRA 5342-01053. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 2008UALA03613 1 20080626 A 5420 BUSHING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NR 2 PYLON INBOARD MID SPAR FITTING BUSHING MIGRATED .030 NO CORROSION OR ROTATION. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 EA 2008 7 22 A6WA200840396 1 20080507 A 7110 RING CNDAIR CL600 CL6002B19 1900309 EA COWLING WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 437AW 7744 CORE COWL 445 CLOSURE RING WORN BEYOND LIMITS. CORE COWL 445AB CLOSURE RING REPLACES IAW 71-12-01-300-820-A01 REPAIR. ( A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840465 1 20080521 A 5260 SKIN CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 REPAIR DENTS IN AIRSTAIR DOOR UPPER FWD CORNER COVER AND UPPER AFT CORNER COVER. REPAIRED IAW REO 601R-52-11-827. FWD UP PER CORNER COVER REPLACED IAW SRM 51-42-13. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840468 1 20080502 A 5313 LONGERON CNDAIR CL600 CL6002B19 1900309 EA BS 319 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 438AW 7748 CORROSION AT PASSENGER DOOR LOWER LONGERON ON FUSELAGE AT FS319. CORROSION AT PAX DOOR LOWER LONGERON AT FS 319 REMOVED IAW CRJ 200 SRM 51-21-06. (A) 2 L 7 2 4F RT A21EA 20080721 NM 2008 7 21 SWAA083732 1 20080706 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM L/E SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED 18Y CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED AT AUX TRACK CUTOUT. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083661 1 20080702 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 480, STR 15R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083662 1 20080702 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 480, STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083660 1 20080702 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 24L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20080721 NM 2008 7 21 SWAA083669 1 20080702 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080722 NM 2008 7 22 2008UALA03064 1 20080528 A 3610 339910031 CONTROLLER BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 1 ENGINE SHORTED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 785UA 26954 THE "AIR SPLY L HTR" C-B ON P110 POS M16 WILL NOT RESET. SUSPECT HIGH PRESSURE CONTROLLER/FAN AIR SHORTED. REPLACED LT FAN HP CONTROLLER. RAN BOTH ENGINES. OPS OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080722 NM 2008 7 22 2008UALA02993 1 20080524 A 2432 18550000 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE E&E BAY FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 651UA 25389 THE 'MAIN BAT CHGR' EICAS MSG DISPLAYED. CYCLED STBY POWER THROUGH OFF-BATT, NO HELP. FOUND BATTERY TO BE FAULTY. REP LACED BATTERY PER MM 24-31-01, OPS CHECKED OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 NM 2008 7 22 2008UALA03202 1 20080603 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 674UA 29242 SEATS 24L TO 31L, SEAT EEL INOPERATIVE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080722 NM 2008 7 22 2008UALA03211 1 20080605 A 2612 CONTROL PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE WARNING MALFUNCTIONED A UALA K NONE O OTHER TX TAXI/GRND HDL 1 WP 29 202UA 24717 CREW REPORTS RED CARGO FIRE LIGHT ILLUMINATED SYSTEM WILL NOT TEST. INVESTIGATE DISCHARGED DISTINGUISHING SYSTEM. FOUN D FAULTY FIRE DETECTION CONTROL PANEL. REPLACED FIRE DETECTION CONTROL PANEL. 2 L 7 2 4F 4 F RT A16WE E21EU 20080722 EA 2008 7 22 A6WA200840459 1 20080530 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 5340 7281 CRACK FOUND ON MACHINED FITTING FS 461 RBL 9 OUTBOARD. REPLACED IAW SRM 51-42-06 & 51-42-21. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840460 1 20080530 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 CRACK ON FLOORBEAM ANGLE FS 621 LBL 40. CRACK ON FLOOR SUPPORT ANGLE AT FS 621 LBL 40 REPAIRED IAW REO 601R-53-61-117 RE V C. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840401 1 20080513 A 2701 CONTROL COLUMN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT LOOSE A A6WA K NONE F FLT CONT AFFECTED CR CRUISE 1 GL 31 433AW 7289 REQUEST INSPECTION OF FIRST OFFICER`S CONTROL COLUMN FOR SUSPECTED EXCESSIVE PLAY IN NEUTRAL POSITION. PERFORMED OPS CHE CK OF ELEVATOR CONTROL SYSTEM USING PITCH FEEL CHECK IAW AWAC SUPPLEMENT 2006-004A. OPS CHCEK GOOD. NO DEFECTS NOTED. (A ) 2 L 7 2 4F RT A21EA 20080722 2008 7 22 SWAA083914 4 20080715 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 301SW 22941 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080722 NM 2008 7 22 SWAA083956 1 20080716 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080722 EA 2008 7 22 A6WA200840321 1 20080411 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 404AW 7294 CRACK FOUND AT FS 484 LBL 36 WL 73. CRACK REPAIRED AT FS 484 LBL 36 WL 73.00 IAW REO 601R-53-41-059 REV A. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840470 1 20080505 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 438AW 7748 LT LOWER SILL CORRODED AROUND NUT PLATE HOLES BTWN FS 574 TO FS 621 AT LBL 43 AND WL 73. CORROSION REMOVED AROUND NUT P LATE HOLES ON SILL IAW SRM 51-21-06. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840472 1 20080507 A 5210 GUARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR TORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 438AW 7748 PAX DOOR WEATHER GUARD IS TORN AND RETAINER IS CRACKED. REPLACED PAX DOOR WEATHER GUARD RETAINER IAW SRM 51-42-13 AND SR M 51-41-02. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840478 1 20080507 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 438AW 7748 FLOOR SUPPORT ANGLE AT FS 621.00, WL 73.50, LBL 40 IS CRACKED, DIMESNSIONS OF CRACK IS .400" LONG. DAMAGED PORTION OF A SSY ANGLE 601R35031-239 CUT AWAY, IAW REO 601R53-60-117 REV A, AT FS 621.00, WL 73.50, LBL 40, REPAIRED IAW REO 601R53-6 1-117 REV C. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840404 1 20080514 A 5220 H341937 HANDLE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CORRODED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 442AW 7778 OUTER HANDLE CREW ESCAPE HATCH IS CORRODED, DOESN`T OPEN FREELY. OUTER HANDLE CREW ESCAPE HATCH REPLACED IAW AMM 52-22- 03-400-801. OPS TEST COMPLIED WITH IAW AMM 52-22-710-081. (A) 2 L 7 2 4F RT A21EA 20090129 EA 2009 1 29 A6WA200840426 1 20080521 A 3220 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA NOSE LACK OF LUBE A A6WA O OTHER E VIBRATION/BUFFET DE DESCENT 1 GL 31 438AW 7748 WHEN LANDING GEAR WAS SELECTED DOWN, A CLICKING OR BINDING SOUND WAS HEARD FROM NOSE GEAR AREA UNTIL NOSE GEAR WAS LOCKE D DOWN. SWUNG NLG ON GROUND, LUBED NLG PER AMM 12-32-00. OK FOR SERVICE. 2 L 7 2 4F RT A21EA 20080722 NM 2008 7 22 ABXA080160 1 20080509 A 5754 114T412481 PANEL BOEING 767 767281 1385109 NM L/E SLAT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 783AX 23016 NR 4 SLAT INNER SURFACE PANEL CRACKED NEAR I/B TRACK. REMOVED AND REPLACED ON NR 0129 IAW B767. (A) 2 L 7 2 4F RT A1NM 20080722 NM 2008 7 22 ABXA080161 1 20080512 A 5320 113T1623125 ANGLE BOEING 767 767281 1385109 NM FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 783AX 23016 EXFOLIATION ON PANEL MOUNT FLANGE AT NUT PLATE-4 AREAS0 JUST INBOARD OF GEAR. REMOVED AND REPLACED UPPER T-ANGLE ON PAN EL CLOSE OUT BEAM ABOVE MAIN LANDING GEAR (LT) IAW SRM 51-40-02. (A) 2 L 7 2 4F RT A1NM 20080722 WP 2008 7 22 ABXA080163 1 20080519 A 5311 99115205 FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 HOLE WITH CRACK IN FRAME STA 218, LONGERON 12 LEFT. REPAIRED IAW DC9 SSRM DWG K05159. (A) 2 L 7 2 4F A6WE 20080722 WP 2008 7 22 ABXR080169 1 20080502 A 2761 39232592 SUPPORT DOUG DC9 DC915F 3022037 WP RT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 783AX 47010 RIGHT WING OUTBOARD SPOILER HAD OUTBOARD ACTUATOR SUPPORT BRACE CRACKED, UPPER END. REMOVED AND REPLACED OUTBOARD ACTUA TOR SUPPORT BRACE IAW DC0 SRM 51-30-1, 51-30-2 AND 51-30-5. (A) 2 L 7 2 4F A6WE 20080722 WP 2008 7 22 ABXR080170 1 20080502 A 5720 591000644 ANGLE DOUG DC9 DC915F 3022037 WP CENTER WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 783AX 47010 CENTER WING TO FUSELAGE ANGLE CRACKED AND SEPERATED ABOVE REPAIR STRAP FORWARD SPAR AREA AT APPROX. RIGHT BUTT LINE 48. REMOVED AND REPLACED FITTING IAW DC9 SRM. (A) 2 L 7 2 4F A6WE 20080722 WP 2008 7 22 ABXR080173 1 20080508 A 5313 59114279 LONGERON DOUG DC9 DC915F 3022037 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 783AX 47010 LONGERON 16 LEFT WAS CRACKED AT STA 801 FRAME UPPER ATTCH FASTENER. REMOVED AND REPLACE LONGERON IAW SRM 53-02, FIG 18, SHEET 1. (A) 2 L 7 2 4F A6WE 20080722 WP 2008 7 22 ABXA080179 1 20080620 A 3260 4924737502 TARGET DOUG DC9 DC941 302207N WP RT MLG DEFECTIVE A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 960AX 47762 RIGHT GEAR UNSAFE LIGHT ON AFTER TAKE OFF, RECYCLED GEAR STILL ON. REPLACED STIKER/TARGET ASSEMBLY IAW DC9 MM. (A) 2 L 7 2 4F A6WE 20080722 EA 2008 7 22 A6WA200840512 1 20080616 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 444ZW 7788 PAX DOOR AFT DRAG ANGLE CRACKED. REPLACED ANGLE IAW SRM 51-42-06 AND 51-42-13. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840510 1 20080610 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 444ZW 7788 INTERCOSTAL CRACK ON LT SIDE AT STR 14 BTWN FRAME 621.00 AND 625.00. INTERCOSTAL REPLACED IAW SRM 51-42-06. (A) 2 L 7 2 4F RT A21EA 20080724 NM 2008 7 24 SWAA083704 1 20080703 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 485WN 32473 EEPLS SECTION NR 2 BROKEN. REMOVED AND REPLACED EEPLS SECTION PER MM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 2008UALA03043 1 20080527 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 CABIN FLOORBEAM AT STA 377.7, AT LBL 62 IS CORRRODED. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW 53-00-98 FIG 825. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03077 1 20080529 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR OBSTRUCTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 512UA 24809 DOOR 1R HARD TO DISARM. DEBRIS UNDER GIRT BAR. REMOVED BOTTLE CAP FROM UNDER GIRT BAR. DOOR ARMING SYS OPS CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03095 1 20080529 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN UNSECURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 513UA 24810 EXIT PATH LIGHTING STRIP IN REAR OF AIRCRAFT HAS COME LOOSE, LAST ROW IN COACH. RE-INSTALLED EEL LIGHTING, ALL OPS TEST S NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03247 1 20080607 A 2120 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN ODOR A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 366UA 24535 CREW REPORT: F/A REPORT ELECTRICAL BURN SMELL FROM FWD COFFEEMAKER AREA. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 EU 2008 7 24 2008UALA03276 1 20080608 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 403UA 442 CREW OXYGEN SYSTEM LOW. RECORD PRESS PRIOR TO SERVICING. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 EU 2008 7 24 2008UALA03277 1 20080607 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 417UA 483 THE 3 SVC EMERGENCY LIGHT TEST FAILS, "EXT LOADS L AFT". 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03280 1 20080609 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EEL INOP, SEAT 51C. RELAMPED EMERGENCY LIGHT, OP CHECKED OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080724 NM 2008 7 24 2008UALA03281 1 20080606 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 641UA 25091 RIGHT FWD CABIN EEL INOPERATIVE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080724 EU 2008 7 24 2008UALA03289 1 20080608 A 3200 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LANDING GEAR VIBRATION A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 449UA 851 GEAR VIBRATION AFTER LIFT OFF UNTIL GEAR HANDLED RAISED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03290 1 20080609 A 5610 WINDOW BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT ARCED A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 306UA 23667 CAPTS L2 WINDOW BEGAN ELECTRICAL ARCING AT POINT OF WIRING EMBEDDED BETWEEN PANES. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03291 1 20080610 A 2612 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE FIRE WARNING MALFUNCTIONED A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 668UA 30024 LEFT ENGINE FIRE LOOP 2 STATUS MESSAGE WOULD NOT RESET. 2 L 7 2 4F 4 F RT A1NM E24NE 20080724 NM 2008 7 24 2008UALA03031 1 20080525 A 3350 20131A LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 197UA 26901 FC EMERGENCY LIGHTS FLASHING ON THE RT AISLE. COULD NOT DUPLICATE ON GROUND. REPLACED POWER SUPPLY M6000 AT DOOR 1R (P RECAUTIONARY). TESTED OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080724 EU 2008 7 24 2008UALA03062 1 20080527 A 5320 SHEAR PLATE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 447UA 836 LEFT SHEAR PLATE BETWEEN FRAME 69 AND 70 HAS EVIDENCE OF SURFACE CORROSION ON UPPER SURFACE AND AT FASTENER HOLES. ACCO MPLISHED MAJOR REPAIR AT DEN. REMOVED LT SHEAR PLATE AND DRILLED NEW PLATE TO FIT, CLEANED AND TOP COATED AREA. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03116 1 20080601 A 5610 WINDOW BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT OPEN A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 537UA 25157 1ST OFFICER'S WINDOW OPENED. RTFL. CHECK WINDOW OPERATION AND SEAL FOR DAMAGE AND WINDOW OPS NORMAL AND NO SEAL DEFECT S NOTED. CLOSED WINDOW. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03143 1 20080530 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 R2 DOOR UPPER HINGE ARM CUTOUT HAS A CRACK. ACCOMPLISHED MAJOR REPAIR AT GSO. REPAIRED FRAME IAW MM 52-11-87 AND SRM 5 1-40-02. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03180 1 20080603 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 532UA 25072 EMERGENCY EXIT LIGHT ROW 15 TO ROW 20 INOP. LOOSE CONNECTOR. SECURED LOOSE CONNECTOR AT SEAT 20, ALL OPS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03184 1 20080603 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 L4 DOOR HANDLE BOX HAS CORRODED INSERTS ON TOP OF BOX. INSTALLED NEW HANDLE BOX PER UAL SM 50-52-11-06-JD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03190 1 20080602 A 5497 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 NR 2 PYLON HAS SEVERAL CORRODED WIRES AT GROUND STUD LOCATION SHEARED FROM GROUND. RE-TERMINATED WIRES IAW BSW PM 20-30 -11. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03198 1 20080603 A 7330 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT MALFUNCTIONED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 589UA 28707 L ENG SEC CONT STATUS MESSAGE. CHECKED FOR EPCS MESSAGES LISTED ON MM CHAPTER 71 EICAS AND EPCS MESSAGES SERVICE TIP, N O MESSAGES FOUND. ERASED STATUS MESSAGE. PUT EEC SWITCH ON P61 PANEL TO SEC POSITION, NO MESSAGES APPEARED. ACFT OK F OR SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03256 1 20080606 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 STA 279 STR 8L HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE AND INSTALLED SINGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03257 1 20080606 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 FWD ENTRY DOOR UPPER FUSELAGE HINGE CUTOUT HAS ONE EACH FASTENER HOLE WITH CRACK INDICATION AT BS 303 AND STRINGER S-10L . MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. VERIFIED REMOVAL WITH HFEC. INSTALLED DOUBLER/FILLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03316 1 20080610 A 2612 PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE SYSTEM NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 306UA 23667 CARGO FIRE SYSTEM WILL NOT TEST - PANEL BLANK. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03323 1 20080611 A 2701 CONTROL COLUMN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT STIFF A UALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 914UA 25381 CREW REPORTS EXCESSIVE CONTROL COLUMN FORCE REQUIRED FOR PITCH. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NE 2008 7 24 2008UALA03328 2 20080612 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RIGHT SURGES A UALA O OTHER W R INADEQUATE Q C PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 204UA 28713 222007 RIGHT ENGINE EXPERIENCED 2 INCIDENTS OF SURGE AS EVIDENCED BY POPPING NOISE AND RPM ROLLBACK FOLLOWED BY FULL RECOVERY. PARAMETERS ARE NORMAL. SURGE WAS NOT COMMENSURATE WITH THROTTLE MOVEMENT. ALL FIM TROUBLESHOOTING, INCLUDING EXTENSIV E BOROSCOPE INSPECTION (BSI), REVEALED NO CONDITION TO ACCOUNT FOR THE SURGE. NO FAULT FOUND.SUSPECT WAKE TURBULENCE EN COUNTER. MM BLENDED SOME VERY MINOR HPC BLADE DAMAGE FOUND DURING BSI. THIS DAMAGE WAS NOT SUFFICIENT TO CAUSE ENGINE S URGE AND COULD HAVE CONTINUED IN SERVICE WITHOUT BLENDING. THE PROBLEM DID NOT REOCCUR. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080724 NM 2008 7 24 2008UALA03339 1 20080612 A 2120 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN ODOR A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 29 301UA 23642 ACRID SMOKEY SMELL RETURNED UPON LANDING. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03306 1 20080609 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 644UA 25094 EEL LIGHT IN FRONT OF LAV 103 INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20080724 NM 2008 7 24 2008UALA03308 1 20080609 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CAVIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 644UA 25094 EEL LIGHT AT SEATS 5EF INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20080724 NM 2008 7 24 2008UALA03224 1 20080605 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 FWD ENTRY DOOR LOWER FUSELAGE HINGE CUTOUT HAS ONE EACH FASTENER HOLE WITH CRACK INDICATION AT BS 303 AND STRINGER S-13L . MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRICATED SINGLE STAINLESS EXTERNAL SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 2008 7 24 SWAA083812 4 20080709 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 356SW 25251 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083915 1 20080715 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 13R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083887 1 20080714 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083886 1 20080714 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083946 1 20080715 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM CRACKED AT BS 738, RBL 5.5. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083933 1 20080715 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080722 NM 2008 7 22 SWAA083685 1 20080702 A 5512 65C25727 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED 18Y CHECK, FOUND RH HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 141. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080722 EU 2008 7 22 08FDEA02059A 1 20080528 A 5312 A53984654200 BULKHEAD AIRBUS 300 A300B4622R 3930312 EU AFT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 AFT PRESSURE BULKHEAD - CRACK IN THE SKIN AT INTERIOR OF A HOLE (AT 3 O'CLOCK) IN THE APU DUCT FLANGE ATTACHMENT. AF T PRESSURE BULKHEAD SKIN WAS REPAIRED AS PER EA 6-5310-121644. 2 L 7 2 4F RT A35EU 20080722 NM 2008 7 22 SWAA083679 1 20080702 A 2560 33500007 GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 8 DEF. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 20080722 EA 2008 7 22 A6WA200840473 1 20080507 A 5420 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA RT NACELLE BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 438AW 7748 RT ENGINE NOSE INLET HAS A SUPPORT ASSY BROKEN FOR THE T2 LINE AT 12 O`CLOCK POSTIOIN. RT ENGINE NOSE INLET SUPPORT ASS Y FOR T2 LINE AT 12 O`CLOCK POSITION REPLACES IAW SRM 51-42-06. (A) 2 L 7 2 4F RT A21EA 20080722 NM 2008 7 22 ABXA080158 1 20080506 A 5230 140T26033 BEAM BOEING 767 767281 1385109 NM CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 783AX 23016 AFT LOWER CARGO DOOR BEAM WAS CORRODED AT ALL NUT PLATES. REMOVED AND REPLACED BEAM IAW B767 DWG 140T2603 AND SRM. (A) 2 L 7 2 4F RT A1NM 20080724 NM 2008 7 24 SWAA083709 1 20080702 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 622SW 27932 RIGHT OVERWING EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED EXIT LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 2008UALA02949 1 20080522 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 193UA 26890 CEILING EMERGENCY LIGHT ROW 17 INOP. RELAMPED EMERGENCY LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080724 NM 2008 7 24 2008UALA03045 1 20080527 A 5320 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 CABIN RT BETWEEN BS 1420 AND 1440 AT STR 17R CORROSION. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED AND REPLACED WEB IAW SRM 53-60-13. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 EU 2008 7 24 2008UALA03244 1 20080608 A 2611 SMOKE WARNING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E&E BAY ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 466UA 1343 AVIONICS SMOKE/ECAM. RTFL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03279 1 20080607 A 2613 OVERHEAT LOOP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT WING FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 337UA 24241 FOUND WING OVERHEAT LOOP M1204 BAD. SUSPECT IMPROPERLY INSTALLED. REPLACED RT OVERHEAT LOOP ENGINE PYLON IAW MM26-18-1 1. OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 EU 2008 7 24 2008UALA03058 1 20080527 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 447UA 836 FLOORBEAM ITEM 175 HAS CORROSION. ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED BEAM 175 TRANSFERRED CLIPS AND SPLICES TO NEW BEAM PARTS. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 UPS08M52412 1 20080505 A 5330 SKIN DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C AFT FUSELAGE EXTERIOR, RIGHT SIDE AT STA 2033 BETWEEN LONGERONS L39 & L 40, CORROSION FOUND SURROUNDIN G FASTENER HOLE. ATTACH FASTENERS & INNER SUPPORTS REMOVED PER SRM 51-31-01 V II R35. SKIN CORROSION REMOVED PER SRM 5 1-21-01 VII R35. DAMAGE SKIN TRIMMED OFF PER SRM 53-20-00 FIG 2. HFEC C/O PER DACNDTSPM R13 PT 06.10.01. 001 ON TRIMME D OFF AREA FOUND NO CRACK EVIDENT. REPAIR PARTS FAB AND INSTALLED PER SRM 53-20-00 FIG 2 VI R35 & SRM 51-31-01 VII R35. 2 L 7 3 4F RT A22WE 20080724 NM 2008 7 24 2008UALA03157 1 20080602 A 5347 SEAT TRACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 CABIN, PREVIOUS REPAIR ON END OF SEAT TRACK BS 377.7 IS CORRODED, APPROX RBL 40. ACCOMPLISHED MAJOR REPAIR AT GSO. REM OVED DAMAGE AND FABRICATED REPAIR IAW REO G12351 REV B. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03193 1 20080604 A 3350 32145410 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 850UA 1653 RIGHT EPSU BATTERY FAILS EMERGENCY LIGHT CHECK. REPLACED EPSU BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 2008 7 24 2008UALA03200 4 20080604 A 2565 D37085101 HOSE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 419UA 487 HOSE BROKE DURING INFLATION. HOSE DID NOT SWIVEL DURING INFLATION CAUSING HOSE TO BREAK. REPLACED HOSE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NE 2008 7 24 2008UALA03288 2 20080609 A 7261 BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A UALA O OTHER W K B INADEQUATE Q C FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 512UA 24809 STINK ODOR IN FLIGHT DECK AT TAKEOFF AND LANDING. NR 1 ENG BEARING FAILURE CAUSING OIL LEAK/COKING ODOR COMING IN THROU GH ENG BLEED AIR. REPLACED NR 1 ENG. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03317 1 20080610 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP, 1ST, 2ND, 3RD FROM FWD. RELAMPED EMERGENCY LIGHT, OPERATION CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080724 NM 2008 7 24 SWAA083809 1 20080713 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 14R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083932 1 20080715 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083934 1 20080715 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BETWEEN BS 669 AND BS 665, LBL 24.75. REPAIRED FLOORBEAM PER SW A EA. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083935 1 20080715 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 433, RBL 3. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083712 1 20080704 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING 22Y CK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 550, RBL 50, WL 208. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083713 1 20080704 A 5322 6546529 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING 22Y CK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 550, RBL 28, WL 208. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083714 1 20080703 A 3350 6574550 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 724SW 27856 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EVAC SLIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083719 1 20080704 A 3350 65C27093 SIGN BOEING 737 7377H4 1384404 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 769SW 30588 DURING SCHEDULED 8Y CHECK, FOUND G-4 GALLEY EMERGENCY EXIT SIGN DAMAGED. REMOVED AND REPLACED EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 20080731 NE 2008 7 31 2008UALA03624 2 20080630 A 7261 7543549 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BYPASS VALVE LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 544UA 25322 717952 OIL LEAKING FROM LEFT ENGINE. *S/D* NR 5 DRAIN LEAKING, SEALS BAD. REPLACED FUEL OIL HEAT EXCHANGER AND BYPASS VALVE AND SEALS, ENG RUNS ARE DRY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080731 NM 2008 7 31 CALA0800676 1 20080707 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM BS 747 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 LEFT STATION 747 FRAME CRACKED AT AIR CONDTIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. CUT OUT DAMAGE AT STA TION 747 LEFT S-8 AND S-9 AND REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 SWAA083770 1 20080709 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500D S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 SWAA083769 1 20080709 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500C S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 YEN2008F00008 1 20080617 A 2120 SENSOR EMB ERJ190 ERJ190100IGW 3260408 NM MALFUNCTIONED A YENA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 15 279JB 19000090 AIR RETURN TO DEPARTURE, AIR CONDITIONING VAPORS FOGGED UP FLIGHT DECK SO INTENSE WE WERE UNABLE TO SEE FLT INSTRUMENTS, ON CLIMB OUT OF 5000 RECYCLED PACK AND TURNING HEAT WAY UP VAPORS WENT AWAY. REMOVED AND REPLACED VENTURI DP SENSOR IA W FIM TASK 21-51-00-810-812. OPS CHECK OF AMS OK, NO FAULTS NOTED. REPLACED RECIR FILTERS AS PRECAUTION. (K) 2 L 7 2 4F RT A57NM 20080801 NM 2008 8 1 08FDEA02460 1 20080625 A 5313 STRINGER BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 SKIN BULGE JUST FWD OF STATION 1010 STR 27L. REMOVED FASTENERS FROM AFFECTED AREA IAW SRM 51-30-2, CUTOUT STRINGER SECTI ON (DIM 10 1/4" LONG) IAW B727 SRM 53-10-3 FIG 1, REMOVED EXISTING SPLICE IAW SRM 51-30-2, FABRICATED REPAIR PARTS IAW SRM 51-10-2, CLEANED SKIN AND NO CORROSION NOTED, INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 53-10-3 FIG1. 2 L 7 3 4F A3WE 20080804 NM 2008 8 4 08FDEA02579 1 20080630 A 5720 6521656132 BRACKET BOEING 727 727225 1384077 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 SEAL RETAINER ON SNRM NR N00362 IS CORRODED. FOUND BRACKET UNDER RETAINER CORRODED AT WS 167 TO 222 AFT OF SPAR LOWER C HORD. REPLACED BRACKET (STIFFENER) ON NON ROUTINE W/U NR N00362. SEE ITEM NR 16 ON JPF. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080804 NM 2008 8 4 08FDEA02582 1 20080630 A 5320 65575702 SUPPORT BOEING 727 727225 1384077 NM BS 1030 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 DOT 9 AFT PIT, RT Z-ANGLE, LOWER SURFACE CORRODED AROUND TIE DOWN FITTING, LOCATED STA 1030 14", RBL 20" TO RBL 22" WA TER LINE 149 Z-ANGLE IS REPLACED WITH NEW, P/N 65-57570-2 AND WILL BE INSTALLED ON W/C 5310-7-2354 E2 P1R. 2 L 7 3 4F A3WE 20080804 SW 2008 8 4 WGEA2008000063 1 20080519 A 2621 FX002002 CARTRIDGE ECLIPS EA500 ECLIPSEEA500 3350000 SW FIRE EXTING FAILED A WGEA O OTHER O OTHER NR NOT REPORTED 1 EA 27 160DJ 149 000077 NR 2 ENGINE FIRE EXTINGUISHING AGENT LEAKING. REPLACED FIREX CARTRIDGE WITH SERVICEABLE UNIT. PER EA 500 AMM 26-20-00. (A) 1 L 7 2 4J RT A00002AC 20080804 SO 2008 8 4 LR7A08085 1 20080701 A 5523 BEAM LKHEED 382 382G 526414U SO ELEVATOR TAB CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 636 4763 DURING SCHEDULED B-2 CHECK, PER JOB CARD HB2703, FOUND RT ELEVATOR TRIM TAB INBD FRONT BEAM CRACK AT HSS72. REPAIR ACCO MPLISHED IAW SMP583 FIG 55-30-04 . 2 H 7 4 4T A1SO 20080804 NM 2008 8 4 08FDEA02463 1 20080625 A 5315 FLOORBEAM BOEING 757 757236 1384971 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 MAIN CABIN BS 418, BL0 TO LBL 15, FLOORBEAM HAS AREAS OF CORROSION AROUND FASTENER HOLES. CLEANED AREA AND CHECKED LI MITS IAW SRM 51-10-3 AND 53-00-51, DETAIL 3. FLOORBEAM OUT OF LIMITS PER SRM 53-00-51, DETAIL 3; ORIGINAL MATERIAL THIC KNESS .125 INCH, AFTER REWORK .094 INCH. CUT OUT DAMAGED AREA PER SRM 53-00-51, FIG 201, REPAIR NR 5. FABRICATED REPAI R PARTS, ON TRAVELER NR T8/745527, AND INSTALLED PER SRM 53-00-51, REPAIR NR 5. THIS REPAIR IS A CATEGORY "A" MAJOR REP AIR WITH NO FOLLOW UP TRACKING. 2 L 7 2 4F RT A2NM 20080804 WP 2008 8 4 08FDEA02504 1 20080626 A 5330 SKIN DOUG MD10 MD1010F 3022112 WP BS 1195-1216 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 INTERIOR FUSELAGE SKIN HAS CORROSION IN AREAS AROUND THE DRAIN HOLES FROM FS 1195 - 1216; STRINGERS 51R - 51L. 2 L 7 3 4F RT A22WE 20080804 WP 2008 8 4 08FDEA02815 1 20080710 A 5210 BEAM DOUG MD10 MD1010F 3022112 WP R3 DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 R3 DOOR NR 1 DOOR BEAM, AFT STOP LUG IS CRACKED. REMOVED & REPLACED THE R3 DOOR IAW EA 8-5210-116995. 2 L 7 3 4F RT A22WE 20080804 WP 2008 8 4 08FDEA02817 1 20080710 A 5320 AEA00265 INTERCOSTAL DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 LEFT MLG WW AFT BULKHEAD OUTBD SIDE OF THE WELL INTERCOSTAL AT FS 1521 JUST BELOW THE FLAP BUSS PULLEY IS CORRODED. REM OVED AND REPLACED THE INTERCOSTAL IAW SRM 51-35-01, VOL II. FABRICATED A NEW INTERCOSTAL IAW DWG AEA 0026, REV M. ALOD INED AND PRIMED IAW SRM 51-21-01, VOL II. PART MARKED INTERCOSTAL P/N FX AEA0026-5 IAW GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20080804 EU 2008 8 4 08FDEA02163 1 20080605 A 5320 A5398673320400 INTERCOSTAL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 665FE 769 THE INTERCOSTAL FROM EMPENNAGE FRAME 86 TO FRAME 87; AT STRINGER 34R IS BENT. REMOVED INTERCOSTAL IAW A300-600 SRM 51-4 0-21. REPLACED INTERCOSTAL CHORD IAW A300-600 SRM 51-40-21 AND SRM 51-72-10. INSTALLED INTERCOSTAL IAW A300-600 SRM 51 -40-21. 2 L 7 2 4F RT A35EU 20080804 WP 2008 8 4 NWAA082559867 1 20080608 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 776NC 47786 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE TAIL COMPARTMENT HAD INOPERATIVE LIGHTS FOR THE CATWALK. MAINTENANCE REPLACED THE BATTERIES. OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F RT A6WE 20080804 NM 2008 8 4 NWAA082633146 1 20080521 A 5330 SKIN AIRBUS A319 A319114 3930350 NM FUSELAGE DENTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 346NB 01796 DURING H-CHECK FUSELAGE SKIN WAS DENTED FORWARD OF FRAME 74 BETWEEN S24-S25. REPAIRED PER EA 32-212140. (A) 2 L 7 2 4F RT A28NM 20080804 WP 2008 8 4 WXOA070209 1 20080610 A 3260 SENSOR DOUG DC9 DC987 3022087 WP DIRTY A WX0A C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 WP 19 945MA 49725 FLIGHT CREW REPORTED DURING THE TAKEOFF ROLL THE "WINDSHEAR WARNING AND GROUND PROXIMITY SYSTEM WAS NOT INDICATING PROPE RLY". OUTFLOW VALVE WOULD NOT CLOSE AND THE FLIGHT DIRECTOR COMMAND BARS WHERE MISSING. MAINTENANCE DEPARTMENT PERSONNE L PERFORMED A RETURN TO SERVICE TEST OF THE PROXIMITY SYSTEM, CLEANED ALL AFFECTED SENSORS IAW AMM 32-60-04 AND 05. SYS TEM OPERATIONAL TEST WAS NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A6WE 20080804 NM 2008 8 4 2008UALA03661 1 20080701 A 5210 DOUBLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 R-1 DOOR INTERNAL DOUBLER GOUGED AT TORQUE TUBE, LOWER SECTION. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED DOUBL ER, CUT OUT DAMAGE, AND INSTALLED NEW DOUBLER PER SRM 52-10-01, REPAIR 6 AND SRM 51-10-01 PRP C. CURRRTG PTC 18040. THI S IS A CAT B REPAIR. REQUIRES L FEC INSP EVERY 12,000 CYC. 2 L 7 2 4F 4 F RT A2NM E17NE 20080804 NM 2008 8 4 2008UALA03671 1 20080702 A 2910 HYDRAULIC SYSTEM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RIGHT LOW PRESSURE A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 771UA 26932 HYD PRESS DEM R LOW RIGHT HYDRAULIC DEMAND PUMP PRESSURE WITH PUMP COMMANDED ON OR PUMP SWITCHED OFF. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080828 EA 2008 8 28 MAS2008F00018 1 20080808 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77278 7278 AIRSHUTTLE 1001 IN HNL REPORTED A SERVICE DOOR EXIT LT AND CABIN EMERGENCY FLOOD LIGHT INOPERATIVE. MAINTENANCE RELAMPE D THE EMERGENCY LIGHTS. (S) 2 L 7 2 4F RT A21EA 20080804 NM 2008 8 4 2008UALA03689 1 20080702 A 5754 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 3 SLAT DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NR 3 SLAT REMOVED FROM A-C 6352. SLAT DENTED 56 INCHES FROM INBOARD END. DAMAGED CAUSE IN WIND STORM. 2 L 7 2 4F 4 F RT A1NM E24NE 20080804 NM 2008 8 4 2008UALA03690 1 20080702 A 5497 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 NACELLE DETERIORATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 57UA 27112 NR 1 ENG HYD BAY (PYLON) CONNECTOR D00916 HAS DETERIORATED INSULATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 20080804 NM 2008 8 4 2008UALA03632 1 20080630 A 3830 VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LAVATORY TOILET STUCK A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 642UA 25092 FWD LAV TANK INDICATING FULL. HALF OF LAVS NOW NOT WORKING. ECONOMY LAVATORY BY DOOR 2L TOILET WILL NOT STOP FLUSHING, FOUND STUCK VALVE. USED A WET PILLOW PER SAM. FLUSHED BOTH TANKS THRU SEVERAL TIMES WITH HONEY-BEE AND PRESERVICE. RES ET TOILET TANK LOGIC MODULES LIGHTS EXTINGUISHED BOTH SYSTEMS OPS CHECK SATIS. PERFORMED LAVATORY WASTE LEVEL SERVICE CH ECK. CHECKS OKAY. CLEANED WATER LEVEL SENSOR. CHECKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20080804 NM 2008 8 4 2008UALA03635 1 20080628 A 3350 767 BULB BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 382UA 24657 RIGHT EXT OVERWING EXIT EMERGENCY LIGHT INOP. FOUND BURNED OUT LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE . 2 L 7 2 4F 4 F RT A16WE E21EU 20080804 NM 2008 8 4 2008UALA03656 1 20080701 A 2810 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT FUEL TANK INOPERATIVE A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 589UA 28707 CENTER TANK RIGHT FUEL VALVE WILL NOT OPEN. 2 L 7 2 4F 4 F RT A2NM E17NE 20080804 NM 2008 8 4 2008UALA03691 1 20080702 A 2997 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 HYD SYS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NR 1 ENG PYLON HYD BAY CONNECTOR D02134 SADDLE CLAMP IS MISSING. 2 L 7 2 4F 4 F RT A1NM E24NE 20080804 EU 2008 8 4 M7K2008F00052 1 20080410 A 7700 CHIP DETECTOR UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE CONTAMINATED E M7KA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 19 822MH 4687 4142 23069 ENGINE CHIP WARNING LIGHT ILLUMINATED. AN UNEVENTFUL PRECAUTIONARY LANDING TO FIRST SUITABLE SPOT PERFORMED. ALL ENGIN E CHIP DETECTORS WERE INSPECTED FOR ABNORMAL METAL. ONE, NOT RECOVERABLE, HAIRLIKE SLIVER, FOUND ON THE ELECTRICITY WIR ED DETECTOR WAS REMOVED. GROUND PENALTY RUN COMPLETED. NO DEFECT FOUND. SUSPECT SLIVER GENERATED DURING ASSEMBLY OR N ORMAL OPERATION. NO FURTHER CHIPS FOUND UP THE DATE OF THIS REPORT. INITIAL DATE OF CHIP WAS MARCH 20, 2008. 75+ ENGI NE HRS ELAPSED SINCE OCCURRENCE WITH NO FURTHER PROBLEM REPORTED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080804 EU 2008 8 4 MAL2008F00011 1 20080618 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 BELLY PANEL 193AL DAMAGED 4 INCHES AFT OF GPU RECEPTACLE DOOR. REPAIRED. (K) 2 L 7 2 4T RT A52EU 20080804 SO 2008 8 4 CHQA200800133 1 20080706 A 2131 2099L011100 CONTROLLER EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007A 03030 GL CABIN PRESSURE UNCONTROLLABLE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 263SK 18938 145199 CAE311771 FLIGHT 5980, DURING CLIMB, FLIGHT CREW WAS UNABLE TO GET THE AC TO PRESSURIZE USING EITHER MANUAL OR AUTO PRESSURIZATIO N MODES. FLIGHT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. THE PRESSURIZATION SYS WAS PLACED ON MEL AND THE AC R ESUMED FLYING UNTIL THE MEL WS CLEARED ON THE 7TH. MAINT FOUND THE VACUUM LINE (P/N: 123-07692-407) LEAKING AND REPLACED IT. MANUAL PRESSURIZATION CONTROLLER WAS ALSO FOUND TO BE NOT CONTROLLING PRESSURIZATION AND IT WAS REPLACED. (A) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080804 NM 2008 8 4 DHL2008F00002 1 20080709 A 5754 STRUCTURE BOEING 727 727214 138407R NM NR 5 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 788AT BN68 21958 L/E SLAT HAS 2 SMALL CRACKS AT IB SLAT TRACK ATTACH POINT. CRACKS WERE BURNISHED OUT WITH MINIMAL MATERIAL LOSS IAW SRM 51-10-01. (K) 2 L 7 3 4F A3WE 20080804 SO 2008 8 4 CHQA200800132 1 20080706 A 3350 RPS1B BATTERY EMB 135 EMB135LR 3260305 SO ALLSN AE3007 AE3007A 03030 GL EMEGENCY LIGHTS NO TEST A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 844RP 3683 145620 CAE311813 THE FWD AND AFT EMERGENCY LIGHT STRIPS WERE NOT TESTING. IT WAS FOUND THAT THE NR 1 EMERGENCY LIGHT POWER SUPPLY WAS NOT TESTING AND WAS REPLACED. AFTER REPLACEMENT THE EMERGENCY LIGHTS FUNCTIONED NORMALLY. (A) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080805 CE 2008 8 5 S8A2008F00003 1 20080713 A 2150 73838426P1 ACM CESSNA 500 S550 2076607 CE PWA JT15 JT15D4 52112 NE OVERHEATED E S8AA O OTHER M OVER TEMP CR CRUISE 1 EA 39 91ML 8481 S5500132 APPROX 30 MILES SOUTH, AT FL410, EMERGENCY PRESSURIZATION AUTOMATICALLY ACTIVATED, FLIGHT CREW INITIATED A DESCENT AND C ONTACTED ATC. DURING DESCENT, FLIGHT CREW NOTED THAT THE CABIN ALT PRESSURIZATION CONTROLLER INDICATED THAT THE CABIN W AS ABOVE 10,000 FT WITH NO MASTER WARNING AND CONTINUED TO CLIMB TO ABOVE 15,000 FT WITH STILL NO MASTER WARNING. AT TH AT POINT O2 MASKS WERE DEPLOYED MANUAL BY FLIGHT CREW AS A PRECAUTION. FLIGHT CREW SWITCHED THE SOURCE SELECTOR TO THE LT POSITION AND THE CABIN PRESSURE CORRECTED ITSELF. THERE WERE 2 PASSENGERS, 2 FLIGHT CREW ON AC, PIC ELECTED TO DIVER T, ENROUTE, APPROACH AND LANDING WERE UNEVENTFUL. AC WAS INSPECTED WITH NO DEFECTS NOTED. GROUND RUN WAS ACCOMPLISHED 1 L 7 2 4F 4 F RT A22CE E1NE 20080805 CE 2008 8 5 GUU2008F00010 1 20080620 A 2820 10138901189 CHECK VALVE BEECH 1900 1900D 1154162 CE FUEL SYSTEM LEAKING A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 17 81536 UE152 FLIGHT 9186, DURING FLIGHT, STRONG ODOR OF FUEL IN CABIN. REPLACED LT AUX TANK TRANSFER LINE CHECK VALVE. (A) 2 L 7 2 4T RT A24CE 20080805 EA 2008 8 5 N6WA0080603 1 20080620 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 163GJ 10255 EMERGENCY LIGHT INOPERATIVE 3RD OVERHEAD LIGHT FROM FRONT. ITEM DEFERRED IAW MEL 33-51-01-2A, DMI 3877 CAT C. (S) 2 L 7 2 4F RT A21EA 20080805 NE 2008 8 5 C8G2008F00001 2 20080604 A 7320 78360018073 EEC BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE INOPERATIVE A C8GA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 29 620DL 22910 DURING CLIMB OPERATION, OIL PSI WENT TO -4, N1=0, N2=0, ENGINE SHUTDOWN. AC RETURNED TO DEPARTURE WHERE IT LANDED WITHO UT INCIDENT. TROUBLESHOT SYSTEM AND FOUND EEC TO BE AT FAULT. REMOVED AND REPLACED EEC, OPS AND LEAK CHECKS GOOD. NO OTHER DEFECTS NOTED. AC WAS RETURNED TO SERVICE. (K) 2 L 7 2 4F 4 F RT A2NM E17NE 20080805 EU 2008 8 5 M7K2008F00068 1 20080108 A 3150 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE WARNING LIGHT FAILED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 810MH 1310 3949 23209 PILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWE VER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED M UCH LONGER THAN TYPICAL THIS IS A RECURRING PROBLEM FOR THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY OF THIS MOD E AC. THIS PART CAN ON OCCASION ALSO CAUSE ENGINE FLUCTUATIONS IN FLIGHT WHEN THE RESISTANCE VALUE SIGNAL IS DISRUPTED FOR A LITTLE AS 1/20TH OF A SECOND, WHICH IS THE SAMPLE RATE FOR THE ENGINE CONTROL SYS. AN ADDITIONAL FACTOR FOR THESE TYPE OF FAULTS IS NO RESET FUNCTION AVAILABLE TO THE PILOT TO DIFFERENTIATE BETWEEN A MOMENTARY OR AN ACTIVE FAULT. ON 1 G 7 2 3U 3 U H9EU E00054EN 20080805 EU 2008 8 5 NSV2008F00009 1 20080719 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 347CJ 340B347 DURING OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYS ON A LINE CHECK 2 FLOOR PROXIMITY AND 2 COVE EMERGENCY LIGHTS WERE F OUND TO BE NOT ILLUMINATING EMERGENCY POWER SUPPLY 23LN WAS REPLACED IAW WORK CARD 33-50-02S AND SYS CHECKED GOOD. AC W AS RETURNED TO SERVICE. (K) 2 L 7 2 4T RT A52EU 20080805 EA 2008 8 5 VNA2008F00004 1 20080630 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* 30015 NE FUSELAGE DAMAGED A VNAA K NONE O OTHER IN INSP/MAINT 1 GL 05 262PS 7962 CREW REPORTED A LIGHTNING STRIKE FOUND DURING PREFLIGHT INSPECTION. MAINT PERFORMED AN ENROUTE AND DETAILED LIGHTNING S TRIKE INSPECTION. MAINT FOUND SEVERAL AREAS OF BURN DAMAGE. MAINT REPAIRED ALL DAMAGE IAW REO NR 601R-55-12-170 AND IAW THE AC MM. AIRCRAFT WAS RELEASED FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A21EA 20080805 NM 2008 8 5 BEF2008F00000 1 20080629 A 2910 NAS16128 O-RING BOEING 757 757231 1384950 NM PWA 2037 PW2040 NE HYD FILTER CRACKED A BEFA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 19 741PA 24737 AC WAS AIRBORN ENROUTE, WHEN "L HYD QTY" EICAS MESSAGE APPEARED, FOLLOWED BY "L HYD SYS PRESS" EICAS MESSAGE. AIRCRAFT RETURNED, MECHANICS FOUND HYD LEAK AT O-RING INSTALLED AT LT HYD CASE DRAIN DELTA P INDICATOR. MECHANICS REMOVED AND RE PLACED O-RING, SERVICED HYD SYS AND OPS CHECK SYSTEM, OK. AC RETURNED TO SERVICE @ 14:09Z, 4 HRS 14 MIN AFTER ARRIVING BACK. (K) 2 L 7 2 4F 4 F RT A2NM E17NE 20080805 GL 2008 8 5 Z5F2008F00002 2 20080704 A 7261 ENGINE CESSNA 525 525 2076601 CE WILINT FJ44 FJ441A GL LEFT LEAKING E Z5FA E ENGINE SHUTDOWN K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 63 418CS 525B0108 LIGHT SMOKE IN CABIN, THEN LT ENG MADE A LOUD POPPING SOUND, LOW OIL PRESSURE ILLUMINATED AND ENGINE ROLLED BACK, SHUTDO WN IN FLIGHT. AFTER LANDING, FOUND THAT ENGINE HAD LOST OIL. (COMING OUT OF TAIL PIPE, DRAIN MAST AND SG EXHAUST). AC CURRENTLY IN MAINTENANCE. WILL UPDATE UPON COMPLETION OF MAINTENANCE. (K) 1 L 7 2 4F 4 F RT A1WI E3GL 20080805 EU 2008 8 5 M7K2008F00065 1 20080108 A 3150 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE WARNING LIGHT FAILED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 808MH 479 3914 23072 PILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWE VER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED M UCH LONGER THAN TYPICAL THIS IS A RECURRING PROBLEM FOR THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY OF THIS MOD E AC. THIS PART CAN ON OCCASION ALSO CAUSE ENGINE FLUCTUATIONS IN FLIGHT WHEN THE RESISTANCE VALUE SIGNAL IS DISRUPTED FOR A LITTLE AS 1/20TH OF A SECOND, WHICH IS THE SAMPLE RATE FOR THE ENGINE CONTROL SYS. AN ADDITIONAL FACTOR FOR THESE TYPE OF FAULTS IS NO RESET FUNCTION AVAILABLE TO THE PILOT TO DIFFERENTIATE BETWEEN A MOMENTARY OR AN ACTIVE FAULT. ON 1 G 7 2 3U 3 U H9EU E00054EN 20080805 EU 2008 8 5 M7K2008F00070 1 20080108 A 3150 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE WARNING LIGHT FAILED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 806MH 3833 23220 PILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWE VER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED M UCH LONGER THAN TYPICAL THIS IS A RECURRING PROBLEM FOR THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY OF THIS MOD E AC. THIS PART CAN ON OCCASION ALSO CAUSE ENGINE FLUCTUATIONS IN FLIGHT WHEN THE RESISTANCE VALUE SIGNAL IS DISRUPTED FOR A LITTLE AS 1/20TH OF A SECOND, WHICH IS THE SAMPLE RATE FOR THE ENGINE CONTROL SYS. AN ADDITIONAL FACTOR FOR THESE TYPE OF FAULTS IS NO RESET FUNCTION AVAILABLE TO THE PILOT TO DIFFERENTIATE BETWEEN A MOMENTARY OR AN ACTIVE FAULT. ON 1 G 7 2 3U 3 U H9EU E00054EN 20080805 NM 2008 8 5 DHL2008F00003 1 20080709 A 2460 6917530 MODULE BOEING 727 727227 1384078 NM AC METER SMOKE A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 782DH 21998 WHILE SWITCHING AC VOLT SELECTOR SWITCH FROM EXTERNAL TO APU, SMOKE CAME FROM BEHIND BACK OF PNL AND VOLT AND FREQ GAGES BECAME INOP IN ALL POSITIONS, NO RESIDUAL EITHER. REMOVED AND REPLACED AC METER MODULE ASSY IAW 24-20-00. OPS CHECKS NORMAL IAW SAME DURING ALL PHASES OF OPERATION. NO FLIGHT NR. FLT 125 CANCELLED. AIRCRAFT WAS GROUNDED. (K) 2 L 7 3 4F A3WE 20080805 EU 2008 8 5 M7K2008F00077 1 20080303 A 5302 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM CRACKED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 816MH 4038 23096 CRACK FOUND DURING ROUTINE INSPECTION RADIATING FROM A SCREW HOLE TO THE EDGE OF THE MACHINED FLANGE AND ACROSS THE ENTI RE FLANGE. PART WAS REMOVED IN TWO PIECES. A NEW FITTING WAS MATCH DRILLED AND INSTALLED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080724 NM 2008 7 24 2008UALA03333 1 20080611 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 507UA 24743 DOOR 4R EXT EMERGENCY LIGHT INOP. BULB INOP. RELAMPED DOOR 4R EXT EMERGENCY LIGHT, OPS CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03330 1 20080611 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR OUT OF ADJUST A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 545UA 25323 DOOR 3R WILL NOT ARM. GIRT BAR SETTING OUT OF ADJUSTMENT. ADJUSTED GIRT BAR SETTING, ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03329 1 20080612 A 3620 MR36193 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BLEED AIR SYS FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 535UA 25130 PER CREW LEFT ENG BLEED LIGHT CAME ON. RTFL. FAN AIR TEMP SENSOR FAILURE. REPLACED FAN AIR TEMP SENSOR AND FAN AIR OV ERTEMP SWITCH. ACCOMPLISHED A HIGH POWER RUN, ALL SYSTEMS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03429 1 20080613 A 3350 362624 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 307UA 23668 EMERGENCY ESCAPE PATH FLOOR LIGHTING INOP FROM ROW 15 BACK. FOUND BURNED OUT LIGHT STRIPS. REPLACED LIGHT STRIPS OP CH ECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03416 1 20080616 A 2612 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 FIRE HANDLE BURNED OUT A UALA O OTHER P NO WARNING INDICATION IN INSP/MAINT 1 WP 29 301UA 23642 NR 2 FIRE HANDLE LIGHT OUT. FOUND BURNED OUT LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03415 1 20080616 A 2130 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 364UA 24533 PRESSURIZATION PROBLEM. RTFL. REPLACED S106 AND S805. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 2008 7 24 2008UALA03404 4 20080616 A 2565 101651205 BARREL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE UNSERVICEABLE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 644UA 25094 LEAKING BARREL. REPLACED BARREL. READY FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080724 NM 2008 7 24 2008UALA03370 1 20080615 A 2425 745329A IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE FAULTY A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 656UA 25394 RT GEN DRIVE LIGHT AND EICAS ILLUM. DISCONNECTED RT GEN PER IRREG, APU ON LINE. REPLACED RIGHT ENG. IDG IAW MM24-11-0 1 OP CHECKED GOOD, AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080725 NM 2008 7 25 2008UALA03299 1 20080609 A 3510 MF20010 OXYGEN MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CAPTAIN'S LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 854UA 1731 O2 STILL SHOWS SLOW LEAK ABOUT 100 LBS PER 20 MIN. CAPT O2 MASK HAS PIN HOLE LEAK IN HOSE. REPLACED CAPT MASK ASSY, SE RVICED CREW O2 TO FULL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 NM 2008 7 25 2008UALA03300 1 20080609 A 3510 OXYGEN BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW UNDERSERVICED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 801UA 686 CREW OXYGEN BOTTLE NEEDS SERVICE. SERVICED CREW O2 TO FULL, NO LEAKS NOTED AT TIME. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 NM 2008 7 25 2008UALA03301 1 20080609 A 3397 WIRE HARNESS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 804UA 759 EMERGENCY EEL LIGHTS AT ROWS 15A AND 24A ARE INOP. DAMAGED HARNESS TO ROW 15. REPAIRED DAMAGED HARNESS. ALL LIGHTS TE ST GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 NE 2008 7 25 VNAA0805013 2 20080509 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RIGHT CONTAMINATED A VNAA A UNSCHED LANDING C B F.O.D. SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 05 246PS 7920 CREW REPORTED A STRONG CHEMICAL ODOR COMING FROM VENTILATION SYSTEM. CREW ELECTED TO RETURN TO DAY AND LANDED WITHOUT I NCIDENT. MAINTENANCE INSPECTED AND FOUND THE RIGHT ENGINE WASH FROM THE PREVIOUS NIGHTS MAINTENANCE CAUSING THE SMELL. MAINTENANCE PERFORMED ENGINE GROUND RUNS TO DISSIPATE THE SOLUTION IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. NO CHEMICAL SMELLS AFTER GROUND RUNS AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080725 NM 2008 7 25 2008UALA03459 1 20080617 A 2730 341203 ROD END AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE ELEVATOR WORN A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 802UA 690 AIRFRAME VIBRATION ON CLIMBOUT. *S/D* LEFT OUTBOARD BLUE ELEVATOR ACT ROD END HAS PLAY. REPLACED LT OUTBOARD ELEV ROD . 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 NM 2008 7 25 2008UALA03233 1 20080606 A 3150 WARNING SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 117UA 28810 WARNING & MONITORING INSTRUMENTS UNRELIABLE. RTFL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080805 SW 2008 8 5 PNS2008F00005 1 20080404 A 5400 STRUCTURE SWRNGN SA227 SA227* SW NACELLE DAMAGED E PNSA O OTHER O OTHER NR NOT REPORTED 1 AL 03 650PA AC775B AC TO BE EXTENSIVELY DAMAGED FROM AN APPARENT HARD LANDING. FLIGHT CREW STATED THEY WERE UNAWARE WHERE OR HOW THE DAMAG E WAS MADE. THE DAMAGE WAS NOTICED WHEN MAINT MOVE THE AC TO THE HANGER FOR OTHER MAINTENANCE. THE BULK OF THE DAMAGE CONSIST OF BOTH ENGINE NACELLE`S BULKED AND WRINKLED, BOTH WINGS IB OF NACELLES WRINKLED, WRINKLES AND SHEARED RIVETS IN MAIN GEAR WELL AREAS. THE AC WAS TAKEN OUT OF SERVICE PENDING FINAL DECISION ON DISPOSITION OF AC. (K) 2 L 7 2 4T RT A5SW 20080805 CE 2008 8 5 DXTA200803167 1 20080710 A 3150 WARNING MESSAGE CESSNA 680 680CE 2076811 CE ILLUMINATED E DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 377QS 6800187 CYAN MESSAGES "AP FAIL L-R AND YD FAIL A-B" IN FLIGHT AT FL 370. (A) 2 L 7 2 4F RC T00012WI 20080805 NM 2008 8 5 PID2008F00008 1 20080719 A 3350 7637 BULB BOEING 737 737291 138448W NM EMERGENCY LIGHTS INOPERATIVE A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 583CC 21069 L1 DOOR EMERGENCY LIGHT INOP. REPLACED BULB, REF MM 33-51-0. (A) 2 L 7 2 4F A16WE 20080805 NM 2008 8 5 RYN2008F00008 1 20080723 A 2997 GROUND WIRE BOEING 757 757231 1384950 NM HYD SYSTEM DAMAGED A RYNA O OTHER N FALSE WARNING NR NOT REPORTED 1 CE 07 151GX 24451 LT HYDRAULIC LOW PRESSURE LIGHT AND PTU STATUS MESSAGE APPEARED ON EICAS SCREEN. REPAIRED GROUND WIRE AT THE DISCONNECT (D6240) LEFT PYLON AREA, SYSTEM OPS CHECKED NORMAL. (A) 2 L 7 2 4F RT A2NM 20080805 EA 2008 8 5 COMA0860319 1 20080708 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 640 S9L CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 918CA 7018 DURING FA 640 FRAME INSPECTION FOUND 640 FRAME CRACKED ON LT SIDE AT STRINGER 9 CUTOUT. CUT OUT DAMAGED SECTION OF FRAM E AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH REO 601R-53-61-557. (A) 2 L 7 2 4F RT A21EA 20080805 NM 2008 8 5 F3LA200800317 1 20080608 A 5320 D5367302100000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 77 1851 REFERENCE NON ROUTINE C044396. DURING C4 S1 C CHECK INSPECTION NOTED AFT PIT TRANSITION PANEL 151AE HAS PUNCTURE DAMAGE . MAINTENANCE REMOVED DAMAGE, CLEANED PANEL AND REPAIRED PUNCTURE DAMAGE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53- 02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 SO 2008 8 5 C2XA08IA145 1 20080624 A 2510 7021170951 CONTROL PANEL EMB 145 EMB145XR 3260214 SO COCKPIT SHORTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14116 22761 22761 145672 FLIGHT 2885 - THE FLIGHT CREW REPORTED A BURNING SMELL EMANATING FROM THE FLIGHT DIRECTOR PANEL. THE PANEL WAS REPLACED . OPERATIONALLY TESTED AND THE DISCREPANCY CLEARED. (S) 2 L 7 2 4F RT 20080805 NM 2008 8 5 F3LA200800320 1 20080610 A 5321 D5361060500100 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 REFERENCE NON ROUTINE C044797. DURING C4 S1 C-CHECK INSPECTION NOTED PANEL 222FF HAS SEVERE CORROSION ON BOTTOM SIDE. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF WORK CARD CP753-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 SO 2008 8 5 CHQA200800125 1 20080625 A 3350 100865 BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 564RP 8087 145524 CAE312502 MAINTENANCE FOUND THAT THE OVERWING EMERGENCY LIGHTS INOP DURING TEST. THE NR 4 EMERGENCY LIGHT BATTERY WAS REPLACED AN D THE OVERWING LIGHTS OPERATED NORMALLY. (A) 2 L 7 2 4T RT T00011AT 20080731 NM 2008 7 31 HNAA0800190 1 20080601 A 5210 DOOR DHAV DHC8 DHC8102 2809003 NM AIRSTAIR OUT OF ADJUST A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 940HA 40264 321 AIRSTAIR DOOR INSIDE HANDLE IS HARD TO OPEN. DFRL 05JUN08 14:27 AVP MT LUBED DOOR STOPS NO FIX. FERRY ACFT TO MDT FOUN D DOOR TO BE HANGING UP AT THE SILL AREA. ADJUSTED DOOR IAW 8M/M 52-10-00. OPS CHECK OK. (S) 2 H 7 2 4T RT A13NM 20080731 EU 2008 7 31 YEN2008F00002 1 20080601 A 2121 20092455102 COOLING FAN AIRBUS 320 A320232 3930326 EU E/E BAY SMOKE A YENA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 EA 15 564JB 10841 2020 AIR TURN BACK, DECLARED EMERGENCY, AFT AVIONICS SMOKE ALARM, REMOVED AND REPLACED AFT RACK COOLING FAN IAW LTV MM 23-39- 00, OPS CHECK GOOD IAW MM 23-30-00. (K) 2 L 7 2 4F RT A28NM 20080731 EU 2008 7 31 YEN2008F00009 1 20080619 A 2530 COFFEEMAKER AIRBUS 320 A320232 3930326 EU GALLEY ODOR A YENA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 15 646JB 2945 IN CRUISE, HAD ELECTRICAL FUMES IN FAT GALLEY APPROX 5 MIN, IT DISSIPATED C/W TSM 23-39-00-810-801. NO FAULTS FOUND AND NO DAMAGE NOTED DUE TO LTV SYS, OPS TEST NORMAL AT THIS TIME. ACCOMPLISHED TSM TASK 24-00-00-810-823. ELECTRICAL BURN ING ODOR OR FUMES IN CABIN. NO DEFECTS OR DAMAGE FOUND. FOUND COFFEE MAKER BIN 507 HAD A BURNED ODOR, ALL 3 HIGH VOLT CB POPPED. REMOVED AND REPLACED COFFEE MAKER BIN 507 IAW AMM 25-35-15-04, OPS AND LEAK CHECK NORMAL. 2 L 7 2 4F RT A28NM 20080731 NE 2008 7 31 C8G2008F00000 2 20080603 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D17R 52049 NE NR 3 LOCKED A C8GA A UNSCHED LANDING R X J PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 SO 29 89427 70565 21365 656881 DURING APPROACH, THE NR 3 ENGINE COMPRESSOR STALLED AND ENGINE FLAMED OUT. THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED N1 WAS UN-MOVEABLE. REMOVED AND REPLACED NR 3 ENGINE, OPS AND LEAK CHECKS GOOD. NO OTHER DE FECTS WERE NOTED. AC WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F 4 F A3WE E2EA 20080801 WP 2008 8 1 08FDEA02090 1 20080602 A 5730 ARB126331 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 357FE 46939 LEFT WING INBD LOWER L/E PANEL 516 DB IS CHAFED AT THE CONTACT SURFACE. REMOVED PANEL. BLENDED OUT CHAFFED AREA. FABR ICATED; PRIMED & BONDED THE REPAIR DOUBLER IAW SRM 57-00-01 VOL II PG 31 & EA 8-5720-118511. EDGE SEALED, PRIMED & PAINTED IAW SRM 51-71-00 VOL II & EA 8-5720-118511. INSTALLED PANEL IAW SRM 51-31-01 VOL II & EA 8-5720-118511. 2 L 7 3 4F RT A22WE 20080801 NM 2008 8 1 2008UALA02984 1 20080525 A 4900 B556902 ACTUATOR BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE APU MALFUNCTIONED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 217UA 30550 UNABLE TO GET BLEED AIR FROM APU. STATUS MSG'S APU & APU BLEED AIR WITH MAINT MSG'S 49-10990 INLET GUIDE VANE ACTUATOR DOES NOT FOLLOW COMMAND AND 49-10980 INLET GUIDE VANE ACTUATOR LVDT CIRCUIT FAILED. SFOLM REPLACED THE INLET GUIDE VANE ACTUATOR. THE APU OPS CHECKED OK. NO ADDITIONAL SHOP INFORMATION IS AVAILABLE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080804 NM 2008 8 4 08FDEA02569 1 20080630 A 5210 65643811U PANEL BOEING 727 727225 1384077 NM PAX DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 PANEL RACK: FWD ENTRY DOOR LINER, SLIDE PACK PANEL CRACKED AT CUT OUTS. REMOVED AND REPLACED DOOR LINER SLIDE PAN REF S RM 51-30-02 PG 13-14. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080804 WP 2008 8 4 08FDEA02576 1 20080630 A 5313 ADA3003505 LONGERON DOUG DC10 DC1010 3022110 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 FWD CARGO COMPT TUNNEL AREA FOUND CORROSION WITH EXFOLIATION. 2 L 7 3 4F A22WE 20080804 SO 2008 8 4 LR7A08087 1 20080701 A 5312 3425828L BULKHEAD LKHEED 382 382G 526414U SO FS 880 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 636 4763 DURING SCHEDULED B-2 CHECK, PER JOB CARD HB5302, FOUND LT AFT FUSELAGE INTERIOR LOWER BULKHEAD WEB CRACKED THROUGH FASTE NER HOLE AT FS 880L, WL200. REPAIR IAW DRAWING 342582 BY FABRICATING AND INSTALLING WEB. 2 H 7 4 4T A1SO 20080804 SW 2008 8 4 WGEA2008000064 1 20080617 A 2621 FX002002 CARTRIDGE ECLIPS EA500 ECLIPSEEA500 3350000 SW FIRE EXTING FAILED A WGEA O OTHER O OTHER NR NOT REPORTED 1 EA 27 163DJ 95 000081 NR 2 ENGINE FIRE EXTINGUISHING AGENT LEAKING. REPLACED FIREX CARTRIDGE WITH SERVICEABLE UNIT. PER EA 500 AMM 26-20-00. (A) 1 L 7 2 4J RT A00002AC 20080804 EU 2008 8 4 08FDEA02498 1 20080626 A 5315 A53778807202 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND OLD UPPER FLANGE SPLICE REPAIR AT FWD CARGO FLOOR STRUCTURE C 27 RT WITHOUT ANY DOCUMENTATION. REPAIR RENEWED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02825 1 20080711 A 5754 A57863251162 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CHAFING MARKS ON LOWER SKIN AT RIB 21, LT SLAT NR 1 REPAIR PERFORMED BY CUT OUT THE DAMAGED SKIN AND INSTALLING AN EXTERNAL DOUBLER IAW RAS/FOK/098/2008 ISS A, APPROVED BY EA 6-5742-120040. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02594 1 20080701 A 5315 A53974322214 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON CROSS BEAM C 63 OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02595 1 20080701 A 5320 A53974341200 FLOOR SUPPORT AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND OLD FILLER REPAIR IN AFT CARGO COMPARTMENT AT FLOOR STRUCTURE C 63-64, Y 805. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02573 1 20080630 A 5230 A52378014204 SKIN AIRBUS 310 A310203 3930313 EU CARGO DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 423FE 281 BULK CARGO DOOR SKIN HAS GOUGE MEASURING 1.0 SQ IN BY .030 IN DEEP, LOWER AFT EXTERNAL SURFACE SMOOTHED OUT GOUGE AND IN STALLED EXTERNAL SKIN REPAIR ON BULK CARGO DOOR SKIN BETWEEN FR 68 AND FR 69 LOWER AFT IAW A310-200 SRM 52-30-00, FIG 20 3, PG 215/216. 2 L 7 2 4F RT A35EU 20080804 NM 2008 8 4 KCSA081296 1 20080622 A 5315 FLOORBEAM BOEING 747 747122 1384872 NM BS 1265 RBL 108 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STA-1265 FLOOR INTERCOSTAL, UPPER CHORD HAS CORROSION ON AFT SIDE UPPER FLANGE RBL-108 AT NUT PLATE HOLES. (B) 2 L 7 4 4F RT A20WE 20080804 WP 2008 8 4 08FDEA02297 1 20080617 A 5311 AGA00163 FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 AFT BAGGAGE COMPARTMENT FRAME AT BS 1853 RBL 12 TO LBL 12 HAS CORROSION. REMOVED CORROSION IN REF TO SRM 51-21-01; VOL II. ORIGINAL THICKNESS 0.071 IN REF TO SRM 51-10-01; VOL III. REMOVED 0.017. REMAINING THICKNESS IS 0.054. AREA IS O UT OF LIMITS IN REF TO SRM 53-00-01; FIG 1-B; VOL I. REPAIRED AREA IN REF TO SRM 53-30-00; VOL I; FIG 8. 2 L 7 3 4F RT A22WE 20080804 NM 2008 8 4 KCSA081276 1 20080611 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 1800 RBL 59 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 709CK 20247 AFT PIT FLOORBEAM WEB CRACKED NEAR TOP AT BS 1800, RBL-59. (B) 2 L 7 4 4F RT A20WE 20080804 NM 2008 8 4 AALA200801697 1 20080624 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 788AN 30011 DFW - EMERGENCY LIGHT AT SEAT 20C LENS BROKEN. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080804 EA 2008 8 4 A6WA200840496 1 20080609 A 5210 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 PAX DOOR AFT STIFFENER ON AFT WEB 601R3117745-7 CRACKED. PAX DOOR AFT STIFFENER ON AFT WEB REPLACED IAW SRM 51-42-06 & SRM 51-42-13. (A) 2 L 7 2 4F RT A21EA 20080804 2008 8 4 A6WA200840490 4 20080605 A 3417 8220372445 ADC CNDAIR CL600 CL6002B19 1900309 EA NR 1 FAULTED A A6WA O OTHER J WARNING INDICATION LD LANDING 1 GL 31 401AW 12705 7280 RECEIVED ADC NR 1 FAILURE INDICATION WITH MACH TRIM CAS MESSAGE DURING APPROACH. REMOVED AND REPLACED AIR DATA COMPUTER NR 1. (A) 2 L 7 2 4F RT A21EA 20080804 NM 2008 8 4 AALA200801706 1 20080625 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT 31C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 31C. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080725 NM 2008 7 25 CALA0800642 1 20080623 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM BS 867 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 LEFTHAND SIDE STATION 867 FRAME BETWEEN S-8 AND S-9 AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED LEFTHAND SIDE STATION 867 FRAME BETWEEN S-8 AND S-9 PER EA 5310-04498 OPERATION 02. 2 L 7 2 4F RT A16WE 20080725 NM 2008 7 25 CALA0800644 1 20080623 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM BS 747 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 LEFTHAND SIDE STATION 747 FRAME BETWEEN S-8 AND S-9 AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED FRAME AT STATION 747L BETWEEN S-8 AND S-9 PER EA5310-04498 OPERATION 02. 2 L 7 2 4F RT A16WE 20080725 NM 2008 7 25 CALA0800637 1 20080623 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM BS 827 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 LEFTHAND SIDE STATION 827 FRAME BETWEEN S-8 AND S-9 AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED FRAME AT STATION 827 BETWEEN S-8 AND S-9 A/C BRACKET MOUNT PER EA5310-04498, OPERATION 02. 2 L 7 2 4F RT A16WE 20080725 NM 2008 7 25 2008UALA01816 1 20080401 A 5100 UNKNOWN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU UNKNOWN A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 308UA 23669 FLIGHT DIVERTED DUE TO CRACKING NOISE IN FRONT OF A/C. *S/D* COULD NOT FIND CAUSE OR DUPLICATE NOISE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080725 EU 2008 7 25 2008UALA03114 1 20080602 A 7500 GA554912 TRANSDUCER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 BLEED MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 470UA 1427 CABIN TEMPERATURE PROBLEM. RTFL. *S/D* FOUND PRESS BLEED TRANSDUCER ON NR 2 ENG BAD. REPLACED PRESS BLEED TRANSDUCER , RAN ENGS. PACK TEMPS AND CONDITION AIR OPS NORMAL. ALSO REPLACED AFT CABIN TRIM VALVE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 EU 2008 7 25 2008UALA03159 1 20080602 A 3350 SIGN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 444UA 824 AT DOOR 1L - EXIT LIGHT AT LOWER LEFT SIDE IS LOOSE. *S/D* SIGN IS BROKEN. REPLACED EMERGENCY EXIT SIGN AT LEFT LOWER DOOR 1L. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 NM 2008 7 25 2008UALA03367 1 20080614 A 2121 033638500 BLOWER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EQUIP COOLING FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 643UA 25093 EQ COOLING OVERHEAT INDICATION. RTFL. AFTER TROUBLESHOOTING SUSPECT FWD CARGO DETECTOR BLOWER AT FAULT. REPLACED FWD CARGO DETECTOR 2. MSG CLEARED. TEST NORMAL. REPLACED EQUIP COOLING FWD RACK EXHAUST FAN ACCT NOISY. EQ COOLING EXHAUST H AS LOW AIR FLOW. REMOVED DAMAGED FILTER SCREEN FROM DUCT BELOW ACRU, EXH AIRFLOW OK. REPLACED THE LOW FLOW DETECTOR P/N 11197-5MOD1. REPLACED THE EQ COOLING OVERHEAT SWITCH S41 P/N 3000-46-12. REPLACED THE EQ COOLING INDICATION CARD M867 IN THE P50 PANEL. 2 L 7 2 4F 4 F RT A1NM E24NE 20080725 NM 2008 7 25 2008UALA03500 1 20080620 A 3510 OXYGEN MASK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW LEAKING A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 386UA 24661 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. SUSPECT PRE FLIGHT CHECKS. LEAK CHECKED O2 BOTTLES, MASK BOX. SUSPECT CAPTAINS O2 MASK. SWAPPED OBSERVERS MASK WITH CAPTAIN'S MASK. REPLACED OBSERVERS MASK WITH NEW MASK SERVICE D O2 TO 1800 PSI. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080725 NM 2008 7 25 2008UALA03502 1 20080620 A 3510 OXYGEN BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW SYS READS LOW A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 849UA 1649 COCKPIT OXYGEN BOTTLE LOW. *S/D* SERVICED CREW O2 TO FULL, NO LEAKS NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 NM 2008 7 25 2008UALA03505 1 20080622 A 5310 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 811UA 847 BEAM NR 155 FOUND CORRODED. *S/D* ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED CORRODED BEAM 155 CONT OF AMIS ITEM 51420 16. BEAM 155 BEGAN TRANSFER OF BRACKETS AND DRILLING MOUNTING HOLES. CONT OF AMIS ITEM 5142023 -INSTALLED BEAM 155. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 NM 2008 7 25 2008UALA03510 1 20080621 A 5310 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 811UA 847 BEAM 90 FOUND CORRODED. *S/D* ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED BEAM AND ATTACHING BRACKETS. CONT OF AMIS IT EM 5142024 INSTALLED BRACKETS ON NEW BEAM PICKED UP HOLES FOR AFT SPLICE PLATE. BEAM BUILT UP, PAINTED AND INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 NM 2008 7 25 CALA0800635 1 20080623 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 787 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 LEFTHAND SIDE STATION 787 FRAME BETWEEN S-8 AND S-9 AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED CRACKED LEFTHAND FRAME STATION 787 BETWEEN S-8 AND S-9 A/C BRACKET MOUNT REF EA5310-04498 OP 02. 2 L 7 2 4F RT A16WE 20080725 EA 2008 7 25 VNAA0805009 1 20080506 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS MALFUNCTIONED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 207PS 7873 CREW REPORTED A FLAPS FAIL AT 20 DEGREES WARNING MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO LEX AND LANDED WITHOU T INCIDENT. MAINTENANCE INSPECTED AND PERFORMED A FUNCTIONAL TEST OF THE FECU BIT TEST SKEW DETECTION. SYSTEM OPS CHEC KED GOOD AND MESSAGE CLEARED IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080725 EA 2008 7 25 VNAA0805025 1 20080519 A 3244 18X44 TIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NLG WORN A VNAA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 05 248PS 59 7925 CREW REPORTED THE NOSE GEAR MADE A STRANGE THUMPING SOUND DURING RETRACTION. CREW ELECTED TO CONTINUE ON TO CLT, REQUES TED EMERGENCY EQUIPMENT TO STAND BY. THE AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE TIRES IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080725 EA 2008 7 25 SWIA200819832 1 20080701 A 2910 LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA O OTHER K FLUID LOSS NR NOT REPORTED 1 NM 07 472CA 7667 FLT 2685 - HYDRAULIC SYSTEM NR 2 QUANTITY WENT TO ZERO. REPLACED LEAKING PRESSURE SERVICE LINE ON THE MANIFOLD IAW AMM 29-11-05. 2 L 7 2 4F RT A21EA 20080725 SO 2008 7 25 SWIA200819819 1 20080622 A 5210 HANDLE EMB 120 EMB120ER 3260203 SO PAX DOOR WORN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 224SW 120294 FLT 3632 - MAIN CABIN DOOR DOES NOT OPEN PROPERLY FROM INSIDE THE CABIN. REPLACED INNER PAX DOOR HANDLE IAW AMM 52-11-0 1. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080725 EA 2008 7 25 SWIA200819833 1 20080704 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BROKEN A SWIA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 NM 07 440SW 7589 FLT 3752 - CEILING EMERGENCY EXIT SIGN FELL DOWN INFLIGHT. REPLACED LENS AS REQUIRED. 2 L 7 2 4F RT A21EA 20080725 EA 2008 7 25 SWIA200819838 1 20080705 A 5610 1393222 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAULTY A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 412SW 7101 FLT NR 3781 - "R WINDOW HEAT" CAUTION MESSAGE COMES ON IN FLIGHT. REPLACED RIGHT SIDE WINDOW. OPS CHECKS GOOD IAW MM 5 6-12-0. 2 L 7 2 4F RT A21EA 20080725 EA 2008 7 25 SWIA200819820 1 20080629 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 416SW 7089 FLT 1001 - FIRST OFFICERS WINDOW IS BROKEN. REPLACED RIGHT WINDOW IAW MM 56-12-01. OPS AND LEAK CHECK GOOD, PN NP13932 2-6, S/N OFF 01047H1052. 2 L 7 2 4F RT A21EA 20080725 EA 2008 7 25 SWIA200819822 1 20080624 A 7830 SWITCH CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER OUT OF ADJUST A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 464SW 7827 FLT NR 4000 - R REV UNLOCKED CAUTION MESSAGE ON CLIMB-OUT. ADJUSTED RIGHT THRUST REVERSER STOW SWITCH IAW MM 78-37-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080725 EA 2008 7 25 SWIA200819823 1 20080625 A 5210 CAM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 417SW 7400 FLT 2804 - PAX DOOR IS DIFFICULT TO OPEN. INSPECTED AND LUBRICATED DOOR CAMS AND DOOR ASSIST MECHANISM. OPS CHECK GOOD . 2 L 7 2 4F RT A21EA 20080725 EA 2008 7 25 SWIA200819844 1 20080711 A 3231 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR FAULTY A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 427SW 15467 15467 7497 FLT 4083 - RECEIVED A "GEAR DISAGREE" AND "NOSE DOOR" WARNING MESSAGES. GEAR THEN LOCKED DOWN AND NOSE DOOR CLOSED. RE PLACED THE NOSE LANDING GEAR HYDRAULIC SELECTOR VALVE IAW CRJ MM 32-33-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080725 EA 2008 7 25 SWIA200819847 1 20080709 A 3260 SWITCH CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A SWIA O OTHER N FALSE WARNING AP APPROACH 1 NM 07 408SW 7055 FLT 4112 - NOSE GEAR DID NOT INDICATE DOWN AND LOCKED WHEN SELECTING GEAR DOWN. REPLACED RIGHT NOSE DOOR OPEN MICROSWIT CH PER AMM 32-61-15. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080725 SO 2008 7 25 SWIA200819852 1 20080710 A 3097 TERMINAL EMB 120 EMB120ER 3260203 SO WINDSHEILD HEAT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 294SW 120321 FLT 5705 - NOTICED SMOKE COMING FROM THE BASE OF THE RIGHT WINDSHIELD ON CLIMB-OUT. INSPECTED AND SECURED WINDSHIELD HE AT TERMINALS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080725 CE 2008 7 25 FLH2008F00000 1 20080510 A 2131 CONTROLLER LEAR 45 45LEAR 5170805 CE CABIN PRESSURE FAILED E FLHA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 21 345MA 054 AIRCRAFT WAS AT CRUISE PHASE OF FLIGHT AT FL450 ON 5/10/2008 AT 1840 HOURS WHEN THE PLANE EXPERIENCED A GRADUAL DEPRESSU RIZATION AND HAD TO MAKE AN EMERGENCY DECENT AND UNSCHEDULED LANDING. THE AIRCRAFT WAS MOVED TO SERVICE CENTER FOR COMP REHENSIVE TESTING OF THE PRESSURIZATION SYSTEM TO DETERMINE THE CAUSE OF THE FAILURE. AT THIS TIME SB 45-21-13 IS BEING INCORPORATED TO REPLACE THE CABIN PRESSURE CONTROLLER. AFTER ALL WORK WAS PERFORMED THE CONSENSUS IS THAT THE CABIN PRE SSURE CONTROLLER WAS THE ROOT CAUSE OF FAILURE. (K) 2 L 7 2 4F RT T00008WI 20080725 WP 2008 7 25 MT92008F00004 2 20080619 A 7200 NAS42HT648 SPACER SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP PPC SHAFT MISINSTALLED E MT9A O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 05 26932 AC660 IN FLIGHT, THE PPC INPUT LEVER TO THE PPC SHAFT CAME OFF AND PREVENTED THE CREW FROM BEING ABLE TO RETARD THE POWER TO T HE LT ENGINE. THIS FORCED THEM TO DO AN INFLIGHT SHUTDOWN OF THAT ENGINE. THE INVESTIGATION FOUND THAT THE SCREW AND S PACER THAT SECURES THE ARM TO THE SHAFT WAS NOT INSTALLED. FURTHER INVESTIGATION SHOWED A DISCREPANCY BETWEEN THE MM A ND THE IPC MANUAL FOR INSTALLING THESE PARTS IAW TO AC SN. THE OLDER SN AC (BELOW AC664) ARE NOT INSTRUCTED TO INSTALL THEM (71-00-15 (5) (D). ALSO, THE IPC CONTRADICTS ITSELF 76-10-40, FIG 7 CALLS FOR THE INSTALLATION OF THESE PARTS FOR SN 420-683 HOWEVER 76-10-50 LIMITS INSTALLATION OF THESE PARTS TO SN 664-683. (K) 2 L 7 2 4T 4 T RT A8SW E4WE 20080725 NM 2008 7 25 HNA2008F00004 1 20080709 A 3350 6013211X POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE EMERGENCY LIGHTS BROKEN A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 816EX 39912 329 RT FWD EMERGENCY LIGHT IS DIM. REMOVED AND REPLACED BATTERY, FOUND CAMLOCK ON BATTERY BROKEN CAUSING LOOSE CONNECTION. OPS CHECK GOOD. (K) 2 H 7 2 4T 4 T RT A13NM E20NE 20080725 NM 2008 7 25 DHL2008F00000 1 20080702 A 5754 PIN BOEING 727 727264 138408M NM PWA JT8 JT8D17 52049 NE RT WING L/E DAMAGED A DHLA O OTHER O OTHER NR NOT REPORTED 1 GL 05 765AT 23014 SMALL DAMAGE ON NR (6) L/E SLAT AT IB GUIDE PIN EXISTING DOUBLER. DAMAGE WAS BLENDED SMOOTH LESS THAN 1 INCH X .100 MAT ERIAL LOSS, WORK ACCOMPLISHED IAW SRM 57-50-01. (K) 2 L 7 3 4F 4 F A3WE E2EA 20080722 NM 2008 7 22 SWAA083678 1 20080702 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 716SW 27850 DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. R&R LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080722 WP 2008 7 22 ABXA080166 1 20080520 A 5311 9919619504N FRAME DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 RIGHT AFT MAIN FRAME FS 737, FRAME CRACKS EXCEEDS LIMITS OF EXSISTING 5935650. FRAME HAD CRACKS AT FORWARD POINTS H & I AND AFT FLANGE POINTS G & J. REMOVED & REPLACED MAIN FRAME IAW DC9 SRM. (A) 2 L 7 2 4F A6WE 20080722 WP 2008 7 22 ABXR080168 1 20080502 A 2761 3923259501 SUPPORT DOUG DC9 DC915F 3022037 WP LT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 783AX 47010 LEFT WING OUTBOARD SPOILER HAD OUTBOARD ACTUATOR BRACE CRACKED. REMOVED AND REPLACED OUTBOARD ACTUATOR BRACE IAW DC9 SR M 51-30-1, 51-30-2, AND 51-30-5. (A) 2 L 7 2 4F A6WE 20080804 NM 2008 8 4 2008UALA03660 1 20080701 A 5420 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 NACELLE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 517UA 24861 NR 2 ENG FWD PYLON HYDRAULIC PRESSURE LINE FEED THROUGH ELBOW IS LOOSE AND WEARING INTO FIRE WALL. *S/D* ACCOMPLISHED MAJOR REPAIR IN SFO. REPAIRED PYLON WEB PER MM 54-51-95. 2 L 7 2 4F 4 F RT A2NM E17NE 20080804 NM 2008 8 4 2008UALA03669 1 20080701 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 590UA 28708 RIGHT FWD EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOP. S/D* WORN CONTACTS, BULB INOP. REPLACED CONTACT AND ASSY, OP C HECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080804 SO 2008 8 4 C2XA08ON135 1 20080615 A 2612 FIRE DETECTOR EMB 145 EMB145LR 3260212 SO ENGINE MALFUNCTIONED A C2XA O OTHER P NO WARNING INDICATION CR CRUISE 1 SW 27 22909 16530 13275 145459 FLT 7804 - LAX - FLIGHT CREW REPORTED ENG DETECTION FAIL ON DESCENT. MX RESET FIRE DETECTION SYSTEM. OPERATIONALLY CHE CKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080804 NE 2008 8 4 2008UALA03649 2 20080629 A 7230 BLADES BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 726555 RIGHT ENGINE, BLADE 10 IS 'TORN' AT END. BADLY DAMAGED. *S/D* UNKNOWN FOD DAMAGE. REPLACED NR 2 ENG 1ST STAGE FAN BL ADES 10 AND 28, ACCOMPLISHED ENG RUNS, SATISFACTORY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080804 CE 2008 8 4 AJC2008F00000 1 20080613 A 7500 99124862 HEAT EXCHANGER CESSNA 560 560XL 2076702 CE BLEED SYSTEM CRACKED E AJCA O OTHER J WARNING INDICATION CR CRUISE 1 EA 65 90CF 5605080 LEVELED OFF AT 10,000 MSL 40 MILES FROM LANDING ON LEVEL OFF WE SELECTED CLIMB POWER TO ACCELERATE THE AC IAW ATC REQUES T. RT ENGINE FIRE LIGHT CAME ON, ITT 680C, N2 98 PERCENT N1 90 PERCENT. RETARDED RT THROTTLE SLIGHTLY AND LIGHT WENT O UT IMMEDIATELY. NO SECONDARIES, LANDED. IT WAS THE NEAREST SUITABLE AIRPORT. MAINT FOUND LEAK IN BLEED AIR PRECOOLER DUCT SEAL. (K) 2 L 7 2 4F RT A22CE 20080805 EU 2008 8 5 M7K2008F00078 1 20080303 A 5302 350A23422220 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 812MH 128 3956 23179 CRACK FOUND DURING ROUTINE INSPECTION RADIATING FROM A SCREW HOLE TO THE EDGE OF THE MACHINED FLANGE. A NEW FITTING WAS MATCH DRILLED AND INSTALLED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080805 EU 2008 8 5 M7K2008F00071 1 20080303 A 3150 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE WARNING LIGHT DEFECTIVE E M7KA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 847MH 4266 23416 PILOT REPORTS AMBER GOVERNOR LIGHT ILLUMINATED DURING FLIGHT. A FAULT CODE WAS GENERATED INDICATING THE POTENTIOMETER A S THE LIKELY DEFECTIVE UNIT. A NEW PART WAS INSTALLED AND NO FURTHER DEFECTS WERE NOTED. THIS IS A RECURRING PROBLEM FO R THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY FOR THIS AC MODEL. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080805 CE 2008 8 5 DXTA200803175 1 20080714 A 2100 MOTOR CESSNA 500 560CESSNA 2076750 CE FREON VENT FAILED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 839QS 5600690 SMOKE OBSERVED COMING FROM FREON AIR VENTILATION DUCT ON UNDERSIDE OF AIRCRAFT. BURNING ODOR LIKE INSULATION THROUGHOUT AIRCRAFT. SUSPECT WINDINGS ON MOTOR FOR FREON AIR FAILED. NO OTHER DAMAGE NOTED AFTER INSPECTION. MX DETERMINED TO BE FR EON MOTOR. (A) 2 L 7 2 4F RT A22CE 20080805 EU 2008 8 5 M7K2008F00066 1 20080108 A 3150 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE WARNING LIGHT FAILED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 812MH 967 3956 23072 PILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWE VER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED M UCH LONGER THAN TYPICAL THIS IS A RECURRING PROBLEM FOR THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY OF THIS MOD E AC. THIS PART CAN ON OCCASION ALSO CAUSE ENGINE FLUCTUATIONS IN FLIGHT WHEN THE RESISTANCE VALUE SIGNAL IS DISRUPTED FOR A LITTLE AS 1/20TH OF A SECOND, WHICH IS THE SAMPLE RATE FOR THE ENGINE CONTROL SYS. AN ADDITIONAL FACTOR FOR THESE TYPE OF FAULTS IS NO RESET FUNCTION AVAILABLE TO THE PILOT TO DIFFERENTIATE BETWEEN A MOMENTARY OR AN ACTIVE FAULT. ON 1 G 7 2 3U 3 U H9EU E00054EN 20080805 EA 2008 8 5 HNA2008F00024 1 20080618 A 2530 180140 COFFEEMAKER DHAV DHC8 DHC8311 1386006 EA GALLEY BURNED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 07 333EN 34796 221 HOT JUG IN WARMER NR 1 HAS BURNING SMELL. REPLACED HOT JUG. FOUND ONE BURNED PIN IN OLD JUG. (K)- 2 H 7 2 4T RT A13NM 20080805 CE 2008 8 5 DXTA200803177 1 20080715 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE MLG WEAK E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 367QS 5600367 BOTH F/O-SIDE BRAKE PEDALS ARE VERY MUSHY. THEY TRAVEL 3/4 OF THE WAY DOWN BEFORE BREAKING OCCURS. (A) 2 L 7 2 4F RT A22CE 20080805 EA 2008 8 5 S9BA2008026 1 20080802 A 5411 C6W1512141 LONGERON DHAV DHC6 DHC6300 2802606 EA RT NACELLE CRACKED A S9BA O OTHER O OTHER NR NOT REPORTED 1 SO 29 888PV 620 RT HAND NACELLE INBOARD LONGERON CRACKED 10 1/2 INCHES AFT OF THE FWD END. REMOVED AND REPLACED RT HAND INBD LONGERON I AW AC 4313-1B CH 4, RD 6-54-036 AND VERIFIED MOD 6/1655 IS INSTALLED PER AD 80-13-12 R1. (A) 1 H 7 2 3T RT A9EA 20080805 SO 2008 8 5 C2X2008F00008 1 20080721 A 2432 32845001 BATTERY EMB 145 EMB145EP 3260221 SO MASTER OVERTEMP A C2XA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 NM 13 12934 145019 LCH - FLIGHT 2830, THE CREW REPORTED A BATTERY 2 OVERTEMP WARNING ON EICAS. THE AIRCRAFT DIVERTED TO LCH WHERE IT LANDE D WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO BATTERY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080805 NM 2008 8 5 F3LA200800321 1 20080610 A 5321 D5361087600000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 77 1851 REFERENCE NON ROUTINE C044794. DURING C4 S1 C-CHECK INSPECTION NOTED PANEL 221FF HAS LITE CORROSION ON BOTTOM SIDE. MA INTENANCE REMOVED AND REPLACED FLOOR PANEL 221FF IN ACCORDANCE WITH THE REQUIREMENTS OF WORK CARD SP753-12. UPON COMPLE TION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 NM 2008 8 5 F3LA200800328 1 20080611 A 5320 D5347112420000 SHEAR PLATE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 REFERENCE NON ROUTINE 34332. DURING C3 S1 C-CHECK INSPECTION NOTED CABIN FLOOR LATERAL SHEAR PLATE AT Y1162 BETWEEN FRA MES 69 AND FRAMES 70 HAS AREAS OF CORROSION ON TOP AND BOTTOM SIDES. MAINTENANCE REMOVED AND REPLACED LATERAL SHEAR PLA TE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEP TABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080724 NM 2008 7 24 2008UALA03246 1 20080608 A 3040 ANTI-ICE SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING J W B WARNING INDICATION INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 848UA 1647 ANTI ICE RIGHT WINDSHIELD ECAM WITH STRONG ODOR IN COCKPIT AND CABIN. RTFL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03298 1 20080609 A 2560 3F17645501 GIRT BAR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU R1 DOOR OUT OF ADJUST A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 914UA 25381 CREW REPORT: DOOR 1R GIRT BAR WILL NOT PROPERLY REST ON STOWAGE CLIPS. CLEANED GIRT BAR AND ADJUSTED GIRT BAR STOWAGE RETAINERS. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA02982 1 20080523 A 3510 MXP401600U STOWAGE BOX AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 836UA 1460 F/O O2 MASK WILL NOT TEST IN STOWED POSITION, APPEARS OK WHEN REMOVED FROM STORAGE. SHORT IN O2 BOX. REPLACED F/O O2 M ASK STOWAGE BOX. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 EU 2008 7 24 2008UALA03053 1 20080527 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 447UA 836 FLOORBEAM ITEM 235 HAS CORROSION. ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED FLOORBEAM AND RE-INSTALLED NEW. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03192 1 20080604 A 3350 32145410 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 850UA 1653 LEFT EPSU BATTERY FAILS EMERGENCY LIGHT CHECK. REPLACED EPSU BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03254 1 20080606 A 5322 SHEAR TIE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 FWD ENTRY DOOR CUTOUT FWD SIDE WEB FWD ATTACH POINT & INBOARD RADIUS CRACKED AT BS 294.5 AND STRINGER S-7L. MAJOR REPAI R ACCOMPLISHED: REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03255 1 20080606 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 INTERCOSTAL CRACKED STA 294 AT STRINGER 12L. MAJOR REPAIR ACCOMPLISHED: REPLACED INTERCOSTAL WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03286 1 20080606 A 2611 22179374 FAN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SMOKE DETECTOR FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 775UA 26947 DETECTOR FAN 2 CARGO AFT AFT CARGO COMPARTMENT SMOKE DETECTOR FAN NR 2 FAILURE. REPLACED AFT CARGO SMOKE DETECTOR NR 2 FAN ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080724 NM 2008 7 24 2008UALA03321 1 20080610 A 3200 UNKNOWN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU LANDING GEAR MALFUNCTIONED A UALA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 29 932UA 26658 ACFT WILL NOT TAXI STRAIGHT, PULLS TO THE LEFT. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03225 1 20080605 A 5230 CROSSBEAM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT CARGO DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 AFT CARGO DOOR, MIDDLE LOWER CROSSBEAM T-CHORD SEVERELY GOUGED 21 INCHES FROM AFT END, JUST BELOW MECHANISM BOX CUTOUT. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPLACEMENT CHORD. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03227 1 20080605 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 LEFT AFT FUSELAGE CRACKED BS 942- 946 AT STR 24L, JUST FWD OF POTABLE WATER SERVICE PANEL. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER/TRIPLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 SWAA083856 1 20080713 A 5314 6562125 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND LT KEEL BEAM WEB CORRODED AT BS 540, LBL 6.5. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083854 1 20080713 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083811 1 20080709 A 5753 6546435303 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083916 1 20080715 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 13R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 2008UALA03311 1 20080610 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE BENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 AFT CARGO FRAME BENT STA 1400, STR 26L TO 27L. ACCOMPLISHED MAJOR REPAIR AT GSO-RPR DAMAGE FRAME IAW SRM 53-00-07 REPAI R 5 DETAIL I. THIS REPAIR IS A CAT B REPAIR IN ZONE 3 AND REQUIRES SUPPLEMENTA L INSPECTIONS STARTING IN 12,000 FLT CYC LES AND 11,000FC THEREAFTER THIS INSP CONSISTS OF BOTH DETAIL VISUAL AND NDT. CURRENT P TC IS 20618. 2 L 7 2 4F 4 F RT A2NM E17NE 20080725 NM 2008 7 25 CALA0800645 1 20080623 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM BS 907 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 LEFTHAND SIDE STATION 907 FRAME BETWEEN S-8 AND S-9 AIRCONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRED FRAME AT STATION 907 BETWEEN S-8 AND S-9 PER EA5310-04498 OPERATION 02. 2 L 7 2 4F RT A16WE 20080725 EU 2008 7 25 2008UALA03134 1 20080530 A 3350 D9239003500060 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 432UA 587 EPSU UNIT R FAILED ON 3 SVC CK. *S/D* EPSU FAILURE. REPLACED EPSU, ALL TESTS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 EU 2008 7 25 2008UALA03223 1 20080605 A 3222 O-RING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG STRUT LEAKING A UALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 WP 29 432UA 587 NOSE GEAR DOORS WOULD NOT CLOSE. RTFL. *S/D* INTERNAL STRUT LEAK- O-RING ISSUE. NLG STRUT REPACKED, SERVICED. GEAR SWINGS WERE NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 NM 2008 7 25 2008UALA03508 1 20080621 A 5310 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 811UA 847 BEAM 145 FOUND CORRODED. *S/D* ACCOMPLISHED A MAJOR REPAIR AT DEN. REMOVED BEAM. PICKED UP HOLES FOR SPLICE PLATES A ND INSTALLED TOP PLATES. BEAM BUILT UP, PAINTED AND READY TO INSTALL. INSTALLED BEAM 145. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 EA 2008 7 25 SWIA200819825 1 20080702 A 3230 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA MLG ILLUMINATED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 947SW 7786 FLT 6098 - RECEIVED A "GEAR DISAGREE" WARNING MESSAGE. RECYCLED GEAR AND ALL THREE GEAR CAME DOWN. INSPECTED AND CYCLE D GEAR SYSTEM SEVERAL TIMES IAW AMM 32-30-00. COULD NOT DUPLICATE FAULT. 2 L 7 2 4F RT A21EA 20080725 SO 2008 7 25 SWIA200819835 1 20080704 A 5413 STRINGER EMB 120 EMB120ER 3260203 SO LT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 284YV 120284 FIRST LEFT SIDE FUEL PANEL INBOARD OF NACELLE HAS A CRACKED STRINGER AT FRAME 8, RIB 9. PERFORMED REPAIR ON STRINGER PE R EMB 120 SRM 57-20-03. 2 L 7 2 4T RT A31SO 20080725 NE 2008 7 25 E302008F00000 2 20080711 A 7320 70EMK01010 EEC GULSTM G1159 GIV 3980115 SO TMECA ARRIUS ARRIUS2K1 NE ENGINE MALFUNCTIONED E E30A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 108DU 1149 3300333012 ON JULY 11, 2008 AT APPROX 1050AM THE AC LIFTED OFF AND AT APPROXIMATELY 25 TO 30 FT BOTH ENGINES LOST POWER. PILOT INI TIATED A RIGHT PEDAL TURN AND ATTEMPTED TO LAND AT THE TAKEOFF POINT, THE AIRCRAFT LANDED IN THE GRASS SHORT OF THE PAD ON TOP OF THE GUARD FENCE. (K) 2 L 7 2 4F 3 U RT A12EA E34NE 20080725 NE 2008 7 25 IXX2008F00001 2 20080701 A 7297 CONNECTOR DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE NR 2 ENGINE DIRTY A IXXA O OTHER N FALSE WARNING CR CRUISE 1 SW 11 830BX 45973 DURING CRUISE, NR 2 ENGINE FIRE WARNING AND BELL CAME ON INTERMITTEN FOR 1-2 SECONDS. THE CREW ACCOMPLISHED, RAN CHECK LIST AND SHUTDOWN NR (2) ENGINE. THE FIRE BELL STOPPED AFTER FIRE HANDLE WAS MOVED TO FULL FWD POSITION. THE FIRE BOT TLES WERE NOT DISCHARGED. THE CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED NR 2 FIRE WARNING SYS AND FOUND LT F AN ELEMENT CONNECTOR WET, RT FIRE DETECTOR ELEMENT CONNECTOR PLUG, DIRTY. MAINTENANCE CLEANED BOTH CONNECTOR PLUG, AND REPLACED LT AND RT FAN ELEMENT, AND LT AND RT FIRE DETECTOR ELEMENT, OPS CHECK GOOD IAW MM 26-10-1, ERH 70-1-01. AC WAS RETURNED TO SERVICE. (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 20080725 NM 2008 7 25 XV62008F00000 1 20080603 A 7603 CONTROL CABLE DORNER DO32 DO328100 2996000 NM PWA 119 PW119C NE HARTZL HDE6C HDE6C3B NE POWER LEVER OBSTRUCTED D XV6A O OTHER C F.O.D. NR NOT REPORTED 1 WP 19 331MX 3074 PCEAB0005 HL227 R/S POWER LEVER WOULD NOT GO INTO GROUND IDLE AFTER LANDING. FOUND HINGE FROM COCKPIT DOOR INTERFERING WITH CABLES/ PUL LEYS TRAVEL AT RT AVIONICS AFT SIDE. REMOVED FOD AS REQUIRED. CABLES/ PULLEYS GROUND RUN SATISFACTORY. A/C APPROVED F OR RTS. (K) 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 20080725 WP 2008 7 25 MWE2008F00012 1 20080716 A 2497 WIRE HARNESS DOUG DC9 DC981 3022081 WP INVERTER MISINSTALLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 13 803ME 48029 WITH EMERGENCY POWER SWITCH ON, AC EMERGENCY POWER BUSS OFF LIGHT ILLUMINATED. FOUND INVERTER WIRES MISWIRED. REMOVED AND REPLACED EMERGENCY INVERTER. (K) 2 L 7 2 4F A6WE 20080725 CE 2008 7 25 GUU2008F00000 1 20080622 A 2800 CHECK VALVE BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA FUEL SYSTEM ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 81536 UE152 PILOT DISCREPANCY: PILOT REPORTED DURING FLIGHT FUEL ODOR IN CABIN. REPLACED RT FUEL TRANSFER LINE CHECK VALVE. (K) 2 L 7 2 4T 3 T RT A24CE E2NE 20080725 2008 7 25 HNA2008F00003 4 20080606 A 3442 MI5853505 TRANSCEIVER DHAV DHC8 DHC8311 1386006 EA WX RADAR SYS MALFUNCTIONED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 327EN 261 LOG PAGE 271884, SEQ NR 1- RADAR ONLY PAINTS 2 RED SPOKES. REMOVED AND REPLACED RT IAW 34-41-01. OPS CHECK GOOD. (K) 2 H 7 2 4T RT A13NM 20080725 NM 2008 7 25 PID2008F00004 1 20080606 A 3350 900835A BATTERY PACK BOEING 737 7372K5 138448X NM PWA JT8 JT8D15 52051 NE EMERGENCY LIGHTS INOPERATIVE A PIDA O OTHER O OTHER NR NOT REPORTED 1 EA 39 249TR 22598 MID CABIN CEILING - EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACKS AT MID CABIN CEILING. OPS CH ECK, EMERGENCY EXIT LIGHTS GOOD, IAW MM33-51-81. (K) 2 L 7 2 4F 4 F RT A16WE E2EA 20080725 NM 2008 7 25 Q2S2008F00000 1 20080608 A 2612 FIRE WARNING BOEING 747 747206B 1384856 NM NR 4 NACELLE ILLUMINATED A Q2SA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 63 748SA 21110 IN FLIGHT ON CLIMBOUT, NR 4 ENGINE FIRE WARNING LIGHT ILLUMINATED, ACCOMPLISHED AIRCRAFT OPERATING MANUAL (AOM) (SAI OP- 523) PROCEDURES. FIRE INDICATIONS WENT OUT WHEN ENGINE SHUTDOWN. NO FIRE BOTTLES BLOWN. NR 4 ENGINE CENTER LOWER ACCES S DOOR FOUND OPEN AFTER LANDING. POST FLIGHT: CLOSED AND SECURED NR 4 ENGINE LOWER ACCESS DOOR IAW AMM 78-30-01. ACCO MPLISHED HIGH POWER ENGINE RUNS ON NR 4 ENGINE AND FOUND TO BE WITHIN ALL PARAMETERS OF OTHER ENGINES WITH EXCEPTION OF NR 4 THRUST LEVER 3/4 BEHIND NR 1, 2, AND 3. IAW AOM, VOL 1, LIMITATIONS OKAY FOR CONTINUED SERVICE. AS PRECAUTION, LO CKED OUT NR 4 ENGINE HIGH STAGE VALVE IAW AMM 36-11-17. TRANSFERRED TO DI NR 16258 IAW DDPG, MEL 36-1 (2). PLACARD INST 2 L 7 4 4F RT A20WE 20080805 NM 2008 8 5 F3LA200800319 1 20080610 A 5321 D5361076000000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 77 1851 REFERENCE NON ROUTINE C044808. DURING C4 S1 C-CHECK INSPECTION NOTED PANEL 222EF SPLICE PLATE CORRODED. MAINTENANCE RE MOVED AND REPLACED FLOOR PANEL SPLICE PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF WORK CARD CP753-12. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 NM 2008 8 5 F3LA200800343 1 20080613 A 5270 DHE1141 PROXIMITY SWITCH AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE L1 DOOR FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 915FR 77 1851 REFERENCE NON ROUTINE C045163. DURING C4 S1 C-CHECK INSPECTION NOTED CHECK DOOR SWITCH POWER SUPPLIED BY EMERGENCY LIGH T SYSTEM FAILS AT PAGE 4 STEP 3, WORK CARD C335004-2 FOR THE FORWARD DOORS AND WORK CARD C335004-2 AT PAGE 6 STEP 8 FOR THE L1 DOOR. MAINTENANCE REMOVED AND REPLACED PROXIMITY SWITCH 13WVI IN ACCORDANCE WITH THE REQUIREMENTS OF AMM 52-71-1 1-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE AND OPERATIONAL CHECKED GOOD. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 EA 2008 8 5 HNAA0800213 1 20080620 A 3350 OL3071BPEGPL BULB DHAV DHC8 DHC8311 1386006 EA EMERGENCY LIGHTS BURNED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 328EN 29356 281 N/A FLOOR EMERGENCY LIGHT INOP AT ROW 6. REPLACED BULB, OPS CHECK GOOD. (A) 2 H 7 2 4T RT A13NM 20080805 WP 2008 8 5 NWAA083169917 1 20080719 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 967N 47573 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INO PERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (A) 2 L 7 2 4F A6WE 20080805 NM 2008 8 5 HNAA0800233 1 20080715 A 3397 CONNECTOR DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS DIRTY A HNAA O OTHER N FALSE WARNING CL CLIMB 1 EA 07 825EX 388 EMERGENCY LIGHTS WERE FLASHING FOR ABOUT ONE MINUTE AFTER ROTATION. CREW REPORTED. (S) 2 H 7 2 4T RT A13NM 20080805 EU 2008 8 5 DHL2008F00013 1 20080708 A 5740 ATTACH ANGLE AEROSP ATR42 ATR42300 8680920 EU LT WING SKIN CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 918FX 262 DURING THE YEARLY INSPECTION FOUND EXFOLIATION CORROSIOIN LEVEL 2. THE CORROSION WAS ON LT LOWER WING SKIN ATTACH ANGLE THAT ATTCHES THE WING SKIN TO THE LT OUTBOARD NACELLE SKIN AT RIB 12. REPAIRED IAW ATR 42 SRM 51-21-42, 51-21-58, 51-2 2-02 AND ATR REPAIR INSTRUCTION DO/TS-3056/08-10463. (A) 2 H 7 2 4T RT A53EU 20080805 EA 2008 8 5 A6WA200840540 1 20080708 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OUT OF RIG A A6WA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 31 431AW 7256 AIRCRAFT ROLLS LT WITH THRUST, EVEN IN DESCENT AND CRUISE. APPROXIMATELY 50% TRIM RWD. CAPTAIN YOKE HAS FREE PLAY (LT AND RT), FIRST OFFICERS YOKE NORMAL. FLAPS FOUND OUT OF RIG. FLAPS HAVE BEEN RIGGED USING AMM 27-51-00. BOTH LT AND R T CONTROL WHEEL QUADRANTS CABLE TENSIONS FOUND OUT OF TOLERANCE, BOTH QUADRANTS CORRECT CABLE TENSIONS USING AMM 27-11-0 0. FOUND SYS OK AT THIS TIME. (A) 2 L 7 2 4F RT A21EA 20080805 SO 2008 8 5 RAIA00807016 1 20080720 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BLOWN A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 811HK 145256 PRE FLIGHT 5574 - PHL - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB. (A) 2 L 7 2 4T RT T00011AT 20080805 SO 2008 8 5 C2XA08ON145 1 20080620 A 3230 23093009503 ARM EMB 145 EMB145LR 3260212 SO MLG OUT OF LIMITS A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14907 16450 12557 145468 FLT MX - ONT - WHILE PERFORMING 5A CHECK INSPECTION ON LT MLG TRAILING ARM AND DRAG BRACE QC INSPECTOR FOUND THAT THE TR AILING ARM HAD PLAY AND THAT THE MAIN DRAG BRACE WAS LOOSE AT CENTER JOINT. MAINTENANCE REMOVED AND REPLACED THE LT MLG TRAILING ARM AND CLEANED, INSPECTED, AND CHECKED DIMENSIONAL LIMITS AND WERE FOUND WITHIN LIMITS. OPERATIONALLY CHECKE D SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080805 NM 2008 8 5 PID2008F00009 1 20080719 A 3350 9721050 BATTERY PACK BOEING 737 737291 138448W NM EMERGENCY LIGHTS INOPERATIVE A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 583CC 21069 L1 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK FOR L1 DOOR INTERVALVE MODULE. OPERATION CHECK IS GOOD , REF MM 33-51-0. (A) 2 L 7 2 4F A16WE 20080805 EA 2008 8 5 TRAX200800919 1 20080717 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGNECY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 914EV 7752 RT SIDE FUSELAGE REAR EXTERNAL EMERGENCY LIGHT INOP. RELAMPED REAR EXTERIOR EMERGENCY LIGHT AT RT SIDE OF FUSELAGE IAW CRJ 200 AMM 33-51-21. OPS CHECK GOOD. (A) 2 L 7 2 4F RT A21EA 20080805 EA 2008 8 5 TRAX200800823 1 20080622 A 5240 ROLL PIN CNDAIR CL600 CL6002B19 1900309 EA DOOR HANDLE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 820AS 7188 SERVICE DOOR WILL NOT LATCH IN OPEN POSITION WHEN OPENED FROM INSIDE THE ACFT. ALSO DIFFICULT TO OPEN FROM OUTSIDE. F LT 4167 DEL 155 MINS. REMOVED AND REPLACED DOOR HANDLE ROLL PIN IAW AMM 52-41-01. OPS CHECK GOOD. (S) 2 L 7 2 4F RT A21EA 20080805 EA 2008 8 5 TRAX200800829 1 20080624 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 977EV 7720 FS 280.0 LBL 9.0 I/B CLIP CRACKED. REMOVED OLD CRACKED CLIP AT FS 280.00 LBL 9 I/B. INSTALLED NEW SERVICEABLE CLIP IAW CRJ 200 SRM 51-42-21. (S) 2 L 7 2 4F RT A21EA 20080724 NM 2008 7 24 SWAA083920 1 20080715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CORRODED AT BS 847, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083943 1 20080715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083936 1 20080715 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 344, STR 4L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083941 1 20080715 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083937 1 20080715 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, LBL 2.5. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083715 1 20080704 A 2612 473925 SENSOR BOEING 737 7377H4 1384404 NM FWD CARGO BAY FAULTY A SWAA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 29 728SW 27860 AIR TURBACK / DECLARED EMERGENCY. FWD CARGO COMPT FIRE WARN INDICATION. FOUND FWD CARGO COMPT B2 SENSOR FAULTY. REMOV ED AND REPLACED FWD CEU AND B2 SENSOR PER MM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083718 1 20080704 A 3350 100031 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 758SW 27873 DURING SCHEDULED MV1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT 7 DEF. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 20080724 2008 7 24 2008UALA03335 4 20080611 A 2565 SPRING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 558UA 26654 NR 1 DOOR SLIDE ARM LEVER COVER SPRING BROKEN. DOES NOT STOW CORRECTLY. REPLACED COVER, FUNCTIONS CORRECTLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03315 1 20080610 A 2910 HYDRAULIC LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT WING BENT A UALA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 29 544UA 25322 DURING TAXI FLIGHT CONTROL CHECK, WHEN MOVING TO LEFT WING DOWN, APPROX HALF WAY FROM NEUTRAL TO FULL LWD, AN ADDITIONAL 3-4 LBS OF PRESSURE REQUIRED. NEUTRAL TO FULL RWD NO ADDITIONAL PRESSURE IS REQUIRED, PER CREW. BENT HYD LINE HITTING AILERON PUSH ROD. REPLACE LINE OPERATION CHECK. PUSH ROD CLEAR LINE NO LEAKS. AILERON OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 EU 2008 7 24 2008UALA03425 1 20080617 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 477UA 1514 LEFT FWD EMERGENCY LIGHT BATTERY FAILED EMERGENCY LIGHT TEST AND SELF TEST. REPLACED FWD LEFT EMERGENCY LIGHT BATTERY. TESTS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03393 1 20080614 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 83UA 24658 DURING SCRIBE LINE NDT "EQ1850" A CRACK INDICATION WAS NOTED USING HFEC INSP NDT PART 6. SCANNER PROBE AT LOCATION S-4R , STA 727+57 (AREA MARKED). STANDARD STD-1831 USED, INDICATION LARGER THAN LOCATION C ON STD. REPAIR BEFORE FURTHER FL IGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03382 1 20080614 A 2620 6937307149 CONTROL PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE CONTROL FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 340UA 24244 RIGHT BOTTLE DISCHARGE LIGHT FAILS TO COME ON WHEN PRESSED. CREW COMMENTS: LEFT TEST-ONLY L & APU TEST. RIGHT TEST - ONLY APU TEST. FOUND FAULTY TEST PANEL. REPLACED FIRE CONTROL PANEL REF MM26-21-51 OP CHECKS OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 2008 7 24 2008UALA03379 4 20080613 A 2565 D31591478U1 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 929UA 26652 DOOR 1L IS DIFFICULT TO ARM. SUSPECT FAULTY SLIDE ASSEMBLY. REPLACED SLIDE ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVIC E. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03369 1 20080615 A 2910 211C223534 SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HYD SYS FAULTY A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 651UA 25389 LEFT HYDRAULIC SYSTEM FAILURE. RTFL. FOUND FAULTY SWITCH. REPLACED S30 SWITCH OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080725 EU 2008 7 25 2008UALA03092 1 20080529 A 5210 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DOOR 1R READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 471UA 1432 DOOR 1R DOOR PRESSURE AT 500. SERVICED DOOR 1R ASSIST BOTTLE TO 1750 PSI. NO LEAKS WERE NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 EU 2008 7 25 2008UALA03093 1 20080529 A 5753 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT WING TE FLAP DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 497UA 1847 LEFT INBOARD FLAP DENT AND ABRASION ON TRAILING EDGE, CENTER AFT OF NR 2 TIRE. FOUND AND REPORTED BY RAMP DURING WALKAR OUND. *S/D* IDENTIFIED BY SRM 57-50-00- 001 PG 7 INBOARD FLAP. DAMAGE AREA PER SRM 57-52-00-101 PG 4 AS ZONE 2, PER T ABLE 101 PG 2. DENT IN SKIN ALLOWABLE FIGURE 117 (PG 20). DISBONDING FIGURE 115 (PG 18). CRACK PER FIGURE 109 (PG 12) TAPED CRACK IS 5-16 LONG AS TEMP REPAIR. PERMANENT REPAIR REQUIRED WITHIN 3 MONTHS PER 57-52-00-114 PAGE 12. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 EA 2008 7 25 VNAA0805011 1 20080508 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS MALFUNCTIONED A VNAA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 GL 05 259PS 7945 CREW REPORTED A FLAPS FAIL AT 0 DEGREES DURING FINAL APPROACH. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE CIRCUIT BREAKERS AND PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MAN UAL. SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080725 NM 2008 7 25 2008UALA03491 1 20080620 A 5320 SPACER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L2 GIRT BAR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 811UA 847 DOOR 2L AFT GIRT BAR FITTING SPACER PLATE FOUND CORRODED. REMOVED CORROSION, PRIMED AND PAINTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 NM 2008 7 25 MWE2008F00009 1 20080713 A 3397 WIRE DOUG MD88 MD88 3023688 NM EMERGENCY LIGHTS DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 601ME 49762 EMERGENCY ESCAPE FLOOR PATH LIGHTS OUT AT SEAT (SF). FOUND DAMAGED, SPLICED WIRES. (K) 2 L 7 2 4F RT A6WE 20080725 WP 2008 7 25 IXX2008F00003 1 20080701 A 2612 FIRE WARNING DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE NR 2 ENGINE INTERMITTENT A IXXA O OTHER N FALSE WARNING CR CRUISE 1 SW 11 830BX 45973 DURING CRUISE, NR 2 ENGINE FIRE WARNING AND BELL INTERMITTENT FOR 1-2 SECONDS. THE CREW RAN CHECK LIST AND SHUT DOWN NR (2) ENGINE. THE FIRE BELL STOPPED AFTER FIRE HANDLE WAS MOVED TO FULL FWD POSITION. THE FIRE BOTTLES WERE NOT DISCHAR GED. THE CREW LANDED WITHOUT INCIDENT. C/A: IN WORK. (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 20080725 NM 2008 7 25 MWE2008F00020 1 20080705 A 7830 7150922505 ANGLE BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 928ME 55194 LT THRUST REVERSER LOWER BUCKET Z-FRAME REPAIR IS CRACKED AT STA 35.669 OB SIDE. FABRICATED AND INSTALLED ANGLE. (K) 2 L 7 2 4F TR A6WE 20080725 NM 2008 7 25 MWE2008F00019 1 20080705 A 7830 7150922505 ANGLE BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 928ME 27 55194 LT THRUST REVERSER LOWER BUCKET Z-FRAME REPAIR IS CRACKED AT STA 26.666 IB SIDE. FABRICATED AND INSTALLED ANGLE. (K) 2 L 7 2 4F TR A6WE 20080725 EA 2008 7 25 FDK2008F00001 1 20080710 A 2560 HOOK CNDAIR CL600 CL6002D24 1390016 EA GE CF34 CF348C5 30050 NE OVERWING MISSING A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 601LR 15145 OVERWING ESCAPE HOOK MISSING. MX INSTALLED MISSING HOOK. (K) 2 L 7 2 4F 4 F RT A21EA E00063EN 20080725 NM 2008 7 25 PID2008F00002 1 20080630 A 3350 LAMP BOEING 767 767277 1385128 NM EMERGENCY LIGHT INOPERATIVE A PIDA O OTHER O OTHER NR NOT REPORTED 1 EA 39 767MW 22694 DURING 30 DAY CHECK; NOTED R2 DOOR EMERGENCY LIGHT IS INOPERATIVE. RELAMPED IAW MM 33-51-00. OPS CHECK GOOD. (K) 2 L 7 2 4F RT A1NM 20080725 WP 2008 7 25 DUF2008F00000 2 20080710 A 7261 S9413554 O-RING SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP OIL SYSTEM CRACKED E DUFA O OTHER K FLUID LOSS NR NOT REPORTED 1 GL 27 3108B AC509 P44134C WHILE ENROUTE, THE PILOT NOTICED HIS LT ENGINE OIL PRESSURE GAUGE FLUCTUATING. SHORTLY THERE AFTER THE "LOW OIL PRESSUR E" LIGHT ILLUMINATED. SINCE HE WAS VERY CLOSE TO HIS DESTINATION, THE PILOT ELECTED TO SHUTDOWN THE ENGINE AND SECURE IT AS A PRECAUTION. PILOT MADE UNEVENTFUL SINGLE ENGINE LANDING. UPON INVESTIGATION MY MAINT , IT WAS DISCOVERED THAT TH E OIL PRESSURE LINE DAMPER FITTING O-RING HAD FAILED AND ALLOWED OIL TO SEEP PAST THE FITTING. THIS DEPLETED THE ENGINE OIL SUPPLY UNTIL, THERE WAS AN INSUFFICIENT AMOUNT TO MAINTAIN THE PROPER PRESSURE. A NEW O-RING WAS INSTALLED AND GRO UND RUNS PERFORMED WITH NO LEAK NOTED. (K) 2 L 7 2 4T 4 T RT A8SW E4WE 20080725 CE 2008 7 25 GLB2008F00003 1 20080714 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA FS 163. CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 21 100UX UE100 POPPED RIVET HEADS AND CRACK FOUND AT STATION 163.975 ABOVE AIRSTAIR DOOR. MAINTENANCE STOP DRILLED AROUND RIVETS AND RE PAIRED THE AFFECTED AREA IAW B1900D SRM 53-90. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1. (K) 2 L 7 2 4T 3 T RT A24CE E4EA 20080725 2008 7 25 MWE2008F00007 4 20080707 A 2565 100503117 SLIDE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D* NE TAILCONE UNWANTED DEPLOY A MWEA O OTHER W INADEQUATE Q C CL CLIMB 1 GL 13 804ME 48030 DURING CLIMB, THE PITCH AUTHORITY (ELEVATOR) FELT STIFF ALTHOUGH CONTROLLABLE, PRIMARY PITCH TRIM WORK OK, ALT LONG TRIM AND AUTO PILOT WORKED NORMAL INSP OF AFT ACCESSORY COMPARTMENT FOR ELEVATOR AUTHORITY ISSUE FOUND THE TAIL CONE SLIDE HAD DEPLOYED IN THE TAIL CONE COMPARTMENT. REMOVED AND REPLACED TAIL CONE SLIDE. (K) 2 L 7 2 4F 4 F A6WE E2EA 20080725 EA 2008 7 25 FDK2008F00002 1 20080702 A 5270 SWITCH CNDAIR CL600 CL6002D24 1390016 EA GE CF34 CF348C5 30050 NE PAX DOOR DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 606LR 15173 PAX DOOR CAUTION MESSAGE IN FLIGHT. MX RE-REPACKED PSCU AND CLEANED SWITCHES. (K) 2 L 7 2 4F 4 F RT A21EA E00063EN 20080725 EA 2008 7 25 FDK2008F00003 1 20080630 A 5270 WARNING MESSAGE CNDAIR CL600 CL6002D24 1390016 EA GE CF34 CF348C5 30050 NE PAX DOOR ILLUMINATED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 606LR 15173 PASSENGER DOOR LATCH, CAUTION MESSAGE AND PROX SYS FAULT 2. OPS CHECK GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E00063EN 20080728 EA 2008 7 28 VNAA0805020 1 20080515 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE WING MALFUNCTIONED A VNAA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 GL 05 254PS 7935 CREW REPORTED A FLAPS FAIL AT 8 DEGREES DURING DESCENT INTO DCA. CREW ELECTED TO DECLARE AN EMERGENCY AND LANDED WITHOU T INCIDENT. MAINTENANCE INTERROGATED THE FECU, BITE CHECK AND SKEW DETECTOR. MAINTENANCE RESET THE FLAP CHANNELS IN AC CORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080728 EA 2008 7 28 VNAA0805019 1 20080514 A 5244 H50002064115 LATCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF348C1 30049 NE COMM PANEL BROKEN A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 05 706PS 10150 CREW REPORTED AFTER TAKEOFF HEARD A WHINING NOISE COMING FROM THE NOSE OF THE AIRCRAFT. CREW ELECTED TO RETURN TO CLT A ND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE COMM PANEL LATCH WAS BROKEN. MAINTENANCE REMOVED AND R EPLACED THE LATCH IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080728 WP 2008 7 28 UPS08852589 1 20080611 A 5347 DC853B007002 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 STA 950 LBL 24 SEAT TRACK WORN MAIN CABIN. REPLACED MAIN CABIN SEAT TRACK PLUG AT STA 950 AND LBL 24 IAW SRM 53-0 2-03 FIG 006. 2 L 7 4 4F RT 4A25 20080728 NM 2008 7 28 NOC2008F00003 1 20080617 A 3397 WIRE BOEING 767 76736N 1385152 NM EMERGENCY LIGHTS DAMAGED A NOCA O OTHER O OTHER NR NOT REPORTED 1 EA 15 768NA 29898 EMERGENCY LIGHTS AT ROW 12D THRU 20D INOPERATIVE. SPLICED MADE REPAIRED WIRING IAW SWPM CH 20. ALL OPS CHECKED GOOD. NO DEFECTIVE PART. (K) 2 L 7 2 4F RT A1NM 20080729 NM 2008 7 29 ASAA0843144 1 20080506 A 5340 6935352Y1 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 STRINGER TIE CLIP CRACKED IN FORWARD CARGO BAY AREA. REPLACED CLIP PER SRM 51 40 02. 2 L 7 2 4F RT A16WE 20080729 CE 2008 7 29 DXTA200803131 1 20080617 A 2150 A/C PACK CESSNA 750 750 2076810 CE ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 926QS 7500026 BAD ODOR COMING FROM COCKPIT/CABIN PACKS SMELLS LIKE A COMBINATION OF DIRTY SOCKS AND BURNED OIL. (B) 2 L 7 2 4J RT T00007WI 20080729 NM 2008 7 29 ASAA0843156 1 20080507 A 5311 90526913 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 FRAME CRACKED AT PSU RAIL BRACKET. REPAIRED FRAME PER EA 5310 02797. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800902 1 20080710 A 2750 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 836AS 7263 FLAPS FAIL AT 25 WHEN SELECTING FLAPS TO 30 FROM 20. EMERGENCY VEHICLES WERE ON STANDBY AS A PRECAUTION (SKEW DETECTION SYSTEM). REMOVED AND REPLACED FLAP POWER DRIVE UNIT IAW AMM 27-52-01. FLAPS OPERATE NORMALLY AT ALL SELECTED POSITIONS . 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 ASAA0843164 1 20080501 A 5754 65C26602302 SLAT BOEING 737 7374Q8 138447Q NM NR 5 DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 NR 5 SLAT OUTBOARD END DELAMINATED. REPLACED CORE AND INSTALLED DOUBLER PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083982 1 20080715 A 3350 417A5601 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 902WN 36615 DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080730 EA 2008 7 30 REX2008F00013 1 20080622 A 3233 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF RIG A REXA A UNSCHED LANDING E P VIBRATION/BUFFET NO WARNING INDICATION CL CLIMB 1 SO 25 8913A 7913 UPON GEAR RETRACTION A LOUD "KNOCKING" NOISE WAS HEARD, NO CAUTION OR WARNING MESSAGES RECEIVED BUT NOISE CONTINUED. FO LLOWED QRH AND DECIDED TO RETURN TO DTW, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. NOSE GEAR DOOR ACTUATOR RE-RIG GED AND OPERATIONAL CHECK PERFORMED IAW BOMBARDIER AMM. (S) 2 L 7 2 4F RT A21EA 20080730 NM 2008 7 30 CALA0800693 1 20080708 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM BS 400 S9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14629 27533 FRAME CRACKED STATION 400 AT S-9 RIGHT. REPAIRED FRAME PER EA 5310-04498 OP2. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800703 1 20080707 A 2121 6454051 FAN BOEING 737 737524 1384721 NM RT A/C PACK FAILED A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 46625 37189 37189 27529 PASSING THROUGH 11000 ON DESCENT ELECTRICAL AND/OR RUBBER BURNING ODOR, WAS NOTED, NO SMOKE OBSERVED. A/C SMOKE FUME CH ECKLIST PERFORMED AND ODOR LESSENED WHEN RT PACK ISOLATED. ODOR STARTED QUICKLY IN FIRST CLASS THRU MID CABIN AND DISSI PATED SOMEWHAT ONCE THE RIGHT PACK TURNED OFF AND ISOLATION CLOSED. AFTER LANDING AN ODOR WAS STILL APPARENT TO FIRE PE RSONNEL. PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-95-201, UNABLE TO DUBLICATE ON GROUND. TROUBLESHOT FOR RECIRCU LATION FAN FAILURE. AIRCRAFT OK TO CONTINUE SERVICE. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083988 1 20080720 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 747 S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080730 EU 2008 7 30 MAL2008F00001 1 20080617 A 5260 7253710871 RAIL SAAB SF340 340B 7860101 EU AIRSTAIR CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 422XJ 340B422 AIR STAIRS RAIL CORRODED, P/N 7253710-871. AIR STAIR RAIL REPAIRED IN ACCORDANCE WITH EO S53592. (S) 2 L 7 2 4T RT A52EU 20080730 EA 2008 7 30 VNAA0804011 1 20080413 A 7500 GG670800053 SENSOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE LT BLEED TEMP FAILED A VNAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 05 709PS 3736 10165 CREW REPORTED A LT ENG BLEED CAUTION MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LT PRESSURE SHUT OFF VALVE AND THE LT BLEED TEMP SENSOR. MAINTENANCE REMOVED AND REPLACED TH E LT BLEED TEMP SENSOR IN ACCORDANCE WITH THE ACFT MAINTENANCE MANUAL. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E00063EN 20080730 NM 2008 7 30 SWAA084010 1 20080719 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500A S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083992 1 20080720 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 987 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 987, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800664 1 20080702 A 5320 651758243 STIFFENER BOEING 737 737524 1384721 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 STATION 178 BULKHEAD RBL 17 WL 234 VERTICAL BEAM WEB CRACKED. REMOVED, FABRICATED AND INSTALLED UPPER WEB AT RBL 17 IAW ECRA 5310-04794. 2 L 7 2 4F RT A16WE 20080730 EA 2008 7 30 VNAA0804013 1 20080411 A 2750 860D10018 FCU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS FAILED A VNAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 05 221PS 9993 7889 CREW REPORTED A FLAPS FAIL CAS MESSAGE DURING APPROACH/LANDING. THE ARFF RESPONDED AND THE ACFT TAXIED TO THE GATE. MA INTENANCE INSPECTED AND DEFERRED THE FECU PER MEL 27-51-01-2. MAINTENANCE REMOVED AND REPLACED THE FECU IN ACCORDANCE W ITH THE ACFT MAINTENANCE MANUAL. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080725 NM 2008 7 25 2008UALA03259 1 20080606 A 5713 STRINGER SPLICE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT WING MISMANUFACTURED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 544UA 25322 RIGHT WING UPPER STRINGER SPLICES 757-3503 -8 AND -10 HAVE SHORT EDGE MARGIN (WINGLET MOD). ACCOMPLISHED MAJOR REPAIR A T GSO-TRIMMED -8 STR SPLICE PER REO-G12358. NDT INSP PER PT 6, 51-00-19. NO DEFECTS NOTED. ROTO PEENED PER REO AND SRM 51-20-13. INSTALLED 757-3503-10 SPLICE PER REO N-R 30599. 2 L 7 2 4F 4 F RT A2NM E17NE 20080725 NM 2008 7 25 2008UALA03262 1 20080608 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMEGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 544UA 25322 EXTERIOR EMERGENCY LIGHT ON AFT CARGO DOOR INOP. *S/D* LAMP INOP. RELAMPED EXT LIGHT OF AFT CARGO. 2 L 7 2 4F 4 F RT A2NM E17NE 20080725 NM 2008 7 25 2008UALA03264 1 20080607 A 2720 6439105 PCU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER LEAKING A UALA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 29 590UA 28708 CREW REPORTS HYD QTY LOSS LEFT SYS RESERVOIR REPORTS 1.3 DOWN TO .92. *S/D* RUDDER CENTER PCU LEAKING. REPLACED CENTE R PCU FOR RUDDER AND PERFORMED LEAK CHECK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080725 2008 7 25 2008UALA03293 4 20080609 A 2210 B546CCM0104 COMPUTER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FLT MANAGE FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 829UA 1211 DUAL FMGC FAILURE. RTFL. *S/D* FMGC 2 FAILED-ARRINC INTERLOOP TEST FAILS. FMGC2 INOP UPON ARRIVAL. REPLACED FMGC2. PERFORMED AFS AND LAND TEST PER MM 22-96-00 AND MM 22-97-00. CHECKS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 NM 2008 7 25 2008UALA03231 1 20080605 A 3600 PNEUMATIC SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE MALFUNCTIONED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 654UA 25392 ENGINE NR 1, PNEUMATIC PRESSURE IS 10 PSI AT IDLE REQUIRED ENG TO RUN UP TO BLEED SHIFT BEFORE IS STARTS TO WORK. THEN GOT 31 PSI ON IDLE. RAN ENG TWICE SAME ISSUE, SUSPECT HI STAGE. REPLACED PRV AND PRV CONTROLLER. OP CHK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20080725 NM 2008 7 25 2008UALA03236 1 20080606 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 1E AFT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 772UA 26930 SEAT 1E AFT EMERGENCY LIGHT MISSING. EMERGENCY LIGHT ASSY REPLACED AND TESTED OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080725 NM 2008 7 25 2008UALA03237 1 20080606 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 1F AFT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 772UA 26930 SEAT 1F AFT EMERGENCY LIGHT ASSY MISSING. LIGHT ASSY REPLACED AND TESTED NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080725 NM 2008 7 25 CALA0800643 1 20080623 A 5311 6546596 FRAME BOEING 737 737524 1384721 NM BS 727B S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 LEFTHAND SIDE STATION 727B FRAME BETWEEN S-8 AND S-9 AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRE D FRAME AT STATION 727B BETWEEN S-8 AND S-9 PER EA5310-04498, OPERATION 02. 2 L 7 2 4F RT A16WE 20080725 NM 2008 7 25 CALA0800639 1 20080623 A 5311 6546596 FRAME BOEING 737 737524 1384721 NM BS 727B S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 RIGHTHAND SIDE STATION 727B FRAME BETWEEN S-8 AND S-9 AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIR ED FRAME AT STATION 727B BETWEEN S-8 AND S-9 PER EA5310-04498, OPERATION 02. 2 L 7 2 4F RT A16WE 20080725 NM 2008 7 25 CALA0800641 1 20080623 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM BS 907 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 RIGHTHAND SIDE STATION 907 FRAME BETWEEN S-8 AND S-9 AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRE D FRAME AT STATION 907 BETWEEN S-8 AND S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080725 NM 2008 7 25 2008UALA03430 1 20080617 A 2612 6937307149 MODULE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE DETECTION FALSE INDICATION A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 312UA 23673 WITH POWER OFF CARGO FIRE DETECTION PANEL LIGHTS ARE ON. FOUND FAULTY DETECTION PANEL. REPLACED CARGO FIRE DETECTION PA NEL REF MM 26-00-02. OPS CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080725 NM 2008 7 25 2008UALA03504 1 20080621 A 5310 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 811UA 847 BEAM NR 175 FOUND CORRODED. *S/D* ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED BEAM CONT OF AMIS ITEM 5142012. REPLACED WITH NEW BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 NM 2008 7 25 2008UALA03506 1 20080621 A 5311 FRAME AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 811UA 847 RIGHT CORNER LATERAL SHEAR PLATE SUPPORT FRAME FOUND CORRODED ON UPPER AND LWR SURFACES. *S/D* ACCOMPLISHED A MAJOR RE PAIR IN DEN. REMOVED SHEAR PLATE SUPPORT FRAME FROM FR69 - FR70 RT SIDE. COMPLETED INSTALL OF SUPPORT FRAME. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 NM 2008 7 25 2008UALA03507 1 20080621 A 5320 SHEAR PLATE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 811UA 847 RIGHT CORNER LATERAL SHEAR PLATE BETWEEN FR69 AND FR70 FOUND CORRODED. *S/D* ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVE D RT SHEAR PLATE. CONT OF AMIS ITEM 5142020 -COMPLETED INSTALL OF RT SHEAR PLATE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 NM 2008 7 25 2008UALA03509 1 20080621 A 5310 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 811UA 847 BEAM 140 FOUND CORRODED. *S/D* ACCOMPLISHED A MAJOR REPAIR AT DEN. REMOVED BEAM CONT OF AMIS ITEM 5142025. INSTALLED FITTINGS ON NEW BEAM CONT OF AMIS ITEM 5142042. BEAM BUILT UP, PAINTED AND INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 EA 2008 7 25 VNAA0805017 1 20080512 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LEFT MALFUNCTIONED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 253PS 7934 CREW REPORTED A LT PACK FELL OFF LINE FOLLOWED BY A HIGH PRESSURE CAS MESSAGE. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED AN OPERATIONAL TEST OF THE ACS SYSTEM IN ACCORDANCE WITH THE AIR CRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080725 NM 2008 7 25 CALA0800646 1 20080626 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM BS 827 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 RIGHTHAND SIDE STATION 827 FRAME BETWEEN S-8 AND S-9 AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRAKCED. REPAIRE D FRAME AT STATION 827 BETWEEN S-8 AND S-9R PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080725 NM 2008 7 25 CALA0800648 1 20080628 A 5320 6935365Y6 INTERCOSTAL BOEING 737 737524 1384721 NM BS 380-400 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 INTERCOSTAL CRACKED AT BL 0 BETWEEN STATIONS 380-400. REMOVED AND REPLACED DAMAGED INTERCOSTAL CAP ANGLE AT STATIONS 38 0-400 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080725 NM 2008 7 25 CALA0800649 1 20080629 A 5320 65C3397053 INTERCOSTAL BOEING 737 737524 1384721 NM BS 340-360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 INTERCOSTAL CRACKED AT BL 0 BETWEEN STATIONS 360-340. REMOVED AND REPLACED DAMAGED INTERCOSTAL AT STATIONS 340-360 BL 0 IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080725 2008 7 25 SWIA200819829 4 20080630 A 2562 ELT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 438SW 7574 FLT 4037 - ELT IS UNSERVICEABLE. REPLACED ELT IAW CRJ AMM 25-62-00. OPS CHECK OK, P/N 453-0150, S/N OFF 67578. 2 L 7 2 4F RT A21EA 20080725 EA 2008 7 25 SWIA200819831 1 20080701 A 2421 ADG CNDAIR CL600 CL6002B19 1900309 EA UNWANTED DEPLOY A SWIA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 NM 07 432SW 7548 FLT 4006 - ADG DEPLOYED INFLIGHT. RESTOWED ADG PER CRJ MM 24-23-01. 2 L 7 2 4F RT A21EA 20080725 EA 2008 7 25 SWIA200819814 1 20080626 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 407SW 7034 FLT 2720 - LAST EMERGENCY CEILING FLOOD LIGHT IS INOP. REPLACED BULB AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080725 EA 2008 7 25 SWIA200819815 1 20080627 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA RIGHT FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 07 918SW 7645 FLT 6006 - RECEIVED A PACK HI TEMP CAUTION MESSAGE ALONG WITH REPORTED LIGHT SMOKE IN CABIN. REPLACED RIGHT PACK AIR CY CLE MACHINE IAW AMM 21-12-00. OPS AND LEAK CHECK GOOD, P/N 782790-15, S/N OFF 200106038. 2 L 7 2 4F RT A21EA 20080725 SO 2008 7 25 SWIA200819816 1 20080625 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO GALLEY BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 224SW 120294 EMERGENCY LIGHT STRIP IS INOP NEAR THE GALLEY. REPLACED EMERGENCY LIGHT STRIP AS REQUIRED. 2 L 7 2 4T RT A31SO 20080725 EA 2008 7 25 SWIA200819788 1 20080616 A 2613 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA MLG OVERHEAT NO TEST A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 952SW 7805 FLT 5990 - MAIN LANDING GEAR BAY OVERHEAT WOULD NOT TEST CORRECTLY. REPLACED MAIN LANDING GEAR OVERHEAT CONTROLLER AS R EQUIRED. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 20080725 EA 2008 7 25 SWIA200819836 1 20080706 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 426SW 7468 FLT 3835 - CAPTAINS SIDE WINDOW IS CRACKED. REPLACED CAPTAINS SIDE WINDOW IAW CRJ 200 MM 56-12-01, P/N OFF 601R33033-11 , S/N OFF 00258H7823. 2 L 7 2 4F RT A21EA 20080725 EA 2008 7 25 SWIA200819839 1 20080705 A 5610 13932212 WINDOW CNDAIR CL600 CL6002C10 1390015 EA COCKPIT FAULTY A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 708SK 10156 "R WINDOW HEAT" MESSAGE INFLIGHT. REPLACED RIGHT WINDOW PER CRJ MM 56-12-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080725 SO 2008 7 25 SWIA200819840 1 20080701 A 3350 BULB EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 585SW 120353 FLOOR EMERGENCY LIGHTING IS NOT WORKING. RELAMPED BULB. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080725 EA 2008 7 25 SWIA200819841 1 20080706 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 946SW 7776 FLT 6146 - RIGHT SIDE WINDSHIELD INNER PLY CRACKED WHILE PARKED AT GATE. REPLACED RIGHT WINDOW IAW AMM 56-12-01, P/N NP -139322-2, S/N OFF 02346H2842. 2 L 7 2 4F RT A21EA 20080725 EA 2008 7 25 SWIA200819843 1 20080708 A 7830 O-RING CNDAIR CL600 CL6002D24 1390016 EA THRUST REVERSER LEAKING A SWIA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 NM 07 800SK 15060 RECEIVED A "HYD 1 LO PRESS" CAUTION MESSAGE FOLLOWED BY AN "HYD EDP1" CAUTION MESSAGE. RETURNED TO SLC. REPLACED A FAU LTY O-RING AT THE THRUST REVERSER STOW LINE IAW CRJ 900 MM 78-32-00. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080725 SO 2008 7 25 SWIA200819821 1 20080627 A 2611 CONNECTOR EMB 120 EMB120ER 3260203 SO SMOKE DETECTOR LOOSE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 565SW 120340 FLT 3594 - NR 2 BAGGAGE SMOKE DETECTOR WILL NOT TEST. SECURED CONNECTOR ON SMOKE DETECTOR 2. ALL OPS CHECKS NORMAL. 2 L 7 2 4T RT A31SO 20080730 NM 2008 7 30 SWAA083696 1 20080704 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM BS 500C S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 15R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083720 1 20080704 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM BS 559 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083957 1 20080716 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727C S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083831 1 20080712 A 3350 767 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 259WN 35554 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083965 1 20080716 A 5311 6978188 FRAME BOEING 737 7373H4 1384600 NM BS 767 S13R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 13R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080731 SO 2008 7 31 C2XA08IA140 1 20080610 A 3350 7137216502 SIGN EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13965 145125 IAH - FLIGHT 2499, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE AISLE PATH LIGHTING BEYOND ROW 12 WOULD NOT IL LUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFT CEILING LIGHT ASSEMBLY. OPERATIONALLY CHECKED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080731 SO 2008 7 31 C2XA08ON133 1 20080607 A 3350 BULB EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT BURNED OUT A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 11189 7824 4194 14500931 FLT MX - ONT - WHILE PERFORMING 1A CHECK AND OPERATIONALLY CHECK EMERGENCY LIGHTS THE FWD EXIT SIGN AT ROW 12 DID NOT FU LLY ILLUMINATE. MX REMOVED AND REPLACED FWD EXIT SIGN AT ROW 12. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEA SED TO RETURN FOR SERVICE. (S) 2 L 7 2 4F RT 20080731 EA 2008 7 31 COMA0860312 1 20080627 A 3350 FUSE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BLOWN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 720SW 7297 FLOOR TRACK EMERGENCY LIGHTING STRIP FROM ROW 9 AFT FAILED TO ILLUMINATE DURING TEST. REPLACED INTERNAL FUSE ON EMERGEN CY LIGHT BATTERY CHARGER. (S) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 COMA0860317 1 20080707 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS 559 RBL 9 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 963CA 7127 DURING 559 INSPECTION FOUND .4 INCH CRACK ON INBOARD SIDE AND .5 INCH CRACK AT OUTBOARD SIDE, LOWER END, OF VERTICAL STI FFENER, RBL 9, FS 559. CUT OUT DAMAGE AND INSTALLED DOUBLERS PER BOMBARDIER REO 601R-53-41-057. (S) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 COMA0860302 1 20080622 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA LT WING TE FLAPS FAILED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 927CA 7671 7031 EN ROUTE FROM MCI TO CVG RECEIVED FLAPS FAIL CAUTION MSG AT 0 DEG. EMERGENCY DECLARED. ACFT LANDED SAFELY AT CVG. RE MOVED AND REPLACED LT BPSU. (S) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 COMA0860315 1 20080705 A 2910 MS219266D ELBOW CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A COMA L ABORTED APPROACH K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 01 779CA 7306 DURING APPROACH INTO LGA RECEIVED A GEAR DISAGREE WARNING MESSAGE, CREW DECLARED AN EMERGENCY, ABORTED APPROACH, THEN LA NDED WITHOUT INCIDENT ON SECOND ATTEMPT. REPLACED LEAKING ELBOW FITTING ON BYPASS RUNAROUND VALVE, PERFORMED GEAR SWING S, NO DEFECTS NOTED. (S) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 COMA0860272 1 20080608 A 5320 PAN CNDAIR CL600 CL6002B19 1900309 EA FS 193 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 30545 7117 FLOOR BELOW TRUSS CRACKED ON LT SIDE BELOW ACCUMULATOR GAUGE AT FS 193.00. REPAIRED FLOOR IAW REO 601R-53-11-081. (S) 2 L 7 2 4F RT A21EA 20080731 NM 2008 7 31 HNAA0800194 1 20080610 A 3350 0L3071BPEGPL LAMP DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS BURNED OUT A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 810EX 308 EMERGENCY FLOOR FLIGHTS OUT 3 & 5 POSITION. (S) 2 H 7 2 4T RT A13NM 20080731 NM 2008 7 31 HNAA0800187 1 20080523 A 3230 SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM MLG MALFUNCTIONED A HNAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 07 911HA 034 LANDING GEAR WOULD NOT RETRACT. GEAR SELECT PANEL BOTH INTRANSIT AND GREEN SAFE LIGHTS ILLUMINATED, DUPLICATED DISCREPA NCY ON JACKS FOR THE FIRST TIME. TAPPED ON LANDING GEAR SELECTOR VALVE AND GEAR RETRACTED. REMOVED AND REPLACED LANDIN G GEAR SELECTOR VALVE IAW 32-30-41R, OPS AND LEAK CHECK GOOD. SEE HA300 SEQ 6 ACFT RELEASED FOR EVALUATION FLIGHT DUE T O AFTER GEAR RETRACTION NO GEAR DOORS WILL CLOSE, MAINTENANCE REMOVED AND REPLACED RELAYS 3261-K5, 3261-K6 & 3261-K7 OPS CHECK GOOD ON GROUND, MAINTENANCE ACTION COMPLETE. SUBJECT TO SATISFACTORY EVAL FLIGHT. FACT 24 MAY 08 10:59 SBY EVAL FLT SAT. (S) 2 H 7 2 4T RT A13NM 20080731 EA 2008 7 31 COMA0860299 1 20080620 A 2621 346000371 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA AFT EQUIP BAY INTERMITTENT A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 713CA 15335 7245 EN ROUTE FROM CLE TO SYR RECEIVED CARGO BOTTLE LOW CAUTION MSG AT 28500. STAYED ON FOR 3 MIN THEN WENT OUT. EMERGENCY DECLARED, ACFT RETURNED BACK TO CLE AND LANDED SAFELY. REMOVED AND REPLACED CARGO FIRE BOTTLE. (S) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 COMA0860273 1 20080608 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FS 202 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 30545 7117 FORWARD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE AT FS 202.75. REPAIRED FORWARD PRESSURE BULKHEAD AT FS 202.75 IAW CRJ REO 601R-53-11-563. (S) 2 L 7 2 4F RT A21EA 20080731 NM 2008 7 31 HNAA0800196 1 20080607 A 7712 SEL0C2N INDICATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ENGINE TORQUE DEFECTIVE A HNAA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 07 808EX 13362 4732 299 NR 1 TO GAUGE, ANALOG PORTION INOPERATIVE. REMOVED AND REPLACED NR 1 TQ IND IAW MM 77-10-00, PAGES 201 & 202. OPS CHEC K GOOD, OK FOR SERVICE. (S) 2 H 7 2 4T 4 T RT A13NM E20NE 20080731 EA 2008 7 31 COMA0860278 1 20080609 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30068 NE THRUST REVERSER ILLUMINATED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 590SW 7077 EN ROUTE FROM LGA TO CHS RECEIVED LEFT REV UNLOCK MSG. ACFT DIVERTED TO JFK AND LANDED SAFELY. INSPECTED LT ENG T/R SY STEM. NO DEFECTS FOUND. PERFORMED OPS CHECKS OF T/R SYSTEM. ALL CHECKS GOOD. COULD NOT DUPLICATE MSG ON GROUND. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080731 EA 2008 7 31 CHQA200800117 1 20080618 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS SEIZED A CHQA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 465SM 2904 2904 7612 E873561 FLIGHT 5707, PNS TO IAH. ON APPROACH WHEN FLAPS WERE SELECTED FROM 30 TO 45, A FLAPS FAIL EICAS CAUTION MESSAGE WAS DIS PLAYED AND THE FLAPS WERE STUCK AT 42. THE FLIGHT WENT AROUND AND THEN LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGAT ED THE FECU AND FOUND THAT THE FLAP POWER DRIVE UNIT WAS AT FAULT. THE PDU WAS REPLACED AND THE ACFT WAS RETURNED TO SE RVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080731 EA 2008 7 31 COM2008F00000 1 20080615 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 420CA 19470 7451 RECEIVED FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED PDU. NO FURTHER DEFECTS . (S) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 COMA0860281 1 20080611 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 640 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 7117 DURING HMV-6, INSPECTION FOUND FLANGE OF FS 640 FRAME CRACKED BETWEEN STRINGERS 13R AND 14R. DAMAGED PORTION OF FLANGE CUT OUT AND REPAIR DOUBLER INSTALLED PER REO 601R-53-61-691. (S) 2 L 7 2 4F RT A21EA 20080731 SO 2008 7 31 C2XA08IA135 1 20080605 A 3350 BR90002 BALLAST EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14514 145303 IAH - FLIGHT 2452, DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL ODOR IN THE CABIN. MAINTENANCE INSPECTED THE ACFT, AND REMOVED AND REPLACED THE LIGHT BALLAST AT ROW SIX. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT W AS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080731 EA 2008 7 31 COMA0860303 1 20080621 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 927CA 7031 EN ROUTE FROM LGA TO CMH RECEIVED FLAPS FAIL CAUTION MSG AT 0 DEG. EMERGENCY DECLARED, ACFT LANDED SAFELY AT CMH. COMP LIED WITH TASK CARD SI-2-27I0001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION. (S) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 C2XA08ON138 2 20080611 A 7200 PANEL EMB 145 EMB145XR 3260214 SO RROYCE AE3007 AE3007A1E 54169 EA LEFT ENGINE OPEN A C2XA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 SW 27 12163 11900 6363 14500811 CAE312696 FLT 0224 - SMF - FLIGHT CREW HEARD A LOUD "BANG" AFTER TAKE OFF/CLIMB - E1 LOSING POWER AS INCREASING ALTITUDE TO SMF AN D DID AN AIR-RETURN AND DID NOT DECLARE AN EMERGENCY. MAINTENANCE FOUND OUTER BYPASS PANEL BLOWN OPEN AT 11 O`CLOCK. M AINTENANCE REINSTALLED OUTER BYPASS PANEL. OPERATIONALLY AND LEAK CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4F 4 F RT TE6CH 20080731 SO 2008 7 31 C2XA08ON139 1 20080614 A 3397 CONNECTOR EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS LOOSE A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 12201 6023 3184 14500959 FLT MX - ONT - WHILE PERFORMING 1A CHECK AND OPERATIONAL CHECK OF THE FWD EXIT SIGN AT ROW 12, IT WAS FOUND NOT ILLUMINA TING. MAINTENANCE PERSONNEL FOUND LOOSE CONNECTOR AND RE-ADJUSTED. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS REL EASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4F RT 20080731 EA 2008 7 31 C2XA08CL071 2 20080615 A 7261 KV291C8 CARBON SEAL EMB 135 EMB135ER 3260203 SO RROYCE AE3007 AE3007A13 54166 EA NR 2 ENGINE LEAKING A C2XA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION LD LANDING 1 SW 27 14508 145220 CAE311307 CLE FLIGHT 2290. THE CREW REPORTED ON SHORT FINAL RECEIVED AN ENG 2 LOW OIL PRESSURE WARNING MESSAGE. THE ENG WAS SHUT DOWN BY THE CREW IMMEDIATELY AFTER LANDING. MAINTENANCE INSPECTED AND FOUND MAJOR OIL LEAK AT THE REAR OF THE ENG. TH E NR 2 ENG WAS REPLACED. THE TEAR DOWN REPORT FROM ROLLS ROYCE INDICATED THE NR 5 AND 6 CARBON SEALS WERE LEAKING. THE SEALS WERE REPLACED AT THE OVERHAUL SHOP. (A) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080731 SO 2008 7 31 C2XA08CL066 1 20080607 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS FAULTY A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 11150 145756 CLE FLIGHT 2519. THE CREW REPORTED THE EMERGENCY LIGHT OVER THE EXIT ROW WAS INOPERATIVE. MAINTENANCE INSPECTED AND RE PLACED THE EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4F RT 20080731 SO 2008 7 31 CHQA200800106 1 20080606 A 3260 8005701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL NLG CRACKED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 275SK 145345 CAE312704 FLIGHT 5977, BUF TO CLE. UPON INITIAL CLIMB, THE GEAR WAS RAISED AND THE CREW SUSPECTED THAT THE NOSE GEAR DOOR REMAINE D OPEN DUE TO VIBRATIONS NEAR THE NOSE OF THE ACFT. EICAS SHOWED 3 WHITE UP INDICATIONS FOR THE GEAR. CREW RECYCLED TH E GEAR WITH NO CHANGE. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND REPLACED THE K0642 RELAY WHICH DID NOT CLEAR THE FAULT. THROUGH FURTHER TROUBLESHOOTING NOSE GEAR DOOR PROX SWITCH WAS CHANGED AND THE DOORS OPERATED NORMALLY. (S) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080731 GL 2008 7 31 CHQA200800114 2 20080615 A 7321 367934002 FCU EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007A 03030 GL LT ENGINE FALSE INDICATION A CHQA O OTHER O OTHER NR NOT REPORTED 1 GL 11 264SK 145221 CAE311337 FLIGHT 5855, ORF TO RIC. DURING CLIMB THE CREW RECEIVED A FUEL IMBALANCE AND FUEL LOW LEVEL MESSAGE ON EICAS FOR THE LT FUEL TANK. THE FLIGHT DIVERTED AND LANDED WITHOUT INCIDENT. THE FUEL QUANTITY WAS VERIFIED WITH THE MAGNETIC STICKS A ND THE LT FUEL INDICATION WAS DEFERRED. LATER THE REPEATER INDICATOR SHOWED A LT FCU FAIL MESSAGE AND THE FCU WAS REPLA CED. (S) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080731 SO 2008 7 31 C2XA08ON130 1 20080531 A 2810 DRAIN VALVE EMB 145 EMB145XR 3260214 SO VENTRAL TANK OPEN A C2XA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 27 11187 14500927 FLT 33 - TUL - FLIGHT CREW REPORTED FUEL LEAKING FROM VENTRAL TANK DURING PREFLIGHT. CONTRACT MAINTENANCE FROM AMERICAN AIRLINES CLOSED DRAIN VALVES. LEAK CHECK SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. TSN: 7747 CSN 4219 (S) 2 L 7 2 4F RT 20080731 EA 2008 7 31 HNAA0800185 1 20080531 A 3320 BV00330012150 BALLAST DHAV DHC8 DHC8311 1386006 EA CABIN LIGHTS BURNED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 327EN 29199 261 STRONG ELECTRICAL ODOR WHEN OVERHEAD LIGHT SELECTED ON, AT ROWS 9 THRU 11. INSPECTED AND FOUND ODOR COMES FROM ROW 9/10 AC OVERHEAD BULBS. REMOVED BOTH BULBS FROM OVERHEAD LIGHT SOCKETS 9/10 AC. PULLED C/B S2 ON RT C/B PANEL IAW SP 33.1 MEL 31MAY 08 15:47 PHL C15211 33-2 CABIN INTERIOR NORMAL LIGHTING SYSTEM JUN 08 03:42 ROA FOUND SOCKET AFT AT ROW9 AC BU RNT AND SMOKED. REPLACED SOCKET AND BALLAST IAW 33-00. OPS CHECK GOOD. CLEARED MEL. (S) 2 H 7 2 4T RT A13NM 20080725 EA 2008 7 25 SWIA200819850 1 20080712 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 935SW 7725 FLT 5820 - LEFT SIDE WINDOW CRACKED WHILE IN FLIGHT. REPLACED LEFT SIDE WINDOW IAW MM 56-12-01, P/N OFF: NP139322-001, S/N OFF: 02241H4783. 2 L 7 2 4F RT A21EA 20080725 EA 2008 7 25 SWIA200819851 1 20080710 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 944SW 7764 FLT 5844 - RIGHT WING CENTER EMERGENCY EXIT LIGHT IS INOP. INSTALLED A SERVICEABLE LAMP. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 20080725 CE 2008 7 25 GUU2008F00007 1 20080628 A 2810 TANK BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA FUEL SYSTEM LEAKING A GUUA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 81536 UE152 DURING FLIGHT, STRONG FUEL ODOR PRESENT IN CABIN. LT AUX TANK SUSPECT, LEAK AREA, REMOVED OLD SEALANT AND APPLIED NEW S EALANT. SEALANT CURE TIME ACCOMPLISHED. PERFORMED LEAK CHECK, NO FUEL NOTED. (K) 2 L 7 2 4T 3 T RT A24CE E2NE 20080725 NM 2008 7 25 R612008F00001 1 20080626 A 2780 SLAT SYSTEM EMB ERJ170 ERJ170200LR 3260121 NM GE CF34 CF34* 30015 NE LE SLATS MALFUNCTIONED A R61A O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 124HQ 17000200 CREW RECEIVED A SLAT FAIL MESSAGE ON APPROACH. DECLARED AN EMERGENCY AND LANDED AIRCRAFT WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT TO EVALUATE, CLEARED SF ACE INHIBITS SLAT FAIL MESSAGE CLEARED AND FLAP SLOW RATE MESSAG E APPEARED PLACED SLAT SLOW RATE ON MEL 27-53-02. RETURNED AC TO SERVICE. (K) 2 L 7 2 4F 4 F RT A56NM 20080725 EU 2008 7 25 VQI2008F00002 1 20080625 A 2120 UNKNOWN AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE CABIN SMOKE A VQIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 636VA 3460 AT APPROX 15:25Z (4 HOURS INTO FLIGHT) A CRUISE ALTITUDE, A "SMELL OF SMOKE BETWEEN ROWS 25 AND 26 LASTED APPROX 30 MIN" , BY AN IN-FLIGHT TEAM MEMBER. AFTER BEING ADVISED OF THE ISSUE VIA ACARS, MAINT CONTROL ADVISED THE CREW TO COMPLETEL Y TURN OFF THE IN-FLIGHT ENTERTAINMENT SYS (IFE) AS A PRECAUTION AND POSSIBLE FAULT ISOLATION. UPON LANDING, CREW MEMBE RS BRIEFED MAINT TECH FOR TROUBLESHOOTING ISSUE. AFTER A DETAILED VISUAL INSP AND EXTENSIVE OPS CHECK OF SUSPECTED SYS COMPONENTS, THE DISCREPANCY COULD NOT BE DUPLICATED DURING THE OVERNIGHT MAINT CHECK. SINCE NO DEFECT OR MALFUNCTION CO ULD BE IDENTIFIED, NO COMPONENTS WERE REPLACED. STC`S AND PMA`S ARE IN COMPLIANCE. AS OF NOW THERE ARE NO KNOWN AD OR 2 L 7 2 4F 4 F RT A28NM E38NE 20080725 SW 2008 7 25 P4Y2008F00000 1 20080607 A 5330 SKIN BELL 214 214ST 1182106 SW GE CT7TS CT72A 30030 NE FUSELAGE CRACKED E P4YA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 EA 39 5748M 28102 343014 STRUCTURAL DAMAGE TO AC LT SIDE TRANSMISSION AREA CAUSED BY CONTACT WITH FORKLIFT BASE DURING CARGO LOADING OPERATIONS. (K) 2 G 7 2 4U 4 U H10SW E8NE 20080722 EA 2008 7 22 A6WA200840467 1 20080502 A 5320 CROSSBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 438AW 7748 CROSSBEAM CRACKED AT FS 280 AND RBL 9.0. CROSSBEAM AT FS 280 RBL 9.0 REPAIRED IAW REO 601R-53-11-171 REV D. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840400 1 20080505 A 7603 THROTTLE CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE OUT OF ADJUST A A6WA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 31 431AW 7256 UPON ENGINE SHUTDOWN, RIGHT ENGINE CONTINUED TO RUN WITH THRUST LEVER IN SHUTOFF POSITION. WORKED THROTTLE LEVER, ENGIN E EVENTUALLY SHUTDOWN. ADJUSTED THROTTLE CONTROL RIGHT ENGINE IAW 76-11-17. PERFORMED IDLE SPEED CHECK IAW 70-00-00. OPS CHECK GOOD. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840379 1 20080501 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 435AW 7724 GEN NR 1 CAS MESSAGE AROUND 18,000 FT ON CLIMBOUT. COMPLIED WITH QRH AND STARTED APU. APU OIL CAS MASSAGE AT FL 29.0. APU OIL CHECK AND TEST COMPLIED WITH. C/W FIM 49-60-00 AND AMM 49-10-00 OPS TEST OF APU CHECKS NORMAL. VERIFIED NO ECU FAULT. CODES AND OIL SERVICE FOUND FULL APU OPS NORMAL. 2 L 7 2 4F RT A21EA 20080724 NM 2008 7 24 2008UALA03076 1 20080528 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN ODOR A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 515UA 24840 FLIGHT ATTENDANT REPORTS A "HOT PACK DUCTING" SMELL NEAR HER JUMP SEAT AT DOOR 2L. CHECK ELECTRICAL EQUIPMENT AROUND DO OR 2L FOR ANY BURNT AND ELECTRICAL SMELL. REMOVED AND INSPECTED AREA ABOVE DOOR 2L. NO ABNORMALITY FOUND AND NO BAD SM ELL. CHECKED WITH PACKS RUNNING AND NOTICED NO HOT AIR SMELL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 2008 7 24 2008UALA03243 4 20080606 A 3140 WARNING SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE COCKPIT ACTIVATED A UALA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 WP 29 117UA 28810 BOTH EICAS SCREENS CONSTANTLY CYCLING RANDOM WARNINGS AND MESSAGES. RTFL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080724 2008 7 24 2008UALA03294 4 20080609 A 3140 WARNING MESSAGE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 643UA 25093 FWD EQUIPMENT COOLING EICAS. 2 L 7 2 4F 4 F RT A1NM E24NE 20080724 NM 2008 7 24 2008UALA03302 1 20080610 A 3350 58721 LENS BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 930UA 26655 EXIT PATH LIGHTING AT ROW 3ABC COMING UP. FOUND LIGHT BROKEN. REPLACED THE FLOOR EEL LIGHT COVER AS NEEDED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 EU 2008 7 24 2008UALA03060 1 20080527 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 447UA 836 FLOORBEAM ITEM 210 HAS CORROSION. ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED BEAM 210 TRANSFERRED ALL CLIPS, AND INSTAL LED SPLICES. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03142 1 20080531 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 541UA 25253 ONE EMERGENCY LIGHT BULB DOES NOT ILLUMINATE ABOVE FWD RT OVERWING EXIT HATCH. LAMP INOP. RELAMPED LIGHT AT FWD RT OVE RWING EXIT, OPS CHECK WAS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03167 1 20080602 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 EXTERNAL FUSELAGE SKIN CORRODED UNDER FWD AIRPHONE ANTENNA LOC BS 1390. ACCOMPLISHED A MAJOR REPAIR AT GSO. REPAIR PER REO G12355 AND EVA 71616. THIS REPAIR HAS RECEIVED ONLY 1ST STAGE APPROVAL PENDING FATIGUE AND DTA EVALUATION BY BOEIN G TO SHOW COMPLIANCE WITH 14CFR 25.571 AND 26.43D. AIRPLANE MUST BE REMOVED FROM SERVICE ON 28MAY09 UNLESS A NEW 8100-9 IS ISSUED FINDING COMPLIANCE WITH 14CFR 25.571 AND 26.43D. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03324 1 20080611 A 5753 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT WING TE FLAP DAMAGED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 329UA 24149 LEFT INBOARD AFT FLAP CREASED FROM BIRD STRIKE. FOUND DAMAGE OUT OF LIMITS. REPLACED LEFT IB AFT FLAP REF MM 27-51-11 PG 401, ALL GAPS CHECKED WITHIN LIMITS, OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03327 1 20080609 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 845UA 1585 AIRCRAFT FAILS 3 SVC EMERGENCY LIGHTS TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03307 1 20080609 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 644UA 25094 LEFT EXT EMERGENCY LIGHT AFT OF WING INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20080724 NM 2008 7 24 2008UALA03229 1 20080605 A 5320 INTERCOSTAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 CABIN, JUST FWD OF L-2 DOOR CUTOUT, STR 12 CHORD SHOWS EVIDENCE OF CRACK JUST BELOW RADIUS BLOCK. MAJOR REPAIR ACCOMPLI SHED: REMOVED INTERCOSTAL WEB. FORMED & INSTALLED NEW INTERCOSTAL WEB (P/N 143N8334-27). 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 SWAA083806 1 20080713 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 15L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083938 1 20080715 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 435, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083711 1 20080704 A 5754 65C26602217 SLAT BOEING 737 7373G7 1384595 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING MV2 CK, FOUND NR 2 L/E SLAT OUTBOARD T/E DELAMINATED. REMOVED AND REPLACED SLAT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083717 1 20080704 A 3350 300432 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 752SW 29804 DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 2008UALA03332 1 20080611 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 507UA 24743 DOOR 2R EXT EMERGENCY LIGHT INOP. BULB INOP. RELAMPED DOOR 2R EXT EMERGENCY LIGHT, OPS CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03413 1 20080615 A 2910 PRESSURE SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE LEAKING A UALA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 29 661UA 27158 L HYD QUANTITY ZERO. RAMP NOTES, FLUID LEAKING FROM LEFT ENGINE. PACKING IN LT SYSTEM PRESSURE SWITCH TORN. REPLACED S WITCH AND PACKING. SERVICED HYDRAULIC RESERVOIR AND PRESSURE CHECKED OP CHECK NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080725 NM 2008 7 25 2008UALA03260 1 20080606 A 5415 FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 NR 1 PYLON "DELTA" FITTING CRACKED ON OUTBOARD SIDE. ACCOMPLISHED MAJOR REPAIR AT GSO. REPLACED DELTA FITTING PER SRM 51-40-02. LEAK CHECKED ALL LINES PER MM 29-00-98, LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080725 NM 2008 7 25 CALA0800640 1 20080623 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM BS 867 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 RIGHTHAND SIDE STATION 867 FRAME BETWEEN S-8 AND S-9 AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRE D FRAME AT STATION 867 BETWEEN S8 AND S9R PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080725 EA 2008 7 25 VNAA0805015 1 20080512 A 5246 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF348C1 30049 NE SERVICE PANEL OPEN A VNAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 05 702PS 10135 CREW REPORTED A SERVICE PANEL DOOR LEFT OPEN. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE I NSPECTED AND FOUND THE SERVICE PANEL DOOR OPEN. MAINTENANCE SECURED THE DOOR CLOSED. NO DEFECTS OR DAMAGE AT THIS TIME . AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080725 NM 2008 7 25 CALA0800650 1 20080627 A 5330 6546881 SKIN BOEING 737 737524 1384721 NM BS 1019 S11L DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 DENT IN FUSELAGE SKIN LEFTHAND AT STATION 1019 BELOW S-11 OUT OF ALLOWABLE DAMAGE LIMITS PER SRM 53-00-01 FIG 101. CUT OUT DENTED SKIN AND INSTALLED REPAIR IAW SRM 53-80-01 FIG 201. TOTAL ADDITIONAL WEIGHT OF REPAIR PARTS .325 LB. 2 L 7 2 4F RT A16WE 20080725 EA 2008 7 25 SWIA200819834 1 20080705 A 2612 47259702 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA FIRE DETECTOR FAILED A SWIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 07 965SW 7871 FLT 6150 - LEFT FIRE FAIL MESSAGE DURING TAXI OUT. REPLACED FIRE DETECTION CONTROLLER WITH A SERVICEABLE UNIT. OPS CHE CK GOOD. 2 L 7 2 4F RT A21EA 20080725 SO 2008 7 25 SWIA200819849 1 20080709 A 3233 ACTUATOR EMB 120 EMB120ER 3260203 SO LT MLG FAILED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 237SW 120314 FLT 3618 - RECEIVED A LEFT MAIN DISAGREEMENT LIGHT ON CLIMB-OUT. REPLACED LEFT MAIN LANDING GEAR ACTUATOR IAW 32-32-10. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 20080725 SW 2008 7 25 LEU2008F00000 1 20080715 A 6520 1B8045P CHIP DETECTOR BOLKMS 117 BK117C2 5626002 SW TMECA ARRIEL ARRIEL1E 60034 NE T/R GEAR BOX SHORTED E LEUA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 17 373TC 9073 ON 7/15/2008 AIRCRAFT MADE A PRECAUTIONARY LANDING DUE TO ILLUMINATION OF A TAIL ROTOR CHIP CAUTION LIGHT. INSPECTION R EVEALED A DEFECTIVE CHIP DETECTOR WHICH GAVE A FALSE INDICATION. (K) 1 G 7 2 3U 3 U H13EU E19EU 20080725 CE 2008 7 25 Z5F2008F00000 1 20080708 A 2611 47359717 SMOKE DETECTOR CESSNA 525 525 2076601 CE CARGO BAY DEFECTIVE E Z5FA O OTHER N FALSE WARNING AP APPROACH 1 EA 63 409CS 2654 525B0045 ON APPROACH, CREW OBSERVED BAGGAGE SMOKE ANNUNCIATION. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT, FIRE DEPART MENT PERSONNEL FOUND NO INDICATION OF SMOKE OR FIRE. MAINT PERSONNEL TROUBLESHOT SYSTEM AND REPLACED SUSPECTED DEFECTIV E SMOKE DETECTOR AND TESTED SYSTEM WITH "SMOKE IN A CAN" AND DETERMINED SYSTEM OPERATIONAL CHECK SATISFACTORY. AC RETURN ED TO SERVICE. (K) 1 L 7 2 4F RT A1WI 20080725 NM 2008 7 25 HNA2008F00005 1 20080709 A 3350 6013211X POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE EMERGENCY LIGHTS BROKEN A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 816EX 39912 329 RT FWD EMERGENCY LIGHT IS DIM. REMOVED AND REPLACED BATTERY, FOUND CAMLOCK ON BATTERY BROKEN , CAUSING LOOSE CONNECTION . OP CHECK GOOD. (K) 2 H 7 2 4T 4 T RT A13NM E20NE 20080725 NM 2008 7 25 GTI2008F00001 1 20080519 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 506NK 2490 RT FLOORBEAM - Y1292 FRAME 68-69 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM. (K) 2 L 7 2 4F RT A28NM 20080725 CE 2008 7 25 GUU2008F00004 1 20080705 A 3240 BRAKE ASSY BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA RIGHT WEAK A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81538 UE199 AFTER LANDING, CAPTAINS RT BRAKE PEDAL LOST PRESSURE. GRAVITY BLED ALL BRAKES. OPS CHECK GOOD. (K) 2 L 7 2 4T 3 T RT A24CE E2NE 20080725 CE 2008 7 25 GUU2008F00006 1 20080704 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA FUEL SYSTEM ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 81536 UE152 DURING FLIGHT, STRONG SMELL OF FUEL VAPORS IN CABIN. DRAINED RT AUX TANK. TEST RAN AIRCRAFT FOR 40 MINUTES. NO FUEL SME LL NOTED. (K) 2 L 7 2 4T 3 T RT A24CE E2NE 20080725 CE 2008 7 25 26N2008F00000 1 20080531 A 2916 991242322 VALVE CESSNA 525 525 2076601 CE WILINT FJ44 FJ44 66000 GL HYD MANIFOLD UNSERVICEABLE E 26NA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 EA 05 72JW 1640 5250406 WHILE ON A TRAINING FLIGHT THE FLIGHT CREW SELECTED "FLAPS" ON APPROACH. AS THEY LINED UP ON THE ILS THEY SELECTED "SPE ED BRAKES" AND REALIZED THAT THY HAD NO HYDRAULICS ON THE AIRCRAFT. WHEN "GEAR DOWN" WAS SELECTED, THE CREW DID NOT SEE A DOWN AND LOCKED CONDITION. FOLLOWING EMERGENCY CHECK LIST, THE GEAR WAS BLOWN DOWN WITH THE EMERGENCY EXTENSION PROC EDURE AND THE AC CONFIGURED WITH 3 IN THE GREEN FOR LANDING. AC LANDED UNEVENTFULLY. MAINT INSPECTED THE AC FOR LEAKS AND FOUND NONE. ELECTRICAL PWR WAS APPLIED TO THE AC AND THE LANDING GEAR AND HYDRAULIC SYS CHECKED ELECTRICALLY WITH N O PROBLEM FOUND. THE AC WAS JACKED AND HYDRAULIC PRESSURE APPLIED WITH THE LT PUMP TO ATTEMPT A GEAR SWING. INDICATION 1 L 7 2 4F 4 F RT A1WI E3GL 20080725 WP 2008 7 25 IXX2008F00014 1 20080718 A 2612 FIRE WARNING DOUG DC8 DC873F 302199F WP NR 4 ILLUMINATED A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 602AL 45991 DURING CLIMB, THE NR 4 FIRE WARNING CAME ON. THE CREW ACCOMPLISHED THE APPROPRIATE CHECKLIST AND DISCHARGED BOTH FIRE B OTTLES. THE AC LANDED WITHOUT INCIDENT. CORRECTIVE ACTION IN WORK. (K) 2 L 7 4 4F RT 4A25 20080725 NE 2008 7 25 QML2008F00003 2 20080612 A 7320 A1282Z3 DRAIN VALVE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE LEAKING E QMLA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 03 115LN 4155 19065 ENROUTE TO SCENE, CREW MEMBER DETECTED A FUEL ODOR. THERE WERE NO UNUSUAL COCKPIT INDICATIONS SUCH AS EXCESSIVE FUEL CO NSUMPTION, BUT, IAW BRIEFING THE PILOT ABORTED THE FLIGHT AND RETURNED TO BAS. MAINTENANCE FOUND A DRAIN VALVE ON THE F UEL FILTER LEAKING. (K) 1 G 7 1 3U 3 U H9EU E19EU 20080725 NE 2008 7 25 QML2008F00004 2 20080612 A 7530 430110212 MODULATOR BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650A2 41560 NE NR 2 AIR FLOW STICKING E QMLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 03 158BK DURING ANNUAL TRAINING/CHECK RIDE, THERE DEVELOPED AN UNCOMMANDED, INTERMITTENT TORQUE SPLITS OF UP TO 25 PERCENT WITH N O COLLECTIVE MOVEMENTS OR TORQUE MATCHING ATTEMPTS. N1 AND TOT INDICATIONS FOLLOWED EACH ENGINE THROUGH THE SPLITS. FUR THER TROUBLESHOOTING PROVIDED NO CONCLUSIVE REASON FOR THESE SPLITS. THIS AIRCRAFT HAD EXPERIENCED THE SAME PROBLEMS JU ST A COUPLE OF WEEKS AGO AND HAD AN ENGINE CHANGE AS A RESULT. DECISION WAS MADE TO RETURN AC TO AN AIRFIELD INSTEAD OF THE HOSPITAL PAD DUE TO THE DESIRE TO SHOOT A SINGLE-ENGINE PROFILE TO LANDING. EMERGENCY WAS DECLARED TO TOWER AND A SUCCESSFUL RUN-ON LANDING ACCOMPLISHED. AFTER MAINT EVALUATION AND TROUBLESHOOTING, IT WAS DETERMINED TO BE THE AIR FLO 1 G 7 2 3U 3 U H13EU E5NE 20080725 WP 2008 7 25 IXX2008F00015 1 20080718 A 2612 FIRE WARNING DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE ILLUMINATED A IXXA O OTHER J WARNING INDICATION CR CRUISE 1 SW 11 820BX 46065 DURING CRUISE, THE NR (3) FIRE WARNING CAME ON. THE CREW ACCOMPLISHED THE APPROPRIATE CHECK LIST AND DISCHARGED BOTH FI RE BOTTLES, AND CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. CORRECTIVE ACTION IN PROGRESS (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 20080725 NM 2008 7 25 MWE2008F00015 1 20080703 A 7830 DOOR BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE THRUST REVERSER CRACKED A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 918ME 55180 RT THRUST REVERSER UPPER DOOR, Z FRAME, AT STA 26.666 HAS A CRACKED REPAIR AT THE RT END. FABRICATED AND INSTALLED DOUB LER. (K) 2 L 7 2 4F 4 F TR A6WE E00061EN 20080725 EA 2008 7 25 N6W2008F00000 1 20080628 A 2751 5893783 SENSOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* 30015 NE FLAP SKEW FAILED A N6WA O OTHER J WARNING INDICATION LD LANDING 1 CE 03 153GJ 10219 FLAP FAIL CAUTION MESSAGE. REMOVED AND REPLACED LT IB FLAP, SKEW DETECTOR IAW CRJ700 AMM 27-52-48. OPS CHECK GOOD. LT WING IB FLAP OB POSITION.(K) 2 L 7 2 4F 4 F RT A21EA 20080725 EU 2008 7 25 NSV2008F00002 1 20080604 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN SMOKE A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 27 370PX 340B300 AFTER SHUTTING DOWN RT ENGINE MASTER WARNING CARGO SMOKE LIGHT ILLUMINATED, STAYED ON, DISCHARGED EXTINGUISHER IN CARGO COMPARTMENT. NO SMOKE/ FLAMES NOTED BY GROUND CREW ALSO SMELLED ELECTRICAL SMOKE IN FORWARD CABIN AREA. INSPECTED GALL EYS, AVIONICS COMPARTMENT AND FWD CABIN LIGHT FIXTURES FOR EVIDENCE OF BURNED WIRES. NONE FOUND. DEFERRED CARGO COMPART MENT FIRE BOTTLES IAW MEL 26-13-2 CAT C ID 31069. ONCE AIRCRAFT WAS IN AIRPORT, THE AVIONICS TECH WAS ABLE TO DUPLICATE THE ERRONEOUS CARGO SMOKE LIGHT, AND ATTRIBUTED IT TO LOW VOLTAGES ON BOTH BATTERIES. BOTH MAIN BATTERIES AND CARGO FI RE BOTTLES WERE REPLACED AND CORRECTED PROBLEM. (K) 2 L 7 2 4T 4 T RT A52EU E8NE 20080725 WP 2008 7 25 IXX2008F00005 1 20080711 A 2612 FIRE WARNING DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE NR 3 NACELLE MALFUNCTIONED A IXXA O OTHER N FALSE WARNING CR CRUISE 1 SW 11 603AL 46003 DURING FLIGHT, NR 3 ENGINE FIRE WARNING LIGHT ILLUMINATED MOMENTARILY. FLIGHT CREW RETARDED THE THROTTLES AND SHUTDOWN THE ENGINE. THE FIRE LIGHT AND WARNING WENT OUT. APPROX 30 MINUTES LATER FIRE WARNING CAME BACK ON. FLIGHT CREW FIRED ONE BOTTLE AND AGENT DISCHARGED. LIGHT WENT OUT AND NEVER CAME BACK ON. AC FLEW DIRECT TO ARRIVAL AIRPORT AND LANDED W ITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED ALL FIRE SENSING ELEMENT ON NR 3 ENGINE. OPS CHECK GOOD IAW MM 26-10-16. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 20080725 2008 7 25 RYN2008F00000 4 20080701 A 3460 COMPUTER BOEING 757 757236 1384971 NM RROYCE RB211 RB211* 54555 NE FCC MALFUNCTIONED A RYNA O OTHER J WARNING INDICATION CR CRUISE 1 GL 31 526NA 24794 AIR TURN BACK, DUE TO LOSS OF ALL 3 AUTO PILOTS AND THE CAPTAIN`S FLIGHT DIRECTOR, COULD NOT ENTER RVSM AIRSPACE. RESET LT FCC AND ACCOMPLISHED TEST 2 AND 10 IAW AMM 22-30-00. ALL CHECKED NORMAL. (K) 2 L 7 2 4F 4 F RT A2NM A12EU 20080725 WP 2008 7 25 J7E2008F00000 2 20080612 A 7200 66002023 MODULATING VALVE LEAR 35 35LEAR 5170600 CE GARRTT TFE731 TFE731* 01518 WP RT ENGINE FAILED E J7EA O OTHER O OTHER NR NOT REPORTED 1 WP 07 35AX 1716 1433 280 AT FL400 ENROUTE, THE RAT WAS ABOUT -38C AND NOT IN ICING CONDITIONS. DURING DESCENT, NOTED ABNORMALLY HIGH N1 & ITT IN DICATIONS FOR DESCENDING FLIGHT AT IDLE. FOUND COULD ADD POWER, BUT NOT REDUCE IT . ACTIVATED NAC HEAT ON BOTH ENGINES IN AN ATTEMPT TO RESTORE NORMAL OPERATIONS, SUSPECTING ICE MAY HAVE SOMEHOW FORMED IN THE PT2/TT2 PROBES. THIS RESULTE D IN NO CHANGE TO THE SITUATION. ELECTED TO RUN THE ABNORMAL ENG OPS CHECKLIST. LT THRUST LEVER WAS RETARDED TO IDLE & LT FUEL COMPUTER WAS SWITCHED TO THE OFF POSITION. ENG DID IN FACT SPOOL DOWN TO ABOUT 35 PERCENT N1, BUT WE ALSO INSTA NTANEOUSLY LOST CABIN PRESSURE. OBSERVED THE CABIN CLIMB/DESCENT GAUGE "PEGGED" ON CLIMB. INITIATED AN EMERGENCY DESCE 2 L 7 2 4F 4 F A10CE E6WE 20080725 WP 2008 7 25 IXX2008F00016 1 20080710 A 2612 FIRE DETECTOR DOUG DC8 DC873F 302199F WP NR 3 NACELLE MALFUNCTIONED A IXXA O OTHER O OTHER NR NOT REPORTED 1 SW 11 602AL 45991 DURING CRUISE, NR 3 FIRE WARNING CAME ON, THE CREW DISCHARGED BOTH FIRE BOTTLES AND SHUTDOWN NR 3 ENGINE. THE CREW LAND ED WITHOUT INCIDENT. MAINTENANCE REPLACED RT CORE SENSING ELEMENT, LT AND RT FAN FIRE SENSING ELEMENT, AND BOTH FIRE BO TTLES, OPS CHECK GOOD IAW MM 26-10-1, AND 26-20. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 4 4F RT 4A25 20080725 CE 2008 7 25 BQV2008F00000 1 20080701 A 3240 30146 BRAKE BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A60A 52043 NE RIGHT LEAKING E BQVA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 01 689BV BB338 UPON TAXI OUT AT AIRCRAFT LOST BRAKING ON RT MLG. THE AIRCRAFT WAS BROUGHT TO MAINTENANCE SEALS ON THE RT BRAKE ASSY WE RE REPLACED SYS WAS BLEED AND SERVICED WITH FLUID. NO DEFECTS NOTED; AIRCRAFT WAS RETURNED TO SERVICE. (K) 1 L 7 2 4T 4 T A24CE E4EA 20080725 NM 2008 7 25 GTI2008F00002 1 20080519 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 506NK 2490 MINOR CORROSION ON FLOOR SUPPORT Y254, FRAME 67-68. REMOVED AND REPLACED FLOOR SUPPORT. (K) 2 L 7 2 4F RT A28NM 20080725 CE 2008 7 25 ESP2008F00000 1 20080705 A 2497 70008840 CIRCUIT BREAKER LEAR 35 35A 5170602 CE GARRTT TFE731 TFE731* 01518 WP RT CB PANEL LOOSE E ESPA O OTHER O OTHER NR NOT REPORTED 1 SO 11 568PA 205 (30) MINUTES AFTER THE ACTIVATION OF WINDSHIELD HEAT, THE RT ESSENTIAL BUS CIRCUIT BREAKER POPPED. CREW COMPLETED EMERG ENCY CHECKLIST FOR AN ELECTRICAL FAILURE. THE CIRCUIT BREAKER WOULD NOT RESET. ATC GAVE VECTORS AND DESCENT. CREW DID A VISUAL APPROACH. NO EMERGENCY WAS DECLARED BY THE FLIGHT CREW, AIRPLANE LANDED WITHOUT INCIDENT. (K) 2 L 7 2 4F 4 F A10CE E6WE 20080725 NM 2008 7 25 GTI2008F00003 1 20080519 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSLEAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 506NK 2490 FLOOR SUPPORT Y254, FRAME 68-70 HAS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT. (K) 2 L 7 2 4F RT A28NM 20080728 WP 2008 7 28 UPS08852585 1 20080610 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 SEAT TRACK CRACKED AT LBL 60 AND STA 1303. REPAIRED CABIN SEAT TRACK AT STA 1303 AND LBL 60 IAW SRM 53-02-03-0 FIG 0006D. 2 L 7 4 4F RT 4A25 20080728 WP 2008 7 28 UPS08852584 1 20080613 A 5230 WEB DOUG DC8 DC871F 302199D WP CARGO DOOR CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 C-PIT CROSS SLIDE DOOR INTERIOR SURFACE AT AFT UPPER AREA, INTERNAL WEB HAS REPAIR DOUBLER WITH SEVER E CHAFE WEAR. FABRICATED AND REPLACED C-PIT DOOR INTERIOR WEB REPAIR DOUBLER IAW SRM 52-02-00 FIG 002, SRM 52-04-01 FIG 001. 2 L 7 4 4F RT 4A25 20080728 WP 2008 7 28 UPS08852583 1 20080606 A 5320 PANEL DOUG DC8 DC871F 302199D WP RT MLG CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 RIGHT WING LANDING GEAR WELL SEAL PANEL CRACK REPAIR. REPAIRED RIGHT WING GEAR WELL SEAL PNL VERTICA L WEB AND SPLICE DOUBLER IAW DWG 5643410, SRM 57-02-00-0 FIG 2A, SRM 51-01-20D, SRM 51-01-21-0, SRM 51-01-20A-0, SRM 51- 03-00-0. 2 L 7 4 4F RT 4A25 20080728 NM 2008 7 28 NOC2008F00001 1 20080606 A 5610 WINDOW BOEING 767 76739H 1385311 NM COCKPIT MALFUNCTIONED A NOCA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 760NA 26257 ON TAKEOFF ROLL AT 70 KTS "R SIDE WINDOW" EICAS CAUTION MESSAGE DISPLAYED, ABORTED TAKEOFF. C/A: REMOVED AND REPLACED R 3 WINDOW IAW MM 56-11-10. OPS CHECK OK. (K) 2 L 7 2 4F RT A1NM 20080728 CE 2008 7 28 DJF2008F00001 1 20080604 A 5400 SKIN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LT INLET CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 482LX RK413 DURING ROUTINE MAINTENANCE THE LT INLET SKIN AT THE INLET TEMP PROBE WAS FOUND CRACKED. THE SDR WILL BE UPDATED UPON CO MPLETION OF THE C/A. (K) 2 H 7 2 4F 4 F RT A16SW E25EA 20080728 CE 2008 7 28 DJF2008F00008 1 20080613 A 5522 HINGE BRACKET CESSNA 750 750 2076810 CE LT ELEVATOR CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 701LX 5519 7500114 DURING PHASE INSPECTION IT WAS FOUND THAT THE LT ELEVATOR IB HINGE BRACKET WAS CRACKED BEYOND LIMITS. (K) 2 L 7 2 4J RT T00007WI 20080728 CE 2008 7 28 DJF2008F00000 1 20080619 A 7160 SKIN BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LT INLET CRACKED E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 439LX RK284 DURING A ROUTINE SERVICE CHECK IT WAS NOTED THAT THE LT ENGINE INLET INNER SKIN WAS CRACKED AT THE 9 O’CLOCK POSITION. THE SDR WILL BE UPDATED UPON COMPLETION OF THE C/A. (K) 2 H 7 2 4F 4 F RT A16SW E25EA 20080728 CE 2008 7 28 DJF2008F00007 1 20080612 A 3340 LIGHT BEECH MU300 400A 1155402 CE TAIL MISSING E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 710TA RK183 DURING A PHASE 1 INSPECTION IT WAS FOUND THAT THE VERTICAL TAIL NAVIGATION LIGHT ASSY WAS MISSING. THE SDR WILL BE UPDA TED UPON COMPLETION OF THE CORRECTIVE ACTION. (K) 2 H 7 2 4F RT A16SW 20080728 CE 2008 7 28 DJF2008F00006 1 20080621 A 2611 SMOKE DETECTOR RAYTHN DH125 HAWKER800XP 7150012 CE CARGO BAY MALFUNCTIONED E DJFA O OTHER N FALSE WARNING CR CRUISE 1 EA 23 807LX 258413 WHILE AT CRUISE THE CREW REPORTED UPON OPENING THE FLIGHT DECK HEAT VALVE THE BAGGAGE FIRE LIGHT ILLUMINATED INTERMITTEN TLY. MX GAINED ACCESS TO ALL 3 SMOKE DETECTORS WITH ENGINE AND APU RUNNING FOR OVER AND HOUR VERIFIED NO SMOKE, AN OPS CHECK OF THE SYS REVEALED NO ISSUES. (K) 2 L 7 2 4F RT A3EU 20080728 NM 2008 7 28 UPS08M52610 1 20080629 A 2450 CIRCUIT BREAKER DOUG MD11 MD11F 3023600 NM COCKPIT TRIPPED A IPXA D RETURN TO BLOCK O OTHER UK UNKNOWN 1 SO 01 283UP 48484 INSPECTION TYPE:N/A MULTIPLE CIRCUIT BREAKERS TRIPPED & WILL NOT RESET. WORK ACCOMPLISHED PER EO MD11-2400-29911-C. REP LACED DAMAGED WIRE BUNDLE AND RELATED COMPONENTS. 2 L 7 3 4F RT A22WE 20080728 WP 2008 7 28 UPS08852606 1 20080524 A 3210 FITTING DOUG DC8 DC873F 302199F WP RT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 RIGHT WHEEL WELL AT UPPER FWD BULKHEAD, HYDRAULIC MANIFOLD PULLEY BRACKET IS CRACKED. REMOVED CRACKE D FITTING, REPAIRED AND RE-INSTALLED FITTING IAW SRM 20-16-0, 51-1-8, DPS 4.706, DPS9.18. 2 L 7 4 4F RT 4A25 20080728 2008 7 28 WRN2008F00001 4 20080616 A 3457 CONNECTOR AIRBUS 300 A300B4203 3930306 EU GPS ANTENNA DIRTY A WRNA O OTHER O OTHER NR NOT REPORTED 1 EA 39 505TA 6600 271 AFTER TAKEOFF, APPROX 40 MINUTES INTO FLIGHT, AC TURNED BACK DUE TO NAV PROBLEMS WITH GPS SYSTEM. GPS SYS NR 2 PREVIOUS LY MEL, NR 1 GPS SYS WENT TO DR MODE. AIRCRAFT RETURNED TO BASE, NORMAL LANDING ACCOMPLISHED. MX CLEANED AND RESET CON NECTION ON GPS ANTENNA CONNECTOR IAW 34-58-11. THIS ACTION CLEARED NR 2 GPS MEL AND CORRECTED NR 1 GPS SYS GOING TO DR MODE. SYSTEMS OPERATES SATISFACTORY, AC RETURNED TO SERVICE. (K) 2 L 7 2 4F RT A35EU 20080728 NM 2008 7 28 UIE2008F00001 1 20080701 A 5311 FRAME BOEING 747 747243B 1384830 NM BS 400 CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 540MC 22508 FRAME CRACKED AT STATION 400, STRINGER 22R. REPLACED DAMAGED FRAME IAW SRM 51-10-01 AND SRM 51-30-02. (K) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 UPS08652605 1 20080623 A 3260 284T0520U2 BRACKET BOEING 767 76734AF 1385212 NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 325UP 27751 INSPECTION TYPE:AD NOSE LANDING GEAR WHEEL WELL RT SENSOR BRACKET CRACK. CRACK LENGTH .375 INCH. NOSE LANDING GEAR WHE EL WELL RT SENSOR SUPPORT BRACKET REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20080728 NM 2008 7 28 UPS08652604 1 20080627 A 3350 BPS73 POWER SUPPLY BOEING 767 76734AF 1385212 NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 312UP 27763 INSPECTION TYPE:PS1 EMERGENCY LIGHTS ARE INOP WITH NO PWR. REMOVED AND REPLACED PWR SUPPLY UNIT IAW MM 33-51-07-2, SYST EM OPS CHECKS NORMAL. 2 L 7 2 4F RT A1NM 20080728 EU 2008 7 28 NSV2008F00001 1 20080604 A 3320 LIGHT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE CABIN SPARKS A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 27 294CJ 340B294 FA SAW SPARKS COMING OUT OF THE WINDOW LIGHTS OVER ROW 2F WHEN BATTERIES ARE ON, NO LIGHT IN THE CABIN ILLUMINATES. INS PECTED LIGHT AND SOCKETS AT ROW 2 & 3, NO DEFECTS NOTED. PERFORMED OPERATIONAL TEST OF CABIN LIGHTS SYSTEM IAW AMM 33-2 1-05-05 WINDOW LIGHT AT SEAT 8A FOUND INOPERATIVE. DEFERRED IAW MEL 33-20-1-1 CAT C ID 31077. (K) 2 L 7 2 4T 4 T RT A52EU E8NE 20080722 EA 2008 7 22 A6WA200840476 1 20080507 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 438AW 7748 CRACK ON PAX DOOR EDGE MEMBER AT FS 316. CRACK ON PAX DOOR EDGE MEMBER AT FS 316 REPAIRED IAW REO 601R-52-11-279. (A) 2 L 7 2 4F RT A21EA 20080722 EA 2008 7 22 A6WA200840402 1 20080513 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ODOR A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 439AW 7753 ELECTRICAL ODOR WHILE AT GATE. PACKS ON APU BLEEDS. NOTED SCENT FROM LEFT SIDE FIRST. INSPECTED LIGHTS IN FLIGHT DECK , NO ODOR DETECTED, PERFORMED ENGINE FIRE TEST, NO ODOR OR DEFECTS DETECTED. INSPECTED AVIONICS BAY, NO SMOKE OR ODOR D ETECTED. NO ELECTRICAL ODOR COMING FROM EITHER PACK WITH APU AIR OR ENGINE AIR. NO ODOR DETECTED WHEN WINDOW HEAT OR P ITOT HEAT SELECTED ON, NO ODOR DETECTED WHEN SELECTING THRU FANS, DISPLAY OR ARINC. AIRCRAFT OK FOR SERVICE. (A) 2 L 7 2 4F RT A21EA 20080722 WP 2008 7 22 ABXA080162 1 20080519 A 5320 991050118 CUSP WEB DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 CUSP WEB CRACKED FORWARD OF STA 560 RT. REPAIRED CRACK IAW DC9 SRM. (A) 2 L 7 2 4F A6WE 20080724 NM 2008 7 24 SWAA083710 1 20080702 A 3397 W116092820 WIRE BOEING 737 7373G7 1384595 NM CABIN CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 EMERGENCY EXIT LIGHT ILLUMINATED ERRATICALLY. FOUND ELEC WIRE CHAFED AT BS 945. REPAIRED PER MM. 2 L 7 2 4F RT A16WE 20080805 NM 2008 8 5 F3L2008F00000 1 20080610 A 5320 D53913679020002 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 REFERENCE NON ROUTINE 34045. DURING C3 S1 C-CHECK INSPECTION NOTED FORWARD CARGO PIT PROFILE AT FRAME C28 HAS CORROSION IN NUT PLATE AND RIVETS. MAINTENANCE REMOVED CORROSION FROM NUT PLATE PROFILE AND FOUND PROFILE TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11, SRM 51-46-11 AND SRM 51-44 -11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 NM 2008 8 5 NWAA082775647 1 20080617 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 547US 26494 DURING OVERNIGHT MAINTENANCE SEVERAL EMERGENCY LIGHTS, INCLUDING ESCAPE PATH LIGHTS AT ROWS 23 THROUGH 25, AND EXIT SIGN S AT ROWS 21DEF AND 22ABC WOULD NOT TEST. MAINTENANCE REPLACED THE ASSOCIATED EMERGENCY LIGHT BATTERY PACK AT 21DEF, AL L OPERATIONS CHECKED NORMAL. (A) 2 L 7 2 4F RT A2NM 20080805 EU 2008 8 5 NWAA082823305 1 20080620 A 3350 POWER SUPPLY AIRBUS 330 A330323 3930335 EU EMERGENCY LIGHTS FAULTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 805NW 00552 EPSU FAULT (17WC), REPLACED POWER SUPPLY (17WC) AND CHECKS GOOD. (A) 2 L 7 2 4F RT A46NM 20080805 GL 2008 8 5 C2XA08ON152 2 20080710 A 7200 ENGINE EMB 145 EMB145XR 3260214 SO ALLSN AE3007 AE3007A 03030 GL LEFT MALFUNCTIONED A C2XA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 27 14186 8821 14500924 CAE312828 FLT 0110 - ELP - FLIGHT CREW REPORTED LOST E1 OIL QTY DROPPED TO 2 QTS, OIL TEMP WENT INTO THE RED ON CLIMB, E1 SHUTDOWN ON ITS OWN. FLIGHT CREW DECLARED EMERGENCY AND LANDED IN ELP WITHOUT INCIDENT, WHERE MX PERSONNEL IS CURRENTLY CHANGIN G E1. MX PERSONNEL COMPLETED ENGINE 1 R/R OPERATIONALLY CHECKED SATISFACTORY AIRCRAFT WAS RELEASED TO RETURN TO SERVICE . (A) 2 L 7 2 4F 4 F RT TE6CH 20080805 NM 2008 8 5 NWAA082866623 1 20080624 A 5250 STRIKER BOEING 747 747251B 1384892 NM COCKPIT DOOR UNKNOWN A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 623US 21705 FLIGHT DECK DOOR LOCK FAIL LIGHT ILLUMINATED. SMOKE WAS DETECTED FROM DOOR LOCK MECHANISM. FLIGHT DECK ACCESS SWITCH S ET TO OFF AND SMOKE CEASED. COCKPIT DOOR SYSTEM PLACARD INOP PER MEL 52-33A AND ENTERED IN LIDS AND REMOVED DDG. (A) 2 L 7 4 4F RT A20WE 20080805 EU 2008 8 5 AALA200801557 1 20080607 A 3411 0851HV PITOT TUBE AIRBUS 300 A300B4605R 3930308 EU FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 80052 460 PTY INFLIGHT T2110/07JUN LIM TO MIA. CAPTAINS AIR SPEED INDICATION INOPERATIVE. LANDED PTY WITHOUT INCIDENT. REPLACED CAPTAINS PITOT PROBE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080805 EU 2008 8 5 AALA200801689 1 20080623 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80058 466 MIA - EMERGENCY LIGHT AT SEAT 9G DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 9G. SYSTEM GROUND CHECKE D NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080805 EU 2008 8 5 F3LA200800498 1 20080715 A 5321 D5367303801000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 941FR 18 2518 DURING C2 C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 161BF WAS PUNCTURED. MAINTENANCE REPAIRED DAMAGE IAW T HE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F 4 F RT A28NM E37NE 20080806 NM 2008 8 6 TSAA0832021 1 20080615 A 3230 69355006 ACTUATOR BOEING 737 7372X6C 1384552 NM LT MLG LOCK INOPERATIVE A TSAA O OTHER J WARNING INDICATION AP APPROACH 1 WP 13 840AL 23124 FLIGHT 916 LIH-HNL. ON APPROACH CREW SELECTED GEAR DOWN AND NOTED INDICATION FOR LEFT MAIN GEAR NOT LOCKED. CREW PULLE D MANUAL RELEASE HANDLE AND GOT ALL 3 GEARS DOWN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT MAIN GE AR LOCK ACTUATOR IAW AMM 32-32-51 PG 401-403. THE AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A16WE 20080806 EA 2008 8 6 A6WA200840497 1 20080607 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 CROSSBEAM OF PILOTS BULKHEAD OUTBOARD CLIP CRACKED FS 280 LBL 9. CLIP AT CROSS BEAM OF PILOTS BULKHEAD FS 280, LBL 9 RE PLACED IAW CRJ 200 SRM 51-42-06. (A) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 A6WA200840499 1 20080608 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 CROSSBEAM AT PILOTS BULKHEAD CRACKED. CROSS BEAM REPAIRED IAW REO 601R-53-11-171 REV D SCHEME B. (A) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 TRAX200800694 1 20080527 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 PASSENGER DOOR HARD TO OPEN, HANDLE OPERATES OK. DOOR REQUIRES HARD PUSH TO OPEN. OPERATED PASSENGER DOOR. DIDN`T FIN D ANY FAULTS. OPS CHECK GOOD IAW CRF-200 AMM 52-11-00. (S) 2 L 7 2 4F RT A21EA 20080806 EU 2008 8 6 SIMA200819904 1 20080716 A 7400 6071T20P20 CONTROL UNIT SAAB SF340 340B 7860101 EU RIGHT MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 313AE 340B313 ON FLIGHT 3063 CREW REPORTED ON TAKEOFF RT ENG TORQUE GAUGE WENT TO ZERO. IGNITION LIGHT CAME ON IN FLIGHT MOMENTARILY. CREW RETURNED TO LAX WITH NO OTHER PROBLEMS. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED RT DECU IAW GE CT7 MM 7 4-00-00 PERFORMED ENG RUNS IAW GE CT7 MM 72-00-00 OPERATIONAL CHECK GOOD. ACFT RETURNED TO SERVICE. (S) 2 L 7 2 4T RT A52EU 20080806 NM 2008 8 6 KCS2008F00001 1 20080711 A 2612 FIRE WARNING BOEING 747 7472B4B 138481B NM APU BAY ILLUMINATED A KCSA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 23 710CK 21097 APU FAULT NOT LISTED. APU FIRE WARNING INTERMITTENTLY IN FLIGHT. (S) 2 L 7 4 4F RT A20WE 20080806 WP 2008 8 6 AALA200801443 1 20080531 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7547A 53029 LGA - EXTERNAL EMERGENCY LIGHTS AT AFT FUSELADE INOPERATIVE. REPLACED BATTERY PACK FOR EXTERNAL EMERGENCY LIGHTS AT AFT FUSELAGE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080806 EA 2008 8 6 A6WA200840508 1 20080528 A 5321 FLOOR PANEL CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 CRACK FOUND ON FLOOR WEB FS 280 RBL 9. FLOOR WEB AT FS 280 RBL 0 REPAIRED IAW CRJ 200 REO 601R-53-11-171 REV D SCHEME B . (A) 2 L 7 2 4F RT A21EA 20080806 WP 2008 8 6 WXOA070210 1 20080611 A 7160 5930645501 INLET DOUG DC9 DC983 3022083 WP RT NACELLE DENTED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 981GA 49423 FLIGHT CREW REPORTED DURING THE WALKAROUND INSPECTION A LARGE DENT ON THE RIGHT WING SLAT 0 AND THE RIGHT ENGINE INLET N ACELLE. MAINTENANCE DEPARTMENT PERSONNEL REPLACED THE 0 SLAT AND WITH THE ASSISTANCE OF BOEING THE INLET COWL WAS INSPE CTED AT THE END OF EACH DAY WITH NO FURTHER DAMAGE NOTED. THE INLET COWL WAS REPLACED BY MAINTENANCE ON JUNE 13TH IAW A MM 71-10-01 AND THE AIRCRAFT WAS RETURNED TO SERVICE. SLAT ASSY P/N 5930504-2, S/N 535, DENTED, RIGHT WING. (A) 2 L 7 2 4F RT A6WE 20080806 WP 2008 8 6 WXOA070201 1 20080525 A 3350 20131A BATTERY PACK DOUG DC9 DC987 3022087 WP EMERGENCY LIGHTS FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 949MA 49779 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A6WE 20080806 WP 2008 8 6 WXOA070208 1 20080608 A 3240 TRANSDUCER DOUG DC9 DC983 3022083 WP MLG WHEEL LOOSE A WX0A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 19 879GA 53486 FLIGHT CREW REPORTED THE "WHEEL NOT TURNING LIGHT ILLUMINATED ON TAKEOFF." THE AIRCRAFT ABORTED THE TAKEOFF ROLL AND RE TURNED TO THE GATE. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE AIRCRAFT AND DETERMINED THE WHEEL TRANSDUCER PINS LO OSE INSIDE THE WHEEL HUD CAP. THE TRANSDUCER PINS WHERE RE-INSTALLED AND THE SYSTEM OPERATIONAL CHECK WAS NORMAL. AIRC RAFT WAS RETURNED TO SERIVCE. (A) 2 L 7 2 4F RT A6WE 20080806 WP 2008 8 6 WXOA070212 1 20080607 A 3350 20131A BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 869GA 53294 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTME WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A6WE 20080806 SO 2008 8 6 C2XA08RI094 1 20080619 A 3240 39807 CONTROL VALVE EMB 145 EMB145LR 3260212 SO BRAKE SYS DEFECTIVE A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 16541 20701 216 145542 FLIGHT 2295 - EWR - FLIGHT CREW REPORTED "BRK INBD INOP" ON EICAS DURING APPROACH. CREW ABORTED APPROACH, AND PROCEEDED WITH NEW APPROACH AND LANDED ACFT UNEVENTFULLY. EWR MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080806 NM 2008 8 6 KCSA081330 1 20080717 A 5411 FRAME BOEING 747 747246B 1384864 NM NR 2 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 NR 2 PYLON REAR ENG MOUNT BULKHEAD OUTBOARD AFT FRAME WEB CRACKED .500 INCH AT NAC STA 221.9. (S) 2 L 7 4 4F RT A20WE 20080806 WP 2008 8 6 WXOA070200 1 20080521 A 3350 AD4002 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 887GA 49932 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETUR NED TO SERVICE. (A) 2 L 7 2 4F A6WE 20080804 NM 2008 8 4 KCSA081321 1 20080715 A 5414 SKIN BOEING 747 747246F 1384850 NM NR 2 NACELLE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 NR 2 PYLON INBOARD NAC STA-220 SKIN DAMAGED. (A) 2 L 7 4 4F RT A20WE 20080804 WP 2008 8 4 08FDEA02473 1 20080625 A 5313 AEA05411 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 FOUND L52 AT STA 1575 CRACKED. REMOVED DAMAGED L52 AND INSTALLED A NEW LONGERON P/N AEA 0541-1 IAW DAC DWG NEA 6076; R EV AK. 2 L 7 3 4F RT A22WE 20080804 EU 2008 8 4 08FDEA02481 1 20080625 A 5347 A5327923800200 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN DECK FLOOR SEAT TRACK HAS CORROSION; C77 - C78; LBL 32. REMOVED CORROSION IAW A300-600 SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16. REMOVED SEAT TRACK SECTION FROM EXISTING SPLICE AND FRAME 76 10 INCHES TO FRAM E 80/82 IAW FEDEX A300-600 SRM 51-40-21; PARA 7. MATERIAL ID FOR THE FABRICATION OF A NEW SEAT TRACK IS A53274005-T7951 1 IAW A300-600 SRM 53-18-16. FABRICATED AND INSTALLED THE NEW SEAT TRACK IAW A300-600 SRM 53-10-16; PG 208A. PART MARK ED SEAT TRACK IAW FEDEX GMM 7-0-1001. 2 L 7 2 4F RT A35EU 20080804 WP 2008 8 4 08FDEA02816 1 20080710 A 5311 AEA02733 FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 CENTER WING LOWER BARREL INTERNAL FRAME AFT FACE LOWER FLANGE HAS CORROSION JUST BELOW THE BLEED AIR DUCT; FS 1381; STRI NGER 51R TO STRINGER 51L. REMOVED CORROSION. ORIGINAL THICKNESS, 0.080. MATERIAL LOSS IS 0.029. REMAINING THICKNESS 0.051 IAW SRM 53-00-01, VOL I. REMOVED THE FRAME AND INTERCOSTAL IAW DAC DWG AEA 0273, REV G. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II. APPLIED TOP COAT IAW SRM 51-21-01, VOL II. PART MARKED IAW GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20080804 EU 2008 8 4 08FDEA02823 1 20080711 A 5754 A57840120203 PAN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND OLD DOUBLER REPAIR ON RT SLATNR 1 FOLDING NOSE INNER PAN. REPAIR PERFORMED IAW SB A300-57-6067 (REPLACEMENT OF IN NER PAN), APPROVED BY EA 6-5742-120037. 2 L 7 2 4F RT A35EU 20080804 NM 2008 8 4 08FDEA02234 1 20080612 A 5347 ACA7104521 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 598FE 48597 MAIN DECK SEAT TRACK AT STA 525, X = -8 FOUND HOLE ELONGATED. DAMAGED SEAT TRACK AT MAIN DECK STA 525 TO STA 555, X = - 8 REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080804 NM 2008 8 4 KCSA081320 1 20080715 A 5414 SKIN BOEING 747 747246F 1384850 NM NR 2 NACELLE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 705CK 21034 NR 2 PYLON INBOARD SKIRT CHAFED THROUGH RUB STRIP AT NAC STA-220. (A) 2 L 7 4 4F RT A20WE 20080804 EU 2008 8 4 08FDEA02506 1 20080626 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 GOUGED FLOOR SUPPORT FITTING AT THE MAIN CARGO DECK FRAME 41; LBL 77. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02509 1 20080627 A 5730 A5797142930 SKIN AIRBUS 310 A310203 3930313 EU ZONE 600 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 423FE 281 PREVIOUS EXTERNAL BONDED REPAIR DOUBLER LOCATED ON RT WING O/B FLAP TRAILING EDGE LOWER SKIN BETWEEN RIBS 3 AND 4 MEASUR ING 5.7 INCH BY 5.7 INCH REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT EXTERNAL BON DED REPAIR DOUBLER LOCATED ON RT WING O/B FLAP TRAILING EDGE LOWER SKIN BETWEEN RIBS 3 AND 4 IAW SRM 57-53-12 FIG 207 SH EETS 1 AND 2. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 AALA200801379 1 20080524 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 SJU - EMERGENCY LIGHT AT LT SEAT ROWS 19 TO 28 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LT SEAT ROWS 19 TO 28. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080804 SO 2008 8 4 CX2A08ON155 1 20080712 A 7500 2304877 TUBE EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL NR 1 BLEED CRACKED A C2XA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 27 12563 10484 145612 CAE311858 FLT 0119 - ONT - FLIGHT CREW PERFORMED AN AIR RETURN DUE TO POSSIBLE E1 BLEED LEAK. MX PERSONNEL REMOVED AND REPLACED C RACKED 14TH STAGE OFF-TAKE TUBE. OPERATIONALLY AND LEAK CHECKED SATISFACTORY AND AIRCRAFT WAS RELEASED TO RETURN FOR SE RVICE. (A) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080804 NM 2008 8 4 F3LA200800309 1 20080606 A 5315 D5347219320000 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 5 2198 REFERENCE NON ROUTINE 34329. DURING C3 S1 C-CHECK INSPECTION NOTED THE CABIN FLOOR LONGERON BEAM Y765 HAD CORROSION ARO UND FASTNER HOLE AT FRAME 68 AND BARE METAL FROM FRAME 66 TO FRAME 68. MAINTENANCE REMOVED AND REPLACED RT HAND CABIN F LOOR LONGERON BEAM Y765 FROM FRAME 66 TO FRAME 70 IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080804 EA 2008 8 4 A6WA200840501 1 20080603 A 5220 SHAFT CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 CREW ESCAPE HATCH OUTER HANDLE SHAFT IS CORRODED. CREW ESCAPE HATCH OUTER HANDLE SHAFT REPLACED IAW CMM 52-22-03. (A) 2 L 7 2 4F RT A21EA 20080804 EU 2008 8 4 AALA200801554 1 20080606 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 JFK - EMERGENCY EXIT SIGN LIGHT AT LT NR FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LT NR FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080804 WP 2008 8 4 AALA200801439 1 20080530 A 3350 LAMP DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 21 9615W 53562 SFO - EMERGENCY LIGHT AT OVERHEAD SEAT 16B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 16B. SYSTEM GROUND C HECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A6WE 20080804 NM 2008 8 4 AALA200801422 1 20080528 A 3350 LIGHT BOEING 777 777223 1385213 NM GALLEY BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT RIGHT FORWARD GALLEY IS BROKEN. REPLACED LIGHT ASSEMBLY AT RIGHT FORWARD GALLEY. SYSTEM GROUN D CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080804 NM 2008 8 4 2008UALA03682 1 20080702 A 2997 GROUND WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 HYD PUMP CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NR 1 HYD PUMP WIRE IS CHAFED DOWN TO PRIMARY CONDUCTOR. REPLACED GROUND WIRE PER B 767 WDM 29-11-12, SWPM 20-10-11, AND 20-20-12. OPS CHECKED ELECT HYD PUMP PER MM29-11-00, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080804 NM 2008 8 4 2008UALA03688 1 20080702 A 5497 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 NACELLE CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NR 1 ENG PYLON HYD BAY WIRE W390-082-18 IS CHAFED. 2 L 7 2 4F 4 F RT A1NM E24NE 20080804 CE 2008 8 4 DXTA200803174 1 20080714 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE MLG INOPERATIVE E DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 379QS 5600479 POWER BRAKES WILL NOT FUCTION "POWER BRAKE LOW PRESS" AND "ANTI SKID INOP" LIGHTS STAY ON. (A) 2 L 7 2 4F RT A22CE 20080805 SO 2008 8 5 C2XA08RI085 1 20080613 A 3350 3104404 FUSE BRUCE EMB 145 EMB145LR 3260212 SO BATTERY BURNED A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 26545 10440 7331 145558 EWR - DURING ROUTINE MAINTENANCE, EWR MAINTENANCE FOUND EXTERIOR OVERWING EMERGENCY LIGHTS LT AND RT INOPERATIVE. MAINT ENANCE REMOVED AND REPLACED SUB-MINI FUSE AT EMERGENCY BATTERY PACK POSITION 4 AND PERFORMED OPERATIONAL CHECK SUCCESSFU LLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080805 NM 2008 8 5 DHL2008F00028 1 20080703 A 5330 SKIN BOEING 727 7272M7 138407S NM BS 303 S12L GOUGED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 FUSELAGE INNER SKIN BELOW UPPER HINGE IS GOUGED BS 303 STRINGER 12L TO 306.65 LT HAND. FABRICATED REPAIR AND INSTALLED IAW EVA B253-00086 REV 03 DATED 2 JULY 08 AND BOEING REPAIR SKETCH 1-364663355-12 IN CONJUNCTION WITH BOEING TELEX 1-864 663355-B DATED 6-23-08. REFERENCE FORM 8100-9 (DOA-300064-NW) FOR REPAIR APPROVAL AND AMOC`S TO AD 98-11-03 R1 (PARA A) AND AD 2007-12-14 (PARA M) DATED 7-18-08. (A) 2 L 7 3 4F A3WE 20080805 EA 2008 8 5 CHQA200800152 1 20080719 A 2130 CABIN PRESSURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE MALFUNCTIONED A CHQA O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 639BR 7313 GEE872507 FLIGHT 5588, MCI TO IAH. DURING IDLE DESCENT WHILE DESCENDING AT APPROXIMATELY 2,500 FPM, THE CABIN ALTITUDE WAS OBSERV ED TO CLIMB AT 900 FPM ON BOTH CPAM`S. THE FLIGHT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE PERFORMED PRESSURIZATION CHECKS AND COULD NOT DUPLICATE THE FAULT PER CRJ AMM 21-31-00. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080805 EA 2008 8 5 TRAX200800913 1 20080716 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 922EV 7822 BOTTOM ATTACH ANGLE FOR BAGGAGE DOOR LINTEL BEAM MEMBER IS CRACKED IN AREA OF OUTBOARD FASTENER APPROX .50" LONG. REMOV ED CRACKED BOTTOM ATTACH ANGLE FOR BAGGAGE DOOR LINTEL BEAM. LOCATED, DRILLED AND INSTALLED A NEW SERVICEABLE ANGLE IAW CRJ200 SRM 51-40-11 AND 51-42-21. (A) 2 L 7 2 4F RT A21EA 20080805 EA 2008 8 5 TRAX200800916 1 20080716 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 LT WING EMERGENCY MID LIGHT INOP. RELAMPED LT WING EMERGENCY MID LIGHT IAW 33-51-21. (A) 2 L 7 2 4F RT A21EA 20080805 SO 2008 8 5 CHQA200800150 1 20080717 A 2910 AE71379016 HOSE EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL HYD SYSTEM CHAFED A CHQA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 11 287SK 145460 CAR312670 FLIGHT 5923, GSO TO CLE. ON DESCENT INTO CLE, THE FLIGHT CREW RECEIVED AN E1 HYD PUMP FAIL MESSAGE. THE QRH WAS FOLLOW ED AND IT WAS DETERMINED THAT THERE WAS NO QUANTITY INDICATING ON SYSTEM 1. LANDED WITHOUT INCIDENT, TAXIED CLEAR OF RU NWAY AND WAITED FOR TOW BACK TO GATE. MAINTENANCE FOUND THE PRESSURE HOSE COMING FROM THE E1 EDP WAS WORN THROUGH BY AN ADEL CLAMP. THE PRESSURE HOSE ON THE E1 EDP WAS REPLACED AND EDO WAS INSPECTED PER THE AMM, NO LEAKS OR FURTHER DEFECT S WERE NOTED. (A) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080805 NM 2008 8 5 AALA200801657 1 20080618 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 673AN 29423 DFW - EMERGENCY LIGHT AT SEAT 31D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 31D. SYSTEM GROUND CHECK ED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080731 NM 2008 7 31 C8GA20080019 1 20080625 A 7720 10200012 SENSOR BOEING 727 727200 138407E NM ENGINE TEMP INOPERATIVE A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 713AA 22469 FLT 245 FROM EWR TO BDA. DURING TAKEOFF THE NR 2 ENG HAD A HIGH OIL TEMP LIGHT, CREW PERFORMED ENG SHUTDOWN AND THE ACF T RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE NR 2 ENG OIL TEMP BULB WAS AT FAULT. REMOVED AND REPLACED OIL TEMP BULB. PERFORMED OPS AND LEAK CHECKS GOOD. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE. (S) 2 L 7 3 4F RT A3WE 20080731 NM 2008 7 31 HALA0800617 1 20080603 A 5420 CHANNEL BOEING 767 76733A 1385209 NM NR 2 PYLON CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 589HA 33422 THE VERTICAL U-CHANNEL IS CRACKED AT AFT INBOARD EDGE OF NR 2 ENG PYLON, 7: INBOARD OF THE DIAGONAL BRACE AFT MOUNT FIT TING. REMOVED AND REPLACED VERTICAL U-CHANNEL AT AFT INBOARD EDGE OF NR 2 ENG PYLON PER SRM 54-53-70/ 101 AND SRM 51-70 -11-06-0 FIG 1. (S) 2 L 7 2 4F RT A1NM 20080731 SO 2008 7 31 C2XA08RI080 1 20080610 A 2400 M835366022M RELAY EMB 145 EMB145XR 3260214 SO ELECTRICAL SYS INOPERATIVE A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 23139 145731 FLIGHT 2489 - RIC - AFTER TAKEOFF, FLIGHT CREW REPORTED ELECTRICAL EMERGENCY ABNORMAL MESSAGE ON EICAS AND PERFORMED AIR RETURN. RIC MX REMOVED AND REPLACED RELAY K0021 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RE TURN TO SERVICE. (S) 2 L 7 2 4F RT 20080731 EA 2008 7 31 HNAA0800195 1 20080607 A 3231 54C546347 SEQUENCE VALVE DHAV DHC8 DHC8311 1386006 EA NLG INOPERATIVE A HNAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 07 327EN 29274 29274 261 ON CLIMBOUT NOSE GEAR DOOR ADVISORY LIGHT ILLUMINATED ALONG WITH LOUD NOISE FROM NOSE GEAR AREA. LIGHT WENT OUT AND THE N SAME PROBLEM REOCCURRED. GEAR SELECTED DOWN. PERFORMED LANDING GEAR DOOR SEQ CONTROL CIRCUIT OPS CHECK IAW WC 32-32- 15Q. REPLACED NW DOOR SEQ VALVE IAW MM 32-20-36. (S) 2 H 7 2 4T RT A13NM 20080731 SO 2008 7 31 C2XA08IA141 1 20080610 A 2120 UNKNOWN EMB 135 EMB135LR 3260305 SO CABIN ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 29515 145309 IAH - FLIGHT 2386, DURING POST FLIGHT INSPECTION THE FLIGHT ATTENDANT REPORTED A BURNING ODOR IN THE CABIN. MAINTENANCE INSPECTED THE ACFT, NR 2 PACK SYSTEM, AND CABIN LIGHTS, ALL WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080731 SO 2008 7 31 C2XA08ON140 1 20080614 A 3350 LIGHT EMB 145 EMB145XR 3260214 SO CABIN MALFUNCTIONED A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 12163 11900 6363 14500811 FLT 0050 - ONT - FLIGHT CREW REPORTED AN ELECTRICAL ABNORMAL WARNING/EMERGENCY LIGHT NOT ARM MSG WHEN ARMED. MX RESET E MERGENCY LIGHT SYSTEM. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4F RT 20080731 SO 2008 7 31 C2XA08ON131 1 20080531 A 3350 7137216502 SIGN EMB 145 EMB145XR 3260214 SO OVERWING EXIT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11187 14500927 FLT MX - ONT - 1A CHECK - WHILE PERFORMING OPS CHECKS ON EMERGENCY LIGHTING SYSTEM IN CABIN, QC INSPECTOR FOUND FWD CEIL ING PANEL MOUNTED OVERWING EXIT SIGN DOES NOT FULLY ILLUMINATE. MAINTENANCE PERSONNEL REMOVED AND REPLACED FWD CEILING EXIT LOCATING SIGN ASSY. OPERATIONALLY CHECK SATISFACTORY AND ACFT WAS RELEASED TO RETURN TO SERVICE. TSN: 7747 CSN 42 19. (S) 2 L 7 2 4F RT 20080731 SO 2008 7 31 C2XA08CL069 1 20080612 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13956 145078 CLE FLIGHT 3060. THE CREW REPORTED THE FORWARD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND REPAIRED WIR E TO SERVICE DOOR EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4T RT T00011AT 20080731 NM 2008 7 31 SWAA083975 1 20080717 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 SWAA083974 1 20080717 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 SWAA083998 1 20080715 A 5512 65C25727 SKIN BOEING 737 7375H4 138449D NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 124. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843134 1 20080507 A 5311 654655514 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 RIGHT FRAME AT STA 867 CRACKED AT PSU RAIL BRACKET. REPAIRED PER EA 5310 02797. 2 L 7 2 4F RT A16WE 20080729 CE 2008 7 29 DXTA200803137 1 20080622 A 3040 HEATER CESSNA 750 750 2076810 CE WINDSHIELD INOPERATIVE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 979QS 7500079 IN FLIGHT LEFT WINDSHIELD HEAT INOP CAS CAME ON FOLLOWED BY A STRONG ACRID HOT ELECTRICAL SMELL. (B) 2 L 7 2 4J RT T00007WI 20080729 NM 2008 7 29 ASAA0843136 1 20080513 A 5100 NONE BOEING 737 7374Q8 138447Q NM NONE A ASAA O OTHER O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 CARRY OUT PREVENT MOD ON BS 348.2 TO BS 360 STR 16 PER EM 5310 02389 STEP 4. CARRY OUT PREVENT MOD ON BS 348.2 TO BS 36 0 STR 16 PER EM 5310 02389 STEP 4. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843145 1 20080506 A 5320 69353501 TIE CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 TIE CLIP AT STA 787 RBL 15 HAS CORROSION. REPLACED TIE CLIP WITH REPAIR PART. 2 L 7 2 4F RT A16WE 20080729 CE 2008 7 29 DXTA200803117 1 20080613 A 3260 INDICATOR CESSNA 560 560XL 2076702 CE MLG MALFUNCTIONED E DXTA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 07 694QS 5605194 AFTER TAKEOFF UPON GEAR RETRACTION THE NOSE GEAR (GREEN) DOWN LOCK LIGHT REMAINED ILLUMINATED. (B) 2 L 7 2 4F RT A22CE 20080806 EA 2008 8 6 TRAX200800831 1 20080624 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621-625 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 977EV 7720 RT FS 621 - FS 625 UPPER OBLIQUE ANGLE CRACKED .5 INCH IN LENGTH. REMOVED AND REPLACED RT FS 621 - FS 625 OBLIQUE ANGLE IAW CRJ 200 SRM 51-42-06. (S) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 TRAX200800832 1 20080624 A 5230 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 977EV 7720 CARGO DOOR FWD C-CHANNEL CRACKED, APPROX .5" LONG. REMOVED AND REPLACED CARGO DOOR FWD C-CHANNEL IAW CRJ 200 SRM 51-42- 06. (S) 2 L 7 2 4F RT A21EA 20080806 EU 2008 8 6 AALA200801411 1 20080527 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 50051 459 SDQ - EMERGENCY LIGHTS AT LEFT HAND FIRST CLASS INOPERATIVE. REPAIRED LOOSE CONNECTION AFT OF ROW 2 FOR EMERGENCY LIGHT S AT LEFT HAND FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080806 WP 2008 8 6 ABXA080157 1 20080612 A 3260 UPLOCK SWITCH DOUG DC9 DC941 302207N WP LT MLG MALFUNCTIONED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 952AX 47615 STA SWF, CPM GEAR RETRACTION, AFTER TAKEOFF, LEFT "GEAR UNSAFE" LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND NOTED THAT LEFT HEAR DOWN "GREEN LIGHT" ILLUMINATED WITHOUT DELAY. "NO CYCLE TIME" UPON RETRACTION ALL INDICATIONS WERE NORMAL. D EFERRED CLEARED DI 60662. RESHIMMED LT UPLATCH SWITCH IAW DC9 MM 32-60-01-2. PERFORMED LANDING GEAR SWING POSITION AND WARNING CHECK IAW DC9 MM 32-60-00-2. OPS CHECK GOOD. (A) 2 L 7 2 4F A6WE 20080806 EA 2008 8 6 A6WA200840506 1 20080528 A 5312 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA BS 449-529 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 CORROSION FOUND ON PRESSURE FLOOR WEB FS 449 TO FS 529 RBL 45. CORROSION ON PRESSURE FLOOR WEB FS 449 TO FS 529 RBL 45 BLENDED IAW CRJ 200 SRM 51-21-06. (A) 2 L 7 2 4F RT A21EA 20080806 NM 2008 8 6 AALA200801462 1 20080601 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 798AN 30797 DFW - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR GALLEY COMPARTMENT AREA IS DAMAGE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR GALLEY COMPARTMENT AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 EA 2008 8 6 TRAX200800808 1 20080620 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 930EV 8014 FL280.00 FLOORBEAM INBOARD AND OUTBOARD CLIP AT LBL 9 ARE CRACKED. REMOVED AND REPLACED BROKEN CLIPS WITH NEW CLIPS AT LBL 9 FS 280 FLOORBEAM, INBOARD AND OUTBOARD. WORK DONE IAW CRJ200 SRM 51-42-20. (S) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 TRAX200800821 1 20080619 A 5310 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 977EV 7720 TWO INCH CRACK ON TAIL JUST UNDER AND TO THE RIGHT OF THE NAV LIGHT. REPAIRED 2 INCH SCRATCH INTO THE WIRE MESH ON TAIL CONE UNDER THE RT OF NAV LIGHT. NOT A CRACK IAW REO 601R-53-84-001 CRJ SRM 51-74-02. NEED PAINTED. PAINTED REPAIR ARE A IAW SRM 51-74-02. (S) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 TRAX200800820 1 20080621 A 3350 COVER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 842AS 7304 EMERGENCY LIGHT PLASTIC COVER DAMAGED, MISSING FROM EMERGENCY EXIT LIGHT BY MAIN CABIN DOOR. REPLACED EMERGENCY EXIT LI GHT ASSEMBLY PER AMM 33-53-19. (S) 2 L 7 2 4F RT A21EA 20080806 EU 2008 8 6 TRAX200800683 1 20080523 A 2611 SMOKE DETECTOR AEROSP ATR72 ATR72212 8680945 EU E/E BAY FALSE ACTIVATION A ASOA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SO 27 634AS 370 ELECTRICAL SMOKE INDICATION ON CAP WITH CRC ON APPROACH. FLT 4533 & 4434 CX. (EMERGENCY DECLARED). REMOVED AND REPLAC ED AVIONICS SMOKE DETECTOR. (S) 2 H 7 2 4T RT A53EU 20080806 NM 2008 8 6 AALA200801421 1 20080528 A 3350 LIGHT BOEING 777 777223 1385213 NM GALLEY BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT LEFT FORWARD GALLEY IS BROKEN. REPLACED LIGHT ASSEMBLY AT LEFT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 SO 2008 8 6 C2XA08IA142 1 20080619 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145EP 3260221 SO LAVATORY FALSE ACTIVATION A C2XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 14945 14553 145049 BTR - FLIGHT 2010, THE CREW REPORTED A LAV SMOKE DETECTOR INDICATION. THE ACFT DIVERTED TO BETWEEN WHERE IT LANDED WITH OUT INCIDENT. MAINTENANCE INSPECTED THE ACFT, AND REMOVED AND REPLACED THE LAV SMOKE DETECTOR. OPERATIONALLY CHECKED W ITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080806 NM 2008 8 6 2008UALA03700 1 20080702 A 5340 141T4890501 BRACKET BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L2 WINDOW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 CRACK FOUND IN L2 WINDOW TRACK BRACKET. REPLACED L2 WINDOW BRACKET. 2 L 7 2 4F 4 F RT A1NM E24NE 20080806 NM 2008 8 6 AALA200801430 1 20080528 A 3350 HOUSING BOEING 777 777223 1385213 NM EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 776AN 29582 DFW - EMERGENCY LIGHT AT LEFT NR ONE CLOSET DAMAGED. REPLACED HOUSING ASSEMBLY FOR EMERGENCY LIGHT AT LEFT NR ONE CLOSE T. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 SO 2008 8 6 CHQA200800144 1 20080714 A 3350 RPS1B BATTERY EMB 135 EMB135LR 3260305 SO ALLSN AE3007 AE3007A 03030 GL EMERGENCY LIGHTS INOPERATIVE A CHQA O OTHER O OTHER NR NOT REPORTED 1 GL 11 844RP 16314 16314 145620 CAE311813 MAINTENANCE FOUND THE FORWARD, GALLEY, CENTER AND AFT EMERGENCY LIGHTS INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACKS W ERE REPLACED FOR THE FORWARD, GALLEY, CENTER AND AFT EMERGENCY LIGHTS AND ALL FOUR OPERATED NORMALLY. GALLEY BATTERY: P /N: RPS1-B, S/N: 16078, TSN: 3720, TSO: 3720, CENTER BATTERY: P/N: RPS1-B, S/N: 16851, TSN: 17401, TSO: 17401, AFT BATTE RY: P/N: RPS1-B, S/N: 17569, TSN: 7313, TSO: 7313. (S) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080806 NM 2008 8 6 AALA200801737 1 20080630 A 3350 WIRE BOEING 777 777223 1385213 NM EMERGENCY LIGHTS SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 JFK - EMERGENCY LIGHTS AT FORWARD GALLEY INOPERATIVE. REPAIRED SHORTED LIGHT ASSEMBLY FOR EMERGENCY LIGHTS AT FORWARD G ALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20080729 NM 2008 7 29 ASAA0843165 1 20080509 A 5313 6546579619 STRINGER BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 APU COMPARTMENT TORQUE BOX STRINGER CORRODED. REPLACED STRINGER PER SRM 51 40 02. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800691 1 20080708 A 5200 65C3623 SKIN BOEING 737 737524 1384721 NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 DENTS ON AFT CARGO DOOR SKIN FORWARD CORNER (OUT OF LIMITS). INSTALLED FASTENERS AND REPAIR DOUBLER PER B737 SRM 52-00- 01. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA084005 1 20080719 A 5743 115A5211 TRUNNION BOEING 737 737705 13844SC NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 270WN 29089 DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA084006 1 20080719 A 5743 115A5211 TRUNNION BOEING 737 737705 13844SC NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 270WN 29089 DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA084008 1 20080719 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 282WN 32534 EEPLS LENS LOOSE AT ROW 3 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA084007 1 20080717 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 282WN 32534 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080730 EU 2008 7 30 COEA0813911 1 20080529 A 5330 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE MISREPAIRED A COEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 13 911FX 045 FOUND DURING HEAVY CHECK AT COE. PREVIOUSLY INSTALLED REPAIR DOUBLER ON THE EXTERNAL SKIN BETWEEN FRAMES 5 & 6 JUST ABO VE RT AFT NLG DOOR IS INSTALLED WITH CHERRY MAX RIVETS. REMOVED CHERRY MAX RIVETS AND INSTALLED SOLID RIVETS. (S) 2 H 7 2 4T RT A53EU 20080730 2008 7 30 SWAA083981 4 20080715 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 786SW 29811 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800701 1 20080710 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM BS 747 S9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14629 27533 FRAME CRACKED STATION 747 AT S-9L. INSTALLED REPAIR ON FRAME AT STATION 747 S-9L PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA084059 1 20080719 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 510-517D CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 510 AND BS 517D, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 NE 2008 7 30 COEA0802903 2 20080705 A 7261 OIL CAP AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 1 ENGINE UNSECURE A COEA E A ENGINE SHUTDOWN UNSCHED LANDING W K J INADEQUATE Q C FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 13 903FX 179 AIR TURNBACK, & ENG SHUTDOWN: FLT 8813 CPR TO JAC: ON CLIMBOUT FROM CPR AT APPROXIMATELY 500 FT AGL. THE CREW NOTICED FLUCTUATING OIL PRESSURE ON THE NR 1 ENG FOLLOWED BY AN AUDIO MASTER WARNING AND LOW OIL PRESSURE LIGHT. A PRECAUTIONA RY ENG SHUTDOWN OF NR 1 ENG WAS PERFORMED. THE RETURN TO CPR WAS MADE WITHOUT INCIDENT. INSPECTION OF THE NR 1 ENG FOU ND THE ENG OIL CAP PARTIALLY OFF. AN ENG LOW OIL PRESSURE INSPECTION WAS PERFORMED. INSPECTION OF THE OIL CAP FOUND NO DEFECTS. SERVICED ENG OIL SYSTEM & REINSTALLED OIL CAP. (S) 2 H 7 2 4T 4 T RT A53EU E20NE 20080730 NM 2008 7 30 CALA0800662 1 20080703 A 5714 111A72024 STRUCTURE BOEING 737 737724 13844BY NM CENTER WING WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 15712 28783 WING CENTER SECTION RIGHT-HAND LOWER CHORD AT STATION 530 40RBL HAS A HOLE. REPAIR COMPLETED PER ECRA 5351-01064 ON WIN G TO BODY FAIRING SUPPORT RBL 40.1 LOWER CHORD REPAIR. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800698 1 20080710 A 3234 NA HANDLE BOEING 737 737724 13844BY NM MLG OUT OF RIG A CALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 16732 28948 ON TAKEOFF, GEAR RETRACTION NOSE GEAR INDICATION SHOW RED AND GREEN. NOSE GEAR DID NOT RETRACT WITH GEAR HANDLE UP. (WI TH WIND NOISE). GEAR EXTENDED NORMALLY. REF N/R 4262634 FOUND GEAR HANDLE OUT OF RIG. CHECKED PRESSURE AND "X" DIMENS IONON N/L/G, LUBED GEAR AND PERFORMED GEAR SWING. ALL OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800699 1 20080710 A 5610 PA140N21391S WINDOW BOEING 737 737824 13844BZ NM COCKPIT CRACKED A CALA O OTHER O OTHER CR CRUISE 1 SW 27 12225 28934 PASSENGER WINDOW 2F CRACKED. REMOVED AND REPLACED NUMBER 2F WINDOW AS PER MM 56-21-11-400-801. CHECKS GOOD. M&E 29-56 21-3-0011. 2 L 7 2 4F RT A16WE 20080730 2008 7 30 SWAA083922 4 20080715 A 2565 6949956 CABLE BOEING 737 7375H4 138449D NM L2 DOOR SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED BRDG CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE FRAYED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083872 1 20080711 A 5520 REP4HE8 BEARING BOEING 737 7373G7 1384595 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT HORN BEARING PER MM. 2 L 7 2 4F RT A16WE 20080806 NM 2008 8 6 AALA200801739 1 20080630 A 3350 FUSE BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 768AA 33540 JFK - EMERGENCY LIGHTS AT SEAT ROWS 30AJ TO 37AJ INOPERATIVE. REPLACED FUSE IN BATTERY PACK FOR EMERGENCY LIGHTS AT SEA T ROWS 30AJ TO 37AJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20080806 SO 2008 8 6 CHQA200800145 1 20080714 A 3244 302K631 TIRE EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL RT MLG FAILED A CHQA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 11 569RP 228 228 14500816 CAE312567 FLIGHT 6413, CVG TO STL. DURING THE TAKEOFF ROLL BETWEEN 80KTS AND V1 SPEED, THE FLIGHT CREW NOTICED A VIBRATION AND SL IGHT POPPING SOUND. THE THRUST LEVERS WERE IMMEDIATELY PULLED BACK AND WERE PUT INTO REVERSE WHILE BRAKING AND STOPPING THE ACFT. THE ACFT THEN TAXIED CLEAR OF THE RUNWAY WITHOUT INCIDENT. MAINTENANCE PERFORMED THE LG TIRE TREAD INSPECTI ON, FOUND SCUFF MARKS ON RT I/B FLAP, GEAR DOORS, FUSELAGE, AND E2 INLET AND SPINNER. BOTH RT MLG TIRES HAD BLOWN ON TA KEOFF. THE BRAKE LINES ON THE RT GEAR WERE FOUND TO BE LEAKING HYDRAULIC FLUID. THE BORESCOPE INSPECTION OF E2 FOUND N O DEFECTS. BOTH RT MAIN TIRES WERE REPLACED ALONG WITH 2 E2 FAN BLADES, ALL E2 BYPASS VANES, RT BRAKES, RT GEAR DOOR, R 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080806 WP 2008 8 6 AALA200801442 1 20080530 A 2120 SR093600219 DUCT DOUG DC9 DC982 3022082 WP A/C PACK LEAKING A AALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 21 954U 49426 ORD INFLIGHT T564/30MAY. AT FLIGHT LEVEL 310 PRESSURIZATION FLOW LIGHT ILLUMINATED AND THE CABIN ALTITUDE WAS CLIMBING AT 300 TO 500 FEET PER MINUTE. DECLARED AN EMERGENCY AND BEGAN A DESCENT. DURING DESCENT CREW TURNED ON ANTI ICE TO TH E TAIL AND THE PRESSURIZATION RETURNED TO NORMAL. LANDED ORD WITHOUT INCIDENT. REPLACED BLOWN DUCT IN RIGHT AIR CONDIT IONING PACK SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080806 NM 2008 8 6 AALA200801429 1 20080528 A 3350 SIGN BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 670AA 25335 DFW - EMERGENCY LIGHT PLACARD FOR FORWARD EXIT AT SEAT ROW 18ABC DAMAGED. REPLACED PLACARD FOR EMERGENCY LIGHT FORWARD EXIT AT SEAT 18ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080806 NM 2008 8 6 AALA200801736 1 20080630 A 3350 BPS73 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 332AA 22331 JFK - EMERGENCY EXIT SIGN LIGHTS AT LT AND RT OVERWING EXITS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN LIGHTS AT LT AND RT OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A1NM 20080806 EA 2008 8 6 TRAX200800908 1 20080713 A 5300 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA BS 559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 CORROSION FOUND AT FS 559 RBL 44. REMOVED CORROSION AT FS 559 RBL 44 IAW SRM 51-21-06. MATERIAL LOSS .002 FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 51-21-06. RESTORED FINISH IAW SRM 51-25-00. (S) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 TRAX200800910 1 20080714 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 980EV 7759 EMERGENCY EXIT LIGHT ASSY AT CABIN ENTRY BULKHEAD BROKEN AND HANGING BY WIRES. CHANGED EMERGENCY PATH LIGHT ASSY AT THE ENTRY BULKHEAD IAW CRJ 200 AMM 33-51-01. LIGHT OPS CHECK GOOD. (S) 2 L 7 2 4F RT A21EA 20080806 SO 2008 8 6 CHQA200800143 1 20080714 A 2131 2225ON030301 CONTROLLER EMB 135 EMB135LR 3260305 SO ALLSN AE3007 AE3007A 03030 GL CABIN PRESSURE INOPERATIVE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 836RP 11037 11037 145713 CAE312376 FLIGHT 6384, CVG TO TRI. DURING CLIMB AT 3,000 FT, THE CREW NOTICED THAT THE CABIN ALTITUDE WAS CLIMBING RAPIDLY. THE FLIGHT LEVELED OFF AT 8,000 FT AND PREPARED TO RETURN TO CVG. THE FLIGHT RETURNED TO CVG AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED THE AUTO PRESSURIZATION MODE AND RELEASED THE ACFT. THE DEFERRAL WAS CLEARED ON 07/14/2008 WHEN TH E DIGITAL PRESSURE CONTROLLER WAS REPLACED. (S) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080806 NM 2008 8 6 AALA200801428 1 20080528 A 3350 0201804001 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 670AA 25335 DFW - EMERGENCY LIGHT AT SEAT 9D MISSING CLEAR LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECK ED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080806 NE 2008 8 6 ABXA080193 2 20080212 A 7310 21N04269 SWITCH BOEING 767 767232 1385132 NM GE CF6 CF680A 30025 NE FILTER INDICATOR DEFECTIVE A ABXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 750AX 1637 22227 RT ENG FUEL FILTER DISPLAYED. REMOVED AND REPLACED RT ENG FUEL FILTER IAW B767 MM 73-11-02/201. REMOVED AND REPLACED R T ENG FUEL FILTER INDICATOR SWITCH IAW MM 73-24-01-4. OPS CHECK AND ENG IDLE RUN IAW 71-00-00-5. LEAK CHECK GOOD. (S) 2 L 7 2 4F 4 F RT A1NM E13NE 20080806 NM 2008 8 6 AALA200801455 1 20080601 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 DFW - EMERGENCY LIGHT AT SEAT 38G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 38G. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 NM 2008 8 6 AALA200801386 1 20080524 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 640A 24598 DFW - EMERGENCY LIGHTS AT SEAT ROWS 9 TO 15 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 9 TO 1 5. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080806 NM 2008 8 6 AALA200801399 1 20080526 A 3350 HOUSING BOEING 777 777223 1385213 NM EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT AT LT NR ONE DOOR DAMAGED. REPLACED LIGHT HOUSING FOR EMERGENCY LIGHT AT LT NR ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 WP 2008 8 6 AALA200801444 1 20080531 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7547A 53029 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 23 TO 29 INOPERATIVE. CLEANED CORROSION ON BATTERY PACK FOR EMERGENCY LIGH TS AT OVERHEAD SEAT ROWS 23 TO 29. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080806 WP 2008 8 6 AALA200801450 1 20080601 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 227AA 49177 LGA - EMERGENCY LIGHT AT SEAT 3D INOPERATIVE. REPLACED LAMP ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 3D. SYSTEM GROUND CHE CKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080730 NM 2008 7 30 2008UALA03588 1 20080625 A 5753 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT WING TE FLAP GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 LT WING INBOARD FLAP UPPER SURFACE OUTBOARD EDGE GOUGED. PREVIOUS REPAIR DAMAGED. REMOVED PREVIOUS REPAIR AND INSTALLE D BONDED REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080730 NM 2008 7 30 2008UALA03591 1 20080622 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW READS LOW A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 810UA 843 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. *S/D* SERVICED CREW O2 TO FULL, NO LEAKS NOTED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080730 NM 2008 7 30 SWAA083701 1 20080704 A 5311 6546570 FRAME BOEING 737 7373H4 1384600 NM BS 947 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947, STR 11L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083967 1 20080716 A 5311 6978188 FRAME BOEING 737 7373H4 1384600 NM BS 787 S13R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 13R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080731 EA 2008 7 31 COMA0860314 1 20080701 A 5346 BEAM CNDAIR CL600 CL6002B19 1900309 EA FS 640 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 442CA 18474 7483 CRACK ON ENG BOX BEAM ON TOP WEB SKIN AT FS 640 BETWEEN BL0.00 AND RBL 9.00. REPAIRED BOX BEAM IAW REO 601R-53-61-345. (S) 2 L 7 2 4F RT A21EA 20080731 NE 2008 7 31 CHQA200800112 2 20080614 A 7261 7225363 PROBE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 2 OIL LEVEL FALSE INDICATION A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 642BR 18175 18175 7356 GEE873284 FLIGHT 5503, SDF TO IAH. DURING CLIMB THROUGH 24,000 FT, THE FLIGHT CREW NOTICED THE NR 2 ENG OIL TEMP CLIMB INTO THE A MBER RANGE. THE FLIGHT LEVELED OFF TO ALLOW A REDUCTION IN POWER FOR THE ENGINE. IT WAS NOTICED THAT THE ASSOCIATE HYD RAULIC AND FUEL TEMPERATURES CONFIRMED THE HIGH TEMP CONDITION. THE FLIGHT RETURNED TO SDF AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE ENG OIL LEVEL WAS LOW AND THE OIL LEVEL PROBE WAS MALFUNCTIONING. AFTER REPLACING THE PROBE AND SERVICING THE OIL, THE ENGINE OPERATED NORMALLY. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080731 EA 2008 7 31 COMA0860291 1 20080616 A 5340 6013501251 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 625 S15L CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 7117 DURING HMV-6, INSPECTION FOUND FRAME 625 TO STRINGER 15L ATTACH CLIP CRACKED. REMOVED AND REPLACED CLIP IN ACCORDANCE W ITH SRM 51-42-20. (S) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 COMA0860287 1 20080613 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR LEAKING A COMA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 01 713CA 33668 7245 LANDING GEAR WOULD NOT EXTEND. FLUID LEVEL OF HYD SYSTEM 3 WAS 5%. DECLARED EMERGENCY, PERFORMED EMERGENCY EXTENSION, LANDED WITHOUT INCIDENT. REPLACED MLG PRIORITY VALVE, WHICH WAS LEAKING AT EXPANSION FITTING. SERVICED SYSTEM 3. NO F URTHER DEFECTS. (S) 2 L 7 2 4F RT A21EA 20080731 EU 2008 7 31 COEA0803911 1 20080605 A 5320 WASB12 FLOOR SUPPORT AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 911FX 045 FOUND DURING HEAVY CHECK AT COE. MAJOR REPAIR: RT LONGITUDINAL FLOOR SUPPORT AT FRAME 36R IS CRACKED ABOVE STRINGER 18 R. REPAIRED PER EMPIRE AIRLINES EO 5315-01 REV B. REMOVED & REPLACED RT LONGITUDINAL FLOOR BEAM FROM FRAME 36R TO 40R. (S) 2 H 7 2 4T RT A53EU 20080731 EA 2008 7 31 COMA0860286 1 20080613 A 2750 860D10018ABCD CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 927CA 2058 7031 RECEIVED FLAP FAIL MESSAGE AT CRUISE. DECLARED EMERGENCY, LANDED HSV WITHOUT INCIDENT. REPLACED FECU. NO FURTHER DEFE CTS. (S) 2 L 7 2 4F RT A21EA 20080731 SO 2008 7 31 C2XA08CL068 1 20080607 A 2613 81662410 THERMOSTAT EMB 145 EMB145XR 3260214 SO NR1 ENGINE FAULTY A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 17146 15293 15293 145746 EWR FLIGHT 2373. THE CREW REPORTED A BLEED 1/2 OVERTEMP MESSAGE IN ICING CONDITIONS. THE ACFT DIVERTED INTO CLE WITHOU T INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 BLEED THERMOSTAT. OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4F RT 20080731 NM 2008 7 31 SWAA083980 1 20080717 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED MV2 CHECK, MID CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080731 2008 7 31 C2XA08CL070 4 20080612 A 2300 7510700806 RADIO EMB 145 EMB145XR 3260214 SO COMM 1 INOPERATIVE A C2XA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 27 17138 23045 23045 145727 IAH FLIGHT 2187. THE CREW REPORTED, WERE UNABLE TO TRANSMIT ON COMM 1. THE ACFT DIVERTED INTO CLE AND LANDED WITHOUT I NCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 COMM UNIT. OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4F RT 20080731 EA 2008 7 31 TRAX200800708 1 20080530 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 424 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 CORROSION DAMAGE ON LT PRESSURE FLOOR SILL FS 424.00 AT LBL 36.0 TO LBL 45.0 (MARKED). JOB COMPLETE REMOVED MINOR SURF ACE CORROSION DAMAGE ON PRESSURE FLOOR SILL ASSEMBLY REINFORCING ANGLE AT FS 424.00 AT LBL 36. BLENDED AREA DIMENSIONS ARE 1"X.5"X.002"MAX DEPTH, 1.5"X1.5"X.006", 5"X.5"X.002". MAXIMUM MATERIAL REMOVAL ALLOWED IS .008". BLENDED AREA IS W ITHIN LIMITS PER CRJ 200 SRM. (B) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 TRAX200800710 1 20080530 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 FLOOR SUPPORT STRINGER CORRODED AT PAX DOOR SILL (MARKED). JOB COMPLETE REMOVED CORROSION PER CRJ 200 SRM 51-21-06. M ATERIAL REMOVED .004", WITHIN LIMITS. REMOVED UPPER FLOORBOARD ATTACH ANGLE AND AFT PAX DOOR ARM FITTING FOM. (B) 2 L 7 2 4F RT A21EA 20080806 NM 2008 8 6 AALA200801391 1 20080525 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 760AN 31477 DFW - EMERGENCY LIGHT AT SEAT ROW 21G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 21G. SYSTEM GROUND C HECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 NM 2008 8 6 AALA200801410 1 20080526 A 2780 SENSOR BOEING 767 767323 1385205 NM LT WING SLAT INOPERATIVE A AALA O OTHER O OTHER AP APPROACH 1 SW 21 397AN 29604 JFK INFLIGHT T160/26MAY. SLAT ASYMMETRY MESSAGE ON APPROACH. LANDED JFK WITHOUT INCIDENT. REPLACED NR FOUR SLAT SENSO R. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080806 NM 2008 8 6 AALA200801361 1 20080521 A 3350 1317 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 661AA 25295 DFW - EMERGENCY LIGHT AT FORWARD OVERHEAD SEAT ROW 17ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FORWARD OVER HEAD SEAT ROW 17ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080806 EU 2008 8 6 AALA200801408 1 20080526 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 JFK - EMERGENCY LIGHT AT OVERHEAD AISLE RT NR TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD AISLE RT NR TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080806 NM 2008 8 6 AALA200801409 1 20080526 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 JFK - EMERGENCY LIGHT AT SEAT 20H MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20H. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 NM 2008 8 6 DHLA200800080 1 20080717 A 7711 TRANSMITTER BOEING 727 727200 138407E NM PWA JT8 JT8D17R 52049 NE NR 3 ENGINE MALFUNCTIONED A DHLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 01 741DH 21931 FLT 577, DURING ENG ACCELERATION NR 3 EPR FLUCTUATES RAPIDLY. ALL OTHER ENG PARAMETERS NORMAL. BRAKE ENERGY NORMAL. D EFERRED PER MEL 77-1-1, DMI CONTROL 3319. MAINTENANCE CONTROLLER RPR AT 0942(Z). AIRCRAFT GROUNDED. REMOVED AND REPLA CED NR 3 ENG EPR TRANSMITTER IAW AMM 77-11-11. OPS CHECK NORMAL ON ENG RUN. THIS CLEARS DMI NR33119. (S) 2 L 7 3 4F 4 F RT A3WE E2EA 20080806 WP 2008 8 6 ARWA20080701 1 20080717 A 2720 B-NUT DOUG DC10 DC1010 3022110 WP HYDRAULIC LINE LOOSE A ARWA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 29 68041 46900 NR 1 HYDRAULIC SYSTEM LOSS PRESSURE AND QUANTITY ZERO. RUDDER STAND-BY POWER OFF, IGHT ON. REPAIRED LINE AND FOUND LOO SE B-NUT AT LT HORIZONTAL STABILIZER TRIM MOTOR. TIGHTENED B-NUT IAW DEIO M/M 20-10-0. PERFORMED OPERATIONAL CHECK, FO UND NORMAL IAW DEIO M/M 27-43-01. (S) 2 L 7 3 4F A22WE 20080806 NE 2008 8 6 I5HA0824006 2 20080716 A 8500 R2800 ENGINE CVAC 240 T29B 2422644 WP PWA R2800 R2800* 52026 NE LEFT DAMAGED A I5HA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 25 150PA 137 278 P27759 JUST AFTER TAKEOFF AT APPROXIMATELY 1700 (L) CREW OBSERVED A HIGH OIL TEMPERATURE INDICATION ON THE LT ENG. THE CAPTAIN REDUCED POWER AND THE OIL TEMPERATURE CAME DOWN BUT THE OIL PRESSURE ALSO CAME DOWN TO AN ABNORMALLY LOW PRESSURE. THE CREW DECLARED AN EMERGENCY AND RETURNED TO STT. AFTER LANDING UNEVENTFULLY, THE CREW SHUT DOWN THE LT ENG AND TAXIED T O THE PARKING AREA. THE CREW ATTEMPTED TO PULL THE PROPELLER THROUGH BUT WAS ONLY ABLE TO MOVE IT A SHORT DISTANCE. TH ERE WAS A GRINDING NOISE HEARD IN THE NOSE CASE. SUBSEQUENT INSPECTION BY A MECHANIC REVEALED SIGNIFICANT AMOUNTS OF ME TAL IN THE OIL SCREEN. THE LT ENG WILL BE REMOVED AND REPLACED. OPEN. (S) 2 L 7 2 4R 4 R 6A6 5E8 20080804 NM 2008 8 4 2008UALA03647 1 20080628 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 516UA 24860 EEL LIGHT STRIP AT MID LAV INOP WHEN EMERGENCY LIGHTS SELECTED TO ON POSITION. *S/D* CONNECTOR DISCONNECTED AT EEL STR IP. SECURED CONNECTOR, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080805 CE 2008 8 5 DXTA200803164 1 20080708 A 3220 LANDING GEAR CESSNA 680 680CE 2076811 CE NOSE MALFUNCTIONED E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 385QS 6800115 ON GEAR RETRACTION, NOSE GEAR MADE A NOTICEABLE CLUNK AND BANG AND THE RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. (A) 2 L 7 2 4F RC T00012WI 20080805 NE 2008 8 5 C8G2008F00003 2 20080611 A 7261 439563 FITTING BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE BYPASS SWITCH LOOSE A C8GA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 29 708AA 22465 DURING CLIMB OPERATION, THE NR 2 ENGINE LOW OIL PSI LIGHT ILLUMINATED AND OIL QUANTITY WENT TO EMPTY. THE NR 2 ENG WAS SHUTDOWN, AN EMERGENCY WAS DECLARED AND THE AC LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED THAT THE NR 2 ENGINE OIL FILTER BYPASS SWITCH GEARBOX FITTING WAS AT FAULT. REPAIRED GEARBOX INSERT, OPS AND LEAK CHECKS GOOD. NO OTHER DEF ECTS WERE NOTED. AC WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F 4 F A3WE E2EA 20080805 CE 2008 8 5 GLB2008F00007 1 20080618 A 3230 LANDING GEAR BEECH 1900 1900D 1154162 CE MALFUNCTIONED A GLBA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NM 21 211GL UE211 PILOTS REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT PROPERLY AND AIR RETURNED TO DEPARTURE. MAINT PERFORMED NUMEROU S GEAR RETRACTIONS AND EXTENSIONS IAW MM 32.00. NO DEFECTS WERE NOTED. (K) 2 L 7 2 4T RT A24CE 20080805 NM 2008 8 5 YEN2008F00010 1 20080621 A 3350 340022 POWER SUPPLY EMB ERJ190 ERJ190100IGW 3260408 NM EMERGENCY LIGHTS DISCHARGED A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 187JB 7184 19000009 ON ROUTINE MAINTENANCE, AFT GALLEY OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED AFT GALLEY EMERGENCY LIGHT POWER UNIT IAW MM 33-50-01, OPS CHECK GOOD. (K) 2 L 7 2 4F RT A57NM 20080805 EA 2008 8 5 MAL2008F00010 1 20080713 A 2150 A/C PACK CNDAIR CL600 CL6002D24 1390016 EA SMOKE A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 925XJ 15183 SMOKE WAS SMELLED AND SEEN COMING FROM RT PRESSURIZATION PACK FROM ABOUT THE LAST FIVES ROW OF THE CABIN. COULD NOT DUP LICATE PROBLEM. CHECKED AFT EQUIPMENT BAY FOR LEAKS, NO LEAKS NOTED. (K) 2 L 7 2 4F RT A21EA 20080805 EU 2008 8 5 M7K2008F00067 1 20080108 A 3150 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE WARNING LIGHT FAILED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 806MH 89 3833 23230 PILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWE VER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED M UCH LONGER THAN TYPICAL THIS IS A RECURRING PROBLEM FOR THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY OF THIS MOD E AC. THIS PART CAN ON OCCASION ALSO CAUSE ENGINE FLUCTUATIONS IN FLIGHT WHEN THE RESISTANCE VALUE SIGNAL IS DISRUPTED FOR A LITTLE AS 1/20TH OF A SECOND, WHICH IS THE SAMPLE RATE FOR THE ENGINE CONTROL SYS. AN ADDITIONAL FACTOR FOR THESE TYPE OF FAULTS IS NO RESET FUNCTION AVAILABLE TO THE PILOT TO DIFFERENTIATE BETWEEN A MOMENTARY OR AN ACTIVE FAULT. ON 1 G 7 2 3U 3 U H9EU E00054EN 20080805 NM 2008 8 5 DHL2008F00029 1 20080708 A 5330 SKIN BOEING 727 7272M7 138407S NM BS 303 CRACKED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 L1 DOOR FRAME 303 9 CRACK ON INBOARD FASTENER HOLE INSIDE UPPER HINGE CUTOUT. REPAIRED L-1 DOOR FRAME BS 303.95 UPPER H INGE CUTOUT IAW EVA B253-00089 REV IR DATED 2 JULY 08 AND BOEING TELEX 1-864663355-15 WITH REPAIR SKETCH 1-864663355-12, FABRICATED CLIP ANGLE P/N 50-7946U79 IAW EC-01023-001 DATED 7/8/08 WITH DRAWING 50-7946 REV H DATED 3-13-93, REFERENCE FORM 8100-9 (DOA-300064-NM) FOR REPAIR APPROVAL AND DTA REQUIREMENTS NLT 7-10-09. DATED 7/18/08 EC-01026 GENERATED FOR D TA TRACKING. (A) 2 L 7 3 4F A3WE 20080805 SO 2008 8 5 C2XA08IA154 1 20080704 A 3297 D3899926KA98SN CONNECTOR EMB 145 EMB145LR 3260212 SO NLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16561 145610 IAH - FLIGHT 555, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDE D WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE CONNECTOR P2834, OPERATIONALLY TES TED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080805 EA 2008 8 5 A6WA200840542 1 20080713 A 3230 16520101 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA NLG INOPERATIVE A A6WA O OTHER J WARNING INDICATION CL CLIMB 1 GL 31 401AW 23130 7280 AFTER TAKEOFF RECEIVED GEAR DISAGREE MESSAGE, CYCLED GEAR PER QRH AND NOSE GEAR RETRACTED. REMOVED AND REPLACED (NLG) R ETRACTION ACTUATOR, OPS CHECK GOOD IAW CRJ AMM 32-53-01. (A) 2 L 7 2 4F RT A21EA 20080805 EA 2008 8 5 N6WA0080702 1 20080716 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA SPOILERS ILLUMINATED A N6WA O OTHER J WARNING INDICATION AP APPROACH 1 CE 03 162GJ 10254 FLIGHT 6323 - PWM. APPROACHING PWM STOWED SPOILERS OF SPOILERON AND OUTBOARD FLIGHT SPOILERS MESSAGE. PERFORMED SUPPLE MENTAL GUIDANCE PROCEDURES 10-27-61-6. CLEARED MESSAGES IAW FLT CREW OPERATING MANUAL CFS-013-01. (A) 2 L 7 2 4F RT A21EA 20080805 EA 2008 8 5 A6WA200840432 1 20080520 A 5420 PLATE CNDAIR CL600 CL6002B19 1900309 EA RT PYLON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 406AW 7402 RT PYLON TRAILING EDGE, INBOARD UPPER BONDING PLATE CORRODED. CORROSION REMOVED IAW CRJ 200 SRM 51-21-06 AND WITHIN LI MITS IAW SRM 54-00-00. (A) 2 L 7 2 4F RT A21EA 20080805 EA 2008 8 5 A6WA200840489 1 20080606 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 202 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 FWD PRESSURE BULKHEAD AT FS 202, LBL 23.71, WL 69.00 IS CRACKED. FWD PRESSURE BULKHEAD AT FS 202.00, LBL 23.71 WL 69.00 REPAIRED IAW REO 601R-53-11-563. (A) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 A6WA200840480 1 20080604 A 2760 855D10011 SENSOR CNDAIR CL600 CL6002B19 1900309 EA BRAKE POSITION MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 31 437AW 12778 7744 FLAP FAIL MESSAGE WHEN FLAPS SET TO 8 DEGREES ON APPROACH TO LGA. DIVERTED TO PHL, ZERO FLAP LANDING. REMOVED AND REPL ACED RT BPSU LAW AMM 27-51-10. OPS CHECK AND RIG CHECK OF BPSU AND FLAPS ARE GOOD AT THIS TIME. (A) 2 L 7 2 4F RT A21EA 20080806 SO 2008 8 6 C2XA08ON142 1 20080617 A 2611 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO LAVATORY DIRTY A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 11192 7800 4206 14500936 FLT 0210 - SMF - FLIGHT CREW REPORTED LAV SMOKE DETECTOR ACTIVATED ON CLIMB. MAINTENANCE REMOVED, CLEANED, REINSTALLED LAV SMOKE DETECTOR SENSOR ASSY. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4F RT 20080806 NM 2008 8 6 KCSA081329 1 20080717 A 5411 FRAME BOEING 747 747246B 1384864 NM NR 3 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 NR 3 PYLON REAR ENG MOUNT BULKHEAD OUTBOARD FWD FRAME WEB CRACKED .500 INCH AT NAC STA 221.9. (S) 2 L 7 4 4F RT A20WE 20080806 WP 2008 8 6 WXOA070202 1 20080525 A 3350 6011779 BATTERY PACK DOUG DC9 DC987 3022087 WP EMERGENCY LIGHTS FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 949MA 49779 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. ( A) 2 L 7 2 4F RT A6WE 20080806 WP 2008 8 6 WXOA070203 1 20080525 A 3350 AD4002 BATTERY DOUG DC9 DC987 3022087 WP EMERGENCY LIGHTS FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 949MA 49779 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETUR NED TO SERVICE. (A) 2 L 7 2 4F RT A6WE 20080806 2008 8 6 2008UALA03681 4 20080702 A 2565 81020401 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 SLIDE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 2L SLIDE LIGHT DID NOT ILLUM. SENSOR SWITCH S10219 FAULTY. REPLACED SENSOR SWITCH 10219, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080806 NM 2008 8 6 2008UALA03699 1 20080702 A 5340 141T489019 BRACKET BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L2 WINDOW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 663UA 27160 WINDOW L2 LOWER TRACK BRACKET CASTING CRACKED AT FWD OUTBOARD EDGE. REPLACED 2L WINDOW BRACKET. 2 L 7 2 4F 4 F RT A1NM E24NE 20080806 NE 2008 8 6 AALA200801433 2 20080529 A 7230 BLADES DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE COMPRESSOR BIRD INGESTION A AALA A UNSCHED LANDING C E F.O.D. VIBRATION/BUFFET CL CLIMB 1 SW 21 432AA 49350 725576 DFW INFLIGHT T2020/29MAY. FLIGHT ATTENDANTS REPORTED ENGINE VIBRATIONS IN AFT CABIN. RETURNED TO DFW AND LANDED WITHOU T INCIDENT. VISUAL INSPECTION REVEALED BIRD INGESTION TO NR ONE ENGINE. REPLACED THREE PAIR FAN BLADES. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F 4 F A6WE E9NE 20080806 NE 2008 8 6 AALA200801417 2 20080528 A 7200 UL16672 TUBE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4B3 NE P1 SENSE BROKEN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 630AA 24588 31060 MCO INFLIGHT T1247/28MAY MIA TO ORD. NR TWO ENGINE ENGINE PRESSURE RATIO REMAINED AT CLIMB. ALL OTHER INDICATIONS DROP PED LOWER AS ALTITUDE INCREASED. LANDED MCO WITHOUT INCIDENT. REPLACED NR TWO ENGINE BROKEN P1 SENSE LINE AT FUEL FLOW GOVERNOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F 4 F RT A2NM E12EU 20080731 SW 2008 7 31 WGEA200800060 1 20080606 A 2621 FX002002 FIRE BOTTLE ECLIPS EA500 ECLIPSEEA500 3350000 SW NR 1 LEAKING A WGEA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 27 162DJ 150 000079 NR 1 ENG PHOSTREX BOTTLE LEAKING. CLEANED ENG AND AIRFRAME OF ALL PHOSTREX AFTER REMOVING FIRE BOTTLE. INSTALLED SERVI CEABLE FIRE BOTTLE REMOVED FROM ACFT N156DJ. (S) 1 L 7 2 4J RT A00002AC 20080731 NE 2008 7 31 C8GA20080017 2 20080604 A 7320 78360018073 EEC BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE ENGINE MALFUNCTIONED A C8GA O OTHER J WARNING INDICATION CL CLIMB 1 SO 29 620DL 22910 FLT P0002 FROM PTY TO MFA. DURING CLIMB OPERATION OIL PSI WENT TO -4, N1=0, N2=0 ENG SHUTDOWN. ACFT RETURNED TO PTY WH ERE IT LANDED WITHOUT INCIDENT. TROUBLESHOT SYSTEM AND FOUND EEC TO BE AT FAULT. REMOVED AND REPLACED EEC, OPS CHECKS GOOD. NO FURTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE. (S) 2 L 7 2 4F 4 F RT A2NM E17NE 20080731 SO 2008 7 31 C2XA08RI081 1 20080602 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 13970 145146 FLIGHT 2251 - IND - FLIGHT CREW REPORTED ELECTRICAL SMELL IN COCKPIT. SYSTEM RESET WAS PERFORMED AND NO DEFECTS WAS NOT ED. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080731 EA 2008 7 31 COMA0860284 1 20080610 A 3230 46193 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAULTY A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 713CA 24284 7245 RECEIVED NOSE GEAR DISAGREE MESSAGE ON APPROACH. FOLLOWED QRH, DECLARED EMERGENCY. LANDING GEAR LOWERED ON RECYCLE. L ANDED WITHOUT INCIDENT. REPLACED MGL PRIORITY VALVE. NO FURTHER DEFECTS. (S) 2 L 7 2 4F RT A21EA 20080731 SO 2008 7 31 CHQA200800115 1 20080615 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007A 03030 GL EMERGENCY LIGHTS DEFECTIVE A CHQA O OTHER O OTHER NR NOT REPORTED 1 GL 11 264SK 145221 CAE311337 THE LT EXTERNAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE DURING OVERNIGHT MAINTENANCE. MAINTENANCE FOUND THE NR 2, 5, AND 6 INVERTERS INOPERATIVE. AFTER REPLACING THE DEFECTIVE INVERTERS, THE EMERGENCY LIGHTS FUNCTIONED NORMALLY. (S ) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080731 NM 2008 7 31 2008UALA03618 1 20080628 A 5313 STRINGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 785.9 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 FWD PIT BS 785.9, S-39R STRINGER END FITTING IS CORRODED. REPLACED STRINGER END FITTING. INSTALLED FITTING. 2 L 7 2 4F 4 F RT A1NM E24NE 20080731 NM 2008 7 31 2008UALA03621 1 20080629 A 4910 7321387012 DOOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU ACTUATOR MALFUNCTIONED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 589UA 28707 THREE TRIES APU WILL NOT START - STATUS MSG APU DOOR. RESET C/B FOR APU DOOR ACT. CYCLED DOOR 2 TIMES ON GROUND AND TH EN STARTED 2 TIMES WITH AIR AND ELEC. LOAD ALL OPS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080731 NM 2008 7 31 CALA0800673 1 20080707 A 5311 6546534 FRAME BOEING 737 737524 1384721 NM BS 520 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 LEFT STATION 520 FRAME CRACKED AT AIR CONDTIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. REMOVED DAMAGE, FABRI CATED AND INSTALLED REPAIR ANGLES PER EA 5310-04498 AT STATION 520 LEFTHAND FRAME BETWEEN S-8 AND S-9. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 SWAA083807 1 20080713 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727E S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 CALA0800678 1 20080707 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM BS 867 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 LEFT STATION 867 FRAME CRACKED AT AIR CONDTIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. CUT OUT DAMAGE AT FRA ME STATION 867 LEFTHAND BETWEEN S-8 AND S-9, REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 CALA0800682 1 20080707 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM BS 907 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 RIGHT STATION 907 FRAME CRACKED AT AIR CONDTIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. CUT OUT DAMAGE AT ST ATION 907 RIGHTHAND BETWEEN S-8 AND S-9, REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 CALA0800683 1 20080707 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM BS 867 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 RIGHT STATION 867 FRAME CRACKED AT AIR CONDTIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. CUT OUT DAMAGE AT ST ATION 867 RIGHTHAND S-8 AND S-9, REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080731 EU 2008 7 31 PNS2008F00004 1 20080626 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 583-608 DENTED E PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 679PA 340B345 A DENT WAS NOTICED ON THE LT SIDE JUST FWD OF CARGO DOOR AC WAS REMOVED FROM SERVICE PENDING A REPAIR. NO EMERGENCY ACT ION WAS TAKEN AS DENT WAS DISCOVERED ON THE GROUND AND BROUGHT TO THE ATTENTION OF MAINT. THE DENT IS LOCATED AT STA 58 3-608 AND BETWEEN SL 1520 AND 1522. (K) 2 L 7 2 4T RT A52EU 20080731 EU 2008 7 31 PNS2008F00001 1 20080623 A 3397 WIRE SAAB SF340 340B 7860101 EU EMERGENCY LIGHT BROKEN E PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 676PA 316 DURING A SCHEDULED INSPECTION OF THE EMERGENCY LIGHTING SYSTEM, THE OVER WING EXIT LIGHTS FAILED TO ILLUMINATE. MAINT F OUND WIRE LN139-22 BROKE AT FUSE 71LN. THE WIRE WAS REPAIRED AND THE SYSTEM OPS CHECKED NORMAL. AC WAS RETURNED TO SER VICE AFTER INSPECTION WAS COMPLETED. (K) 2 L 7 2 4T RT A52EU 20080731 EU 2008 7 31 PNS2008F00003 1 20080519 A 3350 BULB SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE E PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 679PA 340B345 DURING F/A TRAINING, THE F/A ACTIVATED THE EMERGENCY LIGHTS AND NOTED THAT THE ARM LIGHT WAS NOT ILLUMINATED. MAINT REP LACED THE BULB AND THE SYSTEM OPERATED NORMALLY. THERE WAS NO EMERGENCY AS THIS WAS A GROUND TRAINING SESSION. (K) 2 L 7 2 4T RT A52EU 20080731 NM 2008 7 31 C8G2008F00005 1 20080625 A 7720 10200012 BULB BOEING 727 727200 138407E NM NR 2 ENG TEMP INOPERATIVE A C8GA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 29 713AA 22469 DURING TAKEOFF THE NR 2 ENG HAD A HIGH OIL TEMP LIGHT, CREW PERFORMED ENG SHUTDOWN AND THE AC RETURNED TO DEPARTURE WHER E IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE NR 2 ENG OIL TEMP BULB WAS AT FAULT. REMOVED AN D REPLACED OIL TEMP BULB. PERFORMED OPS AND LEAK CHECKS, GOOD. NO OTHER DEFECTS WERE NOTED. AC WAS RETURNED TO SERVIC E. (K) 2 L 7 3 4F RT A3WE 20080801 WP 2008 8 1 08FDEA02427 1 20080615 A 5522 SKIN DOUG MD10 MD1010F 3022112 WP RT ELEVATOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 554FE 88711 LTV46708 46708 ON MX POST FLIGHT INSP FOUND RT OUTBOARD ELEVATOR DAMAGED. APPEARS TO BE LIGHTNING STRIKE AT OUTBOARD TIP AND TIP TRAIL ING EDGE OF ELEVATOR ACCOMPLISHED RT OUTBOARD ELEVATOR INSTALLATION STEP NR 3-B ITEM NR 18 AND STEP NR 3-C 1 THRU 9. 2 L 7 3 4F RT A22WE 20080801 EU 2008 8 1 08FDEA02394 1 20080624 A 5320 A53973085208 SILL AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 AFT CARGO COMP DOOR SILL BEAM WITH MILD CORROSION ALONG FLOOR LEVEL FR 59A RBL62 (158CM). REMOVED THE RELATED STRUCTURE PER SRM 51-40-21.2. REMOVED CORROSION PER SRM 51-74-10. APPLIED ALODINE TO THE REMOVED AREA. MEASURED THE REMAINING THICKNESS PER NTM51-10-04.101, THE THICKNESS IS 0.081 INCH. THE DETAILED REPAIR SEE EA NR 6-5310-117355. 2 L 7 2 4F RT A35EU 20080801 NM 2008 8 1 08FDEA02019 1 20080528 A 5100 NONE BOEING 757 757200 1384950 NM IAW SRM NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 919FD 24636 PATCH REPAIR ON OUTBOARD LEADING EDGE OF LH WING OUTBOARD FLAP TO BE EVALUATED. EXISTING REPAIR EVALUATED AND FOUND PR EVIOUSLY ACCOMPLISHED IAW SRM 57-53-01 FIG.202. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. NOT AN SDR 2 L 7 2 4F RT A2NM 20080801 NM 2008 8 1 2008UALA03006 1 20080526 A 2150 1942704 HEAT EXCHANGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 A/C PACK CRACKED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 646UA 25283 NR 1 PACK IS PUTTING OUT 50 DEGREE AIR, FOUND A 8" CRACK IN NR 1 HEAT EXCHANGER. FOUND CRACK IN HEAT EXCHANGER. REPL ACED HEAT EXCHANGER ASSEMBLY. IAW MM21-51-02 RAN BOTH PACKS NO DEFECTS NOTED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080804 NM 2008 8 4 08FDEA02575 1 20080630 A 5753 652678739 SHIM BOEING 727 727225 1384077 NM LT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 PANEL RACK, LT WING I/B FLAP ASSY O/B FWD NR 3 FAIRING HAS CRACK ON INTERIOR TAPERED/CHAFF SHIM. REMOVED SHIM AND REI NSTALLED NEW SHIM. REF MM 51-51-011-8 PGS 1-5. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080804 NM 2008 8 4 08FDEA02580 1 20080630 A 5315 FLOORBEAM BOEING 757 7572B7 1384964 NM BS 1640 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 906FD 27148 CABIN FLOORBEAM, HAS CORROSION, BS 1640, LBL 6 - RBL 6. COMPLIED WITH EA F-5310-110867, REV -, DATED 05/20/2008. EA CL ASSIFIED REPAIR AS A MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20080804 SO 2008 8 4 LR7A08089 1 20080701 A 5523 BRACKET LKHEED 382 382G 526414U SO ELEVATOR TAB CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 636 4763 DURING SCHEDULED B-2 CHECK, PER JOB CARD HB2703, FOUND ELEVATOR BRACKETS IN TRIM TAB WELL CRACKED AT HSS77R AND HSS113R. REPAIR BY BRACKET FABRICATION AND INSTALLATION IAW SMP583 CH 51-60 AND 70 AND DRAWING 353948-4R. 2 H 7 4 4T A1SO 20080804 SO 2008 8 4 LR7A08090 1 20080701 A 5320 ANGLE LKHEED 382 382G 526414U SO FS 557 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 636 4763 DURING SCHEDULED B-2 CHECK, PER JOB CARD HB3200, FOUND RT MLG WHEEL WELL CHINE ANGLE CRACKED AT FS557 WL141. REPAIR IAW SMP583 FIG 51-140-19. 2 H 7 4 4T A1SO 20080804 NM 2008 8 4 08FDEA02470 1 20080625 A 5532 PANEL BOEING 727 727225 1384077 NM ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 TAIL DOCK VERTICAL STAB LT TOP PNL 9706 HAS DELAM ON PNL RADIUS IN CTR OF PNL. REPAIRED PANEL NR 9706 REF SRM 51-40-9 P AR 3, 4. "THIS IS CLASSIFIED AS A MINOR REPAIR." 2 L 7 3 4F A3WE 20080804 NM 2008 8 4 08FDEA02482 1 20080625 A 5340 6545313Y2 STRINGER CLIP BOEING 727 727225 1384077 NM BS 804 S7R CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 MID CABIN AT STA 804 STRINGER 7R STRINGER CLIP CRACKED. REMOVED STRINGER CLIP STA 804 STR 7R. REF 727 SRM 51-30-2 P1. MATCH DRILLED NEW STRINGER CLIP P/N 65-4531342 A 18793 P/O 1038874. REF 727 SRM 51-30-2 P1. INSTALLED NEW STRINGER CL IP STA 804 STR 7R REF 727 SRM 51-30-2 P1. THIS REPAIR IS CLASSIFIED AS MINOR REPAIR. 2 L 7 3 4F A3WE 20080804 EU 2008 8 4 08FDEA02505 1 20080626 A 3231 DOOR AIRBUS 310 A310222 3930315 EU NLG INOPERATIVE A FDEA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CE 21 422FE 346 NOSE GEAR DOORS NOT RETRACT ON GEAR RETRACTION. LOUD NOISE AND SHUTTER WAS FELT WHEN GEAR HANDLE PLACED IN NEUTRAL POSI TION. RETURNED TO INDY. LANDED WITH SAFE GEAR INDICATION. 2 L 7 2 4F RT A35EU 20080730 NM 2008 7 30 CALA0800665 1 20080702 A 5311 651630087 FRAME BOEING 737 737524 1384721 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 STATION 178 SIDE CHORD RIGHT-HAND SIDE AT WL 207 IS CRACKED. REMOVED AND REPLACED RIGHT-HAND SIDE CHORD IAW B737 SRM 51 -40-02 AND EC/RA 5310-04794, EC/RA 5310-04794. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 CALA0800670 1 20080623 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM BS 400 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 STATION 400 RIGHT FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. REPAIRED CRACKED FR AME AT BODY STATION 400 AT A/C BRACKET BETWEEN S-8R AND S-9R PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083923 1 20080714 A 2432 279202 CHARGER BOEING 737 7373H4 1384600 NM BATTERY FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 606SW 27926 AIR TURNBACK, ACRID ODOR REPORTED IN CABIN AND FLIGHT DECK. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083904 1 20080714 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 578 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080806 EU 2008 8 6 AALA200801418 1 20080528 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA O OTHER O OTHER CR CRUISE 1 SW 21 59081 639 SJU INFLIGHT T1555/28MAY. EMERGENCY LIGHT AT RIGHT HAND AISLE EXIT ILLUMINATED IN FLIGHT. REPLACED BATTERY PACK FOR EM ERGENCY LIGHT AT RIGHT HAND AISLE EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080806 NM 2008 8 6 AALA200801438 1 20080530 A 3350 1317 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 922AN 29523 LGA - EMERGENCY LIGHT AT SEAT ROW 25ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 25ABC. SYSTEM GROUN D CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A16WE 20080806 WP 2008 8 6 AALA200801432 1 20080529 A 2560 BATTERY DOUG DC9 DC982 3022082 WP FLASHLIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 561AA 53091 LGA - EMERGENCY FLASHLIGHT AT FORWARD JUMP SEAT INOPERATIVE. REPLACED BATTERIES FOR EMERGENCY FLASH LIGHT AT FORWARD JU MP SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080806 EU 2008 8 6 AALA200801406 1 20080526 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 JFK - EMERGENCY LIGHT AT RT NR FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT NR FOUR DOOR. SYSTEM GRO UND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080806 NM 2008 8 6 AALA200801364 1 20080522 A 3350 60030451 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9413T 53188 SFO - EMERGENCY LIGHTS AT OVERHEAD SEAT 25D AFT TO TAIL CONE INOPERATIVE. CHARGED BATTERY PACK FOR EMERGENCY LIGHT AT O VERHEAD SEAT 25D AFT TO TAIL CONE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT 20080806 NM 2008 8 6 USAA920081377 1 20080714 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 946 S24L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 443US 24842 CLT - RON - MAJOR REPAIR - CRACK IN FUSELAGE JUST FORWARD OF AFT LT WATER SERVICE PANEL AT S24L AND FORWARD OF FRAME 946 . REPAIRED FUSELAGE JUST FORWARD OF AFT LT WATER SERVICE PANEL AT S24L AND FORWARD OF FRAME 946 IAW US AIRWAYS EA NR100 570. (S) 2 L 7 2 4F RT A16WE 20080806 NE 2008 8 6 DXTA200803181 2 20080717 A 7310 FUEL SYS CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE LT ENGINE FLUCTUATES E DXTA A UNSCHED LANDING R Y E PARTIAL RPM/PWR LOSS ENGINE STOPPAGE VIBRATION/BUFFET CR CRUISE 1 GL 07 325QS 5600425 LT FUEL FLOW FLUCTUATION DURING CLIMB AND CRUISE FOLLOWED BY LT ENG FAILURE, FOLLOWED BY LT ENGINE VIBRATION. 2 L 7 2 4F 4 F RT A22CE E25EA 20080806 NM 2008 8 6 AALA200801452 1 20080601 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 617AM 24525 DFW - EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 29D. SYSTEM GROUND CHECK ED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080806 EA 2008 8 6 TRAX200800830 1 20080624 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 977EV 7720 FS 280 RBL 9.0 O/B CLIP CRACKED. REMOVED OLD CRACKED CLIP AT FS 280.00 RBL 9 O/B. INSTALLED NEW SERVICEABLE CLIP IAW C RJ 200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 TRAX200800838 1 20080625 A 5210 HINGE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FOD A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 ACFT PASSENGER DOOR DIFFICULT TO OPEN AFTER FLIGHT. REMOVED DEBRIS FROM PASSENGER DOOR HINGE TRACK. PERFORMED OPS CHEC K OF MAIN PASSENGER DOOR IAW AMM 52-11-00. NO DEFECTS NOTED. (S) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 TRAX200800840 1 20080626 A 5210 LATCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 FORWARD DOOR DIFFICULT TO OPEN FROM INSIDE AND OUTSIDE. LUBED AND CLEANED PASSENGER DOOR LATCH. OPS CHECK GOOD AT THIS TIME REF: 52-00-00 AND 20-00-00. (S) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 SIMA200819901 2 20080715 A 7261 OIL SYSTEM EMB 135 EMB135LR 3260305 SO RROYCE AE3007 AE3007A13 54166 EA NR 1 ENGINE LEAKING A SIMA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 729AE 18117 18117 145343 CAE311310 ON FLIGHT 4881 CREW REPORTED OIL SMELL IN THE COCKPIT THROUGHOUT ALL PHASES OF FLIGHT. ACFT REMOVED FROM SERVICE. REMO VED AND REPLACED NR 1 ENG. OPERATIONAL CHECK GOOD, NO SMOKE. ACFT RETURNED TO SERVICE. (S) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080807 NM 2008 8 7 KCSA081344 1 20080724 A 5411 FRAME BOEING 747 747122 1384872 NM NR 2 NACELLE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 #2 PYLON NAC STA 200, BETWEEN STR 2 &3 HAS CHAFFED DAMAGED ON OUTBOARD SIDE OF FRAME. (A) 2 L 7 4 4F RT A20WE 20080807 NM 2008 8 7 KCSA081357 1 20080729 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2040 S34R CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FUSELAGE SKIN CORRODED AT BS 2040, STR 34R. (S) 2 L 7 4 4F RT A20WE 20080724 EU 2008 7 24 2008UALA02996 1 20080525 A 2611 SMOKE WARNING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 467UA 1359 AVIONIC SMOKE ECAM, NO SMOKE PERCEPTIBLE. FLIGHT DIVERTED. FOUND NO EVIDENCE OF SMOKE OR ODORS ON MAIN DECK OR E&E COM PARTMENT, ECAM HAD CLEARED UPON ARRIVAL, SUCCESSFULLY TESTED AEVC AND SCDU REF AMM 21-26-00. CHECK PFR REPORT FOR FAILU RE MESSAGES, NONE FOUND. TESTED LWR CARGO FIRE SYSTEM - NORMAL, AND RESET FWC'S PRECAUTIONARY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03278 1 20080606 A 2612 PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT CONTAMINATED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 318UA 23950 COFFEE SPILLED ON CENTER CONSOLE IN COCKPIT. FLUID GOT ONTO CARGO FIRE SUPPRESSION PANEL ONLY AND DOES NOT TEST. BOTH CARGO FIRE BOTTLES ARE BLOWN. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 EU 2008 7 24 2008UALA03292 2 20080609 A 7200 ENGINE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 FLAMED OUT A UALA O OTHER X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 WP 29 399UA 24674 721621 NR 1 ENGINE FLAMEOUT ON TAXI OUT. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 EU 2008 7 24 2008UALA03056 1 20080527 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 447UA 836 FLOORBEAM ITEM 165 HAS CORROSION. ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED BEAM 165 FOR CORROSION WORK CONT OF AMIS I TEM 0912012. REPLACED BEAM REF SRM 53-41-14. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 EU 2008 7 24 2008UALA03061 1 20080527 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 447UA 836 DOOR SILL 2R HAS CORROSION AT FRAME 66 AND 68 AT NUT PLATE (MARKED). ACCOMPLISHED MAJOR REPAIR AT DEN. REMOVED DAMAGE, MFG REPAIR PARTS, TREATED PRIMED AND TOP COATED WITH PAINT. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 UPS08M52413 1 20080504 A 5320 WEB DOUG MD11 MD11 3023602 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C CABIN LT L27 STA 1946-1986 CHORD WEB AREA FOUND SURFACE CORRODED AS MARKED. LT L27 STA 1946-1986 CORR OSION ON WEB SURFACE REMOVED PER SRM 51-21-01 VII R35. CABIN - LT 27 STA 1946-1986 CHORD WEB REMOVED PER SRM 51-31-01 V II R35. NEW WEB FAB PER DWG AGA7145-503 AND INSTALLED PER SRM 51-31-01 VII R35. 2 L 7 3 4F RT A22WE 20080724 2008 7 24 2008UALA03221 4 20080605 A 3497 286W20211 WIRE HARNESS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WEATHER RADAR SHORTED A UALA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 WP 29 553UA 25277 CREW REPORT: WX FAIL RADAR SAMC TEXT: ANTENNA MSG ON BOTTOM OF SCREEN. RESET CB TO TRANCVR UNIT, NO HELP. HARNESS SHO RTED FROM FWD BULKHEAD TO SCANNER. REPLACED HARNESS. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 EU 2008 7 24 2008UALA03314 1 20080610 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN UNKNOWN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 479UA 1538 EPSU INT LOAD FWD L FOUND ON 3SVC CHECK. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03326 1 20080607 A 3510 OXYGEN MASK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 806UA 788 F/O OXYGEN MASK WILL NOT PRESS TO TEST. MASK INFLATES AND WORKS BUT TEST FUNCTION INOP. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 SWAA083860 1 20080713 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 353SW 24889 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083918 1 20080715 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727B, STR 13L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083884 1 20080714 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 25R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083889 1 20080714 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083931 1 20080715 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 2008UALA03334 1 20080611 A 2150 6319001 ACM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A/C BAY FAULTY A UALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION IN INSP/MAINT 1 WP 29 530UA 25043 AFTER TURNING ON APU & PACKS SMOKE IN CABIN SET OFF SMOKE ALARMS. ACM FAILURE, POSSIBLE BEARING FROZEN. REPLACED ACM, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03381 1 20080614 A 3350 30043233 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EXTERIOR BURNED OUT A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 338UA 24242 DOOR 2R EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT INOP. FOUND LIGHT BURNED OUT AND FUSE BLOWN. REPLACED LIGHT ASSEMBLY AND FUSE OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080725 NM 2008 7 25 2008UALA03240 1 20080606 A 2421 OIL SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE IDG LOW A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 548UA 25396 INOP APU AND ENGINE GENERATOR. AMBER ALERT DECLARED. UNEVENTFUL LANDING. *S/D* LOW OIL QTY IN IDG. SERVICED IDG, RA N ENGINES AT FULL ELECTRICAL LOAD, NO PROBLEMS. 2 L 7 2 4F 4 F RT A2NM E17NE 20080725 NM 2008 7 25 CALA0800638 1 20080623 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM BS 747 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13624 27528 RIGHTHAND SIDE STATION 747 FRAME BETWEEN S-8 AND S-9 AIR CONDITIONING (A/C) BRACKET INBOARD MOUNT HOLE CRACKED. REPAIRE D FRAME AT STATION 747 BETWEEN S-8 AND S-9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080725 EA 2008 7 25 SWIA200819827 1 20080628 A 3520 OXYGEN MASK CNDAIR CL600 CL6002B19 1900309 EA CABIN UNWANTED DEPLOY A SWIA G O2 MASK DEPLOYED O OTHER NR NOT REPORTED 1 NM 07 934SW 7722 FLT 6562 - ALL OXYGEN MASKS DROPPED IN CABIN WHILE STARTING APU. RESTOWED OXYGEN MASKS PER AMM 35-20-00. 2 L 7 2 4F RT A21EA 20080725 EA 2008 7 25 SWIA200819846 1 20080705 A 2710 6224404101 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA SERVO AILERON WORN A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 457SW 7773 FLT 4083 - AILERON CONTROLS FEEL STIFF. REPLACED AILERON SERVO IAW CRJ MM 22-11-21 AND COPILOT'S CONTROL YOKE BEARING I AW MM 27-11-01. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080725 WP 2008 7 25 IXX2008F00004 1 20080711 A 3222 STRUT DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE NLG CONTAMINATED A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 604BX 46046 DURING TAKEOFF, FLIGHT CREW WAS UNABLE TO RAISE GEAR HANDLE. FLIGHT CREW ACCOMPLISHED CHAPTER 3 PORCEDURE IN COCKPIT OP ERATING MANUAL AND RAISED GEAR. GROUND CONTROL RELAY CIRCUIT BREAKER RELAYS WERE OPEN FOR FLIGHT AND RESET AFTER LANDI NG. AC LANDED UNEVENTFUL. MAINTENANCE REMOVED NOSE STRUT, FOUND TRASH IN FLUID RETURN REBOUND CHECK VALVE, FLUSHED OUT TRASH, REPACKED, AND REINSTALLED CHECK VALVE. OPS CHECK GOOD IAW MM 32-21-2. AC WAS RETURNED TO SERVICE. (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 20080725 NM 2008 7 25 PID2008F00001 1 20080713 A 7930 1163P181 BYPASS SWITCH BOEING 737 7372K5 138448X NM PWA JT8 JT8D15 52051 NE OIL FILTER INOPERATIVE A PIDA O OTHER J WARNING INDICATION CR CRUISE 1 EA 39 250TR 22597 OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. SHUTDOWN RT ENGINE IAW QRH. DIVERTED FLT. INSPECTED NR 2 MAIN ENGINE OI L FILTER AND CLEANED BYPASS CONNECTOR SWITCH. RAN NR 2 ENGINE, BYPASS CONNECTOR SWITCH. RAN NR 2 ENGINE, BYPASS LIGHT DID NOT ILLUMINATE. PERFORMED OPS CHECK IAW MM 79-02. RELEASED ON MEL 79-02 CNTRL NR 0713001. 7/16/2008 REMOVED AND RE PLACED NR 2 ENG BYPASS SWITCH. RUN-UP OPS CHECKED GOOD IAW 79-35-11 MEL CLEARED. (K) 2 L 7 2 4F 4 F RT A16WE E2EA 20080725 CE 2008 7 25 U5Q2008F00000 1 20080604 A 3233 IENI8 SWITCH LEAR 60 60LEAR 5170707 CE LT MLG ACTUATOR STICKING E U5QA O OTHER O OTHER NR NOT REPORTED 1 GL 07 198HB 198 NO GEAR DOWN INDICATION (GREEN LIGHT). CYCLED GEAR, STILL NO DOWN AND LOCKED ON LT SIDE. NOSE AND RT OK. ACTIVATED EM ERGENCY BLOW DOWN AND LIGHT CAME ON. MADE NORMAL LANDING. MAINT FOUND BALL AND SWITCH STICKING. LUBED AND ADJUSTED. ( K) 2 L 7 2 4F RT A10CE 20080725 2008 7 25 WRN2008F00000 2 20080607 A 7210 CF6A6BMF1 GEARBOX AIRBUS 300 A300B4203 3930306 EU NR 2 ENG CONTAMINATED A WRNA O OTHER O OTHER NR NOT REPORTED 1 EA 39 501TR 53 ON CLIMBOUT STJ FL230, OIL QTY DECREASING RAPIDLY. PERFORMED PRECAUTIONARY SHUTDOWN PROCEDURES, OIL PRESSURE WAS NOT LO ST, OIL TEMP RISE TO 130 DEGREES. REPLACED GEARBOX IAW MM 72-60-01. OPS CHECK GOOD ON NR 2 ENGINE. (K) 2 L 7 2 4F RT A35EU 20080728 EA 2008 7 28 VNAA0805021 1 20080516 A 7722 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE COCKPIT MALFUNCTIONED A VNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 05 229PS 7898 CREW REPORTED THE LEFT AND RIGHT HAND ITT SPIKED ON TAKEOFF ROLL. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WIT HOUT INCIDENT. MAINTENANCE INSPECTED THE LEFT AND RIGHT HAND ITT WITHIN LIMITS IN ACCORDANCE WITH THE AIRCRAFT MAINTENA NCE MANUAL. MAINTENANCE COMPLIED WITH THE ABORTED TAKEOFF INSPECTION. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20080728 NM 2008 7 28 UIE2008F00003 1 20080701 A 5311 FRAME BOEING 747 747243B 1384830 NM BS 400 S22R CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 540MC 22508 FRAME CRACKED AT STATION 400 STRINGER 22R. REPLACED DAMAGED FRAME IAW SRM 51-10-01 AND SRM 51-30-02. (K) 2 L 7 4 4F RT A20WE 20080728 EU 2008 7 28 UPS08152598 1 20080619 A 5753 SKIN AIRBUS A300 A300F4622R 3930360 EU T/E FLAP CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 152UP 0835 INSPECTION TYPE:5YR 2EA CHAFE MARKS ON UPPER SURFACE OF RT INBOARD FLAP AT RIB 12 & 14 STR 2.2 & 2.3. 2EA AREAS FOUND OU T OF LIMITS ON NRC 196779. CUT OUT 2EA DAMAGED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300 SRM 57-50-00 FIG 205. 2 L 7 2 4F RT A35EU 20080728 EU 2008 7 28 UPS08152596 1 20080617 A 5321 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 152UP 0835 INSPECTION TYPE:5YR MAIN DECK CARGO FLOOR PNL 231RG HAS BROKEN EDGE. REPAIRED MAIN CARGO FLR PNL 231RG IAW A300 SRM 53- 10-20 TABLE 201 PAR 8A. 2 L 7 2 4F RT A35EU 20080728 EU 2008 7 28 QML2008F00002 1 20080705 A 3110 POWER SUPPLY BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101* NE INSTRUMENT PANEL BURNED E QMLA E D ENGINE SHUTDOWN RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 117TX 7177 PRIOR TO TAKEOFF FROM HOSPITAL HELIPAD, THE PILOT INSTRUMENTS LIGHTS WENT DARK. SOON AFTERWARDS THERE WAS THE ODOR OF B URNING INSULATION IN THE COCKPIT. AC SHUTDOWN, DISCUSSION WITH THE MAINT TECH CONCLUDED A SUSPECTED PILOT INSTRUMENT PO WER SUPPLY FAILURE. AC WAS PLACED ON MEL STATUS AND RETURNED TO HOME BASE FOR INSPECTION. THE SUSPECTED PART WAS REMOV ED AND INDEED HAD THE ODOR OF BURNED INSULATION. (K) 1 G 7 2 3U 3 U H13EU E5NE 20080728 EU 2008 7 28 2008UALA03499 1 20080619 A 2710 3945128102 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ELAC FAILED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 411UA 464 ELEVATOR - AILERON COMPUTER (ELAC) 2 INOP. CHANNEL 4 CPU FAILURE (INTERNAL) ON ELAC 2. REPLACED ELAC 2, OPS CHECKED GO OD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 SO 2008 7 28 YJU2008F00000 1 20080707 A 3244 384F832 TIRE GULSTM G1159 G1159A 3970109 SO RROYCE SPEY SPEY5118 54523 EU RT MLG UNSERVICEABLE E YJUA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 07 797BD 388 11194 PILOTS REPORTED THAT ON TAKEOFF, THEY FELT A BUMP FOLLOWING THE VR CALLOUT. AFTER LANDING, IT WAS DISCOVERED THAT THE N R 3 MAIN TIRE TREAD HAD COMPLETELY SEPARATED FROM THE TIRE DOWN TO THE CORD AREA. THE TREAD COMING OFF DAMAGED THE FLAP TORQUE TUBE, SEVERED THE CONTROL CABLES FOR THE SPOILERS AND SPEED BRAKES FOR THE RT WING, AND ALSO PUNCTURED THE WING JUST IB OF THE FLAPS. THE ENGINE NACELLE, FUSELAGE AND WINGS EXHIBITED DENTS OF VARIOUS SIZES AND DEPTH ALONG WITH BLAC K RUBBER SCUFF MARKS FROM THE TIRE TREAD. THE NR 3 TIRE PRESSURE WAS FOUND TO BE 161 PSI AT 67450 LBS RAMP WEIGHT 2 DAY S AFTER THE INCIDENT. (K) 2 L 7 2 4F 4 F A12EA E2EU 20080730 2008 7 30 SWAA083924 4 20080715 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED CV CHECK, R1 DOOR EMERGENCY EVAC SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083873 1 20080710 A 3350 101114 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 723SW 27855 DURING SCHEDULED MV1 CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083697 1 20080704 A 5320 6545866 SUPPORT FITTING BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND KEEL BEAM SUPPORT FITTING CRACKED AT BS 727, LBL 5. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083721 1 20080704 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 834 S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 834, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083702 1 20080704 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 380, LBL 0. REPAIRED SKIN PER EA & ACO. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083966 1 20080716 A 5311 6978188 FRAME BOEING 737 7373H4 1384600 NM BS 767 S14R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 767, STR 14R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080731 SO 2008 7 31 C2XA08ON136 1 20080614 A 2612 FIRE DETECTOR EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 16546 15241 11598 145562 FLT 0303 - AUS - FLIGHT CREW REPORTED BAD FIRE DETECTOR. MX RESET FIRE DETECTION SYSTEM. OPERATIONALLY CHECKED SATISFA CTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080731 EA 2008 7 31 HNAA0800197 1 20080607 A 3260 YD4N RELAY DHAV DHC8 DHC8311 1386006 EA NLG DEFECTIVE A HNAA O OTHER N FALSE WARNING LD LANDING 1 EA 07 327EN 261 UPON LANDING GEAR RETRACTION NOSE RED UNSAFE LIGHT ILLUMINATED ALONG WITH TRANSIT LIGHT IN HANDLE AND AMBER NOSE GEAR DO OR LIGHTS. NOSE GEAR RETRACTED AND AFTER ABOUT 10 SECONDS THERE WAS A THUMPING NOISE ALONG WITH DOOR AND UNSAFE LIGHTS STILL ILLUMINATING INTERMITTENTLY. REPLACED TIME DELAY RELAY 3261-K11, MM 32-20 RESET PSEU, CYCLED GEAR, OPS CHECK GOOD . (S) 2 H 7 2 4T RT A13NM 20080731 EA 2008 7 31 COMA0860305 1 20080625 A 2913 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM TRIPPED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 934CA 7042 RECEIVED HYD PUMP 3A CAUTION MESSAGE, THEN HYD 3 LOW PRESSURE CAUTION. ABORTED APPROACH, PERFORMED QRH, LANDED WITHOUT INCIDENT. FOUND HYD 3A CIRCUIT BREAKER POPPED. RESET BREAKER, NO FURTHER DEFECTS. (S) 2 L 7 2 4F RT A21EA 20080731 SO 2008 7 31 C2XA08CL067 1 20080608 A 3350 1317 BULB EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS FAULTY A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 14945 145049 DURING ROUTINE MAINTENANCE THE AFT OVERHEAD WHITE EMERGENCY FLOOD LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AN D REPLACED THE AFT OVERHEAD WHITE EMERGENCY LIGHT BULB. OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4F RT T00011AT 20080731 NM 2008 7 31 C8GA200800A 1 20080611 A 7722 152BL801E INDICATOR BOEING 727 727225 1384077 NM EGT MALFUNCTIONED A C8GA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 29 801EA 22432 FLT 738 FRO TOL TO SLW. DURING TAKEOFF ROLL THE NR 2 ENG EGT INDICATOR WENT TO ZERO INDICATION. THE TAKEOFF WAS ABORTE D. THE ACFT RETURNED TO THE BLOCKS WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED NR 2 ENGINE EGT INDICATOR AT FAUL T. THE NR 2 ENG EGT INDICATOR WAS REMOVED AND REPLACED. OPS CHECK GOOD. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURN ED TO SERVICE. (S) 2 L 7 3 4F A3WE 20080731 EA 2008 7 31 VNAA0806005 1 20080607 A 5240 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE GROUND POWER OPEN A VNAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 05 708PS 10160 CREW REPORTED AN EXTERNAL GROUND POWER DOOR LEFT OPEN AFTER TAKEOFF. THE CREW ELECTED TO RETURN TO CLT AND LANDED WITHO UT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO DAMAGE OR DEFECTS. MAINTENANCE SECURED THE DOOR CLOSED. ACFT WAS RELE ASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E00063EN 20080731 EA 2008 7 31 COMA0860294 1 20080619 A 2750 890D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 514CA 13241 7809 RECEIVED FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY, RAN QRH, LANDED WITHOUT INCIDENT. REPLACED FECU. NO FURTH ER DEFECTS. (S) 2 L 7 2 4F RT A21EA 20080731 NM 2008 7 31 2008UALA03619 1 20080628 A 5414 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NR 1 PYLON STRUT I/B SIDE STRUT ACCESS HOLE FOR PANEL 416BR AFT UPPER CORNER SKIN IS CRACKED. STOP DRILLED CRACK. FABRI CATED & INSTALLED 2EA DOUBLERS. HFEC INSP, NO CRACK PAST STOP DRILL. 2 L 7 2 4F 4 F RT A1NM E24NE 20080731 NM 2008 7 31 CALA0800680 1 20080707 A 5311 65C34355 FRAME BOEING 737 737524 1384721 NM BS 482 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 RIGHT STATION 482 FRAME CRACKED AT AIR CONDTIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. CUT OUT DAMAGE AT ST ATION 482 RIGHTHAND AT S-8 AND S-9, REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080731 2008 7 31 YEN2008F00005 4 20080601 A 2300 1707789E MODULE EMB ERJ190 ERJ190100IGW 3260408 NM COMMS MALFUNCTIONED A YENA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 15 203JB 6238 19000023 DECLARED EMERGENCY, THE SPDA FAIL EICAS APPEARED IN FLIGHT ON THE ELEC PG THE AC BUSS TIE, APU ICON, AC BUSS 2, TRU, DC BUSS 2. DC US ICON FLASHED FROM GREEN POWERED TO DASHES. COMPLIED W/QRH PROCEDURE. AFTER LDG ENG 1, 2 NO DISPLAY MSG AND CARGO FIRE PROT FAULT APPEARED AFTER LDG. REPLACED SPOA COMMS MODULE SLOT 8 SPDA, NR 2, MM 24-61-07-400-301-A. (K) 2 L 7 2 4F RT A57NM 20080731 EU 2008 7 31 YEN2008F00003 1 20080601 A 2913 3031863001 PUMP AIRBUS 320 A320232 3930326 EU HYD SYSTEM CRACKED A YENA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 15 558JB 13426 1915 ENG 1 PUMP LOW PRESSURE, DECLARED EMERGENCY, MANUAL GEAR EXTENSION, NOSEWHEEL STEERING INOP. REMOVED AND REPLACED ENG D RIVEN HYD PUMP NR 1, IAW 29-11-51-04, REMOVED AND REPLACED CASE FILTER IAW AMM 29-11-11-43 T/S IAW TSM 29-11-00-810-804, OPS CHECK OK. 2 L 7 2 4F RT A28NM 20080804 NM 2008 8 4 08FDEA02464 1 20080625 A 5344 66168497 HINGE BOEING 727 727225 1384077 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 GROUND POWER ACCESS PANEL. TOP HINGE BRACKET CRACKED REMOVED DAMAGED PART PER REF SRM 51-30-02 PG 1-3, FABRICATED NEW P ART PER REF DWG NR 66-16849-7, TREATED AND PRIMED NEW PART PER REF SRM 51-10-02. INSTALLED NEW PART PER REF SRM 51-30-0 2 PG 1-3. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080804 SW 2008 8 4 WGEA200800065 1 20080712 A 3244 M16901 TIRE ECLIPS EA500 ECLIPSEEA500 3350000 SW RT MLG FAILED A WGEA O OTHER O OTHER LD LANDING 1 EA 27 146DJ 000058 NR 1 "RIGHT MAIN GEAR TIRE BLEW-OUT DURING LATTER PORTION OF LANDING ROLLOUT". RT TIRE BLOWN ON LANDING, DAMAGE TO RT G EAR DOOR AND LOWER SKIN AFT OF GEAR WELL. REPLACED TIRE AND ROUTED AIRCRAFT TO MAINTENANCE FACILITY. (A) 1 L 7 2 4J RT A00002AC 20080804 WP 2008 8 4 08FDEA02577 1 20080630 A 5755 NRC6048 SKIN DOUG DC10 DC1010 3022110 WP NR 2 SPOILER CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 RT WING T/E MODERATE CORROSION ON LOWER SKIN SPOILER NR 2. 2 L 7 3 4F A22WE 20080804 EU 2008 8 4 08FDEA02484 1 20080625 A 5347 A5361251820002 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 660FE 759 MDCC SEAT TRACK NR 2 LT HAS AREA OF CORROSION BETWEEN FR 14A AND FR 17 REMOVED LEVEL 1 CORROSION. REMOVED AND REPLACED SEAT TRACK WITH NEW PART AT TRACK NR 2 LT BETWEEN FR 14A AND FR 17 IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02485 1 20080625 A 5315 A53779699200 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 660FE 759 THRU FWD CARGO FRAME 31, MDCC FLOORBEAM BETWEEN SEAT TRACK NR 4 LT AND NR 5 LT HAS .250 INCH CRACK REMOVED DAMAGED SECT ION AND INSTALLED CROSSBEAM REPAIR AT FR 31 BETWEEN SEAT TRACK NR 4 LT AND NR 5 LT IAW A300-600 SRM 53-10-15, FIG 206. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02502 1 20080626 A 5311 A53970021202 FRAME AIRBUS 310 A310203 3930313 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 423FE 281 PREVIOUS FRAME REINFORCING PLATE REPAIR LOCATED IN MAIN CABIN ON FRAME 54.2 INNER FLANGE BETWEEN STRINGERS 11 TO 15 LT, HAS 1 EACH EXTERNAL FORMED REPAIR PLATE MEASURING 21.8 INCHES LONG BY 2.2 INCHES TALL AND THE FRAME INNER FLANGE HAS A C UT OUT MEASURING 11 INCHES LONG. REPAIR NOT IAW EA6-5321-50501 REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED COR RECT REPAIR IN MAIN CABIN ON FRAME 54.2 INNER FLANGE BETWEEN STRINGERS 11 TO 15 LT IAW EA6-5310-121285. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02793 1 20080709 A 5321 B5327070500000 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN DECK FLOORBOARD 262 WF IS BROKEN. MATERIAL ID N 407 35039-003, PO 613022.1 AND FABBED A NEW PANEL IAW FEDEX DWG SR Z 25-- 5; REV F. PART MARKED IAW FEDEX GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02794 1 20080709 A 5321 B5327028300200 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN DECK FLOORBOARD NR 251 XF IS CRACKED. MAT ID N 407 35039-003, PO 613022.1. FABBED A NEW PANEL IAW SRZ 25-005; REV F. PART MARKED IAW GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02795 1 20080709 A 5321 B5327027600200 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN DECK FLOOR BOARD NR 251 RT IS CRACKED. MAT ID N 407 35039-003, PO 613022.1. FABBED A NEW PANEL IAW FEDEX SRZ 25-0 05; REV F. PART MARKED IAW FEDEX GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080804 NM 2008 8 4 08FDEA02563 1 20080630 A 5320 654N0244447 SILL BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 AFT CARGO DOOR LOWER SILL FROM BS 1380 TO BS 1440 HAS CORROSION IN NUMEROUS AREAS. CORROSION FOUND EXCEED B757-200 SRM 51-10-02 ALLOWABLE LIMITS. REMOVED AND REPLACED LOWER SILL PANEL IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. RE PAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080804 EU 2008 8 4 08FDEA02589 1 20080521 A 5100 NONE AIRBUS 300 A300B4622R 3930312 EU IAW SRM NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 721FD 477 PREVIOUS REPAIR FOUND LOCATED ON RUDDER RT STA270-869 RIB BR2-7, OUTER SKIN. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PERMANENT REPAIR WAS PERFORMED IAW FEDEX EA 6-5540-118158R. NOT AN SDR. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02590 1 20080701 A 5753 A57960000002 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND OLD DOUBLER REPAIR ON LT INNER FLAP LOWER SKIN RIB 17-17A. DOUBLER REPAIR RENEWED IAW RAS/FOK/178/2008 ISS A, APP ROVED BY EA 6-5752-120097. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02826 1 20080711 A 5754 A57864064286 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 2 SLAT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND ON LT SLAT NR 2 TRAILING EDGE BOTTOM SKIN ATTACHMENT HOLES CHAFING MARKS AND UNDETERMINED HOLES. REPAIR PERFORMED BY REMOVING THE DAMAGED SKIN PANEL AND INSTALLING A REPLACEMENT SKIN PANEL IAW RAS/FOK/089/2008ISS A, APPROVED BY EA 6 -5743-120041. 2 L 7 2 4F RT A35EU 20080804 NM 2008 8 4 08FDEA02567 1 20080630 A 5280 651841585 HINGE BOEING 727 727225 1384077 NM NLG DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 NLG STRUT WELL CUT OUT LT AFT DR SEAL RETAINER IS CORRODED BS 282-334, LBL 17, WL 150 (MRK). REMOVED OLD SEAL RETAINER, REF:SRM 51-30-02. INSTALLED NEW SEAL RETAINER, REF: SRM 51-30-02, P-1. THIS IS CLASSIFIED AS A MINOR REPAIR. THREE HINGE BRACKETS REMOVED FOR ACCESS TO SEAL RETAINER RIVET PATTERN. TO BE INSTALLED AND CHECKED FOR FIT, RIG, AND FUNCTIO N ON CARD NR 71C130-00. INSTALLED LT AFT NLG DOOR HINGES IAW SRM 51-30-02 P1. REMOVED LT AFT NLG DOOR TO FOM AND INSTA LLED DOOR AFTER OTHER MAINTENANCE COMPLETED IAW MM 32-22-001-4. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080804 SO 2008 8 4 LR7A08091 1 20080708 A 6120 7143257 VALVE LKHEED 382 382G 526414U SO NR 3 PROP DAMAGED A LR7A E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 AL 03 404LC 1107 4763 DURING CRUISE FLIGHT, CREW REPORTED NR 3 PROPELLER RPM OUT OF LIMITS. PERFORMED ENGINE SHUT DOWN IAW ESP. NR 3 PROPELL ER VALVE HOUSING REPLACED IAW LAC JOB CARD HN61135, OPS CHECK GOOD. 2 H 7 4 4T A1SO 20080804 NM 2008 8 4 08FDEA02232 1 20080612 A 5230 AFA83461 SKIN DOUG MD11 MD11F 3023600 NM CARGO DOOR CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 598FE 48597 CENTER CARGO DOOR LOWER AFT CUTOUT FOUND CHAFED. CHAFED MARK AT CENTER CARGO DOOR LOWER AFT CUTOUT REPAIRED AS PER SRM 53-50-00 FIGURE 17 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080804 NM 2008 8 4 08FDEA02233 1 20080612 A 5330 ADA31391 SKIN DOUG MD11 MD11F 3023600 NM BS 1009 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 598FE 48597 FORWARD CARGO DOOR CUTOUT LOWER AFT FOUND WITH CHAFFING. CHAFFED MARK ON FORWARD CARGO DOOR CUTOUT LOWER AFT SKIN EDGE BLENDED OUT AND FOUND WITHIN LIMIT AS PER SRM 53-50-00 FIGURE 17 VOLUME I. MATERIAL REMOVED AT EDGE 0.023 INCH. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080804 NM 2008 8 4 KCSA081283 1 20080615 A 5320 INTERCOSTAL BOEING 747 747122 1384872 NM BS 1700-1720 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 AFT PIT INTERCOSTAL DENTED AT STR-36R BETWEEN BS 1700 AND 1720. (B) 2 L 7 4 4F RT A20WE 20080804 NM 2008 8 4 KCSA081285 1 20080615 A 5311 FRAME BOEING 747 747122 1384872 NM BS 1580 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 AFT PIT FLOORBEAM UPPER CHORD DENTED AT BS 1580, BL-0. (B) 2 L 7 4 4F RT A20WE 20080804 NM 2008 8 4 KCSA081316 1 20080710 A 5414 SKIN BOEING 747 747122 1384872 NM NR 3 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 NR 3 PYLON LT SKIN AT NAC STA-208 HAS TWO CRACKS BELOW DOUBLER. (A) 2 L 7 4 4F RT A20WE 20080804 NM 2008 8 4 KCSA081324 1 20080716 A 5313 STRINGER BOEING 747 747246B 1384864 NM BS 1478 S5L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 FOUND STRINGER 5-L IS CRACKED .750 AT STA-1478. (A) 2 L 7 4 4F RT A20WE 20080804 EU 2008 8 4 08FDEA02319 1 20080618 A 5330 A5397327521000 SKIN AIRBUS 300 A300F4605R 3930327 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 THE AFT CARGO DOOR CUTOUT; EXTERNAL SKIN UPPER AFT CORNER IS GOUGED. REMOVED PANEL 152 YW 7 FASTENERS (5 EACH) TO FOM IA W SRM 51-40-21. BLENDED OUT GOUGE IAW SRM 51-73-10. CHECKED LIMITS IAW SRM 53-17-12 AT INTERVALS A, B, C AND D AND WAS FOUND TO BE WITHIN LIMITS IAW SRM 53-17-12. ALODINED IAW SRM 51-21-10. PRIMED IAW SRM 51-23-01. INSTALLED FASTENERS (5 EACH) AND PANEL 152 YW IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080804 NM 2008 8 4 KSCA081317 1 20080710 A 5310 DOOR FRAME BOEING 747 747246B 1384864 NM BS 2231 S16R CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 R-5 DOOR FRAME HAS A CRACK 1.250 INCH AT STA-2231 BETWEEN STR-16R AND 17R. (A) 2 L 7 4 4F RT A20WE 20080804 EU 2008 8 4 08FDEA02510 1 20080627 A 5511 A5517756220000 STRINGER AIRBUS 310 A310203 3930313 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 423FE 281 4 SQ INCHES OF CORROSION EXIST AT RT HORIZONTAL STAB L/E UPPER FLANGE APPROXIMATELY RIB 5 IN AND AROUND 2 EACH NUTPLAT ES. "PREVIOUS REWORK SURFACE" REMOVED LEVEL 1 CORROSION AND INSTALLED REPAIR STRAP AND SHIM AT RT HORIZONTAL STAB L/E UPPER FLANGE APPROXIMATELY RIB 5 IAW A310-200 SRM 55-11-21 FIG 205/206. 2 L 7 2 4F RT A35EU 20080804 NM 2008 8 4 08FDEA02512 1 20080627 A 5312 6516317199 BULKHEAD BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 NOSE WHEEL WELL AFT WALL (STA 351) SURFACE UNDER DOWN LOCK ACTUATOR MOUNT IS CORRODED. REMOVED CORROSION, NDT, MATERIAL THICKNESS, ORIG. "T" = .072" MAT REMAINING =.065". .007' MAT LOSS. WITHIN LIMITS REF FED EX EA NR 7-5310-113999, TREA TED AND PRIMED, AND APPLIED CIC TO AFFECTED AREA REF SRM 51-10-6, 51-30-1, 51-30-2 PG 1-10. THIS IS CLASSIFIED AS A MIN OR REPAIR, LEVEL 1 CORROSION. 2 L 7 3 4F A3WE 20080804 NM 2008 8 4 KCSA081292 1 20080619 A 5347 SEAT TRACK BOEING 747 747122 1384872 NM BS 350-370 WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 F/E INBOARD SEAT TRACK WORN BETWEEN BS 350 AND 370. (B) 2 L 7 4 4F RT A20WE 20080804 NM 2008 8 4 ARWA20080603 1 20080622 A 7603 THROTTLE DOUG DC10 DC1040F 3023507 NM NR 3 OBSTRUCTED A ARWA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 29 140WE 46920 UPON INITIATION OF TAKEOFF ROLL NR 3 POWER LEVER WOULD NOT ADVANCE BEYOND 128 EPR. RETURNED TO RAMP. OPENED ENGINE FOU ND HYD TEMP C/P WIRE AROUND THROTTLE BELL CRANK BEHIND HYD FILTER MODULE. SECURED WIRE IAW M/M 20-30-07. OPS CHECK THR OTTLE IAW MM 76-11-02 OPERATIONAL CHECK NORMAL. THROTTLE MOVES FULL TRAVEL. (A) 2 L 7 3 4F RT A22WE 20080804 NM 2008 8 4 AALA200801648 1 20080617 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 925AN 29526 DFW - EMERGENCY LIGHT AT SEAT ROW 12 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 12. SYSTEM GROUND CHE CKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A16WE 20080804 NM 2008 8 4 AALA200801672 1 20080619 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080804 2008 8 4 AALA200801463 4 20080602 A 2561 LIFE VEST BOEING 777 777223 1385213 NM COCKPIT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 775AN 29584 LHR - EMERGENCY CREW LIFE VEST MISSING FROM FLIGHT DECK. REPLACED CREW LIFE VEST AT FIRST OFFICERS SEAT STOWAGE. SYSTE M GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080804 EA 2008 8 4 A6WA200840430 1 20080530 A 3240 601R751481 TRANSDUCER CNDAIR CL600 CL6002B19 1900309 EA BRAKE PRESSURE MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 31 436AW 12659 7734 INBOARD BRAKE PRESSURE CAUTION MESSAGE IN FLIGHT. NOTED HYDRAULIC NR 3 SYSTEM QUANTITY AT 90%. CAUTION MESSAGE WAS INT ERMITTENT. REMOVED AND REPLACED PRESSURE TRANSDUCER MT2GD AND CLEANED CONNECTOR P2GD IAW AMM 32-47-00, OPS AND LEAK CHE CK GOOD AT THIS TIME. (A) 2 L 7 2 4F RT A21EA 20080728 SO 2008 7 28 FDK2008F00005 1 20080715 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C 03047 GL EMERGENCY LIGHTS DISCHARGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 GALLEY EMERGENCY LIGHT INOP. MX REPLACED NR 2 EMERGENCY LIGHT BATTERY PACK ASSY, OPS CHECK GOOD. (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080728 EU 2008 7 28 2008UALA03424 1 20080613 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW PRESSURE A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 424UA 506 OXYGEN HIGH PRESSURE INDICATION AMBER ON DOOR-OXY SYSTEM ECAM PAGE - DOOR-OXY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 NM 2008 7 28 2008UALA03419 1 20080617 A 3350 LIGHT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN MISSING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 852UA 1671 EMERGENCY EXIT LIGHTING AT 1L IS MISSING - BROKEN. FWD CLOSET DIVIDER AT DOOR 1L MISSING AISLE LENS CAP AND LAMP. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 NM 2008 7 28 2008UALA03418 1 20080617 A 3510 OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW O2 LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 852UA 1671 CREW O2 LEVEL LOW. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 NM 2008 7 28 2008UALA03410 1 20080615 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT INOP CEILING ROW 12. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 20080728 NM 2008 7 28 NSV2008F00004 1 20080612 A 5220 HANDLE BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA EMERGENCY EXIT UNSECURE A NSVA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 27 200WQ 4200 IN FLIGHT, AT FL220, THERE WAS A MASTER WARNING, FUSELAGE DOOR INDICATION. THE FORWARD EMERGENCY EXIT DOOR INDICATED OP EN. THE F/A CHECKED THAT THE DOOR WAS SECURE BUT HANDLE DID NOT LOCK, TO BE COMPLETELY CLOSED. AC MAINTAINED PRESSURIZ ATION. MASTER WARNING INDICATION WENT OUT ON FINAL. C/A: CLEANED EMERGENCY EXIT PROX SWITCH AND CHECKED CLEARANCE ON P SEU, FOUND TO BE IN SERVICEABLE CONDITION IAW O400 MM 52-71-01-710-801. (K) 2 H 7 2 4T 4 T RT A13NM E00062EN 20080728 EU 2008 7 28 NSV2008F00003 1 20080612 A 3350 8013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS DISCHARGED A NSVA O OTHER O OTHER NR NOT REPORTED 1 EA 27 346CJ 340B346 ALL EMERGENCY LIGHTS ON, POWER SUPPLY DRAINED. (K) 2 L 7 2 4T RT A52EU 20080728 NM 2008 7 28 2008UALA03408 1 20080615 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 SEAT EEL INOP ROW 58 LT. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080728 EU 2008 7 28 2008UALA03378 1 20080615 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 447UA 836 EMERGENCY LIGHT SYSTEM FAILED TEST AFTER SLIDE REPLACEMENT LT EMERGENCY BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 EA 2008 7 28 TRAX200800619 1 20080511 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 907EV 7648 FS 280 CLIP ON I/B SIDE OF RBL 9 IS CRACKED. REMOVED DAMAGED/CRACKED CLIP. INSTALLED NEW CLIP P/N 601R31113-58 IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 20080728 EU 2008 7 28 2008UALA03376 1 20080613 A 3520 O2 GENERATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 496UA 1845 L2 DOOR MASK FOUND GENERATOR PINNED WITH STREAMER AND D LAV MASK WAS TUCKED UNDER STRAP IN BOX. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 2008 7 28 2008UALA03371 4 20080614 A 2330 ENTERTAIN SYS AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN MALFUNCTIONED A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 848UA 1647 ELECTRICAL BURNING SMELL BACK OF THE AIRCRAFT. PAX ENT SYS DOES NOT TURN ON-OFF. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 EA 2008 7 28 TRAX200800636 1 20080514 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 349-477 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE AT RBL 9 FS 349.00 TO FS 477.40. BLENDED DAMAGE ON ON CABIN FLOOR SEAT TRA CKS FS 349 TO FS 477 REMOVED .015" OF MATERIAL. WITHIN LIMITS ALLOWED .035" WORK DONE IAW SRM 53-21-49. 2 L 7 2 4F RT A21EA 20080728 EU 2008 7 28 2008UALA03196 1 20080603 A 2710 4829572 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ELAC FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 425UA 508 ELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN, F-CTL. ELAC NR 1 FAULTY. REPLACED ELAC-1 - OPS TEST OK. LAND CAT III CAP ABILITY TEST OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 EA 2008 7 28 TRAX200800638 1 20080514 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 669-977 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 CABIN SIDE SEAT RAILS HAVE CORROSION DAMAGE AT S15L FS 669.00 TO FS 977.00. BLENDED CORROSION FOUND ON S15L FS 669.00 T O FS 977.00 REMOVED .019" OF MATERIAL WITHIN LIMITS ALLOWED TO REMOVE .035" OF MATERIAL. ALL WORK DONE IAW SRM 53-42-49 AND 53-51-49. 2 L 7 2 4F RT A21EA 20080804 EA 2008 8 4 SIMA200816802 1 20080612 A 2780 SLAT SYSTEM CNDAIR CL600 CL6002C10 1390015 EA SLATS MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION LD LANDING 1 SW 21 507AE 10059 ON FLIGHT 3583 - DURING LANDING THE CREW RECEIVED A SLAT FAIL INDICATION. CREW DECLARED AN EMERGENCY. MDC REFLECTED A MECHANICAL JAM. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOOT SYSTEM IAW FIM 27-81-09. NO DEFECTS NOTED. OPERATION CHE CK GOOD IAW AMM 27-50-00 (NO PARTS REPLACED) AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A21EA 20080804 WP 2008 8 4 ARWA20080601 1 20080604 A 2751 96010206 TRANSMITTER DOUG DC10 DC1010 3022110 WP TE FLAP POSITION FAILED A ARWA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 29 68041 46900 DURING TAXI TAKEOFF CONFIGURATION TEST FAILED. REMOVED AND REPLACED LT OUTBOUND FLAPS POSITION TRANSMITTER IN ACCORDANC E WITH DC10-M/M 27-54-03, OPERATIONAL CHECK FOUND NORMAL IN ACCORDANCE WITH DC10 M/M 27-54-03. (A) 2 L 7 3 4F A22WE 20080804 EA 2008 8 4 A6WA200840482 1 20080406 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 INTERCOSTAL AT FS 484.0, WL 72.0, RBL 36.0 IS CRACKED. INTERCOSTAL REPAIRED IAW REO 601-53-41-059. (A) 2 L 7 2 4F RT A21EA 20080804 NM 2008 8 4 AALA200801476 1 20080602 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 674AN 29424 DFW - EMERGENCY LIGHT AT SEAT 36D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 36D. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080804 NM 2008 8 4 NWAA082906313 1 20080627 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 673US 30268 DURING OVERNIGHT CHECK, FOUND EMERGENCY PATH LIGHTS IN B-ZONE RT SIDE INOP. MAINTENANCE REMOVED AND REPLACED POWER SUPP LY. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 4 4F RT A20WE 20080804 EU 2008 8 4 AALA200801548 1 20080606 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 JFK - EMERGENCY EXIT SIGN LIGHT AT LT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LT NUMBER ONE DO OR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 AALA200801552 1 20080606 A 3350 82400 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 JFK - EMERGENCY EXIT SIGN LIGHT AT RT NR TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT NR TWO DOOR. SY STEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 SIMA200816803 1 20080613 A 2150 7769106 ACM SAAB SF340 340B 7860101 EU RIGHT SEIZED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 307AE 10251 340B307 ON FLIGHT 3227 DURING CLIMB THE CREW DECLARED A EMERGENCY FOR SMOKE SMELL IN COCKPIT AND CABIN. AIRCRAFT RETURNED TO DF W WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RT HAND ACM SEIZED. REMOVED AND REPLACED RT HAND ACM. PERFOR MED OPERATIONAL CHECKS NO SMELL DETECTED IN COCKPIT OR CABIN. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4T RT A52EU 20080804 SO 2008 8 4 SIMA200817503 1 20080618 A 2560 P2070009120 FLASHLIGHT EMB 145 EMB145LR 3260212 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 658AE 145760 ON FLIGHT 3354 CREW REPORTED ELECTRICAL SMELL IN BACK OF CABIN. CREW DECLARED AN EMERGENCY AND LANDED IN MCI. SMELL GO T STRONGER ON THE GROUND. AC TOWED TO GATE, AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT HAND HELD FLAS HLIGHT. OPERATION CHECK GOOD NO SMOKE NOTED. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080804 NM 2008 8 4 AALA200801638 1 20080616 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 377AN 25446 SFO - EXTERNAL EMERGENCY LIGHT AT LT AFT INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LT AFT. SYSTEM GRO UND CHECK NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080804 WP 2008 8 4 AALA200801692 1 20080624 A 3020 320115C ANTI-ICE VALVE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1 INTAKE MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 9628W 53598 708583 DFW - INFLIGHT T1776/24JUN. CREW REPORTED NR ONE ENGINE START VALVE INDICATION AFTER TAKEOFF. CREW SHUT DOWN ENGINE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME EIGHT MINUTES. FOUND OUTBOARD ANTI ICE VALVE NOT CLOSI NG COMPLETELY. REPLACED OUTBOARD ANTI ICE VALVE ON NUMBER ONE ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F 4 F RT A6WE E9NE 20080804 NM 2008 8 4 TSAA0879020 1 20080610 A 7932 39101201001 TRANSMITTER BOEING 737 7372X6C 1384552 NM OIL QTY FAILED A TSAA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 WP 13 841AL 23123 FLIGHT 913 HNL-LIH. DURING TAKEOFF, THE NR 2 ENGINE OIL QUANTITY DECREASED. ELECTED TO ABORT TAKEOFF. INDICATIONS RET URNED TO NORMAL DURING ABORT; ALL ENGINE PARAMETERS WERE NORMAL. MX REMOVED AND REPLACED THE NR 2 ENGINE OIL QUANTITY T RANSMITTER. OPS AND LEAK CHECK OKAY. AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A16WE 20080804 NM 2008 8 4 F3LA200800322 1 20080610 A 5320 D5391550320001 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 REFERENCE NON ROUTINE C044450. DURING C4 S1 C-CHECK INSPECTION NOTED FORWARD CARGO PIT PROFILE FOR LOWER AFT BULKHEAD H AS CORROSION IN NUT PLATE HOLES FROM STRINGER 28 LT TO STRINGER 28 RT. MAINTENANCE REMOVED AND REPLACED PROFILE AT STRI NGER 28 LT TO STRINGER 28 RT IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-44-11 AND SRM 51-42-11. UPON COMPLETION OF T HE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080804 NM 2008 8 4 2008UALA03658 1 20080701 A 5411 SPAR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 NACELLE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NR 1 ENG PYLON TOP, BELOW ACCESS 441DT, RT SIDE, UPPER SPAR WEB CRACKED AT EXISTING REPAIR, CRACK NOT TERMINATED. REMOV ED THE EXISTING REPAIR. FABRICATED AND INSTALLED A DOUBLER, RADIUS FILLER, AND REPAIR FILLER. 2 L 7 2 4F 4 F RT A1NM E24NE 20080904 EA 2008 9 4 QXEA200800704 1 20080709 A 2611 8221310104 DCU CNDAIR CL600 CL6002C10 1390015 EA NR 1 FAILED A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 617QX 12936 10130 PDX- FLIGHT 2621 - AT 120 KNOTS AFT LAV SMOKE WARNING. ABORTED TAKEOFF AND RETURN TO GATE. MAINTENANCE REPLACED NR 1 A ND NR 2 DCU. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A21EA 20080804 NM 2008 8 4 2008UALA03662 1 20080701 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 523 S24L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 EXT FUSELAGE BS 523 STR 24L STATIC DISCHARGE AROUND FASTENER HOLE. *S/D* ACCOMPLISHED TEMP REPAIR AT GSO. REMOVED RIV ET AND ACP HFEC PER NDT MANUAL 51-00-11 PT 6 BY QC 400. INSTALLED BLIND FASTENER IAW SRM 51-40-02 AND MM 53-30-95 PG 60 2. INSP BY QC 382 ON NR D4475Z PER MM 53-30-95 PG 602. CHERRY MAX FASTENERS NEED TO BE RE-CHECKED AT EACH C-CK AND REP LACED WITH SOLID FASTENER AT NEXT HMV. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080728 EU 2008 7 28 2008UALA03194 1 20080602 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 461UA 1266 CREW 02 NEEDS SERVICE. SERVICED CREW O2 TO FULL, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 SWAA083716 1 20080702 A 3350 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 745SW 29491 DURING SCHEDULED MV2 CHECK, FOUND AFT LT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 20080725 NM 2008 7 25 2008UALA03230 1 20080605 A 7500 77328915 CONTROLLER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE ILLUMINATED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 651UA 25389 LEFT ENG BLEED LGT & L ENG HPSOV EICAS MSG DURING DESCENT WITH ENG BLEED SW ON, & ENG RUNNING. FOUND FAULTY HIGH PRESSU RE CONTROLLER. REPLACED HIGH PRESSURE CONTROLLER IAW 36-11-19 OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080725 EA 2008 7 25 SWIA200819826 1 20080629 A 3350 LENS CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 776SK 10241 SERVICE DOOR LOWER EMERGENCY LIGHT LENS COVER IS BROKEN. REPLACED SERVICE DOOR LOWER LIGHT LENS COVER AS REQUIRED. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080725 SO 2008 7 25 SWIA200819828 1 20080703 A 2611 BATTERY EMB 120 EMB120ER 3260203 SO SMOKE DETECTOR WEAK A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 297SW 120327 FLT 5722 - LAVATORY SMOKE DETECTOR SOUNDS INTERMITTENTLY. REPLACED LAV SMOKE DETECTOR BATTERY. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 20080725 SO 2008 7 25 SWIA200819817 1 20080625 A 5210 ROLLER EMB 120 EMB120ER 3260203 SO PAX DOOR OUT OF ADJUST A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 224SW 120294 MAIN CABIN DOOR IS DIFFICULT TO OPEN. INSPECTED AND ADJUSTED FORWARD, UPPER ROLLER IAW AMM 52-11-00. OPS CHECK NORMAL. 2 L 7 2 4T RT A31SO 20080725 EA 2008 7 25 SWIA200819837 1 20080705 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG DOOR OUT OF ADJUST A SWIA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 NM 07 408SW 7055 FLT NR 4042 - RECEIVED A GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE WHEN EXTENDING GEAR. ADJUSTED PROX SENSOR PS 17GA IAW AMM 32-61-05. ALL OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 20080725 SO 2008 7 25 SWIA200819824 1 20080625 A 3397 CONNECTOR EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS LOOSE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 216SW 120285 FLT 3610 - EMERGENCY LIGHTS AT ROW 4 AND 5 ARE INOPERATIVE. SECURED CONNECTOR AND REPLACED LAMPS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080725 EA 2008 7 25 SWIA200819848 1 20080707 A 7830 SWITCH CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER DIRTY A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 417SW 7400 FLT 2522 - RECEIVED 'L REV UNLOCKED' MESSAGE INFLIGHT. CLEANED AND INSPECTED ALL SWITCHES AND PDU ON LEFT REVERSER. OP S CHECK GOOD. 2 L 7 2 4F RT A21EA 20080725 CE 2008 7 25 GUU2008F00005 1 20080705 A 2120 FUEL BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA CABIN ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 81536 UE152 DURING FLIGHT, STRONG ODOR OF FUEL IN CABIN, PASSENGERS COMPLAINED. AUX TANKS SHOW ZERO FUEL ON GUAGES. INSPECTED AUX TANKS FOUND NO FUEL PRESENT, INSPECTED CABIN CLEANED RESIDUAL FUEL CABIN FLOOR. (K) 2 L 7 2 4T 3 T RT A24CE E2NE 20080725 2008 7 25 UHL2008F00002 4 20080601 A 3497 WIRE EMB ERJ170 ERJ170100SE 3260406 NM GE CF34 CF34* 30015 NE NR 2 TAT PROBE BURNED A UHLA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 GL 11 653RW 1786 17000076 ON TAXI OUT FROM THE GATE, CREW RECEIVED AN ADS 2 HEATER FAULT EICAS MESSAGE FOLLOWED BY AN ELECTRICAL SMOKE SMELL IN TH E COCKPIT. AIRCRAFT RETURNED TO GATE. MAINT FOUND WIRES TO THE TAT 2 PROBE BURNED AND PINS MELTED. THE TAT2 SENSOR, C ONNECTOR PLUG AND ADSP4 PROBE WERE REPLACED. TAT 2 PROBE PN 102AW1AF. 2 L 7 2 4F 4 F RT A56NM 20080725 2008 7 25 HNA2008F00000 4 20080629 A 3442 TRANSMITTER DHAV DHC8 DHC8102 2809003 NM WX RADAR SYS FAILED A HNAA J DUMP FUEL O OTHER CR CRUISE 1 EA 07 828EX 35942 392 LOG PAGE 269950-2. RADAR SHOWS FAULT MESSAGES "STAB OFF" AND "IN FIT 6" IN FLIGHT. REMOVED AND REPLACED WEATHER RADAR T RANSMITTER UNIT. (K) 2 H 7 2 4T RT A13NM 20080725 EU 2008 7 25 WRN2008F00002 1 20080616 A 2130 88003A0101 VALVE AIRBUS 300 A300B4203 3930306 EU GROUND VENT STUCK A WRNA O OTHER O OTHER NR NOT REPORTED 1 EA 39 510TA 100 AFTER TAKEOFF, PRESSURIZATION MALFUNCTION OCCURRED. ACCOMPLISHED ABNORMAL PROCEDURES. AC RETURNED TO FIELD. LANDING N ORMAL. MX FOUND GROUND VENT VALVE STUCK CLOSED. MX CLEANED AND RESET GROUND VENTING VALVE IAW 21-31-17, PG 501. OPS CHECKED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (K) 2 L 7 2 4F RT A35EU 20080725 2008 7 25 IXX2008F00006 4 20080710 A 3400 C267072 TRANSDUCER DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE SPEED COMMAND DEFECTIVE A IXXA O OTHER O OTHER NR NOT REPORTED 1 SW 11 821BX 45811 DURING CLIMB OUT, AT 240 KIAS WITH A 9 DEGREE PITCH NOSE UP STICK SHAKER CAME ON STEADY. IT CYCLED ON AND OFF RANDOMLY FOR 15 MINUTES UNTIL LANDING. STALL WARNING TEST SWITCH WAS TOGGLED WITH NO EFFECT. THE CREW LANDED WITH NO FURTHER IN CIDENT. MAINTENANCE REPLACED LIFT SPEED COMMAND TRANSDUCER. OPS CHECK GOOD IAW MM 34-16-0. AC WAS RETURNED TO SERVICE . (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 20080728 2008 7 28 NOC2008F00000 4 20080610 A 3460 COMPUTER BOEING 757 75728A 1384976 NM FLT DIRECTOR MALFUNCTIONED A NOCA O OTHER O OTHER NR NOT REPORTED 1 EA 15 754NA 29381 AIR TURN BACK, DUE TO FMS PROBLEM - WAS GIVEN AN ALTITUDE OF FL 280, ALTITUDE SELECT, NR 2 FLIGHT DIRECTOR PROBLEM, IT EM REMAINS OPEN. (K) 2 L 7 2 4F RT A2NM 20080804 NM 2008 8 4 2008UALA03664 1 20080701 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1440 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 AFT PIT FRAME DENTED STA 1440, STR 26L. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. CUT OUT DAMAGE AND NDT INSP PER 51-00 -19, DAMAGE REMOVED. INSTALLED DOUBLER REPAIR PER SRM 53-0 0-01, REPAIR 5 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E17NE 20080804 NE 2008 8 4 2008UALA03667 2 20080701 A 7261 ENGINE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 1 OIL CONSUMPTION A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 676UA 30028 724365 NR 1 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT. 2 L 7 2 4F 4 F RT A1NM E24NE 20080804 NE 2008 8 4 2008UALA03670 2 20080702 A 7230 BLADE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE HPC DAMAGED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 WP 29 128UA 30023 727947 ENGINE EGT WENT UP RAPIDLY, ENGINE SHUT DOWN. RTFL. ENGINE WAS REPLACED AT LAX PRIOR TO FURTHER FLIGHT. SHOP TEARDOWN REVEALED THAT FIVE HP COMPRESSOR STAGE-6 BLADES HAD LEADING EDGE FOD. ONE ADDITIONAL STAGE-6 BLADE HAD A SMALL 'SHARK BI TE' FROM ITS TRAILING EDGE NEAR THE TIP. THE REMAINING COMPRESSOR STAGES HAD SEVERE IMPACT DAMAGE. THERE WAS NO DAMAGE ON STAGE-5. ROOT CAUSE IS ATTRIBUTED TO FOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20080804 NM 2008 8 4 2008UALA03686 1 20080702 A 5497 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 NACELLE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NR 1 ENG PYLON HYD BAY WIRE AT CONNECTOR D00 036 PIN 2 (SWITCH S310) IS HEAT DAMAGED. FOUND WIRE AT CONNECTOR D00036 PI N 2 (SWITCH S310) IS HEAT DAMAGE. REPLACED WIRE AT D00036P PER BSWPM 20-61-11 AND WDM 29-32-11. OPS CHECKS GOOD 2 L 7 2 4F 4 F RT A1NM E24NE 20080804 NM 2008 8 4 2008UALA03687 1 20080702 A 5497 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 NACELLE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 57UA 27112 NR 1 ENG PYLON HYD BAY CONNECTOR D02118 HAS DAMAGED SOCKET. REPLACED SOCKET AT CONNECT OR D02118P PER BSWPM 20-60-09 AN D WDM 78-34-11. OPS CHECKS GOOD ON NR 37006, NR 36897. 2 L 7 2 4F 4 F RT A1NM E24NE 20080730 NM 2008 7 30 SWAA083951 1 20080716 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500A S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083950 1 20080716 A 5311 6546541 FRAME BOEING 737 7373H4 1384600 NM BS 663 S1-2R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 1 AND STR 2R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083810 1 20080709 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM BS 750 S18L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083977 1 20080717 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM BS 727B S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080730 NM 2008 7 30 SWAA083976 1 20080717 A 5311 6546538 FRAME BOEING 737 7373H4 1384600 NM BS 597 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080731 SO 2008 7 31 C2XA08SH084 1 20080611 A 5330 14535011005 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 SHV - DURING C-CHECK IT WAS FOUND THAT THE LT REAR FUSELAGE SKIN WAS DENTED AT FRAME 65/STRINGER 16L, DIRECTLY BELOW THE FORWARD LOWER CORNER OF THE CARGO DOOR CUTOUT. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 51-40-02. THE A CFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080731 EA 2008 7 31 COM2008F00001 1 20080616 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 915CA 7013 RECEIVED FLAP FAIL MESSAGE ON APPROACH. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH SI-2-2710001 FLAP C AUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION. FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. (S) 2 L 7 2 4F RT A21EA 20080731 SO 2008 7 31 CHQA200800107 1 20080607 A 3260 8005701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL NLG INOPERATIVE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 578RP 14500865 CAE311697 FLIGHT 6351, BNA TO MCO. JUST AFTER TAKEOFF, THE LANDING GEAR WAS RETRACTED AND A LOUD NOISE AND VIBRATION CAME FROM TH E NOSE OF THE ACFT. THE GEAR INDICATED 3 UP AND LOCKED ON EICAS. THE GEAR WAS RECYCLED AND THE CONDITION CONTINUED. T HE FLIGHT LANDED IN BNA WITHOUT INCIDENT. MAINTENANCE SWAPPED THE NOSE LANDING GEAR DOOR PROX SWITCH WITH THE NR 2 UPLO CK PROXIMITY SWITCH AND THE ACFT WAS TEST FLOWN. THE NOSE GEAR DOORS OPERATED NORMALLY AND THE SWAPPED SWITCH WAS LATER REPLACED. (S) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080731 NE 2008 7 31 C8GA20080016 2 20080603 A 7230 COMPRESSOR BOEING 727 727227 1384078 NM PWA JT8 JT8D17R 52049 NE NR 3 ENGINE STALLED A C8GA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 SO 29 89427 70565 3651 21365 FLT 0001 FROM MIA-PTY. DURING APPROACH TO PTY THE NR 3 ENG COMPRESSOR STALLED AND ENG FLAMED OUT. THE ACFT LANDED WITH OUT INCIDENT. POST FLIGHT INSPECTION REVEALED N1 UNMOVEABLE. REMOVED AND REPLACED THE NR 3 ENGINE. OPS AND LEAK CHEC KS GOOD. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE. (S) 2 L 7 3 4F 4 F A3WE E2EA 20080731 NM 2008 7 31 SWAA083999 1 20080717 A 5310 6546817 CREASE BEAM BOEING 737 7375H4 138449D NM BS 434 S17L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 434, STR 17L. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 20080728 EU 2008 7 28 RMX2008F00002 1 20080717 A 5302 1053040212 FITTING UROCOP 117 BK117C1EURO 8680975 EU TMECA ARRIEL ARRIEL1 60030 NE TAILBOOM CRACKED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 317MC 7505 DURING A SCHEDULED INSPECTION, THE TAIL ROTOR GEARBOX CASTING PN 105-30402.12 WAS DISCOVERED CRACKED. REMOVED AND REPL ACED THE GEARBOX WITH A NEW CASTING PN 105-30402.12 1 G 7 2 3U 3 U H13EU E19EU 20080728 CE 2008 7 28 QRE2008F00000 1 20080710 A 7603 3008787 ROD END CESSNA 425 425 2076018 CE PWA PT6 PT6A135 52043 NE THROTTLE BINDING E QREA O OTHER O OTHER NR NOT REPORTED 1 EA 63 425WD 653 4250130 THE PILOT MENTIONED UPON LENDING THE LT ENGINE NG DID NOT GO ALL THE WAY BACK TO IDLE SPEED, BUT STAYED AT 80 PERCENT. UPON EXAMINATION OF THE FUEL CONTROL LINKAGE, IT WAS NOTED THAT THE FUEL CONTROL ARM WAS NOT RESTING ON THE IDLE STOP, B UT WAS UP ABOUT 1 INCH. USING LIGHT HAND PRESSURE THE LINKAGE WAS PUSHED TO THE STOP. THE FUEL CONTROL ARM AFT ROD END WAS FOUND TO BE BOUND AND CAUSING THE PROBLEM. INSPECTION OF THE ROD END DISCLOSED NO OBVIOUS DEFECTS. REPLACED ROD E ND WITH A NEW UNIT AND OPS SHOW NORMAL. (K) 1 L 7 2 3T 4 T RT A7CE E4EA 20080728 EU 2008 7 28 UPS08152597 1 20080619 A 5753 SKIN AIRBUS A300 A300F4622R 3930360 EU T/E FLAP CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 152UP 0835 INSPECTION TYPE:5YR 2EA CHAFE MARKS ON UPPER SURFACE OF RT INBOARD FLAP AT RIB 18 & 19 STRINGER 2.2. 2EA AREAS FOUND OUT OF LIMITS ON NRC 196779. CUT OUT 2EA DAMAGED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLER IAW A300 SRM 57-50-00 FIG 205. 2 L 7 2 4F RT A35EU 20080728 NM 2008 7 28 MWE2008F00017 1 20080703 A 7830 715K9004507 FRAME BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE THRUST REVERSER CRACKED A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 918ME 55180 RT THRUST REVERSER LOWER Z-FRAME, AT STA 26.666 HAS A CRACKED REPAIR AT THE LT END. FABRICATED AND INSTALLED DOUBLER. (K) 2 L 7 2 4F 4 F TR A6WE E00061EN 20080728 EA 2008 7 28 TRAX200800783 1 20080612 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 752EV 10166 RT AFT GALLEY HAS SEVERAL INOP EMERGENCY LIGHT BULBS. REMOVED AND REPLACED SEVERAL LIGHT BULBS IN RT AFT GALLEY FLOOR L EVEL EMERGENCY FLOOD LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800854 1 20080630 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 409-559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 NUMEROUS AREAS OF MINOR CORROSION ON PRESSURE FLOOR SILL FROM FS 409.0+128 TO FS 559.0, RBL 36.0 TO RBL 47.0 WL 73.0. REMOVED MINOR CORROSION FROM PRESSURE FLOOR SILL FROM FS 409.0+128 TO FS 559.0, RBL 36.0 TO RBL 47.0, WL 73.0 IAW SRM 51 -21-06. RUBATEX TAPE REQUIRE INSTALLATION. INSTALLED RUBATEX TAPE ON PRESSURE FLOOR SILL FROM FS 409.0 TO FS 559.0, RB L 36.0 TO RBL 47.0, WL 73.0 IAW AMM 53-01-01-400-802. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800639 1 20080514 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 379-669 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 CABIN SIDE SEAT RAILS HAVE CORROSION DAMAGE AT S15R FS 379.00 TO FS 669.40. BLENDED CORROSION FOUND ON S15R FS 379 TO F S 669.40 REMOVED .015" OF MATERIAL WITHIN LIMITS ALLOWED TO REMOVE .035" OF MATERIAL. ALL WORK DONE IAW SRM 53-31-49. 2 L 7 2 4F RT A21EA 20080728 EU 2008 7 28 2008UALA03181 1 20080604 A 3520 SOLENOID AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 445UA 826 CABIN OXYGEN FAILED AT 3 DEF, 6 ABC, 8 DEF, 10 DEF, 10 ABC, 13 DEF, 19 DEF, 23 DEF, AND AFT ATTENNDANT SEAT. LATCH SOLE NOIDS FAULTY AT EACH LOCATION. REPLACED LATCH SOLENOIDS AND OP CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 2008 7 28 2008UALA03177 4 20080603 A 2350 MICROPHONE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT SHORTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 431UA 571 CAPTAIN'S OXYGEN MASK MICROPHONE IS INOPERATIVE. CREW COMMENTS: MIC IS INTERMITTANT. SHORT IN MIC/MASK. REPLACED CAP T O2 MASK ASSY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 EA 2008 7 28 TRAX200800640 1 20080514 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 379-669 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 CABIN SIDE SEAT RAILS HAVE CORROSION DAMAGE AT S15L FS 379.00 TO FS 669.40. BLENDED DAMAGE FOUND ON S15L FS 379 TO FS 6 69.40 REMOVED .024" OF MATERIAL WITHIN LIMITS ALLOWED TO REMOVE .035". ALL WORK DONE IAW SRM 53-21-49 AND 53-31-49. 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 2008UALA03487 1 20080619 A 5320 FLOOR SUPPORT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 MAIN CABIN FLOOR SUPPORT ANGLE -SPLASH GUARD- HAS CORROSION AT BS 285 AND RBL 83. 2 L 7 2 4F 4 F RT A1NM E24NE 20080728 EA 2008 7 28 TRAX200800643 1 20080514 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 477-693 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE AT LBL 9 FS 477.40 TO FS 693.00. BLENDED CORROSION ON CABIN FLOR SEAT RAIL S LBL 9 FS 477 TO FS 693 REMOVED .021" OF MATERIAL WITHIN LIMITS ALLOWED TO REMOVE .035" OF MATERIAL. ALL WORK DONE IAW SRM 53-31-49. 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 WXOA070213 1 20080618 A 3350 20131A BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 404NV 49765 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL CHARGED THE EMERGENCY POWER SUPPLY BATTERY PACKS. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A6WE 20080728 EA 2008 7 28 A6WA200840481 1 20080406 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 INTERCOSTAL FS 484.0 WL 72.0, LBL 27.0 ANGLE IS CRACKED. CORRECTIVE ACTION IN PROGRESS. (A) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800613 1 20080508 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 928EV 8006 RT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED IN OUTBOARD RADIUS. RESOLVED ON W/O 90038 TASKCARD N/R 00181. REPAIRED RT FS 621.00 FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117 REV C STEPS 1-7. REQUIRES TOP COAT. APPLIED TOP COAT AS NEEDED IA W CRJ 200 SRM 51-25-01. PRESSURE CHECK DUE. PERFORMED LEAK CHECK OF RT 621.00 FLOOR SUPPORT ANGLE IAW CRJ AMM TASK 21- 32-00-863-801. NO LEAKS NOTED AT THIS TIME. C/W ASA REO 601R-53-61-117. [SUPPLEMENTAL SDR CLOSED 6/24/08] (A) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 AALA200801310 1 20080509 A 5315 146T12105 FLOORBEAM BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 338AA 22335 AFT CARGO FLOOR BEAM J CHANNEL INNER CHORD AT STATION 1285 HAS CORROSION REMOVAL ON UPPER HORIZONTAL FLANGE. MATERIAL R EMAINING IS BEYOND SRM LIMITS. REPAIRED IN ACCORDANCE WITH MRD 767 3196. CHORD SHOULD BE REPLACED BY THE NEXT C CHECK FOLLOWING 05 09 2008. (A) 2 L 7 2 4F RT A1NM 20080728 WP 2008 7 28 AALA200801311 1 20080512 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL BATTERY PACK AT OVERHEAD SEAT 29DEF FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK AT OVERHEAD SEAT 29DEF. SYSTEM G ROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F A6WE 20080728 EA 2008 7 28 TRAX200800678 1 20080521 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR NO TEST A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 924EV 7830 EMERGENCY HANDLE OF THE PAX DOOR FAILS FORCE TEST. LUBED PAX DOOR IAW AMM 12-20-52-640-810. PERFORMED FUNCTIONAL TEST OF PAX DOOR INNER HANDLE TEST GOOD AT THIS TIME IAW AMM 52-11-00-720-802. 2 L 7 2 4F RT A21EA 20080728 WP 2008 7 28 AALA200801312 1 20080512 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7520A 49897 TUL BATTERY PACK AT OVERHEAD SEAT 25DEF FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK AT OVERHEAD SEAT 25DEF. SYSTEM G ROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F A6WE 20080728 NM 2008 7 28 AALA200801313 1 20080515 A 3350 105630 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 393AN 29430 LAX EMERGENCY LIGHT AT FORWARD SEAT 2AB INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FORWARD SEAT 2AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A1NM 20080728 EA 2008 7 28 TRAX200800620 1 20080511 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 907EV 7648 FS 280 FLOOR SUPPORT STRUCTURE IS CRACKED O/B OF LBL 9 AT MLG MANUAL RELEASE PULLEY BRACKET. CUT AWAY CRACKED SECTION O F FLOOR ANGLE IAW REO 601R-53-11-138. COMPLIED WITH REO 601R-53-11-138. PERFORMED LPI OF FS 280 ANGLE LBL 9 REPAIR IAW NDTM 51-20-08. NO INDICATIONS NOTED AT THIS TIME. INSTALLED REPAIR ANGLE AT FS 280 LBL 9 IAW REO 601R-53-11-138. APPLI ED PAINT TO REPAIR IAW SRM 51-25-01. FABRICATED REPAIR ANGLE THAT WAS INSTALLED ON STEP 3 USING 7075-0 .050 PO 83061/1. HEAT TREATED PART TO 7075-T62 AS REQUIRED IAW REO 601R-53-11-138 STEPS 3-5 AND AMS2771 FOR HEAT TREAT. 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 AALA200801322 1 20080515 A 2612 FIRE WARNING BOEING 757 757223 1384957 NM NR 2 ENGINE MALFUNCTIONED A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 187AN 32381 VVI INFLIGHT T9222/15MAY MIA TO LPB. NR 2 ENGINE FIRE WARNING OVERHEAT EICAS MESSAGE AND ASSOCIATED LIGHTS AND BELLS. LANDED VVI WITHOUT INCIDENT. NO EVIDENCE OF FIRE. PERFORMED ADJUSTMENT AND TEST OF NR 2 ENGINE FIRE WARNING SYSTEM. S YSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A2NM 20080728 EA 2008 7 28 TRAX200800651 1 20080516 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 907EV 7648 PAX DOOR EXTERNAL HANDLE IS CRACKED. SB 601R-51-119 REV A, DOORS, PASSENGER DOOR, REPLACEMENT OF THE OUTER HANDLE INCOR PORATED. PAINTED PAX DOOR HANDLE IAW 51-25-01. 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 AALA200801318 1 20080515 A 3350 OL3071BPEGPL LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 MIA EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NORM AL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 EA 2008 7 28 TRAX200800668 1 20080519 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 929EV 8007 PAX DOOR OUTER HANDLE IS CRACKED. REMOVED CRACKED HANDLE INSTALLED NEW HANDLE KIT 601R52-119K1 IAW AMM 52-11-03-400-802 . PAX DOOR HANDLE REQUIRES FUNCTIONAL TEST. PERFORMED FUNCTIONAL TEST OF THE PAX DOOR OUTER HANDLE IAW AMM -52-11-03-72 0-802. FUNCTIONAL TEST GOOD. REMOVED STEP 832DT TO ACCESS REPAIR AND REINSTALLED SAME SERVICEABLE STEP IAW CRJ 200 AMM 52-11-04-400-805. OK TO INSTALL. ASA RII COMPLIED WITH. 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 KCSA081314 1 20080707 A 5330 SKIN BOEING 747 747122 1384872 NM BS 735-745 S34L CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STA 735 TO STA 745 AT S34L HAS EVIDENCE OF CORROSION UNDER LAP SKIN AND AROUND FASTENERS (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 KCSA081315 1 20080707 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 705 S33L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 BS 705, S33L CRACKED .5 INCHES (B) 2 L 7 4 4F RT A20WE 20080728 CE 2008 7 28 DXTA200803100 1 20080606 A 2721 TRIM SYSTEM CESSNA 680 680CE 2076811 CE RUDDER INOPERATIVE E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 307QS 6800130 RUDDER TRIM INOP. CANNOT ADJUST TRIM. (B) 2 L 7 2 4F RC T00012WI 20080728 NM 2008 7 28 KCS2008F00000 1 20080617 A 2120 UNKNOWN BOEING 747 747209B 138489B NM CABIN ODOR A KCSA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 715CK 22447 NR 1 PACK EMITTING A SULFUR ODOR IN COCKPIT DURING FLIGHT. NO FIRM CAUSE FOR PROBLEM FOUND. 2 L 7 4 4F RT A20WE 20080728 SO 2008 7 28 MAS2008F00000 1 20080617 A 3350 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 859MJ 145769 FDM 6172 JFK-ALB. LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MX REPLACED INVERTER NR 4 AND OPS CHECKED. (B) 2 L 7 2 4T RT T00011AT 20080728 SO 2008 7 28 MAS2008F00007 1 20080606 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 9962 MCO-RIC. RT WING EMERGENCY LIGHT INOP. MX RESECURED THE CONNECTOR, OPS CHECK GOOD. (B) 2 L 7 2 4T RT T00011AT 20080728 EA 2008 7 28 TRAX200800863 1 20080701 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 REAR PRESSURE BULKHEAD WEB THAT SURROUND THE LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX .2" IN LENGTH 1005 FULL SCREEN HEIGHT FAILED NDT INSP. (B) REPAIR PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETED AND THE REPAIR C/W TH E REQUIREMENTS OF EC/TC AND REO 601R-53-61-1230 REV D. RII C/W 53000002. (A) 2 L 7 2 4F RT A21EA 20080728 WP 2008 7 28 MAS2008F00009 1 20080617 A 2910 CONTROL VALVE DOUG DC8 DC871F 302199D WP HYD SYSTEM LEAKING A MASA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 820BX 46065 ON CLIMBOUT FROM KPHL HYDRAULIC PRESSURE WENT TO ZERO, HYDRAULIC FLUID LEVEL TO STANDPIPE, THE CREW DECLARED EMERGENCY A ND LANDED INTO KTOL WITHOUT INCIDENT. MAINTENANCE INSPECTED HYDRAULIC SYSTEM AND FOUND SLOT CONTROL VALVE LEAKING, MAINT ENANCE REPLACED SLOT CONTROL VALVE AND SERVICED HYDRAULIC SYSTEM. OPERATIONAL CHECK GOOD IAW DACO DC-8 MM 27-80-4. AIRC RAFT RETURNED TO SERVICE. (B) 2 L 7 4 4F RT 4A25 20080728 NM 2008 7 28 AALA200801323 1 20080516 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 342AN 33081 DFW EMERGENCY LIGHT AT SEAT 27H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 27H. SYSTEM GROUND CHECKED NORM AL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A1NM 20080728 EA 2008 7 28 MASA200800460 1 20080610 A 3350 LS6006182 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH FLT 2818 PHX-DSM. EMERGENCY FLOOR LIGHT STRIP AT ROW 12 INOP AND PULLED UP FROM THE RETAINER. MX REPLACED THE LIGHT STRIP ASSEMBLY. (B) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 AALA200801324 1 20080516 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 774AN 29581 JFK EMERGENCY LIGHT AT CREW REST LT NUMBER THREE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT CREW RE ST LT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 NM 2008 7 28 AALA200801325 1 20080516 A 3350 OL3071BPEGPL LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 770AN 29578 MIA EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NORM AL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 NM 2008 7 28 AALA200801333 1 20080517 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 674AN 29424 MIA EMERGENCY LIGHT AT SEAT ROW 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 26. SYSTEM GROUN D CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A2NM 20080728 NM 2008 7 28 AALA200801334 1 20080518 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 775AN 29584 DFW EMERGENCY LIGHT AT RT HAND FORWARD GALLEY CART AREA BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RT HAND FORWARD GALLEY CART AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 NM 2008 7 28 AALA200801335 1 20080518 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 649AA 24607 DFW EMERGENCY LIGHT AT AFT SEAT 17D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT AFT SEAT 17D. SYSTEM G ROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A2NM 20080728 NM 2008 7 28 AALA200801346 1 20080519 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 760AN 31477 DFW EMERGENCY LIGHT AT LT NUMBER ONE CLOSET DOOR DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LT NUMBER ONE CLOSET DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 EA 2008 7 28 TRAX200800894 1 20080707 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 850AS 7355 EXTERIOR AFT EMERGENCY LIGHT INOP. REPLACED AFT EMERGENCY LIGHT ON FUSELAGE IAW SRM 33-51-21. OPS CK GOOD. (B) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800628 1 20080514 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 LT 280 WED CORRODED---[OPEN] (B) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 MASA200800461 1 20080611 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 518LR 12400 10259 ASH FLT 7302 IAD-JAX. ALL EMERGENCY LIGHTS WILL NOT ILLUMINATE. MX R&R BATTERIES. (B) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 KCSA081287 1 20080615 A 5311 FRAME BOEING 747 747122 1384872 NM BS 1760 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 AFT PIT FLOORBEAM UPPER CHORD DENTED AT B.S.1760, RBL-23 (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 AALA200801347 1 20080519 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 760AN 31477 DFW EMERGENCY LIGHT AT RT NUMBER ONE DOOR GALLEY COMPARTMENT AREA DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RT NUMBER ONE DOOR GALLEY COMPARTMENT AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 NM 2008 7 28 AALA200801352 1 20080519 A 3350 LENS BOEING 767 767323 1385205 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 385AM 27059 DFW EMERGENCY LIGHT AT SEAT 21B MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21B. SYSTEM GROUND CHECKED NOR MAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A1NM 20080731 NM 2008 7 31 WRLA2008053 1 20080617 A 2530 COFFEEMAKER DOUG MD11 MD11 3023602 NM GALLEY ODOR A WRLA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 11 273WA 48519 AFT GALLEY COFFEEMAKER 5 OR 8 HAS STRONG ELECTRICAL SMELL. BOTH SHUT OFF IN FLIGHT. FOUND COFFEEMAKER NR 8 POPPED. NR 5 COFFEEMAKER OPS CHECK OK PER MM 25-32-15. CHECKED OPERATION, OPERATES NORMAL NEF ITEM N25JU1808-721 CLEARED. (S) 2 L 7 3 4F RT A22WE 20080731 SO 2008 7 31 C2XA08IA138 1 20080608 A 3260 8005701 PROXIMITY SENSOR EMB 145 EMB145XR 3260214 SO NLG INOPERATIVE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 31131 145705 DGO - FLIGHT 2036, DURING CLIMB OUT THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS, AND THE LANDING GEAR WOULD NOT RETRACT. THE ACFT RETURNED TO DGO WEHRE IT LANDED WITHOUT INCIDENT. THE ACFT WAS FERRIED TO IAH WHERE M AINTENANCE INSPECTED THE ACFT, AND REMOVED AND REPLACED THE NLG WEIGHT ON WHEELS PROXIMITY SENSOR. OPERATIONALLY CHECKE D WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080731 EA 2008 7 31 COMA0860285 1 20080612 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 927CA 7031 RECEIVED FLAP FAIL MESSAGE AT CRUISE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH SI-2-27I0001 FLAP CAU TION MESSAGE "FIRST EVENT" MAINTENANCE ACTION. FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES. (S) 2 L 7 2 4F RT A21EA 20080731 EA 2008 7 31 COMA0860297 1 20080622 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 7117 DURING HMV NR 6 INSPECTION, NDT INSPECTION FOUND A CRACK ON THE FS 559 LBL 18, LOWER CAP ANGLE. CUT OUT DAMAGE SECTION OF CAP ANGLE AND SPLICED IN NEW SECTION WITH DOUBLERS IN ACCORDANCE WITH REO 601R 53-41-260. (S) 2 L 7 2 4F RT A21EA 20080731 NM 2008 7 31 2008UALA03617 1 20080629 A 3510 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CAPTAIN'S DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 OXYGEN MASK DEFECTIIVE AT1 (1=CAPT,2=1ST OFF,3=1ST OBS). CREW COMMENTS: CAPT O2 MASK EMERGENCY PRESS TO TEST BUTTON ST ICKS ON. DIRT ACCUMULATION IN SWITCH. REPLACED O2 MASK, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080731 NM 2008 7 31 CALA0800675 1 20080707 A 5311 6546536 FRAME BOEING 737 737524 1384721 NM BS 559 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 LEFT STATION 559 FRAME CRACKED AT AIR CONDTIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. INSTALLED REPAIR ANGL ES STATION 559 LEFTHAND BRACKET BETWEEN S-8 AND S-9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 SWAA083775 1 20080709 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727B S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 NSV2008F00006 1 20080713 A 3350 LIGHT BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY ILLUMINATED A NSVA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 EA 27 200WQ 4200 AC DIVERTED FOR PRECAUTIONARY LANDING DUE TO RT FWD EMERGENCY EXIT LIGHT ILLUMINATED. DOOR OPS CHECKED GOOD, WO NR 0392 920. (K) 2 H 7 2 4T RT A13NM 20080731 EU 2008 7 31 NSV2008F00008 1 20080712 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A NSVA O OTHER O OTHER NR NOT REPORTED 1 EA 27 369PX 340B295 EMERGENCY LIGHTS 481 N, 66LN, 31LN, AND 61LN INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY 21LN, OPS C HECK GOOD. (K) 2 L 7 2 4T RT A52EU 20080731 CE 2008 7 31 CIE2008F00002 1 20080713 A 3250 STEERING SYS LEAR 55 55LEAR 5170702 CE GARRTT TFE731 TFE731* 01518 WP NLG MALFUNCTIONED E CIEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 03 717EB 016 AIRCRAFT WOULD NOT TURN ON THE GROUND VIA NOSEWHEEL STEERING OR VIA APPLICATION OF ASYMMETRIC TRUST AND BRAKE AFTER LAND ING. AC WAS STOPPED ON THE RUNWAY AFTER ROLL OUT AND WAS UNABLE TO ENGAGE THE NOSE WHEEL STEERING. AC WAS SUBSEQUENTLY TOWED FROM THE RUNWAY TO THE FBO. MAINT WAS DISPATCHED AND AN OPERATIONAL TEST OF NOSE WHEEL STEERING IAW MM 32-50-00, PAGE 201. OPERATIONAL CHECK OF NOSE WHEEL STEERING IS GOOD. CHECKED SECURITY OF ELECTRICAL CONNECTORS TO STEERING SYST EM COMPONENTS. NO DEFECTS NOTED. CANNOT DUPLICATE DISCREPANCY. SERVICED NOSE STRUT AFTER STEERING OPERATIONAL CHECK WI TH NITROGEN TO PROPER DIMENSION IAW MM SECTION 12-10-00. AC CONTINUED ON WITHOUT FURTHER AND LANDED WITH NO PROBLEMS. 2 L 7 2 4F 4 F A10CE E6WE 20080801 NM 2008 8 1 08FDEA02461 1 20080625 A 5330 53FX130111 SKIN BOEING 727 727227 1384078 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 DENT IN LEFT FWD FUSELAGE STA 545 ABOVE STR 24L (RVSM AREA). REPAIRED DENT IAW EA 7-5330-116991. 2 L 7 3 4F A3WE 20080804 NM 2008 8 4 08FDEA02581 1 20080630 A 5311 65163253 FRAME BOEING 727 727225 1384077 NM BS 804 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 MULTIPLE UNFILLED HOLES ON FRAME 804 BETWEEN 4L AND STR 5L INSTALLED DOUBLER ON FRAME REF SRM 51-40-3, THIS IS CLASSIFIE D AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080804 SO 2008 8 4 LR7A08088 1 20080701 A 5210 LONGERON LKHEED 382 382G 526414U SO PAX DOOR CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 636 4763 DURING SCHEDULED B-2 CHECK, PER JOB CARD HB5305, FOUND CREW DOOR LONGERON CRACKED THRU RIVET HOLE ADJACENT TO MICROSWITC H AT FS 241 WL195. REPAIR IAW SMP583 FIG 51-140-19. 2 H 7 4 4T A1SO 20080804 NM 2008 8 4 08FDEA02574 1 20080630 A 5347 658624533 SEAT TRACK BOEING 727 727225 1384077 NM BS 910-914 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 CABIN SEAT TRACK AT STA 910 - STA 914, LBL 31, WL 208 IS CORRODED REMOVED SEAT TRACK, VERIFIY MATERIAL ID AS BAC1520-792 7178T651 ATAG NR A20604, P/O 1039090. FABRICATED SEAT TRACK, ALODINED, PRIMED AND INSTALLED IAW:BAC1520-792 REV B AND IPB 53-42-00 AND SRM 51-30-05. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080804 EU 2008 8 4 08FDEA02508 1 20080626 A 5320 GUSSET AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 A GUSSET IS CRACKED AT STRINGER 26L AFT OF FRAME 79. 2 L 7 2 4F RT A35EU 20080804 NM 2008 8 4 08FDEA02572 1 20080630 A 5320 69191222 CHANNEL BOEING 727 727225 1384077 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 NLG W/W AFT BULKHEAD STA 351.2, CRACK ON DOWN LOCK ACTUATOR MOUNT U-CHANNEL. COMING OUT OF UPPER LEFT FASTENER HOLE. R EMOVED DOWN LOCK ACTUATOR MOUNT U-CHANNEL, DRILLED UP NEW CHANNEL P/N 69-19122-2, AND INSTALLED. REF DWG 69-18194 AND S RM 51-30-02 PG 1-10 THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080804 EU 2008 8 4 08FDEA02478 1 20080625 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN DECK FLOOR SEAT TRACK HAS CORROSION; C76-C77; RBL 17 (IN 3 SPOTS) REMOVED CORROSION AND CHECKED LIMITS IAW A300-60 0 SRM 53-10-16; FIG 102. FOUND SEAT TRACK TO BE OUT OF LIMITS. REMOVED OLS SEAT TRACK BETWEEN C76 AND C77 AND INSTALLE D A NEW SEAT TRACK IAW A300-600 SRM 51-41-21. MATERIAL ID FOR THE NEW SEAT TRACK IS A5327400500053, PO 617932.1 IAW A30 0-600 SRM 53-18-16. FABRICATED A NEW SEAT TRACK IAW AIRBUS DWG A53279206218. ALODINED; PRIMED AND PAINTED IAW A300-600 AMM 51-75-10-8. PART MARKED NEW SEAT TRACK IAW FEDEX GMM 7-0-1001. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02494 1 20080626 A 5320 A53978036202 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION AT LOWER BULK CARGO DOOR STOP FITTING C 67 AND C69. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51- 72-10. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02798 1 20080709 A 5321 B5327031800400 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN DECK FLOORBOARD 261 UF IS BROKEN. MAT ID N 407 35039-003, PO 613022.1. FABBED A NEW PANEL IAW FEDEX SRZ 25-005; R EV F. PART MARKED IAW FEDEX GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080804 EA 2008 8 4 A6WA200840483 1 20080406 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 INTERCOSTAL AT FS 484.0, WL 72.0, LBL 36 IN CRACKED. INTERCOSTAL REPAIRED IAW REO 601R-53-41-059. (A) 2 L 7 2 4F RT A21EA 20080804 EU 2008 8 4 NWAA082753253 1 20080615 A 3350 EPSU AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 353NW 786 EMERGENCY ESCAPE LIGHTING EPSU 13WL INOP. REPLACED EPSU 13WL, CHECKS OK. (A) 2 L 7 2 4F RT A28NM 20080804 NM 2008 8 4 AALA200801658 1 20080618 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 673AN 29423 DFW - EMERGENCY LIGHT AT RT AFT LAVATORY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RT AFT LAVATORY. SYSTEM GR OUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080804 WP 2008 8 4 NWAA082579867 1 20080608 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 776NC 47786 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN LIGHTS FOR THE FWD OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (A) 2 L 7 2 4F RT A6WE 20080804 SO 2008 8 4 SIMA200816404 1 20080606 A 3320 B0C900022 BALLAST EMB 135 EMB135LR 3260305 SO CABIN LIGHTS ODOR A SIMA O OTHER B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 SW 21 703MR 145173 ON FLIGHT 4772 CREW REPORTED THE SMELL OF BURNING WIRES COMING FROM RT SIDE PANEL LIGHTS AT ROWS 9 AND 10. SMELL GOES A WAY WHEN LIGHT ARE TURNED OFF. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RT SIDE WALL BALLAST SEAT 10BC IAW EMB AMM 33-21-04, LIGHTS OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080804 WP 2008 8 4 WXOA070205 1 20080528 A 3350 20131A BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 879GA 53486 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERTIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. ( A) 2 L 7 2 4F RT A6WE 20080804 NM 2008 8 4 2008UALA03665 1 20080701 A 5210 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 R2 DOOR NEEDS REPAIR DOUBLER AT UPPER HINGE ARM CUTOUT. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. HFEC INSP CRACK REMOV ED, REF NDT51-00-19, PT 6, VERIFIED CRACK REMOVED. INSTALLED MM 52-11 -87 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E17NE 20080804 NM 2008 8 4 2008UALA03630 1 20080630 A 2750 FLAP SYSTEM BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU TE FLAPS INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 928UA 26651 FLAPS WOULD NOT RETRACT AFTER TAKEOFF. CYCLED INDICATOR C/B, NO HELP. RTFL. 2 L 7 2 4F 4 F RT A16WE E21EU 20080804 NM 2008 8 4 2008UALA03636 1 20080627 A 3397 58791 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 364UA 24533 EEL LIGHTS INOP ROWS 10-14. REPLACED FEEDER CABLE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080804 NM 2008 8 4 2008UALA03648 1 20080629 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROWS 12-14 UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 EXIT PATH LIGHTING ROWS 12-13-14 LOOSE. *S/D* SECURED STRIP, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080804 NM 2008 8 4 2008UALA03650 1 20080629 A 2697 586557331 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE APU FIRE DETECT TRIPPED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 209UA 30215 APU REMOTE FIRE IND-AUTO DISC ARM CIRCUIT BREAKER FOUND POPPED AND WILL NOT RESET. FOUND APU FIRE BOTTLE ARMED LIGHT SH ORTED. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080804 NM 2008 8 4 2008UALA03653 1 20080630 A 2611 824PTY SMOKE DETECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AFT LAV FALSE ACTIVATION A UALA O OTHER N FALSE WARNING CR CRUISE 1 WP 29 377UA 24642 CREW REPORT: AFT LAV SMOKE DETECTOR GOES OFF INTERMITTENTLY. FOUND FAULTY SMOKE DETECTOR. REPLACED SMOKE DETECTOR OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080804 CE 2008 8 4 DXTA200803160 1 20080704 A 2120 UNKNOWN CESSNA 560 560XL 2076702 CE COCKPIT ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 690QS 5605090 SHORTLY AFTER TAKEOFF CREW COULD SMELL (ELEC) STINKING. (A) 2 L 7 2 4F RT A22CE 20080805 CE 2008 8 5 GUU2008F00014 1 20080623 A 3230 LANDING GEAR BEECH 1900 1900D 1154162 CE MALFUNCTIONED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 16540 UE172 FLIGHT 9216, AFTER TAKEOFF, LANDING GEAR CIRCUIT BREAKER POPPER WHEN GEAR SELECTED UP. INSPECTED MLG PERFORMED OPERATION AL CHECK. COULD NOT DUPLICATE. (A) 2 L 7 2 4T RT A24CE 20080805 EU 2008 8 5 M7K2008F00079 1 20080414 A 5302 350A23422221 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAIL BOOM CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 816MH 4038 23096 CRACK FOUND DURING ROUTINE INSPECTION ON THE MOUNTING FLANGE SURFACE RADIATING FROM A MOUNTING BORE AND TO THE EDGE OF T HE FLANGE. A NEW FITTING WAS MATCH DRILLED AND INSTALLED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080805 EU 2008 8 5 WRN2008F00003 1 20080618 A 7722 8DJ175LXR8 INDICATOR AIRBUS 300 A300B4203 3930306 EU NR1 EGT UNSERVICEABLE A WRNA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 05 501TR 53 DURING CRUISE, ENG NR1 EGT OFF SCALE HIGH INDICATION. POINTER AT 6 O`CLOCK POSITION. POINTER AND DIGITAL READOUT AGREED. AMBER EGT LIGHT ON, ENGINE EGT LIGHT ON MWP, AND SSC. AC RETURNED TO FIELD, ABNORMAL PROCEDURES WERE PERFORMED AND APPR OX. 8500 LBS OF FUEL WAS DUMPED TO ACCOMPLISH SAFE LANDING WT. AIRCRAFT LANDED NORMAL. C/A REMOVED AND REPLACED NR1 ENG EFT INDICATOR IAW 77-21-11 PG 401. TEST OK WIAW 77-21-11 PG 501. DURING TROUBLESHOOTING FOUND EFT BOTTOM LT THERMOCOUPLE HARNESS AND PROBE RESISTANCE OUT OF LIMITS IAW 77-21-01 PG 202. REMOVED AND REPLACED THERMOCOUPLE HARNESS AND PROBE IAW 77-21-01 PG 202. LOW PRESSURE AND HIGH PRESSURE TURBINE SECTIONS BOROSCOPED AND FOUND SATISFACTORY. MAX POWER ASSURANCE 2 L 7 2 4F RT A35EU 20080805 CE 2008 8 5 GUU2008F00009 1 20080625 A 3234 LIGHT BEECH 1900 1900D 1154162 CE MLG HANDLE LOOSE A GUUA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 17 81538 UE199 FLIGHT 9306, DURING APPROACH LIGHTS IN LANDING GEAR HANDLE INOPERATIVE. SECURED LIGHT ASSEMBLY ON LANDING GEAR HANDLE. (A) 2 L 7 2 4T RT A24CE 20080805 CE 2008 8 5 DXTA200803158 1 20080702 A 3230 LANDING GEAR CESSNA 680 680CE 2076811 CE INOPERATIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 311QS 6800196 GEAR WILL NOT RETRACT AFTER TAKEOFF. (A) 2 L 7 2 4F RC T00012WI 20080805 EU 2008 8 5 M7K2008F00072 1 20080303 A 3150 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE WARNING LIGHT DEFECTIVE E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 804MH 3750 23058 PILOT REPORTS AMBER GOVERNOR LIGHT ILLUMINATED DURING FLIGHT. A FAULT CODE WAS GENERATED INDICATING THE POTENTIOMETER A S THE LIKELY DEFECTIVE UNIT. A NEW PART WAS INSTALLED AND NO FURTHER DEFECTS WERE NOTED. THIS IS A RECURRING PROBLEM FO R THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY FOR THIS AC MODEL. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080805 EU 2008 8 5 M7K2008F00073 1 20080303 A 3150 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL1 60030 NE WARNING LIGHT DEFECTIVE E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 807MH 3912 23130 PILOT REPORTS AMBER GOVERNOR LIGHT ILLUMINATED DURING FLIGHT. A FAULT CODE WAS GENERATED INDICATING THE POTENTIOMETER A S THE LIKELY DEFECTIVE UNIT. A NEW PART WAS INSTALLED AND NO FURTHER DEFECTS WERE NOTED. THIS IS A RECURRING PROBLEM FO R THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY FOR THIS AC MODEL. (K) 1 G 7 2 3U 3 U H9EU E19EU 20080805 2008 8 5 ZZDA2008133 4 20080728 A 3400 066011271602 TRANSPONDER BOEING 737 737 UTILSYS NM NR 1 OVERHEATED A ZZDA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 37 344AT 36718 ELECTRICAL FUMES NOTICED AND SMELL INCREASED. PERFORMED QRH PROCEDURE. AS A PRECAUTION, PULLED ATC NR 1 C/B ALSO AND S MELL DISSIPATED. FOUND NR 1 TRANSPONDER HOT TO THE TOUCH. REMOVED AND REPLACED NR1 TRANSPONDER IAW MM 34-53. SELF TE ST GOOD. THIS CLEARS MDR 147159, PLACARD REMOVED. 2 L 7 2 4F RT A16WE 20080805 NE 2008 8 5 CIE2008F00001 2 20080714 A 7420 IGNITION LEAD CESSNA 500 560CESSNA 2076750 CE PWA JT15 JT15D5 52112 NE RT ENGINE OUT OF POSITION E CIEA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 NM 03 594M 5600279 DURING TAKEOFF, THE PILOT REPORTS THAT THE RT ENG POWER LEVER IS BINDING. MAX POWER ON TAKEOFF ROLL 83 PERCENT. ABORTE D TAKEOFF AT 30 KNOTS. ONCE THE AC RETURNED TO MAINT FACILITY; THE RT ENG COWLING WAS REMOVED AND FOUND THE RT ENG OB I GNITER LEAD ELBOW POSITIONED IN THE WRONG DIRECTION CAUSING THE THROTTLE LINKAGE TO THE FUEL CONTROL TO BIND. REPOSITIO NED IGNITER LEAD AND RETORQUED CONNECTOR NUT TO 140 IN LBS IAW MM 74-20-02. RT THROTTLE MOVES FREELY AND OPERATES NORMA LLY. THE LT ENG COWLING WAS REMOVED FOR VERIFICATION, THE LT ENG OB IGNITER LEAD ELBOW WAS POSITIONED CORRECTLY; WHICH IT WAS. PICTURES OF THE IMPROPER IGNITER ORIENTATION WERE TAKEN AND IT WAS ADDRESSED WITH THE TECHS RESPONSIBLE FOR THE 2 L 7 2 4F 4 F RT A22CE E25EA 20080805 WP 2008 8 5 ABX2008F00000 1 20080706 A 3350 60030451 POWER SUPPLY DOUG DC9 DC941 302207N WP EMERGENCY LIGHTS DEFECTIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 951AX 47616 EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY PACK IAW DC9 AMM 33-53-00. (K) 2 L 7 2 4F A6WE 20080805 SO 2008 8 5 SIM2008F00012 1 20080714 A 2120 UNKNOWN EMB 135 EMB135LR 3260305 SO CABIN ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 729AE 145343 ON FLIGHT 4735, CREW REPORTED STRONG OIL ODOR IN COCKPIT IN ALL PHASES OF FLIGHT. AC REMOVED FROM SERVICE. COMPLIED WI TH ETN NR: EM-72-034R4, NO DEFECTS NOTED. RAN BOTH ENGINE IAW AMM NR 71-00-00/36-00-00, NO OIL NOTED, NO OIL CONSUMED. RAN APU IAW AMM 49-10-00. NO DEFECTS NOTED, AIRCRAFT RETURNED TO SERVICE. (K) 2 L 7 2 4F RT T00011AT 20080805 EU 2008 8 5 M7K2008F00063 1 20080108 A 3150 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE WARNING LIGHT INOPERATIVE E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 818MH 1067 4131 23322 PILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWE VER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED M UCH LONGER THAN TYPICAL THIS IS A RECURRING PROBLEM FOR THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY OF THIS MOD E AC. THIS PART CAN ON OCCASION ALSO CAUSE ENGINE FLUCTUATIONS IN FLIGHT WHEN THE RESISTANCE VALUE SIGNAL IS DISRUPTED FOR A LITTLE AS 1/20TH OF A SECOND, WHICH IS THE SAMPLE RATE FOR THE ENGINE CONTROL SYS. AN ADDITIONAL FACTOR FOR THESE TYPE OF FAULTS IS NO RESET FUNCTION AVAILABLE TO THE PILOT TO DIFFERENTIATE BETWEEN A MOMENTARY OR AN ACTIVE FAULT. ON 1 G 7 2 3U 3 U H9EU E00054EN 20080805 CE 2008 8 5 DXTA200803169 1 20080712 A 2720 LIMITER CESSNA 750 750 2076810 CE RUDDER MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 934QS 7500034 AMBER RUD LIMIT FAIL A CAS MESSAGE ILLUMINATED AT ABOUT 1000` AFTER TAKE OFF. RUD LIMITED AT 32 PERCENT. RETURNED AND LA NDED AT DEPARTURE AIRPORT. (A) 2 L 7 2 4J RT T00007WI 20080805 NM 2008 8 5 UIE2008F00017 1 20080630 A 7830 SKIN BOEING 747 747243B 1384830 NM THRUST REVERSER DENTED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 540MC 22508 NR 3 ENGINE, RT SIDE ABOUT 4 O`CLOCK POSITION HAS 2 DENTS. NR 3 ENGINE REVERSER REPAIRED IAW ENGINE MANUAL 78-32-01, RE PAIR NR 4. (K) 2 L 7 4 4F RT A20WE 20080805 NM 2008 8 5 UIE2008F00025 1 20080705 A 5412 FASTENER BOEING 747 747243B 1384830 NM NR 4 PYLON LOOSE A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 540MC 22508 NR 4 PYLON AFT BULKHEAD CHORD FOUND SEVERAL ATTACH FASTENERS LOOSE. REPLACED FASTENERS IAW MFG MESSAGE NR 1-875740529-4 . (K) 2 L 7 4 4F RT A20WE 20080805 NM 2008 8 5 YEN2008F00004 1 20080601 A 7160 DUCT EMB ERJ190 ERJ190100IGW 3260408 NM INTAKE LOOSE A YENA O OTHER O OTHER NR NOT REPORTED 1 EA 15 216JB 19000026 AIR RETURN TO DEPARTURE DUE SOUND IN COCKPIT AS IF N1 OR NX SYNC WAS OFF. ENG INDICATIONS NORMAL. FOUND AIR INTAKE FOR BOTH RT AND LT DUCT ON 191FL LOOSE, TIGHTENED CLAMPS AND SECURED, OPS CHECK OK. (K) 2 L 7 2 4F RT A57NM 20080805 NM 2008 8 5 YEN2008F00016 1 20080708 A 3231 17070760903 ROD EMB ERJ190 ERJ190100IGW 3260408 NM NLG DOOR BENT A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 229JB 19000032 LG NOSE DOOR OPEN CAUTION ON EICAS AFTER GEAR LEVER WAS SELECTED UP ON TAKEOFF, PERFORMED QRH MESSAGE, EXTINGUISHED AFTE R GEAR WAS LOWERED DURING AIR RETURN, INDICATIONS WERE NORMAL WITH GEAR DOWN, REMOVED AND REPLACED LT AFT DOOR SENSOR IA W AMM 32-61-13, PG 401, ADJUSTED NLG DOOR POSITION SENSOR IAW AMM 32-61-13-820-802A. REMOVED AND REPLACED NLG AFT DOOR LINKAGE ROD IAW 32-22-03, ACCOMPLISHED NLG GEAR SWING IAW AMM 32-61-13. OPS CHECK OK. (K) 2 L 7 2 4F RT A57NM 20080805 SO 2008 8 5 SIM2008F00009 1 20080711 A 3240 CONTROLLER EMB 135 EMB135LR 3260305 SO BRAKE MALFUNCTIONED A SIMA C ABORTED TAKEOFF E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 SW 21 707EB 145195 CREW NOTED DURING TAKEOFF, NOSE WHEEL SHIMMY/VIBRATION. ALSO, AIRCRAFT PULLS TO THE LT WITH TILLER IN NEUTRAL POSITION. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE C/A - REMOVED AND REPLACED BRAK E CONTROL UNIT IAW MM 32-41-02. OPS CHECK GOOD. REMOVED AND REPLACED THE LT AND RT NOSE WHEEL ASSY IAW AEAI W/C 32-700 -17. AC RETURNED TO SERVICE. (K) 2 L 7 2 4F RT T00011AT 20080805 2008 8 5 HNA2008F00009 4 20080529 A 2340 50891 SWITCH DHAV DHC8 DHC8102 2809003 NM PA SYSTEM DIRTY A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 810EX 39905 308 F/A HANDSET CONTROL PANEL EMERGENCY SWITCH STICKS. REMOVED AND REPLACED F/A PA CONTROLLER IAW 8 MM 23-40-06. OPS CHECK ED GOOD. (K) 2 H 7 2 4T RT A13NM 20080805 EU 2008 8 5 YEN2008F00015 1 20080711 A 2133 VFT300B00 OUTFLOW VALVE AIRBUS 320 A320232 3930326 EU IAE V2522 V2522A5 NE FIN 22HO FAILED A YENA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 15 558JB 22960 8178 1915 AIR RETURN TO DEPARTURE, AVIONICS EXTRACT VALVE REMAINED FULLY OPEN AFTER TAKEOFF WHEN EXTRACT BUTTON WAS IN NORMAL AND OVRD. REMOVED AND REPLACED VALVE SKIN AIR OUTLET IAW AMM 21-26-53-04, OPS CK NORMAL, OK FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A28NM E40NE 20080805 WP 2008 8 5 NWAA083029759 1 20080709 A 3350 FUSE DOUG DC9 DC941 302207N WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 759NW 47287 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR SEVERAL ROWS OF COACH SEATS IN THE CABIN HA D FAILED. MAINTENANCE REPLACED THE ASSOCIATED FUSE AT THE AFT LT OVERWING EXIT. OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F A6WE 20080805 NM 2008 8 5 DHL2008F00025 1 20080606 A 5344 HINGE BOEING 727 7272M7 138407S NM CARGO DOOR CRACKED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 MAIN CARGO DOOR AFT HINGE SECTION IS CRACKED AT FUSELAGE SIDE BS 650. REMOVED AFT HINGE SECTION AT MAIN CARGO DOOR SIDE BS 650 AND INSTALLED NEW SECTION WITH MS 20001+16-7200 AND PO 9002527 DIMENSION 17 IAW BOEING 727-200 FREIGHTER MAINTEN ANCE MANUAL FIGURE 5201B CHAPTER 52 REVISION LEVEL G. LEAK CHECK GOOD IAW B727 MM 05-51-74. (A) 2 L 7 3 4F A3WE 20080805 NM 2008 8 5 F3LA200800304 1 20080607 A 5320 D5391635420040 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 REFERENCE NON ROUTINE 34044. DURING C3 S1 C CHECK INSPECTION NOTED FORWARD CARGO PIT HAS CORROSION BETWEEN FRAMES C28 A ND FRAMES C34. MAINTENANCE REMOVED PROFILE AND INSTALLED NEW PROFILE AND ATTACH ANCHORS AND SPLICE IN ACCORDANCE WITH T HE REQUIREMENTS OF SRM 51-42-11 AND SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 NM 2008 8 5 F3LA200800313 1 20080608 A 5320 D5347219021000 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 REFERENCE NON ROUTINE 34326. DURING C3 S1 C-CHECK INSPECTION NOTED LT HAND CABIN FLOOR LONGERON BEAM Y1162 BETWEEN FRAM ES 66 AND FRAME 68 HAS CORROSION AROUND TWO FASTENER HOLES. MAINTENANCE REMOVED THE CORROSION AND FOUND TO BE OUT OF LI MITS. MAINTENANCE REMOVED AND REPLACED BEAM IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-00-14 BLOCK 201. UPON COMPLE TION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 SO 2008 8 5 CHQA200800126 1 20080626 A 7500 NM1024200200 CLAMP EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL BLEED SYSTEM LOOSE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 257JQ 14500812 CAE311677 FLIGHT 3080, SDF TO LGA. JUST AFTER TAKEOFF CREW RECEIVED AN EL BLEED LEAK MESSAGE. THE PROPER QRH CHECK LISTS WERE RU N WHILE THE AIRCRAFT PREPARED TO RETURN TO SDF. THE AIRCRAFT LANDED WITHOUT INCIDENT. WHILE INSPECTING THE NR 1 BLEED SYSTEM, MAINTENANCE FOUND THE CLAMPS ON THE PRSOU LOOSE. THE CLAMPS WERE TIGHTENED AND THE BLEED SYSTEM OPERATED NORMAL LY. (A) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080805 NM 2008 8 5 F3LA200800318 1 20080610 A 5315 D5347648720000 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 77 1851 REFERENCE NON ROUTINE C044885. DURING C4 S1 C-CHECK INSPECTION NOTED AFT CARGO COMPARTMENT FLOOR FRAME 59 U-CHANNEL IS CORRODED FROM STRINGER 41 RT TO STRINGER 38 LT. MAINTENANCE REMOVED AND REPLACED U-CHANNEL IN ACCORDANCE WITH THE REQUI REMENTS OF SRM 51-44-11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 SO 2008 8 5 CHQA200800151 1 20080719 A 3230 7455503 CONTROLLER EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL MLG FAULTY A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 275SK 20824 145345 CAR312704 FLIGHT 5680, ATL TO CLE. AFTER TAKEOFF, THE GEAR WAS COMMANDED UP AND INDICATED THREE UP AND WHITE. THE CREW NOTICED A VIBRATION COMING FROM THE FLOOR TOWARDS THE NOSE OF THE AIRCRAFT. IT WAS DECIDED TO CYCLE THE GEAR TO SEE IF THE NOISE /VIBRATION CONTINUED. AFTER SELECTING THE GEAR TO THE DOWN POSITION AND GETTING A THREE GREEN INDICATION, A LG AIR/GND FAIL MESSAGE APPEARED ON EICAS. THE AIRCRAFT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ALL HA RNESSES AND PROX SWITCHES WITH NO DEFECTS NOTED. THE LANDING GEAR LEVER WAS REPLACED AND THE AIRCRAFT PLACED ON JACKS A ND THE GEAR WAS SWUNG APPROXIMATELY 8 TIMES WITH NO FURTHER DEFECTS. (A) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080805 WP 2008 8 5 ARWA20080602 1 20080621 A 7797 CONNECTOR DOUG DC10 DC1030F 3023504 WP EGT INDICATOR LOOSE A ARWA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 SO 29 524MD 46999 EGT FAILED IN FLIGHT, PERFORMED ENGINE FAILURE SHUTDOWN IN FLIGHT CHECK LIST. LANDED UNEVENTFUL. TIGHTENED NR 3 ENGINE CONNECTOR PL-8036 IN ACCORDANCE WITH M/M 20-30-01. OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH M/M 77-21-004 WD 77-21-0 1 PG 005. (A) 2 L 7 3 4F RT A22WE 20080805 EA 2008 8 5 SIMA200816406 1 20080609 A 3250 STEERING SYS CNDAIR CL600 CL6002C10 1390015 EA NLG MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 522AE 10147 ON FLIGHT 4494, CREW REPORTED ON TAKEOFF EICAS MSG "STEERING INOP" CAUTION MSG ILLUMINATED. CREW FOLLOWED AOM VOL 1 AND ELECTED TO CONTINUE ON TO ORD. CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY AND USING DIFFERENTIAL THRUST TAXIE D TO A HOLDING PAD WHERE CREW FOLLOWED AOM VOL 1 AND RESET NOSE WHEEL STEERING SYSTEM SUCCESSFULLY. AIRCRAFT REMOVED FR OM SERVICE. TROUBLESHOOT IAW CRJ 700 FIM 32-50-00, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800630 1 20080514 A 5210 MOTOR CNDAIR CL600 CL6002B19 1900309 EA DOOR ASSIST MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 882AS 7503 PAX DOOR WOULD NOT OPEN ALL THE WAY. T/S SYSTEM - FOUND DOOR ASSIST MOTOR HOLDING DOOR. CYCLED C/B FOR DOOR ASSIST. DOOR OP CHECKS OK IAW AMM 52-11-00. (B) 2 L 7 2 4F RT A21EA 20080728 CE 2008 7 28 DXTA200803109 1 20080609 A 3260 WARNING LIGHT CESSNA 750 750 2076810 CE NLG DOOR ILLUMINATED E DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 913QS 7500113 NOSE DOOR OPEN L MESSAGE DISPLAYED AFTER TAKEOFF AT GEAR RETRACTION. (B) 2 L 7 2 4J RT T00007WI 20080728 NM 2008 7 28 AALA200801357 1 20080520 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW EMERGENCY LIGHT AT SEAT ROW 20C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 20C. SYSTEM GROUND CHEC KED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 EU 2008 7 28 USAA920081172 1 20080527 A 5347 D53112827202 DUMMY RAIL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 652AW 0953 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN DUMMY RAIL, BS 709 FR 16, +Y503.2. REPLACED CABIN DUMMY RAIL, BS 709 FR 16, +Y503.2 IAW A320 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080728 NM 2008 7 28 USAA920081165 1 20080601 A 5754 65C2660121 WEDGE BOEING 737 73733A 1384673 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 PHX - MAJOR REPAIR - B CHECK - LT WING NR1 SLAT TRAILING EDGE WEDGE DELAMINATED. REPLACED THE LT WING NR 1 SLAT TRAILIN G EDGE WEDGE IAW DRAWING 65C26601. (S) 2 L 7 2 4F RT A16WE 20080728 EU 2008 7 28 USAA920081180 1 20080524 A 5540 D5537713800000 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 652AW 0953 SAL - MAJOR REPAIR - C7 CHECK - NR 2 RUDDER HINGE FITTING HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 1926 RIB 4. R EPLACED NR 4 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 1926 RIB 4 IAW AMM 55-36-41. (S) 2 L 7 2 4F RT A28NM 20080728 NM 2008 7 28 USAA920081263 1 20080605 A 5315 FLOORBEAM BOEING 737 7373S3 1384711 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW 23713 CLT - C-22 - MAJOR REPAIR - FLOORBEAM CORRODED AT BS 787, RBL 24. REPAIRED FLOORBEAM AT BS 787, RBL 24 IAW B737 SRM 53 -60-53 & SRM 51-10-02. (S) 2 L 7 2 4F RT A16WE 20080728 EU 2008 7 28 USAA920081188 1 20080609 A 2913 887673 PUMP AIRBUS A319 A319112 3930323 EU NR 1 ENGINE LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 768US 28688 28688 1389 FLT 921 - AT CRUISE, CREW RECEIVED A GREEN HYD LOW QUANTITY INDICATION FOLLOWED BY A LOW PRESS WARNING. CREW NOTICED LO W LEVEL AT 25000 THEN ALT WENT TO 0 QUANTITY THEN 0 PRESS. CREW DIVERTED TO CLT. THE LANDING WAS UNEVENTFUL AND THE AI RCRAFT WAS TOWED TO THE GATE. MX REPLACED THE GREEN HYDRAULIC PUMP. OPERATIONAL LEAK CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 20080725 EA 2008 7 25 G0C2008F00000 2 20080703 A 8530 AEL65102 CYLINDER HEAD BNORM BN2 BN2B26 1520350 EU LYC O540 O540E4C5 41532 EA ENGINE SEPARATED E G0CA O OTHER O OTHER NR NOT REPORTED 1 NM 11 2119V 2105 L2259340A NR 5 CYLINDER FAILED DUE TO CYLINDER HEAD SEPARATION FROM BARREL. AC IMMEDIATELY DIVERTED TO NEAREST AIRFIELD FOR REPAI R. AC LANDED SAFELY, POWER SETTING AT FAILURE WAS 25 IN MAN PRESSURE, 2200 RPM. AC WAS IN CRUISE SEGMENT. ENG WAS IN COMPLIANCE WITH ALL CURRENT AD`S. (K) 1 H 7 2 3O 3 O RT A17EU E295 20080728 WP 2008 7 28 UPS08852586 1 20080612 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 RIGHT AFT SERVICE DOOR AFT JAMB GOUGED STA 1660 AND L-12R. REPAIRED RIGHT AFT SERVICE DOOR AFT JAMB AT STA 1660 AND L12R IAW SRM 53-02-00 FIG 1B AND DWG 5772789. 2 L 7 4 4F RT 4A25 20080728 NM 2008 7 28 UIE2008F00002 1 20080624 A 5330 SKIN BOEING 747 747243B 1384830 NM BS 770 S28-29L SCRATCHED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 540MC 22508 FORWARD CARGO STA 770 LT SIDE STRINGER 28L TO 29L, FUSELAGE SKIN FOUND SCRATCHED COMMON AT LOWER PAX RELIEF VALVE. (K) 2 L 7 4 4F RT A20WE 20080728 EU 2008 7 28 UPS08152595 1 20080617 A 5321 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 152UP 0835 INSPECTION TYPE:5YR MAIN DECK CARGO FLOOR PNL 241DF HAS BROKEN EDGE. REPAIRED MAIN CARGO FLOOR PNL 241DF IAW A300 SRM 5 3-10-20 TABLE 201 PAR 8A. 2 L 7 2 4F RT A35EU 20080728 2008 7 28 2008UALA03423 4 20080616 A 2565 CABLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 496UA 1845 R2 DOOR ESCAPE SLIDE CABLE IS BROKEN. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 NM 2008 7 28 2008UALA03091 1 20080529 A 2711 285T00115116 MODULE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEFT MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 648UA 25285 RUDDER RATIO & AILERON LOCKOUT EICAS MSG. FLIGHT DIVERTED. REPLACED LT STAB TRIM AILERON LOCKOUT MODULE (SAM). SHOP FI NDINGS: NFF 2 L 7 2 4F 4 F RT A1NM E24NE 20080728 NM 2008 7 28 2008UALA03027 1 20080526 A 3350 GE209 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 117UA 28810 DOOR 1L UPPER SILL FWD EMERGENCY LIGHT INOP. FOUND BURNED OUT LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080807 NM 2008 8 7 AALA200801749 1 20080701 A 3350 LENS BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 909AN 29511 DFW - EMERGENCY LIGHT AT SEAT ROW 13D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHECK ED NORMAL OPERATION. (A) 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 2008UALA03703 1 20080703 A 5330 143T3561 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 465 S36L-38R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 66885 27112 LOWER EXT FUSELAGE SKIN CREASED AT BS 465 STR 36L TO 38R. REPAIRED SKIN CREATED CF9055 TO FOLLOW UP INSPECTION. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080807 NM 2008 8 7 2008UALA03709 1 20080706 A 3150 WARNING SWITCH BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN ALTITUDE MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 367UA 24536 ORAL WARNING HORN PROBLEM CAUSED DIVERSION. FOUND FAULTY CABIN ALTITUDE WARNING SWITCH. REPLACED CABIN ALTITUDE WARNIN G SWITCH. 2 L 7 2 4F 4 F RT A16WE E21EU 20080807 NM 2008 8 7 2008UALA03710 1 20080705 A 3800 UNKNOWN BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 218UA 30222 RUNNING OUT OF WATER AND LAVS SHUTTING DOWN. FLIGHT DIVERTED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080807 NM 2008 8 7 2008UALA03711 1 20080707 A 2780 BOLT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BEARING FROZEN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 351UA 24319 LEADING EDGE SLAT PROBLEM. RTFL. FOUND BOLT TO LEADING EDGE WING SUPPORT FITTING FROZE IN SPHERICAL BEARING. REPAIRED. 2 L 7 2 4F 4 F RT A16WE E21EU 20080807 EU 2008 8 7 AALA200801549 1 20080606 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 JFK - EMERGENCY EXIT LIGHT AT LT NR ONE DOOR AISLE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LT NR ONE DOOR AIS LE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080807 WP 2008 8 7 AALA200801555 1 20080606 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 DFW - EMERGENCY LIGHT AT CABIN LENS DAMAGED. REPLACED LENS FOR EMERGENCY LIGHT AT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080807 NM 2008 8 7 AALA200801366 1 20080522 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 693AA 26973 JFK - EMERGENCY LIGHT AT SEAT ROW 15DEF INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 15DEF. SYSTEM GROUN D CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 AALA200801484 1 20080602 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 650AA 24608 DFW - EMERGENCY LIGHT AT RT NUMBER FOUR SLIDE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT RT NR FOUR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 AAL200801495 1 20080603 A 2780 285N001140 FSCU BOEING 757 757223 1384957 NM FLAP/SLATS INOPERATIVE A AALA O OTHER J WARNING INDICATION DE DESCENT 1 SW 21 618AA 24526 BOS INFLIGHT T264/03JUN. FLAPS/SLATS WOULD NOT LOWER. CREW USED ALTERNATE PROCEDURE. LANDED BOS WITHOUT INCIDENT. RE PLACED NR ONE FLAP SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 CALA0800705 1 20080716 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM BS 400 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 LEFT SIDE STATION 400 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES AT STATION 400 LEFT FRAME BETWEEN S-8 AND S-9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 CALA0800706 1 20080716 A 5311 65C34355 FRAME BOEING 737 737524 1384721 NM BS 482 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 LEFT SIDE STATION 482 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES AT STATION 482 LEFT FRAME BETWEEN S-8 AND S-9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 CALA0800707 1 20080716 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 787 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 RIGHT SIDE STATION 787 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED AIR CO NDITIONING (A/C) RAIL BRACKET IAW EA5310-04498. CUT OUT DAMAGED AREA OF FRAME IAW EA 5310-04498. INSTALLED REPAIR ANGL ES IAW EA 5310-04498. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 CALA0800709 1 20080716 A 5320 65C3397335 INTERCOSTAL BOEING 737 737524 1384721 NM BS 312-328 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 INTERCOSTAL CRACKED AT STATION 312 TO 328 BL 45L. REMOVED AND REPLACED INTERCOSTAL IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 AALA200801487 1 20080602 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 780AN 29956 DFW - EMERGENCY LIGHT AT SEAT 20C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 NM 2008 8 7 AALA200801489 1 20080602 A 3350 LIGHT BOEING 777 777223 1385213 NM GALLEY DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 780AN 29956 DFW - EMERGENCY LIGHT AT LT NR ONE GALLEY CLOSET HAS BROKEN LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LT NR ONE GALLEY CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 NM 2008 8 7 AALA200801367 1 20080522 A 3350 0201804001 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 693AA 26973 JFK - EMERGENCY LIGHT AT SEAT ROW 15DEF MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 15DEF. SYSTEM GROU ND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 CALA0800733 1 20080719 A 5312 6516300291 BULKHEAD BOEING 737 737524 1384721 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 STATION 178 BULKHEAD AT WL 218 LBL 0 WEB IS CRACKED. REPLACED 178 BULKHEAD CENTER WEB PER EC/RA5310-04799. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 CALA0800725 1 20080718 A 5312 111A1101 BULKHEAD BOEING 737 737724 13844BY NM BS 663 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23721 28940 FIBERGLASS BULKHEAD AT STA 663.75 CRACKED AROUND LEFT RAM AIR EXHAUST BOOT. REPAIRED DAMAGED AREA PER SRM 57-10-10. 2 L 7 2 4F RT A16WE 20080807 WP 2008 8 7 AALA200801496 1 20080603 A 3350 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 496AA 49734 LGA - SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROW 21 TO AFT CABIN INOPERATIVE. RESECURED LOOSE BATTERY FOR SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROW 21 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080807 NM 2008 8 7 AALA200801374 1 20080523 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 LAX - EMERGENCY LIGHTS AT CENTER AFT FOUR SEAT ROWS INOPERATIVE. RESEATED CONNECTOR AT SEAT ROW 42CD. SYSTEM GROUND CH ECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 NM 2008 8 7 AALA200801375 1 20080523 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 789AN 30252 LAX - EMERGENCY LIGHTS AT CENTER AFT FOUR SEAT ROWS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT CENTER A FT FOUR SEAT ROWS. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 NM 2008 8 7 AALA200801377 1 20080523 A 3350 767 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 386AA 27060 SFO - EXTERIOR EMERGENCY LIGHT AT LT NR FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LT NR FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080807 NM 2008 8 7 AALA200801472 1 20080602 A 3350 LIGHT BOEING 757 757223 1384957 NM ROW 12 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 196AA 32390 DFW - EMERGENCY LIGHT AT SEAT ROW 12 INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 12. SYSTEM G ROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 CALA0800714 1 20080717 A 5320 141N3517056 FLOOR SUPPORT BOEING 757 757224 1384958 NM BS 333 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 18119 27561 CORROSION AT FLOOR SUPPORT STA 333, LBL-20. REMOVED AND REPLACED FLOOR SUPPORT FITTING AT STA 333, LBL-20. INSTALLED N EW FASTENERS, REF SRM 51-40-02, REF BOEING DWG 141N5170. 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 CALA0800715 1 20080716 A 5320 65C3397035 INTERCOSTAL BOEING 737 737524 1384721 NM BS 344-360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 INTERCOSTAL CRACKED AT STA 344 TO 360 BL 11L. REMOVED CRACKED INTERCOSTAL AT STA 344 TO 360 BL 11L AND INSTALLED NEW IN TERCOSTAL IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 CALA0800716 1 20080716 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 787 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 LEFT SIDE STA 787 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED A/C RAIL BR ACKET CUT OUT DAMAGED AREA AND REPAIRED FRAME AT STA 787 LT BETWEEN S-8 AND S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 CALA0800717 1 20080715 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM BS 400 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 RIGHT SIDE STA 400 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REPAIRED FRAME AT STA 400 S-8 AND S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 AALA200801355 1 20080520 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW - EMERGENCY LIGHT AT SEAT ROW 21C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 21C. SYSTEM GROUND CH ECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 EA 2008 8 7 COMA0806325 1 20080717 A 2751 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAULTY A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 27 447CA 16708 7552 RECEIVED FLAP FAIL ON APPROACH. DECLARED EMERGENCY, ABORTED APPROACH, LANDED WITHOUT INCIDENT. REPLACED RT BPSU. NO F URTHER DEFECTS. (S) 2 L 7 2 4F RT A21EA 20080807 EA 2008 8 7 COMA0880009 1 20080718 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 27 676CA 21601 15127 EMERGENCY LIGHTS WILL NOT COME ON. REPLACED BATTERY PACK NR1. (S) 2 L 7 2 4F RT A21EA 20080807 EA 2008 8 7 COMA0860324 1 20080716 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 27 447CA 16708 7552 FLAPS FAIL CAUTION MSG RECEIVED WHEN FLAPS SELECTED TO 45 DEG ON APPROACH. ACFT LANDED SAFELY. REMOVED AND REPLACED RT BPSU. (S) 2 L 7 2 4F RT A21EA 20080807 NM 2008 8 7 AALA200801464 1 20080602 A 3350 LAMP BOEING 767 767223 1385123 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 321AA 22322 LAX - EMERGENCY LIGHT AT SEAT 20B MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 20B. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080807 WP 2008 8 7 AALA200801726 1 20080628 A 3397 WIRE DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9401W 53137 LGA - EMERGENCY LIGHT AT FORWARD GALLEY EXIT SIGN INOPERATIVE. REPAIRED BROKEN WIRE AT TERMINAL FOR EMERGENCY LIGHT AT FORWARD GALLEY EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A6WE 20080807 EA 2008 8 7 TRAX200800907 1 20080713 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 FLOOR SUPPORT ANGLE CRACKED AT FS 484 LBL 27. REMOVED FLOOR SUPPORT ANGLE AT FS 484 LBL 27 AND DRILLED NEW ANGLE IAW CR J 200 SRM 53-41-00. OK TO INSTALL FLOOR SUPPORT ANGLE. (S) 2 L 7 2 4F RT A21EA 20080807 WP 2008 8 7 AALA200801727 1 20080628 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9401W 53137 LGA - SEAT MOUNTED EMERGENCY LIGHT AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT AB5 1 FOR SEAT MOUNTED EMERGE NCY LIGHT AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A6WE 20080805 EA 2008 8 5 COMA0860331 1 20080722 A 2621 365000183 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA E/E BAY LOW A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 916CA 13876 7014 EN ROUTE FROM RDU TO BOS RECEIVED CARGO BOTTLE LOW MSG. EMERGENCY DECLARED, A/C DIVERTED AT ACY AND LANDED SAFELY. REM OVED AND REPLACED LT CARGO FIRE BOTTLE. (A) 2 L 7 2 4F RT A21EA 20080805 NM 2008 8 5 F3LA200800326 1 20080610 A 5321 D5367324200000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 77 1851 REFERENCE NON ROUTINE C44993. DURING C4 S1 C-CHECK INSPECTION NOTED AFT PIT FLOOR PANEL 151VG HAS A 2 INCH SECTION MISS ING ON TOP PIECE SHOWING COMPOSITE ALONG EDGE. MAINTENANCE CUT OUT DAMAGE, TRIMMED CORE, INSTALLED NEW CORE AND REPAIRE D LOWER SKIN FLOOR PANEL 151VG IN ACCORDANCE WITH THE REQUIREMENTS OF EA A0-53T-10131 AND AMM 25-00-00-370-003. UPON CO MPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 NE 2008 8 5 A6WA200840538 2 20080707 A 7261 SCAVENGE PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT ENGINE OIL FAILED A A6WA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 31 447AW 7821 AT CRUISE, AT FL310, LT OIL PRESSURE WARNING MESSAGE, OIL PRESSURE WENT TO 15-20 PSI. RAN QRH, AT IDLE PSI RETURNED TO APPROX 30 PSI FOR LESS THAN 1 MINUTES. THEN RECEIVED LT OIL PRESSURE WARNING AGAIN AND PERFORMED LT ENGINE SHUTDOWN. E NGINE WINDMILLED FOR 39 MINUTES, OIL PRESSURE NEVER GOT LOWER THAN 15 PSI. NORMAL LANDING AND ROLLOUT. BRAKE TEMPS NOR MAL. REMOVED AND REPLACED ENGINE NR 1 LUBE AND SCAVENGE PUMP PER AMM 79-21-01. RAN ENGINE AND NO LEAKS APPARENT. C/W OIL CONSUMPTION CHECK AND OIL PRESSURE INSPECTION. NO DEFECTS NOTED. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080805 NM 2008 8 5 AALA200801579 1 20080610 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 787AL 30010 DFW - EMERGENCY LIGHT AT SEAT ROW 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 23C. SYSTEM GROUND CH ECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080805 EU 2008 8 5 NWAA082743209 1 20080613 A 3350 BATTERY PACK AIRBUS 320 A320211 3930320 EU EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 309US 118 WHEN PERFORMING EMERGENCY LIGHT TEST, EPSU 11WL FAILED. REPLACED EPSU BATTERY PACK, CHECKS OK. (A) 2 L 7 2 4F RT A28NM 20080805 NM 2008 8 5 AALA200801485 1 20080602 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 780AN 29956 DFW - EMERGENCY LIGHT AT SEAT ROW 40G INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT ROW 40G. SYSTEM GROUND C HECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080805 NM 2008 8 5 AALA200801486 1 20080602 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 780AN 29956 DFW - EMERGENCY LIGHT AT SEAT ROW 20C INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT ROW 20C. SYSTEM GROUND C HECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080805 NM 2008 8 5 AALA200801494 1 20080603 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 762AN 31479 JFK - EMERGENCY LIGHT AT OVERHEAD MAIN CABIN CREW REST DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD MAIN CABIN CREW REST DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080805 EA 2008 8 5 A6WA200840498 1 20080606 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 CROSSBEAM AT PILOTS BULKHEAD CRACKED. REPAIRED IAW REO 601R-53-11-171 REV D SCHEME B. (A) 2 L 7 2 4F RT A21EA 20080805 WP 2008 8 5 AALA200801497 1 20080603 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 LGA - FORWARD LOWER EMERGENCY FLASHLIGHT MISSING SAFETY STRAP. REPLACED SAFETY STRAP FOR FORWARD LOWER EMERGENCY FLASHL IGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080806 EA 2008 8 6 A6WA200840507 1 20080528 A 5321 PRESSURE PANEL CNDAIR CL600 CL6002B19 1900309 EA BS 449-529 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 CORROSION ON PRESSURE FLOOR WEB FS 449 TO FS 529 LBL 45. CORROSION BLENDED IAW CRJ 200 SRM 51-21-06. (A) 2 L 7 2 4F RT A21EA 20080806 SO 2008 8 6 C2XA08RI092 1 20080619 A 3350 1317 BULB EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT BURNED A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 23139 145731 FLIGHT 2218 - RIC - DURING ROUTINE MAINTENANCE, RIC MAINTENANCE FOUND EMERGENCY LIGHTS AT ROW 12 INOPERATIVE. RIC MAINT ENANCE REMOVED AND REPLACED BURNED BULBS AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO S ERVICE. (S) 2 L 7 2 4F RT 20080806 EU 2008 8 6 F3LA200800493 1 20080715 A 5321 D5367302100000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 943FR 18 2518 DURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151AE WAS PUNCTURED. MAINTENANCE REPAIRED THE DAMAGE I AW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND F OUND ACCEPTABLE. (S) 2 L 7 2 4F 4 F RT A28NM E37NE 20080806 WP 2008 8 6 AALA200801728 1 20080628 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9401W 53137 LGA - SEAT MOUNTED EMERGENCY LIGHT AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT AB5 4 FOR SEAT MOUNTED EMERGENCY LIGHT AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A6WE 20080806 WP 2008 8 6 WXOA070207 1 20080531 A 3350 20131A BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 877GA 53467 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A6WE 20080806 EA 2008 8 6 TRAX200800822 1 20080622 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 972EV 7534 LT WING AFT EMERGENCY LIGHT INOPERATIVE. RELAMPED LT WING AFT EMERGENCY LIGHT IAW CRJ200 AMM 33-51-21. OP CHECKED GOOD AT THIS TIME. (S) 2 L 7 2 4F RT A21EA 20080806 NM 2008 8 6 AALA200801419 1 20080528 A 3350 7024092008 LENS BOEING 767 767323 1385205 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 394AN 29431 JFK - EMERGENCY LIGHT AT RIGHT NR ONE DOOR EXIT SIGN MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT NR ONE DO OR EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080806 NM 2008 8 6 KCSA081325 1 20080717 A 5411 FRAME BOEING 747 747246B 1384864 NM NR 1 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 NR 1 PYLON REAR ENG MOUNT BULKHEAD INBOARD FWD. FRAME WEB CRACKED ONE INCH AT NAC STA 221.9. (S) 2 L 7 4 4F RT A20WE 20080806 NM 2008 8 6 AALA200801420 1 20080528 A 2780 ELECTRONIC UNIT BOEING 737 737823 13844BZ NM SLAT/FLAPS FAULTED A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 904AN 29506 DFW - CREW REPORTED FLAPS STUCK AT 15 DEGREES DURING APPROACH. LANDED DFW WITHOUT INCIDENT. REPLACED FLAP SLAT ELECTRI CAL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A16WE 20080806 SO 2008 8 6 C2XA08IA144 1 20080619 A 3350 7287580505 LIGHT EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14938 145029 IAH - FLIGHT 2361, DURING POSTFLIGHT INSPECTION THE CREW REPORTED THE FRONT AISLE PATH LIGHT STRIP TO BE INOPERATIVE. M AINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPRO VED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080806 EA 2008 8 6 TRAX200800685 1 20080524 A 2910 LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 879AS 7600 HYD 1 MSG PSI FLUXED AND QTY WENT FROM 70 TO 5%. ENG OPERATED 32 MIN WITH 0 PSI ON HYD SYS 1 (EN ROUTE TO ATL ACFT DIVE RTED TO BNA DUE TO MTC, EMERGENCY DECLARED). FLT 4740 DEL 79 MINS. REMOVED AND REPLACED HYD LINE P/N 601R752501 PER CR J AMM 29-00, NO HELP. REMOVED AND REPLACED HYD LINE 601R75286-37 AND ELBOW ASSY. NO HELP. FOUND HYD LINE 601R75286-61 TO BE CRACKED. REMOVED AND REPLACED HYD LINE IAW CRL AMM 29-00, OPS/LEAK CHECK GOOD. REFER TO LOD 37705-2. (S) 2 L 7 2 4F RT A21EA 20080806 NM 2008 8 6 AALA200801423 1 20080528 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT OVERHEAD RIGHT NR ONE DOOR INOPERATIVE. REPLACED LAMP AT OVERHEAD RIGHT NR ONE DOOR. SYSTEM G ROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 NE 2008 8 6 ABXA080192 2 20080205 A 7321 8063508 MEC BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE RT ENGINE DEFECTIVE A ABXA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 23 749AX 935 22226 RT ENG COMPRESSOR STALL AT LEVEL OFF 37000` ENG STABLE AT POWER REDUCTION. ENG PARAMETERS NORMAL EVENT RECORDED. RIGGE D VSV, CHECKED FEEDBACK CABLE, WITHIN LIMITS. COMPLIED WTIH BOROSCOPE INSPECTION. NO DAMAGE NOTED IAW B767 MM 75-31-03 -5-72-00-00-6. REMOVED AND REPLACED RT ENG MEC IAW B767 MM 73-2-01-4. OPS AND LEAK CHECKED GOOD AND IDLE GEAR RUN PER MM 71-00/50. (S) 2 L 7 2 4F 4 F RT A1NM E13NE 20080806 NM 2008 8 6 ABXA080194 1 20080328 A 2913 3508807 PUMP BOEING 767 767281 1385109 NM HYD SYSTEM DEFECTIVE A ABXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 786AX 256 23019 EDP HYDRAULIC PRESSURE LOW - LOW PRESSURE LIGHT ILLUMINATED. HAD EICAS MESSAGE LEFT HYDRAULIC PRIMARY PUMP. REMOVED AN D REPLACED NR 1 ENG DRIVEN HYDRAULIC PUMP IAW B767 MM 29-11-05-4. OPS CHECKED GOOD. (S) 2 L 7 2 4F RT A1NM 20080806 EU 2008 8 6 AALA200801445 1 20080601 A 3350 LENS AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 77080 626 MIA - EMERGENCY LIGHT AT SEAT 2G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 2G. SYSTEM GROUND CHECKED NOR MAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080806 NM 2008 8 6 AALA200801453 1 20080601 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 798AN 30797 DFW - EMERGENCY LIGHT AT SEAT 36C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 36C. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 NM 2008 8 6 AALA200801400 1 20080526 A 3397 WIRE BOEING 777 777223 1385213 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT WIRING AT RT NR ONE DOOR GALLEY EXPOSED. SECURED WIRING FOR EMERGENCY LIGHT AT RT NR ONE DOOR. S YSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080731 NM 2008 7 31 CALA0800660 1 20080701 A 5553 65538344 FITTING BOEING 737 737524 1384721 NM VERTICAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16646 28907 AFT RIGHT OUTBOARD VERTICAL STABILIZER FORWARD FAIL-SAFE LUG INSIDE DIAMETER HAS CORROSION. OVERSIZED BORE TO REMOVE AL L CORROSION DAMAGE, INSPECTED REWORKED AREA, INSTALLED REPAIR BUSHING AND REINSTALLED DRAG ANGLE PER ECRA 5342-01054. 2 L 7 2 4F RT A16WE 20080731 EA 2008 7 31 COMA0860296 1 20080619 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNSECURE A COMA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 SO 01 810CA 7370 RECEIVED PAX DOOR OUTER HANDLE CAUTION MESSAGE ON CLIMB. RETURNED BOS, LANDED WITHOUT INCIDENT. FOUND OUTER HANDLE NOT STOWED. INSPECTED OUTER HANDLE FOR DEFECTS IN LATCH. NONE FOUND. STOWED OUTER HANDLE. NO FURTHER DEFECTS. (S) 2 L 7 2 4F RT A21EA 20080731 NM 2008 7 31 CALA0800672 1 20080707 A 5311 65C34355 FRAME BOEING 737 737524 1384721 NM BS 482 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 LEFT STATION 482 FRAME CRACKED AT AIR CONDTIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. REMOVED DAMAGE, FABRI CATED AND INSTALLED REPAIR ANGLES AT STATION 482 LEFTHAND BETWEEN S-8 AND S-9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080731 NM 2008 7 31 CALA0800681 1 20080707 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM BS 360 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 RIGHT STATION 360 FRAME CRACKED AT AIR CONDTIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. REPAIRED CRACKED FRA ME AT STATION 360 RIGHTHAND PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080731 EU 2008 7 31 NSV2008F00007 1 20080712 A 3350 601321 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT INOPERATIVE A NSVA O OTHER O OTHER NR NOT REPORTED 1 EA 27 249CJ 340B249 FLOOR EMERGENCY ESCAPE LIGHT WILL NOT ILLUMINATE AT SEAT 2D AND 4D. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY P OS NR 1 IAW WORK CARD 33-50-025, OPS CHECK GOOD. (K) 2 L 7 2 4T RT A52EU 20080731 NM 2008 7 31 C8G2008F00004 1 20080620 A 5344 007F8362301 HINGE BOEING 757 757232 1384965 NM PAX DOOR DAMAGED A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 620DL 22910 DURING CLIMB OPERATION THE FWD ENTRY DOOR EICAS MESSAGE APPEARED WITH THE ASSOCIATED OVERHEAD LIGHT. THE AC RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE FWD ENTRY DOOR WAS NOT CENTERED I N THE DOOR FRAME WHEN CLOSED. THE FWD ENTRY DOOR HINGE WAS REMOVED AND REPLACED. OPS AND LEAK CHECKS GOOD. NO OTHER D EFECTS WERE NOTED. AC WAS RETURNED TO SERVICE. (K) 2 L 7 2 4F RT A2NM 20080731 NM 2008 7 31 YEN2008F00013 1 20080706 A 2150 ACM EMB ERJ190 ERJ190100IGW 3260408 NM CONTAMINATED A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 239JB 19000040 AIR RETURN, AFTER TAKEOFF THE ODOR OF SMOKE WAS NOTICED BY SEVERAL PASSENGERS AND CREW. THE COCKPIT CREW DETECTED HOT A IR COMING OUT OF THE AIR VENTS. ODOR DISSIPATED SHORTLY THEREAFTER, UPON INSPECTION FOUND EVIDENCE OF COFFEE CONTAMINAT ION IN RT ACM. CLEANED ACM. OPS CHECK NORMAL. AC OK FOR SERVICE AMM 21-51-00. (K) 2 L 7 2 4F RT A57NM 20080731 EU 2008 7 31 PNS2008F00002 1 20080623 A 2613 1734362450 DETECTOR SAAB SF340 340B 7860101 EU LT TAIL PIPE MALFUNCTIONED E PNSA O OTHER J WARNING INDICATION NR NOT REPORTED 1 AL 03 365PX 340B265 ON JUNE 22, 2008, THE FLIGHT CREW HAD A LEFT TAIL PIPE HOT LIGHT, AN INFLIGHT ENGINE SHUTDOWN WAS MADE, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT MADE AN UNEVENTFUL LANDING AT DEPARTURE AIRPORT. THE LIGHT WENT OUT A FEW MINUTES BEFORE LAN DING, AND THE TOTAL FLIGHT TIME WAS 23 MINUTES. MAINT REPLACED ALL THREE HEAT DETECTORS AFTER TROUBLESHOOTING THE SYSTE M, THE SYSTEM CHECKED NORMAL AND THE AC WAS RETURNED TO SERVICE. THE FLIGHT WAS BEING OPERATED UNDER FLIGHT NR 245. (K ) 2 L 7 2 4T RT A52EU 20080804 EU 2008 8 4 08FDEA02591 1 20080701 A 5753 A57960000002 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND OLD DOUBLER REPAIR ON LT INNER FLAP LOWER SKIN RIB 14-14A. DOUBLER REPAIR RENEWED IAW RAS/FOK/178/2008 ISS A, APP ROVED BY EA 6-5752-120097. 2 L 7 2 4F RT A35EU 20080804 NM 2008 8 4 AALA200801500 1 20080603 A 3350 LIGHT BOEING 757 757223 1384957 NM LT OVERWING DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 690AA 25696 DFW - EMERGENCY LIGHT PLACARD AT LEFT HAND FORWARD OVERWING DAMAGED. REPLACED PLACARD FOR EMERGENCY LIGHT AT LEFT HAND FORWARD OVERWING. SYSTEM GROUND CHECK NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080804 EA 2008 8 4 SIMA200817001 1 20080617 A 3240 5013642 BRAKE ASSY CNDAIR CL600 CL6002C10 1390015 EA NR 4 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 507AE 778 10059 ON FLIGHT 4131 - CREW REPORTED ON CLIMBOUT AT FL 160 BRAKE OVERHEAT WARNING MESSAGE ON EICAS ALONG WITH THE NR 4 BRAKE T EMP INDICATION ERRATIC. CREW ELECTED TO RETURN TO THE FIELD. CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED AND TAXIED T O THE GATE SAFELY AND WITHOUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH ETN 32-016, REMOVED AND R EPLACED NR 4 BRAKE ASSEMBLY IAW AE MTX WC 32-007. TAXI TEST SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A21EA 20080804 EA 2008 8 4 A6WA200840495 1 20080602 A 5340 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 718 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 NR 2 HYDRAULIC MANIFOLD SUPPORT BRACKET AT FS 718.00 RT CRACK FOUND IN AFT LOWER CORNER. NR 2 HYDRAULIC MANIFOLD SUPPOR T BRACKET AT FS 718.00 RT REWORKED IAW REO 601R-53-62-031. (A) 2 L 7 2 4F RT A21EA 20080804 WP 2008 8 4 AALA200801693 1 20080624 A 3350 LAMP DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 567AM 53293 LGA - EMERGENCY LIGHT AT RT HAND CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT HAND CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A6WE 20080804 SO 2008 8 4 SIMA200816801 1 20080612 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 629AE 145130 ON FLIGHT 3411 DURING PREFLIGHT THE CREW FOUND THE EMERGENCY EXIT IDENTIFIER OVER GALLEY AND THE OVERHEAD CENTER AISLE A T EMERGENCY EXIT ROW DOES NO ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. WHEN MAINTENANCE ARRIVED ALL THE EMERGENCY LIG HTS WERE OPERATING AS INDICATED. NO MAINTENANCE PERFORMED AND NO PARTS INSTALLED. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080804 NM 2008 8 4 F3LA200800296 1 20080606 A 5321 D536167800000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE CABIN DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 77 1851 REFERENCE NON ROUTINE C045066. DURING C4 S1 C CHECK INSPECTION NOTED FLOOR PANEL 221BF HAS DELAMINATION AROUND SCREW HO LES. MAINTENANCE REMOVED DELAMINATED AREA AND APPLIED MOISTURE BARRIER FOIL IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PAGE 245 FIGURE 212. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080804 NM 2008 8 4 2008UALA03663 1 20080701 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1380-1400 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 MAIN CABIN RT SIDE CREASE BEAM WEB UPPER SURFACE CORRODED FROM STA 1380 TO STA 1400, RBL 71. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. REPLACED WEB PER BAC DWG 1 46N5590 REV BN, MM51-21-00 AND SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E17NE 20080806 EU 2008 8 6 AALA200801403 1 20080526 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 JFK - EMERGENCY LIGHT AT RT NR TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT NR TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080806 NM 2008 8 6 AALA200801396 1 20080526 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NR FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NR FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 EA 2008 8 6 TRAX200800828 1 20080624 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 EMERGENCY LIGHT IN CEILING AT ROW 16 INOPERATIVE. CABIN EMERGENCY LIGHTS - CEILING LEVEL FLOODLIGHTS. RESECURED EMERGE NCY LIGHT IN CEILING AT ROW 16. OPS CHECK GOOD IAW AMM 33-51-09 DEFER CLEARED PLACARD REMOVED. (S) 2 L 7 2 4F RT A21EA 20080807 NM 2008 8 7 KCSA081355 1 20080729 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2080-2130 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FUSELAGE SKIN CORRODED BETWEEN BS2080 AND 2130, STR 34L. (S) 2 L 7 4 4F RT A20WE 20080807 NM 2008 8 7 CALA0800737 1 20080721 A 5320 65C33367 INTERCOSTAL BOEING 737 737524 1384721 NM BS 947-967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 CORROSION FOUND ON STRAP BETWEEN STATION 967 AND 947 LBL 47. REMOVED CORROSION FOUND TO BE BEYOND LIMITS OF SRM 53-60-1 5. REMOVED AND REPLACED INTERCOSTAL LBL 47 BETWEEN STATION 967 AND 947 PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080807 WP 2008 8 7 AALA200801756 1 20080702 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 419AA 49331 LGA - EXTERIOR EMERGENCY LIGHT AT OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHT AT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080807 NM 2008 8 7 CALA0800724 1 20080717 A 5754 65C26686 SKIN BOEING 737 737524 1384721 NM NR 5 SLAT DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 RIGHT WING NR 5 SLAT OUTBOARD END DELAMINATED. REPAIRED DAMAGE TO NR 5 SLAT OUTBOARD END PER BAC 737-500 SRM 51-70-10. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 AALA200801369 1 20080522 A 3233 161000181 ACTUATOR BOEING 757 757223 1384957 NM MLG INOPERATIVE A AALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 21 630AA 24588 ORD INFLIGHT T1740/22MAY LT HYDRAULIC QUANTITY INDICATION FOLLOWED BY LOSS OF LT SYSTEM HYDRAULIC PRESSURE. RUDDER TRIM DID NOT WORK DURING INITIAL APPROACH. AFTER TWO ATTEMPS RUDDER TRIM WORKED NORMALLY. LANDED ORD WITHOUT INCIDENT. RE PLACED LT MAIN LANDING GEAR DOWN LOCK ACTUATOR AND LEFT MAIN LANDING GEAR DOWN LOCK ACTUATOR HYDRAULIC LINE. SYSTEM GRO UND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 EA 2008 8 7 COMA0860318 1 20080707 A 2897 J425 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA FUEL INDICATOR SHORTED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 811CA 21081 7380 FLIGHT 5579. DURING CLIMBOUT OF RIC RECEIVED A FUEL IMBALANCE INDICATION WITH LEFT AUTO CROSSFLOW STATUS MESSAGE, FLIGH T DIVERTED TO JFK. CLEARED CONNECTOR J425 FOR P425 HARNESS TO LEFT WING FUEL PROBES AND REPLACES BACKSHELL PLUG P3QD. (A) 2 L 7 2 4F RT A21EA 20080807 EA 2008 8 7 COMA0860326 1 20080718 A 2460 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA TRIPPED A COMA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 868CA 7427 EN ROUTE FROM GSO TO LGA RECEIVED DC EMERGENCY BUSS CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY IN LGA. FOUND C/ B P1 R7 EMERGENCY BUSS SENSE, OUT. RESET C/B OPS CHECK GOOD. NO OTHER DEFECTS. (A) 2 L 7 2 4F RT A21EA 20080807 NM 2008 8 7 AALA200801376 1 20080523 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 361AA 24042 LAX - EMERGENCY LIGHT AT LT NR THREE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LT NR THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080807 NM 2008 8 7 CALA0800727 1 20080718 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM BS 827 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 LEFT SIDE STATION 827 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED A/C RAI L BRACKET, CUT OUT DAMAGED AREA AND REPAIRED FRAME AT STATION 827 LEFT BETWEEN S-8 AND S-9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 AALA200801729 1 20080629 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 798AN 30797 LHR EMERGENCY LIGHT AT FORWARD GALLEY FLOOR RT AISLE MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT FORWARD GALLEY FLOOR RT AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20080807 NM 2008 8 7 AALA200801740 1 20080701 A 3350 0202365001 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 798AN 30797 NRT EMERGENCY LIGHT AT FORWARD GALLEY RT HAND AISLE MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT FORWARD GALLEY R T HAND AISLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20080807 EA 2008 8 7 A6WA200840486 1 20080606 A 5340 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 HYDRAULIC SUPPORT BRACKET (P/N 601R75262-153) CRACKED IN RT MLG BAY. HYDRAULIC SUPPORT BRACKET IN RT MLG BAY IAW REO 60 1R-53-42-007. (A) 2 L 7 2 4F RT A21EA 20080807 EA 2008 8 7 A6WA200840488 1 20080606 A 7110 BRACKET CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 ON RT ENGINE INLET BRACKET FOUND CRACKED AT STATION XN155.845 NEAR 5 O`CLOCK POSITION (LOOKING FWD). RT ENGINE BRACKET AT STATION XN 138.845 NEAR 5 O’CLOCK POSITION (LOOKING FWD) REPLACED IAW CRJ 200 SRM 51-42-06 & SRM 51-42-13. (A) 2 L 7 2 4F RT A21EA 20080804 NM 2008 8 4 2008UALA03684 1 20080702 A 3897 HEATING ELEMENT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE WATER TANK LINE BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 ELECTRICAL HEATER TAPE HAS BURNED THROUGH ON AFT WATER TANK LINE STA 1650 STR 27R AFT CARGO COMPARTMENT. REPLACED HEAT TAPE OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080804 NM 2008 8 4 2008UALA03651 1 20080701 A 2920 PRESSURE SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYD PTU FAULTY A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 551UA 25399 POWER TRANSFER UNIT STATUS MSG DISPLAYED. PRESSURE SWITCH S10246 FAULTY. REPLACED PRESSURE SWITCH S10246, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080804 NM 2008 8 4 2008UALA03652 1 20080701 A 3397 FEEDER CABLE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 938UA 26671 AFT EEL FLOOR SECTION INOP. FOUND FAULTY FEEDER CABLE. REPLACED FEEDER CABLE OP CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 20080804 SO 2008 8 4 GUU2008F00012 1 20080531 A 5210 SWITCH EMB 120 EMB120ER 3260203 SO DOOR ACTUATOR DIRTY A GUUA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 17 283AS 120236 FLIGHT 9215. PILOT DISCREPANCY: FORWARD DOOR ACTUATOR LIGHT ILLUMINATED, TO OPEN DOOR EMERGENCY VALVE HAD TO BE USED. C/ A CLEANED AND RESECURED FORWARD DOOR ACTUATOR SWITCH. (A) 2 L 7 2 4T RT A31SO 20080805 EU 2008 8 5 M7K2008F00061 1 20080108 A 3150 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE WARNING LIGHT INOPERATIVE E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 807MH 1799 3912 23130 PILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWE VER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED M UCH LONGER THAN TYPICAL THIS IS A RECURRING PROBLEM FOR THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY OF THIS MOD E AC. THIS PART CAN ON OCCASION ALSO CAUSE ENGINE FLUCTUATIONS IN FLIGHT WHEN THE RESISTANCE VALUE SIGNAL IS DISRUPTED FOR A LITTLE AS 1/20TH OF A SECOND, WHICH IS THE SAMPLE RATE FOR THE ENGINE CONTROL SYS. AN ADDITIONAL FACTOR FOR THESE TYPE OF FAULTS IS NO RESET FUNCTION AVAILABLE TO THE PILOT TO DIFFERENTIATE BETWEEN A MOMENTARY OR AN ACTIVE FAULT. ON 1 G 7 2 3U 3 U H9EU E00054EN 20080805 EA 2008 8 5 COMA0860329 1 20080722 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 940CA 14021 7048 ON CLIMBOUT FROM CVG RECEIVED NOSE GEAR DISAGREE. EMERGENCY DECLARED, A/C RETURNED BACK TO CVG AND LANDED SAFELY. REMO VED AND REPLACED NLG SELECTOR VALVE. (A) 2 L 7 2 4F RT A21EA 20080805 EU 2008 8 5 SIM2008F00013 1 20080603 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS DISCHARGED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 240DS 340B240 MAINTENANCE REPORTED EMERGENCY LIGHTS ABOVE MAIN CABIN DOOR AND FLIGHT ATTENDANTS JUMP SEAT INOPERATIVE. AIRCRAFT REMOV ED FROM SERVICE. REMOVED AND REPLACED SERVICEABLE EMERGENCY POWER SUPPLY 21LN IAW SAAB AMM 33-50-10, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4T RT A52EU 20080805 NM 2008 8 5 F3LA200800337 1 20080611 A 5321 D5367162400000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CABIN DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 REFERENCE NON ROUTIN 34301. DURING C3 S1 C-CHECK INSPECTION NOTED CABIN FLOOR PANEL 251FF HAS AREA OF DELAMINATION FROM FRAME 47 TO FRAME 64. MAINTENANCE REPAIRED PANEL IN ACCORDANCE WITH SRM 53-42-13-400-001. UPON COMPLETION OF THE REPA IR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 NM 2008 8 5 DHL2008F00027 1 20080612 A 5313 STRINGER BOEING 727 7272M7 138407S NM BS 620 S28L CORRODED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 EXFOLIATED CORROSION ON STRINGER 28L CHANNEL BETWEEN BS 620 AND BS 640. REPAIRED STRINGER BS 620-640 STRINGER 28L IAW B 727 SRM 53-10-3 FIG 1 DETAIL 1. (A) 2 L 7 3 4F A3WE 20080805 EA 2008 8 5 COMA0860330 1 20080722 A 2621 346000371 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA E/E BAY LOW A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 916CA 13877 7014 EN ROUTE FROM RDU TO BOS RECEIVED CARGO BOTTLE LOW MSG. EMERGENCY DECLARED, A/C DIVERTED TO ACY AND LANDED SAFELY. REM OVED AND REPLACED RT CARGO FIRE BOTTLE. (A) 2 L 7 2 4F RT A21EA 20080805 NM 2008 8 5 F3LA200800327 1 20080611 A 5320 D5347047700800 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 REFERENCE NON ROUTINE 33985. DURING C3 S1 C-CHECK INSPECTION NOTED AFT CARGO COMPARTMENT LT SIDE PROFILE HAS CORROSION BETWEEN FRAMES C57 AND C58. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH SRM 51-72-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 EU 2008 8 5 F3LA200800368 1 20080616 A 5321 D5367424100000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 941FR 18 2483 REFERENCE NON ROUTINE C045369. DURING C2 C-CHECK INSPECTION NOTED AFT PIT FLOOR PANEL 151PE HAS SEVERAL PUNCTURES. MAI NTENANCE REPAIRED PANEL 151PE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-02-00 PARAGRAPH 8C FUGURE 204. UPON COMPLET ION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 WP 2008 8 5 NWAA082509927 1 20080604 A 3397 GROUND WIRE DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8920E 45835 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY FLOOD LIGHT FOR THE AFT EVACUATION SLIDE WAS NOT FUNCTIONAL. A GROUNDING POINT AT L2-110 WAS FOUND TO BE LOOSE. RE-SECURED GROUND AND OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F A6WE 20080805 NM 2008 8 5 F3LA200800324 1 20080610 A 5315 5347706700000 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 77 1851 REFERENCE NON ROUTINE C044879. DURING C4 S1 C-CHECK INSPECTION NOTED AFT CARGO COMPARTMENT STANCHION RECEPTABLE AND ARE A CORRODED AT FLOOR FRAME 56 AND STRINGER 37 RT. MAINTENANCE REPAIRED IN ACCORDANCE WITH EA A9-53R-30365 AND SRM 51-42- 11, SRM 51-75-12, SRM 51-21-11 AND NTM 51-10-01 AND AIRBUS DRAWING 53477067. UPON COMPLETION OF THE REPAIR IT WAS INSPE CTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 NE 2008 8 5 UIEA200800269 2 20080720 A 7200 CF650E2 ENGINE BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE NR 2 VIBRATION A UIEA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 EA 15 522MC 21783 BLOCK TURNBACK NR 2 ENGINE EGT FLAG IN VIEW WITH UNUSUAL NOISE (RUMBLING) HEARD AND FELT DURING THROTTLE MOVEMENT FROM N R 2 ENGINE. REPLACED ENGINE IAW WORK CARD E2008. (A) 2 L 7 4 4F 4 F RT A20WE E23EA 20080807 SO 2008 8 7 C2XA08CL075 1 20080629 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13990 145277 DURING ROUTINE MAINTENANCE THE COCKPIT STEP EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE RESECURED THE ELECTRICAL CONNECTOR ON THE COCKPIT STEP EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4T RT T00011AT 20080807 2008 8 7 HNAA0800230 4 20080713 A 3442 TRANSCEIVER DHAV DHC8 DHC8102 2809003 NM WX RADAR SYSTEM FAULTED A HNAA O OTHER G MULTIPLE FAILURE CL CLIMB 1 EA 07 808EX 40793 40793 299 RADAR SHOWED TX FLT IN FLIGHT AND WOULD NOT PAINT WEATHER. AIR RETURN TO LGA. MAINTENANCE REPLACED RADAR R/T OPS CHECK GOOD. (S) 2 H 7 2 4T RT A13NM 20080807 NM 2008 8 7 2008UALA03634 1 20080630 A 2611 FIRE LOOP AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 2 NACELLE FALSE ACTIVATION A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 840UA 1522 FIRE LOOP A FAULT DISPLAYED ON UPPER ECAM SCREEN - ENG 2. FDU FAILING INTERMITTENTLY. FIRE LOOP CHECK FOR CHAFING AND SHOOK WIRE BUNDLE AND WAS UNABLE TO DUPLICATE. ACP CHECK OF POST FLT REPORT AND PREVIOUS LEG REPORTS AND NO FAULTS NOTE D. REPLACED FDU. 2 L 7 2 4F 4 F RT A28NM E40NE 20080807 WP 2008 8 7 AALA200801473 1 20080602 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 DFW - EMERGENCY LIGHT AT SEAT ROW 11D SHROUD DAMAGED. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 11D. SYSTEM GROU ND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080807 NM 2008 8 7 AALA200801474 1 20080602 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 674AN 29424 DFW - EXTERIOR EMERGENCY LIGHT AT LT NR ONE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LT NR ONE D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 EA 2008 8 7 COMA0860321 1 20080713 A 3350 362624 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 27 965CA 7131 FLIGHT 9422. DURING LINE CHECK FOUND ROW 2-5 EMERGENCY FLOOR LIGHTS INOP. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT S TRIP. (A) 2 L 7 2 4F RT A21EA 20080807 NM 2008 8 7 AALA200801388 1 20080525 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 684AA 25341 DFW - EMERGENCY LIGHT AT SEAT ROW 18D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 18D. SYSTEM GROUND CH ECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 AALA200801397 1 20080526 A 3397 WIRE BOEING 777 777223 1385213 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT WIRING AT MAIN DECK CREW REST FORWARD CLOSET EXPOSED. SECURED WIRING FOR EMERGENCY LIGHT AT MAIN DECK CREW REST FORWARD CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 NM 2008 8 7 AALA200801398 1 20080526 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHTS AT SEAT ROWS 30 TO 45 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 30 TO 45. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 EA 2008 8 7 TRAX200800843 1 20080626 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 836AS 7263 SERVICE DOOR WON’T CLOSE. SERVICE DOOR OPS CHECK GOOD IAW CRJ 200 AMM 52-40-01. ACFT OK FOR SERVICE. (S) 2 L 7 2 4F RT A21EA 20080807 SO 2008 8 7 C2XA08SH088 1 20080619 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 10575 145640 SHV - DURING C-CHECK IT WAS FOUND THAT THE CENTER OMEGA BEAM WAS CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEAM IAW EMB 145 SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080807 EA 2008 8 7 TRAX200800845 1 20080623 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 EMERGENCY LIGHT IN LT LOWER GALLEY INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BULB IN LT LOWER GALLEY IAW CRJ AM M 33-51-01. OPS CHECK GOOD. (S) 2 L 7 2 4F RT A21EA 20080807 SO 2008 8 7 C2XA08RI095 1 20080623 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DEFECTIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15980 145202 RIC - DURING ROUTINE MAINTENANCE, RIC MAINTENANCE FOUND FLOOR BOARD EMERGENCY LIGHTS INOPERATIVE FROM ROW 12A TO 19A. M AINTENANCE REMOVED AND REPLACED EMERGENCY FLOOR BOARD LIGHT INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080807 SO 2008 8 7 C2XA08TY067 1 20080618 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 16976 145171 FLOOR EMERGENCY LIGHT STRIPS NR 3 AND NR 4 INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY NR 3 IAW EMB 145 A MM 33-50-04. OPS CHECK GOOD. (S) 2 L 7 2 4T RT T00011AT 20080807 SO 2008 8 7 C2XA08TY066 1 20080618 A 3350 66367 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 26549 145571 EMERGENCY LIGHT FLOOR STRIP WILL NOT ILLUMINATE BETWEEN ROWS 8A AND 10A. REMOVED AND REPLACED EMERGENCY LIGHT FLOOR STR IP IAW EMB 145 AMM 33-50-08. OPS CHECK GOOD. (S) 2 L 7 2 4T RT T00011AT 20080807 SO 2008 8 7 C2XA08TY064 1 20080613 A 5740 14569009409 BRACKET EMB 145 EMB145LR 3260212 SO LT AILERON WORN A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 16976 145171 LT AILERON PCA BRACKET MIGRATED HAT BUSHING. REMOVED AND REPLACED AILERON PCA FITTING IAW EC 5750-01177. (S) 2 L 7 2 4T RT T00011AT 20080805 NE 2008 8 5 DHL2008F00019 1 20080716 A 2197 JBS9121 RESISTOR SKRSKY S76 S76B 8143007 NE K-1 RELAY BURNED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 520AC 499 760380 AIR CONDITIONING SYSTEM WOULD RUN FOR ABOUT 10 SECONDS THEN QUIT. FOUND THE SPRING RESISTOR BURNED OFF OF THE K-1 RELAY WHICH IS MOUNTED ON THE COMPRESSOR PALLET. SUSPECT THE SPRING RESISTOR EXPERIENCED FATIGUE CRACKING WHERE IT ATTACHES TO THE RELAY TERMINAL. THE RELAY TERMINAL WAS BURNED AND MELTED. RECOMMEND TO CHECK THIS SPRING RESISTOR FOR FATIGUE C RACKS. (A) 1 G 7 2 4U H1NE 20080805 2008 8 5 HNAA0800215 4 20080623 A 3442 DISPLAY DHAV DHC8 DHC8102 2809003 NM WX RADAR SYS MALFUNCTIONED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 838EX 161 RETURN TO FIELD WEATHER RADAR SCREEN PAINTS MULTIPLE LINES AND COLORS RRD WEATHER RADAR RT, OPS CHECK GOOD. (A) 2 H 7 2 4T RT A13NM 20080805 NE 2008 8 5 UIEA200800268 2 20080718 A 7532 73836222 BLEED VALVE BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE NR 1 ENGINE LEAKING A UIEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 15 540MC 22508 LT WING LEADING EDGE OVERHEAT LIGHT ILLUMINATED. LIGHT DID NOT GO OUT UNTIL THROTTLE WAS RETARDED. FOUND PYLON VALVE L EAKING. REPLACED VALVE, OPS CHECKED OK. (A) 2 L 7 4 4F 4 F RT A20WE E23EA 20080805 NM 2008 8 5 ARWA20080702 1 20080718 A 2910 O-RING DOUG DC10 DC1040F 3023507 NM HYD SYSTEM LEAKING A ARWA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 29 140WE 46661 HYDRAULIC SYSTEM QTY STARTED TO DROP AT OP OF DESCENT. PERFORMED THE HYD QTY LOSS ALTERATIVE. OPS CHECKLIST. FLUID LO SS CONTINUED. PERFORMED SINGLE HYD SYS FAILURE ABNORMAL CHECKLIST, PERFORMED AT 50 FLAP NORMAL CONFIGURATION, FLT LANDE D UNEVENTFUL AFTER LANDING REQUESTED EQUIP IN TO BE TESTED TO CARGO RAMP DUE TO LIMITED LT TURN CAPABILITIES. T/S HYD L EAK TO NR 1 SYS MANIFOLD LEAK THROUGH O-RING AT PRESSURE SWITCH ON MANIFOLD, R & R PACKING & REPLENISHED & RESERVICED IA W MM 12-13-02, PERFORMED LEAK & OPS CHECK IAW MM 29-00-00. FOUND NORMAL, PERFORMED HYD SYS BLEED & PERFORMED TEST IAW M M 29-03-00, ALL SYSTEMS NORMAL. 2 L 7 3 4F RT A22WE 20080805 NM 2008 8 5 F3LA200800303 1 20080607 A 5320 D5391635520000 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 REFERENCE NON ROUTINE 34043. DURING C3 S1 C-CHECK INSPECTION NOTED CORROSION ON THE RT SIDE FORWARD CARGO COMPARTMENT R T PROFILE BETWEEN FRAMES C28 AND C34. MAINTENANCE REMOVED PROFILE ON THE RT SIDE FORWARD CARGO COMPARTMENT AT FRAME C28 TO FRAME C34 AND REPLACED WITH NEW PROFILE IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-72-11 AND SRM 51-42-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 NM 2008 8 5 DHL2008F00010 1 20080623 A 5210 WEB BOEING 727 7272M7 138407S NM L1 DOOR CRACKED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 L-1 DOOR LOWER FORWARD BOTTOM OF DOOR HAS CRACKED WEB. INSTALLED NEW LOWER WEB FROM L-1 DOOR WITH MATERIAL 7075-T6 .075 SIZE 37 5 X 8 AND PO 9007406 IAW B727 SRM 51-30-2 52-10-1 FIG 1 AND 51-10-1. (A) 2 L 7 3 4F A3WE 20080805 NM 2008 8 5 AALA200801730 1 20080629 A 3241 MODULE BOEING 757 757223 1384957 NM ANTI SKID SYS INOPERATIVE A AALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 629AA 24587 MIA INFLIGHT T1944/29JUN SJU TO IAD. CREW REPORTED RT HYDRAULIC SYSTEM LOSS. SHUT DOWN RT HYDRAULIC SYSTEM. LANDED MI A WITHOUT INCIDENT. REPLACED RT HAND ANTISKID CONTROL MODULES. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A2NM 20080805 NM 2008 8 5 RYN2008F00009 1 20080723 A 5610 141T480013 WINDSHIELD BOEING 757 757236 1384971 NM COCKPIT CRACKED A RYNA O OTHER O OTHER NR NOT REPORTED 1 CE 07 526NA 24794 LEFT NR 1 WINDSHIELD CRACKED. REPLACED LEFT NR 1 WINDSHIELD AND WINDOW HEAT CONTROLLER IAW AMM 56-11-01 AND AMM 50-41-0 1 OPS CHECKED NORMAL. (A) 2 L 7 2 4F RT A2NM 20080805 SO 2008 8 5 RAIA00807015 1 20080719 A 2700 UNKNOWN EMB 145 EMB145 3260210 SO UNKNOWN UNKNOWN A RAIA A UNSCHED LANDING F FLT CONT AFFECTED LD LANDING 1 CE 03 820HK 145064 FLT 5574 - RIC - DURING LANDING AT 50 FT ALTITUDE, THE CREW REPORTED THAT THE PLANE YAWED TO THE LT WITH A 15-20 DEGREE ROLL TO THE LT. NO WIND GUST REPORTED. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE AUTOPILOT SYSTEM AND PERFORME D A DETAILED VISUAL INSPECTION OF ALL THE FLIGHT CONTROL SURFACES. IN ADDITION, THE AIRCRAFT HAS HAD A MAINTENANCE CHEC K FLIGHT. NO DEFECTS NOTED DURING ALL PHASES OF INSPECTION AND FLIGHT CHECK. (A) 2 L 7 2 4F RT T00011AT 20080805 EA 2008 8 5 TRAX200800914 1 20080716 A 2621 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY LOW A ASOA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 849AS 7347 INFLT RECEIVED CARGO LOW BOTTLE MSG, FOLLOWED QRH AND RETURNED TO GSP. FLT 4291 DEL 121 MINS (CARGO COMPARTMENT FIRE EX TINGUISHING SYSTEM). REMOVED AND REPLACED CARGO FIRE BOTTLE IAW CRJ 200 AMM 26-25-01. OPS CHECK GOOD AT THIS TIME. SP 450 C/W (A) 2 L 7 2 4F RT A21EA 20080805 EA 2008 8 5 TRAX200800835 1 20080625 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 333 S25L CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 CORROSION ON FRAME AND SKIN AT FS 333 STR 25 LT. FABRICATED AND DRILLED -1 DOUBLER. INSTALLED -1 DOUBLED, AND -2 FRAME INSERT REF CRJ200 SRM 51-42-06. SEALED REPAIR AREA, REFINISHED REPAIR AREA, AND BLENDED AREA ON STRAP AO23. REINSTALL ED HYD CLAMPS, ABOVE WORK DONE REF REO 601R-53-21-904. JOB COMPLETE. CC7021316. BLENDED STRAP AND REMOVED CORROSION. BLENDED AREA MEASURES 1"X1.2" WITH .002" MATERIAL REMOVED. REPORTED BLEND DIMENSIONS TO ENGINEERING. REF CRJ200 SRM 5 1-21-16 PSP7019749 25JUN08. (S) 2 L 7 2 4F RT A21EA 20080805 EA 2008 8 5 TRAX200800836 1 20080625 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 857AS 7411 MAIN CABIN DOOR DIFFICULT TO CLOSE (OUTER HANDLE). PERFORMED OPERATIONAL TEST OF PASSENGER DOOR IAW CRJ 200 MM 52 11 00 WITH NO DEFECTS NOTED AT THIS TIME. (S) 2 L 7 2 4F RT A21EA 20080805 WP 2008 8 5 WRL2008F00006 1 20080721 A 5313 STRINGER DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE BS 766 S36L CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 137WA 48282 DURING INSPECTION FOUND LEVEL 2 CORROSION ON STR 36L AT FSTA 766 (N/R 19). (A) 2 L 7 3 4F 4 F A22WE E23EA 20080805 NM 2008 8 5 DHL2008F00008 1 20080610 A 5730 SKIN BOEING 727 7272M7 138407S NM LT WING CRACKED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 LT WING UPPER LEADING EDGE WS 507 AFT CORNER OF HOOK CUT OUT IS CRACKED. REMOVED HOOK SEAL IAW B727 SRM 51-30-2. STOP DRILLED CRACK DIMENSION .250 IAW B727 SRM 51-10-1. CUT OUT STRAP DIMENSION 7.875" X 1.875" IAW B727 SRM 57-30-4 FIG 9. FABRICATED PLATE REPAIR USING 301 1/2 HD 1/2 .025 DIMENSION 7.875" X 4.5" PO 9006497, ONE FILLER USING 301 1/2 HD .040 DIMENSION 7.875" X 1.875" PO 9006904, TWO BACKING STRAPS USING 2024-T3 .063 PO 9006767 DIMENSION 1.25" X .625" IAW B727 SRM 57-30-4 FIG 9. TREATED AND PRIMED REPAIR PARTS IAW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-30-2 A ND 57-30-4 FIG 9. INSTALLED HOOK SEAL IAW B727 SRM 51-30-2 AND MM 51-30-51. (A) 2 L 7 3 4F A3WE 20080805 NM 2008 8 5 F3LA200800302 1 20080609 A 5347 D53112782201 SEAT TRACK AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 77 1851 REFERENCE NON ROUTINE C044835. DURING C4 S1 C-CHECK INSPECTION NOTED CORROSION ON SEAT TRACK AT Y1292 BETWEEN FRAME 19 AND FRAME 20. MAINTENANCE REMOVED AND REPLACED BEAM IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETI ON OF THE REPAIR IN WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080807 SO 2008 8 7 C2XA08ON148 1 20080621 A 3350 82301 SIGN EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11184 8870 4980 14500917 FLT MX - ONT - WHILE PERFORMING 3A CHECK INSPECTION ON EXIT SIGN ON ROW NR12 IT DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LIGHT SIGN. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE . (S) 2 L 7 2 4F RT 20080807 SO 2008 8 7 C2XA08TY061 1 20080604 A 3350 LAMP EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 16112 145660 COCKPIT OVERHEAD EMERGENCY LIGHT AND NR1 OVERHEAD EMERGENCY LIGHT AND FWD LT OVERWING EMERGENCY LIGHT INOPERATIVE. REMO VED AND REPLACED NR1 EMERGENCY BATTERY BASE IAW EMB145XR AMM 33-50-00. OPS CHECK GOOD. REMOVED AND REPLACED LT OVERWIN G LAMP IAW EMB145XR AMM 33-50-07. OPS CHECK GOOD. (S) 2 L 7 2 4F RT 20080807 NM 2008 8 7 ABXA080195 1 20080403 A 5270 WARNING LIGHT BOEING 767 767232 1385132 NM CARGO DOOR FALSE ACTIVATION A ABXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 750AX 22227 MAIN CARGO DOOR LIGHT ILLUMINATED ON CLIMBOUT. INSPECTED MAIN CARGO DOOR LOCKS. FOUND DOOR IN LOCKED POSITION. LIGHT WENT OUT ON LANDING. OPERATED DOOR 5 CYCLES. OPS CHECKED GOOD ON GROUND IAW MM 52-32-1 PROCEDURE. (S) 2 L 7 2 4F RT A1NM 20080807 EU 2008 8 7 08FDEA02583 1 20080630 A 5754 A5796030500300 SKIN AIRBUS 300 A300F4605R 3930327 EU RT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 RIGHT WING CENTER FLAP UPPER SKIN HAS A WORN AREA APPROXIMATELY 70 INCH FROM THE INBD END AND 23 INCHES FROM THE AFT EDG E. BLENDED AREA AND FOUND AREA OUT OF ALLOWABLE LIMITS IAW A300-600 SRM 57-50-00; FIG SHEET 5; NOTE 1. FABBED REPAIR D OUBLER; TREATED; PRIMED AND INSTALLED IAW A300-600 SRM 57-50-00; PGS 217 - 220. 2 L 7 2 4F RT A35EU 20080807 EU 2008 8 7 08FDEA02584 1 20080630 A 5753 SKIN AIRBUS 300 A300F4605R 3930327 EU LT WING TE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 LEFT INBD FLAP LOWER SKIN; FWD OUTBD; HAS A PAINTED OVER GOUGE. BLENDED DAMAGE IAW A300-600 SRM 57-50-00. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 57-50-00. INSTALLED REPAIR IAW A300-600 SRM 57-50-00; PG 218; FIG 205. 2 L 7 2 4F RT A35EU 20080807 NM 2008 8 7 08FDEA02199 1 20080608 A 2612 4059027903 FIRE DETECTOR DOUG MD11 MD11F 3023600 NM CARGO BAY FAILED A FDEA F ACTIVATE FIRE EXT. N FALSE WARNING LD LANDING 1 CE 21 631FE 48454 AFTER LANDING SYD RECEIVED LVL3 CARGO FIRE LWR FWD ALERT DISCHARGED BOTTLE AND COMPLETED QRH AFTER A/C STOPPED. ATC NOT IFIED AND FIRE CREW INSPECTED AREA AND FOUND COLD. REMOVED AND REPLACED NR 1 LWR CARGO FIRE EXTINGUISHER BOTTLE/CARTRID GE. REMOVED AND REPLACED MSC. REMOVED AND REPLACED FWD CARGO OVERHEAT HEAT DETECTOR. REMOVED AND REPLACED 5 FWD CARGO SMOKE DETECTOR UNITS. REMOVED AND REPLACED MSC, REMOVED AND REPLACED CARGO HEAT DETECTOR. 2 L 7 3 4F RT A22WE 20080807 EU 2008 8 7 08FDEA02731 1 20080708 A 5310 A53988727205 CROSSBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON AFT FACE OF CROSS STRUT C87 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080807 EU 2008 8 7 08FDEA02620 1 20080519 A 5347 A5361251920001 SEAT TRACK AIRBUS 300 A300B4622R 3930312 EU BS 1163-1232 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 PREVIOUS REPAIR FOUND LOCATED ON SEAT-TRACK LT, STA Y953, FRAME 14-14C. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETE RMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUS REPAIRED PART REPLACED BY NEW SEAT-TRACK Y953 IN ACCORDANCE WITH SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080807 EU 2008 8 7 08FDEA02621 1 20080523 A 5347 A5361251920001 SEAT TRACK AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 CABIN FLOOR, CORROSION ON SEAT-TRACK Y953 BETWEEN FRAMES 11 AND 12. SEAT-TRACK REPLACED IN ACCORDANCE WITH SRM 51-72-10 . 2 L 7 2 4F RT A35EU 20080807 EU 2008 8 7 08FDEA02622 1 20080519 A 5730 A57240948 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 721FD 477 PREVIOUS REPAIR FOUND LOCATED ON LT WING, RIB 4-5, AT SHROUD BOX TOP SKIN. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR D ETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR NOT IN ACCORDANCE WITH APPROVED DA TA. NEW REPAIR INSTALLED AS PER FEDEX EA 6-5710-121643. 2 L 7 2 4F RT A35EU 20080807 EU 2008 8 7 08FDEA02623 1 20080519 A 5330 A53811923206 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 721FD 477 PREVIOUS REPAIR FOUND LOCATED ON FUSELAGE LT STA 1212-1260, STGR 28-30 LT, FR 15-16A, BELOW FWD LT DOOR. REPAIR REQUIRE S EVALUATION FOR MAJOR/MINOR DETERMIANTION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUAT ED AND FOUND NOT TO CONFORM TO APPROVED DATA. NEW REPAIR ACCOMPLISHED AS PER FEDEX EA 6-5330-117334. 2 L 7 2 4F RT A35EU 20080807 WP 2008 8 7 08FDEA02625 1 20080702 A 2910 ARK7003616 PIPE DOUG MD10 MD1010F 3022112 WP HYD SYSTEM LOOSE A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 21 571FE 47830 HYD 3 ELEV OFF ALERT 45 MINUTES INTO FLIGHT. R&R RT MLG TRIM CYLINDER. PEFORMED GEAR RETRACTION. 2 L 7 3 4F RT A22WE 20080806 EA 2008 8 6 A6WA200840516 1 20080616 A 3260 TARGET CNDAIR CL600 CL6002B19 1900309 EA RT UPLOCK LOOSE A A6WA O OTHER N FALSE WARNING CL CLIMB 1 GL 31 451AW 7832 RT MLG DISAGREE ON DEPARTURE. COMPLIED WITH QRH GEAR CAME DOWN ALL THREE SHOWED LOCKED. RT UPLOCK TARGET FOUND LOOSE, RETIGHTENED PER CMM 32-30-16 FUNCTION TEST OF EXTENSION AND RETRACTION TEST GOOD. (A) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 TRAX200800695 1 20080527 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 844AS 7317 FLAP FAIL AT 8 DEGREES (EN ROUTE TO ATL ACFT DIVERTED TO MDT DUE TO MTC, EMERGENCY DECLARED). PERFORMED EXTERNAL VISUAL CHECK OF FLAPS IN ALL SETTINGS. NO TWISTING OR SKEWING DETECTED. CYCLED FLAPS MULTIPLE TIMES WITH NO FURTHER FAULTS N OTED. INTERROGATED FECU AND NO CURRENT FAULTS EXIST IAW TEMP REV 27-01 AND FIM 27-50-00, AC OK FOR SERVICE. (S) 2 L 7 2 4F RT A21EA 20080806 WP 2008 8 6 AALA200801731 1 20080629 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 291AA 49303 DFW - EMERGENCY LIGHT AT SEAT 18D HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND C HECKED NORMAL OPERATION. (S) 2 L 7 2 4F A6WE 20080806 NM 2008 8 6 2008UALA03693 1 20080702 A 5344 HINGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 L2 DOOR HAS A CRACK AT UPPER HINGE ARM CUTOUT. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. ACCOMPLISHED HFEC OF CUTOUT PE R 757 NDT 6-51-00-19, AND FOUND A CRACK APPROXIMATELY .3750 INCH LONG. REMOVED DAMAGE AND ACP'D INSURANCE CUT, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER PER MM 52-11-87. 2 L 7 2 4F 4 F RT A2NM E17NE 20080805 WP 2008 8 5 NWAA082769763 1 20080618 A 3350 BATTERY DOUG DC9 DC941 302207N WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 763NW 47396 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS ROWS OF SEATS IN THE CABIN H AD FAILED. MAINTENANCE REPLACED THE BATTERIES. OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F A6WE 20080805 NM 2008 8 5 F3LA200800310 1 20080610 A 5320 D5347112320300 SUPPORT BRACKET AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 REFERENCE NON ROUTINE 34649. DURING C3 S1 C-CHECK INSPECTION NOTED RT HAND CABIN SUPPORT BRACKET AT LETRAL SHEAR PLATE STATION Y1162 BETWEEN FRAMES 69 AND FRAMES 70 REQUIRE REPLACEMENT DUE TO CORROSION. MAINTENANCE REMOVED AND REPLACED SU PPORT BRACKET IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 SO 2008 8 5 C2XA08RI087 1 20080615 A 2800 367934002 CONDITIONER EMB 145 EMB145XR 3260214 SO WING FUEL INOPERATIVE A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 31131 7342 3815 145705 FLIGHT 2753 - EWR - FLIGHT CREW REPORTED LOSS OF FUEL QUANTITY INDICATION AND FUEL LOW LEVEL WARNING ON EICAS. CREW DEC LARED EMERGENCY AND LANDED ACFT WITHOUT INCIDENT. EWR MAINTENANCE REMOVED AND REPLACED WING FUEL CONDITIONER UNIT AND P ERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080805 WP 2008 8 5 NWAA082789876 1 20080616 A 3397 CONNECTOR DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 785NC 48110 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN LIGHT FOR THE FWD RT OVERWING HATCH WAS INOPERATIVE. MAINTENANCE FOUND THE WIRE RECEPTACLE UNPLUGGED. AFTER CONNECTOR WAS RE-SECURED THE LIGHTS FUNCTIONED WITHOUT PROBLEM. (A) 2 L 7 2 4F RT A6WE 20080805 NM 2008 8 5 F3LA200800286 1 20080602 A 5320 D5347217220500 BEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 REFERENCE NON ROUTINE C044730. DURING C4 S1 C-CHECK INSPECTION NOTED CORROSION ON UPPER SURFACE OF Y1292 RT BEAM 7 INCH ES FORWARD OF FRAME 68. MAINTENANCE REMOVED OLD BEAM Y1292 AND INSTALLED NEW BEAM IN ACCORDANCE WITH THE REQUIREMENTS O F SRM 51-42-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 SO 2008 8 5 CX2A08ON154 1 20080711 A 2810 2770138101 FLAPPER VALVE EMB 145 EMB145XR 3260214 SO RT WING WORN A C2XA O OTHER K FLUID LOSS CR CRUISE 1 SW 27 14168 10967 14500840 FLT 7671 - SLC - PAX NOTIFIED CREW OF FUEL LEAK RT WING AND CREW NOTICED 300LBS OF FUEL LOST. MX PERSONNEL REMOVED AND REPLACED RT FLAPPER VALVE. OPERATIONALLY AND LEAK CHECKED SATISFACTORY AND AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. (A) 2 L 7 2 4F RT 20080805 2008 8 5 NWAA082733162 4 20080614 A 2565 CABLE AIRBUS A319 A319114 3930350 NM ESCAPE SLIDE BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 362NB 01982 RT OVERWING EMERGENCY EXIT ESCAPE SLIDE ACTUATING CABLE FOUND BROKEN. REPLACED RT OVERWING SLIDE EXIT DOOR FLEXIBLE CAB LE ASSEMBLY, CHECKED GOOD. (A) 2 L 7 2 4F RT A28NM 20080805 WP 2008 8 5 NWAA082669881 1 20080606 A 5553 ATTACH ANGLE DOUG DC9 DC951 3022051 WP BS 1266 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 676MC 47652 DURING LINE CHECK FOUND CRACK IN THE RT DORSAL FIN ATTACH ANGLE AT BS 1266. REPAIRED PER EA 98-213301. (A) 2 L 7 2 4F RT A6WE 20080805 NM 2008 8 5 AALA200801483 1 20080602 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 683A 25340 DFW - EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 29D. SYSTEM GROUND CHECK ED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080805 SO 2008 8 5 C2XA08RI093 1 20080619 A 3240 429515 CONTROL UNIT EMB 145 EMB145LR 3260212 SO BRAKE DEFECTIVE A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 16541 15234 145542 FLIGHT 2295 - EWR - FLIGHT CREW REPORTED "BRK INBD INOP" ON EICAS DURING APPROACH. CREW ABORTED APPROACH, AND PROCEEDED WITH NEW APPROACH AND LANDED ACFT UNEVENTFULLY. EWR MAINTENANCE REMOVED AND REPLACED BRAKE CONTROL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080805 EA 2008 8 5 TRAX200800827 1 20080624 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA MID WING INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 908EV 7654 MID WING FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW CRJ 200 AMM 33-51-01. (S) 2 L 7 2 4F RT A21EA 20080806 NM 2008 8 6 AALA200801434 1 20080529 A 2913 PUMP BOEING 757 757223 1384957 NM HYD SYSTEM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 612AA 24488 DFW INFLIGHT T2167/29MAY. LEFT ELECTRIC HYDRAULIC PUMP INDICATION ILLUMINATED ON EICAS. RETURNED TO DFW AND LANDED WIT HOUT INCIDENT. REPLACED LEFT ELECTRIC HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080806 EA 2008 8 6 A6WA200840493 1 20080609 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 319-349 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 SERVICE DOOR LOWER SILL PLATE CORRODED. CORROSION ON SERVICE DOOR LOWER SILL PLATE REMOVED IAW CRJ 200 SRM 51-21-06. ( A) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 A6WA200840494 1 20080609 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 579-621 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 CARGO DOOR LOWER SILL FS 579-621 CORRODED. CORROSION REMOVED IAW CRJ 200 SRM 51-21-06. (A) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 A6WA200840458 1 20080609 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 31 425AW 7663 FLAPS FAILED AT ZERO IN FLIGHT. BRAKE TEMPS WERE IN NORMAL RANGE AT LANDING. COMPLIED WITH RESET PROCEDURE IAW AWAC SU PP 98-018B STEPS 1.3 AND 1.4 FLAPS SYSTEM RESET OK. AIRCRAFT RELEASED FOR SERVICE. (A) 2 L 7 2 4F RT A21EA 20080806 NM 2008 8 6 TSA2008F00000 1 20080615 A 3230 69355006 ACTUATOR BOEING 737 7372X6C 1384552 NM LT MLG LOCK INOPERATIVE A TSAA O OTHER J WARNING INDICATION AP APPROACH 1 WP 13 840AL 23124 FLIGHT 916 LIH-HNL. ON APPROACH CREW SELECTED GEAR DOWN AND NOTED INDICATION FOR LEFT MAIN GEAR NOT LOCKED. CREW PULLE D MANUAL RELEASE HANDLE AND GOT ALL 3 GEARS DOWN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT MAIN GE AR LOCK ACTUATOR IAW AMM 32-32-51 PG 401-403. THE AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A16WE 20080806 EA 2008 8 6 TRAX200800834 1 20080624 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 977EV 7720 REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX .2 INCH IN LENGTH 100% FULL SCREEN HEIGHT. FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD AT LINTEL ATTACHMENT FITTING IAW REO 601R-53-61-1230. REQUIRES PAINT. PAINTED REPAIR AREA IAW SRM 51-25-01. (S) 2 L 7 2 4F RT A21EA 20080804 EU 2008 8 4 08FDEA02562 1 20080630 A 5320 A53612213 SUPPORT AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON SUPPORT C11-19 Y-1456 AND Y1959 SPLICE REPAIR PERFORMED IAW SRM 53-12-15 FIG 207. 2 L 7 2 4F RT A35EU 20080804 WP 2008 8 4 08FDEA02818 1 20080710 A 5347 AGA38551 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 AFT CARGO BILGE SEAT TRACK IS CORRODED AT STA 1831 TO 1840 AND LBL 20. REMOVED CORROSION IAW SRM 51-21-01, VOL II. SEA T TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00, VOL I. REMOVED SEAT TRACK FROM STA 1781 TO 1960 IAW SRM 51-31-01, V OL II. MATERIAL ID FOR THE NEW SEAT TRACK S4929311. MACHINED SCALLOPS AND FORMED TRACK IAW DWG AGA 3855, REV H. DRIL LED AND COUNTERSUNK IAW SRM 51-31-01, VOL II. PART MARKED SEAT TRACK IAW GMM 7-0-1000. ALODINED AND PRIMED IAW SRM 51- 21-01, PGS 21 AND 25, VOL II. INSTALLED NEW SEAT TRACK IAW SRM 51-31-01, VOL II. 2 L 7 3 4F RT A22WE 20080804 EU 2008 8 4 08FDEA02819 1 20080710 A 5340 A5361031839301 ATTACH ANGLE AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 ATTACH ANGLE ALONG FRAME 12A RIGHT IS CRACKED ON FWD SIDE APPROX 6 INCHES BELOW THE FLOOR. REMOVED ANGLE IN REF TO A300 -600F SRM 51-40-21; PARA 6. RECEIVED A NEW ANGLE, PO 624972.1. LOCATED AND DRILLED IN REF TO A300-600F SRM 51-40-21; P ARA 6. INSTALLED IN REF TO AIRBUS DWG A5361037801. 2 L 7 2 4F RT A35EU 20080804 EU 2008 8 4 08FDEA02593 1 20080701 A 5754 A57840120200 PAN AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND ON LT FOLDING NOSE SLAT NR 1 AN UNDEFINED HOLE AT INNER PAN. INNER PAN HAS TO BE CHANGED. REPAIR PERFORMED BY RE PLACEMENT OF INNER PAN IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080804 WP 2008 8 4 AALA200801670 1 20080619 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7509 49803 LGA - EMERGENCY LIGHTS AT OVERHEAD FORWARD CABIN DOOR, FORWARD GALLEY AND COCKPIT INOPERATIVE. REPLACED BATTERY PACK FO R EMERGENCY LIGHTS AT OVERHEAD FORWARD CABIN DOOR, FORWARD GALLEY AND COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080804 WP 2008 8 4 AALA200801440 1 20080530 A 3350 LAMP DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9615W 53562 SFO - EMERGENCY LIGHT AT OVERHEAD SEAT 27D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A6WE 20080804 NM 2008 8 4 AALA200801460 1 20080601 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 DFW - EMERGENCY LIGHT AT SEAT 22G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22G. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080804 EA 2008 8 4 TRAX200800705 1 20080530 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 881AS 7496 EMERGENCY FLOOR TRACK LIGHTING AT 5CD INOP. REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHTING AT 5CD IAW AMM 33-51-01 . OPS CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080804 NM 2008 8 4 2008UALA03672 1 20080701 A 3397 58791 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 339UA 24243 EEL LIGHTS INOP ROW 15 & AFT. FOUND LEAD CABLE AND LIGHT STRIP BAD. REPLACED LEAD CABLE AND LIGHT SEGMENT OP CHECKED G OOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080804 NM 2008 8 4 ZZDA2008132 1 20080724 A 5512 593614318 SKIN BOEING 717 717200 1383700 NM VERTICAL STAB CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 992AT 55136 VERTICAL STAB RT TIP SKIN CRACKED. REPLACED DAMAGED SKIN IAW EA 17-55-01246IR REFERENCE NRWC N046661. MAJOR REPAIR, FORM 337 SUBMITTED. 2 L 7 2 4F TR A6WE 20080804 SO 2008 8 4 C2X2008F00003 1 20080628 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13956 145078 FWD EMERGENCY PROX LIGHT STRIP INOPERATIVE. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT INVERTER IAW AMM 33-50-11. OPS C HECK GOOD. (K) 2 L 7 2 4T RT T00011AT 20080805 CE 2008 8 5 GUU2008F00013 1 20080618 A 3260 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE MLG OUT OF ADJUST A GUUA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 17 46AR UE27 FLIGHT 6005, DURING FLIGHT, LANDING GEAR HANDLE LIGHT ILLUMINATED SEVERAL TIMES HYD FLUID LOW ANNUNCIATOR WAS NOT ILLUMI NATED AND AIRSPEED KEPT UNDER 180KIAS. C/A ADJUSTED RT MLG UPLOCK SWITCH. OPS CHECK NORMAL. (A) 2 L 7 2 4T RT A24CE 20080805 CE 2008 8 5 DXTA200803170 1 20080713 A 2150 A/C PACK CESSNA 750 750 2076810 CE RIGHT SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 952QS 7500200 RT PAC IS CAUSING CABIN SMOKE. TEMP IS OVER 200 DEGREES. PAC IS CAUSING CABIN SMOKE IN BOTH THE "ON" AND "OFF" POSITION. (A) 2 L 7 2 4J RT T00007WI 20080805 NM 2008 8 5 C8G2008F00006 1 20080708 A 2421 GENERATOR BOEING 727 7272A1 138407F NM NR 1 MALFUNCTIONED A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 287SC 21345 AFTER TAKEOFF DURING CLIMB OUT, THE NR 1 GENERATOR EXPERIENCED A SPEED FAULT WITH THE NR 3 GENERATOR PREVIOUSLY DEFERRED . THE AC RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED. THE NR 1 CSD S PEED SWITCH CONNECTOR WAS RESEATED, RERACKED, GENERATOR CONTROL PANEL AND RESET CIRCUIT BREAKER. OPERATED ENGINE AND PE RFORMED OPS CHECKS, CHECKED GOOD. NO OTHER DEFECTS WERE NOTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F A3WE 20080805 NM 2008 8 5 UIE2008F00016 1 20080630 A 7830 SKIN BOEING 747 747243B 1384830 NM THRUST REVERSER DENTED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 NR 1 ENGINE LT "C" DUCT (REVERSER) EXTERIOR FOUND WITH 1 EACH DENT AT 7 O`CLOCK POSITION. NR 1 REVERSER EXTERIOR SURFAC E DENT REPAIRED IAW CF650 ENGINE MANUAL 78-32-01, REPAIR NR 4. (K) 2 L 7 4 4F RT A20WE 20080805 SO 2008 8 5 FFK2008F00000 1 20080618 A 2910 HYC5005 POWERPACK PIPER PA34 PA34200T 7103406 SO HYD SYSTEM DEFECTIVE E FFKA O OTHER J WARNING INDICATION AP APPROACH 1 EA 39 6935C 347870167 PILOT EXPERIENCED PROBLEM WITH HIS LANDING GEAR WHILE ON APPROACH. THE GEAR UNSAFE LIGHT FLICKERED ON AND OFF WHILE ENR OUTE; WHEN GEAR LEVER WAS PUT DOWN, NOTHING HAPPENED. AFTER EXECUTING A CHECKLIST TO TROUBLESHOOT, HE DETERMINED THAT S OMETHING IN THE SYSTEM HAD MALFUNCTIONED. MAINTENANCE TROUBLESHOT PROBLEM TO A DEFECTIVE HYDR POWERPACK PN HYC5005, SN AH10437, TIS/TSO-43 HOURS, DATE OF LAST O/H MARCH 13, 2008. (K) 1 L 7 2 3O A7SO 20080805 NM 2008 8 5 DHL2008F00024 1 20080531 A 5754 BRACKET BOEING 727 7272M7 138407S NM LT KRUEGER FLAP CRACKED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 LT WING NR 1 KRUEGER FLAP ACTUATOR INBOARD AND OUTBOARD ATTACH BRACKETS ARE CRACKED IN THE CORNERS. REMOVED BRACKETS (2 EACH) IAW B727 SRM 51-30-2. FABRICATED BRACKETS WITH 2024-T3 .036 3.5" X 7.5" PO 9006767 IAW BOEING ENGINEERING DOCUME NT 65-16275 AND B72 SRN 51-20-1. LOCATED, DRILLED AND DEBURRED HOLES AT BRACKET IAW B727 SRM 51-30-5. TREATED PRIMED N EW BRACKETS IAW B727 SRM 51-10-2. INSTALLED NEW BRACKETS IAW B727 SRM 51-30-2 AND DOCUMENT 65-16725 DWG REV D PL REV OR G. (A) 2 L 7 3 4F A3WE 20080805 EA 2008 8 5 TRAX2008000921 1 20080718 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 F/A REPORTS THAT MAIN ENTRY DOOR IS DIFFICULT TO OPEN. PERFORMED OPERATIONAL TEST OF PAX DOOR IAW CRJ200 AMM 52-11-00-7 10-801. NO DIFFICULTY OPENING OR CLOSING DOOR. OPS CHECKS GOOD. OK FOR SERVICE. (A) 2 L 7 2 4F RT A21EA 20080805 WP 2008 8 5 WXOA070206 1 20080528 A 3350 AD4002 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 887GA 49932 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETUR NED TO SERVICE. (A) 2 L 7 2 4F A6WE 20080805 SO 2008 8 5 C2XA08IA159 1 20080708 A 3397 M2430842F CONNECTOR EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS OVERHEATED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 27 13936 145025 TUL - FLIGHT 2845, THE CREW REPORTED SMOKE AND A SMELL OF FIRE AT SEAT 18A DURING DESCENT. THE AIRCRAFT LANDED AT TUL W ITHOUT INCIDENT WHERE MAINTENANCE MEL`D THE PSU FOR SEAT 18A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT CONTINUED TO IAH ON FLIGHT 2886 WHERE MAINTENANCE REMOVED AND REPLACED A CONNECTOR ON THE PSU, OPERATIONALLY CH ECKED WITH NO DEFECTS, REMOVED THE MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080805 WP 2008 8 5 NWAA083149869 1 20080718 A 3397 CONNECTOR DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS LOOSE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 778NC 48100 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAI LED. MAINTENANCE FOUND A LOOSE ELECTRICAL CONNECTOR. RE-SEATED THE CONNECTOR AND OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F RT A6WE 20080805 EA 2008 8 5 TRAX200800839 1 20080625 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 CATERING ADVISED, CANNOT OPEN SERVICE DOOR FROM OUTSIDE. CLEANED AND LUBED SERVICE DOOR HANDLE. OPS CHECK AFTER SEVERA L CYCLES. REF CRJ200 AMM 52-41-03. (S) 2 L 7 2 4F RT A21EA 20080805 NM 2008 8 5 AALA200801511 1 20080604 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 636AM 24594 DFW - EMERGENCY LIGHT AT SEAT 16D HAD BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKE D NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080805 EA 2008 8 5 TRAX200800825 1 20080623 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 F/A REPORTS MAIN DOOR HARD TO OPEN. CLEANED AND LUBED DOOR HANDLE AMM 52-11. (S) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 TRAX200800818 1 20080621 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 930EV 8014 IN AFT EQUIP BAY, FS 625, RT CLIP CRACKED AT APPROX 4 O`CLOCK POSITION. REMOVED AND REPLACED FS 625, RT CLIP AT APPROX 4 O`CLOCK POSITION. ALL WORK DONE IAW CRJ 200 SRM 51-42-06. (S) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 A6WA200840345 1 20080414 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 605 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 443AW 7781 FLOOR LANDING PLATE CRACKED AT FS 605, LBL 43. DAMAGE CUTOUT, NDT PERFORMED ON CUTOUT, REDUNDANT HOLE PLUGGED IAW REO 6 01R-53-61-433. 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 A6WA200840504 1 20080605 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 310-349 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 PAX DOOR LOWER SILL CORRODED FS 310.00 AND FS 349.00. CORROSION ON PAX DOOR LOWER SILL BLENDED IAW CRJ 200 SRM 51-21-06 . (A) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 TRAX200800698 1 20080528 A 3230 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 681BR 7680 AFTER TAKEOFF RECEIVED A GEAR DISAGREE AND NOSE GEAR DOOR MESSAGE NOSE GEAR FAILED TO RETRACT (AIRCRAFT RETURNED TO FAY AFTER TAKEOFF--EMERGENCY DECLARED). FLT 4640 CX. FOUND CODE D046 ERR IN PSEU (NOSE GEAR RETRACT SOLENOID) (SELECTOR VA LVE). REMOVED AND REPLACED NOSE GEAR SELECTOR VALVE IAW M/M 32-33-10. CYCLED GEARS 12X WITH NO DEFECTS, OPS AND LEAKS CHECK GOOD. ACFT OK FOR SERVICE. (S) 2 L 7 2 4F RT A21EA 20080806 WP 2008 8 6 AALA200801414 1 20080527 A 2560 3913359545 RELEASE CABLE DOUG DC9 DC983 3022083 WP TAILCONE FRAYED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 951TW 53470 TUL - TAILCONE RELEASE CABLE IS FRAYED FROM LEFT HAND LATCH ASSEMBLY TO UPPER SUPPORT BRACKET AND FROM PULL HANDLE TO UP PER LEFT AND BLOCK ASSEMBLY. REPLACED TAIL CONE RELEASE CABLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A6WE 20080806 EA 2008 8 6 TRAX200800819 1 20080621 A 2612 FIRE LOOP CNDAIR CL600 CL6002B19 1900309 EA ENGINE OUT OF POSITION A ASOA A UNSCHED LANDING W N INADEQUATE Q C FALSE WARNING CL CLIMB 1 SO 27 825AS 7207 CLIMBOUT APPROX 12K FT RECEIVED MASTER WARNING L 14TH DUCT WARNING. INITIALLY CAME ON, THEN WENT OUT, THEN CAME ON AGAI N. RAN QRH WARNING RETURNED. RAN QRH. (RETURN TO BTR, CAPTAIN DECLARED EMERGENCY). FLT 4816 DEL 265 MINS. INSPECTIO N OF LT 14TH STAGE DUCT AND BLEED LEAK DETECTION SYSTEM REVEALED LEAK DETECTION LOOP FOULING ON STRUCTURE WITHIN PYLON A REA. REPOSITION LOOP AND OPS CHECKED SYSTEM IAW AMM 36-21-00. NO FURTHER DEFECTS NOTED AT THIS TIME. (S) 2 L 7 2 4F RT A21EA 20080806 SO 2008 8 6 C2XA08RI091 1 20080617 A 3350 110049 CHARGER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS DEFECTIVE A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 34111 145659 FLIGHT 2391 - EWR - DURING ROUTINE MAINTENANCE, EWR MAINTENANCE FOUND MULTIPLE EMERGENCY EXIT LIGHTS INOPERATIVE AT OVER WING EXITS. MAINTENANCE REMOVED AND REPLACED NR 3 EMERGENCY BATTERY CHARGER ASSY AND PERFORMED OPERATIONAL CHECK SUCCES SFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080806 NM 2008 8 6 AALA200801431 1 20080528 A 3350 COVER BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 776AN 29582 DFW - EMERGENCY LIGHT AT RIGHT NR ONE DOOR MISSING COVER AND WIRING IS EXPOSED. REPLACED COVER FOR EMERGENCY LIGHT AT R IGHT NR ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 SO 2008 8 6 C2XA08ON143 1 20080617 A 2750 FLAP SYSTEM EMB 145 EMB145XR 3260214 SO TE FLAPS MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 16183 8797 4974 14500914 FLT 7696 - LAP - FLIGHT CREW REPORTED FLAP OVERSPEED AT 45 DEGREES, 171 KNOTS FOR 3 SECONDS. MAINTENANCE FERRY FLIGHT T O ONT BUT IT HAD TO CLEAR CUSTOMS IN LAX. MAINTENANCE AND INSPECTION DEPARTMENT PERFORMED NDT AND VISUAL INSPECTION ON FLAP TRACKS. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4F RT 20080806 NM 2008 8 6 AALA200801734 1 20080629 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 752AN 30260 MIA - EMERGENCY LIGHT AT SEAT 26C BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECK ED NORMAL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20080806 WP 2008 8 6 AALA200801389 1 20080525 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 568AA 49349 DFW - EMERGENCY LIGHT AT SEAT ROW 18D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 18D. SYSTEM GROUND C HECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A6WE 20080806 CE 2008 8 6 DXTA200803180 1 20080717 A 3150 WARNING MESSAGE CESSNA 750 750 2076810 CE PITCH FEEL FALSE ACTIVATION E DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 930QS 7500130 THE "PITCH FEEL FAIL" AMBER CAS MESSAGE ILLUMINATED AT 3000 FEET AFTER TAKEOFF. MESSAGE WENT OUT AFTER LANDING. (S) 2 L 7 2 4J RT T00007WI 20080806 NM 2008 8 6 KCSA081328 1 20080717 A 5411 FRAME BOEING 747 747246B 1384864 NM NR 4 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 NR 4 PYLON REAR ENG MOUNT BULKHEAD OUTBOARD FWD FRAME WEB CRACKED .750 INCH AT NAC STA 221.9. (S) 2 L 7 4 4F RT A20WE 20080806 EA 2008 8 6 TRAX200800909 1 20080714 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 OUTBOARD CLIP AT FRAME STA 484, LBL 27 IS CRACKED. REMOVED CRACKED CLIP FROM PREVIOUS REPAIR. FABRICATED NEW - 1 CLIP FROM 2024 T-3. LPI WAS ACCOMPLISHED ON -1 CLIP FROM 2024 T-3. 063 REF REO 601R-53-41-059 AND CRJ 200 AMM 51-20-08. MB1 4369 7/14/2008. NO DEFECTS NOTED. OK TO INSTALL. (S) 2 L 7 2 4F RT A21EA 20080806 EU 2008 8 6 KCS2008F00002 1 20080715 A 5310 MY20812001 FRAME AMD FALCON FALCON20 2730103 EU WINDSHIELD CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 192CK 23618 18906 192 CENTER WINDSHIELD FRAME WAS FOUND CRACKED DURING INSPECTION. THE WINDOW FRAME WILL BE REPLACED USING APPROVED PROCEDURE S, DRAWINGS, AND NEW WINDOW FRAME. NOTE, COMPLETE PART NUMBER ON FRAME IS NOT LEGIBLE. (S) 2 L 7 2 4F RT A7EU 20080807 NM 2008 8 7 KCSA081335 1 20080722 A 5310 DOOR FRAME BOEING 747 747122 1384872 NM BS 800 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 LT BS-800 L-2 DOOR CUT OUT HAS A .5" CRACK AT STR-18L. (A) 2 L 7 4 4F RT A20WE 20080807 NM 2008 8 7 KCSA081345 1 20080724 A 5411 FRAME BOEING 747 747122 1384872 NM NR 2 NACELLE GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 NR 2 PYLON NAC STA 200 HAS A DEEP GOUGE AT FRAME BETWEEN STR 1 & 2 RT SIDE. (A) 2 L 7 4 4F RT A20WE 20080807 NM 2008 8 7 KCSA081354 1 20080729 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 745-800 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STR 34L CORRODED BETWEEN BS 745 AND 800. (S) 2 L 7 4 4F RT A20WE 20080807 NM 2008 8 7 CALA0800722 1 20080716 A 5340 693535214 STRINGER CLIP BOEING 737 737524 1384721 NM BS 380 S8R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 RIGHT SIDE STA 380 STRINGER 8 CLIP CRACKED. REMOVED DAMAGED STRINGER CLIP AT STA 380 RT S-8 RECEIVED NEW FROM STOCK LOC ATED, DRILLED AND INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080807 WP 2008 8 7 AALA200801556 1 20080606 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 59523 49915 DFW - EMERGENCY LIGHT AT CABIN LENS DAMAGED. REPLACED LENS FOR EMERGENCY LIGHT AT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080807 NM 2008 8 7 CALA0800732 1 20080719 A 5312 6516300291 BULKHEAD BOEING 737 737524 1384721 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 STATION 178 BULKHEAD AT WL 234 RBL 17 WEB IS CRACKED AT FASTENER HOLE. REPLACED 178 BULKHEAD CENTER WEB PER EC/RA 5310- 04799. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 CALA0800734 1 20080719 A 5312 6516300291 BULKHEAD BOEING 737 737524 1384721 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 STATION 178 BULKHEAD AT WL 207. FASTENER HOLE CRACKED IN WEB. REPLACED 178 BULKHEAD CENTER WEB PER EC/RA5310-04799. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 AALA200801467 1 20080602 A 3350 767 LAMP BOEING 767 767223 1385123 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 321AA 22322 LAX - EXTERIOR EMERGENCY LIGHT AT LEFT NR ONE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LT NR ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080807 NM 2008 8 7 HNAA0800232 1 20080715 A 3350 6138443 BATTERY DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHT DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 930HA 126 EMERGENCY EXIT SIGN FWD RT INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY. OPS CHECK GOOD. (S) 2 H 7 2 4T RT A13NM 20080807 EU 2008 8 7 F3LA200800492 1 20080715 A 5321 D5367301800100 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 943FR 18 2518 DURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151UG WAS PUNCTURED. MAINTENANCE RECORDED THAT THIS IS EITHER A DUPLICATE WRITE-UP (161UG- NON ROUTINE C047467) OR SHOULD HAVE BEEN WRITTEN AS 152UG, WHICH HAD DAMAGE ALSO. THE DAMAGE REPAIR FOR 152UG WAS PERFORMED IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMP LETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F 4 F RT A28NM E37NE 20080807 NM 2008 8 7 AALA200801741 1 20080701 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 NRT EMERGENCY LIGHT AT LT NR 1 DOOR INOPERATIVE. REPLACED BATTERY PACK M33093 FOR EMERGENCY LIGHT AT LT NR 1 DOOR. SYS TEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20080807 NM 2008 8 7 AALA200801724 1 20080628 A 2560 BATTERY BOEING 777 777223 1385213 NM FLASHLIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 LHR EMERGENCY FLASHLIGHT AT LT NR 2 DOOR FORWARD SEAT INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASH LIGHT AT LT NR 2 DOOR FORWARD SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20080807 NM 2008 8 7 AALA200801475 1 20080602 A 3350 60030451 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 674AN 29424 DFW - EMERGENCY LIGHT EXIT SIGN AT OVERHEAD MID LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT EXIT SI GN AT OVERHEAD MID LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 AALA200801458 1 20080601 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 DFW - EMERGENCY LIGHT AT SEAT 25G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25G. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 WP 2008 8 7 AALA200801401 1 20080526 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 245AA 49257 LGA - EMERGENCY LIGHT AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080807 NM 2008 8 7 08FDEA02628 1 20080702 A 5753 SKIN BOEING BOEING 727 727225 1384077 NM TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 LEFT WING INBD TE MID FLAP S/N BN 492 HAS LWR SURFACE DELAM AT 3 INCH FWD OF AFT EDGE AND 20 INCH THROUGH 336 INCH OB OF INBD END. REPLACED MID FLAP, NEW SERVICEABLE MID FLAP. INSTALLED ON W/C 75C075-00, THIS IS CLASSIFIED AS A MINOR REPA IR. 2 L 7 3 4F A3WE 20080807 EU 2008 8 7 08FDEA02630 1 20080702 A 5347 A538131090200 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN ARTICULATING SEAT TRACK RIGHT NR 6 BETWEEN FRAME 38.2 AND FRAME 40 HAS AN ATTACH HOLE THAT IS WORN OUT OF LIM ITS. RECEIVED A NEW SEAT TRACK, PO 624240.1. LOCATED AND DRILLED THE NEW SEAT TRACK IAW A300-600 SRM 51-40-40. TRANS FERRED THE ATTACH CLIPS FROM THE OLD TRACK IAW A300- 600M SRM 51-40-21; PARA 7. INSTALLED THE NEW ARTICULATING SEAT TRACK IAW FEDEX A300-600 EO E6-5310-7-3322 PT1. 2 L 7 2 4F RT A35EU 20080807 NM 2008 8 7 08FDEA02768 1 20080708 A 5730 SKIN DOUG MD11 MD11F 3023600 NM LT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 601FE 48401 11 FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING HFEC OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTO UT. 2 L 7 3 4F RT A22WE 20080808 WP 2008 8 8 08FDEA02770 1 20080709 A 5330 ACA3554501 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 EXT FUSELAGE LWR SURFACE FOUND CRACK ON SKIN (UPPER CORNER). 2 L 7 3 4F RT A22WE 20080808 WP 2008 8 8 08FDEA02772 1 20080709 A 5330 ABA70464 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 EXT FUSELAGE LWR SURFACE FOUND DEEP DENT 2 INCH BY 1 INCH DEEP .074" ON SKIN. 2 L 7 3 4F RT A22WE 20080808 NM 2008 8 8 08FDEA02775 1 20080709 A 5340 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 601FE 48401 MAIN DECK CARGO DOOR LOWER JAMB SPOOL FITTING NR 2 FOUND HOLES A, B, C AND D OVERSIZED TO 0.520 INCH. 2 L 7 3 4F RT A22WE 20080808 NM 2008 8 8 08FDEA02784 1 20080709 A 5313 655848825 STRINGER BOEING 727 727225 1384077 NM BS 945 S18A LT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 LT FUSELAGE OVERWING BS 945, STR18A (L) REMOVED DAMAGED SECTION OF LT S-18A, INSPECTED SKIN AREA UNDER REMOVED STRINGER SECTION AND FUSELAGE SKIN (NO DEFECTS NOTED). DRILLED HOLES IN REPAIR ANGLES, FABRICATED SHIMS AND INSTALLED ALL REPAIR PARTS. REFERENCE EA NR 7-5310-113997. CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080808 NM 2008 8 8 08FDEA02787 1 20080709 A 5330 6554580 SKIN BOEING 727 727225 1384077 NM ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 HEAVY CHAFE MARK FROM WING-TO-BODY FAIRING ON RT SIDE OF FUSELAGE AT BS 950D 10 TO 950D 13 WL 197 BLENDED DAMAGE REF SR M 53-30-1. ORIGINAL THICKNESS .140 REMOVED .038 AT DEEPEST BLEND OUT REMAINING MATERIAL .102 MATERIAL LOSS OUT OF LIMI TS REF SRM 51-30-1. THIS IS CLASSIFIED AS A MAJOR REPAIR. AREA TO BE REPAIRED ON N/R N00256. 2 L 7 3 4F A3WE 20080808 EU 2008 8 8 08FDEA02791 1 20080523 A 5347 A5361221420001 SEAT TRACK AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 CABIN FLOOR, CORROSION ON TRACK Y730 BETWEEN FR 11-11A. TRACK REPLACED AS PER SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02796 1 20080709 A 5230 STRUCTURE BOEING 727 727233 138408A NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 NUMBER 3 CARGO DOOR LOWER FWD "T" CHORD CRACKED AT FASTENERS REPAIRED LOWER FWD "T" CHORD. REMOVED LWR INNER DOOR SKIN REF SRM 51-30-2. FABRICATED REPAIR ANGLES AND FILLER REF SRM 51-40-04 PG 14-16 FIG 3. TREATED AND PRIMED REPAIR PARTS REF SOPM 20-44-04 PG 3 AND 20-43-03 PG 6. INSTALLED REPAIR ANGLES AND FILLER SRM 51-40-04 PG 14-16. INSTALLED LWR INNE R DOOR SKIN REF SRM 51-30-02 PG 2 AND 8. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080808 NM 2008 8 8 08FDEA02633 1 20080702 A 5720 65267861 WEB BOEING 727 727225 1384077 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 LEFT WING INBD T/E NR 4 JACKSCREW/ELEPHANT EAR FAIRING. CRACKED AT UPPER AFT INBD CLOSER WEB INSTALLED DOUBLER AND FILL ER REF SRM 51-40-2 PG 6, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080808 NM 2008 8 8 08FDEA02634 1 20080702 A 5330 6554583 SKIN BOEING 727 727225 1384077 NM ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 LT LOWER FUSELAGE WING TO BODY FAIRING BLENDED AREA OUT OF LIMITS. DAMAGE AT LAP JOINT STR 26L - 2.6' FWD OF FR 950E AN D DAMAGE AT 2.7L BELOW STR 26L REMOVED AND REINSTALLED FAIRING SUPPORT, REMOVED DAMAGE AREA, OUT OF LIMITS. FABRICATED DOUBLER AND STRUCTURAL FILLER, REF SRM 51-30-02, 53-30-3 FIG 5 AND FIG 24. TREATED AND PRIMED, AND TEFLON COATED REF 51 -30-3 FIG 24. INSTALLED REPAIR PARTS REF SRM 53-30-3 FIG 5 AND 24. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080808 EU 2008 8 8 08FDEA02736 1 20080708 A 5730 A57240880 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON UPPER SURFACE OF BOTTOM SKIN RIB 6A-7A, AFT OF REAR SPAR, LT WING. REPAIR PERFORMED BY BLEND OUT COR ROSION AND REPROTECT THE AREA IAW RAS/BAE/1007293/2008 ISS A, APPROVED BY EA 6-5751-120113. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02738 1 20080708 A 5220 A53970875200 COVER AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND SCRUB MARKS AT EMERGENCY EXIT, C 56-57.1, P14-15A, LT ON COVER SHEET. REPAIR PERFORMED BY REWORK TO SMOOTH CONTOU R, NDT FOR CRACK FREE CONDITION AND FLAP PEENING IAW RAS/EFW/9000052/2008 ISS A, APPROVED BY EA 6-5316-123022. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02703 1 20080704 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 AFTER REMOVAL OF OLD DOUBLER REPAIR IAW DR 276 FOUND STRINGER 2.9 DAMAGED AT LT INNER FLAP. REPAIR PERFORMED IAW RAS/FO K/150/2008 ISS C, APPROVED BY EA 6-5752-123003. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02499 1 20080626 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 609FE 48549 DURING OPEN HOLE HFEC INSPECTION, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATION AT HOLE NR B (3RD LAYER). MOUNTING HOLE NR B ON THE MAIN CARGO DOOR NR 7 JAMB SUPPORT BUSHING REPAIR CARRIED OUT AS PER SRM 53- 50-00 FIG 10 VOL I. CRACKED FITTING ON NR 7 JAMB AREA REMOVED AND REPLACED WITH A NEW FITTING AS PER SRM 51-33-01 VOL I I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080808 EU 2008 8 8 08FDEA02742 1 20080708 A 5753 A57960000002 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND OLD DOUBLER REPAIR ON LT INNER FLAP UPPER SKIN NEAR RIB 27, STRG 2.1 AND 2.2 WITHOUT AI APPROVAL. DOUBLER REPAIR RENEWED IAW RAS/FOK/198/2008 ISS A, APPROVED EA 6-5752-123008. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02745 1 20080708 A 5340 A53973612204 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CRACK IN CONNECTING FITTING C 62 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02726 1 20080707 A 5320 WEB AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 THE CABIN FLOOR WEB AT FRAME C28 - C30 LBL 78-98 HAS CORROSION. REMOVED PANELS (2EA) IAW A300-600 SRM 51-40-22. LOCATE D AND DRILLED PANELS (2EA) IAW A300-600 SRM 51-40-21 AND SRM 51-40-40; PG 1. MACHINED A WEB IAW AIRBUS DWG A53781984 (1 EA). ALODINED AND PRIMED IAW AMM 51-21-00 AND AMM 1300 51-23/10. MATERIAL USED 2024- T3, PO 606256.2 AND PO 65440 75.2. MARKED PANEL P/N FXA537781984 IAW FEDEX GMM 7-0-1001 AND AIRBUS DWG A53781984. INSTALLED PANELS IAW A300-600 SR M 51-40-22. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02727 1 20080707 A 5320 WEB AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 THE CABIN FLOOR WEB FROM FRAME C26 - C28; LBL 78 - 98 HAS CORROSION. REMOVED PANEL IAW A300-600 SRM 51-40-2. LOCATED A ND DRILLED PANELS IAW A300-600 SRM 51-40-21 AND SRM 51-40-40;PG1. INSTALLED PANELS IAW A300-600 SRM 51-40-22. REMOVE D AND REINSTALLED SEAT TRACK SPLICE IAW IAW A300-600 SRM 51-40-22, PO 624383.1 AND 624075.2. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02729 1 20080707 A 5754 SLAT TRACK AIRBUS 300 A300F4605R 3930327 EU RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 RIGHT WING NR 3 SLAT NR 10 TRACK LOWER LUG BOLT IS CRACKED. REMOVED AND REPLACED RIGHT WING NR 3 SLAT; NR 10 TRACK LOWE R BOLT IAW FEDEX A300-600 AMM 27-80-12-04; PG 2; STEP D-4. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02753 1 20080602 A 2550 A25771305 CARGO TRACK AIRBUS 300 A300B4622R 3930312 EU CARGO BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 FWD CARGO COMPT ROLLER TRACK NR 4 BETWEEN FR 27-32 WITH CORROSION. NEW ROLLER TRACK INSTALLED AS PER AMM 25-52-51-4-01. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02754 1 20080708 A 5313 655457446 STRINGER BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 CABIN S3L HAS CORROSION FROM BODY STA 720A-740 REMOVED CORROSION FROM STA 720A - 740 STR 3L. MATERIAL THICKNESS .045 AN D .056, MATERIAL LOSS .008 TO .015 ALL AREAS OUT OF LIMITS. REMOVED DAMAGED STR 3L STA 720A 12 TO 740. REMOVED AND REI NSTALLED STR 3L CLIPS AT STA 720B, 720C, 720D, 720E AND 720F. FABRICATED NEW STRINGER 3L STA 720A 12 AND 720 AND SPLICE PLATES. TREATED, PRIMED AND TOP COATED SKIN AT 3L STR 720-740. REF SRM 51-30-2 P1-6. 51-10-2 PG7, 53-10-1 PG 1-2A FIG 1, 53-10-3 PG 5-8B, AND MM 51-20-151-7. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080808 EU 2008 8 8 08FDEA02730 1 20080707 A 5321 B5327027600800 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN DECK FLOORBOARD NR 251 QH IS CRACKED. FABRICATED A NEW FLOOR PANEL IAW FEDEX DWG SRZ 25-005; REV F. MATERIAL ID A 402 H 35039-003, PO 622013.1 IAW FEDEX DWG SRZ 25-005; REV F. PART MARKED IAW FEDEX GMM 7- 0-1000. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02526 1 20080627 A 5321 B5327047602700 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 231 AH IS CRACKED AND CRUSHED. FABBED NEW PANEL, POTTED EDGES, CURED, SANDED, POTTED INSERT S, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02644 1 20080703 A 5320 B5327052100200 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CARGO DECK FLOOR PANEL 232 BH AT FRAME 28; RBL 97 HAS A BROKEN CORNER. FABBED A NEW PANEL IAW FEDEX DWG SRZ 25-005 , REV F. MATERIAL ID A 402 H 35039-003IAW FEDEX DWG SRZ 25-005, REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02646 1 20080703 A 5320 B5327047602800 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CABIN FLOOR PANEL 231 YG UPPER SURFACE HAS NUMEROUS PUNCTURES AND THE AFT END IS CRUSHED AND BROKEN. FABBED A NEW PANEL IAW FEDEX DWG SRZ 25-005; REV F. MATERIAL ID A 402 H 35039-003 IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02647 1 20080703 A 5321 B5327036100600 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN DECK FLOORBOARD 252 DH EDGE IS BROKEN. FABBED A NEW FLOOR PANEL IAW FEDEX DWG SRZ 25-005; REV F. MATERIAL ID A 4 02 H 35039-003 IAW FEDEX DWG SRZ 25-005; REV F. PART MARKED IAW FEDEX GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02805 1 20080710 A 5754 A53910219203 SUPPORT AIRBUS 300 A300B4622R 3930312 EU KRUEGER FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON KRUEGER FLAP STRUCTURE RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02597 1 20080701 A 5340 A53974321004 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORRODED CORNER FITTING AT C 63 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02693 1 20080704 A 5330 A53970852200 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON SKIN PANEL AT EMERGENCY EXIT C56A-57A, P15 LT REPAIR PERFORMED BY SMOOTH BLEND OUT, NDT FOR CRACK FRE E AND FLAP PEENING IAW RAS/EFW/9000045/2008 IIS.B, APPROVED BY EA 6-5316-120052. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02651 1 20080703 A 5415 A5461254620095 FITTING AIRBUS 310 A310203 3930313 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 423FE 281 NR 2 ENGINE PYLON SPIGOT RECEPTICLE FITTING BEARING RACE CORRODED. REMOVED LEVEL 1 CORROSION, REMOVED AND REPLACED NR 2 ENGINE PYLON UPPER AND LOWER SPIGOT FITTINGS IAW FEDEX EA 6-5450-121273, RELEASE DATE 20 MAY, 2008. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02763 1 20080708 A 5754 SLAT TRACK AIRBUS 300 A300F4605R 3930327 EU LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 LEFT WING NR 2 SLAT; NR 5 TRACK LOWER MOUNT BOLT IS CRACKED. REMOVED DAMAGED BOLT AND REPLACED WITH A NEW BOLT IAW A30 0-600 AMM 27-80-12-4. TOOL NR T8342K. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02602 1 20080701 A 5100 NONE AIRBUS 300 A300B4622R 3930312 EU NONE NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 743FD 630 FOUND OLD FILLER REPAIR ON CROSSBEAM C 57.2 LT BETWEEN Y-140 AND Y-1470 WITHOUT ANY OLD DOCUMENTATION. REPAIR PERFORMED IAW SRM 53-10-15 FIG 208. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02603 1 20080701 A 5315 A53974222202 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND IN AFT CARGO COMPARTMENT CORRODED CROSSBEAM AT C 66, AD SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02604 1 20080701 A 5310 A53973100200 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON BEAM 10, C 67-69, P 45 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02605 1 20080701 A 5310 A53973057200 BEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND NICKS AND OLD REWORKS ON BEAM SECTION, C 67-69, P 45 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080807 NM 2008 8 7 KCSA081343 1 20080724 A 5411 RIB BOEING 747 747122 1384872 NM NR 2 NACELLE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 #2 PYLON NAC STA. 180 RT SIDE OF SUPPORT RIB DAMAGED AT NACELLE ANTI-ICE PRESSURE SWITCH MOUNT BRACKET FORWARD ATTACH PO INT. (A) 2 L 7 4 4F RT A20WE 20080807 NM 2008 8 7 KCSA081333 1 20080721 A 5420 STIFFENER BOEING 747 747122 1384872 NM NR 2 PYLON DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 #2 PYLON NAC STA 180 BULKHEAD STIFFENER DAMAGED ON AFT CENTER SIDE OF BULKHEAD. (A) 2 L 7 4 4F RT A20WE 20080807 NM 2008 8 7 KCSA081338 1 20080722 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 710-730 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STA 710 TO 730 STR-34L HAS DAMAGE ON UPPER FLANGE OF STRINGER. (A) 2 L 7 4 4F RT A20WE 20080807 NM 2008 8 7 2008UALA03708 1 20080705 A 2780 FLAP SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LE FLAPS INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 351UA 24319 LEADING EDGE FLAPS FAILED TO RETRACT. FLIGHT DIVERTED. REPLACED FLAP SLAT ACCESSORY UNIT. SHOP FINDINGS: NO FAULT FOU ND. 2 L 7 2 4F 4 F RT A16WE E21EU 20080807 NM 2008 8 7 CALA0800735 1 20080721 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM EMERGENCY LIGHTS INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 76054 29449 AISLE EMERGENCY LIGHTS FROM ROWS 1-4 DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK CHARGER AND B ATTERY PACK IAW AMM 33-51-07. BATTERY PACK S/N 83779 BATTERY CHARGER S/N 17660. 2 L 7 2 4F RT A1NM 20080807 WP 2008 8 7 AALA200801762 1 20080703 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 479AA 49654 LGA - EMERGENCY LIGHTS AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD GALLEY. SY STEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080807 NM 2008 8 7 AALA200801773 1 20080704 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 175AN 32394 DFW - EMERGENCY LIGHT AT SEAT 16D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CH ECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 AALA200801750 1 20080701 A 3350 SHROUD BOEING 737 737823 13844BZ NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 909AN 29511 DFW - EMERGENCY LIGHT AT SEAT ROW 13D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND C HECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 AALA2008017373 1 20080522 A 2821 SWITCH BOEING 767 767223 1385123 NM FUEL FILTER INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 328AA 22328 JFK INFLIGHT T117/23MAY. CREW REPORTED BOTH ENGINE FUEL FILTER CLOG INDICATIONS. RETURNED TO JFK AND LANDED WITHOUT IN CIDENT. REPLACED LT AND RT ENGINE FUEL FILTERS. REPLACED LT AND RT ENGINE FUEL FILTER DIFFERENTIAL PRESSURE SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080807 NM 2008 8 7 AALA200801547 1 20080606 A 3397 8111417201 CONTACT BOEING 757 757223 1384957 NM EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 643AA 24601 JFK - EMERGENCY LIGHT AT RT AFT OVERWING INOPERATIVE. REPLACED CLIP FOR EMERGENCY LIGHT AT RT AFT OVERWING. SYSTEM GRO UND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 AALA200801465 1 20080602 A 3350 0201804001 LENS BOEING 767 767223 1385123 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 321AA 22322 LAX - EMERGENCY LIGHT AT SEAT 20B MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20B. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080807 NM 2008 8 7 AALA200801390 1 20080525 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 684AA 25341 DFW - EMERGENCY LIGHT AT SEAT ROW 18D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 18D. SYSTEM G ROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 SO 2008 8 7 C2XA08CL074 1 20080629 A 2131 22250N030301 CONTROLLER EMB 145 EMB145LR 3260212 SO CABIN PRESSURE INTERMITTENT A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 29906 14131 14131 145472 CLE FLIGHT 2542 - THE CREW REPORTED THE ACFT WOULD NOT PRESSURIZE. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT . MAINTENANCE INSPECTED AND REPLACED THE DIGITAL CONTROLLER. OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4T RT T00011AT 20080807 SO 2008 8 7 C2XA08SH085 1 20080618 A 5751 14569009610 FITTING EMB 145 EMB145LR 3260212 SO RT AILERON WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 10575 145640 SHV - DURING C-CHECK IT WAS FOUND THAT THE RT AILERON PCA FITTING HAD MIGRATED HAT BUSHINGS. THE HOLES WERE FOUND TO BE WORN OUT OF LIMITS AND WOULD NOT RETAIN THE BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FITTING IAW CONTIN ENTAL EXPRESS EC5750-01177. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080807 SO 2008 8 7 C2XA08SH082 1 20080611 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14974 145161 SHV - DURING C-CHECK IT WAS FOUND THAT THE RT OMEGA BEAM HAT SECTION WAS CORRODED AROUND NUT PLATE HOLES AT FRAME 18. M AINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EXPRESSJET EC532001411. THE ACFT WAS APPROVED FOR R ETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080808 NM 2008 8 8 08FDEA02786 1 20080709 A 5330 6554580 SKIN BOEING 727 727225 1384077 NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 EXTERIOR FUSELAGE SKIN RT SIDE AT BS 950E 1 INCH STR S-18R 4 INCH SKIN IS GOUGED. REMOVED DAMAGE REF SRM 53-30-1. NDT' D ORIGINAL MATERIAL THICKNESS .140. REMOVED .044 .096 MATERIAL REMAINING. REPAIRED ON N00256. THIS IS CLASSIFIED AS A MAJOR REPAIR. MATERIAL LOSS OUT OF LIMITS REF SRM 53-30-1 AREA TO BE REPAIRED ON N00256. 2 L 7 3 4F A3WE 20080808 NM 2008 8 8 08FDEA02789 1 20080709 A 5311 FRAME BOEING 727 727227 1384078 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 SCREW MARKS ON FRAME 1110 AT STR 27R AND 27L UNDER TIE DOWN POINTS. 2 L 7 3 4F A3WE 20080808 EU 2008 8 8 08FDEA02797 1 20080709 A 5321 B5327048402900 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CARGO DECK FLOOR PANEL 232 TG; TOP SURFACE IS CRUSHED AFT OF FRAME 21. MATERIAL ID A 402 H 35039-003, PO 613022.1 I AW FEDEX DWG SRZ 25-005, REV F. PART MARKED NEW FLOOR PANEL IAW FEDEX GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080808 WP 2008 8 8 08FDEA02632 1 20080702 A 5730 ARB10661 SKIN DOUG DC10 DC1010 3022110 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 40061 46973 LT WING L/E CHORD FIXED PANEL FOUND CRACK. REPAIRED WING LOWER L/E STRINGER DOUBLER IAW SRM 57-10-00 FIG 49 VOL I. 2 L 7 3 4F A22WE 20080808 NM 2008 8 8 08FDEA02487 1 20080626 A 5347 NFA622239 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 MID CABIN AFTER REMOVAL OF FLOOR PANELS AT APPROXIMATELY STATION 1540, X = - 75.50, FOUND SEAT TRACK FLANGE CORROSION. CABIN STATION 1540, X = -75.50, SEAT TRACK REPAIRED AS PER SRM 53-70-00, FIG 6, VOL I. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080808 NM 2008 8 8 08FDEA02496 1 20080626 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 609FE 48549 DURING OPEN HOLE HFEC INSPECTION, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATIONS AT HOLES NR B AND NR C (3RD LAYER). MOUNTING HOLES NR B AND NR C ON THE MAIN CARGO DOOR NR 4 JAMB SUPPORT BUSHING REPAIR CARRIE D OUT AS PER SRM 53-50-00 FIG 10 VOL I. CRACK FITTING ON NR 4 JAMB AREA REMOVED AND REPLACED WITH A NEW FITTING AS PER SRM 51-33-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080808 EU 2008 8 8 08FDEA02743 1 20080708 A 5754 SLAT TRACK AIRBUS 300 A300F4605R 3930327 EU RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 RIGHT WING NR 3 SLAT; NR 9 TRACK LOWER LUG BOLT IS CRACKED REMOVED AND REPLACED BOLT ON THE RIGHT WING NR 3 SLAT NR 9 TR ACK IAW FEDEX A300-600 AMM 27-80-12-4; PG 2; STEP D-4. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02744 1 20080708 A 5754 SLAT TRACK AIRBUS 300 A300F4605R 3930327 EU RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 RIGHT WING NR 3 SLAT; NR 8 TRACK LOWER LUG BOLT IS CRACKED. REMOVED NR 3 SLAT; NR 8 TRACK LOWER BOLT AND INSTALLED A NE W BOLT FOR THE NR 3 SLAT; NR 8 TRACK IAW FEDEX A300-600 AMM 27-80-12-4. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02755 1 20080708 A 5311 651592231 FRAME BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 CRACK IN MAIN FRAME STA 380, BETWEEN STRINGER 7R AND RIGHT FWD DOOR, CUTOUT FRAME. REPAIRED FRAME REF SRM 53-10-4 FIG 2 , REMOVED AND REINSTALLED DOOR TRIM AND DOOR TRIM SUPPORT REF SRM 51-30-02 PG'S 1-10. THIS IS CLASSIFIED AS A MAJOR REP AIR. 2 L 7 3 4F A3WE 20080808 NM 2008 8 8 08FDEA02638 1 20080703 A 5320 146N5417U11 FLOOR SUPPORT BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FLOOR SUPPORTS FROM BS 1340 TO BS 1445, RBL 3, 6, 11, 16 HAVE CORROSION AROUND NUTPLATE HOLES. CORROSION REMOVED AND FO UND EXCEED LIMITS IN B757-200 SRM 51-10-02. STRINGER REMOVED AND REPLACED IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 RE V 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080808 NM 2008 8 8 08FDEA02692 1 20080703 A 5320 146N54442 FLOOR SUPPORT BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FLOOR SUPPORT FROM BS 1445 TO BS 1640, RBL 3, 6, 11, HAS CORROSION AROUND NUTPLATE HOLES. CORROSION FOUND EXCEEDED DAMA GE LIMITS IN B757 SRM 51-10-02. REMOVED AND REPLACED STRINGER IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAI R IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080808 EU 2008 8 8 08FDEA02757 1 20080708 A 3350 1009841 LIGHT AIRBUS 300 A300F4605R 3930327 EU ZONE 200 FAILED A FDEA K NONE L NO TEST IN INSP/MAINT 1 CE 21 665FE 769 L-1 AND R-1 OVERHEAD EXIT LIGHTS ARE INOP. REPLACED BOTH R1 AND L1 EMERGENCY LIGHT ASSEMBLIES. OPS CHECK GOOD IAW FEDE X A300-600 AMM 33-51-13-4. PARTS CANNIBILIZED FROM A/C N674FE. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02612 1 20080701 A 5311 A53776575203 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CHAFING MARKS AT C 32 AND 37 BETWEEN P 14-15 OUT OF LIMIT. INNER FLANGE REPAIR PERFORMED IAW SRM 53-10-13 FIG 202 . 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02613 1 20080701 A 5313 A53612213203 LONGERON AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON LONGERON , C12A-14, Y 450 REPAIR PERFORMED IAW SRM 53-12-15 FIG 207. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02699 1 20080704 A 5313 A53971006200 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION AT STRINGER P 52 LT, C 54.3-55. REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CORROSION REMOVAL AND FLAP PEENING IAW RAS/EFW/9000056/2008 ISS A, APPROVED BY EA 6-5316-123004. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02614 1 20080701 A 5347 A53612518200 SEAT TRACK AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON SEAT TRACK, C17-19, Y 450. REPAIR PERFORMED IAW SRM 53-12-16 FIG 201. 2 L 7 2 4F RT A35EU 20080808 WP 2008 8 8 08FDEA02615 1 20080701 A 2611 SMOKE DETECTOR DOUG MD10 MD1010F 3022112 WP CARGO BAY FALSE ACTIVATION A FDEA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 CE 21 554FE 46708 AT FL 350 GOT LEVEL 3 LOWER FWD CARGO FIRE FLASHING DISCHARGE SWITCH/FIRE WARNING. DISCHARGED AGENT AND LANDED. FIRE C REW FOUND NO FIRE EVIDENCE ON A/C. R&R 4 SMOKE DETECTORS IN LOWER FORWARD CARGO COMPARTMENT 2 L 7 3 4F RT A22WE 20080808 WP 2008 8 8 08FDEA02617 1 20080701 A 5310 WINDOW FRAME DOUG MD10 MD1010F 3022112 WP COCKPIT WINDOW DAMAGED A FDEA O OTHER O OTHER CR CRUISE 1 CE 21 68057 48264 LOUD NOISE THAT APPEARED TO COME FROM THE CAPT'S SLIDING WINDOW AREA. A VIBRATION COULD BE FELT ON THE POST IN THE WIND OW ARM. BUT COMMUNICATION WAS NEARLY IMPOSSIBLE WITH ATC. EVENTUALLY AN EMERGENCY WAS DECLARED. LOWER ALTITUDE AND LO WER AIRSPEED HELPED. NOISE REMAINED UNTIL DESCENT BELOW 19,000 FT AND FL 270. R&R CAPTS SLIDING WINDOW FRAME INNER SE AL. 2 L 7 3 4F RT A22WE 20080808 EU 2008 8 8 08FDEA02700 1 20080704 A 5311 A53981260202 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 300 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND MISDRILLED HOLE AT C 75A, P26 LT. REPAIR PERFORMED BY INSTALLING A BUSH IAW RAS/EFW/9000050/2008 ISS B, APPROVED BY EA 6-5318-120121. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02351 1 20080620 A 5753 NRC6762501 VANE DOUG MD11 MD11F 3023600 NM TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 586FE 48487 LEFT WING INBOARD FLAP VANE LOWER SURFACE FOUND DELAMINATED FROM STATION XIFH 156 TO XIFH 206. LEFT WING INBOARD FLAP VANE ASSEMBLY REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT AND TEST CARRIED OUT FOUND 'SATIS' AS PER AMM 27-5 0-22-5. 2 L 7 3 4F RT A22WE 20080808 EU 2008 8 8 08FDEA02517 1 20080627 A 5321 B5327046200600 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 232 GG IS CRACKED AND CRUSHED. FABRICATED A NEW PANEL NR 232 GG; LOCATED HOLES FROM THE OLD PANEL; COUNTERBORED AND POTTED INSERTS; POTTED EDGES; CURED; SANDED; APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080806 SO 2008 8 6 SIMA200819903 1 20080715 A 3234 8271013 HANDLE EMB 145 EMB145LR 3260212 SO MLG MALFUNCTIONED A SIMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 21 935AE 14500920 ON FLIGHT 3676 - CREW REPORTED ON LANDING GEAR EXTENSION THE AURAL WARNING ALERTED LANDING GEAR. CREW EXECUTED A MISSED APPROACH AND CHECKED AOM ITEMS. GEAR EXTENDED WHEN LANDING GEAR LEVER WAS PLACED IN THE DOWN POSITION BUT THE GEAR WAS ABNORMALLY SLOW. ACFT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED GEAR HANDLE IAW EMB 1 45 AMM 32-52-02, OPERATIONAL CHECKED GOOD. ACFT RETURNED TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080806 WP 2008 8 6 AALA200801732 1 20080629 A 3350 BATTERY DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 569AA 49351 SFO - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 3B TO 6B INOPERATIVE. RESEATED BATTERIES FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 3B TO 6B. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A6WE 20080806 SO 2008 8 6 C2XA08TY062 1 20080603 A 3397 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS OVERHEATED A C2XA O OTHER M OVER TEMP NR NOT REPORTED 1 SW 27 16918 145397 NR 4 EMERGENCY BATTERY INVERTER IS REAL HOT WHEN EMERGENCY LIGHT IS NOT ON. REMOVED AND REPLACED NR 4 INVERTER IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD. (S) 2 L 7 2 4T RT T00011AT 20080806 NM 2008 8 6 AALA200801425 1 20080528 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT LEFT NR THREE DOOR FORWARD LENS BROKEN. REPLACED LENS AT LEFT NR THREE DOOR. SYSTEM GROUND CH ECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 NM 2008 8 6 AALA200801413 1 20080527 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 DFW - EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER THREE D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 NM 2008 8 6 AALA200801725 1 20080628 A 3040 CONTROL UNIT BOEING 767 767223 1385123 NM WINDOW HEAT INOPERATIVE A AALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SW 21 327AA 22327 AFW INFLIGHT T9660/28JUN. LT NR 1 OUTER WINDSHIELED CRACKED DURING FLIGHT. RETURNED TO AFW AND LANDED WITHOUT INCIDENT . REPLACED LT FORWARD WINDOW HEAT CONTROL UNIT. REPLACED LT FORWARD WINDSHIELD AND WIPER. SYSTEM GROUND CHECKED NORMA L OPERATION. (S) 2 L 7 2 4F RT A1NM 20080806 EA 2008 8 6 TRAX200800809 1 20080620 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 930EV 8014 FS 280.00 FLOORBEAM OUTBOARD CLIP AT RBL 9 IS CRACKED. REMOVED AND REPLACED BROKEN CLIP WITH NEW AT RBL 9 FS 280 FLOORB EAM OUTBOARD, ALSO FOUND INBOARD CLIP NEEDED REPLACING AND REPLACED SAME. WORK DONE IAW CRJ200 SRM 51-42-20. (S) 2 L 7 2 4F RT A21EA 20080806 WP 2008 8 6 AALA200801415 1 20080528 A 3222 59632541 PISTON DOUG DC9 DC983 3022083 WP NLG BENT A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 967TW 53617 ONT - NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REPLACED BENT PISTON. REPLACED CYLINDER SHOCK STRUT, SEALS AN D UPPER AND LOWER TORQUE LINKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A6WE 20080806 EA 2008 8 6 TRAX200800699 1 20080528 A 3230 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 681BR 7680 AFTER TAKEOFF, MOVED GEAR HANDLE TO THE UP POSITION (NOSE GEAR DOOR & GEAR DISAGREE) WARNING MESSAGES. NOSE GEAR SHOWIN G GREEN DOWN & LOCKED. TOUCHED DOWN LESS THAN 300FMP (AIRCRAFT RETURNED TO ATL AFTER TAKEOFF, EMERGENCY DECLARED). FLT 4601 DEL 180 MINS. REMOVED AND REPLACED PRIORITY VALVE IAW CRJ 200 AMM 32-33-15 OPS CHECK OK. (S) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 CHQA200800149 1 20080716 A 5200 22850081142 ACCESS PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE DEPARTED A CHQA O OTHER O OTHER NR NOT REPORTED 1 GL 11 648BR 16876 16876 7406 E872739 FLIGHT 5590, SDF TO CLE. THE FLIGHT CREW DISCOVERED ON THE POST FLIGHT INSPECTION THAT THE E2 LOWER NOSE ACCESS COWL WA S NOT ON THE ACFT. MAINTENANCE INSPECTED E2 AND INSTALLED A NEW LOWER ACCESS COWLING. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080806 NM 2008 8 6 KCSA081327 1 20080717 A 5411 FRAME BOEING 747 747246B 1384864 NM NR 1 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 NR1 PYLON REAR ENG MOUNT BULKHEAD OUTBOARD AFT FRAME WEB CRACKED ONE INCH AT NAC STA 221.9. (S) 2 L 7 4 4F RT A20WE 20080806 NM 2008 8 6 NSV2008F00010 1 20080717 A 5270 PROXIMITY SENSOR BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY EXIT MALFUNCTIONED A NSVA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 EA 27 200WQ 4200 EMERGENCY DECLARED - AIR RETURN TO EWR FOR FWD EMERGENCY DOOR LIGHT. CLEANED CONTACT POINTS ON FWD EMERGENCY EXIT PROXI MITY SENSOR. OPS CHECK PERFORMED IAW Q400 AMM 52-22-00-710-802. OPS CHECK GOOD. LIGHT NOT ILLUMINATED. (S) 2 H 7 2 4T RT A13NM 20080806 NM 2008 8 6 AALA200801427 1 20080528 A 3350 D71702001 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EMERGENCY LIGHT AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080728 CE 2008 7 28 DJF2008F00009 1 20080609 A 3340 LIGHT BEECH MU300 400A 1155402 CE TAIL MISSING E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 740TA RK123 DURING A PHASE 1 INSPECTION IT WAS FOUND THAT THE VERTICAL TAIL NAVIGATION LIGHT ASSY WAS MISSING. THE SHEET METAL WAS REPAIRED AND LIGHT ASSY REPLACED. (K) 2 H 7 2 4F RT A16SW 20080728 WP 2008 7 28 UPS08852582 1 20080619 A 5320 47533601 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 FS 834 L22L INTERCOSTAL END FITTING CRACKED. REPLACED INTERCOSTAL END FITTING AT FS 834 AND L22L IAW SRM 51-01-24-0, SRM 51-01-20D. 2 L 7 4 4F RT 4A25 20080728 NM 2008 7 28 PID2008F00005 1 20080701 A 3350 20131A BATTERY PACK BOEING 737 737228 13844AG NM PWA JT8 JT8D15 52051 NE EMERGENCY LIGHTS INOPERATIVE A PIDA O OTHER O OTHER NR NOT REPORTED 1 EA 39 251TR 23792 AFT EMERGENCY EXIT LIGHTS NOT WORKING. REMOVED AND REPLACED AFT BATTERY PACK IAW MM 33-51-57. LIGHTS WORKING NORMAL. (K) 2 L 7 2 4F 4 F RT A16WE E2EA 20080728 WP 2008 7 28 UPS08852581 1 20080613 A 5313 S1616757 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 MAIN CABIN AT STA 1748 LONGERON 15R CRACKED WHERE LONGERON ATTACHES TO CANTED FRAME. REPAIRED LONGER ON 15R FROM STA 1741 TO 1766 IAW SRM 53-02-02 FIG 10, SRM 51-03-02, SRM 51-01-21 AND SRM 51-01-20D. 2 L 7 4 4F RT 4A25 20080728 WP 2008 7 28 UPS08852580 1 20080613 A 5313 S1616757 LONGERON DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 MAIN CABIN AT STA 1753 HAS LONGERON 14R CRACKED WHERE LONGERON ATTACHES. REPAIRED L14R FROM STA 1745 TO 1766 IAW SRM 51-01-21, SRM 51-01-20D, SRM 53-02-02 FIG 10 AND SRM 51-03-01. 2 L 7 4 4F RT 4A25 20080728 WP 2008 7 28 UPS08852579 1 20080521 A 5753 FLAP DOUG DC8 DC873F 302199F WP WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 INTERIM REPAIR TO RT INBOARD FLAP AT TRAILING EDGE XM-75. REMOVED INTERIM REPAIR, FABBED AND INSTALL ED REPAIR DOUBLER IAW SRM 51-1-21, 51-1-21A, 51-1-8, 51-1-9A. 2 L 7 4 4F RT 4A25 20080728 WP 2008 7 28 UPS08852578 1 20080525 A 5755 HINGE FITTING DOUG DC8 DC873F 302199F WP NR 1 SPOILER GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 LEFT WING NR 1 SPOILER HINGE FITTING GOUGED NEAR STA XW38. REMOVED AND REPLACED HINGE FITTING IAW SR M, 51-1-8, 51-3-0, 51-3-2. 2 L 7 4 4F RT 4A25 20080728 NM 2008 7 28 NOC2008F00002 1 20080614 A 2612 CONNECTOR BOEING 757 75728A 1384976 NM LT FIRE LOOP LOOSE A NOCA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 15 754NA 29381 LT ENGINE FIRE LOOP 2 STATUS MSG. SECURE CONNECTOR AT LOWER AFT DETECTOR NR 4 T5500. NO DEFECTIVE PART. 2 L 7 2 4F RT A2NM 20080728 CE 2008 7 28 FFS2008F00000 1 20080606 A 5330 11440002473 SKIN BEECH 1900 1900C 1154161 CE FUSELAGE DENTED E FFSA A UNSCHED LANDING O OTHER CL CLIMB 1 AL 01 575Z 28694 UC136 BIRD STRIKE ON TAKEOFF RESULTING IN DENTING OF FUSELAGE NOSE SKIN BEYOND MFG ALLOWABLE CONTOUR CHANGE LIMITS. AC RETURN ED TO AIRPORT FOR UNEVENTFUL LANDING. (K) 2 L 7 2 4T RT A24CE 20080728 EU 2008 7 28 UPS08152576 1 20080620 A 3211 A57241959 HOUSING AIRBUS A300 A300F4622R 3930360 EU RT MLG TRUNION GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 122UP 0807 INSPECTION TYPE:SV RIGHT LANDING GEAR FWD TRUNNION BEARING HOUSING HAS A DEEP GOUGE ON LWR SIDE. ACCOMPLISHED REPAIR OF RT LANDING GEAR FWD TRUNNION BEARING HOUSING LWR SIDE IAW SAA EA 300-5751-01-A1426, UPS EO A300-5740-29720-A, AND AIRBU S RAS/BAE/1007668/2008. 2 L 7 2 4F RT A35EU 20080728 EU 2008 7 28 UPS08152575 1 20080620 A 3211 A57241959 HOUSING AIRBUS A300 A300F4622R 3930360 EU LT MLG TRUNION GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 122UP 0807 INSPECTION TYPE:SV LEFT LANDING GEAR FWD TRUNNION BEARING HOUSING HAS A DEEP GOUGE ON LWR SIDE. ACCOMPLISHED REPAIR OF LT LANDING GEAR FWD TRUNNION BEARING HOUSING LWR SIDE IAW SAA EA 300-5751-01-A1425, UPS EO A300-5740-29719-A, AND AIRBUS RAS/BAE/1007667/2008. 2 L 7 2 4F RT A35EU 20080728 NM 2008 7 28 UIE2008F00007 1 20080621 A 5312 PRESSURE PANEL BOEING 747 7472D7B 1384803 NM NOSE WHEEL WELL CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 524MC 21784 NOSE WHEEL WELL TOP PANEL WEB FOUND WITH A CRACK AT BS 304 AT RBL11. CRACK LENGTH IS 2.250 INCHES. INTERIM REPAIR ACCOM PLISHED IAW SRM 53-10-04, FIG 116, SHEETS 1 AND 6 AND FIG 117, SHEETS 1 THRU 10. REQUIRES INITIAL INTERNAL DETAIL VISUA L INSPECTION PRIOR TO 15,000 FC. REF EO. (K) 2 L 7 4 4F RT A20WE 20080728 CE 2008 7 28 CVU2008F00000 1 20080707 A 8011 MHJ4004R STARTER BEECH 80 65B80 1152812 CE LYC O720 IO720* 41546 EA ENGINE INTERMITTENT E CVUA O OTHER O OTHER NR NOT REPORTED 1 WP 13 44MA 1068 LD412 A1B PART REMOVED FOR OVERHAUL AFTER INTERMITTENT OPERATION. (K) 1 L 7 2 3O 3 O 3A20 1E15 20080728 WP 2008 7 28 UPS08852603 1 20080528 A 5311 561237618 FRAME DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 FLIGHT DECK STA -52 RT SIDE FRAME HAS CORROSION BY SUBFLOOR AREA. REPAIRED FLT DECK FRAME AT STA -52 AND SUBFLOOR AREA IAW EA 008- 5310-01-A1403. 2 L 7 4 4F RT 4A25 20080728 NM 2008 7 28 PID2008F00003 1 20080710 A 3260 189915 SENSOR BOEING 737 737228 13844AG NM PWA JT8 JT8D15 52051 NE RT MLG FAILED A PIDA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 39 251TR 23792 GEAR WOULD NOT RETRACT. OVER RIDE TRIGGER USED TO RETRACT GEAR. AC RETURNED TO FIELD. PERFORMED OVERWEIGHT LANDING INS PECTION IAW MM 05-51-291. AC IS SAFE FOR INTENDED FERRY FLIGHT.. 7/11/2008: FOUND AIR SAFETY SENSOR BAD. REPLACED AIR SAFELY SENSOR AND OPS CHECKED IAW MM 32-09-200. (K) 2 L 7 2 4F 4 F RT A16WE E2EA 20080722 WP 2008 7 22 ABXA080155 1 20080527 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 981AX 47273 COCKPIT EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. REPLACED EMERGENY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00 . (A) 2 L 7 2 4F A6WE 20080724 EU 2008 7 24 2008UALA02999 1 20080526 A 2910 NAS1611115 O-RING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE PTU CHECK VALVE FAILED A UALA A UNSCHED LANDING W K INADEQUATE Q C FLUID LOSS CR CRUISE 1 WP 29 416UA 479 LOSS OF PRESSURE IN YELLOW HYD SYSTEM. FLT RTFL. YELLOW ELECTRIC HYD PUMP IS LEAKING. REPLACED O-RING ON PTU CHECK VA LVE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03245 1 20080608 A 3242 BRAKE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT MLG LEAKING A UALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 29 662UA 27159 LEFT MLG HAD HYDRAULIC LEAK ON FWD LEFT BRAKE. ARRIVED WITH THE MAIN GEAR SMOKING. LT MLG HAD HYD LEAK ON FWD LEFT BRAK E. SUSPECT BRAKING ACTIVITY MIXED WITH HYD FLUID CAUSED THE FIRE. IADMM PUT THE FIRE OUT. REPLACED NR 1 FWD BRAKE. ACP' D BRAKE TEMP-HIGH ENERGY STOP CONDITION. NO DEFECTS FOUND AND ALSO ACP'D BRAKE SEIZURE CONDITIONAL INSPECTION. NO DEFECT S FOUND. 2 L 7 2 4F 4 F RT A1NM E24NE 20080808 EU 2008 8 8 08FDEA02701 1 20080704 A 5740 A57110530211 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND DAMAGE AT HOLE H CENTER TANK FITTING C 47 RT REPAIR PERFORMED BY REAM UP UNTIL DAMAGE REMOVAL, NDT FOR CRACK FREE AND SPOTFACING IAW RAS 70510800/026/2008 ISS A, APPROVED BY 6-5710-120111. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02706 1 20080526 A 5415 A5461102400300 FITTING AIRBUS 300 A300B4622R 3930312 EU NR 2 PYLON WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 PYLON NR 2, WING/PYLON AFT ATTACH FITTING AT RIB 18 WITH PLAY AT BEARING HOUSING. THE FEDEX EA 6-5451-117329 WAS ACCOMP LISHED. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02708 1 20080704 A 5753 SKIN AIRBUS 300 A300F4605R 3930327 EU TE FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 660FE 759 RT WING INBD FLAP LEADING EDGE AND UPPER SURFACE HAS 7 IN BY .250 IN WEAR MARK AT WS 80. REPAIRED RT WING INBD FLAP LEA DING EDGE BETWEEN FLAP RIB 18 AND RIB 20D IAW A300-600M SRM 57-50-00, FIG 208. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02711 1 20080705 A 5320 652954852 WEB BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 FUSELAGE 1183 BULKHEAD LT SIDE LOWER OTBD FLOOR WEB CRACKED REMOVED DAMAGED PART (DITCHING PAN AND ANGLE ). FABRICATED , HEAT TREATED, ALODINED, PRIMED AND INSTALLED IAW REF SRM 51-30-02 51-10-02, 51-20-5. BOEING DWG 65-29567 THIS IS CL ASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080808 NM 2008 8 8 08FDEA02712 1 20080705 A 5330 65545803 SKIN BOEING 727 727225 1384077 NM ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 BLENDED AREA LT LOWER FUSELAGE AFT WING TO BODY FAIRING OUT OF LIMITS. DAMAGE AT FR 950F AND 3.5 INCH FWD AND BELOW STR 25L AND INCH OF FR 950F ON STR 25L. REPAIRED BY INSTALLING A DOUBLER REF SRM 53-30-3 FIG 5. REMOVED AND REINSTALLED W ING TO BODY PANEL REF SRM 51-30-02 PGS 1-4, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080808 NM 2008 8 8 08FDEA02713 1 20080705 A 5720 652165688 RETAINER BOEING 727 727225 1384077 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 LT WING LOWER T/E PANEL SEAL RETAINER IS CORRODED WS 167 TO 222 JUST AFT OF AFT SPAR LWR CHORD FABRICATED NEW, 2 EA SEA L RETAINERS ON LT WING LOWER T/E PANEL FROM WS 162 TO 222. REF DWG 65-21656-88, TREATED, PRIMED, AND INSTALLED REF SRM 51-10-2 PG 1-7, 51-30-10 PG 1, 2, 13. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080808 EU 2008 8 8 08FDEA02536 1 20080627 A 5321 B5327037200300 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 262 AH IS CRACKED, BROKEN. FABRICATED NEW PANEL NR 262 AH, LOCATED HOLES FROM THE OLD PANEL , COUNTERBORED AND POTTED INSERTS, POTTED, CURED AND SANDED EDGES, APPLIED ANTI-SKID AND PART MARKED IAW FEDEX DWG SRZ 2 5-005; REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02527 1 20080627 A 5321 B5327046201000 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 231 KG IS CRACKED AND CRUSHED. FABBED NEW FLOOR PANEL; POTTED EDGES, CURED, SANDED, POTTED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005, REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02537 1 20080627 A 5321 B5327046702800 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 231 YG IS CRACKED. FABRICATED NEW PANEL NR 231 YG, LOCATED THE HOLE FROM THE OLD PANEL. CO UNTERBORED AND POTTED INSERTS, POTTED, CURED AND SANDED EDGES, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005 ; REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02548 1 20080627 A 5321 B5327028200000 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 252 YG IS CRACKED AND CRUSHED. FABRICATED A NEW FLOOR PANEL NR 252 YG, LOCATED HOLES FROM T HE OLD PANEL, POTTED EDGES, CURED, SANDED, POTTED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02549 1 20080627 A 5321 B5327001400261 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 252 UH IS CRACKED AND CRUSHED. FABRICATED A NEW FLOOR PANEL 252 UH, POTTED EDGES, CURED, SA NDED, POTTED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005, REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 M7K2008F00103 1 20080414 A 5302 350A23422320 MOUNT UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 808MH 3298 3914 23072 DURING ROUTINE INSP, A CRACK WAS DISCOVERED RADIATING FROM A MOUNTING BORE HOLE TO THE EDGE OF THE MOUNTING FLANGE AND I NWARD TOWARD THE CENTER OF THE FLANGE FROM THE SAME BORE HOLE. TOTAL CRACK LENGTH EXCEEDS 1.5 INCHES. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00132 1 20080414 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE DEFECTIVE E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 847MH 345 4266 23416 A FAULT CODE WAS GENERATED ON SHUTDOWN INDICATING A DEFECTIVE COLLECTIVE POTENTIOMETER. A NEW PART WAS INSTALLED AND NO FURTHER FAULT WAS DETECTED. THIS IS A RECURRING FAULT FOR THIS PART WHICH HAS EFFECTED THE DISPATCH RELIABILITY FOR TH IS MODEL AC. SUGGEST NEW DESIGN OR MFG BE FOUND FOR THIS PART AS SOON AS POSSIBLE. (K)- 1 G 7 2 3U 3 U H9EU E00054EN 20080811 WP 2008 8 11 MWE2008F00024 1 20080724 A 2410 CSD DOUG DC9 DC981 3022081 WP PWA JT8 JT8D1 52044 NE GENERATOR OVERSERVICED A MWEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 13 814ME 48010 RT CSD OUTLET TEMPERATURE WAS IN YELLOW ARC AND RISING. FOUND RT CSD WAS OVERSERVICED, DRAINED CSD TO PROPER LEVEL. (K ) 2 L 7 2 4F 4 F A6WE E2EA 20080811 EU 2008 8 11 QML2008F00005 1 20080717 A 3340 02471131 HOUSING AGUSTA A109 A109E 0260119 EU PWA PW206 PW206A NE SEARCH LIGHT CRACKED E QMLA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 03 1UW 11034 ON STARTUP AND PRIOR TO TAKEOFF, PILOT NOTICED SX-5 SEARCHLIGHT SEEMED TO BE VIBRATING EXCESSIVELY. SHUTDOWN AIRCRAFT T O INVESTIGATE AND FOUND BRACKET HOLDING RT SIDE OF LIGHT, BROKEN COMPLETELY THROUGH. THE RT SIDE WELDED MOUNT FITTING O F THE SEARCHLIGHT HOUSING WAS FOUND TO BE CRACKED AROUND THE ENTIRE WELD AND SEPARATED FROM THE HOUSING ALONG WITH THE E LEVATION DRIVE/STOP. (K) 1 G 7 2 3U 3 U RT H7EU E42NE 20080811 NE 2008 8 11 M7K2008F00084 2 20080414 A 7412 EXCITER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE IGNITION SYS FAILED E M7KA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 19 824MH 282 4173 23416 DURING ATTEMPTED START IGNITERS FAILED TO ACTIVATE. INVESTIGATION REVEALED CIRCUIT BREAKER HAD POPPED. RESETTING THE B REAKER FOR A GROUND TEST REVEALED NO FUNCTION. THIS PART HAS BEEN DEEMED NON REPAIRABLE BY THE ENGINE MFG. AS NO SECON D BOX IS EMBODIED REPLACEMENT OF ANY SUSPECT BOX IS PRUDENT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00121 1 20080303 A 6320 S1130021089 TRANSMITTER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE M/R GEARBOX INTERMITTENT E M7KA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 807MH 301 M3154 3912 23130 PILOT REPORTED THAT THE MAIN GEARBOX LOW OIL PRESSURE WARNING LIGHT ILLUMINATED INTERMITTENTLY AT IDLE. A NEW OIL PRESS URE TRANSMITTER WAS INSTALLED AND NO FURTHER FALSE INDICATIONS NOTED. THIS SWITCH HAS A MODERATE FAILURE RATE USUALLY B Y LOSING ITS LOW END CALIBRATION AND ILLUMINATING WHEN AC IS IDLING. SUGGEST A DESIGN UPDATE IS REQUIRED TO IMPROVE THI S TRANSMITTERS RELIABILITY. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00120 1 20080303 A 6320 S1130021089 TRANSMITTER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE GEARBOX OIL SYS INTERMITTENT E M7KA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 813MH 1610 3967 23183 PILOT REPORTED THAT THE MAIN GEARBOX LOW OIL PRESSURE WARNING LIGHT ILLUMINATED INTERMITTENTLY AT IDLE. A NEW OIL PRESS URE TRANSMITTER WAS INSTALLED AND NO FURTHER FALSE INDICATIONS NOTED. THIS SWITCH HAS A MODERATE FAILURE RATE USUALLY B Y LOSING ITS LOW END CALIBRATION AND ILLUMINATING WHEN AC IS IDLING. SUGGEST A DESIGN UPDATE IS REQUIRED TO IMPROVE THI S TRANSMITTERS RELIABILITY. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 2008 8 11 MWE2008F00029 4 20080731 A 2565 4019991 LANYARD DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE ESCAPE SLIDE DETACHED A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 822ME 49759 LANYARD TO AFT SLIDE PACK DETACHED. REINSTALLED LANYARD. (K) 2 L 7 2 4F 4 F RT A6WE E9NE 20080811 EU 2008 8 11 M7K2008F00104 1 20080414 A 5340 350A25040500 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE OIL COOLER CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 808MH 2104 3914 46079 DURING ROUTINE INSPECTION, A CRACK WAS DISCOVERED RADIATING TO THE EDGE OF THE MOUNTING FLANGE AND INWARD TOWARD THE CEN TER OF THE FLANGE FROM THE EDGE OF THE SCREW CONTACT SURFACE. TOTAL CRACK LENGTH EXCEEDS 2.5 INCHES. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00097 1 20080303 A 3300 PK16QCSSP4X1KMA POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE CABIN LIGHTS INTERMITTENT E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 807MH 3377 3912 23130 AT FULL BRIGHTNESS ADJUSTMENT ALL CONTROLLED LIGHTING FLICKERS ON AND OFF INTERMITTENTLY. REPLACEMENT WITH NEW PART COR RECTED THE DEFECT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 CE 2008 8 11 Z5F2008F00001 1 20080620 A 3240 BRAKE SYS CESSNA 500 550 2076604 CE MLG WEAK E Z5FA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 63 303CS 5500814 DURING TAXI, WHILE PULLING INTO PARKING AREA, CAPTAIN`S BREAKS LOST ALL PRESSURE WITH PEDALS DROPPING TO FLOOR. MAINTEN ANCE, INSPECTED, SERVICED AND PERFORMED ENTIRE BRAKE BLEED. NO FURTHER DEFECTS, DURING TAXI, BRAKE SYSTEM WORKED PROPER LY, NO DEFECTIVE PARTS. AC RETURNED TO SERVICE. (K) 1 L 7 2 4F A22CE 20080811 EA 2008 8 11 TRAX200800671 1 20080519 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 907EV 7648 JOB 8764811 OPERATION 252 FS 280 CLIP AT LBL 9.0 OUTBRD IS CRACKED. REMOVED CRACKED FS 280.0 CLIP AT OUTBOARD LBL 9 AND INSTALLED NEW SERVICEABLE CLIP IAW CRJ 200 SRM 51-42-13 AND 51-42-21. [SDR CLOSED](B) 2 L 7 2 4F RT A21EA 20080807 EA 2008 8 7 COMA0860327 1 20080720 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FS 559 RBL 18 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 918CA 35774 7018 DURING MID CK 8, INSPECTION FOUND .25 INCH CRACK ON INBOARD SIDE LOWER END, OF VERTICAL STIFFENER, AT RBL 18, FS 559. C UT OUT DAMAGE AND INSTALLED DOUBLER PER BOMBARDIER REO 601R-53-41-067. (A) 2 L 7 2 4F RT A21EA 20080808 WP 2008 8 8 08FDEA02773 1 20080709 A 5330 ABA70484 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 EXT FUSELAGE LWR SURFACE FOUND DEEP DENT 2.50 INCH BY 1.50 INCH DEEP .082 INCH ON SKIN. 2 L 7 3 4F RT A22WE 20080808 EU 2008 8 8 08FDEA02522 1 20080627 A 5321 B5327048402200 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 232 WG IS CRUSHED. FABBED A NEW FLOOR PANEL, POTTED EDGES, CURED, SANDED, POTTED INSERTS, A PPLIED NON-SKID AND PART MARKED IAW FEDEX SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02739 1 20080708 A 5754 6516221 SLAT BOEING 727 727233 138408A NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 LT WING NR 4 SLAT FENCE UPPER AFT END COMPOSITE IS CRACKED AND DELAMED. REPAIRED NR 4 SLAT FENCE REF SRM 51-40-9 STEP 7 PG 9 AND AMM 51-20-051-7 PG 1 AND 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080808 EU 2008 8 8 08FDEA02525 1 20080627 A 5321 B5327048300400 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 231 CG IS CRUSHED. FABBED A NEW PANEL 231 CG; POTTED INSERTS, POTTED, CURED, SANDED EDGES, APPLIED NON-SKID TAPE AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02802 1 20080710 A 5753 A57960300003 SKIN AIRBUS A300 A300F4622R 3930360 EU RT TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND OLD FLUSH DOUBLER RPAIR ON RT CENTER FLAP NOSE SKIN WITHOUT ANY OLD DOCUMENTATION. REPAIR RENEWED IAW SRM 57-50-0 0 FIG 208. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02804 1 20080710 A 5754 A53510217203 FITTING AIRBUS 300 A300B4622R 3930312 EU KRUEGER FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON KRUEGER FLAP STRUCTURE RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080724 NM 2008 7 24 2008UALA03274 1 20080608 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 810UA 843 FLOORBEAM 150 REMOVED FROM FR65 TO FR70, FOR CORROSION. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03296 1 20080609 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 AFT CARGO FRAME DENTED STA 1540, STR 26L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED SECTION OF INBOARD FLANGE. FORME D & INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 EU 2008 7 24 2008UALA03055 1 20080527 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 447UA 836 FLOORBEAM ITEM 255 HAS CORROSION. ACCOMPLISHED MAJOR REPAIR AT DEN. FLOORBEAM ITEM 255 HAS CORROSION. (MARKED) REF SR M 53-41-14 FIG 1 ITEM 255. REMOVED BEAM 255, ON WORK TABLE. CONT OF AMIS ITEM 0912011: PICKED UP HOLES FOR SPLICE ANG LE ON NEW BEAM. CONTINUED WORKING BEAM PART ON TABLE. INSTALLED BEAM 255, NEEDS RIVETS FOR SHEAR PLATE ATTACH INSTALLE D. CONTINUED WORKING BEAM. COMPLETED INSTALL OF BEAM 255. 2 L 7 2 4F 4 F RT A28NM E40NE 20080724 NM 2008 7 24 2008UALA03117 1 20080601 A 3810 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE POTABLE WATER OPEN A UALA O OTHER W E INADEQUATE Q C VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 540UA 25252 VIBRATION IN THE AFT CABIN FLOOR LED TO DIVERSION. WATER FILL VALVE AND PANEL LEFT OPEN SUSPECT ALL ISSUES ARE RELATED TO WATER FILL VENT VALVE NOT BEING CLOSED, BLEEDING HEAD PRESSURE. CAUSING WATER COMPRESSOR TO VIBRATE FLOOR AND CLUNKI NG WATER LINE DUE TO AIR IN SYSTEM PERFORMED VISUAL SEARCH OF EXTERIOR OF A/C - OK. CLOSED VALVE AND ACCESS DOOR. FURT HER FLIGHTS WERE CLEAN. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 2008 7 24 2008UALA03149 4 20080530 A 2565 5A29011 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 641UA 25091 LEAKING ASPIRATOR. THERE IS NO PHYSICAL DAMAGE TO THE ASPIRATOR. REPLACED ASPIRATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 20080724 2008 7 24 2008UALA03218 4 20080604 A 2565 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 550UA 25398 DOOR 1 LEFT SLIDE PRESSURE IS ONE NEEDLE OUT OF THE GREEN BAND. PRESSURE LEAK IN SLIDE BOTTLE. REPLACED SLIDE ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03252 1 20080606 A 5340 ATTACH FITTING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 399UA 24674 INTERCOSTAL WEB FWD LOWER ATTACH CLIP CRACKED AT FWD INBOARD CORNER AT STRINGER S-11L BETWEEN BS 294.5 AND 303.9 FWD OF 1L ENTRY DOOR. MAJOR REPAIR ACCOMPLISHED: REPLACED INTERCOSTAL WEB. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 NM 2008 7 24 2008UALA03261 1 20080608 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 544UA 25322 FWD PIT AT STA 520 BETWEEN STR 25L AND 26L FRAME HAS DENT. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE. INSTALLED DOUBL ER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 2008 7 24 2008UALA03266 4 20080606 A 2565 D31039202 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 2R DOOR LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 503UA 24624 CREW REPORT: 2R SLIDE PACK PRESSURE LOW. PRESSURE LEAK. REPLACED SLIDE ASSY AT DOOR 2R. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03269 1 20080607 A 3350 20121 POWER SUPPLY BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 202UA 24717 RAMP REPORTS FLOOR LEVEL EMERG 'EXIT' LIGHTS ARE ON AT BOTH AFT DOORS, UPPER 'EXIT' LIGHT IS ON ABOVE DOOR 2LT, AND RT F USE SLIDE LIGHT ALSO ON. REPLACED BATTERY POWER SUPPLY ASSEMBLY. 2 L 7 2 4F 4 F RT A16WE E21EU 20080724 2008 7 24 2008UALA03297 4 20080609 A 2565 CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE BINDING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 538UA 25222 RT OVERWING SLIDE BACK UP CABLE IS BINDING. CABLE OUT OF POSITION. PROPERLY RE-ROUTED CABLE TO PRESSURE BOTTLE SUPPORT SHROUD AND OPS CHECK GOOD AND REINSTALLED CLEVIS PIN TO MASTER CONTROL VALVE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 SWAA083801 1 20080713 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083855 1 20080713 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 15L CRACKED AT BS 360. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083879 1 20080714 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED SPV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083888 1 20080714 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 16L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083885 1 20080714 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 767, STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083947 1 20080715 A 5753 65464353 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083945 1 20080715 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083939 1 20080715 A 5311 6545805 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 277, STR 16R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 SWAA083940 1 20080715 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080724 NM 2008 7 24 2008UALA03331 1 20080611 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 507UA 24743 DOOR 4L EXT EMERGENCY LIGHT INOP. BULB INOP. RELAMPED DOOR 4L EXT EMERGENCY LIGHT, OPS CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NE 2008 7 24 2008UALA03319 2 20080610 A 7397 WIRE HARNESS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE SHORTED A UALA O OTHER N FALSE WARNING DE DESCENT 1 WP 29 589UA 28707 717999 RECEIVED "L ENG SECONDARY CONTROL" EICAS STATUS MSG. WIRING HARNESS D42048 HAS SHORTED. REPAIRED HARNESS D42048, ALL C ONT CHECKS ARE GOOD, ITEM HAS NOT REPEATED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080724 NM 2008 7 24 2008UALA03318 1 20080610 A 3597 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT SHORTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 538UA 25222 FIRST OBSERVER'S MASK P/A DOES NOT TRANSMIT. WIRE SHORT. REPLACED FIRST OBSERVERS O2 MASK STOWAGE BOX, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080725 EU 2008 7 25 2008UALA03484 1 20080618 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 436UA 638 DENT IN RVSM AREA 9.25" FROM STATIC PORT, AREA R6 IN FORWARD LOWER LEFT OF STATIC PORT. DENT IS .010 " DEEP, .25"WIDE X .375" TALL. -OK - :PER SRM 53-00-11 DIAGRAM 10 2, WITHIN AERODYNAMIC RVSM REQUIREMENT. CF9019 CREATED FOR PERMANENT REPAIR FOR NEARNESS -FORM REQUIREMENT. AREA IS CRACK FREE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 NM 2008 7 25 CALA0800611 1 20080616 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM BS 360 S8-9 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16642 28903 FOUND FRAME CRACK AT THE AIR CONDITION (A/C) BRACKET AT BODY STATION 360 BETWEEN S-8 AND S-9. REPAIRED PER ECRA 5310-04 787. 2 L 7 2 4F RT A16WE 20080725 NM 2008 7 25 CALA0800647 1 20080628 A 5320 65C3397035 INTERCOSTAL BOEING 737 737524 1384721 NM BS 340-360 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 INTERCOSTAL CRACKED AT BODY STATIONS 340-360 LBL 11. REMOVED AND REPLACED DAMAGED INTERCOSTAL CAP ANGLE AT STATION 340- 360, LBL 11 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080725 EA 2008 7 25 SWIA200819830 1 20080702 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 705SK 10145 EMERGENCY EXIT SIGN ON FORWARD BULKHEAD IS INOP. REPLACED SERVICE DOOR EMERGENCY LIGHT. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 20080725 EA 2008 7 25 SWIA200819818 1 20080627 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA RIGHT OVERHEATED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 445SW 7651 FLT 3743 - RIGHT PACK WAS SMOKING IN AUTO MODE. REPLACED RIGHT ACM IAW AMM 21-51-10. OPS CHECK GOOD, P/N 782790-15, S/ N OFF 200110263. 2 L 7 2 4F RT A21EA 20080725 EA 2008 7 25 SWIA200819845 1 20080710 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG DISCHARGED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 432SW 7548 FLT 3811 - RECEIVED A NOSE GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE. RECYCLED GEAR. SERVICED NOSE GEAR STRUT I AW AMM 12-12-32. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080725 2008 7 25 IXX2008F00002 4 20080702 A 3414 10906 INDICATOR DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE AIRSPEED INOPERATIVE A IXXA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SW 11 820BX 46065 ON TAKEOFF ROLL, CAPTAIN AIRSPEED DID NOT REGISTER 80 KNOTS (ANALOG NEEDLE AT ZERO, DIGITAL READOUT ERROR). CREW REJECTE D TAKEOFF AT 80 KNOTS, THE CREW RETURNED TO BLOCKS WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED CAPTAIN MACH AIRS PEED INDICATOR OPERATIONAL AND LEAK CHECK GOOD IAW MM 34-12-1. MAINTENANCE ALSO ACCOMPLISHED REJECTED TAKEOFF INSPECTION IAW , NO DEFECTS NOTED. AC WAS RETURNED TO SERVICE. (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 20080725 NE 2008 7 25 Q2S2008F00001 2 20080621 A 7230 COMPRESSOR BOEING 747 747300 1384920 GL PWA JT9 JT9D7R4G2 52054 NE NR 1 ENGINE STALLED A Q2SA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 EA 63 749SA 24194 715125 WHILE THROTTLING ENGINE TO TAKEOFF POWER, ENGINE NR 1 HAD MULTIPLE COMPRESSOR STALLS. TAKEOFF POWER WAS 1.53, COMPRESSO R STALLS STARTED WHEN POWER WAS APPROACHING 1.35. AIRCRAFT RETURNED TO BLOCKS. (K) 2 L 7 4 4F 4 F RT A20WE E3NE 20080725 2008 7 25 HNA2008F00002 4 20080629 A 3442 071131900 RADAR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE WX SYSTEM FAILED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 828EX 392 RADAR SPIKES RADAR FAILED ENROUTE TO FLO. THUNDERSTORM ACTIVITY WAS AHEAD OF THE FLIGHT. DISPATCHER AND CAPTAIN CHOSE TO HAVE FLIGHT RETURN. REMOVED AND REPLACED RADAR RT. OPS CHECK GOOD IAW SB 34-18. (K) 2 H 7 2 4T 4 T RT A13NM E20NE 20080725 EA 2008 7 25 S9B2008F00000 1 20080609 A 2121 AGC10AGC05 FUSE DHAV DHC6 DHC6 2802606 EA PWA PT6 PT6* 52043 EA A/C FAN BURNED A S9BA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 29 573SA 573 AIR CONDITION CABIN FAN INOPERATIVE ON HIGH, MAKES A BURNING SMELL ON LOW. REPLACED 3 BLOWN FUSES WITH NEW. GROUND OPS CHECK, NO ODORS OR DISCREPANCIES NOTED . (K) 1 H 7 2 3T 3 T RT A9EA E2NE 20080725 SW 2008 7 25 MT92008F00003 1 20080619 A 7100 NAS13513H16 SCREW SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP PPC SHAFT MISINSTALLED E MT9A O OTHER W INADEQUATE Q C CR CRUISE 1 SW 05 26932 AC660 P44414C IN FLIGHT, THE PPC INPUT LEVER TO THE PPC SHAFT CAME OFF AND PREVENTED THE CREW FROM BEING ABLE TO RETARD THE POWER TO T HE LT ENGINE. THIS FORCED THEM TO DO AN INFLIGHT SHUTDOWN OF THAT ENGINE. THE INVESTIGATION FOUND THAT THE SCREW AND S PACER THAT SECURES THE ARM TO THE SHAFT WAS NOT INSTALLED. FURTHER INVESTIGATION SHOWED A DISCREPANCY BETWEEN THE MM A ND THE IPC MANUAL FOR INSTALLING THESE PARTS IAW TO AC SN. THE OLDER SN AC (BELOW AC664) ARE NOT INSTRUCTED TO INSTALL THEM (71-00-15 (5) (D). ALSO, THE IPC CONTRADICTS ITSELF 76-10-40, FIG 7 CALLS FOR THE INSTALLATION OF THESE PARTS FOR SN 420-683 HOWEVER 76-10-50 LIMITS INSTALLATION OF THESE PARTS TO SN 664-683. (K) 2 L 7 2 4T 4 T RT A8SW E4WE 20080725 CE 2008 7 25 YAD2008F00000 1 20080711 A 3260 1003810061 SWITCH BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE NLG FAILED E YADA O OTHER O OTHER NR NOT REPORTED 1 AL 03 113AX UC41 PILOT REPORTED NOSE GEAR UNSAFE WARNING AFTER VARIOUS ATTEMPTS AT GEAR EXTENSION. GREEN LIGHT CAME ON AT TOUCHDOWN. VE RIFIED NOSE GEAR DRAG BRACE SWITCH PLUNGER WAS "STICKY" AND WAS DEFLECTING STRIKER PLATE INSTEAD OF DEPRESSING SWITCH PL UNGER. REPLACED FAILED SWITCH. (K) 2 L 7 2 4T 4 T RT A24CE E4EA 20080728 EA 2008 7 28 VNAA0805022 1 20080518 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF348C1 30049 NE SERVICE DOOR MALFUNCTIONED A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 05 706PS 10150 CREW REPORTED AN INTERMITTANT SERVICE DOOR EICAS MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOU T INCIDENT. MAINTENANCE INSPECTED AND REMOVED THE INNER HANDLE. MAINTENANCE PERFORMED A DETAILED INSPECTION OF THE HAN DLE ASSEMBLY. NO DEFECTS FOUND. MAINTENANCE REINSTALLED THE INNER HANDLE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE M ANUAL. MAINTENANCE PERFORMED A CHECK OF THE PROXY SENSOR PX36 WHICH CHECKED GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080728 WP 2008 7 28 UPS08852590 1 20080626 A 3350 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:N/A ON EMERGENCY LIGHT TEST STANDBY ATTITUDE INDICATOR (SAI) AND STANDBY ALTIMETER INSTRUMENT LIGHTS INO P. EMERGENCY LIGHTING SYS CHECKS OK M/M 33-50-01-2-2. 2 L 7 4 4F RT 4A25 20080728 EA 2008 7 28 DJF2008F00004 1 20080615 A 2120 UNKNOWN CNDAIR CL601 CL6012A12 1900303 EA COCKPIT SMOKE E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 664CW 3064 WHILE REFUELING THE AC, THE CREW NOTED A SIGNIFICANT AMOUNT OF SMOKE IN THE COCKPIT. (SDR WILL BE COMPLETED AFTER MAINT ENANCE/ INSPECTION IS COMPLETE). (K) 2 L 7 2 4F RT A21AE 20080728 NM 2008 7 28 2008UALA03469 1 20080619 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR OBSTRUCTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 552UA 26641 DOOR 4R ARMING LEVER OUT OF ADJUSTMENT. FOUND A PIECE OF SAFETY WIRE AT THE GIRT BAR MECHANISM PUSHROD, CAUSING ROD TO BIND. REPOSITIONED WIRE, AFTER RE-INSTALL, OPS CHECK OF DOOR EMERGENCY MECHANISM, NORMAL NO BINDING. 2 L 7 2 4F 4 F RT A2NM E17NE 20080728 NM 2008 7 28 UPS08M52602 1 20080320 A 5330 SKIN DOUG MD11 MD11 3023602 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:C FWD CARGO DOOR CUTOUT AFT LOWER SKIN EDGE FROM RT L37-L42 FOUND SEVERAL BLENDOUT REPAIRS AS MARKED. F WD CARGO DOOR CUTOUT AFT LOWER HEATING TUBE & SKIN FASTENERS REMOVED. SKIN BLENDED REPAIR AREA TRIM OUT & REPROTECTED. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. REPAIR DOUBLERS & FILLERS FABRICATED, WITH HOLES PICKED UP, PR OTECTED & PAINTED. FAB REPAIR DOUBLERS & FILLERS INSTALLED. HEATING TUBE INSTALLED. 2 L 7 3 4F RT A22WE 20080728 WP 2008 7 28 UPS08852591 1 20080612 A 5320 47504211 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 FITTING CRACKED AT STA 680 AND LT LONGERON 13 AT MAIN CABIN. REPLACED FITTING AT STA 680 AND L13L IA W SRM 57-01-20D, SRM 51-03- 02. 2 L 7 4 4F RT 4A25 20080728 WP 2008 7 28 IXX2008F00010 1 20080712 A 2697 CONNECTOR DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE FIRE WARNING DAMAGED A IXXA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 11 830BX 45973 DURING CRUISE, NR 4 ENGINE FIRE WARNING LIGHT AND BELL CAME ON, THE CREW SHUTDOWN NR 4 ENGINE AND AS SOON AS T-HANDLE WA S PULLED THE BELL STOPPED AND LIGHT WENT OUT. THE CREW RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MAIN TENANCE REPLACED LT AND RT CORE SENSING ELEMENT, LT FAN SENSING ELEMENT, CONNECTOR P1-7072 AND CONNECTOR P1-7087. OPERA TIONAL CHECK GOOD IAW MM 26-10-0 AND 25-50-1. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 20080728 2008 7 28 HUN2008F00000 4 20080623 A 2562 110323 ANTENNA BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A42 52043 NE ELT CRACKED E HUNA O OTHER O OTHER NR NOT REPORTED 1 NM 01 999MM BB1997 ELT ANTENNA DEVELOPING HAIRLINE CRACKS APPROXIMATELY 1 INCH FROM THE BASE. THIS IS THE 3RD REPLACEMENT. SUSPECTED ICE OR FOD, BUT HAVE FOUND NO EVIDENCE OF EITHER. (K) 1 L 7 2 4T 4 T A24CE E4EA 20080728 EU 2008 7 28 UPS08152607 1 20080628 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 145UP 0828 INSPECTION TYPE:N/A EMERGENCY LIGHT TEST FAILED. REMOVED AND REPLACED LAV EMERGENCY LIGHT BULB IAW A300 MM 33-51-21-04. OPS CHECKS NORMAL. 2 L 7 2 4F RT A35EU 20080728 EU 2008 7 28 UPS08152600 1 20080613 A 2740 A55371714202 FITTING AIRBUS A300 A300F4622R 3930360 EU VERTICAL STAB CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 152UP 0835 INSPECTION TYPE:5YR VERTICAL STABILIZER LT GREEN SERVO FWD FITTING CHAFED AT ATTACH POINT. BLENDED OUT DAMAGE VERTICAL STABILIZER GREEN SERVO FWD FITTING IAW SAA EA 300-5530-01-A1427, UPS EO A300-5530-29724-A AND AIRBUS RAS/DAHAM/4025263/2 008. 2 L 7 2 4F RT A35EU 20080728 WP 2008 7 28 IXX2008F00009 1 20080626 A 2400 SWITCH DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE OVERRIDE BROKEN A IXXA O OTHER O OTHER NR NOT REPORTED 1 SW 11 825BX 45978 DURING CLIMB-OUT, OVER RIDE TOGGLE SWITCH BROKE OFF. AIRCRAFT RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MAINTENA NCE REMOVED AND REPLACED OVER RIDE SWITCH; OPS CHECK GOOD IAW UAL MM 74-20-36. (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 20080728 NM 2008 7 28 MWE2008F00010 1 20080713 A 3350 1315 LIGHT DOUG MD88 MD88 3023688 NM TAILCONE INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 822ME 49759 FORWARD TAILCONE EMERGENCY LIGHT INOPERATIVE, RELAMPED. (K) 2 L 7 2 4F RT A6WE 20080728 EU 2008 7 28 UPS08152599 1 20080613 A 2740 A55371713202 FITTING AIRBUS A300 A300F4622R 3930360 EU HORIZ STAB CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 152UP 0835 INSPECTION TYPE:5YR VERTICAL STABILIZER LT BLUE SERVO FWD FITTING CHAFED AT ATTACH POINT. BLENDED OUT DAMAGE ON BLUE SE RVO FWD FITTING IAW SAA EA 300-5530- 01-A1427, UPS EO A300-5530-29724-A AND AIRBUS RAS/DAHAM/4025263/ 2008. 2 L 7 2 4F RT A35EU 20080728 WP 2008 7 28 IXX2008F00011 1 20080711 A 3210 LANDING GEAR DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE MALFUNCTIONED A IXXA O OTHER O OTHER NR NOT REPORTED 1 SW 11 604BX 46046 DURING TAKEOFF, FLIGHT CREW WAS UNABLE TO RAISE GEAR HANDLE. FLIGHT CREW ACCOMPLISHED CHAPTER 3 PROCEDURES IN COCKPIT O PERATING MANUAL AND RAISED GEAR. GROUND CONTROL RELAY CIRCUIT BREAKER RELAYS WERE OPEN FOR FLIGHT AND RESET AFTER LANDI NG. AC LANDED UNEVENTFUL. OPEN (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 20080728 CE 2008 7 28 MTN2008F00000 1 20080711 A 3220 26940022 SHIMMY DAMPENER CESSNA 208 208B 2073701 CE PWA PT6 PT6* 52043 EA NLG MALFUNCTIONED E MTNA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 EA 68 962FE 208B0078 ON TAKEOFF ROLL A STRONG VIBRATION WAS COMING FROM THE NOSE LANDING GEAR. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETUR NED TO THE RAMP. MAINT REMOVED AND REPLACED THE SHIMMY DAMPENER AND RETURNED THE AC TO SERVICE. (K) 1 H 7 1 3T 3 T A37CE E2NE 20080728 EU 2008 7 28 UPS08152594 1 20080617 A 5321 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 152UP 0835 INSPECTION TYPE:5YR MAIN DECK CARGO FLOOR PNL 242LT HAS CRACK ON EDGE. REPAIRED MAIN CARGO FLOOR PNL 242LT IAW A300 SRM 53-10-20 TABLE 201 PAR 8A. 2 L 7 2 4F RT A35EU 20080728 NM 2008 7 28 2008UALA03511 1 20080620 A 5320 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 811UA 847 DOOR 2R, CREW DOOR SILL BEAM FOUND CORRODED. ACCOMPLISHED MAJOR REPAIR AT DEN. DOOR 2R, CREW DOOR SILL BEAM HAS EXCESS IVE MATERIAL REMOVED ON UPPER INBOARD FLANGE APPROX 4 INCHES FWD OF FR68 BY- 96274-MFG. SILL REPAIR PRIMED PAINTED, AND INSTALLED SRM 53-41-14. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 EU 2008 7 28 2008UALA03498 1 20080620 A 2913 D2913510100060 PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 FAILED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 439UA 683 YELLOW HYDRAULIC SYSTEM FAILURE. FLIGHT DIVERTED. NR 2 EDP FAILURE. REPLACED NR 2 ENG HYD PUMP, SERVICED HYD TO FULL, LEAKS CHECKED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 EU 2008 7 28 2008UALA03427 1 20080616 A 5210 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR DAMAGED A UALA O OTHER C F.O.D. IN INSP/MAINT 1 WP 29 482UA 1584 THE 1L DOOR DAMAGED DUE TO AIRSTAIR CONTACTING DOOR BOTTOM. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 EU 2008 7 28 QML2008F00001 1 20080612 A 2810 A1282Z3 DRAIN VALVE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE FUEL FILTER LEAKING E QMLA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 03 115LN 4155 ENROUTE TO SCENE, ONE CREWMEMBER DETECTED A FUEL ODOR. THERE WERE NO UNUSUAL COCKPIT INDICATION SUCH AS EXCESSIVE FUEL CONSUMPTION; BUT, IAW BRIEFING, THE PILOT ABORTED THE FLIGHT AND RETURNED TO BASE. MAINT FOUND A DRAIN VALVE ON THE FUE L FILTER LEAKING. (K) 1 G 7 1 3U 3 U H9EU E19EU 20080728 EU 2008 7 28 2008UALA03426 1 20080617 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN ODOR A UALA H DEACTIVATE SYST/CIRCUITS W INADEQUATE Q C NR NOT REPORTED 1 WP 29 477UA 1514 FLT ATTENDANTS REPORT ELECTRICAL SMELL FROM AFT GALLEY. SMELL DISSIPATED WHEN LIGHTS, OVEN, CHILLERS AND C-M'S TURNED O FF. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 EU 2008 7 28 2008UALA03421 1 20080617 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 402UA 439 EMERGENCY LIGHT TEST ON CIDS PANEL FAILED IT'S TEST. FAULTED THE UNIT. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 CE 2008 7 28 2008F00018 1 20080705 A 2800 UNKNOWN BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA FUEL SYSTEM ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 29 81536 UE152 DURING FLIGHT STRONG SMELL OF FUEL IN CABIN, PASSENGERS COMPLAINED. AUX TANKS SHOW ZERO FUEL ON GUAGES. INSPECTED AUX TANKS FOUND NO FUEL PRESENT. INSPECTED CABIN CLEANED RESIDUAL FUEL FROM CABIN FLOOR. (K) 2 L 7 2 4T 3 T RT A24CE E2NE 20080728 2008 7 28 HNA2008F00001 4 20080629 A 3442 0711319 TRANSCEIVER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE RADAR FAILED A HNAA O OTHER O OTHER CR CRUISE 1 EA 07 828EX 392 RADAR SPIKES, RADAR FAILED ENROUTE, THUNDERSTORM ACTIVITY WAS AHEAD OF THE FLIGHT. DISPATCHER AND CAPTAIN CHOSE TO HAVE FLIGHT RETURN. REMOVED AND REPLACED RADAR TR. OPS CHECK GOOD IAW SB 34-18. (K) 2 H 7 2 4T 4 T RT A13NM E20NE 20080728 EU 2008 7 28 NSV2008F00005 1 20080624 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY MALFUNCTIONED A NSVA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 27 370PX 340B300 LAV SMOKE LIGHT ILLUMINATED AFTER ENGINE START, NO SMOKE FROM LAV. AIRCRAFT RETURNED TO GATE AND MX SENT. MAINTENANCE DEFERRED LAV REF. NEF 232. (K) 2 L 7 2 4T RT A52EU 20080728 EU 2008 7 28 NSV2008F00000 1 20080629 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU CABIN ODOR A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 27 277MJ 340B277 AIR RETURN/ EMERGENCY DECLARED. AVIONICS SMOKE LIGHT WITH INDICATION OF SMOKE ODOR IN COCKPIT AT 9000 FT AFTER AUTOPIL OT ENGAGED. COMPLETED SMOKE DETECTION SYSTEM CHECK IAW AMM 26-13-00-05, SYSTEM CHECK AGAIN. INSPECTED AVIONICS BAY, NO FAULTS FOUND. GROUND OPS CHECK OF AVIONICS SYSTEM, OK. COULD NOT DUPLICATE LIGHT OR SMELL. (K) 2 L 7 2 4T RT A52EU 20080728 2008 7 28 DJF2008F00002 2 20080624 A 7261 ENGINE RAYTHN DH125 HAWKER800XP 7150012 CE NR 2 OVERSERVICED E DJFA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 23 893CW 258603 UPON TAXIING IN AFTER LANDING THE CREW REPORTED THE DUCT OVERHEAT LIGHT ILLUMINATED FOLLOWED BY SMOKE IN THE COCKPIT AND CABIN. THE CREW SHUTDOWN BOTH ENGINES AND STILL REPORTED SMOKE, AFTER SHUTTING DOWN THE BLEED AIR FROM THE APU THE SMO KE CLEARED AND THE APU WAS SHUTDOWN. MAINTENANCE FOUND THE NR 2 ENGINE OVER SERVICED, THEY REMOVED ONE QT OIL. MAINTENA NCE THEN PERFORMED APU AND ENGINE GROUND OPS CHECKS ALONG WITH A FULL ENVIRONMENTAL SYSTEM OPS CHECKS WITH NO DEFECTS FO UND. THE AC WAS RESTARTED AND HAS SINCE FLOWN WITH NO ISSUES. (K) 2 L 7 2 4F RT A3EU 20080728 NM 2008 7 28 2008UALA03407 1 20080615 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 SEAT EEL INOP 49 LT. RELAMPED EMERGENCY, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080728 NM 2008 7 28 2008UALA03406 1 20080615 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 WALL EEL INOP LT SIDE LAV 111. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080728 NM 2008 7 28 2008UALA03394 1 20080615 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT INOP ROW 1J FWD SECTION. RELAMPED EMERGENCY LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080728 EU 2008 7 28 2008UALA03375 1 20080613 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 496UA 1845 L2 DOOR SILL AT C68 IS CORRODED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 2008 7 28 2008UALA03374 4 20080613 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R1 DOOR LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 437UA 655 DOOR 1R SLIDE PRESSURE IS LOW. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 EA 2008 7 28 TRAX200800657 1 20080518 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 907EV 7648 LT SIDE FS 484 FLOOR SUPPORT INTERCOSTAL HAS A CRACKED FLANGE ON THE I/B SIDE OF LBL 36 AND A CRACK ATTACH ANGLE ON THE O/B SIDE OF LBL 27. DISCONNECTED MOUNT BOLTS ON CABLE GUIDE IAW 51-41-04. REPAIRED LT FS 484 LBL 36 I/B SIDE AND O/B S IDE OF LBL 27 IAW B/A REO 601R-53-41-059 APPLICABLE STEPS. INSTALLED SAME SERVICEABLE MOUNT BOLTS ON CABLE GUIDE IAW S RM 51-41-04. PRESSURE CHECKS DUE. PERFORMED LEAK CHECK OF THE LT SIDE FS 484 FLOOR SUPPORT INTERCOSTAL LBL 36 AND O/B L BL 27 IAW AMM 21-32-00-863-801. NO LEAKS NOTED AT THIS TIME. REPAIRED LT SIDE FS 484 FLOOR SUPPORT INTERCOSTAL IAW REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 2008UALA03372 1 20080616 A 5321 FLOOR PANEL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 810UA 843 AFT RIGHT FLOOR PANEL (TRIANGULAR) 262CF HAS CORROSION PITS AND MISSING METAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 EA 2008 7 28 TRAX200800635 1 20080514 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 379-477 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE AT LBL9 FS 379.00 TO FS 477.40. BLENDED CORROSION ON LBL 9 FS 349 TO FS 4 77.40 REMOVED .020" OF DAMAGE WITHIN LIMITS ALLOWED .035" OF REMOVAL. ALL WORK DONE IAW SRM 53-21-49. DK 7022603 JOB C OMPLETE. 2 L 7 2 4F RT A21EA 20080728 2008 7 28 2008UALA03222 4 20080605 A 3442 6225132622 TRANSCEIVER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE WEATHER RADAR INTERMITTENT A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 818UA 882 WEATHER RADAR SYSTEM INOP, RTFL. TRANSCEIVER IS INTERMITTENT. REPLACED TRANSCEIVER, OPS CHECK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 EU 2008 7 28 2008UALA03195 1 20080604 A 3510 OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW O2 LOW PRESSURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 464UA 1290 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. RESERVICE 1360 PSI. SERVICED 1740 PSI., NO LEAKS WERE NOT ED AT TIME OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 EA 2008 7 28 TRAX200800617 1 20080510 A 5530 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 VERTICAL STAB LOWER RT DRAG ANGLE IS CRACKED. PERFORMED EDDY CURRENT INSPECTION OF RIGHT V/STAB TO FUSELAGE DRAG ANGLE TO LOCATE END OF CRACK IAW NDTM 51-20-006 END OF CRACK IS MARKED. CUT AWAY DAMAGE FROM VERTICAL STAB LOWER RT DRAG ANGL E IAW REO 670-55-31-018. PERFORMED EDDY CURRENT INSPECTION OF CUT LINES ON RIGHT VERTICAL STAB TO FUSELAGE DRAG ANGLE IA W REO 670-55-31-018 PER NDTM 51-20-006 NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 20080724 NM 2008 7 24 2008UALA03428 1 20080615 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 FUSELAGE SKIN CRACKED LEFT SIDE OF FUSELAGE AT STATION 510 BETWEEN WINDOWS. 2 L 7 2 4F 4 F RT A16WE E21EU 20080725 EU 2008 7 25 2008UALA03503 1 20080622 A 7500 GA554912 TRANSDUCER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 BLEED FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 448UA 842 NR 1 ENG BLEED AIR TRIPPED OFF AND WOULD NOT RESET. RTFL. *S/D* BMC1 FAULTED 8HA1, AIR REGULATOR TRANSDUCER. REPLACED AIR REGULATOR TRANSDUCER, 8HA1, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080725 EA 2008 7 25 SWIA200819842 1 20080710 A 7603 LINKAGE CNDAIR CL600 CL6002B19 1900309 EA LT THROTTLE BROKEN A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 908SW 7540 FLT 6736 - LEFT ENGINE WENT TO IDLE CUTOFF WHILE REDUCING POWER. REPLACED THROTTLE QUADRANT ASSEMBLY AS REQUIRED PER AM M 76-11-01, P/N: FE210-008, S/N OFF: FR-787. 2 L 7 2 4F RT A21EA 20080725 CE 2008 7 25 GUU2008F00003 1 20080701 A 3297 WIRE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA MLG BROKEN A GUUA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 87555 UE234 AFTER TAKEOFF LANDING GEAR DID NOT RETRACT, LANDING GEAR CIRCUIT BREAKER POPPED WHEN HANDLE PUT DOWN WITH ONLY (2) GREEN LIGHTS. CIRCUIT BREAKER PUSHED IN AND GEAR WENT DOWN BREAKER POPPED AGAIN. RETURNED TO PBI LANDED WITHOUT INCIDENT. RE PAIRED BROKEN WIRE SPLICE AT LT LANDNG GEAR UPLOCK SWITCH. (K) 2 L 7 2 4T 3 T RT A24CE E4EA 20080725 WP 2008 7 25 MWE2008F00011 1 20080715 A 2422 2644000501 INVERTER DOUG DC9 DC981 3022081 WP EMERGENCY POWER INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 FOUND EMERGENCY POWER INVERTER NOT WORKING PROPERLY. REMOVED AND REPLACED EMERGENCY INVERTER. (K) 2 L 7 2 4F A6WE 20080725 NM 2008 7 25 GTI2008F00004 1 20080519 A 5320 SHEAR WEB AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 506NK 2490 CORNER SHEAR WEB CORRODED - Y1732 FRAME 69-70. REMOVED AND REPLACED SHEAR WEB. (K) 2 L 7 2 4F RT A28NM 20080725 NM 2008 7 25 MWE2008F00018 1 20080705 A 7830 7150922505 ANGLE BOEING 717 717200 1383700 NM THRUST REVERSER CRACKED A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 928ME 55194 RT THRUST REVERSER UPPER BUCKET HAS A Z-FRAME REPAIR THAT IS CRACKED AT STA 26.666 OB SIDE. FABRICATED AND INSTALLED AN GLE. (K) 2 L 7 2 4F TR A6WE 20080725 NE 2008 7 25 MT92008F00002 2 20080627 A 7314 025323150 PUMP CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE ENGINE FAILED E MT9A K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 05 9766B 208B0112 DURING AN OPERATIONAL INSPECTION, THE FUEL PUMP WAS REJECTED IAW SB1645. A REPLACEMENT PUMP WAS INSTALLED (TSO 0.0) AND ON THE OPERATIONAL RUN CHECKS THE FUEL PRESSURE LOW LIGHT AND THE FUEL PUMP ON LIGHT ON THE ANNUNCIATOR PANEL STARTED C YCLING WHEN THE TORQUE WENT ABOVE 1400 FT LPS. THIS PUMP WAS REPLACED WITH A SECOND PUMP (TSO 0.0). THE OPERATIONAL RU N CHECK PRODUCED THE SAME RESULTS AS THE FIRST REPLACEMENT PUMP DID. THE RESERVOIR TANK PRESSURE WAS CHECKED USING A GA UGE PLUMBED INTO THE SYSTEM AND IT WAS FOUND THAT AT IDLE, THE PRESSURE WAS 6.5 PSI. AS THE POWER WAS INCREASED AT 1200 FT LBS OF TORQUE, PRESSURE STARTED DROPPING OFF AND AT 1400 FT LBS OF TORQUE SYSTEM PRESSURE WAS AT 3.25 PSI. A THIRD PU 1 H 7 1 3T 3 T A37CE E4EA 20080725 NM 2008 7 25 MWE2008F00021 1 20080704 A 7830 715K9004507 ANGLE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE THRUST REVERSER CRACKED A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 902ME 55166 LT THRUST REVERSER DOOR Z-FRAME REPAIR AT STA 26.666 IS CRACKED ON THE IB SIDE. FABRICATED AND INSTALLED ANGLE. (K) 2 L 7 2 4F 4 F TR A6WE E00061EN 20080725 WP 2008 7 25 IXX2008F00013 1 20080718 A 2612 FIRE WARNING DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE FALSE ACTIVATION A IXXA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 11 821BX 45811 DURING CRUISE, THE NR 1 ENGINE FIRE WARNING LIGHT AND BELL CAME ON. THE FIRE WARNING LIGHT WENT OUT AND THE BELL STOPPE D RINGING. THE CREW TESTED THE SUCCESSFULLY TESTED THE SYSTEM AND PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN, AFTER ONE HOUR MORE OF FLIGHT TIME THE FIRE WARNING LIGHT ILLUMINATED AND THE BELL SOUNDED, THE CREW DISCHARGED BOTH FIRE BOTTLES. THE AIRCRAFT LANDED WITHOUT INCIDENT. (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 20080728 WP 2008 7 28 UPS08852587 1 20080611 A 5347 DC853B007002 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C1 STA 330 LBL 45 MAIN CABIN SEAT TRACK IS WORN IN 2 PLACES. REPLACED MAIN CABIN SEAT TRACK PLUG AT STA 330 AND LBL 45 IAW SRM 53-02-03 FIG 006. 2 L 7 4 4F RT 4A25 20080728 CE 2008 7 28 IEY2008F00000 1 20080701 A 5340 661503517 SUPPORT BRACKET CESSNA 560 560XL 2076702 CE FUSELAGE CRACKED E IEYA O OTHER O OTHER NR NOT REPORTED 1 GL 03 170SD 5605091 FOUND ENVIRONMENTAL CONTROL UNIT SUPPORT BRACKET CRACKED ON PRE-FLIGHT. 2 CRACKS ON EACH SIDE OF BENDS OF BRACKET, 1ST 4 INCHES LONG, THE 2ND 2 INCHES LONG. IF THE SECOND CRACK WAS ANY LONGER COMPLETE FAILURE OF SUPPORT BRACKET WOULD HAVE OCCURRED. RECOMMEND PARTICULAR ATTENTION BE PLACED TO INSPECT THIS AREA, WEIGHT OF ECU IS APPROXIMATELY 35 POUNDS. RE F MM, CHAPTER 21. (K) 2 L 7 2 4F RT A22CE 20080728 2008 7 28 EIA2008F00001 4 20080608 A 2565 7A124935 SLIDE BOEING 747 747230B 1384889 NM LT DOOR FAILED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 19 488EV 23287 CREW MEMBER OPENED LT UPPER DECK DOOR AND SLIDE DEPLOYED BUT DID NOT INFLATE. MEL ENTERED HOLD OPEN UNTIL FORMAL FIX. (K) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 2008UALA03373 1 20080615 A 3350 32145410 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 818UA 882 EPSU BATTERY FWD LEFT DISPLAYED AFTER CIDS EMERGENCY LIGHT TEST. REPLACED BATTERY ON 10WL EPSU. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 EA 2008 7 28 TRAX200800622 1 20080513 A 5420 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 978EV 7723 UPPER SURFACE OF ENGINE SUPPORT BEAM APPEARS CRACKED AT B.L. 0 AND FS 640. POSSIBLE CRACK NEEDS VERIFIED. PERFORMED EDD Y CURRENT INSPECTION OF ENGINE SUPPORT BEAM AT BL 0.00, FS 640.00, ENGINE SUPPORT BEAM VERIFIED CRACKED AT RIGHT HAND FA STENER HOLE FORWARD SIDE IAW NDTM 51-20-06. REPAIRED CRACKED UPPER SURFACE OF ENGINE SUPPORT BEAM IAW REO 601R-53-61-34 5 AND EO600-53-72-0001 REFER TO ATTACHED M-234 FOR. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800893 1 20080707 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 821AS 7194 AFT INTERIOR EMERG. LIGHT INOP. RELAMPED EMERGENCY AFT INTERIOR LIGHT IAW AMM 33-51-16. OPS CK GOOD. 2 L 7 2 4F RT A21EA 20080728 EU 2008 7 28 2008UALA03072 1 20080528 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 447UA 836 DOOR SILL 2L HAS CORROSION AT APPROX FRAME 68. CORROSION - ACP'ED REWORK, PRIMER AND TOP COAT REF SRM 53-00-14. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 2008 7 28 2008UALA03235 4 20080605 A 2565 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 589UA 28707 INBOARD CREW REPORTS DOOR 1 RIGHT HARD TO ARM. 2 L 7 2 4F 4 F RT A2NM E17NE 20080728 EA 2008 7 28 TRAX200800642 1 20080514 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 693-677 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE AT RBL 9 FS 693.00 TO FS 977.00. BLENDED CORROSION FOUND ON RBL 9 FS 693 T O FS 977 REMOVED .018" OF MATERIAL WITHIN LIMITS ALLOWED TO REMOVE .035" OF MATERIAL. ALL WORK DONE IAW SRM 53-41-49 AND 53-51-49. 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 2008UALA03232 1 20080606 A 5210 ROD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 524UA 24977 UNABLE TO DISARM DOOR 1R, FOUND LOWER GATE ACTUATING ROD BROKEN AND CORRODED AT LOWER ROD END BEARING. 2 L 7 2 4F 4 F RT A2NM E17NE 20080728 EA 2008 7 28 TRAX200800644 1 20080514 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 477-693 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE AT RBL 9 FS 477.40 TO FS 693.00. BLENDED CORROSION FOUND ON RBL 9 FS 477.4 0 TO FS 693.00 REMOVED .005" OF MATERIAL WITHIN LIMITS ALLOWED TO REMOVE .035" ALL WORK DONE IAW SRM 53-31-49. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800606 1 20080506 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 928EV 8006 RT INTERCOSTAL ANGLE BETWEEN FA 625.00 AT STR 14 HAS A 1" CRACK. REMOVED AND REPLACED RT INTERCOSTAL WITH NEW SERVICEAB LE INTERCOSTAL IAW REO 601R-53-61-422 AND SRM 51-42-21. (A) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800689 1 20080526 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 924EV 7830 SUPPORT ANGLE AT FS 280, RBL 9, INBD AND OTBD ARE CRACKED. REMOVED PSU PNL 11AB, 2AB AND 3AB IAW AMM 25-28-01-000-803. PSU PANELS 11AB, 2AB, AND 3AB REQUIRE REINSTALL. PSU PANEL 1AB, 2AB AND 3AB REINSTALLED PSU PANELS 1AB, 2AB AND 3AB I AW AMM 25-28-01-400-803 OPS CKS DUE. TEST POF PSU PPANEL 1AB 2AB AND 3AB IAW MM 33-24-00-710-801, 23-31-00-710-801, 33-2 2-00-710-801, AND 35-20-00-710-803 NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800614 1 20080508 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 928EV 8006 LT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED IN OUTBOARD RADIUS. RESOLVED ON W/O 90038 TASKCARD N/R 00182. REPAIRED LT FS 621.00 FLOOR SUPPORT ANGLE IAW REO 610R-53-61-117 REV C STEPS 1-7. REQUIRES TOP COAT. APPLIED TOPCOAT AS NEEDED IAW CRJ 200 SRM 51-25-01. LEAK CHECK DUE. PERFORMED LEAK CHECK OF LT 621.00 FLOOR SUPPORT ANGLE IAW CRJ AMM TASK 21-32-00 -863-801. NO LEAKS NOTED AT THIS TIME. C/W ASA REO 610R-53-61-117. [SUPPLEMENTAL SDR CLOSED 6/24/08] (A) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800690 1 20080526 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 924EV 7830 FS 484 ANGLE IS CRACKED AT THE OUTBOARD SIDE OF LBL 27. REMOVED AND REPLACED CRACKED ANGLE IAW REO 601R-53-41-059 WITH NEW SERVICEABLE PART. COMPLIED WITH REO 601R-53-41-059 STEP 1 THRU 5. RII COMPLIED WITH 5300040. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 MASA200800465 1 20080612 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STIFF A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 47202 7202 DIFFICULTY OPENING THE PAX DOOR. MX UNABLE TO DUPLICATE PROBLEM--OPS GOOD. (B) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800615 1 20080510 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 PAX DOOR EXIT PLACARD WORN. REPLACED EXIT PLACARD PER AMM 11-30-02. 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 AALA200801320 1 20080515 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 792AN 30253 MIA EMERGENCY LIGHT AT SEAT 24C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NOR MAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 NM 2008 7 28 AALA200801314 1 20080515 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 920AN 29521 LGA EMERGENCY LIGHT AT SEAT ROW 9 HAS BROKEN LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 9. SYSTEM GROUND CHEC KED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A16WE 20080728 EA 2008 7 28 TRAX200800632 1 20080514 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 978EV 7723 LT BATTERY RIB CRACKED. REMOVED AND DISGARDED DOUBLER PN 601R10203-31. TRIMMED AWAY DAMAGE AS SHOWN ON REO 601R-57-51- 046. CLEANED UP CUT LINE TO SMOOTH FINISH, FABRICATED -5 DOUBLER FROM 7075-0 .063 HEAT TREATED TO T-6 AND -7 FILLER FRO M 7075-T-6 .050 LOCATED ALL FASTERNER HOLES AND TRIMMED TO SIZE PER REO 601R-57-51-046. ALODINED, PRIMED AND PAINTED REP AIR PARTS SRM. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800862 1 20080701 A 5320 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR TRACK CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 861AS 7445 CARGO DOOR FWD TRACK LWR ATTACH STRUCTURE CHANNEL CRACKED. (MARKED) REMOVED AND REPLACED BAD CHANNEL BRACKET PER SRM 5 1042-06 . 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 AALA200801315 1 20080515 A 3350 LENS BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 920AN 29521 LGA EMERGENCY LIGHT AT SEAT ROW 9 HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 9. SYSTEM GROUND CHE CKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A16WE 20080728 NM 2008 7 28 AALA200801317 1 20080515 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 MIS EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORM AL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080808 NM 2008 8 8 08FDEA02690 1 20080703 A 5315 7075T6071 FLOORBEAM BOEING 757 757236 1384971 NM BS 365 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 MAIN CABIN FLOOR STA 365 RBL 58 FLOORBEAM CORROSION. REMOVED DAMAGE, FABRICATED ANGLES MAE TRAV T8/748437. FABRICATED T-CHORDS MAE TRAV T8/748430, IAW SRM 53-00-51. INSTALLED REPAIR PARTS STA 365 RBL 34-70 IAW SRM 53-00-51 FIG 201. RE PAIR 3. MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20080808 EU 2008 8 8 08FDEA02762 1 20080708 A 5754 SLAT TRACK AIRBUS 300 A300F4605R 3930327 EU RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 RIGHT WING NR 2 SLAT; NR 6 TRACK LOWER MOUNT BOLT IS CRACKED AND THE NUT IS CORRODED. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02698 1 20080704 A 5313 A53971006202 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION AT STRINGER P 53 LT, C 54.3-55. REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CORROSION REMOVAL AND FLAP PEENING IAW RAS/EFW/9000055/2008 ISS A, APPROVED BY EA 6-5316-123004. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02585 1 20080630 A 5754 SLAT TRACK AIRBUS 300 A300F4605R 3930327 EU LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 LEFT WING NR 2 SLAT NR 4 TRACK LOWER ATTACH BOLT IS CRACKED. REMOVED DAMAGED BOLT AND REPLACED IT WITH A NEW ONE IAW A3 00-600 AMM 27-80-12-4. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 PNS2008F00006 1 20080729 A 3213 SLEEVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE MLG CRACKED A PNSA O OTHER K FLUID LOSS NR NOT REPORTED 1 AL 03 109XJ 1005 340A109 PILOT WROTE UP A DISCREPANCY FOR HYDRAULIC OIL AROUND 31 GEAR LEG. MAINT FOUND THE NR 1 BRAKE ASSY LEAKING, PART WAS RE MOVED AND SENT OUT FOR O/H AND FIND THE CAUSE OF LEAK. VENDOR O/H UNIT FOUND THAT ONE OF THE CYLINDER SLEEVES PN 201264 8 WAS CRACKED AROUND THE NUT PORTION OF THE SLEEVE WITH PART OF THE NUT MISSING CAUSING THE O-RING TO BE EXPOSED TO THE ATMOSPHERE AND THEREBY LEAKING IAW THE CMM. THERE IS NO CRACK DETECTING INSP FOR THE CYLINDER SLEEVE ONLY A VISUAL INSP . VENDOR WILL, IN THE FUTURE, START A FLUORESCENT DYE PENETRANT INSP ON THE CYL SLEEVES. THE CRACK LOCATION MAKES IT V ERY DIFFICULT TO DETECT WITH A VISUAL INSP DUE TO CRACK EMANATING AT THE RADIUS OF THE NUT AND SHANK OF THE CYLINDER SLE 2 L 7 2 4T 4 T RT A52EU E8NE 20080811 EA 2008 8 11 CIE2008F00003 2 20080717 A 7320 304964201 FCU BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA LT ENGINE MALFUNCTIONED E CIEA K NONE O OTHER IN INSP/MAINT 1 NM 03 60PD BB58 PCER0024 WHILE PERFORMING ENGINE RUN UP AT RUNWAY 36R RUN UP, LT ENGINE WAS FOUND TO BE UNRESPONSIVE AFTER LT ENGINE PROP GOVERNO R CHECK WAS COMPLETE. N1 DROPPED BELOW 50 PERCENT AND CONTINUED TO DROP. FUEL FLOW ALSO DROPPED AND CONTINUED TO DROP. ENG WAS THEN SHUTDOWN AND MOTORED FOR 30 SECONDS. REPLACEMENT FCU WITH MODES S/B 24 ACCOMPLISHED, WAS INSTALLED AND T ORQUED. THE P3 AND THE PY LINES WERE MM 73-20-00. A NEW O-RING WAS INSTALLED, TORQUED AND SAFETIED. THE CONDITION LEV ER WAS CONNECTED TO THE CONTROL ARM AND BOLT WAS TIGHTENED, TORQUED AND SAFETIED. FCU DRAIN LANE WAS CONNECTED. AIRFRA ME FUEL RETURN LINE WAS INSTALLED AND TORQUED. THE 11" ROD WAS INSTALLED AND THE DEAD BAND INITIALLY SET. UNIT NEEDS T 1 L 7 2 4T 4 T A24CE E4EA 20080811 NM 2008 8 11 UIE2008F00023 1 20080707 A 7810 SKIN BOEING 747 747243B 1384830 NM NR 4 EXHAUST CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 CARRY OUT NR 4 PYLON EXHAUST SKIN CRACK CONDITIONAL CHECK REF EO NR 4754A250. REPAIRED CRACK IAW MFG MESSAGE 1-29998488 2-19. (K) 2 L 7 4 4F RT A20WE 20080811 NM 2008 8 11 BEF2008F00001 1 20080704 A 2913 623303 PUMP BOEING 757 757200 1384950 NM PWA 2037 PW2040 NE HYD SYSTEM INOPERATIVE A BEFA O OTHER J WARNING INDICATION CR CRUISE 1 WP 19 741PA 24737 2 HOURS INTO FLIGHT LT HYD ACMP PRESSURE DROPPED TO LESS THAN 200 PSI. AMBER LIGHT ON SWITCH ON SWITCH ILLUMINATED. QR H COMPLIED WITH , LT ACMP DESELECTED. RETURNED TO DEPARTURE AIRPORT. (K) 2 L 7 2 4F 4 F RT A2NM E17NE 20080811 NM 2008 8 11 HNA2008F00011 1 20080527 A 3350 OLBPE3071GPL LAMP DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS BURNED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 911HA 57470 034 2ND RED FLOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB OPS CHECK GOOD MEL 33-13-2, CLEARED. (K) 2 H 7 2 4T RT A13NM 20080811 EU 2008 8 11 M7K2008F00141 1 20080414 A 6220 350A31182703 FREQ ADAPTER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE M/R HEAD CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 807MH 2135 M2628 3912 23130 DURING ROUTINE INSP A CRACK IN THE YELLOW BLADES FREQUENCY ADAPTER WAS FOUND TO EXCEED THE MM 10MM LIMITATION, CRACK WAS FOUND ON THE T/E SIDE OF THE ADAPTER. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 NE 2008 8 11 R612008F00003 2 20080710 A 7200 ENGINE EMB ERJ170 ERJ170200LR 3260121 NM GE CF34 CF348E5 30061 NE NR 2 POWER LOSS A R61A O OTHER J R WARNING INDICATION PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 11 131HQ 17000215 DURING AC DESCENT, CREW RECEIVED AN EICAS ENGINE CONTROL FAULT MESSAGE AND ENGINE WAS DECELERATING. CREW FOLLOWED QRH P ROCEDURES AND SHUTDOWN NR 2 ENGINE. DECLARED AN EMERGENCY LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO AC RE SET POWER AND CLEARED ALL ENGINE CONTROL FAULTS IAW SB 170-73-A0005. MAINT AND CREW COMPLETED ALL REQUIRED OPERATIONAL CHECKS. ALL OPERATIONAL CHECKS WERE GOOD AND MAINT RETURNED AC TO SERVICE. (K) 2 L 7 2 4F 4 F RT A56NM E00063EN 20080811 EA 2008 8 11 S9BA2008025 1 20080713 A 2730 C8CF11377 BELLCRANK DHAV DHC6 DHC6300 2802606 EA ELEVATOR WORN A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 562CP 562 DURING AD 89-24-06 FOUND ELEVATOR BELL CRANK WORN. REMOVED AND REPLACED ELEVATOR BELL CRANK. NO OTHER DEFECTS NOTED. (S) 1 H 7 2 3T RT A9EA 20080811 SO 2008 8 11 SIM2008F00017 1 20080721 A 5320 EPMEM53EP54701 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 842AE 145673 DURING MBV A PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THAT EXISTING REPAIR DOUBLER A ND CLEANED THE AREA. POSITIONED, MARKED, DRILLED, TREATED AND INSTALLED NEW REPAIR DOUBLER PN EPNEM53EP54701. REPAIRS PERFORMED IAW SRM 53-00-10. AC RETURNED FOR SERVICE. (K) 2 L 7 2 4F RT T00011AT 20080811 NM 2008 8 11 USAA920081366 1 20080704 A 5320 6935352U14 TIE CLIP BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT-Q3 CHECK MAJOR REPAIR NR 03C10853043/007. TIE CLIP CRACKED AT BS867, S9L. REPLACED TIE CLIP AT BS867, S9L IAW B737 SRM 52-10-02 AND SRM 52-40-02. (B) 2 L 7 2 4F RT A16WE 20080811 GL 2008 8 11 ZLW2008F00000 1 20080612 A 2760 C473 ECU BOMBDR BD100 BD1001A10 1390044 GL GROUND SPOILERS FAILED E ZLWA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SW 05 480CB 255 20147 THE GROUND SPOILER ELECTRONIC CONTROL UNIT FAILED PRIOR TO SCHEDULED FLIGHT. (K) 2 L 7 2 4F RT T00005NY 20080806 EU 2008 8 6 SIMA200819905 1 20080715 A 5311 FRAME SAAB SF340 340B 7860101 EU FS 686 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 392AE 340B392 DURING A HMBV INSPECTION, THE RT SIDE FUSELAGE FRAME AT FS 686.888 WAS FOUND DENTED. STRAIGHTENED THE FRAME FLANGE. PE RFORMED NDT OF FRAME FLANGE, NO CRACKS NOTED. FABRICATED A REPAIR DOUBLER USING AL 2024-T3. DRILLED, TREATED AND INSTA LLED REPAIR DOUBLER. REPAIR DONE IAW SAAB 340 SRM (SRM 72LKS 3079 REV 50) CHAPTER 53-80-30. ACFT RETURNED TO SERVICE. (S) 2 L 7 2 4T RT A52EU 20080806 NM 2008 8 6 AALA200801733 1 20080629 A 3350 8200037750 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 752AN 30260 MIA - EMERGENCY LIGHT AT SEAT 21C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHTS AT SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20080806 NM 2008 8 6 AALA200801738 1 20080630 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 782AN 30003 JFK - EMERGENCY LIGHTS AT FORWARD FIRST CLASS CABIN CLOSET AREA INOPERATIVE. REPLACED IN WALL LIGHT ASSEMBLY FOR EMERGE NCY LIGHTS AT FORWARD FIRST CLASS CABIN CLOSET AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20080806 NM 2008 8 6 AALA200801437 1 20080530 A 3350 1317 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 922AN 29523 LGA - EMERGENCY LIGHT AT SEAT ROW 20ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 20ABC. SYSTEM GROUN D CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A16WE 20080806 WP 2008 8 6 ABXA080191 1 20080715 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC931 3022065 WP EMERGENCY LIGHT DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 946AX 47003 EMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-00. (S) 2 L 7 2 4F A6WE 20080806 WP 2008 8 6 AALA200801448 1 20080601 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 227AA 49177 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 28 TO 30 INOPERATIVE. CLEANED CORROSION ON BATTERY PACK AT SEAT ROW 28 FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 28 TO 30. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080806 WP 2008 8 6 AALA200801451 1 20080601 A 3350 LAMP DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9681B 53631 SFO - EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT A6WE 20080806 NM 2008 8 6 AALA200801454 1 20080601 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 DFW - EMERGENCY LIGHT AT SEAT 40C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 40C. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 NM 2008 8 6 AALA200801385 1 20080524 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 640A 24598 DFW - EMERGENCY LIGHT AT RIGHT NR TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT NR TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080806 NM 2008 8 6 AALA200801393 1 20080525 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 628AA 24586 DFW - EMERGENCY LIGHT AT SEAT ROW 17D INOPERATIVE. REPAIRED CONNECTION FOR EMERGENCY LIGHT AT SEAT ROW 17D. SYSTEM GRO UND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080806 NM 2008 8 6 AALA200801395 1 20080526 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 791AN 30254 DFW - EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 WP 2008 8 6 AALA200801402 1 20080526 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 245AA 49257 LGA - EMERGENCY LIGHT AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080806 EU 2008 8 6 AALA200801404 1 20080526 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 JFK - EMERGENCY LIGHT AT LT NR ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LT NR ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080806 NM 2008 8 6 AALA200801363 1 20080522 A 3397 CONNECTOR DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9413T 53188 SFO - EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPLACED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECK ED NORMAL OPERATION. (A) 2 L 7 2 4F RT 20080806 EU 2008 8 6 AALA200801407 1 20080526 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 JFK - EMERGENCY LIGHT AT LT NR FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LT NR FOUR DOOR. SYSTEM GRO UND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080806 WP 2008 8 6 AALA200801362 1 20080521 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 510AM 49804 LGA - EMERGENCY LIGHT AT SEAT ROW 13CDE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 13CDE. SYST EM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 2008 8 11 EYD2008F00000 4 20080727 A 3130 1301561 CHECK VALVE BRAERO DH125 HS125700A 4230170 EU GARRTT TFE731 TFE731* 01518 WP CABIN PRESSURE FAILED E EYDA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 19 411PA NA0211 WHILE ENROUTE, THE FLIGHT CREW EXECUTED AN EMERGENCY DESCENT DUE TO A "CABIN ALTITUDE" WARNING LIGHT, MAINTENANCE HAS FO UND 2 DEFECTIVE CHECK VALVES, PN 130156-1 AND 2 PRESSURE REGULATORS, PN 1024665, THAT WERE SUSPECT. ARE ALSO REPLACING THE ENTRY DOOR SEAL AS A PRECAUTION. (K) 2 L 7 2 4F 4 F A3EU E6WE 20080811 NM 2008 8 11 AALA200801751 1 20080701 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 909AN 29511 DFE - EMERGENCY LIGHT AT SEAT ROW 13D MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 13D. SYSTEM GROUND CHE CKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A16WE 20080811 NM 2008 8 11 AALA200801759 1 20080702 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 601AN 27052 DFW - EMERGENCY LIGHT AT LT AFT OVERWING DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LT AFT OVERWING. SYST EM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 NM 2008 8 11 AALA200801652 1 20080607 A 3397 WIRE DOUG MD80 MD83 3023681 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9412W 53187 SFO - EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHE CKED NORMAL OPERATION. (A) 2 L 7 2 4F RT 20080811 NM 2008 8 11 AALA200801612 1 20080613 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AM 24594 DFW - EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 29D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 NM 2008 8 11 AALA200801610 1 20080613 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AM 24594 DFW - EMERGENCY LIGHT AT SEAT 16C INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 16C. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 WP 2008 8 11 AALA200801534 1 20080605 A 2781 833605A CONTROLLER DOUG DC9 DC982 3022082 WP L/E SLAT INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 7525A 49917 PHX INFLIGHT T1023/05JUN AUS TO SJC. DURING SLAT RETRACTION SLAT DISAGREE LIGHT ILLUMINATED. LANDED PHX WITHOUT INCIDE NT. REPLACED PROXIMITY SWITCH CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 NM 2008 8 11 AALA200801535 1 20080605 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 797AN 30012 DFW - EMERGENCY LIGHT AT SEAT 20C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080811 NM 2008 8 11 AALA200801515 1 20080604 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 762AN 31479 DFW - EMERGENCY LIGHTS AT OVERHEAD SEAT 22G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 22G. SYSTE M GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080811 NM 2008 8 11 AALA200801524 1 20080604 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 762AN 31479 DFW - EMERGENCY LIGHTS AT SEAT 25C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080811 WP 2008 8 11 AALA200801577 1 20080610 A 2560 BATTERY DOUG DC9 DC982 3022082 WP FLASHLIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 274AA 49271 LGA - EMERGENCY FLASHLIGHT AT FORWARD LOWER CABIN INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT FORWARD LOW ER CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 EU 2008 8 11 AALA200801760 1 20080703 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 MIA - EMERGENCY LIGHT AT LT NR THREE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LT NR THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080811 NM 2008 8 11 AALA200801785 1 20080706 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 638AA 24596 DFW - EMERGENCY LIGHTS AT SEAT ROWS 27 TO 36 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 27 TO 36. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 EA 2008 8 11 HNA2008F00016 1 20080626 A 5240 DOOR DHAV DHC8 DHC8311 1386006 EA SERVICE OPEN A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 336EN 336 RETURNED TO GATE, MAINTENANCE CLOSED DOOR (SERVICE DOOR WARNING LIGHT ILLUMINATED PRIOR TO TAKEOFF). (K) 2 H 7 2 4T RT A13NM 20080811 NM 2008 8 11 DXTA200803166 1 20080709 A 2120 UNKNOWN AMD FALC50 FALCON2000 2730170 NM CABIN ODOR E DXTA K NONE O B OTHER SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 07 280QS 181 DURING TEST OF THE EMERGENCY LIGHTS SYSTEM, FROM "ARM" TO "ON" THERE WAS AN INTENSE FOREIGN ODOR, SUSPECT SULFUR ODOR. S TARTED IN COCKPIT AND WAS DETECTED THROUGHOUT CABIN. (A) 2 L 7 2 4F RT A50NM 20080811 EU 2008 8 11 HAEA200800205 1 20080604 A 2612 3601709004001 FIRE LOOP AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE NR 1 NACELLE SHORTED E HAEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 05 221TW 11344 221 304319B AC DEPARTED AND CLIMBED TO 3000 FT MSL. NR1 ENG FIRE WARNING HORN AND LIGHT ACTIVATED. AC DECLARED EMERGENCY AND RETURNE D TO DEPARTURE. MAINT FOUND NO EVIDENCE OF FIRE. DISCOVERED NR1 FIRE LOOP SHORTED OUT. REPOSITIONED AND TESTED FIRES SYS WARNING. OPS CHECK SYS IS NORMAL. (A) 2 L 7 2 4F 4 F A7EU E7EA 20080811 WP 2008 8 11 AALA200801644 1 20080617 A 2421 GENERATOR DOUG DC9 DC983 3022083 WP NR 1 ENGINE MALFUNCTIONED A AALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SW 21 963TW 53613 PHX INFLIGHT T1406/17JUN. CAPTAIN AND FIRST OFFICERS ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EFIS) SCREENS CYCLED ON AND O FF FOR 60 TO 90 SECONDS FOLLOWED BY NR ONE GENERATOR TRIPPING. RESET NR ONE GENERATOR. EFIS CONTINUED TO CYCLE BUT THE NUMBER ONE GENERATOR REMAINED ON. REPLACED NR ONE CONSTANT SPEED DRIVE AND GENERATOR. SYSTEM GROUND CHECKED NORMAL OP ERATION. (A) 2 L 7 2 4F RT A6WE 20080811 NM 2008 8 11 AALA200801613 1 20080613 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 636AM 24594 DFW - EMERGENCY FLOODLIGHT AT SEAT 29D NOT BONDED TO BULL NOSE TRIM. BONDED EMERGENCY FLOODLIGHT AT SEAT 29D TO BULL NO SE TRIM. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 EA 2008 8 11 HNA2008F00017 1 20080626 A 2150 ACM DHAV DHC8 DHC8311 1386006 EA MALFUNCTIONED A HNAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 07 337EN 284 CABIN HOT PACK CAUTION LIGHT ILLUMINATED ON TAXI OUT. MAINT REPLACED REAR AIR CYCLE MACHINE. OPS CHECK GOOD. (K) 2 H 7 2 4T RT A13NM 20080811 NM 2008 8 11 AALA200801646 1 20080617 A 3350 SHROUD BOEING 737 737823 13844BZ NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 925AN 29526 DFW - EMERGENCY LIGHT AT SEAT ROW 7 HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 7. SYSTEM GROU ND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A16WE 20080811 CE 2008 8 11 GUU2008F00015 1 20080616 A 3297 WIRE BEECH 1900 1900D 1154162 CE UPLOCK SWITCH BROKEN A GUUA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 17 190YV UE190 FLIGHT 5403, DURING APPROACH, LANDING GEAR INDICATOR CIRCUIT BREAKER POPPED NO GREEN OR RED LIGHTS WHEN GEAR INTRANSIT O R DOWN AND LOCKED. C/A REPAIRED BROKEN WIRE ON RT MLG UPLOCK SWITCH. (A) 2 L 7 2 4T RT A24CE 20080811 NM 2008 8 11 HNA2008F00008 1 20080316 A 5315 85350471111 FLOORBEAM DHAV DHC8 DHC8102 2809003 NM BS 253 CRACKED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 846EX 326 FOUND FLOORBEAM CRACKED AT FUSE STA 253 APPROX, IN FRONT OF RT EMERGENCY EXIT DOOR. REPLACED WITH NEW PART NR 853204711 11 AND INSTALLED WITH SOLID RIVETS IAW SRM 51-40-00. (K) 2 H 7 2 4T RT A13NM 20080811 WP 2008 8 11 AALA200801704 1 20080625 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7530 49922 LGA - EMERGENCY FLASHLIGHT AT FORWARD CABIN UPPER POSITION HAS BROKEN SAFETY STRAP. REPLACED SAFETY STRAP FOR EMERGENCY FLASHLIGHT AT FORWARD CABIN UPPER POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 WP 2008 8 11 AALA200801712 1 20080626 A 1100 PLACARD DOUG DC9 DC982 3022082 WP TAILCONE WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 474 49649 LGA - PLACARD AT TAIL CONE OUTER EMERGENCY EXIT WORN. REPLACED PLACARD FOR AT TAIL CONE EMERGENCY EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 NM 2008 8 11 AALA200801527 1 20080604 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 762AN 31479 DFW - EMERGENCY LIGHTS AT SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080811 WP 2008 8 11 AALA200801763 1 20080703 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 479AA 49654 LGA - EMERGENCY LIGHT AT OVERWING EXIT INOPERATIVE. RE-SECURED BATTERY PACK FOR EMERGENCY LIGHT AT OVERWING EXIT. SYST EM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 EA 2008 8 11 N6WA0080701 1 20080716 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA COCKPIT ODOR A N6WA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 153GJ 10219 FLIGHT 6388-DIVERTED. SMOKE IN COCKPIT AT 37000 OVER JHW, PERFORMED APPROPRIATE CHECKLISTS, DIVERTED. PERFORMED OPS AN D LEAK CHECK AT OF AC DISTRIBUTION SYSTEM IAW AMM 21-51-00. LEAK CHECK OF BLEED AIR DISTRIBUTION SYSTEM IAW AMM 38-10-0 0. PERFORMED GROUND POWER RUN IAW AMM 71-00-00. NO FAULTS FOUND. (S) 2 L 7 2 4F RT A21EA 20080811 NM 2008 8 11 AALA200801576 1 20080610 A 2740 6355C00001 ACTUATOR BOEING 737 737823 13844BZ NM STABILIZER TRIM MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 917AN 29518 CUN INFLIGHT T364/10JUN CZM TO DFW. CREW REPORTED STABILIZER TRIM FAULT DURING CLIMB. LANDED CUN WITHOUT INCIDENT. CA PTAIN REPORTED NO SIGNIFICANT CONTROL PROBLEMS. REPLACED STABILIZER TRIM ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERAT ION. (A) 2 L 7 2 4F RT A16WE 20080811 WP 2008 8 11 AALA200801792 1 20080707 A 3397 WIRE HARNESS DOUG DC9 DC983 3022083 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 984TW 53634 SFO - EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. SECURED WIRE HARNESS FOR EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND CHE CKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A6WE 20080813 NE 2008 8 13 NWAA083069941 2 20080710 A 7200 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D15 52051 NE NR 2 FLAMED OUT A NWAA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 GL 01 3324L 57548 47899 47103 708313 DURING TOP OF DESCENT AS THRUST WAS REDUCED, ENGINE NR 2 FLAMED OUT. FLIGHT CREW DIVERTED TO ABE PERFORMING AN UNEVENTF UL LANDING. MAINTENANCE REPLACED ENGINE NR 2. (A) 2 L 7 2 4F 4 F A6WE E2EA 20080813 SO 2008 8 13 RAIA00807017 1 20080725 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 806HK 145112 PRE FLT 7888-IAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE DEFERRED THE AFFECTED LIGHT IAW MEL PROCEDURES. (S) 2 L 7 2 4F RT T00011AT 20080814 NM 2008 8 14 UPS08M52653 1 20080613 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 271UP 48572 INSPECTION TYPE-C, RT WING NR 3 FUEL TANK STRINGER 10 END SUSPECT CRACK AS MARKED. CRACK AT STR 10 OF RHW TANK SLOTTED OUT IAW SRM 57-20-00 IFG.10V.1 R 40. HFEC INSP C/OUT IAW NDT SPM R.13 PART 06.10.01.001 ON SLOTTED A REA FOUND NO CRAC K EVIDENT. REP PARTS FAB IAW SRM 57-20-00 FIG.10V.1R.40 REP PARTS HOLES P/UP IAW SRM 57-20-00 FIG.10V.1R.40. OK TO INST ALL REP PARTS STR 10 RHW SPLICE FASTENERS AT REPAIR AREA. 2 L 7 3 4F RT A22WE 20080814 NM 2008 8 14 UPS08M52654 1 20080613 A 5313 STRINGER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 271UP 48572 INSPECTION TYPE-C, LT WING FUEL TANK UPPER STRINGER 39 END SUSPECT CRACK. CRACK AT STR 9 LHW SLOTTED OUT IAW SRM 57-20- 00 FIG10 V.1R.40.HFEC INSP C/OUT IAW NDTSPM R.13 PART 06-10-01.001 ON SLOTTED OUT AREA FOUND NO CRACK EVIDENT. REP PART S FAB IAW SRM 57-20-00 FIG.10V.1R.40. REP PARTS HOLES P/UP IAW SRM 57-20-00 FIG.10V.1R.40. OK TO INSTALL REP PARTS STR 9 LT WING SPLICE END & FASTENER AT REPAIR AREA. 2 L 7 3 4F RT A22WE 20080814 CE 2008 8 14 DJF2008F00010 1 20080729 A 2797 WIRE BEECH MU300 400A 1155402 CE COCKPIT SEVERED A DJFA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 EA 23 429LX RK265 REPORTED CO-PILOT`S ROLL TRIM WOULD NOT TRIM WHEN MOVED TO THE RT. MAINTENANCE FOUND THE ROLL TRIM WIRING SEVERED AT TH E YOKE. THE WIRING HAD CONTACTED THE PRIMARY FLIGHT DISPLAY. THE WIRING WAS REPAIRED AND THE ACFT WAS RETURNED TO SERV ICE. (S) 2 H 7 2 4F RT A16SW 20080814 WP 2008 8 14 UPS08852790 1 20080702 A 5720 STRUCTURE DOUG DC8 DC871F 302199D WP RT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, RT WING LE AUX TANK UPPER T CAP HAS DOUBLE DRILLED HOLE STA. XFS 92. FABBED AND INSTALLED REPAIR D OUBLER IAW SRM, 51-1-8, 51-1-26, 57-2-1 F IG37. 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 UPS08852752 1 20080627 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, CORRODED LOWER ATC-2 ANTENNA INSTALLATION AREA EXTERNAL SKIN AT STA. Y 427-5 RBL3. FABBED AND INST ALLED REPAIR DOUBLER IAW SRM, 51-1-8, 53-2-00 FIG 1F51- 3-2, 51-1-22. 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 UPS08852757 1 20080630 A 5347 3657502U509 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, F/O'S BOTH LT AND RT SEAT TRACKS HAVE ELONGATED HOLES. REMOVED AND REPLACED SEAT TRACKS IAW SRM, 51 -1-20D, 51-1-24, 51-3-1. 2 L 7 4 4F RT 4A25 20080814 EU 2008 8 14 08FDEA03040 1 20080724 A 7830 DOOR AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 NR 2 ENGINE INBD REVERSER LOWER DOOR FLANGE IS DAMAGED. EVALUATED 6 WORN AREAS. 2 HAD MATERIAL LOSS OF .005 AND 2 EA H AD MATERIAL LOSS OF 0.010. THESE 4 AREAS ARE WITHIN LIMITS REF MRA CMM 78-32-02. 1 AREA HAD A MATERIAL LOSS OF 0.045 & 1 AREA HAD 100% MATERIAL LOSS. 2 AREAS FOUND TO BE OUT OF LIMITS REF MRA CMM 78-32-02. CUT OUT DAMAGE REF MRA CMM 78-3 2-01 & EA 6-7830-123624. FABRICATED; PRIMED & INSTALLED WEAR STRIPS REF MRA CMM 78-32-01. 2 L 7 2 4F RT A35EU 20080814 EU 2008 8 14 08FDEA03049 1 20080724 A 5347 A53611640200 SEAT TRACK AIRBUS 310 A310222 3930315 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 455FE 331 MAIN DECK FLOOR LEVEL COURIER COMPT TRACK BETWEEN FR 15A-FR 16A, -Y950 WITH EXFOLIATION CORROSION. REPLACED THE SEAT TR ACK PER SRM 51-40-21 & DWG A53611640200. RESTORED FINISH PER SRM 51-75-10 2 L 7 2 4F RT A35EU 20080814 WP 2008 8 14 08FDEA02892 1 20080715 A 5311 ADA00675 FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 IN THE CAC, THE FUSELAGE FRAME LOWER ANGLE IS CORRODED ON THE AFT SIDE AT STA 1119 FROM LONGERON 40R TO 41 R. FUSELAGE FRAME IN THE CAC, LOWER ANGLE CORROSION AT STA 1119, LONGERON 40R TO LONGERON 41R. FOUND TO BE OUT OF LIMITS. REMOVED "J" CHANNEL AS PART OF THE "J" CHANNEL REPAIR ACCOMPLISHED ON N/R N00967. 2 L 7 3 4F RT A22WE 20080814 WP 2008 8 14 IXX2008F00035 1 20080709 A 5754 SKIN DOUG DC8 DC872F 302199E WP SLOT VANE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR RT WING OUTBOARD SLOT VANE LEADING EDGE AT STATION XOLDI 6.224. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECT ION. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLERS, FILLERS, AND INTERNAL DOUBLERS. CLEANED, TREATED AND P RIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XOLDI 6.224 - XOLDO 67.000 IAW FAA FOR M 8110-3 08378 DATED 07/11/2008. SEMAN DRAWING ED-4809 DATED 06/23/08, DC8 SRM 51-1-21, SRM 51-3-0, DC8 NDT SPM PART 06- 10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-1-20D AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 IXX2008F00054 1 20080614 A 5751 SKIN DOUG DC8 DC872F 302199E WP AILERON MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD AILERON UPPER SKIN IMPROPER REPAIRS AT STATION XA 630.000-724. 000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, DOUBLER. BONDED PA RTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. PERFORMED BALANCE FOUND WITHIN LIMITS MOME NT =3326.3 IN-LB. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XW 546.000-XA 724.000 IAW DC8 SRM 57-8-1 FIGURE 4 ITEM "F" AND "G", DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DOUGLAS DRAWING 5763133, DC8 SRM 51-1-9 TR 51-142, SRM 51-1-9A TR 51-141, DC8 SRM 51-1-8B, IAW DC8 SRM 51-4-3 PAGES 1-6, DC8 SRM 51-1-11, AND SRM 51-1-21. (S) 2 L 7 4 4F RT 4A25 20080814 NM 2008 8 14 08FDEA02923 1 20080716 A 3340 694710566 MODULE BOEING 727 727233 138408A NM LANDING LIGHT FAILED A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 CE 21 266FE 21672 DURING GEAR EXTENSION RECEIVED UNSAFE NOSEGEAR (NO GREEN LIGHT) ALL GEAR INDICATIONS S/O PANEL NORMAL, NO GEAR WARNING H ORN DURING THROTTLE REDUCTION. COMPLIED WITH QRH, MANUAL GEAR EXTENDED. LIGHT REMAINED OUT. AFTER CRANKING NOSEWHEEL TO STOPS, LIGHT REMAINED OUT. TESTED LIGHT FOR SECOND TIME, LIGHT BLINKED AND THEN CAME ON. ON GROUND, LIGHT TESTS INT ERMITTENTLY. REMOVED AND REPLACED LANDING GEAR LIGHT MODULE. 2 L 7 3 4F RT A3WE 20080814 WP 2008 8 14 IXX2008F00055 1 20080613 A 5753 SKIN DOUG DC8 DC872F 302199E WP T/E FLAP MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP PANEL UPPER PART HAS IMPROPER REPAIR AT STATION 360.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PR IMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XF 345.000-360.000 IAW DC8 SRM 57-1-0 PA GE 1, SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 4 ITEM "B" TR 57-94 DATED 10-01-2002, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51- 3-0, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 08FDEA03006 1 20080721 A 5320 AFA0161115 SUPPORT ANGLE DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 CENTER PIT CEILING SUPPORT AT STA 1761, FROM BL 80R TO BL 110R P/N AFA0161-115 IS SMASHED. REMOVED CEILING SUPPORT ANGL E AT FS 1761 FROM BL 80R TO BL 110R. MATERIAL ID FOR THE ANGLE IS 2024-T3, 0.040, PO 614877.2. FABRICATED, LOCATED AND DRILLED ANGLE IAW DAC DWG AFA0161, REV AV. ALODINED AND PRIMED ANGLE IAW DC/MD-10 SRM 51-21-01, VOL II. INSTALLED ANG LE IAW DC/MD-10 SRM 51-31-01, VOL I. 2 L 7 3 4F RT A22WE 20080814 NM 2008 8 14 08FDEA03059 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL TANK ACCESS CUTOUT 642AB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS C LASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080814 EA 2008 8 14 TRAX200800949 1 20080731 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA A/C BAY DIRTY A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 927EV 7844 FUEL SMELL IN FLIGHT. SUSPECT BOTH LT AND RT PACK SOCKS. SMELL MOST INTENSE WHEN INCREASE OUTFLOW TEMP TO MAINTAIN CAB IN TEMP. REPLACED BOTH COALESCER SOCKS PER CRJ 200 AMM 21-51-13. OPS CHECK GOOD. (S) 2 L 7 2 4F RT A21EA 20080814 2008 8 14 WWQ2008F00000 4 20080802 A 3442 MI5853511 DISPLAY GULSTM G1159 G1159 3953505 SO RROYCE SPEY SPEY* NE WEATHER RADAR SHORTED E WWQA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 07 712AS 423 FLIGHT WW171. DEPARTED MIV TO IAD. CLIMBING OUT OF 8000 FT, CREW NOTICED THE RADAR SCREEN START TO FLICKER. IMMEDIATE LY SHUT THE RADAR OFF. CREW DETECTED WHAT APPEARED TO BE SMOKE RELATED TO ELECTRICAL FIRE. CREW SAW HEAVY SMOKE COMING OUT OF THE DASHBOARD. DECLARED AN EMERGENCY. AFTER PERFORMING CORRECT CHECKLIST & ASSESSING THE SITUATION SMOKE HAD D ISSIPATED & CAPT DECIDED THAT THERE WAS NO LONGER AN EMERGENCY. REQUESTED TO FLY BACK TO MIV. LANDED AT 1405 WITH NO A DDITIONAL PROBLEMS. INSPECTED THE COCKPIT & DETERMINED THE WEATHER RADAR CONTROL UNIT (CRT) HAD SHORTED OUT INTERNALLY. INSPECTED BEHIND THE INSTRUMENT PANEL & ASSOCIATED WIRING GOING TO THE WEATHER RADAR CONTROL UNIT (CRT), & NO DEFECTS 2 L 7 2 4F 4 T RT A12EA E2EU 20080814 EU 2008 8 14 YENA2008075 1 20080731 A 3231 114079016 SELECTOR VALVE AIRBUS 320 A320232 3930326 EU LANDING GEAR FAILED A YENA O OTHER J WARNING INDICATION CL CLIMB 1 EA 15 510JB 20490 280 1280 FLT 201, JFK-LGB, RETURNED TO JFK, NOSE WHEEL DOOR WOULD NOT CLOSE AFTER TAKEOFF. REMOVED AND REPLACED THE DOOR SELECTO R VALVE PER MM 32-31-12-000-001, OPS CHECK GOOD. NO LEAKS. 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 KCSA081374 1 20080811 A 5320 WEB BOEING 747 747249F 1384849 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 BILGE TORQUE BOX UPPER WEB DENTED AT BS670, LBL36 AND LBL40, WL118. (S) 2 L 7 4 4F RT A20WE 20080814 NM 2008 8 14 KCSA081342 1 20080724 A 5411 FRAME BOEING 747 747221F 1384868 NM NR 4 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 747CK 21743 NR 4 PYLON NAC STA 221.90 OUTBOARD AFT FRAME IS CRACKED .500" AT SKIN ATTACHMENT. (A) 2 L 7 4 4F RT A20WE 20080814 NM 2008 8 14 USAABB08123 1 20080722 A 2560 BLOCK BOEING 757 757225 1384959 NM GIRT BAR MISSING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 923UW 22203 CLT - THE GIRT BAR ENGAGEMENT LIGHT EXTINGHISHED WITH THE EVACUATION SLIDE ARMED LEVER IN ARMED POSITION AT ENTRY DOOR 4 L. MAINTENANCE REPLACED A MISSING 4L DOOR GIRT BAR FLOOR ATTACH BLOCK. ADJUSTED GIRT BAR AND OPERATIONALLY CHECKED OK. (S) 2 L 7 2 4F RT A2NM 20080814 NM 2008 8 14 USAA920081474 1 20080804 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 840AW 2690 FLT 321 LAX-LAS- EMERGENCY EQUIPMENT - FORWARD ACFT RT FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT INOPERATIVE. MAINTENANCE RE MOVED AND REPLACED FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 USAA920081488 1 20080731 A 5320 D53480043204 SILL AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 833AW 1844 SAL-BC4 -MAJOR REPAIR- CORROSION ON LOWER SILL OF L2 DOOR AT FR67, Y1732. REPAIRED LOWER SILL OF L2 DOOR AT FR67, Y1732 IAW A319 SRM 53-41-14. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 USAA920081477 1 20080730 A 5347 D53371112004 SEAT TRACK AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 833AW 1844 SAL-BC4 -MAJOR REPAIR- CORROSION ON SEAT TRACK AT FR44 THRU FR46, Y1292. REPLACED SEAT TRACK AT FR44 THRU FR46, Y1292 I AW A319 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080814 EU 2008 8 14 USAA920081493 1 20080807 A 3350 321430 BATTERY AIRBUS A319 A319112 3930323 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 765US 1371 FLT 1774 CLT-EEL- OPERATIONAL TEST OF EMERGENCY LIGHTS FAILED TEST STEP 5A, EPSU LOAD AFT LT. MAINTENANCE REMOVED AND R EPLACED THE EMERGENCY POWER SUPPLY UNIT 13WL BATTERY PER AIRBUS MAINTENANCE MANUAL 33-51-38. OPERATIONAL TEST GOOD. (S ) 2 L 7 2 4F RT A28NM 20080815 NM 2008 8 15 08FDEA02939 1 20080716 A 5730 6527172 PANEL BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 PANEL 3617 BOTTOM AFT END CRACKED REPAIRED PANEL 3617 REF SRM 51-40-9 STEPS 3D, 4E, 4F, PGS 3-7 AND AMM 51-20-051 PG1, A MM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080815 NM 2008 8 15 08FDEA03051 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL TANK ACCESS CUTOUT 641GB HAS CORROSION AND BARE METAL. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080815 NM 2008 8 15 08FDEA03066 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL TANK ACCESS CUTOUT 641AB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS C LASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080815 EU 2008 8 15 08FDEA02489 1 20080626 A 5411 A5461129900061Z RIB AIRBUS 310 A310222 3930315 EU ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 WEB CRACKED LOWER END FORWARD OF RIB 18 RIGHT SIDE NR 2 PYLON. DRILLED CRACK STOP HOLES PER SRM 54-52-31. REMOVED THE RELATED FASTENERS PER SRM 51-40-21. MANUFACTURED THE DOUBLERS AND BROKE SHARP EDGES PER SRM 51-26-20. DRILLED FASTENER HOLES TO THE WEB AND THE DOUBLERS PER SRM 51-40-50. INSTALLED THE DOUBLER PER SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA02491 1 20080626 A 5420 A5461129900060Z WEB AIRBUS 310 A310222 3930315 EU ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 WEB CRACKED OUTBOARD OF PRECOOLER NR 1 PYLON. DRILLED CRACK STOP HOLES PER SRM 54-52-31. REMOVED THE RELATED FASTENERS PER SRM 51-40-21. MANUFACTURED THE DOUBLER AND BROKE SHARP EDGES PER SRM 51-26-20. DRILLED FASTENER HOLES TO THE WEB AND THE DOUBLER PER SRM 51-40-50. INSTALLED THE DOUBLER PER SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA03092 1 20080725 A 5347 A53610798200 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 455FE 331 MAIN DECK FLOOR TRACK WITH EXFOLIATION CORROSION BETWEEN FR 15-FR 19 -Y1550. REPLACED THE FLOOR TRACK PER SRM51-40-21. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA02587 1 20080701 A 5540 R5537020900000 ARM AIRBUS 310 A310222 3930315 EU RUDDER HINGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 NR 1 RUDDER HINGE ARM FORWARD ATTACH AREA FORWARD OF BEARINGS EXFOLIATED. REMOVED CORROSION AND POLISHED REWORK AREA PE R SRM 51-76-10, APPLIED ALODINE TO THE REWORK AREA PER SRM 51-21-10. PERFORM HFEC TO REWORK AREA FOR CRACK, NO CRACK FO UND PER NTM 51-10-09/801 AND REPAIRED PER EA 6-5530-117380. MAJOR REPAIR PER GMM 6-2-100. 2 L 7 2 4F RT A35EU 20080815 WP 2008 8 15 08FDEA03011 1 20080722 A 5100 NONE DOUG DC10 DC1030F 3023504 WP NOT AN SDR NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 318FE 46837 FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 08FDEA03014 1 20080722 A 5730 ARB1067 SKIN DOUG DC10 DC1030F 3023504 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 RT WING L/E FOUND CRACK ON LEADING EDGE LOWER EXTERNAL SIDE. 2 L 7 3 4F RT A22WE 20080815 EU 2008 8 15 08FDEA02986 1 20080721 A 5320 A53988424202 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION AT CROSS STRUT C 84 LT OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA02987 1 20080721 A 5720 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION UNDER STATIC DISCHARGER RT WING TIP. REPAIR PERFORMED BY BLEND OUT THE CORROSION, CUT THE AREA AND PERF ORM A PATCH REPAIR IAW RAS/FOK/008/2008 ISS A, APPROVED BY EA 6-5730-120120. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA03016 1 20080722 A 5730 A57247017003 PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION AT TRANSITION OF SHROUD BOX AND TOP SKIN PANEL RT OUTER WING REPAIR PERFORMED BY CORROSION BLEND OUT, RI B CUT AND INSTALLING AN INFILL AND EXTERNAL PLATES IAW DRAWING R572-40274, APPROVED BY RAS /BAE/1007435/2008 ISS A AND E A 6-5720-123005. 2 L 7 2 4F RT A35EU 20080815 NM 2008 8 15 08FDEA02718 1 20080706 A 5753 ARB0029509 STRAP DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 601FE 48401 LEFT WING OUTBOARD FLAP INBOARD FORWARD FLAP HINGE TENSION STRAP FOUND CRACKED. LEFT WING OUTBOARD FLAP INBOARD FLAP HINGE TENSION STRAP REMOVED AND REPLACED AS PER FEDEX EO NR 1-5750-7-5004 PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 08FDEA02719 1 20080706 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM BS 666 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 601FE 48401 MAIN DECK CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND 3RD LAYER CRACK INDICATION AT HOLE A, C AND D. MAIN DECK CAR GO DOOR LOWER JAMB SUPPORT FITTING NR 3 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 08FDEA02721 1 20080706 A 5320 ACA72251 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM BS 757 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 601FE 48401 MAIN DECK CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND 2ND LAYER BEAM WITH CRACK INDICATION AT HOLE D. REPAIR CARRI ED OUT AS PER FEDEX EA NR 1-5310-122531, TITLE: FUSELAGE MAIN CARGO DOOR LOWER JAMB BORE HOLES AT APPROXIMATE STA = 737 AND 757 REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080815 EU 2008 8 15 08FDEA03017 1 20080722 A 5755 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 3 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD TS0723 613 FOUND DELAMINATION ON SPOILER NR 3 LT UPPER FLANGE OF FWD END OF HINGE ARM. REPAIR PERFORMED IAW SRM 57-72-11 FIG 205, APPROVED BY RAS/DABRE/7008957/2008 ISS A AND EA 6-5772-123006 ISS A. 2 L 7 2 4F RT A35EU 20080815 WP 2008 8 15 08FDEA03069 1 20080725 A 5730 ARB126470 SKIN DOUG MD10 MD1010F 3022112 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 RIGHT WING L/E PANEL 615 DB IS CRACKED AT A FASTENER HOLE. FABRICATED A NEW REPAIR DOUBLER & LOCATED THE HOLES IAW SRM 57-00-01 & 57-10-00 VOL I PG 12-A FIG 4. ALODINED & PRIMED IAW SRM 51-21-01; VOL II. INSTALLED IAW SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 20080815 EU 2008 8 15 08FDEA02990 1 20080721 A 5542 SKIN AIRBUS 300 A300B4622R 3930312 EU RUDDER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD HF1317 613 FLUID INGRESS ON RUDDER RT SIDE PANEL. REPAIR PERFORMED IAW SRM 51-77-10 AND RAS/DAHAM/4024567/2008 ISS, APPROVED BY EA 6-5540-117180. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA02993 1 20080721 A 5751 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD FH1374 613 FOUND OLD PATCH REPAIR ON LT AILERON LOWER SKIN TRAILING EDGE AREA RIB 13- 17 WITH BAD OLD DOCUMENTATION. THE REPAIR R ENEWED IAW RAS/FOK/139/2008 ISS A, APPROVED BY EA 6-5761-120107. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 UPS08152907 1 20080722 A 5321 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 153UP 0839 INSPECTION TYPE-5 YR, MAIN CABIN FLOOR PANEL Z261BH IS CRACKED. REPAIRED MAIN CABIN FLOOR PANEL Z261BH REF. A-300-600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 UPS08152908 1 20080722 A 5320 A5398111320051 SHEAR PLATE AIRBUS A300 A300F4622R 3930360 EU FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 153UP 0839 INSPECTION TYPE-5 YR, MAIN CARGO COMPARTMENT RT FR 79 FLOOR LEVEL SHEAR PLATE CRACKED FWD OF AFT PRESSURE BULKHEAD. REP LACED RT FR79 FLOOR LEVEL SHEAR PLATE REF. A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 UPS08152909 1 20080723 A 5321 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 153UP 0839 INSPECTION TYPE-5 YR MAIN CARGO COMPARTMENT FLOORBOARD NR 242UK CRACKED AT TOP SURFACE AND BOTTOM T/E AT FR. 38.2. REPA IRED MAIN CARGO COMPARTMENT FLOORBOARD NR 242UK AT FR.38.2 REF. A-300-600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 UPS08152910 1 20080729 A 3350 SIGN AIRBUS A300 A300F4622R 3930360 EU EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 120UP 0805 CREW ENTRY DOOR TOP EXIT SIGN (LIGHT) BOTTOM LIGHTS INOP. RELAMPED CREW DOOR EXIT SIGN BOTTOM LAMPS IAW AMM 35-51-13-04 . OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 20080815 NM 2008 8 15 UPS08M52891 1 20080516 A 5753 HINGE DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, LT WING OB FLAP IB AFT HINGE LOWER MOUNTING FOUND 02EA BORE RUSTY. LT AFT OB FLAP IB HINGE LOWER MOUNTING FWD & AFT BORE CORROSION REMOVED IAW BSOPM 20-11-02 REV 61.FPI C/O IAW DAC NDT SPM REV 13 PART 0 8 ON REWORKED AREA. FOUND NO CRACK/CORROSION EVIDENT. REWORKED BO RES(02EA) REAMED IAW EN 1288-08.REWORKED AREA ETCH INSPECTED & FOU ND SATIS IAW EN 1288-08.BUSHINGS(02EA) FAB & INSTALLED IAW EN 1288-08. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52935 1 20080712 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 23 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INSTA LLED BUSHING IAW EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52915 1 20080723 A 5330 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, LOWER FWD CARGO DOOR JAMB AFT LOWER DOUBLER FOUND GOUGED. REMOVED, FABRICATED AND INSTALLED DOUBLE R IAW MD-11 SRM 51-31-01 AND 53-50-00 FIG 17 SEET 3 OF 9. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 UPS08852904 1 20080626 A 5313 LONGERON DOUG DC8 DC871F 302199D WP L31R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, AC COMPT. STA 62, HAS L31R WITH EXFOLIATION CORROSION. REMOVED DAMAGE AND FABBED AND INSTALLED R EPAIR DOUBLER IAW, SRM, 51-1- 8, 53-2-0 FIG. 1F, 51-1-21. 2 L 7 4 4F RT 4A25 20080815 NM 2008 8 15 UPS08M52932 1 20080712 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 29 LT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING,AND INSTALLE D BUSHING IAW EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52933 1 20080713 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 20 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INS TALLED BUSHING IAW EO, MD11-5510-19409-N AND SAA TRAVELER 80538450001. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08552881 1 20080714 A 5330 SKIN BOEING 757 75724APF 1384969 NM BS 1825 S3-6R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 421UP 25281 INSPECTION TYPE:C2 APU INLET DUCT TO FUSELAGE SKIN HAS CORROSION EMINATING FROM NUTPLATE HOLES. REPAIRED AREA IAW ATS E R 08-2389 2 L 7 2 4F RT A2NM 20080815 WP 2008 8 15 UPS08852768 1 20080715 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHTS INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 810UP 46001 EMERGENCY LIGHT INOPERATIVE. R&R EMERGENCY BATTERY/RELAY PACK AND TESTED IAW MM 33-50-01-2-2. 2 L 7 4 4F RT 4A25 20080815 NM 2008 8 15 UPS08M52854 1 20080526 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR17 FOUND CORRODED. CORROSION REMOVED AT BARREL NUT BORE IAW SRM 51-21-01 VII REV35. BORE REAM TO 1.067"DIA, REMAINING BLEND OUT 0.050", BOTTOM REMAINING, BLEND OUT 0.045" DEEP, FOUND EXCEEDING LIMIT IAW EO MD11-5510-19409M.10X MAGN DVI C/O & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT BORE NR 17 R T WAS ACCOMPLISHED IAW EN1229-08 & IS ACCEPTABLE IAW EO MD11-5510-30011A. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52855 1 20080531 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 31 FOUND CORRODED CORROSION AT BARREL NUT BORE REMOVED IAW SRM 5 1-21-01 VII REV35.BORE REAM TO 1.162"DIA, REMAINING BLEND OUT AT BOTTOM RADIUS 0.130" DEEP FOUND EXCEEDING EO LIMIT IAW EO MD11-5510-19409M.10X MAGN DVI FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT BORE NR31 RT WAS ACCOMPLISHED IAW EN 1 2 52-08 & IS ACCEPTABLE IAW EO MD11-5510-30012A. 2 L 7 3 4F RT A22WE 20080814 WP 2008 8 14 UPS08852787 1 20080701 A 5540 WEB DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C1, CRACK HAS EXTENDED BEYOND STOP DRILL IN RUDDER HINGE CUT-OUT, NR 2 FROM BOTTOM. REMOVED AND REPLACE D WEB IAW SRM,51-1-8, 51-1-21, 51-3-1. 2 L 7 4 4F RT 4A25 20080814 EA 2008 8 14 TRAX200800931 1 20080725 A 3397 PIN CNDAIR CL600 CL6002B19 1900309 EA CONNECTOR NOT SEATED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 926EV 7843 RT OVERWING EMERGENCY EXIT (EYE LEVEL) LIGHT DOES NOT WORK FROM BATTERY PACK NR 4. TROUBLESHOT USING CRJ 200 WDM 33-51- 00 AND 33-52-00 AND FOUND WIRE LY10D22 CONTACT PIN NOT SEATED IN TB105-3. SECURED WIRE CONTACT INTO TERMINAL MODULE IAW EESPM 20-18-00. RT EMER EXIT SIGN NOW ILLUMINATES NORMALLY DURING BATTERY PACK 4 OP TEST IAW AMM 33-51-04-710-801. SU PPLEMENTAL SDR CLOSED 7/31/08. (A) 2 L 7 2 4F RT A21EA 20080814 WP 2008 8 14 UPS08852732 1 20080619 A 5340 36440462SAAU FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, NR 4 ALT. STRINGER 65 TO FRONT SPAR FITTING CRACKED. REMOVED, FABRICATED AND INSTALLED FRONT SP AR FITTING. IAW DWG. 3644046 SRM 51-01-20D AND 51-03-01-0. 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 UPS08852662 1 20080610 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 68 RBL 24 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, SEAT TRACK DAMAGED AT RBL 24 BS 68. REMOVED SEAT TRACK BS 55-90, FABRICATED AND INSTALLED REPLAC EMENT SEAT TRACK SECTION IAW SRM 53-03-02 FIG. 6, 53-07-01 FIG 06, 51-1-0 8, AND 51-01-24. 2 L 7 4 4F RT 4A25 20080814 NM 2008 8 14 KCSA081361 1 20080729 A 5340 STRINGER CLIP BOEING 747 747246B 1384864 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 STR 25R CLIP CRACKED AT BS 1560. (S) 2 L 7 4 4F RT A20WE 20080814 NM 2008 8 14 USA2008F00018 1 20080725 A 4920 APU BOEING 757 7572B7 1384964 NM MALFUNCTIONED A USAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 19 935UW 27201 MCO FLT 816 EN ROUTE CUN TO CLT. CREW RECEIVED NUMEROUS LAVATORY SMOKE DETECTOR WARNINGS, AND AN ODOR OF SMOKE IN BOTH THE COCKPIT AND CABIN. ALSO RECEIVED AN APU OVERHEAT MESSAGE. THE FLIGHT DIVERTED TO MCO AND LANDED WITHOUT FURTHER IN CIDENT. MAINTENANCE PLACED THE APU ON MEL. (S) 2 L 7 2 4F RT A2NM 20080814 WP 2008 8 14 UPS08852751 1 20080701 A 5240 FITTING DOUG DC8 DC871F 302199D WP BS 1660 L21R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, MAIN CABIN RT/LT AFT SEVICE DOOR LWR AFT TORQUE BOX HAS CORROSION AND CRACKED STAS.1660 L21R. REMOV ED AND REPLACED FITTING IAW SRM. 51-1-8, 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 20080814 SO 2008 8 14 C2XA08RI106 1 20080727 A 2842 367934002 SIGNAL COND UNIT EMB 145 EMB145XR 3260214 SO FUEL SYSTEM INOPERATIVE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 11119 11487 5291 145677 FLIGHT 3000 - EWR - FLIGHT CREW REPORTED, LOST ALL FUEL INDICATION AFTER TAKEOFF (RT AND LT) AND HAD INTERMITTENT FUEL L OW LEVEL INDICATION ON EICAS. CREW PERFORMED AIR RETURN WITHOUT INCIDENT. EWR MX REMOVED AND REPLACED FUEL CONDITIONIN G SIGNAL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080814 WP 2008 8 14 08FDEA02890 1 20080715 A 5311 ADA00675 FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 IN CAC FUSELAGE FRAME LOWER ANGLE IS GOUGED/DENTED ON THE AFT SIDE AT STA 1119 FROM LONGERON 36R TO 40R. FUSELAGE FRAME IN THE CAC, LOWER ANGLE GOUGE/DENT AT STA 1119, LONGERON 36R TO LONGERON 40R. FOUND TO BE OUT OF LIMITS. REMOVED "J" CHANNEL AS PART OF THE "J" CHANNEL REPAIR ACCOMPLISHED ON N/R N00967. 2 L 7 3 4F RT A22WE 20080814 EU 2008 8 14 08FDEA02903 1 20080715 A 5320 A5398111320051 SHEAR WEB AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CRACKED SHEAR WEB BETWEEN FRAME 79 AND FRAME 80/82 RIGHT SIDE AT MAIN CABIN DECK FLOOR LEVEL. REMOVED AND REPLACED SHEA R WEB IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080814 CE 2008 8 14 DXTA200803209 1 20080731 A 3240 BRAKE SYS CESSNA 500 560CESSNA 2076750 CE MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 383QS 5600483 DURING LANDING, THE LT SEAT BRAKES ARE RELEASING AT AROUND 30 KNOTS. (S) 2 L 7 2 4F RT A22CE 20080814 NM 2008 8 14 KCSA081368 1 20080804 A 5313 STRINGER BOEING 747 747122 1384872 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STR 37L CRACKED AT BS 384. (S) 2 L 7 4 4F RT A20WE 20080814 SO 2008 8 14 C2XA08SH042A 1 20080801 A 3240 21707 BRAKE ASSY EMB 145 EMB145XR 3260214 SO NR 3 DRAGGING A C2XA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 27 14173 8366 14500872 AIR RETURN DUE TO LANDING GEAR LEVER DISAGREE-RT MAIN GEAR NOT RETRACTING DUE TO BLOWN TIRE. (S) 2 L 7 2 4F RT 20080814 EA 2008 8 14 TRAX200800947 1 20080730 A 5230 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 926EV 7843 CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.0 INCH IN RADIUS. REMOVED AND REPLACED CARGO DOOR SUUPPORT BEAM ANGLE IAW SRM 51-42-21. PRESSURE CHECK DUE. PERFORMED PRESSURE CHECK IAW AMM 21-32-00-863-801. NO DISCREPANCIES NOTE D AT THIS TIME. (S) 2 L 7 2 4F RT A21EA 20080814 NM 2008 8 14 NWAA083576311 1 20080802 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 671US 26477 RACEWAY EMERGENCY LIGHT IS INOPERATIVE FORWARD TO AFT NR 3. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD, AND ACFT WAS RETURNED TO SERVICE. (S) 2 L 7 4 4F RT A20WE 20080814 NM 2008 8 14 F3LA200800533 1 20080731 A 5321 D5367314700000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2 2209 DURING C3 C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL, 152WG, WAS DAMAGED. MAINTENANCE REPAIRED THE PUNCTURE DAMAGE IN TRANSITION PANEL 152WG IAW THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. MAINTENANCE PREPARED AND PAINTE D THE TRANSITION PANEL IAW THE REQUIREMENTS OF AMM 25-00-00-370-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080814 SO 2008 8 14 RAIA00807020 1 20080729 A 5210 DOOR EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A RAIA K NONE O OTHER NR NOT REPORTED 1 CE 03 838HK 145321 FLT 7988-ORD- PASSENGER DOOR DIFFICULT TO OPEN AND CLOSE. MAINTENANCE LUBED THE CABIN DOOR. OPERATIONAL CHECK OF THE D OOR PROVED GOOD. (S) 2 L 7 2 4T RT T00011AT 20080814 NM 2008 8 14 USAA920081444 1 20080730 A 5752 654645519 TAB BOEING 737 7373B7 1384580 NM LT AILERON DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT-Q6- MAJOR REPAIR - LT AILERON TAB OUTBOARD CORNER DELAMINATED. REPAIRED LT AILERON TAB OUTBOARD CORNER IAW B737 SRM 57-60-01. (S) 2 L 7 2 4F RT A16WE 20080814 NM 2008 8 14 USAA920081472 1 20080721 A 5540 D5537131800200 HINGE FITTING AIRBUS A319 A319132 3930340 NM RUDDER EXCESS PLAY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803AW 0931 SAL-C7- MAJOR REPAIR - EXCESSIVE PLAY ON HINGE NR 4 OF RUDDER. REPLACED NR 4 HINGE FITTING NR 4 AT RIB NR 6, HORIZONTAL STABILIZER STATION 2632 IAW A319 AMM27-21-00. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 USAA920081454 1 20080715 A 5330 6545775594 SKIN PANEL BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 168AW 23629 MCN-C21- MAJOR REPAIR - CRACK IN FUSELAGE SKIN PANEL AT BS 727D, S23R. REPAIRED FUSELAGE SKIN PANEL AT BS 727D, S2R IAW B737 SRM 53-00-01 AND TYPICAL REPAIR 53-33. (S) 2 L 7 2 4F RT A16WE 20080815 WP 2008 8 15 08FDEA02932 1 20080716 A 5753 ARC04442 SKIN DOUG MD10 MD1010F 3022112 WP RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 RIGHT WING INBD LOWER SURFACE SKIN HAS MULTIPLE DENTS JUST INBD OF THE OUTBD HINGE. CHECKED DENTS AND FOUND 2 OUT OF LI MITS IAW SRM 57-10-00, VOL I, FIG 48 AT STA XIFH 250 AND XIFH 254. REMOVED DAMAGED AREAS AND FABRICATED 2 REPAIR DOUBLE RS IAW SRM 57-10-00, VOL I, FIG 85. ALODINED AND PRIMED 2 REPAIR DOUBLERS IAW SRM 51-21-01, VOL II. INSTALLED 2 REPAIR DOUBLERS IAW SRM 57-10-00, FIG 85. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 08FDEA03025 1 20080723 A 5753 ARC2217506 FITTING DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 40061 46973 RT WING OUTBD FLAP CRACK ON FITTING. REPAIRED AREA IAW EA 8-5750-120139. 2 L 7 3 4F A22WE 20080815 EU 2008 8 15 08FDEA03024 1 20080723 A 5330 A53812189201 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 CORROSION FOUND ON SKIN PANEL C 39/40, P 27-29 RT REPAIR PERFORMED BY REPLACEMENT OF PANEL AND FASTENER HL12-VF6 IAW RAS 70507112/019/2008 ISS A, APPROVED BY EA 6-5314-120049. 2 L 7 2 4F RT A35EU 20080806 NM 2008 8 6 ABXA080197 1 20080617 A 3242 4025010030 METERING VALVE BOEING 767 767232 1385132 NM BRAKE DEFECTIVE A ABXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 746AX 22223 RT HYDRAULIC QUANTITY DECREASED TO .34 QTY. STABLE WITH EDP DEPRESSURIZED AND ACMP OFF. EVENT OCCURRED IN CRUISE, GEAR OFF, FLAPS UP. FOUND BRAKE METERING VALVE MODULE BYPASSING HYDRAULIC FLUID FROM RT TO CENTER SYSTEM. REMOVED AND REPL ACED BRAKE METERING VALVE MODULE (MAIN) IAW AMM 32-41-03-4. SYSTEM OPS AND LEAK CHECKED GOOD. (S) 2 L 7 2 4F RT A1NM 20080806 NM 2008 8 6 ABXA080189 1 20080714 A 3350 20131A BATTERY PACK BOEING 767 767232 1385132 NM EMERGENCY LIGHT DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 744AX 22221 EMERGENCY LIGHTS BATTERY PACK M735 WOULD NOT ILLUMINATE EMERGENCY LIGHTS. REMOVED BATTERY PACK FROM N739AX, INSTALLED I N 744AX IAW B767 MM 33-51-07. OPS CHECK GOOD. (S) 2 L 7 2 4F RT A1NM 20080806 NE 2008 8 6 ABXA080196 2 20080516 A 7321 8063508 MEC BOEING 767 767232 1385132 NM GE CF6 CF680A 30025 NE RT ENGINE DEFECTIVE A ABXA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 23 744AX 454 22221 RT ENG COMPRESSOR STALL ON CLIMBOUT. PERFORMED CALLED FOR ITEMS. ENG RESPONDED OK AT 80-85% N1 BUT STALLED AGAIN AT CL IMB POWER. REMOVED AND REPLACED NR 2 ENG MEC IAW B767 MM 73-21-07-4. TESTED MEC IAW B767 MM 71-00-00. NR 2 ENG COMPRE SSOR STALL AT 84%. (S) 2 L 7 2 4F 4 F RT A1NM E13NE 20080806 NE 2008 8 6 WRLA2008059 2 20080716 A 7261 ENGINE DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE NR 3 OIL CONSUMPTION A WRLA O OTHER E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 SO 11 275WA 48631 GEC8284 EDDP/K JFK 07/16 ITEM: PRECAUTIONARY SHUT DOWN OF NR 3 ENG DUE TO OIL QUANTITY IN THE RESERVOIR, 2 QUARTS, BOXE D IN YELLOW ON SHUT DOWN. OIL TEMP 108C OIL PRESSURE 146PSID AT FL 280 THROTTLE IDLE, N2 69.5. OPEN. (S) 2 L 7 3 4F 4 F RT A22WE E24NE 20080806 EU 2008 8 6 USAA920081379 1 20080716 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 620AW 25941 14832 052 CMH - FLT 143 - LT MID CABIN EMERGENCY LIGHT POWER SUPPLY FAILS TEST. MX REPLACED POWER SUPPLY UNIT 11WL PER AMM 33-51- 38. OPERATIONAL TEST WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080806 CE 2008 8 6 DXTA200803182 1 20080717 A 2710 TRIM SYSTEM CESSNA 560 560XL 2076702 CE AILERONS OUT OF ADJUST E DXTA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 07 678QS 5605616 DURING OCF FLIGHT FOR CONTROL CABLE CHANGE, WITH THE AILERON AND RUDDER TRIM WHEELS CENTERED, THE PLANE ROLLED LT AGGRES SIVELY ON TAKEOFF AND AT CRUISE SPEED. THE AILERON TRIM IS ABOUT .25 INCH TO THE RT WHEN LEVEL. (S) 2 L 7 2 4F RT A22CE 20080806 CE 2008 8 6 DXTA200803178 1 20080716 A 7500 UNKNOWN CESSNA 750 750 2076810 CE ALLSN AE3007 AE3007A 03030 GL PYLON BLEED UNKNOWN E DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 989QS 7500089 PYLON BLEED LEAK (R) ILLUMINATED ON FINAL APPROACH AND AGAIN ON THE GROUND. THERE IS ALSO A BURNING ODOR IN THE CABIN. (S) 2 L 7 2 4J 4 F RT T00007WI TE6CH 20080806 WP 2008 8 6 I5HA0858005 1 20080405 A 3250 10150 ACTUATOR CVAC 580 580 2422806 WP ALLSN A6441 A6441FN606 GL STEERING SYSTEM DAMAGED A I5HA O OTHER O OTHER NR NOT REPORTED 1 GL 25 581P 29 HC479 DURING A STORM IN MIA ON APRIL 6, 2008 A CARGO CAN (ULB) WAS THROWN INTO THE RT SIDE OF N581P. THE RT PROPELLER WAS ALS O STRUCK A GLANCING BLOW. THERE WAS SIGNIFICANT DAMAGE TO THE SKIN AND SUPPORT STRUCTURE BENEATH THE SKIN. THERE WAS D AMAGE TO WIRING IN THE AREA. THE NOSE STEERING ACTUATOR WAS ALSO DAMAGED. DAMAGE AREA WAS BETWEEN FUSELAGE STATIONS 72 TO 125 AT APPROXIMATELY BETWEEN STRINGERS 11 AND 3. THE PROPELLER AND REDUCTION GEARBOX WERE REMOVED AND INSPECTED. N O DAMAGE TO EITHER. N581P WAS REPAIRED AND THE ACFT TEST FLOWN ON JULY 3, 2008. THE ACFT WAS RETURNED TO SERVICE JULY 8, 2008. (S) 2 L 7 2 4T RT 6 C P898 20080806 CE 2008 8 6 DXTA200803179 1 20080716 A 3150 WARNING HORN BEECH MU300 400A 1155402 CE ACTIVATED E DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 161QS RK435 DURING TAKEOFF ROLL WARNING HORN CAME ON. (S) 2 H 7 2 4F RT A16SW 20080806 WP 2008 8 6 AALA200801447 1 20080601 A 5620 N5951584501 WINDOW DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA E A ENGINE SHUTDOWN UNSCHED LANDING C R J F.O.D. PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 21 7509 49803 717841 DFW INFLIGHT T2094/01JUN. DURING CRUISE OUTTER WINDOW PANE AT SEAT 26F FAILED AND WAS INJESTED INTO THE NR TWO ENGINE. CREW SHUT DOWN NR TWO ENGINE. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 20 MINUTES. THE NOSE C OWL AND NR TWO ENGINE COMPRESSOR BLADES WERE DAMAGED BELOW MIDSPAN. REPLACED WINDOW PANE ASSEMBLY. REPLACED NR TWO ENG INE AND ISOLATORS ON 02 JUN AT DFW. WINDOW PANE SENT TO TUL ENGINEERING FOR EVALUATION. SYSTEM GROUND CHECKED NORMAL O PERATION. (A) 2 L 7 2 4F A6WE 20080804 NM 2008 8 4 2008UALA03628 1 20080630 A 2830 S343T00339 ACTUATOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FUEL JETTISON MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 797UA 26924 FUEL JETTISON NOZZLE RIGHT JETTISON NOZZLE VALVE IS NOT IN COMMANDED POSITION. STATUS MSG01- LATCHED CRUISE MODE DEPEN DENT; RIGHT JETTISON NOZZLE VALVE IS NOT IN COMMANDED POSITION. DB- ELMS P210 ELECTRONICS UNIT MSG-2812007 LATCHED ER M ODE. SUSPECT FAULTY JETTISON NOZZLE VALVE ACTUATOR. REPLACED RIGHT FUEL JETTISON NOZZLE ACTUATOR REF MM 28-31-03 OP CH ECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080804 NM 2008 8 4 R612008F00004 1 20080628 A 2751 1702286A SENSOR EMB ERJ170 ERJ170200LR 3260121 NM SLAT SKEW FAILED A R61A O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 124HQ 17000200 CREW RECEIVED A SLAT FAIL MESSAGE ON APPROACH. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISP ATCHED TO THE AIRCRAFT TO EVALUATE. MAINTENANCE REMOVED AND REPLACED LT HAND OUT BOARD SLAT SKEW SENSOR SYSTEM OPERATION AL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A56NM 20080804 CE 2008 8 4 DXTA200803161 1 20080704 A 4920 APU CESSNA 680 680CE 2076811 CE SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 389QS 6800149 STARTED APU ON GROUND, GOT SMOKE IN CABIN, KOSU. (A) 2 L 7 2 4F RC T00012WI 20080804 SO 2008 8 4 CHQA200800124 1 20080625 A 3350 66367 LIGHT EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007A 03030 GL CABIN INOPERATIVE A CHQA O OTHER O OTHER NR NOT REPORTED 1 GL 11 265SK 145226 CAE312062 FLIGHT 5981, STL TO IAH. FLIGHT CREW REPORTED THE FLOOR EMERGENCY LIGHT STRIP INOP BETWEEN ROWS 3 AND 7 INOP. MAINTENA NCE DEFERRED THE LIGHT STRIP. (A) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080805 EU 2008 8 5 M7K2008F00062 1 20080108 A 3150 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE WARNING LIGHT INOPERATIVE E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 815MH 187 4022 46079 PILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWE VER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED M UCH LONGER THAN TYPICAL THIS IS A RECURRING PROBLEM FOR THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY OF THIS MOD E AC. THIS PART CAN ON OCCASION ALSO CAUSE ENGINE FLUCTUATIONS IN FLIGHT WHEN THE RESISTANCE VALUE SIGNAL IS DISRUPTED FOR A LITTLE AS 1/20TH OF A SECOND, WHICH IS THE SAMPLE RATE FOR THE ENGINE CONTROL SYS. AN ADDITIONAL FACTOR FOR THESE TYPE OF FAULTS IS NO RESET FUNCTION AVAILABLE TO THE PILOT TO DIFFERENTIATE BETWEEN A MOMENTARY OR AN ACTIVE FAULT. ON 1 G 7 2 3U 3 U H9EU E00054EN 20080805 EU 2008 8 5 M7K2008F00074 1 20080303 A 3150 006SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE WARNING LIGHT DEFECTIVE E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 808MH 3914 23072 PILOT REPORTS AMBER GOVERNOR LIGHT ILLUMINATED DURING FLIGHT. A FAULT CODE WAS GENERATED INDICATING THE POTENTIOMETER A S THE LIKELY DEFECTIVE UNIT. A NEW PART WAS INSTALLED AND NO FURTHER DEFECTS WERE NOTED. THIS IS A RECURRING PROBLEM FO R THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY FOR THIS AC MODEL. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080805 EU 2008 8 5 YEN2008F00014 1 20080707 A 2700 3945128206 COMPUTER AIRBUS 320 A320232 3930326 EU NR 1 ELAC FAULTED A YENA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 15 646JB 7117 2945 AIR RETURN TO DEPARTURE AIRPORT, L AIL FAULT, RAIL, FAULT RT AFTER TAKEOFF, NO AUTO PILOT ALT LAW, NO OTHER INDICATIONS, REMOVED AND REPLACED NR 1 ELAC IAW MM 27-30-34-000. OPS CHECK GOOD. (K) 2 L 7 2 4F RT A28NM 20080805 NM 2008 8 5 UIE2008F00026 1 20080705 A 5412 FASTENER BOEING 747 747243B 1384830 NM NR1 PYLON LOOSE A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 540MC 22508 NR 1 PYLON AFT BULKHEAD CHORD FOUND SEVERAL ATTACH FASTENERS, LOOSE. REPLACED FASTENERS IAW MFG MESSAGE NR 1-875740529- 4. (K) 2 L 7 4 4F RT A20WE 20080805 EU 2008 8 5 M7K2008F00064 1 20080108 A 3150 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE WARNING LIGHT FAILED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 818MH 4131 46047 PILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWE VER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED M UCH LONGER THAN TYPICAL THIS IS A RECURRING PROBLEM FOR THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY OF THIS MOD E AC. THIS PART CAN ON OCCASION ALSO CAUSE ENGINE FLUCTUATIONS IN FLIGHT WHEN THE RESISTANCE VALUE SIGNAL IS DISRUPTED FOR A LITTLE AS 1/20TH OF A SECOND, WHICH IS THE SAMPLE RATE FOR THE ENGINE CONTROL SYS. AN ADDITIONAL FACTOR FOR THESE TYPE OF FAULTS IS NO RESET FUNCTION AVAILABLE TO THE PILOT TO DIFFERENTIATE BETWEEN A MOMENTARY OR AN ACTIVE FAULT. ON 1 G 7 2 3U 3 U H9EU E00054EN 20080805 EA 2008 8 5 A6WA200840541 1 20080713 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR DAMAGED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 421ZW 7346 SERVICE DOOR OUTER HANDLE PLUNGER BROKE OFF. RESECURED HANDLE PLUNGER IAW AMM 52-40. (A) 2 L 7 2 4F RT A21EA 20080805 EA 2008 8 5 TRAX200800920 1 20080718 A 5210 MECHANISM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LOCK DIRTY A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 MAIN ENTRY DOOR VERY DIFFICULT TO OPEN. CLEANED LOCKING MECHANISM ON PAX DOOR, CYCLED PAX DOOR, NO FURTHER DEFECTS NOT ED. (A) 2 L 7 2 4F RT A21EA 20080805 EA 2008 8 5 A6WA200840427 1 20080523 A 2120 DUCT CNDAIR CL600 CL6002B19 1900309 EA COOL AIR SEPARATED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 438AW 7748 DISPLAY COOL CAUTION MESSAGE IN FLIGHT. RAN QRH AND MESSAGE PERSISTED. MESSAGE EXTINGUISHED BELOW 8000 FT. FOUND COOL ING AIR SUPPLY DUCT PARTED AT CLAMP. RE-INSTALLED CLAMP IAW 21-20-00. NO FURTHER DEFECTS FOUND AT THIS TIME. (A) 2 L 7 2 4F RT A21EA 20080805 EA 2008 8 5 TRAX200800915 1 20080716 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 835AS 7258 RT SIDE FUSELAGE AFT EMERGENCY EXTERIOR LIGHT INOP. RELAMPED AFT EMERGENCY LIGHT AT RT EXTERIOR SIDE OF FUSELAGE IAW CR J 200 AMM 33-51-21. OPS CHECK GOOD. (A) 2 L 7 2 4F RT A21EA 20080805 2008 8 5 RAIA00806027 4 20080630 A 3420 7014300901 DISPLAY EMB 145 EMB145 3260210 SO ATTITUDE ODOR A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 805HK 1866 145096 FLT 3563 - IND - F/O`S MFD FAILED DURING CRUISE FOLLOWED BY AN ELECTRICAL BURNING SMELL IN THE COCKPIT. MAINTENANCE INS PECTED THE COCKPIT AVIONICS SYSTEMS AND REPLACED THE F/O`S MFD. NO OTHER DEFECTS NOTED. (A) 2 L 7 2 4F RT T00011AT 20080805 EA 2008 8 5 TRAX200800912 1 20080715 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 932EV 8016 SEVERAL EMERGENCY LIGHTS OUT. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY CHARGER IAW CRJ 200 AMM 33-52-01. CHECKED GO OD. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY CHARGER IAW CRJ 200 AMM 33-52-01. CHECKED GOOD. (A) 2 L 7 2 4F RT A21EA 20080805 SO 2008 8 5 C2X2008F00004 1 20080721 A 3260 852701 UPLOCK SWITCH EMB 145 EMB145LR 3260212 SO NLG FAULTY A C2XA O OTHER N FALSE WARNING CL CLIMB 1 NM 13 12540 145537 CLE FLIGHT 2141 - THE CREW REPORTED A LOUD RUMBLING FROM THE NOSE GEAR WITH GEAR RETRACTED INDICATING UP AND LOCKED. TH E CREW SUSPECTED THE GEAR DOORS WERE NOT CLOSED. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR UPLOCK SQUENCE SWITCH . OPERAITONAL CHECKS WERE GOOD. (A) 2 L 7 2 4T RT T00011AT 20080805 SO 2008 8 5 C2X2008F00005 1 20080718 A 3397 66367 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 NM 13 26545 145558 IAH - FLIGHT 2510, THE CREW REPORTED THE EMERGENCY LIGHT AT ROW 12 FRONT WAS INOPERATIVE. MAINTENANCE RE-SECURED A LOOS E WIRE ON THE AFFECTED EMERGENCY LIGHT, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080805 NM 2008 8 5 ARQA20080703 1 20080718 A 2910 LINE DOUG DC10 DC1040F 3023507 NM HYD SYSTEM LEAKING A ARWA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 29 140WE 46661 EVIDENCE OF HYDRAULIC LEAK LT HAND WHEEL WB 11. REPAIRED SECTION OF HYDRAULIC LINE DAMAGED, USING TYPE 3 REPAIRED IN AC CORDANCE WITH DC10-MM 20-10-01. LEAK CHECK FOUND NORMAL. (A) 2 L 7 3 4F RT A22WE 20080805 NM 2008 8 5 AALA200801479 1 20080602 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 762AN 31479 JFK - EMERGENCY LIGHT EXIT SIGN AT OVERHEAD LT NR ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT EXIT SIGN AT OVERHEAD LT NR ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080805 NM 2008 8 5 NWAA082563137 1 20080607 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 337NB 17311 17311 1685 SEAT ROWS 11, 15, 16, AISLE EMERGENCY EGRESS LIGHTS INOPERATIVE. REPLACED 3RD LT EMERGENCY POWER SUPPLY UNIT. OPS CHEC K GOOD. (A) 2 L 7 2 4F RT A28NM 20080805 EU 2008 8 5 AALA200801551 1 20080606 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 JFK - EMERGENCY EXIT SIGN LIGHT AT LT NR TWO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LT NR TWO DOOR. S YSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080805 EA 2008 8 5 A6WA200840428 1 20080524 A 3297 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA ANTI SKID SYS UNKNOWN A A6WA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 31 413AW 7585 RT OUTBOARD MLG TIRE FLAT. SUSPECT ANTI-SKID PROBLEM. REMOVED AND REPLACED RIGHT OUTBOARD GEAR HARNESS ASSEMBLY IAW AW AC SUPP 06-051, OPS CHECK GOOD AT THIS TIME. (A) 2 L 7 2 4F RT A21EA 20080805 NM 2008 8 5 AALA200801508 1 20080604 A 3350 GE767 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 601AN 27052 BOS - EXTERNAL EMERGENCY LIGHT AT RT NR ONE ENTRY DOOR INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT RT NR ONE ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080805 EA 2008 8 5 C2XA08ON141 2 20080616 A 7421 23062672 IGNITER EMB 145 EMB145XR 3260214 SO RROYCE AE3007 AE3007A1E 54169 EA ENGINE INOPERATIVE A C2XA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 27 11192 7800 4206 14500936 CAE312764 FLT 0519 - AUS - FLIGHT CREW REPORTED E2 DRIPPING FUEL WHILE RUNNING ACCORDING TO GROUND RAMP. MAINTENANCE INSPECTED AN D FOUND FUEL FROM PREVIOUS ABORTED/HUNG START (NOT DRIPPING WHEN RUNNING). FOUND E2A IGNITER INOPERATIVE. MAINTENANCE PLACED ON MEL. ON 06/18/2008 FLIGHT CREW REPORTED DURING START ENG NR 2 WAS LEAKING A STREAM OF FUEL FROM LOWER COWLING - FOLLOW THE START FUEL STILL LEAKING BUT AT REDUCED RATE. MAINTENANCE REMOVED AND REPLACED IGNITERS. OPERATIONALLY A ND LEAK CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN TO SERVICE. (S) 2 L 7 2 4F 4 F RT TE6CH 20080806 NM 2008 8 6 WXOA070204 1 20080527 A 3350 20131A BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 872GA 53295 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. (A) 2 L 7 2 4F RT 20080806 EA 2008 8 6 A6WA200840502 1 20080609 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 429AW 7711 PASSENGER DOOR WILL NOT OPEN WITHOUT EXCESSIVE FORCE. CLEANED AND LUBED PAX DOOR IAW AMM 12-26-52 AS REQUIRED OPS CHECK S SEVERAL TIMES NO DEFECTS NOTED AT THIS TIME. (A) 2 L 7 2 4F RT A21EA 20080806 NE 2008 8 6 AALA200801435 2 20080530 A 7230 BLADE BOEING 757 757223 1384957 NM RROYCE RB211 RB211535* NE COMPRESSOR FAILED A AALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 21 637AM 24595 31104 ORD INFLIGHT T780/30MAY. NR ONE ENGINE COMPRESSOR STALL DURING TAKEOFF POWER. CREW HEARD TWO LOUD REPORTS AND FELT AIR CRAFT VIBRATE. CABIN CREW AND PASSENGERS REPORTED BURST OF FLAME. ALL INDICATIONS NORMAL. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. NO SECONDARY INDICATIONS FOR ENGINE FLAME. FOUND MULTIPLE STAGE THREE HIGH PRESSURE COMPRESSOR BLADE S DAMAGED. REPLACED NR ONE ENGINE ON 30 MAY AT ORD. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F 4 F RT A2NM E12EU 20080806 WP 2008 8 6 AALA200801449 1 20080601 A 2560 1001191 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 227AA 49177 LGA - EMERGENCY FLASHLIGHT AT LT NR ONE DOOR INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT AT LT NR ONE DOOR. SYSTEM GROU ND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080806 EA 2008 8 6 TRAX200800841 1 20080626 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 977EV 7720 INTERCOSTAL AT FS 461 RLB 9 CRACKED AT TOP. UPON FURTHER INVESTIGATION FOUND ANGLE CRACKED AT FS 484 RBL 36 INSTEAD OF FS 461 RBL 9. (S) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 TRAX200800810 1 20080620 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 755EV 10185 EMERGENCY LIGHTS INOPERATIVE. RESET SYSTEM OPS OK PER 33-51-01. (S) 2 L 7 2 4F RT A21EA 20080807 NM 2008 8 7 KCSA081341 1 20080723 A 5320 STIFFENER BOEING 747 747122 1384872 NM BS 1267 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 EVIDENCE OF CRACKING ON VERTICAL WEB STIFFENER AT APPROX. BS 1267, WL 116, LBL 4. (A) 2 L 7 4 4F RT A20WE 20080807 NM 2008 8 7 KCSA081337 1 20080722 A 5311 FRAME BOEING 747 747122 1384872 NM BS 800 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 LT BS 800 BELOW STR-17L HAS A .250 CRACK FROM EDGE OF FASTENER. (A) 2 L 7 4 4F RT A20WE 20080807 NM 2008 8 7 KCSA081336 1 20080722 A 5320 SUPPORT BOEING 747 747122 1384872 NM BS 806 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 GILL LINER SUPPORT AFT LOWER ATTACH FASTENER HOLE HAS .5" CRACK AT STA 806 BETWEEN S18 AND 17 LT. (A) 2 L 7 4 4F RT A20WE 20080807 NM 2008 8 7 2008UALA03169 1 20080602 A 2120 420365 VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE E/E BAY COOLING FAULTY A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 646UA 25283 FWD EQUIPMENT OVERHEAT EICAS MESSAGE CAME ON PASSING 10000 FEET AND EXTINGUISHED PASSING 18000 FT. SUSPECT FAULTY COOLI NG OVERRIDE VALVE. REPLACED FWD E&E COOLING OVERRIDE VALVE PER MM 21-58-20. OPS CHECK OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080807 NM 2008 8 7 2008UALA03802 1 20080709 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 L-1 DOOR, LOWER GATE CORRODED. *S/D* REPLACED LWR GATE REF SM-5 0-52-11-02-JD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080807 NM 2008 8 7 2008UALA03828 1 20080710 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 654UA 25392 FLOOR EEL FWD RT AISLE AT FWD GALLEY IS INOP. FOUND BROKEN LEAD CABLE. REPAIRED FEEDER CABLE OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080807 2008 8 7 2008UALA03704 4 20080703 A 3400 INDICATION SYS BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT MULTIPLE FAIL A UALA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 WP 29 662UA 27159 CAPT AIR SPEED ALTIMITER & VSI FAILED. RTFL. 2 L 7 2 4F 4 F RT A1NM E24NE 20080807 NM 2008 8 7 2008UALA03705 1 20080704 A 2700 UNKNOWN BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE UNKNOWN A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 672UA 30027 LANDED UNDER AMBER ALERT DUE TO FLAP/RUDDER PROBLEM. 2 L 7 2 4F 4 F RT A1NM E24NE 20080807 NM 2008 8 7 2008UALA03706 1 20080705 A 2910 HYDRAULIC SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 652UA 25390 HYDRAULIC FLUID LOSS. FLIGHT DIVERTED. 2 L 7 2 4F 4 F RT A1NM E24NE 20080807 NM 2008 8 7 CALA0800718 1 20080716 A 5320 6545855 SILL BOEING 737 737524 1384721 NM R2 DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 R2 DOOR SILL WEB HAS CORROSION ON UPPER AND LOWER SURFACES. REMOVED R-2 DOOR SILL WEB IAW B737 SRM 51-40-02 MATL ID FOR NEW SIL WEB 7075 T6 .063 IAW B737 SRM 53-60-15. FABBED NEW WEB IAW BAC DWG 65-45855. ALODINED AND PRIMED IAW B737 SRM 51-20-01 INSTALLED WEB IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 CALA0800720 1 20080716 A 5240 6545855122 ANGLE BOEING 737 737524 1384721 NM R2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 AFT CABIN R2 DOOR Z-ANGLE HAS CORROSION. REMOVED R2 DOOR Z-ANGLE IAW B737 SRM 51-40-02, INSTALLED NEW R2 DOOR Z-ANGLE I AW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 AALA200801478 1 20080602 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 674AN 29424 DFW - EMERGENCY LIGHT EXIT SIGN AT OVERHEAD RT NR ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT EXIT SIGN AT OVERHEAD RT NR ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 AALA200801480 1 20080602 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 683A 25340 DFW - EXTERIOR EMERGENCY LIGHT AT LT NR TWO DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LT NR TWO D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 AALA200801481 1 20080602 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 683A 25340 DFW - EXTERIOR EMERGENCY LIGHT AT LT NR THREE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LT NR THR EE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 AALA200801482 1 20080602 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 683A 25340 DFW - EXTERIOR EMERGENCY LIGHT AT FORWARD RIGHT NR TWO DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT FORWARD RT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 AALA200801492 1 20080603 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 762AN 31479 JFK - EMERGENCY LIGHTS AT RT AND LT NR FOUR DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RT AND LT NR FOUR DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 NM 2008 8 7 CALA0800708 1 20080716 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM BS 440 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 LEFT SIDE STATION 440 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES AT LEFT SIDE FRAME STATION 440 BETWEEN S-8 AND S-9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 CALA0800710 1 20080716 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM BS 747 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 RIGHT SIDE STATION 747 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED DAMAGE , FABRICATED AND INSTALLED REPAIR ANGLES IAW EA5310-04498. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 CALA0800711 1 20080716 A 5315 BAC15181211 FLOORBEAM BOEING 737 737724 13844BY NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23721 28940 FLOORBEAM STATION 986 AND LBL 43 HAS CORROSION AT FASTENER HOLE AREA. REMOVED DAMAGE AND INSTALLED REPAIR FLOORBEAM BS 986 LT 43 PER EC/RA 5321-01429. 2 L 7 2 4F RT A16WE 20080807 EA 2008 8 7 COMA0880014 1 20080718 A 2720 LIMITER CNDAIR CL600 CL6002D24 1390016 EA RUDDER MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 548CA 15159 DURING T/O RECEIVED RUDDER LIMITER CAUTION MSG. EMERGENCY DECLARED, A/C DIVERTED TO EWR AND LANDED SAFELY. PERFORMED P OST 2 TEST PER FIM AND AMM, MSG CLEARED, OPS CHECK GOOD. (A) 2 L 7 2 4F RT A21EA 20080807 NM 2008 8 7 AALA200801358 1 20080520 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW - EMERGENCY LIGHT AT SEAT ROW 26C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 26C. SYSTEM GROUND CH ECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 WP 2008 8 7 AALA200801378 1 20080524 A 2120 A/C PACK DOUG DC9 DC982 3022082 WP DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 255AA 49287 ICT INFLIGHT T684/24MAY MCI TO DFW. CREW REPORTED SMOKE IN CABIN. LANDED ICT WITHOUT INCIDENT. AIRCRAFT OUT OF SERVIC E FOR EVALUATION. NO DEFECTS FOUND. PERFORMED AIR CONDITIONING PACK BURNOUT. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080807 NM 2008 8 7 CALA0800730 1 20080719 A 5311 143A1120 FRAME BOEING 737 737724 13844BY NM BS 480 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23721 28940 FRAME CRACKED AT STATION 480 BETWEEN S8L AND S9L. REPAIRED CRACKED FRAME BODY STATION 480 BETWEEN S-8 AND S-9 RIGHT PER EC/RA 5310-04806. 2 L 7 2 4F RT A16WE 20080807 NE 2008 8 7 AALA200801370 2 20080522 A 7310 AD92272480 FUEL FILTER AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE NR 2 ENGINE DIRTY A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 14061 471 695421 MCO INFLIGHT T1075/22MAY. NR TWO ENGINE FUEL CLOG LIGHT ILLUMINATED. FOLLOWED FUEL CLOG PROCEDURE AND INDICATION EXTIN GUISHED. APPLIED TAKEOFF POWER AND LIGHT ILLUMINATED AGAIN. REDUCED POWER AND LIGHT WENT OUT. RETURNED TO MCO AND LAN DED WITHOUT INCIDENT. FOUND SMALL AMOUNT OF DEBRIS IN FUEL FILTER. REPLACED FUEL FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F 4 F RT A35EU E13NE 20080807 NM 2008 8 7 AALA200801499 1 20080603 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 690AA 25696 DFW - EMERGENCY LIGHTS AT BULLNOSE SEAT 23ABC INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT BULLNOSE SEAT 23ABC. S YSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 EA 2008 8 7 COMA0860328 1 20080722 A 2760 4916406 SECU CNDAIR CL600 CL6002B19 1900309 EA SPOILERS FAILED A COMA O OTHER N FALSE WARNING CL CLIMB 1 SO 27 786CA 12253 7333 ON CLIMBOUT RECEIVED SPOILERON FAULT MSG, CAS MISCOMP MSG, GRND SPOILER DEPLOY CAUTION MSG, FLT SPLRS CAUTION, SPOILERON CAUTION, NO CONTROL PROBLEMS EXPERIENCED ONLY MSG`S. EMERGENCY DECLARED, A/C LANDED SAFELY IN CVG. MSG`S CLEARED ON L ANDING. REMOVED AND REPLACED NR 1 SECU. (A) 2 L 7 2 4F RT A21EA 20080807 WP 2008 8 7 AALA200801372 1 20080522 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 463AA 49593 MSP - EMERGENCY LIGHT AT SEAT ROW 18DEF MISSING LENS. REPLACED LENS AT SEAT ROW 18DEF. SYSTEM GROUND CHECKED NORMAL OP ERATION. (A) 2 L 7 2 4F A6WE 20080807 NM 2008 8 7 AALA200801469 1 20080602 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 196AA 32390 DFW - EXTERIOR EMERGENCY LIGHT AT LT NR FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LT NR FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 AALA200801470 1 20080602 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 196AA 32390 DFW - EXTERIOR EMERGENCY LIGHT AT RT NR FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RT NR FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 CALA0800713 1 20080715 A 5320 6545834N551 INTERCOSTAL BOEING 737 737524 1384721 NM BS 328-344 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 INTERCOSTAL CRACKED AT STA 328 TO 344 BL 45L. REMOVED CRACKED INTERCOSTAL AT STA 328 TO 344 BL 45L AND INSTALLED NEW IN TERCOSTAL IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 AALA200801359 1 20080520 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 179AA 32397 DFW - EMERGENCY LIGHT AT RIGHT NR TWO DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RIGHT NR TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 AALA200801491 1 20080603 A 5210 BATTERY BOEING 777 777223 1385213 NM DOOR ASSIST MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 798AN 30797 LHR RT NR TWO DOOR POWER ASSIST BATTERY MISSING. REPLACED MODULE FOR RT NR TWO DOOR POWER ASSIST. SYSTEM GROUND CHECKE D NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 NM 2008 8 7 F3LA200800499 1 20080718 A 5321 31953000140 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY BROKEN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C4 S1 C CHECK, INSPECTION NOTED THE AFT CARGO FLOORBOARD, 151CE, HAD TWO BROKEN CORNERS. MAINTENANCE REMOVED AND REPLACED FLOOR PANEL 151CE. INSTALLATION WAS COMPLETED ON EMPIRE AERO CENTER NON ROUTINE NR 9642. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F 4 F RT A28NM E37NE 20080807 NM 2008 8 7 AALA200801742 1 20080701 A 3260 PSEU BOEING 767 767323 1385205 NM MLG INOPERATIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 369AA 25196 DFW INFLIGHT T963/01JUL. AFTER TAKEOFF CREW REPORTED EICAS PROBE HEAT AND LANDING GEAR INDICATIONS. RETURNED TO DFW AN D LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SENSOR ELECTRONICS UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A1NM 20080807 EU 2008 8 7 F3LA200800496 1 20080715 A 5321 D5367414400000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 943FR 18 2518 DURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151FE WAS PUNCTURED. MAINTENANCE REPAIRED DAMAGE IAW T HE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F 4 F RT A28NM E37NE 20080805 EA 2008 8 5 TRAX200800817 1 20080621 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 930EV 8014 IN AFT EQUIP BAY, FS 625, LT CLIP CRACKED AT APPROX 8 O`CLOCK POSITION. REMOVED AND REPLACED FS 625, LT CLIP AT APPROX 8 O`CLOCK POSITION. ALL WORK DONE IAW CRJ200 SRM 51-42-06 M. (S) 2 L 7 2 4F RT A21EA 20080805 NM 2008 8 5 DHL2008F00026 1 20080613 A 5320 CHANNEL BOEING 727 7272M7 138407S NM BS 303 CORRODED A DHLA O OTHER O OTHER NR NOT REPORTED 1 SO 01 750DH 21951 CORROSION, NOSE GEAR TRUNNION WELL LT FORWARD C-CHANNEL BS 303. REMOVED CORROSION ON LT FORWARD C-CHANNEL BS 303 IAW B7 27 SRM 51-10-6. EVALUATED OUT OF LIMITS IAW B727 SRM 53-10-1 FIG 1. REMOVED AND REPLACED C-CHANNEL IAW B727 SRM 51-30- 2. (A) 2 L 7 3 4F A3WE 20080805 EA 2008 8 5 A6WA200840535 1 20080702 A 2421 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA NR 2 IDG LOW A A6WA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 426AW 7669 ON TAKEOFF RECEIVED GEN NR 2 OFF AND IDG NR 2 FAIL MESSAGES. ABORTED TAKEOFF AT 80 KNOTS. BTMS READ 7-7-5-5. FOUND NR 2 IDG LOW ON OIL. SERVICED NR 2 IDG IAW AMM 12-13-24. OPS AND LEAK CHECK GOOD. (A) 2 L 7 2 4F RT A21EA 20080805 SO 2008 8 5 C2XA08ON146 1 20080620 A 3350 82321 SIGN EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS BURNED OUT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12201 6059 3202 14500959 FLT MX - ONT - WHILE PERFORMING ROUTINE CHECK INSPECTION ON CENTER CEILING, FWD EMERGENCY EXIT LIGHT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FWD EMERGENCY CEILING EXIT LIGHT SIGN. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASE TO RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080805 NM 2008 8 5 AALA200801507 1 20080604 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 387AM 27184 DFW - EMERGENCY FLOOD LIGHT AT RIGHT NR ONE ENTRY DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT NR ONE ENTR Y DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080806 NM 2008 8 6 AALA200801436 1 20080530 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 757AN 32636 MIA - EMERGENCY LIGHT AT SEAT 26C MISSING LENS. REPLACED LENS CAP ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GRO UND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 EU 2008 8 6 AALA200801441 1 20080530 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14068 511 MIS - EMERGENCY LIGHTS AT RIGHT SIDE OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT SIDE OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080806 EU 2008 8 6 F3LA200800494 1 20080715 A 5321 D5367302000000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE CABIN PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 943FR 18 2518 DURING C2 C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151BE WAS PUNCTURED. MAINTENANCE REPAIRED THE DAMAGE I AW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND F OUND ACCEPTABLE. (S) 2 L 7 2 4F 4 F RT A28NM E37NE 20080806 NM 2008 8 6 AALA200801735 1 20080630 A 3350 BPS73 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 332AA 22331 JFK - EMERGENCY LIGHTS AT OVERHEAD MID COACH CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A1NM 20080806 NM 2008 8 6 AALA200801412 1 20080527 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 DFW - EMERGENCY LIGHT AT OVERHEAD SEAT ROW 27B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT ROW 27B. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 EA 2008 8 6 TRAX200800686 1 20080522 A 5320 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 529-531 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 929EV 8007 LT MLG WHEEL WELL HYD SUPPORT BRACKET AT FS 529.35 TO FS 531.75 BETWEEN LBL 18 AND LBL 27 IS CRACKED .750 INCH LONG. RE MOVED CRACKED BRACKET, INSTALLED NEW BRACKET P/N 601R75262-159 IAW CRJ 200 SRM 51-42-06. (S) 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 TRAX200800681 1 20080511 A 5220 HINGE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 907EV 7648 CREW ESCAPE HATCH RT HINGE ARM IS CRACKED. REPLACED CREW ESCAPE HATCH RT HINGE ARM IAW CRJ 200 AMM 52-22-00-820-804, ST EPS 3 B1, E. REQUIRES INSTALL, FIT AND CLEARANCE CHECK. FIT AND CLEARANCE CHECK OF CREW ESCAPE HATCH IAW CRJ 200 AMM 5 2-22-00-220-802. CREW ESCAPE HATCH REQUIRES INSTALLATION. 2 L 7 2 4F RT A21EA 20080806 EA 2008 8 6 TRAX200800696 1 20080527 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCONNECTED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 876AS 7376 EMERGENCY FLOOR LIGHTS (FIRST ORANGE PANEL) WILL NOT ILLUMINATE. FLT 4929 DEL 18 MINS. RECONNECTED EMERGENCY LIGHT TRA CK AT SEAT 1C & D. OPS CHECK GOOD IAW AMM 33-51. (S) 2 L 7 2 4F RT A21EA 20080806 EU 2008 8 6 F3LA200800495 1 20080715 A 5321 D5367402800000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 943FR 18 2518 DURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151DE WAS PUNCTURED. MAINTENANCE REPAIRED DAMAGE IAW T HE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F 4 F RT A28NM E37NE 20080806 NM 2008 8 6 HNAA0800231 1 20080714 A 6120 78249050 CONTROL UNIT DHAV DHC8 DHC8102 2809003 NM NR1 PROPELLER FAULTED A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 942HA 163 NR 1 ENG PROP SPEED WENT TO 1217 ON TO ROLL ABORTED TAKEOFF. ABORTED T/O RETURNED TO GATE. MAINTENANCE REPLACED NR 1 P ROP CONTROL UNIT AND TRANSFER TUBE OPS AND LEAK CHECK GOOD FLIGHT 4436. (S) 2 H 7 2 4T RT A13NM 20081119 NM 2008 11 19 SWAA086271 1 20081115 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 680, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080806 NM 2008 8 6 AALA200801424 1 20080528 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW - EMERGENCY LIGHT AT LEFT NR THREE DOOR INOPERATIVE. REPLACED LAMP AT LEFT NR THREE DOOR. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 SO 2008 8 6 C2XA08ON147 1 20080621 A 3350 82301 SIGN EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS BURNED OUT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11184 8870 4980 14500917 FLT MAINTENANCE - ONT - WHILE PERFORMING 3A CHECK INSPECTION ON EXIT SIGN ON ROW NR 1 IT DID NOT ILLUMINATE. MAINTENANC E REMOVED AND REPLACED EMERGENCY AND LIGHT SIGN. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4F RT 20080806 EA 2008 8 6 TRAX200800700 1 20080528 A 5210 LATCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 PASSENGER DOOR HARD TO OPEN. FLT 4608 DEL 35 MINS. ADJUSTED DOOR LATCH CAM SPIGOTS IAW AMM 52-11-00. PASSENGER DOOR O PENS AND CLOSES NORMALLY. NO DEFECTS NOTED. ACFT OK FOR SERVICE. (S) 2 L 7 2 4F RT A21EA 20080806 WP 2008 8 6 AALA200801446 1 20080601 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 428AA 49340 LAS - EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD FIRS T CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080806 WP 2008 8 6 AALA200801392 1 20080525 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7535A 49989 LGA - EMERGENCY LIGHT AT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD GALLEY. SYST EM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080806 NM 2008 8 6 AALA200801394 1 20080525 A 2910 B4724EE0232K HOSE BOEING 757 757223 1384957 NM HYD SYSTEM LEAKING A AALA O OTHER K FLUID LOSS AP APPROACH 1 SW 21 668AA 25333 MCO INFLIGHT T2064/25MAY. LEFT HYDRAULIC SYSTEM QUANTITY LOSS ON SHORT FINAL. LANDED MCO WITHOUT INCIDENT. FOUND FLEX LINE FAILURE AT LEFT WHEEL WELL. REPLACED HYDRAULIC FLEX LINE, ENGINE DRIVEN PUMP AND FILTERS. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080806 EU 2008 8 6 AALA200801405 1 20080526 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 JFK - EMERGENCY LIGHT AT RIGHT NR THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NR THREE DOOR. SY STEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080806 NE 2008 8 6 ABXA080198 2 20080629 A 7321 1305M68P03 EEC BOEING 767 767281 1385109 NM GE CF6 CF680A 30025 NE LT ENGINE DEFECTIVE A ABXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 786AX 150 23019 CLOSE TO V1 SPEED, LT EEC LIGHT, THEN LT ENG OVERTEMP LIGHT. ENG WENT TO 974, WHEN THRUST LEVEL RETARDED, LIGHT OUT. R EMOVED AND REPLACED LT ENG EEC IAW B767 MM 73-21-07-04. EEC TEST GOOD, OPS CHECK GOOD ON GROUND RUN IAW 767 AMM 72-00-0 0-0. (S) 2 L 7 2 4F 4 F RT A1NM E13NE 20080806 EU 2008 8 6 USAA920081378 1 20080715 A 2910 D2901010200200 LINE AIRBUS A319 A319112 3930323 EU HYDRAULIC SYS CRACKED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 722US 1097 FLL-DCA-FLT 1712 - CREW RECEIVED A GREEN HYDRAULIC SYSTEM LOW MESSAGE. CREW DIVERTED TO BWI. AS A PRECAUTION, CREW DEC LARED AN EMERGENCY. THE LANDING WAS UNEVENTFUL. CREW WAS ABLE TO EXIT THE RUNWAY BY DIFFERENTIAL BRAKING. ACFT WAS TO WED TO THE GATE. MX REPLACED CRACKED LT CASE HYDRAULIC LINE AND CASE DRAIN FILTER. OPERATIONAL TEST WAS GOOD. ACFT WAS RETURNED TO SERVICE. (S) 2 L 7 2 4F RT A28NM 20080806 NM 2008 8 6 USAA920081380 1 20080717 A 3397 CONNECTOR BOEING 737 7373G7 138447J NM EMERGENCY LIGHT DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 158AW 23780 PHX - FLT 493 - SEAT ROWS 6 ABC AND 8 ABC EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. MX RECONNECTED EMERGENCY ESCAPE P ATH LIGHTING PLUG. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A16WE 20080806 EA 2008 8 6 TRAX200800837 1 20080625 A 5210 LATCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF RIG A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 PASSENGER DOOR WILL NOT CLOSE WHILE UTILIZING OUTER HANDLE. INSPECTED PASSENGER DOOR AND FOUND THE FWD PULL IN LEVER TO BE HITTING THE FACE OF THE FWD DOOR CAM. REMOVED DOOR PANEL 832AL, REMOVED FWD PULL IN LEVER P/N 600-31689-36. INSTAL LED NEW SERVICEABLE PULL IN LEVER P/N 600-31089-36 IAW S/B 601R-52-111. RIG THE DOOR LATCH MECHANISM. (S) 2 L 7 2 4F RT A21EA 20080806 SO 2008 8 6 SIMA200819902 1 20080715 A 3350 20131A BATTERY PACK EMB 135 EMB135KL 3260302 SO EMERGENCY LIGHT DISCHARGED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 823AE 145582 ON FLIGHT 3643 CREW REPORTED EMERGENCY LIGHTING INOPERATIVE ON PREFLIGHT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLA CED NR 2 AND 4 EMERGENCY BATTERY IAW AMM 33-50-04. OPS CHECKS GOOD. AFT RETURNED TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080807 NM 2008 8 7 KCSA081347 1 20080724 A 5313 LONGERON BOEING 747 747122 1384872 NM BS 1348 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 LT WHEEL WELL OVERWING LONGERON HAS CORROSION AT STA 1348, LBL 120, WL 153. (A) 2 L 7 4 4F RT A20WE 20080807 NM 2008 8 7 KCSA081358 1 20080729 A 5330 SKIN BOEING 747 747122 1384872 NM BS 755 S23R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FUSELAGE SKIN DAMAGED AT BS 755, STR 23R. (S) 2 L 7 4 4F RT A20WE 20080807 NM 2008 8 7 KCSA081359 1 20080729 A 5330 SKIN BOEING 747 747122 1384872 NM BS 539 S39R CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FUSELAGE SKIN CORRODED BELOW STR 39R AT BS 539. (S) 2 L 7 4 4F RT A20WE 20080807 NM 2008 8 7 AALA200801774 1 20080704 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 175AN 32394 DFW - EMERGENCY LIGHT AT SEAT 20D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CH ECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 CALA0800721 1 20080716 A 5311 6546525 FRAME BOEING 737 737524 1384721 NM BS 380 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 RIGHT SIDE STA 380 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REMOVED A/C RAIL B RACKET CUTOUT DAMAGED AREA AND REPAIRED FRAME AT STA 380 RT BETWEEN S-9 AND S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080728 EA 2008 7 28 TRAX200800771 1 20080603 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA CABIN WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 684BR 7708 CREW ESCAPE HATCH EXTERNAL PLACARDS ARE UNREADABLE. REAPPLIED SILKSCREENS ON CREW ESCAPE HATCH IAW MM 11-10-03-400-801. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800773 1 20080608 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 NR 2 AND 4 CEILING EMERGENCY FLOOD LIGHTS INOP. REMOVED AND REPLACED NR 4 BATTERY PACK AND BATTERY CHARGER IAW AMM`S 33 -51-04 AND 33-51-05. OPS CHECK GOOD. CLEARED DEFER AND REMOVED PLACARD. 2 L 7 2 4F RT A21EA 20080815 WP 2008 8 15 08FDEA02832 1 20080711 A 5720 AUB43477 INTERCOSTAL DOUG MD10 MD1010F 3022112 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 LEFT WING TIP INSIDE PANEL NR 528 DB INTERCOSTAL UPPER ANGLE IS CRACKED IN NUMEROUS PLACES. REMOVED LEFT WING TIP IAW MD-10 AMM 57-23-01-2. REPAIRED THE WING TIP IAW DC/MD-10 SRM 57-00-01, FIG 4, VOL I AND SRM 57-20-00, VOL I. COMPLIED WITH FEDEX EA 8-5720-118527 TITLE " WINGS - LT WING TIP FORMER AT YIO 833.430". REINSTALL LT WING TIP IAW MD-10 AMM 57 -23-01-2. OPS CHECK OF THE HIGH INTENSITY AND NAV LIGHTS IS GOOD IAW MD-10 AMM 33-47-00-4; PG 9 AND AMM 33-44-00-4, PG 6. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 08FDEA02814 1 20080710 A 5714 ARC1953507 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING OUTBD FLAP UPPER SKIN SURFACE IS CRACKED BETWEEN THE SECOND AND THIRD FLAP VANE TRACK. REMOVED DAMAGED AREA I AW DC/MD-10 SRM 57-10-00; VOL I, FIG 85. FABRICATED REPAIR DOUBLER AND FILLER IAW DCMD-10 SRM 57-10-00, VOL I, FIG 85 . ALODINED AND PRIMED REPAIR DOUBLER AND FILLER IAW DC/MD-10 SRM 51-21-01, VOL II. INSTALLED DOUBLER AND FILLER IAW DC /MD-10 SRM 57-10-00, VOL I, FIG 85. 2 L 7 3 4F RT A22WE 20080815 EU 2008 8 15 08FDEA02393 1 20080624 A 5753 A2757030220400 TRUNNION AIRBUS 310 A310222 3930315 EU NR 1 JACKSCREW CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 RT WING, UPON SCHEDULED INSP FOUND NR 1 FLAP SCREWJACK TRUNNION AND BUSHING WITH LIGHT PITTING CORROSION INSTALLED NEW F LAP SCREWJACK TRUNNION AND BUSHING PER AMM 27-54-37-4. PERFORMED OPS CHECK PER AMM 27-54-00-5, OPERATION NORMAL 2 L 7 2 4F RT A35EU 20080815 NM 2008 8 15 08FDEA02760 1 20080708 A 5330 651842015 SKIN BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 275FE 22040 LWR FUSELAGE, DRAIN HOLE DAMAGED AT STA. 355 STR 30. REMOVED SKIN PANEL IAW B727 SRM 51-30-2. FABRICATED NEW SKIN MAT USED 2024T3 .050 (27 BY 8.75) IAW B727 SRM 53-30-2 FIG 2 AND 51-30-5. TREATED AND PRIMED NEW SKIN AREA IAW B727 SRM 51- 10-2. INSTALLED NEW SKIN IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 20080815 WP 2008 8 15 08FDEA03027 1 20080723 A 5754 NRB6033 SKIN DOUG DC10 DC1030F 3023504 WP NR 6 SLAT WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 RT WING L/E SLAT NR 6 FOUND DEEP WEAR INTERNAL SIDE. 2 L 7 3 4F RT A22WE 20080815 EU 2008 8 15 08FDEA02989 1 20080721 A 5542 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 300 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD HF1317 613 FLUID INGRESS ON RUDDER LT SIDE PANEL. REPAIR PERFORMED IAW SRM 51-77-10 AND RAS/DAHAM/4024567/2008 ISS, APPROVED BY EA 6-5540-117180. 2 L 7 2 4F RT A35EU 20080815 NM 2008 8 15 08FDEA03019 1 20080722 A 3230 LANDING GEAR BOEING 727 727233 138408A NM MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 271FE 22036 ON DEPARTURE, LANDING GEAR FAILED TO RETACT. COULD NOT RAISE HANDLE PAST OFF. PULLED LATCH AND AURAL C/B'S, STILL COUL D NOT RAISE HANDLE PAST OFF POSITION. SYSTEM FAILED EXTENSION TEST, PER RED TABS DID NOT ATTEMPT TO USE LEVER LATCH TR IGGER. 2 L 7 3 4F RT A3WE 20080815 NM 2008 8 15 08FDEA03035 1 20080724 A 5330 SKIN BOEING 757 75723A 1384967 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 LIGHTNING STRIKE MARK ON FUSELAGE AT BS 1310 BETWEEN S-18R AND S-19R. LIGHTNING STRIKE DAMAGE REPAIR CARRIED OUT IAW B7 57-200 SRM 53-00-01 REV 93, SECT 1, PARA 3 REPAIR 6. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080815 NM 2008 8 15 UPS08M52864 1 20080714 A 5720 STRUCTURE DOUG MD11 MD11F 3023600 NM LT WINGLET CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE-C, LT WING LOWER WINGLET FOUND CRACKED AT AFT FITTING DURING BOROSCOPE INSPECTION. LT WING LOWER WINGLE T CRACKED AFT FITTING REPLACED IAW EO MD11-5720- 27680-A APPENDIX D. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52865 1 20080714 A 5720 STRUCTURE DOUG MD11 MD11F 3023600 NM RT WINGLET CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 277UP 48578 INSPECTION TYPE-C, RT WING LWR WINGLET FOUND CRACKED AT AFT FITTING. DURING BOROSCOPE INSPECTION. RT WING LOWER WING LET CRACKED AFT FITTING REPLACED IAW EO MD11-5720-276 80-A APPENDIX E. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08552837 1 20080702 A 5414 SKIN BOEING 757 75724APF 1384969 NM NR 1 NACELLE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 457UP 25478 INSPECTION TYPE-C, CORROSION ON LWR STRUT OF THE NR1 ENGINE CNA 6 O'CLOCK POSITION PPS206. REPLACED SKIN OF LWR STRUT S KIN MATERIAL THICKNESS OUT OF LIMITS. 2 L 7 2 4F RT A2NM 20080815 EU 2008 8 15 UPS08152727 1 20080701 A 5753 A5724007120000 BRACKET AIRBUS A300 A300F4622R 3930360 EU NR 3 FLAP TRACK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 139UP 0822 INSPECTION TYPE-1C, LT WING NR 3 FLAP TRACK IB SUPPORT ANGLE CRACKED. REMOVED AND REPLACED IB SUPPORT ANGLE FROM L T WING NR 3 FLAP TRACK IAW A-300 SRM 51-40-00. 2 L 7 2 4F RT A35EU 20080815 NM 2008 8 15 UPS08652867 1 20080715 A 5720 114T2300293 WEB BOEING 767 76734AF 1385212 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 303UP 27241 LT WING L/E STA 504 FWD NOSE BEAM WEB LWR AREA CRACK (CRACK LENGTH 1" APPROX). LT WING L/E FWD NOSE BEAM WEB REPLACED I AW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 JUST BETWEEN OSS 499.6 AND OSS 565.9. 2 L 7 2 4F RT A1NM 20080815 NM 2008 8 15 UPS08552888 1 20080716 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 1580 S25-26L DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 421UP 25281 INSPECTION TYPE-C2, DENT IN FRAME INNER FLANGE STA 1580 BETWEEN STR25L-26L REPAIRED IAW SRM 53-00-7-2R5 MPI NR 1980 1. 2 L 7 2 4F RT A2NM 20080815 WP 2008 8 15 UPS08852893 1 20080630 A 5310 DOUBLER DOUG DC8 DC871F 302199D WP BS 1766 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, POSSIBLE CRACK IN RADIUS OF REPAIR DOUBLER ON BOTTOM OF J-BEAM, APB, 60 COMPT. STA 1766 BL0. REMOV ED CRACKED DOUBLER,FABBED AND INSTALLED REPAIR DOUBLER IAW, SRM. 51-1-8, 53-2-5, 51-1-24, 51-1-20D, 51-3-1. 2 L 7 4 4F RT 4A25 20080818 NM 2008 8 18 UPS08M52808 1 20080721 A 3150 WARNING MESSAGE DOUG MD11 MD11F 3023600 NM ILLUMINATED A IPXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 01 256UP 48405 IFSD - ENGINE 1 "OIL FILTER" MSG ACCOMPANIED BY HIGH OIL TEMP INDICATION. REPLACED NR 1 ENGINE IAW T/C 9100. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 UPS08552863 1 20080717 A 5347 CARGO TRACK BOEING 757 75724APF 1384969 NM CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 421UP 25281 INSPECTION TYPE-C2, CORROSION ON MAIN DECK CARGO TRACK UPPER SURFACE AT NUTPLATE HOLES BS 1120-1146, LBL 23, WL 208. RE MOVE AND REPLACE SEAT TRACK FROM BS 1080 TO 1180 LBL 23. 2 L 7 2 4F RT A2NM 20080818 NM 2008 8 18 UPS08552873 1 20080716 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM BS 1510 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 421UP 25281 INSPECTION TYPE-C2, CORROSION AFT CARGO BAY FLOORBEAM BS 1510, RBL 12. REMOVE AND REPLACE FLOORBEAM, BS 1510, RBL 12. 2 L 7 2 4F RT A2NM 20080818 WP 2008 8 18 UPS08852742 1 20080701 A 5313 DC853B00939 LONGERON DOUG DC8 DC871F 302199D WP FS 1739-1720 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, L15L CRACKED AT CANTED FRAME, MAIN CABIN, STA 1729 REMOVED LONGERON SECTION FS 1739-1720. FABR ICATED AND INSTALLED LONGER ON SPLICE AND REPAIR STRAPS. IAW SRM 53-02-02 FIG 10 AND 53-05-03. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852748 1 20080614 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1530-1610 BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, SEAT TRACK AT LBL 45 BS 1600 MAIN CABIN HAS SEVERAL TANGS BROKEN OFF. FABRICATED NEW SEAT TRACK SEC TION BS 1530-1610 LBL45 AND INSTALLED IA IAW SRM 53-02-03-0 FIG 008A, 51-01-08,51-03-00,51-03-01 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852729 1 20080706 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, FLOOR PANEL F94/F94A HAS SEVERAL ELONGATED HOLES AND A CRACK AT THE EDGE, CUT OUT DAMAGE IAW SRM 53- 02-03 FIG 005A. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-02-03,AND 51-1-21. 2 L 7 4 4F RT 4A25 20080818 NM 2008 8 18 UPS08552633 1 20080702 A 3350 POWER SUPPLY BOEING 757 75724APF 1384969 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 473UP 28846 OUTSIDE EMERGENCY LIGHT INOP. R/R POWER SUPPLY IAW MM 33-51-07-2. 2 L 7 2 4F RT A2NM 20080818 NM 2008 8 18 UPS08652666 1 20080701 A 5754 114T2300292 WEB BOEING 767 76734AF 1385212 NM RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 301UP 27239 RT WING L/E OSS 695 NOSE BEAM SUPPORT WEB LWR AREA FOUND CRACKED. (CRACK LENGTH 1" APPROX ) RHW AT OSS 694 TO OSS 717 L /E NOSE BEAM SUPPORT WEB REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20080818 NM 2008 8 18 UPS08652667 1 20080701 A 5754 114T2300272 WEB BOEING 767 76734AF 1385212 NM RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 301UP 27239 RT WING L/E OSS 664 NOSE BEAM SUPPORT BEAM LOWER AREA FOUND CRACKED (CRACK LENGTH .7500"). RHW AT OSS 648 TO OSS 694 L/ E NOSE BEAM SUPPORT WEB REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20080818 NM 2008 8 18 UPS08652668 1 20080701 A 5754 114T2300271 WEB BOEING 767 76734AF 1385212 NM LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 301UP 27239 LT WING OSS 664 & 679 NOSE BEAM WEB LOWER AREA FOUND CRACKED. (CRACK LENGTH 2" & 3") LHW AT OSS 648 TO OSS 694 L/E NOSE BEAM SUPPORT WEB REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20080818 WP 2008 8 18 UPS08852618 1 20080611 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP FS 38 LBL 59 WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, SUPPORT STRUCTURE AROUND MM PUMP HANDLE FITTING WORN HANDLE, FITTING VERY LOOSE, IN FLOOR A L1 DOOR, STA 38 LBL 59 FABRICATED AND INSTALLED 2EA REPAIR DOUBLERS IAW SRM 53-02-00 FIG 001B AND DC8 SRM 51-01-20D. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852627 1 20080613 A 5320 TORQUE BOX DOUG DC8 DC871F 302199D WP FS 1205-1220 CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, C-PIT AT BS 1220, TORQUE BOX BENEATH CROSS-SLIDE DOOR HAS REPAIR DOUBLER WITH DEEP CHAFE WEAR, GOUGE S FABRICATED AND REPLACED REPAIR DOUBLER IAW DWG 3753772 AND SRM 53- 02-00 FIG 025, 51-01-20D. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852635 1 20080615 A 5532 SKIN DOUG DC8 DC871F 302199D WP VERTICAL STAB BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1 VERTICAL FIN, RT SIDE AFT OF ISOLATION STRIP HAS SKIN BULGING AND FASTENERS PULLING. REMOVED FASTENE RS FOR ACCESS IAW SRM 51-01-21. NO CORROSION NOTED ON A REA. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 55-02-00, A ND 51-01-21. 2 L 7 4 4F RT 4A25 20080818 NM 2008 8 18 UPS08M52614 1 20080401 A 5350 FRAME DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE TAILCONE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSP TYPE-C, FWD TAILCONE ACCESS CUT OUT LT FRAME, FOUND CHAFED MARK ON PREVIOUS REPAIR. FWD TAILCONE UPPER FWD DOOR O PENING MECH ASSY REMOVED FOR ACCESS. CHAFE MARK FOUND OUT OF LIMIT & REMOVED IAW SRM 51-31-01 VII R35. FAB NEW FWD TAIL CONE FRAME WITH HEAT TREATMENT C/O. NEW FRAME REWORKED, HOLES KED-UP, PROTECTED & PAINTED. NEW FRAME INSTALLED. OPENING MECH ASSY INSTALLED. FWD TAILCONE UPR DOOR ADJUSTED & OPS CHECKED C/O 'SATISFACTORY'. 2 L 7 3 4F 4 F RT A22WE E24NE 20080818 NM 2008 8 18 UPS08M52617 1 20080702 A 3340 5D0108117 SWITCH DOUG MD11 MD11F 3023600 NM COCKPIT SHORTED A IPXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 252UP 48768 SHOWER OF SMOKE AND SPARKS WAS EMITTED FROM THE RUNWAY TURNOFF LIGHT SWITCH WHEN TOUCHED. CB "R LDG AND TAXI LIGHT" POP PED. FOUND SWITCHES S1-9090 AND S1-9091 TOUCHED CONNECTION ON SW1-236 WHICH CAUSED SPARKS AND BURN MARKS. R/R S1-236 I AW WDM 33-42-01. R/R S1-9090 IAW WDM 33-43-01. OPS CHECK OK. CB'S RESET. S1-9091 LT WING & RUNWAY TURNOFF LIGHT. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 UPS08652923 1 20080731 A 2781 INDICATOR BOEING 767 76734AF 1385212 NM LE FLAPS MALFUNCTIONED A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 306UP 27759 ATB - RECEIVED MESSAGE AND FLAP INDICATOR SHOWED LE FLAPS NOT UP. RAN CHECKLISTS. REMOVED AND REPLACED IAW 27-58-02-4 F LAP POSITION INDICATOR OPERATION CHECKED SATISFACTORY IAW 27-58-00-5. 2 L 7 2 4F RT A1NM 20080818 WP 2008 8 18 UPS08852924 1 20080708 A 5313 STRINGER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2 NR 4 ALT STRINGER -65 TO FRONT SPAR Z FITTING CRACKED. REMOVED AND REPLACED STINGER IAW SRM,51-1- 20D, 51-1-8. 2 L 7 4 4F RT 4A25 20080818 NM 2008 8 18 08FDEA02975 1 20080718 A 5347 S492915018 SEAT TRACK DOUG MD10 MD1030F 3024020 NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 303FE 46802 MCD SEAT TRACK IS GOUGED AT RBL 7 STATION 635. BLENDED AREA FOUND OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED NEW TRACK AND INSTALLED NEW SEAT TRACK ON MAE TRAVELER T8/747973 AND IAW SRM 53-70-00 FIG 1 AND FIG 5. REPAIR IS CLASSIFIED AS A MAJOR REPAIR, REPORTABLE DISCREPANCY AND RII. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 UPS08552953 1 20080706 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM BS 1183 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 457UP 25478 INSPECTION TYPE-C2, CORROSION ON SEAT TRACK LBL 45 BS 1183 WL 208. REPLACED CORRODED SECTION OF SEAT TRACK DUE TO CORRO SION BLENDS BEING OUT OF LIMITS. 2 L 7 2 4F RT A2NM 20080818 NM 2008 8 18 UPS08552968 1 20080706 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM BS 1200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 457UP 25478 INSPECTION TYPE-C-2, CORROSION UPPER SURFACE FLOORBEAM, BS 1200, RBL 57-LBL 57, WL 208. CORROSION BLENDS OUT OF LIMITS FABRICATED ANGLE REPAIR, STIFFENERS AND CLIP FOR REPAIR IAW ER 08-2334. 2 L 7 2 4F RT A2NM 20080818 NM 2008 8 18 UPS08M52960 1 20080718 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 1 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 UPS08M52963 1 20080719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE:1C, FOUND CORROSION IN NR 16 LT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED RE PAIR BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 SWAA084020 1 20080716 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM BS 504D CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED HC1 CHECK, FOUND KEELBEAM CORRODED AT BS 504D, STR 28L, WL 148. REPAIRED KEELBEAM PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084019 1 20080721 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 EMERGENCY LIGHT LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084063 1 20080721 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 448WN 33721 EMERGENCY LIGHT LENS MISSING AT RH OVERWING EXIT. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084031 1 20080721 A 5311 6545874 FRAME BOEING 737 7375H4 138449D NM BS 291 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED BRDG CHECK, FOUND STUB FRAME CRACKED AT BS 291, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084030 1 20080721 A 5753 65C30462 SKIN BOEING 737 7375H4 138449D NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED BRDG CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED AT UPPER SURFACE RT SIDE. REPAIRED FLAP PER S RM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084033 1 20080721 A 5310 6546817 CREASE BEAM BOEING 737 7375H4 138449D NM BS 424 S17L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 424, STR 17L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084032 1 20080721 A 5754 SKIN BOEING 737 7375H4 138449D NM LT WING LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED BRDG CHECK, FOUND LT WING NR 1 L/E SLAT INBOARD END DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084065 1 20080718 A 3350 10107451 SIGN BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND FWD CABIN EMERGENCY EXIT SIGN CRACKED. R&R EXIT SIGN PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084045 1 20080721 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 727C S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED A TBS 727C, STR 6L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080814 2008 8 14 NWAA08272928 4 20080612 A 2565 SLIDE DOUG DC9 DC931 3022065 WP TAILCONE FAILED A NWAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 01 8921E 48014 4137 45836 THE AIRCRAFT ARRIVED AT EAU AS A DIVERTED FLIGHT DUE TO CABIN PRESSURIZATION FAILURE. DURING GROUND OPERATIONS AT EAU, R AMP PERSONNEL INADVERTENTLY JETTISONED THE TAIL CONE AND THE SLIDE FAILED TO DEPLOY. ENGINEERING WAS BROUGHT ON-SITE TO OBSERVE & EVALUATE REPEATED ATTEMPTS AT SLIDE DEPLOYMENT VIA TAILCONE SEPARATION. THE SLIDE FAILED TO DEPLOY ON AT LEAST THREE ATTEMPTS AND WAS THEN REPLACED. (A) 2 L 7 2 4F A6WE 20080814 NM 2008 8 14 F3LA200800531 1 20080731 A 5321 D5367301200000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY SCRATCHED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2 2209 DURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT LT LOWER TRANSITION PANEL 131BF HAS DEEP SCRATCHES ALONG BOTTO M EDGE. MAINTENANCE REMOVED DAMAGED AREA AND CLEANED IAW THE REQUIREMENTS OF SRM 53-02-00 PAGE 214. MAINTENANCE FILLED DAMAGED AREA IAW THE REQUIREMENTS OF SRM 53-02-00 FIGURE 204 AND PAINTED TRANSITION PANEL IAW THE REQUIREMENTS OF AMM 2 5-00-00-370-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 F3LA200800543 1 20080801 A 5320 STRUCTURE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2 2209 DURING C3 C-CHECK, INSPECTION NOTED LIGHT CORROSION AT NUT PLATE LOCATIONS ON LT TRANSITION PROFILE AT FRAME 26. MAINTE NANCE BLENDED CORROSION AND UPSIZED HOLE TO .3400, WITH MAXIMUM MATERIAL REMOVED OF .012, IAW THE REQUIREMENTS OF A319 SRM 51-73-00. MAINTENANCE FABRICATED REPAIR DOUBLER (2024-T3 .040), TREATED, PRIMED AND PAINTED, AND INSTALLED DOUBLER IAW THE REQUIREMENTS OF ENGINEERING AUTHORIZATION A9-53R-30529. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUN D ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 QXEA200800857 1 20080801 A 3260 860TS09Y00 CONTROL PANEL BOMBDR DHC8 DHC8402 1390042 NM COCKPIT MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 19 419QX 17360 1321 4145 BOI - FLIGHT 2498. AFTER GEAR RETRACTION THE NOSE GEAR GREEN LIGHT REMAINED ON. PERFORMED CHECKLIST WITH NO HELP. PER FORMED ALTERNATE EXTENSION AND RETURNED TO THE FIELD AT BOI AND ACCOMPLISHED UNEVENTFUL LANDING. REPLACED THE LANDING G EAR CONTROL PANEL. OPERATIONAL CHECKS GOOD. ACFT RETURNED TO SERVICE. (S) 2 H 7 2 4T RT A13NM 20080814 EA 2008 8 14 COMA0870021 1 20080731 A 2781 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA L/E SLAT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 398CA 10112 FLIGHT 5622 RECEIVED SLAT FAIL CAUTION MESSAGE. DECLARED EMERGENCY, RETURNED TO ATL, LANDED WITHOUT INCIDENT. PERFORME D RESET AND CLEARED INHIBITS. VISUALLY INSPECTED SLATS AND SLAT DISCONNECT SYSTEM. PERFORMED OPERATIONAL CHECK. NO FU RTHER DEFECTS. (S) 2 L 7 2 4F RT A21EA 20080814 NM 2008 8 14 USAASB08057 1 20080802 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 434US 24556 DFW - MAINTENANCE REPORTED THE EMERGENCY LIGHTING IN THE AFT CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AF T CABIN RT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A16WE 20080814 EU 2008 8 14 USAA920081447 1 20080731 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 663AW 1419 FLT 376 SMF-PHL - EMERGENCY EQUIPMENT - FLASHLIGHT UNDER FORWARD FACING FLIGHT ATTENDANT SEAT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080814 EU 2008 8 14 USAA920081459 1 20080803 A 5210 FE277000 ACTUATOR AIRBUS A321 A321211 3930370 EU L2 DOOR LEAKING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 169UW 26774 2904 1455 FLT 899 LGA-CLT - EMERGENCY EQUIPMENT - L2 DOOR ASSIST BOTTLE LEAKS. MAINTENANCE REMOVED AND REPLACED THE L2 DOOR ASSIS T ACTUATOR IAW AIRBUS MM 52-11-14. OPERATIONAL CHECK NORMAL. (S) 2 L 7 2 4F RT A28NM 20080815 EU 2008 8 15 08FDEA03043 1 20080724 A 5347 A537819300100 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 686FE 804 MAIN DECK LT SIDE SEAT TRACK 4L AT FRAME 20 HAS 3 ELONGATED SCALLOPS. REMOVED AND REPLACED SEAT TRACK 4L FROM FRAMES 18 TO 26 IAW A300-600 SRM 51-72-10 AND 51-40-21. 2 L 7 2 4F RT A35EU 20080815 WP 2008 8 15 08FDEA02974 1 20080718 A 5320 S2929627T INTERCOSTAL DOUG MD10 MD1010F 3022112 WP ZONE 100 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 FWD PIT STA 775, LONGERON 33R INTERCOSTAL IS BENT. REMOVED INTERCOSTAL REF DC/MD-10 SRM 51-35-01, VOL II. FAB MATERIAL ID S2929627 ALUM, FORMED SECTION 2027-T3, PO 469828.2 REF DC/MD-10 SRM 53-13-01, VOL III, PG 38. LOCATED FASTENER HOL ES IN INTERCOSTAL REF DC/MD-10 SRM 51-31-01, VOL II. ALODINE, PRIME AND TOP COAT REF DC/MD-10 SRM 51-21-01, VOL II. PA RT MARKED INTERCOSTAL REF FEDEX GMM 7-0-1000, FRX 2929627T TOMCO - GSO JULY 17 2008. 2 L 7 3 4F RT A22WE 20080815 EU 2008 8 15 08FDEA02980 1 20080612 A 5311 A53834139 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 FUSELAGE, FR 47 HOLE K REF TO EO 6-5310-7-5017 PT4, FOUND DAMAGED. HOLE K REPAIRED AS PER FEDEX EA 6-5310-121645. 2 L 7 2 4F RT A35EU 20080815 NM 2008 8 15 08FDEA03067 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL ACCESS PANEL CUTOUT 541BB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080815 NM 2008 8 15 08FDEA03068 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL ACCESS PANEL CUTOUT 541CB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080815 NM 2008 8 15 08FDEA03034 1 20080724 A 5330 SKIN BOEING 757 75723A 1384967 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 LIGHTNING STRIKE MARK ON FUSELAGE AT BS 1294, 2 INCHES BELOW S-18R. LIGHTNING STRIKE DAMAGE REPAIR CARRIED OUT IAW B757 -200 SRM 53-00-01 REV 93, SECT 1 PARA 3 REPAIR 6. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080815 NM 2008 8 15 08FDEA03036 1 20080724 A 5315 7075T60100 FLOORBEAM BOEING 757 75723A 1384967 NM ZONE 200 DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 919FD 24636 MAIN DECK FLOORBEAM AT BS 365, RBL 62 HAS AN UNFILLED HOLE. DAMAGED PART OF BEAM REPAIRED IAW B757-200 SRM 53-00-51 REV 93 DETAIL 1. REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080815 WP 2008 8 15 08FDEA03037 1 20080724 A 5512 ALC72251 SKIN PANEL DOUG DC10 DC1030F 3023504 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 DURING INSPECTION OF COSTANT AND OUTER SECTION MACHINED SKIN PANELS ON HORIZONTAL STAB, FOUND NR 5 PANELS WITH CRACK, A RE WITHIN LIMITS IAW TABLE MM PANELS P/N: 7228-1, 7227-1, 7281-2, 7226-1 AND 7225-1SEE ATTACHED SHEET FOR DETAIL. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52914 1 20080719 A 5712 ARB292913 RIB DOUG MD11 MD11F 3023600 NM LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, LT WING LE RIB FWD OF XORS 917 CRACKED ON AFT END, REMOVED, FABRICATED, AND INSTALLED RIB IAW M D-11 SRM 51-31-01, DWG ARB2920, SAA TRAVELER 80538380001, AND MD-11 SRM 51-35-01. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52925 1 20080710 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 5 RT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED BUSHING, AND INS TALLED BUSHING IAW EO MD11-5510-19409-N AND SAA TRAVELER 80538290001. 2 L 7 3 4F RT A22WE 20080728 NM 2008 7 28 KCSA081301 1 20080628 A 5310 TORQUE BOX BOEING 747 747122 1384872 NM BS 1840-1860 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 AFT BILGE UPPER TORQUE BOX WEB HAS SEVERAL DENTS AT STA. 1840 TO 1860, LBL 46 TO LBL 62 (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 KCSA081308 1 20080702 A 5711 FRAME BOEING 747 747122 1384872 NM LT WING DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FOUND FRAME WEB DAMAGED APPROX.20" FWD OF I/B AILERON @WBL-455 (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 KCSA081307 1 20080702 A 5312 BULKHEAD BOEING 747 747122 1384872 NM BS 1241 RBL 98 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 RT WHEEL WELL CANTED BULKHEAD AT STA. 1241 HAS CORROSION ON LOWER CHORD INBOARD OF BULKHEAD FITTING RBL 98 (B) 2 L 7 4 4F RT A20WE 20080728 EA 2008 7 28 TRAX200800665 1 20080519 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 929EV 8007 BRACKET AND ATTACHING ANGLE ONN RT ACM SUPPORT STRUCTURE ARE CRACKED, MARKED. REMOVED CRACKED BRACKET AND ANGLE AND INS TALLED NEW SERVICEABLE PARTS IAW SRM 51-42-06. (B) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 AALA200801327 1 20080516 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 796AN 30796 NRT EMERGENCY FLOOR LIGHT AT FIRST CLASS CLOSET HANGING LOOSE. SECURED EMERGENCY FLOOR LIGHT AT FIRST CLASS CLOSET. SY STEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 EA 2008 7 28 MASA200800452 1 20080606 A 5210 SEAL CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR FOD A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 649BR 7414 ASH FLT 7247 IAD-BHM SERVICE DOOR WILL NOT OPEN. MX REMOVED DEBRIS FROM THE DOOR SEAL AND TSA STICKERS FROM HINGE AREA --OPS CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 MASA200800455 1 20080607 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 912FJ 15012 ASH FLIGHT 2764 PHX-RNO. RT EMERGENCY LIGHT OUT AT EXIT SIGN MID CABIN. MX RELAMPED AND SYSTEM CHECKED GOOD. (B) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 MASA200800451 1 20080606 A 5210 MECHANISM CNDAIR CL600 CL6002B19 1900309 EA DOOR HANDLE LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75987 7405 ASH FLT 7197 ORD-SBN. PAX DOOR WILL NOT OPEN FROM OUTSIDE. LUBED INNER HANDLE MECHANISM. (B) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 AALA200801326 1 20080516 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 MIA EMERGENCY LIGHT AT SEAT 25C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NOR MAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 NM 2008 7 28 AALA200801328 1 20080517 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 751AN 30798 DFW EMERGENCY LIGHT AT LT NUMBER ONE DOOR FORWARD GALLEY CLOEST BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LT NUMBER ONE DOOR FORWARD GALLEY CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 WP 2008 7 28 AALA200801331 1 20080517 A 2697 JD3899926WD35SN CONNECTOR DOUG DC9 DC983 3022083 WP FIRE DETECTION CORRODED A AALA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 9622A 53593 AMA INFLIGHT T1661/17MAY DFW TO SEA. AFT CARGO FIRE INDICATION. FIRE BOTTLE DISCHARGED. LANDED AMA WITHOUT INCIDENT. NO EVIDENCE OF FIRE. FOUND CARGO ELECTRONICS UNIT CONNECTOR WITH CORROSION. REPLACED AFT CARGO ELECTRONICS UNTIL CONN ECTOR AND FIRE BOTTLES. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A6WE 20080728 NM 2008 7 28 AALA200801339 1 20080518 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 792AN 30253 JFK EMERGENCY LIGHT AT SEAT 21G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED NOR MAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 NM 2008 7 28 AALA200801340 1 20080518 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 JFK EMERGENCY LIGHT AT OVERHEAD SET 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 22C. SYSTEM GR OUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 NM 2008 7 28 AALA200801341 1 20080518 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 790AN 30251 JFK EMERGENCY LIGHT AT SEAT 23C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23C. SYSTEM GROUND CHECKED NOR MAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 NM 2008 7 28 AALA200801338 1 20080518 A 3350 OL3071BPEGL LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 762AN 31479 JFK EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NORM AL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 NM 2008 7 28 AALA200801348 1 20080519 A 3397 CONNECTOR BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 760AN 31477 DFW EMERGENCY LIGHT AT RT NUMBER ONE DOOR MISSING WIRE CONNECTOR. REPLACED CONNECTOR FOR EMERGENCY LIGHT AT RT NUMBER O NE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 NM 2008 7 28 AALA200801343 1 20080519 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 655AA 24613 DFW EMERGENCY LIGHT AT SEAT 21D INOPERATIVE. REPLACED BATTERY PACK AT MID CABIN OVERHEAD FOR EMERGENCY LIGHT AT SEAT 21 D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A2NM 20080728 EU 2008 7 28 TRAX200800623 1 20080513 A 3350 BULB AEROSP ATR72 ATR72 EU EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 630AS 336 ASD EMERGENCY LIGHT INOP. REPLACED BULB IN ASD EMERGENCY LIGHT IAW AMM 33-51-24. OPS CK GOOD. (B) 2 H 7 2 4T RT 20080728 NM 2008 7 28 KCSA081295 1 20080621 A 5311 FRAME BOEING 747 747122 1384872 NM BS 1265 S26R CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FUSELAGE FRAME WEB IS CRACKED AT STA. 1265, BELOW STR. 26R (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 KCSA081272 1 20080604 A 3350 LIGHT BOEING 747 747132 1384882 NM CABIN INOPERATIVE A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 709CK 20247 EMERGENCY LIGHT INOP ABOVE UPPER DECK STAIRS (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 KCSA081277 1 20080611 A 5730 SKIN BOEING 747 747122 1384872 NM LT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 LT WING UPPER SKIN CORRODED AT AFT RABBET AREA W.S.522 (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 AALA200801342 1 20080519 A 3350 LENS BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 655AA 24613 DFW EMERGENCY LIGHT AT SEAT 28D HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A2NM 20080728 EA 2008 7 28 TRAX200800876 1 20080704 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 980EV 7759 AFT TWO EMERGENCY LIGHTS IN THE CEILING INOP RELAMPED AFT TWO EMERGENCY LIGHTS IA 33-51-16. 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 AALA200801353 1 20080519 A 3350 LENS BOEING 767 767323 1385205 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 385AM 27059 DFW EMERGENCY LIGHT AT RT HAND AFT OVERWING MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RT HAND AFT OVERWING. S YSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A1NM 20080728 NM 2008 7 28 USAA920081317 1 20080628 A 5322 SHEAR TIE BOEING 757 757225 1384959 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925UW 22205 BFM - MAJOR REPAIR - C3 CHECK - LEVEL 2 CORROSION ON SHEAR TIE, BS 1320, S28-29L. REPLACED SHEAR TIE, BS 1320, 28L-S29L IAW B757 SRM 51-40-02. (S) 2 L 7 2 4F RT A2NM 20080728 NM 2008 7 28 USAA920081186 1 20080519 A 5240 65554787 GATE BOEING 737 7374B7 1384702 NM SERVICE DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 CHECK - LEVEL 2 CORROSION ON THE AFT SERVICE DOOR LOWER GATE. REPLACED THE AFT SERVICE DOOR LOW ER GATE IAW B737 SRM 51-40-02. (S) 2 L 7 2 4F RT A16WE 20080728 EU 2008 7 28 USAA920081178 1 20080605 A 4990 1604941 OIL COOLER AIRBUS A319 A319112 3930323 EU APU INOPERATIVE A USAA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 EA 19 738US 4080 1731 1254 FLT 1744 CLT - PHL - ELECTRICAL POWER LOSS - AIRCRAFT DEPARTED CLT WITH THE NR1 IDG ON MEL. CREW REPORTED APU AUTO SHUT DOWN AT FL 330. RESTARTED AT FL 290 AND FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED TH E APU OIL COOLER. OPERATIONAL AND LEAK CHECKS WERE GOOD. (S) 2 L 7 2 4F RT A28NM 20080728 NM 2008 7 28 USAA920081200 1 20080604 A 5755 654645170A SKIN PANEL BOEING 737 7373B7 1384580 NM NR 6 SPOILER DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 530AU 24412 CLT - MAJOR REPAIR - C4 CHECK - RT WING NR 6 SPOILER UPPER SURFACE DISBONDED. REPLACED RT WING NR 6 SPOILER IAW B737 AM M 27-61-11. (S) 2 L 7 2 4F RT A16WE 20080725 NE 2008 7 25 IXX2008F00012 2 20080711 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM56 CFM56* 13802 NE NR 3 FIRE A IXXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 11 603AL 46003 DURING FLIGHT, NR 3 ENGINE FIRE WARNING LIGHT ILLUMINATED MOMENTARILY. FLIGHT CREW RETARDED THE THROTTLES AND SHUTDOWN THE ENGINE. THE FIRE LIGHT AND WARNING WENT OUT. APPROX 30 MINUTES LATER FIRE WARNING CAME BACK ON. FLIGHT CREW FIRED (1) BOTTLE AND AGENT DISCHARGED LIGHT WENT OUT AND NEVER CAME BACK ON. AC FLEW DIRECT TO DESTINATION AND LANDED WITHOU T FURTHER INCIDENT. (OPEN) (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 20080725 NM 2008 7 25 GTI2008F00000 1 20080505 A 5311 FRAME AIRBUS A321 A321231 3940032 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 587NK 2476 FRAME 69 LT AND RT HAVE EVIDENCE OF CORROSION. REMOVED AND REPLACED SHEAR PLATES. (K) 2 L 7 2 4F RT A28NM 20080725 NM 2008 7 25 R612008F00000 1 20080628 A 2751 1702286A SENSOR EMB ERJ170 ERJ170200LR 3260121 NM GE CF34 CF348E5 30061 NE SLAT SKEW FAILED A R61A A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 11 124HQ 1350 17000200 CREW RECEIVED A SLAT FAIL MESSAGE ON APPROACH DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATC HED TO THE AIRCRAFT TO EVALUATE. MAINTENANCE REMOVED AND REPLACED LT OB SLAT SKEW SENSOR SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 2 4F 4 F RT A56NM E00063EN 20080725 EA 2008 7 25 FDK2008F00004 1 20080716 A 5270 WARNING MESSAGE CNDAIR CL600 CL6002D24 1390016 EA GE CF34 CF348C5 30050 NE PAX DOOR LATCH FALSE ACTIVATION A FDKA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 606LR 15173 PAX DOOR LATCH CAUTION MSG. MX OPS CHECKED GOOD. (K) 2 L 7 2 4F 4 F RT A21EA E00063EN 20080725 WP 2008 7 25 IXX2008F00008 1 20080708 A 2612 FIRE WARNING DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE NR 2 ILLUMINATED A IXXA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 11 820BX 46065 DURING CRUISE, NR 2 FIRE WARNING CAME ON, THE CREW DISCHARGED BOTH FIRE BOTTLES AND SHUTDOWN NR (2) ENGINE. CREW LANDED WITHOUT INCIDENT. IN WORK. (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 20080725 NE 2008 7 25 IXX2008F00007 2 20080706 A 7200 ENGINE DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE NR 3 OIL CONSUMPTION A IXXA O OTHER O OTHER NR NOT REPORTED 1 SW 11 71CX 45961 DURING CRUISE, THE CREW SHUTDOWN NR 3 ENGINE DUE TO OIL QUANTITY DROPPING TO LESS THAN ONE GALLON, OIL PRESSURE GAUGE FL UCTUATING, OIL TEMP WAS ABOVE 115C, OIL PRESSURE LIGHT INTERMITTENT, THE CREW LANDED WITHOUT FURTHER INCIDENT. AC WAS A UTHORIZED FERRY FLIGHT FOR MAINTENANCE. MAINT CONFIRMED OIL RESERVOIR IS FULL AND AIRCRAFT SAFE FOR FLIGHT. ENGINE CHA NGE IN WORK. (K) 2 L 7 4 4F 4 F 4A25 1E8 20080725 CE 2008 7 25 MT92008F00005 1 20080717 A 3150 WARNING LIGHT CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE ILLUMINATED E MT9A K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 05 9469B 208B0079 AFTER ENGINE INSTALLATION FROM OVERHAUL, THE PERFORMANCE RUN PRODUCED THE "AUX FUEL PUMP" AND "FUEL PRESSURE LOW" LIGHTS ON THE ANNUNCIATOR PANEL CYCLING ON AND OFF TOGETHER. THIS HAPPENS WHEN THE FUEL PRESSURE IN THE HOPPER TANK DROPS BEL OW 4.75 PSI. (FUEL PUMP 0.00) (K) 1 H 7 1 3T 3 T A37CE E4EA 20080725 CE 2008 7 25 GUU2008F00001 1 20080704 A 2910 HYDRAULIC SYSTEM BEECH 1900 1900D 1154162 CE PWA PT6 PT6* 52043 EA LOW A GUUA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 29 16540 UE172 DURING APPROACH AFTER SELECTING THE LANDING GEAR DOWN THE "J" LOCK ENGAGED AND THE CIRCUIT BREAKER TRIPPED IMMEDIATELY. FOUND HYDRAULIC SYSTEM LOW SERVICED HYDRAULIC SYSTEM. OPERATIONAL CHECK NORMAL. (K) 2 L 7 2 4T 3 T RT A24CE E2NE 20080728 NM 2008 7 28 UIE2008F00005 1 20080621 A 5730 FAIRING BOEING 747 7472D7B 1384803 NM LT WING DAMAGED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 524MC 21784 LT IB FLAP NR 3, MOVEABLE FLAP TRACK FAIRING HAS A HOLE AT WBL 353.0 HOLE SIZE IS 4.0 INCHES X 7.0 INCHES. PERMANENT R EPAIR ACCOMPLISHED IAW B747200, SRM 51-40-09, FIG 6 SHEET 1 THRU 3, 250 DEGREES F CURE IAW SRM 51-40-12. ALSO, REFERENC E EO 4757A449. (K) 2 L 7 4 4F RT A20WE 20080728 WP 2008 7 28 UPS08852577 1 20080528 A 5340 ATTACH FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C2 AFT ACCESSORY COMPT STA 1580, L21L FLOORBEAM ATTACH FITTING HAS CORROSION. REMOVED AND REPLACED END FITTING IAW SRM, 51-1-8, 51-1-20D, 51-3-1. 2 L 7 4 4F RT 4A25 20080728 NM 2008 7 28 UIE2008F00006 1 20080621 A 5312 PRESSURE PANEL BOEING 747 7472D7B 1384803 NM NOSE WHEEL WELL CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 524MC 21784 NOSE WHEEL WELL TOP PANEL WEB FOUND WITH A CRACK AT BS 310 AT LBL 10. CRACK LENGTH IS 1.125 INCHES. INTERIM REPAIR ACC OMPLISHED IAW SRM 53-10-04, FIG 116. SHEETS 1 AND 6 AND FIG 117 SHEETS 1 THRU 10. REQUIRES INITIAL INTERNAL DETAIL VIS UAL INSPECTION PRIOR TO 15,000 FC. (K) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 2008UALA03478 1 20080618 A 4960 MR49533225 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU FAULTY A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 548UA 25396 APU FAILED 3 START ATTEMPTS AT FL360. APU 60189 HAS EXHIBITED STARTING ISSUES SINCE LATE MAY. PRIOR TO THIS EVENT ECU MR49613-127 WAS REPLACED WITH MR49613-40 ON 6/8/08. THE -127 UNIT TESTED WITH NO FAULT FOUND. INLET PRESSURE SENSOR MR 49533-225 WAS REPLACED WITH MR49533-75 ON 6/18/08. THE -225 UNIT TESTED WITH NO FAULT FOUND. THE STARTING ISSUES CONTI NUED SINCE THIS EVENT ON 6/18/2008. 2 L 7 2 4F 4 F RT A2NM E17NE 20080728 NM 2008 7 28 2008UALA03462 1 20080618 A 2432 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MAIN FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 552UA 26641 AIRCRAFT WILL NOT ACCEPT POWER. MAIN BATTERY FAILURE. REPLACED MAIN AIRCRAFT BATTERY, CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080728 CE 2008 7 28 DJF2008F00005 1 20080612 A 3340 45A23325001 CAP BEECH MU300 400A 1155402 CE VERTICAL TAIL MISSING E DJFA K NONE O OTHER IN INSP/MAINT 1 EA 23 710TA RK183 DURING A PHASE 1 INSPECTION IT WAS FOUND THAT THE VERTICAL TAIL NAVIGATION LIGHT ASSY WAS MISSING. THE CAP ASSY AND TAI L NAV LIGHT ASSY WERE REPLACED. (K) 2 H 7 2 4F RT A16SW 20080728 EU 2008 7 28 UPS08152593 1 20080613 A 5321 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 152UP 0835 INSPECTION TYPE:5YR MAIN CARGO COMPARTMENT FLOOR PNL 251KG HAS TEMP REPAIR. REMOVED TEMP REPAIR AND REPAIRED MAIN CARGO COMPARTMENT FLOOR PNL IAW A300 SRM 53-10-20 TABLE 201 PAR 8A. 2 L 7 2 4F RT A35EU 20080728 NM 2008 7 28 2008UALA03417 1 20080617 A 3350 BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 816UA 871 ON EMERGENCY LIGHT TEST, FAULT KEEPS COMING UP EPSU BATT AFT L. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 EA 2008 7 28 TRAX200800892 1 20080707 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 DOOR HANDLE RELEASE BUTTON ON SERVICE LUBE DOOR HANDLE IAW AMM 52-00 AC OK FOR SERVICE (B) 2 L 7 2 4F RT A21EA 20080728 EU 2008 7 28 2008UALA03182 1 20080603 A 5210 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 460UA 1248 NR 2R DOOR ASSIST BOTTLE WILL NOT HOLD AIR. FOUND BOTTLE EMPTY. FOUND LEAKING AT O-RING FOR SCHRADER VALVE. REPLACED SCHRADRER VALVE AND PACKINGS, RESERVICED BOTTLE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 NM 2008 7 28 2008UALA03490 1 20080620 A 5320 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 811UA 847 DOOR 2L,CREW DOOR SILL BEAM FOUND CORRODED ON UPPER INBOARDD FLANGE AROUND 2EA NUT PLATE HOLES JUST FWD OF FR68. ACCOMP LISHED MAJOR REPAIR AT DEN--REMOVED CORROSION, REF SRM -53-41-14 AND REPLACED NUT PLATES. 2 L 7 2 4F 4 F RT A28NM E40NE 20080815 NM 2008 8 15 UPS08M52846 1 20080517 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR1 FOUND CORRODED EXISTING SLEEVE BUSHING REMOVED IAW EO MD11-551 0-19409M. CORROSION AT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.549" DIA, REMAINING BLEND OUT 0.050" DEE P, BOTTOM SURFACE CLEANED & REMAINING MAT'L THK CHK MIN. 0.290" THICK. BORE FOUND EXCEEDING LIMITS IAW EO. REPAIRED B/N BO RE NR 01RH WAS ACCOMP IAW EN 1186-08 & IS ACCEPT IAW EO MD11-5510-30008A. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 UPS08852767 1 20080715 A 2121 FAN DOUG DC8 DC871F 302199D WP COCKPIT SMOKE A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 755UP 46055 LT PACK FAN FAILED ON TAXI OUT CAUSING SMOKE IN COCKPIT AND PACK TO NOT OPERATE. PACK TRIP LIGHT CAME ON, PLACED ON MEL 21-42. CONTROL M380173 PLACARD INSTALLED. 2 L 7 4 4F RT 4A25 20080815 NM 2008 8 15 UPS08M52760 1 20080715 A 2560 GIRT BAR DOUG MD11 MD11F 3023600 NM L1 DOOR INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 L1 DOOR WILL NOT CLOSE. NEED CLOSING LP NR. MX ADJUSTED THE GIRT BAR AND THE DOOR OPS CHECKED GOOD. 2 L 7 3 4F RT A22WE 20080815 2008 8 15 UPS08852796 4 20080720 A 2565 GAUGE DOUG DC8 DC871F 302199D WP L1 DOOR SLIDE WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 ENTRY DOOR EMERGENCY ESCAPE SLIDE NEED TO BE REPOSITIONED IN ORDER TO READ THE GAUGE FOR BOTTLE AIR PRESSURE. REMOVED L 1 EMERGENCY ESCAPE SLIDE. INSTALLED ADDITIONAL SUPPORT BLOCKS IN L1 EMERGENCY SLIDE CONTAINER REF BLUEPRINT AND INSTALL ED ON L1 DOOR IAW MM 25-60-01-2. 2 L 7 4 4F RT 4A25 20080815 NM 2008 8 15 UPS08M52844 1 20080527 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 8 FOUND CORRODED CORROSION REMOVED AT BARREL NUT BORE IAW SRM 5 1-21-01 VII REV 35. BORE REAM TO 0.988" DIA REMAINING BLEND OUT 0.095" DEEP, BOTTOM SURFACE CLEANED. BORE BLEND OUT FOU ND EXCEEDING LIMITS IAW EO MD11-5510-19409M.10X MAGNIFICATION DVI C/O & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT BORE NR8 RH WAS ACCOMP IAW EN 1237-08 & IS ACCEPTABLE IAW MD11-5510-30010A. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52845 1 20080524 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, LT HORIZ STAB BARREL NUT BORE NR33 FOUND CORRODED CORROSION AT BARREL NUT BORE REMOVED IAW SRM 5 1-21-01 VII REV 35. BORE REAM TO 1.178" DIA, REMAINING SIDEWALL BLEND OUT 0.020" DEEP, BOTTOM SURFACE REMAINING BLEND OU T 0.065" DEEP, BLEND OUT AT BORE FOUND EXCEEDING LIMITS IAW EO MD11-5510-19409M. REPAIRED BARREL NUT BORE NR 33 LT WAS ACCOMP LISHED IAW EN 1222-08 & IS ACCEPTABLE IAW EO MD11-5510-29972-A. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52856 1 20080602 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 16 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.067"DIA, REMAINING BLEND OUT 0.068" DEEP, BOTTOM SURFACE CLEAN & BORE BLEND OUT, EX CEEDED LIMITS IAW EO MD11-5510-19409M.10X MAGN DVI C/O & FOUND NO CORROSION EVIDENT. REPAIR BARREL NUT BORE NR 16 RT WA S ACCOMPLISHED IAW EN1246-08 & IS ACCEPTABLE IAW EO MD11-5510-30011A. 2 L 7 3 4F RT A22WE 20080818 WP 2008 8 18 UPS08852738 1 20080701 A 5311 FRAME DOUG DC8 DC871F 302199D WP FS 702-875 L21L GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, GOUGE ON THE STA 702.875 LT FRAME JUST ABOVE THE UPPER SURFACE OF CUSP EXTRUSION(LONGERON 210 IN MA IN CABIN). DRILLED HOLE TO REMOVE DAMAGE AND PLUGGED HOLE. IAW SRM 53-02-00 FIG 0 01F. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852739 1 20080701 A 5311 FRAME DOUG DC8 DC871F 302199D WP FS 360 L21L GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, GOUGE ON THE STA 360 LT FRAME JUST ABOVE THE UPPER SURFACE OF THE L21. REPAIRED GOUGE IAW SRM 53-0 2-00-0 FIG 001F. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852741 1 20080701 A 5340 577384444 STRINGER CLIP DOUG DC8 DC871F 302199D WP FS 1766 L6R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, L6R ATTACH CLIP CRACKED AT APB, STA 1766, MAIN CABIN. REMOVED, FABRICATED AND INSTALLED REPLACE MENT CLIP IAW DWG 5773844 AND 5191-20D. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852743 1 20080630 A 5347 3657502U507 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2 CAPT BOTH LT AND RT SEAT TRACKS HAVE ELONGATED HOLES. REMOVED AND REPLACED CAPT'S LT AND RT SEAT TR ACKS IAW SRM 51-01-24 AN AND 51-01-20D. 2 L 7 4 4F RT 4A25 20080818 NM 2008 8 18 UPS08652726 1 20080702 A 5330 143T31213 SKIN BOEING 767 76734AF 1385212 NM BS 559 S4R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 301UP 27239 INSPECTION TYPE-C, FX RT UPPER FUSELAGE BS 559 S4R SKIN EXTERNAL SURFACE DENT TO REPAIRED PATCH AREA. BS 553 TO 568 S3 -4R TO S6R AREA APPROX SKIN REPAIRED IAW RS R53-31-36027. THIS REPAIR CLASSIFY AS CAT B WITH THE ADDITIONAL INSPECTION I AW RS R53-31-36027 AND UPS EO B767-5310-29926-A. 2 L 7 2 4F RT A1NM 20080818 NM 2008 8 18 UPS08652642 1 20080707 A 5210 PANEL BOEING 767 76734AF 1385212 NM L1 DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 L1 DOOR SIDE BUMPER AND SIDE PANEL DAMAGED. REMOVED INTERIOR PANEL FOR CREW ENTRY DOOR HANDLE AND SENT TO SM. REPAIRED S IDEWALL PANEL REF 767 AMM 25 00 00 08. 2 L 7 2 4F RT A1NM 20080818 EU 2008 8 18 UPS08152684 1 20080708 A 2133 OUTFLOW VALVE AIRBUS 300 A300B4622R 3930312 EU CABIN PRESSURE FAILED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 121UP 0806 AFTER T/O AT 1,000', PRESSURE REGULATOR NR1 FAILED. REMOVED AND REPLACED FWD CABIN PRESSURE OUTFLOW VALVE IAW MM 21-31- 12-04. 2 L 7 2 4F RT A35EU 20080818 WP 2008 8 18 UPS08852634 1 20080611 A 5330 SKIN DOUG DC8 DC871F 302199D WP FS 1704 L28L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, FOUND 1.0 CRACK AT BS 1704 L28L NEED APPX "D" TO REPAIR IAW SRO DWG NR SRO8530032. CUTOUT DAMAGED A REA IAW SRO 8530032. FABRICATED AND INSTALLED REPAIR DOUBLER/REPAIR PARTS IAW SRO 8530032. 2 L 7 4 4F RT 4A25 20080818 2008 8 18 UPS08M52626 4 20080701 A 2210 AUTOPILOT SYS DOUG MD11 MD11F 3023600 NM FAILED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 278UP 48577 BOTH AUTOPILOTS FAILED IN FLIGHT. FOUND HARD FAULT ON LT OB AILERON MOD LVDT. REPLACED TRANSDUCER IAW MM 27-13-34-4. AC COMPLISHED AUTOPILOT RTS FOR FCC 2. NO FAULTS FOUND. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 UPS08552929 1 20080720 A 5753 SKIN BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE RT WING TE FLAP DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 430UP 25461 INSPECTION TYPE-C, RT IB MAIN FLAP UPPER SURFACE JUST OB OF AFT FLAP HAS MULTIPLE SMALL DENTS. MEASURED ALL DENTS ON R T IB FLAP UPPER SURFACE IAW SRM 57-53-01- 1A, DETAIL VII, FOUND (1EA) DENT AT GRID LOCATION "J5" TO BE OUT OF LIMITS. M EASUREMENT FOR THE DENTS WAS W=.700, DEPTH=.026/ THE A RATIO IS .700/.026=26.923; DAMAGE IS LESS THAN 30. 2. SANDED AND PREPED ONE DENT, THAT IS OUT OF LIMITS, FILLED DAMAGED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080818 WP 2008 8 18 UPS08852949 1 20080729 A 5240 SKIN DOUG DC8 DC871F 302199D WP SERVICE DOOR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C1 GOUGE ON INNER SKIN OF RT CTR SERVICE DOOR JUST ABOVE BAYONET. FABRICATED AND INSTALLED REPAIR DOUBL ER IAW SRM 52-03-00 AND 51-01-21- 0 FIG 033. 2 L 7 4 4F RT 4A25 20080818 NM 2008 8 18 UPS08552985 1 20080801 A 2130 SELECTOR BOEING 757 75724APF 1384969 NM CABIN PRESSURE INOPERATIVE A IPXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 01 404UP 23726 EICAS MSG CABIN ALTITUDE DISPLAYED, CABIN ALT AND CABIN ALTITUDE LIGHTS ILLUMINATED UNABLE TO RESTORE PRESSURE USING MAN UAL MODE. OUTFLOW VALVE INDICATED FULLLY CLOSED. CABIN RTAE OF CLIMB FLUCTUATED WILDLY. CREW DONNED 02 MASKS. R/R CABIN PRESSURE SELECTOR IAW 21-31-01-4. OPS NORMAL. ACCOMPLISHED PRESS CONTROLLER BITE FIM 21-30-00 FIG 103. NO FAULTS. ALSO A CCOMPLISHED FIG 109. PRESSURIZED A/C CHECKED FOR LEAKS. CHECKS GOOD. 2 L 7 2 4F RT A2NM 20080818 NM 2008 8 18 SWAA084022 1 20080718 A 5230 STRUCTURE BOEING 737 7373H4 1384600 NM CARGO DOOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 002596378 26585 DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CREASED AT FWD END. R&R CARGO DOOR PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084064 1 20080721 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 449WN 32469 DURING SCHEDULED HC1 CHECK, RH MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084047 1 20080721 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 727E S2L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED A TBS 727E, STR 2L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084076 1 20080722 A 3350 20131A BATTERY PACK BOEING 737 7373K2 13844BA NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED SPV CHECK, FOUND MID CABIN EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK AND BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084086 1 20080722 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM BS 727D S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084080 1 20080722 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084081 1 20080722 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 616 S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 5L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084082 1 20080722 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 727D S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084097 1 20080723 A 5311 6546526 FRAME BOEING 737 7373Q8 1384670 NM BS 400 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084073 1 20080720 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 741SA 29277 R2 DOOR EMERGENCY EXIT LIGHT INOP. R&R LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080818 2008 8 18 SWAA084107 4 20080724 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 259WN 35554 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084099 1 20080722 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM BS 736E S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 736E, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080818 2008 8 18 SWAA084110 4 20080723 A 2565 1061323433 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. R&R EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084125 1 20080724 A 5754 SKIN BOEING 737 7373H4 1384600 NM RT WING SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND RH WING NR 6 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084124 1 20080724 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND RH AFT CABIN EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084115 1 20080724 A 3350 767 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 472WN 33831 DURING SCHEDULED MV2 CHECK, FOUND RH AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. R&R LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080818 2008 8 18 SWAA084116 4 20080724 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084104 1 20080724 A 5315 6545815 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 344, RBL 12 TO LBL 12. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 UPS08M53018 1 20080710 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 29 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INS TALLED BUSHING IAW E.O. MD11-5510-19409-N AND SAA TRAVELER 80538330001. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 USAA920081462 1 20080722 A 5347 D53112827202 DUMMY RAIL AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803AW 0931 SAL-C7-MAJOR REPAIR - DUMMY RAIL CORRODED AT BS FR16 BL Y503. REPLACED DUMMY RAIL AT BS FR16 BL Y503 IAW A319 SRM 57-72 -11. (S) 2 L 7 2 4F RT A28NM 20080819 EA 2008 8 19 SWIA200819923 1 20080731 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 919SW 7657 F/A REPORTS AN EMERGENCY LIGHT POD IS INOPERATIVE. (FLIGHT NR 5946) RELAMPED LIGHT IAW AMM 33-51-16. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 20080819 NM 2008 8 19 USAA920081467 1 20080722 A 5320 D53480019217 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803AW 0931 SAL-C7-MAJOR REPAIR - CRACKED TRAY PLATE AT FR68 TO FR69, -Y1738. REPLACED -TRAY PLATE AT FR68 TO FR69, -Y1738 IAW A319 SRN 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080819 EA 2008 8 19 SWIA200819900 1 20080724 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002C10 1390015 EA CARGO BAY FAILED A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 611SK 10035 "FIRE SYS FAULT" STATUS MESSAGE APPEARED. (FLIGHT NR 3882) REPLACED AFT CARGO SMOKE DETECTOR 2 IAW AMM 26-15-01. OPS C HECK GOOD. 2 L 7 2 4F RT A21EA 20080819 EA 2008 8 19 SWIA200819912 1 20080726 A 3310 HOLDER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT SHORTED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 986SW 7967 F/O`S CHART HOLDER SHORTED OUT. (FLIGHT NR 6438) SECURED HARDWARE ON CHART HOLDER. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080819 EA 2008 8 19 SWIA200819790 1 20080619 A 7830 1267587 DRIVE UNIT CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER FAULTY A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 464SW 70 70 7827 REVERSER UNLOCKED CAUTION MESSAGE. (FLIGHT NR 3881) REPLACED THE RT THRUST REVERSER PDU IAW 78-30-01. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 20080819 NE 2008 8 19 SWIA200819791 2 20080622 A 7200 ENGINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE LT ENGINE VIBRATION A SWIA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 NM 07 776SK 10241 N1 VIBRATION ADVANCED TO YELLOW ARC ON LT ENGINE. PEFORMED PRECAUTIONARY SHUTDOWN AND DIVERTED TO MSP. (FLIGHT NR 6126 ) INSPECTED FAN BLADES AND RAN ENGINE IAW MM 72-00-00. ALL INDICATIONS NORMAL. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080819 EA 2008 8 19 SWIA200819792 1 20080619 A 3210 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 408SW 7055 NOSE GEAR WOULD NOT EXTEND AND RECEIVED A GEAR DISAGREE MESSAGE. RECYCLED GEAR HANDLE AND THE NOSE GEAR EXTENDED CORREC TLY. (FLIGHT NR 4048) INSPECTED AND SWUNG GEAR SEVERAL TIMES IAW MM 32-30-00. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 20080819 NM 2008 8 19 UPS08M53045 1 20080717 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 7 RT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED AND INSTALLED REPAI R BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M53046 1 20080718 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR12 LT BARREL NUT BORE HOLE REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080728 EA 2008 7 28 TRAX200800688 1 20080526 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 924EV 7830 SUPPORT ANGLES AT FS 280, LBL 9, INBD AND OTBD ARE CRACKED. REMOVED BOTH I/B AND O/B SUPPORT ANGLES AT FS 280 LBL 9 IAW SRM 51-42-06 AND 51-42-21. LOCATED AND STARTED TO INSTALL BOTH I/B AND O/B SUPPORT ANGLES AT FS 280 LBL 9 IAW SRM 51-4 2-06 AND 51-42-21. COMPLETED INSTALLATION IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 A6WA200840429 1 20080430 A 5220 H341933 HANDLE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH CORRODED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 437AW 12579 7744 CREW ESCAPE HATCH OUTSIDE HANDLE IS SEIZED AND CORRODED. CREW ESCAPE HATCH HANDLE REPLACED IAW CRJ 200 AMM 52-22-03-400 -801 AND HARTWELL CMM 52-22-03. (A) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 AALA200801321 1 20080515 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 792AN 30253 MIA EMERGENCY LIGHT AT SEAT 34G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 34G. SYSTEM GROUND CHECKED NOR MAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 EA 2008 7 28 TRAX200800655 1 20080518 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 907EV 7648 RT SIDE FS 464 FLOOR SUPPORT INTERCOSTAL HAS A CRACKED FLANGE ON THE I/B SIDE OF RBL 36 AND A CRACKED ATTACH ANGLE ON TH E O/B SIDE OF RBL 27. DISCONNECTED MOUNT BOLTS ON CABLE GUIDE IAW 51-41-04. REPAIRED RT SIDE FS 484 INTERCOSTAL I/B OF RBL 36 AND O/B SIDE OF RBL 27 IAW REO 601R-53-41-059. INSTALLED SAME SERVICEABLE MOUNT BOLTS ON CABLE GUIDE IAW SRM 51- 41-04. PERFORMED LEAK CHECK OF THE RT SIDE FS 484 FLOOR SUPPORT INTERCOSTAL RBL 36 AND O/B RBL 27 IAW AMM 21-32-00-863-8 01. NO LEAKS NOTED AT THIS TIME. REPAIRED RT SIDE F.S. 484 FLOOR SUPPORT INTERCOSTAL IAW REO 601R-53-41-059 AND REO 60 1R-53-41-059. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800662 1 20080519 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 929EV 8007 FS 484 RIGHT INTERCOSTAL CLIP IS CRACKED 1/4" BL27.00 O/B. REPAIRED INTERCOSTAL CLIP AT FS 484 AT RBL 36.00 IAW REO 601 R-53-41-059 AND REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 KCSA081298 1 20080625 A 5311 FRAME BOEING 747 747122 1384872 NM BS1319 LBL120 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STA-1319 LBL-120 LOWER FRAME TO LONGERON SUPPORT CRACKED 1" (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 KCSA081306 1 20080702 A 5711 SPAR CAP BOEING 747 747122 1384872 NM RT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 R/H WING REAR SPAR TOP CHORD IS CORRODED ON UPPER SURFACE AT WBL 460 (B) 2 L 7 4 4F RT A20WE 20080728 2008 7 28 DXTA200803099 2 20080606 A 7320 EEC CESSNA 560 560XL 2076702 CE LT ENGINE MALFUNCTIONED E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 624QS 5605302 LT EEC FAILED DURING TO ROLL. (B) 2 L 7 2 4F RT A22CE 20080728 NM 2008 7 28 KCSA081310 1 20080705 A 5320 STRAP BOEING 747 747246B 1384864 NM BS1860-1880 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 AFT BILGE FUSELAGE TENSION STRAP IS CRACKED AT STA. 1860 TO 1880, STR 37L. (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 KCSA081309 1 20080702 A 5347 SEAT TRACK BOEING 747 747246B 1384864 NM BS 570 RBL 23 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 STA-570 RBL-23 SEAT TRACK CRACKED .5" (B) 2 L 7 4 4F RT A20WE 20080728 EA 2008 7 28 TRAX200800616 1 20080510 A 5530 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 707EV 10057 VERTICAL STAB LOWER LT DRAG ANGLE IS CRACKED CUT AWAY DAMAGE FROM VERTICAL STAB LOWER LT DRAG ANGLE IAW REO 670-53-31-0 18. INSTALLED DOBLER AND FILLER, FILLET SEAL REPAIR PARTS AND FINAL PAINT AND LT DRAG ANGLE. ALL WORK DONE IAW REO 670- 53-31-018. (B) 2 L 7 2 4F RT A21EA 20080728 WP 2008 7 28 AALA200801337 1 20080518 A 2822 3980001 PUMP DOUG DC9 DC982 3022082 WP FUEL SYSTEM ACTIVATED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 487AA 49680 ATL INFLIGHT T2233/18MAY RSW TO STL. CENTER FORWARD FUEL BOOST PUMP POPPED CIRCUIT BREAKER. LANDED ATL WITHOUT INCIDEN T. REPLACED CENTER FORWARD FUEL BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F A6WE 20080728 EA 2008 7 28 TRAX200800748 1 20080604 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 379-477 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 LT CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE FS 379.00 TO FS 477.00. REMOVED SEAT RAIL ASSY INSPECTED AND FOUND CORR OSION UNDER SEAT RAIL. PREPPED, PRIMED AND PAINTED AREA ON FUSELAGE SKIN IAW SRM 53-00-49. REPLACED SEAT RAIL AT FLOOR S TATION 379.00 TO 477.00 IAW AMM 53-00-49. (B) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800672 1 20080519 A 5210 MECHANISM CNDAIR CL600 CL6002B19 1900309 EA DOOR HANDLE LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 PAX DOOR VERY DIFFICULT TO OPEN AND CLOSE. LUBRICATED PAX DOOR LATCH MECHANISM, OPS CHECK GOOD IAW CRJ-200 AMM 52-11-02. ---[SDR CLOSED](B) 2 L 7 2 4F RT A21EA 20080728 WP 2008 7 28 AALA200801350 1 20080519 A 2410 CSD DOUG DC9 DC983 3022083 WP NR 1 ENGINE FAILED A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 SW 21 9681B 53631 ONT INFLIGHT T1419/19MAY STL TO LAS. NUMBER ONE ENGINE CONSTANT SPEED DRIVE OIL PRESSURE LOW INDICATION DURING FLIGHT. L ANDED ONT WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE CONSTANT SPEED DRIVE AND CONSTANT SPEED DRIVE AIR/OIL HEAT EXCHAN GER. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A6WE 20080728 NM 2008 7 28 USAA920081249 1 20080619 A 3350 20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 504AU 23379 FLT 1129 - CLT - EEL - AFT RT EMERGENCY LIGHT OVER AFT RT DOOR WILL NOT ILLUMINATE. MX REPLACED THE BATTERY PACK. OPER ATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A16WE 20080819 SO 2008 8 19 SWIA200819893 1 20080709 A 5315 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FLOORBEAM CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 563SW 120338 BUTT STRAP AT PAX DOOR ENTRANCE HAS SIGNS EXFOLIATION. (FOUND AT C-CHECK) REPLACED BUTT STRAP AT PAX DOOR ENTRANCE IAW SRM 51-10-02. 2 L 7 2 4T RT A31SO 20080815 WP 2008 8 15 08FDEA03022 1 20080722 A 5414 AUB710817 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 NR 1 PYLON PANEL 437 FR IS CHAFED AT FASTENER HOLES. NR 1 PYLON PANEL 437 FR WAS CHAFED BEYOND ALLOWABLE LIMITS REQUIRE D SRM REPAIR IAW DC/MD-10 SRM 54-00-01, VOL I. MATERIAL ID FOR SRM REPAIR 2024-T3, 0.071, PO 614899.4 IAW DC/MD-10 SRM 54-51-02, VOL III. FABRICATED REPAIR IAW DC/MD-10 SRM 54-00- 01, VOL I. ALODINE AND PRIMED REPAIR DOUBLER IAW DC/MD-10 DRM 51-21-01, VOL II. INSTALLED REPAIR IAW DC/MD-10 SRM 51-31-01, VOL II. UT GAUGE USED T8225P. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 08FDEA03076 1 20080725 A 5755 SKIN DOUG DOUG MD10 MD1010F 3022112 WP NR 2 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 THE RIGHT WING NR 2 SPOILER IS DELAMINATED ON THE LOWER SURFACE AT THE OUTBOARD CORNER. REMOVED NR 2 RT WING SPOILER IA W AMM 27-60-01-4. REPAIRED BY REMOVING DELAMINATED LOWER SKIN; DOUBLER & CORE. FABRICATED & BONDED A NEW LOWER SKIN ; DOUBLER & CORE IAW SRM 57-10-00; VOL I & DWG ARC 1347. INSTALLED THE HARDWARE & SEALS IAW SRM 51-31-01 & 57-10-00 ; VOL I. SEALED & PAINTED SPOILER IAW SRM 51-41-01; VOL II & SRM 51-21-02; VOL II. RE-INSTALLED NR 2 RT WING SPOILER PER AMM 27-60-01-4. GAP & OPS CHECKS GOOD PER AMM 27-60-01-4 & 27-60-01-6. 2 L 7 3 4F RT A22WE 20080815 EU 2008 8 15 08FDEA02490 1 20080626 A 5315 A53974219220 FLOORBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 AFT CARGO COMPARTMENT FLOORBEAM UPPER CHORD ALONG FR 63 LBL60 (153CM) WITH EXFOLIATION CORROSION. REMOVED THE RELATED B ALL MAT TRAY PER AMM 25-52-22-4. CUT OUT AND REMOVED DAMAGED CROSSBEAM SECTION PER SRM 51-27-00. FABRICATED THE REPAIR PARTS PER SRM 53-10-15. DRILLED FASTENER HOLES TO THE REPAIR PART PER SRM 53-10-15. APPLIED ALODINE PER SRM 51-21-00. APPLIED PRIMER AND TOPCOAT TO THE REPAIR PARTS PER SRM 51-23-00. INSTALLED REPAIR PARTS PER SRM 51-40-21. RESTORED F INISH PER SRM 51-75-10. APPLIED CORROSION PREVENTIVE COMPOUND PER AMM 51-22-00. INSTALLED THE BALL MAT TRAY PER AMM 25 -52-22-4. 2 L 7 2 4F RT A35EU 20080815 WP 2008 8 15 08FDEA02765 1 20080708 A 5730 ARB124911 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING FIXED L/E INTERNAL STA XFS 664 AT THE RIB, TOP STRAP IS CRACKED. REMOVED RIB TO FOM, REMOVED DOUBLER SPLICE. MATERIAL ID FOR A DOUBLER SPLICE 7075-0, 0.071, PO 620987.4 IAW DAC DWG ARB 1249; REV AA. FABRICATED A NEW DOUBLER SPL ICE IAW DAC DWG 1249-11. HT IAW TPS 1003, REV A, LOAD NR HT071408.1. LOCATED AND DRILLED HOLES IAW DC/MD-10 SRM 51-33 -01, VOL II. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01, PGS 21 AND 24, VOL II. INSTALLED NEW DOUBLER SPLICE AND RI B IAW DC/MD-10 SRM 51-33-01, VOL II. PART MARKED IAW FEDEX GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08652870 1 20080716 A 5320 141T52822 STIFFENER BOEING 767 76734AF 1385212 NM FLOORBEAM CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 303UP 27241 INSPECTION TYPE-C, MEC STA 246 LBL 25" FLOORBEAM SUPPORT STIFFENER CRACKED (CRACK LENGTH .3750" APPROX). FX MEC STA 24 6 LBL 25" FLOORBEAM SUPPORT STIFFENER REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20080815 NM 2008 8 15 UPS08B52894 1 20080624 A 5730 SKIN BOEING 747 747400 13848AT NM RT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 572UP INSPECTION TYPE-C2, DRILL START IN LOWER SKIN OF RT WING OB, L/E, NEXT TO A RIVET, FWD AND IB OF 3RD. PANEL FROM OB END CUT OUT DAMAGE, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM, 51-1-8, 5 1-1-21, 51-2-0 FIG.7, 2 L 7 4 4F RT A20WE 20080815 NM 2008 8 15 UPS08M52889 1 20080516 A 5753 HINGE DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, LT WING OB FLAP IB AFT HINGE UPPER MOUNTING FOUND 06EA BORE RUSTY. LT AFT OB FLAP IB HINGE UPPER MO UNTING IB SIDE BORES(03EA) & OB SIDE BORES (03EA) CORROSION REMOVED IAW BSOPM20-11-02 REV 61.FPI C/O IAW DAC NDT SPM REV 13 PT 08 ON REWORKED AREA & FOUND NO CRACK & NO CORROSION EVIDENT. REWORKED BORES(05EA) REAMED IAW EN1288-08. BUSHING (05EA) FAB AND INSTALLEDIAW EN 1288-08. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08652871 1 20080716 A 5315 141T514616 STIFFENER BOEING 767 76734AF 1385212 NM FLOORBEAM CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 303UP 27241 INSPECTION TYPE:C FX MEC STA 246 LBL 50" FLOORBEAM SUPPORT STIFFENER CRACKED (CRACK LENGTH .5" APPROX) FX MEC STA 24 6 LBL 50" FLOORBEAM SUPPORT STIFFENER REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 2 L 7 2 4F RT A1NM 20080815 NM 2008 8 15 UPS08652862 1 20080716 A 5315 STIFFENER BOEING 767 76734AF 1385212 NM FLOORBEAM CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 303UP 27241 FX MEC STA 246 LBL 40", FLOORBEAM SUPPORT STIFFENER CRACK. (CRACK LENGTH 1/2" APPROX). FX MEC STA 246 LBL 40" FLOORBEAM SUPPORT STIFFENER REPAIR AS IAW SRM 53-10-51-2R 4 FIG 201 THIS REPAIR IS A CATEGORY 'B' REPAIR. REPEAT INSPECTION IS R EQUIRED IAW SRM 53-10-51-2R 4 FIG 201 TABLE II AT THE INTERNAL 3000 FLT CYC OR 24 MONTHS WHICH EVER OCCURS FIRST. (REF U PS MPI NR 19787) 2 L 7 2 4F RT A1NM 20080815 NM 2008 8 15 UPS08652868 1 20080715 A 5720 114T2300293 WEB BOEING 767 76734AF 1385212 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 303UP 27241 LT WING L/E STA 525 FWD NOSE BEAM WEB LT WING AREA CRACK. (CRACK LENGTH .7500" APPROX). LT WING L/E FWD NOSE BEAM WEB R EPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 JUST BETWEEN OSS 499.6, AND OSS 565.9 REF HX NRC NR 50462 FOR WO RKING DETAIL. 2 L 7 2 4F RT A1NM 20080815 NM 2008 8 15 UPS08652869 1 20080717 A 5720 114T2300272 WEB BOEING 767 76734AF 1385212 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 303UP 27241 RT WING L/E NOSE BEAM LOWER SUPPORT WEB FOUND CRACKED AT ILS 676 (CRACK LENGTH 1.25") RT WING L/E NOSE BEAM SUPPORT WE B REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 JUST BETWEEN OSS 648 AND OSS 694. 2 L 7 2 4F RT A1NM 20080815 NM 2008 8 15 UPS08M52847 1 20080518 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT HORIZONTAL STABILIZER BARREL NUT BORE NR27 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35.BORE REAM TO 1.178" DIA,REMAINING BLEND OUT 0.025" DEEP, BOTTOM REMAINING BLEND OUT 0.055" D EEP. BORE BLEND OUT FOUND EXCEEDING LIMITS IAW EO MD11-551 0-19409M. 10X MAG DVI C/O & FOUND NO CORROSION EVIDENT. REP AIRED B/N BO RE NR 27RH WAS ACCOMP IAW EN1209-08 & IS ACCEPT IAW EO MD11-5510-30012A. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08552882 1 20080716 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 1560 S26L DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 421UP 25281 INSPECTION TYPE-C2, DENT IN FRAME INNER FLANGE STA 1560 STR26L. REPAIR IAW SRM 53-00-07-2R5 MPI NR P19803. 2 L 7 2 4F RT A2NM 20080815 NM 2008 8 15 UPS08552883 1 20080716 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 1500 S25-26R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 421UP 25281 INSPECTION TYPE-C2, AFT CARGO BAY DENT IN FRAME INNER FLANGE STA 1500 BETWEEN STR25R-26R. REPAIRED IAW SRM 53-00-07-2R5 MPI # P19802. 2 L 7 2 4F RT A2NM 20080818 NM 2008 8 18 UPS08552874 1 20080716 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM BS 1510 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 421UP 25281 INSPECTION TYPE-C2, CORROSION AFT CARGO BAY FLOORBEAM ST 1510, RBL 7. REMOVE AND REPLACED AFT CARGO BAY FLOORBEAM BS 1 510, RBL 7. 2 L 7 2 4F RT A2NM 20080728 2008 7 28 USAAEMB08007 4 20080705 A 2565 SLIDE EMB ERJ190 ERJ190100IGW 3260408 NM L1 DOOR DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 945UW 19000062 PHL - WHILE AT THE GATE THE L1 EMERGENCY SLIDE FELL OFF BUSTLE AND RESTED ON THE JETWAY DUE TO STITCHING ON THE SLIDE TH AT GAVE WAY. MAINTENANCE REMOVED AND REPLACED THE SLIDE. (S) 2 L 7 2 4F RT A57NM 20080728 NM 2008 7 28 F3LA200800356 1 20080617 A 5321 D5367204500000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 REFERENCE NON ROUTINE 34659. DURING C3 S1 C CHECK INSPECTION NOTED SEVERAL LARGE DENTS ON IPPER SURFACE OF BULK CARGO FL OOR PANEL 161CF. MAINTENANCE REPAIRED PANEL 161CF IN ACCORDANCE WITH SRM 53-02-00 REPAIR 204. UPON COMPLETION OF THE R EPAIR IT WAS INSPECTED AND FOUND ACCETABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080728 EA 2008 7 28 A6WA200840415 1 20080512 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 442AW 7778 PAX DOOR AFT DRAG ANGLE CRACK. PAX DOOR DRAG ANGLE REPAIRED IAW REO 601R-53-11-513 REV A. 2 L 7 2 4F RT A21EA 20080728 2008 7 28 ASAA0853173 4 20080710 A 2310 8220990004 TRANSCEIVER BOEING 737 737890 1384527 NM GE CF34 CF34* 30015 NE HF COMM MALFUNCTIONED A ASAA O OTHER O OTHER CR CRUISE 1 NM 02 559AS 223 35178 HF 2 WORKED NORMALLY FOR FIRST 3 HRS, IT THEN QUIT TRANSMITTING BUT WILL RECEIVE. PERFORMED HF COMM NR 2 SYSTEM OPERATI ONAL TEST LRU BITE W GREEN NO FAULTS. PERFORMED NR 1 & 2 HF COMM SYSTEM TEST REF 23 11 00 VOICE COMMUNICATION WITH SAN FRAN GOOD XMIT AND RECEIVE. PRECAUTIONARY REPLACED NR 2 HF TRANSCEIVER REF 22 11 21. 2 L 7 2 4F 4 F RT A16WE 20080728 NM 2008 7 28 ASAA0843113 1 20080506 A 5315 654681179 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 FLOORBEAM UPPER FLANGE CORRODED. REPLACED BEAM PER EA 5310 02800. 2 L 7 2 4F RT A16WE 20080728 SO 2008 7 28 RAIA00806005 1 20080610 A 5210 UNKNOWN EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 851HK 145340 FLT 8066 - RIC - CABIN DOOR HARD TO OPEN. MAINTENANCE LUBED MAIN CABIN DOOR, AND OPS CHECK GOOD. (S) 2 L 7 2 4T RT T00011AT 20080728 SO 2008 7 28 RAIA00806014 1 20080614 A 3260 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO NLG OUT OF ADJUST A RAIA O OTHER O OTHER CL CLIMB 1 CE 03 852HK FLT 7936-IAD - LANDING GEAR DID NOT RETRACT FOLLOWING TAKEOFF. MAINTENANCE FOUND THE NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SENSOR OUT OF ADJUSTMENT. THE SENSOR WAS ADJUSTED AND SEVERAL GEAR EXTENSIONS AND RETRACTIONS WERE PERFORMED WITH NO ADDITIONAL DEFECTS NOTED. (S) 2 L 7 2 4T RT T00011AT 20080728 SO 2008 7 28 RAIA00806015 1 20080618 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 840HK 145341 PRE FLT 7945 - SGF - RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE CLEANED AND RESEATED THE EMERGENCY LIGHT CONNECTOR. OPERATIONAL CHECKED GOOD. (S) 2 L 7 2 4T RT T00011AT 20080728 SO 2008 7 28 RAIA00806002 1 20080608 A 3297 CONNECTOR EMB 145 EMB145EP 3260221 SO NLG DIRTY A RAIA O OTHER O OTHER CL CLIMB 1 CE 03 826HK 145016 FLT 5515 - STL - RETURN FROM FLIGHT - NOSE GEAR DID NOT RETACT WITH GEAR HANDLE SELECTED UP. MAINTENANCE CLEANED UPLOCK PROX SWITCH CONNECTORS. (S) 2 L 7 2 4F RT T00011AT 20080728 EA 2008 7 28 REX2008F00002 1 20080628 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A REXA K NONE J WARNING INDICATION CR CRUISE 1 SO 25 8631E 12734 11994 7631 FLAP FAIL MESSAGE DURING CRUISE, QRH FOLLOWED, EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. FLAP SYSTEM RESET PER BOMB ARDIER FIM AND PLACED ON 72 HOUR WATCH. THE 72 HOUR WATCH PERIOD CLEARED BY REMOVING AND REPLACING THE RT BRAKE POSITIO N SENSING UNIT (BPSU) IAW BOMBARDIER AMM. (S) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 REX2008F00001 1 20080625 A 3250 STEERING SYS CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF RIG A REXA K NONE J WARNING INDICATION AP APPROACH 1 SO 25 8836A 7836 NOSE WHEEL STEERING INOPERATIVE MESSAGE ON APPROACH. QRH FOLLOWED MESSAGE REMAINED. LANDING UNEVENTFUL. NOSE WHEEL ST EERING SYSTEM RIGGED PER BOMBARDIER AMM 32-51-01. (S) 2 L 7 2 4F RT A21EA 20080728 2008 7 28 2008UALA03352 4 20080612 A 2565 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR OBSTRUCTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 585UA 26709 THE 1R DOOR WILL NOT ARM. DEBRIS UNDER GIRT BAR. CLEANED DEBRIS UNDER GIRT BAR. DOOR ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080728 NM 2008 7 28 2008UALA03384 1 20080613 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 538UA 25222 EXTERNAL FWD OVERWING EMERGENCY EXIT LIGHT INOP RT. LAMP INOP. RELAMPED EXIT LIGHT ASSY, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080728 NM 2008 7 28 2008UALA03385 1 20080613 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 538UA 25222 DENT AT APPROX STA 630 LT APPROX 2' BELOW WINDOW. ACCOMPLISHED A MAJOR REPAIR AT DEN. THIS IS A CAT B RPR AND REQUIRES SUPPLEMENTAL INSP TO BEGIN AT 37500FC. 5 CF ITEMS BEING CREATED TO ACP THIS TASK PER EVA 71659 CREATED CF9049, CF9050, CF9051, CF9052 AND CF 90 53 FOR THE SUPPLEMENTAL INSPECTIONS STARTING AT 37,500FC CURRENT PTC IS 20618. INSP TO BEGIN I N 16882FC. 2 L 7 2 4F 4 F RT A2NM E17NE 20080728 NM 2008 7 28 2008UALA03386 1 20080613 A 2611 PU90499R3 SMOKE DETECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAVATORY INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 538UA 25222 K-LAV SMOKE DETECTOR IS INOPERATIVE. SMOKE DETECTOR IS INOP. REPLACED K LAV SMOKE DETECTOR. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080728 NM 2008 7 28 2008UALA03387 1 20080615 A 3397 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 538UA 25222 EEL'S RIGHT SIDE BY DOOR 1R, OVER DOOR 1R AND CTR, EXIT BETWEEN 1ST CLASS AND ECONOMY, EEL ABOVE SEAT 14C ARE INOP. LOO SE CONNECTOR. SECURED CONNECTOR FOR POWER SUPPLY FOR EMERGENCY EXIT SIGNS AT DOOR 1R AND CTR AND TEST, FOUND GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080728 NM 2008 7 28 2008UALA03596 1 20080626 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 AFT PIT AT BS 1480, APPROX STR 26L, FRAME HAS DENT AT INBOARD FLANGE. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED DAMAGE , FABRICATED REPAIR AND INSTALLED PER SRM 53-00-07 REPAIR 5. THIS IS A CAT B REPAIR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSPECTION STARTING AT 50000FC AND 12000FC THEREAFTER PER SRM 53-00-07 REPAIR 5 TABLE II. THESE INSP ARE BOTH DETAIL V ISUAL AND NDT CURRENT PTC IS 18040. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 NE 2008 7 29 2008UALA03598 2 20080627 A 7200 BLADE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE NR 2 ENGINE DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 791UA 26933 222180 NR 2 ENGINE FAILED BOROSCOPE INSP 2ND STAGE BLADES HAS 2 EACH BLADES WITH DAMAGE. ENGINE REPLACED. TWO HP TURBINE STAG E-2 BLADES WERE FOUND WITH MISSING PORTIONS OF THE CONCAVE AIRFOIL PLATFORM. THE FAILED BLADES, SERIAL NOS. CKLBHY9532 & CKLBHY7580 HAD IDENTICAL TIMES AND CYCLES. NUMEROUS OTHER STAGE-2 BLADES HAD RESULTANT DAMAGE. ALSO, STAGE-3 VANES HAD DAMAGE REQUIRING LP TURBINE DISASSEMBLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080729 EA 2008 7 29 REX2008F00014 1 20080710 A 3220 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA NOSE MALFUNCTIONED A REXA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 CE 21 825AY 8025 GEAR DISAGREE MESSAGE (NOSE NOT DOWN AND LOCKED) ON APPROACH, QRH FOLLOWED GEAR LOCKED DOWN EMERGENCY DECLARED WITH UNEV ENTFUL LANDING. AFTER LANDING THE F/A REPORTED SMOKE COMING FROM ROW A. TROUBLESHOT SYSTEM IAW MM AND REPLACED THE NLG PRIORITY VALVE. GEAR SWING WAS NORMAL AND AC WAS RELEASED FOR SERVICE. MAINT PERFORMED HIGH POWER RUNS ON BOTH ENGINE "SMOKE" WAS DETERMINED TO BE CONDENSATION FROM THE AIR CONDITIONING SYSTEM. (K) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 HNA2008F00012 1 20080611 A 3350 6004791 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS DISCHARGED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 936HA 33757 145 EMERGENCY EXIT SIGN ABOVE AIRSTAIR DOOR ENTRANCE INOPERATIVE. REMOVED AND REPLACED 3351, PS1 BATTERY PACK IAW 33-52-00. (K) 2 H 7 2 4T RT A13NM 20080729 NM 2008 7 29 2008UALA03342 1 20080613 A 2421 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RIGHT FAILED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 545UA 25323 RIGHT GENERATOR DISCONNECTED. RTFL. IDG FAILURE (LOW OIL) - TEARDOWN INCONCLUSIVE. REPLACED IDG. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 2008 7 29 SIM2008F00001 4 20080710 A 3444 ALTIMETER EMB 145 EMB145LR 3260212 SO RADIO MALFUNCTIONED A SIMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 21 617AE 145093 ON FLIGHT 4111 CREW REPORTED ON APPROACH, AFTER LANDING GEAR DEPLOYMENT SHOWING DOWN AND LOCK, GPWS WARNING TOO LOW GEAR AC WAS IN POSITIVE CLEARANCE WITH GROUND. CREW ABORTED APPROACH AND DECLARED EMERGENCY. CREW HAD TOWER CONFIRM LANDIN G GEAR DEPLOYMENT. AC LANDED SAFELY AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. AC REMOVED FROM SERVICE C/A MEL 3 4-20. REMOVED AND REPLACED RADIO ALTIMETER IAW AMM 34-31-01, OPS TEST GOOD. AC RETURNED TO SERVICE MEL RESTORED. (K) 2 L 7 2 4T RT T00011AT 20080729 EA 2008 7 29 HNA2008F00013 1 20080607 A 6123 AUTOFEATHER SYS DHAV DHC8 DHC8311 1386006 EA INOPERATIVE A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 329EN 290 ABORTED TAKEOFF DUE TO AUTOFEATHER NOT ARMING ON THE TAKEOFF ROLL, ABORTED TAKEOFF AT 90-95 KNOTS, RETURNED TO GATE. GR OUND RAN AC AUTOFEATHER ARMS AT ABOUT 74 PERCENT TORQUE, OK FOR SERVICE. (K) 2 H 7 2 4T RT A13NM 20080729 NM 2008 7 29 UIE2008F00019 1 20080629 A 7830 STRUCTURE BOEING 747 747243B 1384830 NM THRUST REVERSER DENTED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 540MC 22508 NR 1 ENG IB THRUST REVERSER OUTER SURFACE FOUND LARGE DENT AT THE UPPER POSITION. NR 1 ENGINE IB THRUST REVERSER DENT R EPAIRED IAW ENGINE MANUAL 78-32-01 REPAIR NR 4. (K) 2 L 7 4 4F RT A20WE 20080729 SO 2008 7 29 SIM2008F00003 1 20080712 A 3240 21707 BRAKE ASSY EMB 135 EMB135KL 3260302 SO NR 3 DISINTEGRATED A SIMA D RETURN TO BLOCK M B J OVER TEMP SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 821AE 145577 ON FLIGHT 3127, CREW REPORTED ON TAXI OUT THE BRAKE DEGRADE/BRAKE LO PRESS AND HYD SYS 2 AT BOTTOM OF YELLOW BAND AND EV IDENCE OF HYDRAULIC LEAK AT RT MAIN LANDING AREA. AIRCRAFT REMOVED FROM SERVICE C/A: INSPECTED AND FOUND NR 3 BRAKE HAD DISINTEGRATED REMOVED AND REPLACED NR 3 BRAKE ASSY. AC RETURNED TO SERVICE. (K) 2 L 7 2 4F RT T00011AT 20080729 EA 2008 7 29 HNA2008F00019 1 20080629 A 5610 8SC0043010 WINDSCREEN DHAV DHC8 DHC8311 1386006 EA COCKPIT CRACKED A HNAA O OTHER O OTHER CL CLIMB 1 EA 07 333EN 34850 221 F/O WINDSCREEN DEVELOPED CRACKS AFTER DEPARTURE. REMOVED AND REPLACED F/O WINDSCREEN. (K) 2 H 7 2 4T RT A13NM 20080729 NM 2008 7 29 UIE2008F00008 1 20080618 A 5753 SKIN BOEING 747 74747UF 1384812 NM LT OB FOREFLAP DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 408MC 29261 FOUND DURING A-CHECK. REPAIR THE DAMAGE FOUND ON L/E OF LEFT OB FOREFLAP MEASURING 12 INCHES LONG BY 2 INCHES WIDE IAW SRM 51-70-07. REPAIR CARRIED OUT IAW EO 4457A145. (K) 2 L 7 4 4F RT A20WE 20080729 NM 2008 7 29 UIE2008F00024 1 20080706 A 5313 STRINGER BOEING 747 747243B 1384830 NM BS 320 S25L CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 540MC 22508 STA 320, STRINGER 25L HAS FATIGUE CRACK. FRAME REPAIRED AT STA 320 LT SIDE IAW SRM 53-10-04, FIG 10. (K) 2 L 7 4 4F RT A20WE 20080729 2008 7 29 2008UALA03412 4 20080615 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 523UA 24932 FOUND DOOR 1L SLIDE ON FLOOR. RESECURED SLIDE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 EA 2008 7 29 TRAX200800750 1 20080604 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 477-693 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 LHS CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE FS 477.00 TO FS 693.00. REMOVED SEAT RAIL ASSY INSPECTED AND FOUND COR ROSION UNDER SEAT RAIL. PREPPED, PRIMED AND PAINTED AREA ON FUSELAGE SKIN IAW SRM 53-00-49. REPLACED SEAT RAILS AT FLOOR STATION 477.00 TO 693.00 IAW AMM 53-00-49. (B) 2 L 7 2 4F RT A21EA 20080728 NE 2008 7 28 UHL2008F00001 2 20080610 A 7321 4120T00P48 FADEC EMB ERJ170 ERJ170100SE 3260406 NM GE CF34 CF34* 30015 NE RT ENGINE DEFECTIVE A UHLA O OTHER O OTHER NR NOT REPORTED 1 GL 11 643RW 5318 17000060 IN CRUISE, NR 2 ENG WENT TO IDLE AND CREW RECEIVED AN ENG 2 CONTROL FAULT EICAS MSG. THE CREW WAS UNABLE TO CONTROL ENG 2 TRUST AND PERFORMED ENG 2 PRECAUTIONARY SHUTDOWN, DECLARED AN EMERGENCY, DIVERTED AND LANDED WITHOUT INCIDENT. MAINT REMOVED AND REPLACED THE E2 FADEC. (K) 2 L 7 2 4F 4 F RT A56NM 20080728 EU 2008 7 28 UPS08152592 1 20080613 A 5321 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 152UP 0835 INSPECTION TYPE:5YR MAIN CARGO COMPARTMENT FLOOR PNL 252YG PUNCTURED. REPAIRED MAIN CARGO COMPARTMENT FLOOR PNL 252YG I AW A300 SRM 53-10- 20 TABLE 201 PAR 8A. 2 L 7 2 4F RT A35EU 20080728 CE 2008 7 28 GUU2008F00002 1 20080702 A 3260 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE LT MLG OUT OF ADJUST A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 87555 UE234 DURING FLIGHT LANDING GEAR IN TRANSIT LIGHT ILLUMINATED. ADJUSTED LEFT LANDING GEAR UPLOCK SWITCH. (K) 2 L 7 2 4T RT A24CE 20080728 CE 2008 7 28 JBG2008F00002 1 20080630 A 2910 605700311 HOSE LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE HYD SYSTEM LEAKING E JBGA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 11 260AN 124 PILOT REPORTED A LOSS OF HYDRAULICS DURING FLIGHT AT CRUISE FL400. INSPECTION REVEALED THAT THE RT ENGINE DRIVEN HYDR P UMP PRESSURE SIDE HYDRAULIC LINE WAS LEAKING, AND ALLOW THE AC`S HYDR SYS FLUID BE DEPLETED. FURTHER INSP REVEALED THAT LINE HAD FAILED INTERNALLY AND WHEN PRESSURE WAS APPLIED THE HOSE WOULD SWELL AND BEGIN TO LEAK. THE PROBABLE CAUSE OF THE FAILURE IS AGE AND POSSIBLE EMBRITTLEMENT OF THE HOSE. TO POSSIBLY PREVENT RECURRENCE OF SUCH FAILURES A TIME INTE RVAL FOR REPLACEMENT OF AGEING HOSES MAY BE NEEDED. (K) 2 L 7 2 4F 4 F RT A10CE E35NE 20080728 CE 2008 7 28 VQM2008F00000 1 20080703 A 2731 99142871 CONTROL UNIT CESSNA 650 650 2076802 CE GARRTT TFE731 TFE731* 01518 WP PITCH TRIM INOPERATIVE E VQMA O OTHER O OTHER NR NOT REPORTED 1 NM 03 651PW 6500090 HORIZ PITCH TRIM CONTROL ADVISORY UNIT WAS REPLACED AND OPERATIONALLY CHECKED GOOD IAW MM 27-40-01. AT PREFLIGHT, PILOT NOTICED TRIM INDICATION WAS NORMAL, THEN IT BEGAN INDICATING MOVEMENT WHILE TRIM SWITCHES WERE NOT ENGAGED. WITH TRIM INDICATION AT TAKEOFF THE PILOT PERFORMED A VISUAL INSPECTION OF HORIZONTAL STAB POSITION AND CONFIRMED STAB POSITION W AS IN FULL DOWN WHILE INDICATOR SHOWED GREEN T/O MARK. FLIGHT WAS CANCELLED AND ANOTHER TRIM ADVISORY UNIT WAS ORDERED, UNIT WAS REPLACED THE NEXT DAY. UNIT WAS RECENTLY REPAIRED ON WO NR 1199756 DATED FEB 18, 2008 AND BOUGHT ON JULY 2, 2 008 AND INSTALLED THAT SAME DATE. (K) 2 L 7 2 4F 4 F A9NM E6WE 20080728 CE 2008 7 28 EO72008F00000 1 20080702 A 2121 903840311 FAN BEECH 90 C90A 1152911 CE PWA PT6 PT6* 52043 EA CABIN LOCKED E EO7A O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 07 396AS LJ1540 CABIN FAN FAILED WHICH CAUSED SMOKE IN THE CABIN. AIRCRAFT WAS LANDED WITHOUT INCIDENT. (K) 1 L 7 2 3T 3 T RT 3A20 E2NE 20080728 CE 2008 7 28 DJF2008F00003 1 20080622 A 2150 A/C PACK BEECH MU300 400A 1155402 CE MALFUNCTIONED E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 23 785TA RK239 DURING AIR CONDITIONER OPERATION, UNIT PULLED HIGH AMPS AND POPPED AIR CONDITIONER CIRCUIT BREAKER. A BURNING ODOR WAS APPARENT NEAR THE REAR OF THE AIRCRAFT. OPEN. (K) 2 H 7 2 4F RT A16SW 20080728 NE 2008 7 28 UHL2008F00000 2 20080602 A 7320 1103P1114 PRESSURE SWITCH EMB ERJ170 ERJ170100SE 3260406 NM GE CF34 CF34* 30015 NE RT ENGINE DEFECTIVE A UHLA O OTHER O OTHER NR NOT REPORTED 1 GL 11 648RW 17000068 CREW REPORTED ENG 2 FUEL LOW PRESSURE INDICATION AND FUEL FEED 2 FAULT. CREW FOLLOWED QRH PROCEDURES; DECLARED AN EMERG ENCY, DIVERTED AND LANDED WITHOUT INCIDENT. MAINT REPLACED THE LOW PRESSURE FUEL SWITCH. (K) 2 L 7 2 4F 4 F RT A56NM 20080728 NM 2008 7 28 MWE2008F00013 1 20080703 A 7830 715K9004507 ANGLE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE THRUST REVERSER CRACKED A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 918ME 55180 RT THRUST REVERSER DEFLECTOR DOOR (UPPER) Z FRAME HAS A CRACKED REPAIR AT THE LT END AT STA 26.666. FABRICATED AND INST ALLED ANGLE. (K) 2 L 7 2 4F 4 F TR A6WE E00061EN 20080728 NM 2008 7 28 2008UALA03179 1 20080603 A 3320 COVER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN MISSING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 840UA 1522 SIDE WALL LIGHT COVER AT RIGHT OVERWING EXIT IS MISSING. REPLACED OVERWING SLIDE ARM SLIDE COVER. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 NM 2008 7 28 AALA200801316 1 20080515 A 3350 0202226001 SHROUD BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 920AN 29521 LGA EMERGENCY LIGHT AT SEAT ROW 9 HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 9. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A16WE 20080728 NM 2008 7 28 AALA200801319 1 20080515 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 792AN 30253 MIA EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NOR MAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 EA 2008 7 28 MASA200800453 1 20080607 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 956LR 15056 ASH FLT 2937 OKC-PHX. OVERHEAD CABIN INTERIOR EMERGENCY LIGHT INOP. RELAMPED. (B) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 MASA200800458 1 20080608 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA CABIN ODOR A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 515MJ 10117 ASH FLT 7192 IAD-BOS. BURNING ODOR FROM MID AND AFT CABIN. MX PERFORMED OPERATIONAL CHECKS OF AIR CONDITIONING AND ELEC TRICAL SYSTEMS--COULD NOT DUPLICATE FAULT. (B) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 MASA200800473 1 20080616 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 97325 7325 ASH FLT 2767, PHX-MRY. PAX DOOR DIFFICULT TO OPEN. MX INSPECTED DOOR-OP CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 KCSA081273 1 20080605 A 3350 LIGHT BOEING 747 747132 1384882 NM BS 780 INOPERATIVE A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 709CK 20247 UPPER DECK EMERGENCY LIGHT INOP AT BS 780 (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 KCSA081281 1 20080612 A 5411 FRAME BOEING 747 747212B 1384886 NM NR 2 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 NR 2 PYLON REAR ENG. MOUNT BULKHEAD FWD. O/B FRAME IS CRACKED AT NAC STA 221.9 (B) 2 L 7 4 4F RT A20WE 20080728 EA 2008 7 28 TRAX200800865 1 20080701 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 559 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 FS 559 BULKHEAD WEB HAS INDICATIONS AT WL 58.70 I/B OF RBL 18 APPROX 1.3" IN LENGTH AND O/B OF RBL 9 APPROX .4" IN LENGT H, AND CAP ANGLE AT LBL 18, AND RBL 18 APPROX .5 IN LENGTH FAILED NDT INSP. (B) REPAIRED FS 559 BULKHEAD WEB AND CAP A NGLE ON LT AND RT SIDE FROM LBL 27 TO LBL 9 AND RBL 27 TO RBL 9 IAW REO 601R-53-41-754. RII C/W 5300002. 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 KCSA081290 1 20080618 A 5330 SKIN BOEING 747 747122 1384872 NM BS 550 S41-42R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 EXTERNAL FUSELAGE SKIN IS DAMAGED AT STA. 550, BETWEEN STR. 41R AND 42R (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 AALA200801329 1 20080517 A 2751 TRANSMITTER BOEING 737 737823 13844BZ NM T/E FLAP OUT OF ADJUST A AALA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 SW 21 959AN 30828 TPA INFLIGHT T1938/17MAY. TRAILING EDGE FLAP ASYMMETRY INDICATION. CLEANED AND ADJUSTED RT HAND FLAP TRANSMITTER. SYS TEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A16WE 20080728 NM 2008 7 28 KCSA081280 1 20080611 A 5412 BULKHEAD BOEING 747 747132 1384882 NM NR 4 NACELLE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 709CK 20247 NR 4 PYLON NAC STA 221.9 BULKHEAD WEB CHAFED AROUND HYD. PRESS. LINE (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 KCSA081274 1 20080611 A 3350 LIGHT BOEING 747 747132 1384882 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 709CK 20247 ROUND EMERGENCY LIGHT AT L-1 MAIN ENTRY DOOR AFT SIDE IS INOP (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 AALA200801330 1 20080517 A 3350 CM767 LIGHT BOEING 757 757223 1384957 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 613AA 24489 SJU EXTERIOR EMERGENCY LIGHT AT LT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMB ER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A2NM 20080728 NM 2008 7 28 KCSA081282 1 20080612 A 5210 FRAME BOEING 747 747122 1384872 NM BS 808 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 MAIN DECK R2 DOOR LOWER FORWARD CORNER VERTICAL FRAME IS CRACKED 1" LONG AT STA.808, WL 205 (B) 2 L 7 4 4F RT A20WE 20080728 EA 2008 7 28 TRAX200800903 1 20080710 A 3244 TIRE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A ASOA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 978EV 7723 NOSE TIRE BLEW OUT AT ROTATION ON T.O. SPEED KIAS. RETURNED TO ATL EMERGENCY DECLARED. FLT 4901 DEL 278 MINS..NC REMOV ED AND REPLACED LT AND RT NOSE TIRES IAW CRJ-200 AMM 32-42-01. [SDR CLOSED] (B) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800721 1 20080601 A 5530 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 708EV 10060 RT DRAG ANGLE (EMPENAGE-VERTICAL) APPEARS CRACKED. PERFORMED ET INSPECTION OF SUSPECT CRACK IAW NDTM 51-20-006. FOUND ANGLE TO BE CRACKED. MARKED END OF CRACK. (B) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 KCSA081275 1 20080611 A 5412 BULKHEAD BOEING 747 747132 1384882 NM NR 3 NACELLE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 709CK 20247 NR 3 PYLON NAC STA 221.9 BULKHEAD WEB CHAFED AT HYD. PRESS. LINE (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 KCSA081289 1 20080618 A 5311 FRAME BOEING 747 747122 1384872 NM BS 434 S26R CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STA. 434 R1 DOOR FRAME HAS CRACK AT INBOARD HOLE OF FRAME AT STR. 26R (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 ASAA0843172 1 20080709 A 2750 65503253 LINK BOEING 737 7374Q8 138447Q NM FLAP TRANMISSION WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 52151 25101 NR 5 FLAP TRANSMISSION UPPER BALL LINK WORN. REPLACED TRANSMISSION REF 27-51-71-004-001 AND 27-51-71-404-026. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 CALA0800723 1 20080717 A 5320 143A511011 FLOOR SUPPORT BOEING 737 737724 13844BY NM BS 500-520 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23721 28940 CABIN MAIN DECK FLOOR SUPPORT WEB CRACKED STA 500 TO 520 BL 0. FABRICATED AND INSTALLED REPAIR PER ECRA 5310-04804. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 CALA0800731 1 20080719 A 5311 6546545 FRAME BOEING 737 737524 1384721 NM BS 706 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17627 27531 STATION 706 LEFT FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9 INBOARD HOLE. REPAIRED FRAME AT ST ATION 706 BETWEEN S-8 AND S-9L PER EA5310-04498 AND EC/RA5310-04805. 2 L 7 2 4F RT A16WE 20080807 EU 2008 8 7 AALA200801550 1 20080606 A 3350 LAMP AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 80057 465 JFK - EMERGENCY EXIT SIGN LIGHT AT RT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT NUMBER ONE D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080807 NM 2008 8 7 AALA200801477 1 20080602 A 3350 LIGHT BOEING 757 757223 1384957 NM EXTERIOR DIRTY A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 674AN 29424 DFW - EXTERIOR EMERGENCY LIGHT AT RT NR FOUR DOOR INOPERATIVE. CLEANED AND SECURED LIGHT ASSEMBLY FOR EXTERIOR EMERGENC Y LIGHT AT RT NR FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 AALA200801368 1 20080522 A 3350 0202226001 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 693AA 26973 JFK - EMERGENCY LIGHT AT SEAT ROW 15DEF MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 15DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 AALA200801356 1 20080520 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 771AN 29579 DFW - EMERGENCY LIGHT AT SEAT ROW 21C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 21C. SYSTEM GROUND C HECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 EU 2008 8 7 AALA200801468 1 20080602 A 2842 SENSOR AIRBUS 300 A300B4605R 3930308 EU FUEL QTY FAULTED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 59081 639 MIA INFLIGHT T2141/02JUN. CREW REPORTED UNWANTED RT OUTER TANK FUEL FEED DURING NORMAL FUEL MANAGEMENT AND INNER TANK I NDICATION. ADJUSTED FUEL QUANTITY SENSOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080807 EU 2008 8 7 AALA200801723 1 20080628 A 2820 VALVE AIRBUS 300 A300B4605R 3930308 EU FUEL SYSTEM INOPERATIVE A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 70054 461 MIA INFLIGHT T816/26JUN. INBOUND TO MIA CREW REPORTED FUEL IMBALANCE. LANDED MIA WITHOUT INCIDENT. REPLACED LT OUTER ISOLATION VALVE AND ACTUATOR, LT INNER FUEL STICK AND SEALS OF LT OUTER FUEL FEED MANIFOLD BETWEEN RIBS 8 AND 9. REPLA CED LT INNER TANK REFUEL/DEFUEL SWITCH ON REFUEL PANEL AND COUPLING SEALS OF LT INNER BOOST PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A35EU 20080807 EA 2008 8 7 A6WA200840492 1 20080609 A 5330 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 615 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 CARGO DOOR NET ATTCHMENT FITTING AT FS 615 LBL 40 CORRODED. CORROSION REMOVED IAW CRJ 200 SRM 51-21-06. (A) 2 L 7 2 4F RT A21EA 20080807 EA 2008 8 7 A6WA200840484 1 20080406 A 5340 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 529 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 HYDRAULIC SUPPORT BRACKET (P/N 601R75262-157) CRACKED IN RT MLG BAY. HYDRAULIC SUPPORT BRACKET REPLACED IN RT MLG BAY I AW REO 601R-53-42-007. (A) 2 L 7 2 4F RT A21EA 20080807 EA 2008 8 7 A6WA200840485 1 20080606 A 5340 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 531 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 HYDRAULIC SUPPORT BRACKET (P/N 601R75262-159) CRACKED IN LT MLG BAY. HYDRAULIC SUPPORT BRACKET REPLACED IN LT MLG BAY I AW REO 601R-53-42-007. (A) 2 L 7 2 4F RT A21EA 20080807 SO 2008 8 7 C2XA08RI088 1 20080615 A 3233 22250100003 SOLENOID VALVE EMB 145 EMB145LR 3260212 SO NLG DEFECTIVE A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 13968 21844 145138 FLIGHT 3001 - EWR - FLIGHT CREW REPORTED THAT IT SOUNDED LIKE LANDING GEAR DOORS OPEN IN FLIGHT. EWR MAINTENANCE REMOVE D AND REPLACED NOSE LANDING GEAR DOOR SOLENOID VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080807 2008 8 7 COMA0860323 4 20080711 A 2211 6229815704 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA NR 1 FAILED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 420CA 19746 7451 FLIGHT 5675. EN ROUTE FROM VHZ TO BOS FELT AND SAW (1/2 SLIP INDICATOR) UNCOMMANDED RUDDER MOVEMENT. REMOVED AND REPLA CED NR 1 FCC. (A) 2 L 7 2 4F RT A21EA 20080807 NM 2008 8 7 2008UALA03633 1 20080629 A 3350 D9239003500060 BATTERY PACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 827UA 1022 WHILE ACCOMPLISHING EMERGENCY LIGHT TEST "BATTERY EPSU RIGHT" DISPLAYED. *S/D* EPSU FAILURE. REPLACED EPSU. 2 L 7 2 4F 4 F RT A28NM E40NE 20080807 SO 2008 8 7 C2XA08RI090 1 20080616 A 3320 7287501543 LIGHT EMB 145 EMB145LR 3260212 SO CABIN SMOKE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 22971 145149 FLIGHT 2528 - EWR - FLIGHT CREW REPORTED THAT MULTIPLE PASSENGERS COMPLAINED OF ELECTRICAL SMOKE SMELL IN CABIN BY ROW 1 5. EWR MAINTENANCE REMOVED AND REPLACED SEAT 15 A CEILING LIGHT ASSY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACF T WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080807 NM 2008 8 7 AALA200801457 1 20080601 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 DFW - EMERGENCY LIGHT AT SEAT 35G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 35G. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 SO 2008 8 7 C2XA08ON144 1 20080620 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145XR 3260214 SO NLG INOPERATIVE A C2XA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 27 12201 6082 3215 14500959 FLT 0117 - ONT - FLIGHT CREW REPORTED A LOUD BANGING NOISE ON GEAR RETRACTION WHILE CLIMBING. FLIGHT CREW RETURNED TO B LOCK. MAINTENANCE INSPECTED, REMOVED AND REPLACED NLG UPLOCK BOX PROXIMITY SWITCH AND PERFORMED A TEST FLIGHT. OPERATI ONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4F RT 20080807 SO 2008 8 7 C2XA08SH090 1 20080620 A 5551 14521904424 FITTING EMB 145 EMB145XR 3260214 SO HORIZONTAL STAB WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16147 145749 SHV - DURING C-CHECK IT WAS FOUND THAT THE RT HORIZONTAL STAB HINGE PIN FITTING HAD MIGRATED PLAIN BUSHINGS. MAINTENANC E PERFORMED A REAMING PROCEDURE TO THE SECOND OVERSIZE IAW EMB 145XR SRM 55-10-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080818 WP 2008 8 18 UPS08852740 1 20080709 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 896 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, LT MLG DOOR SWITCH STA 896.500 HAS 1 EA ELONGATED HOLE AT SUPPORTING WEB. REPAIRED IAW EO DC8-3260 -16914-A. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852899 1 20080630 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, OBSERVERS FWD SEAT TRACK HAS ELONGATED HOLES REMOVED AND REPLACED SEAT TRACK IAW, SRM, 51-3-2, 5 1-1-8, 51-3-0. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852601 1 20080627 A 5730 PANEL DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 LT WING PANEL CORROSION. REMOVED DAMAGED SKIN. ACCOMPLISHED STEPS 1-6 OF EO DC8-5720-29785 APPENDIX A. ACCOMPLISHED RE PAIR STEPS 1-9 OF EO DC8-5720-29785-A. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852636 1 20080611 A 5313 LONGERON DOUG DC8 DC871F 302199D WP FSS 120 L3A RT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, MAIN CABIN 9G NET ANCHOR FITTING L3A RT HAS EXFOLIATION CORROSION AT BS 120. REMOVED DAMAGED LONGER ON SECTION BS 110 TO BS 120 3A RT REF SRM 53- 02-02 FIG 10 AND SRM 51-01-21. FABRICATED NEW LONGERON SECTION AND REPAIR STRAPS (2EA). INSTALLED REPAIR PARTS IAW SRM 51-01-21, AND 53-02-02 FIG 10. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852916 1 20080615 A 5540 ANGLE DOUG DC8 DC871F 302199D WP RUDDER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1 RUDDER "L" ANGLE CRACKED AT LT SIDE OF TOAD STOOL. (RUDDER TORQUE TUBE) REMOVED FABRICATED AND REPL ACED "L" ANGLE IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852973 1 20080724 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C1, FLOOR PANEL 626D HAS DAMAGE AT 2 CORNERS AS MARKED EDGE DAMAGE OUT OF LIMITS IAW, SRM 53-2-0 FIG 1F , FABRICATED AND REPLACED FLOOR PANEL SKIN IAW DWG 3619130 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 20080818 NM 2008 8 18 UPS08M52961 1 20080718 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 31 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 UPS08M52962 1 20080719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 31 LT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 SWAA084021 1 20080716 A 5320 6545410 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM BS 706-708 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED HC1 CHECK, FOUND LONGITUDINAL FLOOR SUPPORT WEB CRACKED AT BS 706 AND BS 708, LBL 25. REPAIRED FLOOR S UPPORT PER ER. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084038 1 20080719 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 AFT CABIN EMERGENCY FLASHLIGHT INOP. R&R FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084075 1 20080723 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 929 S25L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER 25L CRACKED AT BS 929. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084088 1 20080720 A 5312 6545819 PRESSURE PANEL BOEING 737 7375H4 138449D NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED BRDG CHECK, FOUND NLG WW RT CEILING WEB CUTOUT CRACKED. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 20080818 2008 8 18 SWAA084089 4 20080723 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084090 1 20080723 A 5311 6546593 FRAME BOEING 737 7373Q8 1384670 NM BS 500A S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084114 1 20080724 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 440LV 29835 EMERGENCY LIGHT END CAP LOOSE AT ROW 1 ABC. SECURED END CAP PER MM. 2 L 7 2 4F RT A16WE 20080818 2008 8 18 SWAA084117 4 20080724 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080807 SO 2008 8 7 C2XA08SH091 1 20080620 A 5330 14520552001 SKIN EMB 145 EMB145XR 3260214 SO FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16147 145749 SHV - DURING C-CHECK IT WAS FOUND THAT THE CENTER FUSELAGE SKIN HAD AN INTERNAL GOUGE BETWEEN FRAMES 16 AND 17, AND STRI NGERS 3R AND 4R. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB 145XR SRM 53-21-01. THE ACFT WAS APPROVED FOR RETURN T O SERVICE. (S) 2 L 7 2 4F RT 20080807 SO 2008 8 7 C2XA08TY063 1 20080619 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 16976 145171 LT FWD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04. OPS CH ECK GOOD. (S) 2 L 7 2 4T RT T00011AT 20080807 SO 2008 8 7 C2XA08SH086 1 20080619 A 5320 13500157401 SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 17 10575 145640 SHV - DURING C-CHECK IT WAS FOUND THAT THE TOILET EXTERNAL WASTE VALVE SUPPORT WAS CORRODED AT FRAME 60. MAINTENANCE RE MOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB145 SRM 53-31-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE . (S) 2 L 7 2 4T RT T00011AT 20080807 SO 2008 8 7 C2XA08SH089 1 20080620 A 5551 14521904423 FITTING EMB 145 EMB145XR 3260214 SO HORIZONTAL STAB GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16147 145749 SHV - DURING C-CHECK IT WAS FOUND THAT THE LT HORIZONTAL STAB HINGE PIN FITTING WAS GOUGED. MAINTENANCE PERFORMED A REA MING PROCEDURE TO THE FIRST OVERSIZE IAW EMB 145XR SRM 55-10-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080807 SO 2008 8 7 C2XA08TY065 1 20080617 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 11551 145411 LT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY IAW EMB 145 AMM 33-50-04. O PS CHECK GOOD. (S) 2 L 7 2 4T RT T00011AT 20080807 SO 2008 8 7 C2XA08TY058 1 20080613 A 3350 7137216501 LIGHT EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 14947 145054 EMERGENCY LIGHT IN MID CEILING, AFT SIDE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW EMB 145 AMM 33-51-01. O PS CHECK GOOD. (S) 2 L 7 2 4F RT T00011AT 20080807 EA 2008 8 7 C2XA08TY060 2 20080612 A 7320 AO269 MODULE EMB 145 EMB145XR 3260214 SO RROYCE AE3007 AE3007A1E 54169 EA ENGINE MALFUNCTIONED A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 13202 14500962 ACFT GOES TO ET10 RSV POWER ON ITS OWN UNCOMMANDED IN FLIGHT. WILL NOT STAY IN ANY OTHER THRUST RATING. REMOVED AND RE PLACED RESISTOR MODULE IAW EMB 145 AMM 73-22-02. OPS CHECK GOOD. (S) 2 L 7 2 4F 4 F RT TE6CH 20080807 SO 2008 8 7 C2XA08CL073 1 20080623 A 3350 B6245305 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INTERMITTENT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14977 145175 CLE - DURING MAINTENANCE CHECK MAINTENANCE FOUND THAT THE MAIN CABIN DOOR EMERGENCY LIGHT WORKED INTERMITTENTLY. MAINTE NANCE REMOVED AND REPLACED THE MAIN CABIN DOOR EMERGENCY LIGHT ASSEMBLY. ALL OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4T RT T00011AT 20080807 2008 8 7 CHQA200800148 4 20080716 A 3425 6229336400 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE AHRS FAILED A CHQA O OTHER O OTHER NR NOT REPORTED 1 GL 11 647BR 18057 18057 7399 E872717 FLIGHT 5577, IAH TO CRP. DURING CLIMB THE CREW REPORTED THAT THE FIRST OFFICER`S ATTITUDE AND HEADING REFERENCE DATA DI SAPPEARED WHEN THE AUTO-PILOT WAS ENGAGED. THE ACFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FAU LT CODES FOR BOTH THE NR 2 AHRS COMPUTER AND NR 2 FCC CARD ON THE MDC. BOTH WERE REPLACED AND NO FURTHER FAULTS WERE NO TED. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080807 NM 2008 8 7 KCSA081326 1 20080717 A 5411 FRAME BOEING 747 747246B 1384864 NM NR 1 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 NR 1 PYLON REAR ENG MOUNT BULKHEAD INBOARD AFT FRAME WEB CRACKED ONE INCH AT NAC STA 221.9. (S) 2 L 7 4 4F RT A20WE 20080807 NM 2008 8 7 08FDEA02479 1 20080625 A 5530 651749319 SKIN BOEING 727 727225 1384077 NM TAIL CONE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 TAIL CONE: VERTICAL STAB PNL 9703 HAS NUMEROUS PUNCTURES AND DELAM. REPAIRED PANEL NR 9703. REF SRM 51-40-9 PAR 3, 4 P AGES 2A-6. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080807 NM 2008 8 7 08FDEA02619 1 20080702 A 5313 6572703 STRINGER BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 CABIN S-2L HAS CORROSION FROM BS 720A - 740 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGE SECTION, INSTAL LED REPAIR AND RESTORED STRINGER TO ORIGINAL FINISH IAW REF SRM 53-10-01 AND 53-10-3 AND 53-10-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080807 NM 2008 8 7 08FDEA02624 1 20080702 A 5311 65159401 FRAME BOEING 727 727225 1384077 NM BS 740 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 TWO DRILL STARTS AT AFT LIP OF STA 740 FRAME BETWEEN STR 7R AND 8R. REMOVED DAMAGE .197 REMOVED FROM EDGE .200 INCH ALL OWED WITHIN LIMITS REF SRM 53-10-1 FIG 1 DETAIL 7, AND EA NR 7-5310-11400, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080807 NM 2008 8 7 08FDEA02626 1 20080702 A 5314 652355567 KEELBEAM BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 LOWER FUSELAGE INTERIOR OF KEEL BEAM, BS 760 TO 761, LBL 5 TO RBL5, WL 146, TO WL 146, KEAL BEAM FRAME T LOWER ATTACH A NGLE CORRODED. REMOVED DAMAGED STIFFENER AND REPLACED WITH A NEW STIFFENER 65-23555-67, PER REF SRM 51-30-02 PG 1-15. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080807 NM 2008 8 7 08FDEA02627 1 20080702 A 5340 69459474 FITTING BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 LOWER FUSELAGE, CORROSION ON TIE FITTING, STA 337 EXTIOR RBL 17", BELOW LANDING GEAR DRAG BRACE FITTING SUPPORT BEAM. R EMOVED AND REPLACED TIE FITTING STA 337, RBL 17 BELOW AND 13-14. 2 L 7 3 4F A3WE 20080806 EA 2008 8 6 A6WA200840515 1 20080615 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 465AW 7893 FLAPS FAILED AT 30 DEGREES ON APPROACH, COMPLIED WITH QRH LANDED IN BUF. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEM ENT 98-018B STEPS 1.3 AND 1.4 FLAPS SYSTEMS RESET OK. (A) 2 L 7 2 4F RT A21EA 20080819 EA 2008 8 19 SWIA200819861 1 20080715 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 937SW 7735 F/O FORWARD WINDOW SHATTERED. (FLIGHT NR5827) REPLACED RT WINDSHIELD IAW 56-11-01.P/N: NP-139321-6 S/N OFF: 02266H6 478. 2 L 7 2 4F RT A21EA 20080819 NM 2008 8 19 USAA920081483 1 20080726 A 3210 D3215303000800 PIN AIRBUS A319 A319132 3930340 NM LT MLG CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803AW 0931 SAL-C7 -MAJOR REPAIR- CORROSION ON REAR PINTLE PIN OF LT MAIN LANDING GEAR. REPLACED REAR PINTLE PIN OF LT MAIN LANDING GEAR IAW TASK CARD R4M32311. (S) 2 L 7 2 4F RT A28NM 20080819 NM 2008 8 19 USAA920081456 1 20080717 A 5312 651758243 BULKHEAD BOEING 737 73733A 1384673 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 168AW 23629 MCN-C21- MAJOR REPAIR - CRACK ON VERTICAL STIFFENER WEB AT BS 178 WL 225.5 BL 17L. REPAIRED VERTICAL STIFFENER WEB AT B S 178 WL 225.5 BL 17L IAW B737 SRM 53-10-01. (S) 2 L 7 2 4F RT A16WE 20080819 SO 2008 8 19 SWIA200819902 1 20080727 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO CABIN SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 578SW 120346 ON CLIMB OUT THERE WAS A STRONG SMOKE SMELL AND LAV DETECTOR SOUNDED. (FLIGHT NR 5538) INSPECTED LT PACK. CYCLED RAM A IR SWITCH. SYSTEM OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 20080819 NM 2008 8 19 USAA920081457 1 20080729 A 3397 WIRE BOEING 737 7374B7 1384702 NM CABIN UNSECURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT-C2-EEL- EMERGENCY LIGHT "EXIT" SIGN ON CEILING ABOVE AFT SERVICE DOOR HAS INTERMITTENT OPERATION. SECURED WIRES IN ENVIRONMENTAL PLUG. NO LONGER INTERMITTENT. (S) 2 L 7 2 4F RT A16WE 20080819 EA 2008 8 19 SWIA200819895 1 20080722 A 2720 RUDDER PEDAL CNDAIR CL600 CL6002B19 1900309 EA COCKPIT NOISY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 965SW 7871 CREW REPORTS A THUMPING SOUND DURING FLIGHT. (FLIGHT NR 1008) RETORQUED CAPTAINS RUDDER PEDAL PIVOT BOLTS IAW RJ-SL-27- 086. OPS CHECK GOOD FOR CONTINUED SERVICE. 2 L 7 2 4F RT A21EA 20080819 SO 2008 8 19 SWIA200819898 1 20080717 A 3397 WIRE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE EMERGENCY LIGHT INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 585SW 120353 FORWARD EMERGENCY LIGHTS ARE INOPERATIVE. (FLIGHT NR 5759) REPAIRED WIRING AT EMERGENCY LIGHT. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 20080819 EA 2008 8 19 SWIA200819932 1 20080603 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* 30015 NE LT NACELLE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 956SW 7825 LT AND RT ENGINE AFT THRUST FITTINGS HAVE SIGNS OF CORROSION. (FOUND AT C-CHECK) REPLACED THRUST FITTINGS IAW AMM 71-22 -01-400-801. 2 L 7 2 4F 4 F RT A21EA 20080819 EA 2008 8 19 REX2008F00023 1 20080731 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 8505Q 7505 ON CLIMBOUT OF MEM RECEIVED OVER SPEED CLACKER AND FLAP FAILURE MESSAGE. QRH FOLLOWED, RETURNED TO MEM WITH UNEVENTFUL LANDING. SYSTEM INSPECTED BY MAINTENANCE WITH NO DEFECTS AND NO PRIOR FAULT CODES BEFORE THIS EVENT. RESET FLAP SYSTEM AND PLACED ON 72 HOUR WATCH PER AD2006-12-21. (S) 2 L 7 2 4F RT A21EA 20080819 SO 2008 8 19 SWIA200819934 1 20080731 A 5310 BEAM EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE PAX DOORWAY CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 217SW 120286 PAX DOOR HINGE BEAM HAS AREAS OF CORROSION WHERE BUSHINGS ARE INSTALLED FOR FWD AND AFT HINGES. REPLACED PAX DOOR HINGE BEAM IAW SRM 51-25-00, 51-22-00, 51-40-02, 51-40-04, AND 51-40-07. 2 L 7 2 4T 4 T RT A31SO E20NE 20080819 SO 2008 8 19 SWIA200819935 1 20080722 A 5210 BUSHING EMB 120 EMB120ER 3260203 SO PAX DOOR WORN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 217SW 120286 MAIN CABIN DOOR IS HARD TO CLOSE AND OPEN. REPLACED PAX DOOR BUSHINGS AND BOLTS IAW AMM 20-10-00 AND INSTALLED DOOR IAW AMM 52-10-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080819 NE 2008 8 19 SWIA200819884 2 20080720 A 7230 PAD CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* 30015 NE NR 2 ENGINE WORN A SWIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 07 718SK 10184 NR 2 ENGINE SHUTDOWN DUE TO HIGH VIBRATION LEVELS ON CLIMBOUT. (FLIGHT NR 6083) REPLACED BLADE WEAR PADS ON THE NR 12 A ND NR 24 BLADES. PERFORMED FAN BLADE LUBE AND FAN TRIM BALANCE IAW MANUAL 72-00-00. VIB CHECK GOOD. PN: 4114T15P02 S/N OFF: IHI2887R PN: 4114T15P02 S/N OFF: IHI2897R 2 L 7 2 4F 4 F RT A21EA 20080819 WP 2008 8 19 UPS08853006 1 20080728 A 5230 DOOR FRAME DOUG DC8 DC871F 302199D WP BS 220 DAMAGED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C1, MAIN CARGO DOOR UPPER FRAME CENTER DOOR JAM HAS A DOUBLE DRILLED HOLE AT STA 220 & 6L. CUTOUT DAMA GE IAW SRM 53-02-00, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-02-00,51-1-20D, AND 51-1-21. 2 L 7 4 4F RT 4A25 20080819 SO 2008 8 19 RAIA00808005 1 20080804 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 03 816HK 145055 PRE FLT 5577 -STL- EMERGENCY LIGHT AT PASSENGER DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB. SYSTEM OP S CHECKED GOOD. (S) 2 L 7 2 4T RT T00011AT 20080819 NM 2008 8 19 PID2008F00011 1 20080731 A 2560 20131A BATTERY PACK BOEING 767 767277 1385128 NM ESCAPE HATCH DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 767MW 22694 DURING PREFLIGHT RT OVERWING ESCAPE HATCH SQUIB TEST LIGHT DIM. REMOVED AND REPLACED RT OVERWING ESCAPE HATCH EMERGENCY LIGHT BATTERY PACK. OPS CHECK WAS NORMAL IAW AMM 25-65-00. (S) 2 L 7 2 4F RT A1NM 20080819 NM 2008 8 19 UPS08M53020 1 20080713 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 26 LT BARREL NUT BORE HOLE REMOVED CORROSION, FABRICATED BUSHING, AND INST ALLED BUSHING IAW EO MD11-5510-19409-N SAA TRAVELER 80538440001. 2 L 7 3 4F RT A22WE 20080806 EA 2008 8 6 A6WA200840505 1 20080528 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 589 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 402AW 7281 CRACK FOUND ON FLOOR LANDING PLATES FS 589 LBL 45. FLOOR LANDING PLATES FS 589 LBL 45 REPAIRED IAW CRJ 200 REO 601R-53- 61-433. (A) 2 L 7 2 4F RT A21EA 20080806 SO 2008 8 6 C2XA08SH087 1 20080619 A 5340 14525381007 BUTTSTRAP EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 10575 145640 SHV - DURING C-CHECK IT WAS FOUND THAT THE CARGO COMPRATMENT CENTER BUTTSTRAP WAS CRACKED AT FRAME 71. MAINTENANCE FABR ICATED AND INSTALLED A REPAIR PIECE IAW CONTINENTAL EXPRESS EC5320-01412. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080806 EU 2008 8 6 TRAX200800824 1 20080623 A 5220 HANDLE AEROSP ATR72 ATR72212 8680945 EU EMERGENCY EXIT MISINSTALLED A ASOA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 633AS 344 ROW 1D EMERGENCY EXIT HANDLE VERY HARD TO PULL. INSTALLED RT EMERGENCY HATCH CORRECTLY. OPS CHECK GOOD. (S) 2 H 7 2 4T RT A53EU 20080806 2008 8 6 AALA20081416 4 20080528 A 2565 D31021107 SLIDE AIRBUS 300 A300B4605R 3930308 EU R3 DOOR FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 90070 513 TUL - RIGHT NR THREE EMERGENCY ESCAPE SLIDE DID NOT FULLY DEPLOY ON TEST. REPLACED EMERGENCY ESCAPE SLIDE FOR RIGHT NR THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080806 SO 2008 8 6 C2XA08IA143 1 20080619 A 2510 12315660401 HOLDER EMB 135 EMB135LR 3260305 SO COCKPIT ODOR A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 11526 15663 12991 145410 HSV - FLIGHT 2990 THE CREW REPORTED SMOKE IN THE COCKPIT WITH THE SOURCE IN THE VICINITY OF THE STEER DISCONNECT TRIGGER . THE ACFT RETURNED TO HSV WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE CAPTAIN`S CHART HOLDER ON MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. THE ACFT LANDED IN IAH WHERE MAINTENANCE REPLACED THE CAPTAIN`S CHART HOL DER. OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080806 2008 8 6 HNAA0800234 4 20080717 A 3442 066308601 DISPLAY DHAV DHC8 DHC8102 2809003 NM WX RADAR BURNED A HNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 827EX 34486 34486 390 RADAR SCREEN WENT BLANK INFLIGHT WITH A BURNING SMELL. CREW DECLARED EMERGENCY TO ATC. CREW TURNED RADAR OFF. MAINTEN ANCE REPLACED RADAR INDICATOR. OPS CHECK GOOD. (S) 2 H 7 2 4T RT A13NM 20080806 NM 2008 8 6 AALA200801426 1 20080528 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW - EXTERIOR EMERGENCY LIGHT AT RIGHT NR FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RIGHT N R FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 EA 2008 8 6 CHQA200800146 1 20080716 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE HYD SYSTEM LOW PRESSURE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 653BR 5224 5224 7438 E872823 FLIGHT 5701, AEX TO IAH. AFTER TAKEOFF WHILE THE LANDING GEAR WAS IN TRANSIT THE FLIGHT CREW RECEIVED A NOSE DOOR OPEN AND GEAR DISAGREE EICAS WARNING MESSAGE. THE CREW FOLLOWED THE QRH AND RETURNED TO AEX AND LANDED WITHOUT INCIDENT. TH E ACFT WAS FERRIED BACK TO IAH FOR FURTHER TROUBLESHOOTING. MAINTENANCE FOUND THAT THE NR3A HYDRAULIC PUMP WAS ON DEFER RAL AND THAT THE 3B PUMP WAS NOT PRODUCING ENOUGH PRESSURE TO OPERATE THE HYDRAULIC SYSTEM. BOTH OF THE SYSTEM 3 ELECTR IC MOTOR DRIVEN HYDRAULIC PUMPS WERE REPLACED AND THE GEAR SYSTEM OPERATED NORMALLY. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080806 NM 2008 8 6 ABXA080190 1 20080714 A 3350 20131A BATTERY PACK BOEING 767 767232 1385132 NM EMERGENCY LIGHT DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 744AX 22221 EMERGENCY LIGHT BATTERY PACK M737 WOULD NOT ILLUMINATE EMERGENCY LIGHTS. REMOVED BATTERY PACK FROM 739AX , INSTALLED IN 744AX IAW B767 M 33-51-07. OPS CHECKED GOOD. (S) 2 L 7 2 4F RT A1NM 20080806 NM 2008 8 6 AALA200801384 1 20080524 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 640A 24598 DFW - EMERGENCY LIGHT AT LEFT NR TWO DOOR SIDEWALL INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT NR TW O DOOR SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080806 NM 2008 8 6 AALA200801387 1 20080525 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 789AN 30252 DFW - EMERGENCY LIGHT AT SEAT ROW 11D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 11D. SYSTEM GROUND C HECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080806 NM 2008 8 6 AALA200801456 1 20080601 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 DFW - EMERGENCY LIGHT AT SEAT 37G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 37G. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 NM 2008 8 7 KCSA081356 1 20080729 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1960-2010 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FUSELAGE SKIN CORRODED BETWEEN BS1960 AND 2010, STR 34L. (S) 2 L 7 4 4F RT A20WE 20080807 NM 2008 8 7 2008UALA03707 1 20080705 A 2120 UNKNOWN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY SMOKE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 118UA 28811 SMOKE IN GALLEY. FLIGHT DIVERTED. 2 L 7 4 4F 4 F RT A20WE E24NE 20080807 NM 2008 8 7 2008UALA03816 1 20080709 A 3510 232N800197 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 LEAK IN CAPT'S OXYGEN MASK. HEAD STRAP HAS LEAK. LEAKING HEAD STRAP ON O2 MASK. REPLACED CAPT O2 MASK ASSY, OPS CHECK ED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080807 NM 2008 8 7 CALA0800736 1 20080721 A 3350 D71702030 CHARGER BOEING 767 767424ER 1385270 NM EMERGENCY LIGHTS INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 76054 29449 GALLEY 4 EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK CHARGER AND BATTERY PACK AT ROW 6AB IAW AMM 33-51-07. BATTERY PACK S/N 83766; BATTERY CHARGER S/N 12712. 2 L 7 2 4F RT A1NM 20080807 NM 2008 8 7 CALA0800738 1 20080721 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM BS 867 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 LEFT SIDE STATION 867 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. CUT OUT DAMAGED AREA AND REPAIRED FRAME AT STATION 867 LEFT BETWEEN S-8 AND S-9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080807 WP 2008 8 7 AALA200801754 1 20080702 A 7800 CLAMP DOUG DC9 DC982 3022082 WP AUGMENTATION LEAKING A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 403A 49314 TUL INFLIGHT T9610/02JUL. CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE INDICATION JUST AFTER TAKEOFF. RETURNED TO T UL AND LANDED WITHOUT INCIDENT. REPLACED LT AUGMENTATION VALVE CLAMP OUTBOARD SIDE. SYSTEM GROUND CHECKED NORMAL OPERA TION. (A) 2 L 7 2 4F A6WE 20080807 NM 2008 8 7 F3LA200800325 1 20080610 A 5320 D5397496700000 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 REFERENCE NON ROUTINE C044887. DURING C4 S1 C CHECK INSPECTION NOTED AFT CARGO COMPARTMENT FLOOR FRAME CAP AT FRAME 59 FROM STRINGER 38 LT TO STRINGER 38 RT IS CORRODED. MAINTENANCE REMOVED FRAME 59 PROFILE, UPSIZED AND COUNTERSUNK HOLES AS REQUIRED, INSTALLED NEW PROFILE ON FRAME 59 FROM STRINGER 38 LT AND STRINGER 38 RT IN ACCORDANCE WITH THE REQUIREMENT S OF SRM 51-42-11, SRM 51-44-00, SRM 51-44-11 AND SRM 51-46-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUN D ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080807 NM 2008 8 7 AALA200801490 1 20080602 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 780AN 29956 DFW - EMERGENCY LIGHT AT RT NR ONE GALLEY CART AREA HAS BROKEN LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LI GHT AT RT NR ONE GALLEY CART AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 NM 2008 8 7 AALA200801493 1 20080603 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 762AN 31479 JFK - EMERGENCY LIGHT AT FIRST CLASS GALLEY AFT BULKHEAD INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FIRS T CLASS GALLEY AFT BULKHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 NM 2008 8 7 AALA200801461 1 20080601 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 798AN 30797 DFW - EMERGENCY LIGHT AT SEAT 21G MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 NM 2008 8 7 AALA200801471 1 20080602 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 196AA 32390 DFW - EXTERIOR EMERGENCY LIGHT AT LT NUMBER TWO DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LT NR T WO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 CALA0800728 1 20080718 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM BS 907 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 LEFT SIDE STATION 907 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) A/C BRACKET INBOARD HOLE. REMOVED A/C BRACKET, CUT OUT DAMAGED AREA & REPAIRED FRAME AT STATION 907 LEFT BETWEEN S-8 AND S-9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 CALA0800729 1 20080719 A 5311 143A1113 FRAME BOEING 737 737724 13844BY NM BS 440 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 23721 28940 FRAME CRACKED AT STATION 440 BETWEEN S8R AND S9R. REPAIRED CRACKED FRAME BODY STATION 440 BETWEEN S-8 AND S-9 RIGHT PER EC/RA 5310-04806. 2 L 7 2 4F RT A16WE 20080807 NM 2008 8 7 CALA0800712 1 20080715 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM BS 440 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 RIGHT SIDE STA 440 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET INBOARD HOLE. REPAIRED CRACKED F RAME AT STA 440 BETWEEN S-8 AND S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080807 EA 2008 8 7 A6WA200840487 1 20080605 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 574 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 449AW 7818 CARGO BAY FLOOR SILL FOUND CRACKED AT FS 574.00. CARGO BAY FLOOR SILL AT FS 574.00 REPAIRED IAW REO 601R-53-61-1741. ( A) 2 L 7 2 4F RT A21EA 20080807 EA 2008 8 7 COMA0860322 1 20080713 A 3350 OL3071BPEGPL LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 27 712CA 7244 FLIGHT 5416. GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMPS. (A) 2 L 7 2 4F RT A21EA 20080807 NM 2008 8 7 AALA200801466 1 20080602 A 3350 0202226001 SHROUD BOEING 767 767223 1385123 NM EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 321AA 22322 LAX - EMERGENCY LIGHT AT SEAT 20B SHROUD DAMAGED. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 20B. SYSTEM GROUND CHECK ED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080807 NM 2008 8 7 AALA200801383 1 20080524 A 3350 LIGHT BOEING 757 757223 1384957 NM ROW 31 ABC INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 640A 24598 DFW - EMERGENCY LIGHT AT SEAT ROW 31ABC INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 31ABC. SY STEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 NM 2008 8 7 08FDEA02629 1 20080702 A 5320 652558116 ANGLE BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 PANEL NR 3338 HAS FRETTING CORROSION AROUND EDGE AT MOUNT HOLE. REMOVED CORROSION, ORIGINAL THICKNESS .036". REMOVED . 010", .026" REMAINING. MATERIAL IS OUT OF LIMITS REF SRM 53-10-1 PG 1 DETAIL 1. FABRICATED NEW STIFFENER ANGLE 7075-O- .040, HEAT TREATED TO T-6. REF DWG 65-25581, DOCUMENT 65-25581 REV C. TREATED AND PRIMED AND PAINTED. THIS IS CLASS IFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080808 WP 2008 8 8 08FDEA02771 1 20080709 A 5330 ADA02201 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 DURING INSPECTION EXT FUSELAGE LWR SURFACE FOUND DEEP DENT AND NICK 3 INCH BY .75 INCH DEEP .047 INCH ON SKIN. 2 L 7 3 4F RT A22WE 20080819 EA 2008 8 19 SWIA200819885 1 20080719 A 3297 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 427SW 7497 UPON GEAR RETRACTION, RECEIVED A GEAR DISAGREE. NOSE GEAR REMAINED DOWN AND LOCKED. (FLIGHT NR 3981) REPLACED GEAR DOO R SWITCH HARNESS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080819 NM 2008 8 19 UPS08M53034 1 20080721 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 10 RT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED AND INSTALLED RE PAIR BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 EA 2008 8 19 SWIA200819910 1 20080730 A 3040 HEATING ELEMENT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT WINDOW FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 07 935SW 7725 SMOKE COMING FROM LT WINDOW HEAT BLOCK AND RECEIVED A LT WINDOW HEAT CAUTION MESSAGE. TURNED OFF LT WINDSHIELD HEAT. (F LIGHT 6380) REPLACED CAPTAINS SIDE WINDOW IAW CRJ MM 56-12-01. P/N NP-139322-11 S/N OFF 08012H2159. 2 L 7 2 4F RT A21EA 20080819 NM 2008 8 19 NWAA083375534 1 20080718 A 5414 SKIN BOEING 757 757251 1384970 NM NR 2 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 543US 26490 DURING ENG CHANGE FOUND CRACK IN NR 2 PYLON RT SIDE SKIN AT NAC STA 132. REPAIRED PER EA 55-212961. (S) 2 L 7 2 4F RT A2NM 20080819 NM 2008 8 19 NWAA083596308 1 20080804 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN INCORRECT A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 668US 24223 LT OVERWING EXTERIOR EMERGENCY LIGHT AFT POSITION INOPERATIVE. MAINTENANCE CORRECTED WIRING TO LIGHT ASSEMBLY L1166. O PERATIONAL CHECKED GOOD, AND ACFT WAS RETURNED TO SERVICE. (S) 2 L 7 4 4F RT A20WE 20080819 WP 2008 8 19 NWAA083629857 1 20080802 A 3397 WIRE DOUG DC9 DC951 3022051 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 766NC 47739 DURING LINE CHECK, MAINTENANCE FOUND THAT THE RED EMERGENCY LIGHT AT SEAT 13D IS INOPERATIVE DUE TO BROKEN WIRES IN THE OUTER SEAT TRACK. MAINTENANCE REPAIRED BROKEN WIRES AND THE LIGHT RETURNED TO AN OPERATIONAL CONDITION. (S) 2 L 7 2 4F RT A6WE 20080819 EA 2008 8 19 SWIA200819863 1 20080713 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 435SW 7555 EMERGENCY FLOOR LIGHTING AFT OF ROW 8 IS INOPERATIVE. (FLIGHT NR 3831) REPLACED FLOOR LIGHTING CONNECTOR AS REQUIRED. O PS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080819 EA 2008 8 19 SWIA200819927 1 20080804 A 3230 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG FAILED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 454SW 7749 RECEIVED A GEAR DISAGREE MASTER WARNING. MANUALLY EXTENDED GEAR. (FLIGHT NR 3856) REPLACED NOSE DOOR SELECTOR VALVE IA W MM 33-22-20 AND LANDING GEAR CONTROL HANDLE IAW MM 32-31-01. PN 750006000 S/N OFF 0034IP/N OFF 7-45502-5 S/N OFF 1182 . 2 L 7 2 4F RT A21EA 20080819 WP 2008 8 19 UPS08852999 1 20080707 A 5411 STRINGER DOUG DC8 DC871F 302199D WP NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C2 NR 1 ALT STRINGER -54 CACKED APPROX. AT XRS 480- NR1 PYLON FABBED AND INSTALLED REPAIR IAW SRM, 51-1 -8, 51-1-20D, 51-3-00. 2 L 7 4 4F RT 4A25 20080819 EA 2008 8 19 SWIA200819922 1 20080731 A 2150 ACM CNDAIR CL600 CL6002C10 1390015 EA LEFT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 774SK 10240 BURNING ODOR REPORTED IN FLIGHT DECK AREA. (FLIGHT NR 6630) REPLACED LT AIR CYCLE MACHINE IAW 21-51-08. OPS AND LEAK CH ECK GOOD. PN: GG670-95009-1 S/N OFF: 1042. 2 L 7 2 4F RT A21EA 20080819 NM 2008 8 19 UPS08M53035 1 20080722 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 33 RT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED AND INSTALLED RE PAIR BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 EA 2008 8 19 SWIA200819869 1 20080715 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* 30015 NE PAX DOOR OUT OF ADJUST A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 492SW 7168 PAX DOOR IS HARD TO OPEN FROM OUTSIDE. (FLIGHT NR 4091) ADJUSTED INNER HANDLE RETENSION MECHANISM IAW AMM 52-11-00. PAX DOOR OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA 20080819 SO 2008 8 19 SWIA200819870 1 20080710 A 3520 OXYGEN MASK EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE ROW 7 UNWANTED DEPLOY A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 236SW 120312 THE O2 MASK AT ROW 7 DROPPED IN FLIGHT. (FLIGHT NR 5473) INSPECTED AND RESTOWED O2 MASKS AS REQUIRED. 2 L 7 2 4T 4 T RT A31SO E20NE 20080819 EA 2008 8 19 SWIA200819871 1 20080716 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 464SW 7827 RT WINDOW HEAT CAUTION MESSAGE ON CLIMB OUT. (FLIGHT NR 4018) REPLACED RT SIDE WINDOW IAW 56-12-01. OPS AND LEAK CHECK GOOD. P/N NP-139322-6, S/N OFF 04056H6501. 2 L 7 2 4F RT A21EA 20080819 NM 2008 8 19 UPS08553007 1 20080730 A 5320 SUPPORT BOEING 757 75724APF 1384969 NM BS 645-765 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 INSPECTION TYPE-2C, FWD CARGO COMP, RT FLOOR TO SIDEWALL SUPPORT IS CORRODED AT TIE DOWN F FITTINGS BS 645-765.5. REMOV ED AND REPLACED IAW SRM 51-40-02-0G, DRW NR 143N5366. 2 L 7 2 4F RT A2NM 20080819 NM 2008 8 19 UPS08M53025 1 20080717 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 30 LT BARREL NUT BORE HOLE REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080808 NM 2008 8 8 08FDEA02774 1 20080709 A 5340 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 601FE 48401 MAIN DECK CARGO DOOR LOWER JAMB SPOOL FITTING NR 1 FOUND HOLES A, B, C AND D OVERSIZED TO 0.520 INCH. 2 L 7 3 4F RT A22WE 20080808 NM 2008 8 8 08FDEA02776 1 20080709 A 5340 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 601FE 48401 MAIN DECK CARGO DOOR LOWER JAMB SPOOL FITTING NR 5 FOUND HOLES A, C AND D OVERSIZED TO 0.520 INCH. 2 L 7 3 4F RT A22WE 20080808 NM 2008 8 8 08FDEA02780 1 20080709 A 5320 69459473 SUPPORT BRACKET BOEING 727 727233 138408A NM NLG WW CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 CORROSION AROUND BOLT HOLE AT STA 340 FITTING SUPPORT BRACKET JUST BEHIND NOSE WHEEL WELL LT SIDE. REMOVED FITTING SUPP ORT AT STA 340 AFT OF NOSE WHEEL WELL LT SIDE. TREATED AND PRIMED NEW SUPPORT FITTING REF SRM 51-30-2 PG 1-20 AND MM 51 -20-7. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080808 EU 2008 8 8 08FDEA02783 1 20080709 A 5754 A53510219203 SUPPORT AIRBUS 300 A300B4622R 3930312 EU KRUEGER FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORRODED SUPPORT ON RT KRUEGER FLAP STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02520 1 20080627 A 5321 B5327046501400 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 232 NG IS CRACKED AND CRUSHED. FABBED FLOOR PANEL; POTTED EDGES, CURED, SANDED, POTTED INSE RTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02521 1 20080627 A 5321 B5327047601600 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 232AH IS CRACKED ACROSS. FABBED A NEW FLOOR PANEL, POTTED EDGES, CURED, SANDED, POTTED INSE RTS, APPLIED NON SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005, REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02514 1 20080627 A 5321 B5327047801600 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 CABIN FLOOR BOARD NR 242 BF HAS A BROKEN CORNER. FABRICATED A NEW PANEL NR 242 BF; LOCATED THE HOLES FROM THE OLD PANEL ; COUNTEREDBORED AND POTTED INSERTS; POTTED EDGES; CURED AND SANDED; APPLIED ANTI-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02785 1 20080709 A 5330 6554575 SKIN BOEING 727 727225 1384077 NM BS 727D S19L WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 LT LOWER FUSELAGE JUST FWD OF LT LANDING LIGHT, BS 727D 14 STR19L, SKIN LAP HAS WEAR REMOVED DAMAGED AREA. REMOVED INTE RNAL REPAIR, FABRICATE SKIN DOUBLER AND FILLER. TREATED, PRIMED AND INSTALLED REPAIR. REF SRM 53-30-3 FIG 5, SRM 51-30 -02 PG 1-10. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080808 NM 2008 8 8 08FDEA02788 1 20080709 A 5330 65545803 SKIN BOEING 727 727225 1384077 NM ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 CHAFE MARKS ON FUSELAGE SKIN FROM WING-TO BODY FAIRING ATTACH SCREWS, RT SIDE OF FUSELAGE BS 950D 9 TO 950D 12 BLENDED O UT DAMAGE. REF SRM 53-30-1 DETAIL 1. ORIGINAL THICKNESS .140 INCH, REMOVED .037 INCH REMAINING THICKNESS .103 INCH OU T OF LIMITS. REF SRM 53-30-1 PG 2A DETAIL 1. REPAIRED SKIN BY INSTALLING A DOUBLER. REF FED EX EA NR 7-5330-114002. ALODINED AND PRIMED. REF SRM 51-10-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080808 NM 2008 8 8 08FDEA02792 1 20080709 A 5754 SKIN BOEING 727 727227 1384078 NM NR 1 SLAT DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 NR 1 SLAT UPPER SURFACE HAS ONE DENT AT WS 760. 2 L 7 3 4F A3WE 20080808 EU 2008 8 8 08FDEA02732 1 20080708 A 5730 A57240188 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND OLD DOUBLER REPAIR ON LT WING TOP SKIN, TRAILING EDGE, RIB 18-19 WITHOUT ANY OLD DOCUMENTATION. DOUBLER REPAIR RE NEWED IAW RAS/BAE/1007270/2008 ISS A, APPROVED BY EA 6-5751-120109 . 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02733 1 20080708 A 5310 A53611192204 WINDOW FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION IN 7 FASTENER HOLES OF WINDSHIELD FRAME LT/RT. REPAIR PERFORMED BY OVERSIZING OF HOLES, NDT FOR CRACK F REE CONDITION AND INSTALLING NEW FASTENER IAW RAS 70507106/2008 ISS A, APPROVED BY EA 6-5311-120048. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02737 1 20080708 A 5313 A53971007220 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON STRINGER P 51 LT, C 54.2-57.1 REPAIR PERFORMED BY CUT THE FRAME 54.3 TO INSTALL NEW STRINGER PROFILE, PERFORM SPLICE REPAIR AT STRINGER AND FRAME IAW RAS/EFW/9000058/2008 ISS C, APPROVED BY EA 6-5316-123001. 2 L 7 2 4F RT A35EU 20080808 WP 2008 8 8 08FDEA02800 1 20080709 A 5320 AEA00246 INTERCOSTAL DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 RIGHT MLG WW AFT BULKHEAD AT L 36R WEB IS CORRODED AT THE STANSION. REMOVED AND REPLACED THE INTERCOSTAL IAW DC/MD-10 S RM 51-35-01; VOL II. FABRICATED A NEW INTERCOSTAL IAW DAC DWG NR AEA 0027, REV S. ALODINED AND PRIMED IAW DC/MD-10 SR M 51-21-01; VOL II. PART MARKED INTERCOSTAL P/N FX - AEA0024-6 IAW FEDEX GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20080808 WP 2008 8 8 08FDEA02801 1 20080709 A 5320 AEA00266 INTERCOSTAL DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 RIGHT MLG WW AT FS 1521; INTERCOSTAL NEXT NEXT TO THE FLAPS BUSS PULLEYS IS CORRODED. REMOVED AND REPLACED THE INTERC OSTAL IAW DC/MD-10 SRM 51-35-01; VOL II. FABRICATED A NEW INTERCOSTAL IAW DAC DWG AEA0026, REV M. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01; VOL II. PART MARKED INTERCOSTAL P/N FX - AEA0026-6 IAW FEDEX GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20080808 NM 2008 8 8 08FDEA02637 1 20080702 A 5313 6554574 STRINGER BOEING 727 727225 1384077 NM BS 720A-720B CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 LOWER SIDE SURFACE ON STR 8L AT 720A 10 INCH TO FS HAS AREAS OF SURFACE CORROSION REMOVED CORROSION BY BLENDING, NDT FOU ND BLENDED AREA TO BE WITHIN LIMITS WITH ORIGINAL BEING .045". BLENDED AREA TO BE AT .041' ON LOWER SURFACE ON STR 8L A T FS 720A 10 INCHES REF SRM 53-10-1 FIG 1, WORK ACCOMPLISHED ON EA NR 7-5310114005, LEVEL 1 CORROSION THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080808 NM 2008 8 8 08FDEA02467 1 20080625 A 5720 6483372 ANGLE BOEING 727 727227 1384078 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 RT WING L/E STA 90 VERTICAL ANGLE CRACKED LWR SIDE. FABRICATED REPAIR ANGLE FILLER FROM 7075-T6 .050 PO NR 9007294 DIMS 7 INCH BY 2 1/2 INCH, FILLER 2 INCH BY 1 INCH. INSTALLED REPAIR PARTS AT RT WING LE STA 90 IAW SRM 51-40-3 FIG 1, SRM 57-20-2 FIG 1 AND SRM 51-30-2. 2 L 7 3 4F A3WE 20080808 WP 2008 8 8 08FDEA02471 1 20080625 A 5315 FLOORBEAM DOUG MD10 MD1010F 3022112 WP BS 1701 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 383FE 46616 FOUND THE REPAIR LOCATED IN THE CENTER PIT FLOORBEAM LOWER CARGO FLANGE AT STA 1701; RBL 28 TO RBL 39 REQUIRES EVALUATIO N FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EVALUATED REPAIR AND FOUND NOT TO COMPLY WITH FAA APPROVED DATA. REPAIRED CENTER PIT FLOORBEAM IAW DC/MD-10 SRM 53-60-01; VOL I; FIG 3. 2 L 7 3 4F RT A22WE 20080808 EU 2008 8 8 08FDEA02480 1 20080625 A 5347 A5327040500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN DECK FLOOR SEAT TRACK HAS CORROSION; C76 - C77; BL 00 (2 SPOTS). BLENDED THE CORROSION AND CHECKED THE LIMITS IAW A300-600 SRM 53-10-16; FIG 102. FOUND THE SEAT TRACK TO BE OUT OF LIMITS. SEAT TRACK REPLACED ON NON-ROUTINE N00576 FROM FRAMES C 73 - C 80. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02483 1 20080625 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN DECK FLOOR SEAT TRACK HAS CORROSION; C78; BL00. BLENDED THE CORROSION AND CHECKED THE LIMITS IAW A300-600 SRM 53- 10-16; FIG 102. FOUND THE SEAT TRACK TO BE OUT OF LIMITS. REMOVED THE OLD SEAT TRACK FROM FRAME C73 - C80 AND INSTALLE D A NEW TRACK IAW A300-600 SRM 51-41-21. MATERIAL ID FOR THE NEW TRACK A5327400500053, PO 617760.1 IAW A300-600 SRM 53- 18-16. FABRICATED A NEW SEAT TRACK IAW AIRBUS DWG A53279239200. ALODINED, PRIMED AND PAINTED IAW A300-600 AMM 51-75-10 -8. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02746 1 20080708 A 5312 A53810967200 PRESSURE PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND NICK IN PRESSURE MEMBRANE AT C 51, TRACK 5, RT REPAIR PERFORMED BY SMOOTH REWORK, NDT FOR CRACK FREE CONDITION IAW RAS 70511614/009/2008 ISS A , APPROVED BY EA 6-5315-120080. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02747 1 20080708 A 5340 A53974224218 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION AT CLIP C 68, P 56-57 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02749 1 20080708 A 5340 A53973177255 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION AT CLIP C 64, P 55-56 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02750 1 20080708 A 2750 ROLLER BOEING 727 727227 1384078 NM TE FLAPS OUT OF ADJUST A FDEA A UNSCHED LANDING E VIBRATION/BUFFET DE DESCENT 1 CE 21 481FE 21463 ON DESCENT TO IAD AIRFRAME BUFFET AT 290 KNOTS 270FL FOLLOWED QRH AT 14,000 250 KTS NO BUFFET FELT. FLAPS 15 DEGREES L ANDING ACCOMP FOR WING LEVEL NEED 1/2 UNIT OF TRIM RUDDER. CONTROL WHEEL SHOWED 35 DEGREES RIGHT WITH NO TRIM. OPS CHE CK SPOILERS ALL DEPLOY EVENLY AND NO EVIDENCE OF FLUID BYPASS. WHILE TURNING CONTROL COLUMN WHEEL INSPECTED CABLES AND QUARDRUM: NO OBVIOUS DEFECTS FOUND. LOWERED FLAPS AND VISUALLY INSPECTED ROLLERS AND TRACK: ALL LOOKED OK. PHYSICALLY LIFTED ON FLAPS AND FOUND LEFT OUTBOARD AFT FLAP EXCESSIVE PLAY. ADJUSTED DEAD WEIGHT ROLLER ECCENTRIC AND OUTBOARD RO LLERS ECCENTRIC IAW MM 27-51-012-4. OPERATED FLAPS AND OPS CHECKED GOOD. 2 L 7 3 4F A3WE 20080808 WP 2008 8 8 08FDEA02716 1 20080705 A 3240 BRAKE DOUG MD10 MD1010F 3022112 WP NR 3 FIRE A FDEA O OTHER B A SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE TX TAXI/GRND HDL 1 CE 21 363FE 8178 4 48263 NR 3 BRAKE CAUGHT ON FIRE AT GATE. REMOVE AND REPLACE NR 3 BRAKE IAW MD-10 MM 32-43-01-4, ALSO INSPECTED ADJACENT AREA FOR DAMAGE AND NO DAMAGE NOTED. 2 L 7 3 4F RT A22WE 20080808 NM 2008 8 8 08FDEA02639 1 20080703 A 5320 146N5417U11 FLOOR SUPPORT BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FLOOR SUPPORT FROM BS 1340 TO BS 1445, LBL 3, 6, 11, 16 HAVE CORROSION AROUND NUTPLATE HOLES. CORROSION REMOVED. FOUND EXCEEDED ALLOWABLE LIMITS IN B757-200 SRM 51-10-02. REMOVED AND REPLACED STRINGER IAW B757-200 SRM 51-10-02 AND SRM 5 1-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080808 NM 2008 8 8 08FDEA02642 1 20080703 A 5320 164N544419 FLOOR SUPPORT BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FLOOR SUPPORTS FROM BS 1445 TO BS 1640, LBL 3, 6, 11, HAVE CORROSION AROUND NUTPLATE HOLES. CORROSION REMOVED AND FOUND EXCEEDED ALLOWABLE LIMITS IN B757-200 SRM 51-10-02. STRINGER REPLACED IAW B757-200 SRM 51-10-02 AND SRM 51-40-02 REV 9 3. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080808 EU 2008 8 8 08FDEA02645 1 20080703 A 5320 B5327080000000 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN CARGO DECK FLOOR PANEL 232 CF IS CRACKED. FABBED A NEW FLOOR PANEL IAW FEDEX DWG SRZ 25-005; REV F. MATERIAL ID A 402 H35039-003 IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02803 1 20080710 A 5330 A53812189201 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON SKIN PANEL C 39-40, P 39-40 RT. REPAIR PERFORMED BY CORROSION REWORK AND INSTALLING A DOUBLER AND SH IMS IAW RAS/70511475/007/2008 ISS A, APPROVED BY EA 6-5315-120075. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02809 1 20080710 A 5414 311N504651 SKIN BOEING 757 75727B 1384921 NM ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 916FD 24137 SURFACE CORROSION FOUND ON PYLON NUMBER ONE LEFT SIDE INNER SKIN AFT OF ACCESS PANEL 433CL. EVALUATE AND RECTIFY. REPL ACED LEFT SIDE INNER SKIN AFT OF ACCESS PANEL 433CL OF PYLON NUMBER ONE IN ACCORDANCE WITH BOEING DRAWING 311N5046, BOEI NG DRAWING 311N5002, AND B757-200 SRM 51-10-02 REV 93. REPAIR CLASSIFIED AS MAJOR PER FEDEX GMM 6-02-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080808 EU 2008 8 8 08FDEA02596 1 20080701 A 5100 NONE AIRBUS 300 A300B4622R 3930312 EU NONE NONE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND OLD SPLICE REPAIR IN AFT CARGO COMPARTMENT AT C 63 LT, BETWEEN Y 805 AND Y 1470 WITHOUT ANY OLD DOCUMENTATION. NE W SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG.207 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02599 1 20080527 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU RT WING TE FLAP MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 721FD 477 PREVIOUS REPAIR FOUND LOCATED ON INBD FLAP RT, RIB 24B, LOWER AND TOP SKIN T/E. REPAIR REQUIRES EVALUATION FOR MAJOR MI NOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO EXISTING SRM REPAIR. NEW REPAIR WAS ACCOMPLISHED IAW EA 6-5710-121641. 2 L 7 2 4F RT A35EU 20080819 NM 2008 8 19 UPS08M52988 1 20080430 A 5753 SKIN DOUG MD11 MD11F 3023600 NM RT WING TE FLAP WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT WING IB FLAP CTR VANE TRACK CUTOUT SKIN FOUND WORN AS MARKED. REMOVED RT WING IB FLAP VANE IAW AM M27-50-22 REV 53. DAMAGED AREA ON RT WING IB FLAP CTR VANE TRACK CUTOUT SKIN AREA TRIMMED OUT IAW EN NR 1176-08.HF EC I NSP C/O ON TRIMMED OUT AREA FOUND NO CRACK EVIDENT. NEW REPAIR DOUBLER & REPAIR FILLER FAB IAW EN NR 1176-08.NEW FAB RE PAIR DOUBLER & FILLER INSTALLED AT RT WING IB FLAP CTR VANE TRACK CUTOUT AREA IAW EN NR 1176-08. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M53037 1 20080721 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 16 RT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED AND INSTALLED REPAI R BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 EU 2008 8 19 TRAX200800956 1 20080802 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 640AS 405 A/S/D EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED A/S/D EMERGENCY FLOOD LIGHT IAW ATR 72 AMM 33-51-24. PERFORMED OPS CHECK OF THE EMERGENCY LIGHTING SYSTEM IAW ATR 72 AMM 33-51-24. NO DEFECTS FOUND. (S) 2 H 7 2 4T RT 20080819 NM 2008 8 19 UPS08M53015 1 20080710 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 11 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING AND INSTALL ED BUSHING IAW EO MD11-5510-19409-N AND SAA TRAVELER 80538310001. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 UPS08552872 1 20080716 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM BS 1510 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 421UP 25281 INSPECTION TYPE-2C, CORROSION AFT CARGO BAY ON FLOOR SUPPORT STA 1510 RBL 2.5. REMOVED AND REPLACED FLOOR SUPPORT IAW S RM 53-00-53-1A, SRM51-40-02-0G. 2 L 7 2 4F RT A2NM 20080818 WP 2008 8 18 UPS08852625 1 20080609 A 5320 CHANNEL DOUG DC8 DC871F 302199D WP MAIN CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, FLOOR PANEL NR680 HAS SMALL 3 STIFFENERS CRACKED AS MARKED. FABRICATED AND REPLACED 3EA CRACKED HAT CHANNELS IAW SRM 51-1-4 AND DWG NR 52755898, DWG NR 3619352. ALSO FOUND FLOORBOARD CORRODED OUT OF LIMITS. FABRICATED NEW FLOORBOARD IAW SRM 51-1-4, DWG NR 52755898, AND DWG NR 3619352. 2 L 7 4 4F RT 4A25 20080818 NM 2008 8 18 UPS08M52941 1 20080715 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 3 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INST ALLED BUSHING IAW UPS EO, MD11-5510-19409-N AND SAA TRAVELER 80538520001. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 UPS08552952 1 20080706 A 5320 FLOOR SUPPORT BOEING 757 75724APF 1384969 NM BS 1023 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 457UP 25478 INSPECTION TYPE-C2, CORROSION ON LONGITUDINAL BEAM, LBL 25, BS 1023, WL 208. ENGINEERING ISSUED TO INSTALL REPAIR DOUBL ER'S DUE TO CORROSION BLENDS BEING OUT OF LIMITS. 2 L 7 2 4F RT A2NM 20080818 NM 2008 8 18 UPS08M52959 1 20080708 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 36 RT BARREL NUT BORE HOLE AND BOTTOM SURFACE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING IAW EA 011-5510-01-A1472, EO 5510-30129-A, AND EO 5510-19409-N. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 SWAA084023 1 20080719 A 2560 PH22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 17 DEF. R&R STRIP PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084028 1 20080717 A 3350 311500 LENS BOEING 737 7375H4 138449D NM EMERGENCY LIGHT DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 L2 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084029 1 20080721 A 5753 SKIN BOEING 737 7375H4 138449D NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED BRDG CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED AT OUTBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084039 1 20080717 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 LT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084044 1 20080721 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 727A S5L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED A TBS 727A, STR 5L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084046 1 20080721 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 727E S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED A TBS 727E, STR 8L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084074 1 20080722 A 2560 65C34691 GIRT BAR BOEING 737 7377H4 1384404 NM R1 DOOR DIRTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 232WN 32500 R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STUCK WILL NOT LOCK. CLEANED GIRT BAR PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084087 1 20080723 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 418WN 29823 DURING SCHEDULED MV2 CHECK, FOUND LH FWD CABIN EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084092 1 20080723 A 5311 6546532 FRAME BOEING 737 7373Q8 1384670 NM BS 480 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA . 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084091 1 20080723 A 5311 6546555 FRAME BOEING 737 7373Q8 1384670 NM BS 867 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084105 1 20080722 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM BS 947 S24-25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947.5, BETWEEN STR 24R AND STR 25R. REPAIRE SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084123 1 20080724 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM BS 947 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080819 SO 2008 8 19 SWIA200819903 1 20080725 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 226SW 120296 LT WINDSHIELD CRACKED. (FLIGHT NR 5416) INSTALLED WINDOW IAW EMB 120 MM 56-11-01. 2 L 7 2 4T RT A31SO 20080819 EA 2008 8 19 S9BA2008027 1 20080806 A 5413 C6W1512S142 LONGERON DHAV DHC6 DHC6300 2802606 EA LT NACELLE CRACKED A S9BA O OTHER O OTHER NR NOT REPORTED 1 SO 29 533SW 4 533 LT ENG NACELLE INBOARD LONGERON CRACKED 10.5 INCHES AFT OF THE FWD END. REMOVED AND REPLACED LT ENG INBOARD LONGERON IA W AC 43.13-1B CH 4, RD 6-54-036. (S) 1 H 7 2 3T RT A9EA 20080819 SO 2008 8 19 SWIA200819883 1 20080405 A 5520 ROD END EMB 120 EMB120ER 3260203 SO ELEVATOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 292SW 120319 LT AND RT ELEVATOR UPPER BELLCRANK ROD ENDS SHOW SIGNS OF CORROSION. (FOUND AT C-CHECK) REPLACED THE LT AND RT ELEVATOR ROD END ASSEMBLIES IAW AMM 27-00-00. 2 L 7 2 4T RT A31SO 20080819 EU 2008 8 19 NWAA083643305 1 20080801 A 3350 BATTERY AIRBUS 330 A330323 3930335 EU CABIN FAULTY A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 805NW 00552 PERFORMING EMERGENCY LIGHTS OPERATION CHECK, EPSU 12WL & 15 WL FAULTS BATTERY. REPLACED BATTERY OF EPSU 12WL & 15WL, TE STS OK (L/P 2908998, 2909005). (S) 2 L 7 2 4F RT A46NM 20080819 2008 8 19 SWIA200819911 4 20080727 A 3425 6229336400 COMPUTER CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE NR 2 AHRS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 07 765SK 10231 CIRCUIT BREAKER 2K4 POPPED AND RECEIVED A PITCH FEEL FAULT MESSAGE, A YAW DAMP 2 MESSAGE AND WAS UNABLE TO RESET AUTOPIL OT. (FLIGHT NR 6424) REPLACED NR 2 AHRS COMPUTER WITH SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080819 SO 2008 8 19 SWIA200819873 1 20080503 A 5753 STRUCTURE EMB 120 EMB120ER 3260203 SO NACELLE FLAP CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 LT NACELLE FLAP HAS AN INTERNAL CRACK. (FOUND AT C-CHECK) REPLACED LT NACELLE FLAP IAW MM 27-50-03. 2 L 7 2 4T RT A31SO 20080819 SO 2008 8 19 SWIA200819878 1 20080421 A 2720 ROD END EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE RUDDER CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 301YV 120301 RUDDER II ROD ENDS HAVE SURFACE CORROSION. (FOUND AT C-CHECK) REPLACED UPPER AND LOWER RUDDER II CONTROL ROD ENDS IAW A MM 27-21-02 2 L 7 2 4T 4 T RT A31SO E20NE 20080819 SO 2008 8 19 SWIA200819879 1 20080421 A 5210 FRAME EMB 120 EMB120ER 3260203 SO PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 301YV 120301 PAX DOOR FWD AND AFT MID CORNERS ARE CRACKED. (FOUND AT C-CHECK) REPLACED FRAME AND INSTALLED DOUBLERS IAW SRM 120 52-1 0-02. 2 L 7 2 4T RT A31SO 20080819 EA 2008 8 19 SWIA200819868 1 20080713 A 5210 LATCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 495CA 7774 PASSENGER DOOR WILL NOT CLOSE COMPLETELY. (FLIGHT NR 2678) REPLACED LATCH LOCK ASSEMBLY IAW MM 52-12-01. OPS AND RIG CH ECKS GOOD. 2 L 7 2 4F RT A21EA 20080819 WP 2008 8 19 UPS08853000 1 20080616 A 5100 NONE DOUG DC8 DC871F 302199D WP SCHEDULED MAINT NONE A IPXA O OTHER O OTHER NR NOT REPORTED 1 SO 01 752UP 45952 INSPECTION TYPE-C2, COMPLY WITH MPI 19584 REGARDING REPLACEMENT OF EXISTING REPAIR AT AT L28R IAW WAN3 1369154 AND EO DC 8-5330-20248-E APPX.E FABBED AND INSTALLED REPAIR DOUBLER IAW, EA NR 008-5330-01-A1449, SRO 853 0032. NOT AN SDR. 2 L 7 4 4F RT 4A25 20080819 EU 2008 8 19 UPS08153051 1 20080723 A 5321 B5327073900000 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CARGO BAY DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 153UP 0839 INSPECTION TYPE-5YR, MAIN CARGO COMPT FLOOR PNL 231GH AT FR27 LT SIDE, FOUND DELAMINATED. REPAIRED MAIN CARGO COMPT FL OOR PNL 231GH AT FR27 LT SIDE REF SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02694 1 20080704 A 5420 R54610314 STRAP AIRBUS 300 A300B4622R 3930312 EU ZONE 400 UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND OLD REPAIR ON RT AFT PYLON BOX NOT PERFORMED IAW DRAWING R546-10314. REPAIR RENEWED IAW DRAWING R546-10314 AND RA S 034632/010/2004 ISS A, APPROVED BY EA 6-5451-120101. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02695 1 20080704 A 5730 A57340085206 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION ON LT WING TOP SKIN, REAR SPAR AREA RIB 25-29 REPAIR PERFORMED BY BLEND OUT CORROSION, NDT FOR CRACK FRE E IAW RAS/BAE/1007272/2008 ISS A, APPROVED BY EA 6-5720-120108. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02650 1 20080703 A 5415 A5461254620095 FITTING AIRBUS 310 A310203 3930313 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 423FE 281 NR 1 ENGINE PYLON SPIGOT RECEPTICLE FITTING BEARING RACE CORRODED. REMOVED LEVEL 1 CORROSION, REMOVED AND REPLACED NR 1 ENGINE PYLON UPPER AND LOWER SPIGOT FITTINGS IAW FEDEX EA 6-5450-121272, RELEASE DATE 20 MAY, 2008. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02515 1 20080627 A 5321 A5228536900300 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 222QF IS CRACKED. FABBED A NEW FLOOR PANEL; POTTED THE EDGES; CURED; SANDED; POTTED INSERT S; APPLIED THE NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02601 1 20080701 A 5313 A53974527228 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION AT STRINGER P 57, C 65-72 OUT OF LIMIT STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02696 1 20080704 A 5411 A54611750 SPAR AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CRACK ON PYLON NR 2 LOWER SPAR UPPER SURFACE, RIB 10A. REPAIR PERFORMED IAW DRAWING R546-10344 AND RAS/70507447/0 04/2008 ISS A, APPROVED BY EA 6-5450-120039. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02607 1 20080701 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU TE FLAP UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD FH1126 630 FOUND OLD FLUSH DOUBLER REPAIR ON LT OUTER FLAP NOSE SKIN RIB 11-13 NOT PERFORMED IAW SRM 57-50-00 FIG 208. FLUSH DOU BLER REPAIR RENEWED IAW SRM 57-50-00 FIG 208. 2 L 7 2 4F RT A35EU 20080807 WP 2008 8 7 AALA200801744 1 20080701 A 2560 BATTERY DOUG DC9 DC982 3022082 WP FLASHLIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 431AA 49343 LGA - EMERGENCY FLASHLIGHT AT RT AFT CABIN NOT CHARGING. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT RT AFT CABIN. SY STEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080807 NM 2008 8 7 AALA200801516 1 20080604 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 762AN 31479 DFW - EMERGENCY LIGHTS AT SEAT 21G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 NM 2008 8 7 AALA200801526 1 20080604 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 762AN 31479 DFW - EMERGENCY LIGHTS AT SEAT 21C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 NM 2008 8 7 CALA0800719 1 20080716 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM BS 747 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16647 28908 LEFT SIDE STA 747 FRAME CRACKED BETWEEN S-8 AND S-9 AT AIR CONDITIONING (A/C) BRACKET. REMOVED A/C RAIL BRACKET CUTOUT DAMAGED AREA AND REPAIRED FRAME AT STA 747 LT BETWEEN S-8 AND S-9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080807 EA 2008 8 7 COMA0860320 1 20080703 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FS 202 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 963CA 7127 CRACK ON FS 202 AROUND PARKING BRAKE CABLE. REPAIRED CRACK ON FS 202 AROUND PARKING BRAKE CABLE IAW EA 10-5311-01914. (A) 2 L 7 2 4F RT A21EA 20080807 NM 2008 8 7 AALA200801488 1 20080602 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 780AN 29956 DFW - EMERGENCY LIGHT AT SEAT 40G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 40G. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080807 NM 2008 8 7 AALA200801365 1 20080522 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 617AM 24525 LAX - EMERGENCY LIGHTS AT SEAT 9D AND 15D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT 9D AND 15D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080807 WP 2008 8 7 AALA200801498 1 20080603 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 982TW 53632 SFO - EMERGENCY LIGHT AT SEAT 27D INOPERATIVE. RECONNECTED SIDEWALL CONNECTOR FOR EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A6WE 20080807 NE 2008 8 7 AALA200801371 2 20080522 A 7230 BLADES DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 1 ENGINE DAMAGED A AALA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 21 446AA 49472 709715 ABQ INFLIGHT T526/22MAY. NR ONE ENGINE EXPERIENCED BIRD STRIKE ON TAKEOFF. RETURNED TO ABQ AND LANDED WITHOUT INCIDENT . REPLACED THREE PAIRS OF BLADES. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F 4 F A6WE E9NE 20080807 EU 2008 8 7 F3LA200800497 1 20080715 A 5321 D5367301900000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 943FR 18 2518 DURING C2 C CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 161UG WAS PUNCTURED. MAINTENANCE RECORDED THAT THIS NO N ROUTINE HAS THE PANEL NUMBER INCORRECTLY INDICATED. THE DAMAGED PANEL IS 151UG. MAINTENANCE REPAIRED DAMAGE TO PANEL 151UG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECT ED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F 4 F RT A28NM E37NE 20080807 EA 2008 8 7 CHQA200800147 1 20080716 A 3260 PS11GA UPLOCK SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT MLG OUT OF ADJUST A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 638BR 7311 E872506 FLIGHT 5596, IAH TO BRO. AFTER TAKEOFF THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT WHEN THE GEAR WAS SELE CTED UP. THE GEAR LEVER WAS MOVED BACK TO THE DOWN POSITION AND THE LT MAIN LANDING GEAR INDICATED A RED UNSAFE CONDITI ON. THE GEAR FINALLY INDICATED DOWN AND LOCKED WHEN THE EMERGENCY EXTENSION WAS PERFORMED. THE ACFT THEN LANDED WITHOU T INCIDENT. MAINTENANCE WAS ABLE TO DUPLICATE THE FAULT WITH THE ACFT ON JACKS AND INSPECTED THE PROX SWITCHES ALONG WI TH THE PRIORITY VALVE, AND SELECTOR VALVE. THE UPLOCK PROX SWITCH FOR THE LT MAIN LANDING GEAR WAS IN NEED OF ADJUSTMEN T AND AFTER WHICH THE RETRACTION SYSTEM OPERATED NORMALLY. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080807 NM 2008 8 7 08FDEA02766 1 20080708 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 601FE 48401 MAIN DECK SEAT TRACK FLANGE UPPER SURFACE AT STA 1159, X = 8 FOUND CORROSION. 2 L 7 3 4F RT A22WE 20080807 NM 2008 8 7 08FDEA02767 1 20080708 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1281-1361 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 601FE 48401 MAIN DECK SEAT TRACK FLANGE AT STA 1281 TO STA 1361, X = -75.5 UPPER SURFACE FOUND CORROSION. 2 L 7 3 4F RT A22WE 20080808 NM 2008 8 8 08FDEA02769 1 20080708 A 5730 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 601FE 48401 05 FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING HFEC OPEN HOLE INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR C UTOUT. 2 L 7 3 4F RT A22WE 20080808 EU 2008 8 8 08FDEA02790 1 20080519 A 5330 A53811923206 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 721FD 477 PREVIOUS REPAIR FOUND LOCATED ON LT FUSELAGE, STA 4415-4521 AT FR 68-70 BETWEEN STGR 36-44 LT. REPAIR REQUIRES EVALUAT ION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR NOT IN AC CORDANCE WITH PREVIOUS APPROVED DATA. FEDEX EA 6-5330-121637, ISSUED TO COVER THE DISCREPANCIES, WAS COMPLIED WITH. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02631 1 20080702 A 5310 65219057 CREASE BEAM BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 MID CABIN CREASE BEAM WEB CRACKED AT STA 945, LBL 47, WL 208. REPLACED WEB REF SRM 51-30-02 PG 6, DRAWING NR 65-21905 . THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080808 EU 2008 8 8 08FDEA02740 1 20080708 A 5220 A53970890200 FRAME AIRBUS 300 A300B4622R 3930312 EU EMERGENCY EXIT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND SCRUB MARKS AT EMERGENCY EXIT, C 55, P14-15A, LT ON INNER FRAME FLANGE. REPAIR PERFORMED BY REWORK TO SMOOTH CONT OUR, NDT FOR CRACK FREE CONDITION AND FLAP PEENING IAW RAS/EFW/9000052/2008 ISS A, APPROVED BY EA 6-5316-123023. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02469 1 20080625 A 5753 A57960418200200 SKIN AIRBUS 300 A300F4605R 3930327 EU TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 LEFT CENTER FLAP LOWER SURFACE AFT OF THE INBD CARRIAGE IS DENTED. THE DENT IS OUT OF LIMITS; REPAIRED IAW A300-600 SRM 57-50-00; FIG 205; PGS 220 - 224. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02476 1 20080625 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN DECK FLOOR SEAT TRACK HAS CORROSION; C76-C77; RBL 32 (IN 2 SPOTS), SEAT TRACK FOUND TO BE OUT OF LIMITS. RECEIVED A NEW TRACK P/N A5327400500053; PO 617932.1 PER SRM 53-18-16; PGS 3 AND 9. LOCATED AND DRILLED THE NEW TRACK PER A30 0-600 SRM 53-10-16. INSTALLED TRACK PER A300-600 SRM 51-41-21. APPLIED CIC PER A300-600 AMM 51-22-00-0. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02748 1 20080708 A 5340 A53974221250 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION AT CLIP C 66, P 56-57 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02751 1 20080708 A 5320 25FX13541 RETAINER BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 MAIN DECK GILL LINER RETAINER RAIL, HOLE CRACKED, BS 1170 STR 8R REMOVED GILL LINER RETAINER RAIL, DRILLED UP NEW RETAIN ER RAIL, AND INSTALLED NEW RETAINER RAIL, IN REF TO SRM 51-30-2 PG 1-15 AND SRM 51-30-5 PG 5. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080808 NM 2008 8 8 08FDEA02811 1 20080710 A 5313 6518420450 STRINGER BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 STRINGER 5R CRACKED BOTH IND/UPPER AND INB/LOWER FLANGES AT STA 340 FWD LAV AFT WALL MOUNTS REMOVED DAMAGED SECTION OF S TRINGER, FABRICATED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS REF PART 1 OF EA 7-5310-113998. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080808 EU 2008 8 8 08FDEA02598 1 20080701 A 5320 A53974265200 PROFILE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORRODED CORNER PROFILE AT C 63-64, P 46 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02652 1 20080703 A 5311 6516526 FRAME BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 467FE 21449 TOOLING DAMAGE AT STA 783 FRAME JUST I/B OF STR 4R REMOVED DAMAGE PER SRM 53-10-4. FABRICATED REPAIR PARTS PER SRM 53-1 0-4. TREATED AND PRIMED PER SRM 51-30-02. INSTALLED REPAIR PER SRM 51-30-02 PG 1-13 AND 53-10-04. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080808 EU 2008 8 8 08FDEA02606 1 20080701 A 5100 NONE AIRBUS 300 A300B4622R 3930312 EU NONE NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 743FD 630 FOUND OLD SPLICE REPAIR IN FWD CARGO COMPARTMENT AT UPPER FLANGE C 38.2 RT WITHOUT ANY OLD DOCUMENTATION. REPAIR PERFOR MED BY REPLACEMENT OF PART IAW SRM 51-72-10 AND DRAWING R537B1760. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02609 1 20080701 A 5313 A53974203 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION AT STRINGER P 53, C 71-72 LT OUT OF LIMIT STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02610 1 20080701 A 5313 A53974203 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION AT STRINGER P 56, C 70-72 RT OUT OF LIMIT, STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02697 1 20080704 A 5313 A53971006208 STRINGER AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORROSION AT STRINGER P 56 LT, C 55-58. REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CORROSION REMOVAL AND FL AP PEENING IAW RAS/EFW/9000048/2008 ISS A, APPROVED BY EA 6-5316-120115. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02616 1 20080701 A 5753 SKIN AIRBUS 300 A300F4605R 3930327 EU LT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 LEFT WING CENTER FLAP, UPPER SURFACE IS CHAFED BY RIVETS ON THE SPOILER SUPPORT ARM BETWEEN SPOILERS NR 3 AND NR 4. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02702 1 20080704 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD FH1112 613 FOUND OLD DOUBLER REPAIR ON LT INNER FLAP LOWER SKIN BETWEEN RIB 1C-4 NOT PERFORMED IAW RAS/FOK/140/2002 (DOUBLER THIC KNESS). REPAIR RENEWED IAW RAS/FOK/150/2008 ISS C, APPROVED BY EA 6-5752-123003. 2 L 7 2 4F RT A35EU 20080808 WP 2008 8 8 08FDEA02704 1 20080704 A 5740 ARB1335 BRACKET DOUG DC10 DC1010 3022110 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 40061 46973 PERFORMED INSP AFTER REMOVAL PANEL RT WING WITH OAN J/C MD10-2780620-1JR FOUND NR 3 CRACKS ON BRACKETS, RT WING DROOPED LEADING EDGE INTERNAL SIDE. REPAIRED AREA IAW SRM 57-00-01 FIG 10 SHT 1 VOL I. 2 L 7 3 4F A22WE 20080808 EU 2008 8 8 08FDEA02705 1 20080704 A 5753 SKIN AIRBUS 300 A300F4605R 3930327 EU TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 660FE 759 RT WING INBD FLAP LOWER SURFACE HAS DENT, APPROX WS 140, DIMENSIONS 4 IN BY 2 IN BY .125 IN DEEP. REPAIRED RT WING INBD FLAP LOWER SURFACE IAW FEDEX EA 6-5750-121297, RELEASE DATE 9 JUNE, 2008. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02715 1 20080705 A 5753 6521631318 SKIN BOEING 727 727227 1384078 NM RT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 RT O/B FOREFLAP O/B L/E CRACKED. HFEC INSPECTED RT OB FOREFLAP IAW NDTM PT 6 51-00-00 FIG 23 ONE CRACK NOTED ENDS MARKE D. STOP DRILLED CRACK DIMS .250 IAW SRM 51-10-1. HFEC INSPECTED STOP DRILL IAW NDTM PT 6 51-00-00 FIG 23 CRACK TERMINA TES IN STOP DRILL HOLE. FABRICATED REPAIR USING 2024-T3 .063 PO NR 9006699 DIMS 5 INCH BY 5 INCH IAW SRM 57-50-2 FIG 4, 57-50-4 FIG 7, 51-30-5 AND 51-30-8. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR IAW SRM 57-50-4 FIG 7. 2 L 7 3 4F A3WE 20080808 NM 2008 8 8 08FDEA02724 1 20080707 A 5314 6518636378 KEELBEAM BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 RT WHEEL WELL INBD SIDE ON 870 BULKHEAD AND KEEL BEAM CHORD CRACKED. REMOVED AND REPLACED RT WHEEL WELL BS 870 BULKHEAD CHORD WITH NEW CHORD PO NR 819337 IAW B727 SRM 51-30-5 AND SRM 51-30-2. 2 L 7 3 4F A3WE 20080808 EU 2008 8 8 08FDEA02368 1 20080620 A 5753 A5796000000251 SKIN AIRBUS 300 A300F4605R 3930327 EU RT WING TE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 RIGHT WING INBD FLAP L/E IS GOUGED AT TWO PLACES. REPAIRED RIGHT WING INBD FLAP L/E SECTION IAW A300-600F SRM 57-50-00; FIG 208. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02539 1 20080627 A 5321 A5327062002400 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 241 RG IS CRACKED. FABRICATED A NEW FLOOR PANEL, POTTED EDGES, CURED, SANDED, POTTED INSERT S, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02531 1 20080627 A 5321 B5327048402400 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 232 TG IS PUNCTURED ON THE TOP AND BOTTOM. FABBED A NEW FLOOR PANEL, POTTED EDGES, CURED, S ANDED, POTTED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02533 1 20080627 A 5321 B5327047800800 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DOOR FLOOR PANEL 241 DF IS CRUSHED. FABBED NEW PANEL 241 DF; POTTED INSERTS, POTTED, CURED, SANDED EDGES, A PPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005, REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02546 1 20080627 A 5321 B5327028700200 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 251 BH IS CRACKED AND CRUSHED. FABRICATED A NEW FLOOR PANEL, POTTED EDGES, CURED, SANDED, P OTTED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02538 1 20080627 A 5321 A5327061400400 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 241 EK IS CRACKED. FABBED A NEW FLOOR PANEL; POTTED EDGES, CURED, SANDED, POTTED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005, REV F. 2 L 7 2 4F RT A35EU 20080808 EA 2008 8 8 ZLJ2008F00000 1 20080724 A 5330 SKIN CNDAIR CL600 CL6001A11 1900308 EA BS 740 CORRODED B ZLJR O OTHER O OTHER NR NOT REPORTED 1 EA 17 100QR 1043 SURFACE CORROSION DISCOVERED ON FUSELAGE SKIN ADJACENT TO PRE-COOLER EXHAUSTS ON LT AND RT SIDES OF FUSELAGE. DISCREPAN CY DISCOVERED WHILE PERFORMING PROCEDURE C53-00-814. CORROSION DEEMED TO BE UNUSUALLY SEVERE. (K) 2 L 7 2 4F RT A21EA 20080819 NM 2008 8 19 UPS08M53026 1 20080716 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 24 LT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED BU SHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M53036 1 20080721 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 19 RT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 EA 2008 8 19 SWIA200819918 1 20080731 A 5100 NONE CNDAIR CL600 CL6002D24 1390016 EA GE CF34 CF348C5 30050 NE NOT AN SDR NONE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 800SK 15060 POSSIBLE TAIL STIKE ON LANDING. (FLIGHT NR 4125) PERFORMED TAIL STRIKE INSPECTION IAW 32-71-00. NO DISCREPENCIES NOTED . 2 L 7 2 4F 4 F RT A21EA E00063EN 20080819 NM 2008 8 19 UPS08553061 1 20080730 A 5530 SUPPORT BOEING 757 75724APF 1384969 NM VERTICAL STAB CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 INSPECTION TYPE-C2, VERTICAL STAB LWR LEADING EDGE FAIRING SUPPORT RIB IS CHAFED, BS 1681. REMOVED & REPLACED RIB. 2 L 7 2 4F RT A2NM 20080819 WP 2008 8 19 UPS08852998 1 20080703 A 5711 SPAR DOUG DC8 DC871F 302199D WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, POSSIBLE CRACK AT CENTER SPAR WEB FLANGE JUST IB XRS 358 NR 4 MAIN. REMOVED DAMAGE AND FABBED AND I NSTALLED REPAIR IAW SRM., 57-2-0, 51-1- 8, 51-1-21. 2 L 7 4 4F RT 4A25 20080819 NM 2008 8 19 UPS08M52989 1 20080430 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C, RT WING FUEL TANK UPPER STRINGER NR 14 END SUSPECT CRACK. HFEC INSP C/O IAW DAC NDTSPM REV13 06-10- 01.001 & FOUND CRACK APPROX 1 13 INCH. SPLICE FITTING AT RT WING FUEL TANK UPPER STRINGER NR 14 AREA REMOVED FOR ACCESS . HFEC INSP C/O, CONFIRM CRACK END & MARKED OUT. DAMAGED PORTION OF RT WING FUEL TANK UPPER STRINGER NR 14 TRIMMED OFF IAW EN NR 1189-08. NEW FAB REPAIR STRINGER & REPAIR STRAP INSTL IAW EN NR1189-08 & SRM. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M52969 1 20080605 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C, RT WING OB FLAP OB FWD HINGE ACTUATOR MOUNTED IB BORE FOUND CORRODED. RT OB FLAP OB HINGE ACTUATOR MOUNTED IB BORE CORROSION REMOVED AND FOUND EXCEED LIMIT IAW CMM57-44-09 PG 602-607 R61.FPI C/O IAW DAC NDT SP R13 PT 08 ON REWORK AREA, FOUND NO CRACK AND NO CORROSION EVIDENT. REWORKED AREA ETCH INSPECTED AND FOUND SATIS IAW EN1298-08.BU SHING FAB IAW EN1298-08. FABRICATED BUSHING INSTALLED IAW EN 1298-08. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M52971 1 20080518 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C, RT WING OB FLAP OB FWD HINGE BARREL NUT SPOT FACE CORRODED. RT FWD OB FLAP OB HINGE BARREL NUT SPOT FACE CORROSION REMOVED IAW CMM57-44-09 PG 602-607 R61. FPI C/O IAW DAC NDT SPM R13 PT 08 ON REWORKED AREA, FOUND NO CRA CK, NO CORROSION EVIDENT. RT FWD OB FLAP OB HINGE BARREL NUT SPOTFACE EVALUATED, FOUND ACCEPTED IAW EN1298-08. REWORKE D AREA ETCH INSPECTED, FOUND 'SATIS' IAW EN1298-08. 2 L 7 3 4F RT A22WE 20080819 SO 2008 8 19 C2XA08IA183 1 20080731 A 2750 3631001007MOD3 CONTROL UNIT EMB 135 EMB135LR 3260305 SO T/E FLAP INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 12528 14688 14688 145504 IAH-FLIGHT 2411, THE CREW REPORTED THAT THE FLAPS FAILED CLIMBING THROUGH 15000 FEET AT 0 DEGREES. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FECU (FLAP ELECTRONIC CONTROL UNIT). OPERA TIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080819 NM 2008 8 19 UPS08M52972 1 20080507 A 5320 ACA01437 HANGER ASSY DOUG MD11 MD11F 3023600 NM BS 602 BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C, FWD CGO COMPT/ AT STATION 602, LBL 42 FWD BULKHEAD SUPPORT HANGER WITH P/N: ACA0143-7 FOUND BROKEN. FWD CARGO STA 602, LBL 42 FWD BULKHEAD SUPPORT HANGER REMOVED IAW SRM 51 -33-01 VII R35. NEW HANGER FAB IAW EN 1219-08. NEW FAB HANGER HEAT TREAT TO RT 900 CONDITION IAW EN NR 1219-08. HOLES TRANSFERED ONTO NEW FAB HANGER IAW SRM 51-31-01 VII R35. NEW FAB HANGER PRIMED IAW SRM51-21-01 V II R35. NEW HANGER INSTALLED AT FWD CGO IAW SRM 51-33-01 VII REV 35. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M52986 1 20080424 A 5753 FAIRING DOUG MD11 MD11F 3023600 NM TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C, RT WING IB FLAP ELEPHANT EAR FAIRING FOUND GOUGED AND DENTED. RT WING IB FLAP, IB FAIRING, REMOVED I AW CMM57-52-03 R61. GOUGED AND DENTED AREAS MEASURED, EVALUATED & FOUND OUT OF LIMIT IAW SRM57-00-01 VI R35. DAMAGED SK IN PORTION ON RT WING IB FLAP IB FAIRING AREA TRIMMED OFF IAW EN NR 1289-08. NEW SKIN PORTION, INTERNAL SPLICE DOUBLER & 02EA REPAIR DOUBLER FAB AND INSTALLED IAW EN NR 1289-08. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M52987 1 20080430 A 5753 SKIN DOUG MD11 MD11F 3023600 NM LT WING TE FLAP WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C, LT WING IB FLAP CTR VANE TRACK CUTOUT SKIN FOUND WORN AS MARKED. REMOVED LT WING IB FLAP VANE IAW AM M27-50-22 R53. CHAFFING MARKS ON LT WING IB FLAP CTR VANE TRACK CUTOUT SKIN AREA BLEND OUT IAW EN NR 1175-0 8. FPI C/O ON REWORKED AREA, FOUND NO CRACK & NO CORROSION EVIDENT. REWORKED AREAS REPROTECTED IAW EN NR 1175-08. LT IB FLAP VAN E REINSTALLED IAW MM27-50-22 REV 53. 2 L 7 3 4F RT A22WE 20080819 SO 2008 8 19 C2XA08RI103 1 20080716 A 3320 5113WW LIGHT EMB 135 EMB135ER 3260203 SO CABIN DEFECTIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16511 145267 FLIGHT 2513 -EWR- FLIGHT CREW REPORTED ELECTRICAL BURNING ODOR IN FORWARD CABIN. EWR MX REMOVED AND REPLACED PASSENGER CABIN LIGHT AT ROW 1A AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080819 EU 2008 8 19 UPS08152975 1 20080722 A 5753 A57960690201 SKIN AIRBUS A300 A300F4622R 3930360 EU RT WING TE FLAP CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 153UP 0839 INSPECTION TYPE:5 YR, RT WING OB FLAP L/E IB CHAFED. REPAIRED RT WING OB FLAP L/E IB SIDE REF A-300-600 SRM 57-50-0 0 F IG 208. 2 L 7 2 4F RT A35EU 20080819 SO 2008 8 19 C2XA08IA188 1 20080804 A 3260 8005701 PROXIMITY SENSOR EMB 145 EMB145XR 3260214 SO MLG INOPERATIVE A C2XA K NONE N FALSE WARNING CL CLIMB 1 SW 27 12145 145745 IAH - FLIGHT 2352 - CREW REPORTED, AFTER TAKEOFF THE LANDING GEAR DID NOT INITIALLY RETRACT, AND HAD THE ASSOCIATED DISA GREE MESSAGE ON EICAS. THE ACFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE TRAILING ARM PROXIMITY SENSOR. OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080819 EA 2008 8 19 SWIA200819798 1 20080502 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 614SK 10051 PAX DOOR OUTER HANDLE IS CRACKED. (FOUND AT C-CHECK) COMPLIED WITH REPLACEMENT OF PAX DOOR OUTER HANDLE IAW SB 670BA-52 -030. 2 L 7 2 4F RT A21EA 20080808 CE 2008 8 8 XOR2008F00000 1 20080709 A 3240 21576 BRAKE BEECH 200 B200 1152922 CE PWA PT6 PT6A42 52043 NE MLG SMOKE E XORA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 63 200EG BB1501 PILOTS DEVIATED FROM THE PILOT OPERATING PROCEDURES FOR TAXIING OF THE AC PROCEEDING A MLG BRAKE AND WHEEL TIRE CHANGE THE AC RETURNED TO THE RAMP AREA WITH NO ABNORMAL INDICATIONS, OTHER THAN THE BRAKE/RUDDER PEDALS ACHIEVING EXCESSIVE TR AVEL TO THE FLIGHT DECK FLOOR. UPON EXITING THE AC, THEY NOTED THAT THE MAIN WHEEL BRAKES HAD BEGAN TO OMIT SMOKE AND W ERE OBVIOUSLY OVERHEATED FROM EXCESSIVE BRAKING. ALL MLG BRAKES, WHEEL AND TIRES WERE REPLACED. INCLUDING THE BRAKE SU PPLY LINE HYD HOSES. THE MLG STRUTS WERE INSPECTED FOR ANY HEAT RELATED DAMAGE. (K) 1 L 7 2 4T 4 T A24CE E4EA 20080808 EU 2008 8 8 M7K2008F00111 1 20080324 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE DEFECTIVE E M7KA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 846MH 330 4248 23399 FAILURE CODE AT SHUTDOWN INDICATED A FAULT WITH THE COLLECTIVE POTENTIOMETER. INSTALLED NEW POTENTIOMETER AND NO FURTHE R PROBLEM NOTED. THIS IS A VERY COMMON FAULT FOR THIS PART THAT EFFECTS THE DISPATCH RELIABILITY FOR THIS MODEL AIRCRAF T. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080808 EU 2008 8 8 M7K2008F00117 1 20080303 A 5100 350A58004523 HINGE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE UNKNOWN CRACKED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 818MH 838 4131 23322 DURING ROUTINE 100 HR INSPECTION A CRACK WAS FOUND RADIATING HORIZONTALLY FROM THE SECOND HOLE FROM THE ONE END AND ACRO SS THE CORNER OF THE FIRST HOLE ON THE OPPOSITE HINGE END WITH A TOTAL SEPARATION OF THE HINGE CORNER METAL. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EU 2008 8 11 M7K2008F00100 1 20080414 A 5302 350A23422221 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 822MH 4142 23069 DURING ROUTINE INSP, A CRACK WAS DISCOVERED STARTING AT ATTACHMENT BORE HOLE AND RADIATING OFF THE EDGE OF THE ATTACHMEN T FLANGE. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 NM 2008 8 11 ABX2008F00002 1 20080714 A 3350 20131A BATTERY PACK BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE EMERGENCY LIGHTS DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 744AX 22221 EMERGENCY LIGHT BATTERY PACK M734 WOULD NOT ILLUMINATE EMERGENCY LIGHTS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PA CK M734 IAW MM 33-51-07. OPS CHECKED GOOD. (K) 2 L 7 2 4F 4 F RT A1NM E13NE 20080811 EU 2008 8 11 IJA2008F00001 1 20080517 A 2450 7271825 CIRCUIT BREAKER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE SEARCH LIGHT FAILED E IJAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 CE 07 911EM 3603 ON MAY 17, 2008, THE PILOT REPORTED ELECTRIC SYS FAILURE AND MADE A PRECAUTIONARY LANDING DUE TO THE FAILURE, IN A FIEL D. ON INSP OF THE ACFT, MAINT PERSONNEL FOUND THE ACFT BATTERY DEAD, INSTALLED NEW/ SERVICEABLE BATTERY. GROUND RAN AC TO TEST SYS. ON START GENERATOR CAME ON LINE NORMALLY WITH NORMAL OUTPUT. AT WHICH TIME ACFT WAS REPOSITIONED TO ITS BASE. REPOSITION FLT TO BASE FOUND ELECTRIC SYS WORKING WITHOUT DEFECTS. UPON ARRIVAL, THE MECHANIC NOTED THE SEARCH L IGHT WAS INOPERATIVE. REMOVAL OF THE SEARCH LIGHT BULB FOUND THE BULB HAD BROKEN IN HALF AND THE WIRING HAD SHORTED TO THE SEARCH LIGHT HSG. THIS CAUSED THE GENERATOR TO TRIP OFF LINE (ELECTRIC SYS FAILURE). AT THE TIME THE WIRING FOR TH 1 G 7 1 3U 3 U H9EU E19EU 20080811 EU 2008 8 11 M7K2008F00081 1 20080414 A 5302 350A23422221 FITTING UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE TAILBOOM CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 808MH 391 3914 23072 FOUND CRACKED INTO 2 PIECES DURING ROUTINE INSP ON THE MOUNTING FLANGE SURFACE RADIATING FROM A MOUNTING BORE AND TO BOT H EDGES OF THE FLANGE. A NEW FITTING WAS MATCH DRILLED AND INSTALLED. THIS IS A FAIRLY COMMON FAILURE FOR THIS PART. S UGGEST A MORE DURABLE MATERIAL BE USED SUCH AS TITANIUM OR STAINLESS STEEL. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EA 2008 8 11 TRAX200800647 1 20080514 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 978EV 7723 LT SIDE 202 PRESSURE BULKHEAD CRACKED AT BRAKE SYSTEM PUSHROD RESOLUTION DESCRIPTION: (RESOLVED ON W/O: 90658 TASKCARD: N/R-00092) REPAIRED CRACKED PRESSURE BULKHEAD LT SIDE STA 202.75 ON WORK ORDER 90661 TASK CARD E0600-53-0217C/W SDR CLOS ED (B) 2 L 7 2 4F RT A21EA 20080811 EU 2008 8 11 M7K2008F00083 1 20080414 A 3340 LIGHT UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ANTI COLLISION FAILED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 816MH 1985 4038 23096 DURING PREFLIGHT INSP, ANTI-COLLISION LIGHT FAILED TO ILLUMINATE. INVESTIGATION REVEALED CIRCUIT BREAKER HAD POPPED. R ESETTING THE BREAKER FOR A GROUND TEST REVEALED NO FUNCTION. THIS PART HAS BEEN DEEMED NOT REPAIRABLE BY THE AIRFRAME M FG. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 EA 2008 8 11 FFK2008F00001 2 20080723 A 7414 BL68256013 MAGNETO PIPER PA32 PA32RT300 7103215 SO LYC O540 IO540* 41532 EA ENGINE BROKEN E FFKA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 39 169BW 373 32R7885080 PILOT REPORTED OIL LEAKING FROM THE ENGINE COWLING AFTER THE LAST FLIGHT OF THE DAY. MAINT TROUBLESHOT PROBLEM TO BE CO MING FROM THE DUEL MAGNETO, PN BL-68256013, SN- G07GA121R, TSO 373. THE BOTTOM MOUNTING FLANGE HAD BROKEN OFF OF THE MA GNETO HSG CAUSING THE OIL LEAK. (K) 1 L 7 1 3O 3 O A3SO 1E4 20080811 WP 2008 8 11 MWE2008F00026 1 20080725 A 2170 21P101 COALESCER BAG DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE CONTAMINATED A MWEA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 GL 13 809ME 48071 FWD LAVATORY SMOKE DETECTOR WENT OFF AND THERE WAS VISUAL GRAY SMOKE IN CABIN AND COCKPIT. REMOVED AND REPLACED WATER S OCKS DUE TO OIL CONTAMINATION FROM NOTED APU OIL LEAK. (K) 2 L 7 2 4F 4 F A6WE E2EA 20080811 SO 2008 8 11 SIM2008F00019 1 20080721 A 3260 SQUAT SWITCH EMB 135 EMB135KL 3260302 SO LT MLG FAILED A SIMA O OTHER G J MULTIPLE FAILURE WARNING INDICATION CL CLIMB 1 SW 21 804AE 145487 ON FLIGHT, CREW REPORTED A LG AIR/GRD FAIL ANNUNCIATION AFTER TAKEOFF. LANDING GEAR HANDLE STUCK IN DOWN POSITION. OTH ER ANNUNCIATIONS INCLUDED 1-2 WOW INOP AND SPS ADVANCED. AC RETURNED TO FIELD. AC REMOVED FROM SERVICE. REMOVED AND R EPLACED NLG WOW SWITCH IAW AMM 32-63-01. OPS CHECK GOOD. REMOVED AND REPLACED LT MLG AFT WOW SWITCH IAW AMM 32-63-02. OPS CHECK GOOD. AC RETURNED FOR SERVICE. (K) 2 L 7 2 4F RT T00011AT 20080811 EU 2008 8 11 QML2008F00006 1 20080722 A 6320 CASE UROCOP EC135 EC135P2 5620027 EU PWA PW206 PW206B 0 NE M/R TRANSMISSION CRACKED E QMLA K NONE O OTHER IN INSP/MAINT 1 NM 03 137LN 1640 0339 DURING A ROUTINE 800 HOUR INSPECTION, A CRACK WAS DISCOVERED IN THE WEBBING OF THE MAIN TRANSMISSION. THE CRACK IS IN T HE MAIN CASE SUPPORT BUT THE IPC DOES NOT PROVIDE ANY TRANSMISSION SUBASSEMBLY PN. (K) 1 G 7 2 3U 3 U H88EU E42NE 20080811 EA 2008 8 11 TRAX200800687 1 20080526 A 2913 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 871AS 7537 HYD 1 LOW PRESS WARNING FOLLOWED BY HYD EDP 1A WARNING OPERATED ENGINE 1. 11 WITH THE FAILED PUMP. PUMP CAVATED A LOUD NOISE AND VIBRATION AFTER T/O. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLT 4596 DEL 126 MINS REMOVED AND REPLACED NR 1 HYD EDP IAW CRJ200AMM29-11-00. OPS CHECK GOOD, [SDR CLOSED] 2 L 7 2 4F RT A21EA 20080819 EA 2008 8 19 SWIA200819799 1 20080502 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* 30015 NE BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 614SK 10051 STA280 LOWER CROSSBEAM IS CORRODED. (FOUND AT C-CHECK) COMPLIED WITH REPAIRS OF STA280 CROSSBEAM IAW SRM 51-42-06-001-00 1-A01. 2 L 7 2 4F 4 F RT A21EA 20080819 EU 2008 8 19 UPS08152982 1 20080723 A 5321 B5327074400000 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CARGO DECK DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 153UP 0839 INSPECTION TYPE:5 YR, MAIN CARGO COMPT FLOOR PNL NR 231QJ AT FR 26 LT SIDE FOUND DELAMINATED. REPAIRED MAIN CABIN FLOOR PNL NR 231QJ AT FR 26 LT SIDE IAW A300-600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20080819 NM 2008 8 19 UPS08M52942 1 20080719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR34 RT BOLT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INS TALLED BUSHING IAW EO MD11-5510-19409-N AND SAA TRAVELER 80538760001. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M52943 1 20080723 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 33 LT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INSTALL ED BUSHING IAW UPS EO MD11-5510-19409-N AND SAA TRAVELER 80538950001 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M52944 1 20080717 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION ON NR21 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING AND INSTALLED BUSHING IAW UPS EO MD11-5510-19409-N AND SAA TRAVELER 80538550001. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 ASAA0843295 1 20080630 A 5320 659659244 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 767-779 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AFT CARGO FLOOR SUPPORT IS CORRODED REMOVED DAMAGED AREA FABRICATED REPAIR PARTS & INSTALLED IAW EA 53 20 01844. 2 L 7 2 4F 4 F RT A16WE E21EU 20080819 NM 2008 8 19 ASAA0843307 1 20080630 A 5320 655384410 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 767-779 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 CORROSION ON UPPER SURFACE OF FLOOR SUPPORT AT STA 767 RBL1380 REMOVED DAMAGE AND FABRICATED REPAIR PARTS & INSTALL PER ASA EA 5320 01844 2 L 7 2 4F 4 F RT A16WE E21EU 20080819 NM 2008 8 19 ASAA0843265 1 20080710 A 5755 654645262A SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 NR 5 SPOILER DENTED ON THE TOP SIDE IB END CENTER OF PANEL PREPPED DAMAGED AREA FABBED DOUBLER & BONDED REPAIR IAW SRM 5 1 70 10 PG 257. 2 L 7 2 4F 4 F RT A16WE E21EU 20080819 WP 2008 8 19 DHLA200800085 1 20080731 A 2697 899827 CONNECTOR DOUG DC8 DC873F 302199F WP FIRE LOOP LOOSE A DHLA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 873SJ 351 117 46091 WHEN REDUCING THRUST FOR DESCENT, NR 1 FIRE WARNING ILLUMINATED. RAN EMERGENCY PROCEDURE. TROUBLESHOT FIRE WARNING SYS PER MM 26-10-0. FOUND FAN CASE FIRE LOOP CONNECTOR BKSHL LOOSE AND GNDING. SECURED AND CLEANED ALL CONNECTIONS. AIRC RAFT WAS GROUNDED. FLIGHT 803. (S) 2 L 7 4 4F RT 4A25 20080819 NM 2008 8 19 F3LA200800542 1 20080730 A 5320 D5391635420040 PROFILE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2 2209 DURING C3 C-CHECK, INSPECTION NOTED THE TRANSITION PROFILE, LT SIDE BETWEEN FRAMES 28 AND 29 HAD CORROSION AT THE NUT PL ATE LOCATIONS. MAINTENANCE REMOVED AND REPLACED TRANSITION PROFILE IAW THE REQUIREMENTS OF A319 SRM 51-72-11. UPON COM PLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080819 NM 2008 8 19 SWAA084136 1 20080727 A 5311 6545804 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED PAE CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 259, STR 11R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084147 1 20080727 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084148 1 20080724 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 R1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080819 2008 8 19 SWAA084149 4 20080724 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080819 2008 8 19 SWAA084150 4 20080727 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080819 2008 8 19 SWAA084151 4 20080725 A 2565 61621469 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084152 1 20080725 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 602SW 27953 RIGHT OVERWING EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084157 1 20080727 A 5330 6545800 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND FWD SERVICE DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084158 1 20080727 A 5312 6545409 PRESSURE PANEL BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663, LBL 39. REPAIRED WEB PER EA. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084168 1 20080728 A 5230 6547952 TORQUE TUBE BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR TORQUE TUBE CRACKED. REMOVED AND REPLACED TORQUE TUBE PER BOEING DRAWI NG AND SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084170 1 20080728 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 503C, STR 16L. REPAIRED SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084179 1 20080728 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084098 1 20080723 A 3350 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 757LV 29850 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080819 SO 2008 8 19 SWIA200819882 1 20080405 A 5315 BUTTSTRAP EMB 120 EMB120ER 3260203 SO FLOORBEAM CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 292SW 120319 BUTT STRAP UNDER LAV IS CORRODED. (FOUND AT C-CHECK) REPLACED BUTT STRAP IAW EMB 120, SRM 51-10-02, PAGE 3 AND 51-40-02 . 2 L 7 2 4T RT A31SO 20080819 NM 2008 8 19 USAA920081465 1 20080722 A 5320 D5347112420 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803AW 0931 SAL-C7- MAJOR REPAIR - SHEAR PLATE CORRODED BETWEEN FR69 TO FR70, Y1738. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Y17 38 IAW A319 SRM 51-42-11 AND 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080819 EA 2008 8 19 SWIA200819924 1 20080802 A 3397 TERMINAL BLOCK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS FAILED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 438SW 7574 NUMEROUS FWD EMERGENCY LIGHTS ARE INOPERATIVE. (FLIGHT NR 3748) REPLACED TB110 TERMINAL BLOCK IAW WDM 33-52-00. OPS CHE CK GOOD. 2 L 7 2 4F RT A21EA 20080819 EA 2008 8 19 REX2008F00025 1 20080801 A 3230 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8554A 7554 ON APPROACH INTO KMSP, WHEN GEAR WAS LOWERED THE AURAL "GEAR DISAGREE" WARNING WENT OFF WITH A RED NOSE GEAR INDICATION. CREW DECLARED AN EMERGENCY AND MANUALLY LOWERED THE GEAR. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KMSP. MAINTENANCE MET THE ACFT ON THE TAXIWAY AND PINNED THE GEAR. MAINTENANCE INSPECTED THE GEAR AND REPLACED THE NOSE LAND ING GEAR PRIORITY VALVE PER BOMBARDIER AMM. (S) 2 L 7 2 4F RT A21EA 20080819 NM 2008 8 19 NWAA083366746 1 20080711 A 5320 WEB BOEING 747 747222B 1384904 NM NLG CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 646NW 23737 DURING "L" CHECK FOUND CRACK IN VERTICAL WEB OF RT NOSE WHEEL ACCESS PANEL CUTOUT AT BS 348. REPAIRED PER EA 67-210594. (S) 2 L 7 4 4F RT A20WE 20080819 WP 2008 8 19 NWAA083609853 1 20080731 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 762NC 47710 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE AFT SECTION HAD FAILED. MAINTENANCE REP LACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (S) 2 L 7 2 4F RT A6WE 20080819 SO 2008 8 19 SWIA200819880 1 20080421 A 5315 BUTTSTRAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE FLOORBEAM CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 301YV 120301 BUTT STRAP IN FRONT OF LAV IS CORRODED. (FOUND AT C-CHECK) REPLACED BUTT STRAP IN FRONT OF LAV IAW SRM 51-10-02 AND SEC URED IAW 51-40-07. 2 L 7 2 4T 4 T RT A31SO E20NE 20080819 EA 2008 8 19 SWIA200819862 1 20080712 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 409SW 7056 CABIN DOOR FWD UPPER CORNER IS DAMAGED. (FLIGHT NR3983) REPLACED CORNER CAP ON PASSENGER DOOR IAW SRM 52-10-31. 2 L 7 2 4F RT A21EA 20080819 WP 2008 8 19 ABXA080214 1 20080730 A 3397 WIRE DOUG DC9 DC931 3022065 WP COCKPIT SHORTED A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 944AX 47550 SMALL ELECTRICAL SPARKS NOTED ON CAPTAIN`S CHART LIGHT. MAP AND BRIEFCASE LIGHT C/B TRIPPED. RESET ONCE, TRIPPED AGAIN . FOUND CHART HOLDER LOOSE ON YOKE ALLOWING WIRES TO SHORT. TIGHTENED HOLDER ASSY AS REQUIRED. LIGHTS OPERATED NORMAL IAW DC9 AMM CHAPTER 33. (S) 2 L 7 2 4F A6WE 20080819 NE 2008 8 19 UPS08652984 2 20080802 A 7200 074821338M51P03 ENGINE BOEING 767 76734AF 1385212 NM GE CF6 CF680C2B7 NE LEFT BIRD INGESTION A IPXA A UNSCHED LANDING C E F.O.D. VIBRATION/BUFFET CL CLIMB 1 SO 01 303UP 27241 INSPECTION TYPE-ETOP ATB - ON TAKEOFF UPS 232 INGESTED A BIRD TO THE LT ENGINE CAUSING VIBRATION. THE CREW DECLARED AN E MERGENCY AND RETURNED TO DEPARTURE. THEY DID NOT SHUT DOWN THE ENGINE. COMPLETE FAN BLADE SET REPLACED IAW AMM 72-31-0 2-4. ENGINE VIB CHECKED. SATISFACTORY LT ENGINE SPINNER REPLACED IAW AMM 72-31-01-4. 2 L 7 2 4F 4 F RT A1NM E13NE 20080819 NM 2008 8 19 UPS08553062 1 20080731 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 1500 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 INSPECTION TYPE-C2, FRAME DENTED ON IB FRAME BS 1500, STR 23L, TRIMMED OUT DAMAGED AREA FABRICATED & INSTALLED REPAIR PA RTS. 2 L 7 2 4F RT A2NM 20080819 NM 2008 8 19 UPS08553063 1 20080729 A 5320 STRUCTURE BOEING 757 75724APF 1384969 NM APU INLET DUCT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 INSPECTION TYPE-C2, APU INLET DUCT CONTACT AREA IS CORRODED, BS 1787-1825, STR 3R-6R. TRIMMED OUT CORRODED PART SPLICE REPAIR PARTS IAW B757-5310-30212-A. 2 L 7 2 4F RT A2NM 20080819 NM 2008 8 19 UPS08M53027 1 20080717 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 30 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAI R BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M53028 1 20080717 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1/C, FOUND CORROSION IN NR 12 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 SO 2008 8 19 C2XA08CL088 1 20080712 A 2150 8152914 SWITCH EMB 145 EMB145LR 3260212 SO NR 1 PACK FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 16999 145307 MCI FLIGHT 2986 - THE CREW REPORTED A PACK 1 OVERLOAD IN FLIGHT EVEN AFTER 5 RESETS. THE MESSAGE REOCCURRED EVEN WHEN P ACK 1 WAS DESELECTED. THE ACFT RETURNED TO MCI AND LANDED WITHOUT INCIDENT. THE SYSTEM WAS PLACED ON MEL. ON 7/13/08 THE NR 1 PACK OVERTEMP SWITCH WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4T RT T00011AT 20080819 NM 2008 8 19 SWAA084140 1 20080727 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED HC2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT LENS CRACKED AT BS 11 ABC. REMOVED AND REPLACED LIGHT L ENS PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084141 1 20080727 A 5753 6546430100 SKIN BOEING 737 7373H4 1384600 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED HC2 CHECK, FOUND RIGHT WING INBOARD FORE FLAP OUTBOARD UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084142 1 20080727 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 930 AND BS 945, STR 25R AND STR 24R. REPAIRED SKIN P ER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084176 1 20080728 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084178 1 20080728 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084177 1 20080728 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084165 1 20080726 A 2121 215204 GASPER FAN BOEING 737 7373H4 1384600 NM E&E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 609SW 27929 FLIGHT CREW REPORTED BURNING ELECTRICAL ODOR. TURNED OFF GASPER FAN ODOR DISSIPATED. REMOVED AND REPLACED GASPER FAN P ER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084194 1 20080728 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 271, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084183 1 20080728 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080811 CE 2008 8 11 VGR2008F00000 1 20080729 A 3220 LANDING GEAR BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA NOSE COLLAPSED E VGRA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 GL 11 44US BB56 FLIGHT CREW REPORTED NOT GETTING NOSE GEAR GREEN "DOWN AND LOCKED" LIGHT AFTER EXTENDING LANDING GEAR. FLY BY THE TOWER CONFIRMED THE NOSE GEAR NOT LOCKED DOWN. THE AC WAS DIVERTED, WHERE IT MADE AN EMERGENCY LANDING WITH THE NOSE GEAR NO T DOWN AND LOCKED. UPON TOUCHDOWN, THE NOSE GEAR COLLAPSED AND THE NOSE OF THE ACFT CAME IN CONTACT WITH THE RUNWAY. T HERE WERE NO INJURIES REPORTED WITH CREW OR PASSENGERS. (K) 1 L 7 2 4T 4 T A24CE E4EA 20080811 CE 2008 8 11 DXTA200803105 1 20080608 A 3260 INDICATION SYS CESSNA 560 560XL 2076702 CE NLG MALFUNCTIONED E DXTA O OTHER N FALSE WARNING CL CLIMB 1 GL 07 624QS 5605302 THE NOSE WHEEL GREEN LIGHT WOULDN’T GO OUT AFTER THE GEAR WAS SELECTED UP. (B) 2 L 7 2 4F RT A22CE 20080811 EU 2008 8 11 M7K2008F00075 1 20080303 A 6700 116SF2C502W253 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COLLECTIVE DEFECTIVE E M7KA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 19 850MH 4327 23472 PILOT REPORTS AMBER GOVERNOR LIGHT ILLUMINATED DURING FLIGHT. A FAULT CODE WAS GENERATED INDICATING THE POTENTIOMETER A S THE LIKELY DEFECTIVE UNIT. A NEW PART WAS INSTALLED AND NO FURTHER DEFECTS WERE NOTED. THIS IS A RECURRING PROBLEM FO R THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY FOR THIS AC MODEL. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 CE 2008 8 11 DXTA200803097 1 20080605 A 3240 BRAKE SYS CESSNA 560 560XL 2076702 CE MLG MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 679QS 5605279 LT BRAKE IS EXTREMELY SENSITIVE AIRCRAFT JERKS LT ON EVERY BRAKE APPLICATION. (B) 2 L 7 2 4F RT A22CE 20080807 NM 2008 8 7 2008UALA03629 1 20080630 A 3231 DOOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NLG OUT OF RIG A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 817UA 873 HEAVY MODERATE AIRFRAME VIBRATION FELT THROUGHOUT A/C. RTFL. NLG DOOR MISMATCH (FAIR). RE-RIGGED NLG DOORS, MISMATCH CORRECTED, NO REPEATS ON SUBSEQUENT FLIGHTS. 2 L 7 2 4F 4 F RT A28NM E40NE 20080807 SO 2008 8 7 C2XA08RI089 1 20080615 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO MLG DEFECTIVE A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 27 26545 145558 FLIGHT 2580 - EWR - FLIGHT CREW REPORTED NOSE LANDING GEAR MAKES LOUD THUMP DURING RETRACTION. EWR MAINTENANCE REMOVED AND REPLACED NOSE LANDING GEAR DOWNLOCK PROXIMITY SWITCH AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVE D TO RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080807 WP 2008 8 7 AALA200801382 1 20080524 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 584AA 53247 DFW - EMERGENCY LIGHT AT SEAT 24D HAD DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 24D. SYSTEM GROUND C HECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080807 NM 2008 8 7 AALA200801459 1 20080601 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 798AN 30797 DFW - EMERGENCY LIGHT AT SEAT 26G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED NO RMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080808 NM 2008 8 8 08FDEA02777 1 20080709 A 5311 651634571 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 LWR AFT CARGO PIT, CORROSION ON UPPER FLANGE OF FRAME AT STA 1090 STR 27L REMOVED CORROSION, ORIGINAL "T" .063, REMOVED .017, REMAINING .046 OUT OF LIMITS. FABRICATED REPAIR DOUBLER FROM 7075-0 .063, HEAT TREAT T6, APPLIED ALODINE, PRIMER AND INSTALLED REPAIR DOUBLER, TIE DOWN REMOVED AND REINSTALLED FOR ACCESS REF SRM 51-40-3 PG 1-6, 51-30-2 PG 8, DRW 65- 1634516345-71. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A3WE 20080808 NM 2008 8 8 08FDEA02779 1 20080709 A 5310 BAC15061133 CREASE BEAM BOEING 727 727225 1384077 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 467FE 21449 FUSELAGE OUTER CREASE BEAM CHORD (STR 17L) CRACKED REMOVED CREASE BEAM CHORD, STR 17L, FROM STE 620 TO STA 663. VERIFIE D MATERIAL TO BE BAC1506-1133 7075-T-6, ATAG NR A00531. LOCATED AND DRILLED FASTENER HOLES IN NEW CHORD. TREATED AND P RIMED NEW CHORD. INSTALLED NEW CHORD AND APPLIED CORROSION INHIBITOR COMPOUND REF SRM 51-30-02 PG 2, SRM 53-10-2 FIG 9, SRM 51-30-30 5 PG 3-5, SRM 51-40-4 FIG 1, SRM 51-20-014 -7, PG 1-7. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080808 EU 2008 8 8 08FDEA02781 1 20080709 A 5754 A53510216205 FITTING AIRBUS 300 A300B4622R 3930312 EU KRUEGER FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORRODED FITTING ON RT KRUEGER FLAP STRUCTURE REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02782 1 20080709 A 5754 A53510217203 FITTING AIRBUS 300 A300B4622R 3930312 EU KRUEGER FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND CORRODED FITTING ON RT KRUEGER FLAP STRUCTURE. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02655 1 20080703 A 5415 A003002600000 BEARING AIRBUS 300 A300F4605R 3930327 EU ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 NR 1 PYLON; AFT CENTER PYLON ATTACH BEARING HAS PLAY IN ALL DIRECTIONS. REMOVED AND INSTALLED A NEW BEARING ASSEMBLY RE F A300-600 AMM 54-51-75-4. 2 L 7 2 4F RT A35EU 20080808 WP 2008 8 8 08FDEA02503 1 20080626 A 5330 AYB7030 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 CENTER WING LOWER (BARREL), INTERIOR FUSELAGE SKIN HAS CORROSION; FS 1257 - 1278; STRINGER 52L - STRINGER 51L. REMOVE D/BLENDED CORROSION ON THE INTERNAL SURFACE OF THE SKIN AND FOUND IT TO BE OUT OF LIMITS IAW DC/MD-10 SRM 53-00-01; VOL I. ORIGINAL THICKNESS, 0.080. REMAINING THICKNESS AFTER CORROSION REMOVAL, 0.034. MATERIAL REMOVED, 0.046. UT GAUGE USED T8225R. CUTOUT DAMAGE; FABRICATED REPAIR DOUBLERS AND FINGER DOUBLERS IAW DC/MD-10 SRM 53-20-00; FIG 6; VOL I. A LODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01; VOL II. INSTALLED THE REPAIR IAW DC/MD-10 SRM 53-20-00; FIG 6; VOL I; SHEET 2. 2 L 7 3 4F RT A22WE 20080808 EU 2008 8 8 08FDEA02741 1 20080708 A 5311 A53970889201 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD 613 FOUND SCRUB MARKS AT EMERGENCY EXIT, C 57.2, P14-15A, RT ON INNER FRAME FLANGE. REPAIR PERFORMED BY REWORK TO SMOOTH CO NTOUR, NDT FOR CRACK FREE CONDITION AND FLAP PEENING IAW RAS/EFW/9000054/2008 ISS A, APPROVED BY EA 6-5316-123024. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02648 1 20080703 A 5321 B5327037000400 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN DECK FLOORBOARD 262 HF IS BROKEN. FABBED A NEW PANEL IAW FEDEX DWG SRZ 25-005, REV F. MATERIAL ID A 402 H 35039-0 03 IAW FEDEX DWG SRZ 25-005, REV F. PART MARKED IAW FEDEX GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080819 NM 2008 8 19 SWAA084184 1 20080728 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084203 1 20080729 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 222WN 34290 DURING SCHEDULED MV3 CHECK, FOUND EEPLS INOP AT ROW 8 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084216 1 20080728 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULE 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084215 1 20080728 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULE 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITTI NG PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084214 1 20080728 A 5315 6546811 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, LBL 45. REMOVED AND REPLACED CHORD PER SRM. 2 L 7 2 4F RT A16WE 20080819 2008 8 19 SWAA084217 4 20080729 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 423WN 29827 L1 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084224 1 20080729 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084225 1 20080729 A 2560 6557463 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084233 1 20080729 A 5330 6545776 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 941, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084235 1 20080731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084240 1 20080731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084246 1 20080731 A 5311 6546550 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084247 1 20080731 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 755SA 27871 DURING SCHEDULED HC1 CHECK, MID CABIN EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK S PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084248 1 20080731 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 755SA 27871 DURING SCHEDULED HC1 CHECK, AFT CABIN EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084249 1 20080731 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 755SA 27871 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PA CK PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843266 1 20080624 A 5755 SKIN SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 REF SAD 5060511: NR 5 SPOILER UPPER SURFACE DENTED 6" FROM T/E 12" FROM OB EDGE PREPPED DAMAGED AREA FABBED DOUBLER + BO NDED REPAIR IAW SRM 51 70 10 PG 257. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084256 1 20080731 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 11R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843228 1 20080624 A 5330 65457755 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 860-876 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 FUSELAGE SKIN IS DENTED. REMOVED DAMAGED SECTION AND INSTALLED FILLER DOUBLER AND TRIPLER IAW SRM 53 27. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084258 1 20080731 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084270 1 20080801 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 814, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084275 1 20080801 A 5330 6545576 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 933, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084277 1 20080801 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843226 1 20080630 A 5315 FLOORBEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 1016 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AFT LT GALLEY FLOORBEAM FASTENER HOLE IS CORRODED. REPLACE EXISTING REPAIR STRAP IAW SRM 53-00-51. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0853214 1 20080722 A 2131 71211997101AC CONTROLLER BOEING 737 737890 1384527 NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE FAULTED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 583AS 4018 35681 AUTO FAIL LIGHT ALONG WITH ALTN LIGHT ILLUMINATED CLEARED NUISANCE MSG FROM NR 2 PRESS CONT SYSTEM OPS CHECK NORMAL IAW AMM 21 31 00 700 802. (GROUND TEST) 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084283 1 20080803 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084288 1 20080803 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084289 1 20080803 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084291 1 20080803 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084292 1 20080803 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084293 1 20080803 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084299 1 20080801 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED SPV CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20080820 2008 8 20 SWAA084300 4 20080803 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080808 EU 2008 8 8 08FDEA02758 1 20080708 A 3350 1009841 LIGHT AIRBUS 300 A300F4605R 3930327 EU ZONE 200 FAILED A FDEA K NONE L NO TEST IN INSP/MAINT 1 CE 21 665FE 769 L-1 AND R-1 OVERHEAD EXIT LIGHTS ARE INOP. REPLACED BOTH R-1 AND L-1 EMERGENCY LIGHT ASSEMBLIES. OPS CHECK GOOD IAW FE DEX A300-600 AMM 33-51-13-4. PARTS CANNIBILIZED FROM A/C N674FE. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02707 1 20080528 A 5347 A5378197520900 SEAT TRACK AIRBUS 300 A300B4622R 3930312 EU ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 SEAT-TRACK AT Y-1959 WORN AT FRAME 29. SEAT-TRACK WAS REPAIRED AS PER FEDEX EA 6-5310-117332. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02714 1 20080705 A 5753 6521631317 SKIN BOEING 727 727227 1384078 NM LT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 494FE 21532 LT O/B FOREFLAP O/B L/E CRACKED. HFEC INSPECTED LT OB FOREFLAP IAW NDTM PT 6 51-00-00 FIG 23 ONE CRACK NOTED ENDS MARKE D. STOP DRILLED CRACK IAW SRM 51-10-1 DIMS .250. HFEC INSPECTED STOP DRILL IAW NDTM 51-00-00-FIG 23 CRACK TERMINATES I N STOP DRILL HOLE. FABRICATED REPAIR USING 2024-T3 .063 PO NR 9006699 DIMS 3 1/2 INCH BY 4 INCH IAW SRM 57-50-2 FIG 4, 57-50-4 FIG 7, 51-30-5, 51-30- 8. TREATED AND PRIMED REPAIR IAW SRM 51-10-2. INSTALLED REPAIR IAW SRM 57-50-4 FIG 7. 2 L 7 3 4F A3WE 20080808 EU 2008 8 8 08FDEA02725 1 20080707 A 5330 A5361088020000 SKIN PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 A FASTENER IN THE FUSELAGE SKIN HAS LIGHTNING STRIKE DAMAGE AT THE LEFT SKIN LOWER FLAP SPLICE BETWEEN FRAME 2 AND FRAME 3. REMOVED FASTENER IAW A300-6003-10-12. COLD WORKED THE HOLE A300-600 SRM 51-40- 49. INSTALLED A NEW FASTENER IN TH E LEFT SKIN LOWER SPLICE BETWEEN FRAMES 2 AND 3 IAW A300-600 SRM 51-40-12. PAINTED AREA IAW A300-600 SRM 51-23-10. 2 L 7 2 4F RT A35EU 20080808 NM 2008 8 8 08FDEA02564 1 20080630 A 5730 APB74411 SKIN DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 609FE 48549 MAIN DECK CARGO COMPARTMENT, CORROSION FOUND ON UPPER SURFACE OF PRESSURE BOUNDARY OVER WING AT STA 1227, XCW= 72.5 RT F ASTENER AREA APPROXIMATELY 1 INCH DIAMETER. UPPER SURFACE CORROSION ON MAIN DECK CARGO COMPARTMENT AT STA 1227 XCW=72.5 FASTENER AREA. REMOVED AS PER SRM 51-21-01 VOL II AND FOUND WITHIN LIMIT AS PER SRM 57-20-00 FIG 13 VOL I, ORIGINAL TH ICKNESS: 0.168 INCH, MATERIAL REMOVED: 0.012 INCH, REMAINING THICKNESS, 0.156 INCH. REPAIR CLASSIFIED AS MINOR AS PER F EDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080808 EU 2008 8 8 08FDEA02530 1 20080627 A 5321 A5327048402800 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 231 TG IS CRUSHED; BROKEN AND PUNCTURED. FABBED A NEW FLOOR PANEL, POTTED EDGES, CURED, SAN DED, POTTED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02532 1 20080627 A 5321 B5327047801800 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 241 BF IS CRUSHED AND CUT. FABBED A NEW PANEL 241 BF; POTTED INSERTS, POTTED, CURED, SANDED EDGES, APPLIED NON-SKID TAPE AND PART MARKED IAW FEDEX DWG SRZ 25-005; REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02545 1 20080627 A 5321 B5327021800000 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO DECK FLOOR PANEL 251 AH IS CRACKED AND CRUSHED. FABRICATED A NEW FLOOR PANEL NR 251 AH, LOCATED HOLES FROM T HE OLD PANEL, POTTED EDGES, CURED, SANDED, POTTED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005, REV F. 2 L 7 2 4F RT A35EU 20080808 EU 2008 8 8 08FDEA02547 1 20080627 A 5321 B5327027600800 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 674FE 781 MAIN CARGO FLOOR PANEL 251 QH IS CRACKED AND CRUSHED. FABRICATED A NEW FLOOR PANEL NR 251 QH, POTTED EDGES, CURED, SAND ED, POTTED INSERTS, APPLIED NON-SKID AND PART MARKED IAW FEDEX DWG SRZ 25-005, REV F. 2 L 7 2 4F RT A35EU 20080811 EU 2008 8 11 M7K2008F00090 1 20080324 A 5350 350A58004523 HINGE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE EXCHANGER INLET CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 821MH 200 4134 23319 DURING ROUTINE INSPECTION A CRACK WAS FOUND IN THE HINGE MOUNTING FLANGE RADIATING FROM THE OUTERMOST LT ATTACHMENT SCRE W BORE. REMOVAL OF ATTACHMENT SCREW REVEALED THE FLANGE CORNER HAD SEPARATED FROM THE REST OF THE HINGE. THIS IS A VER Y COMMON FAILURE FOR THIS PART. A MORE DURABLE MATERIAL SUCH AS SS OR TITANIUM MAY BE REQUIRED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 2008 8 11 ARW2008F00000 4 20080723 A 3416 4005123902 INDICATOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650* 30018 NE ALTIMETER FAILED A ARWA O OTHER O OTHER CL CLIMB 1 SO 29 524MD 46999 F/O ALTIMETER FAILED IN TAKEOFF; WORKED OK IN CLIMB AND CRUISE. REMOVED AND REPLACED ALTIMETER INDICATOR IAW MM 34-02-0 1; PERFORMED OPS CHECK IAW M34-12-00; FOUND NORMAL. (K) 2 L 7 3 4F 4 F A22WE E23EA 20080811 CE 2008 8 11 DXTA200803098 1 20080605 A 3240 BRAKE SYS CESSNA 500 560CESSNA 2076750 CE MLG MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 327QS 5600327 BRAKE APPLICATION FROM THE CO-PILOT`S SEAT ARE SLUGGISH, BRAKES FEEL SOFT. (B) 2 L 7 2 4F RT A22CE 20080811 EA 2008 8 11 TRAX200800674 1 20080520 A 5210 FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 PSG DOOR STUCK AND WOULD NOT OPEN UPON ARRIVAL INTO SHV. LUBED AND CLEANED SHOOT DOOR FITTINGS AND PERFORMED OPS CK ON ASD IAW CRJ200 AMM 12-20-52 AND CRJ200 AMM 52-11-00. OPS CK GOOD A/C OK FOR SERVICE. [SDR CLOSED] 2 L 7 2 4F RT A21EA 20080811 EU 2008 8 11 COE2008F00001 1 20080714 A 7714 56777508012 INDICATOR AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 2 ENG TORQUE FAILED A COEA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 NM 13 919FX 266 ABORTED TAKEOFF, FLT NR 8202: DURING TAKEOFF ROLL THE CREW NOTICED THAT ANALOG PORTION ON THE NR 2 ENGINE TORQUE GAGE WA S INOPERATIVE. TAKEOFF WAS ABORTED AND THE AC WAS SAFELY TAXIED BACK TO THE BLOCKS. REMOVED AND REPLACED THE TORQUE GA UGE. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 20080811 EA 2008 8 11 S9B2008F00001 2 20080620 A 7230 COMPRESSOR DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA NR 2 ENGINE NOISY A S9BA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 29 562CP 562 PGO266 UNUSUAL NOISE NOTED IN COMPRESSOR SECTION NR 2 ENGINE, UPON START UP, REMOVED ENGINE FROM SERVICE WILL CLOSE SDR WHEN SO URCE OF NOISE IS FOUND AND CORRECTED. (K) 1 H 7 2 3T 4 T RT A9EA E4EA 20080820 2008 8 20 SWAA084301 4 20080803 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843267 1 20080718 A 5753 6546430132 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 RT IB FOREFLAP LOWER SURFACE HAS A DENT ON IB END REMOVED DAMAGE FABBED FILLER & DOUBLER, BONDED IAW SRM 51-70-10 REPAIR S. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084306 1 20080803 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084307 1 20080803 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080820 2008 8 20 SWAA084308 4 20080803 A 2565 6949956 CABLE BOEING 737 7373Q8 1384670 NM EVAC SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084309 1 20080803 A 3350 M1132 FUSE BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 690SW 23783 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED FUSE PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084310 1 20080803 A 5330 65C38192 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 515, STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084312 1 20080803 A 5753 115A2714 FLAP BOEING 737 7377H4 1384404 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 776WN 30591 DURING SCHEDULED 8Y CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20080819 SO 2008 8 19 SWIA200819933 1 20080723 A 5310 WINDOW FRAME EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 FUSELAGE FRAME BEHIND CAPTS DV WINDOW IS CRACKED. (FOUND AT C-CHECK) REPLACED CRACKED FRAME IAW SRM 51-10-02 PAR 3. 2 L 7 2 4T RT A31SO 20080819 WP 2008 8 19 UPS08852991 1 20080805 A 2910 FITTING DOUG DC8 DC873F 302199F WP HYD SYSTEM INOPERATIVE A IPXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 874UP 46074 IN CRUISE, HYD QTY DROPPING RUN CK LIST, STOPPED AT AUX PUMP LEVEL. PRESS NEVER BELOW 3000 PSI. R/R HYD FITTING AT LT M LG AFT HYD MANIFOLD, FAR OB POS FOR BOGIE TR TRIM CYL. REPACKED FITTING W/REF TO AMM 2-13-00-2. SERVICED MAIN HYD RESERV IOR W/REF TO AMM 12-30-01-3. NO LEAKS NOTED. OK FOR SERVICE. 2 L 7 4 4F RT 4A25 20080819 NM 2008 8 19 PID2008F00012 1 20080808 A 2560 P4010021 BATTERY BOEING 737 7372K5 138448X NM FLASHLIGHT INOPERATIVE A PIDA O OTHER O OTHER NR NOT REPORTED 1 SO 05 250TR 22597 FOUND FWD F/A FLASHLIGHT NOT WORKING. REPLACED BATTERY IN FLASHLIGHT. OPS CHECK GOOD, AMM 25-69-0. (S) 2 L 7 2 4F RT A16WE 20080819 SO 2008 8 19 SWIA200819905 1 20080725 A 2611 47359713 SMOKE DETECTOR EMB 120 EMB120ER 3260203 SO CARGO BAY FALSE ACTIVATION A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 584SW 9976 9976 120352 BAGGAGE SMOKE "WARN" ON GLARESHIELD. (FLIGHT NR 3610) REPLACED AFT CARGO SMOKE DETECTOR IAW AMM 26-15-01. OPS CHECK GO OD. 2 L 7 2 4T RT A31SO 20080819 WP 2008 8 19 UPS08853010 1 20080724 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C1, COCKPIT FLOOR PNL 680 HAS 1 FASTENER HOLE WITH IMPROPER E.D. AND 1 FASTENER HOLE CRACKED TO EDGE. CUTOUT CRACKED AREA IAW SRM 53-02-00 FIG 23, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-02-00,51-01-21. 2 L 7 4 4F RT 4A25 20080819 EA 2008 8 19 SWIA200819925 1 20080803 A 7120 BUSHING CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* 30015 NE LT ENG MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 706SK 10149 LT ENGINE FWD MOUNT LINK AND BUSHINGS ARE CORRODED. REPLACED LT ENGINE LINK AND BUSHINGS IAW AMM 71-00-00. 2 L 7 2 4F 4 F RT A21EA 20080819 EU 2008 8 19 NWAA083653351 1 20080803 A 3350 NWAD321430 BATTERY PACK AIRBUS A330 A330223 3940031 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 851NW 00609 DURING 1/2 A-CHECK, FOUND EPSU BATTERY FOR LOWER DECK CREW REST BAD. REPLACED BATTERY PACK IN EPSU 19WL, CHECKS GOOD. (S) 2 L 7 2 4F RT A46NM 20080819 EA 2008 8 19 SWIA200819913 1 20080725 A 3520 OXYGEN MASK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* 30015 NE CABIN UNWANTED DEPLOY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 927SW 7693 02 MASKS DROPPED WHEN HYDRAULICS WERE SELECTED ON USING GPU AT THE GATE. RESTOWED ALL 02 MASKS IAW MM 35-13-00. OPS CH ECK GOOD. 2 L 7 2 4F 4 F RT A21EA 20080819 EA 2008 8 19 SWIA200819908 1 20080729 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT LOOSE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 926SW 7687 EMERGENCY FLOOR LIGHTING IS INOPERATIVE. (FLIGHT NR6016) SECURED CONNECTOR ON EMERGENCY LIGHTS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080819 WP 2008 8 19 UPS08852996 1 20080728 A 5340 37797624501 FITTING DOUG DC8 DC871F 302199D WP BS 680 L6R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C1, MAIN CABIN, FUSELAGE SPLICE FITTING CRACKED STA 680 L-6R. REMOVED AND REPLACED FITTING IAW SRM 51 -03-01. 2 L 7 4 4F RT 4A25 20080819 WP 2008 8 19 UPS08852997 1 20080805 A 2910 LINE DOUG DC8 DC871F 302199D WP HYD SYSTEM LEAKING A IPXA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 718UP 46018 CREW LOST HYDRAULIC QTY AND PRESSURE. AFTER TOP OF CLIMB, CREW DECLARED AN EMERGENCY. LANDED SAFELY AND A/C WAS TOWED T O GATE. FOUND HYD LINE FOR BOGIE TRIM CYL LOCATED ON REAR SIDE OF THE LT LANDING GEAR, LEAKING. REMOVED AND RE-INSTALLE D A FLEX LINE AS NEEDED SECURED LINE. PRESSURED HYD SYS. OPS AND LEAK CHECK GOOD. 2 L 7 4 4F RT 4A25 20080819 NM 2008 8 19 UPS08M53017 1 20080711 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 17 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INSTAL LED BUSHING IAW E.O. MD1-5510-19409-N AND SAA TRAVELER 80538320001. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M53024 1 20080716 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 15 LT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED R EPAIR BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 SO 2008 8 19 C2X2008F00018 1 20080805 A 3350 82321 LIGHT EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE O OTHER CR CRUISE 1 SW 27 34110 11952 11952 145658 ACFT WAS IN FOR A SERVICE CHECK AND THE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE AT ROW 12. MAINTENANCE REMOVED AND R EPLACED THE EXIT ROW 12 IAW EMB 145XR AMM 3350-08. OPS CHECK GOOD AND WAS RELEASED BACK TO SERVICE. (S) 2 L 7 2 4F RT 20080819 NM 2008 8 19 UPS08M53016 1 20080713 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 14 RT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED BUSHING, AND INSTA LLED BUSHING IAW E.O. MD11-5510-19409-N AND SAA TRAVELER 80538430001. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M52970 1 20080423 A 5320 FLOOR SUPPORT DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:C, REFERENCE TO EO MD11-5310-27496D, UNABLE TO OBTAIN SUPPORT ASSY ABA7430 -1 OR THE RAW MATERIAL DUE TO LONG LEAD TIME SUPPORT FABRICATED IAW DWG ABA7430 & EN NR 1172-08. FPI C/O IAW DP S 4.707 REV 'AW'. NO CRACK EVID ENT ON FABRICATED FLOOR SUPPORT. FLOOR SUPPORT REPROTECTED IAW SRM51-21-01 VII R35. FLOOR SUPPORT LOCATED & INSTALLED IAW DWG SP11530074 & EN 1172-08 AND REFER EO MD11-5310-2 7496-D. 2 L 7 3 4F RT A22WE 20080819 2008 8 19 UPS08553008 2 20080805 A 7200 ENGINE BOEING 757 75724APF 1384969 NM LEFT VIBRATION A IPXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 470UP 25486 LT ENG VIBRATION IN AMBER BAND. VIBRATION NORMAL AT IDLE. OCCURRED AT THRUST REDUCTION AT TOP OF CLIMB. COMPLIED WITH S TEPS 1-4 OF FIM 71-05-00 FIG 108 WITH NO DEFECTS NOTED. COMPLETED ALL REMAINING STEPS OF FIM 71-05-00 FIG 108. VIBRATION SURVEY C/W ALL WITHIN LIMITS. 2 L 7 2 4F RT A2NM 20080819 SO 2008 8 19 C2XA08CL087 1 20080721 A 3297 D3899926FA98SA CONNECTOR EMB 145 EMB145LR 3260212 SO NR 4 BRAKE FAULTY A C2XA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SW 27 13989 145271 CLE FLIGHT 2311 - THE CREW REPORTED A NR 4 BRAKE OVERTEMP MESSAGE IN FLIGHT. AN EMERGENCY WAS DECLARED AND THE ACFT LAN DED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 4 BRAKE TEMP SENSOR CONNECTOR. OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4T RT T00011AT 20080819 NM 2008 8 19 ASAA0843317 1 20080630 A 5320 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 767-779 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AFT PIT FLOOR SUPPORT AT STA 767 LBL 3.0 IS CORRODED REMOVED DAMAGED AREA FABBED REPAIR PARTS & INSTALLED IAW ASA EA 532 0 01844. 2 L 7 2 4F 4 F RT A16WE E21EU 20080819 NM 2008 8 19 F3LA200800529 1 20080731 A 5315 D5347217220500 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2 2209 DURING C3 C-CHECK, INSPECTION NOTED CORROSION AROUND THE NUT PLATE HOLE ON FLOORBEAM Y1292 AT FRAME 67, AND TOOLING MARK BETWEEN FRAME 67 AND 68 APPROXIMATELY 8 INCHES LONG. MAINTENANCE REMOVED AND REPLACED FLOORBEAM Y1292 BETWEEN FRAME 67 AND FRAME 68, IAW THE REQUIREMENTS OF A319 SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCE PTABLE. (S) 2 L 7 2 4F RT A28NM 20080819 NM 2008 8 19 KCSA081373 1 20080805 A 5330 SKIN BOEING 747 747122 1384872 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STA 1740 STR 34R SKIN DAMAGED AROUND FASTENERS. (S) 2 L 7 4 4F RT A20WE 20080819 NM 2008 8 19 SWAA084159 1 20080727 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084192 1 20080728 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084223 1 20080729 A 5755 HINGE BOEING 737 7373H4 1384600 NM NR 5 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW MA3136 23697 RIGHT WING NR 5 GROUND SPOILER HINGE BROKEN. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084229 1 20080729 A 5754 65C26603202A SLAT BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084234 1 20080731 A 5311 6546530 FRAME BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 460, STR 28R TO STR 28L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843229 1 20080624 A 5330 655298865 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 986-1016 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 FUSELAGE SKIN IS DENTED. REPLACED DAMAGED SECTION IAW SRM 51-40- 02. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843231 1 20080729 A 5320 65479765 CUSP WEB BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 810-825 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 CUSP WEB IS CORRODED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR IAW SRM 51 70 13. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 2008 8 20 SWAA084267 4 20080801 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084317 1 20080804 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 268WN 32524 L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843301 1 20080624 A 5330 6546881115 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 1026-1040 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 DENT IN FUSELAGE LT SIDE AFT OF PRESSURE BULKHEAD CUTOUT DAMAGED AREA FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW ASA EA 533002375. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843304 1 20080624 A 5330 65458001139 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 196 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 REF SAD 5785173: DENT & CREASE ON BOTTOM OF FUSELAGE AT APPROX STA 196 FWD OF ACCY DOOR REMOVED DAMAGED AREA FABBED REPA IR PARTS AND INSTALLED IAW EA 5330 02373. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843314 1 20080626 A 5754 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 SLAT LOWER SURFACE IB END IS CHAFED. REMOVED DAMAGED AREA FABRICATED A DOUBLER AND BONDED THE REPAIR SRM 51-70-10 REPAI R 4. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843311 1 20080625 A 5753 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU RT WING TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 RT IB FORE FLAP CHAFED ON THE TOP IB SIDE REMOVED PREVIOUS DOUBLER PREPPED AREA, FABBED REPAIR & BONDED REPAIR IAW SRM 5 1-70-10 REPAIR 2. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084320 1 20080804 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084330 1 20080802 A 3211 6546544 FITTING BOEING 737 7373Y0 1384671 NM LT MLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED SPV CHECK, FOUND LT MLG W/W BS 695 FITTING WEB CRACKED. REMOVED AND REPLACED FITTING PER SRM AND BOEIN G DRAWING. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084336 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0893177 1 20080712 A 5210 571411 GUST LOCK BOEING 737 737990 NM GE CFM56 CFM567B24 NE L1 DOOR STUCK A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 303AS N6000670 30016 FA REPORTS GUST LOCK L1 DOOR VERY DIFFICULT TO UNSEAT CLEANED AND LUBED L1 DOOR HOLD OPEN LOCK. OPS CK OK. 2 L 7 4 4F 4 F RT A16WE E00055EN 20080820 NM 2008 8 20 ASAA0873178 1 20080713 A 5220 144A65942 BEARING BOEING 737 737790 13844CN NM EMERGENCY EXIT DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 612AS AC612 30162 RT OVERWING EMERGENCY EXIT DOOR WILL NOT OPEN HANDLE OPENS BUT DOES NOT UNLATCH. OPENED MIG 2C-222854. FOUND RT OVERWIN G EMER DOOR LOWER AFT BEARING PLATE DAMAGED. INSTALLED BEARING PLATE DOOR RIG, CK GOOD REF 52-22-00-820-801 REQ'S EMERG EXIT DOOR SYST TEST (PSEU). ACCOMPLISHED EMERG EXIT DOOR SYS TEST OK IAW 52-22-00-400-801. 2 L 7 2 4F RT A16WE 20080811 EU 2008 8 11 PDL2008F00000 1 20080611 A 6123 8551 AUTOFEATHER SYS CASA CN235 CN235 2410306 EU FAILED A PDLA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 27 1269J 012 AUTOFEATHER FAIL LIGHT ILLUMINATED. AUTOFEATHER COMPUTER REPLACED AND AC RETURNED TO SERVICE. (K) 2 H 7 2 4T RT A21NM 20080811 CE 2008 8 11 DXTA200803106 1 20080608 A 2120 UNKNOWN CESSNA 750 750 2076810 CE COCKPIT FUMES E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 950QS 7500050 CREW NOTED FUMES IN COCKPIT WHILE LEVEL AT FL350. (B) 2 L 7 2 4J RT T00007WI 20080811 SO 2008 8 11 MCC2008F00002 2 20080601 A 8530 CYLINDER BEECH 58 58 1152740 CE CONT O550 IO550C SO NR 4 DAMAGED E MCCA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SW 11 106GA TH437 824276R ENGINE STARTED RUNNING ROUGH AND PILOT NOTICED OIL LEAKING ON COWLING. ENGINE WAS SECURED AND A UNEVENTFUL LANDING MADE . MAINT FOUND CYL NR 4 HAVING BROKEN STUDS AND CYLINDER STARTING TO SEPARATE FROM ENGINE. ALSO FOUND ROCKER BOX COVER SCREWS LOOSE/MISSING. ENGINE REMOVED FOR REPAIR. (K) 1 L 7 2 3O 3 O 3A16 E3SO 20080811 NM 2008 8 11 HNA2008F00021 1 20080702 A 3350 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS MALFUNCTIONED A HNAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 07 930HA 126 CABIN EMERGENCY LIGHTS INTERMITTENT ILLUMINATION DURING TAXI AND FLIGHT. A/C FERRIED FOR REPLACEMENT OF LIGHTS CONTROL B OX. OPS CHECKED GOOD. (K) 2 H 7 2 4T RT A13NM 20080811 NM 2008 8 11 C8G2008F00007 1 20080620 A 5210 DOOR BOEING 757 757232 1384965 NM MAIN PAX OUT OF ADJUST A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 620DL 22910 DURING CLIMB OPERATION THE FWD ENTRY DOOR EICAS MESSAGE APPEARED WITH THE ASSOCIATED OVERHEAD LIGHT. THE ACFT RETURNED WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED THAT THE FWD ENTRY DOOR WAS NOT CENTERED IN THE DOOR FRAME WHEN CLOSED. THE FWD ENTRY DOOR HINGE WAS REMOVED AND REPLACED. OPS AND LEAK CHECK GOOD. NO OTHER DEFECTS WERE NOTED. AC WAS RETURNED TO SERVICE. (K) 2 L 7 2 4F RT A2NM 20080811 NM 2008 8 11 WRL2008F00005 1 20080624 A 3210 ACA7061 FITTING DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE MLG CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 380WA 48407 DURING LANDING GEAR REPLACEMENT, MAINT FOUND CORROSION ON CENTER LANDING GEAR LT PILLOW BLOCK AFT UPPER SURFACE OF PILLO W BLOCK AFT BOLT HOLE CORRODED. REWORKED AREA IAW SRM 53-40-00 FIG 16 IAW SERVICE REQUEST ID 1-8801879663.(K) 2 L 7 3 4F 4 F RT A22WE E24NE 20080811 CE 2008 8 11 26N2008F00001 1 20080804 A 2710 CONTROL CABLE CESSNA 510 510 2076617 CE PWC PW615 PW615FA 52282 NE AILERON FROZEN E 26NA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 EA 05 1693L 5100026 CREW REPORTED AILERONS FROZE AFTER FLYING THROUGH MOISTURE. AC REPOSITIONED FOR FURTHER EVALUATION AND RESOLUTION. (K) 1 L 7 2 4F 4 F RT A00014WI E00073EN 20080811 CE 2008 8 11 ACS2008F00000 1 20080603 A 3097 2TC1220 CIRCUIT BREAKER CESSNA 402 402C 207590R CE DEICE SYS BURNED E ACSA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 AL 01 4630N 402C0001 ELECTRICAL ODOR AND SMOKE IN CABIN DURING APPROACH. SUBSEQUENT INSPECTION FOUND LOOSE SCREW SECURING WIRE TO CIRCUIT BR EAKER TERMINAL AND EVIDENCE OF ARCING. (K) 1 L 7 2 3O A7CE 20080811 WP 2008 8 11 AALA200801710 1 20080626 A 3397 GROUND WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 418AA 49329 SFO - EMERGENCY LIGHTS AT SEAT ROWS 18 TO AFT CABIN INOPERATIVE. SECURED GROUND WIRE AT OVERHEAD SEAT ROW 18 FOR EMERGE NCY LIGHTS AT SEAT ROWS 18 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 NM 2008 8 11 AALA200801662 1 20080618 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 673AN 29423 DFW - EMERGENCY LIGHT AT AFT COACH CABIN INOPERATIVE. REPLACED BATTERY PACK AT STATION 1635 FOR EMERGENCY LIGHT AT AFT COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 WP 2008 8 11 AALA200801745 1 20080701 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 587AA 53250 LGA - EMERGENCY LIGHT AT FIRST CLASS CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 NM 2008 8 11 AALA200801545 1 20080606 A 3350 PBS73 BATTERY PACK BOEING 767 767223 1385123 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 329AA 22329 JFK - EMERGENCY EXIT SIGN LIGHT AT OVERHEAD RT BY MID LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SI GN LIGHT AT OVERHEAD RT ON BY MID LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080811 NM 2008 8 11 AALA200801649 1 20080617 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 925AN 29526 DFW - EMERGENCY LIGHT AT SEAT ROW 12 MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT ROW 12. SYSTEM GROUND C HECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A16WE 20080811 WP 2008 8 11 AALA200801651 1 20080607 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9412W 53187 SFO - EMERGENCY LIGHT AT SEAT 9D INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY LIGHT AT SEAT 9D. SYSTEM GROUND CHECK ED NORMAL OPERATION. (A) 2 L 7 2 4F RT A6WE 20080811 NM 2008 8 11 AALA200801650 1 20080617 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 198AA 32392 DFW - EMERGENCY LIGHTS AT RT OVERWING EXIT MARKER INOPERATIVE. REPLACED BATTERY PACK AT M10568 FOR EMERGENCY LIGHTS AT RT OVERWING EXIT MARKER. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 NM 2008 8 11 AALA200801609 1 20080613 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AM 24594 DFW - EMERGENCY LIGHT AT SEAT 14D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 14D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 NM 2008 8 11 AALA200801668 1 20080619 A 3350 0219241005 SIGN BOEING 737 737823 13844BZ NM CABIN CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 902AN 29504 LGA - EMERGENCY LIGHT EXIT SIGN AT AFT GALLEY DOOR CRACKED. REPLACED EXIT LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT AFT GAL LEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A16WE 20080811 WP 2008 8 11 AALA200801641 1 20080617 A 2160 319886211 VALVE DOUG DC9 DC982 3022082 WP A/C BAY INOPERATIVE A AALA A UNSCHED LANDING J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 472AA 49647 DFW INFLIGHT T1550/17 JUN. RT AIR CONDITIONING SUPPLY TEMPERATURE HIGH INDICATION ON CLIMB. CREW REPORTED AN OVERHEAT SMELL. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED PRESSURE TRANSMITTER VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 NM 2008 8 11 AALA200801514 1 20080604 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 783AN 30004 DFW - EMERGENCY LIGHTS AT MID COACH CLASS INOPERATIVE. REPLACED BATTERY PACK AT STATION 1518 FOR EMERGENCY LIGHT AT MID COACH CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080811 EU 2008 8 11 AALA200801775 1 20080705 A 3350 P4010049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 33069 512 SJU - EMERGENCY LIGHT BATTERY PACK AT SEAT ROWS 6 TO 18 FAILED TEST. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 6 TO 18. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A35EU 20080811 NM 2008 8 11 RYN2008F00001 1 20080711 A 2910 HYDRAULIC SYSTEM BOEING 757 757200 1384950 NM LEFT LOW PRESSURE A RYNA O OTHER J WARNING INDICATION CR CRUISE 1 GL 31 151GX 24451 AIR TURN BACK DUE TO LT HYDRAULIC LOW PRESSURE LIGHT AND PTU STATUS MESSAGE APPEARED ON EICAS SCREEN. ACCOMPLISHED PTU SYS CHECK IAW FIM 29-22-00, FIGURE 104, OPS CHECKED NORMAL. PLACED ON DEFERRAL, THE LT HYDR PUMP LOW PRESSURE INDICATIO N SYS IAW MEL 29-31-02. (K) 2 L 7 2 4F RT A2NM 20080811 NM 2008 8 11 MWE2008F00028 1 20080801 A 3350 2232 LAMP BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE EMERGENCY LIGHT INOPERATIVE A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 926ME 55192 LT WING EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT. (K) 2 L 7 2 4F 4 F TR A6WE E00061EN 20080811 CE 2008 8 11 DJFA2008063 1 20080714 A 7160 INLET BEECH MU300 400A 1155402 CE RT ENGINE CRACKED A DJFA O OTHER O OTHER NR NOT REPORTED 1 EA 23 470LX RK478 REPORTED RT ENGINE INLET CRACKED AT 9:00 POSITION. OPEN. (S) 2 H 7 2 4F RT A16SW 20080811 NM 2008 8 11 HNA2008F00020 1 20080702 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A HNAA O OTHER O OTHER CR CRUISE 1 EA 07 846EX 326 3 OCCURRENCES IN A ROW OF EMERGENCY LIGHTS GOING ON IN FLIGHT. NR 1 FLT 4577 CLT, NR 2 4276 GSP, NR 3 4196 MDT. CREW RE PORTED: NR 1 REMOVED AND REPLACED EMERGENCY LIGHTS CONTROL BOX AC RELEASED FOR SERVICE. FAILED AGAIN, SAME PROBLEM NR 2 FLIGHT, F/A PANEL EMERGENCY LIGHT SWITCH WAS REPLACED AND AC RELEASED FOR SERVICE. FAILED AGAIN ON NR 3 FLIGHT AND EME RGENCY LIGHT POWER SUPPLIES WERE REPLACED. DATE OF ENTRY IN AC RECORDS IS JULY 3, AS OF THIS DATE JULY 4, NOT REPORTED AS TO FURTHER DISCREPANCIES. REPORT WILL BE AMENDED UPON FURTHER INFORMATION. (K) 2 H 7 2 4T RT A13NM 20080811 NM 2008 8 11 DXTA200803172 1 20080714 A 5100 UNKNOWN GULSTM 200 200 4500308 NM UNKNOWN UNKNOWN E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 701QS 141 NO A/S ON TAKEOFF ROLL, ABORTED T/O. (A) 2 L 7 2 4F RT A53NM 20080811 CE 2008 8 11 DXTA200803159 1 20080703 A 3150 WARNING MESSAGE CESSNA 750 750 2076810 CE ILLUMINATED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 916QS 7500116 AFTER TAKEOFF WE BROUGHT THE THRUST LEVERS TO CLIMB POWER. AT THAT TIME RECEIVED A RED CAS "PYLON BLEED LEAK L" MESSAGE. EMERGENCY DECLARED. (A) 2 L 7 2 4J RT T00007WI 20080811 CE 2008 8 11 71108N504CS1 1 20080711 A 2161 99125185 CONTROLLER CESSNA 560 560XL 2076702 CE CABIN TEMP FAILED E Z5FA O OTHER O OTHER CR CRUISE 1 EA 63 504CS 6287 5605229 DURING CRUISE AT FLIGHT LEVEL 350 CABIN CLIMBED TO 10,000 FT WITH ASSOCIATED CABIN ALTITUDE ANNUNCIATION. AN EMERGENCY DESCENT TO FLIGHT LEVEL 220 WAS MADE AT WHICH TIME THE CABIN ALTITUDE WAS CONTROLLABLE. THE ACFT DIVERTED TO AN AIRPORT WHERE REPAIRS COULD BE MADE. THE CABIN TEMP CONTROLLER WAS REPLACED AND THE AC RETURNED TO SERVICE. (S) 2 L 7 2 4F RT A22CE 20080811 NM 2008 8 11 AALA200801789 1 20080707 A 2560 BATTERY BOEING 777 777223 1385213 NM FLASHLIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 775AN 29584 LHR - EMERGENCY FLASHLIGHT AT RT NR TWO DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT RT NR TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080811 NM 2008 8 11 AALA200801614 1 20080613 A 3350 TRIM PANEL BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 636AM 24594 DFW - EMERGENCY LIGHT BULLNOSE TRIM AT SEAT ROW 14 LOOSE. SECURED BULLNOSE TRIM FOR EMERGENCY LIGHT AT SEAT ROW 14. SY STEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 2008 8 11 AALA200801810 4 20080708 A 2565 AAP3109 SLIDE BOEING 767 767323 1385205 NM DOOR FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 344AN 33083 SFO - LT OVERWING SLIDE HESITATED DURING TEST DEPLOYMENT AND IMMEDIATELY DEFLATED. SLIDE WAS CAUGHT MOMENTARILY ON LATC H RODS. FOUND ONE ROD BENT AND ONE SHEARED. REPLACED SLIDE AND ACTUATORS FOR LT OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080811 EU 2008 8 11 WRN2008F00004 1 20080623 A 5320 SILL AIRBUS 300 A300B4203 3930306 EU CARGO DOORWAY FOD A WRNA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 05 510TA 100 AC AFTER TAKEOFF, LOUD WHISTLING NOISE HEARD AND AC HAD PROBLEMS PRESSURIZING. AC MADE UNSCHEDULED STOP, WITH NORMAL LAN DING. FOUND F.O.D. AND DEBRIS IN MAIN CARGO DOOR SILL AREA. REMOVED F.O.D. AND DEBRIS FROM CARGO DOOR SEAL AREA IAW 52-7 0-00. SEAL FOR MAIN CARGO DOOR INSPECTED IAW A300 52-36-11 SUPPLEMENT MANUAL, SEAL LEAK CK SATISFACTORY. AC RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A35EU 20080811 CE 2008 8 11 GUU2008F00008 1 20080620 A 2910 1013880167 HOSE BEECH 1900 1900D 1154162 CE HYD SYSTEM LEAKING A GUUA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 17 190YV UE190 FLIGHT 9159, DURING APPROACH, LANDING GEAR CIRCUIT BREAKER RELAY POPPER TWICE MANUALLY EXTENDED LANDING GEAR, DISCOVERED HYD FLUID LEAKING FROM RT WHEEL WELL. C/A REPLACED RT MLG ACTUATOR RETRACT HOSE ASSY. (A) 2 L 7 2 4T RT A24CE 20080811 CE 2008 8 11 GUU2008F00011 1 20080622 A 5220 HANDLE BEECH 1900 1900D 1154162 CE EMERGENCY EXIT FROZEN A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 81535 UE147 DURING SCHEDULED ROUTINE MAINT, DISCOVERED RT AFT EMERGENCY EXIT OUTER HANDLE FROZEN. CLEANED AND LUBRICATED RT AFT EMER GENCY DOOR OUTER HANDLE. (A) 2 L 7 2 4T RT A24CE 20080811 NM 2008 8 11 AALA200801683 1 20080622 A 3397 PIN BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 39356 24037 DFW - EMERGENCY LIGHTS AT SEAT ROW 4AB DIM. SECURED LOOSE PIN FOR EMERGENCY LIGHTS AT SEAT ROW 4AB. SYSTEM GROUND CHEC KED NORMAL OPERATION. (A) 2 L 7 2 4F RT A1NM 20080811 NM 2008 8 11 AALA200801701 1 20080625 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 762AN 31479 JFK - EMERGENCY LIGHT AT SEAT 32G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 32G. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080811 WP 2008 8 11 AALA200801765 1 20080703 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 479AA 49654 LGA - EMERGENCY EXIT SIGN LIGHT AT RT FORWARD OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT SIGN LIGHT AT RT F ORWARD OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 SO 2008 8 11 GLB2008F00008 1 20080714 A 2130 12042892001 SHAFT EMB 120 EMB120ER 3260203 SO LT VENT WORN A GLBA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 03 108UX 120108 SIGNIFICANT EVENT - ACFT 108UX DIVERSION TO CYS FLT 5121. PILOTS REPORTED RAPID DEPRESSURIZATION AT 25,000 FT. PASSENG ER OXYGEN MASKS DROPPED. LT SHAFT ASSY (P/N120-42892-001) AND COVER DOOR P/N120-48319-001 IN THE LT VENTILATION VALVE A SSY WERE REMOVED ANRE REPLACED IAW MM 21-51. OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4T RT A31SO 20080811 SO 2008 8 11 GLB2008F00009 1 20080717 A 2613 M11951752429902 SENSOR EMB 120 EMB120ER 3260203 SO LT DUCT LEAK WORN A GLBA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 03 108UX 120108 INFLIGHT SHUTDOWN - AIR RETURN - AC N108UX - FLT5136 ENROUTE, PILOTS REPORTED A NR1 ENG DUCT LEAK, WAITED FOR THE ANNUNC IATOR TO EXTINGUISH WITHOUT LUCK. PILOTS SHUTDOWN THE NR1 ENG AND RETURNED TO DEPARTURE CITY "LBF". MAINT REMOVED AND REPLACED THE LT DUCT LEAK SENSORS IAW MM 36-10 AT 5 LOCATIONS ALONG THE DUCT. ADDITIONALLY THEY REMOVED AND REPLACED T HE DUCT BOOT AND O-RINGS THAT APPEARED WORN ON THE BLEED AIR COUPLING ON TOP OF THE LT WING. OP CHECKS WERE GOOD. (S) 2 L 7 2 4T RT A31SO 20080811 NM 2008 8 11 AALA200801716 1 20080626 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 685AA 25342 DFW - EMERGENCY LIGHT AT FIRST CLASS CABIN. REPLACED BATTERY PACK AT M10798 FOR EMERGENCY LIGHT AT FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F RT A2NM 20080811 NM 2008 8 11 AALA200801521 1 20080604 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 762AN 31479 DFW - EMERGENCY LIGHTS AT SEAT 36C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 36C. SYSTEM GROUND CHECKED N ORMAL OPERATION. (A) 2 L 7 2 4F RT T00001SE 20080811 EA 2008 8 11 N6WA0080601 1 20080619 A 5220 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT FALSE ACTIVATION A N6WA O OTHER N FALSE WARNING LD LANDING 1 CE 03 151GJ 10216 RT EMERGENCY DOOR MESSAGE ON LANDING. PERFORMED OPS CHECK ON EMERGENCY DOOR. NO DEFECTS NOTED AT THIS TIME. (S) 2 L 7 2 4F RT A21EA 20080811 EU 2008 8 11 M7K2008F00091 1 20080324 A 5344 350A58004523 HINGE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE INLET CRACKED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 822MH 608 4142 23069 DURING ROUTINE INSPECTION, A CRACK WAS FOUND IN THE HINGE MOUNTING FLANGE RADIATING FROM THE OUTERMOST LT ATTACHMENT SCR EW BORE. REMOVAL OF ATTACHMENT SCREW REVEALED THE FLANGE CORNER HAD SEPARATED FROM THE REST OF THE HINGE. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080811 WP 2008 8 11 AALA200801787 1 20080707 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 236AA 49251 LGA - EXTERIOR EMERGENCY LIGHTS AT AFT CARGO INOPERATIVE. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHTS AT AFT CA RGO. SYSTEM GROUND CHECKED NORMAL OPERATION. (A) 2 L 7 2 4F A6WE 20080811 EU 2008 8 11 M7K2008F00093 1 20080324 A 6210 350A21491800 BLADE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE MAIN ROTOR CRACKED D M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 848MH 138 4290 23460 PREFLIGHT INSPECTION REVEALED THAT HAMMER BLADE HAD CRACKED IN TWO AND THE WEIGHTS AND BLADE WERE CAPTURED BY THE CONTAI NMENT BOX ASSY. AS THIS BLADE IS NORMALLY UNDER A 1200 FLEX PER MINUTE OPERATION IT IS EXPECTED TO WORK HARDEN OR FATIG UE OVER TIME. THIS BLADE FAILED AFTER A VERY SHORT TIME SPAN, HOWEVER, AS COMPARED TO NORMAL. SUSPECT A METAL DEFECT OF SOME NATURE. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20080813 WP 2008 8 13 NWAA083049865 1 20080707 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 774NC 47776 DURING THE LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAILED. MAINTENANCE REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (A) 2 L 7 2 4F RT A6WE 20080813 EA 2008 8 13 COMA086334 1 20080729 A 3610 9799981 VALVE CNDAIR CL600 CL6002B19 1900309 EA FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 589SW 5967 7072 ON CLIMBOUT FROM CVG LT A/C PACK FAILED OFF, RT A/C PACK FLUCTUATING IN PRESSURE. ACFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED LT 10TH STAGE SHUT OFF VALVE. (S) 2 L 7 2 4F RT A21EA 20080813 SO 2008 8 13 SIM2008F00020 1 20080725 A 3350 22013BR110049 CHARGER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 689EC 14500853 ON FLIGHT 4272 CREW NOTED ON THE GROUND THAT THE EMERGENCY FLOOR LIGHTS FROM 1A TO 7A WERE INOPERATIVE, AND 2 EXIT SIGNS , ONE BY SERVICE DOOR AND ONE ON FWD BULKHEAD WERE INOPERATIVE. ACFT REMOVED FROM SERVICE. REPLACED BATTERY AND CHARGE R ASSEMBLY FOR BATTERY POWER SUPPLIES 1 AND 2. ACFT RETURNED TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080813 EA 2008 8 13 TRAX200800934 1 20080726 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DIRTY A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 MAIN PASSENGER DOOR HANDLE REPORTED BY FLIGHT ATTENDANT, DIFFICULT TO STOW. ONCE STOWED, THE DOOR CLOSED INDICATION WAS DIFFICULT TO SHOW. COMPLIED WITH INSPECTION OF PAX DOOR LOCKING MECHANISM/CLEANED AND LUBED INNER HANDLE AND EXTERNAL HANDLE SERVICE LETTER RJ-52-003. (S) 2 L 7 2 4F RT A21EA 20080820 NM 2008 8 20 ASAA0843326 1 20080721 A 5730 65454288 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 776AS 25109 EXFOLIATION CORROSION FOUND ON UPPER WING SKIN AT FS 592 RBL 63 REPAIRED IAW EA 5710 01153. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 2008 8 20 SWAA084325 4 20080804 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 453WN 29847 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080820 2008 8 20 SWAA084326 4 20080804 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 477WN 33988 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084327 1 20080804 A 3350 20131A BATTERY PACK BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED MV1 CHECK, LT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084341 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084342 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084343 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084348 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084352 1 20080802 A 5743 115A5211 FITTING BOEING 737 7377H4 1384404 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 725SW 27857 DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084360 1 20080805 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 282WN 32534 DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0853217 1 20080722 A 2160 3989083 CONTROL VALVE BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE A/C PACK TEMP FAILED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 579AS 5582 35187 WHEN MASTER CAUTION RECALL PRESSED AIR CONDITIONING AND LT PACK LIGHT ILLUMINATED. WHEN MASTER CAUTION RESET BOTH LIGHT EXTINGUISH. CONFIRMED LT PACK TCV FAILED NR 1 ZONE TEMP CONT REF MM 21 51 00. REMOVED & REPLACED LT PACK TCV LK & OPS N ORMAL GROUND VERIFICATION SUCCESSFUL REF MM 21-51-10. LT PACK TEMP CONTROL VALVE VERIFIED REF IPC 21-51-10-03 ITEM 90. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 NM 2008 8 20 ASAA0853219 1 20080723 A 2160 3989083 CONTROL VALVE BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE A/C PACK TEMP FAULTED A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 585AS 3597 35683 ON RECALL AMBER "CONT CAB" ZONE TEMP LIGHT COMES ON. ZONE TEMP LIGHT GOES OFF ON RESET VERIFIED EXISTING FAULT ACCOMPLI SHED FIM TASK 21 62 00 810 842. FLIGHT DECK TRIM VALVE FAULT ON LT CONTROLLER. ACCOMPLISHED FIM 21 62 00 810 833. CON TROLLER BITE AND RESET OK WITH NO FURTHER FAULTS. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 NM 2008 8 20 ASAA0843200 1 20080630 A 5230 65C362311 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 AFT CARGO DOOR EXTERNAL SKIN HAS NUMEROUS DENTS WITH CREASES REMOVED DAMAGED SKIN FABRICATED LOCATED DRILLED AND INSTALL ED A REPLACEMENT SKIN IAW SRM 52-30-01 FIG. 201-51-40-02 PG. 2. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843202 1 20080630 A 5230 65C361831 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 FWD CARGO DOOR HAS APPROX 1 INCH DENT WITH CREASE IN AFT CENTER OF DOOR SKIN CUT OUT DAMAGED AREA FABRICATED LOCATED DRI LLED AND INSTALLED IAW EA 12766 AND EA NR 533002368. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843327 1 20080721 A 5730 65454288 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 776AS 25109 EXFOLIATION CORROSION FOUND ON UPPER WING SKIN AT FS 608.5 RBL 62 REPAIRED IAW EA 5710 01153. 2 L 7 2 4F 4 F RT A16WE E21EU 20080813 EA 2008 8 13 TRAX200800933 1 20080725 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 926EV 7843 LT AND RT FS 625 OBLIQUE ANGLES ARE CRACKED. OPEN. (S) 2 L 7 2 4F RT A21EA 20080814 WP 2008 8 14 IXX2008F00037 1 20080609 A 5754 SKIN DOUG DC8 DC872F 302199E WP SLOT VANE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON RT WING OUTBOARD SLOT VANE LEADING EDGE AT STATION XOLDO 67. 000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INS PECTION. NO CRACK, NO CORROSION FOUND. FABRICATED DOUBLERS, FILLERS, INTERNAL DOUBLERS. CLEANED, TREATED AND PRIMED A REA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XOLDI 6.224-XOLDO 67.000 IAW FAA FORM 8110-3 08378 DATED 07/11/2008, SEMAN DRAWING ED-4809 DATED 06/23/08, DC8 SRM 51-1-21, SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001 , DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-1-20D AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 EA 2008 8 14 TRAX200800930 1 20080725 A 5240 HANDLE CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 355CA 10067 SERVICE DOOR OUTER HANDLE BROKEN. REMOVED AND REPLACED SERVICE DOOR HANDLE IAW CRJ 700 AMM 52-41-03-000-081-A01 AND 52- 41-03-400-801-A01. COMPLIED WITH SERVICE DOOR OPERATIONAL TEST DUE TO HANDLE REPLACEMENT IAW CFR 700 AMM 52-41-00-710-8 01. OPS CHECKED GOOD. COMPLIED WITH RII PER SP607 AND CRJ 700 AMM 52-41-03-400-801-A01. ALL WORK FOUND SATISFACTORY A T THIS TIME MB7011995. (S) 2 L 7 2 4F RT A21EA 20080814 NM 2008 8 14 USAA920081434 1 20080724 A 5315 D53472189202 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803AW 0931 SAL - C7 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR67 TO FR69, -Y1292. REPLACED FLOORBEAM AT FR67 TO FR69, -Y1292 IA W SRM A319 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080814 CE 2008 8 14 DXTA200803202 1 20080728 A 8011 STARTER CESSNA 500 560CESSNA 2076750 CE LT ENGINE MALFUNCTIONED E DXTA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 302QS 5600402 STARTER DISENGAGE PROBLEM - ABORTED LT ENG START WHEN N2 AT 25% AND NO N1. ENG APPEARED TO SHUTDOWN NORMALLY. F/O CHEC KED, ENG WAS STILL RUNNING AND SMOKE WAS COMING OUT OF GENERATOR EXHAUST VENT, SHUT THE ENG DOWN USING THE ENG FIRE SWIT CH, ABOUT 20 SECONDS AFTER THROTTLE TO CUTOFF. (S) 2 L 7 2 4F RT A22CE 20080814 WP 2008 8 14 08FDEA03000 1 20080721 A 5420 WSP095913 BRACKET DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 NR 1 ENGINE INBD FAN COWL INTERIOR SURFACE BRACKET IS WORN AT APPROX THE 3 O'CLOCK POSITION. REMOVED BRACKET IAW SRM 51 -31-01, VOL II. FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01, VOL I AND DAC DWG PLWSPO959, REV H. MATERIAL ID 2024-T3, 0 .032 IAW DAC DWG PLWSP0959, REV H. FABRICATED A BRACKET IAW DWG PLWSP0959, REV H. ALODINED AND PRIMED IAW SRM 51-21-01 , VOL II. PART MARKED BRACKET FX WSP0959-13 IAW GMM 7-0-1000. INSTALLED BRACKET IAW SRM 51-31-01, VOL II. 2 L 7 3 4F RT A22WE 20080814 EU 2008 8 14 MAL2008F00015 1 20080723 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 CORROSION NOTED ON I/B FWD SIDE OF CENTER SEAT TRACK BL 0 STA 297-STA 303.25. REPAIRED IAW EOS53342. (S) 2 L 7 2 4T RT A52EU 20080814 WP 2008 8 14 IXX2008F00030 1 20080616 A 5320 FINGER DOUBLER DOUG DC8 DC872F 302199E WP COCKPIT CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND COCKPIT FINGER DOUBLER WITH CORROSION AT STATION FS 188.000-208.000 LT BOTTOM L INE 60. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK NO CORROSI ON FOUND FABRICATED SEGMENT PANEL, EXTERNAL REPAIR DOUBLERS, INTERNAL REPAIR FINGER DOUBLER, STRAPS, AND INTERNAL REPAI R FINGER DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-11, FAA F ORM 8110-3 08378 DATED 07/11/08 SEMAN DRAWING ED-4805 DATED 06/24/08, DC8 SRM 51-1-8B PAGES 17-18, DC8 SRM 53-2-0 PAGE 2 -M, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51-1-8B. (S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 IXX2008F00032 1 20080609 A 5753 SKIN DOUG DC8 DC872F 302199E WP T/E FLAP DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP UPPER SKIN DENTED AT STATION XW 104.000. REMOVED FASTENER S AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 1 ITEM "D", DC8 SRM 57-1-0 PAGE 1, SRM 51-1-2 1, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-3-0 AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 IXX2008F00041 1 20080609 A 5753 SKIN DOUG DC8 DC872F 302199E WP T/E FLAP MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND LT WING INBOARD FLAP UPPER SKIN HAS IMPROPER REPAIR AT STATION XW 104.000. REM OVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AR EA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 1 ITEM "D", DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-3-0, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 NM 2008 8 14 08FDEA02924 1 20080716 A 5220 50797890 FRAME BOEING 727 727233 138408A NM EMERGENCY HATCH CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 RIGHT FWD EMERGENCY HATCH FRAME LOWER OUTER SURFACE CORRODED BETWEEN SEAL RETAINER AND SKIN REMOVED CORROSION REF SRM 52 -00-2. NDT THICKNESS ORIG "T" .063 LOSS .005 .058. REMAINING DAMAGE WITHIN LIMITS REF SRM 53-10-1 FIG 1 SHEETS 1, 2, 3 . TREATED, PRIMED AND PAINTED REWORK REF SRM 51-10-2 AND MM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080814 NM 2008 8 14 08FDEA03052 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL TANK ACCESS CUTOUT 641HB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS C LASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080814 NM 2008 8 14 08FDEA03056 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL TANK ACCESS PANEL CUTOUT 641KB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAI R IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080814 EA 2008 8 14 TRAX200800943 1 20080728 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 GL 23 926EV 7843 JUST OUTBOARD LBL 9, FL 280 UPPER SILL CRACKED APPROX 1 INCH LONG AT MLG EMERGENCY RELEASE CABLE BRACKET. (S) 2 L 7 2 4F RT A21EA 20080814 NM 2008 8 14 WRLA2008068 1 20080804 A 5320 AEA0526 DOUBLER DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE CTR LDG BAY CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 276WA 48632 DURING "A4" CHECK INSPECTION IN ZRH FOUND TWO CRACKS IN THE LT AND RT MACHINED DOUBLERS IN THE CENTER LANDING GEAR BAY S TA Y=1381. THE CRACKS WERE LOCATED IN THE VERTICAL ROW OF RIVETS THAT ATTACH THE DOUBLER TO THE VERTICAL STIFFENER. TH E CRACKS STARTED AND ENDED IN RIVET HOLES. (S) 2 L 7 3 4F 4 F RT A22WE E24NE 20080814 NE 2008 8 14 YENA2008073 2 20080801 A 7230 COMPRESSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE STALLED A YENA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 EA 15 569JB 2075 FLT 1262, LGB-SMF, AIR RETURN TO LGB, ENG NR 1 COMPRESSOR STALL (ECAM) THRUST LEVERS AT CL DETENT LEVEL AT FL230 "BANG" AND YAW AND VIBRATION SAW ZERO EPR, THEN WENT BACK TO NORMAL. DID NOT SHUT DOWN IAW QRH 6-26. PERFORMED TSM 71-00-00-7 10-013-A, GVI, BLEED VVALVE CK, VSV LUBE, BOROSCOPE OK. HI POWER TEST NR 11, ALL TEST OK, CHECK OK, ALL ENG PARAMETERS NORMAL. ACFT OK FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A28NM E40NE 20080820 NM 2008 8 20 ASAA0843209 1 20080718 A 5340 STRINGER CLIP BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU BS 794 CORRODED A ASAA O OTHER O OTHER IN INSP/MAINT 1 NM 02 705AS 29318 STRINGER TIE CLIP AT BS 794 RBL 13.8 HAS CORROSION REPAIRED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843210 1 20080703 A 5311 54C323945 FRAME BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU BS 601 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 705AS 29318 FOUND CRACK ON LT FUSELAGE FRAME AT STA 601 DIRECTLY ABOVE THE CENTER WING REPAIRED IAW EA 5310 02804. PERFORM 1 STAGE DTA INSPECTION REQUIREMENTS WITHIN 12 MONTH FROM JUL 11 2008. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843325 1 20080721 A 5730 65454288 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 776AS 25109 EXFOLIATION CORROSION FOUND ON UPPER WING PLANK AT FS591, RBL67 REPAIRED IAW EA 5710 01153. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 EA 2008 8 20 TRAX0800933A 1 20080725 A 3397 PIN CNDAIR CL600 CL6002B19 1900309 EA CABIN NOT SEATED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 926EV 7843 JOB 8783411 OPERATION 37. RT OVERWING EMERGENCY EXIT (EYE LEVEL) LIGHT DOES NOT WORK FROM BATTERY PACK NR 4. TROUBLESH OT USING CRJ 200 WDM 33-51-00 AND 33-52-00 AND FOUND WIRE LY10D22 CONTACT PIN NOT SEATED IN TB105-3. SECURED WIRE CONTA CT INTO TERMINAL MODULE IAW EESPM 20-18-00. RT EMERGENCY EXIT SIGN NOW ILLUMINATES NORMALLY DURING BATTERY PACK 4 OP TE ST IAW AMM 33-51-04-710-801. SUPPLEMENTAL SDR CLOSED 7/31/08 (A) 2 L 7 2 4F RT A21EA 20080820 EA 2008 8 20 SWIA200819804 1 20080507 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 764SK FS 280 COCKPIT FLOOR SUPPORT IS CRACKED AT LBL 9. (FOUND AT C-CHECK) REPLACED COCKPIT FLOOR SUPPORT IAW SB 670BA-53-026 & SRM 51-42-06-001-001-A01 & 51-23-00-001-001-A01. 2 L 7 2 4F RT A21EA 20080820 EA 2008 8 20 SWIA200819892 1 20080717 A 3297 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE MLG DAMAGED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 767SK 10233 AFTER TAKE-OFF, RECEIVED A "GEAR DISAGREE" WARNING MESSAGE. (FLIGHT NR 6331) REPAIRED A PIN ON THE LANDING GEAR SELECT OR VALVE CONNECTOR. OPS CHECK GOOD IAW AMM 32-30-00. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080820 NM 2008 8 20 ASAA0843196 1 20080630 A 5330 6546881194 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU BS 1016 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 DENT ON FUSELAGE SKIN, STA1016 +16 LBL 8 IS CREASED REF SAD ITEM 5050829 CUT OUT DAMAGED AREA FABRICATED DOUBLER LOCATED DRILLED AND INSTALLED IAW SRM 53-80-01, FIG. 201, PAGES 201TO 205. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843199 1 20080701 A 5330 65C329541 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU BS 807 S26-27R DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 RT EXTERNAL FUSELAGE DENT BELOW AFT PIT OPENING STA 807, STR 26R TO STR 27R CUTOUT DAMAGED AREA FABRICATED FILLER AND RE PAIR DOUBLER LOCATED DRILLED AND INSTALLED IAW EA 5330 02363 AND EA 12774. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 EA 2008 8 20 SWIA200819856 1 20080709 A 3010 GG670800125 CONTROLLER CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE ANTI ICE SYS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 728SK 10192 LT BLEED DUCT MESSAGE ON CLIMB OUT WITH A LOSS OF PRESSURIZATION. (FLIGHT NR 6116) REPLACED ANTI ICE LEAK CONTROLLER A ND PERFORMED FLIGHT TEST. ALL CHECKS OK. P/N GG670-80012-3, S/N OFF: 00452. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080820 NM 2008 8 20 SWAA084564 1 20080813 A 3350 101114 LENS BOEING 737 7373Y0 1384671 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED HC2 CHECK, FOUND CENTER ISLE OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080819 SO 2008 8 19 C2XA08ON162 1 20080804 A 4930 UNKNOWN EMB 145 EMB145XR 3260214 SO APU FUEL PUMP LOOSE A C2XA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 27 12163 12325 6590 14500811 FLT 0210-SMF- FLIGHT CREW REPORTED APU LEAKING FUEL FROM DRAIN. CREW RESET APU MASTER AND FOUND PUMP IN THE ON POSITION . STARTED APU AND SYSTEMS. OPERATIONALLY AND LEAK CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. ( S) 2 L 7 2 4F RT 20080819 EA 2008 8 19 SWIA200819890 1 20080721 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR FAULTY A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 698BR 5839 5839 7799 WHEN SELECTING GEAR DOWN, RECEIVED THE GEAR DISAGREE WARNING MESSAGE. NOSE GEAR THEN LOCKED INTO PLACE. (FLIGHT NR 275 4) REPLACED NOSE DOOR SELECTOR VALVE IAW AMM 32-22-00. 2 L 7 2 4F RT A21EA 20080819 EA 2008 8 19 SWIA200819793 1 20080621 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA LEFT FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 963SW 7865 SMOKE COMING FROM THE AIR CONDITIONING VENTS. (FLIGHT NR 6760) DETERMINED LT PACK WAS OVERHEATING. REPLACED LT AIR CYC LE MACHINE IAW AMM 21-51-10. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080819 EA 2008 8 19 C2X2008F00019 2 20080807 A 7220 14575001409 INLET EMB 145 EMB145XR 3260214 SO RROYCE AE3007 AE3007A1E 54169 EA NR 2 ENGINE CORRODED A C2XA K NONE O OTHER CR CRUISE 1 SW 27 16178 14500889 TYS - DURING A 2C INSPECTION CORROSION WAS FOUND IN THE NR 2 ENG AIR INLET ATTACH POINT HOLES. MAINTENANCE REWORKED THE ATTACH POINT HOLES IAW EC 5420-01136 AND WILL BE RELEASED AT THE END OF THE C-CHECK. (S) 2 L 7 2 4F 4 F RT TE6CH 20080819 NM 2008 8 19 ASAA0843256 1 20080624 A 5330 654577683 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 727E S26L DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 REF SAD 4745257: EXTERIOR FUSELAGE STA 727E+13 IS DENTED ABOVE STR 26L DENT IS CREASED, REMOVED THE DAMAGE FABBED FILLER , DOUBLER, TRIPLER & INSTALLED REPAIR PARTS IAW SRM 53-00-01 REPAIR PG 231-233. 2 L 7 2 4F 4 F RT A16WE E21EU 20080819 CE 2008 8 19 DXTA200803216 1 20080805 A 2120 UNKNOWN CESSNA 680 680CE 2076811 CE CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 305QS 6800088 DIRTY SOCK ODOR COMING FROM AIR VENTS. (S) 2 L 7 2 4F RC T00012WI 20080819 NM 2008 8 19 SWAA084106 1 20080722 A 2121 64540501 FAN BOEING 737 7377H4 1384404 NM E&E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 924WN 36628 AT FL 390 FLIGHT CREW REPORTED A POSSIBLE ELECTRICAL ODOR IN CABIN, NO SMOKE. TURNED OFF GASPER AND RECIRC FANS ODOR DI SSIPATED. REMOVED AND REPLACED RECIRC FAN PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084133 1 20080727 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 290WN 36632 L1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080819 2008 8 19 SWAA084134 4 20080726 A 2565 D31354 SLIDE BOEING 737 7373Y0 1384671 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084135 1 20080727 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 LEFT OVERWING EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084160 1 20080727 A 2560 P4010021 BATTERY BOEING 737 737317 138447P NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 693SW 23174 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084166 1 20080728 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 213WN 34217 EEPLS END CAP MISSING AT ROW 1 ABC. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084167 1 20080728 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER 27R CORRODED AT BS 1006 TO BS 1016. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084171 1 20080728 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084193 1 20080728 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 3L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084189 1 20080728 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084182 1 20080728 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 2008 8 19 SWAA084204 4 20080728 A 2565 6949956 CABLE BOEING 737 7373Y0 1384671 NM EVAC SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084222 1 20080728 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULE 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 8R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084241 1 20080731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084250 1 20080731 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 232WN 32500 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080814 NM 2008 8 14 KCSA081377 1 20080811 A 5311 FRAME BOEING 747 747249F 1384849 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 FWD PIT BS640 FUSELAGE FRAME DENTED AT LBL29, WL101. (S) 2 L 7 4 4F RT A20WE 20080814 NM 2008 8 14 KCSA081350 1 20080727 A 5347 SEAT TRACK BOEING 747 747246B 1384864 NM COCKPIT CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 CAPTAIN`S FWD OUTBOARD SEAT TRACK IS CRACKED AT THE STOP. (A) (S) 2 L 7 4 4F RT A20WE 20080814 EU 2008 8 14 USAA920081458 1 20080801 A 2560 P4010021 BATTERY AIRBUS A321 A321211 3930370 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 186US 1701 FLT 1627 LGA-CLT - EMERGENCY EQUIPMENT - AFT EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BAT TERY. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080814 EU 2008 8 14 USAA920081491 1 20080807 A 3397 WIRE AIRBUS 320 A320232 3930326 EU CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 656AW 1079 FLT 296 LAS-SEA- EEL- AISLE EMERGENCY LIGHTING AT ROW 4L IS INOPERATIVE. MAINTENANCE RECONNECTED THE WIRING. OPERATION AL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 USAA920081453 1 20080727 A 5753 6546431279 FLAP BOEING 737 7374B7 1384702 NM LT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT-C2-MAJOR REPAIR - 11 INCH SPLIT AT INBOARD TRAILING EDGE AND 2 AREAS OF DELAMINATION ON LT OUTBOARD FOREFLAP. REPLA CED LT OUTBOARD FOREFLAP IAW B737 AMM 27-51-37. (S) 2 L 7 2 4F RT A16WE 20080815 WP 2008 8 15 08FDEA02935 1 20080716 A 5753 ARC1953502 SKIN DOUG MD10 MD1010F 3022112 WP RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 RIGHT WING OUTBD FLAP LOWER SURFACE SKIN HAS A DENT 29 INCH OUTBD OF THE SPRING CARTRIDGE. CHECKED THE DENT AND FOUND I T TO BE OUT OF LIMITS IAW DC/MD-10 SRM 57-10-00, FIG 48, VOL I. CUT OUT THE DAMAGED AREA. MATERIAL ID FOR THE DOUBLER IS 2024-T3, 0.050, PO 623408.1. FABRICATED DOUBLER IAW DC/MD-10 SRM 57-10-00, FIG 85, VOL I. ALODINED AND PRIMED IA W DC/MD-10 SRM 51-21-01, VOL II, PGS 21-24, VOL II. INSTALLED IAW DC/MD-10 SRM 51-35-02, VOL II. THE NON-ROUTINE NUMBE R DOCUMENTED ON THIS SDR IS INCORRECT. PLEASE CORRECT THE NON-ROUTINE NUMBER TO N00293. 2 L 7 3 4F RT A22WE 20080815 EU 2008 8 15 08FDEA02967 1 20080718 A 5100 NONE AIRBUS 300 A300B4622R 3930312 EU NOT AN SDR NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 743FD 630 FOUND OLD REPAIR AT SLAT NR 1 RT INBOARD ARM BASE, RIB 2 A, WITH REFENCE TO RAS/FOK/054/2004. REPAIR DEVIATES FROM RA S REPAIR RENEWED (SKIN INSERT ) IAW RAS/FOK/148/2008 ISS A, APPROVED BY EA 6-5742-120081. 2 L 7 2 4F RT A35EU 20080815 WP 2008 8 15 08FDEA03077 1 20080725 A 5755 SKIN DOUG MD10 MD1010F 3022112 WP NR 3 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 THE RIGHT WING NR 3 SPOILER IS DELAMINATED ON THE LOWER SURFACE AT THE INBD CORNER. REPLACED THE LOWER SKIN; DOUBLER & PARTIAL CORE. BONDED REPAIR IAW SRM 57-10-00; VOL I & SRM 51-71-00; VOL II. PRIMED & SEALED SPOILER IAW SRM 51- 21-01; VOL II. REMOVED; RE-INSTALLED & THE GAP & OPS CHECKS ARE GOOD IAW MD-10 AMM 67-60-01-4 & 27-60-01-1. 2 L 7 3 4F RT A22WE 20080815 EU 2008 8 15 08FDEA02477 1 20080625 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 675FE 789 MAIN DECK FLOOR SEAT TRACK HAS CORROSION, C76-C77;RBL 32. IN 2 SPOTS SEAT TRACK FOUND TO BE OUT OF LIMITS. RECEIVED A NEW TRACK P/N A5327400500053, PO 617932.1 PER SRM 53-18-16, PGS 3 AND 9. LOCATED AND DRILLED THE NEW TRACK PER A300-6 00 SRM 53-10-16. INSTALLED TRACK PER A300-600 SRM 51-41-21. APPLIED CIC PER A300-600 AMM 51-22-00-0. THIS SDR WAS GEN ERATED IN ERROR. FOR THE SDR DETAILS FOR N/R N00566 SEE SDR TRACKING NR 08-2476. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA02488 1 20080626 A 5411 A5461129900061Z RIB AIRBUS 310 A310222 3930315 EU PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 WEB CRACKED LOWER END FORWARD OF RIB 18 LEFT SIDE NR 2 PYLON. DRILLED CRACK STOP HOLES PER SRM 51-40-21. REMOVED THE R ELATED FASTENERS PER SRM 51-40-21. MANUFACTURED THE DOUBLER AND BROKE SHARP EDGES PER SRM 51-26-20. DRILLED FASTENER H OLES TO THE WEB AND THE DOUBLER PER SRM 51-40-50. INSTALLED THE DOUBLER PER SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA02500 1 20080626 A 5315 A53610731208 FLOORBEAM AIRBUS 310 A310222 3930315 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 MAIN DECK CROSSBEAM C14, LBL 55.0, INNERGRANULAR CORROSION ON LOWER FLANGE. REMOVED CORROSION PER SRM 51-74-10. MEASUR ED REMAINING THICKNESS PER NTM 51-10-04. FOUND WITHIN LIMIT (REMAINING THICKNESS: 0.096 INCH). APPLIED FLAP PEENING PE R SRM 51-29-00. REPAINTED AREA PER SRM 51-75-10. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA03089 1 20080725 A 5347 A25213126204 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 455FE 331 MAIN DECK FLOOR TRACK WITH EXFOLIATION CORROSION BETWEEN FR 15 TO FR 17 Y50. REPLACED THE FLOOR TRACK PER SRM51-40-21. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA03090 1 20080725 A 5347 A25213126204 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 455FE 331 MAIN DECK FLOOR TRACK WITH EXFOLIATION CORROSION BET FR 15 TO FR 17 Y50. REPLACED THE FLOOR TRACK PER SRM51-40-21. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA03091 1 20080725 A 5347 A25213126205 SEAT TRACK AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 455FE 331 MAIN DECK FLOOR TRACK WITH EXFOLIATION CORROSION FR15 - FR17 -Y50. REPLACED THE FLOOR TRACK PER SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080815 WP 2008 8 15 08FDEA03081 1 20080725 A 5755 SKIN DOUG MD10 MD1010F 3022112 WP NR 2 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 THE RIGHT WING NR 2 SPOILER SKIN IS DELAMINATED ON THE LOWER SURFACE AT THE INBD CORNER. THE REPAIR OF THE INBD LOWER C ORNER OF THE RT WING NR 2 SPOILER WAS ACCOMPLISHED ON NON-ROUTINE N00269. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 08FDEA03101 1 20080728 A 5512 ALC72051 SKIN DOUG DC10 DC1010 3022110 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 40061 46973 DURING INSP OF HORIZ STAB UPPER AND LOWER CONSTANT SECTION SKIN PLANK FLANGE, FOUND 4 PANEL WITH CRACK IN FLYABLE LIMIT , P/N 7208-1, P/N 7207-1, P/N 7205-1, P/N 7204-1, SEE ATTACHED INSPECTION FINDING FORM. REPAIRED AREA IAW EA NR 8-5510- 120477. 2 L 7 3 4F A22WE 20080815 WP 2008 8 15 08FDEA03073 1 20080725 A 5755 SKIN DOUG MD10 MD1010F 3022112 WP NR 2 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING SPOILER NR 2 IS DELAMINATED ON THE LOWER SURFACE AT THE INBD CORNER. 2 L 7 3 4F RT A22WE 20080815 NE 2008 8 15 08FDEA02586 2 20080630 A 7261 ENGINE AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7 52054 NE NR 2 FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 21 451FE 31879 303 707704 ECAM ADVISORY "NR 2 ENGINE OIL PSI ZERO". NO OTHER PROBLEMS, OIL QUANTITY 15 QTS, OIL TEMP 100 DEGREES. NO "LOW OIL PR ESURE" OR "OIL CLOG" LIGHTS. ALL ENGINE PARAMETERS NORMAL FL 320. TAT -14 DEGREES C, SAT -44 DEGREES C. FOLLOWED QRH, NO LEFT ECAM INDICATIONS. LAX U PER PWR PLANT ENGINEERING AWAITING TRANSMITTER FOM OAK. REMOVED AND REPLACED CB FOR OIL PRESSURE SYSTEM, 14ESAS/PERFORMED SECOND GROUND RUN, PER JRH. SYSTEM OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A35EU E20EA 20080815 EU 2008 8 15 08FDEA02588 1 20080701 A 5315 A53610731208 FLOORBEAM AIRBUS 310 A310222 3930315 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 MAIN DECK CROSSBEAM C14(FR14) -Y1220 TO -Y1300 LOWER FREE FLANGE WITH EXFOLIATION CORROSION. REMOVED THE PULLEY BRACKET PER AMM 20-29-11-0. REMOVED CORROSION PER SRM 51-74-10. APPLIED ALODINE TO THE REWORKED AREA PER SRM 51-21-10. MEASU RED REMAINING THICKNESS IS 0.096 INCH PER NTM51-10-04. IT IS WITHIN THE LIMIT PER SRM 53-12-15-101. APPLIED FLAP PEENI NG INTENSITY=0.15MM.N TO THE REWORKED AREA PER SRM 51-29-00. APPLIED PAINT PER SRM 51-75-10. INSTALLED PULLEY BRACKET PER AMM 20-29-11-0. PERFORMED INSPECTION TO THE REWORKED AREA PER SRM 53-12-15-1-001-00. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA03045 1 20080724 A 5347 A5381314300000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 686FE 804 MAIN DECK LEFT SIDE SEAT TRACK 4 AT FRAME 54 HAS 2 ELONGATED SCALLOPS. REMOVED DAMAGED TRACK FROM FRAMES 54 TO 54.2 AND INSTALLED NEW TRACK IAW A300-600 SRM 51-72-10 AND 51-40-21. RESTORED PROTECTIVE COATING IAW A300-600 SRM 51-75-10. 2 L 7 2 4F RT A35EU 20080815 WP 2008 8 15 08FDEA03009 1 20080722 A 5100 NONE DOUG DC10 DC1030F 3023504 WP NOT AN SDR NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 318FE 46837 FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 08FDEA03010 1 20080722 A 5100 NONE DOUG DC10 DC1030F 3023504 WP NOT AN SDR NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 318FE 46837 FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 08FDEA02764 1 20080708 A 7110 ASL00401 ADAPTER DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 NR 1 ENGINE LEFT CORE COWL LEADING EDGE IS WORN. ADAPTER REMOVED AND REPLACED PER DC/MD-10 SRM 51-31-01. 2 L 7 3 4F RT A22WE 20080815 EU 2008 8 15 08FDEA02844 1 20080712 A 2780 518B000001 JACKSCREW AIRBUS 310 A310324 3930206 EU SLATS STUCK A FDEA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 CE 21 805FD 456 SLATS STUCK AT O DEG, C/W QRH, EMERGENCY DECLARED, LANDED UNEVENTFULLY AT SYR. REMOVED AND REPLACED RIGHT NR 2 JACKSCRE W ASSY PER A310-300MM ATA 27-84-22-4. 2 L 7 2 4F RT A35EU 20080815 NM 2008 8 15 08FDEA02983 1 20080719 A 5720 6521656225 RETAINER BOEING 727 727233 138408A NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 LEFT MLG W/W LOWER FWD WING PANEL HAS CORROSION ON SEAL RETAINER STRIP NEAR LOWER MLG SUPPORT BEAM, WSS 217. REMOVED AN D REPLACED LEFT MLG W/W LOWER FWD WING PANEL SEAL RETAINER AT WSS 217 REF SRM 51-30-2 PG 2 AND DWR 65-21656. THIS IS CL ASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080815 NM 2008 8 15 08FDEA02984 1 20080719 A 5350 65585058 FAIRING BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 RT BODY FAIRING PANEL NR 3349 CRACKED AT EDGE. REMOVED DAMAGED EDGE PLATE. VERIFIED MATERIAL FOR NEW EDGE PLATE, FABRI CATED NEW EDGE PLATE, TREATED AND PRIMED AND INSTALLED. REF DWR 65-58505 AND SRM 51-10- 2 PG1, 51-30-2 PG1. THIS IS C LASSIFIED AS A MINOR REPAIR 2 L 7 3 4F RT A3WE 20080815 NM 2008 8 15 08FDEA02985 1 20080719 A 5420 651950861 BRACKET BOEING 727 727233 138408A NM NR 1 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 NR 1 ENG UPPER COWL, BRACKET CRACKED AT FWD O/B LOWER CORNER REMOVED AND REPLACED CRACKED SEGMENT, PAINTED AFFECTED AREA OF COWLING. REF SRM 51-30-2 PG 2, MM 51-20-151-7 PG1-5. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A3WE 20080815 NM 2008 8 15 08FDEA02720 1 20080706 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM BS 757 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 601FE 48401 MAIN DECK CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND 3RD LAYER CRACK INDICATION AT HOLE A, B, C AND D. MAIN DECK CARGO DOOR LOWER JAMB CRACKED SUPPORT FITTING NR 7 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR BUSHINGS FABRICATED AND INSTALLED AS PER SRM 53-50-00 FIGURE 10, VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 08FDEA02722 1 20080706 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM BS 737 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 601FE 48401 MAIN DECK CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND 3RD LAYER CRACK INDICATION AT HOLE A, B, C AND D. MAIN DECK CARGO DOOR LOWER JAMB CRACKED SUPPORT FITTING NR 6 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR BUSHINGS FABRICATED AND INSTALLED AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080815 EU 2008 8 15 08FDEA03018 1 20080722 A 5755 SKIN AIRBUS 300 A300B4622R 3930312 EU NR 4 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD TS0569 613 FOUND DELAMINATION ON SPOILER NR 4 LT UPPER FLANGE OF FWD END OF HINGE ARM. REPAIR PERFORMED IAW SRM 57-72-11 FIG 205, APPROVED BY RAS/DABRE/7009949/2008 ISS A AND EA 6-5772-123051. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA03039 1 20080724 A 5751 A57661504200 SKIN AIRBUS 310 A310203 3930313 EU LT WING AILERON FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 430FE 394 PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING AILERON LOWER SKIN BETWEEN RIBS 12 TO 16 MEASURES 18.5 X 11.3 IN CHES REPAIR NOT IAW SRM REQUIREMENTS. REMOVED 3 EACH FASTENERS FROM PREVIOUS REPAIR DOULBLER AND INSTALLED 3EACH CORRE CT FASTENERS ON LEFT WING AILERON LOWER SKIN BETWEEN RIBS 12 TO 16 IAW A310-200 SRM 57-61-12 FIG 201. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA02618 1 20080702 A 5753 A5794251200064 ROLLER AIRBUS 310 A310222 3930315 EU RT WING TE FLAP INOPERATIVE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 RT INBD FLAP TRACK NR 2, UPON REMOVAL OF INBD FLAP FOUND 2 FRONT CARRIAGE ROLLER AND 1 REAR CARRIAGE ROLLER SEIZED. D ISASSEMBLED ROLLERS PER CMM 27-51-54, CLEANED AND INSPECTED, FOUND ROLLERS WITH SURFACE CORROSION ON MATING SURFACE. RE MOVED THE ROLLERS PER CMM 27-51-54. CLEANED THE ROLLERS PER CMM 27-51-54. LUBRICATED THE ROLLERS PER AMM 12-22-00-0. INSTALLED THE ROLLERS PER CMM 27-51-54. 2 L 7 2 4F RT A35EU 20080820 NM 2008 8 20 SWAA084257 1 20080731 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 777QC 30592 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, LBL 43 TO RBL 36. REPAIRED UPPER CHORD PER S WA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843230 1 20080629 A 5320 654797632 CUSP WEB BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 827-847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 CUSP WEB CORRODED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR PARTS IAW SRM 51 70 13. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084264 1 20080801 A 3350 8200048901 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 238WN 34713 L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084276 1 20080801 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084281 1 20080803 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084282 1 20080803 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084294 1 20080803 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 448WN 33721 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084311 1 20080803 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843306 1 20080625 A 5753 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 RT IB FORE FLAP LOWER SURFACE DENTED APPROX 2" IB OF THE 2ND TRACK. REMOVED FACTORY DOUBLER PREPPED AREA FABBED REPAIR DOUBLER & BONDED REPAIR IAW SRM 51 70 10 REPAIR 2. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843300 1 20080625 A 5755 654645262A SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU NR 5 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 NR 5 GROUND SPOILER HAS SEVERAL DENTS ON LOWER SURFACE. PREPPED DAMAGED AREA FABRICATED REPAIR DOUBLERS & BOND IAW SRM 51-70-10 PG 251. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084319 1 20080804 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084335 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084344 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084349 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843211 1 20080629 A 5311 FRAME BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU BS 440 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 705AS 29318 FWD CARGO PIT FWD FRAME HAS GOUGE AT BS 440 RBL 28 REPAIRED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0853322 1 20080808 A 2841 100370750 INDICATOR BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE FUEL QTY FAILED A ASAA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 02 570AS 28633 35185 NR 1 REFUELING INDICATOR AT WING PANEL INOP, FLT DECK INDICATIONS NML. COULD NOT DUPLICATE ACCOMP. FQIS BITE NO FAULTS A CCOMP. GRD TEST, TEST PASS REF. FIM 28-41 TASK 801. REMOVED WING REFUEL PANEL. ACCOMP GVI OF WIRES FOR NR 1 TANK IND AND OHMED SAME WIRES NO DISCREPANCIES NOTED. REINSTALLED PANEL. REPLACED NR 1 TANK INDICATOR WITH SERVICABLE ONE. PART VERI FIED BY MC EDD. OPS TEST PASS. REF MM 28-41-61-400-801 & WDM 28-44-11. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 EA 2008 8 20 TRAX200800982 1 20080807 A 5210 INTERCOSTAL CNDAIR CL600 CL6002C10 1390015 EA ASD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 ASD 318 INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL 318 ON PASSENGER DOOR IAW SRM 51-42-06. (S) 2 L 7 2 4F RT A21EA 20080820 NM 2008 8 20 ASAA0843324 1 20080721 A 5730 65454288 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 776AS 25109 EXFOLIATION CORROSION FOUND ON UPPER WING PLANK AT FS 661, RBL 57 REPAIRED IAW EA-5710 01153. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 EA 2008 8 20 SWIA200819859 1 20080709 A 2711 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA AILERON TRIM MALFUNCTIONED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 934SW 7722 AILERON TRIM STICKS AND WILL NOT TRIM TO THE RIGHT. (FLIGHT NR 6052) REPLACED AILERON/RUDDER TRIM CONTROL PANEL IAW AMM 27-12-10. 2 L 7 2 4F RT A21EA 20080820 EA 2008 8 20 SWIA200819860 1 20080715 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 935SW 7725 RT WINDOW SHATTERED ON CLIMBOUT. (FLIGHT NR 6394) REPLACED RT SIDE WINDOW IAW 56-12-01. P/N:NP-139332-6, S/N OFF: 031 40H4504. 2 L 7 2 4F RT A21EA 20080820 NM 2008 8 20 SWAA084561 1 20080817 A 2130 32144464 VALVE BOEING 737 7373Q8 1384670 NM A/C BAY FAULTY A SWAA K NONE J WARNING INDICATION DE DESCENT 1 SW 29 672SW 23406 CABIN ALTITUDE HORN SOUNDED. PLACED PACKS ON HIGH RAN EMERGENCY DESCENT CHECKLIST. R&R HIGH STAGE VALVE PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843186 1 20080629 A 5753 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 RT WING IB FORE FLAP HAS MULTIPLE DENTS ON LOWER SURFACE PREPARED DAMAGED AREA FABRICATED DOUBLER AND BONDED IAW SRM 51- 70-10, REPAIR 2. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843187 1 20080629 A 5753 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 LT WING OB AFT FLAP HAS SEVERAL DENTS ON UPPER SURFACE. PREPARED DAMAGED AREA, FABRICATED REPAIR DOUBLERS AND BONDED IAW SRM 51-70-10, REPAIR 2. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843188 1 20080629 A 5753 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 LT WING OB AFT FLAP HAS SEVERAL DENTS ON LOWER SURFACE PREPARED DAMAGED AREA FABRICATED REPAIR DOUBLERS AND BONDED IAW S RM 51-70-10, REPAIR 2. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843201 1 20080712 A 5753 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 RT WING T/E AFT OB FLAP, 3 EACH DENTS CLOSE TOGETHER 5 TO 2 INCHES FROM T/E AND 21 INCHES FROM IB END. PREPARED DAMAGED AREA FABRICATED REPAIR DOUBLER AND BONDED IAW SRM 51-70-10, REPAIR 2. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 USA2008F00020 1 20080728 A 3397 WIRE BOEING 737 7373G7 1384595 NM COCKPIT BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 306AW 24633 PHX - MAINTENANCE REPORTED THE FLIGHT DECK EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIR E 003-22. OPERATIONAL CHECK GOOD IN ASSOCIATION WITH MM 33-51-11 AND CHAPTER 20. (A) 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 08FDEA02972 1 20080718 A 5320 6061587075T65 FLOOR SUPPORT DOUG MD10 MD1030F 3024020 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 303FE 46802 MCD FLOOR PANEL IS CRACKED AT STA 1891 LBL 59. REMOVED FLOOR PANEL AND FOUND CRACKED FLOOR SUPPORT WITH LOOSE FASTENERS . FABRICATED NEW FLOOR SUPPORT AND NEW FLOOR PANEL, INSTALLED NEW SUPPORT AND PANEL, TIGHTENED FASTENERS IAW MAE TRAVEL ERS T8/747683,T8/750032, SRM 51-31-01, 51-21-01 AND AMM 12-22-01-7. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR, REPORT ABLE DISCREPANCY AND RII. 2 L 7 3 4F RT A22WE 20080820 NM 2008 8 20 ASAA0843191 1 20080702 A 5753 6546430129 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU FOREFLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 LT WING IB FORE FLAP DENT WITH A CREASE ON UPPER SURFACE CENTER AREA, REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND BONDED IAW SRM 51-70-10, REPAIR 4. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843181 1 20080629 A 5755 654645268A SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU NR 4 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 LT WING NR4 SPOILER LOWER SURFACE HAS MULTIPLE DENTS, PREPARED DAMAGED AREA, FABRICATED FILLERS AND REPAIR DOUBLERS AND BONDED IAW SRM 51-70-10, REPAIR 4. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843184 1 20080629 A 5755 654645170A SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 LT WING NR1 SPOILER, 2 EACH DENTS ON LOWER SURFACE, PREPARED DAMAGED AREA FABRICATED DOUBLER AND BONDED IAW SRM 51-70-10 , REPAIR 2. 2 L 7 2 4F 4 F RT A16WE E21EU 20080815 NM 2008 8 15 08FDEA03038 1 20080724 A 5755 SKIN BOEING 727 727233 138408A NM NR 2 SPOILER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 275FE 22040 DELAM SPOTS TOP NR 2 SPOILER REMOVED DAMAGE AREAS, CLEANED AND PREP IAW B727 SRM 51-40-20 PG 12-14,42-47. FABRICATED R EPAIR FILLERS (2) APPROX 7 BY 5, 22 BY 3 AND REPAIR DOUBLERS (2) APPROX 10 BY 6.5 AND 25 BY 4.5 USING .025 7075 T6 IAW B 727 SRM 51-40-20 PG 14-15, 23-24 AND B727 SRM 57-50-2 PG 14 AND 17. HOT BONDED REPAIR REPAIR IAW B727 SRM 51-40-20 PG 5 6-62. 2 L 7 3 4F RT A3WE 20080815 EU 2008 8 15 08FDEA02995 1 20080721 A 5320 A5398939523251 ANGLE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 THE APU COMPARTMENT AFT BULKHEAD HAS A PUNCTURE JUST BELOW THE LEFT LATCH RECEPTICLE. REMOVED PUNCTURED BULKHEAD ANGLE IAW A300-600 SRM 51-40-21. REMOVED THE INTERCOSTAL FOR ACCESS IAW A300-600 SRM 51-40-21. LOCATED, DRILLED AND INSTALL ED A NEW ANGLE P/N A5398939523251 IAW A300-600 SRM 51-72-10 AND SRM 51-41-20. INSTALLED THE INTERCOSTAL IAW A300-600 SR M 51-72-10 AND SRM 51-41-20. 2 L 7 2 4F RT A35EU 20080815 NM 2008 8 15 UPS08M52849 1 20080518 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT HORIZONTAL STABILIZER BARREL NUT BORE NR30 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED I AW SRM 51-21-01 VII REV 35. BORE REAM TO 1.178" DIA REMAINING BLEND OUT 0.040" DEEP, BORE BLEND OUT FOUND EXCEEDING LIM ITS IAW EO MD11-5510-19409M.10X MAGNIFICATION DETAIL VISUAL INSP & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT BORE NR 30 RT WAS ACCOMPLISHED IAW EN 1210-08 & IS ACCEPTABLE IAW EO MD11-5510-30012-A. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08552884 1 20080717 A 5320 FLOOR SUPPORT BOEING 757 75724APF 1384969 NM BS1020-1040 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 421UP 25281 INSPECTION TYPE-C2, CORROSION ON LONGITUDINAL BEAM UPPER CHORD IB FLANGE AT 2EA NUTPLATE HOLES BS1020-1040 LBL23 WL208. REPAIRED LONGITUDINAL BEAM UPPER CHORD IB FLANGE BS1020-1040 LBL23 WL208 IAW ATS ER 08-2401 DATED 25JUL08. 2 L 7 2 4F RT A2NM 20080815 NM 2008 8 15 UPS08552885 1 20080717 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM BS 1057 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 421UP 25281 INSPECTION TYPE-C, CORROSION ON MAIN DECK FLOOR SUPPORT UPPER SURFACE BS1057 BLO-LBL25 WL208. REMOVED & REPLACED FLOOR SUPPORT. 2 L 7 2 4F RT A2NM 20080815 NM 2008 8 15 UPS08552887 1 20080717 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM BS 1080-1100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 421UP 25281 INSPECTION TYPE-C2, CORROSION ON MAIN DECK SEAT TRACK UPPER SURFACE AT NUTPLATE HOLES BS1080-1100 LBL1 WL208. REPLACED CORRODED SEATTRACK IAW SRM53-00-52-1A1. 2 L 7 2 4F RT A2NM 20080815 WP 2008 8 15 UPS08852912 1 20080725 A 3350 LAMP DOUG DC8 DC871F 302199D WP EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 EMERGENCY EXIT LIGHTS ABOVE L-1 DOOR INOPERATIVE. EMERGENCY EXIT LIGHTS RELAMPED IAW AMM 33-50-02-2. 2 L 7 4 4F RT 4A25 20080815 NM 2008 8 15 UPS08B52898 1 20080729 A 3150 WARNING MESSAGE BOEING 747 747400 13848AT NM FALSE ACTIVATION A IPXA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 575UP EICAS MESSAGE EMERGENCY LIGHTS WITH EMERGENCY SWITCH ARMED. RESET PASSENGER CABIN EMERGENCY LIGHT SWITCH. OPS CHECK NOR MAL. 2 L 7 4 4F RT A20WE 20080815 NM 2008 8 15 UPS08M52890 1 20080516 A 5753 HINGE DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, LT WING OB FLAP IB AFT HINGE UPPER MOUNTING FOUND CENTER BORE CORRODED. LT AFT OB FLAP IB HINGE UPP ER MOUNTING CENTER BORE CORROSION REMOVED IAW BSOPM 20-11-02 REV 61 FPI C/O IAW DAC NDT SPM REV 13 PT 08 ON REWORKED ARE A & FOUND NO CRACK & NO CORROSION EVIDENT. LT AFT OB FLAP I B HINGE UPPER MOUNTING CENTER BORE FINAL DIA OF 2.020" EVAL UATED & FOUND ACCEPTED IAW EN1288-08. FLAP PEENING C/O ON RWK AREA IAW EN1288-08. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 UPS08852895 1 20080624 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING DAMAGED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, DRILL START IN LOWER SKIN OF R/W OB, L/E, FWD OF 3RD. PANEL FROM OB END. REMOVED DAMAGE, FAB AND IN STALLED REPAIR DOUBLER IAW SRM 51-1-8, 57-2- 0 FIG.7 51-1-21. 2 L 7 4 4F RT 4A25 20080815 WP 2008 8 15 UPS08852896 1 20080611 A 5347 DC853B00700L SEAT TRACK DOUG DC8 DC871F 302199D WP BS 680 LBL24 WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C2 STA.680 LBL 24 MAIN CABIN SEAT TRACK WORN, CUT OUT DAMAGE. REMOVED AND REPLACED SEAT TRACK SECTION I AW, SRM 51-1-8, 53-2-3, 51-3-0. 2 L 7 4 4F RT 4A25 20080815 NM 2008 8 15 UPS08M52853 1 20080531 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR34 FOUND CORRODED EXISTING SLEEVE BUSHING REMOVED & CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REMAINING BLEND OUT 0.030" DEEP, BOTTOM SURFACE CLEANED, BORE BLEND OUT EXCEEDED LIMIT IAW EO MD11-5510-19409M. 10X MAGN.DVI C/O & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT B ORE NR 34 WAS ACCOMP IAW EN1240-08 & IS ACCEPTABLE IAW EO MD11-5510-30012A. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08552838 1 20080716 A 5322 SHEAR TIE BOEING 757 75724APF 1384969 NM BS 1300 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 421UP 25281 INSPECTION TYPE-2C, AFT CARGO BAY CRACKED SHEAR TIE BS 1300 BETWEEN STR 20L-21L. REMOVED AND REPLACED SHEAR TIE AT BS 1300 BETWEEN STR 20L-21L IAW SRM 51-40-02-0G; SRM 51-30-01, SRM 51-40-05. 2 L 7 2 4F RT A2NM 20080815 NM 2008 8 15 UPS08M52921 1 20080723 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 4 LT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INST ALLED BUSHING IAW EO, MD11-5510-19409-N AND SAA TRAVELER 80538960001. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52928 1 20080712 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 7 LT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INSTA LLED BUSHING IAW EO, MD11-5510-19409-N AND SAA TRAVELER 80538340001. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52931 1 20080713 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 32 LT BARREL NUT BORE HOLE REMOVED CORROSION, FABRICATED BUSHING, AND INST ALLED BUSHING IAW UPS EO, MD11-5510-19409-N AND SAA TRAVLER 80538500001. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52937 1 20080715 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 35 LT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INST ALLED BUSHING IAW UPS EO, MD11-5510-1949-N AND SAA TRAVELER 80538400001. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52842 1 20080524 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, LT HORIZ STAB BARREL NUT BORE NR17 FOUND CORRODED. CORROSION AT BARREL BORE REMOVED IAW SRM 51-21 -01 VII REV 35. BORE REAM TO 1.067" DIA REMAINING BLEND OUT 0.035", BOTTOM SURFACE CLEANED & BORE FOUND OUT OF LIMIT IAW EO MD11-5510-19409M.10X MANIFICATION DVI C/O & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT BORE NR17 LT WAS ACC OMPLISHED IAW EN 1223-08 & IS ACCEPTABLE IAW EO MD11-5510-29971-A. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 UPS08852793 1 20080703 A 5320 FLOOR SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, FLIGHT COMP SUB-FLOOR ARERA AT STA.- 99.0, RBL27 HAS AN ANGLE SUPPORT CORRODED AND RIVET MISSING. REMOVED AND REPLACED ANGLE SUPPORT IAW SRM, 51-1-8, 51-1-21, 51-1-24 2 L 7 4 4F RT 4A25 20080815 EU 2008 8 15 UPS08152905 1 20080722 A 5321 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU CABIN GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 153UP 0839 INSPECTION TYPE-5 YR, MAIN CABIN FLOOR PANEL NR Z251BN HAS SEVERAL GOUGES. REPAIRED MAIN CABIN FLOORBOARD NR Z251BN REF. A-300-600 SRM 53-10-20 TABLE 201 PARA. 8A. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 UPS08152906 1 20080722 A 5321 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CABIN GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 153UP 0839 INSPECTION TYPE-5 YR, MAIN CABIN FLOOR PANEL NR Z251XJ HAS SEVERAL GOUGES. REPAIRED CABIN FLOOR PANEL NR Z251XJ REF. A-300-600 SRM 53-10-20 TABLE 2 01 PARA. 8A. 2 L 7 2 4F RT A35EU 20080815 NM 2008 8 15 UPS08B52754 1 20080626 A 5755 GUSSET BOEING 747 747400 13848AT NM NR 4 SPOILER GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 572UP INSPECTION TYPE-C2, R/W REAR SPAR AT IB HINGE OF NR4 SPOILER PARTITION RIB ATTACH BRACKET GOUGED AND BENT. REMOVED AND REPLACED GUSSET ON SPOILER PARTITION IAW SRM 51-1-8, 51-1- 21. 2 L 7 4 4F RT A20WE 20080815 NM 2008 8 15 UPS08552839 1 20080717 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 421UP 25281 INSPECTION TYPE-2C, CAPT'S SEAT TRACKS SHOW SIGNS OF CORROSION AT FASTENERS. REMOVED AND REPLACED FWD IB AND OB AND AFT OB TRACKS WITH NEW IAW OHM 20-50-01. 2 L 7 2 4F RT A2NM 20080815 NM 2008 8 15 UPS08M52843 1 20080515 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 09 FOUND CORRODED EXISTING REPAIR SLEEVE BUSHING REMOVED IAW EO MD11-5510-19409M. BARREL NUT BORE SURFACE CLEANED & MEASURED 1.065" DIA,BOTTOM SURFACE CLEANED & MINIMUM THK MEASURED 0 .122" THICK, BORE SIZE FOUND OUT OF LIMIT IAW EO MD11-5510-19409M. REPAIRED BARREL NUT BORE NR 09 RT WAS ACCOMPLISHED I AW E N 1185-08 & IS ACCEPTABLE IAW EO MD11-5510-30010-A. 2 L 7 3 4F RT A22WE 20080814 WP 2008 8 14 UPS08852685 1 20080708 A 5210 STRUCTURE DOUG DC8 DC873F 302199F WP PWA JT3D JT3D3 52039 NE PAX DOOR DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 DENT IN MAIN ENTRY DOOR AROUND AFT FRAME. 2 L 7 4 4F 4 F RT 4A25 1E8 20080814 WP 2008 8 14 IXX2008F00031 1 20080609 A 5754 SKIN DOUG DC8 DC872F 302199E WP SLOT VANE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND ELONGATED HOLES ON RT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095. 000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING, FABRICATED NEW SKIN. CLEANED, TREATED AN D PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XILD 7095.000 - XS 247.000 IAW DC8 SRM 57-3-2 FIGURE 10 PAGE 22 ITEM F, DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-3-0 AN D SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 UPS08852791 1 20080630 A 5313 STRINGER DOUG DC8 DC871F 302199D WP BS 1766-1772 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, L 17R CRACKED UNDER END FITTING , STA. 1766-1772, 60 COMPT. REMOVED AND INSTALLED NEW END FITTING I AW SRM, 51-1-8, 51-3-0, 53-5-1 FIG.F. 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 UPS08852792 1 20080702 A 5711 SPAR DOUG DC8 DC871F 302199D WP RT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, RT WING FRONT SPAR T CAP HAS DOUBLE DRILLED HOLE XFS 92.5. CLEANED HOLE AND INSTALLED BUSHING IAW SRM, EO DC8-5710-29984-A, 51-1- 8, 51-1-24. 2 L 7 4 4F RT 4A25 20080814 NM 2008 8 14 UPS08652673 1 20080707 A 3350 SIGN BOEING 767 76734AF 1385212 NM CABIN UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 EMERGENCY LIGHT ASSY REMOVED FROM CREW ENTRY DOOR HANDLE PANEL. REINSTALLED EMERGENCY EXIT SIGN AND OPS CHECK NORMAL . 2 L 7 2 4F RT A1NM 20080814 NM 2008 8 14 USA2008F00014 1 20080723 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 438US 24560 CLT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT OVER THE AFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLAC ED THE BATTERY CHARGER ASSEMBLY IN THE AFT GALLEY. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A16WE 20080814 NM 2008 8 14 USAA920081433 1 20080725 A 5315 D53472193200 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803AW 0931 SAL - C7 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT FR67 TO FR70, -Y765. REPLACED FLOORBEAM AT FR67 TO FR70, -Y765 IAW SRM A319 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 USAA920081428 1 20080708 A 5752 654645522C TAB BOEING 737 737401 1384701 NM RT AILERON DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT - Q3 - MAJOR REPAIR - RT AILERON TAB DELAMINATED. REPLACED RT AILERON TAB IAW US AIRWAYS JOB CARD 03C40627010. (S ) 2 L 7 2 4F RT A16WE 20080814 WP 2008 8 14 IXX2008F00039 1 20080612 A 5730 SKIN DOUG DC8 DC872F 302199E WP RT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND RT WING LEADING EDGE LOWER SKIN CORRODED AT STATION XW 736.000-761.000. REMOVE D CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND R EPAIR PART. INSTALLED REPAIR PARTS IAW DC8 SRM 57-3-2 FIGURE 8 PAGE 19 ITEM "A", DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 57 -2-0 FIGURE 7, DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-1-20D, AND 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080814 WP 2008 8 14 IXX2008F00053 1 20080612 A 5320 FITTING DOUG DC8 DC872F 302199E WP A/C BAY CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND ACND COMPARTMENT CLIP CORRODED AT STATION 235.000 LONGERON 31 LEFT. REMOVED CO RROSION. FOUND OUT OF LIMITS. REMOVED CORRODED CLIP. FABRICATED NEW CLIP. CLEANED, TREATED AND PRIMED CLIP. INSTALL ED CLIP IAW DC8 SRM 51-1-20D, SRM 51-3-1, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 51-1-20D, DC8 SRM 53-2-0, DC8 SRM 51-1-8B. (S) 2 L 7 4 4F RT 4A25 20080814 NM 2008 8 14 08FDEA03060 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL TANK ACCESS CUTOUT 642BB HAS CORROSION. REPAIR CARRIED OUT IAW B757-200 SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS C LASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080814 CE 2008 8 14 DXTA200803212 1 20080802 A 2750 FLAP CESSNA 750 750 2076810 CE WING FAILED E DXTA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 07 952QS 7500200 FLAPS FAIL ON ENG START. (S) 2 L 7 2 4J RT T00007WI 20080814 2008 8 14 C772008F00000 4 20080804 A 2565 SLIDE EMB ERJ170 ERJ170200LR 3260121 NM R1 DOOR UNWANTED DEPLOY A C77A K NONE O OTHER TX TAXI/GRND HDL 1 EA 27 614CZ 17000205 F/A INADVERTENTLY DEPLOYED DOOR R1 SLIDE WHILE ATTEMPTING TO ARM BEFORE TAXI. ACFT IS BEING DELAYED AND A NEW EMERGENCY EVACUATION SLIDE IS BEING INSTALLED PER THE AMM. (S) 2 L 7 2 4F RT A56NM 20080814 SO 2008 8 14 C2X2008F00016 1 20080801 A 5610 SEAL EMB 145 EMB145XR 3260214 SO COCKPIT WINDOW OUT OF POSITION A C2XA K NONE O OTHER CR CRUISE 1 SW 27 16151 14024 14024 145758 ACFT WAS EN ROUTE TO EWR FROM LIT WHEN THE DV WINDOW SEAL STARTED SQUALLING. CREW DIVERTED THE FLIGHT TO TYS WHERE MAIN TENANCE REPOSITIONED THE DV WINDOW SEAL ON THE CAPTAIN’S SIDE. LEAK CHECK GOOD AND SIGNED OFF TO SERVICE. (S) 2 L 7 2 4F RT 20080814 EA 2008 8 14 COMA086337 1 20080731 A 2621 365000183 FIRE BOTTLE CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 971CA 22011 7145 FLIGHT 5308 CARGO LOW BOTTLE MESSAGE CAME ON. PERFORMED QRH, RETURNED TO CMH. LANDED WITHOUT INCIDENT. REPLACED FIRE BOTTLE. NO FURTHER DEFECTS. (S) 2 L 7 2 4F RT A21EA 20080814 2008 8 14 USAA920081468 4 20080702 A 2565 WIRE HARNESS AIRBUS A319 A319112 3930323 EU L1 DOOR MISROUTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 710UW 1019 PIT-DROP-IN-EEL - L-1 DOOR SLIDE EMERGENCY WIRE HARNESS IMPROPERLY ROUTED. CORRECTED WIRE HARNESS ROUTING. (S) 2 L 7 2 4F RT A28NM 20080814 NM 2008 8 14 USAA920081450 1 20080730 A 5330 6545776 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 445US 24863 CLT - RON/LAP INSP - MAJOR REPAIR - FUSELAGE SKIN CRACKED AT BS 727F +18 AND 727G, S25L. REPAIRED IAW US AIRWAY EA10058 4. (S) 2 L 7 2 4F RT A16WE 20080815 EU 2008 8 15 08FDEA02968 1 20080718 A 5100 NONE AIRBUS 300 A300B4622R 3930312 EU NOT AN SDR NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 743FD 630 FOUND AT SLAT NR 1 RIB 2A, PLUGGED HOLES, MOST LIKELY FROM PRODUCTION OF SLAT. REPAIR PERFORMED BY LEAVE IT AS IT IS AN D TOPCOAT THE AREA IAW RAS/FOK/149/2008 ISS A, APPROVED BY EA 6-5742-120081. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA02969 1 20080718 A 5320 A53771417206 SILL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON SILL BEAM, FWD CARGO COMPARTMENT, C25A. REPAIR PERFORMED BY CUT OUT THE UPPER FLANGE AND INSTALLING REPAIR ANGLE IAW RAS/EFW/9000051/2008 ISS A, APPROVED BY EA 6-5313-123031. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA02979 1 20080616 A 5753 A57942174208 FITTING AIRBUS 300 A300B4622R 3930312 EU FLAP TRACK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 721FD 477 LT WING NR 3 TRACK FRONT CARRIAGE INTERIOR FITTING WITH CORROSION, DETECTED WHILE PERFORMING N0800. THE NR 3 TRACK FRON T CARRIAGE WAS REPLACED BY ONE FABRICATED AS PER FEDEX EA 6-5740-120510. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA02492 1 20080626 A 5100 NONE AIRBUS 310 A310222 3930315 EU NOT AN SDR NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 456FE 318 NR 2 PYLON REPAIR INSTALLED ON PRECOOLER WEB DOES NOT MEET REQUIREMENTS PER SRM. REMOVED THE ORIGINAL REPAIR PART PER S RM 51-40-21. DRILLED CRACK STOP HOLES (4.8MM) PER SRM 54-52-31. FABRICATED REPAIR PART PER SRM 54-52-31. DRILLED FAST ENER HOLES TO THE REPAIR PART PER SRM 54-52-31. INSTALLED THE REPAIR PART PER SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080815 WP 2008 8 15 08FDEA02830 1 20080711 A 3340 HOUSING DOUG MD10 MD1010F 3022112 WP LT WING STROBE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 383FE 46616 LEFT WING TIP T/E LIGHT ASSY HOUSING IS CHAFED AND THE LENS ATTACH HOLES ARE ELONGATED. REMOVED LEFT T/E HIGH INTENSITY LIGHT IAW MD 10 AMM 33-47-00-4. REMOVED AND REPLACED THE STROBE BRACKET AND STROBE IAW DC/MD 10 SRM 51-35-01, VOL II. REINSTALLED LEFT T/E HIGH INTENSITY LIGHTS IAW MD-10 AMM 33-47-00-4. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 08FDEA03026 1 20080723 A 5100 NONE DOUG DC10 DC1030F 3023504 WP NOT AN SDR NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 318FE 46837 MAIN CABIN EXISTING ANGLE REPAIR ON TEE FLOOR SUPPORT. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 08FDEA03008 1 20080721 A 5314 149N713094 KEELBEAM BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 LOWER FUSELAGE KEEL BEAM AREA, SURFACE CORROSION ON CENTER SUPPORT FRAME AT BS 900. CORROSION FOUND EXCEED ALLOWABLE DA MAGE LIMITS IN B757-200 SRM 53-00-71. CHORD REMOVED AND REPLACED IAW B757-200 SRM 51-40-02 REV 93. REPAIR IS CLASSIFIE D AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080815 WP 2008 8 15 08FDEA03012 1 20080722 A 5100 NONE DOUG DC10 DC1030F 3023504 WP NOT AN SDR NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 318FE 46837 FWD CARGO COMPARTMENT EXISTING REPAIR ON STANCHION. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 08FDEA02994 1 20080721 A 5320 69471112 INTERCOSTAL BOEING 727 727233 138408A NM BS 740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 273FE 22038 DELTA BEAM AT STA 740 HAS CORROSION AROUND AND UNDER HEADS OF SEVERAL FASTENERS. CAN BE SEEN THRU ACCESS HOLE BELOW B EAM. REMOVED CORROSION. ORIGINAL "T" .107 LOSS AT LOWEST POINT IS .028 REMAINING "T" IS .079. OUT OF LIMITS REF SRM 5 3-10-1 FIG 101 DETAIL I. REMOVED FWD DELTA BOX INTERCOSTAL REF 51-30-2 PG 1-6 MANUFACTURED NEW INTERCOSTAL P/N 69-47111 -2 REF DWG 69-47111. TREATED AND PRIMED REF SRM 51-10-2 PG 7. INSTALLED REF SRM 51-30-2 PG 1-6. 2 L 7 3 4F RT A3WE 20080815 NM 2008 8 15 UPS08M52850 1 20080530 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 28 FOUND CORRODED, CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51 -21-01 VII REV35. BORE REAMED TO 1.178" DIA, REMAINING BLEND OUT 0.060", BOTTOM REMAINING 0.070" DEEP. BORE BLEND OUT FOUND EXCEEDING LIMITS IAW EO MD11-5510-19409M. 10X MAGNIFICATION DVI C/O & FOUND NO CORROSION EVIDENT. REPAIR BARREL NUT BORE NR 28 RT WAS ACCOMP IAW EN 1239-08 & IS ACCEPT IAW EO MD11-5510-30012-A. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52851 1 20080602 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, LT HORIZ STAB BARREL NUT BORE NR 22 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51 -21-01 VII REV 35. BORE REAM TO 1.067" DIA, REMAINING BLEND OUT 0.015" DEEP, BOTTOM SURFACE CLEANED, BLEND OUT AT SIDEWA LL FOUND OUT OF LIMITS IAW EO MD11-5510-19409M. 10 X MAGNIFICATION DVI C/O & FOUND NO CORROSION EVIDENT. REPAIR BARREL NUT BORE WAS ACCOMP IAW EN1248-08 & IS ACCEPTABLE IAW EO MD11-5510-29971A. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 UPS08852736 1 20080711 A 5310 FRAME DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 PITS 32 AND 34 CARGO DOOR INNER CRACKS. ISSUED DEFERRAL D380080 IAW EO DC8-5230-29933-A. DAMAGE CONSISTS OF 2.0" LONG CRACK LOCATED ON THE INSIDE RADIUS OF FRAME. VERIFIED ENDS OF CRACK IAW NDT MANUAL 06-10-01 MARKED ENDS. MEASURED CRAC K TO BE 2.0" LONG. STOP DRILLED CRACKS IAW EO DC8-5230-29933 STEP 6 (A) 4. AFTER STOP DRILL HFEC PERFORMED, NO CRACKS F OUND. DEFERRAL WAS FOR REPEAT INSPECTIONS. 2 L 7 4 4F RT 4A25 20080815 NM 2008 8 15 UPS08M52918 1 20080713 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP INSPECTION TYPE-1C, CORROSIOIN FOUND IN NR 14 LT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED BUSHING, AND I NSTALLED BUSHING IAW EO MD11-5510-19409-N AND SAA TRAVELER 80538470001. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52938 1 20080715 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE:1C CORROSION FOUND IN NR 2 LT BARREL NUT BORE HOLE REMOVED CORROSION, FABRICATED BUSHING, AND INSTAL LED BUSHING IAW EO, MD11-5510-19409-N AND SAA TRAVLER 80538410001. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52857 1 20080518 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, LT HORIZ STAB BARREL NUT BORE NR30 FOUND CORRODED. EXISTING REPAIR BUCKET BUSHING REMOVED IAW EO MD11-5510-19409M. MINOR CORROSION AT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BOTTOM WAS BORED THRU & BORE MEASURED TO 1.255"DIA, REMAINING BLEND OUT 0.040", FOUND BORE EXCEEDED LIMITS IAW EO MD11-5510-19409M. REPAIRED BARREL NUT BORE NR30 LT WAS ACCOMP IAW EN 1202-08 & IS ACCEPTABLE IAW EO MD11-5510-29972A. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52848 1 20080523 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 36 FOUND CORRODED CORROSION AT BORE NR36 RT REMOVED IAW SRM 51- 21-01 VII REV 35. BORE REAM TO 2.538" DIA, REMAINING BLEND OUT 0.098" DEEP, BOTTOM REMAINING BLEND OUT 0.150" DEEP, BOR E EXCEEDED LIMITS IAW EO MD11-5510-19409M.10X MAGNIFICATION DVI C/O & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT B ORE NR 36 RT WAS ACCOMP IAW EN1221-08 & IS ACCEPTABLE IAW EO MD11-5510-30009-A. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08552877 1 20080708 A 5320 FLOOR SUPPORT BOEING 757 75724APF 1384969 NM BS 1045-1065 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 457UP 25478 INSPECTION TYPE-C2, CORROSION ON STUB BEAM UPPER CHORD IB & OB FLANGES, BS1045-1065 LBL25, WL208. CORROSION OUT OF LIMI TS, REMOVED, FABRICATED, & REPLACED STUB BEAM. 2 L 7 2 4F RT A2NM 20080818 NM 2008 8 18 UPS08M52861 1 20080603 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 35 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 VII REV 35. BORE REAM TO 1.178"DIA, REMAINING BLEND OUT 0.095" DEEP, BOTTOM REMAINING BLEND OUT 0.068"DEEP, FOU ND EXCEEDING LIMITS IAW EO MD11-5510-19409M.10X MAGN DVI C/O & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT BORE NR 35 RT WAS ACCOMPLISHED IAW EN1254-08 & IS ACCEPTABLE IAW EO MD11-5510-30012A. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 UPS08552840 1 20080717 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 421UP 25281 INSPECTION TYPE-2C, FO'S SEAT TRACK SHOWS SIGNS OF CORROSION AT FASTENERS. REMOVED AND REPLACED SEAT TRACK OB AFT AND I B, OB FWD POSITIONS IAW OHM 20-50-01. 2 L 7 2 4F RT A2NM 20080818 EU 2008 8 18 UPS08152761 1 20080630 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING TE FLAP CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 139UP 0822 INSPECTION TYPE-1C, LT WING CENTER FLAP UPPER SKIN 6 EA. RIVETS CHAFFED BETWEEN NR3 AND NR 4 SPOILERS. REPAIRED LT. WI NG CENTER FLAP UPPER SKIN BETWEEN NR3 AND NR4 SPOILERS IAW SRM 57-50-00 FIG. 205. 2 L 7 2 4F RT A35EU 20080818 WP 2008 8 18 UPS08852737 1 20080629 A 5511 RIB DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE HORIZONTAL STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, AFT END OF RIB CRACKED IN RT HORIZ STAB L/E STA. XFS 47.5. STOP DRILLED CRACK, FABRICATED AND IN STALLED REPAIR DOUBLERS IAW SRM 5 1-3-02, 55-02-00 FIG 2. 2 L 7 4 4F 4 F RT 4A25 E2GL 20080818 NM 2008 8 18 UPS08652724 1 20080702 A 5320 140T130U38 ANGLE BOEING 767 76734AF 1385212 NM BS 1085 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 301UP 27239 INSPECTION TYPE-C, AFT CARGO COMPT BS 1085 RBL 26 UNDER FLOOR CHORD ANGLE CRACK. CRACK LENGTH .7500", AFT CARGO COMPT STA1085 RBL26 UNDER FLOOR CHORD ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20080818 WP 2008 8 18 UPS08852728 1 20080628 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 260 BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, BROKEN SEAT TRACK LUG ON MAIN CARGO FLOOR STA 260 BL 0. CUT OUT DAMAGE IAW 53-02-03 FIG 006D INST ALLED 2EA PLUGS AND 2EA CHANN ELS IAW 51-03-00. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852900 1 20080724 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, COURIER AREA FLOOR PANEL F27 SPONGEY FABRICATED NEW FLOOR PANEL IAW, SRM,. 53-2-1, 51-1-8, 53-21-1, 51-1-21. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852901 1 20080626 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 55 RBL 38 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, A/C COMPT. BS 55, RBL 38, FLOORBEAM HAS EXFOLIATION CORROSION. REMOVED CORROSION, FABBED AND INSTA LLED REPAIR IAW, SRM, 51-1-8, 51-2- 00, 51-1-21A, 51-3-0. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852902 1 20080630 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, EXTERIOR FUSELAGE HOLD OPEN RECEPTACLE FOR L1 DOOR HAS CRACKED REPAIR DOUBLER. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM, 51-1-8, 51-1-5, 51-3-0. 2 L 7 4 4F RT 4A25 20080818 NM 2008 8 18 UPS08M52640 1 20080616 A 5753 FITTING DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 271UP 48572 INSPECTION TYPE-C, LT WING OB FLAP STOP BOLT FITTING (SECOND RIB FROM IB) SUSPECT CRACK AS MARKED. HFEC INSP CARRIED OU T IAW NDT SPM R.13 PART 06.10.01.001 ON STOP BOLT FOUND CRACKED AS MARKED. CRACKED STOP BOLT FITTING & ATTACHED PARTS RE MOVED IAW SRM 51-31-01V.2 & SRM 51-33-01V.2R.40. NEW STOP BOLT FITTING HOLES PICKED UP IAW SRM 51-31-01&51-33-01V.2R.40 . NEW STOP BOLT FITTING PROTECTED IAW SRM 51-21-01V.2R.40. OK TO INSTALL NEW STOP BOLT FITTING. 2 L 7 3 4F RT A22WE 20080818 EU 2008 8 18 UPS08152683 1 20080709 A 2910 HYDRAULIC SYSTEM AIRBUS 300 A300B4622R 3930312 EU FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 157UP 0846 LOSS OF GREEN HYDRAULIC SYSTEM. 2 L 7 2 4F RT A35EU 20080818 NM 2008 8 18 UPS08652866 1 20080716 A 5414 SKIN BOEING 767 76734AF 1385212 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 303UP 27241 NR 2 PYLON LT MOST FWD PYLON STRUT ACCESS CUTOUT CRACKED AT AFT UPPER CORNER (CRACK LENGTH 1" APPROX). NR2 PYLON LT MO ST FWD PYLON STRUT ACCESS CUTOUT AFT UPPER CORNER SKIN REPAIRED IAW HX RS NR R54-51-36029 AND UPS EO NR B767-5430- 30063 -A. 2 L 7 2 4F RT A1NM 20080818 WP 2008 8 18 UPS08852619 1 20080611 A 5321 FLOORBOARD DOUG DC8 DC871F 302199D WP FS 270 LBL 31 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, MAIN CABIN, CORROSION ON FLOORBOARD, STA. 270 LBL31 REMOVED CORROSION, FABRICATED REPAIR DOUBLER , 2EA ANGLES AND INSTALLED IAW SRM 53-02-00 FIG 1F,53-02-03 FIG 10,53-02-03 FIG 10 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852628 1 20080702 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP EMERGENCY LIGHT FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 806UP 46006 ON PRE-DEPARTURE CK, EMERGENCY EXIT LIGHT CK FAILED. FOUND SW IN ON POSITION. REPLACED AND TESTED BATTERY PACK IAW 33- 50-01-2 CKS OK. 2 L 7 4 4F RT 4A25 20080818 NM 2008 8 18 UPS08M52613 1 20080324 A 5330 SKIN DOUG MD11 MD11 3023602 NM PWA 4460 PW4460 NE FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE-C, CENTER CARGO DOOR CUTOUT, FOUND PREVIOUS REPAIR DOUBLER AT LOWER AFT EDGE CRACKED AND WITH NON STANDA RD FASTENERS AS MARKED. CENTER CARGO DOOR CUTOUT-LOWER AFT SIDE HEATING TUBE REMOVED. PREVIOUS REPAIR DOUBLER REMOVED. SKIN TRIMMED & PROTECTED. HFEC INSP C/O ON TRIMMED OFF AREA & FOUND NO CRACK EVIDENT. 3EA REPAIR DOUBLERS & 3EA FILLERS FAB, WITH HOLES PICKED-UP, PROTECTED & PAINTED. 3EA REPAIR DOUBLERS & 3 EA FILLERS INSTALLED. HEATING TUBE RE-INSTALLED. 2 L 7 3 4F 4 F RT A22WE E24NE 20080818 NM 2008 8 18 UPS08M52620 1 20080702 A 3397 SWITCH DOUG MD11 MD11F 3023600 NM GE CF6 CF680 30025 NE EXTERINAL LIGHTS SPARKS A IPXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 252UP 48768 SPARKS/SMOKE FROM WING & RUNWAY TURNOFF LIGHT SWITCHES. OPEN 2 L 7 3 4F 4 F RT A22WE E13NE 20080818 WP 2008 8 18 UPS08852638 1 20080612 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, F/E SEAT TRACKS BOTH FWD & AFT HOLES ARE ELONGATED. REMOVED AND REPLACED F/E SEAT TRACKS IAW SRM 5 1-03-01. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852639 1 20080611 A 5320 CHANNEL DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, U CHANNEL CRACKED BOTTOM OF COCKPIT FLOOR PANEL NR 678. FABRICATED AND INSTALLED U CHANNEL IAW DWG 2755898, SRM 51-3-2, AND 51 -1-21. 2 L 7 4 4F RT 4A25 20080818 NM 2008 8 18 UPS08M52631 1 20080326 A 5753 BUSHING DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE-C, LT WING IB FLAP OB HINGE PIVOT POINT IB LUG BUSHING FOUND CORRODED. CORROSION REMOVED EXCEED LIMIT CMM 57-52-03 PG 442-444 R60 ORIG DIA 1.188, FINAL 1.257 MAX ALLOWABLE 1.220. FPI C/O DACNDTSPMR13PT8 NO CORR EVIDENT. RW K AREA PORTECTED, PAINTED & STEP BUSHING FABRICATED IAW EN1179-08. HEAT TREAT D PS5.00-2 HRC41.7 IAW DPS1.05-5. MPI C/ O NDT SPM R13PT07 NO CRACK EVIDENT. BUSHING CAD PLATED & INSTALLED IAW EN1179-08. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 UPS08652951 1 20080731 A 2780 PSEU BOEING 767 76734AF 1385212 NM LE FLAP FAULTED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 306UP 27759 2ND ATB - LE FLAP ASSYMETRY. REF FIM 27-81-00 FIG 107 PSEU FAULTED S280. INSPECTED TARGET AND AFFECTED SLAT. NO DAMAGE FOUND. CLEARANCE WITHIN LIMITS AT .111 INCH. TESTED INDUCTANCE IAW FIM 32-09-03 FIG 108. FOUND S280 OUT OF LIMITS READIN G 5.8 MILLIHENRYS. REPLACED S280 IAW MM 27-88-01-2. PSEU BITE NORMAL IAW FRIM 32-09-03. 2 L 7 2 4F RT A1NM 20080818 NM 2008 8 18 UPS08M52939 1 20080724 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 36 LT BARREL NUT BORE HOLE AND BOTTOM SURFACE RADIUS. REMOVED CORROSION, FABRI CATED BUSHING, INSTALLED BUSHING IAW UPS EO MD11-5510-19409-N AND SAA TRAVELER 80538810001. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 08FDEA03044 1 20080724 A 5330 2024T3507180 SKIN DOUG MD10 MD1030F 3024020 NM ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 303FE 46802 FUSELAGE SKIN CHAFED BELOW UPPER CARGO DOOR. BLENDED 22 AREAS AND CHECKED LIMITS FOUND TO BE SERV IAW SRM 53-00-01. CH ECKED 7 AREAS FOUND OUT OF LIMITS. FABRICATED DOUBLERS AND FILLERS, TREATED AND PRIMED AND INSTALLED PARTS ALL IAW SRM 53-50-00. REPAIR IS CLASSIFIED AS A MAJOR REPAIR, IS RDR, IS SDR AND IS RII. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 UPS08552878 1 20080706 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM BS 1056 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 457UP 25478 INSPECTION TYPE-C2, CORROSION ON FLOORBEAM BL 0 TO LBL 25, BS 1056, WL 208. FOUND DAMAGE TO BE OUT OF LIMITS, REMOVED D AMAGED PART, FABRICATED NEW FLOORBEAM & INSTALLED. 2 L 7 2 4F RT A2NM 20080818 NM 2008 8 18 UPS08552974 1 20080706 A 5347 CARGO TRACK BOEING 757 75724APF 1384969 NM BS 1195 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 457UP 25478 INSPECTION TYPE-C2, CORROSION ON MAIN DECK CARGO TRACK BL 0, BS 1195, WL 208, CORROSION OUT OF LIMITS, REMOVED AND REPL ACED SEAT TRACK. 2 L 7 2 4F RT A2NM 20080818 NM 2008 8 18 UPS08M52964 1 20080719 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE:1C, FOUND CORROSION IN NR 19 LT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED RE PAIR BUSHING IAW EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 UPS08M52966 1 20080721 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE:1C, FOUND CORROSION IN NR 28 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED RE PAIR BUSHING IAW EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 SWAA084027 1 20080719 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 485WN 32473 EMERGENCY LIGHT LENS LOOSE AT ROW 2 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084034 1 20080721 A 5315 6546811 FLOORBEAM BOEING 737 7375H4 138449D NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM UPPER TEE CAP CORRODED AT BS 986, RBL 32. R&R TEE CASP PER SRM. 2 L 7 2 4F RT A16WE 20080818 2008 8 18 SWAA084036 4 20080717 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084037 1 20080717 A 5520 REP4HE8 BEARING BOEING 737 7373H4 1384600 NM RT ELEVATOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED BRDG CHECK, RT ELEVATOR FAILED FREE PLAY CHECK. R&R HORN BEARING PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084040 1 20080717 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 2390 27713 DURING SCHEDULED HC1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. R&R FLAP PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084041 1 20080717 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 20621540 27713 DURING SCHEDULED HC1 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. R&R FLAP PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084043 1 20080721 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 727A S2L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED A TBS 727A, STR 2L. R&R STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080814 EA 2008 8 14 TRAX200800952 1 20080729 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 936EV 8038 AFT ASD ANCHOR FITTING HAS CORROSION DAMAGE ON SERRATED SIDE. REMOVED AND REPLACED ANCHOR FITTING SERRATED PLATE IAW SB 601R-52-093. (S) 2 L 7 2 4F RT A21EA 20080814 EU 2008 8 14 YENA2008072 1 20080803 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN FAILED A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 547JB 24867 8775 1849 EMERGENCY LIGHTS FAILED WEEKLY CHECK. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AT POSITION 10WL, BITE CHECK GO OD AMM 33-51-38. (S) 2 L 7 2 4F RT A28NM 20080814 EA 2008 8 14 VNAA0807017 1 20080725 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE WING MALFUNCTIONED A VNAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 GL 05 250PS 7929 CREW REPORTED THE FLAPS FAILED AT 20 DEGREES. CREW ELECTED TO DIVERT TO RDU AND LANDED WITHOUT INCIDENT. MAINTENANCE I NSPECTED ACFT AND FOUND NO DEFECTS. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080814 NM 2008 8 14 USAA920081473 1 20080803 A 5512 65C27494 SKIN BOEING 737 7374B7 1384702 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 455UW 24997 CLT -MAJOR REPAIR- CRACK ON UNDERSIDE OF RT HORIZONTAL STABILIZER AT STA82.07 1.75 INCHES FWD OF REAR SPAR. REPAIRED UN DERSIDE OF RT HORIZONTAL STABILIZER AT STA 82.07 1.75 INCHES FWD OF REAR SPAR IAW TYPICAL REPAIR NR 55-10-07, REV C. (K ) 2 L 7 2 4F RT A16WE 20080814 NM 2008 8 14 USAA920081479 1 20080714 A 5320 654585569 SILL BOEING 737 73733A 1384673 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 168AW 23629 MCN-C21 -MAJOR REPAIR- CORROSION ON DOOR SILL WEB LOWER SURFACE AT BS 991, WL 208.1, BL 48.5R. REPLACED DOOR SILL WEB L OWER SURFACE AT BS 991, WL 208.1, BL 48.5R IAW B737 SRM 53-60-15-1A1. (S) 2 L 7 2 4F RT A16WE 20080814 NM 2008 8 14 USAABB08126 1 20080802 A 2560 MEGAPHONE BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 915AW 22209 PHX - THE AFT MEGAPHONE WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE AFT MEGAPHONE. (S) 2 L 7 2 4F RT A2NM 20080814 NM 2008 8 14 USAA920081481 1 20080726 A 5347 D53472090004 SEAT TRACK AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803AW 0931 SAL-C7 -MAJOR REPAIR- CORROSION ON RAIL SEAT LOCATION AT FR66 AND Y1292. REPLACED RAIL SEAT LOCATION AT FR66 AND Y1292 IAW A319 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080815 NM 2008 8 15 08FDEA02723 1 20080706 A 5320 ACA72251 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 601FE 48401 MAIN DECK CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND 2ND LAYER BEAM WITH CRACK INDICATION AT HOLE B. REPAIR CARRI ED OUT AS PER FEDEX EA NR 1-5310-122531, TITLE: FUSELAGE MAIN CARGO DOOR LOWER JAMB BORE HOLES AT APPROXIMATE STA = 737 AND 757, REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080815 EU 2008 8 15 08FDEA02992 1 20080721 A 5751 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 742FD FH1370 613 FOUND TWO OLD PATCH REPAIRS ON RT AILERON LOWER SKIN TRAILING EDGE AREA RIB 10-12 AND 4-10 WITHOUT OLD DOCUMENTATION. THE TWO REPAIRS RENEWED IAW RAS/FOK/138/2008 ISS A, APPROVED BY EA 6-5761-120106 . 2 L 7 2 4F RT A35EU 20080815 NM 2008 8 15 UPS08552886 1 20080717 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM BS 1040-1080 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 421UP 25281 INSPECTION TYPE-C, CORROSION ON MAIN DECK SEAT TRACK SUPPORT LT FLANGE AT NUTPLATE LOCATIONS BS1040-1080-LBL1 WL208. RE MOVED & REPLACED SEAT TRACK SUPPORT. 2 L 7 2 4F RT A2NM 20080815 NM 2008 8 15 UPS08M52852 1 20080603 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT HORZ STAB BARREL NUT BORE NR 19 FOUND CORRODED EXISTING REPAIR SLEEVE BUSHING REMOVED. BORE SURFACE CLEANED & MEASURE 1.126" DIA, BOTTOM SURFACE CLEANED & MAT'L THK REMAINING 0.082" MIN, FOUND BORE CLEAN HOLE CON D * BORE SIZE EXCEED LIMITS IAW EO MD11-5510-19409 M.10X MAGN DVI C/O & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NUT BORE NR19 RT WAS ACCOMP IAW EN1257-08 & IS ACCEPT IAW EO MD11-5510-30011A. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52936 1 20080712 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 32 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INS TALLED BUSHING IAW EO MD11-5510-19409-N AND SAA TRAVELER 80538390001. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52919 1 20080721 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR3 LT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INSTA LLED BUSHING IAW EO, MD11-5510-19409-N AND SAA TRAVELER 80538770001 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52920 1 20080722 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP INSPECTION TYPE-1C FOUND CORROSION IN NR 13 LT BARREL NUT BORE HOLE REMOVED CORROSION, FABRICATED BUSHING, AND INSTA LLED BUSHING IAW EO, MD11-5510-19409-N AND SAA TRAVELER 80538790001. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52765 1 20080716 A 2560 GIRT BAR DOUG MD11 MD11F 3023600 NM LT DOOR STUCK A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 LT DOOR WOULD NOT BE ARMED, LEVER STUCK. ADJUSTED LT DOOR SLIDE GIRT BAR IAW AMM 25-61-01. OPS CHECKED GOOD. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08552875 1 20080724 A 2560 ESCAPE REEL BOEING 757 75724APF 1384969 NM COCKPIT UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 424UP 25369 REF M380690 NR4 INERTIAL ESCAPE REEL REMOVED. REPLACED NR 4 INERTIAL ESCAPE REEL IAW MM 25-61-02-2. 2 L 7 2 4F RT A2NM 20080815 NM 2008 8 15 UPS08M52859 1 20080517 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT HORZ STAB BARREL NUT BORE NR 24 FOUND CORRODED CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51 -21-01 VII REV 35. BORE REAM TO 1.067"DIA, REMAINING BLEND OUT 0.040" DIA, BOTTOM REMAINING BLEND OUT 0.060" DEEP, BORE FOUND BLEND OUT EXCEEDING LIMITS IAW EO MD11-5510- 19409M.10X MAGN DVI & FOUND NO CORROSION EVIDENT. REPAIRED BARREL NU T BORE NR24 RT WAS ACCOMP IAW EN1238-08 & IS ACCEPT IAW MD11-5510-30011A. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52860 1 20080517 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 21 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51-21-01 REV 35. BORE REAM TO 1.067"DIA, REMAINING BLEND OUT 0.083" DEEP, BOTTOM REMAINING BLEND OUT 0.045", BORE BLEND OUT FOUND EXCEEDING LIMITS IAW EO MD11-5510-19409M.1 0X MAGN DVI C/O & FOUND NO CROSSION EVIDENT.REPAIRED AT BARREL NUT BOR E NR 21 RT ACCOMP IAW EN 1234-08 & IS ACCEPTABLE IAW EO MD11-5510-30011A. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 UPS08652725 1 20080702 A 5320 140T0130U39 ANGLE BOEING 767 76734AF 1385212 NM BS 1085 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 301UP 27239 INSPECTION TYPE-C, AFT CARGO COMPT BS 1085 LBL 26 UNDER FLOOR CHORD ANGLE CRACK. CRACK LENGTH .6250", AFT CARGO COMPT B S 1085 LBL 26 UNDER FLOOR CHORD ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20080818 WP 2008 8 18 UPS08852903 1 20080703 A 5711 SPAR CAP DOUG DC8 DC871F 302199D WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, CRACK AT CENTER SPAR CAP WEB FLANGE JUST IB XRS255 NR MAIN. STOP DRILLED CRACK , FABBED AND INSTALL ED REPAIR DOUBLER IAW. SRM., 51 -1-8, 57-2-0 FIG. 2, 51-1-20D. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852621 1 20080606 A 5230 SKIN DOUG DC8 DC871F 302199D WP CARGO DOOR DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, PIT 33 DOOR SKIN DENTS, REF D-373766. REMOVED EXISTING REPAIR DOUBLER ON C PIT DOOR IAW SRM 51-1-2 1 AND 51-1 -20D. HFEC PREVIOUS CUTOUT AND DENTED AREAS, NO CRACKS NOTED IAW NDTSP M 06-10-01. FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW SRM 5 2-02-00 FIG 2,52-02-00,AND 51-01-21. 2 L 7 4 4F RT 4A25 20080820 NM 2008 8 20 ASAA0843237 1 20080629 A 5340 693535214 STRINGER CLIP BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 STRINGER CLIP IS CRACKED. REPLACED CLIP IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843238 1 20080629 A 5340 69353521 STRINGER CLIP BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 STRINGER CLIP IS CRACKED. REPLACED CLIP IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843239 1 20080629 A 5340 69353521 STRINGER CLIP BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 STRINGER CLIP IS CRACKED. REPLACED CLIP PER SRM 51 40 02. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843240 1 20080625 A 5753 6546486149 WEDGE BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 LT IB MID FLAP T/E WEDGE IS DENTED ON LOWER SURFACE. REMOVED DAMAGED SECTION AND INSTALLED FILLER DOUBLER AND BONDED RE PAIR IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843244 1 20080625 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU NR 6 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 NR6 SPOILER LOWER SURFACE IS DENTED. INSTALLED REPAIR DOUBLER AND BONDED REPAIR IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843247 1 20080625 A 5753 65C2632017 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU T/E FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 LT OB MID FLAP LOWER SURFACE IS DENTED. BOND REPAIRED WITH DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 2008 8 20 ASAA0853257 4 20080801 A 3442 6225135202 DRIVE UNIT BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE WEATHER RADAR FAILED A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 570AS 20112 35185 PWS FAILED AFTER ENGINE START. REPLACED WXR ANT DRIVE UNIT WITH SERVICABLE ONE. VERIFIED PN. OPS TEST PASS REF MM 34-43 -11-000-802. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 NM 2008 8 20 ASAA0843274 1 20080729 A 5315 65C3394116 FLOORBEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 FLOORBEAM AT STA 312, RBL 6 CORRODED. REMOVES STA 312 FLOOR BEAM " T" CAMP FABBED FLOORBEAM T CAP 2 + 3 REPAIR PARTS + I NSTALLED REPLACEMENT T CAP 2 + 3 PARTS IAW SRM 53-10-51, REPAIR 5. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843282 1 20080629 A 5315 65C339421 FLOORBEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 FLOORBEAM AT STA 328 FROM RBL 12 TO THE R1 DOOR HAS CORROSION ON THE UPPER T CAP. REMOVED FLOORBEAM, T CAP FABBED T CAP AND SPLICE REPAIR PARTS, INSTALLED ALL REPAIR PARTS IAW EA NR 12768. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843285 1 20080718 A 5313 FITTING BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AT THE AFT SIDE OF THE APB STRINGER 5R END FITTING IS GOUGED. REMOVED AND REPLACED STRINGER 5R END FITTING ON THE AFT SI DE OF THE APB IAW SRM 51-40-02, FIG 8. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843287 1 20080718 A 5313 FITTING BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AT THE AFT SIDE OF THE APB STRINGER 4RT END FITTING IS GOUGED. REMOVED AND REPLACED STRINGER 4RT END FITTING ON THE AFT SIDE OF THE APB IAW SRM 51-40-02, P6. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 EU 2008 8 20 F3LA200800426 1 20080707 A 5321 D53480019216 SHEAR PLATE AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 805FR 1660 DURING C-CHECK INSP, NOTED CORROSION AROUND FAR RT NUTCLIP HOLE ON SHEAR PLATE ALONG FRAME 68 BETWEEN Y765 AND Y1292. MA INT REMOVED, FABRICATED AND INSTALLED SERVICEABLE SHEAR PLATE AT FRAME 68 BETWEEN Y765 AND Y1292 IAW DRAWING O53670099, SRM 51-21-11, SRM 51-31-00 AND SRM 53-42-12-420-051B. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABL E. (B) 2 L 7 2 4F 4 F RT 20080820 NM 2008 8 20 F3LA200800478 1 20080711 A 5320 D5347047400290 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP, NOTED CORROSION ON AFT CARGO COMPARTMENT LT PROFILE, FWD AREA OF AFT CARGO, AT FRAME C47 TO FRAME C 51. MAINT REMOVED AND REPLACED PROFILE AT FRAME C47 TO FRAME C51 IAW SRM 51-72-11, 51-21-11 AND 51-42-11. UPON COMPLETIO N FO THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 EU 2008 8 20 F3LA200800415 1 20080701 A 5320 D5367301200000 PANEL AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 805FR 1660 DURING C-CHECK INSP NOTED FWD CARGO PIT TRANSITION PANEL 131BF IS DAMAGED. MAINT REPAIRED FWD CARGO PIT TRANSITION PANEL 131BF IAW SRM 53-02-00 PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. ( B) 2 L 7 2 4F 4 F RT 20080820 2008 8 20 SWAA084532 4 20080815 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084531 1 20080817 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED FWD SERVICE DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20080820 EU 2008 8 20 F3LA200800545 1 20080807 A 5321 D5367302100000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CARGO BAY DAMAGED A F3LA K NONE O OTHER UK UNKNOWN 1 NM 03 915FR 65 1851 LINE MECHANIC NOTED THE AFT CARGO PIT TRANSITION PANEL 151AE WAS DAMAGED. MAINT REPAIRED DAMAGED PANEL 151AE IAW SRM 53 -02-00, STEP 2, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080819 NM 2008 8 19 SWAA084181 1 20080728 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 22R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084195 1 20080726 A 2121 215201 FAN BOEING 737 7373Q8 1384670 NM E&E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 29 662SW 23255 DECLARED EMERGENCY. ON DESCENT INTO ELP CREW REPORTED STRONG BURNING SMELL. GASPER AND RECIRC FANS TURNED OFF SMELL DI SSIPATED. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084205 1 20080728 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT UPPER HINGE CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084206 1 20080728 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084251 1 20080731 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 298WN 32543 DURING SCHEDULED HC1 CHECK, FOUND RT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084252 1 20080731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 14R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084259 1 20080731 A 5311 6546529 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 440, STR 25L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084265 1 20080801 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 238WN 34713 DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 12 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084266 1 20080803 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 268WN 32524 L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084278 1 20080801 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843251 1 20080625 A 5753 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 RT IB AFT FLAP LOWER SURFACE DENTED. BOND REPAIRED IAW SRM 51-70-16. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084318 1 20080804 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084353 1 20080803 A 3350 416A5600 SIGN BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 728SW 27860 R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN ASSY PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0853218 1 20080723 A 2131 2193301AC CONTROLLER BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE CABIN PRESSURE FAULTED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 585AS 3597 35683 "AUTO FAIL" ILLUMINATED. CONFIRMED AUTO FAIL LIGHT ON.RESET POWER. RAN BITE TEST IAW FIM TASK 21 31 TASK 801. ALL CABIN CONTROLLER TEST PASS. AUTO FAIL LIGHT IS OUT. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 NM 2008 8 20 ASAA0843208 1 20080629 A 5311 652C72370 FRAME BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU BS 492 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 705AS 29318 FWD CARGO PIT FRAME UPPER STRAP CORRODED REPAIRED IAW SRM 51-40-02-51-50- 05. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NE 2008 8 20 ASAA0853203 2 20080718 A 7261 OIL SYSTEM BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 1 ENGINE LOW A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 587AS 2932 35684 895977 NR1 ENGINE OIL QUANTITY READS 13 QUARTS ENG NR1 OIL ADDED: 6 QTS,ENG NR2 OIL ADDED: 5 QTS, APU OIL ADDED : 0. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 NM 2008 8 20 08FDEA02973 1 20080718 A 5347 601096418 SEAT TRACK DOUG MD10 MD1030F 3024020 NM FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 303FE 46802 MAIN CARGO, LUGS ON SEAT TRACK WORN AT FS 1279 LBL 47. REMOVED DAMAGED SECTION, FABRICATED NEW SECTION, FABRICATED SPLI CE HAT/PLATE AND INSTALLED ALL REPAIR PARTS ON MAE TRAVELERS T8/748246 AND T8/748248 IAW SRM 53-70-00. REPAIR IS CLASSI FIED AS A MAJOR REPAIR, REPORTABLE DISCREPANCY AND RII. 2 L 7 3 4F RT A22WE 20080820 NM 2008 8 20 ASAA0843189 1 20080629 A 5753 46430129 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU FOREFLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 LT WING OB FORE FLAP HAS SEVERAL DENTS ON LOWER SURFACE PREPARED DAMAGED AREA FABRICATED REPAIR DOUBLERS AND BONDED IAW SRM 51-70-10, REPAIR 2. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843293 1 20080627 A 5311 654659673 FRAME BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AFT PIT FRAME AT STA 727C IS DENTED ABOVE THE STR 24L REMOVED DAMAGED AREA FABBED FILLER + REPAIR ANGLES + INSTALLED IAW SRM 51-70-11, FIG 1. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084553 1 20080817 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 F3LA200800451 1 20080711 A 5321 D5367303600000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 940FR 2465 DURING C-CHECK INSP, NOTED AFT PIT PANEL 161CF DAMAGED. MAINT REMOVED DAMAGE AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 NM 2008 8 20 SWAA084545 1 20080817 A 5312 6517853 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179, LBL 5.7. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 F3LA200800392 1 20080622 A 5321 D53673310000000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 32 2448 DURING C-CHECK INSP NOTED FWD PIT FLOOR PANEL 131AF HAS SEVERAL PUNCTURES. MAINT REPAIRED FLOOR PANEL 131AF IAW SRM 53- 02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 NM 2008 8 20 F3LA200800405 1 20080628 A 5321 D53672280000000 FLOORBOARD AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSP NOTED AFT CARGO PIT FWD FLOORBOARD PANEL 151PE HAS A HOLE AT THE AFT LT EDGE. MAINT REMOVED DAMAGED AREA AND FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACC EPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 NM 2008 8 20 SWAA084530 1 20080817 A 5743 115A5211 FITTING BOEING 737 737705 13844SC NM RT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 271LV 29090 DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 F3LA20800387 1 20080622 A 5210 D5211009820000 HOOK AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE L2 DOOR INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSP NOTED L2 DOOR LATCH HANDLE CAN BE OPERATED WHILE DOOR IS OPEN. MAINT REMOVED AND REPLACED L2 DOOR I NNER HANDLE LOCK HOOK IAW AMM 52-13-21-420-052 STEP 17. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPT ABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 NM 2008 8 20 F3LA200800291 1 20080602 A 5320 D5367223600000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 162CF HAS DENTS AND GOUGES. REMOVED DAMAGE AND CLEANED PANEL FILLED D ENTS AND REPAIRED PUNCTURE DAMAGE IAW SRM 51-73-00 STEP 3C AND SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 NM 2008 8 20 SWAA084528 1 20080815 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 255WN 32513 EEPLS INOP AT ROW 1 ABC. R&R LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084543 1 20080817 A 5330 65C381921 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 265 AND BS 271, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084537 1 20080817 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080821 EU 2008 8 21 F3LA200800375 1 20080619 A 5755 D5754013720000 SLEEVE AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE LT WING SPOILER DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 941FR 2483 DURING C-CHECK INSP, NOTED LT WING NR FOUR SPOILER ATTACH BOLT IS ROTATED IN LUG ON SPOILER. MAINT MACHINED .040 OFF AN TI-ROTATION WEB VERIFIED SS MATERIAL FOR REPAIRED PO RT090486 AND BONDED AND THE REINFORCING PLATE TO THE ANTI-ROTATION WEB FOR THE CENTER HINGE IAW EA A9-57R-30397 STEPS 3, 4, 5, AND 6. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FO UND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800340 1 20080613 A 5321 D536722700000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP NOTED AFT CARGO FLOOR PANEL 152TG HAS A CRACK AND A HOLE. MAINT REPAIRED PANEL 152TG IAW SRM 53-02- 00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 EU 2008 8 21 F3LA200800404 1 20080626 A 2560 GIRT BAR AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE L1 DOOR OBSTRUCTED A F3LA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 03 913FR 1863 DURING CLIMB OUT THE FLIGHT CREW RECEIVED AN INDICATION L1 DOOR UNARMED LIGHT CAME ON AND THE AC RETURNED TO DEPARTURE. MAINT FOUND DEBRIS STUCK IN THE L1 DOOR GIRT BAR FITTING STOP LEVER AREA. MAINT CLEANED THE DEBRIS AND OPS CHECKED GOO D IAW AMM 53-11-00-310-034 AND THE AC WAS RETURNED TO SERVICE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 EU 2008 8 21 F3LA200800283 1 20080602 A 5315 D5347219320000 FLOORBEAM AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 77 1851 DURING C-CHECK INSP, NOTED FLOORBEAM Y765 RT HAS PITTING CORROSION AT FRAME 68 ON TOP SURFACE. MAINT REMOVED BEAM AND I NSTALLED NEW BEAM IAW DRAWING D53472815 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCE PTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 EU 2008 8 21 F3LA200800362 1 20080616 A 5320 D5367403400000 PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 941FR 2483 DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151HE HAS SEVERAL PUNCTURES. MAINT REPAIRED PANEL 151HE IAW SRM 53-0 2-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 EU 2008 8 21 F3LA200800414 1 20080701 A 5320 D5367221800000 PANEL AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 805FR 1660 REFERENCE NON ROUTINE C046424. DURING C-CHECK INSPECTION NOTED FWD CARGO PIT TRANSITION PANEL 132DG IS DAMAGED. MAINT RE PAIRED FWD CARGO PIT TRANSITION PANEL 132DG IAW SRM 53-02-00 PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT W AS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT 20080821 NM 2008 8 21 F3LA200800300 1 20080609 A 5315 D5311141420000 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 77 1851 DURING C-CHECK INSP, NOTED CORROSION ON FLOOR TRACK AT Y189 FRAME 20. MAINT REMOVED DAMAGED FLOORBEAM Y189 AND INSTALLE D NEW FLOORBEAM FROM FRAME 20 TO FRAME 24 IAW SRM 51-42-11 PARAGRAPH 7. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800301 1 20080609 A 5320 D5347047520600 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 77 1851 DURING C4 S1 C-CHECK INSP, NOTED AFT CARGO COMPARTMENT LT FLOOR PROFILE IS CORRODED FROM FRAME 51 TO FRAME 56 AT STRINGE R 38 LT. MAINT REMOVED AND REPLACED LT HAND FLOOR PROFILE IAW SRM 51-42-11 PARAGRAPH 5. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 ASAA0843292 1 20080720 A 5315 6545834103 FLOORBEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 312 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 FLOORBEAM LOWER STABILIZER AT STA 312, BL42 IS CRACKED STOP DRILLED, CRACKED FABBED DOUBLER AND INSTALLED REPAIR IAW SRM 53 10 51. 2 L 7 2 4F 4 F RT A16WE E21EU 20080821 WP 2008 8 21 I5HA0858005C 1 20080405 A 5100 340311020744 ANGLE CVAC 580 580 2422806 WP DAMAGED A I5HA O OTHER O OTHER NR NOT REPORTED 1 GL 25 581P 29 DURING A STORM (MIA) A CARGO CAN (ULB) WAS THROWN INTO THE RT SIDE OF N581P. THE RT PROPELLER WAS ALSO STRUCK A GLANCIN G BLOW. THERE WAS SIGNIFICANT DAMAGE TO THE SKIN AND SUPPORT STRUCTURE BENEATH THE SKIN. THERE WAS DAMAGE TO WIRING IN THE AREA. THE NOSE STEERING ACTUATOR WAS ALSO DAMAGED. DAMAGE AREA WAS BETWEEN FUSELAGE STATIONS 72 TO 125 AT APPROXI MATELY BETWEEN STRINGERS 11 AND 3. THE PROPELLER AND REDUCTION GEARBOX WERE REMOVED AND INSPECTED. NO DAMAGE TO EITHER . N581P WAS REPAIRED AND THE ACFT TEST FLOWN ON JULY 3, 2008. THE ACFT WAS RETURNED TO SERVICE JULY 8, 2008. (S) 2 L 7 2 4T RT 20080821 WP 2008 8 21 I5HA0858005E 1 20080405 A 5100 340311020734 CHANNEL CVAC 580 580 2422806 WP DAMAGED A I5HA O OTHER O OTHER NR NOT REPORTED 1 GL 25 581P 29 DURING A STORM (MIA) A CARGO CAN (ULB) WAS THROWN INTO THE RT SIDE OF N581P. THE RT PROPELLER WAS ALSO STRUCK A GLANCIN G BLOW. THERE WAS SIGNIFICANT DAMAGE TO THE SKIN AND SUPPORT STRUCTURE BENEATH THE SKIN. THERE WAS DAMAGE TO WIRING IN THE AREA. THE NOSE STEERING ACTUATOR WAS ALSO DAMAGED. DAMAGE AREA WAS BETWEEN FUSELAGE STATIONS 72 TO 125 AT APPROXI MATELY BETWEEN STRINGERS 11 AND 3. THE PROPELLER AND REDUCTION GEARBOX WERE REMOVED AND INSPECTED. NO DAMAGE TO EITHER . N581P WAS REPAIRED AND THE ACFT TEST FLOWN ON JULY 3, 2008. THE ACFT WAS RETURNED TO SERVICE JULY 8, 2008. (S) 2 L 7 2 4T RT 20080821 EU 2008 8 21 F3LA200800555 1 20080816 A 5320 D5348015900600 BLANKING PLATE AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 806FR 2218 DURING C-CHECK INSP, NOTED R2 FWD GIRT BAR BLANKING PLATE HAS CORROSION. MAINT REMOVED AND REPLACED BLANKING PLATE WITH NEW ONE FROM STOCK AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCE PTABLE. (S) 2 L 7 2 4F 4 F RT 20080821 NM 2008 8 21 F3LA200800372 1 20080619 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED RT HAND CABIN FLOOR PANEL 262FF HAS CORROSION. MAINT REMOVED AND REPLACED CABIN FLOOR PANEL 262FF IAW ROUTINE CARD 9625. UPON COMPLETION OR THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM 20080821 NM 2008 8 21 F3LA200800307 1 20080606 A 5321 D5367221800000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED THE FWD FLOOR PANEL 132DG HAS A PUNCTURE. MAINT CLEANED AND PREPPED DAMAGED, APPLIED FILLER, FABRICATED REPAIR PATCH AND INSTALLED REPAIR PATCH IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AN D FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800311 1 20080608 A 5320 D5347646100000 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP NOTED AFT CARGO PIT RT SIDE PROFILE HAS CORROSION SEVERAL PLACES BETWEEN FRAMES C59 TO FRAME C61. M AINT REMOVED AND REPLACED PROFILE IAW SRM 51-72-11, SRM 51-44-11 AND SRM 51-46-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800292 1 20080602 A 5320 D5367223700000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 DURING C4 S1 C-CHECK INSPECTION NOTED AFT PIT TRANSITION PANEL 162BF HAS DENTS. MAINT REMOVED DAMAGE AND CLEANED PANEL F ILLED DENTS ON PANEL 162BF IAW SRM 53-02-00. STEP 3C. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABL E. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800373 1 20080619 A 5315 D53480043204 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED LT CABIN FLOOR LONGERON BEAM Y1732 AT FRAME 66 HAS CORROSION AROUND FASTENER HOLE. MAINT FAB RICATED REPAIR ANGLES AND FILLER AND ACCOMPLISHED REPAIR IAW EA A0-53F-12234, EA A0-53T-12235, SRM 53-41-14 FIGURE 201 A ND SRM 53-51-14 FIGURE 201. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800306 1 20080605 A 5320 D5347646000000 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED THE AFT CARGO COMPARTMENT HAS CORROSION ON RT PROFILE BETWEEN FRAMES C54 AND FRAMES C55. MAI NT REMOVED AND REPLACED PROFILE AT AFT CARGO RT HAND SIDE BETWEEN FRAMES C54 AND C55 IAW SRM 51-72-11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IN WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800350 1 20080617 A 5321 D5367226800000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED AFT CARGO FLOOR PANEL 151FE HAS A HOLE. MAINT REPAIRED PANEL 151FE IAW SRM 53-02-00. UPON COM PLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800342 1 20080613 A 5321 D5367151300000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED FLOOR PANEL 242LF HAS DAMAGED ON TOP SURFACE PEELED BACK 4" X 6" ON AFT CORNER. MAINT REPAIRE D PANEL 242LF IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800352 1 20080617 A 5321 D5367175302200 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED AFT CABIN FLOOR PANEL 261HG DAMAGED BEYOND LIMITS. MAINT REMOVED AND REPLACED PANEL 261HG IA W SRM 53-22-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800351 1 20080617 A 5321 D53672027000000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED CARGO FLOOR PANEL 151TG HAS A HOLE. MAINT REPAIRED PANEL 151TG IAW SRM 53-02-00 REPAIR 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800316 1 20080608 A 5321 D5367179900000 FLOORBOARD AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP NOTED LAVATORY A FLOORBOARD 221PF HAS A HOLE AND IS DELAMINATED. MAINT REMOVED AND REPLACED FLOORPAN EL 221PF IAW AMM 53-22-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 SWAA084361 1 20080805 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 302 S28R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER 28R CORRODED AT BS 302. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084378 1 20080806 A 5310 6546818 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 967 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED 22Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 967, LBL 49. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084373 1 20080806 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 201LV 29854 EEPLS LENS CRACKED AT ROW 2 ABC. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084362 1 20080805 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 277 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 16R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084404 1 20080807 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080818 WP 2008 8 18 UPS08852623 1 20080611 A 5330 SKIN DOUG DC8 DC871F 302199D WP FS 270 L11L GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, MCD CUTOUT HAS REPAIR DOUBLER AND "L" ANGLE GOUGED BLENDED ANGLE, WITHIN LIMITS IAW SRM 53-2-0 FIG 1F. FABRICATED AND INSTALLED NEW DOUBLER IAW SRM 53-2-0 FIG 1B,51-1-21, AND 51-1-2 1A. 2 L 7 4 4F RT 4A25 20080818 NM 2008 8 18 UPS08652624 1 20080701 A 2721 MODULE BOEING 767 76734AF 1385212 NM GE CF6 CF680 30025 NE RUDDER TRIM MALFUNCTIONED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 314UP 27742 RUDDER TRIM STUCK AT 4 UNITS. T/S IAW FIM 27-21-00 FIG 106 FOUND RUDDER TRIM CONTROL PANEL FAULT. R/R AILERON AND RUDDER TRIM CONTROL MODULE IAW MM 27-21-23-2. OPS GOOD. 2 L 7 2 4F 4 F RT A1NM E13NE 20080818 NM 2008 8 18 UPS08M52611 1 20080610 A 5320 STRUCTURE DOUG MD11 MD11 3023602 NM AIR CON BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, AIR CON SYS NR 1 COMPARTMENT INTERIOR, AFT BILGE AREA, EXISTING ANGLE DOUBLER FOUND CORRODED. ATTACH CORROSION FRAME SUPPORTS AND RIB REMOVED IAW SR M51-31-01 VII R35. FRAME, SUPPORTS AND RIB CORROSION REMOVED IAW SRM 5 1-21-01 VII R35. REWORK AREA CLEANED AND REPROTECTED IAW SRM 51-21-01 VII R35. REINSTALLED FRAME,SUPPORTS & RIB ON FUS ELAGE AIR CON NR 1 SYS INTERIOR BILGE AREA IAW SRM 51-31-01 VII R35. 2 L 7 3 4F RT A22WE 20080818 2008 8 18 UPS08M52632 4 20080624 A 2565 BATTERY DOUG MD11 MD11F 3023600 NM ESCAPE SLIDE INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 252UP 48768 EVAC SLIDE REMOTE PRESS TO TEST INDICATING SYSTEM WON'T TEST. REPLACED BATTERY & LAMP. NO HELP. DEFERRED IAW MM 25-61-2 . REPLACED BATTERIES. SYSTEM OPS NORMAL IAW MM 25-61-15-4. M378674 CLOSED 2 L 7 3 4F RT A22WE 20080818 WP 2008 8 18 UPS08852659 1 20080612 A 5240 STRAP DOUG DC8 DC871F 302199D WP SERVICE DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, RT FWD SERVICE DOOR, FWD JAMB HAS RIVET INSTALLED THROUGH EDGE OF STRAP STA. 165 L20R. REMOVED STRA P, FABRICATED AND INSTALLED NEW STRAP IAW SRM 51-01-21 53-02-00. 2 L 7 4 4F RT 4A25 20080818 EU 2008 8 18 UPS08152913 1 20080722 A 5322 A5398111320051 SHEAR PLATE AIRBUS A300 A300F4622R 3930360 EU FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 153UP 0839 INSPECTION TYPE:5 YR MAIN CARGO COMPARTMENT LT FR 79 FLOOR LEVEL SHEAR PLATE CRACKED FWD OF AFT PRESSURE BULKHEAD. REPL ACED MAIN CARGO COMPARTMENT LT FR 79 FLOOR LEVEL SHEAR PLATE REF. A-300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080818 WP 2008 8 18 UPS08852922 1 20080730 A 3350 LIGHT DOUG DC8 DC873F 302199F WP COCKPIT BURNED OUT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 811UP 46089 EMERGENCY LIGHT DISARM CHECK LIGHT BURNED OUT. R&R EMERGENCY LIGHT DISARM CHECK LIGHT IAW 33-10-00. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 20080818 NM 2008 8 18 UPS08M52940 1 20080716 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 27 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INSTAL LED BUSHING IAW UPS EO, MD11-5110-19409-N AND SAA TRAVELER 80538570001. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 UPS08552954 1 20080706 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM BS 1195 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 457UP 25478 INSPECTION TYPE-C2, CORROSION ON CARGO TRACK LBL 25, BS 1195, WL 208. CORROSION BLENDS OUT OF LIMITS REMOVED AND REPLAC ED SEAT TRACK. 2 L 7 2 4F RT A2NM 20080818 NM 2008 8 18 UPS08552955 1 20080731 A 5711 PLATE BOEING 757 75724APF 1384969 NM LT WING SPAR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 INSPECTION TYPE-C2, LT WING T/E AFT LOWER SPAR WIGGLE PLATE BROKEN FWD OF NR 5 SPOILER AT RSS342. REMOVED AND REPLAC ED WIGGLE PLATE IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 20080818 EU 2008 8 18 UPS08152978 1 20080722 A 5321 B5327077900100 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 153UP 0839 INSPECTION TYPE: 5 YR, MAIN CABIN FLOOR PANEL NR 252BN IS CRACKED AT FWD END. REPAIRED MAIN CABIN FLOOR PANEL NR 252BN FWD CRACK IAW SRM 53- 10-20 FIG 201 PARA 8. 2 L 7 2 4F RT A35EU 20080818 NM 2008 8 18 UPS08M52957 1 20080626 A 5711 ARB7188 SPAR CAP DOUG MD11 MD11F 3023600 NM LT WING LE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, LT WING LWR FWD SPAR CAP XORS 799 HAS EXFOLIATED CORROSION. REMOVED CORROSION AND FOUND OUT OF LIM ITS, CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM VOL 1 57-10-00 FIG.45. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 UPS08M52967 1 20080708 A 5754 ARB2363502 SKIN DOUG MD11 MD11F 3023600 NM RH WING LE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE:1C, RT WING FIXED LE ABOVE NR 3 PYLON LWR SKIN FOUND GOUGED. REMOVED SKIN PANEL, FABRICATED AND INS TALLED REPLACEMENT SKIN PANEL IAW SRM VOL.3 57-43-01 FIG.1, VOL.2 51-31-01 AND DWG ARB2363. 2 L 7 3 4F RT A22WE 20080818 2008 8 18 SWAA084026 4 20080719 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 451WN 32495 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080818 2008 8 18 SWAA084048 2 20080717 A 7320 8063214 MEC BOEING 737 737317 138447P NM NR 1 ENGINE FAULTY A SWAA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 SW 29 686SW 23175 DURING DESCENT NR 1 ENGINE HANG UP AT 50% FOR TWO TO THREE MINUTES, THEN ROLLS BACK. R&R NR 1 MEC PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084049 1 20080719 A 3040 2315 CONTROLLER BOEING 737 7373Q8 1384670 NM WINDOW HEAT FAULTY A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 687SW 23388 FLIGHT DECK R1 WINDOW ARCED INFLIGHT. R&R WINDOW HEAT CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084405 1 20080807 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM BS 706 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084406 1 20080807 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 927 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND STRINGER STRINGER CLIP CRACKED AT BS 927, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084396 1 20080806 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 717SA 27851 DURING SCHEDULED HC1 CHECK, AFT RT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080821 2008 8 21 SWAA084397 4 20080806 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 737JW 27869 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVACV SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843309 1 20080630 A 5753 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU RT WING TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 RT IB FORE FLAP UPPER SURFACE CHAFED ALONG OB EDGE. REMOVED DAMAGED AREA FABBED FILLER, DOUBLER, BONDED REPAIR IAW SRM 51-70-10 REPAIR 4. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843241 1 20080625 A 5753 WEDGE BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 LT IB MID FLAP T/E WEDGE IS DENTED. INSTALLED DOUBLER AND BONDED REPAIR IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084337 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084338 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080820 2008 8 20 SWAA084354 4 20080804 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 764SW 27878 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080820 EA 2008 8 20 TRAX200800990 1 20080809 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 751EV 10163 LT OVERWING EMERGENCY EXIT LOWER LIGHTED EXIT SIGN HAS SEVERAL BULBS INOPERATIVE. REMOVED AND REPLACED LT LOWER EMERGEN CY EXIT SIGN BAD BULBS IAW CRJ 700 AMM 33-51-05. (S) 2 L 7 2 4F RT A21EA 20080820 NM 2008 8 20 ASAA0843194 1 20080630 A 5330 6546881115 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU BS 1040 S12-13L DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 FUSELAGE DENT AT STA 1040 AND BETWEEN STR 12L TO 13L US CREASED REF SAD 5088799 CUT OUT DAMAGED AREA FABRICATED REPAIR D OUBLER AND INSTALLED IAW DRM 53-80-01, FIG 201 REPAIR 3. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843197 1 20080701 A 5330 65C357986 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU BS 909 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 RT EXTERNAL FUSELAGE PROTRUSION DENT AT STA 909 ON STR 17R CUTOUT DAMAGED AREA FABRICATED FILLERS DOUBLER TRIPLER LOCATE D DRILLED AND INSTALLED IAW EA 5330 02365 AND EA 12769. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 2008 8 20 SWIA200819858 4 20080712 A 2210 6229968101 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA YAW DAMPER FAULTY A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 403SW 7028 RECEIVED UNCOMMANDED YAW DURING FLIGHT. (FLIGHT NR 2512) REPLACED YAW DAMPER NR2 LINEAR ACTUATOR IAW AMM 22-22-01. OPS CHECK GOOD. P/N 622-9968-101, S/N OFF 714. 2 L 7 2 4F RT A21EA 20080820 NM 2008 8 20 SWAA084556 1 20080817 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 EU 2008 8 20 USAA920081413 1 20080724 A 2560 P207003001 FLASHLIGHT AIRBUS 320 A320214 3930316 EU CABIN DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 123UW 1310 FLT 845 BOS-ORD EE FORWARD BREAKAWAY FLASHLIGHT USED. MAINTENANCE REMOVED AND REPLACED THE FORWARD INBOARD FLASHLIGHT A ND SEAL WITH SERVICEABLE UNIT. OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F RT A28NM 20080820 NM 2008 8 20 ASAA0843180 1 20080629 A 5755 654645268A SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 RT WING IB GROUND SPOILER HAS MULTIPLE DENTS ON LOWER SURFACE PREPARED DAMAGED AREA FABRICATED FILLERS AND REPAIR DOUBLE RS AND BONDED IAW SRM 51-70-10, REPAIR 4. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843294 1 20080628 A 5320 65479577 INTERCOSTAL BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AFT PIT INTERCOSTAL AT STA 847, 867 AT STR 35 R IS CORRODED REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-05, FIG 2. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084529 1 20080817 A 5743 115A5211 FITTING BOEING 737 737705 13844SC NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 271LV 29090 DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084538 1 20080817 A 3350 65C27028 LIGHT BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 8 DEF. FOUND LIGHT ASSY DISCONNECTED. CONNE CTED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 F3LA200800282 1 20080601 A 5320 D5347112320200 SUPPORT AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 DURING C-CHECK INSP, NOTED THE SUPPORT FRAME FOR SHEAR PLATE CORRODED ON BOTTOM SURFACE AT NUTCLIP HOLES LOCATED AT THE LT OB SIDE AT FRAME 70. MAINT REMOVED CORRODED SUPPORT FRAME AND INSTALLED NEW SUPPORT FRAME IAW SRM 51-42-11 AND SRM 5 1-44-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 ASAA0843316 1 20080630 A 5320 654659247 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AFT PIT FLOOR SUPPORT AT STA 767, LBL 8.10 UPPER SURFACE IS CORRODED. REMOVED DAMAGED AREA FABBED REPAIR PARTS AND INST ALLED IAW EA 5320-01844. 2 L 7 2 4F 4 F RT A16WE E21EU 20080821 NM 2008 8 21 F3LA200800298 1 20080605 A 5340 D5211155400040 FITTING AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 77 1851 DURING C-CHECK INSP, NOTED L2 DOOR AFT TOP SLIDE ATTACH POINT BRACKET CORRODED. MAINT REMOVED CORRODED FITTING AND INST ALLED SERVICEABLE FITTING IAW SRM 51-42-11 PARAGRAPH 5, AMM 20-21-11-911-01 AND AMM 20-21-11-991-003 SHEET 203. UPON CO MPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800395 1 20080624 A 5320 D5367301800000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSP, NOTED AFT CARGO PIT FWD LT HAND UPPER TRANSITION PANEL 151UG HAS SEVERAL HOLES. MAINT REPAIRED FLO OR PANEL IAW THE REQUIREMENTS OF SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCE PTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800348 1 20080617 A 5321 D53672237000000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED CARGO FLOOR PANEL 162BF HAS TWO HOLES. MAINT REPAIRED AFT CARGO FLOOR PANEL 162BF IAW SRM 53 -02-00 REPAIR 207. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800353 1 20080617 A 5321 D5367204300000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED AFT CARGO FLOOR PANEL 151HE HAS A DENT AND A HOLE. MAINT REPAIRED PANEL 151HE IAW SRM 53-02- 00 REPAIR 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 2008UALA03696 1 20080702 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1440 S1 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 LIGHTNING STRIKE ON FUSELAGE SKIN AT STA 1445, 1 INCH LEFT OF STR 1. *S/D* DAMAGE FROM LIGHTNING STRIKE. REMOVE DAMAG E PER MM 53-30 -95 PG 603, ITEM B BY DRILL HOLE. ACP HEFC INSP PER NDT MM 51-00 -16, NO CRACK FOUND, INSTALL BLIND FAST ENER PER MM 53-30-95. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NE 2008 8 21 SWAA084418 2 20080807 A 7230 CFM567 ENGINE BOEING 737 7377H4 1384404 NM GE CFM56 CFM56* 13802 NE LEFT STALLED A SWAA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 29 400WN 27891 888280 DECLARED EMERGENCY, NR 1 ENG COMPRESSOR STALLED, VIBRATION INDICATION AND N1 ROLLED BACK TO 15 PERCENT. REMOVED AND REP LACED NR 1 ENG PER MT. 2 L 7 2 4F 4 F RT A16WE E2GL 20080821 NM 2008 8 21 SWAA084410 1 20080807 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 277 S10L/R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03722 1 20080705 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 698 S26-28R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 EXTERNAL FUSELAGE SKIN STATIC DISCHARGE AT BS 698 BETWEEN STR 26R AND 28R. *S/D* LIGHTNING DISCHARGE. REMOVED RIVET A ND ACP HFEC NO CRACK INDICATED. INSTALLED BLIND FASTENER IAW SRM 53-30-95. CHERRY MAX FASTENER MUST BE REINSPECTED AT EVERY C CHECK AND A SOLID FASTENER INSTALLED AT NEXT HMV. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NM 2008 8 21 2008UALA03723 1 20080705 A 5310 CREASE BEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 940-960 S17L CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 CREASE BEAM AREA BETWEEN STA 940 TO 960, STR 17L HAS CORROSION. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED WEB, FAB NEW WEB REF BOA DWG 144N5150 REC AND 144N5140. INSTALLED PER SRM 51-4-02. 2 L 7 2 4F 4 F RT A2NM E17NE 20080818 NM 2008 8 18 SWAA084051 1 20080718 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM BS 933 S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 933, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084052 1 20080718 A 5330 6545765 SKIN BOEING 737 7373Q8 1384670 NM BS 506B S18R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506B, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084066 1 20080720 A 5343 6546543 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED MV2 CHECK, FOUND LT MLG 685 FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084067 1 20080720 A 5343 6546544 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 DURING SCHEDULED MV2 CHECK, FOUND RT MLG 685 FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080818 2008 8 18 SWAA084077 4 20080722 A 2565 D31354 SLIDE BOEING 737 7373K2 13844BA NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED SPV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084085 1 20080722 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084084 1 20080722 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM BS 907 S4L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4L. R&R STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084078 1 20080722 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500D S5R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5R. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084079 1 20080722 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500D S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084083 1 20080722 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM BS 908 S4R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4R. R&R STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084071 1 20080720 A 5753 SKIN BOEING 737 7373A4 1384585 NM RT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 674AA 2284 23252 DURING SCHEDULED MV2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. R&R FLAP PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084095 1 20080723 A 5311 6546554 FRAME BOEING 737 7373Q8 1384670 NM BS 847 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084094 1 20080723 A 5311 65C25228 FRAME BOEING 737 7373Q8 1384670 NM BS 727C S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727C, STR 8R. REPAIRED FRAME PER SWA E A. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084093 1 20080723 A 5311 6546536 FRAME BOEING 737 7373Q8 1384670 NM BS 559 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084072 1 20080723 A 5311 6546555 FRAME BOEING 737 7373Q8 1384670 NM BS 867 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084100 1 20080722 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM BS 730D S23R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730D, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03728 1 20080706 A 2121 731378A FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXHAUST SEIZED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 543UA 25698 AFT EQ EXHAUST FAN 1 STATUS MSG. *S/D* AFT EQ EXHAUST FAN FAILURE, BEARING WEAR. REPLACED AFT EQ EXHAUST FAN 1, OPS C HECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NM 2008 8 21 2008UALA03730 1 20080706 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 BACKSHOP - 2R DOOR, CORROSION AT BASKET CAM ATTACHMENT INSERT LOCATION 1 PLACE. *S/D* AFTER FURTHER ANALYSIS, IT HAS B EEN DETERMINED THIS IS NOT AN SDR REPORTABLE EVENT. THIS REPORT IS RELATED TO A COMPONENT NOT INSTALLED ON AN AIRFRAME IN A BACKSHOP. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NM 2008 8 21 2008UALA03733 1 20080706 A 2780 SWITCH BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 676UA 30028 EICAS MSG L/E SLAT ASYM DISPLAYED, LEADING EDGE LIGHT ILLUM WITH THE FLAP LEVER IN 1. BOTH FLAP POINTERS ARE CORRECT. FOUND FAULTY SWITCH. REPLACED SW282. OP CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20080821 NM 2008 8 21 2008UALA03752 1 20080703 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 526UA 24994 DOOR 1L, 2L AND 3L EXTERIOR EMERGENCY LIGHTS INOP. *S/D* BULBS INOP. REPLACED BULBS, OPERATES NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NM 2008 8 21 2008UALA03754 1 20080706 A 3350 INVERTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 549UA 25397 EEL LIGHT FROM ROW 16 TO ROW 23 IS INOP. INVERTER INOP. REPLACED INVERTOR, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NM 2008 8 21 SWAA084416 1 20080807 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND NLG WHEEL WELL RT CEILING PANEL CUTOUT WEB CRACKED. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084417 1 20080807 A 5312 6545819 PRESSURE PANEL BOEING 737 7373H4 1384600 NM NLG W/W CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND NLG WHEEL WELL LT CEILING PANEL CUTOUT WEB CRACKED. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084369 1 20080805 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 312, LBL 3 TO LBL 7. REPAIRED FLOORBEAM PER SRM AND BOEING DRAWING. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03766 1 20080707 A 2612 6937307149 MODULE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE DETECTION INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 349UA 24253 CREW REPORTS, CARGO FIRE SUPPRESSION PANEL WON’T TEST. ONLY GET THE 4 DETECTOR LIGHTS. NO FAIL LIGHTS OR FIRE LIGHT CO MES ON. REPLACED MODULE OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080821 NM 2008 8 21 SWAA084386 1 20080806 A 3350 65C27093 LIGHT BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080821 2008 8 21 SWAA084370 4 20080731 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 715SW 27849 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084371 1 20080805 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 776WN 30591 DURING SCHEDULED 8Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084372 1 20080805 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 909WN 32458 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084384 1 20080806 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM BS 706 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080821 2008 8 21 SWAA084359 4 20080805 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 251WN 32510 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084426 1 20080808 A 5322 6546569 SHEAR TIE BOEING 737 7373Q8 1384670 NM BS 986 S25L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 986, STR 25L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03111 1 20080530 A 2432 18550000 BATTERY BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE MASTER FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 667UA 29239 MAIN BATTERY CHARGER STATUS MESSAGE WOULD NOT ERASE. *S/D* SUSPECT FAULTY BATTERY. REPLACED MAIN BATTERY. OPS CHECKS GOOD. REF: MM 24-31-02. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080821 NM 2008 8 21 2008UALA03312 1 20080610 A 3610 23417441 PRECOOLER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 1 ENGINE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 783UA 26950 LEFT ENGINE PRECOOLER LEAKING BEYOND LIMITS. *S/D* SUSPECT FAULTY PRE COOLER. REPLACED PRE COOLER LEAK CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080821 NM 2008 8 21 2008UALA03284 1 20080608 A 3350 767 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 773UA 26929 DOOR 3L EXTERIOR EMERGENCY LIGHT INOPERATIVE. *S/D* SUSPECT FAULTY LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SE RVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080821 NM 2008 8 21 2008UALA03287 1 20080607 A 2120 UNKNOWN BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE GALLEY ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 785UA 26954 BURNING ODOR IN BC GALLEY WHEN ALL COFFEEMAKERS ON. CHECKED COFFEEMAKERS, HOT PLATES, OVENS, CEILING LIGHTS, GALLEY LI GHTS AND A CHILLER ALL OK. NO BURNING SMELL ON ARRIVAL. COULD NOT DUPLICATE PROBLEM. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080821 NM 2008 8 21 2008UALA03083 1 20080529 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 5A FWD AND AFT LIGHT ASSY'S. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080821 NM 2008 8 21 2008UALA03109 1 20080531 A 7500 97980612 CONTROL VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT ENGINE SURGE MALFUNCTIONED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 668UA 30024 NR 1 ENGINE WOULD NOT START ON APU DUCT LOW 20 PSI NR 2 STARTED DID XBLEED. *S/D* PER HNL "CHECKED THE DUCT PRESSURE FLUCTUATES WITH NO LOAD. CLEANED SURGE VALVE FILTER, NO HELP. REPLACED SURGE CONTROL VALVE MR49532-222 (979806-12) WI TH MR49532-231. ENGINE START GOOD 30 PLUS PSI ". NO SHOP FINDINGS ARE AVAILABLE ON OFF UNIT. 2 L 7 2 4F 4 F RT A1NM E24NE 20080821 NM 2008 8 21 2008UALA03188 1 20080603 A 2910 AE7093101 LINE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE HYD SYSTEM WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 226UA 30226 FOUND OUTER INSULATION ON HYD PRESS HOSE BURNED THROUGH TO STAINLESS BRAIDED LAYER. *S/D* FOUND HYDRAULIC LINE FRAYED. REPLACED PRESSURE HYDRAULIC LINE, NO LEAKS FOUND. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080821 NM 2008 8 21 2008UALA03206 1 20080602 A 7500 32907449 VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE BLEED SYS FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 204UA 28713 BLEED FAMV R RIGHT ENGINE BLEED FAN AIR MODULATING VALVE (FAMV) FAILED OPEN OR CLOSED, OR RIGHT AIR SUPPLY AND CABIN PRE SSURE CONTROLLER FAILURE. STATUS MSG-3610320 LATCH DC MODE. *S/D* SUSPECT FAN AIR MODULATING VALVE. REPLACED NR 2 EN GINE FAMV IAW MM 36-11-16. OPERATION TEST PER 36-10-00-700-804. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080821 NM 2008 8 21 2008UALA03209 1 20080601 A 8012 8088846 START VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 ENGINE FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 776UA 26937 ENGINE START VALVE L LEFT STARTER AIR VALVE POSITION DISAGREES WITH COMMANDED POSITION OR STARTER AIR VALVE POSITION IND ICATION IS LOST. STATUS CREW COMMENTS: CHRONIC MSG-8061561 INACTV ES MODE, MSG-8061561 INACTV ES MODE. *S/D* FOUND F AULTY START VALVE. REPLACED NR 1 ENGINE START VALVE PER MM 80-11-02 AND OPS CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080821 NM 2008 8 21 2008UALA03220 1 20080604 A 3350 285W0955102 BATTERY PACK BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 784UA 26951 PED 1L EPAS BATTERY PACK GREEN TEST LIGHTS INOP. *S/D* SUSPECT FAULTY BATTERY. REPLACED 9V BATTERIES IAW MM 52-11-20. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080822 NM 2008 8 22 F3LA200800384 1 20080621 A 5320 D5347112420100 SHEAR PLATE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP NOTED RT CABIN FLOOR LATERAL SHEAR PLATE AT Y1162 BETWEEN FRAMES 69 AND FRAMES 70 HAS AREAS OF CORRO SION. MAINT REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUN D ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM 20080822 NM 2008 8 22 F3LA200800429 1 20080707 A 5321 D5367161400100 FLOORBOARD AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 DURING C-CHECK INSP NOTED CABIN FLOORBOARD 242FF IS PUNCTURED IN THE CENTER OF THE PANEL. MAINT PREPPED FLOORBOARD 242FF FOR REPAIR AND REPAIRED IAW SRM 53-12-00 PARAGRAPH 5B FIGURE 202. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FO UND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800407 1 20080628 A 5320 D5367402100000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSP NOTED AFT CARGO PIT FWD LT HAND LOWER TRANSITION PANEL 151AE HAS A HOLE AT FWD LOWER END. MAINT REP AIRED AND INSTALLED SERVICEABLE PANEL 151AE IAW SRM 53-42-14-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AN D FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM 20080818 NM 2008 8 18 SWAA084126 1 20080724 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 727 S27L/R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 727, STR 27L AND BS STR 27R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084127 1 20080724 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 980 S23L BUCKLED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN BUCKLED AT BS 980, STR 23L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084128 1 20080724 A 5311 6517684 FRAME BOEING 737 7373H4 1384600 NM BS 303 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 303.9, STR 16L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084113 1 20080724 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 401WN 29813 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084102 1 20080724 A 5320 6936642 BEAM BOEING 737 7373H4 1384600 NM 178 BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED SPV CHECK, FOUND FWD PRESSURE BULKHEAD VERTICAL BEAM CRACKED AT BS 178, LBL 17. REPAIRED BEAM PER SR M. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084120 1 20080724 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT WING TE FLAP DEBONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 2067 27718 DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD FORE FLAP UPPER SURFACE DSBONDED AT OUTBOARD END. R&R FLAP PER MM. 2 L 7 2 4F RT A16WE 20080818 2008 8 18 SWAA084121 4 20080724 A 2565 D31354433 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. R&R EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084122 1 20080724 A 5330 6545800 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 USAA920081487 1 20080731 A 5320 D53480043205 SILL AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 833AW 1844 SAL-BC4 -MAJOR REPAIR- CORROSION ON LOWER SILL OF R2 DOOR AT FR67, STR 23R, -Y1732. REPAIRED LOWER SILL OF R2 DOOR AT F R67, STR 23R, -1732 IAW A319 SRM 53-41-14. (S) 2 L 7 2 4F RT A28NM 20080819 WP 2008 8 19 UPS08852976 1 20080703 A 5320 FINGER DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2, FLIGHT COMP SUB-FLOOR AREA, BETWEEN STA 8 AND -12 LBL 60 HAS FINGER DOUBLER CORRODED WITH SEVERAL PO PPED RIVETS. REMOVED FINGER DOUBLER,CLEANED SUBFLOOR AREA. FABRICATED AND INSTALLED FINGER DOUBLER. IAW DWG NR 5612298 AND SRM 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 20080819 WP 2008 8 19 UPS08853004 1 20080729 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C1, TWO MOUNT TABS SHEARED THRU ATTACH RIVETS FOR INTERCOSTAL IN COCKPIT SUBFLOOR STA 8 TO -12 BL 0. FA BRICATED AND INSTALLED 2EA REPAIR DOUBLER IAW SRM 53-02-00 FIG 1B 51-1-21. 2 L 7 4 4F RT 4A25 20080819 NM 2008 8 19 UPS08M53031 1 20080721 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 22 LT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED AND INSTALLED RE PAIR BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M53041 1 20080717 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 27 LT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED AND INSTALLED RE PAIR BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 EU 2008 8 19 USAA920081451 1 20080730 A 5540 D5537123500600 HINGE FITTING AIRBUS 320 A320231 3930325 EU RUDDER LOOSE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 627AW 66 SAL-C6-MAJOR REPAIR - EXCESSIVE PLAY ON RUDDER HINGE BEARING NR 4 AT VERTICAL STABILIZER STA 2632 RIB NR 6. REPLACED RU DDER HINGE FITTING NR 4 AT VERTICAL STABILIZER STA 2632 RIB NR6 IAW A320 AMM 55-36-41. (S) 2 L 7 2 4F RT A28NM 20080819 SO 2008 8 19 SWIA200819789 1 20080621 A 6120 7902015 ACTUATOR EMB 120 EMB120ER 3260203 SO PROPELLER FLUCTUATES A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 563SW 11712 8642 120338 NR 2 PROP HAS MINOR FLUCTUATIONS. (FLIGHT NR 3618) REPLACED RT PROP ACTUATOR IAW MM 61-13-04. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 20080819 2008 8 19 SWIA200819894 4 20080720 A 2210 6228315402 COMPUTER EMB 120 EMB120ER 3260203 SO AUTOPILOT MALFUNCTIONED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 227SW 16159 16159 120304 FO`S AUTOPILOT PERFORMED AN UNCOMMANDED ROLL TO THE RT. (FLIGHT NR 5485) REPLACED NR 2 AUTOPILOT COMPUTER AND NR 2 ADI. OPS CHECK GOOD IAW MM 22-10-00 AND 34-21-00. P/N 787-6173-013. S/N OFF 4544. 2 L 7 2 4T RT A31SO 20080822 EU 2008 8 22 F3LA200800382 1 20080623 A 3350 BR964424 LAMP AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE EMERGENCY LIGHT BURNED OUT A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 810FR 3110 DURING A HEAVY MAINT CHECK INSP, NOTED ROWS 3 AND 11 AFT MOUNTED LAMP OF EMERGENCY LIGHT MOUNTED SEATS INOP. MAINT REMOV ED AND REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-19 PAGE BREAK 401. UPON COMPLETION OF THE MAINT IT WAS INSPECTED, FOUND ACCEPTABLE AND THE EMERGENCY LIGHT OPERATIONAL CHECKED GOOD. (A) 2 L 7 2 4F 4 F RT 20080822 NM 2008 8 22 F3LA200800394 1 20080624 A 5321 D5367425000000 FLOORBOARD AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSPECTION NOTED TWO CRACKS FOUND ON FLOORBOARD 161NF DURING REMOVAL. MAINT REPAIRED FLOOR PANEL 161NF I AW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800397 1 20080624 A 5320 D5367314600000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSP, NOTED AFT CARGO PIT FORWARD RT LOWER TRANSITION PANEL 152TG HAS A HOLE AT BOTTOM AFT OF CENTER TIE DOWN CUT OUT. MAINT REPAIRED TRANSITION PANEL 152TG IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS I NSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800378 1 20080620 A 5321 D5367302100000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP NOTED AFT CARGO FLOOR PANEL 151AE HAS CORNER DAMAGE. MAINT REMOVED DAMAGED AREA AND REPAIRED AFT CA RGO FLOOR PANEL 151AE IAW OF SRM 53-02-00. UPON COMPLETIONS OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 EU 2008 8 22 F3LA200800363 1 20080616 A 5320 D5367414400000 PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 941FR 2483 DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151FE HAS SEVERAL PUNCTURES. MAINT REPAIRED PANEL 151FE IAW SRM 53-0 2-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800536 1 20080731 A 5321 D5367223600000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2 2209 DURING C3 C-CHECK, INSP NOTED THE AFT CARGO PIT FLOOR PANEL, 162CF, WAS PUNCTURED IN SEVERAL PLACES. MAINT REPAIRED THE PUNCTURE DAMAGE IN FLOOR PANEL 162CF IAW THE REQUIREMENTS OF SRM 53-02-00 FIGURE 204. MAINT PREPARED AND PAINTED THE F LOOR PANEL IAW THE REQUIREMENTS OF AMM 25-00-00-370-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEP TABLE. (S) 2 L 7 2 4F 4 F RT A28NM 20080822 NM 2008 8 22 F3LA200800539 1 20080728 A 5320 D5348015900700 BLANKING PLATE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2 2209 DURING C-CHECK, INSP NOTED THE R2 AFT GIRT BAR BLANKING PLATE HAD CORROSION. MAINT REMOVED AND REPLACED CORRODED R2 DOO R AFT GIRT BAR FITTING BLANKING PLATE IAW AMM 52-13-31-400-007. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUN D ACCEPTABLE. (S) 2 L 7 2 4F 4 F RT A28NM 20080822 NM 2008 8 22 F3LA200800446 1 20080710 A 5340 D5323099920000 FITTING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE WORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED BEAM NR TWO AT AFT WALL OF FWD CARGO COMPARTMENT MOUNT AND WALL BEAM HAS EXCESSIVE PLAY. MAINT REMOVED AND REPLACED BEAM NR 11 AFT WALL MOUNT FITTING IN THE FWD CARGO BAY IAW SRM 51-72-11 PAGE 1 AND 2. UPON COMPLET ION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800341 1 20080615 A 5321 D5367161400100 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP NOTED CABIN FLOOR PANEL 242FF HAS AREA OF ELIMINATION. MAINT REPAIRED FLOOR PANEL 2422FF IAW SRM 53 -02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 EU 2008 8 22 F3LA200800521 1 20080726 A 5321 D5367407200000 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 808FR 3038 LINE MAINT NOTED THE AFT CARGO COMPARTMENT TRANSITION PANEL 151FH WAS DAMAGED. MAINT REPAIRED TRANSITION PANEL 151FH IA W SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT 20080822 NM 2008 8 22 F3LA200800460 1 20080711 A 5321 D5367424400000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 940FR 2465 DURING C-CHECK INSP NOTED AFT PIT FLOOR PANEL 151CE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COM PLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800520 1 20080727 A 3350 E0062B1A4AD0A SWITCH AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE EMERGENCY LIGHTS FAULTY A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 904FR 33 1579 DURING PRE-FLIGHT INSP, CREW NOTED THE EMERGENCY EXIT AND AISLE LIGHTS WERE ILLUMINATED IN THE ARMED POSITION. MAINT RE MOVED AND REPLACED THE TOGGLE SWITCH AND PERFORMED AN OPS CHECK IAW AMM 33-51-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM 20080822 EU 2008 8 22 F3LA200800523 1 20080726 A 5321 D5367520200400 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 808FR 3038 LINE MAINT NOTED THE AFT CARGO COMPARTMENT FLOOR PANEL 151CH WAS DAMAGED. MAINT REPAIRED FLOOR PANEL 151CH IAW SRM 53-0 2-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT 20080822 NM 2008 8 22 F3LA200800485 1 20080715 A 5320 D5347706800000 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT SMALL PROFILE RT SIDE JUST INSIDE DOOR FWD OF FRAME C56 HAS CORROSIO N. MAINT REMOVED SMALL PROFILE, FABRICATED NEW PROFILE, TREATED, PRIMED AND TOP COATED NEW PROFILE AND INSTALLED IAW SRM 51-21-11, 51-53-11, 51-42-11 AND DRAWING NR D53477068. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTA BLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800510 1 20080722 A 5321 D5367314700000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 942FR 50 2497 DURING C2 C-CHECK, INSP NOTED THE AFT CARGO PIT FWD RT LOWER TRANSITION PANEL 152WG WAS PUNCTURED. MAINT REPAIRED TRANS ITION PANEL 152WG IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM 20080822 NM 2008 8 22 F3LA200800509 1 20080722 A 5321 D5367301800000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE PEELING A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 942FR 50 2497 DURING C-CHECK, INSP NOTED THE PREVIOUS REPAIRS PEELING LOOSE ON THE AFT CARGO PIT FWD LT UPPER TRANSITION PANEL 151UG. MAINT REPAIRED TRANSITION PANEL 151UG IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM 20080822 NM 2008 8 22 F3LA200800518 1 20080722 A 5321 D5367314000000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 942FR 50 2497 DURING C-CHECK, INSP NOTED THE AFT CARGO PIT AFT RT LOWER TRANSITION PANEL 162BF WAS GOUGED AND A PREVIOUS REPAIR WAS PE ELING UP. MAINT REPAIRED TRANSITION PANEL 162BF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPE CTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM 20080822 EU 2008 8 22 F3LA200800427 1 20080707 A 5315 D5347217220400 FLOORBEAM AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 805FR 1660 DURING C-CHECK INSP NOTED FLOORBEAM Y1292 LT HAS CORROSION AT FIRST, SECOND AND THIRD NUTCLIP HOLES. MAINT REMOVED AND R EPLACED FLOORBEAM IAW SRM 51-72-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT 20080820 EA 2008 8 20 SWIA200819857 1 20080709 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE EMERGENCY LIGHT BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 429SW 7518 LOWER EMERGENCY LIGHT BY MAIN CABIN DOOR IS BROKEN. (FLIGHT NR 3810) REPLACED EXIT SIGN ASSEMBLY IAW CRJ 33-51-19. OPS CHECK OK. 2 L 7 2 4F 4 F RT A21EA E15NE 20080820 NM 2008 8 20 SWAA084563 1 20080813 A 5753 6546435238 SKIN BOEING 737 7373Y0 1384671 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP UPPER SURFACE DELAMINATED. R&R FLAP PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084562 1 20080813 A 5753 6546431280 SKIN BOEING 737 7373Y0 1384671 NM T/E FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED HC2 CHECK, FOUND RT WING FORE FLAP UPPER SURFACE DELAMINATED. R&R FLAP PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084555 1 20080817 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084554 1 20080817 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843236 1 20080629 A 5320 6517688165 STRUCTURE BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 CHORD CORRODED. REPLACED CHORD IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843246 1 20080625 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU NR 8 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 NR 8 SPOILER LOWER SURFACE IS DENTED. INSTALLED REPAIR DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 2008 8 20 ASAA0853264 4 20080801 A 3442 6225132633 TRANSCEIVER BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE WEATHER RADAR FAILED A ASAA O OTHER J WARNING INDICATION IN INSP/MAINT 1 NM 02 570AS 2703 35185 PWS FLAGS IN VIEW AS WELL AS WX RADAR RT 'FAIL' DISPLAYED. VERIFIED FAULT. REMOVED & REPLACED WETHER RADAR TRANCIEVER IA W MM 34-43-41. ALSO REMOVED & REPLACED RADAR ANTENNA MOUNT IAW MM 34-43-11. OPS TESTED IAW MM 34-43-00-710-802-001. TEST S OK. ACCOMP GVI FOR INST OF BOTH WXR RT AND ANTENNA. ACCOMP GROUND VERIFICATION FOR WXR TEST PASS. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 NM 2008 8 20 ASAA0843277 1 20080712 A 5313 65C3354712 FITTING BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 STRINGER 16L END FITTING ON THE AFT SIDE OF THE APB HAS A GOUGE MARKS. REMOVED AND REPLACED STRINGER 16L END FITTING IAW SRM 51-40-02, PG 4. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843284 1 20080630 A 5313 6545765168 STRINGER BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 STRINGER 8R IS CRACKED AT NUMEROUS LOCATIONS FROM STA 500, 500A, AND 500B. REMOVED DAMAGED SECTION OF STRINGER, FABBED F ILLER, REPAIR ANGLES AND INSTALLED PARTS IAW SRM 53-00-03, REPAIR 3. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 F3LA200800482 1 20080715 A 2571 D5391408220000 BATTERY BOX AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE WORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP, NOTED AFT BATTERY TRAY OB FWD AND AFT MOUNTS HAVE WEAR. MAINT REMOVED AND REPLACED AFT BATTERY TRA Y, OB FWD AND AFT MOUNTS IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 NM 2008 8 20 SWAA084544 1 20080815 A 3350 101331 LENS BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. R&R LENS PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084526 1 20080817 A 3350 411A2212 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 218WN 32489 R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. R&R LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 F3LA200800412 1 20080702 A 5310 D5347112420100 SHEAR PLATE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 DURING C-CHECK INSP, NOTED LT INTERCOSTGAL WEB UNDER LATERAL SHEAR PLATE AT STRINGER 23 LT FROM FRAME 69 TO FRAME 70 HAS CORROSION ON TOP AND BOTTOM SIDES. MAINT REMOVED CORRODED WEB, DRILLED, TREATED AND PRIMED HOLES AND INSTALLED NEW WEB IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 EU 2008 8 21 F3LA200800359 1 20080616 A 5210 A5211052600000 BUFFER AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE L1 DOOR NO TEST A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 941FR 2483 DURING C-CHECK INSP, NOTED L1 DOOR HOLD OPEN LATCH BUTTON FAILED PRESS TEST. MAINT ADJUSTED L1 DOOR BUFFER IAW AMM 52-1 1-00-820-001 STEP 4J. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800439 1 20080707 A 5330 SKIN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE BS 927 S38L DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 DURING C-CHECK INSP, NOTED LIGHTNING STRIKE BURN MARK BELOW FWD CARGO DOOR STATION 927 AT STRINGER 38. MAINT REPAIRED BY REMOVING BLIND FASTENER COLD WORKING HOLE AND INSTALLING LOCK FASTENER IAW SRM 51-42-11, SRM 51-48-00 AND SRM 53-21-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800370 1 20080619 A 5321 D5367227800200 FLOORBOARD AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED AFT CARGO FLOORBOARD 151GE HAS A DAMAGED EDGE. MAINT REPAIRED FLOORBOARD 151GE IAW SRM 53-02 -00 FIGURE 207. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800331 1 20080611 A 5320 D5347217220500 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED RT CABIN FLOOR SUPPORT Y1162 BETWEEN FRAMES 66 AND FRAMES 68 HAS SEVERAL AREAS OF CORROSION A ND SIX SHEARED RIVET HEADS. MAINT REMOVED AND REPLACED FLOOR SUPPORT Y1162 BETWEEN FRAMES 68 AND FRAME 69 IAW SRM 51-72 -11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 EU 2008 8 21 F3LA200800358 1 20080616 A 5210 A5211052600000 LATCH AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE L2 DOOR NO TEST A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 941FR 2483 DURING C-CHECK INSP, NOTED L2 DOOR HOLD OPEN LATCH BUTTON FAILED PRESS TEST. MAINT ADJUSTED L2 DOOR BUFFER IAW AMM 52-13 -00-820-001 STEP 4J. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 SWAA084394 1 20080806 A 5313 BAC1498 STRINGER BOEING 737 7373Q8 1384670 NM BS 380 S15L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND STRINGER 15L CRACKED AT BS 380. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03721 1 20080705 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1400 S25-27L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 AFT PIT FRAME DENTED STA 1400, STR 25-27L. ACCOMPLISHED MAJOR REPAIR AT GSO. CUT OUT DAMAGE AND INSTALLED DOUBLER RPR PER SRM 53-00-07, RPR 5. VERIFIED DAMAGE REMOVAL PER NDT 51-00-19. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NM 2008 8 21 SWAA084400 1 20080807 A 3350 767 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 298WN 32543 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03698 1 20080702 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1379 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 LIGHTNING STRIKE ON RIVET EDGE AT STA 1379, STR 1. *S/D* DAMAGE FROM LIGHTNING STRIKE. REMOVED DAMAGED FASTENER, A CP HEFC INSP PER NDT MM 51-00-16. NO CRACK FOUND. INSTALLED BLIND FASTENER PER MM 53-30-95. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NM 2008 8 21 SWAA084367 1 20080805 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 650SW 2322 27720 DURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED AT UPPER AND LOWER SURFACE. REMOVED AND REP LACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03081 1 20080529 A 3350 GE209 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT LIGHT INOP AT DOOR 3 RIGHT FWD SILL LIGHT. *S/D* FOUND BURNED OUT LAMP. REPLACED LAMP OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080821 NM 2008 8 21 2008UALA03753 1 20080705 A 3397 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 EEL FEEDER AT STA 1075, SEAT ROW 18 DAMAGED. FEEDER ASSY DAMAGED, UNKNOWN. REPLACED FEEDER ASSY, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080815 EU 2008 8 15 08FDEA02640 1 20080703 A 5210 A52111339202 LONGERON AIRBUS 310 A310222 3930315 EU PAX DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 LT PAX/CREW DOOR LONGERON POSITION NR 2 WITH MILD/EXFOLIATION CORROSION BETWEEN FR15A-16. REMOVED CORROSION PER SRM 51- 74-10. APPLIED ALODINE TO THE REWORKED AREA PER SRM 51-21-10. MEASURED REMAINING THICKNESS PER NTM 51-10-04. THE ORI GINAL THICKNESS IS 0.063 INCH PER DWG:A52111307 ALLOWABLE DAMAGE IS 20 PERCENT PER SRM 52-10-00. EXCEEDED LIMIT. CUT O UT THE CORRODED AREA AND DEBURR THE CUT EDGES PER SRM 52-10-00. FABRICATED THE REPAIR PART PER SRM 52-10-00. DRILLED F ASTENER HOLES TO THE REPAIR PART PER SRM 51-40-50. APPLIED ALODINE TO THE REPAIR PART PER SRM 51-21-10. APPLIED PRIMER TO THE REPAIR PART PER SRM 51-75-10. INSTALLED THE REPAIR PART PER SRM 51-40-21. APPLIED FINISH PER SRM 51-75-10. 2 L 7 2 4F RT A35EU 20080815 EU 2008 8 15 08FDEA02641 1 20080703 A 5320 A53610792731 FLOOR SUPPORT AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 456FE 318 FR 12 - FR 12A Y1456 LONGERON FOR SUPPORTING OF MAIN DECK FLOOR CORRODED. REPAIRED THE DAMAGE PER EA NR 5310-117358. 2 L 7 2 4F RT A35EU 20080815 WP 2008 8 15 08FDEA03013 1 20080722 A 5100 NONE DOUG DC10 DC1030F 3023504 WP NOT AN SDR NONE A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 318FE 46837 FWD CARGO COMPARTMENT STRUT SUPPORT BEAM NOT IN CONFIGURATION. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 08FDEA03029 1 20080723 A 5414 AUB710813 SKIN DOUG MD10 MD1010F 3022112 WP NACELLE DOOR CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 NR 1 PYLON PANEL 437 LL IS CHAFED AT THE FASTENER HOLES. BLENDED AREA IAW DC/MD-10 SRM 54-00-01, VOL I, FIG 1-A. ORIGI NAL MATERIAL THICKNESS 0.071 IAW DC/MD-10 SRM 54-51-0 AND FOUND TO BE OUT OF LIMITS 54-00-01, VOL I, FIG 1-A. UT GAUGE USED IS T8225P. MATERIAL ID THE PANEL IS 7075-T6, 0.071, PO 623403.4 AND THE FILLER IS 2024-T3, 0.016, PO 346313.2 IN REF TO DAC DWG AUB 7108, REV AN. FABRICATED THE PANEL AND FILLER IAW DAC DWG AUB 7108, REV AN. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01, VOL II, PGS 21-24. ASSEMBLED PANEL IAW DAC DWG AUB 7108, REV AN. PART MARKED PANEL IAW FEDEX G MM 7-0-1001. 2 L 7 3 4F RT A22WE 20080815 WP 2008 8 15 UPS08852686 1 20080707 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 CORROSION RT LWR FUSE AFT OF THE E&E DOOR APPROX. STA 70. STARTED ECA FORM 011382. INSTALLED TIME LIMITED REPAIR IAW EO DC8-5330-29905A. ALL WORK PERFORMED ON ECA FORMS 011382 AND 011385. REPAIR DEFERRED FOR 24 MONTHS. 2 L 7 4 4F RT 4A25 20080815 NM 2008 8 15 UPS08M52917 1 20080717 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 35 RT BARREL NUT BORE HOLE REMOVED CORROSION, FABRICATED BUSHING AND INSTA LLED BUSHING IAW EO MD11-5510-19409-N AND SAA TRAVELER 80538710001. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52926 1 20080712 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 5 LT BARREL NUST BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND IN STALLED BUSHING IAW EO, MD11-5510-19409-N AND SAA TRAVELER 80538370001. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52927 1 20080710 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 8 LT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING AND INST ALLED BUSHING IAW EO, MD11-5510-19409-N AND SAA TRAVELER 80538360001. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52930 1 20080712 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 20 LT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED BUSHING, AND INS TALLED BUSHING IAW EO MD11-5510-19409-N AND SAA TRAVELER 80538480001. 2 L 7 3 4F RT A22WE 20080815 NM 2008 8 15 UPS08M52858 1 20080602 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE-C, RT HORIZ STAB BARREL NUT BORE NR 22 FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED IAW SRM 51- 21-01 VII REV 35. BORE REAM TO 1.067" DIA, REMAINING BLEND OUT 0.040" DEEP, BOTTOM SURFACE REMAINING BLEND OUT 0.055" D EEP, BORE BLEND OUT EXCEED EO LIMITS IAW EO MD11-5 510-19409M.10X MAGN DVI C/O & FOUND NO CORROSION EVIDENT. REPAIRED B/ N BORE NR 22 RT WAS ACCOMP IAW EN1253-08 & IS ACCEPT IAW MD11-5510-30011A. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 UPS08552876 1 20080706 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 457UP 25478 INSPECTION TYPE-C2, CORROSION ON UPPER SURFACE OF FLOOR SUPPORT, BS 1055 RBL 27,WL 208. DAMAGE WAS OUT OF LIMITS, FABRI CATED NEW FLOOR SUPPORT AND INSTALLED. 2 L 7 2 4F RT A2NM 20080818 WP 2008 8 18 UPS08852622 1 20080612 A 5340 37540152 FITTING DOUG DC8 DC871F 302199D WP BS 390 L21R DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, RT FWD TYPE 1 DOOR, FWD LWR JAMB BELT FRAME END FITTING HAS DOUBLE DRILLED HOLES STA 390 L-21R. RE MOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-1-21,AND 51-01-2. 2 L 7 4 4F RT 4A25 20080818 NM 2008 8 18 UPS08552612 1 20080629 A 2560 ESCAPE REEL BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 441UP 27386 EMERGENCY ESCAPE REEL NR3 INOP. REMOVED AND REPLACED NR 3 EMERGENCY DESCENT DEVICE. 2 L 7 2 4F RT A2NM 20080818 WP 2008 8 18 UPS08852637 1 20080613 A 5340 ATTACH FITTING DOUG DC8 DC871F 302199D WP FS 1260 L15R MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, CABIN BS 1260 L15R, INTERCOSTAL CLIP MISSING FABRICATED AND INSTALLED CLIP IAW SRM 53-04-01 FIG 051, AND 51-1 -20D. 2 L 7 4 4F RT 4A25 20080818 NM 2008 8 18 UPS08M52629 1 20080407 A 5720 DUCT DOUG MD11 MD11F 3023600 NM LT WING CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE-C, LT WING ANTI-ICE TELESCOPIC DUCT LOWER DOOR FWD AREA FOUND CHAFING MARK. LT WING ANTI-ICE TELESCOPIC DUCT LWR DOOR PANEL REMOVED IAW AMM 20-50-02R53. CHAFING MARK REMOVED FOUND EXCEED LIMIT IAW SRM 57-00-01 VIR 35. NEW P ANEL FABRICATED IAW DWG ARM 0078. HEAT TREAT TO T62 IAW DPS7.00-1 HRB 75.4 IS ACCEPTABLE LIMITS IAW DPS1.05-3. FASTENER HOLES PICKUP IAW SRM 51-31-01VII R35. PROTECTED & PAINTED IAW SRM51-21-01VII R35. INSTALLED IAW AMM 20-50-03R53. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 UPS08M52630 1 20080326 A 5753 BUSHING DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE-C, LT WING IB FLAP OB HINGE PIVOT POINT OB LUG BUSHING FOUND CORRODED. CORROSION REMOVED EXCEED LIMIT CMM 57-52-03PG442-444R60 ORIG DIA 1.187" FINAL 1.258" MAX ALLOWABLE 1.220". FPI C/O NDT SPM R13PT8 NO CORROSION EVIDENT. AREA PROTECTED & PAINTED, BUSHING FABRICATED IAW EN1179-08. HEAT TREAT DPS 5.00- 2 HRC 43.7 IAW DPS1.05-5. MPI C/O NDT SPM R13PT7 ON BUSHING NO CRACK. BUSHING CAD PLATED & INSTALLED ON EN1179-08. 2 L 7 3 4F RT A22WE 20080818 WP 2008 8 18 UPS08852658 1 20080614 A 5340 ATTACH BRACKET DOUG DC8 DC871F 302199D WP BS 690 L17L DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, CABIN STA. 690 LONG 17L INTERCOSTAL ATTACH BRACKET HAS DRILL START. REMOVED, FABRICATED AND INSTALL ED NEW "T" SUPPORT ANGLE IAW SRM 53-2-0 FIG 1F, DWG 3768038, 51-01-20D. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852660 1 20080612 A 5220 FRAME DOUG DC8 DC871F 302199D WP EMERGENCY EXIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, RT FWD TYPE 1 EMERGENCY EXIT DOOR HAS CRACKED FRAME IN 2 PLACES, IB & OB ENDS OF DOOR TORQUE TUBE. REMOVED, FABRICATED, AND INSTALLED 2 REPLACEMENT WEBS IAW SRM 52-02 -00 FIG2, 51-01-21, AND 52-07-01. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852661 1 20080612 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, FLOOR PANEL F87 HAS 3 EA SCREW HOLES CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED 2EA. DOUBLER S IAW SRM 53-2-3 FIG 010, AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 20080818 NM 2008 8 18 08FDEA02970 1 20080718 A 5347 601096418 SEAT TRACK DOUG MD10 MD1030F 3024020 NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 303FE 46802 MAIN CABIN SEAT TRACK IS DAMAGED AT SEVERAL AREAS FROM STATION 1629 TO 1661 AT RBL 27 BLENDED SEAT TRACK AT STATIONS 162 9 - 1651 RBL 27 FOUND TO BE IN LIMITS (ORIGINAL THICKNESS .145, AFTER REWORK .140) IAW SRM 53-70-00 FIG 5. BLENDED SEAT TRACK AT 1661 FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 FIG 5. CUT OUT DAMAGED SECTION, FABRICATED NEW SEAT TRACK SEC TION, SPLICE HAT/PLATE. INSTALLED NEW TRACK AND REPAIR PARTS REMOVED AND REINSTALLED FLOOR PANELS ALL IAW TRAVELERS T8/ 748751, T8/748710, T8/749337, SRM 53-70-00 FIG 1 AND SRM 51-31-01. REPAIR IS CLASSIFIED AS A MAJOR REPAIR, REPORTABLE D ISCREPANCY AND RII. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 SWAA084024 1 20080718 A 5552 65C2688427A TAB BOEING 737 7373H4 1384600 NM LT ELEVATOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 397SW 27691 DURING SCHEDULED MV1 CHECK, FOUND LT ELEVATOR TRIM TAB ROD END LOOSE. R&R ELEVATOR TAB PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084042 1 20080718 A 5210 STRUCTURE BOEING 737 7373H4 1384600 NM PAX DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 001052 27713 DURING SCHEDULED HC1 CHECK, FOUND FWD ENTRY DOOR CRACKED AT LOWER STOP MOUNT. R&R DOOR PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084118 1 20080724 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080819 EA 2008 8 19 SWIA200819897 1 20080723 A 3350 SIGN CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* 30015 NE EMERGENCY LIGHT INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 614SK 10051 EMERGENCY EXIT SIGN AT PAX DOOR IS INOPERATIVE. (FLIGHT NR 3951) REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-51-05. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA 20080819 2008 8 19 USAA920081448 4 20080729 A 2210 SC47003 YAW DAMPER AIRBUS A319 A319112 3930323 EU LEFT LEAKING A USAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 EA 19 766US 24845 2008 1378 FLT 1740 BUF-PHL - EMERGENCY LANDING - ON APPROACH FROM BUF TO PHL, CREW STATED LOSS OF GREEN HYDRAULIC SYSTEM. ACFT LA NDED SAFELY AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE REMOVED AND REPLACED THE LT YAW DAMPER ACTUATOR. O PERATIONAL AND LEAK CHECKS WERE GOOD. (S) 2 L 7 2 4F RT A28NM 20080819 EA 2008 8 19 REX2008F00029 1 20080812 A 3234 75005000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG MALFUNCTIONED A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 8672A 7672 ON CLIMBOUT RECEIVED GEAR DISAGREE. QRH FOLLOWED, DECLARED EMERGENCY AND RETURNED TO AIRPORT WITH UNEVENTFUL LANDING. MAINTENANCE INSPECTED ACFT AND REPLACED THE MAIN LANDING GEAR SELECTOR VALVE. PERFORMED OPERATIONAL CHECKS PER BOMBARDI ER AMM. (S) 2 L 7 2 4F RT A21EA 20080819 EA 2008 8 19 REX2008F00022 1 20080729 A 3297 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA WEIGHT ON WHEELS NOT SEATED A REXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 813AY 8013 WEIGHT ON WHEEL INPUT CAUTION MESSAGE IN CRUISE, QRH FOLLOWED. MESSAGE WENT AWAY ON ITS OWN ONLY TO LATER RETURN IN FLI GHT. QRH FOLLOWED, DIVERTED TO MEM WITH UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ACFT AND FOUND A WOW HARNESS CON NECTOR NOT COMPLETELY LOCKED. CONNECTOR SECURED, OPERATIONAL CHECKS PERFORMED PER BOMBARDIER AMM. (S) 2 L 7 2 4F RT A21EA 20080819 WP 2008 8 19 UPS08852993 1 20080730 A 5753 SKIN DOUG DC8 DC871F 302199D WP RT WING TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1, RT WING OB FLAP STA XF 228 HAS EXISTING REPAIR DOUBLER GOUGED AT UPPER FLAP SKIN, NEXT TO AFT FIXED PANEL OF FLAP HINGE COVER REMOVED EXISTING DOUBLER FABRICATED AND REPLACED REPAIR DOUBLER IAW SR M 51-1-21A, 57-2-8 FIG 2A,57-7-01 FIG 4, AND 51-3-0. 2 L 7 4 4F RT 4A25 20080819 SO 2008 8 19 SWIA200819904 1 20080725 A 5210 FITTING EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE PAX DOOR DIRTY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 224SW 120294 MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN. (FLIGHT NR 3614) INSPECTED AND CLEANED MAIN CABIN DOOR FITTINGS AND OPERATED DOOR MULTIPLE TIMES. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 20080819 SO 2008 8 19 RAIA00808003 1 20080803 A 3244 31690 TIRE EMB 145 EMB145LR 3260212 SO RT MLG SEPARATED A RAIA A UNSCHED LANDING E M VIBRATION/BUFFET OVER TEMP CL CLIMB 1 CE 03 832HK 145771 FLT 7949 -DEN- CREW REPORTED FEELING VIBRATION AS GEAR WAS RETRACTED AND A FLAP FAIL MESSAGE AT 9 DEGREES. IN ADDITION, ON LANDING THE NR 1 BRAKE TEMP INDICATION SHOWED AN OVERHEAT. MAINTENANCE INSPECTED AND FOUND THE NR 2 MLG WHEEL`S TRE AD SEPARATED. MAINTENANCE REMOVED AND REPLACED THE RT MLG WHEEL ASSEMBLIES AND THE NR 1 BRAKE ASSEMBLY. AN OPERATIONAL CHECK OF THE FLAP SYSTEM WAS GOOD. (S) 2 L 7 2 4T RT T00011AT 20080819 EA 2008 8 19 RAIA00808002 2 20080801 A 7200 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO RROYCE AE3007 AE3007A1 54165 EA MALFUNCTIONED A RAIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 03 834HK 145269 310166 FLT 7945 -SGF- CREW REPORTED THAT THE N2 OF THE NR 1 ENG WAS AT 102.3 PERCENT AND THAT THE VIBE WAS CLIMBING TO THE TOP OF THE GREEN. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENG. (S) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080819 EA 2008 8 19 SWIA200819906 1 20080726 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 961SW 7857 AFT CEILING EMERGENCY POD LIGHT IS NOT WORKING. (FLIGHT NR 5929) RELAMPED AFT CEILING EMERGENCY LIGHT PER 33-21-01. OP S CHECK GOOD. 2 L 7 2 4F RT A21EA 20080819 NM 2008 8 19 UPS08M53019 1 20080710 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 11 LT BARREL NUT BORE HOLE REMOVED CORROSION, FABRICATED BUSHING AND INSTA LLED BUSHING IAW E.O. MD11-5510-19409-N AND SAA TRAVELER 80538350001. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M53032 1 20080721 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 25 LT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED AND INSTALLED R EPAIR BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 WP 2008 8 19 NWAA083359928 1 20080710 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8921E 45836 DURING L-CHECK FOUND CRACK IN FUSELAGE SKIN AT LOWER CORNER OF FORWARD CARGO DOOR JAMB. REPAIRED PER EA 99-213625. (S) 2 L 7 2 4F A6WE 20080819 NM 2008 8 19 UPS08M53021 1 20080715 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 6 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INST ALLED BUSHING IAW E.O. MD11-5510-19049-N AND SAA TRAVELER 80538530001. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08553056 1 20080630 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM BS 1015 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 INSPECTION TYPE-2C, CORROSION ON TOP OF FLOORBEAM INTERCOSTAL BS 1015, LBL 25 TO LBL 45, WL 207. REMOVED AND REPLACED I NTERCOSTAL IAW SRM 51-40-02-00. 2 L 7 2 4F RT A2NM 20080819 SO 2008 8 19 SWIA200819874 1 20080503 A 5310 DOOR FRAME EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 PAX DOOR UPPER CORNER FRAME CRACKED. (FOUND AT C-CHECK) REPLACED UPPER FRAME IAW SRM 51-10-02. 2 L 7 2 4T 4 T RT A31SO E20NE 20080819 WP 2008 8 19 NWAA083639852 1 20080803 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 761NC 47709 DURING LINE CHECK, MAINTENANCE FOUND THE EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTE RY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (S) 2 L 7 2 4F RT A6WE 20080819 SO 2008 8 19 SWIA200819875 1 20080503 A 5520 BEARING EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE RT ELEVATOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 RT ELEVATOR TRIM TAB BEARING IS CORRODED. (FOUND AT C-CHECK) REPLACED RT TRIM TAB HINGE BEARING IAW MM 55-22-00. 2 L 7 2 4T 4 T RT A31SO E20NE 20080819 SO 2008 8 19 SWIA200819876 1 20080503 A 2497 WIRE EMB 120 EMB120ER 3260203 SO RCCB DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 EMERGENCY BUSS CONTACTOR 2 AND GASPER FAN RCCB HAS DISCOLORED WIRING. (FOUND AT C-CHECK) REPLACED CONTACTORS AND WIRING IAW EMB 120 24-00-00. 2 L 7 2 4T RT A31SO 20080819 EU 2008 8 19 MAL2008F00020 1 20080730 A 5753 FLAP SAAB SF340 340B 7860101 EU WING DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 RT FLAP HAS A DENT AT WS 42.4, TOP INBOARD EDGE. REPAIRED IAW EOS51031. THIS EO PROVIDES A GENERIC COLD BOLD (WET LAYU P) REPAIR IAW SAAB SRM 51-70-50. (S) 2 L 7 2 4T RT A52EU 20080819 EA 2008 8 19 SWIA200819864 1 20080711 A 5210 CAM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 417SW 7400 THE PASSENGER DOOR WILL NOT OPEN OR CLOSE. (FLIGHT NR 2531) CLEANED AND INSPECTED PAX DOOR MECHANISM AND CAMS. CYCLED DOOR SEVERAL TIMES. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080819 2008 8 19 ANCF200800018 4 20080728 A 3497 WIRE DOUG DC9 DC983 3022083 WP BROKEN A ANCF O OTHER J WARNING INDICATION CL CLIMB 1 SO 23 161BS 53464 AIR TURNBACK, MALFUNCTION, DURING CLIMB AT 14000 FT A/P DISCONNECTS AND F/D MALFUNCTIONS CAME AGAIN. FD BOTH ON 2 WAS S ELECTED AND SWITCHED TO DFGS NR 2 AND MALF, COME AGAIN, AT 2900 FT BOTH FMA S GOES BLANK AND A/P AND ALT FUNCTION WERE L OST. DURING APP WINDSHEAR INOP ANNUN WERE ON, ON THE EOAP. IAW WDM 34-22-11/506 SH 3-4 THE EFIS SYSTEM WIRING WAS CHEC KED BETWEEN THE F/O PFD AND SYMBOL GENERATOR 2 AND WAS FOUND IN GOOD CONDITION. IAW WDM 34-24-02/566 THE LINE 2F302T24N B IN TB G30-18 WAS FOUND BROKEN AND IT WAS REPAIRED. IAW AMM 22-01-05/210 THE RETURN TO SERVICE TEST WAS ACCOMPLISHED S ATISFACTORY. (S) 2 L 7 2 4F RT A6WE 20080819 EA 2008 8 19 SWIA200819867 1 20080715 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 427SW 14970 14970 7497 NOSE GEAR WOULD NOT EXTEND. CYCLED GEAR AGAIN TO GET THREE GREEN INDICATIONS. (FLIGHT NR 3803) REPLACED NOSE GEAR HYDR AULIC SELECTOR VALVE IAW MM 32-33-10. ALL OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 20080819 NM 2008 8 19 ASM2008F00000 1 20080806 A 3150 WARNING SYSTEM BOEING 777 7772Q8 1385238 NM COCKPIT MALFUNCTIONED W ASMF C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 23 746AM 32719 ACFT REJECTED TAKEOFF AT 80 KNOTS DUE TO THE E/E COMPARTMENT LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED DOOR LIGH T TEST IAW MM 62-71-00, ALL CORRECT. THE HIGH ENERGY STOP INSPECTION WAS PERFORMED IAW MM 05-51-14, ALL CORRECT. (S) 2 L 7 2 4F RT T00001SE 20080819 NM 2008 8 19 UPS08553012 1 20080730 A 5420 BRACKET BOEING 757 75724APF 1384969 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 INSPECTION TYPE-C2, BRACKET IS CRACKED IN THE NR 2 ENG PYLON HYD BAY, OB SIDE AT FWD LWR CORNER OF PANEL 445AR CUTOUT, N AS STA 208. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02-0G. 2 L 7 2 4F RT A2NM 20080821 NM 2008 8 21 2008UALA03272 1 20080608 A 4900 263BA1011 BATTERY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 775UA 26947 APU BATTERY CHARGING 62 AMPS, POPPED CB. *S/D* SUSPECT FAULTY BATTERY AND CHARGER. REPLACED APU BAT AND CHARGER REF M M 24-31-05 AND 24-31-06. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080821 NM 2008 8 21 2008UALA03360 1 20080613 A 2133 20224785 MOTOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE OUTFLOW VALVE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 672UA 30027 CABIN ALT AUTO 1 STATUS MSG. *S/D* AFTER TROUBLESHOOTING FOUND OUT FLOW VALVE MOTOR TO BE FAULTY. REPLACED NR 1 (AFT) AC OUTFLOW VALVE MOTOR PER MM 21-31-05, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080821 NM 2008 8 21 2008UALA03361 1 20080611 A 2120 CD01109F2 FILTER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN AIR DIRTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 209UA 30215 EQUIPMENT COOLING FAN WARNING HORN KEEPS GOING OFF. *S/D* SUSPECT DIRTY FILTER. REPLACED FILTER, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080822 NM 2008 8 22 F3LA200800417 1 20080703 A 5320 D5347034820000 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE EMERGENCY LIGHT CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT CENTER FLOORBEAM BETWEEN FRAME C60 AND FRAME C61 HAS CORROSION. MAINT RE MOVED AND REPLACED FLOORBEAM BETWEEN FRAME C60 AND FRAME C61 IAW REQUIREMENTS OF SRM 51-72-11. UPON COMPLETION OF THE RE PAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 EU 2008 8 22 F3LA200800385 1 20080623 A 3250 C247361001 SERVO CONTROL AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE NLG STEERIN INOPERATIVE A F3LA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 03 806FR 2218 DURING TAXI OUT, THE FLIGHT CREW RECEIVED A NOSE WHEEL STEERING FAULT AND LOSS OF STEERING. MAINT REMOVED AND REPLACED NLG STEERING SERVO CONTROL VALVE IAW AMM 32-51-51 PAGE BREAK 401. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOU ND ACCEPTABLE AND OPERATIONAL CHECKED GOOD. (A) 2 L 7 2 4F 4 F RT 20080822 EU 2008 8 22 F3LA200800440 1 20080709 A 2120 UNKNOWN AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE GALLEY ODOR A F3LA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 941FR 48 2483 DURING TAXI THE F/A NOTICED A FAINT ODOR FOR A DURATION LESS THAN FIVE SECONDS. DURING TAKEOFF ROLL THE F/A NOTICE THAT SAME DOOR AGAIN. THE ODOR WAS LOCATED IN THE AFT GALLEY ON THE LT SIDE OF THE ACFT. NO OTHER OCCURANCES WERE NOTED FOR T HE DURATION OF THE FLIGHT. MAINT PERFORMED AN AIR QUALITY TEST IAW TSM 21-00-00-810-802. THE AC WAS INSPECTED AND NO SO URCE OF ODOR WAS LOCATED AND THE AC CONTINUED SERVICE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800516 1 20080722 A 5321 D5367303600000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 942FR 50 2497 DURING C-CHECK, INSP NOTED THE AFT CARGO PIT AFT LT UPPER TRANSITION PANEL 161CF WAS PUNCTURED IN THE CENTER, COVERED WI TH TAPE. MAINT REPAIRED TRANSITION PANEL 161CF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPE CTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM 20080822 NM 2008 8 22 F3LA200800511 1 20080722 A 5321 D5367302000000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 942FR 50 2497 DURING C2 C-CHECK, INSP NOTED THE AFT CARGO PIT FWD LT UPPER TRANSITION PANEL 151BE WAS PUNCTURED. MAINT REPAIRED TRANS ITION PANEL 151BE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM 20080822 NM 2008 8 22 F3LA200800437 1 20080707 A 5330 SKIN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 DURING C-CHECK INSP NOTED LIGHTNING STRIKE BURN MARK BELOW FWD CARGO DOOR STATION 979 AT STRINGER 38. MAINT REMOVED AND REPLACED BLIND FASTNER WITH HI-LOCK AFTER COLD WORKING HOLE AT STATION 979 STRINGER 38 IAW SRM 53-21-11 FIGURE 210. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800434 1 20080707 A 5321 D5367302000000 FLOORBOARD AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT FLOORBOARD 151BE HAS A PUNCTURE IN IT. MAINT CLEANED, PREPPED AND REPAIR ED FLOORBOARD 151BE IAW SRM 53-02-00 PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND A CCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 EU 2008 8 22 F3LA200800522 1 20080726 A 5321 D5367520200600 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 808FR 3038 LINE MAINT NOTED THE AFT CARGO COMPARTMENT FLOOR PANEL 151DH WAS DAMAGED. MAINT REPAIRED FLOOR PANEL 151DH IAW SRM 53-0 2-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT 20080822 NM 2008 8 22 F3LA200800517 1 20080722 A 5321 D5367303801000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 942FR 50 2497 DURING C-CHECK, INSP NOTED THE AFT CARGO PIT AFT LT LOWER TRANSITION PANEL 161BF WAS PUNCTURED. MAINT REPAIRED TRANSITIO N PANEL 161BF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM 20080822 NM 2008 8 22 F3LA200800456 1 20080711 A 5320 D5367402800000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 940FR 2465 DURING C-CHECK INSP NOTED AFT PIT PANEL 151DE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800458 1 20080711 A 5321 D536714700000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 940FR 2465 DURING C-CHECK INSP NOTED AFT PIT PANEL 152WG DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080819 SO 2008 8 19 SWIA200819915 1 20080714 A 2710 CONTROL CABLE EMB 120 EMB120ER 3260203 SO AILERON STIFF A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 576SW 120345 AILERON CONTROLS FEEL STIFF IN FLIGHT. (FLIGHT NR 5536) ADJUSTED LT AND RT AILERON TENSIONS IAW MM 27-00-00. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080819 SO 2008 8 19 SWIA200819916 1 20080731 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 565SW 120340 CAPTAINS WINDSHIELD CRACKED. (FLIGHT NR 3620) REPLACED LT WINDSHIELD IAW AMM 56-10-01. OPS AND LEAK CHECK GOOD. P/N: NP-151311-1 S/N OFF: 97204H1888 2 L 7 2 4T RT A31SO 20080819 2008 8 19 SWIA200819917 3 20080802 A 6110 O-RING EMB 120 EMB120ER 3260203 SO TRANSFER TUBE DAMAGED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 297SW 120327 RT ENGINE NP SURGED AFTER TAKE-OFF. (FLIGHT NR 5702) REPLACED TRANSFER TUBE O-RINGS AND ADJUSTED PCU IAW AMM 61-10-02. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080819 WP 2008 8 19 UPS08853013 1 20080727 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1746 L16L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C1, MAIN CABIN, L16L CRACKED AT BS 1746 CANT FRAME, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTI ON IAW SRM 53-02-02 FIG 10,51-01-20D,51-03-01. 2 L 7 4 4F RT 4A25 20080819 NM 2008 8 19 UPS08M53022 1 20080715 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 9 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INSTALL ED BUSHING IAW E.O. MD11-5510-19409-N AND SAA TRAVELER 80538540001. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M53023 1 20080716 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 6 LT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED RE PAIR BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 EA 2008 8 19 SWIA200819886 1 20080717 A 5210 FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 417SW 7400 MAIN CABIN DOOR IS HARD TO OPEN. (FLIGHT NR 2813) ADJUSTED BOTH MAIN CABIN DOOR SPIGOT FITTINGS. OPS CHECK GOOD IAW 52 -00-00. 2 L 7 2 4F RT A21EA 20080819 NE 2008 8 19 ASM2008F00001 2 20080803 A 7230 BLADE BOEING 777 7772Q8 1385238 NM GE GE90 GE9094B 30045 NE RT ENGINE BENT W ASMF K NONE O OTHER IN INSP/MAINT 1 SW 23 776AM 20975 20975 28692 900364 DURING TRANSIT CHECK, THE MAINTENANCE PERSONNEL PERFORMED A BOROSCOPIC INSPECTION DETECTING BLADES TIP BENDED IN THE FIR ST STAGE OF HIGH PRESSURE COMPRESSOR ROTABLE SECTION AND A IGV SCRATCHED IN THE RT ENG, OUT OF LIMITS IAW MM 72-00-00. THE RT ENG WAS REPLACED AND TESTED IAW MM 71-00-02 AND 71-00-00, ALL CORRECT. 2 L 7 2 4F 4 F RT T00001SE E00049EN 20080819 SO 2008 8 19 SWIA200819872 1 20080717 A 3397 RELAY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT MALFUNCTIONED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 288SW 120316 WITH EMERGENCY LIGHTS IN THE ARM POSITION, LIGHTS STAY ILLUMINATED. (FLIGHT NR 5728) REPLACED RELAY K0201. OPS CHECK G OOD. 2 L 7 2 4T RT A31SO 20080819 EU 2008 8 19 UPS08153043 1 20080805 A 5321 B5327077600100 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CARGO BAY PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 153UP 0839 INSPECTION TYPE:5 YR, MAIN CARGO COMPT FLOOR PNL APPROX FR26 IN AFT CABIN HAS PUNCTURE. REPAIRED MAIN CABIN FLOOR PNL, NR 252WJ REF SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20080819 EU 2008 8 19 UPS08153044 1 20080717 A 5321 B5317075600000 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CARGO DECK DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 153UP 0839 INSPECTION TYPE:5 YR, MAIN CARGO DECK POS P4R, FLOOR INTERIM REPAIR. REPAIRED MAIN CABIN FLOOR PNL NR 241LH REF SRM 53-10-20, TABLE 201, PARA 8A. 2 L 7 2 4F RT A35EU 20080819 EU 2008 8 19 UPS08153055 1 20080808 A 2780 COMPUTER AIRBUS A300 A300F4622R 3930360 EU NR 2 INOPERATIVE A IPXA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 166UP 0805 AFTER TAKEOFF FLAPS STARTED RETRACTING AND ECAM MESSAGE CAME UP, FLT CTR FLAPS SYS 2 FAULT. RAN QRH PROCEDURE AND CYCLE D FLAPS. FLAPS STAYED STUCK AND WOULD NOT EXTEND. IN ADDITION, BROKE SAFETY ON FLAP OVRD TO POSITION SYSTEM TO "OFF". ATC DECLARED EMERGENCY. T/S IAW TSM 27-50-00 TO AT 3 SLAT/FLAP CONTROL COMPUTER. R&R NR 2 SFCC IAW MM 27-51-18-4 AND CHECKED IAW MM 27-51-00. ALL CHECKS NORMAL. RAN FLAPS SEVERAL TIMES WITH ENGINES RUNNING. 2 L 7 2 4F RT A35EU 20080819 NM 2008 8 19 UPS08553003 1 20080730 A 5320 SUPPORT BOEING 757 75724APF 1384969 NM BS 620-645 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 INSPECTION TYPE-C2, FWD CARGO COMPARTMENT RT FLOOR TO SIDEWALL SUPPORT IS CORRODED AT TIE DOWN FITTINGS, BS 620 TO 645. 5 REMOVED AND REPLACED IAW SRM 51-40-02-0G, MFG DRG NR 143N5366. 2 L 7 2 4F RT A2NM 20080819 NM 2008 8 19 UPS08553009 1 20080730 A 5320 SUPPORT BOEING 757 75724APF 1384969 NM BS 765-845 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 INSPECTION TYPE-C2, FWD CARGO COMP, RT FLOOR TO SIDEWALL SUPPORT IS CORRODED AT TIE DOWN FITTINGS BS 765.5 TO 845. REM OVED AND REPLACED IAW SRM 51-40-02-0G; DRW NR 143N5366. 2 L 7 2 4F RT A2NM 20080819 NM 2008 8 19 UPS08553059 1 20080730 A 5320 SUPPORT BOEING 757 75724APF 1384969 NM BS 765-845 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 INSPECTION TYPE-2C, FWD CARG COMP. RT FLOOR TO SIDEWALL SUPPORT IS CORRODED AT TIE DOWN FITTINGS BS 765.5 TO 845. REMOV ED AND REPLACED IAW SRM 51-40-02-0G; DWG NR 143N5366. 2 L 7 2 4F RT A2NM 20080819 SO 2008 8 19 SWIA200819929 1 20080707 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 298SW 120328 CENTER FRAME UNDER FLOOR BOARD AT ROW 10 HAS SURFACE CORROSION. (FOUND AT C-CHECK) REPLACED CENTER FRAME UNDER FLOOR BO ARD AT ROW 10 IAW SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 20080819 NM 2008 8 19 UPS08553060 1 20080802 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 820 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 INSPECTION TYPE-C2, WHILE WORKING FWD CARGO COMP FRAME AT BS 820 BETWEEN STR 246 & 256 MISDRILLED FRAME AT STR 26L. C UT OUT DAMAGE AND SPLICED IN REPAIR FRAME SECTION. 2 L 7 2 4F RT A2NM 20080819 NM 2008 8 19 UPS08M53038 1 20080722 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP INSPECTION TYPE-1C, FOUND CORROSION IN NR 22 RT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 SO 2008 8 19 C2XA08CL092 1 20080805 A 4920 M4504113A APU EMB 135 EMB135ER 3260203 SO APU BAY FAULTY A C2XA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 27506 9308 9308 145206 CLE FLIGHT 2630 - THE CREW REPORTED A LAV SMOKE WARNING MESSAGE ON THE EICAS AFTER SELECTING COOLING PACKS DURING TAXI. THE ACFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE APU. OPERATIONAL CHECK S WERE GOOD. (S) 2 L 7 2 4F RT T00011AT 20080819 SO 2008 8 19 C2XA08RI104 1 20080719 A 3213 BOLT EMB 145 EMB145LR 3260212 SO MLG STRUT SHEARED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12540 2700 1147999005 145537 DURING INSTALLATION OF MAIN LANDING GEAR OLEO STRUT ASSEMBLY, UPPER ATTACHMENT BOLT SHEARED AT TORQUE BELOW 1200 IN LBS. RIC MX REMOVED AND REPLACED UPPER ATTACHMENT BOLT, APPLIED TORQUE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. (S) 2 L 7 2 4T RT T00011AT 20080819 SO 2008 8 19 SWIA200819887 1 20080721 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE LT WING CRACKED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 232SW 120306 FOUND STRINGER 10 AT RIB 9 TO BE CRACKED INSIDE LT IB NR 1 FUEL PANEL. PERFORMED REPAIR TO STRINGER 10 AT RIB 9 IAW SRM 57-20-03. 2 L 7 2 4T 4 T RT A31SO E20NE 20080819 EA 2008 8 19 SWIA200819888 1 20080718 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 927SW 7693 FLOOR EMERGENCY LIGHTING IS INOPERATIVE. (FLIGHT NR 6103) REPLACED EMERGENCY LIGHT CHARGER ASSEMBLY IAW AMM 33-51-01. 2 L 7 2 4F RT A21EA 20080818 WP 2008 8 18 UPS08852744 1 20080630 A 5347 36575041 SEAT TRACK DOUG DC8 DC871F 302199D WP COCKPIT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C2 F/E'S AFT SEAT TRACK HAS ELONGATED HOLES. REMOVED AND REPLACED F/E'S AFT SEAT TRACK IAW SRM 51-01-24 . 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852747 1 20080612 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP BS 190 L10-21R GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, RT FWD SERVICE DOOR AFT JAMB WEB HAS 5 AREAS OF DRILL STARTS, GOUGES AND HOLES. STA 190 BETWEEN L-2 1R AND L-10R. PLUGGED TOP 3 AREA HOLES IAW SRM 53-02-00 FIG 1F. FABRICATED AND INSTALLED REPAIR DOUBLER AT BOTTOM 2 AR EA IAW SRM 53-02-00 FIG 23. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852897 1 20080707 A 5751 SKIN DOUG DC8 DC871F 302199D WP LT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, 2 INCH CRACK IN LT AILERON AS MARKED ON LEADING EDGE AT X 499, STOP DRILLED CRACK , FABBED AND INST ALLED REPAIR DOUBLER IAW, SRM, 51- 1-8, 57-2-0 FIG. 2 , 51-3-1. 2 L 7 4 4F RT 4A25 20080818 EU 2008 8 18 UPS08152643 1 20080704 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU PWA 4158 PW4158 NE COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 156UP 0845 EMERGENCY EXIT LIGHTS FLICKER WHEN SUPPOSE TO BE ON. COMPLIED WITH OPERATIONAL TEST OF EMERGENCY LIGHTING IAW AMM 33-51 -00- 05. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A35EU E24NE 20080818 WP 2008 8 18 UPS08852656 1 20080612 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP FS 1620 L21L CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, LT AFT ENTRY DOOR, FWD LWR JAMB HAS INTERGRANULAR CORROSION AND IS CRACKED BS 1620 L21L (DOOR PAN). CUT OUT DAMAGED AREA IAW SRM 53-02-00 FIG 001F. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-2 FIG 1D AND 51- 1-20D. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852657 1 20080612 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP BS 165 L21R DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE-C1, RT FWD SERVICE DOOR, FWD JAMB WEB HAS HOLE DRILLED OVER FRAME STA 165 ABOVE L21R. INSTALLED PLUG IA W SRM 53-02-00 AND 51+01-21. 2 L 7 4 4F RT 4A25 20080818 WP 2008 8 18 UPS08852946 1 20080729 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 240 LBL 45 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C1 MAIN CABIN, SEAT TRACK PLUG DAMAGED AND ATTACH SCREWS (2EA) TOO HIGH-S TA. 240 LBL 45. REMOVED AND R EPLACED PLUG AT MAIN CABIN SEAT TRACK STA 240 LBL 45 IAW SRM 51-3-00 PG1. 2 L 7 4 4F RT 4A25 20080818 NM 2008 8 18 UPS08M52965 1 20080721 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE:1C, CORROSION FOUND IN NR 25 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED RE PAIR BUSHING IAW EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080818 NM 2008 8 18 SWAA084025 1 20080718 A 3350 411A2212 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 424WN 29828 R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084035 1 20080718 A 3350 65C27093 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080822 NM 2008 8 22 F3LA200800459 1 20080711 A 5321 D5367314600000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 940FR 2465 DURING C-CHECK INSP NOTED AFT PIT PANEL 152UG DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800463 1 20080711 A 5321 D5367424000000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 940FR 2465 DURING C-CHECK INSP NOTED FWD PIT FLOOR PANEL 131CG DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COM PLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800476 1 20080711 A 5320 D5391379020002 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED CORROSION ON PROFILE PARALLEL WITH FRAME C28 FWD CARGO COMPARTMENT. MAINT REMOVED AND REPLACED CORRODED PROFILE ON FRAME C28 IN FWD CARGO COMPARTMENT IAW FO A319 SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS I NSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800473 1 20080711 A 5313 D5347218920400 LONGERON AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED RT LONGERON BEAM AT Y-1162 FROM FRAME 68 TO FRAME 69 HAD AREAS OF CORROSION. MAINT REMOVED AND REPLACED FLOORBEAM LONGERON Y-1162 FROM FRAME 68 TO FRAME 69 IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INS PECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800471 1 20080711 A 5320 D5391550320010 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED CORROSION SEVERAL PLACES ON PROFILE LT SIDE AFT OF FRAME C28 FWD CARGO COMPARTMENT. MAINT REMO VED OLD PROFILE AT FRAME C28 ON LT SIDE, LOCATED AND DRILLED HOLES ON NEW PROFILE AND INSTALLED NEW PROFILE IAW SRM 51-7 2-11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800490 1 20080716 A 5414 6421000501 SKIN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE NR 1 NACELLE DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED THAT THE DAMAGE ON NR 1 ENGINE INLET COWL REQUIRES PERMANENT REPAIR OF DENT AT THE 2 O`CLOCK P OSITION. MAINT REPAIRED DAMAGED AREA IAW CMM 54-10-00, REPAIR PROCEDURE NR 23. UPON COMPLETION OF THE REPAIR IT WAS INSP ECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800457 1 20080711 A 5321 D5367414400000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 940FR 2465 DURING C-CHECK INSP NOTED AFT PIT PANEL 151FE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080728 EA 2008 7 28 TRAX200800650 1 20080516 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNSERVICEABLE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 907EV 7648 OPERATION 145 EXIT PLACARD ON PAX DOOR STEP 832BT IS UNSERVICEABLE. REMOVED AND INSTALLED NEW SERVICEABLE EXIT PLACARD O N PAX DOOR STEP 832BT IAW AMM 11-30-00-400-801. 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 2008UALA03380 1 20080613 A 5320 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 301UA 23642 THE 520 STR 12L HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED: MANUFACTURED & INSTALLED 1EA DOUBLER, 1EA TRIPLER AND APPLIED PRIMER. 2 L 7 2 4F 4 F RT A16WE E21EU 20080728 EA 2008 7 28 TRAX200800627 1 20080514 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 280 SUPPORT BEAM CORRODED. REMOVED AND REPLACED STA 280 SUPPORT BEAM PN CC670-34175-7 AS PER SRM 51-42-21, 51-42-06. RE O 670-53-11-047, AND SB 670BA-53-026. 2 L 7 2 4F RT A21EA 20080728 EU 2008 7 28 2008UALA03377 1 20080614 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 440UA 702 RAMP REPORTS FUSELAGE ABRASION TWO FEET AFT AND ABOVE DOOR 1L. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 NM 2008 7 28 2008UALA03191 1 20080603 A 2730 31075215 CONTROL UNIT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LT ELEVATOR FAULTY A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 816UA 871 ELAC 2 FAULT INDICATIONS. SERVO 34CE1 FAILING CAUSING ELAC 2 TO FAULT CHRONICALLY. REPLACED LT INBOARD ELEVATOR SERVO CONTROL UNIT 34CE1, ADJUSTED AND OPS TESTED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 EA 2008 7 28 TRAX200800641 1 20080514 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 693-977 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE AT LBL 9 FS 693.00 TO FS 977.00. BLENDED CORROSION FOUND ON LBL 9 FS 693 T O FS 977 REMOVED .028" OF MATERIAL WITHIN LIMITS ALLOWED TO REMOVE .035" OF MATERIAL. ALL WORK DONE IAW SRM 53-41-49 AN D 53-51-49. 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 KCSA081302 1 20080628 A 5320 WEB BOEING 747 747122 1384872 NM BS 1680-1700 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 AFT BILGE UPPER TORQUE BOX WEB HAS SEVERAL DENTS AT STA. 1680 TO 1700, RBL 47 TO RBL 56 (B) 2 L 7 4 4F RT A20WE 20080728 EA 2008 7 28 TRAX200800861 1 20080701 A 5340 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 861AS 7445 CARGO DOOR TRACK SUPPORT TO AFT PRESSURE BULKHEAD LWR ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED ATTACH ANGLE IAW S RM 51-42-21. 2 L 7 2 4F RT A21EA 20080818 NM 2008 8 18 SWAA084050 1 20080718 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM BS 877 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 877, STR 25R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084070 1 20080720 A 5755 HINGE BOEING 737 7373H4 1384600 NM NR 5 SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN MA5122 27715 RT WING NR 5 GROUND SPOILER HINGE BROKEN. R&R SPOILER PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084109 1 20080724 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500D S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 22L. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084108 1 20080724 A 5311 6545804 FRAME BOEING 737 7373H4 1384600 NM BS 259 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 259, STR 11R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084101 1 20080723 A 2560 P22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED HC1 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT LH OVERWING EMERGENCY EXIT. R&R STRIP PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084112 1 20080724 A 3350 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080818 2008 8 18 SWAA084119 4 20080724 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080819 EA 2008 8 19 SWIA200819901 1 20080726 A 3244 TIRE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 928SW 7701 NOSE TIRE BLEW OUT ON TAKE-OFF. (FLIGHT NR 6107) COMPLIED WITH TIRE BURST INSPECTION AND REPLACED LT AND RT NOSE TIRES IAW MM 32-42-01.PN 5010598 S/N OFF APR01-3456. 2 L 7 2 4F RT A21EA 20080819 EU 2008 8 19 USAA920081449 1 20080729 A 2810 L95F50603 DISC AIRBUS A321 A321211 3930370 EU FUEL SYSTEM RUPTURED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 180US 1525 FLT 1167 CLT-SFO - DIVERSION - THE CREW REPORTED A FUEL IMBALANCE PROBLEM AND THE ACFT DIVERTED TO BNA. MAINTENANCE FOU ND THE OVERPRESSURE PROTECTOR DISC RUPTURED. REMOVED AND REPLACED THE OVERPRESSURE PROTECTOR DISC. (S) 2 L 7 2 4F RT A28NM 20080819 EA 2008 8 19 REX2008F00021 1 20080731 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG LOW A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 8672A 7672 ON CLIMBOUT AND GEAR RETRACTION RECEIVED "GEAR DISAGREE" WARNING. QRH FOLLOWED AND RETURNED TO AIRPORT WITH UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE GEAR AND SERVICED THE NOSE LANDING GEAR STRUT NITROGEN/HYDRAULICS, GEAR SWINGS PERFO RMED WITH NO DEFECTS PER BOMBARDIER AMM. (S) 2 L 7 2 4F RT A21EA 20080819 WP 2008 8 19 UPS08852995 1 20080724 A 5420 STIFFENER DOUG DC8 DC871F 302199D WP NR 4 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1, NR 4 PYLON RT INTERIOR STRUCTURE AREA HAS A CRACKED STIFFENER AT STA. YN 326. FABRICATED AND REPL ACED STIFFENER IAW DWG 5756791, AND 51-01-24,51-01- 21D. 2 L 7 4 4F RT 4A25 20080819 SO 2008 8 19 SWIA200819877 1 20080503 A 4940 CONTACTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE APU STARTER DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 APU STARTER CONTACTOR IN RT RELAY BOX IS DISCOLORED. (FOUND AT C-CHECK) REPLACED THE APU STARTER CONTACTOR IAW AMM 25-0 0-00. 2 L 7 2 4T 4 T RT A31SO E20NE 20080819 SO 2008 8 19 SWIA200819909 1 20080730 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT DAMAGED A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 308SW 120326 FIRST TWO FLOOR EMERGENCY LIGHTS ARE INOP. (FLIGHT NR 5438) REPAIRED WIRING TO EMERGENCY LIGHTS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080819 EA 2008 8 19 SWIA200819899 1 20080722 A 3297 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* 30015 NE NLG FAULTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 427SW 7497 UPON RETRACTION OF LANDING GEAR RECEIVED A "GEAR DISAGREE" WITH A "NOSE DOOR OPEN" MESSAGE. (FLIGHT NR 3805) INSPECTED AND CLEARED FAULTS IN PSEU. REPLACED BOTH NOSE GEAR HARNESSES. OPS CHECK GOOD IAW MM 32-61-05. 2 L 7 2 4F 4 F RT A21EA 20080819 NM 2008 8 19 NSV2008F00016 1 20080807 A 6120 CONTROLLER BOMBDR DHC8 DHC8402 1390042 NM PWC 150 PW150A EA NR 1 ENGINE MALFUNCTIONED A NSVA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 EA 27 187WQ 4187 FA0425 AT 14000 FT WENT BELOW MIN/880 WITH CONDITION LEVERS. RETURNED CONDITION LEVER TO MIN 850 IMMEDIATELY. NR 1 AND NR 2 P EC FAILED AND PROPS WENT TO 1080 RPM ON FINAL APPROACH TO EWR AIRSPEED 180 ALT 3000 FT. NR 1 ENG CYCLES IN AND OUT OF F EATHER. MANUALLY FEATHERED NR 1 ENG AND SHUT NR 1 ENG DOWN WITH QRC. NORMAL LANDING. PULLED OFF RUNWAY AND SHUTDOWN N R 2 ENG PER NORMAL CHECKLIST. RETRIEVED DATA FROM THE EMU IAW Q400 AMM 45-00-73-742-801. FOUND FAULT CODES 280 AND 238 SET ON PROPELLER NR 1 AND NR 2. PERFORMED TROUBLESHOOTING IAW FIM TASK 61-20-06-810. OPS CHECK GOOD. NO FAULTS STORE D. 2 H 7 2 4T 4 T RT A13NM E00062EN 20080819 EU 2008 8 19 NSV2008F00017 1 20080807 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A NSVA O OTHER O OTHER NR NOT REPORTED 1 EA 27 202SR 340B202 MAIN EMERGENCY LIGHTS IN CABIN OUT. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AT SEAT 5A CWC 33-50-026. OPS CHECK GO OD. P/N ON/OFF 60-1321-1, S/N: OFF 17486, S/N: ON 12291. (S) 2 L 7 2 4T RT A52EU 20080819 SO 2008 8 19 SWIA200819866 1 20080709 A 3520 OXYGEN MASK EMB 120 EMB120ER 3260203 SO ROW 5 UNWANTED DEPLOY A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 224SW 120294 ROW 5 OXYGEN MASKS DEPLOYED. (FLIGHT NR 5474) RESTOWED O2 MASKS AS REQUIRED. 2 L 7 2 4T RT A31SO 20080819 EA 2008 8 19 SWIA200819926 1 20080802 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 417SW 7400 MAIN CABIN DOOR OUTER HANDLE WOULD NOT OPEN DOOR. (FLIGHT NR 5901) INSPECTED AND LUBED PAX DOOR IAW 52-11-00. CYCLED DO OR SEVERAL TIMES AND OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080819 EA 2008 8 19 SWIA200819921 1 20080731 A 3230 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG INOPERATIVE A SWIA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 07 454SW 7749 RECEIVED A "GEAR DISAGREE WARNING" ON APPROACH. GEAR EXTENDED NORMALLY ON NEXT APPROACH. (FLIGHT NR 3940) REPLACED NO SE GEAR SELECTOR VALVE IAW MM 32-33-10. INSPECTED LANDING GEAR SYSTEM AND SWUNG GEAR SEVERAL TIMES. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080819 WP 2008 8 19 UPS08853014 1 20080726 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1754 L14L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C1, L14R CRACKED IN LOWER RADIUS AT BS 1754 APPROX (SEEN IN BACKSIDE OF LONGERON) AT LONGERON SPLICE IN MAIN CABIN. FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION IAW SRM 53-02-02 FIG10, 53-05-03, 51-01-20D, AND 51- 03-01. 2 L 7 4 4F RT 4A25 20080819 EA 2008 8 19 SWIA200819919 1 20080730 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* 30015 NE CABIN SMOKE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 983CA 7169 SMOKE REPORTED IN THE REAR OF THE PASSENGER CABIN. (FLIGHT NR 2811) INSPECTED AND RAN BOTH AIR CONDITIONING SYSTEMS. V ERIFIED THAT THERE WAS NO SMOKE IN CABIN. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA 20080819 SO 2008 8 19 C2XA08CL095 1 20080806 A 2150 8151138 SLEEVE EMB 145 EMB145XR 3260214 SO A/C PACK BLOWN A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 16147 145749 EWR FLIGHT 2879, THE CREW REPORTED A BLEED VALVE 2 FAIL IN FLIGHT. THE ACFT DIVERTED INTO CLE AND LANDED WITHOUT FURTHE R INCIDENT. MAINTENANCE INSPECTED AND REPLACED A BLOWN SLEEVE ON THE NR 2 ENVIRONMENTAL CONTROL UNIT. ALSO REPLACED TH E NR 2 BLEED PUSH BUTTON P/N 4800-112. OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4F RT 20080819 SO 2008 8 19 C2XA08SH097 1 20080724 A 5320 14525480603 SILL EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27152 145759 SHV - DURING C-CHECK LOWER INTERNAL PORTION OF BAG DOOR CUTOUT HAS VARIOUS AREAS OF CORROSION FROM FR 65 TO FR 68. MX R EMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL FROM FR 6T TO FR 68 IAW EMB 145 XR SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN FOR SERVICE. (S) 2 L 7 2 4F RT 20080819 NM 2008 8 19 UPS08M53030 1 20080721 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 28 LT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED AND INSTALLED BUSHI NG IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 EU 2008 8 19 UPS08152977 1 20080723 A 5321 B5327077900100 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU FUSELAGE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 153UP 0839 INSPECTION TYPE:5 YR, MAIN CABIN COMPT, FLOOR PANEL 252BN AT FR. 72 FOUND BROKEN. REPAIRED MAIN CABIN FLOOR PANEL 252B N AT FR 72 IAW SRM 53- 10-20 FIG 201 PARA 8A. 2 L 7 2 4F RT A35EU 20080819 EA 2008 8 19 SWIA200819794 1 20080623 A 5210 ROLLER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 417SW 7400 MAIN CABIN DOOR IS VERY DIFFICULT TO OPEN. (FLIGHTNR 2875) ADJUSTED PAX DOOR SPIGOT ROLLER ASSEMBLY AND AFT MIDDLE LATC H PIN IAW AMM CHAPTER 52-11-00. CABIN DOOR OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 20080819 EA 2008 8 19 SWIA200819795 1 20080622 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FAILED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 496CA 7791 RT WINDSHIELD SHATTERED WHILE AT CRUISE. (FLIGHT NR 2876) REPLACED WINDSHIELD IAW AMM 56-11-01. OPS AND LEAK CHECK GOOD . P/N OFF 601R33033-18 S/N OFF 03017H4489. 2 L 7 2 4F RT A21EA 20080819 EA 2008 8 19 SWIA200819796 1 20080620 A 2731 SWITCH CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* 30015 NE STAB TRIM FAILED A SWIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 NM 07 494CA 7765 STAB TRIM AND MACH TRIM CAUTION MESSAGE. STAB TRIM WOULD NOT ENGAGE. (FLIGHT NR 2534) REPLACED F/O TRIM DISCONNECT SWI TCH IAW AMM 27-41-30. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA 20080819 EA 2008 8 19 SWIA200819800 1 20080502 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF34* 30015 NE COCKPIT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 614SK 10051 COCKPIT AFT FLOOR SUPPORT IS CORRODED. (FOUND AT C-CHECK) INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01. 2 L 7 2 4F 4 F RT A21EA 20080819 EU 2008 8 19 UPS08152979 1 20080723 A 5321 B5327082100100 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 153UP 0839 INSPECTION TYPE-5, YR MAIN CARGO COMPT RT FLOORBOARD NR 262DM CRACKED BOTTOM SIDE AT TIE- DOWN CUT OUT. REPAIRED MAIN C ABIN FLOORBOARD NR 262DM IAW SRM 53-10-20 FIG 201 PARA 8A. 2 L 7 2 4F RT A35EU 20080819 EU 2008 8 19 UPS08152980 1 20080724 A 5321 B5327082300000 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 153UP 0839 INSPECTION TYPE:5 YR, MAIN CABIN FLOOR PNL NR 262BM IS CRACKED ON THE AFT END. REPAIRED MAIN CABIN FLOOR PNL NR 262BM I AW SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20080819 EU 2008 8 19 UPS08152981 1 20080722 A 5321 B5327074500000 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 153UP 0839 INSPECTION TYPE:5 YR, MAIN CABIN FLOOR PNL NR 231SG IS CRACKED AT THE FWD END. REPAIRED MAIN CABIN FLOOR PNL NR 231SG I AW SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20080819 NM 2008 8 19 UPS08M52945 1 20080716 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 24 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INSTALL ED BUSHING IAW MD11-5510-19409-N AND SAA TRAVELER 80538560001. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M52947 1 20080716 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 18 LT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INSTALL ED BUSHING IAW UPS EO MD11-5510-19409-N AND SAA TRAVELER 80538590001. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M52948 1 20080717 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 21 LT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INSTALL ED BUSHING IAW UPS EO MD11-5510-19409-N AND SAA TRAVELER 80538620001 2 L 7 3 4F RT A22WE 20080819 2008 8 19 ASAA0853320 4 20080803 A 2230 305RAA1 SERVO BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE AUTOTHROTTLES FAULTED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 585AS 3720 35683 AUTO-THROTTLES WILL NOT STAY ENGAGED, COULD NOT DUP. ACCOMP FIM22 31 805 GND VERIFICATION INFLT HIST, LOGGED 22 31688. AT CURRENT STATUS CK NML IAW FIM INITAL EVAL FOUND TO BE INTERMITTENT FAULT. NO HISTORY 60DAYS. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080819 NM 2008 8 19 ASAA0843297 1 20080627 A 5320 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 727F CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AFT PIT FLOOR SUPPORT RAIL AFT OF STA 727F IB OF STRINGER 28R IS CORRODED REMOVED DAMAGED AREA FABRICATED REPAIR PARTS & INSTALLED IAW EA 5320 1844. 2 L 7 2 4F 4 F RT A16WE E21EU 20080819 NM 2008 8 19 ASAA0843310 1 20080627 A 5320 654659245 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AFT PIT FLOOR SUPPORT RAIL IS CORRODED AFT OF STA 727 RT IB OF STRINGER 28 LT. REMOVED DAMAGED AREA FABRICATED REPAIR PA RTS AND INSTALLED IAW EA 5320 01845. 2 L 7 2 4F 4 F RT A16WE E21EU 20080819 NM 2008 8 19 ASAA0843255 1 20080624 A 5330 65458001128 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 348-366 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 REF SAD 6058905: FUSELAGE LOWER SKIN DENT AT STA 354 STR 23 24R.DENT IS CREASED WITHIN 3" OF A SPLICE REMOVED DAMAGE A REA FABBED FILLER DOUBLER, TRIPLER & INSTALLED REPAIR PARTS IAW SRM T.R 53-27 FIG 201 DETAIL XXIX. 2 L 7 2 4F 4 F RT A16WE E21EU 20080819 SO 2008 8 19 CHQA200800156 1 20080729 A 2740 3621001013 CONTROL UNIT EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL HORIZ STAB FAULTY A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 563RP 22095 22095 145509 CAE312314 FLIGHT 6349, CVG TO LIT. DURING INITIAL CLIMB THE FLIGHT CREW RECEIVED A PTRIM MAIN INOP MESSAGE ON EICAS. THE CREW PE RFORMED THE APROPRIATE QRH CHECKLIST ITEMS AND THE ACFT LANDED WITHOUT INCIDENT BACK AT CVG. MAINTENANCE TROUBLESHOT TH E FAULT TO THE HORIZONTAL STAB CONTROL UNIT AND REPLACED IT. THE TRIM SYSTEM OPS CHECKED GOOD AND THE ACFT WAS RETURNED TO SERVICE. (S) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080819 NM 2008 8 19 ASAA0843258 1 20080625 A 5753 6546431285 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU LT WING TE FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 LT OB FOREFLAP L/E IS GOUGED ON PREVIOUS REPAIR DOUBLER AT THE INBOUND END REMOVED DAMAGE ED DOUBLER FABBED & INSTALLED REPAIR IAW SRM 57 53 01 PG 202 203. 2 L 7 2 4F 4 F RT A16WE E21EU 20080819 EA 2008 8 19 COMA0870024 1 20080803 A 3610 AS18954300 COUPLING CNDAIR CL600 CL6002C10 1390015 EA LT PYLON LEAKING A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 656CA 10143 ON CLIMBOUT FROM CVG RECEIVED LT BLEED DUCT WARNING MSG, WARNING MSG CLEARED AND WAS REPLACED BY BLEED CAUTION MSG. ACF T RETURNED BACK TO CVG AND LANDED SAFELY. INSPECTED ACFT, SUSPECT LT ENG PYLON DUCT V-BAND COUPLING LEAKING. REMOVED A ND REPLACED LT ENG PYLON BLEED DUCT V-BAND COUPLING. (S) 2 L 7 2 4F RT A21EA 20080819 EA 2008 8 19 COMA086343 1 20080807 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 477CA 7670 FOUND CORROSION AT FS 280 LBL 10 TO RBL 10 PILOT`S FLOOR CAP ANGLE. REPAIRED FS 280 FLOOR IAW 601R-53-11-136 & EA105310 02294. (S) 2 L 7 2 4F RT A21EA 20080819 WP 2008 8 19 DHLA200800086 1 20080731 A 2697 899827 CONNECTOR DOUG DC8 DC873F 302199F WP FIRE LOOP LOOSE A DHLA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 873SJ 351 117 46091 WHEN REDUCING THRUST FOR DESCENT, NR 1 FIRE WARNING ILLUMINATED. RAN EMERGENCY PROCEDURE. TROUBLESHOT FIRE WARNING SYS PER MM 26-10-0. FOUND FAN CASE FIRE LOOP CONNECTOR BKSHL LOOSE AND GNDING. SECURED AND CLEANED ALL CONNECTIONS. AIRC RAFT WAS GROUNDED. FLIGHT 803. (S) 2 L 7 4 4F RT 4A25 20080819 CE 2008 8 19 DJFA2008065 1 20080804 A 3150 WARNING SYSTEM BEECH MU300 400A 1155402 CE COCKPIT ACTIVATED A DJFA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 23 745TA RK145 REPORTED DURING CLIMBOUT MASTER WARNING AND RT THRUST REVERSER UNLOCK LIGHT ILLUMINATED. COMPLETED EMERGENCY PROCEDURES AND DIVERTED TO KFTY. (S) 2 H 7 2 4F RT A16SW 20080819 EU 2008 8 19 MAL2008F00021 1 20080730 A 5753 FASTENER SAAB SF340 340B 7860101 EU T/E FLAP UNKNOWN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 REPLACED FASTENERS IN LT FLAP FAIRING AFT BULKHEAD UPPER FLANGE TO REAR SPAR IAW EOS57051. FLAP FAIRING AFT BULKHEAD UP PER FLANGE TO REAR SPAR - ALTERNATIVE FASTENER REPLACEMENT AUTHORIZATION. STANDARD SRM REPAIR PROCEDURES. NO INFORMATI ON ON THE PART CONDITION AT THIS TIME. (S) 2 L 7 2 4T RT A52EU 20080819 EU 2008 8 19 MAL2008F00022 1 20080804 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 407XJ 340B407 DURING EMERGENCY LIGHT FUNCTIONAL CHECK, POWER SUPPLY 21LN FAILED. THE 21LN WAS REMOVED AND REPLACED TO CORRECT FAILURE . (S) 2 L 7 2 4T RT A52EU 20080819 NM 2008 8 19 SWAA084130 1 20080725 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 212WN 32485 DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084131 1 20080724 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 249WN 34951 EEPLS ASSY LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084137 1 20080727 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED PAE CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084139 1 20080727 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084143 1 20080727 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR CUTOUT FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084146 1 20080727 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084154 1 20080727 A 3350 MC157721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED MV3 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084155 1 20080724 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 L1 DOOR EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 20080819 2008 8 19 SWAA084156 4 20080724 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 648SW 27718 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084169 1 20080728 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 460, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080819 2008 8 19 SWAA084172 4 20080728 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084174 1 20080728 A 5311 6545693 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084053 1 20080719 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 DURING SCHEDULED 10Y CHECK, FOUND EMERGENCY LIGHT INOP AT ROW 22 ABC. R&R LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084068 1 20080720 A 5312 6545819 PRESSURE PANEL BOEING 737 7375H4 138449D NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED BRDG CHECK, FOUND NLG WW LT CEILING WEB CUTOUT CRACKED. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084069 1 20080720 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 430-450 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 430 AND BS 450, RBL 3. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084096 1 20080723 A 5311 6546550 FRAME BOEING 737 7373Q8 1384670 NM BS 787 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084129 1 20080724 A 5322 6546543 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 639 S7L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 639, STR 7L. R&R SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084111 1 20080723 A 3350 6128251 CHARGER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS FAULTY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. R&R BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 20080818 NM 2008 8 18 SWAA084103 1 20080724 A 5310 141A5506 CREASE BEAM BOEING 737 7377H4 1384404 NM BS 294-338 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 777QC 30592 DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM CHORD CORRODED BETWEEN BS 294 AND BS 338, RBL 56. R&R CHORD PER SRM. 2 L 7 2 4F RT A16WE 20080819 SO 2008 8 19 SWIA200819896 1 20080719 A 5753 ATTACH BRACKET EMB 120 EMB120ER 3260203 SO LT NACELLE FLAP BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 295UX 120295 LT NACELLE FLAP HAS A CRACKED ATTACH BRACKET. (FLIGHT NR 5480) REPLACED THE LT NACELLE FLAP IAW 27-50-03. 2 L 7 2 4T RT A31SO 20080819 EA 2008 8 19 SWIA200819931 1 20080603 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 956SW 7825 FS 280 FLOOR SUPPORT IS CRACKED ALONG THE OB SIDE OF RBL 9. (FOUND AT C-CHECK) COMPLIED WITH REPAIRS AT FS 280 AND RBL 9 IAW MFG REO 601R-53-11-171, REV. "D". 2 L 7 2 4F RT A21EA 20080819 EA 2008 8 19 SWIA200819936 1 20080803 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA GE CF34 CF348C5 30050 NE CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 804SK 15067 EMERGENCY CABIN LIGHT INOPERATIVE. (FLIGHT NR 4070) REPLACED EMERGENCY LIGHT IAW 33-51-21. OPS CHECK OK. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080819 EA 2008 8 19 SWIA200819937 1 20080803 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 910EV 7727 FWD CEILING EMERGENCY EXIT LIGHT IS INOP. (FLIGHT NR 4096) REPLACED NR 2 CHARGER ASSEMBLY IAW MM 33-51-00. OPS CHECK G OOD. 2 L 7 2 4F RT A21EA 20080819 SO 2008 8 19 SWIA200819938 1 20080804 A 5210 ROLLER EMB 120 EMB120ER 3260203 SO PAX DOOR LACK OF LUBE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 569SW 120344 MAIN CABIN DOOR IS DIFFICULT TO OPEN. (FLIGHT NR 5561) LUBED PAX DOOR ROLLERS AND CONTACT POINTS. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080819 WP 2008 8 19 UPS08852983 1 20080707 A 5340 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C2, NR 1 ALT STRINGER -65 TO FRONT SPAR FITTING CRACKED REMOVED AND REPLACED FITTING IAW SRM, 51-1-2 0D, 51-1-8, 51-1-2451-1-12. 2 L 7 4 4F RT 4A25 20080819 EA 2008 8 19 SWIA200819907 1 20080724 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BROKEN A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 443SW 7638 BROKEN WINDSCREEN EMERGENCY EXIT SIGN. (FLIGHT NR 4122) REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080819 SO 2008 8 19 C2XA08RI105 1 20080719 A 3213 BOLT EMB 145 EMB145LR 3260212 SO MLG STRUT SHEARED A NWAA K NONE O OTHER IN INSP/MAINT 1 SW 27 12540 2700 1147999008 145537 DURING INSTALLATION OF MAIN LANDING GEAR OLEO STRUT ASSEMBLY, LOWER ATTACHMENT BOLT SHEARED AT TORQUE BELOW 1200 IN LBS. RIC MX REMOVED AND REPLACED LOWER ATTACHMENT BOLT, APPLIED TORQUE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. (S) 2 L 7 2 4T RT T00011AT 20080819 EA 2008 8 19 MAL2008F00023 1 20080804 A 3234 SELECTOR VALVE CNDAIR CL600 CL6002D24 1390016 EA LANDING GEAR MALFUNCTIONED A MALA O OTHER O OTHER AP APPROACH 1 GL 15 926XJ 15184 GEAR EXTENSION FAILED ON APPROACH TO DTW. PERFORMED EMERGENCY LANDING GEAR EXTENSION AND LANDED IN DTW. (S) 2 L 7 2 4F RT A21EA 20080819 NM 2008 8 19 UPS08553057 1 20080730 A 5320 SUPPORT BOEING 757 75724APF 1384969 NM BS 645-765 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 INSPECTION TYPE-2C, FWD CARGO COMP RT FLOOR TO SIDEWALL SUPPORT IS CORRODED AT TIE DOWN FITTINGS BS 645 TO 765.5 REMOVE D AND REPLACED IAW SRM 51-40-02-0G, DRW NR143N5366. 2 L 7 2 4F RT A2NM 20080819 NM 2008 8 19 UPS08553058 1 20080730 A 5320 SUPPORT BOEING 757 75724APF 1384969 NM BS 620-645 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 INSPECTION TYPE-2C, FWD CARGO COMPARTMENT RT FLOOR TO SIDEWALL SUPPORT IS CORRODED AT TIE DOWN FITTINGS BS 620 TO 645.5. REMOVED AND REPLACED IAW SRM 51-40-02-0G, DRG NR 143N5366. 2 L 7 2 4F RT A2NM 20080819 NM 2008 8 19 UPS08553050 1 20080806 A 3350 LAMP BOEING 757 75724APF 1384969 NM EMERGENCY LIGHT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 473UP 28846 EMERGENCY EXIT EGRESS LIGHT INOPERATIVE. RELAMPED THE EMERGENCY EXIT EGRESS LIGHT IAW AMM 33-51-06-2 TASK 33-51-06-962- 001. OPS CHECKED GOOD. 2 L 7 2 4F RT A2NM 20080819 EA 2008 8 19 SWIA200819920 1 20080726 A 3244 TIRE CNDAIR CL600 CL6002C10 1390015 EA MLG FAILED A SWIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 727SK 10191 BOTH NR 1 AND NR 2 MLG TIRES BURST ON TAKE-OFF. REPLACED NR1 AND NR2 TIRE ASSEMBLIES IAW MM 32-41-01 AND COMPLIED WITH RELATED REPAIRS. PN: 5013641 S/N OFF: APR04-1169 2 L 7 2 4F RT A21EA 20080819 NM 2008 8 19 UPS08M53040 1 20080710 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 8 RT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 SO 2008 8 19 SWIA200819930 1 20080706 A 5210 DOOR FRAME EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 298SW 120328 PAX DOOR FRAME IS CRACKED UNDER AFT LOWER STOP. (FOUND AT C-CHECK) REPAIRED FRAME UNDER LOWER AFT STOP ON PAX DOOR IAW SRM 52-10-02. 2 L 7 2 4T 4 T RT A31SO E20NE 20080819 WP 2008 8 19 UPS08853049 1 20080730 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 80 L36 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C1, FWD LOWER CARGO COMP FLOOR SUPPORT BRACKET CRACKED AT FUS STA 80 LONGERON 36 AS MARKED. REMOVED, F ABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL (BRACKET) IAW SRM 51-01-20D,DWG 4619078, AND SRM 51-03-01. 2 L 7 4 4F RT 4A25 20080819 EA 2008 8 19 SWIA200819889 1 20080720 A 2421 ADG CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* 30015 NE MALFUNCTIONED A SWIA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 969SW 7876 ADG DEPLOYED DURING TRANSFER TO EXTERNAL POWER. (FLIGHT NR 5984) RESTOWED ADG IAW 24-23-0. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA 20080819 NM 2008 8 19 SWAA084175 1 20080728 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084180 1 20080728 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084196 1 20080726 A 3350 311500 LENS BOEING 737 7373G7 1384595 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 671SW 23785 DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084186 1 20080728 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084185 1 20080728 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084190 1 20080728 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 1. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084161 1 20080726 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 755 TO BS 778, RBL 13. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084164 1 20080726 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 908WN 36620 EEPLS END CAP AT ROW 1 ABC MISSING. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084207 1 20080728 A 5230 6547953 DOOR FRAME BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR FRAME CRACKED AT PULLEY BRACKET. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084208 1 20080728 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084213 1 20080728 A 5551 6551524 FITTING BOEING 737 7373H4 1384600 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND LT HORIZONTAL STABILIZER CLEVIS LUG FITTING FACES CORRODED. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084212 1 20080728 A 5551 6551524 FITTING BOEING 737 7373H4 1384600 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULE BRDG CHECK, FOUND RT HORIZONTAL STABILIZER CLEVIS LUG FITTING FACES CORRODED. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 20080728 EA 2008 7 28 MASA200800456 1 20080607 A 3350 BULB CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 924FJ 15024 ASH FLT 2709 IAH-PHX. LIGHTED EXIT SIGN AT 15A HAS 1 BULB BURNED OUT. RELAMPED---OPS GOOD. (B) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 MASA200800457 1 20080608 A 3350 BULB CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 912FJ 15012 ASH FLT 2889 BFL-PHX. BOTH FLOOR LEVEL LIGHTED EXIT SIGNS HAVE A BULB OUT. RELAMPED. (B) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 MASA200800476 1 20080617 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCONNECTED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH FLT 2802 PHX-SBA EMERGENCY FLOOR PATH LIGHTING INOP. MX RESECURED FLOOR LIGHT PATH CONNECTION. (B) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 KCSA081304 1 20080630 A 5531 SPAR BOEING 747 747122 1384872 NM VERTICAL STAB CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 VERTICAL STAB LEADING EDGE SPAR AT BL-0 FIN STA-225 SKIN DAMAGED (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 AALA200801332 1 20080517 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 674AN 29424 MIA EMERGENCY LIGHT AT RT NUMBER THREE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RT NUMBER THREE D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A2NM 20080728 EA 2008 7 28 MASA200800470 1 20080615 A 3520 1170252223 O2 GENERATOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 37178 30378 7178 ASH FLT 2866 LAS-MFR CABIN ALT CAUTION MESSAGE WITH PASSENGER MASK DEPLOYMENT AND DISPLAY COOL CAUTION. DECLARED AND E MERGENCY. MX REINSTALLED CARGO DOOR SEAL AND REPLACED O2 GENERATORS. (B) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 TRAX200800872 1 20080702 A 5751 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA AILERON CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 861AS 7445 CORROSION FOUND IN LEFT AILERON AROUND THE HINGE INTERNAL AREA. OPEN (B) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 NWAA082615514 1 20080518 A 5532 SKIN PANEL BOEING 757 757251 1384970 NM VERTICAL STAB DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 514US 23202 DURING INSPECTION FOUND DAMAGE TO VERTICAL STABILIZER LT SIDE SKIN PANEL. REPAIRED PER EA 55-213388. (A) 2 L 7 2 4F RT A2NM 20080728 EA 2008 7 28 TRAX200800631 1 20080514 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA OUT OF ADJUST A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 838AS 7276 ASD HARD TO CLOSE, ADJUSTED PAX DOOR COUNTERBALANCE SYSTEM IAW MM 52-11-17. OK FOR SERVICE. (B) 2 L 7 2 4F RT A21EA 20080728 SO 2008 7 28 MAS2008F00002 1 20080613 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FDM 6210 JFK-RDU. MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. MX LUBED ROLLERS OPS CHECKED GOOD. (B) 2 L 7 2 4T RT T00011AT 20080728 NM 2008 7 28 KCSA081313 1 20080705 A 5411 FRAME BOEING 747 747122 1384872 NM NR 2 NACELLE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 NR 2 PYLON LT SIDE FRAME IS CHAFFED AT FIRE BOTTLE AFT SUPPORT ATTACH POINT AT NAC STA. 162 (B) 2 L 7 4 4F RT A20WE 20080728 EA 2008 7 28 TRAX200800722 1 20080601 A 5530 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 708EV 10060 LT DRAG ANGLE APPEARS CRACKED PERFORMED ET INSPECTION OF SUSPECT CRACK IAW NDTM 51-20-006. FOUND ANGLE TO BE CRACKED. MARKED END OF CRACK. (B) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 AALA200801345 1 20080519 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 793AN 30255 DFW EMERGENCY LIGHT AT LT NUMBER ONE CLOSET DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LT NUMBER ONE CLOSE T DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 NM 2008 7 28 USAA920081193 1 20080513 A 5320 6545834 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - Q6 - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT, BS 323, RBL 11. REPLACED CABIN FLOOR SUPPORT, BS 32 3, RBL 11 IAW B737 SRM 51-10-02 AND 51-40-02. (S) 2 L 7 2 4F RT A16WE 20080728 NM 2008 7 28 USAABB08112 1 20080630 A 2910 271T45859 MODULE BOEING 767 767201 1385125 NM HYDRAULIC SYS LEAKING A USAA O OTHER K FLUID LOSS AP APPROACH 1 EA 19 250AY 23902 ARN FLT 752 EN ROUTE PHL ARN. DURING APPROACH, THE CENTER HYDRAULIC SYSTEM BEGAN TO DEPLETE. BY THE TIME THE FLIGHT LA NDED, THE CENTER HYDRAULIC SYSTEM WAS AT ZERO QUANTITY. THE AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE REPLACED THE C ENTER HYDRAULIC MODULE ASSEMBLY. OPERATIONAL AND LEAK CHECKS OK. (S) 2 L 7 2 4F RT A1NM 20080728 EU 2008 7 28 USAA920081261 1 20080616 A 5321 D5367521000000 FLOOR PANEL AIRBUS 320 A320232 3930326 EU CARGO BAY DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 679AW 2613 CLT - BC-2 - MAJOR REPAIR - DELAMINATION ON FLOOR PANEL 131EF IN FORWARD CARGO COMPARTMENT AT FR 28 - 31, BL Y765 TO Y-7 65. REPLACED FLOOR PANEL 131HF IN FORWARD CARGO COMPARTMENT AT FR 28 - 31, BL Y765 TO Y-765 IAW A320 SRM 53-02-00. (S) 2 L 7 2 4F RT A28NM 20080728 NM 2008 7 28 USAA920081286 1 20080630 A 5523 66C2038428 TAB BOEING 737 7374B7 1384702 NM ELEVATOR TAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 449US 24893 CLT - C2 - MAJOR REPAIR - CRACK ON RT ELEVATOR TAB AT NR 3 HINGE CUTOUT. REPAIRED RT ELEVATOR TAB AT NR 3 HINGE CUTOUT IAW TYPICAL REPAIR 55-20-03 AND B737 SRM 51-70-17. (S) 2 L 7 2 4F RT A16WE 20080728 EA 2008 7 28 A6WA200840422 1 20080514 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A A6WA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 31 437AW 7744 FLAP FAILURE AFTER TAKEOFF DURING RETRACTION FROM 20 DEGREES. FAILED AT 16 DEGREES. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4, FLAP SYSTEM RESET OK. (S) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 ASAA0843114 1 20080506 A 5320 69514113 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 FORWARD CARGO BAY INTERCOSTAL ANGLE CRACKED. REPLACED INTERCOSTAL PER SRM 53 30 04 51 40 05 AND 51 40 02. 2 L 7 2 4F RT A16WE 20080728 NM 2008 7 28 ASAA0843115 1 20080511 A 5340 693535214 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 STRINGER TIE CLIP CRACKED. REPLACED CLIP PER SRM 51 40 02. 2 L 7 2 4F RT A16WE 20080728 SO 2008 7 28 RAIA00806009 1 20080611 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 816HK 145055 MX - STL - EMERGENCY LIGHT 13 INOP. MAINTENANCE RELAMPED LIGHT ASSEMBLY. (S) 2 L 7 2 4T RT T00011AT 20080728 SO 2008 7 28 RAIA00806011 1 20080612 A 3240 38793500 SHUTOFF VALVE EMB 145 EMB145LR 3260212 SO BRAKE SYSTEM INOPERATIVE A RAIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 CE 03 811HK 145256 FLT 5507 - STL - INBOARD BRAKE INOP EICAS MESSAGE. MAINTENANCE REMOVED AND REPLACED BRAKE SHOT OFF VALVE. (S) 2 L 7 2 4T RT T00011AT 20080728 SO 2008 7 28 RAIA000806013 1 20080614 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 836HK 145695 PRE FLT 7988 - OKC - MAIN CABIN DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE DEFERRED THE MAIN DOOR EMERGENCY LIG HT IN ACCORDANCE WITH MEL PROCEDURES. (S) 2 L 7 2 4T RT T00011AT 20080728 SO 2008 7 28 RAIA00806003 1 20080608 A 2840 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO FUEL SYSTEM ACTIVATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 833HK 145240 FLT 7896 - DEN - ABORTED TAKEOFF - EI FUEL IMPENDING BYPASS EICAS MESSAGE. MAINTENANCE INSPECTED AND DEFERRED PER MEL. (S) 2 L 7 2 4T RT T00011AT 20080728 SO 2008 7 28 RAIA0080612 1 20080612 A 3231 22250100003 SOLENOID VALVE EMB 145 EMB145 3260210 SO NLG DEFECTIVE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 806HK 15617 465 145112 FLT 7990 - ALG - NLG DOOR WILL NOT CLOSE. MAINTENANCE REMOVED AND REPLACED DOOR SOLENOID VALVE. (S) 2 L 7 2 4F RT T00011AT 20080728 SO 2008 7 28 RAIA00806010 1 20080612 A 3230 23092900201 UPLOCK EMB 145 EMB145 3260210 SO NLG INOPERATIVE A RAIA K NONE O OTHER CL CLIMB 1 CE 03 803HK 23274 258 145077 FLT 3518 - BDL - NLG DID NOT RETRACT AFTER TAKEOFF. MAINTENANCE REMOVED AND REPLACED NLG UPLOCK BOX. (S) 2 L 7 2 4F RT T00011AT 20080728 EA 2008 7 28 REX2008F00004 1 20080702 A 2730 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA ELEVATOR JAMMED A REXA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 25 8554A 7554 ON SHORT FINAL ELEVATOR CONTROL BECAME WHAT APPEARED TO BE "JAMMING" INTERMITTENTLY. ELEVATOR SYSTEM CHECKED GOOD ON GR OUND. UPON FURTHER INSPECTION NOTICED VERTICAL STABILIZER VISOR PANELS DEFORMED. PANELS REMOVED, ELEVATOR ATTACHMENT P OINTS, ATTACHMENT HARDWARE, POWER CONTROL UNITS (PCU), PULLEYS, CABLES, PUSH RODS AND ASSOCIATED HARDWARE INSPECTED PER BOMBARDIER AMM WITH NO DEFECTS NOTED. VISOR PANELS DETERMINED NOT TO BE A PROBABLE CAUSE FOR "POSSIBLE JAM." VISOR PAR T NUMBERS RT UPPER 600-2113-44 RT LOWER 600-21134-44 NO SERIAL NUMBER. (S) 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 REX2008F00000 1 20080702 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A REXA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 8646A 7646 RECEIVED STAB/MACH TRIM CAUTION MESSAGE IN FLIGHT QRH FOLLOWED. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. MESSAG E CLEARED AFTER LANDING WITH NO REPEAT. ACFT WAS POWERED DOWN AND BACK ON. NO FURTHER MESSAGES RECEIVED. (S) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 2008UALA03356 1 20080612 A 3510 HOSE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OXYGEN MASK DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 598UA 28751 OXYGEN MASK HOSE DEFECTIVE AT 2 (1=CAPT, 2=1ST OF, 3= 1ST OBS). CREW COMMENTS: HOSE IS BROKEN. BROKEN MASK HOSE (UNKN OWN DAMAGE). REPLACED HOSE ASSY, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080728 NM 2008 7 28 2008UALA03488 1 20080619 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 DOOR 2R NEEDS REPAIR DOUBLER AT UPPER HINGE CUTOUT. ACCOMPLISHED MAJOR REPAIR AT GSO. ACP HFEC FOUND CRACK IN LW RT IN BOARD CORNER REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW MM. 2 L 7 2 4F 4 F RT A2NM E17NE 20080728 NM 2008 7 28 2008UALA03489 1 20080619 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 DOOR 2L NEEDS REPAIR DOUBLER AT UPPER HINGE CUTOUT. ACCOMPLISHED MAJOR REPAIR AT GSO. ACP HFEC NO DEFECT FOUND. INSTA LLED REPAIR DOUBLER IAW MM 52-11-87. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 NM 2008 7 29 HNA2008F00025 1 20080619 A 3350 OL3071BPEGPL BULB DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHTS BURNED OUT A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 931HA 50805 132 7TH FLOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPS CHECK GOOD. (K) 2 H 7 2 4T RT A13NM 20080819 NM 2008 8 19 SWAA084211 1 20080728 A 5753 6545321 FLAP TRACK BOEING 737 7373H4 1384600 NM T/E FLAP CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 336SW 23940 DURING SCHEDULED BRDG CHECK, FOUND RT WING NR 2 T/E AFT FLAP AFT ATTACH POINT CORRODED. REMOVED AND REPLACED FLAP TRACK PER SWA EA. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 ASAA0873273 1 20080731 A 5330 143A3232 SKIN BOEING 737 737790 13844CN NM BS 470-485 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 644AS 30795 BAG TUG HIT BELLY OF AIRCRAFT. FUSELAGE SKIN DENTED AT STA NR 480 BETWEEN STR 24L & 25L. INSTALLED EXTERNAL DOUBLER IAW SRM 53-00-01 REPAIR 3 REPLACED SHEAR TIE, PN 142A0023Y29. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084198 1 20080725 A 2560 416A15005 ESCAPE ROPE BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 450WN 32470 DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EMERGENCY ESCAPE ROPE MISSING. INSTALLED ESCAPE ROPE PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084218 1 20080729 A 3350 65C27093 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 458WN 33857 R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084220 1 20080729 A 5315 6546809 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 947, RBL 40 TO RBL 45. REMOVED AND REPLACED CHO RD PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084221 1 20080729 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084199 1 20080727 A 2560 P4010021 BATTERY BOEING 737 7373Y0 1384671 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED MV3 CHECK, FOUND FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084231 1 20080729 A 5311 6546529 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 440, STR 25L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084236 1 20080731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084242 1 20080731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084243 1 20080731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084244 1 20080731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084245 1 20080731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084253 1 20080731 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559, STR 14L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084255 1 20080731 A 3350 417A5601 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 919WN 36625 DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843227 1 20080624 A 5330 6545800696 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 323-355 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 FUSELAGE DENTED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 53 27. 2 L 7 2 4F 4 F RT A16WE E21EU 20080729 NM 2008 7 29 2008UALA03388 1 20080613 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 AFT PIT FRAME AT BS 1320 BETWEEN STR 25R-26R INBOARD FLANGE IS DENTED. ACCOMPLISHED MAJOR REPAIR AT GSO. REPAIRED IAW SRM 53-00-07 RPR 5. THIS IS A CAT B REPAIR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSP STARTING AT 50,000 TOTAL FLT CYCLES PER SRM 53-00-07 REPAIR 5 TBL II AND 12,000 FC THEREAFTER. INSP CONSIST OF BOTH VISUAL AND NDT. CURRENT PTC IS 14404. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 NM 2008 7 29 2008UALA03389 1 20080613 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 AFT PIT FS 1520 STR 26L HAS DENT IN FRAME. ACCOMPLISHED MAJOR REPAIR AT GSO. REPAIRED IAW SRM 53-00-07 REPAIR 5. THIS IS A CAT B REPAIR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSP STARTING AT 50,000 TOTAL FLT CYCLES PER SRM 53-00-07 RPR 5 T BL II AND 12,000FC THEREAFTER. INSP CONSIST OF BOTH VISUAL AND NDT. CURRENT PTC IS 144 04. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 SO 2008 7 29 SIM2008F00000 1 20080708 A 3240 21707 BRAKE ASSY EMB 145 EMB145LR 3260212 SO NR 3 DISINTEGRATED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 21 677GB 15096 145784 CREW REPORTED A LOT OF SMOKE COMING FROM RT MLG ON LANDING. THE CREW PUSHED ON THE BRAKES AND LOST APPROX 50 PERCENT OF BRAKING AND THEN CREW RECEIVED A BRAKE DEGRADED MESSAGE ON EICAS. THE NR 3 BRAKE DISINTEGRATED ON LANDING. ON POST FL IGHT A LOT OF DEBRIS WAS NOTED ON THE TARMAC LEADING UP TO THE GATE WHICH APPEARED TO BE BRAKE PARTS. AC REMOVED FROM S ERVICE. C/A REMOVED AND REPLACED NR 3 BRAKE AND TIRE ASSY. AIRCRAFT RETURNED TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20080729 NM 2008 7 29 HNA2008F00026 1 20080625 A 2422 WARNING LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT ILLUMINATED A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 942HA 163 REJECTED TO AT 45 KNOTS DUE TO SECONDARY INVERTER CAUTION LIGHT COMING ON DURING ROLL. GOT OFF THE RUNWAY AND CALLED MX CONTROL. DID NOT RETURN TO GATE, MEL WAS ISSUED. (K) 2 H 7 2 4T RT A13NM 20080729 EA 2008 7 29 VNA2008F00005 1 20080709 A 5240 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF343B1 30070 NE EXTERNAL COMMS OPEN A VNAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 05 716PS 10171 CREW REPORTED THE EXTERNAL COMMUNICATIONS DOOR LEFT OPEN. CREW RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAIN TENANCE INSPECTED AND FOUND NO DEFECTS. MAINT SECURED THE DOOR CLOSED. AC WAS RELEASED FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 20080729 NM 2008 7 29 WRL2008F00002 1 20080705 A 5730 ARB3954U8 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 274WA 48633 DURING 1C + 12A CHECK FOUND RT WING L/E SPLICE DOUBLER HAD CRACK AT STATION XORS 683. REPLACED DAMAGE DOUBLER IAW MD 11 SRM 51-35-01 VOL LL, REV 40 COND CHECK NORMAL AND JOB COMPLETED. (K) 2 L 7 3 4F RT A22WE 20080729 NM 2008 7 29 WRL2008F00001 1 20080706 A 5753 ARC4125T RIB DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 274WA 48633 DURING 4C + 12A, CHECK FOUND STOP RIB CRACKED AT LT OB FLAP. IAW DOCUMENT NR 08-57-56 SEC 1, ADJUST LT OB FLAP NR 2 UP STOP BOLT IN THE RIB COND CHK NORMAL. (K) 2 L 7 3 4F RT A22WE 20080729 NM 2008 7 29 WRL2008F00004 1 20080706 A 5753 RIB DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 274WA 48633 DURING 1C + 12A CHECK FOUND STOP RIB CRACKED AT RT OB FLAP. IAW DOCUMENT NR 08-57-57 SECTION 1, ADJUST RT OB FLAP NR 2 UP STOP BOLT IN THE RIB. COND CHECK NORMAL. (K) 2 L 7 3 4F RT A22WE 20080729 NM 2008 7 29 UIE2008F00013 1 20080604 A 5330 SKIN BOEING 747 74748EF 13848BL NM FUSELAGE CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 419MC 28367 FOUND FIBERGLASS SKIN PANEL 293CL CRACKED. REPAIRED IAW SRM 53-00-70 AND SRM 51-70-07. (K) 2 L 7 4 4F RT A20WE 20080729 NM 2008 7 29 UIE2008F00012 1 20080604 A 5330 SKIN BOEING 747 74748EF 13848BL NM FUSELAGE CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 419MC 28367 FOUND FIBERGLASS SKIN PANEL 294CR CRACKED. REPAIRED IAW SRM. (K) 2 L 7 4 4F RT A20WE 20080729 NM 2008 7 29 HNA2008F00018 1 20080627 A 2120 UNKNOWN DHAV DHC8 DHC8102 2809003 NM CABIN ODOR A HNAA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 07 906HA 9 UNKNOWN ELECTRICAL ODOR ACCOMPANIED BY LIGHT SMOKE. MAINT WAS ON AC FOR APPROX 2.5 HOURS, SUSPECT WATER GOT ON TOP OF A DVISORY DISPLAY PANEL WHICH WAS CURRENTLY MEL`D. (K) 2 H 7 2 4T RT A13NM 20080729 SO 2008 7 29 SIM2008F00006 1 20080713 A 2910 14570264401 HOSE EMB 145 EMB145 3260210 SO HYD SYSTEM LEAKING A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SW 21 612AE 145079 CREW REPORTED LOSS OF ENGINE 1 HYDRAULIC PRESS AND FLUID AFTER EXTENDING MLG ON LANDING. HYDRAULIC 1, LOW QUT MESSAGE I LLUMINATED ON CLIMB OUT/ AFTER LANDING GEAR ENGINE 1 HYDRAULIC FAIL MSG ILLUMINATED. LOST NW STEERING HAD TO BE TOWED T O GATE. AIRCRAFT REMOVED FROM SERVICE. C/A - REMOVED AND REPLACED LT HYDRAULIC HOSES IAW AMM 32-33-08 OPS CHECK GOOD. N O FURTHER DISCREPANCIES NOTED AT THIS TIME. AC RETURNED TO SERVICE. (K) 2 L 7 2 4F RT T00011AT 20080729 NM 2008 7 29 UIE2008F00015 1 20080614 A 2697 CONNECTOR BOEING 747 74747UF 1384812 NM FIRE WARNING SYS LOOSE A UIEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 497MC 29258 DURING CLIMB EICAS "FIRE WARNING". FOUND CONNECTOR LOOSE AND RETIGHTENED SAME. OPS AND INDICATION NORMAL ON THE GROUND IAW AMM 26-10-01. (K) 2 L 7 4 4F RT A20WE 20080729 NM 2008 7 29 2008UALA03390 1 20080613 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 AFT PIT FRAME STA 1480 STR 26L HAD DENT. ACCOMPLISHED MAJOR REPAIR AT GSO. REPAIRED IAW SRM 53-00-07 REPAIR 5. THIS I S A CAT B REPAIR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSP STARTING AT 50,000 TOTAL FLT CYCLES PER SRM 53-00-07 REPAIR 5 TBL II AND 12,000FC THEREAFTER. INSP CONSIST OF BOTH VISUAL AND NDT. CURRENT PTC IS 144 04. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 NM 2008 7 29 UIE2008F00022 1 20080707 A 5313 STRINGER BOEING 747 747243B 1384830 NM BS 396 S25L CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 540MC 22508 STA 396, STRINGER 25 L, FATIGUE CRACKED. REPLACED STRINGER IAW DWG 65B11089. (K) 2 L 7 4 4F RT A20WE 20080729 NM 2008 7 29 2008UALA03396 1 20080614 A 2697 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE LOOP DIRTY A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 547UA 25368 EICAS MSG - LEFT ENGINE FIRE LOOP 1. DIRTY CONNECTION. CLEANED ALL FIRE LOOP CONNECTORS ON NUMBER 1 ENG, SYS OPS CHECK ED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080820 NM 2008 8 20 ASAA0843253 1 20080624 A 5330 654577882 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 907-915 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 FUSELAGE SKIN IS DENTED. REMOVED DAMAGED AREA. INSTALLED FILLER DOUBLER AND TRIPLER PER SRM 53 00 01 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084260 1 20080731 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 777QC 30592 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 727D, RBL 8 TO LBL 8. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084261 1 20080731 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 777QC 30592 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, RBL 8 TO LBL 17. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0873254 1 20080730 A 5240 571411 BUTTON BOEING 737 737790 13844CN NM R1 DOOR FAILED A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 617AS 30542 CATERER UNABLE TO CLOSE R1 DOOR. REMOVED & REPLACED GALLEY SERVICE (R1) DOOR RELEASE BUTTON ASSY IAW MM 52 41 21. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084269 1 20080801 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 847, STR 17L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843224 1 20080701 A 5320 692471 ANGLE BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 312-336 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 FWD PASSENGER (L 1) DOOR LOWER CUTOUT Z ANGLE IS CORRODED. REPLACED ANGLE IAW SRM 51 40 02. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084272 1 20080801 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 331SW 23695 FUSELAGE SKIN CRACKED AT BS 757, STR 14R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843225 1 20080701 A 5310 65317875 CHANNEL BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU L1 DOORWAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 L 1 DOOR LOWER CUTOUT U CHANNEL IS CORRODED. REPLACED CHANNEL IAW SRM 51 40 02. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084274 1 20080801 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED CV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 526, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084284 1 20080803 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084285 1 20080803 A 5320 6545410 STIFFENER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND VERTICAL STIFFENER CRACKED AT BS 727B, RBL 45.50, WL 208. REMOVED AND REPLACED STIFFE NER PER SRM AND BOEING DRAWING. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084290 1 20080803 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084295 1 20080803 A 3350 8200048901 LENS BOEING 737 7377H4 1384404 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER NR NOT REPORTED 1 SW 29 464WN 32468 FWD CABIN EMERGENCY EXIT LIGHT LENS FELL OFF DURING FLIGHT. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084297 1 20080801 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED SPV CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084298 1 20080801 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 617SW 27700 DURING SCHEDULED SPV CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0873216 1 20080721 A 2913 66087 PUMP BOEING 737 737790 13844CN NM GE CFM56 CFM567B24 NE HYD SYSTEM FAILED A ASAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 02 626AS 16809 30793 888208 ON CLIMBOUT AT APPROX FL260 MASTER CAUTION LIGHT ILLUMINATED. NR 1 ENG DRIVEN HYD PUMP LOW PRESS. LIGHT ILLUMINATED NR 1 HYDRAULIC QTY INDICATED 60 PERCENT MOMENTARILY, EVENTUALLY THIS READING RETURNED TO 106 PERCENT AND REMAINED STABLE RA N QRH CHECKLIST NR1 HYD ENG PUMP REMOVED NR 1 ENG EDP REF MM 29-11-11-000-802-002-2 THROUGH 29-11-11-000-802-002-2 P5 ST EP 7 PUT CAPSON THE RETURN & CASE DRAIN BUT WILL NOT HOLD PRESSURE INSTALLED NR 1 ENG EDP IAW MM 29-11-11-400. OPS AND LEAK CHECK GOOD. ACCOMPLISHED TSR NR 0811960 FLUSHED OUT 'A' SYS HYD REF MM 29-11-00-170-801. OPS & LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 NM 2008 8 20 SWAA084304 1 20080803 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084305 1 20080803 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843268 1 20080625 A 5753 65C46430131 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 LT IB FORE FLAP T/E DENTED ON LOWER SURFACE ABOVE THE CENTER TRACK REMOVED DAMAGE FABBED FILLER & REPAIR PARTS, BONDED I AW SRM 51-70-10 REPAIR 4. 2 L 7 2 4F 4 F RT A16WE E21EU 20080819 WP 2008 8 19 UPS08852994 1 20080729 A 5753 STRUCTURE DOUG DC8 DC871F 302199D WP LT WING TE FLAP DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1, TWO HOLES IN LT FLAP EITHER SIDE OF FLAP STATION 219 BACKSIDE OF FLAP. CUT OUT DAMAGE, FABRICATED A ND INSTALLED 2EA REPAIR DOUBLERS IAW SRM 5 7-02-01 FIG 2Q,51-01-09, AND 51-01-21A 2 L 7 4 4F RT 4A25 20080819 NM 2008 8 19 UPS08M53033 1 20080721 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 13 RT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED AND INSTALED REP AIR BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 EU 2008 8 19 UPS08153064 1 20080810 A 2133 OUTFLOW VALVE AIRBUS A300 A300F4622R 3930360 EU CABIN PRESSURE INOPERATIVE A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 137UP 0820 CREW WAS UNABLE TO PRESSURIZE THE AIRCRAFT AFTER DEPARTURE. NR1 & NR2 AUTOMATIC CABIN PRESSURE CONTROLLERS INOPERATIVE. CREW SWITCHED TO MANUAL. MANUAL SYSTEM UNABLE TO CONTROL CABIN PRESSURE. NR1 AUTO PRESS SYS DEFERRED IAW MEL. REPLACED FWD OUTFLOW VALVE PER MM 21-31-12-04. PLACARD REMOVED. D382069 CLEARED. 2 L 7 2 4F RT A35EU 20080819 NM 2008 8 19 NWAA083615638 1 20080804 A 3242 BRAKE BOEING 757 757251 1384970 NM RT MLG MALFUNCTIONED A NWAA K NONE O OTHER TX TAXI/GRND HDL 1 GL 01 538US 26485 AFTER LANDING AND TRANSFER TO NORMAL BRAKES, THE FLIGHT CREW REPORTED THAT THE RT BRAKE PEDAL WENT ALL OF THE WAY TO THE FLOOR WITH NO BRAKING ACTION ON THE RT MAIN LANDING GEAR BRAKES. LT MAIN LANDING GEAR BRAKES OPERATED NORMALLY. ONCE IN THE GATE, MAINTENANCE FOUND THE BRAKES ON THE RT MAIN LANDING GEAR TO OPERATE NORMALLY. (S) 2 L 7 2 4F RT A2NM 20080819 NM 2008 8 19 NWAA083555509 1 20080731 A 2120 UNKNOWN BOEING 757 757251 1384970 NM CABIN ODOR A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 509US 23198 EN ROUTE THE CABIN CREW AND PASSENGERS REPORTED A STRONG, ACRID, ODOR LIKE BURNING PLASTIC THROUGHOUT THE ACFT. ACCORDI NG TO REPORTS SOME PASSENGERS REPORTED THAT THE FUMES WERE IRRITATING THEIR THROATS. THE FLIGHT CREW DECLARED AN EMERGE NCY, DIVERTED TO DSM AND LANDED UNEVENTFULLY. AT THE TIME OF THIS WRITING MAINTENANCE IS WORKING ON THE ACFT TRYING TO DETERMINE THE SOURCE OF THE FUMES. OPEN. (S) 2 L 7 2 4F RT A2NM 20080819 NM 2008 8 19 NWAA083663158 1 20080804 A 5330 SKIN AIRBUS A319 A319114 3930350 NM FUSELAGE PUNCTURED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 358NB 01897 DURING GROUND OPERATIONS LOWER FUSELAGE SKIN WAS PUNCTURED AT FR 58-59, S42R-S43R. REPAIRED PER EA 31-213006. (S) 2 L 7 2 4F RT A28NM 20080819 EA 2008 8 19 SWIA200819865 1 20080711 A 5210 PLUNGER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR HANDLE INOPERATIVE A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 984CA 7171 UNABLE TO OPEN MAIN CABIN DOOR. (FLIGHT NR 2791) INSPECTED AND CLEANED INNER HANDLE PLUNGER. REPLACED PAX DOOR WHEEL S PRING IAW MM 52-11-13. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080819 SO 2008 8 19 SWIA200819928 1 20080710 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 298SW 120328 UNDER FLOOR CROSSMEMBER AT ROW 9 MIDDLE RT CTR AREA IS CORRODED. (FOUND AT C-CHECK) REPLACED UNDER FLOOR CROSS MEMBER A T ROW 9 IAW SRM 51-40-02. 2 L 7 2 4T RT A31SO 20080819 WP 2008 8 19 UPS08853047 1 20080730 A 5240 DOUBLER DOUG DC8 DC871F 302199D WP SERVICE DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C1, CORROSION ON A DOUBLER INSIDE RT FWD SERVICE DOOR FWD TORQUE BOX JUST BELOW LOWER HINGE. REMOVED A ND REPLACED FITTING (DOUBLER) SRM 51-01-20D,51-03-00. 2 L 7 4 4F RT 4A25 20080819 NM 2008 8 19 UPS08M53039 1 20080710 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, CORROSION FOUND IN NR 2 RT BARREL NUT BORE HOLE, REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08553011 1 20080730 A 5415 SUPPORT BRACKET BOEING 757 75724APF 1384969 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 423UP 25325 INSPECTION TYPE-C2, THE UPR CONDUIT SUPPORT BRACKET IS CRACKED IN NR2 ENG PYLON HYD BAY AT AFT OB EDGE, NAS STA 278. RE MOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-02-0G, DRW PL313N3033. 2 L 7 2 4F RT A2NM 20080819 WP 2008 8 19 UPS08853048 1 20080729 A 5313 FITTING DOUG DC8 DC871F 302199D WP BS 1345 L28L GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C1, D PIT STA 1345 LONGERON 28L, LONGERON FITTING GOUGED AT RADIUS. REMOVED AND REPLACED FITTING IAW SR M 51-1-20D,51-3-2. 2 L 7 4 4F RT 4A25 20080819 EA 2008 8 19 TRAX200800957 1 20080802 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A ASOA K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 934EV 8028 FLAPS FAIL CAUTION MSG WHEN SELECTING FROM 20 TO 30 DEGREES (EMERGENCY DECLARED). REMOVED AND REPLACED FECU, PERFORMED TEST GOOD. OPERATED FLAPS NUMEROUS TIMES. OPS CHECK GOOD. NO MESSAGES NOTED REF CRJ200 AMM 27-51-05, 27-51-10 AND 27- 51-00. (S) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 2008UALA03398 1 20080614 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 550UA 25398 DOOR 3R NOT ARMING. REMOVED SLIDE AT DOOR 3R, LUBED ARMED, DISARMED BEARINGS AND OPS CHECKED SLIDE OPERATION. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 NM 2008 7 29 2008UALA03399 1 20080613 A 3350 COVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 EMERGENCY LIGHT STRIP ROW 34 NEEDS REPAIR. REPLACED BROKEN STRIP COVER. EMERGENCY LIGHT CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 EA 2008 7 29 TRAX200800746 1 20080604 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 669-977 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 LT CABIN SIDE SEAT RAILS HAVE CORROSION DAMAGE FS 669.40 TO FS 977.00. REPAIRED DAMAGED AREAS OF CABIN SIDE WALL SEAT R AILS FROM FS 669.40 TO 977.00 IAW SRM 53-41-49 AND SRM 53-51-49. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800745 1 20080604 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 349-669 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 RT CABIN SIDE SEAT RAILS HAVE CORROSION DAMAGE FS 349.00 TO FS 669.40. REPAIRED DAMAGED AREAS OF CABIN SIDE WALL SEAT R AILS FROM FS 349.00 TO 669.40 IAW SRM 53-21-49 AND SRM 53-31-49. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800737 1 20080603 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA BS 406 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 FS 406+128 BULKHEAD VERTICAL STIFFENER BEAM AT RBL 36 CRACKED AT INBOARD SIDE BOTTOM FASTENER APPROX 1/4" LONG. PERFORM ED REPAIR IAW REO 601R-53-41-189 AND REO 601R-53-41-476. (A) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 UIE2008F00004 1 20080701 A 5320 PUNCTURED PANEL BOEING 747 74747UF 1384812 NM BS 1660-1680 PUNCTURED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 496MC 29257 AFT CARGO COMPARTMENT TORQUE BOX TOP PANEL AT STA 1660 TO 1680 RT SIDE FOUND PUNCTURED AT 2 LOCATIONS. TORQUE BOX TOP P ANEL REPAIRED IAW EO. (K) 2 L 7 4 4F RT A20WE 20080728 CE 2008 7 28 MTN2008F00001 1 20080709 A 3220 26940022 SHIMMY DAMPENER CESSNA 208 208B 2073701 CE PWA PT6 PT6* 52043 EA NLG MALFUNCTIONED E MTNA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 EA 68 962FE 208B0078 ON TAKEOFF ROLL, A STRONG VIBRATION WAS COMING FROM NOSE LANDING GEAR. THE TAKEOFF WAS ABORTED AND THE AC RETURNED TO T HE RAMP. MAINT SERVICED THE SHIMMY DAMPENER AND RETURNED THE AC TO SERVICE. (K) 1 H 7 1 3T 3 T A37CE E2NE 20080728 CE 2008 7 28 GLB2008F00004 1 20080714 A 5330 SKIN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A6 52043 EA FS 293-300 S12R CRACKED A GLBA O OTHER O OTHER NR NOT REPORTED 1 NM 21 192GL UE192 BELLY SKIN CRACKED APPROXIMATELY 2 INCHES IN LENGTH AT FS 298.25 TO FS 300.25 APPROXIMATELY 5 INCHES OB OF STRINGER 12R AND APPROX 2 INCHES FROM OB EDGE OF BELLY SKIN. MAINTENANCE REMOVED DAMAGED SKIN AND PATCHED IAW SRM 53-90. PATCH 18 I NCHES BY 4.5 INCHES. .040. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1. (K) 2 L 7 2 4T 3 T RT A24CE E4EA 20080728 EU 2008 7 28 2008UALA03422 1 20080614 A 5210 CYLINDER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR LOOSE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 496UA 1845 R2 DOOR DAMPER EMERGENCY OPERATIONS CYLINDER PERCUSSION LEVER GUIDE LOOSE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 NM 2008 7 28 2008UALA03420 1 20080616 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 836UA 1460 EPSU L FWD FAULT. REPLACED EPSU (10WL). TESTS OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080728 NM 2008 7 28 MWE2008F00016 1 20080703 A 7830 FRAME BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE THRUST REVERSER CRACKED A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 918ME 55180 RT THRUST REVERSER UPPER DOOR Z-FRAME AT STA 35.669 HAS A CRACKED REPAIR AT THE RT END. FABRICATED AND INSTALLED DOUBLE R. (K) 2 L 7 2 4F 4 F TR A6WE E00061EN 20080728 EU 2008 7 28 MTN2008F00002 1 20080703 A 2913 4019501 PUMP AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE HYD SYSTEM INOPERATIVE A MTNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 68 907FX 286 AFTER DEPARTURE, THE BLUE HYDR SYS PRESSURE WENT TO -0-PSI. THE FLAPS WOULD NOT RETRACT, AFTER COMPLETING THE APPROPRIA TE CHECKLIST, THE CREW DECIDED TO RETURN TO DEPARTURE. AFTER TROUBLESHOOTING THE MECHANIC FOUND A BAD HYDR PUMP. (K) 2 H 7 2 4T 4 T RT A53EU E20NE 20080728 2008 7 28 UHL2008F00003 4 20080616 A 3400 COMPUTER EMB ERJ170 ERJ170100SE 3260406 NM GE CF34 CF34* 30015 NE MALFUNCTIONED A UHLA O OTHER O OTHER NR NOT REPORTED 1 GL 11 856RW 17000078 AT CRUISE ALTITUDE CREW RECEIVED AN EICAS MESSAGE ELEV THRU COMP FAIL. SHORTLY THEREAFTER WE NOTICED THE N1 AND ITT GAU GES ON BOTH ENGINE WERE FLUCTUATING WHILE IN CRUISE FLIGHT WITH NO ADJUSTMENTS TO THE THROTTLES. AS CREW STARTED THEIR DESCENT THEY RECEIVED AN EICAS MESSAGE "GROUND SPOILERS FAIL" AND SHORTLY AFTER RECEIVED "AOA LIMIT FAIL EICAS" MESSAGE. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE DOWNLOAD OF FHDB/DVDR FAULT CODES POINTING AT ADS P NR 3. MAINTENANCE RESET POWER, PERFORMED RTS TO VERIFY ALL FMC ARE GOOD AND CLEARED INHIBITS ON FLAP CHANNELS. MAINT ENANCE ACCOMPLISHED A FINAL RESET OF AIRCRAFT POWER, CYCLED FLAPS AND RAN ENGINES; ALL FAULTS CLEARED, NO CORRELATIONS F 2 L 7 2 4F 4 F RT A56NM 20080728 EU 2008 7 28 P4Y2008F00001 1 20080714 A 6123 8551 COMPUTER CASA CN235 CN235 2410306 EU GE CT7TP CT77A 30030 NE AUTOFEATHER FAILED E P4YA O OTHER O OTHER NR NOT REPORTED 1 EA 39 1269J 012 PILOT REPORTED AUTO FEATHER TEST INOPERATIVE ON THE LT ENGINE. MAINTENANCE REPLACED THE AUTO FEATHER COMPUTER AND RETUR NED THE AIRCRAFT TO SERVICE. (K) 2 H 7 2 4T 4 T RT A21NM E8NE 20080728 NM 2008 7 28 MWE2008F00014 1 20080703 A 7830 715K9004509 ANGLE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE THRUST REVERSER CRACKED A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 918ME 55180 RT THRUST REVERSER DEFLECTOR DOOR UPPER Z FRAME HAS A CRACKED REPAIR AT THE LT END AT STA 35.669. FABRICATED AND INSTAL LED ANGLE. (K) 2 L 7 2 4F 4 F TR A6WE E00061EN 20080728 NM 2008 7 28 UHL2008F00004 1 20080616 A 3250 STEERING SYS EMB ERJ170 ERJ170100SE 3260406 NM GE CF34 CF34* 30015 NE NLG MALFUNCTIONED A UHLA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 646RW 17000066 DURING APPROACH LANDING GEAR WAS SELECTED CREW RECEIVED AN EICAS MASTER CAUTION "STEER FAIL". CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINT CONTROL INSTRUCTED THE CREW TO RESET CIRCUIT BREAKER B-25, CLEARING THE PROBLEM AND THE AC TAXIED TO THE GATE UNDER OUR OWN POWER. MESSAGE WAS NOT ON EICAS WHEN MAINTENANCE ARRIVE ON AC. NOSE WHEEL STE ERING SYSTEM FUNCTION CHECK WAS ACCOMPLISHED NO DEFECTS NOTED. DISCREPANCY HAS NOT REPEATED THIS DATE. (K) 2 L 7 2 4F 4 F RT A56NM 20080728 EA 2008 7 28 TRAX200800633 1 20080514 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 978EV 7723 LT OTBD FLOORBEAM ANGLE CRACKED AT STA 280 BULKHEAD. REMOVED LT OTBD FLOORBEAM ANGLE AT STA 280 ALL WORK DONE IAW SR M 51-42-21. INSTALLED LT OTBD FLOORBEAM ANGLE AT STA 280 ALL WORK DONE IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 20080728 EA 2008 7 28 MASA200800454 1 20080607 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 928LR 15028 ASH FLT 2659 CLT-SAT. EMERGENCY LIGHT OUT AT ROW 7. MX RELAMPED AND SYSTEM CHECKED GOOD. (B) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 KCSA081291 1 20080619 A 5730 SKIN BOEING 747 747212B 1384886 NM RWS 538 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 21939 CORROSION ON RT. WING LOWER SKIN AT BOOST PUMP CUTOUT WS 538 (B) 2 L 7 4 4F RT A20WE 20080728 EA 2008 7 28 TRAX200800774 1 20080608 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 845AS 7324 1 EA LT AND RT AFT OVERWING EXITS LIGHTS INOP. REMOVED AND REPLACED NR 4 EMERG LIGHTING BATTERY PACK AND BATTERY CHARGE R IAW AMM`S 33-51-04 AND 33-51-05. OPS CHECK GOOD. CLEARED DEFER AND REMOVED PLACARD. 2 L 7 2 4F RT A21EA 20080728 CE 2008 7 28 DXTA200803135 1 20080621 A 2701 CONTROL COLUMN CESSNA 750 750 2076810 CE COCKPIT RATCHETING E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 989QS 7500089 CONTROL YOKE HAS A DEAD ZONE WHEN MOVING AILERON FROM NEUTRAL POSITION THEN "RATCHETS" RESULTING IN EXCESSIVE & JERKY I NPUT. (B) 2 L 7 2 4J RT T00007WI 20080728 EA 2008 7 28 MASA200800459 1 20080609 A 5220 SEAL CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT FOD A MASA O OTHER C F.O.D. NR NOT REPORTED 1 SW 07 918FJ 15018 ASH FLT 2734 PHX-LGB. RT OVERWING EMERGENCY EXIT SQUEALS IN FLT. MX REMOVED DEBRI FROM SEAL, CLEANED SEAL, AND APPLIED L UBE TO SEAL--OPS CHECK AND LEAK CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 KCSA081278 1 20080611 A 5315 FLOORBEAM BOEING 747 747122 1384872 NM BS1660 S49L DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 AFT PIT FLOORBEAM UPPER "I" CHORD DENTED AT BS1660 ABOVE STR-49L (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 KCSA081286 1 20080615 A 5315 FLOORBEAM BOEING 747 747122 1384872 NM BS 1800 RBL12 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 AFT PIT FLOORBEAM UPPER CHORD DENTED AT B.S.1800, RBL-12 TO RBL-18 (B) 2 L 7 4 4F RT A20WE 20080728 NM 2008 7 28 KCSA081294 1 20080621 A 5311 FRAME BOEING 747 747122 1384872 NM BS 1265 S26L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FUSELAGE FRAME WEB IS CRACKED AT STA. 1265, BELOW STR. 26L (B) 2 L 7 4 4F RT A20WE 20080728 EA 2008 7 28 TRAX200800621 1 20080512 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 833AS 7246 EMERGENCY EXIT LIGHT BY PAX DOOR ON WARDROBE, HAS CRACK ON LENS COVER. REMOVED AND REPLACED FLOOR-LIGHT EMERGENCY FLOODL IGHT LENS COVER IAW AMM 33-51-19. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 AALA20081336 1 20080518 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 649AA 24607 DFW EMERGENCY LIGHTS AT LT HAND OVERHEAD SEAT ROW 23 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LT HAND OVERHEAD SEAT ROW 23. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT A2NM 20080728 EA 2008 7 28 TRAX200800601 1 20080505 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 920EV 7810 TRANSVERSE BEAM CRACKED AT FS 280.0 LBL 12.0 IN UPPER RADIUS JUST O/B OF EMER EXTENSION CABLE PULLEY BRACKET. REPAIRED FS 280 TRANSVERSE BEAM BETWEEN LBL 9.0 AND LBL 12.0 IAW REO 601R-53-11-138. (B) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 AALA200801344 1 20080519 A 3350 LIGHT BOEING 777 777223 1385213 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 790AN 30251 DFW EXTERNAL EMERGENCY LIGHT AT LT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LT NUMBE R FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 NM 2008 7 28 KCSA081279 1 20080611 A 5730 SKIN BOEING 747 747122 1384872 NM RT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 RT WING UPPER SKIN CORRODED AT WBL 148, 6" FWD OF REAR SPAR (B) 2 L 7 4 4F RT A20WE 20080728 EA 2008 7 28 TRAX200800626 1 20080513 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 922EV 7822 EMERGENCY FLOOR LIGHTS AFT OF RT EMERGENCY EXIT INOP. REMOVED AND REPLACED EMERGENCY FLOOR LIGHT SEGEMENT NR 11 IAW AMM 33-51-01. OPS CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080819 SO 2008 8 19 C2XA08IA184 1 20080802 A 3397 W102382720N WIRE EMB 135 EMB135LR 3260305 SO SERVICE DOOR BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14514 145303 IAH - DURING MAINTENANCE INSPECTION THE EMERGENCY LIGHT ON THE SERVICE DOOR SWING ARM WAS FOUND TO BE INOPERATIVE. MAIN TENANCE REPAIRED BROKEN WIRE, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S ) 2 L 7 2 4F RT T00011AT 20080819 SO 2008 8 19 C2XA08ON163 1 20080805 A 2612 3601133500230C90 FIRE LOOP EMB 145 EMB145LR 3260212 SO NR 1 ENGINE INOPERATIVE A C2XA K NONE O OTHER DE DESCENT 1 SW 27 16546 15640 11891 145562 FLT 0970 - GEG - FLIGHT CREW REPORTED, ENG 2 FIRE DETECTION FAILED. MX FERRY FLIGHT TO ONT FOR REPAIR. MX PERSONNEL RE MOVED AND REPLACED ENG FIRE LOOP. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080819 SO 2008 8 19 C2XA08IA185 1 20080802 A 3350 7137216502 SIGN EMB 135 EMB135LR 3260305 SO CABIN DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14514 145303 IAH - DURING MAINTENANCE INSPECTION LT EMERGENCY EXIT IDENTIFIER AT THE EXIT ROW WAS FOUND TO BE INOPERATIVE. MAINTENAN CE INSPECTED THE LIGHT, RESECURED THE CONNECTIONS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR R ETURN TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080819 NM 2008 8 19 UPS08M53029 1 20080722 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 7 LT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING IAW E.O. MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 UPS08M52956 1 20080731 A 3350 BATTERY PACK DOUG MD11 MD11F 3023600 NM EMERGENCY LIGHT FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 289UP 48455 DURING PREFLIGHT, EMERGENCY LIGHT TEST FAILED. BATTERY LOW. REMOVED AND REPLACED RECHARGEABLE BATTERY, EMERGENCY LIGHTS , POWER SUPPLY. PERFORMED OPS TEST SYSTEM OK IAW MM 33-51-01-4. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 KPV2008F00000 1 20080806 A 2611 473054 SMOKE WARNING DHAV DHC8 DHC8103 1386005 NM CARGO BAY MALFUNCTIONED A KPVA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 13 829EX 146 (PIREP) SMOKE WARNING LIGHT CAME ON INTERMITTENTLY (FLICKERED ON/OFF). PERFORMED SMOKE WARNING TEST IAW DHC-8 MM 26-12- 00 PG 201. NO DEFECTS NOTED. (S) 2 H 7 2 4T RT A13NM 20080819 NM 2008 8 19 SWAA084145 1 20080727 A 3350 1619 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 358SW 26595 DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084153 1 20080725 A 3350 65C27093 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084173 1 20080728 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084188 1 20080728 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 6R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 2008 8 19 SWAA084219 4 20080729 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 634SW 27937 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084200 1 20080727 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 703SW 27837 R2 DOOR EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084201 1 20080727 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 EEPLS LENS MISSING AT ROW 2 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084226 1 20080729 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084228 1 20080729 A 2560 6949956 CABLE BOEING 737 7375H4 138449D NM EVAC SLIDE MISROUTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084230 1 20080729 A 5754 65C26602312A SLAT BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 20080728 EA 2008 7 28 TRAX200800629 1 20080514 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 RT 280 WEB CORRODED. OPEN (B) 2 L 7 2 4F RT A21EA 20080728 NM 2008 7 28 AALA200801354 1 20080520 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 771AN 29579 DFW EMERGENCY LIGHT AT SEAT ROW 20C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 20C. SYSTEM GROUND CHE CKED NORMAL OPERATION. (CLOSED) (A) 2 L 7 2 4F RT T00001SE 20080728 NM 2008 7 28 USAA920081319 1 20080630 A 5532 SKIN BOEING 757 757225 1384959 NM VERTICAL STAB DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925UW 22205 BFM - MAJOR REPAIR - C3 CHECK - VERTICAL STABILIZER RT SIDE REAR SPAR WEB SKIN HAS DELAMINATION, VERTICAL STABILIZER STA TION 150-175. REPAIRED VERTICAL STABILIZER RT SIDE REAR SPAR WEB SKIN, VERTICAL STABILIZER STATION 150-175 IAW B757 SRM 51-70-07. (S) 2 L 7 2 4F RT A2NM 20080728 NM 2008 7 28 ASAA0843133 1 20080506 A 5320 65479573 SILL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 AFT CARGO PIT DOOR SILL PLATE STA 783 TO 847 CORROSION AROUND FASTENER HOLES TOP AND BOTTOM OF PLATE CORROSION ON AFT CA RGO DOOR SILL PLATE AT BS 793 TO BS 847 WAS BLENDED OUT AND FOUND TO BE BEYOND ALLOWABLE LIMITS IAW 737 400 SRM 51 40 05 AND 51 40 02. REPAIR PERFORMED IAW B737 400 SRM. 2 L 7 2 4F RT A16WE 20080728 SO 2008 7 28 RAIA00806008 1 20080611 A 3350 RPS113 BATTERY PACK EMB 145 EMB145 3260210 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 802HK 145066 MX - STL - GALLEY EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. (S) 2 L 7 2 4F RT T00011AT 20080728 NM 2008 7 28 2008UALA03481 1 20080619 A 3213 CYLINDER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT MLG CORRODED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 525UA 24978 GLAND NUT AND CARRIER CORRODED, REMOVED INNER CYL FOUND. EXTENSIVE CORROSION ON INNER SURFACE OF OUTER CYL. REPLACED L T MAIN LANDING GEAR, GEAR SENT TO SHOP FOR OVERHAUL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080728 2008 7 28 DXTA200803124 4 20080614 A 3400 INDICATION SYS CESSNA 750 750 2076810 CE MULTIPLE FAIL E DXTA C ABORTED TAKEOFF G J MULTIPLE FAILURE WARNING INDICATION TO TAKEOFF 1 GL 07 948QS 7500149 AT AIRSPEED ALIVE, MACH TRIM & YD KICK OFF AND BOTH AMBER CAS MESSAGES ON EICAS. ABORTED T/O. (B) 2 L 7 2 4J RT T00007WI 20080729 NM 2008 7 29 2008UALA03604 1 20080627 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT ENGINE MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 776UA 26937 THE "L" GEN FAILS TO TAKE BUS AFTER ENG START. SUSPECT FAULTY IDG. REPLACED NR 1 ENGINE IDG PER MM 24-11-01. ACCOMPLIS HED LEAK CHECK AND OPERATIONAL CHECK OF ENGINE IDG, NO DEFECTS OBSERVED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080729 NM 2008 7 29 ZZDA2008126 1 20080628 A 2612 CONTROL MODULE BOEING 737 7377BD 1384511 NM FIRE WARNING MALFUNCTIONED A ZZDA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 37 336AT 36716 WHEEL WELL FIRE INDICATION AFTER TAKEOFF. PERFORMED FIM 26-18 TASK 802, RESEATED FIRE CONTROL MODULE LOOSE IN RACK. RE MOVED AND REPLACED FIRE CONTROL MODULE AS PRECAUTIONARY PER 26-18-07, SYS OP CHECK GOOD. 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 REX2008F00016 1 20080711 A 2731 SWITCH CNDAIR CL600 CL6002B19 1900309 EA STAB TRIM INOPERATIVE A REXA O OTHER F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 CE 21 827AY 8027 STAB TRIM RUN AWAY. CAPTAIN`S SWITCH NOT FUNCTIONING. MAINTENANCE FOUND NO STAB TRIM RUN AWAY. THE CAPTAIN`S SWITCH W AS NOT CONTROLLING THE TRIM. SWITCH WAS REPLACED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (K) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 UIE2008F00014 1 20080607 A 2997 WIRE BOEING 747 74747UF 1384812 NM HYD PUMP CHAFED A UIEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 499MC 29260 DURING CRUISE, EICAS ADVISORY "HYD PRESS ENGINE 1" ON HYD SYNOPTIC. NR EDP AND DEMAND PUMPS RUNNING. THEN NOTED EDP IN TERMITTENT AND IAW CHECKLIST EDP SWITCH OFF, BUT PUMP DID NOT SWITCH OFF. (EDP CONTINUED RUNNING INTERMITTENTLY AND DEMA ND PUMP RUNNING). LATER NOTICED THAT "EDP PRESS 1 CIRCUIT BREAKER WAS POPPED. ATTEMPTED RESET BUT C/B POPPED AGAIN. AF TER CONSULTING WITH MCC AND DISPATCH, DIVERTED. FOUND AND REPAIRED CHAFED WIRING AT EDP, DEPRESSURIZATION SOLENOID CONN ECTOR IAW WDM 29-11-01. NR 1 SYSTEM DEPRESSURIZATION SOLENOID CIRCUIT BREAKER RESET AND OPERATIONS CHECKED OKAY IAW 29- 17-00. (K) 2 L 7 4 4F RT A20WE 20080729 EA 2008 7 29 TRAX200800749 1 20080604 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 349-477 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 RT CABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE FS 349.00 TO FS 477.00. INSTALLED NEW RT CABIN FLOOR SEAT RAIL BETWEEN FS 349.00 TO 477.00 PER SRM 53-00-49. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800747 1 20080604 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 669-977 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 RT CABIN SIDE SEAT RAILS HAVE CORROSION DAMAGE FS 669.40 TO FS 977.00. REPAIRED DAMAGED AREAS OF CABIN SIDE WALL SEAT R AILS FROM FS 669.40 TO 977.00 IAW SRM 53-41-49 AND SRM 53-51-49. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800736 1 20080603 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA BS 409 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 FS 409+128 BULKHEAD VERTICAL STIFFENER BEAM AT LBL 9 CRACKED AT OUTBOARD SIDE LOWER RADIUS APPROX 1/4" LONG. REMOVED 2 CLAMPS FROM HYD LINES AT LBL 9 OUTBD TO ACCESS FOR REPAIR IAW SRM 51-41-02. REPAIRED IAW REO 601R-53-41-237 AND REO 601R -53-41-237. REINSTALLED 2 CLAMPS ON HYD LINE AT LBL 9 IAW AMM 20-22-01-220-801. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800757 1 20080605 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA BS 310 S26L/R CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 FRAME FS 310 IS CORRODED BETWEEN STR 26L AND 26R. CLEANED FRAME FOUND TO BE OUT OF LIMITS AT CENTER S26R, REMOVED FASTE NERS PER SRM 51-42-06. 2. REMOVED FASTENERS TO S25R PER SRM 51-42-06. FASTENERS AT LT TOP SIDE AT SPLICE 6 EACH STILL NEED TO BE REMOVED. (A) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800759 1 20080605 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA BS 295 S26L/R CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 AFT SIDE OF FRAME AT FS 295 IS CORRODED BETWEEN S26L AND S26R. BLENDED CORROSION WITHIN LIMITS PER SRM 53-00-01 ALODI NE, PRIMER, PAINT. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800756 1 20080605 A 5100 NONE CNDAIR CL600 CL6002C10 1390015 EA NO DAMAGE NONE A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 708EV 10060 CORROSION AT SUBFRAMES BETWEEN S26L/R AND S27 JUST FWD OF FS 364.00 AT AFT CORNER. UPON FURTHER INSPECTION NO CORROSION FOUND AT FS 346.00 S26L-26R. (B) 2 L 7 2 4F RT A21EA 20080729 2008 7 29 TRAX200800762 2 20080604 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA LEFT FAILED A ASOA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 935EV 8037 L ENG OIL PRESS MSG DURING FLT--ENROUTE TO PHF A/C DIVERTED TO CAE DUE TO MTC--EMERGENCY DECLARED, FLT 4898 DEL 169 MINS REMOVED AND REPLACED LT ENGINE ASSY IAW AMM 71-00-00 LEAK AND OPS CHECK GOOD NO DEFECTS NOTED. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800885 1 20080705 A 5530 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 SUSPECT CRACK ON LT SIDE VERTICAL STAB TO FUSELAGE DRAG ANGLE. (B) REFER TO STEPS 3-9 ON M-234 FOR WORK ACCOMPLISHED D K 7022603. REFER TO STEP NUMBER THREE ON M-234 FOR WORK ACCOMPLISHED FOR THIS STEP. 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800850 1 20080628 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA SLATS ILLUMINATED A ASOA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 717EV 10088 ON APPROACH SLAT FAIL CAUTION MSG RAN QRH CONTACTED MTC. RESET SYSTEM AND CLEARED INHIBITS PER MCC. FLT 4277 DEL 31 MINS . NC DISCREPANCY NO LONGER EXISTS. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800734 1 20080603 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA BS 409 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 FS 409.0+128 BULKHEAD VERTICAL STIFFENER BEAM AT LBL 27 AT INBOARD SIDE CRACKED APPROX 1/4" LONG AT BOTTOM FASTENER. (B) COMPLIED WITH REPAIR IAW REO 601R-53-41-056 AND REO 601R-53-41-056. (A) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800884 1 20080705 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 MAIN AVIONICS COMPARTMENT UNDER FLOOR CRAWLWAY, FLOORBEAM ANGLE IS CORRODED AT FS 280 STR 27. BLENDED OUT MINOR CORROSI ON IAW SRM 51-21-06. MATERAL REMOVED .003 IN OUT OF .006 IN MAX ALLOWED IAW SRM 53-22-55. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800886 1 20080705 A 5530 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTCAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 RIGHT SIDE VERTICAL TO FUSELAGE DRAG ANGLE IS CRACKED. REFER TO STEPS 2-9 ON M-234 FORM ATTACHED FOR WORK ACCOMPLISHED D K 7022603. REMOVED RT VERTICAL DRAG ANGLE PAINT IAW CRJ 700 SRM 51-26-00. (S) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800717 1 20080521 A 5210 601R317631 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 924EV 7830 THE PAX DOOR EXTERIOR HANDLE AND FLAPPER ARE CRACKED. REMOVED HANDLE AND REPLACED IAW AMM 52-11-03-400-802 AND SB 601R -52-119. ACCOMPLISH CLOSEOUT SECTION C AND INSTALLED PROXIMITY SWITCH TARGET ON DOOR HANDLE. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 ASAA0843123 1 20080507 A 5311 654655514 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 LEFT FRAME AT STA 867 CRACKED AT PSU RAIL BRACKET REPAIR PER EA 5310 02797. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843130 1 20080507 A 5311 90526911 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 RIGHT FRAME AT STA 747 AT PSU RAIL BRACKET CRACKED. REPAIRED PER EA 5310 02797. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0853171 1 20080706 A 8012 32896302 START VALVE BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE NR 2 ENGINE MALFUNCTIONED A ASAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 02 583AS 3835 35681 894764 WHILE TRYING TO START ENG NR 2 MOVED START SWITCH TO GND DID NOT GET A "START VALVE OPEN" LIGHT OR N2 INDICATION COMPLET ED FIM TASK 80 70 00 810 804 F00. DRY MOTORED ENGINE SUCCESSFUL, TWO ATTEMPTS NO FAULTS IN BITE CHECK RECENT OR HISTORI CAL. NO HISTORY 30 DAYS IN ARCTIC. BVI OF NR 2 STARTER AND VALVE NO FAULTS NOTED PER ETOPS MANUAL E05 00 05. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080729 NE 2008 7 29 ZZDA2008131 2 20080715 A 7200 BR700715A130 ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NR 1 FAILED A ZZDA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SO 37 940AT 55004 DEPARTING 12R THE LEFT ENGINE FAILED AT ABOUT 300' AGL. HIGH TGT NOTED. NO BIRDS SIGHTED. OVERWEIGHT LANDING AT 109K. FOUND NR 1 ENGINE FODDED DUE TO INTERNAL FAILURE. REMOVED AND REPLACED ENG IAW W/C 603 ON W/O 177916. ALL OPERATIONS NORMAL - AUTOLAND C/W ON T/C 625. 2 L 7 2 4F 4 F TR A6WE E00061EN 20080729 NM 2008 7 29 USAA920081173 1 20080524 A 2560 P4010021 BATTERY BOEING 757 7572B7 1384964 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 942UW 27807 MCN - EMERGENCY EQUIPMENT - ETOPS WINGLET MOD - MAIN CABIN FLASHLIGHT INOPERATIVE WHEN BATTERY LEADS ARE CONNECTED. REM OVED AND REPLACED BATTERY ON MAIN CABIN FLASHLIGHT. (S) 2 L 7 2 4F RT A2NM 20080729 NM 2008 7 29 USAA920081168 1 20080602 A 3350 20131A BATTERY PACK BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 308AW 24710 6110101 - MCN - RT OVERWING EMERGENCY EXIT LIGHT INOP. MX REPLACED THE BATTERY PACK. OPERATIONAL CHECK FAILED. MX REP LACED SECOND BATTERY PACK. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A16WE 20080729 EU 2008 7 29 USAA920081170 1 20080528 A 5347 D53472190203 SEAT TRACK AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 652AW 0953 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SEAT RAIL BEAM, BS 3158 FR 66, -Y1292. REPLACED CABIN SEAT RAIL BEAM , BS 3158 FR 66, -Y1292 IAW SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080925 WP 2008 9 25 08FDEA03882 1 20080915 A 5414 AWB710813 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 3 PYLON PANEL 487 HR IS CHAFED AND HAS BARE METAL. BLENDED AREA IAW SRM 54-00-01; VOL I. ORIGINAL MATERIAL THICKNES S, 0.071 IAW SRM 54-51-01; VOL III. MATERIAL LOSS 0.020. REMAINING THICKNESS 0.051. FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01;VOL I. FABRICATED PANEL IAW DWG AUB 7108; REV "A" ALODINED AND PRIMED IAW SRM 51-21-01; VOL II. PAINTED IA W SRM 51-21-01; VOL II. MARKED PANEL IAW GMM 7-0-1001. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03883 1 20080915 A 5315 FLOORBEAM BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 CABIN FLOORBEAM, BS 345, BL0 - RBL 10, UPPER CHORD CORRODED. REPAIRED FLOOR BEAM UPPER CHORD, BS 345, BL0 - RBL 10 IAW SRM 53-00-51, REPAIR NR 3. THIS IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING. 2 L 7 2 4F RT A2NM 20080925 EU 2008 9 25 08FDEA03798 1 20080910 A 5315 A5361220420000 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 THERE ARE TOOL MARKS ON THE FLOOR CAPS IN THE MAIN CABIN AT FRAME 11, LBL 20 TO RBL 10. REMOVED DAMAGE. MATERIAL ID FO R REPAIR. FABRICATED AND INSTALLED REPAIR IAW SRM 51-70-10. ALODINED AND PRIMED IAW AMM 51-75-10-8. 2 L 7 2 4F RT A35EU 20080925 WP 2008 9 25 08FDEA03921 1 20080917 A 5512 ALC1744503 SKIN DOUG MD10 MD1010F 3022112 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT HORIZONTAL STAB UPPER SKIN AT APPROX XE 72, STRINGER NR 11 IS CRACKED. REPAIRED SKIN PER EA 8-5510-123649. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03922 1 20080917 A 5320 6558504 INTERCOSTAL BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 LWR EXT FUSE WING BODY FRG SUPPORT FRAME INTERCOSTAL ASSY INT SURF IS CORRODED BS 773, LBL9- RBL 9, WL 140. FABRICATED NEW SPLICE PLATE AND INSTALLED, REF BOEING DWG 65-58504. REMOVED FRAME SUPPORT, REMOVED CORROSION ON SLICE PLATE MATERI AL LOSS 50 PERCENT OUT OF LIMITS. INSTALLED NEW SPLICE PLATE TO THE FRAME SUPPORT, INSTALLED FRAME SUPPORT AT BS 773, LBL 9-RBL 9, WL 140. INSTALLED TWO NEW BLOCK AND ROD ASSY ON FRAME SUPPORT REF SRM 51-30-02 PG 2-15. 2 L 7 3 4F A3WE 20080925 NM 2008 9 25 08FDEA03923 1 20080917 A 5347 53FX14971 SEAT TRACK BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 CORROSION AT ATTACH FASTENER ON SEAT TRACK, FS 1174, LBL25, WL 208 REMOVED CORROSION, NDT VERIFIED MATERIAL LOSS AND CHE CK FOR DEFECTS, NO DEFECTS WERE FOUND. ORIGINAL THICKNESS .065 INCH REMAINING .061 INCH MATERIAL LOSS .004 INCH WITHIN LIMITS. REF EA NR 7-5310-114032. TREATED AND PRIMED AREA REF SRM 51-10-02. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080822 NM 2008 8 22 F3LA200800470 1 20080714 A 5320 D5391550320010 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED CORROSION SEVERAL PLACES ON AFT MOST PROFILE AT FWD CARGO COMPARTMENT AFT OF FRAME C30. MAINT REMOVED AND REPLACED PROFILE IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 EU 2008 8 22 F3LA200800553 1 20080812 A 5315 D5347217220400 FLOORBEAM AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 806FR 30 2218 DURING C-CHECK, INSP NOTED 3 OB NUT CLIP HOLES CORRODED ON FLOORBEAM Y1292 (L-2) AT FR 67. MAINT REMOVED AND REPLACED F LOORBEAM IAW SRM 51-42-11, PARAGRAPH 5. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT 20080822 EU 2008 8 22 F3LA200800558 1 20080816 A 5320 D5348015800700 BLANKING PLATE AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 806FR 30 2218 DURING C-CHECK, INSP NOTED L2 AFT GIRT BAR BLANKING PLATE HAS CORROSION. MAINT REMOVED AND REPLACED BLANKING PLATE WITH NEW ONE FROM STOCK AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCE PTABLE. (S) 2 L 7 2 4F RT 20080822 NM 2008 8 22 F3LA200800530 1 20080731 A 5315 D5347217220400 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2 2209 DURING C3 C-CHECK, INSP NOTED 5 NUT CLIP HOLES CORRODED ON FLOORBEAM Y1292 (L-2) BETWEEN FRAME 66 AND FRAME 68. MAINT RE MOVED ALL FASTENERS FROM THE FLOORBEAM, REMOVED DAMAGED FLOORBEAM, AND INSTALLED NEW FLOORBEAM AND FASTENERS IAW SRM 51- 42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080822 SO 2008 8 22 SIMA200817504 1 20080620 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 654AE 145437 ON FLIGHT 4272, MAINTENANCE REPORTED EMERGENCY EXIT SIGN OVER FLIGHT ATTENDANTS JUMP SEAT, CEILING LIGHT BY GALLEY AND L IGHT BY STEP UP TO FLIGHT DECK INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY POWER SUPPLY ( HOLDER AND ELECTRONIC ASSY) NR 1 IAW EMB AMM 33-50-04. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080822 SO 2008 8 22 SIMA200816402 1 20080610 A 3230 35022022 ELECTRONIC UNIT EMB 135 EMB135LR 3260305 SO MLG MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 21 737MW 145396 ON FLIGHT 4816 - CREW REPORTED GEAR WOULD NOT RETRACT FOLLOWED BY AN AIR/GRND FAIL EICAS MESSAGE. AFTER LDG 1-2 WOW MES SAGE ON EICAS. NO EMERGENCY DECLARED AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LGEU PER CMC FINDINGS. GEAR SWINGS GOOD WITH NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080822 SO 2008 8 22 SIMA200817802 1 20080625 A 3230 ELECTRONIC UNIT EMB 145 EMB145LR 3260212 SO MLG MALFUNCTIONED A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 633AE 145148 ON FLIGHT 4113, CREW REPORTED WHEN AIRCRAFT BECAME AIRBORNE, "LG AIR/GND FAIL" MESSAGE APPEARED ON EICAS AND GEAR HANDLE WOULD NOT MOVE SO GEAR WOULD NOT RETRACT. RETURNED FOR LANDING WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMO VED AND REPLACED LANDING GEAR ELECTRONIC UNIT IAW EMB AMM 32-32-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVI CE. (A) 2 L 7 2 4T RT T00011AT 20080822 SO 2008 8 22 SIMA200818201 1 20080626 A 3234 745501 CONTROL LEVER EMB 145 EMB145LR 3260212 SO COCKPIT INOPERATIVE A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 633AE 145148 ON FLIGHT 3968 - CREW REPORTED AFTER TAKEOFF THEY RECEIVED LANDING GEAR AIR/GROUND FAIL AND FEAR WOULD NOT RETRACT. AIR CRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LT MAIN LANDING GEAR WOW PROX SW NR 2. OPERATIONAL CHECK GOOD. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER. REMOVED AND REPLACED CARDAN JOINT ON RT MAIN LANDING GEAR. FCF PASSED. AIRCRAFT RETURNED AT SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080822 SO 2008 8 22 SIMA200818401 1 20080701 A 3260 8005701 PROXIMITY SWITCH EMB 135 EMB135KL 3260302 SO NLG INOPERATIVE A SIMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 831AE 145616 ON FLIGHT 4431 - CREW REPORTED AFTER TAKEOFF LDG AIR/GND FAIL EICAS MESSAGE AND THE LANDING GEAR WILL NOT RETRACT. CREW ELECTED TO DIVERT TO ALB. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NOSE LANDING GEAR AIR/GROUND PROX SWITC H PER EMB 140 AMM 32-63-02. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080822 SO 2008 8 22 SIMA200816403 1 20080609 A 3260 852701 SQUAT SWITCH EMB 135 EMB135LR 3260305 SO LT MLG MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 728AE 145328 ON FLIGHT 4732 - AFTER TAKEOFF CREW REPORTED THAT WHEN GEAR HANDLE SELECTED UP THEY RECEIVED A LANDING GEAR AIR/GND FAIL MESSAGE AND GEAR WOULD NOT RETRACT. RETURNED TO RDU. AFTER LANDING RECEIVED MULTIPLE CAUTIONS/WARNINGS INCLUDING 1C 1 -2 WOW INOP, AHRS 1-2 BASIC MODE. AIRCRAFT. EMERGENCY WAS NOT DECLARED. AIRCRAFT REMOVED FROM SERVICE. FOUND LT GEAR SHOCK ABSORBER WOW SWITCH INOP. REMOVED AND REPLACED LT GEAR SHOCK ABSORBER WOW SWITCH IAW AMM 32-61-01. OPERATIONAL C HECK GOOD IAW AMM 32-60-08/32-63-00. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080822 SO 2008 8 22 C2XA08ON165 1 20080806 A 7933 23073715 SENSOR EMB 145 EMB145XR 3260214 SO RROYCE AE3007 AE3007A1E 54169 EA LT ENGINE TEMP INOPERATIVE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 13161 5722 2990 14500805 FLT 0043-BOI, FLIGHT CREW REPORTED E1 HIGH OIL TEMP ON CLIMBOUT OF GEG TO ONT. E1 WAS SHUT DOWN INTENTIONALLY AND FLIGH T WAS DIVERTED TO BOI WHERE IT LANDED SAFELY WITHOUT INCIDENT. ALSO OVERWEIGHT LANDING WAS REPORTED. CONTRACT MAINTENA NCE REMOVED AND REPLACED THE E1 OIL TEMP SENSOR AND C/W OVERWEIGHT COMPLIANCE CHECKS. OPERATIONALLY CHECKED SATISFACTOR Y AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4F 4 F RT TE6CH 20080822 WP 2008 8 22 NWAA083739961 1 20080730 A 2130 UNKNOWN DOUG DC9 DC931 3022065 WP CABIN PRESSURE UNKNOWN A NWAA B G EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 GL 01 924RW 47185 WHILE IN CRUISE AT FL350 THE CABIN PRESSURE STARTED TO CLIMB. CREW DESCENDED TO FL330 IN AN ATTEMPT AT CABIN PRESSURE C ONTROL WHICH DID MAINTAIN SETTING UNTIL TOP OF DESCENT. AT THAT POINT, WITH ANT-ICE ON DUE TO WEATHER AND WITH THROTTLE S RETARDED FOR DESCENT, THE CREW LOST CONTROL OF CABIN PRESSURIZATION AND THE OXYGEN MASKS DEPLOYED. CREW DECLARED AN EMERGENCY AND PERFORMED A RAPID DESCENT TO 10,000 FEET. FLIGHT LANDED AT OPF WITHOUT FURTHER INCIDENT. NO CORRECTIVE M AINTENANCE ACTION WAS PERFORMED AS AIRFRAME WAS BEING DELIVERED TO OPF FOR DECOMMISSIONING. (S) 2 L 7 2 4F A6WE 20080822 EA 2008 8 22 VNAA0808003 1 20080804 A 5200 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE ELECTRICAL PANEL OPEN A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 718PS 10175 CREW ELECTED TO RETURN TO CLT FOR GROUND POWER DOOR LEFT OPEN. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED A CFT WITH NO DEFECTS NOTED. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E00063EN 20080822 EA 2008 8 22 QXEA200800874 1 20080811 A 3240 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA BRAKES UNKNOWN A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 19 604QX 10019 SEA - ON LANDING ROLL OUT THE ACFT PULLED RT WITH EQUAL BRAKING APPLIED. TEMPS 01 LT AND 04 RT. MAINTENANCE PERFORMED AN INSPECTION OF THE BRAKES WITH NO DEFECTS NOTED. PERFORMED A TAXI CHECK AT VARIOUS SPEEDS WITH NO DEFECTS NOTED. COU LD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED. (S) 2 L 7 2 4F RT A21EA 20080822 WP 2008 8 22 NWAA083749759 1 20080812 A 3350 FUSE DOUG DC9 DC941 302207N WP EMERGENCY LIGHT FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 759NW 47287 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAI LED. MAINTENANCE REPLACED THE ASSOCIATED FUSE IN THE POWER SUPPLY PACK IN THE FIRST CLASS EMERGENCY EXIT LIGHT AT DOOR 1R. OPS CHECK WAS GOOD. (S) 2 L 7 2 4F A6WE 20080822 NM 2008 8 22 2008UALA03817 1 20080710 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1420 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 AFT PIT FRAME DENTED AT INBOARD FLANGE, BS 1420 BETWEEN STR 25L - 26L, 2 PLACES. ACCOMPLISHED MAJOR REPAIR AT GSO. CUT OUT DAMAGE AND INSTALLED DOUBLER RPR PER SRM 53-00-07, RPR 5. CREATED FOR REQUIRED REINSPECTIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 20080822 SO 2008 8 22 SIMA200822204 1 20080808 A 3240 9067404 VALVE EMB 135 EMB135KL 3260302 SO BRAKES FAILED A SIMA O OTHER F FLT CONT AFFECTED LD LANDING 1 SW 21 809AE 16578 145521 ON FLIGHT 4600 CREW REPORTED UPON TOUCHDOWN ALL FOUR BRAKES LOCKED AND ALL FOUR TIRES BLEW OUT. THE WHEEL RIMS WERE GRO UND AWAY AND CAUSED A LOT OF SPARKS AND FLAMES. THE TOWER CALLED CRASH, FIRE RESCUE AND REPORTED AN ACFT FIRE. THE PAS SENGERS PERFORMED AN EMERGENCY EVACUATION ON THE ACTIVE RUNWAY. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED FOUR M AIN LANDING GEAR TIRES AND BRAKE ASSEMBLIES. REMOVED AND REPLACED BRAKE VALVE. ACCOMPLISHED HIGH DRAG AND SIDE LOAD IN SPECTIONS, PERFORMED FUNCTIONAL CHECKS OF MAIN BRAKE AND FREE FALL SYSTEM. FUNCTIONAL CHECKS GOOD. RE-INSTALLED RT AND LT EMERGENCY EXIT DOORS AND RESET CIRCUIT BREAKERS. ACFT RETURNED TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080822 SO 2008 8 22 C2XA08IA189 1 20080804 A 4930 M4951830 FUEL NOZZLE EMB 145 EMB145XR 3260214 SO APU DIRTY A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 34110 5437 5437 145658 IAH - FLIGHT 2532, THE CREW REPORTED A STRONG FUEL ODOR DURING TAKEOFF AND CLIMB, THAT WENT AWAY ONCE THE APU BLEEDS WER E CLOSED AND THE APU SHUT DOWN. THE ACFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PLACED THE APU ON MEL 49-00-0 0 CAT-"C" CONTROL 151787, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. ON 08/05/08 TYS MAINTENANCE REMOVED AND REPL ACED THE APU FUEL NOZZLES, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED. THE MEL WAS REMOVED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080822 NM 2008 8 22 KCSA081380 1 20080813 A 5311 FRAME BOEING 747 747122 1384872 NM BS 1315 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 716CK 19753 CORROSION ON DOUBLER ON TOP OF RT OVERWING LONGERON AT BS 1315, RBL 123, WL 158. (S) 2 L 7 4 4F RT A20WE 20080822 NM 2008 8 22 KCSA081382A 1 20080811 A 5340 ATTACH ANGLE BOEING 747 747249F 1384849 NM BS 440 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 BS 440 S10R LT SIDE FRAME AFT SIDE, STRINGER ATTACH ANGLE CRACKED IN RADIUS .250 INCH CRACK MARKED UPPER DECK. (S) 2 L 7 4 4F RT A20WE 20080822 WP 2008 8 22 ABXA080215 1 20080805 A 3350 60030451 BATTERY PACK DOUG DC9 DC941 302207N WP EMERGENCY LIGHT DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 182 47513 COCKPIT EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY BATTERY PACK IAW DC9 MM 33-51-00. OPS CHE CKED GOOD. (S) 2 L 7 2 4F A6WE 20080822 NM 2008 8 22 USAA920081502 1 20080808 A 5313 6545775 STRINGER BOEING 737 7374B7 1384702 NM BS 727 S26R CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 427US 24549 CLT- RON - MAJOR REPAIR - CORROSION ON STRINGER AT BS 727G S26R. REPAIRED STRINGER AT BS 727G S26R IAW US AIRWAYS EA100 591. (S) 2 L 7 2 4F RT A16WE 20080822 CE 2008 8 22 GUU2008F00034 1 20080809 A 2150 ACM BEECH 1900 1900D 1154162 CE ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 17 81533 UE137 FLIGHT 9128 VPS/TPA. DURING DESCENT ACM BLOWS BURNING ODOR OUT OF FLOOR WHEN HEAT IS DECREASED IN MANUAL MODE. RAN ENG S AND PERFORMED OPERATIONAL CHECK OF ACM SYSTEM IN MANUAL AND AUTO MODES. NO ODOR NOTED. (S) 2 L 7 2 4T RT A24CE 20080822 SO 2008 8 22 C2XA08SH110 1 20080819 A 5540 12007255003 HINGE EMB 145 EMB145LR 3260212 SO RUDDER DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15912 145439 SHV - DURING C-CHECK RUDDER NR 2 UPPER HINGE UPPER HAT BUSHING MIGRATED. MAINTENANCE REMOVED AND REPLACED RUDDER 2 UPPE R HINGE IAW EMB 145 SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080825 EA 2008 8 25 COMA086355 1 20080809 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 310 DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 965CA 7131 PASSENGER DOOR CUTOUT AIRFRAME SIDE FWD LOWER CORNER EXISTING REPAIR IS DAMAGED. REPAIRED PASSENGER DOOR CUTOUT AIRFRAM E SIDE LOWER FWD CORNER PER CRJ REO 601R-53-21-180 REV (A) AND SR99-5140-0001 SECTION 1. (S) 2 L 7 2 4F RT A21EA 20080825 SO 2008 8 25 SIMA200822402 1 20080809 A 3230 22230100003 SOLENOID VALVE EMB 135 EMB135KL 3260302 SO NLG FAILED A SIMA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 SW 21 853AE 145742 ON FLIGHT 3111 CREW REPORTED FLYING AT 11,000. AT 310KTS A LOUD BANG WAS HEARD FROM NOSE AREA AND THEN A LOUD ROAR UNTI L LANDING GEAR WAS DOWN AND LOCKED, 3 GREEN AND NO CMC INDICATIONS WITH NO EICAS MESSAGES. EMERGENCY WAS DECLARED. LAN DING WAS NORMAL. ACFT WAS TOWED TO THE GATE FROM THE RUNWAY AND PASSENGERS DEPLANED AT GATE. ACFT REMOVED FROM SERVICE . REMOVED AND REPLACED NOSE LANDING DOOR SOLENOID VALVE IAW EMB 140 AMM 32-33-021. OPERATIONAL CHECK GOOD. ACFT RETUR NED TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080825 NM 2008 8 25 USAA920081500 1 20080810 A 5330 6545776 SKIN BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 PHX - B CHECK- MAJOR REPAIR - CRACK ON FUSELAGE SKIN AT BS 927 S26R. REPAIRED FUSELAGE SKIN AT BS 927 S26R IAW B737 SRM 53-00-01 REPAIR 31. (S) 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084268 1 20080801 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084271 1 20080801 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED MV2 CHECK, FOUND RT AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084314 1 20080803 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, LBL 8 TO LBL 13. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843271 1 20080625 A 5753 65C46430131 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 LT IB FORE FLAP T/E IS DENTED ON LOWER SURFACE ABOVE IB TRACK REMOVED DAMAGE. FABBED FILLER & DOUBLER & BOUNDED REPAIR IAW SRM 51-70-10 REPAIR 2. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843272 1 20080625 A 5753 65C2632017 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU LT WING TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 LT OB MID FLAP LOWER SURFACE IS CHAFED ABOVE NR 2 FLAP TRACK FAIRING. IB & OB SIDES REMOVED DAMAGE FABBED FILLER & DOUBL ER & BONDED IAW SRM 51-70-10, REPAIR 4. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843283 1 20080624 A 5330 65C3235719 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 355-379 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 DENT IN FUSELAGE SKIN ALONG STR 17L OVER 2 RIVETS AT STA 375 REMOVED PREVIOUS REPAIR REMOVED DAMAGED AREA FABBED FILLERS + DOUBLERS + INSTALLED REPAIR IAW EA NR12755. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843298 1 20080624 A 5330 6546881175 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 1088 S24L DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 FUSELAGE SKIN DENTED STA 1088 STR 24L REMOVED DAMAGE FABRICATED AND INSTALLED DOUBLER AND STRUCTURAL FILLER IAW ASA EA 5 330-02372. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843303 1 20080716 A 5330 65C323621 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 855-881 CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 FUSELAGE SKIN CHAFED FROM DORSAL FIN FWD SEAL BLENDED AREA FABRICATED AND INSTALLED REPAIR DOUBLER SPLICE STRAPS AND TAP ERED FILLERS IAW SRM 53-60-01 REPAIR 10 PROCEDURE II. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843296 1 20080629 A 5315 65C3394016 FLOORBEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 294 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 FLOORBEAM UPPER CHORD AT STA 294.5 FROM RBL 26-RBL 50 IS CORRODED UNDER FWD GALLEY REMOVED DAMAGED AREA FABBED REPAIR PA RTS & REPAIR ANGLES & INSTALLED IAW SRM 53-10-51 FIG 201. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843305 1 20080624 A 5754 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU NR 6 SLAT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 NR 6 SLAT HAS 3 DENTS IN T/E WEDGE UPPER SURFACE 19-32" FROM IB END PREPAIRED DAMAGED AREA FABRICATED REPAIR PARTS & BON DED IAW SRM 51-70-10, REPAIR 4. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843299 1 20080625 A 5753 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU NR 7 FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 RT OB MID FLAP CHAFED ABOVE NR 7 FLAP TRACK FAIRING. REMOVED DAMAGED AREA FABRICATED AND INSTALLED FILLER AND DOUBLER I AW SRM 51 70 10 REPAIR 4. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843308 1 20080625 A 5753 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 RT IB FORE FLAP HAS SEVERAL DENTS ON THE LOWER SURFACE ABOVE THE IB TRACK REMOVED PREVIOUS REPAIR & FACTORY DOUBLER FABB ED REPAIR DOUBLER & BLENDED REPAIR IAW SRM 51-70-10 REPAIR 2. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843302 1 20080626 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU NR 3 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 NR 3 SPOILER DENTED ON LOWER SURFACE 4" IB OF OUBD END & 5" AFT OF FWD EDGE PREPAIRED DAMAGED AREAS FABRICATED REPAIR DO UBLERS & BONDED REPAIR IAW SRM 51-70-10 REPAIR 2. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843252 1 20080625 A 5754 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 RT OB AFT FLAP LOWER SURFACE IS DENTED. INSTALLED BONDED DOUBLERS IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843243 1 20080701 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU NR 3 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 NR 3 SPOILER LOWER SURFACE IB T/E IS DENTED. INSTALLED DOUBLERS AND BONDED REPAIRS IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084331 1 20080804 A 5311 6546563 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 967, STR 27L TO STR 27R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080820 2008 8 20 ASAA0853318 4 20080803 A 3442 6225132633 TRANSCEIVER BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE WX RADAR SYS FAILED A ASAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 02 577AS 25547 35186 WX FAIL MESSAGE ILLUMINATED INTERMITTENTLY FOR 15 MIN THEN HARD FAILED SEVERAL MINUTES LATER THE ASSOCIATED PWS FAIL ILL UMINATED, BOTH STAYED ON FOR REMAINDER OF FLT. FOUND WXR RT DEAD, WOULD NOT EVEN TEST. REPLACED WXR R/T REF MM 34-43-41 OPS CK OK. PART VERIFICATION COMPLETED. GROUND VERIFICATION COMPLETED. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 NM 2008 8 20 SWAA084321 1 20080804 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084323 1 20080804 A 5311 6546595 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843232 1 20080627 A 5347 655384410 CARGO TRACK BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 911-947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AFT CARGO TIE DOWN TRACK IS CORRODED. REPLACED TIE DOWN TRACK IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0853263 1 20080802 A 2421 762185H GCU BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 1 ENGINE FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 579AS 5630 35187 DURING ENGINE APU FIRE SYS TEST (TASKCARD 74126002 STEP 2.E) NR 1 ENGINE IDG RESISTANCE BETWEEN PINS 2 AND 3 OF CONNECTO R DP 1206 MEASURED 69K OHMS IN THE "ON" POSITION (MINIMUM IS 230K OHMS). SUSPECT NR 1 GCU. NR 1 GCU REPLACED & INSTALLA TION TEST CARRIED OUT SERVICEABLE IAW AMM 24-21-01-400-801. NR 1 ENG IDG RESISTANCE BETWEEN PINS 2 & 3 OF CONNECTOR DP12 06 MEASURED SERVICEABLE AT 241 KOHMS (MIN. 230KOHMS) IAW ENG APU FIRE EXT SYS TEST TC 74126002 STEP 2E. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 2008 8 20 ASAA0853249 4 20080730 A 3442 6225132633 TRANSCEIVER BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE WX RADAR SYS FAILED A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 570AS 30416 35185 "PWS FAIL" ILLUMINATED ON NAV DISPLAY ON TAXI IN. DUPLICATED FAULT ALONG W WXR FAIL FALG. ALSO FOUND UNKNOWN FLUID, COFF EE, SODA ON TOP & ON TRAY OF WXR R/T. CLEANED FLUID FROM TRAY & AREA. REPLACED WXR RT REF MM:34 43 41. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 2008 8 20 ASAA0853250 4 20080730 A 3442 6225132633 TRANSCEIVER BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE WX RADAR SYS FAULTED A ASAA O OTHER J WARNING INDICATION LD LANDING 1 NM 02 583AS 4120 35681 DURING LANDING ROLL "PWS FAIL" ILLUMINATED ON BOTH CAPT AND FONAV DISPLAY. WEATHER RADAR OPERATED NORMAL INFLIGHT. VE RIFED DISCREPANCY PWS FAIL ANNUNCIATED ON BOTH CAPT'S & FO'S DISPLAY. CYCLED WRX CB GROUND VERIFICATION TEST PASSED REF MM 34-43-00. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 2008 8 20 SWAA084328 4 20080804 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084340 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084346 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084347 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0873221 1 20080723 A 5280 113A81005 DOOR BOEING 737 737790 13844CN NM LT MLG OUT OF ADJUST A ASAA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 NM 02 609AS 32211 29752 UNUSUAL VIBRATION FELT IN FLOOR OF AC DURING FLIGHT, STRONGEST VIBRATION IN OVERWING AREA AT CABIN. ALSO A SUBTLE YAWING MOTION FELT IN REAR GALLEY AREA EVERY FEW SECONDS. PASSENGER OBSERVED LT IB FLAP TRACK FAIRING WAS VIBRATING. PRECAUT IONARY EMERGENCY DECLARED & AC DIVERTED. (CREW REPORTED NO NOISE ASSOCIATED WITH VIBRATION) DURING CONDITIONAL INSPECTIO N OF MLG WING DOORS, FOUND LT MLG WING DOOR OUT OF ADJUSTMENT.ADJUSTED LT MLG WING DOOR IAW MM TASK 32-12-21-000-801 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0853193 1 20080716 A 2421 7588429101 FILTER BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 1 IDG TRIPPED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 558AS AAAH004485 35177 ON SCWA FOUND NR1 ENG IDG DPI POPPED ACCOMPLISHED FIM TASK 24-11-00-810-803 AND EA 2410-01025. RAN ENG AND RED BUTTON IS NOT EXTENDED. FAULT CORRECTED REF STEP F1(B). 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 EA 2008 8 20 TRAX200800604 1 20080506 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 826AS 7210 ENTRANCE EMERGENCY LIGHT BASE BROKEN (RESOLVED ON W/O: 89597 TASKCARD: N/R-00002) R/R ENTRANCE EMERGENCY LIGHT ASSY IAW CRJ 200 AMM 33-51. OP CK GOOD.--[SDR CLOSED](B) 2 L 7 2 4F RT A21EA 20080820 NM 2008 8 20 ASAA0853204 1 20080719 A 2131 2193301AA CONTROLLER BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE CABIN PRESSURE FAULTED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 558AS 7971 35177 "AUTO FAIL" LIGHT ILLUMINATED. PERFORMED FIM TASK 21-31-00-810-801. FAULT NO LONGER EXISTS. GROUND VERIFICATION TEST SU CCESSFUL. PERFORMED TEST ON NR1 & NR 2 CONTROLLERS. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 NM 2008 8 20 ASAA0853205 1 20080719 A 4990 38810521 FILTER BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE APU TRIPPED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 587AS 35684 APU FILTER DELTA P INDICATOR POPPED. 41-91-13 INSPECTION AND LEAK CHECK IAW TASK49-91-13-600-801. REMOVED AND REPLACED OIL FILTER REF MM 49-91-12-000-802.GND VERIFICATION SUCCESSFUL. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 EA 2008 8 20 TRAX200800605 1 20080506 A 3234 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A ASOA K NONE J WARNING INDICATION CL CLIMB 1 SO 27 854AS 7382 LANDING GEARS FAILED TO RETRACT AFTER TAKEOFF, "PARK BRAKE SOV" AND ANTI SKID INBD" MESSAGES SHOWN. EMERGENCY DECLARED. FOUND DI11 FAULT IN PSEU, L/G CNTRL HANDLE. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE IAW CRJ-200 M/M 32-31-01. PERFORMED FUNCTIONAL TEST OF L/G EXT/RET SYSTEM. IAW CRJ-200 M/M 32-30-00, NO DEFECTS. PBSOV AND ANTI-SKID INBD MSG`S RELATED TO L/G HANDLE FAULT. A/C OK FOR SERVICE.--[SDR CLOSED](B) 2 L 7 2 4F RT A21EA 20080820 NM 2008 8 20 ASAA0843328 1 20080728 A 5310 65C323945 BEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 601 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 776AS 25109 BS 601, STUB BEAM INNER HORD LOWER FASTENER HOLE CRACKED REPAIRED IAW EA 5310-02807. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 EA 2008 8 20 SWIA200819801 1 20080502 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 614SK 10051 LOWER FLOOR WEB AT FS280 IS CORRODED. (FOUND AT C-CHECK) REPLACED LOWER FLOOR WEB AT STA280 IAW SRM 51-42-21-001-001-A0 1 AND 51-42-13-0011-001-A01. 2 L 7 2 4F RT A21EA 20080820 EA 2008 8 20 SWIA200819803 1 20080507 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 764SK 10229 FS 280 FLOORBEAM AT LBL 10 IS CRACKED. (FOUND AT C-CHECK) REPLACED FLOORBEAM IAW SRM 51-42-06-001-001-A01 AND SB 670BA- 53-026 REV B, AND SB670-53-11-047, REV D. 2 L 7 2 4F RT A21EA 20080820 SO 2008 8 20 SWIA200819881 1 20080421 A 2497 WIRE EMB 120 EMB120ER 3260203 SO DC RELAY BOX DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 301YV 120301 DAMAGED WIRE W206-0051019 FOUND IN LT DC 1 RELAY BOX. (FOUND AT C-CHECK) REPLACED THE WIRE IAW EMB 120, WDM 21-51-00 AN D THE RCCB IAW MM 24-52-05. OPS CHECKS GOOD. 2 L 7 2 4T RT A31SO 20080820 NM 2008 8 20 ASAA0843195 1 20080701 A 5330 6546881115 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU BS 1028 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 LT EXTERNAL FUSELAGE DENT ABOVE REPAIR AT STA 1028, STR 13L, CUTOUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND INSTALLE D IAW DRM 53-80-01, FIG 201, REPAIR 3. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843198 1 20080701 A 5330 65C357978 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU BS 1001 S5L DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 LT EXTERNAL FUSELAGE PROTRUDING DENT AT STA 1001 ON STR 5L CUT OUT DAMAGED AREA FABRICATED FILLER DOUBLER AND TRIPLER LO CATED DRILLED AND INSTALLED IAW EA 5330-02364 AND EA 12771. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 EA 2008 8 20 SWIA200819854 1 20080423 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 955SW 7817 RT AFT ENGINE MOUNT THRUST FITTING IS CORRODED. (FOUND AT C-CHECK) REPLACED THRUST FITTING IAW AMM 71-22-01-400-801. 2 L 7 2 4F RT A21EA 20080820 EA 2008 8 20 SWIA200819855 1 20080423 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 955SW 7817 LT ENGINE MOUNT THRUST FITTING IS CORRODED. (FOUND AT C-CHECK) REPLACED THRUST FITTING ON IAW AMM 71-22-01-400-801. 2 L 7 2 4F 4 F RT A21EA E15NE 20080820 NM 2008 8 20 SWAA084566 1 20080813 A 5330 6545776 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 923, STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080819 SO 2008 8 19 C2XA08SH098 1 20080724 A 5320 14522178005 SILL EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27152 145759 SHV - DURING C-CHECK CORROSION UNDER THRESHOLD AT SERVICE DOOR. MX REMOVED AND REPLACED SERVICE DOOR CENTER SILL IAW EM B 145 XR SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080819 SO 2008 8 19 C2XA08SH099 1 20080724 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11181 14500904 SHV - DURING C-CHECK CORROSION ON CENTER OMEGA BEAM AT FR 20. MX REMOVED AND REPLACED CENTER OMEGA BEAM BETWEEN FR 18-2 4 IAW EMB 145 XR SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080819 EA 2008 8 19 SWIA200819914 1 20080728 A 3397 BALLAST CNDAIR CL600 CL6002B19 1900309 EA CABIN LIGHTS FAILED A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 927SW 7693 ELECTRICAL SMOKE ODOR IN CABIN. (FLIGHT NR 5933) REPLACED OVERHEAD LIGHT BALLAST NEAR ROW 4 IAW AMM 33-21-00. OPS CHEC K GOOD. 2 L 7 2 4F RT A21EA 20080820 NM 2008 8 20 SWAA084527 1 20080817 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 232WN 32500 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084542 1 20080817 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 759, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084539 1 20080817 A 5753 65C34062 SKIN BOEING 737 7373H4 1384600 NM FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED SPV CHECK, FOUND LT WING FORE FLAP UPPER SKIN DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 F3LA200800345 1 20080617 A 5321 D5367314700000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 REFERENCE NON ROUTINE 34384. DURING C3 S1 C-CHECK INSP NOTED AFT CARGO FLOOR PANEL 152WG HAS A DENT AND A HOLE. MAINT REPAIRED FLOOR PANEL 152WG IAW SRM 53-02-00 REPAIR 204 AND REPAIR 207. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800448 1 20080710 A 5320 D5323099920000 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE WORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED BEAM NR FOUR AT AFT WALL MOUNT HAS EXCESSIVE PLAY AT MOUNT AT FLOOR TRACK IN THE FWD CARGO COM PARTMENT. MAINT REMOVED AND REPLACED BEAM NR FOUR AFT WALL MOUNT FITTING IN THE FWD CARGO COMPARTMENT IAW SRM 51-72-11 P AGE 1 AND 2. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 ASAA0843315 1 20080630 A 5320 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AFT PIT FLOOR SUPPORT AT STA 767, LBL 12.50 IS CORRODED REMOVED DAMAGED AREA FABBED REPAIR PARTS AND INSTALLED IAW EA 53 20-01844. 2 L 7 2 4F 4 F RT A16WE E21EU 20080821 WP 2008 8 21 I5HA0858005D 1 20080405 A 5100 340311020789 ANGLE CVAC 580 580 2422806 WP DAMAGED A I5HA O OTHER O OTHER NR NOT REPORTED 1 GL 25 581P 29 DURING A STORM (MIA) A CARGO CAN (ULB) WAS THROWN INTO THE RT SIDE OF N581P. THE RT PROPELLER WAS ALSO STRUCK A GLANCIN G BLOW. THERE WAS SIGNIFICANT DAMAGE TO THE SKIN AND SUPPORT STRUCTURE BENEATH THE SKIN. THERE WAS DAMAGE TO WIRING IN THE AREA. THE NOSE STEERING ACTUATOR WAS ALSO DAMAGED. DAMAGE AREA WAS BETWEEN FUSELAGE STATIONS 72 TO 125 AT APPROXI MATELY BETWEEN STRINGERS 11 AND 3. THE PROPELLER AND REDUCTION GEARBOX WERE REMOVED AND INSPECTED. NO DAMAGE TO EITHER . N581P WAS REPAIRED AND THE ACFT TEST FLOWN ON JULY 3, 2008. THE ACFT WAS RETURNED TO SERVICE JULY 8, 2008. (S) 2 L 7 2 4T RT 20080821 NM 2008 8 21 F3LA200800461 1 20080711 A 5320 D5367415100000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 940FR 2465 DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151GE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00, FIGURE 204. UP ON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800288 1 20080602 A 5315 D5347218920400 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 DURING C-CHECK INSP, NOTED FLOORBEAM 1292 RT AT FRAME 68 CORROSION IN OB NUTCLIP HOLE. MAINT INSTALLED NEW FLOORBEAM Y12 92 FROM FRAME 68 TO FRAME 69 IAW THE REQUIREMENTS OF SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FO UND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800293 1 20080604 A 5315 D5347218820400 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 DURING C-CHECK INSP NOTED CORROSION ON BEAM Y1292 LT UPPER OB SIDE NUTCLIP HOLE AT FRAME 68. MAINT REMOVED CORRODED FLOO RBEAM Y1292 AND INSTALLED NEW FLOORBEAM FROM FRAME 68 TO FRAME 69 IAW SRM 51-42-00 AND DRAWINGS D53472780, D53472816 AND E53473250. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA20080030 1 20080611 A 5321 D5367160000000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP NOTED CABIN FLOOR PANEL 251SF HAS LARGE PUNCTURE HOLE. MAINT REPAIRED PANEL 251SF IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 EU 2008 8 21 F3LA200800364 1 20080616 A 5320 D5367415100000 PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 941FR 2483 DURING C-CHECK INSP, NOTED AFT PIT TRANSITION PANEL 151GE HAS SEVERAL PUNCTURES. MAINT REPAIRED PANEL 151GE IAW SRM 53- 02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 SWAA084395 1 20080806 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM EMEGENCY LIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 717SA 27851 DURING SCHEDULED HC1 CHECK, FWD LT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080821 2008 8 21 2008UALA03720 4 20080703 A 2310 5309045 COUPLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HF RADIO FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 589UA 28707 R HF RADIO FAIL TO TRANSMIT BUT RECEPTION IS GOOD. COUPLER IS FAULTY. REPLACED COUPLER. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NM 2008 8 21 SWAA084407 1 20080807 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080821 2008 8 21 SWAA084363 4 20080805 A 2565 6557463 FITTING BOEING 737 7373H4 1384600 NM R2 DOOR SLIDE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE AFT FITTING CRACKED. REMOVED AND REPLACED FITTING PER SR M. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084368 1 20080805 A 3350 65C27093 LIGHT BOEING 737 7373A4 1384585 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084379 1 20080806 A 3350 LENS BOEING 737 7373K2 13844BA NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084415 1 20080807 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM BS 435 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 435, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03082 1 20080529 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 5F FWD AND AFT LIGHT ASSY'S. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080821 NM 2008 8 21 SWAA084423 1 20080809 A 3350 101114 LENS BOEING 737 7375H4 138449D NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 L1 DOOR SIDEWALL EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084424 1 20080808 A 3350 311500 LIGHT BOEING 737 7373A4 1384585 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED 1/2D BRDG CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084385 1 20080806 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 922 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 922, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03285 1 20080606 A 2913 PTX30080093 TRANSDUCER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HYD PRESSURE FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 774UA 26936 FOUND LATCHED HYD PUMP PRI C2 MSG. *S/D* SUSPECT FAULTY PRESSURE TRANSDUCER. REPLACED PRESSURE TRANSDUCER, OP CHECKED OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080822 NM 2008 8 22 F3LA200800500 1 20080719 A 5320 D5347112420100 SHEAR PLATE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK, INSP NOTED THE RT LATERAL SHEAR PLATE AT Y-1162, FROM FRAME 69 TO FRAME 70, HAD CORROSION AND FOUR SHEAR ED FASTENERS AT THE FWD EDGE. MAINT REMOVED AND REPLACED THE LATERAL SHEAR PLATE AT Y-1162 AT FRAME 69 TO FRAME 70 IAW SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800336 1 20080611 A 5321 D5367175900300 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP NOTED FLOOR PANEL 262EF HAS SEVERAL PUNCTURES. MAINT REMOVED AND REPLACED FLOOR PANEL IAW REQUIREMEN TS OF WORK CARD CP753-36. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 EU 2008 8 22 F3LA200800519 1 20080722 A 5343 D59831 SUPPORT AIRBUS A318 A318111 3940019 EU LANDING GEAR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 802FR 39 1991 DURING SCHEDULED MAINT TASK CARD TC32711-02, INSP NOTED A CRACK ON THE FWD ANTI-ROTATION LUG. MAINT REMOVED AND REPLACE D THE UPPER SUPPORT ASSEMBLY IAW THE REQUIREMENTS OF ENGINEERING AUTHORIZATION A8-32R-30496. UPON COMPLETION OF THE REP AIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F RT 20080822 EU 2008 8 22 F3LA200800421 1 20080707 A 5320 D53670099 SHEAR PLATE AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 805FR 1660 DURING C-CHECK INSP NOTED CORROSION AROUND FAR RT NUTCLIP HOLE ON SHEAR PLATE ALONG FRAME 68 BETWEEN Y765 AND Y1292. MAI NT REMOVED SHEAR CONNECTING PLATE, FABRICATED AND INSTALLED SHEAR CONNECTING PLATE IAW DRAWING D53670099 AND SRM 51-42-1 1. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT 20080822 NM 2008 8 22 F3LA200800479 1 20080711 A 5320 D5397497200200 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED CORROSION ON THE AFT CARGO COMPARTMENT PROFILE AT FRAME C56. MAINT REMOVED AND REPLACED PROFIL E IN AFT CARGO COMPARTMENT AT FRAME C56 IAW A319 SRM 51-72-11 AND 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECT ED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM 20080822 NM 2008 8 22 F3LA200800462 1 20080711 A 5321 D5367403400000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 940FR 2465 DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151HE DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPO N COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 SO 2008 8 22 SIMASUP200817803 1 20080625 A 2810 CAP EMB 145 EMB145LR 3260212 SO FUEL CELL OPEN A SIMA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SW 21 620AE 145102 ON FLIGHT 4431, CREW REPORTED ON THE GROUND. LT WING TANK FUEL CAP CAMEO OPEN IN FLIGHT. FUEL CAP WAS ONLY SECURED BY THE LANYARD. CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO THE FIELD. AIRCRAFT REMOVED FROM SERVICE. COMPLIED W ITH FUEL CAP SEAL INSPECTION. RE-INSTALLED CAP, NO DEFECTS NOTED. INSPECTED SURROUNDING AREAS. NO DEFECTS NOTED AIRCR AFT RETURNED TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080822 EU 2008 8 22 SIMA200817804 1 20080616 A 5311 FRAME SAAB SF340 340B 7860101 EU BS 258 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 394AE 340B394 DURING A HMBV INSPECTION, A PREVIOUS REPAIR ON FLOOR FRAME 258.0 WAS FOUND CORRODED. REMOVED THE DAMAGED FILLER PLATE A ND CLEANED THE AREA. FABRICATED A FILLER, DRILLED HOLES, CLEANED, TREATED AND INSTALLED FILLER. REPAIR DONE IAW SAAB 3 40 SRM (SRM 72LKS 3079 REV 50) CHAPTER 53-70-30. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4T RT A52EU 20080822 NM 2008 8 22 KCSA081381 1 20080813 A 5320 ANGLE BOEING 747 747122 1384872 NM BS 1379 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 716CK 19753 INSIDE LONGERON BOX TEE ANGLE AT WL 113, STA 1379, RBL 115 CORRODED. (S) 2 L 7 4 4F RT A20WE 20080822 NM 2008 8 22 KCSA081380A 1 20080811 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 460 S12L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 BS 460 S12L FRAME DOUBLER AFT SIDE, CRACKED .375 INCH AT STRINGER CUTOUT, INBOARD UPPER CORNER. CRACK MARKED UPPER DECK . (S) 2 L 7 4 4F RT A20WE 20080822 NM 2008 8 22 USAA920081503 1 20080807 A 5311 6558280 FRAME BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT-Q6 - MAJOR REPAIR - CRACK ON FRAME AT BS 360 BETWEEN S8L & S9L. REPAIRED FRAME AT BS 360 BETWEEN S8L & S9L IAW US A IRWAYS TYPICAL REPAIR 53-10-20E. (S) 2 L 7 2 4F RT A16WE 20080822 NM 2008 8 22 USAA920081504 1 20080731 A 5311 6546554 FRAME BOEING 737 7373B7 1384580 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT-Q6 - MAJOR REPAIR - CRACK ON FRAME AT BS 847 BETWEEN S8L & S9L. REPAIRED FRAME AT BS 847 BETWEEN S8L & S9L IAW US A IRWAYS TYPICAL REPAIR 53-10-20E. (S) 2 L 7 2 4F RT A16WE 20080822 WP 2008 8 22 AALA200801824 1 20080709 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 594AA 53284 LGA - EMERGENCY LIGHTS IN MID CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 20DEF FOR EMERGENCY LIGHTS IN MID CA BIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A6WE 20080825 EU 2008 8 25 USAA920081494 1 20080806 A 5347 D5347209300000 SEAT TRACK AIRBUS A319 A319112 3930323 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 PIT - S4-MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK BEAM BETWEEN FR67 & FR68, -Y765. REPLACED SEAT TR ACK BEAM BETWEEN FR67 & FR68, -Y765. (S) 2 L 7 2 4F RT A28NM 20080825 EU 2008 8 25 USAA920081513 1 20080812 A 5315 D5347219420800 FLOORBEAM AIRBUS A319 A319112 3930323 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 PIT - S4-MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, Y512. REPLACED FLOORBEAM AT FR66, Y512 IAW A319 SRM 51-42-11. (S) 2 L 7 2 4F RT A28NM 20080825 NM 2008 8 25 USAA920081533 1 20080731 A 5320 D53471124200 SHEAR PLATE AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 833AW 1844 SAL - BC4 - MAJOR REPAIR - GALVANIC CORROSION ON SHEAR PLATE AT FR69 TO FR70, Y1297. REPLACED SHEAR PLATE AT FR69 TO FR 70, Y1297 IAW A319 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080825 NM 2008 8 25 KCSA081402 1 20080816 A 7120 MOUNT BOEING 747 747249F 1384849 NM NR 2 ENGINE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 NR 2 PYLON AFT ENG MOUNT HAS 9 HOLES ELONGATED AT WL 145, LAL 1 TO RBL 9 FOR AFT ENG MOUNT BULKHEAD WEB FRAMES ATTACH AT NAC STA 221.9. (S) 2 L 7 4 4F RT A20WE 20080825 NM 2008 8 25 KCSA081403 1 20080816 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2030 S34R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 716CK 19753 EXTERNAL FUSELAGE SKIN IS DAMAGED AT AFT SIDE OF BULK CARGO DOOR CUTOUT AREA AT STA 2030, STR 34R. (S) 2 L 7 4 4F RT A20WE 20080825 NM 2008 8 25 KCSA081392 1 20080815 A 5411 FRAME BOEING 747 747249F 1384849 NM NR 2 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 NR 2 PYLON REAR ENG MOUNT BULKHEAD LT FORWARD FRAME WEB IS CRACKED (.250 INCHES) AT 221.9, LBL 5, WL 148.5. (S) 2 L 7 4 4F RT A20WE 20080825 NM 2008 8 25 NSV2008F00019 1 20080807 A 2916 975265 RELIEF VALVE BOMBDR DHC8 DHC8402 1390042 NM HYD RESERVOIR LEAKING A NSVA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 27 195WQ 1088 4195 NR 1 HYD FAILURE IN FLIGHT, NO FLUID IN NR 1 RESERVOIR. NO PRESSURE IN NR 1 SYSTEM. RAN QRH, LANDED FLAPS 0 AND EMERGE NCY BRAKE. SKYDORL LEAKING FROM LT SIDE OF ACTF WHERE WING ROOT MEETS FUSELAGE. REMOVED AND REPLACED RELIEF VALVE ON N R 1 SYSTEM IAW Q400 AMM 29-11-51-000-801. PERFORMED LEAK AND OPS CHECK GOOD IAW Q400 AMM 29-11-51-710-801. NO LEAKS FO UND. P/N ON 975255-5, S/N OFF 0238, S/N ON 0039. (S) 2 H 7 2 4T RT A13NM 20080825 EA 2008 8 25 COMA086346 1 20080811 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 640 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 477CA 14838 7670 LT SIDE 640 FRAME CRACKED. REPAIRED LT FS 640 FRAME, PER REO 601R-53-061, 601R-53-506, 601R-61-569, & 601R-53-61-366. (S) 2 L 7 2 4F RT A21EA 20080825 NM 2008 8 25 AALA200801836 1 20080530 A 5347 141T5121 SEAT TRACK BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AA 22327 AFW - SEAT TRACK HAS CORROSION REMOVAL. REPAIRED PER MRB 767 3216. (S) 2 L 7 2 4F RT A1NM 20080825 NM 2008 8 25 AALA200801835 1 20080605 A 5320 145T8750 WEB BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AA 22327 AFW - CLOSURE PANEL WEB, PRESSURE DECK HAS CORROSION REMOVAL. MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIRED PER MR B 767 3214. AREA OF DISCREPANCY IS A DEPTH OF 0.082 INCHES. (S) 2 L 7 2 4F RT A1NM 20080825 SO 2008 8 25 C2XA08SH103 1 20080809 A 5230 14523918001 SKIN EMB 145 EMB145XR 3260214 SO CARGO DOOR CORRODED A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 14180 14500900 SHV - DURING C-CHECK IT WAS FOUND THAT THE CARGO DOOR INNER SKIN HAD AREAS OF CORROSION. MAINTENANCE REMOVED THE CORROS ION BY BLENDING AND PERFORMED A DOUBLER REPAIR IAW EXPRESSJET EC5230-01189. THE ACFT WAS APPROVED FOR RETURN TO SERVICE . (S) 2 L 7 2 4F RT 20080825 NM 2008 8 25 KCSA081400 1 20080816 A 5313 STRINGER BOEING 747 747249F 1384849 NM BS 990 S45R CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 FUSELAGE STRINGER IS CORRODED AT STA 990, STR 45R. (S) 2 L 7 4 4F RT A20WE 20080825 CE 2008 8 25 DXTA200803218 1 20080807 A 2130 UNKNOWN CESSNA 680 680CE 2076811 CE CABIN PRESSURE UNKNOWN E DXTA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 GL 07 388QS 6800113 IN THE DESCENT, CABIN PRESSURE BEGAN TO CLIMB AT 6000 FPM THEN DESCEND AT 6000 FPM. DEPLOYED THE PAX OXYGEN MASKS AND I NITIATED AN EMERGENCY DESCENT. (S) 2 L 7 2 4F RC T00012WI 20080825 WP 2008 8 25 IXX2008F00082 1 20080609 A 5730 SKIN DOUG DC8 DC872F 302199E WP RT WING DENTED A IXXA O OTHER O OTHER NR NOT REPORTED 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBD FLAP UPPER SKIN DENTED AT STATION XW 104.000. REMOVED FASTENERS A S NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PA RT. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 1 ITEM "D", DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-3-0 AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080825 NM 2008 8 25 KCSA081391 1 20080815 A 5411 FRAME BOEING 747 747249F 1384849 NM NR 2 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 NR 2 PYLON REAR ENG MOUNT BULKHEAD LT AFT FRAME WEB IS CRACKED (.750 INCHES) AT 221.9, LBL 5, WL 148.5. (S) 2 L 7 4 4F RT A20WE 20080825 NM 2008 8 25 AALA200801837 1 20080530 A 5347 141T5121 SEAT TRACK BOEING 767 767223 1385123 NM BS 341 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AA 22327 AFW - SEAT TRACK HAS CORROSION REMOVAL. REPAIRED PER MRB 767 3216. (S) 2 L 7 2 4F RT A1NM 20080825 2008 8 25 DXTA200803228 4 20080815 A 3160 DISPLAY CESSNA 500 560CESSNA 2076750 CE COCKPIT FAILED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 309QS 5600509 TURNED ON AVIONICS - FMS HAD NO SCREEN (SCREEN BLACK) AND DETECTED SMOKE, KTEB. (S) 2 L 7 2 4F RT A22CE 20080825 SO 2008 8 25 C2XA08CL096 1 20080808 A 2560 P4010030 BATTERY EMB 145 EMB145LR 3260212 SO FLASHLIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14974 145161 CLE FLIGHT 2522, THE CREW REPORTED THE CAPTAIN` S EMERGENCY FLASHLIGHT WAS DIM. MAINTENANCE INSPECTED AND REPLACED THE CAPTAIN`S FLASHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4T RT T00011AT 20080825 NM 2008 8 25 AALA200801879 1 20080715 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 657AM 24615 DFW - EMERGENCY LIGHT AT SEAT 21D INOPERATIVE. REPLACED CONNECTOR AT SIDEWALL FOR EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A2NM 20080825 NM 2008 8 25 2008UALA03794 1 20080708 A 3350 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 549UA 25397 DURING EMERGENCY LIGHTS TEST BOTH RT OVERWING AND LT AFT OVERWING LIGHTS INOP. BATTERY FAILURE. REPLACED BATTERY ON M1 0770 PWR SUPPLY AND BULB FOR RT AFT WING, OPS CK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080825 NM 2008 8 25 2008UALA03807 1 20080709 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 540-555 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 EXTERNAL FUSELAGE SKIN STATIC DISCHARGE BETWEEN BS 540 AND 555 STR 26R AND 28R. ACCOMPLISHED MAJOR REPAIR AT GSO. REMO VED RIVETS AND ACP HFEC WITH NO CRACKS INDICATED PER NDT MANUAL 51-00-11 PT 6 BY QC 400. INSTALLED BLIND FASTENER PER S RM 51-40-02 AND MM 53-30-95 PG 602. PER MM 53-30-95 PG 602 CHERRY MAX FASTENERS MUST BE REINSPECTED AT EACH C-CK AND RE PLACED WITH SOLID FASTENER AT NEXT HMV. 2 L 7 2 4F 4 F RT A2NM E17NE 20080825 NM 2008 8 25 KCSA081378 1 20080813 A 5320 STIFFENER BOEING 747 747122 1384872 NM BS 1366 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 716CK 19753 CORROSION ON LT OVERWING LONGERON BOX FRAME STIFFENER. (S) 2 L 7 4 4F RT A20WE 20080825 NM 2008 8 25 NWAA083783149 1 20080812 A 3350 BATTERY PACK AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 349NB 01815 LT OVERWING EMERGENCY EGRESS LIGHTING POWER SUPPLY FAULTS DURING SYSTEM TEST. REPLACED LT OVERWING EPSU BATTERY PACK, C HECKS GOOD. (S) 2 L 7 2 4F RT A28NM 20080825 WP 2008 8 25 NWAA083769862 1 20080811 A 5330 SKIN DOUG DC9 DC951 3022051 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 771NC 47769 DURING H-CHECK, FOUND CRACK IN FUSELAGE SKIN AT THE UPPER FORWARD CORNER OF PASSENGER ENTRY DOOR JAMB. REPAIRED PER EA 98-213637. (S) 2 L 7 2 4F RT A6WE 20080825 NM 2008 8 25 KCSA081381A 1 20080811 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 460 S12L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 BS 460 3.00 INCH ABOVE S12L FRAME OUTBOARD FLANGE CRACKED IN RADIUS OF DOUBLER .375 INCH LONG AFT SIDE. CRACK MARKED UP PER DECK. (S) 2 L 7 4 4F RT A20WE 20080819 EA 2008 8 19 SWIA200819797 1 20080624 A 2701 BEARING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* 30015 NE CONTROL COLUMN BINDING A SWIA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 07 964SW 7868 CONTROL YOKE HAS A BINDING FEEL ALONG WITH AN AUDIBLE SOUND WHEN AILERONS ARE FULLY DEFLECTED. (FLIGHT NR 5999) REPLACE D CAPTAINS AND FIRST OFFICERS CONTROL WHEEL SHAFT BEARINGS IAW MM 27-11-01. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA 20080819 SO 2008 8 19 C2XA08CL094 1 20080805 A 5210 PE64042K6028017S BUSHING EMB 145 EMB145LR 3260212 SO PAX DOOR WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16919 145393 CLE - FLIGHT 2552 THE CREW REPORTED, UNABLE TO OPEN THE MAIN CABIN DOOR FROM INSIDE. MAINTENANCE INSPECTED AND REPLACED THE FORWARD BUSHINGS ON THE LINK SUPPORT OF THE MAIN CABIN DOOR. THE MAIN DOOR CABLES WERE ALSO ADJUSTED AND OPERATION AL CHECKS WERE GOOD. (S) 2 L 7 2 4T RT T00011AT 20080819 NM 2008 8 19 UPS08M52950 1 20080713 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 257UP 48451 INSPECTION TYPE-1C, FOUND CORROSION IN NR 4 RT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED BUSHING, AND INSTALLE D BUSHING IAW UPS EO MD11-5510-19409-N AND SAA TRAVELER 80538680001. 2 L 7 3 4F RT A22WE 20080819 NM 2008 8 19 ASAA0853222 1 20080725 A 4960 2118966222 ECU BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE APU FAILED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 557AS 28257 35176 EAPU FAULT LIGHT ILLUMINATED. TURNED OFF 3 TIMES DURING PREFLT WITH APU IN OFF POSITION PERFORMED FIM 49-60-00-810. FOU ND FAULT CODE 4961156 IN FAULT HISTORY. REMOVED AND REPLACED APU ECU. OPS TEST AND BITE TEST GOOD REF FIM 49-60-00-810. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080819 SO 2008 8 19 CHQA200800160 1 20080805 A 2150 8152403 ACM EMB 135 EMB135KL 3260302 SO ALLSN AE3007 AE3007A 03030 GL A/C BAY SEIZED A CHQA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 380SK 14196 14196 145613 CAE311970 FLIGHT 5285, BDL TO STL. SHORTLY AFTER TAKEOFF WHILE PASSING THROUGH 2000 FT THE FLIGHT CREW NOTICED SMOKE IN THE COCKP IT ALONG WITH A LIGHT HAZE. THE ODOR AND HAZE WAS CONFIRMED BY THE FLIGHT ATTENDANT. THERE WERE NO FIRE WARNINGS OR EI CAS MESSAGES. THE HAZE AND ODOR DISAPPEARED BEFORE THE ACFT LANDED. MAINTENANCE TROUBLESHOT THE FAULT TO A SEIZED ACM ON PACK 1. THE NR 1 PACK WAS DEFERRED, AND THE ACM WAS LATER REPLACED ON AUGUST 6TH WITH NO FURTHER DEFECTS NOTED. (S) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080819 WP 2008 8 19 DHLA200800087 1 20080805 A 2697 WIRE HARNESS DOUG DC8 DC873F 302199F WP NR 1 ENGINE DEFECTIVE A DHLA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 01 873SJ 46091 FIRE WARNING ON NR 1 ENG. PERFORMED ABNORMAL CHECKLIST, SECURED NR 1 ENG. REPLACED HOT SECTION LT AFT HARNESS PER W/D/ M 26-1-1. FIRE WARN CHECKS SERV PER MM 26-10-0 AND PNEUMATICS CHECK SERV PER JRH 12.2. P/N D51A56108-3. FLIGHT NUMBER 160, ACFT WAS GROUNDED. PART WAS REPLACED. HARNESS D51A56108-3. (S) 2 L 7 4 4F RT 4A25 20080819 NE 2008 8 19 EIAA2008028 2 20080805 A 7200 ENGINE BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 1 FAILED A EIAA O OTHER Y ENGINE STOPPAGE CL CLIMB 1 NM 09 487EV 23286 517970 NR 1 ENG FAILED ON CLIMBOUT AT FL 180 AT 0850Z. WINDMILLING INDICATIONS WERE 26 PERCENT, N1 EGT WAS 151, N2 22 PERCENT OIL PRESSURE 5 PSI, OIL TEMP 95 DEGREES, N1 VIBRO 4 EGT OVER TEMP. YELLOW BALL ILLUMINATED IMMEDIATELY, EGT EXCEEDENCE NEEDLE SHOWS OFF SCALE OVER TEMP, SINGLE "BANG" AT TIME OF FAILURE. (S) 2 L 7 4 4F 4 F RT A20WE E23EA 20080819 2008 8 19 SWAA084132 4 20080724 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 259WN 35554 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084138 1 20080727 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED PAE CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084144 1 20080723 A 3350 20121 CHARGER BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED SERVICE CHECK, FOUND RT AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084187 1 20080728 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084162 1 20080726 A 5610 5893543129 WINDOW BOEING 737 7377H4 1384404 NM COCKPIT CRACKED A SWAA K NONE O OTHER CR CRUISE 1 SW 29 772SW 27880 FLIGHT DECK R1 WINDOW ARCED AT FL 370, R1 WINDOW OUTER PANE CRACKED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 20080819 2008 8 19 SWAA084163 4 20080726 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 774SW 27882 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084210 1 20080728 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 460, STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084197 1 20080725 A 2560 416A15005 ESCAPE ROPE BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 450WN 32470 DURING SCHEDULED HC1 CHECK, FOUND LT OVERWING EMERGENCY ESCAPE ROPE MISSING. INSTALLED ESCAPE ROPE PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084227 1 20080729 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 28L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084239 1 20080731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084262 1 20080801 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 232WN 32500 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084263 1 20080801 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 232WN 32500 EEPLS LENS LOOSE AT ROW 1 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084280 1 20080803 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084286 1 20080801 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 391SW 27378 L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084287 1 20080803 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080820 2008 8 20 ASAA0853215 4 20080722 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE FLT MANAGE FAULTED A ASAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 583AS 4018 35681 UPON TAXI OUT FMC DISAGREE CAME ON BOTH FMC'S STAYED ON FOR 6-8MINUTES AND BOTH WENT OFF AS WE TAXIED IN. FMC DISAGREE EXTINGUISHED BEFORE AIRCRAFT RETURNED TO GATE. PERFORMED FIM TASK 34-61-00-810-835 FOR PRECAUTIONARY PURPOSES. DETERM INED TO BE INTERMITTENT NUISANCE MSG. NO 30 DAY HISTORY. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 NM 2008 8 20 SWAA084303 1 20080803 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843312 1 20080715 A 5754 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU NR 6 SLAT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 OB L/E OF NR 6 SLAT IS DENTED REMOVED DAMAGED AREA FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57 43 01 FIG 201. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 2008 8 20 ASAA0853319 4 20080804 A 2310 G7404124 CONTROL PANEL BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 1 HF SYSTEM FAILED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 584AS 3868 35682 NR1 HF LIGHT ILLUMINATED ON CAPTAIN`S RADIO SELECT TUNE PANEL REGARDLESS OF WHICH RADIO IS SELECTED REMOVED AND REPLACED NR1 HF VHF COMM FRQ TUNING PANEL NR1 COMM OPS CK GOOD REF MM 23 11 01. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 NM 2008 8 20 ASAA0843234 1 20080629 A 5320 65468226 CUSP WEB BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 802-804 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 CUSP WEB CORRODED. REMOVED DAMAGED SECTION AND INSTALLED FILLER AND DOUBLER IAW SRM 51 70 13. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084324 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0853321 1 20080806 A 2131 71211997101AC CONTROLLER BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE CABIN PRESSURE FAULTED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 559AS 25052 35178 AUTO FAIL AND ALTN ILLUMINATED ON PRESSURIZATION PANEL. CYCLED AUTO PRESS SELECTOR CONTROL PANEL SWITCH. ALTERNATE FAIL LIGHT WENT OUT. PERFORMED BITE TEST IAW FIM 21-31-00.VERIFY SELECTOR PANEL LRU FAIL FAULT AND CLEARED SYS TEST NORMAL AND OPS OK. NO HISTORY 30 DAYS. NR 2 CONT. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 NM 2008 8 20 SWAA084351 1 20080802 A 5743 115A5211 FITTING BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 725SW 27857 DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084356 1 20080804 A 5315 141A5214 ANGLE BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 777QC 30592 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM ZEE ANGLE CORRODED AT BS 294 TO BS 338, RBL 56. REPAIRED ANGLE PER SRM. 2 L 7 2 4F RT A16WE 20080820 2008 8 20 ASAA0853223 4 20080727 A 3460 1762000101 COMPUTER BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE FLT MANAGE MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 584AS 3778 35682 FMC DISAGREE MSG WHEN FLAPS LOWERED VERIFIED DISCREPANCY. PERFORMED FMC RESET PROCEDURES IAW FIM 34-61-00-810-835. SYST EM RESET OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 EA 2008 8 20 TRAX200800962 1 20080804 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA ASD CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 738EV 10146 ASD AFT DRAG ANGLE CRACKED. CUT AWAY SECTION OF AFT ASD DRAG ANGLE IAW REO 670-52-11-072. PERFORMED EDDY CURRENT INSPE CTION OF CUT LINES ON AIRSTAIR DOOR AFT DRAG ANGLE IAW REO 670-52-11-072 PER CRJ700 NDTM 51-20-006. NO DEFECTS NOTED. (S) 2 L 7 2 4F RT A21EA 20080820 EA 2008 8 20 SWIA200819802 1 20080502 A 5310 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA BS 981 CHAFED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 614SK 10051 FUSELAGE IS CHAFED AT CENTER LINE AND BS 981. (FOUND AT C-CHECK) COMPLIED WITH REPAIRS IAW REO 670-53-61-368. 2 L 7 2 4F RT A21EA 20080820 EA 2008 8 20 TRAX200800703 1 20080530 A 3230 DRAG BRACE CNDAIR CL600 CL6002B19 1900309 EA NLG DEFECTIVE A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 908EV 7654 GEAR UNSAFE INDICATION AT 500 FT ON FINAL APPROACH ON GO AROUND RECYCLED GEAR AND GOT THREE GREEN INDICATIONS THEN UNSAF E INDICATION AT 500 FEET. 3RD ATTEMPT 3 GREEN INDICATION COMPLETE THROUGH LANDING, EMERGENCY DECLARED. REMOVED AND REP LACED NOSE LANDING GEAR DRAG BRACE IAW CRJ200 AMM 32-21-05. OP`S CHECK GOOD. DEFER CLEARED PLACARD REMOVED. [SDR CLOSE D](B) 2 L 7 2 4F RT A21EA 20080820 EA 2008 8 20 SWIA200819853 1 20080423 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 955SW 7817 FS 280 FLOOR ANGLE IS CRACKED AT LBL 9.0. (FOUND AT C-CHECK) REPAIRED FLOOR ANGLE IAW REO 601R-53-11-138. 2 L 7 2 4F RT A21EA 20080820 NM 2008 8 20 SWAA084565 1 20080813 A 5754 65C26601 SLAT BOEING 737 7373Y0 1384671 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT DELAMINATED AT OUTBOARD T/E END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084560 1 20080817 A 5310 6547956 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER CORNER. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084557 1 20080817 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. R&R STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 USA2008F00022 1 20080726 A 2560 P4010021 BATTERY BOEING 737 7373G7 1384595 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 322AW 25400 PHX - MAINTENANCE REPORTED THE FORWARD FLIGHT ATTENDANT STATION FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACE D THE FLASHLIGHT BATTERY, OPERATIONAL CHECK GOOD. (A) 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 USAA920081414 1 20080717 A 5414 311A1102 SKIN PANEL BOEING 737 737401 1384701 NM NR 1 PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 424US 23991 CLT -MAJOR REPAIR- Q3 CHECK- CRACKED NR 1 PYLON SKIN PANEL, NAC 189,50. REPAIRED NR 1 PYLON SKIN PANEL AT NAC 189.50 IA W US AIRWAYS TYPICAL REPAIR 54-30-07. (A) 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 08FDEA02971 1 20080718 A 5347 601096418 SEAT TRACK DOUG MD10 MD1030F 3024020 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 303FE 46802 MAIN CABIN SEAT TRACK IS DAMAGED AT SEVERAL AREAS FROM STATION 1079 TO STATION 1179 RBL 47. BLENDED AREAS FOUND OUT OF LIMITS. REMOVED DAMAGE AREA OF SEAT TRACK. FABRICATED NEW SECTION AND SPLICE HAT/PLATE INSTALLED NEW PARTS IAW TRAVELE RS T8/748481 AND T8/748484, SRM 53-70-00. REPAIR IS CLASSIFIED AS A MAJOR REPAIR, REPORTABLE DISCREPANCY AND RII. 2 L 7 3 4F RT A22WE 20080820 WP 2008 8 20 08FDEA02976 1 20080718 A 5350 NKC60221 ATTACH ANGLE DOUG MD10 MD1010F 3022112 WP TAILCONE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 TAILCONE ACCESS PANEL, CUT OUT, FWD EDGE LATCHING POSITIONS ARE MISSING MATERIAL IN 2 PLACES. FABRICATED A NEW ATTACH ANGLE IAW DC/MD-10 SRM 53-52-01, VOL III AND DAC DWG NRC 6022. ALODINED AND PRIMED ANGLE IAW DC/MD-10 SRM 51-21/01, VO L II. REMOVED AND INSTALLED ANGLE IAW DC/MD-10 SRM 51-35-01, VOL II. 2 L 7 3 4F RT A22WE 20080820 NM 2008 8 20 ASAA0843190 1 20080629 A 5753 6546430129 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU FOREFLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 LT WING IB FORE FLAP HAS MULTIPLE DENTS ON LOWER SURFACE (4 EACH). PREPARED DAMAGED AREA FABRICATED FILLERS AND DOUBLERS AND BONDED IAW SRM 51-70-10, REPAIR 4. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843182 1 20080629 A 5755 654645268A SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU NR 4 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 LT WING NR4 GROUND SPOILER HAS SEVERAL DENTS ON UPPER SURFACE, PREPARED DAMAGED AREA FABRICATED FILLERS AND REPAIR DOUBL ERS AND BONDED IAW SRM 51-70-10, REPAIR 4. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843235 1 20080629 A 5340 69353521 STRINGER CLIP BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 STRINGER CLIP CRACKED. REPLACED CLIP IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 20080825 CE 2008 8 25 DXTA200803225 1 20080817 A 3220 WHEEL CESSNA 750 750 2076810 CE NLG VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 983QS 7500083 SEVERE NOSE WHEEL SHIMMY OCCURRED DURING TAKEOFF ROLL AT APPROX 60 KNOTS REQUIRING AN ABORT. (S) 2 L 7 2 4J RT T00007WI 20080825 NM 2008 8 25 2008UALA03400 1 20080614 A 2150 22023224 DUCT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT A/C PACK CRACKED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 649UA 25286 LT PACK INOPERATIVE - REHEATER INLET DUCT CRACKED. *S/D* SUSPECT IMPROPER INSTALLATION. REPLACED LT PACK REHEATER DUC T PER MM 21-51-21. OP CHECKS NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080825 EU 2008 8 25 2008UALA03718 1 20080704 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 456UA 1128 SEAT 25ABC ESCAPE PATH LIGHT BROKEN. UNKNOWN DAMAGE. REPLACED LIGHT ASSY, OPS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 20080821 2008 8 21 2008UALA03750 4 20080703 A 2565 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR SLIDE NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 520UA 24890 SLIDE LIGHT DOOR 2L NO LONGER ILLUMINATED. *S/D* MISSING HARDWARE REQUIRED TO ARM MECHANISM (UNKNOWN DAMAGE). REPLACE D MISSING HARDWARE FOR AFT ROD END THAT ARMS THE DOOR. INSTALLED, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NM 2008 8 21 2008UALA03764 1 20080708 A 2133 OUTFLOW VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN PRESSURE OPEN A UALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 518UA 24871 PRESSURIZATION BECAME UNCONTROLLABLE. FLIGHT DIVERTED. FOUND E&E EXHAUST VALVE STICKING OPEN. REPLACED VALVE, ALL PRE SSURIZATION TESTS WERE NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NM 2008 8 21 SWAA084425 1 20080808 A 3350 311500 LIGHT BOEING 737 7373A4 1384585 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED 1/2D BRDG CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03207 1 20080604 A 2910 S271W13034 CONTROL UNIT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HYD SYTEM FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 210UA 30216 HYD PUMP DEM C1 LOW CENTER HYDRAULIC DEMAND PUMP NR 1 PRESSURE WHEN COMMANDED ON, OR CENTER DEMAND PUMP NR 1 OVERHEATED. STATUS MSG03- NOT ACTIVE INITIAL CLIMB MODE DEPENDENT; AIR DRIVEN PUMP (ADP) (C1) SPEED IS OUT OF RANGE. DB- HYDRAULI C INTERFACE MODULE (HYDIM) (CR) MSG-2910440 ACTIVE DC MODE, MSG-2910440 ACTIVE DC MODE, MSG-2911100 INACTV IC MODE. *S/ D* SUSPECT FAULTY SPEED CONTROL UNIT. REPLACED ADP C1 LOGIC SPEED CONTROL UNIT PER MM 29-11-15-401, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080822 NM 2008 8 22 F3LA200800436 1 20080707 A 5330 SKIN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 REFERENCE NON ROUTINE 29004. DURING C-CHECK INSP NOTED LIGHTNING STRIKE FOUND AT FRAME 25 STATION 1003 STRINGER 41R. MAI NT REPAIRED BY REMOVING BLIND FASTNER AND INSTALLED HI-LOCK IAW SRM 51-42-11, SRM 51-48-00, AND SRM 53-21-11. UPON COMPL ETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800501 1 20080719 A 5320 D5348004320501 SILL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE R2 DOOR DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK, INSP NOTED THE R2 DOOR SILL PLATE REQUIRED REPLACEMENT DUE TO MISDRILLED HOLE. MAINT REMOVED AND REPLACE D R2 DOOR SILL PLATE IAW A319 SRM 51-42-11 AND 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPT ABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800406 1 20080628 A 5320 D5367303801000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSP, NOTED AFT CARGO PIT AFT LT HAND TRANSITION PANEL 161BF HAS A HOLE AT AFT TOP END. MAINT REPAIRED AN D INSTALLED SERVICEABLE PANEL 161BF IAW SRM 53-42-44-400-001. COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEP TABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800338 1 20080612 A 3320 Z080H0005110 DEU AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CABIN LIGHTS ODOR A F3LA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 919FR 1980 DURING FLIGHT, THE FLIGHT CREW NOTICED MANY CABIN LIGHTS ON THE RT SIDE OF THE AC COMING ON AND OFF. THE F/A ALSO NOTIC ED A BURNING ODOR OVER SEAT ROWS 16 TO 18 ON AC RT. MAINT REMOVED AND REPLACED 200RH 12 DEU-A IAW AMM 23-73-46 PAGE BRE AK 401 AND OPERATIONAL CHECKED GOOD. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND THE AIRCRAFT WAS RETURNED TO SE RVICE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800299 1 20080607 A 5321 D5367228000000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 77 1851 DURING C-CHECK INSP, NOTED AFT PIT FLOOR PANEL 151PE HAS SURFACE CORROSION AROUND ATTACHMENT HOLES AND EDGES. MAINT CLE ANED CORROSION, FILLED COUNTER SINK AREA, PREPPED AND PRIMED PANEL 151PE IAW DRAWING 319-53-0001-11 AND AMM 25-00-00-870 -001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 EU 2008 8 22 F3LA200800503 1 20080720 A 5240 D5211022720200 TORSION BAR AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE R2 DOOR OUT OF ADJUST A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 943FR 18 2518 DURING C-CHECK, INSP NOTED THE R2 DOOR WOULD NOT ARM WITH DOOR CLOSED AND LOCKED. THIS OCCURRED DURING OPERATION OF THE DOOR WHILE PERFORMING TASK CARD C528002-2. MAINT ADJUSTED TORSION BAR AND PERFORMED OPS CHECK IAW AMM 52-11-21-400-001 AND TASK CARD C528002-2. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800339 1 20080612 A 5321 D5367150500000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED CABIN FLOOR PANEL 252HF AREA OF ELIMINATION. MAINT REPAIRED PANEL 252HF IAW SRM 53-02-00. UPO N COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 EU 2008 8 22 F3LA200800424 1 20080707 A 5321 D5367180500400 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 805FR 1660 DURING C-CHECK INSP NOTED FLOOR PANEL 261FF HAS CORROSION ON SURFACE. MAINT REMOVED AND REPLACED FLOOR PANEL 261FF IAW A MM 53-42-12-400-002. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT 20080820 NM 2008 8 20 ASAA0843245 1 20080624 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU NR 6 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 NR 6 SPOILER UPPER SURFACE IS DENTED. INSTALLED REPAIR DOUBLER AND BONDED REPAIR IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 2008 8 20 ASAA0853261 4 20080802 A 3442 WARNING SYSTEM BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE COCKPIT MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION UK UNKNOWN 1 NM 02 558AS 11240 35177 WX FAIL MESSAGE ILLUMINATED INTERMITTENTLY. CONFIRMED WX TRANSCEIVER SECURED IN RACK CONFIRMED WX CONTROL PANEL CONNECT ORS SECURED NO OTHER FAULTS NOTED. NO HISTORY PAST 30 DAYS. PERF WX OPERATION TEST IAW 34-43-00-710-802-001. NO FAULT S NOTED AT THIS TIME. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 NM 2008 8 20 ASAA0843260 1 20080627 A 5311 65465547 FAILSAFE BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 CORROSION ON FAILSAFE AT STA 847 BETWEEN STR 28L, 28R IN AFT CARGO PIT REMOVED DAMAGED AREA FABBED FILLER, REPAIR ANGLE, INSTALLED IAW SRM 53-70-11, FIG 1. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843290 1 20080712 A 5313 FITTING BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AT THE APB STRINGER 15L END FITTING HAS GOUGES. REMOVED & REPLACED STRINGER 15L END FITTING ON THE AFT SIDE OF THE APB I AW SRM 51-40-05, P1. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843288 1 20080720 A 5315 6545834103 FLOORBEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 FLOORBEAM STABILIZER AT STA 312 + BL 45 R IS CRACKED BROKEN FABRICATED DOUBLER + INSTALLED REPAIR IAW SRM 51-70-13, PG 3 . 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843291 1 20080701 A 5320 65528942 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 CENTER ISLE FLOOR SUPPORT AT STA 540 IS CRACKED REMOVED + REPLACE FLOOR SUPPORT IAW SRM 51-40-05. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843276 1 20080712 A 5313 6549914521 FITTING BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 STRINGER 14 L, END FITTING ON THE AFT SIDE OF THE APB HAS A GOUGE MARKS. REMOVED AND REPLACED STRINGER 14L END FITTING IAW SRM 51-40-02, PG 4. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843278 1 20080712 A 5313 6C3354713 FITTING BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AT THE AFT SIDE OF THE APB STRINGER 21L END FITTING IS GOUGED. REMOVED AND REPLACED STRINGER 21L END FITTING ON THE AFT SIDE OF THE APB IAW SRM 51-40-02, FIG 8. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843279 1 20080712 A 5313 65C3354713 FITTING BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AT THE AFT SIDE OF THE APB STRINGER 20L END FITTING IS GOUGED. REMOVED AND REPLACED STRINGER 20L END FITTING ON THE AFT SIDE OF THE APB IAW SRM 51-40-02, FIG 8. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843281 1 20080712 A 5313 65C3354713 FITTING BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AT THE AFT SIDE OF THE APB STRING 17L END FITTING IS GOUGED REMOVE AND REPLACE APB STRINGER 17L END FITTING ON THE AFT S IDE OF THE APB IAW SRM 51-40-02, FIG 8, PG 6. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843286 1 20080712 A 5313 6549914524 FITTING BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AT AFT SIDE OF THE APB STRINGER 18L END FITTING IS GOUGED. REMOVED AND REPLACED STRINGER 18L END FITTING ON THE AFT SID E OF THE APB IAW SRM 51-40-02, P 4. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084552 1 20080817 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084551 1 20080817 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 F3LA200800481 1 20080711 A 5321 D5367175604800 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP, NOTED FLOOR PANEL 261PF HAD COMPOSITE DAMAGE. MAINT REMOVED AND REPLACED FLOOR PANEL 261PF WITH NEW PANEL, REFERENCED ON EAC NON ROUTINE ITEM 9651. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. ( B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 NM 2008 8 20 SWAA084548 1 20080817 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 636WN 27709 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 28R. R&R SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 F3LA200800526 1 20080728 A 5321 D5367162400000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2 2209 DURING C-CHECK, INSP NOTED THE FLOOR PANEL 251FF NEEDED TOP LAYER OF COMPOSITE REPAIRED IN SEVERAL PLACES. MAINT REPAIR ED FLOOR PANEL 251FF IAW SRM 53-02-00 FIGURE 212. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F RT A28NM 20080820 EU 2008 8 20 F3LA200800422 1 20080707 A 5315 D53472190210 FLOORBEAM AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 805FR 1660 DURING C-CHECK INSP NOTED FLOORBEAM Y1292 HAS CORROSION AT FWD OB NUTCLIP HOLE AT FRAME 66 JUST AFT OF LT LAVATORY. MAIN T BLENDED CORROSION AND OVERSIZED HOLE, FABRICATED FLANGE BUSHING AND TREATED PRIMED AND PAINTED IAW EA A8-53R-30435 AND SRM 51-75-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT 20080820 NM 2008 8 20 SWAA084547 1 20080817 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED SPV CHECK, FOUND LT AFT CABIN EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084191 1 20080728 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 2L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084209 1 20080728 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084202 1 20080727 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 793SA 27888 EEPL INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084232 1 20080729 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 791SW 27886 L1 DOOR EMERGENCY EXIT LIGHT ASSY INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084237 1 20080731 A 5312 6546568 BULKHEAD BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084238 1 20080731 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 5R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080819 NM 2008 8 19 SWAA084254 1 20080731 A 5322 69353656 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 13L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084273 1 20080801 A 3350 3071BPEGPL LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED A2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084279 1 20080803 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L AND STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084296 1 20080801 A 3350 8200048901 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 490WN 32476 R2 DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084302 1 20080803 A 5311 6546533 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, STR 25L TO BS 26L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084313 1 20080803 A 2560 PH22300L GLOWSTRIP BOEING 737 7377H4 1384404 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 776WN 30591 DURING SCHEDULED 8Y CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP DELAMINATED AT ROW 8 DEF. REMOVED AND REPLACED EEPLS STRI P PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843269 1 20080719 A 5320 6935365Y6 INTERCOSTAL BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 380-400 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 INTERCOSTAL BETWEEN STA 380-400 AT BL "0" HAS UPPER ANGLE CRACKED AT THE FWD END. REMOVED DAMAGED ANGLE & REPLACE IAW SR M 51-40-02. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084315 1 20080803 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 747, STR 25L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084316 1 20080803 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NE 2008 8 20 ASAA0853259 2 20080801 A 7261 OIL SYSTEM BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE NR 1 ENGINE LOW A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 557AS 8300 35176 892792 BOTH ENGINES LOW ON OIL. NR 1 ENG ADDED 4 QTS. NR 2 ENG ADDED 4 QTS. APU ADD 0 QTS. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 NM 2008 8 20 SWAA084333 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0853179 1 20080714 A 2430 0802070501 TRANSFORMER BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE EE BAY FAULTED A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 559AS 7149 35178 AFTER ENGINE START DURING POWER TRANSFER UNIT LIGHT ILLUMINATED. FOUND THE FOLLOWING CB OPEN P91 PANEL TR1 P92 PANEL DC BUSS 2 TRANSFER & TR 2 RESET C B'S SYSTEM OPS CK OK. IAW FIM TASK 24-31-00-810. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 NM 2008 8 20 ASAA0873220 1 20080723 A 2913 66087 PUMP BOEING 737 737790 13844CN NM HYD SYSTEM FAILED A ASAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 02 626AS 29682 30793 NR1 ENG HYD PUMP LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. QUANTITY PERCENT FLUCUATED FROM 78 PERCENT TO 106 PERCENT FO R 20 MIN THEN SLOW DECREASE TO 48 PERCENT FOR 10 MIN THEN INCREASE TO 88 PERCENT FOR 10 MIN THEN SLOW DECREASE TO 15 PER CENT. FLIGHT CONTROL LIGHT BLINKED MOMENTARILY UPON LANDING WITH SPOILER DEPLOYMENT. REMOVED AND REPLACED NR1 ENGINE E DP IAW MM 29-11-11 OPS & LEAK CHECK GOOD. NOTE "A" SYSTEM HYDRAULIC FILTERS REPLACED. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084345 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084350 1 20080804 A 5313 6551968 STRINGER SPLICE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CORRODED AT BS 910, STR 24L. REMOVED AND REPLACED STRINGER SPLICE PE R SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084355 1 20080804 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 776WN 30591 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 29 TO LBL 43. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084357 1 20080804 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 777QC 30592 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 8. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0853213 1 20080721 A 2421 7588429101 FILTER BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE IDG TRIPPED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 557AS AAAH004440 35176 LT ENGINE IDG DELTA "P" INDICATOR EXTENDED. ACCOMPLISHED FIM TASK 24-11-00-810-803 REMOVED AND REPLACED. LT ENG. IDG SC AVENGE AND CHARGE FILTERS IAW AMM 24-11-41-400-801 IDLE RAN LT ENG NO LEAKS NOTED AND IDG DELTA "P" INDICATOR IS NORMAL. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 NM 2008 8 20 ASAA0843206 1 20080718 A 5311 FRAME BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU BS 440 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 705AS 29318 FWD PIT FWD FRAME GOUGED BS 440 RBL 28 REPAIRED PER SRM 51 40 02 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843207 1 20080629 A 5230 654796039 FRAME BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 705AS 29318 AFT CARGO DOOR AFT FRAME AT BS 847 FOUND CORRODED RBL 17 ON UPPER FLANGE REPAIRED IAW SRM. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0853212 1 20080720 A 8012 32896302 START VALVE BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 1 ENGINE FAILED A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 570AS 5734 35185 ON STARTING ENGINE NR 1, WHEN START SWITCH PUT TO GROUND THERE WAS NO START VALVE LIGHT ILLUMINATION AND NO N2 ROTATION BUT THE EGT GAUGE DID ILLUMINATE. DID NOT SEE A DUCT PRESSURE RISE ON THE DUCT PRESSURE GAUGE. REMOVED AND REPLACED NR 1 ENGINE START VALVE REF MM 80-11-03. OPS CK OK. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 SO 2008 8 20 SWIA200819891 1 20080717 A 2697 CONNECTOR EMB 120 EMB120ER 3260203 SO SMOKE DETECTOR LOOSE A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 565SW 120340 TEST NR2 ON BAGGAGE SMOKE AND FIRE SYSTEM DOES NOT WORK. (FLIGHT NR 5566) RESECURED CONNECTOR PLUG ON AFT CARGO SMOKE D ETECTOR. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20080820 NM 2008 8 20 SWAA084568 1 20080813 A 2560 PH22300L GLOWSTRIP BOEING 737 7373Y0 1384671 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED HC2 CHECK, FOUND EEPLS PHOTOLUMINESCENT STRIP WORN AT ROW 11 ABC. R&R STRIP PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843192 1 20080709 A 5330 6546881175 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU BS 1026 S20L DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 WHILE INSTALLING REPAIR AT 1028 DAMAGED SKIN NOTED AT STA 1026 JUST ABOVE STR 20L (SEVERAL PROTRUDING DENTS). CUTOUT DAM AGED SKIN FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-80-01, FIG 201, REPAIR 3. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084550 1 20080817 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 F3LA200800452 1 20080711 A 5321 D5367304000100 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 940FR 2465 DURING C-CHECK INSP, NOTED AFT PIT PANEL 162EF DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 NM 2008 8 20 SWAA084549 1 20080817 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084546 1 20080817 A 5312 6517852 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179, LBL 17. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 F3LA200800388 1 20080622 A 5320 D5367413600000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSP NOTED FWD PIT TRANSITION PANEL 132EG HAS A PUNCTURE. MAINT REPAIRED TRANSITION PANEL 132EG IAW SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 NM 2008 8 20 F3LA200800389 1 20080622 A 5320 D5367413200000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSP NOTED FORWARD PIT TRANSITION PANEL 132DG HAS A PUNCTURE. MAINT REPAIRED TRANSITION PANEL 132DG IAW SRM 53-02-00, FIG 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 NM 2008 8 20 F3LA200800357 1 20080617 A 5753 D5757024000100 ARM AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FLAP TRACK CHAFED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP NOTED RT NR TWO FLAP TRACK DRIVE LEVER EXTENSION ARM THAT ATTACHES TO FLAP AT AFT ATTACH POINT IS CH AFING INTO FITTING ON OB EAR BOTTOM END AND IB EAR TOP END. MAINT REPAIRED AREA IAW EA A9-57R-30378, SRM 51-73-00 AND SR M 51-21-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 NM 2008 8 20 F3LA2008290 1 20080602 A 5320 D5367301200000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 DURING C-CHECK INSP, NOTED FWD PIT TRANSITION PANEL 131BF HAS GOUGE IN CORE. MAINT REMOVED DAMAGE AND CLEANED PANEL REP AIRED PUNCTURED DAMAGE PANEL 131BF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUN D ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 NM 2008 8 20 F3LA200800333 1 20080611 A 5320 D5367227300000 SILL AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 DURING C-CHECK INSP, NOTED UPON CLOSURE OF AFT PIT CORROSION WAS FOUND ON THE SILL WEDGE PANEL 152YG. MAINT INSTALLED A NEW PANEL IAW WORK CARD CP753-25. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 NM 2008 8 20 F3LA200800443 1 20080710 A 5313 D5347218820400 LONGERON AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP, NOTED THE LT LONGERON BEAM AT Y1162 AND FRAME 68 HAS AREAS OF CORROSION. MAINT REMOVED AND REPLACED THE LT LONGERON BEAM AT Y1162 AND FRAME 68 IAW SRM 51-72-11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSP ECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 NM 2008 8 20 SWAA084541 1 20080817 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084536 1 20080817 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084534 1 20080817 A 3350 MS155721 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 351SW 24572 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. R&R LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084533 1 20080814 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 F3LA200800346 1 20080617 A 5330 D53113402206 SKIN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C3 S1 C-CHECK INSP NOTED RT FUSELAGE SKIN DENT BETWEEN FRAME 12 AND FRAME 13 ABOVE LWR EDGE OF STRINGER 29. MAIN T PERFORMED PERMANENT REPAIR IAW EA A9-53R-11684 REVISION C AND SRM 53-11-11. UPON COMPLETION OF THE REPAIR IT WAS INSP ECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800347 1 20080617 A 5321 D5367204701000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED CARGO FLOORBOARD PANEL 161BF HAS TWO HOLES. MAINT REPAIRED PANEL 161BF IAW SRM 53-02-00 REPA IR PROCEDURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800295 1 20080605 A 5321 D5367175000000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 77 1851 DURING C-CHECK INSP NOTED FLOOR PANEL 251JG HAS DAMAGE IN TWO PLACES ON UPPER SURFACE. MAINT REMOVED DAMAGE AND APPLIED MOISTURE BARRIER IAW SRM 53-02-00 AND SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABL E. (A) 2 L 7 2 4F 4 F RT A28NM 20080821 NM 2008 8 21 F3LA200800398 1 20080624 A 5320 D5367314500000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSP, NOTED AFT CARGO PIT FWD RT UPPER TRANSITION PANEL 152XG HAS SEVERAL HOLES. MAINT REPAIRED TRANSITIO N PANEL 152XG IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 ASAA0843313 1 20080627 A 5320 6546592503 FLOOR SUPPORT BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AFT PIT FLOOR SUPPORT AT STA 767, RBL 3.0 IS CORRODED. REMOVED DAMAGED AREA FABBED REPAIR PARTS AND INSTALLED IAW EA 532 0 01845. 2 L 7 2 4F 4 F RT A16WE E21EU 20080821 WP 2008 8 21 I5HA0858005A 1 20080405 A 5100 3403110207197 ANGLE CVAC 580 580 2422806 WP FUSELAGE DAMAGED A I5HA O OTHER O OTHER NR NOT REPORTED 1 GL 25 581P 29 DURING A STORM (MIA) A CARGO CAN (ULB) WAS THROWN INTO THE RT SIDE OF N581P. THE RT PROPELLER WAS ALSO STRUCK A GLANCIN G BLOW. THERE WAS SIGNIFICANT DAMAGE TO THE SKIN AND SUPPORT STRUCTURE BENEATH THE SKIN. THERE WAS DAMAGE TO WIRING IN THE AREA. THE NOSE STEERING ACTUATOR WAS ALSO DAMAGED. DAMAGE AREA WAS BETWEEN FUSELAGE STATIONS 72 TO 125 AT APPROXI MATELY BETWEEN STRINGERS 11 AND 3. THE PROPELLER AND REDUCTION GEARBOX WERE REMOVED AND INSPECTED. NO DAMAGE TO EITHER . N581P WAS REPAIRED AND THE ACFT TEST FLOWN ON JULY 3, 2008. THE ACFT WAS RETURNED TO SERVICE JULY 8, 2008. (S) 2 L 7 2 4T RT 20080821 EU 2008 8 21 F3LA200800559 1 20080816 A 5320 D5347112420100 SHEAR PLATE AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 806FR 30 2218 DURING C-CHECK INSP, NOTED CORROSION AROUND NUT CLIP HOLE APPROX 4.25 INCHES AFT OF FWD END ON RT SIDE FLOORBEAM ALONG Y 1292 BETWEEN FR68 AND FR69. MAINTENANCE BLENDED AREA, FABRICATED FLANGE BUSHING AND INSTALLED IAW THE REQUIREMENTS OF E NGINEERING AUTHORIZATION A8-53R-30558. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F 4 F RT 20080821 NM 2008 8 21 F3LA200800403 1 20080624 A 5320 D5367314000000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSP, NOTED AFT CARGO PIT AFT RT LOWER TRANSITION PANEL 162BF HAS A HOLE AT AFT CENTER SECTION. MAINT RE PAIRED TRANSITION PANEL 162BF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACC EPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800454 1 20080711 A 5320 D5367425000000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 940FR 2465 DURING C-CHECK INSP, NOTED AFT PIT PANEL 161NF DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800297 1 20080606 A 5321 D5367160000000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 77 1851 DURING C-CHECK INSP NOTED FLOOR PANEL 231XG HAS TWO SMALL PUNCTURE HOLES ON SURFACE. MAINT REPAIRED PUNCTURE DAMAGE TO FLOOR PANEL 231XG IAW SRM 53-02-00 STEP 8A. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800294 1 20080608 A 5315 D53476572000 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 77 1851 DURING C-CHECK INSP NOTED THE CENTER LONGITUDINAL FLOORBEAM FROM FRAME 58 TO FRAME 59 HAS CORROSION AROUND THE FWD NUTPL ATE HOLE. MAINT REPAIRED THE FLOORBEAM IAW EA A9-53R-30355 AND SRM 51-75-00, SRM 53-00-14 AND SRM 51-42-11. UPON COMPLET ION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800287 1 20080602 A 5320 D5367226800000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 DURING C-CHECK INSP, NOTED AFT PIT TRANSITION PANEL 151FE HAS DENTS. MAINT REMOVED DAMAGE AND CLEANED PANEL, FILLED DENT S, PANEL 151FE IAW SRM 51-73-00 STEP 3C. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800289 1 20080602 A 5320 D5367204300000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE CARGO BAY DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 DURING C-CHECK INSP NOTED AFT PIT TRANSITION PANEL 151HE HAS DENTS. MAINT REMOVED DAMAGE AND CLEANED PANEL FILLED DENTS ON PANEL 151HE IAW SRM 53-73-00 STEP 3C. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NE 2008 8 21 M7K2008F00069 2 20080108 A 7320 POTENTIOMETER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE MALFUNCTIONED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 810MH 3949 23209 PILOT REPORTS AMBER GOVERNOR LIGHT CAME ON IN FLIGHT. NO FAULT CODE WAS GENERATED INDICATING A POTENTIOMETER DEFECT HOWE VER CIRCUMSTANCES REPORTED POINTED TO THIS. A NEW POTENTIOMETER HAS BEEN INSTALLED. PROBLEM FIXED THIS PART HAS LASTED M UCH LONGER THAN TYPICAL THIS IS A RECURRING PROBLEM FOR THIS PART THAT HAS EFFECTED THE DISPATCH RELIABILITY OF THIS MOD E AC. THIS PART CAN ON OCCASION ALSO CAUSE ENGINE FLUCTUATIONS IN FLIGHT WHEN THE RESISTANCE VALUE SIGNAL IS DISRUPTED FOR A LITTLE AS 1/20TH OF A SECOND, WHICH IS THE SAMPLE RATE FOR THE ENGINE CONTROL SYS. AN ADDITIONAL FACTOR FOR THESE TYPE OF FAULTS IS NO RESET FUNCTION AVAILABLE TO THE PILOT TO DIFFERENTIATE BETWEEN A MOMENTARY OR AN ACTIVE FAULT. ON 1 G 7 2 3U 3 U H9EU E00054EN 20080821 EU 2008 8 21 F3LA200800381 1 20080620 A 2613 D55181715 RELAY AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE APU DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 941FR 2483 DURING C-CHECK INSP NOTED OPS TEST OF APU AUTO FIRE EXTINGUISHING EXITING CIRCUIT AND THE APU LOW PRESSURE VALVE OPERATI ON USING EACH INDIVIDUAL MOTOR IN TURN AND TEST APU EMERGENCY SHUTDOWN CIRCUIT FAILS. MAINT REMOVED AND REPLACED RELAY 3 9WF AND OPS CHECKED GOOD. ALL WORK WAS COMPLETED IAW TSM 26-22-00-810-804 AND AMM 26-22-00-710-002. UPON COMPLETION OF T HE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800428 1 20080707 A 5321 D5367150500000 FLOORBOARD AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 DURING C-CHECK INSP NOTED FLOORBOARD 251HF HAS A CRACK IN THE TOP OF THE BOARD. MAINT PREPPED AREA OF DAMAGE ON FLOORBOA RD 251HF FOR REPAIR AND REPAIRED IAW ARM 53-12-00 PARAGRAPH 5B FIGURE 202. UPON COMPLETION OF THE REPAIR IT WAS INSPECTE D AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 EU 2008 8 21 F3LA200800344 1 20080617 A 5321 D5367311800200 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 809FR 3092 DURING HEAVY SERVICE CHECK INSP, NOTED AFT CARGO COMPARTMENT FLOOR PANEL 151DH WAS DAMAGED. MAINT COMPLETED PERMANENT RE PAIR ON PANEL 151DH IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT 20080821 NM 2008 8 21 F3LA200800349 1 20080617 A 5321 D5367204500000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED CARGO FLOOR PANEL 161CF HAS THREE HOLES IN IT. MAINT REPAIRED PANEL 161CF IAW SRM 53-02-00 R EPAIR 204 AND REPAIR 207. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 SWAA084376 1 20080806 A 5730 65C252045 SKIN BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED HC1 CHECK, FOUND LT WING UPPER SKIN CRACKED AT STA 251. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084389 1 20080806 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 747 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084390 1 20080806 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 787 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084391 1 20080806 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM BS 706 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084392 1 20080806 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM BS 706 S9R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 9R CRACKED AT BS 706. REPAIRED STRINGER PER SRM V. 2 L 7 2 4F RT A16WE 20080821 2008 8 21 SWAA084374 4 20080806 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 251WN 32510 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03717 1 20080706 A 3150 WARNING MESSAGE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 216UA 30549 BLEED OFF ENG LEFT MESSAGE PER CREW AND SHOWS INOP ON SYNOPTIC PAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080821 NM 2008 8 21 SWAA084401 1 20080807 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 288 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 288, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084402 1 20080807 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 360 S11L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084403 1 20080807 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080822 NM 2008 8 22 F3LA200800449 1 20080713 A 3320 Z030H0005110 DEU AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CABIN LIGHTS INOPERATIVE A F3LA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 919FR 1980 DURING FLIGHT MANY CABIN LIGHTS WERE COMING ON AND OFF ON AC RT. THE F/A NOTICED A BURNING SMELL OVER ROWS 16,17 AND 18 ON AC RT. MAINT FOUND DEU-A 200RH12 INOPERATIVE AND HAD A SMELL TO IT. MAINT REMOVED AND REPLACED DEU-A 200RH12 IAW AMM 23-73-46 AND OPS CHECKED NORMAL AND THE AC WAS RETURNED TO SERVICE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 EU 2008 8 22 F3LA200800441 1 20080708 A 2560 GIRT BAR AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE OUT OF ADJUST A F3LA O OTHER J WARNING INDICATION CL CLIMB 1 NM 03 805FR 1660 DURING CLIMB OUT THE L2 AND R2 DOOR DISARMED AT 8500 FT AND REARMED DURING DESCENT AT 10000 FT. MAINT ADJUSTED GIRT BAR FITTINGS ON THE L2 AND R2 DOORS AND OPS AND RIG CHECKED GOOD IAW AMM 52-11-00-820-001, AMM 25-62-44-400-006 AND AMM 05-5 3-00-780-003. UPON COMPLETION OF THE REPAIR THE AC WAS INSPECTED AND WAS FOUND ACCEPTABLE AND THE AC RETURNED TO SERVICE . (B) 2 L 7 2 4F 4 F RT 20080822 NM 2008 8 22 F3LA200800435 1 20080707 A 5320 D5347112320300 SHEAR PLATE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 DURING C-CHECK INSP NOTED LT LATERAL SHEAR PLATE AT Y1162 FROM FRAME 69 TO FRAME 70 HAS CORROSION AND FOUR SHEARED FASTN ERS AT FWD END. MAINT REMOVED AND REPLACED LT LATERAL SHEAR PLATE AT Y1162 FRAME 69 TO FRAME 70 IAW SRM 51-72-11. UPON C OMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800480 1 20080711 A 5347 D5347209000300 SEAT TRACK AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED THE RT LONGERON BEAM Y-765 AT FRAME 66 HAD CORROSION AROUND THE HOLE. MAINT REMOVED AND REPLAC ED CORRODED LONGERON BEAM AT Y-765 FRAME 64 TO FRAME 66 IAW SRM 51-42-11 AND 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800491 1 20080715 A 7120 D5461025200000 FITTING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE NR 1 NACELLE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED THE NR 1 ENGINE PYLON PANEL NR 413CL MOUNTS STRUCTURE WAS CRACKED AT AFT UPPER SCREW HOLE. MAI NT REPAIRED NR 1 ENGINE PYLON PANEL NR 413CL MOUNT STRUCTURE AT AFT UPPER HOLE IAW SRM 54-52-12 AND 51-42-11. UPON COMPL ETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800483 1 20080715 A 5320 D5397470900000 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT PROFILE AT FRAME C63 IS GOUGED AND HAS A RIVET PULLING THROUGH. MAIN T REMOVED AND REPLACED PROFILE AT FRAME C63 IAW SRM 51-72-11, 51-21-11 AND 51-42-11. UPON COMPLETION OF THE REPAIR IT WA S INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 SO 2008 8 22 SIMA200816401 1 20080604 A 5751 14573900417 BOLT EMB 145 EMB145LR 3260212 SO NR 1 ALIERON DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 687JS 9701 14500846 WHILE INVESTIGATING SCRATCHES ON THE NUMBER ONE AILERON MAINTENANCE DISCOVERED THAT THE NUMBER ONE AILERON DAMPENER TO A ILERON ATTACHMENT FITTING BOLT WAS NOT ATTACHED TO THE AILERON. IT WAS LATER DISCOVERED THAT THE NUMBER ONE AILERON DA MPENER BOLT WAS SHEARED AND THE REMAINING BOLT SHANK WAS FOUND STILL STUCK IN THE DAMPENER BOLT HOLE. IT WAS ALSO FOUND THAT THE AILERON DAMPENER ATTACH FITTING WAS GOUGED AND DAMAGED ALONG WITH THE AILERON SHROUD. AIRCRAFT REMOVED FROM S ERVICE. REMOVED AND REPLACED THE NUMBER ONE DAMPENER BOLT AND AILERON SHROUD. THE AILERON DAMPENER ATTACH FITTING WAS PASSED. THE REPAIR WAS DIFFERED UNTIL THE NEXT "C" CHECK. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080822 EU 2008 8 22 SIM2008F00015 1 20080602 A 2121 EVCTA465A FAN SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 232AE 340B232 ON FLIGHT 3278 - CREW NOTED, AFTER NR 2 ENGINE START SMOKE ODOR IN THE COCKPIT AND CABIN. NOTICED THAT THE LT RECIRC LI GHT HAD ILLUMINATED AND ALL OTHER INDICATIONS WERE NORMAL OTHER THEN THE SMOKE. CREW DECLARED AN EMERGENCY AND LANDED W ITHOUT INCIDENT PASSENGERS DEPLANED SAFELY. AIRCRAFT REMOVED FROM SERVICE. FOUND PASSENGER COMPARTMENT AIR RECIRCULATI ON FAN BURNED OUT. REMOVED AND REPLACED FAN IAW SAAB 340 AMM 21-22-10. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO S ERVICE. (A) 2 L 7 2 4T RT A52EU 20080822 EU 2008 8 22 GUU2008F00036 1 20080812 A 3150 WARNING LIGHT SAAB SF340 340B 7860101 EU LT TAILPIPE FALSE INDICATION A GUUA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 17 9CJ 340B224 LT TAIL PIPE HOT. ILLUMINATED DURING TAKEOFF AT 100 KTS. PERFORMED LT TAIL PIPE HOT (LIGHT) DETECTION SYSTEM AND RAN L T ENG AT FULL POWER SETTING IAW SAAB 340 AMM 71-00-00 AND NO DISCREPANCY NOTED AT THIS TIME. (S) 2 L 7 2 4T RT A52EU 20080825 EA 2008 8 25 COMA086344 1 20080811 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 640 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 477CA 14838 7670 RT SIDE 640 FRAME CRACKED. REPAIRED RT SIDE FS 640 FRAME IAW REO 601R-53-61-366, 601R-53-61-506, 601R-53-61-569. (S) 2 L 7 2 4F RT A21EA 20080825 2008 8 25 DXTA200803220 4 20080808 A 3460 INDICATION SYS CESSNA 680 680CE 2076811 CE MLG MALFUNCTIONED E DXTA O OTHER N FALSE WARNING CL CLIMB 1 GL 07 311QS 6800196 AFTER TAKEOFF, POSITIONED GEAR HANDLE UP. THE MAINS CAME UP BUT THE NOSE DID NOT RETRACT AND THE RED UNLOCK LIGHT STAYE D ILLUMINATED. (S) 2 L 7 2 4F RC T00012WI 20080825 WP 2008 8 25 IXX2008F00081 1 20080609 A 5730 SKIN DOUG DC8 DC872F 302199E WP RIGHT WING DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD SLOT VANE LEADING EDGE HAS ELONGATED HOLES AT STATION XS 247.00 0. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XILD 7095.000 - XS 247.000 IAW DC8 SR M 57-3-2 FIGURE 10 PAGE 22 ITEM F, DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-3-0, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080825 NM 2008 8 25 2008UALA03805 1 20080709 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR OUT OF TOLERANCE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 L-2 DOOR REQUIRES DOUBLER AT UPPER HINGE ARM CUTOUT. ACCOMPLISHED MAJOR REPAIR AT GSO. INSTALLED DOUBLER RPR PER MM 52 -11-87. 2 L 7 2 4F 4 F RT A2NM E17NE 20080825 NM 2008 8 25 2008UALA03824 1 20080710 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR OUT OF RIG A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 588UA 26717 SLIDE 3R ARMED LIGHT WILL NOT ILLUMINATE. TETHER STRAP INTERFERENCE WITH ARMING MECHANISM. REROUTED TETHER FOR GIRT BA R. GND CHECKS OK, ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080825 SO 2008 8 25 C2XA08SH101 1 20080809 A 4910 14526850401 FIREWALL EMB 145 EMB145LR 3260212 SO APU BAY CRACKED A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 13975 145163 SHV - DURING C-CHECK IT WAS FOUND THAT THE APU FIREWALL WAS CRACKED AROUND RIVETS AT 3 O`CLOCK POSITION. MAINTENANCE PE RFORMED A DOUBLER REPAIR IAW EXPRESSJET EC5330-01827. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080821 NM 2008 8 21 SWAA084408 1 20080807 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZONTAL STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 452WN 29846 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 139. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843242 1 20080625 A 5753 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU LT WING TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 LT OB AFT FLAP LOWER SURFACE CHAFED. REMOVED DAMAGED EXISTING DOUBLER AND INSTALLED NEW DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 2008 8 20 SWAA084329 4 20080802 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084332 1 20080804 A 5311 65C22909 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084334 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 3R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084339 1 20080804 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 SWAA084322 1 20080804 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843233 1 20080627 A 5347 65538449 CARGO TRACK BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 911-947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AFT CARGO TIE DOWN TRACK IS CORRODED. REPLACED TIE DOWN TRACK. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084567 1 20080813 A 5330 6545776 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080820 EU 2008 8 20 USAA920081412 1 20080724 A 3397 SPLICE AIRBUS 320 A320231 3930325 EU CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625AW 064 FLT 401 ORD-PHX - EEL EMERGENCY PATH LIGHT INOP ROW 17 LT. MAINTENANCE REPLACED BROKEN SPLICES UNDER SEAT. OPERATIONAL CHECK WAS GOOD. (A) 2 L 7 2 4F RT A28NM 20080820 NM 2008 8 20 ASAA0873275 1 20080723 A 2731 251A24207 CONTROL VALVE BOEING 737 737790 13844CN NM ELEVATOR TAB FAILED A ASAA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 NM 02 609AS 29599 29752 UNUSUAL VIBRATION FELT IN FLOOR OF AC DURING FLIGHT, STRONGEST VIBRATION IN OVERWING AREA AT CABIN. ALSO, A SUBTLE YAWIN G MOTION FELT IN REAR GALLEY AREA EVERY FEW SECONDS. PRECAUTIONARY EMERGENCY DECLARED & AC DIVERTED. REF LP 6428995, DU RING CONDITIONAL INSPECTION FOUND RT ELEVATOR TAB CONTROL VALVE FAILED IN FLAP DOWN POSITION. REMOVED & REPLACED OER 27 -31-35-000-801. OPS GOOD. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843262 1 20080703 A 5315 654583470 FLOORBEAM BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 FLOORBEAM LOWER STABILIZER AT STA 312 + BL "O" AS IS CRACKED STOPPED DRILLED THE CRACK, FABBED A DOUBLER + INSTALLED THE REPAIR IAW SRM 53-10-51, REPAIR 4. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 F3LA200800409 1 20080701 A 2120 UNKNOWN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CABIN ODOR A F3LA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 929FR 2240 DURING FLIGHT, FLIGHT CREW NOTED AN ODOR OF GAS IN AFT GALLEY. MAINT INSPECTED AC FOR UNSATISFACTORY CABIN AIR QUALITY IAW TSM 21-00-00-810-802. NO ODOR OR SOURCE OF ODOR WAS NOTED. FIRE DEPARTMENT AND HAZMAT CREW INSPECTED THE CABIN AND CARGO COMPARTMENT, AND ALL LUGGAGE. NO ODOR OR SOURCE OF ODOR WAS NOTED AND AC CONTINUED SERVICE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 2008 8 20 SWAA084540 4 20080814 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 F3LA200800411 1 20080702 A 2571 D5391215720000 FITTING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE BATTERY TRAY WORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 DURING C-CHECK INSP NOTED FWD BATTERY TRAY OB AFT MOUNT HAS WEAR. MAINT REMOVED AND REPLACED FWD BATTERY TRAY OB AFT MOU NT IAW SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800400 1 20080624 A 5320 D5367414400000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSP, NOTED AFT CARGO PIT FWD LT UPPER TRANSITION PANEL 151FE HAS A HOLE AT FWD TOP CORNER. MAINT REPAIR ED TRANSITION PANEL 151FE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTA BLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800379 1 20080620 A 5315 D5348004320501 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP NOTED RT CABIN FLOOR LOGERON BEAM Y1732 AT FRAME 66 HAS CORROSION AROUND FASTENER HOLE. MAINT FABRI CATED ANGLES AND FILLER AND ACCOMPLISHED DETAILED REPAIR IAW EA A0-53F-12234, EA A0-53R-30370 AND SRM 53-41-14. UPON COM PLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800369 1 20080616 A 2560 D531112191203 MOUNT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED R1 DOOR FWD GIRT BAR MOUNT AFT TWO HOLES IN FUSELAGE WEB HAVE CORROSION AROUND THEM. MAINT R EMOVED CORROSION AND MADE UP REPAIR SHIMS IAW EA A9-53R-30358. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 EU 2008 8 21 F3LA200800367 1 20080616 A 5321 D5367423900000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 941FR 2483 DURING C-CHECK INSP, NOTED AFT PIT FLOOR PANEL 151CE HAS SEVERAL PUNCTURES. MAINT REPAIRED PANEL 151CE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 SWAA084377 1 20080806 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR UPPER HINGE. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03713 1 20080703 A 3150 WARNING MESSAGE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 215UA 30221 HIGH GAIN AND SAT SYS STATUS MESSAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080821 NM 2008 8 21 SWAA084398 1 20080806 A 3350 3071BPEGPL LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 776WN 30591 DURING SCHEDULED 8Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084409 1 20080807 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 277 S11R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03695 1 20080702 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1415 S1 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 LIGHTNING STRIKE ON RIVET EDGE AT STA 1415, STR 1. DAMAGE FROM LIGHTNING STRIKE. REMOVED AND REPLACED DAMAGED FASTENER WITH BLIND FASTENER PER MM 53-30-95, P602, ITEM 6. FASTENER WILL BE REINSPECTED AT NEXT C-CK AND REPLACED AT NEXT D-CK . 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NM 2008 8 21 SWAA084411 1 20080807 A 5322 69353656 SHEAR TIE BOEING 737 7375H4 138449D NM BS 328 S20R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 513SW 24190 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 328, STR 20R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084399 1 20080806 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM BS 466 S16R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 466, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084365 1 20080805 A 5310 6516352 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT LOWER CORNER. REPAIRED FRAME PER ACO. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084366 1 20080805 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S28L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500A, STR 28L, WL 148. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03724 1 20080705 A 5320 CUSP WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1420 S17R CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 CORROSION AT CUSP AT STR 17R AND STA 1420 TO 1420. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED CORRODED WEB AND F AB NEW WEB REF BOEING DWG INSTALLED REF SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NM 2008 8 21 2008UALA03729 1 20080705 A 2120 FILTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AIR SUPPLY CLOGGED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 550UA 25398 EQ COOLING HORN SOUNDED & OVERHEAT LIGHT IS ON. *S/D* AIR SUPPLY FILTER CLOGGED, NO AIR FLOW. REPLACED FILTER AND CLE ANED SENSOR, SYS CHECKED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080825 NM 2008 8 25 2008UALA03368 1 20080614 A 2100 672951001 SHUTOFF VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COOLING FAN FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 652UA 25390 EQUIPMENT COOLING FAN EICAS MESSAGE. AFTER TROUBLESHOOTING FOUND SHUTOFF VALVE TO BE FAULTY. REPLACED VALVE PER MM 21- 23-08, ALL OPS & INDICATIONS NOW NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080825 NM 2008 8 25 2008UALA03401 1 20080614 A 2121 732591F FAN BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE SHORTED A UALA O OTHER J WARNING INDICATION LD LANDING 1 WP 29 674UA 29242 FWD EQUIP SUPPLY FAN STATUS MSG SHORTLY AFTER LANDING. BURNING SMELL IN COCKPIT FOR 4 MINS. SUSPECT EQUIPMENT SUPPLY F AN SHORTED. REPLACED FAN PER MM 21-58-06. TEST NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080825 NM 2008 8 25 2008UALA03402 1 20080616 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 ENGINE FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 218UA 30222 ELEC GEN SYS R IDG HAS DISCONNECTED OR A PROTECTIVE TRIP OF THE GENERATOR CONTROL BREAKER HAS OCCURRED OR A PROTECTIVE T RIP OF THE BTB HAS OCCURRED. STATUS MSG01- LATCHED CLIMB MODE DEPENDENT; INTEGRATED DRIVE GENERATOR (R) FREQUENCY IS L OW. DB- GENERATOR CONTROL UNIT (R) MSG-2431632 LATCHD CL MODE. *S/D* SUSPECT FAULTY BEARING. REPLACED IDG PER MM 24 -11-01 PG 401 AND MM 24-11-00 PG 501. OPS & LEAK CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080825 NM 2008 8 25 2008UALA03403 1 20080613 A 3350 2073771001 LENS BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE EMERGENCY LIGHT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 793UA 26946 LIGHT COVER ON THE AFT SIDE OF DOOR 4L IS MISSING. *S/D* SUSPECT IMPROPERLY INSTALLED. REPLACED LIGHT COVER. AC OK F OR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080825 NM 2008 8 25 2008UALA03796 1 20080708 A 3397 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 EEL LIGHT BAR AT APPROX STA 650 DAMAGED. *S/D* REPAIRED BROKEN LIGHT BAR CABLE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080825 EA 2008 8 25 HNAA08A0003 1 20080612 A 5210 STRUCTURE DHAV DHC8 DHC8311 1386006 EA PAX DOOR CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 335EN 32270 32270 375 CORROSION PAX DOOR GOOSENECK FOUND CORRODED FWD AND AFT. REPLACED PAX DOOR GOOSENECK. (S) 2 H 7 2 4T RT A13NM 20080825 EA 2008 8 25 TRAX200800992 1 20080810 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 AFT DRAG ANGLE IS CRACKED NEAR DOOR ASSIST PULLEY. WORK COMPLETED IAW: REMOVED AND REPLACED 670-52-11-072-1 AFT ANGLE SECTION (PREVIOUSLY REPAIRED) AS PER REO 670-52-11-072. JOB COMPLETE. (S) 2 L 7 2 4F RT A21EA 20080825 EU 2008 8 25 NSV2008F00020 1 20080814 A 3397 WIRE SAAB SF340 340B 7860101 EU EMERGENCY LIGHT DISCONNECTED A NSVA K NONE O OTHER IN INSP/MAINT 1 EA 27 339CJ 340B339 DURING OPS CHECK OF EMERGENCY LIGHTS ON LC1, LIGHTS 46LN AND 66LN WERE INOPERATIVE. FOUND WIRE TO FUSE 70LN PULLED OFF OF FUSE. WIRE WAS RE-SECURED TO FUSE 70LN. OPERATONAL CHECK OF LIGHTS WAS GOOD. (S) 2 L 7 2 4T RT A52EU 20080825 CE 2008 8 25 DXTA200803233 1 20080818 A 2120 UNKNOWN CESSNA 750 750 2076810 CE COCKPIT ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 944QS 7500144 IN FLIGHT CREW DETECTED DEEP MUSTY ODOR FOLLOWED BY BURNING ODOR FROM ENVIRONMENTAL SYSTEM. (S) 2 L 7 2 4J RT T00007WI 20080825 EU 2008 8 25 USAA920081521 1 20080812 A 5320 D5347219420400 FLOOR SUPPORT AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 PIT -S4- MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT DUMMY RAIL AT FR68, Y630. REPLACED FLOOR SUPPORT DU MMY RAIL AT FR68, Y630 IAW A319 SRM 51-42-00. (S) 2 L 7 2 4F RT A28NM 20080825 NM 2008 8 25 AALA200801866 1 20080713 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 602AN 27053 DFW - EMERGENCY LIGHT AT SEAT 33 INOPERATIVE. REPAIRED CONNECTOR AT WALL DISCONNECT FOR EMERGENCY LIGHT AT SEAT 33. SY STEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A2NM 20080825 WP 2008 8 25 AALA200801857 1 20080711 A 3397 WIRE DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 447AA 49473 LGA - EMERGENCY LIGHTS AT SEAT ROW 21 TO AFT CABIN INOPERATIVE. REPAIRED SHORT IN WIRING AT SEAT ROW 31DEF FOR EMERGENC Y LIGHTS AT SEAT ROW 21 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F A6WE 20080825 EU 2008 8 25 USAA920081540 1 20080818 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 656AW 1079 FLT 12 SEA-PHX - EMERGENCY EQUIPMENT - ACFT LEFT AFT FLASHLIGHT NOT BLINKING AND ACFT RIGHT AFT FLASHLIGHT LOOSE. MAINT ENANCE REMOVED AND REPLACED THE LT AFT FLASHLIGHT BATTERY AND SECURED THE RT AFT FLASHLIGHT HOLDER. (S) 2 L 7 2 4F RT A28NM 20080825 EU 2008 8 25 USAA920081515 1 20080813 A 3350 321430 BATTERY AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 770UW 1393 FLT 1231 PHL-TPA - EMERGENCY EQUIPMENT - CENTER EMERGENCY LIGHT BATTERY LOW POWER. MAINTENANCE REMOVED AND REPLACED CEN TER EMERGENCY LIGHT BATTERY. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080825 EU 2008 8 25 YENA2008076 1 20080810 A 2700 3945126102 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ELAC FAILED A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 603JB 27467 3713 2352 FLT 233, SLC-LGB, AFTER TAKEOFF ACFT SUFFERED A L&R AIL FAULT WITH ACFT ONLY ABLE TO FLY IN ALTERNATE LAW. PER PFR MSGS ELAC AIL ORDER DISAGREE & ELAC 2 AIL ORDER DISAGREE WERE FOUND. PER TSM 27-93-00-810-949 STEP 4A. ELAC (2CE1) NEEDS RE PLACING. PERFORMED TSM 34-13-00-810-967. NO PRESENCE OF WATER WAS FOUND ON ANY OF THE ADIRS OR ADIRS AREA. REMOVED AN D REPLACED ELAC 1 (2CE1) IAW 27-93-34-04. OPS TEST NORMAL THIS TIME. NO FAULTS FOUND. (S) 2 L 7 2 4F 4 F RT A28NM E40NE 20080825 NM 2008 8 25 QXEA200800357 1 20080330 A 5522 SKIN DHAV DHC8 DHC8202 2809007 NM RT ELEVATOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 356PH 502 PDX-C4 CHECK FOUND DENT ON THE BOTTOM OF THE RT ELEVATOR AT STN YH92.20, APPROX 13 INCHES FWD OF THE AFT SPAR. FOUND OU T OF LIMITS IAW RD8-55-1448. HFEC INSP FOR CRACKS, NO CRACKS NOTED. REMOVED RIVETS, FABRICATED REPAIR DOUBLER IAW RD8- 55-1930. INSTALLED DOUBLER IAW RD8-55-1930 STEPS 9-13. (S) 2 H 7 2 4T RT A13NM 20080825 NM 2008 8 25 AALA200801863 1 20080713 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 631AA 24589 JFK - EMERGENCY LIGHTS AT SEAT 26D TO LAST ROW INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT 26D TO L AST ROW. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A2NM 20080825 NM 2008 8 25 AALA200801860 1 20080713 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 617AM 24525 JFK - EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT 2A FOR EMERGENCY LIGHTS AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A2NM 20080825 NM 2008 8 25 AALA200801858 1 20080711 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 758AN 32637 DFW - EMERGENCY LIGHT AT SEAT 20C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED N ORMAL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20080825 WP 2008 8 25 AALA200801856 1 20080711 A 2780 SWITCH DOUG DC9 DC982 3022082 WP COCKPIT INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 234AA 49181 DFW - INFLIGHT T1776/11JUL - CREW REPORTED SLAT DISAGREE LIGHT ILLUMINATED AFTER ROTATION. RETURNED TO DFW AND LANDED W ITHOUT INCIDENT. REPLACED FLAP HANDLE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F A6WE 20080825 EU 2008 8 25 USAA920081520 1 20080812 A 5347 D5347209300000 SEAT TRACK AIRBUS A319 A319112 3930323 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 PIT -S4- MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON SEAT TRACK BEAM BETWEEN FR67 TO FR68, -765. REPLACED SEAT TR ACK BEAM BETWEEN FR7 TO FR68, -Y765. (S) 2 L 7 2 4F RT A28NM 20080825 NM 2008 8 25 KCSA081408 1 20080818 A 5312 BULKHEAD BOEING 747 747122 1384872 NM BS 1241 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 716CK 19753 CORROSION ON CANTED BULKHEAD LOWER AFT CORD AT BS 1241, LBL 95. (S) 2 L 7 4 4F RT A20WE 20080825 NM 2008 8 25 KCSA081405 1 20080730 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 770 S41R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 AT BS 770, STRINGER 41R DAMAGED. (S) 2 L 7 4 4F RT A20WE 20080825 EA 2008 8 25 VNAA0808002 1 20080801 A 5200 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE GROUND POWER OPEN A VNAA A UNSCHED LANDING W INADEQUATE Q C NR NOT REPORTED 1 GL 05 705PS 10144 CREW ELECTED TO RETURN TO MSY FOR GROUND POWER DOOR LEFT OPEN. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED A CFT WITH NO DEFECTS NOTED. ACFT WAS RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E00063EN 20080825 NM 2008 8 25 AALA200801890 1 20080716 A 3350 02031461201 SIGN BOEING 737 737823 13844BZ NM EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 943AN 30599 LGA - EMERGENCY EXIT IDENTIFIER LIGHT AT RT NR 1 DOOR NEAR GARBAGE BIN BROKEN. REPLACED EXIT LIGHT IDENTIFIER ASSEMBLY AT RT NR 1 DOOR NEAR GARBAGE BIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A16WE 20080825 SO 2008 8 25 C2XA08SH100 1 20080801 A 3240 21707 BRAKE ASSY EMB 145 EMB145XR 3260214 SO NR 3 DRAGGING A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 14173 14500872 DEN - FLIGHT 7790 - AFTER TAKEOFF PERFORMED AIR RETURN DUE TO LANDING GEAR LEVER DISAGREE - RT MAIN LANDING GEAR WOULD N OT RETRACT DUE TO BLOWN TIRE. MAINTENANCE REMOVED AND REPLACED THE NR 3 BRAKE ASSEMBLY IAW EMB 145XR AMM 32-49-03, NR 3 AND NR 4 MAIN WHEEL ASSEMBLIES, RT MLG AUXILLARY BRACE STRUT AND DOWNLOCK ACTUATOR/MOUNT BRACKET/HARNESS/PROXIMITY SWIT CH, AND VARIOUS LINES AND BRACKETS IN THE WHEEL WELL. THE RT ENG REQUIRED 3 FAN BLADES AND 14 OUTER BYPASS VANES REPLAC ED FOR FOD DAMAGE. THE ACFT WAS APPROVED FOR FERRY FLIGHT TO SHV FOR FURTHER MAINTENANCE. MAINTENANCE AT SHV REMOVED A ND REPLACED THE RT INBOARD FLAP, FLAP SHROUD, AND REPAIRED MINOR SKIN DAMAGE TO THE RT WING LOWER SURFACE. RT ENG VIBRA 2 L 7 2 4F RT 20080826 NM 2008 8 26 KCSA081362 1 20080731 A 5415 GUSSET BOEING 747 747209B 138489B NM NR 4 NACELLE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 NR 4 PYLON EDP PRESSURE LINE UNION FITTING CHAFING INSIDE PYLON. (A) 2 L 7 4 4F RT A20WE 20080826 NM 2008 8 26 WRLA2008064 1 20080731 A 2520 ACTUATOR DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE SEAT BACK 18G ODOR A WRLA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 11 278WA 48746 FLT 1000 (KIAH/FNLU) ITEM: DURING FLIGHT, SMOKE/FUMES IN CABIN IN VICINITY OF ROW 16 & 17. MAINTENANCE FOUND LARGEST A CTUATOR AT SEAT 18G AS SOURCE OF ELECTRICAL ODOR. DEACTIVATED CONTROL BOX FOR SEATS 18 D&G BY STOWING CONNECTORS AND PU LLED C/B. REMOVED AND REPLACED SEAT ASSY PER MD-11 MM 26-21-01. (A) 2 L 7 3 4F 4 F RT A22WE E24NE 20080826 EA 2008 8 26 MASA200800466 1 20080612 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY DOOR OUT OF ADJUST A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 926LR 15026 ASH FLT 2834 PHX-TUS. LEFT AFT EMERGENCY DOOR CAUTION EN ROUTE TO TUS. ADJUSTED PROX SENSOR. (B) 2 L 7 2 4F RT A21EA 20080826 SO 2008 8 26 WWQ2008F00001 1 20080801 A 8011 YU10352 STARTER GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU RT ENGINE WORN E WWQA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 07 995GG 9182 1519 1074 16257 RT ENG FAILED TO START. FOUND THAT THE STARTER WAS BAD. DURING THE STARTER REPLACEMENT NOTICED ABNORMAL WEAR ON THE EN G GEAR BOX STARTER GEAR. CONTACTED ENGINEERING DEPARTMENTS TO ASK FOR LIMITATIONS. AFTER ENGINEERING DEPARTMENTS REVIE WED THE PICTURES, DETERMINED THAT THE STARTER GEAR BOX GEAR REQUIRED FURTHER EVALUATIONS. AFTER OPERATOR OBTAINED A REN TAL ENG, OBTAINED A SPECIAL FLIGHT PERMIT (FERRY FLIGHT) AND FLEW THE ACFT FROM KTEB TO KTUL. AFTER ARRIVING IN KTUL ON 08/01/08 , ENGINEERS DETERMINED THE STARTER GEAR IN THE GEAR BOX REQUIRED REPLACEMENT. A RENTAL ENG IS BEING INSTALLED AND ENG S/N 16257 GEAR BOX STARTER GEAR WILL BE REPLACED. (S) 2 L 7 2 4F 4 F RT A12EA E25NE 20080826 EU 2008 8 26 MAL2008F00019 1 20080730 A 5753 FASTENER SAAB SF340 340B 7860101 EU TE FLAP UNKNOWN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 REPLACED FASTENERS IN RT FLAP FAIRING AFT BULKHEAD UPPER FLANGE TO REAR SPAR IAW EOS57051. FLAP FAIRING AFT BULKHEAD UP PER FLANGE TO REAR SPAR - ALTERNATIVE FASTENER REPLACEMENT AUTHORIZATION. STANDARD SRM REPAIR PROCEDURES. NO INFORMATI ON ON THE PART CONDITION AT THIS TIME. (S) 2 L 7 2 4T RT A52EU 20080826 EA 2008 8 26 TRAX200800805 1 20080619 A 2750 FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 843AS 7310 FLAPS FAIL EICAS CAUTION MSG WHEN FLAPS SELECTED FROM 20 TO 30. FLT 4343 CX. REMOVED AND REPLACED FECU IAW CRJ200 AMM 27-51-05, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080826 WP 2008 8 26 IXX2008F00065 1 20080617 A 5730 SKIN DOUG DC8 DC872F 302199E WP LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C-CHECK INSPECTION, FOUND LT WING CRACKED ON LEADING EDGE UPPER SKIN AT STATION XCW 69.500. REMOVED FAST ENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION, FABRICATED DOUBLER, FILLER PLUG. PERFORMED HEAT TREATMENT CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTE NERS AND REPAIR PARTS IAW SRM 57-2-1 FIGURE 20 SHEETS 1, 2, 3 SRM 51-1-20D, SRM 57-2-1 FIGURE 20 SHEET 1, SRM 51-1-12 FI GURE 7, NDT SPM PART 06-10-01-001, SRM 57-3-2 FIGURE 15 ITEM "J", SRM 51-10-0 FIGURE 21, SRM 51-1-1 PAGES 1, 13 AND 17 S RM 51-1-8, AND SRM 51-1-11. (S) 2 L 7 4 4F RT 4A25 20080826 NM 2008 8 26 2008UALA03784 1 20080709 A 3510 MF20010 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CAPTAIN'S NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 597UA 28750 CAPTAIN'S O2 MASK COMM WILL NOT TEST. *S/D* SHORT IN O2 MASK ASSY. REPLACED CAPT O2 MASK ASSY. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080826 NM 2008 8 26 2008UALA03772 1 20080708 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1480 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 AFT PIT LT SIDE SLANT AREA HAS DENTED FRAME AT STA 1480 AT STR 26L. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. REPAIRED ON NR 31083. 2 L 7 2 4F 4 F RT A2NM E17NE 20080826 NM 2008 8 26 2008UALA03774 1 20080708 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1560 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 AFT PIT AT STA 1560, APPROX STR 26L, FRAME DENTED AT INBOARD FLANGE. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. AFT PIT AT STA 1560, APPROX STR 26L, FRAME DENTED AT INBOARD FLANGE. RPR FRAME IAW SRM 53-00-07 RPR 5 DETAIL I. THIS IS A CAT B RPR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSPECTIONS STARTING AT 50,000C AND 12,000C THEREAFTER PER SRM 53-00-07 RPR 5 TABLE II. THIS INSP CONSISTS OF BOTH DETAILED VISUAL AND NDT. CURRENT PTC IS 20699. 2 L 7 2 4F 4 F RT A2NM E17NE 20080826 NM 2008 8 26 2008UALA03777 1 20080708 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1433 S28-29R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 FUSELAGE APPROX AT BS 1433 BETWEEN S28-29R SKIN HAS ELONGATED HOLE. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED FASTENE R AND CLEANED UP HOLE. INSTALLED BLIND FASTENER IAW SRM 51-40-02 AND MM 53-30-95 PG 602. PER MM 5 3-30-95 PG 602 BLIND FASTENER MUST BE REINSPECTED AT EACH C-CK AND REPLACED WITH A SOLID FASTENER AT NEXT HMV. 2 L 7 2 4F 4 F RT A2NM E17NE 20080826 NM 2008 8 26 USAA920081512 1 20080731 A 5315 D53112782202 FLOORBEAM AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 833AW 1844 SAL -BC4- MAJOR REPAIR - FLOORBEAM CORRODED AT FR12 TO FR24, -Y1292. REPLACED FLOOR BEAM AT FR12 TO FR24, -Y1292 IAW A3 19 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080826 WP 2008 8 26 IXX2008F00074 1 20080611 A 5313 LONGERON SPLICE DOUG DC8 DC872F 302199E WP BS 1610 L17R CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE SPLICE FITTING CRACKED AT STATION FS 1610.000 LONGERON 17RT. REMO VED CRACKED SPLICE FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-21, SRM 51 -1-20D, DC8 SRM 51-1-8B, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080826 WP 2008 8 26 IXX2008F00075 1 20080612 A 5340 LONGERON CLIP DOUG DC8 DC872F 302199E WP BS 235 L31L CORRODED A IXXA O OTHER O OTHER NR NOT REPORTED 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND AC COMPARTMENT CLIP CORRODED AT STATION 235.000 LONGERON 31LT. REMOVED CORROSI ON. FOUND OUT OF LIMITS. REMOVED CORRODED CLIP. FABRICATED NEW CLIP. CLEANED, TREATED AND PRIMED CLIP. INSTALLED CL IP IAW DC8 SRM 51-1-20D, SRM 51-3-1, DC8 SRM 51-1-8 PAGED 17-18, DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 51-1-20D, DC8 SRM 53-2- 0, DC8 SRM 51-1-8B. (S) 2 L 7 4 4F RT 4A25 20080822 NM 2008 8 22 F3LA200800469 1 20080714 A 5315 DAN338C05 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT CENTER FLOORBEAM HAS CORROSION BETWEEN FRAME C57 AND FRAME C58. MAINT RE MOVED AND REPLACED CORRODED FLOORBEAM AT FRAME C57 AND FRAME C58 IAW SRM 51-41-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800488 1 20080715 A 5310 D53477121200 DOOR FRAME AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO DOORWAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED CORROSION ON TOP LEG OF FRAME C55A AT FWD EDGE OF C2 DOOR. MAINT REPAIRED DAMAGE ON TOP LEG OF FRAME C55A IAW EA NR A9-53R-30442. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 SW 2008 8 22 SIMA200816501 1 20080605 A 5315 FLOORBEAM SWRNGN SA227 SA227AC 8780603 SW GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 340AE AC510 DURING A HMBV INSPECTION, THE L ANGLE ON FRAME 225 AT THE GALLEY FLOOR AREA WAS FOUND TO HAVE LEVEL TWO CORROSION. FABR ICATED A FILLER, SHIM AND REPAIR ANGLE. TREATED ALL PARTS AND INSTALLED IN AIRCRAFT. REPAIR DONW IAW SAAB 340 SRM (SRM 72LKS 3079 REV 50) CHAPTER 53-70-30. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4T RT A8SW 20080822 SO 2008 8 22 C2XA08IA190 1 20080802 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12201 14500959 SLC-FLIGHT 7672, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE FORWARD EMEGENCY EXIT SIGN WAS INOPERATIVE. MAI NTENANCE OPERATIONALLY CHECKED THE EMERGENCY LIGHTING WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERV ICE. DURING POST FLIGHT INSPECTION ON FLIGHT 7672 IN MCI, THE DISCREPANCY REPEATED. MAINTENANCE REMOVED AND REPLACED T HE NR 6 EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE . (S) 2 L 7 2 4F RT 20080822 WP 2008 8 22 AALA200801829 1 20080709 A 2560 STRAP DOUG DC9 DC983 3022083 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 594AA 53284 LGA - EMERGENCY FLASHLIGHT AT FORWARD UPPER POSITION HAS BROKEN SAFETY STRAP. REPLACED SAFETY STRAP FOR EMERGENCY FLASH LIGHT AT FORWARD UPPER POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A6WE 20080822 WP 2008 8 22 AALA200801827 1 20080709 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 594AA 53284 LGA - EMERGENCY LIGHTS AT OVERHEAD COCKPIT INOPERATIVAE. REPLACED BATTERY PACK AT B5-23 FOR EMERGENCY LIGHTS AT OVERHEA D COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A6WE 20080822 NM 2008 8 22 KCSA081383 1 20080813 A 5343 ATTACH ANGLE BOEING 747 747122 1384872 NM MLG CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 716CK 19753 CORROSION FOUND ON ATTACH ANGLE OF LANDING GEAR SUPPORT BEAM AT STA 1350, RBL 35. (S) 2 L 7 4 4F RT A20WE 20080822 NM 2008 8 22 AALA200801891 1 20080716 A 3350 PBS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 172AJ 32400 JFK - EMERGENCY EXIT SIGN AT RT NR 4 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN AT RT NR 4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A2NM 20080822 WP 2008 8 22 IXX2008F00076 1 20080612 A 5313 LONGERON DOUG DC8 DC872F 302199E WP BS 1320-1340 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO BAY LONGERON 36 CORRODED AT STATION 1320.000-1340.000. REMOVED CORRO SION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED LONGERON SEGMENT. FABRICAT ED SPLICE OF EXTRUSION. CLEANED, TREATED AND PRIMED AREA AND SPLICE. INSTALLED NEW FASTENERS AND LONGERON SEGMENT IAW SRM 53-2-2 PAGE 6 FIGURE 4A, SRM 51-1-8 PAGES 17-18, SRM 53-2-0 PAGE 2P, SRM 53-2-2 FIGURE 10 SHEET 2, SRM 53-2-2 FIG 10 SHEET 4 TR 53-193 DATED 03/15/04, SRM 51-1-8B, SRM 51-2-0 FIGURE 52 SHEET 1, SRM 51-2-0 FIGURE 50 SHEET 65, SRM 53-4-1 FIGURE 44B SHEET 2 ITEM "L", SRM 51-1-20D, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080822 NM 2008 8 22 AALA200801849 1 20080710 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 762AN 31479 BOS - EMERGENCY LIGHT AT FIRST CLASS CLOSET DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FIRST CLASS CLOSET D OOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20080822 EU 2008 8 22 SIMA200822403 1 20080810 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT FAILED A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 218AE 340B218 ON FLIGHT 3270 - ON GROUND CREW REPORTED ALL EMERGENCY LIGHTS INOPERATIVE ON PREFLIGHT. ACFT REMOVED FROM SERVICE. FOU ND EMERGENCY POWER SUPPLY 21 LN BATTERY DRAINED. REMOVED AND REPLACED POWER SUPPLY 21LN IAW SAAB AMM 33-50-10-04. OPER ATIONAL CHECK GOOD AT THIS TIME WITH NO FURTHER DEFECTS NOTED. ACFT RETURNED TO SERVICE. (S) 2 L 7 2 4T RT A52EU 20080825 2008 8 25 COMA086345 4 20080811 A 3422 6225812006 FLUX DETECTOR CNDAIR CL600 CL6002B19 1900309 EA NR 2 FAILED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 960CA 30807 7117 EFIS COMP MON MSG, FIRST OFFICER`S HEADING DIFFICULT TO RIGHT. ACFT RETURNED BACK TO CVG, LANDED SAFELY. REMOVED AND R EPLACED NR 2 FLUX DETECTOR. (S) 2 L 7 2 4F RT A21EA 20080825 NM 2008 8 25 UIEA200800284 1 20080815 A 5320 INTERCOSTAL BOEING 747 7472D7B 1384803 NM BS 1200 CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 524MC 21784 BS 1200 RBL 110 FLOORBEAM INTERCOSTAL WEB CRACKED. REPAIRED IAW BOEING SERVICE REQUEST 1912291334 APPROVED BY FAA FORM 8100-9 DATED 04 AUGUST 2008, DETAILS OF WORK KEPT AT ATLAS ENGINEERING ORDER EO-4753B190. (S) 2 L 7 4 4F RT A20WE 20080825 NM 2008 8 25 2008UALA03804 1 20080709 A 5210 DOUBLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR OUT OF TOLERANCE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 R-2 DOOR REQUIRES DOUBLER AT UPPER HINGE ARM CUTOUT. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. INSTALLED DOUBLER PER MM 52-11-87. 2 L 7 2 4F 4 F RT A2NM E17NE 20080825 EU 2008 8 25 2008UALA03666 1 20080702 A 2612 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LAVATORY INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 496UA 1845 LAV SMOKE DETECTOR INOPERATIVE. REPLACED LAV F SMOKE DETECTOR R EF MM 26-17-15, BITE TESTED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080825 NM 2008 8 25 2008UALA03795 1 20080709 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 598UA 28751 EXTERIOR EMERGENCY EXIT LIGHT INOP, DOOR 4L. LAMP INOP. RELAMPED ASSY, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080825 EU 2008 8 25 F3LA200800550 1 20080811 A 5321 D5367406500000 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CARGO BAY GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 806FR 30 2218 DURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT RT AFT UPPER TRANSITION PANEL 132EG HAD A GOUGE. MAINTENANCE REPAIRED DAMAGED PANEL 132EG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF TH E REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT 20080825 EU 2008 8 25 F3LA200800552 1 20080812 A 5320 D53480043204 SILL AIRBUS A318 A318111 3940019 EU FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 806FR 30 2218 DURING C3 C-CHECK, INSPECTION NOTED THE VERY AFT NUT PLATE HOLE ON L-2 DOOR SILL AT FRAME 68, JUST AFT OF GIRT BAR FITTI NG ASSEMBLY, WAS CORRODED. MAINTENANCE CUTOUT DAMAGE, MANUFACTURED REPAIR DOUBLER AND INSTALLED IAW THE REQUIREMENTS OF ENGINEERING AUTHORIZATION A8-53R-30556. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT 20080825 NM 2008 8 25 AALA200801861 1 20080713 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 617AM 24525 JFK - EMERGENCY LIGHTS AT MID COACH CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT 20D FOR EMERGENCY LIGHTS AT MID CO ACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A2NM 20080826 SO 2008 8 26 C2XA08CL093 1 20080805 A 3040 4800104 SWITCH EMB 145 EMB145XR 3260214 SO WINDSHIELD HEAT INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 14153 145761 CLE FLIGHT 2786 - THE CREW REPORTED A WINDSHIELD NR 2 HEAT FAIL ON CLIMB. THE ACFT RETURNED TO CLE WITHOUT FURTHER INCI DENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 WINDSHIELD HEAT PUSH BUTTON. OPERATIONAL CHECKS WERE GOOD. (S) 2 L 7 2 4F RT 20080826 WP 2008 8 26 IXX2008F00089 1 20080730 A 3260 SWITCH DOUG DC8 DC873F 302199F WP MLG DOOR INOPERATIVE A IXXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 11 602AL 45991 FLIGHT ATN 802, DURING CRUISE FROM KTOL, GEAR DOOR NOT LATCHED LIGHT CAME ON INTERMITTENT. THE CREW ACCOMPLISHED ABNORM AL CHECK 3-13-01. THE CREW LANDED IN KLAX WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND BAD MAIN LANDING DOOR SWITCH. M AINTENANCE REPLACED SWITCH. OPERATIONAL CHECK GOOD IAW EO 32-DC8-3730, DC8 MAINTENANCE MANUAL 32-8. ACFT HAS RETURNED TO SERVICE. (S) 2 L 7 4 4F RT 4A25 20080826 EU 2008 8 26 USAA920081495 1 20080809 A 3520 21214001 SOLENOID AIRBUS 320 A320232 3930326 EU EMERGENCY OXYGEN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 663AW 1419 PHASE 4 CHECK PHX - EMERG EQUIP - L2 DOOR OVERHEAD EMERGENCY OXYGEN GENERATOR FAILED SYSTEM TEST. DOOR WILL NOT OPEN. MAINTENANCE REMOVED AND REPLACED THE L2 DOOR OVERHEAD EMERGENCY OXYGEN CONTAINER SOLENOID. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A28NM 20080826 SO 2008 8 26 RAIA00808014 1 20080811 A 5240 ROLLER EMB 145 EMB145 3260210 SO SERVICE DOOR LACK OF LUBE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 807HK 145119 POST FLT 8039 -STL- SERVICE DOOR HARD TO OPEN AND CLOSE. MAINTENANCE LUBRICATED THE ROLLERS AND PERFORMED AN OPERATIONA L CHECK OF THE SERVICE DOOR. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT T00011AT 20080826 NM 2008 8 26 2008UALA03775 1 20080708 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1520 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 AFT PIT AT STA 1520, STR 25L FRAME DENTED AT INBOARD FLANGE. SUPPLEMENTAL DATA UPDATE ACCOMPLISHED MAJOR REPAIR AT GSO. RPR FRAME IAW SRM 53-00-07 RPR 5 DETAIL I. THIS IS A CAT B RPR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSPECTIONS STARTI NG AT 50,000C AND 12,000C THEREAFTER PER SRM 53-00-07 RPR 5 TABLE II. THIS INSP CONSISTS OF BOTH DETAILED VISUAL AND ND T. CURRENT PTC IS 20699. 2 L 7 2 4F 4 F RT A2NM E17NE 20080826 EU 2008 8 26 USAA920081523 1 20080815 A 5315 D53472190210 FLOORBEAM AIRBUS A319 A319112 3930323 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 PIT -S4- MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, Y1292. REPLACED FLOORBEAM AT FR66, Y1292 IA W A319 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080826 NM 2008 8 26 USAA920081522 1 20080814 A 5330 65C35795 SKIN BOEING 737 7373B7 1384580 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT-Q6 -MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT BS 727D, S23R. REPAIRED FUSELAGE SKIN AT BS 727D, S23R IAW US AIRWAYS EA 100595. (S) 2 L 7 2 4F RT A16WE 20080826 EA 2008 8 26 TRAX200800799 1 20080617 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 EMERGENCY LIGHT CEILING ROW 17, LIGHT OUT. REMOVED AND REPLACED EMERGENCY LAMP AT ROW 17 OVERHEAD. OPS CK GOOD REF 33- 50-01. 2 L 7 2 4F RT A21EA 20080826 SO 2008 8 26 MAS2008F00008 1 20080604 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 843MJ 145478 FDM 6025 JFK-CVG. ROW 12 OVERHEAD AFT EMERGENCY LIGHT INOP. MX RESET EMERGENCY LIGHT SYSTEM, OPS CK GOOD. (B) 2 L 7 2 4T RT T00011AT 20080826 CE 2008 8 26 DXTA200803222 1 20080811 A 3234 HANDLE CESSNA 750 750 2076810 CE MLG INOPERATIVE E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 990QS 7500190 THE LANDING GEAR HANDLE WOULD NOT MOVE AFTER TAKEOFF. (S) 2 L 7 2 4J RT T00007WI 20080826 EU 2008 8 26 COEA0803703 1 20080808 A 3240 8904091000 VALVE FOKKER F27 F27MK600 4990706 EU MLG FAILED A COEA O OTHER G P MULTIPLE FAILURE NO WARNING INDICATION TX TAXI/GRND HDL 1 NM 13 703FE 10420 BRAKE FAILURE. DURING MAINTENANCE TAXI ACFT LOST ALL STEERING AND NORMAL BRAKING FUNCTIONS. EMERGENCY BRAKING ACTIVATI ON WAS USED TO STOP THE ACFT. (S) TEARDOWN REPORT FROM VENDOR CONFIRMED THAT THE UNIT FAILED TO GIVE AIR PRESSURE. THE RINGS, SEALS, SEATS AND BALL VALVE WERE FOUND WORN. REPAIRED PRESSURE REDUCING VALVE. ACFT REPAIR BY REMOVING AND REPLA CING THE PRESSURE REDUCING VALVE ON THE BRAKE SYSTEM. (K) 2 H 7 2 4T A817 20080826 EA 2008 8 26 REX2008F00034 1 20080805 A 2750 860D1008 FCU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A REXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 8631E 7631 IN CRUISE RECEIVED SPEED CLACKER FOLLOWED BY FLAP FAIL MESSAGE. QRH FOLLOWED, EMERGENCY DECLARED LAND WITH FLAPS AT ZER O UNEVENTFUL. REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT (FECU) PER BOMBARDIER AMM. OPERATIONAL CHECK PERFO RMED. (S) 2 L 7 2 4F RT A21EA 20080826 GL 2008 8 26 CX2A08ON153 1 20080707 A 3350 82321 SIGN AMTR 1100 1100RMINIMAX 1181008 GL CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12220 6186 2267 FLT 7751 -LAX - FLIGHT CREW REPORTED EXIT LIGHT CEILING SIGN AT ROW 12 INOPERATIVE. MX PERSONNEL REMOVED AND REPLACED E XIT LIGHT CEILING SIGN AT ROW 12. OPERATIONALLY CHECKED SATISFACTORY AND RELEASED TO RETURN TO SERVICE. (A) 1 M 7 1 3I NC EXPA1M71 20080826 SO 2008 8 26 C2XA08TY070 1 20080704 A 3350 GE1317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13995 145295 LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP. OPS CK GOOD, AIRCRAFT RELEASED AND RETURNED TO S ERVICE. FLT HRS-19303. CYC-14520. (A) 2 L 7 2 4T RT T00011AT 20080826 SO 2008 8 26 C2XA08SH093 1 20080711 A 5751 BUSHING EMB 145 EMB145LR 3260212 SO BRACKET MIGRATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16919 145393 SHV - DURING C-CHECK RT AILERON OUTBOARD CONTROL ROD ATTACHING BRACKET ON AILERON, HAS MIGRATED HAT BUSHING. MX REMOVED AND REPLACED RT AILERON OUTBOARD CONTROL ROD ATTACHING BRACKET IAW EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080826 GL 2008 8 26 C2XA08CL080 2 20080706 A 7321 367934005 FUEL CONTROL EMB 145 EMB145XR 3260214 SO ALLSN AE3007 AE3007A 03030 GL FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 11113 3806 145662 IAH - FLIGHT 2187 - THE CREW REPORTED A "FUEL XFER INOP" MESSAGE ON THE EICAS IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RELEASED THE AIRCRAFT IAW MEL 28-21-12. MAINTENANCE REPLACED T HE VENTRAL FUEL CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD. (A) 2 L 7 2 4F 4 F RT TE6CH 20080826 SO 2008 8 26 C2XA08CL081 1 20080704 A 2897 M83726302002P RELAY EMB 145 EMB145XR 3260214 SO FUEL SYSTEM FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 12157 145787 IAH - FLIGHT 2738 - THE CREW REPORTED A "VENTRAL XFER INOP" MESSAGE ON THE ECIAS IN FLIGHT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RELEASED THE AIRCRAFT IAW MEL 28-21-12. ON 7/9/08 MAINTENAN CE REPLACED THE LOW LEVEL TIME DELAY RELAY K7208. OPERATIONAL CHECKS WERE GOOD. MEL WAS CLEARED AND THE AIRCRAFT WAS R ELEASED FOR SERVICE. (A) 2 L 7 2 4F RT 20080826 SO 2008 8 26 C2XA08SH094 1 20080711 A 5751 BUSHING EMB 145 EMB145LR 3260212 SO ATTACH FITTING MIGRATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16919 145393 SHV - DURING C-CHECK BOTH HAT BUSHING ON RT AILERON DAMPER ATTACHMENT FITTING ON AILERON ARE MIGRATED. MX REMOVED AND R EPLACED RT AILERON DAMPER ATTACHING FITTING IAW EMB 145-SRM-51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080826 SO 2008 8 26 C2XA08IA161 1 20080711 A 3350 78211 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 19966 145131 IAH - FLIGHT 2510 - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE SECOND AND THIRD AISLE PATH LIGHTING STRIPS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER THREE EMERGENCY LIGHT INVERTER, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080826 SO 2008 8 26 C2XA08IA157 1 20080707 A 3297 D3899926KA98SN CONNECTOR EMB 135 EMB135LR 3260305 SO NLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16520 145372 IAH - FLIGHT 2497, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON ROTATION. THE AIRCRAFT RETURNED TO IAH W HERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEELS PROXIMITY SENS OR CONNECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080826 SO 2008 8 26 C2XA08IA164 1 20080714 A 2810 2770138101 CHECK VALVE EMB 145 EMB145LR 3260212 SO FUEL SYSTEM LEAKING A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 13978 145180 IAH-FLIGHT 2350, THE CREW REPORTED A FUEL LEAK FROM THE RT HAND WING. THE AIRCRAFT LANDED AT ORD WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE RT WING NACA INLET FLAPPER CHECK VALVE. LEAK CHECKED WITH NOT DEFECTS AND THE AIRC RAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080826 SO 2008 8 26 C2XA08TY071 1 20080708 A 3350 5113WW LAMP EMB 145 EMB145 3260210 SO EMERGENCY LIGHT BLOWN A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 18987 20000 145261 THE LT EMERGENCY ROW EXIT SIDEWALL LIGHT WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE LT SIDEWALL LIGHT IAW EMB 145AMM 33-21-06. OPS CHECK GOOD. (A) 2 L 7 2 4F RT T00011AT 20080826 EA 2008 8 26 COMA086353 1 20080809 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 965CA 7131 RT UPPER WEB-ENG SUPPORT BEAM ASSEMBLY CRACKED. COMPLIED WITH REPAIR TO UPPER WEB-ENG SUPPORT. BEAM ASSEMBLY BETWEEN B L 27.5 AND 36.2 PER REO601R-53-61-569. (S) 2 L 7 2 4F RT A21EA 20080826 NM 2008 8 26 USAA920081538 1 20080817 A 5330 6545774 SKIN BOEING 737 7373S3 1384711 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 PHX- DAILY -MAJOR REPAIR- FUSELAGE SKIN CRACKED AT BS 747, S23L. REPAIRED FUSELAGE SKIN AT BS747 S23L IAW B737 SRM TEMP ORARY REVISION 53-33 REPAIR 31. (S) 2 L 7 2 4F RT A16WE 20080826 NM 2008 8 26 USAA920081528 1 20080805 A 5320 146N530094 SUPPORT BOEING 757 7572G7 1384963 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 909AW 24522 MCN-C3 -MAJOR REPAIR- INTERGRANULAR CORROSION ON SUPPORT AT BS 1681.8, WL 208.1, BL 0. REPLACED SUPPORT AT BS 1681.8, W L 208.1, BL 0 IAW B757 SRM 51-40-02-0G. (S) 2 L 7 2 4F RT A2NM 20080826 WP 2008 8 26 IXX2008F00073 1 20080609 A 5753 SKIN DOUG DC8 DC872F 302199E WP LT WING TE FLAP MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND LT WING INBOARD FLAP UPPER SKIN HAS IMPROPER REPAIR AT STATION XW 104.000. REM OVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AR EA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 1 ITEM "D", DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-3-0, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080826 NM 2008 8 26 2008UALA03585 1 20080624 A 2150 1942704 HEAT EXCHANGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ENVIRON CONTROLS FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 655UA 25393 CREW COMMENTS: GOT HOT IN CABIN 74-79-81, HAVE TO OPERATE RT PACK IN STBY C TO HAVE A COMFORTABLE TEMP. *S/D* SUSPECT FAULTY HEAT EXCHANGER. REPLACED LEFT HEAT EXCHANGER IAW MM 21-51-02, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080826 EA 2008 8 26 TRAX200800790 1 20080615 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 FWD ENTRY DOOR EMERGENCY LIGHT BROKEN. FLT 4839 DEL 22 MINS. REPLACED LIGHT ASSY OPS OK PER 33-50-01. 2 L 7 2 4F RT A21EA 20080826 EA 2008 8 26 TRAX200800775 1 20080605 A 5330 DOUBLER CNDAIR CL600 CL6002C10 1390015 EA BS 295-310 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 ANTENNA DOUBLER BETWEEN FS 295.00 AND 310 AT STR 27 IS CORRODED. JOB COMPLETE. BLENDED CORROSION OUT OF ANTENNA DOUBLE R BETWEEN FS 295.00 AND 310 AT STRINGER 27 THICKNESS CHECK PERFORMED .007" MATERIAL WAS REMOVED PART IS OUT OF LIMITS AL L WORK DONE IAW CRJ 700 SRM 51-21-06 KJ 7025361 6/11/2008. REMOVED ANTENNA DOUBLER FR AND CLEANED AREA UNDER DOUBLER, N O CORROSION FOUND. 2 L 7 2 4F RT A21EA 20080826 SO 2008 8 26 C2XA08IA174 1 20080724 A 3350 20131A BATTERY PACK EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 17196 17597 14500945 SAT - DURING MAINTENANCE INSPECTION THE FORWARD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. (A) 2 L 7 2 4F RT 20080826 NM 2008 8 26 KCSA081389 1 20080811 A 5340 STRINGER CLIP BOEING 747 747249F 1384849 NM BS 440 S10R CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 BS 440 S10R LT SIDE FRAME AFT SIDE, STRINGER ATTACH ANGLE CRACKED IN RADIUS .250 INCH CRACK MARKED. UPPER DECK. (S) 2 L 7 4 4F RT A20WE 20080826 NM 2008 8 26 KCSA081390 1 20080811 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 440 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 BS 440 S10R FRAME OUTBOARD FLANGE CRACKED IN RADIUS .375 INCH. CRACK MARKED. UPPER DECK. (S) 2 L 7 4 4F RT A20WE 20080826 SO 2008 8 26 RAIA00808006 1 20080806 A 2120 UNKNOWN EMB 145 EMB145EP 3260221 SO CABIN SMOKE A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 03 826HK 145016 FLT 6545-STL - DURING DESCENT, LOUD POPPING SOUND STARTED COMING FROM THE MID CABIN AREA, FOLLOWED BY LIGHT SMOKE IN CAB IN AND THE COCKPIT. MAINTENANCE PERFORMED AN INSPECTION AND FUNCTIONAL CHECK OF THE NR 1 PACK SYSTEM WITH NO DEFECTS NO TED. (S) 2 L 7 2 4F RT T00011AT 20080826 CE 2008 8 26 DXTA200803232 1 20080815 A 2150 A/C PACK CESSNA 500 560CESSNA 2076750 CE ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 394QS 5600394 AIR CONDITIONER WAS ON FOR TWO MINUTES, THEN STARTED BLOWING HOT AIR. AIR CONDITIONER LIGHT WAS NOT ON, THEN A BURNING ELECTRICAL ODOR CAME THROUGH THE CABIN. KATL-KSGJ. (S) 2 L 7 2 4F RT A22CE 20080826 WP 2008 8 26 IXX2008F00088 1 20080818 A 2700 30042502 ACTUATOR DOUG DC8 DC872F 302199E WP TRIM SYS DEFECTIVE A IXXA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SW 11 721CX 46013 FLIGHT ATN103/KWRI TO PANC - DURING CRUISE FROM KWRI BOTH PILOT`S AND COPILOT`S YOKE TRIM SWITCHES INOPERATIVE. THE CRE W DIVERTED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RT LONG TRIM ACTUATOR, OPERATIONAL CHECK GOOD IAW 27-41-10. ACFT WAS RETURNED TO SERVICE. (S) 2 L 7 4 4F RT 4A25 20080826 NM 2008 8 26 UIEA200800286 1 20080815 A 5310 DOOR FRAME BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 524MC 21784 LEFT NR 1 MAIN ENTRY DOOR FORWARD FRAME UPPER HINGE CUTOUT AREA CRACKED. REPAIRED IAW BOEING SERVICE REQUEST 1912258448 APPROVED BY FAA FORM 8100-9 DATED 6 AUG 2008, DETAILS OF WORK KEPT AT ATLAS ENGINEERING ORDER EO 4752A146. (S) 2 L 7 4 4F RT A20WE 20080826 WP 2008 8 26 IXX2008F00083 1 20080612 A 5312 BULKHEAD DOUG DC8 DC872F 302199E WP BS 680 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND MIDDLE ACCESSORY COMPARTMENT BULKHEAD CRACKED AT STATION 680.000 LT BOTTOM LINE 20-30. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING DOUBLER AND SPLICE. REMOVED DAMAGED AREA. FA BRICATED DOUBLER, DOME SEGMENT, SPLICE, DOUBLER, FINGER DOUBLER, FILLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED AN D PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 53-2-5 FIGURE 13 SHEET 1 T/R 53-17 7 SHEETS 1-2 DATED 9/20/03, DC8 SRM 51-1-1 PAGES 1, 13 AND 17, DC8 SRM 51-1-8B, 51-1-11, 51-1-21, 51-1-20D, AND 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080827 EA 2008 8 27 REX2008F00017 1 20080721 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8775A 12968 7775 GEAR DISAGREE WHEN GEAR SELECTED DOWN ON APPROACH INTO DTW, QRH FOLLOWED DECLARED EMERGENCY, UNEVENTFUL LANDING. REMOVE D AND REPLACED NOSE LANDING GEAR SELECTOR VALVE IAW AMM OPERATIONAL AND LEAK CHECK PERFORMED WITH NO DEFECTS. (A) 2 L 7 2 4F RT A21EA 20080827 EA 2008 8 27 CHQA200800138 1 20080711 A 5753 601R1014063 BRACKET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT WING TE FLAPS UNSECURE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 701BR 7448 GEE872845 FLIGHT 5586, RDU TO CLE. UPON FLAP RETRACTION FROM FLAPS 20 TO FLAPS 8 THE CREW RECEIVED A FLAP FAIL MESSAGE. THE MESS AGE WAS CONFIRMED AND THE LT FLAP WAS AT 11 DEGREES WHILE THE RT FLAP WAS AT 10 DEGREES. THE QRH CHECKLIST WAS FOLLOWED AND THE AIRCRAFT LANDED BACK AT RDU WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FLAP SYSTEM AND FOUND THE RT OUTBOAR D FLAP FAIRING SPACER BRACKET UNSECURED AND BINDING AGAINST THE ACTUATOR ARM. THE BRACKET WAS RE-SECURED, FLAPS RESET A ND THE SYSTEM OPS CHECKED GOOD. THERE WAS NO DAMAGE TO EITHER PART AND THE AIRCRAFT WAS RELEASED. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080827 EA 2008 8 27 CHQA200800130 1 20080702 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE EMERGENCY LIGHT BURNED OUT A CHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 701BR 7448 GEE983845 MAINTENANCE FOUND THE EXTERNAL EMERGENCY LIGHT AFT OF THE SERVICE DOOR TO BE INOPERATIVE DURING TESTING. THE LIGHT WAS REPLACED AND THE EMERGENCY LIGHT SYSTEM OPERATED NORMALLY. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080825 CE 2008 8 25 DGC2008F00000 1 20080816 A 2913 PF24390515BCE562 PUMP RKWELL NA265 NA26565 7630107 CE HYDRAULIC SYS INOPERATIVE E DGCA O OTHER O OTHER NR NOT REPORTED 1 CE 03 570R 46575 HYDRAULIC PRESSURE SYSTEM FAILURE, DISCOVERED PUMP INOPERATIVE. (S) 2 L 7 2 4J A2WE 20080825 NM 2008 8 25 USAA920081535 1 20080814 A 5347 6546B13 SEAT TRACK BOEING 737 7373B7 1384580 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT -Q6- MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT BS 328 TO BS 344, RBL 24. REPAIRED SEAT TRACK AT BS 328 TO BS 344, RBL 24 IAW B737 SRM 53-00-52. (S) 2 L 7 2 4F RT A16WE 20080825 SW 2008 8 25 EHS2008F00001 1 20080811 A 3213 MS28775111 O-RING GULSTM 500 500S 0141107 SW STRUT LEAKING A EHSA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 07 519WA 3081 WHILE FLYING A FIRE MISSION IN SUPPORT OF USFS, THE PILOT NOTICED THE RT GEAR START TO EXTEND FOLLOWED BY A LOSS OF HYDR AULIC PRESSURE. PILOT RETURNED TO THE AIRPORT AND LANDED. THE PROBLEM WAS TRACED TO THE RT MAIN GEAR RETRACT CYLINDER. UPON DISASSEMBLY OF THE RETRACT CYLINDER, THE O-RING AROUND THE SHAFT WAS FOUND TO BE SPLIT. THE SPLIT O-RING ALLOWED THE HYDRAULIC FLUID TO BE PUMPED OUT. THE SEALS AND O-RINGS WERE REPLACED. PROBABLE CAUSE: POSSIBLE DIRTY SHAFT ALLO WING FOREIGN MATERIAL TO SPLIT THE O-RING. PILOT WAS ADVISED TO MAKE SURE SHAFTS ARE KEPT CLEAN. (S) 1 H 7 2 3O 6A1 20080825 NM 2008 8 25 UIEA200800285 1 20080815 A 5310 DOOR FRAME BOEING 747 7472D7B 1384803 NM R4 DOOR CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 524MC 21784 RT NR 4 MAIN ENTRY DOOR FWD FRAME LOWER HINGE CUTOUT AREA CRACKED. REPAIRED IAW BOEING SERVICE REQUEST 1912258253 APPRO VED BY FAA FORM 8100-9 DATED 07 AUGUST 2008, DETAILS OF WORK KEPT AT ATLAS ENGINEERING ORDER EO-4752A148. (S) 2 L 7 4 4F RT A20WE 20080825 SO 2008 8 25 C2XA08TY083 1 20080809 A 3350 1317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16918 4745 4745 145397 EMERGENCY CEILING LIGHT AT ROW 14 INOPERATIVE. REMOVED AND REPLACED LAMP IAW EMB 145MM 33-50-08. OPS CHECK GOOD. ACFT RELEASED AND RETURNED TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080825 NM 2008 8 25 2008UALA03806 1 20080709 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1500 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 AFT PIT LT SIDE SLANT AREA HAS DENTED FRAME STA 1500 AT STR 26L. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. CUT OUT DAMA GE AND INSTALLED NEW STR SECTION PER SRM 53-00-07, RPR 5. 2 L 7 2 4F 4 F RT A2NM E17NE 20080825 NM 2008 8 25 KCSA081388 1 20080811 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 460 S12L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 BS 460 3.00 INCH ABOVE S12L FRAME OUTBOARD FLANGE CRACKED IN RADIUS OF DOUBLER .375 INCH LONG AFT SIDE. CRACK MARKED. UPPER DECK. (S) 2 L 7 4 4F RT A20WE 20080825 NE 2008 8 25 NWAA083775640 2 20080811 A 7300 PROBE BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 1 ENGINE UNKNOWN A NWAA E ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 01 540US 4168 4168 26487 DURING CRUISE FLIGHT AT 37,000FT ENG NR 1 FLAMEOUT. FLIGHT CREW WAS SUCCESSFUL IN RESTARTING ENG NR 1 AND CONTINUED TO DESTINATION. MAINTENANCE REPLACED ENG NR 1 PT2/TT2 PROBE, EEC AND PERFORMED BOROSCOPE INSPECTION. (S) 2 L 7 2 4F 4 F RT A2NM E17NE 20080825 SO 2008 8 25 C2XA08ON164 1 20080808 A 5610 12042177503 WINDOW EMB 145 EMB145LR 3260212 SO COCKPIT OUT OF ADJUST A C2XA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 27 11551 14818 11370 145411 FLT 0312-IAH, FLIGHT CREW REPORTED LOUD PIERCING SQUEAL FROM CAPT DV WINDOW ON FLIGHT FROM AUS TO JAX DIVERTED TO IAH. MAINTENANCE PERSONNEL RE-ADJUSTED DV WINDOW. OPERATIONALLY AND LEAK CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETUR N FOR SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080825 CE 2008 8 25 GUU2008F00035 1 20080804 A 3240 BRAKE BEECH 1900 1900D 1154162 CE MLG WEAK A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 178YV UE178 FLIGHT 9148 MHH/FLL. PILOT REPORTED FIRST OFFICER LT RUDDER PEDAL GOES TO THE FLOOR WHEN DEPRESSED AND NO BRAKES. BACK BLED BRAKE SYSTEM. OPERATIONAL CHECK NORMAL. (S) 2 L 7 2 4T RT A24CE 20080825 EU 2008 8 25 2008UALA03719 1 20080706 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 456UA 1128 EMERGENCY PATH LIGHTS AT ROWS 18, 14 & 17 INOP. *S/D* REPLACED EMERGENCY PATH LIGHTS, OK FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080825 EA 2008 8 25 TRAX20080994 1 20080810 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR OUT OF ADJUST A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 978EV 7723 SVC - DOOR OUTER HANDLE WILL NOT STOW. REMOVED, CLEANED AND REINSTALLED SERVICE DOOR INNER HANDLE & ACTUATOR IAW CRJ 20 0 MM 52-41-03. OPS CHECK GOOD, OUTER HANDLE STOWS PROPERLY. (S) 2 L 7 2 4F RT A21EA 20080825 EU 2008 8 25 USAA920081529 1 20080815 A 2120 VD390100 FAN AIRBUS A321 A321211 3930370 EU CABIN FAILED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 180US 26567 3163 1525 FLT 1511 CLT-PHX- BURNING ODOR - FLIGHT ATTENDANT REPORTED FUMES IN FIRST CLASS AND AROUND ROW 20. R&R THE CABIN RECIRC ULATION FAN 14HG. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20080825 NM 2008 8 25 QXEA200800358 1 20080330 A 5522 SKIN DHAV DHC8 DHC8202 2809007 NM RT ELEVATOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 356PH 502 PDX -C4 CHECK- FOUND A CREASE ON THE BOTTOM OF THE RT ELEVATOR AT STN YH94.20, APPROX 6 INCHES FWD OF THE AFT SPAR. CRE ASE IS APPROX 5.5 INCHES LONG. FOUND OUT OF LIMITS IAW RD8-55-1448. HFEC INSP FOR CRACKS, NO CRACKS NOTED. REMOVED RI VETS, FABRICATED REPAIR DOUBLER IAW RD8-55-1930. INSTALLED DOUBLER IAW RD8-55-1930 STEPS 9-13. (S) 2 H 7 2 4T RT A13NM 20080825 NM 2008 8 25 AALA200801859 1 20080713 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 626AA 24584 LGA - EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUN D CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A2NM 20080825 WP 2008 8 25 AALA200801851 1 20080711 A 2120 DUCT DOUG DC9 DC982 3022082 WP RT A/C PACK LEAKING A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 208AA 49159 DFW - INFLIGHT T493/11JUL - CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED DURING CLIMB THROUGH FLIGH T LEVEL 180. LIGHT EXTINGUISHED AFTER SHUTTING OFF RT A/C PACK. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND RU PTURED DUCT IN AFT COMPARTMENT ON RT SIDE. REPLACED DUCT IN AFT COMPARTMENT ON RT SIDE. SYSTEM GROUND CHECKED NORMAL O PERATION. (S) 2 L 7 2 4F A6WE 20080825 NM 2008 8 25 2008UALA03812 1 20080709 A 4930 38760263 CONTROL UNIT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU ECU FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 597UA 28750 APU AUTO SHUTDOWN TWO STARTS. *S/D* APU ECU FAILED. REPLACED ECU, STARTS SUCCESSFULLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080826 2008 8 26 UIEA200800295 4 20080818 A 3441 46300161300413 INU BOEING 747 747228F 1384895 NM NR 1 FAILED A UIEA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 15 809MC 20887 NR 1 INS DIFFERS FROM NR 2 INS BY 35 NM OR 50 KTS. FAILED ACCURACY TEST. DUMPED FUEL AND DIVERTED TO JFK. REPLACED NR 1 INU AND ALIGNED OPS CHECKED OK PER 34-41-03. (S) 2 L 7 4 4F RT A20WE 20080826 EA 2008 8 26 MASA200800469 1 20080614 A 5270 601R852001 SENSOR CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR MALFUNCTIONED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 925FJ 15025 ASH FLT 2605 CLT-SRQ. PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE. REMOVED AND REPLACED SENSOR PX107. (B) 2 L 7 2 4F RT A21EA 20080826 EA 2008 8 26 COMA086354 1 20080809 A 5321 FLOOR SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 460 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 965CA 7131 PRESSURE FLOOR SKIN AT STA 460 BETWEEN LBL 9 AND RBL 9 IS CRACKED. REPAIRED PRESSURE FLOOR SKIN WEB AT FS 460.00 WITH T EMPORARY REPAIR PER REO 601R-53-41-103 REV D. (S) 2 L 7 2 4F RT A21EA 20080826 EA 2008 8 26 COMA086357 1 20080817 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 640 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 916CA 7014 DURING FS 640 FRAME INSPECTION FOUND 640 FRAME CRACKED ON LT SIDE AT REINFORCEMENT ANGLE. REMOVED DAMAGED SECTION OF FR AME FROM STRINGER 6-20 AND REPLACED WITH SPLICED IN REPAIR FRAME, SKIN DOUBLER AND REINFORCEMENT ANGLE IAW WITH CRJ SB 6 01R-53-061, REO 601R-53-61-506, 601R-53-61-366 AND 601R-53-61-569. (S) 2 L 7 2 4F RT A21EA 20080826 NE 2008 8 26 YENA2008078 2 20080812 A 7200 4W5198 POWERPLANT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 STALLED A YENA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 15 510JB 21020 16093 1280 V10934 FLT 489, BOS-LGB, AIR RETURN TO BOS, ENG NR1 STALL ON DEPARTURE AT APPROX 100FT ALT. WITH THRUST REDUCTION ECAM INDICAT ION WENT AWAY AND CONTINUED TO CLIMB TO FL230. PERFORMED QRH 6-26 ITEMS AND STALL OCCURRED AGAIN. WITH NUMBER 1 THRUST LEVER TO IDLE WENT AWAY. ON RETURN TO BOS INDICATIONS NORMAL UNTIL 10 MILES OUT. ECAM INDICATED 1 STALL AND REMAINED. COMPLETED ECAM ACTIONS AND SHUT DOWN NR1 ENG. LANDED SAFELY AND RETURNED TO GATE. ACCOMPLISHED LPC/HPC BOROSCOPE. DA MAGE TO STG 3 HPC, BEYOND LIMITS. REMOVED AND INSTALLED NR1 ENG PER WORK ORDER 24077. (S) 2 L 7 2 4F 4 F RT A28NM E40NE 20080826 EA 2008 8 26 COMA086352 1 20080809 A 7120 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 965CA 7131 LT UPPER WEB-ENG SUPPORT BEAM ASSEMBLY CRACKED. COMPLIED WITH REPAIR TO UPPER WEB-ENG SUPPORT. BEAM ASSEMBLY BETWEEN B L27.5 AND 36.2 PER REO601R-53-51-569. (S) 2 L 7 2 4F RT A21EA 20080826 EA 2008 8 26 A6WA200840553 1 20080729 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A A6WA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 GL 31 454AW 7842 AFTER TAKEOFF "FLAPS FAIL" MESSAGE. FLAPS FAILED AT 20 DEGREES. COMPLIED WITH QRH. LANDING WEIGHT WITHIN LIMITS (46,4 00 LBS), BRAKE TEMPERATURES NORMAL. COMPLIED WITH RESET PROCEDURE IAW AWAC SUPP 98-018B STEPS 1.3 AND 1.4. FLAP SYSTEM RESET OK. (S) 2 L 7 2 4F RT A21EA 20080826 NM 2008 8 26 2008UALA03366 1 20080612 A 2160 32907706 ISOLATION VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE ENVIRON CONTROLS FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 788UA 26942 L BLEED ISOLATION VALVE FAULT. SUSPECT FAULTY ISOLATION VALVE. REPLACED LT ISOLATION VALVE PER MM 36-12-01. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080821 2008 8 21 2008UALA03734 4 20080706 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR SLIDE UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 DOORS 2L AND 2R WON'T ARM. *S/D* LANYARD LOOSE, CAUSING INTERFERENCE. SECURED LANYARD, DOOR ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 2008 8 21 2008UALA03736 4 20080703 A 2565 D31354437 SLIDE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 938UA 26671 AT DOOR 2R ON THE BOTTOM OF THE SLIDE PACK, THERE IS SOME TRIM STICKING OUT. SUSPECT IMPROPERLY INSTALLED. REPLACED SL IDE PER MM 25-61-35. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20080821 NM 2008 8 21 2008UALA03741 1 20080703 A 2560 65B549299 GIRT BAR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L5 DOOR SLIDE INADEQUATE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 122UA 29168 DOOR 5L FWD GIRT BAR SLIDER MISSING. REPLACED DOOR 5L GIRT BAR SLIDER. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080821 NM 2008 8 21 2008UALA03768 1 20080707 A 3600 PNEUMATIC SYSTEM BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE FLUCTUATES A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 673UA 29241 RT DUCT PRESSURE FLUCTUATES DURING DESCENT, WITH ENG RUNNING, LT & RT ISOL VLVS CLSD, & BLD SW ON. DUCT PSI FLUCTUATES BETWEEN 998. CREW COMMENTS: 18 PSI TO 32 PSI. FLUX ALSO SEEN IN EPR +-- .03 AND N1+-- .3. 2 L 7 2 4F 4 F RT A1NM E24NE 20080821 NM 2008 8 21 2008UALA03770 1 20080707 A 3510 OXYGEN SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 562UA 26664 CAPTAIN'S OXYGEN MASK YELLOW FLOWBAR INOP BUT O2 FLOWING TO MASK & HARNESS. CAPTAIN`S O2 MASK BOX (UNKNOWN ISSUE). REP LACED CAPTAIN`S O2 MASK BOX, ALL OPS TESTS ARE GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NM 2008 8 21 SWAA084382 1 20080806 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 288 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 288 STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084358 1 20080801 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 200WN 32482 EEPLS LENS BROKEN AT ROW 2 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084387 1 20080806 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 2130 27710 DURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP OUTBOARD LOWER SURFACE DELAMINATED. REMOVED AND REPLACE D FLAP PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03320 1 20080610 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 1 FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 206UA 30212 L ENG IDG DRIVE LIGHT NOT ILLUMINATED. LT BULB PRESS TO TEST OK. MAINT MSG 24-31801. *S/D* SUSPECT FAULTY IDG AND BU G. REPLACED IDG PER MM 24-11-01 AND BUG IAW MM 24-25-01. ACCOMPLISHED ENGINE RUNS, NO LEAKS OIL SERVICED AS REQUIRED. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080821 NM 2008 8 21 2008UALA03363 1 20080611 A 3610 339910230 CONTROLLER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 ENGINE FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 227UA 30555 NR 2 ENGINE PRSOV CONTROLLER FAILED HEALTH CHECK. *S/D* SUSPECT FAULTY CONTROLLER. REPLACED CONTROLLER PER MM 36-11-1 8-401. OPS CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080821 NM 2008 8 21 2008UALA03178 1 20080604 A 2435 873602 POWER SUPPLY BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE STARTER GEN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 226UA 30226 STATUS MSG01- ACTIVE CRUISE HARD; POWER SUPPLY ASSEMBLY (LEFT) HAS NO OUTPUT ON FLIGHT CONTROLS ARINC 629 BUSS (LEFT). D B- LEFT AIMS MSG-2458811 ACTIVE ER HARD. SUSPECT FAULTY POWER SUPPLY ASSEMBLY. REPLACED L-PSA PER MM 24-35-01, OP CHEC KED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080821 NM 2008 8 21 2008UALA03210 1 20080601 A 2425 1701766 GENERATOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE AUX FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 799UA 26926 NR 2 BUG SHOWED SERVICE ON MFD. *S/D* SUSPECT FAULTY BEARING. REPLACED BACKUP GENERATOR PER MM 24-25-01, OPS CHECK GO OD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080822 NM 2008 8 22 F3LA200800402 1 20080624 A 5320 D5367313900000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSP, NOTED AFT CARGO PIT AFT RT UPPER TRANSITION PANEL 162CF HAS SEVERAL HOLES AT AFT END. MAINT REPAIR ED TRANSITION PANEL 162CF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTA BLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800527 1 20080728 A 5321 D5367160100000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2 2209 DURING C-CHECK, INSP, NOTED THE FLOOR PANEL 251LF NEEDED TOP LAYER OF COMPOSITE REPAIRED IN SEVERAL PLACES. MAINT REPAI RED FLOOR PANEL 251LF IAW SRM 53-02-00 PARAGRAPH 8.A FIGURE 201. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FO UND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM 20080822 EU 2008 8 22 F3LA200800386 1 20080624 A 5330 D534764082 SKIN AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 919FR 1980 DURING WALK AROUND MAINT, NOTED LT FUSELAGE GOUGED AND DAMAGED FRAME 57 TO FRAME 58 AND STRINGER 30 LT TO STRINGER 31 LT . MAINT PERFORMED A PERMANENT REPAIR IAW SRM 53-00-11 FIGURE 203 AND E.A. A9-53R-30409. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT E37NE 20080822 EU 2008 8 22 F3LA200800420 1 20080703 A 5320 D5348015800500 BLANKING PLATE AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 805FR 1660 DURING C-CHECK INSP, NOTED GIRT BAR BLANKING PLATE ON R2 DOOR AFT HAS CORROSION. MAINT REMOVED AND REPLACED R2 DOOR GIRT BAR BLANKING PLATES IAW WORK CARD C250001-03. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT 20080822 NM 2008 8 22 F3LA200800401 1 20080624 A 5320 D5367303600000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSP NOTED AFT CARGO PIT AFT LT UPPER TRANSITION PANEL 161CF HAS HOLES IN SEVERAL PLACED. MAINT REPAIRED TRANSITION PANEL 161CF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABL E. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800334 1 20080611 A 5311 D5347715400400 FRAME AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 DURING C-CHECK INSP NOTED AFT CARGO FLOOR FRAME 59 HAS CORROSION AT NUTPLATE HOLES. MAINT REPAIRED HOLES WITH REPAIR DO UBLERS IAW EA A9-53R-30346. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) THE PERMANENT REPA IR FOR CORROSION DAMAGE WAS DEFERRED FOR 500 FLIGHT CYCLES. CUT AND REMOVED DAMAGED FRAME SECTION AND SLICED IN NEW SEC TION, PN D53477711000000. MX WAS COMPILED WITH IAW EO A9-53R-30346. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AN D FOUND ACCEPTABLE. PERMANENT REPAIR ACCOMPLISHED AT AIRCRAFT TT: 21534 AND TOTAL CYCLES: 9251 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800447 1 20080710 A 5347 D5323099920000 CARGO TRACK AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY WORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP, NOTED BEAM NR 11 HAS EXCESSIVE PLAY AFT WALL OF FWD CARGO PIT AT FLOOR TRACK. MAINT REMOVED AND REP LACED BEAM NR 11 AFT WALL MOUNT FITTING IN FWD CARGO BAY IAW SRM 51-72-11 PAGE 1 AND 2. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 EU 2008 8 22 F3LA200800556 1 20080816 A 5320 D5348015900700 BLANKING PLATE AIRBUS A318 A318111 3940019 EU GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 806FR 30 2218 DURING C-CHECK, INSP NOTED R2 AFT GIRT BAR BLANKING PLATE HAS CORROSION. MAINT REMOVED AND REPLACED BLANKING PLATE WITH NEW ONE FROM STOCK AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCE PTABLE. (S) 2 L 7 2 4F RT 20080822 EU 2008 8 22 F3LA200800557 1 20080816 A 5320 D5348015800600 BLANKING PLATE AIRBUS A318 A318111 3940019 EU GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 806FR 30 2218 DURING C-CHECK, INSP NOTED L2 FWD GIRT BAR BLANKING PLATE HAS CORROSION. MAINT REMOVED AND REPLACED BLANKING PLATE WITH NEW ONE FROM STOCK AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCE PTABLE. (S) 2 L 7 2 4F RT 20080822 NM 2008 8 22 F3LA200800537 1 20080731 A 5321 D5367204500000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2 2209 DURING C-CHECK, INSP NOTED THE AFT CARGO PIT FLOOR PANEL, 161CF WAS PUNCTURED. MAINT REPAIRED THE PUNCTURE DAMAGE IN FL OOR PANEL 161CF IAW SRM 53-02-00 FIGURE 204. MAINT PREPARED AND PAINTED THE FLOOR PANEL 161CF IAW THE REQUIREMENTS OF A MM 25-00-00-370-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F 4 F RT A28NM 20080822 NM 2008 8 22 F3LA200800513 1 20080722 A 5321 D5367414400000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 942FR 50 2497 DURING C-CHECK, INSP NOTED THE AFT CARGO PIT CENTER LT UPPER TRANSITION PANEL 151FE WAS PUNCTURED. MAINT REPAIRED TRANS ITION PANEL 151FE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM 20080822 NM 2008 8 22 F3LA200800512 1 20080722 A 5321 D5367302100000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 942FR 50 2497 DURING C-CHECK, INSP NOTED THE AFT CARGO PIT FORWARD LT LOWER TRANSITION PANEL 151AE WAS GOUGED IN THE CENTER OF THE PAN EL. MAINT REPAIRED TRANSITION PANEL 151AE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM 20080822 NM 2008 8 22 F3LA200800453 1 20080711 A 5321 D5367303801000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 940FR 2465 DURING C-CHECK INSP AFT PIT PANEL 161BF DAMAGED. MIANT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800455 1 20080711 A 5321 D5367424100000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 940FR 2465 DURING C-CHECK INSP NOTED AFT PIT PANEL 151PE DAMAGED. MAINT REMOVED DAMAGED AREA, FILLED DAMAGED AREA IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800486 1 20080716 A 5320 D5347646100000 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT RT SIDE PROFILE HAD CORROSION AT FRAME 59 ON RT SIDE IAW A319 SRM 51 -72-11 AND 51-44-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 EU 2008 8 22 F3LA200800554 1 20080816 A 5321 D5367180500400 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 806FR 30 2218 DURING C3 C-CHECK, INSP NOTED FLOOR PANEL 261FF HAS CORROSION ON LOWER SURFACE. MAINT REMOVED AND REPLACED FLOOR PANEL 261FF WITH A NEW PANEL AND INSTALLED ON TASK CARD C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND A CCEPTABLE. (S) 2 L 7 2 4F 4 F RT 20080822 NM 2008 8 22 F3LA200800445 1 20080710 A 5340 D5323099920000 FITTING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE WORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED THE FWD CARGO COMPARTMENT AFT WALL BRACE MOUNT AT UPPER FLOOR TRACKS HAS EXCESSIVE PLAY ON BEA M NR 1. MAINT REMOVED AND REPLACED BEAM NR 1 AFT WALL MOUNT FITTING IN THE FWD CARGO BAY IAW SRM 51-72-11 PAGE 1 AND 2. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800433 1 20080707 A 5321 D5367202700000 FLOORBOARD AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT FLOORBOARD 151TG HAS A PUNCTURE IN IT. MAINT CLEANED, PREPPED AND REPAIR ED FLOORBOARD 151TG IAW SRM 53-02-00 PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND A CCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800431 1 20080707 A 5321 D5367227100000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT FLOORBOARD 152TG HAS A PUNCTURE IN PANEL. MAINT CLEANED, PREPPED AND REP AIRED FLOORBOARD 152TG IAW SRM 53-02-00 PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUN D ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800442 1 20080710 A 5313 D5347219220000 LONGERON AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED THE LT LONGERON BEAM AT Y765 AND FRAME 68 HAS AREAS OF CORROSION. MAINT REMOVED AND REPLACED T HE LT LONGERON BEAM AT Y765 AND FRAME 68 IAW SRM 51-42-11 PAGE 1 AND 2.UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AN D FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800438 1 20080707 A 5330 SKIN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 DURING C-CHECK INSP NOTED LIGHTNING STRIKE ON FASTNER AT FRAME 26 STATION 1057 STRINGER 40. MAINT REPAIRED BY MOVING BLI NG FASTNER AND COLD WORKING HOLE AND INSTALLING HI-LOCK IAW SRM 51-42-11, SRM 51-48-00 AND SRM 53-21-11 FIGURE 201. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 NM 2008 8 20 SWAA084559 1 20080817 A 5743 6567172 FITTING BOEING 737 7373H4 1384600 NM LT MLG CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED HC1 CHECK, FOUND LT MLG FWD WALKING BEAM FITTING CRACKED. R&R FITTING PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843185 1 20080629 A 5753 SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 RT WING IB FORE FLAP DENTED ON UPPER SURFACE 6 INCHES FROM OB EDGE. PREPARED DAMAGED AREA FABRICATED DOUBLER AND BONDED IAW SRM 51-70-10, REPAIR 2. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 SWAA084558 1 20080817 A 5752 6546455 TAB BOEING 737 7373H4 1384600 NM LT AILERON DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND LT WING AILERON TAB T/E DELAMINATED. R&R TAB PER MM. 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 USA2008F00021 1 20080726 A 3350 1012721 LIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 435US 24557 CLT - MAINTENANCE REPORTED THE EMERGENCY LIGHT ASSEMBLY AT SEAT 12C (AISLE) NEEDS REPLACED. MAINTENANCE REMOVED AND REP LACED THE EMERGENCY LIGHT ASSEMBLY AT SEAT 12C. OPERATIONAL CHECK GOOD. (A) 2 L 7 2 4F RT A16WE 20080820 NM 2008 8 20 ASAA0843183 1 20080629 A 5755 654645170A SKIN BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU NR 3 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 LT WING NR3 SPOILER LOWER SURFACE HAS ONE DENT 9 INCHES FROM OB END, PREPARED DAMAGED AREA, FABRICATED DOUBLER AND BONDE D IAW SRM 51-70-10, REPAIR 2. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0843248 1 20080626 A 5753 6546431285 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FOREFLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 LT OB FOREFLAP SURFACE IS DENTED. BOND REPAIRED WITH DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F 4 F RT A16WE E21EU 20080820 NM 2008 8 20 ASAA0853270 1 20080802 A 4920 38007021 APU BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE APU BAY MAKING METAL A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 579AS 7897 35187 DELTA P INDICATOR FOUND EXTENDED MAGNETIC CHIP DETECTOR REMOVED AND FOUND TO BE COVERED IN (SILVER COVERED) METAL PARTIC LES. APU UNSERVICEABLE IAW AMM 49-91-81-200-801. PARA H ITEM 1. APU REPLACED WITH SERVICEABLE UNIT IAW TC 78349010. 2 L 7 2 4F 4 F RT A16WE E00055EN 20080820 EU 2008 8 20 F3LA200800425 1 20080707 A 5321 D5367180500500 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 805FR 1660 DURING C-CHECK INSP, FLOOR PANEL 262FF HAS CORROSION ON SURFACE. MAINT REMOVED AND REPLACED FLOOR PANEL 262FF IAW AMM 53 -42-12-400-002. UPON COMPLETION OF THE REPAIR, INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT 20080820 NM 2008 8 20 F3LA200800332 1 20080611 A 5320 53112534 PLATE AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE L1 GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 DURING C-CHECK INSP, NOTED L1 DOOR GIRT BAR PLATE ON SILL IS CORRODED. MAINT REMOVED OLD GIRT BAR PLATE, FABRICATED NEW PLATE AND INSTALLED NEW GIRT BAR PLATE IAW DRAWING 351-1234 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INS PECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080820 NM 2008 8 20 F3LA200800413 1 20080702 A 5320 INTERCOSTAL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 DURING C-CHECK INSP NOTED RT INTERCOSTAL WEB UNDER LATERAL SHEAR PANEL AT STRINGER 23 RT FROM FRAME 69 TO FRAME 70 HAS C ORROSION ON BOTTOM SIDE. MAINT REMOVED CORRODED INTERCOSTAL, LOCATED AND DRILLED NEW INTERCOSTAL, TREATED AND PRIMED HOL ES AND INSTALLED NEW INTERCOSTAL WEB IAW SRM 51-72-11, SRM 51-42-11 AND SRM 51-21-11. UPON COMPLETION OF THE REPAIR IT W AS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800376 1 20080620 A 5321 D5367314500000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP NOTED AFT CARGO FLOOR PANEL 152XG HAS FOUR HOLES IN IT. MAINT REPAIRED FLOOR PANEL 152XG IAW SRM 53 -02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 EU 2008 8 21 F3LA200800504 1 20080720 A 5240 D5211009820000 HOOK AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE R2 DOOR OUT OF ADJUST A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 943FR 18 2518 DURING C-CHECK INSP, NOTED THE R2 DOOR INSIDE HANDLE CAN BE OPERATED WHILE DOOR IS NOT CLOSED. MAINT ADJUSTED THE R2 DO OR HOOK IAW AMM 52-11-21-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800396 1 20080624 A 5320 D5367301900000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSP, NOTED AFT CARGO PIT FWD LT LOWER TRANSITION PANEL 151TG HAS A HOLE AT THE AFT CENTER SECTION. MAIN T REPAIRED TRANSITION PANEL IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEP TABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800285 1 20080603 A 5320 D5367204701000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE CARGO BAY DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 DURING C-CHECK INSP, NOTED AFT PIT TRANSITION PANEL 161BF HAS A DENTS. MAINT REMOVED DAMAGE AND CLEANED PANEL, FILLED D ENTS ON PANEL 161BF IAW SRM 51-73-00 STEP 3C. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800305 1 20080605 A 5320 D5391550320001 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED THE FWD CARGO COMPARTMENT AFT MOST PROFILE HAS CORROSION ON SEVERAL SPOTS BETWEEN FRAMES C30 AND FRAME C34. MAINT REMOVED AND REPLACED PROFILE IAW SRM 51-72-11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800312 1 20080608 A 5315 D5347217220400 FLOORBEAM AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED CABIN FLOORBEAM Y1292 AT FRAME 66 HAS CORROSION AROUND FASTENER. MAINT REMOVED CORROSION ON L ONGERON BEAM Y1291 AT FRAME 66 AND FOUND TO BE OUT OF LIMITS. MAINT REMOVED AND REPLACED FLOORBEAM Y1292 AT FRAME 66 IA W SRM 53-00-14. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800355 1 20080617 A 5321 D5367223700000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED DENT IN UPPER SURFACE OF BULK CARGO FLOOR PANEL 162BF. MAINT REPAIRED PANEL 162BF IAW SRM 53- 02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 EU 2008 8 21 F3LA200800361 1 20080616 A 5240 A52110526000000 LATCH AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE R1 DOOR NO TEST A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 941FR 2483 DURING C-CHECK INSP, NOTED R1 DOOR HOLD OPEN LATCH BUTTON FAILED PRESS TEST. MAINT ADJUSTED R1 DOOR BUFFER IAW AMM 52-1 1-00-820-001 STEP 4J. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 SWAA084393 1 20080806 A 5754 65C20662 SKIN BOEING 737 7373Q8 1384670 NM NR 4 SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 4 L/E SLAT CRACKED AT INBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084388 1 20080806 A 5311 6558280 FRAME BOEING 737 7373A4 1384585 NM BS 360 S25L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 360, STR 25L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084364 1 20080805 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM BS 922 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 922, STR 24L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084413 1 20080807 A 3350 311500 LENS BOEING 737 7373A4 1384585 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED BRDG CHECK, FOUND RT OVERWING EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084381 1 20080806 A 5315 6516300 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 178, LBL 27, WL 208. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084375 1 20080806 A 3350 767 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 282WN 32534 DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03362 1 20080613 A 3350 3071BPEGPL LAMP BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE EMERGENCY LIGHTS BURNED OUT A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 793UA 26946 EMERGENCY LIGHTS ON AFT END OF SEATS 2E & 3E ARE INOP. *S/D* SUSPECTED FAULTY LAMPS. REPLACED SEAT LIGHTS, OP CHECKED OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080822 NM 2008 8 22 F3LA200800371 1 20080619 A 5321 D536730180000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED AFT CARGO FLOOR PANEL 151UG HAS SEVERAL HOLES AND DENTS. MAINT REPAIRED FLOOR PANEL 151UG IA W EA A0-53F-12307. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800418 1 20080703 A 5210 FE240004 BOTTLE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE L2 DOOR ASSIST LOW A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 DURING C-CHECK INSP, NOTED L2 DOOR ASSIST BOTTLE PRESSURE IS LOW. MAINT SERVICED L2 DOOR ASSIST BOTTLE IAW AMM 52-10-00- 614-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800505 1 20080720 A 3350 BR9279468 SIGN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE EMERGENCY LIGHTS BROKEN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK, INSP NOTED R1 DOOR FWD LOWER EXIT LIGHT IS BROKEN. MAINT REMOVED AND REPLACED R1 DOOR FWD LOWER EXIT LI GHT IAW AMM 33-51-13-400-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800430 1 20080707 A 5321 D5367302100000 FLOORBOARD AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 REFERENCE NON ROUTINE 36564. DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT FLOORBOARD 151AE IS PUNCTURED. MAINT CLEANE D PREPPED AND REPAIRED FLOORBOARD 151AE IAW OF SRM 53-02-00 PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WA S INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800515 1 20080722 A 5321 D5367425000000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 942FR 50 2497 DURING C-CHECK, INSP NOTED THE AFT CARGO PIT FLOOR PANEL 161NF WAS PUNCTURED SEVERAL TIMES. MAINT REPAIRED FLOOR PANEL 1 61NF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE.(A) 2 L 7 2 4F 4 F RT A28NM 20080822 NM 2008 8 22 F3LA200800514 1 20080722 A 5321 D5367402800000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 942FR 50 2497 DURING C-CHECK, INSP NOTED THE AFT CARGO PIT CENTER LT LOWER TRANSITION PANEL 151DE WAS PUNCTURED. MAINT REPAIRED TRANSI TION PANEL 151DE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM 20080822 2008 8 22 F3LA200800410 4 20080702 A 2565 62158101 STUD AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE L1 DOOR SLIDE BROKEN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 901FR 1488 DURING A DAILY CHECK MAINT NOTED THE L1 DOOR EVACUATION SLIDE AT ATTACH BOLT BROKEN AFT SIDE OF L1 DOOR EVACUATION SLIDE . MAINT REMOVED AND REPLACED ATTACH STUD ASSY ON AFT SIDE OF L1 DOOR SLIDE IAW THE REQUIREMENTS OF AMM 25-62-44-400-007. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE AND THE AC WAS RETURNED TO SERVICE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800432 1 20080707 A 5321 D5367302800000 FLOORBOARD AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT FLOORBOARD 151DE HAS A PUNCTURE IN IT. MAINT CLEANED, PREPPED AND REPAIR ED FLOORBOARD 151DE IAW SRM 53-02-00 PARAGRAPH 8C FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND A CCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800444 1 20080710 A 5330 SKIN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED LIGHTNING STRIKE ON FASTNER AT FRAME 29 STATION 1270 STRINGER 41. MAINT REPAIRED BY REMOVING B LIND FASTNER AND COLD WORKING HOLE AND INSTALLING LOCK FASTENER IAW SRM 51-42-11, SRM 51-48-00 AND SRM 53-21-11. UPON CO MPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800477 1 20080711 A 5320 D5323095420002 FITTING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED CORROSION ON PLATE BELOW TIE-DOWN PLATE AT FRAME C29 FWD CARGO COMPARTMENT. MAINT REMOVED AND REPLACED FITTING, REINSTALLED PLATE AND TIE-DOWN AT FWD CARGO COMPARTMENT FRAME C29 IAW SRM 51-42-11 AND 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800472 1 20080711 A 5320 D5347217220500 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED RT LONGERON BEAM AT Y-1292 FROM FRAME 66 TO FRAME 68 HAD AREAS OF CORROSION. MAINT REMOVED AND REPLACED FLOOR SUPPORT LONGERON Y-1292 FROM FRAME 66 TO FRAME 69 IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800489 1 20080716 A 2560 D5311219120300 FITTING AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE R1 GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED THE R1 DOOR GIRT BAR FITTING IB MOUNT HOLES ON SILL PLATE HAD CORROSION. MAINT BLENDED CORROSI ON IAW SRM 51-74-00. MAINT REPAIRED AREAS THAT WERE DEEPER THAT .016" WITH A FILLER AND FILLED AREAS THAT WERE LESS THAN .016" WITH ADHESIVE IAW EA NR A9-53R-30461. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800487 1 20080711 A 5751 D564000001100A SKIN AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE RT WING AILERON CHAFED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED THE RT AILERON APPEARS TO BE CHAFING AT IB LOWER EDGE. MAINT CLEANED AREA OF DAMAGE AND REPAI RED IAW SRM 51-75-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800484 1 20080715 A 5320 D5397496700000 PROFILE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED THE AFT CARGO COMPARTMENT PROFILE AT FRAME C59 HAD CORROSION AT BOTH ENDS OF THE PROFILE. MAIN T REMOVED AND REPLACED THE PROFILE IAW SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE . (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800416 1 20080703 A 5321 REPAIR FLOORBOARD AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 1943 DURING C-CHECK INSP NOTED FLOORBOARD 241FF HAS DELAMINATION ALONG THE EDGE OF THE FLOORBOARD. MAINT PREPPED AREA OF DAMA GE ON FLOORBOARD 241FF FOR REPAIR AND REPAIRED IAW SRM 53-02-00 PARAGRAPH 8J FIGURE 212. UPON COMPLETION OF THE REPAIR I T WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 SO 2008 8 22 SIMA200816503 1 20080610 A 5320 SILL EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 834AE 145631 DURING A MBV INSPECTIONS, THE BAGGAGE DOOR CUT OUT LOWER SILL WAS FOUND CORRODED WITH LEVEL TWO CORROSION. REMOVED THE DAMAGED SILL AND CLEANED THE AREA. POSITIONED AND DRILLED NEW PART, CLEANED AND INSTALLED, WORK DONE IAW EMB 145 SRM (S RM EMB 14511142 REV 40) CHAP 51-20-03, 51-40-02, 05. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080822 SO 2008 8 22 SIMA200817501 1 20080619 A 3350 2013A1 BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DISCHARGED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 643AE 145200 ON FLIGHT 4242 - MAINTENANCE REPORTED OVERHEAD MID CABIN CEILING EMERGENCY LIGHT (EXIT SIGN) NOT IN SERVICE AND RT SIDE MID CABIN EMERGENCY SIGN NOT IN SERVICE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BATTERY HOLDER ASSY NR 4 IAW EMB A45 AMM 33-50-04. OPERATIONAL CHECKED GOOD. ALSO REPLACED EMERGENCY MARKING SIGN ASSY ON RT SIDE AFT OF EMERGE NCY EXIT DOOR IAW EMB 145 AMM 33-50-14. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080822 SO 2008 8 22 SIMA200816405 1 20080606 A 2150 815203 ACM EMB 145 EMB145LR 3260212 SO NR 2 ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 637AE 145170 ON FLIGHT 4498 - CREW REPORTED THE ODOR OF BURNING IN CABIN AND COCKPIT. FLIGHT ATTENDANT REPORTED SLIGHT HAZE IN CABIN IN CLIMB APPROX 15 MIN AFTER TAKEOFF. DISSIPATED QUICKLY (5MIN) WITH NR 1 BLEED AND RECIRCULATION FAN TURNED OFF. DI VERTED INTO CMI. AIRCRAFT REMOVED FROM SERVICE. UPON INVESTIGATION FOUND NR 2 ACM TO BE SEIZED AND NR 2 RECIRCULATION FAN TO BE MAKING NOISE. REMOVED AND REPLACE ACM AND NR 2 RECIRCULATION FAN. NO FURTHER SMOKE OR ODORS NOTED AT THIS TI ME. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080822 EU 2008 8 22 SIMA200816502 1 20080606 A 5320 FLOOR SUPPORT SAAB SF340 340B 7860101 EU GALLEY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 301AE 340B301 DURING A HMBV INSPECTION, A PREVIOUS REPAIR ON THE GALLEY FLOOR FRAME 258.0 WAS FOUND CORRODED WITH LEVEL TWO CORROSION . REMOVED THE DAMAGED FILLER TO REMOVED THE CORROSION. FABRICATED NEW ANGLE FILLER, DRILLED AND TREATED NEW PART. DON E IAW SAAB 340 SRM (SRM 72LKS 3079 REV 50) CHAPTER 53-70-30. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4T RT A52EU 20080822 SO 2008 8 22 SIMA200817803 1 20080625 A 2810 CAP EMB 145 EMB145LR 3260212 SO FUEL CELL OPEN A SIMA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SW 21 620AE 145102 ON FLIGHT 4431 - CREW REPORTED ON THE GROUND, LT WING TANK FUEL CAP CAME OPEN IN FLIGHT. FUEL CAP WAS ONLY SECURED BY T HE LANYARD. CREW ELECTED TO RETURNED TO THE FIELD. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH FUEL CAP SEAL INSPECT ION. RE-INSTALLED CAP, NO DEFECTS NOTED. INSPECTED SURROUNDING AREAS. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE . (A) 2 L 7 2 4T RT T00011AT 20080822 SO 2008 8 22 SIMA200818402 1 20080701 A 2760 M835366022M02 RELAY EMB 135 EMB135LR 3260305 SO SPOILER SYS FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 719AE 145276 ON FLIGHT 4870 - CREW REPORTED AFTER TAKEOFF THAT THEY GOT A SPOILER FAIL EICAS MSG. THE CREW DECLARED AN EMERGENCY AND RETURN TO THE FIELD. MESSAGE EXTINGUISHED AFTER LANDING. AIRCRAFT REMOVED FROM SERVICE. TROUBLESHOT IAW EMB FIM 27-6 3-00-820-807. REMOVED AND REPLACED RELAYS K0479, K0482, K1202, K0030, K0031 QLWO. OPERATION CHECK GOOD IAW EMB MM 27-0 3-00. REFORMED CHECK FLIGHT CHECK FLIGHT GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080822 NM 2008 8 22 AALA200801831 1 20080618 A 3350 D71702001 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 919AN 29520 TUL - EMERGENCY LIGHT BATTERY PACK AT SEAT ROW 19 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROW 1 9. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A16WE 20080822 WP 2008 8 22 IXX2008F00086 1 20080612 A 5730 SKIN DOUG DC8 DC872F 302199E WP RT WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND RT WING LEADING EDGE LOWER SKIN CORRODED AT STATION XW 736.000-761.000. REMOVE D CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND R EPAIR PART. INSTALLED REPAIR PARTS IAW DC8 SRM 57-3-2 FIGURE 8 PAGE 19 ITEM "A", DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 57 -2-0 FIGURE 7, DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-1-20D, AND 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080822 NM 2008 8 22 KCSA081379 1 20080813 A 5311 FRAME BOEING 747 747122 1384872 NM BS 1297 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 716CK 19753 CORROSION ON FRAME ABOVE RT OVERWING LONGERON AT BS 1297, RBL 121, WL 160. (S) 2 L 7 4 4F RT A20WE 20080822 EU 2008 8 22 COEA0806816 1 20080806 A 5711 S57112450200 SPAR AEROSP ATR72 ATR72212 8680945 EU RT WING CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 816FX 26364 347 RT WING FRONT SPAR UPPER FLANGE ANGLE IS SHOWING WEAR MARKS. RT WING FRONT SPAR TOP FLANGE HAS FRETTING DAMAGE WHERE TH E ANTI CHAFE STRIP IS WORN THROUGH. REPAIRED BY BLENDING DAMAGED AREA AND LEAVING AS IS. (S) 2 H 7 2 4T RT A53EU 20080822 EA 2008 8 22 REX2008F00032 1 20080810 A 3150 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA WARNING SYS UNKNOWN A REXA O OTHER G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 SO 25 8631E 7631 AT FL 260 280KTS RECEIVED OVERSPEED CLACKER THEN FLAPS HALF SPEED FOLLOWED BY FLAPS FAIL MESSAGE. QRH FOLLOWED, DECLARE D EMERGENCY WITH UNEVENTFUL LANDING. FLAPS RESET PER FIM AND PLACED ON 72 HOUR WATCH AD 2006-12-21. (S) 2 L 7 2 4F RT A21EA 20080822 CE 2008 8 22 GUU2008F00032 1 20080803 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE COCKPIT ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 17 231YV UE231 FLIGHT 5406 PBI/FLL. DURING FLIGHT LIGHT FUEL ODOR INSIDE ACFT. INSPECTED FUEL AUX TANKS. RAN ENGS WITH BLEEDS OPEN. NO FUEL ODOR DETECTED. (S) 2 L 7 2 4T RT A24CE 20080822 NE 2008 8 22 AALA200801897 2 20080717 A 7250 TURBINE BLADES DOUG DC9 DC982 3022082 WP PWA JT8 JT8D* NE NR1 ENGINE FAILED A AALA A UNSCHED LANDING F Y J FLT CONT AFFECTED ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SW 21 574AA 53151 PVR - INFLIGHT T326/17 JUL. CREW REPORTED LOUD BANG FOLLOWED BY A YAW AND WIND SHEAR ALERT AS GEAR WAS RETRACTED. CAPT AIN REPORTED NR 1 ENG ROLLED BACK WHILE SHUTTING IT DOWN. SINGLE ENG TIME 12 MINUTES. RETURNED TO PVR AND LANDED WITHO UT INCIDENT. FIRE CREW REPORTED SMOKE IN NR 1 ENG. ACFT WOULD NOT MOVE WHEN ATTEMPT WAS MADE TO TAXI BACK TO GATE. RE PLACED NR 1 ENG ON 24 JUL AT PVR DUE TO TURBINE BLADE FAILURE. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F 4 F A6WE E2EA 20080822 NM 2008 8 22 2008UALA03818 1 20080710 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1580 S26-27L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 AFT PIT LT SIDE SLANT AREA HAS DENTED FRAME STA 1580 BETWEEN STR 26L AND 27L. ACCOMPLISHED MAJOR REPAIR AT GSO. CUT OU T DAMAGE AND INSTALLED DOUBLER RPR PER SRM 53-00-07, RPR 5. CREATED FOR REQUIRED REINSPECTIONS. 2 L 7 2 4F 4 F RT A2NM E17NE 20080822 NM 2008 8 22 2008UALA03819 1 20080710 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1380 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 AFT PIT FRAME IS DENTED AT INBOARD FLANGE AT BS 1380, STR 26L. ACCOMPLISHED MAJOR REPAIR AT GSO. CUT OUT DAMAGE AND IN STALLED DOUBLER RPR PER SRM 53-00-07, RPR 5. 2 L 7 2 4F 4 F RT A2NM E17NE 20080822 NM 2008 8 22 2008UALA03820 1 20080710 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1480 S25-26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 AFT PIT AT STA 1480 BETWEEN, STR 25L AND STR 26L, FRAME DENTED AT INBOARD FLANGE. ACCOMPLISHED MAJOR REPAIR AT GSO. CU T OUT DAMAGED FROM FRAME AND INSTALLED DOUBLER RPR PER SRM 53-00-07, RPR 5. 2 L 7 2 4F 4 F RT A2NM E17NE 20080822 WP 2008 8 22 IXX2008F00080 1 20080616 A 5720 STIFFENER DOUG DC8 DC872F 302199E WP RT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C-CHECK INSPECTION, FOUND RT WING TRAILING EDGE STIFFENER CRACKED AT STATION XW 19.000. REMOVED CRACKED STIFFENER. FABRICATED STIFFENER. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND STIFFENER. INSTALLED STIFFENER IAW DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATION 2003-05, ED SEMAN 4816 DATED 07 /14/2008, DACO DPS 4.707, DC8 SRM 51-1-8B, DC8 SRM 51-1-21, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080822 EU 2008 8 22 MAL2008F00028 1 20080722 A 2150 ACM SAAB SF340 340B 7860101 EU ODOR A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 426XJ 340B426 IN CRUISE AT 17K FT SMELLED BURNING ODOR AND SAW SMALL METAL PARTICLES BLOWING OUT OF VENTS. REPLACED RT ACM. (S) 2 L 7 2 4T RT A52EU 20080822 EU 2008 8 22 AALA200801887 1 20080621 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 MIA - EMERGENCY LIGHT AT SEAT 14G INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 14G. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A35EU 20080825 WP 2008 8 25 ABXA080216 1 20080814 A 5610 WINDOW DOUG DC9 DC941 302207N WP COCKPIT STICKING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 FIRST OFFICER`S SLIDING WINDOW WOULD NOT OPEN. OPS CHECKED FIRST OFFICER`S WINDOW NUMEROUS TIMES. OPS CHECKED NORMAL. DID NOT STICK, IAW DC9 AMM. (S) 2 L 7 2 4F A6WE 20080825 NM 2008 8 25 USAASB08060 1 20080807 A 2782 65C3805911 ACTUATOR BOEING 737 7374B7 1384702 NM NR 3 LE SLAT FAILED A USAA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 EA 19 444US 29081 1185 24862 CLT FLT 1631, ON CLIMBOUT FROM CLT, EN ROUTE TO TPA, THE NR 3 LEADING EDGE SLAT FAILED TO RETRACT CAUSING THE ACFT TO RO LL APPROXIMATELY 10 TO 15 DEGREES. PILOT WAS ABLE TO CORRECT THE ROLL WITH REDUCED SPEED AND AILERON INPUT. FLIGHT RET URNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. ACFT TAXIED TO THE GATE ON ITS OWN. AN EMERGENCY WAS DECLAR ED. FDR ANALYSIS CONFIRMED NO UNCOMMANDED MOVEMENT FROM THE RUDDER. MAINTENANCE REMOVED AND REPLACED THE NR 3 LEADING EDGE SLAT ACTUATOR PER MM 27-81-41. LEAK CHECK AND OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A16WE 20080825 EU 2008 8 25 USAA920081497 1 20080809 A 2560 GIRT BAR AIRBUS A321 A321211 3930370 EU R2 DOOR SLIDE DIRTY A USAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 19 170US 1462 FLT 938 MCO-CLT - EES - R2 DOOR SLIDE WILL NOT ARM. MAINTENANCE CLEANED AND LUBED THE GIRT BAR. OPERATIONAL CHECK GOOD . (S) 2 L 7 2 4F RT A28NM 20080820 NM 2008 8 20 SWAA084535 1 20080817 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20080728 SO 2008 7 28 RAIA00806007 1 20080611 A 3350 1010861 LIGHT EMB 145 EMB145 3260210 SO CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 802HK 145066 MX - STL - OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY. (S) 2 L 7 2 4F RT T00011AT 20080728 SO 2008 7 28 RAIA00806004 1 20080608 A 7830 WARNING SYSTEM EMB 145 EMB145 3260210 SO COCKPIT ACTIVATED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 805HK 145096 FLT 3501 - IND - ABORTED TAKEOFF - NR 2 T/R DISAGREE EICAS MESSAGE. MAINTENANCE DEFERRED NR 2 TR PER MEL. (S) 2 L 7 2 4F RT T00011AT 20080728 SO 2008 7 28 RAIA00806012 1 20080613 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 840HK 145341 PRE FLT 7945 - MKE - RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND A LOOSE CONNECTOR AT THE LIGHT ASS EMBLY. CONNECTOR WAS RESECURED AND THE LIGHT FUNCTIONED PROPERLY. (S) 2 L 7 2 4T RT T00011AT 20080728 NM 2008 7 28 2008UALA03355 1 20080613 A 2131 233N31011 CONTROLLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN PRESSURE FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 551UA 25399 CABIN ALTITUDE CONTROL PANEL WHEN SELECTED TO MANUAL "AUTO OFF" LIGHT DOES NOT COME ON. CONTROLLER IS FAULTY. REPLACED CABIN PRESSURE SELECTOR AND AUTOMATIC PRESSURE CONTROLLER 2. OPS CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080728 NM 2008 7 28 2008UALA03492 1 20080620 A 5210 7610179 BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR CORRODED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 536UA 25156 THE 3R DOOR HARD TO ARM & DISARM. INTERNAL BEARING RUSTED AND SIEZED. REPLACED BEARING. DOOR OPS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080728 NM 2008 7 28 2008UALA03495 1 20080619 A 2730 PCU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT DEFECTIVE A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 544UA 25322 WHILE TROUBLESHOOTING DF053 WITH A RT ELEVATOR PCU MESSAGE, GOT LT PCU MESSAGE ON EICAS. TROUBLESHOT MESSAGE DOWN TO LT ELEVATOR RT PCU BAD. REPLACED PCU, OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 NM 2008 7 29 2008UALA03597 1 20080626 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 AFT PIT FRAME DENTED STA 1340, STR 25R - 26R. ACCOMPLISHED MAJOR REPAIR AT GSO. REMOVED DAMAGE, FABRICATED REPAIR AND INSTALLED PER SRM 53-00-07 REPAIR 5. THIS IS A CAT B REPAIR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSPECTION STARTING AT 50000FC AND 12000FC THEREAFTER PER SRM 53-00-07 REPAIR 5 TABLE II. THESE INSP ARE BOTH DETAIL VISUAL AND NDT CURRENT PT C IS 18040. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 NM 2008 7 29 2008UALA03599 1 20080627 A 2150 420365 VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE COCKPIT FAULTY A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 677UA 30029 DEBRIEFED CREW AND NOTED ON APPROACH AT APPROX 4K FEET AND EQUIP COOLING POS ON OVERRIDE, THE "NO COOLING" LIGHT ILLUMIN ATED UNTIL ACFT BLOCKED INTO GATE. AFTER EXTENSIVE TROUBLE SHOOTING FOUND FAULTY OVERRIDE VALVE AND EQUIPMENT COOLING C ARD. REPLACED COOLING CARD AND OVERRIDE VALVE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080729 NM 2008 7 29 WRL2008F00000 1 20080706 A 5712 ARC41252 RIB DOUG MD11 MD11F 3023600 NM RT WING CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 274WA 48633 DURING 1C + 12A CHECK, FOUND STOP RIB CRACKED AT RT OB FLAP. IAW DOCUMENT NR 08-57-57 SECTION 1, ADJUSTED RT OB FLAP NR 2 UP STOP BOLT IN THE RIB. CONDITIONS CHK NORMAL. (K) 2 L 7 3 4F RT A22WE 20080729 NM 2008 7 29 UIE2008F00011 1 20080611 A 5311 FRAME BOEING 747 74747UF 1384812 NM BS 1740-1780 CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 499MC 29260 MAIN DECK CARGO COMPARTMENT RT AFT SIDEWALL CRACKS FOUND ON FRAME INNER FLANGE AT STA 1740 AND 1780. JUST ABOVE FRAME S PLICE AT BETWEEN STRINGER 11R AND 12R. REPAIRED IAW EO 4463A178. (K) 2 L 7 4 4F RT A20WE 20080729 EA 2008 7 29 TRAX200800758 1 20080605 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 SKIN SPLICE DOUBLER JUST AFT OF FS 280.00 IS CORRODED BETWEEN STR-25L AND 25R. JOB COMPLETE. REMOVED RIVETS FROM CORRODE D AREA, BLENDED ALL OF THE CORROSION FROM THE SKIN SPLICE DOUBLER AFT OF 280 BETWEEN STRINGER 25 LT AND STRINGER 25 RT A LL WORK DONE IAW SRM 51-21-06. (A) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800729 1 20080602 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 202 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 202.75 PRESSURE BULKHEAD IS CRACKED AT LOWER LT CORNER 1.0" ABOVE AND 1.0" BELOW CUTOUT FOR PARKING BRAKE CABLE. COMPLI ED WITH REO 601R-53-11-1412, INSTALLED SERVICEABLE INSULATION BLANKETS IAW AMM 25-81-01-400-801. COMPLIED WITH EC/TC R EO 601R-53-11-1412 IAW REO 601R-53-11-1412. (A) 2 L 7 2 4F RT A21EA 20080729 NE 2008 7 29 2008UALA03449 2 20080617 A 7311 HEAT EXCHANGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE DAMAGED A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 597UA 28750 SERVICED IDG WITH 46 PUMPS OF OIL CONSUMPTION IN 9 HOURS. FUEL/OIL HEAT EXCHANGER BREAKING DOWN CAUSING AN OIL STARVE I N THE IDG. REPLACED IDG. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 NE 2008 7 29 2008UALA03581 2 20080624 A 7230 COMPRESSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE STALLED A UALA O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 WP 29 648UA 25285 724366 LEFT ENGINE COMPRESSOR STALL WHEN THROTTLES ADVANCED. ALSO OCCURRED DURING REVERSER OPERATION. UNABLE TO FIND ANY DAMA GE TO ACCOUNT FOR THE REPORTED STALL. ADDITIONALLY, NO SURGE FLAG WAS SET. BECAUSE OF REPEATED POWERPLANT INTERFACE MAN AGEMENT UNIT (PIMU) FAULTS THE EEC WAS REPLACED. SUBSEQUENT HIGH POWER RUNS, AND ACCEL-DECEL CHECKS WERE OK WITH NO STAL L OR SURGE. THE AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER PROBLEMS. 2 L 7 2 4F 4 F RT A1NM E24NE 20080729 EA 2008 7 29 TRAX200800766 1 20080605 A 5230 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 CARGO DOOR FWD TRACK BOTTOM U CHANNEL IS CRACKED 1/4" LONG AT BOTTOM I/B RIVET. REMOVED CRACKED IAW SRM 51-42-06. LOCA TED FASTENER HOLES IN NEW PART AND INSTALLED IAW SRM 51-40-11 AND 51-42-06. J. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800664 1 20080519 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA CABIN WORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 929EV 8007 CREW ESCAPE HATCH EXTERIOR "EMERGENCY EXIT" PLACARD IS WORN. APPLIED NEW SILKSCREEN EXIT PLACARD IAW MM 11-10-03-400-80 1. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800739 1 20080603 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA BS 409 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 FS 409.0+128 BULKHEAD VERTICAL STIFFENER BEAM AT RBL 18 CRACKED AT OUTBOARD SIDE BOTTOM FASTENER APPROX .25 INCH LONG. COMPLIED WITH REPAIR OF FS 409 + 128 BULKHEAD VERTICAL STIFFENER AT RBL 27 IAW ASA CARD: REO 601R-53-41-056 AND BOMBAR DIER REO601R-53-41-056. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800740 1 20080603 A 5310 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.5" IN LENGTH. REMOVED CRACKED ANGLE AND INSTALLED NEW SERVICEAB LE PART IAW SRM 51-42-21. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800851 1 20080629 A 2780 PDU CNDAIR CL600 CL6002C10 1390015 EA SLATS FAILED A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 717EV 10088 LANDING IN ATL 2ND SLAT FAIL 2ND FLIGHT/EMERGENCY DECLARED REMOVED AND REPLACED SLAT POWER DRIVE UNIT IAW 27-81-37 SLAT AND FLAPS SYSTEM CHECK GOOD NO DEFECTS NOTED AT THIS TIME IAW THE AMM. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800733 1 20080603 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 976EV 7601 RT FWD EXTERIOR EMER LIGHT INOP RELAMPED RT FWD EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800732 1 20080603 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 LT SIDE OF BS 280 FLOORBEAM CORRODED BEYOND LIMITS. PICKED FASTENER HOLES EXISTING IN LT 280 BEAM CC670-341-75-7 IAW CR J SRM 51-40-06. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800888 1 20080702 A 5310 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA BS 559 S23R CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 827AS 7212 MINOR CORROSION AROUND FASTENERS BELOW LAV SERVICING POINT FS 559+80 - 559+112 STR 23R. REMOVED FASTENERS BELOW LAV SER VICING POINT. REMOVED CORROSION & REINSTALLED FASTENERS IAW SRM 51-42-06 & SRM 51-21-06. PRESSURIZATION CHECK DUE. PR ESSURIZATION CHECK GOOD IAW AMM 21-32-00-863-801. REPAINT THE BELLY FUSELAGE TO MATCH SURROUNDING AREA. PAINTED REPAI R IAW SRM 51-25-16. (S) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800755 1 20080605 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STIFF A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 829AS 7232 THE F/A REPORT THE MAIN DOOR IS UNUSUALLY DIFFICULT TO OPEN. CYCLE PAX DOOR SEVERAL TIMES. NO DEFECT NOTED AT THIS TIME . IAW AMM 52-11-00. (B) 2 L 7 2 4F RT A21EA 20080826 SO 2008 8 26 C2XA08RI100 1 20080709 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 16999 145307 FLIGHT 2014 - RDU - FLIGHT CREW REPORTED STRONG SMOKE ODOR IN COCKPIT DURING FLIGHT. RIC MX PERFORMED OPERATIONAL CHECK OF WINDSHIELDS 1 AND 2 HEAT, RAN PACKS, RAN BOTH ENGINES AND PERFORMED INSPECTION OF ELECTRICAL COMPONENTS. ALL CHECK WERE PERFORMED SUCCESSFULLY AND NO SMOKE ODOR WAS NOTICED. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080826 EA 2008 8 26 COMA086347 1 20080811 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 477CA 7670 DURING HMV-3 INSPECTION, FOUND UPPER CAP OF FS 280 FLOOR WEB CORRODED FROM LBL 9-RBL 9. CUT OUT DAMAGED SECTION OF WEB AND CAP, INSTALLED WEB DOUBLER, FILLER, AND UPPER CAP ANGLE PER EA 10-5310-02294. (S) 2 L 7 2 4F RT A21EA 20080826 EU 2008 8 26 MAL2008F00025 1 20080730 A 5753 RIB SAAB SF340 340B 7860101 EU LT FLAP CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 448XJ 340B448 LT FLAP, AFT COVE RIB CRACKED AND MISSING RIVET. INSTALLED NEW AFT COVE RIB P/N 7257840081. IAW SAAB340 SRM 51-40-22 A ND EOS57051. REPLACED FASTENERS IN LT FLAP FAIRING AFT BULKHEAD UPPER FLANGE TO REAR SPAR IAW EOS57051. FLAP FAIRING A FT BULKHEAD UPPER FLANGE TO REAR SPAR - ALTERNATIVE FASTENER REPLACEMENT AUTHORIZATION. STANDARD SRM REPAIR PROCEDURES. ADDENDUM FOR MISSING PART CONDITION INFORMATION. (S) 2 L 7 2 4T RT A52EU 20080826 EA 2008 8 26 TRAX200800791 1 20080615 A 3350 BULB CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 903EV 7621 RT WING FWD EMERGENCY LIGHT INOP. REMOVED AND REPLACED RT WING FWD EMERGENCY LIGHT BULB IAW CRJ 200 AMM 33-43-01, OPS C K GOOD. 2 L 7 2 4F RT A21EA 20080925 NM 2008 9 25 08FDEA03925 1 20080917 A 5347 53FX939500 SEAT TRACK BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 SEAT TRACK DAMAGED AT FS 1164 TO FS 1160, BL 0, WL 208 REMOVED DAMAGED, NDT VERIFIED MATERIAL LOSS AND CHECKED FOR DEFEC TS, NO DEFECTS FOUND. ORIGINAL THICKNESS .175 REMAINING.167 MATERIAL LOSS .008" WITHIN LIMITS REF EA 7-5310-114031. TR EATED AND PRIMED AREA REF SRM 51-10-02. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080925 NM 2008 9 25 08FDEA03928 1 20080917 A 5347 53FX9392 SEAT TRACK BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 CORROSION ON SEAT TRACK I/B FLANGE FROM FS 1171 - FS 1146, LBL 24, WL 208. REMOVED CORROSION ON SEAT TRACK, NDT VERIFI ED MATERIAL LOSS AND CHECKED FOR DEFECTS, NO DEFECTS WERE FOUND. ORIGINAL THICKNESS .135 INCH REMAINING .127 INCH MATER IAL LOSS .008 INCH WITHIN LIMITS REF EA 7-5310-114032. TREATED AND PRIMED AREA. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080925 NM 2008 9 25 DL76G081125 1 20080827 A 2421 729825L IDG BOEING 767 767332 1382001 NM NR 1 MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 172DZ 29691 RTB - DUE TO LT ENG GEN W/N POWER BUSS MIP. REMOVED AND REPLACED LT IDG. 2 L 7 2 4F RT A1NM 20080925 NM 2008 9 25 08FDEA03367 1 20080810 A 5347 AFA7795509 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 587FE 48489 MAIN DECK CARGO AT APPROXIMATELY STA 1641, X = 27.5 FOUND SEAT TRACK CORROSION. CABIN MAIN DECK CARGO SEAT TRACK REP AIRED FROM STA 1631 TO STA 1651, X = 27.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2 -100. 2 L 7 3 4F RT A22WE 20080929 NM 2008 9 29 UPS08553307 1 20080821 A 5320 WEB BOEING 757 75724APF 1384969 NM BS 375-435 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 MAIN CARGO FLOOR SHEAR WEB UPPER SURFACE HAS AREAS OF CORROSION BS 375- 435 LBL 45-65 WL 208. REPAIR ED MAIN CARGO FLOOR SHEAR WEB IAW EO B757-5310-30503-A. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 SWAA085064 1 20080914 A 5322 6546546 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 767 S27L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080929 NM 2008 9 29 UPS08553317 1 20080817 A 5320 FLOOR SUPPORT BOEING 757 75724APF 1384969 NM BS 879-894 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 FLOOR SUPPORT IS CORRODED BS 879-894 LBL 65 WL 208. REPAIRED PER ATS ER 08-2804A. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 2008UALA05824 1 20080920 A 5320 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 804UA 759 CORROSION ON L2 DOOR SILL FWD OF FR 68. REPAIRED PER SRM 53-41-14 ON NR K8564G. 2 L 7 2 4F 4 F RT A28NM E40NE 20081024 WP 2008 10 24 08FDEA04351 1 20081015 A 5753 ARC24501 SKIN DOUG DC10 DC1030F 3023504 WP RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 RT WING INBD FLAP FOUND DEEP DENT ON UPPER SKIN 0.50 INCH BY 0.50 INCH DEEP .062 INCH. REPAIRED AREA IAW SRM 57-10-00 F IG 85 SHT 1 VOL I. 2 L 7 3 4F RT A22WE 20080929 NM 2008 9 29 2008UALA05827 1 20080921 A 3397 794640 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT LIGHT INOP. ACROSS DOOR 1 RIGHT LOWER WALL EMERGENCY LIGHT. SECURED CONNECTOR. OPS CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 NM 2008 9 29 2008UALA05832 1 20080921 A 3397 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT SIGN INOP, JUST AFT OF DOOR 4 RIGHT. REPLACED FEEDER CABLE. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 NM 2008 9 29 2008UALA05833 1 20080921 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT LIGHT INOP. ACROSS DOOR 4 LEFT LOWER WALL EMERGENCY LIGHT. REPLACED FEEDER CABLE. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 2008 9 29 2008UALA05835 4 20080922 A 2565 7A1323113 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 178UA 24385 RT UPPER DECK SLIDE ARM-DISARM LEVER HARD TO MOVE. REPLACED UPPER DECK SLIDE ASSY. FUNCTION OPERATES NORMALLY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 NM 2008 9 29 2008UALA05837 1 20080921 A 7921 OIL COOLER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT ENGINE MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 781UA 26945 777052 L ENG OIL QTY INDICATION DROPPING INDICATED 2 QTS WITH TEMPERATURE RISING, CREW REPORT. REPLACED AIR COOLED OIL COOLER. RUN, OPS LEAK CHECK OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080929 NM 2008 9 29 DL764081210 1 20080921 A 5240 DOOR BOEING 767 767432ER 1385134 NM R1 OBSTRUCTED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 835MH 29708 DOOR 1R SHOWED OPEN ON TAXI OUT. DOOR APPEARS TO BE OUT OF TRACK FOUND DEBRIS IN DOOR WAY. CLEANED AND INSPECTED. FOU ND NO OTHER PROBLEMS. DOOR OPS AND ARMS NORMAL. CREW RESET DOOR AND LIGHT WENT OUT. RETURNED TO GATE FOR MTC TO INSPEC T. 2 L 7 2 4F RT A1NM 20080929 NM 2008 9 29 DLM88081213 1 20080922 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 645 L30 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DL 49542 FUSELAGE SKIN FOUND CRACKED AND BULGED AT STA 645 AND L30. DAMAGE WAS TRIMMED OUT. WHILE TRIMMING ADDITIONAL DAMAGE WA S FOUND TO THE INTERNAL DOOR SURROUND DOUBLER AT STA 626. TOOLING DAMAGE AT HOLES LOCATED AT STA 629. THE SKIN WAS REP AIRED BY SPLICING A NEW SECTION PER SRM 53-04 FIG 12C, INTERNAL DOUBLER WAS REPAIRED BY INSTALLING AN INTERNAL REPAIR DO UBLER. OVERSIZED HOLES WERE REPAIRED BY INSTALLING OVERSIZED FASTENERS. 2 L 7 2 4F RT A6WE 20080929 NM 2008 9 29 DLM88081215 1 20080922 A 2740 ACTUATOR DOUG MD88 MD88 3023688 NM TRIM MOTOR BROKEN A DALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 27 977DL 53258 HOUSING FOUND CRACKED AND BROKEN PIECE HANGING ON WIRES. ALT TRIM INOP. REMOVED AND REPLACED ALT TRIM MOTOR ACTUATOR P ER M/M CKS OK. 2 L 7 2 4F RT A6WE 20080929 WP 2008 9 29 08FDEA04019 1 20080924 A 5230 FITTING DOUG MD10 MD1010F 3022112 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 MAIN CARGO DOOR LOWER JAMB FITTING AT SPOOL LOCATION NR 3 HAS A CRACK INDICATION AT HOLE A. REMOVED & REPLACED FITTING IN REF TO SRM 51-38-04. REPAIREDUPPER BEAM IN REF TO SRM 53-50-00. 2 L 7 3 4F RT A22WE 20080929 NM 2008 9 29 08FDEA04024 1 20080924 A 5347 7178T6511 SEAT TRACK BOEING 757 75723A 1384967 NM BS 680-780 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 MAIN CABIN, SEAT TRACK BS 680 TO BS 780 LBL 45.5 HAS CORROSION AND GOUGED. REMOVED AND REPLACED SEAT TRACK, TRAVELER NR T8-758325, IAW 51-40-02. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 08FDEA04025 1 20080924 A 5347 BAC152079224 SEAT TRACK BOEING 757 75723A 1384967 NM BS 440-680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 MAIN CABIN SEAT TRACK BS 440-680 CROWN SCRATCHED, GOUGED AND HAS CORROSION ON BS 675 LBL 45.5. REMOVED SEAT TRACK, FAB SEAT TRACK ON TRAVELER NR T8-758687 AND INSTALLED SEAT TRACK IAW 51-10-02. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 08FDEA04026 1 20080924 A 5330 SKIN BOEING 757 75723A 1384967 NM BS 1500-1520 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 FUSELAGE SKIN BETWEEN STA 1500 AND 1520, STR 24L AND 25L HAS SMALL PUNCTURE DAMAGE REMOVED DAMAGE, FAB REPAIR PARTS, AND LOCATED AND DRILLED REPAIR PARTS IAW SRM 53-00-01 REPAIR 7. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-20-01. INSTALL ED REPAIR PARTS IAW 51-40-02, MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 08FDEA04027 1 20080924 A 5347 7178T6511 SEAT TRACK BOEING 757 75723A 1384967 NM BS 418-440 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 MAIN CABIN SEAT TRACK, STA 418-440, RBL 45, IS GOUGED AND HAS CORROSION. REMOVED CORROSION FROM DAMAGED AREA. DAMAGED A REA CHECKED OUT OF LIMITS. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK PER TRAVELER NR T8/756397. PREP AND PAINTED S EAT TRACK IAW 51-21-10. INSTALLED NEW SEAT TRACK AT STA 418-440 RBL 45 IAW 51-40-02. 2 L 7 2 4F RT A2NM 20080929 EU 2008 9 29 08FDEA04031 1 20080925 A 5730 A57241371002 PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CHAFING ON PANEL 471AT, LT WING, RIB 7-8 PANEL REPLACED IAW DRAWING R572-40275, APPROVED BY RAS/BAE/1007905/2008 I SS A AND EA 6-5741-123099. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA04034 1 20080925 A 5542 SKIN AIRBUS A300 A300F4622R 3930360 EU RUDDER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND ON RUDDER LT SIDE NEAR HOISTING POINTS FLUID INGRESS (SEVERAL AREAS) WITH DEBONDING. REPAIR PERFORMED BY BONDING REPAIRS IAW RAS/DAHAM/4025347/2008 ISS A, APPROVED BY EA 6-5541-123055. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA04036 1 20080925 A 5330 A53812189201 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSION ON FUSELAGE SKIN, C 39-40, P 27-28 RT AT KRUEGER FLAP AREA. REPAIR PERFORMED BY REPLACEMENT OF SKIN PAN EL IAW RAS/70512709/008/2008, APPROVED BY EA 6-5315-123058. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA04037 1 20080925 A 5330 A53831283202 SPLICE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 744FD 664 FOUND DURING SKIN PANEL REPAIR IAW DR 187 SIX OVERSIZED HOLES ON FUSELAGE SKIN, C 39-40, P 27-28 LT IN SPLICE A538-31283 -202. REPAIR PERFORMED BY INSTALLATION OF SHOULDERED BUSHES IAW RAS/70512709/008/2008, APPROVED BY EA 6-5315-123058. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA04039 1 20080925 A 5347 A5327501820600 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 MAIN CABIN SEAT TRACK AT FRAME 57.1, Y 45.0 IS WORN AT THE TANG. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-10-16. 2 L 7 2 4F RT A35EU 20080929 NM 2008 9 29 DL757081217 1 20080825 A 5410 STRUCTURE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 716458 1 HOLE IS OVERIZED TO .437 (NEXT NOMINAL STANDARD) ON NR 1 ENG PYLON I/B SIDE. INSTALLED 1 FASTENER AND COLLAR IAW SRM 51-40-02. COMPLIED WITH ERA 469688. 2 L 7 2 4F 4 F RT A2NM E17NE 20080729 NM 2008 7 29 2008UALA03590 1 20080625 A 2910 HYDRAULIC SYSTEM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CENTER SYSTEM FAILED A UALA O OTHER W K INADEQUATE Q C FLUID LOSS AP APPROACH 1 WP 29 212UA 30218 LOST ENTIRE CENTER HYDRAULIC SYSTEM AT 1000 FEET ON FINAL APPROACH. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080729 EA 2008 7 29 TRAX200800882 1 20080705 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 LT FS 280 FLOORBEAM CORRODED. (B) BLENDED MINOR CORROSION AREAS (3 TOTAL) ON FLOORBEAM IAW REO 670-53-11-046. .004 M ATERIAL REMOVED. BLENDED AREAS WITHIN LIMITS. PERFORMED CUTOUT OF DAMAGED AREA FLOORBEAM, AND FABRICATED FILLER PER RE O 670-53-11-310. (S) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800731 1 20080603 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 RT BS 280 FLOORBEAM CORRODED OUT OF LIMITS. PICKED UP EXISTING FASTENER HOLES RT 280 BEAM CC 670-341-75-7 IAW SRM 51-40 -06. (B) 2 L 7 2 4F RT A21EA 20080729 EU 2008 7 29 TRAX200800723 1 20080601 A 2613 DETECTOR AEROSP ATR72 ATR72212 8680945 EU BRAKE TEMP MALFUNCTIONED A ASOA O OTHER N FALSE WARNING CR CRUISE 1 SO 27 635AS 372 HOT BRAKE TEMP IN CRUISE. FLT 4216 DEL 31 MINS. (BRAKE TEMP LIGHT SYSTEM) REMOVED AND REPLACED LT O/B AND I/B COMPENSA TORS IAW ATR 72 JIC 32-42-56. OPS CHECK GOOD. DEFER CLEARED. PLACARD REMOVED. (B) 2 H 7 2 4T RT A53EU 20080729 EA 2008 7 29 TRAX200800712 1 20080530 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 907EV 7648 BOTH L/R AFT EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 4 BATTERY PACK IAW AMM 33-51-04-400-801 OPS CK GOOD. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800726 1 20080602 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A ASOA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 845AS 7324 PAX DOOR CANNOT BE OPENED FROM INSIDE. FLT 4254. OPS CHECK DOOR SEVERAL TIMES. OPS CHECKED GOOD. LUBED OUTER DOOR STOW HANDLE. OPS GOOD. OK FOR SERVICE IAW 52-11-01. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800763 1 20080605 A 5220 HANDLE CNDAIR CL600 CL6002C10 1390015 EA ESCAPE HATCH CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 CREW ESCAPE HATCH OUTER HANDLE IS CORRODED. REMOVED AND REPLACED OUTSIDE HANDLE ON CREW ESCAPE HATCH IAW AMM 52-22-02. REFER TO EO 700-52-0057. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800889 1 20080706 A 5210 STRUT CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 317CA 10055 PAX DOOR DIFFICULT TO CLOSE AND HITS HARD WHEN OPENNING. FLT 4286. REMOVED AND REPLACED FWD AND AFT GAS STRUTS ON ASD O PS CHECK GOOD IAW MM 52-11-17. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 2008UALA03638 1 20080628 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EEL INOP SEAT 5E AFT SECTION. 2 L 7 4 4F 4 F RT A20WE E24NE 20080729 EU 2008 7 29 TRAX200800761 1 20080605 A 5240 LINKAGE AEROSP ATR72 ATR72 EU SERVICE OBSTRUCTED A ASOA K NONE C F.O.D. IN INSP/MAINT 1 SO 27 643AS 413 SERVICE DOOR WILL NOT CLOSE. FLT 4223. REMOVED INSULATION FROM LINKAGE OPS CHECKED NORMAL PER JIC 52-40-10-OPT. (B) 2 H 7 2 4T RT 20080729 EA 2008 7 29 TRAX200800728 1 20080602 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 732 S10-11R CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 FUSELAGE SKIN IS CRACKED AT RT FS 732 2.5L BETWEEN STR 10 &11 AND CHAFING DAMAGE FROM CONTACT WITH T/E PYLON BETWEEN FS 700.00 AND FS 755.00 BETWEEN S9-12. (B) REPAIRED SKIN IAW REO 601R-53-61-268 REV A NOTES 1-16. COMPLIED WITH REO 601 R-53-61-268 AND COMPLETED ALL REQUIRED FORMS. (A) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800713 1 20080530 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 886AS 7531 PAX DOOR UPPER STEP HAS CRACK APPROXIMATELY 4" LONG REMOVED AND REPLACED PAX DOOR TOP STEP IAW AMM 52-11. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800720 1 20080601 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA OUT OF ADJUST A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 936EV 8038 SERVICE DOOR WILL NOT OPEN FROM THE OUTSIDE. ADJUSTED SERVICE DOOR PER MM REF 52-41-00 OPS CHECK OK. (B) 2 L 7 2 4F RT A21EA 20080729 NM 2008 7 29 ASAA0843120 1 20080606 A 5322 654655138 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 STRINGER SHEAR TIE PREVIOUS REPAIR CORRODED. REPAIRED PER SRM 53 00 07. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843121 1 20080506 A 5315 654681179 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 FLOORBEAM UPPER FLANGE IS CORRODED. REPAIRED PER EA 5310 02800. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843126 1 20080507 A 5311 90526911 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA O OTHER O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 RIGHT FRAME AT STATION 480 CRACKED AT PSU RAIL BRACKET. RIGHT FRAME AT STATION 480 AT PSU RAIL BRACKET REPAIRED IAW CAS CADE ERO 8337 ASA EA 5310 02797. 2 L 7 2 4F RT A16WE 20080929 NM 2008 9 29 DLM88081218 1 20080907 A 5347 SEAT TRACK DOUG MD88 MD88 3023688 NM BS 680-710 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 SEAT TRACK HAS EXFOLIATED CORROSION AT STA 680-710 LBL 24.5, REPLACED SECTION. 2 L 7 2 4F RT A6WE 20080929 NM 2008 9 29 DL757081219 1 20080823 A 5754 SKIN BOEING 757 757232 1384965 NM NR 3 SLAT GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 SMALL GOUGE ON T/E OF SLAT NR 3. BONDED SKIN FILLER AND INTERNAL DOUBLER AND CORE PLUG IAW SRM 51-70-10. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 DLM88081220 1 20080918 A 5320 PLATE DOUG MD88 MD88 3023688 NM BS 1680 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 MAIN CABIN AFT DECK PLATE STA 1680 LBL 47 TO RBL 51 HAS CORROSION ON UPPER SURFACE, REPAIRED. 2 L 7 2 4F RT A6WE 20080929 NM 2008 9 29 DLM88081222 1 20080909 A 5220 SKIN DOUG MD88 MD88 3023688 NM EMERGENCY EXIT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 CREASE ON EXTERNAL SKIN OF AFT LT WING EMERGENCY EXIT DOOR REPAIRED. 2 L 7 2 4F RT A6WE 20080929 NM 2008 9 29 DL764081223 1 20080924 A 2131 CONTROLLER BOEING 767 767432ER 1385134 NM CABIN PRESSURE FAULTED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 837MH 29710 ON TAXI OUT, CAB AUTO INOP EICAS MSG CAME ON. RESET CB ON P11 CAB ALT 1 AND CBN ALT 2. PERFORMED BIT ON BOTH CONTROLLE RS. TEST FOR AUTO 1 AND 2 SHOWS CONTROLLER FAULT. PERFORMED VERIFY RESET NO FAULTS AND NO STATUS MSG NO FAULT LIGHT FO R ALT 1 AND 2, SYS CHK GOOD. 2 L 7 2 4F RT A1NM 20080929 NM 2008 9 29 DL757081224 1 20080819 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1620 S27-28R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 FUSELAGE STA 1620 BETWEEN S27R AND S28R LWR SIDE HAS DENT. INSTALLED DOUBLER AND 2 FILLERS IAW SRM 53-00-01. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 DL757081225 1 20080820 A 5347 SEAT TRACK BOEING 757 757232 1384965 NM BS 686-710 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 SEAT TRACK HAS EXFOLIATED CORROSION AT STA 686-710 LBL 45.5. REMOVED SEAT TRACK FROM STA 669 TO STA 788 LBL 45.5 IAW SR M 53-00-51. INSTALLED REPLACEMENT SEAT TRACK IAW SRM 51-20-01. 2 L 7 2 4F RT A2NM 20080929 WP 2008 9 29 08FDEA03990 1 20080922 A 5330 ADA31391 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 THE EXTERIOR SKIN HAS 2 SCRATCHES 0.750 LONG AND A DENT THAT IS 0.020 LONG AND 0.100 DEEP LOCATED 52 INCHES AFT OF THE LOWER FWD CARGO DOOR AND APPROX 36 INCHES ABOVE THE WHITE LINE. SEQUENCE NR 000830, WRI NR 53105938. REPAIRED THE DA MAGED AREA IAW DC/MD-10 SRM 53-20-00, FIG 6, SHEET 3, VOL I. 2 L 7 3 4F RT A22WE 20080929 NM 2008 9 29 08FDEA04006 1 20080923 A 5414 311N504631 SKIN BOEING 757 75723A 1384967 NM ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 NR 1 PYLON O/B AFT 311N5046-31 SKIN PANEL ASSY HAS CORROSION ON INNER SURFACE. REMOVED AND INSTALLED STRIKER PLATE AND MOUNT FITTING PER SRM 51-40-02 AND DRAWING 311N5108. REMOVED AND INSTALLED HEAT SHIELD PER SRM 51-40-02. REMOVED AND I NSTALLED FWD FAIRING PER SRM 51-40-02. REMOVED O\B AFT SKIN PER SRM 51-40-02. RECEIVED NEW SKIN ON FEDEX SERVICABLE TA G NR 4541B3 LOCATED AND DRILLED NEW SKIN AND INSTALLED SKIN PER SRM 51-40-02 AND DRWG 311N5002 CAT A MAJOR REPAIR NO FOL LOW UP INSPECTION REQUIRED. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 08FDEA04007 1 20080923 A 5310 7075T6050C CREASE BEAM BOEING 757 75723A 1384967 NM BS 1600-1620 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 MAIN CABIN STA 1600-1620, RT SIDE CREASE BEAM WEB AND I/B CHORD HAVE CORROSION. REMOVED WEB IAW SRM 51-40-02. FABRICAT ED NEW WEB ON MAE TRAV NR T8/75784 IAW SRM 51-21-01. INSTALLED WEB ON STA 1600 IAW SRM 51-40-02. MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 08FDEA04008 1 20080923 A 5320 70750071C CHANNEL BOEING 757 75723A 1384967 NM BS 1280 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 FRAME STA 1280 HAS GOUGES ON DIFF, AREAS BETWEEN S5R TO S14R. BLENDED AREAS, IAW SRM 53-00-07. FABRICATED REPAIR PARTS ON MAE TRAV NR T8/753587 AND T8/753544. INSTALLED REPAIR PARTS ON FRAME STA 1280 IAW SRM 51-40-02. MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 08FDEA04009 1 20080923 A 5412 BULKHEAD BOEING 757 757236 1384971 NM NR 1 PYLON DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 NR 1 PYLON MID BULKHEAD LT SIDE HAS 1 NUT PLATE WITH DOUBLE DRILLED FASTENER HOLES. REPAIR COMPLIED WITH EA F 5452- 110 907 AND MAE EA 757- 54521-16-A1802, REV, MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20080929 2008 9 29 08FDEA04010 4 20080923 A 3400 UNKNOWN DOUG MD11 MD11F 3023600 NM UNKNOWN A FDEA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC AP APPROACH 1 CE 21 620FE 48791 DURING ILS APPROACH TO SFS, IN LIGHT TO MODERATE PRECIP, AT'S AND AP DISCONNECTED, ALSO HAD IAS COMPARATOR WARNING, W/ 5 TO 15 KTS DIFFERENCE. ALSO LEVEL 2 SEL ELEV FEEL MANUAL, LSAS ALL FAIL AND TWO OR MORE MOMENTARY LEVEL 2 ALERTS OCCUR RED. ON GO AROUND, ALL ALERTS BEGAN TO EXTINGUISHED, ATTEMPTED 2ND ILS APPROACH, ALL AS ABOVE RE-OCCURRED AGAIN. CFDS CURRENT FAULTS, NIL. FRONT FACE INSPECTION FOR FAULT BALL ON ALL 3 ADC'S, REVEALED NONE. PER RECOMMENDATION FROM MOCC , ADJUSTMENT TEST PER AMM 34-16-01-5 CARRIED OUT, ALL R-T-S TEST PASSED ON ALL 3 ADC'S, ADDITIONAL VISUAL INSPECTION ON ALL PITOT TUBES, NIL OBSTRUCTION, ACFT OK FOR SVC. 2 L 7 3 4F RT A22WE 20080929 NM 2008 9 29 08FDEA04011 1 20080923 A 2422 260CZ01 RELAY DOUG MD11 MD11F 3023600 NM MALFUNCTIONED A FDEA J DUMP FUEL H ELECT. POWER LOSS-50 PC CR CRUISE 1 CE 21 528FE 48623 DURING CRUISE RECEIVED LEVEL 1 "R EMER AC OFF". F/O LOST MCDU NR 2 AND FMC2, DEU NR 2, DU4, 5 AND 6 NOTE: VERBAL FROM C REW ON POST FLIGHT, DUMPED 62.0 LB FUEL DUE ATB. CHECKED EPCU FAULT REVIEW AND FOUND "LEG 1 IN AIR" REAC SENSE RELAY/I NTFC. CHECKED CURRENT FAULT AND ALSO HAD "REAC SENSE RELAY/INTFC". A/C HAS HISTORY. REPLACED RELAY R2-5157 PER FIM, POWER RETURNED. RAN ENGINES. DURING SHUTDOWN ALERT RETURNED. REPLACED RT EMER AC BUSS FEED RCCB.(B1-138) AMM 24-50-0 1-4. SYSTEM NEEDS OPS CHECK. REMOVED AND REPLACED R2-18 RIGHT EMERGENCY TRANSFER RELAY REF MM 24-25-03-2, RAN ENGINES SEVERAL TIMES, ALL INDICATIONS NORMAL, MM SUBTASK 24-25-03-820-001. 2 L 7 3 4F RT A22WE 20081015 WP 2008 10 15 22AA20081001 1 20081003 A 2910 HYDRAULIC LINE DOUG DC10 DC1030F 3023504 WP MAIN CARGO DOOR DAMAGED A 22AA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 19 450ML 47831 AFTER CLOSING CARGO DOOR FOR DEPARTURE, HARD ODOR OF HYDRAULIC FLUID IN FLIGHT DECK. REMOVED AND REPLACED MAIN CARGO DO OR CLOSE LINE AS REQUIRED; OPERATIONAL CHECK NORMAL IN ACCORDANCE WITH M/M 52-34-01, NO LEAKS FOUND. 2 L 7 3 4F RT A22WE 20080929 WP 2008 9 29 08FDEA04018 1 20080924 A 5340 FITTING DOUG MD10 MD1010F 3022112 WP DOOR FRAME CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 MAIN CARGO DOOR LOWER JAMB FITTING AT SPOOL LOCATION NR 2 HAS CRACK INDICATIONS AT HOLES A, C AND D. REMOVED & REPLACED FITTING IN REF TO SRM 51-33-01. REPAIRED HOLES IN UPPER BEAM IN REF TO SRM 53-50-00. 2 L 7 3 4F RT A22WE 20080729 NM 2008 7 29 ASAA0843127 1 20080507 A 5311 90526913 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 RIGHT FRAME AT STATION 500A CRACKED AT PSU RAIL BRACKET. RIGHT FRAME AT STATION 500A AT PSU RAIL BRACKET REPAIRED IAW C ASCADE ERO 8337 AND ASA EA 5310 02797. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0843128 1 20080507 A 5311 90526913 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 756AS 25097 RIGHT FRAME AT STA 727B CRACKED AT PSU RAIL BRACKET. RIGHT FRAME AT STA 727B AT PSU RAIL BRACKET REPAIRED IAW CASCADE E RO 8337 ASA EA 5310 02797. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ASAA0853170 1 20080701 A 2131 71231997303AB CONTROLLER BOEING 737 737890 1384527 NM CABIN PRESSURE MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION UK UNKNOWN 1 NM 02 584AS 3485 35682 AUTO FAILED ON PRESSURIZATION ALTN MODE SELECTED AUTO FAIL LIGHT OUT. UNABLE TO DUPLICATE DISCREPANCY NR 2 CONTROLLER L OGGED FAULT CODE 101 FOR FLIGHT 479. ACCOMPLISHED FIM 31 803 FOUND FAULT TO BE INTERMITTENT. GROUND VERIFICATION TEST PASSED REF MM 21 31 00. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 ZZDA2008129 1 20080710 A 3350 AD8039491 POWER SUPPLY BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 915AT 55085 FOUND AISLE EMERGENCY LIGHTS ROW 1 THROUGH 10 INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY IAW AMM 33-51. OPS CHECK GOOD. REF NRWC N064491. 2 L 7 2 4F TR A6WE 20080729 NM 2008 7 29 ASAA0843175 1 20080629 A 5755 654645170A SKIN BOEING 737 737490 1384715 NM NR 2 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 797AS 28892 NR 2 SPOILER HAS DENT ON UPPER SURFACE ABOUT 9 INCHES FROM O/B END. PREPARED DAMAGED AREA. FABRICATED REPAIR DOUBLER A ND BONDED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20080729 NM 2008 7 29 USAA920081166 1 20080601 A 5754 65C2660399 WEDGE BOEING 737 73733A 1384673 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 166AW 23627 PHX - MAJOR REPAIR - B CHECK - LT WING NR 3 SLAT TRAILING EDGE WEDGE DELAMINATED. REPLACED THE LEFT WING NR 3 SLAT TRAI LING EDGE WEDGE IAW DRAWING 65C26603. (S) 2 L 7 2 4F RT A16WE 20080729 EA 2008 7 29 TRAX200800890 1 20080706 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 843AS 7310 LT SIDE OF FUSELAGE EXTERNAL AFT EMERGENCY LIGHT INOP. RELAMP LT SIDE OF FUSELAGE EXTERNAL AFT EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. (B) 2 L 7 2 4F RT A21EA 20080729 EA 2008 7 29 TRAX200800905 1 20080712 A 5240 SHEAR PIN CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 SERVICE DOOR SHEAR PIN RELEASE HANDLE INOPERATIVE. FLT 4497. REMOVED AND REPLACED SERVICE DOOR SHEAR PIN OPS CHECKED G OOD. IN ACCORDANCE WITH AMM 42-41-00. OK FOR SERVICE. (B) 2 L 7 2 4F RT A21EA 20080924 EU 2008 9 24 08FDEA03300 1 20080807 A 5415 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU NACELLE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 CORROSION FOUND IN BOLT HOLES OF FORWARD PYLON TO ENGINE ATTACH FITTING. REPAIR PERFORMED BY REWORK OF CORROSION, NDT F OR CORROSION FREE CONDITION. REPLACE THE TAPERED SHIM AND PROTECT RIB 8 WITH CADMIUM PLATING IAW RAS/70511822/004/2008 ISS A, APPROVED BY EA 6-5451-120089. 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03748 1 20080906 A 5320 65209842 FITTING BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 DAMAGED TENSION TIE AT STA 362 STR 17L. REMOVED AND REPLACED DAMAGED TENSION TIE AT BS 362 STR 17L WITH NEW TIE PART NU MBER 65-20984-2 PO NR. 2 L 7 3 4F RT A3WE 20080924 NM 2008 9 24 08FDEA03749 1 20080906 A 5414 65196854032 SKIN BOEING 727 727233 138408A NM ZONE 100 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 TORN SKIN NR 1 ENGINE INLET COWL 4 O`CLOCK POS INBD SIDE AT COWL ATTACH LIP. CUT OUT DAMAGED AREA DIMS 1 1/2" BY 1" IAW SRM 51-10-1. FABRICATED DOUBLER REPAIR AND FILLER IAW SRM 54-30-3 FIG 3A. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 54-30-3 FIG 3A. 2 L 7 3 4F RT A3WE 20080924 EU 2008 9 24 08FDEA03750 1 20080906 A 5347 R5307008820400 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 651FE 728 MDCC SEAT TRACK NR 1 HAS 3 AREAS OF CORROSION BETWEEN FR 74 AND 8 IN AFT OF FR 76 REMOVED LEVEL 1 CORROSION FROM NR 1. REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED SEAT TRACK SPLICE REPAIR BETWEEN FR 74 AND FR 77 IAW A300-600 SRM 53 -10-16, FIG 208, PAGE 247/248. 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03751 1 20080906 A 5712 651626238 RIB BOEING 727 727233 138408A NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 RIGHT WING TIP INTERIOR CRACKED WBL 624. REMOVED WING TIP IAW B727 MM 57-20-001-4. REMOVED WING TIP RIB IAW B727 SRM 5 1-30-2. LOCATED AND DRILLED NEW RIB IAW B727 SRM 51-30-5. INSTALLED NEW RIB IAW B727 SRM 51-30-2 AND REINSTALLED WING TIP IAW B727 MM 57-20-001-4. 2 L 7 3 4F RT A3WE 20080924 WP 2008 9 24 08FDEA03318 1 20080808 A 5320 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 358FE 46633 MCD LATCH SPOOL BACK UP FITTING HOLES SHOW DEFECT POS NR 1 HOLE C AND D MARKED IN RED. REPAIRED SPOOL BRACKET HOLES, RE PLACED BACK UP FITTING, FABRICATED REPAIR BUSHINGS AND FUNCTIONAL CHECK IAW SRM 53-50-00 VOL 1 FIG 17, MAE TRAVELER T8/7 52908 AND WORK CARD E-9-5230-7-5000. REPAIR IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A22WE 20080924 WP 2008 9 24 08FDEA03319 1 20080808 A 4910 ACA33501 ANGLE DOUG DC10 DC1010 3022110 WP APU BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 AIR CONDITIONING COMPT PACK NR 1, FOUND EXFOLIATION CORROSION ON CAP ANGLE AND CLIP. 2 L 7 3 4F A22WE 20080924 WP 2008 9 24 08FDEA03320 1 20080808 A 5320 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 358FE 46633 MCD LATCH SPOOL BACKUP FITTING HOLES SHOW DEFECT POS NR 7 HOLES A, B, C AND D MARKED IN RED. REPAIRED SPOOL BRACKET HOL ES, REPLACED BACK UP FITTING. FABRICATED REPAIR BUSHINGS AND FUNCTIONAL CHECK IAW SRM 53-50-00 VOL 1 FIG 17, MAE TRAVIL ERT8/752909 AND WORK CARD E 9-5230-7-5000. REPAIRED CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F RT A22WE 20080929 NM 2008 9 29 08FDEA03933 1 20080918 A 5720 6922241 CHANNEL BOEING 727 727227 1384078 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 RT WING, I/B AILERON O/B L/E SEAL MOUNT BRACKET/UNDERWING PANEL MOUNT BRACKET CRACKED 10 INCH I/B FROM O/B END OF AILERO N REMOVED SEAL MOUNT BRACKET AND ATTACH ANGLE, FABRICATED NEW "U" CHANNEL. FABRICATED NEW ATTACH ANGLE, HEAT TREATED TO T4 CONDITION. U CHANNEL AND ATTACH ANGLE WERE TREATED, PRIMED, AND TOP COATED. U CHANNEL AND ATTACH ANGLE INSTALLED R EF SRM 51-30-2. DWR 69-22241, 65-19288, GMM 7-0-1-001. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080929 EU 2008 9 29 08FDEA03934 1 20080918 A 5347 A5383221120400 SEAT TRACK AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 808FD 439 MDCC SEAT TRACK 3R CORRODED 2 AREAS AT FRAME 46 4 INCH SQ IN REMOVED LEVEL 1 CORROSION ON SEAT TRACK SECTION AND INSTALL ED NEW SEAT TRACK 3R FROM FRAME 44 TO 49 IAW A300-600 FREIGHTER SRM 53-10-16 FIG 102 PG 105 AND SRM 51-40- 21. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03935 1 20080918 A 5330 A53777381200 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 808FD 439 RIGHT SIDE FUSELAGE FR 37 STRINGER 30 1 LIGHTNING STRIKE REMOVED DAMAGED AREA AT FR37 RT SIDE STR 30 AND INSTALLED REPAI R DOUBLER IAW SRM 53-10-12 FIG 224 SHEET 3. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03284 1 20080806 A 5321 B5327038001800 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DOOR PANEL NR 252 XG; IS CRACKED; HAS EDGE DAMAGE AND PUNCTURED. FABRICATED NEW PANEL IAW SRM 53-10-20 AND D WG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03285 1 20080806 A 5321 B5327028200000 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DOOR PANEL NR 252 YG, IS CRACKED AND PUNCTURED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03897 1 20080916 A 5330 A5377608020200 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 EXTERIOR FUSELAGE UPPER SKIN HAS STATIC DISCHARGE AT FRAME 65; BETWEEN STRINGER 2 L AND 3 L. BLENDED AREA IAW SRM 53-10 -12; FIG 220. MATERIAL THICKNESS 0.071. MATERIAL LOSS 0.005. MATERIAL REMAINING 0.066. FOUND TO BE WITHIN LIMITS IAW SRM 53-17-12. ACCOMPLISHED HFEC INSPECTION OF THE BLENDED AREA IAW NTM 51-10-08. ALODINED AND PRIMED IAW SRM 51-21-01 . 2 L 7 2 4F RT A35EU 20080929 SO 2008 9 29 LR7A08102 1 20080819 A 5320 3567299 CHANNEL LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HC5211, FOUND RAMP DOOR FLOOR BOARD RT INNER HAT-SECTION CRACKED AT RS0 TO 10. WL146, RBL33. REPAIRED BY REPLACING HAT-SECTION IAW SMP583 CHAP 51-60, 51-70 AND DWG 356729. 2 H 7 4 4T A1SO 20080929 SO 2008 9 29 LR7A08103 1 20080819 A 5320 33766471 CHANNEL LKHEED 382 382G 526414U SO FS 208 WL140 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HC3215 FOUND NWW U CHANNEL CRACKED AT FS 208, WL140, BL0. REPAIRED BY REPLACIN G CHANNEL IAW SMP583 CHAPTER 51-70. 2 H 7 4 4T A1SO 20080929 SO 2008 9 29 LR7A08104 1 20080819 A 5320 34004237R FRAME LKHEED 382 382G 526414U SO FAIRING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HC5321 FOUND CARGO COMPT PRESSURIZE FAIRING FORMER CRACKED AT FS 477, WL284, RB L16.5. REPAIRED BY FABRICATING AND INSTALLING FORMER IAW SMP583 CHAP 51-60, 51-70, AND DWG 340042. 2 H 7 4 4T A1SO 20080929 EU 2008 9 29 08FDEA03412 1 20080814 A 5310 A53611192204 WINDOW FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND ON FUSELAGE NOSE SECTION, WINDSHIELD FRAME LT, C 2-7 AN OLD REPAIR (DEVIATED RIVETS INSTALLED). REPAIR PERFORME D BY REMOVING EXISTING REPAIR, OVERSIZE THE HOLES AND INSTALL RIVETS IAW RAS/70512490/028/2008 AND EA 6-5311-123044. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03413 1 20080814 A 5730 A57247030 PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND DELAMINATION ON RT OUTER SHROUD BOX TOP SKIN HONEYCOMB REPAIR PERFORMED BY IAW SRM 51-77-12 AND RAS/BAE/1007735/20 08 ISS A, APPROVED BY EA 6-5751-123040. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03414 1 20080814 A 5315 A53974224220 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND DOUBLE HOLE AT CROSSBEAM C 68, Y-525, AFT CARGO COMPARTMENT. SPLICE REPAIR OF CROSSBEAM PERFORMED IAW SRM 53-10-1 5 FIG 207. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03415 1 20080814 A 5315 A53974268200 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSION ON CROSS BEAM C 58 IN AFT CARGO COMPARTMENT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080929 SO 2008 9 29 LR7A08111 1 20080819 A 3010 3517833L EJECTOR LKHEED 382 382G 526414U SO CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HC5711 FOUND ANTI-ICE EJECTOR LOCKHEED P/N 351783-3L CRACKED. REPAIRED BY WELD ING IAW LAC MEA 382-30-08-042 R1. 2 H 7 4 4T A1SO 20080929 SO 2008 9 29 LR7A08112 1 20080819 A 2120 3419921 DUCT LKHEED 382 382G 526414U SO CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HC2111 FOUND CABIN AIR REDISTRIBUTION DUCT P/N 341992-1 CRACKED. REPAIRED BY W ELDING IAW LAC MEA 382-21-08-047 R1. 2 H 7 4 4T A1SO 20080929 EU 2008 9 29 08FDEA03263 1 20080805 A 5730 A57843103206 SKIN AIRBUS 310 A310324 3930206 EU NR 1 SLAT DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 812FD 467 DENT IN RT NR 1 LEADING EDGE SLAT, DENT MEASURES 4 INCH LONG BETWEEN RIBS 7 AND 8, 35 INCHES FROM INBD EDGE, 5 1/2 INCHE S BELOW PAINTED SURFACE, AND 5/32 INCH DEEP. REMOVED DAMAGE AND REPAIRED DENT ON RT NR 1 LEADING EDGE SLAT BETWEEN RIBS 7 AND 8, 35 INCH FROM INBD EDGE, 5 1/2 INCHES BELOW PAINTED SURFACE IAW A310-300 SRM 57-40-00-FIG 206. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03287 1 20080806 A 5321 B5327027801800 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DOOR PANEL NR 252 UH, IS CRACKED AND CRUSHED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG S RZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03822 1 20080911 A 5321 A2551027600100 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CONTAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 MAIN WHEEL WELL FLOOR PANEL 147 AF IS DELAMINATED AND SOAKED WITH HYDRAULIC FLUID. FABRICATED A NEW PANEL IAW DWG SRZ 2 5-005; REV "G". PART MARKED IAW GMM 7- 0-1000. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03840 1 20080911 A 5330 A5361063323200 SKIN PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 EXTERNAL FUSELAGE SKIN HAS EVIDENCE OF LIGHTNING STRIKE AT FRAME 13 A; STRINGERS 20 R TO 21 R, (JUST FWD OF THE L-1 DOOR ). COMPLIED WITH THE PERMANENT LIGHTNING STRIKE REPAIR PAE SRM 53-10-12; FIG 203; SHEET 1. 2 L 7 2 4F RT A35EU 20080926 WP 2008 9 26 08FDEA03841 1 20080911 A 5347 AWJ73221 TIE ROD DOUG MD10 MD1010F 3022112 WP ZONE 100 BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 CENTER PIT CARGO SYSTEM HAS 2 BROKEN TIE ROD SUPPORTS AT STA 1765, (P/N AWJ 7322-1). REMOVED AND REPLACED P/N AWJ 7322- 1 (2) IAW SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 20080926 EU 2008 9 26 08FDEA03843 1 20080911 A 5330 A5387000120000 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 EXTERNAL UPPER FUSELAGE SKIN HAS STATIC DISCHARGE AT FRAME 44, STRINGER 1. REMOVED AND REPLACED STRINGER 2 R. REMOVED AND REPLACED RIVET IAW SRM 53-10-12, FIG 220. ACCOMPLISHED A BHEC INSPECTION OF THE FASTENER HOLE IAW NTM PT6 51-10-01. 2 L 7 2 4F RT A35EU 20080926 WP 2008 9 26 08FDEA02266 1 20080614 A 5347 NDA6022 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 MAIN CABIN EXFOLIATION CORROSION ON SEAT TRACK. REPAIR AREA IAW SRM 53-70-00 FIG 1 VOL 1. 2 L 7 3 4F A22WE 20080929 NM 2008 9 29 2008UALA05717 1 20080913 A 5300 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1400 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 FRAME DENTED AFT PIT BS 1400 STR 26L-25L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080929 NM 2008 9 29 2008UALA05825 1 20080920 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 1E UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 777UA 26916 SEAT 1E EMERGENCY LIGHT FELL OFF, CREW TAPED COVER AT FC GALLEY WALL. FOUND LIGHT OUT OF POSITION. SECURED ASSEMBLY. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080929 EU 2008 9 29 08FDEA03261 1 20080805 A 5315 A53778807202 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSION ON UPPER FLANGE AT C 27 RT OUT OF LIMIT. TOP CAP BEAM REPAIR PERFORMED IAW SRM 53-10-15 FIG 207. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03262 1 20080805 A 5330 LAP JOINT AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND OLD BUSH REPAIR IN LAP JOINT, C 38, P 43 RT WITHOUT ANY DOCUMENTATION. LAP JOINT REPAIR PERFORMED IAW SRM 53-10-12 FIG 217 AND NEW STRAP INSTALLED IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080929 NM 2008 9 29 08FDEA03518 1 20080820 A 5313 A6A7112511 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 TWO CRACKS FOUND DURING X-RAY INSPECTION AT STA 6-100, LONGERON 2R SPLICE. CRACK LENGTH APPROXIMATELY 1 INCH, AT STA 6- 100, LONGERON 2R CRACKED STRINGER SPLICE REMOVED AND REPLACED AS PER SRM 51-21-01 VOLUME II. NEW SPLICE FABRICATED AS PER DWG A6A7112. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080929 NM 2008 9 29 08FDEA03521 1 20080820 A 5320 6517510120 WEB BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 AFT AIRSTAIR, LEFT LOWER TORQUE BOX WEB HAS DAMAGED AREA ON PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2 , TRIMMED OUT AREA DIMS 1 1/4 INCH BY 3/4 INCH IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 6 AND 51- 40-2 FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1. 2 L 7 3 4F RT A3WE 20080929 NM 2008 9 29 08FDEA03400 1 20080813 A 5315 6517593132 FLOORBEAM BOEING 727 7272S2F 1384O81 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 MAIN DECK FLOORBEAM INTERCOSTAL MID CHORD EXISTING REPAIR DOUBLER IS CRACKED BS 302, WL 207 FABRICATED NEW REPAIR ANGLE REF SRM 51-40-3 PG 1. TREATED AND PRIMED REF SRM 51-10-2 PG 1-9. INSTALLED ANGLE REF SRM 51-30-2 PGS 1-7. THIS IS CLA SSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080929 NM 2008 9 29 08FDEA03402 1 20080813 A 5320 6516317251 FRAME BOEING 727 7272S2F 1384O81 NM WING TO BODY FRG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 LWR EXT FUSE BODY FRAME LWR CHORD IS CORRODED BS 351, LBL 17, WL 148-150. REMOVED CORROSION AT LWR EXT FUSE BODY FRAME LWR CHORD STA 351 LBL 17 - RBL 17, REF SRM 51-10-6 PG 1-5. MATERIAL LOSS 50 PERCENT, FOUND OUT OF LIMITS REF SRM 53-10- 1 FIG 1. REMOVED AND REPLACED LWR CHORD (TEE ANGLE) REF BOEING DWR 65-16317, SRM 51-30-5 PG 1, 51-30-2 PG 2-5. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080929 NM 2008 9 29 08FDEA03403 1 20080813 A 3610 65801552 DUCT BOEING 727 7272S2F 1384O81 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 RT EXT FUSE NR 3 ENG FAN AIR EXH PORT ASSY IS FRETTED/CRACKED. REMOVED AND REPLACED FAN AIR EXH POT ASSY REF SRM 51-30- 2 PG 1-32, REF MM 51-20-151-7 PG 1-5, REF MM 36-00-001-2 PG 1-4. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080929 WP 2008 9 29 08FDEA03903 1 20080916 A 5347 6045007075T65 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 571FE 47830 UPPER CARGO COMPARTMENT SEAT TRACK 107L, FS 1175L HAS SEAT TRACK LOBE BROKEN OFF. REMOVED AND REINSTALLED FLOOR PANEL, REMOVED AND REPLACED SEAT TRACK FAB NEW TRACK AND SPLICES ON MAE TRAVELERS T8/758247, T8/758229, SRM 53-21-08-2, 53-70-0 0 FIG 1. MAJOR REPAIR RII RDR AND SDR. 2 L 7 3 4F RT A22WE 20080929 EU 2008 9 29 08FDEA03938 1 20080918 A 5347 A5327400520000 SEAT TRACK AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 808FD 439 MDCC SEAT TRACK 4R CORRODED 2 AREAS FRAME 42 AND 44 4 SQ INCH. REMOVED LEVEL 1 CORROSION. REMOVED AND REPLACED SEAT TR ACK FROM FR 40 TO 44.5 RT AT Y-1456 IAW SRM 53-10-16 FIGURE 203 SHEET 5. 2 L 7 2 4F RT A35EU 20080930 NM 2008 9 30 UPS08M53142 1 20080811 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 11 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED BUSH ING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080930 NM 2008 9 30 UPS08M53150 1 20080812 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 20 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080930 NM 2008 9 30 UPS08M53151 1 20080816 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 21 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080930 NM 2008 9 30 UPS08M53153 1 20080814 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 32 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080930 NM 2008 9 30 UPS08M53159 1 20080812 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 11 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REP AIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080930 NM 2008 9 30 UPS08M53160 1 20080816 A 5712 RIB DOUG MD11 MD11F 3023600 NM LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C LT WING FIXED L/E SUPPORT RIB FOUND CRACKED AT SING STA XORS 683. REMOVED, FABRICATED, AND INSTALLED RIB IAW MD-11 SRM 51-33-01, DWG ARB3954, AND MD-11 SRM 51-21-01. 2 L 7 3 4F RT A22WE 20080930 NM 2008 9 30 UPS08M53161 1 20080816 A 5740 BRACKET DOUG MD11 MD11F 3023600 NM LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C LT WING L/E COMP ACCESS DOOR 518FB O/B SUPPORT BRACKET CRACKED. REMOVED, FABRICATED, AND INSTALLED B RACKET IAW DWG 2918, MD-11 SRM 51-35-01, 51-33-01. 2 L 7 3 4F RT A22WE 20080930 NM 2008 9 30 2008UALA04344 1 20080819 A 3510 GASKET AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE OXYGEN MASK CRUSHED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 823UA 952 O2 LEAK. 70 PSI LOSS IN 30 MIN. FOUND CRUSHED GASKET LEAKING, AT CAPT O2 MASK. REPLACED CRUSHED GASKET AT CAPTAINS O 2 MASK, ALL LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 CALA0800803 1 20080821 A 5510 65C251568 FITTING BOEING 737 737524 1384721 NM HORIZONTAL STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 STATION 482 S16R TIE-CLIP CRACKED. REMOVED AND REPLACED TIE CLIP AT STATION 482 S16R REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800809 1 20080822 A 5311 6546540 FRAME BOEING 737 737524 1384721 NM BS 747 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 BODY STATION 747 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN S8L AND S9L. REPAIRED CRACKED FRAME AT STATION 747 LEFT SIDE AT AC BRACKET BETWEEN STR 8 AND STR 9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800816 1 20080822 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM BS 827 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 BODY STATION 827 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REPAIRED CRACKED FRAME A T STATION 827 LEFT AT AC BRACKET BETWEEN STR 8 AND 9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800819 1 20080822 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 787 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 BODY STATION 787 RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REMOVED CRACK AND INSTA LLED REPAIR ANGLES PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800821 1 20080823 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM BS 867 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14628 27532 RIGHT FRAME IS CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 867 BETWEEN STR 8 AND STR 9. REP AIRED RIGHT FRAME AT STATION 867 BETWEEN STR 8 AND STR 9 PER EA 5310-04498 OP2. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800826 1 20080824 A 5310 65C33503 DOOR FRAME BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 R-2 DOOR AFT FRAME WEB CORRODED OUT OF LIMITS PER SRM 51-10-02. FABRICATED PARTS PER BAC DRWG65C33583, REMOVED AND REPL ACED FRAME SECTION IAW 51-10-02. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800827 1 20080824 A 5310 6546566 DOOR FRAME BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 R2 DOOR AFT FRAME CORRODED AT STR 17R BETWEEN ATTACH CLIP AND FRAME. REPAIRED R2 DOOR AFT FRAME AT STR 17R BETWEEN ATTA CH CLIP AND FRAME PER BOEING DWG 65-46566, B737 SRM 51-70-11 AND B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800828 1 20080825 A 5510 BRACKET BOEING 737 737524 1384721 NM HORIZONTAL STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14628 27532 HORIZONTAL STABILIZER CENTER SECTION TRUSS STRUCTURE HAS A CRACKED BRACKET AT APPROXIMATELY STATION 1121 LEFT SIDE CENTE R. REMOVED AND REPLACED CRACKED FITTING ON HORIZONTAL STABILIZER CENTER SECTION TRUSS AT APPROXIMATELY STATION 1121 LEF T SIDE CENTER IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800829 1 20080825 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM BS 440 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14628 27532 LEFT FRAME CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 440 BETWEEN STRINGERS 8 AND 9. REPAI RED FRAME PER EA 5310-04498, OP 02. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800831 1 20080825 A 5311 6546650 FRAME BOEING 737 737524 1384721 NM BS 787 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14628 27532 LEFT FUSELAGE FRAME STATION 787 IS CRACKED BETWEEN STRINGERS 8L AND 9L. REPAIRED FRAME PER EA 5310-04498 OP 2. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 2008UALA04126 1 20080803 A 3350 362624 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 349UA 24253 EEL LIGHT INOP AT ROW 18. *S/D* REPLACED LAMP, OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 20080930 NM 2008 9 30 2008UALA04129 1 20080805 A 3397 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EEL INOP: SEAT 3A AFT SECTION. *S/D* SECURED CONNECTOR. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04131 1 20080805 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY LIGHT INOP: CEILING AT 44 LT. RELAMPED, OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 EU 2008 9 30 2008UALA04143 1 20080805 A 5330 PANEL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 408UA 457 CORROSION AT CUTOUT FOR AFT LAV SERVICE PANEL ON LWR AFT FUSELAGE. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR DOUBLER . 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA04179 1 20080808 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 SEAT 43ABC EMERGENCY LIGHT IS INOP. RELAMPED, CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04182 1 20080808 A 3350 20131A CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 LEFT OVERWING FWD TWO EMERGENCY LIGHT IS INOP. REPLACED EMERGENCY LIGHT BATTERY CHARGER UNIT. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04183 1 20080808 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 RT FWD OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED, OP CHECKED OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04184 1 20080808 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EEL'S INOP, SEAT ROW 28L, 47R, LAV 116 SIDEWALL. RELAMPED ALL; OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04185 1 20080808 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY EXIT LIGHT INOP, DOOR 2L. REPLACED BATTERY PACK, OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04190 1 20080809 A 5320 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 814UA 862 DOOR SILL 2R CORRODED (MARKED). REMOVED SILL PAN. PICKED UP HOLES IN NEW SILL PAN & INSTALLED CLIPS. INSTALLED SILL P AN. INSTALLED ALL FASTENERS THROUGHT EXTERNAL SKIN & FRAME STA 67. INSTALLED REST OF FASTENERS & SPLICE. INSTALLED FA STENERS AT LWR & AFT SIDE 2R SEAL PLATES. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA04195 1 20080808 A 2130 1305027 CONTROL PANEL BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE COCKPIT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 666UA 29238 UNABLE TO SET ALTITUDE IN CABIN ALTITUDE CONTROL. REMOVED & REPLACED CABIN ALTITUDE CONTROL PANEL. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA04198 1 20080809 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 803UA 748 DENT - CREASE LT SIDE OF FUSELAGE FR 26 BETWEEN STRINGERS 39L & 38L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGE. FABRI CATED & INSTALLED EXTERNAL DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 20080924 NM 2008 9 24 08FDEA03630 1 20080828 A 5320 7075T60063 CHANNEL BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 LT FUSELAGE PANEL 197EL CENTER SUPPORT FRAME CHANNEL FACE HAS CORROSION. CORROSION FOUND EXCEEDED ALLOWABLE SRM LIMITS. CHANNEL REMOVED AND REPLACED IAW B757-200 SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA . 2 L 7 2 4F RT A2NM 20080925 WP 2008 9 25 08FDEA03924 1 20080917 A 5522 SKIN DOUG MD10 MD1010F 3022112 WP LT ELEVATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT STAB DROOP ELEVATOR LOWER SURFACE IS CRACKED. CHECKED THE LIMITS ON THE DENT. DEEPEST POINT 0.065 IAW DEPTH GAUGE T8492C DUE 10-25-08 AND FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 51-80-01; VOL II; NOTE K. CUT OUT DAMAGE IAW DC/MD- 10 SRM 55-10-00; VOL I. MATERIAL ID FOR THE REPAIR DOUBLER 2024-T3, 0.040 IAW DC/MD-10 SRM 55-10-00; VOL I. FABRICATED THE REPAIR DOUBLER IAW DC/MD-10 SRM 55-10-00; VOL I. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-01; VOL II. INSTALLED THE REPAIR DOUBLER IAW DC/MD-10 SRM 55-10-00; VOL I. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03926 1 20080917 A 5347 53FX939500 SEAT TRACK BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 CORROSION ON TOP OF SEAT TRACK ATTACH FLANGE, FS 1140-1173, RBL1, WL 208. REMOVED CORROSION, NDT VERIFIED MATERIAL LOSS AND DEFECTS, NO DEFECTS FOUND. ORIGINAL THICKNESS .190, .175 REMAINING, MATERIAL LOSS .015 WITHIN LIMITS REF EA 7-5310 -11403. TREATED AND PRIMED AREA REF SRM 53-10-02. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080925 NM 2008 9 25 08FDEA03927 1 20080917 A 5347 53X939500 SEAT TRACK BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 CORROSION ON SEAT TRACK ATTACH FLANGE, FS 1171 TO 1162, LBL 1, WL 208 REMOVED CORROSION, NDT VERIFIED MATERIAL LOSS AND CHECK FOR DEFECTS. NO DEFECTS WERE FOUND, ORIGINAL THICKNESS .190 INCH, REMAINING .174 INCH, MATERIAL LOSS .016 WITHIN LIMITS, REF EA 7-5310-144031. TREATED AND PRIMED AREA REF SRM 51-10-02. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080925 EU 2008 9 25 08FDEA03953 1 20080919 A 5347 A5383202020400 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 663FE 766 MDCC SEAT TRACK CORRODED AT NR 3RT BETWEEN FRAME 41 AND FRAME 43, 4 SQ INCHES REMOVED LEVEL 1 CORROSION AND REMOVED AND REPLACED SEAT TRACK SECTION AT TRACK NR 3 RT, BETWEEN FR 40 AND FR44.5 IAW A300-600 SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080925 SO 2008 9 25 SWIA200820024 1 20080816 A 3080 SENSOR EMB 120 EMB120ER 3260203 SO ICE PROTECTION BURNED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 297SW 120327 ICE PROTECTION CURRENT SENSOR ASSEMBLY CHARRED AND DETERIORATED. C-CHECK, REPLACED LEFT ICE PROTECTION CURRENT SENSOR. 2 L 7 2 4T RT A31SO 20080925 WP 2008 9 25 08FDEA03815 1 20080911 A 5730 NRC6060 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 RT WING INBD FLAP FOUND DEEP DENT ON LOWER SKIN 0.25 INCH BY 0.25 INCH DEEP .066 INCH (SUSPECT CRACK ). REPAIRED DENT I AW SRM 57-00-01 FIG 4 SHT 2 VOL I. 2 L 7 3 4F RT A22WE 20080926 NM 2008 9 26 08FDEA03256 1 20080805 A 3297 CONNECTOR BOEING 727 727233 138408A NM LT MLG DAMAGED A FDEA O OTHER S J AFFECT SYSTEMS WARNING INDICATION CR CRUISE 1 CE 21 276FE 22041 DURING CRUISE AT FL 350 THE RUDDER LOAD LIMITER LIGHT AND BOTH THE RED AND GREEN LEFT GEAR LIGHTS ILLUMINATED AT THE SAM E TIME. DURING THE DESCENT THE RED AND GREEN LEFT GEAR LIGHTS ILLUMINATED INTERMITTENTLY WHILE THE RUDDER LOAD LIMITE R REMAINED ILLUMINATED. UPON LOWERING THE GEAR HANDLE THE LEFT GEAR RED LIGHT ILLUMINATED AND THE GREEN LIGHT EXTINGUI SHED. REMOVED AND REPLACED CONNECTOR D4658P DUE TO SEVERAL BENT PINS IAW WDM 32-64- 01, 27-22-01, 27-51-11 AND WIRE HO OKUP LIST. PERFORMED OPS CHECK OF RUDDER LOAD LIMIT, REF WRI 27-21/0031. OPS CHECK OF LT MLG DOWNLOCK SENSOR ACCOMPL ISHED. ALL GEAR INDICATIONS WERE NORMAL, REF WDM 32-64-01, MM 32-61-091-4. 2 L 7 3 4F RT A3WE 20080929 NM 2008 9 29 UPS08553303 1 20080905 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 520 S7R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 FRAME DENTED BS 520, 4 INCHES ABOVE STR 7R. REPAIRED FRAME PER SRM 53-00-07-2R FIG 201. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 2008UALA05700 1 20080913 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT LIGHT INOP AT SEAT 56 HJK. FOUND LAMP INOPERATIVE. REPLACED LAMP. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 NM 2008 9 29 SWAA085066 1 20080914 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 500A S28L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080929 NM 2008 9 29 2008UALA05715 1 20080913 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1580 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 AFT PIT STA 1580, STR 25L, FRAME DENTED INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION AND INSTALL ED DOUBLER FRAME REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080929 NM 2008 9 29 2008UALA05830 1 20080921 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT LIGHT INOP. AT CEILING ROW 43 LEFT. LAMP FOUND INOP. REPLACED LAMP. OPS CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 NM 2008 9 29 2008UALA05831 1 20080921 A 3350 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT SIGN INOP. JUST FWD OF DOOR 4 LEFT. REPLACED FEEDER CABLE. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 EU 2008 9 29 2008UALA05836 1 20080921 A 5220 MECHANISM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY EXIT JAMMED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 405UA 452 LEFT OVERWING EXIT IS NOT ARMED. FOUND DEBRIS IN MECHANISM. UNJAMMED OVERWING EXIT DOOR ARMED IND MECHANISM. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA04202 1 20080811 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 814UA 862 FLOORBEAM 140 CORRODED (MARKED). COMPLETED BEAM ASSY. PAINTED FLOORBEAM & INSTALLED BOLTS. INSTALLED FLOORBEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA04203 1 20080811 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 814UA 862 FLOORBEAM 145 CORRODED (MARKED). ASSEMBLED FLOORBEAM. INSTALLED BOLTS AND PAINTED. INSTALLED FASTENERS TO COMPLETE FL OORBEAM AND PAINTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA04224 1 20080809 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY LIGHT SEAT 5F AFT INOP. RELAMPED, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04232 1 20080809 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY LIGHT INOP, D-ZONE AFT END RT AISLE. REPLACED BATTERY PACK, OP CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04234 1 20080810 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT EMERGENCY LIGHT INOP AT DOOR 4 LEFT GALLEY LOWER FWD WALL EMERGENCY LIGHT. REPLACED LIGHT ASSY, OPS CHEC K NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04237 1 20080810 A 3350 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT LIGHT INOP FROM SEATS 45 THRU 53 LEFT. REPLACED POWER FEEDER CABLE. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04246 1 20080811 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 803UA 748 DENT AND SCRATCH BEHIND NOSE GEAR AND JUST ABOVE YELLOW ANT. UNDER ACCESS DOOR. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA04255 1 20080812 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 SEAT 47 HJK EMERGENCY LIGHT INOP. RELAMPED, CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04277 1 20080814 A 4900 263BA1011263BC10 BATTERY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 214UA 30220 APU BATTERY FOUND DEAD. REPLACED BATTERY & BATTERY CHARGER. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080930 2008 9 30 2008UALA04343 4 20080819 A 2565 MR25611 SLIDE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R1 DOOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 805UA 783 THE 'ESPU EXT LOAD FWD L' FAULT DISPLAYED ON PTP DISPLAY DURING EMERGENCY LIGHTING TEST. ISOLATED FAULT TO DOOR 1R ESCA PE SLIDE. INSTALLED NEW SLIDE PACK (MR25611) AT DOOR 1R. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 2008 9 30 2008UALA05416 4 20080822 A 2300 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY CALL UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 408UA 457 CABIN EMERGENCY CALL GOING OFF BY ITSELF. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA05420 1 20080822 A 5210 CYLINDER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L2 DOOR INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 L-2 DOOR MANUAL DEPLOY GAS CYLINDER INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA05431 1 20080823 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ROW 1L INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 ROW 1 LT EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT, OPS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA05436 1 20080823 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 LT MID LAV EMERGENCY LIGHT INOPERATIVE, CROSS AISLE EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 20080929 NM 2008 9 29 2008UALA05838 1 20080921 A 2731 HOUSING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SAM MODULE CRACKED A UALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 29 543UA 25698 ELEV ASYM AND STAB TRIM EICAS MESSAGE ON LOWER EICAS ON TAKEOFF, REPEAT GRIPE. FOUND L SAM MODULE BAD, FOUND HOUSING BO DY CORRODED AND CRACKED 360 DEGREES AROUND. REPLACED SAM MODULE, REPLACED ELEVATOR ASSYMETRY ACTUATOR, PERFORMED ELEVAT OR ASYM TEST 85625 -GOOD STAB TRIM MODULE M524 OPS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080929 NM 2008 9 29 2008UALA05839 1 20080922 A 5320 CHANNEL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 480, S10R CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 BS 480, STR 10R CRACKED IN CHANNEL AT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED PER S/B 747-53-A2484 FIG 18. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 NM 2008 9 29 2008UALA05841 1 20080922 A 3350 78961 COVER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 776UA 26937 EMERGENCY LIGHT DAMAGED AT SEAT 9D. REPLACED LIGHT COVER AT 9D. OPS CHECK OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080929 NM 2008 9 29 2008UALA05842 1 20080918 A 5730 113T161332 PANEL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT WING SPLIT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 RT WING LOWER PANEL 651VB (REAR OF LDG GEAR) HAS 5.5 INCH SPLIT IN FWD EDGE. REPAIRED T/E PANEL ON R&R. COMPLETED GEAR SWINGS FOR ADEQUATE CLEARANCE BTWN RIGHT GEAR FIXED STRUT DOOR & LWR WING PANEL. 2 L 7 2 4F 4 F RT A1NM E24NE 20080929 NM 2008 9 29 2008UALA05843 1 20080922 A 2910 LINE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HYD SYSTEM DAMAGED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 774UA 26936 HYDRAULIC PRESSURE PROBLEM, RTFL. FOUND CENTER HYD SYSTEM RETURN LINE AT STA 16 DAMAGED IN AFT CARGO PIT FROM APU BLEED AIR DUCT FAILURE. REPAIRED HYD LINE AT STA 16 IN AFT PIT. LEAK CK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080929 NM 2008 9 29 DL75A081212 1 20080920 A 2131 CONTROLLER BOEING 757 757212 1384951 NM CABIN PRESSURE MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 751AT 23125 ON TAXI OUT BOTH CABIN MODE ALT SELECTS AUTO INOP. RTB. BOTH SHOWED AC MOTOR RESET RAN VERIFY CKS GOOD MSG ERASED, NO HISTORY. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 DL764081214 1 20080922 A 5312 BULKHEAD BOEING 767 767432ER 1385134 NM BS 955 LBL 90 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 841MH 29714 DURING AN INSPECTION DURING HMV AT HAECO CORROSION WAS FOUND ON THE BS 955 BULKHEAD WEB AT LBL 90. THE CORROSION WAS RE MOVED WITH A 3 INCH BY 10 INCH CUTOUT AND A DOUBLER INSTALLED PER ER/A 467812-14. 2 L 7 2 4F RT A1NM 20080929 WP 2008 9 29 08FDEA04020 1 20080924 A 5340 FITTING DOUG MD10 MD1010F 3022112 WP DOOR FRAME CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 MAIN CARGO DOOR LOWER JAMB FITTING AT SPOOL LOCATION NR 4 HAS A CRACK INDICATION AT HOLE C. 2 L 7 3 4F RT A22WE 20080929 WP 2008 9 29 08FDEA04021 1 20080924 A 5340 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP DOOR FRAME CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 MAIN CARGO DOOR LOWER JAMB FITTING AT SPOOL LOCATION NR 7 HAS CRACK INDICATIONS AT HOLES B AND D. REMOVED & REPLACED FI TTING IN REF TO SRM 51-33-01. REPAIRED UPPER BEAM IN REF TO SRM 53-50-00. 2 L 7 3 4F RT A22WE 20080929 EU 2008 9 29 08FDEA04022 1 20080924 A 5311 A5377365100000 FRAME AIRBUS 310 A310222 3930315 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 FWD PIT, FRAME 33 LEFT HAS CORROSION UNDER THE OUTBD ROLLER TRAY AT THE FRAME. REMOVED ROLLER TRAY & TRANSITION PANEL I AW SRM 51-40-21. REMOVED CORROSION FROM CROSS BEAM IAW SRM 51-74-10. AREA FOUND TO BE OUT OF LIMITS IAW SRM 51-74-01. FABRICATED A CROSS BEAM SECTION IAW SRM 53-10-15 & DWG A53773651. ALODINED IAW SRM 51-21-10. PRIMED & PAINTED IAW SR M 51-23-10. INSTALLED ROLLER TRAY & TRANSITIONAL IAW AMM 25-52-21-4. 2 L 7 2 4F RT A35EU 20080929 NM 2008 9 29 08FDEA04023 1 20080924 A 5310 70750063B CREASE BEAM BOEING 757 75723A 1384967 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 FR-1020, CREASE BEAM WEB CORRODED, FWD SIDE OF FR-1020 REMOVED AND REPLACED WEB AND ANGLE IAW SRM 51-40-02, MAJOR REPAIR . 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 08FDEA04028 1 20080925 A 5320 AEA0526U2 DOUBLER DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 CENTER LANDING GEAR WHEEL WELL, FOUND FORWARD RIGHT LOWER CORNER DOUBLER CRACKED. CRACKED DOUBLER REMOVED AND REPLACE D AS PER SRM 51-35-01 AND SRM 51-33-01. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080929 EU 2008 9 29 08FDEA04029 1 20080925 A 5730 A57247017245 PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 600 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND DELAMINATION ON RT OUTBOARD TRAILING EDGE PANEL REPAIR PERFORMED IAW SRM 57-51-12 PAGE 201 PARA 4, FIG 216, APPROV ED BY RAS/1007710/2008 ISS A AND EA 6-5751-123095. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA04030 1 20080925 A 5310 A53610131 WINDOW FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORRODED FASTENER HOLES IN WINDSHIELD FRAME. REPAIR PERFORMED BY REAM UP THE CORRODED HOLES, NDT FOR CORROSION FR EE CONDITION AND INSTALL FASTENER IAW RAS/70512884/015/2008 ISS A, APPROVED BY EA 6-5311-123131. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA04032 1 20080925 A 5540 A55471556257 PLATE AIRBUS 300 A300B4622R 3930312 EU ZONE 300 CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND ON RUDDER RT SIDE THE LIGHTNING PROTECTION PLATE CORRODED. REPAIR PERFORMED BY REPLACEMENT OF LIGHTNING PROTECTIO N PLATE IAW RAS/DAHAM/4025347/2008 ISS A, APPROVED BY EA 6-5541-123055. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA04033 1 20080925 A 5542 SKIN AIRBUS 300 A300B4622R 3930312 EU RUDDER DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND ON RUDDER RT SIDE NEAR RIB 0 FLUID INGRESS (4 AREAS) WITH DEBONDING. REPAIR PERFORMED BY BONDING REPAIRS IAW RAS/ DAHAM/4025347/2008 ISS A, APPROVED BY EA 6-5541-123055. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA04035 1 20080925 A 5330 A53812189200 SKIN PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSION ON FUSELAGE SKIN , C39-40, P 27-28 LT AT KRUEGER FLAP AREA. REPAIR PERFORMED BY REPLACEMENT OF SKIN PAN EL IAW RAS/70512709/008/2008, APPROVED BY EA 6-5315-123058. 2 L 7 2 4F RT A35EU 20080929 NM 2008 9 29 08FDEA04038 1 20080925 A 5711 651928874 FRAME BOEING 727 727227 1384078 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 RT WING, I/B AILERON LOWER T/E PANEL FRAME CRACKED WITH MISSING ATTACH FASTENER AT AFT END OF FRAME 10 INCH O/B FROM I/B END OF AILERON REMOVED DAMAGED PANEL FRAME REF SRM 51-30-2. VERIFIED MATERIAL OF FRAME TO BE BAC1506-1625 7075-T6. FABRICATED REPLACEMENT FRAME REF DWG 65-19288. TREATED AND PRIMED FRAME REF SRM 51-10-2. INSTALLED FRAME REF SRM 51-30 -2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080929 NM 2008 9 29 DLM88081216 1 20080831 A 5330 DOUBLER DOUG MD88 MD88 3023688 NM STA 1470 S29-30R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 948DL 49879 LOWER EXTERNAL FUSELAGE AT FS 1470 VHF ANT MOUNT HAS CORROSION BETWEEN 29R AND 30. REPLACED DOUBLER. 2 L 7 2 4F RT A6WE 20080929 NM 2008 9 29 DL757081221 1 20080824 A 5220 STRUCTURE BOEING 757 757232 1384965 NM EMERGENCY EXIT DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 LT FWD OVERWING EMERGENCY ESCAPE HATCH DOOR LWR RT SIDE EDGE DENTED. REFORMED AREA AT LT FWD OVERWING ESCAPE HATCH DOOR LWR RT SIDE IAW SRM 51-30-01. 2 L 7 2 4F RT A2NM 20080929 EU 2008 9 29 08FDEA04005 1 20080923 A 5347 R538D1042200 SEAT TRACK AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 808FD 439 MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE HAS SCRATCH AT FR 40 LT, BELOW FLOOR PANEL 231QH, AFT SIDE REMOVED DAMAGED S EAT TRACK AND FABRICATED AND INSTALLED REPLACEMENT TRACK AT TRACK NR 4LT BETWEEN FR 40 AND FR 45 IAW AIRBUS DRAWING A538 11923 AND A310-300 SRM 51-40-21. ADJACENT DUMMY TRACK P/N Y53829790200 AND CROSS BEAM P/N A5381316820000 WERE ALSO REPL ACED DUE TO DAMAGED. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA04012 1 20080924 A 2700 UNKNOWN AIRBUS 300 A300F4605R 3930327 EU UNKNOWN A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CE 21 654FE 738 RUDDER TRIM WOULD NOT OPERATE, NOTICED DURING CRUISE FLIGHT, INOP WITH A/P ON AND OFF. DEBRIEFED FLIGHT CREW IN DETAIL . IN CRUISE FLIGHT, WITH AUTO PILOT IN COMMAND THEY NOTICED THEY COULD NOT GET THE RUDDER TRIM TO OPERATE, NO FAULTS ON PANEL OR ECAM, INDICATIONS NORMAL. PERFORMED GROUND SCANS, AUTOPILOT FUNCTION TESTS WITH HYDRO POWER RUNNING RUDDER T RIM FULL SCALE 22DEG /- WITH AUTO RECENTERING. PERFORMED FULL SCALE AIL TRIM WITH NORMAL INDICATIONS NO FAULTS NOTED O N CONTROL PANEL. ALL TESTS AND CHECKS ON GROUND NORMAL A/P SYSTEM NORMAL CHECKS. SUSPECT CREW ERROR IN TRIM OPERATION S WITH A/P'S IN COMMAND MODE. SYSTEM OK TO RETURN TO SERVICE, NO CHANGE TO CAT STATUS OR RVSM. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA04013 1 20080924 A 5330 A53772016200 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 426FE 245 LOWER FUSELAGE LT FR 18 TO FR 23 BETWEEN STR 37 AND STR 39 HAS 6 LIGHTNING STRIKES. REWORKED LIGHTNING STRIKES IAW SR M 51-40-21, 51-10-30, AND 51-10-10. TREATED AND PRIMED IAW 51-21-10, PAINTED IAW MM 51-75-10. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA04014 1 20080924 A 5330 A53772519200 SKIN AIRBUS 310 A310203 3930313 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 426FE 245 LOWER FUSELAGE FWD CARGO DOOR CUTOUT FWD LOWER EDGE BELOW REPAIR DOUBLER HAS SKIN GOUGES 5 INCH LONG. BLENDED AREA FOUN D TO BE WITH IN LIMITS IAW SRM 53-10-12, AND 51-73-10 FIG 201. TREATED, PRIMED AND PAINTED IAW SRM 51-21-10, AND MM 51- 75-10-8. 2 L 7 2 4F RT A35EU 20080929 NM 2008 9 29 08FDEA04015 1 20080924 A 7711 JG298A4 TRANSMITTER BOEING 727 727277 138408S NM EPR MALFUNCTIONED A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 21 246FE 22068 WITH T/O PWR SET ENGINE NR 3 N1 WAS 87 PECENT WITH EPR SET AT STD PWR 2.12, DEFERED EPR INDICATION. REMOVED AND REPLACE D THE EPR TRANSMITTER. 2 L 7 3 4F RT A3WE 20080929 WP 2008 9 29 08FDEA04017 1 20080924 A 5320 ADA39473 INTERCOSTAL DOUG MD10 MD1010F 3022112 WP BS 910 L43R CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 FWD LOWER CARGO LONGERON 43R INTERCOSTAL AT STA 910 IS CRACKED. REPAIRED INTERCOSTAL, LONGERON 43 RT IAW SRM 53-00-01. 2 L 7 3 4F RT A22WE 20080929 EU 2008 9 29 08FDEA03283 1 20080806 A 5321 B5327028000800 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DOOR PANEL NR 252 VF; IS CRACKED AND PUNCTURED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03936 1 20080918 A 5347 R5307008820000 SEAT TRACK AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 808FD 439 MDCC SEAT TRACK NR 1 CORRODED AT FRAME 71 2 SQ IN REMOVED LEVEL 1 CORROSION. REMOVED AND REPLACED SEAT TRACK SECTION AT FR71 TO 74 AND INSTALLED NEW SECTION IAW SRM 53-10-16 FIG 208 SHEET 1, PG 247/248. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03937 1 20080918 A 5315 B53774171200 FLOORBEAM AIRBUS 310 A310324 3930206 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 808FD 439 MDCC FLOOR FRAME 30 HAS 1 INCH CRACK BETWEEN SEAT TRACK 2L AND 3L REMOVED CRACK AND INSTALLED FLOORBEAM REPAIR BETWEEN S EAT TRACK 2L AND 3L AT FR 30 IAW SRM 53-10-15 FIGURE 211 SHEET 1 AND 2. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03896 1 20080916 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND ELONGATED HOLES ON RT WING BOTTOM SKIN AND PYLON SUPPORT BRACKET. REPAIR PERFORMED BY DRAWING R571-50532 (OVERSIZ ING THE HOLES INSTALL FREEZE PLUGS), APRROVED BY RAS/BAE/10078756/2008 ISS A AND EA 6-2900-123069. 2 L 7 2 4F RT A35EU 20080929 NM 2008 9 29 08FDEA03391 1 20080812 A 5340 6614827 BRACKET BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 CORROSION ON RT A/C BAY FWD COMPARTMENT LIGHT LENS RETAINER AND LIGHT MOUNT BRACKET. REPLACED FWD COMPARTMENT LIGHT, LE NS RETAINER AND LIGHT MOUNT BRACKET. REFERENCE SWPM 20-84-10, PG 3-5; SRM 51-30-02 PG 2-3; BOEING DRW NR 66-14827-1/1. OPERATIONAL TEST OF LIGHT GOOD. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080929 WP 2008 9 29 08FDEA03899 1 20080916 A 5420 AVB70659 FAIRING DOUG MD10 MD1010F 3022112 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 2 ENGINE PYLON LEFT SIDE APRON AT THE RAMP FAIRING IS CRACKED APPROXIMATELY 10 INCH. REMOVED APPRON IAW SRM 51-31-01 . FORMED NEW APPRON IAW SRM 51-10-00 & AMM 7-0-1-104. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED APPRON IAW SRM 51 -31-01. 2 L 7 3 4F RT A22WE 20080929 SO 2008 9 29 LR7A08105 1 20080819 A 5312 35970112 BULKHEAD LKHEED 382 382G 526414U SO FS 902 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HC5315 FOUND FUSELAGE INTERIOR BULKHEAD WEB CRACKED AT FS 902, WL280, LBL15. R EPAIRED IAW SMP583 FIG 51-140-17. 2 H 7 4 4T A1SO 20080929 SO 2008 9 29 LR7A08106 1 20080819 A 5420 COLLAR LKHEED 382 382G 526414U SO NR 1 ENGINE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HC7201 FOUND NR 1 ENGINE FIRESEAL COLLAR ASSY CRACKED AT 3 O'CLOCK. REPAIRED B Y WELDING IAW LAC MEA 382-71-08-044 R1. 2 H 7 4 4T A1SO 20080929 SO 2008 9 29 LR7A08107 1 20080819 A 5420 COLLAR LKHEED 382 382G 526414U SO NR 2 NACELLE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HC7201 FOUND NR 2 ENGINE FIRESEAL COLLAR ASSY CRACKED AT 9 O'CLOCK. REPAIRED B Y WELDING IAW LAC MEA 382-71-08-045 R1. 2 H 7 4 4T A1SO 20080929 SO 2008 9 29 LR7A08108 1 20080819 A 3010 102651 DUCT LKHEED 382 382G 526414U SO CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HC5712 FOUND COMPENSATOR DUCT P/N 10265-1 CRACKED. REPAIRED BY WELDING IAW LAC MEA 382-30-08-041 R1. 2 H 7 4 4T A1SO 20080929 EU 2008 9 29 08FDEA03410 1 20080814 A 5753 A57960300002 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CHAFING MARKS ON LT CENTER FLAP UPPER SKIN RIB 13-13A. REPAIR PERFORMED BY REWORK OF CHAFING MARKS AND INSTALLING A NEW CHAFING PLATE IAW, RAS/197/2008 ISS A, APPROVED BY EA 6-5753-123011. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03411 1 20080814 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CHAFING MARKS ON LT CENTER FLAP UPPER SKIN AFT OF REPAIR SPAR, RIB 4-4A AND 15-16. REPAIR PERFORMED BY REWORK OF CHAFING MARKS AND INSTALLING A NEW CHAFING PLATE IAW RAS/197/2008 ISS A, APPROVED BY EA 6-5754-123032. 2 L 7 2 4F RT A35EU 20080929 SO 2008 9 29 LR7A08109 1 20080819 A 3010 3517833R EJECTOR LKHEED 382 382G 526414U SO CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HC5712 FOUND ANTI-ICE EJECTOR PN 351783-3R CRACKED. REPAIRED BY WELDING IAW LA C MEA 382-30-08-043 R1. 2 H 7 4 4T A1SO 20080929 SO 2008 9 29 LR7A08110 1 20080819 A 2120 3773561 DUCT LKHEED 382 382G 526414U SO CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HC2111 FOUND RECIRCULATING AIR DUCT PN 377356-1 CRACKED. REPAIRED BY WELDING I AW LAC MEA 382-21-08-046 R1. 2 H 7 4 4T A1SO 20080929 EU 2008 9 29 08FDEA03264 1 20080805 A 5330 A53978149200 SKIN AIRBUS 310 A310324 3930206 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 812FD 467 EXTERNAL LT FUSELAGE SKIN HAS 2 DENTS. NR 1 AT FRAME 60 BETWEEN STRINGER 43 AND 44L 4 INCHES ABOVE BOTTOM SKIN LAP MEAS URES 6 INCHES LONG BY .800 INCHES WIDE BY .037 INCHES DEEP. NR 2 DENT AT FRAME 61 BETWEEN STRINGER 43 AND 44L 3 INCHES ABOVE SKIN LAP MEASURES 2 INCHES LONG BY .600 INCHES WIDE BY .017 INCHES DEEP. MEASURED ON PAINTED SURFACE. DISTANCE O F DENTS FROM FRAMES OUT OF LIMITS IAW SRM 53-10-12 DIAGRAM 109. REPAIRED DENTS, NR 1 AT FRAME 60 BETWEEN STRINGER 43 AN D 44L 4 INCHES ABOVE BOTTOM SKIN LAP, NR 2 DENT AT FRAME 61 BETWEEN STRINGER 43 AND 44L 3 INCHES ABOVE SKIN LAP, IAW SRM 53-10-12 FIG 216. 2 L 7 2 4F RT A35EU 20080929 WP 2008 9 29 08FDEA03265 1 20080805 A 5313 ACA33533 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 NR 1 AIR CONDITIONING COMP FUSELAGE SKIN, ANGLES; INTERCOSTAL WEB AND FASTENERS ARE CORRODED BETWEEN STA 562 AND STA 593 ; LONGERON 43L IMMEDIATELY OUTBOARD OF THE EXHAUST BOX. REPLACED CORRODED THROUGH LONGERON SECTION ACA 3353-3 LEFT BY SPLICING IN A NEW PIECE AT STA 561-593 IN REF TO DC/MD-10 SRM 53-00-01; FIG 7 AND EA 8-5310-117022 "FUSELAGE, A/C BAY LO NGERON CORROSION AT STA 561-578 - REPAIR". CLEANED SKIN AND INTERCOSTAL AND UPON FURTHER EVALUATION FOUND NO CORROSION PRESENT. ALODINED AND PRIMED ALL BARE METAL IN REF TO DC/MD-10 SRM 51-21-01; VOL II; PGS 9; 21 AND 24. REPLACED 2 CO RRODED CLIPS AND CORRODED HARDWARE IN REF TO DAC DWG ACA 3816 AND SRM 51-31-01; VOL II; . 2 L 7 3 4F RT A22WE 20080929 WP 2008 9 29 08FDEA03266 1 20080805 A 5330 NDA63131 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 LEFT LOWER FUSELAGE SKIN IS BULGED AT FS 1113, LONGERON 45L. REPAIRED THE SKIN IN REFERENCE WITH DC/MD-10 SRM 53-20-00; VOL I; FIGURE 6; SHEET 7. 2 L 7 3 4F RT A22WE 20080929 WP 2008 9 29 08FDEA03267 1 20080805 A 5330 NDA621351 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 LEFT EXTERNAL FUSELAGE SKIN IS BULGED AT FS 1123; LONGERON 46L. REPAIRED SKIN IAW EA NR 8-5330-117009. 2 L 7 3 4F RT A22WE 20080929 EU 2008 9 29 08FDEA03288 1 20080806 A 5321 B5327027700200 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DOOR PANEL NR 251 TH, LOWER SURFACE IS CRACKED AND PUNCTURED ON THE UPPER SURFACE. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03289 1 20080806 A 5321 B5327027801200 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DOOR PANEL NR 251 UM, IS CRUSHED, CRACKED AND PUNCTURED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03290 1 20080806 A 5321 B5327027800800 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO DOOR PANEL NR 251 VH, IS CRUSHED; CRACKED; HAS BROKEN INSERTS AND IS PUNCTURED. FABRICATED NEW PANEL IAW SRM 53-10-20 AND DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03309 1 20080807 A 5753 A5796000000251 SKIN AIRBUS 300 A300F4605R 3930327 EU LT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 WHILE ACCOMPLISHING EO 6-5750-7-5000 PT 3 "WINGS INBD FLAP, REPLACEMENT NOSE RIB 7 LT, STEP 10; THE ACCESS HOLE HAS B EEN PREVIOUSLY CUT AND IS 0.500" TOO LARGE. FLAP WAS FOUND TO BE BEYOND TIMELY REPAIR. RECEIVED NEW FLAP REF TAG NR 6934A5. FOR INSTALLATION OF THE FLAP SEE NON-ROUTINE N00518. NO FURTHER ACTION IS REQUIRED. 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 08FDEA03820 1 20080911 A 5330 65564225 SKIN BOEING 727 727227 1384078 NM BS 480-490 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 FUSELAGE LT, STATIC PORTS AREA HAS WORN AROUND EDGES AND POSITIVE STEP HEIGHT IS ON MAX LIMITS (0.006 INCH). REMOVED FA STENERS FROM AREA IAW SRM 51-30-2. FABRICATED DOUBLER AND TRIPLER IAW EA NR 7-5330-117032. TREATED AND PRIMED DOUBLER AND TRIPLER AND AFFECTED AREA IAW SRM 51-10-2. INSTALLED REPAIR WASHERS IAW SRM 51-30-8. INSTALLED DOUBLER AND TRIPLER IAW EA NR 7-5330-117032. TRIMMED OUT STATIC PORT HOLES AND SPOT FACE ORIGINAL SKIN IAW EA NR 7-5330-117032. 2 L 7 3 4F A3WE 20080926 NM 2008 9 26 08FDEA03821 1 20080911 A 5710 6521655440 BEAM BOEING 727 727227 1384078 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 RT WING T/E "J " BEAM IS CRACKED AT WBL 118 REMOVED T/E PANEL FOR ACCESS IAW SRM 51-30-2. REMOVED "J" BEAM AS REQUIRED BY SRM 51-30-2. FABRICATED NEW "J" BEAM IAW DRAWIING NR 65-21655-10 REV "J". TREATED AND PRIMED AFFECTED PARTS IAW SRM 51-10- 2. INSTALLED NEW "J" BEAM AND T/E PANEL IAW SRM 51-30-2 AND DRAWING NR 65-21655-10 REV "J". 2 L 7 3 4F A3WE 20080926 EU 2008 9 26 08FDEA03839 1 20080911 A 5321 B5327048401400 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 MAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 60 AND FRAME 62, RBL 18 AND RBL 37. 242 QJ FABRICATED FLO ORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080926 WP 2008 9 26 08FDEA03842 1 20080911 A 5414 AUB703625 PANEL DOUG MD10 MD1010F 3022112 WP NR 1 PYLON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 1 PYLON PANEL 738 GL IS CHAFED AT THE MATING SURFACE. FABBED REPAIR PARTS IAW EA 8-5480-123637 & SRM 54-00-01. ALO DINED & PRIMED FILLERS IAW SRM 51-21-01. INSTALLED REPAIR PARTS PER EA 8-5480-123637 & SRM 54-00-01. 2 L 7 3 4F RT A22WE 20080926 EU 2008 9 26 08FDEA03844 1 20080911 A 5330 A5387000120000 SKIN AIRBUS 310 A310222 3930315 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 EXTERIOR UPPER FUSELAGE SKIN HAS STATIC DISCHARGE BETWEEN FRAME 40/41 AND FRAME 42; STRINGER 2 R AND STRINGER 3 R. REMO VED AND REPLACED RIVET IAW SRM 53-10-12; FIG 220. ACCOMPLISHED A BHEC INSPECTION OF THE FASTENER HOLE IAW NTM PT6 51-10 -01. 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 08FDEA03054 1 20080724 A 5730 112N4102 SKIN BOEING 757 75723A 1384967 NM RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FUEL TANK ACCESS CUTOUT 641EB HAS CORROSION. REPAIR CARRIED OUT IAW SRM 57-20-01 REV 93 REPAIR 5. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080821 NM 2008 8 21 F3LA200800399 1 20080624 A 5320 D5367314700000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSP, NOTED AFT CARGO PIT FWD RT LOWER TRANSITION PANEL 152WG HAS A HOLE AT AFT CENTER SECTION. MAINT RE PAIRED TRANSITION PANEL 152WG IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACC EPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800284 1 20080602 A 5320 D5367221800000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM565 CFM565B6 13802 NE CARGO BAY DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 915FR 1851 DURING C4 S1 C-CHECK INSP NOTED FWD PIT TRANSITION PANEL 32DG HAD A CORNER DELAMINATED. MAINT CLEANED DAMAGED AREA AND REPAIRED DAMAGE IAW SRM 53-02-00 PAGE 209. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 EU 2008 8 21 F3LA200800419 1 20080703 A 5320 D5348015800600 PLATE AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE GIRT BAR COVER CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 805FR 1660 DURING C-CHECK INSP NOTED GIRT BAR BLANKING PLATE L2 AFT HAS CORROSION. MAINT REMOVED AND REPLACED CORRODED L2 AFT GIRT BAR BLANKING PLATES IAW WORK CARD C250001-03. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT 20080821 2008 8 21 F3LA200800524 4 20080726 A 2565 DHE1141 SENSOR AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE R2 DOOR SLIDE FAULTY A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 923FR 62 2019 FLIGHT CREW NOTED THE R2 DOOR INDICATION IS INOPERATIVE. WHILE CLOSED AND ARMED, THE ELECTRONIC CENTRALIZED AC MONITORI NG INDICATION IS AN AMBER BLOCK AND "SLIDE ARMED" INDICATION IS NOT ILLUMINATED. THIS DEFECT HAS BEEN DEFERRED (1063174 ) AND IS DUE ON 8/05/08. (A) THE FOLLOWING SUPPLEMENTAL INFORMATION IS BEING ADDED; MAINT REMOVED AND REPLACED THE DOOR HOOK SENSOR (DETECTOR) IAW AMM 52-71-11. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 7/31/0 8. (A) 2 L 7 2 4F 4 F RT A28NM 20080821 NM 2008 8 21 F3LA200800393 1 20080625 A 3230 664700500A4D CONTROL UNIT AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE MLG MALFUNCTIONED A F3LA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 926FR 2198 AFTER TAKEOFF THE FLIGHT CREW NOTICED THE NLG FAILED TO RETRACT. THE FLIGHT CREW FOLLOWED THE ECAM AND CYCLED GEAR AND N OSE GEAR RETRACTED NORMALLY AND THE AC RETURNED TO DEPARTURE. MAINT PERFORMED GEAR SWING SUCCESSFULLY 8 TIMES AND REMOVE D AND REPLACED NR 2 LGCIU IAW TSM 32-31-00-810-812 AND ARM 32-31-31-71 PAGE BREAK 401. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED, BITE CHECK WAS NORMAL AND OPERATIONAL CHECKED GOOD. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 ASAA0843289 1 20080712 A 5313 STRINGER FITTING BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU BS 1016 S17AL GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 755AS 25096 AT THE AFT SIDE OF THE APB STRINGER 17A LT END FITTING IS GOUGED. REMOVED AND REPLACED STRINGER 17A LT END FITTING ON TH E AFT SIDE OF THE APB IAW SRM 51-40-02, P4. 2 L 7 2 4F 4 F RT A16WE E21EU 20080821 NM 2008 8 21 F3LA200800354 1 20080617 A 5321 D5367204701000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP, NOTED CRACKED DENT ON UPPER SURFACE OF BULK CARGO FLOOR PANEL 161BF. MAINT REPAIRED PANEL 161BF IA W SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 EU 2008 8 21 F3LA200800360 1 20080616 A 5240 A52110526000000 LATCH AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE R2 DOOR NO TEST A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 941FR 2483 DURING C-CHECK INSP NOTED R2 DOOR HOLD OPEN LATCH BUTTON FAILED PRESS TEST. MAINT ADJUSTED R2 DOOR BUFFER IAW AMM 52-11 -00-820-001 STEP 4J. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 EU 2008 8 21 F3LA200800366 1 20080616 A 5320 D5367301800100 PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 941FR 2483 DURING C-CHECK INSP, NOTED AFT PIT TRANSITION PANEL 152UG HAS SEVERAL PUNCTURES. MAINT REPAIRED PANEL 152UG IAW SRM 53-0 2-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 F3LA200800315 1 20080608 A 5321 D5367150100000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP NOTED CABIN FLOOR PANEL 251TF HAS A LARGE PUNCTURE HOLE. MAINT REPAIRED FLOOR PANEL 251TF IAW SRM 5 3-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080821 NM 2008 8 21 2008UALA03712 1 20080707 A 3800 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE WATER SYSTEM UNKNOWN A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 653UA 25391 WATER SYSTEM PROBLEM. RTFL. 2 L 7 2 4F 4 F RT A1NM E24NE 20080821 NM 2008 8 21 2008UALA03697 1 20080702 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1345 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 LIGHTNING STRIKE ON RIVET EDGE AT STR1, STA 1345. *S/D* DAMAGE FROM LIGHTNING STRIKE. REMOVED DAMAGED FASTENER, A CP HEFC INSP PER NDT MM 51-00-16. NO CRACK FOUND. INSTALL BLIND FASTENER PER MM 53-30-95. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 2008 8 21 2008UALA03702 4 20080702 A 2565 BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 513UA 24810 LOW BOTTLE PRESSURE. PRESSURE GAUGE LOCK NUT LOOSE. TIGHTENED AND REFILLED. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NE 2008 8 21 SWAA084419 2 20080808 A 7230 CFM567 ENGINE BOEING 737 7377H4 1384404 NM GE CFM56 CFM56* 13802 NE LEFT STALLED A SWAA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SW 29 736SA 27868 874891 NR 1 ENG COMPRESSOR STALLED. REMOVED AND REPLACED NR 1 ENG PER MT. 2 L 7 2 4F 4 F RT A16WE E2GL 20080821 NM 2008 8 21 SWAA084420 1 20080808 A 5230 6547952 DOOR BOEING 737 7373H4 1384600 NM CARGO BAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO DOOR FWD LOWER CORNER CRACKED. REMOVED AND REPLACED AFT CARGO DOOR PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084412 1 20080807 A 5311 6546533 FRAME BOEING 737 7373A4 1384585 NM BS 500 S27-28L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 500, STR 27L TO STR 28L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084414 1 20080807 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 793SA 27888 EEPLS LENS MISSING AT ROW 2 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084380 1 20080806 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM BS 440 S17R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084422 1 20080808 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT COVER CRACKED. REMOVED AND REPLACED LIGHT COVER ASSY PE R MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 SWAA084383 1 20080806 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM BS 500A S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03340 1 20080612 A 3350 S283T0143 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 661UA 27158 THREE OVERWING AND DOOR 1L EMERGENCY LIGHTS WON'T COME ON. *S/D* SUSPECT FAULTY POWER SUPPLY. REPLACED POWER SUPPLY, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080821 NM 2008 8 21 2008UALA03336 1 20080611 A 3350 20131A POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 647UA 25284 EEL LIGHTS ON LT SIDE AT 19 - 22 INOP. *S/D* SUSPECT FAULTY POWER SUPPLY ASSEMBLY. REPLACED POWER SUPPLY, AC OK FOR S ERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080822 EU 2008 8 22 F3LA200800374 1 20080618 A 5321 D5367228300000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 941FR 2483 DURING C-CHECK INSP, NOTED AFT PIT SCREW PULLING THROUGH FLOOR PANEL 151CE NEXT TO FORWARD TIE DOWN BY SILL PLATE. MAIN T REPAIRED PANEL 151CE IAW EA A0-53T-10131. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080930 NM 2008 9 30 2008UALA05438 1 20080823 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ROW 5 LT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 ROW 5 LT EMERGENCY LIGHT INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA05459 1 20080825 A 2120 UNKNOWN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 104UA 26902 ELECTRICAL ODOR MAIN DECK GALLEY. RTFL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 EU 2008 9 30 2008UALA05463 1 20080823 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 419UA 487 YELLOW HYD SYSTEM FAILURE. FLIGHT DIVERTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NE 2008 9 30 2008UALA05464 2 20080824 A 7200 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 EPR UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 402UA 439 NR 2 ENGINE EPR FAULT. RTFL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA05465 1 20080824 A 2130 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN PRESSURE UNKNOWN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 832UA 1321 CABIN PRESSURE PROBLEM. RTFL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA05473 1 20080825 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ROW 5 RT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 ROW 5 RT EMERGENCY LIGHT INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA05526 1 20080828 A 2520 SEAT BOEING 737 737322 1384676 NM ROW 6 DEF LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 364UA 24533 THE 6 DEF ROW OF SEATS IS LOOSE. SECURED LEG ATTACH POINTS. SEAT IS SECURED. 2 L 7 2 4F RT A16WE 20080930 2008 9 30 2008UALA05517 4 20080828 A 2397 490S1 COUPLING BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE HF SYSTEM FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 670UA 29240 HF TRANSMISSION AND RECEPTION ARE INOP, WEAK, GARBLED INTERMITTENT, ETC AT ALL CREW STNS (1 = L HF, 2 = R HF) 2 CREW COM MENTS: RT HF RECEPTION REPORTED INTERMITTENT BY SFO RADIO. DURING POSITION REPORTS IT CUTS OUT. RT HF TRANSCEIVER WIL L TUNE BUT REC WEAK. LT SIDE TUNING INTERMITTENT. REPLACED TRANSCEIVER. FOUND RIGHT HF WITH STATIC, FOUND LT HF WORKING INTERMITTENTLY. WORKS FOR 5 MIN ON POWER UP THEN GOES OUT. SLAVED IN R541 (REF WD23-25-14) NO HELP. SWAPPED COUPLERS AN D FAULT FOLLOWED. REPLACED HF COUPLER, TESTED BOTH LH AND RT HF, BOTH OP 'S CHECKS GOOD. NO FAULTS. OK FOR SERVICE 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA05512 1 20080829 A 3510 OXYGEN BOTTLE BOEING 737 737322 1384676 NM CREW LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 CREW O2 AT 1550 PSI. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 2008UALA05451 1 20080824 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY CEILING LIGHT ROW 44 LT INOP. RELAMPED, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA05450 1 20080824 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE SEAT 16H BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 667UA 29239 FLT ATT REPORTED SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT BROKEN OFF SEAT 16H. REMOVED BROKEN LIGHT FROM ACFT AND STOWE D WIRES. REPLACED EMERGENCY LIGHT. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA05442 1 20080823 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 500 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 FWD PIT FRAME DENTED UPPER FLANGE AT BS 500 AND STR 25L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080930 NM 2008 9 30 2008UALA05429 1 20080823 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 117UA 28810 LEFT OVERWING 4 EACH EMERGENCY LIGHT IS INOP. REPLACED BATTERY. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA05423 1 20080823 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 117UA 28810 DOOR 3 LEFT CEILING 1 EA EMERGENCY LIGHT IS INOP. RELAMPED, CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 NM 2008 9 29 2008UALA05834 1 20080921 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT LIGHT INOP, AT DOOR 4 LEFT FWD LOWER WALL GALLEY AREA. REPLACED FEEDER CABLE. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080822 NM 2008 8 22 F3LA200800377 1 20080620 A 5321 D536720600100 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP NOTED AFT CARGO FLOOR PANEL 152UG HAS A DENT AND A HOLE. MAINT REPAIRED AFT CARGO FLOOR PANEL 152UG IAW SRM 53-02-00 PARAGRAPH 8E. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 EU 2008 8 22 F3LA200800423 1 20080707 A 5315 D53472188204 FLOORBEAM AIRBUS A318 A318111 3940019 EU CFMINT CFM56 CFM565B8P 13022 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 805FR 1660 DURING C-CHECK INSP NOTED FLOOR BEAM Y1292 HAS CORROSION AT NUTCLIP HOLE AT FRAME 68 OB SIDE JUST FWD OF GALLEY. MAINT B LENDED CORROSION AND OVERSIZED HOLE, INSTALLED FLANGE BUSHING TREATED PRIMED AND PAINTED IAW EA A8-53R-30435 AND SRM 51- 75-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT 20080822 NM 2008 8 22 F3LA200800465 1 20080714 A 5311 D534771800000 FRAME AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED AFT CARGO COMPARTMENT INSIDE OF C2 DOOR SHORT ANGLE PIECE AT FRAME C59 HAS CORROSION. MAINT RE MOVED SHORT ANGLE PIECE APPLIED PROTECTION TREATMENT FABRICATED NEW SHORT ANGLE TREATED, PRIMED AND PAINTED AND INSTALLE D IAW SRM 51-72-11, SRM 51-21-11, SRM 51-23-11 AND SRM 51-42-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUN D ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800475 1 20080711 A 2560 D5311201300000 GIRT BAR AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE R1 DOORWAY STICKING A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED R1 GIRT BAR FITTING FOR DOOR SLIDE STOP LEVER STICKS, DOES NOT SNAP BACK WHEN PRESSED DOWN AND RELEASED. MAINT REMOVED AND REPLACED WITH NEW GIRT BAR FITTING IAW AMM 52-11-31-000-003 AND 52-11-31-400-003. UPON COMP LETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800474 1 20080711 A 5347 D53913795200000 CARGO TRACK AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 918FR 19 1943 DURING C-CHECK INSP NOTED CORROSION ON PLATE BELOW TIE-DOWN PLATE UNDER FRAME C25 FWD CARGO PIT. MAINT REMOVED PLATE AND BLENDED CORROSION, MORE THAN 50 PERCENT MATERIAL LOSS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-14 OUT TO LIMITS OR A CTIONS NOT STATED. MAINT FABRICATED AND INSTALLED PLATE IAW EA NR 918-5299 AND SRM 51-42-11. UPON COMPLETION OF REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 MZZA080002 1 20080807 A 2560 ACREM1A MEGAPHONE BOEING 737 737824 13844BZ NM CABIN INOPERATIVE A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 27246 28956 FORWARD MEGAPHONE FOUND INOPERATIVE. REMOVED AND REPLACED FORWARD MEGAPHONE IAW IFM 25-60-01. OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20080822 WP 2008 8 22 IXX2008F00085 1 20080612 A 5311 FRAME DOUG DC8 DC872F 302199E WP BS 255 L25L CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND ACCESSORY COMPARTMENT FRAME CRACKED AT STATION 255.000 LONGERON 25LT. REMOVED DAMAGED FRAME SEGMENT. FABRICATED NEW SEGMENT. PERFORMED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0 FIGURE 2 SHEET 5 TR 53-125 DATED 8/31/01, SHEET 6 PAGES 5-6, DC8 SRM 5 1-1-8B, SRM 53-2-0 FIGURE 2 SHEET 1, SRM 53-3-2 FIGURE 3 SHEET 2A ITEM "U", SRM 53-3-2 FIGURE 3 SHEET 2, SRM 51-2-0 FIGU RE 52 SHEET 1, SRM 53-2-0 FIGURE 2 SHEET 7-8 TR 53-110 DATED 11-10-00, DC8 SRM 51-1-1 PAGES 1,13,17, SRM 51-1-11, SRM 51 -1-20D, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080822 NM 2008 8 22 DXTA200803221 1 20080811 A 2120 UNKNOWN AMD FALC50 FALCON2000 2730170 NM CONTROL PANEL ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 218QS 118 AHS 2 CIRCUIT BREAKER POPPED. RESET AND CIRCUIT BREAKER POPPED WITHIN 1 SECOND. THE CREW NOTICED AN ELECTRICAL ODOR CO MING FROM THE CIRCUIT BREAKER PANEL AND FROM AIR VENTS IN GALLEY AREA. (S) 2 L 7 2 4F RT A50NM 20080822 WP 2008 8 22 AALA200801894 1 20080716 A 3230 39567851 LINK DOUG DC9 DC983 3022083 WP MLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 9622A 53593 SFO - INFLIGHT T1544/16 JUL. CREW REPORTED VIBRATION AND NOISE DURING CLIMB. ACFT DID FLYBY AT SFO AND NOTICED RT FORW ARD NOSE GEAR DOOR OPEN. RETURNED TO SFO AND LANDED WITHOUT INCIDENT. REPLACED RT FORWARD NOSE GEAR DOOR LINK. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A6WE 20080825 EA 2008 8 25 COMA086349 1 20080809 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 965CA 7131 RT INTERNAL SKIN DOUBLER AT STA 640 IS CRACKED. FABRICATED PARTS AT STA 640 IAW CRJ REO 601R-53-61-506. (S) 2 L 7 2 4F RT A21EA 20080825 EU 2008 8 25 SIMA200822201 1 20080807 A 2434 23080031 GENERATOR SAAB SF340 340B 7860101 EU LEFT DC FAILED A SIMA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SW 21 298AE 340B298 ON FLIGHT 4772 AFTER TAKEOFF CREW REPORTED LT DC GEN LIGHT ON CWP. CREW ELECTED TO RETURN TO FIELD. EMERGENCY WAS DECL ARED, ACFT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED LT DC GEN IAW MTX W/C 24-47-33. A CFT RETURNED TO SERVICE. (S) 2 L 7 2 4T RT A52EU 20080825 WP 2008 8 25 IXX2008F00061 1 20080609 A 5730 SKIN DOUG DC8 DC872F 302199E WP RT WING DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND NICKS RT WIND OUTBOARD FLAP UPPER SKIN AT STATION XF 345.000. REMOVED FASTENER S AS NEEDED TO PERFORM REPAIR, REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XF 345.000-360.000 IAW DC8 SRM 57-7-1 FIGURE 4 TR 57-94 DATED 10-01-2002, DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-3-0, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080825 EU 2008 8 25 USAA920081496 1 20080809 A 3510 G2F21285 BOTTLE AIRBUS 320 A320232 3930326 EU EMERGENCY O2 DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 663AW 1419 PHASE 4 CHECK PXH - EMERG EQUIP - L-1 DOOR OVERHEAD EMERGENCY OXYGEN GENERATOR FAILED SYSTEM TEST. DOOR WILL NOT OPEN. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR OVERHEAD EMERGENCY OXYGEN CONTAINER. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4F RT A28NM 20080825 EU 2008 8 25 USAA920081525 1 20080815 A 5315 D53472188204 FLOORBEAM AIRBUS A319 A319112 3930323 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 PIT - S4- MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR68, Y1162. REPLACED FLOORBEAM AT FR68, Y1162 I AW A319 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080825 EA 2008 8 25 COMA0870025 1 20080811 A 5297 SH67059062001 WIRE HARNESS CNDAIR CL600 CL6002C10 1390015 EA CARGO DOOR DAMAGED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 379CA 10102 ON CLIMBOUT FROM CVG RECEIVED PROX SYSTEM FAULT 1 STATUS MESSAGE FOLLOWED BY CARGO DOOR CAUTION AND PASS DOOR WARNING ME SSAGE. NO CABIN PRESSURE LOSS. ACFT RETURNED BACK TO CVG AND LANDED SAFELY. FOUND CARGO DOOR HARNESS DAMAGED. REMOVE D AND REPLACED CARGO DOOR WIRE HARNESS. (S) 2 L 7 2 4F RT A21EA 20080825 NM 2008 8 25 UIEA200800288 1 20080815 A 5311 FRAME BOEING 747 7472D7B 1384803 NM BS 360 CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 524MC 21784 BS 360 FRAME WEB NEAR STRINGER 14L CRACKED. REPAIRED IAW BOEING SERVICE REQUEST 1911055155 APPROVED BY FAA FORM 8100-9 DATED 6 AUG 2008, DETAILS OF WORK KEPT AT ATLAS ENGINEERING ORDER EO4753B183. (S) 2 L 7 4 4F RT A20WE 20080825 2008 8 25 WGEA200800068 4 20080811 A 3417 1008555 ADC ECLIPS EA500 ECLIPSEEA500 3350000 SW NR 2 FAILED A WGEA O OTHER N FALSE WARNING AP APPROACH 1 EA 27 153DJ 214 214 000072 AT 1300Z DURING DESCENT AND APPROACH, CAS MESSAGES AIRSPEED AND ALTITUDE DISAGREE SHOWED UP. LT SIDE WAS 50-60 KNOTS GR EATER THAN RT AND THE ALTITUDE WAS 300 FEET GREATER ON THE LT SIDE. IN ADDITION THE STANDBY WAS SHOWING 10 KNOTS GREATE R THAN THE RT SIDE, AND 100 FEET GREATER THAN THE RT SIDE. DURING TAXI IN THE CONDITIONS REMAINED THE SAME. DRAINED 1. 5 OZ OF WATER FROM STATIC SYSTEM, REPLACED ADC2 DUE TO ERRATIC READINGS, PERFORMED ALL OP CHECKS WITH SATISFACTORY RESUL TS IAW EA500 MM 34-10-16. NOTE: INSTALLED ADC IS A NEW PART. (S) 1 L 7 2 4J RT A00002AC 20080825 WP 2008 8 25 IXX2008F00072 1 20080609 A 5730 SKIN DOUG DC8 DC872F 302199E WP LEFT WING MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK, FOUND IMPROPER REPAIR ON LT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095.000 AND XS 247.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREAT ED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND PLATING IAW DC8 SRM 57-3-2 FIGURE 10 PAGE 22 ITEM F, DC 8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-3-0, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080825 NM 2008 8 25 2008UALA03793 1 20080708 A 2560 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FLASHLIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 25019 DOOR 2L RT EMERGENCY FLASHLIGHT IS INOP. BATTERY INOP. REPLACED BATTERY, OPS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080825 EA 2008 8 25 TRAX200800987 1 20080808 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 686BR 7715 PAX DOOR FWD WEB IS CRACKED IN ZONE 2 & 3. REPAIRED PAX DOOR FWD WEB IAW BOMBARDIER REO 601R-52-11-702. SEAL AND PAINT REQUESTED STEP 11. SEALED AND PAINTED REPAIR AREA ON PAX DOOR FWD WEB IAW BOMBARDIER REO 601R-52-11-702 STEP 11. COMP LIED WITH ALL STEPS OF ASA EC/TC REO 601R-52-11-702. (S) 2 L 7 2 4F RT A21EA 20080825 CE 2008 8 25 GUU2008F00038 1 20080809 A 5520 1016200111 HINGE BRACKET BEECH 1900 1900D 1154162 CE ELEVATOR CORRODED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 69549 25747 UE194 AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT OUTBOARD ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED RT OUTBOARD ELEVATO R HINGE BRACKET. (S) 2 L 7 2 4T RT A24CE 20080825 NM 2008 8 25 AALA200801838 1 20080530 A 5347 141T5121 SEAT TRACK BOEING 767 767223 1385123 NM BS 341 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AA 22327 AFW - SEAT TRACK HAS CORROSION REMOVAL. REPAIRED PER MRB 767 3216. (S) 2 L 7 2 4F RT A1NM 20080825 CE 2008 8 25 GLB2008F00014 1 20080804 A 6123 AUTOFEATHER SYS BEECH 1900 1900D 1154162 CE MALFUNCTIONED A GLBA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 03 251GL UE251 ACFT 251GL - 07/21/2008 - FLIGHT 5133 - PILOTS REPORTED THAT UPON DEPARTURE FROM LBL TO DEN THE AUTOFEATHER ACTIVATED IN FLIGHT AS POWER WAS BEING INCREASED. MAINTENANCE PERFORMED OPERATIONAL CHECKS ON AUTOFEATHER SYSTEM IAW BEECH 1900D MM 61-21 WITH NO DEFECTS NOTED. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. OPERATIONAL CHECKS GOOD. (S) 2 L 7 2 4T RT A24CE 20080825 EA 2008 8 25 TRAX200800968 1 20080805 A 5343 TRUNNION CNDAIR CL600 CL6002C10 1390015 EA MLG CORRODED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 738EV 10146 CORROSION ON RT MLG FWD TRUNNION. REFER TO N/R-00201 FOR DOCUMENTATION AS THE LANDING GEAR WAS REMOVED AND REPLACED FOR EO 700-32-023. LANDING GEAR WAS SENT TO THE GEAR SHOP. (S) 2 L 7 2 4F RT A21EA 20080825 EA 2008 8 25 TRAX200800975 1 20080806 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 738EV 10146 FS 280 FWD ANGLE (FLIGHT STATION FWD FLOOR LAND) CORRODED. REMOVED FWD ANGLE AT FS 280. ALL WORK DONE IAW CRJ 700 SRM 51-42-06. DRILLED UP FWD ANGLE IAW SRM 51-42-06. (S) 2 L 7 2 4F RT A21EA 20080825 NM 2008 8 25 2008UALA03823 1 20080710 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR OBSTRUCTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 579UA 26697 DOOR 2L WON`T ARM AND DISARM PROPERLY. FOUND STATIC LINE TANGLED IN GIRT BAR. FREED LINE AND STOWED, OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080825 NM 2008 8 25 2008UALA03838 1 20080710 A 3510 232N80011 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CAPTAIN'S FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 CAPTAIN'S O2 MASK DOES NOT TRANSMIT THROUGH PA. WIRING SHORT INTERNAL TO MASK. REPLACED CAPT O2 MASK ASSY, OPS CHECKE D NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080825 NE 2008 8 25 USAABB08125 2 20080802 A 7397 CONNECTOR BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211* 54555 NE GOVERNOR DAMAGED A USAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 EA 19 206UW 27808 PHL FLT 1209 PHL TO SXM - DURING TAKEOFF ROLL, TNE NR 2 ENG WOULD NOT DEVELOP TAKEOFF POWER. THE CREW ABORTED THE TAKEO FF AT 60 KNOTS AND RETURNED TO THE GATE. MAINTENANCE REPAIRED THE CONNECTOR ON THE FUEL FLOW GOVERNOR SOLENOID. OPERAT IONALLY CHECKS OK. (S) 2 L 7 2 4F 4 F RT A2NM A12EU 20080825 SO 2008 8 25 RAIA00808010 1 20080811 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO EMERGENCY LIGHT LOOSE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 821HK 145068 PRE FLT 5574 -PHL- SEVERAL EMERGENCY LIGHTS INOPERATIVE IN THE CABIN. MAINTENANCE RESECURED A LOOSE CONNECTOR TO THE PO WER SUPPLY. LIGHTS OPS CHECKED GOOD. (S) 2 L 7 2 4F RT T00011AT 20080825 SO 2008 8 25 RAIA00808011 1 20080811 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 817HK 145058 PRE FLT 5470 -STL- EMERGENCY LIGHTS INOPERATIVE IN THE CABIN. MAINTENANCE RE-SECURED WIRING TO THE POWER SUPPLY. LIGHT S OPS CHECKED GOOD. (S) 2 L 7 2 4T RT T00011AT 20080825 SO 2008 8 25 RAIA00808013 1 20080811 A 5240 ROLLER EMB 145 EMB145 3260210 SO SERVICE DOOR LACK OF LUBE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 807HK 145119 POST FLT 8039 -STL- PASSENGER DOOR HARD TO OPEN AND CLOSE. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE PASSENGER DOOR WITH NO DEFECTS NOTED. (S) 2 L 7 2 4F RT T00011AT 20080825 NM 2008 8 25 KCSA081407 1 20080818 A 5340 BRACKET BOEING 747 747122 1384872 NM BS 1350 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 716CK 19753 CORROSION ON ATTACH ANGLES ON INBOARD AND OUTBOARD SIDE OF BRACKET AT BS 1350, LBL 78, WL 139. (S) 2 L 7 4 4F RT A20WE 20080825 NM 2008 8 25 2008UALA03485 1 20080618 A 3350 S283T0143 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 EMERGENCY ESCAPE PATH LIGHTING COMES ON FROM ROW 28 TO DOOR 2R (ONLY ON RIGHT SIDE OF A-C). AFTER TROUBLESHOOTING FOUND FAULTY POWER SUPPLY. REPLACED POWER SUPPLY M734 AND OPS CHECKS OK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080825 EU 2008 8 25 SIMA200821901 1 20080805 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS MALFUNCTIONED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 323AE 340B323 ON FLIGHT 3019 - ON GROUND CREW REPORTED EMERGENCY LIGHTS IN CABIN ROWS 10, 11, 12, 14 DO NOT STAY ILLUMINATED. ACFT RE MOVED FROM SERVICE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AT POSITION 24LN, OPERATIONAL CHECK GOOD. ACFT RETURNE D TO SERVICE. (S) 2 L 7 2 4T RT A52EU 20080825 NM 2008 8 25 Q2SA748005 1 20080813 A 7500 PRECOOLER BOEING 747 747206B 1384856 NM GE CF6 CF650E2 30018 NE BLEED AIR SYS LEAKING A Q2SA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 63 748SA 21110 455863 ON TAKEOFF FROM KMIA, UNABLE TO OBTAIN NECESSARY N1 OF 113.6 PERCENT FOR NR 2 ENG. AT N1 OF 109.0 PERCENT, RED WARNING CAME ON AND N1 MAINTAINED INDICATION AT 109.0 PERCENT. ON CLIMBOUT FROM KMIA, BOTH CHANNEL A & B NACELLE TEMPERATURE IN DICATIONS WERE 5.0. REDUCED THRUST LEVER TO IDLE AND BOTH NACELLE TEMPS REDUCED TO 2.25 (A) AND 2.75 (B). ACFT RETURNE D TO KMIA. NO FUEL WAS DUMPED. INSPECTION FOUND BLEED AIR PRECOOLER LEAKING WITH CRACKED FLANGE. ENG CHANGE REQUIRED. ALL AD`S ARE CURRENT FOR THIS ENG. (S) 2 L 7 4 4F 4 F RT A20WE E23EA 20080825 EA 2008 8 25 REX2008F00031 1 20080812 A 4980 EXHAUST DUCT CNDAIR CL600 CL6002B19 1900309 EA APU FIRE A REXA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SO 25 8908D 7908 DURING POSTFLIGHT WALKAROUND AT KIDA, THE FIRST OFFICER SPOTTED AN APU EXHAUST PIPE FIRE. THE CAPTAIN PUSHED THE APU FI RE SWITCH AND WHEN THE FIRE CONTINUED, DISCHARGED THE APU FIRE BOTTLE. THE FIRE ABATED TEMPORARILY, BUT THEN REIGNITED. THE FIRST OFFICER EXTINGUISHED THE FIRE WITH A PORTABLE FIRE EXTINGUISHER SUPPLIED BY GROUND PERSONNEL. MAINTENANCE I NSPECTED THE APU AND DETERMINED THERE WAS NO FIRE OUTSIDE OF THE APU ITSELF. THE APU WAS DEFERRED PER ESTABLISHED COMPA NY PROCEDURES AND THE ACFT RELEASED FOR SERVICE. (S) 2 L 7 2 4F RT A21EA 20080825 NM 2008 8 25 KCSA081379A 1 20080811 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 460 S12R CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 BS 460 S12R FRAME DOUBLER AFT SIDE CRACKED .500 INCH AT STRINGER CUTOUT, INBOARD UPPER CORNER. CRACK MARKED UPPER DECK. (S) 2 L 7 4 4F RT A20WE 20080825 WP 2008 8 25 AALA200801881 1 20080715 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA O OTHER O OTHER NR NOT REPORTED 1 SW 21 3515 49892 LGA - EMERGENCY LIGHT AT OVERHEAD TAIL CONE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD TAIL CON E. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F A6WE 20080825 NM 2008 8 25 2008UALA03414 1 20080614 A 3610 32153024 VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 1 ENGINE FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 797UA 26924 BLEED OFF ENG L - EICAS MSG ON TAXIOUT. SUSPECT FAULTY HIGH PRESSURE SHUT OFF VALVE. REPLACED NR 1 ENGINE HPSOV REF AM M 36-11-07. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080825 NM 2008 8 25 KCSA081382 1 20080813 A 5242 SKIN BOEING 747 747122 1384872 NM E/E DOOR DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 716CK 19753 FWD E&E DOOR HAS SMALL DENT AT L/E ON SKIN. (S) 2 L 7 4 4F RT A20WE 20080825 CE 2008 8 25 GUU2008F00033 1 20080803 A 3240 BRAKE BEECH 1900 1900D 1154162 CE MLG WEAK A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 81533 UE137 FLIGHT 9232 TPA/EYW - PILOT REPORTED, CAPTAIN`S RT BRAKE PEDAL GOES TO THE FLOOR. NO BRAKING ACTION AT ALL. FIRST OFFI CER`S BRAKES WORK MINIMALLY. BLED RT BRAKE. OPERATIONAL CHECK GOOD. (S) 2 L 7 2 4T RT A24CE 20080825 EA 2008 8 25 N6WA0080802 1 20080811 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 154GJ 10224 C8312-ORD. CEILING EMERGENCY FLOODLIGHT INOPERATIVE OVER ROW 16. DEFERRED LIGHT IAW MEL 33-51-01-2A. (S) 2 L 7 2 4F RT A21EA 20080825 EU 2008 8 25 USAA920081499 1 20080810 A 2421 766219 IDG AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ZONE 500 INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 648AW 13283 2771 770 V10570 FLT 98 -LAS-DTW- AIR TURNBACK - CREW REPORTED TR1 AND ELEC GEN 1 FAULT ON CLIMBOUT AND "ELEC AC BUS 1 FAULT." MAINTENAN CE REMOVED AND REPLACED THE NR 1 ENG INTEGRATED DRIVE GENERATOR PER AIRBUS MAINTENANCE MANUAL 24-21-51. OPERATIONAL CHE CK GOOD. (S) 2 L 7 2 4F 4 F RT A28NM E40NE 20080825 NM 2008 8 25 USAA920081501 1 20080808 A 5755 SKIN BOEING 737 7374B7 1384702 NM ZONE 600 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 457UW MA13685 25021 CLT -C6- MAJOR REPAIR - NR 9 SPOILER UPPER SKIN AND HONEYCOMB ASSEMBLY DELAMINATED. REPLACED NR 9 SPOILER IAW B737 AMM 27-62-91. (S) 2 L 7 2 4F RT A16WE 20080825 SO 2008 8 25 C2XA08SH102 1 20080809 A 5751 14569009410 BRACKET EMB 145 EMB145XR 3260214 SO RT AILERON WORN A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 11150 145756 SHV - DURING C-CHECK IT WAS FOUND THAT THE RT AILERON PCA BRACKET HAD A MIGRATED HAT BUSHING. THE HOLE WAS WORN OUT OF LIMITS AND WOULD NOT RETAIN THE BUSHING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145XR SRM 51-40- 02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080825 SO 2008 8 25 SIMA200822202 1 20080807 A 2434 GENERATOR EMB 135 EMB135LR 3260305 SO LEFT DC FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 724AE 145301 ON FLIGHT 4772 AFTER TAKEOFF CREW REPORTED LT DC GEN LIGHT ON CWP. CREW ELECTED TO RETURN TO FIELD. EMERGENCY WAS DECL ARED, ACFT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED LT DC GEN IAW MTX W/C 24-47-33. A CFT RETURNED TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080929 NM 2008 9 29 2008UALA05845 1 20080922 A 5320 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 804UA 759 CORROSION ON R2 DOOR SILL BETWEEN FR 67 AND 68. MAJOR REPAIR. CUT OUT DAMAGE AND INSTALLED REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 20080929 WP 2008 9 29 08FDEA03904 1 20080905 A 5512 ALC7439501 SKIN DOUG MD10 MD1010F 3022112 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT HORIZONTAL STAB SKIN PANEL AFT SECTION (UPPER) SHOWS A CRACK INDICATION BETWEEN THE 2 BLACK DOTS APPROX 0.430 LONG AND 0.875 OFF THE AFT EDGE OF THE SKIN PANEL. REPAIRED SKIN PANEL PER EA 8-5510-123505. 2 L 7 3 4F RT A22WE 20080929 WP 2008 9 29 08FDEA03905 1 20080916 A 5410 ATL00553 HEAT SHIELD DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 2 ENGINE LEFT FAN COWL LOWER FWD INSIDE CORNER CHAFFING PLATE IS WORN AND TORN. REMOVED LOWER FWD HEAT SHIELD. FABR ICATED REPAIR FOR HEAT SHIELD AND INSTALLED DC/MD-10 DAC DWG ATL OO55 AND SRM 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 20080929 SO 2008 9 29 LR7A08101 1 20080819 A 5330 33873518L SKIN LKHEED 382 382G 526414U SO FS 507 WARPED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 2474 4606 DURING SCHEDULED C-9 CHECK, PER JOB CARD HST5301 FOUND LT MLG LOWER FAIRING SKIN WARPED AT FS 507, WL130, LBL50. REPAIR ED IAW SMP583 CHAP 51-60, 51-70 AND DWG 338735. 2 H 7 4 4T A1SO 20080929 EU 2008 9 29 08FDEA03405 1 20080813 A 5321 B5327080100000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 MAIN CABIN FLOOR PANEL 232 LG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 LG; POTTED EDGES, COMPLETED CURE AND SANDED T HE EDGE POTTING. INSTALLED INSERTS, APPLIED NON-SKID AND PART MARKED THE PANEL IAW DWG SRZ 25-005, REV "G". 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03408 1 20080813 A 5347 R538D104820200 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 430FE 394 MD CARGO COMPT CLS ADAPTER AT FR 43 BETWEEN SEAT TRACK 2RT AND 3 RT HAS 2 INCH CRACK. REMOVED AND REPLACED MDCC CLS ADA PTER AT FR 43 BETWEEN SEAT TRACK 2RT AND 3RT IAW A310-200 SRM 21-72-10. 2 L 7 2 4F RT A35EU 20080929 NM 2008 9 29 08FDEA03524 1 20080820 A 5320 6517510120 WEB BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 RT LOWER TORQUE BOX INBD WEB HAS A CRACK AT BOLT STA 1223. STOPPED DRILLED CRACK 2 EACH DIMS .250 IAW SRM 51-10-1, HFEC CRACK TO VERFY TERMINATION AT STOP DRILL IAW NDTM PT6 51-00-00 FIG 23. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. INSTALLED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1. 2 L 7 3 4F RT A3WE 20080929 NM 2008 9 29 08FDEA03188 1 20080730 A 5711 ARB72072 SPAR DOUG MD11 MD11F 3023600 NM ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 RIGHT WING, DURING ACCOMPLISHMENT OF EA NR 1-5710-105596C PART 2, REAR SPAR LOWER CHORD FORWARD AND AFT TENSION TIES AT STA XORS 1088 FOUND FASTENER HOLE ELONGATED. ELONGATED HOLE AT REAR SPAR LOWER CHORD FORWARD AND AFT TENSION TIES AT ST A XORS 1088. REPAIRED AS PER EA NR 1-5710-124327, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080929 NM 2008 9 29 08FDEA03189 1 20080730 A 5730 ARB74053 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 06 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS 690 AND STA XORS 700. LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND STA XORS 70 0 06 EACH CRACKED FASTENER HOLES REPAIRED AS PER EA NR 1-5710-124333, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080929 NM 2008 9 29 08FDEA03190 1 20080730 A 5730 ARB74054 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 13 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOU T BETWEEN STA XORS 690 AND STA XORS 700. RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 690 AND STA XORS 700, 1 3 EACH CRACKED FASTENER HOLES REPAIRED AS PER EA NR1-5710-124332, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080929 EU 2008 9 29 08FDEA03191 1 20080730 A 2910 AE4636E0195000 HOSE AIRBUS 300 A300B4622R 3930312 EU HYD SYSTEM DAMAGED A FDEA R AUTOROTATION K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CE 21 749FD 536 TOTAL LOSS OF GREEN HYD SYSTEM ON SHORT FINAL GEAR DOWN FLAPS 40 DEGREES DECLARED EMERGENCY LANDED USED DIFF BRAKING ST OPPED ON CENTERLINE MAINTENANCE PINNED AND TOWED TO GATE. TURNED PUMPS OFF WHEN DIRECTED BY ECAM BEFORE LANDING. FOUN D LT FLEX LINE AT TOP OF NOSE GEAR STRUT GOING TO ACTUATOR DAMAGED AT FITTING AND CAUSING LEAK. DAMAGED LINE REMOVED A ND SYSTEM ISOLATED. REINSTALLED BOTH NLG ACTUATOR FLEX HOSES. CYCLED LANDING GEAR PER AMM 32-31-00-5, 3 TIMES, OPS AN D LEAK CHECK OK. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03193 1 20080731 A 5320 A2557381120200 STIFFENER AIRBUS 300 A300F4605R 3930327 EU ZONE 100 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 AFT CARGO DOOR CUTOUT, UPPER FWD CORNER, WEB PANEL IS BENT. REMOVED THE SURROUNDING STRUCTURE TO ACCESS THE DAMAGE IAW SRM 51-40- 21; PARA 5; 6 AND 7. REMOVED DAMAGED AREA IAW SRM 51-71-30; FIG 201. FABRICATED REPAIR PARTS AND INSTALL ED IAW SRM 51-71-30; 201. RE-INSTALLED SURROUNDING STRUCTURE IAW SRM 51-40-21; PARA 5; 6 AND 7. 2 L 7 2 4F RT A35EU 20080930 NM 2008 9 30 CALA0800818 1 20080822 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM BS 827 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 BODY STATION 827 RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REPAIRED CRACKED FRAME AT STATION 827 RIGHT AT AC BRACKET BETWEEN STR 8 AND 9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800820 1 20080822 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM BS 440 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 BODY STATION 440 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REMOVED CRACK, FABRICATE D AND INSTALLED REPAIR ANGLES PER EA5310-04498 ON FRAME STA 440 LEFT SIDE BETWEEN STR 8 LT AND STR 9 LT. 2 L 7 2 4F RT A16WE 20080930 2008 9 30 2008UALA04047 4 20080730 A 2565 O-RING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU SLIDE BOTTLE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 309UA 23670 LOW BOTTLE. GAUGE ADAPTER & RUPTURE DISK O-RING LEAKING. REPLACED WITH NEW. 2 L 7 2 4F 4 F RT A16WE E21EU 20080930 NM 2008 9 30 2008UALA04127 1 20080802 A 3350 CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 OVERWING LT EMERGENCY LIGHT 2 LOWER LIGHT INOP. *S/D* REPLACED BATTERY CHARGER. OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04139 1 20080805 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 54 RT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY LIGHT INOP: SEAT 54 RT. REPLACED LIGHT ASSY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04160 1 20080806 A 5240 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 594UA 28145 R-2 DOOR REQUIRES REPAIR DOUBLER AT UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED: INSTALLED REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 20080930 NM 2008 9 30 2008UALA04212 1 20080808 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROW 21 LT UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 EMERGENCY LIGHT AT ROW 21 LT IS LOOSE. SECURED LIGHT. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080930 NM 2008 9 30 2008UALA04222 1 20080809 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY LIGHT SEAT 5E AFT INOP. RELAMPED, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA05419 1 20080822 A 5240 F1314 SPRING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE R1 DOOR WEAK A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 R-1 DOOR DEPLOYMENT BAR GAS SPRING WEAK. REPLACED SPRING. OPS OKAY FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA05430 1 20080823 A 2822 PUMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUEL BOOST MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 773UA 26929 DURING LEFT AFT BOOST PUMP REMOVAL FOUND REMOVAL VALVE PLATE WITH NO PRELOAD RESULTING IN VALVE PLATE DRIFTING OPEN AFTE R PUMP REMOVAL. LEFT MAIN TANK FWD BOOST PUMP REPLACED, ALONG WITH HOUSING. OP CHKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080930 NM 2008 9 30 2008UALA05439 1 20080823 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ROW 5 RT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 ROW 5 RT EMERGENCY LIGHT INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA04227 1 20080811 A 3397 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY LIGHT ROW 55 LT INOP. FOUND LOOSE CONNECTOR. RE-SECURED EEL CONNECTOR. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04213 1 20080809 A 3397 UNKNOWN CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 EMERGENCY ESCAPE LIGHT INOP AT MID LAV. FOUND DAMAGED DISCONNECT CONNECTOR. REPAIRED THE DISCONNECT CONNECTOR. OPS CH ECKS OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080930 NM 2008 9 30 2008UALA04210 1 20080810 A 2697 CONNECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE LOOP CONTAMINATED A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 528UA 25018 EICAS MSG - R ENG FIRE LP 1. CREW COMMENTS: R ENG FIRE LOOP 1. FOUND CONNECTORS ON LOOP 1 VERY CONTAMINATED. CLEANED BOTH CONNECTORS, RESISTANCE CHECKS WITHIN LIMITS. MESSAGE CLEARED. SYSTEM TESTS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080930 WP 2008 9 30 UPS08853228 1 20080728 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 781 L15R DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 MAIN CABIN, DOUBLE DRILLED HOLE IN BELTFRAME STA 781 L15R. FABBED AND INSTALLED REPAIR DOUBLER IAW S RM 51-1-8, 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 20080930 WP 2008 9 30 UPS08853229 1 20080815 A 5322 SHEAR TIE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 AFTER REMOVAL OF EXISTING DOUBLER PER EO DC8-5330-27215 FOUND SHEAR TIE CRACKED AT STA 12 L21L-22L, H IDDEN UNDER DOUBLER. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-1-8, 51-1-20D, 51-1-21, 51- 3-1. 2 L 7 4 4F RT 4A25 20080930 WP 2008 9 30 UPS08853230 1 20080730 A 5313 STRINGER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1, NR 4 ALT THRU 505B, STRINGER 54 CRACKED AT APPROX XRS 490. FABRICATED AND INSTALLED 2 REPAIR SPLICE S IAW SAA EA 088-5710-01-1474. 2 L 7 4 4F RT 4A25 20081001 2008 10 1 SWAA085214 4 20080925 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR UNWANTED DEPLOY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 505SW 24182 L1 EMERGENCY EXIT DOOR SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085209 1 20080923 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 490WN 32476 DURING SCHEDULED HC2 CHECK, FOUND MID CABIN LT AND RT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND RE PLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080821 NM 2008 8 21 2008UALA03694 1 20080702 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1380 S4L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 LIGHTNING STRIKE AT EXT FUSELAGE SKIN AT STA 1380, 1 INCH BELOW STR 4L. DAMAGE FROM LIGHTNING STRIKE. REMOVED DAMAGED PER MM 53- 30-95, P603, ITEM B. ACP HFEC INSP ON HOLE PER NDT MM 51-00-16, NO CRACK FOUND. INSTALL BLIND FASTENER PER MM 53-30-95. WORK IS A CP ON WU D9822Y BY GSO AMT 1746, 3212, AND INSP BY QC031. CF IS CREATED TO CHECK FASTENER AT NE XT C-CK AND REPLACE AT NEXT HMV. ** MF5159 CREATED TO MONITOR ** 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NM 2008 8 21 SWAA084421 1 20080808 A 5210 SKIN BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR LOWER AFT CORNER SKIN CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20080821 2008 8 21 2008UALA03727 4 20080705 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 DOOR READS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 593UA 28144 SLIDE AT DOOR 3L PRESSURE LOW. *S/D* CYLINDER FITTING LEAK INSIDE SLIDE ASSY. REPLACED DOOR SLIDE AT 3L. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NM 2008 8 21 2008UALA03751 1 20080705 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 526UA 24994 RIGHT HAND EXTERIOR OVERWING FWD EMERGENCY LIGHT INOP. *S/D* BULB INOP. REPLACED LIGHT BULB, CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080821 NM 2008 8 21 2008UALA03358 1 20080613 A 3350 BATTERY PACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 656UA 25394 EMERGENCY PATH LIGHTS & WINDOW 'EXIT' LIGHTS FLASHING ON-OFF DURING FLIGHT. *S/D* SUSPECT BATTERY. REPLACED BATTERY P ACK. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080821 NM 2008 8 21 2008UALA03084 1 20080529 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 4F FWD AND AFT LIGHT ASSY'S. *S/D* FOUND LOOSE CONNECTION. SECURED CONNECTION, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080821 NM 2008 8 21 2008UALA03359 1 20080611 A 3600 7732887810 SHUTOFF VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 657UA 27112 NR 1 ENG PRSOV FAILED HEALTH CHECK REFERENCE PRESSURE LOW. *S/D* DURING HEALTH CHECK FOUND PRESSURE REGULATING SHUT OF F VALVE FAULTY. REPLACED PRSOV. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080822 NM 2008 8 22 F3LA200800390 1 20080622 A 5320 D5367306800000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSP, NOTED FWD PIT TRANSITION PANEL 132BF HAS SEVERAL PUNCTURES. MAINT REPAIRED TRANSITION PANEL 132BF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800391 1 20080622 A 5320 D5367360700000 PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 939FR 2448 DURING C-CHECK INSP, NOTED FWD PIT TRANSITION PANEL 132CF HAS SEVERAL PUNCTURES. MAINT REPAIRED TRANSITION PANEL 132CF IAW SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800335 1 20080611 A 5321 D5367321000000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP NOTED CARGO PIT FLOOR PANEL 161DF HAS A DAMAGED AREA. MAINT REPAIRED PANEL 161DF IAW SRM 53-02-00. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800383 1 20080621 A 5320 D5347112420100 SHEAR PLATE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP NOTED RT CABIN FLOOR LATERAL SHEAR PLATE AT Y1162 BETWEEN FRAMES 69 AND FRAMES 70 HAS AREAS OF CORRO SION. MAINT REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-72-11. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUN D ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800541 1 20080728 A 5320 D5348015800600 BLANKING PLATE AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5P 13016 NE GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2 2209 DURING C-CHECK, INSP NOTED THE L2 AFT GIRT BAR BLANKING PLATE HAD CORROSION. MAINT REMOVED AND REPLACED CORRODED L2 DOO R AFT GIRT BAR FITTING BLANKING PLATE IAW AMM 52-13-31-400-007. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUN D ACCEPTABLE. (S) 2 L 7 2 4F 4 F RT A28NM 20080822 NM 2008 8 22 F3LA200800380 1 20080620 A 5511 D55181715 SPAR CAP AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE HORIZONTAL STAB DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 926FR 2198 DURING C-CHECK INSP NOTED LT HORIZONTAL STABILIZER OB REAR SPAR LOWER CAP HAS COMPOSITE DAMAGE LOCATED OB OF RIB 11 18 I NCHES OF REAR SPAR TEE SEPARATED. MAINT REMOVED DAMAGED AREA ON LT HORIZONTAL STABILIZER OB REAR SPAR AND APPLIED REPAIR DAMAGE IAW SRM 51-77-11 AND EA A9-55R-30340. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (A) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 2008 8 22 COEA0802912 4 20080811 A 3417 7000700942 ADC AEROSP ATR42 ATR42300 8680920 EU NR 1 INTERMITTENT A COEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 13 912FX 047 OVER FLY KTN & SIT: FLT 7202 SEA-KTN-SIT-JNU. EN ROUTE TO KTN FROM SEA THE NR 1 AIR DATA COMPUTER (ADC) STARTED TO IN TERMITTENTLY FAIL. SINCE THE NR 2 ADC AND STANDBY SYSTEM WERE OPERATING NORMALLY, A DECISION TO BYPASS KTN AND SIT SO M AINTENANCE COULD BE ACCOMPLISHED WAS MADE. REMOVED AND REPLACED NR 1 ADC. (S) 2 H 7 2 4T RT A53EU 20080822 NM 2008 8 22 UIEA200800282 1 20080814 A 5754 PANEL BOEING 747 7472D7B 1384803 NM RT WING CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 522MC 21783 RT WING UPPER LEADING EDGE PANEL HAS A 20.0 INCH COMPOSITE CRACK AT ILES 522.56 AND IS 26 INCHES FROM FORWARD END OF PAN EL. PERMANENT REPAIR ACCOMPLISHED AS PER 747-200 SRM 51-40-09 FIG 18, SHEETS 2 AND 5, PREPEG LAYUP 250 DEGREES F CURE P ER SRM 51-40-12. REFERENCE ATLAS AIR EO 4757A457. (S) 2 L 7 4 4F RT A20WE 20080822 SO 2008 8 22 SIMA200822401 1 20080809 A 7500 DUCT EMB 135 EMB135LR 3260305 SO BLEED SYSTEM BLOWN A SIMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 713AE 145249 ON FLIGHT 4896 - CREW REPORTED ON CLIMBOUT, THERE WAS SMOKE IN COCKPIT AND CABIN. CREW DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. SMOKE CLEARED AFTER LANDING WITH BLEED AND PACKS OFF. ACFT REMOVED FROM SERVICE. FOUND AIR DUCTS BLOWN OFF. RE-SECURED BLOWN OFF AIR DUCTS UNDER FLOOR ROW 6. ACFT RETURNED TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080822 NM 2008 8 22 KCSA081386 1 20080811 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 460 S12R CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 BS 460 S12R FRAME DOUBLER AFT SIDE CRACKED .500 INCH AT STRINGER CUTOUT, INBOARD UPPER CORNER. CRACK MARKED. UPPER DEC K. (S) 2 L 7 4 4F RT A20WE 20080825 NM 2008 8 25 2008UALA03803 1 20080709 A 5240 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 CORROSION UNDER R-4 DOOR CAM PLATE INSERTS. REPLACED HANDLE BOX REF CM M-52-11-25. 2 L 7 2 4F 4 F RT A2NM E17NE 20080825 NM 2008 8 25 2008UALA03779 1 20080709 A 2150 COUPLING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE A/C PACK DISCONNECTED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 518UA 24871 PRESSURIZATION PROBLEM. RTFL. FLEX DUCT COUPLING DISCONNECTED AND DAMAGED. FOUND RUBBER FLEX COUPLING ON LEFT PACK OFF RIGHT SIDE HAS A HOLE. REPLACED AND SECURED, PRESSURIZED A/C NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080825 NM 2008 8 25 KCSA081406 1 20080818 A 5420 STIFFENER BOEING 747 747132 1384882 NM FIREWALL CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 709CK 20247 OUTBOARD STIFFENER ON FIREWALL CRACKED AT PNEUMATIC DUCT CLAMP ATTACH POINT. (S) 2 L 7 4 4F RT A20WE 20080825 EA 2008 8 25 TRAX200800991 1 20080809 A 5241 SUPPORT ANGLE CNDAIR CL600 CL6002C10 1390015 EA GALLEY DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 CORROSION FOUND ON THE SERVICE DOOR GALLEY SUPPORT ANGLE. (S) 2 L 7 2 4F RT A21EA 20080825 NM 2008 8 25 USAA920081510 1 20080731 A 5310 D53472172205 BEAM AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 833AW 1844 SAL - BC4 - MAJOR REPAIR - GALVANIC CORROSION ON BEAM AT FR67, -Y1180. REPLACED BEAM AT FR67, -Y1180 IAW A319 SRM 51-42 -11. (S) 2 L 7 2 4F RT A28NM 20080825 CE 2008 8 25 GUU2008F00028 1 20080806 A 5220 HANDLE BEECH 1900 1900D 1154162 CE EMERGENCY EXIT LACK OF LUBE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 87554 UE227 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RT AFT EMERGENCY EXIT HANDLE IS JAMMED. LUBRICATED RT AFT EMERGENCY EXI T HANDLE ASSEMBLY. (S) 2 L 7 2 4T RT A24CE 20080825 WP 2008 8 25 AALA200801825 1 20080709 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 594AA 53284 LGA - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 25DEF FOR EMERGENCY LIGHTS IN AFT CA BIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A6WE 20080825 EU 2008 8 25 F3LA200800549 1 20080811 A 5321 D536731400000 FLOOR PANEL AIRBUS A318 A318111 3940019 EU FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 806FR 30 2218 DURING C3 C-CHECK, INSPECTION NOTED THE AFT CARGO PIT RT TRANSITION PANEL 162BF WAS DAMAGED. MAINTENANCE REPAIRED DAMAG ED PANEL 162BF IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT WA S INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT 20080825 EU 2008 8 25 USAA920081518 1 20080813 A 5320 D53480043204 SILL AIRBUS A319 A319112 3930323 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 PIT -S4- MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON LOWER L2 DOOR SHAPE SILL PLATE AT FR66 TO FR68. REPLACED LOW ER L2 DOOR SHAPE SILL PLATE FR66 TO FR68 IAW A319 DRAWING D5348009. (S) 2 L 7 2 4F RT A28NM 20080825 EU 2008 8 25 F3LA200800547 1 20080811 A 5321 D5367331100000 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 806FR 2218 DURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT FORWARD FLOOR PANEL 131CG HAS SEVERAL HOLES. MAINTENANCE REPAI RED DAMAGED PANEL 131CG IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REP AIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT 20080825 SO 2008 8 25 GUU2008F00041 1 20080803 A 3350 SOCKET EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DIRTY A GUUA K NONE L NO TEST IN INSP/MAINT 1 SO 17 283AS 120236 AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED BOTH OVERWING EMERGENCY LIGHTS INOPERATIVE. CLEANED LIGHT SOCKET. OPERATIO NAL CHECK NORMAL. (S) 2 L 7 2 4T RT A31SO 20080825 CE 2008 8 25 GUU2008F00039 1 20080813 A 3230 MS24171D1 RELAY BEECH 1900 1900D 1154162 CE NLG INOPERATIVE A GUUA O OTHER O OTHER AP APPROACH 1 SO 17 81538 UE199 FLIGHT 9225 TPA/JAX, DURING APPROACH NOSE LANDING GEAR RELAY CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER AND RECYCLED GEAR. NOSE GEAR EXTENDED NORMALLY WITH THREE GREEN. REPLACED LANDING GEAR RELAY. OPERATIONAL CHECK NORMAL. (S) 2 L 7 2 4T RT A24CE 20080825 NM 2008 8 25 AALA200801862 1 20080713 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 780AN 29956 DFW - EMERGENCY LIGHT AT SEAT 27HJ INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 27HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20080825 NM 2008 8 25 AALA200801853 1 20080711 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 790AN 30251 MIA - EMERGENCY LIGHT AT SEAT 21G MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT SEAT 21G. SYSTEM GROUND CHECKED NO RMAL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20080825 SO 2008 8 25 N93A17082008 1 20080817 A 2530 2510006901 OVEN GULSTM G1159 GIV 3980115 SO GALLEY ODOR E N93A H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 13 495QS 1295 OVEN PRODUCED SMOKE. FLIGHT ATTENDANT PULLED CIRCUIT BREAKER. SMOKE DISSIPATED (FOOD BURNT ODOR). OVEN REPLACED AS PR ECAUTION. SUSPECT BURNT FOOD. (S) 2 L 7 2 4F RT A12EA 20080825 EU 2008 8 25 N932008F00002 2 20080815 A 7321 CASC516 REGULATOR GULSTM G1159 GIV 3980115 SO RROYCE TAY TAY6118 EU RT ENG FUEL FLOW MALFUNCTIONED E N93A E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 13 495QS 309 1295 AFTER TAKEOFF RT ENG WOULD NOT RESPOND TO THROTTLE SETTING AND REMAINED AT TAKEOFF POWER. ENG WAS SHUTDOWN. (S) 2 L 7 2 4F 4 F RT A12EA E25NE 20080825 SO 2008 8 25 GUU2008F00042 1 20080616 A 3260 CONTROL MODULE EMB 120 EMB120ER 3260203 SO MLG MALFUNCTIONED A GUUA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 17 285AS 120265 FLIGHT 5402 FLL/FLL. AFTER TAKEOFF, LANDING GEAR LIGHT ON MAP REMAINS ILLUMINATED. REPLACED LANDING GEAR CONTROL MODUL E AND MULTI ALARM PANEL. (S) 2 L 7 2 4T RT A31SO 20080825 EA 2008 8 25 QXEA200800746 1 20080710 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 565 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 612QX 10042 PDX-C4 CHECK. LT OUTBOARD SEAT TRACK HAS CORROSION AND GOUGES AT STATION 565.00. BLENDED CORROSION AND GOUGES. MATERI AL REMOVED IS WITHIN LIMITS. HFEC FOR CRACKS, NONE FOUND. ALODINE AREA IAW REO 670-53-00-013. (S) 2 L 7 2 4F RT A21EA 20080825 SO 2008 8 25 C2XA08ON169 1 20080815 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN ODOR A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 12175 10004 5428 14500878 FLT 7686-ONT- FLIGHT CREW REPORTED SMOKE IN CABIN AREA AND DECLARED EMERGENCY AND PERFORMED AN AIR-RETURN TO ONT, WHERE IT LANDED SAFELY WITHOUT INCIDENT, AND PASSENGERS WERE DE-PLANED SAFELY. MAINTENANCE PERFORMED HIGH POWER RUNS AND COUL D NOT DUPLICATE. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4F RT 20080825 NM 2008 8 25 AALA200801865 1 20080713 A 3350 1158291 SIGN BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 631AA 24589 JFK - EMERGENCY LIGHT SIGN AT RT OVERWING DOOR INOPERATIVE. REPLACED SIGN FOR EMERGENCY LIGHT AT RT OVERWING DOOR. SYS TEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A2NM 20080825 NM 2008 8 25 AALA200801852 1 20080711 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 DFW - EMERGENCY LIGHT AT AFT OVERHEAD GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT AFT OVERHEAD GALLEY. SY STEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20080825 EA 2008 8 25 N6WA0080801 1 20080808 A 3350 BEL40004211 LENS CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT CRACKED A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 164GJ 10256 FLMX-STL. EMERGENCY LIGHT ON LT SIDE AFT OF EMERGENCY EXIT IS CRACKED. REPLACED LENSE IAW MM 33-51-16. (S) 2 L 7 2 4F RT A21EA 20080825 CE 2008 8 25 GUU2008F00040 1 20080809 A 5520 1016200121 HINGE BRACKET BEECH 1900 1900D 1154162 CE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 17 69549 25747 UE194 AT SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT INBOARD ELEVATOR HINGE BRACKET EXFOLIATED. REPLACED LT INBOARD ELEVATOR HINGE BRACKET. (S) 2 L 7 2 4T RT A24CE 20080825 NM 2008 8 25 2008UALA03801 1 20080709 A 2821 FILTER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUEL SYS DIRTY A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 306UA 23667 NR 2 ENG FUEL FILTER BYPASS MSG. RTFL. REPLACED FUEL FILTER. 2 L 7 2 4F 4 F RT A16WE E21EU 20080825 NE 2008 8 25 AALA200801855 2 20080711 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 1 MAKING METAL A AALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SW 21 73444 49470 718547 PHL - INFLIGHT T1415/11JUL - CREW REPORTED LT ENG OIL CLOG INDICATION DURING CLIMB FOLLOWED BY ENG UNCOMMANDED SHUTDOWN. RETURNED TO PHL AND LANDED WITHOUT INCIDENT. SINGLE ENG TIME 15 TO 17 MINUTES. REPLACED NR 1 ENG ON 13 JUL AT PHL DU E TO OIL LEAK AND METAL FOUND IN OIL. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F 4 F A6WE E9NE 20080825 EU 2008 8 25 F3LA200800548 1 20080811 A 5321 D5367303600000 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 806FR 2218 DURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT LT TRANSITION PANEL 161CF WAS DAMAGED. MAINTENANCE REPAIRED D AMAGED PANEL 161CF IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR I T WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT 20080825 NM 2008 8 25 2008UALA03813 1 20080710 A 5753 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT WING TE FLAP DAMAGED A UALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 29 644UA 25094 RIGHT INBOARD MID AND AFT T/E FLAP HAS DAMAGE TO LOWER SURFACE. ALSO LOWER WING PANEL (652CB) WAS PUNCTURED AND HAS INT ERIM REPAIR ACCOMPLISHED. 2 L 7 2 4F 4 F RT A1NM E24NE 20080825 EA 2008 8 25 TRAX200800986 1 20080808 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 686BR 7715 PAX DOOR AFT WEB IS CRACKED IN ZONE 3. REPAIRED PAX DOOR AFT WEB IAW BOMBARDIER REO 601R-52-11-702. SEAL AND PAINT REQ UESTED STEP 11. SEALED AND PAINTED REPAIRED AREA ON PAX DOOR AFT WEB IAW BOMBARDIER REO 601R-52-11-702 STEP 11. COMPLI ED WITH ALL STEPS OF AS EC/TC REO 601R-52-11-702. (S) 2 L 7 2 4F RT A21EA 20080825 NM 2008 8 25 AALA200801850 1 20080711 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM GALLEY MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 787AL 30010 NRT - EMERGENCY LIGHT ASSEMBLY AT LT FIRST CLASS GALLEY MISSING. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LT FIRS T CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20081001 EU 2008 10 1 08FDEA04114 1 20080929 A 5321 A5327608400000 FLOOR PANEL AIRBUS 310 A310222 3930315 EU CABIN DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 MAIN CABIN FLOOR PANEL NR 232 NG IS DAMAGED BETWEEN FRAME 26 AND FRAME 26/32, RBL 18 TO RBL 38. FABRICATED A NEW FLOOR PANEL NR 232 NG IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20081001 EU 2008 10 1 08FDEA04115 1 20080929 A 5321 A2551020300000 FLOOR PANEL AIRBUS 310 A310222 3930315 EU A/C BAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 DETERIORATED/CRACKED CORNERS OF AIR CONDITIONING BAY FLOOR PANEL 143 DF. FABRICATED A NEW FLOOR PANEL NR 143 DF IAW DWG SRZ 25-005, REV "G". 2 L 7 2 4F RT A35EU 20081001 EU 2008 10 1 08FDEA04116 1 20080929 A 5321 B7327060900400 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 MAIN CARGO FLOOR BOARD NR 242 AJ IS CRACKED AT FRAMES 50 - 54. MATERIAL ID FOR THE FLOOR PANEL IAW DWG SRZ 25-005, REV "G" AND ENGINEERING REPORT 91-019 QPL. MATERIAL P/N 402H35039-003, PO 626008.1. FABRICATED A NEW FLOOR PANEL PER DWG SRZ 25-005; REV "G". PAINT IAW AMM 51-23-20-0. 2 L 7 2 4F RT A35EU 20081001 NM 2008 10 1 SWAA085204 1 20080922 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727D + 10 STR 19R. REMOVED AND REPLACED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085202 1 20080923 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 343SW 24151 DURING SCHEDULED C2 CHECK, FOUND SKIN CRACKED AT BS 792, STR 19L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 UPS08M53404 1 20080916 A 5321 WSP0786U501 FLOOR PANEL DOUG MD11 MD11F 3023600 NM CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 282UP 48452 INSPECTION TYPE:2C RCB FLOOR PANEL 7 HAS CORROSION ON UPPER SURFACE. PROCURED NEW FLOOR PANEL. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 UPS08M53403 1 20080915 A 5720 STRAP DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 282UP 48452 INSPECTION TYPE:2C LT WING SPLICE STRAP AT L/E WING STA 683 IS CRACKED. REMOVED, FABRICATED, AND INSTALLED SPLICE STRAP IAW DWG ARB3954 MD-11 SRM 51-35-01, 51-31-01, 51-33-01. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 UPS08553412 1 20080927 A 3350 LIGHT BOEING 757 75724APF 1384969 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 430UP 25461 INSPECTION TYPE:N/A ENTRY DOOR EMERGENCY LIGHT HAS 4 LAMPS OUT. RELAMPED EMERGENCY EXIT SIGN PER AMM 33-51-01-2. 2 L 7 2 4F RT A2NM 20081001 WP 2008 10 1 08FDEA04122 1 20080929 A 5420 AVB70659 FAIRING DOUG MD10 MD1010F 3022112 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 2 ENGINE PYLON LEFT SIDE APRON AT THE RAMP FAIRING IS CRACKED APPROX 10 INCHES. THIS SDR WAS GENERATED TO CORRECT BL OCK 7 ON SDR TRACKING NR 08-3899. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 UPS08553402 1 20080927 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 424UP 25369 INSPECTION TYPE:C2 MCB LBL 45 - LBL 65, BS 1200, FLOORBEAM UPPER SURFACE HAS CORROSION AT FASTENER HOLES. REMOVED CORRO SION AND REPAIRED FLOORBEAM PER ATS ER 08-3012 AND UPS EO B757-5310-30666-A. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 08FDEA04124 1 20080929 A 5220 50797849 RETAINER BOEING 727 727227 1384078 NM DOOR SEAL CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 LT FWD EMERGENCY EXIT HATCH, SEAL RETAINER ON DOOR HAS SEVERAL HOLES CRACKED OUT. REPLACED AFT ATTACH ANGLE. FABRICATE D ATTACH ANGLE REF: DWG NR 50-07978. TREATED, PRIMED AND PAINTED REF:SRM 51-10-2 PG 1-10 AND MM 51-20-151-7 PG 1. INST ALLED REF SRM 51-30-2 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081001 NM 2008 10 1 UPS08553398 1 20080926 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 424UP 25369 INSPECTION TYPE:C2 MCB LBL45, BS 900 - 1040, SEAT TRACK O/B FLANGE UPPER SURFACE HAS CORROSION AT NUMEROUS FASTENER HOLE S. REPAIRED CORRODED SEAT TRACK FLANGE PER UPS EO B757-5310-30643-A. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 UPS08553397 1 20080915 A 5420 SUPPORT CHANNEL BOEING 757 75724APF 1384969 NM NR 2 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 452UP 25473 INSPECTION TYPE:MOD NR 2 PYLON UPPER UNDERWING FAIRING, FWD SUPPORT CHANNEL ASSY IS WORN AND CHAFED. REPLACED FWD SUPPO RT CHANNEL IAW SRM 51-40-02-0G. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 UPS08553392 1 20080916 A 5320 WEB BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 424UP 25369 INSPECTION TYPE:C2 COCKPIT FLOOR HAS CORROSION BS 271 RBL 6.5 WL 208. REPAIRED COCKPIT FLOOR IAW SRM 51-70-13-0G. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 UPS08553387 1 20080915 A 5420 CHANNEL BOEING 757 75724APF 1384969 NM PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 452UP 25473 INSPECTION TYPE:MOD CHANNEL CHAFED. REMOVED AND REPLACED CHANNEL IAW 51-40-02-0G. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 CALA0800923 1 20080922 A 5314 65C385021 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 KEEL BEAM FOUND WITH CORROSION IN FORWARD CARGO AT BODY STATION 500D+8" TO 500D+12.5" AT LBL 6.5". REPAIRED KEEL BEAM P ER B737 SRM 53-60-12, REINSTALLED REMOVED COMPONENTS, PERFORMED LEAK CHECK, NO LEAKS PRESENT AT THIS TIME IAW B737-300 M M 36-19-15. 2 L 7 2 4F RT A16WE 20080825 EA 2008 8 25 A6WA200840554 1 20080730 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 428AW 7695 SUSPICIOUS ODOR IN FRONT OF CABIN, APPEARS ELECTRICAL IN NATURE. DETERMINED ELECTRICAL ODOR COMING FROM POWER UNIT/DIMM ER CEILING LIGHTS B101. REMOVED AND REPLACED CEILING LIGHTS POWER UNIT DIMMER B101 IAW AMM 33-20-04, REMOVED AND REPLAC ED SIDEWALL LIGHTS DIMMER B102 IAW 33-21-10, REMOVED AND REPLACED CEILING LIGHT POWER RELAY IAW AMM 33-21-06, REMOVED AN D REPLACED SIDEWALL LIGHTS POWER RELAY IAW AMM 33-21-12. OPS CHECK GOOD. (S) 2 L 7 2 4F RT A21EA 20080826 NE 2008 8 26 QXEA200800697 2 20080628 A 7261 OIL SYSTEM DHAV DHC8 DHC8202 2809007 NM PWA 120 PW123D 52152 NE NR 1 ENGINE OVERSERVICED A QXEA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 355PH 500 PDX - CREW REPORTS OIL ODOR IN CABIN. FOUND ENGINE OIL FOR NR 1 OVER SERVICED. ADJUSTED LEVEL. GROUND RUN CHECKS OK. RETURNED TO SERVICE. NO PARTS REPLACED. (A) 2 H 7 2 4T 4 T RT A13NM E20NE 20080826 NM 2008 8 26 QXEA200800667 1 20080620 A 5100 NONE BOMBDR DHC8 DHC8402 1390042 NM NOT AN SDR NONE A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 09 408QX 4050 GEG - FLIGHT 2378 - ODOR PRESENT IN FWD CABIN DURING DESCENT. SMELLED LIKE SOLVENT. MAINTENANCE FOUND IT TO BE FROM TH E GARBAGE CAN. REMOVED TRASH AND WASHED TRASH CAN. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. NOT AN SDR 2 H 7 2 4T RT A13NM 20080826 NM 2008 8 26 QXEA200800809 1 20080718 A 3260 327 LAMP DHAV DHC8 DHC8202 2809007 NM MLG INDICATOR MALFUNCTIONED A QXEA O OTHER N FALSE WARNING AP APPROACH 1 NM 09 350PH 488 PDX-FLIGHT 2096 (PDT-PDX). ON APPROACH THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. PERFORMED ALTERNATE EXTENSION AND RECEI VED 3 GREEN LIGHTS. FLEW BY TOWER TO CONFIRM GEAR DOWN. CHECKS OF CFR CALLED. PERFORMED UNEVENTFUL LANDING. MAINTENA NCE REPLACED THE LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 H 7 2 4T RT A13NM 20080826 EA 2008 8 26 QXEA200800696 1 20080629 A 2611 4462534 SMOKE DETECTOR CNDAIR CL600 CL6002C10 1390015 EA LAVATORY MALFUNCTIONED A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 09 617QX 10504 6706 10130 PDX-FLIGHT 2565. ABORTED TAKEOFF AT 100 KNOTS FOR AFT SMOKE DETECTOR CAUTION. RETURN TO GATE. MAINTENANCE INSPECTED A ND FOUND NO OIL, SMOKE OR FLAMES. REPLACED LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. RETURNED TO SERVICE. (A ) 2 L 7 2 4F RT A21EA 20080826 SO 2008 8 26 C2XA08ON161 1 20080802 A 7500 BLEED AIR SYS EMB 145 EMB145XR 3260214 SO ALLSN AE3007 AE3007A 03030 GL WARNING MESSAGE A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 11176 10262 5745 14500881 FLT 7661 -ABQ- FLIGHT CREW REPORTED BLEED 1/2 OVERTEMP. SYSTEM WAS RESET SUCCESSFULLY AS PER MX CTRL. CREW RAN BOTH EN G AND BLEED SYSTEM AND COULD NOT DUPLICATE. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERV ICE. (S) 2 L 7 2 4F 4 F RT TE6CH 20080826 CE 2008 8 26 GUU2008F00030 1 20080809 A 5210 SNUBBER BEECH 1900 1900D 1154162 CE PAX DOOR UNKNOWN A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 16540 UE172 FLIGHT 9237 GHB/FLL, PILOT REPORTED FORWARD DOOR HARD TO PULL. SERVICED AIRSTAIR DOOR SNUBBER. (S) 2 L 7 2 4T RT A24CE 20080826 CE 2008 8 26 GUU2008F00031 1 20080809 A 5210 LOCK BEECH 1900 1900D 1154162 CE PAX DOOR CAM OUT OF ADJUST A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 87550 UE205 FLIGHT 2014 TNT/FLL, PILOT REPORTED MAIN CABIN DOOR DIFFICULT TO OPEN, ONE OR MORE CAM LOCKS OUT OF ALIGNMENT. ADJUSTED TWO LOWER FORWARD CAM LOCKS. (S) 2 L 7 2 4T RT A24CE 20080826 WP 2008 8 26 AALA200801823 1 20080709 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7542A 49996 LGA - EMERGENCY LIGHTS AT REAR SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT REAR SERVICE DOO R. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F A6WE 20080826 EA 2008 8 26 MASA200800467 1 20080613 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX UNKNOWN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 27191 7191 ASH FLT 2722 PHX-SBA. CAPT COULD NOT OPEN THE MAIN CABIN DOOR. MX OPENED THE DOOR WITH NO PROBLEM AND FOUND NO FAULTS AFTER INSPECTING DOOR AND FRAME. (B) 2 L 7 2 4F RT A21EA 20080826 NM 2008 8 26 USAA920081534 1 20080808 A 5320 6545834256 INTERCOSTAL BOEING 737 7373B7 1384580 NM BS 314 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT -Q6- MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL AT BS 314, WL 208, RBL 10. REPLACED INTERCOSTAL AT BS 314, WL 208, RBL 10 IAW BOEING DRAWING 65-45834. (S) 2 L 7 2 4F RT A16WE 20080826 EA 2008 8 26 CHQA200800161 1 20080806 A 2910 601R7528661 LINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE HYD SYSTEM CHAFED A CHQA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 11 486CA 7707 GEE FLIGHT 5723, SDF TO IAH. DURING CRUISE THE CREW RECEIVED A NR1 HYDRAULIC SYSTEM LOW PRESSURE MSG AND THE HYDRAULIC SYNO PTIC PAGE INDICATED ZERO QUANTITY. THE FLIGHT CREW FOLLOWED THE QRH CHECKLISTS AND THEN LANDED AT LIT WITHOUT INCIDENT. MAINTENANCE INSPECTED THE HYDRAULIC SYSTEM AND FOUND THE PRESSURE RETURN LINE AND CASE DRAIN LINES HAD CHAFED THROUGH EACH OTHER IN THE AFT EQUIPMENT BAY. MAINTENANCE REPLACED THE HYDRAULIC LINES, THE NR1 EDP, AND SERVICED THE HYDRAULIC SYSTEM. THERE WERE NO FURTHER LEAKS OR DEFECTS NOTED. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080826 NM 2008 8 26 2008UALA03798 1 20080709 A 5714 PANEL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 955 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 MAIN CABIN STA 955, UPPER SURFACE OF WING BOX PANEL CORRODED AT LBL 36. REMOVED CORROSION DAMAGE TO CENTER WING BOX PAN EL AT LBL36, TRIMMED THE FLOORBEAM LOWER CHORD AND THE UPPER WING SKIN. FABRICATED A FILLER FOR THE WING SKIN CUT-OUT, A -1 AND -4 FILLER, -2 DOUBLER, AND -3 TRIPLER AND I NSTALLED. REPAIRED THE REAR SPAR UPPER CHORD WITH A REPAIR ANGLE, SP LICE REPAIRED THE 85625 LOWER CHORD AND FABBED AND INSTALLED FLOOR BEAM SPLICE FITTINGS AND FLOORBEAM WEB DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 20080826 SO 2008 8 26 RAIA00808008 1 20080806 A 3240 429513 CONTROL UNIT EMB 145 EMB145LR 3260212 SO BRAKE SYSTEM WEAK A RAIA O OTHER J WARNING INDICATION LD LANDING 1 CE 03 814HK 19885 19885 145046 FLT 5598 -MIA- ON LANDING, CREW REPORTED THAT THE INBOARD BRAKES WERE INEFFECTIVE AND THAT THE OUTBOARD BRAKES WERE OVER HEATING. MAINTENANCE REMOVED AND REPLACED THE BRAKE CONTROL UNIT AND THE NR 4 BRAKE ASSEMBLY. (S) 2 L 7 2 4T RT T00011AT 20080826 WP 2008 8 26 NWAA083569853 1 20080731 A 2710 PULLEY DOUG DC9 DC951 3022051 WP AILERONS DEFECTIVE A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 762NC 47710 FLIGHT RETURNED TO A SAFE LANDING AT DTW AFTER CREW DETERMINED AILERONS WERE BINDING DURING LT TURNS. CONTROL CHECK WAS NORMAL ON THE GROUND BOTH BEFORE TAKEOFF AND DURING TAXI IN AFTER RETURN. LT TURNS REQUIRED THE MOST EFFORT BUT AILERO N CONTROL WAS DIFFICULT IN BOTH DIRECTIONS AND ROLL RESPONSE WAS NOTABLY SLOW WITH AUTOPILOT ENGAGED. MAINTENANCE REPLA CED A DEFECTIVE AILERON CONTROL PULLEY IN THE RT WING. CABLE TENSION AND RIG WAS ACCOMPLISHED AND THE SYSTEM RETURNED T O OPERATIONAL CONDITION. (S) 2 L 7 2 4F RT A6WE 20080826 EU 2008 8 26 COEA0803816 1 20080805 A 7160 FLANGE AEROSP ATR72 ATR72212 8680945 EU LT INTAKE DUCT CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 816FX 347 LEVEL 2 CORROSION: LT WING FUEL OVERFLOW/VENT TANK NACA DUCT (AIR INTAKE DUCT) FLANGE HAS AREAS OF SURFACE CORROSION. CORROSION BLENDOUT TO MATTING SURFACE OF FLANGE WAS BLENDED BEYOND SRM LIMITS. REMOVED & REPLACED DUCT ASSEMBLY. (S) 2 H 7 2 4T RT A53EU 20080826 NM 2008 8 26 2008UALA03771 1 20080708 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1540 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 AFT PIT LT SIDE SLANT AREA HAS DENTED FRAME STA 1540 AT STR 26L. *S/D* ACCOMPLISHED A MAJOR REPAIR AT GSO. RPR FRAME IAW SRM 53-00-07 RPR 5 DETAIL I. THIS IS A CAT B RPR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSPECTIONS STARTING AT 50,000 C AND 12,000C THEREAFTER PER SRM 53-00-07 RPR 5 TABLE II. THIS INSP CONSISTS OF BOTH DETAILED VISUAL AND NDT. CURRENT PTC IS 20699. 2 L 7 2 4F 4 F RT A2NM E17NE 20080826 NM 2008 8 26 2008UALA03773 1 20080708 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1440 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 AFT PIT FRAME DENTED AT INBOARD FLANGE BS 1440, STR 26L. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. RPR FRAME IAW SRM 53 -00-07 RPR 5 DETAIL I. THIS IS A CAT B RPR IN ZONE 1 AND REQUIRES SUPPLEMENTAL INSPECTIONS STARTING AT 50,000C AND 12,0 00C THEREAFTER PER SRM 53-00-07 RPR 5 TABLE II. THIS INSP CONSISTS OF BOTH DETAILED VISUAL AND NDT. CURRENT PTC IS 206 99. 2 L 7 2 4F 4 F RT A2NM E17NE 20080826 WP 2008 8 26 IXX2008F00079 1 20080610 A 5730 SKIN DOUG DC8 DC872F 302199E WP LT WING MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON LT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095. 000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED A ND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-3-2 FIGURE 10 PAGE 22 ITEM "F", DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-3-0, AND SRM 51-31-1. (S) 2 L 7 4 4F RT 4A25 20080826 NM 2008 8 26 UIEA200800281A 1 20080814 A 5730 PANEL BOEING 747 7472D7B 1384803 NM RT WING CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 522MC 21783 RT WING UPPER AFT TRAILING EDGE PANEL, OUTBOARD OF INBOARD AILERON HAS 2 EACH SMALL COMPOSITE CRACKS AT WBL 445.00. FOR WARD CRACK IS .500 INCH LONG AND AFT CRACK IS 1.0 INCH LONG. PERMANENT REPAIR ACCOMPLISHED AS PER 747-200 SRM 51-40-09 FIG 2, SHEETS 2 AND 5, PREPREG LAYUP 250 DEGREES F CURE PER SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO 4757A456. (S) 2 L 7 4 4F RT A20WE 20080826 EA 2008 8 26 TRAX200800782 1 20080612 A 3350 BULB CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 752EV 10166 CEILING EMERGENCY LIGHT SECOND FROM FRONT INOP. REMOVED AND REPLACED SECOND FROM FRONT CEILING EMERGENCY LIGHT BULB. O PS CHECK GOOD. 2 L 7 2 4F RT A21EA 20080826 NE 2008 8 26 YENA2008079 2 20080814 A 7200 4W5198 POWERPLANT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 FLAMED OUT A YENA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION LD LANDING 1 EA 15 715JB 259 259 3554 V12980 FLT 354, BUR-JFK, UPON LANDING NR 1 ENG FLAMED OUT ON ROLL OUT, AFTER ENG 1 COMP FAIL ECAM FOLLOWED BY ENG 1 FAIL ECAM. DVDR ANALYSIS DETERMINED NR1 ENG REQUIRES ENG REPLACEMENT DUE TO EGT OVERLIMIT. REMOVED AND REPLACED NR1 ENG PER TC A3 20-71-00-20-400-040. OPS CHECK OK. (S) 2 L 7 2 4F 4 F RT A28NM E40NE 20080826 NM 2008 8 26 KCSA081396 1 20080816 A 5420 STIFFENER BOEING 747 747122 1384872 NM NR 1 NACELLE WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 NR 1 PYLON DUCT SUPPORT STIFFENER WORN AT DUCT LINK OUTBOARD SIDE OF SPAR AT NAC STA 198. (S) 2 L 7 4 4F RT A20WE 20080822 NM 2008 8 22 F3LA200800464 1 20080711 A 5321 D5367413300000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CFMINT CFM56 CFM565B5 NE CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 940FR 2465 DURING C-CHECK INSP NOTED FWD PIT PANEL 131EG DAMAGED. MAINT REPAIRED DAMAGE IAW SRM 53-02-00 FIGURE 204. UPON COMPLETIO N OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B) 2 L 7 2 4F 4 F RT A28NM E37NE 20080822 NM 2008 8 22 F3LA200800532 1 20080731 A 5321 D5367324200000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 927FR 2 2209 DURING C-CHECK, INSP NOTED THE AFT PIT FLOOR PANEL, 151VG, WAS DAMAGED. MAINT REPAIRED THE PUNCTURE DAMAGE IN FLOOR PAN EL 151VG IAW SRM 53-02-00 FIGURE 204. MAINT PAINTED THE FLOOR PANEL IAW THE REQUIREMENTS OF AMM 25-00-00-370-001. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080822 NM 2008 8 22 MZZA0800001 1 20080705 A 2560 ACREM1A MEGAPHONE BOEING 737 737824 13844BZ NM CABIN INOPERATIVE A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 14228 28792 AFT MEGAPHONE INOP. REMOVED AND REPLACED 1 EA MEGAPHONE AS REQ'D, IAW AMM 25-64-00. 2 L 7 2 4F RT A16WE 20080822 GL 2008 8 22 SIMA200817801 2 20080623 A 7200 23072309 CARBON SEAL EMB 135 EMB135LR 3260305 SO ALLSN AE3007 AE3007A 03030 GL NR 1 ENGINE LEAKING A SIMA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 716AE 145264 ON FLIGHT 4788 - CREW REPORTED ON A FOUL ODOR COMING BLEED SYSTEM ESPECIALLY ON CLIMB AND DESCENT. ODOR RESIDUE WAS STI LL PRESENT IN COCKPIT ON THE GROUND. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ENGINE 1 ZERO CARBON SEAL. L EAKS AND NO ODOR NOTED AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080822 SO 2008 8 22 SIM2008F00014 1 20080602 A 3350 20131A BATTERY PACK EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT DISCHARGED A SIMA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 704PG 145174 ON FLIGHT 4859 - CREW NOTED ON GROUND THAT SEVERAL EMERGENCY LIGHTS WILL NOT ILLUMINATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 EMERGENCY BATTERY IAW AE WC NR 33-700-19. OPERATIONAL CHECK GOOD NO OTHER DEFECTS NOTED. A IRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080822 EA 2008 8 22 SIMA200817502 1 20080620 A 2150 GG6709500095 ACM CNDAIR CL600 CL6002C10 1390015 EA RIGHT SEIZED A SIMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 500AE 10025 ON FLIGHT 3661 - CREW REPORTED ON TAXI OUT PAX CABIN FILLED UP WITH SMOKE. AIRCRAFT RETURNED TO GATE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RT ACM IAW AMM 21-51-08. OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4F RT A21EA 20080822 NM 2008 8 22 AALA200801832 1 20080604 A 5315 141T5113 FLOORBEAM BOEING 767 767223 1385123 NM BS 325 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 327AA 22327 AFW - FLOORBEAM UPPER CAP AT STATION 325 HAD CORROSION. REMOVED FROM THE HORIZONTAL FLANGES FROM RT BUTTLINE 11 TO RT B UTTLINE 50. REPAIRED PER MRB 767-3220. (S) 2 L 7 2 4F RT A1NM 20080822 2008 8 22 SIMA200822203 2 20080808 A 7200 ENGINE EMB 145 EMB145LR 3260212 SO NR 2 MALFUNCTIONED A SIMA O OTHER R P PARTIAL RPM/PWR LOSS NO WARNING INDICATION NR NOT REPORTED 1 SW 21 638AE 145172 ON FLIGHT 3457 - CREW REPORTED TWO TIMES DURING FLIGHT E2 N1 DROPPED TO IDLE (N1-60 PRECENT AND N1-72-73 PERCENT) WITH N O INDICATION ON EICAS. (S) 2 L 7 2 4T RT T00011AT 20080822 2008 8 22 AALA200801821 4 20080709 A 2210 2589445933 ACTUATOR DOUG DC9 DC982 3022082 WP YAW DAMPER FAILED A AALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 21 466AA 49596 DFW INFLIGHT T1767/09JUL. CREW REPORTED YAW DAMPER FAILED ON CLIMB. FLIGHT GUIDANCE CIRCUIT BREAKER POPPED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED YAW DAMPER ACTUATOR. REPLACED LT AILERON SENSOR, LT ELEVATOR SENSOR AND D IGITAL FLIGHT GUIDANCE CIRCUIT BREAKER C17 AS PRECAUTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F A6WE 20080822 EA 2008 8 22 COMA086348 1 20080809 A 5330 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 965CA 7131 LT INTERNAL SKIN DOUBLER AT STA 640 IS CRACKED. FABRICATED PARTS AT STA 640 IAW CRJ REO 601R-53-61-506. (S) 2 L 7 2 4F RT A21EA 20080825 EU 2008 8 25 NSV2008F00018 1 20080810 A 2611 CONNECTOR SAAB SF340 340B 7860101 EU SMOKE DETECTOR UNKNOWN A NSVA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 27 202SR 340B202 AVIONICS SMOKE LIGHT CAME ON INFLIGHT FOR A FEW SECONDS. RESET CONNECTOR TO SMOKE DETECTOR IAW SAAB AMM 28-13-00. OPS CHECKED GOOD. (S) 2 L 7 2 4T RT A52EU 20080825 SO 2008 8 25 CHQA200800162 1 20080809 A 3350 78241 INVERTER EMB 135 EMB135LR 3260305 SO ALLSN AE3007 AE3007A 03030 GL EMERGENCY LIGHTS INOPERATIVE A CHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 834SK 145596 CAE311920 MAINTENANCE FOUND THE EMERGENCY EXIT SIGN NEXT TO THE RT OVERWING EXIT INOPERATIVE. THROUGH TROUBLESHOOTING, THE NR 5 I NVERTER WAS FOUND TO BE THE CAUSE OF THE FAULT. THE INVERTER WAS REPLACED AND THE EMERGENCY LIGHT OPERATED NORMALLY. ( S) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080825 NM 2008 8 25 UIEA200800271 1 20080731 A 5330 SKIN BOEING 747 74747UF 1384812 NM BS 2618 S46R DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 493MC 29254 DURING WALKAROUND DAMAGE FOUND AT TAIL POST AREA BS 2618 STRINGER 46R. PART 1 INTERIM REPAIR ACCOMPLISHED IAW EO 4453A1 39. PART 2 INITIAL HFEC AT NEXT "A" CHECK. PART 3 REPEAT INSPECTION DVI AT EVERY "A" CHECK. PART 4 PERMANENT REPAIR A T NEXT "C" CHECK. (S) 2 L 7 4 4F RT A20WE 20080825 NM 2008 8 25 2008UALA03839 1 20080710 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 542UA 25276 R2 DOOR LOWER GATE CORRODED AND CRACKED. REPLACED LWR GATE PER MM 52-11-38. 2 L 7 2 4F 4 F RT A2NM E17NE 20080825 NM 2008 8 25 AALA200801822 1 20080709 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 374AA 25201 JFK - EMERGENCY LIGHT SIGNS AT NR 2 EXIT DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT SIGNS AT NR 2 EXI T DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A1NM 20080825 NM 2008 8 25 KCSA081378A 1 20080811 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 460 S12R CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 BS 460 ABOVE S12R APPROX 1 INCH, FRAME OUTBOARD FLANGE CRACKED AT FASTENER HOLE. CRACK .250 INCH LONG. MARKED UPPER DE CK. (S) 2 L 7 4 4F RT A20WE 20080825 EU 2008 8 25 QML2008F00007 1 20080812 A 2435 150SG122Q STARTER GEN SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL2B 60037 NE ENGINE DISINTEGRATED E QMLA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 03 104LN 420 420 4094 23285 GENERATOR LIGHT ILLUMINATED JUST AFTER TAKE OFF FOR AN NVG TRAINING FLIGHT, WITH AN ELECTRICAL BURNING/OZONE ODOR IN THE COCKPIT. THE PILOT RETURNED TO BASE AND LANDED WITHOUT FURTHER INCIDENT. ELECTRICAL ODOR DISPERSED BEFORE LANDING. U PON INSPECTION OF THE STARTER/GENERATOR, MAINTENANCE FOUND CARBON BRUSH AND COPPER METAL DEBRIS COVERING THE ENG DECK. THE STARTER/GENERATOR WAS REMOVED AND BRUSH AREA INSPECTED. FOUND THE FAN SHROUD TO BE SPOTWELDED TO A SINGLE BRUSH RET AINING SPRING. REMOVED THE FAN SHROUD AND FOUND ALL BRUSHES HAD BEEN DESTROYED WITH CONNECTING WIRES PULLED AND PROTRUD ING THROUGH THE BRUSH GUIDES ON THE COMMUTATOR SIDE. UPON FURTHER INSPECTION, IT WAS FOUND THAT 2 COMMUTATOR SEGMENTS H 1 G 7 1 3U 3 U H9EU E00054EN 20080825 NM 2008 8 25 USAA920081509 1 20080731 A 5310 D53472172205 BEAM AIRBUS A319 A319132 3930340 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 833AW 1844 SAL -BC4- MAJOR REPAIR - GALVANIC CORROSION ON BEAM AT FR69, -Y1180. REPLACED BEAM AT FR69, -Y1180 IAW A319 SRM 51-42-1 1. (S) 2 L 7 2 4F RT A28NM 20080825 NM 2008 8 25 2008UALA03845 1 20080707 A 3150 WARNING MESSAGE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 798UA 26928 FUEL IMBALANCE MSG DISPLAYED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080825 EA 2008 8 25 HNAA08A0005 1 20080612 A 5340 BRACKET DHAV DHC8 DHC8311 1386006 EA PAX DOOR CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 335EN 375 CORROSION PAX DOOR BOTTOM BRACKET ZED SUPPORT FWD AND AFT FOUND CORRODED. REPLACED PAX DOOR BOTTOM BRACKET. (S) 2 H 7 2 4T RT A13NM 20080825 EA 2008 8 25 QXEA200800739 1 20080710 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 427 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 612QX 10042 PDX - C4 CHECK. LT OUTBOARD SEAT TRACK HAS CORROSION AND GOUGES AT STATION 427.00. BLENDED CORROSION AND GOUGES. MATE RIAL REMOVED IS WITHIN LIMITS. HFEC FOR CRACKS, NONE FOUND. ALODINE AREA IAW REO 670-53-00-013. (S) 2 L 7 2 4F RT A21EA 20080825 EA 2008 8 25 QXEA200800741 1 20080710 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 460 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 612QX 10042 PDX - C4 CHECK. LT OUTBOARD SEAT TRACK HAS CORROSION AND GOUGES AT STATION 460.00. BLENDED CORROSION AND GOUGES. MATE RIAL REMOVED IS WITHIN LIMITS. HFEC FOR CRACKS, NONE FOUND. ALODINE AREA IAW REO 670-53-00-013. (S) 2 L 7 2 4F RT A21EA 20081001 NM 2008 10 1 CALA0800922 1 20080925 A 5320 65C33970 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 FORWARD WET AREA CROSSBRACE CRACKED AT FLOORBOARD ATTACH HOLES BETWEEN STATION 360-380 LBL 12. ORIGINAL DAMAGE WAS TO I NTERCOSTAL LOCATED AT LBL 12 BETWEEN BODY STATIONS 344-360, REMOVED DAMAGE TO UPPER FLANGE OF INTERCOSTAL AT LBL 12 BETW EEN BS 344 TO BS 360. FABRICATED AND INSTALLED REPAIR PER 737-500 SRM 51-70-11 FIG 1. 2 L 7 2 4F RT A16WE 20081001 2008 10 1 SWAA085232 4 20080925 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 765SW 29805 FOUND R1 DOOR EMERGENCY ESCAPE SLIDE LOOSE. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085231 1 20080925 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT FWD FUSE BS 400, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085229 1 20080925 A 2560 65C34691 GIRT BAR BOEING 737 7377H4 1384404 NM EVAC SLIDE OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 453WN 29847 DURING SCHEDULED HC1 CHECK, FOUND L1 SLIDE DOOR GIRT BAR OUT OF ADJUST. ADJUSTED GIRT BAR PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085222 1 20080924 A 2560 P2070001 SEAL BOEING 737 7373H4 1384600 NM FLASHLIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 DURING SCHEDULED C2 CHECK, FOUND AFT INBOARD FLASHLIGHT SEAL BROKEN. REMOVED AND REPLACED SEAL PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085221 1 20080924 A 2560 65C34691 GIRT BAR BOEING 737 7373H4 1384600 NM EVAC SLIDE OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EMERGENCY ESCAPE SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED GIRT BAR PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 ASAA0853532 1 20080925 A 4990 38809381 OIL FILTER BOEING 737 737890 1384527 NM APU FAULTY A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 583AS P7571 35681 WHILE ACCOMPLISHING TC 78349013 FOUND APU OIL FILTER DELTA P INDICATOR EXTENDED. REMOVED AND REPLACED APU OIL FILTER, N O CONTAMINATION NOTED. INSPECTED MAGNETIC DRAIN PLUG, NO CONTAMINATION NOTED. RAN APU FOR 15 MINS. NO LEAKS NOTED. G ROUND VERIFICATION SUCCESSFUL. REF AMM'S49 91 13 & 49 91 81 & EMM 05 00 05. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 ASAA0853535 1 20080926 A 2421 7588429101 OIL FILTER BOEING 737 737890 1384527 NM NR 1 IDG FAULTY A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 577AS AAAH004892 35186 FOUND NR 1 ENG IDG DPI POPPED, RESET DPI PER 24 11 41. REMOVED AND REPLACED SCAVENGE AND CHARGE FILTER PER SAME REF. S ERVICED TO FULL PER 12 13 21, RAN ENGINE FOR 5 MIN. NO LEAK, STAYS RESET. 2 L 7 2 4F RT A16WE 20081001 2008 10 1 ASAA0853534 4 20080925 A 2210 2A7206B AUTOPILOT SYS BOEING 737 737890 1384527 NM COCKPIT MALFUNCTIONED A ASAA K NONE F FLT CONT AFFECTED AP APPROACH 1 NM 02 577AS 6071 35186 DURING AUTOLAND APPROACH AUTOPILOT DID NOT MAINTAIN GLIDE SLOPE. FCC'S FLT FAULT REVIEW SHOWS FOR FLT DISCEP OCCURRED: MAIN ELEC TRIM TRIM RELAY CHAN A MSG 22 1208. PERFORMED FIM 22 13 TASK 818 WITH INTERMITTANT FAULT. SPEED STAB CHAN B ITE 20.32 AND LAND VERIFY TEST NR 49 REF FIM 22 11 TASK 801, ALL GOOD. 2 L 7 2 4F RT A16WE 20081001 SO 2008 10 1 SWIA200820075 1 20080917 A 3350 SIGN EMB 120 EMB120ER 3260203 SO CABIN BROKEN A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 295UX 120295 EMERGENCY EXIT SIGN AT 6C BROKEN. FLT 5493. REPLACED SIGN. 2 L 7 2 4T RT A31SO 20081001 NM 2008 10 1 UPS08M53379 1 20080922 A 5330 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:N/A, DENT AND CRACK DAMAGE FOUND ON FUSELAGE SKIN AT STA 1741 TO STA 1761 L LT, LONGERON 38 AND 39. DAM AGED AREA TRIMMED OUT, LENGTH = 12" X WIDTH = 5.5" AND REPAIRED AS PER SRM 53-20-00 FIG 2, VOL I, REV 40, AND UPS EO MD1 1-5330-18894C. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 ZZDA2008159 1 20080919 A 5320 J0622803 THRESHOLD BOEING 717 717200 1383700 NM CARGO BAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 954AT 55016 FWD CARGO DOOR THRESHOLD CORRODED BEYOND LIMITS. REPAIRED PER B717 SRM 53-20-15, INSTALLED NEW PAN. 2 L 7 2 4F TR A6WE 20081001 NM 2008 10 1 SWAA085166 1 20080923 A 5322 6545765 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CRACKED AT STA 540, LBL 40, WL 206. REPAIR SHEAR TIME PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085165 1 20080922 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 L1 DOOR EMERGENCY EXIT SIGN BROKEN. REPAIRED SIGN PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085164 1 20080922 A 3350 10107451 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT 8 DEF. REMOVED AND REPLACED BATTERY PACK PER AMM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085159 1 20080920 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 727D + 10, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085157 1 20080923 A 5314 6547978 BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND LT BEAM WEB CORRODED AT STA 500C TO 500D. REPAIRED WEB BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085156 1 20080923 A 5320 6545819 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND NLG WHEEL WEB CRACKED AT LBL 7.75. REPAIRED WEB PER SWA ACO. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 2008UALA05846 1 20080922 A 3320 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LIGHT SHORTED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 179UA 25158 AFT CEILING LIGHT IN AFT AUX GALLEY SHORTED OUT CAUSING BURN MARKS ON CEILING PULLED. REPLACED LIGHT ASSY AND CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081001 NM 2008 10 1 2008UALA05847 1 20080923 A 5320 ANGLE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE BS 1600 DAMAGED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 774UA 26936 2 ANGLE SIDE PANELS AT STA 1600 DAMAGED. REPLACED SIDE PANELS AT STA 1600 AS REQUIRED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081001 2008 10 1 SWAA085189 4 20080919 A 2565 6567380 COVER BOEING 737 7373T0 1384582 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 R1 EMERGENCY EXIT SLIDE COVER LOOSE. REPOSITIONED COVER PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085188 1 20080919 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 673AA 23251 DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT STA 939, STR 21R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080929 NM 2008 9 29 2008UALA05844 1 20080919 A 3350 5872158731 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 EMERGENCY ESCAPE PATH LIGHTING IS LOOSE IN THE AFT SECTION OF ECONOMY CLASS. REMOVED AND REPLACED UPPER & LOWER EEL TRA CK AND COVER. EEL LIGHTS OP CHECK OKAY. 2 L 7 2 4F 4 F RT A16WE E2GL 20080929 NM 2008 9 29 DL77L081204 1 20080919 A 2421 IDG BOEING 777 777232 1385232 NM NR 1 MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 702DN 29741 LT GEN DRIVE LIGHT ILLUMINATED WITH GEN OFF LIGHT ILLUM AFTER PUSHBACK SERVICED LT IDG. NO HELP. PLACED L GEN INOP PER MEL 24-11-01. MAINT ACTION C/W. REMOVED AND REPLACED LEFT IDG PER MM OPS CK OK MCO AND PLAC REMOVED. 2 L 7 2 4F RT T00001SE 20080929 NE 2008 9 29 DL76L081206 2 20080921 A 7320 EEC BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 180DN 25985 724314 AFTER LEFT ENG START, LT ENG CONTROL STATUS MSG APPEARED FOLLOWED BY LT ENG C2 STATUS MSG. PERFORMED LT ENG PIMU READOU T. FOUND BITE MSG CH-A LOST POWER AND CH-B UNIT FAIL. CYCLED EEC C/B AND PIMU RESET. ALL MESSAGES CLEARED. RAN LT EN G IN DLE AND NO FAULTS APPEARED. AFTER ENG RUN RECHECKED LT PIMU BITE READOUT. NO FAULTS SHOWN. 2 L 7 2 4F 4 F RT A1NM E24NE 20080929 NE 2008 9 29 DL76L081207 2 20080920 A 7320 ROTOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE PMA DRIVE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 198DN 28455 727738 RT ENG EEC MSG, AUTO THROTTLES INOP, RT CTR FUEL PUMP, NO RT ENG N2 DISPLAY. ALL OCCURRED INFLT EN ROUTE TO CVG. FOUND PMA ROTOR DAMAGED DUE TO DRIVE ASSY FAILURE. BEARING PIECES MISSING AND PRESUMED TO HAVE ENTERED THE GEARBOX WHEN BEAR ING FAILED. METAL ON THE MCD. WILL CHANGE ENG TO FACILITATE GEARBOX REPLACEMENT. 2 L 7 2 4F 4 F RT A1NM E24NE 20080929 NE 2008 9 29 DL76P081209 2 20080921 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 BIRD INGESTION A DALA A UNSCHED LANDING C J F.O.D. WARNING INDICATION CL CLIMB 1 SO 27 143DA 48117 6863 25991 724139 DURING T/O HAD BIRDSTRIKE ON LEFT SIDE OF AIRCRAFT. RETURNED MCO. MTC FOUND DENT IN FUSELAGE FWD OF LEFT PITOT PROBES. AOA VANE SHEARED OFF. PITOT PROBES IMPACTED. LEFT ENGINE HAS 2 FAN BLADES BENT OUT OF LIMITS AND SOME MINOR ACOUSTIC AL LINER DAMAGED. VISUAL AND HPC BORO INSP REF MM 72-00-00-206-24. NO DISCREPANCIES NOTED. REPLACED LT AOA SENSOR PER AMM. INSP AREA PER SRM 51-10-03 AREA IS WITHIN LIMITS. REPLACED BLADE 7 8 26 AND 27 PER MM. ENG RUN VIBE CHKS NML. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 UPS08M53143 1 20080814 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 14 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080930 NM 2008 9 30 CALA0800808 1 20080822 A 5311 6546596 FRAME BOEING 737 737524 1384721 NM BS 727B S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 BODY STATION 727B LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN S8L AND S9L. REPAIRED CRACKED FRAME AT STATION 727B AT A/C BRACKET BETWEEN STR 8 AND S9 LEFT PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800810 1 20080822 A 5311 6546596 FRAME BOEING 737 737524 1384721 NM BS 727B S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 BODY STATION 727B RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN S8R AND S9R. REPAIRED CRACKED FRAME AT RIGHT SIDE BODY STATION 727B BETWEEN S8R AND S9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800811 1 20080822 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM BS 867 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 BODY STATION 867 RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND STR 9. REPAIRED CRACKED FR AME AT STATION 867 RIGHT AT AC BRACKET BETWEEN STA 8 AND 9 PER EA 5310-04498 OP2. 2 L 7 2 4F RT A16WE 20080825 EU 2008 8 25 F3LA200800546 1 20080811 A 5321 D5367520100000 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 806FR 30 2218 DURING C3 C-CHECK, INSPECTION NOTED THE FORWARD CARGO PIT FORWARD FLOOR PANEL 131AF HAS SEVERAL HOLES. MAINTENANCE REPA IRED DAMAGED PANEL 131AF IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPH 8C, FIGURE 204. UPON COMPLETION OF THE RE PAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT 20080825 CE 2008 8 25 DXTA200803234 1 20080818 A 3240 BRAKE CESSNA 500 560CESSNA 2076750 CE MLG INOPERATIVE E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 844QS 5600629 LOSS OF BRAKES ON TAXI INTO PARKING. REQUIRED USE OF EMERGENCY BRAKES. (S) 2 L 7 2 4F RT A22CE 20080825 NM 2008 8 25 2008UALA03808 1 20080709 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 540 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 FWD PIT STA 540 LT SIDE FRAME DENTED ABOVE SPLICE STR 25L. *S/D* ACCOMPLISHED MAJOR REPAIR AT GSO. CUT OUT DAMAGE AND INSTALLED DOUBLER RPR PER REO-G12385 REV B, AND EVA-71745. 2 L 7 2 4F 4 F RT A2NM E17NE 20080826 EU 2008 8 26 COEA0803742 1 20080728 A 7712 1004PGSB TRANSMITTER FOKKER F27 F27MK600 4990706 EU ENGINE TORQUE FAILED A COEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 13 742FE 1202 10349 ABORTED TAKEOFF. FLIGHT 100 GEG. ABORTED TAKEOFF DUE TO LOSS OF TORQUE INDICATION ON LT ENGINE. TAXIED AIRCRAFT BACK TO RAMP WITHOUT INCIDENT. REMOVED AND REPLACED THE LT ENGINE TORQUE TRANSMITTER. (A) 2 H 7 2 4T A817 20080826 WP 2008 8 26 AALA200801828 1 20080709 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 594AA 53284 LGA - EMERGENCY LIGHTS AT SEAT ROWS 7DEF TO 9DEF INOPERATIVE. REPLACED BATTERY PACK AT B5 102 FOR EMERGENCY LIGHTS AT S EAT ROWS 7DEF TO 9DEF. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A6WE 20080826 EU 2008 8 26 USAA920081508 1 20080808 A 2530 112251 COFFEEMAKER AIRBUS A319 A319112 3930323 EU GALLEY SMOKE A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 714US 1046 FLT 981, SMOKE CAME OUT FWD COFFEEMAKER WHEN TURNED ON. R & R FORWARD COFFEEMAKER. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20080826 NM 2008 8 26 2008UALA03776 1 20080708 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1681 S16-18R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 FRAME AT BS 1681 BETWEEN STR'S 16 - 18R HAS DAMAGE. ACCOMPLISHED A MAJOR REPAIR AT GSO. AT HMV-2 A FRAME REPAIR WAS ACP AT BS 1681 BETWEEN S16 -18R PER EVA IMC-20468A. DUE TO BACO DTA RESULTS IT HAS BEEN DETERMINED THAT THIS REPAIR IS TIM E LIMITED TO 24 MO'S AND NOT TO EXCEED 2000 FLT CYC'S FROM HMV-2 WHICH WAS AT 07SEP2002 WITH PTT=39131 & PTC=11700. PER EVA IMC-20468 REV B, REMOVE OLD REPAIR AND REPLACE WITH NEW REPAIR PRIOR TO 24 MO'S FROM 07SEP2002 OR 13700 CYC'S, WHIC HEVER COMES FIRST, NOTE EVA REPAIR INSTRUCTIONS. -INF- :MF3134 CREATED TO RECHECK AT EVERY C CHECK. PERMANENT REPAIR AT HMV 3 SCHEDULED FOR 04SEP0 8 PER EVA IMC 20468 REV C. 2 L 7 2 4F 4 F RT A2NM E17NE 20080826 WP 2008 8 26 IXX2008F00071 1 20080611 A 5313 LONGERON DOUG DC8 DC872F 302199E WP BS 1610 L17R CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C-CHECK INSPECTION, FOUND AFT FUSELAGE CRACKED AT STATION FS 1610.000 LONGERON 17 RT. REMOVED DAMAGED LO NGERON. CLEANED, TREATED AND PRIMED AREA. INSTALLED LONGERON. IAW DC8 SRM 53-5-2 FIGURE 5 SHEET 1 PAGE 16 ITEM "B", D C8 SRM 51-1-8B, DC8 SRM 53-1-0 PAGE 1, SRM 51-1-21, 51-1-20D, SRM 51-2-0 FIGURE 50 SHEET 37, 51-3-0, AND SRM 51-3-1. (S ) 2 L 7 4 4F RT 4A25 20080826 EA 2008 8 26 TRAX200800804 1 20080618 A 3397 WIRE CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 NR 1 EMERGENCY LIGHT POWER SUPPLY CONNECTOR HAS A BROKEN WIRE. JOB COMPLETED. REPAIRED BROKEN WIRE AND INSTALLED NEW B ACKSHELL ON PLUG JB11AP1 IAW CRJ 700 EEC-SPM 20-44-05. OPS CHECK OF EMERGENCY LIGHTS GOOD, NO DEFECTS NOTED JA 7015230. 2 L 7 2 4F RT A21EA 20080826 NM 2008 8 26 USAA920081536 1 20080815 A 5512 65C27494 SKIN BOEING 737 7373B7 1384580 NM ZONE 300 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT-Q6 -MAJOR REPAIR - CRACK ON LT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 138.7 AND 147.9. REPAIRED LT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 138.7 AND 147.9 IAW US AIRWAYS EA 100592. (S) 2 L 7 2 4F RT A16WE 20080826 NM 2008 8 26 USAA920081537 1 20080817 A 5330 6545775 SKIN BOEING 737 7373S3 1384711 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 PHX- DAILY -MAJOR REPAIR- FUSELAGE SKIN CRACKED AT BS 727E S22R. REPAIRED FUSELAGE SKIN AT BS 727E S22R IAW B737 SRM TE MPORARY REVISION 53-33 REPAIR 31. (S) 2 L 7 2 4F RT A16WE 20080826 EA 2008 8 26 TRAX200800778 1 20080611 A 2910 LINE CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM FAILED A ASOA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 847AS 7335 HYDRAULIC SYSTEM 3 LOST ALL FLUID WHEN GEAR EXTENDED. EMERGENCY DECLARED, EMERGENCY TRUCKS FOLLOWED A/C TO THE GATE. R EMOVED AND REPLACED 3B HYDRAULIC PUMP PRESSURE LINE IAW CRJ 200 AMM 29-12-18. OPS AND LEAK CK GOOD. LINE P/N AE4096G00 60-000. 2 L 7 2 4F RT A21EA 20080826 NM 2008 8 26 2008UALA03365 1 20080612 A 2780 654W00382 FSEU BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE LE FLAPS FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 786UA 26938 EICAS STATUS MESSAGE FLAP SLAT CONTROL 2 SHOWS ON STATUS PAGE. *S/D* SUSPECT FAULTY FLAP-SLAT ELECTRONIC UNIT. REPLAC ED NR 2 FSEU, OPS CHECKED GOOD IAW MM 27-51-01. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080826 NM 2008 8 26 NWAA083725502 1 20080809 A 5414 SKIN BOEING 757 757251 1384970 NM NR 1 NACELLE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 502US 23191 DURING NR1 ENG CHANGE FOUND CRACK IN PYLON SKIN AT NAC STA 132. REPAIRED PER IA 55-213789 SECT I. SECT II REQUIRES PER MANENT REPAIR TO BE ACCOMPLISHED WITHIN 24 MONTHS OR 3000 CYCLES AFTER SECTION 1. (S) 2 L 7 2 4F RT A2NM 20080826 SO 2008 8 26 C2XA08IA150 1 20080625 A 2810 2770138101 FLAPPER VALVE EMB 135 EMB135LR 3260305 SO FUEL SYSTEM INOPERATIVE A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 27523 145389 CRW - FLIGHT 3104, THE CREW REPORTED A FUEL LEAK FROM THE RT WING VENT ON CLIMB. THE AIRCRAFT RETURNED TO CRW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT WING OUTBOARD FLAP VALVE, OPERATIONALLY CHECKED WITH N O DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080826 SO 2008 8 26 C2XA08IA149 1 20080702 A 5210 14540853401 DOOR EMB 135 EMB135LR 3260305 SO MAIN PAX OUT OF ADJUST A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29515 16719 145309 IAH - FLIGHT 2975, THE CREW REPORTED THAT THE MAIN CABIN DOOR GETS HUNG UP WHEN OPENING ON THE UPPER RT. MAINTENANCE AD JUSTED THE PAX DOOR, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080826 SO 2008 8 26 C2XA08ON159 1 20080711 A 3610 8166102 VALVE EMB 145 EMB145XR 3260214 SO BLEED SYSTEM INOPERATIVE A C2XA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 27 12163 12113 14500811 FLT 0216 - ONT - FLIGHT CREW REPORTED BLEED 1 AND 2 OVERTEMP IN ICING CLIMBOUT. THRUST TO ELIMINATE MSG, ICING WAS AT 2 40. ALSO HAD A PACK 2 MEL OVERLOAD-AIR RUSHING IN COCKPIT. MX PERSONNEL REMOVED AND REPLACED PACK 2 OVERTEMP SWITCH AN D NR 2 FAN AIR VALVE. OPERATIONALLY CHECKED SATISFACTORY AND AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. OVERTEMP SWI TCH: P/N 782100-11, S/N 2698, TSN:4807, CSN:2541. FAN AIR VALVE: P/N 816610-2, S/N 2004010117, TSN:12113, CSN:6479. ( A) 2 L 7 2 4F RT 20080826 SO 2008 8 26 C2XA08ON149 1 20080625 A 3397 DIODE EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT LOOSE A C2XA O OTHER L NO TEST NR NOT REPORTED 1 SW 27 12166 11618 14500831 FLT 1380 - JQF - FLIGHT CREW REPORTED LT FWD EXTERNAL EMERGENCY LIGHT INOP. MX PERSONNEL RESEATED DIODE OPERATIONALLY C HECKED SATISFACTORY. AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. (A) 2 L 7 2 4F RT 20080826 SO 2008 8 26 C2XA08R1097 1 20080630 A 2133 2097K021100 OUTFLOW VALVE EMB 145 EMB145LR 3260212 SO CABIN PRESSURE INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 29906 14989 145472 FLIGHT 2306 - EWR - FLIGHT CREW REPORTED CABIN ALTITUDE SHOWING DASHES. CREW PERFORMED AIR RETURN AND LANDED AIRCRAFT W ITHOUT INCIDENT. EWR MX REMOVED AND REPLACED ELECTRO-PNEUMATIC OUTFLOW VALVE AND DIGITAL PRESSURE CONTROLLER. MX PERFO RMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. DIGITAL PRESSURE CONTROLLER INFORMATI ON REPORTED ON SDR C2XA08R1098. (A) 2 L 7 2 4T RT T00011AT 20080826 SO 2008 8 26 C2XA08R1096 1 20080629 A 2120 14520375401 DUCT EMB 145 EMB145XR 3260214 SO CABIN AIR DISCONNECTED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14117 145674 FLIGHT 3144 - IAD - FLIGHT CREW REPORTED SMOKE IN CABIN DURING CLIMB. CREW PERFORMED AIR RETURN AND LANDED BACK IN IAD WITHOUT INCIDENTS. MX FOUND TUBE UNDER SEAT 9A DISCONNECTED. MX RECONNECTED DUCT AND PERFORMED OPERATIONAL CHECK SUCCE SSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. (A) 2 L 7 2 4F RT 20080826 SO 2008 8 26 CX2A08ON156 1 20080712 A 2810 864682 DRAIN EMB 145 EMB145XR 3260214 SO RT FUEL LEAKING A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 14203 5448 14500964 FIT 0450 -SAN- FLIGHT CREW REPORTED RT SIDE FUEL DRAIN ON BELLY LEAKING. MX PERSONNEL REMOVED AND REPLACED RT OUTBOARD DRAIN. OPERATIONALLY AND LEAK CHECKED SATISFACTORY AND AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. (A) 2 L 7 2 4F RT 20080826 SO 2008 8 26 C2XA08CL079 1 20080705 A 3397 W734000120 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14959 145091 DURING ROUTINE MAINTENANCE THE MAIN CABIN DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND RESECURED WIR E W734-0001-20. OPERATIONAL CHECKS WERE GOOD. (A) 2 L 7 2 4T RT T00011AT 20080826 SO 2008 8 26 C2XA08TY072 1 20080708 A 3350 78241 INVERTER EMB 145 EMB145 3260210 SO EMERGENCY LIGHT FAILED A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 18987 2000 145261 THE UPPER EMERGENCY EXIT SIGN AT THE LT EMERGENCY EXIT HATCH WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE EXIT LIGHT INVERTER NR 4 IAW EMB 145 AMM 3321-06. OPS CHECK WAS GOOD. (A) 2 L 7 2 4F RT T00011AT 20080826 SO 2008 8 26 C2XA08IA181 1 20080730 A 2121 26006881102 FAN EMB 135 EMB135LR 3260305 SO E/E BAY INOPERATIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 17521 * 145378 ICT - FLIGHT 2720 - DURING POST FLIGHT INSPECTION THE CREW REPORTED A BURNING ODOR FROM THE FORWARD AVIONICS. MAINTENAN CE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE NUMBER ONE AHRS FAN, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE A IRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080826 SO 2008 8 26 C2X2008F00006 1 20080719 A 3297 W101069124 WIRE EMB 145 EMB145EP 3260221 SO EMER BRK HANDLE BROKEN A C2XA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION IN INSP/MAINT 1 SW 27 14939 145030 IAH - FLIGHT 3056 ON TAKEOFF ROLL THE CREW REPORTED SEEING HOT EMBERS AND DETECTING SMOKE FROM UNDER THE CAPTAINS DASH, WITH THE CIRCUIT BREAKER ON THE OVERHEAD POPPING. THE CREW ABORTED TAKEOFF, AND TAXIED BACK TO THE GATE WITHOUT INCIDEN T. MAINTENANCE INSPECTED THE AIRCRAFT AND REPAIRED A BROKEN WIRE ON THE EMERGENCY BRAKE HANDLE PANEL LIGHT, REPAIRED SE VERAL BURNT WIRES UNDER CAPTS DASH, OPERATIONALLY CHECKED SYSTEMS WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080826 EA 2008 8 26 COMA086350 1 20080809 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 965CA 7131 LT SIDE FUSELAGE FRAME DOUBLER AT FS 640.00 IS CRACKED. COMPLIED WITH MODIFICATION K601R36009-R AT FS 640 IAW S/B 601R- 53-061. (S) 2 L 7 2 4F RT A21EA 20080826 SO 2008 8 26 C2XA081A175 1 20080727 A 3150 WARNING LIGHT EMB 145 EMB145XR 3260214 SO ILLUMINATED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 27 11107 145654 IAH - FLIGHT 2836, THE CREW REPORTED AN AIR GROUND FAIL MESSAGE ON EICAS AFTER T/O THAT REMAINED ON DURING THE ENTIRE FL IGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY TESTED THE AI R GROUND SYSTEM WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4F RT 20080826 NM 2008 8 26 KCSA081404 1 20080818 A 5320 SILL BOEING 747 747249F 1384849 NM BS 440 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 DOOR L-1 DOOR FRAME LOWER SILL FWD CORNER CRACK EXTENDS BEYOND STOP DRILL. (S) 2 L 7 4 4F RT A20WE 20080826 NM 2008 8 26 KCSA081395 1 20080815 A 5420 STIFFENER BOEING 747 747122 1384872 NM NR 1 NACELLE WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 NR 1 PYLON DUCT SUPPORT STIFFENER WORN AT DUCT LINK INBOARD SIDE OF SPAR AT NAC STA 198. (S) 2 L 7 4 4F RT A20WE 20080826 SO 2008 8 26 MAS2008F00005 1 20080606 A 2611 47359713 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO NR 2 NO TEST A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 844MJ 15581 145481 FDM 6161 JFK-ROC. BAGGAGE COMPARTMENT FIRE EXTINGUISHER TEST INOPERATIVE. MX REPLACED NR 2 SMOKE DETECTOR AND OPS CHEC KED. (B) 2 L 7 2 4T RT T00011AT 20080826 2008 8 26 DXTA200803217 4 20080807 A 3160 CONTROLLER CESSNA 500 560CESSNA 2076750 CE CENTRAL DISPLAY SEPARATED E DXTA C ABORTED TAKEOFF D INFLIGHT SEPARATION TO TAKEOFF 1 GL 07 347QS 5600357 CAPTAIN PFD CONTROLLER EJECTED FROM PANEL ON TAKEOFF. TAKEOFF DISCONTINUED. (S) 2 L 7 2 4F RT A22CE 20080930 NM 2008 9 30 CALA0800813 1 20080822 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM BS 440 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 BODY STATION 440 RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REPAIRED CRACKED FRAME AT BODY STATION 440 RIGHT SIDE BETWEEN S-8R AND S-9R AT AC RAIL BRACKET PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 2008UALA04204 1 20080811 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 814UA 862 FLOORBEAM 185 CORRODED (MARKED). REMOVED CORROSION. ASSEMBLY OF FLOORBEAM COMPLETED. PAINTED & INSTALLED FLOORBEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA04205 1 20080810 A 3350 2506500994001 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 NO SLIDE LIGHTS ON FWD DOORS. REPLACED LIGHT ASSEMBLY INDICATOR. ALL OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080930 NM 2008 9 30 2008UALA04225 1 20080811 A 3350 20131A CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 OVERWING EMERGENCY LIGHT LT 2 TOP INOP. REPLACED BATTERY CHARGER. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04233 1 20080810 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT LIGHT INOP. UPPER DECK CEILING JUST FWD OF ROW 17 AND LIGHT JUST AFT OF ROW 17. RELAMPED, LIGHTS OP CHE CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA05505 1 20080827 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1661 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 MAIN CABIN, BLEND OUT ON UPPER CHORD OF BS 1661 FLOORBEAM AT RBL 60. *S/D* MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED AREA. FABRICATED & INSTALLED A NEW T-SECTION AND SPLICES. 2 L 7 2 4F 4 F RT A2NM E17NE 20080930 NM 2008 9 30 2008UALA05504 1 20080827 A 3350 CAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 374UA 24639 EMER LIGHT STRIP END CAP MISSING AT 1B. 2 L 7 2 4F 4 F RT A16WE E21EU 20080930 EU 2008 9 30 2008UALA05502 1 20080827 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 451UA 865 FLOORBEAM 225 CORRODED AROUND FWD NUT PLATE HOLE (MARKED). MAJOR REPAIR ACCOMPLISHED: REMOVED BEAM, DRILLED BEAM AND A TTACH ANGLES. INSTALLED FLOORBEAM 225 IN A/C. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA05497 1 20080826 A 3350 LENS BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 675UA 29243 OVERWING EMERGENCY LIGHT LENS MISSING. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA05493 1 20080826 A 2530 5619022 COFFEEMAKER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 171UA 24322 AFT GALLEY SMOKE APPEARING. OCCURRED JUST PRIOR TO LANDING AND ELECTRICAL POWER REMOVED FROM GALLEY AS A PRECAUTION. P ER FLIGHT ATTENDENTS, THEY SAW A SMALL AMOUNT OF SMOKE COMING FROM AREA NEAR AFT LEFT COFFEE WARMER. OPERATED ALL AFT GA LLEY EQUIPMENT. CHECKED AREA. NO SMOKE DETECTED. CLEANED COFFEE WARMER AS PRECAUTION. NO REPEAT OF REPORTED SMOKE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 EU 2008 9 30 2008UALA05492 1 20080827 A 3350 20131A BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 498UA 1865 ESPU UNIT EMERGENCY LEFT MSG ON CIDS PANEL. REPLACED ESPU BATTERY 11WL. EMERGENCY LIGHT TEST NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA05487 1 20080826 A 2120 UNKNOWN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 29 171UA 24322 SMOKE APPEARED IN AFT GALLEY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA05486 1 20080826 A 2700 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE AILERONS UNKNOWN A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 658UA 27113 THE "AIL LOCK" LIGHT ON AT HIGH SPEED. EICAS MSG "AILERON LOCKOUT" DISPLAYED. OUTBOARD AILERONS INDICATED MOVEMENT - U NLOCKED BOTH. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 EU 2008 9 30 2008UALA05484 1 20080826 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 451UA 865 DOOR 2L SILL IS CORRODED (MARKED). 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 EU 2008 9 30 2008UALA05482 1 20080826 A 5100 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE UNKNOWN UNKNOWN A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 472UA 1435 MECHANICAL PROBLEM INCURRED. FLIGHT DIVERTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080826 EA 2008 8 26 TRAX200800794 1 20080603 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS AN INDICATION NOTED APPROX .2 INCH IN LENGTH 100PERCENT. FAILED NDT INSPECTION. REPAIR REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1230, REV D. REPAIR PER EC/TC RE O 601R-53-61-1230 HAS BEEN COMPLETE. 2 L 7 2 4F RT A21EA 20080826 NM 2008 8 26 2008UALA03364 1 20080613 A 8012 8110402600U SOLENOID BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE START VALVE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 779UA 26941 ENGINE START VALVE R RIGHT STARTER AIR VALVE POSITION DISAGREES WITH COMMANDED POSITION OR STARTER AIR VALVE POSITION IN DICATION IS LOST. STATUS MSG-8061562 INACTV SD MODE. *S/D* SUSPECT FAULTY STARTER VALVE SOLENOID. REPLACED STARTER A IR VALVE SOLENOID REF MM 80-11-07. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080826 SO 2008 8 26 C2XA08ON166 1 20080806 A 3150 WARNING LIGHT EMB 145 EMB145XR 3260214 SO FALSE ACTIVATION A C2XA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 27 14177 9942 5643 14500888 FLT 7718-LAX, FLIGHT CREW REPORTED ENG REF A/I DISAGREE MESSAGE ON EICAS. RESET SYSTEM AS PER MAINTENANCE CONTROL. OPE RATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080826 WP 2008 8 26 IXX2008F00066 1 20080617 A 5310 DOOR FRAME DOUG DC8 DC872F 302199E WP CARGO DOORWAY WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE "B" DOOR JAMB WORN AT STATION 503.000 LONGERON 27-28 RT. REM OVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FO UND. FABRICATED REPAIR DOUBLER, FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AN D REPAIR PARTS IAW DC8 SRM 51-1-11, SRM 51-3-1, FAA FORM 8110-3 08378 DATED 07/11/08, SEMAN DRAWING ED4808 DATED 06/20/0 8, DC8 SRM 51-1-21, SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B. (S) 2 L 7 4 4F RT 4A25 20080826 WP 2008 8 26 IXX2008F00077 1 20080620 A 5311 FRAME DOUG DC8 DC872F 302199E WP BS 350 L21 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FRAME CLIP CRACK AT STATION XF 350.000 LONGERON 21. REM OVED CRACKED FRAME CLIP. FABRICATED FRAME CLIP. PERFORMED HEAT TREATMENT. PERFORMED NDT INSPECTION, NO CRACK NO CORRO SION. CLEANED, TREATED AND PRIMED AREA AND FRAME CLIP. INSTALLED FRAME CLIP DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATION 2003-05 AND SEMAN ED 4814, DC8 SRM 51-1-1 PAGE 1,13, 17, DACO DPS 4.707, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-1-20D AND 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080826 EA 2008 8 26 TRAX200800796 1 20080607 A 5320 ARM CNDAIR CL600 CL6002B19 1900309 EA CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 PANEL 196AR BOTTOM HINGE ARM CORRODED SEVERELY. REMOVED BOTTOM HINGE ARM IAW ASA SRM 51-42-21 AND ASSEMBLED NEW HINGE A RM USING P/N 601R35323-279 IAW ASA SRM 51-42-06. INSTALLED NEW HINGE ARM ON PANEL 196AR IAW CRJ 200. 2 L 7 2 4F RT A21EA 20080826 NM 2008 8 26 QXEA200800871 1 20080808 A 2120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 19 413QX 4060 SEA-FLIGHT 2201 - FLIGHT ATTENDANT COMPLAINS OF A PETROLEUM ODOR FROM THE BLEED AIR SYSTEM. PASSENGERS COMPLAINED DURIN G THE FLIGHT AND ONE FLIGHT ATTENDANT BECAME SICK. MAINTENANCE PERFORMED A GROUND RUN WITH THE BLEEDS ON WITH NO DEFECT S NOTED. COULD NOT DUPLICATE PROBLEM. RETURNED TO SERVICE. NO PARTS REPLACED. (S) 2 H 7 2 4T RT A13NM 20080826 EA 2008 8 26 QXEA200800873 1 20080810 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002C10 1390015 EA LAVATORY ACTIVATED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 19 617QX 10130 PDX-FLIGHT 2514. ABORTED TAKEOFF AT 80 KNOTS FOR A LAVATORY SMOKE DETECTOR WARNING. RETURNED TO THE GATE. ACFT DOWN F OR ENG REPLACEMENT IN PDX. (S) 2 L 7 2 4F RT A21EA 20080826 WP 2008 8 26 NWAA083759917 1 20080812 A 3397 WIRE DOUG DC9 DC932 3022066 WP EMERGENCY LIGHT BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3350 47573 DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROW 21 OF THE CABIN WAS INOPERATIVE. MAINTE NANCE FOUND A BROKEN WIRE, REPAIRED IT WITH A SPLICE, AND FUNCTIONALLY CHECKED THE SYSTEM. (S) 2 L 7 2 4F A6WE 20080826 SO 2008 8 26 C2XA08IA152 1 20080705 A 3350 LIGHT EMB 145 EMB145EP 3260221 SO LT OVERWING INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17928 145007 IAH - DURING A-CK INSPECTION THE LT HAND OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECT ED THE LIGHT ASSY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080826 SO 2008 8 26 MAS2008F00003 1 20080612 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN UNKNOWN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FDM 6154 JFK-PWM. RIGHT EMERGENCY EXIT OVERWING LIGHT OUT AT ROW 12. MX CANNOT DUPLICATE DISCREPANCY. CYCLED SWITCH, NO FAULT NOTED. OPS GOOD. (B) 2 L 7 2 4T RT T00011AT 20080826 EA 2008 8 26 TRAX200800637 1 20080514 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 669 S15R CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 707EV 10057 CABIN SIDE SEAT RAILS HAVE CORROSION DAMAGE AT STR 15R FS 669.00 TO FS 977.00-(MARKED). BLENDED CORROSION FOUND ON SIDE SEAT RAIL AT STR 15R FS 669 TO FS 977 REMOVED .014" OF MATERIAL WITHIN LIMITS OF CRJ 700 SRM 53-41-49 AND 53-51-49. RE STORED SURFACE FINISH AND RE-IDENTIFIED SEAT RAILS AS PER CRJ 700 SRM 53-41-49 AND 53-51-49. JOB COMPLETE. SUPPLEMENTA L SDR CLOSED 6/24/08. 2 L 7 2 4F RT A21EA 20080826 EU 2008 8 26 USAA920081524 1 20080815 A 5315 D534721722204 FLOORBEAM AIRBUS A319 A319112 3930323 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 PIT-S4 -MAJOR REPAIR- LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 & FR68, FROM Y1162 TO 1292. REPLACED FLOO RBEAM BETWEEN FR66 TO FR68, Y1162 TO Y1292 IAW A319 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080826 SO 2008 8 26 CHQA200800163 1 20080814 A 2400 14521325405 CONTROL PANEL EMB 135 EMB135KL 3260302 SO ALLSN AE3007 AE3007A 03030 GL ELECTRICAL INTERMITTENT A CHQA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 GL 11 379SK 17457 12775 145606 CAE312091 FLIGHT 5302, STL TO AUS - DURING CRUISE THE CREW RECEIVED AN ELECTRICAL ABNORMAL MESSAGE. THE ELECTRICAL STATUS PAGE WA S CHECKED AND FOUND THAT THE BATTERIES WERE NOT CHARGING. THE CREW FOLLOWED THE QRH AND STARTED THE APU BUT THE MESSAGE S DID NOT CLEAR. THE FLIGHT DIVERTED TO XNA WHERE IT LANDED WITHOUT INCIDENT. WHEN THE ENGS WERE SHUT DOWN WITH THE AP U STILL RUNNING THE MESSAGES CLEARED. ON CALL MAINTENANCE PERFORMED AN ELECTRICAL RESET AND RAN THE ENGS WITH THE CREW WITH NO FURTHER FAULTS NOTED. THE OVERHEAD ELECTRICAL CONTROL PANEL WAS REPLACED LATER THAT DAY IN STL WITH NO FURTHER DEFECTS NOTED. (S) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080826 NM 2008 8 26 KCSA081385 1 20080811 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 460 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 BS 460 ABOVE S12R APPROX 1 INCH FRAME OTBD FLANGE CRACKED AT FASTENER HOLE. CRACK .250 INCH LONG. CRACK MARKED. UPPER DECK. (S) 2 L 7 4 4F RT A20WE 20080826 NE 2008 8 26 A6WA200840555 2 20080803 A 7261 CARBON SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT ENGINE LEAKING A A6WA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 31 432AW 7257 IN FLIGHT RT ENG OIL PRESSURE FLUCTUATED BETWEEN 30-45 PSI. ON SHORT FINAL RECEIVED "RT ENG OIL PRESSURE" WARNING MESSA GE, PRESSURE FLUCTUATED BETWEEN 23-33 PSI. ALSO, RECEIVED AURAL "ENG OIL" WARNING. REMOVED AND REPLACED RT ENG INTEGRA TED DRIVE GENERATOR CARBON SEAL. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080930 NM 2008 9 30 2008UALA05470 1 20080825 A 5310 STRUCTURE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 815UA 867 FUSELAGE DENT AT STR 10R FRAME 34. *S/D* MAJOR REPAIR. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA05453 1 20080825 A 3350 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY EXIT LIGHT DOOR 5 LT INOP. REPLACED BATTERY. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA05452 1 20080825 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY LIGHT FROM ROW 55 TO 61 INOP. REPLACED BATTERY PACK. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 EU 2008 9 30 2008UALA05448 1 20080824 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 451UA 865 FLOOR BEAM 205 IS CORRODED (MARKED). *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM 205. REMOVED ANGLES, WORKING ON BENCH. INSTALLED GALLEY ATTACH POINTS, DRILLED NEW SPLICE ANGLES. INSTALLED NEW SPLICE ANGLES. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 EU 2008 9 30 2008UALA05485 1 20080826 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 451UA 865 FLOORBEAM 245 CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM. TRANSFERRED ATTACHING PARTS AND IS READY FO R FIT INTO AC. BEAM INSTALLED. INSPECTED THE INSTALLATION OF BEAM 245 FOR SECURITY AND FOUND SECURE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081001 2008 10 1 SWAA085215 4 20080925 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 765SW 29805 R1 EMERGENCY EXIT DOOR SLIDE LOOSE. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081001 2008 10 1 SWAA085213 4 20080925 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR UNWANTED DEPLOY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 489WN 33855 L1 ENTRY DOOR EMERGENCY EXIT SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081001 EU 2008 10 1 08FDEA04117 1 20080929 A 5347 A5327828820300 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 THE ADAPTER TRACK AT FRAME 61 RIGHT SIDE BUTT LINE 1456 HAS SCALLOPS BROKEN OFF. REMOVED FLOOR PANEL 252 UH TO GAIN ACC ESS IAW AMM 53-10-25-4. RECEIVED A NEW ADAPTER TRACK PO 592553.5. LOCATED AND DRILLED THE NEW ADAPTER TRACK IAW SRM 51 -40-40. INSTALLED THE NEW ADAPTER TRACK REF DWG A53278288; REV "A" AND SRM 51-40-21, PARA 7. INSTALLED FLOOR PANEL 25 2 UH REF AMM 53-10-25-4. 2 L 7 2 4F RT A35EU 20081016 NM 2008 10 16 USAASB08095 1 20081009 A 3260 CIRCUIT BREAKER BOEING 737 7373B7 1384580 NM COCKPIT TRIPPED A USAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 19 533AU 24515 ON APPROACH TO PHL, CREW RECEIVED NO RED OR GREEN GEAR INDICATION LIGHTS WHEN GEAR LEVER WAS LOWERED. PERFORMED LIGHT T EST AND PRESS-TO-TEST WITH NO SUCCESS. ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURE. PERFORMED MANUAL GEAR EXTENSIO N AND VISUAL VIEW PORT CHECK TO VERIFY THREE GEAR DOWN AND LOCKED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE MASTER ANNUNCIATOR SECTION 5 CIRCUIT BREAKER OUT. RESET CIRCUIT BREAKER. ALL GEAR LIGHTS TEST AND INDICATE NORMALLY. LEFT ENGINE REVERSER, RIGHT ENGINE OIL PRESSURE AND BOTH ENGINE FIRE WARNING LIGHTS TEST OK. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 UPS08553389 1 20080916 A 5320 SUPPORT BOEING 757 75724APF 1384969 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 424UP 25369 INSPECTION TYPE:C2 SUPPORT IS CRACKED FWD CARGO BS 845, LBL 51, WL 174. REMOVED AND REPLACED SUPPORT IAW SRM 51-40-02-0 G. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 SWAA085228 1 20080925 A 2560 65C34691 GIRT BAR BOEING 737 7377H4 1384404 NM EVAC SLIDE OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 453WN 29847 DURING SCHEDULED HC1 CHECK, FOUND R2 SLIDE DOOR GIRT BAR OUT OF ADJUST. ADJUSTED GIRT BAR PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 UPS08M53378 1 20080909 A 5720 STRAP DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 282UP 48452 INSPECTION TYPE:2C LT WING SPLICE STRAP AT LEADING EDGE WING STA 562 IS CRACKED WHERE MARKED. REMOVED AND REPLACED SPLI CE STRAP IAW SRM 51-31-1, 51-21-1, 51-33-1. 2 L 7 3 4F RT A22WE 20081001 WP 2008 10 1 UPS08853383 1 20080920 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:N/A REPAIR DOUBLER AT FUSELAGE FRAME 50 AND STRINGER 24L REQUIRED REPLACEM MENT D385232. REMOVED DOUBLE R, ACCOMPLISHED STEPS APPENDIX-A (1) THRU (6). PER PRELIMINARY EO DC8-5330-30623-A. DAMAGE REMOVAL VERIFIED OK TO INSTA LL FABRICATED DOUBLER. C/W EO DC8-5330-30623A. 2 L 7 4 4F RT 4A25 20081001 NM 2008 10 1 CALA0800920 1 20080925 A 5330 6545800 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 R1 DOOR FUSELAGE SKIN AFT OF LOWER CUTOUT CRACKED. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PLATES AND FILLERS PER SRM 53-10-01 REPAIR 2. RESTORATION OF AIRCRAFT FINISH WILL BE ACCOMPLISHED ON L/P 9698525 SEQ N00667. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 2008UALA05782 1 20080918 A 2432 893003 CHARGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MAIN BATTERY FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 549UA 25397 MAIN BATTERY CHARGER EICAS MESSAGE. REPLACED MAIN BATTERY CHARGER. 2 L 7 2 4F 4 F RT A2NM E17NE 20081001 NM 2008 10 1 2008UALA05770 1 20080918 A 2421 729825G IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 VIBRATION A UALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 WP 29 517UA 24861 LT GEN DRIVE LIGHT WITH VIBRATION. FLIGHT DIVERTED. REPLACED NR 1 ENGINE IDG. SERVICED IDG. RAN ENGINE. OPS CHECK NORM AL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081001 NM 2008 10 1 2008UALA05771 1 20080918 A 2910 LINE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE HYD SYSTEM LOOSE A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 829UA 1211 Y RSVR LO LVL DISPLAYED ON UPPER ECAM SCREEN - HYD. FOUND LOOSE LINE AT KEEL BEAM. SECURED HYD LINE AT KEEL BEAM, PUMP REPLACED FOR CAVITATION AND FILTERS DOWNLINE. SERVICED SYSTEM AND ALL LEAK CHECKS WERE GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20081001 NM 2008 10 1 2008UALA05772 1 20080918 A 2612 FIRE LOOP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 NACELLE FAULTY A UALA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 647UA 25284 L ENG FIRE LOOP 1 ON STATUS PAGE AND FIRE-OVHT SYS ON EICAS, ABORTED TAKEOFF AT 63 KNOTS. RESISTANCE HIGH AT CARD M681 PINS 19 & 20. CHECKED ENG 1 LOOPS . LOOPS OK. FOUND BAD LUG ON FWD BOTTOM LOOP. REPLACED LUG. RESISTANCE CHECKS NORMAL. SYSTEM TESTED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081001 NM 2008 10 1 2008UALA05775 1 20080917 A 2421 IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MALFUNCTIONED A UALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 551UA 25399 RIGHT GEN DRIVE LIGHT NOT ILLUMINATED AT GATE. REPLACED IDG, ALL OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20080826 EA 2008 8 26 C2X2008F00010 2 20080713 A 7320 367934005 FCU EMB 145 EMB145XR 3260214 SO RROYCE AE3007 AE3007A1E 54169 EA ENGINE INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 12157 13236 145787 FLIGHT 2245 - OKC - FLIGHT CREW REPORTED VENTRAL TANK FAIL MESSAGE ON EICAS. CREW DIVERTED FLIGHT AND LANDED WITHOUT IN CIDENT. MX REMOVED AND REPLACED VENTRAL FUEL CONDITIONING UNIT AND PERFORMED OPERATIONAL SUCCESSFULLY. AIRCRAFT WAS AP PROVED TO RETURN TO SERVICE. (A) 2 L 7 2 4F 4 F RT TE6CH 20080827 EA 2008 8 27 CHQA200800139 1 20080711 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS MALFUNCTIONED A CHQA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 11 465SM 7612 GEE873561 FLIGHT 5732, HRL TO IAH. ON APPROACH WHILE SELECTING FLAPS 45, THE FLAPS FAILED AT 42 DEGREES. THE FLIGHT LANDED WITHO UT INCIDENT. THE AIRCRAFT FLAP SYSTEM WAS INSPECTED, RESET AND OPERATED SEVERAL TIMES. THE AIRCRAFT WAS THEN FERRIED T O SDF FOR FURTHER TROUBLESHOOTING. THE FECU LRU AND FAULT LOGS WERE RECORDED AND THE SYSTEM WAS TROUBLESHOT IN ACCORDAN CE WITH FIM 27-50-00. PERFORMED SELF-TEST OF FLAP MOTOR AND BRAKE ASSEMBLY IAW AMM 27-52-05. PERFORMED TORQUE CHECK OF FLAP SYSTEM IAW AMM 27-53-00 AND CHECKED GOOD. PERFORMED TORQUE CHECK OF BPSU IAW AMM 27-51-10 AND CHECKED GOOD. THE LT AND RT BPSU`S WERE RE-RIGGED PER AMM 27-51-10, NO FURTHER DEFECTS WERE NOTED. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080827 CE 2008 8 27 DXTA200803201 1 20080727 A 2120 UNKNOWN CESSNA 750 750 2076810 CE CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 970QS 7500070 FOUL ODOR COMING FROM AIR DISTRIBUTION SYSTEM. (A) 2 L 7 2 4J RT T00007WI 20080827 EA 2008 8 27 VNAA0807013 1 20080722 A 5240 DOOR CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE MAINT SERVICE OPEN A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 05 723PS 10181 CREW REPORTED HIGH PITCHED NOISE IN FLIGHT AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT LANDING WITHOUT INCIDENT. MAIN TENANCE INSPECTED AND FOUND THE MAINTENANCE SERVICE DOOR OPEN. MAINTENANCE INSPECTED AND SECURED THE DOOR WITH NO DEFEC TS. AIRCRAFT WAS RELEASED FOR SERVICE. (A) 2 L 7 2 4F 4 F RT A21EA E00063EN 20080827 2008 8 27 DXTA200803199 4 20080725 A 3414 INDICATOR AMD FALC50 FALCON2000 2730170 NM AIRSPEED INOPERATIVE E DXTA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 GL 07 259QS 159 ON TAKEOFF ROLL NO AIRSPEED WAS INDICATED ON F/O`S INDICATOR, TAKEOFF WAS ABORTED. (A) 2 L 7 2 4F RT A50NM 20080827 NM 2008 8 27 KCSA081332 1 20080720 A 3350 LIGHT BOEING 747 747212B 1384886 NM LAVATORY INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 703CK 21939 UPPER DECK EMERGENCY LIGHT FWD OF LAV INOP. (A) 2 L 7 4 4F RT A20WE 20080827 EA 2008 8 27 HNAA0800209 1 20080615 A 3397 WIRE DHAV DHC8 DHC8311 1386006 EA EMERGENCY LIGHT BROKEN A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 333EN 34768 221 ROW 11AC EMERGENCY EXIT SIGN INOP. REPAIRED BROKEN GROUND WIRE AS REQUIRED, OPS CHECK GOOD. (A) 2 H 7 2 4T RT A13NM 20080827 NM 2008 8 27 HNAA0800208 1 20080611 A 2530 CA16371 RECEPTACLE DHAV DHC8 DHC8102 2809003 NM GALLEY BURNED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 931HA 50754 132 WARMER NR 1 SOCKET ON AIRCRAFT LOOKS DAMAGED AND DOES NOT WORK. WARMER NR 2 OPERATES NORMALLY. WARMER NR 2 HAS SMOKE O DOR WHEN SELECTED ON. INSPECTED FOR DAMAGE FOUND BOTH AIRCRAFT SOCKETS TO BE DAMAGED DURING HIDDEN DAMAGE INSPECTION, R EF LOG BOOK PG 269250-1 BOTH RECEPTACLES WERE REPLACED, OPS CHECK GOOD. (A) 2 H 7 2 4T RT A13NM 20080827 EA 2008 8 27 VNAA0807008 1 20080719 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 207PS 10838 7873 CREW REPORTED THE NOSE GEAR WOULD NOT RETRACT ON CLIMBOUT. THE CREW FOLLOWED QRH AND RETURNED TO RDU LANDING WITHOUT IN CIDENT. MAINTENANCE INSPECTED AIRCRAFT AND CHANGED THE 3A HYDRAULIC PUMP. OPERATION CHECKS WERE PERFORMED WITH NO DEFE CTS AND AIRCRAFT WAS RELEASED FOR SERVICE. (A) 2 L 7 2 4F RT A21EA 20080827 CE 2008 8 27 DXTA200803200 1 20080727 A 3150 WARNING LIGHT CESSNA 750 750 2076810 CE ILLUMINATED E DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 916QS 7500116 RUDDER LIMIT FAIL B CAS MESSAGE CAME ON IN FLIGHT. LIMITED TO 26 PERCENT. (A) 2 L 7 2 4J RT T00007WI 20080827 CE 2008 8 27 DXTA200803186 1 20080719 A 3220 LANDING GEAR CESSNA 750 750 2076810 CE NOSE VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 920QS 7500120 SEVERE NOSE SHIMMY ON TAKEOFF. STARTED AS ACFT GAINED SPEED THRU EST 30-40 KTS. ABORTED AT APPROX 40-50 KTS. (A) 2 L 7 2 4J RT T00007WI 20080826 NM 2008 8 26 KCSA081384 1 20080811 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 440 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 BS 440 S10R FRAME CRACKED .500 INCH AT STRINGER CUTOUT. CRACK MARKED UPPER DECK. (S) 2 L 7 4 4F RT A20WE 20080826 CE 2008 8 26 DXTA200803229 1 20080815 A 5210 PIN CESSNA 500 560CESSNA 2076750 CE PAX DOOR STUCK E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 826QS 5600782 MAIN CABIN DOOR STUCK CLOSED. CANNOT ENTER ACFT. DOOR HANDLE MOVEMENT SEEMS NORMAL. DOOR PINS WILL NOT RETRACT. (S) 2 L 7 2 4F RT A22CE 20080826 CE 2008 8 26 DXTA200803226 1 20080817 A 3246 WHEEL CESSNA 750 750 2076810 CE NLG VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 913QS 7500113 STRONG NOSE WHEEL SHIMMY ON TAKEOFF. ABORTED TAKEOFF. (S) 2 L 7 2 4J RT T00007WI 20080827 EA 2008 8 27 VNAA0807010 1 20080720 A 2840 73664320 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUEL QTY FAILED A VNAA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 GL 05 220PS 242 7877 CREW REPORTED A FUEL IMBALANCE AMBER MSG INFLIGHT. THE RT FUEL AND TOTAL FUEL QUANTITY INDICATORS SHOWED "DASHED". CRE W ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND CHANGED THE FUEL QUANTITY CO MPUTER. MAINTENANCE CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080827 SO 2008 8 27 CHQA200800136 1 20080709 A 2930 INDICATION SYS EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007A 03030 GL HYD SYSTEM MALFUNCTIONED A CHQA O OTHER N FALSE WARNING DE DESCENT 1 GL 11 261SK 145144 CAR312650 FLIGHT 5820. OKC TO CLE. DURING DESCENT THE FLIGHT CREW RECEIVED A HYDRAULIC 1 LOW QUANTITY MESSAGE ON EICAS AND VERIF IED THE MESSAGE THROUGH THE HYDRAULIC SYSTEM PAGE. THE FLIGHT LANDED IN CLE WITHOUT INCIDENT. MAINTENANCE INSPECTED TH E AIRCRAFT HYDRAULIC SYSTEM UNDER HEAVY LOAD AND NO LEAKS WERE FOUND AS PER MM 29-10-00. THE HYDRAULIC SYSTEM WAS SERVI CED PER MM 12-31-01 AND THE AIRCRAFT WAS RETURNED TO SERVICE. (A) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080827 EA 2008 8 27 CHQA200800137 1 20080710 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS OUT OF RIG A CHQA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 GL 11 701BR 7448 GEE872845 FLIGHT 5716 - IAH TO JAX. DURING CLIMB WHEN THE FLAPS WERE SELECTED FROM 8 TO 0 THE RT FLAP RETRACTED TO 0 AND LT FLAP FROZE AT 3 DEGREES AND A FLAP FAIL MESSAGE APPEARED ON EICAS. THE APPROPRIATE CHECK LISTS WERE FOLLOWED AND THE FLIGHT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A FLAP RE-RIG AND THE FLAP SYSTEM OPERATED NORMALLY. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080825 EU 2008 8 25 USAA920081526 1 20080815 A 5315 D53472075001 FLOORBEAM AIRBUS A319 A319112 3930323 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 PIT - S4- MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, -Y1730. REPLACED FLOORBEAM AT FR66, -Y1730 IAW A319 SRM 51-72-11. (S) 2 L 7 2 4F RT A28NM 20080825 WP 2008 8 25 IXX2008F00058 1 20080617 A 5310 DOOR FRAME DOUG DC8 DC872F 302199E WP CARGO DOORWAY WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE "B" DOOR JAMB WORN AT STATION 503.000 LONGERON 27-28 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, SRM 51-3-1, FAA FORM 8110-3 08378 DATED 07/11/08, SEMAN DRAWING ED-4808 DATED 06/ 20/08, DC8 SRM 51-1-21, SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B. (S) 2 L 7 4 4F RT 4A25 20080825 NM 2008 8 25 KCSA081394 1 20080815 A 5411 FRAME BOEING 747 747249F 1384849 NM NR 3 NACELLE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 NR 3 PYLON REAR ENG MOUNT BULKHEAD LT AFT FRAME WEB IS CRACKED (.250 & .250 INCHES) AT 221.9, LBL 5, WL 150. (S) 2 L 7 4 4F RT A20WE 20080825 GL 2008 8 25 C2XA08SH104 2 20080810 A 7200 ENGINE EMB 135 EMB135LR 3260305 SO ALLSN AE3007 AE3007A 03030 GL NR 2 CONTAMINATED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14522 145383 SHV - FLT 2714, IAH-TXK, DURING CRUISE CREW DETECTED SMOKE ODOR IN COCKPIT. FLIGHT ATTENDANT DETECTED NO ODOR OR ANYTHI NG UNUSUAL IN THE PASSENGER COMPARTMENT. THE ACFT MADE AN UNEVENTFUL LANDING AT TXK. INSPECTION BY MAINTENANCE REVEALE D RESIDUAL OIL ON AND AROUND THE NR 2 ENG. MAINTENANCE CLEANED THE RESIDUAL OIL AND PERFORMED A LEAK CHECK AND OPERATIO NAL CHECK THAT REVEALED NO LEAKS OR ANY DISCREPANCIES. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080825 SO 2008 8 25 N932008F00001 1 20080804 A 2160 UNKNOWN GULSTM G1159 GIV 3980115 SO COCKPIT TEMP UNKNOWN E N93A O OTHER O OTHER NR NOT REPORTED 1 SO 13 465QS 1463 AT FL 450 SMOKE IN CABIN AND COCKPIT. COCKPIT TEMP WOULD NOT GO ABOVE 67 DEGREES F AT A DUCT TEMP OF 176 DEGREES F. UN ABLE TO DUPLICATE, COCKPIT TEMP CONTROLLER AND BOTH WATER SEPARATOR BAGS WERE REPLACED AS PRECAUTION. THE ACFT WAS FLOW N ON AN OPERATIONAL CHECK FLIGHT AND DISCREPANCY DID NOT REOCCUR. TEMP CONTROLLER P/N 607714-6-4 S/N 061C-2510 WATER SE PARATOR BAGS (2 EACH) P/N 832237-30. (S) 2 L 7 2 4F RT A12EA 20080825 NM 2008 8 25 KCSA081387 1 20080811 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 460 S12L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 BS 460 S12L FRAME DOUBLER AFT SIDE CRACKED .375 INCH AT STRINGER CUTOUT, INBOARD UPPER CORNER. CRACK MARKED. UPPER DEC K. (S) 2 L 7 4 4F RT A20WE 20080825 EA 2008 8 25 REX2008F00030 1 20080811 A 7830 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE THRUST REVERSER UNKNOWN A REXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 841AY 8041 AT LEVEL CRUISE FROM KTYS TO KMSP, THE RT THRUST REVERSER DEPLOYED MASTER CAUTION ILLUMINATED. THERE WERE NO UNUSUAL AC FT FLIGHT CHARACTERISTICS NOTED. FLIGHT CREW PERFORMED THE QRH WHICH REQUIRED LANDING AT NEAREST SUITABLE AIRPORT. THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC AND WAS DIVERTED. OTHERWISE APPROACH AND LANDING MADE. CFR LOOKED ACFT OVE R ON TAXIWAY AND RELEASED IT TO THE GATE. MAINTENANCE INSPECTED THE RT THRUST REVERSER AND FOUND NO MECHANICAL DISCREPA NCIES. PROBLEM WAS DETERMINED TO BE WITH THE INDICATION SYSTEM. THE THRUST REVERSER WAS DEFERRED USING ESTABLISHED COM PANY MEL PROCEDURES AND THE ACFT RELEASED FOR SERVICE. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080825 EU 2008 8 25 USAA920081519 1 20080812 A 5347 D53480048202 SEAT TRACK AIRBUS A319 A319112 3930323 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 PIT -S4- MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON RAIL AT L2 DOOR SILL ABOVE FR67. REPLACED RAIL AT L2 DOOR SILL ABOVE FR67 IAW A319 SRM 53-41-11. (S) 2 L 7 2 4F RT A28NM 20080825 EU 2008 8 25 USAA920081539 1 20080818 A 2913 887673 PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYD SYSTEM INOPERATIVE A USAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 19 664AW 25975 3928 1621 V11188 FLT 438 TPA-LAS - EMERGENCY LANDING - CREW REPORTED `HYD G RSVR LO LVL` AND `HYD G ENG 1 PUMP LOW PR` INDICATIONS. AN E MERGENCY WAS DECLARED DUE TO POSSIBLE LOSS OF NOSE WHEEL STEERING ON LANDING. THE ACFT LANDED WITHOUT INCIDENT AND WAS TOWED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENG HYDRAULIC PUMP. OPERATIONAL AND LEAK CHECKS WERE GOOD . (S) 2 L 7 2 4F 4 F RT A28NM E40NE 20080825 CE 2008 8 25 COEA0801876 1 20080813 A 3220 26430902 SHIMMY DAMPENER CESSNA 208 208B 2073701 CE NLG FAILED A COEA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 13 876FE 402 208B0207 ABORTED TAKEOFF: DURING THE TAKEOFF ROLL, AS SPEED INCREASED, THE NOSE GEAR BEGAN TO SHAKE. TAKEOFF ABORTED DUE TO THE VIBRATION. THE NOSE GEAR VIBRATION SUBSIDED AS THE ACFT SLOWED AND WAS NOT FELT ON THE TAXI BACK TO THE RAMP. REMOVED AND REPLACED NOSE LANDING GEAR SHIMMY DAMPENER ASSY. (S) 1 H 7 1 3T A37CE 20080825 NM 2008 8 25 2008UALA03782 1 20080708 A 2701 CONTROL COLUMN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT VIBRATION A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 653UA 25391 VIBRATION FELT IN CONTROL COLUMN. FLIGHT DIVERTED. 2 L 7 2 4F 4 F RT A1NM E24NE 20080825 NM 2008 8 25 AALA200801864 1 20080713 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 631AA 24589 JFK - EMERGENCY LIGHT ARROWS AT LT AND RT NR 4 DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT ARROWS AT L T AND RT NR 4 DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (S) 2 L 7 2 4F RT A2NM 20080826 EA 2008 8 26 CHQA200800159 1 20080805 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS MALFUNCTIONED A CHQA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 11 473CA 7668 E873451 FLIGHT 5608, IAH TO CVG. WHILE ON APPROACH TO CVG, WHEN THE CREW SELECTED THE FLAPS FROM 29 TO 30, RECEIVED A FLAPS FA IL MESSAGE. THE ACFT PERFORMED A GO-AROUND TO RUN THROUGH THE QRH CHECKLISTS. THE ACFT THEN LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN ELECTRICAL RESET IAW FIM 27-50-00. THE FLAPS WERE THEN RUN 7 TIMES WITH NO FURTHER FAULTS NOTE D. (S) 2 L 7 2 4F 4 F RT A21EA E15NE 20080826 EA 2008 8 26 TRAX20080993 1 20080810 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR OUT OF POSITION A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 978EV 7723 SERVICE DOOR OUTER HANDLE WILL NOT STOW. REPOSITIONED GALLEY SERVICE DOOR HANDLE. OPS CHECK GOOD IAW CRJ200 AMM 52-41- 00. (S) 2 L 7 2 4F RT A21EA 20080826 SO 2008 8 26 CHQA200800157 1 20080803 A 5246 14571518411 DOOR EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL FUEL SERVICE UNLATCHED A CHQA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 GL 11 296SK 145514 CAE311464 FLIGHT 3083, LGA TO GSO. JUST AFTER TAKEOFF AT APPROXIMATELY 500FT THE CREW RECEIVED A FUELING DOOR OPEN EICAS MESSAGE. THE MESSAGE APPEARED AND DISAPPEARED SEVERAL TIMES. THE FLIGHT CREW COMPLETED THE APPROPRIATE QRH CHECKLISTS AND RETU RNED TO LGA FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE FUEL DOOR AND FOUND THE DOOR PARTIALLY UNLATCHED. AFT ER INSPECTING THE DOOR AND LATCHES FOR DAMAGE, THE DOOR WAS CLOSED AND THERE WERE NO FURTHER DEFECTS NOTED. (S) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080826 NM 2008 8 26 2008UALA03783 1 20080708 A 3150 WARNING MESSAGE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 669UA 30025 THE 'R IDG VALVE' EICAS MSG DISPLAYED. 2 L 7 2 4F 4 F RT A1NM E24NE 20080826 EA 2008 8 26 COMA086358 1 20080817 A 5315 60034017351 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FS 280 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 964CA 29977 7129 FOUND CORROSION ON UNDER FLOOR FRAME AT FS 280 BETWEEN LBL 9.00 AD RBL 9.00. REMOVED AND REPLACED FLOOR SUPPORT IAW CRJ SRM 51-42-06. (S) 2 L 7 2 4F RT A21EA 20080826 SO 2008 8 26 C2XA08ON151 1 20080709 A 2731 3621001013 CONTROL UNIT EMB 145 EMB145XR 3260214 SO STAB TRIM INOPERATIVE A C2XA O OTHER S F AFFECT SYSTEMS FLT CONT AFFECTED CL CLIMB 1 SW 27 14168 9836 14500840 FLT 7665 - ONT - FLIGHT CREW REPORTED MAIN PITCH TRIM INOPERATIVE. MX PERSONNEL REMOVED AND REPLACED HORIZONTAL STAB CO NTROL UNIT. OPERATIONALLY CHECKED SATISFACTORY, AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. (A) 2 L 7 2 4F RT 20080826 SO 2008 8 26 C2XA08IA153 1 20080704 A 3260 805701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16561 145610 IAH - FLIGHT 555, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDE D WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE NOSE LANDING GEAR WOW PROXIMITY SWITCH . OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080826 SO 2008 8 26 C2XA08IA151 1 20080706 A 3210 LANDING GEAR EMB 145 EMB145XR 3260214 SO MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 21154 145772 PHX - FLIGHT 2899, THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MESSAGE ON CLIMB AND THE GEAR WOULD NOT RETRACT. TH E AIRCRAFT RETURNED TO PHX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, RESET THE AIR GROUND S YSTEM, OPERATIONALLY CHECKED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4F RT 20080826 SO 2008 8 26 C2XAA08ON160 1 20080713 A 2910 MS21902JB FITTING EMB 145 EMB145XR 3260214 SO HYD SERV PORT LOOSE A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 12167 7540 14500834 FLT 7660 - BOI - FLIGHT CREW REPORTED HYD LOW QTY ADVICE ON T/O. MONITORED DURING FLIGHT, SLOWLY DECREASE. DIVERTED TO BOI. MX PERSONNEL FOUND HYD SERVICE PORT FITTING LOOSE, TIGHTEN IT, SERVICED, PRESSURED. OPERATIONALLY CHECKED SATISF ACTORY AND AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. (A) 2 L 7 2 4F RT 20080826 SO 2008 8 26 C2XA08RI099 1 20080705 A 4930 4951610 MANIFOLD EMB 145 EMB145XR 3260214 SO APU INOPERATIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16151 145758 FLIGHT 2358 - EWR - FLIGHT CREW REPORTED STRONG FUEL ODOR IN THE ACFT. EWR MX REMOVED AND REPLACED APU SECONDARY FUEL M ANIFOLD ASSEMBLY IAW ENGINE MANUAL 49-31-06 AND PERFORMED OPERATIONAL AND LEAK CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVE D TO RETURN TO SERVICE. (A) 2 L 7 2 4F RT 20080826 WP 2008 8 26 IXX2008F00067 1 20080611 A 5313 LONGERON DOUG DC8 DC872F 302199E WP BS 1610 L17L CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE CRACKED AT STATION FS 1610.000 LONGERON 17 LT. REMOVED DAMAGED LO NGERON. CLEANED, TREATED AND PRIMED AREA. INSTALLED LONGERON IAW DC8 SRM 53-5-2 FIGURE 5 SHEET 1 PAGE 16 ITEM "B", DC8 SRM 51-1-8B, DC8 SRM 53-1-0 PAGE 1, SRM 51-1-21, 51-1-20D, SRM 51-2-0 FIGURE 50 SHEET 37, 51-3-0, AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080826 WP 2008 8 26 IXX2008F00070 1 20080613 A 5753 SKIN DOUG DC8 DC872F 302199E WP RT WING TE FLAP MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP UPPER PANEL HAS IMPROPER REPAIR AND DENTS AT STATION XW 30 00 TO STATION XW 92.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, AND BONDED DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 1 PAGE 2, DC8 SRM 57-1-0 PAGE 1, SRM 51-3-0, SRM 51-1-21, DC8 S RM 57-7-1 FIG 1 ITEM "A", DC8 SRM 51-1-9 TR 51-142, SRM 51-1-9A TR 51-141, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-3-0 AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080827 CE 2008 8 27 DXTA200803189 1 20080719 A 2750 FLAP SYSTEM CESSNA 500 560CESSNA 2076750 CE TE FLAPS MALFUNCTIONED E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 336QS 5600336 AFTER TAKEOFF, THE FLAP HANDLE WOULD NOT MOVE IN ORDER TO RETRACT. THE FLAP HANDLE WOULD NOT MOVE IN ORDER TO EXTEND FL APS EITHER. FLAPS ARE STUCK AT 7 DEGREES. (A) 2 L 7 2 4F RT A22CE 20080827 NM 2008 8 27 WRLA2008069A 1 20080820 A 5310 AEA05261AEA0526 DOUBLER DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE WHEEL WELL CRACKED A WRLA O OTHER O OTHER NR NOT REPORTED 1 SO 11 275WA 48631 DURING INSPECTION FOUND CRACK ON CLG WHEEL WELL LT AND RT DOUBLER AT Y=1381, X=31.5 AND -31.5. REPAIRED CRACK AREA IAW EI W2008A53B-761 REV.00. JOB COMPLETED AND CONDITION CHECK NORMAL. (S) 2 L 7 3 4F 4 F RT A22WE E24NE 20080827 2008 8 27 UG8A08GM08181 2 20080820 A 7532 32158682 BLEED VALVE GULSTM GIVX GIVXG350 3980220 SO LEFT ENGINE INOPERATIVE E UG8A C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 23 5116 1408 4023 THE "L-BLEED PRESSURE HIGH" AMBER CAS WAS NOTED ON TAKEOFF ROLL BEGINNING. LT ENG BLEED AIR PRESSURE REGULATING VALVE F AILED TO REGULATE PROPERLY. TROUBLESHOOTING REQUIRED. DEFERRED LT BLEED AIR SYSTEM PER MEL 36-1.1 AND COMPLETED TASK M 36.1.1. ACFT WAS RETURNED TO SERVICE. REMOVED AND REPLACED THE LT ENG BLEED AIR REGULATING AND SHUTOFF VALVE. LEAK C HECK PER CMP CODE 710007 AND OPERATIONAL CHECK PER CMP CODE 361215 "BLEED SYSTEM OPERATIONAL CHECK" WERE GOOD. THE DEFE RRAL HAS BEEN CLEARED AND ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT A12EA 20080827 EA 2008 8 27 MAS2008F00021 1 20080809 A 3250 4480000501 ECU CNDAIR CL600 CL6002C10 1390015 EA NLG STEERING MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 516LR 2021 1351 10258 ASH FLT 7053 IAD-ATL. NOSE WHEEL STEERING INOPERATIVE CAUTION MESSAGE. REMOVED AND REPLACED ECU AND PRESSURE SWITCH. (S) 2 L 7 2 4F RT A21EA 20080827 EA 2008 8 27 A6WA200840528 1 20080621 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 202 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 446AW 7806 CRACK EXIST OF FWD PRESSURE BULKHEAD AT FS 202.0, LBL 23.71, PARKING BRAKE AREA. FWD PRESSURE BULKHEAD AT FS 202 AND LB L 23.71 REPAIRED IAW CRJ 200 REO 601R-53-11-563. (A) 2 L 7 2 4F RT A21EA 20080827 EA 2008 8 27 A6WA200840530 1 20080625 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 446AW 7806 INTERCOSTAL AT FS 484 LT LBL 36 CRACKED. PERFORM REO 601R-53-41-057. (A) 2 L 7 2 4F RT A21EA 20080827 NM 2008 8 27 HNA2008F00040 1 20080812 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 814EX 40629 40629 318 EMERGENCY LIGHTS FLASHED OFF AND ON DURING TAXI IN. CREW REPORTED TO MAINTENANCE. MAINTENANCE PERFORMED EMERGENCY LIGH TS OPS CHECK PER WORK CARD 33-50-03. OPS CHECK GOOD. (S) 2 H 7 2 4T RT A13NM 20080827 EA 2008 8 27 A6WA200840531 1 20080627 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 446AW 7806 ANGLE CRACKED ON BULKHEAD AT FS 621 AND CARGO DOOR BEAM. ANGLE REPLACED ON BULKHEAD FS 621 AND CARGO DOOR BEAM IAW CRJ 200 SRM 51-42-21. (A) 2 L 7 2 4F RT A21EA 20080827 EA 2008 8 27 A6WA200840550 1 20080718 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN PRESSURE FALSE ACTIVATION A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 407AW 7424 RECEIVED CABIN ALTITUDE MASTER WARNING MESSAGE IN FLIGHT AIRCRAFT ALTITUDE 12,000FT CABIN ALTITUDE 10,200FT, PRESSURIZAT ION WORKED IN NORMAL MODE. REF LOG 186158/1-COMPLIED WITH OPS CHECK OF CABIN PRESSURIZATION IN MANUAL MODE IAW AMM 21-3 1-00, OPS CHECK AND LEAK CHECK GOOD ON THE GROUND. (A) 2 L 7 2 4F RT A21EA 20080827 NM 2008 8 27 HNA2008F00037 1 20080811 A 3240 21565 BRAKE ASSY DHAV DHC8 DHC8102 2809003 NM MLG SMOKE A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 936HA 50336 50336 145 NR 2 BRAKE ASSY SMOKING. RETURNED TO GATE. INSPECTED BRAKE ASSY, NO DEFECTS NOTED. FLIGHT 4615 PHF. (S) 2 H 7 2 4T RT A13NM 20080827 EA 2008 8 27 MAS2008F00020 1 20080810 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH FLT 2810 PHX-DSM - EMERGENCY FLOOR LIGHTS SEGMENTS 6 AND 7 INOPERATIVE. MAINTENANCE FIXED LOOSE CONNECTION. OPS GO OD. (S) 2 L 7 2 4F RT A21EA 20080827 NM 2008 8 27 F3LA200800564 1 20080816 A 5330 SKIN AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 948FR 47 2836 MAINTENANCE NOTED LIGHTNING STRIKE DAMAGE AT LAP SEAM AT STRINGER 6L, .25 INCH FROM RIVET EDGE AT FRAME 29. ENGINEERING AUTHORIZATION A9-53R-30571 INDICATES MAJOR REPAIR. (S) MX COMPLIED WITH ENGINEERING AUTHORIZATION NR A9-53R-30571. UP ON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. REQUIREMENT TO REINSPECT REPAIR AT 32,800 FLIGHT CY CLES. 2 L 7 2 4F RT A28NM 20080827 EA 2008 8 27 HNA2008F00034 1 20080612 A 5311 FRAME DHAV DHC8 DHC8311 1386006 EA BS 434 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 335EN 32270 32270 375 SURFACE CORROSION FOUND ON FRAME BS 434.50 RT STRINGER 31. SURFACE CORROSION REMOVED IAW EO8-53-08-3218 LPI ACCOMPLISHE D. (S) 2 H 7 2 4T RT A13NM 20080827 EA 2008 8 27 MAS2008F00038 1 20080814 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INTERMITTENT A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 47202 7202 AIRSHUTTLE 7173 IN ORD REPORTED THE EXIT LIGHT ON THE SERVICE DOOR INOPERATIVE. MAINTENANCE RESET THE SYSTEM AND WERE U NABLE TO DUPLICATE THE PROBLEM. (S) 2 L 7 2 4F RT A21EA 20080827 EA 2008 8 27 MAS2008F00039 1 20080816 A 2613 90001273 CONTROL UNIT CNDAIR CL600 CL6002D24 1390016 EA OVERHEAT SYSTEM MALFUNCTIONED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 908FJ 7144 5581 15008 ASH 2648 SAT-CLT. NR 2 MLG BRAKE OVERHEAT WARNING AFTER LANDING. MAINTENANCE REMOVED AND REPLACED ASCU. (S) 2 L 7 2 4F RT A21EA 20080827 EA 2008 8 27 MAS2008F00047 1 20080819 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR MALFUNCTIONED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 926LR 15026 ASH FLT 2623 CLT. MAIN DOOR WARNING INDICATION WITH DOOR CLOSED AND LOCKED. RESECURED SPLICE SP127. (S) 2 L 7 2 4F RT A21EA 20080828 EA 2008 8 28 HNAA08A0001 1 20080612 A 5243 85321086059 DOOR DHAV DHC8 DHC8311 1386006 EA LAV SERVICE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 335EN 32270 32270 375 CORROSION FOUND ON LAVATORY SERVICE PANEL. REPLACED LAV SERVICE PANEL. (S) 2 H 7 2 4T RT A13NM 20080828 EA 2008 8 28 HNAA08A0002 1 20080613 A 5347 SEAT TRACK DHAV DHC8 DHC8311 1386006 EA BS 129-197 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 335EN 32270 32270 375 CORROSION FOUND ON RT SEAT TRACK BETWEEN STA 129.75 AND 197.50. SEAT TRACK REPLACED FROM STA 109.00 TO 187.00 IAW RD8-5 3-2797. (S) 2 H 7 2 4T RT A13NM 20080828 EA 2008 8 28 A6WA200840533 1 20080627 A 5410 FLANGE CNDAIR CL600 CL6002B19 1900309 EA RT NACELLE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 446AW 7806 ON RT ENG AT FLANGE FOUND CRACKED AT 9 O’CLOCK. CRACK REPAIRED ON RT ENG AT FLANGE AT 9 O’CLOCK IAW REO 601R-71-00-3859 . (A) 2 L 7 2 4F RT A21EA 20080828 EA 2008 8 28 A6WA200840529 1 20080625 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 446AW 7806 INTERCOSTAL AT FS 484 RBL 36 IS CRACKED. PERFORM REO 601R-53-41-059 REV A. (A) 2 L 7 2 4F RT A21EA 20080828 EA 2008 8 28 MAS2008F00026 1 20080810 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 77195 24374 20740 7195 ASH FLT 7188 CAE- OVERNIGHT. FLAPS FAILED AT 0 DEGREES WHEN SELECTED TO 8 DEGREES. REMOVED AND REPLACED LT AND RT BPSU AND FLAP LEVER. (S) 2 L 7 2 4F RT A21EA 20080828 NM 2008 8 28 EIA2008029 1 20080718 A 5210 81420021 BOTTLE BOEING 747 747230B 1384889 NM DOOR ASSIST LOW PRESSURE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 488EV 23287 LT UPPER DECK SLIDE DOOR ASSIST BOTTLE READS "0" PSI. REPLACED LT UPPER DECK DOOR ASSIST BOTTLE IAW B747 MM 25-68-05. (S) 2 L 7 4 4F RT A20WE 20080828 EA 2008 8 28 A6WA200840539 1 20080709 A 5210 CABLE CNDAIR CL600 CL6002B19 1900309 EA DOOR ASSIST DISLODGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 467AW 7900 PASSENGER DOOR WILL ONLY PARTIALLY OPEN. FOUND POWER ASSIST MOTOR CABLE WAS OUT OF ROLLER TRACK. REMOVED AND REPLACED PAX DOOR POWER ASSIST MOTOR IAW 52-11-08. C/W ELECTRICAL 52 &51. DOOR ASSIST OPS CHECKS GOOD. (A) 2 L 7 2 4F RT A21EA 20080828 EA 2008 8 28 MAS2008F00041 1 20080817 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 933LR 15033 ASH 2819 AUS-PHX - CAPTAIN REPORTED ONE CEILING LEVEL EMERGENCY FLOOD LIGHT INOPERATIVE. MAINTENANCE RELAMPED. (S) 2 L 7 2 4F RT A21EA 20080828 NM 2008 8 28 HNA2008F00048 1 20080819 A 3110 LAMP DHAV DHC8 DHC8102 2809003 NM CONTROL PANEL BURNED OUT A HNAA O OTHER L NO TEST NR NOT REPORTED 1 EA 07 825EX 33942 33942 388 EMERGENCY BUTTON ON FAS CONTROL PANEL NOT BACKLIT. REPORTED TO MAINTENANCE. RELAMPED FAS EMERGENCY BUTTON ON CONTROL P ANEL. OK FOR SERVICE. (S) 2 H 7 2 4T RT A13NM 20080828 EA 2008 8 28 MAS2008F00012 1 20080803 A 5210 HOUSING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR HANDLE UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 715SF 7115 ASH FLT 7159 - IAD-CLE - PASSENGER DOOR OUTER HANDLE WILL NOT STOW FROM INSIDE. MAINTENANCE RESECURED PULL ROD HOUSING. (S) 2 L 7 2 4F RT A21EA 20080828 NM 2008 8 28 MAS2008F00030 1 20080812 A 3350 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 445YV 445 ASH FLT 7177 - DEN-ASE - AFT CEILING AND EXTERNAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE CHANGED THE POWER SUPPLY. (S) 2 H 7 2 4T RT A13NM 20080828 EA 2008 8 28 MAS2008F00051 1 20080820 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS OUT OF RIG A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75991 7422 FLT 7197 - ORD-SBN - FLAP FAIL CAUTION MESSAGE. MAINTENANCE COMPLIED WITH PART A AND RIGGED FLAPS. (S) 2 L 7 2 4F RT A21EA 20080828 SO 2008 8 28 SIMA200823501 1 20080820 A 3350 20131A BATTERY EMB 135 EMB135LR 3260305 SO EMERGENCY LIGHT INOPERATIVE A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 725AE 145312 ON FLIGHT 4661 - CREW REPORTED EMERGENCY LIGHTS OVER GALLEY INOPERATIVE. ACFT REMOVED FROM SERVICE. REMOVED AND REPLAC ED EMERGENCY LIGHT BATTERY OVER GALLEY. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE. (S) 2 L 7 2 4F RT T00011AT 20080828 EA 2008 8 28 MAS2008F00043 1 20080817 A 3397 CIRCUIT BOARD CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS DAMAGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 923FJ 15023 ASH 2916 - PHX-COS - EMERGENCY LIGHTS FLICKERING ON AND OFF INTERMITTENTLY DURING TAXI-OUT. MAINTENANCE REMOVED AND REP LACED PRINTED CIRCUIT BOARD ASSEMBLY. (S) 2 L 7 2 4F RT A21EA 20080828 EA 2008 8 28 MAS2008F00050 1 20080819 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 914FJ 15014 ASH FLT 2926 - PHX-DEN - EMERGENCY LIGHT ABOVE ROW 10 INOPERATIVE. MAINTENANCE RELAMPED LIGHT. (S) 2 L 7 2 4F RT A21EA 20080825 NM 2008 8 25 AALA200801854 1 20080711 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 790AN 30251 MIA - EMERGENCY LIGHT AT SEAT 21G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT SEAT 21G. SYSTEM GROUND CHECKED NORM AL OPERATION. (S) 2 L 7 2 4F RT T00001SE 20080825 EU 2008 8 25 F3LA200800551 1 20080811 A 5321 D536740740000 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 806FR 30 2218 DURING C3 C-CHECK, INSPECTION NOTED THE AFT CARGO PIT LT TRANSITION PANEL 151HH WAS DAMAGED. MAINTENANCE REPAIRED DAMAG ED PANEL 151HH IAW THE REQUIREMENTS OF A319 SRM 53-02-00, PARAGRAPSH 8C, FIGURE 204. UPON COMPLETION OF THE REPAIR IT W AS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT 20080825 NM 2008 8 25 KCSA081393 1 20080815 A 5411 FRAME BOEING 747 747249F 1384849 NM NR 3 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 NR 3 PYLON REAR ENG MOUNT BULKHEAD LT AFT FRAME WEB IS CRACKED (.250 INCHES & .750 INCHES) AT 221.9, LBL 6, WL 148.5. ( S) 2 L 7 4 4F RT A20WE 20080825 WP 2008 8 25 IXX2008F00084 1 20080614 A 5753 SKIN DOUG DC8 DC872F 302199E WP LT WING TE FLAP WORN A IXXA O OTHER O OTHER NR NOT REPORTED 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND LT OUTBOARD FLAP SKIN ON EXHAUST GATE WORN AT STATION XF 250.000. REMOVED FAST ENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 4 TR 57-94 DATED 10-01-02, DC8 SRM 57- 1-0 PAGE 1, SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 4 ITEM "C" TR 57-94, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND SRM 51-1-21. (S) 2 L 7 4 4F RT 4A25 20080826 EA 2008 8 26 REX2008F00018 1 20080721 A 2721 601R5122623 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA AILE/RUDDER TRIM MALFUNCTIONED A REXA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 8886A 11180 7886 RUDDER TRIM RUNAWAY WITH FULL DEFLECTION TO THE LT ON CLIMBOUT. REMOVED AND REPLACED AILERON RUDDER TRIM CONTROL PANEL IAW AMM. (A) 2 L 7 2 4F RT A21EA 20080826 EA 2008 8 26 TRAX200800777 1 20080610 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 EMERGENCY FLOOR TRACK LIGHTING LAMPS ROWS 9 TO 12 AND LT AND RT AFT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP. REMOV ED AND REPLACED NR 4 AFT BATTERY PACK ASSEMBLY AND BATTERY CHARGER ASSEMBLY IAW CRJ 200 AMM 33-51-04. OPS CHECK GOOD. A/C OK FOR SERVICE. 2 L 7 2 4F RT A21EA 20080826 SO 2008 8 26 C2XA08IA155 1 20080704 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 29906 17537 145472 IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE FIRST THREE SECTIONS OF AISLE PATH LIGHTING WERE FOUND TO B E INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 EMERGENCY LIGHT BATTERY, OPERATIONALLY CHECKED WITH NO DEF ECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080826 SO 2008 8 26 C2XA08R1098 1 20080630 A 2131 22250N030301 CONTROLLER EMB 145 EMB145LR 3260212 SO CABIN PRESSURE INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 29906 1440 145472 FLIGHT 2306 - EWR - FLIGHT CREW REPORTED CABIN ALTITUDE SHOWING DASHES. CREW PERFORMED AIR RETURN AND LANDED AIRCRAFT W ITHOUT INCIDENT. EWR MX REMOVED AND REPLACED ELECTRO-PNEUMATIC OUTFLOW VALVE AND DIGITAL PRESSURE CONTROLLER. MX PERFO RMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. ELECTRO-PNEUMATIC OUTFLOW VALVE INFOR MATION REPORTED ON SDR C2XA08R1097. (A) 2 L 7 2 4T RT T00011AT 20080826 EA 2008 8 26 C2XAA08ON158 2 20080712 A 7320 23078837 FADEC EMB 145 EMB145XR 3260214 SO RROYCE AE3007 AE3007A1E 54169 EA NR 1 ENGINE INOPERATIVE A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 17196 7601 14500945 CAE312876 FLT 0417 - SAT - FLIGHT CREW REPORTED E1 FLUCTUATIONS IN FUEL FLOW-N1-ITT FL270. MX PERSONNEL REMOVED AND REPLACED E1 F ADEC 1B AND FPMU. OPERATIONALLY CHECKED SATISFACTORY AND AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. FADEC 1B: P/N 23 078837, S/N BX 161593, TSN:8335, CSN:4504. FPMU: P/N 23077658, S/N SCP05086, TSN:7523, CSN:3995 (A) 2 L 7 2 4F 4 F RT TE6CH 20080826 EA 2008 8 26 TRAX200800793 1 20080603 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 REAR PRESSURE BULKHEAD WEB HAS AN INDICATION NOTED APPROX 1.1 INCH IN LENGTH AT WL 108 RBL 36.20. FAILED NDT INSPECTION 50 PERCENT. REPAIRED REAR PRESSURE BULKHEAD WEB AT WL 108 AND RBL 36.20 IAW REO 601R-53-61-2678. COMPLIED WITH EC/TC REO 601R-53-61-2678 IAW BOMBARDIER REO 601R-53-61-2678. 2 L 7 2 4F RT A21EA 20080826 NM 2008 8 26 USAA920081532 1 20080804 A 5320 146N518017 STRAP BOEING 757 7572G7 1384963 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 909AW 24522 MCN-C3- MAJOR REPAIR - CRACK ON STABILIZATION STRAP BS 1660 BL 24.75. REPAIRED STABILIZATION STRAP BS 1660 BL 24.75 IAW B757 SRM 51-40-02-0G. (S) 2 L 7 2 4F RT A2NM 20080826 EA 2008 8 26 TRAX200800789 1 20080615 A 2560 MEGAPHONE CNDAIR CL600 CL6002C10 1390015 EA CABIN INTERMITTENT A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 MEGAPHONE WORKS INTERMITTENTLY. JOB COMPLETED. INSPECTED MEGAPHONE AND FOUND TO BE SERVICEABLE IAW CRJ 700 AMM 25-60. 2 L 7 2 4F RT A21EA 20080826 EA 2008 8 26 TRAX200800792 1 20080615 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 916EV 7757 CABIN DOOR DIFFICULT TO OPEN AND CLOSE. OPERATIONAL CHECKED GOOD, IN ACCORDANCE WITH AMM 52-11-00. OK FOR SERVICE. 2 L 7 2 4F RT A21EA 20080826 SO 2008 8 26 C2XA081A176 1 20080726 A 2131 CONTROLLER EMB 145 EMB145XR 3260214 SO CABIN PRESSURE MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 17108 145655 IAH - FLIGHT 2259 - DURING CRUISE, THE CREW REPORTED THAT THE AIRCRAFT CABIN RATE OF CHANGE BECAME ERRATIC. THE AIRCRAF T RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE DIGITAL PRESSURE CONTROLLER, O PERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4F RT 20080826 SO 2008 8 26 C2X2008F00007 1 20080720 A 7500 S242230 O-RING EMB 145 EMB145LR 3260212 SO RROYCE AE3007 AE3007A1 54165 EA BLEED AIR FAILED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 18982 145223 IAH - FLIGHT 2944 - DURING PREFLIGHT THE CREW REPORTED A BURNING ODOR AND BLEED LEAK NR 2 INDICATION. MAINTENANCE INSPE CTED THE AIRCRAFT AND REMOVED AND REPLACED A BLOWN O-RING IN THE CARGO COMPARTMENT, LEAK AND OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080826 SO 2008 8 26 C2X2008F00009 1 20080715 A 2131 92185A010200 CONTROLLER EMB 145 EMB145LR 3260212 SO CABIN PRESSURE INOPERATIVE A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 27 13914 14717 145430 FLIGHT 2874 - CHS - FLIGHT CREW REPORTED AUTO PRESS FAIL IN FLIGHT. MX REMOVED AND REPLACED DIGITAL PRESSURIZATION CONT ROLLER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080827 EA 2008 8 27 VNAA0807012 1 20080722 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE MULTIPLE FAIL A VNAA C ABORTED TAKEOFF G J MULTIPLE FAILURE WARNING INDICATION TO TAKEOFF 1 GL 05 215PS 7880 E873907 CREW REJECTED TAKEOFF AT 85 KNOTS DUE TO MASTER CAUTION LIGHT 900 DEG AND FLASHING ITT ON LT ENGINE. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED ENGINE AND FOUND ALL PARAMETERS WITHIN LIMITS AND NO DEFECTS. AIRCRAFT WAS RELEASED FOR SERVICE. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080828 NM 2008 8 28 F3LA200800565 1 20080816 A 5330 SKIN AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 948FR 47 2836 MAINTENANCE NOTED LIGHTNING STRIKE DAMAGE AT LAP SEAM AT STRINGER 6L, .25 INCH FROM RIVET EDGE AT FRAME 28. ENGINEERING AUTHORIZATION A9-53R-30571 INDICATES MAJOR REPAIR. (S) MX COMPLIED WITH ENGINEERING AUTHORIZATION NR A9-53R-30571. U PON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. REQUIREMENT TO REINSPECT REPAIR AT 32,800 FLIGHT C YCLES. 2 L 7 2 4F RT A28NM 20080828 EA 2008 8 28 MAS2008F00048 1 20080819 A 5210 CABLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 97325 7325 FLIGHT 2783 - PHX-MRY - UNABLE TO OPEN MAIN PAX DOOR. MAINTENANCE ADJUSTED GAS SPRING CABLE TENSION. OPS GOOD. (S) 2 L 7 2 4F RT A21EA 20080828 EA 2008 8 28 MAS2008F00036 1 20080813 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 17175 7175 ASH 7186 - ORD-ROC - NOSE GEAR DISAGREE ON APPROACH. MAINTENANCE REPAIRED NLG PROX SENSOR BRACKET AND SWUNG GEARS. (S) 2 L 7 2 4F RT A21EA 20080828 EA 2008 8 28 MAS2008F00052 1 20080820 A 5270 PROXIMITY SWITCH CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR MALFUNCTIONED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 926LR 15026 ASH FLT 2773 - SAT-PHX - PASSENGER DOOR WARNING MESSAGE. REPLACED PROX SWITCH. (S) 2 L 7 2 4F RT A21EA 20080828 EA 2008 8 28 MAS2008F00049 1 20080819 A 2560 MEGAPHONE CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EQUIP INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 502MJ 10050 ASH FLT 7128 - ORD-CLT - MEGAPHONE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED MEGAPHONE. (S) 2 L 7 2 4F RT A21EA 20080828 EA 2008 8 28 MAS2008F00053 1 20080820 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR FALSE ACTIVATION A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 904FJ 15004 ASH FLT 2615 - IAD-CLT - ON TAXI IN PAX DOOR OUTER HANDLE CAUTION MESSAGE ILLUMINATED ON EICAS. MAINTENANCE RESET. OPS GOOD. (S) 2 L 7 2 4F RT A21EA 20080828 NM 2008 8 28 QXEA200800368 1 20080330 A 5330 SKIN DHAV DHC8 DHC8202 2809007 NM BS 160 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 356PH 502 PDX-C4 CHECK - BURNT RIVET APPROX 6 INCHES AFT OF STA X160.500 & 3 INCHES OUTBOARD OF STR 4L. REPAIRED DAMAGE TO SKIN P ER D8-200 RD8-53-137 PG 3 STEP 1. HFEC IAW PSM 1-82-7A PART 6 51-00-02 PER RD8-53-137. NO DEFECTS NOTED. (S) 2 H 7 2 4T RT A13NM 20080828 NM 2008 8 28 QXEA200800532 1 20080521 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 411QX 4055 PDX-C4 CHECK- SEAT TRACK NR 11 HAS CORROSION ON TRACK AT APPROX STA X17.85 AND X27.4 AND X93.00. REMOVED NR 11 SEAT TRA CK AND INSTALLED NEW NR 11 SEAT TRACK REF DHC8-400 SRM 51-40-15 & 51-42-05. (S) 2 H 7 2 4T RT A13NM 20080828 NM 2008 8 28 NWAA083976729 1 20080821 A 3350 BATTERY BOEING 747 747251F 1384898 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 629US 22388 DURING OVERNIGHT CHECK FOUND COCKPIT EXIT SIGN WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED BATTERY. OPERATIONAL C HECKED GOOD, AND ACFT WAS RETURNED TO SERVICE. (S) 2 L 7 4 4F RT A20WE 20080828 EA 2008 8 28 QXEA200800602 1 20080530 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 797 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 610QX 10033 RFD-C4 CHECK - CORRODED SIDE SEAT TRACK ON RT SIDE AT FS 797. BLENDED CORROSION FROM RT SIDE SEAT TRACK AT FS 797. REM OVED .005 MATERIAL FOR BLEND, WITHIN LIMITS. MAX ALLOWABLE BLEND IS .035 INCHES. ALL WORK DONE IAW CRJ BOMB REO 670-53 -00-013. TREATED IAW CRJ 700 SRM 51-21-11. (S) 2 L 7 2 4F RT A21EA 20080828 EA 2008 8 28 A6WA200840551 1 20080718 A 2910 887055 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM INOPERATIVE A A6WA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 31 449AW 9408 7818 HYD 2 LOW PRESSURE CAUTION MESSAGE IN FLIGHT, COMPLIED WITH QRH, ENGINE NR 2 RAN APPROXIMATELY 45 MINUTES WITH ZERO HYDR AULIC QUANTITY. FOUND PRESSURE LINE DISCONNECTED FROM PRESSURE MANIFOLD, RECONNECTED LINE. LEAK CHECKED GOOD. REMOVED AND REPLACED EDP NR 2 DUE TO EXCESSIVE CAVITATION IAW AMM 29-11-01 AND AWAC SUPP 06-029, OPS AND LEAK CHECK GOOD. FOUN D SEVERAL DAMAGED FAIRLEADS. REPLACED DAMAGED FAIRLEADS IAW AMM 29-11. (A) 2 L 7 2 4F RT A21EA 20080828 NE 2008 8 28 COEA0801700 2 20080818 A 7310 O-RING CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE FUEL NOZZLE WORN A COEA C E ABORTED TAKEOFF ENGINE SHUTDOWN B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS TO TAKEOFF 1 NM 13 700FX 208B0419 ABORTED TAKEOFF. FLT 7665 BLI TO ORS: THE ENG LOST POWER AND WENT TO LOW IDLE. AFTER STOPPING THE ODOR OF FUEL COULD BE DETECTED. AS A PRECAUTION, THE ENG WAS SHUTDOWN. MAINTENANCE FOUND ONE OF THE FUEL TRANSFER TUBES BETWEEN FUEL NOZZ LES 9 & 10 BACKED OUT OF NOZZLE 9. REMOVED AND REPLACED THE FUEL NOZZLE TRANSFER TUBE RETAINER AND REINSTALLED THE TRAN SFER TUBES WITH NEW O-RINGS. (S) 1 H 7 1 3T 3 T A37CE E4EA 20080828 2008 8 28 DXTA200803194 4 20080720 A 3160 DISPLAY RAYTHN DH125 HAWKER800XP 7150012 CE NR 1 MDF FAILED E DXTA O OTHER B P SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION NR NOT REPORTED 1 GL 07 880QS 258570 NR 1 MDF WENT COMPLETELY BLANK IN FLIGHT, NOTICED A SLIGHT ODOR SO PULLED MFD BREAKER AS A PRECAUTION. (A) 2 L 7 2 4F RT A3EU 20080828 NM 2008 8 28 ABXA080183 1 20080603 A 5330 141T333040 SKIN BOEING 767 767232 1385132 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 742AX 22217 LOWER AFT CORNER OF R1 DOOR CUTOUT HAD CRACKS IN BOTH SKIN LAYERS. REPAIRED DOOR CORNER IAW B767 SRM 53-10-01. (A) 2 L 7 2 4F RT A1NM 20080828 WP 2008 8 28 ABXA080182 1 20080602 A 5312 59101303 BULKHEAD DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 LT LOWER CORNER OF AFT PRESSURE BULKHEAD DOOR JAMB SKIN WAS CRACKED. CAN BE SEEN FROM CATWALK. REMOVED WALKWAY, REPAIR ED AREA IAW REA D953-57424 MR. RE-INSTALLED WALKWAY IAW DC9 SRM 51-30-4. (A) 2 L 7 2 4F A6WE 20080826 SO 2008 8 26 MAS2008F00006 1 20080606 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX LACK OF LUBE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FDM 6149 JFK - MAIN CABIN DOOR HARD TO OPEN. MX LUBED DOOR. (B) 2 L 7 2 4T RT T00011AT 20080826 SO 2008 8 26 C2XA08IA178 1 20080727 A 2450 860CC01 CONTACTOR EMB 145 EMB145LR 3260212 SO ELECTRICAL MALFUNCTIONED A C2XA O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 27 13949 145057 IAH - FLIGHT 2350, THE CREW REPORTED THAT AT FL360, THE AIRCRAFT LOST ALL ELECTRICAL POWER FOR 10 SECONDS, POWER RETURNE D FOR 2 SECONDS, WAS INTERMITTENT FOR 2 MINUTES WITH T/O CONFIG, AUTOPILOT, FLAPS, STALL WARNINGS. THE POWER WAS FINALL Y RESTORED AFTER THREE MINUTES. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ESSENTIAL BUSS CONTACTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080827 SO 2008 8 27 CHQA200800134 1 20080708 A 2930 INDICATION SYS EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL HYDRAULIC SYS MALFUNCTIONED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 282SK 145409 CAE312622 FLIGHT 3043, LGA TO IND. DURING CLIMBOUT OF LGA THE FLT CREW RECEIVED A HYDRAULIC 1 LOW QUANTITY EICAS MESSAGE. THE HY DRAULIC QUANTITY INDICATED AT THE TOP OF THE YELLOW RANGE. THIRTY MINUTES LATER THE QTY INDICATION HAD DROPPED TO JUST BELOW ONE THIRD OF THE YELLOW RANGE. AT THAT TIME IT WAS DECIDED TO DIVERT TO CMH, WHERE THE AIRCRAFT LANDED WITHOUT IN CIDENT. MAINTENANCE INSPECTED THE NR 1 HYDRAULIC SYSTEM AND RAN ALL SYSTEMS AND SERVICED THE NR 1 HYDRAULIC SYSTEM. NO LEAKS WERE NOTED ON THE OUTSIDE OF THE AIRCRAFT IAW EMB MM 29-00-00 AND 12-31-01. NO OTHER DEFECTS WERE NOTED AND THE AIRCRAFT RETURNED TO SERVICE. (A) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080827 EA 2008 8 27 VNAA0807011 1 20080721 A 5100 NONE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NOT AN SDR NONE A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 248PS 7925 CREW REPORTED A BIRD STRIKE ON NOSE OF AIRCRAFT. CREW ELECTED TO RETURN TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANC E CLEANED AND INSPECTED AIRCRAFT. NO DAMAGE WAS NOTED AND AIRCRAFT WAS RELEASED TO SERVICE. (A) [NOT AN SDR] 2 L 7 2 4F 4 F RT A21EA E15NE 20080827 EA 2008 8 27 VNAA0807014 1 20080724 A 2150 782790 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LEFT FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 05 237PS 7906 CREW REPORTED, THE LT PACK TEMP TO BE 113 DEG C AND UNCONTROLLABLE IN AUTO OR MANUAL. CREW ELECTED TO RETURN TO DTW LAN DING WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LT AIR CYCLE MACHINE. CHECKS WE RE ACCOMPLISHED WITH NO DEFECTS AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (A) 2 L 7 2 4F 4 F RT A21EA E15NE 20080827 NM 2008 8 27 ABXA080201 1 20080717 A 5410 311T106577 DOOR BOEING 767 767232 1385132 NM NR 2 PYLON MISSING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 741AX 22215 STA MIA, ON WALKAROUND, MAINTENANCE FOUND CIRCULAR PANEL ON NR 2 PYLON OUTBOARD SIDE MISSING. DEFERRED DI 61119. CLEAR ED DI, INSTALLED NEW PANEL ON NR 2 PYLON. (A) 2 L 7 2 4F RT A1NM 20080827 EU 2008 8 27 KCS2008F00005 1 20080715 A 5310 MY20812001 WINDOW FRAME AMD FALC20 FALCON20D5 2730003 EU COCKPIT CRACKED A KCSA O OTHER O OTHER NR NOT REPORTED 1 GL 23 192CK 23619 192 CENTER WINDSHIELD FRAME WAS FOUND CRACKED DURING INSPECTION REQUIRED BY FALCON JET. THE WINDOW FRAME WILL BE REPLACED U SING FALCON JET APPROVED PROCEDURES, DRAWINGS AND NEW WINDOW FRAME. NOTE, COMPLETE PART NUMBER ON FRAME IS NOT LEGIBLE. (A) 2 L 7 2 4F RT A7EU 20080827 NM 2008 8 27 KCSA081340 1 20080723 A 5414 SKIN BOEING 747 747209B 138489B NM NR 3 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 715CK 22447 INBOARD SIDE OF NR 3 PYLON EXTERIOR SKIN CRACKED .500 IN NAC STA 176 FROM EDGE OF SKIN EXTENDING UNDER PREVIOUS REPAIR D OUBLER. (A) 2 L 7 4 4F RT A20WE 20080827 NM 2008 8 27 P5CA0801568 1 20080605 A 3150 WARNING LIGHT BOEING 747 74746NF 13848BT NM ILLUMINATED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 451PA 30809 DURING PUSHBACK AND ENGINE START "HYD DEM 3" STATUS MESSAGE APPEARED. AIRCRAFT CAME BACK TO BLOCKS. "ITEM WAS DEFERRED IAW MEL 29-11-2-2. NO OTHER ISSUES. (A) 2 L 7 4 4F RT A20WE 20080827 EA 2008 8 27 REX2008F00020 1 20080725 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8694A 13715 7694 RECEIVED "FLAP FAIL" MESSAGE ON APPROACH, QRH FOLLOWED WITH UNEVENTFUL LANDING. REMOVED AND REPLACED THE RT BRAKE POSIT ION SENSING UNIT (BPSU) AND RIGGED FLAPS IAW AMM. (A) 2 L 7 2 4F RT A21EA 20080827 NM 2008 8 27 HNAA0800214 1 20080622 A 7930 APT761000100DW TRANSMITTER DHAV DHC8 DHC8102 2809003 NM NR 1 ENG OIL SYS MALFUNCTIONED A HNAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 07 941HA 49072 161 AIR RETURN NR 1 OIL PRESS GAUGE FLUXED FROM 50 TO 0 THEN BACK TO 40. W/NO OIL WARNING LIGHT SO ENGINE WAS NOT SHUT DOWN . REMOVED AND REPLACED OIL PRESS XMITTER OPS AND LEAK CHECK GOOD. DEPARTURE AIR READINGS NORMAL. REMOVED AND REPLACED NR 2 ENGINE OIL PRESSURE SWITCH P/N 8D1437 OPS AND LEAK CHECK GOOD. (A) 2 H 7 2 4T RT A13NM 20080827 CE 2008 8 27 DXTA200803184 1 20080719 A 3246 WHEEL CESSNA 750 750 2076810 CE NLG VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 955QS 7500055 SEVERE NOSE WHEEL SHIMMY VIBRATION STARTED AT APPROX 100KTS ON TAKEOFF ROLL. DID NOT STOP UNTIL APPROX 60 KTS DURING AB ORT. (A) 2 L 7 2 4J RT T00007WI 20080827 NE 2008 8 27 P5CA0801569 2 20080613 A 7200 ENGINE BOEING 747 74746NF 13848BT NM GE CF6 CF680 30025 NE NR 4 FAILED A P5CA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 EA 15 450PA 30808 AT DESCENT, ENGINE NR 4 SHUT DOWN AND RESTARTED 6 TIMES. AFTER THE 6TH RESTART ENGINE SHUTDOWN AND LEFT OFF. AIRCRAFT LANDED SAFELY AND WITHOUT DECLARING EMERGENCY. FOUND NR 4 ENGINE OUT OF BOROSCOPE LIMITS PER AMM. REMOVED AND REPLACED NR 4 ENGINE. (A) 2 L 7 4 4F 4 F RT A20WE E13NE 20080827 NM 2008 8 27 DXTA200803185 1 20080719 A 2780 SLAT SYSTEM GULSTM 200 200 4500308 NM MALFUNCTIONED E DXTA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 07 712QS 073 WHEN RETRACTING SLATS AFTER TAKEOFF A THUD WAS FELT AND SLATS WOULD NOT RETRACT. SLATS UNBALANCED. MESSAGE APPEARS ON EICAS. (A) 2 L 7 2 4F RT A53NM 20080827 NM 2008 8 27 DXTA200803190 1 20080720 A 3230 LANDING GEAR GULSTM 200 200 4500308 NM LEFT UNLOCKED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 727QS 113 UPON GEAR RETRACTION, THE LT MAIN GEAR INDICATOR SHOWED RED CROSSHATCH GEAR UNSAFE WITH THE NOSE AND RT MAIN SHOWING UP AND LOCKED. REPEAT WRITE UP FROM 6/24/08. FOLLOWED QRH PP E6-3 "GEAR DOES NOT LOCK UP" CHECKLIST. (A) 2 L 7 2 4F RT A53NM 20080827 CE 2008 8 27 DXTA20083188 1 20080719 A 2120 UNKNOWN CESSNA 560 560XL 2076702 CE CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 662QS 5605262 JUST PRIOR TO LEVEL OFF AT 15,000 FT, STARTED SMELLING A STRONG "BURNING" ODOR. AT LEVEL OFF, WITH POWER REDUCED, THE O DOR DISSIPATED. ODOR RECURRED ON APPROACH WITH POWER INCREASES. (A) 2 L 7 2 4F RT A22CE 20080827 NM 2008 8 27 ABXA080208 1 20080710 A 5347 96F667576507 SEAT TRACK BOEING 767 767281 1385109 NM BS 424-500 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 773AX 22788 SEAT TRACK STA 424-500 HAD CORROSION RT BUTT LIVE 18. REPLACED SEAT TRACK BS 325-555, RT BUTT LIVE 18 IAW B767 SRM. (A ) 2 L 7 2 4F RT A1NM 20080827 NM 2008 8 27 WRLA2008068A 1 20080820 A 5310 AEA05261 DOUBLER DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE CLG WHEEL WELL CRACKED A WRLA O OTHER O OTHER NR NOT REPORTED 1 SO 11 274WA 48633 DURING A CHECK INSPECTION SR TECHNICS, CRACKS FOUND ON CENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD LT SIDE AROUND LA TERAL CONTROL MIXER DOUBLERS. REPAIRED PER WORLD AIRWAYS ENGINEERING REPAIR AUTHORIZTION DOCUMENT 08-53-73. (S) 2 L 7 3 4F 4 F RT A22WE E24NE 20080827 EA 2008 8 27 MAS2008F00017 1 20080804 A 3350 1317 BULB CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 935LR 15035 ASH FLT 2831 PHX-TUS. EMERGENCY FLOOD LIGHT 3RD FROM AFT INOPERATIVE. MAINTENANCE REPLACED BULB, OPS CHECK GOOD. (S) 2 L 7 2 4F RT A21EA 20080827 EA 2008 8 27 MAS2008F00025 1 20080810 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA EMEGENCY LIGHT BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75998 7336 ASH FLT 7074 ORD-MBS. EMERGENCY FLOOR LIGHT STRIP LENS AT ROW 1 WAS BROKEN. MAINTENANCE REPLACED THE LIGHT STRIP AND O PS CHECKED. (S) 2 L 7 2 4F RT A21EA 20080827 EU 2008 8 27 YENA2008080 1 20080816 A 3610 342B040000 THERMOSTAT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR2 ENGINE FAILED A YENA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 535JB 1739 FLT 640, SFO-JFK, DIVERTED TO LGB, ENG 1 AND ENG 2 BLEED FAULTS DURING TAKEOFF DEPARTURE PHASE, ENG 2 BLEED FAULT OCCURR ED FIRST. REPLACED NR 2 ENG THERMOSTAT FIN7170HM2. LEAK CHECK GOOD. REF AMM 36-11-06. REMOVED AND REPLACED NR 1 ENG FAN AIR VALVE THERMOSTAT FOR TROUBLESHOOTING IAW 36-11-43-04 71770HM1. LEAK CHECK OK. (S) 2 L 7 2 4F 4 F RT A28NM E40NE 20080827 NM 2008 8 27 F3LA200800563 1 20080816 A 5330 SKIN AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 5330 47 2836 MAINTENANCE NOTED LIGHTNING STRIKE DAMAGE AT LAP SEAM AT STRINGER 6L, .25 INCH FROM RIVET EDGE AT FRAME 30. ENGINEERING AUTHORIZATION A9-53R-30571 INDICATES MAJOR REPAIR. (S) MX COMPLIED WITH ENGINEERING AUTHORIZATION NR A9-53R-30571. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. REQUIREMENT TO REINSPECT REPAIR AT 32,800 FLIGHT CYCLES. 2 L 7 2 4F RT A28NM 20080827 EU 2008 8 27 S6G2008F00000 1 20080814 A 6330 1090330171 FITTING AGUSTA A109 A109E 0260119 EU TRANSMISSION CRACKED A S6GA O OTHER O OTHER NR NOT REPORTED 1 GL 15 30NM 11065 REPLACE TRANSMISSION TORQUE PLATE DOUBLER P/N 109-0330-17-1 AT CUSTOMER FACILITY. REMOVED AND REPLACED LT TRANSMISSION TORQUE PLATE FITTING P/N 109-030-17-1 IAW AGUSTA DRAWING 109-0330-14 ISSUE B, AGUSTA TIMS00000316 DATED 09/29/2006, PSEA W109/2008/TIMS00002266 AND A109 SRM 3-3-1. NOTE: LT FWD SHIM MEASURED 0.066 INCH, AFT SHIM MEASURED 0.0035 INCH. RT A FT SHIM MEASURED 0.074 INCH. (S) 1 G 7 2 3U RT H7EU 20080827 NM 2008 8 27 HNA2008F00041 1 20080812 A 3246 WHEEL DHAV DHC8 DHC8102 2809003 NM NLG OUT OF BALANCE A HNAA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 EA 07 826EX 32161 32161 389 AFTER TAKEOFF SEVERE NOSE TIRE SHIMMY. CREW BURNED FUEL TIL GOOD TO LAND, RETURNED TO PHL. BURNED OFF FUEL, RETURNED T O FIELD. MAINTENANCE REPLACED NOSE WHEELS. NO OTHER DEFECTS NOTED. (S) 2 H 7 2 4T RT A13NM 20080827 NM 2008 8 27 HNA2008F00039 1 20080812 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 809EX 41576 41576 302 EMERGENCY LIGHTS FLASHED OFF AND ON DURING TOUCHDOWN. PILOT REPORTED TO MAINTENANCE. PERFORMED EMERGENCY LIGHTS CHECK PER WORK CARD 33-50-03. OPS CHECK GOOD. (S) 2 H 7 2 4T RT A13NM 20080827 EA 2008 8 27 MAS2008F00022 1 20080810 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 942LR 15042 ASH FLT 2836 PHX-BUR. GALLEY EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE RELAMPED. (S) 2 L 7 2 4F RT A21EA 20080827 2008 8 27 HNA2008F00044 4 20080812 A 3442 071013190030 RADAR DHAV DHC8 DHC8102 2809003 NM WX SYSTEM INOPERATIVE A HNAA O OTHER G MULTIPLE FAILURE CR CRUISE 1 EA 07 980HA 32924 32924 376 WEATHER RADAR W/N PAINT, TX FAULT AND AFC MESSAGE. ACFT DIVERTED TO LGA. MAINTENANCE REMOVED AND REPLACED RADAR RT. O PS CHECK GOOD. (S) 2 H 7 2 4T RT A13NM 20080827 NM 2008 8 27 HNA2008F00049 1 20080820 A 3350 316 BULB DHAV DHC8 DHC8102 2809003 NM EMERGENCY LIGHT INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 825EX 388 MOST REAR OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPS CHECK GOOD. (S) 2 H 7 2 4T RT A13NM 20080828 EA 2008 8 28 MAS2008F00023 1 20080810 A 5210 SEAL CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 905J 15005 ASH FLT 2766 PHX-SAT - PASSENGER DOOR NOISY WITH A VISUAL GAP IN THE UPPER LT CORNER. INSPECTED AND CLEANED DOOR AND S EAL. OPS GOOD. (S) 2 L 7 2 4F RT A21EA 20080828 SO 2008 8 28 C2XA08ON168 1 20080814 A 2720 15H0048PH PRESSURE SWITCH EMB 145 EMB145XR 3260214 SO RUDDER INOPERATIVE A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 27 11194 8442 4393 14500940 FLT 0002 -OKC- FLIGHT CREW REPORTED RUDDER 2 SYSTEM INOP ON APPROACH AND DECLARED EMERGENCY AND IT LANDED SAFELY WITHOUT INCIDENT. MAINTENANCE RESET RUDDER SYSTEM 2 AND RELEASED THE ACFT ON A FERRY FLIGHT TO AUS. REMOVED AND REPLACED BOTH PRESSURE SWITCHES. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S) 2 L 7 2 4F RT 20080828 NM 2008 8 28 F3LA200800560 1 20080816 A 5330 SKIN AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 948FR 47 2836 MAINTENANCE NOTED LIGHTNING STRIKE DAMAGE AT LAP SEAM AT STRINGER 6L, BETWEEN FRAME 27 AND FRAME 28, 1.5 INCHES. ENGINE ERING AUTHORIZATION A9-53R-30571 INDICATES MAJOR REPAIR. (S) MX COMPLIED WITH ENGINEERING AUTHORIZATION NR A9-53R-3057 1. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. REQUIREMENT TO REINSPECT REPAIR AT 32,800 FLIG HT CYCLES. 2 L 7 2 4F RT A28NM 20080828 NM 2008 8 28 USAA920081542 1 20080812 A 5320 65C105922 FLOOR SUPPORT BOEING 737 7373G7 1384595 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN-C19 - MAJOR REPAIR - EXFOLIATION CORROSION ON FLOOR SUPPORT AT BS 947 TO BS 967, RBL 8. REPLACED FLOOR SUPPORT AT B S 947 TO BS 967, RBL 8 IAW B737 SRM 51-40-02-0G. (S) 2 L 7 2 4F RT A16WE 20080828 EA 2008 8 28 A6WA200840527 1 20080623 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 446AW 7806 CRACK FOUND ON CROSS BEAM AT FS 280.00 RBL 9.0. CROSS BEAM AT FS 280.00 RBL 9 REPAIRED IAW CRJ 200 REO 601R-53-11-171 R EV D SCHEME A. (A) 2 L 7 2 4F RT A21EA 20080828 NM 2008 8 28 F3LA200800566 1 20080816 A 5330 SKIN AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 948FR 47 2836 MAINTENANCE NOTED LIGHTNING STRIKE DAMAGE AT LAP SEAM AT STRINGER 6L, .25 INCH FROM RIVET EDGE AT FRAME 27. ENGINEERING AUTHORIZATION A9-53R-30571 INDICATES MAJOR REPAIR. (S) MX COMPLIED WITH ENGINEERING AUTHORIZATION NR A9-53R-30571. U PON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. REQUIREMENT TO REINSPECT REPAIR AT 32,800 FLIGHT CY CLES. 2 L 7 2 4F RT A28NM 20080828 NE 2008 8 28 A6WA200840537 2 20080705 A 7200 ENGINE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* 30015 NE NR 2 SHUTDOWN A A6WA E A ENGINE SHUTDOWN UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 GL 31 434AW 7322 AIR DIVERT TO IAD, ENGINE NR 2 SHUTDOWN ON TAKEOFF. FELT DISTINCT POP ON THROTTLE CONTROLS. ENGINE SPOOLED UP NORMALLY . UPON LEVEL-OFF, FIRST OFFICER ATTEMPTED TO REDUCE POWER AND RT ENGINE FAILED TO RESPOND. FLEW AROUND ON BOTH ENGINE FOR ABOUT 10 MINUTES BEFORE PERFORMING A PRECAUTIONARY SHUTDOWN. USED RT ENGINE FIRE PUSH TO SHUTDOWN THE ENGINE. DID NOT PUSH THE FIRE BOTTLE BUTTON. CORRECTIVE ACTION IN PROGRESS. (A) 2 L 7 2 4F 4 F RT A21EA 20080828 EA 2008 8 28 MAS2008F00033 1 20080812 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 931LR 15031 ASH FLT 2683 CLT-MEM - EMERGENCY FLOOR STRIPPING COVER NEEDS SECURED. MAINTENANCE FOUND THE ENTIRE SECTION NEEDED REPLA CED AND REPLACED IT. (S) 2 L 7 2 4F RT A21EA 20080828 EA 2008 8 28 HNA2008F00042 1 20080812 A 3150 858301 PSEU DHAV DHC8 DHC8311 1386006 EA WARNING HORN MALFUNCTIONED A HNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 07 337EN 34300 34300 284 ABORTED TAKEOFF DUE TO TAKEOFF WARNING HORN. MAINTENANCE COMPLIED WITH TAKEOFF WARNING WORK CARD. CHECK GOOD WITH NO F AULTS. MAINTENANCE REPLACED THE PSEU AS A POSITIVE MAINTENANCE ACTION. (S) 2 H 7 2 4T RT A13NM 20080828 EA 2008 8 28 MAS2008F00044 1 20080818 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNSECURE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 97325 7325 FLT 2719 - PHS-SBA - PAX DOOR OUTER HANDLE WILL NOT STOW. MAINTENANCE REPOSITIONED ACFT TO LEVEL RAMP. OPS GOOD. (S) 2 L 7 2 4F RT A21EA 20080828 EA 2008 8 28 MAS2008F00045 1 20080817 A 3250 PRESSURE SWITCH CNDAIR CL600 CL6002C10 1390015 EA NLG STEERING MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 501MJ 10047 ASH FLT 7046 - ORD-PWM - NOSE WHEEL STEERING INOPERATIVE CAUTION MESSAGE. MAINTENANCE RERACKED ECU AND CLEANED PRESSURE SWITCH ON MANIFOLD. OPS GOOD. (S) 2 L 7 2 4F RT A21EA 20080828 CE 2008 8 28 GUU2008F00043 1 20080818 A 5210 STRUT BEECH 1900 1900D 1154162 CE PAX DOOR MALFUNCTIONED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 87554 UE227 FLIGHT 9137 - ASD-FLL - PILOT REPORTED MAIN CABIN DOOR FALLS RAPIDLY. SERVICED MAIN CABIN DOOR STRUT. (S) 2 L 7 2 4T RT A24CE 20080825 EU 2008 8 25 COEA0804703 1 20080812 A 5711 SPAR FOKKER F27 F27MK600 4990706 EU LT WING PUNCTURED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 703FE 37189 10420 MAJOR REPAIR: LT WING FRONT SPAR WEB HAS A PUNCTURE HOLE AT WS 11560. DISCOVERED DURING MAINTENANCE AFTER TAXI INCIDEN T. (S) CUT OUT THE DAMAGED AREA ON THE WING FRONT SPAR WEB PLATE. FABRICATED AND INSTALLED A REPAIR PLATE WITH FILLER S. ISSUED FIELD ENGINEERING ORDER NR 5730-11 TO FACILITATE THE REPAIR. 2 H 7 2 4T A817 20080825 EU 2008 8 25 USAA920081516 1 20080813 A 2530 26253590002 CHILLER AIRBUS A319 A319112 3930323 EU GALLEY FAULTY A U30A K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 17 725UW 24225 2375 1135 FLT 1177-LGA-CLT- BURNING ODOR - FORWARD CHILLER HAS A BURNING ODOR. TURNED CHILLER OFF AND ODOR DISSIPATED. MAINTENAN CE REMOVED AND REPLACED FORWARD CHILLER. OPERATIONAL CHECK WAS GOOD. (S) 2 L 7 2 4F RT A28NM 20080825 NM 2008 8 25 ABXA080218 1 20080809 A 5343 BOLT BOEING 767 767281 1385109 NM TRUNNION MISSING A ABXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 796AX 23146 LT MAIN LANDING GEAR TRUNNION DOOR FITTING ON TOP OF STRUT MISSING AFT BOLT AND ATTACHING HARDWARE. INSTALLED CORRECT H ARDWARE PER IPC 32-12-01-5, SHEET 2 AND AMM 32-12-06. (BOLTS 2 EA-BACB30LJ6U15). (S) 2 L 7 2 4F RT A1NM 20080826 CE 2008 8 26 GUU2008F00029 1 20080803 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE CABIN ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 17 231YV UE231 FLIGHT 5406 PBI/FLL, DURING FLIGHT LIGHT FUEL ODOR INSIDE ACFT. INSPECTED FUEL AUX TANKS, RAN ENGS WITH BLEEDS OPEN. N O FUEL ODOR DETECTED. (S) 2 L 7 2 4T RT A24CE 20080826 NM 2008 8 26 USAA920081517 1 20080811 A 5330 6545775 SKIN BOEING 737 7374B7 1384702 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 488UW 25022 CLT -C6- MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT BS 727D, S23R. REPAIRED FUSELAGE SKIN AT BS 727D, S23R IAW B737 SRM 5 3-00-01 REPAIR 31 (TR 53-27). (S) 2 L 7 2 4F RT A16WE 20080826 WP 2008 8 26 IXX2008F00068 1 20080609 A 5730 SKIN DOUG DC8 DC872F 302199E WP RT WING MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON RT WING OTBD SLOT VANE LEADING EDGE AT STATION XOLDO 67.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECT ION. NO CRACK, NO CORROSION FOUND. FABRICATED DOUBLERS, FILLERS, INTERNAL DOUBLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XOLDI 6.224-XOLDO 67.000 IAW FAA FORM 8110-3 0837 8 DATED 07/11/2008, SEMAN DRAWING ED4809 DATED 06/23/08, DC8 SRM 51-1-21, SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-1-20D AND SRM 51-3-1. (S) 2 L 7 4 4F RT 4A25 20080826 EA 2008 8 26 TRAX3200800943 1 20080728 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 926EV 7843 JUST OUTBOARD LBL 9, FS 280 UPPER SILL CRACKED APPROX 1 INCH LONG AT MLG EMERGENCY RELEASE CABLE BRACKET. REMOVED MLG E MERGENCY RELEASE CABLE BRACKET IAW SRM 51-41-02. REPAIRED LBL 9 FS 280 UPPER SILL IAW REO 601R-53-11-138-NC AND DEVIATI ON REO 601R-53-11-1441. RE-INSTALLED MLG EMERGENCY RELEASE CABLE BRACKET IAW SRM 51-41-02. FUNCTIONAL TEST OF EMERGENC Y GEAR EXTENSION DUE. PERFORMED FUNCTIONAL TEST OF EMERGENCY GEAR EXTENSION IAW AMM 32-34-00-720-801. FUNCTIONAL TEST OK AT THIS TIME. COMPLIED WITH ASA ECTC REO 601R-53-11-1441 IAW REO 601R-53-11-1441. COMPLIED WITH ASA EC-TC REO 601R- 53-11-138. ASA RII COMPLIED WITH. (S) 2 L 7 2 4F RT A21EA 20080826 SO 2008 8 26 C2XA08IA158 1 20080708 A 2750 14568000434 FLAP EMB 135 EMB135LR 3260305 SO RT WING OUT OF ADJUST A C2XA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 27 12528 14676 145504 IAH - FLIGHT 2460, THE CREW REPORTED A FLAP FAIL MESSAGE IN FLIGHT AND PERFORMED AN EMERGENCY DESCENT AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE RT HAND INBOARD FLAP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4F RT T00011AT 20080826 SO 2008 8 26 C2XA08IA162 1 20080709 A 3350 7287580509 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15980 145202 MCI - DURING MAINTENANCE INSPECTION THE AISLE PATH LIGHTING BETWEEN SEATS 15A & 17A WERE FOUND TO BE INOPERATIVE. MAINT ENANCE REMOVED AND REPLACED THE AFFECTED LIGHT STRIP, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. (A) 2 L 7 2 4T RT T00011AT 20080826 EA 2008 8 26 C2XA08IA160 2 20080713 A 7261 OIL SYSTEM EMB 145 EMB145EP 3260221 SO RROYCE AE3007 AE3007A1P 54571 EA LT ENGINE LEAKING A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 27 14942 145037 CAE311333 IAH - FLIGHT 2684, THE CREW REPORTED THAT THE NUMBER ONE ENGINE OIL QUANTITY DROPPED TO 3 QTS IN FLIGHT WHILE PRESSURE A ND TEMPERATURE REMAINED NORMAL. THE CREW SHUT DOWN THE NUMBER ONE ENGINE AS A PRECAUTION AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY TESTED WITH NO DEFECTS, AND TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20080826 SO 2008 8 26 C2XA08CL078 1 20080703 A 3350 3104404 FUSE EMB 145 EMB145LR 3260212 SO BATTERY PACK INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26545 145558 DURING ROUTINE MAINTENANCE BOTH AFT EXTERNAL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE FUSE ON THE NR 4 EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECKS WERE GOOD. (A) 2 L 7 2 4T RT T00011AT 20080826 SO 2008 8 26 C2XA08CL085 1 20080714 A 2560 P4010030 BATTERY EMB 145 EMB145XR 3260214 SO FLASHLIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17159 145792 DURING ROUTINE MAINTENANCE THE FIRST OFFICER’S EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE FLA SHLIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD. (A) 2 L 7 2 4F RT 20080826 SO 2008 8 26 C2XA08CL082 1 20080707 A 5310 NAS109634 SCREW EMB 145 EMB145XR 3260214 SO DOOR FRAME LOOSE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11137 145721 DURING ROUTINE MAINTENANCE THE LT EMERGENCY EXIT HATCH WOULDN’T OPEN. MAINTENANCE INSPECTED AND FOUND SCREW LOOSE ON SI DE OF DOOR FRAME. THE SCREW WAS TIGHTENED AND OPERATIONAL CHECKS OF THE DOOR WAS GOOD. (A) 2 L 7 2 4F RT 20080826 2008 8 26 USAABB08132 4 20080813 A 2565 D30654122 SLIDE BOEING 757 7572B7 1384964 NM ZONE 200 FAILED A USAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 19 942UW 39225 3308 27807 PHL - WHILE PARKED AT A REMOTE GATE, THE L1 DOOR WAS ACCIDENTALLY OPENED WHILE THE EMERGENCY EVACUATION SLIDE WAS STILL ARMED. THE SLIDE DEPLOYED, BUT DID NOT INFLATE. MAINTENANCE REPLACED THE EMERGENCY EVACUATION SLIDE AT THE L1 DOOR. O K FOR SERVICE. (S) 2 L 7 2 4F RT A2NM 20080826 CE 2008 8 26 AWK2008F00000 1 20080809 A 2121 414F FAN CESSNA 750 750 2076810 CE COCKPIT ODOR E AWKA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 25 747XJ 2993 7500247 CREW REPORTED A PUFF OF SMOKE FROM BEHIND THE COPILOT SEAT AND A BURNED ELECTRICAL ODOR DURING DESCENT INTO CMH. REMOVE D COCKPIT ZONE TEMPERATURE SENSOR/FAN ASSY COVER AND FOUND TRACE EVIDENCE OF SMOKE MARKS. SUSPECT THAT FOD WAS TRAPPED IN THE ZONE TEMPERATURE FAN ASSY AND CAUSED SMOKE. REMOVED AND INSTALLED A NEW COCKPIT ZONE TEMPERATURE SENSOR P/N: 991 4130-6 AND FAN ASSY P/N: 414F. (S) 2 L 7 2 4J RT T00007WI 20080826 WP 2008 8 26 IXX2008F00087 1 20080609 A 5753 SKIN DOUG DC8 DC872F 302199E WP RT WING TE FLAP WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 721CX 46013 DURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP UPPER SKIN SHOWS WEAR AT STATION XF 211.000. REMOVED FAS TENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND R EPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 4 TR 57-94 DATED 10-01-02, DC8 SRM 57-1- 0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, AND DC8 SRM 51-1-11. (S) 2 L 7 4 4F RT 4A25 20080827 EA 2008 8 27 REX2008F00019 1 20080718 A 5220 STOP FITTING CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT OUT OF ADJUST A REXA K NONE O OTHER IN INSP/MAINT 1 SO 25 8673D 7673 RIGHT OVERWING EMERGENCY EXIT WOULD NOT OPEN. ADJUSTED RT EMERGENCY DOOR FRAME STOPS IAW AMM 52-22-01. OPERATIONALLY C HECKS GOOD. (A) 2 L 7 2 4F RT A21EA 20080827 SO 2008 8 27 RAIA00806026 1 20080629 A 3397 WIRE EMB 145 EMB145 3260210 SO LIGHT ASSY LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 804HK 145082 PRE-FLT 3564 - STL - EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RE-SECURED WIRING TO THE LIGHT AND PERFORMED AN OPERATION AL CHECK OF THE SYSTEM WITH NO DEFECTS NOTES. (A) 2 L 7 2 4F RT T00011AT 20080827 NM 2008 8 27 P5CA0801570 1 20080627 A 8012 START VALVE BOEING 747 74746NF 13848BT NM NR 1 ENGINE FAILED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 451PA 30809 DURING PUSHBACK AND ENGINE START NR 1 STARTER CUTOUT MESSAGE APPEARED. AIRCRAFT RETURNED TO BLOCKS. START VALVE WAS RE PLACED, BUT NO HELP. ITEM WAS THEN DEFERRED IAW MEL 80-11-1. NO OTHER ISSUES. (A) 2 L 7 4 4F RT A20WE 20080828 SO 2008 8 28 C2XA08IA194 1 20080817 A 2810 2770138103 VALVE EMB 145 EMB145LR 3260212 SO LT WING WORN A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 12900 145511 IAH - FLIGHT 3048 - THE CREW REPORTED THAT AFTER TAKEOFF THE LT WING WAS LEAKING FUEL WITH AN IMBALANCE DEVELOPING. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT WING FLAP VALVE. LEAK CHECK WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080828 NM 2008 8 28 F3LA200800561 1 20080816 A 5330 SKIN AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 948FR 47 2836 MAINTENANCE NOTED LIGHTNING STRIKE DAMAGE ON PRODUCTION SEAM FRAME 24, 3.5 INCHES BELOW STRINGER 7L. ENGINEERING AUTHO RIZATION A9-53R-30571 INDICATES MAJOR REPAIR. (S) 2 L 7 2 4F RT A28NM 20080828 NM 2008 8 28 MAS2008F00046 1 20080818 A 5210 ROD DHAV DHC8 DHC8202 2809007 NM PAX DOOR BROKEN A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 436YV 436 ASH FLT 7098 - ASE-DEN - PASSENGER DOOR FWD SUPPORT ROD BROKEN. MAINTENANCE REMOVED AND REPLACED STRUT. OPS CHECK GOOD . (S) 2 H 7 2 4T RT A13NM 20080828 EA 2008 8 28 HNAA08A0004 1 20080618 A 5311 8533013108 FRAME DHAV DHC8 DHC8311 1386006 EA BS 593 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 335EN 32270 32270 375 CORROSION FOUND ON FRAME STA X593.5 BETWEEN STR 30 AND 31 RT SIDE. REPAIRED IAW SRM 51-40-00 AND DRAWING 85330908. (S) 2 H 7 2 4T RT A13NM 20080828 NM 2008 8 28 ABXA080185 1 20080603 A 5330 141T33340 SKIN BOEING 767 767232 1385132 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 742AX 22217 LOWER FORWARD OF R1 DOOR CUTOUT HAD A CRACK IN OUTER SKIN LAYER. REPAIRED LOWER FORWARD CORNER OF R1 DOOR IAW B767 SRM 53-10-01. (A) 2 L 7 2 4F RT A1NM 20080828 NM 2008 8 28 ABXA080184 1 20080603 A 5330 141T83208 SKIN BOEING 767 767232 1385132 NM FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 742AX 22217 LOWER AFT CORNER OF R1 DOOR CUTOUT HAD CRACKS IN BOTH SKIN LAYERS. REPAIRED DOOR CORNER IAW B767 SRM 53-10-01. (A) 2 L 7 2 4F RT A1NM 20080828 SO 2008 8 28 C2XA08RI111 1 20080819 A 2810 14569701405 VALVE EMB 145 EMB145XR 3260214 SO FUEL DIST INOPERATIVE A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 12166 14500831 FLIGHT 502 - RDU - FLIGHT CREW PERFORMED AIR RETURN DUE TO FUEL LEAKING FROM RT WING. CREW LANDED ACFT UNEVENTFULLY. M AINTENANCE REMOVED AND REPLACED FLAP VALVE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4F RT 20080828 NM 2008 8 28 KCSA081420 1 20080821 A 5330 SKIN BOEING 747 747249F 1384849 NM BS 1000 S40R CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 STA 1000 SKIN CORRODED AT STRINGER 40R. (S) 2 L 7 4 4F RT A20WE 20080828 SO 2008 8 28 CHQA200800164 1 20080818 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CABIN SMOKE A CHQA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 GL 11 259JQ 145763 CAE311619 FLIGHT 3080, SDF TO LGA - CREW RECEIVED A LAV SMOKE INDICATION DURING CLIMBOUT WITH A NOTICEABLE ODOR. THE MESSAGE CLEA RED WITHIN 30 SECONDS AND THE ODOR DISSIPATED WITHIN 2 MINUTES. THE ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED BOTH ENGS FOR SIGNS OF DEFECTS AND OIL POOLING WITH NO DEFECTS NOTED. BOTH BLEEDS WERE ISOLATED AND THE ENGS WERE RUN WITH NO DEFECTS NOTED. THE LAVATORY SMOKE DETECTION SYSTEM WAS ALSO TROUBLESHOT PER THE FIM WITH NO DEFECTS NOTED. (S) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20080828 SO 2008 8 28 RAIA00808016 1 20080815 A 5210 LATCH EMB 145 EMB145EP 3260221 SO PASSENGER DOOR LACK OF LUBE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 827HK 145021 PRE FLT 5483 - STL - PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE MAIN DOOR LATCH ASSEMBLY. OPS CHECKE D GOOD. (S) 2 L 7 2 4F RT T00011AT 20080828 NM 2008 8 28 USAABB08136 1 20080817 A 3350 2506500994001 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937UW 27245 BOS - THE EMERGENCY ESCAPE SLIDE LIGHT WAS INOPERATIVE AT THE R4 DOOR. MAINTENANCE REPLACED THE R4 DOOR EMERGENCY ESCAP E SLIDE LIGHT ASSEMBLY. OPERATIONALLY CHECKS OK. (S) 2 L 7 2 4F RT A2NM 20080829 NM 2008 8 29 SWAA084597 1 20080819 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM BS 440 S28R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER 28R CRACKED AT BS 440. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084600 1 20080819 A 5755 6545412 FITTING BOEING 737 7373Q8 1384670 NM NR 4 SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 4 SPOILER OUTBOARD LUG FITTING CRACKED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084601 1 20080819 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 714CB 27848 EEPLS LENS LOOSE AT ROW 8 ABC. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084685 1 20080825 A 5330 6545774 SKIN BOEING 737 737317 138447P NM BS 747 S24L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 24L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084733 1 20080826 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM BS 727B S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084739 1 20080826 A 5340 65C27314 STRINGER CLIP BOEING 737 7373T0 1384582 NM BS 344 S10R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 10R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080829 2008 8 29 SWAA084686 4 20080821 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 773SA 27881 R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPLACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084687 1 20080825 A 5315 147A5506 FLOORBEAM BOEING 737 7377H4 1384404 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 775SW 30590 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM TEE CAP CORRODED AT BS 986.5, BETWEEN RBL 14 AND LBL 40. REPAIRED TEE CAP PE R SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084690 1 20080825 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 400 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084744 1 20080826 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM BS 291 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN BEAR STRAP CRACKED AT FWD SERVICE DOOR BS 291.5, WL 232.5. REPAIRED S KIN PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084702 1 20080825 A 3350 3071BPEGPL LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084704 1 20080825 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 460 S15R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 460, STR 15R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 PCS2008F00001 1 20080819 A 5270 WARNING LIGHT BOEING 727 7272K5 138004P NM CARGO DOOR FALSE ACTIVATION A PCSA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 SO 17 909PG 21852 AMERIJET FLIGHT 8116 ON 8/19/08 TTPP-KMIA DIVERTED TO TJSJ. CREW LOG ITEM "AT FL340 BOTH CAPT AND FIRST OFFICER CARGO D OOR LIGHTS ILLUMINATED ALONG WITH FE CARGO DOOR AMBER LIGHT ALONG WITH DOOR WARNING AND MAIN CARGO DOOR NOT CLOSED LIGHT ON. POWER MASTER PANEL ILLUMINATED AND WOULD NOT RESET. FOLLOWED PROCEDURE LANDING IN SJU. ALL LIGHTS EXTINGUISHED A T 15000 FT." MAINTENANCE CHECKED THE DOOR ON ARRIVAL. FOUND PROPERLY CLOSED AND LOCKED WITH ALL LIGHTS EXTINGUISHED. THE DOOR WAS OPERATIONALLY CHECKED SEVERAL TIMES WITH NORMAL OPERATION PER THE AEI MM. THE ACFT WAS PRESSURIZED ON THE GROUND AND ALL LIGHTS STAYED EXTINGUISHED. THE ACFT WAS RETURNED TO SERVICE AND OPERATED NORMALLY ON THE CONTINUING FLI 2 L 7 3 4F RT A3WE 20080829 NM 2008 8 29 ABXA080222 1 20080807 A 5210 141T333053 STRUCTURE BOEING 767 767232 1385132 NM PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 745AX 22222 L1 DOOR LOWER AFT CORNER HAD CRACK STARTING FROM FASTENER HOLE, CRACK WAS .125 INCHES LONG. REPAIRED L1 DOOR LOWER AFT CORNER, IAW B767 SRM. (S) 2 L 7 2 4F RT A1NM 20080829 EA 2008 8 29 REX2008F00036 1 20080815 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A REXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 8631E 11577 7631 RECEIVED "FLAP FAIL" MESSAGE IN CRUISE, QRH FOLLOWED. EMERGENCY DECLARED FOLLOWED BY UNEVENTFUL LANDING. REMOVED AND RE PLACED RIGHT WING BRAKE POSITION SENSING UNIT (BPSU) IAW BOMBARDIER AMM, OPERATIONALLY CHECK FLAPS. (S) 2 L 7 2 4F RT A21EA 20080829 EA 2008 8 29 REX2008F00040 1 20080815 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A REXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 8631E 11577 7631 RECEIVED "FLAP FAIL" MESSAGE IN CRUISE. QRH FOLLOWED. EMERGENCY DECLARED FOLLOWED BY UNEVENTFUL LANDING. REMOVED AND REPLACED RT WING BRAKE POSITION SENSING UNIT (BPSU) IAW BOMBARDIER AMM, OPERATIONALLY CHECK FLAPS. (S) 2 L 7 2 4F RT A21EA 20080829 SO 2008 8 29 SIMA200823302 1 20080818 A 3240 21707 BRAKE EMB 145 EMB145LR 3260212 SO NR 3 FAILED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 668HH 145785 ON FLIGHT 3402 CREW REPORTED NR 3 BRAKE CAME APART DURING LANDING. ACFT REMOVED FROM SERVICE. REPLACED NR 3 BRAKE AND WHEEL ASSY AND PERFORMED INSPECTION OF RT GEAR AXLE ASSY. NO DEFECTS NOTED, REPLACED NR 4 BRAKE FOR PRECAUTION AND INSP ECTED NR 4 WHEEL ASSY. NO DEFECTS NOTED, BRAKE CHECKS GOOD. ACFT RETURNED TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080829 EA 2008 8 29 TRAX200801010 1 20080816 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA COCKPIT INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 871AS 7537 FIRST OFFICER`S FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FIRST OFFICER`S FLASHLIGHT. OPS CHECK GOOD IAW AMM 25-61- 04. (S) 2 L 7 2 4F RT A21EA 20080924 NM 2008 9 24 08FDEA03786 1 20080910 A 5754 ARB1667 SKIN DOUG MD11 MD11F 3023600 NM RT NR 3 SLAT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 623FE 48794 RIGHT WING NR 3 SLAT ASSY LOWER SECTION TRAILING EDGE FOUND WITH CHAFE MARKS. AREA REPAIRED AS PER EA 1-2780-122549, T HIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 08FDEA03787 1 20080910 A 5280 ANB70932 HINGE DOUG MD11 MD11F 3023600 NM RT MLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 623FE 48794 RT MAIN LANDING GEAR DOOR FOUND CRACK ON CENTER HINGE. REMOVED AND REPLACED AS PER SRM 51-31-01. 2 L 7 3 4F RT A22WE 20080924 EU 2008 9 24 08FDEA03788 1 20080910 A 5754 A53510218203 FITTING AIRBUS 300 A300B4622R 3930312 EU RT WING K FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSION OUT OF LIMIT ON RT WING, ON STRUCTURE FOR KRUEGER FLAP ATTACHMENT. REPAIR PERFROMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03789 1 20080910 A 5754 A53510219203 FITTING AIRBUS 300 A300B4622R 3930312 EU RT WING K FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSION OUT OF LIMIT ON RT WING, ON STRUCTURE FOR KRUEGER FLAP ATTACHMENT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03790 1 20080910 A 5754 A53510220201 FITTING AIRBUS 300 A300B4622R 3930312 EU RT WING K FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSION OUT OF LIMIT ON RT WING, ON STRUCTURE FOR KRUEGER FLAP ATTACHMENT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03578 1 20080825 A 5414 311N51931 SKIN PANEL BOEING 757 757236 1384971 NM NR 1 PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 NR 1 PYLON O/B FWD 311N5193-1 SKIN PANEL HAS CORROSION ON INNER SURFACE. REMOVED AND REPLACED SKIN PANEL IAW SRM 51-40- 02,AND DWG. 311N5002, 311N5108, CATEGORY A MAJOR REPAIR, NO FOLLOW-UP TRACKING REQUIRED. 2 L 7 2 4F RT A2NM 20080924 EU 2008 9 24 08FDEA03144 1 20080729 A 5321 B5327050600400 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN DECK FLOOR BOARD NR 232 YG IS DAMAGED. FABRICATED NEW FLOORBOARD NR 232 YG IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03579 1 20080825 A 5414 311N504632 SKIN PANEL BOEING 757 757236 1384971 NM NR 2 PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 NR 2 PYLON INTERIOR SURFACE BETWEEN PANELS 443 AR AND 443 BR HAS LIGHT CORROSION. REMOVED AND REPLACED NR 2 PYLON O/B S KIN PANEL P/N 311N5046-32 IAW DWG 311N5002 AND SRM 51-40-02, CATEGORY A MAJOR REPAIR NO FOLLOW-UP TRACKING REQUIRED . 2 L 7 2 4F RT A2NM 20080924 EU 2008 9 24 08FDEA03332 1 20080808 A 5321 R532B385100000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 262 AH IS DAMAGED. REPAIRED CABIN FLOOR PANEL 262 AH BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARK ED AND APPLIED NON-SKID TAPE IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080924 WP 2008 9 24 08FDEA03377 1 20080811 A 5313 AYB70132 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 CORROSION ON LONGERON 51L FROM BODY STA 1441 TO 1461. REMOVED DAMAGED SECTION OF LONGERON 51L FROM FS 1430 TO 1520 IAW SRM 51-33-01; PG 1; VOL II. LOCATED AND DRILLED NEW SECTION OF LONGERON 51L AND 2 EA SPLICES IAW DWG AYB 7013 AND SRM 53-00-01; FIG 9; PG 32; VOL I. ALODINED AND PRIMER NEW SECTION OF LONGERON AND 2 SPLICES IAW SRM 51-21-01; PGS 21 AND 24; VOL II. APPLIED TOP COAT OF PAINT IAW SRM 51-21-02; PG 1; VOL II. PART MARKED NW LONGERON FX AYB 7013-1IAW GMM 7- 0-1001. INSTALLED NEW SECTION OF LONGERON AND SPLICES IAW SRM 51-33-01; PG 1; VOL II AND SRM 53-00-01; FIG 9; PG 32; VO L I. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 08FDEA03108 1 20080729 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT F ITTING AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB CRACKED NR 1 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 08FDEA03791 1 20080910 A 5311 6515029 FRAME BOEING 727 727227 1384078 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 TOP OF FRAME DAMAGED UNDER "Z" FLOOR SUPPORT, FS 520, RBL 7, WL 155. REMOVED DAMAGE AT TOP OF FRAME. NDT VERIFIED DAMA GE REMOVAL, FABRICATED REPAIR DOUBLER, TREATED AND PRIMED DOUBLER AND DAMAGE CUT OUT. INSTALLED REPAIR DOUBLER, REF S RM 51-40-3 FIG 1, NDT MAN PART 6, 51-00-00 FIG 23. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080924 NM 2008 9 24 08FDEA03614 1 20080828 A 5347 69175901 SEAT TRACK BOEING 727 727227 1384078 NM BS 380-420 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 MAIN CARGO COMPARTMENT, CORROSION ON SEAT TRACK RBL 45 STA 380 STA 420 REMOVED 9G BULKHEAD AND ATTACHMENT PARTS FOR ACCE SS IAW SRM 51-30-2 AND VENTURA SRM. REMOVED FLOOR PANELS IAW SRM 53-20-012. REMOVED DAMAGED SEAT TRACK AND FABRICATED NEW SEAT TRACK AND INSTALLED IAW SRM 53-10-2 FIG 7, P-F SRM 53-10-2 FIG 7A AND SRM 51-30-2. REINSTALLED 9G BULKHEAD AN D ATTACHMENT PARTS, FLOOR PANELS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20080924 NM 2008 9 24 DLM8K081126 1 20080828 A 5330 593602161 SKIN DOUG MD88 MD88 3023688 NM FS 1322-1388 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DE 53419 SKIN DENTS AT FS 1322-1388, L-24L-26L DUE TO GROUND DAMAGE. DAMAGE WAS CUTOUT AND REPAIR DOUBLERS WERE INSTALLED. 2 L 7 2 4F RT A6WE 20080924 NM 2008 9 24 DL76G081127 1 20080828 A 2120 UNKNOWN BOEING 767 767332 1382001 NM CABIN ODOR A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 1610D 30594 INTERMITTENT BURNING RUBBER/PLASTIC ODOR IN MID CABIN DURING CRUISE. ODOR CENTERED AT ROW 17 CAME FROM AIR VENTS. STRO NGER ON LEFT SIDE OF CABIN BARELY NOTICEABLE ON RIGHT SIDE. TURNED GASPER FAN OFF ODOR DISSIPATED. NOTIFIED ATL MTC AC ARS 1825Z. RAN RECIRC FANS AND GASPER CANNOT DUPLICATE ODOR. NO ODOR NOTICED. 2 L 7 2 4F RT A1NM 20080924 2008 9 24 DL764081128 4 20080828 A 3442 ANTENNA BOEING 767 767432ER 1385134 NM WX RADAR SYS FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 840MH 29717 WXR RADAR FAILED. REPLACED ANTENNA, PERFORMED TEST OK . 2 L 7 2 4F RT A1NM 20080924 NM 2008 9 24 DL76G081130 1 20080831 A 2131 CONTROLLER BOEING 767 767332 1382001 NM CABIN PRESSURE FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1604R 30180 RTB - ON TAXI OUT, HAD CABIN ALT AUTO PRESS 1 AND 2 INOP. RESET PRESS CONTROLLERS. 2 L 7 2 4F RT A1NM 20080924 NM 2008 9 24 DL764081131 1 20080831 A 4920 38006081 TURBINE BOEING 767 767432ER 1385134 NM APU FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 842MH 17800 29715 P1031 APU FAULT ON FIRST TWO GROUND START ATTEMPTS. REMOVED AND REPLACED APU PER M/M. APU HOURS 10420. 2 L 7 2 4F RT A1NM 20080924 EU 2008 9 24 08FDEA03145 1 20080729 A 5321 B5327048401700 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN DECK FLOORBOARD NR 232 TG IS DAMAGED. FABRICATED NEW FLOORBOARD NR 232 TG IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03146 1 20080729 A 5347 A537819752500 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 CABIN SEAT TRACK HAS A GOUGE BETWEEN FRAMES 27 AND 28, RBL 37 INCH. REMOVED AND REPLACED DAMAGED SEAT TRACK SECTION FRO M FRAME 27 - 31 IAW SRM 51-40-21, PARAGRAPH 7 AND SRM 53-10-16, FIG 201/201A, SRM 51-21-10 AND SRM 51-23-10. WORKED IN CONJUNCTION WITH SNRM N00782. 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 DL76L081132 1 20080830 A 4940 CLUTCH BOEING 767 767332 1382001 NM APU STARTER DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 189DN 27643 25990 APU WILL NOT START. REMOVED APU STARTER AND FOUND CLUTCH DAMAGED. REMOVED APU. STARTED INSTALLING NEW APU. INSTALLED NEW APU PER AMM. RAN APU CHECKS GOOD. MCO AND PLACARD REMOVED. 2 L 7 2 4F RT A1NM 20080924 NM 2008 9 24 08FDEA03273 1 20080806 A 5312 AEA05261 DOUBLER DOUG MD11 MD11F 3023600 NM MLG WW BULKHEAD CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 587FE 48489 CENTER LANDING GEAR WHEEL WELL LEFT BULKHEAD FORWARD LOWER DOUBLER FOUND CRACKED. CRACKED DOUBLER REMOVED AND REPLACE D WITH NEW PART AT CENTER LANDING GEAR WHEEL WELL LEFT BULKHEAD FORWARD LOWER AREA AS PER SRM 51-33-01 VOLUME II. REPAI R CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 EU 2008 9 24 08FDEA03275 1 20080806 A 2697 51444133 CONNECTOR AIRBUS 310 A310203 3930313 EU FIRE DETECTION INOPERATIVE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 425FE 264 AFTER T/O FROM KIND, NR 2 ENG SHOWED ADVISORY FRO "NAC HEAT" OF 90. LEVELED OFF AT 15,000 FEET AND SLOWED TO 200 K. NAC HEAT DID NOT REDUCE. CONSULTED GOC AND RETURNED TO KIND AS EMERGENCY A/C. FIRE DEPT FOUND NO HOTSPOTS. SINGLE-ENG TA XIED TO PARKING. CREW DEBRIEFED REVEALED NO LEFT ECAM SCREEN ADVISORY OR INSTRUCTIONS. ENGINE PAGE CAME UP ON RIGHT EC AM. NO FIRE WARNING ASSOCIATED WITH ENGINE. WENT TO DISCONNECT CONNECTOR DH6 AND FOUND WIRE PULLED OUT OF CONNECTOR. REPLACED CONNECTOR DH6 PER ESPM AND PERFORMED ADJUSTMENT TEST OF FIRE AND OVERHEAT DETECTION SYSTEM. TESTS OK. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03641 1 20080828 A 2911 BSG0015505 PRESSURE SWITCH AIRBUS 310 A310222 3930315 EU HYD SYSTEM FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 456FE 318 YELLOW HYD PUMP FAILED AT FLAP RETRACTION. PERFORMED NR 2 ENGINE RAN,VERIFIED YELLOW HYD SYS PRESSURE IS 2900 PSI ON EC AM, YELLOW SYS LOW PRESS LIGHT FLICKER MOMENTARILY DURING FLAPS EXTENSION AND RETRACTION, NEED PRESS SWITCH CPN 0030767 , MPN BSG0001-5505 NIL IN SFS STORE. ACN RELEASED FOR SERVICE PER MEL/CDL: 29-34-01-B CATEGORY: C EXPIRATION: 07SEP08 " MEL 29-34-01-B: ENG 2 HYD PUMP LOW PRESSURE LIGHT(S) INOP. MONITOR ECAM HYD PWR PAGE FOR LOW PRESSURE WARNINGS. REFER TO MEL 29-34-01-B FOR (O) PROCEDURE TO VERIFY CORRECT PUMP OPERATION PRIOR TO DEPARTURE." C/0372261. REMOVED AND REPLAC ED Y SYS ENG PUMP SW (6GD) PER AMM 29-13-62-4. PERFORMED ENG RUN PER JRH, NO HYD LEAK FOUND, TEST NORMAL. HYDRAULIC IN 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03855 1 20080912 A 2840 INDICATION SYS AIRBUS 300 A300F4605R 3930327 EU FUEL QUANTITY MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 660FE 0382 759 CLIMBING THROUGH 20,000 FT ECAM INDICATED AUTO FUEL FEED FAULT 2 CTR PUMPS FAULTED. TURNED CTR PUMPS OFF THEN LT OUTER SHOWED XXS OVERHEAD BLANK. RT OUTER TANK QTY DROPPED STEADILY TO 870 LBS THEN SHOWED XXS INNER TANKS THEN STEADILY DROP PED TO BELOW 5000 IN EACH TANK DOWN TO 4.6/4.5. TOTAL FUEL ON LT ECAM SHOWED XX AS DID GW CG CHECKLIST CALLED FOR PULLIN G RESETTING CB FOR FQI CHANNEL SUPPLY 1. NO IMPROVEMENT. R & R FUEL QTY COMPUTER IAW AMM 28-42-38-4. OPS CHECKED NORM AL WITH EXCEPTION OF LT OUTER INDCATION REMAINS BLANKED. PERFORMED FAULT ISOLATION IAW TSM 28-42-00 FIG.107, RECEIVED E RROR CODES 312,322 AND 331. LT OUTER TANK PROBE 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03858 1 20080912 A 5730 A5735000220000 SKIN AIRBUS 310 A310222 3930315 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 LEFT WING FUEL TANK DOOR CUT OUT BETWEEN RIB 23 AND RIB 24 IS CORRODED. REMOVED CORROSION AND CHECKED LIMITS. ORIGINAL THICKNESS 0.600. MATERIAL REMOVED 0.003. REMAINING THICKNESS 0.597 AND IS FOUND TO BE WITHIN LIMITS IAW A310 SRM 57-2 0-12; PG 68; FIG 7A AND A310 SRM 57-20-12; PARA A-1 (A); FIG 201. ACCOMPLISHED PFPI IAW A310 NTM 51-90-00. ALODINED AN D PRIMED IAW A310 SRM 51-20-10 AND A310 SRM 57-20-12, PG 201B PARA 3-A. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03859 1 20080912 A 5730 A5735000220000 SKIN AIRBUS 310 A310222 3930315 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 LEFT WING FUEL TANK DOOR CUT OUT BETWEEN RIB 23 AND RIB 24 IS CORRODED. REMOVED CORROSION AND CHECKED LIMITS. ORIGINAL THICKNESS 0.600. MATERIAL REMOVED 0.003. REMAINING THICKNESS 0.597 AND IS FOUND TO BE WITHIN LIMITS IAW A310 SRM 57-2 0-12; PG 68; FIG 7A AND A310 SRM 57-20-12; PARA A-1 (A); FIG 201. ACCOMPLISHED PFPI IAW A310 NTM 51-90-00. ALODINED AN D PRIMED IAW A310 SRM 51-20-10 AND A310 SRM 57-20-12; PG 201B PARA 3-A. THIS SDR WAS GENERATED IN ERROR. FOR SDR DETAI LS SRR SDR TRACKING NR 08-3858 FOR N/R N00971. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03860 1 20080912 A 5730 A5735000220000 SKIN AIRBUS 310 A310222 3930315 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 LEFT WING FUEL TANK DOOR CUT OUT BETWEEN RIB 22 AND RIB 23 IS CORRODED. REMOVED CORROSION AND CHECKED LIMITS. ORIGINAL THICKNESS 0.600. MATERIAL REMOVED 0.003. REMAINING THICKNESS 0.597 AND IS FOUND TO BE WITHIN LIMITS IAW A310 SRM 57-2 0-12; PG 68; FIG 7A AND A310 SRM 57-20-12; PARA A-1 (A); FIG 201. UT GAUGE USED T 8225T. ACCOMPLISHED PFPI IAW A310 NT M 51-90-00. ALODINED AND PRIMED IAW A310 SRM 51-20-10 AND A310 SRM 57-20-12, PG 201B PARA 3-A. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03861 1 20080912 A 5730 A5735000220000 SKIN AIRBUS 310 A310222 3930315 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 LEFT WING FUEL TANK DOOR CUT OUT BETWEEN RIB 21 AND RIB 22 IS CORRODED. REMOVED CORROSION AND CHECKED LIMITS. ORIGINAL THICKNESS 0.600. MATERIAL REMOVED 0.002. REMAINING THICKNESS 0.598 AND IS FOUND TO BE WITHIN LIMITS IAW A310 SRM 57-2 0-12; PG 68; FIG 7A AND A310 SRM 57-20-12; PARA A-1 (A), FIG 201. UT GAUGE USED T 8225T. ACCOMPLISHED PFPI IAW A310 NT M 51-90-00. ALODINED AND PRIMED IAW A310 SRM 51-20-10 AND A310 SRM 57-20-12; PG 201B PARA 3-A. 2 L 7 2 4F RT A35EU 20080925 EA 2008 9 25 QXEA200800437 1 20080421 A 5320 CHANNEL CNDAIR CL600 CL6002C10 1390015 EA CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 612QX 10042 PDX C4 CHECK, ABOVE 280 BEAM AT COCKPIT ENTRY, CAMLOCS AND CAMLOC SUPPORT ARE CORRODED. REMOVED ATTACHMENT ANGLE AT COC KPIT ENTRY IAW SRM 51-40-11. DRILLED UP NEW ANGLE IAW SRM 51-40-11. INSTALLED NEW CAMLOC CHANNEL IAW CRJ 700 SRM 51-42 -06. 2 L 7 2 4F RT A21EA 20080925 NM 2008 9 25 08FDEA03866 1 20080914 A 5311 ABA72213 FRAME DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 620FE 48791 UPON LOWER NOSE SKIN OPEN-UP FOUND ADJACENT FRAME AT STA 421.507, X=-20 CRACKED. FRAME AT STA 421.507, X = -21.25 CARRI ED OUT REPAIR AS PER FEDEX EA NR 1-5310-123101 PT1, TITLE: FUSELAGE, MAINFRAME BS 421.5 FRAME, X = -21.25 - FLANGE CRACK REPAIR. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 EU 2008 9 25 08FDEA03868 1 20080915 A 5320 A53610607207 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSION ON RUN OUT FITTING C16-17, P 44 RT OUT OF LIMIT. REPAIR PERFORMED IAW SRM 53-12-14 FIG 201. 2 L 7 2 4F RT A35EU 20080925 WP 2008 9 25 08FDEA03914 1 20080917 A 5347 601076418 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 571FE 47830 MAIN DECK SEAT TRACK AT STA 849, LBL 75 HAS GOUGE MARK. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1,FIG 1, S HT 1. FABRICATED NEW SEAT TRACK UNDER MAE TRAVELER NR 78/758027 IAW SRM 53-70-00. BLENDED GOUGE OUT OF LIIMITS .240 AF TER REWORK MAX REWORK .260 IAW SRM 53-70-00. REMOVED AND REPLACED 2 FLOOR PANELS STA 823-999 LBL 48-75 IAW AMM 53-21-08 -02. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03915 1 20080917 A 5347 SEAT TRACK BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 MAIN CABIN SEAT TRACK, BS 680, LBL 46, HAS CORROSION AT FASTENER HOLES. REMOVED AND REPLACED SEAT TRACK ASSY, BS 440-68 0, LBL 46, IAW SRM 51-40-02 AND SRM 53-00-52, FIG 101, DETAIL 5. REPLACEMENT SEAT TRACK FABRICATED ON MAE TRAVELER NR T 8/753948. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING. 2 L 7 2 4F RT A2NM 20080925 EU 2008 9 25 08FDEA03917 1 20080917 A 5315 A5327534520000 FLOORBEAM AIRBUS 310 A310222 3930315 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 FUSELAGE INTERIOR MAIN CARGO DECK CROSSBEAM LOWER CAP IS DAMAGED AT FRAME C 60 AND RBL 78. REMOVED DAMAGE IAW EA 6-5310 -7-123653. MILLED DOWN AREAS ON CROSSBEAM IAW EA 6-5310-123653. FABRICATED REPAIR ANGLE, REPAIR STRAP & FILLER IAW EA 6-5310-123653. ALODINED IAW SRM 51-26-10. PRIMED & PAINTED IAW SRM 51-23-10. INSTALLED REPAIR PARTS IAW EA 6-5310-123 653. 2 L 7 2 4F RT A35EU 20080925 WP 2008 9 25 08FDEA03920 1 20080917 A 5512 ALC7441503 SKIN DOUG MD10 MD1010F 3022112 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT HORIZONTAL STAB UPPER SKIN AND APPROX XE 72, STRINGER NR 6 IS CRACKED. REPAIRED SKIN PER EA 8-5510-123649. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03773 1 20080908 A 5330 655452533 SKIN BOEING 727 727233 138408A NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 SCIBE MARKS IN FUSELAGE SKIN FROM STA 690 TO 720D STR 19L TO 19R. CUTOUT DAMAGED SKIN DIMS 50 1/4" BY 33 1/4". FABRICA TED NEW SKIN SECTION FROM 2024-T3 .063 PO NR 8204312. FABRICATED REPAIR STRAP AND FABRICATED 2 SHIMS. INSTALLED REPAIR PARTS AT BS 690-720D BETWEEN STR 25L TO 25R IAW SRM 53-30-3 FIG 12. 2 L 7 3 4F RT A3WE 20080925 EU 2008 9 25 08FDEA03774 1 20080908 A 5247 A5247132501000 DOOR AIRBUS 310 A310222 3930315 EU APU BAY DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 RIGHT APU COMPARTMENT DOOR HAS A DENT ON THE FWD PORTION OF THE EXTERNAL SKIN. FABRICATED REPAIR IAW SRM 52-41-00. ALO DINED IAW SRM 51-21-10. PRIMED IAW SRM 51-23-10. INSTALLED REPAIR IAW SRM 51-40-20 AND SRM 52-42-11. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03775 1 20080908 A 5730 A57242401020100 PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 650FE 726 LEFT WING LOWER T/E PANEL 575 FB LAND AND AIRFRAME MATING SURFACE IS CHAFFED AND HAS BARE METAL. REMOVED CAMLOCKS AND S EAL TO FOM IAW SRM 51-40-00. FABRICATED A REPAIR DOUBLER IAW EA NR 6-5720-123627. PREPPED PANEL SKIN AND DOUBLER FOR B ONDING IAW SRM 51-21-10; LAYED UP; BAGGED AND CURED IAW SRM 51-77-12. ALODINED REPAIR IAW SRM 51-21-10. EDGE SEALED R EPAIR IAW SRM 51-77-12. PRIMED AND RESTORED FINISH IAW SRM 51-75-10. REINSTALLED SEAL AND CAMLOCKS IAW SRM 51-41-00. 2 L 7 2 4F RT A35EU 20080828 EA 2008 8 28 MAS2008F00034 1 20080813 A 3350 1317 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 513MJ 10111 ASH FLT 7140 - MCI-ORD - ONE CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. MAINTENANCE REPLAMPED. (S) 2 L 7 2 4F RT A21EA 20080828 WP 2008 8 28 NWAA083969855 1 20080819 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 764NC 47717 DURING LINE CHECK, MAINTENANCE FOUND THAT THE LT SIDE EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REPLA CED THE POWER SUPPLY AND THE LIGHT RETURNED TO AN OPERATIONAL CONDITION. (S) 2 L 7 2 4F RT A6WE 20080828 EA 2008 8 28 HNAA08A0006 1 20080612 A 5340 85320596111 FITTING DHAV DHC8 DHC8311 1386006 EA BS 424 S31R CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 335EN 32270 32270 375 CORROSION FOUND AT STR 31 RT AT FRAME 424.12. FITTING REPLACED WITH NEW PART. (S) 2 H 7 2 4T RT A13NM 20080828 NM 2008 8 28 QXEA200800531 1 20080521 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 411QX 4055 PDX-C4 CHECK - SEAT TRACK NR 10 HAS CORROSION AT APPROX STA X1.5 AND X16.5 AROUND BOLT HOLES. REMOVED NR 10 SEAT TRACK AND INSTALLED NEW NR 10 SEAT TRACK REF DHC8-400 SRM 51-40-15 & 51-42-05. (S) 2 H 7 2 4T RT A13NM 20080828 NM 2008 8 28 QXEA200800529 1 20080521 A 5320 THRESHOLD BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 411QX 4055 PDX-C4 CHECK FWD EMERGENCY EXIT THRESHOLD HAS CORROSION EVIDENT AROUND DOOR FITTINGS AND THRESHOLD RETAINING HARDWARE. REMOVED EXIT THRESHOLD FRAME DRILLING OUT 20 RIVETS. DRILLED UP NEW THRESHOLD AND INSTALLED IAW Q400 SRM 51-40-07 & 51- 42-05. (S) 2 H 7 2 4T RT A13NM 20080828 NM 2008 8 28 QXEA200800533 1 20080521 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 411QX 4055 PDX-C4 CHECK - THE LOWER FLANGE ON FRAME X71.2 BETWEEN STR 31&32L HAS CORROSION. REMOVED CORROSION IAW D8/400 RD8/4-53- 2344 STEPS 1&2. HFEC INSPECTED IAW Q400 NDTM PART 6 61-00-01 NO CRACKS NOTED. UT THICKNESS CHECK IAW Q400 NDTM PART 15 1-00-04 HIGH .040 LOW .036, WITHIN LIMITS IAW RD 8/4-53-2344. ALODINED, PRIMED AND PAINTED IAW RD8/4-53/2344 STEP 4, 5& 6 PG 2. (S) 2 H 7 2 4T RT A13NM 20080828 2008 8 28 HNA2008F00038 3 20080811 A 6197 WIRE DHAV DHC8 DHC8102 2809003 NM AUTOFEATHER SYS BROKEN A HNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 07 912HA 57653 57653 040 ABORTED TAKEOFF DUE TO AUTOFEATHER ARM LIGHT DID NOT ILLUMINATE. FERRIED TO SBY. MAINTENANCE REPAIRED WIRE AT POWER LE VER MICROSWITCH 6121S13. OPS CHECK GOOD. (S) 2 H 7 2 4T RT A13NM 20080828 EU 2008 8 28 MAS2008F00054 1 20080814 A 5220 SKIN SAAB SF340 340B 7860101 EU ESCAPE HATCH DENTED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 411XJ 340B411 CREW HATCH HAS DENT .005 INCHES DX.75 INCHES X 1 INCH IN THE AFT RT CORNER OF OUTER SKIN. REPAIRED DENT ON CREW HATCH I AW EO S52028. FOR MORE INFO SEE CONTINUATION CARD 085397. CONTINUATION CARD 085397 NR1 DENT IN CREW HATCH OUTER SKIN R EQUIRES DIMENSION EVALUATION. DENT IS 0.125 INCHES FROM CHEM MILL EDGE, OTHERWISE WITHIN ALLOWABLE LIMITS PER SRM 51-10 -10. NR 2 DENT REQUIRES NDT EVAL. DENT IS DISBONDED. HFEC TEST CHECKED GOOD PER NDT 51-6 AND 51-10. NR 3 DENT IS DIS BONDED. REPAIRED DENT ON CREW HATCH OUTER SKIN, PRIMED AND PAINTED DOUBLER. (S) 2 L 7 2 4T RT A52EU 20080828 EU 2008 8 28 MAS2008F00057 1 20080814 A 5311 FRAME SAAB SF340 340B 7860101 EU BS 677 DENTED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 411XJ 340B411 RIB ON RT SIDE OF CARGO BAY IS DENTED AT STATION 677 JUST ABOVE WL 73.5. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER IA W EOS53476 AND SRM 51-20-00 AND 51-40-00. (S) 2 L 7 2 4T RT A52EU 20080828 CE 2008 8 28 YAD2008F00001 1 20080821 A 3260 444EN495 SQUAT SWITCH BEECH BEECH 1900 1900C 1154161 CE RT MLG INTERMITTENT E YADA O OTHER F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 AL 03 112AX GLA904PS UC45 DURING A PILOT TRAINING FLT MLG WAS EXTENDED USING ALTERNATE EXTENSION PUMP IAW QRH AND POH. AFTER EXERCISE, PILOT RESE T MLG CONTROL CIRCUIT BREAKER & SELECTED GEAR UP. PILOT REPORTED THAT ALTHOUGH THEY COULD HEAR MLG MOTOR/PUMP RUNNING, MLG DID NOT RETRACT, ALL DOWN & LOCKED GREEN LIGHTS REMAINED ON, & CONTROL CIRCUIT BREAKER TRIPPED AFTER 16 SECONDS (M OTOR CONTROL CIRCUIT PROTECTION TIME DELAY). ACFT LANDED UNEVENTFULLY. MX COULD NOT DUPLICATE FAULT EVEN AFTER ATTEMPT ING TO RECREATE EXACT ORIGINAL SCENARIO - UNLESS HAND PUMP HANDLE WAS NOT STOWED. ACFT RELEASED FOR SERVICE. WHILE ACF T WAS BEING LOADED FLT CREW NOTICED THAT MLG SELECTOR HANDLE SAFETY LATCH WAS DISENGAGING AS SOON AS SHIP POWER TURNED O 2 L 7 2 4T RT A24CE 20080828 NM 2008 8 28 F3LA200800579 1 20080821 A 5320 D53471124200 SHEAR PLATE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 928FR 2236 DURING C3 C-CHECK, INSPECTION NOTED THE LT LATERAL SHEAR PLATE HAS LIGHT CORROSION AT CLIP NUT HOLES BETWEEN FR 68 AND F R 70. MAINTENANCE REMOVED AND REPLACED SHEAR PLATE IAW THE REQUIREMENTS OF A319 SRM 51-42-11, PARAGRAPH 6. UPON COMPLE TION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (S) 2 L 7 2 4F RT A28NM 20080828 NM 2008 8 28 F3LA200800569 1 20080819 A 5321 D5367202600100 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 928FR 2236 DURING C3 C-CHECK, INSPECTION NOTED AFT PIT PANEL 152UG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURE DAMAGE TO PANEL 152U G IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCE PTABLE. (S) 2 L 7 2 4F RT A28NM 20080828 EU 2008 8 28 NWAA083983253 1 20080821 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 353NW 3887 311 786 FOUND SEVERAL PAIRS OF SEAT ROW EMERGENCY EGRESS LIGHTING INOPERATIVE DURING LINE CHECK. REPLACED EPSU, CHECKED GOOD. (S) 2 L 7 2 4F RT A28NM 20080828 CE 2008 8 28 DJF2008F00012 1 20080821 A 2612 FIRE WARNING RAYTHN DH125 HAWKER800XP 7150012 CE CARGO BAY FALSE ACTIVATION A DJFA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 23 805LX 258374 THE CREW REPORTED THAT THE BAGGAGE FIRE LIGHT ILLUMINATED IN FLIGHT. CREW VERIFIED INDICATION ONLY AFTER LANDING AND TH E ISSUE WAS PUT ON MEL. (S) 2 L 7 2 4F RT A3EU 20080828 EU 2008 8 28 USAA920081560 1 20080819 A 5320 D53471124203 SHEAR PLATE AIRBUS A319 A319112 3930323 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 PIT-S4- MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, -Y1292. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, -Y1292 IAW US AIRWAYS ENGINEERING ORDER 5307Y284 & A319 SRM 51-42-11. (S) 2 L 7 2 4F RT A28NM 20080828 SO 2008 8 28 C2XA08RI114 1 20080807 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14920 145380 RIC - DURING ROUTINE MAINTENANCE, RIC MAINTENANCE EMERGENCY LIGHT STRIP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED E MERGENCY LIGHT INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S) 2 L 7 2 4T RT T00011AT 20080828 2008 8 28 DXTA200803192 4 20080721 A 3140 DISPLAY CESSNA 750 750 2076810 CE INSTRUMENT PANEL INOPERATIVE E DXTA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 GL 07 978QS 7500187 ON DEPARTURE AT 1500 FT AGL AND 200 KNOTS EICAS SCREEN WENT BLANK THEN WAS REPLACED BY A RED X EICAS (AMBER) DISPLAYED O N PILOT AND COPILOT PFD. ALL FLIGHT DIRECTOR BUTTONS FAILED WITH ALTITUDE HOLD BUTTON ENGAGED. COULDN’T DISENGAGE ALT HOLD OR ENGAGE OTHER FUNCTIONS. DISENGAGED AUTO PILOTS TO FLY. EICAS SCREEN CAME BACK ON WHILE TURNING FINAL AT APPROX 170 KNOTS INDICATED. (A) 2 L 7 2 4J RT T00007WI 20080828 NM 2008 8 28 ABXA080186 1 20080603 A 5210 141T333039 SKIN BOEING 767 767232 1385132 NM L1 DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 742AX 22217 AFT LOWER CORNER OF L1 DOOR CUTOUT HAD A CRACK IN OUTER SKIN LAYER. REPAIRED AFT LOWER CORNER OF L1 DOOR IAW B767 SRM 5 3-10-01, FIG 201 AND REA B653-57443. (A) 2 L 7 2 4F RT A1NM 20080828 NM 2008 8 28 KCSA081348 1 20080724 A 5320 INTERCOSTAL BOEING 747 747246B 1384864 NM BS 2701 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 700CK 22990 UPPER FUSELAGE FRAME INTERCOSTAL IS DAMAGED AT STA 2701.5, BL 0. (A) 2 L 7 4 4F RT A20WE 20080828 CE 2008 8 28 DXTA200803193 1 20080720 A 2910 HYDRAULIC SYSTEM CESSNA 750 750 2076810 CE LOW E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 941QS 7500141 DURING GEAR RETRACTION LOST HYD -A- SYSTEM AND ALL HYD FLUID ON THE -A- SIDE. HYD FLUID VISIBLE IN BOTH MAIN GEAR WELLS . HYD VOLUME LOW -A-, -B- AND HYD PUMP FAIL A CHECKLIST WERE DONE WITH GEAR BLOW DOWN. (A) 2 L 7 2 4J RT T00007WI 20080828 2008 8 28 DXTA200803195 4 20080722 A 3414 INDICATOR CESSNA 680 680CE 2076811 CE AIRSPEED READS LOW E DXTA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 07 306QS 6800207 COPILOTS A/S INDICATOR WAS NOT INCREASING ABOVE 35 KTS. PILOTS INDICATOR WAS INDICATING 80KTS. CHECK TWICE WITH SAME R ESULTS. (A) 2 L 7 2 4F RC T00012WI 20080828 WP 2008 8 28 ABXA080187 1 20080706 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP EMERGENCY LIGHT DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 951AX 47616 EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-0. (A) 2 L 7 2 4F A6WE 20080828 NM 2008 8 28 KCSA081422 1 20080823 A 5315 FLOORBEAM BOEING 747 747249F 1384849 NM BS 720 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 FORWARD BILGE HAS A DENT IN FLOORBEAM WEB AT STA 720, LBL 46, WL 108. (S) 2 L 7 4 4F RT A20WE 20080828 NE 2008 8 28 N6WA0080803 2 20080820 A 7200 ENGINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C5B1 30052 NE LEFT VIBRATION A N6WA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CE 03 152GJ 10218 8403-MCI - LT ENG HIGH VIBRATION IN FLIGHT. INSPECTED LT ENG FAN BLADES FOR STIFFNESS, NO DEFECTS NOTED. PERFORMED RU N VIBRATION CHECK WITH CREW. VIBE NORMAL AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E00063EN 20080828 NM 2008 8 28 KCSA081418 1 20080821 A 5313 STRINGER BOEING 747 747249F 1384849 NM BS 660 S44L DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 STRINGER CLIP DENTED AT STA 660 STRINGER 44L. (S) 2 L 7 4 4F RT A20WE 20080828 NM 2008 8 28 DHLA200800089 1 20080820 A 2612 FIRE WARNING BOEING 727 7272B7 138407L NM MLG WW FALSE ACTIVATION A DHLA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 770AT 21953 FLT 549 - DURING CRUISE FLIGHT AT FL360, WHEEL WELL FIRE RED LIGHT ILLUMINATED FAINTLY FOR 1 SECOND ACCOMPANIED BY 1 DIN G OF THE FIRE BELL. INSPECTED AND TESTED SYSTEM PER MM CH 26-12-0. NO DEFECTS FOUND. SYSTEM OP CHECKS GOOD. ACFT WAS GROUNDED. 2 L 7 3 4F A3WE 20080828 2008 8 28 USAABB08135 4 20080817 A 2565 D30654122 SLIDE BOEING 757 757225 1384959 NM L1 DOOR DETACHED A USAA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 EA 19 921UW 40059 3308 22201 CLT - THE L1 DOOR EMERGENCY ESCAPE SLIDE WAS FOUND NOT COMPLETELY ATTACHED TO THE DOOR. MAINTENANCE REPLACED THE L1 DOO R EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. (S) 2 L 7 2 4F RT A2NM 20080828 NM 2008 8 28 USAABB08137 1 20080817 A 3350 2506500994001 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 937UW 27245 BOS - THE EMERGENCY ESCAPE SLIDE LIGHT WAS INOPERATIVE AT THE L4 DOOR. MAINTENANCE REPLACED THE L4 DOOR EMERGENCY ESCAP E SLIDE LIGHT ASSEMBLY. OPERATIONALLY CHECKS OK. (S) 2 L 7 2 4F RT A2NM 20080828 NM 2008 8 28 P5CA0801567 1 20080508 A 5720 TIE ROD BOEING 747 74746NF 13848BT NM RT WING MLG WW BROKEN A P5CA O OTHER O OTHER NR NOT REPORTED 1 EA 15 454PA 30812 ON WALKAROUND FOUND A TIE ROD AND CLEVIS BROKEN ON THE RT WING GEAR WHEEL WELL AT WBL 238.38 FIXED TRAILING EDGE UPPER R IB. REMOVED DAMAGED PARTS AND VISUALLY INSPECTED AREA IN ACCORDANCE WITH EO 4457A140. (A) 2 L 7 4 4F RT A20WE 20080828 EA 2008 8 28 QXEA200800600 1 20080530 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 785 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 610QX 10033 RFD - C4 CHECK - CORRODED SIDE SEAT TRACK ON LT SIDE AT FS785. BLENDED CORROSION FROM LT SIDE SEAT TRACK AT FS 785. RE MOVED .009 MATERIAL FOR BLEND, WITHIN LIMITS, MAX ALLOWABLE BLEND IS .035 INCHES. ALL WORK DONE IAW CRJ BOMB REO 670-53 -00-013. TREATED IAW CRJ BOMB REO 670-53-00-013. (S) 2 L 7 2 4F RT A21EA 20080829 NM 2008 8 29 SWAA084429 1 20080810 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT, BS 304, WL 234 TO WL 261. REPAIRED SKIN PER SRM & ER. 2 L 7 2 4F RT A16WE 20080829 2008 8 29 SWAA084430 4 20080810 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 R1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. REPOSITIONED SLIDE ASSY PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084431 1 20080808 A 3350 BR2013 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 458WN 33857 EEPLS INOP AT AFT END. SECURED EEPLS SECTION. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084594 1 20080819 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 500C S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 637SW 27710 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084595 1 20080819 A 3350 101331 LENS BOEING 737 7373G7 1384595 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 RIGHT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084599 1 20080819 A 5310 6545833 CREASE BEAM BOEING 737 7373Q8 1384670 NM BS 188 S17L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 688SW 23254 DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 188, STR 17L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084603 1 20080818 A 3250 4129RA9 VALVE BOEING 737 7373Y0 1384671 NM NLG STEERING INOPERATIVE A SWAA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 29 665WN 23497 RETURN TO GATE. NLG STEERING INOP, LOCKED HARD RIGHT. REMOVED AND REPLACED METERING VALVE PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084605 1 20080819 A 5330 6545800 SKIN BOEING 737 7373A4 1384585 NM BS 291 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 291, BETWEEN WL 260 AND WL 350. REPAIRED SKIN PER SWA EA . 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084606 1 20080819 A 5312 6546568 BULKHEAD BOEING 737 7373A4 1384585 NM BS 1016 S6L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016, STR 6L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084735 1 20080826 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED SPV CHECK, FOUND FWD LT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084740 1 20080826 A 5311 6546538 FRAME BOEING 737 7373T0 1384582 NM BS 597 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084741 1 20080826 A 5340 65C27314 STRINGER CLIP BOEING 737 7373T0 1384582 NM BS 380 S23L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 23L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084742 1 20080826 A 3350 20131A BATTERY PACK BOEING 737 737317 138447P NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED MV2 CHECK, FOUND LT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084688 1 20080825 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 252WN 34973 EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084689 1 20080825 A 3350 1619 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED MV2 CHECK, FOUND LOWER LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084691 1 20080825 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 867 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084692 1 20080825 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 867 S9L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084694 1 20080825 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM BS 867 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867,STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084743 1 20080826 A 3350 767 LAMP BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 775SW 30590 DURING SCHEDULED 8Y CHECK, FOUND RT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PE R MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084699 1 20080825 A 2121 215201 FAN BOEING 737 7375H4 138449D NM E&E BAY FAULTY A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 29 503SW 24180 DIVERSION - FLIGHT CREW REPORTED STRONG BURNING ODOR IN CABIN. BURNING ODOR DISSIPATED AFTER GASPER FAN TURNED OFF. RE MOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 20080829 NM 2008 8 29 SWAA084701 1 20080825 A 5312 6517582 VERTICAL BEAM BOEING 737 7373H4 1384600 NM BS 178 BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 643SW 27716 DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20080829 EA 2008 8 29 REX2008F00038 1 20080814 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A REXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 8631E 7631 FLAP FAILURE MESSAGE IN CRUISE FL330. OVERSPEED WARNING SOUNDING THEN FLAP FAILURE AT ZERO. QRH FOLLOWED. DIVERTED TO IAD, DECLARED EMERGENCY WITH UNEVENTFUL LANDING. TROUBLESHOT PER BOMBARDIER FIM AND AMM, ALL LRUS PASSED. VERIFIED RI GGING OF THE LT AND RT BRAKE POSITION SENSING UNITS, (BPSU) FOUND TO BE CORRECT. PERFORMED OPERATIONAL CHECKS OF THE FL AP SYSTEM IAW BOMBARDIER AMM WITH NO DEFECTS FOUND. (S) 2 L 7 2 4F RT A21EA 20080829 SO 2008 8 29 C2XA08TY087 1 20080820 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12142 145735 RT SIDEWALL LARGE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED INVERTER NR 5 IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD. ACFT RELEASED AND RETURNED TO SERVICE. (S) 2 L 7 2 4F RT 20080829 NM 2008 8 29 KCSA081409 1 20080820 A 5315 FLOORBEAM BOEING 747 747249F 1384849 NM BS 540 GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 STA 540 FLOORBEAM GOUGED ON UPPER CHORD LBL 41. (S) 2 L 7 4 4F RT A20WE 20080924 EU 2008 9 24 08FDEA03487 1 20080818 A 5340 A5381026720001 ATTACH FITTING AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 650FE 726 MAIN CARGO FLOOR SUPPORT AND WEB, LOWER OUTBD ATTACH FITING IS CRACKED AT FRAME 48, FLOOR LOCATION -Y 1456. REMOVED AND REPLACED ATTACH FITTING IAW SRM 51-40-21; PARA 10-B. 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03374 1 20080811 A 5315 FLOORBEAM BOEING 757 75727B 1384921 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 916FD 24137 CORROSION FOUND ON FLOORBEAM AT STA 365, RBL 3 TO RBL 51. EVALUATE AND RECTIFY. REPAIR CARRIED OUT ON FLOORBEAM UPPER CHORD AT STATION 365 BETWEEN RBL 3 AND RBL 51 IN ACCORDANCE WITH B 757-200 SRM 53-00-51 FIGURE 201 REPAIR 1, REVISION 93 . REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-02-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080924 EU 2008 9 24 08FDEA03140 1 20080729 A 5321 B5327063200000 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CABIN FLOOR BOARD AT FRAME 54; LBL 77 INCH TO 97 INCH IS BROKEN. FABRICATED NEW FLOORBOARD NR 241 LK IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03783 1 20080909 A 5310 DOOR FRAME AIRBUS 310 A310222 3930315 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 THE DOOR FRAME FITTING IS CRACKED, AFT CARGO LOWER FWD CORNER. COMPLIED WITH FEDEX E.A. 6-5310-123645. 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03785 1 20080910 A 5753 ARC2736 SKIN DOUG MD11 MD11F 3023600 NM RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 623FE 48794 RT WING INBOARD FLAP LOWER SKIN CENTER AREA FOUND WITH SEVERAL DENTS. TRIMMED OUT AND REPAIR CARRIED OUT AS PER SRM 57- 10-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 EU 2008 9 24 08FDEA03583 1 20080825 A 5320 A9242053520200 CHANNEL AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 E/E COMPARTMENT, BATTERY FWD MOUNT CHANNEL IS CRACKED. REMOVED MOUNT CHANNEL IAW SRM 51-40-21. COMPLIED WITH EA 6-5320 -117009. RE-INSTALLED REPAIRED MOUNT CHANNEL IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03362 1 20080810 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 587FE 48489 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B AND NR C. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 FABRICATED AS PER FEDE X EA NR 1-5300-122409A, TITLE: FUSELAGE, GENERAL: MAIN CARGO DOOR LOWER JAMB SPOOL FITTING, MATERIAL SUBSTITUTION. SUPP ORT FITTING NR 5 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR BUSHING FABRICATED AND INSTALLED ON MAIN CA RGO DOOR LOWER JAMB WEB AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 WP 2008 9 24 08FDEA03099 1 20080728 A 5320 AFA71321 SUPPORT FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 MAIN CARGO DOOR JAMB AT SPOOL FITTING NR 6; HOLE "A" HAS A CRACK INDICATION IN THE BACK UP FITTING, (HOLE IS 0.574 INCH DIA.) REMOVED SUBSTRUCTURE AND WEB TO GAIN ACCESS TO THE NR 6 SPOOL BACK UP FITTING IAW SRM 51-33-01; VOL II. LOCATED AND DRILLED NEW BACK UP FITTING IAW 51-33-01; VOL II. INSTALLED NEW BACK UP FITTING AFA 7132-1 IAW SRM 51-33-01; VOL II . RE-INSTALLED SUB STRUCTURE AND WEB IAW SRM 51-33-01; VOL II. INSTALLED BUSHING IAW SRM 53-50-11; VOL I. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 08FDEA03106 1 20080729 A 5343 ACA7017501 TRUNNION DOUG MD11 MD11F 3023600 NM NLG CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 NOSE LANDING GEAR WHEEL WELL LEFT TRUNNION FITTING FOUND CRACKED. TRIMMED OUT AND REPAIR CARRIED OUT AS PER SRM 53-40- 00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 08FDEA03107 1 20080729 A 5711 ARB74131 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 LEFT WING, UPPER SPAR CAP FASTENER HOLE AT STA XORS 878 FOUND ELONGATED. LEFT WING UPPER SPAR CAP STA XORS 878 ELONGATE D HOLE REPAIRED AS PER FEDEX EA NR 1-5710-124328, TITLE: WINGS BASIC WING STRUCTURE, LEFT WING UPPER SPAR STA XORS = 878 , ELONGATED HOLE REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03988 1 20080922 A 5310 CREASE BEAM BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 MAIN CABIN CREASE BEAM, I/B CHORD, BS 900-1040, LBL 62, HAS CORRODED SPOTS. REMOVED AND REPLACED CREASE BEAM IAW SRM 51 -10-02, 51-40-02, AND 53-40-13. THIS REPAIR IS CLASSIFIED AS A "MAJOR" REPAIR, CATEGORY "A", WITH NO FOLLOW UP TRACKING REQUIREMENTS. 2 L 7 2 4F RT A2NM 20080925 EU 2008 9 25 08FDEA03602 1 20080826 A 2780 516A000002 LIMITER AIRBUS 310 A310324 3930206 EU SLAT TORQUE MALFUNCTIONED A FDEA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 CE 21 805FD 3783 3783 456 DURING APPROACH WITH LANDING GEAR DOWN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT O/H. SLATS/FLAPS CYCLED PER QRH, THE LIGHT/FAULTS CLEARED CONFIGURED AGAIN THE SLATS STUCK AT 15 DEGREES . FOLLOWED QRH FOR SLATS STUCK LANDING. ON FINAL APPROACH FLAP HANDLE AT 40 DEGREES SLATS BROKE FREE AND WENT TO 30 DE GREES SLATS WITH 40 DEG FLAPS. THE LANDING WAS UNEVENTFUL. SLAT/FLAP RETRACT ON THE GROUND WAS NORMAL. CHECKED SLAT 0 POSITION AND INDEX OF LT APU, WW IPPU AND FPPU, CHK OK. REMOVED AND REPLACED RT APU ALL AMM 27-81-19-4. REMOVED AND R EPLACED RT SLAT TORQUE LIMITER PER AMM 27-84-12-4. OPS CHECKED NORMAL PER AMM 27-84-00-5. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03353 1 20080809 A 5542 A5547150001608 SKIN AIRBUS 310 A310324 3930206 EU RUDDER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 812FD 467 UPON INSPECTION OF RUDDER BY THERMOGRAPHY IAW EO 6-5530-7-5004 PT 2 PARA 8 STEP C AND D THE FOLLOWING DEFECTS WERE NOTED IN ADDITION TO ORIGINAL FINDINGS REF EA 6-5740-118399 THE UPPER RT PORTION OF THE RUDDER HAS 1 ADDITIONAL AREA OF MOIST URE MEASURING .960 WIDE BY .600 TALL APPROX 1.5 INCHES AFT OF 37MM NOTED AREA. REMOVED DAMAGE AND REPAIRED RUDDER IAW E A 6-5540-121333, RELEASE DATE 24 JUL, 2008. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03322 1 20080808 A 5321 R532B370700100 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 BROKEN FLOORBOARD AT RBL 72; FRAME 43 TO FRAME 47. REPAIRED CABIN FLOOR PANEL 242 WH BY FABBING A NEW PANEL USING THE O LD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSER TS. PART MARKED AND APPLIED NON-SKID TAPE IAW FEDEX DWG SRZ 25-005, REV "G". 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03323 1 20080808 A 5321 R531B360300000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOORBOARD IS CRACKED FROM FRAME C19 TO C22, LBL 24. FABRICATED A NEW PANEL FROM THE OLD PANEL, LOCATED HOLES, CO UNTERBORED, POTTED EDGES, CURED POTTING, SANDED THE EDGES, INSTALLED INSERTS, APPLIED NON-SKID AND PART MARKED IAW DWG S RZ 25-005; REF G. 2 L 7 2 4F RT A35EU 20080925 WP 2008 9 25 08FDEA03624 1 20080828 A 5320 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 1 SPOOL BACK UP FITTING "HOLE D" HAS A CRACK INDICATION IN THE BACK UP FITTING. FITTING REQUIRES REMOVAL. REMOVED A ND REPLACED THE FITTING IAW SRM 53-33-01; VOL II AND EO 9-5230-7-5000 PT 2. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03625 1 20080828 A 5320 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 4 SPOOL BACK UP FITTING "HOLE A" HAS A CRACK INDICATION. BACK UP FITTING REQUIRES REMOVAL. REMOVED WEB ASSEMBLY A T FS 675 - 695 AND THE INTERCOSTAL AT FS 675 - 690 TO FOM IAW SRM 51-33-01; VOL II. INSTALLED BUSHINGS IN THE MCD LOWER JAMB BEAM AS REQUIRED. REMOVED AND REPLACED THE SPOOL BACK UP FITTING AND THE INTERCOSTAL AT FS 675 - 690 IAW SRM 51-3 3-01; VOL II. 2 L 7 3 4F RT A22WE 20080925 EU 2008 9 25 08FDEA03324 1 20080808 A 5321 R532B361700000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOORBOARD AT FRAME C22 - C26, LBL 48 IS CRACKED. REPAIRED CABIN FLOOR PANEL 23 JG BY FABBING A NEW PANEL USING T HE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE I NSERTS. PART MARKED AND APPLIED NON-SKID TAPE IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080925 NE 2008 9 25 DL75E081119 2 20080825 A 7261 BEARING BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A DALA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 27 706TW 23911 728711 28165 728711 NR 5 BEARING FAILED OIL IN TAIL PIPE. REPLACED NR 1 ENG. REPLACED NR 1 ENG PER 6T103. 2 L 7 2 4F 4 F RT A2NM E17NE 20080925 NM 2008 9 25 08FDEA03804 1 20080910 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 623FE 48794 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIA HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRA CK INDICATIONS AT HOLES A AND D. MAIN CARGO DOOR LOWER JAMB, CRACKED NR 3 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03806 1 20080910 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 623FE 48794 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIA HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRA CK INDICATIONS AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB CRACKED NR 7 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03807 1 20080910 A 5730 ARB2886504 SKIN DOUG MD11 MD11F 3023600 NM RT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 623FE 48794 RIGHT WING LEADING EDGE LOWER SECTION AT APPROX STA XORS 392, OUTBOARD OF ANTI-ICE TELESCOPIC DUCT, FOUND WITH CHAFE MAR KS. REPAIR CARRIED OUT AS PER EA 1-5740-122551, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 EU 2008 9 25 08FDEA03809 1 20080911 A 5415 A54612350200 MOUNT AIRBUS 300 A300B4622R 3930312 EU ZONE 400 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CHAFING MARKS ON PYLON NR 1 FWD MOUNT FITTING ON PYRAMID. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARK, NDT FOR CRACK FREE CONDITION AND CADMIUM PLATING IAW RAS/70512885/011/2008 ISS A, APPROVED BY EA 6-5451-123062. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03811 1 20080911 A 5320 A53832100208 WEB AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CRACK IN WEBS ABOVE CENTER TANK TANK AT C 47 , BETWEEN BEAM 1-2 LT AND RT. REPAIR PERFORMED BY PERFORMING CRACK S TOP HOLE AND INSTALLING A DOUBLER IAW RAS /70512671/004/2008 ISS A, APPROVED BY EA 6-5315-123074. 2 L 7 2 4F RT A35EU 20080925 SO 2008 9 25 SWIA200820022 1 20080725 A 2497 BUSS BAR EMB 120 EMB120ER 3260203 SO APU RELAY BURNED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 564SW 120339 FOUND BUSS BARS IN APU RELAY BOX BURNED. C-CHECK, INSTALLED NEW SERVICABLE BUSS BARS. 2 L 7 2 4T RT A31SO 20080925 SO 2008 9 25 SWIA200820023 1 20080725 A 2497 CONTACTOR EMB 120 EMB120ER 3260203 SO APU RELAY BURNED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 564SW 120339 FOUND CONTACTOR IN APU AUX RELAY BOX BURNED. C-CHECK, REPLACED APU CONTACTOR IN APU AUX RELAY SHELF. 2 L 7 2 4T RT A31SO 20080925 SO 2008 9 25 SWIA200820025 1 20080724 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 564SW 120339 JUMP SEAT FLOORBOARD, LT AND RT FLOOR PROP ANGLES ARE CRACKED. C-CHECK, REPLACED RT FLOOR PROP ANGLES. 2 L 7 2 4T RT A31SO 20080926 EU 2008 9 26 08FDEA03826 1 20080911 A 5321 A532102100000 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 AVIONICS COMPARTMENT FLOOR PANEL 122 JF HAS EDGE DAMAGE. FABBED A NEW PANEL IAW PANEL IAW DWG SRZ 25-005 "G". PART MAR KED IAW GMM 7-0-1001. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03506 1 20080819 A 5753 A57960032200201 SKIN AIRBUS 300 A300F4605R 3930327 EU LT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 LEFT WING INBD FLAP L/E HAS A DENT APPROXIMATELY 6' FROM THE INBD EDGE OF THE FLAP. REPAIRED THE LEFT WING INBD FLAP L/ E SECTION IAW SRM 57-50-00, FIG 208. 2 L 7 2 4F RT A35EU 20080926 WP 2008 9 26 08FDEA03254 1 20080805 A 5321 ABA72034 FLOOR PANEL DOUG DC10 DC1030F 3023504 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 AFTER REMOVAL FLOOR PANEL ON COCKPIT AREA WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE. 2 L 7 3 4F RT A22WE 20080926 WP 2008 9 26 08FDEA03255 1 20080805 A 5730 ARB23122 SKIN DOUG DC10 DC1010 3022110 WP ZONE 600 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 RT WING L/E DROOPED FOUND DEEP WEAR ON EXT SKIN. REPAIRED AREA IAW SRM 57-10-00 VOL I FIG 39. 2 L 7 3 4F A22WE 20080926 EU 2008 9 26 08FDEA03827 1 20080911 A 5321 B5327027300000 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 600 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 MAIN DECK CARGO COMPARTMENT FLOOR BOARD 252 GF IS TORN BETWEEN FRAME 57.1 AND FRAME 58, RBL 18 AND RBL 37. FABRICATED A NEW PANEL IAW DWG SRZ 25-005; REV "G". PART MARKED IAW GMM 7- 0-1000. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03834 1 20080911 A 5321 B5327048401200 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 MAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 43 AND FRAME 47; LBL 57 AND LBL 77. NR 241 WH FABRICATED F LOORBOARD IAW FEDEX DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03835 1 20080911 A 5321 B5327048401200 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 MAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 40 AND FRAME 43; LBL 57 AND LBL 77. NR 241 TH FABRICATED F LOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03836 1 20080911 A 5321 B5327048401600 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 MAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 34 AND FRAME 37; RBL 17 AND RBL 37. NR 242 GF FABRICATED FLOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03837 1 20080911 A 5321 B5327048401600 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 MAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 34 AND FRAME 37; RBL 17 AND RBL 37. FABRICATED FLOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03513 1 20080820 A 5720 A57247016 SHROUD AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON TOP SKIN OF OUTER SHROUD BOX, RIB 25-28 LT OUT OF LIMIT. REPAIR PERFORMED BY CUT AWAY THE AFFECTED R IBS, REWORK OF CORROSION AND INSTALLING MANUFATURED ANGLES TO THE CUT RIB POSITIONS IAW RAS/BAE/1007548/2008 ISS A, APPR OVED BY EA 6-5751-120095. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03385 1 20080812 A 7160 8198021 ACTUATOR AIRBUS 300 A300B4622R 3930312 EU STATOR VANE FAILED A FDEA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 CE 21 749FD 536 NR 1 ENG COMPRESSOR STALL BEGINNING DESCENT FROM FL350 ENG WOULD NOT RESTART. WINDMILLING WITHOUT OIL PRESSURE WAS 15 MINUTES. REMOVED AND REPLACED THE STATOR VANE ACTUATOR . 2 L 7 2 4F RT A35EU 20080929 NM 2008 9 29 UPS08553315 1 20080814 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 1640 S25-26L DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 CUSTOMER REQUEST REPAIR AREA OF BS 1640 FRAME STR 25L TO 26L PER EO B757-5310-27669-B REPORT FINDINGS TO CUSTOMER. REPORTED FINDING TO CUSTOMER AND REPAIR 1640 FRAME & CHORD PER EO B757-5310-27669-C. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 2008UALA05704 1 20080913 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT LIGHT INOP UPPER DECK CEILING ROW 17. FOUND DEFECTIVE LAMP. REPLACED LAMP. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 NM 2008 9 29 2008UALA05716 1 20080913 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1410 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 FRAME DENTED AFT PIT BS 1410 AND STR 26L - 25L. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION AND INSTALLED DOUBL ER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080929 2008 9 29 2008UALA05719 4 20080913 A 2397 CONNECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU O2 MASK COMM UNDERSERVICED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 326UA 23958 F/O SIDE OXYGEN MASK COMM CONNECTOR DISCONNECTED. REPAIRED O2 BOX CONNECTOR. 2 L 7 2 4F 4 F RT A16WE E21EU 20080924 NM 2008 9 24 08FDEA03109 1 20080729 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT F ITTING AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB CRACKED NR 2 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 08FDEA03792 1 20080910 A 5311 6515930 FRAME BOEING 727 727227 1384078 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 TOP OF FRAME DAMAGED UNDER "Z" FLOOR SUPPORT FS 540, RBL 7, WL 155. REMOVED DAMAGE AT TOP OF FRAME, NDT VERIFIED DAMAG E REMOVAL. FABRICATED REPAIR DOUBLER, TREATED AND PRIMED DOUBLER AND DAMAGED CUT OUT. INSTALLED REPAIR DOUBLER. REF SRM 51-40-3, FIG 1/ NDT MAN, PART 6 51-00-00, FIG 23 THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20080924 NM 2008 9 24 08FDEA03117 1 20080729 A 5310 ACA72251 DOOR FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 CRACK INDICATION FOUND ON SECOND LAYER DURING HFEC OPEN HOLE INSPECTION ON 0.520 INCH HOLE AT MAIN CARGO DOOR NR 7 LOWER JAMB AT HOLE B. MAIN CARGO DOOR NR 7 LOWER JAMB AT HOLE B, CRACKED SECOND LAYER REPAIRED AS PER FEDEX EA NR 1-5310-124 330, TITLE: FUSELAGE, MAINFRAME, MAIN CARGO DOOR LOWER JAMB BORE HOLES AT STA 757.708. REPAIR CLASSIFIED AS MAJOR PER G MM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 08FDEA03611 1 20080828 A 5330 6554583153 SKIN BOEING 727 727227 1384078 NM BS 1010 S22-23L DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 FUSELAGE LT SIDE SKIN BULGE AT STA 1030 AND STA 1010 AND STR 22L - STR 23L CUTOUT DAMAGED AREA DIM 8" PER 4 3/4" IAW SRM 53-30-3 FIG 3. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3 FIG 3 AND 53-30-2 FIG 2. TREATED AND PRIMED DOUBL ER AND AREA IAW SRM 51-10-2. INSTALLED REPAIR WASHER AND REPAIR PARTS IAW SRM 51-30-8 AND 51-30-2. 2 L 7 3 4F A3WE 20080924 NM 2008 9 24 08FDEA03613 1 20080828 A 5330 65564225 SKIN BOEING 727 727227 1384078 NM BS 660-680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 FWD CARGO COMPARTMENT, FUSE SKIN IS CORRODED STR 28L FROM STA 660 TO STA 680 WITH EXFOLIATION CUTOUT DAMAGED AREA DIM 12 .9 INCH AND FABRICATED REPAIR FILLER AND 2 REPAIR SPLICES IAW SRM 53-10-3 FIG 1. TREATED AND PRIMED REPAIR PARTS AND AR EA IAW SRM 51-10-2. INSTALLED REPAIR PARTS AT STRINGER 28L BTW STA 660 NAD STA 680 IAW B727 SRM 53-10-3 FIG 1 AND SRM 5 1-30-2. 2 L 7 3 4F A3WE 20080924 NM 2008 9 24 DL76G081129 1 20080828 A 3610 SHUTOFF VALVE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE PNEUMATIC SYS FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1605 30198 704233 RT ENGINE PNEUMATIC PRESSURE FLUCTUATING ON TAXI OUT. REMOVED PRSOV. INSTALLED PRSOV PER MM. PERFORMED OPS CK PER MM . ALL NML. PERFORMED HI PWR RUN CK OUT PER MM. ALL NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 20080926 WP 2008 9 26 08FDEA02265 1 20080614 A 5347 NEA6022 SEAT TRACK DOUG DC10 DC1010 3022110 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 MAIN CABIN EXFOLIATION CORROSION ON SEAT TRACK. REPAIR AREA IAW SRM 53-70-00 FIG.1 SHT 3 AND 4 VOL I. 2 L 7 3 4F A22WE 20080929 NM 2008 9 29 UPS08553302 1 20080812 A 5247 STRUCTURE BOEING 757 75724APF 1384969 NM APU DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 CORROSION EMANATING AROUND NUT PLATES ON APU INLET DOOR STRUCTURE. REPAIR PER ATS ER 08-2706 DATED 0 2SEP08. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 2008UALA05718 1 20080913 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1540 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 AFT PIT STA 1540 FRAME DENTED AT STR 25L AT INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED FRAME SECTION A ND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080929 NM 2008 9 29 2008UALA05840 1 20080922 A 5320 CHANNEL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 480 S10L CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 BS 480, STR 10L CRACKED IN CHANNEL AT FASTENER HOLE. MAJOR REPAIR ACCOMPLISHED PER S/B 747-53A2484 FIG 24. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 WP 2008 9 29 08FDEA03900 1 20080916 A 5730 ARB25104 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 RIGHT WING LOWER L/E PANEL 616 HB IS CHAFED. BLENDED AREA IAW SRM 57-00-01; VOL I; FIG 1-A. ORIGINAL MATERIAL THICKNES S 0.090 IAW SRM 57-31-01; VOL III. MATERIAL LOSS 0.022. REMAINING THICKNESS 0.068 AND FOUND OUT OF LIMITS IAW SRM 57-0 0-01; VOL I. CUT OUT THE DAMAGE IAW SRM 57-00-01; VOL I. FABRICATED THE FILLER AND DOUBLER IAW SRM 57-00-01; VOL I A ND SRM 57-31-01; VOL III. ALODINED AND PRIMED IAW SRM 51-21-01; VOL II; PGS 21 - 24. 2 L 7 3 4F RT A22WE 20080929 EU 2008 9 29 08FDEA03515 1 20080820 A 5720 A57247016 SHROUD AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION ON TOP SKIN OF OUTER SHROUD BOX, RIB 25-28 RT OUT OF LIMIT. REPAIR PERFORMED BY CUT AWAY THE AFFECTED R IBS, REWORK OF CORROSION AND INSTALLING MANUFACTURED ANGLES TO THE CUT RIB POSITIONS IAW RAS/BAE/1007548/2008 ISS, APPRO VED BY EA 6-5751-120095. 2 L 7 2 4F RT A35EU 20080929 NM 2008 9 29 08FDEA03520 1 20080820 A 5551 6954077 FITTING BOEING 727 7272S2F 1384O81 NM HORIZONTAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 GENERATED BY EO 7-5510-7-5000, HORIZONTAL STAB RT HINGE FITTING O/B BUSHING BORE HAS CORROSION OVERSIZED LUG BORE TO 2.2 244 INCH CORROSION REMOVED. HFEC INSPECTED BORE NO DEFECTS NOTED. FABRICATED OVERSIZE BUSHING, CAD PLATED BUSHING. IN STALLED OVERSIZE BUSHING IN LUG, IAW MM 55-10-051-8. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080929 NM 2008 9 29 08FDEA03399 1 20080813 A 3234 652848310 HANDLE BOEING 727 727233 138408A NM MLG DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 LEFT AND RIGHT MLG DOOR RELEASE HANDLES ARE GOUGED. BLENDED GOUGES AT LEFT AND RIGHT MLG DOOR RELEASE HANDLES IAW EA 7- 3210-117011. 2 L 7 3 4F RT A3WE 20080929 NM 2008 9 29 08FDEA03401 1 20080813 A 5720 69166384 SUPPORT ANGLE BOEING 727 7272S2F 1384O81 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 RIGHT WING OB LE CAVITY, LE UPPER SKIN FORMED SUPPORT ANGLE CRACKED AT AFT END ABOVE TAI DUCT AT INBD END OF NR 5 SLAT W ELL. REMOVED INTERCOSTAL AND SUPPORT ANGLE AT SLAT STA 260. FABRICATED NEW SUPPORT ANGLE. VERIFIED MATERIAL 2024 T-3, FAB'D WITH 2024-0, HEAT TREATED TO 2024 T-3. INSTALLED NEW SUPPORT ANGLE AND REINSTALLED INTERCOSTAL REF SRM 51-30-2 P G 2-3, DWR 69-16638. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080929 WP 2008 9 29 08FDEA03939 1 20080918 A 5313 AYB70131 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 CENTER WHEEL WELL LONGERON 52 IS CORRODED AT FS 1481. REMOVED DAMAGED SECTION OF LONGERON. FABRICATED NEW SECTION OF L ONGERON, LOCATED, & DRILLED IAW DWG AYB 7013. FABRICATED LONGERON SPLICES. LOCATED & DRILLED IAW SRM 53-00-01. ALODIN ED & PRIMED NEW SECTION OF LONGERON & SPLICES IAW SRM 51-21-01. APPLIED TOP COAT OF PAINT IAW SRM 51-21-01. PART MARKE D IAW GMM 7-0-1001. INSTALLED LONGERON & SPLICES IAW SRM 53-00-01 & SRM 51-33-01. 2 L 7 3 4F RT A22WE 20080929 EU 2008 9 29 08FDEA03310 1 20080807 A 5753 RIB AIRBUS 300 A300B4622R 3930312 EU RT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 WHILE ACCOMPLISHING EO 6-5750-7-5000 PT 4 "WINGS - INBD FLAP, REPLACEMENT NOSE RIB 7 RT", STEP 10; THE ACCESS HOLE HAS BEEN PREVIOUSLY CUT AND IS 0.500" TOO LARGE. OMITTED FASTENERS AT EXTENDED CUT OUT; INSTALLED OVERSIZED FASTENERS AND P ERFORMED SPAR REPAIR IAW EA 6-5750-117001. 2 L 7 2 4F RT A35EU 20080929 NM 2008 9 29 08FDEA03311 1 20080808 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 587FE 48489 DURING OPEN-HOLE INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRAC K INDICATIONS AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FABRICATED AS PER FEDEX EA NR 1-5 300-122409A, SUPPORT FITTING NR 3 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR BUSHING FABRICATED AND IN STALLED ON MAIN CARGO DOOR LOWER JAMB WEB AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100. 2 L 7 3 4F RT A22WE 20080930 NM 2008 9 30 UPS08M53145 1 20080816 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 6 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAI R BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080930 NM 2008 9 30 UPS08M53146 1 20080811 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 5 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAI R BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080930 NM 2008 9 30 2008UALA04348 1 20080819 A 2611 SMOKE DETECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE E/E BAY FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 769UA 26921 DET CHAN 2 E-E SMOKE ELECTRICAL EQUIPMENT (E-E) COOLING SMOKE DETECTOR CHANNEL 2 FAILS BITE CHECK. STATUS MSG01- ACTIV E CRUISE HARD; E-E COOLING SMOKE DETECTOR HAS NO OUTPUT OR IS FAILED. DB- CARGO SMOKE DETECTOR CH 2 (LWR FWD) MSG02- AC TIVE CRUISE HARD; E-E COOLING SMOKE DETECTOR HAS NO OUTPUT OR IS FAILED. MSG-2620070 ACTIVE ER HARD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080930 NM 2008 9 30 CALA0800804 1 20080821 A 5340 STRINGER CLIP BOEING 737 737524 1384721 NM BS 400 S16R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 STATION 400 S16R TIE CLIP CRACKED. REMOVED AND REPLACED TIE CLIP AT STA 400 S16R REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800805 1 20080822 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 787 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 BODY STATION 787 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN S8L AND S9L. REPAIRED CRACKED FRAME A T STATION 787 LEFT SIDE AT AC BRACKET BETWEEN STR 8 AND 9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800812 1 20080822 A 5311 6546540 FRAME BOEING 737 737524 1384721 NM BS 747 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 BODY STATION 747 RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REMOVED CRACK AND INSTA LLED REPAIR ANGLES PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800817 1 20080822 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 907 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 BODY STATION 907 RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REPAIRED CRACKED FRAME AT STATION 907 RIGHT AT AC RAIL BRACKET BETWEEN STR 8 AND 9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800822 1 20080823 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM BS 787 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14628 27532 RIGHT FRAME CRACKED AT FASTENER FOR AIR SUPPORT RAIL MOUNT LOCATED AT STATION 787 BETWEEN STR 8 AND STR 9. REPAIRED FRA ME AT STATION 787 BETWEEN STRINGERS 8 AND 9 PER EA5310-04498 OP2. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800824 1 20080824 A 5311 143A1120 FRAME BOEING 737 737724 13844BY NM BS 480 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27722 28789 CABIN STATION 480 FRAME CRACKED BETWEEN S8 LT AND S9 LT. REPAIRED CRACKED FRAME BODY STATION 480 STR 8 AND STR 9 LEFT R EF EC/RA 5310-04824 REV A. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800830 1 20080824 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM BS 400 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14628 27532 LEFT FRAME CRACKED AT FASTENER FOR AIR GRILL SUPPORT RAIL MOUNT LOCATED AT STATION 400 BETWEEN STRINGERS 8 AND 9. REPA IRED FRAME PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 2008UALA04057 1 20080728 A 3350 BATTERY PACK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT DISCHARGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 332UA 24193 EMERGENCY EXIT LIGHTS ON AND OFF INTERMITTENTLY. REPLACED BATTERY & CHARGER FOR M1197. LIGHTS OPERATE NORMALLY. 2 L 7 2 4F 4 F RT A16WE E21EU 20080930 NM 2008 9 30 2008UALA04130 1 20080805 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 26 ABC INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 EMERGENCY LIGHT INOPERATIVE: SEAT 26 ABC. REPLACED LIGHT ASSY. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04180 1 20080808 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 SEAT 56ABC EMERGENCY LIGHT IS INOP. *S/D* RELAMPED, CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 NM 2008 9 29 UPS08553323 1 20080912 A 5610 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT CONTAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 R1 WINDOW WATER INGRESS AT BUS BAR. *SUPPLEMENTAL SDR* REMOVED AND REPLACED F/O'S NR 1 WINDOW UP TO STEP 20 (REQUIRES INSPECTION TORQUE) & HEATING SYSTEM CHECK AND WINDOW WIPER OPERATIONAL CHECK. STEPS 26&27 ARE COMPLETED PER AMM 56-11-0 1-4. REF LP 59803 TORQUED WINDOW HEAT TERMINALS PER MM 56-11-0-4. COMPLETED INSTALLATION OF R1 WINDSHIELD PER MM 56-11 -01-4. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 UPS08653313 1 20080911 A 5610 WINDOW BOEING 767 76734AF 1385212 NM COCKPIT DELAMINATED A IPXA O OTHER O OTHER CR CRUISE 1 SO 01 312UP 27763 INSPECTION TYPE:N/A DIVERSION - R2 WINDOW HAS DELAMINATION APPROX 3 INCHES HIGH COVERING THE LOWER FORWARD HALF OF THE W INDOW. SLIGHT DISTORTION OF VIEW. DISCOVERED AFTER AIRBORNE. REVISED AND REPLACED R2 WINDOW ASSY AS REQ'D PER 50-11-0 2-40. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A1NM 20080924 EU 2008 9 24 08FDEA03376 1 20080811 A 5330 A53978149200 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 430FE 394 DENT ON FUSELAGE SKIN LOCATED AT FR 68 ABOVE LT STRINGER 44 MEASURING 4 IN BY 1.5 IN BY .025 DEEP CUT OUT DAMAGED AREA A ND INSTALLED SKIN REPAIR AT LONGITUDINAL LAP JOINT BETWEEN FR 68 AND FR 69, STR 44 LT IAW A310-200 SRM 53-10-12, FIG 216 SHT 1. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03489 1 20080818 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 650FE 726 MAIN CABIN FRAME 48 SUB-FLOOR AT Y 145.6 FLOORBEAM WEB LOWER INBD MOUNT IS CRACKED. REMOVED AND REPLACED THE FITTING IAW A300-600 SRM 51-40-21;PARA 10-B. 2 L 7 2 4F RT A35EU 20080924 WP 2008 9 24 08FDEA03490 1 20080818 A 2750 AYG70305505MODF CONTROL VALVE DOUG MD10 MD1010F 3022112 WP TE FLAPS FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 68052 66077 47806 LVL 2 FLAP DISAGREE AFTER TAKEOFF RAN QRH AND MADE NORMAL LANDING. CREW REPORTED IT TOOK 10 MINUTES FOR FLAPS TO EXTEND 35 DEGREES FOR LANDING. REMOVED AND INSTALLED I/B FLAP CNTL VALVE AND SECURED HYD LINES TO OTHER VALVES REF MD10-10 A MM 27-52-02-2. OPS CK AND LEAK CK GOOD. OFF MFG AYG7030-5505MODFX SRL SEM391, ON MFG AYG7030-5511, SRL SEM2176. 2 L 7 3 4F RT A22WE 20080924 EA 2008 9 24 SWIA200820038 1 20080909 A 3260 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING ILLUMINATED A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 913SW 7597 "STEERING INOP" FOLLOWED BY GEAR DISAGREE WARNING MSG. JACKED THE NOSE GEAR AND PERFORMED SEVERAL GEAR RETRACTIONS, NOS E GEAR OPERATES NORMALLY. 2 L 7 2 4F RT A21EA 20080924 EA 2008 9 24 SWIA200820039 1 20080907 A 3250 STEERING SYS CNDAIR CL600 CL6002C10 1390015 EA NLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION LD LANDING 1 NM 07 746SK 10202 CAUTION STEERING INOP. MESSAGE UPON TOUCH DOWN (WOW) RUNWAY 120 IN SAT AIRCRAFT VEERED OFF THE RUNWAY. CLEARED NWS PLT HANDWHEEL FAULT CHECKED RIGGING OF NWS CONTROL BOX. PERFORMED TAXI CHECK. 2 L 7 2 4F RT A21EA 20080924 WP 2008 9 24 08FDEA03229 1 20080804 A 5330 AFA601411 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 THE LOWER FUSELAGE SKIN IS DENTED AT FS 1682, LONGERON 44L. REPAIRED AREA AT STA 1682, LONGERON 44L IN REFERENCE TO SRM 53-20-00; VOL I; FIG 6. 2 L 7 3 4F RT A22WE 20080924 EU 2008 9 24 08FDEA03238 1 20080804 A 5753 A5796000000351 SKIN AIRBUS 300 A300F4605R 3930327 EU RT WING TE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 RIGHT WING INBD FLAP UPPER SKIN 1 INCH FROM THE INBD END IS GOUGED. BLENDED GOUGE IAW A300-600 SRM 51-73-10. ORIGINAL MATERIAL THICKNESS 0.031 IAW A300-600 SRM 57-52-12; ITEM 45. REMOVED 0.004. REMAINING MATERIAL 0.027 AND FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 57-50-00; FIG 101, SHEET 5. REPAIRED AREA IAW A300-600 SRM 57-50-00, FIG 205. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03571 1 20080825 A 5754 A53510207200 SKIN AIRBUS 300 A300B4622R 3930312 EU KRUEGER FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 KRUEGER FLAP WAS DAMAGED DURING FUNCTION CHECKS REPAIR PERFORMED BY REPLACEMENT OF KRUEGER FLAP ASSY IAW AMM 27-87-11/40 1. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03572 1 20080825 A 5754 A53510285004 VANE AIRBUS 300 A300B4622R 3930312 EU KRUEGER FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 KRUEGER FLAP VANE WAS DAMAGED DURING FUNCTION CHECKS. REPAIR PERFORMED BY REPLACEMENT OF KRUEGER FLAP VANE ASSY IAW AMM 27-87-12/401. 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03314 1 20080808 A 5710 6521655439 SUPPORT BEAM BOEING 727 727233 138408A NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 275FE 22040 LT WING TRAILING EDGE SUPPORT BEAM CUT OUT ON SPOILER NR 7 IS CRACKED AT WBL 122 REMOVED "J" BEAM IAW B727 SRM 51-30-2. FABRICATED NEW "J" BEAM FROM BAC 1506 860 7075 T6 (DIM 81 INCHES IN LENGTH) AND TREATED AND PRIMED IAW B727 SRM 51-10-2 . INSTALLED "J" BEAM IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 20080924 NM 2008 9 24 08FDEA03315 1 20080808 A 7160 65196854541 SKIN BOEING 727 727233 138408A NM NR 1 NOSE COWL DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 275FE 22040 NR 1 ENGINE NOSE COWL SKIN DAMAGED AT 9 O'CLOCK POSITION CUT OUT DAMAGE AREA DIM 4 3/4 BY 3 1/2 IAW B727 SRM 54-30-3 FIG 5. CUT OUT ACCESS HOLE DIM 5 IN ABOVE DAMAGE IAW B727 SRM 54-30-3 FIG 3. FABRICATED DOUBLER REPAIRS FROM 2024T3, 0.04 0 INCH AND FILLER FROM 2024T3 0.032 INCH IAW B727 SRM 54-30-3. FABRICATED ACCESS DOOR MAT 2024T3, 0.050 INCH AND RING F ROM 2024T3, 0.010 AND DOUBLER FROM MAT 0.063 INCH AND PLATE FROM 2024T3 0.063 INCH IAW B727 SRM 54-30-3. TREATED AND PR IMED REPAIR PARTS AND CUT OUT AREA IAW B727 SRM 51-10-2. INSTALLED ALL REPAIR PARTS IAW B727 SRM 51-30-2. 2 L 7 3 4F RT A3WE 20080924 EU 2008 9 24 08FDEA03573 1 20080825 A 5320 R257B100307200 PAN AIRBUS 300 A300F4605R 3930327 EU PDU GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 FWD CARGO COMPART, EMT BALL MAT 131 XG PDU PAN IS GOUGED AT A MOUNT HOLE. REPAIRED BALL MAT 131 XG PDU PAN IAW EA 6-255 0-117025. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03575 1 20080825 A 5751 A5724476600639 PANEL AIRBUS 300 A300F4605R 3930327 EU LT AILERON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 LEFT AILERON BOOSTER PANEL IS CRACKED. REPLACED THE LEFT AILERON BOOSTER PANEL IAW A300-600 AMM 27-11-28-4. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03138 1 20080729 A 5321 B5327060600200 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CABIN FLOOR PANEL BETWEEN FRAMES 40 TO 43 AND LBL 57 INCH TO 77 INCH IS BROKEN. FABRICATED NEW FLOOR BOARD NR 241 TH IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03491 1 20080818 A 5320 SILL BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 R2 DOOR LOWER SILL HAS SEVERAL SPOTS OF SURFACE CORROSION. MINOR SURFACE CORROSION REMOVED IAW SRM 51-10-02 REV 93 AND FOUND WITHIN ALLOWABLE LIMITS. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080924 NM 2008 9 24 08FDEA03112 1 20080729 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTI NG AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB CRACKED NR 5 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-3 1-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 DLM90081106 1 20080729 A 5320 593607195 INTERCOSTAL DOUG MD90 MD9030 3023690 NM BS 1328-1344 L30 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DN 53395 FOUND INTERCOSTAL EXFOLIATED, REPLACED. 2 L 7 2 4F RT A6WE 20080924 NM 2008 9 24 DLM90081108 1 20080731 A 5320 99360749 FITTING DOUG MD90 MD9030 3023690 NM BS 1261276 L29 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DN 53395 FOUND CLIP CORRODED. REPLACED CLIP. 2 L 7 2 4F RT A6WE 20080924 NM 2008 9 24 DL764081110 1 20080823 A 4920 38006081 ENGINE BOEING 767 767432ER 1385134 NM APU INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 845MH 11468 29719 APU NO START. REMOVED AND REPLACED STARTER NO HELP 320051. REMOVED AND REPLACED APU BATTERY NO HELP 320051. RMOVED AN D REPLACED APU ASSY PER AMM. OPS AND LEAK CKS GOOD. SWAPPED OVER IGV ACT ASSY S/A 2022 AND STARTER S/N 274 PER AMM. C KS GOOD. 2 L 7 2 4F RT A1NM 20080924 NM 2008 9 24 DL764081111 1 20080823 A 2910 HYDRAULIC SYSTEM BOEING 767 767432ER 1385134 NM RT RF MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 844MH 29717 P1003 RIGHT RF HYD QTY IND TRANSFERED FROM CENTER TO RIGHT TANK USED ALTERNATE PROCEDURE. 2 L 7 2 4F RT A1NM 20080924 EA 2008 9 24 SWIA200820050 1 20080912 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 706SK 10149 FLT 6722 - OVERHEAD EMERGENCY LIGHT. RELAMPED. 2 L 7 2 4F RT A21EA 20080924 NM 2008 9 24 DL76L081149 1 20080514 A 3350 SIGN BOEING 767 767332 1382001 NM EMERGENCY LIGHTS INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 NS/FSB SIGN 16CDF IS INOP. CONNECTED NS/FSB SIGN AT SEAT 16CDF IAW MM 33-24-00, OP CHECK GOOD IAW MM 33-24-00. 2 L 7 2 4F RT A1NM 20080924 NM 2008 9 24 08FDEA03272 1 20080805 A 5313 AGA7036503 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 AFT CARGO, RIGHT LONGERON 42 AT STA 1955 FOUND CORROSION. AFT CARGO, RIGHT LONGERON 42 AT STA 1955 CARRIED OUT REPAIR A S PER SRM 53-10-00 FIGURE 2 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. LONGERON REPAIR WAS ALSO CARRIED OUT IN REFERENCE TO FEDEX EA NR 1-5310-124322, TITLE, FUSELAGE, MAINFRAME, REPAIR RIGHT LONGERON 42L AT STATION 1953.0. 2 L 7 3 4F RT A22WE 20080924 EU 2008 9 24 08FDEA03799 1 20080910 A 2810 A5517781020400 FITTING AIRBUS 300 A300F4605R 3930327 EU RT FUEL TANK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 RIGHT THS INTERNAL FUEL TANK HOIST POINT FITTING IS CRACKED AT THE FWD SPAR, ACCESS 343 EB. WORK ACCOMPLISHED ON E.A. 6 -5510-7-5001. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03348 1 20080808 A 5321 R532B363100000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 241 DF IS DAMAGED. REPAIRED CABIN FLOOR PANEL 241 QH BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARK ED AND APPLIED NON-SKID TAPE IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03349 1 20080808 A 5321 R532B363000000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 241 EF IS DAMAGED REPAIRED CABIN FLOOR PANEL 241 EF BY FABBING A NEW PANEL USING THE OLD PANEL AS A TE MPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SKID TAPE IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03350 1 20080809 A 5330 6518420282 SKIN BOEING 727 727233 138408A NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 275FE 22040 FUSELAGE SKIN BELOW L1 DOOR CUTOUT HAS 2 VERTICAL DENTS AT STA 320 BETWEEN STR 17L - 19L. EVALUATED 2 DENTS AND MEASURE D DENTS A: 1.0 Y: .019 A/Y 45.2 AND DENT 4 A: 2.4 Y: .053 A/Y 45.2, A/Y RATIO WITHIN LIMITS BUT DENTS ARE COMMON TO TEAR STRAP AND LESS THAN 10 INCHES FROM LAP SEAM IAW B727 SRM 53-30-1. REPAIRED DENTS AT FUSELAGE SKIN BELOW L1 DOOR CU T-OUT STA 320 AND BETWEEN STR 17L - 19L IAW FX EA 7-5330-122389, FUSELAGE SKIN PANEL BETWEEN STATION 312 - 320 STR 17L T O STR 20L DENTS. 2 L 7 3 4F RT A3WE 20080924 NM 2008 9 24 08FDEA03801 1 20080910 A 5280 NNB678620 FRAME DOUG MD11 MD11F 3023600 NM MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 623FE 48794 RT MAIN LANDING GEAR DOOR UPPER SIDE SURFACE CENTER FRAME CRACKED AT 2 LOCATIONS. REPAIRED AS PER EA 1-5280-123102, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 08FDEA03364 1 20080810 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 587FE 48489 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B , NR C AND NR D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FABRICATED AS PER EA NR 1-5300-122409A, SUPPORT FITTING NR 7 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR BUSHING FABR ICATED AND INSTALLED ON MAIN CARGO DOOR LOWER JAMB WEB AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJ OR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 WP 2008 9 24 08FDEA03378 1 20080811 A 5411 AUB70951 RIB DOUG MD10 MD1010F 3022112 WP NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 NR 2 ENG BEAVER TAIL NR 2 AND NR 3 RIB CRACKED OR MISSING AT TRAILING EDGE. REMOVED DAMAGED RIB AND INSTALLED NEW RIBS REFERENCE DC/MD-10 SRM 51-35-01; VOL II AND 51-31-01; VOL II. 2 L 7 3 4F RT A22WE 20080930 NM 2008 9 30 2008UALA04181 1 20080808 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 UPPER DECK CEILING EMERGENCY LIGHT NEAR SEAT ROW 16 IS INOP. RELAMPED, CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04186 1 20080807 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SEAT 16C INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 518UA 24871 THE 15C EMERGENCY LIGHT HAS DETACHED. PIECE IN COCKPIT, 16C IS INOPERATIVE. REPLACED EMERGENCY LIGHT STRIP ON SEAT 16C . OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080930 NM 2008 9 30 2008UALA04197 1 20080808 A 3610 32144887 SHUTOFF VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 595UA 28748 LT ENGINE PRSOV NOT FULLY CLOSING AFTER ENGINE SHUTDOWN. REPLACED PRSOV, CHECKS GOOD. LT PRSOV & APU BLEED LIGHT WORK NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080930 NM 2008 9 30 2008UALA04207 1 20080809 A 3350 58671 INVERTER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 313UA 23674 EMERGENCY LIGHTS INOP ROWS 9-15. REPLACED INVERTER M1388. OP TEST OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 20080930 NM 2008 9 30 2008UALA04209 1 20080810 A 3350 20131A BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 520UA 24890 DOOR 1R EMERGENCY SLIDE LIGHT, EXIT LOCATOR, PASS EXIT SIGN, CL DIV EXIT LIGHT AND 1 EMER AISLE LIGHT INOP. REPLACED BA TTERY ASSY FOR M730. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080930 NM 2008 9 30 2008UALA04216 1 20080809 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 UPPER DECK EMERGENCY CEILING LIGHT ABOVE ROW 17 INOP. REPLACED LAMP, OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04223 1 20080809 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY LIGHT SEAT 2A AFT INOP. RELAMPED, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04228 1 20080811 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY CEILING LIGHT ABOVE ROW 16 INOP. RELAMPED, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04229 1 20080811 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY CEILING LIGHT TOP OF STAIRS UPPER DECK INOP. RELAMPED, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04230 1 20080811 A 3397 794640 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY LIGHT ON LT WALL LAV 110 DOOR 2L INOP. *S/D* RESECURED EMERGENCY LIGHT CONNECTOR. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04231 1 20080811 A 3397 794640 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY LIGHT ON WALL FWD OF LAV 110 DOOR 2L INOP. RESECURED EMERGENCY LIGHT CONNECTOR. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04238 1 20080810 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT LIGHT INOP AT DOOR 5 LEFT CEILING ENTRY. REPLACED LAMP. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04239 1 20080810 A 3397 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT LIGHT INOP ACROSS DOOR 4 LEFT LOWER WALL EMERGENCY LIGHT. REPLACED POWER FEEDER CABLE, OPS CHECKS NORMAL . 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04245 1 20080811 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 803UA 748 FUSELAGE DENT LEFT OF FWD ELECTRONICS DOOR. MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 20080924 NM 2008 9 24 DL76P081154 1 20080904 A 8011 774860A4 STARTER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 144DA 27584 724687 NR 1 ENG NO START NO ROTATION, FOUND STARTED AT FAULT. REPLACED STARTER. 2 L 7 2 4F 4 F RT A1NM E24NE 20080924 2008 9 24 DLM88081156 4 20080904 A 2565 SLIDE DOUG MD88 MD88 3023688 NM LOW PRESSURE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 954DL 49885 FWD SVC DOOR SLIDE PRESSURE LOW. REPLACED SVC DOOR SLIDE PACK PER MM. 2 L 7 2 4F RT A6WE 20080924 NE 2008 9 24 DL76G081157 2 20080906 A 7200 ENGINE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1602 42473 29694 704809 FOUND DURING SERVICE CHECK, FOUND METAL ON MCD. SHOP ANALYST REPORTS BEARING MATERIAL. MUST REPLACE ENGINE, E/C IN WOR K ATL. 2 L 7 2 4F 4 F RT A1NM E13NE 20080925 EU 2008 9 25 08FDEA03853 1 20080912 A 5553 A55570012202 ATTACH FITTING AIRBUS AIRBUS 310 A310203 3930313 EU VERTICAL STAB CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 426FE 245 VERT STAB ATTACH FITTING CORROSION L AND R SIDE. COMPLIED WITH EA 6-5536-110931 RII:680053. COMPLIED WITH EA 6-5536-11 0931. 2 L 7 2 4F RT A35EU 20080925 NM 2008 9 25 08FDEA03944 1 20080919 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 DURING OPEN-HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH C RACK INDICATIONS AT HOLES A, B AND D. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIF IED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03946 1 20080919 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CRACK INDICATIONS AT HOLES A, C AND D. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03947 1 20080919 A 5347 A5A7082503 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 MAIN DECK SEAT TRACK BETWEEN STA 5-73 TO 5-93 RBL 8.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENTAS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03949 1 20080919 A 5730 ARB74024 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 DURING HFEC INSPECTION, FOUND 14 FASTENER HOLES WITH CRACK INDICATIONS AT RIGHT WING LOWER SKIN PANELS OUTER WING ACCE SS DOOR CUTOUT BETWEEN XORS 683.400 AND 713.600. REPAIRED AS PER EA 1-5710-122560, THIS REPAIR IS CLASSIFIED AS MINOR P ER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 EU 2008 9 25 08FDEA03335 1 20080808 A 5321 R532B363800000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 241 GF IS DAMAGED. REPAIRED CABIN FLOOR PANEL 241 GF BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARK ED AND APPLIED NON-SKID TAPE IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03962 1 20080922 A 5754 SKIN AIRBUS AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD FH1488 664 FOUND 2 AREAS OF CHAFING MARKS ON LT SLAT NR 1 LOWER SKIN. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS IAW RAS/FOK/ 226/2008 ISS A, APPROVED BY EA 6-5742-123060. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03964 1 20080922 A 5753 SKIN AIRBUS AIRBUS 300 A300B4622R 3930312 EU LT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD FH1140 664 FOUND 2 AREAS OF CHAFING MARKS ON LT OUTER FLAP TOP SKIN, RIB 4-5 AND 15-17. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS IAW RAS/FOK/227/2008 ISS A, APPROVED BY EA 6-5754-123065. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03965 1 20080922 A 5753 SKIN AIRBUS AIRBUS 300 A300B4622R 3930312 EU LT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD FH1141 664 FOUND 2 AREAS OF CHAFING MARKS ON LT CENTER FLAP TOP SKIN, RIB 13-15 AND 20-21. REPAIR PERFORMED BY BLEND OUT THE CHAFI NG MARKS IAW RAS/FOK/229/2008 ISS A, APPROVED BY EA 6-5753-123084. 2 L 7 2 4F RT A35EU 20080925 NM 2008 9 25 08FDEA03966 1 20080922 A 5753 NRC6762502 VANE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 RIGHT WING, INBOARD FLAP VANE LOWER OUTBOARD HALF FOUND DELAMINATION, APPROXIMATELY 7 INCH BY 37 INCH. REMOVED AND REPL ACED AS PER AMM 27-50-22-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 FOUND 'SATISFACTORY'. REPAIR CLASSI FIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03967 1 20080922 A 5347 A6A70821 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 MAIN DECK SEAT TRACK BETWEEN STA 1119 TO 6-10 LBL 8.5 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS P ER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03974 1 20080922 A 5531 AJC75151 SPAR CAP DOUG MD11 MD11F 3023600 NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 HFEC INSPECTION CARRIED OUT AND FOUND ONE CRACK INDICATION ON RIGHT SIDE RADIUS OF LOWER SPAR CAP AT LOWER VERTICAL ST ABILIZER. REPAIRED AS PER SRM 55-20-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080930 NM 2008 9 30 2008UALA05415 1 20080822 A 2620 FIRE BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CARGO BAY MALFUNCTIONED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 171UA 24322 BTL LOW CARGO B MSG DISPLAYED AND DISCHARGE LIGHT ON OVERHEAD PANEL ILLUMINATED, NO FWD OR AFT LIGHT ON. REPLACED FIRE "B" BOTTLE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA05426 1 20080823 A 3350 36367 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 EMERGENCY LIGHT LAMP INOP ROW 11. REPLACED EMERGENCY LIGHT LAMP. 2 L 7 2 4F 4 F RT A16WE E21EU 20080930 NM 2008 9 30 2008UALA05432 1 20080823 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 LT FWD EXTERIOR GROUND ILLUMINATION EMERGENCY LIGHT INOP. CLEANED AND SECURED LAMP, AND CONTACT, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA05434 1 20080823 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ROW 9 LT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 ROW 9 LT EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA05435 1 20080823 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ROW 14 LT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 ROW 14 LT EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA05454 1 20080825 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY LIGHT AFT GALLEY BOTTOM WALL LT INOP. RESECURED EMERGENCY LIGHT CONNECTOR. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NE 2008 9 30 2008UALA05455 2 20080824 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 SURGES A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 676UA 30028 729015 NR 2 ENGINE SURGE. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA05460 1 20080825 A 3397 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 EMERGENCY LIGHTS ARE INOP FROM ROW 16 TO AFT GALLEY. REPLACED WALL FEEDER CABLE. EMERGENCY LIGHT BATTERY NEEDS TO CHA RGE TO FINISH OPS CHECK. 2 L 7 2 4F 4 F RT A16WE E21EU 20080930 NM 2008 9 30 2008UALA05461 1 20080825 A 5753 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LT WING TE FLAP PUNCTURED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 117UA 28810 LEFT INBOARD FORE FLAP LEADING EDGE HAS A LARGE PUNCTURE. REMOVED LEFT INBOARD FORE FLAP. COMPLETE FORE FLAP INSTALLAT ION FROM ITEM 3 PAGE 407 TO COMPLETION. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NE 2008 9 30 2008UALA05467 2 20080825 A 7250 TURBINE BLADES BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT ENGINE FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 665UA 29237 727788 LEFT ENGINE SURGE DET STATUS MSG. FOUND METAL IN THE TAILPIPE. THE ENGINE WAS REPLACED AT PRIOR TO FURTHER FLIGHT. SH OP TEARDOWN REVEALED THAT THE ENGINE HAD SUFFERED AN HP TURBINE STAGE-2 BLADE UNDER PLATFORM STRESS CORROSION (SCC) FAIL URE. ONE BLADE FRACTURED AT THE PLATFORM, WITH A PORTION OF THE PLATFORM MISSING. THIS CAUSED FAILURE OF THREE ADJACEN T BLADES. MANUFACTURER HAS INTRODUCED A NEW MATERIAL BLADE WITH AN IMPROVED UNDER PLATFORM COATING TO PRECLUDE SCC FAIL URES. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA05468 1 20080826 A 2120 UNKNOWN BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 665UA 29237 HEAVY ODOR (BURNING SMELL) IN CABIN. RTFL. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA05469 1 20080825 A 5730 116W2501 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT WING DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 774UA 26936 LT WING SKIN PANEL HAS 10 INCH CRACK AND DELAMINATION. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080930 NM 2008 9 30 2008UALA05471 1 20080825 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 677UA 30029 EMERGENCY LIGHT AT SEAT 13 NOT LIGHTED WHEN LIGHTS ON. SINGLE SEAT LIGHT INOP 13H. ADJACENT LIGHTS ALL WORK OK. RESEA TED CONNECTOR AT OUTBOARD SEAT. LIGHT OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 WP 2008 9 30 UPS08853136 1 20080816 A 5320 ANGLE DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 SIDE WALL STRUCTURAL DAMAGE IN POSITION 2/3 AREA, ATTACHED Z-ANGLE DAMAGED. *SUPPLEMENTAL SDR* FABRICATED AND INSTALLE D Z-ANGLE ON 3RD FROM FLOOR AT POS 2/3 PER SRM 57-1-21. 2 L 7 4 4F RT 4A25 20080930 NM 2008 9 30 2008UALA05516 1 20080828 A 3150 WARNING MESSAGE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 643UA 25093 NR 2 BLEED HPSOV EICAS MSG. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA05449 1 20080824 A 5310 STRUCTURE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 815UA 867 FUSELAGE DENT AFT OF FRAME 23 JUST BELOW STR 22L. *S/D* MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 20080929 NM 2008 9 29 2008UALA05823 1 20080920 A 5220 H2052K3833 LATCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY EXIT CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 LT OVERWING COMPARTMENT DOOR LATCHES (4 EA) HAS CORROSION AND EXCESSIVE WEAR MARKS. REPLACED 4 LATCHES AT LT OVERWING S LIDE COMPARTMENT DOOR. INSPECTED AND OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20080929 NM 2008 9 29 2008UALA05829 1 20080921 A 3397 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT INOP, ROWS 45 THRU 53 LEFT. CABLE FOUND DEFECTIVE. REPLACED FEEDER CABLE. OPS CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 NM 2008 9 29 08FDEA02873 1 20080713 A 2432 31433001 BATTERY DOUG MD11 MD11F 3023600 NM UNKNOWN A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 21 576FE 48501 AFTER LEVEL OFF AT FL390, APPROX 20 MIN AFTER T/O GOT LVL 1 BATT LOW ALERT. DIVERTED TO KLAS BATT SHOWED AMBER BOXED 8 OR 7. REMOVED AND REPLACED A/C BATTERIES IAW AMM 24-34-02-4. PERF DC TIE BUSS OPS CHECK. REMOVED AND REPLACED BATTERY CHARGER. REMOVED AND REPLACED BATTERY AMMETER SHUNT S4-1 RELAY, BAT CHARGER TRANSFER R2-217, RCCB BATTERY CHARGER B1-1 57, AND REPLACED PLUGS P1-1957, P1-1958, AND P1-1959 PER SWP. PERFORMED WIRING CHECKS PER AWD 24-33-01. PERFORMED EME RGENCY POWER TEST WITH NORNAL FINDINGS. STARTED APU WITH NO FAULTS AND BATTERY RECOVERY NORMAL AFTER START. RAN ALL 3 ENGINES PER JRH AND POWERED ALL 3 BUSSES WITH NORMAL RESULTS D/C SYSTEM CHECKS NORMAL. 2 L 7 3 4F RT A22WE 20080929 EU 2008 9 29 08FDEA03404 1 20080813 A 5753 SKIN AIRBUS 300 A300F4605R 3930327 EU LT WING TE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 LEFT WING INBD FLAP T/E UPPER SURFACE EXTERNAL SKIN IS GOUGED IN TWO PLACES. BLENDED GOUGE SMOOTH IAW A300-600 SRM 51-7 3-10. GOUGED INBD FLAP UPPER SKIN FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 57-50-00; PG 108. FABBED REPAIR AND INSTA LLED BOTH IAW A300-600 SRM 57-50-00; PGS 220 - 226. 2 L 7 2 4F RT A35EU 20080929 NM 2008 9 29 08FDEA03406 1 20080813 A 5720 65166383 ANGLE BOEING 727 7272S2F 1384O81 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 LEFT WING OB LE CAVITY, LE UPPER SKIN FORMED SUPPORT ANGLE CRACKED AT AFT END ABOVE TAI DUCT AT INBD END OF NR 4 SLAT WE LL. REMOVED INTERCOSTAL AND DAMAGED SUPPORT ANGLE, FABRICATED NEW SUPPORT ANGLE, HEAT TREAT "T-3". TREAT AND PRIMED SU PPORT ANGLE, INSTALLED SUPPORT ANGLE AND INTERCOSTAL REF SRM 51-10-2, 51-30-2 P 2 AND 32, MM 51-20-151-7 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080929 NM 2008 9 29 08FDEA03407 1 20080813 A 5720 6521655 ANGLE BOEING 727 7272S2F 1384O81 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 LT WING ROOT TE UPPER PNL IB OF NR 7 SPOILER HAS FRETTED/CRACKED IB SUPPORT ANGLE BS 950A, WBL 70. REPLACED SUPPORT ANG LES REF SRM 51-30-02 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080929 EU 2008 9 29 08FDEA03409 1 20080813 A 3411 MS21902D5 PITOT LINE AIRBUS 300 A300F4605R 3930327 EU ZONE 100 LEAKING A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 650FE 726 STAND-BY PITOT SYSTEM FAILS THE LEAK TEST. TROUBLE SHOOT SYSTEM IAW AMM 34-10-00. FOUND DAMAGED UNION AT THE STANDBY PITOT TUBE. REMOVED AND REPLACED THE UNION IAW 34-11-15-4. TESTED AND LEAK CHECKED THE STANDBY PITOT SYSTEM IAW AMM 34-10-00-5. NO LEAKS DETECTED. 2 L 7 2 4F RT A35EU 20080929 NM 2008 9 29 08FDEA03523 1 20080820 A 5320 6517510120 WEB BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 RIGHT LOWER TORQUE BOX INBD WEB IS CRACKED WITH A STOP DRILL AT LIGHTNING HOLE BS 1223. HFEC CRACK TO VERIFY TERMINATIO N IAW NDTM PT6 51-00-00 FIG 23. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. INSTALLED REPAIR DO UBLER IAW SRM 51-40-2 FIG 1. 2 L 7 3 4F RT A3WE 20080929 NM 2008 9 29 08FDEA03525 1 20080820 A 5330 655458312 SKIN BOEING 727 727233 138408A NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 SKIN DENTED RIGHT AFT FUSELAGE FROM C-3 DOOR CUTOUT STA 1148 TO STA 1183 STR 20R. CUT OUT DAMAGED SKIN, FABRICATED RE PAIR FILLER USING 2024-T3 .100 PO NR 8221343 DIMS 42 7/8 INCH BY 12 INCH, DOUBLER, TRIPLER. INSTALLED REPAIR PARTS IAW EA 7-5330-117015 - FUSELAGE SKIN CREASE BELOW STR 20R LAP SPLICE BS 1140-1183, REPAIR. 2 L 7 3 4F RT A3WE 20080929 NM 2008 9 29 08FDEA03312 1 20080808 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 587FE 48489 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK INDICATIONS AT HOLES A, C AND D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FABRICATED AS PER FEDEX EA NR 1 -5300-122409A. SUPPORT FITTING NR 4 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR BUSHING FABRICATED AND INSTALLED ON MAIN CARGO DOOR LOWER JAMB WEB AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GM M 6-2-100. 2 L 7 3 4F RT A22WE 20080929 NM 2008 9 29 08FDEA03187 1 20080730 A 5347 AEA732515 SEAT TRACK DOUG MD11 MD11F 3023600 NM BS 1531 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 MAIN DECK SEAT TRACK AT STA 1531, X = -75.5 FOUND CORROSION. MAIN DECK SEAT TRACK AT STA 1531, X = -75.5 CORROSION REMO VED AS PER SRM 51-21-01 VOLUME II. ORIGINAL MATERIAL THICKNESS = 0.100", REMAINING THICKNESS = 0.096 INCH, MATERIAL REM OVED = 0.004 INCH AND FOUND WITH LIMIT AS PER SRM 53-70-00 FIGURE 3 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-10 0. 2 L 7 3 4F RT A22WE 20080929 NM 2008 9 29 08FDEA03192 1 20080731 A 5330 6518420496 SKIN BOEING 727 727233 138408A NM BS 334 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 275FE 22040 EXISTING TOOL MARKS ON SKIN AT FUSELAGE STA 334 BY UNDER HAT SECTION AREA OF STR 10R. BLENDED OUT DAMAGE IAW SRM 51-10- 1, AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG 1 AND 2. REPAIRED SKIN IAW EA 7-5330-122358-FUSELAGE, AD 2002-07-09 AND AD 98-11-03-65-18420-6 SKIN DRILL MARK REPAIR AT BS 341 STR 10R LAP JOINT EO 7-5330-7-5000; SB 727-53A0222-EO 7-5100-7-4 304. 2 L 7 3 4F RT A3WE 20080929 EU 2008 9 29 08FDEA03195 1 20080731 A 5310 A5211122552020 DOOR FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 THE AVIONICS COMPARTMENT DOOR HINGE FRAME IS CRACKED THROUGH, DOOR 121B, RIGHT HINGE. REMOVED AVIONICS COMPARTMENT DOOR TO FACILITATE THE REPAIR IAW AMM 52-41-14-4. REPAIRED THE CRACKED ANGLE IAW SRM 51-41-14; FIG 201. REMOVED AND REPLA CED BRAKE FORM SECTION P/N A5211074420100, PO NR 628155.1 IAW SRM 51-40-21. REINSTALLED AVIONICS COMPARTMENT DOOR IAW A MM 52-41-14-4. DOOR WARNING SYSTEM TEST "GOOD" REF AMM 52-41-14-5. 2 L 7 2 4F RT A35EU 20080929 EU 2008 9 29 08FDEA03196 1 20080731 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO SEAT TRACK IS CHAFFED AT FRAME 78; BL "0". REMOVED CORROSION; BLENDOUT IS WITHIN LIMITS PER SRM 53-10-16. TREATED, PRIMED AND PAINTED AREA PER SRM 51-23-10. 2 L 7 2 4F RT A35EU 20080930 WP 2008 9 30 UPS08853157 1 20080729 A 5753 SKIN DOUG DC8 DC871F 302199D WP LT WING TE FLAP WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 2 WORN AREAS EITHER SIDE OF O/B FLAP STA 340 LT FLAP. FABRICATED AND INSTALLED REPAIR DOUBLER ON O/B SIDE OF STA 340 IAW SRM 57-07-01 AND 51,1-21A. 2 L 7 4 4F RT 4A25 20080925 EU 2008 9 25 08FDEA03975 1 20080922 A 5710 A57111092202 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND DAMAGED HOLES DURING ACCOMPLISHMENT OF SB A300-57-6049 (HOLE N, Y, U) ON VERTICAL FLANGE, C 47, LHS. REPAIR PERFO RMED BY OVERSIZING THE HOLES OF EXTERNAL FITTING AND INSTALL A CONICAL WASHER AT HOLE U IAW RAS/70512903/024/2008 ISS A, APPROVED BY EA 6-5710-123133. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03976 1 20080922 A 5710 A57110533207 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND DAMAGED HOLES DURING ACCOMPLISHMENT OF SB A300-57-6049 (HOLE I, L, N, U) ON VERTICAL FLANGE, C 47, RHS. REPAIR PE RFORMED BY OVERSIZING THE HOLES, EXTERNAL FITTING CUT OUT AT HOLE I AND NDT FOR DAMAGE FREE CONDITION IAW RAS/70512903/0 24/2008 ISS A, APPROVED BY EA 6-5710-123133. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03977 1 20080922 A 5710 A57111092202 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND DAMAGED HOLES DURING ACCOMPLISHMENT OF SB A300-57-6086 (HOLE E, F, P) ON HORIZONTAL FLANGE, C 47, LT. REPAIR PERF ORMED BY OVERSIZING THE HOLES AND NDT FOR DAMAGE FREE CONDITION IAW RAS/70512903/024/2008 ISS A, APPROVED BY EA 6-5710-1 23133. 2 L 7 2 4F RT A35EU 20080925 WP 2008 9 25 08FDEA03980 1 20080922 A 5347 NEA60225 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 MAIN CARGO DECK SEAT TRACK HAS CORROSION BETWEEN STA 1151 AND 1173, LBL 27. REMOVED DAMAGED SECTION OF SEAT TRACK. FAB RICATED A REPAIR SECTION; SPLICE & SPLICE PLATE AND INSTALLED IAW SRM 51-21-01. REMOVED & RE-INSTALLED FLOOR BOARDS I NBD AND OUTBD OF LBL 27 BS 1099-1239 IAW SRM 51-31-01. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03981 1 20080922 A 5347 NDA60225 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 MAIN CARGO SEAT TRACK HAS CORROSION BETWEEN STA 994 AND 1010, LBL 27. REMOVED CORROSION AND FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM 53-70-00. LOCATED & DRILLED FOR CHANNEL IAW SRM 53-70-00. REMOVED FLOOR PANEL IAW AMM 53-21-01-8. I NSTALLED CHANNEL STRAP IAW SRM 53-70-00. INSTALLED FLOOR PANEL IAW AMM 53-21-01-8. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03983 1 20080922 A 5347 S4929148 SEAT TRACK DOUG MD10 MD1010F 3022112 WP BS 1480-1540 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION BETWEEN STA 1480 AND 1540, LBL 107. REMOVED CORROSION AND FOUND T O BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED DAMAGED SEAT TRACK IAW SRM 51-31-01. REPAIRED SEAT TRACK IAW SRM 53-70-00 . ALODINED & PRIMED IAW SRM 51-21-01. REMOVED & RE-INSTALLED FLOOR PANEL IAW AMM 53-21-02-2. REMOVED & RE-INSTALLED A IR GRILLS IAW AMM 53-23-02-2. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 DL757081120 1 20080826 A 5330 SKIN BOEING 757 757232 1384965 NM L1 CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 636DL 23763 THE FUSELAGE SKIN WAS FOUND CRACKED AT THE UPPER FORWARD CORNER OF THE L1 DOOR CUTOUT. DAMAGE CUTOUT MEASURED 1.35 INCH WIDE BY 3 INCH LONG. AREA WAS INSPECTED AND NO ADDITIONAL CRACKS WERE FOUND. A REPAIR DOUBLER AND TRIPLER WERE INSTAL LED. 2 L 7 2 4F RT A2NM 20080926 NM 2008 9 26 2008UALA05787 1 20080918 A 3350 60243 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 541UA 25253 EMERGENCY EXIT LIGHTS ARE DIM ON THE FLOOR IN FIRST CLASS. REPLACED LIGHT AT MID GALLEY. 2 L 7 2 4F 4 F RT A2NM E17NE 20080926 EU 2008 9 26 08FDEA03637 1 20080829 A 3231 A5281062500052 DOOR AIRBUS 310 A310222 3930315 EU NLG OUT OF SEQUENCE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 THERE ARE TIRE ROTATION MARKS ON THE INNER SURFACE OF BOTH NLG MAIN DOORS. SUSPECT NLG DOORS ARE OUT OF SEQUENCE. GEAR RETRACTION REQUIRED FOR FINAL SIGN OFF. TIRE ROTATION MARKS REMOVED DURING ACFT WHEEL WELL / LANDING GEAR WASH REF WOR K CARD 40C0002. PERFORMED NLG & MLG RETRACTION TEST REF AMM 32-31-00, NO DISCREPANCIES NOTED. PERFORMED FREE FALL TE ST REF AMM 32-33-00, NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 08FDEA03498 1 20080819 A 5320 6525550 SUPPORT ANGLE BOEING 727 7272S2F 1384O81 NM FAIRING SUPPORT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 RT WHEEL WELL, LOWER FUSELAGE FAIRING SUPPORT FRAME HAS CORROSION, RBL 21, STA 950 FABRICATED TEE ANGLE FROM RT WHEEL WE LL FUSELAGE FAIRING SUPPORT STA 950 REFB DWR 65-25550 AND CUSTOMER REQUEST, HEAT TREATED TRACKING NUMBER 2008-08-057. T REATED AND PRIMED, REF SRM 51-10-2 PG 1-7. INSTALLED REF SRM 51-30-2 PG 2,4-13. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20080926 NM 2008 9 26 08FDEA03499 1 20080819 A 5347 651960216 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 HOLE WITH ZERO EDGE DISTANCE DRILLED IN SEAT TRACK FLANGE STA 990 RBL45. FABRICATED NEW SEAT TRACK SECTIONS. FABRICATE D REPAIR ANGLE SPLICES 4 EACH AND INSTALLED NEW SEAT TRACK SECTIONS AT BS 950-1020 RBL 45 IAW SRM 53-10-5 FIG 1 AND SRM 53-10-2 FIG 7. 2 L 7 3 4F RT A3WE 20080926 NM 2008 9 26 08FDEA03500 1 20080819 A 5340 651842040 STRINGER CLIP BOEING 727 727233 138408A NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 STA 355 STR 7R STRINGER CLIP DAMAGED. FABRICATED NEW STRINGER, 2 NEW ANGLES AND NEW EXTRUSION IAW SRM 53-10-3 FIG 2. INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG 2 AND SRM 53-10-2 FIG 9. 2 L 7 3 4F RT A3WE 20080926 NM 2008 9 26 08FDEA03501 1 20080819 A 5347 65236383 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 MAIN CABIN SEAT TRACK BS 520 BL0 HAS CORROSION. FABRICATED NEW SEAT TRACK SECTION. INSTALLED NEW SEAT TRACK SECTION US ING PREVIOUS GOOD SPLICES IAW SRM 53-10-5 FIG 1 AND SRM 53-10-2 FIG 7. 2 L 7 3 4F RT A3WE 20080926 NM 2008 9 26 08FDEA03356 1 20080810 A 5315 65208281 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 SURFACE CORROSION STA 720D RBL 12 TOP OF FLOORBEAM. REMOVED CORROSION IAW SRM 51-10-6, FOUND CORROSION OUT OF LIMITS IA W SRM 53-10-1 FIG 4, CUTOUT DAMAGED AREA IAW SRM 53-10-8 FIG 3, FABRICATED UPPER CHORD, 2 SUPPORT ANGLES AND 2 REINFORCE MENT STRAPS IAW SRM 53-10-8. ALODINED AND PRIMED PARTS IAW SRM 51-10-2 AND INSTALLED PARTS IAW SRM 53-10-8 FIG 3. 2 L 7 3 4F RT A3WE 20080926 EU 2008 9 26 08FDEA03892 1 20080916 A 5340 A53810771201 ATTACH FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CHAFING MARKS AT REAR MLG DOOR ACTUATOR FITTING OUT OF LIMIT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51- 72-10. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03260 1 20080805 A 5347 A53612518200 SEAT TRACK AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSION ON SEAT TRACK C14-15A, Y 450 OUT OF LIMIT. SEAT TRACK REPAIRED IAW SRM 53-12-16 FIG 201. 2 L 7 2 4F RT A35EU 20080930 NM 2008 9 30 UPS08M53147 1 20080812 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 17 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080930 NM 2008 9 30 UPS08M53154 1 20080811 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 5 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080930 NM 2008 9 30 CALA0800807 1 20080822 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM BS 400 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 BODY STATION 400 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN S8L AND S9L. REMOVED CRACK, FABRICATE D AND INSTALLED REPAIR ANGLES PER EA 5310-04498 ON FRAME STATION 400 LEFT SIDE BETWEEN STR 8 LT AND STR 9 LT. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800814 1 20080822 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM BS 400 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 BODY STATION 400 RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REPAIRED CRACKED FRAME AT STATION 400 RIGHT SIDE AT (AC) BRACKET BETWEEN STR 8 AND 9 PER EA5310-04498. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800815 1 20080822 A 5311 6546525 FRAME BOEING 737 737524 1384721 NM BS 380 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 BODY STATION 380 RIGHT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STR 8 AND 9. REPAIRED CRACKED FRAME AT STATION 380 RIGHT SIDE AT AC BRACKET BETWEEN STR 8 AND 9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 2008UALA04199 1 20080809 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 803UA 748 FUSELAGE DENT FWD OF FR 22 STR 24L. MAJOR REPAIR ACCOMPLISHED: REMOVED ADJACENT DOUBLER REPAIR. CUT OUT EXISTING DAMA GE. FABRICATED & INSTALLED EXTERNAL DOUBLER INCORPORATING ADJACENT REPAIR & CURRENT DENT CUTOUT. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA04226 1 20080811 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 EMERGENCY LIGHT ROW 44LT INOP. RELAMPED, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04346 1 20080820 A 3350 767 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 562UA 26664 DOOR 1L EXTERIOR EMERGENCY LIGHT IS INOP. RELAMPED EXTERIOR EMERGENCY LIGHT AT DOOR 1L. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20080930 NM 2008 9 30 2008UALA04347 1 20080819 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 566UA 26670 EXTERIOR EMERGENCY LIGHT INOP AT DOOR 3R. 2 L 7 2 4F 4 F RT A2NM E17NE 20080930 NM 2008 9 30 2008UALA05433 1 20080823 A 3350 362624 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 FWD GALLEY CROSS AISLE EMERGENCY LIGHT INOP. REPLACED CROSS AISLE EMERGENCY LIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA04211 1 20080809 A 2611 233N610315 PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE DETECTION FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 531UA 25042 LEFT ENGINE NR 2 SQUIB DOES NOT TEST PROPERLY. SHORT IN SQUIB TEST PANEL. REPLACED SQUIB TEST PANEL, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20080930 NM 2008 9 30 UPS08553232 1 20080807 A 5320 SUPPORT BOEING 757 75724APF 1384969 NM BS 620-825 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 453UP 25474 INSPECTION TYPE:C CORROSION ON RIGHT FLOOR TO SIDEWALL PLATE IN THE FORWARD CARGO BAY, BS 620-825, RBL 22, WL 156. BLEN DED CORROSION, BLEND AT BS 700 OUT OF LIMITS, REPAIRED YAW SRM 51-70-13-0G. 2 L 7 2 4F RT A2NM 20080930 NM 2008 9 30 UPS08553233 1 20080821 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM BS 900 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 BS 900 BL 0 RBL 25 WL 208 FLOOR SUPPORT UPPER COVER BROKEN. FABRICATED & REPLACED IAW SRM 51-20-01 5 3-01-60. 2 L 7 2 4F RT A2NM 20080930 WP 2008 9 30 UPS08853234 1 20080728 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 781 L15R DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C1 MAIN CABIN DOUBLE DRILLED HOLE IN BELTFRAME STA 781L-15R. FABBED AND INSTALLED REPAIR DOUBLER IAW SR M 51-1-8, 53-2-0. 2 L 7 4 4F RT 4A25 20081001 NM 2008 10 1 2008UALA05872 1 20080923 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 AFT PIT STA 1600 FRAME DENTED AT STR 22L TO 23L. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF FRAME AND INSTA LLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080926 EU 2008 9 26 08FDEA03894 1 20080916 A 5320 SILL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND OLD REPAIR WITH SOME MISSING FASTENER ON AFT CARGO DOOR SILL BEAM WITHOUT OLD RECORD AVAILABLE. REPAIR WAS PERF ORMED IAW SRM 53-17-18 PB 201 PARA 10 , MISSING FASTENER INSTALLED, NDT FOR CRACK FREE CONDITION PERFORMED, APPROVED BY RAS/EFW/9000103/2008 ISS A AND EA 6-5317-123135.. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03895 1 20080916 A 5730 A57340087 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND ELONGATED HOLES ON LT WING BOTTOM SKIN AND PYLON SUPPORT BRACKET. REPAIR PERFORMED BY DRAWING R571-50532 (OVERSIZ ING THE HOLES INSTALL FREEZE PLUGS), APRROVED BY RAS/BAE/10078756/2008 ISS A AND EA 6-2900-123069. 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 08FDEA03508 1 20080819 A 5320 SILL BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 L1 DOOR SILL FACE HAS LIGHT CORROSION IN SEVERAL AREAS. MINOR CORROSION BLENDED OUT AND AREA TREATED, FOUND WITHIN ALLO WABLE LIMITS IAW SRM 53-00-01 REV 93, DETAIL II FIG 101. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20080926 EU 2008 9 26 08FDEA03509 1 20080820 A 5347 A25775051207 TRACK AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 ROLLER TRACK IN AFT CARGO COMPARTMENT,C 56-58, Y -1470 WAS DAMAGED. REPAIR SOLUTION IAW SRM 53-10-15 WAS NOT APPLICAB LE DUE TO EXISTING SHEAR PLATES BETWEEN C 57-57.3 ROLLER TRACK REPAIR WAS PERFORMED IAW RAS/EFW/9000085/2008 ISS A, AP PROVED BY EA 6-5316-123068. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03510 1 20080820 A 5720 A57260300006 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 743FD 630 FOUND CORROSION UNDER STATIC DISCHARGER ON RT WING TIP. REPAIR PERFORMED BY CORROSION REWORK AND INSTALLING AN EXTERNAL PATCH IAW RAS/FOK/160/2008 ISS A, APPROVED BY EA 6-5730-120085. 2 L 7 2 4F RT A35EU 20080929 NM 2008 9 29 UPS08553316 1 20080816 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM BS 1720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 CORROSION ON UPPER SURFACE OF FLOOR SUPPORT AT STA 1720 RBL 4. REPAIRED OUT OF LIMITS. CORROSION BL END PER EO B757-5310-30513A WITH DOUBLER, TRIPLERS AND FILLERS. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 2008UALA05707 1 20080913 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT LIGHT INOP AT DOOR 2 LEFT FWD AND AFT SILL LIGHTS. FOUND BATTERY INOP. REPLACED BATTERY, OPS CHECKS NOR MAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 NM 2008 9 29 2008UALA05822 1 20080920 A 5210 FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 DOOR 4L LWR FWD LOCKING CRACK FITTING CORRODED BEYOND LIMITS. REPLACED THE CRANK FITTING. REPLACED THE CRANK FITTING. 2 L 7 2 4F 4 F RT A2NM E17NE 20081008 NM 2008 10 8 KCS2008F00018 1 20080912 A 5313 STRINGER BOEING 747 747249F 1384849 NM BS 990 S46L CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 STRINGER 46-L CORRODED AT STA-990. (K) 2 L 7 4 4F RT A20WE 20081008 EU 2008 10 8 NSV2008F00023 1 20080903 A 5300 STRUCTURE SAAB SF340 340B 7860101 EU VIBRATION A NSVA O OTHER E VIBRATION/BUFFET CL CLIMB 1 EA 27 193CJ 340B193 AIRPLANE SHAKES DURING CLIMBOUT AT SLOW SPEED AND DURING APPROACH. CAPTAINS CONTROL COLUMN SHAKES. MOVES APPROXIMATELY 3 INCHES. VIBRATION DIMINISHES SOME IN CRUISE FLIGHT. VIBRATION STOPPED COMPLETELY WHEN FLAPS SELECTED TO 15 DEG ON A PPROACH. 2 L 7 2 4T RT A52EU 20081008 NM 2008 10 8 AALA200802061 1 20080809 A 3350 LENS BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AM 24491 DFW EMERGENCY LIGHT LENS AT OVERHEAD SEAT 17A LOOSE. SECURED LENS FOR EMERGENCY LIGHT AT OVERHEAD SEAT 17A. SYSTEM GRO UND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 NM 2008 10 8 2008UALA05701 1 20080913 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT LIGHT INOP AT DOOR 5 RIGHT FWD SILL LIGHT. LAMP INOP. REPLACED LAMP. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081008 NM 2008 10 8 AALA200802140 1 20080819 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 948AN 30086 DFW EMERGENCY LIGHT AT SEAT ROW 17 INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 17. SYSTEM GRO UND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 AALA200802160 1 20080821 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 JFK EMERGENCY LIGHTS AT RT SEAT ROWS 30 TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK M33401 FOR EMERGENCY LIGHTS AT RT SEAT ROW 30 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802164 1 20080822 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 662AA 25296 DFW EMERGENCY LIGHTS AT AFT SEAT ROW 3 BULLNOSE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT SEAT ROW 3. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 NM 2008 10 8 AALA200802175 1 20080823 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 772AN 29580 JFK EMERGENCY LIGHT AT SEAT 21G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 WP 2008 10 8 08FDEA03622 1 20080828 A 5730 ARB11113 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING OUTBD TRAILING EDGE PANEL 525 AT INNER SKIN IS CRACKED. CRACKED SKIN ON THE LEADING EDGE OF PANEL 525 AT REQUI RES AN SRM DOUBLER. FABRICATED THE DOUBLER IAW SRM 57-10-00 VOL I. INSTALLED DOUBLER IAW SRM 51-31-01 VOL II & SRM 57-1 0-00 VOL I. APPLIED PRIMER ON THE DOUBLER IAW SRM 51-21-01 VOL II. 2 L 7 3 4F RT A22WE 20081008 NM 2008 10 8 KCSA081472 1 20080917 A 5311 FRAME BOEING 747 747122 1384872 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FRAME AT STA 2716.6 CRACKED BEYOND PREVIOUS STOP DRILL RBL 24 W/L 314 ON APU SUPPORT BEAM. 2 L 7 4 4F RT A20WE 20081008 NM 2008 10 8 USAA920081695 1 20080902 A 5311 65C22909 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03C20853011/005 FRAME CRACKED AT BS500C BETWEEN S20R & S21R. REPAIRED FRAME AT BS500C BETWEEN S2 0R & S21R IAW B737 SRM 51-70-11. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 USAA920081696 1 20080902 A 5311 65C22908 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03C20853011/004 FRAME CRACKED AT BS500B BETWEEN S20R & S21R. REPAIRED FRAME AT BS500B BETWEEN S2 0R & S21R IAW B737 SRM 51-70-11 & BOEING DRAWING NR 65-3550-1. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 USAA920081697 1 20080916 A 5311 65C22910 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03C20853011/003 FRAME CRACKED AT BS500D BETWEEN S20L & S21L. REPAIRED FRAME AT BS500D BETWEEN S2 0L & S21L IAW B737 SRM 51-70-11. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 USAASB08083 1 20080915 A 2497 WIRE BOEING 737 7373B7 1384580 NM APU GENERATOR LOOSE A USAA O OTHER H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 531AU 24478 PIT FLT1174 FLIGHT DEPARTED CLT WITH THE NR 2 CSD ON MEL AND THE RT BUS BEING POWERED BY THE APU. ON CLIMB OUT, CREW RE PORTED THE RT BUS DROPPING OFF LINE INTERMITTENTLY. OCCURRED 2 MORE TIMES ON LEVEL OUT. CREW WAS ABLE TO REINSTATE EAC H TIME BY CYCLING APU GENERATOR SWITCH. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT PIT. MX FOUND A LOOSE WIRE CONNECTION ON APU GENERATOR. SECURED WIRE. COULD NOT DUPLICATE BUS DROPPING OFF LINE. OPS CHECK GOOD. CLEARED M EL ON NR 2 CSD WITH THE REPLACEMENT OF THE NR 2 CSD. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 USAA920081687 1 20080816 A 5230 6547952183X SKIN BOEING 737 7374B7 1384702 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 451UW 24934 CLT RON MAJOR REPAIR LOG NR 4393062 AFT CARGO DOOR SKIN CRACKED AT AFT END OF HANDLE CUTOUT. REPAIRED AFT CARGO DOOR SK IN AT AFT END OF HANDLE CUTOUT IAW US AIRWAYS EA NR 111648. 2 L 7 2 4F RT A16WE 20081008 EU 2008 10 8 AALA200802129 1 20080818 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 8067A 510 JFK EMERGENCY LIGHT AT SEAT 7C BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 7C. SYSTEM GROUND CHECKED N ORMAL OPS. 2 L 7 2 4F RT A35EU 20081008 EU 2008 10 8 AALA200802128 1 20080818 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 8067A 510 JFK EMERGENCY LIGHT AT SEAT 13C BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 13C. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A35EU 20081008 EU 2008 10 8 08FDEA03818 1 20080911 A 5534 A5537244621200 STIFFENER AIRBUS 310 A310222 3930315 EU ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 REAR STIFFENER BETWEEN THE TRAILING EDGE OF RIB 7 & THE RIB ON THE RIGHT SIDE OF THE VERTICAL STAB IS CRACKED. REMOVED & REPLACED STIFFENER IAW SRM 51-40-21 & 51-72-10. 2 L 7 2 4F RT A35EU 20081008 EA 2008 10 8 TRAX200801124 1 20080906 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 PAX DOOR HANDLE INSIDE VERY HARD TO OPEN. RAN OPS TEST ON PAX DOOR IAW AMM 52-11-21-710-801. OPS CK GOOD. NO DEFECTS NOTED. A/C OK FOR SVC AT THIS TIME. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801097 1 20080903 A 5534 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 CRACKED DRAG ANGLE RT LOWER VERT STAB. MARKED. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801111 1 20080904 A 2750 ECU CNDAIR CL600 CL6002B19 1900309 EA E&E BAY LOOSE A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 860AS 7433 FLAP FAILURE CAUTION MSG ON 4 MILE FINAL. FLAPS FAILED AT 30`. VERIFIED ON SYNOPTIC PAGE. EMERGENCY VEHICLES ROLLED A S A PRECAUTION. T/S SYSTEM FOUND FECU LOOSE IN RACK. PERFORMED FECU TEST AFTER TIGHTENING KNOBS. IAW AMM 27-51-05 PG 501-504. SYSTEM OP CHECKED OK. A/C OK FOR SERVICE. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801118 1 20080905 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 980EV 7759 JOB 8775921 OPERATION 165 FOUND INBD AND OTBD CLIP ANGLES AT FS 280 AND RBL 9 TO BE CRACKED. SUP 9/11/08 - REMOVED INBD AND OTBD CLIPS AT FS 280 RBL 9 IAW CRJ 200, SRM 51-42-06 AND 51-42-21. INBD AND OTBD CLIPS REQUIRE INSTALL. INSTALLED NEW INBD ANGLE IAW CRJ 200 SRM 51-42-06 AND 51-42-21. RBL 9 FS 280.00. REPLACED OTBD SLIP ANGLE FS 280.00, RBL 9 9AW, C RJ 200 SRM 51-42-06 AND 51-42-21.(K) 2 L 7 2 4F RT A21EA 20081008 WP 2008 10 8 WRLA2008074 1 20080909 A 5330 SKIN DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 303WL 46917 DURING INSPECTION FOUND CORROSION RT MLG WW. STA 1505 AT LONGERON 35R SKIN, INTERCOSTAL AND FRAME ATTACH. REF DELTA NR 41. 2 L 7 3 4F 4 F RT A22WE E23EA 20081008 EU 2008 10 8 MAL2008F00034 1 20080907 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU COCKPIT ODOR A MALA B EMER. DESCENT J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 402XJ 340B402 ON OVERHEAD PANEL, THE L PITOT LIGHT ILLUMINATED INFLIGHT WITH AN ELECTRICAL BURNING SMELL ASSOCIATED. RAN THE QRH AND SMELL PERSISTED. DIVERTED TO FARGO AND EMERGENCY DECLARED. DISCONNECTED BATTS AND CIRCUIT BREAKER J27 PULLED. R&R THE LT CURRENT SENSOR PN OFF QR50V SN OFF C1-94907. SN ON QR50V, SN ON CP-85534 IAW WITH THE SAAB 340 AMM 30-30-00-05. DU RING OPS CHECKS NO SMOKE OR BURNING SMELL NOTED. RETURNED ACFT TO SERVICE FOR WORK PERFORMED. CONNECTED BOTH BATTERIES . 2 L 7 2 4T RT A52EU 20081001 NM 2008 10 1 SWAA085216 1 20080925 A 3397 WIRE BOEING 737 7377H4 1384404 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 242WN 32505 FOUND EMERGENCY EXIT FLOOR TRACK LIGHT INOP. RECONNECTED WIRES PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085211 1 20080923 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED SPV CHECK, FOUND L1 ENTRY DOOR LOWER HINGE SKIN CRACKED AT FASTENER HOLES. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085210 1 20080923 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 490WN 32476 DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST AT ROW 16 ABC. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085208 1 20080923 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 490WN 32476 DURING SCHEDULED HC2 CHECK, FOUND AFT LT AND RT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081001 WP 2008 10 1 08FDEA04119 1 20080929 A 5753 ARC01541 HINGE DOUG MD10 MD1010F 3022112 WP LT WING TE FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 LEFT WING INBD FLAP OUTBD HINGE FWD HALF OUTBD FACE LOWER EDGE HAS WEAR MARKS IN 5 SPOTS JUST INBD OF THE NUTPLATES. RE MOVED HINGE FAIRING IAW SRM 51-31-01. BLENDED WORN AREAS, FOUND TO REQUIRE REPAIR IAW SRM 51-44-07. BLEND AREA IS 0.06 5. FABRICATED REPLACEMENT CLIPS & SHIMS IAW SRM 57-20-00. ALODINED, PRIMER & PAINTED REPAIR PARTS & BLENDED AREAS IAW SRM 51-21-10. INSTALLED ANGLES IAW SRM 57-20-00. RE-INSTALLED HINGE FAIRING IAW SRM. 2 L 7 3 4F RT A22WE 20081001 WP 2008 10 1 08FDEA04121 1 20080929 A 5711 ARB06342 SPAR DOUG MD10 MD1010F 3022112 WP RT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 RIGHT WING INBD T/E AT THE MAIN LANDING GEAR SUPPORT, LOWER FWD AUX SPAR SPLICE HAS CORROSION. REPLACED SPLICES IAW DWG ARB 0621 AT THE RIGHT WING INBD TRAILING EDGE AT THE MLG LOWER FWD & AFT SPAR SPLICES. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 SWAA085207 1 20080923 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM COCKPIT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 490WN 32476 DURING SCHEDULED HC2 CHECK, FOUND LT FWD EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTER Y PACK PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085206 1 20080923 A 5512 6573782 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 490WN 32476 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZ STAB AFT OF LEADING EDGE SKIN CRACKED AT BS 147.90. REPAIRED CRACK PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085197 1 20080924 A 5313 BAC1498 STINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 354, STR 25R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085196 1 20080905 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 867, STR 26L. REPAIRED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 UPS08B53409 1 20080801 A 5320 65B09631612 TENSION TIE BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 579UP 26062 INSPECTION TYPE:BCF STA 1180 TENSION TIE LT AFT CHANNEL 6EA FASTENER HOLE CRACK ABOUT OR MORE THAN 0.030 INCH. REPLACED CRACKED TENSION TIE AS PER DWG 65B09631 & SRM 51-40-02. 2 L 7 4 4F RT A20WE 20081001 NM 2008 10 1 UPS08553395 1 20080922 A 5311 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 424UP 25369 INSPECTION TYPE:C2 DENT IN FRAME AT BS 660 BETWEEN 522-23R IS MORE THAN THE MAXIMUM ACCEPTABLE MANUFACTURE'S LIMITS. RE MOVED DAMAGED SECTION AND REPAIRED FRAME PER SRM 51-70-11-0G. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 UPS08553394 1 20080916 A 5320 SUPPORT ANGLE BOEING 757 75724APF 1384969 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 424UP 25369 INSPECTION TYPE:C2 AFT CARGO COMPARTMENT BS 1640 WL 200 LBL 20 AFT BULKHEAD SUPPORT ANGLE CRACKED. REMOVED CRACKED SUPP ORT ANGLE, FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-30-01-0G, SRM 51-40-05-0G, SRM 51-40-02-0G, DWG 453N1804. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 UPS08553393 1 20080916 A 5320 SUPPORT BOEING 757 75724APF 1384969 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 424UP 25369 INSPECTION TYPE:C2 FWD CARGO BAY, AFT BULKHEAD SUPPORT IS CRACKED AT BS 845, RBL 51 WL 174. REMOVED AND REPLACED SUPPOR T IAW SRM 51-40-02-0G. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 UPS08553384 1 20080926 A 5610 SLIDING WINDOW BOEING 757 75724APF 1384969 NM COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 467UP 25483 INSPECTION TYPE:N/A L2 SLIDING WINDOW DELAM/CRACKING, MOISTURE INTRUSION. OUT OF LIMITS. REMOVED WINDOW UP TO STEP 10 AMM 56-11-02-4. INSTALLED L2 WINDOW PER MM 56-11-02-4. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 CALA0800924 1 20080928 A 3350 ADD71701100 BATTERY PACK BOEING 737 737924 13848A1 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 75410 30127 R-2 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER AMM 33-51-06-960-805, OPS CHE CK GOOD. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 CALA0800921 1 20080926 A 5512 6573782 SKIN BOEING 737 7373T0 1384582 NM HORIZ STAB GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 02/21/2008, LEFT HORIZONTAL STABILIZER STATION 108 16 INCHES AFT OF LEADING EDGE PANEL APPROXIMATELY 8.5" X 2.5" X .300 DEPTH. COMPLETED INTERIM REPAIR OF LEFT HORIZONTAL STABILIZER PER SRM 55-10-01 REPAIR 4, ISSUED DIP TO INSPECT FASTENER S EVERY 3,000 FLT HRS AND INSTALL SOLID FASTENERS WITHIN 15,000 FLT CYC'S AFTER BLIND FASTENERS INSTALLED. 09/26/2008, REMOVED DAMAGE AND INSTALLED PERMANENT REPAIR PER SRM 55-10-01, REPAIR 7. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085230 1 20080925 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 344, STR 22R TO 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085225 1 20080924 A 2560 65C34691 GIRT BAR BOEING 737 7373H4 1384600 NM EVAC SLIDE OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 DURING SCHEDULED C2 CHECK, FOUND L2 SLIDE DOOR GIRT BAR OUT OF ADJUST. ADJUSTED GIRT BAR PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085224 1 20080925 A 3397 WIRE BOEING 737 7377H4 1384404 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 242WN 32505 FOUND FIRST EMERGENCY EXIT FLOOR TRACK LIGHT INOP. RECONNECTED WIRES PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085219 1 20080924 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED MV2 CHECK, FOUND STRINGER CRACKED AT BS 500B + 2.4, STR 10R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085218 1 20080925 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND R1 L-ANGLE STRINGER FWD OF GALLEY SERVICE DOOR CRACKED AT BS 294.5, STRINGER 17R. REM OVED AND REPLACED ANGLE PER SRM. 2 L 7 2 4F RT A16WE 20081001 2008 10 1 ASAA0853530 4 20080921 A 3160 1741010201 CDU BOEING 737 737890 1384527 NM COCKPIT FAULTY A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 559AS 7944 35178 FIRST OFFICER MCDU TACTILE FEEDBACK ON LINE SELECT KEYS 1L 2L 5L 6L AND 6R IS INOP. VERFIED PROBLEM. REPLACED F/O'S FM S MCDU PART VERIFIED. ALSO REF MM 34 61 01 000 802 & 400 802 FOR REMOVE AND REPLACE & GND VERIFICATION TEST. OPS NML. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 ASAA0853531 1 20080925 A 2421 761574B IDG BOEING 737 737890 1384527 NM NR 1 ENGINE MALFUNCTIONED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 558AS 8721 35177 NR 1 ENG IDG DELTA P POPPED. RESEARCH IN ARCTIC SHOWS THIS IS THE 3RD EXTENTION ON THIS IDG ACCOMPLISHED MM 24 11 41 20 0 801, REMOVED & REPLACED IDG OIL FILTERS. NO DEBRIS FOUND. REMOVED AND REPLACED NR 1 ENGINE IDG. REF MM 24 11 11. N R 1 ENGINE IDG OPS LEAK CHECKS NORMAL REF MM TASK 24 11 00 700 802. 2 L 7 2 4F RT A16WE 20081001 EA 2008 10 1 SWIA200820076 1 20080921 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 954SW 7815 EMERGENCY FLOOD LIGHT INOP (FLT 6409). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081001 NM 2008 10 1 UPS08M53377 1 20080917 A 5720 STIFFENER DOUG MD11 MD11F 3023600 NM LT WING BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:1C BROKEN STIFFENING RIB ON BOTTOM OF LT WING UPPER I/B LEADING EDGE PANEL 516ET. REMOVED AND REPLACED 2 EACH Z-STIFFENERS IAW SRM 51-33-01, 51-21-1, 51-35-1. 2 L 7 3 4F RT A22WE 20081001 2008 10 1 CALA0800919 4 20080920 A 2565 65C1990115 CABLE BOEING 737 7373T0 1384582 NM EVAC SLIDE BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12313 23364 DURING NR 3 SERVICE CHECK FOUND L2 DOOR ESCAPE SLIDE LATCH CABLE TO HAVE BROKEN STRANDS. INSTALLED NEW CABLE AND HARDWA RE PER AMM 25-61-35. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085163 1 20080919 A 2560 P2070001 SEAL BOEING 737 7373Y0 1384671 NM FLASHLIGHT TORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 EMERGENCY FLASHLIGHT SEAL TORN. REMOVED AND REPLACED SEAL PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085162 1 20080919 A 5330 6545776 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED C4 CHECK, FOUND SKIN CRACKED AT STR 24L, STA 908 + 3. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085161 1 20080922 A 5330 6550570 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 665WN 23497 DURING SCHEDULED C4 CHECK, FOUND R2 DOOR LOWER HINGE CUTOUT SKIN CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085160 1 20080918 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT 360, ABOVE STR 20 RT. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 08FDEA04126 1 20080929 A 5320 65575695 FLOOR SUPPORT BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 AFT CARGO PIT-STA 1166-1148 RBL 22 CORROSION ON FLOOR SUPPORT REMOVED CORROSION, MATERIAL OUT OF LIMITS. FABRICATED A N EW ANGLE REF BOEING DWG BAC 1490-2711. TREATED AND PRIME THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081001 NM 2008 10 1 08FDEA04127 1 20080929 A 5320 65575695 FLOOR SUPPORT BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 AFT CARGO PIT-STA 1166-1148 RBL 22 CORROSION ON FLOOR SUPPORT REMOVED CORROSION, MATERIAL OUT OF LIMITS. FABRICATED A N EW ANGLE REF BOEING DWG BAC 1490-2711. TREATED AND PRIMED, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081001 NM 2008 10 1 2008UALA05848 1 20080923 A 5520 ATTACH FITTING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT ELEVATOR CRACKED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 772UA 26930 LT ELEVATOR OTBD PCA ATTACH FITTING IS CRACKED AT LWR CORD INBD LUG, ON ELEVATOR, BY- 80904. LT ELEVATOR REPLACED WITH SERVICEABLE LEASED UNIT ON OV W-US. RIGGED AND OP CHECKED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081001 NM 2008 10 1 SWAA085190 1 20080916 A 2560 65C34691 GIRT BAR BOEING 737 7377H4 1384404 NM EVAC SLIDE OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 710SW 27844 R2 EMERGENCY EXIT DOOR SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED GIRT BAR HOLDER PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085187 1 20080918 A 5314 6545866 KEELBEAM BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 662SW 23255 DURING SCHEDULED HC2 CHECK, FOUND KEEL BEAM CORRODED AT BS 500C + 10. REMOVED AND REPLACED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20080929 NM 2008 9 29 2008UALA05828 1 20080921 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY EXIT SIGN INOP, JUST AFT OF DOOR 1 RIGHT, SECURED CONNECTOR. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 NM 2008 9 29 DL757081205 1 20080920 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1720 S27R-29L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 617DL 22907 FUSELAGE SKIN FOUND WITH CORROSION AT STA 1720 BETWEEN S-27R AND S-29L. CUTOUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLE R/TRIPLER. 2 L 7 2 4F RT A2NM 20080929 NE 2008 9 29 DL76G081208 2 20080921 A 7532 79275511 CONTROLLER BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 BLEED INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 171DZ 29690 706112 AFTER ENG START RT BLEED VALVE LIGHT STAYED ILLUM WHEN SELECTED ON. CYCLED C/B PER MTC INTSRUCTIONS, VALVE STAYED CLOSE D. REPLACED NR 2 ENG PRV, RAN ENG, NOW BLEED AIR CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E13NE 20080930 NM 2008 9 30 UPS08M53144 1 20080811 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 8 LEFT BARREL NUT BOREHOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080930 NM 2008 9 30 UPS08M53156 1 20080812 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 8 RIGHT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080930 NM 2008 9 30 CALA0800806 1 20080822 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM BS 907 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 BODY STATION 907 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN S8L AND S9L. REPAIRED CRACKED FRAME A T STATION 907 LEFT AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN S8 AND S9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800823 1 20080824 A 5311 146A1143 FRAME BOEING 737 737724 13844BY NM BS 867 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27722 28789 CRACK IN BELT FRAME STATION 867 BETWEEN STR 8 AND 9 LEFT AT FASTENER FOR OVERHEAD BIN MOUNT. REPAIRED CRACKED FRAME BOD Y STATION 867 STR 8 AND 9 LEFT REF EC/RA 5310-04824 REV A. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 CALA0800825 1 20080825 A 5340 66235743 ATTACH FITTING BOEING 737 737524 1384721 NM BS 706 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14628 27532 SUPPORT ANGLE CLIP IS CRACKED AT LEFT SIDE STATION 706 AND WINDOW UPPER U-CHANNEL INTERCOSTAL. REMOVED SUPPORT ANGLE CL IP AT STATION 706, FABRICATED, TREATED, PRIMED AND INSTALLED SUPPORT ANGLE CLIP AT STATION 706L REF SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 ASAA0843419 1 20080825 A 5752 TAB BOEING 737 7374Q8 138447Q NM LT AILERON GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 784AS 28199 LT WING AILERON TRIM TAB T/E GOUGED. LT WING AILERON TRIM TAB T/E GOUGE REPAIRED IAW B737 400 SRM CH 51 70 06. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 2008UALA04220 1 20080809 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY LIGHT LT AFT GALLEY BOTTOM OF WALL INOP. REPLACED LAMP ASSY, OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA05427 1 20080823 A 3350 362624 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 EMERGENCY LIGHT LAMP INOP ROW 12. REPLACED LAMP. 2 L 7 2 4F 4 F RT A16WE E21EU 20080930 NM 2008 9 30 2008UALA05506 1 20080827 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1400 S26L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 AFT PIT FRAME DENTED AT STA 1400 AND STR 26L. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED AREA, FABRICATED AND INSTALLE D A REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080930 NM 2008 9 30 2008UALA05501 1 20080828 A 2910 HYDRAULIC SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE OVERHEATED A UALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 29 827UA 1022 GREEN HYD SYSTEM OVERHEAT AFTER TAKEOFF. FLIGHT DIVERTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 EU 2008 9 30 2008UALA05500 1 20080827 A 5100 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE UNKNOWN A UALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 WP 29 454UA 1104 LOSS OF FMGC1 & GPWS. RTFL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA05499 1 20080827 A 7400 UNKNOWN BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE IGNITER UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 783UA 26950 222223 SLOW LIGHT OFF ON NR 1 IGNITOR. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080930 NM 2008 9 30 2008UALA05489 1 20080827 A 2800 UNKNOWN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUEL SYSTEM UNKNOWN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 651UA 25389 BOTH MAIN TANKS FED WHILE THERE WAS 12000 LBS IN CENTER TANKS. RIGHT MAIN TANK FED FASTER, IMBALANCE OF 2000 LBS. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA05483 1 20080826 A 3220 LANDING GEAR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NOSE VIBRATION A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 840UA 1522 NOSE GEAR VIBRATION. FLIGHT DIVERTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081001 EU 2008 10 1 08FDEA04113 1 20080929 A 5321 SRZ25005251BH FLOOR PANEL AIRBUS 310 A310222 3930315 EU ZONE 200 BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 MAIN CARGO COMPARTMENT FLOOR PANEL NR 251 BH IS BROKEN. FABRICATED A NEW FLOOR PANEL NR 251 BH IAW DWG SRZ 25-005, REV "G". 2 L 7 2 4F RT A35EU 20081001 NM 2008 10 1 08FDEA04099 1 20080929 A 5740 ATTACH FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 LEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR INBOARD ATTACHMENT POINT INNER SURFACE FOUND PITTING CORROSION . 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 SWAA085195 1 20080919 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 25L AND STR 26L. REPAIRED SHEAR TIE PER SRM . 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 UPS08M53408 1 20080928 A 5710 FRAME DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:1C RT WING L/E LOWER SURFACE PNL FRAME AT WING STA 506 IS CRACKED. REMOVED CRACKED PANEL, FABRICATED AN D INSTALLED REPAIR DOUBLER IAW MD-11 SRM 51-35-02 VOL 2 PG 2, AND DWG ARB2933. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 UPS08M53407 1 20080916 A 5321 WSP0785Y501 FLOOR PANEL DOUG MD11 MD11F 3023600 NM CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 282UP 48452 INSPECTION TYPE:2C RCB FLOOR PNL 10 HAS CORROSION ON UPPER SURFACE. PROCURED AND DRILLED NEW FLOOR PANEL IAW MD-11 SRM 51-31-01. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 UPS08M53406 1 20080916 A 5321 WSP0788501 FLOOR PANEL DOUG MD11 MD11F 3023600 NM CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 282UP 48452 INSPECTION TYPE:2C RCB FLOOR PANEL 4 HAS CORROSION ON UPPER SURFACE. PROCURED AND DRILLED NEW FLOOR PANEL IAW MD-11 SRM 51-31-01. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 ZZDA2008160 1 20080925 A 5330 SKIN BOEING 717 717200 1383700 NM FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 956AT 55018 FOUND 2 DENTS WITH GOUGES AT FS 266 ABOVE LONGERON 18L. REPAIRED PER B717 SRM 53-00-01, INSTALLED FLUSH REPAIR. 2 L 7 2 4F TR A6WE 20081001 NM 2008 10 1 SWAA085186 1 20080919 A 3350 20121 POWER SUPPLY BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 521SW 25320 DURING SCHEDULED MV2 CHECK, FOUND RT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT POWER SUPPLY PER MM . 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085185 1 20080919 A 5511 182A1500 SPAR BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 437WN 29832 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZ STAB LOWER IN SPAR CRACKED AT STA 101.90 21.5 TO STA 101.90 48.5. REPAIRED S PAR PER SRM. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 KCSA081453 1 20080910 A 5412 BULKHEAD BOEING 747 747146 1384905 NM NR 3 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 NR 3 PYLON NAC STA 221.9 BULKHEAD WEB CHAFFED AT HYD FITTINGS. 2 L 7 4 4F RT A20WE 20081008 NM 2008 10 8 KCSA081454 1 20080910 A 5320 ATTACH ANGLE BOEING 747 747122 1384872 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 DOOR OPENING REINFORCEMENT FRAME ATTACH ANGLE DAMAGED AT BS 2230, STR 24R. 2 L 7 4 4F RT A20WE 20081008 NM 2008 10 8 KCSA081455 1 20080910 A 5320 ATTACH ANGLE BOEING 747 747122 1384872 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 DOOR OPENING REINFORCEMENT DRAME ATTACH ANGLE DAMAGED AT BS 2230, STR 23R. 2 L 7 4 4F RT A20WE 20081008 GL 2008 10 8 CHQA200800174 2 20080906 A 7261 23073567 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL NR 2 ENGINE LEAKING A CHQA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 11 569RP 14500816 CAE312591 FLIGHT 6036, CMH TO BOS. JUST AFTER TAKE OFF AT ABOUT 200 FT AGL, THE FLIGHT CREW RECEIVED A LAV SMOKE EICAS MSG. THE FLIGHT ATTENDANT REPORTED THAT THERE WAS NO SMOKE COMING FROM THE LAVATORY. THE INDICATION DISAPPEARED BEFORE THE FLIGH T CREW WAS ABLE TO RUN THE QRH CHECKLISTS. THE ACFT LANDED BACK AT CMH WITHOUT INCIDENT. MX INSPECTED THE ENGINES AND FOUND THE E2 ZERO CARON SEAL WAS LEAKING AND FOUND OIL POOLING JUST AFT OF THE FAN BLADES. THE ZERO CARBON SEAL WAS REP LACED ON E2 AND THE ENGINES WERE RUN WITH NO FURTHER DEFECTS NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081008 NM 2008 10 8 USAA920081658 1 20080909 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319132 3930340 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 828AW 26237 26237 1552 LOGPAGES 4436783, 4436784 & 4436787 FLT NR 0272 PHX-MSP EMERGENCY EQUIPMENT. EMERGENCY PATH LIGHTS AT SEAT 8C AND 10C A ND EMERGENCY OVERWING LIGHTS DO NOT WORK RT SIDE. RESET RT OVERWING EMERGENCY POWER SUPPLY UNIT 12WL. OPS CHECK WAS GOO D. 2 L 7 2 4F RT A28NM 20081009 2008 10 9 USAABA08029 4 20080907 A 3457 TLS755010101B RECEIVER AIRBUS 330 A330323 3930335 EU GPS FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 275AY 23955 0370 LHR FLT 728 PHL TO LHR THE FIRST OFFICERS GPS BECAME INOPERATIVE. THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED MULTI MODE RECEIVER NR 2. OPS CHECKS OK. 2 L 7 2 4F RT A46NM 20081009 NM 2008 10 9 USAABB08149 1 20080906 A 2150 20224324 ACTUATOR BOEING 767 7672B7 1385107 NM LT PACK FAILED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 255AY 17616 25257 PHL FLT 742 ENROUTE PHL TO BCN. ABOUT 1 HOUR INTO FLIGHT, RECEIVED L INOP AND PACK OFF LIGHTS, WITH L PACK TEMP DISPLAY ED ON EICAS. THE CONDITION DID NOT RESET WHEN STAND BY WAS SELECTED AND RESET WAS PUSHED. SINCE THE FLIGHT COULD NOT C ONTINUE INTO ETOPS OPERATION, IT RETURNED TO FIELD PHL AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE LT PACK RAM AIR EXHAUST DOOR ACTUATOR. OPS CHECKS OK. 2 L 7 2 4F RT A1NM 20081009 EU 2008 10 9 USAA920081648 1 20080907 A 3350 LIGHT AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A USAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 19 632AW 81 LOG PAGE 8163386 FLT NR 14 PHX-JFK-EEL. ACFT EMERGENCY LIGHTS WERE ON 15-20 MINS DUE TO GROUND POWER FAILURE AT GATE. FLIGHT ATTENDANT REPORTED EMERGENCY LIGHTS WENT OUT. FLICKERED OFF BEFORE GATE POWER RESTORED. CHARGED STATE OF EMERGE NCY LIGHTS NOW IN QUESTION. MX RESET CONNECTORS ON EMERGENCY LIGHT PACKS. BITE CHECK OF LIGHTS GOOD. 2 L 7 2 4F RT A28NM 20081009 NM 2008 10 9 USAA920081649 1 20080827 A 5312 654656841 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 SAL C19 MAJOR REPAIR NR 6093461. CRACK FOUND ON BULKHEAD AT CENTER CIRCUMFERENTIAL TEAR STRAP AT BS1016, S7R. REPAIRED BULKHEAD AT CENTER CIRCUMFERENTIAL TEAR STRAP AT BS1016, S7R IAW B737 SRM 53-8-08 FIGURE 1201, DETAIL III. 2 L 7 2 4F RT A16WE 20081009 EU 2008 10 9 AALA200802101 1 20080814 A 3230 C665023 LEVER AIRBUS 300 A300B4605R 3930308 EU LANDING GEAR BROKEN A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 7076A 610 MIA INFLIGHT T377/14AUG. CREW REPORTED NR 1 PITCH TRIM, AUTOTHROTTLES, AND STANDBY PITOT HEAT INOPERATIVE. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR LEVER. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A35EU 20081009 WP 2008 10 9 AALA200802098 1 20080813 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7538A 49992 LGA EMERGENCY LIGHTS AT AFT LAVATORY AREA INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT AFT LAVATORY AREA. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081009 NM 2008 10 9 AALA200802091 1 20080813 A 3350 OL387BPGPL LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 DFW EMERGENCY LIGHT IN MID CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN MID CABIN. SYSTEM GROUND CHECKED NO RMAL OPS. 2 L 7 2 4F RT T00001SE 20081009 NM 2008 10 9 AALA200802090 1 20080813 A 3350 OL387BPGPL LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 DFW EMERGENCY LIGHT IN MID CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN MID CABIN. SYSTEM GROUND CHECKED NO RMAL OPS. 2 L 7 2 4F RT T00001SE 20081009 EA 2008 10 9 REX2008F00047 1 20080830 A 5210 G80082 SEAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DEFECTIVE A REXA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 8758D 7758 ACFT ENCOUNTERED BIRD STRIKE ON TAKEOFF, NO NEGATIVE AFFECTS NOTED BY CREW. WHILE CLIMBING THROUGH 9,900 FEET, CREW HEA RD LOUD, AIR RUSHING SOUND AND NOTED THE CABIN RATE RAPIDLY RISING. CREW DECLARED AN EMERGENCY AND REQUESTED A LOWER AL TITUDE. CREW EXECUTED QRH PROCEDURE FOR UNPRESSURIZED FLIGHT AND REGAINED CONTROL OF CABIN PRESSURIZATION. CREW RETURN ED TO MSP AND PERFORMED AN OVERWEIGHT LANDING. CREW REQUESTED LONGEST RUNWAY FOR LANDING AND REFERENCED THE CFM PROCEDU RE FOR OVERWEIGHT LANDING. CREW HAD EMERGENCY PERSONNEL STANDING BY ON GROUND. CREW COMPLETED ALL CHECK LISTS AND MADE AN UNEVENTFUL LANDING. THE DOOR INDICATIONS PAGE SHOWED ALL DOORS AS GREEN AND NORMAL. MX COMPLIED WITH BIRD STRIKE I 2 L 7 2 4F RT A21EA 20081009 NM 2008 10 9 USAA920081650 1 20080822 A 5320 6936656 SHEAR WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 SAL C19 MAJOR REPAIR NR 6097658 CRACK ON SHEAR WEB BETWEEN BS927 & BS847 BLO. REPAIRED SHEAR WEB BETWEEN BS927 & BS847 BLO IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 USAA920081651 1 20080809 A 2597 P4010021 WIRE BOEING 737 7373G7 1384595 NM FLASHLIGHT DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN C19 EES NR 6126423 FORWARD GALLEY EMERGENCY FLASHLIGHT HAS BARE WIRE AT CONNECTOR. REPLACED FORWARD GALLEY EMERGENC Y FLASHLIGHT POWER UNIT. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 QXEA200800986 1 20080917 A 3297 471509 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM NLG FAULTY A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 19 431QX 4164 SEA AFTER TAKEOFF FROM BOI, THE RT GEAR DOOR LIGHT REMAINED ILLUMINATED. FLIGHT CONTINUED TO SEA. PERFORMED AN EMERGEN CY GEAR EXTENSION ON APPROACH TO SEA AND ACCOMPLISHED AN UNEVENTFUL LANDING. ACFT FERRY TO PDX FOR REPAIRS. IN PDX, MX FOUND MULTIPLE PSEU FAULTS IN MEMORY. REPLACED THE NOSE GEAR HARNESS AND THE PSEU AS A PRECAUTION. CHECKS GOOD. RETU RNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081009 EA 2008 10 9 QXEA200800676 1 20080612 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK NUMEROUS CORROSION SPOTS ON RT SIDE SEAT RAIL FS 573 TO 675. REMOVED CORROSION FROM SEAT TRACK AT FS 573 T O 675. .010 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 QXEA200800678 1 20080612 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK NUMEROUS CORROSION SPOTS ON RT SIDE SEAT RAIL FS 713 TO 784. FOUND OUT OF LIMITS AFTER BLEND. REMOVED COR RODED SEAT TRACK FROM FS 713 TO 784 IAW CRJ 700 SRM 51-41-02. INSTALLED NEW SEAT TRACK IAW CRJ 700 SRM 51-41-00, 51-41- 02 AND 51-23-00. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 QXEA200800670 1 20080612 A 5210 ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK PAX DOOR MID CAP ANGLE CORRODED. REMOVED CORRODED MID CAP ANGLE IAW CRJ 700 SRM 51-41-00. LOCATED HOLES I N NEW ANGLE ATTACHED 5 NUTPLATES. TRANSFERRED BRACKETS FROM OLD TO NEW PART IAW CRJ 700 SRM 51-42-06. INSTALL MID CAP ANGLE IAW CRJ 700SRM 51-41-00. 2 L 7 2 4F RT A21EA 20081009 NM 2008 10 9 QXEA200800657 1 20080609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK LT INBD SEAT TRACK NR 5 IS CORRODED BETWEEN THE PILOTS BULKHEAD AND FS 70.5. CLEANED AREA. REMOVED RIVETS AS NECESSARY AND BLENDED OUT CORROSION, .024 MATERIAL REMOVED. WITHIN LIMITS PER RD8/4-53-884, PROXIMITY TO FASTENER H OLE OUT OF LIMITS. MAPPED FOR ENGINEERING. HFEC IAW -8 400 NDTM PART 6, 51-00-01 NO CRACKS NOTED. ALODINED INSTALL RI VET, PRIMED AND PAINTED IAW RD 8/4-53-2336 SECT 1, SHETT 4 PARA 4-9. 2 H 7 2 4T RT A13NM 20081009 EA 2008 10 9 QXEA200800681 1 20080612 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK NUMEROUS CORROSION SPOTS ON LT SIDE SEAT RAIL FS 861 TO 985. REMOVED CORROSION FROM SEAT TRACK AT FS 861 T O 985. .015 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013 AND CRJ SRM 51-21-16. 2 L 7 2 4F RT A21EA 20081009 NM 2008 10 9 QXEA200800661 1 20080609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK SEAT TRACK NR 9 HAS CORROSION AT STA X789.102. BLENDED FOUND OUT OF LIMITS IAW RD8/4-53-884, MAPPED FOR EN GINEERING, DAMAGE FOUND WITHIN LIMITS IAW RD 8/4-53-884 REV 3. HFEC INSPECTED AREA PER NDTM PT 6, 51-00-02 NO CRACKS NO TED. ALODINED PRIMED AND PAINTED IAW Q400 SRM 51-21-10, RD8/4-53-884. 2 H 7 2 4T RT A13NM 20081009 EA 2008 10 9 QXEA200800671 1 20080612 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK BURN MARK FOUND ON FUSELAGE SKIN BETWEEN FS 592 AND FS 613. REMOVED RIVET FORWARD OF BURN MARK IAW CRJ 700 0 SRM 51-42-06. BLENDED DAMAGE REMOVED .025 MATERIAL IAW REO 670-53-31-101. PERFORMED ECI ON BLENDED AREA IAW REO 670- 53-31-101 NO DEFECTS NOTED. TREATED IAW CRJ 700 SRM 51-21-11. INSTALLED RIVET AND PRIMED AND PAINTED IAW CRJ 700 SRM 5 1-21-11, REO 670-53-31-101. 2 L 7 2 4F RT A21EA 20081009 NM 2008 10 9 QXEA200800634 1 20080609 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK FUSELAGE FRAME ANGLE HAS CORROSION AROUND 2 RIVETS AT OB END LOCATED AT FS X-84.200 IB OF STR 30R. REMOVED RIVETS IAW -8 400 SRM 51-42-05. CLEANED AND REMOVED CORROSION IAW -8 400 RD8/4-53-2344 STEPS 1-2. HFEC INSP IAW -8 40 0 NDTM PT 6, 51-00-01 NO CRACKS NOTED. UT THICKNESS CHECK IAW -8 400 NDTM PART 1, 51-00-04. INSTALL 2 RIVETS IAW -8 40 0 SRM 51-42-05. ALODINE PRIMED AND PAINTED IAW -8 400 SRM 51-21-10-02-01, 51-25-10, AND 51-25-15. 2 H 7 2 4T RT A13NM 20081009 EU 2008 10 9 TRAX200801164 1 20080912 A 3350 SIGN AEROSP ATR72 ATR72212 8680945 EU CABIN DETACHED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 640AS 405 F/A REPORTS SERVICE DOOR EMERGENCY EXIT SIGN NEEDS TO BE REATTACHED. FLT 4253 DEL 20 MINS. REATTACHED EMERGENCY EXIT S IGN LT COVER. LT OP CHECKS OK IAW JIC 33-50. 2 H 7 2 4T RT A53EU 20081009 CE 2008 10 9 DXTA200803287 1 20080924 A 3242 BRAKE CESSNA 500 560CESSNA 2076750 CE LANDING GEAR WEAK E DXTA K NONE O OTHER LD LANDING 1 GL 07 398QS 5600522 UPON LANDING ROLLOUT, BRAKES VERY WEAK. 2 L 7 2 4F RT A22CE 20081009 NM 2008 10 9 QXEA200800641 1 20080609 A 5320 SILL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK MCD ENTRYWAY SIL PLATE HAS SPOTS OF CORROSION ON UPPER AND LOWER SURFACES. REMOVED THRESHOLD BY DRILLING O UT RIVETS. REMOVED CORROSION REF RD8/4-53-1660 STEP 1, 3-9, HFEC INSPECTED IAW -8 400 NDTM PT 6, 51-00-01, NO CRACKS NO TED. UT THICKNESS CHECKED IAW -8 400 NDTM PT 1, 51-00-04, INSTALLED NEW THRESHOLD IAW -8 400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 20081009 NM 2008 10 9 QXEA200800637 1 20080609 A 5753 SKIN BOMBDR DHC8 DHC8402 1390042 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK LT WING OTBD FLAP IS CHAFFED ON THE UPPER SURFACE APPROX AT STA YW 250. AND YW 265. BLENDED AREA TO SMOOTH CONTOUR TO REMOVE DAMAGE. HFEC IAW -8 400 NDTM PT 6, 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECK IAW -8 400 NDTM PT 1, 51-00-04. BLEND WITHIN LIMITS PER Q400 SRM 57-52-30 TABLE 1 PG 102. PREPPED AND PAINTED IAW Q400 SRM 51-25-05 PG 2 06 PARA F-1-4. 2 H 7 2 4T RT A13NM 20081009 NM 2008 10 9 2008UALA05632 1 20080908 A 3510 6225219120 TRANSCEIVER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU OXYGEN MASK FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 375UA 24640 FIRST OBSERVERS OXYGEN MASK WILL NOT TRANSMIT WITH MASK ON. FOUND NR 3 TRANSCEIVER FOUND FAULTY. REPLACED TRANSCEIVER. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 20081009 NM 2008 10 9 2008UALA05633 1 20080908 A 3350 58674 INVERTER BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 938UA 26671 EMERGENCY LIGHT INOPERATIVE FROM ROW 14 TO BACK OF ACFT. FOUND FAULTY INVERTER. REPLACED INVERTER. TESTS OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 20081009 EA 2008 10 9 QXEA200800632 1 20080530 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 610QX 10033 RFD C4 CHECK CORRODED SIDE SEAT TRACK ON RT SIDE @ FS 453. REMOVED CORROSION FROM TRACK, OUT OF LIMITS IAW REO 670-53-0 0-013. REMOVED CORRODED SEAT TRACK IAW 670-53-00-013 AND CRJ 700 SRM 51-41-00. PREPARED NEW TRACK FOR INSTALL IAW CRJ SRM 51-40-11. INSTALLED NEW TRACK IAW CRJ SRM 51-41-02. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 QXEA200800679 1 20080612 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK NUMEROUS CORROSION SPOTS ON RT SIDE SEAT RAIL RS 784 TO 861. REMOVED CORROSION FROM SEAT TRACK AT FS 784 T O 861. .010 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013. 2 L 7 2 4F RT A21EA 20081009 EU 2008 10 9 2008UALA05635 1 20080908 A 2621 BA21758 FIRE BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AFT LAV LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 411UA 464 AFT LAV FIRE BOTTLE IS SHOWING RED BAND. REPLACED AFT LAV FIRE BOTTLE. OKAY FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081009 EA 2008 10 9 QXEA200800669 1 20080612 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK FS 280 SHOWS SIGNS OF CORROSION. BLENDED CORROSION FROM LT FS 280 BULKHEAD. .002 MATERIAL REMOVED, IAW CR J 700 SRM 53-11-10. BLENDED CORROSION FROM RT FS 280 BULKHEAD, .003 MATERIAL REMOVED. IAW CRJ 700 SRM 53-11-10. TREAT ED IAW CRJ 700 SRM 51-21-11, PRIMED IAW SRM 51-25-06 TOPCOAT APPLIED IAW SRM 51-25-00. 2 L 7 2 4F RT A21EA 20081009 NM 2008 10 9 2008UALA05642 1 20080906 A 3510 MXP401600U OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 806UA 788 CREW OXY PSI SLOWLY DECREASING WITH NO CREW USE. IN ABQ CREW O21300 PSI - 1HR LATER 1200P. FOUND STICKY PRESS TO TEST PLUNGER AT 1ST OBSERVER'S LOCATION.REPLACED O2 MASK & BOX. OPS TEST OKAY. SERVICED CREW O2. NO SYSTEM BLEED DOWN WITH IN 45 MINUTES. 2 L 7 2 4F 4 F RT A28NM E40NE 20081009 NM 2008 10 9 QXEA200800656 1 20080609 A 5753 SKIN BOMBDR DHC8 DHC8402 1390042 NM T/E FLAP CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK LT WING OTBD FLAP IS CHAFFED ON THE UPPER SURFACE BETWEEN STATION YW 209.019 AND 227.019. BLENDED AREA TO SMOOTH CONTOUR TO REMOVE DAMAGE. HFEC IAW -8 400 NDTM PART 6 51-00-01 NO CRACKS NOTED. UT THICKNESS IAW -8 400 NDTM PA RT 1 51-00-04 MAPPED FOR ENGINEERING. BLEND FOUND WITHIN LIMITS IAW RD 8/4-57-1012. PRIMED AND PAINTED IAW Q400 SRM 51 -25-05 PG 216 PAR F-1-4. 2 H 7 2 4T RT A13NM 20081009 NM 2008 10 9 2008UALA05891 1 20080925 A 3350 78671 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SEAT 26C MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 LIGHT ASSY AT 26C IS MISSING. LIGHT ASSY MISSING. INSTALLED NEW LIGHT ASSEMBLY. OPERATIONS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081009 NM 2008 10 9 2008UALA05681 1 20080910 A 3350 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 658UA 27113 EMERGENCY ESCAPE PATH LIGHTING BESIDE 10FG WON'T COME ON DURING EMERGENCY LIGHT TEST. CABLE REPAIRED USING SPLICE CRIMP ER METHOD. IT NOW OPS SATISFACTORY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081009 NM 2008 10 9 QXEA200800660 1 20080609 A 5311 FRAME BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK CORROSION ON FUSELAGE FRAME AT STA X234.475 AND RT STR 29. REMOVED CORROSION IAW -8 400 SRM 51-21-00 PARA 1-3 AND 4A(1) & 2 (B). UT THICKNESS CHECKED BLENDED AREA IAW -8 400 NDTM PART 1, 51-00-04, HFEC INSP IAW -8 400 NDTM PA RT 6, 51-00-01 NO CRACKS NOTED. MAPPED FOR ENGINEERING, WITHIN LIMITS IAW RD8/4-53-2378. ALODINED PRIMED AND PAINTED I AW Q400 SRM 51-21-10, 51-25-65 AND 51-25-15. 2 H 7 2 4T RT A13NM 20081009 EA 2008 10 9 TRAX200801190 1 20080918 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 931EV 8015 JOB 8801521 OPERATION 163 PAX DOOR AFT DRAG ANGLE IS CRACKED. 2 L 7 2 4F RT A21EA 20081009 NM 2008 10 9 2008UALA05899 1 20080926 A 3350 FU305 FUSE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 331UA 24192 EXTERIOR EMERGENCY EXIT LIGHT INOP AT DOOR 2R. FOUND BLOWN FUSE ON POWER SUPPLY. REPLACED AT DOOR 2R. OP CHECKS NORMA L. 2 L 7 2 4F 4 F RT A16WE E21EU 20081009 EA 2008 10 9 TRAX200801193 1 20080919 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 922EV 7822 EXT RT SIDE EMERGENCY CENTER LIGHT INOP. RESOLVED ON W/O 101005 TASKCARD NR 00006. WORK COMPLETED IN ACCORDANCE WITH A MM. R&R EMERGENCY LIGHT ON RT SIDE IAW CRJ 200 33-51-21. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20081009 NM 2008 10 9 KCSA081489 1 20080923 A 5347 SEAT TRACK BOEING 747 747249F 1384849 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 MAIN DECK SEAT TRACK CORRODED AT BS 670, RBL 28. 2 L 7 4 4F RT A20WE 20081009 NM 2008 10 9 KCSA081491 1 20080925 A 5347 SEAT TRACK BOEING 747 747249F 1384849 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 MAIN DECK SEAT TRACK DAMAGED BETWEEN BS 1320 AND 1340, LBL 34. 2 L 7 4 4F RT A20WE 20081009 NM 2008 10 9 KCSA081493 1 20080925 A 5347 SEAT TRACK BOEING 747 747249F 1384849 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 MAIN DECK SEAT TRACK DAMAGED AT BS 1200, LBL 11. 2 L 7 4 4F RT A20WE 20081009 WP 2008 10 9 DHLA200800099 1 20080923 A 3350 5708458505 BATTERY DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A DHLA K NONE L NO TEST NR NOT REPORTED 1 SO 01 801DH 7554 46033 EMERG LTS BATTERY DISCHARGED REPLACED BATTERY PACK FOR EMER LTS PER MM 33-50-01 CHECKS SERV. N/A FLT NR. ACFT WAS GROU NDED 2 L 7 4 4F RT 4A25 20081009 EA 2008 10 9 TRAX200801134 1 20080907 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 682BR 7691 JOB 8769125 OPERATION 44 PAX DOOR AFT ANCHOR FITTING IS CRACKED AND SWIVEL LEVER ATTACH PIN LUGS ARE ELONGATED. RESOLVE D ON W/O 99839 TASKCARD NR 00175. C/A REMOVED PAX DOOR AFT ANCHOR FITTING AND SWIVEL LEVER. INSTALLED SERVICEABLE ANCH OR FITTING AND SWIVEL LEVER IAW CRJ 200 AMM 52-11-17-400-804 STEP 2B. CONNECTED CABLE TO ANCHOR FITTING SWIVEL IAW CRJ 200 AMM 52-11-17-400-804 STEP 3A. ADJUSTMENT OF PAX DOOR COUNTERBALANCE SYSTEM DUE. PERFORMED ADJUSTMENT CK OF PAX DOO R COUNTERBALANCE SYSTEM IAW CRJ 200 AMM 52-11-17-820-802. ADJUSTMENT GOOD AT THIS TIME. PERFORMED OPS TEST OF PAX DOOR COUNTERBALANCE IAW CRJ 200 AMM 52-11-17-710-802. OPS TEST GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 TRAX200801188 1 20080918 A 5312 ISOLATOR CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 683BR 7692 JOB 8769211 OPERATION 165 5 ISOLATORS ON FS 621 BULKHEAD IN CARGO BAY ARE CRACKED. RESOLVED ON W/O 100685 TASKCARD NR 0 0240. C/A REPLACED THE 5 CRACKED ISOLATORS ON FS 621 BULKHEAD IAW CRJ 200 SRM 51-42-13. 2 L 7 2 4F RT A21EA 20081009 SO 2008 10 9 SIMA200826803 1 20080922 A 3231 22250005000 SOLENOID VALVE EMB 145 EMB145LR 3260212 SO NLG MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 21 638AE 145172 ON FLIGHT 3942 CREW REPORTED AT 22,000 FT .77 MACH GEAR UNSAFE MSG ON EICAS. GEAR DOOR OPEN. CREW DECLARED EMERGENCY I NTO ORD AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. C/A REPLACED NLG DOOR SOLENOID VALVE. IAW EMB 145 AMM 32-33-02. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081009 GL 2008 10 9 CHQA200800186 2 20080922 A 7200 AE3007A1P ENGINE EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL NR 1 LEAKING A CHQA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 GL 11 273SK 12646 145331 CAE312347 FLIGHT 6142 CMH TO JFK. DURING TAKE OFF AT ABOUT 500 FT AGL THE FLIGHT CREW NOTICED AN OIL LIKE SMELL WITH NO EICAS MSG S. AT 1000 AGL LAV SMOKE APPEARED ON EICAS. THE FLIGHT ATTENDANT INSPECTED THE LAVATORY AND FOUND NO SIGNS OF SMOKE OR FIRE. THE LAV SMOKE INDICATION DISAPPEARED AFTER 1 MINUTE AND THE SMELL DISSIPATED AFTER ABOUT 2 MINUTES. THE CREW AC COMPLISHED THE APPLICABLE QRH CHECK LISTS AND LANDED WITHOUT INCIDENT. MX RAN THE ENGINES AND PACKS AND WERE ABLE TO DU PLICATE THE ODOR WHILE RUNNING OFF OF E1. THE ENGINE WAS INSPECTED AND THE 14TH STAGE BLEED DUCTING HAD A STRONG ODOR O F OIL AND THE FIRST STAGE COMPRESSOR BLADES HAD SOME DISCOLORATION. E1 WAS CHANGED AND THERE WERE NO FURTHER DEFECTS NO 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081009 EA 2008 10 9 SIMA200826601 2 20080918 A 7200 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO RROYCE AE3007 AE3007A1 54165 EA RIGHT MALFUNCTIONED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 675AE 14500806 CAE312831 ON FLIGHT 4176 CREW REPORTED RECEIVING A LAV SMOKE INDICATION ON CLIMB ON EICAS FOLLOWED BY FA REPORT OF SMOKE IN CABIN. CREW RETURNED FOR AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. C/A DETERMINED OIL/SMOKE SMELL TO BE COMIN G FROM NR 2 ENGINE. R&R NR 2 ENGINE IAW AE MTC 71-000-00. OPS CHECKS AND LEAK CK GOOD. NO DEFECTS FOUND AT THIS TIME. ACFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081009 EU 2008 10 9 2008UALA05563 1 20080901 A 2612 73040102 FIRE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 NACELLE INOPERATIVE A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 468UA 1363 ENG NR 1 FIRE TEST DOES NOT WORK. NO BELL OR LIGHT. SQUIB LIGHTS DO ILLUMINATE. NO ECAM. FOUND FAULTY FIRE DETECTION UN IT.REPLACED APU FDU. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20081009 EU 2008 10 9 08FDEA03902 1 20080916 A 5347 A5327400500053 SEAT TRACK AIRBUS 310 A310 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 SEAT TRACK IS DAMAGED AT FRAME 54; RBL 18. REMOVED THE DAMAGED TRACK & INSTALLED A NEW TRACK WITH SPLICE IAW SRM 53-10- 16. 2 L 7 2 4F RT A35EU 20081009 NM 2008 10 9 F3LA2008100600662 1 20081003 A 5315 D5347217220400 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 931FR 52 2253 DURING C3 C-CHECK, INSPECTION NOTED FLOORBEAM Y1292 AT FRAME 68, FORWARD AND AFT HOLES HAVE CORROSION. MAINTENANCE BLEN DED CORROSION AND OVERSIZED HOLES IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-00-14, FIGURE 102. MAINTENANCE PER FORMED ROTO-PROBE INSPECTION (NO DAMAGE REMAINS, TREATED, PRIMED AND PAINTED IN ACCORDANCE WITH THE REQUIREMENTS OF ENGI NEERING AUTHORIZATION A9-53R-30663. 2 L 7 2 4F RT A28NM 20081009 NM 2008 10 9 F3LA2008100600663 1 20081003 A 5321 D5367175900000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CABIN DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 931FR 52 2253 REFERENCE NON-ROUTINE C052153. DURING C3 C-CHECK, INSPECTION NOTED PASSENGER FLOOR PANEL 261EF HAS A CUT ON THE SURFACE . MAINTENANCE REPAIRED FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 212. 2 L 7 2 4F RT A28NM 20081009 NM 2008 10 9 F3LA2008100600665 1 20081004 A 5321 D5367175500000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CABIN DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 931FR 52 2253 DURING C3 C-CHECK, INSPECTION NOTED PASSENGER FLOOR PANEL 261DF HAS AREAS OF DELAMINATION. MAINTENANCE REPAIRED FLOOR P ANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 212. 2 L 7 2 4F RT A28NM 20081009 NM 2008 10 9 2008UALA05942 1 20080930 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 EEL LIGHT BAR INOP AT LEFT FWD CLOSET. 2 L 7 2 4F 4 F RT A1NM E24NE 20081009 NM 2008 10 9 2008UALA05952 1 20081001 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EVAC SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 SLIDE EMERGENCY LIGHT NOT ON AT DOOR 5 RT. LIGHT FOUND INOPERATIVE. REPLACED LIGHT ASSY. OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081009 NM 2008 10 9 SWAA085304 1 20081001 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM T-CAP CORRODED AT BS 947.5, RBL 2 TO LBL 4. REMOVED AND REPLACED BEAM PER S RM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085305 1 20081001 A 5311 6545767 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 440, BETWEEN STR 13R TO 19R. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085306 1 20081001 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 19L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085307 1 20081001 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 492, STR 27R. REMOVED AND REPLACED SPLICE PER SWA DWG. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 2008UALA05849 1 20080923 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 127UA 28813 RIGHT OVERWING FWD LIGHT ASSY FWD LAMP IS INOP. REPLACED LIGHT ASSEMBLY, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081001 NM 2008 10 1 2008UALA05851 1 20080923 A 3350 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 127UA 28813 SEAT 3A AFT EMERGENCY LIGHTS INOP. RELAMPED, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081001 NM 2008 10 1 2008UALA05779 1 20080917 A 5320 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 R-2 DOOR REQUIRES A REPAIR DOUBLER AT THE UPPER HINGE CUT-OUT OF FRAME. MAJOR REPAIR ACCOMPLISHED, INSTALLED A FRAME DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081001 NM 2008 10 1 2008UALA05766 1 20080917 A 3397 7945243 CABLE BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 SEAT 3J FWD AND AFT EMERGENCY LIGHT IS INOP REPLACED BAD UNDERSEAT CABLE. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081001 NM 2008 10 1 2008UALA05769 1 20080917 A 5322 SHEAR TIE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 817UA 873 SHEAR PLATE AFT OF DOOR 2R AND FRAME 69 DAMAGED BY CORROSION. MAJOR REPAIR ACCOMPLISHED, REPLACED SHEAR TIE. COMPLETED INSTALLING WIRES THROUGH SHEAR PLATE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081001 EU 2008 10 1 2008UALA05774 1 20080917 A 3510 MXP401600U OXYGEN MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CAPTAIN'S NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 460UA 1248 CAPT O2 MASK FAILS TO TEST IN STORAGE BOX. MASK OPS NORMAL BUT NOT TEST. SUPPLEMENTAL DATA UPDATE, MASKS OPS NORMAL BU T WILL NOT TEST. SWAPPED CAPTAIN'S AND 2ND OBS MASK. OPS CHKD GOOD. LEAK CHECKED GOOD. REPLACED 2ND OBSERVERS O2 MAS K. 2 L 7 2 4F 4 F RT A28NM E40NE 20081001 NM 2008 10 1 08FDEA04044 1 20080925 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 HFEC INSPECTION CARRIED OUT ON DIAMETER 0.460 INCH HOLES AT MAIN DECK CARGO DOOR NR 1 SPOOL FITTING FOUND CRACK INDICATI ON ON HOLE NR A, B, C AND WITH CRACK INDICATION. SPOOL FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 08FDEA04046 1 20080925 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 HFEC INSPECTION CARRIED OUT ON DIAMETER 0.460 INCH HOLES AT MAIN DECK CARGO DOOR NR 2 SPOOL FITTING FOUND CRACK INDICATI ON ON HOLE NR A, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 08FDEA04054 1 20080926 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 HFEC INSPECTION CARRIED OUT ON DIAMETER 0.460 INCH HOLES AT MAIN DECK CARGO DOOR NR 5 SPOOL FITTING, FOUND CRACK INDICAT ION ON HOLE A, B, C AND D. REMOVED AND REPLACED AS PER SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 08FDEA04056 1 20080926 A 5315 7075T6040C FLOORBEAM BOEING 757 75723A 1384967 NM BS 1681 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 MAIN CABIN FLOORBEAM BS 1681.8 UPPER T-CHORD LOWER SURFACE LBL58.22-RBL58.22 CORRODED. REMOVED CORROSION FOUND TO BE OU T OF LIMITS IAW SRM 53-00-51, FAB NEW T-CHORD ON TRAVELER NR T8-756288, T8-756289, T8-756213. INSTALLED FABRICATED PART S IAW 51-40-02. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 08FDEA04057 1 20080926 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 HFEC INSPECTION CARRIED OUT ON DIAMETER 0.460 INCH HOLES AT MAIN DECK CARGO DOOR NR 6 SPOOL FITTING, FOUND CRACK INDICAT ION ON HOLE A, B, C AND D. REMOVED AND REPLACED AS PER SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 08FDEA04059 1 20080926 A 5315 BAC1505100703 FLOORBEAM BOEING 757 75723A 1384967 NM BS 1640 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 CABIN FLOORBEAM STA 1640 LBL 58 HAS CORROSION. REMOVE CORROSION IAW SRM 51-40-02 CHECK LIMITS FOUND TO BE OUT OF LIMITS IAW SRD 53-00-51. REMOVED DAMAGED FLOORBEAM IAW SRM 53-00-01, RECEIVED EXTRUSION BAC1505-100 703 BATCH NR 0001493411ON MAE T8-54170, LOCATED AND DRILLED EXTRUSION IAW SRM 51-40-05. INSTALLED EXTRUSION IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 08FDEA04062 1 20080926 A 5720 ARB2886504 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 RIGHT WING LEADING EDGE TELESCOPIC DUCT CUT OUT INBOARD DOUBLER FOUND CHAFED. DOUBLER REPAIRED AS PER SRM 57-10-00. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 08FDEA04064 1 20080926 A 5230 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 HFEC INSPECTION CARRIED OUT ON DIAMETER 0.520 INCH HOLES AT MAIN DECK CARGO DOOR NR 6 SPOOL FITTING. FOUND CRACK INDICA TION ON HOLE 'B' SECOND LAYER FROM TOP. CARRIED OUT REPAIR AS PER E.A. 1-5310-123123. THIS REPAIR CLASSIFIED AS MAJOR P ER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 08FDEA04065 1 20080926 A 5230 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 HFEC INSPECTION CARRIED OUT ON DIAMETER 0.520" HOLES AT MAIN DECK CARGO DOOR NR 7 SPOOL FITTING, FOUND CRACK INDICATION ON HOLE 'B' SECOND LAYER FROM TOP. CARRIED OUT REPAIR AS PER E.A. 1-5310-123123. THIS REPAIR CLASSIFIED AS MAJOR PER G MM 6-2-100. 2 L 7 3 4F RT A22WE 20081009 NM 2008 10 9 SWAA085315 1 20081001 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND BELLY SKIN CRACKED AT BS 450, BL 0 TO RBL 1.5. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085316 1 20081001 A 5713 6546404 STRINGER BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED SPV CHECK, FOUND RT WING U9 STRINGER CRACKED AT WING STA 583, ON VERTICAL LEG. REMOVED AND REPLACED ST RINGER PER IND EA. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085323 1 20081001 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947.5, STR 25R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085324 1 20081001 A 5315 6546804 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND MAIN CABIN FLOORBEAM CRACKED AT BS 663 BL 0. REPAIRED BEAM PER DHN EA. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085334 1 20081001 A 5311 65C22910 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND FRAME CRACKED AT BS 500D, STR 21R AND STR 21L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085337 1 20081001 A 3222 162A11202 CYLINDER BOEING 737 73776Q 13845AA NM NLG FAILED A SWAA K NONE O OTHER LD LANDING 1 SW 29 551WN 30280 AFTER LANDING RT NLG WHEEL CAME OFF, AXLE FAILURE. REMOVED AND REPLACED NLG INNER CYLINDER ASSY PER MM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085342 1 20081001 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727C, STR 14L TO STR 15L. REMOVED AND REPLACED TIE PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 ASAA0873543 1 20080916 A 5315 147A55068 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 AFT PASSENGER CABIN CORROSION ON TOP OF FLOORBEAM BS 986.5 RBL 4 RBL 23. AFT PASSENGER CABIN CORROSION ON TOP OF FLOORB EAM BS 986.5 RBL 4 RBL 23 REPAIRED IAW ERO 8676 AND EA 5320 01853. PERFORM FIRST STAGE DTA INSP REQUIREMENTS WITHIN 12 MONTHS FROM 19 SEP 08. SEAMC BILL NOTIFIED. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 ASAA0873546 1 20080915 A 5312 143A948534 ANGLE BOEING 737 737790 13844CN NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 FWD CARGO PIT AFT BULKHEAD LOWER ANGLE BETWEEN STR 26R AND STR 26L AT BS 500D. AREA BLENDED AND FOUND TO BE BEYOND ALLO WABLE DAMAGE LIMIT. LOWER ANGLE REMOVED AND REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 51 20 05 & 51 40 02. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 ASAA0873547 1 20080915 A 5320 143A750180 ANGLE BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 FWD CARGO PIT LT Z-ANGLE CORRODED BETWEEN BS 495 AND 500D. CORRODED FWD CARGO PIT LT Z-ANGLE CORRODED BETWEEN BS 495 AN D 500D REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53 30 53. 2 L 7 2 4F RT A16WE 20081010 EA 2008 10 10 MAL2008F00035 1 20080914 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN CRACKED A MALA O OTHER O OTHER NR NOT REPORTED 1 GL 15 924XJ 15179 EMERGENCY FLOOR PATH LIGHTING ASSY HAS CRACKS IN (2) PLACES; ON THE (2) MOST FORWARD STRIPS TO THE RT SIDE. REMOVED AND REPLACED EMERGENCY FLOOR PATH LIGHTING ASSEMBLIES. (K) 2 L 7 2 4F RT A21EA 20081010 NM 2008 10 10 ASAA0873550 1 20080922 A 5320 141A5410U12 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 FWD PAX CABIN INTERCOSTAL CRACKED BS 312 328 RBL 31. FWD PAX CABIN INTERCOSTAL CRACKED BS 312 328 RBL 31 REPLACED IAW B 737 700 SRM 51 40 02 NEW PART P/N 141A5410U12. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 ABX2008F00003 1 20080903 A 7920 SPINNER BOEING 767 767281 1385109 NM GE CF6 CF680A 30025 NE NR 1 ENGINE LEAKING A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 791AX 23141 EXHAUST FUMES IN COCKPIT DURING HIGH THRUST SETTINGS. GROUND RAN ENGINES AND FOUND LEFT ENGINE PRODUCING SMOKE EXHAUST F UMES FROM VENTS WITH LEFT BACK ON. FOUND OIL IN NR 1 ENGINE SPINNER. RESEALED NR 1 BEARING MANIFOLD AND FAN ROTOR SPIN NER IAW AMM 72-31-00-2 AND 72-31-01-4. (K) 2 L 7 2 4F 4 F RT A1NM E13NE 20081010 NM 2008 10 10 ASAA0873551 1 20080915 A 5320 146A75022 CHANNEL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 CORROSION ON Z-CHANNEL RT BS 727C BS 767 RBL 20 AFT CARGO PIT. CORRODED ON ZEE CHANNEL AT RT BL 20 AFT CARGO PIT BETWEE N BS 727 + 4 BS 847 REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 51 20 05. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 ASAA0873538 1 20080916 A 5320 143A75014 ANGLE BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 FWD CARGO PIT RT SIDE ZEE ANGLE CORRODED BETWEEN BS 500A AND BS 500D. REPLACE WITH MADE REPAIR PART IAW B737 700 SRM 53 30 53. 2 L 7 2 4F RT A16WE 20081010 CE 2008 10 10 GUU2008F00050 1 20080810 A 5100 UNKNOWN BEECH 1900 1900D 1154162 CE LEAKING A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 29 81536 UE152 DURING FLIGHT, STRONG FUEL ODOR IN CABIN, MADE PASSENGER SICK. REMOVED AND CLEANED OLD SEALANT AT SUSPECTED FUEL LEAK A REA AND RESEALED. NO LEAKS NOTED. (K) 2 L 7 2 4T RT A24CE 20081001 NM 2008 10 1 08FDEA04067 1 20080926 A 5313 BAC1498131 STRINGER BOEING 727 727227 1384078 NM BS 1150 S26R CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 AFT CARGO PIT, STA 1150, RBL 24, CORROSION ON UNDER SIDE OF STRINGER 26. REMOVED CORROSION STR 26 R ORIGINAL .090, REMO VED .032, REMAINING .058 OUT OF LIMITS. FABRICATE STRINGER & SPLICES. ALODINED PRIMED PARTS, INSTALLED REPAIR PARTS RE F SRM 53-10-1, 53-10-3 FIG 1, DWG65-16348. THIS IS CLASSIFIED A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081001 2008 10 1 ASAA0853526 4 20080920 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 02 577AS 6014 35186 NO "ACARS" PROMPT ON EITHER FMC ACARS INOP. PERFORM SIM TASK 23 27 00 810 815 OPEN AND RESET C/B FMC C/BS SYS OPS NORMA L AFTER RESET. PERFORMED ACARS OPERATIONAL TEST REF MM 23 27 00, OPS NORMAL. PERFORMED L & R FMC OPERATIONAL TEST, REF MM 34 61 00 OPS NORMAL. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 CALA0800918 1 20080923 A 5320 65C33419 SUPPORT BOEING 737 7373T0 1384582 NM CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 PARTITION SUPPORT CRACKED AFT OF STA 1016. REMOVED AND REPLACED PARTITION SUPPORT PER 737-300 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 CALA0800917 1 20080923 A 5315 255T1241 STIFFENER BOEING 767 767224 1385170 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69154 30433 BS 246 FLOORBEAM FWD SIDE ONE STIFFENER FOUND CRACKED AT RBL 8 BS 246 FLOORBEAM FWD SIDE RBL 8 STIFFENER REPLACED PER SR M 51-10-02 AND FASTENERS INSTALLED PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081001 NM 2008 10 1 CALA0800916 1 20080923 A 5347 141T5121253 SEAT TRACK BOEING 767 767224 1385170 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69154 30433 FWD CARGO M/D SEAT TRACK CRACKED AT BS 412 LBL 20. FWD CARGO M/D SEAT TRACK BS 412 LBL 20 REPAIRED PER ECRA 5320-01905. 2 L 7 2 4F RT A1NM 20081001 NM 2008 10 1 ASAA0843525 1 20080911 A 5755 SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 LT WING NR 2 SPOILER DENTED ON UPPER SURFACE 12 INCHES FROM O/B END. PREPARED DAMAGED AREA, FABRICATED DOUBLER AND BOND ED IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 ASAA0853523 1 20080921 A 5320 143A94057 SUPPORT BRACKET BOEING 737 737890 1384527 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 551AS 34593 LINEAR SUPPORT BRACKET DENTED TEMP REPAIR INSTALLED PER WA 5320 01842 STA 5000 STR 23R 24R. REPAIRED SUPPORT BRACKET IA W B737 800 SRM 51 70 11 FIG 202. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 ASAA0853521 1 20080920 A 3020 WARNING SYSTEM BOEING 737 737890 1384527 NM NR 1 ENGINE MALFUNCTIONED A ASAA K NONE N FALSE WARNING UK UNKNOWN 1 NM 02 557AS 8816 35176 ENG NR 1 COWL VALVE OPEN LIGHT ON. RAN NR 1 ENGINE AND CYCLED NR 1 ENGINE COWL ANTI ICE VALVE. OPS NORMAL. REF AMM 30 21 00 710 801 STEPS E (1) (A), (2 3 4 5). REF FIM 30 21 00 810 804 STEPS E(2 3). REF ETOPS MANUAL E05 00 05 PAGE 5 ST EPS (7 8 9). GROUND VERIFICATION SUCCESSFUL. 2 L 7 2 4F RT A16WE 20081001 2008 10 1 ASAA0853520 4 20080918 A 2211 8221604101 COMPUTER BOEING 737 737890 1384527 NM AUTOPILOT SYS FAILED A ASAA K NONE J WARNING INDICATION CL CLIMB 1 NM 02 587AS 3649 35684 AUTOTHROTTLE LIM ILLUMINATED IN CLIMB FROM 370 390 WITH AUTOTHROTTLES ENGAGED. NORMAL OPS WITH AUTOTHROTTLE OFF (NOTE: 2 KNOB SPLIT WITH AUTOTHROTTLE LIMIT ILLUMINATED AND CLIMBING). TS FAULT CODES FOUND AT CURRENT STATUS TEST WOULD NOT E NGAGE. RESET FCC A BREAKERS AND AT CURRENT STATUS TEST CHECKED GOOD. REPLACED FCC A PER AMM REF TASKS 22 11 33 000 801 400 801 CHECKED GOOD SOFTWARE VERIFIED CORRECT. VERIFIED ENG 1&2 TAT PROBE IND NORMAL. VERIFED NO FAULTS WITH TLA RES OLVER OR AUTOTHROTTLE BRAKE ASSY PER FIM REF 22 31 00 810 812. PERFORMED DFCS LRU INTERFACE TEST FOR FCC BITE GRP NR 35 LAND VERIFY TEST BITE GRP 49 (AMM 22 11 00 201) AND HGS SENSOR TEST FOR FCC AT PER AMMS REF 34 36 00 ALL TESTS PASS. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 ASAA0853519 1 20080920 A 2131 2193301AA CONTROLLER BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 02 558AS 8661 35177 AUTO FAIL LIGHT ILLUMINATED PRESSURIZATION PANEL. DUPLICATED FAULT BOTH PRESSURIZATION CONTROLLERS SHOWED CONTROL PANEL FAULT. RESET & CLEARED FAULTS ON BOTH AUTO PRESS CONTROLLERS AND ACCOMPLISHED FIM 21 31 00 810 801, OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085154 1 20080919 A 2121 215201 GASPER FAN BOEING 737 7377H4 1384404 NM E&E BAY FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 29 422WN 29826 CREW REPORTED BURNING SMELL THROUGH VENTS ON DESCENT. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085153 1 20080922 A 2910 251A21021 FITTING BOEING 737 7377H4 1384404 NM ELEVATOR SYS LOOSE A SWAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 29 278WN 36441 ELEVATOR FEEL DIFFERENTIAL PRESSURE LIGHT ILLUMINATED IN FLIGHT WITH APPEARANT SLOW LEAK IN A-HYDRAULIC SYSTEM. FOUND L OOSE FITTING AT ELEVATOR FEEL COMPUTER. SECURED PNEUMATIC FITTING PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085152 1 20080921 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085139 1 20080921 A 5311 6546540 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17L AND STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085138 1 20080921 A 3350 3071BPEGPL LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085137 1 20080921 A 3350 3071BPEGPL LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085136 1 20080918 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 455WN 32462 EEPLS LENS LOOSE AT ROW 2 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085149 1 20080921 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081024 EU 2008 10 24 ASOA200801367 1 20081019 A 3350 COVER AEROSP ATR72 ATR72 EU CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 641AS 387 EMERGENCY LIGHT COVER IS MISSING ON SERVICE DOOR. 2 H 7 2 4T RT 20081024 NM 2008 10 24 F3LA2008102200675 1 20081020 A 5315 D53472172205 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 F3LA 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON FLOORBEAM Y1292 BETWEEN FRAME 66 AND FRAME 68, PASSENGER CABIN. MAI NTENANCE REMOVED AND REPLACED FLOORBEAM IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2. 2 L 7 2 4F RT A28NM 20081001 NM 2008 10 1 SWAA085144 1 20080921 A 3350 417A5600 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 718SW 27852 DURING SCHEDULED 10Y CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT ASSY LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085143 1 20080921 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 K11A2008102372208 1 20081014 A 5320 INTERCOSTAL BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER NR NOT REPORTED 1 GL 23 722CK 20948 INTERCOSTAL CORROSION UNDER F/S SEAT TRACK (CORROSION OUT OF LIMITS). 2 L 7 3 4F RT A3WE 20081001 NM 2008 10 1 SWAA085142 1 20080921 A 5313 BAC1498 STRINGER BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND STRINGER 24L CORRODED AT BS 967. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20080929 EU 2008 9 29 08FDEA03194 1 20080731 A 5315 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 100 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 AFT CARGO COMPARTMENT, CABIN FLOORBEAM AT FRAME 60, LOWER FLANGE IS BENT AT APPROX BL -Y 1830. COMPLIED WITH EA 6-5310- 123366 "FUSELAGE - C60 CROSSBEAM, PERMANENT REPAIR OF THE LOWER FLANGE DEFLECTION AT APPROX -Y 183.0. 2 L 7 2 4F RT A35EU 20080930 NM 2008 9 30 CALA0800802 1 20080821 A 5510 65C25156503 FITTING BOEING 737 737524 1384721 NM HORIZONTAL STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14653 28914 HORIZONTAL STABILIZER CENTER SECTION TRUSS STRUCTURE HAS A CRACKED BRACKET AT APROXIMATELY STATION 1121 LT SIDE CENTER P /N 65C25156-8. REMOVED AND REPLACED CRACKED FITTING ON HORIZONTAL STABILIZER CENTER SECTION TRUSS AT APPROXIMATELY STAT ION 1121 LT SIDE CENTER IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20080930 NM 2008 9 30 2008UALA04188 1 20080808 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1360 S27-28R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 FRAME AT BS 1360 STR 27R-28R HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED: INSTALLED NEW FRAME REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080930 NM 2008 9 30 2008UALA04189 1 20080808 A 5320 PLATE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 814UA 862 RT SHEAR PLATE CORRODED (MARKED). REMOVED PLATE. PICKED UP HOLES. INSTALLED FASTENERS. INSTALLED SHEAR PLATE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA04206 1 20080808 A 3350 20131A BATTERY PACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EMERGENCY LIGHT FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 823UA 952 EMERGENCY LIGHT BATTERY FAULT LEFT. REPLACED BATTERY PACK. OPS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA04217 1 20080809 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY CEILING LIGHT ABOVE ROW 16 INOP. REPLACED LAMP, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA05425 1 20080823 A 3350 CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 117UA 28810 LEFT SIDE A ZONE EMERGENCY LIGHT, SEATS 1A-5A IS INOP. FOUND UNDER SEAT CABLE OFF. RECONNECTED, CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA05437 1 20080823 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ROW 1 RT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 654UA 25392 ROW 1 RT EMERGENCY LIGHT INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 EU 2008 9 30 2008UALA04191 1 20080809 A 2611 PPA120300 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LAVATORY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 407UA 456 LAV F SMOKE DETECTOR INOP. FOUND FAULTY SMOKE DETECTOR. REPLACED SMOKE DETECTOR, OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA04153 1 20080804 A 3510 MXP401600U OXYGEN SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CREW LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 844UA 1581 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. SERVICED TO 1840 PSI. OKAY FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA04132 1 20080805 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 LOWER WALL EMERGENCY LIGHT INOP ACROSS FROM DOOR 4 LT. REPLACED LIGHT ASSY. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081001 NM 2008 10 1 08FDEA04100 1 20080929 A 5740 ATTACH FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 LEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR INBOARD ATTACHMENT POINT INBOARD SURFACE FOUND PITTING CORROSI ON. 2 L 7 3 4F RT A22WE 20081001 2008 10 1 SWAA085201 4 20080923 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 773SA 27881 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085200 1 20080921 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 FOUND EMERGENCY BULLNOSE LIGHT LENS MISSING AT ROW 10 ABC. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 UPS08553400 1 20080926 A 5330 SKIN BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 424UP 25369 INSPECTION TYPE:C2 FUSELAGE SKIN HAS A DENT AT BS 392, BETWEEN STRINGER 23 AND 24 LEFT. FOUND DENT TO BE GOUGED, REMOVE D DAMAGE AND INSTALLED FASTENER TO FILL HOLE PER UPS EO B757-5330-30657 AND ATS ER 08-2999. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 ASAA0843528 1 20080922 A 5230 57094 SEAL BOEING 737 7374Q8 138447Q NM CARGO DOOR FAILED A ASAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 02 765AS 002200 25102 AT CRUISE FL340 CABIN ALT WARNING HORN CAME ON CABIN ALT WAS 10.5 11.0, RAN CABIN ALT WARN HORN RAPID DEPRESS CK LIST. CONTROLLED CABIN AT ABOUT 11 12 THOUSAND BEGAN NORMAL DESCENT AND DECLARED EMERGENCY DEVIATE YVR. ABOUT FL190 CABIN PRE SS FELT LIKE IT WAS EXCESSIVE. CRACKED OUTFLOW OPEN AND GOT 4K FT MIN INCREASE CLOSED OUTFLOW + CAUGHT CABIN AGAIN. CA BIN GOT COLD, PRESSURIZED AIRCRAFT PER MM 05 51 91 702 001 AND FOUND THE FOLLOWING. UNABLE TO PRESSURIZE USING ONE AIR C OND PACK REQUIRED RT ENG AND APU AS BLEED SOURCE AND BOTH PACKS OPERATING TO REACH 4 PSID. DECAY RATE FROM 4 PSID TO 2. 5 PSID WAS 50 SECS. OUT OF LIMITS. FOUND AIR LEAKS AT NOSE GEAR DOWNLOCK VIEWER IN NOSE W/W AND FROM MAIN CARGO DOOR. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085155 1 20080923 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 307SW 22947 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT STA 360, STR 21R. REMOVED AND REPLACED STRINGER SPLICE PE R SRM. 2 L 7 2 4F RT A16WE 20081001 NE 2008 10 1 2008UALA05820 2 20080920 A 7297 WIRE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE NR 2 ENGINE BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 675UA 29243 NR 2 ENG FOUND WIRES BURNED 6 INCHES BELOW CORE DISCONNECT D4216P. REPLACE WIRE W3538-202B-18, W3538-202R-1 8 AND SHIEL D, PINS 5, 6, 7 AT D4216P TO IDG D10966 PINS 9 AND 10. REF WD 24-21-21. WIRE 561-0734 AOG NR R2902. REF WIRE LIST PG 1 927. ROUTED WIRE FROM IDG D10966 P-9,10 TO D4216P. PINNED AND SEC'D D10966. STILL NEED CONN D4216P. HARNESS SEC'D FM IDG TO UPPER CLAMPS. COMPLETED WIRE REPAIR & PINS INSTALLED IN NEW CONNECTOR. SECURED ALL BUNDLES, SAFETY WIRED REMAIN ING BACK SHELLS, AND SECURED ALL CONNECTORS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081001 NM 2008 10 1 2008UALA05757 1 20080916 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 817UA 873 FLOORBEAM 95 CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED BOLTS AT FWD END OF BEAM. REMOVED BEAM AND SPLICE. INSTALL ED ALL BRACKETS. ATTACHED TO BEAM 95, INSTALLED AND MOUNTED TO FRAME 65 AND 66. INSTALLED FORWARD SPLICE AT FRAME 64. INSTALLED BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081001 NM 2008 10 1 08FDEA04072 1 20080927 A 5311 691632998 FRAME BOEING 727 727227 1384078 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 RT AFT EMERGENCY EXIT HATCH CUTOUT, AFT FRAME DAMAGED AT RIVET LOCATION BLENDED AREA OF FRAME, FABRICATED REPAIR PARTS, CAD PLATED, TREATED, PRIMED AS NEEDED. INSTALLED ALL PARTS AND REMOVED FASTENERS AND SIDEWALLS FOR ACCESS REF EA 7-5310 -114033. 2 L 7 3 4F A3WE 20081001 NM 2008 10 1 08FDEA04074 1 20080927 A 7830 32726024 ACTUATOR GE DOUG MD11 MD11F 3023600 NM GE CF6 CF680 30025 NE THRUST REVERSER BROKEN A FDEA O OTHER O OTHER LD LANDING 1 CE 21 603FE 591101 48459 FOUND NR 1 LT T/R DAMAGED. FOUND LT LWR SCREWJACK BROKE OFF AND DAMAGED THE TRANSLATING COWL, DAMAGED PARTS FOUND AT RU NWAY TOUCH DOWN AREA. VISUALLY INSPECTED LT WING, FLAP, AFT FUSELAGE, STAB SURFACE AND NO DAMAGE FOUND. MANUAL DEPLOY AND STOW NR 1 RT REVERSER HALF AND FOUND OK. REVERSER P/N MUST BE 683L216G04 FOR NR1 LT CONFIG PER IPC. REMOVED AND R EPLACED NR 1 ENGINE LT T/R COWL AS PER MM 78-33-01-4 AND CARRIED OUT ADJUSTMENT TEST PER MM 78-30-00-5. ALL CHECKED NORM AL. ACFT OK FOR SERVICE. CLOSED ALL NR 1 ENGINE COWLS PER MM 71-10-00. 2 L 7 3 4F 4 F RT A22WE E13NE 20081001 NM 2008 10 1 2008UALA05761 1 20080917 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 817UA 873 FLOORBEAM 140 CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED AND DISASSEMBLED FLOORBEAM. TRANSFERED HOLES TO NEW BEAM. ATTACHED SPLICE ANGLES TO ATTACH BEAM 140 TO BEAM 145. BUILT AND INSTALLED 3 BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081001 NM 2008 10 1 2008UALA05801 1 20080922 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 198UA 28716 1ST CLASS SEAT EEL LIGHT ON SIDE ARM REST IS DAMAGED SEAT LOCATION IS 4A. FOUND LIGHT DAMAGED. REPLACED LIGHT AT SEAT 4A OP CHK'D GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20081001 NM 2008 10 1 2008UALA05806 1 20080921 A 2913 65057 PUMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 663UA 27160 L HYD SYS MAINT STATUS MESSAGE. FOUND L EDP SHAFT SHEARED, REPLACED PUMP, OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081001 EU 2008 10 1 08FDEA03197 1 20080731 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CARGO SEAT TRACK HAS LIGHT CORROSION IN THE CENTER OF THE TRACK AT FRAME 78; RBL 18 INCH. REMOVED CORROSION; BLEND OUT IS WITHIN LIMITS PER A300-600 SRM 53-10-16. TREATED, PRIMED AND PAINTED AREA PER A300-600 SRM 51-23-10. 2 L 7 2 4F RT A35EU 20081001 EU 2008 10 1 08FDEA03416 1 20080814 A 5320 A53973100200 BEAM AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSION ON BEAM 10, C 67-69 RT, P45-46. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20081001 EU 2008 10 1 08FDEA03417 1 20080814 A 5315 A53978264200 FLOORBEAM AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CRACK ON FITTING FOR CROSSBEAM, C 67RH, P45. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20081001 EU 2008 10 1 08FDEA03418 1 20080814 A 5320 A53974262202 CHANNEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND IN AFT CARGO COMPARTMENT DEFORMED LONGITUDINAL PROFILE C66-69, Y140. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20081001 EU 2008 10 1 08FDEA03419 1 20080814 A 5320 A53974262202 CHANNEL AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND IN AFT CARGO COMPARTMENT DEFORMED LONGITUDINAL PROFILE C66-69, Y-525. REPAIR PERFROMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20081001 NM 2008 10 1 08FDEA03203 1 20080801 A 5320 143N534639 FLOOR SUPPORT BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 FLOOR SUPPORT AT BS 750 RBL 8 HAS CORROSION. CORROSION FOUND EXCEED SRM LIMITS. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-10-02 AND SRM 51-40-02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 08FDEA03204 1 20080801 A 5420 313N504295 FAIRING BOEING 757 75723A 1384967 NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 NR 2 PYLON STRUT AFT FAIRING LOWER PAN SKIN, AFT HAS ABOUT 1/3 INCH LONG CRACK NEAR PPSTA 276. CRACKED SKIN REMOVED AND REPLACED IAW B757-200 SSRM 54-50-70 REV 93 AND AMM 20-11-00 REV 2. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITE RIA. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 08FDEA03205 1 20080801 A 5420 313N504295 FAIRING BOEING 757 75723A 1384967 NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 NR 1 PYLON STRUT AFT FAIRING LOWER PAN SKIN, AFT FOUND WITH A CRACK ABOUT 1/2 INCHES LONG. CRACKED SKIN REMOVED AND REP LACED IAW B757-200 SRM 54-50-70 REV 93 AND AMM 20-11-00 REV 2. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20081001 WP 2008 10 1 08FDEA03207 1 20080801 A 5315 NDA6324 FLOORBEAM DOUG DC10 DC1030F 3023504 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 FWD CARGO COMPT, CRACK ON BEAM. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 2008UALA05807 1 20080922 A 4930 211734220 CONTROL UNIT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE APU FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 666UA 29238 APU FAULT. ECU FOUND FAULTY. REPLACED ECU. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081001 SO 2008 10 1 SWIA200820034 1 20080903 A 3260 TARGET EMB 120 EMB120ER 3260203 SO LT MLG OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 232SW 120306 LEFT MAIN WOULD NOT RETRACT. FOUND TARGET BACKED OFF ON LEFT GEAR. ADJUSTED TARGET. 2 L 7 2 4T RT A31SO 20081001 EA 2008 10 1 SWIA200820035 1 20080906 A 3222 STRUT CNDAIR CL600 CL6002C10 1390015 EA NLG DISCHARGED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 703SK 10139 "STEERING INOP" CAUTION MSG. AFTER TAKEOFF, NLG STRUT BOTTOMED OUT. OPS CHECK OF NLG STEERING NORMAL. 2 L 7 2 4F RT A21EA 20081001 WP 2008 10 1 08FDEA03212 1 20080801 A 5411 AUB70313 SPAR DOUG MD10 MD1010F 3022112 WP ZONE 400 SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 THE NR 3 PYLON STA YN 417, UPPER SPAR WEB AT THE BULKHEAD HAS 1 SHEARED FASTENER. REPLACED FASTENER IAW MD-10-10 AMM 20 -50-02-2. PERFORMED BHEC TEST ON THE NR 3 PYLON UPPER SPAR WEB AT THE BULKHEAD IAW STSPM 06-10-01.003. NO DEFECTS NOTE D. 2 L 7 3 4F RT A22WE 20081001 EU 2008 10 1 08FDEA03214 1 20080801 A 5321 A5327027300000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 MAIN DECK FLOOR BOARD 232 LG IS PUNCTURED. REMOVED DAMAGE; PREPPED FOR LAY UP. MAT ID'D; LAYED UP REPAIR PLYS AND STA RTED CURE. COMPLETED CURE AND SANDED IAW A300-600 SRM 53-10-21. 2 L 7 2 4F RT A35EU 20081001 NM 2008 10 1 08FDEA03426 1 20080814 A 5730 113N161115 SKIN BOEING 757 757236 1384971 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 LT WING REAR SPAR UPPER FITTING, UPPER SKIN LOWER SURFACE, ALONG THE AFT EDGE WHERE SKIN OVERLAPS THE REAR SPAR'S UPPER CAP, IS CORRODED JUST ABOVE LT DEFUEL VALVE. REPAIRED WING PANEL IAW FEDEX EA F-5730-110881, REV -, DATED 06/19/2008 AN D SB 757-57- 0036, REV 1, DATED 06/04/92. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 2008UALA05808 1 20080922 A 5754 SKID SHOE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT WING SLAT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 570UA 26678 LEFT WING, AFT OF NR 3 LEADING EDGE SLAT ON TOP OF WING, A PREVIOUS OVERLAY REPAIR IS PEELING UP. AREA 2 BY 9 INCHES. DAMAGE BETWEEN LEADING EDGE SLAT AND FWD WING SPAR. PREVIOUS HOT BOND REPAIR ON NR 3 L/E SLAT IS SEPARATING. REMOVED DA MAGED MATERIAL FROM SLAT. NEW CORE MATERIAL CUT AND READY TO POT IN. FITTED HONEYCOMB FILLER MATERIAL. COMPLETED REPA IR IAW 51-70-10. 2 L 7 2 4F 4 F RT A2NM E17NE 20081001 NM 2008 10 1 2008UALA05809 1 20080921 A 3000 8106012 VALVE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE RT ENGINE INOPERATIVE A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 792UA 26934 ANTI ICE ENG R -EICAS STATUS MESSAGE. RT ANTI-ICE VALVE FAILED. REPLACED VALVE. OPS CHECKS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081001 NM 2008 10 1 2008UALA05811 1 20080919 A 5320 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 605-625 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 EXTERNAL FUSELAGE BETWEEN BS 605 AND 625 AND BETWEEN STR 16L AND 17L, PREVIOUS REPAIR DOUBLER IS DENTED. MAJOR REPAIR A CCOMPLISHED, REMOVED DAMAGED DOUBLER AND INSTALLED SKIN DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 NM 2008 10 15 SWAA085421 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 2008UALA05814 1 20080919 A 2597 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 RT OVER WING SLIDE BOTTLE FAILS PRESSURE TEST. FOUND WIRE LEADING TO CONNECTOR DO5542 BROKEN. REPAIRED WIRE. OPS CHEC KS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081001 NM 2008 10 1 2008UALA05816 1 20080920 A 3350 80541 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY LIGHT FWD GALLEY RT WALL INOP. RELAMPED. CHECKS OK 2 L 7 4 4F 4 F RT A20WE E24NE 20081001 NM 2008 10 1 2008UALA05817 1 20080920 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY LIGHT FROM ROW 35 THRU 45 INOP. FOUND BATTERY FAULTY. REPLACED BATTERY. CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081001 NM 2008 10 1 2008UALA05819 1 20080920 A 3350 362624 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE SEAT ROW 20A DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 325UA 23957 EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 20A. FOUND SINGLE ELEMENT AT SEAT ROW 20A DISCONNECTED. RECONNECTED. OP CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 20081001 NM 2008 10 1 08FDEA03427 1 20080814 A 5347 143N51151 SEAT TRACK BOEING 757 7572B7 1384964 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 906FD 27148 UPON REMOVAL OF SEAT TRACK AT LBL 24, BS 540-640, MAIN CABIN, IT WAS DISCOVERED THAT THERE WERE SEVERAL EXISTING ELONGAT ED FASTENER HOLES. TWO EACH AT BS 540-620 AND ONE EACH ON THE FOWARD SIDE OF BS 640. REPAIRED SEAT TRACK PER MAE EA 75 7-5335-16-F0975, REV -, DATED 06/02/2008, ON MAE NON- ROUTINE NR 68500220001. FEDEX NON-ROUTINE N01155 DOCUMENTS ACCOM PLISHMENT OF THIS REPAIR PER ABOVE NOTED MAE REFERENCES. 2 L 7 2 4F RT A2NM 20081001 EU 2008 10 1 08FDEA03329 1 20080808 A 5321 R532B387400000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 261 AH IS DAMAGED. REPAIRED CABIN FLOOR PANEL 261 AH BY FABBING A NEW PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARK ED AND APPLIED NON-SKID TAPE IAW FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20081016 NM 2008 10 16 DL757081233 1 20080926 A 5312 148N23039 BULKHEAD BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 DURING HMV AT SAA, CORROSION WAS FOUND IN THE RADIUS OF THE AFT LOWER CHORD OF THE AFT PRESSURE BULKHEAD AT STA 1862. T HE CORROSION WAS REMOVED BY BLENDING TO A DEPTH OF 0.030 INCH. THE AREA WAS TREATED FOR CORROSION PREVENTION AND APPROV ED AS IS BY BOEING ENGINEERING. A DAMAGE TOLERANCE ANALYSIS IS REQUIRED WITHIN 12 MONTHS. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 SWAA085110 1 20080916 A 3350 8200048901 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 293WN 36612 R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085109 1 20080917 A 5755 6573735 SPOILER BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED 14Y CHECK, FOUND RT WING NR 5 SPOILER CRACKED AT OUTBOARD ATTACH FITTING. REMOVED AND REPLACED NR 5 SP OILER PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085108 1 20080916 A 5322 6546546 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 827, LBL 16 TO LBL 18. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085107 1 20080916 A 3350 1619 LIGHT BOEING 737 7373T5 1384608 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085095 1 20080917 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT AT BS 450, BL 0. REPAIRED SKI N PER ER. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085106 1 20080917 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 540, STR 23L. REPAIRED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085102 1 20080917 A 5311 6546552 FRAME BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CORRODED. AT BS 827, STR 25L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085101 1 20080917 A 5311 6558280 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085100 1 20080917 A 5312 6517853 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED 18Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7, WL 183. REPAIRED WEB PER ER. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085099 1 20080917 A 5311 6546534 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 CALA0800911 1 20080917 A 5315 141T5147 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69154 30433 CABIN STATION 246 FLOORBEAM LBL 40 AFT UPPER MID CHORD FOUND CRACKED. CABIN STATION 246 FLOORBEAM LBL 40 AFT UPPER MID CHORD REPAIRED PER SRM 53-10-51 REPAIR FIG 201 REF ECRA 5310-04838. 2 L 7 2 4F RT A1NM 20081001 WP 2008 10 1 UPS08853339 1 20080916 A 2120 UNKNOWN DOUG DC8 DC871F 302199D WP COCKPIT ODOR A IPXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 01 755UP 46055 INSPECTION TYPE:N/A ATB - RETURNED TO YHM AFTER SMOKE SMELL IN C/P AT 2,000 FEET. COMPLIED WITH GENERAL INSPECTION AS P ER DC8 MM CH 5-00-00, WITH NO DEFECT NOTED AT THIS TIME. ENG RUNS CARRIED OUT WITH GENERATORS AND PACKS ON. A/C OK FOR SERVICE. COULD NOT DUPLICATE SNAG. 2 L 7 4 4F RT 4A25 20080924 EU 2008 9 24 08FDEA03141 1 20080729 A 5321 B5327063200000 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CABIN FLOOR BOARD AT FRAME 54; LBL 77 INCHES TO 97 INCHES IS BROKEN. THIS SDR WAS GENERATED IN ERROR. FOR DETAIL S SEE SDR TRACKING NR 08-3140. 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 DL76G081133 1 20080109 A 5754 SKIN BOEING 767 767332 1382001 NM NR 6 SLAT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 172DZ 29691 FOUND ON W/A NR 6 SLAT DAMAGE. REPLACED PNL 511 CB. 2 L 7 2 4F RT A1NM 20080924 NM 2008 9 24 08FDEA03274 1 20080806 A 5312 AEA05262 DOUBLER DOUG MD11 MD11F 3023600 NM MLG WW BULKHEAD CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 587FE 48489 CENTER LANDING GEAR WHEEL WELL RIGHT BULKHEAD FORWARD LOWER DOUBLER FOUND CRACKED. CRACKED DOUBLER REMOVED AND REPLAC ED WITH NEW PART AT CENTER LANDING GEAR WHEEL WELL RIGHT BULKHEAD FORWARD LOWER AREA AS PER SRM 51-33-01 VOLUME II. REP AIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 EU 2008 9 24 08FDEA03333 1 20080808 A 5321 R532B364200000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 241 MF IS DAMAGED. FABRICATED NEW PANEL IAW A300-600 SRM 53-10-20 AND FEDEX DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080925 NM 2008 9 25 08FDEA03886 1 20080915 A 5412 311N5043 BULKHEAD BOEING 757 75723A 1384967 NM ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 NR 1 STRUT MID BULKHEAD LOWER FLANGES RT FWD FITTING BOLT HOLE CRACKED. REF CARD 5450-7-5005 P1 CARD 15 OF 33. NR 1 NA CELLE STRUT MID-BULKHEAD LOWER FLANGE RT FWD FITTING BOLT HOLE REPAIRED IAW FEDEX EO F-5450-7-5005 PT 5. REPAIR IS CLAS SIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 2 4F RT A2NM 20080925 NM 2008 9 25 08FDEA03609 1 20080828 A 5330 655457561 SKIN BOEING 727 727227 1384078 NM BS 720F-740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 492FE 21530 FWD CARGO COMPARTMENT, STR 26R IS CORRODED BETWEEN STA 720F AND STA 740 WITH EXFOLIATION REMOVED RT PACK CHECK VALVE AND DUCT IAW FEDEX MM 21-20-004 AND SRM 51-30-2. CUTOUT DAMAGED AREA DIM 10 1/2 INCH LONG. FABRICATED REPAIR FILLER FROM BAC1498-147 AND REPAIR SPLICE FROM BAC1498-131 IAW B727 SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. TREATED AND PRIMED PARTS I AW B727 SRM 51-10-2. INSTALLED REPAIR PARTS IAW B727 SRM 51-10-3 NAD 51-30-2. REINSTALLED RT PACK CHECK VALVE AND DUCT IAW B727 MM 21-20-004 AND SRM 51-30-2. LEAK AND OPS CHECKS GOOD. 2 L 7 3 4F A3WE 20080925 EU 2008 9 25 08FDEA03856 1 20080912 A 2130 CABIN PRESSURE AIRBUS 300 A300B4622R 3930312 EU FAILED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 CE 21 730FD 659 SHORTLY AFTER TAKEOFF CABIN PRESS 1 AND 2 FAILED. MANUAL PRESSURE WORKED OK. TROUBLESHOT REF TSM 21-31-00. PERFORMED OPERATIONAL TEST OF PRESSURIZATION CONTROL SYSTEM REF MM 21-31-00-5. OPS CHECK NORMAL. NO DEFECTS NOTED. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03857 1 20080912 A 5730 A5735000220000 SKIN AIRBUS 310 A310222 3930315 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 LEFT WING FUEL TANK DOOR CUT OUT BETWEEN RIB 24 AND RIB 25 IN CORRODED. REMOVED CORROSION AND CHECKED LIMITS. ORIGINAL THICKNESS 0.276. MATERIAL REMOVED 0.002. REMAINING THICKNESS 0.274 AND IS FOUND TO BE WITHIN LIMITS IAW A310 SRM 57-2 0-12; PG 68; FIG 7A AND A310 SRM 57-20-12; PARA A-1 (A); FIG 201. UT GAUGE USED T 8225T. ACCOMPLISHED PFPI IAW A310 NT M 51-90-00. ALODINED AND PRIMED IAW A310 SRM 51-20-10 AND A310 SRM 57-20-12, PG 201B PARA 3-A. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03862 1 20080912 A 5730 A5735000220000 SKIN AIRBUS 310 A310222 3930315 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 LEFT WING FUEL TANK DOOR CUT OUT BETWEEN RIB 20 AND RIB 21 IS CORRODED. REMOVED CORROSION AND CHECKED LIMITS. ORIGINAL THICKNESS 0.600. MATERIAL REMOVED 0.002. REMAINING THICKNESS 0.598 AND IS FOUND TO BE WITHIN LIMITS IAW A310 SRM 57-2 0-12; PG 68; FIG 7A AND A310 SRM 57-20-12; PARA A-1 (A); FIG 201. UT GAUGE USED T 8225T. ACCOMPLISHED PFPI IAW A310 NT M 51-90-00. ALODINED AND PRIMED IAW A310 SRM 51-20-10 AND A310 SRM 57-20-12, PG 201B PARA 3-A. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03863 1 20080912 A 5340 FXA53610690201 ATTACH FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 426FE 245 MAIN DECK RT SIDE BETWEEN FR 13 AND FR 13 A, ATTACH ANGLE ABOVE GALLEY SIDE FITTING HAS A CRACK. REMOVED AND REPLACED F RAME FITTING BETWEEN FR13 AND 13A IAW SRM 51-40-00 AND 51-40-21. 2 L 7 2 4F RT A35EU 20080925 NM 2008 9 25 08FDEA03864 1 20080913 A 5712 ARB75657 RIB DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 623FE 48794 LEFT WING, LEADING EDGE COMPARTMENT RIB AT XOS 1003 FOUND CRACK. REMOVED AND REPLACED WITH NEW RIB AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03865 1 20080914 A 5320 ABA867819 INTERCOSTAL DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 620FE 48791 UPON LOWER NOSE SKIN OPEN-UP FOUND ADJACENT INTERCOSTAL AT STA 410 CRACKED. INTERCOSTAL AT STA 410, X = -1.750 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. FABRICATED INTERCOSTAL AS PER DOUGLAS DRAWING ABA8678. REPAIR CLASSIFIED A S MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03916 1 20080917 A 5347 6045007075 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 571FE 47830 UPPER CARGO COMPARTMENT SEAT TRACK 107L, FS 979 HAS A WORN LOBE AND HOLE OUT OF ROUND. BLENDED AREAS IAW SRM 53-70-00 F IG 5 SHT 1 2 ORIGINAL .145 AFTER REWORK .120 MAT. LOSS .025 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00 VOL 1 FIG 1 SHT 1. FABRICATED NEW SEAT TRACK UNDER MAE TRAVELER NR T8/758243. FABRICATED NEW SPLICE HASTS AND PLATES UNDER MAE TRAVELER NR T8/75849. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03918 1 20080917 A 5730 ARB128057 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING OUTBD L/E PANEL 527 AB IS WORN AT THE LATCH. FABBED DOUBLER REF SRM 57-00-01; VOL I. BLENDED WORN AREA AND F OUND OUT OF LIMITS REF SRM 57-00-01; VOL I. ALODINED AND PRIMED REF SRM 51-21-01, VOL II. INSTALLED DOUBLER REF SRM 5 1-35-01; VOL II. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03919 1 20080917 A 5347 NEA60227 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 MAIN CABIN SEAT TRACK AT STA 1385; LBL 75 IS WORN. REMOVED DAMAGED AREA IAW SRM 51-31-01; VOL II. MATERIAL ID FOR THE NEW TRACK S4929405 IAW SRM 53-42-01; VOL III. FABRICATED A NEW SEAT TRACK CHANNEL AND PLATE IAW SRM 53-70-00; VOL I. A LODINED, PRIMED AND PAINTED IAW SRM 51-21-02; VOL II. INSTALLED THE NEW SEAT TRACK IAW SRM 51-31-02; VOL II. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03867 1 20080914 A 5330 ABA7047517 SKIN DOUG MD11 MD11F 3023600 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 620FE 48791 NOSE SKIN LOWER PANEL INSTALLATION, REPAIR OF SKIN DENT AT BS.421.5 BETWEEN X=0 AND X=-21. REFERENCE WRI NR 53-30/5861. LOWER FUSELAGE SKIN AT STA 421.5, BETWEEN X = 0 AND X = -21 CARRIED OUT REPAIR AS PER EA NR1-5330-121688. REPAIR OF S KIN DENT AT BS 421.5 BETWEEN X = 0 AND X = -21. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 EU 2008 9 25 08FDEA03940 1 20080918 A 5315 A5378193720600 ADAPTER AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 MAIN DECK CARGO COMPARTMENT CROSS TRACK AT FRAME 32; LBL 54. DAMAGE TO ADAPTER IS BEYOND LIMITS IAW SRM 53-10-15. REMO VED DAMAGED ADAPTER IAW SRM 51-40-21. LOCATED, DRILLED & INSTALLED THE NEW ADAPTER IAW DWG 10A53791837 & SRM 51-40-21. 2 L 7 2 4F RT A35EU 20080925 GL 2008 9 25 08FDEA03600 2 20080826 A 7320 154DN3 SENSOR AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2* GL FUEL SYSTEM FAILED A FDEA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 CE 21 661FE 760 NR 1 ENGINE N1 INDICATION BECAME UNSTABLE DURING CLIMB. REPEAT WRITE-UP. THEN EGT EXCEEDED LIMITS AT 952 DEG THEN FUEL FLOW INDICATION BECAME UNSTABLE WITH SURGING AND YAW. REMOVED AND REPLACED THE FUEL FILTER AND THE TEMP INLET SENSOR ( T 1.2). REF AMM 73-12-02-4, AND 73-23-06-4. COMPLETED HIGH PWR RUN PER JRH, ALL PARAMETERS WERE WITHIN LIMITS. 2 L 7 2 4F 4 F RT A35EU E23EA 20080925 EU 2008 9 25 08FDEA03601 1 20080826 A 2750 4907905 COMPUTER AIRBUS 310 A310324 3930206 EU TE FLAPS FAILED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED DE DESCENT 1 CE 21 810FD 452 ON APPROACH TO KBUR APPROX 5000' MSL, WHEN SELECTING 20 DEGREES FLAP, T/E FLAPS STUCK AT 15 DEGREES WITH SYS 1 AND 2 FLA P FAULT LIGHTS ILLUMINATED. DIVERTED TO LAX. LANDED WITH 30/15 IAW QRH PROCEEDURES. PERFORMED THE REMAINING OF THE T /S AND FOUND NO DEFECT. REMOVED AND REPLACED SFCC 1 AND 2 IAW MM 27-51-18-4. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03952 1 20080919 A 5320 A5361112020000 SUPPORT ANGLE AIRBUS 310 A310222 3930315 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 MAIN CABIN AT C 17 AND CUSP LINE AREA THE FRAME SUPPORT ANGLE HAS CORROSION ON THE LEFT SIDE. FABRICATED, ALODINED, PRI MED AND PAINTED THE NEW BRACKET SUPPORT ANGLE LEFT SIDE IAW A310-200 SRM 51-40-21; 51-22-00 AND 51-23-10. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03336 1 20080808 A 5321 R532B373600000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 728FD 581 CABIN FLOOR PANEL 241 QH IS DAMAGED. REPAIRED CABIN FLOOR PANEL 241 QH BY FABRICATING A NEW PANEL USING THE OLD PANEL A S A TEMPLATE. LOCATED AND COUNTERBORED HOLES. POTTED CURED AND SANDED THE EDGES. POTTED AND CURED THE INSERTS. PART MARKED AND APPLIED NON-SKID TAPE IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20080925 NM 2008 9 25 08FDEA03352 1 20080809 A 5330 651842011 SKIN BOEING 727 727233 138408A NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 275FE 22040 FUSELAGE SKIN BELOW L1 DOOR CUTOUT HAS 2 SMALL DENTS BETWEEN STA 320 - 316 AND BETWEEN STR 19-20L. EVALUATED 02 DENTS B ELOW L1 DOOR USING MECHANICAL MEANS AND FOUND DENTS WITHIN LIMITS, BUT DENTS ARE LESS THAN 10 INCHES FROM THE LAP SEAM IAW SRM 53-30-1 FIG 1. PERFORMED HFEC INSPECTION AND NO DEFECTS NOTED. DENTS ACCEPATBLE "AS IS" IAW EA NR 7-5330-1223 89. 2 L 7 3 4F RT A3WE 20080925 NM 2008 9 25 08FDEA03354 1 20080809 A 5753 652811545 FAIRING BOEING 727 7272S2F 1384O81 NM NR 3 FLAP TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 LEFT WING INBD T/E LWR SURFACE, NR 3 FLAP TRACK FAIRING INBD ATTACH L- ANGLE CRACKED BETWEEN 2 FASTENERS, 12 INCHES FW D OF T/E PANELS AFT EDGE. REMOVED DAMAGED PORTION OF NR 3 FLAP TRACK FWD FAIRING INBD ATTACH L- ANGLE. FABRICATED FILL ER AND DOUBLER, AND INSTALLED. REF SRM 51-40-03 FIG 1 AND BOEING DOC NR 65-28115. THIS IS CLASSIFIED AS A MINOR REPAIR . 2 L 7 3 4F A3WE 20080925 WP 2008 9 25 08FDEA03626 1 20080828 A 5320 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 5 SPOOL BACK UP FITTING "HOLE C" HAS A CRACK INDICATION. BACK UP FITTING REQUIRES REMOVAL. REMOVED WEB ASSEMBLY AT FS 695 - 735 AND THE INTERCOSTAL AT FS 695 - 710 TO FOM IAW SRM 51-33-01; VOL II. INSTALLED BUSHINGS IN THE MCD LOWER J AMB BEAM AS REQUIRED. REMOVED AND REPLACED THE SPOOL BACK UP FITTING IAW SRM 53-50- 00; VOL I; FIG 17. RE-INSTALLED T HE WEB ASSEMBLY AT FS 695 - 735 AND THE INTERCOSTAL AT FS 695 - 710 IAW SRM 51-33-01; VOL II. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03627 1 20080828 A 5320 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 7 SPOOL BACK UP FITTING "HOLES A; B AND D" HAVE A CRACK INDICATION. BACK UP FITTING REQUIRES REMOVAL. REMOVED AND R EPLACED THE BACK UP FITTING IAW SRM 53-50-00; VOL I AND EO 9-5230-7-5000 PT2. 2 L 7 3 4F RT A22WE 20080925 EU 2008 9 25 08FDEA03628 1 20080828 A 5210 A5211041500200 FITTING AIRBUS 300 A300F4605R 3930327 EU R1 DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 650FE 726 RUST AT THE R-1 DOOR SLING ADAPTER HOLES (2 PLACES). REMOVED AND REPLACED HOIST FITTING (2EA) IAW FE A300-600 SRM 51-40 -21. 2 L 7 2 4F RT A35EU 20080925 WP 2008 9 25 08FDEA03629 1 20080828 A 5754 SKIN DOUG MD10 MD1010F 3022112 WP NR 1 SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 RIGHT NR 1 SLAT LOWER SURFACE SKIN IS CRACKED AT A FASTENER HOLE, TRAILING EDGE APPROX 1 INCH FROM THE INBD END. REMOVE D RIGHT WING NR 1 SLAT IAW AMM 27-80-01-4. OPENED SKIN FOR ACCESS. REMOVED THE CRACKED SECTION. FABRICATED A REPAIR , INSTALLED REPAIR AND RE-INSTALLED SKIN IAW SRM 57-10-00; FIG 30 AND SRM 51-35-01, VOL II. ALODINED AND PRIMED THE REP AIR IAW SRM 51-21-01; VOL II. RE-INSTALLED, AND ACCOMPLISHED GAP AND OPS CHECKS FOR THE RIGHT WING NR 1 SLAT IAW AMM 27 -80-01-4. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03805 1 20080910 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 623FE 48794 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIA HOLES, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRA CK INDICATIONS AT HOLE D. MAIN CARGO DOOR LOWER JAMB, FOR CRACKED BOLT HOLE NR D AT NR 4 SUPPORT FITTING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 10 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03808 1 20080910 A 5730 ARB2886504 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 623FE 48794 RIGHT WING LEADING EDGE LOWER SECTION AT STA XORS 372, INBOARD OF ANTI-ICE TELESCOPIC DUCT, FOUND WITH CHAFE MARKS. CHAFE MARK SMOOTHED AND REPAIR CARRIED OUT AS PER EA 1-5740-122551, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03368 1 20080810 A 5320 A6A709417 STANCHION DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 587FE 48489 FORWARD CARGO COMPARTMENT FOUND AFT BULKHEAD LOCATION WITH LINERS SUPPORTING STANCHION X = -9 INCHES WITH CORROSION. FORWARD CARGO COMPARTMENT AFT BULKHEAD LOCATION WITH LINERS SUPPORTING STANCHION X = -9 INCHES CARRIED OUT REPAIR AS PE R EA NR 1-5310-122419. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 SO 2008 9 25 SWIA200820026 1 20080724 A 5320 SUPPORT ANGLE EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 564SW 120339 AFT SUPPORT ANGLE IS CRACKED IN FRONT OF PAX DOOR. C-CHECK, REPLACED AFT SUPPORT ANGLE. 2 L 7 2 4T RT A31SO 20080925 SO 2008 9 25 SWIA200820027 1 20080722 A 5411 FRAME EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 564SW 120339 RT NACELLE O/B WHEEL WELL FRAME IS CRACKED. C-CHECK, INSTALLED REPAIR DOUBLER TO NR 2 NACELLE WHEEL WELL INNER WEB SUPP ORT INTERCOSTAL O/B SIDE. 2 L 7 2 4T RT A31SO 20080925 EU 2008 9 25 08FDEA03812 1 20080911 A 5320 A53832103206 WEB AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CRACK IN WEBS ABOVE CENTER TANK TANK AT C 47, BETWEEN BEAM 3-4 LT AND RT. REPAIR PERFORMED BY PERFORMING CRACK ST OP HOLE AND INSTALLING A DOUBLER IAW RAS /70512671/004/2008 ISS A, APPROVED BY EA 6-5315-123074. 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 08FDEA03502 1 20080819 A 5315 65208351 FLOORBEAM BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 MAIN CABIN BS 1070 LBL8 LOWER FLANGE ON FLOORBEAM HAS CORROSION. REMOVED 2 EACH PREVIOUS REPAIRS ON FLOORBEAM IAW SRM 5 1-30-2. REMOVED CORROSION ON LBL 8, FOUND AREA OUT OF LIMITS IAW SRM 51-10-6 AND 53-10-1. CUT OUT DAMAGED AREA IAW SRM 53-10-8 FIG 8. FABRICATED 2 ANGLES AND 2 FILLERS IAW SRM 53-10-8 FIG 8. INSTALLED NEW PARTS IAW SRM 53-10-8 FIG 8. 2 L 7 3 4F RT A3WE 20080926 NM 2008 9 26 08FDEA03503 1 20080819 A 5320 6517510119 WEB BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 LEFT LOWER TORQUE BOX INBD WEB LIGHTNING HOLE ROUTE OUT IS GREATER THAN SRM LIMIT. CRACK DISCOVERED ADJACENT TO ROUTE O UT. STOP DRILLED CRACK IAW SRM 51-10-1. HFEC CRACK INDICATES CRACK ENDS AT STOP DRILL IAW NDTM 51-00-00 FIG 23. FABRI CATED 1 REPAIR TO COVER ROUTE OUT AND CRACK IAW SRM 53-10-2 FIG 6. INSTALLED DOUBLER REPAIR IAW 51-40-2 FIG 1. 2 L 7 3 4F RT A3WE 20080926 NM 2008 9 26 08FDEA03504 1 20080819 A 5347 65236385 SEAT TRACK BOEING 727 727223 1384074 NM ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 SEAT TRACK WORN STA 640 BL 0. FABRICATED NEW SEAT TRACK SECTION AND INSTALLED SEAT TRACK SECTION USING PREVIOUS GOOD CO NDITION SPLICES IAW SRM 53-10-5 FIG 1 AND SRM 53-10-2 FIG 7. 2 L 7 3 4F A3WE 20080926 WP 2008 9 26 08FDEA03505 1 20080819 A 5313 AYB70131 LONGERON DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 LONGERON 52 AT STA 1480 IN THE CENTER LANDING GEAR COMPARTMENT HAS CORROSION. REMOVED DAMAGED SECTION OF LONGERON 52 IA W SRM 51-33-01; PG 1; VOL II. LOCATED AND DRILLED NEW SECTION OF LONGERON 52 AND 2 SPLICES IAW DWG AYB 7013 AND SRM 53-0 0-01; FIG 9; PG 32; VOL I. ALODINED AND PRIMED NEW SECTION OF THE LONGERON AND 2 SPLICES IAW SRM 51-21-01; PGS 21 7 24 ; VOL II. APPLIED TOP COAT OF PAINT IAW SRM 51-21-01; PG 1; VOL II. PART MARKED NEW LONGERON FX AYB 7013-1 IAW GMM 7- 0-1001. INSTALLED NEW SECTION OF LONGERON AND 2 SPLICES IAW SRM 51-33-01; PG 1; VOL II AND SRM 53-00-01, FIG 32; VOL I . 2 L 7 3 4F RT A22WE 20080926 EU 2008 9 26 08FDEA03828 1 20080911 A 5321 B5327027602300 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 MAIN CABIN FLOOR BOARD IS TORN BETWEEN FRAME 58 AND FRAME 60, RBL 18 AND RBL 37. FABRICATED A NEW PANEL IAW DWG SRZ 25- 005; REV "G". PART MARKED IAW GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03829 1 20080911 A 5321 B5327027500300 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 MAIN DECK CARGO COMPARTMENT FLOORBOARD 252 NH HAS A TORN CORNER BETWEEN FRAME 58 AND FRAME 60; RBL 0 AND RBL 18. FABBED A NEW PANEL IAW DWG SRZ 25-005; REV "G". PART MARKED IAW GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03830 1 20080911 A 5321 A5327027801800 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 MAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 60 AND FRAME 62, RBL 18 AND RBL 37. FABBED A NEW PANEL IA W DWG SRZ 25-005, REV "G". PART MARKED IAW GMM 7- 0-1000. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03832 1 20080911 A 5321 A5327400500053 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 MAIN DECK CARGO COMPARTMENT FLOORBOARD 262 AH IS TORN BETWEEN FRAME 77 AND FRAME 80, RBL 57 AND RBL 70. FABRICATED FLOO RBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03833 1 20080911 A 5321 A5327400500053 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 MAIN DECK CARGO COMPARTMENT FLOORBOARD IS CRACKED BETWEEN FRAME 77 AND FRAME 88; RBL 30 AND RBL 45. FABRICATED FLOORBOA RD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080926 EU 2008 9 26 08FDEA03838 1 20080911 A 5321 B5327048401400 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 MAIN DECK CARGO COMPARTMENT FLOORBOARD IS TORN BETWEEN FRAME 37 AND FRAME 38.2; RBL 17 AND RBL 34. NR 242 MF FABRICATE D FLOORBOARD IAW DWG SRZ 25-005; REV "G". PART MARKED PANEL IAW GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20080929 NM 2008 9 29 UPS08553320 1 20080819 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM BS 335-440 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:3C MAIN CARGO SEAT TRACK IS CORRODED ON O/B FLANGE AND RADIUS BS 335-440 LBL 45, WL 208. REPAIRED OUT O F LIMITS CORROSION PER EO 08-2794 AND UPS EO B757-5340-30527-A. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 UPS08553321 1 20080814 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 1640 S23-24R DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:3C PREVIOUS REPAIR ARE OF THE BS 1640 FRAME STR 23R TO STR 24R EO REPAIR B757-5310-27668A REQUIRED. REP ORT FINDINGS TO CUSTOMER. REMOVE PREVIOUS REPAIR REPORTED FINDING AND REPAIR BS 1640 FRAME FROM STR 23R TO 24R PER EO B 757-5310-27668-B. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 UPS08553322 1 20080911 A 5610 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 442UP 27387 F/O'S (R2) SLIDING WINDOW HAS MOISTURE INGRESS AND CRACKING AROUND ENTIRE PERIPHERY. REMOVED AND REPLACED F/O'S R2 SLID ING WINDOW PER MM 56-11-02-4. CHECKS OK. 2 L 7 2 4F RT A2NM 20080929 NM 2008 9 29 2008UALA05821 1 20080920 A 5240 RUB STRIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR GATE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 DOOR R2 LWR GATE LWR RUB STRIP CRACKED. FOUND CORROSION AND OVERSIZED HOLES FOR STRIP ATTACH. REPLACED GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 20080924 NM 2008 9 24 08FDEA03566 1 20080823 A 3230 S4913807AS04500 CABLE DOUG MD11 MD11F 3023600 NM MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 524FE 48480 ON TAKEOFF RT MAIN GEAR INDICATED UNSAFE AFTER RAISING HANDLE. ALSO, CONFIRMED ON SD. QRH HAD US CYCLE. SAME INDICATI ON, ON GEAR DOWN, ALL INDICATED SAFE. INSTALLED NEW TARGET RT MLG GEAR WELL DOOR 32-61-15-4. ADJ CLEARANCE BET PROX SE NSOR AND THE TARGET ASSEMBLY 32-61-15-4. REMOVED AND REPLACED RT MLG FOLLOW UP CTL CABLE 20-20-06-2. CARRIED LANDING G EAR POSITION FOLLOW UP CABLE ADJ 32-31-00-010-021. PERFORMED LANDING GEAR EXT/RET IAW AMM 32-30-00-00 FOUND SATIS. 2 L 7 3 4F RT A22WE 20080924 EU 2008 9 24 08FDEA03375 1 20080811 A 5297 CONNECTOR AIRBUS 300 A300F4605R 3930327 EU DOOR WARNING SYS DISCONNECTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 650FE 726 WHILE PERFORMING THE RESIDUAL CABIN PRESSURE WARNING SYSTEM OPS CHECK THE LIGHT ON THE L-1 DOOR DOES NOT COME ON. FOUND LIGHT 73 WN DISCONNECTED ON THE L-1 DOOR. RECONNECTED THE CONNECTOR. OPS CHECK WAS GOOD IAW A300-600 AMM 52-73-15. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03292 1 20080806 A 5311 A5381231020001 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 FRAME 44 FROM STRINGER 25L TO STRINGER 26L, FASTENER HOLE "B" AS CALLED OUT IN EO E6-5310-7-5006 PT1 STEP 70 STILL SHOWS A CRACK INDICATION AFTER REAMING IT TO A MAX SIZE OF 0.437. REMOVED FRAME 44 SECTION FROM S22-27L IAW SRM 51-40-21, PA RA 'S 6 AND 7. RECEIVED NEW FRAME SECTION P/N A5381231020001. LOCATED AND DRILLED NEW FRAME 44 SECTION REFERENCING DWG A53812304, REV "A" AND SRM 51-40-21, PARA'S 6 AND 7. 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03293 1 20080806 A 5730 7075T60063 SKIN DOUG MD11 MD11F 3023600 NM LT WING CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 587FE 48489 LEFT WING, FIXED LEADING EDGE TELESCOPE DUCT CUTOUT REPAIR DOUBLER AT XOS 467 FOUND CHAFFED. REMOVED DAMAGED REPAIR DOU BLER AS PER SRM 51-31-01 VOLUME II. FABRICATED NEW DOUBLER AND INSTALLED AT LEFT WING FIXED LEADING EDGE TELESCOPE DUCT CUTOUT AS PER SRM 57-10-00 FIGURE 43 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 EA 2008 9 24 SWIA200820036 1 20080911 A 5610 NP13932211 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 903SW 5 5 7425 CAPTAIN'S WINDOW CRACKED AT 35000 FT (6307 09-11-08). REMOVED AND REPLACED LT SIDE WINDOW (CAPTAIN SIDE WINDOW) IAW CRJ MM 56-12-01 AND P/N, NP-139322-11 S/N ON, 08025H1360, S/N OFF: 00031H8684. 2 L 7 2 4F RT A21EA 20080924 EA 2008 9 24 SWIA200820037 1 20080908 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 988CA 7204 RIGHT LOWER EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. REPLACED RIGHT LOWER EMERGENCY EXIT SIGN. 2 L 7 2 4F RT A21EA 20080924 EA 2008 9 24 SWIA200820040 1 20080909 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 410SW 7066 EMERGENCY LIGHT BULB IN CEILING ROW 3 IS INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20080924 EA 2008 9 24 SWIA200820041 1 20080909 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 925SW 7682 LEFT FUSELAGE AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LT SIDE EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081010 NM 2008 10 10 ASAA0873539 1 20080916 A 5320 143A812619 SHIELD BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 FWD CARGO PIT RT SHIELD AT BL 21 BETWEEN BS 495 AND 500A CORRODED. RT SHIELD AT FWD CARGO PIT BL 21 BETWEEN BS 492 AND BS 500A REPLACED IAW B737 700 SRM 51 40 02 AND 53 30 15. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 ASAA0873540 1 20080917 A 5320 143A81108 SILL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 FWD CARGO DOOR SILL PLATE FAYING SURFACE ANCHOR NUT AREA CORROSION NOTED. FWD CARGO DOOR SILL PLATE REPLACED WITH NEW P ART IAW B737 700 SRM 51 40 02 REFER TO PARTIAL WORK FOR DETAILS. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085347 1 20080930 A 5330 6560552 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT BS 360, STR 15L. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085348 1 20081001 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR LOWER HINGE CUTOUT SKIN CRACKED. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081010 WP 2008 10 10 AALA200802239 1 20080829 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 557AN 53087 LGA EXTERIOR EMERGENCY LIGHTS AT AFT RT AND LT HAND FUSELAGE INOPERATIVE. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHTS AT AFT RT AND LT HAND FUSELAGE. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081010 WP 2008 10 10 AALA200802238 1 20080829 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9629H 53599 LGA EMERGENCY LIGHT AT SEAT 16D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT A6WE 20081010 NM 2008 10 10 AALA200802231 1 20080828 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 179AA 32397 JFK EMERGENCY LIGHTS AT SEAT 31D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 AALA200802236 1 20080828 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 179AA 32397 JFK EMERGENCY LIGHTS AT SEAT 36D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 36D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 AALA200802250 1 20080830 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 766AN 32880 DFW EMERGENCY LIGHT AT SEAT 35C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 35C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081010 NM 2008 10 10 AALA200802258 1 20080901 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 197AN 32391 DFW EMERGENCY LIGHT AT RT NR 4 DOOR INOPERATIVE. REPLACED EMERGENCY LAMP FOR EMERGENCY LIGHT AT RT NR 4 DOOR. SYSTEM G ROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 AALA200802248 1 20080830 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 766AN 32880 DFW EMERGENCY LIGHT AT SEAT 25C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081010 NM 2008 10 10 SWAA085349 1 20081001 A 5330 6545890 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR UPPER HINGE CUTOUT SKIN CRACKED. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085350 1 20081002 A 2560 6557463 MOUNT BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND L1 FLOOR MOUNT SLIDE GIRT BAR CORRODED. REMOVED AND REPLACED MOUNT PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085351 1 20081002 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND LT CREASE BEAM WEB CORRODED AT BS 400 TO BS 420. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085353 1 20080930 A 3350 65C27095 CHARGER BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085358 1 20081001 A 3350 65C27095 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 492WN 33866 DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20080924 WP 2008 9 24 08FDEA02943 1 20080716 A 5712 ARB11233 RIB DOUG MD10 MD1010F 3022112 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 LEFT WING L/E INTERIOR RIB IS CRACKED AT STA XFS 580. REMOVED CRACKED RIB IAW DC/MD-10 SRM 51-35-01, 51-33-01; VOL II. MATERIAL ID FOR THE RIB IS 7075-0, 0.063, PO 613435.3. FABRICATED IAW DAC DWG ARB 1162, REV "S". ALODINED AND PRIME D IAW DC/MD-10 SRM 51-21-01; PGS 21 - 24; VOL II. INSTALLED IAW DAC DWG ARB 11621, REV "S" AND DC/MD-10 SRM 51-33-01; V OL II. 2 L 7 3 4F RT A22WE 20080924 WP 2008 9 24 08FDEA03228 1 20080804 A 2421 766972 GCU DOUG MD10 MD1010F 3022112 WP NR 2 INOPERATIVE A FDEA F A ACTIVATE FIRE EXT. UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CE 21 571FE 74072 74072 47830 AT CRUISE, NOTICED SLIGHT ELEC ODOR FOLLOWED BY LEVEL 2 ELEC ALERTS AND MOMENTARY GEN 2 OFF SWITCH ILLUMINATED. ODOR CO NTINUED TO INCREASE COMPLETED PHASE 1, O2 MASKS DONNED. DIVERTED TO KSDF EVACUATED AIRCRAFT. DEPLOYED SLIDE 1L BLEW F IRE AGENT TO ALL THREE ENGINES AND APU. FOUND NR 2 GENERATOR GCU WITH BLACK SOOT AND EVIDENCE OF HEAT DAMAGE. REMOVED AND REPLACED NR 2 GCU. AS PRECAUTIONARY REMOVED AND REPLACED EPCU RAN ALL THREE ENGINES VERIFIED ALL ELECTRICAL SYST EMS AND MOTOR INDICATIONS NORMAL. 2 L 7 3 4F RT A22WE 20080924 EU 2008 9 24 08FDEA03235 1 20080804 A 5753 A5796000720000 SKIN AIRBUS 300 A300F4605R 3930327 EU LT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 LEFT WING INBD FLAP LOWER SURFACE IS DENTED INBD OF THE FLAP TRACK. UPON FURTHER INVESTIGATION THE DENT WAS FOUND TO BE GOUGED. BLENDED GOUGE SMOOTH IAW SRM 51-73-10. FLAP SKIN WAS FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00; PG 108. R EPAIRED LOWER SKIN IAW SRM 57-50-00, PGS 222-226. 2 L 7 2 4F RT A35EU 20080924 EU 2008 9 24 08FDEA03574 1 20080825 A 5730 A5714129900000 PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 RIGHT SIDE WING BOX REAR SPAR BOTTOM PANEL HOLE "U" HAS A CRACK INDICATION AT THE 6 O'CLOCK POSITION FOUND WITH BHEC. R EPAIRED THE RIGHT SIDE WING BOX REAR SPAR BOTTOM PANEL HOLE "U" IAW EA 6-5710-117013 "FUSELAGE - AD 2005 -23 - 08 - S/B A300-57-0649R06 FRAME 47 OVERSIZE "U" HOLE, REPAIR". 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 DL76L081134 1 20080109 A 3610 ISOLATION VALVE BOEING 767 767332 1382001 NM CUSTOMER AIR INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 189DN 25990 L ISOL VALVE EICAS MSG, SWAPPING WITH CTR LEFT ISOLATION VLV. REPLACED AND CHECKED OK. PN 2780539-103. 2 L 7 2 4F RT A1NM 20080924 EU 2008 9 24 08FDEA03137 1 20080729 A 5347 A5381387120000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 MAIN CABIN SEAT TRACK BETWEEN FRAMES 43 AND 44 AT RBL 77 INCH HAS WORN SCALLOPS. REMOVED AND INSTALLED NEW SEAT TRACK I AW DWG A53610365 AND SRM 51-40- 21. FABRICATED SEAT TRACK IAW DWG A53610365. 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 DL764081135 1 20080901 A 2421 IDG BOEING 767 767432ER 1385134 NM RT ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 829MH 29700 RT ENGINE IDG DID NOT COME ON LINE AFTER START. RESET BPCU RAN ENG CHKS OK. 2 L 7 2 4F RT A1NM 20080924 NM 2008 9 24 DLM88081136 1 20080831 A 5330 5936434129 SKIN DOUG MD88 MD88 3023688 NM FS 363 L29-30R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 935DL 49722 SKIN CORROSION AT FS 363-370, L-29R-L30. CORROSION WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED. 2 L 7 2 4F RT A6WE 20080924 NM 2008 9 24 08FDEA03492 1 20080818 A 5280 STRUCTURE DOUG MD11 MD11F 3023600 NM LT MLG DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 610FE 48603 LT MAIN LANDING GEAR DOOR SUSPECTED CRACKED AT I/B MOUNTING AREA (BELOW AFT BOLT). COMPLIED WITH EA 1-5280-124351, DOOR S, MAIN LANDING GEAR DOOR, LT MLG DOOR CRACK REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 08FDEA03110 1 20080729 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT F ITTING AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB CRACKED NR 3 SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 08FDEA03111 1 20080729 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460 INCHES HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES A, B, C AND D. MAIN CARGO DOOR LOWER JAMB CRACKED NR 4 SUPPORT FITTING REMOVED AND REPLACED AS PER SR M 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 DLM90081104 1 20080724 A 5320 SUPPORT DOUG MD90 MD9030 3023690 NM STA 160-200 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DN 53395 FOUND SUPPORT CORRODED. REPLACED SUPPORT. 2 L 7 2 4F RT A6WE 20080924 NM 2008 9 24 DLM90081105 1 20080723 A 5320 SUPPORT DOUG MD90 MD9030 3023690 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DN 53395 FOUND SUPPORT CORRODED. REPLACED SUPPORT. 2 L 7 2 4F RT A6WE 20080924 NM 2008 9 24 DLM90081107 1 20080730 A 5347 SEAT TRACK DOUG MD90 MD9030 3023690 NM BS 1269 LBL 54 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DN 53395 FOUND SEAT TRACK GOUGED, REPAIRED. 2 L 7 2 4F RT A6WE 20080924 NE 2008 9 24 DL75E081109 2 20080821 A 7200 BEARING BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 706TW 33024 28165 727214 DUE TO HOC ON NR 1 ENGINE AND FAILURE OF BUMBER BEARING INSPECTION OPN 5122 LAX 20AUG. PLEASE REPLACE NR 1 ENGINE. REP LACED NR 1 ENG PER TRANS 6T103. 2 L 7 2 4F 4 F RT A2NM E17NE 20080924 NE 2008 9 24 DL76S081112 2 20080824 A 7310 GASKET BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE ENG FUEL LINE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 121DE 44679 23435 580401 HAD FUEL IMBALANCE DURING FLIGHT. LEFT SIDE WAS 1300-1400 LBS LOWER THAN RIGHT. AFTER BALANCED TOTAL FUEL WAS LESS THA N CALCULATED. DETERMINED FUEL LEAK WAS POSSIBLE AND DIVERTED TO LAS. FOUND FUEL LINE FROM FCU TO FUEL PUMP LINE GASKET LEAKING. REPLACED SAME. WET MOTOR AND IDLE RAN, NO LEAKS. 2 L 7 2 4F 4 F RT A1NM E13NE 20081010 NM 2008 10 10 SWAA085359 1 20081001 A 3350 BR2013 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 493WN 32477 FOUND EMERGENCY EXIT FLOOR LIGHT COVER MISSING AT SEAT 1C. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085361 1 20080930 A 3350 100031 SIGN BOEING 737 7373Y0 1384671 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED 22Y CHECK, R2 EMERGENCY EXIT DOOR SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085366 1 20081001 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 25R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085368 1 20081001 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FRAME CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SR M. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085372 1 20081001 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND SKIN CRACKED AT BS 500D + 16, STR 7R. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081010 2008 10 10 SWAA085378 4 20081002 A 2565 416A2200 SLIDE BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 469WN 33859 FOUND L2 DOOR SLIDE FLAPPER HANGING. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085379 1 20081002 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 500D BETWEEN STR 22L TO 23L. REMOVED AND REPLACED TIE PER SR M. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085383 1 20081002 A 3350 65C27095 BATTERY PACK BOEING 737 7377Q8 1384418 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 799SW 28209 DURING SCHEDULED HC2 CHECK, RT AFT CABIN EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081010 EU 2008 10 10 UPS08153425 1 20080924 A 5321 B5327074900000 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 231XG CRACKED FROM INSIDE. REPAIRED MAIN CABIN FLOOR PANEL 231XG REF A300-60 0 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081010 EU 2008 10 10 UPS08153426 1 20080924 A 5321 B5327081100000 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CARGO BAY DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR 1 EA ROUND BOTTOM DENT WITH INDICATION OF DELAMINATION ON UPPER SURFACE OF LT AFT MAIN CARGO COMPT FLOOR PNL. MKD 261BH. REPAIRED MAIN CABIN FLOOR PANEL 261BH REF A300-600 SRM 51-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081010 EU 2008 10 10 UPS08153433 1 20080928 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU LAVATORY INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 121UP 0806 INSPECTION TYPE:N/A LAV MIRROR EMERGENCY LIGHT OUT. RELAMPED & OPS CHECKED GOOD PER IPC 33-51-21-02. 2 L 7 2 4F RT A35EU 20081010 EU 2008 10 10 UPS08153434 1 20080929 A 5321 B5327074400000 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 232TG HAS GOUGES. REPAIRED MAIN CABIN FLOORBOARD 232TG REF A300-600 SRM 53-1 0-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081010 EU 2008 10 10 UPS08153436 1 20080929 A 5321 B5327076600200 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 251LJ HAS TEMP REPAIRS. REPAIRED MAIN CABIN FLOOR PANEL 251LJ REF A300-600 S RM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081010 2008 10 10 RYN2008F00015 4 20081001 A 3420 ADI BOEING 757 7572G5 1384912 NM FAILED A RYNA O OTHER O OTHER NR NOT REPORTED 1 GL 31 929RD 23929 F/O ADI BANKING OUT INTERMITTENTLY. REPLACED F/O ADI. (K0 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 RYN2008F00016 1 20081001 A 2150 A/C PACK BOEING 737 737* NM RIGHT MALFUNCTIONED A RYNA O OTHER O OTHER NR NOT REPORTED 1 GL 31 672RY 24672 RT PACK TRIPPED. DEFERRED RT PACK. (K) 2 L 7 2 4F RT A16WE 20081010 EA 2008 10 10 ASA2008F00001 1 20080903 A 5260 STEP CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR CRACKED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 740EV 10151 ASD AFT SIDEWALL CRACKED AT 2ND STEP RISER. CUT OUT DAMAGED ON AFT SIDE PANEL NR 2 STEP IAW REO 670-52-11-104. PERFORM ED EDDY CURRENT INSPECTION OF CUT OUT ON AIRSTAIR DOOR 2ND STEP RISER ON AFT SIDEWALL IAW REO 670-52-11-104 IAW CRJ 700, NDTM 51-20-006. NO DEFECTS NOTED 2 L 7 2 4F RT A21EA 20080924 EA 2008 9 24 SWIA200820047 1 20080909 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 413SW 7102 FLT 6769 - FORWARD CABIN EMERGENCY FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20080924 EA 2008 9 24 SWIA200820049 1 20080912 A 5610 NP13932114 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 962SW 7617 7617 7859 F/O WINDSHIELD CRACKED. REPLACED CO PILOTS MAIN WINDSHIELD, PN NP-139321-14 SN ON 08211H5273 SN OFF 05300H5950. 2 L 7 2 4F RT A21EA 20080924 EA 2008 9 24 SWIA200820051 1 20080913 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 606SK 10250 FLT 3800 - EMERGENCY LIGHT NEXT TO THE MAIN CABIN DOOR, HAS ONE INOP LIGHTBULB, RELAMPED. 2 L 7 2 4F RT A21EA 20080924 EU 2008 9 24 08FDEA03800 1 20080910 A 2810 A5517781120200 FITTING AIRBUS 300 A300F4605R 3930327 EU RT FUEL TANK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 RIGHT THS INTERNAL FUEL TANK HOIST POINT FITTING IS CRACKED AT THE FWD SPAR, ACCESS 343 BB. WORK ACCOMPLISHED ON EA 6-5 510-7-5001. 2 L 7 2 4F RT A35EU 20080924 NM 2008 9 24 08FDEA03363 1 20080810 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 587FE 48489 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B , NR C AND NR D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FABRICATED AS P ER FEDEX EA NR 1-5300-122409A, TITLE: FUSELAGE, GENERAL: MAIN CARGO DOOR LOWER JAMB SPOOL FITTING, MATERIAL SUBSTITUTION . SUPPORT FITTING NR 6 REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR BUSHING FABRICATED AND INSTALLED ON MAIN CARGO DOOR LOWER JAMB WEB AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 08FDEA03365 1 20080810 A 5347 AFA7795507 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 587FE 48489 CABIN, MAIN DECK CARGO COMPARTMENT AT APPROXIMATELY STATION 1761 TO 1821, X = -8.50 FOUND SEAT TRACK CORROSION. CABIN M AIN DECK CARGO COMPARTMENT SEAT TRACK REPAIRED FROM STA 1761 TO STA 1831, X = -8.50 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080924 NM 2008 9 24 DL76L081155 1 20080903 A 3350 SWITCH BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 181DN 25986 724687 EMERGENCY LIGHTS WILL NOT TURN OFF. REPLACED EMERGENCY LIGHT PANEL DAL P/N 331702405. 2 L 7 2 4F 4 F RT A1NM E24NE 20080925 NM 2008 9 25 QXEA200800425 1 20080418 A 5344 HINGE FITTING DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK - MCD LAY SHAFT, AFT HINGE FITTING HAS PITTING AROUND BOLT HOLES. REMOVED MCD LAY SHAFT. SEPARATED LAYSHA FT AND DRILLED OUT AFT HINGE FITTING. DRILLED UP AND INSTALL NEW HINGE FITTING REF SRM 51-40-00. INSTALLED MCD LAY SHA FT. 2 H 7 2 4T RT A13NM 20080925 NM 2008 9 25 08FDEA03888 1 20080916 A 5330 53FX130113 SKIN BOEING 727 727227 1384078 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 DURING STRINGER REPAIR AT FS 550 AND STR 26L EXISTING HOLE LOCATED IN STRINGER ONLY WAS DRILLED THRU FUSELAGE SKIN. THE HOLE THRU THE SKIN IS BETWEEN 2 MANUFACTURING SKIN FALLING ON THE EDGE OF THE FWD SKIN LEAVING NO EDGE DISTANCE. FABRI CATED REPAIR DOUBLER AND FILLER FOR SKIN DOUBLER STA 550 STR 26L REF P-F SRM 53-30-2 PG 6-8 FIG 1A. TREATED, PRIMED AND INSTALLED REPAIR DOUBLER, FILLER REF SRM 51-10-6 PG 1-7, 53-30-2 FIG 1A 53-30-2 PG 2. THIS IS CLASSIFIED AS A MINOR RE PAIR. CAT "B" REPAIR. SEE SRM 53-30-3 P7 TABLE III FOR INSPECTION REQUIREMENTS. 2 L 7 3 4F A3WE 20080925 WP 2008 9 25 08FDEA02280 1 20080616 A 5730 ARB09832 DOUBLER DOUG DC10 DC1010 3022110 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 40061 46973 RT WING MODERATE EXFOLIATION CORROSION ON LOWER BEAVER TAIL. ACCOMPLISHED EA NR 8-5710-120489. 2 L 7 3 4F A22WE 20080925 WP 2008 9 25 08FDEA03854 1 20080912 A 5730 ARB1066 SKIN DOUG DC10 DC1010 3022110 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 10060 46970 LT WING L/E FOUND CRACK ON LOWER EXT SKIN L/E. 2 L 7 3 4F A22WE 20080925 NM 2008 9 25 08FDEA03945 1 20080919 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 DURING OPEN-HOLE HFEC INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 FOUND WITH C RACK INDICATIONS AT HOLES A AND D. CARRIED OUT REPAIR AS PER SRM 53-50-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03948 1 20080919 A 5730 ARB74023 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 DURING HFEC INSPECTION, FOUND 11 FASTENER HOLES WITH CRACK INDICATIONS AT LEFT WING LOWER SKIN PANELS OUTER WING ACCES S DOOR CUTOUT BETWEEN XORS 683.400 AND XORS 713.600. REPAIRED AS PER EA 1-5710-122559, THIS REPAIR CLASSIFIED AS MINO R PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03950 1 20080919 A 5420 AUB7063501 WEB DOUG DC10 DC1030F 3023504 WP ZONE 400 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 ENGINE PYLON NR 1 FOUND 3 CRACKS ON UPPER FWD SECTION STRUCTURE, RT SIDE, FIRST CRACK 2 INCHES LONG ON INT ANGLE AT ST A YN 213, SECOND CRACK 2 INCHES LONG ON WEB AT STA YN 213 RT, THIRD CRACK 2 INCHES LONG ON WEB AT STA YN 213 LT. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03753 1 20080907 A 5711 ARB1985502 SPAR DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 594FE 48552 RIGHT WING, TRAILING EDGE REAR SPAR AT STA XORS = 197.20 LANDING GEAR BRACE SUPPORT ROD LOWER FITTING 02 EACH CRACK FO UND NEAR FASTENER. RIGHT WING TRAILING EDGE REAR SPAR AT STA XORS = 197.20 LANDING GEAR BRACE SUPPORT ROD LOWER FITTI NG REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II, AND FUEL LEAK CHECK CARRIED OUT AS PER AMM 12-11-04 AND FOUND SAT ISFACTORY. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03321 1 20080808 A 5320 651759390 INTERCOSTAL BOEING 727 7272S2F 1384O81 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 211FE 22933 MAIN DECK FLOORBEAM INTERCOSTAL UPPER CHORD IS BUCKLED/CRACKED BS 304-312, LBL 22. FABRICATED REPAIR ANGLE REF SRM 51-4 0-3 FIG 1. TREATED AND PRIMED REF SRM 51-10-2 PGS 1-9. INSTALLED REPAIR REF SRM 51-30-2 PG 1-7. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081010 EA 2008 10 10 ASA2008F00002 1 20080903 A 5260 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA AIRSTAIR DOOR CRACKED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 740EV 10151 ASD FWD SIDEWALL CRACKED AT 2ND STEP RISER. REPAIRED STEP RISER IAW 670-52-11-104 WORK COMPLETED. CUT OUT DAMAGED SECTI ON OF STEP IAW REO 670-52-11-104. PERFORMED ET INSPECTION OF CUTLINE IAW REO 670-52-11-104 IAW CRJ 700 NDTM 51-20-006. NO DEFECT FN7013735. (K) 2 L 7 2 4F RT A21EA 20081010 EA 2008 10 10 ASA2008F00003 1 20080903 A 5240 HANDLE CNDAIR CL600 CL6002C10 1390015 EA DOOR CRACKED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 740EV 10151 ASD EXTERNAL HANDLE CRACKED. REFER TO W/O 99613 EC/TC SB 670BA-52-030 FOR WORK ACCOMPLISHED FOR THE REMOVAL AND REPLACEM ENT OF THE ASD EXTERIOR HANDLE ASSY. (K) 2 L 7 2 4F RT A21EA 20081010 EA 2008 10 10 ASA2008F00004 1 20080903 A 5240 SKIN CNDAIR CL600 CL6002C10 1390015 EA DOOR CRACKED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 740EV 10151 ALSO INNER SKIN CRACKED AT FWD CORNER UNDER UPPER STEP. CUTOUT DOOR EDGE MEMBER IAW REO 670-52-11-154. PERFORMED ET INSP ECTION OF CUTLINE IAW REO 670-52 NDTM 51-20-006. NO DEFECTS NOTED. FN7013735 090708 (K) 2 L 7 2 4F RT A21EA 20081009 NM 2008 10 9 F3LA2008100600668 1 20081004 A 3251 C247360012 SERVO CONTROL AIRBUS A319 A319111 3930336 NM NLG STEERING UNRESPONSIVE A F3LA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 21 924FR 1 2030 ON TAXI OUT, SPEED LESS THAN 10KTS, AIRCRAFT SWERVED TO THE LEFT (UNCOMMANDED) AND DID NOT RESPOND TO STEERING IMPUTS. STOPPED AIRCRAFT USING BRAKES, RECEIVED ELECTRONIC CENTRALIZED AIRCRAFT MONITORING MESSAGE: WHEEL N/W STEERING FAULT. MAINTENANCE REMOVED AND REPLACED SERVO-CONTROL MODULE AND PERFORMED FUNCTIONAL TEST OF NOSE WHEEL STEERING IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 32-51-51-400-001, 32-51-00-720-003 AND 32-51-00-720-004. 2 L 7 2 4F RT A28NM 20081009 NM 2008 10 9 ASAA0853537 1 20080928 A 4940 28B5457 STARTER GEN BOEING 737 737890 1384527 NM APU FAILED A ASAA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 02 583AS 4812 35681 BLUE MAINT LIGHT ON APU ILLUMINATED. PERFORMED FIM TASK 49 40 00 810 806 CONFIRMED FAULT REMOVED AND REPLACED STARTER G ENERATOR REF MM 49 41 21 OPS & LEAK CHECK GOOD. CONFIRMED FAULT CORRECTED W CDU AND FIM TASK 49 40 00 810 806. 2 L 7 2 4F RT A16WE 20081009 2008 10 9 2008UALA04089 4 20080803 A 3441 ADIRU AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE E&E BAY MALFUNCTIONED A UALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 29 839UA 1507 FLIGHT CONTROL ALTERNATE LAW, RTFL. *S/D* RERACKED AND SECURED ALL THREE ADIRU-S IN RADIO RACK. ACCOMPLISHED TSM TASK 34-13-00-810-967 AND ACCOMPLISHED BITE TESTS OF ADIRU-S PER AMM 34-13-00 ALL GRD TESTED OK, NO FAULTS. ACCOMPLISHED AF S AND LAND TEST PER AMM 22-97-00. SYSTEM GRD TESTED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081009 NM 2008 10 9 2008UALA05940 1 20080930 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 644UA 25094 BROKEN EEL LIGHTING RIGHT SIDE IN FIRST CLASS. REPLACED BROKEN ELCTRO LUMINESCENT LIGHT STRIP & POWER RIBBON. REPLACED PLASTIC COVER AND SYSTEM. OPS CKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081009 NM 2008 10 9 SWAA085310 1 20081001 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 16L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085318 1 20081001 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 9R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085325 1 20081001 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, STRINGER CLIP CRACKED AT BS 500C TO BS 500D, STR 26R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085336 1 20081001 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 20L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085343 1 20081001 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727D, STR 14L TO STR 15L. REMOVED AND REPLACED TIE PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 ASAA0873548 1 20080917 A 5320 141A541016 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 FWD PASSENGER CABIN INTERCOSTAL CRACKED BS 328 344 LBL 46. FWD PASSENGER CABIN INTERCOSTAL REPLACED WITH NEW PART BS 32 8 344 LBL 46 IAW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 ASAA0873549 1 20080917 A 5320 141A541013 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE SCRATCHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 FWD PASSENGER CABIN SCRATCH ON FLOOR SUPPORT STRUCTURE BS 340 BS 344 LBL 10. FLOOR SUPPORT STRUCTURE MADE REPAIR PART ( ILLEGIBLE) BS 340 BS 344 LBL 10 IAW B737 700 SRM 51 40 02 & DWG 141A5410. 2 L 7 2 4F RT A16WE 20081010 2008 10 10 R612008F00009 4 20080906 A 3497 M83723 CONNECTOR EMB ERJ170 ERJ170100SU 3260403 NM TAT SENSOR BURNED A R61A O OTHER O OTHER NR NOT REPORTED 1 GL 11 807MD 17000020 CREW DETECTED ODOR SMOKE IN THE COCKPIT FOLLOWED QRH PROCEDURES DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAIN T TROUBLESHOT PROBLEM, FOUND THE TOTAL AIR TEMPERATURE CONNECTOR BURNED. REMOVED AND REPLACED CONNECTOR AND TAT SENSOR A S A PRECAUTION, OPERATIONAL CHECK OF SYSTEM CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 2 4F RT A56NM 20081010 EA 2008 10 10 A6WA200840585 1 20080828 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA CABIN AIR ODOR A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 409AW 7447 LT PACK AIR HAS AN ODOR OF OIL/ RUBBER. CLEANED LT COALESCER IAW AMM 21-51-13 PERFORMED OPS CK OF LT ACM IAW AMM 21-51- 00. NO DEFECT NOTED, NO ODOR DETECTED. (K) 2 L 7 2 4F RT A21EA 20080925 EU 2008 9 25 08FDEA03954 1 20080919 A 5347 R53070088200 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 663FE 766 MAIN DECK CARGO COMPARTMENT SEAT TRACK NR 2 RT HAS 4 SQ IN OF CORROSION AT FR 27 AND 4 SQ IN OF CORROSION AT FR 30. REM OVED LEVEL 1 CORROSION AND REMOVED DAMAGED SEAT TRACK SECTION AT TRACK NR 2RT AND INSTALLED SEAT TRACK SPLICE REPAIR BET WEEN FR 27 AND FR 30 IAW SRM 53-10-16, FIG 208, SHEET 1. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03955 1 20080920 A 5347 A53832211204 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 663FE 766 MAIN DECK CARGO COMPARTMENT SEAT TRACK NR 2 RT HAS CORROSION 3 AREAS BETWEEN FR 51 AND FR 53 REMOVED LEVEL 1 CORROSION A ND CUT OUT DAMAGED SECTION OF SEAT TRACK NR 2RT AND INSTALLED SPLICE REPAIR BETWEEN FR 51 AND FR 53 IAW SRM 53-10-16, FI G 205. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03960 1 20080922 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU RT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD FH1141 664 FOUND CHAFING MARKS ON RT CENTER FLAP TOP SKIN RIB 13-15 AND 20-21. REPAIR PERFORMED BY CUT OUT THE SKIN AREA AND CHAFI NG PLATE AT RIB 13-13A AND INSTALL AN EXTERNAL DOUBLER AND A NEW CHAFING PLATE, BLEND OUT CHAFING MARK AT RIB 20-21 AN D INSTALL A NEW CHAFING PLATE IAW RAS/FOK/230/2008 ISS A , APPROVED BY EA 6-5753-123085. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03961 1 20080922 A 5347 A25775023208 TRACK AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 HEAVY CORROSION FOUND ON ROLLER TRACK AND DURING REPAIR A HOLE WAS MISDRILLED HOL, C 63, Y140 LT. REPAIR PERFORMED BY I NSTALLING A BUSHING IN ROLLER TRACK IAW RAS/DAHAM/4025692/2008 ISS A, APPROVED BY EA 6-5317-123138. 2 L 7 2 4F RT A35EU 20080925 EU 2008 9 25 08FDEA03963 1 20080922 A 5753 SKIN AIRBUS AIRBUS 300 A300B4622R 3930312 EU NR 1 SLAT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD FW1488 664 FOUND 2 AREAS OF CHAFING MARKS ON RT SLAT NR 1 LOWER SKIN. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS IAW RAS/FOK/ 234/2008 ISS A, APPROVED BY EA 6-5742-123083. 2 L 7 2 4F RT A35EU 20080925 NM 2008 9 25 08FDEA03968 1 20080922 A 5313 ACA37961 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 DURING HFEC INSPECTION CARRIED OUT AT LEFT SIDE NOSE LANDING GEAR TRUNNION FITTING TRIM-OUT, FOUND LONGERON CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01. FABRICATED LONGERON AS PER EA 1-5310-123111, THIS REPAIR IS CLASSIFIED AS MINO R PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03969 1 20080922 A 5313 ACA37962 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 DURING HFEC INSPECTION CARRIED OUT AT RIGHT SIDE NOSE LANDING GEAR TRUNNION FITTING TRIM-OUT FOUND LONGERON CRACKED. REMOVED AND REPLACED AS PER SRM 51-35-01. LONGERON FABRICATED AS PER EA 1-5310-123112, THIS REPAIR IS CLASSIFIED AS MIN OR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03970 1 20080922 A 5347 A5A7082503 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 MAIN DECK FLOOR RBL 8.5 SEAT TRACK FLANGE FOUND CORRODED BETWEEN STA 5-11 AND STA 5-53. REPAIRED BY SECTIONAL SEAT TRAC K REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03971 1 20080922 A 5347 A5A7082503 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 MAIN DECK FLOOR RBL 8.5 SEAT TRACK FLANGE FOUND CORRODED AT APPROXIMATELY STA 5-87. REPAIRED BY SECTIONAL SEAT TRACK REP LACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03972 1 20080922 A 5347 A5A7082503 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 MAIN DECK FLOOR RBL 8.5 SEAT TRACK FLANGE AT APPROXIMATELY STA 5-75 FOUND CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT AS PER SRM 53-70-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03973 1 20080922 A 5531 AJC75151 SPAR CAP DOUG MD11 MD11F 3023600 NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 HFEC INSPECTION CARRIED OUT AND FOUND ONE CRACK INDICATION ON ONE FASTENER TO EDGE OF LEFT LOWER FORWARD SPAR CAP FORWAR D FLANGE AT LOWER VERTICAL STABILIZER. REPAIR CARRIED OUT AS PER SRM 55-20-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100. 2 L 7 3 4F RT A22WE 20080925 EU 2008 9 25 08FDEA03978 1 20080922 A 5710 A57111092203 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND DAMAGED HOLES DURING ACCOMPLISHMENT OF SB A300-57-6086 (HOLE G,T) ON HORIZONTAL FLANGE, C47, RT. REPAIR PERFORM ED BY OVERSIZING THE HOLES, NDT FOR DAMAGE FREE CONDITION AND INSTALLING A CONICAL WASHER IN HOLE T IAW RAS/70512903/024 /2008 ISS A, APPROVED BY EA 6-5710-123133. 2 L 7 2 4F RT A35EU 20080925 WP 2008 9 25 08FDEA03979 1 20080922 A 5347 NDA60223 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 MAIN DECK CARGO COMPARTMENT SEAT TRACK IS GOUGED AT STA 880; LBL 8. BLENDED GOUGES, EXCEEDS LIMITS. REMOVED FLOOR PAN ELS AT BS 775-969 LBL 28 & RBL 28 IAW SRM 51-31-01 VOL II. REMOVED SEAT TRACK FROM BS 860-900 LBL 8 IAW SRM 51-31-01 VOL II. FABBED SEAT TRACK IAW SRM 53-70-00 VOL I. ALODINED & PRIMED THE SEAT TRACK IAW 51-21-01 VOL II. INSTALLED S EAT TRACK IAW SRM 51-31-01 VOL II. INSTALLED FLOOR PANELS IAW SRM 51-31-01. 2 L 7 3 4F RT A22WE 20080925 WP 2008 9 25 08FDEA03982 1 20080922 A 5347 NEA60229 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION BETWEEN STA 1321 AND STA 1351, LBL 107. REMOVED CORROSION AND FOUN D OUT OF LIMITS IAW SRM 53-70-00. FABBED NEW TRACK, 2 HAT SPLICES & 2 SPLICE PLATES IAW SRM 53-70-00. ALODINED & PRIM ED IAW SRM 51-21-01. INSTALLED NEW SECTION IAW SRM 53-70-00. REMOVED & RE-INSTALED GRILL MOUNT & DECOMPRESSION PANEL I AW SRM 51-31-01. 2 L 7 3 4F RT A22WE 20080925 NM 2008 9 25 08FDEA03984 1 20080922 A 5347 NFA60229 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 263FE 21625 MAIN DECK CARGO COMPARTMENT SEAT TRACK HAS CORROSION BETWEEN STA 1765 AND STA 1785, LBL 106. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS IAW SRM 53-70-00. FABRICATED CHANNEL IAW SRM 53-70-00. ALODINED & PRIMED IAW SRM 51-21- 01. INS TALLED CHANNEL REPAIR IAW SRM 53-70-00. REMOVED REPLACED FLOOR PANEL AT LBL 106; STA 1760 TO 1820 IAW AMM 53-21-01-8. 2 L 7 3 4F RT A3WE 20080926 NM 2008 9 26 08FDEA03497 1 20080818 A 5313 7075T6 STRINGER BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 CORROSION ON STRINGER 6R AT BS 686 IN MAIN CABIN. CORROSION FOUND BEYOND SRM LIMITS. REPAIR CARRIED OUT IAW SRM 51-40- 02 REV 93. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 2 4F RT A2NM 20080926 NM 2008 9 26 08FDEA03357 1 20080810 A 5347 65236382 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 CORROSION AT SEAT TRACK OUTBOARD FLANGE TOP STA 425 RBL 45. FABRICATED NEW SEAT TRACK SECTION FROM BS 390 TO BS 480. F ABRICATED REPAIR SPLICES. INSTALLED NEW SEAT TRACK SECTION AND SPLICE AT BS 390 TO BS 480 RBL 45 IAW SRM 53-10-5 FIG 1 AND SRM 53-10-2 FIG 7. 2 L 7 3 4F RT A3WE 20080926 WP 2008 9 26 08FDEA03257 1 20080805 A 5751 SKIN DOUG MD10 MD1010F 3022112 WP LT AILERON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 46984 LEFT OUTBD AILERON LOWER SKIN IS CORRODED/BULGED AROUND THE HINGE FITTING. LEFT WING OUTBD AILERON WAS REPLACED ON SNRM N00728. CORROSION WAS FOUND TO BE OUT OF LIMITS. 2 L 7 3 4F RT A22WE 20080926 EU 2008 9 26 08FDEA03890 1 20080916 A 5712 A57140491205 RIB AIRBUS 300 A300B4622R 3930312 EU ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CHAFING MARKS IN RT WING STRUCTURE RIB 27-28, IN AREA OF NACA DOOR. REPAIR PERFORMED BY POLISHING THE DAMAGED STR UCTURE TO SMOOTH CONTOUR, CUT OUT DAMAGED STRUTURE AND INSTALLING A REPAIR ANGLE AT NACA DOOR SURROUND REAR STIFFENER IA W RAS BAE10076602008 ISS A, APPROVED BY EA 6-5713-123056. 2 L 7 2 4F RT A35EU 20080926 WP 2008 9 26 08FDEA03258 1 20080805 A 5751 STRUCTURE DOUG MD10 MD1010F 3022112 WP LT AILERON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 LEFT OUTBD AILERON IS BULDGING AROUND THE RIB ATTACH FASTENERS AT XOA 960. LEFT WING OUTBD AILERON WAS REPLACED ON SNRM N00728. CORROSION WAS FOUND TO BE OUT OF LIMITS. 2 L 7 3 4F RT A22WE 20080926 WP 2008 9 26 08FDEA03259 1 20080805 A 5310 DOOR FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 THE MAIN CARGO DOOR JAMB HAS A CRACK INDICATION AT FITTING NR 7; HOLE "B". REMOVED AND REPLACED THE NR 7 LOWER FITTING, CARGO DOOR LATCH SPOOL P/N AFA 7132-1 AT STA 757L LBL 112 IN REF TO SRM 51-33-01; VOL II, PG 1. INSTALLED REPAIR BUSHI NG FREEZE PLUG IN HOLE B OF LOWER JAMB UPPER AND LOWER BEAMS AT SAT 757L LBL 112 IN REF TO SRM 53-50-00; VOL I; FIG 17. 2 L 7 3 4F RT A22WE 20080926 EU 2008 9 26 08FDEA03893 1 20080916 A 5730 A57247017002 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORROSION ON TOP SKIN LOWER SURFACE ON OUTER SHROUD BOX , RIB 25-29 LT. REPAIR PERFORMED BY CUT OUT RIBS TO GAIN ACCESS, BLEND OUT THE CORROSION AND REPROTECT THE AREA AND INSTALL REPAIR ANGLES TO THE CUT RIBS IAW RAS/BAE/1007773/200 8 ISS A, APPROVED BY EA 6-5751-123100. 2 L 7 2 4F RT A35EU 20080926 NM 2008 9 26 08FDEA03370 1 20080810 A 5730 ARB74023 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 587FE 48489 8 FASTENERS HOLES FOUND CRACK INDICATIONS AS MARKED DURING OPEN-HOLE HFEC INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.400 AND STATION XORS = 713.600. REPAIR CARRIED OUT AT LEFT WING FUEL TANK LOWER SKIN CUTOUT AS PER EA NR 1-5710-122418, THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20080929 NM 2008 9 29 SWAA085065 1 20080914 A 5322 6546546 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 767 S26R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080929 NM 2008 9 29 SWAA085067 1 20080914 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM BS 500 S28R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 500, STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20080929 NM 2008 9 29 2008UALA05702 1 20080913 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY EXIT LIGHT INOP AT FLIGHT DECK CEILING. FOUND DEFECTIVE LAMP. REPLACED LAMP. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20080929 2008 9 29 2008UALA05710 4 20080913 A 2565 DHE1141 SENSOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOOR SLIDE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 815UA 867 DOOR 2R SLIDE ARMED INDICATION READS DISARMED WITH DOOR CLOSED AND SLIDE ARMED IN FLIGHT. REPLACED DOOR HOOK PROXIMITY SENSOR. ADJUSTED DOOR HANDLE SENSOR 17WV2. ALL SYSTEMS TEST NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081008 EA 2008 10 8 VNAA0809006 1 20080913 A 3350 59257 INVERTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CABIN FAILED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 05 206PS 7860 DURING SCHEDULED MX, FORWARD EMERGENCY TRACK LIGHTING AND EXIT OVER LT WING FAILED. MX R&R THE NR 2 INVERTER. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20081008 NM 2008 10 8 AALA200802144 1 20080820 A 3242 BRAKE BOEING 767 767323 1385205 NM NR 5 OVERHEATED A AALA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SW 21 39367 25194 PAP INFLIGHT T871/20AUG. REPORTED HIGH ENERGY STOP AFTER LANDING. NR 5 WHEEL BRAKE REPORTED INTERMITTENT FLAME ON TAXI . FIRE EXTINGUISHED. REPLACED NR 5 BRAKE ASSEMBLY AND NR 5 TIRE. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081008 WP 2008 10 8 AALA200802146 1 20080820 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 73444 49470 LGA EMERGENCY LIGHT AT FORWARD GALLEY DOOR INOPERATIVE. REPAIRED WIRING AT CONNECTOR FOR EMERGENCY LIGHT AT FORWARD GAL LEY DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081008 NM 2008 10 8 UIE2008F00037 1 20080912 A 7500 227565M2 RELIEF VALVE BOEING 747 747341 13848AM NM NR 3 ENGINE FAILED A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 355MC 23395 AIR TURN BACK. DURING CLIMB AT APPROX FL 230, NR 3 ENGINE FIRE HANDLE ILLUMINATED. ACCOMPLISHED FHB ENGINE FIRE PROCEDUR ES. LIGHT EXTINGUISHED AFTER THRUST LEVER SET TO IDLE. INCREASE IN NACELLE TEMP INSPECTION CARRIED OUT IAW AMM. FOUND PR ESSURE RELIEF AT FAULT. REMOVED AND REPLACED VALVE OPS CHECKED AND LEAK CHECKED OK. (K) 2 L 7 4 4F RT A20WE 20081008 NM 2008 10 8 AALA200802135 1 20080819 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 794AN 30256 ORD EMERGENCY LIGHT AT SEAT 26G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081010 NM 2008 10 10 NWAA084196309 1 20080908 A 3397 WIRE BOEING 747 747451 1384940 NM EMERGENCY LIGHT LOOSE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 669US 24224 DURING OVER NIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTS FROM ROW 51 TO 65 ABC INOPERATIVE. MAINTENANCE REPAIRED LOOSE WIR E AT PIN CONNECTION. OPS CHECKED GOOD, AND AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 4 4F RT A20WE 20081010 2008 10 10 ANCF200800022 4 20080830 A 3442 20414440406 DRIVE ASSY BOEING 767 767383 1385214 NM WX RADAR ANTENNA INTERMITTENT W ANCF A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 23 984AN 12590 24357 AIR TURN BACK DUE REPORT: "WXR FAIL DISPLAYED ON HSI WITH 02=R SYSTEM SELECTED. WXR FAIL ANTENNA ON HSI. NOTE: PREVIOUSL Y REPORTED ON FLIGHT 020 OF 8/30/2008. SWEEP (GHOST IMAGE WITH) ON HSI, WEATHER DISPLAY WITH 03=R BOTH SYSTEM SELECTED. NOTE: PREVIOUSLY REPORTED ON FLIGHT 020 OF 8/30/2008 AND FLIGHT 081 OF 8/29/2008. WXR FAIL DISPLAYED ON HSI WITH 05 BO TH SYSTEM SELECTED. WXR FAIL ANT ON HSI." PERFORMED FIM 34-43-00, FIG 103 CONFIRMED WXR ANTENNA FAULT. R/R WXR ANTENNA. IAW 34-43-05/401 TST OK ON BOTH SYSTEM. AC OK FOR SERVICE. (K) 2 L 7 2 4F RT A1NM 20081010 NM 2008 10 10 SWAA085371 1 20081001 A 5310 6547978 CREASE BEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED 18Y CHECK, FOUND LT CREASE BEAM CRACKED BETWEEN BS 346 TO BS 347. REMOVED AND REPLACED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085377 1 20081002 A 5512 65C25727 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED SPV CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 125. REPAIRED PER PAE ER. 2 L 7 2 4F RT A16WE 20081010 EU 2008 10 10 UPS08153427 1 20080928 A 5321 A5328532502000 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR CREW ENTRY AREA FLOOR PNL IS CRACKED AND DISBONDING ON OUTBOARD CORNER WHERE MARKED. REPAIRED MAIN CABIN FLOOR PANEL 221FF REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081010 NM 2008 10 10 CALA0800940 1 20081002 A 5347 141T5121 SEAT TRACK BOEING 767 767224 1385170 NM CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76156 30435 FORWARD CARGO STATION 412 CABIN FLOORBEAM SEAT TRACK FOUND CRACKED AT LBL 20. CABIN FLOORBEAM SEAT TRACK AT STATION 412 LBL 20 REPAIRED PER ECRA 5320-01907, HFEC FOUND NO CRACK. 2 L 7 2 4F RT A1NM 20081010 NM 2008 10 10 CALA0800942 1 20081002 A 5340 507946117 ATTACH FITTING BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 ATTACH CLIP STATION 294.5 LT STR 10 CRACKED. INSTALLED REPAIR/MODIFICATION PER ECRA 5311-01423. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 CALA0800943 1 20081002 A 5320 6547690 ANGLE BOEING 737 737524 1384721 NM CARGO BAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 AFT CARGO COMPARTMENT RIGHT FLOOR TO SIDEWALL TRANSITION ANGLE IS CRACKED AT STATION 747 AND STATION 727C. REMOVED DAMA GED SECTION OF AFT CARGO COMPARTMENT RIGHT TRANSITION ANGLE FROM STATION 747 TO STATION 727C, FABRICATED REPAIR FROM BAC 1496-377 EXTRUSION PO PAC45511Q, IAW B737 SRM 53-60-53. ALODINED AND PRIMED IAW B737 SRM 51-20-01. INSTALLED IAW B737 SRM 53-60-53. 2 L 7 2 4F RT A16WE 20081010 EU 2008 10 10 AALA200802251 1 20080831 A 2133 A2127346100000 COVER AIRBUS 300 A300B4605R 3930308 EU CABIN PRESSURE BROKEN A AALA A UNSCHED LANDING O OTHER UK UNKNOWN 1 SW 21 80052 460 NAS INFLIGHT T861/31AUG MCO TO SJU. CREW REPORTED PRESSURIZATION FAULT. LANDED NAS WITHOUT INCIDENT. REPLACED FLAPPER VALVE COVER. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A35EU 20081010 CE 2008 10 10 GUU2008F00055 1 20080924 A 3230 MS2417D1 RELAY BEECH 1900 1900D 1154162 CE LANDING GEAR FAILED A GUUA O OTHER O OTHER AP APPROACH 1 SO 17 69549 UE194 FLIGHT 9132 MIA/TPA PILOT DISCREPANCY. DURING APPROACH WHEN LANDING GEAR CONTROL SELECTED DOWN CIRCUIT BREAKER POPPED. HAD TO RESET SEVERAL TIMES BEFORE ALL GEAR CAME DOWN AND LOCKED 3 GREEN. C/A REPLACED LANDING GEAR RELAY. OPS CHECK N ORMAL. TEST FLIGHT SATISFACTORY. 2 L 7 2 4T RT A24CE 20081010 NM 2008 10 10 AALA200802243 1 20080830 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 799AN 30258 JFK EMERGENCY LIGHT AT SEAT 4D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 4D. SYSTEM GROUND CHECKED NORMA L OPS. 2 L 7 2 4F RT T00001SE 20081010 NM 2008 10 10 AALA200802240 1 20080829 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 646AA 24604 DFW EMERGENCY LIGHTS AT FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK AT M10796 FOR EMERGENCY LIGHTS FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 AALA200802253 1 20080831 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 376AN 25445 MIA EXTERIOR EMERGENCY LIGHTS AT LOWER FORWARD AND AFT OVERWING EMERGENCY EXIT DOOR. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHTS AT LOWER FORWARD AND AFT OVERWING EMERGENCY EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081010 NM 2008 10 10 AALA200802187 1 20080818 A 5320 143T8205 SILL BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 378AN 25447 AFW OUTER CHORD AT FORWARD CARGO DOOR CUT OUT LOWER MAIN SILL HAD CORROSION. AREA OF DISCREPANCY IS 1.2 INCH BY 1 INCH WITH A DEPTH OF .019 INCH. REPAIRED PER SRM 530001. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081010 EU 2008 10 10 YENA2008091 1 20080924 A 3610 6730C010000 VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 LEAKING A YENA O OTHER J WARNING INDICATION UK UNKNOWN 1 EA 15 621JB 13303 2491 FLT NR 26 FLL-JFK AIR RETURN TO FLL, DUAL ENG BLEED FAULT 1 FAILED AT 1200`, 2 FAILED AT 11,200`. FOUND NR 1 ENG FAN AI R VALVE LEAKING FROM DIAPHRAGM. REMOVED AND REPLACED NR 1 FAN AIR VALVE IAW 36-11-54. OPS AND LEAK CHECK OK. ENG RUN- UP IAW AMM 71-00-00, SATISFACTORY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081010 NM 2008 10 10 AALA200802234 1 20080828 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 179AA 32397 JFK EMERGENCY LIGHTS AT SEAT 34D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 34D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 AALA200802228 1 20080828 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 179AA 32397 JFK EMERGENCY LIGHTS AT SEAT 28D INOPERATIVE. REPLACED LAMP FOR LIGHT AT SEAT 28D. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 AALA200802229 1 20080828 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 179AA 32397 JFK EMERGENCY LIGHTS AT SEAT 29D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 29D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A2NM 20081010 SO 2008 10 10 SIMA200827303 1 20080927 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 630AE 145132 ON FLIGHT 4105 CREW ADVISES CEILING EMERGENCY EXIT LIGHT OVER ISLE ROW 11 IS INOPERATIVE. ACFT REMOVED FROM SERVICE. C /A RESET AND RESCUED CEILING EMERGENCY EXIT LIGHT ON ROW 11 IAW AE EMB 145 AMM STANDARD MX PRACTICES. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081010 NM 2008 10 10 2008UALA05765 1 20080917 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 528UA 25018 EEL FLOOR STRIP INOP AT FWD AFT LAV. SHORT IN EEL WIRING. REPLACED EEL STRIP. CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081010 NM 2008 10 10 2008UALA05938 1 20080929 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 AFT PIT STA 1480 BETWEEN STR 25L AND 26L FRAME IS DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FUSELA GE FRAME. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081010 NM 2008 10 10 2008UALA05955 1 20081001 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 RT AFT LIGHT BAR INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20081010 NM 2008 10 10 2008UALA05962 1 20081002 A 5320 SHEAR PLATE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 818UA 882 SHEAR PLATE AFT OF DOOR 2R BETWEEN FRAME 69 AND FRAME 70 CORRODED. REMOVED SHEAR PLATE AFT OF DOOR 2R. REPLACED WITH N EW SHEAR PLATE AFT OF DOOR 2R. INSPECTED THE INSTALLATION OF THE SHEAR PLATE AND FOUND SECURE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081010 NM 2008 10 10 2008UALA05964 1 20081001 A 2913 6506606 PUMP BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE NR 1 ENGINE LEAKING A UALA O OTHER W K INADEQUATE Q C FLUID LOSS NR NOT REPORTED 1 WP 29 671UA 30026 NR 1 ENGINE EDP IS LEAKING THROUGH DRAIN TUBE. LEAK IS BEYOND LIMITS. REPLACED NR 1 ENG EDP AND GARLOK SEAL. OKAY FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081010 NM 2008 10 10 2008UALA05965 1 20081002 A 3040 CONTROLLER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE WINDOW HEAT INOPERATIVE A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 209UA 30215 STATUS MSG WINDOW HEAT LEFT. REPLACED WINDOW HEAT CONTROLLER. OP GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081010 NM 2008 10 10 2008UALA05967 1 20081002 A 2822 7G1103600U SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT BOOST PUMP FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 642UA 25092 L FWD FUEL PUMP INDICATES PUMP ON WITH SWITCH OFF AND APU OFF. LIGHT TESTS OK. RESET CONNECTOR ON PRESSURE SWITCH, NO HELP. REPLACED LEFT FWD BOOST PUMP PRESSURE SWITCH. OPS CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081010 WP 2008 10 10 IXX2008F00092 1 20080903 A 2121 X702256D FAN DOUG DC8 DC8* WP PWA JT3D JT3D* 52039 NE DEFECTIVE A IXXA D RETURN TO BLOCK B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 SW 11 799AL 45922 AFTER LANDING, DURING TAXI IN THE CREW DETECTED AN ODOR OF SMOKE. THE CREW TURNED OFF RT RECIRCULATION FAN THE ODOR WEN T AWAY. MAINT DEFERRED RT RECIRCULATION FAN. MAINT REPLACED RT RECIRCULATION FAN, OPS CHECK GOOD IAW MM 21-21-1. AC WAS RETURNED TO SERVICE. (K) 2 L 7 4 4J 4 F F 4A25 1E8 20081010 NE 2008 10 10 IXX2008F00093 2 20080907 A 7200 LINE DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D3 52039 NE PT 2 LOOSE A IXXA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 11 71CX 45961 DURING TAKEOFF ROLL, NR (1) ENGINE WOULD NOT ACCELERATE PAST 78 PERCENT. NR 2 WITH CORRESPONDING LOW N1, FUEL FLOW AND E GT. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS. MAINT INSPECTED AND FOUND LOOSE PT2 LINE ON PRBC VALVE. MAINT RE CONNECTED LINE. OPERATIONAL CHECK GOOD. ACFT WAS RETURNED TO SERVICE. (K) 2 L 7 4 4F 4 F 4A25 1E8 20081010 WP 2008 10 10 IXX2008F00094 1 20080906 A 2697 CONNECTOR DOUG DC8 DC871F 302199D WP NR 2 FIRE LOOP DAMAGED A IXXA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 11 828BX 45993 DURING CRUISE, NR (2) FIRE WARNING LIGHT CAME ON STEADY, THE CREW SHUTDOWN NR (2) ENGINE AND DISCHARGED (1) FIRE BOTTLE , LIGHT WENT OUT. (20 MINUTES OUT, NR (2) FIRE WARNING LIGHT CAME BACK ON MOMENTARILY AND FIRE LOOPS WOULD ONLY TEST IN TERMITTENTLY, THE CREW DISCHARGED THE (2ND) BOTTLE. THE CREW LANDED WITHOUT FURTHER INCIDENT. MAINT INSP AND FOUND (4) FIRE LOOPS CONNECTORS DAMAGED. MAINT REPLACED (2) ENGINE FIRE LOOPS AND BOTH FIRE BOTTLES. OPS CHECK GOOD IAW WDM 26-0 1-01. MM 26-10, AND ERH 70.01. ACFT WAS RETURNED TO SERVICE. (K) 2 L 7 4 4F RT 4A25 20081010 SO 2008 10 10 RAIA00809004 1 20080905 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS ACTIVATED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 811HK 145256 EMERGENCY LIGHT INOPERATIVE IN THE CABIN. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB AT THE AFFECTED LIGHT ASSY. O PS CHECKED GOOD. (K) 2 L 7 2 4T RT T00011AT 20081010 NM 2008 10 10 AALA200802201 1 20080826 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 184AN 29594 DFW EXTERIOR EMERGENCY LIGHT AT LT HAND AFT DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LT HAND AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081014 NM 2008 10 14 UPS08653453 1 20080926 A 5315 141T5814136 STIFFENER BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 330UP 27756 INSPECTION TYPE:N/A CABIN STA 240 LBL 25 FLOORBEAM ATT STIFFENER CRACKED. CRACK LENGTH 1 INCH. DEFECTIVE STIFFENER REP LACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081014 NM 2008 10 14 UPS08653454 1 20080925 A 5320 451T260365 FLOOR SUPPORT BOEING 767 76734AF 1385212 NM CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 330UP 27756 INSPECTION TYPE:N/A AFT CARGO COMPT STA 1324 FLOOR SUPPORT BEAM UPPER WEB FOUND CRACKED. CRACK LENGTH 1 INCH APPROX. F LOOR SUPPORT BEAM UPPER WEB REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081014 NM 2008 10 14 UPS08653455 1 20080926 A 5320 148T731241 SUPPORT BRACKET BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 330UP 27756 INSPECTION TYPE:N/A EMP - JACKSCREW COMPARTMENT RT STA 1767.25 (STR 22) SUPPORT BRACKET FOUND CRACK. CRACK LENGTH .5 IN CH APPROX. SUPPORT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081014 NM 2008 10 14 UPS08653456 1 20080924 A 5730 SKIN BOEING 767 76734AF 1385212 NM RT WING GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 330UP 27756 INSPECTION TYPE:N/A DMID383810 - RT WING L/E SKIN GOUGE TEMP REPAIR I/B NR 2 ENG ABOVE KRUEGER FLAP. RT WING L/E SKIN A T BETWEEN ISS337.6-345.5 AREA SKIN REPAIRED AS PER RS R57-41-36117 & UPS EO B767-5730-30466-A. 2 L 7 2 4F RT A1NM 20081014 WP 2008 10 14 UPS08853469 1 20081004 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 805UP 46117 CRACK IN SKIN STA 25 STRINGER 33. CORROSION FOUND. REMOVED FASTENERS & MADE 3" C/O IN SKIN AT STA 25 L34-33R PER SRM 51-01-08-0. REMOVED CORROSION PER SRM 51-01-08. REPAIR COMPLETED REF NRC 225282 & 225283. PERMANENT REPAIR AT OR BEFORE NEXT C-CHECK PER DC8-5330-30787. 2 L 7 4 4F RT 4A25 20081014 NM 2008 10 14 UPS08M53459 1 20080806 A 5753 WEDGE DOUG MD11 MD11F 3023600 NM T/E FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:C LT WING O/B FLAP T/E DELAMINATION. REPAIRED LT WING O/B FLAP T/E WEDGE PANEL DELAMINATED AREA AS PER EN1339-08 AND UPS EO MD11-5750-30265A. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 UPS08M53461 1 20080806 A 5320 FITTING DOUG MD11 MD11F 3023600 NM CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:N/A CTR CARGO FRAME SHEAR CLIP AT STATION 1681 BILGE AREA L52 FOUND CORROSION. FRAME SHEAR CLIP CORROSI ON REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOL II REV 40. MATERIAL REMOVED 0.008" ORIGINAL THK 0.071" REMAINED 0.06 8" FOUND WITHIN LIMITS PER SRM 53-00-01 FIG 2 VOL I REV 40. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 UPS08M53465 1 20080806 A 5311 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:N/A CTR CARGO FRAME AT STA 1801 BILGE ARE L52 FOUND CORROSION. FRAME CHANNEL CORROSION REMOVED AND REPR OTECTED PER SRM 51-21-01. MATERIAL REMOVED 0.006" ORIGINAL THK 0.071" REMAINED THK 0.065" FOUND WITHIN LIMIT PER SRM 53 -30-00. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 UPS08M53466 1 20080806 A 5311 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:N/A CTR CARGO FRAME AT STA 1841 BILGE AREA BETWEEN L50 - L52 RT FOUND CORROSION. FRAME CHANNEL CORROSIO N REMOVED AND REPROTECTED AS PER SRM 51-21-01 MATERIAL REMOVED 0.008" ORIGINAL THK 0.071" REMAINED THK 0.063" FOUND WITH IN LIMIT PER SRM 53-30-00. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 UPS08M53467 1 20080806 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:N/A CTR CARGO STA 1561 - 1601 BILGE AREA LONGERON 48 RT FOUND CORROSION. CTR CARGO STA 1561 - 1601 LONG ERON RT REPAIRED AS PER SRM 53-10-00. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 UPS08M53468 1 20080806 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:N/A CTR CARGO STA 1641 BILGE AREA LONGERON 48 RT FOUND CORROSION. CTR CARGO STA 1641 L48 RT LONGERON CO RROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01. MATERIAL REMOVED 0.012" ORIGINAL THK 0.100" REMAINED THK 0.088" FO UND WITHIN LIMIT PER SRM 53-00-01. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 CALA0800948 1 20081006 A 5314 6562125 KEELBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 RIGHT KEEL BEAM HAS CORROSION ON OUTBOARD FLANGE AT STATION 500D PLUS 3 - 6. REPAIRED KEEL BEAM RIGHT SIDE PER SRM 53-6 0-12 PAGE 206 FIGURE 201. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 CALA0800949 1 20081006 A 5754 65C26602312A SKIN BOEING 737 737524 1384721 NM L/E SLAT DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 RIGHT WING NUMBER 5 SLAT TRAILING EDGE OUTBOARD END DELAMINATED. REPAIRED DELAMINATION ON OUTBOARD END OF NUMBER 5 SLAT PER B737-500 SRM 51-70-10. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 CALA0800951 1 20081006 A 3350 D71701100 BATTERY PACK BOEING 737 737824 13844BZ NM CABIN DISCHARGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 37287 31636 BATTERY PACK AT SEAT ROWS 12A AND 20A FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK FOR SEAT ROWS 12A AND 20 A PER AMM 33-51-06. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 F3LA2008100700671 1 20080929 A 2560 D5348015900600 BLANKING PLATE AIRBUS A319 A319111 3930336 NM GIRT BAR CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 931FR 52 2253 DURING C3 C-CHECK, INSPECTION NOTED THE R2 FORWARD DOOR GIRT BAR FITTING BLANKING PLATE IS CORRODED ON UPPER AND LOWER S URFACE. MAINTENANCE REMOVED CORRODED GIRT BAR BLANKING PLATE AND INSTALLED NEW, REFERNCE WORK CARD C534103-01. 2 L 7 2 4F RT A28NM 20081014 NM 2008 10 14 USAASB08093 1 20081006 A 2432 279202 CHARGER BOEING 737 7374B7 1384702 NM E&E BAY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 449US 51389 51389 24893 DURING CRUISE, EN ROUTE FROM PHL TO PBI, CREW RECEIVED BOTH IRS DC FAIL LIGHTS. CREW SUSPECTS BATTERY CHARGER INOPERATI VE. BATTERY WAS AT 18 VOLTS WHEN DISPATCH WAS CONTACTED. BATTERY WAS AT 17 VOLTS WHEN THE SECOND MESSAGE WAS SENT THAT THE CIRCUIT BREAKERS WERE ALL IN. CREW WAS INSTRUCTED TO LAND IF THE BATTERY VOLTAGE CONTINUED TO DROP. BATTERY WAS N OW AT 14 VOLTS. CREW DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. BATTERY WAS 10 VOLTS. NO EMERGENCY WAS DECL ARED. MAINTENANCE FOUND THE BATTERY CHARGER NOT CHARGING. REMOVED AND REPLACED THE BATTERY CHARGER. ALSO, REMOVED AND REPLACED MAIN BATTERY AND BUSS PROTECTION PANEL. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 AALA200802157 1 20080715 A 3350 D717010100 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 920AN 29521 TUL EMERGENCY LIGHT BATTERY PACK AT MID CABIN STATION 565 DID NOT PASS FUNCTIONAL TEST. REPLACED BATTERY PACK FOR EMERG ENCY LIGHTS AT MID CABIN STATION 565. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 AALA200802166 1 20080822 A 3350 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AA 24585 DFW LT FORWARD EMERGENCY LIGHT EXIT IDENTIFIER PLACARD IS DAMAGED. REPLACED PLACARD FOR LT FORWARD EMERGENCY LIGHT EXIT IDENTIFIER. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 WP 2008 10 8 AALA200802176 1 20080824 A 2120 TUBE DOUG DC9 DC982 3022082 WP A/C BAY BROKEN A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 70529 49921 DFW INFLIGHT T875/24AUG. CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE INDICATION FLICKERED ON AND OFF FOR ABOUT 5 SE CONDS. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED BROKEN TUBE ON RT AIR CONDITIONING PACK FLOW CONTROL VALV E AND LT AND RT PACK DUCT SEALS. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081008 NM 2008 10 8 USAA920081691 1 20080917 A 3350 P4010021 BATTERY PACK AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 808AW 1088 FLT 472 YYC PHX EEL FORWARD CABIN FLASHLIGHT NOT CHARGING. INSTALLED NEW BATTERY PACK. ALSO INSTALLED NEW SAFETY STRIP . OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081008 2008 10 8 USAA920081683 4 20080912 A 2565 RESERVOIR AIRBUS 320 A320232 3930326 EU CABIN UNKNOWN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 674AW 2359 LOG PAGE 8163605. FLT NR 567 PHX MCO. EMERGENCY EQUIPMENT. POST FLIGHT REPORT INDICATES SLIDE BOTTLE EMER R. MX R&R THE RT OFFWING ESCAPE SLIDE RESERVOIR. IAW MM 25-62-46. 2 L 7 2 4F RT A28NM 20081008 NM 2008 10 8 USAA20081690 1 20080917 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 23879 PIT FPBH MAJOR REPAIR IOG NR 4352192 HIGH FREQUENCY EDDY CURRENT REVEALED CRACK INDICATION AT 4 FASTENERS BS178, WL234, RBL5.7. REPAIRED CRACK AT FASTENERS BS178, WL234, RBL5.7 IAW B737 SRM 53-10-08 FIG 201 REPAIR 9. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 AALA200802113 1 20080815 A 3350 P4010051112 MODULE BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AM 24594 JFK EMERGENCY LIGHT AT FIRST CLASS CABIN INOPERATIVE. REPLACED MODULE FOR EMERGENCY LIGHT AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 WP 2008 10 8 08FDEA03768 1 20080908 A 5740 ARL05007 ATTACH BRACKET DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING FUEL TANK FWD FUEL LINE CLAMP ATTACH BRACKET IS CRACKED AT XORS 714; ACCESS OPENING 536 BB. REMOVED & INSTA LLED INTERCOSTAL IN REF TO SRM 51-31-01 VOL II. FABRICATED INTERCOSTAL P/N ARL 0500-7 IN REF TO DWG ARL 0500; REV "BU" . ALODINED IN REF TO SRM 51-21-01 VOL II. PART MARKED IX ARL 0500-7 IN REF TO GMM 7-0-1000. 2 L 7 3 4F RT A22WE 20081008 WP 2008 10 8 08FDEA03769 1 20080908 A 5740 ARL05007 ATTACH BRACKET DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING FUEL TANK FWD FUEL LINE CLAMP ATTACH BRACKET IS CRACKED AT XORS 738; ACCESS OPENING 536 CB. REMOVED & INSTA LLED INTERCOSTAL IN REF TO SRM 51-31-01; VOL II. FABRICATED INTERCOSTAL P/N ARL 0500-7 IN REF TO DWG ARL 0500; REV "B U". ALODINED IN REF TO SRM 51-21-01; VOL II. PART MARKED IN REF TO GMM 7-0-1000. 2 L 7 3 4F RT A22WE 20081008 WP 2008 10 8 08FDEA03770 1 20080908 A 5740 ARL050029 ATTACH BRACKET DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING OUTBD FUEL TANK FUEL LINE CLAMP ATTACH BRACKET IS CRACKED AT XORS 653; FWD & OUTBD OF ACCESS OPENING 535 BT . REMOVED & INSTALLED INTERCOSTAL IN REF TO SRM 51-31-01; VOL II. FABRICATED INTERCOSTAL P/N ARL 0500-29 IN REF TO D AC DWG ARL 0500; REV "BU". ALODINED IN REF TO SRM 51-21-01; VOL II. PART MARKED IN REF TO GMM 7-0-1000. 2 L 7 3 4F RT A22WE 20081008 WP 2008 10 8 08FDEA03771 1 20080908 A 5740 ARL050143 ATTACH BRACKET DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING FUEL TANK FUEL LINE ATTACH BRACKET IS CRACKED AT XORS 538; ACCESS OPENING 534 CT. REMOVED & INSTALLED INTER COSTAL IN REF TO SRM 51-31-01; VOL II. FABRICATED INTERCOSTAL IN REF TO DWG ARL 0501 REV "BU". ALODINED IN REF TO SRM 51-21-01 VOL II. PART MARKED IN REF TO GMM 7-0-1000. 2 L 7 3 4F RT A22WE 20081008 EU 2008 10 8 08FDEA03831 1 20080911 A 5321 B5327027200600 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 676FE 790 CABIN FLOOR BOARD 251 RG IS CRACKED BETWEEN FRAME 57.1 & FRAME 58; LBL 57 & LBL 77. FABBED NEW FLOOR PANEL IAW DWG SRZ 25-005, REV "G". PART MARKED IAW GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20081008 EA 2008 10 8 TRAX200801099 1 20080904 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 280 FWD FLOOR SUPPORT CORRODED. SUP-9/15/200. REMOVED FWD 280 SUPPORT ANGLE ( FOUND TO BE OUT OF LIMITS) ISW CRJ 700 SRM 51-42-06, BAT 7023167, DRILLED NEW FWD ANGLE IAW CRJ 200 SRM 51-40-11. (K) 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801105 1 20080904 A 5534 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 LT AFT V/STAB TO FUSELAGE DRAG ANGLE CRACKED AT 67.5% REAR SPAR DATUM. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801115 1 20080905 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 980EV 7759 JOB 8775921 OPERATION 154 RT FLOOR SUPPORT ANGLE AT FS 621 AND LBL 36 HAS A 1" CRACK. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801114 1 20080905 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 CORROSION AT FWD SIDE OF FS 319 FRAME BETWEEN STR 26 AND 27L. 9/15/2008 SUP - W/O 99022 TASKCARD N/R 00164) WORK COMPLE TED IAW REMOVED 5 RIVETS FROM THE 319 TO GAIN ACCESS TO THE CORROSION. REMOVED .004 OF CORROSION FROM THE FS 319 WITHIN LIMITS IAW CRJ 700 SRM 53-21-06. REINSTALLED RIVETS AND ALODINE, PRIME, PAINTED FS 319 FRAME IAW CRJ 700 SRM 51-42-06. D K 7022603 JOB COMPLETE. (K) 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801113 1 20080905 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 CORROSION AT AFT SIDE OF FS 295 FRAME BETWEEN STR 26L AND 26R. 9/13/2008 SUP-RESOLVED ON W/O 99022 TASKCARD NR 00165. WORK COMPLETED IAW: REMOVED (6) RIVETS FROM FS 295 BETWEEN STR 26L AND 26R TO GAIN ACCESS TO THE CORROSION. REMOVED .0 03" OF CORROSION FROM THE FS295 WITHIN LIMITS IAW CRJ700 SRM 53-21-06. REINSTALLED RIVETS AND ALODINE, PRIME, PAINTED FS 295 FRAME IAW CRJ 700 SRM 51-42-06. REINSTALLED RIVETS AND ALODINE, PRIME, PAINTED FS 295 FRAME IAW CRJ 700 SRM 51-42- 06. DK 7022603 JOB COMPLETE 9/15/2008. (K) 2 L 7 2 4F RT A21EA 20081008 EU 2008 10 8 MAL2008F00033 1 20080908 A 2751 INDICATOR SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A MALA B EMER. DESCENT N FALSE WARNING AP APPROACH 1 GL 15 456XJ 340B456 FLAP CAUTION LIGHT WENT OFF 2 TIMES. RT FLAP INDICATOR MOVE DOWN, FLAP CAUTION LIGHT ILLUMINATED. SPLIT FLAP INDICATIO N GREEN LIGHT ON. FLAPS TEST 1 PANEL, NO CONTROL PROBLEMS EMERGENCY LANDING JAN. VISUALLY VERIFIED FLAPS IN UP POSITIO N AND INDICATED AGREEMENT AND FOUND SAFE FOR 1 TIME FERRY FLIGHT FROM JAN TO MEM TO REPAIR FLAP SPLIT CAUTION MSG. R&R DUAL INDICATOR FLAP POSITION PN ON/OFF 522858. SN OFF 9809551 ON 9805739 PER AMM 27-53-10-4. OPS CHECK GOOD IAW 27-51- 00-05. 2 L 7 2 4T RT A52EU 20081008 NM 2008 10 8 KCSA081456 1 20080910 A 5320 ATTACH ANGLE BOEING 747 747122 1384872 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 DOOR OPENING REINFORCEMENT FRAME ATTACH ANGLE DAMAGED AT BS 2230, STR 25R. 2 L 7 4 4F RT A20WE 20081008 NM 2008 10 8 KCSA081457 1 20080910 A 5315 FLOORBEAM BOEING 747 747122 1384872 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 BULK PIT FLOORBEAM UPPER CHORD DAMAGED AT BS 2080, RBL 23 2 L 7 4 4F RT A20WE 20081008 EU 2008 10 8 USAA920081636 1 20080907 A 3250 C247360012 SERVO CONTROL AIRBUS 320 A320232 3930326 EU NLG STEERING FAULTY A USAA O OTHER J WARNING INDICATION LD LANDING 1 EA 19 661AW 30668 30663 1284 LOG PAGE 8174263 FLT NR 291 LAS-SEA EMERGENCY LANDING. CREW ADVISED DISPATCH OF A NOSE WHEEL STEERING FAULT. NOSE WHEE L MAY NOT CENTER. CAPTAIN DECLARED AN EMERGENCY AND REQUESTED EMERGENCY EQUIPMENT. THE LANDING WAS UNEVENTFUL AND ACFT WAS TOWED TO THE GATE. MX R&R THE NOSE WHEEL STEERING SERVO CONTROL 6GC PER AIRBUS MX MANUAL 32-51-51. 2 L 7 2 4F RT A28NM 20081008 EU 2008 10 8 USAA920081655 1 20080909 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AW 17827 17827 1935 LOG PAGE 7977295 FLT NR 720 PHX EMERGENCY LIGHT TEST FAILS EPSU EXTERNAL LOAD EMERGENCY RT. MX R&R THE RT OVERWING EMER GENCY POWER SUPPLY UNIT 12WL. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081009 EA 2008 10 9 TRAX200801102 1 20080904 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 LT 280 WEB CORRODED. 2 L 7 2 4F RT A21EA 20081009 NM 2008 10 9 USAA920081657 1 20080822 A 5315 6546810 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 SAL C19 MAJOR REPAIR NR 6097659 GALVANIC CORROSION ON FLOOR BEAM UPPER CORD AT BS967, RBL 28. REPAIRED FLOOR BEAM UPPER CORD AT BS967, RBL28 IAW B737 SRM 53-00-51. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 2008UALA05574 1 20080903 A 2611 CGAB140001 SMOKE DETECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO BAY FAILED A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 313UA 23674 FWD PIT FIRE DETECTOR LOOP -A SHOWS FAILED AND CANNOT BE RESET. FOUND FAULTY SMOKE DETECTOR. REPLACED FWD "A" LOOP FWD PIT SMOKE DETECTOR. OP CHECKS NORMAL. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081009 NM 2008 10 9 USAA920081637 1 20080904 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 23379 PIT FPBH MAJOR REPAIR EO NR 5300V152 & LOG NR 4352189. 5 INCH CRACK AFT OF BULKHEAD BS178 TO 182, WL226-234, RBL17. RE PAIRED BULKHEAD BS178 TO 182, WL226-234, RBL17 IAW B737 SRM 53-10-08 REPAIR NR 12. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 AALA200802105 1 20080815 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 637AM 24595 DFW EMERGENCY LIGHT AT AFT LT OVERWING HATCH INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT AFT LT OVERWING HATCH. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081009 NM 2008 10 9 AALA200802100 1 20080814 A 3350 CHARGER BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 DFW EMERGENCY LIGHTS AT FORWARD COACH CABIN INOPERATIVE. REPLACED CENTER FORWARD BATTERY PACK CHARGER FOR EMERGENCY LIG HTS AT FORWARD COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081009 NM 2008 10 9 AALA200802095 1 20080813 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 785AN 30005 DFW EMERGENCY LIGHT IN MID CABIN MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT IN MID CABIN. SYSTEM GROUND CHECKED N ORMAL OPS. 2 L 7 2 4F RT T00001SE 20081009 NM 2008 10 9 AALA200802094 1 20080813 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 785AN 30005 DFW EMERGENCY LIGHT IN MID CABIN MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT IN MID CABIN. SYSTEM GROUND CHECKED N ORMAL OPS. 2 L 7 2 4F RT T00001SE 20081009 NM 2008 10 9 AALA200802092 1 20080813 A 3350 OL387BPGPL LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 DFW EMERGENCY LIGHT IN MID CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN MID CABIN. SYSTEM GROUND CHECKED NO RMAL OPS. 2 L 7 2 4F RT T00001SE 20081009 EA 2008 10 9 REX2008F00048 1 20080902 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A REXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 8672A 7672 WHILE IN CRUISE AT FL300 OVER SPEED CLACKER FOLLOWED BY FLAPS FAIL CAUTION MSG. QRH FOLLOWED DECLARED EMERGENCY WITH UN EVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21. 2 L 7 2 4F RT A21EA 20081014 SO 2008 10 14 RAIA2008100800031 1 20080929 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 837HK 145255 DURING PRE FLIGHT INPSECTION, IT WAS DISCOVERED THAT SEVERAL OF THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE RESE CURED THE CONNECTOR TO THE AFFECTED LIGHT ASSEMBLIES. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081014 SO 2008 10 14 RAIA2008100800033 1 20080930 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 831HK 145232 DURING PRE FLIGHT INSPECTION, IT WAS DISCOVERED THAT ONE OF THE EMERGENCY LIGHTS WAS INOPERATIVE. MAINTENANCE REPLACED THE BULB AT THE AFFECTED LIGHT ASSEMBLY. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081014 SO 2008 10 14 RAIA2008100800035 1 20081003 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR STICKING A RAIA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 03 831HK 145232 DURING GROUND HANDLING, THE FLIGHT ATTENDANT HAD DIFFICULTY OPENING THE MAIN PASSENGER DOOR. MAINTENANCE LUBRICATED THE MAIN CABIN DOOR ROLLERS AND HANDLE. DOOR OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081014 NM 2008 10 14 YENA2008100800096 1 20081008 A 2780 SLAT EMB ERJ190 ERJ190200IGW NIR NM WING MALFUNCTIONED A YENA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 EA 15 231JB 19000033 CREW REPORTED SLATS FAIL ON APPROACH, DECLARED EMERGENCY, LANDED UNVENTFULLY. PERFORMED FIM TASK 27083-00-810-814-A AND FOUND NO FAULTS, NO MESSAGES PRESENT AT THIS MOMENT. OPERATIONAL CHECK IS OK. 2 L 7 2 4F RT A57NM 20081014 NM 2008 10 14 YENA2008092 1 20080925 A 2910 5116403 HYDRAULIC LINE EMB ERJ190 ERJ190100IGW 3260408 NM HYDRAULIC SYSTEM LEAKING A YENA O OTHER K FLUID LOSS UK UNKNOWN 1 EA 15 187JB 6084 19000009 FLT NR 1081 JFK-CLT AIR RETURN TO JFK, HYD 2 LO QTY EICAS FOLLOWED BY HYD 2 LO PRESS. C/W QRH PROCEDURE. REMOVED AND R EPLACED NR 2 ENG EDP AND LEAKING HYD PRESSURE LINE AS PER 29-11-01. LEAK CHECK OK IAW AMM 29-11-00. 2 L 7 2 4F RT A57NM 20081014 NM 2008 10 14 SWAA085405 1 20081003 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085406 1 20081003 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 20R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085384 1 20081004 A 3350 PL22300L STRIP BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 461WN 32465 DURING SCHEDULED MV1 CHECK, FOUND EEPLS STRIP CRACKED. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085385 1 20081003 A 3350 412A1120 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 737JW 27869 FOUND EMERGENCY EXIT BULL NOSE LIGHT LENS MISSING AT 1C. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085394 1 20081004 A 3350 65C27095 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081009 SO 2008 10 9 SIMA200826801 1 20080918 A 5320 14521700007 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 844AE 145682 DURING CPCP INSPECTION FOUND OMEGA BEAM SSI 53-20-11 CORRODED. REPAIRED OMEGA BEAM IAW EMB SRM 53-00-10 BY REMOVING COR ROSION AND INSTALLING A DOUBLER OVER THE CUTOUT AREA. ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081009 GL 2008 10 9 CHQA200800184 2 20080921 A 7261 4252070 CARBON SEAL EMB 135 EMB135KL 3260302 SO ALLSN AE3007 AE3007A 03030 GL NR 2 ENGINE LEAKING A CHQA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 297SK 145522 CAE312179 FLIGHT 5286, STL TO RDU. WHILE CLIMBING THROUGH FL240 THE FLIGHT CREW RECEIVED A E2 LOW OIL PRESSURE EICAS MSG. WHEN T HE ENGINE PAGE WAS BROUGHT UP ON THE DISPLAY E2 SHOWED 4 QUARTS OF OIL. THE CREW FOLLOWED THE QRH AND PULLED POWER BACK TO 88% WITH NO CHANGE IN OIL PRESSURE. THE THROTTLE WAS THEN PULLED BACK TO IDLE STILL WITH NO CHANGE IN OIL PRESSURE. THE ENGINE WAS THEN SHUT DOWN AND THE FLIGHT RETURNED TO STL AND LANDED WITHOUT INCIDENT. MX INSPECTED E2 AND FOUND TH E CARBON SEAL FOR GENERATOR NR 2 LEAKING OIL. THE SEAL WAS REPLACED AND THE ENGINE SERVICED WITH OIL AND WAS RUN WITH N O FURTHER LEAKS OR DEFECTS NOTED. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081009 SO 2008 10 9 SIMA200826603 1 20080920 A 2810 2770138101 FLAPPER VALVE EMB 145 EMB145LR 3260212 SO LT WING LEAKING A SIMA C ABORTED TAKEOFF K FLUID LOSS TO TAKEOFF 1 SW 21 928AE 14500911 ON FLIGHT 9808 CREW REPORTED AN ABORTED TAKE OFF FOR LT WING FUEL LEAKING FROM WING VENT. C/A R&R LT OUTBOARD FLAP VALV E. LEAK CHECK GOOD IAW AMM 28-11-04. ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081009 SO 2008 10 9 SIMA200826602 1 20080920 A 2700 UNKNOWN EMB 135 EMB135KL 3260302 SO FLT CONTROL VIBRATION A SIMA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 SW 21 843AE 145680 ON FLIGHT 4108 CREW REPORTED A FLUTTER/VIBRATION IN THE FLIGHT CONTROLS DURING ALL PHASES OF FLIGHT. STARTED AT 150KTS, VIBRATION FELT WITH GEAR IN UP OR DOWN POSITION. VIBRATION FELT WITH AUTO PILOT ON AND OFF, PACKS ON, CREW NOTED THE V IBRATION THROUGH FLIGHT CONTROLS AS A CONSTANT SHIMMY. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT RE MOVED FROM SERVICE. AWAITING FOLLOW UP. 2 L 7 2 4F RT T00011AT 20081009 SO 2008 10 9 SWIA200820077 1 20080923 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 564SW 120339 FORWARD EMERGENCY LIGHT INOP. (FLT 5464) ALL FORWARD EMERGENCY LIGHTS CHECK NORMAL. 2 L 7 2 4T RT A31SO 20081009 NM 2008 10 9 CALA2008100600944 1 20081006 A 5311 6556655 FRAME BOEING 737 737524 1384721 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 BODY STATION 787 AT STRINGER 25R FRAME CLOSE-OUT WEB DAMAGED. REMOVED DAMAGED WEB CLOSE-OUT AT BODY STATION 787 AT STR 25R IAW B737 SRM 51-40-02, FABRICATED NEW WEB PER BOEING DRAWING 65-56655. ALODINED AND PRIMED PER B737 SRM 51-20-01. INSTALLED NEW WEB CLOSE-OUT SECTION IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081009 EA 2008 10 9 REX2008F00049 1 20080906 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 8721B 7721 ON APPROACH WHILE SELECTING FLAPS 30 RECEIVED FLAP FAIL MSG. QRH COMPLETED, EMERGENCY DECLARED WITH UNEVENTFUL LANDING. RESET FLAP SYSTEM AND PLACED ON 72 HOUR WATCH AD 2006-12-21. 2 L 7 2 4F RT A21EA 20081009 NM 2008 10 9 USAA920081652 1 20080821 A 5311 6517684133 DOUBLER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN C19 MAJOR REPAIR NR 6124653. FRAME DOUBLER CRACKED AT BS303.9, S16L, WL216. REPLACED FRAME DOUBLER AT BS303.9, S16 L, WL216 IAW B737 SRM 51-40-02-OG. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 USAA920081654 1 20080906 A 5753 6546431279 WEDGE BOEING 737 7374B7 1384702 NM T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 456UW 25020 CLT C4 MAJOR REPAIR NR 03C30057003/017 & LOG NR 5030687. 2 AREAS OF DELAMINATION ON LT OTBD FOREFLAP WEDGE UPPER SURFAC E. REPLACED LT OTBD FOREFLAP IAW B737 AMM 27-51-37. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 QXEA200800638 1 20080609 A 5312 BULKHEAD BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK SUSPECTED CORROSION AT TOP OF X836.452 AND Y9.250 I/B OF BULKHEAD ATTACH POINT UPPER CARGO DECK. CLEANED S MALL AREA OF CORROSION IAW SRM 51-21-00 & SRM 51-26-00. HFEC INSPECTED AREA PER 1-84-7A PT 6, 51-00-02 NO CRACKS NOTED. THICKNESS CHECKED AREA PER 1-84-7A PT 1, 51-00-04. HI .048 LO .045, .003 MAT. REMOVED. PREPPED AREA WITH ETCH AND AL ODINE IAW -8 400 SRM 51-21-10 AND APPLIED PRIMER, PAINT IAW SRM -8 400 51-25-10. 2 H 7 2 4T RT A13NM 20081009 EA 2008 10 9 QXEA200800633 1 20080530 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 610QX 10033 RFD C4 CHECK CORRODED SIDE SEAT TRACK ON RT SIDE @ FS 469. REMOVED CORROSION FROM TRACK, OUT OF LIMITS IAW REO 670-53-0 0-013. REMOVED CORRODED SEAT TRACK IAW 670-53-00-013. PREPARED NEW TRACK FOR INSTALL IAW CRJ SRM 51-40-11. INSTALLED NEW TRACK IAW CRJ SRM 51-41-02. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 QXEA200800672 1 20080612 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK CORROSION FOUND UNDER LOWER TCAS ANTENNA ON STRUCTURE. REMOVED ANTENNA IAW CRJ 700 AMM 34-43-07-000-801. BLENDED CORROSION .008 MATERIAL REMOVED IAW REO670-53-21-362. PERFORMED ECI NO DEFECT NOTED IAW REO670-53-21-362. TREA TED AREA AND INSTALLED ANTENNA IAW REO 670-53-21-362 AND CRJ AMM 34-43-07. 2 L 7 2 4F RT A21EA 20081009 NM 2008 10 9 QXEA200800655 1 20080609 A 5320 STRAP BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK AFT CARGO PIT DOOR LOWER MAIN SILL STRAP UNDER PANEL 144DZ HAS CORROSION ON TOP AROUND NUTPLATE HOLES AND R IVETS BETWEEN APPROX STA X747.602 AND 774.602. POLISHED OUT LIGHT SURFACE CORROSION, NEGLIGIBLE MATERIAL REMOVED IAW Q4 00 SRM 51-20-00. UT THICKNESS CHECK IAW D8-400 NDTM PART 1 51-00-04, HFEC INSPECTED IAW D8-400 NDTM PART 6 51-00-01 NO CRACKS NOTED. MAPPED FOR ENGINEERING. FOUND WITHIN LIMIT IAW RD8/4-53-2379 INSTALL SILL, ALODINED, PRIMED. 2 H 7 2 4T RT A13NM 20081009 EA 2008 10 9 TRAX200801169 1 20080915 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A ASOA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 843AS 7310 FLAPS FAILED AT 20 DEGREES AND WOULD NOT RETRACT AFTER DEPARTURE. ENROUTE TO ATL A/C DIVERTED TO CAE DUE TO MTC. EMERG ENCY VEHICLES ROLLED AS A PRECAUTION. R&R LT BPSU IAW CRJ-200 M/M 27-51-10. OPS CK GOOD. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 TRAX200801170 1 20080914 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF RIG A ASOA K NONE N FALSE WARNING LD LANDING 1 SO 27 846AS 7328 UPON MAIN GEAR TOUCHDOWN RECEIVED NOSE GEAR YELLOW BOX. INITIATED G.A. AND RECEIVED UNSAFE CAUTION WITH NOSE GEAR RED. 3 GREEN NEXT TIME AROUND. EMERGENCY DECLARED. EMERGENCY VEHICLES ON STANDBY AS PRECAUTION. FOUND NLG DOWNLOCK PROX SE NSORS PS1GA AND PS2GA TO BE OUT OF RIG. RIGGED PROX SENSORS PS1GA AND PS2GA IAW CRJ 200 AMM 32-61-05. OPS CHECK GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 TRAX200801171 1 20080914 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 977EV 7720 LOWER EMERG EXIT SIGN NEAR FLOOR BROKEN AT PAX BOARDING DOOR. REPLACED LENS AMM 33-51-19. 2 L 7 2 4F RT A21EA 20081009 CE 2008 10 9 DXTA200803280 1 20080919 A 2120 UNKNOWN CESSNA 560 560XL 2076702 CE SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 07 643QS 5605588 STARTING THE APU WITH BLEEDS ON, SMOKE POURED OUT OF THE OVERHEAD WEMAKS AND FLOOR AREA. KLAX-KCLT. 2 L 7 2 4F RT A22CE 20081009 CE 2008 10 9 DXTA200803278 1 20080919 A 2740 TRIM SYSTEM RAYTHN DH125 HAWKER800XP 7150012 CE FAULTY E DXTA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 07 873QS 258573 AIRPLANE RUNS OUT OF FORWARD TRIM NEAR VMO AT 25000 FEET AND 310 KNOTS THE TRIM WAS AT THE FORWARD STOP. 2 L 7 2 4F RT A3EU 20081009 CE 2008 10 9 DXTA200803285 1 20080923 A 3230 UNKNOWN CESSNA 750 750 2076810 CE LANDING GEAR MALFUNCTIONED E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 940QS 7500285 AFTER TAKE OFF, RETRACTED LANDING GEAR THE MAIN GEAR RETRACTED WHILE THE NOSE GEAR INDICATED DOWN AND LOCKED. 2 L 7 2 4J RT T00007WI 20081009 NM 2008 10 9 QXEA200800639 1 20080609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK THERE IS AN AREA OF PITTING 16" TO 29" AFT OF FWD END OF NR 12 SEAT TRACK ON OTBD SIDE. BLEND OUT PITTING, FOUND WITHIN LIMITS IAW RD8/4-53-884. ORIGINAL .081" REMAINING .076" MAT REMOVED .005". HFEC INSPECTED IAW -8 400 PT 6, 51-00-01, NO CRACKS NOTED. ALODINED PRIMED AND PAINTED IAW RD 8/4-53-884 SECT 1 PG 6 APRA 6,7,8. 2 H 7 2 4T RT A13NM 20081009 NM 2008 10 9 QXEA200800642 1 20080609 A 5320 FITTING BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK FRAME CLIPS UNDER CENTER FLOOR AT STA X94. ARE CORRODED IN SEVERAL LOCATIONS. REMOVED CORROSION IAW RD8/4- 53-2344 SECT 1 SHEET 1&2 STEPS 1-2. HFEC INSPECTED IAW -8 400 NDTM PT 6, 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECK IAW -8 400 NDTM PT 1, 51-00-04. APPLIED ALODINE PRIMED AND PAINTED IAW Q400 SRM 51-21-10, 51-25-10, 51-25-15 AND 51-25 -05. 2 H 7 2 4T RT A13NM 20081009 NM 2008 10 9 2008UALA05634 1 20080908 A 3350 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 778UA 26940 EMERGENCY LIGHT BROKEN AT SEAT 39G. DISCOVERED BROKEN LAMP. REPLACED LAMP. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081009 NM 2008 10 9 2008UALA05637 1 20080907 A 3510 BOTTLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE OXYGEN SYS LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 644UA 25094 CREW OXYGEN PRESSURE BELOW 3SVC REQUIRED LIMITS (1.620 PSI). UNIT FOUND UNDERSERVICED. SERVICED O2 TO FULL. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081009 NM 2008 10 9 2008UALA05680 1 20080911 A 2621 30903822U1 SQUIB BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FIRE BOTTLE INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 FIRE EXTINGUISHING BOTTLE SQUIB CHECK FOR ENGINE NR 2, 2B-BOTTLE INOP. SQUIB FOUND INADEQUATE. REPLACED SQUIB. GROUN D CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081009 NM 2008 10 9 2008UALA05892 1 20080925 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE SEAT 1F INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 782UA 26948 FLT ATTENDANT REPORTS EEL LIGHT AT SEAT 1F IS INOP. LIGHT FOUND INOPERATIVE. REPLACED LIGHT AT SEAT 1F AFT POSITION. OPS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081009 NM 2008 10 9 2008UALA05683 1 20080911 A 3350 767 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 530UA 25043 DOOR 1L ARMED LIGHT INOP. RELAMPED DOOR 1L ARM LIGHT. AFTER RELAMP LIGHT OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081009 2008 10 9 2008UALA05684 4 20080911 A 2565 D30654 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR SLIDE UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 590UA 28708 UNABLE TO ARM DOOR 1R. SECURED LANYARD. OPS OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081009 NM 2008 10 9 2008UALA05685 1 20080910 A 2432 018550000 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MASTER FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 548UA 25396 BATTERY CHARGER STATUS MESSAGE WILL NOT ERASE. REPLACED BATTERY. OPS GOOD. NO FAULTS. 2 L 7 2 4F 4 F RT A2NM E17NE 20081009 EA 2008 10 9 QXEA200800675 1 20080612 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK NUMEROUS CORROSION SPOTS ON RT SIDE SEAT RAIL FS 483 TO 573. REMOVED CORROSION FROM SEAT TRACK AT FS 483 T O 573. .015 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013. 2 L 7 2 4F RT A21EA 20081009 NM 2008 10 9 QXEA200800640 1 20080609 A 5730 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK FUEL PANEL 524AT APERTURE HAS SLIGHT CORROSION AROUND SCREW HOLES. CLEANED LIGHT CORROSION USING SCOTCH BR ITE PAD AS PER -8 400 RD 8/4-57-445 PG 1 THRU 4 STEP 1 THRU 3. MAX MAT REMOVED .002" WITHIN LIMITS PER D8-400 RD8/4-57- 445. HFEC INSPECTED IAW 1-84-7A PT 6, 51-00-02 NO CRACKS NOTED. ALODINED IAW RD8/4-57-445 SECT 1 PG 4 ISSUE STEPS 5&6. 2 H 7 2 4T RT A13NM 20081009 EA 2008 10 9 TRAX200801155 1 20080910 A 5220 SEAL CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT LACK OF LUBE A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 826AS 7210 JOB 8721021 OPERATION 170 RT OVERWING EMERGENCY EXIT FAILED TO OPEN AT 30 10 LBF. RESOLVED ON W/0 98649 TASKCARD NR 002 20. C/A CLEANED AND APPLIED DC33 TO SEAL AND PINS ON RT OVERWING EMER EXIT. PERFORMED FUNC TEST OF EXIT IAW CRJ 200 AM M 52-21-00-720-801. FOUND HANDLE OPERATING WITHIN LIMITS AT THIS TIME. ASARII C/W 5300014 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 TRAX200801138 1 20080908 A 3350 COVER CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER NR NOT REPORTED 1 SO 27 826AS 7210 JOB 8721021 OPERATION 105 LT WINDSCREEN EXIT SIGN COVER IS BROKEN ON CORNER. RESOLVED ON W/O 98649 TASKCARD NR 00131. C/A R&R EXIT SIGN COVER ON LT WINDSCREEN IAW CRJ 200 AMM 33-51-13-400-801. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 TRAX200801191 1 20080918 A 5230 ANGLE CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 931EV 8015 JOB 8801525 OPERATION 79 CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX .3" IN LENGTH. RESOLVED ON W/0 100588 TA SKCARD NR 00271 C/A REMOVED DAMAGED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET IAW CRJ 200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 20081009 WP 2008 10 9 08FDEA03898 1 20080916 A 5730 ARC12437 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING INBD LOWER TE PANEL 545 BB IS WORN. PANEL FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01. FABRICATED IAW DWG ARC 1283. HEAT TREATED IAW TPS 1003. ALODINED & PRIMED IAW SRM 51-21-01. PAINTED IAW SRM 51-21-02. PART MARKED IAW GMM 7 -0-1001. 2 L 7 3 4F RT A22WE 20081009 EA 2008 10 9 TRAX200801196 1 20080919 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 683BR 7692 JOB 8769211 OPERATION 194 CABIN FLOOR SUPPORT STRUCTURE FS 280, RBL 9 CLIP IS CRACKED 1/2" OTBD. RESOLVED ON W/O 100685 TASKCARD NR 00268. C/A R&R CABIN FLOOR SUPPORT STRUCTURE FS 280, RBL 9 CLIP. O/B WITH NEW PART IAW CRJ 200 SRM 51-42- 13 AND 51-42-21. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 TRAX200801197 1 20080919 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 683BR 7692 JOB 8769211 OPERATION 195 CABIN FLOOR SUPPORT STRUCTURE FS 280, LBL 9 CLIP IS CRACKED 1/2" OTBD. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 TRAX200801186 1 20080916 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA CABIN ODOR A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 754EV 10173 BOTH FAS COMPLAINED OF A STRONG FUEL ODOR DURING FLIGHT. IN AFT CABIN AFT OF ROW 14. RAN APU BOTH A/C PACKS AND FUEL P UMP SYSTEMS NO DEFECTS NOTED REF CRJ-700MM 21-51-00 28-23-02. 2 L 7 2 4F RT A21EA 20081009 EU 2008 10 9 2008UALA05588 1 20080904 A 2730 31075217 ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ELEVATOR FAILED A UALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 29 408UA 457 ELAC 2 PITCH FAULT DISPLAYED ON UPPER ECAM SCREEN. LEFT ELEV GREEN ACT FAILING. REPLACED ELEV LG ACTUATOR 34CE1, OPS T ESTED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20081009 NM 2008 10 9 2008UALA05939 1 20080930 A 2560 COVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 EMERGENCY EVAC SLIDE 2R DOOR CARRIER BOX CRACKED AT SIDE. REPLACED SLIDE AT DOOR 2R. 2 L 7 2 4F 4 F RT A2NM E17NE 20081009 NM 2008 10 9 2008UALA05951 1 20081001 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EVAC SLIDE INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 SLIDE EMERGENCY LIGHT NOT ON AT DOOR 1 LT. LIGHT FOUND INOPERATIVE. REPLACED LIGHT ASSY. OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081009 NM 2008 10 9 SWAA085317 1 20081001 A 3350 8200048801 LENS BOEING 737 737301 1384611 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085326 1 20081001 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A TO BS 500B, STR 26R. REMOVED AND REPLACED CLIP PER S RM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 UIE2008F00039 1 20080914 A 5310 BEAM BOEING 747 7472D7B 1384803 NM FUSELAGE CORRODED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 523MC 21782 RT NR 5 MAIN ENTRY DOOR FWD EDGE BEAM AND LOWER HINGE CUTOUT AREA CORROSION. REPAIRED IAW SERVICE REQUEST 1-954744333 AP PROVED BY FORM 8100-9 DATED 5 SEPT, 2008, DETAILS OF WORK KEPT AT EO-4752A154. (K) 2 L 7 4 4F RT A20WE 20081010 NM 2008 10 10 UIE2008F00041 1 20080914 A 5311 FRAME BOEING 747 7472D7B 1384803 NM BS 1740 S12-13R DENTED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 523MC 21782 BS 1740 FRAME BETWEEN S-12R AND S-13R DENT. REPAIRED IAW MFG SERVICE REQUEST 1-954640770 APPROVED BY FORM 8100-9 DATED 1 2 SEP 2008, DETAILS OF WORK KEPT AT EO -4753B201. (K) 2 L 7 4 4F RT A20WE 20081010 NM 2008 10 10 SWAA085340 1 20081001 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 25L TO 26L. REMOVED AND REPLACED TIE PER PAE ER. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085341 1 20081001 A 2560 PL22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND PHOTOLUMINESCENT LIGHT STRIP DELAMINATED IN CABIN. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 UIE2008F00042 1 20080914 A 5330 SKIN BOEING 747 7472D7B 1384803 NM FUSELAGE CORRODED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 523MC 21782 CENTER SECTION UPPER SKIN PANEL AT REAR SPAR LBL 100.0, LBL 108.65 CORROSION. REPAIRED IAW MFG SERVICE REQUEST 1-9576581 61 APPROVED BY FORM 8100-9 DATED 9 SEPT 2008, DETAILS OF WORK KEPT AT EO-4752A462. (K) 2 L 7 4 4F RT A20WE 20081010 EU 2008 10 10 HXS2008F00002 1 20080929 A 6720 350A21136324 BRACKET SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE RUDDER PEDALS CRACKED D HXSA O OTHER O OTHER NR NOT REPORTED 1 AL 05 6094E 2750 ON THE BOTTOM SIDE OF THE FOOT PEDAL CONTROLS, ON THE RT PILOT SIDE, THE BRACKET THAT IS PART OF THE BELLCRANK ASSY, BRA CKET PN 350A21-1313-24, HAS A CRACK IN IT. REMOVED BRACKET AND REPLACED WITH A SERVICEABLE BRACKET AND RETURNED AC TO SE RVICE. THIS AC HAS BEEN PREVIOUSLY CONVERTED TO LT PILOT IN CHARGE SEAT IAW MFG MODIFICATIONS. THIS BRACKET IS WHAT HOLD S THE CENTERING ROD FOR THE FOOT PEDAL BELLCRANK IN THE FOOT PEDAL FLIGHT CONTROLS. (K) 1 G 7 1 3U 3 U H9EU E19EU 20081010 EU 2008 10 10 HXS2008F00003 1 20080929 A 2720 360A21136324 BRACKET SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE RUDDER PEDALS CRACKED E HXSA O OTHER O OTHER NR NOT REPORTED 1 AL 05 970TH 9011 ON BOTTOM SIDE OF THE FOOT PEDAL CONTROLS, ON THE RT PILOT SIDE, THE BRACKET THAT IS PART OF THE BELLCRANK ASSY, BRACKET PN 350A211183-24, HAS A CRACK IN IT. REMOVED THE BRACKET AND REPLACED WITH A SERVICEABLE BRACKET AND RETURNED AC TO SER VICE. THIS AC HAS BEEN PREVIOUSLY CONVERTED TO LT PILOT CHARGE IAW MFG MODIFICATIONS. THIS BRACKET IS WHAT HOLDS THE CEN TERING ROD FOR THE FOOT PEDAL BELLCRANK IN THE FOOT PEDAL FLIGHT CONTROLS. (K) 1 G 7 1 3U 3 U H9EU E19EU 20081010 NM 2008 10 10 CALA0800938 1 20081001 A 5210 65164243 TORQUE BOX BOEING 737 737524 1384721 NM L2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 L-2 DOOR TWO MOUNT HOLES ON TORQUE BOX CORRODED. REMOVED AND REPLACED L2 DOOR TORQUE BOX AS CORROSION WAS FOUND TO BE O UT OF LIMITS PER B737 CMM 52-6-03. 2 L 7 2 4F RT A16WE 20081010 EU 2008 10 10 HXS2008F00004 1 20080929 A 6720 350A21136324 BRACKET SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE RUDDER PEDALS CRACKED E HXSA O OTHER O OTHER NR NOT REPORTED 1 AL 05 143TH 9043 ON THE BOTTOM SIDE OF THE FOOT PEDAL CONTROLS, ON THE RT PILOT SIDE, THE BRACKET THAT IS PART OF THE BELLCRANK ASSY, BRA CKET PN 350A21-1363-24, HAS A CRACK IN IT. REMOVED BRACKET AND REPLACED WITH A SERVICEABLE BRACKET AND RETURNED AC TO SE RVICE. THIS AC HAS BEEN PREVIOUSLY CONVERTED TO LT PILOT IN CHARGE IAW MFG MODIFICATION. THIS BRACKET HOLDS THE CENTERI NG ROD FOR THE FOOT PEDAL BELLCRANK IN THE FOOT PEDAL FLIGHT CONTROLS. (K) 1 G 7 1 3U 3 U H9EU E19EU 20081010 EU 2008 10 10 HXS2008F00005 1 20080929 A 6720 350A21136324 BRACKET SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE RUDDER PEDALS CRACKED E HXSA O OTHER O OTHER NR NOT REPORTED 1 AL 05 913LP 2383 ON THE BOTTOM SIDE OF THE FOOT PEDAL CONTROLS, ON THE RT PILOT SIDE, THE BRACKET THAT IS PART OF THE BELLCRANK ASSY, BRA CKET PN 350A21-1363-24, HAS A CRACK IN IT. REMOVED BRACKET AND REPLACED WITH A SERVICEABLE BRACKET AND RETURNED AC TO SE RVICE. THIS AC HAS BEEN PREVIOUSLY CONVERTED TO LT PILOT IN CHARGE IAW MFG MODIFICATION. THIS BRACKET IS WHAT HOLDS THE CENTERING ROD FOR THE FOOT PEDAL BELLCRANK IN THE FOOT PEDAL FLIGHT CONTROLS. (K) 1 G 7 1 3U 3 U H9EU E19EU 20081009 NM 2008 10 9 KCSA081492 1 20080925 A 5347 SEAT TRACK BOEING 747 747249F 1384849 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 MAIN DECK SEAT TRACK DAMAGED BETWEEN BS 1140 AND 1240, LBL 34. 2 L 7 4 4F RT A20WE 20081009 NM 2008 10 9 KCSA081495 1 20080925 A 3350 LIGHT BOEING 747 747236B 1384804 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 701CK 21730 RT UPPER DECK SLIDE EMERGENCY LIGHT INOP. 2 L 7 4 4F RT A20WE 20081009 EA 2008 10 9 TRAX200801153 1 20080910 A 5230 ANGLE CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 682BR 7691 JOB 8769125 OPERATION 78 CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPRO .3" IN LENGTH. RESOLVED ON W/O 99839 TASK CARD NR 00280. C/A R&R CARGO DOOR SUPPORT BEAM LOWER ANGLE WITH A NEW SERVICEABLE ANGLE IAW CRJ 200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 TRAX200801152 1 20080910 A 5320 PANEL CNDAIR CL600 CL6002B19 1900309 EA CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 682BR 7691 JOB 8769121 OPERATION 94. PANEL 282ARW HAS NUMEROUS CRACKS ON THE BOTTOM FLANGE. RESOLVED ON W/O 99838 TASKCARD NR 002 74. C/A REPLACED 282ARW WITH SERVICEABLE UNIT. REF BSC FORM M212 FOR INSTALLATION. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 TRAX200801128 1 20080907 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 682BR 7691 JOB 8769121 OPERATION 80 CABIN FLOOR SUPPORT FS 280 LT AND RT CLIPS ARE CRACKED RBL 9 AND LBL 9. RESOLVED ON W/O 99838 TASKCARD NR 00083. C/A R&R CABIN FLOOR SUPPORT FS 280 LT INBD AND RT INBD AND OTBD CLIPS IAW CRJ 200 SRM 51-42-06 AND 5 1-42-21. LT O/B FS 280 FLOOR BEAM CLIP DUE REPLACEMENT. REMOVED ALTERNATE EXTENSION PULLEY BRACKET AT FS 280 LBL 11 FOR ACCESS BY REMOVING 4 BOLTS AND 4 NUTS. R&R LT O/B FS 280 FLOOR SUPPORT CLIP AT LBL 9 IAW CRJ 200 SRM CH 51-42-06 AND 5 1-42-21. REINSTALLED ALTERNATE EXTENSION PULLEY BRACKET AT FS 280 LBL 11. BY REINSTALLING 4 BOLTS AND 4 NUTS AND TORQUI NG NUTS IAW CRJ 200 AMM TASK 20-21-00-910-801. ALTERNATE EXTENSION REQUIRES OPS CHECK. PERFORMED OPS TEST OF THE LG MA 2 L 7 2 4F RT A21EA 20081009 CE 2008 10 9 GLB2008F00030 1 20080919 A 5511 SPAR BEECH 1900 1900D 1154162 CE HORIZ STAB DAMAGED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 122UX 24954 UE122 MAJOR REPAIR FOR CONFORMITY REPLACEMENT REQUESTED OF HORIZONTAL STABILIZER MAIN SPAR CENTER WEB REPAIR. PRIOR REPAIR DO ES NOT CONFORM TO SRM DATA. MX REPLACED THE MAIN SPAR CENTER WEB REPAIR IAW BEECH 1900D SRM 55-91. REPAIR APPROXIMATEL Y 5.75" BY 4.75" OUT OF 2024 T-3 .063. HI-LOK AND RIVETS REFERENCE SRM 55-91. RII INSPECTION COMPLIED WITH PER TASKCAR D 8.2.1. HORIZONTAL STABILIZER OBTAINED AS AN ASSEMBLY DUE TO DAMAGE THAT OCCURRED IN AN INCIDENT. CONFORMITY CHECK RE VEALED A POSSIBLE CONFLICT WITH THE SRM SO IT WAS DECIDED TO PERFORM THE ABOVE MENTIONED REPAIR. 2 L 7 2 4T RT A24CE 20081009 NM 2008 10 9 HNAA0800289 1 20080914 A 3620 7821004 PRESSURE SWITCH DHAV DHC8 DHC8102 2809003 NM BLEED AIR SYS STUCK A HNAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 07 825EX 34111 388 NR2 ENGINE BLEED HOT CAUTION LIGHT ILLUMINATED DURING FLIGHT. LIGHT GOES OUT WHEN SWITCH SELECTED OFF, FERRYING TO SBY. R&R D BLEED OVERTEMP SWITCH IAW AMM 21-11-26 NO FIX. R&R D NR2 ENGINE HP BLEED VALVE. INSTALLING NEW USING RETAINED HARDWARE, AND REMOVED, CLEANED, REINSTALLED HP SENSING LINE. R&R NR2 HP PRESSURE SWITCH. IAW AMM 21-11-21. R&R D NR 2 PRSOV. IAW AMM 21-11-11. R&R D NR 1 ENGINE HP PRESSURE SWITCH IAW AMM 21-11-21. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 20081009 SO 2008 10 9 SIMA200826805 1 20080923 A 2121 4611028900 FAN EMB 145 EMB145LR 3260212 SO CABIN DEFECTIVE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 907AE 14500895 ON FLIGHT 3686 CREW REPORTED ON TAKEOFF AN INTERMITTENT BURNING SMELL COMING FROM AIR CONDITIONING SYSTEM. ACFT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. C/A R&R NR 1 RECIRCULATION FAN. ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081009 SO 2008 10 9 SIMA200826802 1 20080921 A 3320 7317041605 LIGHT EMB 135 EMB135KL 3260302 SO LAVATORY BURNED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 846AE 145692 ON FLIGHT 4354 CREW REPORTED ON ARRIVAL THAT THE FLIGHT ATTENDANT SMELLED SMOKE COMING FROM LAV AREA NEAR THE ELT. CREW CONFIRMED SMELL BUT NO VISIBLE SMOKE. ACFT REMOVED FROM SERVICE. C/A FOUND FLUORESCENT BULB ABOVE TOILET WITH BURNT S OCKET. REMOVED BULB. DEFER LAVATORY PER MEL 38-03 AUTH 090830DM-C. C/A R&R LIGHT HARNESS ASSEMBLY. OPS CHECK GOOD. IAW EMB AMM. MEL ITEM RESTORED. ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081009 SO 2008 10 9 SIMA200826605 1 20080917 A 5320 14523186001 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 837AE 145647 DURING MBV INSPECTION THE LT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. DAMAGE WAS CUT OUT. FABRICATED A REPAIR DOUBLE (AL2024T3.050), FILLER (AL2024T3.050) AND 2 SHIMS (AL2024T3.040). DRILLED, CLEANED, ALODINED, PRIMED AND INSTALLED REP AIR PARTS IAW EMB SRM 51-00-10. ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081009 SO 2008 10 9 SIMA200826604 1 20080921 A 2120 UNKNOWN EMB 145 EMB145 3260210 SO LAVATORY ODOR A SIMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 SW 21 612AE 145079 ON FLIGHT 3444 CREW REPORTED STRONG SMELL EMANATING FROM LAV. THEN LAV SMOKE INDICATION CAME ON. THE CAPT REPORTS IT W AS A STRANGE SMELL SHE HAS NOT SMELLED BEFORE. STATES SHE FELT LIKE SHE GOT HIGH FROM SMELL. IMMEDIATELY THEY DECLARED AN EMERGENCY AND TURNED BACK TO PIA. SMELL WENT AWAY BUT THEN WHEN RAISED THRUST SETTING FOR LANDING SMELL CAME BACK. WAS NOT AN OVERWEIGHT LANDING. CFR DID RESPOND UPON LANDING. HOWEVER THE SMELL HAD DISSIPATED SO THEY TAXIED TO THE G ATE WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. AWAITING FOLLOW UP. 2 L 7 2 4F RT T00011AT 20081009 CE 2008 10 9 GUU2008F00053 1 20080924 A 3260 WARNING SYSTEM BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A GUUA O OTHER N FALSE WARNING AP APPROACH 1 SO 17 87552 UE216 FLIGHT 99184 FLL/EYW PILOT DISCREPANCY. DURING APPROACH FLAPS AT 35 DEGREE SELECTION, LANDING GEAR UNSAFE LIGHT ILLUMIN ATED WITH 3 GREEN DOWN AND LOCKED LIGHT. CONTINUED TO EYW AND LANDED WITHOUT INCIDENT. C/A CHECKED SECURITY OF LANDING GEARS AND SWITCHES ALL SECURE, LANDING GEAR OPS CHECKED 3 CYCLES NO FAULTS NOTED. COULD NOT DUPLICATE. 2 L 7 2 4T RT A24CE 20081009 NM 2008 10 9 2008UALA05564 1 20080901 A 5210 MECHANISM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EXIT DOOR 2R ARM UNDERSERVICED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 653UA 25391 EXIT DOOR 2R ARMING LEVER & BUTTON HARD TO OPERATE. FOUND MECHANISM UNDERSERVICED. CLEANED & LUBED ARMING MECHANISM. O PS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081009 EU 2008 10 9 08FDEA03901 1 20080916 A 5330 A5397812620000 SKIN AIRBUS 310 A310 EU ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 THE FUSELAGE SKIN IS DENTED AROUND RIVETS T FRAMES 70 - 72; STRINGER 22R. RE-EVALUATED THE AREA & FOUND TO BE OUT OF L IMITS IAW SRM 53-17-12 & SRM 53-10-00. REMOVED DAMAGED AREA IAW SRM 53-10-12. FABRICATED THE FILLER & DOUBLER REPAIR IAW SRM 53-10-12. ALODINED & PRIMED IAW SRM 53-23-10. INSTALLED DOUBLER REPAIR IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20081009 SO 2008 10 9 SWIA200820078 1 20080826 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 565SW 120340 RIGHT WING STRINGER AFT OF SECOND OUTBOARD FUEL ACCESS PANEL CRACKED. (C-CHECK) REPAIRED PER SRM 57-20-03. 2 L 7 2 4T RT A31SO 20081009 SO 2008 10 9 SWIA200820079 1 20080826 A 5320 STRIP EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 565SW 120340 PASSENGER DOOR CUTOUT HAS CORROSION AT BOTTOM. (C-CHECK) REPLACED BOTTOM STRIP AT DOOR CUTOUT. 2 L 7 2 4T RT A31SO 20081009 NM 2008 10 9 F3LA2008100600658 1 20081003 A 5315 D5347217220200 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 931FR 52 2253 DURING C3 C-CHECK, INSPECTION NOTED FLOORBEAM Y1292 AT FRAME 66, FORWARD HOLE HAS CORROSION. MAINTENANCE BLENDED CORROS ION, OVERSIZED HOLE, ROTO-PROBED, TREATED, PRIMED AND PAINTED IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-00-14, NONDESTRUCTIVE TESTING MANUAL 51-10-01 PART 6, 51-10-08 PART 6 AND ENGINEERING AUTHORIZATION A9-53R-30664. 2 L 7 2 4F RT A28NM 20081009 NM 2008 10 9 F3LA2008100600659 1 20081004 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 931FR 52 2253 DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 262FF IS CORRODED ON UPPER AND LOWER SURFACE. MAINTENANCE REMOVED FLOOR PANEL AND INSTALLED SERVICEABLE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-12-400-002. 2 L 7 2 4F RT A28NM 20081009 NM 2008 10 9 F3LA2008100600660 1 20081003 A 5315 D5347217220400 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 931FR 52 2253 DURING C3 C-CHECK, INSPECTION NOTED FLOORBEAM Y1292 BETWEEN FRAME 66 AND FRAME 68, HAS CORROSION IN SEVERAL HOLES. MAIN TENANCE BLENDED CORROSION AND OVERSIZED HOLES, HOLES OUT OF LIMITS PER SRM 53-00-14. MAINTENANCE REMOVED CORRODED FLOOR BEAM AND UPPER COUPLER AND INSTALLED SERVICEABLE FLOORBEAM AND UPPER COUPLER IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-72-11 PARAGRAPH 5B(1) - 6A(2), DRAWINGS D53472816 AND D53472780. 2 L 7 2 4F RT A28NM 20081009 NM 2008 10 9 F3LA2008100600661 1 20081003 A 5315 D5347210220000 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 931FR 52 2253 DURING C3 C-CHECK, INSPECTION NOTED FLOORBEAM Y1292 BETWEEN FRAME 66 AND FRAME 68, HAS CORROSION IN SEVERAL HOLES. MAIN TENANCE BLENDED CORROSION AND OVERSIZED HOLES, HOLES OUT OF LIMITS PER SRM 53-00-14. MAINTENANCE REMOVED CORRODED FLOOR BEAM AND UPPER COUPLER AND INSTALLED SERVICEABLE FLOORBEAM AND UPPER COUPLER IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 51-72-11 PARAGRAPH 5B(1) - 6A(2), DRAWINGS D53472816 AND D53472780. 2 L 7 2 4F RT A28NM 20081009 NM 2008 10 9 F3LA2008100600664 1 20081004 A 5321 D5367175900300 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CABIN DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 931FR 52 2253 DURING C3 C-CHECK, INSPECTION NOTED PASSENGER FLOOR PANEL 262EF HAS AREAS OF DELAMINATION. MAINTENANCE REPAIRED FLOOR P ANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 212. 2 L 7 2 4F RT A28NM 20081009 NM 2008 10 9 F3LA2008100600666 1 20081004 A 5321 D5367302100000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 931FR 52 2253 DURING C3 C-CHECK, INSPECTION NOTED SEVERAL PUNCTURES AND EDGE DELAMINATION TO AFT CARGO TRANSITION PANEL 151AE. MAINTE NANCE REMOVED AND REPLACED CARGO PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-14-400-001. 2 L 7 2 4F RT A28NM 20081009 NM 2008 10 9 F3LA2008100600667 1 20081004 A 2612 330TS08Y CONTROL PANEL AIRBUS A319 A319111 3930336 NM COCKPIT FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 21 931FR 52 2253 DURING C3 C-CHECK, INSPECTION NOTED THE FIRE PANEL DISCHARGE LIGHT FOR THE NR 1 FIRE BOTTLE OF THE NR 2 ENGINE FAILS TO ILLUMINATE DURING THE OPERATIONAL CHECK OF THE BOTTLE LOW PRESSURE INDICATING CIRCUIT TEST. MAINTENANCE REMOVED AND REP LACED FIRE PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 26-12-12-00-001, 26-12-00-710-001 AND 26-21-00-720-005. 2 L 7 2 4F RT A28NM 20081009 NM 2008 10 9 SWAA085308 1 20081001 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, 16L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085309 1 20081001 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 26R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085311 1 20081001 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED 14Y CHECK, FOUND FWD CARGO SHEAR TIE CORRODED AT BS 360, LBL 10. REMOVED AND REPLACED TIE PER SRM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085312 1 20081001 A 5322 6546529 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 440, STR 14R TO STR 15R. REPAIRED PER AAR EA. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085314 1 20081001 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND BELLY SKIN CRACKED AT BS 410, AFT BL 0. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085319 1 20081001 A 5311 65546540 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 639, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085320 1 20081001 A 5314 6545866 KEELBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND RT MLG W/W KEEL BEAM CORRODED AT BS 721. REPAIRED BEAM PER BOEING DRW. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085322 1 20081001 A 5330 6545765 SKIN BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO COMPT SKIN CORRODED AT BS 500 TO 500A BETWEEN STR 28L TO 28R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085328 1 20081001 A 5322 69353656 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 13L TO STR 14L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085330 1 20081001 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 13L. REMOVED AND REPLACED CLIP PER PAE EA. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085331 1 20081001 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 13R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085332 1 20081001 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CRACKED AT BS 440, STR 28R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085338 1 20081001 A 5322 BAC1518 SHEAR TIE BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 781WN 30601 DURING SCHEDULED 8Y CHECK, FOUND FWD CENTER TANK SHEAR TIE CORRODED AT BS 540 LBL 54.6 TO RBL 32.4. REMOVED AND REPLACE D TIE PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085339 1 20081001 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER PAE ER. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 ZZDA2008163 1 20081003 A 3350 8039251 CHARGER BOEING 717 717200 1383700 NM CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 932AT 55073 EMERGENCY PATH LIGHTING AT SEATS 1DF, 2DF & 3DF WOULD NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY PATH LIGHTING BATT ERY CHARGER AT LOCATION 222AR, REF AMM 33-51. 2 L 7 2 4F TR A6WE 20081010 NM 2008 10 10 ASAA0873542 1 20080916 A 5320 147A57102 ANGLE BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 AFT PASSENGER CABIN CORROSION ON FLOOR ANGLE BS 986.5 +7 RBL 38. AFT PASSENGER CABIN CORROSION ON FLOOR ANGLE BS 986.5 +7 RBL 38 BLENDED AND FOUND BEYOND ALLOWABLE LIMITS IAW B737 700 SRM 53 70 57. REPLACED WITH NEW PART IAW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 ASAA0873544 1 20080916 A 5315 147A55055 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 AFT PASSENGER CABIN CORROSION ON TOP FLOORBEAM STA 967 RBL 17 AFT PASSENGER CABIN CORROSION OF TOP FLOORBEAM STA 967 RBL 17. REPAIRED IAW CASCADE ERO 4 AND ASA 5320 01854. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 ASAA0873545 1 20080915 A 5320 146A81236 SILL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 AFT CARGO DOOR SILL PLATE FAYING SURFACE CORRODED AROUND ANCHOR NUTS. REPLACED SILL WITH NEW PART IAW B737 700 SRM 51 4 0 02 AND 51 40 05. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 ASAA0873552 1 20080915 A 5347 146A7501 CARGO TRACK BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 CORROSION ON AFT CARGO TIE DOWN TRACK BS 787 BS 847 RBL 14. CORRODED AFT CARGO TIE DOWN TRACK BS 787 BS 847 RBL 14 REPL ACED WITH NEW TIE DOWN TRACK IAW B737 700 DWG 146A7501 MADE FROM BAC1520 1397. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 ASAA0873553 1 20080915 A 5320 146A75021 CHANNEL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 AFT CARGO Z-CHANNEL BS 727E +10 TO BS 847 CORRODED LBL 20 CORROSION ON Z CHANNEL BS 727E +10 TO BS 847 CORRODED LBL 20 I N AFT CARGO PIT BLENDED AND FOUND TO BE BEYOND LIMITS. REPLACED WITH MADE REPAIR PART IAW 737 700 SRM 53 00 53 REPAIR 6 . 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 ASAA0873554 1 20080915 A 5320 143A101011 TIE CLIP BOEING 737 737790 13844CN NM FUSELAGE MISSING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 FWD CARGO STR 27L BS 500D TIE CLIP MISSING. FWD CARGO PIT AT BS 500B STA 27L TIE CLIP REPLACED IAW 737 700 SRM 51 40 02 . 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 ASAA0873555 1 20080915 A 5320 146A8127 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 CORROSION ON AFT CARGO PIT FLOORBOARD SUPPORT WEB BS 767 787 RBL 20. AFT CARGO PIT FLOORBOARD SUPPORT WEB BS 767 787 RB L 20 REPLACED WITH MADE REPAIR PART IAW 737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081010 NE 2008 10 10 DJF2008F00014 2 20080909 A 7200 ENGINE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE MAKING METAL E DJFA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 23 465LX RK454 REPORTED LOW OIL PRESSURE IN FLIGHT. THE AFFECTED ENGINE WAS SHUTDOWN, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERT ED. MAINTENANCE FOUND METAL IN THE OIL SYSTEM. THE ENGINE WAS REMOVED FOR OEM EVALUATION. AIRCRAFT RETURNED TO SERVICE . (K) 2 H 7 2 4F 4 F RT A16SW E25EA 20081010 CE 2008 10 10 GUU2008F00049 1 20080910 A 5220 DOOR BEECH 1900 1900D 1154162 CE EMERGENCY EXIT OUT OF ADJUST A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 53545 UE185 DURING SCHEDULED ROUTINE MAINT, DISCOVERED LT EMERGENCY EXIT DOOR DOES NOT CLOSE PROPERLY. READJUSTED LT EMERGENCY EXIT DOOR. (K) 2 L 7 2 4T RT A24CE 20081010 NM 2008 10 10 AALA200802233 1 20080828 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 179AA 32397 JFK EMERGENCY LIGHTS AT SEAT 33D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 33D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 AALA200802230 1 20080828 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 179AA 32397 JFK EMERGENCY LIGHTS AT SEAT 30D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 30D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 AALA200802225 1 20080828 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 179AA 32397 JFK EMERGENCY LIGHTS AT SEAT 25D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 AALA200802218 1 20080827 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 MIA EMERGENCY LIGHT AT RT HAND OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RT HAND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081010 NE 2008 10 10 I5H2008F00001 2 20080716 A 8500 R2800 ENGINE CVAC 240 T29B 2422644 WP PWA R2800 R2800* 52026 NE LEFT MAKING METAL A I5HA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 25 150PA 137 278 P27759 JUST AFTER TAKEOFF, AT APPROXIMATELY 1700, THE CREW OBSERVED A HIGH OIL TEMPERATURE INDICATION ON THE LT ENGINE. THE CAP TAIN REDUCED POWER AND THE OIL TEMPERATURE CAME DOWN BUT THE OIL PRESSURE ALSO CAME DOWN TO AN ABNORMALLY LOW PRESSURE. THE CREW DECLARED AN EMERGENCY AND RETURN TO DEPARTURE. AFTER LANDING UNEVENTFULLY, THE CREW SHUTDOWN THE LT ENGINE AND TAXIED TOT HE PARKING AREA. THE CREW ATTEMPTED TO PULL THE PROPELLER THROUGH, BUT WAS ONLY ABLE TO MOVE IT A SHORT DIST ANCE. THERE WAS A GRINDING NOISE HEARD IN THE NOSE CASE. SUBSEQUENT INSPECTION BY A MECHANIC REVEALED SIGNIFICANT AMOUNT S OF METAL IN THE OIL SCREEN. LT ENGINE WILL BE REMOVED AND REPLACED. OPEN (K) 2 L 7 2 4R 4 R 6A6 5E8 20081010 WP 2008 10 10 I5H2008F00002 1 20080802 A 5511 SPAR CVAC 440 440 2422902 WP HORIZONTAL STAB CORRODED A I5HA O OTHER O OTHER NR NOT REPORTED 1 GL 25 587X 361 REMOVED INTERGRANULAR CORROSION FROM THE RT HORIZONTAL STABILIZER SN 384RH UPPER REAR SPAR (3) FT OB OF THE UPPER AFT RT HORIZONTAL STABILIZER ATTACH FITTING. REPAIR ACCOMPLISHED IAW DWG NR R361-055-001-001, REV A DATED JULY 15, 2008. (K) 2 L 7 2 4R 6A6 20081010 NM 2008 10 10 SWAA085356 1 20080930 A 3350 079123 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 446WN 29842 DURING SCHEDULED MV3 CHECK, FOUND EMERGENCY EXIT FLOOR LIGHT TRACK COVER BROKEN. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085357 1 20081001 A 3350 65C27095 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 492WN 33866 DURING SCHEDULED HC2 CHECK, RT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085364 1 20081001 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR LOWER OPENING CREASE BEAM CORRODED. REMOVED AND REPLACED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085373 1 20081001 A 5330 6545772 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 731 TO BS 791 AT STR 14L. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081010 2008 10 10 SWAA085374 4 20081001 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM EMERGENCY EXIT OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED SPV CHECK, FOUND L2 EMERGENCY EXIT SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085375 1 20081002 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, STR 27R TO STR 26R. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081010 EU 2008 10 10 UPS08153439 1 20080924 A 5321 B5327074900100 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU CABIN BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 232XG BROKEN AT LEFT FWD EDGE. PERMANENTLY REPAIRED MAIN CABIN FLOOR PANEL R EF A300-600 SRM 53-10- 20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081010 EU 2008 10 10 UPS08153440 1 20080924 A 5321 B5327082100000 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 261FH CRACKED LEFT CORNER. REPAIRED MAIN CABIN FLOOR PANEL 261FH REF A300-60 0 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081010 EU 2008 10 10 UPS08153441 1 20080923 A 5754 A5724199320200 RIB AIRBUS A300 A300F4622R 3930360 EU KRUEGER FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR LT WING K-FLAP WELL RIB CRACKED IN LOWER RADIUS. REPAIRED LEFT WING KRUEGER FLAP WELL RIB BY REPLA CEMENT OF PART REF A300-600 SRM 51-40-21 PAGE 1 PARA 5, 6 AND 7. 2 L 7 2 4F RT A35EU 20081010 NM 2008 10 10 UPS08553444 1 20081002 A 5330 SKIN BOEING 757 75724APF 1384969 NM BS 210 S23L DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 GROUND CREW RAN STAIRS INTO LEFT SIDE OF FUSELAGE APPROX BS 210, S 23. DENT SIZE IS 6 INCHES LONG X .150 DEEP. ASSIGNE D TO DEFERRAL LIST D385769 ASSIGNED. FERRY PERMIT 9079 ISSUED (FERRY TO SAT). OPEN 3 CUTOUT BY 0.04" PER SRM 53-00-01 -2R & MICROFINISH EDGE OF CUTOUTS. FAB REPAIR DOUBLER PER EA 757-5310-01-A1524. FAB REPAIR FILLER 3 PER EA 757-5310-01- A1524. FAB REPAIR DOUBLER & REPAIR FILLER (3). TREATED & PRIMED ALL PARTS PER EA 757-5310-01-A1524. ACCOMPLISHED EA 757- 5310-01-A1524 IAW EO B757-5330-30752. 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 RYN2008F00014 1 20081001 A 2421 IDG BOEING 757 7572G5 1384912 NM FAILED A RYNA O OTHER O OTHER NR NOT REPORTED 1 GL 31 929RD 23929 IDG FAILED NO FREQUENCY OR VOLT. REPLACED IDG IAW AMM 24-11-1. CHECKED GOOD. (K) 2 L 7 2 4F RT A2NM 20081010 SO 2008 10 10 FDK2008F00007 1 20080825 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 ROW 12 OVERHEAD AFT EMERGENCY LIGHT INOPERATIVE. MX RESET EMERGENCY LIGHT SYS OPS CHECK GOOD. (K) 2 L 7 2 4T RT T00011AT 20081010 SO 2008 10 10 FDK2008F00008 1 20080825 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 827MJ 145217 EMERGENCY LIGHT FLOOR STRIP AT ROW 1 IS INOPERATIVE. MX REPLACED STRIP OPS CHECKED GOOD. (K) 2 L 7 2 4T RT T00011AT 20081010 NM 2008 10 10 ASAA0873541 1 20080916 A 5320 147A8540U8 SILL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 AFT PASSENGER CABIN CORROSION ON DOOR ENTRY INNER CHORD BS 936 BS 980 RBL 54. CORRODED ENTRY DOOR INNER CHORD BETWEEN B S 936 BS 980 RBL 54 FOUND TO BE BEYOND REPAIRABLE DAMAGE LIMIT. SILL CHORD REPLACED WITH NEW PART P/N 147A8540U8 IAW SR M 51 40 02. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 ASAA0873556 1 20080917 A 5320 141A52136 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 623AS 30166 FWD PASSENGER CABIN CORROSION ON LATERAL INTERCOSTAL BS 270 RBL 11 LBL 10. CORROSION FOUND ON FWD PASSENGER CABIN CORRO SION ON LATERAL INTERCOSTAL BS 270 RBL 11 LBL 10 WAS FOUND TO BE BEYOND LIMITS AND THEREFORE WAS REPAIRED DAW ERO 8684 A ND ASA EA 5310 02820. REPLACE THE SUBJECT INTERCOSTAL WITHIN 24 MONTHS FROM 26 SEP 08. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 AALA200802226 1 20080828 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 179AA 32397 JFK EMERGENCY LIGHTS AT SEAT 26D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 AALA200802227 1 20080828 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 179AA 32397 JFK EMERGENCY LIGHTS AT SEAT 27D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 27D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 AALA200802259 1 20080901 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 607AM 27058 DFW EMERGENCY LIGHT AT RT FORWARD OVERWING INOPERATIVE. REPLACED EMERGENCY LAMP FOR EMERGENCY LIGHT AT RT FORWARD OVERW ING. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 SWAA085352 1 20081002 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BS 425 TO BS 440. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085360 1 20080930 A 3350 100031 SIGN BOEING 737 7373Y0 1384671 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED 22Y CHECK, FOUND R1 EMERGENCY EXIT DOOR LIGHT SIGN MISSING. REMOVED AND REPLACED SIGN PER MM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085367 1 20081001 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 QXEA200800417 1 20080418 A 5314 KEELBEAM DHAV DHC8 DHC8202 2809007 NM BS 201 S31P CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 C4-CHECK- SUSPECT CORROSION ON BOTTOM OF VERT KEEL BEAM AT STR 31P AND STA X201. REPAIRED IAW SRM. (K) 2 H 7 2 4T RT A13NM 20081010 NM 2008 10 10 SWAA085369 1 20081001 A 5311 6546539 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 616, BELOW STR 17L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085370 1 20081001 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS. 294.5, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085382 1 20081002 A 3350 65C27095 BATTERY PACK BOEING 737 7377Q8 1384418 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 799SW 28209 DURING SCHEDULED HC2 CHECK, RT MID CABIN EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081010 EU 2008 10 10 UPS08153424 1 20080924 A 5321 B5327084200200 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 242UJ CRACKED INTERNALLY. REPAIRED MAIN CABIN FLOOR PANEL 242UJ REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081010 EU 2008 10 10 UPS08153435 1 20080929 A 5321 B5327074500000 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU CABIN PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 231SG PUNCTURED. REPAIRED MAIN CABIN FLOOR PANEL 231SG REF A300-600 SRM 5 3-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081010 EA 2008 10 10 A6WA200840570 1 20080805 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 445AW 7804 INTERCOSTAL CLIP FS 484 LBL 27 CRACKED. NEW INTERCOSTAL CLIP INSTALLED FS 484, LBL 27 IAW CRJ 200 SRM 51-42-21. (K) 2 L 7 2 4F RT A21EA 20081010 EA 2008 10 10 A6WA200840572 1 20080808 A 5420 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA RT NACELLE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 445AW 7804 RT ENGINE UPPER CORE COWL AFT U CHANNEL IB SIDE CRACKED. RT ENGINE UPPER CORE COWL AFT U CHANNEL IB SIDE REPAIRED IAW SH ORTS CMM 20-12-00. (K) 2 L 7 2 4F RT A21EA 20081010 EA 2008 10 10 A6WA200840573 1 20080808 A 5320 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 523 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 445AW 7804 RT WHEEL WELL HYDRAULIC SUPPORT BRACKET AT FS 523.60 IS CRACKED. RT WHEEL WELL HYDRAULIC SUPPORT BRACKET AT FS 523.60 IS REPLACED IAW CRJ 200, SRM 51-42-06. (K) 2 L 7 2 4F RT A21EA 20081010 EA 2008 10 10 A6WA200840575 1 20080808 A 5320 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 445AW 7804 FS 280.00 LBL 9.0, WL 71.00 IB SUPPORT CLIP IS CRACKED. IB SUPPORT CLIP AT FS 280.00, LBL 9.00, WL 71.00. REPLACED IAW REO 601R-53-11-171, REV D. (K) 2 L 7 2 4F RT A21EA 20081010 NM 2008 10 10 WXO2008F00002 1 20080813 A 3350 AD4002 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS FAILED E WXOA K NONE L NO TEST IN INSP/MAINT 1 WP 07 872GA 53295 DURING A ROUTINE OVERNIGHT SERVICE CHECK, INSPECTION REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOUL D NOT TEST. MAINT REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERA TIONAL CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (K) 2 L 7 2 4F RT 20081010 WP 2008 10 10 WXO2008F00003 1 20080813 A 3350 AD4002 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS FAILED E WXOA K NONE L NO TEST IN INSP/MAINT 1 WP 07 878GA 53487 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINT REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTE M WOULD NOT TEST. MAINT REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (K) 2 L 7 2 4F RT A6WE 20081010 NM 2008 10 10 WXO2008F00004 1 20080817 A 3350 AD4002 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS FAILED E WXOA K NONE L NO TEST IN INSP/MAINT 1 WP 07 892GA 49826 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINT REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTE M WOULD NOT TEST. MAINT REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (K) 2 L 7 2 4F RT 20081010 NM 2008 10 10 WXO2008F00005 1 20080818 A 3350 60030451 BATTERY PACK DOUG MD88 MD88 3023688 NM EMERGENCY LIGHTS FAILED E WXOA K NONE L NO TEST IN INSP/MAINT 1 WP 07 401NV 49761 DURING A ROUTINE OVERNIGHT SERVICE CHECK, INSP REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINT REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMP LISHED IAW AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. (K) 2 L 7 2 4F RT A6WE 20081010 NM 2008 10 10 CALA0800939 1 20081003 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 FUSELAGE STATION 400 LEFT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGER'S 8L AND 9L. REPAIRED FRAME 400 LT PER EA 5310-04498 BETWEEN STR 8L AND 9L. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 CALA0800941 1 20081002 A 5315 141T5108 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76156 30435 CABIN FLOOR SUPPORT FOUND CORRODED AT BODY STATION 325 BETWEEN LBL 21-58. FLOOR SUPPORT BEAM BODY STATION 325 LBL 14 - 63 REPAIRED PER SRM 53-00-51 REPAIR 1 FIG 201, HFEC FOUND NO CRACK. 2 L 7 2 4F RT A1NM 20081001 NM 2008 10 1 08FDEA04042 1 20080925 A 5313 AEA74761 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 CRACK INDICATION FOUND ON STA 6-100 AFT SIDE LONGERON 1R OUTBOARD FLANGE APPROXIMATELY 2 INCHES LONG IMAGE ON X-RAY FI LM. REPAIRED AS PER SRM 53-10-00. LONGERON REWORKED AS PER DRAWING AEA7476. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10 0. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 08FDEA04055 1 20080926 A 5315 BCA1505100703 FLOORBEAM BOEING 757 75723A 1384967 NM BS 324 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 CABIN FLOORBEAM FS 324 RBL 32 GOUGED. REMOVED GOUGE ON FLOORBEAM. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 S HEET 3 DETAIL 3. REMOVED FLOORBEAM, AND FLOOR SUPPORT FOR ACCESS FAB NEW T- CHORD AND INSTALLED IAW 51-40-02. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 08FDEA04058 1 20080926 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 HFEC INSPECTION CARRIED OUT ON DIAMETER 0.460 INCH HOLES AT MAIN DECK CARGO DOOR NR 7 SPOOL FITTING, FOUND CRACK INDICAT ION ON HOLE A, B, C AND D. REMOVED AND REPLACED AS PER SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 08FDEA04060 1 20080926 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 HFEC INSPECTION CARRIED OUT ON DIAMETER 0.460 INCH HOLES AT MAIN DECK CARGO DOOR NR 3 SPOOL FITTING, FOUND CRACK INDICAT ION ON HOLE B, C AND D. REMOVED AND REPLACED AS PER SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 08FDEA04061 1 20080926 A 5310 BAC1515553 CREASE BEAM BOEING 757 75723A 1384967 NM BS 324 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 FWD OF STA 324 RT SIDE I/B CREASE BEAM CHORD HAS CORROSION. REMOVED CORROSION FOUND TO OUT OF LIMITS. INSTALLED NEW CREASE BEAM IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 08FDEA04063 1 20080926 A 5230 ACA72261 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 HFEC INSPECTION CARRIED OUT ON DIAMETER 0.520 INCHES HOLES AT MAIN DECK CARGO DOOR NR 5 SPOOL FITTING, FOUND CRACK INDIC ATION ON HOLE C AT DOOR JAMB FIRST LAYER. CARRIED OUT REPAIR AS PER EA 1-5310-123123. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 08FDEA04066 1 20080926 A 5720 652165688 RETAINER BOEING 727 727227 1384078 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 LT WING REAR SPAR LWR CHORD APPROX STA 182, SEAL RETAINER CORRODED REMOVED SEAL RETAINER REF SRM 51-30-2. FABRICATED NE W RETAINER REF DWG 65-21656. TREATED AND PRIMED REF SRM 51-10-2 PGS 1-3. INSTALLED SEAL RETAINER REF SRM 51-30-2 PG'S 1-3. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081001 NM 2008 10 1 CALA0800915 1 20080923 A 5311 146A1133 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27724 28791 FRAME CRACKED AT STA 787 BETWEEN S9LT AND S8LT AT OVERHEAD BIN BRACKET. REPAIRED CRACKED FRAME BS 787 STR 8-9 LT PER EC /RA 5310-04841. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 CALA0800914 1 20080923 A 5311 146A1133 FRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27724 28791 CRACKED FRAME AT STATION 787 BETWEEN S9-S8 RT. REPAIRED CRACKED FRAME BS 787 STR 8-9 RT PER EC/RA 5310-04841. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 CALA0800913 1 20080923 A 5311 143A1113 BELTFRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27724 28791 CABIN RT SIDE BELT FRAME STA 440 CRACKED AT OVERHEAD SUPPORT FITTING BETWEEN STRINGERS 8RT AND 9RT. REPAIRED CRACKED FR AME BS 440 STR 8-9 RT PER EC/RA 5310-04841. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 CALA0800912 1 20080923 A 5311 143A1111 BELTFRAME BOEING 737 737724 13844BY NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27724 28791 CABIN RT SIDE BELT FRAME STA 400 CRACKED AT OVERHEAD SUPPORT FITTING BETWEEN STRINGERS 8RT AND 9RT. REPAIRED CRACKED FR AME BS 400 STR 8 - 9 RT PER EC/RA 5310-04841. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 ASAA0843524 1 20080907 A 5755 SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 LT WING NR 0 SPOILER DENTED ON LOWER SURFACE NEAR CENTER AT T/E. REMOVED DAMAGED AREA, PREPARED AREA, FABRICATED FILLER AND DOUBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 ASAA0873522 1 20080911 A 5320 143A5240910 CHANNEL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 LEFT AND RIGHT PANEL CHANNELS CRACKED AT STA 538 BL 0. REPAIRED CHANNELS IAW AAR EA 12908 AND ALASKA EA 5320 01851. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085151 1 20080921 A 5230 6547953 DOOR FRAME BOEING 737 7373H4 1384600 NM AFT CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND AFT CARGO DOOR LOWER AFT FRAME CRACKED. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085135 1 20080918 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 422WN 29826 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 138 AND STA 157. REPAIRED SKI N PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085134 1 20080921 A 5322 65C27714 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CRACKED AT BS 360, STR 7R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085150 1 20080921 A 5310 6517685 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND FWD DOOR CUTOUT AFT FRAME CRACKED AT LOWER STOP. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 08FDEA03431 1 20080814 A 5522 65261633 SKIN BOEING 727 727233 138408A NM RT ELEVATOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 223FE 20935 LARGE HOLE IN RT ELEVATOR, INSIDE NR 3 BALANCE PANEL ACCESS, PUNCTURE HOLE. REMOVED WEB AND ANGLE IAW SRM 51-30-2. FAB RICATED WEB AND (1) EA ANGLE IAW DRAWING 65-26163 REV C. BONDED WEB PER BMS 5-69 IAW DRAWING 65-26163 REV C. HEAT TREA TED ANGLE IAW ER 2-37153-801 REV A. ALODINE AND PRIME PARTS IAW SRM 51-10-2. INSTALLED PARTS IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 20081001 NM 2008 10 1 SWAA085148 1 20080921 A 5230 6549889 SKIN BOEING 737 7373H4 1384600 NM FWD CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND FWD CARGO DOOR SKIN CRACKED AT HANDLE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 08FDEA03432 1 20080815 A 3213 ARG73765517 CYLINDER DOUG MD11 MD11F 3023600 NM MLG DAMAGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 598FE 48597 DURING GEAR RETRACTION RED GEAR INDICATION REMAINED ILLUMINATED FOR RIGHT MAIN GEAR APPROXIMATELY FIVE SECONDS LONGER TH AN THE OTHER GEAR. REMOVED AND REPLACED RETRACT CYLINDER IAW MM 32-33-20-4. REMOVED AND REPLACED RT MLG BUNGEE (UNLOCK ) CYLINDER REF MM 32-33-02-4. ACCOMPLISHED DOOR PROX SENSOR RTS PER MM 32-61-15-5 STEP 3. PERFORMED MLG OPS CK AND TIM ING CK PER MM 32-31-00-5. OPS CK GOOD (RT MLG RETRACT TIME 10 SECONDS MAX PER MM IS 13 SECONDS). FOUND RT MAIN UPLOCK PROX SENSOR STOP INSTALLED INCORRECT. REPOSITION PROX STOP AND READJUSTED PROX GAP REF M/M 32-61-15-5. PERFORMED GEAR SWING, OPS CHECK NORMAL, REF SEQ04 W/O 42407. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 SWAA085147 1 20080921 A 5330 6545768 BEAR STRAP BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN BEAR STRAP CORRODED AT BS 967, STR 27R AND STR 26R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081001 EU 2008 10 1 08FDEA03433 1 20080815 A 5310 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORRODED CLIP AT C 68, P 55-56 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20081010 EA 2008 10 10 ASA2008F00000 1 20081003 A 5240 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 740EV 10151 ASD AFT SIDEWALL DRAG ANGLE CRACKED. WORK COMPLETED IAW CURT OUT CRACKED DRAG ANGLE IAW REO 670-52-11-072. PERFORMED E DDY CURRENT INSPECTION OF CUT OUT ON AFT DRAG ANGLE ON AIRSTAIR DOOR IAW REO 670-52-11-072 IAW CRJ 700NDTM 51-20-2006. NOT DEFECTS NOTED. 2 L 7 2 4F RT A21EA 20081010 EA 2008 10 10 ASA2008F00005 1 20080903 A 5240 SKIN CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 740EV 10151 ASD INNER SKIN CRACKED AT AFT CORNER UNDER UPPER STEP. CUTOUT DOOR EDGE MEMBER IAW REO 670-52-11-154. PERFORMED ET INSPE CTION OF CUTLINE IAW REO 670-52-11-154 IAW CRJ 700, NDTM 51-20-006. NO DEFECTS NOTED. FN7013735. 090708. (K) 2 L 7 2 4F RT A21EA 20081009 NM 2008 10 9 KCSA081494 1 20080925 A 5347 SEAT TRACK BOEING 747 747249F 1384849 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 MAIN DECK SEAT TRACK CORRODED BETWEEN BS 610 AND 620, RBL 46. 2 L 7 4 4F RT A20WE 20081009 EA 2008 10 9 TRAX200801187 1 20080918 A 3350 COVER CNDAIR CL600 CL6002B19 1900309 EA CABIN CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 683BR 7692 JOB 8769211 OPERATION 152 EMERGENCY FLOODLIGHT COVER AND BASE ON AFT LOWER SIDE OF WARDROBE CRACKED AND BROKEN. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 CHQA200800185 1 20080921 A 7830 601R516363 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE COCKPIT FAULTED A CHQA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 11 701BR 15213 7448 GEE872845 FLIGHT 5601 IAH TO JAX. DURING FLIGHT THE CREW RECEIVED AN E2 REV ICON INTERMITTENTLY. THE REVERSER DID NOT DEPLOY. T HE FLIGHT LANDED WITHOUT INCIDENT. THE REVERSER WAS PLACED ON MEL AND THE ACFT WAS RELEASED BACK TO SERVICE. THE MEL W AS CLEARED ON THE 22ND WHEN THE THRUST REVERSER CONTROL PANEL WAS REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 20081009 CE 2008 10 9 GUU2008F00052 1 20080921 A 3230 CIRCUIT BREAKER BEECH 1900 1900D 1154162 CE COCKPIT POPPED A GUUA O OTHER O OTHER AP APPROACH 1 SO 17 69549 UE194 FLIGHT 9130 FPO/FLL PILOT DISCREPANCY DURING APPROACH, WHEN LANDING GEAR HANDLE SELECTED DOWN THE LANDING GEAR CIRCUIT B REAKER POPPED. RESET THE CIRCUIT BREAKER AND THE LANDING GEAR EXTENDED NORMALLY. C/A TROUBLE SHOT LANDING GEAR SYSTEM. NO DEFECTS NOTED. SERVICED HYDRAULIC FLUID TO CORRECT LEVEL. LANDING GEAR OPS CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081009 NM 2008 10 9 F3LA2008100600669 1 20081002 A 5320 D5348015800600 PLATE AIRBUS A319 A319111 3930336 NM CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 931FR 52 2253 DURING C3 C-CHECK, INSPECTION NOTED THE L-2 FORWARD GIRT BAR FITTING BLANKING PLATE HAS CORROSION ON CORNER. MAINTENANC E REMOVED AND REPLACED L-2 DOOR FORWARD GIRT BAR FITTING BLANKING PLATE IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 52-13-31-400-007. 2 L 7 2 4F RT A28NM 20081009 NM 2008 10 9 SWAA085321 1 20081001 A 5753 6546435 FLAP BOEING 737 737301 1384611 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085327 1 20081001 A 5330 6518420 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 271, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085333 1 20081001 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 15R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 F3LA2008100700672 1 20080929 A 5320 D5348015900700 BLANKING PLATE AIRBUS A319 A319111 3930336 NM ZONE 800 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 931FR 52 2253 DURING C3 C-CHECK, INSPECTION NOTED THE R2 DOOR AFT GIRT BAR FITTING BLANKING PLATE IS CORRODED ON LOWER SURFACE. MAINT ENANCE REMOVED GIRT BAR BLANKING PLATE AND INSTALLED NEW, REFERENCE WORK CARD C534103-01. 2 L 7 2 4F RT A28NM 20081010 EU 2008 10 10 HXS2008F00000 1 20080929 A 2700 360A21136324 BRACKET SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1D1 60053 NE RUDDER PEDALS CRACKED E HXSA O OTHER O OTHER NR NOT REPORTED 1 AL 05 403AE 3281 22117 ON THE BOTTOM SIDE OF THE FOOT PEDAL CONTROLS, ON BOTH THE RT AND LT SIDES, THERE IS A BRACKET THAT IS PART OF THE FOOT PEDAL BELLCRANK ASSY, THE LT BRACKET PN 350A21136324, HAS A CRACK IN IT. THE RT BRACKET, SAME PN, CRACKED ALL THE WAY TH ROUGH WHICH ALLOWED THE FOOT PEDAL BELLCRANK PN 350A27-1170-00, TO GO OUT OF ALIGNMENT AND CONTACT THE SURROUNDING SUPPO RT STRUCTURE THUS CAUSING A .25 INCH GROOVE INTO THE BELLCRANK. REMOVED BRACKETS AND REPLACED WITH SERVICEABLE BACKETS A ND ALSO REMOVED AND REPLACED THE BAD BELLCRANK WITH A SERVICEABLE BELLCRANK AND RETURNED AC TO SERVICE. THIS AC HAS BEEN PREVIOUSLY CONVERTED TO LT PILOT IN CHARGE IAW MFG MODIFICATION. THIS BRACKET IS WHAT HOLDS THE CENTERING ROD FOR THE F 1 G 7 1 3U 3 U H9EU E19EU 20081010 NM 2008 10 10 CALA0800936 1 20080930 A 3350 ADD71701100 BATTERY PACK BOEING 737 737824 13844BZ NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 24212 28772 EMERGENCY LIGHT ON LEFT-HAND AFT BULLNOSE, LIGHTS ON SEATS 9-14 AND 26-29 ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACKS M1694 AND M1672, SYSTEM OPERATIONAL CHECKS OK PER AMM 33-51-06-960-805. 2 L 7 2 4F RT A16WE 20081010 EA 2008 10 10 A6WA200840582 1 20080824 A 7930 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE LOW PRESSURE A A6WA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 439AW 7753 LT ENGINE OIL PRESSURE MESSAGE IN CRUISE, COMPLIED WITH QRH AND SHUTDOWN ENGINE, DIVERTED. OIL PRESSURE INDICATING BETW EEN 10 AND 20 PSI REGARDLESS OF THROTTLE POSITION. RED WARNING EXTINGUISHED AFTER THROTTLE IDLE BUT FLICKERED ON AND OFF . CORRECTIVE ACTION IN PROGRESS. (K) 2 L 7 2 4F RT A21EA 20081010 NM 2008 10 10 KNN2008F00001 1 20080909 A 5330 SKIN BOEING 737 737291 138448W NM BS 986-1016 DENTED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 DURING CURRENT C-CHECK, FOUND MULTIPLE DENTS ON FUSELAGE SKIN BETWEEN STA 986.5 TO 1016 FROM STR 14L TO 15. CUTOUT DAMAG E AND INSTALLED A REPAIR IAW MFG MESSAGE 1-915180265-1 AND ACO-085342 WITH AN 8100-9. (K) 2 L 7 2 4F A16WE 20081010 NM 2008 10 10 SWAA085355 1 20081002 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND MAIN CABIN CREASE BEAM CRACKED AT BS 617 TO BS 639, LBL 60. REMOVED AND REPLACED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085365 1 20081001 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CRACKED AT BS 312, RBL 42. REMOVED AND REPLACED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085380 1 20081002 A 3350 311500 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 737JW 27869 FOUND EMERGENCY EXIT BULL NOSE LIGHT LENS MISSING AT 1C. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085381 1 20081002 A 3350 65C27095 BATTERY PACK BOEING 737 7377Q8 1384418 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 799SW 28209 DURING SCHEDULED HC2 CHECK, FWD LT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081010 EU 2008 10 10 UPS08153428 1 20080922 A 5753 A57960306200 RIVET AIRBUS A300 A300F4622R 3930360 EU T/E FLAP CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR LT WING CENTER FLAP MID CENTER HAVE RIVET HEADS CHAFED. REPAIRED LT WING CENTER FLAP CENTER AREA R EF A300-600 SRM. 2 L 7 2 4F RT A35EU 20081010 NM 2008 10 10 UPS08653442 1 20081003 A 2761 O-RING BOEING 767 76734AF 1385212 NM SPOILER ACTUATOR BROKEN A IPXA O OTHER K FLUID LOSS DE DESCENT 1 SO 01 304UP 27242 INSPECTION TYPE:N/A LOSS OF CENTER HYD QTY & CENTER HYD PRESSURE. CREW DECLARED EMERGENCY. NOSE WHEEL STEERING WAS AVA ILABLE AND TAXIIED TO GATE UNASSISTED. VERIFIED HYD LEAK AT NR 9 SPOILER ACT HOUSING CAP. FOUND O-RING UNDER CAP FLAT AND BROKEN, REF IPC 27-61-02 FIG 51. REPLACED O-RING. LEAK CHECK OK OF SPOILER. SERVICED CENTER HYD SYSTEM TO FULL. ON ARRIVAL A/C HYD WAS AT 20 PERCENT. 2 L 7 2 4F RT A1NM 20081010 CE 2008 10 10 GLB2008F00029 1 20080919 A 5510 114640000637 STABILIZER BEECH 1900 1900D 1154162 CE DAMAGED A GLBA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 03 122UX 24954 UE122 MAJOR REPAIR ACFT 122UX WHILE TAXIING THE ACFT TO THE GATE THE PILOTS STRUCK A JETWAY WITH THE TAIL OF THE ACFT DAMAGING THE VERTICAL AND HORIZONTAL STABILIZERS. THE STABILIZER WAS DAMAGED AND TWISTED TO THE LT FROM VERTICAL STABILIZER POS ITION CSS 39.289 TO CSS 69.184. THE HORIZONTAL STABILIZER WAS DAMAGED AT THE RT HAND OTBD EDGE AT HSS 110.63. MX R&R T HE VERTICAL STABILIZER IAW BEECH 1900D55-30-00 AND R&R THE HORIZONTAL STABILIZER IAW BEECH 1900D MM 55-10-00. RII INSPE CTIONS COMPLIED WITH FOR BOTH PER TASKCARDS 8.2.1. 2 L 7 2 4T RT A24CE 20081010 WP 2008 10 10 WRLA2008076 1 20080925 A 2520 INSULATION DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE LAVATORY OUT OF POSITION A WRLA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 11 136WA 47844 FLT T8000/RMS/25 DURING FLIGHT BURN ODOR WAS NOTED IN COCKPIT AND CABIN. FLIGHT ATTENDANT OBSERVED LIGHT SMOKE AND BURN ODOR EMANATING FROM FORWARD AND MID GALLEY VENTS. C/A REMOVED INSULATION MATERIAL DEBRIS FROM THE INSIDE OF THE LAV VE NT DUCT ASSY. LAV/GALLEY VENT AND CARGO HEAT NORMAL. FOLLOWED PROCEDURES IAW BOEING ERA 08-21-93. 2 L 7 3 4F 4 F A22WE E23EA 20081010 WP 2008 10 10 AALA200802244 1 20080830 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 585AA 53248 LGA EXTERIOR EMERGENCY LIGHTS AT AFT OVERWING DOOR INOPERATIVE. RESEATED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHTS AT AFT OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081010 WP 2008 10 10 AALA200802245 1 20080830 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN NOT SEATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 585AA 53248 LGA EMERGENCY LIGHTS AT CAT WALK INOPERATIVE. RESEATED BATTERY PACK FOR EMERGENCY LIGHTS AT CAT WALK. SYSTEM GROUND CH ECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081010 NM 2008 10 10 AALA200802188 1 20080818 A 5311 143T8204 FAILSAFE BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 378AN 25447 AFW FAIL SAFE STRAP AT FORWARD CARGO DOOR CUT OUT LOWER MAIN SILL HAD CORROSION. AREA OF DISCREPANCY IS 2 INCHES BY 1.8 INCH WITH A DEPTH OF .024 INCH. REPAIRED PER SRM 530001 AND PERFORMED HIGH FREQUENCY EDDY CURRENT TEST. NO CRACKS FOU ND. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081010 NM 2008 10 10 USAA920081678 1 20080913 A 5311 6546525 FRAME BOEING 737 7374B7 1384702 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CRACKS EMANATING FROM FASTENERS AT FRAME 380 BETWEEN S20L AND S21L. REPAIRED FRAME 380 BETWEEN S20L AND S21L IAW TYPICA L REPAIR NR 53-60-07. (K) 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 USAA920081680 1 20080821 A 5311 6546555 FRAME BOEING 737 7373G7 1384595 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 EXFOLIATION CORROSION ON FRAME AT BS 867, BL 0. REPAIRED FRAME AT BS 867, BL 0 IAW SRM 53-00-07-2R. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 AALA200802232 1 20080828 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 179AA 32397 JFK EMERGENCY LIGHTS AT SEAT 32D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 32D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 AALA200802235 1 20080828 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 179AA 32397 JFK EMERGENCY LIGHTS AT SEAT 35D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 35D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 AALA200802224 1 20080828 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 179AA 32397 JFK EMERGENCY LIGHTS AT FORWARD AND AFT OF LT & RT HAND NR 4 DOORS AND SEAT ROWS 25D TO 36D INOPERATIVE. REPLACED BATTE RY PACK AT M10801 FOR EMERGENCY LIGHT AT FORWARD AND AFT LT & RT HAND NR 4 DOORS AND SEAT ROWS 25D TO 36D. SYSTEM GROUN D CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081010 SO 2008 10 10 SIMA200827304 1 20080927 A 2120 UNKNOWN EMB 135 EMB135LR 3260305 SO CABIN ODOR A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 708AE 145205 ON FLIGHT 4574 DURING CRUISE CREW ADVISES NOTICEABLE BURNING SMELL IN COCKPIT. ACFT REMOVED FROM SERVICE. C/A PERFORME D VISUAL INSPECTION OF CABIN BALLASTS, CABIN LIGHTS, CONTROL MODULE. NO DEFECTS NOTED. NO BURNING SMELL NOTED AT THIS TIME. ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081010 NM 2008 10 10 2008UALA05756 1 20080916 A 3610 2790598101 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 FAULTY A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 552UA 26641 SPLIT DUCTS AT 30000 RT 10 PSI HIGHER THAN LEFT AT CRUISE THRUST SMALLER SPLIT AT IDLE THRUST. NR 2 HIGH STAGE VALVE WE AK. REPLACED NR 2 HIGH STAGE VALVE. OPS CHECK ON GROUND RUN NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081010 NM 2008 10 10 2008UALA05947 1 20080930 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY EXIT SIGN INOP JUST AFT OF LAV 102. REPLACED BATTERY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081010 2008 10 10 SIM2008F00023 4 20080907 A 3400 6226342022 ADI SAAB SF340 340B 7860101 EU MALFUNCTIONED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 298AE 340B298 ON FLIGHT 3275, AT CRUISE, CREW REPORTED NR 2 EADI FLICKERED AND EXTINGUISHED INOPERATIVE WITH SLIGHT ELECTRICAL ODOR WH ICH SOON DISSIPATED. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED EADI IAW AMM 34-24-10-04 COMPLIED WITH ADJUST TEST NO DEFECTS. ACFT RETURNED TO SERVICE. (K) 2 L 7 2 4T RT A52EU 20081010 NM 2008 10 10 2008UALA05954 1 20081001 A 5330 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 LT UPPER FUSELAGE EXT SKIN HAS DENT AT STA 1197 + 88 BETWEEN STR 1L AND STR 1R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAM AGE & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081010 NM 2008 10 10 2008UALA05959 1 20081002 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 818UA 882 BEAM 140 CORRODED. REMOVED FLOORBEAM 140. TRANSFERRING FASTENER HOLES TO NEW BEAM. INSTALLING FASTENERS IN NEW BEAM. INSTALLED BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081010 NM 2008 10 10 2008UALA05963 1 20081002 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 818UA 882 BEAM 150 CORRODED. REMOVED FLOORBEAM 150. REMOVED BRACKETS AND DRILLED NEW BEAM AND READY FOR BRACKET INSTALL ON NEW B EAM. INSTALLED BEAM, NEEDS 2 BOLTS AT STA 70, 8 BOLTS AT STA 68. COMPLETED INSTALLATION OF BEAM. INSPECTED FINAL INST ALLATION OF BEAM 150. FOUND SERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081010 NM 2008 10 10 2008UALA05966 1 20081002 A 7330 SWITCH BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 792UA 26934 ENG FUEL VALVE LEFT STATUS MSG. FOUND LT ENG CUTOFF SW INOP. REPLACED RELAY K76104 DUE TO PREVIOUS HITS. REPLACED LEFT ENG FUEL CUTOFF SWITCH. ENG RUN CHECKS OKAY. NO EXISTING FAULT MESSAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081010 NM 2008 10 10 2008UALA05968 1 20081003 A 4920 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU MISSING A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION IN INSP/MAINT 1 WP 29 598UA 28751 APU FAILED TO START. FAULT LIGHT ILLUM AND EICAS MSG. APU FAULT DISPLAYED. SECOND ATTEMPT INDICATES (SLOW ACCEL, HUNG START). FOUND MISSING HARDWARE SENSOR ON LT SIDE OF APU PLENNUM. NONE STOCKED AT IAD. UNABLE TO DETERMINE IF THE LIS TED PARTS WILL COMPLETE THE REPAIR AS IPC DOES NOT SHOW VIEW INSIDE THE PLENUM. THE APU WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081010 WP 2008 10 10 IXX2008F00095 1 20080911 A 2612 FIRE WARNING DOUG DC8 DC871F 302199D WP NR 2 MALFUNCTIONED A IXXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 11 823BX 46064 DURING CRUISE, NR 2 FIRE WARNING CAME ON INTERMITTENTLY. THE CREW SHUTDOWN NR 2 ENGINE, WAS UNABLE TO ACCOMPLISH FIRE W ARNING TEST. THE CREW DISCHARGED 1 FIRE BOTTLE, ACCOMPLISHED FIRE WARNING TEST. SEVERAL MINUTES LATER NR 2 FIRE WARNING CAME ON AGAIN, THE CREW DISCHARGED THE 2ND FIRE BOTTLE. FIRE WARNING TESTED GOOD. THE CREW LANDED WITHOUT FURTHER INC IDENT. (K) 2 L 7 4 4F RT 4A25 20081010 SO 2008 10 10 RAIA00809003 1 20080904 A 7500 DUCT EMB 145 EMB145 3260210 SO BLEED SYSTEM DISCONNECTED A RAIA O OTHER O OTHER NR NOT REPORTED 1 SW 99 821HK 145068 DURING CLIMB CREW RECEIVED A BLEED 1 AND 2 LEAK MESSAGE ON THE EICAS. MAINT INSPECTED THE NR 1 AND NR 2 BLEED SYS. FOU ND THE NR 2 PACK EXHAUST DUCT TO BE DISCONNECTED. DUCT WAS RESECURED AND NO OTHER DEFECTS WERE NOTED. (K) 2 L 7 2 4F RT T00011AT 20081010 NM 2008 10 10 AALA200802202 1 20080826 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 184AN 29594 DFW EMERGENCY LIGHT AT OVERHEAD SEAT 23C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 23C. SYSTEM G ROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081010 WP 2008 10 10 AALA200802200 1 20080826 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70529 49921 LGA EMERGENCY LIGHTS AT FORWARD OVERHEAD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT FORWARD OVERH EAD CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081010 WP 2008 10 10 AALA200802199 1 20080826 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70529 49921 LGA EMERGENCY LIGHT AT SEAT 20D HAS BROKEN LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 20D. SY STEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081010 WP 2008 10 10 AALA200802198 1 20080826 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70529 49921 LGA EMERGENCY LIGHTS AT TAIL COMPARTMENT INOPERATIVE. RESEATED BATTERY FOR EMERGENCY LIGHTS AT TAIL COMPARTMENT. SYSTE M GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081010 WP 2008 10 10 AALA200802197 1 20080826 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 961TW 53611 BOS EMERGENCY EXIT SIGN AT OVERHEAD FORWARD OVERWING DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN AT OVERHEAD FORWARD OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081001 NM 2008 10 1 SWAA085146 1 20080921 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 15R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 08FDEA04483 1 20081022 A 5311 651634112 FRAME BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 AFT LOWER CARGO PIT STA 1010 BETWEEN STR 28R AND 27R FRAME CORRODED 2 L 7 3 4F A3WE 20081001 NM 2008 10 1 SWAA085145 1 20080921 A 5313 6551698 STRINGER SPLICE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 24R. REMOVED AND REPLACED STRINGER SPLICE PE R SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 F3LA2008102200674 1 20081021 A 3250 D231197501 ELECTRICAL BOX AIRBUS A319 A319111 3930336 NM NLG STEERING MALFUNCTIONED A F3LA O OTHER J WARNING INDICATION CL CLIMB 1 NM 21 913FR 20 1863 FLIGHT NUMBER 435 FROM OMA TO DEN, FLIGHT CREW NOTICED NOSE WHEEL STEERING DISPLAY IN "AMBER" ON MEMO PAGE. NORMAL LAND ING IN DENVER. AFTER SHUTTING DOWN NR 2 ENGINE, LOST ALL STEERING. MAINTENANCE REMOVED AND REPLACED THE NOSE WHEEL STE ERING DEACTIVATION ELECTRICAL BOX AND PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH A319 AMM 32-51-12 PB 401. MAINTENA NCE ALSO REMOVED AND REPLACED THE BRAKING STEERING CONTROL UNIT AS PRECAUTIONARY PROCEDURE AND PERFORMED OPERATIONAL CHE CK IN ACCORDANCE WITH A319 AMM 32-42-34 PB 401 AND 22-97-00-710-001. 2 L 7 2 4F RT A28NM 20081024 NM 2008 10 24 F3LA2008102200677 1 20081020 A 5315 D53472189204 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON FLOORBEAM -Y1292 AT FRAME 68, PASSENGER CABIN. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IN ACCORDANCE WITH A319 SRM 51-42-11 PAGE 1 AND 2. 2 L 7 2 4F RT A28NM 20081016 EA 2008 10 16 VNAA2008100900002 1 20081007 A 2751 601R930303 TRANSMITTER CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP FAILED A VNAA K NONE O OTHER DE DESCENT 1 GL 05 220PS 11119 7887 CREW REPORTED IN DESCENT AT 290KTS W/AUTOPILOT ON, UCA AND FLAP INDICATORS DEPLOYED ON EICAS PAGE. FLAP INDICATOR SHOWE D GREEN BAR MOVEMENT AND READOUT MOVED TO 2 DEG. AIRCRAFT HAD PITCH OSCILLATIONS OF APPROX 3 DEG NOSE UP AND DOWN. MAI NTENANCE REMOVED AND REPLACED THE FLAP TRANSMITTER. NO OTHER DEFECTS WERE NOTED AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20080930 NM 2008 9 30 UPS08M53148 1 20080816 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C FOUND CORROSION IN NR 18 LEFT BARREL NUT BORE HOLE. REMOVED CORROSION, FABRICATED AND INSTALLED REPA IR BUSHING IAW UPS EO MD11-5510-19409-N. 2 L 7 3 4F RT A22WE 20080930 NE 2008 9 30 2008UALA04351 2 20080820 A 7200 UNKNOWN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ENGINE UNKNOWN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 214UA 30220 ENG IGNITOR L1 LEFT ENGINE FAILED TO IGNITE USING IGNITOR 1. 2 L 7 2 4F 4 F RT T0001SE E46NE 20080930 NM 2008 9 30 2008UALA04114 1 20080803 A 3350 78961 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EEL INOP: SEAT 4A AFT SECTION. *S/D* FOUND FAULTY LIGHT. REPLACED LAMP, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04215 1 20080809 A 3320 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26877 UPPER DECK FWD DOOR CEILING LIGHT INOP. REPLACED LAMP, OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 NM 2008 9 30 2008UALA04247 1 20080811 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 814UA 862 FLOORBEAM 150 CORRODED (MARKED). REMOVED FLOORBEAM. TRANSFERRED BRACKETS ONTO NEW FLOORBEAM. CONNECTED FLOORBEAMS 150 AND 95 TOGETHER AND HAVE THEM IN PLACE. INSTALLED FLOORBEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA04193 1 20080808 A 2611 824PTY SMOKE DETECTOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU AFT LAVATORY INOPERATIVE A UALA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 WP 29 923UA 26643 PAX WAS SMOKING IN AFT LT LAV AND SMOKE DET DID NOT GO OFF. FOUND FAULTY SMOKE DETECTOR. REPLACED SMOKE DETECTOR, OP C HECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 20081001 NM 2008 10 1 ZZDA2008161 1 20080924 A 3350 8039251 POWER SUPPLY BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 932AT 55073 EMERGENCY BATTERY SUPPLY STA 332 INOPERATIVE. REPLACED EMERGENCY BATTERY SUPPLY PER MM 33-50. OPS CHECK GOOD. 2 L 7 2 4F TR A6WE 20081001 EU 2008 10 1 08FDEA04112 1 20080929 A 5321 SRZ25005242UG FLOORBOARD AIRBUS 310 A310222 3930315 EU CABIN DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 MAIN CABIN FLOORBOARD NR 242 UG IS DAMAGED, CRACKED. FABRICATED A NEW FLOORBOARD NR 242 UG IAW DWG SRZ 25-005, REV "G" . 2 L 7 2 4F RT A35EU 20081001 NM 2008 10 1 SWAA085205 1 20080922 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 787 + 4 STR 17L. REMOVED AND REPLACED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081010 WP 2008 10 10 AALA200802196 1 20080826 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9626F 53596 LAX EMERGENCY PORTABLE LIGHT AT LT NR 1 DOOR INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT AT LT NR 1 DOOR. SYSTEM GR OUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081014 NM 2008 10 14 UPS08653449 1 20080927 A 5754 BRACKET BOEING 767 76734AF 1385212 NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 330UP 27756 INSPECTION TYPE:N/A LT WING NR 6 SLAT INNER LOWER NR 5 AND NR 8 BRACKET FOUND CRACK 2EA CRACK LENGTH .5 INCH APPROX. TW O BRACKETS REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081014 NM 2008 10 14 UPS08653450 1 20080929 A 5754 BRACKET BOEING 767 76734AF 1385212 NM L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 330UP 27756 INSPECTION TYPE:N/A RT WING NR 7 SLAT 3EA BRACKET NR 10, 11, 12 FOUND CRACK. CRACK LENGTH .5 INCH APPROX. RT WING NR 7 SLAT 3EA BRACKET NR 10, 11, 12 REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081014 NM 2008 10 14 UPS08653452 1 20080926 A 5315 141T514622 STIFFENER BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 330UP 27756 INSPECTION TYPE:N/A CABIN STA 246 RBL 10 FLOORBEAM ATT STIFFENER CRACKED. CRACK LENGTH 1 INCH. DEFECTIVE STIFFENER REP LACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081014 NM 2008 10 14 UPS08M53462 1 20080806 A 5311 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:N/A CTR CARGO FRAME AT STA 1661 BILGE AREA BETWEEN L51 LT & RT FOUND CORROSION. FRAME SHEAR CLIP CORROS ION REMOVED AND REPROTECTED AS PER SRM 51-21- 01. MATERIAL REMOVED 0.005" ORIGINAL THK 0.071" REMAINED 0.066" FOUND WIT HIN LIMIT PER SRM 53-00-01 FIG 2. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 CALA0800944 1 20081006 A 5320 6556655 WEB BOEING 737 737524 1384721 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 BODY STATION 787 AT STRINGER 25R FRAME CLOSE-OUT WEB DAMAGED. REMOVED DAMAGED WEB CLOSE-OUT AT BODY STATION 787 AT STR 25R IAW B737 SRM 51-40-02, FABRICATED NEW WEB PER BOEING DRAWING 65-56655. ALODINED AND PRIMED PER B737 SRM 51-20-01. INSTALLED NEW WEB CLOSE-OUT SECTION IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 CALA0800945 1 20081006 A 5320 6517684638 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 WEB CRACKED BODY STATION 294.3 LT INTERCOSTAL 12. REMOVED AND REPLACED CRACKED WED PER ECRA 5311-01424 REV A. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 CALA0800947 1 20081006 A 3213 161T1120 LUG BOEING 767 767224 1385170 NM LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76156 30435 EA3210-01986 REV B LEFT MAIN LANDING GEAR INNER CYLINDER PIVOT BORE OF INBOARD LUG FOUND CORROSION AFTER BUSHING REMOVED . MAIN LANDING GEAR INNER CYLINDER INBOARD LUG PIVOT BORE REPAIRED IAW ECRA 3210-02114. GEAR RETRACTION TEST COMPLETED IAW AMM 32-32-00. 2 L 7 2 4F RT A1NM 20081014 CE 2008 10 14 J7SA60196081002 1 20081002 A 2120 UNKNOWN LEAR 60 60LEAR 5170707 CE COCKPIT SMOKE E J7SA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 05 252FX 60196 FLIGHT CREW REPORTED AT LEVELING OFF AT FL 410, OBSERVED A PUFF OF SMOKE (THE SIZE OF A FOOTBALL) RISE FROM THE LOWER AR EA OF THE COPILOT'S CONTROL YOKE. THE SMELL WAS MORE A RUBBER SMELL AND NOT SO MUCH ELECTRICAL. COPILOT REPORTED THE S AME SMELL COULD BE DETECTED IN THE AREA OF THE BATTERY COMPARTMENT. THE SMOKE CLEARED WITHIN A VERY SHORT TIME AND DID NOT RETURN. FLIGHT CREW REPORTED NO CIRCUIT BEAKERS POPPED, NO WARNING LIGHTS ILLUMINATED, AND NO SYSTEMS FAILED TO FUN CTION. MX PULLED UP COCKPIT FLOORBOARDS AND FOUND NO EVIDENCE OF BURNING. PERFORMED ENGINE RUNS WITH CABIN AIR ON/OFF, GENERATORS ON AND LOADED UP, EVERYTHING TURNED ON. NO BREAKERS POPPED, NO SMOKE OR BURNING SMELL NOTED. COULD NOT DUP 2 L 7 2 4F RT A10CE 20081014 EA 2008 10 14 VNAA2008100700001 1 20081003 A 5280 CC670330983 DOOR CNDAIR CL600 CL6002C10 1390015 EA NLG BROKEN A VNAA O OTHER O OTHER UK UNKNOWN 1 GL 05 718PS 10175 POST FLIGHT INSPECTION REVEALED AFT NOSE LANDING GEAR DOOR WAS BENT AND BROKEN. MAINTENANCE REMOVED, REPLACED AND REPAI RED DAMAGE TO NOSE LANDING GEAR DOOR AREA OF AIRCRAFT. NO OTHER DAMAGE WAS NOTED AND AIRCRAFT WAS RELEASED FOR SERVICE . 2 L 7 2 4F RT A21EA 20081014 WP 2008 10 14 IXXA08SMN129S 1 20080411 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C-CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 35 LONGERON 25.5 RIGHT. REMOVED FASTENERS AS NEE DED TO PERFORM REPAIR. REMOVED EXISTING SPLICE DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED SKIN SEGMENT, SPLICE DOUBLERS, INTERNAL FINGER DOUBLER, INTERNAL DOUBLER, AND INTERNAL DOU BLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS DC8 SRM 51-1-11, 51 -1-20D, 51-3-1, FAA FORM 8110-3 NUMBER 08188 DATED 04/23/08, SEMAN DRAWING ED-4755 DATED 04/21/08, DC8 SRM 51-1-21, SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 20081014 NM 2008 10 14 UIEA200800325 1 20080926 A 5330 SKIN BOEING 747 7472D7B 1384803 NM FUSELAGE DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 FUSELAGE SCRIBE LINE OVERLAPPED SKIN BETWEEN STA 670 TO 741 AT STR 34R DAMAGED. REPAIRED IAW BOEING SERVICE REQUEST 1-7 51139674 APPROVED BY FAA FORM 8100-9 DATED 26 SEP 2008. DETAILS OF WORK PERFORMED KEPT ON ATLAS ENGINEERING ORDER EO475 3B207 AND EO4753B114. 2 L 7 4 4F RT A20WE 20081014 SO 2008 10 14 RAIA2008100800034 1 20081001 A 3230 800571 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG DEFECTIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 819HK 145062 DURING CLIMBOUT OF STL, CREW HEARD BANGING NOISE FROM NOSE GEAR WITH GEAR RETRACTED. MAINTENANCE REMOVED AND REPLACED T HE LT NLG FWD DOWNLOCK PROXIMITY SWITCH AND CONNECTOR IN ACCORDANCE WITH AMM PROCEDURES. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081014 SO 2008 10 14 RAIA2008100800036 1 20081004 A 3397 CONNECTOR EMB 145 EMB145 3260210 SO CABIN DIRTY A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 821HK 145068 DURING PRE FLIGHT INSPECTION, IT WAS DISCOVERED THAT THE EMERGENCY LIGHT OVER THE SERVICE DOOR DID NOT WORK. MAINTENANC E CLEANED THE CONNECTOR TO THE APPLICABLE EMERGENCY LIGHT BATTERY. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 20081014 EU 2008 10 14 YENA2008100800094 1 20081003 A 5270 89331 PROXIMITY SENSOR AIRBUS 320 A320232 3930326 EU CARGO DOOR FAILED A YENA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 597JB 16730 2307 AFTER TAKEOFF FROM POP-JFK, RECEIVED DOOR FWD CARGO ECAM MESSAGE INDICATING DOOR WAS UNLOCKED. REMOVED AND REPLACED PRO X SENSOR 30WV FOR FWD CARGO DOOR PER AMM 52-71-12-04. OPS CHECK OK. 2 L 7 2 4F RT A28NM 20081014 SO 2008 10 14 RAIA2008100800037 1 20081005 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 835HK 145670 DURING THE PRE FLIGHT INSPECTION, IT WAS DISCOVERED THAT THE EMERGENCY LIGHT AT THE MAIN PASSENGER DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081001 NM 2008 10 1 SWAA085203 1 20080922 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 346SW 24153 DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 360 + 12 STR 15L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085199 1 20080923 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED MV1 CHECK, FOUND FWD EMERGENCY FLOOR LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081001 2008 10 1 UPS08853411 4 20080925 A 2565 RETAINER DOUG DC8 DC873F 302199F WP ESCAPE SLIDE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 SLIDE CONTAINER IS OPEN. DEFERRED M385289 ASSIGNED. SLIDE CONTAINER RETAINER BROKEN DEFERRED MAIN ENTRY ESCAPE SLIDE P ER MEL 52-7-4. SLIDE REMOVED AND ROUTED TO AMDC. COURIER SEATS NOT TO BE OCCUPIED. INSTALLED EVACUATION SLIDE PER AMM 25-60-01. PLACARDS REMOVED. 2 L 7 4 4F RT 4A25 20081001 NM 2008 10 1 UPS08553401 1 20080926 A 5420 SUPPORT BOEING 757 75724APF 1384969 NM LT NACELLE CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 424UP 25369 INSPECTION TYPE:C2 NR 1 ENGINE STRUT LT NAC STRUT STA 214.0 SUPPORT STRUCTURE CHAFED. BLENDED CHAFED AREA; BLEND FOUND TO EXCEED STRUCTURAL LIMITS; REMOVED AND REPLACED DISCREPANT ZEE CHANNEL. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 SWAA085220 1 20080924 A 2560 PL22300LH GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 DURING SCHEDULED C2 CHECK, FOUND PHOTOLUMINESCENT STRIP DAMAGED AT SEAT 9C. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085170 1 20080922 A 3350 20131SWA BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT ROW 1 THRU ROW 6. REMOVED AND REPLACED BATTERY PACKS PE R AMM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085167 1 20080921 A 2560 PL22300L GLOWSTRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED 14Y CHECK, FOUND EMERGENCY EVACUATION PHOTOLUMINESCENT STRIPS WORN IN CABIN. REMOVED AND REPLACED STRI PS PER AMM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085158 1 20080923 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 606SW 27926 R1 EMERGENCY EXIT SIGN LENS FELL OFF. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 08FDEA04125 1 20080929 A 5347 651960132 SEAT TRACK BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 MAIN CABIN BS 1110 SEAT TRACK AT RBL 45 IS CORRODED REMOVED AND REINSTALLED FLOORBOARDS RBL 24 TO RBL 62 STA 1070-1110. REMOVED CORROSION ON SEAT TRACK ORIGINAL MATERIAL THICKNESS .070 MATERIAL LOSS .022. REMAINING .048 OUT OF LIMITS AAR TOOL IN17-0112 CAL DUE 12-11-08. REMOVED SEAT TRACK SECTION STA 1110=1135. FABRICATED TREATED, PRIMED, AND INSTALLED NEW SEAT TRACK SECTION STA 1110-1135 RBL 45. DISPLACED AND REINSTALLED CEILING PANEL STA 1130-1140 RBL 25-50, REF SRM 51-30-2, 51-10-6, 53-10-1 FIG 3, AND DWG 65-19601. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081001 NM 2008 10 1 SWAA085193 1 20080923 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND LT KEEL BEAM CORRODED AT STA 663 TO 727. REMOVED AND REPLACED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085192 1 20080917 A 2560 6557463 BRACKET BOEING 737 7377H4 1384404 NM EVAC SLIDE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 745SW 29491 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR SLIDE AFT ANCHOR BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085191 1 20080918 A 5330 141A37024 SKIN BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 718SW 27852 DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT EXTERNAL POWER RECEPTACLE DOOR CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 08FDEA04068 1 20080926 A 5720 652165688 RETAINER BOEING 727 727227 1384078 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 LT WING SPAR UNDERWING PANEL SEAL RETAINER HAS CORROSION O/B OF APU FIRE BOTTLE AT WS 182 TO 200. FABRICATED SEAL RET AINER REF DWR 65-21656. TREATED AND PRIMED REF SRM 51-10-2 PG 1- 9. INSTALLED SEAL RETAINER REF 51-30-2 P1-3. THIS I S A CLASSIFIED A MINOR REPAIR. 2 L 7 3 4F A3WE 20081001 NM 2008 10 1 2008UALA05758 1 20080916 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 817UA 873 FLOORBEAM 80 CORRODED. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED BOLTS AT FWD END OF BEAM. REMOVED AND DISASSEMBLED FLOORBEAM. TRANSFERRED HOLES TO NEW BEAM. PICKED UP HOLES ON FWD SPLICE. INSTALLED AFT SPLICE. INSTALLED BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081001 EU 2008 10 1 08FDEA04069 1 20080926 A 5310 A53779699200 CROSSBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 663FE 766 MAIN DECK CARGO COMPARTMENT FR 31 FWD FACE UPPER SIDE HAS .100 IN CRACK, BETWEEN SEAT TRACKS NR 4 LT AND TRACK NR 5 LT R EMOVED CRACK AT CROSSBEAM FR 31 AND INSTALLED CROSSBEAM CRACK REPAIR AT STIFFENER BETWEEN TRACKS NR 4 LT AND TRACK NR 5 LT IAW A300-600 FREIGHTER SRM 53-10- 15, FIG 212, SHEETS 1 AND 2. 2 L 7 2 4F RT A35EU 20081001 EU 2008 10 1 08FDEA04070 1 20080926 A 5347 A532274005 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 663FE 766 MAIN DECK CARGO COMPARTMENT SEAT TRACK 2 RT HAS CORROSION AT FR 41,3 SQ IN. REMOVED LEVEL 1 CORROSION AT MDCC SEAT TRAC K NR 2RT. REMOVED DAMAGED SECTION AND INSTALLED SEAT TRACK SPLICE REPAIR BETWEEN FR 40 AND FR 45,TRACK NR 2RT IAW A300- 600 SRM 53-10-16, FIG 201, PAGE 207/208. 2 L 7 2 4F RT A35EU 20081014 NM 2008 10 14 SWAA085407 1 20081006 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 18L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085409 1 20081006 A 5610 57176145 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 315SW 23337 L1 COCKPIT WINDOW ARCING. REMOVED AND REPLACED L1 WINDOW AND CONTROLLER PER MM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085413 1 20081006 A 5310 6547978 CREASE BEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED 18Y CHECK, FOUND LT CREASE BEAM CORRODED BETWEEN BS 312 TO BS 344. REMOVED AND REPLACED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085388 1 20081005 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085392 1 20081004 A 3350 65C27095 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 HNAA0800290 1 20080914 A 3610 7821004 SWITCH DHAV DHC8 DHC8102 2809003 NM BLEED AIR SYS BROKEN A HNAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 07 942HA 2490 163 NR 2 BLEED HOT CAUTION LIGHT ILLUMINATED IN FLIGHT. R&R NR 2 ENGINE HIGH PRESSURE BLEED SWITCH. REFERENCE MM 21-11-21. GROUND RUN OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 20081009 SO 2008 10 9 SIMA200826804 1 20080922 A 3350 22250005000 SIGN EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 643AE 145200 ON FLIGHT 3943 CREW REPORTED AFT PORTION OF OVERHEAD EXIT SIGN AT ROW 12 FAILS TO ILLUMINATE. ACFT REMOVED FROM SERVICE . C/A R&R AFT OVERHEAD SIGN LIGHT AT ROW 12 IAW EMB AMM 33.50/15 OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081009 SO 2008 10 9 SWIA200820080 1 20080923 A 3397 WIRE EMB 120 EMB120ER 3260203 SO STROBE LIGHT BURNED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 226SW 120296 RIGHT STOBE LIGHT INOP. (C-CHECK) REPLACED BURNED WIRE TO TERMINAL. 2 L 7 2 4T RT A31SO 20081009 NM 2008 10 9 F3LA2008100600670 1 20081002 A 5320 D5348015800600 PLATE AIRBUS A319 A319111 3930336 NM CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 931FR 52 2253 DURING C3 C-CHECK, INSPECTION NOTED L-2 GIRT BAR FITTINGS ATTACH PLATE HOLES HAVE CORROSION. MAINTENANCE FABRICATED REPA IR DOUBLER AND FILLER, TREATED, PRIMED, PAINTED AND INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF ENGINEERING AUTHORI ZATION A9-53R-30662. 2 L 7 2 4F RT A28NM 20081009 NM 2008 10 9 ASAA0853536 1 20080929 A 3040 8300005604 WARNING SYSTEM BOEING 737 737890 1384527 NM WINDOW HEAT ACTIVATED A ASAA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 02 558AS 35789 35177 WINDOW HEAT OVERHEAT LIGHT ILLUMINATED (LEFT SIDE) AFTER REAPPLYING POWER IAW THE QRH PROCEDURE THE OVERHEAT LIGHT CAME ON AGAIN. THE OUTSIDE STATED AIR TEMP WAS 60C, CONFIRMED LEFT SIDE WINDOW HEAT OVERHEAT ONE WITH WINDOW HEAT C/B POPPED . RESET WINDOW HEAT PWR LT SIDE PER 20 60 01. PERFORMED OPS CHECK PER 30 41 00, NO FAULTS NOTED AT THIS TIME. COULD N OT DUPLICATE DISCREPANCY. NO FURTHER DISCREPANCIES NOTED. 2 L 7 2 4F RT A16WE 20081009 2008 10 9 2008UALA05511 4 20080829 A 2310 8220330001 TRANSCEIVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HF COMM FAILED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 598UA 28751 RADIO PROBLEM. SHOP REPORT: FOUND INTERMITTENT RX. RPL Q6 & Q7 IN RX. REPLACED RT HF TRANSCEIVER. 2 L 7 2 4F 4 F RT A2NM E17NE 20081009 EU 2008 10 9 2008UALA05586 1 20080904 A 2913 PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYDRAULIC SYS DEFECTIVE A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 461UA 1266 BLUE SYSTEM HYD PROBLEM. RTFL. BLUE SYSTEM EDP SUSPECT FAILING. REPLACED BLUE SYSTEM EDP, RESERVOIR AND SYSTEM ACCUMU LATOR, BLED BLUE HYD SYSTEM & OPERATION NOW NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081009 NM 2008 10 9 2008UALA05934 1 20080930 A 7930 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT ACTIVATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 652UA 25390 THE 'R OIL FILTER' STATUS MSG DISPLAYED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081009 NM 2008 10 9 2008UALA05935 1 20080930 A 2432 K24006 RELAY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE MAIN BATTERY FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 779UA 26941 ELEC STANDBY SYS ELECTRICAL DC-STANDBY POWER SYSTEM FAILED THE SYSTEM SELF-CHECK. STATUS MSG-2413035 ACTIVE DC MODE MSG -2413035 ACTIVE DC MODE. REPLACED MAIN BATTERY RELAY. CHECKS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081009 NM 2008 10 9 2008UALA05936 1 20080930 A 3350 3071BPEGPL LAMP BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 222UA 30553 EMERGENCY LIGHT AT SEAT 18G IS OUT. LAMP FOUND INOP. REPLACED LAMP. OP TESTS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081001 NM 2008 10 1 08FDEA04071 1 20080926 A 5711 ARB74132 SPAR CAP DOUG MD11 MD11F 3023600 NM ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 RIGHT WING REAR SPAR UPPER CAP AT STA XORS 676, 875, AND 887 FOUND HOLE ELONGATED. CARRIED OUT REPAIR AS PER EA NR 1- 5710-123124. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 2008UALA05759 1 20080917 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 817UA 873 FLOORBEAM 150 CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM. ASSEMBLED AND PICKED UP HOLES. ATTACHED TO BEAM 95 AND STARTED INSTALLATION. INSTALLED BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081001 EU 2008 10 1 08FDEA04073 1 20080927 A 2611 CG7G011 SMOKE DETECTOR AIRBUS 300 A300B4622R 3930312 EU ZONE 100 FAILED A FDEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 21 716FD 358 AV SMOKE ALARM ON TAXI OUT. ACFT SUFFERED RAIN INGRESSION, DRIED OUT COURIER AREA AND AVIONICS BAY AREA. VERIFIED THAT FLOOR AND DRIP PAN DRAINS ARE CLEAR AND DRAIN NORMALLY. REMOVED AND REPLACED AVIONICS DUCT SMOKE DETECTOR 13WA PER A MM 26-15-12-4. PERFORMED SATISFACTORY OPS CHECK PER AMM 26-15-00. OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A35EU 20081001 NM 2008 10 1 2008UALA05760 1 20080917 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 817UA 873 FLOORBEAM 145 CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED AND DISASSEMBLED FLOORBEAM. TRANSFERED HOLES TO NEW BEAM. INSTALLED SPLICE ANGLES TO ATTACH BEAM 145 TO BEAM 140. INSTALLED FLOORBEAM TO FRAME. INSTALLED SECURING FASTENERS. 2 L 7 2 4F 4 F RT A28NM E40NE 20081001 NM 2008 10 1 2008UALA05762 1 20080917 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 817UA 873 FLOORBEAM 175 CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM AND ANCHOR FITTINGS. INSTALLED ANCHOR FITTINGS AND FI TTED BEAM 175 INTO ACFT. DRILLED HOLES FOR AFT END BRACKET. STARTED INSTALLATION OF BRACKET. STILL NEED TO ATTACH TO FRAME. INSTALLED FLOORBEAM 175 IN AC. 2 L 7 2 4F 4 F RT A28NM E40NE 20081001 NM 2008 10 1 2008UALA05800 1 20080919 A 4920 ENGINE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE APU FAILED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 793UA 26946 APU EMITS SMOKE FROM TAIL PIPE. OIL QTY RAPIDLY DROPPED TO ZERO. TURBINE BLADE TIP DAMAGE ON OLD APU. REPLACED APU. OP S NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081001 NM 2008 10 1 2008UALA05802 1 20080919 A 8011 35054367 STARTER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 648UA 25285 L ENG START VALVE WON'T OPEN. START VALVE MALFUNCTIONED. REPLACED STARTER AND STARTER VALVE. ALL CHK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081001 2008 10 1 2008UALA05803 4 20080918 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR SLIDE UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 DOOR 1R WILL NOT ARM. SECURED LOOSE LANYARD ON SLIDE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081001 NM 2008 10 1 2008UALA05804 1 20080920 A 2797 WIRE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE TE FLAP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 214UA 30220 WHILE RETRACTING FLAPS DURING TESTING OF CALLOUT AM6818 SKEW SENSOR R8A BLANKS TO ZERO ON EICAS. FLAP POS 1 TO 5 AND AG AIN FROM 5 TO 15. FOUND WIRE 8478-2003B DAMAGED NEAR DM27324 SNSR 7A. REPAIRED REF GNMM 2-0-15. FSEU SYSTEM TEST OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081001 EU 2008 10 1 2008UALA05805 1 20080921 A 3510 FITTING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW OXYGEN LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 465UA 1341 CREW OXYGEN SYSTEM-LOW. RECORD PRESSURE PRIOR TO SERVICING. LEAKED CHECKED CREW O2 SYS, FOUND TWO SMALL LEAKS AT THE S ERVICE FITTING & HOSE FITTING ON FRONT OF O2 BOTTLE. SERVICED CREW O2 TO NR 3 SERVICE LIMITS. (STARTING PRESS 1400 PSI) NO OTHER LEAKS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081001 EU 2008 10 1 08FDEA03198 1 20080731 A 5347 A5327400500053 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 THE MAIN CABIN SEAT TRACK AT FRAME 30, LBL 40 INCH HAS A BENT FLANGE. REMOVED DAMAGED SEAT TRACK PER SRM 51-41-21. LO CATED AND DRILLED TRACK PER SRM 53-10-16. INSTALLED SEAT TRACK AND SPLICES PER SRM 51-41-02, SRM 53-10-16 AND DWG A5378 1911. APPLIED CIC PER AMM 51-22-00-0. 2 L 7 2 4F RT A35EU 20081001 WP 2008 10 1 08FDEA03199 1 20080731 A 5753 ARC27362 SKIN DOUG MD10 MD1010F 3022112 WP RT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 372FE 46610 RIGHT WING INBD FLAP LOWER SKIN SURFACE HAS AREAS OF DENTS. FABRICATED A NEW SKIN PANEL ASSEMBLY IAW EA NR 8-5750-11853 4. 2 L 7 3 4F RT A22WE 20081001 EU 2008 10 1 08FDEA03420 1 20080814 A 5320 A53973057202 FLOOR SUPPORT AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND IN AFT CARGO COMPARTMENT CORROSION ON SECTION BEAM C67-69, P 45-46 RT. REPAIR PERFROMED BY REPLACEMENT OF PART IA W SRM 51-72-10. 2 L 7 2 4F RT A35EU 20081001 EU 2008 10 1 08FDEA03421 1 20080814 A 5320 A53973263210 STRAP AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 DURING P TO F FOUND FRAME COUPLING WITH TO LESS RIVET PITCH. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20081001 WP 2008 10 1 08FDEA03206 1 20080801 A 5320 NJC6010 CHANNEL DOUG DC10 DC1030F 3023504 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 FWD CARGO COMPT SEVERE CORROSION WITH EXFOLIATION ON CHANNEL UPPER SIDE. REPAIRED CHANNEL IAW SRM 53-70-00 VOL I FIG 7. 2 L 7 3 4F RT A22WE 20081001 WP 2008 10 1 08FDEA03208 1 20080801 A 5730 NRC6066525 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 LT WING OUTBD FLAP FOUND CRACKS ON LWR SKIN. 2 L 7 3 4F RT A22WE 20081001 EU 2008 10 1 08FDEA03209 1 20080801 A 5320 A5397822420401 RETAINER AIRBUS 300 A300F4605R 3930327 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 AFT CARGO DOOR CUT-OUT AFT SIDE SEAL LAND IS NICKED AND GOUGED IN SEVERAL PLACES AT BOTH TOP AND BOTTOM CORNERS. REMOVE D AND REPLACED THE AFT CARGO DOOR SEAL LANDS (3EA) IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 20081001 WP 2008 10 1 08FDEA03210 1 20080801 A 5420 ANGLE DOUG MD10 MD1010F 3022112 WP ZONE 400 LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 THE NR 3 PYLON AFT BULKHEAD TO SPAR ANGLE, INBD AND OUTBD SIDES HAS 1 EA BOLT PER SIDE LOOSE AT PYLON STA YN 417. REMOV ED AND REPLACED 2 EA FASTENER IAW DC/MD-10 SRM 51-31-01; VOL II AND TORQUED IAW DC/MD-10 AMM 20-30-02-2. PERFORMED HFEC EDDY CURRENT INSPECTION. NO CRACKS NOTED. 2 L 7 3 4F RT A22WE 20081001 WP 2008 10 1 08FDEA03211 1 20080801 A 5411 SPAR DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 564FE 46984 THE NR 3 PYLON UPPER SPAR OUTBD AND INBD SPAR ANGLES HAVE 3 BOLTS; FWD TO AFT; BOTH SIDES LOOSE AND 7 FROM INBD TO OUTBD ARE LOOSE ON THE UPPER WEB AT PYLON STA YN 358. COMPLIED WITH FEDEX EA 8-5450-123625. 2 L 7 3 4F RT A22WE 20081001 EU 2008 10 1 08FDEA03213 1 20080801 A 5340 A5361181520000 ATTACH FITTING AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 664FE 768 THE MAIN CARGO DECK FLOORBEAM TO FRAME AFT ATTACH LINK IS CRACKED AT FRAME 12A, RBL 79". REMOVED AND REPLACED THE FITT ING IAW AS300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 20081001 EA 2008 10 1 QXEA200800557 1 20080502 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 613QX 10045 RFD C4 CHECK LT FS 280 BEAM CORRODED. REMOVED LT FS 280 BEAM IAW CRJ 700 SRM 51-42-06 AND 51-42-13. PERFORM LPI ON LT 280 CROSSBEAM IAW CRJ 700 NDTM 51-20-008 NO DEFECTS NOTED. LOCATED HOLES IN NEW BEAM AND INSTALLED BEAM IAW CRJ 700 SRM 51-40-11, 51-42-07, 51-42-14, 51-42-22, 51-42-21 AND 51-23-02. 2 L 7 2 4F RT A21EA 20081001 NM 2008 10 1 2008UALA05810 1 20080919 A 5270 GUARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1L OUT OF POSITION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 DOOR 1L CAN BE ARMED WITHOUT MOVING ARMING GUARD. REPOSITIONED THE GUARD TO PREVENT ARMING WITHOUT MOVING GUARD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081001 2008 10 1 2008UALA05812 4 20080919 A 2565 GAUGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LIFE RAFT LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 AFT CABIN LIFE RAFT COMPT, 1 LIFE RAFT FAILED PRESSURE CHECK. LEAK FOUND AT GAUGE. REMOVED AND REPLACED GAUGE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081001 NM 2008 10 1 2008UALA05815 1 20080919 A 3350 COVER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 644UA 25094 EMERGENCY LIGHTS AT SEAT 14B COVERED BY DUCT TAPE REPAIR IN AREA. FOUND COVER IS MISSING. REPLACED EMERGENCY LIGHT TRA CK COVER. LIGHTS OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081001 NM 2008 10 1 2008UALA05818 1 20080920 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26877 EMERGENCY SIGN DR3R FWD INOP. BATTERY FOUND FAULTY. REPLACED BATTERY. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081001 NM 2008 10 1 08FDEA03428 1 20080814 A 5315 601141518 FLOORBEAM DOUG MD10 MD1030F 3024020 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 304FE 46992 LWR FWD CARGO COMPT FLOOR SUPPORT FITTING ATTACHED ON FLOORBEAM UPPER FLANGE HAS CORROSION AROUND FASTENER HOLES AT STA 791, X 4 - 25. FABRICATED NEW FLOOR SUPPORT ON MAE TRAVELER NR T8/754204. REMOVED AND REPLACED SUPPORT IAW SRM 51-31-0 1. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 08FDEA03429 1 20080814 A 5315 70750063 FLOORBEAM DOUG MD10 MD1030F 3024020 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 304FE 46992 LWR FWD CARGO COMPT FLOOR SUPPORT ANGLE ATTACHED ON FLOORBEAM UPPER FLANGE HAS CORROSION AROUND FASTENER HOLE AT STA 1 059, X 41-55. FABRICATED NEW FLOOR SUPPORT ON MAE TRAVELER T8/754037. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-31 -01. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 08FDEA03430 1 20080814 A 5315 601141518 FLOORBEAM DOUG MD10 MD1030F 3024020 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 304FE 46992 LWR FWD CARGO COMPT FLOOR SUPPORT FITTING ATTACHED ON FLOORBEAM UPPER FLANGE HAS CORROSION AROUND FASTENER HOLES AT STA 735, X4 - 25. FABRICATED NEW SUPPORT ON MAE TRAVELER T8/754216. REMOVED AND REPLACED SUPPORT IAW SRM 51-31-01. MAJOR REPAIR. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 DL757081235 1 20080926 A 5330 143N34713 SKIN BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 DURING HMV AT SAA, CORROSION WAS FOUND ON THE BELLY SKIN UNDER THE RADIO ALTIMETER ANTENNA. THE CORROSION WAS REMOVED A ND A REPAIR WAS INSTALLED PER BOEING INSTRUCTIONS. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 SWAA085105 1 20080917 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 500A, BETWEEN STR 15R AND STR 16R. REPAIRED SHEAR TIE PER S RM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085104 1 20080917 A 5311 6546554 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 847, 27L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 2008UALA05937 1 20080930 A 2560 ATTACH FITTING AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EVAC SLIDE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 804UA 759 RIGHT FORWARD ENTRY DOOR SLIDE LOWER AFT ATTACH FITTING TO DOOR CRACKED. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081009 NM 2008 10 9 2008UALA05941 1 20080930 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 THREE EACH CROSS AISLE LIGHTS INOP. FOUND BROKEN AND CUT WIRES ON LIGHT BARS AT FWD VCC CABINET AREA. REPLACED LIGHT BA RS , OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081009 NM 2008 10 9 2008UALA05949 1 20080930 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY EXIT LIGHT INOP AT DOOR 2 RIGHT BUSTLE LIGHT. REPLACED LIGHT ASSY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081009 NM 2008 10 9 SWAA085313 1 20081001 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED 16Y CHECK, FOUND BELLY SKIN CRACKED AT BS 390, RBL 1.5 TO RBL 3 AFT. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 SWAA085329 1 20081001 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 500D, STR 13L. REPAIRED SHEAR TIE PER PAE EA. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085344 1 20081001 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 20Y CHECK, FOUND FRAME CORRODED AT BS 500C, STR 28L AND STR 28R. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 CALA0800935 1 20080929 A 5320 69778262 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 FORWARD CARGO INTERCOSTAL DAMAGED BETWEEN STATIONS 380-400 AT S-22R. REPAIRED FORWARD CARGO INTERCOSTAL DAMAGED BETWEEN STATIONS 380-400 AT S-22R PER B737-500 SRM 51-70-11. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 CALA0800937 1 20081001 A 5230 6547952 SKIN BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 C-2 DOOR EXTERIOR SKIN CRACKED AT HANDLE CUTOUT AFT UPPER CORNER. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBL ER AND FILLER PER SRM 52-00-01 FIG 201. 2 L 7 2 4F RT A16WE 20081010 EU 2008 10 10 HXS2008F00001 1 20080929 A 2720 360A27117000 BELLCRANK SNIAS 350 AS350B3 8680954 EU TMECA ARRIEL ARRIEL1D1 60053 NE RUDDER PEDALS CRACKED E HXSA O OTHER O OTHER NR NOT REPORTED 1 AL 05 403AE 3281 ON THE BOTTOM SIDE OF THE FOOT PEDAL CONTROLS, ON BOTH THE RT AND LT SIDES, THERE IS A BRACKET THAT IS PART OF THE FOOT PEDAL BELLCRANK PN 350A27-1170-00, TO GO OUT OF ALIGNMENT AND CONTACT THE SURROUNDING SUPPORT STRUCTURE THUS CAUSING A . 2500 INCH GROOVE INTO THE BELLCRANK. REMOVED BRACKETS AND REPLACED WITH SERVICEABLE BRACKETS AND ALSO REMOVED AND REPLAC ED THE BAD BELLCRANK WITH A SERVICEABLE BELLCRANK AND RETURNED AC TO SERVICE. (K) 1 G 7 1 3U 3 U H9EU E19EU 20081010 WP 2008 10 10 IXX2008F00090 1 20080828 A 2910 HYDRAULIC SYSTEM DOUG DC8 DC871F 302199D WP FAILED A IXXA O OTHER J WARNING INDICATION DE DESCENT 1 SW 11 825BX 45978 AT TOP OF DECENT, THE ACFT LOST HYDRAULIC FLUID DOWN TO THE STAND PIPE. OPEN. (K) 2 L 7 4 4F RT 4A25 20081010 EU 2008 10 10 HXS2008F00008 1 20080929 A 6720 350A21136324 BRACKET SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE UNDER FWD FLOOR CRACKED E HXSA O OTHER O OTHER NR NOT REPORTED 1 AL 05 145TH 9060 9862 ON THE BOTTOM SIDE OF THE FOOT PEDAL CONTROLS, ON THE RT PILOT SIDE, THE BRACKET THAT IS PART OF THE BELLCRANK ASSY, BRA CKET PN 350A21-13636-24, HAS A CRACK IN IT. REMOVED BRACKET AND REPLACED WITH A SERVICEABLE BRACKET AND RETURNED AC TO S ERVICE. THIS AC HAS BEEN PREVIOUSLY CONVERTED TO LT PILOT IN CHARGE IAW MFG MODIFICATION. THIS BRACKET IS WHAT HOLDS THE CENTERING ROD OR THE FOOT PEDAL BELLCRANK IN THE FOOT PEDAL FLIGHT CONTROLS. (K) 1 G 7 1 3U 3 U H9EU E19EU 20081010 EA 2008 10 10 FDK2008F00009 1 20080625 A 3250 STEERING SYS CNDAIR CL600 CL6002D24 1390016 EA NLG MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 601LR 15145 ABORTED TAKEOFF DUE TO NOSE WHEEL STEERING ISSUES. THE ACFT PULLED TO THE RT ON TAKEOFF ROLL OUT. MX RESECURED. (K) 2 L 7 2 4F RT A21EA 20081010 NM 2008 10 10 SWAA085345 1 20081001 A 3350 101114 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 239WN 34714 FOUND L1 EMERGENCY EXIT DOOR LIGHT COVER MISSING. REPLACED LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085346 1 20080928 A 5322 6516323 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 344, RBL 17. REMOVED AND REPLACED TIE PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 AALA200802257 1 20080901 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 197AN 32391 DFW EMERGENCY LIGHT AT LT NR 1 DOOR INOPERATIVE. REPLACED EMERGENCY LAMP FOR EMERGENCY LIGHT AT LT NR 1 DOOR. SYSTEM G ROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 SWAA085103 1 20080917 A 5754 65C26602 SLAT BOEING 737 737301 1384611 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 L/E SLAT DELAMINATED AT INBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085098 1 20080917 A 5311 6546593 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085097 1 20080917 A 5311 6546538 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085096 1 20080917 A 5330 6545800 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE SKIN CRACK AT FWD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081001 EU 2008 10 1 UPS08153338 1 20080917 A 5330 SKIN AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 122UP 0807 INSPECTION TYPE:N/A FUSELAGE DENT FWD OF LOWER AFT CARGO DOOR OUT OF LIMITS. ENGINEERING EVALUATING. INSPECTED AREAS J UST FWD OF FRAME 58, BETWEEN STR 33 AND STR 29. CHECKED MATERIAL REMAINING WITH ULTRA SOUND AND FOUND TO BE WITHIN REWO RK LIMITS PER A300 SRM 53-10-13 DIA 101 PERM ALLOWABLE REWORK. 2 L 7 2 4F RT A35EU 20081001 NM 2008 10 1 ZZDA2008158 1 20080916 A 5220 PANEL BOEING 737 73776N 13844CH NM EMERGENCY EXIT JAMMED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 169AT 32744 LEFT OVERWING EMERGENCY EXIT DOOR KICK PANEL JAMMED. RE-SECURED PANEL IAW AMM 52-22-51. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085122 1 20080918 A 5322 6546569 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 927, STR 20R TO 21R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 2008UALA03913 1 20080719 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 211 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 350UA 24301 DURING SKIN REPLACEMENT HAD SURPLUS OF FASTENER HOLES AT RT AND LT STA 211.8 - 3.5 INCHES ABOVE LOWER SKIN LAP. *S/D* MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 20081002 SO 2008 10 2 C2XA08RI141 1 20080926 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13975 145163 RIC - MX - DURING ROUTINE MAINTENANCE RIC MX FOUND FORWARD EMERGENCY LIGHT STRIP NOT ILLUMINATING. MX RECONNECTED LOOSE WIRING AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20080930 NM 2008 9 30 2008UALA05414 1 20080822 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 660 S25L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 FWD PIT AT STA 660 STR 25L, FRAME DENTED. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGE & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20080930 NM 2008 9 30 2008UALA04244 1 20080811 A 5320 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 803UA 748 R2 DOOR SILL HAS HEAVY CORROSION IN NUMEROUS LOCATIONS. MAJOR REPAIR ACCOMPLISHED: REPLACED SILL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 EU 2008 9 30 2008UALA05445 1 20080824 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 451UA 865 FLOORBEAM 210 IS CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM 210. TRANSFERRED ATTACH BRACKETS AN D STARTED ATTACHING TO BEAM 175. BEAMS 210 AND 175 ARE TOGETHER AND NEED THE FWD END DRILLED TO BRACKETS IN A/C. PICKE D UP REMAINING HOLES AND INSTALLED FWD SPLICE AND CROSS BEAM ATTACH BOLTS. WIRE BUNDLE NOT ATTACHED. SECURED WIRE BUND LE TO FLOORBEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081001 WP 2008 10 1 08FDEA04120 1 20080929 A 5730 ARC0258503 PANEL DOUG MD10 MD1010F 3022112 WP LT WING DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING LOWER T/E PANEL NR 541 HB DELAMINATED AROUND EDGE. REPAIRED BY REMOVING; FABRICATING & BONDING A NEW OUTER SK IN, INNER DOUBLER, HONEYCOMB CORE AND INNER SKIN IAW E.A. 8-5720-123638 AND TPS 1001; REV " E ". PRIMED; SEALED & PAIN TED PANEL IAW E.A. 8-5720-123638 & SRM 51-21-02. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 SWAA085198 1 20080924 A 5512 6573782 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND LT HORIZ STAB LOWER SKIN CRACKED AT BS 134.00. REMOVED AND REPLACED LT HORIZ STAB PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 08FDEA04123 1 20080929 A 5740 6521795409 ATTACH FITTING BOEING 727 727227 1384078 NM NR 4 FLAP TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 "PANEL RACK" INBD T/E NR 4 FLAP TRACK AFT FAIRING HAS CRACK IN MOUNT BRACKET AT FWD OUTBOARD END. FABRICATED NEW MOUNT BRACKET AND INSTALLED REF BOEING DOCUMENT 65-21795, SRM51-30-2 PG1-8 GMM 7-0-1001, SRM 51-10-2 PG 7, MM 51-20-151-7 PG 1 . THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081001 NM 2008 10 1 UPS08553399 1 20080926 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 424UP 25369 INSPECTION TYPE:C2 MCB LBL 0 - LBL 25, BS 1200, FLOORBEAM UPPER SURFACE HAS CORROSION AT NUMEROUS FASTENER HOLES. BEGAN DAMAGE REMOVAL PER ATS ER 08-3012, FOUND ADDITIONAL AREAS OF CORROSION AND TRANSFERRED WORK TO CUST CARD NR 779379. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 UPS08553396 1 20080915 A 5420 BRACE BOEING 757 75724APF 1384969 NM RT PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 452UP 25473 INSPECTION TYPE:MOD RT UNDERWING FAIRING STRUCTURE, RT FWD SIDE SUPPORT BRACE IS CRACKED AT PPS 185.0. REMOVED AND REPL ACED FWD SIDE SUPPORT BRACE IAW SRM 51-40-02-0G. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 MZZA080003 1 20080926 A 5610 58935734 WINDOW BOEING 737 737824 13844BZ NM COCKPIT BROKEN A CALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 35236 11399 28801 R-4 WINDOW OUTER PANE SHATTERED. REMOVED AND REPLACED R-4 WINDOW PER AMM 56-11-31. WINDOW HEAT OPS CHECKS NORMAL, ROTA BLE PARTS CHANGE WAS INDICATED-TT NR 1231942 S/N OFF 04338, WINDSHIELD, B737 OFF 99-5617-9-9001 4338, ON 99-5617-9-9001 8141. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085223 1 20080924 A 3350 8210248801 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 200WN 32482 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT FLOOR RED LIGHT LENS BROKEN AT OVERWING EXIT. REMOVED AND REPLACED LEN S PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 ASAA0843529 1 20080925 A 2131 7638101 CONTROLLER BOEING 737 7374Q8 138447Q NM CABIN PRESSURE MALFUNCTIONED A ASAA K NONE J WARNING INDICATION CR CRUISE 1 NM 02 765AS 53514 25102 AT CRUISE 350 CABIN ALT HORN SOUNDED. CABIN PRESSURE VERIFIED TO BE BETWEEN 10,000 - 11,000 FT, 2 PSI DIFFERENTIAL. RA N CHECK. LIST NO AUTOFAIL LIGHT. MOVED SWITCH TO STBY AND SET CRUISE ALT OF 7000 FT IN WINDOW. CABIN STARTED DOWN AT 700 FPM. BEGAN DESCENT INTO ARC AND SLOWLY REGAINED THE CABIN ALT. REMOVED & REPLACED CABIN PRESS CONT REF AMM 21 31 2 1, OPS CHECK GOOD REF AMM 21 31 00 702 001. 2 L 7 2 4F RT A16WE 20081001 WP 2008 10 1 UPS08853382 1 20080920 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA A UNSCHED LANDING O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE:N/A DOUBLER AT FUSELAGE STATION 902, LT SIDE OF FUSELAGE REQUIRES REPLACEMENT. REMOVED EXISTING DOUBLER AND SHIM PER SRM 51-1-00, C/W EO DC8-5330-3 9 UP TO STEP 6. INSTALLED 28 1/4" HI-LOKS IN REPAIR DOUBLER PER PRELIMINAR Y EO DC8 5330-30619-A. COMPLETED INSTALLATION OF REPAIR DOUBLER PER EO DC8 5330-30619-A. DEFERRED TIME LIMITED REPAIR, REF D-385258. 2 L 7 4 4F RT 4A25 20081001 NM 2008 10 1 UPS08553381 1 20080907 A 5412 311N32712 BULKHEAD BOEING 757 75724APF 1384969 NM NR 1 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 434UP 25465 INSPECTION TYPE:C, NR 1 PYLON MIDSPAR BULKHEAD LOWER O/B CORNER CHAFED. ORG MAT THICKNESS OF OUTER EDGE OF BULKHEAD IS .210 DEEPEST DAMAGED AREA IS .034. BLENDED NR 1 PYLON AFT FITTING LOWER O/B CORNER PER STEP 1 EA 757-5453-27-A1811. ND T STEP 2 OF EA757-5453-27-A1811. ACCOMPLISHED ON MAE TRAVELER T8/760081 ECA114086. 2 L 7 2 4F RT A2NM 20081001 NM 2008 10 1 UPS08553380 1 20080907 A 5412 311N32712 BULKHEAD BOEING 757 75724APF 1384969 NM NR 1 PYLON CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 434UP 25465 INSPECTION TYPE:SV NR 1 PYLON MIDSPAR BULKHEAD LOWER I/B CORNER CHAFED. ORG MAT THICKNESS OF OUTER EDGE OF BULKHEAD IS .210 DEEPEST DAMAGED AREA IS .030. BLENDED NR 1 PYLON AFT FITTING LOWER I/B CORNER I/B CORNER PER STEP 1 OF EA 757-5453 -27-A1811, ON MAE TRAVELER T8/760081. 3.NDT-STEP 2 OF EA757-5453-27-A1811, ACCOMPLISHED ON MAE TRAVELER T8/760081 ECA 11 4087. 2 L 7 2 4F RT A2NM 20081001 2008 10 1 ASAA0853527 4 20080923 A 2210 8221604101 AUTOLAND SYS BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA K NONE O OTHER LD LANDING 1 NM 02 577AS 6047 35186 PERFORMED AUTOLAND AS REQUESTED. ALL OK UNTIL LAST 40FT AC STARTED GOING LEFT OF CENTERLINE AND TOUCHED DOWN APPROX HAL F WAY BETWEEN LEFT RUNWAY EDGE AND CENTERLINE DID NOT GET APPROACH WARN DFCS FFR SHOWS NO FAULTS. PERFORMED FULL LAND V ERIFY TEST REF MM 22 11 00 PG 94, TEST PASSED. HGS SYS TEST REF MM 34 36 00 PASSED AC REMAINS CAT IIIA AUTOLAND AND HGS QUAL. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 2008UALA05778 1 20080917 A 3350 767 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 535UA 25130 NR 2 LT MAIN ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081001 NM 2008 10 1 SWAA085183 1 20080922 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT STA 908, STR 4R. REMOVED AND REPLACED SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085182 1 20080919 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 FOUND EMERGENCY EXIT BULLNOSE LIGHT LENS MISSING AT ROW 10 ABC. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085181 1 20080921 A 3350 65C27095 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED MV1 CHECK, FOUND R1 EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085180 1 20080924 A 3350 6573709 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED MV1 CHECK, FOUND R2 EXTERIOR EMERGENCY EXIT LIGHT INOP. REPAIRED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085177 1 20080913 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND STR CLIP CRACKED AT STA 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 2008UALA05768 1 20080917 A 3397 7945243 CONNECTOR BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 SEAT ROW 55 HJK - 60 HJK EMERGENCY LIGHTS INOP. FOUND UNDER SEAT CONNECTOR DISCONNECTED. RECONNECTED. OP CHECKS NORMA L. 2 L 7 4 4F 4 F RT A20WE E24NE 20081001 NM 2008 10 1 SWAA085176 1 20080918 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 416WN 32453 EMERGENCY EXIT FLOOR LIGHTING LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 AALA200802223 1 20080828 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 179AA 32397 JFK EMERGENCY LIGHT AT RT HAND AFT LAVATORY DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RT HAND AFT LAVATORY DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 AALA200802242 1 20080830 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 JFK EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 22H TO 27J INOPERATIVE. REPLACED BATTERY PACK AT RT NR 3 DOOR FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 22H TO 27J. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081010 NM 2008 10 10 SWAA085354 1 20081002 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND AFT FRAME CRACKED AT BS 767, STR 26R TO STR 27R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085362 1 20081002 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND SKIN CRACKED AT BS 360, STR 13R TO STR 28R. REPLACED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085363 1 20081001 A 3350 300432 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 711HK 27845 DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT 3 DEF. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 SWAA085376 1 20081002 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED C3 CHECK, FOUND SKIN CRACKED AT BS 500C, STR 10R. REMOVED AND REPLACED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081010 EA 2008 10 10 QXEA200800550 1 20080529 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 601QX 10009 C4-CHECK - FWD AVIONICS AND FLIGHT CONTROL COMPARTMENT HAS CORROSION ON FRAME AROUND NUTPLATE HOLES AT CRAWL WAY PANEL F WD IB AND OB ATTACHING POINTS ST FS 235.00. DRILLED OUT FWD LT AND RT NUTPLATES. BLENDED OUT CORROSION FROM UPPER SURFA CE AROUND LT AND RT NUTPLATES. BLENDED OUT CORROSION ON EDGE AFT OF LT AND RT NUTPLATE HOLES. REMOVED APPROX .030 INCH M ATERIAL FROM LT EDGE APPROX .050 INCH FROM RT EDGE. WORK DONE IAW SRM. (K) 2 L 7 2 4F RT A21EA 20081010 EU 2008 10 10 UPS08153423 1 20080924 A 5321 B5327077600100 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 252WJ HAS TEMPORARY REPAIR RT SIDE CENTER EDGE OF PANEL. REPAIRED MAIN CABIN FLOOR PANEL 252WJ REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081010 EU 2008 10 10 UPS08153437 1 20080929 A 5321 B5327083600000 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU CABIN PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR MAIN CARGO FLOORBOARD 242PM HAS A PUNCTURE. REPAIRED MAIN CARGO FLOOR PANEL REF A300-600 SRM 53-10 -20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081010 EU 2008 10 10 UPS08153438 1 20080929 A 5321 B5327079400200 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR MAIN CABIN FLOORBOARD 241YK HAS TEMP REPAIR. PERMANENTLY REPAIRED MAIN CABIN FLOOR PANEL REF A300- 600 SRM 53-10- 20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081010 EA 2008 10 10 A6WA200840567 1 20080730 A 5320 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 529 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 445AW 7804 RT WHEEL HYDRAULIC SUPPORT BRACKET AT FS 529.98, BTW RBL 18-27 IS CRACKED. CRACK LENGTH IS .250 INCH. NEW RT WHEEL WEL L HYDRAULIC SUPPORT BRACKET INSTALLED AT FS 529.98 BTW RBL 18-27 IAW CRJ 200 SRM 51-42-06. (K) 2 L 7 2 4F RT A21EA 20081010 EA 2008 10 10 A6WA200840568 1 20080806 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 574 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 445AW 7804 CRACK FOUND ON CARGO BAY FLOOR SILL FS 574, LBL 45. ON CARGO BAY FLOOR SILL FS 574, LBL45 CRACK IS REPAIRED IAW REO 601 R53-61-1741. (K) 2 L 7 2 4F RT A21EA 20081010 EA 2008 10 10 A6WA200840569 1 20080806 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 589 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 445AW 7804 CRACK FOUND ON LOWER SILL OF CARGO DOOR FS 589, LBL 45. ON LOWER SILL OF CARGO DOOR FS 589 LBL45, CRACK IS REPAIRED IAW REO 601R-53-61-433. (K) 2 L 7 2 4F RT A21EA 20081010 EA 2008 10 10 A6WA200840571 1 20080808 A 5320 SUPPORT BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 531 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 445AW 7804 LT WHEEL WELL HYDRAULIC SUPPORT BRACKET AT FS 531.75, BTW LBL 18-27 IS CRACKED LENGTH OF CRACK IS 0.350". LT WHEEL WELL HYDRAULIC SUPPORT BRACKET AT FS 531.75 BTW LBL 18-27, IS REPLACED IAW CRJ 200 SRM 51-42-06. (K) 2 L 7 2 4F RT A21EA 20081010 EA 2008 10 10 A6WA200840576 1 20080808 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 445AW 7804 FS 280, RBL 9.00, WL 71.00 IB CLIP CRACKED. FS 280, RBL 9, WL 71.00 IB CLIP REPLACED IAW CRJ 200, SRM 51-42-06 AND 51-4 2-20. (K) 2 L 7 2 4F RT A21EA 20081010 EA 2008 10 10 A6WA200840577 1 20080808 A 5320 CROSSBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 445AW 7804 FS 280.00, RBL 9.00, WL 70.00, CROSS BEAM IS CRACKED IN THE LOWER RADIUS. CROSSBEAM AT FS 280.00, RBL 9.0, WL 70.00. R EPAIRED IAW REO 601R-43-11-171, REV D. (K) 2 L 7 2 4F RT A21EA 20081001 NM 2008 10 1 SWAA085175 1 20080922 A 3350 417A54701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 264LV 32521 L1 DOOR EXIT LIGHT COVER MISSING. REPLACED COVER PER SWA EA. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 2008UALA05773 1 20080918 A 3350 3071BPEGPL LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 771UA 26932 EMERGENCY LIGHT INOP 2E. RESECURED LOOSE CONNECTOR. RELAMPED EEL STRIP AT 2E BATH LIGHTS. OPS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081001 NM 2008 10 1 2008UALA05783 1 20080918 A 4920 ENGINE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE APU OIL CONSUMPTION A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 675UA 29243 APU OIL CONSUMPTION ABOVE LIMIT. 2 L 7 2 4F 4 F RT A1NM E24NE 20081001 EU 2008 10 1 08FDEA03422 1 20080814 A 5320 A53973261228 FITTING AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 DURING P TO F FOUND FRAME COUPLING WITH TO LESS RIVET PITCH. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20081001 EU 2008 10 1 08FDEA03423 1 20080814 A 5320 A53974259200 FLOOR SUPPORT AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORRODED FLOOR SUPPORT AT C 63-64, Y-800. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20081001 SO 2008 10 1 SWIA200820028 1 20080722 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 564SW 120339 RT FLOOR PROP CRACKED AT FRAME 13. C-CHECK, INSTALLED FILLER AND DOUBLER. 2 L 7 2 4T RT A31SO 20081001 SO 2008 10 1 SWIA200820030 1 20080616 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 296SW 120325 RT FLOORBOARD PROP ANGLE IS CRACKED UNDER JUMPSEAT FLOORBOARD. C-CHECK, REPLACED RT FLOORBOARD PROP ANGLE. 2 L 7 2 4T RT A31SO 20081001 SO 2008 10 1 SWIA200820031 1 20080616 A 5411 FRAME EMB 120 EMB120ER 3260203 SO RT NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 296SW 120325 RIGHT NACELLE FRAME NR 1 CRACKED AT TENSION MOUNT AREAS IB AND OB. C-CHECK, REPLACED NACELLE FRAME NR 1. 2 L 7 2 4T RT A31SO 20081010 NM 2008 10 10 AALA200802249 1 20080830 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 766AN 32880 DFW EMERGENCY LIGHT AT SEAT 35C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 35C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081010 NM 2008 10 10 AALA200802241 1 20080830 A 3350 PBS73 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 353AA 24034 JFK EMERGENCY LIGHTS AT LT AND RT HAND OVERWING ESCAPE DOOR INOPERATIVE. REPLACED BATTERY PACK AT RT NR 3 DOOR FOR EMER GENCY LIGHTS AT LT AND RT HAND OVERWING ESCAPE DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081010 NM 2008 10 10 2008UALA05764 1 20080917 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 528UA 25018 EEL FLOOR STRIP INOP AT FRONT OF COACH. EEL DAMAGE. REINSTALLED LIGHT STRIP. CHECKS OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081010 NM 2008 10 10 2008UALA05943 1 20080930 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY EXIT LIGHT INOP UPPER DECK CEILING AT ROW 17. REPLACED LAMP, OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081010 NM 2008 10 10 2008UALA05944 1 20080930 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY EXIT SIGN INOP AT TOP OF DOOR 2 RIGHT. REPLACED BATTERY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081010 NM 2008 10 10 2008UALA05945 1 20080930 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY EXIT LIGHTS INOP AT DOOR 2 RIGHT FWD AND AFT SILL LIGHTS. REPLACED BATTERY. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081010 NM 2008 10 10 2008UALA05953 1 20081001 A 3350 FU305 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BATTERY FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 121UA 29167 EMERGENCY LIGHTS NOT ON FROM DOOR 2 LT BATTERY. REPLACED FUSES, OP CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081010 SO 2008 10 10 SIM2008F00024 1 20080908 A 2841 4800101 SWITCH EMB 135 EMB135KL 3260302 SO FUEL QTY INDI FAILED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 809AE 145521 AT CRUISE CREW REPORTED TANK 1 FUEL QUANTITY WENT FROM DASHES TO 0 IN FLIGHT. CREW DECLARED FUEL EMERGENCY TO GET PRIORI TY HANDLING. ACFT REMOVED FROM SERVICE. PERFORMED TROUBLESHOOTING IN REF TO FIM 27-43-0-810-802-A REMOVED AND REPLACED B ACK UP SYSTEM CUT OUT SWITCH. OPS CHECK GOOD IAW AMM 27-40-00. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. (K) 2 L 7 2 4F RT T00011AT 20081010 SO 2008 10 10 SIM2008F00025 1 20080905 A 3320 BR900022 BALLAST EMB 145 EMB145LR 3260212 SO CABIN LIGHTS ODOR A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 639AE 145182 ON FLIGHT 3448 CREW REPORTED ODD ODOR COMING FROM LAST 2 ROWS OF CABIN. ACFT REMOVED FROM SERVICE. INSPECTED AND FOUND BALLAST AT 16A CEILING BURNED. REMOVED AND REPLACED BALLAST ABOVE ROW 16A IAW EMB 145 AMM 33-21-05 OPERATIONAL CHECKED G OOD. NO FURTHER ODOR NOTED. (K) 2 L 7 2 4T RT T00011AT 20081010 SO 2008 10 10 SIM2008F00026 1 20080905 A 2150 ACM EMB 145 EMB145LR 3260212 SO NR 2 ODOR A SIMA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 669MB 145788 ON FLIGHT 4125 CREW REPORTED DURING TAKEOFF SMOKE ODOR IN COCKPIT. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 2 AIR CYCLE MACHINE IAW AMM 21-51-03. ACFT RETURNED TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081010 EA 2008 10 10 SIMA200825503 1 20080907 A 5210 PLUNGER CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR HANDLE DISENGAGED B SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 517AE 10124 ON FLIGHT 3118, CREW REPORTED DURING CLIMB OUT AT APPROX 1500 FT CREW HEARD NOISE IN COCKPIT ALONG WITH NR 1 FA. MAIN P AX DOOR HANDLE MOVED ABOUT 2 INCHES AND RED INDICATION NOTED ON ALIGNMENT MARKS. PRESSURIZATION HELD STEADY THROUGH OUT FLIGHT. CREW ELECTED TO RETURN TO DEPARTURE. ACFT LANDED SAFELY AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. ACFT RE MOVED FROM SERVICE. FOUND PLUNGER NOT FULLY ENGAGED WITH PAX DOOR HANDLE IN THE STOWED POSITION. ADJUSTED PUSH ROD ASSY IAW AMM 52-11-02. PERFORMED OPERATIONAL TEST OF THE PAX DOOR IAW AMM 52-11-00. OPERATIONAL CHECK GOOD. ACFT RETURNED T O SERVICE. (K) 2 L 7 2 4F RT A21EA 20081010 WP 2008 10 10 WRL2008F00008 1 20080906 A 5320 INTERCOSTAL DOUG DC10 DC1030F 3023504 WP BS 1606 L31R CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 303WL 46917 DURING INSP, FOUND CORROSION IN THE RT MLG WHEEL WELL STA 1606 AT LONGERON 31R, INTERCOSTAL SKIN ATTACH, REF DELTA NR 40 . REMOVED CORROSION ON SKIN AND FRAME AT LONGERON 31R BETWEEN STA 1505-1521, WITHIN LIMITS IAW SRM 53-00-01. TREAT AND PAINTED SKIN AND FRAME IAW SRM 53-00-01. FABRICATED NEW INTERCOSTAL. ON DELTA SHOP ORDER AP5798, INSTALLED INTERCOSTAL, IAW DWG AEA0026. (K) 2 L 7 3 4F RT A22WE 20081010 SO 2008 10 10 C2X2008F00050 1 20080906 A 3230 SEQUENCE VALVE EMB 145 EMB145LR 3260212 SO MLG MALFUNCTIONED A C2XA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 27 13566 145622 FLIGHT 2825 - FLIGHT CREW REPORTED THAT DURING CLIMBING OUT, THEY HEARD A SOUND LIKE GEAR WAS STILL DOWN WITH GEAR LEVE R UP AND GEAR INDICATION SHOWING UP POSITION. CREW RECYCLED GEAR TWICE AT AIR SPEED UNDER 200KNT, NOISE ONLY SLIGHTLY C HANGED WHEN GEAR WENT UP. FLIGHT CREW AIR RETURNED TO DEPARTURE UNEVENTFULLY. MX REMOVED AND REPLACED NOSE LANDING GEAR SEQUENCE VALVE , REMOVED AND REPLACED NOSE LANDING GEAR RT DOOR, AND THIRD UPPER LOCK BOX PROXIMITY SW. MX PERFORMED LE AK AND OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081010 SO 2008 10 10 RAIA00809007 1 20080907 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 850HK 145003 MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. MAINT LUBED THE DOOR ROLLERS AND PERFORMED SEVERAL OPS CHECKS OF THE DOOR OPERATING MECHANISMS WITH O DEFECTS NOTED. (K) 2 L 7 2 4T RT T00011AT 20081010 SO 2008 10 10 RAIA00809012 1 20080911 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN/GALLEY LOOSE A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 832HK 145771 EMERGENCY LIGHT STRIP AT GALLEY NOT SECURE. MAINT RESECURED THE LOOSE EMERGENCY LIGHT STRIP. OPS CHECKED GOOD. (K) 2 L 7 2 4T RT T00011AT 20081010 SO 2008 10 10 C2XA08SH120 1 20080910 A 5310 14525480603 DOOR FRAME EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11184 14500917 DURING C-CHECK, BAGGAGE DOOR CUTOUT LOWER BEAM CORRODED IN VARIOUS AREAS MARKED. MX REMOVED AND REPLACED BAGGAGE DOOR LO WER FLOORBEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED TO RETURN FOR SERVICE. (K) 2 L 7 2 4F RT 20081010 SO 2008 10 10 C2XA08SH118 1 20080910 A 5240 14590016015 HINGE EMB 145 EMB145XR 3260214 SO SERVICE DOOR DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 21154 145772 DURING C-CHECK, SERVICE DOOR UPPER HINGE AT FUSELAGE HAS MIGRATED HAT BUSHING. MX REMOVED AND REPLACED SERVICE DOOR UPPE R HINGE AT FUSELAGE HAT BUSHING IAW EC5240-01036. THE ACFT WAS APPROVED TO RETURN FOR SERVICE. (K) 2 L 7 2 4F RT 20081010 NM 2008 10 10 2008UALA05972 1 20081003 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA O OTHER L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY LIGHT FWD GALLEY CEILING INOP. LIGHT FOUND INOPERATIVE. REPLACED LAMP, CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081010 NM 2008 10 10 2008UALA05973 1 20081003 A 3350 FU305 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE POWER SUPPLY BLOWN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 LEFT BOTTOM 2 OVERWING EMERGENCY LIGHT INOP. LIGHT FOUND INOP. REPLACED FUSE ON POWER SUPPLY. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081010 NM 2008 10 10 2008UALA05974 1 20081003 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 SEAT 5A AFT EMERGENCY LIGHT INOP. LAMP IS UNSERVICEABLE. REPLACED LAMP. ALL CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20081014 CE 2008 10 14 J7SA452027081003 1 20081003 A 3222 MS288892 SCHRADER VALVE LEAR 45 45LEAR 5170805 CE NLG LEAKING E J7SA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 05 610F 1972 452027 NOSE WHEEL STEERING FAIL CAS DURING GEAR RETRACTION. HASH MARKS ON ALL THREE GEAR INDICATIONS AFTER RETRACTION. LOWERE D GEAR AGAIN AND RECEIVED GREEN LIGHTS ON ALL THREE. COULD NOT CLEAR NWS FAIL CAS. NOSE GEAR WAS TURNED TO THE LEFT. CREW DECLARED AN EMERGENCY AND PERFORMED AN AIR RETURN TO KBED WITH UNEVENTFUL LANDING AND TAXI. MX FOUND NLG STRUT WIT H NO PRESSURE & SCHRADER VALVE LEAKING. REMOVED AND REPLACED NLG STRUT SCHRADER VALVE AND SERVICED STRUT. PERFORMED EX T & RETRACTION F/T & OPS TEST OF NWS. ALL TESTS NORMAL. VISUALLY CHECKED NLG ASSY WITH NO DEFECTS NOTED. 2 L 7 2 4F RT T00008WI 20081010 NM 2008 10 10 F3L2008F00005 1 20080906 A 5315 D5347217220400 FLOOR SUPPORT AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 929FR 26 2240 REF: NON ROUTINE C050602. DURING C3 C-CHECK, INSPECTION NOTED SEVERAL NUT PLATE HOLES ON FRAME Y-1292 BETWEEN FRAME 66 A ND FRAME 68, HAD CORROSION. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IAW WITH THE REQUIREMENTS OF A319 SRM 51-42-11. U PON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (K) 2 L 7 2 4F RT A28NM 20081010 NM 2008 10 10 F3LA200800600 1 20080906 A 5315 D53472172202 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 929FR 26 2240 REF NON ROUTINE C050600. DURING C3 C-CHECK, INSPECTION NOTED FWD NUT PLATE HOLE ON FRAME Y-1292 AT FRAME 66, HAD CORROSI ON. MAINT REMOVED CORROSION FROM HOLE, FABRICATED REPAIR BUSHING AND INSTALLED IAW WITH THE REQUIREMENTS OF ENGINEERING AUTHORIZATION NR A9-53R-30598. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (K) 2 L 7 2 4F RT A28NM 20081010 EA 2008 10 10 A6WA200840578 1 20080808 A 5320 CROSSBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 445AW 7804 FS 280.00, LBL 9.0, WL 70.00 CROSS BEAM CRACKED IN THE LOWER RADIUS. FS 280, LBL9, WL 70.00. CROSSBEAM CUTOUT IAW REO 601R-53-11-171, REV D. (K) 2 L 7 2 4F RT A21EA 20081010 WP 2008 10 10 WXO2008F00000 1 20080809 A 3350 AD4002 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS FAILED E WXOA K NONE L NO TEST IN INSP/MAINT 1 WP 07 862GA 49556 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINT REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTE M WOULD NOT TEST. MAINT REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. (K) 2 L 7 2 4F RT A6WE 20081010 WP 2008 10 10 WXO2008F00001 1 20080802 A 3350 AD4002 BATTERY PACK DOUG DC9 DC987 3022087 WP EMERGENCY LIGHTS FAILED E WXOA K NONE L NO TEST IN INSP/MAINT 1 WP 07 952MA 49673 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINT REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTE M WOULD NOT TEST. MAINT PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SAT ISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (K) 2 L 7 2 4F RT A6WE 20081010 WP 2008 10 10 WXO2008F00006 1 20080821 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS FAILED E WXOA K NONE L NO TEST IN INSP/MAINT 1 WP 07 879GA 53486 DURING A ROUTINE OVERNIGHT SERVICE CHECK, INSP REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINT REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPL ISHED IAW AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (K) 2 L 7 2 4F RT A6WE 20081010 WP 2008 10 10 WXO2008F00007 1 20080821 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS FAILED E WXOA K NONE L NO TEST IN INSP/MAINT 1 WP 07 894GA 49660 DURING A ROUTINE OVERNIGHT SERVICE CHECK, INSP REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINT REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMP LISHED IAW AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. (K) 2 L 7 2 4F A6WE 20081010 NM 2008 10 10 WXO2008F00008 1 20080828 A 3350 AD4002 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS FAILED E WXOA K NONE L NO TEST IN INSP/MAINT 1 WP 07 892GA 49826 DURING A ROUTINE OVERNIGHT SERVICE CHECK, INSP REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAIN REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL C HECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (K) 2 L 7 2 4F RT 20081010 NM 2008 10 10 USAA920081681 1 20080914 A 5512 SKIN BOEING 737 7374B7 138449C NM ZONE 300 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 439US 24781 LT HORIZONTAL LOWER SKIN CRACKED ALONG AFT SPAR CAP. ACCOMPLISHED TEMPORARY REPAIR IAW REPAIR NR 55-10-08. REPAIRED LT HORIZONTAL LOWER SKIN CRACKED ALONG AFT SPAR CAP 55 INCHES FROM THE ROOT AREA IAW B737 SRM 55-10-07. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 UPS08653429 1 20080929 A 5720 WEB BOEING 767 76734AF 1385212 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 330UP 27756 INSPECTION TYPE:C RT WING FRONT SPAR AREA LES 680 D-NOSE WEB FOUND CRACK (CRACK LENGTH .5 INCH). D-NOSE WEB REPAIRED AS PER SRM 57-41-13-2R3 FIG 201 REPAIR 3. 2 L 7 2 4F RT A1NM 20081010 CE 2008 10 10 GLB2008F00027 1 20080919 A 5530 STABILIZER BEECH 1900 1900D 1154162 CE DAMAGED A GLBA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 03 122UX UE122 MAJOR REPAIR ACFT N122UX WHILE TAXIING THE ACFT TO THE GATE THE PILOTS STRUCK A JETWAY WITH THE TAIL OF THE ACFT DAMAGIN G THE VERTICAL AND HORIZONTAL STABILIZERS. THE VERTICAL STABILIZER WAS DAMAGED AND TWISTED TO THE LT FROM VERTICAL STAB ILIZER POSITION CSS 39.289 TO CSS 69.184. THE HORIZONTAL STABILIZER WAS DAMAGED AT THE RT HAND OTBD EDGE AT HSS 110.63. 2 L 7 2 4T RT A24CE 20081010 CE 2008 10 10 GUU2008F00054 1 20080927 A 5210 12951405913 CABLE ASSY BEECH 1900 1900D 1154162 CE PAX DOOR DEFECTIVE A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 17 87552 UE216 FLIGHT 9208 TPA/PNS PILOT DISCREPANCY. PILOT REPORTED UNABLE TO OPEN MAIN CABIN DOOR. C/A REPLACED UPPER AFT AIRSTAIR DOOR CABLE. OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 20081010 EU 2008 10 10 AALA200802255 1 20080831 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 18066 509 MIA EMERGENCY LIGHT ASSEMBLY AT SEAT 31G MISSING. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 31G. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A35EU 20081010 NM 2008 10 10 AALA200802254 1 20080831 A 3040 CONTROLLER BOEING 767 767223 1385123 NM WINDOW HEAT FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 21 320AA 22321 JFK INFLIGHT T4/31AUG. CAPTAINS WINDSHIELD INNER WINDOW PANE CRACKED FOLLOWED BY ELECTRICAL ARCING IN LOWER LT CORNER. CREW INITIATED EMERGENCY DEPRESSURIZATION PROCEDURES. PRESSURIZATION NEVER GOT ABOVE FL100. LANDED JFK WITHOUT INCIDE NT. REPLACED WINDOW HEAT CONTROL UNIT, WINDOW HEAT CONNECTOR AND LT NR 1 WINDOW. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081010 NM 2008 10 10 2008UALA05946 1 20080930 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY EXIT SIGN INOP ABOVE ROW 22 RIGHT. REPLACED BATTERY. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081010 NE 2008 10 10 2008UALA05956 2 20080930 A 7320 7911004108 EEC BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE FAULTED A UALA K NONE R PARTIAL RPM/PWR LOSS DE DESCENT 1 WP 29 643UA 25093 ENG LOW IDLE L DURING DESCENT. REPLACED ELECTRICAL ENGINE CONTROL. REPLACED IDLE SOLENOID RELAY K434, AIR-GRD BAT RELAY K167, AND RELAY K785. CLEANED CONNECTORS ON FCU. OKAY FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081010 NM 2008 10 10 2008UALA05957 1 20081002 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 818UA 882 BEAM 175 CORRODED. BEAM OUT & BRACKETS INSTALLED ON NEW ONE. INSTALLED BEAM AND FASTENERS WITH SEALANT. INSPECTED BE AM 175 INSTALLATION AND FOUND SERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081010 NM 2008 10 10 2008UALA05960 1 20081002 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 818UA 882 BEAM 80 CORRODED. REMOVED FLOORBEAM 80. TRANSFERRING FASTENER HOLES TO NEW BEAM. INSTALLED BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081010 EA 2008 10 10 A6WA200840564 1 20080805 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 445A 7804 INTERCOSTAL CLIP AT FS 484, RBL 27 CRACKED. NEW INTERCOSTAL CLIP INSTALLED AT FS 484, RBL 27. (K) 2 L 7 2 4F RT A21EA 20081010 EA 2008 10 10 A6WA200840565 1 20080805 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 445AW 7804 INTERCOSTAL AT FS 484, RBL 36 CRACKED. INTERCOSTAL AT FS 484, RBL 36 REPAIRED IAW CRJ 200, REO 601R-53-41-059 REV A. (K) 2 L 7 2 4F RT A21EA 20081010 WP 2008 10 10 AALA200802237 1 20080828 A 2134 PRESSURE SWITCH DOUG DC9 DC983 3022083 WP A/C BAY INOPERATIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 593AA 53256 LAX INFLIGHT T1960/28AUG. BOTH AIR CON PACKS WENT TO ZERO FLOW ON CLIMB. ACFT WOULD NOT PRESSURIZE. RETURNED TO LAX A ND LANDED WITHOUT INCIDENT. REPLACED BOTH LT AND RT HAND SINGLE ENGINE SECON SEGMENT CLIMB PRESSURE SWITCHES. SYSTEM G ROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081010 WP 2008 10 10 AALA200802256 1 20080901 A 3520 OXYGEN MASK DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA G A O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SW 21 236AA 49251 DFW INFLIGHT T323/01SEP. DURING DESCENT THROUGH FL110 PRESSURIZATION FLOW LIGHT ILLUMINATED. OXYGEN MASKS WERE DEPLOYE D AND CREW REPORTED ELECTRICAL SMELL. CREW REPORTED UNABLE TO CONTROL CABIN PRESSURE. LANDED DFW WITHOUT INCIDENT. FO UND OXYGEN MASKS AT SEAT ROW 21 DID NOT DEPLOY. REMOVED DEBRIS FOR MOST FORWARD CABIN PRESSURE SAFETY VALVE. CLEANED A ND RESTOWED MASKS AND CHANGED OXYGEN GENERATORS. INSPECTED SEAT ROW 21 PASSENGER SERVICE UNITS WITH NO FAULTS FOUND. S YSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081010 EU 2008 10 10 USAA920081679 1 20080912 A 2560 P2070003001 FLASHLIGHT AIRBUS 320 A320232 3930326 EU ZONE 200 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 677AW 2430 AFT F/A FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED AFT F/A FLASHLIGHT. OPERATIONAL CHECK WAS GOOD. (K) 2 L 7 2 4F RT A28NM 20081010 NM 2008 10 10 USA2008F00025 1 20080912 A 2750 FLAP SYSTEM BOEING 757 7572B7 1384964 NM TE FLAPS MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 942UW 27807 DURING CLIMBOUT, THE CREW RECEIVED AN ASYMMETRICAL TRAILING EDGE FLAP DISAGREE MESSAGE. THE CREW DECIDED TO RETURN TO F IELD. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING. (K) 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 USA2008F00026 1 20080911 A 5210 863424 ACTUATOR BOEING 767 7672B7 1385107 NM PAX DOOR INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AY 26847 THE FWD R1 ENTRY DOOR BAR ASSY SPRING RETRACT ACTUATOR WAS FOUND INOPERATIVE DURING THE SLIDE DEPLOYMENT CHECK. MAINT R EPLACED FWD R1 ENTRY DOOR BAR ASSY SPRING ACTUATOR. OK FOR SERVICE. (K) 2 L 7 2 4F RT A1NM 20081010 NM 2008 10 10 2008UALA05948 1 20080930 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 195UA 26899 EMERGENCY EXIT LIGHTS INOP ZONE E LEFT AND RIGHT CEILING. REPLACED BATTERY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081010 NM 2008 10 10 2008UALA05950 1 20081001 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 198UA 28716 SEAT 3J EMERGENCY LIGHT ON AISLE ARM IS LOOSE. LIGHT FOUND UNSECURE. REPLACED LAMP. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081010 NM 2008 10 10 2008UALA05958 1 20081002 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 818UA 882 BEAM 145 CORRODED. REMOVED FLOORBEAM 145. TRANSFERRING FASTENER HOLES TO NEW BEAM. INSTALLING FASTENERS IN NEW BEAM. INSTALLED NEW BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081010 2008 10 10 RYN2008F00018 4 20080911 A 2565 SLIDE BOEING 757 757236 1384971 NM UNWANTED DEPLOY A RYNA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 GL 31 526NA 24794 F/O ACCIDENTALLY BLEW L1 DOOR SLIDE. C/A IN WORK. (K) 2 L 7 2 4F RT A2NM 20081010 SW 2008 10 10 WGE2008F00003 1 20080909 A 5752 EM41165 ACTUATOR ECLIPS EA500 ECLIPSEEA500 3350000 SW RT WING TE FLAPS MALFUNCTIONED E WGEA O OTHER O OTHER NR NOT REPORTED 1 EA 27 156DJ 274 000073 REF MX LOG PAGE NR 1317, DISC 1, "FLAP FAIL" DISPLAYED ON CAS. REMOVED AND REPLACED RT IB FLAP ACTUATOR WITH A NEW UNIT IAW EA500 AMM CH 27-51-11. OPS CHECK GOOD. (K) 1 L 7 2 4J RT A00002AC 20081010 NM 2008 10 10 2008UALA05975 1 20081003 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 SEAT 4F AFT EMERGENCY LIGHT INOP. LIGHT IS INOPERABLE. REPLACED LAMP. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081010 EA 2008 10 10 SWIA200820114 1 20080928 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 764SK 10229 AFT OVERHEAD EMERGENCY LIGHT INOP. (FLT 6380) RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081010 EU 2008 10 10 UPS08153445 1 20080922 A 5754 A5724199320300 RIB AIRBUS A300 A300F4622R 3930360 EU L/E SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR RT WING KRUEGER FLAP WELL AT INBOARD RIB SUPPORT IS CRACKED. REPLACED RT WING KRUEGER FLAP WELL RI B REF A300-600 SRM 51-40-21 PAGE 1. 2 L 7 2 4F RT A35EU 20081010 NM 2008 10 10 UPS08553447 1 20081001 A 5330 141N32152 SKIN BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 415UP 23855 INSPECTION TYPE:SV FUSELAGE SKIN DENTS AT FS 200-215 BETWEEN S-23L-26L. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SAA EA 757-5310- A1524 AND UPS EO B757-5330-30752-B. 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 AALA200802193 1 20080826 A 2761 SEAL BOEING 767 767323 1385205 NM SPOILER ACTUATOR BROKEN A AALA J A DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 349AN 33088 DFW INFLIGHT T997/26AUG. CREW REPORTED INDICATION OF LT HAND HYDRAULIC QUANTITY LOSS. RETURNED TO DFW AND LANDED WITHO UT INCIDENT. REPLACED BROKEN PACKAGING ON FILTER CAP IN NR 12 SPOILER ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPS. ETO PS OPERATION. 2 L 7 2 4F RT A1NM 20081010 2008 10 10 AALA200802194 4 20080826 A 2565 D30654122 SLIDE BOEING 757 757223 1384957 NM L1 DOOR FAILED A AALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 194AA 32388 MIA SLIDE AT LT NR 1 DOOR WAS NOT DISARMED AND PARTIALLY DEPLOYED. SLIDE FAILED TO INFLATE. REPLACED LT NR 1 DOOR SLID E AND DOOR ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081010 WP 2008 10 10 AALA200802195 1 20080826 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 491AA 49684 LGA EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081014 NM 2008 10 14 UPS08M53460 1 20080806 A 5330 SKIN PANEL DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:N/A CTR CARGO SKIN PANEL AT STA 1551 BILGE AREA L52 FOUND CORROSION. SKIN PANEL CORROSION REMOVED AND R EPROTECTED AS PER SRM 51-21-01 VOL II REV 40. MATERIAL REMOVED 0.004". ORIGINAL THK 0.068" REMAINED 0.064" FOUND WITHI N LIMITS PER SRM 53-00-01 FIG 2 VOL 1 REV 40. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 CALA0800950 1 20081006 A 5320 69455559 MOUNT BRACKET BOEING 757 757224 1384958 NM CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14120 27562 CORROSION FOUND AT NUMBER 1 CARGO DOOR SILL AREA APPROXIMATELY 12 INCHES FROM FORWARD END OF DOOR CUTOUT. REMOVED AND R EPLACED BRACKET MOUNT PART NUMBER 69-45555-9 PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081014 CE 2008 10 14 J7SA45271080930 1 20080930 A 3233 6632303003003 ACTUATOR LEAR 45 45LEAR 5170805 CE MLG FAILED E J7SA O OTHER J WARNING INDICATION LD LANDING 1 SW 05 435FX 2697 45271 GEAR FAILED TO EXTEND WITH NORMAL PROCEDURE. TRANSIT LIGHTS ILLUM. FREEFALL PROCEDURE WAS SUCCESSFUL. 9/30/08 - MX FE RRY FLT TO HWD. MX PERFORMED THE FSR RECS AND ACCESSED THE L/R INBOARD GEAR DOOR ACTUATORS TO CHK RESISTANCE THRU THE G EAR DOOR DOWN SWITCHES (S97 AND S101). CHECKED FOR 28V AT THE LANDING GEAR CONTROL MANIFOLD, PLUG A70P1 - PIN 5 WITH TH E GEAR DOORS FULLY EXTENDED. 28V WAS BEING RECEIVED HOWEVER MX COULD PHYSICALLY MOVE THE RT GEAR DOOR FORE AND AFT, LES S THAN AN INCH, AND THE VOLT WOULD FLUCTUATE BETWEEN 0 AND 28V. ALSO BACKPINNED THE A70P1 CONNECTOR TO THE LG CONTROL M ANIFOLD ON PIN 5 TO CHECK FOR VOLT UNDER A LOAD. THE VOLT WENT TO 0.5V UNDER A LOAD. THE CURRENT WAS MOST LIKELY BEING 2 L 7 2 4F RT T00008WI 20081014 WP 2008 10 14 IXXA08SMN127S 1 20080411 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C-CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 670 LONGERON 35.5 RIGHT. REMOVED FASTENERS AS NE EDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRACK AND CORROSION FOUND. FAB RICATED REPAIR DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER. INSTALLED NEW FASTENERS AND REPAIR DOUBLE R IAW DC8 SRM 51-1-11, 51-1-21, 51-3-0, 51-3-1, FAA FORM 8110-3 NUMBER 08197 DATED 04/25/08, SEMAN DRAWING ED-3863 REVIS ION 1 DATED 04/21/08, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 20081014 WP 2008 10 14 IXXA08SMN128S 1 20080411 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C-CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 404 LONGERON 35.5 LEFT. REMOVED FASTENERS AS NEE DED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND CORROSION FOUND. FABRICATED REPAIR DOUBLER, INTERNAL FINGER DOUBLER, SKIN FILLER. CLEANED, TREATED AND PRIMED AREA AN D REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-3-1, FAA FORM 8110-3 NUMBER 08244 DATE D 05/08/08 SEMAN DRAWING ED-3861 REVISION1 DATED 04/26/08, DC8 SRM 51-1-21, 51-3-0, 51-1-20D, DC8 NDT SPM PART 06-10-01- 001, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 20081014 SO 2008 10 14 RAIA2008100800032 1 20080929 A 2150 VALVE EMB 145 EMB145LR 3260212 SO NR 1 PACK CLOSED A RAIA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 810HK 145231 DURING CRUISE, PACK 1 VALVE CLOSED UNCOMMANDED. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE NR 1 PACK SYSTEM WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 20081014 EU 2008 10 14 USAABA08030 1 20081006 A 2133 VF1620B00 OUTFLOW VALVE AIRBUS 330 A330323 3930335 EU CABIN PRESSURE DEFECTIVE A USAA B E EMER. DESCENT ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 EA 19 273AY 0337 CDG FLT 755 EN ROUTE CDG TO PHL. AT FL 343, RECEIVED CABIN PRESSURE ADVISORY LIGHT. THE CABIN PRESSURE PAGE ON ECAM DISPLAYED. THE VENT EXTRACT VALVE INDICATED AMBER AND OPEN. THE CABIN PRESSURE REACHED 10,500 FEET. THE FLIGHT CREW P ERFORMED A RAPID DESCENT TO 10,000 FEET AND REGAINED CONTROL OF CABIN PRESSURE. THE FLIGHT RETURNED TO FIELD CDG AND LA NDED WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE OVERBOARD EXTRACT VALVE ON MEL. MAINTENANCE LATER REPLACED THE O VERBOARD EXTRACT VALVE. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A46NM 20081014 SO 2008 10 14 CHQA200800194 1 20081005 A 3397 MS27473E10F35S CONNECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CABIN LOOSE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 268SK 145270 CAE311607 MAINTENANCE FOUND THE BACK SIDE OF THE CENTER AISLE EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE DURING TEST. MAINTENANCE R ESET THE CONNECTOR ON THE LIGHT AND THE SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081014 SO 2008 10 14 GLBA200810081 1 20081004 A 3231 DOOR EMB 120 EMB120ER 3260203 SO NLG UNLATCHED A GLBA B EMER. DESCENT E VIBRATION/BUFFET CR CRUISE 1 NM 03 96ZK 120096 SIGNIFICANT EVENT - EN ROUTE FROM CYS - DEN THE PILOTS REPORTED A LOUD VIBRATION COMING FROM THE NOSE WHEEL AREA, IT STO PPED WHEN THE GEAR WAS EXTENDED. PILOTS DECLARED AN EMERGENCY AND TRUCKS WERE DEPLOYED. MAINTENANCE DETERMINED THAT TH E LEFT HAND FORWARD NOSE LANDING GEAR DOOR WAS FOUND UNLATCHED. MAINTENANCE FOUND NO DEFECTS AND RE-ATTACHED THE DOOR L ATCHES. OPERATIONAL CHECKS GOOD IAW MM 32-22. LANDING WAS UNEVENTFUL. 2 L 7 2 4T RT A31SO 20081014 EU 2008 10 14 YENA2008093 1 20080929 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 598JB 16476 2314 LT EPSU FAILED DURING EMERGENCY LIGHT SYSTEM TEST (13WL). REMOVED AND REPLACED LT EPSU AS PER AMM 33-51-38-04. SYSTEM OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081014 NM 2008 10 14 SWAA085404 1 20081006 A 5330 6546529 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED BETWEEN BS 387.5 TO BS 452.75. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085393 1 20081004 A 3350 65C27095 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081010 WP 2008 10 10 WRL2008F00007 1 20080906 A 5320 INTERCOSTAL DOUG DC10 DC1030F 3023504 WP BS 1505 CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 303WL 46917 DURING INSPECTION FOUND CORROSION IN THE RT MLG WHEEL WELL STA 1505 AT LONGERON 35 R SKIN INTERCOSTAL AND FRAME ATTACH, REF DELTA N/R 41. REMOVED CORROSION ON SKIN AND FRAME AT LONGERON 35R BETWEEN STA 1505-1521, WITHIN LIMITS IAW SRM 53-00 -01, TREAT AND PAINTED SKIN AND FRAME IAW SRM 53-00-01. FABRICATED NEW INTERSCOSTAL ON DELTA SHOP ORDER AP5785, INSTALL ED INTERCOSTAL. IAW DWG AEA0024. (K) 2 L 7 3 4F RT A22WE 20081010 EA 2008 10 10 VNA2008F00006 1 20080906 A 3150 NONE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NONE NONE A VNAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 05 215PS 7880 CREW REPORTED A NR 2 ICE DETECTION MESSAGE. CIRCUIT BREAKERS FOR ICE DETECTOR SYSTEM WERE RESET. NO OTHER DEFECTS WERE N OTED AND ACFT WAS RELEASED FOR SERVICE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 20081010 2008 10 10 CHQ2008F00007 4 20080911 A 3100 DISPLAY EMB 145 EMB145EP 3260221 SO MALFUNCTIONED A CHQA O OTHER O OTHER NR NOT REPORTED 1 GL 11 978RP 145169 WHILE CLIMBING THROUGH 7,000 FT, THERE WAS NO INDICATION ON THE CPAM DISPLAY ON EICAS. CREW REPORTED DASHED LINES FOR CA BIN PSI, RATE OF CLIMB, AND CABIN ALTITUDE. THE ACFT RETURNED TO FILED AND LANDED WITHOUT INCIDENT. MAINT RESET THE CPAM CIRCUIT BREAKER AND CYCLED POWER IAW THE FIM 21-31-00 THE INDICATION RETURNED WITH NO FURTHER DEFECTS NOTED. (K) 2 L 7 2 4F RT T00011AT 20081010 EA 2008 10 10 CHQ2008F00008 1 20080912 A 3150 NONE CNDAIR CL600 CL6002B19 1900309 EA NONE A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 657BR 7491 THE FLIGHT CREW RECEIVED A LT PACK HIGH PRESSURE MESSAGE AFTER TAKEOFF WITH THE RT PACK ON MEL. THE ACFT LANDED BACK AT DEPARTURE WITHOUT INCIDENT. MAINT RESET THE LT PACK AND OPS CHECKED GOOD. THE RT PACK WAS LEFT ON MEL. (K) 2 L 7 2 4F RT A21EA 20081010 EA 2008 10 10 CHQ2008F00009 1 20080912 A 3150 NONE CNDAIR CL600 CL6002B19 1900309 EA NONE A CHQA O OTHER N FALSE WARNING AP APPROACH 1 GL 11 642BR 7356 DURING APPROACH WHEN THE FLIGHT CREW SELECTED FLAPS TO 45 DEGREES, THEY RECEIVED A FLAP FAIL MESSAGE WITH THE FLAPS FAIL ED AT 8 DEGREES. THE ACFT LANDED WITHOUT INCIDENT. MAINT CHECKED THE FECU FOR FAULT CODES WITH NONE PRESENT. THE FECU A ND SKEW DETECTION SYSTEM WERE RESET AND THE FLAP SYSTEM OPERATED NORMALLY. (K) 2 L 7 2 4F RT A21EA 20081010 SO 2008 10 10 CHQ2008F00011 1 20080913 A 2497 RSE116132 SOCKET EMB 135 EMB135KL 3260302 SO LT RELAY BURNED A CHQA G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 376SK 145578 DURING CRUISE, THE FLIGHT CREW RECEIVED A PITOT 1 INOP EICAS MESSAGE AND SMELLED SMOKE. IMMEDIATELY AFTER THEY RECEIVED AN AOA 1 HEAT INOP MESSAGE AND THE FLIGHT INSTRUMENTS ON THE CAPTAIN`S PFD BEGAN TO GIVE ERRONEOUS INDICATIONS. THE FLIG HT CONTROLS WERE TRANSFERRED TO THE F/O AND OXYGEN MASKS WERE DONNED. THE F/A REPORTED SEEING SMOKE AND DURING THE EMERG ENCY DESCENT THE FLIGHT CREW ACTIVATED THE APU AND BAGGAGE COMPARTMENT EXTINGUISHER BOTTLES WITH NO FIRE OR SMOKE INDICA TIONS ON EICAS. THE ACFT LANDED WITHOUT INCIDENT. MAINT INSPECTED THE ACFT AND FOUND THAT THE RELAY SOCKET AND RELAY FOR THE PITOT 1 HEAT SYS IN THE LT RELAY BOX HAD BURNED AND DAMAGED THE RELAYS ABOVE IT IN THE RELAY BOX AS WELL AS THE REL 2 L 7 2 4F RT T00011AT 20081014 NM 2008 10 14 UPS08M53463 1 20080806 A 5311 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:N/A CTR CARGO FRAME AT STA 1721 BILGE ARE L52 FOUND CORROSION. FRAME CHANNEL AND SHEAR CLIP CORROSION R EMOVED AND REPROTECTED AS PER SRM 51-21-01. MATERIAL REMOVED 0.007" ORIGINAL THK 0.071" REMAINED THK 0.064" FOUND WITHI N LIMITS PER SRM 53-30-00. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 UPS08M53464 1 20080806 A 5311 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:N/A CTR CARGO FRAME AT STA 1741 BILGE AREA BETWEEN L51 - L52 LT FOUND CORROSION. FRAME SHEAR CLIP CORRO SION REMOVED AND REPROTECTED AS PER SRM 51-21- 01. MATERIAL REMOVED 0.009" ORIGINAL THK 0.071" REMAINED THK 0.062" FOUN D WITHIN LIMIT PER SRM 53-00-01. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 CALA0800946 1 20081006 A 5320 6517684634 INTERCOSTAL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 WEB CRACKED BODY STATION 294.3 LT INTERCOSTAL 16. REMOVED AND REPLACED CRACKED WEB PER ECRA 5311-01424 REV A. 2 L 7 2 4F RT A16WE 20081014 GL 2008 10 14 S9BA2008028 3 20081002 A 6111 B3007 COUNTERWEIGHT DHAV DHC6 DHC6300 2802606 EA HARTZL HCB3T HCB3T* GL LT PROPELLER LOOSE A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 562CP 288 562 BUA25646 SSB - LEFT PROPELLER BLADE NR 3 COUNTER WEIGHT LOOSE. BOTH MOUNTING BOLTS WERE INSTALLED WITH LOCKING PINS. REMOVED AN D REPLACED PROPELLER. SENDING PROPELLER TO REPAIR STATION FOR EVALUATION. INSPECTED ALL AIRCRAFT IN FLEET FOR LOOSE PR OPELLER WEIGHTS. NONE FOUND. 1 H 7 2 3T RT A9EA 6 C P15EA 20081010 EA 2008 10 10 ASA2008F00006 1 20080903 A 5530 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 709EV 10068 CRACKED DRAG ANGLE LEFT LOWER VERT STAB (MARKED). PERFORMED EDDY CURRENT INSPECTION OF LEFT V/STAB TO FUSELAGE DRAG ANG LE IAW CRJ 700 NDTM 51-20-006. DRAG ANGLE IS VERIFIED CRACKED AND END OF CRACK IS MARKED. PERFORMED CUTOUT OF DAMAGED AREA LOCATED OF LT LOWER VERTICAL STAR AND REMOVED BURS AND SHARP EDGES IAW RFO 670-55-31-018. (K) 2 L 7 2 4F RT A21EA 20081010 EA 2008 10 10 ASA2008F00007 1 20080903 A 5530 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 709EV 10068 CRACKED DRAG ANGLE RT LOWER VERT STAB (MARKED). PERFORMED EDDY CURRENT INSPECTION OF RT V/ STAB TO FUSELAGE DRAG ANGLE I AW CRJ 700 NDTM 51-20-006. DRAG ANGLE IS VERIFIED CRACKED AND END OF CRACK IS MARKED 9/4/08 VTJ7010159. GUT AWAY DAMAGE D AREA OF RT DRAG ANGLE IAW RFO 670-55-31-018. (K) 2 L 7 2 4F RT A21EA 20081010 NM 2008 10 10 F3LA200800605 1 20080907 A 5330 SKIN AIRBUS A319 A319111 3930336 NM FUSELAGE DENTED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 950FR 3028 REF NON ROUTINE C00003. DURING EXIT CHECK, INSPECTION NOTED THE AC INCURRED A BIRD STRIKE CAUSING A DENT IN THE FUSELAGE SKIN BELOW THE RT COCKPIT WINDSHIELD. THE DENT MEASURED 2 INCHES WIDE AND 2 INCHES LONG BY .1250 INCH DEEP. MAINT PERFO RMED A DETAILED VISUAL INSPECTION OF THE AFFECTED AREA, A HIGH FREQUENCY EDDY CURRENT INSPECTION OF ADJACENT FASTENERS AND RECONTOURED THE AREA OF SKIN DAMAGE. MAINT WAS ACCOMPLISHED IAW THE REQUIREMENTS OF ENGINEERING AUTHORIZATION NR A9- 53R-30586, WHICH CLASSIFIED THE REPAIR AS "MAJOR". UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE . (K) 2 L 7 2 4F RT A28NM 20081010 NM 2008 10 10 F3LA200800604 1 20080908 A 5321 D5367175500000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 929FR 26 2240 REF: NON ROUTINE C050752. DURING C3 C-CHECK, INSPECTION FOUND (1) MOUNT BUSHING CORRODED ON FLOOR PANEL 261DE. MAINTENA NCE REMOVED AND REPLACED MOUNT BUSHING ON C-CHECK CARD NR C5341032. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (K) 2 L 7 2 4F RT A28NM 20081010 NM 2008 10 10 F3LA200800603 1 20080903 A 5755 D57745013 HINGE AIRBUS A319 A319111 3930336 NM RT WING SPOILER DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 929FR 26 2240 REF: NOT ROUTINE C050745. DURING C3 C-CHECK, INSPECTION FOUND DAMAGE ON THE RT NR (2) SPOILER ANTI-ROTATION WEB. MAINT M ACHINED AREA, FABRICATED REINFORCING PLATE AND PROTECTED AREA IAW ENGINEERING AUTHORIZATION NR A9-57R-30610. UPON COMPLE TION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. (K) 2 L 7 2 4F RT A28NM 20081010 NM 2008 10 10 F3LA200800602 1 20080903 A 5755 D57745013 HINGE AIRBUS A319 A319111 3930336 NM RT WING SPOILER DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 929FR 26 2240 REF NON ROUTINE C050746. DURING C3 C-CHECK, INSP FOUND DAMAGE ON THE RT NR (4) SPOILER ANTI-ROTATION WEB. MAINT MACHINED AREA, FABRICATED REINFORCING PLATE AND PROTECTED AREA IAW EA NR A9-57R-30609. UPON COMPLETION OF THE REPAIR, IT WAS INS PECTED AND FOUND ACCEPTABLE. (K) 2 L 7 2 4F RT A28NM 20081010 NM 2008 10 10 F3LA200800599 1 20080904 A 5315 D53472172203 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 929FR 2240 REF NON ROUTINE C050605. DURING C3 C-CHECK, INSPECTION NOTED SEVERAL NUT PLATE HOLES ON FRAME Y-1292 BETWEEN FRAME 66 A ND FRAME 68, HAD CORROSION. MAINT REMOVED CORROSION FROM HOLES, FABRICATED REPAIR PROFILE AND FILLER, AND INSTALLED IAW THE REQUIREMENTS OF EA NR A9-53R-30604 AND A 319 SRM 53-00-14, FIGURE 214. UPON COMPLETION OF THE REPAIR, IT WAS INSPE CTED AND FOUND ACCEPTABLE. (K) 2 L 7 2 4F RT A28NM 20081010 EA 2008 10 10 A6WA200840566 1 20080806 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 445AW 7804 CRACK FOUND IN THE AFT DRAG ANGLE OF THE PAX DOOR STAIR ASSY LENGTH OF CRACK 1.50". DRAG ANGLE OF THE PAX DOOR STAIR AS SY, AFT SIDE, REPAIRED IAW CRJ 200 REO 601R 52-11-513. (K) 2 L 7 2 4F RT A21EA 20081010 NM 2008 10 10 ASAA0853557 1 20080930 A 3040 8300005604 CONTROL UNIT BOEING 737 737890 1384527 NM E&E BAY FAILED A ASAA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 02 558AS 8756 35177 LEFT SIDE WINDOW OVERHEAT (C/B POPPED). INSPECTED C/B C392AND RESET IAW MM 20 60 01. PERFORMED FIM 30 41 00 810 814 FO UND 7 BUSS POWER FAULTS. PERFORMED FIM 30 41 00 810 816. SENSOR AT 326 OHMS NML MM 30 41 00 HEAT FILM AT 71 0 OHMS NML 30 41 21. REPLACED WHCU IAW MM 30 41 11 000 801, NO FURTHER DISCREPANCIES NOTED. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 AALA200802246 1 20080830 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 943AN 30599 DFW EMERGENCY LIGHTS AT SEAT ROW 7DEF INOPERATIVE. SECURED CONNECTOR IN SIDEWALL FOR EMERGENCY LIGHTS AT SEAT ROW 7DEF. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081010 NM 2008 10 10 AALA200802247 1 20080830 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 766AN 32880 DFW EMERGENCY LIGHT AT SEAT 25C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081010 NM 2008 10 10 2008UALA05961 1 20081002 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 818UA 882 BEAM 95 CORRODED. REMOVED FLOORBEAM 95. REMOVED BRACKETS AND DRILLED NEW BEAM AND READY FOR BRACKET INSTALL. ALL BRAC KETS AND ATTACH FITTINGS INSTALLED AND READY FOR INSTALLATION INTO AC. BEAM INSTALLED, ATTACHMENT COMPLETE AT FRAME 64, NEEDS BOLTS AT FRAME 66 AND 65. COMPLETED INSTALLATION OF BEAM. FOUND SERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081010 2008 10 10 RYN2008F00019 4 20080911 A 3100 LINE BOEING 757 757200 1384950 NM P1 PROBE BROKEN A RYNA O OTHER O OTHER NR NOT REPORTED 1 GL 31 151GX 24451 LT ENGINE EPR INDICATION BLANKING OUT AND ENGINE HAS LOW POWER. REPLACED THE LT ENGINE P1 PROBE BROKEN SENSE LINE. COMPL IED WITH HIGH POWER ENGINE RUN, NO DEFECT NOTED. (K) 2 L 7 2 4F RT A2NM 20081010 2008 10 10 RYN2008F00021 4 20080910 A 3100 LINE BOEING 757 757236 1384971 NM P1 PROBE BROKEN A RYNA O OTHER O OTHER NR NOT REPORTED 1 GL 31 526NA 24794 PILOT REPORT LT ENGINE NOT MAKING POWER AT FL 20000 WITH THE ENGINE POWER LEVER FULLY FWD AND N1 WAS ONLY 71 PERCENT. RE PLACED THE LT ENGINE P1 PROBE BROKEN SENSE LINE. COMPLIED WITH HIGH POWER ENGINE RUN, NO DEFECT NOTED. (K) 2 L 7 2 4F RT A2NM 20081010 NM 2008 10 10 2008UALA05969 1 20081002 A 2780 CONTROL VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L/E SLAT MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 597UA 28750 AUTO SLAT STALL WARN EXTENSION AND RETRACTION INOP. REPLACED FSEU 3. CHECKS OK. AUTO SLAT CONTROL VALVE REPLACED. OP CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081010 NM 2008 10 10 2008UALA05970 1 20081002 A 3350 32145410 BATTERY PACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 819UA 893 AFTER NR 3 SVC CABIN EMERGENCY LIGHT CHECK, CIDS PANEL SHOWS 33-51-38 EPSU BATTERY EMER L. BATTERY PACK FOUND FAULTY. REPLACED BATTERY PACK. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081010 NM 2008 10 10 2008UALA05971 1 20081003 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 AFT GALLEY AISLE EMERGENCY LIGHT INOP. LIGHT FOUND DEFECTIVE. REPLACED LAMP, OP CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081010 NM 2008 10 10 2008UALA05976 1 20081003 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 SEAT 4E AFT EMERGENCY LIGHT INOP. LIGHT IS DEFECTIVE. REPLACED LAMP. OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20081010 NM 2008 10 10 2008UALA05977 1 20081002 A 5320 STRUCTURE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 818UA 882 CORROSION AROUND NUT PLATE HOLES INBOARD OF AFT GIRT BAR FITTING DOOR 2L. REMOVED CORROSION PER MT 53-025. INSPECTED RE PAIR PER MT53- 025. FOUND SERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081010 NM 2008 10 10 2008UALA05978 1 20081002 A 5320 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 818UA 882 CORROSION IN AREA OF PREVIOUS REPAIR BEAM 190. REMOVED CORROSION. INSPECTED REPAIR PER MT53- 025, FOUND SERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081010 EA 2008 10 10 SWIA200820111 1 20081002 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 367CA 10069 EMERGENCY LIGHT THIRD FROM FRONT OF CABIN IS INOP. (FLT 3837) RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081014 NM 2008 10 14 SWAA085403 1 20081004 A 5322 6546529 SHEAR TIE BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 783SW 29809 DURING SCHEDULED 8Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 32. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 CALA0800956 1 20081007 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 FUSELAGE STATION 867 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 867 BETWEEN S8R AND S9R, FABRICATED AND INSTALLED REPAIR ANGLES PER EA5310-04498. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 CALA0800958 1 20081007 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 FUSELAGE STATION 747 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. CUT OUT DAMAGE AT FUSELAGE STATION 747 BETWEEN S8L AND S9L, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 CALA0800960 1 20081007 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 FUSELAGE STATION 867 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. CUT OUT DAMAGE AT FUSELAGE STATION 867 BETWEEN S8L AND S9L, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 F3LA2008102200676 1 20081020 A 5315 A319111 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON FLOORBEAM LOCATED AT Y1292 AND FRAME 68, PASSENGER CABIN. MAINTENAN CE REMOVED AND REPLACED FLOORBEAM IN ACCORDANCE WITH A319 SRM 51-42-11 PAGES 1 AND 2. 2 L 7 2 4F RT A28NM 20081016 NM 2008 10 16 DHLA2008745504 1 20081007 A 5754 BAC1513347 FITTING BOEING 727 727224 1384076 NM L/E SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 RIGHT WING, NR 8 L/E SLAT TRAILING EDGE CRACKED AT SLAT STA 413. REMOVED AND REPLACED TRAILING EDGE EXTRUSION MEMBER PE R B727 SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 20081024 WP 2008 10 24 K11A2008102291501 1 20081017 A 2450 MS2721243 TERMINAL BLOCK DOUG DC9 DC915F 3022037 WP ELECTRICAL SYS BROKEN A K11A K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 23 915CK 47086 TERMINAL BLOCK AT STA FS 146 FLOORBEAM BROKE, AFTER INVESTIGATION FOUND 2 WIRES DAMAGED. REPLACED WIRE FROM TERMINAL NR 1 TO THE T1 POSITION ON THE LEFT APU BUSS RELAY. ALSO REPLACED TERMINAL END ON THE SECOND ATTACHING IN THE NR 1 POSITI ON OF THE TERMINAL BLOCK. 2 L 7 2 4F A6WE 20081024 NM 2008 10 24 K11A2008102372201 1 20081021 A 5320 STRUCTURE BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20849 LOWER TEE CHORD FLANGE CORRODED, VIEWED THRU ACCESS HOLE ON NLG WHEEL WELL. 2 L 7 3 4F RT A3WE 20081014 NM 2008 10 14 08FDEA04146 1 20080930 A 5753 ARC0502505 HINGE FITTING DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 LEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE AFT LOWER OUTBOARD MOUNTING BORE HOLE INNER SURFACE FOUND WITH PITTING COR ROSION. CORROSION AT LT WING OUTBOARD FLAP INBOARD FORWARD HINGE AFT LOWER OUTBOARD MOUNTING BORE HOLE REMOVED AND FO UND WITHIN LIMIT AS PER CMM 57-44-08. BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-08. REPAIR CLASSIFIED AS MINO R PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 K11A2008102372204 1 20080821 A 5315 FLOORBEAM BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 CORROSION AROUND FASTENER HOLE ON FLOORBEAM BOTTOM CHORD. 2 L 7 3 4F RT A3WE 20081024 NM 2008 10 24 SWAA085617 1 20081019 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 782SA 29808 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 43. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 08FDEA04158 1 20081001 A 5753 ARC198414 HINGE FITTING DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING ARC1984 OUTBOARD AFT MOST MOUNTING HOLE FOUND CORROSION. CORROSION IN AF T MOST MOUNTING HOLE FITTING ARC1984 REPAIRED AS PER E.A. NR 1-5750-122571. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-10 0. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 08FDEA04159 1 20081001 A 5753 ARC198414 HINGE FITTING DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING ARC1984 INBOARD MID MOUNTING HOLE FOUND CORROSION. FITTING ARC1984 REPAI RED AS PER E.A. NR 1-5750-122571. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 DL757081226 1 20080925 A 2530 COFFEEMAKER BOEING 757 757232 1384965 NM GALLEY ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 622DL 22912 ELECTRICAL BURNING ODOR COMING FROM FWD GALLEY AREA (NO SMOKE). MX IN PROGRESS. FOUND WARMER HEATER FWD GALLEY AFT COF FEEMAKER BROKEN. REMOVED AND REPLACED COFFEE MAKER, CKS OK. 2 L 7 2 4F RT A2NM 20081014 WP 2008 10 14 08FDEA04165 1 20081001 A 5730 ARC0280507 SKIN PANEL DOUG MD10 MD1010F 3022112 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 40061 46973 LT WING LWR SURFACE T/E FOUND CRACK ON SKIN PANEL REF IPC 57-32-60-01 ITEM 210 VIEW "A". REPAIRED PANEL IAW SRM 51-71-0 0 PAR 18 B & SRM 57-10-00 FIG 73 SHT 5 VOL I. 2 L 7 3 4F RT A22WE 20081014 CE 2008 10 14 GUU2008F00056 1 20081004 A 5210 12951405933 CABLE ASSY BEECH 1900 1900D 1154162 CE AIRSTAIR DOOR BROKEN A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 49543 UE181 FLIGHT 9146 - TPA/MIA - PILOT REPORTED FORWARD DOOR CAMLOCKS STUCK. DOOR WOULD NOT OPEN FROM INSIDE OR OUTSIDE. REPLA CED FORWARD AIRSTAIR DOOR UPPER FORWARD CABLE ASSEMBLY. 2 L 7 2 4T RT A24CE 20081024 NM 2008 10 24 SWAA085668 1 20081021 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 24R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085673 1 20081021 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED AT BS 1016, BETWEEN STR 6L TO 7L. REPAIRED WEB PER PAE ER. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 08FDEA04176 1 20081002 A 5320 6955655 FITTING BOEING 727 727227 1384078 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 FWD PIT DOOR CUTOUT LWR SILL BEAM TIE DOWN FITTING ASSY ADAPTER PLATE IS CORRODED, BS 565, STR 26R, WL 155. REMOVED ADA PTER PLATED STA 580 REF 51-30-02 PG 1. MATCHED DRILLED FASTENER HOLES REF SRM 51-30-05 DWG 69-55655, PAINTED ADAPTER RE F SRM 51-20-00 PG 7. INSTALLED ADAPTER PLATE REF 51-30-02 PG 1. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081014 EU 2008 10 14 08FDEA04107 1 20080929 A 5321 SRZ25008242SF FLOOR PANEL AIRBUS 310 A310222 3930315 EU CABIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 MAIN CABIN FLOOR PANEL 242 SF IS CRACKED. FABRICATED A NEW FLOOR PANEL 242 SF IAW FEDEX DWG SRZ 25-005; REV G. 2 L 7 2 4F RT A35EU 20081014 NM 2008 10 14 DLM88081228 1 20080925 A 3233 ACTUATOR DOUG MD88 MD88 3023688 NM MLG LEAKING A DALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 944DL 49817 CLIMBING THROUGH 4000 FT MSL ACID ODOR CAME THROUGH THE CABIN AND COCKPIT. DISSIPATED A FEW MINUTES LATER. FOUND LT AN D RT MLG ACTUATORS LEAKING. MOVED ACFT TO THE WASHRACK. REMOVED APU DOOR PANEL FOR CLEANING. REINSTALLED APU DOOR PER M/M AND C/W OPN 5090. ALT DUCT BURNOUT. REMOVED BOTH LT AND RT MLG RETRACT ACTUATORS IAW AMM. REINSTALLED ACTS AFTER SHOP VISIT. OPS AND LEAK CHECK OK. 2 L 7 2 4F RT A6WE 20081014 EA 2008 10 14 SWIA200820120 1 20081003 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 440SW 7589 FLT 3886 - EXTERIOR EMERGENCY LIGHT OVER WING RIGHT SIDE INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081014 NM 2008 10 14 UPS08B53472 1 20080108 A 5311 65B0175224 FRAME BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 579UP 26062 INSPECTION TYPE:BCF RT STA 1180 TENSION TIE FRAME WEB 2EA FASTENER HOLE CRACKED MORE THAN 0.030". REPAIRED CRACKED FRAM E WEB AS PER SRM 53-40-07. 2 L 7 4 4F RT A20WE 20081014 EU 2008 10 14 UPS08153471 1 20081007 A 5753 FAIRING AIRBUS A300 A300F4622R 3930360 EU T/E FLAP DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 148UP 0831 LEFT WING NR 3 MOVEABLE FLAP TRACK FAIRING DAMAGED PAST LIMITS. ACCOMPLISHED PERMANENT REPAIR / PART REPLACED WITHIN 30 DAYS. PER EO A300-5720-30771. 2 L 7 2 4F RT A35EU 20081014 NM 2008 10 14 SWAA085446 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 907, STR 24R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 UIEA200800326 1 20081008 A 5330 SKIN BOEING 747 74747UF 1384812 NM FUSELAGE DAMAGED A UIEA K NONE O OTHER TX TAXI/GRND HDL 1 EA 15 418MC 32840 AIRSTAIRS TRUCK STRUCK AIRCRAFT AFTER BLOCK IN WITH STRUCTURAL DAMAGE FORWARD AND BELOW L-1 DOOR. REPAIR ACCOMPLISHED I AW EO 4453A213 PART 2 INITIAL AND REPEAT INSPECTION. HFEC INSPECTION PRIOR TO ACCUMULATION OF 250 FLIGHT CYCLES OR NEXT "A" CHECK. REPEAT EVERY 1500 FLIGHT CYCLES UNTIL PART 3 IS ACCOMPLISHED AND PERMANENT REPAIR NEXT "C" CHECK. 2 L 7 4 4F RT A20WE 20081014 NM 2008 10 14 SWAA085395 1 20081004 A 3350 65C27095 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 331SW 23695 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 CALA0800953 1 20081007 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 FUSELAGE STATION 747 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 747 BETWEEN S8R AND S9R, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 CALA0800959 1 20081007 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 FUSELAGE STATION 827 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. CUT OUT DAMAGE AT FUSELAGE STATION 827 BETWEEN S8L AND S9L, FABRICATED AND INSTALLED REPAIR PARTS PER EA5310-044498. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 08FDEA04078 1 20080928 A 5320 65848772 SUPPORT BOEING 727 727227 1384078 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 AFT CARGO PIT STA 1010 SIDEWALL SUPPORT CORRODED AT FASTENER HOLES OVER STRINGER 27-26L. BLENDED CORRODED AREA, ORIGINA L "T" .050, REMOVED .014 REMAINING .036 OUT OF LIMITS. SUPPORT FABRICATED FROM 2024-0-.040, HEAT TREAT T3 CONDITION, AP PLIED ALODINE, PRIMED, INSTALLED SUPPORT. REF SRM 51-10-2 P7, 53-10-1 P1-2A, 51-30-2 P8 MM 51-20-151-7 P1. THIS IS CLA SSIFIED A MINOR REPAIR. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 SWAA085481 1 20081007 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CRACKED AT BS 344, RBL 38.5. REMOVED AND REPLACED BEAM PER PAE ER. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 08FDEA04102 1 20080929 A 5753 ATTACH FITTING DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 LEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR OUTBOARD ATTACHMENT POINT INBOARD SURFACE FOUND PITTING CORROSIO N. 2 L 7 3 4F RT A22WE 20081024 WP 2008 10 24 08FDEA04353 1 20081015 A 5330 ACA71691 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 LOWER FUSELAGE DENT ON EXT SKIN DIM, 2 INCH BY 2 INCH DEPTH 0.09 INCH. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 SWAA085482 1 20081008 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 16R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 08FDEA04156 1 20081001 A 5753 ARC199113 HINGE FITTING DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 LEFT WING OUTBOARD FLAP OUTBOARD AFT HINGE AFT FITTING AFT BORE HOLE FOUND PITTING CORROSION. FITTING REPAIRED AS PER E .A. 1-5750-122574. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 DL76P081227 1 20080925 A 2421 GENERATOR BOEING 767 767332 1382001 NM LEFT MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1402A 25989 LEFT ENGINE GEN OFF. STATUS MSGS L ENG EEC C1/TE FLAP SHUTDOWN/HI FLOW INHIBIT, WOULD NOT RESET. RESET EICAS MSGS. NO FAULTS ON BPCU. RAN FLAPS, ALL CKS GOOD. 2 L 7 2 4F RT A1NM 20081014 NM 2008 10 14 08FDEA04167 1 20081001 A 5753 692289411 SUPPORT BRACKET BOEING 727 727227 1384078 NM T/E FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 LEFT WING NR 1 FLAP TRACK - FLAP TRACK TO LOWER TRAILING EDGE PANEL SUPPORT BRACKET IS CRACKED. FABRICATED AND INSTALLE D NEW BRACKET REF DWG 65-2289. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081014 NM 2008 10 14 08FDEA04174 1 20081002 A 5320 69169707 ATTACH ANGLE BOEING 727 727227 1384078 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 MAIN ENTRY DOOR, AFT CUTOUT STRUCTURE BS 344 STR 15R INTERCOSTAL FWD ATTACH ANGLE TO FRAME CRACKED. FABRICATED ANGLE RE F BOEING DRAWING 69-16970, SOPM 20-42-03 PG 3, SOPM 20-44-04-PG 3. REPLACED ANGLE REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081014 WP 2008 10 14 08FDEA04141 1 20080930 A 5322 AEA027319 SHEAR TIE DOUG MD10 MD1010F 3022112 WP FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 STA 1501 SHEAR TIES AT LONGERONS 51R TO 51L ARE CRACKED. REMOVED DAMAGED SHEAR TIE AT FS 1501 FROM LONGERON 45R TO 45L . FABRICATED NEW ONE P/N AEA 0273-19 IAW DAC DWG AEA 0273. LOCATED & DRILLED UP NEW ONE IAW DAC DWG AEA 0273. ALODINE & PRIMED IAW SHEAR TIE IAW DC/MD-10 SRM 51-21-01; PG 21 - 24; VOL II. APPLIED TOP COAT OF PAINT IAW DC/MD-10 SRM 51-2 1-01 PG 8; VOL II. PART MARKED NEW PART FX AEA 0273-19 IAW FEDEX GMM 7-0-1001. RE-INSTALLED NEW SHEAR TIE IAW DC/MD-10 SRM 51-35-01 PG 1; VOL II. 2 L 7 3 4F RT A22WE 20081014 SO 2008 10 14 RAIA2008101300001 1 20081010 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN BROKEN A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 838HK 145321 DURING PRE FLIGHT INSPECTION, THE EMERGENCY LIGHT ON THE STAIRS WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BRO KEN WIRE AT THE LIGHT ASSEMBLY. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081014 EA 2008 10 14 SWIA200820121 1 20080930 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 976SW 7952 NR 3 EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081014 CE 2008 10 14 GUUA10050801 1 20081005 A 3260 1293640693 SOCKET BEECH 1900 1900D 1154162 CE COCKPIT DIRTY A GUUA K NONE O OTHER DE DESCENT 1 SO 29 81536 UE152 FLIGHT 9166 - NAS/FLL - PILOT REPORTED LANDING GEAR ANNUNCIATOR GREEN "L" DOESN'T ILLUMINATE WITH GEAR DOWN. CLEANED AN NUNCIATOR LIGHT SOCKET. 2 L 7 2 4T RT A24CE 20081014 NM 2008 10 14 SWAA085441 1 20081005 A 5315 BAC1509 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 767 + 5, LBL 12. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085440 1 20081005 A 5315 BAC1509 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOORBEAM CORRDED AT BS 767 + 5, LBL 7.5. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081014 EA 2008 10 14 SWIA200820106 1 20080929 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 698BR 2336 343 7799 FLT 6077 - AFTER RETRACTING LANDING GEAR RECEIVED NLG DOOR OPEN WARNING MESSAGE. REPLACED NLG SELECTOR VALVE, PN 750006 000 SN ON 221T SN OFF 1976. 2 L 7 2 4F RT A21EA 20081015 EU 2008 10 15 08FDEA04164 1 20080930 A 5321 SRZ25005232JH FLOORBOARD AIRBUS 310 A310222 3930315 EU CABIN DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 MAIN CABIN FLOORBOARD IS BROKEN BETWEEN FRAMES 36 & 37; BL 36R. FABRICATED NEW FLOORBOARD 232 JH IAW FEDEX DWG SRZ 25- 005; REV G. 2 L 7 2 4F RT A35EU 20081015 NM 2008 10 15 08FDEA04157 1 20081001 A 5753 ARC40092 HINGE FITTING DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING (ARC4009) OUTBOARD FORWARD BORE MOUNTING HOLE FOUND WITH CORROSION. RIGH T WING OUTBOARD FLAP INBOARD HINGE FITTING (ARC4009) OUTBOARD FORWARD BORE MOUNTING HOLE PITTING CORROSION REMOVED AS PE R EO 1-5750-5008 PART 2. FINAL HOLE DIAMETER 0.660", MAXIMUM HOLE DIAMETER 0.660" CORROSION STILL EXIST. FOR FLAP REPL ACEMENT REFER TO SNRM N01221. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081015 SO 2008 10 15 RAI2008F00000 1 20080908 A 3610 14530609401 PRECOOLER EMB 145 EMB145LR 3260212 SO BLEED AIR SYS MALFUNCTIONED A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 840HK 145341 DURING CLIMB, CREW RECEIVED A NR 2 BLEED OVERTEMP MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 2 PRECOO LER AND PRECOOLER DUCT IAW AMM PROCEDURES. OPS CHECKED GOOD. (K) 2 L 7 2 4T RT T00011AT 20081010 EA 2008 10 10 SWIA200820112 1 20080927 A 3260 SENSOR CNDAIR CL600 CL6002C10 1390015 EA LANDING GEAR OUT OF ADJUST A SWIA O OTHER N FALSE WARNING TO TAKEOFF 1 NM 07 709SK 10159 GEAR DISAGREE WARNING MESSAGE WHEN GEAR RETRACTED. (FLT 5842) ADJUSTED NLG WEIGHT OFF WHEELS SENSORS PX03 & PX11. 2 L 7 2 4F RT A21EA 20081010 EA 2008 10 10 SWIA200820113 1 20080927 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 750SK 10207 CABIN EMERGENCY LIGHTS INOPERATIVE ABOVE ROW SEVEN. (FLT 5893) RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081010 EU 2008 10 10 UPS08153446 1 20080927 A 5321 B5327074100200 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR MAIN CARGO FLOOR PANEL IS CRACKED IN 3 PLACES, PANEL 232LF. REPAIRED MAIN CARGO FLOOR PANEL 232LF REF A300-600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081010 NM 2008 10 10 UPS08653448 1 20080926 A 5753 HINGE FITTING BOEING 767 76734AF 1385212 NM T/E FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 330UP 27756 INSPECTION TYPE:N/A LT WING I/B MAIN FLAP AFT FLAP I/B SUPPORT FITTING FOUND CRACK. CRACK LENGTH .5 INCH APPROX. HINGE FITTING REPAIRED AS PER SRM 57-53-02-2R1 FIG 201. 2 L 7 2 4F RT A1NM 20081014 NM 2008 10 14 UPS08653451 1 20080926 A 5315 141T514616 STIFFENER BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 330UP 27756 INSPECTION TYPE:N/A CABIN STA 246 LBL 50 FLOORBEAM ATT STIFFENER CRACKED. CRACK LENGTH 1 INCH. DEFECTIVE STIFFENER REP LACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081014 WP 2008 10 14 IXXA08SMN125S 1 20080411 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C-CHECK INSPECT, FOUND FUSELAGE SKIN FORWARD OF FLAT AFT PRESSURE BULKHEAD HAS IMPROPER REPAIR AT STATION FS 1690.000 LONGERON 28. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. PERFORMED DETAILED VISUAL INSPECTION AND EDDY CURRENT INSPECTION. NO CRACK FOUND. FABRICATED NEW SKIN, INTERNIAL, AND EXTERNAL DOUBLERS. CLEANED, TREATED, PRIMED AREA, AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW S/B 53A080, AD 2008-06-2 3, BOEING SB DC853A080 DATED 06/22/04 ACCOMPLISHMENT INSTRUCTION B WORK INSTRUCTION PARAGRAPH 4 APPENDIX "A" INSPECTION SEQUENCE 02, AND ATI EO 53-DC8-3729 DATED 02/05/07. 2 L 7 4 4F RT 4A25 20081014 WP 2008 10 14 IXXA08SMN126S 1 20080411 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C-CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 1384 LONGERON 35.5 RIGHT. REMOVED FASTENERS AS N EEDED TO PERFORM REPAIR. REMOVED EXISTING INTERNAL FINGER DOUBLER. PERFORMED NDT INSPECTION. NO CRACK AND CORROSION F OUND. FABRICATED INTERNAL FINGER DOUBLER. CLEANED, TREATED AND PRIMED AREA AND INTERNAL FINGER DOUBLERS. INSTALLED NE W FASTENERS AND INTERNAL FINGER DOUBLERS 51-1-20D, 51-3-1 FAA FORM 8110-3 NUMBER 08197 DATED 04/25/08, SEMAN DRAWING ED- 3865 REVISION1 DATED 04/21/08, DC8 SRM 51-1-21, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51-1-8B. 2 L 7 4 4F RT 4A25 20081014 NM 2008 10 14 USAA08159 1 20081006 A 3350 417N52056SP LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 915AW 22209 PHX - THE L3 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE L3 DOOR EMERGENCY EXIT LIGHT ASS EMBLY. 2 L 7 2 4F RT A2NM 20081014 NM 2008 10 14 YENA2008100800095 1 20081006 A 2780 COMPUTER EMB ERJ190 ERJ190100IGW 3260408 NM L/E SLAT OUT OF RIG A YENA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 EA 15 206JB 19000025 ON DESCENT WHILE CONFIGURING FOR THE APPROACH WITH FLAPS SELECTED TO LAND 1/2 SPEED BRAKES, RECEIVED THE FOLLOWING EICAS MSGS. SLAT FAIL, SPOILER FAULT, AOA LIMIT FAIL & SHAKE ANTICIPATED, AFTER REFERENCIN QRH, LANDED WITH FLAPS 2 & SLATS ZERO (0) CONFIGURATION. DUE TO NUMEROUS DIVERGING OF FLAPS/SLATS HANDLE INPUTS CREATED A LATCH FAULT IN THE SF-ACE 1 CO MPUTER. PERFORMED ELECTRICAL RE-RIGGING OF SF-ACES COMPUTER IAW AMM 27-80-00-820-802-A, COULD NOT DUPLICATE FAULT. PER FORMED RETURN TO SERVICE TEST OF THE FLIGHT CONTROL SYSTEM IAW AMM 27-00-00-070-801-A/200. NO MESSAGE PRESENT. A/C OK FOR SERVICE. 2 L 7 2 4F RT A57NM 20081014 EA 2008 10 14 CHQA200800192 1 20081005 A 2611 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE CARGO BAY NO TEST A CHQA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 648BR 18940 10160 7406 GEE872739 FLIGHT 5730, IAH TO BTR. DURING DESCENT AT FL230 THE FLIGHT CREW RECEIVED A SMOKE CARGO MESSAGE AND AURAL WARNING ON EI CAS. THE QRH WAS FOLLOWED AND THE AIRCRAFT LANDED WITH OUT INCIDENT IN BTR. THERE WAS NO SMOKE OR ODOR REPORTED. MAIN TENANCE INSPECTED THE CARGO COMPARTMENT WITH NO SIGNS OF SMOKE OR FIRE FOUND AND TROUBLESHOT THE SYSTEM AND FOUND THAT B OTH CARGO SMOKE DETECTORS WOULD NOT TEST. BOTH SMOKE DETECTORS WERE REPLACED AND THE SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 20081014 SO 2008 10 14 CHQA200800193 1 20081005 A 3397 M8372375R1624N CONNECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CABIN LOOSE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 265SK 145226 CAE312062 DURING INSPECTION THE FRONT FLOOR EMERGENCY LIGHT STRIP AND THE BACK SIDE OF THE OVERHEAD EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE FOUND THE CONNECTOR FOR THOSE LIGHTS TO BE LOOSE. THE CONNECTOR WAS CLEANED AND RECONNECTED A ND THE EMERGENCY LIGHTS OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081121 SO 2008 11 21 GLBA200810031 1 20081003 A 5310 DOOR FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 21 71GL 120071 SUPPLEMENTAL INFORMATION - MAJOR REPAIR. DURING ROUTINE SCHEDULED MAINTENANCE A CRACK WAS FOUND IN THE CARGO DOOR FRAME AT THE LOWER AFT CORNER AT A LATERAL STOP. FRAME CRACKED APPROXIMATELY .800. MAINTENANCE REPAIRED THE CARGO DOOR AT T HE LOWER AFT LATERAL STOP POSITION NR 8 IAW EMB SRM 52-30-02. DOUBLER MADE OF 7475-T761, .063 INCH, SEALANT MIL-S-81733 TYPE IV, RIVETS MS20470AD4-X & MS20470AD5-X . INSTALLED NEW T-SECTION P/N 120-19394-601 WITH NEW HARDWARE P/N HC22-5-X AND COLLARS P/N NC77-5. SEALANT UTILIZED WAS MIL-S-81733 TYPE IV. MAINTENANCE SEALED AROUND PATCH AND NEW T-SECTION W ITH MIL-S-8802 TYPE II. REPAIR DOUBLER WAS ALODINED & PRIMED PRIOR TO INSTALLATION. THE CABLE PULLEY P/N 120-29683-001 2 L 7 2 4T RT A31SO 20081014 2008 10 14 YENA2008100900097 4 20081008 A 2330 LSEBUTK1400101 ELECTRICAL BOX AIRBUS 320 A320232 3930326 EU CABIN FAILED A YENA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 636JB 7999 2755 DURING CRUISE, PAX AND NR 3 FA HEARD 2 LOUD POPS FROM ROW 20DEF. A STRONG ELECTRICAL SMELL WAS DETECTED AFTER THE POPS. POWER WAS SHUT OFF TO ALL LTV'S AND SMELL SUBSIDED. CONTROL BOX UNDER ROW 20DEF WAS NOT HOT TO THE TOUCH. MASTER SWI TCH WAS LEFT IN THE OFF POSITION FOR THE REST OF FLIGHT (LIVE TV SYSTEM-ALL). ACCOMPLISHED TSM 24-00-00-810-823. NO SM ELL PRESENT SYSTEMS WORK NORMAL. COMPLIED WITH TSM TASK 23-39-00-810-801. NO NOTICEABLE ELECTRICAL ODOR. NO POPPING S OUND AND NO NOTICEABLE PHYSICAL DAMAGE TO ANY PART OR WIRING FROM ROWS 18-22DEF, 19D VIDEO FAULTY-INTERMITTENTLY SHOWS B LUE SCREEN ON ALL CHANNELS. REMOVED AND REPLACED XEB AT 19 DEF IAW LTV MM 44-20-17. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081014 NM 2008 10 14 SWAA085408 1 20081005 A 5330 6545765 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED OTS CHECK, FOUND SKIN CRACKED AT BS 520, STRL 16R. REPAIRED PER SWA EA. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085410 1 20081002 A 3350 101331 LIGHT BOEING 737 7373A4 1384585 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR LOWER EXIT LIGHT DAMAGED. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085411 1 20081003 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN DETERIORATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EXIT LIGHT LENS DETERIORATED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081014 2008 10 14 SWAA085412 4 20081006 A 2565 416A2100 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 447WN 33720 FOUND R1 EMERGENCY EXIT SLIDE ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085386 1 20081002 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 27L TO STR 28L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085387 1 20081005 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085389 1 20081005 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085390 1 20081005 A 5312 6517582 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND VERTICAL WEB CRACKED AT BS 178, LBL 16. REMOVED AND REPLACED VERTICAL WEB PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085391 1 20081001 A 5210 6545815 DOOR FRAME BOEING 737 7375H4 138449D NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED 18Y CHECK, FOUND L1 DOOR AFT FRAME CRACKED AT NR 5 STOP FITTING FROM BOTTOM. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085397 1 20081005 A 3350 100031 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED SPV CHECK, FOUND FWD LAV EMERGENCY EXIT LIGHT INOP. REPLAMPED LIGHT PER WDM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085398 1 20081005 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 375SW 26583 FOUND LT EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20081014 2008 10 14 SWAA085400 4 20081005 A 2565 6556685 MOUNT BRACKET BOEING 737 7375H4 138449D NM EVAC SLIDE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED 18Y CHECK, FOUND R2 EMERGENCY ESCAPE SLIDE AFT MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 CALA0800952 1 20081007 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 FUSELAGE STATION 400 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 400 BETWEEN S8R AND S9R, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 CALA0800954 1 20081007 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 FUSELAGE STATION 787 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 787 BETWEEN S8R AND S9R, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 08FDEA04075 1 20080928 A 5313 6561477 STRINGER BOEING 727 727227 1384078 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 STRINGER DAMAGED AT BS 540 WL 152 LBL 23. FABRICATED NEW STRINGER SECTION AND TWO SPLICE REPAIRS ON STRINGER 26L BS 540 LBL 23 REF SRM 53-10-3 FIG 1. TREATED, PRIMED AND INSTALLED REF SRM 51-10-2 PG 1-7, 51-30-2 PG 2, 51-10-3 FIG 1. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081014 NM 2008 10 14 08FDEA04076 1 20080928 A 5340 66157221 STRINGER CLIP BOEING 727 727227 1384078 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 488FE 21491 STRINGER CLIP DAMAGED AT STR 26L, FS 540, LBL 23, WL 152. REMOVED AND REPLACED STRINGER CLIP AT STA 540 STRINGER 26L LB L 23 REF SRM 51-30-2 PG 5. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081014 NM 2008 10 14 08FDEA04077 1 20080928 A 5753 65192507 FLAP TRACK BOEING 727 727227 1384078 NM T/E FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 LEFT WING O/B FLAP TRACK I/B EDGE OF TOP FLANGE GOUGED APPROX 14" AFT OF REAR SPAR. BLENDED GOUGE, MATERIAL REMOVED .01 5 WITHIN LIMITS. MAGNETIC PARTICLE INSPECTED, FLAP PEENED REWORKED AREA, APPLIED ALODINE & PRIMED REF EA 7-5750-118300 P2 PART 1 CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081016 SO 2008 10 16 C2XA08CL106 1 20080907 A 3350 66367 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12957 145080 MSP FLIGHT NR 2373, THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTING DID NOT TEST FROM SEAT 3A TO 5A. MAINT REPLACED THE EMERGENCY LIGHT PATH STRIP. OPERATIONAL CHECKS WERE GOOD. (K) 2 L 7 2 4T RT T00011AT 20081015 SO 2008 10 15 GLBA200810084 1 20081006 A 5330 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE DAMAGED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 71GL 120071 MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A LEFT FUSELAGE SKIN REPAIR ABOVE THE LEFT HEAT EXCHANGER EXIT DUCT DOES NOT CONFORM TO GIVEN DOCUMENTATION. MAINTENANCE REMOVED & RE-INSTALLED REPAIR PATCH PER EMBRAER IC2008-120/08303. 2024 T-3 ALUMINUM, .050" BRF24AD - 5AD RIVETS, MIL-S-81733 SEALANT UTILIZED. 2 L 7 2 4T RT A31SO 20081015 SO 2008 10 15 GLBA200810085 1 20081006 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO FUSELAGE DAMAGED A GLBA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 03 71GL 120071 MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A RIGHT HAND INBOARD WING LOWER STRINGER REPAIR BETWEEN WS 2129 & 25 93 DOES NOT CONFORM TO GIVEN DOCUMENTATION. MAINTENANCE REPAIRED THE LOWER RT INBOARD WING STRINGER NR 8 BETWEEN APPROX IMATE WS 2129 AND WS 2593 IAW SRM 57-20. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1. WO 96049 L/P 223554. 2 L 7 2 4T RT A31SO 20081015 SO 2008 10 15 GLBA200810086 1 20081006 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO RT WING DAMAGED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 71GL 120071 MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A RIGHT HAND INBOARD WING LOWER STRINGER BETWEEN WS 2129 & 2593 DOES NOT CONFORM TO GIVEN DOCUMENTATION. MAINTENANCE REPAIRED LOWER RT INBOARD WING STRINGER 10 BETWEEN APPROXIMATE WS 2129 AND WS 2593 IAW SRM 57-20. 2 L 7 2 4T RT A31SO 20081015 SO 2008 10 15 GLBA200810087 1 20081008 A 5730 SKIN EMB 120 EMB120ER 3260203 SO LT WING DAMAGED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 71GL 120071 MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A REPAIR AT THE LEFT INBOARD LOWER WING SKIN AT THE OUTBOARD AFT COR NER AND OUTBOARD FUEL PANEL AT APPROXIMATELY WS 2293 DOES NOT CONFORM WITH GIVEN DOCUMENTATION. MAINTENANCE REMOVED PAT CH AND INSTALLED NEW PATCH IAW IC2008-120/08137. 2 L 7 2 4T RT A31SO 20081014 NM 2008 10 14 08FDEA04090 1 20080929 A 5753 ATTACH FITTING DOUG MD11 MD11 3023602 NM T/E FLAP SCRATCHED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 RIGHT WING OUTBOARD FLAP INBOARD HINGE AFT MOUNTING LOWER OUTBOARD MOUNTING BORE HOLE INNER FACE FOUND WITH SCRATCH MARK S. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 USAASB08096 1 20081014 A 2751 2061141 INDICATOR BOEING 737 7374B7 1384702 NM COCKPIT FAULTY A USAA L ABORTED APPROACH O OTHER AP APPROACH 1 EA 19 453UW 25344 120 24980 ON APPROACH TO FLL, CREW REPORTED A SPLIT FLAP INDICATION ON INDICATOR WHEN SELECTING FLAPS 25. NO ROLL PROBLEMS WERE E NCOUNTERED. CREW SELECTED FLAPS 15 AND ACCOMPLISHED A GO-AROUND. INDICATOR WENT TO NORMAL. FLIGHT LANDED WITHOUT FURT HER INCIDENT. PER FAULT ISOLATION, MM 27-51-00 CALLED OUT FOR REPLACEMENT OF FLAP POSITION INDICATOR. MAINTENANCE REMO VED AND REPLACED THE FLAP POSITION INDICATOR PER MM 27-58-41. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 DHLA2008745503 1 20081007 A 5751 SKIN BOEING 727 727224 1384076 NM LT AILERON DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 DENTS ON LT O/B AILERON LOWER SURFACE AT LWBL 578. ACCOMPLISHED FLUSH REPAIR BETWEEN LWBL 576-582 IAW B727 SRM 57-50-1 FIG 1. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 DHLA2008745508 1 20080901 A 5311 ATTACH FITTING BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 745DH 20665 UPPER FUSELAGE CARGO CABIN FRAME ATTACHMENT CLIP AT B/S 1090 STRINGER 1L & 2L CRACKED. 2 L 7 3 4F A3WE 20081016 NE 2008 10 16 ZES2008F00000 2 20080709 A 7200 30C4656C CASE AMD FALC50 FALCON2000 2730170 NM PWC PW308 PW308A 52187 NE DIFFUSER CORRODED E ZESA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 03 267BW 790 107 PCECFO243 ABORTED TAKEOFF, DUE TO RT ENGINE CHIP LIGHT. REMOVED CHIP PLUG FOR INSPECTION, FOUND SMALL DEBRIS, CLEANED, DRAINED AN D FLUSHED OIL SYS, INSPECTED OIL FILTER, FOUND NO SIGNIFICANT CONTAMINATION. REINSTALLED FILTER AND SERVICED OIL. GROU ND RUN, FOUND NO CHIP LIGHT DURING RUN. DIFFUSER CORRODED. (K) 2 L 7 2 4F 4 F RT A50NM E00065EN 20081024 NM 2008 10 24 K11A2008102372203 1 20080813 A 5315 FLOORBEAM BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 FLOORBEAM ON THE LOWER SURFACE OF THE UPPER CHORD AT WEB HAS GRINDING MARKS AND CORROSION BEYOND LIMITS. 2 L 7 3 4F RT A3WE 20081014 WP 2008 10 14 08FDEA04140 1 20080930 A 7160 AJC741595 PANEL DOUG MD10 MD1010F 3022112 WP NR 2 ENGINE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 NR 2 ENGINE AT THE 5:00 POSITION; LIP RING PANEL LEFT FAN COWL OPEN / CLOSE IS DELAMINATED / CRACKED & GOUGED WITH LOOSE & SHEARED FASTENERS. REMOVED; FABRICATED & REPLACED THE LOWER SKIN PANEL & ANGLE IAW SRM 51-31-01, 51-35-01, 51-24-01 & 55-31-01 & DWG AJC7415; REV BK. ANGLE MARKED IAW GMM 7-0-1000. 2 L 7 3 4F RT A22WE 20081014 WP 2008 10 14 08FDEA04142 1 20080930 A 5420 AJC7415101 SUPPORT DOUG MD10 MD1010F 3022112 WP NR 2 FAN COWL WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 THE NR 2 FAN COWL LT; LOWER MATING AREA; FOUND FWD LEFT ANGLE SUPPORT WORN TO A KNIFE EDGE. FABRICATED & REPLACED ANGLE SUPPORT IAW DWG AJC 7415, SRM 51-35-01, SRM 51-21-01 & SRM 51-31-01. REMOVED & RE-INSTALLED PARTS TO FACILITATE MAINTE NANCE IAW SRM 51-31-02 & AMM 71-10-01-2 & 20-50-01. NR 2 ENGINE STARTER DUCT LEAK CHECK GOOD IAW AMM 71-00-00-4-0. 2 L 7 3 4F RT A22WE 20081024 NM 2008 10 24 K11A2008102372213 1 20080914 A 5315 FLOORBEAM BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 FLOORBEAM HAS CORROSION ON UPPER CHORD, UPPER SURFACE. 2 L 7 3 4F RT A3WE 20081014 NM 2008 10 14 08FDEA04153 1 20081001 A 5753 ARC40091 HINGE BRACKET DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 LEFT WING OUTBOARD FLAP ASSEMBLY INBOARD HINGE BRACKET ARC4009 MOUNTING BORE HOLE INBOARD NR 2 FOUND WITH PITTING CORROS ION. CORROSION REMOVED AS PER E.O. 1-5750-5008 PART 1. FINAL HOLE DIAMETER = 0.660", MAXIMUM HOLE DIAMETER = 0.660". CO RROSION STILL EXIST. FOR FLAP ASSEMBLY REPLACEMENT REFER TO SNRM N01220. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6- 2-100. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 08FDEA04155 1 20081001 A 5753 ARC198413 HINGE BRACKET DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 LT WING OUTBOARD FLAP ASSEMBLY INBOARD HINGE BRACKET ARC1984 MOUNTING BORE HOLE OUTBOARD NR 3 FOUND WITH PITTING CORROSI ON. MOUNTING BORE HOLE OUTBOARD NR 3 BRACKET ARC1984 REPAIRED AS PER E.A. NR 1-5750-122573. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 08FDEA04161 1 20081001 A 5753 ARC70561 ATTACH FITTING DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 LEFT WING OUTBOARD FLAP VANE ATTACHMENT FITTING NR 4 FROM INBOARD FOUND CORROSION AFTER REMOVED FROM FLAP. CORROSION RE MOVED BY MACHINED AS PER SRM 57-20-00 FIGURE 19 VOLUME I AND EXCEED LIMIT. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2- 100. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 08FDEA04162 1 20081001 A 5753 ATTACH FITTING DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 LEFT WING OUTBOARD FLAP VANE ATTACHMENT FITTING NR 3 FROM INBOARD FOUND CORROSION AFTER REMOVED FROM FLAP. CORROSION RE MOVED BY MACHINED AS PER SRM 57-20-00 FIGURE 19 VOLUME I AND EXCEED LIMITS. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2 -100. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 AALA200802206 1 20080826 A 3350 7024092008 SIGN BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 384AA 26996 JFK EMERGENCY EXIT SIGN AT LT HAND LOWER FORWARD OVERWING EXIT DAMAGED. REPLACED SIGN ASSEMBLY FOR EMERGENCY LIGHT AT L T HAND LOWER FORWARD OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081015 SO 2008 10 15 C2XA08IA211 1 20080918 A 3230 355022002 ELECTRONIC UNIT EMB 145 EMB145XR 3260214 SO MLG MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 24103 17182 145645 IAH FLIGHT 2245. THE CREW REPORTED A LANDING GEAR AIR GROUND FAIL MSG UPON GEAR RETRACTION AFTER TAKE OFF. THE ACFT LA NDED AT IAH WITHOUT INCIDENT WHERE MX R&R THE LANDING GEAR ELECTRONIC UNIT. OPERATIONALLY TESTED WITH NO DEFECTS AND TH E ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081015 SO 2008 10 15 RAIA00809014 1 20080913 A 3320 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A RAIA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CE 03 841HK 145382 DURING PRE-FLIGHT INSPECTION, FA NOTICED SMOKE AT ROW 8C SIDEWALL LIGHTS. MAINT DEFERRED LIGHT AT 8C SIDEWALL IAW MEL PR OCEDURES. (K) 2 L 7 2 4T RT T00011AT 20081015 NM 2008 10 15 AALA200802215 1 20080827 A 2750 PSEU BOEING 737 737823 13844BZ NM TE FLAPS FAILED A AALA O OTHER J WARNING INDICATION DE DESCENT 1 SW 21 931AN 30079 SJO INFLIGHT T2113/27AUG. CREW REPORTED TRAILING EDGE FLAP ASYMMETRY INDICATION. LANDED SJO WITHOUT INCIDENT. REPLACE D PROXIMITY SWITCH ELECTRONIC UNIT (PSEU). SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081015 SO 2008 10 15 RAIA00809015 1 20080913 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 836HK 145695 PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. MAINT REMOVED AND REPLACED THE BULB AT THE PASSENGER DOOR EMERGENCY LIGHT. OPS CHECKED GOOD. (K) 2 L 7 2 4T RT T00011AT 20081015 2008 10 15 Q2SA751006 4 20080928 A 2312 8221045401 TRANSCEIVER BOEING 747 747228F 1384895 NM VHF COMM FAILED A Q2SA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 EA 63 751SA 22678 DURING FLIGHT (EBBR), NR 1 AND NR 2 VHF WOULD NOT RECEIVE TRANSMISSIONS OVER NORMAL DISTANCE, LOST COMMUNICATION WITH AT C. AIR TURN BACK TO EBBR DUE TO VHF TRANSCEIVER FAILURES, NO FUEL DUMP REQUIRED. R&R NR 1 VHF TRANSCEIVER IN ACCORDANCE WITH AMM 23-21-01. SWAPPED NR 2 VHF TRANSCEIVER WITH NR 3 VHF TRANSCEIVER IN ACCORDANCE WITH AMM 23-21-02, NR 2 VHF TR ANSCEIVER OPS CHECKED NORMAL. NR 3 VHF TRANSCEIVER DEFERRED MX IN ACCORDANCE WITH DISPATCH DEVIATION PROCEDURES GUIDE ( DDPG), MEL 23-3 (1), CATEGORY D. 2 L 7 4 4F RT A20WE 20081015 SO 2008 10 15 SIMA200827302 1 20080927 A 3610 14530609401 PRECOOLER EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 909AE 14500899 ON FLIGHT 3992 DURING CRUISE CREW ADVISES THAT THERE IS A BURNING RUBBER OIL ODOR IN THE CABIN. WHEN ON THE GROUND THE TEMPERATURE STABILIZED. ACFT REMOVED FROM SERVICE. C/A R&R NR 2 ENGINE PRECOOLER. OPS CHECK GOOD. ACFT RETURNED TO S ERVICE. 2 L 7 2 4T RT T00011AT 20081015 NM 2008 10 15 2008UALA05984 1 20081004 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 195UA 26899 THE 47H EEL LIGHTS ARE DAMAGED. REPLACED EEL LAMP. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081015 NM 2008 10 15 2008UALA05985 1 20081004 A 2121 65771 BLOWER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU A/C PACK VIBRATION A UALA O OTHER E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 386UA 24661 RAMP REPORTS, STRONG VIBRATION FWD CABIN AND LOUDER IN THE FWD CARGO COMP. NOISE AND VIBRATION STOPPED WHEN NORMAL EXHA UST FAN C/B POPPED. NOW HAVE STRONG ELECTRICAL ODOR IN FWD PART OF AIRCRAFT. REPLACED NORM EXHAUST BLOWER. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20081015 NM 2008 10 15 2008UALA05986 1 20081004 A 3350 CHARGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 647UA 25284 SEAT EEL SECTION 19L TO 23L INOP. REPLACED BATTERY CHARGER AND BATTERY. OPS CHECKED, OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081015 NM 2008 10 15 2008UALA05987 1 20081004 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 STRINGER 18L STA 610, SEVERAL HOLES PREVIOUSLY FREEZE PLUGGED. ACCOMPLISHED MAJOR REPAIR AT GSO. 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 NM 2008 10 15 AALA200802207 1 20080826 A 2780 849704 PSEU BOEING 767 767323 1385205 NM LE FLAPS FAULTED A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 342AN 33081 LAX INFLIGHT T8/26AUG HNL TO DFW. CREW REPORTED FLAP ASYMMETRY EICAS MSG. ON FINAL APPROACH LIGHT EXTINGUISHED. LANDE D LAX WITHOUT INCIDENT. ON TAXI IN LIGHT ILLUMINATED AGAIN. FOUND PROXIMITY SWITCH ELECTRONIC UNIT (PSEU) FAULTING CAR DS 007, 010, AND 014 CAUSING FALSE ASYMMETRY INDICATION. REPLACED PSEU. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081015 SO 2008 10 15 AALA200802221 1 20080827 A 3350 SIGN PIPER PA22 PA22 7102202 SO EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 633A 2236 DFW EMERGENCY LIGHT PLACARD AT AFT LT HAND DOOR DAMAGED. REPLACED PLACARD FOR EMERGENCY LIGHT AT AFT LT HAND DOOR. SYS TEM GROUND CHECKED NORMAL OPS. 1 H 7 1 3O 1A6 20081015 NM 2008 10 15 AALA200802220 1 20080827 A 3350 GE767 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 190AA 32384 LAX EXTERIOR EMERGENCY LIGHT AT RT NR 3 DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RT NR 3 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081015 NM 2008 10 15 2008UALA06002 1 20081005 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 386UA 24661 DOOR 1R CUTOUT HAS A 2 INCH CRACK THRU FASTENER AT LOWER AFT CORNER. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A16WE E21EU 20081015 NM 2008 10 15 2008UALA06003 1 20081005 A 3350 GUARD BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LIGHT SWITCH OUT OF ADJUST A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHTS EICAS PROG TEXT: - ITEM ROLLED FORWARD. ADJUSTED GUARD ON EMERGENCY LIGHT SWITCH AT DOOR 1L. LIGHTS OPERATE NORMAL AND NO MESSAGE. 2 L 7 4 4F 4 F RT A20WE E24NE 20081015 NM 2008 10 15 2008UALA06004 1 20081005 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN TORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 662UA 27159 EEL STRIP TORN LEFT SIDE FIRST ROW OF BUSINESS CLASS. REPLACED 18 FT SECTION FROM ROW 1 TO ROW 8. 2 L 7 2 4F 4 F RT A1NM E24NE 20081015 EU 2008 10 15 2008UALA06007 1 20081006 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 413UA 470 EMERGENCY LIGHTS INOP ROWS 24, 25, 26. REPAIRED WIRING AT SEATS AND RELAMPED. CHECKS OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081015 NM 2008 10 15 2008UALA06010 1 20081005 A 7160 NOSE COWL BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE NR 2 ENGINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 664UA 29236 NR 2 ENG NOSE COWL DAMAGED BY RAMP LD-2 CONTAINER. REPLACED NOSE COWL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081015 NE 2008 10 15 COMA0870026 2 20080927 A 7200 ENGINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE NR 1 VIBRATION A COMA E ENGINE SHUTDOWN E VIBRATION/BUFFET CL CLIMB 1 SO 27 374CA 10090 34019 FLIGHT NR 6421 DURING CLIMBOUT FROM CVG NR 1 ENGINE N1 VIB INCREASED TO 1.8 YELLOW, IN CRUISE VIB WENT TO 2.4 YELLOW. S HUT DOWN ENGINE, RESTARTED ENGINE AND VIB WENT AWAY. EMERGENCY DECLARED. A/C CONTINUED TO MSP AND LANDED SAFELY. INSP ECTED NR 1 ENGINE FAN BLADES, NO DEFECTS NOTED. PERFORMED GROUND RUNS WITH NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A21EA E00063EN 20081015 WP 2008 10 15 AALA200802214 1 20080827 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9302B 49528 SEA EMERGENCY LIGHT AT SEAT 10D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081015 SO 2008 10 15 C2XA08TY110 1 20080924 A 2910 HYDRAULIC SYSTEM EMB 145 EMB145LR 3260212 SO A-SYSTEM LOW A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 27 11539 16726 145536 ACFT DIVERTED BACK TO BNA FROM BNA BECAUSE OF A SYSTEM 1 HYD LOW QUANTITY. MX SERVICED THE HYD SYSTEMS AND OPS CHECKS GO OD IAW AMM 12-13-01. ACFT RELEASED BACK TO SERVICE. 2 L 7 2 4T RT T00011AT 20081015 SO 2008 10 15 C2XA08IA213 1 20080923 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14952 145067 IAH FLIGHT 2026. DURING PREFLIGHT INSPECTION THE CREW REPORTED AN ELECTRICAL BURNING ODOR IN THE FORWARD AREA OF THE CA BIN. MX INSPECTED THE ACFT WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081015 SO 2008 10 15 C2XA08TY108 1 20080924 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BLOWN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14952 24378 145067 ACFT WAS IN FOR A SERVICE ROUTINE AND MX FOUND THE LT OVERWING EMERGENCY EXIT MARKER INOP. MX R&R THE EMERGENCY LIGHT I NVERTER AT THE NR 4 POSITION. IAW EMB 145 AMM 33-50-11. OPS CHECK GOOD AND WAS RELEASED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081015 SO 2008 10 15 C2XA08SH122 1 20080925 A 5320 14521718005 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12160 145799 SHV DURING C CHECK THE RT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 23. MX PERFORMED A DOUBLER REPAIR IAW CONTINENTA L EXPRESS EC5320-01228. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081015 SO 2008 10 15 C2XA08SH121 1 20080925 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12160 145799 SHV DURING C CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MX R&R THE AFFECTED BEAM IAW EMB 145XR S RM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081015 EU 2008 10 15 2008UALA06012 1 20081007 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN SYSTEM LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 440UA 702 GREEN HYD SYSTEM PROBLEM. RTFL. GREEN HYD SYS. [PITCH JACK PRESSURE LINE] HAS A .5 INCH CRACK IN LINE, BELOW TABALIZER BOX LT SIDE OF ACFT. FABRICATED NEW SECTION OF LINE. INSTALLED WITH FITTING. LEAK CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20081015 NM 2008 10 15 2008UALA06013 1 20081007 A 2421 745329F IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 647UA 25284 LOST LEFT GEN DUE TO LEFT DRIVE LIGHT. REPLACED LEFT IDG. RAN ENGINE FOR 5 MIN. IDG OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081015 SO 2008 10 15 C2XA08ON177 1 20080829 A 3150 WARNING LIGHT EMB 145 EMB145LR 3260212 SO THRUST REVERSER FALSE ACTIVATION A C2XA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 27 13553 145585 FLIGHT CREW REPORTED ENG 1 T/R DISAGREE ON TAKEOFF ROLL TWICE AND ON THE SECOND ATTEMPT, MX PERSONNEL RESET CYCLED T/R. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081015 NM 2008 10 15 2008UALA06022 1 20081006 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 MAIN CABIN FWD OF L-2 DOOR, STRINGER WEB CRACKED AT BS 675 AND STR 21L. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACE D WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 20081014 EU 2008 10 14 08FDEA04110 1 20080929 A 5321 A5327608400000 FLOOR PANEL AIRBUS 310 A310222 3930315 EU CABIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 MAIN CABIN FLOOR PANEL 242 YG IS CRACKED. FABRICATED A NEW FLOOR PANEL 242 YG IAW FEDEX DWG SRZ 25-005; REV G. 2 L 7 2 4F RT A35EU 20081014 EU 2008 10 14 08FDEA04106 1 20080929 A 5321 SRZ25005242QJ FLOOR PANEL AIRBUS 310 A310222 3930315 EU CABIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 MAIN CABIN FLOOR PANEL 242 QJ IS CRACKED. FABRICATED A NEW FLOOR PANEL 242 QJ IAW FEDEX DWG SRZ 25-005; REV G. 2 L 7 2 4F RT A35EU 20081014 EU 2008 10 14 08FDEA04108 1 20080929 A 5321 SRZ25008252UH FLOOR PANEL AIRBUS 310 A310222 3930315 EU CABIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 MAIN CABIN FLOOR PANEL 252 VJ IS CRACKED. FABRICATED A NEW FLOOR PANEL 252 VJ IAW FEDEX DWG SRZ 25-005; REV G. 2 L 7 2 4F RT A35EU 20081014 WP 2008 10 14 08FDEA04143 1 20080930 A 5720 ARB24077 CHANNEL DOUG MD10 MD1010F 3022112 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING UPPER L/E PANEL 517 CT HAS A CRACKED CHANNEL. REMOVED CRACKED CHANNEL IAW DC/MD-10 SRM 51-35-01; VOL II. MA TERIAL ID 7075-0, 0.063; PO 629531.1 & FABRICATED IAW DAC DWG ARB 2407; REV G. ALODINED & PRIMED IAW DC/MD-10 SRM 51-21 -01; VOL II; PG 21 - 24. INSTALLED IAW DC/MD-10 SRM 51-35-01 VOL II. 2 L 7 3 4F RT A22WE 20081014 2008 10 14 DL76L081229 4 20080925 A 3460 DISPLAY BOEING 767 767332 1382001 NM COCKPIT FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 191DN 28448 RT FMC CDU FAILED ON TAXI. REPLACED F/OS CDU PER MM. OPS NORMAL. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO E TOPS 2 L 7 2 4F RT A1NM 20081014 EA 2008 10 14 SWIA200820119 1 20080930 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCHARGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 963SW 7865 FLT 6612 - EMERGENCY EXIT ROW FLOOR LIGHTS INOP. REPLACED BATTERY PACK NR 3 INVERTER. 2 L 7 2 4F RT A21EA 20081014 EA 2008 10 14 SWIA200820124 1 20081003 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 810SK 15093 FLT 3968 - AFT CEILING EMERGENCY FLOODLIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081014 NM 2008 10 14 SWAA085438 1 20081005 A 5315 BAC1509 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOORBEAM CORRDED AT BS 767 + 5, RBL 7.5. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085399 1 20081005 A 5340 69353501 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 16R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081014 2008 10 14 SWAA085401 4 20081005 A 2565 416A2100 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 FOUND L1 EMERGENCY EXIT DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085402 1 20081006 A 5311 6558280 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 FOUND SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 CALA0800957 1 20081007 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 FUSELAGE STATION 787 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. CUT OUT DAMAGE AT FUSELAGE STATION 787 BETWEEN S8L AND S9L, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081014 EU 2008 10 14 08FDEA04138 1 20080930 A 5310 A5398126020600 DOOR FRAME AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 426FE 245 LEFT AFT PAX DOOR CUTOUT LOWER AFT DOOR STOP FITTING HAS CORROSION UNDER IT. REMOVED AND REPLACED THE LT AFT PAX DOOR C UTOUT AFT FRAME IAW SRM 51-40-21. PREPPED AND PAINTED IAW AMM 51-75-10-8, PERFORMED DOOR STOP ADJUSTMENT CHECK IAW AMM 52-10-11-5 CHECKED GOOD. 2 L 7 2 4F RT A35EU 20081014 WP 2008 10 14 08FDEA04139 1 20080930 A 5713 ARB12909 FRAME DOUG MD10 MD1010F 3022112 WP LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 LEFT WING FIXED L/E COMP FORMER IS CRACKED ADJACENT TO THE FRONT SPAR UPPER T-CAP AT XOS 751 APPROX MATERIAL ID FOR THE REPAIR ANGLE IS 0.063, 17-7 PF CRES ANNEALED REF DC/MD-10 SRM 57-20-00. FORMED THE REPAIR ANGLE REF DC/MD-10 SRM 51-10- 00; VOL II. RECEIVED ANGLE FROM HEAT TREAT; LOCATED & DRILLED REF DC/MD-10 SRM 51-21-01; VOL II. INSTALLED REPAIR ANGL E REF DC/MD-10 SRM 57-20-00; VOL I. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 08FDEA04152 1 20080930 A 5310 BEAM DOUG MD11 MD11F 3023600 NM DOOR FRAME CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 MAIN DECK CARGO - DOOR LEFT 3 NR 5 BEAM FORWARD STOP FITTING AREA FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31- 01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 08FDEA04160 1 20081001 A 5753 ARC198414 HINGE FITTING DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 RIGHT WING OUTBOARD FLAP INBOARD HINGE AFT FITTING AFT BORE HOLE FOUND WITH PITTING CORROSION. FITTING REPAIRED AS PER E.A. NO. 1-5750-122572. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081014 NM 2008 10 14 08FDEA04163 1 20081001 A 5230 65571411 SKIN BOEING 727 727227 1384078 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 FWD CARGO DOOR (PIT DOOR), EXTERNAL SKIN CRACKED, 30 INCHES AFT OF LEADING EDGE, 3 INCHES ABOVE LOWER EDGE CUTOUT DAMAGE , PERFORMED HFEC INSP OF CUTOUT. NO DEFECTS NOTED. PERFORMED INSURANCE CUT. FABRICATED DOUBLER AND TREATED AND PRIMED REPAIR PARTS AND REPAIR AREA. INSTALLED AND SEALED DOUBLER. REPAIR IS A CAT "B" REPAIR DUE TO FASTENERS IN CRITICAL R OW ON INTERNAL STRUCTURE. REF SRM 52-00-3 FIG 3. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081014 NM 2008 10 14 08FDEA04169 1 20081002 A 5753 ARC0503506 HINGE FITTING DOUG MD11 MD11F 3023600 NM T/E FLAP SCRATCHED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 RIGHT WING OUTBOARD FLAP INBOARD HINGE AFT MOUNTING LOWER INBOARD MOUNTING BORE HOLE INNER FACE FOUND WITH SCRATCH MARKS . SCRATCH MARKS AT RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE AFT MOUNTING LOWER INBOARD MOUNTING BORE HOLE REMOVED AN D FOUND WITHIN LIMIT AS PER CMM 57-44-08. BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-08. REPAIR CLASSIFIED AS MIN OR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081014 EU 2008 10 14 08FDEA04175 1 20081002 A 5311 A57112119200 FITTING AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 426FE 245 CENTER FUSELAGE ZONE 20 - REINFORCE THE UPPER FRAME JUNCTION AT FR 46 LT FASTENERS HOLES CRACKED ON FRAME FOOT FITTING. REMOVED FRAME FOOT IAW SRM 51-40-21. RE-INSTALLED FRAME FOOT PER EA 6-5310-123911 & SRM 51-40-21, INSTALLED BUSHINGS P ER EA 6-5310-123911. 2 L 7 2 4F RT A35EU 20081014 EU 2008 10 14 08FDEA04111 1 20080929 A 5321 SRZ25005242VJ FLOOR PANEL AIRBUS 310 A310 EU CABIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 MAIN CABIN FLOOR PANEL 242 VJ IS CRACKED. FABRICATED A NEW FLOORBOARD 242 VJ IAW FEDEX DWG SRZ 25-005; REV G. 2 L 7 2 4F RT A35EU 20081014 SO 2008 10 14 RAIA2008101300002 1 20081012 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 849HK 145002 DURING PRE FLIGHT INSPECTION, THE EMERGENCY LIGHT AT THE FLIGHT DECK STEP WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESE CURED THE CONNECTION TO THE EMERGENCY LIGHT. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081014 EA 2008 10 14 SWIA200820122 1 20081003 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 936SW 7726 FLT 6663 - FORWARD AND AFT CEILING EMERGENCY FLOOD LIGHTS INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081014 SO 2008 10 14 SWIA200820123 1 20081004 A 3233 1959500007 ACTUATOR EMB 120 EMB120ER 3260203 SO MLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 560SW 120334 ON CLIMB-OUT, LEFT MAIN GEAR WOULD NOT RETRACT. REPLACED LEFT GEAR ACTUATOR, PN 19595-000-07. 2 L 7 2 4T RT A31SO 20081014 NM 2008 10 14 CALA0800962 1 20081008 A 5320 65C333701 FLOOR SUPPORT BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59630 27534 AFT ENTRY STATION 947 - 967 FLOOR SUPPORT AT LBL 25 CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085444 1 20081007 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 468WN 33858 FOUND FWD FLOOR TRACK LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085442 1 20081007 A 3350 417A5700 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 467WN 33830 DURING SCHEDULED MV2 CHECK, FOUND FWD PROXIMITY EMERGENCY FLOOR LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081014 SO 2008 10 14 SWIA200820125 1 20080930 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 270YV 120270 FLT 5708 - EMERGENCY LIGHT OUT AT ROW 5. RELAMPED. 2 L 7 2 4T RT A31SO 20081014 NM 2008 10 14 SWAA085437 1 20081005 A 5315 BAC1509 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 767 + 5, RBL 3. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085436 1 20081007 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 AALA200802205 1 20080826 A 3350 7024092008 SIGN BOEING 767 767323 1385205 NM EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 384AA 26996 JFK EMERGENCY EXIT SIGN AT RT HAND LOWER FORWARD OVERWING EXIT DAMAGED. REPLACED EXIT SIGN ASSEMBLY FOR EMERGENCY LIGHT AT RT HAND LOWER FORWARD OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081015 EA 2008 10 15 RAIA00809006 2 20080907 A 7261 O-RING EMB 145 EMB145LR 3260212 SO RROYCE AE3007 AE3007A12 54164 EA NR 2 ENGINE DEFECTIVE A RAIA O OTHER K FLUID LOSS CL CLIMB 1 CE 03 810HK 145231 DURING CLIMB, CREW SHUTDOWN THE NR 2 ENGINE IN FLIGHT DUE TO LOW OIL AND LOW OIL AND LOW OIL PRESSURE. MAINTENANCE INSP ECTED THE ENGINE AND FOUND A BAD O-RING AT THE NR4 GENERATOR. THE O-RING WAS REPLACED AND LEAK CHECK OF THE NR 2 ENGINE DID NOT PRODUCE ANY OTHER LEAKS. (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081015 EU 2008 10 15 QML2008F00011 1 20080918 A 7810 EXHAUST DUCT PILATS PC12 PC12 7090550 EU NACELLE FOD E QMLA C ABORTED TAKEOFF W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 03 912NM 169 KFMN TO KABQ. AFTER ENGINE STARTUP AND ENVIRONMENTAL SYSTEM TURNED ON, THE PILOT GRADUALLY BECAME AWARE OF A BURNING OD OR IN THE COCKPIT & CABIN. UPON TAXI OUT TO RUNWAY 25 IN KFMN, PILOT SAW BURNING EMBERS/SPARKS COMING FROM PROP AREA AN D ENGINE EXHAUST AREA BLOWING BACK AGAINST THE WINDSHIELD. PILOT INFORMED TOWER THAT HE WAS ABORTING TAKEOFF AND RETURN ING TO HANGAR. UPON RETURN AND ENGINE SHUTDOWN, AFTER MECH WAS INFORMED OF THE PROBLEM, FOUND BURNED RAG NEXT TO THE E XHAUST AREA. RAG REMOVED, NACELLE REASSEMBLED, FLIGHT TO KABQ RESUMED WITHOUT INCIDENT. 1 L 7 1 3T RT A78EU 20081015 EU 2008 10 15 AALA200802190 1 20080825 A 3260 SWITCH AIRBUS 300 A300B4605R 3930308 EU NLG DOOR FAULTY A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 14077 612 MIA INFLIGHT T933/25AUG. CREW REPORTED NOSE GEAR UNSAFE INDICATIONS ON BOTH SYSTEMS AFTER NOSE GEAR RETRACTION. RETURN ED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED LT AND RT HAND SYSTEM NOSE LANDING GEAR DOOR SWITCHES. SYSTEM GROUND C HECKED NORMAL OPS. 2 L 7 2 4F RT A35EU 20081015 SO 2008 10 15 RAIA00809011 1 20080909 A 2697 CONNECTOR EMB 145 EMB145 3260210 SO RT BURST SWITCH LOOSE A RAIA O OTHER J WARNING INDICATION CL CLIMB 1 CE 03 821HK 145068 DRUING CLIMB, CREW RECEIVED A WING ANTI-ICE FAIL MESSAGE ON THE EICAS. MAINT INSPECTED AND FOUND THE NR 2 WING ANTI-ICE BURST PRESSURE SWITCH CONNECTOR PLUG LOOSE. TIGHTENED THE CONNECTOR AND SYSTEM OPS CHECKED GOOD. (K) 2 L 7 2 4F RT T00011AT 20081015 SO 2008 10 15 C2XA08CL109 1 20080924 A 3350 3025103 LIGHT EMB 145 EMB145LR 3260212 SO LT WING INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13970 145146 DURING ROUTINE MX THE LT WING AFT EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE LIGHT A SSEMBLY. OPS CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20081015 NM 2008 10 15 2008UALA05776 1 20080917 A 2700 BYPASS VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WING LEAKING A UALA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 29 550UA 25398 FOUND LEADING EDGE BYPASS VALVE (V10059) LEAKING, CRACKED CASTING. CRACK (FATIGUE) IN CASTING. REPLACED LEADING EDGE B YPASS VALVE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 SW 2008 10 15 QML2008F00010 1 20080919 A 6240 B47131 CHIP DETECTOR BELL 407 407 1182206 SW TRANSMISSION SHORTED E QMLA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 03 247SM 53176 WHILE ENROUTE TO MEDICAL FACILITY, TRANSMISSION CHIPS LIGHT ILLUMINATED AND EMERGENCY PROCEDURE WAS EXECUTED TO AN OPEN FIELD. ALL TRANSMISSION RELATED CHIP PLUGS WERE INSPECTED AND APPEARED TO BE CLEAN. PILOT RAN ACFT UP AND COULD NOT GE T THE SAME FAULT TO CLEAR. TROUBLESHOOTING WITH MECHANIC FOUND THE FREEWHEELING UNIT CHIP PLUG TO BE THE CULPRIT AND NO PART READILY AVAILABLE TO REPLACE IT. ACFT SECURED AT LOCATION UNTIL PARTS ARRIVE. 1 G 7 1 3U O H2SW 20081015 2008 10 15 2008UALA05870 4 20080923 A 2565 D31039202U1 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 586UA 26710 DOOR 2L SLIDE DISLODGED FROM MOUNT. REINSTALLED DOOR 2L SLIDE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 NM 2008 10 15 2008UALA05979 1 20081004 A 3350 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 772UA 26930 THE 1E SIDE WALL EMERGENCY LIGHT FELL OFF. REPLACED LAMP. TESTED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081015 NM 2008 10 15 2008UALA05980 1 20081003 A 3350 767D71702001D717 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 220UA 30223 LIGHT EXTERIOR EMERGENCY DOOR 3L IS INOPERATIVE. REPLACED EXTERIOR LAMP, POWER SUPPLY AND BATTERY PACK. OP CHECKED NOR MAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081015 NM 2008 10 15 2008UALA05981 1 20081003 A 2621 EXTINGUISHER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE AFT CARGO BAY DEFECTIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 507UA 24743 AFT PIT ENG FIRE BOTTLE NR 1 PRESSURE SWITCH IS BAD. NR 1 ENGINE FIRE EXTINGUISHER REPLACED. OP CHECK ACCOMPLISHED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 NM 2008 10 15 2008UALA05982 1 20081003 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 DENT IN CROWN SKIN STA 900, STR 2L TO 3L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER . 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 NM 2008 10 15 2008UALA05983 1 20081003 A 5310 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 507UA 24743 FWD NOSE COMPARTMENT DOOR FWD CUTOUT FRAME IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED J-ANGLE REPAIR. ADJUSTME NT CHECKED FWD LATCH FITTING. SENSOR ADJUSTED & OP CHECKED DOOR SENSOR SYSTEM. 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 NM 2008 10 15 2008UALA05988 1 20081004 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 PREVIOUS REPAIR STA 610, STR 17L, EXT FUSELAGE HAS DENT. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN AND INSTALLE D DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 NM 2008 10 15 2008UALA05989 1 20081004 A 5730 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT WING CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 RIGHT WING, UPPER SKIN AT WBL 95, STA 970 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN AND INSTALLED D OUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081001 NM 2008 10 1 UPS08653345 1 20080913 A 5315 STIFFENER BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 332UP 32843 INSPECTION TYPE:C MEC CABIN FLOORBEAM STA 246 LBL 55 VERTICAL STIFFENER FOUND CRACK (CRACK LENGTH 1 INCH). VERT STIFFEN ER REPLACED AS PER SRM 53-10-51-2R FIG 201 REPAIR 3 UPS MPI P19867 RAISED FOR REPEAT DVI AT 3000 CYC OR 24 MONTHS, WHICH EVER COMES FIRST. 2 L 7 2 4F RT A1NM 20081002 NM 2008 10 2 ASAA0843465 1 20080819 A 5755 654645170A SKIN BOEING 737 737490 1384715 NM NR 2 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 791AS 28886 UPPER SURFACE OF NR 2 SPOILER DENTED. PREPPED AREA, FABRICATED DOUBLER AND BONDED REPAIR IAW SRM 51-70-10. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800848 1 20080904 A 5310 65C80735183 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 FORWARD CARGO DOOR FRAME CRACKED. REMOVED CRACKED DOOR FRAME AND REPLACED SAME WITH NEW DOOR FRAME IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 2008UALA04378 1 20080821 A 5240 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 R-2 DOOR REQUIRES DOUBLER AT UPPER HINGE ARM CUTOUT. *S/D* MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 2008UALA04379 1 20080821 A 5210 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 L-2 DOOR REQUIRES DOUBLER AT UPPER HINGE ARM CUTOUT. *S/D* MAJOR REPAIR ACCOMPLISHED: INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 2008UALA04381 1 20080821 A 5730 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT WING DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 FOUND LEFT WING AFT LOWER FIXED SKIN PANEL DAMAGED ON ARRIVAL. PANEL IS LOCATED JUST AFT OF LEFT GEAR AND FORWARD OF TR AILING EDGE FLAPS. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SKIN AND CORE. INSTALLED A LAY-UP REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 2008UALA05498 1 20080826 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE SEAT 24H MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 SEAT 24H EMERGENCY LIGHT MISSING. REPLACED EMERGENCY LIGHT AT SEAT 24H. 2 L 7 2 4F 4 F RT A1NM E24NE 20080930 NM 2008 9 30 2008UALA05422 1 20080823 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 117UA 28810 SEAT 55HJK EMERGENCY LIGHT IS INOP. RELAMPED, CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20080930 EU 2008 9 30 2008UALA04252 1 20080811 A 3510 MXP401600U OXYGEN SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CREW LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 430UA 568 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. CREW COMMENTS: OXYGEN NEEDS SERVICING. LEAK CHECKED WITH NO LEAKS NOTED. SERVICED TO FULL. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 NM 2008 9 30 2008UALA04249 1 20080811 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 814UA 862 FLOORBEAM 190 CORRODED (MARKED). REMOVED BEAM. INSTALLED NEW FLOORBEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 WP 2008 9 30 UPS08853235 1 20080813 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 200-240 WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 SEAT TRACK WORN AT SEVERAL LOCATIONS BETWEEN STA 200 TO STA 240 LBL 45 IN MAIN CABIN. REPAIRED SEAT TRACK IAW SRM 53-02-3 AND SRM 51-03-0. 2 L 7 4 4F RT 4A25 20080930 WP 2008 9 30 UPS08853242 1 20080829 A 2910 SEAL DOUG DC8 DC873F 302199F WP HYD SYSTEM LEAKING A IPXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 801UP 46101 CREW EXPERIENCED SLOW LOSS OF HYDRAULIC FLUID DURING FLIGHT. COMPLETED LOSS OF HYDRAULIC FLUID CHECKLIST AND WERE ABLE TO STOP THE LOSS. CREW DECLARED AN EMERGENCY & CONTINUED TO SDF WHERE AIRCRAFT LANDED SAFELY. REPLACED HYD QTY TRANSMI TTER SEAL REF MM 29-30-01-2. LEAK CHECKS OK. 2 L 7 4 4F RT 4A25 20080930 EU 2008 9 30 2008UALA05444 1 20080824 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 451UA 865 FLOORBEAM 175 IS CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM 175. TRANSFERRED CABLE ATTACH BRACK ETS AND STARTED ASSEMBLY WITH BEAM 210. BEAM 175 AND 210 ARE TOGETHER AND NEED FWD END OF BEAM PUT INTO AC AND DRILL FW D ATTACH HOLES. PICKED UP REMAINING HOLES, STARTED INSTALL. AFT BOLTS REMAINING. INSTALLED AFT BUSHINGS AND BOLTS. I NSPECTED BEAM 210 AND BUSHINGS AND BOLTS FOR SAFETY AND SECURITY AND FOUND SECURE. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 EU 2008 9 30 2008UALA05446 1 20080824 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 451UA 865 FLOORBEAM 165 CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM 165. REMOVED ANGLES. TRANSFERRED BRACK ETS AND ATTACHED BEAM 165 AND 200 WITH SPLICE ANGLES WORKING ON BENCH. COMPLETED INSTALLATION. 2 L 7 2 4F 4 F RT A28NM E40NE 20080930 EU 2008 9 30 2008UALA05447 1 20080824 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 451UA 865 FLOORBEAM 200 IS CORRODED (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM 200. REMOVED ANGLES ATTACHED TO BEAM 165, DRILLED SPLICE ANGLES FOR BEAM 200 TO 205. COMPLETED INSTALLATION. 2 L 7 2 4F 4 F RT A28NM E40NE 20081001 NM 2008 10 1 SWAA085212 1 20080822 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED SPV CHECK, FOUND L1 ENTRY DOOR UPPER HINGE SKIN CRACKED AT FASTENER HOLES. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 08FDEA04101 1 20080929 A 5531 SPAR CAP DOUG MD11 MD11F 3023600 NM VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 606FE 48602 HFEC INSPECTION CARRIED OUT AND FOUND ONE CRACK ON LEFT SIDE RADIUS OF LOWER FORWARD SPAR CAP AT LOWER VERTICAL STABIL IZER. REPAIR CARRIED OUT AS PER SRM 55-20-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 2008UALA06024 1 20081006 A 5320 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 MAIN CABIN STA 1380-14--, STR 17R WEB CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED WEB, FABRICATED & INSTALLED A NEW W EB. 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 NM 2008 10 15 2008UALA06025 1 20081006 A 5320 CUSP WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 CUSP WEB, STA 1020-1025, LBL 75, WL 208 CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED WEB, FABRICATED & INSTALLED A -4 WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 2008 10 15 S8Y2008F00000 4 20080924 A 3457 430 ANTENNA CIRRUS SR SR22 2130001 GL CONT O550 IO550N 17042 SO GPS LOOSE E S8YA O OTHER O OTHER NR NOT REPORTED 1 EA 27 519SR 272 2072 689850 THE GPS ANTENNAS, NR 1 AND NR 2 ON THIS ACFT ARE HELD IN POSITION WITH DOUBLE SIDED TAPE. IN 272 HRS THEY HAVE COME LOO SE 3 TIMES. THE ANTENNAS SHOULD HAVE MOD TO PERMANENTLY MOUNT THEN ON THE AIRFRAME. 1 L 7 1 3O 3 O NT A00009CH E3SO 20081015 WP 2008 10 15 ESPADJ2088-1 2 20081004 A 7200 30701701 ENGINE LEAR 35 36A 5170603 CE GARRTT TFE731 TFE731* 01518 WP LEFT LACK OF LUBE E ESPA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 11 32PA 12754 79 25 P74132C DEPARTED CARTERSVILLE AIRPORT AND PASSING 2000FT MSL THE MASTER CAUTION AND OIL PRESSURE LIGHTS ILLUMINATED. THE CREW N OTED 0 OIL PRESSURE ON THE LEFT ENGINE AND RETURNED TO THE AIRPORT FOR AN UNEVENTFUL LANDING. GROUND CREW NOTED AN EXTE NSIVE OIL LEAK AND COULD HEAR A GRINDING NOISE COMING FROM THE ENGINE WHILE ATTEMPTING TO ROTATE IT BY HAND. THIS ENGIN E HAS 78.6 HOURS OPERATING TIME SINCE COMPLETION OF MAJOR PERIODIC INSECTION AND CORE REPAIR. ENGINE REMOVED AND RETURN ED TO OVERHAUL FACILITY. 2 L 7 2 4F 4 F A10CE E6WE 20081015 2008 10 15 22AA20080906 4 20080928 A 3441 INU DOUG DC10 DC1030 3023501 WP NR 1 MALFUNCTIONED A 22AA O OTHER O OTHER IN INSP/MAINT 1 SO 19 526MD 46998 INERTIAL NAVIGATION SYSTEM (INS) NR 1 PRE-LAND TEST (PLT) FM FLOW OFF, LIGHT ON. ENTERED ON DMI 22099 IN ACCORDANCE WIT H MEL 34-22, CATEGORY C. PLACARDS INSTALLED AS REQUIRED. 2 L 7 3 4F A22WE 20081015 SO 2008 10 15 GLBA200810032 1 20081003 A 5310 DOOR FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 71GL 120071 MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A CRACK WAS FOUND IN THE CARGO DOOR FRAME AT THE UPPER FORWARD CORN ER AT A LATERAL STOP APPROXIMATELY 1.10 INCH. MAINTENANCE REPAIRED THE CARGO DOOR AT THE LOWER AFT LATERAL STOP POSITIO N NR 1. APPROXIMATELY 8.5 INCH BY 7.5 INCH IAW EMB SRM 52-30-02. DOUBLER MADE OF 7475-T761, .063 INCH, SEALANT MIL-S-8 1733 TYPE IV, RIVETS MS20470AD4-X & MS20470AD5-X. INSTALLED NEW T-SECTION P/N 120-19391-601 WITH NEW HARDWARE HC22-5-X AND COLLARS P/N NC77-5. SEALED WITH, MIL-S-81733 TYP EIV. STOP DRILLED CRACK IAW EMB 120 SRM 51-10-03. 2 L 7 2 4T RT A31SO 20081015 CE 2008 10 15 MTNA100801 1 20081007 A 5755 2622187126221872 HINGE CESSNA 208 208B 2073701 CE SPOILER BINDING E MTNA K NONE O OTHER AP APPROACH 1 EA 68 820FE 10262 0111 AILERONS BINDING ON FINAL APPROACH AND AFTER LANDING. TROUBLESHOT THE AILERON AND SPOILER SYSTEM. FOUND BOTH SPOILER H INGES WORN AND BINDING, ALSO RIGHT AILERON INPUT ROD END CORRODED. REMOVED AND REPLACED BOTH SPOILERS, HINGES, HINGE PI NS AND AILERON INPUT ROD END IAW C-208 MAINTENANCE MANUAL CHAPTER 57-70-00. THE SYSTEM TRAVEL AND RIG CHECKED GOOD. 1 H 7 1 3T A37CE 20081015 NE 2008 10 15 Q2SA758003 2 20081009 A 7200 ENGINE BOEING 747 747281F 13848AB NM GE CF6 CF650E2 30018 NE NR 3 DAMAGED A Q2SA J A DUMP FUEL UNSCHED LANDING C R F.O.D. PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 63 758SA 23138 530210 DURING TAKEOFF AFTER V1 FROM HAAB, BIRD INGESTION INTO NR 3 ENGINE. AIR TURNBACK TO HAAB. FUEL DUMP OF 50,000 LBS. IN SPECTION AFTER LANDING CONFIRMED DAMAGE TO NR 3 ENGINE FAN BLADES, AS WELL AS EVIDENCE OF BIRD STRIKE ON NR 2 ENGINE. N R 1, 3, 4, 6, 11, 13 AND 15 MAIN WHEEL ASSEMBLIES THERMALLED. 2 L 7 4 4F 4 F RT A20WE E23EA 20081015 2008 10 15 ZZDA2008164 4 20081001 A 2565 D29982225 SLIDE BOEING 717 717200 1383700 NM R1 DOOR DEPLOYED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 952AT 55014 R-1 DOOR SLIDE DEPLOYED. REMOVED AND REPLACED R-1 EMERGENCY EVACUATION SLIDE IAW MM 25-61-03. OK FOR SERVICE. 2 L 7 2 4F TR A6WE 20081015 NM 2008 10 15 ASAA0853558 1 20081004 A 2160 3989083 MODULATING VALVE BOEING 737 737890 1384527 NM RT PACK FAILED A ASAA K NONE M OVER TEMP CR CRUISE 1 NM 02 557AS 8954 35176 IN FLIGHT RIGHT PACK TEMP EXCEEDED 80 CELSIUS WITH TEMP CONTROLLERS IN FULL COLD SUPPLY DUCT TEMP 40 CELSIUS CAB TEMP 32 CELSIUS. WORSE WITH TRIM AIR OFF. TURNED PACK OFF AND TEMPS DECREASED. PERFORMED BITE TEST OF BOTH ZONE TEMP CONTROL LERS. FOUND RT TEMP CONTROL VALVE FAILED. SWAP RT TEMP CONTROL VALVE WITH AFT TRIM AIR VALVE. PERFORMED ZONE TEMP CON TROL BITE AND CHECKS GOOD. SYS OPS CHECKED NORMAL. REF FIM 21 61 00 AMM 21 51 10 AND AMM 21 61 21. C N 1003011 VERIFIE D RT OPS CHECKED OK. PERFORMED BITE CHECK ON BOTH TEMP CONTROLLERS RT AFT CABIN ZONE TRIM AIR MOD VALVE FAULT LIGHT ILL UMINATED. REMOVED AND REPLACED RT AFT CABIN ZONE TRIM AIR MOD VALVE, OPS LEAK CHECK GOOD. GROUND VERIFICATION SUCCESSF 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 ZZDA2008165 1 20081006 A 3350 8039491 BATTERY BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 986AT 55089 SEAT ROWS 25 THUR 31 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY SUPPLY ASSY & BATTERY OP'S CHECK GOOD REF MM 3 3-51. 2 L 7 2 4F TR A6WE 20081015 NM 2008 10 15 SWAA085415 1 20081007 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR SKIN CUTOUT CRACKED AT LOWER HINGE. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 SWAA085416 1 20081007 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 218WN 32489 DURING SCHEDULED HC1 CHECK, FOUND EMERGENCY EXIT LIGHT COVER CRACKED BETWEEN 1ABC TO 18ABC. REPLACED COVERS PER MM. 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 SWAA085417 1 20081007 A 3350 300432 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 283WN 36610 DURING SCHEDULED MV2 CHECK, FOUND L1 EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 SWAA085422 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085194 1 20080925 A 5753 6546435 SKIN BOEING 737 7377H4 1384404 NM T/E FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT LT AFT INBOARD FLAP. REPAIRED PER SWA EA. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 UPS08M53405 1 20080917 A 5321 WSP0785Y501 FLOOR PANEL DOUG MD11 MD11F 3023600 NM CARGO BAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 282UP 48452 INSPECTION TYPE:2C RCB FLOOR PANEL 8 HAS CORROSION ON UPPER SURFACE. PROCURED NEW FLOOR PANEL. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 SWAA085217 1 20080924 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 263WN 32520 FOUND FWD EMERGENCY EXIT LIGHT MISSING LENS. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 ASAA0853533 1 20080926 A 2163 213A64041 FILTER BOEING 737 737890 1384527 NM CABIN TEMP CLOGGED A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 570AS 35185 CABIN TEMPERATURE CONTROL WAS VERY ERRATIC IN AUTO CABIN TEMP WOULD RANGE FROM VERY HOT TO VERY COLD WITH EXTREMELY SMAL L MOVEMENTS OF TEMP CONTROLS. ALSO LARGE DIFFERENCES (TEMP) BETWEEN FWD & AFT SELECTIONS OF MAIN CABIN. NO PERMANENT F RC FOUND (FAULT REPORTING CODE) C W FIM TASK 21 61 00 PG501 NO FAULTS LOGGED OPS NORMAL. FOUND FLT DECK SENSE FILTER PL UGGED CLEANED. SEAMC ETOPS ADVISED. NOTE: GRND VERIFICATION TEST GOOD. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085184 1 20080919 A 5511 182A1500 SPAR BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 437WN 29832 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZ STAB LOWER IN SPAR CRACKED AT STA 129.50 36 AND STA 129.50 44. REPAIRED SPAR PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085169 1 20080918 A 5330 6545768 SKIN BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CORRODED AT STA 380 BETWEEN STR 27L & STR 28L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085168 1 20080903 A 5314 6545866 KEELBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND CORRODED KEEL BEAM AT BS 703, LBL 6.5. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085179 1 20080918 A 3397 487191 CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 295WN 32541 DURING SCHEDULED MV1 CHECK, FOUND EMERGENGY EXIT LIGHTS INOP FROM ROW 6 THROUGH ROW 10. RESECURED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085178 1 20080916 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER 26R CORRODED AT BS 840. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 2008UALA05767 1 20080917 A 3350 78671 LAMP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 105UA 26473 SEAT 4F FWD EMERGENCY LIGHT IS INOP. LAMP FOUND DEFECTIVE. REPLACED LAMP. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081001 EU 2008 10 1 08FDEA03424 1 20080814 A 5320 A53974341200 FLOOR SUPPORT AIRBUS 300 A300B4622R 3930312 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 744FD 664 FOUND CORRODED FLOOR SUPPORT AT C 63-64, Y800. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10. 2 L 7 2 4F RT A35EU 20081001 NM 2008 10 1 08FDEA03425 1 20080814 A 5347 SEAT TRACK BOEING 757 757236 1384971 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 SEAT TRACK LBL 45.50 HAS CORROSION ON AFT SIDE OF BS 1120 FLOORBEAM. REMOVED CORROSION FROM SEAT TRACK IAW SRM 53-00-52 . ORIGINAL MATERIAL THICKNESS WAS .084 INCH, AFTER REWORK .044 INCH. FOUND TO BE OUT OF LIMITS PER SRM 53-00-52. REMO VED SEAT TRACK, FABRICATED REPLACEMENT SEAT TRACK PER MAE TRAVELER NRT8/748466 AND SRM 51-40-02. INSTALLED REPLACEMENT SEAT TRACK PER SRM 53-00-52 AND 51-40-02. THIS IS CLASSIFIED AS A MAJOR REPAIR, CATEGORY A REPAIR. NO FOLLOW UP TRACKI NG IS REQUIRED. 2 L 7 2 4F RT A2NM 20081001 SO 2008 10 1 SWIA200820029 1 20080616 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 296SW 120325 LT FLOORBOARD PROP ANGLE CRACKED UNDER JUMPSEAT FLOORBOARD. C-CHECK, REPLACED LT FLOORBOARD PROP ANGLE. 2 L 7 2 4T RT A31SO 20081001 NM 2008 10 1 08FDEA03202 1 20080731 A 5313 ACA37961 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 579FE 48470 01 EACH FASTENER HOLE FOUND CRACK AT 5 AND 9 O'CLOCK POSITIONS (APPROXIMATELY 1/8 INCH LENGTH) AT NOSE LANDING GEAR LEFT SIDE TRUNNION FITTING LOWER LONGERON. CRACK LOWER LONGERON AT NOSE LANDING GEAR LEFT SIDE TRUNNION FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081001 WP 2008 10 1 08FDEA04118 1 20080929 A 5340 RAM142951 ATTACH ANGLE DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 FORWARD LOWER CARGO ROLLER TRAY HAS CORROSION ON THE ATTACH ANGLE LOWER SURFACE AT FS 879, RBL 5 INCH - 8 INCH. COMPLIE D WITH THE REPAIR TO THE ROLLER TRAY ATTACH ANGLE AT STA 879; RBL 8; FWD CARGO COMPARTMENT IAW DC/MD-10 SRM 53-00-01; VOL I; FIG 7. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 CALA0800910 1 20080917 A 5315 141T5107 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69154 30433 CABIN STATION 303 LBL 15 TO LBL 55 FLOOR SUPPORT FOUND CORROSION. CABIN STATION 303 LBL 38 TO LBL 55 CORROSION REMOVED TREATMENT PER SRM 51-10-02 AND PROTECTED PER SRM 51-20-01 WITHIN SRM 53-00-51 ALLOWABLE DMG 1 LIMIT AND LBL 8 TO LBL 38" FLOORBEAM REPAIRED PER SRM 53-00-01 REPAIR 1 FIG 201. 2 L 7 2 4F RT A1NM 20081015 NM 2008 10 15 SWAA085423 1 20081007 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 927, BETWEEN STR 27L TO 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 SWAA085424 1 20081007 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 907, BETWEEN STR 27L TO 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 SWAA085425 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 927, STR 23R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085396 1 20081004 A 3233 654482515 ACTUATOR BOEING 737 7373H4 1384600 NM RT MLG FAULTY A SWAA K NONE J WARNING INDICATION AP APPROACH 1 SW 29 346SW 24153 FOUND RT MLG INDICATION UNSAFE DURING NORMAL EXTENSION RECYCLED ONCE, NO CHANCE. MANUALLY EXTENDED RT MLG AND GOT SAFE INDICATION. REPLACED UPLOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 2008F00022 1 20081012 A 2612 FIRE WARNING BOEING 747 7472B4B 138481B NM PWA JT9 JT9D7J 52054 NE NR 3 ENGINE ACTIVATED A KCSA E ENGINE SHUTDOWN A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 GL 23 710CK 21097 685873 RECEIVED T FIRE WARNING ON CLIMBOUT AT 3500 FT ON NR 3 ENG. FILTER BYPASS LIGHT CAME ON, OIL PRESS WENT TO '0', OIL QTY WENT TO '0', OIL TEMP 160, N1, N2 NORMAL. FIRE HANDLE PULLED, BOTTLES WOULD NOT DISCHARGE (BOTH) HELD OVER 1 MIN. 2 L 7 4 4F 4 F RT A20WE E20EA 20081014 NM 2008 10 14 CALA0800961 1 20081007 A 3350 D71701100 BATTERY PACK BOEING 737 737824 13844BZ NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 33286 31600 BATTERY PACK AT SEAT ROWS 12ABC, 20ABC AND LEFT AFT GALLEY FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK AT SEAT ROWS 12ABC, 20ABC AND LEFT AFT GALLEY PER AMM 33-51-06. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 UPS08B53470 1 20080108 A 5320 65B09631612 TENSION TIE BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 579UP 26062 INSPECTION TYPE:BCF STA 1180 TENSION TIE RT AFT CHANNEL 6EA FASTENER HOLE CRACKED MORE OR THAN ABOUT 0.030". REPLACED C RACKED TENSION TIE AS PER DWG 65B09631 SH14 & SRM 51-40-02. 2 L 7 4 4F RT A20WE 20081014 EA 2008 10 14 SWIA200820126 1 20081002 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 472CA 2937 649 7667 FLT 2642 - ON GEAR EXTENSON, GOT TRIPLE CHIME "GEAR DISAGREE" FOR THE NOSE GEAR. NLG EXTENDED AFTER 30 SECONDS. REPLAC ED NLG SELECTOR VALVE, PN 750006000 SN ON 1032T SN OFF 1570. 2 L 7 2 4F RT A21EA 20081014 EA 2008 10 14 SWIA200820127 1 20081002 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 494CA 7765 FLT 2559 - AFT EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081014 SO 2008 10 14 SWIA200820128 1 20080930 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 581SW 120349 FLT 5702 - FORWARD TWO RED EMERGENCY LIGHTS MISSING. REPLACED TWO RED TRACK LIGHT, EMERGENCY LIGHT ASSEMBLIES. 2 L 7 2 4T RT A31SO 20081014 EA 2008 10 14 SWIA200820104 1 20080927 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 932SW 7714 FLT 6125 - FIRST CEILING EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081014 EA 2008 10 14 SWIA200820105 1 20080926 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DIRTY A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 934SW 7722 FLT 6456 - RIGHT WING EXIT EMERGENCY SIGN INOP. CLEANED ELECTRICAL CONNECTION ON LIGHTING STRIP. 2 L 7 2 4F RT A21EA 20081015 CE 2008 10 15 GUUA10040801 1 20081004 A 3230 571302 MOTOR BEECH 1900 1900D 1154162 CE LANDING GEAR MALFUNCTIONED A GUUA K NONE O OTHER CL CLIMB 1 SO 29 87557 UE246 FLIGHT 9126 - NAS/FLL - AFTER TAKEOFF LANDING GEAR RETRACTION TOOK 14 SECONDS. REPLACED HYDRAULIC MOTOR. OPERATIONAL C HECK NORMAL. 2 L 7 2 4T RT A24CE 20081015 SO 2008 10 15 RAIA00809005 1 20080906 A 3234 CONTROL LEVER EMB 145 EMB145LR 3260212 SO COCKPIT DEFECTIVE A RAIA O OTHER O OTHER CL CLIMB 1 CE 03 817HK 145058 DURING CLIMB, NOSE GEAR DOORS DID NOT RETRACT. MAINT REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER. SYS OPS CHECKE D GOOD. (K) 2 L 7 2 4T RT T00011AT 20081015 WP 2008 10 15 AALA200802209 1 20080827 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7543A 53025 STL EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5107 FOR EMERGENCY LIGHTS AT AFT CABIN. SYSTE M GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081015 NM 2008 10 15 AALA200802217 1 20080827 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 MIA EMERGENCY LIGHT AT LT HAND OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LT HAND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081001 NM 2008 10 1 CALA0800909 1 20080917 A 5315 141T5108 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69154 30433 CABIN STATION 325 LBL 15 TO LBL 64 FLOOR SUPPORT FOUND CORROSION. CABIN STATION 325 LBL 13 TO LBL 64 FLOORBEAM REPAIRED PER SRM 53-00-01 REPAIR 1 FIGURE 201. 2 L 7 2 4F RT A1NM 20081001 NM 2008 10 1 CALA0800908 1 20080917 A 5315 BAC1518399 FLOORBEAM BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 STATION 986.5 FLOORBEAM SURFACE CORROSION AT LBL 29 AND LBL 32. INSTALLED REPAIR STRAP PER SRM 53-00-51 FIGURE 201. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 UPS08M53330 1 20080916 A 5230 SKIN DOUG MD11 MD11F 3023600 NM FWD CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 293UP 48473 INSPECTION TYPE:N/A, LWR FWD CARGO DOOR SKIN CREASE 12 INCHES LONG, OUT OF SRM LIMITS. ACCOMP HFEC OF DENT PER NDTSPRM 06-10-01. NO CRACKS DETECTED. DRILLED OUT (4) FASTENERS IN DENTED AREA. C/W ITEM 3, 4, 5 ON EO MD11-5230-30572 PER ND TSPM 06-10-01-00. C/W DEFERRAL PER SAME EO PERFORM HFEC INSPECT W/IN EVERY 10 CYCLES. REPAIR W/IN 30 DAYS IAW EO MD11- 52-30-30572. 2 L 7 3 4F RT A22WE 20081001 WP 2008 10 1 UPS08853347 1 20080918 A 5730 PANEL DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:N/A LEFT WING TRAILING EDGE PANEL CRACK. 2 L 7 4 4F RT 4A25 20081001 2008 10 1 UPS08553346 4 20080918 A 3400 INDICATOR BOEING 757 75724APF 1384969 NM COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER TO TAKEOFF 1 SO 01 467UP 25483 INSPECTION TYPE:N/A ATB - LOSS OF ALL FLIGHT INSTRUMENT INDICATORS. EMERGENCY DECLARED. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 CALA0800850 1 20080904 A 5315 6545833212 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 270 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 CORROSION ON FLOORBEAM AT BODY STATION 270 FROM LBL 10 - RBL 10 LOCATED AT AFT SIDE OF NLG DOWNLOCK VIEWER PANEL. REPAI RED CORRODED FLOORBEAM AT BODYSTATION 270 FROM LBL 10 - RBL 10 LOCATED AT AFT SIDE OF NLG DOWNLOCK VIEWER PANEL PER CAL EC/RA5320-01701. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 2008UALA05508 1 20080828 A 3350 8100133801 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 36C INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 215UA 30221 SEAT 36C EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OP OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081002 NM 2008 10 2 2008UALA05538 1 20080902 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 36 ABC WRONG PART A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 179UA 25158 SEAT ROW 36ABC EEL IS INADEQUATE. *S/D* IMPROPER PART. REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081002 EU 2008 10 2 2008UALA05539 1 20080830 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 406UA 454 EMERGENCY LIGHT SYS TEST FAULTS "UNIT EMER R". *S/D* REPLACED POWER SUPPLY, OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081002 SO 2008 10 2 C2XA08RI144 1 20080920 A 3320 BR90002 BALLAST EMB 145 EMB145LR 3260212 SO CABIN BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14952 145067 FLIGHT 2897 - EWR - FLIGHT CREW REPORTED ELECTRIC SMELL IN GALLEY. EWR MX REMOVED AND REPLACED BALLAST AT ROW 1A AND PE RFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081002 NM 2008 10 2 2008UALA05544 1 20080830 A 3350 58673 INVERTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 589UA 28707 ROBBED EEL INVERTER FOR A-C 5596. INVERTER GOES ABOVE AFT GALLEY MAIN CEILING LIGHTS. TAPE IDENTIFIES THE 2 CONNECTOR HOOKUPS. HARDWARE IS ATTACHED TO TAPE. *S/D* REPLACED INVERTER. OP CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 2008UALA05558 1 20080831 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1502 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 MAIN CABIN FLOORBEAM T-CAP CORRODED AT BS 1502 AND LBL 28. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION O F T-CAP. FABRICATED A-1 AND -2 REPAIR ANGLES, -3 STRAP AND 4 EACH SHIM AND INSTALLED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NE 2008 10 2 2008UALA05587 2 20080903 A 7200 FMU BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 RIGHT ENGINE START AT 51% N2 AFTER STARTER CUTOUT RIGHT OIL P EICAS CAME ON. ELECTED TO SHUT DOWN. FOUND FAULTY FUEL M ETERING UNIT. REMOVED AND REPLACED FMU AND RAN. ENG START NORMAL ALL INDICATIONS & OIL PRESSURE NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 SO 2008 10 2 C2XA08IA215 1 20080924 A 3230 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO NLG FAULTY A C2XA O OTHER O OTHER CL CLIMB 1 SW 27 18982 145223 IAH - FLT 2400, THE CREW REPORTED THAT NOSE GEAR DOOR DID NOT CLOSE AFTER T/O, AND THAT IT FINALLY CLOSED AFTER CIRCLING THE FIELD FOR 10 MINUTES. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE PROXIMITY SWITCH ON THE NOSE LANDING GEAR UPLOCK BOX. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPR OVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081002 SO 2008 10 2 C2XA08SH124 1 20080928 A 5230 DOOR FRAME EMB 145 EMB145XR 3260214 SO CARGO DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12160 145799 SHV - DURING C-CHECK BAGGAGE DOOR INNER LOWER FRAME HAS CORROSION. MX REPAIRED BAGGAGE DOOR INNER LOWER FRAME IAW EC 52 30-01194. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 20081002 SO 2008 10 2 C2XA08SH125 1 20080928 A 5751 14569009409SD FITTING EMB 145 EMB145XR 3260214 SO AILERON PCA DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12160 145799 SHV - DURING C-CHECK LT AILERON PCA ATTACHMENT HAS MIGRATED BUSHING. MX REMOVED AND REPLACED LT AILERON PCA FITTING IAW EC5750-01177. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 20081002 NM 2008 10 2 UPS08553280 1 20080813 A 5313 STRINGER BOEING 757 75724APF 1384969 NM BS 656 S16R CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 STRINGER 16R IS CRACKED AT BS 656. REPAIRED PER SRM 53-00-03-1A1. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 UPS08553281 1 20080813 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 540 S7R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 FRAME DENTED BS 540 4 INCHES ABOVE STR 7R. REPAIRED DAMAGED FRAME PER SRM 51-70-11-0G, SRM 51-40-02, SRM 53-00-07-2R. 2 L 7 2 4F RT A2NM 20081002 2008 10 2 2008UALA05895 4 20080925 A 2565 LEVER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOOR OUT OF RIG A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 826UA 989 DOOR 2R, PER INBOARD CREW, OK ON GRD WHEN PRESSURIZED SLIDE ARMING HANDLE MOVES OUT APPROX ONE-HALF IN. RE-RIGGED DOOR ARMING LEVER. DOOR ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081002 NM 2008 10 2 2008UALA05894 1 20080925 A 5320 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 804UA 759 R2 DOOR SILL HAS CORROSION AT FRAME 66 -Y1732. INSTALLED RE PAIR PER MT53-025 AND SRM53-41-14 ON NR K8545G. 2 L 7 2 4F 4 F RT A28NM E40NE 20081002 NM 2008 10 2 UPS08553286 1 20080814 A 5720 FRAME BOEING 757 75724APF 1384969 NM RT WING FAIRING CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 RT WING FAIRING 672HB FWD LWR EDGE STIFFENER IS CHAFED AT LOWER O/B SIDE. REMOVED AND REPLACED FRAME PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 UPS08553287 1 20080814 A 5753 PANEL BOEING 757 75724APF 1384969 NM LT WING TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 LEFT O/B FLAP L/E IS GOUGED AT O/B CARRIAGE. BLENDED GOUGE PER ATS ER08-2722 DATED 25AUG08. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 UPS08553288 1 20080814 A 5753 FRAME BOEING 757 75724APF 1384969 NM TE FLAP CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 ACCESS PANEL 572HB FWD EDGE IS CHAFED. REMOVED AND REPLACED FRAME PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 UPS08553289 1 20080815 A 5320 WEB BOEING 757 75724APF 1384969 NM BS 324-334 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 FLT DECK FLOOR SHEAR WEB UPPER SURFACE IS CORRODED AT SEVERAL AREAS BS 324-334 RBL 44-55 WL 208. BLE NDED CORROSION, INSTALLED DOUBLER IAW EO. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 UPS08553290 1 20080815 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM BS 335-365 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 MAIN CARGO SEAT TRACK IS CORRODED BS 335-365 RBL 35 WL 208. BLENDED OUT CORROSION PER ATS ER 08-2774 DATED 28AUG08. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 2008UALA05893 1 20080926 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 331UA 24192 FWD 1 FT SECTION OF CABIN FLOOR MOUNTED EMERGENCY ESCAPE PATH LIGHTING IS INOP. REPLACED SECTION OF EMERGENCY LIGHT. O P CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 20081002 WP 2008 10 2 UPS08853297 1 20080818 A 5340 FITTING DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 STRINGER 65 TO FRONT SPAR Z-FITTING CRACK AT NR 1 ALT THRU ACCESS PANEL 505B. REMOVE AND REPLACE Z- FITTING IAW SRM 51-1-8, 51-3-1, 51-1-24, 51-1-20 D. 2 L 7 4 4F RT 4A25 20081002 NM 2008 10 2 2008UALA05887 1 20080924 A 3320 05939108 BALLAST BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN OVERHEATED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 512UA 24809 STRONG ELECTRICAL SMELL IN FIRST CLASS AND FWD GALLEY. REPLACED BALLAST. CHECKS OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 UPS08M53296 1 20080819 A 5730 SKIN DOUG MD11 MD11F 3023600 NM L/H WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP 48745 INSPECTION TYPE:C1 LEFT WING TELESCOPING DUCT CUTOUT UPPER INBOARD CORNER CRACKED. REPAIRED LT WING L/E TELESCOPING DUC T CUTOUT UPPER INBOARD CORNER REF MD11 SRM VOL 1 57-10-00 FIG 43 AND MD11 SRM VOL 3 57-43-01 FIG 1. 2 L 7 3 4F RT A22WE 20081002 2008 10 2 2008UALA05885 4 20080925 A 2565 5A29011 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE LEAKING A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 56UA PA1560 25394 LEAKY ASPIRATOR. LEAKING AROUND BARREL SEAL. REPLACED ASPIRATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 2008UALA05884 1 20080924 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 STR 15L AT BS 645 IS CRACKED AT FASTENER HOLE, APPROX 3-16 INCHES IN LENGTH, MARKED. MAJOR REPAIR ACCOMPLISHED. CUT OU T DAMAGED SECTION OF STR 15L. INSTALLED SPLICE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 SO 2008 10 2 LR7A08117 1 20080922 A 5311 38848221 FRAME LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 652 4698 DURING SCHEDULED B-3 CHECK, PER JOB CARD HB3200 FOUND RT UPPER MWW FRAME OUTBOARD CAP CRACKED AT FS 577, WL 236, LBL 66. REPAIRED BY REPLACING CAP IAW SMP583 CHAP 51-70. 2 H 7 4 4T A1SO 20081002 SO 2008 10 2 LR7A08116 1 20080922 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 652 4698 DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5302 FOUND AFT FUSELAGE INTERIOR BULKHEAD FLANGE CRACKED AT FS 847, WL 185, R BL 70. REPAIRED IAW SMP583 FIG 53-50-10. 2 H 7 4 4T A1SO 20081002 SO 2008 10 2 LR7A08115 1 20080922 A 5312 BULKHEAD LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 652 4698 DURING SCHEDULED B-3 CHECK, PER JOB CARD HB5302 FOUND AFT FUSELAGE INTERIOR BULKHEAD FLANGE CRACKED AT FS 847, WL 185, L BL 70. REPAIRED IAW SMP583 FIG 53-50-10. 2 H 7 4 4T A1SO 20081002 NM 2008 10 2 CALA0800926 1 20080929 A 5311 6545819215 FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 B737-53-4-0033 NWW LT TUNNEL LEVELING COMPOUND AT BOTTOM AREA BETWEEN FRAMES 259.5 AND 277 IS BUBBLED UP AND LOOSE CTN 5 3-310-202 SEQ 309 03-5310-1-2613. REMOVED AND REPLACED LT NWW CHORD REF SRM 51-40-02 AND BOEING DWG 65-45819. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 2008UALA05605 1 20080831 A 2197 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE SWITCH CONNECTOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 FWD CARGO COMP BELOW FLOOR-EQUIP COOLING SUPPLY AIR OVERHEAT SWITCH CONNECTOR WIRE HAS INSULATOR DAMAGE AND BARE CONDUCT OR EXPOSED 19 INCHES UPSTREAM OF CONNECTOR D00644. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 2008UALA05606 1 20080902 A 2910 HYDRAULIC SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 OVERHEATED A UALA K NONE M J OVER TEMP WARNING INDICATION IN INSP/MAINT 1 WP 29 175UA 24382 NR 4 HYD OVERHEAT, TEMP WOULD RISE TO 96 DGR WITH ADP RUNNING, TEMP WOULD RISE TO 88 DEGREES WITH AUX PUMP RUNNING. DPI INDICATORS ARE IN ON CASE DRAIN MODULE AND RETURN FILTER MODULE. MEASURED TEMPERATURE AT RETURNED MODULE MATCHES FLIGH T DECK INDICATION AND HYD QTY IS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081002 NM 2008 10 2 CALA0800858 1 20080905 A 5411 311N50052 FRAME BOEING 757 757224 1384958 NM LT PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19117 27559 NR 1 ENGINE PYLON, AFT BULKHEAD CRACKED AT HOLE NR 19, REF EA 5440-01234 OP 11 STEP 4.3. COMPLIED WITH PPS205.65 NEW TO RQUE BULKHEAD FITTING REMOVAL AND INSTALLATION REF ECRA 5450-01749. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 CALA0800859 1 20080904 A 5320 65C339726 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 328-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INTERCOSTAL BETWEEN FLOORBEAMS BS 328 AND 344 HAS CORROSION AT BL15R. REMOVED AND REPLACED INTERCOSTAL BETWEEN FLOORBEA MS PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800860 1 20080905 A 5320 141A813117 INTERCOSTAL BOEING 737 737724 13844BY NM BS 303-312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27722 28789 INTERCOSTAL CORRODED BETWEEN BS 303 AND 312 IN E AND E COMPARTMENT ON LEFT SIDE OF TUNNEL. REMOVED AND REPLACED INTERCO STAL BETWEEN STATION 303 AND 312 IN E AND E COMPARTMENT ON LEFT SIDE OF TUNNEL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800861 1 20080905 A 5320 BAC15141732 STRUCTURE BOEING 737 737724 13844BY NM BS 303-312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27722 28789 E AND E COMPARTMENT FRAME BETWEEN STATION 303.9 TO 312 AND STRINGER S23L AREA CORRODED. REPAIRED FRAME BETWEEN STATION 303.9 AND 312 AND STRINGER 23L PER SRM 51-70-12 REPAIR 2. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 2008UALA05850 1 20080923 A 3350 78961 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 127UA 28813 SEAT 5A FWD EMERGENCY LIGHT IS INOP, RELAMPED, CHECKS OK 2 L 7 4 4F 4 F RT A20WE E24NE 20081001 NM 2008 10 1 2008UALA05780 1 20080918 A 2400 263BA1011 BATTERY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 775UA 26947 APU BATTERY VOLTAGE TO LOW TO START THE APU. CAN BE STARTED PNEUMATICALLY. RESET CIRCUIT BREAKER P320 K12, CHARGER OPE RATES NORMAL. BATTERY CHARGED AND APU START NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081001 NM 2008 10 1 2008UALA05781 1 20080918 A 3510 MC1019101 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CAPTAIN'S NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 507UA 24743 CAPTAIN'S O2 MASK DOES NOT TEST OK. REPLACED O2 MASK STOWAGE BOX. TESTS OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081001 NM 2008 10 1 SWAA085173 1 20080910 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND STRIGNER CLIP CRACKED AT RIGHT BS 886, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085172 1 20080908 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 787 STR 26R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085171 1 20080922 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A S26L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081001 EU 2008 10 1 2008UALA05777 1 20080915 A 5270 WARNING MESSAGE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO DOOR FALSE ACTIVATION A UALA C ABORTED TAKEOFF N FALSE WARNING TX TAXI/GRND HDL 1 WP 29 405UA 452 FWD CARGO DOOR ECAM. ABORTED T/O AT 100 KNOTS. CYCLED DOOR ALL WINDOW SHOWED GREEN CREW REPORTS MESSAGE CLEARED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081001 NM 2008 10 1 08FDEA04051 1 20080926 A 5730 ARB2886504 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 623FE 48794 RIGHT WING LEADING EDGE ANTI-ICE TELESCOPIC DUCT CUT-OUT DOUBLER INBOARD AND OUTBOARD LOWER SECTION FOUND WITH CHAFE MAR KS. REPAIR CARRIED OUT AS PER EA NR 1-5740-122551, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081002 NM 2008 10 2 2008UALA05572 1 20080902 A 5730 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE RT WING CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 815UA 867 RT WING TOP SKIN AT REFUEL PORT CUTOUT FLANGE HAVE PITTING CORROSION. REPAIRED PER UA-EVA-71896 AND REO-L01103. RECEIVE D RAS-BAE-1008098-2008. TO BE REINSPECTED AT 123,500 CYCLES. CURRENT PTC 13082. INSPECTION INTERVAL AND METHOD TO BE DET ERMINED BY AIRBUS ON OR BEFORE 123,500 CYCLES. DTA 08-219 CREATED TO TRACK ACCOMPLISHMENT. 2 L 7 2 4F 4 F RT A28NM E40NE 20081002 NM 2008 10 2 2008UALA05577 1 20080903 A 5420 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 PYLON WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 510UA 24780 NR 2 PYLON HYD PRESSURE LINE FITTING AT PYLON STRUT WALL, PYLON SKIN WEB IS WORN. REPAIRED PYLON. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 SO 2008 10 2 C2XA08SH127 1 20080928 A 5320 STRUCTURE EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14977 145175 SHV - DURING C-CHECK CARGO DOOR LOWER CUTOUT HAS AREAS OF CORROSION. MX REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT IA W EMB 145 SRM 51-40-02 AND CPM 51-21-07. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 20081002 SO 2008 10 2 C2XA08SH126 1 20080928 A 5240 BUSHING EMB 145 EMB145LR 3260212 SO SERVICE DOOR MIGRATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14977 145175 SHV - DURING C-CHECK SERVICE DOOR UPPER HINGE AT FUSELAGE HAS MIGRATED HAT BUSHING. MX REWORKED FITTING LOCATED AT SERV ICE DOOR UPPER HINGE AT FUSELAGE AND INSTALLED OVERSIZED BUSHING IAW EC 5240-01036. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 20081002 NM 2008 10 2 CALA0800927 1 20080929 A 5210 507945178 SKIN BOEING 737 7373T0 1384582 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 L-1 DOOR SKIN IS CRACKED AT 4TH STOP FROM TOP, AFT SIDE OF DOOR. TRIMMED OUT CRACK AND INSTALLED REPAIR DOUBLER PER ECR A 5210-02035. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 2008UALA05594 1 20080905 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 1F MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 781UA 26945 EEL 1F MISSING 2F HANGING LOOSE. LIGHT MISSING. REPLACED EMERGENCY LIGHT AT SEAT 1F. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081002 NE 2008 10 2 2008UALA05595 2 20080905 A 7250 TURBINE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 ENGINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 781UA 26945 777034 NR 1 ENGINE HPT DAMAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081002 NM 2008 10 2 2008UALA05596 1 20080904 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE SEAT 2B UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 668UA 30024 THE 2B EMERGENCY LIGHT FELL OFF. FOUND LIGHT UNSECURE. SECURED EMERGENCY LIGHT ASSY TO SIDE OF SEAT 2B. OPS CHECKS OK AY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 2008UALA05597 1 20080904 A 2822 PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUEL BOOST FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 RIGHT AFT MAIN TANK FUEL BOOST PUMP FAILS RESISTANCE CHECK. FOUND HIGH INTERNAL RESISTANCE IN FUEL BOOST PUMP. REPLACE D RT AFT BOOST PUMP. BONDING RESISTANCE CHECK GOOD, OPS, AND LEAK CHK GOOD 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 SWAA085120 1 20080918 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085119 1 20080918 A 5311 65C22908 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 AALA200802216 1 20080827 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 372AA 25199 MIA EMERGENCY LIGHTS AT SEAT ROWS 20H TO 21H INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 20H T O 21H. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081015 EA 2008 10 15 COMA0860397 1 20080928 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN FAILED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 589SW 7072 FLIGHT NR 6361 EMERGENCY LIGHTS BETWEEN ROWS 2-5 AND 8 ARE INOP. R&R LIGHT STRIP. 2 L 7 2 4F RT A21EA 20081015 2008 10 15 2008UALA06014 4 20081006 A 2565 3A24024 ASPIRATOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EVAC SLIDE DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 194UA GS1023 26892 ASPIRATOR DAMAGED & ROTOR STATOR BLADES. FOREIGN OBJECT GOT INSIDE ASPIRATOR AND DAMAGED BARREL AND ROTOR STATOR BLADES . REPLACED ASPIRATOR. 2 L 7 4 4F 4 F RT A20WE E24NE 20081015 NM 2008 10 15 2008UALA06015 1 20081007 A 2421 340545 SHUTOFF VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GENERATOR FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 643UA 25093 HYD MOTOR GENERATOR FAILS TO RUN WHEN TESTED. FOUND V147 AT FAULT. REPLACED R & R HMG SHUTOFF VALVE. OPS & LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081015 SO 2008 10 15 C2XA08SH116 1 20080910 A 5230 14523918001 SKIN EMB 145 EMB145XR 3260214 SO CARGO DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11194 14500940 DURING C-CHECK, CARGO DOOR INNER SKIN HAS CORROSION AROUND NUT PLATE HOLES. MX REPAIRED CORRODED AREAS ON CARGO DOOR INN ER SKIN NUT PLATE HOLES IAW EC523001193. THE ACFT WAS APPROVED TO RETURN FOR SERVICE. (K) 2 L 7 2 4F RT 20081015 SO 2008 10 15 C2XA08SH119 1 20080910 A 5322 14525175001 SHEAR TIE EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11184 14500917 DURING C-CHECK SHEAR CLIP AT FR 65 CARGO DOOR CUT OUT HAS CORROSION. MX REPAIRED FRAME 65 CARGO DOOR CUTOUT LOWER CORNER SHEAR CLIP IAW EC5330-01458. THE ACFT WAS APPROVED TO RETURN FOR SERVICE. (K) 2 L 7 2 4F RT 20081015 NM 2008 10 15 ZZDA2008166 1 20081008 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 957AT 55019 EMERGENCY LIGHTS AT ROWS 1, 2 AND 3 INOP. REMOVED AND REPLACED ROW NR 3 BATTERY PACK ASSY IN REF TO B717 MM 33-51. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F TR A6WE 20081015 NM 2008 10 15 UPS08B53477 1 20080108 A 5320 65B09631716 TENSION TIE BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 579UP 26062 INSPECTION TYPE:BCF STA 1140 RT TENSION TIE FWD CHANNEL 2EA FASTENER HOLE CRACKED MORE THAN 0.030". REPAIRED CRACKED TE NSION TIE AS PER SRM 53-40-30 FIG 201. 2 L 7 4 4F RT A20WE 20081015 NM 2008 10 15 UPS08B53478 1 20080108 A 5320 65B09631610 TENSION TIE BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 579UP 26062 INSPECTION TYPE:BCF STA 1140 LT TENSION TIE AFT CHANNEL 5EA FASTENER HOLE CRACKED ABOUT 0 .030" 3EA FASTENER HOLE CRACKE D MORE THAN 0.030". REPAIRED CRACKED TENSION TIE AS PER SRM 53-40-30 FIG 201. 2 L 7 4 4F RT A20WE 20081015 NM 2008 10 15 UPS08B53479 1 20080108 A 5311 65B0175127 FRAME BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 579UP 26062 INSPECTION TYPE:BCF STA 1160 LT TENSION TIE FRAME WEB 2EA FASTENER HOLE CRACKED MORE THAN 0.050", 6EA FASTENER HOLE CRAC KED ABOUT 0.030". REPAIRED CRACKED TENSION TIE FRAME WEB AS PER SRM 53-40-07. 2 L 7 4 4F RT A20WE 20081015 NM 2008 10 15 UPS08B53480 1 20080308 A 5311 65B01750802 FRAME BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 579UP 26062 INSPECTION TYPE:BCF RT STA 1140 TENSION TIE FRAME 1EA FASTENER HOLE CRACKED MORE THAN 0.0 30". REPAIRED CRACKED TENSION TIE FRAME AS PER SRM 53-40-07. 2 L 7 4 4F RT A20WE 20081015 NM 2008 10 15 UPS08B53481 1 20080108 A 5320 65B09631718 TENSION TIE BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 579UP 26062 INSPECTION TYPE:BCF STA 1180 TENSION TIE RT FWD CHANNEL 6EA FASTENER HOLE CRACK ABOUT OR MORE THAN 0.030". REPLACED CRA CKED TENSION TIE AS PER DWG 65B09631, SH14 AND SRM 51-40-0 2. 2 L 7 4 4F RT A20WE 20081015 NM 2008 10 15 UPS08M53484 1 20081007 A 2560 GIRT BAR DOUG MD11 MD11F 3023600 NM L1 DOOR OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 292UP 48566 INSPECTION TYPE:N/A A/C ARRIVAL FOUND L1 DOOR SLIDE OF THE GIRT BAR OUT OF POSITION. PER AMM 25-61-15-4 RE-INSTALLED TH E GIRT BAR AND L1 DOOR ARM/SIDEARM CHECK NORMAL, L1 DOOR CLOSE/OPEN CHECK NORMAL. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 UPS08M53485 1 20080518 A 5753 HINGE DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A LT WING O/B FLAP I/B FWD HINGE BARREL NUT SPOT FACE CORRODED. LT WING O/B FLAP I/B FWD HINGE BARREL NUT SPOT FACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 UPS08M53486 1 20080818 A 5753 HINGE DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A LT WING O/B FLAP I/B FWD HINGE BARREL NUT LOWER BORE CORRODED. LT WING O/B FLAP I/B FWD HINGE BARRE L NUT LOWER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 UPS08M53487 1 20080818 A 5753 HINGE DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A LT WING O/B FLAP I/B FWD HINGE BARREL NUT UPPER BORE CORRODED. LT WING O/B FLAP I/B FWD HINGE BARRE L NUT UPPER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 UPS08M53494 1 20080816 A 5753 HINGE DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A LT WING O/B FLAP I/B AFT HINGE I/B PIVOT I/B SPOTFACE CORRODED. LT WING O/B FLAP I/B AFT HINGE I/B PIVOT SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-52-04. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 UPS08M53495 1 20080818 A 5753 HINGE DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A LT WING O/B FLAP O/B FWD HINGE BARREL NUT UPPER BORE CORRODED. LT WING O/B FLAP O/B FWD HINGE BARRE L NUT UPPER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 UPS08M53496 1 20080818 A 5753 HINGE DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A LT WING O/B FLAP O/B FWD HINGE LOWER MOUNT I/B BORE FWD & AFT SPOTFACE CORRODED. LT WING O/B FLAP O /B FWD HINGE LOWER MOUNT I/B BORE FWD & AFT SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 UPS08M53500 1 20080818 A 5753 HINGE DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A RT WING O/B FLAP O/B FWD HINGE LOWER MOUNT O/B BORE FWD & AFT SPOTFACE CORRODED. RT WING O/B FLAP O /B FWD HINGE LOWER MOUNT O/B BORE FWD & AFT SPOT FACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 DXTA2008101303304 1 20081012 A 5610 WINDSHIELD GULSTM 200 200 4500308 NM COCKPIT CRACKED E DXTA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 07 722QS 093 CO-PILOT WINDSHIELD SHATTERED WHILE IN CRUISE FLIGHT AT FL350. 2 L 7 2 4F RT A53NM 20081015 EU 2008 10 15 MTNA100802 1 20081006 A 5720 STRUCTURE AEROSP ATR72 ATR72202 8680940 EU LT WING CORRODED A MTNA K NONE O OTHER IN INSP/MAINT 1 EA 68 810FX 25672 220 FOUND CORROSION INSIDE LEFT FUEL FEEDER TANK BETWEEN RIBS 4 AND 5. THERE WERE SEVERAL AREAS FROM STIFFENER 1 TO STIFFEN ER 10. CORROSION REMOVED AS PER SRM ATR72 CH 51-21-42. APPLIED TREATMENT TO NEUTRALIZE ANY HEDDIN CORROSION. PERFORME D FINAL BLEND OUT IAW SRM ATR72 CH 51-21-58. CONFIRMED THAT REMAINING THICKNESS OF BLEADED AREAS HAVE NOT CHANGED REF T ABLE 1 OF ATR SRI NUMBER DO/TS-4240/08-10776. CONFIRMED THE ABSENCES OF CRACKS BY USE OF HF EDDY CURRENT. RESTORED PRO TECTION OF REWORKED AREAS WITH ALODINE 1200 IAW SRM ATR72 CH 51-21-17 AND CH 51-21-28. REFERENCE ANA/E/4462/2008/E-001 AND ANA/E/4462/2008/E-003. 2 H 7 2 4T RT A53EU 20081015 NE 2008 10 15 ZZDA2008167 2 20081009 A 7200 BR700715A13C ENGINE BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE LEFT SHUTDOWN A ZZDA O OTHER Y ENGINE STOPPAGE CR CRUISE 1 SO 37 960AT 55022 IN CRUISE, NR 1 ENGINE AUTO-SHUTDOWN. REMOVED AND REPLACED NR 1 ENGINE IAW AIRTRAN TASK CARD 603. 2 L 7 2 4F 4 F TR A6WE E00061EN 20081015 EA 2008 10 15 ASOA200801306 1 20081007 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 921EV 7819 INBOARD AND OUTBOARD FLOOR SUPPORT CLIPS CRACKED AT FS 280, LBL 9. 2 L 7 2 4F RT A21EA 20081015 EA 2008 10 15 ASOA200801307 1 20081006 A 5240 TAB CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR DEFECTIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 825AS 7207 UNABLE TO OPEN SERVICE DOOR BY USING OUTSIDE RELEASE HANDLE (TAB NOT RELEASING HANDLE). 2 L 7 2 4F RT A21EA 20081015 EA 2008 10 15 ASOA200801309 1 20081007 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 885AS 7521 FLIGHT ATTENDANT FLASHLIGHT INOP. 2 L 7 2 4F RT A21EA 20081015 EA 2008 10 15 ASOA200801314 1 20081008 A 5312 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 921EV 7819 REAR PRESSURE BULKHEAD WEB THAT SURROUNDS LINTEL ATTACHMENT FITTING HAS A INDICATION NOTED APPROX .1 INCH IN LENGTH 60 P ERCENT FULL SCREEN HEIGHT FAILED NDT INSPECTION. REPAIRED LINTEL FITTING IAW REO 601R-53-61-1230 AND REO 601R-53-61-123 0. 2 L 7 2 4F RT A21EA 20081015 EA 2008 10 15 ASOA200801315 1 20081008 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 921EV 7819 FORWARD PRESSURE BULKHEAD AT FS 202.75 SHOWS EVIDENCE OF A CRACK .750 INCH LONG FROM TOP OF HOLE FOR PARKING BRAKE CABLE . PERFORMED EDDY CURRENT INSPECTION, INDICATION NOTED APPROX .5 INCH, FAILED NDT. LT FS 202.75 BULKHEAD WEB REQUIRES REPAIR. REMOVED PARKING BRAKE CABLE FROM BULKHEAD. REPAIRED CRACKED BULKHEAD. APPLIED CORROSION INHIBITING COMPOUND & INSTALLED PARKING BRAKE CABLE. ADJUSTED CABLE. OPS TEST OF THE PARKING BRAKE SYS GOOD. C/W ASA ECTC EO 600-53-217CW . 2 L 7 2 4F RT A21EA 20081015 EA 2008 10 15 ASOA200801316 1 20081008 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 981EV 7768 EMERGENCY EXIT SIGNS ON WARDROBE GALLEY TRIM PANEL AND SERVICE DOOR TRIM PANEL FAILED OPERATION TEST. 2 L 7 2 4F RT A21EA 20081015 EA 2008 10 15 ASOA200801317 1 20081009 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA ASD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 ASD FWD ANCHOR FITTING CRACKED. REMOVED & REPLACED TO COMPLY WITH SB 601R-52-116. PERFORMED MX IAW AMM TASKS; 52-11-17 -000-803, 52-11-17-400-803, AND S.B. 601R-52-116 WITH REO 601R-52-11-1572. COMPLIED WITH ADJUSTMENT AND OPERATIONAL TE ST. CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081016 SW 2008 10 16 WGE2008F00004 1 20080902 A 2620 FX002002 FIRE BOTTLE ECLIPS EA500 ECLIPSEEA500 3350000 SW NR 2 NACELLE LEAKING E WGEA O OTHER O OTHER NR NOT REPORTED 1 EA 27 153DJ 239 000072 NR 2 ENGINE FIRE BOTTLE IS LEAKING. REMOVED UPPER ENGINE NACELLE IAW AMM 54-20-21. REMOVED LOWER ENGINE NACELLE IAW AM M 54-20-22. REMOVED RT L/E PYLON SKIN IAW AMM 54-30-11. REMOVED RT LOWER MIDDLE PYLON SKIN IAW AMM-30-13. REMOVED RT FI RE EXTINGUISHER CARTRIDGE, PN FX00200-2, SN 00254. IAW AMM 26-20-10. C/W EXTINGUISHING CLEANING ( RT PYLON AND ENGINE IAW AMM 26-20-00. (K) 1 L 7 2 4J RT A00002AC 20081016 SO 2008 10 16 C2XA08ON180 1 20080830 A 2910 15793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO NR 2 HYD SYS INOPERATIVE A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 13550 9976 7492 145575 FLIGHT CREW REPORTED IN (3) DIFFERENT STATIONS WHILE TAKEOFF, CLIMB AND CRUISE. RUDDER SYS 2 AND RUDDER SYSTEM 1/2 INOP ERATIVE MSG ON EICAS. MX REMOVED AND REPLACED RUDDER NR 2 SYS PRESSURE SWITCH. OPERATIONALLY CHECKED SATISFACTORY AND AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081016 WP 2008 10 16 JJW2008F00000 1 20080325 A 2197 WIRE ROBSIN R44 R44RAVENII 7640122 WP CABIN AIR CHAFED E JJWA K NONE O OTHER IN INSP/MAINT 1 SO 19 157HP 11057 FOUND WIRING TO FREEZE SWITCH HAD CHAFED THROUGH THE CAPILLARY TUBE TEMP SENSOR RELEASING ALL ITS REFRIGERANT, CAUSING S WITCH TO OPEN AND NOT ALLOW COMPRESSOR TO RUN. SWITCH NOT FIELD REPLACEABLE, HAD TO SENT TO FACTORY FOR REPAIRS. INSTA LLED SPIRAL WRAP ANTI-CHAFE TO WIRING ON REPAIRED PART TO PREVENT REOCCURRENCE. NOTIFIED MFG PRODUCT SUPPORT OF PROBLEM AND WAS TOLD A SERVICE BULLETIN WOULD BE ISSUED. (K) 1 G 7 1 3O H11NM 20081016 EA 2008 10 16 ASOA200801319 1 20081002 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS A INDICATION NOTED APPROX .1 INCH IN LENGTH 100 PERCENT FULL SCREEN HEIGHT FAILED NDT INSPECTION. THIS SDR WILL REMAIN OPEN PENDING MAINTENANCE DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. 2 L 7 2 4F RT A21EA 20081016 EA 2008 10 16 ASOA200801320 1 20081003 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 846AS 7328 AN INDICATION WAS NOTED ON THE 621 BULKHEAD FWD FACE DURING AN EDDY CURRENT INSPECTION AT LBL 9.50, WL 110 .350 IN LENGT H. COMPLIED WITH REO 601R-53-61-1285, STEPS 1 THRU 33 FOR REPAIR TO AFT PRESS BULKHEAD FS 621 LBL 9.0. INCORPORATED RE O 601R-53-61-2880 DISPOSITION FOR LOW ED ON FS 621 PRESSURE BULKHEAD AT LBL 9.5. COMPLIED WITH EC/TC REO 601R-53-61-128 5 AND PROCESSED M-93 WEIGHT CHANGE FORM AS REQUIRED. 2 L 7 2 4F RT A21EA 20081016 NM 2008 10 16 DHLA2008745505 1 20080901 A 5311 ATTACH FITTING BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 745DH 20665 UPPER FUSELAGE CARGO CABIN FRAME ATTACHMENT CLIP CRACKED AT BS 1070 ON STRINGERS 1L & 2L. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 DHLA2008745506 1 20081005 A 5751 SKIN BOEING 727 727224 1384076 NM RT AILERON DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 RIGHT I/B AILERON SKIN DENTED AT RWBL 258 AND 276. ACCOMPLISHED FLUSH REPAIR ON AILERON LOWER SKIN PER B727 SRM 57-50-5 FIG 1. REF N/R 4987-6-21. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 DHLA2008745510 1 20080901 A 5311 ATTACH FITTING BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 745DH 20665 UPPER FUSELAGE CARGO CABIN FRAME ATTACHMENT CLIP AT BS 1050 STRINGER 1 CRACKED. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 DHLA2008745516 1 20080906 A 5320 STRAP BOEING 727 727224 1384076 NM CARGO BAY CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 745DH 20665 UPPER FUSELAGE CARGO CABIN STABILIZER STRAP CRACKED BETWEEN BS 328 TO BS 344 WL 200 LBL 45. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 DHLA2008745517 1 20080912 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 FRAME DENTED AT BS 680, BETWEEN STR 16R AND 17R. REPAIRED FRAME PER B727 SRM 51-40-3 FIG 1. REF N/R 4987-2-65. 2 L 7 3 4F A3WE 20081016 EA 2008 10 16 TRAX200801110 1 20080904 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 LT BS 280 BEAM CORRODED. 9/15/2008 - SUP- (RESOLVED W/O 99610 TASKCARD NR 00181) WORK COMPLETED IAW: INSTALLED DRUO TRAY S IAW SB 670BA-53-026. 2 L 7 2 4F RT A21EA 20081016 NM 2008 10 16 SWAA085499 1 20081009 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER PAE EA. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085501 1 20081009 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085492 1 20081008 A 3350 417A5700 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 244WN 34864 DURING SCHEDULED MV2 CHECK, FOUND FWD EMERGENCY EXIT FLOOR TRACK LIGHT INOP. REPLAMPED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085493 1 20081009 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 857, STR 27R, RBL 8. REMOVED AND REPLACED BEAM PER DHN EA. 2 L 7 2 4F RT A16WE 20081016 2008 10 16 SWAA085506 4 20081009 A 2565 1061323478 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR UNSERVICEABLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 314SW 23336 FOUND R1 DOOR ESCAPE SLIDE PRESSURE GAUGE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085508 1 20081009 A 3260 286A5156 PSEU BOEING 737 7377H4 1384404 NM LANDING GEAR FAULTY A SWAA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 29 248WN 32509 AIR TURNBACK, ON T/O LANDING GEAR WOULD NOT RETRACT NORMALLY. AFTER REFERRING TO QRH, LANDING GEAR RETRACTED NORMALLY W ITH FLAPS UP. T/O WARNING HORN SOUNDED WITH GEAR IN TRANSIT AND UP UNTIL CANCELLED. REMOVED AND REPLACED PSEU AND GROU ND SPOILER INTERLOCK CABLE PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085447 1 20081007 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 520, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085118 1 20080918 A 3350 101073101 LENS BOEING 737 737301 1384611 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS WORN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085117 1 20080918 A 5753 6546431285 FLAP BOEING 737 737301 1384611 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND LT WING OUTBOARD FORE FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800863 1 20080905 A 5320 694962415 ANGLE BOEING 737 7373T0 1384582 NM BS 727E S24R CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 CORROSION ON TRANSITION ANGLE AT STATION 727E S-24R. REMOVED BAD TRANSTION ANGLE, FABRICATED NEW SECTION, ALODINED, PRI MED AND INSTALLED ANGLE PER SRM 51-40-02, SRM 51-40-05 AND AMM 51-20-00. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085131 1 20080916 A 5330 6545777 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERVICE DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085130 1 20080916 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 347SW 24374 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT STA 410, STR 1. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0853476 1 20080907 A 2840 3012803 PROCESSOR BOEING 737 737890 1384527 NM FUEL SYS FAULTED A ASAA O OTHER N FALSE WARNING CR CRUISE 1 NM 02 583AS 4568 35681 DURING CRUISE DEVELOPED 1000 LBS FUEL IMBALANCE WITH ASSOCIATE "IMBAL" ANNUNCIATOR FOR NO OBVIOUS REASON. ACFT WAS NOT BALANCED, FUEL CROSS FEED CLOSED. CENTER TANK EMPTY WITH CENTER BOOST PUMPS OFF. ALL MAIN TANK PUMPS ON. LT QTY REACH ED 7100 LBS RT WAS 8100 LBS. RAN QRH PROCEED REST ABLIL BAL. NO EVIDENTS OF LEAK. FUEL REMAINED IN BALANCE REST OF FL T. CROSS FEED HAD BEEN OPEN BRIEFLY LAST OF CENTER FUEL WAS USED EARLIER IN FLT. EMBALANCE LIGHT CAME ON WENT OFF NORM ALLY REF FIM 28-41-00-810. FQIS HAS NO HISTORY OR CURRENT FAULTS AND BITE TEST OK. NO FAULTS IN CDS BITE AS WELL REM F IM 28-41-00-801. REF FAULT ISOLATION MANUAL 28-21-00-810-815 INITIAL EVALUATION CHECK COMPLETED WITH NO DISCREPANCY NOT 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085128 1 20080918 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 203WN 32483 DURING SCHEDULED MV2 CHECK, FOUND AFT LT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB P ER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085126 1 20080918 A 5315 6546811 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 781WN 30601 DURING SCHEDULED 8Y CHECK, FOUND UPPER FLOORBEAM CAP CORRODED AT STATION 986.5 BETWEEN LBL 7 TO RBL 7. REMOVED AND REPL ACED PER SWA EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085125 1 20080918 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 24R. REMOVED AND REPLACED PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873516 1 20080910 A 5230 143A61121 SKIN BOEING 737 737790 13844CN NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 FWD CARGO DOOR HAS FIVE EA DENTS WITH CREASES BETWEEN STA 455 489 AND BETWEEN BEAMS NR 2 AND NR 4. REMOVED DAMAGED AREA S, FABBED DOUBLER AND INSTALLED THE REPAIR IAW EA 12906. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0843515 1 20080830 A 5210 6545871132 DOOR BOEING 737 737490 1384715 NM R1 LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 703AS 35072 28893 F/A'S REPORT, DOOR R1 HAS LARGE GAP WHEN CLOSED. CHECKED R1 DOOR, FOUND THE DOOR LINER UPPER TRIM COVERING NOT FLUSH WI TH DOOR CUTOUT. OPS CK DOOR, FOUND DOOR HARD TO CLOSE AND UPPER DOOR PNL DIDN'T CLOSE PROPERLY. LUBED DOOR PER T C 431 52005, POST LUBE CK GOOD. DOOR CLOSES SMOOTH AND UPPER DOOR PNL CLOSES. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800868 1 20080905 A 5311 6517684133 FRAME BOEING 737 7373T0 1384582 NM BS 303 S16L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 CRACK ON STIFFENER WHERE LOWER CASTING FOR L-1 DOORSTOP MOUNTS TO FRAME AT BODY STATION 303.9 AFT OF STRINGER 16 AT DOOR CUTOUT. REPAIRED FRAME AT BODY STATION 303.9 AND S16L PER EC/RA 5310-04826. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800869 1 20080905 A 5311 6517684107 FRAME BOEING 737 7373T0 1384582 NM BS 303 S16L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 BODY STATION 303.9 FRAME WEB P/N 65-17684-107 CRACKED AT S16L. BODY STATION 303.9 FRAME WEB REPLACED PER EC/RA 5310-048 26. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0853513 1 20080915 A 2160 6228145 CONTROLLER BOEING 737 737890 1384527 NM CABIN TEMP MALFUNCTIONED A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 570AS 6281 35185 ZONE TEMP LIGHT ILLUMINATED ON RECALL CHECK LIST COMPLETED WILL NOT RESET ACCOMPLISHED ZONE TEMP CONTROLLER BITE COCKPIT TRIM VALVE FAULT ON STANDBY CONTROLLER. VERIFY & RETEST OK REF 21 61 00 PG 501. NO FURTHER DISCREPANCIES NOTED. GROU ND VERIFICATION TEST OK. 2 L 7 2 4F RT A16WE 20081002 WP 2008 10 2 UPS08853333 1 20080724 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 COMPLY WITH MPI P 19578 REGARDING REPAIR AT AFT FUSELAGE L28R IAW WAN 1312722, MPI SUMMARY REPORT PAG E 2 AND EO DC8-5330-20248E APPX E. REPAIRED FUSELAGE SKIN AT L28R IAW UPS EO DC8-5330-20248-E. 2 L 7 4 4F RT 4A25 20081002 NM 2008 10 2 UPS08553336 1 20080917 A 2120 UNKNOWN BOEING 757 75724APF 1384969 NM COCKPIT ODOR A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 408UP 23730 INSPECTION TYPE:N/A EXPERIENCED BRIEF PACK ODOR IN C/P AT CRUISE ALTITUDE. SUSPECT LEFT PACK. PERFORMED TROUBLESHOOTIN G PER FIM 21-00-01 PROCEDURE 2 FOUND NO SYSTEM DEFECTS, OK FOR SERVICE AT THIS TIME. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 ASAA0853512 1 20080914 A 7920 O-RING BOEING 737 737890 1384527 NM LUBRICATION UNIT DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 577AS 5954 YT009812 35186 UPON REMOVAL OF THE NR 1 ENG GEARBOX CHIP DETECTOR FILTER FOUND PIECES OF O-RING PARTICLES. REMOVED AND REPLACED NR 1 E NG LUB UNIT IAW 737NG PT2 MM 79 21 01 400 801 700 STEP G, LEAK CHECK GOOD IAW 737NG PT2 MM 71 00 00 700 301 F00 TEST 3A. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873506 1 20080909 A 5754 114A50403 SKIN BOEING 737 737790 13844CN NM L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 NR 4 SLAT LOWER T/E SURFACE IS CHAFED AT THE ENDS AND TRACK LOCATIONS ABOVE THE ACTR. REMOVED DAMAGED AREA, FABBED FILL ER AND DOUBLER, BONDED THE REPAIR IAW B737 700 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873495 1 20080828 A 5320 146A75023 CHANNEL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 AFT CARGO RT ZEE CHANNEL BS 727 767 CORRODED RT ZONE CHANNEL BS 727 767. REPLACED IAW B737 700 SRM 53 00 53 FIG 202. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873494 1 20080828 A 5320 146A81271 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 AFT CARGO FLOOR SUPPORT WEB BS 767 790 CORRODED. AFT CARGO CORRODED FLOOR SUPPORT WEB AT BS 767 790 REPLACED WITH A NEW PART IAW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 2008UALA05617 1 20080906 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 AFT RIGHT EMERGENCY EXIT LIGHT DOOR HANDLE IS INOP. RELAMPED. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 2008UALA05621 1 20080906 A 5240 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 R-2 DOOR UPPER HINGE CUTOUT REQUIRES REPAIR DOUBLER PER MM 52-11-87. HFEC INSPECTION COMPLETE PER NDT 6-51 -00-19 AND N O CRACKS NOTED. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 ASAA0873485 1 20080828 A 5312 111A1141 BULKHEAD BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 WHEEL WELL AREA BULKHEAD 663 LWR VAPOR BARRIER CRACKED AT LBL 14. REPAIRED IAW B737 700 SRM CH 51 70 04 REPAIR 10. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873484 1 20080905 A 5320 143A75039 INTERCOSTAL BOEING 737 737790 13844CN NM CARGO BAY CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 FWD CARGO INTERCOSTAL AT LBL 22 STR 26L BS 500C AND BS 500D CRACKED. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53 30 53 AND BOEING DRAWING 143A7503 9. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0853511 1 20080914 A 3610 32144464 VALVE BOEING 737 737890 1384527 NM NR 1 ENGINE LEAKING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 577AS 2511 35186 NR 1 ENGINE HIGH STAGE VALVE LEAKS AT BODY. REMOVED AND REPLACED NR 1 ENG HIGH STAGE VALVE IAW 737NG MM 36 11 06 000 80 1 STEP B&C AND MM 36 11 06 400 801 STEP E&F, PERFORMED W T W AAR 516368 D D 28DEC08, PERFORMED INSTALL TEST OF VALVE IAW 737NG MM 36 11 06 400 801 G, TEST GOOD COMPONENT VERIFIED ETOPS BY QC. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085078 1 20080916 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 2R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085077 1 20080916 A 5311 6546558 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085076 1 20080916 A 5311 6546554 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085075 1 20080916 A 5311 6546550 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085071 1 20080916 A 5330 6545777 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT AIR STAIR CUTOUT LOWER FWD CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085070 1 20080916 A 3350 65C32046 LENS BOEING 737 737317 138447P NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 R1 DOOR EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER SWA EA. 2 L 7 2 4F RT A16WE 20081015 WP 2008 10 15 AALA200802252 1 20080830 A 5241 2705574BN PIN DOUG DC9 DC982 3022082 WP GALLEY DOOR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7548A 53030 GDL FOUND BROKEN SCREW AT AFT GALLEY DOOR LEVER MECHANISM. REPLACED PIN AT AFT GALLEY DOOR MECHANISM. SYSTEM GROUND CH ECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081016 NM 2008 10 16 SWAA085475 1 20081007 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 418WN 29823 DURING SCHEDULED MV1 CHECK, FOUND FLOOR EGRESS LIGHT COVER UNSECURED AT MID CABIN. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085476 1 20081008 A 3350 417A5700 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 458WN 33857 DURING SCHEDULED MV2 CHECK, FOUND AFT PROXIMITY EMERGENCY EXIT FLOOR LIGHT COVER MISSING. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085477 1 20081008 A 5322 6946466 SHEAR TIE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED 18Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, CENTER TANK LT FRONT SPAR. REMOVED AND REPLACED SHEAR TI E PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085478 1 20081008 A 2560 PL22300 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 FOUND PHOTOLUMINESCENT LIGHT COVER LOOSE AT ROW 8. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20081014 SO 2008 10 14 SWIA200820107 1 20080928 A 3350 CONTROL UNIT EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT FAILED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 585SW 120353 FLT 5772 - EMERGENCY FLOOR WHITE LIGHT AT 3A IS INOP. REPLACED UNIT. 2 L 7 2 4T RT A31SO 20081014 NM 2008 10 14 SWAA085435 1 20081007 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CRACKED AT BS 1064, STR 17R. REMOVED AND REPLACED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081014 EA 2008 10 14 SWIA200820109 1 20080929 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 611SK 10035 FLT 4036 - CEILING FORWARD EMERGENCY FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081014 EA 2008 10 14 SWIA200820115 1 20080930 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 468CA 7649 FLT 2516 - EMERGENCY LIGHTS NEAR FLOOR AT MAIN CABIN DOOR INOP, RELAMPED. 2 L 7 2 4F RT A21EA 20081014 EA 2008 10 14 SWIA200820117 1 20080801 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 668CA 10162 C-CHECK - FS 280 BEAM CORRODED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081014 NM 2008 10 14 SWAA085434 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 747, STR 26R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085433 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727C, STR 21R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081015 EU 2008 10 15 08FDEA04166 1 20081001 A 5321 SRZ25005232LH FLOORBOARD AIRBUS 310 A310222 3930315 EU CABIN DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 MAIN CABIN FLOORBOARD 232 LT IS BROKEN. FABRICATED NEW FLOORBOARD 232 LT IAW FEDEX DWG SRZ 25-005; REV G. 2 L 7 2 4F RT A35EU 20081015 GL 2008 10 15 CHQA200800187 2 20080917 A 7261 OIL SYSTEM EMB 135 EMB135LR 3260305 SO ALLSN AE3007 AE3007A 03030 GL ENGINE OVERSERVICED A CHQA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 11 841RP 145737 CAE311599 FLIGHT 5050, CMH TO LGA. AFTER TAKE OFF AT ALT TO-1 POWER THE FLIGHT CREW RECEIVED A LAV SMOKE EICAS MSG. THE CREW RET URNED TO FIELD AND WHILE DESCENDING TO LAND THE LAV SMOKE INDICATION WENT AWAY AND THE ACFT LANDED WITHOUT INCIDENT. TH ERE WAS NO VISIBLE SMOKE BUT THERE WAS A NOTICEABLE ODOR IN THE ACFT. MX INSPECTED THE ENGINES AND FOUND THAT BOTH ENGI NES OIL RESERVOIRS WERE OVER SERVICED. THE OIL IN BOTH RESERVOIRS WAS DRAINED TO THE CORRECT LEVELS. BOTH ENGINES AND BOTH PACKS WERE RUN WITH NO FURTHER INDICATIONS OR ODORS NOTED. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081015 NM 2008 10 15 Q2SQ746008 1 20080926 A 3240 26056623 BRAKE ASSY BOEING 747 747206B 1384856 NM GE CF6 CF650E2 30018 NE MLG OVERHEATED A Q2SA O OTHER M B A OVER TEMP SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE LD LANDING 1 EA 63 746SA 21111 ACFT LANDED (KDFW) WITH OVERHEATED BRAKES (725 - 800 DEGREES F) AT NR 4, NR 7, NR 9, NR 10, NR 11, NR 15, NR 16 WHEEL PO SITIONS. FLASH FIRE AT NR 7 BRAKE ASSEMBLY. INSPECTED IN ACCORDANCE WITH AMM 05-51-26 AND AMM 32-41-15. R&R NR 7 MAIN WHEEL ASSEMBLY AS PRECAUTION DUE TO HOT BRAKES, IN ACCORDANCE WITH AMM 32-45-01. NO OTHER DEFECTS OR DAMAGE NOTED. 2 L 7 4 4F 4 F RT A20WE E23EA 20081015 NM 2008 10 15 2008UALA05992 1 20081005 A 3397 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHT SEAT 50 RT INOP. RE-SECURED EEL CONNECTOR. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081015 WP 2008 10 15 AALA200802212 1 20080827 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7543A 53025 STL EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK AT AB53 FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081015 WP 2008 10 15 AALA200802208 1 20080827 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7543A 53025 STL EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5100 FOR EMERGENCY LIGHTS AT FORWARD CABIN . SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081015 NM 2008 10 15 AALA200802219 1 20080827 A 3350 GE767 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 191AN 32385 LAX EXTERIOR EMERGENCY LIGHT AT RT NR 1 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT NR 1 DOOR. SYSTEM GR OUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081015 2008 10 15 AALA200802189 4 20080825 A 2565 SLIDE DOUG DC9 DC982 3022082 WP GALLEY DOOR LOOSE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 494AA 49732 ORD INFLIGHT T321/25AUG. AFT GALLEY SLIDE SLID DOWN DOOR. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REINSTALLED AF T GALLEY DOOR SLIDE PACK. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081015 NM 2008 10 15 2008UALA06000 1 20081005 A 3397 80172424 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 785UA 26954 FWD EMERGENCY LIGHT AT SEAT 3F INOP. SECURED CONNECTOR. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081015 NM 2008 10 15 2008UALA06001 1 20081005 A 2530 OVEN BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE GALLEY DIRTY A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 209UA 30215 BURNING PLASTIC ODOR EVIDENT IN BUSINESS CLASS GALLEY PRIOR DEPT. FOUND EVIDENCE OF MELTED PLASTIC INSIDE WARMING OVEN. REMOVED AND CLEANED WARMING OVEN LINER. NOW OK. NO ODOR NOW EVIDENT. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081015 NM 2008 10 15 2008UALA06006 1 20081006 A 3350 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 520UA 24890 THE 1R DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY POWER PACK FOR M730. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 NM 2008 10 15 2008UALA06008 1 20081005 A 2421 745329F IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE UNDERSERVICED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 656UA 25394 RIGHT ENGINE IDG FILTER DPI EXTENDED. UNIT UNDERSERVICED. REPLACED IDG. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081015 NM 2008 10 15 2008UALA06009 1 20081005 A 5310 DOOR FRAME BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 338UA 24242 FWD RIGHT GALLEY DOOR OPENING CRACKED AT AFT LOWER CORNER. INSTALLED DOUBLER REPAIR AT AFT LWR CORNER OF FWD RT GALLEY DOOR OPENING. 2 L 7 2 4F 4 F RT A16WE E21EU 20081015 NM 2008 10 15 AALA200802213 1 20080827 A 3350 LIGHT BOEING 777 777223 1385213 NM SEAT 34C INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 771AN 29579 DFW EMERGENCY LIGHT AT SEAT 34C INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 34C. SYSTEM GROUND CH ECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081015 SO 2008 10 15 C2XA08IA212 1 20080922 A 3320 BR90002 BALLAST EMB 145 EMB145LR 3260212 SO CABIN LIGHTS INOPERATIVE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14952 145067 IAH FLIGHT 2331 THE CREW REPORTED A ODOR OF HOT WIRES COMING FROM TOP OF BULKHEAD IN FRONT OF SEAT 1A WITH NO SMOKE VISI BLE. THE ACFT LANDED AT IAW WITHOUT INCIDENT WHERE MX PLACED THE CABIN LIGHTING ON MEL 33-20-00/1 CAT C CONTROL NR 1547 36 AFTER DISCONNECTING THE BALLAST AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 09/23/08. MX R&R THE BALLAST AT S EAT 2A. OPS CHECKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081015 NM 2008 10 15 2008UALA06011 1 20081006 A 2133 FLAPPER VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN PRESSURE DAMAGED A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 551UA 25399 CREW REPORT: COCKPIT TEMP 90F - CABIN NORMAL. PRESSURIZATION IRREGULAR ON DESCENT DUE TO EXISTING PROBLEM. CABIN CLIM BED TO 8000FT. FOUND CONDITIONED AIR CHECK VALVE FLAPPER DAMAGED. REPLACED FLAPPER. 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 NM 2008 10 15 2008UALA06019 1 20081003 A 2420 1701768 GENERATOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE GENERATING SYS UNDERSERVICED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 787UA 26939 ELEC BACKUP GEN R RIGHT BACKUP GENERATOR OFF DUE TO A PROTECTIVE TRIP. STATUS MSG01- LATCHED CRUISE MODE DEPENDENT; BA CKUP GENERATOR (R) OIL PRESSURE IS LOW. DB- BACKUP CONVERTER MSG-2446090 LATCHD ER MODE. ON ARRIVAL FOUND BACKUP GEN OIL IS ABOVE LOW LEVEL POSITION. SERVICED OIL AND MOTORED ENG, NO LEAK NOTED. CONCURRED WITH SAMC. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081015 NM 2008 10 15 2008UALA06020 1 20081005 A 2432 263BA1011 BATTERY BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE APU INOPERATIVE A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 787UA 26939 THE "BAT CHARGE APU AND APU BATTERY" STATUS DISPLAYED ON LOWER EICAS. REPLACED CHARGER, NO HELP. REPLACED BATTERY & MES SAGE CLEARED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081015 NM 2008 10 15 2008UALA06021 1 20081005 A 2761 B435428 PCU BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE SPOILER DEFECTIVE A UALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 216UA 30549 WITH SPOILERS EXTENDED AIRCRAFT BANKS RIGHT. FOUND FAULTY MECHANICAL SPOILER POWER CONTROL UNIT. REPLACED NR 7 PCU. LEAKS CHECK & OPS CHECK OKAY. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081015 NM 2008 10 15 2008UALA06023 1 20081006 A 5320 WEB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 MAIN CABIN STA 1400-1420, STR 17R, WEB CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED WEB, FABRICATED & INSTALLED A NEW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 CE 2008 10 15 GLB2008F00031 1 20080902 A 2750 1005240731 MOTOR BEECH 1900 1900D 1154162 CE TE FLAP BURNED A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 21 100UX UE100 PILOTS REPORTED A STRONG ODOR OF SMOKE WITH EYE IRRITATION PRESENT ON TAXI. TURNING OFF BLEEDS TO ENVIRO OFF AS WELL AS TURNING OFF MODE CONTROL, DID NOT CHANGE ODOR . THERE WAS NO VISIBLE SMOKE. MAINT TROUBLESHOT AND FOUND THE SMOKE ODOR T O BE A FLAP MOTOR THAT WAS BURNED INTERNALLY AND CAUSED FLAP MOTOR CIRCUIT BREAKER TO POP. MAIT PLACED THE ITEM ON MEL 2 7-2 CAT.B C/N NR 31666. (K) 2 L 7 2 4T RT A24CE 20081015 SO 2008 10 15 C2XA08RI131 1 20080906 A 3230 SEQUENCE VALVE EMB 145 EMB145LR 3260212 SO NLG MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13566 145622 FLIGHT CREW REPORTED THAT DURING CLIMBING OUT, THEY HEARD A SOUND LIKE GEAR WAS STILL DOWN WITH GEAR LEVER UP AND GEAR I NDICATION SHOWING UP POSITION. CREW RECYCLE GEAR TWICE AT AIR SPEED UNDER 200 KT. NOISE ONLY SLIGHTLY CHANGED WHEN GEAR WENT UP. FLIGHT CREW AIR RETURNED TO DEPARTURE UNEVENTFULLY. MX REMOVED AND REPLACED NLG SEQUENCE VALVE, REMOVED AND R EPLACED NLG RT DOOR, AND THIRD UPPER LOCK BOX PROXIMITY SWITCH. MX PERFORMED LEAK AND OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081015 SO 2008 10 15 C2XA08SH117 1 20080910 A 5310 14525302007 DOOR FRAME EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 21154 145772 DURING C-CHECK MAIN DOOR STRUCTURE HAS CORROSION AROUND LOWER NUTPLATE HOLE. MX REPAIRED MAIN DOOR LOWER NUT PLATE HOLES IAW EC 5210-01154. THE ACFT WAS APPROVED TO RETURN FOR SERVICE. (K) 2 L 7 2 4F RT 20081015 NM 2008 10 15 NSVA2008035 1 20081008 A 3260 PIN BOMBDR DHC8 DHC8402 1390042 NM CONNECTOR BENT A NSVA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 187WQ 4187 GREEN NOSE GEAR DOWN LIGHT STAYED ILLUMINATED AFTER GEAR RETRACTION. ALL OTHER GEAR RETRACTION AND EXTENSION INDICATION S NORMAL. ALT GEAR DOWN EXT LIGHTS AGREED WITH THE GEAR HANDLE. STRAIGHTENED SHORTED PIN FOR N/G SAFE INDICATION, PERF ORMED OPS TEST OF PRIMARY EXTEND RET SYSTEM IAW Q400 AMM 32-31-00 TR32-242, OPS CHECK OK. 2 H 7 2 4T RT A13NM 20081015 EU 2008 10 15 SIMA200828201 1 20081008 A 5347 7253799381 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 384AE 18527 5000 340B384 DURING A HMBV INSPECTION THE SEAT TRACK AT 18.3L WAS FOUND TO BE CORRODED FROM FS 296 TO FS 310. REMOVED A 31 INCH SECT ION OF SEAT TRACK. CUT NEW SECTION OF SEAT TRACK MATERIAL P/N 7253799-381 AND U-BEAM MATERIAL 7253799-379. DRILLED, CL EANED AND TREATED REPAIR PARTS. REPAIR DONE IAW SAAB SRM (79LKS 3079 REV 60) CHAPTER 53-70-60. AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4T RT A52EU 20081015 WP 2008 10 15 AALA200802398 1 20080921 A 3350 0202226001 SHROUD DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 554AA 53084 DFW - EMERGENCY LIGHT AT SEAT 29D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 29D. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081015 NM 2008 10 15 SWAA085418 1 20081002 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO FRAME CORRODED AT BS 440, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 SWAA085419 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 22L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 SWAA085420 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 SWAA085426 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 907, STR 22R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 CALA0800955 1 20081007 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 FUSELAGE STATION 827 RT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. CUT OUT DAMAGE AT FUSELAGE STATION 827 BETWEEN S8R AND S9R, FABRICATED AND INSTALLED REPAIR PARTS PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 SWAA085427 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 867, STR 20R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 SWAA085428 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 24R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 SWAA085429 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 19L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 SWAA085430 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 19L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 2008UALA05994 1 20081005 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY CEILING LIGHT ROW 12 INOP. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081015 NM 2008 10 15 2008UALA05995 1 20081005 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHT SEAT 37 LT INOP. RELAMPED, OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081015 NM 2008 10 15 2008UALA05996 1 20081005 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHT ROW 55 LT INOP. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081015 NM 2008 10 15 2008UALA05997 1 20081005 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY CEILING LIGHT ROW 2 INOP. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081015 EA 2008 10 15 COMA0860396 1 20080928 A 2613 355924400 SENSING ELEMENT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE RT PYLON FAILED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 523CA 7821 FLIGHT NR 6264 ON CLIMBOUT FROM GSO TO CVG RECEIVED RT ENGINE 14TH STAGE DUCT MSG. PERFORMED QRH, EMERGENCY DECLARED. A/C DIVERTED TO ROA AND LANDED SAFELY. R&R RT PYLON SENSING ELEMENT A58WK. 2 L 7 2 4F 4 F RT A21EA E15NE 20081015 SO 2008 10 15 C2XA08SH123 1 20080925 A 5320 14525480603 BEAM EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 12160 145799 SHV DURING C CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED AT FRAME 65-68. MX R&R THE AFFECTED BEAM I AW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081015 NM 2008 10 15 AALA200802204 1 20080826 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 184AN 29594 DFW EMERGENCY LIGHT AT SEAT 17D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 17D. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT A2NM 20081015 SO 2008 10 15 C2XA08TY109 1 20080924 A 2820 2770138101 CHECK VALVE EMB 145 EMB145XR 3260214 SO FUEL SYSTEM LEAKING A C2XA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 27 14204 5069 14500968 ACFT DIVERTED FROM GSP TO IAH INTO TYS DUE TO A FUEL LEAK. MX INSPECTED/VERIFIED NO FUEL LEAK AND WAS DISPATCH. ON TAK EOFF THE LEAK REAPPEARED AND MX R&R THE NR 9 WING FLAP VALVE. NO LEAKS NOTED AND WAS RELEASED BACK TO SERVICE. WORK WA S ACCOMPLISHED IAW EMB 145XR 28-11-04. 2 L 7 2 4F RT 20081015 SO 2008 10 15 C2XA08RI133 1 20080907 A 3350 7287580505 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12957 145080 FLIGHT CREW REPORTED EMERGENCY LIGHT FLOOR STRIP FROM ROWS 3A TO 5A INOPERATIVE. MX REMOVED AND REPLACED LIGHT STRIP AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081015 NM 2008 10 15 2008UALA06026 1 20081006 A 5210 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR GOUGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 DOOR R1, DEEP GOUGE UNDERNEATH UPPER HINGE ARM. MAJOR REPAIR ACCOMPLISHED. CUT AND REMOVED DAMAGED SECTION OF FRAME IN NER DOUBLER. FABRICATED & INSTALLED A REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 NM 2008 10 15 2008UALA06027 1 20081006 A 5210 146N610156 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 DOOR 4R, LWR GATE CORRODED. REPLACED LOWER GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 NM 2008 10 15 2008UALA06032 1 20081008 A 5753 6546434370A FLAP BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU RT WING DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 938UA 26671 RIGHT WING INBOARD TRAILING EDGE FLAP HAS A 4 INCH SPLIT AT THE TRAILING EDGE WITH APPROX 3.5 INCHES OF DELAMINATION IN LENGTH. RT AFT FLAP ROUTED TO SHOP FOR REPAIR. FLAP REINSTALLED. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20081015 2008 10 15 2008UALA06034 4 20081008 A 2565 5A29011B ASPIRATOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE EVAC SLIDE DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 676UA PF0202 30028 FAILED AIR RETENTION. REPLACED ASPIRATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081015 EU 2008 10 15 2008UALA06035 1 20081008 A 2133 VFT300A1AMDTA OUTFLOW VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 472UA 1435 VENT SKIN VALVE FAULT, RTFL. FOUND 22HQ CONNECTOR PIN-INSULATION ISSUES. REPLACED SKIN AIR OUTLET VALVE. PUT VALVE AND CIRCUIT BREAKERS BACK TO NORMAL. OPS CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20081015 NM 2008 10 15 SWAA085414 1 20081004 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 263WN 32520 FOUND LT FWD EMERGENCY EXIT FLOOR LIGHT COVER MISSING. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081015 2008 10 15 UIE2008F00044 2 20080908 A 7200 73836222 ISOLATION VALVE BOEING 747 747230B 1384889 NM ENGINE FAILED A UIEA O OTHER J WARNING INDICATION CL CLIMB 1 EA 15 512MC 21220 AIR TURN BACK. DURING CLIMB BOTH LT AND RT MANIFOLD PRESSURE WAS FLUCTUATING. DURING TROUBLESHOOTING AFTER CRUISE POWER SET 103.4, THE NR 1,3, AND 4 PYLONS VALVES WOULD NOT CLOSE. WITH LT AND RT ISOLATION VALVES CLOSED, IT WAS DETERMINED TH AT THE NR 1 PYLON VALVE WAS PARTIALLY OPEN WITH 8 PSI. THE NR 3 AND NR 4 INDICATED STUCK FULL OPEN WITH 38 PSI. APPROX 7 6.0 KG OF FUEL JETTISONED. NR 1,NR 3 AND NR 4 PYLON VALVES REPLACED AND ALL OPERATIONS NORMAL. ALSO NR 3 PRESSURE REGUL ATING VALVE REPLACED AND OPS CHECKED OK. WIRING CHECKS ALSO ACCOMPLISHED AND CHECKED OK. (K) 2 L 7 4 4F RT A20WE 20081015 NM 2008 10 15 UPS08B53476 1 20080108 A 5320 65B09631716 TENSION TIE BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 579UP 26062 INSPECTION TYPE:BCF LT STA 1140 TENSION TIE FWD CHANNEL 5EA FASTENER HOLE CRACKED, LENGTH ABOUT 0.030"; 3EA FASTENER HOL E CRACKED LENGTH MORE THAN 0.030". REPAIRED CRACKED TENSION TIE AS PER SRM 53-40-30 FIG 201. 2 L 7 4 4F RT A20WE 20081015 EA 2008 10 15 ASOA200801304 1 20080927 A 5260 STEP CNDAIR CL600 CL6002C10 1390015 EA ASD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 ASD UPPER STEP LOWER HALF FWD SIDE CRACKED (DOOR OPEN). 2 L 7 2 4F RT A21EA 20081016 SO 2008 10 16 C2XA08IA207 1 20080904 A 3350 20131A BATTERY PACK EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12166 9350 2562 14500831 DURING INSPECTION, THE NR (1) EMERGENCY LIGHT BATTERY WAS FOUND TO BE DEAD. MAINT REMOVED AND REPLACED THE AFFECTED EMER GENCY LIGHT BATTERY. OPS CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (K) 2 L 7 2 4F RT 20081016 CE 2008 10 16 DXTA2008101303301 1 20081011 A 5610 WINDSHIELD CESSNA 650 650 2076802 CE COCKPIT UNKNOWN E DXTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 305QS 6800088 BIRD STRIKE ON T/O: FRONT LEFT WINDSHIELD AND ABOVE. 2 L 7 2 4F A9NM 20081016 SO 2008 10 16 FDK2008F00011 1 20080909 A 3397 WIRE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS BROKEN A FDKA K NONE O OTHER IN INSP/MAINT 1 SW 07 827MJ 145217 BOTH LOWER EXIT SIGNS AND 2 FLOOR STRIPS INOPERATIVE. MX REPAIRED BROKEN WIRE AT LOWER ASSY. (K) 2 L 7 2 4T RT T00011AT 20081016 NE 2008 10 16 RU32008F00000 2 20080814 A 7200 ENGINE BEECH 300 300BEECH 1152930 CE PWA PT6 PT6A60A 52043 NE LEFT FAILED E RU3A A UNSCHED LANDING E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 15 72 FF7 PCE95331 CLIMBING THRU 7300`, AT CLIMB POWER, HEARD A PRONOUNCED POP, FELT THE ACFT YAW LT AND FELT A DECELERATION. THE PILOT FLY ING CONFIRMED THAT THE LT ENGINE HAD SHUTDOWN AND THE PROP HAD FEATHERED. ATC WAS NOTIFIED AND EMERGENCY WAS DECLARED. T HE ENGINE FAILURE IN FLIGHT EMERGENCY CHECKLIST WAS COMPLETED AS WELL AS THE SINGLE ENGINE LANDING CHECKLIST. AFTER AN U NEVENTFUL LANDING AND TAXI OFF OF THE RUNWAY, THE SHUTDOWN CHECKLIST WAS ACCOMPLISHED AND THE ACFT WAS TOWED TO THE HANG ER. (K) 2 L 7 2 4T 4 T A24CE E4EA 20081016 SO 2008 10 16 C2XA08RI132 1 20080906 A 3200 UNKNOWN EMB 145 EMB145LR 3260212 SO NLG MALFUNCTIONED A C2XA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 27 13566 145622 FLIGHT CREW REPORTED THAT DURING CLIMBING OUT, THEY HEARD A SOUND LIKE GEAR WAS STILL DOWN WITH GEAR LEVER UP AND GEAR I NDICATION SHOWING UP POSITION. CREW RECYCLE GEAR TWICE AT AIR SPEED UNDER 200 KT, NOISE ONLY SLIGHTLY CHANGED WHEN GEAR WENT UP. FLIGHT CREW AIR RETURNED TO DEPARTURE UNEVENTFULLY. MX REMOVED AND REPLACED NLG SEQUENCE VALVE , REMOVED AND R EPLACED NOSE LANDING GEAR RT DOOR AND THIRD UPPER LOCK BOX PROXIMITY SW. MX PERFORMED LEAK AND OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081016 SO 2008 10 16 C2XA08RI135 1 20080907 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14905 145476 DURING ROUTINE MAINT MX FOUND SEVERAL PROXIMITY FLOOR EMERGENCY LIGHT STRIPS INOPERATIVE. MX REMOVED AND REPLACED EMERG ENCY LIGHT INVERTER POSITION 6 AND PERFORMED OPS CHECK SUCCESSFULLY. AC WAS APPROVED TO RETURN TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081016 2008 10 16 A6WA200840592 4 20080923 A 3418 3995100208 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING FAILED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 27304 9033 7781 STALL FAIL MESSAGE ON CLIMB OUT, COMPLIED WITH QRH. ACCOMPLISHED FIM 27-30-00 LRU DIAGNOSTICS REFLECTS SPC2 INTERNAL FA ILURE. REMOVED, REPLACED, AND TESTED SPC COMPUTER IAW AMM 27-35-01, OPS CHECK GOOD. (K) 2 L 7 2 4F RT A21EA 20081016 EA 2008 10 16 ASOA200801321 1 20081003 A 5312 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 846AS 7328 WHILE PERFORMING TASK AWL253-41-201, AN INDICATION WAS NOTED AT THE 559 BULKHEAD CAP ANGLE RADIUS LBL 9 AND LBL 18 APPRO X .500 INCH IN LENGTH. ACCOMPLISHED REPAIR TO (LT SIDE ONLY) 559 BULKHEAD AND CAP ANGLE IAW REO 601R-53-41-260 REV C. REQUIRES PAINT. PAINTED LT SIDE OF BULKHEAD AND CAP ANGLE IAW SRM 51-25-16. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV C. 2 L 7 2 4F RT A21EA 20081016 NM 2008 10 16 DHLA2008745507 1 20080910 A 5320 ATTACH FITTING BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA O OTHER O OTHER UK UNKNOWN 1 SO 01 745DH 20665 UPPER FUSELAGE COCKPIT BS 294 ATTACH CLIP CRACKED AT STRINGER 12L. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 SWAA085500 1 20081009 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CRACKED AT BS 348, 16L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085507 1 20081009 A 3350 PL2230LH0 STRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 756SA 27872 FOUND EEPLS STRIP LOOSE AT ROW 8. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085448 1 20081007 A 5330 6545768 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT BS 380, STR 15R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085450 1 20081007 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND FLOORBEAM CORRODED AT BS 344, RBL 12, WL 207. REPAIRED BEAM PER PAE ER. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 08FDEA04154 1 20081001 A 5753 ARC198413 HINGE BRACKET DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 LT WING OUTBOARD FLAP ASSEMBLY INBOARD HINGE BRACKET ARC1984 MOUNTING BORE HOLE INBOARD NR 2 FOUND WITH PITTING CORROSIO N. INBOARD NR 2 MOUNTING BORE HOLE AT LT WING OUTBOARD FLAP ASSY INBOARD HINGE BRACKET ARC1984 REPAIRED AS PER E.A. NR 1-5750-122573. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081014 EU 2008 10 14 08FDEA04109 1 20080929 A 5321 SRZ25005242NJ FLOOR PANEL AIRBUS 310 A310222 3930315 EU CABIN CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 MAIN CABIN FLOOR PANEL 242 NJ IS CRACKED. FABRICATED A NEW FLOOR PANEL 242 NJ IAW FEDEX DWG SRZ 25-005; REV G. 2 L 7 2 4F RT A35EU 20081014 NM 2008 10 14 UPS08B53473 1 20080108 A 5311 65B0965416 FAILSAFE BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 579UP 26062 INSPECTION TYPE:BCF STA 1220 RT TENSION TIE FRAME FAILSAFE CHORD 1EA FASTENER HOLE CRACKED MORE THAN 0.050". REPAIRED C RACKED FAILSAFE CHORD AS PER SRM 51-70-11. 2 L 7 4 4F RT A20WE 20081014 NM 2008 10 14 SWAA085445 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 727C, STR 22R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085443 1 20081007 A 3350 8100 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 467WN 33830 DURING SCHEDULED MV2 CHECK, FOUND FLOOR PROXIMITY LIGHT AT OVERWING EXIT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081014 NM 2008 10 14 SWAA085439 1 20081005 A 5315 BAC1509 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOORBEAM CORRDED AT BS 767 + 5, LBL 3. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081014 EA 2008 10 14 SWIA200820103 1 20080928 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 935SW 7725 FLT 5966 - CEILING EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081014 EA 2008 10 14 SWIA200820108 1 20080930 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 807SK 15082 FLT 3784 - CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081015 SO 2008 10 15 RAIA00809010 1 20080908 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN NOT SEATED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 815HK 145048 EMERGENCY LIGHT IN THE CABIN INOPERATIVE. MAINT RESEATED THE CONNECTOR TO THE AFFECTED LIGHT ASSEMBLY. OPS CHECKED GOOD . (K) 2 L 7 2 4T RT T00011AT 20081015 SO 2008 10 15 C2XA08ON178 1 20080901 A 3150 WARNING MESSAGE EMB 145 EMB145XR 3260214 SO FALSE ACTIVATION A C2XA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 27 11192 14500936 FLIGHT CREW REPORTED E1 T/R DISAGREE ON T/O ROLL. FLIGHT CREW CYCLED NR 1 T/R AND COULD NOT DUPLICATE MSG. OPERATIONALL Y CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (K) 2 L 7 2 4F RT 20081015 EA 2008 10 15 VNA2008F00007 1 20080908 A 3397 FEEDER CABLE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DAMAGED A VNAA O OTHER O OTHER NR NOT REPORTED 1 GL 05 251PS 7931 CREW REPORTED THE EMERGENCY LIGHTS FROM ROW 2 TO ROW 5 DID NOT WORK. MAINT REMOVED AND REPLACED CABLE AT ROW 6. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE. (K) 2 L 7 2 4F RT A21EA 20081015 NM 2008 10 15 SWAA085431 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 18L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 SWAA085432 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 18L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081015 NM 2008 10 15 UPS08B53482 1 20080108 A 5320 65B09631718 TENSION TIE BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 579UP 26062 INSPECTION TYPE:BCF STA 1180 TENSION TIE LT FWD CHANNEL 6EA FASTENER HOLE CRACK ABOUT OR MORE THAN 0.030". REPLACED CRA CKED TENSION TIE AS DWG 65B09631 AND SRM 51-40-02. 2 L 7 4 4F RT A20WE 20081015 NM 2008 10 15 UPS08B53483 1 20080108 A 5311 65B0175223 FRAME BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 579UP 26062 INSPECTION TYPE:BCF STA 1180 LT TENSION TIE FRAME WEB 2EA FASTENER HOLE CRACKED MORE THAN 0.030". REPAIRED CRACKED FRA ME WEB AS PER SRM 53-40-07. 2 L 7 4 4F RT A20WE 20081015 NM 2008 10 15 UPS08M53488 1 20080818 A 5753 HINGE DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A LT WING O/B FLAP I/B FWD HINGE LOWER MOUNT O/B BORE FWD & AFT SPOT FACE CORRODED. LT WING O/B FLAP I/B FWD HINGE LOWER MOUNT O/B BORE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN DWG ARC0502 LIMIT. R EPAIR CARRIED OUT AS PER CMM 57-44-08. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 UPS08M53489 1 20080818 A 5753 HINGE DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A LT WING O/B FLAP I/B FWD HINGE LOWER MOUNT O/B BORE CORRODED. LT WING O/B FLAP I/B FWD HINGE LOWER MOUNT O/B BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 UPS08M53490 1 20080818 A 5753 HINGE DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A LT WING O/B FLAP I/B FWD HINGE UPPER MOUNT O/B BORE FWD & AFT SPOT FACE CORRODED. LT WING O/B FLAP I/B FWD HINGE UPPER MOUNT O/B BORE FWD & AFT SPOT FACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 UPS08M53491 1 20080816 A 5753 HINGE DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A RT WING O/B FLAP O/B AFT HINGE UPPER MOUNTING CENTER BORE CORRODED. RT WING O/B FLAP O/B AFT HINGE UPPER MOUNTING CENTER BORE CORROSION REMOVED AS PER BSOPM 20-11-02 AND FOUND WITHIN LIMIT AS PER DWG ARC1991. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 UPS08M53492 1 20080816 A 5753 HINGE DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A RT WING O/B FLAP O/B AFT HINGE I/B PIVOT I/B SPOTFACE CORRODED. RT WING O/B FLAP O/B AFT HINGE I/B PIVOT I/B SPOTFACE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-52-04. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 UPS08M53493 1 20080816 A 5753 HINGE DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A RT WING O/B FLAP AFT HINGE O/B PIVOT BORE CORRODED. RT WING O/B FLAP O/B AFT HINGE O/B PIVOT BORE C ORROSION REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-52-04. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 UPS08M53497 1 20080818 A 5753 HINGE DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A LT WING O/B FLAP O/B FWD HINGE UPPER MOUNT I/B BORE FWD SPOTFACE CORROSION. LT WING O/B FLAP O/B FW D HINGE UPPER MOUNT I/B BORE FWD SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 UPS08M53498 1 20080818 A 5753 HINGE DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A LT WING O/B FLAP O/B FWD HINGE BARREL NUT LOWER BORE CORRODED. LT WING O/B FLAP O/B FWD HINGE BARRE L NUT LOWER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09. 2 L 7 3 4F RT A22WE 20081015 NM 2008 10 15 UPS08M53499 1 20080818 A 5753 HINGE DOUG MD11 MD11F 3023600 NM T/E FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A LT WING O/B FLAP O/B FWD HINGE LOWER MOUNT O/B BORE CORRODED. LT WING O/B FLAP O/B FWD HINGE LOWER MOUNT O/B BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09. 2 L 7 3 4F RT A22WE 20081015 2008 10 15 ASAA0853559 4 20081006 A 3442 6225129105 RADAR BOEING 737 737890 1384527 NM COCKPIT MALFUNCTIONED A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 558AS 8831 35177 THE RADAR HAS INTERMITMENT SPOKES OF GREEN AND YELLOW ALONG WITH NORMAL WX RETURNS. UNABLE TO CONFIRM FAULT. WXR SYSTE M TEST GOOD REF MM 34 43 00. FLT CREW CHECK WXR OPS NORMAL. VERIFICATION FLT SATISFACTORY. 2 L 7 2 4F RT A16WE 20081015 CE 2008 10 15 DXTA200803298 1 20081009 A 2120 UNKNOWN RAYTHN 900 HAWKER900XP 4220011 CE COCKPIT ODOR E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 890QS HA0010 INTERMITTENT BURNING SMELL FUMES IN COCKPIT (NO VISABLE SMOKE). 1 L 7 2 4F RT A3EU 20081015 CE 2008 10 15 DXTA200803299 1 20081009 A 3240 BRAKE SYS RAYTHN DH125 HAWKER800XP 7150012 CE MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 872QS 258472 ON LEFT SIDE (CAPT'S SIDE) NO BRAKE PRESSURE ON LEFT PEDAL. LEFT PEDAL GOES TO THE FLOOR. 2 L 7 2 4F RT A3EU 20081015 CE 2008 10 15 DXTA200803300 1 20081009 A 3260 WARNING SYSTEM CESSNA 560 560XL 2076702 CE COCKPIT ACTIVATED E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 698QS 5605653 WHEN LANDING GEAR WAS SELECTED DOWN, THE "RT" GREEN LIGHT ILLUMINATED. THE "LT" GREEN LIGHT DID NOT ILLUMINATE AND THE RED "UNLOCK" LIGHT REMAINED ILLUMINATED. 2 L 7 2 4F RT A22CE 20081015 SO 2008 10 15 SIMA200828001 1 20081001 A 3233 23093700503 ACTUATOR EMB 135 EMB135KL 3260302 SO MLG CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 850AE 13819 145722 WHILE PERFORMING BACKLASH INSPECTION PER AMM WHILE AIRCRAFT WAS IN MAINTENANCE IT WAS DISCOVERED THAT BOTH THE MAIN LAND ING GEAR MANEUVERING ACTUATORS HAD BACKLASH PLAY BEYOND LIMITS OF AMM. IT WAS DETERMINED THAT THE PLAY WAS THE RESULT O F CORROSION. ACTUATORS TDMI FOR 50 CYCLES. REMOVED AND REPLACED LEFT AND RIGHT MANEUVERING ACTUATORS OPERATIONAL CHEC K GOOD IAW EMB AMM32-33-08. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081015 NE 2008 10 15 Q2SA789001 2 20081010 A 7230 COMPRESSOR BOEING 747 747341 13848AM NM GE CF6 CF650E2 30018 NE NR 2 ENGINE STALLED A Q2SA E B ENGINE SHUTDOWN EMER. DESCENT J R WARNING INDICATION PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 63 789SA 23394 517369 EN ROUTE FROM SPIM TO KMIA DURING CLIMB AND CRUISE, NR 2 ENGINE EXPERIENCED HIGHER EGT READING (70 DEG) THAN OTHER ENGIN ES. REDUCED THRUST SETTINGS ON NR 2 ENGINE LOWERED HIGHER EGT READING TO 30 DEG ABOVE OTHER ENGINES, WITH NO ROUGHNESS OR APPARENT ENGINE INSTABILITY. APPROXIMATELY 2 HOURS, 44 MINUTES INTO CRUISE FLIGHT, ENGINE NR 2 EXPERIENCED SEVERAL R APID COMPRESSOR STALLS WITH AUDIBLE BANGS, ALSO RESULTING IN RAPID DROP OF N1. ENGINE IMMEDIATELY CUTOFF, AND PILOT PER FORMED DESCENT FROM FL320 TO FL300, WITH SUBSEQUENT CONTINUATION OF FLIGHT TO KMIA. NO FUEL WAS DUMPED. SUBSEQUENT BOR ESCOPE INSPECTION PERFORMED. ENGINE CHANGE REQUIRED. 2 L 7 4 4F 4 F RT A20WE E23EA 20081015 CE 2008 10 15 NSVA2008036 1 20081009 A 2913 11438800013 POWERPACK BEECH 1900 1900D 1154162 CE FAULTY A NSVA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 27 171CJ UE71 ON ILS TO 22L (BOS) PUT THE LANDING GEAR DOWN AND GOT A WARNING INDICATION HAD TO INITIATE A GO-AROUND AND PERFORM ABNOR MAL GEAR EXT. INSTALLED HYD POWER PACK LANDING GEAR MOTOR RELAY AND NEW LANDING GEAR POWER CB AND REINSTALLED CB IAW BE ECH 1900D 24-00-00. PERFORMED LANDING GEAR, OPS CHECK IAW CWC 32-30-01. 2 L 7 2 4T RT A24CE 20081015 CE 2008 10 15 DXTA2008101403305 1 20081013 A 3260 WARNING LIGHT RAYTHN DH125 HAWKER800XP 7150012 CE COCKPIT ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 873QS 258573 ON GEAR RETRACTION RIGHT MAIN GEAR RED INDICATOR REMAINED LIT. 2 L 7 2 4F RT A3EU 20081016 NM 2008 10 16 SWAA085483 1 20081008 A 5322 6546569 SHEAR TIE BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CORRODED AT BS 947.5, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085489 1 20081008 A 5313 BAC1498 STRINGER BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED MV2 CHECK, FOUND STRINGER CORRODED BS 907, STR 25L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085512 1 20081010 A 3350 417A5900 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 233LV 32501 DURING SCHEDULED HC2 CHECK, AFT LT EMERGENCY EXIT LIGHT BATTERY FAILED TEST. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085517 1 20081012 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 20L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085520 1 20081012 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085509 1 20081012 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 379, BL 0. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 08FDEA04179 1 20081003 A 5310 146N5610 CREASE BEAM BOEING 757 75723A 1384967 NM BS 1380-1400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 MAIN CABIN BS 1380-1400,RT SIDE O.B. CREASE BEAM CHORD HAS CORROSION. REMOVED CORROSION IAW 51-00-53,CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW 53-60-13, SUMITTED E.A.R FOR REPAIR. WORKED DAMAGE PER EA F-5310-123912. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04182 1 20081003 A 5310 CREASE BEAM BOEING 757 75723A 1384967 NM BS 1390-1630 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 MAIN CABIN BS 1620-1640,RT SIDE CREASE BEAM HAS CORROSION. REMOVE CORROSION AND CHECK LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-03. REMOVED CREASE BEAM, FABRICATED BEAM IAW SRM 51-10-02 SECTION 8 . LOCATED AND DRILLED, TREATED AND PRI MED AND INSTALLED IAW 51-40-02. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 SWAA085525 1 20081012 A 5312 BAC1490 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD CHORD CORRODED AT BS 270, LBL 8 TO LBL 10, WL 208. REMOVED AND REPLACED CHOR D PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085526 1 20081012 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CRACKED AT BS 328, RBL 11, WL 206. REPAIRED BEAM PER PAE ER. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085530 1 20081013 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 8R. REMOVED AND REPLACED CLIP PER SI. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085531 1 20081013 A 3350 101331 SIGN BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 FOUND FWD OVERHEAD EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LENS ASSY PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085549 1 20081012 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 791, ABOVE STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085552 1 20081012 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 757, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 08FDEA04195 1 20081003 A 5310 CREASE BEAM BOEING 757 75723A 1384967 NM BS 418-430 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 MAIN CABIN CREASE BEAM BS 391, THERE IS A MISDRILLED HOLE ,AND BS 430-418 HAS CORROSION RT. REMOVED AND REPLACED CREASE BEAM BS 297-395 IAW SRM 51-40-02. FABRICATED ON MAE TRAVELER T8/760162. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" M AJOR REPAIR. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04198 1 20081004 A 5347 SEAT TRACK BOEING 757 75723A 1384967 NM BS 900-1076 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 MAIN CABIN, SEAT TRACK BS 900-1076 LBL 24.75 CROWN SCRATCHES AND GOUGED REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40--0 2 AND SRM 53-00-52, MAJOR REPAIR NO FOLOW-UP REQUIRED. 2 L 7 2 4F RT A2NM 20081015 CE 2008 10 15 DJFA2008072 1 20081010 A 2170 COALESCER BAG BEECH MU300 400A 1155402 CE CABIN AIR ODOR E DJFA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 23 686TA RK328 DURING DESCENT, AFTER INITIATING ENGINE ANTI-ICE, CREW NOTED A BURINING SMELL IN THE CABIN. AIRCRAFT LANDED SAFELY. MA INTENANCE COULD NOT DUPLICATE THE DISCREPANCY. THE COALESCER BAG WAS REPLACED AS A PRECAUTIONARY MEASURE. 2 H 7 2 4F RT A16SW 20081015 2008 10 15 DJFA2008073 4 20081012 A 3460 C500H EFB RAYTHN DH125 HAWKER800XP 7150012 CE COCKPIT MALFUNCTIONED E DJFA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 23 829LX 258466 PRIOR TO DEPARTURE, CREW NOTED BURNING SMELL IN THE COCKPIT THE FOUND EFB INOPERATIVE IN THE COPILOTS SIDE. SUSPECT EFB WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A3EU 20081015 CE 2008 10 15 DJF2008F00015 1 20080820 A 2150 73838433 ACM CESSNA 750 750 2076810 CE A/C BAY FAILED E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 23 701LX 4522 7500114 DURING DESCENT THRU 35000 WE EXPERIENCED A LOUD EXPLOSION FOLLOWED WITH A FOUL CHEMICAL ODOR. MAINT REMOVED FAILED COCK PIT (AFT) TURBINE ASSY AND INSTALLED A REPAIRED UNIT. (K) 2 L 7 2 4J RT T00007WI 20081015 2008 10 15 DXTA2008101503306 4 20081014 A 3160 DISPLAY CESSNA 560 560XL 2076702 CE COCKPIT FAILED E DXTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 651QS 5605251 LOST PFD ON CAPTAINS SIDE AND MFD ON TAKEOFF (70KT) ROLL. 2 L 7 2 4F RT A22CE 20081015 WP 2008 10 15 DHLA200800112 1 20081009 A 2612 FIRE WARNING DOUG DC8 DC873 302199C WP COCKPIT MALFUNCTIONED A DHLA K NONE N FALSE WARNING CR CRUISE 1 GL 05 807DH 45990 PRIOR TO DESCENT NR 3 FIRE WARNING HANDLE ILLUMINATED AND MASTER FIRE WARNING BELL SOUNDED INTERMITTENTLY THEN EXTINGUIS HED FIRE LOOP TESTED OK. RESOLUTION DESCRIPTION: XFERRED TO DMI 33829 PER MEL 26-2-3 PLACARD NR 3 ENG "B" LOOP INOP. CAT C & MXC NOTIFIED. 2 L 7 4 4F RT 4A25 20081015 EU 2008 10 15 YENA200810100008 1 20081009 A 2910 D29010102008001 HYDRAULIC LINE AIRBUS 320 A320232 3930326 EU NR 1 PYLON LEAKING A YENA K NONE K FLUID LOSS CR CRUISE 1 EA 15 640JB 9569 2832 IN CRUISE, INBOUND SJC-JFK, LOSS GREEN HYD SYS PRESSURE, FOUND HYDRAULIC CASE RETURN LINE LEAKING IN NR 1 ENGINE PYLON. REMOVED AND REPLACED NR 1 ENG HYDRAULIC CASE RETURN LINE & REMOVED AND REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP PRECA UTIONARY DUE TO TOTAL HYD FLUID LOSS PER AMM 29-11-51-04. SERVICED GREEN SYSTEM HYD RESERVOIR PER AMM 12-12-29-611-001, OPS LEAK CHECK OK. 2 L 7 2 4F RT A28NM 20081015 NM 2008 10 15 USAASB08094 1 20081009 A 3260 BACC18Z3R CIRCUIT BREAKER BOEING 737 7374B7 1384702 NM COCKPIT FAULTY A USAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 19 435US 24557 ON APPROACH TO PBI, WITH GEAR HANDLE DOWN, CAPTAIN REPORTED HAD NO INDICATION THAT GEAR WAS DOWN. THE ONLY GEAR INDICAT ION WAS A NOSE GEAR RED LIGHT. AT FLYBY THE TOWER CONFIRMED GEAR WAS DOWN. FIRST OFFICER CHECKED THE VIEWERS AND VERIF IED GEAR WAS DOWN AND LOCKED. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. AN EMERGENCY WAS DECLARED . MAINTENANCE JACKED AIRCRAFT AND DUPLICATED FAULT WITH CIRCUIT BREAKER C404 OPEN. REMOVED AND REPLACED CIRCUIT BREAKE R C404 AND ACCOMPLISHED SATISFACTORY CHECK OF WIRING FOR SHORTS AND OPENS FROM C404 TO D2598, PINS 1 AND 18, IN ASSOCIAT ION WITH WDM 32-31-11 AND 32-64-11. SWUNG GEAR NUMEROUS TIMES WITH NO FURTHER FAULTS. 2 L 7 2 4F RT A16WE 20081015 EA 2008 10 15 ASOA200801305 1 20081006 A 5320 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 921EV 7819 CARGO DOOR SUPPORT BEAM LOWER ANGLE CRACKED .3 INCH LONG AT FS 621 BULKHEAD. 2 L 7 2 4F RT A21EA 20081015 EA 2008 10 15 ASOA200801308 1 20081006 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 PAX DOOR AFT WEB IS CRACKED IN 2 PLACES IN ZONE 4 APPROX .125 X .500. COMPLIED W/STEPS 1, 4, 5, 6 & 7 OF BOMBARDIER REO 601R-52-11-702. NDT REQ'ED. PERFORMED EDDY CURRENT INSPECTION ON PAX DOOR AFT WEB IN ZONE 4 CUTOUTS. NO REJECTABLE I NDICATIONS FOUND AT THIS TIME. REPORT ATTACHED IAW STEP 2 OF BOMBARDIER REO 601R-52-11-702A AND CRJ NDTM 51-20-06. RES TORE FINISH IS REQUIRED. COMPLIED W/STEPS 3, 8 & 10 OF BOMBARDIER REO 601R-52-11-702. PAINT REQ'ED. EDGE SEALED REPAI R AND PAINTED IAW REO 601R-52-11-702 STEPS 11 AND 12. COMPLIED W/STEPS 13 THROUGH 17 OF BOMBARDIER REO 601R-52-11-702. SUPPLEMENTAL-SDR CLOSED 11/13/2008. 2 L 7 2 4F RT A21EA 20081015 EA 2008 10 15 ASOA200801310 1 20081007 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 921EV 7819 OUTBOARD FLOOR SUPPORT CLIP CRACKED AT FS 280, RBL 9. 2 L 7 2 4F RT A21EA 20081015 EA 2008 10 15 ASOA200801311 1 20081007 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 921EV 7819 RIGHT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED 1 INCH. REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE WITH NEW IAW REO 610R-53-41-059 REV A. 2 L 7 2 4F RT A21EA 20081015 EA 2008 10 15 ASOA200801312 1 20081008 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 PAX DOOR STUCK CLOSED, WILL NOT OPEN FROM OUTSIDE. 2 L 7 2 4F RT A21EA 20081015 EA 2008 10 15 ASOA200801313 1 20081008 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 839AS 7284 UNABLE TO OPEN PAX DOOR FROM OUTSIDE. -REPEAT- 2 L 7 2 4F RT A21EA 20081016 SO 2008 10 16 CHQ2008F00010 1 20080912 A 3350 3025103 LIGHT EMB 135 EMB135LR 3260305 SO LT OVERWING INOPERATIVE A CHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 834RP 145696 MAINT FOUND THE LT AFT OVER-WING EMERGENCY LIGHT INOPERATIVE. MAINT REPLACED THE LT AFT EMERGENCY FLIGHT ASSY IAW MM 30- 2510-3 AND OPS CHECKED THE EMERGENCY LIGHT SYSTEM GOOD. (K) 2 L 7 2 4F RT T00011AT 20081016 EU 2008 10 16 DGC2008F00002 1 20080912 A 7920 30753851 LINE BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE7315R 01518 WP OILPRESSURE CRACKED E DGCA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 5119 7529 258177 P91479 AT CRUISE FLIGHT, AFTER 1 HR 27 MIN INTO FLIGHT, THE LT OIL PRESSURE INDICATOR FLUCTUATED FROM APPROXIMATELY 42-45 PSI D OWN TO 30-35 PSI TWICE PER SECOND CONTINUOUSLY. OIL TEMP REMAINED NORMAL, ALL OTHER ENGINE INDICATIONS NORMAL, (N1, ITT, N2). APPROXIMATELY 4-6 MINUTES LATER THE OIL PRESSURE INDICATOR FLUCTUATED DOWN TO 25-35 PSI, THE LT ENGINE "OIL PRESS LOW" ANNUCIATOR ILLUMINATED. THE SIC REDUCED POWER TO IDLE, EXECUTED SHUTDOWN PROCEDURES IAW CHECKLIST PROCEDURE. THE P IC DECLARED AN EMERGENCY AND DIVERTED . THE LT ENGINE OIL FILTER BYPASS INDICATOR WAS FOUND POPPED, METAL PIECES WERE F OUND IN THE FILTER AND TRANSFER GEARBOX, AND THE NR 6 BEARING, OIL PRESSURE LINE WAS FOUND CRACKED. (K) 2 L 7 2 4F 4 F RT A3EU E6WE 20081016 SO 2008 10 16 C2XA08TY104 1 20080910 A 3350 82321 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13969 22368 145141 ACFT WAS IN FOR A SERVICE/ ROUTINE CHECK AND THE EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLA CED LIGHT IAW AMM 33-50-09. OPS CHECK GOOD AND WAS RELEASED TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081016 SO 2008 10 16 C2XA08TY105 1 20080911 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18982 21000 145223 ACFT WAS FOUND WITH THE LT SIDE EMERGENCY LIGHT INOPERATIVE. MAINT REMOVED AND REPLACED THE EMERGENCY LIGHT BULB. OPS C HECK GOOD AND WAS RELEASED TO SERVICE. WORK WAS ACCOMPLISHED IAW AMM 33-50-10. (K) 2 L 7 2 4T RT T00011AT 20081016 EA 2008 10 16 A6WA200840591 1 20080922 A 2910 HYDRAULIC SYSTEM CNDAIR CL600 CL6002B19 1900309 EA NR 2 LEAKING A A6WA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 31 402AW 7281 SHORTLY AFTER TAKEOFF, EICAS NR 2 HYDRA LOW PRESSURE, NR 2 HYDRAULIC QUANTITY 5 PERCENT. COMPLIED WITH QRH, RETURNED TO LAND. FLUID DRIPPING FROM AFT EQUIPMENT BAY. OPERATED 35 MINUTES AT 5 PERCENT INDICATED. (K) 2 L 7 2 4F RT A21EA 20081016 SO 2008 10 16 C2XA08RI134 1 20080910 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 27 16961 145103 FLIGHT CREW REPORTED A FAINT SMOKE ODOR IN CABIN DURING TAKEOFF. MX RAN BOTH ENGINES AND AIR CONDITIONING PACK AND COUL D NOT DUPLICATE THE PROBLEM. ACFT WAS APPROVED TO RETURN TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081016 CE 2008 10 16 DXTA2008101303303 1 20081012 A 3240 BRAKE SYS CESSNA 500 560CESSNA 2076750 CE MALFUNCTIONED E DXTA K NONE O OTHER TX TAXI/GRND HDL 1 GL 07 353QS 5600530 CO-PILOTS BRAKES LEFT PEDAL MOVES ABOUT 1 INCH THEN GRABS, RIGHT PEDAL MOVES .5 INCH THEN GRABS. 2 L 7 2 4F RT A22CE 20081016 EA 2008 10 16 ASOA200801318 1 20080929 A 5414 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT NACELLE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 RT ENG LIPSKIN HAS CORROSION ON L/E IN SEVERAL AREAS. COMPLIED WITH CMM 71-61-01-200-802-A01. PERFORMED ULTRASONIC INS PECTION OF RT NOSE INLET LIPSKIN IAW WVAC. FOUND RT NOSE INLET LIPSKIN TO BE WITHIN LIMITS. REQUIRES BLEND IN PITTING AREAS. BLENDED RT ENG LIPSKIN IAW CMM 71-61-01-200-802-A01. POLISHED LIPSKIN IAW MM 51-27-00-140-801. COMPLIED WITH CMM 71-61-01-200-802-A01. PERFORMED ULTRASONIC THICKNESS MEASUREMENT OF RT ENGINE NOSE INLET LIPSKIN REPAIRED AREAS C, D, & E. ALL ZONES FOUND TO BE WITHIN LIMITS. 2 L 7 2 4F RT A21EA 20081016 EA 2008 10 16 ASOA200801323 1 20081006 A 5230 TRACK CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 921EV 7819 CARGO DOOR FWD TRACK U-CHANNEL CRACKED .1 INCH LONG AT BOTTOM OF TRACK. 2 L 7 2 4F RT A21EA 20081016 EA 2008 10 16 ASOA200801324 1 20081010 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 846AS 7328 AT FS 718.0 BETWEEN STRINGERS 11L AND 13L PREVIOUSLY REPAIRED ATTACH ANGLES ARE CRACKED IN RADIUS (2 EA). REMOVED PREVI OUS REPAIRS FROM FS 718.0 BETWEEN STRINGERS 11L AND 12L IAW CRJ 200 SRM 51-42-06 AND 51-42-21. CUTLINE AS PER REO 601R- 53-61-193 AND CRJ 200 NDTM 51-20-08. NO INDICATIONS NOTED AT THIS TIME. REPAIRED FS 718.00 BETWEEN STRINGERS 11L AND 1 2L IAW STEPS 2 THROUGH 6 OF BOMBARDIER REO 601R-53-61-193. STEP 1 OF BOMBARDIER REO 601R-53-61-193 TRIM OUT OF FLANGE W AS PREVIOUSLY COMPLIED WITH. ALL WORK WAS COMPLIED WITH IAW ASA EO 600-53-0067 REV A. SUPPLEMENTAL-SDR CLOSED 11/13/20 08. 2 L 7 2 4F RT A21EA 20081016 NM 2008 10 16 DHLA2008745502 1 20080901 A 5320 ATTACH FITTING BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 745DH 20665 LOWER FUSELAGE E&E COMPARTMENT BS 460 ATTACH CLIPS CRACKED AT STRINGERS 20L & 22L. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 DHLA2008745511 1 20080921 A 5322 69445662 SHEAR TIE BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 FRAME TO SKIN SHEAR TIE CRACKED, BS 950D, BETWEEN STR 13R AND 14R. REMOVED AND REPLACED SHEAR TIE PER B727 SRM 51-10-1 AND 51-30-2. REF N/R 4987-2-420. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 DHLA2008745513 1 20080912 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 MAIN FRAME AT BS 720D HAS DOUBLE DRILLED HOLES IN UPPER FLANGE, AT STR 8R. ACCOMPLISHED FRAME REPAIR PER B727 SRM 53-10 -4 FIG 2. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 SWAA085496 1 20081009 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 706, RBL 45. REMOVED AND REPLACED BEAM PER DHN EA. 2 L 7 2 4F RT A16WE 20081016 CE 2008 10 16 DJFA2008071 1 20081007 A 2110 MOTOR BEECH MU300 400A 1155402 CE COMPRESSOR INOPERATIVE E DJFA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 466CW 1458 RK366 DURING FLIGHT, AIR CONDITIONING CIRCUIT BREAKER POPPED; CREW NOTED A BURNING ODOR. AIRCRAFT LANDED SAFELY. MX FOUND TH E COMPRESSOR MOTOR FIALED. THE MOTOR WAS REPLACED. 2 H 7 2 4F RT A16SW 20081016 NM 2008 10 16 SWAA085505 1 20081009 A 3350 100031 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 783SW 29809 DURING SCHEDULED 8Y CHECK, FOUND EMERGENCY EXIT LIGHT BROKEN ON G4 O/B AFT WALL. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085474 1 20081008 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED 14Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 360 TO BS 380 AT STR 17R. REMOVED AND REPLACED BEAM P ER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085479 1 20081008 A 3260 1061337 SENSOR BOEING 737 7373H4 1384600 NM MLG FAULTY A SWAA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 29 642WN 27715 AIR TURNBACK HAD TO USE LOCK OVERIDE TRIGGER TO RAISE GEAR, CYCLED GEAR, THEN GOT THE CONFIGURATION WARNING HORN ADVANCI NG THRUST REVERSERS. CONFIGURED FOR FLAPS 30LDG RETURNED TO SLC. REMOVED AND REPLACED S106 GROUND SHIFT SENSOR PER MM. 2 L 7 2 4F RT A16WE 20081014 EA 2008 10 14 SWIA200820110 1 20080926 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 961SW 7857 FLT 5887 - EMERGENCY CEILING FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081016 NM 2008 10 16 08FDEA04212 1 20081006 A 5753 ARC40082 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 RIGHT HAND WING OUTBOARD FLAP INBOARD HINGE SUPPORT FITTING FORWARD (ARC4008) OUTBOARD MOUNTING BORE HOLE BETWEEN FLAP AND HINGE FOUND WITH CORROSION. REFER SNRM NR N01221 RIGHT HAND OUTBOARD FLAP ASSEMBLY REPLACEMENT. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 08FDEA04213 1 20081006 A 5320 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 576FE 48501 DURING OPEN HOLE INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WITH CRACK IN DICATIONS AT HOLES A, B, C AND D. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 08FDEA04215 1 20081006 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 576FE 48501 DURING OPEN HOLE INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WITH CRACK IN DICATIONS AT HOLES B, C, AND D. MAIN CARGO DOOR LOWER JAMB, CRACKED NR 3 SUPPORT FITTING REMOVED AND REPLACED AS PER S RM 51-31-01 VOL.II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 DHLA2008745515 1 20080917 A 5753 RIB BOEING 727 727224 1384076 NM T/E FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 RIGHT I/B MID-FLAP O/B RIB AT RWBL 133 CORRODED. REMOVED AND REPLACED RIB SECTION BY FABRICATION IAW B727 SRM 51-10-1 A ND 51-30-2. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 SWAA085494 1 20081009 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 857, STR 27R, RBL 3. REPAIRED BEAM PER DHN EA. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085449 1 20081007 A 5330 6518420 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND L1 DOOR UPPER HINGE SKIN DAMAGED AT BS 306, STR 10L. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085451 1 20081007 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 400, STR 13L TO STR 14L. REPAIRED SHEAR TIE PER PAE ER. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085452 1 20081007 A 5240 507945 DOOR FRAME BOEING 737 7375H4 138449D NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR FRAME CRACKED AT AFT LOWER CORNER. REMOVED AND REPLACED FRAME PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085491 1 20081004 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 255WN 32513 FOUND FWD RT FLOOR EGRESS LIGHT LENS MISSING. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 08FDEA04177 1 20081003 A 5414 311N504632 SKIN PANEL BOEING 757 75723A 1384967 NM NR 2 NACELLE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 NR 2 PYLON TORQUE BOX INTERNAL SKIN HAS CORROSION AT LWR CHORD ATTACHMENT ON SEVERAL LOCATIONS. REMOVED AND INSTALLED HI NGE BRACKET PER SRM 51-40-02. REMOVED AND INSTALLED HEATSHIELD PER SRM 51-40-02. REMOVED AND INSTALLED FWD. FAIRING PER SRM 51-40-02. REMOVED AND INSTALLED STRIKER PLATE PER SRM 51-40-02. REMOVED AFT SKIN PER SRM 51-40-02. RECIEVED NEW O /B SKIN ON SERVICEABLE TAG 3B4751. LOCATWED AND DRILLED NEW O/B SKIN PER SRM 51-40-02AND DRAWING 311N5002. INSATLLED N EW O/B SKIN PER SRM 51-40-02 AND DRAWING 311N5002. 2 L 7 2 4F RT A2NM 20081022 EA 2008 10 22 SWIA200820139 1 20081009 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 453SW 7743 MAIN CABIN DOOR EMERGENCY EXIT LIGHT INOP (FLT 3965). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081016 NM 2008 10 16 08FDEA04211 1 20081006 A 5320 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 576FE 48501 DURING OPEN HOLE INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WITH CRACK IN DICATIONS AT HOLES A, B, C AND D. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 DL738081237 1 20080926 A 7920 FILTER BOEING 737 737832 13844CF NM CFMINT CFM56 CFM567B26US NE NR 1 ENGINE DEFECTIVE A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 3731T 19083 30775 876674 AIR TURNBACK, OIL FILTER BYPASS CAUTION LIGHT LEFT ENG CAME ON IN CLIMBOUT. REDUCED THRUST - LIGHT WENT OUT WHEN THRUST REDUCED TO IDLE. INSPECTED CHIP DETECTORS, NO DEBRIS FOUND. INSPECTED AND REPLACED BOTH THE MAIN AND SCAVANGE OIL FIL TERS PER M/M, ALL ITEMS LEAK CHECK OK. NO MESSAGE RETURNED ON ENGINE RUN. FWD TO MEL 79-00-02. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081016 NM 2008 10 16 DL757081238 1 20080926 A 5751 SPAR BOEING 757 757232 1384965 NM LT AILERON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 683DA 27103 DURING SHOP OVERHAUL VISIT, A CRACK WAS FOUND IN THE SKIN AND SPAR OF THE LT OUTBOARD AILERON. REPAIRED PER 470474-14. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04226 1 20081006 A 5740 69166381 ATTACH ANGLE BOEING 727 727227 1384078 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 RIGHT WING, CRACK IN L/E TOP SKIN ATTACH ANGLE ON LEADING EDGE FRAME AT SLAT STATION 0 AT I/B END OF NR 5 SLAT FABRICATE D NEW ATTACH ANGLE ON RT WING L/E FRAME AT SLAT STA. 0.296. AT I/B END OF NR 5 SLAT REF DWG 65-16209,TREATED, PRIMED, P AINTED AND INSTALLED REF SRM 51-10-2, MM 51-20-151-7, SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 SWAA085457 1 20081006 A 3350 101331 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081014 EA 2008 10 14 SWIA200820118 1 20080616 A 5320 PULLEY CNDAIR CL600 CL6002B19 1900309 EA BS 559 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 492SW 7168 C-CHECK, STA 559 RT SIDE AT PULLEY QUADRANT CRACKED OFF LOWER MOUND BOLT. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081015 CE 2008 10 15 GUUA10020801 1 20081002 A 3260 90422912 ANNUNCIATOR BEECH 1900 1900D 1154162 CE COCKPIT LOOSE A GUUA O OTHER O OTHER DE DESCENT 1 SO 29 82539 UE168 FLIGHT - 9236 - EYW/TPA - PILOT REPORTED "H H" LANDING GEAR POSITION INDICATORS INTERMITTENT. RESET AND RE-SECURED H H ANNUNCIATOR SOCKET ASSEMBLIES. 2 L 7 2 4T RT A24CE 20081015 CE 2008 10 15 GUUA10040802 1 20081004 A 3230 571302 MOTOR BEECH 1900 1900D 1154162 CE LANDING GEAR SLUGGISH A GUUA K NONE O OTHER DE DESCENT 1 SO 29 87557 UE246 FLIGHT 9126 - NAS/FLL - PILOT REPORTED GEAR RETRACTION TOOK 14 SECONDS. REMOVED AND REPLACED HYDRAULIC MOTOR. 2 L 7 2 4T RT A24CE 20081015 SO 2008 10 15 RAIA00809008 1 20080907 A 2130 PRESSURE SYSTEM EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A RAIA O OTHER O OTHER CL CLIMB 1 CE 03 850HK 145003 DURING CLIMB, AUTO PRESSURIZATION SYSTEM DID NOT WORK. MAINT DEFERRED THE AUTO-PRESSURIZATION SYSTEM IAW MEL PROCEDURES. (K) 2 L 7 2 4T RT T00011AT 20081015 EA 2008 10 15 CHQA200800188 1 20080924 A 3350 59257 INVERTER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE EMERGENCY LIGHTS INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 470SM 7702 GEE873537 THE EMERGENCY LIGHT TRACK IN FRONT OF THE EMERGENCY EXIT WOULD NOT ILLUMINATE. MX TROUBLESHOT THE FAULT AND FOUND THE E MERGENCY LIGHT INVERTER OVER THE EMERGENCY EXIT TO BE BAD. THE INVERTER WAS REPLACED AND THE EMERGENCY LIGHTS OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 20081015 SO 2008 10 15 C2XA08ON182 1 20080923 A 2611 SMOKE WARNING EMB 145 EMB145XR 3260214 SO LAVATORY FALSE ACTIVATION A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 12175 14500878 FLT 4930 FLIGHT CREW REPORTED AFTER TAKE OFF LAV SMOKE WARNING INDICATION AND DECLARED EMERGENCY AND WAS CANCELLED AND R ETURN TO BLOCK WHERE MX PERSONNEL PERFORMED A HIGH POWER ENGINE RUNS AND A SMOKE DETECTION SYSTEM ADJUSTMENT TEST. OPS CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 20081015 EA 2008 10 15 SIMA200827301 2 20080926 A 7200 ENGINE EMB 135 EMB135KL 3260302 SO RROYCE AE3007 AE3007A13 54166 EA LEFT SMOKE A SIMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 834AE 145631 CAE312117 ON FLIGHT 3540 DURING CLIMB OUT AT APPROX FL180 CREW DETECTED SMOKE IN THE COCKPIT FOLLOWED BY A LAV SMOKE INDICATION. CREW CONFIRMATION SMOKE IN THE CABIN. CREW THEN NOTICED A LOW OIL QUANTITY ON THE NR 1 ENG (3QTS) AND COMPLETED A PRECA UTIONARY ENGINE SHUT DOWN. THE SMOKE AND SMOKE INDICATION DISSIPATED. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERV ICE. C/A R&R LT ENGINE. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081015 NM 2008 10 15 AALA200802203 1 20080826 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 184AN 29594 DFW EMERGENCY LIGHT AT SEAT ROWS 9D TO 15D INOPERATIVE. REPLACED MODULE AT OVERHEAD RT NR 2 DOOR FOR EMERGENCY LIGHT AT SEAT ROWS 9D TO 15D. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081015 NM 2008 10 15 2008UALA05990 1 20081003 A 2530 CIRCUIT BREAKER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE OVEN FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 128UA 30023 PIGTAIL BURNING ON OVEN N51. POWER WAS REMOVED. PULLED AND CAPPED CIRCUIT BREAKER. RESET CONTROLLER, USING HI TECH GAL LEY CART LOAD TESTER ALL VOLTAGES CHECK OKAY. ALL THREE LEVELS. CORD CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081015 NM 2008 10 15 2008UALA05991 1 20081005 A 5320 ATTACH FITTING AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 818UA 882 EVIDENCE OF CORROSION AROUND FWD GIRT BAR ATTACH FITTING DOOR 2R. INSTALLED CORNER FITTINGS AND GIRT BAR HOOK MOUNT PLA TES ON NEW DOOR SILL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081015 EU 2008 10 15 AALA200802191 1 20080825 A 2820 ACTUATOR AIRBUS 300 A300B4605R 3930308 EU ISOLATION VALVE FAULTY A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 40064 507 MIA INFLIGHT T822/25AUG. CREW REPORTED THE LT OUTER TANK ISOLATION VALVE CLOSED. FUEL SYSTEM OPERATED NORMALLY. CREW WAS CONCERNED ABOUT POSSIBLE FUEL IMBALANCE. LANDED MIA WITHOUT INCIDENT. REPLACED LT HAND OUTER TANK FUEL ISOLATION V ALVE ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A35EU 20081015 WP 2008 10 15 AALA200802210 1 20080827 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7543A 53025 STL EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT AB51 FOR EMERGENCY LIGHTS AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081015 WP 2008 10 15 AALA200802222 1 20080828 A 3350 60030451 LIGHT DOUG DC9 DC982 3022082 WP ROW 13-16 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 232AA 49179 STL EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 13 TO 16 AND BETWEEN AFT LAVATORIES STAYED ON WHEN ALL POWER REMOVED FROM ACF T. RESET EMERGENCY LIGHT SYSTEM AND CHARGED. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081015 WP 2008 10 15 AALA200802211 1 20080827 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7543A 53025 STL EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK AT AB52 FOR EMERGENCY LIGHTS AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081015 NM 2008 10 15 2008UALA05993 1 20081005 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 104UA 26902 EMERGENCY LIGHT SEAT 3A AFT INOP. REPLACED EEL LAMP. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081016 NM 2008 10 16 08FDEA04238 1 20081006 A 5330 65545771 SKIN BOEING 727 727233 138408A NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 221FE 20932 SKIN GOUGED STA 700 STR 28R. CUT OUT DAMAGED SKIN AND FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER IAW SRM 53-30 -3, 53-30-2 AND SRM 51-30-2. 2 L 7 3 4F RT A3WE 20081016 NM 2008 10 16 DL757081252 1 20080929 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 DURING HMV AT SAA, ADDITIONAL DAMAGE WAS FOUND IN A PREVIOUSLY INSTALLED SKIN SPLICE REPAIR BETWEEN STA 610 AND 660, STR INGERS S-15L TO S-19L. A DENT AND CREASE WAS FOUND IN THE SPLICED IN SKIN SECTION AT STA 620 BETWEEN S-16L AND S-17L. THE EXISTING SKIN SPLICE DOUBLER WAS REPLACED WITH A NEW DOUBLER WHICH INCORPORATED A REPAIR FOR THE DENT. 2 L 7 2 4F RT A2NM 20081016 2008 10 16 DL76G081255 4 20080929 A 2565 BACR13CE2 RELAY BOEING 767 767332 1382001 NM EVAC SLIDE FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 16065 30199 SQUIB TEST OF EMERGENCY ESCAPE SLIDE TEST 1 FAILED. TROUBLESHOT PER FIM. REPLACED BATTERY PACK AND POWER SUPPLY, NO HE LP. REPLACED RELAY K839, TEST GOOD. MFR P/N BACR13CE2. 2 L 7 2 4F RT A1NM 20081016 NM 2008 10 16 DL757081256 1 20080930 A 5753 113N13022 FLAP TRACK BOEING 757 757232 1384965 NM T/E FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 604DL 22811 CORROSION ON MOUNT SURFACE OF NR 2 FLAP TRACK. DAMAGE WAS MACHINED AND RE-FINISHED. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081257 1 20080924 A 5322 SHEAR TIE BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION AFT SIDE OF BS 1460 AT STR 29 LT. REPLACED SHEAR TIE IAW 51-40-05-00. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081258 1 20080930 A 5313 STRINGER BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION ON STR 29L BS 1510. REPAIRED STR PER SRM 53-00-03 STEP 1 FIG 201. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081259 1 20080911 A 5311 FRAME BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 FRAME CHORD HAS PITTING CORROSION STA 1862 AT ACCESS DOOR 313AL. C/W REPAIR PER ERA 470550-14. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081260 1 20080930 A 5330 SKIN BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA I CABIN DEPRESSURIZATION O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 FUSELAGE SKIN STA 610 (AT RADIO ALT) HAS CORROSION. REPAIR C/W PER ERA 470545-14. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081264 1 20080930 A 5420 FITTING BOEING 757 757232 1384965 NM NR 1 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 NR 1 PYLON SHEAR TIE DRAG FITTING ASSY HAS ELONGATED HOLE. REPAIR C/W PER ERA 470311-14 REV 1 AND SRM 51-20-07. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081265 1 20080825 A 5414 SKIN BOEING 757 757232 1384965 NM NR 1 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 ONE EACH HOLE IS OVERSIZED TO .437 ON NR 1 PYLON I/B SIDE. REPAIR C/W PER ERA 469688-14 DATED 9/10/08. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081266 1 20080912 A 5712 RIB BOEING 757 757232 1384965 NM LT WING DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 LT WING RIB 25 LOWER SKIN PANEL RIB CHORD HAS SHORT EDGE MARGIN ON UPPER ROW OF FAST HOLES. REPAIR C/W PER ERA 470544-1 4 REV O AND APB DWG 757-3250 REV B. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04239 1 20081006 A 5753 STRUCTURE BOEING 727 727233 138408A NM LT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 221FE 20932 LEFT WING INBD MIDFLAP CRACKED 2 PLACES AT CUTOUTS. REMOVED DAMAGED AREA AND FABRICATED NEW ANGLES AND SPLICE REPAIR IA W SRM 57-50-2 AND 51-40-4. INSTALLED REPAIR PARTS IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 20081016 NM 2008 10 16 DL75E081275 1 20081001 A 5610 WINDSHIELD BOEING 757 7572Q8 1384972 NM COCKPIT CRACKED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 704X 28163 L1 WINDSCREEN EXTERNAL PLY CRACKED. REMOVED AND REPLACED 1 LEFT WINDSHIELD IAW MM 56-11-01 POWER TERMINALS NEED RETORQ ING WITHIN 500 HOURS. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL76L081277 1 20081001 A 8012 8113901 START VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 192DN 28449 724715 LEFT ENGINE START VALVE WOULD NOT OPEN. MANUALLY CYCLED LEFT ENGINE START VALVE, OPS CHECK GOOD. STARTED LEFT ENGINE P ER MM, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081016 NM 2008 10 16 08FDEA04252 1 20081007 A 5347 BAC1520792 SEAT TRACK BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 CABIN SEAT TRACK RBL 45, BS 940-950 OB FLANGE UPPER SURFACE CORRODED REF SNRM N00460 REMOVED AND REINSTALLED FLOOR BOA RDS BS 850-950D RBL 24-45 REMOVED CORROSION ON SEAT TRACK OUT OF LIMITS REMOVED, FABRICATED, TREATED, PRIMED, PAINTED, AND INSTALLED SEAT TRACK STA 890-950+10" REF SRM 51-30-2, 51-10-6, 53-10-1, MM 51-20-071, 53-20-012-4, DWG 65-19601. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 08FDEA04255 1 20081007 A 5315 FLOORBEAM BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 MAIN CABIN FLOORBEAM, BS 1320, RBL 12-25, HAS CORROSION. REPAIRED MAIN CABIN FLOORBEAM, BS 1320, RBL 12-25, IAW SRM 53-0 0-51. CORROSION WAS DETERMINED TO BE OUT OF LIMITS PER SRM 53-00-51. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR R EPAIR WITH NO FOLLOW UP TRACKING REQUIREMENTS. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04256 1 20081007 A 5310 CREASE BEAM BOEING 757 75723A 1384967 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 MAIN CABIN CREASE BEAM, BS 755-BS 865 HAS SEVERAL TOOLING MARKS. REMOVED AND REPLACED CREASE BEAM STA. 755-865 IAW SRM 5 1-40-01, 53-30-13, AND 51-20-01 MAJOR REPAIR NO FOLOW-UP REQUIRED. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04257 1 20081007 A 5347 53FX9762 SEAT TRACK BOEING 727 727233 138408A NM BS 1130 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 221FE 20932 WORN SEAT TRACK RBL 45 STA 1130. REMOVED SEAT TRACK, 2 EACH DOUBLERS AND BEAM EXTENSION, FOUND DAMAGED AREA ON WEB, CUT OUT DAMAGED AREA ON WEB IAW SRM 51-30-2 AND 51-40-2 FABRICATED WEB FILLER, 2 STRAPS, BEAM EXTENSION, BEAM STRAP AND E XTENSION SUPPORT FILLER, FABRICATED NEW SEAT TRACK USING EXTRUDED ALUMINUM BAR AND 2 SIDE DOUBLERS IAW DRAWING 53FX939, INSTALLLED ALL PARTS IAW DRAWING 53FX939. 2 L 7 3 4F RT A3WE 20081016 NM 2008 10 16 DL757081286 1 20081003 A 5330 143N34719 SKIN BOEING 757 757232 1384965 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 662DN 24991 MAINTENANCE AT ATL, A LIGHTNING STRIKE WAS FOUND AT STA 508 BETWEEN S-28R AND S-28L. THE DAMAGE WAS TRIMMED OUT AND REP AIRED PER ER/A 06-232915-14 DATED 02-02-91. AT THE TIME OF ISSUE, AN MRR WAS NOT SUBMITTED. THIS SUBMITTAL CORRECTS TH AT SITUATION. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04262 1 20081007 A 5312 BULKHEAD BOEING 757 75723A 1384967 NM BS 1720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 CABIN FLOOR , FWD. OF AFT PRESSURE BULKHEAD STA. 1720 .LBL 52 TO RBL 52 HAS CORROSION AT SEVERAL PLACES. REMOVED CORRO SION , CHECKED LIMITS ON 6 REWORKED AREAS FOUND ALL 6 AREAS TO BE OUT OF LIMITS IAW SRM 53-00-51. REMOVED DAMAGED PANEL , FABRICATED NEW PRESSURE BULKHEAD PANEL FROM BS 1681 TO 1720 IAW SRM 51-40-02. LOCATED AND DRILLED NEW PART, TREATED AN D PRIMED PART, APPLIED TOP COAT IAW SRM 51-20-00, 51-20-01 AND 51-40-05. INSTALLED NEW DECK PLATE IAW SRM 51-40-02. THIS IS A CATEGORY " A" REPAIR . MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081294 1 20080924 A 5320 146N539151 SUPPORT BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 DURING AAI INSPECTION AT ATS/PAE INSPECTION FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT LBL 20 UPPER AND LOWER SURFACES BS 1450 AFT SEVERAL NUT PLATE LOCATIONS. INVESTIGATED CORROSION ON FLOOR TO SIDEWALL SUPPORT UPPER AND LOWER SURFACES AT BS 1450 LT AT SEVERAL NUT PLATE LOCATIONS, DETERMINED TO BE OUT OF LIMITS DUE TO 100 PERCENT MATERIAL LOSS IAW SRM 53 -00-53. LOCATED AND DRILLED FASTENER HOLES AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT FROM BS 1410-1530 LT IAW 51-40-0 2. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081295 1 20080924 A 5320 146N544417 FLOOR SUPPORT BOEING 757 757232 1384965 NM FUSLAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 DURING AAI INSPECTION AT ATS/PAE INSPECTION FOUND CORROSION ON FLOOR SUPPORT LBL 12 BS 1510 UPPER SURFACE AT SEVERAL NUT PLATE LOCATIONS. REMOVED CORROSION ON FLOOR SUPPORT LBL 12 BS 1510 AT 3 NUT PLATE LOCATIONS. REMAINING MATERIAL THICK NESS 0.05, 0.05, 0.04 OUT OF LIMITS IAW SRM 53-00-53 DETAIL V. REMOVED DAMAGED NUT PLATE LOCATIONS AND FABRICATED REPAI R ANGLES IAW SRM 53-60-53D FROM BAC1505-100-246 7075-T6511 EXTRUSION LOT 840689. INSTALLED REPAIR ANGLE IAW SRM 53-60-53 D AND SRM 51-20-01-0G. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 SWAA085458 1 20081008 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 787 + 4, STR 27R. REPAIRED STRINGER PER PAE ER. 2 L 7 2 4F RT A16WE 20081016 EU 2008 10 16 08FDEA04265 1 20081007 A 5210 A5211101000000 ROD AIRBUS 310 A310203 3930313 EU L1 DOOR BENT A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 CE 21 435FE 369 CLIMBING PAST FL 280, ECAM CAUTIONED LT CABIN DOOR WAS OPENED. PRESSURIZATION WAS CLIMBING AT NORMAL 500 FPM WITH DIFFE RENTIAL AT 8.0 AND CABIN ALTITUDE AT 5000 FT. COMPLIED WITH ECAM AND CHECKED DOOR VISUALLY, IT INDICATED THAT THE DOOR W AS OPENED. RETURNED TO KIND. ON DESCENT PAST 13000 FT, LIGHT WENT OUT & ECAM CLEARED. FOUND UPPER LINKAGE ROD BENT. P ERFORMED INSPECTION AFTER ABNORMAL CREW DOOR MOVEMENT, PRECAUTIONARY, PER AMM 05-51-29-0. R&R UPPER LINKAGE ROD IAW MM 5 2-11-12-4. REPLACED ALL DOOR PANELS. L1 ENTRY DOOR WARNING SYSTEM OP CHECKED NORMAL IAW MM 52-41-00-5. 2 L 7 2 4F RT A35EU 20081016 NM 2008 10 16 08FDEA04268 1 20081008 A 5310 65176853 DOOR FRAME BOEING 727 727227 1384078 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 MAIN ENTRY DOOR 1L CUTOUT, AFT FRAME, BS 344, STR 15L JUST BELOW 2ND STOP FITTING FROM BOTTOM, FRAME CRACKED FABRICATED REPAIR PARTS PER DWG 65-17685-24, -9, -7. REPLACED LWR AFT FRAME REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR . 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 08FDEA04272 1 20081008 A 5330 6518420114 SKIN BOEING 727 727227 1384078 NM BS 338 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 491FE 21529 FUSELAGE LH SIDE, DENT ON LAP SEAM AT STA 338, STR 24R. DENT LOCATED ON LAP SEAM & FOUND OUT OF LIMITS IAW SRM 53-30-1. CUT OUT DAMAGE IAW SRM 53-30-3. FABRICATED FILLER AND DOUBLER IAW SRM 53-30-3. INSTALLED REPAIR WASHER IAW SRM 51-30- 8, TREATED AND PRIMED AREA AND DOUBLER REPAIR IAW SRM 51-10-2, INSTALLED DOUBLER REPAIR IAW SRM 53-30-3 AND 51-30-2. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 08FDEA04273 1 20081008 A 5330 651821191 SKIN BOEING 727 727227 1384078 NM BS 392 S20L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 491FE 21529 FUSELAGE LT SIDE, PROTRUDING DENT AT STA 392 ,STR 20L. EVALUATED DENT AND FOUND OUT OF LIMITS IAW SRM 53-30-1, CUT OUT DAMAGED AREA. FABRICATED DOUBLER REPAIR INTERNAL FILLER AND EXTERNAL FILLER IAW SRM 53-30-3 AND SRM 53-30-2 AND INSTAL LED REPAIR PARTS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 08FDEA04274 1 20081008 A 5347 53FX1398 SEAT TRACK BOEING 727 727227 1384078 NM BS 880-920 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 491FE 21529 MAIN CARGO COMPARTMENT, SEAT TRACK CORRODED AT STA 880 TO STA 920 , BL 0. REMOVED FLOOR BOARD IAW SRM 51-30-2, REMOVED SEAT TRACK OUT OF LIMITS IAW SRM 51-30-2; FABRICAETD NEW SEAT TRACK SECTION, LOCATED AND DRILLED. IAW SRM 53-10-5. DRAW ING 53 FX 1497 REV TREATED AND PRIMED IAW SRM 51-10-2; INSTALLED NEW SEAT TRACK SECTION IAW SRM 51-30-2 AND DRAWING F 53 FX 1479 REV S INSTALL FLOOR BOARD IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 08FDEA04275 1 20081008 A 5755 6516216117 SUPPORT BEAM BOEING 727 727227 1384078 NM LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 491FE 21529 LEFT WING NR 7 SPOILER FALSE SPAR LWR PANEL HAS LOOSE FASTENERS. EVALUATED AND FOUND SUPPORT BEAM CRACKED AT WS 251. RE PAIRED IAW DRAWING SR27-57-038 REV C. 2 L 7 3 4F A3WE 20081016 EU 2008 10 16 08FDEA04281 1 20081009 A 5311 A27112119200 FRAME AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 426FE 245 MAIN DECK REINFORCE UPPER FRAME BASE TO ARCHES JUNCTIONS FRAME FOOT 46 LEFT, REWORK HOLES 23, 26, 27 BY E.A 6-5310-12 3911. REAMED HOLES 23, 26,& 27. TO .433. BUSHINGS FABED ON TRAVELER T8/762882, BUSHINGS INSTALLED IAW E.A 6-5310-12391 1 2 L 7 2 4F RT A35EU 20081016 EU 2008 10 16 08FDEA04254 1 20081007 A 5743 TRUNNION AIRBUS 310 A310222 3930315 EU ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 450FE 162 RIGHT MLG TRUNNION ATTACHMENT POINT HINGE ARM FITTING DOES NOT TAKE GREASE.. REMOVED GREASE SUPPLY DUCT IAW MESSIER DOWT Y CMM 32-16-12. RECOMDITIONED TRUNNION PIN & SUPPLY DUCT PIN HOLE " E " IAW CMM 32-16-12. HOLE SIZE AFTER RECONDITIONI NG IS 1.2685. WITHIN ALLOWABLE TOLERENCE PER CMM 32-16-12. INSTALLED NEW GREASE SUPPLY DUCT & ZERK FITTING IAW CMM 32-1 6-12. 2 L 7 2 4F RT A35EU 20081017 NM 2008 10 17 2008UALA06049 1 20081009 A 2820 7G1103 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUEL SYSTEM FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 547UA 25368 RIGHT CENTER FUEL PUMP PRESSURE LIGHT ON. SWITCH IS FAULTY. REPLACED THE RT CENTER PRESSURE PUMP SWITCH, OPS CHECKED N ORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081017 NM 2008 10 17 08FDEA04307 1 20081011 A 5340 ANB7089501 FITTING DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 576FE 48501 RIGHT MAIN LANDING GEAR WW DOOR LOWER UPLATCH FITTING (FWD AND AFT ) FOUND CRACKED. R & R WITH FABRICATED UPLATCH FITTI NG AS PER SRM 51-33-01. UPLATCH FITTING FABRICATED AS PER DRAWING ANB7089. OPERATIONS CHECK CARRIED OUT ON RT MLG LOWE R UPLATCH FITTING AS PER AMM 32-34-05-700-801 FOUND 'SATISFACTORY'. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 08FDEA04309 1 20081011 A 5313 65564414 STRINGER BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 221FE 20932 CORROSION ON S29R AT BS 970-990. BLENDED OUT S29R FLANGE AS NECESSARY TO REMOVE CORROSION, REMAINING THICKNESS DIMENSION S MAINTAIN A 20-1 BLENDOUT RATIO WITH A MIN 1.0: RADIUS PER MESSAGE 1-1013418906-2,3,4,5,6, AND ARE WITHIN LIMITS. ACCO MPLISHED HFEC AND SURFACE INSP PER NDTM 51-00-00, NO DEFECTS NOTED, FLAP PEENED AREA PER SOPM 20-10-03, FINISHED AREA AN D APPLIED CORROSION INHIBITOR. ALL STEPS ACCOMPLISHED PER EA 7-5330-126853. 2 L 7 3 4F RT A3WE 20081017 NM 2008 10 17 08FDEA04311 1 20081013 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITT ING AT HOLE C. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 F3LA200800314 1 20080608 A 5320 D5397496800400 PROFILE AIRBUS A319 A319111 3930336 NM CARGO BAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 926FR 5 2198 DURING C-3/S-1 C-CHECK, INSPECTION NOTED AFT CARGO COMPARTMENT LEFT SIDE PROFILE AT FRAME C58 HAS CORROSION. MAINTENANC E REMOVED CORRODED PROFILE AND INSTALLED NEW IN ACCORDANCE WITH A319 SRM 51-42-11 PAGE 7 AND 8. 2 L 7 2 4F RT A28NM 20081017 EU 2008 10 17 F3LA200800365 1 20080616 A 5321 D5367402800000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 941FR 18 2483 DURING C2 C-CHECK, INSPECTION NOTED AFT PIT TRANSITION PANEL 151DE HAS SEVERAL PUNCTURES. MAINTENANCE REPAIRED PANEL IN ACCORDANCE WITH A319 SRM 53-02-00, FIGURE 204. 2 L 7 2 4F RT A28NM 20081017 NM 2008 10 17 08FDEA04316 1 20081013 A 5320 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 7 SUPPORT FIT TING AT HOLES A, B, C AND D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. BUSHING REPAIR ON HOLES CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 08FDEA04317 1 20081013 A 5310 DOOR FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 CRACK INDICATION FOUND ON SECOND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" HOLES AT MAIN CARGO DOO R NR 6 LOWER JAMB AT HOLE A. CARRIED OUT REPAIR AS PER FEDEX E.A. 1-5310-125556, REPAIR CLASSIFIED AS MAJOR PER GMM 6 -2-100. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 08FDEA04318 1 20081013 A 5310 ACA72251 DOOR FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 CRACK INDICATION FOUND ON SECOND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" HOLES AT MAIN CARGO DOO R NR 7 LOWER JAMB AT HOLES A AND B. CARRIED OUT REPAIR AS PER FEDEX EA 1-5310-125556, REPAIR CLASSIFIED AS MAJOR PER G MM 6-2-100. 2 L 7 3 4F RT A22WE 20081017 EU 2008 10 17 08FDEA04327 1 20081013 A 5511 A5517860000400 FRAME AIRBUS 300 A300B4622R 3930312 EU HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 LEFT HORIZONTAL STAB L / E PANEL 341 AB OUTBD BOTTOM FORMER IN CRACKED. STOP DRILLED THE CRACK IAW SRM 51-23-10. HFEC STOP DRILL PER NTW 51-10-08. VERIFIED THE CRACK STOPS. FABRICATED & INSTALLED REPAIR ANGLES IAW SRM 55-12-19. 2 L 7 2 4F RT A35EU 20081017 NM 2008 10 17 DLM88081311 1 20081006 A 3213 59353487 CYLINDER DOUG MD88 MD88 3023688 NM RT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DE 53415 CORROSION PITTING WAS FOUND IN THE LOWER LEFT QUADRANT OF THE RT MLG OUTER CYLINDER. AN ER/A WAS ISSUED TO REWORK THE C YLINDER TO REMOVE THE DAMAGE. SAFE-LIFE LIMIT REDUCED TO 26000 CYCLES FROM FAA APPROVAL DATE OF 9-05-2006. 2 L 7 2 4F RT A6WE 20081017 NM 2008 10 17 DL76P081312 1 20081006 A 5420 311T31571 TEE FITTING BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 140LL 25988 THE CLOSEOUT TEE AT THE MIDSPAR FITTING ON THE NR 2 PYLON WAS FOUND CRACKED. AN ER/A WAS ISSUED TO REPLACE THE CLOSEOUT TEE AND COMPLETE AD MANDATED INSPECTIONS. 2 L 7 2 4F RT A1NM 20081017 NM 2008 10 17 DL757081323 1 20081006 A 5347 141N51312 SEAT TRACK BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION ON SEAT TRACK AT BODY STATION 377 TO 440 WL 208. REPAIRED ON NR 00116 PER 51-40-02 BY REPLACEMENT. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 DL757081324 1 20081006 A 5320 143N51292 INTERCOSTAL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 INTERCOSTAL CRACKED AT BODY STATION 680 RBL 25 AT WL 204. REPAIRED PER 51-40-02D ON NR 00092. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 DL757081329 1 20081006 A 5315 146N547713 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION ON FLOORBEAM 1470 AT LBL 8. REPAIRED ON NR 00051PER 51-40-05 FIGURE 4. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 DL757081332 1 20081006 A 5320 146N54592 INTERCOSTAL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION AT INTERCOSTAL STATION 1480 TO 1500 AT STRINGER 26L. REPAIRED ON NR 00124 PER 512-40-02. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 DL757081333 1 20081006 A 5321 453N161123 FLOOR PANEL BOEING 757 757232 1384965 NM AFT CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 609DL 22816 CORROSION ON FLOOR PANEL AT STATION 1510 LBL 17 TO RBL 17. REPAIRED ON NR 00031 PER 53-00-53. 2 L 7 2 4F RT A2NM 20081015 NM 2008 10 15 2008UALA05998 1 20081005 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 785UA 26954 AFT EMERGENCY LIGHT AT SEAT 2E INOP. RELAMPED EMERGENCY LIGHT, TESTED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081015 NM 2008 10 15 2008UALA05999 1 20081005 A 3397 80172424 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 785UA 26954 AFT EMERGENCY LIGHT AT SEAT 1E INOP. SECURED CONNECTOR. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081015 SO 2008 10 15 C2XA08IA214 1 20080923 A 3610 81662410 VALVE EMB 145 EMB145XR 3260214 SO FUSELAGE INOPERATIVE A C2XA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION NR NOT REPORTED 1 SW 27 16112 12801 145660 IAH FLIGHT 2063. THE CREW REPORTED A BLEED 1 OVERTEMP IN FLIGHT. THE CREW CLOSED THE BLEED VALVE IN ACCORDANCE WITH TH E QRH AND THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX R&R THE ENGINE 1 FAN AIR VALVE. OPS CHECKED WI TH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081015 SO 2008 10 15 C2XA08CL108 1 20080924 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13970 145146 DURING ROUTINE MX THE RT WING FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR 2 EMERGEN CY LIGHT BATTERY. OPS CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20081015 SO 2008 10 15 C2XA08RI137 1 20080905 A 3350 375091 SIGN EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14117 145674 FLIGHT 2574 EWR FLIGHT CREW REPORTED AFT CEILING EMERGENCY SIGN INOPERATIVE. EWR MX R&R EMERGENCY EXIT SIGN AND PERFORM ED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081015 NM 2008 10 15 2008UALA06016 1 20081005 A 2913 65057 PUMP BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RT ENGINE MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 676UA 30028 EDP HYD OVERHEAT LIGHT ILLUM. EICAS MSG (L,R) PRIM HYD OVERHEAT DISPLAYED. PULLED BOTH PRESSURE & CASE FILTERS. FOUND METAL CHUNKS IN BOTH FILTERS. REPLACED RT ENGINE HYDRAULIC PUMP ASSY. REPLACED CASE DRAIN FILTER. 2 L 7 2 4F 4 F RT A1NM E24NE 20081015 NM 2008 10 15 2008UALA06017 1 20081006 A 2621 80600031600U FIRE BOTTLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU APU LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 346UA 24250 APU FIRE BOTTLE PRESSURE BELOW LIMIT. REPLACED APU FIRE BOTTLE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081015 NM 2008 10 15 2008UALA06018 1 20081005 A 5754 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L/E SLAT DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 546UA 25367 FOUND NR 2 SLAT MID SECTION AREA DELAMED BOTH THE UPPER AND LOWER SKIN, SIZE IS APPROX 4 X 5 INCHES IN THE MID SECTION A REA.DELAMINATION OF COMPOSITE STRUCTURE. REPAIRED AREA -ACTUAL AREA WAS 1.5X 2.0 REPAIRED REF SRM. 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 SO 2008 10 15 C2XA08ON179 1 20080830 A 2612 RELAY EMB 145 EMB145LR 3260212 SO FIRE DETECTION BURNED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 18557 15176 11580 145596 FLIGHT CREW REPORTED CARGO FIRE EXTINGUISHER SWITCH LIGHT ILLUMINATE IN-FLIGHT AND DECLARED EMERGENCY. FLIGHT CREW RETU RNED TO BLOCK WHERE IT LANDED SAFELY WITHOUT INCIDENT. MX TROUBLESHOOT CARGO FAN AND MEL THE ISSUE. MX PERSONNEL THEN REMOVED AND REPLACED RELAYS K0625 AND K0629. OPERATIONALLY CHECKED SATISFACTORY AND AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081015 SO 2008 10 15 C2XA08RI136 1 20080902 A 3350 PRS1B POWER SUPPLY EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13124 54652 145689 FLIGHT CREW REPORTED BOTH AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY POWER SUPPLY ASSY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (K) 2 L 7 2 4F RT 20081015 SO 2008 10 15 CX2A08ON181 1 20080828 A 7500 40303915 O-RING EMB 145 EMB145XR 3260214 SO BLEED SYSTEM WORN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16170 11287 14500850 FLIGHT CREW REPORTED E2 BLEED LEAK ON CLIMB OUT AND DIVERTED, WHERE MX PERSONNEL REMOVED AND REPLACED DUCT O-RING AFT OF LAV. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (K) 2 L 7 2 4F RT 20081015 NM 2008 10 15 2008UALA06028 1 20081004 A 3510 89151114 OXYGEN SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW O2 LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 127UA 28813 COCKPIT OXYGEN QUANTITY DECREASED TO BELOW 1540 INFLIGHT. SERVICED TO 1760 AT 17DEG C. LEAK CHECKED CREW O2 BOTTLE AREA FITTINGS OK. CHECKED FLIGHT DECK O2 MASKS OKAY. INBD CREW O2 AT 1580 PSI. 2 L 7 4 4F 4 F RT A20WE E24NE 20081015 NM 2008 10 15 2008UALA06029 1 20081006 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 NEED DOUBLER ON DOOR 2R FOR UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED. FABRICATED A REPAIR DOUBLER AND INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 NM 2008 10 15 2008UALA06030 1 20081006 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 DOOR 2L REQUIRES REPAIR DOUBLER FOR UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED. FABRICATED A REPAIR DOUBLER AND INS TALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081015 NM 2008 10 15 2008UALA06031 1 20081007 A 5532 PANEL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE VERTICAL STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 814UA 862 LEFT VERTICAL STAB PANEL 322AL HAS CRACK 13.5 INCHES LONG, 4.25 INCHES BELOW TOP OF PANEL AND 9 INCHES AFT OF CENTER LIN E. REMOVED AND REPAIRED PANEL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081015 NM 2008 10 15 2008UALA06033 1 20081008 A 2913 65057 PUMP BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT ENGINE MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 665UA 29237 EDP HYD OVERHEAT LIGHT ILLUM EICAS MSG (L, R) PRIM HYD OVERHEAT DISPLAYED. PUMP WAS DEACTIVATED. POS 1 (01=L,02=R). S AMC TEXT: AFTER EDP SECURED SEVERAL MINUTES LATER LT QTY DROPPED TO ZERO AND EMDP WAS TURNED OFF. REPLACED LT ENG HYD PUMP AND CASE DRAIN FILTER. GROUND RUN ENGINE, LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081015 SO 2008 10 15 C2XA08ON176 1 20080831 A 3260 0132AFU2 SENSOR EMB 145 EMB145XR 3260214 SO TIRE TEMP INOPERATIVE A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 11176 14500881 FLIGHT CREW ABORTED TAKEOFF AT 30-40 KNOTS FOR BRAKE OVERHEAT EICAS MSG. MX PERSONNEL FROM LAX WAS ON SITE AND THEY REM OVED AND REPLACED NR 3 RT IB BRAKE TEMP SENSOR. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR S ERVICE. (K) 2 L 7 2 4F RT 20081015 SO 2008 10 15 GLBA200810033 1 20081003 A 5330 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE DAMAGED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 71GL 120071 MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A REPAIR TO THE BELLY SKIN BENEATH THE TCAS ANTENNA AT FS 5611 BETWE EN FRAMES 17 & 18 AND STRINGERS 21L & 21R FOUND NOT TO CONFORM TO GIVEN DOCUMENTATION. MAINTENANCE REPAIRED THE BELLY B ENEATH THE TCAS ANTENNA IAW EMB-120 SRM 53-20. REPAIR AREA APPROXIMATELY 8.5" BY 7.750" OUT OF 2024 T3, .050", RRFZ AD RIVETS -4'S & -5'S, SEALANT MIL-S-81733. 2 L 7 2 4T RT A31SO 20081015 SO 2008 10 15 GLBA20081008088 1 20081008 A 5610 WINDOW POST EMB 120 EMB120ER 3260203 SO COCKPIT DAMAGED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 71GL 120071 MAJOR REPAIR - DURING ROUTINE SCHEDULED MAINTENANCE A MAJOR REPAIR AT THE RIGHT DV WINDOW FORWARD POST DOES NOT CONFORM TO GIVEN DOCUMENTATION. ** SUPPLEMENTAL INFORMATION WILL BE PROVIDED UPON COMPLETION OF THE REPAIR ** 2 L 7 2 4T RT A31SO 20081015 NM 2008 10 15 UPS08B53474 1 20080108 A 5311 65B01750806 FAILSAFE BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 579UP 26062 INSPECTION TYPE:BCF STA 1140 RT TENSION TIE FRAME FAILSAFE CHORD 1EA FASTENER HOLE CRACKED MORE THAN 0.050". REPAIRED C RACKED FRAME FAILSAFE CHORD AS PER SRM 53-70-12. 2 L 7 4 4F RT A20WE 20081015 NM 2008 10 15 UPS08B53475 1 20080108 A 5320 65B09631610 TENSION TIE BOEING 747 747400 13848AT NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 579UP 26062 INSPECTION TYPE:BCF STA 1140 TENSION TIE RT AFT CHANNEL 2EA FASTENER HOLE CRACKED MORE THAN 0.030". REPAIRED CRACKED TE NSION TIE AS PER SRM 53-40-30 FIG 201. 2 L 7 4 4F RT A20WE 20081015 CE 2008 10 15 DXTA2008101303302 1 20081012 A 2612 WARNING LIGHT CESSNA 500 560CESSNA 2076750 CE COCKPIT ILLUMINATED E DXTA F ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 GL 07 814QS 5600776 RIGHT ENG FIRE LIGHT ILLUMINATED IN FLIGHT DISCHARGED FIRST BOTTLE, LIGHT EXTINGUISHED. LIGHT RE-ILLUMINATED AND WOULD NOT EXTINGUISH AFTER SECOND BOTTLE DISCHARGED. 2 L 7 2 4F RT A22CE 20081016 SO 2008 10 16 C2XA08TY103 1 20080909 A 3350 3V1317 LAMP EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 18982 145223 LT EXTERNAL, JUST FWD OF L/E, EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10. OPS CHECK GO OD. ACFT STILL IN C-CHECK. (K) 2 L 7 2 4T RT T00011AT 20081016 2008 10 16 JLT2008F00000 2 20080718 A 7314 307085057 PUMP BRAERO DH125 BAE125800A 1500285 EU NR 1 ENG FUEL FAILED E JLTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 19 855GA 258211 ON THE EVENING OF FRIDAY, JULY 18TH, ON CLIMB, EN ROUTE, THE CREW OBSERVED THE LT ENGINE, SN 91535, FUEL LIGHT ILLUMINAT ED. THE CREW REDUCED POWER. ENGINE THEN EXPERIENCED AN UNCOMMANDED INFLIGHT SHUTDOWN. CREW SECURED THE ENGINE AND ATTE MPTED A RESTART. RESTART WAS UNSUCCESSFUL. CREW THEN EXECUTED AN AIR TURNBACK AND SIGNALED AN EMERGENCY LANDING. TROUBL ESHOOTING HAS REVEALED THAT THE FUEL PUMP FAILED A FUNCTIONAL CHECK. (K) 2 L 7 2 4F RT A3EU 20081016 NM 2008 10 16 DHLA2008745501 1 20081009 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 FRAME CRACKED, BS 380, FWD GALLEY DOOR. REPLACED FRAME SECTION BY FABRICATION IAW B727 SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 RYN2008F00020 1 20080910 A 7700 SENSE LINE BOEING 757 7572G5 1384912 NM LT ENGINE BROKEN A RYNA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 GL 31 929RD 23929 PILOT REPORT LT ENGINE NOT MAKING POWER AT FL 20000 WITH THE ENGINE POWER LEVER FULLY FWD AND N1 WAS ONLY 71 PERCENT. RE PLACED THE LT ENGINE P1 PROBE BROKEN SENSE LINE. COMPLIED WITH HIGH POWER ENGINE RUN, NO DEFECT NOTED. (K) 2 L 7 2 4F RT A2NM 20081016 2008 10 16 UIEA200800299 4 20080906 A 3441 46300161300413 INU BOEING 747 747243B 1384830 NM NR 1 FAILED E UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 517MC 23300 AIR TURN BACK, DURING CLIMBOUT BOTH INST WARNING LIGHTS WITH ATT LIGHT ILLUMINATED. CAPT`S ADI ATT AND COMPAS FLAG IN VI EW. CAPTS HSI HDG, FLAG IN VIEW. REMOVED AND REPLACED NR 1 INU IAW 34-41-03. COOLING SYSTEM TESTED OK AND INS NAV TES T OK. (K) 2 L 7 4 4F RT A20WE 20081016 SO 2008 10 16 WIW2008F00000 1 20080813 A 7712 31017262 TORQUE SENSOR AYRES S2 S2RHGT65 0970110 SO GARRTT TPE331 TPE33110 01514 WP ENGINE FAILED G WIWA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 WP 07 30591 678 T65HG023G P37247C ON 8/13/2008 AT APPROX 07:40 AM, AIRPLANE WHILE PERFORMING AERIAL APPLICATION EXPERIENCED A LOSS OF ENGINE POWER AND MAD E AN EMERGENCY LANDING IN A FIELD. SUBSEQUENT INVESTIAGATION REVEALED THE IDLER GEAR BRG (PN 3103035-1) IN THE TORQUE SE NSOR HAD FAILED ALLOWING THE LOSS OF DRIVE INPUT TO THE FUEL CONTROL RESULTING IN LOSS OF ENGINE POWER AND EMERGENCY LAN DING. (K) 1 L 7 1 3T 4 T NC E4WE 20081016 EA 2008 10 16 ASOA200801322 1 20081003 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 846AS 7328 WHILE PERFORMING TASK AWL253-41-201, AN INDICATION WAS NOTED AT THE FS 559 BULKHEAD WEB OUTBOARD OF RBL 9, WL 58.7 APPRO X .300 INCH IN LENGTH AND INBOARD OF RBL 18, WL 58.7 APPROX 1.0 INCH IN LENGTH. REMOVED DAMAGED SECTION OF THE RT WEB, REPAIRED IAW REO 610R-53-41-260 REV C STEPS 1-14. NUT PLATES REQUIRE SEALANT. AREA REQUIRES PAINT AND CORROSION INHIBI TOR. SEALED NUT PLATES, PAINTED AND APPLIED CORROSION INHIBITOR TO REPAIR AREA IAW REO 610R-53-41-260 REV C. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260, REV C. 2 L 7 2 4F RT A21EA 20081016 EA 2008 10 16 ASOA200801325 1 20081010 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 846AS 7328 AT FS 718.0 BETWEEN STRINGERS 11R AND 12R PREVIOUSLY REPAIRED ATTACH ANGLE CRACKED IN RADIUS. REMOVED PREVIOUS REPAIRS FROM FS 718.0 BETWEEN STRINGERS 11R AND 12R IAW CRJ 200 SRM 51-42-06 AND 51-42-21. LPI CUTLINE AS PER REO 601R-53-61-19 3 AND CRJ 200 NDTM 51-20-08. NO INDICATIONS NOTED AT THIS TIME. REPAIRED FS 718.00 BETWEEN STRINGERS 11L AND 12L IAW S TEPS 2 THROUGH 6 OF BOMBARDIER REO 601R-53-61-193. STEP 1 OF BOMBARDIER REO 601R-53-61-193 TRIM OUT OF FLANGE WAS PREVIO USLY COMPLIED WITH. ALL WORK WAS COMPLIED WITH IAW ASA EO 600-53-0067 REV A. SUPPLEMENTAL-SDR CLOSED 11/14/2008. 2 L 7 2 4F RT A21EA 20081016 NM 2008 10 16 DHLA2008745509 1 20081004 A 5210 SKIN BOEING 727 727224 1384076 NM L1 DOOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 745DH 20665 L1 DOOR OUTER SKIN DENTED AT BS 329. ACCOMPLISHED EXTERNAL DOUBLER REPAIR PER B727 SRM 52-00-3 FIG 4. 2 L 7 3 4F A3WE 20081017 NM 2008 10 17 08FDEA04260 1 20081007 A 5320 656040712 PLATE BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 AFT LOWER CARGO BAY, DOOR THRESHOLD WRAP AROUND PLATE CRACKED REMOVED AFT CARGO THRESHOLD, WELDED CRACK ON N/R NOO382 R EINSTALLED THRESHOLD REF SRM 51-30-2. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 SWAA085484 1 20081008 A 5322 6546569 SHEAR TIE BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CORRODED AT BS 947.5, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085488 1 20081008 A 5313 BAC1498 STRINGER BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED MV2 CHECK, FOUND STRINGER CORRODED BS 927, STR 25L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085519 1 20081012 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 927 STR 27L. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081016 2008 10 16 SWAA085510 4 20081012 A 2565 416A2100 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 225WN 34333 FOUND R1 EMERGENCY EXIT DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 08FDEA04180 1 20081003 A 5310 143N833521 STRUCTURE BOEING 757 75723A 1384967 NM BS 660-686 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 BS 660-686 AT S13L, OUTBOARD CHORD IS CRACKED. REMOVED OUTBOARD CHORD IAW 51-40-01, FABRICATED CHORD ON MAE TRAVELER T8 /761457, INSTALLED NEW CHORD IAW SRM 51-40-01. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 SWAA085511 1 20081010 A 3350 417A5900 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 233LV 32501 DURING SCHEDULED HC2 CHECK, RT EMERGENCY EXIT LIGHT BATTERY FAILED TEST. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085527 1 20081011 A 3350 65C27095 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 08FDEA04188 1 20081003 A 5347 SEAT TRACK BOEING 757 75723A 1384967 NM BS 900-1076 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 MAIN CABIN ,SEAT TRACK BS 900 TO 1076 LBL 45.50 CROWN GOUGED AND SCRATCHED. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-4 0-02, 53-00-52. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04189 1 20081003 A 5310 CREASE BEAM BOEING 757 75723A 1384967 NM BS 900-920 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 BS 900- 920 RT SIDE FOUND CREASE BEAM WEB CORRODED. REMOVED AND REPLACED AND FLANGED DOUBLER IAW SRM 51-40-02. REPAIR P ARTS FABRICATED ON MAE TRAVELERS T8/761489 AND T8/761490. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 SWAA085553 1 20081010 A 3350 PL22300L LIGHT BOEING 737 7373G7 1384595 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 690SW 23783 FOUND EMERGENCY EXIT FLOOR LIGHT STRIP LOOSE AT ROW 8 ABC. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 08FDEA04190 1 20081003 A 5310 CREASE BEAM BOEING 757 75723A 1384967 NM BS 1020 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 BS 1020, CREASE BEAM WEB CORRODED, REMOVED AND REPLACED WEB AND ANGLE IAW SRM 51-40-02. REPAIR PARTS FABRICATED ON MAE TRAVELERS T8/759254, T8/760846. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04192 1 20081003 A 5310 BAC1515551 CREASE BEAM BOEING 757 75723A 1384967 NM BS 900-1040 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 CREASE BEAM RT SIDE HAS SCRIBE MARKS AND CORRODED, BS 900-1040. REMOVED AND REPLACED CREASE BEAM IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04193 1 20081003 A 5315 FLOORBEAM BOEING 757 75723A 1384967 NM N/A MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 MAIN CABIN FLOORBEAM BS 1580 LBL 25-45 HAS MISDRILLED HOLES. REPAIRED IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL76S081242 1 20080927 A 3510 38001606 LINE BOEING 767 767332 1382001 NM CREW O2 LEAKING A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 137DL 25306 CREW OXYGEN PRESSURE DROPPED TO 10 PSI. FOUND BAD O2 LINE BEHIND F/O OXYGEN MASK CONTAINER. REPLACED LINE AND CREW O2 BOTTLE. LEAK CHECK GOOD. 2 L 7 2 4F RT A1NM 20081016 NM 2008 10 16 DLM88081243 1 20080926 A 2752 59370525001 ACTUATOR DOUG MD88 MD88 3023688 NM T/E FLAP BYPASSING A DALA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 27 916DL 49591 FLAPS WOULD NOT EXTEND BEYOND 11 DEG FOR LANDING. FOUND RIGHT INBOARD FLAP ACTUATOR BYPASSING. REPLACED RT INBOARD NR 1 FLAP ACTUATOR PER AMM 27-52-02 PB 201. LEAK AND OPS CHECKS GOOD. FINAL INSTALLATION, SAFETY AND OPS CHECK GOOD PER M M 832734, DEPT 250, RII. CREW DECLARED EMERGENCY. AIRCRAFT LANDED UNEVENTFULLY. 2 L 7 2 4F RT A6WE 20081016 2008 10 16 DLM90081247 4 20080927 A 2565 100506201 SLIDE DOUG MD90 MD9030 3023690 NM TAILCONE MALFUNCTIONED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 915DN 53395 INADVERTANT DEPLOYMENT OF TAIL CONE FROM EXTERNAL HANDLE, SLIDE DID NOT DEPLOY. RE-INSTALLED TAIL CONE PER AMM. TAIL C ONE DISPLACEMENT SYS NITROGEN CYLINDER ALSO SERVICED PER AMM. COMPLIED WITH RII REQUIREMENT FOR TAIL CONE INSTALLATION/ SAFETY/SECURITY AND ADJUSTMENT OF TAIL CONE RELEASE SYSTEM PER AMM. 2 L 7 2 4F RT A6WE 20081016 NM 2008 10 16 DL757081249 1 20080929 A 5711 SPAR BOEING 757 757232 1384965 NM LT WING GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 DURING WINGLET MOD, THE LT WING REAR SPAR LOWER CHORD WAS DAMAGED BY TOOLING. A GOUGE WAS BLENDED SMOOTH AND TREATED FO R CORROSION PROTECTION. THE BLEND AND TREATMENT WAS APPROVED BY BOEING. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081276 1 20081001 A 5711 RIB BOEING 757 757232 1384965 NM RT WING DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 RT WING RIB STA 18 HAS 1 EA ELONGATED HOLE AT STR 9.5 FWD OUTBOARD HOLE ON FWD LEG OF STR CHANNEL. REWORKED DAMAGED HOL E TO A FINAL SIZE OF .250, EDGE MARGIN OF .450 IAW 757 SRM 51-40-05 FIG 2. INSTALLED 1 EA FASTENER ON STRINGER CLIP U9. 5 RT WING RIB 18 PER BAC5004-2 AND ERA 470542-14. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 SWAA085535 1 20081013 A 5340 6546529 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085536 1 20081013 A 5340 6546529 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 9R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085537 1 20081013 A 5340 6546529 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 9R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081016 2008 10 16 SWAA085538 4 20081012 A 2565 416A1500 COVER BOEING 737 7377H4 1384404 NM R2 DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 406WN 27894 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT SLIDE VIEW WINDOW COVER MISSING. REMOVED AND REPLACED COVER PE R MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 08FDEA04289 1 20081009 A 5220 652108U21 CASTING BOEING 727 727227 1384078 NM DOOR HANDLE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 L/H FWD EMERGENCY DOOR CASTING AROUND HANDLE HOUSING IS CORROSION REPLACED CASTING AROUND HANDLE HOUSING REF SRM 51-30-0 2 PG 1-5. OPS CHECK OF DOOR OK THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081017 NM 2008 10 17 08FDEA04319 1 20081013 A 5312 AJC700135 STIFFENER DOUG MD11 MD11F 3023600 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 EMPENNAGE: AFT FUSELAGE AFT BULKHEAD STA 2164 AFT SURFACE LOWER LATERAL STIFFENER FOUND CRACKED AT LEFT HAND AND RIGHT HAND SIDE. REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II AND SRM 51-32-01 VOLUME II. NEW STIFFENER REWORKED AS PER DRAWING AJC7001. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081017 EU 2008 10 17 08FDEA04326 1 20081013 A 5230 A523780790200 ATTACH FITTING AIRBUS 300 A300F4605R 3930327 EU CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 BULK CARGO DOOR INTERNAL LATCH ATTACHED FITTING FWD & AFT SIDE IS CRACKED. REMOVED CRACKED FITTING IAW SRM 51-40-21. LOCATED & DRILLED FITTING IAW DWG 17A52378079. INSTALLED NEW FITTING P/N A523780790200 IAW SRM 51-40-21. REMOVED & RE-INSTALLED LATCH ASSY IAW AMM 52-34-21-4. 2 L 7 2 4F RT A35EU 20081017 NM 2008 10 17 DL757081316 1 20081006 A 5315 146N544336 SUPPORT ANGLE BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION FOUND FLOORBEAM SUPPORT ANGLE AT STATION 1497 AT RBL 14. REPAIRED ON NR 00065 PER 53-00-53 DETAIL V. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 08FDEA04263 1 20081007 A 7932 626447 TRANSMITTER BOEING 727 727233 138408A NM OIL PRESSURE FAILED A FDEA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CE 21 258FE 20940 NR 1 ENGINE SHUTDOWN INFLT FOR HIGH OIL PRESSURE (60 PSI) IAW QRH. WINDMILLED FOR 15 MINUTES IN GREEN BAND AND BELOW. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER PER MM 79-33-001-4. RAN ENGINE FOR LEAK AND PRESSURE CHECKS. CHECK OIL P RESSURE WITH DIRECT READING PRESSURE GAUGE SET. OIL PRESSURE REG TO 47 PSI. NEW TRANSMITER PRESSURE READ 47 PSI. ACCO MPLISHED MAX POWER ASSURANCE CHECK AND ALL ENG INDICATION CHECK WITHIN LIMITS, NO VIB FELT, MAX OIL PRESSURE WAS 52-53 PSI ALL WITHIN LIMITS PER JRH. 2 L 7 3 4F RT A3WE 20081017 2008 10 17 UIEA200800327 4 20081007 A 3442 6225136202 RADAR BOEING 747 74747UF 1384812 NM WEATHER RADAR FAILED A UIEA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 15 412MC 30559 RIGHT WEATHER RADAR FAILED APPROX 1 HOUR INTO FLIGHT. LEFT RADAR FAILED WHEN SELECTED. PERFORMED AIR TURNBACK. REMOVE D DRIED AND REINSTALLED THE WAVE GUIDE DUE TO WATER CONDENSATION. REPLACED RADAR ANTENNA MOUNT AND RADAR CONTROL PANEL. WEATHER RADAR CONTROL PANEL RADAR TEST CARRIED OUT OKAY. 2 L 7 4 4F RT A20WE 20081017 NM 2008 10 17 F3LA200800468` 1 20080714 A 5320 D5397496800400 PROFILE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 918FR 19 1943 DURING C-4/S-1 C-CHECK, INSPECTION NOTED AFT CARGO COMPARTMENT PROFILE AT FRAME C58 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 AND 51-21-11. 2 L 7 2 4F RT A28NM 20081017 EU 2008 10 17 F3LA200800506 1 20080717 A 5321 D5367307200200 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 807FR 2276 LINE MAINTENANCE NOTED THE AFT CARGO PIT TRANSITION PANEL 151FH HAD PUNCTURE DAMAGE IN THREE PLACES ON THE UPPER SKIN. MAINTENANCE REPAIRED DAMAGE IN ACCORDANCE WITH A318 SRM 53-02-00, FIGURE 205. 2 L 7 2 4F RT 20081017 GL 2008 10 17 CHQA200800195 2 20081008 A 7261 23073567 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL NR 2 ENGINE LEAKING A CHQA A UNSCHED LANDING K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 11 259JQ 145763 CAE312497 FLIGHT 3055, LGA TO GSO. AFTER TAKEOFF, AT AROUND 200 TO 500 FEET, THE FLIGHT CREW RECEIVED A LAV SMOKE INDICATION ON E ICAS. THE FLIGHT RETURNED TO LGA AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINES AND FOUND THE ZERO BEA RING CARBON SEAL LEAKING OIL INTO THE BLEED SYSTEM. THE AIRCRAFT WAS FERRIED TO SDF WHERE THE ZERO BEARING CARBON SEAL WAS REPLACED WITH NO FURTHER DEFECTS NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081017 NM 2008 10 17 F3LA200800508 1 20080722 A 5210 D5211064320100 BUSHING AIRBUS A319 A319111 3930336 NM R1 DOOR UNSECURE A F3LA K NONE O OTHER UK UNKNOWN 1 NM 21 938FR 59 2406 FLIGHT CREW NOTED THE R1 DOOR WOULD NOT LATCH IN THE OPEN POSITION. MAINTENANCE RESECURED THE GUST LOCK BUSHING IN ACCO RDANCE WITH AMM 52-11-00 PB 501. 2 L 7 2 4F RT A28NM 20081017 NM 2008 10 17 F3LA200800528 1 20080728 A 5321 D5367161400100 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 927FR 2 2209 DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 242FF WAS DAMAGED IN SEVERAL PLACES. MAINTENANCE REPAIRED FLOOR PANEL I N ACCORDANCE WITH A319 SRM 53-02-00, PARAGRAPH 3, SOLUTION B, PAGE 245. 2 L 7 2 4F RT A28NM 20081017 CE 2008 10 17 GUUA10090801 1 20081009 A 3233 2570022 ACTUATOR BEECH 1900 1900D 1154162 CE NLG CRACKED A GUUA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 29 81536 15196 UE152 FLIGHT 9159 TPA/VPS - PILOT REPORTED POST FLIGHT INSPECTION FOUND HYD LEAK NOSE GEAR ACTUATOR AREA. REPLACED NOSE GEAR ACTUATOR. 2 L 7 2 4T RT A24CE 20081017 NM 2008 10 17 KNNA20080021 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 578, STR 3L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 CALA0800966 1 20081013 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59630 27534 LEFT FUSELAGE FRAME IS CRACKED AT PSU RAIL SUPPORT BRACKET MOUNT RIVET LOCATED BETWEEN STRINGER 8 AND 9 AT STATION 440. INSTALLED REPAIR DOUBLER PER EA 5310-04498 OP 2. 2 L 7 2 4F RT A16WE 20081017 2008 10 17 CALA0800967 4 20081013 A 2565 65C1990115 CABLE BOEING 737 737524 1384721 NM EVAC SLIDE BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 46625 27529 R-2 DOOR ESCAPE SLIDE LATCH CABLE HAS BROKEN STRANDS, REFERENCE WORK CARD 24-0550-1-0004 STEP 16. REMOVED AND REPLACED R-2 DOOR ESCAPE SLIDE LATCH CABLE ASSY REF M/M 25-61-35. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 CALA0800971 1 20081013 A 5311 654652 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59630 27534 LEFT FUSELAGE FRAME IS CRACKED AT PSU RAIL SUPPORT BRACKET MOUNT RIVET LOCATED BETWEEN STRINGERS 8 AND 9 AT STATION 827. REMOVED DAMAGE AREA AND INSTALLED REPAIR ANGLES A AND B REF ECRA 5311-01427. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 2008UALA06041 1 20081008 A 2611 PU90499R2 SMOKE DETECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LAVATORY CRACKED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 548UA 25396 LAV A SMOKE DETECTOR CRACKED. REPLACED LAV A SMOKE DETECTOR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081017 NM 2008 10 17 2008UALA06044 1 20081009 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 CREW REPORT: EMERGENCY EXIT LIGHT INOP ROW 45 ABC THRU 57ABC. DISCONNECTED CONNECTOR & FOUND DAMAGE TO SUPPLY WIRE. R ECONNECTED LOOSE EMERGENCY LIGHT CONNECTOR. REPLACED BAD & WET SUPPLY WIRE FOR EMERGENCY LIGHT SYSTEM. OPS CK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081017 NM 2008 10 17 2008UALA06046 1 20081008 A 2432 263BC1012 CHARGER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 772UA 26930 STATUS MSG BATTERY CHARGER APU. REPLACED-CHARGER, NO HELP. RELOADED ELMS P310 ELECTRONIC UNIT OPC AND OPS SW PER MM24- 09-00 PG201 THIS CLEARED THE FAULTS. AFTER RELOAD ACCOMPLISHED TEST OF APU BATTERY & CHARGER. RAN APU FOR HALF HOUR AND THE APU BAT CHARGER POWER CIRCUIT BREAKER ON THE P320 PANEL POPPED. INSTALLED NEW APU BATTERY CHARGER. OP'S CHECKED GOOD . 2 L 7 2 4F 4 F RT T0001SE E46NE 20081017 NM 2008 10 17 2008UALA06047 1 20081008 A 2432 263BA1011 BATTERY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FAULTY A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 772UA 26930 STATUS MSG APU BATTERY. REPLACED BATTERY, NO HELP. RELOADED ELMS P310 ELECTRONIC UNIT OPC AND OPS SWICH PER MM24-09-00. THIS CLEARED STORED FAULTS. AFTER RELOAD ACCPLISHED TEST OF APU BATTERY & CHAGER TO ENSURE PROPER OPS. NO MESSAGES FOUN D ON EICAS. ACCOMPLISHED OPS TEST OF THE APU BATTERY. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081017 NM 2008 10 17 08FDEA04296 1 20081010 A 5311 AGA800219 FRAME DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 576FE 48501 CORROSION ON FRAME LOWER AT AFT CARGO BILGE STA. 1979 L49L-49R. AFT CARGO LOWER FRAME AT BILGE STA. 1979 L49L - L49R D AMAGED REMOVED, REWORKED EXTRUSION P/N: S4933678X7075-0 AS PER DRAWING AGA8002 AND INSTALLED IN PLACED AS PER SRM 51-3 1-01 VOL. II. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 08FDEA04297 1 20081010 A 5311 AGA713447 FRAME DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 576FE 48501 CORROSION ON FRAME LOWER AT AFT CARGO BILGE L50L- L50R. CORRODED FRAME AT AFT CARGO BILGE BS 1967 L50L- L50R REMOVED A ND REPLACED WITH A FABRICATED FRAME AS PER SRM 51-31-01. FRAME FABRICATED AS PER E.A. 1-5310-123128. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 2008UALA06054 1 20081009 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 528UA 25018 EMERGENCY EXIT PATH LIGHTING LOOSE NEAR ROW 14. SECURED EEL STRIP AND COVER. CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081017 NM 2008 10 17 08FDEA04298 1 20081010 A 5330 655457235 SKIN BOEING 727 727225 1384077 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 468FE 21452 SKIN DENTES AND HOLES BS 620 TO 635 S25R. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 DHLA2008745512 1 20080901 A 5311 ATTACH FITTING BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 745DH 20665 UPPER FUSELAGE CARGO CABIN FRAME ATTACHMENT CLIP AT BS 1030 AT STRINGER 1 CRACKED. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 DHLA2008745514 1 20080901 A 5320 ATTACH FITTING BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 SO 01 745DH 20665 UPPER FUSELAGE CARGO CABIN ATTACHMENT CLIP AT BS 950B AT STRINGER 7L CRACKED. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 SWAA085497 1 20081009 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER PAE EA. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085504 1 20081009 A 3350 100031 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 783SW 29809 DURING SCHEDULED 8Y CHECK, FOUND FWD LAV AFT O/B WALL EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085453 1 20081008 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER LD LANDING 1 SW 29 733SA 27865 CENTER CEILING EMERGENCY LIGHT ASSY UNSECURED. SECURED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085485 1 20081008 A 5322 6546569 SHEAR TIE BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED MV2 CHECK, FOUND SHEAR TIE CORRODED AT BS 927.5, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEA R TIE PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085486 1 20081008 A 5313 BAC1498 STRINGER BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED MV2 CHECK, FOUND STRINGER CORRODED BETWEEN BS 933 TO BS 973, STR 26L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085487 1 20081008 A 5313 BAC1498 STRINGER BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED MV2 CHECK, FOUND STRINGER CORRODED BS 1013, STR 27L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085490 1 20081008 A 5330 6545800 BEAR STRAP BOEING 737 7373T5 1384608 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN BEAR STRAP AROUND AFT SERVICE PANEL CORRODED BETWEEN BS 947.5 TO BS 967, STR 25L. REMOVED AND REPLACED BEAR STRAP PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085515 1 20081010 A 3350 417A5700 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 283WN 36610 FOUND EEPLS LIGHT COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085521 1 20081012 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500C, BETWEEN STR 26L TO STR 28L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 08FDEA04178 1 20081003 A 5311 70750050C FRAME BOEING 757 75723A 1384967 NM BS 377 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 AFTER REMOVAL OF DOUBLER FROM TV MONITOR SUPPORT AT BS 377 FOUND SEVERAL HOLES IN FRAME. REMOVED FRAME AT BS 377 FROM S4L TO 4R IAW SRM 51-40-02. FOUND FRAME OUT OF LIMITS IAW SRM 53-00-07 FIG. 101 SHEET NR 1 . FABRICATED NEW SECTION FRAM E BS 377 FROM MAE TRAVELER T8/761952. O.K TO LOCATE AND DRILL NEW FRAME . LOCATED AND DRILLED NEW FRAME SECTION BS 377 S 4L-4R IAW SRM 51-40-05. OK TO TREAT AND PRIME, TREATED AND PRIMED NEW FRAME, INSTALLED NEW FRAME SECTION BS 377 FROM S4L -4R PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 SWAA085523 1 20081012 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 788, BETWEEN STR 26R TO STR 27R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085528 1 20081012 A 5311 6545808 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 291, STR 16R. REPAIRED FRAME PER AAR EA. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085529 1 20081011 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND BELLY SKIN CRACKED AT BS 410, LWR LOBE RADIO ALTIMETER CUTOUT. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085546 1 20081013 A 5311 6545812 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED 18Y CHECK, FOUND FRAME CRACKED AT BS 328, BETWEEN STR 21R TO STR 20R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085547 1 20081011 A 5330 6518420 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR LOWER HINGE SKIN CUTOUT CRACKED AT BS 305, WL 238. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085551 1 20081012 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 797, BELOW STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 08FDEA04196 1 20081003 A 5310 CREASE BEAM BOEING 757 75723A 1384967 NM BS 600-620 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 CREASE BEAM WEB FROM STA 600-620 RBL 65 HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED WEB AND ANGLE TRAVELER T8/7 61895 AND T8/758987 IAW SRM 51-40-02 DRAWING 143N5520. THIS IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04199 1 20081004 A 5230 6557142U29 RETAINER BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 NR 1 CARGO DOOR SEAL RETAINER HAS TWO CRACKS, DRILLED NEW SEAL RETAINER, FWD LOWER CORNER OF NR 1 CARGO DOOR. INSTALLA TION TO BE COMPLETED ON EO 7-5310-7-3369C, REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081016 NE 2008 10 16 DL76G081230 2 20080925 A 7421 PLUG BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 1 ENGINE FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 1608 30573 704871 LEFT ENGINE IGN 1 INOP. REPLACED NR 1 ENGINE 1 IGN PLUG. RAN ENGINE, OPS OK. 2 L 7 2 4F 4 F RT A1NM E13NE 20081016 NM 2008 10 16 08FDEA04214 1 20081006 A 5753 ARC40092 HINGE FITTING DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 RIGHT WING OUTBOARD FLAP INBOARD HINGE FITTING (ARC4009) INBOARD FORWARD BORE MOUNTING HOLE FOUND WITH CORROSION. REF ER SNRM NR N01221 RIGHT HAND OUTBOARD FLAP ASSEMBLY REPLACEMENT. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 SWAA085495 1 20081009 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085498 1 20081009 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER PAE EA. 2 L 7 2 4F RT A16WE 20081016 2008 10 16 SWAA085502 4 20081009 A 2565 6556685 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR ESCAPE SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085503 1 20081009 A 3350 65C27095 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 731SA 27863 DURING SCHEDULED MV2 CHECK, FOUND FWD RT SIDE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085454 1 20081004 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 255WN 32513 FOUND FWD LT FLOOR EGRESS LIGHT LENS MISSING. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081016 2008 10 16 SWAA085480 4 20081008 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085513 1 20081010 A 3350 417A5900 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 233LV 32501 DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT LIGHT BATTERY FAILED TEST AT SEAT 16 ABC. REMOVED AND REPLACED BATTERY PER M M. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085514 1 20081010 A 3350 417A5700 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 249WN 34951 FOUND EMERGENCY EXIT EGRESS LIGHT LOOSE AT FIRST ROW. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 08FDEA04204 1 20081005 A 5315 FLOORBEAM BOEING 757 75723A 1384967 NM BS 377 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 CABIN FLOORBEAM BS 377.7 BL 0- LBL 62, CORRODED AT FASTENER HOLES. REMOVED CORROSION IAW SRM 51-10-02. FABRICATED ANGLE S ON MAE TRAV T8/760222. FABRICATED STRAPS ON MAE TRAV T8/760223. INSTALLED REPAIR PARTS IAW SRM 53-00-51. MAJOR REPA IR. 2 L 7 2 4F RT A2NM 20081022 NM 2008 10 22 UPS08M53541 1 20080516 A 5753 HINGE DOUG MD11 MD11F 3023600 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A LT WING O/B FLAP I/B AFT HINGE UPPER MOUNTING FOUND CENTER BORE CORRODED. LT WING O/B FLAP I/B AFT HINGE UPPER MOUNTING CENTER BORE CORROSION REMOVED AND REPAIRED AS PER EN 1288-08. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 08FDEA04299 1 20081010 A 5313 65564417 STRINGER BOEING 727 727227 1384078 NM BS 950C-E CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 491FE 21529 AFT CARGO COMPARTMENT, S29L HAS CORROSION AND PEELING PROTECTIVE FINISH BS 950C TO 950E. REMOVED CORROSION AND FOUND OU T OF LIMITS IAW SRM 53-10-1, REMOVED FRAMES, INTERCOASTALS, FLOOR SUPPORTS, AND FAIRINGS FOR ACCESS IAW SRM 51-30-2 REMO VED AND REPLACED STRINGER 29L IAW SRM 51-30-2 REINSTALLED FRAMES, INTERCOASTALS, FLOOR SUPPORTS, AND FAIRINGS IAW SRM 51 -30-2. 2 L 7 3 4F A3WE 20081017 NM 2008 10 17 2008UALA06061 1 20081010 A 5210 BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 512UA 24809 DOOR 3R HARD TO ARM-DISARM. DOOR 4R UPPER ARMING MECHANISM CROSSTUBE BEARINGS COMING APART, SEIZED AND CORRODED. REPLA CED ARMING LEVER CROSS TUBE FORWARD BEARING. DOOR OPS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081017 EU 2008 10 17 08FDEA04301 1 20080909 A 5330 A53812632201 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 725FD 572 SKIN DAMAGE LOCATED AT FR40/41 AND S37L. REPAIRED AS PER EA 6-5330-121701. 2 L 7 2 4F RT A35EU 20081017 NM 2008 10 17 08FDEA04304 1 20081010 A 5711 SPAR BOEING 727 727233 138408A NM WS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 221FE 20932 CRACK ON WING CENTER SECTION REAR SPAR WEB STA 870 LBL 13 TO 16. 2 L 7 3 4F RT A3WE 20081017 NM 2008 10 17 KNNA20080026 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 597, STR 1. 2 L 7 2 4F A16WE 20081017 WP 2008 10 17 08FDEA04306 1 20081010 A 5330 ARC31072 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 RIGHT FUSELAGE EXTERIOR SKIN ID DENTED AT BS 499 LONGERON 14R. BLENDED GOUGES; OUT OF LIMITS IAW SRM 53-32-01. NO CRAC KS NOTED PER NTSPM 06-10-01.001. FABRICATED DOUBLER IAW SRM 53-20-00. ALODINED & PRIMED OUTSIDE SKIN IAW SRM 51-21- 01. PRIMED DOUBLER IAW SRM 51-21-01. INSTALLED DOUBLER IAW SRM 53-20-00. COMPLIED WITH E.A. 8-5330-123633. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 KNNA20080028 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 616, STR 6L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080029 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 616, STR 3L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080030 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 616, STR 2L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080031 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 616, STR 1. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080032 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 616, STR 2R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080033 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 639, STR 6L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080038 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 639, STR 6R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080039 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 685, STR 4L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080040 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 685, STR 4R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080041 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 706, STR 8L. 2 L 7 2 4F A16WE 20081016 NM 2008 10 16 DL75E081239 1 20080926 A 2530 OVEN BOEING 757 7572Q8 1384972 NM AFT GALLEY OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE CR CRUISE 1 SO 27 712TW 27624 JFK - OVEN TEMP TOO HOT, FOOD CAUGHT FIRE. AFT GALLEY POS 405, AFT GALLEY NR 2 OVEN INOP. COLLARED C/B. FWD TO NEF PE R FRC 253.30. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DLM8K081241 1 20080926 A 5312 9953015505 BULKHEAD DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DE 49997 THE STA 1463 CANTED BULKHEAD STRUCTURE AND THE OVERLYING AFTERBODY SKIN PANEL BETWEEN THE VERTICAL STABILIZER ATTACH ANG LES WERE FOUND DAMAGED BETWEEN L-2L AND L-2R. CUT OUT DAMAGE AND INSTALLED REPAIRS TO THE BULKHEAD STRUCTURE. REMOVED AND REPLACED THE SKIN PANEL. 2 L 7 2 4F RT A6WE 20081016 WP 2008 10 16 08FDEA04227 1 20081006 A 5753 ARC2147503 FAIRING DOUG MD10 MD1010F 3022112 WP LT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING OUTBD FLAP INBD HINGE LOWER BULLET ASSY LOWER SURFACE IS DENTED. REPAIRED LEFT WING OUTBD FLAP HINGE LOWER BUL LET ASSY IAW EA 8-5750-123660. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 SWAA085456 1 20081006 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 905, STR 3L TO STR 4L. REMOVED AND REPLACED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081016 NE 2008 10 16 DL738081244 2 20080928 A 7250 TURBINE BOEING 737 737832 13844CF NM CFMINT CFM56 CFM567B26US NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SO 27 383DN 27734 30346 874953 CREW HEARD LOUD BANG AT 19000 DURING CLIMBOUT. NR 1 ENG OIL PRESS WENT TO ZERO AND ENG ROLLED BACK. CREW ATB TO SJC. FOUND METAL IN TAILPIPE AND FAN WOULD NOT TURN. REPLACED NR 1 ENGINE PER TRANS 12T102AD C/W RII INSPECTION TRANS 12T120 AD QC 5011. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081016 NM 2008 10 16 DL76L081245 1 20080928 A 3397 WIRE HARNESS BOEING 767 767332 1382001 NM CABIN DEFECTIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 191DN 28448 SEAT 28FG EMERGENCY LIGHT ASSY INOP. REPLACED SEAT HARNESS AT SEAT 28FG, CHECKS GOOD PER AMM. 2 L 7 2 4F RT A1NM 20081016 NM 2008 10 16 08FDEA04248 1 20081006 A 5310 BAC15061903 CREASE BEAM BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 CREASE BEAM ANGLE FITTING ATTACHMENT AND CHORD HAS CORROSION AT S17R, BS 520-540. REMOVED AND REPLACED CREASE BEAM ANGLE S, ANGLE SPLICES, AND O/B CHORD IAW MAE TRAVELERS T8/760009, T8/760007, T8/760010 AND EA F-5310-110929. THIS REPAIR IS C LASSIFIED AS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING REQUIREMENTS. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04249 1 20081006 A 5315 FLOORBEAM BOEING 757 75723A 1384967 NM BS 1600 MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 MAIN CABIN FLOORBEAM , BS 1600 LBL 25.45 HAS MISDRILLED HOLES. REMOVED DAMAGED AREA OF FLOOR , REMOVED STIFFENER, FABRIC ATED NEW PART, ANGLE SHIMS AND STRAPS IAW SRM 53-00-51. TREATED AND PRIMES NEW PARTS, INSTALLED FABRICATED PARTS IAW SRM 51-40-02. THIS IS A CATEGORY "A" REPAIR , " MAJOR REPAIR". 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04250 1 20081006 A 5414 311N51932 SKIN BOEING 757 757236 1384971 NM NR 2 NACELLE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 NR 2 PYLON O/B FWD. 311N5193-3 SKIN PANEL HAS CORROSION ON INNER SURFACE. REMOVED HINGE TO GAIN ACCESS TO REMOVED SKIN P ER SRM 51-40-02, INSTALLED AFT T/R HINGE PER SRM 51-401-02. REMOVED FWD SKIN P/N 311N5193-2 PER SRM 51-40-02, REMOVED C ORROSION PER SRM 54-50-01. OUT OF LIMITS IAW SRM 54-50-0. FWD LOWER DOOR CORNER CUTOUT BS 106- 110 ORIG. MAT. .205 REM AINING MAT .0031. RECEIVED NEW SKIN P/N 311N5193-2. LOCATED AND DRILLED NEW SKIN PER SRM 81-40-05 AND INSTALLED NEW SK IN P/N 311N5193-2 PER DRAWING 311N5002 AND SRM 51-40-02. THIS IS A CATEGORY " A" REPAIR MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20081016 NE 2008 10 16 DL76P081248 2 20080227 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 FAILED A DALA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 1402A 25989 727893 CREW REPORTS LOSING N2 INDICATIONS ALONG WITH A C1 MESSAGE EN ROUTE TO HNL ON FLT 1465. WHEN PMA STATOR REMOVED MTC NOT ED THE PMA ROTOR DRIVE HAS FAILED. REPLACED RT ENGINE PMA. 2 L 7 2 4F 4 F RT A1NM E24NE 20081016 NM 2008 10 16 08FDEA04251 1 20081006 A 5315 141N2930 FLOORBEAM BOEING 757 75723A 1384967 NM BS 324 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 CABIN FLOORBEAM FS 324, RBL 30- 50, CORRODED. ACCOMPLISHED REWORK ON EA F-5310-123907. THIS IS A CATEGORY "A " MAJOR R EPAIR. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04224 1 20081006 A 5220 65C80678107 RETAINER BOEING 727 727227 1384078 NM EMERGENCY EXIT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 RIGHT FWD EMERGENCY EXIT HATCH, SEAL RETAINER ON DOOR, HOLE CRACKED OUT, LOWER AFT CORNER DRILLED AND INSTALLED NEW SEAL RETAINER ON RT FWD EMERGENCY EXIT HATCH ON LOWER CORNERS. REF SRM 51-30-2, PAINTED SEAL RETAINER REF MM 51-20-000-7 THI S IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 DL757081254 1 20080929 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 DURING HMV AT SAA, A DENT WAS FOUND IN A FUSELAGE SKIN SECTION WHICH HAD BEEN PREVIOUSLY SPLICED IN DURING AN EARLIER SK IN REPAIR. THE DENT WAS REMOVED AND REPAIRED PER B757 SRM GUIDELINES. THE ER/A IS CLASSIFIED AS MAJOR AND AD RELATED B ECAUSE OF THE PREVIOUS REPAIR CLASSIFICATION. 2 L 7 2 4F RT A2NM 20081016 2008 10 16 DL76L081269 4 20080930 A 2565 20131A BATTERY BOEING 767 767332 1382001 NM EVAC SLIDE DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 189DN 25990 EMERGENCY ESCAPE SLIDE RT AND LEFT SPOILER FAIL SQUIB TEST. REPLACED BOTH BATTERY AND BATTERY CHARGERS FOR ESCAPE SLIDE AND SPOILER SQUIBS. 2 L 7 2 4F RT A1NM 20081016 NM 2008 10 16 DL76G081270 1 20080930 A 2750 285T004953 FSEU BOEING 767 767332 1382001 NM E&E BAY FAULTY A DALA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 178DZ 30596 ON APPROACH SELECTED FLAPS FROM FLAPS ONE TO FLAPS FIVE AND GOT A T/E FLAP ASYM CAUTION LIGHT. LANDED WITH FLAPS LESS T HAN 5. NO FAULTS FOUND ON FSEU. RT SAM FSEU BITE FAULT BALL SET. CLEARED SAM FAULT. SUBSTITUTED -63 FSEU FOR TROUBLE SHOOTING PURPOSES. ALL FLAP POSITION SENSORS OK PER M/M. BITE TEST PASSED. INSTALLED NEW -53 FSEU BITE TEST PASS CYCL ED FLAPS NUMBEROUS TIMES FLAPS TEST OK. 2 L 7 2 4F RT A1NM 20081016 NM 2008 10 16 DL757081271 1 20080818 A 5330 SKIN BOEING 757 757232 1384965 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 ACCOMPLISH PERM REPAIR PER SRM 53-00-01, FIG 201, SHT 6 ACTL LINE 3103; HOLE/CRACK AT STA 646 LEFT HAND SIDE BELOW S17L. REMOVED EXTERNAL SPLICE AND 5 INTERNAL DOUBLERS IAW ERA470314-14 AND B757 SRM 51-40-02. INSTALLED REPAIR DOUBLER, FIL LER IAW SRM 53-00-01, FIG 201, ITEM 6 OF ERA 470314-14. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081272 1 20081001 A 5754 SKIN BOEING 757 757232 1384965 NM L/E SLAT GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 SMALL GOUGE ON T/E OF SLAT NR 3. REMOVED DAMAGED LOWER SKIN ON NR 3 SLAT AND PREPARED AREA FOR INSTALL OF FLUSH REPAIR IAW B757 SRM 51-70-10 REPAIR 4 FIG 202. BONDED REPAIR DOUBLER IAW SRM 51-70-10. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081273 1 20081001 A 5753 FLAP BOEING 757 757232 1384965 NM WING GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 RIGHT OUTBOARD MAIN FLAP L/E GOUGED ON I/B END. BLENDED OUT GOUGE IAW 757 SRM 51-10-02; OUT OF LIMITS. INSTALLED REPAI R DOUBLER, FILLER, AND CAP END IAW 757 SRMS 51-46-02 AND 57-53-01. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081274 1 20081001 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 UPON DAMAGE REMOVAL OF MAIN CABIN DECK PLATE, FOUND STA 1680 FLOORBEAM CORRODED IN NUMEROUS LOCATION. BLENDED CORROSION IAW 757 SRM 51-10-02. CORROSION FOUND OUT OF LIMITS. REPLACEMENT FLOORBEAM CAP INSTALLED IAW SRM 51-40-02 AND ERA 470 312-14. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04253 1 20081007 A 5347 BAC1520792 SEAT TRACK BOEING 727 727227 1384078 NM BS 940-950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 CABIN SEAT TRACK, RBL 24, BS 940-950, OB FLANGE HAS LIGHT CORROSION ON UPPER SURFACE REF SNRM N00460 REMOVED AND REINS TALLED FLOOR BOARDS BS 850-950E BL 0 TO RBL 25. REMOVED CORROSION ON SEAT TRACK OUT OF LIMITS. REMOVED, FABRICATED, TREA TED, PRIMED, PAINTED AND INSTALLED SEAT TRACK STA 890-950+10" REF SRM 51-30-2, 51-10-6, 53-10-1, MM 51-20-071, 53-20 -012-4, DWG 65-19601, BAC1520-792. THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 DL764081279 1 20081001 A 2822 PUMP BOEING 767 767432ER 1385134 NM FUEL SYSTEM MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 826MH 29713 LEFT AFT BOOST PUMP INOP C/B POPPED. FWD TO MCO AND PLACARD PER MEL 28-22-01A. REPLACED PUMP, CHECKS OK. REMOVED MCO/ PLACARD INSP WIRING AT PUMP, CKS OK. 2 L 7 2 4F RT A1NM 20081016 NM 2008 10 16 DL76L081280 1 20081003 A 5620 140T24014 WINDOW FRAME BOEING 767 767332 1382001 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 185DN 27961 LAYOVER CHECK AT LAX, LIGHTNING STRIKE DAMAGE WAS FOUND AT THE RT WINDOW FRAMES 5 AND 6. THE DAMAGE WAS REPAIRED PER B7 67-300 SRM 56-20-02, FIG 101 AS A TIME-LIMITED REPAIR. PERMANENT REPAIR IS TO REPLACE THE WINDOW FRAMES WITHIN 3000 CYC LES OR 18 MONTHS OF 11-12-04 WHICHEVER OCCURS FIRST. NOTE: ER/A 01-095039-14 REV A WAS ISSUED AS A MAJOR REPAIR BUT NE VER FORMALLY APPROVED. NO RECORD OF A PREVIOUS MRR ENTRY WAS FOUND. 2 L 7 2 4F RT A1NM 20081016 NM 2008 10 16 DL757081281 1 20081003 A 5330 146N37805 SKIN BOEING 757 757232 1384965 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 673DL 25978 DURING PSV IN ATL, A DENT WAS FOUND IN THE FUSELAGE SKIN AT STA 1679 BELOW THE S-20L LAP JOINT. A RECURRING INSPECTION ROUTINE WAS SET UP EVERY 500 FLIGHT HOURS. A PERMANENT REPAIR WAS ACCOMPLISHED BY ACTS IN VANCOUVER DURING HMV DEC 2005 . NOTE: THIS ER/A WAS PREVIOUSLY ISSUED BUT NEVER FORMALLY APPROVED AT THE TIME OF ISSUE NOR WAS AN MRR SUBMITTED. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04258 1 20081007 A 5210 507945238 WEB BOEING 727 727227 1384078 NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 LT MED 1L INTERIOR LOWER FWD CORNER BOTTOM WEB CRACKED APPROX 3/4" FROM INNER SKIN. REMOVED DAMAGE REF SRM 51-40-2 VARI FIED DAMAGE REMOVAL PER HFEC NDT MANUAL PART 6, 51-00-00. FABRICATED REPAIR PARTS REF SRM 51-40-2 INSTALLED REPAIR PART S REF SRM 51-30-2 THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 DL76S081284 1 20081003 A 5311 145T10018 FRAME BOEING 767 767332 1382001 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 136DL 23146 HMV AT YVR, THE INNER CHORD OF THE RT STA 903.5 FRAME WAS FOUND CRACKED. THE CRACK WAS REPAIRED PER ER/A 01-098604-14AD INSTRUCTIONS. NOTE: AT THE TIME OF ISSUE, THE ER/A WAS NEVER FORMALLY APPROVED, NOR WAS AN MRR ISSUED. THIS SUBMITTA L CORRECTS THIS SITUATION. 2 L 7 2 4F RT A1NM 20081016 NM 2008 10 16 08FDEA04259 1 20081007 A 5320 65593184 CHANNEL BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 A/C BAY FAIRING SUPPORT CHANNEL AT BS 776 LBL9-RBL9 CORRODED ON INNER SURFACE. CORROSION FOUND OUT OF LIMITS REF SRM 53- 10-1. REMOVED PANELS 3358L, 3458R & 3217 FOR ACCESS REF SRM51-30-2. REMOVED STIFFNER, BRACKET, & CHANNEL. FABRICA TED NEW STIFFNER, BRACKET, & CHANNEL REF SRM 51-20-1. HEAT TREATED TO T6 REF FORM 8130-3 2008-09-134 & 2008-09-135. RE INSTALLED AFTER TREAT AND PRIME REF SRM 51-10-2 &51-30-2 P1-7. REINSTALLED PANELS 3358L, 3458R &3217 REF SRM 51-30-2 P1- 7. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 DL76S081285 1 20081003 A 5330 146T32621 SKIN BOEING 767 767332 1382001 NM FUSELAGE DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 136DL 23146 HMV AT ACTS, A FUSELAGE SKIN DENT WAS FOUND AND REPAIRED PER ER/A 01-098988-14. NOTE: AT THE TIME OF ISSUE, THE ER/A W AS NEVER FORMALLY APPROVED, NOR WAS AN MRR SUBMITTED. THIS SITUATION HAS NOW BEEN CORRECTED. 2 L 7 2 4F RT A1NM 20081016 NM 2008 10 16 08FDEA04261 1 20081007 A 5320 65175953 PAN BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 RT EXT FUSE FWD LAV SERVICE PAN IS CRACKED AT LOOSE DUMP CABLE FEED THROUGH BS 301, S18-20R GAINED ACCESS TO CRACKED ARE A CLAENED AND REPAIRED CRACKS BY WELDING REF EA7-5240-114036. THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 DLM88081287 1 20081003 A 5330 5911401179 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 954DL 49885 HMV AT ATL, DENTS AND CREASES WERE FOUND AT STA 120 BETWEEN S-18L AND S-19L. THE DAMAGE WAS REPAIRED PER ER/A 09-359999 -14. NOTE: AT THE TIME OF ER/A ISSUE, AN MRR WAS NOT SUBMITTED. THIS CORRECTS THAT SITUATION. 2 L 7 2 4F RT A6WE 20081016 NM 2008 10 16 08FDEA04186 1 20081003 A 5310 CREASE BEAM BOEING 757 75723A 1384967 NM BS 663-756 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 MAIN CABIN CREASE BEAM , BS 663-756 LBL 62 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS AND FOUND T O BE OUT OF LIMITS IAW SRM 53-30-13. REMOVED, FABRICATED AND INSTALLED CREASE BEAM IAW SRM 51-40-02 AND DWG 143N5520. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04240 1 20081006 A 5330 53FX130112 SKIN BOEING 727 727233 138408A NM ZONE 100 MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 221FE 20932 CARGO DOOR SKIN AT BS 650 S25L HAS 2 FASTENERS WITH NOT ENOUGH SPACING. CUT OUT DAMAGED STRINGER AT BS 650 AND S25L , FA BRICATED STRINGER REPAIR SPLICE FABRICATED FILLER, CUT OUT DAMAGED EXT SKIN DIMS .755" FABRICATED FREEZE PLUG, FABRICA TED EXT SKIN DOUBLER, FABRICATED REPAIR TRIPLER. INSTALLED REPAIR PARTS IAW SRM 53-10-3, 51-10-7 AND SRM 53-30-3. 2 L 7 3 4F RT A3WE 20081016 NM 2008 10 16 DL76L081289 1 20081003 A 2421 745329E IDG BOEING 767 767332 1382001 NM LT ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 179DN 25144 ON ENG START LEFT GENERATOR TRIPPED, COULD NOT RESET. FWD TO MCO PLACARD PER MEL 24-00-01. PERFORMED BITE OF BPCU AND FOUND LEFT GEN DIODE REPLACE FAU, REMOVED AND REPLACED LEFT ENGINE IDG PER M/M 24-11-01 RA ENGINE W/NO FAULTS NOTED. DI SCONNECTED IDG AND RECONNECTED W/NO ABNORMAL FIELD TRIP, NO LEAKS NOTED MCO AND PLACARD REMOVED. 2 L 7 2 4F RT A1NM 20081016 NM 2008 10 16 08FDEA04241 1 20081006 A 5347 651960216 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 221FE 20932 CORROSION ON SEAT TRACK ON INBD VERTICAL SIDE FWD OF BS 1070 RBL 25. FOUND CORROSION OUT OF LIMITS, CUT OUT DAMAGED SEAT TRACK FROM BS 950 TO 1134 RBL 25, FABRICATED 2 SEAT TRACK SECTIONS, 4 ANGLE SPLICES, 2 STRAPS AND IAW SRM 53-10-5. INST ALLED REPAIR PARTS IAW SRM 53-10-5. 2 L 7 3 4F RT A3WE 20081016 NM 2008 10 16 SWAA085532 1 20081009 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 08FDEA04267 1 20081008 A 5730 651734781 SKIN BOEING 727 727227 1384078 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 LEFT WING UPPER SURFACE SKIN CRACKED AT NR 4 SPOILER I/B ACTUATOR HINGE CUTOUT REMOVED AND REINSTALLLED NR 4 SPOILER PAN EL, FABRICATED, TREATED, PRIMED, PAINTED, AND INSTALLED DOUBLER REF SRM 57-30-4, 51-10-2, 51-30-2 AND MM 51-20-000-7, MM 27-61-081-4. STOP DRILLED CRACK TO .250" REF SRM 57-30-4, NDT STOP DRILL REF D6-48875, 51-00-00 NO DEFECTS FOUND. SP OILER BOARD OPS CHECK GOOD ON N/R N00480, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 08FDEA04269 1 20081008 A 5310 655714051 GUSSET BOEING 727 727227 1384078 NM CARGO DOOR FRAME CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 LOWER FWD CARGO DOOR S/N 822, INTERNAL LOWER FRAME, 2 GUSSETS ARE CORRODED AT LWR END. 1 AT 28" AFT, 2ND AT 39" AFT. R EMOVED AND REPLACED GUSSETS REF SRM 51-30-02 P 1-4. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081016 WP 2008 10 16 08FDEA04270 1 20081008 A 5320 AEA01613 WEB DOUG MD10 MD1010F 3022112 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 556FE 46710 CENTER LANDING GEAR SPACE LT WALL UPPER AFT CORNER HAS CRACK COMING FROM HOLE FOR THERMOCOUPLE. THIS CRACK HAS BEEN ST OP DRILLED TWICE AND IS CRACKED PAST SECOND STOP DRILL. (VERIFIED CRACKED USING LFEC) REPAIRED CRACK AS REQ., REF. EA 8-5310-118303. WORK C/W PER JPF STEPS 1 THRU 10 FOR REPAIR OF CRACK. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 08FDEA04271 1 20081008 A 5347 651960216 SEAT TRACK BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 221FE 20932 CORROSION ON SEAT TRACK STA 1060 TO 1090 RBL 45. FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1. REMOVED SEAT TRACK FROM BS 1040 TO 1130 RBL 45 IAW SRM 51-30-2, FABRICATED SECTION OF SEAT TRACK IAW SRM 53-10-5, INSTALLED NEW SEAT TRACK IAW SRM 53-10-5. 2 L 7 3 4F RT A3WE 20081016 WP 2008 10 16 08FDEA04144 1 20080930 A 5340 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 389FE 46623 MAIN CARGO DOOR LOWER JAMB FITTING NR 2 AT HOLE " B ' SHOWED INITIAL CRACK INDICATION. AFTER REAMING HOLE " B " TO .5 19 AND ACCOMPLISHMENT OF E.O. 9-5230-7-5000. NO FURTHER INDICATION EXISTS AT THIS TIME. MACHINED 2 REPAIR BUSHINGS IA W SRM 53-50-00. REPAIRED HOLE " B " AT THE NR 2 FITTING LOCATION IN REFERENCE WITH SRM 53-50-00. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 08FDEA04197 1 20081004 A 5320 65244809 SUPPORT ANGLE BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 LT MLG WHEEL ABOVE GEAR UPLOCK MECHANISM, INSIDE BOX FRAME FWD LOWER CORNER, BS 910 LBL 64 TO LBL 68, WL 194, HAS CORRO SION. REMOVED CORROSION , FOUND TO BE OUT OF LIMITS, REMOVED UP LOCK ACTUATOR. REMOVED WEB AND ANGLE ATTACHED TO FRAME . FABRICATED ANGLE, INSTALLED NEW WEB, NEW SUPPORT ANGLE FOR ACTUATOR, REINSTALLED UP LOCK ACTUATOR. REF DWG 65-24480, SRM 51-30-2. CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 08FDEA04279 1 20081008 A 5311 AFA00203 FRAME DOUG MD11 MD11F 3023600 NM BS 1701 L12L DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 576FE 48501 MAIN DECK CARGO COMPARTMENT, LT SIDEWALL STRUCTURE FRAME BS 1701 FOUND DENTED, LONGERON 12L. MAIN DECK CARGO BAY, LT SI DEWALL STRUCTURE FRAME BS 1701 AT L-12L, DENTED AREA REPAIRED AS PER SRM 53-30-00 FIG. 1 VOL. I. REPETITIVE INSPECTION REQUIRED - INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRIED OUT AS PER SRM 53-30-00. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 08FDEA04280 1 20081009 A 5320 6517510119 WEB BOEING 727 727233 138408A NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 221FE 20932 AFT AIRSTAIR AREA LT LOWER TORQUE BOX HAS IMPROPER REPAIR AT LIGHTNING HOLE BS 1240. REMOVED PREVIOUS REPAIR IAW SRM 51- 30-2, CUT OUT DAMAGED AREA ON WEB IAW SRM 51-40-2, FABRICATED DOUBLER REPAIR IAW SRM 51-30-5, 53-10-2 AND 51-40-2, INSTA LLED REPAIR IAW SRM 51-40-2. 2 L 7 3 4F RT A3WE 20081016 EU 2008 10 16 08FDEA04282 1 20081009 A 5711 A57112117201 FRAME AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 426FE 245 CENTER FUSELAGE ZONE 20 REINFORCE THE UPPER FRAME BASE TO ARCH JUNCTION AT FRAME 44 FASTENER HOLE CRACKED ON FRAME FOO T FITTING. COMPLIED WITH E.A 6-5310-123911. 2 L 7 2 4F RT A35EU 20081016 EU 2008 10 16 08FDEA04283 1 20081009 A 5711 A57112182201 FRAME AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 426FE 245 FUSELAGE MAIN FRAME FRAME FOOT 45 RIGHT SIDE ,INSTALL 1ONE CADMIUM PLATED SHOULDERED BUSH MADE OF STAINLESS STEEL 17-4 PH REQUESTED BY E.A 6-5310-123911. FABED BUSHING ON MAE TRAVELER T8/761893, INSTALLED PER E.A 6-5310-123911 2 L 7 2 4F RT A35EU 20081016 NM 2008 10 16 08FDEA04288 1 20081009 A 5315 BAC150510617 FLOORBEAM BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 CABIN FLOORBEAM BS 365, BL0 - RBL 50, UPPER CHORD IS CORRODED. REMOVED AND REPLACED CABIN FLOORBEAM UPPER CHORD, BS 365, BL 0 - RBL 50 IAW SRM 53-00-51. CORROSION WAS DETERMINED TO BE OUT OF LIMITS PER SRM 53-00- 51, FIG 101. THIS REPAIR I S CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING REQUIREMENTS. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04237 1 20081006 A 5330 655457922 SKIN BOEING 727 727233 138408A NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 221FE 20932 SKIN GOUGED BS 990 S24L. BLENDED OUT AREA AND FOUND MATERIAL LOSS OUT OF LIMITS. CUT OUT DAMAGED AREA IAW SRM 53-30-3, F ABRICATED DOUBLER AND FILLER IAW SRM 53-30-3 AND 53-30-3. INSTALLED REPAIR PARTS IAW SRM 53-30-3 AND 51-30-2. 2 L 7 3 4F RT A3WE 20081016 NM 2008 10 16 08FDEA04276 1 20081008 A 5230 65561701 PANEL BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 FWD LOWER CARGO BAY, DOOR THRESHOLD WRAP AROUND SCUFF PLATE CRACKED IN SEVERAL AREAS REMOVED THRESHOLD REF SRM 51-30-2 , WELDED CRACKS REF DWG SR27-53-025 REV.C ON N/R N00383. INSTALLED THRESHOLD REF SRM 51-30-2 PG 2-14 THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081017 NM 2008 10 17 08FDEA04308 1 20081011 A 5280 652848310 LEVER BOEING 727 727233 138408A NM ZONE 700 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 221FE 20932 LEFT AND RIGHT WHEEL WELL MLG DOOR RELEASE HANDLES ARE GOUGED. REWORKED GOUGED AREAS ON LH AND RH WHEEL WELL MLG DOOR RE ALEASE HANDLES IAW B727 SRM 51-10-1, PERFORMED DYE PENETRANT INSPECTION IAW SOPM 20-20-02 NO DEFECTS NOTED TREATED A ND PRIMED AREAS. ALL STEPS ACCOMPLISHED IAW FEDEX EA 7- 3210-123502 "LANDING GEAR - L/H AND R/H MLG DOOR MANUAL RELEASE LEVER GOUGED - REPAIR" 2 L 7 3 4F RT A3WE 20081017 NM 2008 10 17 08FDEA04312 1 20081013 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 3 SUPPORT FIT TING AT HOLE B. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6 -2-100. 2 L 7 3 4F RT A22WE 20081017 2008 10 17 2008UALA06050 4 20081008 A 2565 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 528UA 25018 DOOR 2L SLIDE PRESSURE IS LOW. UNKNOWN PRESSURE LEAK. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081017 NM 2008 10 17 08FDEA04313 1 20081013 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FIT TING AT HOLES A, B, C AND D. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MA JOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 08FDEA04315 1 20081013 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 6 SUPPORT FIT TING AT HOLES A, B, C AND D. REMOVED AND REPLACED AS PER SRM 51-31-01. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 2008UALA06053 1 20081009 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 MAIN CABIN FWD OF DOOR L2, STR WEB CRACKED HI-LOK, STA 675 AT STR 11L. MAJOR REPAIR ACCOMPLISHED. REMOVED CRACKED STRI NGER WEB. FABRICATED & INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 20081017 NM 2008 10 17 08FDEA04328 1 20081013 A 5310 WINDOW FRAME BOEING 757 75723A 1384967 NM BS 335 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 LIGHTENING STRIKE AT LT CABIN WINDOW CUT OUT, BS 335. REPAIRED DAMAGE IAW SRM 56-20-06 AND MAE TRAVELER T8/760848. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING REQUIREMENTS. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 DL757081313 1 20081006 A 5320 453N1859 CHANNEL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION ON CHANNEL AT STATION 1444 TO STATION 1460 AT RBL 17. REPAIRED ON NR 00045 PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081017 EU 2008 10 17 08FDEA04330 1 20081013 A 5720 A5724105920100 STIFFENER AIRBUS 300 A300B4622R 3930312 EU LT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 LEFT WING AILERON ACTUATOR BEAM STIFFENER IS CRACKED JUST OUTBD OF RIB 6A. REMOVED LEFT WING AILERON ACTUATOR BEAM UPPER ATTACH STIFFENER JUST OUTBD OF RIB 6A IAW A300-600 SRM 51-40-21. FABRICATED A NEW STIFFENER IAW FEDEX EA 6-5720-123668 . LEFT WING AILERON ACTUATOR SUPPORT BEAM. INSTALLED NEW STIFFENER IAW A300-600 SRM 51-40-21. 2 L 7 2 4F RT A35EU 20081017 EU 2008 10 17 08FDEA04331 1 20081013 A 5720 A5724105920100 STIFFENER AIRBUS 300 A300B4622R 3930312 EU RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 RIGHT WING AILERON ACTUATOR BEAM STIFFENER IS CRACKED JUST OUTBD OF RIB 6A INSIDE PANEL 675 BB. REMOVED & REPLACED STIF FENER IAW SRM 51-40-21; PARA 5 & 7 AND DWG 25A57246859. 2 L 7 2 4F RT A35EU 20081017 NM 2008 10 17 DL757081319 1 20081006 A 5315 146N54461 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION ON FLOORBEAM STATION 1510 AT LBL 3. REPAIRED ON NR 00061 PER SRM 53-60-53 FIGURE 206. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 DL757081320 1 20081006 A 5320 146N3110187 FITTING BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION ON FASTENERS AT STATION 1441 STRINGER 29L. REPAIRED ON NR 00078 PER 51-40-02 BY REPLACEMENT OF CLIP AND FASTE NERS. 2 L 7 2 4F RT A2NM 20081017 GL 2008 10 17 08FDEA04173 2 20081002 A 7321 FUEL CONTROL DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL NR 3 ENGINE MALFUNCTIONED A FDEA C ABORTED TAKEOFF R X J PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 CE 21 384FE 46617 451125 NR 3 ENGINE FLAMED OUT ON TAKEOFF ROLL. ENGINE ROLLED BACK TO ABOUT 8% N1; FF INTERMITTENT FROM 0-500. EGT LOWER THAN OTHER 2 AT IDLE. REPLACED THE FUEL CONTROL AND FUEL PUMP. 2 L 7 3 4F 4 F RT A22WE E23EA 20081017 NM 2008 10 17 DL757081325 1 20081006 A 5315 146N544714 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION ON FLOORBEAM BS 1470 AT RBL 8. REPAIRED ON NR 00054 PER 51-40-07 STEP 7. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 DL757081327 1 20081006 A 5315 146N544712 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION ON FLOORBEAM STATION 1470 RBL 115. REPAIRED ON NR 00055 PER 51-40-02 STEP 7. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 DL757081330 1 20081006 A 5320 143N512914 ANGLE BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION ON STANDOFF ANGLE AT STATION 1502 STRINGER 28R. REPAIRED ON NR 00069 PER 51-40-02. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 KNNA20080046 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 706, STR 2R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080047 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 706, STR 10R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080048 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 726A, STR 8L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080049 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP STA 727A, STA 6L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080050 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 727A, STR 1. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080051 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 727A, STR 2R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080053 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 727B, STR 7L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080056 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 727B, STR 4R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080057 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 727B, STR 5R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080058 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 727B, STR 6R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080059 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 727B, STR 7R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080060 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 727B, STR 8R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080061 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 747, STR 6L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080062 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 747, STR 5L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080063 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 747, STR 4R. 2 L 7 2 4F A16WE 20081016 NM 2008 10 16 SWAA085518 1 20081012 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 24L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 DL757081331 1 20081006 A 5320 453N185914 CHANNEL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION AT STATION 1470 BBL 0 TO RBL 6. REPAIRED ON NR 00049 PER 51-40-04 FIGURE 1. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04168 1 20081001 A 5322 651634367 SHEAR TIE BOEING 727 727227 1384078 NM BS 1050 S27L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 AFT CARGO PIT BS 1050 AT STRINGER 27L BULGE BETWEEN SKIN AND FRAME REMOVED SHEAR TIE AND FOUND PART TO HAVE EXFOLIATION CORROSION. FABRICATED NEW SHEAR TIE FROM 7075-O AND HEAT TREATED TO T-6. DRILLED FASTENER HOLES. TREATED AND PRIMED A ND PAINTED SHEAR TIE. INSTALLED SHEAR TIE. REF SRM 51-30-02 PG 1-12, DWG DOCUMENT 65-16343 / NON ROUTINE N00721, SRM 5 1-10-2 PG 1-12 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 SWAA085524 1 20081012 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 729A TO BS 733A, STR 26R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 08FDEA04185 1 20081003 A 5414 2024T3375B DOUBLER BOEING 757 75723A 1384967 NM NR 2 PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 NR 2 PYLON PANEL 443 FRAME CUT OUT HAS SURFACE CORROSION. BLENDED AREA IAW 54-50-71 FOUND TO BE OUT OF LIMITS IAW SRM 54 -50-71. REMOVED MACHINE DOUBLER IAW SRM 51-40-02 REPLACED DOULBER IAW SRM 51-10-02. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04187 1 20081003 A 5347 SEAT TRACK BOEING 757 75723A 1384967 NM BS 900-1076 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 MAIN CABIN ,SEAT TRACK BS 900 TO BS 1076 LBL 24.75 CROWN SCRATCHED AND GOUGED. REMOVED AND REPLACED SEAT TRACK STA. 900 TO 1076 LBL 24.75 IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 SWAA085550 1 20081012 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 798, ABOVE STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 08FDEA04191 1 20081003 A 5310 CREASE BEAM BOEING 757 75723A 1384967 NM BS 1300-1320 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 LT SIDE I/B CREASE BEAM BS 1300-1320 HAS CORROSION . REMOVED AND REPLACED CREASE BEAM IAW SRM 51-40-02. FABRICATED ON M AE TRAVELER T8/759465. THIS IS A CATEGORY "A" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04194 1 20081003 A 5320 FLOOR SUPPORT BOEING 757 75723A 1384967 NM BS 1701-1720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 AFT CABIN FLOOR SUPPORT STRUCTURE BETWEEN STA. 1701 AND 1720 RBL 24 ANGLE HAS CORROSION . REPAIRED FLOOR SUPPORT AND N UT PLATE ASSY. IAW SRM 53-60-51 AND 51-40-02. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081232 1 20080926 A 5420 12N70171 DRAG ANGLE BOEING 757 757232 1384965 NM NR 1 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 DURING HMV AT SAA, THE NR 1 PYLON SHEAR TIE DRAG FITTING HAD AN ELONGATED HOLE. THE HOLE WAS OVERSIZED TO REMOVE THE EL ONGATION AND A FREEZE PLUG BUSHING WAS INSTALLED ACCEPT A NOMINAL SIZE FASTENER PER BOEING REPAIR INSTRUCTIONS. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04225 1 20081006 A 5312 69615064 ANGLE BOEING 727 727227 1384078 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 RT MAIN GEAR WHEEL WELL AFT BULKHEAD UPPER OB CORNER BS 950 APPROX RBL 67, PRESSURE DECK ATTACH REPAIR ANGLE CRACKED. REMOVED FLOOR PANEL FOR ACCESS, REMOVED REPAIR ANGLE REF SRM 51-30-2. FABRICATED SPLICE PLATE REF DWG 65-89360. TREATED PRIMED SPLICE PLATE REF SRM 51-10-2. DRILLED UP NEW ANGLE 69-61504-4 REF SRM 51-30-5 PG1 INSTALLED SPLICE PLATE AND A NGLE REF SRM51-30-2 PG 1-9 INSTALLED FLOOR PANELS STA 870-950D RBL 45-62 REF SRM 51-30-2 PGS 1-12 THIS IS CLASSIFIED AS A MAJOR REPAIR 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 DL757081261 1 20080907 A 5711 SPAR BOEING 757 757232 1384965 NM LT WING DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 LT WING REAR SPAR LWR T-CAP HAS TOOLING MARK AT RIB STA 23. COMPLETED REPAIR PER ERA 470321-14 REV O. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081262 1 20080820 A 5347 SEAT TRACK BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 SEAT TRACK HAS CORROSION STA 686-710 LBL 24.5. REMOVED AND REPLACED SEAT TRACK PER SRM 51-00-02. 2 L 7 2 4F RT A2NM 20081016 EU 2008 10 16 08FDEA04264 1 20081007 A 3260 TARGET AIRBUS 300 A300F4605R 3930327 EU NLG MISALIGNED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 650FE 726 ON CLIMB, LANDING GEAR RETRACTED. ECAM DISPLAYED LANDING GEAR RETRACTION FAULT. SELECTED POSITION DET 1 AND 2 GEAR RETR ACTION FAULT REMAINED. FLAPS WOULD NOT RETRACT, STAYED AT 15/20, ONCE LANDING GEAR DOWN ALL FLAP OPERATION RETURNED TO N ORMAL. LOST ALL AUTOMATION ON GEAR RETRACTION RETURNED TO NORMAL WITH GEAR EXTENSION. JACKED ACFT AND FOUND NLG TARGE TS MISALIGNED IAW MM 32-00-00-04. UPON FURTHER INSPECTION FOUND NLG NITROGEN COMPLETLY DEPLETED. DOWN JACKED ACFT AND SERVICED NLG STRUT IAW AMM 12-12-32-0. GEAR OPERATIONAL TEST GOOD IAW AMM 32-31-00-5. 2 L 7 2 4F RT A35EU 20081016 NM 2008 10 16 DL757081292 1 20080924 A 5320 146N543141 SUPPORT BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 DURING AAI INSPECTION AT ATS/PAE INSPECTION FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 1531-1540 RBL 17 AT NUT PLAT E LOCATIONS. REMOVED CORROSION FROM SIDEWALL SUPPORT BS 1531-1540 FOUND TO BE OUT OF LIMITS PER SRM 53-60-53. DRILLED AND LOCATED NEW PART PER SRM 51-40-02 FIG 1 AND INSTALLED PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081293 1 20080924 A 5320 146N543144 SUPPORT BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 DURING AAI INSPECTION AT ATS/PAE INSPECTION FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 1531-1540 LBL 17 AT NUT PLAT E LOCATIONS. REMOVED CORROSION FROM SIDEWALL SUPPORT BS 1531-1540. FOUND TO BE OUT OF LIMITS PER SRM 53-60-53. RECEIV ED NEW PART. DRILLED AND LOCATED NEW PART PER SRM 51-40-02 FIG 1 AND INSTALLED PER 51-40-02. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04277 1 20081008 A 5310 BAC1515553 CREASE BEAM BOEING 757 75723A 1384967 NM BS 1180 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 AREA ABOVE RT MLG WW, BS 1180 BULKHEAD ZONE 141, CREASE BEAM HAS CORROSION AT NUTPLATE. BLENDED AREA AND FOUND TO BE O UT OF LIMITS IAW SRM 53-16-13. REMOVED CREASE BEAM BS 1040-1180, FABRICATED NEW CREASE BEAM IAW SRM 53-30-13 . LOCATED AND DRILLED, TREATED AND PRIMED IAW 51-40-05 AND 51-20-01. INSTALLED CREASE BEAM IAW SRM 51-40-02. THIS IS A CATEGORY "A " REPAIR. MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04181 1 20081003 A 5315 BAC15051000617 FLOORBEAM BOEING 757 75723A 1384967 NM BS 345 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 MAIN CABIN FLOORBEAM, BS 345, RBL 0-25 HAS CORROSION. REMOVED CORROSION FROM BS 345 AT RBL 0-25. CORROSION CHECKED OUT O F LIMITS IAW SRM 53-00-51 . REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS INSTALLED REPAIR PARTS AT BS 345 LBL-53 TO RB L 32 WORK DONE IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04183 1 20081003 A 5347 SEAT TRACK BOEING 757 75723A 1384967 NM BS 1540 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 SEAT TRACK BS 1540 LBL 45 FLANGE CRACKED. REMOVED SEAT TRACK PER SRM 51-40-02. RECEIVED NEW SEAT TRACK PER MAE TRAVELER T8/759349. LOCATED AND DRILLED PER SRM 51-40-05, TREATED AND PRIMED PER SRM 54-20-01 ,PAINTED PER SRM 51-21-00-7, AND IN STALLED PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04218 1 20081006 A 5320 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 576FE 48501 DURING OPEN HOLE INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WITH CRACK IN DICATIONS AT HOLES A, B, C, AND D. MAIN CARGO DOOR LOWER JAMB, CRACKED NR 7 SUPPORT FITTING REMOVED AND REPLACED AS PE R SRM 51-31-01 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 08FDEA04219 1 20081006 A 5730 ARB74023 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 576FE 48501 06 EA FASTENER HOLES FOUND CRACK DURING HFEC INPECTION ON LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS=683.4 AND XORS=713.6. REPAIRED AS PER E.A. 1-5710-122579- A.D. 2007-07-04. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 08FDEA04220 1 20081006 A 5730 ARB74024 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 576FE 48501 05 EA FASTENER HOLES FOUND CRACK DURING HFEC INPECTION ON RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS=683.4 AND XORS=713.6. REPAIRED AS PER E.A. 1-5710-122580 - A.D. 2007-07-04. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 08FDEA04221 1 20081006 A 5730 ARC24431 SKIN DOUG MD11 MD11F 3023600 NM LT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 576FE 48501 LT WING I/B FLAP LOWER SURFACE AT WS 288.14 DENT FOUND. REPAIR CARRIED OUT AT LH WING I/B FLAP LOWER SURFACE AT STA. 28 8.140 AS PER SRM 57-10-00 FIG. 13 VOL. I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081016 WP 2008 10 16 08FDEA04228 1 20081006 A 5720 ARC06362 SPLICE DOUG MD10 MD1010F 3022112 WP ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 RIGHT WING INBD T/E AT THE MAIN LANDING SUPPORT LOWER FWD AUX SPLICE HAS CORROSION. REPLACED 2 SPLICES P/N ARC 0634-2 & P/N ARB 0636-1 IAW DWG ARC 0621. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 08FDEA04242 1 20081006 A 5347 69184251 SEAT TRACK BOEING 727 727233 138408A NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 221FE 20932 CORROSION ON SEAT TRACK LBL 25 BS 560-720. FOUND CORROSION ON SEAT TRACK OUT OF LIMITS. REMOVED SEAT TRACK AND FABRICATE D 2 SECTIONS, SPLICE ANGLELS AND 2 STRAPS IAW SRM 53-10-5. INSTALLED REPAIR PARTS IAW SRM 53-10-5. 2 L 7 3 4F RT A3WE 20081016 NM 2008 10 16 08FDEA04200 1 20081004 A 5322 6556612019 SHEAR TIE BOEING 727 727227 1384078 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 AFT CARGO BILGE FRAME SHEAR TIE CORRODED, BS 950B S28R WL 140 . REMOVED CORROSION REF SRM 51-10-1. HFEC ORIGINAL "T" IS .100', LOSS AT DEEPEST POINT IS .018" REMAINING "T" .082", OUT OF LIMITS REF SRM 53-10-1, REMOVED WEB STIFFNER AND CARGO TIE DOWN TO F.O.M. REPLACED SHEAR TIE REF SRM 51-30-2. REINSTALLED STIFFNER AND CARGO TIE DOWN REF. 51-30-02, C LASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 08FDEA04245 1 20081006 A 5330 655457224 SKIN BOEING 727 727233 138408A NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 221FE 20932 SKIN SCRATCHED BELOW COOLING BLOWER STATIC PORT RT FWD FUSELAGE BS 435 ABOVE S21R. BLENDED AREA AND FOUND MATERIAL LOSS OUT OF LIMITS, CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND REPAIR FILLERS IAW SRM 53-30-3, INSTALLED REPAIR PART S IAW SRM 53-30-3. 2 L 7 3 4F RT A3WE 20081016 NM 2008 10 16 DL76L081296 1 20081004 A 3260 WARNING SYSTEM BOEING 767 767332 1382001 NM TAIL SKID INTERMITTENT A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 183DN 27110 TAIL SKID LIGHT INTERMITTANT AT DEPARTURE. PERFORMED CHECK OF TAIL SKID AS PER MEL 32-71-02B OPS OK AT TAIL SKID YELLO W PLACARD INSTALLED PER MEL. 2 L 7 2 4F RT A1NM 20081016 NM 2008 10 16 DL757081297 1 20081005 A 3350 BR9279108 LENS BOEING 757 757232 1384965 NM R1 DOOR BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 EMERGENCY EXIT LIGHT LENS MOUNT BROKEN AT R-1 DOOR. REPLACED PER AMM33-51-002-05 ON ATS NR CARD 00085. 2 L 7 2 4F RT A2NM 20081016 NE 2008 10 16 DLM88081300 2 20081005 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 MALFUNCTIONED A DALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 27 910DL 45836 49541 718214 RT OIL PRESSURE DROPPED TO 0 AND RT OIL PRESSURE LOW MSG ON EOAP. SECURED RT ENG IN ACCORDANCE WITH THE QRH. OPENED LO WER COWL DOOR, REMOVED MAG CHIP DETECTOR. CLEANED INTO PAPER TOWEL. RE-INSTALLED MAG DETEDCTOR. PAPER TOWEL WITH ME LO CATED IN MCO PLACARD POUCH IN LOG BOOK. REPLACED NR 2 ENGINE PER TRANS 9T102. 2 L 7 2 4F 4 F RT A6WE E9NE 20081016 2008 10 16 DL76G081301 4 20081005 A 3441 HG1050AE10 IRU BOEING 767 767332 1382001 NM PWA JT8 JT8D219 52053 NE E&E BAY MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1603 29695 718214 ON TAXI OUT GOT AN EICAS MSG UNABLE RNP. THIS IS AN ADVISORY MESSAGE AND REQUIRES NO MTC ACTION BUT CREW RTB. T/S PER FIM NTF. REPLACED CTR IRU AS A PRECAUTION. 2 L 7 2 4F 4 F RT A1NM E9NE 20081016 NM 2008 10 16 DL757081304 1 20081006 A 5320 143N851212 SILL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 CORROSION WAS FOUND ON THE C1 DOOR CUTOUT LOWER SILL REQUIRING REPLACEMENT OF THE LOWER SILL OUTER CHORD. THE STA 620 F RAME WEB AND LOWER CHORD WERE ALSO CUT AND SPLICED. ER/A 06-382812-14 PROVIDES DETAILS OF THE REPAIR. 2 L 7 2 4F RT A2NM 20081016 EU 2008 10 16 08FDEA04284 1 20081007 A 3260 DSB11021 TARGET AIRBUS 300 A300F4605R 3930327 EU NLG OUT OF ALIGNMENT A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 650FE 726 ON T/O LDG RETRACTED. ECAM DISPLAYED LDG RETRACTION FAULT. SELECTED POS DET 1 AND 2. GEAR RET FAULT REMAINED ON ECAM. FLAPS WON'T RETRACT, FROM 15/20 ONCE GEAR DOWN ALL FLAP OPS NORMAL. LOST ALL AUTOMATION ON GEAR RET RETURNED TO NORMAL WITH GEAR EXTENSION. FOUND FAULT ON SFCC 1/2, EFCU 1/2, FLC 1/2, ADC 1/2. ALL RESET AND BITE CHECK OK. HARD FAULTS ON PROX BOX. JACKED ACFT AND FOUND NLG TARGETS MISALIGNED IAW MM 32-00-00-04. UPON FURTHER INSPECTION FOUND NLG NITROGEN COMPLETLY DEPLETED. DOWN JACKED ACFT AND SERVICED NLG STRUT IAW AMM 12-12-32-0. GEAR OPERATIONAL TEST GOOD IAW AMM 32-3 1-00-5. 2 L 7 2 4F RT A35EU 20081016 EU 2008 10 16 08FDEA04286 1 20081009 A 5711 A57112118201 FRAME AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 426FE 245 CENTER FUSELAGE ZONE 12 REINFORCE THE UPPER FRAME BASE TO ARCH STRUCTURE AT FRAME 45 FASTENER HOLE CRACKED ON FR4AME F OOT, RIGHT SIDE. COMPLIED WITH E.A 6-5310-123911. 2 L 7 2 4F RT A35EU 20081016 NM 2008 10 16 08FDEA04208 1 20081005 A 5753 ARC050312 HINGE FITTING DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT OUTBOARD BORE HOLE INNER SURFACE FOUND PITTING CORROSION. CORRO SION ON OUTBOARD BORE INNER SURFACE AT RT WING OUTBOARD FLAP OUTBOARD HINGE FORWARD MOUNT REMOVED AND FOUND WITHIN LIMIT AS PER CMM 57-44-09. BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09. REPAIR CLASSIFIED AS MINOR AS PER GMM 6 -2-100. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 DL757081314 1 20081006 A 5313 146N3110187 STRINGER BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION ON STRINGER 29L AT STATION 1510 AT STRINGER 29L. REPAIRED ON NR CARD 00074 PER SRM 53-00-03 DETAIL 2. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 DL757081315 1 20081006 A 5313 146N3110184 STRINGER BOEING 757 757232 1384965 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION AND CRACKS WERE FOUND ON STRINGER S-29L AT STA 1452 TO THE AFT END OF THE STRINGER SEGMENT. A NEW STRINGER SE GMENT WAS SPLICED IN PER ER/A 06-470938-14 WITH BOEING APPROVAL. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 DL757081321 1 20081006 A 5320 143N51294 ATTACH ANGLE BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 WEB ATTACH ANGLE CRACKED AT STATION 660 RBL 45. REPAIRED ON NR 00127 PER 51-20-01. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 DL757081322 1 20081006 A 5311 146N103069 FRAME BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION ON FRAME 1480 AT STRINGER 26R -26L. REPLACED FRAME ON NR 00034 PER 51-40-05. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 KNNA20080023 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 597, STR 3L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 CALA0800969 1 20081013 A 5311 65C33510 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59630 27534 RIGHT FUSELAGE FRAME IS CRACKED AT PSU RAIL SUPPORT BRACKET MOUNT RIVET LOCATED BETWEEN STRINGERS 8 AND 9 AT STATION 440 . REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLES. SEALED AND PRESERVED REPAIR REF EA 5310-04498 OP 2. 2 L 7 2 4F RT A16WE 20081017 EU 2008 10 17 2008UALA05763 1 20080907 A 2897 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUEL SYSTEM BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 425UA 508 CTR TANK PUMP 2 C/B POPPED AT DEPARTURE. FOUND 70-80 OHM SHORT TO GROUND ON CONNECTOR 7577VC-A PINS 47 & 49 WITH FUEL P UMP DISCONNECTED, REF WD 28-21-06. FOUND WIRING BURNED THRU JUST INBOARD OF Y-HYD ACCUMULATOR. REPLACED WIRING FROM 38 QA TO 757 7VC. SYSTEM TESTED OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081017 NM 2008 10 17 2008UALA05868 1 20080924 A 2530 OVEN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GALLEY SHORT A UALA K NONE M OVER TEMP IN INSP/MAINT 1 WP 29 554UA 26644 FIRST CLASS OVEN OVERHEATING. FLT DIVERTED. INTERNAL SHORT IN GALLEY OVEN. REPLACED BOTH FORWARD GALLEY OVENS. OPS C HECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081017 2008 10 17 2008UALA05871 4 20080923 A 2565 TRIGGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 547UA 25368 RIGHT OVERWING SLIDE FAILS PNEUMATIC DEPLOY. TRIGGER IS FAULTY. REPLACED TRIGGER. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081017 NM 2008 10 17 2008UALA05877 1 20080924 A 7830 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE THRUST REVERSER DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 726600 NR 2 ENGINE RT OUTBOARD REVERSER UPPER BIFURCATION PANEL INNER SKIN DELAMINATED FROM FWD END TO AFT END EDGE TO EDGE. REPLACED REVERSER HALF. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 2008UALA06516 1 20081114 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY CEILING LIGHT ABOVE ROW 7 LT INOP. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081017 NM 2008 10 17 KNNA20080066 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 747, STR 7R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080068 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 767, STR 5L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080069 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 767, STR 4L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080070 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 767, STR 2L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080071 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 767, STR 5R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080072 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 767, STR 6R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080073 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 787, STR 3L. 2 L 7 2 4F A16WE 20081020 EA 2008 10 20 QXEA200800682 1 20080612 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 784-861 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK NUMEROUS CORROSION SPOTS ON LT SIDE SEAT RAIL FS 784 TO 861. REMOVED CORROSION FROM SEAT TRACK AT FS 784 T O 861. .015 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013 AND CRJ SRM 51-21-16. 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 COMA0860395 1 20080918 A 5297 K601R507473 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 960CA 7117 ON CLIMBOUT FROM CVG RECEIVED PAX DOOR OUTER HANDLE MSG. A/C RETURNED BACK TO CVG AND LANDED SAFELY. R&R PAX DOOR WIRE HARNESS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20081020 NM 2008 10 20 AALA200802311 1 20080908 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 369AA 25196 DFW EMERGENCY LIGHT AT MID CABIN LOWER LT SIDEWALL INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT MID CABIN L OWER LT SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081020 NM 2008 10 20 NWAA084325810 1 20080922 A 3350 BATTERY PACK BOEING 757 757351 1384991 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 590NW 32990 DURING AN OVERNIGHT LINE CHECK THE LT FORWARD EMERGENCY EXIT SIGN WAS INOPERATIVE. MX ATTEMPTED TO REPLACE THE ASSOCIAT ED BATTERY PACK, BUT THE PROBLEM REMAINED. REPLACEMENT OF THE POWER SUPPLY MODULE FOR THE AFFECTED BATTERY PACK CORRECT ED THE PROBLEM. ALL OPS CHECKED NORMAL AFTER REPLACEMENT OF THE POWER SUPPLY. 2 L 7 2 4F RT A2NM 20081020 NM 2008 10 20 AALA200802301 1 20080907 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 181AN 29591 DFW EXTERIOR EMERGENCY LIGHT AT LT NR 4 DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LT NR 4 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081020 NM 2008 10 20 ASAA0853565 1 20081008 A 2150 1074847 REGULATOR BOEING 737 737890 1384527 NM NR 2 PACK FAILED A ASAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 02 584AS 4607 35682 EXCESSIVE DUCT SPLIT DURING CLIMB & CRUISE FLT LT DUCT 20 RIGHT DUCT 38. ENGINES TRIMMED DURING CRUISE N1 87.7 87.7 N2 62.7 61.8 FF 2.34 2.34 THIS WAS AT CRUISE FL 400. ACCOMP ENG BLEED AIR SYS HEALTH CK NR 1 ENG REF MM 36-11-00-700-801. HIGH STAGE REG FAILED REMOVED & REPLACED HIGH STAGE REG LEAK & OPS CHECK NORMAL REF MM 36-11-07-400-801. GROUND VERIFI CATION SUCCESSFUL. ACCOMP PRECOOLER CONT VALVE SYS HEALTH CHECK REF MM 36-12-00-700-801. GROUND VERIFIED PRECOOLER CON T VALVE FAILED. REMOVED & REPLACED NR 1 ENG PRECOOLER CONT VALVE LEAK & OPS NORMAL REF MM 36-12-00-400-801, GROUND VERI FICATION SUCCESSFUL. ACCOMP HIGH POWER ENGINE RUN ALL DUCT PRESSURES NORMAL AT ALL PWR SETTINGS REF FIG 502 CHART MM 36 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 ASAA0843573 1 20081009 A 5230 007006599 SKIN BOEING 737 7374Q8 138447Q NM CARGO DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 765AS 25102 LOWER LEFT CORNER OF MAIN CARGO DOOR BENT OUT APPROXIMATELY 2 1 2" 3". DOOR WAS CLOSED ON A CORNER OF THE AIRSTAIRS WHI CH APPARENTLY WERE MOVED AFTER CARGO DOOR WAS OPENED. REPAIRED MAIN CARGO DOOR IAW SRM 52-90-01 FIG 203 SHTS 1 3 AND EA 0500-01337. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 F3LA200800630 1 20080923 A 5315 D5347218820400 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON PASSENGER CABIN FLOORBEAM Y1292 AT FRAME 68 TO FRAME 69. MX REMOVED AND REPLACED FLOORBEAM AT FRAME 68 TO FRAME 69 IAW THE REQUIREMENTS OF A319 SRM 51-72-11. UPON COMPLETION OF THE REPAI R, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800641 1 20080925 A 5321 D5367302800000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED DELAMINATION ON FLOOR PANEL 151DE. MX REMOVED AND REPLACED THE FLOOR PANEL IAW T HE REQUIREMENTS OF A319 SRM 53-02-00. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081021 NM 2008 10 21 USA2008F00036 1 20080925 A 2760 285T0012201 MODULE BOEING 757 7572B7 1384964 NM SPOILER MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 206UW 46463 4511 27808 CLT FLT 811, ENROUTE PHL TO CUN. WHILE IN CRUISE FLT, THE SPOILER LIGHT ILLUMINATED, ALONG WITH EICAS MESSAGE "SPOILER" . THE SPOILERS WERE SELECTED DOWN AT THE TIME. AFTER DISCUSSIONS WITH OPERATIONS, THE DECISION WAS MADE TO DIVERT TO C LT. THE FLT LANDED IN CLT WITHOUT FURTHER INCIDENT. MX REPLACED THE SPOILER CONTROL MODULE M532. OPS CHECK OK. 2 L 7 2 4F RT A2NM 20081021 NM 2008 10 21 USA2008F00037 1 20080925 A 5610 141T480013 WINDSHIELD BOEING 767 767201 1385125 NM COCKPIT CRACKED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 249AU 15622 23901 ZRH FLT 710, ENROUTE PHL TO ZRH. WHILE IN CRUISE FLT, THE CAPTAINS SIDE WINDSHIELD OUTER PANE CRACKED AFTER IT HAD ARCE D. NO PRESSURIZATION WAS LOST, SO THE FLT CONTINUED TO ZRH AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE L1 WIN DSHIELD. OPS CHECK OK. 2 L 7 2 4F RT A1NM 20081021 NM 2008 10 21 USAA920081742 1 20080923 A 3350 ABS374A24 TERMINAL AIRBUS A319 A319132 3930340 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 806AW 1056 FLT NR506 - CLE-PHX, ISLE EMERGENCY LIGHT AT SEAT 12C INOPERATIVE. INSTALLED NEW TERMINAL. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081021 NM 2008 10 21 USAA920081760 1 20080825 A 5311 65465292 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 440, S9R. REPAIRED FRAME, BS 440, S9R IAW US AIRWAYS TASK CARD M1C530 02. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081763 1 20080825 A 5311 654655211 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 827, S9R. REPAIRED FRAME, BS 827, S9R IAW US AIRWAYS TASK CARD M1C530 02. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081768 1 20080926 A 5340 69353214 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - MAJOR REPAIR - C18 CHECK, CRACKED STRINGER CLIP, BS 616, S4R. REPLACED STRINGER CLIP, BS 616, S4R IAW B737 SRM 51 -40-02. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081769 1 20080917 A 5311 65458076 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - MAJOR REPAIR - C18 CHECK, CRACKED UPPER STUB FRAME, BS 294.5, S7R, WL 276. REPLACED UPPER STUB FRAME, BS 294.5, S 7R, WL 276 IAW B737-300 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081773 1 20080928 A 5330 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 433US 24555 CLT - MAJOR REPAIR - RON, CRACKED FUSELAGE SKIN, BS 727E, S22L. REPAIRED FUSELAGE SKIN, BS 727, S22L IAW B737 SRM 53-00 -01. 2 L 7 2 4F RT A16WE 20081021 EU 2008 10 21 USAA920081781 1 20080929 A 2560 P4010021 BATTERY AIRBUS A319 A319112 3930323 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST UK UNKNOWN 1 EA 19 762US 1358 FLT NR 9172 - FLL-DCA - EEL FOUR CABIN BREAKAWAY CABIN FLASHLIGHTS USED AND DEPLETED. REMOVED AND REPLACED BATTERIES FO R EMERGENCY FLASHLIGHTS. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081022 EA 2008 10 22 MASA2008101300721 1 20081013 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 154SF 7154 ASH FLT 7161 CAE-ORD. CENTER OVERWING EMERGENCY LIGHT INOPERATIVE. MX RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 MASA2008101300722 1 20081013 A 5240 SEAL CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR DIRTY A MASA K NONE O OTHER CR CRUISE 1 SW 07 37342 7342 ASH FLT 1027 HNK-LIH. SERVICE DOOR SQUEALING IN FLIGHT. MX CLEANED AND LUBED DOOR SEAL. PRESSURE LEAK CHECKED AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 MASA2008101300723 1 20081013 A 5220 HOOK AND LOOP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT WORN A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 929LR 15029 ASH FLT 2878 PHX-ELP. EMERGENCY HANDLE EXIT COVER 15A WILL NOT STAY ON. MX REPLACED VELCRO. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 MASA2008101400725 1 20081014 A 3350 LENS CNDAIR CL600 CL6002D24 1390016 EA CABIN MISSING A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 905J 15005 ASH FLT 2807 PHX-SNA. EMERGENCY EXIT LIGHT LENS ROW 15 A-C MISSING. MX FOUND LENS AND RE-INSTALLED LENS. 2 L 7 2 4F RT A21EA 20081022 SO 2008 10 22 RAIA2008101600002 1 20081014 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 803HK 145077 DURING PRE FLIGHT, INTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE DEFERRED THE AFFECTED LIGHT IN ACC ORDANCE WITH THE MEL PROCEDURES. 2 L 7 2 4F RT T00011AT 20081022 SO 2008 10 22 RAIA2008101600003 1 20081014 A 3320 LIGHT EMB 145 EMB145 3260210 SO CABIN MALFUNCTIONED A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 809HK 145187 POST FLIGHT, SMOKE COULD BE SEEN COMING FROM THE READING LIGHT AT SEAT 12A. MAINTENANCE REMOVED THE BULB FROM THE LIGHT ASSEMBLY AND DEFERRED THE LIGHT ASSEMBLY. 2 L 7 2 4F RT T00011AT 20081016 NM 2008 10 16 08FDEA04229 1 20081006 A 5320 6517688104 WEB BOEING 727 727227 1384078 NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 FWD MAIN ENTRY DOOR FUSELAGE CUTOUT, SILL WEB HAS NUMEROUS GOUGES, UPPER SURFACE BS 320 LBL 64, BLENDED GOUGES GENERA TED EA FOR BLEND ALLOWANCE, BLEND IS WITHIN LIMITS REF EA7-5310-123801 TREATED AND PRIMED REF EA 7-5310-123801 THIS IS C LASSSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 08FDEA04230 1 20081006 A 5220 50797867 RETAINER DOUG MD11 MD11F 3023600 NM EMERGENCY EXIT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 585FE 48481 LEFT FWD EMERGENCY EXIT HATCH, SEAL RETAINERS, TWO RETAINERS CRACKED REPLACED LOWER AFT AND LOWER FWD SEAL RETAINERS ON LT FWD EMERGENCY EXIT HATCH REF DWG 50-7978 AND SRM 51-30-2 THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 08FDEA04231 1 20081006 A 5220 50797824 RETAINER BOEING 727 727227 1384078 NM ZONE 800 CORRODED A FDEA O O O O OTHER OTHER OTHER OTHER O O O OTHER OTHER OTHER IN INSP/MAINT 1 CE 21 485FE 21488 LEFT FWD EMERGENCYEXIT HATCH, SEAL RETAINER ON DOOR HAS CORROSION. REPLACED SEAL RETAINER TOP SIDE OF LT FWD EMERGENCY DOOR REF DWG 50-7978 AND SRM 51-30-2 THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 SWAA085471 1 20081008 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085472 1 20081008 A 5311 6546522 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085473 1 20081008 A 5330 6545771 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED 14Y CHECK, FOUND LT MAIN WHEEL WELL LOWER CHORD SKIN CRACKED AT BS 679. REMOVED AND REPLACED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085534 1 20081013 A 5340 6558280 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085539 1 20081011 A 5743 115A5211 FITTING BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING CORRODED. REPAIRED PER FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 08FDEA04310 1 20081013 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 1 SUPPORT FIT TING AT HOLES A, B AND C. BUSHING REPAIRED AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6 -2-100. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 08FDEA04314 1 20081013 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSPECTION ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FIT TING AT HOLE A, C AND D. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARRIED OUT AS PER SRM 53-5 0-00. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 08FDEA04320 1 20081013 A 5744 ARC050311 HINGE FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 LEFT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR HOLE INBOARD BORE HOLE FOUND WITH CORROSION. CORROSION RE MOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-122591, THIS REPAIR IS C LASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 F3LA200800466 1 20080714 A 5320 D5347047920400 PROFILE AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 918FR 19 1943 DURING C-4/ S-1 C-CHECK, INSPECTION NOTED THE AFT CARGO COMPARTMENT, LEFT SIDE PROFILE AFT OF FRAME C62, HAS CORROSION. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11, 51-21-11 AND 51-44-11. 2 L 7 2 4F RT A28NM 20081017 NM 2008 10 17 F3LA200800467 1 20080714 A 5315 DAN338C05 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 918FR 19 1943 DURING C-4/S-1 C-CHECK, INSPECTION NOTED AFT CARGO COMPARTMENT CENTER FLOORBEAM BETWEEN FRAME C58 AND C59 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED CORRODED FLOORBEAM IN ACCORDANCE WITH A319 SRM 51-42-11. 2 L 7 2 4F RT A28NM 20081017 EU 2008 10 17 F3LA200800502 1 20080717 A 5321 D5367150100000 FLOOR PANEL AIRBUS A319 A319112 3930323 EU FUSELAGE DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 943FR 18 2518 DURING C2 C-CHECK, INSPECTION NOTED THE TOP LAYER DELAMINATED ON FLOOR PANEL 251NF. MAINTENANCE REMOVED DELAMINATED LAY ER AND APPLIED MYLAR PATCH IN ACCORDANCE WITH A319 SRM 53-02-00. 2 L 7 2 4F RT A28NM 20081017 CE 2008 10 17 GUUA10090801R1 1 20081009 A 3233 2570022 ACTUATOR BEECH 1900 1900D 1154162 CE NLG CRACKED A GUUA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 29 81536 15196 UE152 FLIGHT 9159 TPA/VPS - PILOT REPORTED POST FLIGHT FOUND HYD LEAK NOSE GEAR ACTUATOR AREA. REPLACED NOSE GEAR ACTUATOR. 2 L 7 2 4T RT A24CE 20081017 NM 2008 10 17 WX0A070237 1 20081003 A 5320 39361901 BRACKET DOUG MD80 MD83 3023681 NM GIRT BAR CORRODED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 874G 49643 REPLACED AFT GIRT BAR BRACKET P/N 3936190-1 ON THE R-1 DOOR DURING THRESHOLD CORROSION REPAIR. CLEANING AT STATION 174 - 195, RBL - 55. REFERENCE E58 - 6196852. 2 L 7 2 4F RT 20081017 NM 2008 10 17 KNNA20080022 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 597, STR 7L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 CALA0800965 1 20081013 A 3350 D71701100 BATTERY PACK BOEING 737 737724 13844BY NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 24702 28763 SEVERAL ROWS OF EMERGENCY EXIT LIGHTS ARE INOPERATIVE. ISOLATED TO AFT GALLEY OVERHEAD BATTERY PACK. REMOVED AND REPLA CED AFT GALLEY OVERHEAD BATTERY PACK, ALL EMERGENCY LIGHTS CHECK NORMAL. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 CALA0800972 1 20081013 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59630 27534 LEFT FUSELAGE FRAME IS CRACKED AT PSU RAIL SUPPORT BRACKET MOUNT RIVET LOCATED BETWEEN STRINGERS 8 AND 9. CUT OUT DAMAG ED WEB OF FRAME STATION 867 BETWEEN S8L AND S9L AND INSTALLED REPAIR ANGLES REF EA 5310-04498 OP 2. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 CALA0800973 1 20081013 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59630 27534 FUSELAGE STATION 787 BETWEEN S8R AND S9R PSU SUPPORT BRACKET TO FRAME CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 CALA0800974 1 20081013 A 5311 6546525 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59630 27534 RIGHT FUSELAGE FRAME IS CRACKED AT PSU RAIL SUPPORT BRACKET MOUNT RIVET LOCATED BETWEEN STRINGERS 8 AND 9 AT STATION 380 . REPAIRED FRAME STATION 380 RIGHT SIDE REF EA5310-04498. 2 L 7 2 4F RT A16WE 20081017 EU 2008 10 17 08FDEA04293 1 20081009 A 3260 DSB11021 PROXIMITY SENSOR AIRBUS 300 A300F4605R 3930327 EU ZONE 700 FAILED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 CE 21 650FE 726 ON TAKEOFF LANDING GEAR RETRACTED. ECAM DISPLAYED LANDING GEAR RETRACTION FAULT. SELECTED POSITION DET 1 AND 2 GEAR RETR ACTION FAULT REMAINED ON ECAM. FLAPS WOULD NOT RETRACT, STAYED AT 15/20 ONCE LANDING GEAR DOWN ALL FLAP OPERATION RETURN ED TO NORMAL. LOST ALL AUTOMATION ON GEAR RETRACTION RETURNED TO NORMAL WITH GEAR EXTENSION. JACKED ACFT AND FOUND NL G TARGETS MISALIGNED IAW A MM 32-00-00-04. UPON FURTHER INSPECTION FOUND NLG NITROGEN DEPLETED. DOWN JACKED ACFT AND S ERVICED NLG STRUT IAW AMM 12-12-32-0. GEAR OPERATIONAL TEST GOOD IAW AMM 32-31-00-5. 2 L 7 2 4F RT A35EU 20081017 NM 2008 10 17 08FDEA04294 1 20081009 A 5313 7075T6063 STRINGER BOEING 757 75723A 1384967 NM BS 890 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 FWD. PIT STRG 25L CORRODED AT BS 890. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03. CUT OUT DAMAGED AREA IAW SRM 53-00-03, FABRICATED ON MAE TRAVELER T8/762141 IAW SRM 53-00-03. LOCATED AND DRILLED STRINGER IAW SRM 51 -40-05, TREATED AND PRIMED STRINGER IAW SRM 51-20-02. INSTALLED STRINGER IAW SRM 53-00-03. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 08FDEA04295 1 20081009 A 5347 BAC15207927178 SEAT TRACK BOEING 727 727227 1384078 NM BS 720F-750 MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 468FE 21452 STA 720F LBL 45 HAS HOLE FOR FLOORBOARD DRILLED ON EXISTING SEAT TRACK SPLICE ON A FASTENER. REMOVED SEAT TRACK AND SPLI CE BS 720F - 750 LBL 45 IAW SRM 51-30-2. LOCATED, DRILLED, DEBURRED NEW SEAT TRACK SECTION IAW SRM 53-10-5. FABRICATED SPLICE ANGLE IAW SRM 53-10-2 FIG 7, AND 51-30-5, AND 51-30-8. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED, IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20081017 NM 2008 10 17 2008UALA06039 1 20081008 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 665UA 29237 THE 15AB EEL LIGHT INOP. REPLACED LAMP. TEST OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081017 NM 2008 10 17 2008UALA06040 1 20081008 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 665UA 29237 LT MID LAV EEL LIGHT INOP. SECURED CONNECTOR TEST OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081107 NM 2008 11 7 2008UALA06042 1 20081009 A 7920 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT ACTIVATED A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 659UA 27114 THE 'L OIL FILTER' STATUS MSG DISPLAYED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081017 NM 2008 10 17 2008UALA06043 1 20081009 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 664UA 29236 EEL STRIP DAMAGED AT SEAT 16H. REPLACED LIGHT STRIP, TEST OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081017 NM 2008 10 17 2008UALA06045 1 20081009 A 3320 1167008141 ELECTRONIC UNIT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LIGHTS MALFUNCTIONED A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 119UA 28812 REPORT OF SMOKE ODOR AT 41-42 ABC. OCCURRED WHEN COVE LIGHT CAME ON AND READING LIGHT WENT OUT. ODOR DISSIPATED AFTER A WHILE. FOUND OVERHEAD DECODER ABOVE SEAT 41ABC SHORTED, DEACTIVATED OVERHEAD DECODER. NOW ROWS 41 AND 42 ABC WITH NO RESIDING LIGHTS. REPLACED OVERHEAD ELECTRONICS UNIT. 2 L 7 4 4F 4 F RT A20WE E24NE 20081017 NM 2008 10 17 CALA0800963 1 20081010 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 FUSELAGE STATION 360 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET INBOARD RIVET BETWEEN STRINGERS 8 AND 9. REPAIRED 360 FRAME AT STR 8-9 LEFT PER ECRA 5310-04845. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 CALA0800964 1 20081010 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59630 27534 CABIN STATION 907 BETWEEN S8R AND S9R PSU SUPPORT BRACKET TO FRAME CRACKED, APPROXIMATELY 1 INCH. REPAIRED FRAME PER EA 5310-04498 OPT 2. 2 L 7 2 4F RT A16WE 20081017 EU 2008 10 17 08FDEA04303 1 20080909 A 5330 A53812632201 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 725FD 572 SKIN DAMAGE LOCATED AT FR43/44 S40L. REPAIRED AS PER EA 6-5330-121701. 2 L 7 2 4F RT A35EU 20081017 NM 2008 10 17 DL76G081335 1 20081007 A 3610 80217010 SHUTOFF VALVE BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 176DZ 29697 706619 RIGHT ENGINE HPSOV ANNUNCIATOR ILLUMINATED DURING FLIGHT ALONG W/ BLEED LT ON RIGHT PACK. DEACTIVATED RIGHT ENGINE HPSO V AND RIGHT THRUST REVERSER PER MEL 36-11-02 FWD TO MCO AND PLACARD. 2 L 7 2 4F 4 F RT A1NM E13NE 20081017 NM 2008 10 17 UIEA200800330 1 20081013 A 2120 UNKNOWN BOEING 747 747481 NIR NM COCKPIT ODOR A UIEA A UNSCHED LANDING B G SMOKE/FUMES/ODORS/SPARKS MULTIPLE FAILURE CL CLIMB 1 EA 15 429MC 24833 AIR TURNBACK - LLCCAFR SWITCH IN POSITION "BOTH" TEMP SELECTED FOR 7° LOWER FORWARD , AFT MAIN DECK, FWD AND AFT. THE A IR IN THE COCKPIT WAS UNCONTROLLABLE - HIGH PRESS AIR BLOWING AROUND NAV DISPLAY - SELECTED THE LLCCAFR SWITCH OFF TO CO NTROL THE TEMP IN THE COCKPIT CAUSED A BURST OF MIST COMING FROM AND AROUND ALL NAV DISPLAYS & MCP PANEL. THE COCKPIT F ILLED WITH A STRONG ODOR OF OVERHEAT. LOST EICAS DISPLAYS AND PFDS. 2 L 7 4 4F RT A20WE 20081016 NM 2008 10 16 08FDEA04233 1 20081006 A 5414 311N504633 SKIN PANEL BOEING 757 757236 1384971 NM NR 2 NACELLE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 NR 2 PYLON I/B AFT SKIN PANEL, 311N5046-33, HAS CORROSION ON INNER SURFACE. REMOVED AND REPLACED NR 2 PYLON I/B AFT SKIN PANEL IAW SRM 51-40-02 AND DRAWING 311N5002. CORROSION WAS DETERMINED TO BE OUT OF LIMITS IAW SRM 54-50-01. THIS RE PAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING REQUIRED. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04236 1 20081006 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 950D CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 PANEL RACK- AFT PIT "Z" ANGLE BS 950D 10" LT SIDE HAS CORROSION ON TOP SIDE REMOVED CORROSION MATERIAL LOSS OF .015 ORIG INAL THICKNESS .056 REMAINING MATERIAL .041 FOUND OUT OF LIMITS REF SRM 53-10-1. TRANSFERED HOLES TO NEW PART (65-5756 8-13) AND INSTALLED NUT PLATES REF SRM51-30-2 TREATED AND PRIMED REF SRM 51-10-2 AND MM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 08FDEA04243 1 20081006 A 5320 694487713 FLOOR SUPPORT BOEING 727 727227 1384078 NM BS 950A CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 CRACKED IN FLOOR BOARD "Z" ANGLE SUPPORT WEB AT FS 950A + 16, LBL 17, WL 144 REMOVED AND REPLACED SUPPORT WEB REF SRM 51 -30-2 PG 1-10 THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 08FDEA04247 1 20081006 A 5340 66138153 ATTACH ANGLE BOEING 727 727227 1384078 NM BS 910 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 LT MLG WHEEL WELL ABOVE GEAR UPLOCK MECANISM, BS 910 LBL 64 TO LBL 68 WL 194 FWD SIDE OF BOX FRAME LOWER ATTACH ANGLE CORRODED AND CORROSION EMINATING FROM UNDER ANGLE ON LOWER WEB REMOVED ANGLE REF SRM 51-30-2, CLEANED AREA AT SURFACE OF LOWER WEB, NO CORROSION FOUND REF SRM 51-10-2 INSTALLED ATTACH ANGLE REF SRM 51-30-2. (CLASSIFIED AS A MINOR REPAIR ) 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 DL76L081246 1 20080928 A 3830 FITTING BOEING 767 767332 1382001 NM GALLEY CLOGGED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 182DN 25987 A/C RTB DUE TO WATER COMING OUT OF AFT FLOOR DRAINS WHENEVER WATER IS POURED INTO AFT GALLEY DRAINS. ALSO HAD A PROBLEM WITH A WATER LEAK FROM A FWD GALLEY COFFEEMAKER. TURNED OFF WATER IN AFT GALLEY AND DEFERRED WATER PER MEL. PUT FWD C OFFEEMAKER ON NEF. UNCLOGGED GALLEY DRAIN. FOUND CLOG IN Y-FITTING BY BULK CARGO AFT WALL. OK FOR SERVICE. MCO AND P LAC REMOVED. 2 L 7 2 4F RT A1NM 20081016 NM 2008 10 16 DL76L081278 1 20081001 A 2421 753335WE TERMINAL BLOCK BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 IDG UNSERVICEABLE A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 188DN 27583 727725 DURING NR 1 ENGINE IFSD FOUND IDG TERMINAL BLOCK LOOSE AND TERMINALS ARCHED. REPLACED IDG TERMINAL BLOCK. GENERATOR FE EDER CABLE TERMINAL ENDS PER AMM. CONNECTED IDG PER M/M 24-11-20. RAN ENG PER MM, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081016 NM 2008 10 16 DL757081305 1 20081006 A 5330 143N31512 SKIN BOEING 757 757232 1384965 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 LIGHTNING STRIKE DAMAGE WAS FOUND IN THE FUSELAGE SKIN FORWARD OF STA 560 AT S-9R. THE DAMAGE WAS CUT OUT AND REPAIRED PER ER/A 06-450569-14 WITH BOEING APPROVAL. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL76L081306 1 20081006 A 5420 311T31571 TEE FITTING BOEING 767 767332 1382001 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 174DN 24802 THE CLOSEOUT TEE AT THE MIDSPAR FITTING OF THE NR 1 PYLON WAS FOUND CRACKED. THE PART WAS REPLACED PER ER/A 01-452214-1 4AD. 2 L 7 2 4F RT A1NM 20081016 NM 2008 10 16 SWAA085459 1 20081008 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 2, WL 208. REPAIRED BEAM PER PAE ER. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085460 1 20081008 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085464 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085465 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 22L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085466 1 20081007 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 22L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085467 1 20081008 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085470 1 20081008 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 08FDEA04287 1 20081009 A 5322 SHEAR TIE BOEING 727 727227 1384078 NM BS 660 SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 CABIN LEFT SIDE BS 660 FRAME, FWD SIDE SHEAR TIE BETWEEN STR 14L & 15L, 1 EA FASTENER BUCKTAIL SHEARED OFF BLEND OUT T RIPLER, PREFORMED HFEC, NO DEFECTS NOTED. INSTALLED RIVET, FILLED GAP WITH SEALENT, PAINT TO MATCH, ALL IN REF TO EA 7 -5330-113102. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081017 NM 2008 10 17 08FDEA04322 1 20081013 A 5347 65196012 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 468FE 21452 CORROSION ON SEAT TRACK BS 950 LBL 24. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED, LOCATED, DRILLED, AND DEBURRE D SEAT TRACK IAW SRM 53-10-5 AND 51-30-5 AND 51-30-8. TREATED & PRIMED TRACK & REPAIR PARTS IAW SRM 51-10-2. INSTALLE D SEAT TRACK & REPAIR PARTS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20081017 WP 2008 10 17 08FDEA04324 1 20081013 A 5240 AKC72882 ATTACH FITTING DOUG MD10 MD1010F 3022112 WP DOOR GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 RIGHT PATIO DOOR FWD END ATTACH CLIP IS GOUGED. REMOVED OLD STIFFENER (ATTACH CLIP) IAW DC/MD-10 SRM 51-35-01 VOL II. FORMED NEW STIFFENER PER FEDEX GMM 7-0-1001 SECTION 7 ITEM C & IAW DC/MD-10 SRM 51-10-00 VOL II. HEAT TREATED IAW TPS 1 003 REV "A". HRB 62/63 HT 102608-1. LOCATED; DRILLED & DEBURRED PER FEDEX GMM 7-0-1001 SECTION 7 ITEM C & IAW DC/MD-10 SRM 51-31-01 VOL II. ALODINED & PRIMED IAW DC/MD-10 SRM 51-21-01 VOL II. INSTALLED STIFFENER IAW DC/MD-10 SRM 51-35-0 1 VOL II. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 08FDEA04325 1 20081013 A 5414 311N504633 SKIN PANEL BOEING 757 75723A 1384967 NM NR 2 NACELLE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 NR 2 PYLON I/B AFT SKIN PANEL ASSY HAS CORROSION ON INNER SURFACE. REMOVED AND REPLACED SKIN PANEL ASSY PER DWG 311N5002 AND SRM 51-40-02. CORROSION ON SKIN WAS APPROXIMATELY 80% THROUGH MATERIAL. REPAIRED SKIN WAS RECEIVED ON TAG 031B66. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING REQUIREMENTS. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 08FDEA04203 1 20081005 A 5220 50797824 RETAINER BOEING 727 727227 1384078 NM EMERGENCY EXIT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 RIGHT AFT EMERGENCY EXIT HATCH, SEAL RETAINER ON DOOR, HAS HOLE CRACKED OUT. REPLACED UPPER SEAL RETAINER ON RT AFT EME RGENCY EXIT HATCH REF DWG 50-7978 AND SRM 51-30-2 PAINTED SEAL RETAINER REF MM 51-20-000-7 THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081017 EA 2008 10 17 CHQA200800196 1 20081008 A 2916 73021 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE HYDRAULIC SYSTEM FAULTY A CHQA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 11 465SM 3709 3709 7612 GEE873561 FLIGHT 5641, IAH TO LBB. THE FLIGHT CREW RECEIVED A HYDRAULIC SYSTEM 2 LOW PRESSURE MESSAGE ON EICAS. THE SYSTEM 2 QUA NTITY INDICATED 0% BUT THE PRESSURE REMAINED NORMAL DURING FLIGHT. THE AIRCRAFT DIVERTED TO AUS AND LANDED WITHOUT INCI DENT. MAINTENANCE INSPECTED THE HYDRAULIC SYSTEM AND FOUND NO LEAKS. THE SYSTEM 2 RESERVOIR WAS FOUND TO BE AT THE FUL L LEVEL AND THE SYSTEM 2 QUANTITY INDICATION WAS PLACED ON MEL. LATER THAT DAY THE SYSTEM 2 RESERVOIR WAS REPLACED AND THE MEL WAS CLEARED WITH NO FURTHER DEFECTS NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 20081017 NM 2008 10 17 KNNA20080019 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 STRINGER CLIP CRACKED STA 559, STR 4R. 2 L 7 2 4F A16WE 20081017 EU 2008 10 17 2008UALA05753 1 20080916 A 3350 CONTROLLER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 423UA 504 EMERGENCY LIGHT TEST FAILS 3 SERVICE TEST AT FLIGHT ATTENDANT PANEL. FAULT INDICATES "INT LOAD EMER L AFT" PRESENT. RE SET EXIT LIGHT CONTROLLER. EMERGENCY LIGHTS TEST OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081017 NM 2008 10 17 2008UALA06056 1 20081010 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 178UA 24385 FLOOR EEL LIGHT MISSING SEAT 54 HJK. LIGHT DISCOVERED MISSING. REPLACED SEAT EEL LAMP. OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081017 NM 2008 10 17 2008UALA06057 1 20081010 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 178UA 24385 FLOOR EEL LIGHT MISSING SEAT 56HJK. REPLACED EEL LAMP SEAT. OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081017 NM 2008 10 17 2008UALA06060 1 20081010 A 2913 3415251 REGULATOR VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE HYDRAULIC SYSTEM FAULTY A UALA D RETURN TO BLOCK W J INADEQUATE Q C WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 672UA 30027 C-HYD DEM PUMP EICAS AND PRESS LIGHT ILLUM WITH AIR DEM PUMP SWITCH IN ON POSITION ONLY WITH POWER AT IDLE. SUSPECT MAY BE C1 DEMAND PUMP LOW OUTPUT. REPLACED ADP, NO HELP. SUSPECT OVERSPEED CARD. REPLACED SPEED CARD, NO HELP. REPLACED A DP PRESSURE REGULATOR VALVE, OPERATES OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081017 NM 2008 10 17 08FDEA04334 1 20081014 A 5744 ARC050312 HINGE FITTING DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER OUTBOARD BORE HOLE FOUND WITH CORROSION. RT WING OUTBOARD FLA P OUTBOARD HINGE (WING SIDE) LOWER OUTBOARD BORE HOLE CORROSION REPAIRED AS PER E.A. 1-5750-122590, THIS REPAIR CLASSIF IED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 08FDEA04336 1 20081014 A 5744 ARC050214 HINGE DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) LOWER ATTACHMENT OUTBOARD HOLE AFT SPOTFACE FOUND SURFACE CORROSION . SURFACE CORROSION REPAIRED AS PER E.A. 1-5750-122592, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081105 WP 2008 11 5 AALA200802557 1 20080923 A 5347 5936603505 CARGO TRACK DOUG DC9 DC983 3022083 WP BS 1212-1320 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 TUL CORROSION FOUND ON RT TIE DOWN TRACK AT STATION 1212 TO 1320. AREA OF DISCREPANCY IS 108 INCHES BY 2 INCHES. REPLA CED RT TIE DOWN TRACK AT STATION 1212 TO 1320 IN ACCORDANCE WITH SRM 51-10-03 AND 51-30-01. 2 L 7 2 4F RT A6WE 20081020 EA 2008 10 20 QXEA200800689 1 20080612 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK LT SECTION OF THE 280 CROSSBEAM IS CORRODED. BLENDED CORROSION FROM LT FS 280 CROSSBEAM. .020 MATERIAL RE MOVED, BLEND IS OUT OF LIMITS IAW REO 670-53-11-046. REMOVED LT SECTION OF 280 CROSSBEAM IAW CRJ 700 SRM 51-42-06. CUT NEW CROSSBEAM IAW REO 670-53-11-047. PERFORM LPI IAW CRJ NDTM 51-20-008 NO DEFECT NOTED. INSTALLED NEW 280 CROSSBEAM IAW CRJ 700 SRM 51-40-11, REO 670-53-11-046. PRIMED AND APPLIED TOP COAT IAW CRJ 700 SRM 51-25-06 AND 51-21-11. 2 L 7 2 4F RT A21EA 20081022 2008 10 22 PNSA081001 4 20081015 A 2562 G SWITCH SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE ROTOL R390 R3904123F27 NE ELT FAILED A PNSA A UNSCHED LANDING O OTHER CR CRUISE 1 AL 03 364PX 7 7 262 WHILE IN CRUISE THE ELT TURNED ON, FLIGHT CREW ABLE TO RESET AND CONTINUED WITH FLIGHT. TWO DAY LATER THE SAME THING, A BLE TO RESET, WHEN FLIGHT ARRIVED BACK TO MAINTENANCE BASE ELT WAS CHANGED AND TESTED OK. TEAR DOWN REPORT INDICATED TH AT G-SWITCH ACTIVATED DURING TEST AT -20 DEGREES CELCIUS. SWITCH WAS CHANGED AND FUNCTIONED PROPERLY. 2 L 7 2 4T 4 T RT A52EU E8NE 6 C P31NE 20081022 NM 2008 10 22 EIAA2008101600057 1 20081015 A 5210 SKIN BOEING 747 747230B 1384889 NM R1 DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 23286 R1 DOOR SKIN CRACK AT 2 FASTENERS COMMON TO LWR AFT DOOR FRAME. REMOVED DAMAGE, NDT AREA, FABBED AND INSTALLED REPAIR P ER B747 SRM 52-10-02 FIGURE 9. 2 L 7 4 4F RT A20WE 20081022 EA 2008 10 22 MASA2008101600730 1 20081016 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 17275 7275 ASH FLT 2917 LAS-SAN. AFT EMERGENCY FLOOR LIGHTS INOPERATIVE. MX SECURED THE CONNECTOR AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081022 NM 2008 10 22 HNAA2008101700315 1 20080909 A 5315 85320044103104 REPAIR DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 931HA 51167 132 UNRECORDED AND CORRODED REPAIR FOUND ON LT FLOORBEAM AT STATIONS 270.5 AND 240.5. REMOVED UNRECORDED REPAIR AND REPLACE D WITH A REPAIR APPROVED BY EO8-53-08-3278. BRACKETS FABRICATED IN HOUSE IAW DRAWING NUMBER 85320044 AND INSTALLED IAW SRM 51-40-00. 2 H 7 2 4T RT A13NM 20081022 SO 2008 10 22 SIMA200829102 1 20081015 A 3350 78241 INVERTER EMB 135 EMB135KL 3260302 SO CABIN DEFECTIVE A SIMA O OTHER L NO TEST UK UNKNOWN 1 SW 21 801AE 145469 CREW REPORTED ON PRE FLIGHT THAT THE EMERGENCY EXIT SIGN IN CABIN CEILING ONLY ILLUMINATING ON FWD FACE DURING TEST. AF T INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 4 AC/DC POWER INVERTER IAW EMB AMM 33-50-11, OPE RATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081022 NM 2008 10 22 DHLA2000800117 1 20081016 A 3231 661516623 CABLE ASSY BOEING 727 727264 138408M NM NLG DOOR NOISY A DHLA A UNSCHED LANDING E G VIBRATION/BUFFET MULTIPLE FAILURE CL CLIMB 1 GL 05 764AT 22984 FLIGHT 935 - DURING CLIMBOUT HEARD LOUD NOISE SEEMING TO COME FROM NOSE GEAR AREA, MINUTES LATER RED DOORS LIGHT ON FWD PANEL & NOSE GEAR DOOR LIGHT ILLUM ON S/O PANEL. FELT VIBRATION. COMPLETED ABNORMAL PROCEDURE & RETURNED TO ILN. REPL ACED BOTH NOSE GEAR WHEEL WELL DOOR CABLE ASSY'S AND OPS CHECK SERVICEABLE PER MM 32-22-1. UPPER PN OFF/ON 66-15166-27, LOWER PN OFF/ON 66-15166-28. AIRCRAFT WAS GROUNDED. 2 L 7 3 4F A3WE 20081022 EA 2008 10 22 ASOA200801339 1 20081014 A 2750 TORQUE TUBE CNDAIR CL600 CL6002C10 1390015 EA TE FLAP CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 LT WING O/B FLAP I/B TORQUE TUBE CORRODED. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 ASOA200801340 1 20081014 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 934EV 8028 CREW ESCAPE HATCH-EMERGENCY EXIT PLACARD FWD OF THE HANDLE IS MISSING. APPLIED NEW SILKSCREEN FWD OF HANDLE ON CREW ESC APE HATCH IAW CRJ MM 11-10-03-400-801. SUPPLEMENTAL-SDR CLOSED 11/14/2008. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 ASOA200801341 1 20081014 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 934EV 8028 PASSENGER DOOR FWD SIDE SKIN IS CRACKED AT TOP STEP. REPAIRED PASSENGER DOOR FWD SIDE SKIN IAW BOMBARDIER REO 610R-52-1 1-702 AND ASA EC/TC CARD REO 601R-52-11-702. SUPPLEMENTAL-SDR CLOSED 11/14/2008. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 ASOA200801342 1 20081014 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 934EV 8028 PASSENGER DOOR OUTER HANDLE IS CRACKED. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 ASOA200801343 1 20081014 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 934EV 8028 PASSENGER DOOR AFT SIDE SKIN IS CRACKED IN 3 AREAS: TOP STEP, MID STEP AND CUTOUT FOR BOLT HOLE. REPAIRED PASSENGER DO OR AFT SIDE SKIN IAW REO 601R-52-11-702. ECTC REQUIRED. COMPLIED WITH PAX DOOR SIDE SKIN REPAIRS IAW ASA EC/TC REO 601 R-52-11-702. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 ASOA200801348 1 20081015 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 934EV 8028 LBL 27 OUTBOARD SIDE AT FS 484 INTERCOSTAL ANGLE CRACKED IN UPPER RADIUS. REMOVED AND REPLACED LBL 27 OUTBOARD SIDE AT FS 484 INTERCOSTAL ANGLE IAW REO 601R-53-41-059. SA EC/TC REQUIRED. C/W ASA EC/TC REO 601R-53-41-059. RII C/W 5630004 5. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 ASOA200801349 1 20081015 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 934EV 8028 RBL 36 AT FS 484 INTERCOSTAL IS CRACKED IN UPPER RADIUS. REPAIRED RBL 36 AT FS 484 INTERCOSTAL IAW REO 601R-53-41-059 R EV A. AND IAW STD MANUAL 56144. REMOVED RUDDER PULLEY BRACKET AT FS 484 RBL 36 BY REMOVING 2 BOLT & NUT COMBINATION. INSTALLED RUDDER PULLEY BRACKET WITH 2 BOLTS AND NUTS, TORQUED IAW SRM 51-41-04. C/W EC/TC REO 601R-53-41-059. RII C/W 5400005. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 ASOA200801350 1 20081015 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 934EV 8028 LBL 36 AT FS 484 INTERCOSTAL IS CRACKED IN UPPER RADIUS. UNBOLTED PULLEY BRACKET AT LBL 36 FS 484 INTERCOSTAL IAW SRM 51 -41-00. REPAIRED CRACKED INTERCOSTAL AT FS 484 LBL 36 IAW REO 601R-53-41-059. ALL STEPS C/W. PULLEY BRACKET REQUIRES INSTALL. INSTALLED PULLEY BRACKET AT FS 484 LBL 36 IAW SRM 51-41-00. C/W EC/TC REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 ASOA200801356 1 20081016 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 683BR 7692 SEVERAL EMERGENCY LIGHTS WILL NOT EXTINGUISH. BREAKER PULLED PER MTC INSTRUCTIONS. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 ASOA200801358 1 20081016 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 681BR 7680 PAX DOOR LOWER STEP BROKEN. 2 L 7 2 4F RT A21EA 20081022 SO 2008 10 22 CHQA200800200 1 20081015 A 3610 7276045 FILTER ELEMENT EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL BLEED AIR SYS DIRTY A CHQA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 GL 11 284SK 145427 CAE311482 FLIGHT 5941, CLE TO ORD. WHILE CLIMBING THROUGH FL190, THE FLIGHT CREW RECEIVED A BLD 1 OVERTEMP MESSAGE ON EICAS. THE QRH PROCEDURES WERE FOLLOWED AND BLEED 1 WAS DESELECTED AND CROSS BLEED WAS TURNED TO OPEN. THE FLIGHT ENCOUNTERED ICI NG CONDITIONS AND RECEIVED WG A/ICE FAIL, STAB A/ICE FAIL, ICE COND-A/I INOP AND THE BLEED 2 TEMPERATURE WAS INCREASING. THE DECISION WAS MADE TO DIVERT TO SBN WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND INSPECTED THE FAN AIR VALVE FILTER FOR THE NR 1 BLEED SYSTEM AND ALL INDICATIONS WERE NORMAL WHEN THE BLEEDS AND ANTI-ICE SYSTEMS WERE TESTED. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081022 NM 2008 10 22 DHLA2008745524 1 20080911 A 5340 STRINGER CLIP BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 FRAME TO STRINGER ATTACH CLIP CRACKED AT BS 950C AND STR 4L. REMOVED, FABRICATED, AND INSTALLED STRINGER CLIP IAW B727 SRM 51-10-1, 51-30-2, & 51-20-1. REF N/R 4987-2-43. 2 L 7 3 4F A3WE 20081022 NM 2008 10 22 DHLA2008745525 1 20080911 A 5340 STRINGER CLIP BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 FRAME TO STRINGER ATTACH CLIP CRACKED AT BS 720E & STR 4L. REMOVED, FABRICATED, AND REPLACED STR CLIP IAW B727 SRM 51-1 0-1, 51-30-2, AND 51-20-1. REF N/R 4987-2-72. 2 L 7 3 4F A3WE 20081022 NM 2008 10 22 DHLA2008745526 1 20080911 A 5340 STRINGER CLIP BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 DHLA 20665 FRAME TO STRINGER ATTACH CLIP CRACKED AT BS 720D & STR 5L. REMOVED, FABRICATED, AND REPLACED STR CLIP IAW B727 SRM 51-1 0-1, 51-30-2, AND 51-20-1. REF N/R 4987-2-76. 2 L 7 3 4F A3WE 20081022 SO 2008 10 22 CHQA200800201 1 20081016 A 3397 PIN EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CONNECTOR LOOSE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 289SK 145463 CAE312293 FLIGHT 5839, STL TO IAH. DURING TEST THE OVERHEAD EMERGENCY EXIT LIGHT ABOVE ROW EE WAS FOUND TO BE INOP. MAINTENANCE FOUND A LOOSE PIN ON CONNECTOR P8641. THE PIN WAS RESEATED AND THE EMERGENCY LIGHT FUNCTIONED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081022 SO 2008 10 22 CHQA200800202 1 20081017 A 3242 BRAKE SYS EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CONTAMINATED A CHQA O OTHER O OTHER LD LANDING 1 GL 11 275SK 145345 CAE312704 FLIGHT 5927, CLE TO MSP. AFTER TOUCH-DOWN DURING THE LANDING ROLL THE CREW REPORTED THAT THE BRAKE PEDALS ON THE CAPTAI N'S SIDE WENT TO THE FLOOR WITHOUT MUCH EFFECTIVENESS. THE BRAKES THEN BEGAN TO GRAB AND THE THRUST REVERSERS WERE USED TO SLOW THE AIRCRAFT. AT LOWER TAXI SPEEDS THE BRAKES WERE AFFECTIVE AND THE AIRCRAFT TAXIED TO THE GATE WITHOUT INCID ENT. MAINTENANCE BLED ALL FOUR BRAKES, AND TAXI CHECKED THE AIRCRAFT WITH THE CREW. THERE WERE NO FURTHER DEFECTS NOTE D. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081022 SO 2008 10 22 CHQA200800203 1 20081018 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 260SK 145128 CAE311802 FLIGHT 5909, STL TO IAH. DURING TEST THE EMERGENCY LIGHT ON THE LEFT SIDE NEXT TO THE OVERWING EXIT WAS FOUND TO BE INO P. MAINTENANCE SWAPPED EMERGENCY LIGHTS AND SLAVED IN A NEW BATTERY PACK FOR TROUBLESHOOTING WITH NO FIX. THE NR 5 INV ERTER WAS THEN REPLACED AND THE EMERGENCY LIGHTS OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081022 NM 2008 10 22 SWAA085567 1 20081012 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND FRAME WEB CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085568 1 20081012 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 9R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085569 1 20081012 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085570 1 20081012 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 9R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085571 1 20081013 A 3350 417A56014 SIGN BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 410WN 27897 DURING SCHEDULED MV1 CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED SIGN PER MM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085572 1 20081013 A 3350 417A56014 LIGHT BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 447WN 33720 FOUND EEPLS FLOOR TRACK LIGHT CRACKED AT ROW 1. REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085573 1 20081013 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085559 1 20081010 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, BETWEEN STR 23L TO STR 22L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085560 1 20081010 A 5753 6546486130 WEDGE BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND RIGHT WING I/B MID FLAP T/E WEDGE O/B END DELAMINATED. REMOVED AND REPLACED WEDGE PER MM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085561 1 20081010 A 5320 BAC1503100071 STRUCTURE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND LOWER CHORD CORRODED AT BS 219 LBL 6 TO WL 156. REPAIRED CHORD PER PAE ER. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085562 1 20081014 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 5R. REPAIRED WEB PER PAE ER. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085563 1 20081014 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1014, STR 7L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 2008UALA05866 1 20080923 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 SEAT 5A FWD EMERGENCY LIGHT IS INOP. LIGHT IS DEFECTIVE. REPLACED LAMP, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 EA 2008 10 23 ASOA200801244 1 20080929 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED AND REPLACED RT UPPER OBLIQUE ANGLE AT FS 621.0 TO 625.0 IAW SRM 51-40-11, 51-42-06, 51-42-21. SUPPLEMENTAL SDR CLOSED 10/15/08. 2 L 7 2 4F RT A21EA 20081023 CE 2008 10 23 ZESA2008005 1 20080512 A 2120 651542926 AIR DUCT CESSNA 500 550 2076604 CE TAILCONE DISCONNECTED E ZESA O OTHER J WARNING INDICATION CR CRUISE 1 EA 03 889B 5501047 UPON LEVELING OFF AT FL 390, CREW NOTED THAT THE EMER PRESS ANNUNCIATOR CAME ON FOR 2 SEC, THEN EXTINGUISHED. MAINTENAN CE INSPECTED THE AIRCRAFT AND FOUND BOTH ENDS OF THE RAM AIR DUCT DISCONNECTED FROM THE ELBOW IN THE TAIL CONE. A CHECK FLIGHT WAS COMPLETED SATISFACTORILY. 1 L 7 2 4F A22CE 20081017 NM 2008 10 17 F3LA200800601 1 20080906 A 5315 D5347217220400 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 929FR 26 2240 DURING C3 C-CHECK, INSPECTION NOTED SEVERAL NUT PLATE HOLES ON FRAME Y-1292 BETWEEN FRAME 66 AND FRAME 68 HAS CORROSION. MAINTENANCE REMOVED AND REPLACED FLOORBEAM IN ACCORDANCE WITH A319 SRM 51-42-11. 2 L 7 2 4F RT A28NM 20081017 NM 2008 10 17 WX0A070238 1 20081003 A 5320 FLOOR SUPPORT DOUG MD80 MD83 3023681 NM FUSELAGE CORRODED A WX0A K NONE O OTHER IN INSP/MAINT 1 WP 19 874G 49643 FLOORBOARD SUPPORT CORRODED APPROXIMATELY STATION 190 - 200, RBL - 7. INSTALLED STRAP REPAIR PER ESO 80559 DATED 10-2-0 8, USING 0800 7075 T6, 12 INCHES LONG X 5 INCHES WIDE. 2 L 7 2 4F RT 20081017 NM 2008 10 17 KNNA20080017 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA O OTHER O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 360, STR 5L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080018 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 559, STR 2R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080020 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 578, STR 8L. 2 L 7 2 4F A16WE 20081017 2008 10 17 CALA0800968 4 20081013 A 2565 65C1990115 CABLE BOEING 737 737524 1384721 NM EVAC SLIDE BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 46625 27529 L-2 DOOR ESCAPE SLIDE LATCH CABLE HAS BROKEN STRANDS, REFERENCE WORK CARD 24-0550-1-0004 STEP 16. REMOVED AND REPLACED L-2 DOOR ESCAPE SLIDE LATCH CABLE ASSY REF M/M 25-61-35. 2 L 7 2 4F RT A16WE 20081017 EU 2008 10 17 08FDEA04290 1 20081009 A 2421 764067A GCU AIRBUS 300 A300F4605R 3930327 EU NR 2 FAILED A FDEA C ABORTED TAKEOFF H G J ELECT. POWER LOSS-50 PC MULTIPLE FAILURE WARNING INDICATION TO TAKEOFF 1 CE 21 656FE 16999 16999 745 REJECTED TAKEOFF AT 30 KTS DUE TO LOSS OF ALL ELECTRICAL POWER EXCEPT EMERGENCY POWER. MULTIPLE PROBLEMS RELATED TO R AIN DRIPPING INTO AVIONICS BAY. R&R NR 2 GCU AND ALL ASSOCIATED SYSTEMS OPERATE NORMAL ON ACFT. MM 24-41-11-4 AND 24 -41-00-0. 2 L 7 2 4F RT A35EU 20081017 2008 10 17 DL75E081337 4 20081007 A 3460 FMC BOEING 757 7572Q8 1384972 NM GE CF6 CF680C2B6F 30025 NE LEFT MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 703TW 27620 706619 ON TAXI OUT LEFT FMC FAILED. REPLACED LT FMC AS PER AMM CROSSLOAD NAV DATA, ALL CHECKS NORMAL. NO FAULTS NOTED. 2 L 7 2 4F 4 F RT A2NM E13NE 20081017 NM 2008 10 17 SWAA085541 1 20081010 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 DURING SCHEDULED HC1 CHECK, FWD LT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 SWAA085542 1 20081010 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 430WN 33659 DURING SCHEDULED HC1 CHECK, AFT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 SWAA085543 1 20081012 A 3350 417A5700 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 473WN 33832 FOUND FWD EEPLS LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 SWAA085544 1 20081013 A 5330 65C33756 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED 18Y CHECK, FOUND R1 DOOR FUSELAGE SKIN LOWER EXTERNAL HINGE CUTOUT CRACKED. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 SWAA085554 1 20081010 A 3350 417A56014 SIGN BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 703SW 27837 FOUND R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 08FDEA04340 1 20081014 A 5753 STRUCTURE BOEING 727 727233 138408A NM RT WING TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 221FE 20932 CRACK ON AFT STRUCTURE OF RT INBD FLAP WBL 114.2 FABRICATED AFT STRUCTURE REPAIR FILLER, ANGLE SPLICE, INSTALLED REPAIR SPLICE AND FILLER ON RT INBD FLAP IAW SRM 57-50-2, SRM 51-40-4, AND SRM 51-30-2. 2 L 7 3 4F RT A3WE 20081017 NM 2008 10 17 08FDEA04341 1 20081014 A 5330 655457533 SKIN BOEING 727 727227 1384078 NM BS 682 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 491FE 21529 FUSELAGE SURFACE HAS DENT AT STA 682 S24L. COMPLIED WITH HFEC ON DENT IAW NDTM PT.6 51-00-00, CRACK INDICATED. CUT OUT DAMAGED AREA IAW SRM 53-30-3. FABRICATED REPAIR DOUBLER AND FILLER ACCOMPLISED IAW SRM 53-30-3 & 53-30-2. TREATED AND P RIMED AREA IAW SRM 51-10-2 AND INSTALLED REPAIR PART IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20081017 NM 2008 10 17 08FDEA04343 1 20081014 A 5330 651841568 SKIN BOEING 727 727227 1384078 NM BS 180 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 491FE 21529 DENT AROUND FASTENER STA 180 FWD OF LWR NOSE COMPARTMENT CUTOUT. 2 L 7 3 4F A3WE 20081017 NM 2008 10 17 KNNA20080078 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 807, STR 5L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080079 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 807, STR 3R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080082 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 807, STR 6R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080084 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 807, STR 9R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080085 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 807, STR 10R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080087 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 827, STR 3R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 ASAA0843567 1 20080908 A 5320 65479573 THRESHOLD BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 AFT CARGO DOOR LOWER THRESHOLD WEB CORRODED STA 805 TO STA 840 RBL 27 RBL 31 WL 147 WL 151. REMOVED DAMAGED WEB LOCATED DRILLED AND INSTALLED A REPLACEMENT WEB IAW B737 400 SRM 51 40 02 PARA 5 FIG 9 AND 10. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 ASAA0843582 1 20080914 A 5311 6546579531 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 APU INLET FRAME RT SIDE OF TORQUE BOX CORRODED. REMOVED DAMAGED FRAME STIFFENER, LOCATED DRILLED AND INSTALLED REPLACEM ENT STIFFENER IAW B737 400 SRM 51 40 02 PG 2-5. 2 L 7 2 4F RT A16WE 20081020 WP 2008 10 20 ABXA080238 1 20080905 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP EMERGENCY LIGHT DEFECTIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 971AX 47497 EMERGENCY LIGHTING INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8. 2 L 7 2 4F A6WE 20081020 NM 2008 10 20 AALA200802354 1 20080914 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 650AA 24608 LGA EMERGENCY LIGHT AT SEAT 18D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081020 NM 2008 10 20 AALA200802313 1 20080908 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 189AN 32383 DFW EMERGENCY LIGHT BATTERY PACK AT SEAT ROW 9 INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AT SEAT ROW 9. SYSTE M GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081020 EA 2008 10 20 QXEA200800688 1 20080612 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK FOUND CORROSION ON SILL OF AFT CARGO BAY DOOR. BLENDED IAW REO 670-53-61-373, .002 MATERIAL REMOVED. PERF ORMED ECI IAW REO 670-53-61-373 NO DEFECTS NOTED. TREATED, PRIMED AND PAINTED IAW REO 670-53-61-373. 2 L 7 2 4F RT A21EA 20081020 NM 2008 10 20 ABXA080241 1 20080829 A 5330 SKIN BOEING 767 767281 1385109 NM BS 1307 L25-26L BULGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 789AX 23022 SKIN BULGING AROUND RIVETS AT STA 1307L, LONG 26-25L. REPAIRED SKIN IAW ABXAIR REA B653-57726 MR. 2 L 7 2 4F RT A1NM 20081020 WP 2008 10 20 AALA200802285 1 20080906 A 3397 CONTACT DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 290AA 49302 LGA EXTERIOR EMERGENCY LIGHTS AT RT HAND OVERWING EXIT INOPERATIVE. CLEANED AND ADJUSTED CONTACT FOR EXTERIOR EMERGENCY LIGHTS AT RT HAND OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081020 EA 2008 10 20 HNAA0800285 1 20080918 A 4990 167301101 APU DHAV DHC8 DHC8311 1386006 EA APU BAY LEAKING A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 331EN 13145 279 F/A REPORTED SMOKE IN CABIN WHEN ACFT PARKED AT THE GATE. INSPECTED ACFT FOUND NO DEFECTS WITH EXTERNAL DC POWER APPLIE D TO ACFT. STARTED APU, BLEEDS OIL MIST AND SMOKE FILLED THE CABIN AND SELECTED APU OFF. GROUND RAN WITH ENGINE BLEEDS SELECTED INDIVIDUALLY, NO OIL OR SMOKE VISIBLE. R&R THE APU. 2 H 7 2 4T RT A13NM 20081020 NE 2008 10 20 C8G2008F00018 2 20080910 A 7250 TURBINE BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE DAMAGED A C8GA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SO 29 808EA 22439 ON TAKEOFF, JUST AFTER V2 THE NR 2 ENGINE FAILED. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED, WHERE IT LANDED WITH OUT INCIDENT. POST FLIGHT INSP REVEALED TURBINE DAMAGE. THE NR 2 ENGINE WAS REMOVED AND REPLACED. OPS CHECK GOOD. NO OTHER DEFECTS WERE NOTED, ACFT WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F 4 F A3WE E2EA 20081020 EA 2008 10 20 MAS2008F00085 1 20080913 A 5270 SENSOR CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR OUT OF ADJUST A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 510MJ 10101 MAIN CABIN DOOR OUTER HANDLE CAUTION MESSAGE IN FLIGHT. MX ADJUSTED SENSOR AND RESET SYSTEM OPS CHECKED GOOD. (K) 2 L 7 2 4F RT A21EA 20081020 2008 10 20 ARWA20080903 4 20080918 A 2565 SLIDE DOUG DC10 DC1030F 3023504 WP L1 DOOR UNWANTED DEPLOY A ARWA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 SO 29 450ML 47831 L-1 DOOR SLIDE RAFT DEPLOYED. REMOVED L-1 DOOR SLIDE RAFT IAW MM 26-61-07, PERFORMED DOOR CHECK FOUND NORMAL IAW MM 52- 11-07. TRANSFERRED TO DMI NR 22064 IAW MEL 52-10-2,, CAT (C). (K) 2 L 7 3 4F RT A22WE 20081020 EA 2008 10 20 A6WA200840594 1 20080926 A 4920 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY ODOR A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 415AW 14565 7593 RT PAC HAS OIL SMELL WHILE ON APU AIR. OILY SMELL DISSIPATES WHILE ON 10TH STAGE BLEED AIR. REMOVED AND REPLACED APU IA W AMM 49-10-00, OPS CHECK GOOD. (K) 2 L 7 2 4F RT A21EA 20081020 NM 2008 10 20 USAA920081659 1 20080904 A 5311 65C22908 FRAME BOEING 737 7373B7 1384580 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 FRAME CRACKED AT BS 500B BETWEEN S20R AND S21R. REPAIRED FRAME AT BS 500B BETWEEN S20R AND S21R IAW EA NR 100623. (K) 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 NSV2008F00027 1 20080916 A 5230 HANDLE BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR UNSECURE A NSVA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 EA 27 196WQ 4196 ACFT RETURNED TO FIELD AFTER TAKEOFF. AFT CARGO DOOR LIGHT ILLUMINATED AFTER TAKEOFF. FOUND AFT CARGO DOOR HANDLE NOT PROPERLY SECURED. RESEATED DOOR AS REQUIRED. NO FURTHER ACTION REQUIRED AT THIS TIME. (K) 2 H 7 2 4T RT A13NM 20081020 NM 2008 10 20 UPS08M53509 1 20080518 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A RT WING O/B FLAP O/B FWD HINGE ACTUATOR I/B BORE I/B SPOTFACE CORRODED. RT WING O/B FLAP O/B FWD HI NGE ACTUATOR I/B BORE I/B SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09. 2 L 7 3 4F RT A22WE 20081020 NM 2008 10 20 UPS08M53510 1 20080518 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A RT OUTBOARD FLAP OUTBOARD FWD HINGE ACTUATOR OUTBOARD BORE OUTBOARD SPOTFACE CORRODED. RT OUTBOARD FLAP OUTBOARD FWD HINGE ACTUATOR OUTBOARD BORE OUTBOARD SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09. 2 L 7 3 4F RT A22WE 20081020 NM 2008 10 20 UPS08M53521 1 20080520 A 5531 SPAR DOUG MD11 MD11F 3023600 NM VERTICAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A VERTICAL STABILIZER FRONT SPAR RT AT STA ZFS 353.295 FOUND SURFACE CORROSION. SURFACE CORROSION ON VERTICAL STABILIZER FRONT SPAR RT AT STA ZFS 353.295 REMOVED AS PER SRM 51-21-01 VOL II REV 35. REWORKED AREA MATERIAL ORIGINAL THICKNESS 0.190", MATERIAL REMOVED 0.012", REMAINED THICKNESS 0.178". FOUND WITHIN LIMIT AS PER SRM 55-00-01 F IG 1A VOL I REV 35. 2 L 7 3 4F RT A22WE 20081020 EA 2008 10 20 ASOA200801329 1 20081011 A 5240 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA SERVICE DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 750EV 10161 ASD AFT DRAG ANGLE IS CRACKED IN THE RADIUS WHERE MARKED. REPAIRED DRAG ANGLE IAW REO 670-52-11-072. PERFORMED ET IN SPECTION OF CUT LINES PER REO IAW NDTM 51-20-006. NO DEFECTS NOTED. FABRICATE REPAIR ITEMS. SEAL AND WET INSTALL FASTE NERS. INSTALL BLIND FASTENERS. APPLY TOPCOAT. INSTALL SOLID FASTENERS. FILLET SEAL AND INSTALL PLT FASTENERS. COMPL IED WITH STEPS 1-12 ON SHEET TO REO 670-52-11-072. ALL WORK IAW REO 670-52-11-072. 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 ASOA200801330 1 20081012 A 5530 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 750EV 10161 RIGHT SIDE VERTICAL STABILIZER HAS A CRACK IN THE FORWARD DRAG ANGLE AS MARKED. REMOVED EXISTING FASTENERS FROM REPAIR AREA AND CUT AWAY DAMAGE. PERFORMED ET INSPECTION. NO DEFECTS NOTED. FABRICATED FILLERS IAW REO 670-55-31-018. FI NAL TRIMMED DOUBLER, PER REO 670-55-31-018. FABRICATED DOUBLER. OK TO INSTALL. INSTALLED DOUBLER AND FILLER PER REO 670-55-31-018. RESTORED AREA FINISH. 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 ASOA200801331 1 20081012 A 5530 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 750EV 10161 LEFT SIDE VERTICAL STABILIZER HAS A CRACK IN THE FORWARD DRAG ANGLE AS MARKED. PERFORMED EDDY CURRENT INSPECTION ON DRA G ANGLE. END OF CRACK MARKED. CUT AWAY DAMAGE PER REO 670-55-31-018. PERFORMED ET INSPECTION OF CUT LINE. NO DEFECT S NOTED. REPAIRED PER REO 670-55-31-018. PRIMED & PAINTED. 2 L 7 2 4F RT A21EA 20081020 NM 2008 10 20 F3LA200800631 1 20080923 A 5320 D53480043204 SILL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON PASSENGER CABIN LOWER SILL LOCATED AT LT FRAME 67+17 INCHES AND FRAM E 68. MX PERFORMED STRUCTURAL REPAIR IAW THE REQUIREMENTS OF A319 SRM 53-41-14, FIGURE 201. UPON COMPLETION OF THE REP AIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 EU 2008 10 20 USAA920081789 1 20080924 A 5315 D5347228321000 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 PIT - MAJOR REPAIR - S4 CHECK, LEVEL 2 CORROSION ON FLOORBEAM FR 66, -Y465. REPLACED FLOORBEAM, FR 66, -Y465 IAW A319 S RM 51-72-11. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 USAA920081779 1 20080825 A 5311 65465262 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 400, S9L. REPAIRED FRAME BS400, S9L IAW US AIRWAYS TASK CARD M1C53002 . 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 F3LA200800648 1 20080925 A 5321 D5367228500000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE PERFORATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED FLOOR PANEL 131CG WAS PERFORATED. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMEN TS OF A319 SRM 53-02-00 PARA 8C. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800650 1 20080928 A 5321 D5361060500100 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON FLOOR PANEL 222FF, FWD GALLEY AREA. MX REMOVED AND REPLACED THE FLO OR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-12-12-000-001. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND A CCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800628 1 20080926 A 5753 D5757100800000 FLAP AIRBUS A319 A319111 3930336 NM LT WING DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 902FR 13 1515 LINE MX NOTED DAMAGE FROM A BIRD STRIKE ON THE LEADING EDGE OF THE LT WING OUTBOARD FLAP. MX REPAIRED FLAP IAW THE REQU IREMENTS OF A319 SRM 57-53-00, FIGURE 202. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 EU 2008 10 20 F3LA200800626 1 20080925 A 5321 D5367431300000 FLOOR PANEL AIRBUS A318 A318111 3940019 EU FUSELAGE DEBONDED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 808FR 29 3038 DURING C1 C-CHECK, INSPECTION NOTED THE TOP SKIN OF FLOOR PANEL 151BH WAS DISBONDED FROM THE CORE. DAMAGE WAS FOUND TO BE BEYOND REPAIRABLE LIMITS. MX REMOVED AND REPLACED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 AMM 53-42-14-400-001. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT 20081020 EU 2008 10 20 F3LA200800623 1 20080925 A 5321 D5367306800000 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 808FR 29 3038 DURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY FLOOR PANEL 131BF HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANE L IAW THE REQUIREMENTS OF A318 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCE PTABLE. 2 L 7 2 4F RT 20081020 EU 2008 10 20 F3LA200800620 1 20080925 A 5321 D5367331000000 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 808FR 29 3038 DURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY FLOOR PANEL 131AF HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANE L IAW THE REQUIREMENTS OF A318 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCE PTABLE. 2 L 7 2 4F RT 20081020 EU 2008 10 20 F3LA200800621 1 20080925 A 5321 D5367406900000 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 808FR 29 3038 DURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY FLOOR PANEL 131EG HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANE L IAW THE REQUIREMENTS OF A318 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCE PTABLE. 2 L 7 2 4F RT 20081021 NM 2008 10 21 USAA920081743 1 20080916 A 5510 69731201 HINGE PIN BOEING 737 7373G7 1384595 NM HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - MAJOR REPAIR, RT HORIZONTAL STAB OUTER HINGE PIN CORRODED AT BS 1154. REPLACED HORIZONTAL STAB OUTER HINGE PINS A T BS 1154 IAW AMERICA WEST TASK CARD I6C55039. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081754 1 20080825 A 5753 6546430136 SKIN BOEING 737 7373G7 1384595 NM FOREFLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 SAL - MAJOR REPAIR - C17 CHECK, DELAMINATING ON RT WING INBOARD FOREFLAP UPPER SURFACE, WBL 73- WBL 184.275. REPAIRED R T WING INBOARD FOREFLAP UPPER SURFACE, WBL 73- WBL 184.275 IAW B737-300 SRM 51-10-2R 2 L 7 2 4F RT A16WE 20081022 SO 2008 10 22 SIMA200828903 1 20081014 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 683AE 14500833 ON FLIGHT CREW REPORTED ON POST FLIGHT, FLIGHT ATTENDANT FOUND ROW 1-7 FLOOR EMERGENCY LIGHT STRIP INOPERATIVE. ***AWA ITING FOLLOW UP*** 2 L 7 2 4T RT T00011AT 20081022 NM 2008 10 22 DHLA2008745518 1 20081012 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 FUSE SKIN BULGED AT BS 1166, BETWEEN STR 22L & 23L. ACCOMPLISHED SKIN DOUBLER REPAIR IAW COOPESA EO COO-2-53-289-08 DAT ED 09/21/08. REPAIR APPROVAL PER FAA FORM 8110-3 DATED 09/29/08. REF N/R 4987-1-29. 2 L 7 3 4F A3WE 20081022 NE 2008 10 22 HNAA2008101600309 3 20081006 A 6111 8022531 COLLAR HAMSTD 14SF7 DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF7 NE PROPELLER DEBONDED A HNAA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 EA 07 984HA 28813 4368 858183 377 880515 MINOR PROP VIBRATION NR 1 PROP FELT ON TAXI OUT. CLT MAINT INSPECTED FOUND A BLADE COLLAR DISBONDED. REMOVED BLADE COL LAR HALF PER HAM STAND 61-10-00 DNAA ITEM PLACED ON 10 FLIGHT HOUR DMT FOR BLADE REMOVAL AND REPLACEMENT. ROA MAINT REM OVED AND REPLACED NR 3 BLADE ON NR 1 PROP ASSY IAW WC 61-10-07. OPS CHECK GOOD CLEAR DMT. 2 H 7 2 4T RT A13NM 6 C P7NE 20081022 EA 2008 10 22 VNAA2008101600003 1 20081012 A 2560 PL22300LH00 GLOWSTRIP CNDAIR CL600 CL6002C10 1390015 EA CABIN WORN A VNAA K NONE O OTHER UK UNKNOWN 1 GL 05 703PS 10137 CREW REPORTED CABIN FLOOR LIGHTING MISSING TWO (2) SEGMENTS. MAINTENANCE INSPECTION FOUND TWO (2) SECTIONS OF EMERGENCY LIGHT FLOOR PATH PHOTOLUMINESCENT STRIP WORN OUT. ONE STRIP ON RT SIDE FORWARD OF ROW 1 AND ONE STRIP IN FRONT OF LAVA TORY. MAINTENANCE REMOVED AND REPLACED EMERGENCY FLOOR LIGHT, CHECKS GOOD. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 20081022 SO 2008 10 22 CHQA200800197 1 20081013 A 3397 WIRE EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CABIN BROKEN A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 265SK 145226 CAE312062 FLIGHT 5808, STL TO CLE. THE FLOOR EMERGENCY LIGHT STRIP BETWEEN ROWS 1 AND 2 FAILED TO ILLUMINATE DURING TEST. MAINTE NANCE FOUND THE WIRING ATTACHING THE FLOOR STRIP WAS BROKEN. THE LIGHT STRIP WAS REPLACED. AFTER THE LIGHT STRIP WAS R EPLACED, IT WAS FOUND THAT THE NR 2 INVERTER WAS ALSO INOP. THE INVERTER WAS REPLACED AND THE EMERGENCY LIGHTS FUNCTION ED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081022 SO 2008 10 22 SIMA20082901 1 20081015 A 3320 BR900022 BALLAST EMB 135 EMB135LR 3260305 SO CABIN DEFECTIVE A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 717AE 145272 CREW REPORTED ON FLIGHT 4869 DURING CLIMBOUT SMOKE SMELL IN CABIN AT ROWS 1-9. CREW DIVERTED TO BUF. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED BALLAST AT ROW 4A IAW EMB 135 AMM33-21-03. OPERATIONAL CHECK GOOD IAW EMB 135. AIR CRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081022 NM 2008 10 22 DHLA2008745523 1 20081014 A 5754 RIB BOEING 727 727224 1384076 NM LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 RT WING NR 5 L/E SLAT HAS A CRACKED RIB, AT SLAT STA 150. REMOVED AND REPLACED RIB MEMBER, BY FABRICATION, AND ASSOCIAT ED TRACK FITTING PER B727 SRM 57-50-2 FIG 2, 51-10-1, AND 51-30-2. REF N/R 4987-6-173. 2 L 7 3 4F A3WE 20081022 SO 2008 10 22 SIMA200829401 1 20081017 A 2913 AE71379016 HYDRAULIC LINE EMB 135 EMB135LR 3260305 SO HYDRAULIC SYS CHAFED A SIMA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 703MR 145173 ON FLIGHT 4920 DURING CLIMB CREW REPORTED NUMBER ONE HYDRAULIC LOW QUANTITY FOLLOWED BY ENGINE ONE HYDRAULIC PUMP FAIL. CREW DECLARED AN EMERGENCY AND PERFORMED ABNORMAL GEAR EXTENSION WITH NO ISSUES. AIRCRAFT LANDED WITH NO NOSE STEERING AND HAD TO BE TOWED TO THE GATE. THERE WAS A LOUD SQUEAL ON THE LEFT SIDE THAT CAME ON AND OFF FOR ABOUT 5 TO 10 MIN INTERVAL AS REPORTED BY A PASSENGER. AIRCRAFT REMOVED FROM SERVICE. FOUND PRESSURE LINE ON HYDRAULIC DAMPER TO ENGINE DRIVEN PUMP CHAFED FROM CUSHION CLAMP. REPLACED HYDRAULIC HOSE AND NUMBER ONE ENGINE DRIVEN PUMP. LEAK AND OPERATION C HECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081022 SW 2008 10 22 P4Y2008F00002 1 20081001 A 2421 FLLJ400 CURRENT LIMITER FRCHLD SA227 SA227DC 3377521 SW GCU BURNED E P4YA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 39 955BW DC821 CREW REPORTED THAT SMOKE FILLED THE FLIGHT DECK AFTER ENGINE START. MX FOUND A 400 MAP CURRENT LIMITER BURNED. THE CUR RENT LIMITER WAS REPLACED AND THE ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A18SW 20081022 NM 2008 10 22 SWAA085586 1 20081013 A 5743 161A15011 BEARING BOEING 737 73776Q 13845AA NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 550WN 30279 DURING SCHEDULED MV2 CHECK, FOUND LT MLG AFT TRUNNION BEARING INNER RACE SURFACE CORRODED. REMOVED AND REPLACED BEARING PER MM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085587 1 20081014 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 FOUND FWD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS ASSY PER MM. 2 L 7 2 4F RT A16WE 20081022 EA 2008 10 22 TRAX200801260 1 20081001 A 5343 PIN CNDAIR CL600 CL6002C10 1390015 EA LT MLG TRUNNION CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 CORROSION AT LT MLG FWD TRUNNION PIN. 2 L 7 2 4F RT A21EA 20081022 NM 2008 10 22 2008UALA06108 1 20081014 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 118UA 28811 EMERGENCY EXIT LIGHT INOP UPPER DECK CEILING ROW 12. LIGHT IS UNSERVICEABLE. REPLACED LAMP. ALL CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 WP 2008 10 23 AALA200802352 1 20080913 A 3350 P2010031303 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 563AA 49345 LGA EMERGENCY LIGHT AT EMERGENCY EXIT BULKHEAD INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT EMERGENCY EX IT BULKHEAD. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081023 EU 2008 10 23 QML2008F00014 1 20080913 A 2150 MOTOR SNIAS 350 AS350B3 8680954 EU CONDENSER BLOWER SHORTED E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 106LN 3251 DEPARTED ON A ROUTINE EMS MISSION, SHORTLY AFTER DEPARTURE, PILOT ABORTED FLT AND RETURNED TO HELIPAD. INFORMED MAINTENA NCE OF A STRONG ELECTRICAL ODOR IN ACFT CABIN. SOURCE OF ODOR DETERMINED TO BE ELECTRIC MOTOR IN AIR CONDITIONING SYS CO NDENSER BLOWER ASSY WHICH IS LOCATED IN THE RT CARGO BAY. THE MOTOR WHEN TURNED ON WOULD MAKE UNUSUAL SOUNDS, EMIT SPAR KS AND A ELECTRICAL ODOR. AIR CONDITIONER DISABLED, PLACARDED AND ENTERED INTO DEFERRED DISCREPANCY LOG IAW WITH MEL PR OCEDURES. ACFT RETURNED TO SERVICE. (K) 1 G 7 1 3U H9EU 20081023 2008 10 23 QML2008F00013 4 20080913 A 2210 117884141 COMPUTER BOLKMS 117 BK117A4 5626017 EU YAW FAULTED E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 03 911BY 7127 WHILE RETURNING TO BASE, CREW NOTICED AN INCREASING STRONG ELECTRICAL ODOR AS THE ACFT TURNED FINAL. CONTINUED TO THE L ANDING AREA AND PUT THE ACFT OUT OF SERVICE. CREW SAW NO SMOKE BUT ONLY THE ODOR. MAINTENANCE FOUND YAW COMPUTER TO BE FAULTY AND REPLACED IT. NO CIRCUIT BREAKERS WERE DISPLACED AND LOAD METERS READ NORMAL THROUGHOUT THE EVENT. THERE WERE NO OTHER ABNORMALITIES OR DAMAGES. (K) 1 G 7 2 3U H13EU 20081017 EU 2008 10 17 UPS08153557 1 20080926 A 5321 B5327086400200 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR MAIN CARGO FLOORBOARD 222AG IS CRACKED ON EACH SIDE. REPAIRED MAIN CARGO FLOORBOARD 222AG REF A300 -600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081023 NM 2008 10 23 RYN2008F00024 1 20081001 A 5220 STRUCTURE BOEING 727 727232 1384082 NM EMERGENCY EXIT CORRODED A RYNA O OTHER O OTHER NR NOT REPORTED 1 GL 31 727NY 20646 LT HARD AFT OVERWING ESCAPE HATCH CUTOUT LOWER SECTION HAVE CORROSION. REPAIRED LT AFT OVERWING ESCAPE HATCH CUTOUT BY F ABRICATING AND INSTALLING A DOUBLER IAW SRM 53-30-3. (K) 2 L 7 3 4F A3WE 20081023 EA 2008 10 23 COMA0860385 1 20080907 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 430CA 7461 PAX DOOR INNER SKIN DAMAGE FWD. SIDE NEXT TO OUTER HANDLE MECHANISM. REPAIRED IAW EA 10521002322. (K) 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 UPS08553581 1 20081002 A 5311 FRAME BOEING 757 75724APF 1384969 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 FRAME IS DENTED AT BS 1540 BETWEEN STR 26 AND 27 LT. REMOVED DAMAGED SECTION OF FRAME AND REPAIRED P ER SRM 53-00-07-1A1. 2 L 7 2 4F RT A2NM 20081023 WP 2008 10 23 UPS08853594 1 20081014 A 2510 11011BBCQ INERTIA REEL DOUG DC8 DC873F 302199F WP COCKPIT INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE:N/A F/E'S INERTIAL REEL INOP, (SWAPPED WITH 1ST OBSERVERS AND DEFERRED PER MEL). REMOVED AND REPLACED 1 ST OBSERVERS SEAT IAW AMM 25-11-02-2. THIS CLEARS M386600. 2 L 7 4 4F RT 4A25 20081023 EU 2008 10 23 USAA920081664 1 20080908 A 2824 ACTUATOR AIRBUS A321 A321211 3930370 EU CNTR TANK XFER MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 167US 1442 FLT 1417, CREW RECEIVED ECAM FUEL ACTUATOR TRANSFER FAULT IN CRUISE AND ADVISED DISPATCH THAT FUEL HAD BECOME TRAPPED IN THE ADDITIONAL CENTER TANK. CREW PERFORMED QRH PROCEDURES BUT THE MANUAL TRANSFER ATTEMPT WAS UNSUCCESSFUL. FLIGHT DI VERTED AND LANDED WITH INCIDENT. MAINTENANCE ISSUED A DEFERRAL ON THE ADDITIONAL CENTER TANK AUTO TRANSFER SYSTEM, AND L ATER SYSTEM OPERATIONAL CHECK WAS GOOD. FOLLOWING A SUBSEQUENT FUEL ACTUATOR TRANSFER FAULT, MAINTENANCE REPLACED THE F UEL VALVE ACTUATOR. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081023 2008 10 23 HALA0800816 4 20081019 A 3460 FMC BOEING 767 7673CB 1385187 NM FAULTED A HALA D RETURN TO BLOCK O OTHER IN INSP/MAINT 1 WP 13 592HA 33468 ETOPS SIGNIFICANT SYSTEM - BTB - FMC FAULTED F/O CDU BLANK. CHECKED BOTH NR 1 AND NR 2 FMS PER MM 34-60-00 BITE CHECK P ASSED ON BOTH FMC. 2 L 7 2 4F RT A1NM 20081023 NE 2008 10 23 2008UALA06096 2 20081014 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 221UA 30552 222042 ENG VIB MONITOR R RIGHT ENGINE AIRBORNE VIBRATION MONITORING (AVM) SYSTEM IS INOPERATIVE, OR LOSS OF TACHOMETER DATA. S TATUS MSG01- NOT ACTIVE DESCENT INTERMITTENT; 'E' FLANGE ACCELEROMETER (CIRCUIT 1 RIGHT) SIGNAL IS OUT OF RANGE. DB- S IGNAL CONDITIONER UNIT (RIGHT) MSG02- NOT ACTIVE DESCENT INTERMITTENT; 'E' FLANGE ACCELEROMETER (CIRCUIT 1 RIGHT) SIGNAL IS OUT OF RANGE. REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081023 NM 2008 10 23 2008UALA06118 1 20081014 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 182UA 25279 DOOR 1 LT AREA EMERGENCY LIGHT NOT ON. BATTERY FOUND DEFECTIVE. REPLACED BATTERY PACK, OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 NM 2008 10 23 HALA0800817 1 20081017 A 2120 CLAMP BOEING 767 76733A 1385209 NM A/C BAY LOOSE A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM - LT DUCT LEAK. FOUND LOOSE CLAMP ON HEAT EXCHANGER DUCT, RESECURED CLAMP. OPS CHECK, LEAK CHECK GOOD PER AMM 21-51-02 AND 21-51-00. 2 L 7 2 4F RT A1NM 20081023 NM 2008 10 23 UPS08M53625 1 20081012 A 5730 DOUBLER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:1C LT WING FIXED L/E HAS 10 INCH CRACK SIGN ON DOUBLER OUTBOARD OF NR 4 AND NR 5 SLT TRACK XORS 562. RE MOVED DOUBLER, FABRICATED, AND INSTALLED DOUBLER IAW DWG ARB3954 AND MD-11 SRM 51-33-01. 2 L 7 3 4F RT A22WE 20081023 NM 2008 10 23 UPS08M53633 1 20081007 A 5753 FRAME DOUG MD11 MD11F 3023600 NM TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:1C LT WING O/B FLAP O/B HINGE UPPER FWD CUTOUT FRAME FOR ACCESS PANEL 536GL IS CRACKED AT EDGE. REMOVED DAMAGE AND FABBED AND INSTALLED REPAIR DOUBLER IAW SRM VOL 1 57-00-01 PG 6, VOL 2 51-31-01 PG 1. 2 L 7 3 4F RT A22WE 20081023 NM 2008 10 23 UPS08M53641 1 20081013 A 2560 26B175519 SWITCH DOUG MD11 MD11F 3023600 NM R1 DOOR SLIDE INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 291UP 48477 INSPECTION TYPE:N/A R-1 PTT SWITCH FOR SLIDE PRESS INOP, DEFERRED M386502. REMOVED AND REPLACED DOOR SLIDE PTT SW PER M M 20-30-10. OPS CHECKED GOOD PER FIM 25-61-00-1. THIS CLEARS M386502. 2 L 7 3 4F RT A22WE 20081023 EA 2008 10 23 SWIA200820179 1 20080609 A 4910 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA APU INTAKE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 461SW 7811 APU AIR INTAKE DUCT LOWER HALF HAS A CRACKED VERTICAL STIFFENER ON INBOARD SIDE LOWER END (C-CHECK). REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 2008UALA05869 1 20080923 A 5320 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 804UA 759 CORROSION ON R2 DOOR SILL AT BOLT HOLE 6 IN FWD OF AFT GIRT BAR LATCH UNDER SCUFF PLATE. ACCOMPLISHED MAJOR REPAIR AT L CQ. MAJOR REPAIR. REPAIRED PER SRM 53-41-14 ON NR D8530Y BY 306924 AND INSPECTED BY LC5. 2 L 7 2 4F 4 F RT A28NM E40NE 20081023 EU 2008 10 23 2008UALA05879 1 20080924 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 414UA 472 SEAT EEL LIGHTS AT SEATS 1C ,3C, 11C INOP. DAMAGE (UNKNOWN) TO EEL WIRING. REPAIRED WIRING AT SEATS, TESTS OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081023 NM 2008 10 23 2008UALA06076 1 20081013 A 2560 140N276218 FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GIRT BAR DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 DOOR 4R ESCAPE SLIDE GIRT BAR STILL ENGAGE NOTICED BY CATERING DURING DOOR OPENING. DIRT AND DEBRIS ACCUMULATION UNDER GIRT BAR. CLEANED AND LUBRICATED GIRT BAR FITTINGS. DOOR ARMS/DISARMS NORMALLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 NM 2008 10 23 2008UALA06122 1 20081014 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 FWD CARGO PIT FUSELAGE FRAME AT STA 680 IS DENTED IN UPPER FLANGE BETWEEN STR 24L TO 25L. MAJOR REPAIR ACCOMPLISHED. C UT OUT DAMAGE SECTION OR RIB AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 NM 2008 10 23 2008UALA06123 1 20081014 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 FWD CARGO PIT FUSELAGE FRAME AT STA 600 DENTED IN UPPER FLANGE IN AREA BETWEEN STR 23L AND 24R. MAJOR REPAIR ACCOMPLISH ED. CUT OUT DAMAGE & INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 NM 2008 10 23 2008UALA06131 1 20081015 A 2130 8102044 SHUTOFF VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE RIGHT FAULTY A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 218UA 30222 PRESSURIZATION PROBLEM. FLIGHT DIVERTED. SUSPECT FAULTY FCSOV. REPLACED RIGHT UPPER AND LOWER FLIGHT CONTROL SHUTOFF VALVE. RAN ENGINES. NO PROBLEMS FOUND. ALL OPS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081023 NM 2008 10 23 2008UALA06132 1 20081016 A 3150 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 641UA 25091 AFTER T/O, AIR-GND DISAGREE STATUS MSG. RTFL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081023 2008 10 23 2008UALA06138 4 20081015 A 2565 S413T10211 SPRING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE R2 DOOR SLIDE FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 644UA 25094 CABIN DOOR R2 SLIDE DEPLOYMENT BAR FAILS TO RETURN FROM 90 DEGREES. REPLACED GAS SPRING. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081023 EU 2008 10 23 USAA920081669 1 20080816 A 3210 D3215303000800 PIN AIRBUS A319 A319112 3930323 EU MLG CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 MINOR CORROSION ON AFT FACE OF LANDING GEAR PINTAL PIN. REPLACED LANDING GEAR PINTAL PIN. (K) 2 L 7 2 4F RT A28NM 20081023 EU 2008 10 23 YENA2008088 1 20080911 A 2530 UNKNOWN AIRBUS 320 A320232 3930326 EU GALLEY ODOR A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 588JB 2201 DURING CRUISING, F/A DETECTED AN ODOR OF SMOKE IN AFT GALLEY. TURNED AFT RACK POWER OFF AND ODOR WENT AWAY. ACCOMPLISHE D TSM 23-39-00 AND NO DEFECT NOTED. ALL SYSTEM OPERATES WITH NO EVIDENCE OF SMOKE. 2 L 7 2 4F RT A28NM 20081023 NM 2008 10 23 KCSA081488 1 20080922 A 5315 FLOORBEAM BOEING 747 747122 1384872 NM BS 1740 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 AFT PIT FLOORBEAM UPPER T-CHORD CRACKED AT BS 1740, RBL 27. (K) 2 L 7 4 4F RT A20WE 20081023 NM 2008 10 23 USAA920081676 1 20080821 A 5320 BAC1509100146 CHANNEL BOEING 737 7373G7 138447J NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 CORROSION ON CHANNEL BETWEEN BS 727B AND BS 747, LBL 3. REPAIRED CHANNEL BETWEEN BS 727B AND BS 747, LBL 3 IAW SRM 53-0 0-53. (K) 2 L 7 2 4F RT A16WE 20081023 EU 2008 10 23 USAA920081907 1 20081019 A 2121 EVT3454H FAN AIRBUS 320 A320232 3930326 EU ZONE 100 DEFECTIVE A USAA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 656AW 45579 29419 1079 AIR TURNBACK, CREW SENT A CARS MESSAGE REPORTING BLOWER FAN FAULT AND FUMES IN THE COCKPIT. CAPTAIN DONNED O2 MASK AND DECLARED AN EMERGENCY. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINT REMOVED AND REPLACED THE AVIONICS VENT BLOWER FAN IAW MM 21-26-51. (K) 2 L 7 2 4F RT A28NM 20081023 NM 2008 10 23 USA2008F00030 1 20080913 A 3350 20121 CHARGER BOEING 737 7373G7 138447J NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 156AW 23778 MAINT REPORTED THE EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT, AFT OF R2 DOOR, FAILS TO ILLUMINATE. MAINT INSTALLED A NEW CH ARGER ASSY INCLUDING BATTERY PACK (M1137). OPS CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 HALA0800818 1 20081020 A 2612 FIRE WARNING BOEING 767 767300 1385204 NM COCKPIT MALFUNCTIONED A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM - UPON PWR TRNSFR FROM EXT TO APU THE APU FIRE DET 1 EICAS ADVISORY MSG ILLUMINATED IN BOTTOM S CREEN. CYCLED A/C POWER PERFORMED APU FIRE TEST MSG CLEARED AND TESTED NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20081023 NM 2008 10 23 KCSA081486 1 20080922 A 5311 FRAME BOEING 747 747122 1384872 NM BS 1780 S10R DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FUSELAGE FRAME DENTED AT BS 1780, STR10R. (K) 2 L 7 4 4F RT A20WE 20081023 EU 2008 10 23 USAA920081667 1 20080911 A 3150 WARNING LIGHT AIRBUS A321 A321211 3930370 EU SLIDE BOTTLE ILLUMINATED A USAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 19 190UW 23649 2693 1436 EMERGENCY EQUIPMENT - CIDS PANEL CAUTION FOR SLIDE BOTTLE EXIT RT GAUGE READS PRESSURE IN GREEN. MAINT REMOVED AND REPL ACED THE R3 SLIDE BOTTLE IAW MM 25-62-49-00-001. (K) 2 L 7 2 4F RT A28NM 20081023 EA 2008 10 23 N6WA200810204 1 20081020 A 2916 9604501 RESERVOIR CNDAIR CL600 CL6002C10 1390015 EA HYDRAULIC SYS FAULTY A N6WA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 154GJ 10224 HYDRAULIC NUMBER 3 LOW PRESSURE CAUTION IN FLIGHT. REPLACED NUMBER 3 HYDRAULIC RESERVOIR IAW M/M 29-12-30. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 TRAX200801245 1 20080929 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 EXIT SIGN BY SERVICE DOOR OUT / DAMAGED. R&R EXIT SIGN ASSY AT TOP SERVICE DOOR IAW CRJ 200 AMM 33-51-13. OPS CHECK GO OD. 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 AALA200802372 1 20080916 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 784AN 29588 DFW EMERGENCY LIGHT AT SEAT 24G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24G. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081023 NM 2008 10 23 AALA200802414 1 20080922 A 1100 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 187AN 32381 DFW EMERGENCY LIGHT EXIT MARKER DECALS AT RT HAND OVERWING DAMAGED. REPLACED EXIT DECALS FOR EXIT MARKER AT RT HAND OVE RWING. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 KNNA20080024 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 597 STR 2L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080025 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 597 STR 2R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080027 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 597 STR 3R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 UIEA200800331 1 20080925 A 3244 26078012 TIRE BOEING 747 747230B 1384889 NM MLG BLOWN A UIEA K NONE C D J F.O.D. INFLIGHT SEPARATION WARNING INDICATION TO TAKEOFF 1 EA 15 512MC 21220 INTO ANC NR 4 HYD SYSTEM QTY LOSS, COMPLIED WITH FHB, EDP SELECTED OFF AT 1612 HOURS. UPON INSPECTION ON THE GROUND FOU ND NR 11 AND 12 TIRES BLOWN, 11 AND 12 BRAKES DAMAGED, NR 9 AND 10 TIRES DAMAGED AS WELL AS NUMEROUS BODY PANELS DAMAGED . ALSO FOUND THE RIGHT INBOARD MID AND AFT FLAPS BADLY DAMAGED. REPLACED REQUIRED BRAKES AND TIRES IN ADDITIONS TO OT HER TIRES AT COMPANY REQUEST. REPLACED THE MID AND AFT FLAPS ON THE RIGHT INBOARD SIDE. REPLACE THE RT BODY GEAR CONDU IT. REPLACED REQUIRED LANDING GEAR DOORS AND PERFORMED GEAR SWING. TIRE CARCUS FOUND ON RUNWAY AT THE DEPARTED STATION (KIX). 2 L 7 4 4F RT A20WE 20081017 NM 2008 10 17 08FDEA04205 1 20081005 A 5753 ARC050312 HINGE FITTING DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 RIGHT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE ACTUATOR OUTBOARD ATTACHMENT INBOARD FACE FOUND PITTING CORROSION. C ORROSION REMOVED AND FOUND WITHIN LIMIT AS PER CMM 57-44-09. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081017 EU 2008 10 17 08FDEA04339 1 20080918 A 5753 SKIN AIRBUS 300 A300B4622R 3930312 EU RT WING TE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 725FD 572 FLAP INBD RT UPPER SKIN AT FLAP ZONE OF RIB 1 BETWEEN STR 2.1 / STR 2.2 WITH SMALL GOUGE WAS REPAIRED IAW EA 6-5710-121 707 AND SRM 57-50-00. 2 L 7 2 4F RT A35EU 20081017 NM 2008 10 17 KNNA20080037 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 639, STR 5R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080042 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 706, STR 6L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080043 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 706, STR 5L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080044 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 706, STR 4L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080045 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 706, STR 2L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080052 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 727A, STR 7R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080054 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 727B, STR 6L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080055 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 727B, STR 1. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080064 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 747, STR 5R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080065 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 747, STR 6R. 2 L 7 2 4F A16WE 20081023 EU 2008 10 23 USAA920081853 1 20080925 A 5347 D53371110001 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C7 MAJOR REPAIR NR 6062567 CORROSION ON SEAT TRACK AT FR41 TO FR47 Y765. REPLACED SEAT TRACK AT FR41 TO FR47 Y765 I AW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081023 NM 2008 10 23 AALA20802417 1 20080922 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 187AN 32381 DFW EMERGENCY LIGHT EXIT SIGN AT RT NR 3 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT EXIT SIGN AT RT NR 3 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 AALA200802420 1 20080923 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 380AN 25449 JFK EMERGENCY LIGHTS AT LT AND RT NR 1 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LT AND RT NR 1 D OOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081023 WP 2008 10 23 AALA200802366 1 20080915 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 580AA 53157 DFW EMERGENCY LIGHT AT SEAT ROW 25 HAS DAMAGED SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 25. SYSTEM GROU ND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081023 WP 2008 10 23 AALA200802421 1 20080923 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 556AA 53086 LGA EMERGENCY LIGHT AT SEAT 4D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 4D. SYSTEM GROUND CHECKED NORMA L OPS. 2 L 7 2 4F A6WE 20081023 CE 2008 10 23 DJF2008F00016 1 20081002 A 2160 22054903 COOLING TURBINE RAYTHN DH125 HAWKER800XP 7150012 CE AC BAY MALFUNCTIONED A DJFA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 23 828LX 258461 THE CREW REPORTED AFTER LANDING IN KMLB THAT THE CABIN AUTO/MANUAL TEMP CONTROL WAS INOP. THE DUCT OVHT LIGHT ILLUMINAT ED AND THE CABIN FILLED WITH ENVIRONMENTAL SMOKE. MAINTENANCE FOUND THE COOLING TURBINE FAILED. COOLING TURBINE WAS RE PLACED. 2 L 7 2 4F RT A3EU 20081023 EU 2008 10 23 USAA920081852 1 20080925 A 5347 D5713014720300 SEAT TRACK AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C7 MAJOR REPAIR NR 6062564. CORROSION ON SEAT TRACK AT FR36 TO FR41, Y1292. REPLACED SEAT TRACK AT FR36 TO FR41, Y 1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081023 NM 2008 10 23 AALA200802428 1 20080923 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 DFW EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT T00001SE 20081023 EU 2008 10 23 USAA920081815 1 20081006 A 2910 AE7094593 HOSE AIRBUS A321 A321211 3930370 EU HYD SYSTEM DAMAGED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 182UW 1536 FLT 974 EMERGENCY LANDING. ACFT LOST GREEN HYDRAULICS ON CLIMB. CREW DECLARED AN EMERGENCY AND RETURNED TO CLT. ACFT LANDED WITHOUT INCIDENT AND WAS TOWED TO GATE DUE TO LOSS OF NOSEWHEEL STEERING. MX R&R THE DAMAGED CASE DRAIN LINE AND INSPECTED CASE DRAIN FILTER. NO PARTICLES IN FILTER AND PUMP. OPS CHECK WAS GOOD. DAMAGE TO THE LINE WAS INCURRED DU RING RECENT ENGINE CHANGE. 2 L 7 2 4F RT A28NM 20081023 NM 2008 10 23 AALA200802408 1 20080921 A 1100 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 601AN 27052 DFW EMERGENCY LIGHT EXIT PLACARD AT LT HAND OVERWING DAMAGED. REPLACED EXIT PLACARD FOR EMERGENCY LIGHT AT LT HAND OVER WING. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 QXEA200801109 1 20081007 A 5210 NS5625R8 CAM BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR SEIZED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 19 408QX 4050 PDX FLIGHT 2123. AFT PAX DOOR HARD TO OPEN. FOUND FWD UPPER CAM FOLLOWER SEIZED. R&R IAW D-8-400 AMM 52-12-11-000-801 STEP 4B, 52-12-11-400-801 STEP 4M. OPS CHECK GOOD IAW D-8-400 AMM 52-12-00-710-801. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081023 NM 2008 10 23 AALA200802429 1 20080923 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 DFW EMERGENCY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT T00001SE 20081023 NM 2008 10 23 AALA200802431 1 20080923 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 DFW EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT T00001SE 20081023 WP 2008 10 23 ABXA080246 1 20080918 A 2170 1808491 COALESCER BAG DOUG DC9 DC941 302207N WP CABIN AIR ODOR A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 23 959AX 47761 AT TAKE OFF POWER AN ABNORMAL ODOR CAME FROM THE LT AC PACK. AT CRUISE POWER, THE SMELL WENT AWAY. REPLACED THE LT COA LESCER BAG IAW DC9 AMM CHAPTER 21. 2 L 7 2 4F A6WE 20081023 SO 2008 10 23 MAS2008F00086 1 20081001 A 3350 744424 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 852MJ 145567 FDM 9901 CVG. DURING MX WALK AROUND MX FOUND LT EMERG EXIT DOOR LIGHTS INOP. MX R&R EMERGENCY LIGHT. 2 L 7 2 4T RT T00011AT 20081023 EU 2008 10 23 MAL2008F00037 1 20080926 A 5350 SKIN SAAB SF340 340B 7860101 EU TAIL CONE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 340B424 DURING THE 2Y AND N4K NOTED 4 DENTS IN TAIL CONE BETWEEN STA797 AND 803. 1 ABOVE AND 3 BELOW SL1604. REPAIRED IAW EO#S 53620. 2 L 7 2 4T RT A52EU 20081023 EA 2008 10 23 ASOA200801336 1 20081014 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 750EV 10161 FUSELAGE STA 280 FWD FLOOR SUPPORT HAS CORROSION. REINSTALLED DRIP TRAY PER FROM M-234 NR - 0125 PAGE 3. REMOVED 280 FWD FLOOR SUPPORT ANGLE PER SRM 51-42-06. LOCATED FASTENER HOLES ON 280 FWD FLOOR ANGLE PN CC670-33292-13 PER CRJ 700 S RM 51-40-11. INSTALLED NEW ANGLE ON 280 FWD IAW SRM 51-42-06 / PN CC670-33292-13. INSTALLED DRIP TRAY ON RT SIDE OF FS 2 80 IAW SRM 51-42-21-/51-42-13. APPLIED SEALANT & CIC TO FWD ANGLE OF 280. JOB COMPLETE. 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 KPVA 2008-03 1 20081016 A 5311 85320058105 FRAME DHAV DHC8 DHC8103 1386005 NM ZONE 200 CRACKED A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 808W 026 CRACKED FRAME P/N 85320058-105 AT STATION X354.25 AT STRINGER 22. REPAIRED FRAME IAW DRAWING RD 8-53-1039 ISSUE 4. 2 H 7 2 4T RT A13NM 20081023 NM 2008 10 23 KPVA 2008-04 1 20081016 A 5311 85330086 FRAME DHAV DHC8 DHC8103 1386005 NM ZONE 200 CRACKED A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 808W 026 CRACKED FRAME P/N 85330086 AT STATION X510.00 AT STRINGER 22. REPAIRED IAW DRAWING RD 8-53-10335. 2 H 7 2 4T RT A13NM 20081023 2008 10 23 ASAA0853590 4 20081013 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM EE BAY MALFUNCTIONED A ASAA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 02 570AS 6565 35185 FMC DISAGREE LIGHT PROCEDURE FOLLOWED, 11.2 QRH INFO NOTED. ACCOMPLISHED FIM TASK 34 61 00 810 801 FOR GROUND VERIFICAT ION OF ETOPS AC TESTS OK. 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 ASAA0843593 1 20080914 A 5320 6552878102 THRESHOLD BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 AFT CABIN L2 DOOR THRESHOLD INNER CHORD CORRODED STA 946 TO 992. REMOVED DAMAGED INNER CHORD, DRILLED, INSTALLED A REPL ACEMENT INNER CHORD IAW B737 400 SRM 51 40 02 PG 2 4. 2 L 7 2 4F RT A16WE 20081023 EA 2008 10 23 MASA2008102000739 1 20081020 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT MALFUNCTIONED A MASA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 07 920FJ 15020 ASH FLT 2616 CLT-ILM. LT AFT EMERGENCY DOOR CAUTION MESSAGE. MX CYCLED DOOR, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081024 NM 2008 10 24 SWAA085677 1 20081021 A 5312 6549892 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND BULKHEAD CRACKED AT BS 1016, STR 8R. REPAIRED BULKHEAD PER AAR EA. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085669 1 20081021 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 23R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081024 NM 2008 10 24 SWAA085670 1 20081021 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 20R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081027 NE 2008 10 27 M7KA0701084173 2 20080901 A 7250 TURBINE BLADES UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE DAMAGED A M7KA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 19 824MH 4173 23350 POWER CHECK WITH A HIGH TORQUE MARGIN AND OUT OF LIMIT T4 TEMP MARGIN WAS INDICATIVE OF TURBINE BLADE TIP DAMAGE VERIFYI NG DEFECT. ENGINE WAS REPLACED WITH A SERVICEABLE ASSY. THIS TURBINE RUB DEFECT HAS RECENTLY BECOME MORE PREVALENT ON TH ESE ENGINES. ANY CONTACT BETWEEN THE SEGMENT FACES AND THE HP TURBINE BLADE TIPS TRANSFERS METAL TO THE SEGMENTS WHICH B UILDS UP INTO RAISED DEPOSITS WHICH EFFECTIVELY MACHINE GROOVES IN THE BLADE TIPS LEADING TO THE LOSS OF THE TEMP T4 MAR GIN WITH THE GAS BYPASS INCREASING THE POWER TURBINE TORQUE. IT IS NOT CLEAR IF THE SEGMENTS WARP INTO BLADE CONTACT OR THE BLADES STRETCH TO INITIATE THIS DEFECT. IT IS NOT CLEAR IF THE SEGMENTS WARP INTO BLADE CONTACT OR THE BLADES STRET 1 G 7 2 3U 3 U H9EU E00054EN 20081027 NM 2008 10 27 DL76P081348 1 20081012 A 2421 OIL SYSTEM BOEING 767 767332 1382001 NM IDG LOW A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 1402A 25989 ON TAXI OUT, LT GENERATOR OFF FOLLOWED QRD AND GEN RESET. 2 L 7 2 4F RT A1NM 20081027 NM 2008 10 27 DLM88081349 1 20081012 A 2421 CSD DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENG MAKING METAL A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 977DL 53258 725736 ON CLIMB-OUT MULTIPLE GEN RELAY TRANSFERS FOLLOWED BY LEFT CSD OIL PRESSURE LOW MESSAGE QRH FOLLOWED LEFT CSD WOULD NOT DISCONNECT. RTN TO ATL. FOUND CSD FULL OF METAL, REMOVED AND REPLACED TRANSMISSION AND GENERATOR WET SPLINE SERVICED N EEDS LINE TO OIL COOL HOOK U AFTER COOLER REPLACEMENT SEE ITEM 003, ALSO NEED SERVICED. CONNECTED OIL COOLER LINES SERV ICED CSD. INSTALLED PER M/M 24-10-01, GENERATOR INSTALLED PER MM 24-20-01 PG 401. OPS AND CKS OK. 2 L 7 2 4F 4 F RT A6WE E9NE 20081027 NM 2008 10 27 DL76G081351 1 20081012 A 2822 PUMP BOEING 767 7673P6 1385105 NM FUEL BOOST INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 154DL 25241 RTB DUE TO LT CTR FUEL BOOST PUMP INOP. FOUND C/B F15 ON P6 PANEL OUT. NO HIST AND CREW REPORTS IT COULD HAVE BEEN BUM PED W/CREW FLT BAG. OPS CKG GOOD OF PUMP AFTER C/B CLOSED. 2 L 7 2 4F RT A1NM 20081027 NM 2008 10 27 DL764081352 1 20081010 A 5330 143T351117 SKIN BOEING 767 767432ER 1385134 NM BS 654A S19-25R DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 830MH 29701 FUSELAGE/SKIN/LIGHTNING STRIKE STA 654A+22 TO STA 654 BETWEEN STRINGER S-19R AND S-25R, REPAIR. 2 L 7 2 4F RT A1NM 20081027 NM 2008 10 27 DL75E081353 1 20081010 A 2421 241001791 IDG BOEING 757 757231 1384950 NM LEFT FAILED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 721TW 29954 AFTER PUSHBACK ON L ENGINE START AT 50 PERCENT N2 L GEN FAILED W ASSOC L BUSS TIE ISOLATION LIGHT. REPLACED K108 RELAY, NO HELP. FOUND B PHASE FROM IDG BAD. REPLACED IDG LEAK CK OK, OP CK OK. 2 L 7 2 4F RT A2NM 20081027 NM 2008 10 27 DL764081355 1 20081011 A 2410 CONTROL UNIT BOEING 767 767432ER 1385134 NM AC GENERATOR MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 844MH 29717 AFTER STARTING RIGHT ENGINE AIRCRAFT WOULD NOT ACCEPT POWER FROM RIGHT AC GEN. ATTEMPTED RESET OF R GEN CONT AND RIGHT BUSS TIE. NO BPCU FAULTS, REMOVED AND REFITTED BPCU, NOW RT BUSS OK. ENGINE RUN CARRIED OUT ALL OK. 2 L 7 2 4F RT A1NM 20081027 NM 2008 10 27 QXEA200800948 1 20080820 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 410QX 4053 PDX - C CHECK, CORROSION ON FUSELAGE SKIN WHERE VHF NR 3 ANTENNA IS MOUNTED STA X331 TO LOWER FUSELAGE. REMOVED CORROSI ON IAW Q400 SRM 51-21-00. HFEC INSP IAW 8-400 NDTM PT6, 51-00-01. NO CRACKS NOTED. UT THICKNESS CHECK IAW 8 Q400 NDTM PT 1, 51-00-04 LOW .057 HI .060. MAPPED FOR ENGINEERING. ALODINED PER RD 8/4-53-2460. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 USAA920081725 1 20080901 A 5311 6546552 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 SAL - C17 -MAJOR REPAIR, FRAME AT BS 827 HAS A .435 INCH CRACK BETWEEN S8L & S9L AND A .426 INCH CRACK BETWEEN S8R & S9R . REPAIRED FRAME AT BS 827 BETWEEN S8L & S9L, ALSO BETWEEN S8R & S9R IAW AMERICA WEST AIRLINES TASK CARD NR M1C53002. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 QXEA2008102201067 1 20081002 A 5320 PANEL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX-C4-CORROSION AROUND SOME OF THE FASTENERS FOR CARGO BAY PANEL 144FZ. REMOVED MINOR SURFACE CORROSION PER Q400 SRM 5 1-14-00. ALODINED AND PRIMED AREA IAW Q400 SRM 51-25-10 AND 51-21-10. 2 H 7 2 4T RT A13NM 20081028 NM 2008 10 28 QXEA2008102201072 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX-C4- CORROSION ON THE TOP OF THE NR 11 SEAT TRACK AT STA X66.000. BLENDED OUT CORROSION, FOUND OUT OF LIMITS PER RD8 /4-53-884. REMOVED SPLICE, DRIP TRAY, DEFLECTORS AND TRACK. MATCH DRILLED SPLICE TO NEW SEAT TRACK IAW DHC8-400 SRM 51 -40-07. INSTALLED SPLICE IAW DHC8-400 SRM 51-42-05 AND 51-40-15. MATCH DRILLED TRACK TO AIRCRAFT REF Q400 SRM 51-40-07 , 51-40-15 AND 51-21-10. INSTALLED SEAT TRACK IAW Q400 SRM 51-40-05, AND 51-42-05. 2 H 7 2 4T RT A13NM 20081028 SO 2008 10 28 SIMA200829604 1 20081020 A 5320 14521725013 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 651AE 145422 DURING MBV INSPECTION FOUND FORWARD SERVICE DOOR SILL TO BE CORRODED. REPAIRED SILL BY REMOVING CORROSION AND INSTALLIN G A DOUBLER IAW EMB SRM 53-21-10 FIGURE 204. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081028 EU 2008 10 28 USAA920081866 1 20081012 A 2560 P4010021 BATTERY AIRBUS A321 A321211 3930370 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 189UW 1425 FLT 939 PHL-CLT EMERGENCY EQUIPMENT. AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MX R&R THE AFT FLIGHT ATTENDANT FLAS HLIGHT BATTERY. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081028 NM 2008 10 28 AALA200802484 1 20080919 A 5743 115A52119 TRUNNION BOEING 737 737823 13844CB NM LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 LT MLG TRUNNION FITTING CORRODED AT LOWER INBD HOLE OUTER FACE. AREA OF DISCREPANCY IS 2 INCHES BY 2 INCHES WITH A .084 INCH DEPTH. REMOVED CORROSION, TREATED, PRIMED, AND INSTALLED NEW BUSHING PER SRM 57-20-90-R2-2. 2 L 7 2 4F RT A16WE 20081028 WP 2008 10 28 AALA200802513 1 20080924 A 5320 S2932222 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 176 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 TUL FLOORBOARD SUPPORT IS WORN AND CRACKED AT STATION 176. AREA OF DISCREPANCY IS 2 INCHES BY 26 INCHES WITH A DEPTH OF 20 PERCENT PLUS. CRACK LENGTH OF 1 INCH. REPLACED FLOORBOARD SUPPORT PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081028 NM 2008 10 28 AALA200802419 1 20080922 A 2400 CONTACT BOEING 757 757223 1384957 NM RELAY OPEN A AALA A UNSCHED LANDING G H MULTIPLE FAILURE ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 21 197AN 32391 ORD INFLIGHT T268/22SEP SEA TO JFK. CREW REPORTED AIR GROUND SYSTEM EICAS MSG WITH SEVERAL COMPONENT FAILURES OF INERTI AL REFERENCE SYSTEM AND MAIN BATTERY CHARGER FOLLOWED BY FAILURE OF ALL CAPTAINS INSTRUMENTS. LANDED ORD. ON LANDING A CFT WENT OFF END OF RUNWAY. NO INJURIES REPORTED. ACFT HAD BLOWN TIRES. FOUND B1 AND B2 CONTACTS OPEN ON K106 RELAY. REPLACED B1 AND B2 CONTACTS FOR RELAY K106. EICAS COMPUTERS REPLACED. REPLACED MAIN AND APU BATTERIES AND CAPTAINS WI PER MOTOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081028 NM 2008 10 28 ASAA0843604 1 20080907 A 5754 65C26603102SP SKIN BOEING 737 7374Q8 138447Q NM LE SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 RT WING L NR 4 LEADING EDGE SLAT I/B TRAILING EDGE WEDGE HEAVY CHAFE AT I/B END. REMOVED DAMAGED AREA, FABRICATED SKIN AND DOUBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0843605 1 20080913 A 5754 65C26602301 SKIN BOEING 737 7374Q8 138447Q NM LE SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 LT WING NR 2 LEADING EDGE SLAT LOWER SURFACE CHAFED AT O/B TRAILING EDGE WEDGE. REMOVED DAMAGED SKIN, FABRICATED FILLER SKIN AND DOUBLER BONDED IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 2008UALA06158 1 20081017 A 3397 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHT INOPERATIVE ROW 49 LT. SECURED LOOSE CONNECTOR. OPS CHECKED OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081028 NM 2008 10 28 ASAA0843615 1 20080912 A 5755 654645270A SKIN BOEING 737 7374Q8 138447Q NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 LT WING I/B GROUND SPOILER HAS SEVERAL DENTS ON UPPER SURFACE. REMOVED DAMAGED IN 4 EACH AREAS, PREPARED AREAS, FABRICA TED FILLERS AND DOUBLERS, BONDED IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 2008UALA06152 1 20081016 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 510UA 24780 FOUND DENT AND GOUGE JUST AFT OF DOOR 2 LEFT, ON LOWER RIGHT CORNER, AT STATION 760, 8.5 INCHES UP OF WATER LINE. LENGT H OF GOUGE IS 2 INCHES LONG AND DENT WIDTH IS 1 INCH WITH A DEPTH OF .062 DEEP. CLEANED AREA, AND SMOOTHED AREA. AREA IS FREE FROM CRACKS AND CREASES REF SRM 53-00-01. ALSO APPLIED ALODINE. MF3398 CREATED TO MONITOR. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081028 NM 2008 10 28 ASAA0853622 1 20081018 A 2161 6228145 CONTROLLER BOEING 737 737890 1384527 NM E&E BAY FAULTY A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 583AS 5051 35681 DURING LANDING CHECK, "RIGHT PACK" LIGHT ILLUMINATED ON RECALL ACCOMPLISHED FIM TASK 21 53 810 & ZONE TEMP CONTROLLER BI TE PER 21 61 00. RT CONTROLLER SHOWED PACK TEMP SENSOR FAULT. RESET & RAN PACK FOR 1 2 HOUR ON GROUND WITH NO FURTHER FAULTS. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873635 1 20081002 A 5320 147AS660Y21 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 AFT PASSENGER CABIN INTERCOSTAL AT BS 947 BS 967 LBL 51 CORROSION FOUND. AFT PASSENGER CABIN INTERCOSTAL AT BS 947 BS 9 67 LBL 51 REPLACED IAW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085516 1 20081012 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 540, STR 21L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085522 1 20081012 A 5311 6546530 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 460, BETWEEN STR 26L TO STR 27L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 08FDEA04184 1 20081003 A 5347 SEAT TRACK BOEING 757 75723A 1384967 NM BS 1620-1640 MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 MAIN CABIN SEAT TRACK FLANGE 1620-1640, LBL 45 HAS 2 SCREW HOLES ELONGATED. REMOVED DAMAGED SEAT TRACK PER SRM 51-40-02, FABRICATED NEW SEAT TRACK PER MAE TRAVELER T8/752959. LOCATED AND DRILLED PER SRM 51-40-05, TREATED AND PRIMED PER SRM 51-20-01, PAINTED PER SRM 51-21-00-7, AND INSTALLED PER SRM 51-40-02 AND 51-20-05. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 SWAA085548 1 20081011 A 5330 6518420 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR UPPER HINGE SKIN CUTOUT CRACKED AT BS 305, WL 257. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 DL757081231 1 20080925 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 DURING CURRENT HMV, CORROSION WAS FOUND ON THE 1681 FLOORBEAM, ON THE UPPER CHORD (UPPER AND LOWER SURFACE). DUE TO THI S, THE UPPER CAP WAS CUT OUT AND REMOVED PER BOEING INSTRUCTIONS, AND A REPLACEMENT UPPER CAP INSTALLED AS DOCUMENTED IN ER/A 470312-14 (CATEGORY A REPAIR). 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04216 1 20081006 A 5320 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 576FE 48501 DURING OPEN HOLE INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WITH CRACK IN DICATIONS AT HOLES C, AND D. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 08FDEA04217 1 20081006 A 5320 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 576FE 48501 DURING OPEN HOLE INSPECTION ON 0.460" DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WITH CRACK IN DICATIONS AT HOLES C, AND D. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 08FDEA04222 1 20081006 A 5730 ARC27361 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 576FE 48501 LT WING I/B FLAP LOWER SURFACE SCRATCH AND DENT FOUND AT WS 151.3. REPAIR CARRIED OUT AT LT WING INBOARD FLAP LOWER SEG MENT AT STA XW = 151.3 AS PER SRM 57-10-00. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081016 NM 2008 10 16 08FDEA04223 1 20081006 A 5220 650797869 RETAINER BOEING 727 727227 1384078 NM EMERGENCY EXIT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 RT FWD EMERGENCY EXIT HATCH, SEAL RETAINER LOWER AFT HAS CORROSION. FABRICATED SEAL RETAINER REF DWG 50-07978. DRILLED A ND TRIMMED SEAL RETAINER REF SRM 51-30-5, TREATED AND PRIMED REF SRM 51-10-2, PAINTED REF MM 51-20-000-7 LABELED RETAINE R 65-07978-69 REF GMM 7-0-1001 THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 SWAA085455 1 20081006 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 305SW 22945 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 905, STR 6L TO STR 7L. REMOVED AND REPLACED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 DL757081288 1 20081003 A 5414 311N31532 SKIN BOEING 757 757232 1384965 NM NR 2 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 642DL 23996 DURING A SKIN REPAIR PER THE SRM, SEVERAL FASTENER HOLES WERE MISDRILLED IN VARIOUS LOCATIONS AS NOTED IN ER/A 06-362852 -14. THE ER/A PROVIDED REPAIR INSTRUCTIONS. NOTE: AT THE TIME OF ER/A ISSUE, AN MRR WAS NOT SUBMITTED. THIS SUBMITTA L CORRECTS THIS SITUATION. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04246 1 20081006 A 5210 65583942 FITTING BOEING 727 727227 1384078 NM ZONE 800 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 LEFT AFT ENTRY DOOR, FWD LOWER STOP PIN LUG HAS WORN FLAT SPOT REMOVED AND REPLACED L2 DOOR REF AMM 52-14-000-4. REMOVED AND REPLACED FWD LWR STOP FITTING REF SRM 51-30-02. REMOVED AND REPLACED PRESSURE SEAL REF AMM 52-12-011-4 THIS IS CLAS SIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081016 NM 2008 10 16 DL757081290 1 20080928 A 5320 146N54562 INTERCOSTAL BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 DURING AAI INSPECTION AT ATS/PAE INSPECTION FOUND INTERCOSTAL WEB CORRODED BS 1470-1481 RBL 13 IN THE CARGO BILGE AREA. FOUND TO BE OUT OF LIMITS. REPLACED SAME. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081291 1 20080924 A 5320 140N250538 INTERCOSTAL BOEING 757 757232 1384965 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 DURING AAI INSPECTION AT ATS/PAE INSPECTION FOUND THE INTERCOSTAL UPPER FLANGE CRACKED AT BS 662 RBL 45 WL 208. REMOVED UPPER ANGLE BS 662 RBL 45 WL 208 IAW SRM 51-40-04-0G. FABRICATED NEW ANGLE FROM 7075-T6 0.032 LOT 827686 IAW SRM 53-30 -51, 51-40-02, 51-40-05, 51-30-01-0G, 51-20-01-0G. INSTALLED NEW ANGLE IAW SRM 51-40-04-0G. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081298 1 20081005 A 5321 146N5391 FLOOR PANEL BOEING 757 757232 1384965 NM CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION FOUND DURING AAI INSPECTION ON FLOOR PANEL STATION 1492-1538 RBL 17. FLOOR PANEL REPAIRED ON NR 00029 PER 51- 70-1, 51-40-02 AND 51-30-01. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL757081299 1 20081005 A 5347 146N54568 CARGO TRACK BOEING 757 757232 1384965 NM CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION ON ACB CARGO TIE DOWN RAIL BS 1470-1481. RAIL REPLACED ON ATS NR 00056 PER 51-40-02 / 05. 2 L 7 2 4F RT A2NM 20081016 EU 2008 10 16 08FDEA04285 1 20081009 A 2421 764067A GCU AIRBUS 300 A300F4605R 3930327 EU NR 2 FAILED A FDEA C ABORTED TAKEOFF H S ELECT. POWER LOSS-50 PC AFFECT SYSTEMS TO TAKEOFF 1 CE 21 656FE 16999 16999 745 REJECTED TAKEOFF AT 30 KTS DUE TO LOSS OF ALL ELECT POWER EXCEPT EMERGENCY POWER. MULTIPLE PROBLEMS RELATED TO RAIN DR IPPING INTO AVIONICS BAY. SEE ALSO WRI 25-70-1318 - AFTER REJECTED TO. TAXIED BACK TO BLOCKS & INSPECTED AVIONICS BAY. FOUND SIGNIFICANT AMOUNT WATER IN AVIONICS BAY. NR 2 IDG PREVISOULY ON MEL PRIOR TO THIS EVENT. (A/C LOADED IN HEAVY RAIN. ACFT DRAINED OUT. R&R NR 2 GCU AND ALL ASSOCIATED SYSTEMS OPERATE NORMAL ON ACFT. MM 24-41-11-4 AND 24-41-00-0. 2 L 7 2 4F RT A35EU 20081017 2008 10 17 2008UALA06051 4 20081008 A 2565 PANEL BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EVAC SLIDE DELAMINATED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 665UA 29237 RIGHT OVERWING SLIDE PANEL HAS A FOOTBALL SIZE DELAMINATION. DELAMINATED PANEL REMOVED & ROUTED TO SHOP. DOOR ASSY 416T 2009-7 ON ORDER FROM BOEING. REPLACED RT OVERWING SLIDE DOOR. RIGGED AND ADJUSTED. REPLACED KEEPERS. EG EVALUATED THE FL USHNESS CONDITION AND FOUND THAT THE FLUSHNESS OF 0.156 IN LIEU OF THE 0.20 PER MM, IS ACCEPTABLE ALONG THE TRAILING EDG E OF THE PANEL AS IT WILL NOT AFFECT AERODYNAMIC FLOW. 2 L 7 2 4F 4 F RT A1NM E24NE 20081017 NM 2008 10 17 08FDEA04321 1 20081013 A 5347 65196012 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 468FE 21452 CORROSION SEAT TRACK STA. 950 LBL 45. REMOVED SEAT TRACK IAW SRM 51-30-2. FABRICATED SEAT TRACK AND 2 SPLICE ANGLES IAW SRM 53-10-5 FIG 1 AND 51-30-8. TREATED & PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED TRACK & REPAIR PARTS IAW SRM 53 -10-5 & 51-30-5, AND 51-30-8. FABRICATED, DRILLED, DEBURRED SEAT TRACK & SPLICE ANGLES. 2 L 7 3 4F A3WE 20081017 NM 2008 10 17 DL757081308 1 20081006 A 5315 146N5447U15 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 AFT CARGO FLOORBEAM STATION 1470 CORRODED AT LBL 17. REPAIRED ON NR 00050 PER 51-70-11 FIGURE 1 SHT 1. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 08FDEA04329 1 20081013 A 5311 140N2004 FRAME BOEING 757 75723A 1384967 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 AFTER REMOVAL OF DOUBLER FROM TV MONITOR SUPPORT, AT BS 1460, S4L TO S4R, FOUND SEVERAL HOLES ON FRAME. REMOVED AND REPL ACED FUSELAGE FRAME, BS 1460, S4L TO S4R, IAW SRM 53-00-07. REPAIR PARTS FABRICATED ON MAE TRAVELERS T8/761978, T8/76329 8. THIS REPAIR IS CLASSIFIED AS A CATEGORY "B" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 DL757081317 1 20081006 A 5315 146N54441 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION ON FLOORBEAM STATION 1510 AT LBL 7. REPAIRED ON NR 00060 PER 53-60-53 FIG 206. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 DL757081326 1 20081006 A 5315 146N547715 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION ON FLOORBEAM AT STATION 1470 LBL 3. REPAIRED ON NR 00052 PER 51-40-05 FIGURE 4. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 2008UALA05878 1 20080924 A 7830 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE THRUST REVERSER DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 540UA 25252 726600 NR 2 ENGINE LT INBOARD REVERSER UPPER BIFURCATION PANEL IS DELAMINATED INNER SKIN ABOUT 60 PERCENT OF PANEL LENGTH FROM EDGE TO EDGE. REPLACED REVERSER HALF. 2 L 7 2 4F 4 F RT A2NM E17NE 20081017 NM 2008 10 17 2008UALA06036 1 20081008 A 3620 WARNING SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE BLEED AIR SYS ACTIVATED A UALA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 WP 29 811UA 847 ENGINE 1 BLEED FAULT. RTFL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081017 NM 2008 10 17 2008UALA06038 1 20081008 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 665UA 29237 THE 29HJ EEL LIGHT INOP. REPLACED LAMP. TEST OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081017 NM 2008 10 17 2008UALA06048 1 20081009 A 4920 5198588 STARTER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE APU MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 669UA 30025 APU WILL NOT START. APU CRANKS BUT NO RPM INDICATION. CREW COMMENTS: TWO START ATTEMPTS FAULT EICAS ONLY 10 PERCENT R PM ON SECOND. REPLACED APU STARTER. ACCOMPLISHED 2 APU STARTS. OPS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081017 EU 2008 10 17 08FDEA04300 1 20080909 A 5330 A53812632201 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 725FD 572 SKIN DAMAGE LOCATED AT FR47/48 S41LT. REPAIRED AS PER EA 6-5330-121701. 2 L 7 2 4F RT A35EU 20081017 NM 2008 10 17 DL76G081336 1 20081007 A 2730 INDICATOR BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6F 30025 NE COCKPIT MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 154DL 25241 706619 ON TAXI OUT ELEVATOR CONTROL POSITION INDICATOR SHOWS RIGHT ELEVATOR ONLY QUARTER MOVEMENT. LEFT INDICATOR NORMAL. IND ICATION BACK NORMAL AFTER ENG SHUT DOWN AND APU PWR. RESTART ENG ALL IND NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 20081017 NM 2008 10 17 08FDEA04305 1 20081010 A 5322 651750469 SHEAR TIE BOEING 727 727227 1384078 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 LEFT AFT AIR STAIR AREA, BS 1262 SHEAR TIE CRACKED BETWEEN S11-12L REMOVED CRACKED SHEAR TIE, FABRICATED, TREATED AND PRIMED AND INSTALLED SHEAR TIE REPAIR. REF SRM 51-10-2, SRM 51-30-2 PG 1-4, SRM 53-10-04, NDT HOLES AND COUNTERSINKS, NO DEFECTS NOTED, REF NDT MANUAL PART 6. 51-00-00 AND 53-30-00. THIS IS CLASSIFIED AS A MAJOR REPAIR 2 L 7 3 4F A3WE 20081017 NM 2008 10 17 KNNA20080067 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 747, STR 9R. 2 L 7 2 4F A16WE 20081028 NM 2008 10 28 ASAA0873652 1 20081003 A 5320 141A5410U1 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 INTERCOSTAL AT BS 312 BS 328 LBL 47 IS CRACKED. CRACKED INTERCOSTAL AT BS 312 BS 328 LBL 47 REMOVED AND A NEW SERVICEAB LE INTERCOSTAL WAS INSTALLED IAW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873654 1 20081003 A 5320 141A541012 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 FWD PASSENGER CABIN INTERCOSTAL CRACKED AT BS 312 TO BS 328 RBL 31. FWD PASSENGER CABIN CRACKED INTERCOSTAL REMOVED AND NEW SERVICEABLE INTERCOSTAL INSTALLED IAW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873637 1 20081001 A 5321 146A9401 STRAP BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 AFT CARGO PIT FLOOR PANEL T-SPLICE STRAP AT BS 767+6 RBL 20 TO LBL 20 HAS CORROSION. T-SPLICE STRAP CORROSION BLENDED O UT. BLEND AREA FOUND TO BE BEYOND LIMIT. NEW REPAIR STRAP MADE IAW B737 700 SRM 53 00 53 AND 53 60 53. 2 L 7 2 4F RT A16WE 20081028 EA 2008 10 28 MASA2008102100743 1 20081021 A 2621 4739163 FIRE BOTTLE CNDAIR CL600 CL6002C10 1390015 EA NR 1 ENGINE LOW A MASA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 07 519MJ 13262 10260 ASH FLT 7154 ORD-SAV. ENGINE NR 1 FIRE BOTTLE LOW MESSAGE. MX REPLACED THE FIRE BOTTLE AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081028 NM 2008 10 28 HALA2008102300824 1 20081023 A 2150 A/C PACK BOEING 717 717200 1383700 NM AC BAY MALFUNCTIONED A HALA K NONE B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET NR NOT REPORTED 1 WP 13 486HA 55131 OPEN - PACK L OVERHEAT ALONG WITH A BURNING SMELL, GRINDING, RATTLING NOISES AND VIBRATION. OK TO CONTINUE PER C 21-51- 01. 2 L 7 2 4F TR A6WE 20081028 EA 2008 10 28 MASA2008102200744 1 20081022 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 592ML 7410 ASH FLT 7134 ORD-CAK. PASSENGER DOOR OUTER HANDLE IS HARD TO STOW. MX LUBED DOOR. 2 L 7 2 4F RT A21EA 20081028 EA 2008 10 28 MASA2008102200745 1 20081022 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH FLT 2759 PHX-BUR. AFT EMERGENCY FLOOR LIGHT STRIP INOPERATIVE. MX REPLACED THE LIGHT STRIP AND REPAIRED THE WIRING . 2 L 7 2 4F RT A21EA 20081028 EA 2008 10 28 MASA2008102200746 1 20081022 A 4900 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA APU SMOKE A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 650ML 7137 ASH FLT 7275 IAD-CAE. SMOKE COMING FROM APU INLET DURING SHUTDOWN. MX INSPECTED AIRCRAFT AND FOUND NO EVIDENCE OF UNCO NTAINED FIRE AND PLACED APU ON MEL. 2 L 7 2 4F RT A21EA 20081028 EU 2008 10 28 MALA080185 1 20081002 A 5350 FAIRING SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 340B428 TWO DENTS NOTED IN THE WING TO FUSELAGE FAIRINGS. REPAIRED IAW EO S51031. 2 L 7 2 4T RT A52EU 20081028 EA 2008 10 28 ASOA20081254 1 20080930 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 BLENDED 280 RT WEB IAW 51-12-00. PERFORMED UT THICKNESS MEASUREMENT OF FS 280.00 RIGHT BULKHEAD WEB, AFTER BLENDING, IA W REO 670-53-11-052 PER CRJ 700 NDTM 51-20-004. MINIMUM THICKNESS IS .038 INCH. 10/2/08 RESTORED A023 FINISH ON RT FS 280 WEB IAW REO 670-53-11-052. SUPPLEMENTAL SDR CLOSED 10/15/08. 2 L 7 2 4F RT A21EA 20081028 EA 2008 10 28 ASOA200801255 1 20080930 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED FWD FLOOR SUPPORT ANGLE TO BE REPLACED IAW CRJ 700 SRM 51-42-06. BEGAN TO DRILL UP NEW FWD ANGLE. ALL HOLES DR ILLED EXCEPT THE HOLES THAT GO THROUGH THE BRACKET IAW CRJ 700 SRM 51-42-06. PICK UP FASTENER HOLES AND COWL LOCK RECEP TACLE HOLES IN FWD FLOOR SUPPORT ANGLE IAW CRJ 700 SRM 51-42-06. INSTALLED FWD ANGLE ALL WORK DONE IAW CRJ 700 SRM 51-4 2-06. SUPPLEMENTAL SDR CLOSED 10/15/08. 2 L 7 2 4F RT A21EA 20081028 EA 2008 10 28 ASOA200801265 1 20080930 A 2571 BATTERY BOX CNDAIR CL600 CL6002B19 1900309 EA RT WING DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED CONNECTOR AT WS 53.60. REPAIRED RT BATT WEBB AT WS 53.60. REPAIR NR 2. RECONNECTED CONNECTORS AT WS 53-60. C ONNECTOR REQUIRES OPS CHECK. REMOVED RT TIRE BURST PNL. TIRE BURST PNL NEEDS INSTALLED. PERFORMED OPS CHECK OF CONNEC TOR. OPS CHECKS GOOD AT THIS TIME. REFER TO 87752811 OP 81 FOR INSTALLATION OF TIRE BURST PANEL. COMPLIED WITH ASA EC /TC REO 601R-57-51-046. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081028 EA 2008 10 28 ASOA1249 1 20080930 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED LT DRIP TRAY, INTERCOSTAL LBL 18 AND LBL 36 AND INSTR AIR LINE AT LBL 38. REMOVED CABLE PULLEY AND CABLE GUIDE. REMOVED LT FS 280 BEAM TO BE REPLACED. TRIMMED NEW 280 LT BEAM TO FIT. PICK UP ALL FASTENER HOLES, DRILL UP NEW DOU BLERS -7 & -9 WITH ALL SHIMS AND RADIUS PACKERS. TRIMMED BACK LBL 9 FOR CLEARANCE AND TOUCH UP CUTLINE WITH 044. PICK UP FASTENER HOLES ON U BRACKET FOR INTERCOSTAL LBL 18. DRILLED CENTER SPLICE. CUT LINE, NO CRACKS NOTED. OK TO INSTAL L NEW LT 280 BEAM AND ALL REPAIR PARTS. INSTALLED NEW LT 280 BEAM. INSTALLED -7 & -9 DOUBLERS AND SHIMS. INSTALLED L BL 36 AND LBL 18 INTERCOSTALS. INSTALLED T-BRACKET AT LBL 9 TO 280 BEAM. INSTALLED LT PULLEY BRACKET AND GUIDE. INSTA 2 L 7 2 4F RT A21EA 20081028 EA 2008 10 28 ASOA1224 1 20080926 A 5534 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 ASOA PERFORMED EDDY CURRENT INSPECTION OF FORWARD AND AFT V/STAB TO FUSELAGE DRAG ANGLES, LEFT SIDE. FORWARD AND AFT DRAG AN GLES VERIFIED CRACKED, FORWARD DRAG ANGLE IS MARKED AT END OF CRACK. REPAIR OF AFT DRAG ANGLE. REMOVED DAMAGED AREA FR OM FWD DRAG ANGLE ANGLE AND CLEANED UP CUT LINES TAKING CARE NOT TO DAMAGE UNDERLYING STRUCTURE PER NOTE 1 AND 2 OF REO 670-55-31-018. FABRICATED REPAIR FILLERS AND DOUBLERS USING 2024 T3 .090. PERFORMED LPI, NO DEFECTS NOTED. APPLIED PR IMER TO REPAIR FILLER AND DOUBLER AND CUT LINE PER NOTE 5 AND 6 OF REO 670-55-31-018. INSTALLED FASTENERS IN FILLER AND DOUBLER TO REPAIR AREA. FAY SEALED AND APPLIED A023 FINISH TO REPAIR AREA PER STEP 9 OF REO 670-55-31-018 JOB COMPLETE 2 L 7 2 4F RT A21EA 20081028 EA 2008 10 28 ASOA1296 1 20081002 A 5534 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTCIAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED & REPLACED AFT DRAG ANGLE ON VERTICAL STAB LEFT SIDE FAY SEALED AND APPLIED FINISH TO AREA. PERFORMED EDDY CURR ENT INSPECTION OF FORWARD AND AFT V/STAB TO FUSELAGE DRAG ANGLES, RIGHT SIDE. FORWARD & AFT DRAG ANGLES VERIFIED CRACKE D, FORWARD DRAG ANGLE IS MARKED AT THE END OF CRACK. REMOVED RT AFT DRAG ANGLE MADE TEMPLATE FOR AFT RT DRAG ANGLE (IN THE BEND). DRILLED UP FASTENER HOLES FOR RT AFT DRAG ANGLE. PLUGGED DISCREPANT HOLE WITH RIVET. REMOVED 2 SCREWS THAT WERE DRILLED OFF. INSTALLED AFT DRAG & APPLIED PRIMES TO SURFACE. FAY SEALED RT AFT DRAG ANGLE. APPLIED A023 FINISH TO RT AFT DRAG ANGLE. PERFORMED EDDY CURRENT INSPECTION OF FORWARD & AFT V/STAB TO FUSELAGE DRAG ANGLES, LEFT SIDE. FO 2 L 7 2 4F RT A21EA 20081028 EA 2008 10 28 ASOA1250 1 20081002 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED RT DRIP TRAY RBL 9, RBL 36 INTERCOSTALS AND REMOVED PITOT STATIC LINE FROM RBL 38. REMOVED CABLE PULLEY AND CAB LE GUIDE. REMOVED RT FS 280 BEAM TO BE REPLACED. TRIMMED NEW 280 RT BEAM TO FIT. PICK UP ALL FASTENER HOLES. DRILLED UP NEW DOUBLERS 8 & 11 WITH ALL SHIMS & RADIUS PACKERS. TRIMMED BACK RBL 9 FOR CLEARANCE AND TOUCH UP CUT LINE WITH 0 44. REPAIRED RT DRIP TRAY. NDTED CUT LINE ON 280 RT BEAM. PERFORMED EDDY CURRENT INSPECTION OF U-BRACKET. NO DEFECTS NOTED. INSTALLED BEAM & DOUBLER. INSTALLED RBL 18 & RBL 36 INTERCOSTALS. INSTALLED PITOT STATIC FITTING & LINE ON RT SIDE OF 280 BEAM. INSTALLED T-BRACKETS AT RBL 9 TO 280 BEAM. PERFORMED LEAK TEST OF 53 SYSTEM. INSTALLED RT PULLEY B 2 L 7 2 4F RT A21EA 20081028 EA 2008 10 28 ASOA200801267 1 20081002 A 5320 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED DAMAGED CARGO DOOR SUPPORT BEAM LOWER ANGLE & INSTALLED A NEW SERVICABLE ANGLE. REPAIRED REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT. REPAIR PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETED & REPAIR C/W REQUIRE MENTS OF EC/TC & BOMBARDIER REO 601R-53-61-1230 REV D. EXTERIOR FASTENERS AT AFT UPPER CARGO DOOR CUTOUT REQUIRES PAINT . PAINTED EXTERIOR FASTENERS AT AFT UPPER CARGO DOOR CUTOUT. REMOVED RT DRIP TRAY RBL 9, RBL 36 INTERCOSTALS & REMOVED PITOT STATIC LINE FROM RBL 38. REMOVED CABLE PULLEY & CABLE GUIDE. REMOVED RT FS 280 BEAM TO BE REPLACED. TRIMMED NE W 280 RT BEAM TO FIT. PICK UP ALL FASTENER HOLES. DRILLED UP NEW DOUBLERS 8 & 11 WITH ALL SHIMS & RADIUS PACKERS. TRI 2 L 7 2 4F RT A21EA 20081028 EA 2008 10 28 ASOA200801299 1 20081002 A 5320 PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 CUT OUT DAMAGED PORTION OF SIDE PNL. COMPLIED WITH (HFEC) OF THE PAX DOOR FWD SKIN REPAIR. NO INDICATIONS NOTED AT THI S TIME. REPAIR REQUIRED EDGE SEAL AND PAINT. EDGE SEALED REPAIR. ALSO PAINTED REPAIR. REMOVED DAMAGED CARGO DOOR SUP PORT BEAM LOWER ANGLE AND INSTALLED A NEW SERVICABLE ANGLE. REPAIRED REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINT EL ATTACHMENT. EXTERIOR FASTENERS AT AFT UPPER CARGO DOOR CUTOUT REQUIRES PAINT. PAINTED EXTERIOR FASTENERS AT AFT UPP ER CARGO DOOR CUTOUT. REMOVED RT DRIP TRAY RBL 9, RBL 36 INTERCOSTALS & REMOVED PITOT STATIC LINE FROM RBL 38. REMOVED CABLE PULLEY & CABLE GUIDE. REMOVED RT FS 280 BEAM TO BE REPLACED. TRIMMED NEW 280 RT BEAM TO FIT. PICK UP ALL FASTE 2 L 7 2 4F RT A21EA 20081028 NM 2008 10 28 ASAA0853659 1 20081020 A 2421 5911232 VENT BOEING 737 737890 1384527 NM NR 1 IDG LEAKING A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 570AS AAAH004860 35185 NR 1 IDG HAS A HISTORY OF FREQUENT OIL SERVICING. FOUND NR 1 IDG LEAKING FROM SERVICE PORT AND VENT RELIEF BUTTON. REM OVED AND REPLACED FILL PORT AND VENT RELIEF PER CMM 24 11 85, LEAK CHECK OK CLEARED TSR. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0853660 1 20081021 A 2421 761574B IDG BOEING 737 737890 1384527 NM NR 2 ENGINE LEAKING A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 558AS 5244 35177 FOLLOW UP TO FREQUENT NR 2 IDG SERVICING WITH REPORT OF OIL STREAKS. ACCOMPLISH IDG STATIC LEAK CHECK REF AMM 24 11 00 700 801. ACCOMP TSR NO LEAKS FOUND DURING IDLE RUN. REMOVED & REPLACED NR 2 ENG IDG REF MM 24 11 11 LEAK & OPS NORMAL REF MM 24 11 00. P/N VERIFICATION REF IPC 24 11 11 50, GRND VERIFICATION GOOD. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0843662 1 20081007 A 5753 SKIN BOEING 737 7374Q8 138447Q NM FOREFLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 LT OUTBOARD FOREFLAP L/E IS GOUGED 6 INCHES FROM INBOARD END. REMOVED DAMAGED SKIN, FABBED, HEAT TREATED AND INSTALLED REPLACEMENT PART IAW B737 400 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0843663 1 20081009 A 5753 SKIN BOEING 737 7374Q8 138447Q NM FOREFLAP DENTED A ASAA K NONE N FALSE WARNING IN INSP/MAINT 1 NM 02 764AS 25101 LT OUTBOARD FORE FLAP HAS MULTIPLE DENTS ON THE LOWER SURFACE INBOARD END. REMOVED DAMAGED AREAS, FABBED FILLERS AND DO UBLERS AND BONDED THE REPAIRS IAW B737 400 SRM 51 70 10 REP 4. 2 L 7 2 4F RT A16WE 20081028 EA 2008 10 28 ASOA200801297 1 20081004 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED DAMAGED PORTION OF DRAG ANGLE FROM AFT LOCATION OF PAX DOOR. PREVIOUSLY REPAIRED SEGMENT IAW BOMBARDIER REO 601 R-52-11-513. REQUIRES NDT. HFEC OF THE PAX DOOR AFT DRAG ANGLE REPAIR IAW BOMBARDIER REO 601R-52-11-513 STEP 3 AND CRJ 200 NDTM PT 1 51-20-06. NO INDICATIONS NOTED AT THIS TIME. C/W BOMBARDIER REO 601R-52-11-513. REPAIR TO PAX DOOR AFT DRAG ANGLE IN ITS ENTIRITY. SUPPLEMENTAL SDR CLOSED 10/20/08. 2 L 7 2 4F RT A21EA 20081028 EA 2008 10 28 ASOA1272 1 20081002 A 5320 BRACKET CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED CRACKED BRACKET IAW CRJ 200 SRM 51-42-06 AND 51-42-21. LOCATED HOLES IN NEW SERVICEABLE BRACKET IAW SRM 5-40-11 . INSTALLED NEW BRACKET IAW SRM 51-42-06 AND 51-42-21. SUPPLEMENTAL SDR CLOSED. 2 L 7 2 4F RT A21EA 20081028 EA 2008 10 28 ASOA200801276 1 20081003 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED DAMAGED CLIP AT FS 280, RBL 9 OUTBOARD IAW CRJ SRM 51-40-11. REF JOB 8732811 OP 201 FOR FABRICATION & INSTALLAT ION OF NEW SUPPORT OF NEW SUPPORT CLIP AT FS 280 RLB 9.0 O/B SIDE PER REO 601R-53-11-926. SUPPLEMENTAL SDR CLOSED 10/21 /08. 2 L 7 2 4F RT A21EA 20081028 NM 2008 10 28 SWAA085727 1 20081023 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085728 1 20081023 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085729 1 20081023 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CRACKED AT BS 293, BETWEEN STR 12L TO 13L. REPAIRED SHEAR TIE PER SWA EA. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085730 1 20081023 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 21L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085731 1 20081023 A 5330 6545890 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 DURING SCHEDULED SPV CHECK, FOUND BEAR STRAP SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED BEAR STRAP PER AAR E A. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085732 1 20081023 A 5330 6545890 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 DURING SCHEDULED SPV CHECK, FOUND BEAR STRAP SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED BEAR STRAP PER AAR EA . 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085733 1 20081023 A 5312 6517853 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 DURING SCHEDULED SPV CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT LBL 5.7 LOWER AFT CORNER. REPAIRED WEB P ER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085738 1 20081023 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE BELLY SKIN CORRODED BETWEEN BS 445 TO BS 455, WL 148, BETWEEN RBL 5 TO LBL 5. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085739 1 20081023 A 5311 65C25230 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 727E, RBL 17, WL 150. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085743 1 20081022 A 5330 6545767 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 480, STR 17L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085744 1 20081022 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 FOUND OVERWING EEPLS LENS COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085746 1 20081021 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 445, STR 1. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081028 2008 10 28 SWAA085754 4 20081023 A 2565 6556685 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 FOUND L1 DOOR EMERGENCY ESCAPE SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085755 1 20081023 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 879, STR 24R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085756 1 20081023 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 871, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081028 2008 10 28 SWAA085757 4 20081023 A 2565 6556685 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085762 1 20081022 A 3350 81000 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 920WN 32460 FOUND EEPLS LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081028 2008 10 28 SWAA085708 4 20081019 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 620SW 28036 FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085709 1 20081019 A 5322 6546569 SHEAR TIE BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED HC1 CHECK, FOUND AFT CARGO COMPARTMENT SHEAR TIE CORRODED AT BS 986. REMOVED AND REPLACED SHEAR TIE PE R SRM. 2 L 7 2 4F RT A16WE 20081027 NM 2008 10 27 USAA920081889 1 20081012 A 5320 6936656U9 ANGLE BOEING 737 7374B7 138449C NM ZONE 100 FUSEL CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03C10853029/001. SHEAR WEB ANGLE CRACKED BETWEEN BS 927 AND BS 947, BL 0. REPLACED SHEAR WEB AN GLE BETWEEN BS 927 AND BS 947, BLO IAW SRM 53-60-51. 2 L 7 2 4F RT A16WE 20081027 NM 2008 10 27 KCSA081536 1 20081015 A 5320 STRAP BOEING 747 747249F 1384849 NM BS 300 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 NLG SIDEWALL SKIN STRAP CRACKED AT BS 300, LBL33 2 L 7 4 4F RT A20WE 20081027 EA 2008 10 27 QXEA200800889 1 20080728 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK LT OTBD SEAT TRACK HAS CORROSION AT STA X690. BLENDED CORROSION IAW REO 670-53-00-013 SHT 2 STEPS 1-2. MA X MATERIAL REMOVED WAS .025". BLEND IS WITHIN LIMITS IAW REO 670-53-00-013 TABLE 1. ALODINED IAW SRM 51-21-11. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 QXEA200800896 1 20080728 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK LT OTBD SEAT TRACK HAS CORROSION AT STA X883. BLENDED CORROSION IAW REO 670-53-00-013 SHT 2 STEPS 1-2. MA X MATERIAL REMOVED WAS .004", BLEND IS WITHIN LIMITS IAW REO 670-53-00-013 TABLE 1. ALODINED IAW SRM 51-21-11. 2 L 7 2 4F RT A21EA 20081027 NM 2008 10 27 KCSA081534 1 20081014 A 5340 ATTACH FITTING BOEING 747 747122 1384872 NM BS 1350 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 RIGHT BODY GEAR DOOR ACTUATOR A-FRAME ATTACH FITTING CRACKED .75" AT STA 1350. 2 L 7 4 4F RT A20WE 20081027 NM 2008 10 27 KCSA081527 1 20081012 A 5310 DOOR FRAME BOEING 747 747249F 1384849 NM BS 442-450 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 L1 MAIN ENTRY DOOR LOWER FRAME CRACKED AT FWD EDGE BS 442 TO 450. 2 L 7 4 4F RT A20WE 20081027 EA 2008 10 27 QXEA200800901 1 20080728 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK LT INBRD SEAT TRACK HAS CORROSION AT STA X648. BLENDED OUT CORROSION IAW REO 670-53-00-013, MAX MATERIAL R EMOVED. .015" WITHIN LIMITS IAW REO 670-53-00-013. ALODINED IAW CRJ SRM 51-21-11. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 QXEA200800930 1 20080817 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK RT INBD SEAT TRACK NR 15 IS PITTED AT APPROX X668. EVALUATED SEAT TRACK FOUND TO BE OUT OF LIMITS. REMOVE D SEAT TRACK PREPPED AND INSTALLED NEW NR 15 SEAT TRACK IAW Q400 SRM 51-40-15 AND 51-42-05. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 QXEA200800890 1 20080728 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK LT OTBD SEAT TRACK HAS CORROSION AT STA X714. BLENDED CORROSION IAW REO 670-53-00-013 SHT 2 STEPS 1-2. MA X MATERIAL REMOVED WAS .018". BLEND IS WITHIN LIMITS IAW REO 670-53-00-013 TABLE 1. ALODINED IAW SRM 51-21-11. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 QXEA200800898 1 20080728 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK LT INBD SEAT TRACK HAS NICKS AND SCRATCHES AT STA X581, X629, X661, X690. BLENDED OUT NICKS AND SCRATCHES, MAX MATERIAL REMOVED .041". ALL BLENDS WITHIN LIMITS AIW REO 670-53-00-013. FPI INSPECTED IAW HORIZON NDTM CHAPTER 8 NO CRACKS NOTED. ALODINED IAW CRJ SRM 51-21-11. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 QXEA200800891 1 20080728 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK LT OTBD SEAT TRACK HAS CORROSION AT STA X785. BLENDED CORROSION IAW REO 670-53-00-013 SHT 2 STEPS 1-2. MA X MATERIAL REMOVED WAS .007". BLEND IS WITHIN LIMITS IAW REO 670-53-00-013 TABLE 1. ALODINED IAW SRM 51-21-11. 2 L 7 2 4F RT A21EA 20081027 NM 2008 10 27 QXEA200800974 1 20080831 A 5210 FITTING BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 414QX 4061 PDX - C-CHECK, AFT PAX DOOR FWD TRACK LATCH FITTING HAS A GOUGE ACROSS UPPER SURFACE. REPAIRED REF RD 8/4-52-145 STEPS 1, 3-7. HFEC INSPECTED IAW D8 400 NDTM PT 6, 51-00-01 & RD 8/4-52-145 STEP 2. NO CRACKS NOTED. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 USAA920081723 1 20080901 A 5311 65C22909 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 SAL - C17 -MAJOR REPAIR, FRAME AT BS 500C HAS A .409 INCH CRACK BETWEEN S8L & S9L AND A .383 INCH CRACK BETWEEN S8R & S9 R. REPAIRED FRAME AT BS 500C BETWEEN S8L & S9L, ALSO BETWEEN S8R & S9R IAW AMERICA WEST AIRLINES TASK CARD NR M1C53002. 2 L 7 2 4F RT A16WE 20081028 CE 2008 10 28 GUU2008F00065 1 20080914 A 3397 WIRE BEECH 1900 1900D 1154162 CE LANDING LIGHT OUT OF POSITION A GUUA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 29 87551 UE206 AFTER TAKEOFF UPON TURNING BOTH LANDING LIGHTS SWITCHES OFF THERE WAS A SPARK COMING OUT OF THE SWITCH. SPLICED AND REP OSITIONED WIRE AT LT LANDING LIGHT SWITCH. OPS CHECK GOOD. (K) 2 L 7 2 4T RT A24CE 20081028 NM 2008 10 28 ASAA0873644 1 20081003 A 5320 147AS6602 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 AFT PASSENGER CABIN CORROSION ON FLOORBOARD SUPPORT BEAM. CORROSION ON FLOOR SUPPORT BEAM BLENDED OUT. AREA FOUND TO B E BEYOND ALLOWABLE DAMAGE LIMIT. NEW SUPPORT BEAM INSTALLED IAW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873645 1 20081003 A 5315 141A550426 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 FORWARD PASSENGER CABIN MINOR SCRATCH ON FLOORBEAM AT BS 328 RBL 11. SCRATCH AND CORROSION ON FLOORBEAM AT BS 328 RBL 1 1 BLENDED OUT. BLEND AREA FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMIT. FLOORBEAM REPAIRED IAW ERO 8710 AND EA. 2 L 7 2 4F RT A16WE 20081028 EU 2008 10 28 MALA080179 1 20081002 A 5320 PANEL SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 340B428 SIX DISBONDED DENTS NOTED IN FUSELAGE CENTER PANEL ASSEMBLY (193AL). REPAIRED DENTS IAW EO S51031. 2 L 7 2 4T RT A52EU 20081028 NM 2008 10 28 SWAA085711 1 20081020 A 5330 6552988 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 21L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085712 1 20081021 A 3350 81000 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 262WN 32519 FOUND FWD CABIN EGRESS LIGHT LENS LOOSE. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085713 1 20081019 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085714 1 20081021 A 3350 101331 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085695 1 20081020 A 3350 PL2230LH0 STRIP BOEING 737 7373H4 1384600 NM CABIN WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 624SW 27934 DURING SCHEDULED HC1 CHECK, FOUND EEPLS STRIP WORN BETWEEN ROW 15 TO ROW 16 DEF. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085696 1 20081020 A 5312 6545409 PRESSURE PANEL BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED HC1 CHECK, FOUND LT MLG W/W PRESSURE DECK WEB CRACKED AT BS 665 LBL 32. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085700 1 20081020 A 3350 417A5700 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 263WN 32520 DURING SCHEDULED HC1 CHECK, FOUND EEPLS LIGHT LOOSE AT NR 1 POSITION. REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085701 1 20081020 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 295WN 32541 DURING SCHEDULED MV3 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085702 1 20081022 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED MV1 CHECK, FOUND KEEL BEAM CRACKED AT FWD BS 727. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085703 1 20081020 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 362SW 26573 FOUND LT OVERWING EMERGENCY EXIT LENS MISSING. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081029 WP 2008 10 29 AALA200802508 1 20080926 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1437 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 TUL CRACKS IN FUSELAGE SKIN AT STATION 1437 ABOVE AND BELOW LONGERON 3R. AREA OF DISCREPANCY IS 8 INCHES BY 4 INCHES. INSTALLED REPAIR DOUBLER PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081029 WP 2008 10 29 AALA200802510 1 20080924 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1155-1211 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 TUL, TEE ANGLE IN AFT CARGO AT RT LONGERON 27 AT STATION 1155 TO 1211 CORRODED BEYOND SRM LIMITS. INSTALLED NEW T ANGLE IN AFT CARGO AT RT LONGERON 27 AT STATION 1155 TO 1211 PER SRM 51-10-03. 2 L 7 2 4F A6WE 20081029 NM 2008 10 29 2008UALA06177 1 20081017 A 5210 LOCK NUT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 DOOR 2L EMERGENCY POWER ASSIST PRESSURE RESERVOIR RED BAND ON EMERGENCY POWER SPRING CYLINDER ALIGNED PROPERLY. ADJUSTE D CABLE TERMINAL LOCK NUT TO ACHIEVE DIMENSION PER FIG 401 A-A OF MM 52-11-33. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 EU 2008 10 29 USAA920081873 1 20081004 A 5320 D534704860000 WEB AIRBUS 320 A320231 3930325 EU ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C7 MAJOR REPAIR NR 6062298 CORROSION ON WEB AT FR51 TO FR52, S38R. REPLACED WEB AT FR51 TO FR52, S38R IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081029 NM 2008 10 29 USAA920081881 1 20080919 A 5311 6546548 FRAME BOEING 737 7373G7 138447J NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN C18 MAJOR REPAIR NR 6131828 FRAME HAS A .5 INCH CRACK AT BS 747, BETWEEN S8R AND S9R, ALSO BETWEEN S8L AND S9L. REP AIRED FRAME AT BS 747 BETWEEN S8R AND S9R, ALSO BETWEEN S8L AND S9L. IAW TASK CARD NR M1C53002. 2 L 7 2 4F RT A16WE 20081029 WP 2008 10 29 AALA200802502 1 20080922 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 1060 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 LT LOWER FORWARD WINDOW WEB (RING PAN) CRACKED AT FASTENER HOLE. INSTALLED REPAIR DOUBLER PER SRM 53-10-00-25. 2 L 7 2 4F A6WE 20081029 WP 2008 10 29 AALA200802503 1 20080927 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 LONGERON 2 RT IS CRACKED AT FLANGE. ACCOMPLISHED REPAIR SPLICE PER AARD 53-30-00-2. 2 L 7 2 4F A6WE 20081029 WP 2008 10 29 AALA200802501 1 20080922 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 886 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 LT UPPER FORWARD WINDOW WEB (RING PAN) CRACKED. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-25. 2 L 7 2 4F A6WE 20081029 EA 2008 10 29 QXEA200800900 1 20080728 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK LT INBD SEAT TRACK HAS CORROSION AT STA X597. BLENDED OUT CORROSION IAW REO 670-53-00-013, MAX MATERIAL RE MOVED, INNER CHANNEL .003", UPPER CLAW .005". WITHIN LIMITS IAW REO 670-53-00-013. ALODINED IAW CRJ SRM 51-21-11. 2 L 7 2 4F RT A21EA 20081029 NM 2008 10 29 USAA920081870 1 20081004 A 5340 6935352U14 STRINGER CLIP BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03C10853040/003 STRINGER CLIP CRACKED AT BS867, S4L. REPLACED STRINGER CLIP AT BS 867, S4L IAW SR M 51-10-01 AND DRAWING NR 69-35352. 2 L 7 2 4F RT A16WE 20081029 EA 2008 10 29 ASOA200801277 1 20081003 A 5320 SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 280 DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED DAMAGED CLIP AT FS 280, LBL 9 INBOARD IAW SRM 51-40-11. REF JOB 8732811 OP 201 FOR FABRICATION & INSTALLATION O F NEW SUPPORT CLIP AT FS 280 LBL 9 I/B SIDE PER REO 601R-53-11-926. 2 L 7 2 4F RT A21EA 20081029 NM 2008 10 29 2008UALA06184 1 20081019 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR SHORTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 569UA 26677 DOOR 2R AND PARTS OF AFT CABIN EMERGENCY EXIT LIGHTS ARE ON. REPLACED SHORTED BULB FOR DOOR 2 RIGHT EXTERNAL EMERGENCY LIGHT AND REPLACED INOP BATTERY PACK AT STA LOC 1240 ITEM M10699 REF WDM 33-51-14 PG 1 AND MM 33-51-06 AND MM 33-51-07. SYS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 2008UALA06186 1 20081019 A 5210 S413T10211 SPRING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L1 DOOR WEAK A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 644UA 25094 L1 DOOR GAS SPRING WEAK. REMOVED AND REPLACED GAS SPRING. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081029 NM 2008 10 29 2008UALA06187 1 20081019 A 3320 TERMINAL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN OVERHEATED A UALA K NONE M OVER TEMP IN INSP/MAINT 1 WP 29 644UA 25094 P19 PANEL, T180 AND T184 TERMINAL LUGS SHOW SIGNS OF OVERHEATING. REMOVED AND REPLACED TERMINAL LUGS. OPS CHECK GOOD O F FWD INDIRECT CEILING LIGHTS AND SIDEWALL LIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 20081029 NM 2008 10 29 2008UALA06189 1 20081020 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT SEAT 2J INOP. REPLACED EEL LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 20081029 NM 2008 10 29 F3LA200800608 1 20080912 A 5320 D5367301900000 PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 930FR 31 2241 REF NON-ROUTINE C050863. DURING C3-C-CHECK. INSP NOTED THE AFT PIT TRANSITION PANEL 151TG WAS DAMAGED. MAINT REPAIRED DA MAGED FLOOR PANEL IAW WITH THE REQUIREMENTS OF SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR. IT WAS INSPECTE D AND FOUND ACCEPTABLE. (K) 2 L 7 2 4F RT A28NM 20081029 NM 2008 10 29 2008UALA06195 1 20081020 A 5754 SLAT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WING DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 512UA 24809 NR 1 AND NR 2 LEADING EDGE SLAT DAMAGE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 USAASB08101 1 20081026 A 2781 FLAP SYSTEM BOEING 737 737401 138449B NM LE FLAPS MALFUNCTIONED A USAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 EA 19 404US 23886 ON DESCENT TO CLT, FROM FLL, THE NR 2 LEADING EDGE DEVICE INDICATED AN ASYMMETRY/LEADING EDGE FLAP TRANSIT WHEN FLAPS 1 WERE SELECTED. CREW DECLARED AN EMERGENCY AND LANDED AT CLT WITHOUT FURTHER INCIDENT. AINTENANCE CHECKED/WIGGLED WIRES. COULD NOT DUPLICATE PROBLEM. NO HISTORY FOR 90 DAYS. 2 L 7 2 4F RT A16WE 20081029 NE 2008 10 29 2008UALA06196 2 20081020 A 7260 FLANGE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GEAR BOX BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 647UA 25284 727366 NR 1 ENG ANGLE GEAR BOX AFT END HAS LOOSE BOLTS AT 12:00 AND FLANGE EAR IS BROKEN AT 1:00. 2 L 7 2 4F 4 F RT A1NM E24NE 20081029 NM 2008 10 29 2008UALA06197 1 20081019 A 2421 GCU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT GENERATOR MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 540UA 25252 LOST RIGHT GENERATOR. FLIGHT DIVERTED. REPLACED GCU. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 2008UALA06217 1 20081005 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 818UA 882 BEAM 95 CORRODED. REMOVED FLOORBEAM 95. REMOVED BRACKETS AND DRILLED NEW BEAM. ALL BRACKETS AND ATTACH FITTINGS INSTAL LED. BEAM INSTALLED, ATTACHMENT COMPLETE AT FRAME 64, NEEDS BOLTS AT FRAME 66 AND 65. COMPLETED INSTALLATION OF BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081029 NM 2008 10 29 2008UALA06207 1 20081020 A 2120 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN ODOR A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 822UA 948 F/A REPORTED PLASTIC BURNING ODOR NEAR DOOR 2L. SMELL GONE AFTER 5 MINUTES. 2 L 7 2 4F 4 F RT A28NM E40NE 20081029 NM 2008 10 29 2008UALA06166 1 20081017 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 781UA 26945 SEAT 1E EMERGENCY LIGHT IS OUT. REPLACED LIGHT ASSY, OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081029 NM 2008 10 29 2008UALA06167 1 20081017 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 781UA 26945 SEAT 43G EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT, TESTED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081029 2008 10 29 2008UALA06216 4 20080910 A 2565 D31591478U1 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR MALFUNCTIONED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 334UA 24229 DOOR 1L PARTIAL SLIDE DEPLOYMENT. REMOVED SLIDE AND CONTAINER FROM L1 DOOR. INSTALLED NEW SLIDE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081029 NM 2008 10 29 2008UALA06221 1 20081007 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 818UA 882 BEAM 140 CORRODED. REMOVED FLOORBEAM 140. TRANSFERRING FASTENER HOLES TO NEW BEAM. INSTALLING FASTENERS IN NEW BEAM. INSTALLED BEAM 140. 2 L 7 2 4F 4 F RT A28NM E40NE 20081029 NM 2008 10 29 2008UALA06220 1 20081007 A 2421 745329F IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 656UA 25394 RT ENGINE IDG FILTER DPI EXTENDED. REPLACED IDG. OP CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081029 NM 2008 10 29 MZZA0800004 1 20081023 A 3350 D71702030 POWER SUPPLY BOEING 737 737824 13844BZ NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 27246 28956 EMERGENCY LIGHTS INOP EXT R1 DOOR OVERHEAD R1 DOOR AND AT EMERGENCY FLOODLIGHTS ABOVE SEAT 2EF, 3EF AND 4EF. REMOVED AN D REPLACED POWER SUPPLY PER AMM33-51-06-960-806, OPERATION TEST OK PER AMM 33-51-00. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0800977 1 20081023 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59630 27534 LEFT FUSELAGE FRAME IS CRACKED AT PSU RAIL SUPPORT BRACKET MOUNT RIVET LOCATED BETWEEN STRINGERS 8 AND 9 AND STATION 360 . REMOVED SUPPORT RAIL AND ACCOMPLISHED REPAIR PER ECRA 5311-01428. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0800978 1 20081023 A 5315 1417547 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 68155 30434 E AND E COMPARTMENT M/D FLOORBEAM AT STATION 246 MID CHORD FOUND CRACKED AT LBL 40. E AND E COMPARTMENT M/D FLOORBEAM S TATION 246 MID CHORD AT LBL 40 REPAIRED PER SRM 53-10-51, REPAIR 2, FIG 1, REF ECRA5310-04854. HFEC NO CRACK FOUND. 2 L 7 2 4F RT A1NM 20081029 NM 2008 10 29 CALA0800984 1 20081023 A 5320 65528941 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 INTERCOSTAL CRACKED AT ATTACH POINT TO CABIN FLOORBEAM STATION 540, LBL 3. REMOVED AND REPLACED INTERCOSTAL IAW B737 SR M 51-40-02. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0800989 1 20081023 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 BODY STATION 787L FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. CUT OUT DAMAGE ON FRAME AT BODY STATION 787L BETWEEN S-8 AND S-9. FABRICATED REPAIR PARTS AND INSTALLED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0800994 1 20081023 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 BODY STATION 867 RIGHT FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED BODY STATION 867 R IGHT FRAME AT S8 AND S9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0800995 1 20081023 A 5320 BAC1515553 SHEAR WEB BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14121 27563 SHEAR WEB LEFT CORRODED AT STATION 460 TO 640. REPAIRED DAMAGE SECTION OF LT SHEAR WEB FROM STATION 460 TO 520 REF SRM 51-70-12, REMOVED LIGHT SURFACE CORROSION FROM 520 TO 640, FOUND WITHIM LIMITS REF SRM 51-10-02. 2 L 7 2 4F RT A2NM 20081029 NM 2008 10 29 CALA0800996 1 20081023 A 5315 147A5506 FLOORBEAM BOEING 737 737924 13848A1 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 30401 30118 FLOORBEAM AT STATION 986.5 UPPER FLANGE BLENDED OUT OF LIMITS AT LBL 27. INSTALLED REPAIR PER SRM 53-00-51, FIG 203. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0800997 1 20081023 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 BODY STATION 747 RT SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED BODY STATION 747 RIGHT FRAME AT S8 AND S9 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0801000 1 20081023 A 5311 65C3351 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 BODY STATION 440 LT SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRD FRAME AT BODY STA TION 440 LT SIDE AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9 IAW EA 5310-04498. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0801002 1 20081023 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 BODY STATION 360 LT SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED FRAME AT BODY ST ATION 360L BETWEEN S-8 AND S-9 IAW EA 5310-04498. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0801003 1 20081023 A 3350 20121 CHARGER BOEING 737 737724 13844BY NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 17719 28938 EMERGENCY AISLE LIGHTS INOPERATIVE AFT OF EMERGENCY EXIT- ROWS 15 TO 21. REMOVED AND REPLACED BATTERY CHARGER AND BATTE RY PACK AT MID CABIN. OPS CHECKS GOOD. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0801004 1 20081023 A 3350 2760005 FUSE BOEING 737 737824 13844BZ NM POWER SUPPLY BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 77296 34002 EMERGENCY EXIT SLIDE LIGHT LOCATED AT LEFT HAND OVERWING AFT EXIT AT WING ROOT IS INOPERATIVE. FOUND FUSE BLOWN AT POWE R SUPPLY M1670. REPLACED FUSE P/N 2760005, OPERATION CHECKS GOOD REF PER W/D 33-51-13 PG 3 SH 2. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 2008UALA06227 1 20081021 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 AFT CARGO COMPT, FRAME AT BS 1480 LT AND STR 26L HAS A DENT AT INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMA GE AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081028 CE 2008 10 28 DXTA2008102003311 1 20081020 A 3260 WARNING SYSTEM CESSNA 750 750 2076810 CE COCKPIT ACTIVATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 960QS 7500160 UPON DEPARTURE FROM SFO & GEAR RETRACTION, GEAR "UNLOCK" LIGHT ILLUMINATED WITH NO GREEN LIGHTS. 2 L 7 2 4J RT T00007WI 20081028 EA 2008 10 28 HNA2008F00050 1 20081016 A 3320 BR900021 BALLAST DHAV DHC8 DHC8311 1386006 EA CABIN LIGHTS FAILED A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 326EN 234 STRONG ELECTRICAL ODOR IN CABIN OVERHEAD ISLE BETWEEN ROWS 2 AND 4, OVERHEAD FLUORESCENT LIGHT FAILED. AIRCRAFT WAS ON G ROUND. INSPECTED AREA AND FOUND OVERHEAD LIGHT AT 2DF SOCKET BURNED. INSTALLED NEW BULB, NO FIX. INSPECTED SOCKETS, REM OVED AND REPLACED BALLAST INSTALLED NEW BULB OPERATIONAL CHECK GOOD. REMOVED BALLAST, BR9000-21, CONFORMED WITH REQUIREM ENTS OF AD 2006-17-10, AND SHUT POWER OFF TO THE LIGHT FIXTURE. (K) 2 H 7 2 4T RT A13NM 20081028 NM 2008 10 28 ASAA0843607 1 20080914 A 5315 654681025 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 AFT CABIN FLOORBEAM STA 967 CORRODED RBL 40 TO LBL 40. CUT OUT DAMAGED AREA OF UPPER CHORD, FABRICATED REPAIR PARTS, LO CATED, DRILLED, INSTALLED REPAIR PARTS UPPER CHORD IAW B737 400 SRM 53 00 51 FIG 201. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0843606 1 20080917 A 5753 6542451288 SKIN BOEING 737 7374Q8 138447Q NM FOREFLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 RT WING O/B FORE FLAP I/B LEADING EDGE CHAFED FROM CONTACT WITH CAVITY PANEL. CUT OUT DAMAGED AREA, FABRICATED REPAIR P ARTS AND DOUBLER IAW B737 400 SRM 51 53 01 FIG 201 AND INSTALLED. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 2008UALA06162 1 20081017 A 3397 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHT INOPERATIVE SEAT 2J FWD SECTION. SECURED CONNECTOR, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081028 EU 2008 10 28 2008UALA06153 1 20081016 A 5230 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AFT CARGO DOOR CHAFED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 442UA 780 AFT CARGO DOOR LATCH HOOKS CONTACTING LOWER SURFACE OF DOOR SILL. FOUND PREVIOUS DOOR SILL REPLACEMENT DOES NOT HAVE RE LIEF HOLES CUT OUT FOR HOOK CLEARANCE PER DRAWING D53475575. PROVIDED RELIEF HOLES IN LOWER SILL AND REINSTALLED UPPER DOUBLERS INSPECTED PER DRAWING D53475575. 2 L 7 2 4F 4 F RT A28NM E40NE 20081028 NM 2008 10 28 2008UALA06154 1 20081017 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 528UA 25018 EEL LIGHT FLOOR STRIP AT 13ABC DAMAGED. REINSTALLED LOOSE EEL STRIP AND SECURED EEL COVER, OPS CHECKED OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081028 NM 2008 10 28 2008UALA06155 1 20081017 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHT INOP CREW REST STAIRS ILLUM. REPLACED LAMPS. 2 L 7 4 4F 4 F RT A20WE E24NE 20081028 NM 2008 10 28 2008UALA06164 1 20081017 A 3040 HEATER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT WINDOW ODOR A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 646UA 25283 ELECTRICAL ODOR IN FLIGHT DECK. FLIGHT DIVERTED. IDENTIFIED CAUSE TO THE FO'S NR 1 WINDOW HEAT LOWER AFT CONNECTION AN D ASSOCIATED WIRES AND CONTACTS. TURNING OFF WINDOW HEAT INDUCED CESSATION OF ODOR. AREA COOLED TO NORMAL TEMPERATURE. REPLACED FIRST OFFICER'S NR 1 WINDOW. 2 L 7 2 4F 4 F RT A1NM E24NE 20081028 NM 2008 10 28 ASAA0873624 1 20081001 A 5320 146A75022 ANGLE BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 AFT CARGO PIT CORROSION FOUND ON RT ZEE ANGLE AT BS 767 RBL 18. CORROSION FOUND TO BE BEYOND LIMITS IAW B737 700 SRM 53 00 53, FOR REPAIR ACTION REF CARD 5106696. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873626 1 20081003 A 5315 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE SCRATCHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 FWD PASSENGER CABIN FLOORBEAM BS 312-328 LBL 12 SCRATCHED. FLOORBEAM AT BS 312 328 LBL 12 REPLACED WITH MADE REPAIR PAR T IAW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873627 1 20081003 A 5315 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE SCRATCHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 FWD PASSENGER CABIN BS 328 344 LBL 12 FLOORBEAM SCRATCHED. FLOORBEAM BS 328 344 LBL 12 REPLACED WITH MADE REPAIR PART I AW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873629 1 20081001 A 5320 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 AFT CARGO PIT CORROSION ON FLOOR SUPPORT BS 767 + 6 RBL 8.1. AFT CARGO PIT CORROSION ON FLOOR SUPPORT BS 767 + 6 RBL 8. 1 BLEND OUT AND FOUND TO BE BEYOND ALLOWABLE LIMITS AND REPAIR ACCOMPLISHED IAW B737 700 SRM 53 00 53 REPAIR 2 FIG 201. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873655 1 20081002 A 5312 148A22812 BULKHEAD BOEING 737 737790 13844CN NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 DENT ON AFT FACE OF 1016 BULKHEAD 0.032 INCH IN DEPTH BEYOND LIMIT IAW B737 700 SRM 53 80 08. DENT ON AFT FACE OF 1016 BULKHEAD REPAIRED IAW B737 700 SRM 53 80 08 REPAIR 1 AND EA 5310 02829. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873636 1 20081001 A 5320 149A811829 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 AFT CARGO PIT CORROSION AROUND ANCHOR NUTS ON SIDEWALL FLOOR SUPPORT ANGLE AT BS 947 LBL 10 RBL 21. REPLACED SUPPORT AN GLE AT BS 947 WITH A NEW ONE IAW B737 400 SRM 51 40 02 AND 51 40 05. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085763 1 20081023 A 5312 6516300 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 DURING SCHEDULED 12Y CHECK, FOUND HORIZONTAL WEB CRACKED AT BS 178, LBL 18. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085764 1 20081023 A 5312 6517582 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 DURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, LBL 17. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085765 1 20081023 A 5312 6517582 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 DURING SCHEDULED 12Y CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 184, LBL 17. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085685 1 20081017 A 3350 101331 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 417WN 29822 DURING SCHEDULED MV2 CHECK, FOUND OVERHEAD BIN EMERGENCY EXIT LIGHT INOP AT ROW 10 DEF. REPLAMPED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085686 1 20081019 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 436WN 32456 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REPLAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085769 1 20081025 A 3350 417A5500 LIGHT BOEING 737 737705 13844SC NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 270WN 29089 DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING EMERGECY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085772 1 20081025 A 3350 100031 LENS BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 388SW 26591 DURING SCHEDULED 14Y CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN LENS OUT OF POSITION. INSTALLED SIGN PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085773 1 20081024 A 3350 417A5700 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 401WN 29813 DURING SCHEDULED MV2 CHECK, FOUND AFT CABIN EEPLS LIGHTS INOP. REMOVED AND REPLACED LIGHT STRIP PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085774 1 20081023 A 3350 417A5700 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED MV1 CHECK, FOUND EEPLS LIGHT LOOSE AT ROW 1 ABC. SECURED TRACK PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085775 1 20081023 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 455WN 32462 FOUND EEPLS LIGHT COVER LOOSE AT FWD CABIN. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085780 1 20081023 A 5312 6517582 BULKHEAD BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17, WL 223 TO WL 230. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085781 1 20081026 A 3350 101114 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 527SW 26569 DURING SCHEDULED RON CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085786 1 20081024 A 5330 6545774 SKIN BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 784, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085787 1 20081024 A 5330 6545768 SKIN BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 26L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085788 1 20081025 A 5754 6546486 WEDGE BOEING 737 7373T0 1384582 NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED SPV CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE O/B END DELAMINATED. REPAIRED WEDGE PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 2008UALA06172 1 20081017 A 3350 767 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 658UA 27113 EXTERIOR EMERGENCY LIGHT AT DOOR 2L INOP. RELAMPED EMERGENCY LIGHT. OPS CHECK PASSED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081029 NM 2008 10 29 2008UALA06174 1 20081017 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 LT OVERWING MANUAL BACKUP CABLE FAILS OPS CHECK. CUT OUT DAMAGED SKIN REF SRM 53-00-01 FIG 201. FAB FILLER AND DOUBLER REF BAC DWG 146N3750 AND SRM 53-00-01 FIG 201, AND INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 AALA200802492 1 20080925 A 5320 INTERCOSTAL BOEING 737 737823 13844CB NM BS 943 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION ON UPPER SURFACE OF INTERCOSTAL BEYOND LIMITS. REPLACED INTERCOSTAL PER SRM 51-10-02-OG. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802500 1 20080926 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION ON FLOORBEAM AT CLIP NUT HOLE BEYOND LIMITS. REPAIRED PER ESO 61000 DATED 22 SEP 08. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 USAA920081879 1 20080919 A 5311 6546593 FRAME BOEING 737 7373G7 138447J NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN C18 MAJOR REPAIR NR 6131828 FRAME HAS A .250 INCH CRACK AT BS 500A, BETWEEN S8R AND S9R AND A .500 INCH CRACK BETWEE N S8L AND S9L. REPAIRED FRAME AT BS 500A, BETWEEN S8R AND S9R, ALSO BETWEEN S8L AND S9L. IAW TASK CARD NR M1C53002. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 08FDEA04489 1 20081022 A 5313 A5A70251 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 CENTER CARGO, LEFT STA 5-21 LONGERON 41 FOUND EXISTING REPAIR SPLICE FITTING CRACKED. REPAIR SPLICE AT CENTER CARGO L T BS 5-21 LONGERON 41 REMOVED AND REPLACED AS PER SRM 51-33-01. SPLICE FABRICATED AS PER SRM 53-10-00. SPLICE PROCTECT ED AND PAINTED AS PER SRM 51-21-01. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 08FDEA04490 1 20081023 A 5753 ARC0503503 HINGE DOUG MD11 MD11F 3023600 NM ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT UPPER ATTACH INBOARD HOLE FOUND WITH SCORING MARK. SCORING REPAIR ED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 08FDEA04491 1 20081023 A 5753 ARC0503503 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT UPPER ATTACH OUTBOARD HOLE FOUND WITH SCORING MARK. SCORING REPAI RED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 08FDEA04492 1 20081023 A 5753 ARC0503503 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER ATTACH INBOARD HOLE FORWARD MATING SURFACE FOUND WITH CORROS ION. CORROSION REPAIRED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 08FDEA04493 1 20081023 A 5744 ARC0503503 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER ATTACH INBOARD HOLE AFT MATING SURFACE FOUND WITH CORROSION. CORROSION REPAIRED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 08FDEA04520 1 20081024 A 5340 69456282 STRINGER CLIP BOEING 727 7272D4 138407U NM BS 740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FWD PIT (STA 740), STR 27L, END CLIP ON STRINGER CORRODED FABRICATED NEW STRINGER CLIP, TREATED AND PRIMED. REFERENCE B OEING DRAWING NR 69-45628/ITEM NR 2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081029 EU 2008 10 29 08FDEA04529 1 20081024 A 3230 A2527111R1 SEQUENCE VALVE AIRBUS 310 A310203 3930313 EU NLG MALFUNCTIONED A FDEA O OTHER S J AFFECT SYSTEMS WARNING INDICATION AP APPROACH 1 CE 21 426FE 245 UNSAFE NOSE GEAR INDICATION/MANUAL CRANK DOWN. JACK ADAPTER AND TEST BOX SHIPPED FROM LAX, T/S TO SEQUENCE VALVE AND RT NOSE GEAR ACTUATOR. BOTH REPLACED PER 32-31-16-4 AND 32-31-18-4. OPS AND LEAK CHECKS GOOD PER 32-30-158. ALSO, PERF ORMED FREE FALL ACTUATION PER 32-33-00-2. ALL ACTUATION NORMAL. RESTORED AIRCRAFT BACK TO NORMAL CONFIGURATION. A/C O K FOR SERVICE. 2 L 7 2 4F RT A35EU 20081029 WP 2008 10 29 08FDEA04536 1 20081024 A 5412 AUB702527 BULKHEAD DOUG MD10 MD1010F 3022112 WP NR 3 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 NR 3 PYLON AFT MOUNT BY THE "V" BLOCK, THERE IS A SHEARED FASTENER AND LOOSE FASTENERS ALONG THE AFT ROW. REMOVED BOLTS IN REF TO DC/MD-10 SRM 51-31-01; VOL II. ACCOMPLISHED BHEC INSPECTION OF THE HOLES AFT ROW AT THE AFT MOUNT V-BLOCK IA W NDTSPM 60-10-01.003 USING TWS 8209A. CRACKS WERE INDICATED IN 4 HOLES. REAMED 4 HOLES, INDICATED HOLES IN REF TO DC/ MD-10 SRM 54-20-00; FIG 27; VOL I. ACCOMPLISHED BHEC OF REAMED HOLES IAW NDTSPM 60-10-01.003 USING TOOL NR TWS 8209A; N O CRACK NOTED. INSTALLED BUSHINGS IN 4 HOLES IN REF TO DC/MD-10 SRM 54-20-00; PARA 2; VOL I. INSTALLED BOLTS IN ALL HO LES IN REF TO DAC DWG AUB 7025; REV "AS". 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 08FDEA04538 1 20081024 A 2910 AV13J5144 VALVE BOEING 727 727225 1384077 NM HYD SYSTEM LEAKING A FDEA O OTHER K S FLUID LOSS AFFECT SYSTEMS DE DESCENT 1 CE 21 464FE 21288 DURING DESCENT A HYDRAULIC SYSTEM LOST ALL QTY. COMPLIED WITH QRH LOSS OF ALL HYDRAULIC SYSTEM A. ALT FLAPS AND MANU AL GEAR EXT SYST A ENG 1 AND 2 FLAP SHUTOFF SWITCHES CLOSED FOR MORE THAN 5 MIN WITH ENGINES RUNNING. REMOVED AND REPL ACED RT FLAP BYPASS VALVE PER MM 27-51-151-4. ALSO REPLACED A SYS. CASE DRAIN FILTERS PER MM 29-11-041-2 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 08FDEA04539 1 20081025 A 5320 44221015 PANEL BOEING 727 7272D4 138407U NM ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 PFM BOX SHROUD SEVERED ON ONE END AND CRACKED AT OTHER END, PANEL RACK, DOT 3 REPAIRED PFM BOX SHROUD REF SRM 51-40-9 PA R 3 AND 7. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 08FDEA04542 1 20081025 A 5311 FRAME BOEING 757 75723A 1384967 NM ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 AFTER REMOVAL DOUBLER FROM TV MONITOR SUPPORT FOUNDED SEVERAL HOLES ON FRAME AT STA, 1020 REPAIRED FRAME IAW SRM 53-00-0 7 REPAIR NR 3, THIS IS A CATEGORY "B" REPAIR WITH THE FOLLOW-UP INSPECTION. HFEC INSPECTION EVERY 12,000 F/C AS GIVEN I N NDT PART. 6 ,51-00-01 AND REPEAT EVERY 12,000 F/C INTERVALS, AS AN ALTERNATIVE DO A DETAILED VISUAL INSPECTION AT 9,0 00 F/C INTERVALS AFTER INITIAL INSP. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 KNNA20080074 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 787, STR 2L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080075 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 787, STR 2R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080076 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 787, STR 3R. 2 L 7 2 4F A16WE 20081020 WP 2008 10 20 AALA200802286 1 20080906 A 3397 CONTACT DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 290AA 49302 LGA EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 23 TO 30 INOPERATIVE. CLEANED AND ADJUSTED CONTACT AT ROW 25 FOR EMERGENCY L IGHTS AT OVERHEAD SEAT ROWS 23 TO 30. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081020 NM 2008 10 20 AALA200802296 1 20080907 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 798AN 30797 DFW EMERGENCY LIGHT AT FORWARD GALLEY RT SIDE MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FORWARD GALLEY RT SIDE . SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081020 WP 2008 10 20 AALA200802288 1 20080906 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 290AA 49302 LGA EMERGENCY LIGHT AT OVERHEAD AFT SERVICE AREA MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OVERHEAD AFT SERVIC E AREA. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081020 NM 2008 10 20 AALA200802317 1 20080909 A 3350 SOCKET BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 639AA 24597 SEA EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25 WOULD NOT GO OUT WHEN POWER WAS REMOVED FROM ACFT. FOUND BAD LIGHT SOCKET AT SEAT 16D. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHTS AT SEAT ROWS 16 TO 25. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081020 EU 2008 10 20 USAA920081792 1 20080925 A 5347 D5311278220200 SEAT TRACK AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 PIT - MAJOR REPAIR - S4 CHECK, LEVEL 2 CORROSION ON SEAT TRACK FR 20, -Y1292. REPLACED SEAT TRACK, FR 20, -Y1292 IAW A3 19 SRM 51-42-11. 2 L 7 2 4F RT A28NM 20081020 NM 2008 10 20 F3LA200800644 1 20080922 A 5321 D5367225400000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE PERFORATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 919FR 27 1980 DURING C4/S1 C-CHECK, INSPECTION NOTED FLOOR PANEL 131EG WAS PERFORATED. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMEN TS OF A319 SRM 53-02-00,PARA 8C. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081020 EU 2008 10 20 F3LA200800625 1 20080925 A 5321 D5367406500000 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 808FR 29 3038 DURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY TRANSITION PANEL 132EG HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 SRM 53-02-00 PARA 8F AND EO A0-53F-12307. UPON COMPLETION OF THE REPAIR, IT WAS INS PECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT 20081020 EU 2008 10 20 USAA920081787 1 20080924 A 5315 D5347217220599 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 PIT - MAJOR REPAIR - S4 CHECK, LEVEL 2 CORROSION ON FLOORBEAM FR 66 - FR 68, -Y1292. REPLACED FLOORBEAM, FR 66 - FR 68, -Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081020 EU 2008 10 20 F3LA200800622 1 20080925 A 5321 D5367407000000 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CARGO BAY DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 808FR 29 3038 DURING C1 C-CHECK, INSPECTION NOTED FWD CARGO BAY FLOOR PANEL 131DG HAS PUNCTURES AND TEARS. MX REPAIRED THE FLOOR PANE L IAW THE REQUIREMENTS OF A318 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCE PTABLE. 2 L 7 2 4F RT 20081020 EU 2008 10 20 USAA920081795 1 20080924 A 5322 D5347112420200 SHEAR TIE AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 PIT - MAJOR REPAIR - S4 CHECK, LEVEL 2 CORROSION ON RT SHEAR TIE PLATE, FR 69- FR 70, S23R. REPLACED RT SHEAR TIE PLATE , FR 69- FR 70, S23R IAW US AIRWAYS EO 5307Y284. 2 L 7 2 4F RT A28NM 20081021 NM 2008 10 21 USAA920081756 1 20080822 A 5753 6543431200 SKIN BOEING 737 7373G7 1384595 NM FOREFLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 SAL - MAJOR REPAIR - C19 CHECK, RT WING OUTBOARD FOREFLAP UPPER SURFACE DELAMINATED, WBL 202.6 -WBL 414.4. REPAIRED RT WING OUTBOARD FOREFLAP UPPER SURFACE, WBL 202.6 - WBL 414.4 IAW B737-300 SRM 57-70-2R. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081757 1 20080822 A 5320 655056810 WEB BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 SAL - MAJOR REPAIR - C19 CHECK, CORROSION ON WEB, BS 947 -BS 986.5, LBL48. REPAIRED WEB, BS 947 - BS 986.5, LBL48 IAW B 737-300 SRM 51-70-11. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081758 1 20080825 A 5311 90526913 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 727D, S9L. REPAIRED FRAME, BS 727D, S9L IAW US AIRWAYS TASK CARD M1C5 3002. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081759 1 20080825 A 5311 65465252 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 380, S9R. REPAIRED FRAME, BS 380, S9R IAW US AIRWAYS TASK CARD M1C530 02. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081764 1 20080825 A 5311 65465588 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 907, S9R. REPLACED FRAME, BS 907, S9R IAW US AIRWAYS TASK CARD M1C530 02. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081765 1 20080825 A 5311 90526911 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 480, S9L AND S9R. REPAIRED FRAME, BS 480, S9L AND S9R IAW US AIRWAYS TASK CARD M1C53002. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081767 1 20080825 A 5311 654655514 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 867, S9L AND S9R. REPAIRED FRAME, BS 867, S9L AND S9R IAW US AIRWAYS TASK CARD M1C53002. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081774 1 20080904 A 5320 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT - MAJOR REPAIR - Q1 CHECK, LEVEL 2 CORROSION ON Z-ANGLE, BS 992, RBL 33- RBL 45. REPLACED Z-ANGLE, BS 992, RBL 33 - RBL 45 IAW B737 SRM 51-10-51-02. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081775 1 20080903 A 5315 FLOORBEAM BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT - MAJOR REPAIR - Q1 CHECK, LEVEL 2 CORROSION ON FLOORBEAM T-CAP, BS 312, LBL 34- RBL 22. REPLACED FLOORBEAM T-CAP , BS 312, LBL 34 - RBL 22 IAW UB737 SRM 53-10-51-2R5. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081782 1 20080929 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 804AW 1043 FLT NR 0511 - SAN-PHX - EEL FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081021 NM 2008 10 21 USAA922081772 1 20080919 A 5320 65C320747 INTERCOSTAL BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - MAJOR REPAIR - C18 CHECK, LEVEL 2 CORROSION ON INTERCOSTAL, BS 986.5, RBL 38, WL 208. REPLACED INTERCOSTAL, BS 98 6.5, RBL 38, WL 208 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 R5KB10132 1 20081013 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN DISCHARGED I R5KB K NONE L NO TEST IN INSP/MAINT 1 SO 33 422BN 20735 L2 DOOR EMERGENCY EXIT LIGHT INOP. 2 L 7 3 4F A3WE 20081022 CE 2008 10 22 T17A081022001 1 20081002 A 3240 AC67732 CONTROL VALVE RAYTHN 850 HAWKER850XP 7150016 CE BRAKES INADEQUATE E T17A O OTHER J WARNING INDICATION LD LANDING 1 GL 17 403CT 921 258818 LEFT MAIN LANDING GEAR BRAKES WERE LOCKED UP ON LANDING. THE NR 1 AND NR 2 WHEEL AND TIRE ASSEMBLIES WERE DISTROYED. A FTER REPLACING THE WHEELS, NO DEFECTS COULD BE FOUND WITH THE BRAKE SYSTEM. AS A PRECAUTION THE BRAKE CONTROL VALVE WAS REPLACED AS IT WAS THE ONLY COMPONENT THOUGHT TO CREATE THE PROBLEM. 1 L 7 2 4F RT A3EU 20081022 NM 2008 10 22 USAASB08097 1 20081014 A 2120 UNKNOWN BOEING 737 737401 1384701 NM COCKPIT ODOR A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 418US 23985 ON DESCENT, AT APPROXIMATELY 15,000 FT, CREW NOTICED A STRONG ODOR IN THE COCKPIT. SMELLED LIKE SOMETHING OVERHEATED OR WAS BURNING. CABIN CREW VERIFIED ODOR BUT DID NOT NOTICE ANY SMOKE. GALLEY OVENS AND COFFEEMAKERS WERE NOT IN USE AND NO CIRCUIT BREAKERS WERE POPPED. ODOR BECAME STRONGER AND LASTED APPROXIMATELY FIVE MINUTES. CREW DECLARED AN EMERGEN CY. FLIGHT LANDED AT RSW WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. ODOR DISSIPATED ONCE AIRCRAFT ARRIVED. MAIN TENANCE ACCOMPLISHED MM TASK 21-00-01, PAGE 1, FAULT ISOLATION. INSPECTED FORWARD AND MID E & E COMPARTMENTS, BOTH CARG O BAYS, CABIN, COCKPIT, GALLEYS, PACK BAYS, WHEEL WELLS, LAVATORIES AND ENGINES. NO ODORS NOTED. 2 L 7 2 4F RT A16WE 20081022 SO 2008 10 22 SIMA200828901 1 20081015 A 2913 971808 PUMP EMB 145 EMB145LR 3260212 SO HYDRAULIC SYS MALFUNCTIONED A SIMA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 21 649PP 10372 145234 ON FLIGHT 3609 CREW REPORTED HYDRAULIC SYSTEM 2 LOW QUANTITY THEN HYDRAULIC SYSTEM 2 PUMP FAIL AND HYDRAULIC SYS 2 FAIL MESSAGE ON EICAS. CREW DECLARED A EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND R EPLACED NR 2 HYDRAULIC PUMP PER EMB AMM 29-10-03. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081022 NM 2008 10 22 UPS08M53539 1 20080516 A 5753 HINGE DOUG MD11 MD11F 3023600 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A RT WING O/B FLAP I/B AFT HINGE I/B PIVOT BORE CORRODED. RT WING O/B FLAP I/B AFT HINGE I/B PIVOT BO RE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-52-04. 2 L 7 3 4F RT A22WE 20081022 NM 2008 10 22 UPS08M53540 1 20080516 A 5753 HINGE DOUG MD11 MD11F 3023600 NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A RT WING O/B FLAP I/B AFT HINGE I/B AFT HINGE I/B PIVOT I/B SPOTFACE CORRODED. RT WING O/B FLAP I/B AFT HINGE I/B PIVOT I/B SPOTFACE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-52-04 REV 61. 2 L 7 3 4F RT A22WE 20081022 NM 2008 10 22 DHLA2008745522 1 20081012 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 FUSE SKIN EXISTING REPAIR AT BS 367 TO 377, STR 10R TO 12R, IS CORRODED. REMOVED EXISTING REPAIR, FABRICATED NEW REPAIR , AND INSTALLED AS REQUIRED IAW BOEING SB 727-53-0136 REV 3, PART III, METHOD 1, FIG 6. REF N/R 5252-2-432. 2 L 7 3 4F A3WE 20081022 EA 2008 10 22 ASOA200801216 1 20080926 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED AND REPLACED PASSENGER DOOR EXIT, TO OPEN, OPEN, RED ARROW AND RED STRIPE PLACARDS IAW CRJ 200 AMM 11-30-00-400- 801. SUPPLEMENTAL SDR CLOSED 10/15/08. 2 L 7 2 4F RT A21EA 20081022 SO 2008 10 22 FDKA2008101400271 1 20081014 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN DAMAGED A FDKA K NONE L NO TEST IN INSP/MAINT 1 SW 07 827MJ 145217 FRL FLT 6220 IAD-RON. FLOOR EMERGENCY LIGHTS BY THE OVERWING EXITS WERE INOPERATIVE. MX RESOLDERED THE WIRES BACK INTO THE LIGHT AND OPS CHECKED. 2 L 7 2 4T RT T00011AT 20081022 CE 2008 10 22 YADA101408 1 20081014 A 5210 SHAFT BCRAFT BEECH 1900 1900C 1154161 CE PAX DOOR BROKEN E YADA K NONE O OTHER TX TAXI/GRND HDL 1 AL 03 112AX 948 8832 UC45 PILOT COULD NOT OPEN THE FORWARD PASSENGER/CREW DOOR FROM THE INSIDE, HANDLE WAS BROKEN (DOOR SEEMED FROZEN). 2 L 7 2 4T RT A24CE 20081022 NM 2008 10 22 DHLA200800114 1 20081016 A 3230 656021132 ACCESSORY UNIT BOEING 727 727264 138408M NM PWA JT8 JT8D NE LANDING GEAR FAILED A DHLA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 GL 05 764AT 5042 3318 22984 ON CLIMBOUT AT 300KIAS PASSING FL200 RED DOORS LIGHT ON FWD PANEL & NOSE GEAR DOOR LIGHT ON S/O'S PANEL ILLUMINATED. FE LT HEAVY VIBRATION PERFORMED ABNORMAL PROCEDURE AFTER SLOWING TO 260KTS LIGHT WENT OUT /VIBRATION REMAINED. MX INSTRUCT ED, CYCLE GEAR UPON RETRACTION GEAR RETRACTED BUT L/R GEAR DOOR LIGHTS ILLUMINATED ON FWD S/O'S PANEL HEAVY VIBRATION, P ERFORMED ABNORMAL PROCEDURE LIGHTS OUT. RESOLUTION DESCRIPTION: REMOVED AND REPLACED LANDING GEAR ASSY UNIT GROUND FUN CTION OK CHECK FOUND TO BE SERVICEABLE IAW MM 32-09-121. 2 L 7 3 4F 4 F A3WE E2EA 20081022 SO 2008 10 22 FDKA2008101400272 1 20081014 A 5210 DOOR EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 849MJ 145534 FRL FLT 6197 BNA. PASSENGER DOOR HARD TO OPEN. MX LUBED THE DOOR. 2 L 7 2 4T RT T00011AT 20081022 SO 2008 10 22 FDKA2008101500273 1 20081015 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM FLT 8919 TYS-CVG. AFT CEILING EMERGENCY LIGHT INOPERATIVE. MX RESECURED CONNECTOR. 2 L 7 2 4T RT T00011AT 20081022 EA 2008 10 22 MASA2008101300724 1 20081013 A 3234 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 SW 07 27191 18256 7191 ASH FLT 7131 CAK-RON. EMERGENCY DECLARED DUE TO GEAR DISAGREE MESSAGE DURING APPROACH. AIRCRAFT FERRIED TO CAE WHERE M X REMOVED AND REPLACED NLG DOOR SELECTOR VALVE AND NLG RETRACT ACTUATOR. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 MASA2008101400726 1 20081014 A 3350 BATTERY CNDAIR CL600 CL6002D24 1390016 EA CABIN DISCHARGED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 926LR 15026 ASH FLT 2650 CLT-ILM. EMERGENCY LIGHTS IN CABIN INOPERATIVE. MX CHARGED LIGHTS. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 MASA2008101400727 1 20081014 A 5240 SEAL CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR UNKNOWN A MASA K NONE O OTHER CR CRUISE 1 SW 07 37342 7342 ASH FLT 1019 HNL-RON. SERVICE DOOR SQUEALING IN FLIGHT. MX REMOVED AND REPLACED SERVICE DOOR SEAL. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 MASA2008101500728 1 20081015 A 5210 SEAL CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A MASA K NONE O OTHER CR CRUISE 1 SW 07 47202 7202 ASH FLT 7295 FWA-ORD. PASSENGER DOOR SQUEAL ENTIRE FLIGHT, NO PAX DOOR MESSAGES OR PRESSURIZATION DISCREPANCIES. MX RE PAIRED DOOR SEAL. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 MASA2008101500729 1 20081015 A 2560 GLOWSTRIP CNDAIR CL600 CL6002D24 1390016 EA CABIN LOOSE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 903FJ 15003 ASH FLT 2777 PHX-BFL. EMERGENCY PHOTOLUMINESCENT PATH STRIP ROW 1-2 LOOSE. MX REPLACED THE PATH STRIP. 2 L 7 2 4F RT A21EA 20081022 NM 2008 10 22 HNAA2008101600312 1 20081008 A 3260 841005 PSEU DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAULTED A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 839EX 37512 226 UPON TAKEOFF LANDING GEAR WARNING HORN SOUNDED FOLLOWED BY THREE RED LANDING GEAR UNSAFE LIGHTS. ABORTED TAKEOFF, PERFO RMED PSEU BITE TEST, PSEU MEMORY RECALL CODES 45 AND 54 WERE RETRIVED.(45 "NOSE WHEEL STEERING" AND 54 "PSEU DRIVER CARD 1A"). REMOVED AND REPLACED PSEU IAW 32-61-50, PERFORMED GEAR SWING IAW 32-30-00. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 20081022 NM 2008 10 22 ABXA200810160252 1 20080930 A 2742 251T43101 JACKSCREW BOEING 767 767281 1385109 NM HORIZ STAB DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 47998 23143 HORIZONTAL STAB BALL SCREW INSPECTION FAILED IAW J/C 27-030-01. REPLACED HORIZONTAL STABILIZER ACTUATOR. STAB TRIM ACT UATOR ASSY SENT OUT ON R/O 501586374 TO REPAIR VENDOR DELTA AIRLINES INC. REASON FOR REMOVAL STATED AS JACKSCREW PITTED . UNIT WAS EXCHANGED. 2 L 7 2 4F RT A1NM 20081022 SO 2008 10 22 CHQA200800198 1 20081013 A 3350 78241 BATTERY EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CABIN DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 283SK 145424 CAE312071 FLIGHT 5910, IAH TO STL. DURING TEST THE GREEN FLOOR LEVEL EMERGENCY LIGHTS BETWEEN ROWS ONE AND SEVEN WERE NOT ILLUMIN ATING. MAINTENANCE REPLACED THE NR 2 BATTERY POWER SUPPLY AND THE EMERGENCY LIGHTS OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081022 SO 2008 10 22 RAIA2008101600001 1 20081014 A 2150 8152403 ACM EMB 145 EMB145 3260210 SO NR 2 MALFUNCTIONED A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 801HK 22478 11844 145053 CREW REPORTED THAT THE NR 2 AIR CONDITIONING PACK WAS CAUSING SMOKE. MAINTENANCE REMOVED AND REPLACED THE NR 2 AIR CYCL E MACHINE. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 20081016 NE 2008 10 16 DL76S081236 2 20080926 A 7200 CF680A2 ENGINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 MAKING METAL A DALA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 131DN 46481 24852 580398 NR 2 ENGINE OIL PRESSURE WENT TO ZERO, HEARD AUDIBLE STALL. CREW SHUT OFF FUEL LEVER. MTC FOUND METAL IN THE TAIL PIPE . NR 2 ENG REPLACED PER TRANS 1T145. 2 L 7 2 4F 4 F RT A1NM E13NE 20081016 NM 2008 10 16 DLM8K081240 1 20080926 A 5532 5912123511 SKIN DOUG MD88 MD88 3023688 NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 912DE 49997 VERTICAL STABILIZER LT IN SPAR SKIN, SKIN STRAP, FWD SPAR CHORD, AND FWD SPAR WEB FOUND CRACKED. CUT OUT DAMAGE AND INS TALLED REPAIRS. 2 L 7 2 4F RT A6WE 20081029 EU 2008 10 29 08FDEA04543 1 20081025 A 7830 491B131300170 FRAME AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 668FE 772 NR 1 ENG INBD T/R FWD FLANGE FOR MOUNTING RING LATCH ASSY HAS 2 INCH CRACK AT 12 O'CLOCK POS REMOVED CRACK AND REPAIRED NR 1 ENG INBD T/R FWD FLANGE IAW FEDEX EA 6-7830-124133, RELEASE DATE 8 OCTOBER, 2008. 2 L 7 2 4F RT A35EU 20081029 NM 2008 10 29 08FDEA04544 1 20081025 A 5311 6516349144 FRAME BOEING 727 7272D4 138407U NM ZONE 200 WORN A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 FUSELAGE UPPER LOBE INTERIOR STRUCTURE, FRAME 1166 SCRATCHED RBL 68 AT STR R11- R12 BLENDED DAMAGE REF SRM 53-10-1 PG 1 -2A, OUT OF LIMITS, HEAT TREATED NEW REPAIR. REMOVED DAMAGE REF SRM 51-40-3 PG 1-6. TREATED AND PRIMED REPAIR REF SRM 51-20-13 AND 51-20-21. FABRICATED NEW STRINGER CLIP REF DWG 66-15883 ITEM 1, TREATED AND PRIMED CLIP SRM 51-20-13 AND 5 1-20-21. INSTALLED REPAIR AND STRINGER CLIP REF SRM 51-30-2 PG 2-14. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 08FDEA04545 1 20081025 A 5311 651634786 FRAME BOEING 727 7272D4 138407U NM ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 AFT PIT BS 1130 FRAME UPPER CHORD HAS DOUBLE DRILLLED HOLE IB OF TIE DOWN FITTING AT S27L. REMOVED AND INSTALLED FLOOR SUPPORT BRACKET, TIE DOWN BRACKET, FLOOR SUPPORT REF 51-30-2. REPAIRED DAMAGED FRAME REF SRM 51-40-3 FIG 1. TREATED AND PRIMED REF SRM 51-10-2 THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 08FDEA04547 1 20081025 A 5311 651634570 FRAME BOEING 727 7272D4 138407U NM ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 AFT PIT BS 1090 FRAME HAS DOUBLE DRILLED HOLE INBD OF TIEDOWN FITTING AT S27R. REPAIRED IAW SRM 51-40-3. FABRCATED BRA CKET IAW DWG 69-44106 TREATED, PRIMED IAW SRM 51-10-2. THIS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 CALA0800986 1 20081023 A 5320 65C3397011 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 INTERCOSTAL BETWEEN STATIONS 344 TO 360 BL 0 CRACKED AROUND FASTENER HOLES. REPAIRED DAMAGE TO INTERCOSTAL BETWEEN STAT ION 344 TO 360, BL 0 PER B-737-500 SRM 51-70-11 AND 51-10-02. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 2008UALA06228 1 20081021 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 AFT CARGO COMPT FRAME AT BS 1580 AND STR 26R HAS 2 DENTS AT FRAME INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT D AMAGED FRAME SECTION AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 2008UALA06229 1 20081021 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 FWD PIT AT STA 600, STR 23L FRAME DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 DL757081403 1 20081017 A 5330 SKIN BOEING 757 757232 1384965 NM FS 1738 S26-27L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 DENT FROM INSIDE OUT STA 1738 BETWEEN STRINGERS 26L-27L. REPAIRED ON CUST CARD 00153. 2 L 7 2 4F RT A2NM 20081029 2008 10 29 DL76L081394 4 20081021 A 8300 NOZZLE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE GEARBOX FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 181DN 61255 25986 724415 NR 1 ENG FAILED INSPECTION OF MAIN GEARBOX OIL NOZZLES PER EA-51470869-12. C/W EA 51-470869-12 FOUND CONTAMINATES IN BO TH NOZZLES. REQUIRES ENG CHG. REPLACED NR 1 ENG PER R/C TRANSMITTAL 23-. 2 L 7 2 4F 4 F RT A1NM E24NE 20081029 NM 2008 10 29 2008UALA06241 1 20081020 A 3397 362624 CONNECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 348UA 24252 EMERGENCY EXIT FLOOR LIGHTING AT AFT TWO ROWS LOOSE. TROUBLESHOT AND RE-SECURED LOOSE CONNECTION ON EMERGENCY LIGHT STR IP. ALL OPS NORMAL. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081029 NM 2008 10 29 2008UALA06243 1 20081022 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 AFT PIT BS 1420LT, STR 24L, FRAME INBOARD FLANGE DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME A ND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 DL75E081405 1 20081022 A 2750 FLAP SYSTEM BOEING 757 7572Q8 1384972 NM TE FLAPS MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 712TW 27624 T/E FLAP DISAGREE ON FLAP EXTEND 0 DEG TO 5 DEG. PERFORMED VISUAL INSPECTION OF FLAPS AND DRIVE UNITS. NO DEFECTS NOTE D PERFORMED BITE CHECK. NO FAULTS FOUND PER AMM. NO HISTORY. 2 L 7 2 4F RT A2NM 20081029 EA 2008 10 29 SWIA200820182 1 20080612 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 912SW 7595 C-CHECK, UPPER FLANGE FS280 FLOORBEAM AT RBL12 CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 SWIA200820183 1 20080612 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 625 S14L CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 912SW 7595 C-CHECK, INTERCOSTAL ATTACH CLIP CRACKED AT FS 625 LEFT STRINGER 14. REPLACED CLIP PER REO. 2 L 7 2 4F RT A21EA 20081029 EU 2008 10 29 UPS08153716 1 20081013 A 5753 A5796030620000 SKIN AIRBUS A300 A300F4622R 3930360 EU TE FLAP CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 140UP 0823 INSPECTION TYPE:1C3C LT WING CENTER FLAP UPPER MID SECTION REPAIR DOUBLER CHAFED. REMOVED, FABRICATED AND INSTALLED REP AIR DOUBLER ON LT WING CENTER FLAP UPPER MID SECTION REF A300-600 SRM 57-50-00 FIG 205 AND SRM 57-50-00. 2 L 7 2 4F RT A35EU 20081029 EA 2008 10 29 SWIA200820184 1 20080612 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 625 S14R CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 912SW 7595 INTERCOSTAL ATTACH CLIP CRACKED AT FS 625 RIGHT STRINGER 14. C-CHECK, REPLACED CLIP PER REO. 2 L 7 2 4F RT A21EA 20081029 NM 2008 10 29 UPS08M53718 1 20081016 A 5712 ARB7774U52 RIB DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:1C DURING OK TO INSTALL RT WING LOWER WINGLET FOUND CRACK ON RIB. REMOVED AND REPLACED RIB IAW SRM, 51- 35-01, 51-33-01 VOL 2 PG 37 TABLE 12. 2 L 7 3 4F RT A22WE 20081029 EA 2008 10 29 SWIA200820185 1 20081015 A 5753 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA TE FLAP DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710SK 10170 FLT 6204 - DAMAGE FOUND DURING BURST/FLAT TIRE INSPECTION, TRAILING EDGE OF RIGHT INBOARD FLAP HAS DENT. INSTALLED NEW RIGHT INBOARD FLAP, PN CC670-14002-8, SN ON:15049, SN OFF: 10173. 2 L 7 2 4F RT A21EA 20081029 WP 2008 10 29 AALA200802262 1 20080903 A 2150 ACM DOUG DC9 DC982 3022082 WP LEFT FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 70401 49312 CREW REPORTED LT AIR CONDITIONING PACK LOW FLOW INDICATION AND ZERO PRESSURIZATION. RT PACK INOPERATIVE. RETURNED TO D EPARTURE AND LANDED WITHOUT INCIDENT. REPLACED LT AND RT AIR CYCLE MACHINE (ACM). SYSTEM GROUND CHECKED NORMAL OPERATI ON. 2 L 7 2 4F A6WE 20081029 EA 2008 10 29 SWIA200820217 1 20080624 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 772SK 10235 FS 280 FLOORBEAM CRACKED. C-CHECK, REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 SWIA200820219 1 20080624 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 772SK 10235 COCKPIT FLOORBEAM IS CORRODED AND CRACKED. C-CHECK, REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20081029 NM 2008 10 29 UPS08M53719 1 20081007 A 5753 INTERCOSTAL DOUG MD11 MD11F 3023600 NM TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:1C LT I/B FLAP O/B HINGE INTERCOSTAL FOUND CRACKED JUST ABOVE O/B ACTUATOR UPPER ATTACHMENT. REMOVED AN D REPLACED INTERCOSTAL IAW, SRM 51-31-01 VOL 2 PG 1, 51-21- 01 VOL 2 PG 20. 2 L 7 3 4F RT A22WE 20081029 EA 2008 10 29 SWIA200820220 1 20080624 A 5340 BRACKET CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 772SK 10235 FS 280 RT OUTBOARD INTERCOSTAL BRACKET CRACKED. C-CHECK, REPLACED. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 SWIA200820221 1 20080624 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 772SK 10235 FS 280 FLOORBEAM CRACKED RBL 9.0. C-CHECK, REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20081028 NM 2008 10 28 ASAA0873647 1 20081003 A 5320 147A57125 PAN BOEING 737 737790 13844CN NM FUSELAGE PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 AFT PASSENGER CABIN PUNCTURE IN FLOOR PAN BS 1019 LBL 16. PUNCTURE IN FLOOR PAN BS 1019 LBL 16 REPAIRED IAW ASA EA 5310 02828. 2 L 7 2 4F RT A16WE 20081028 EU 2008 10 28 MALA080180 1 20081002 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 340B428 LT INBOARD FLOOR TRACK HAS CORROSION BETWEEN STA 319 AND STA 363. REPAIRED IAW EO S53627. 2 L 7 2 4T RT A52EU 20081028 EU 2008 10 28 MALA080181 1 20081002 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 340B428 SEAT TRACK HAS CORROSION LBL 18.3 FROM STA 521 AND STA 686.888. REPAIRED IAW EO S53060. 2 L 7 2 4T RT A52EU 20081028 EA 2008 10 28 ASOA200801286 1 20081003 A 5320 POST CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 FS 559, LBL 9 POST (OUTBOARD) WAS REPLACED ON FS 559 REPAIR REO 601R-53-41-260 JOB 8752815, OP 68. SUPPLEMENTAL SDR CLO SED 10/21/08. 2 L 7 2 4F RT A21EA 20081028 NM 2008 10 28 ASAA0843661 1 20081008 A 5755 SKIN BOEING 737 7374Q8 138447Q NM NR 1 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 LEFT WING NR 1 SPOILER LOWER SURFACE HAS MULTIPLE DENTS. PREPPED REPAIR AREA, FABBED REPAIR PARTS & BONDED THE REPAIR I AW B737 400 SRM 51 70 10 REP 4. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085745 1 20081021 A 3350 6574550 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 409WN 27896 DURING SCHEDULED MV2 CHECK, FOUND FWD BULLNOSE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 2008UALA06175 1 20081017 A 5753 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAP DEBONDED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 LEFT WING INBOARD FWD FLAP OUTBOARD END UPPER SKIN DISBONDED DOUBLER. REMOVED PREVIOUS REPAIR. BONDED ON NEW DOUBLER R EF REO G12468 REV B. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 AALA200802495 1 20080926 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM BS 947 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 TUL CORROSION ON UPPER SURFACE OF FLOORBEAM BEYOND LIMITS. REPAIRED PER ESO 61000 DATED 22 SEP 08. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 USAA920081869 1 20081012 A 5347 69414372 STRINGER CLIP BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03C20053004/003 STRINGER CLIP CRACKED AT BS 663, 10R. REPLACED STRINGER CLIP AT BS663, 10R IAW S RM 51-10-02. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 USAA920081878 1 20080919 A 5311 6546532 FRAME BOEING 737 7373G7 138447J NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN C18 MAJOR REPAIR NR 6131828 FRAME CRACKED AT BS 480 BETWEEN S8L AND S9L. REPAIRED FRAME AT BS 480, BETWEEN S8L AND S9L. IAW TASK CARD NR M1C53002. 2 L 7 2 4F RT A16WE 20081029 2008 10 29 2008UALA06226 4 20081021 A 2565 S416T203153 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 642UA 25092 LT OVERWING SLIDE IS FAULTY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081029 NM 2008 10 29 2008UALA06214 1 20081019 A 3610 32153024 SHUTOFF VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE BLEED AIR SYS FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 219UA 30551 RT HIGH PRESSURE SHUTOFF VALVE FAILED. HPSOV FAILED. REPLACED WITH NEW VALVE. OP TESTS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081029 NM 2008 10 29 CALA0800987 1 20081023 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 BODY STATION 827L FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. CUT OUT DAMAGE ON FRAME AT BODY STATION 827L BETWEEN S-8 AND S9. FABRICATED REPAIR PARTS AND INSTALLED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 08FDEA04498 1 20081023 A 5340 69445595 ATTACH FITTING BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 AFT LOWER CARGO PIT STA 950E STR 29L ATTACH FITTING CORRODED ON LEFT SIDE. REMOVED ATTACH FITTING REF SRM 51-30-2 PG 32 , MATCH DRILLED NEW ATTACH FITTING REF SRM 51-30-5, INSTALLED NEW ATTACH FITTING REF SRM 51-30-2 PG 2-12 THIS IS CLASS IFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081029 EU 2008 10 29 08FDEA04500 1 20081023 A 5347 A53274005200 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 668FE 772 MDCC SEAT TRACK (Y1959) LT NR 5 AT FRAME 30 HAS 1 ELONGATED SCALLOP. REPAIRED SEAT TRACK (Y1959) LT NR 5 AT FRAME 30 BY USING SPLICE FROM FRAME 27 TO BETWEEN FR 32 AND 33 IAW A300-600 FREIGHTER SRM 53-10-16 FIG 201A PGS 203-208. 2 L 7 2 4F RT A35EU 20081029 EU 2008 10 29 08FDEA04501 1 20081023 A 5347 A53781932202 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 668FE 772 FUSELAGE AUXILIARY STRUCTURES, 2 WORN LOBES ON SEAT TRACK Y2462 RT AT FRAME 20. REMOVED DAMAGED SEAT TRACK SECTION FROM BETWEEN FRAMES 18/19 TO BETWEEN FRAME 27/28 AND REPLACED IAW SRM 53-13-16 CONFIG 2 ITEM 40 AND EA6-5320-105302C PT3. 2 L 7 2 4F RT A35EU 20081029 EU 2008 10 29 08FDEA04502 1 20081023 A 5347 A5381313020000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 THE EXPANSION SEAT TRACK BETWEEN FRAME 54 AND 54.2, RBL 90 IS CRACKED LOCATED; DRILLED AND INSTALLED SEAT TRACK P/N A538 1313020000; S/N 758464 IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20081029 NM 2008 10 29 2008UALA06231 1 20081022 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 783UA 26950 EEL LIGHT MISSING ON SEAT 1E. DISCOVERED LIGHT MISSING. REPLACED MISSING EEL LIGHT ASSEMBLY, TESTS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081029 WP 2008 10 29 08FDEA04503 1 20081023 A 5320 NEA608121 ATTACH FITTING DOUG MD10 MD1010F 3022112 WP BS 1521 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 THE INTERCOSTAL ATTACH FITTING FWD OF BS 1521 IN THE RIGHT WHEEL WELL, OTBD SIDE IS CORRODED ON THE BACK SIDE. REMOV ED ATTACH FITTING IAW SRM 51-35-01. REMOVED CORROSION IAW SRM 51-21-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01. FABBED IAW DWG NEA 6081. ALODINED & PRIMIED IAW SRM 51-21-01. INSTALLED IAW SRM 51-33-01. 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 2008UALA06234 1 20081022 A 5210 PLATE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 820UA 898 DOOR 2 RIGHT SILL PLATE AT GIRT HOOK 4 EA ATTACH HOLES HAVE CORROSION. REMOVED SILL PLATE FOR REPLACEMENT. 2 L 7 2 4F 4 F RT A28NM E40NE 20081029 WP 2008 10 29 08FDEA04508 1 20081023 A 5751 ARC13163 SKIN DOUG MD10 MD1010F 3022112 WP LT AILERON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 LT WING INBD AILERON INBD LOWER NOSE PANEL IS CHAFED. BLENDED OUT DAMAGE. FOUND OUT OF LIMITS IAW SRM 57-00-01. FABR ICATED NEW SKIN PANEL IAW IAW DWG ARC 1316. ALODINED & PRIMED IAW SRM 51-21-01. PAINTED IAW SRM 51-21-01. INSTALLED I AW DWG ARC 1316 & SRM 51-35-01. PART MARKED IAW GMM 7-0-1000. 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 2008UALA06236 1 20081022 A 5210 PLATE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 820UA 898 DOOR 2 RIGHT AFT SHEAR PLATE HAS CORROSION. MAJOR REPAIR ACCOMPLISHED REMOVED SHEAR PLATE. REPLACED SHEAR PLATE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081016 NM 2008 10 16 08FDEA04232 1 20081006 A 5414 311N504631 SKIN PANEL BOEING 757 757236 1384971 NM NR 1 NACELLE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 NR 1 PYLON LT SKIN, INNERWALL IS CORRODED JUST FWD OF PRE-COOLER. REMOVED AND REPLACED LT SKIN PANEL ASSY IAW SRM 51-40- 02 AND DRAWING 311N5002 AND EA F-5450-121408. CORROSION WAS DETERMINED TO BE OUT OF LIMITS IAW SRM 54-50-01. THIS REPA IR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING REQUIRED. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 08FDEA04234 1 20081006 A 5414 311N51931 SKIN PANEL BOEING 757 757236 1384971 NM NR 2 NACELLE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 NR 2 PYLON I/B FWD SKIN PANEL ASSY, HAS CORROSION ON INNER AND OUTER SURFACE. REMOVED AND REPLACED NR 2 PYLON I/B FWD SK IN PANEL ASSY IAW SRM 51-40-02 AND DRAWING 311N5002. CORROSION DETERMINED TO BE OUT OF LIMITS IAW SRM 54-50-01. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING REQUIREMENTS. 2 L 7 2 4F RT A2NM 20081016 NM 2008 10 16 DL76L081307 1 20081006 A 5420 311T31571 TEE FITTING BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 174DN 24802 THE CLOSEOUT TEE AT THE MIDSPAR FITTING AT THE NR 2 PYLON WAS FOUND CRACKED. THE PART WAS REPLACED PER ER/A 01-452215-1 4. 2 L 7 2 4F RT A1NM 20081016 NM 2008 10 16 SWAA085461 1 20081008 A 5311 6546543 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 706, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085462 1 20081008 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085463 1 20081009 A 3233 65448106 ACTUATOR BOEING 737 7373H4 1384600 NM LT MLG FAULTY A SWAA K NONE O OTHER AP APPROACH 1 SW 29 312SW 23334 DURING APPROACH LT MLG WOULD NOT INDICATE DOWN, RETRACTED GEAR, DID MANUAL EXTENSION GEAR DOWN, INDICATION NORMAL. REMO VED AND REPLACED MLG UPLOCK ACTUATOR AND PRIORITY MODULAR VALVE PER MM. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085533 1 20081013 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8R. REPAIRED PER SWA EA. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085468 1 20081008 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081016 NM 2008 10 16 SWAA085469 1 20081008 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 2008UALA06052 1 20081009 A 2421 1701768 GENERATOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE RIGHT FAULTY A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 791UA 26933 RIGHT BUG LOW OIL PRESS MSG, LEAKING. FOUND OIL LEAKING FROM DRAIN 3 AT A RUNNING STREAM ON 1ST ENG RUN. STARTED RT ENG A 2NDTIME OIL LEAKING AT 12 DROPS A MINUTE FROM DRAIN 3. REPLACED RT BACKUP GENERATOR. ALL CHECKS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081017 NM 2008 10 17 08FDEA04323 1 20081013 A 5744 ARC050311 HINGE FITTING DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 LEFT HAND WING: OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) ACTUATOR HOLE OUTBOARD BORE HOLE FOUND WITH CORROSION. CORRO SION REMOVED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. REPAIR CARRIED OUT AS PER EA 1-5750-122591, THIS REPAIR CLA SSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 DL757081309 1 20081006 A 5320 284N17302 SUPPORT BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION ON SIDEWALL SUPPORT AT STATION 1463 RBL 20. REPAIRED PER 51-40-02 ON NR 00044. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 DL76L081310 1 20081006 A 5420 311T31571 ANGLE BOEING 767 767332 1382001 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 185DN 27961 THE NR 2 PYLON MIDSPAR CLOSEOUT ANGLE WAS FOUND CRACKED. ER/A 01-457169-14AD AUTHORIZES REPLACEMENT OF THE CLOSEOUT ANG LE AND PERFORMS ADDITIONAL INSPECTIONS OF THE MIDSPAR FITTINGS. 2 L 7 2 4F RT A1NM 20081017 NM 2008 10 17 DL757081318 1 20081006 A 5315 146N54462 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION ON FLOORBEAM AT STATION 1510 AT RBL 3. REPAIRED ON NR 00062 PER SRM 53-60-53. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 DL757081328 1 20081006 A 5315 146N544714 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 615DL 22822 CORROSION ON FLOORBEAM STATION 1470 RBL 3. REPAIRED ON NR 00053 PER 51-40-07 FIGURE 1. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 08FDEA04235 1 20081006 A 5347 6941211 SEAT TRACK BOEING 727 727227 1384078 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 485FE 21488 TRACK AT STA 870 TO 890 RBL 24 IS CORRODED. REMOVED CORROSION ORIGINAL MATERIAL THICKNESS .100 MATERIAL LOSS .026 REMAI NING .074 OUT OF LIMITS. FABRICATED, TREATED, AND PRIMED SEAT TRACK SECTION STA 870-890 RBL 24 SEAT TRACK SECTION TO BE INSTALLED ON N/R 00782 REF SRM 53-10-0 P16, 51-10-2P7, DWG 69-04121, THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 2008UALA06237 1 20081022 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 340UA 24244 AFT SECTION OF EMERGENCY LIGHTS INOP. REPLACED LIGHT ASSEMBLY OP CHECKED GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081029 NM 2008 10 29 2008UALA06239 1 20081022 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 CRACK ON FRAME, FWD OF R-2 DOOR CUTOUT, BS 665, STR. 12R. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED WEB AND INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 2008UALA06240 1 20081021 A 7740 H150AKM1 INDICATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT NO TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 595UA 28748 STANDBY ENGINE INDICATOR (SEI) WILL NOT BITE TEST. REPLACED SEI. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 DL757081399 1 20081021 A 5321 146N539113 FLOOR SUPPORT BOEING 757 757232 1384965 NM BS 1510-1530 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 CORROSION ON FLOOR SIDEWALL SUPPORT BS 1510 TO BS 1530 LBL 19. REPAIRED ON NR 00042 PER 51-40. 2 L 7 2 4F RT A2NM 20081029 NM 2008 10 29 UPS08M53720 1 20081006 A 5720 SB115700635 FITTING DOUG MD11 MD11F 3023600 NM RT WINGLET CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 279UP 48573 INSPECTION TYPE:C RT WING LOWER WINGLET AFT FITTING FOUND CRACKED. RT WING LOWER WINGLET AFT FITTING REPLACED AS PER EO MD11-5720-27 680-A, APPENDIX E. 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 AALA200802597 1 20080922 A 5311 FRAME BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CRACK FOUND ON FRAME AT RIGHT STATION 380 AND STRINGER 8. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH ECO J1159AA. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802599 1 20080922 A 5311 FRAME BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CRACK FOUND ON FRAME AT RIGHT STATION 440 BETWEEN STRINGERS 8 AND 9. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH ECO J1 159AA. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802600 1 20080922 A 5311 FRAME BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CRACK FOUND ON FRAME AT RIGHT STATION 480 BETWEEN STRINGER 8 AND 9. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH ECO J11 59AA. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802601 1 20080918 A 5343 115A52119 TRUNNION BOEING 737 737823 13844CB NM ZONE 700 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION FOUND ON LEFT FORWARD MAIN LANDING GEAR TRUNNION BUSHINGS. DEPTH OF DISCREPANCY IS .076 INCH. REPAIRED AREA AND INSTALLED NEW BUSHINGS IN ACCORDANCE WITH SRM 57-20-90-R22. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802602 1 20080915 A 5320 141A541016 INTERCOSTAL BOEING 737 737823 13844BZ NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CRACK FOUND AT CLIP NUT HOLES ON INTERCOSTAL AT STATION 294.5 AND BUTTLINE 0. AREA OF DISCREPANCY IS 1 INCH BY 1 INCH. CRACK LENGTH IS .5. REPLACED INTERCOSTAL AT STATION 277 TO 294.5 IN ACCORDANCE WITH SRM 53 10 00. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802603 1 20080917 A 5743 115A50025 TRUNNION BOEING 737 737823 13844CB NM ZONE 700 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION FOUND ON LEFT MAIN LANDING GEAR TRUNNION AT UPPER OUTBOARD HOLE OUTER FACE. AREA OF DISCREPANCY IS .076 BY 3 INCHES DIAMETER WITH A DEPTH OF .076. REPAIRED FASTENER HOLES IN ACCORDANCE WITH SRM 57-20-90-R22. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802608 1 20080924 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM ZONE 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION FOUND ON FLOORBEAM AT STATION 986.5 AT RIGHT BUTTLINE 29.5. REMOVED CORROSION AND REPAIRED PER SRM 53-70-51 A ND 53-00-51 2R. 2 L 7 2 4F RT A16WE 20081029 EA 2008 10 29 SWIA200820209 1 20081019 A 2150 A/C PACK CNDAIR CL600 CL6002B19 1900309 EA LEFT OVERHEATED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 909SW 7558 FLT 6695 - LEFT PACK "HI TEMP" CAUTION ON ECS PAGE AND BURNING ODOR NOTED IN AIRCRAFT. REPLACED LEFT PACK AND LEFT PACK RAM AIR CHECK VALVE. 2 L 7 2 4F RT A21EA 20081029 NM 2008 10 29 AALA200802609 1 20080928 A 5320 WEB BOEING 737 737823 13844CB NM ZONE 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION FOUND ON WEB AND FLOOR SUPPORT IN AFT GALLEY. AREA OF DISCREPANCY IS 2 INCHES BY 4 INCHES. REPAIRED WEB AND REPLACED FLOOR SUPPORT IN ACCORDANCE WITH SRM 51-70-13 2R. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 DHLA2008745557 1 20080911 A 5753 69207621 SUPPORT FITTING BOEING 727 727224 1384076 NM LT WING TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LT WING INBD MID FLAP WBL 129.2 RIB SUPPORT FITTING CRACKED AT FWD LOWER SECTION. REPLACED LT WING INBD MID FLAP SUPPOR T FITTING AT FWD LOWER SECTION WBL 129.2 IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 DHLA2008745558 1 20080905 A 5753 STRAP BOEING 727 727224 1384076 NM RT WING TE FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 RT WING INBD MID FLAP INBD SECTION STRAP WITH CORROSION AT WBL 116. REPLACED STRAP IAW SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 AALA200802610 1 20080930 A 5320 WEB BOEING 737 737823 13844CB NM ZONE 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION FOUND ON UPPER SURFACE OF WEB AT STATION 988. INSTALLED DOUBLER REPAIR TO WEB IN ACCORDANCE WITH SRM 51-70-13 . 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802611 1 20080924 A 5347 CARGO TRACK BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION FOUND ON AFT CARGO TRACK AT STATION 787 RIGHT BUTTLINE 13.84. SPLICED IN NEW CARGO TRACK SECTION IN ACCORDANC E WITH SRM 53-00-53-22 REPAIR 3. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802613 1 20080918 A 5210 SKIN BOEING 737 737823 13844CB NM PAX DOOR BULGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 FOUND AFT ENTRY DOOR OUTER SKIN LOWER FORWARD CORNER BULGED OUT. AREA OF DISCREPANCY WAS 1.5 INCHES BY 2 INCHES. REMOV ED DAMAGED AREA AND INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH SRM 52 00 01 2R. 2 L 7 2 4F RT A16WE 20081029 EA 2008 10 29 SWIA200820214 1 20081021 A 5240 SEAL CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BINDING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 954SW 7815 FLT 6549 - SERVICE DOOR WILL NOT OPEN FROM THE OUTSIDE, HANDLE WILL NOT ROTATE. REPLACED SERVICE DOOR SEAL. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 SWIA200820215 1 20081015 A 2170 LINE CNDAIR CL600 CL6002B19 1900309 EA RT A/C PACK FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 910EV 7727 FLT 3766 - AT 300 AGL RECEIVED "SMOKE TOILET" CAUTION MESSAGE. FOUND OVERBOARD DRAIN RESTRICTOR LINE ON RIGHT PACK CAUS ING LARGE BLEED AIR LEAK INTO APU BAY. RAN RIGHT ENGINE AND PACK, NO SMOKE NOTED. REPLACED DRAIN RESTRICTOR LINE. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 SWIA200820216 1 20081018 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 507CA 7796 FLT 2720 - NR 3 CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081029 WP 2008 10 29 UPS08853599 1 20080929 A 5320 CUSP WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV REMOVE AND REPLACE WITH SRM REPAIR. EFN 8941997-55. ORIGINAL N/R 5 34204 LEFT CUSP MEMBRANE CRACKED AT LBL 45 BETWEEN FS 1580-1600. REMOVED DOUBLER VERIFIED CRACK STOP DRILLED IAW SRM 53-02-00-0. REINSTALLED DOUBLER A ND VERIFIED REPAIR COMPLIES WITH DC-8 SRM 53-02-00-0 FIG 23. 2 L 7 4 4F RT 4A25 20081029 WP 2008 10 29 UPS08853635 1 20080921 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV EVALUATION AND DISPOSITION REPAIR EFN 89419971107 ORIGINAL NRC 534711 R1 DOOR FORWARD DOOR JAB (FUSEL AGE FRAME) REPAIR FOR ELONGATED HOLES. FABRICATED NEW INTERCOSTAL PER DAC DWG 561575700 REV EC, FABRICATED NEW FRAME DO UBLERS AND INSTALLED PER UPS DWG DC8 -53A001 REV A, EO DC8 5310-111728 B. 2 L 7 4 4F RT 4A25 20081029 NM 2008 10 29 UPS08M53723 1 20081025 A 5730 SKIN DOUG MD11 MD11F 3023600 NM LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:1C LEFT WING FIXED LEADING EDGE HAS SKIN DAMAGE. REF D-370970 AND EO MD11-5730-2877-B EXTENDED EXISTING TRIMOUT PER SAA EA 011-5730-01-A1540. HFEC NO CRACKS NOTED, PER NDTSPM 06-10-01.001. FABRICATED AND INSTALLED WEB RIB P/N AR B2875-5SAAU IAW DRWG ARB2875, SAA EA 011-5730-01-A1540 AND SRM 51-33-01, 51-31-01. 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 UPS08M53721 1 20081023 A 3350 SWITCH DOUG MD11 MD11F 3023600 NM COCKPIT FAULTY A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 250UP 48745 INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT TEST. REPLACED EMERGENCY LIGHT TEST SWITCH PER WDM 33-51-01. SWITCH 1-40 2 TEST SEND PER MM 33-50-00-5. THIS CLEARS M387235. 2 L 7 3 4F RT A22WE 20081029 WP 2008 10 29 UPS08853605 1 20081003 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-21 LT INBOARD FLAP EXTERIOR SURFACE AT STA XW1 05 DOES NOT MEET CRITERIA OF AP PENDIX H. FLAP REPAIR MEETS CRITERIA TO BE IAW DC8 SRM 57-02-01-0 FIG 002Q. 2 L 7 4 4F RT 4A25 20081029 2008 10 29 CALA0801010 4 20081025 A 2565 65C1990115 CABLE BOEING 737 7373T0 1384582 NM EVAC SLIDE FRAYED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 ESCAPE SLIDE LATCH CABLE HAS BROKEN STANDS ON (R-2) AFT SERVICE DOOR. INSTALLED NEW CABLE REF AMM 25-61-35. 2 L 7 2 4F RT A16WE 20081029 EA 2008 10 29 ASOA200801370 1 20081020 A 5210 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 917EV 7769 CREW REPORTS, BOTTOM STEP ON PAX DOOR HAS BROKEN OFF FROM DOOR LINKAGE. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA200801371 1 20081020 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA CABIN FAILED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 828AS 7213 EMERGENCY LIGHTS BATTERY PACK NR 3 FAILED TEST. REMOVED FAULTY BATTERY PACK NR 3 IAW AMM 33-51-04-000-801. INSTALLED S ERVICEABLE BATTERY PACK IN SAME LOCATION IAW AMM 33-51-04-400-801. OPS CHECK DUE OF EMERGENCY LIGHTS SYS. PERFORMED OP S CHECK OF BATTERY PACK NR 3 IAW AMM 33-51-04-740-801. OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA200801372 1 20081020 A 7931 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA COCKPIT ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 659CA 10153 AIR RETURN DUE TO "RED" RT ENGINE OIL PRESSURE EICAS MSG IN FLIGHT. RT ENGINE OIL PRESSURE AT ZERO PSI. OIL QUANTITY S TATUS MSG AT 15 PERCENT. FLT 5052 DEL 58 MINS. AIRCRAFT RETURNED TO ICT AFTER T/O. EMERGENCY DECLARED. FLT 5052 CX. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA200801373 1 20081020 A 3211 TRUNNION PIN CNDAIR CL600 CL6002C10 1390015 EA LT MLG CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 LT MLG SHOCK STRUT UPPER (FWD) ATTACHMENT TRUNNION PIN SHOWS SIGN OF CORROSION. AFTER FURTHER INSPECTION FOUND RESIDUE TO BE DRIED CORROSION INHIBITING COMPOUND. REMOVED BOLT, CLEANED AREA AND REINSTALLED BOLT WITH CORROSION INHIBITING C OMPOUND PER AMM 32-00-05. RII SATISFACTORY FOR THE INSTALLATION OF THE FWD TRUNNION PIN ATTACH BOLT PER AMM 32-11-05 AN D SP 607. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA200801375 1 20081020 A 5320 FITTING CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 DURING REMOVAL OF AFT CARGO DOOR COMING, FOUND CRACKED CLIP ON FWD LOWER EDGE, P/N MM670-35699-013. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA200801378 1 20081021 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 748EV 10158 EMERGENCY FLOOR PATH MARKING MISSING FWD LT STRIP BY GALLEY 3. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 FDEA200811124867 1 20081112 A 5311 141N13217 FRAME BOEING 757 75723A 1384967 NM BS 395/S3L - S3R DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 AFTER REMOVAL OF DOUBLER FROM TV MONITOR SPT AT BS 395, S-3L - S-3R, FOUND SEVERAL HOLES ON FRAME. COMPLIED WITH EA 7 57-2550-16-F1312, REV E, FRAME ALTERATION BS 395, B/T S-3L - S-3R. REMOVED SHEAR TIES AND STRINGER CLIPS PER EA STEP 2A 1. REMOVED DAMAGE PER EA STEP 2A2. NDT FOR CRACKS, NO CRACKS NOTED PER EA 2A3. FABBED FRAME PER EA STEP 2A4 ON TRAVEL ER NR T8/763357. FABBED CLIPS AND TIES PER EA STEPS 2A7 AND 2A5. PLUGGED ALL HOLES PER EA STEP 2B6. INSTALLED ALL PAR TS PER EA STEPS 2B5, 2B7, 2B8, 2B12, AND 2B15. REPAIR PARTS "PART MARKED" PER EA 757-2550-16-F1312, REV E. THIS ALTERA TION IS AS A CATEGORY "A" MAJOR ALTERATION. 2 L 7 2 4F RT A2NM 20081029 EA 2008 10 29 ASOA200801392 1 20081024 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 761ND 10213 REFER TO AFDL 447034-3 EMERGENCY LIGHTS. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA200801393 1 20081024 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 761ND 10213 REFER TO AFDL 447034-3 EMERGENCY LIGHTS. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA200801287 1 20081003 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED (14) RIVETS AT FS 409.00+112 BETWEEN STRINGERS 17 AND 19 FOR REMOVAL OF SURFACE CORROSION AND INSPECTION IAW CRJ 200 SRM 51-42-06. REMOVED SURFACE CORROSION AT FS 409.00+112 IAW CRJ 200 SRM 51-21-06. INSTALLED NEW RIVETS AT FS 409 +112 BETWEEN STRINGER 12R AND 13R IAW CRJ 200 SRM 51-42-06. REQ'S PAINT. PAINTED REPAIRED AREA IAW CRJ 200 SRM 51-25-0 1. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081029 NM 2008 10 29 SWAA085801 1 20081027 A 5523 65C26384 TAB BOEING 737 7373H4 1384600 NM ELEVATOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 DURING SCHEDULED 12Y CHECK, FOUND LT ELEVATOR TAB CRACKED AT UPPER LEADING EDGE I/B SIDE OF I/B HINGE CUTOUT. REMOVED A ND REPLACED TAB PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085802 1 20081027 A 3350 6575342 LIGHT BOEING 737 7373Q8 1384670 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 DURING SCHEDULED SPV CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT PLATE MISSING. REMOVED AND REPLACED LIGHT ASSY PER M M. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085790 1 20081025 A 5743 FITTING BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 730SW 27862 DURING SCHEDULED MV3 CHECK, FOUND LT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085791 1 20081025 A 5743 FITTING BOEING 737 7377H4 1384404 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 730SW 27862 DURING SCHEDULED MV3 CHECK, FOUND RT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085792 1 20081025 A 3350 417A56014 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 762SW 27876 FOUND FWD EMERGENCY EXIT SIGN COVER LOOSE. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085797 1 20081027 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085798 1 20081027 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085800 1 20081027 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND NR 2 SLAT L/E LOWER SKIN CRACKED I/B OF ACTUATOR. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081030 EA 2008 10 30 ASOA200801115 1 20080905 A 5320 REPAIR CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 DRILLED OFF, REMOVED OLD PREVIOUS REPAIR RT FLOOR SUPPORT ANGLE AT FS 621. DRILLED UP, COUNTERSUNK AND ALODINED NEW REP AIR PARTS 601R-53-61-117-2 ANGLE AND -4 REPAIR ANGLE AND -6 STRAP FROM 2024-T3 .090. INSTALLED ALL REPAIR PARTS WET USI NG PR1422B½ SEALANT. PRIMED AND PAINTED FASTENERS AND REPAIR PARTS. ALL WORK IAW BOMBARDIER REO 601R-53-61-117, REV C. ALL STEPS OF REO ARE COMPLETE. REPAIR AT RT 621 FLOOR SUPPORT REQ'S DINITROL. APPLIED DINITROL TO REPAIR AREA. RT 6 21 FLOOR SUPPORT REPAIR REQ'S PRESSURIZATION LEAK CHECK. WORK PERFORMED. RT 621 FLOOR SUPPORT REPAIR REQ'S PRESS LEAK CHECK. PERFORMED LEAK CHECK OF THE RT 621 FLOOR SUPPORT REPAIRED. NO LEAK NOTED AT THIS TIME. SUPPLEMENTAL SDR CLOSED 2 L 7 2 4F RT A21EA 20081028 NM 2008 10 28 SWAA085719 1 20081021 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 470WN 33860 FOUND FWD ENTRY EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085720 1 20081019 A 3350 417A5700 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 446WN 29842 DURING SCHEDULED MV1 CHECK, FOUND FWD EEPLS STRIP INOP. REPAIRED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085721 1 20081021 A 2560 65C16820 FITTING BOEING 737 7377H4 1384404 NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 495WN 33869 FOUND R1 DOOR SLIDE GIRT BAR HOLDER CLIP LOOSE. SECURED CLIP PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085722 1 20081021 A 3350 101331 COVER BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 FOUND AFT EMERGENCY EXIT LENS COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085684 1 20081021 A 3350 311500 COVER BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED 14Y CHECK, FOUND OVERHEAD CENTER AISLE EMERGENCY EXIT LIGHT COVER BROKEN. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085694 1 20081021 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 440, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802493 1 20080926 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM BS 947 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION ON UPPER SURFACE OF FLOORBEAM BEYOND LIMITS. REPAIRED PER ESO 61000 DATED 22 SEP 08. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802494 1 20080926 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM BS 947 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION ON UPPER SURFACE OF FLOORBEAM BEYOND LIMITS. REPAIRED PER ESO 61000 DATED 22 SEP 08. 2 L 7 2 4F RT A16WE 20081029 EA 2008 10 29 QXEA200800886 1 20080728 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 485-581 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK LT INBD SEAT TRACK BETWEEN STA FS485-581 HAS CORROSION AT THESE LOCATIONS FS491-493.5, FS499-526, FS531.5-5 43, FS555.5-551. FS568-573. BLENDED CORROSION, MAX MATERIAL REMOVED .021" ALL BLENDS WITHIN LIMITS PER REO 670-53-00-01 3. ALODINED AREA IAW SRM 51-21-11. 2 L 7 2 4F RT A21EA 20081029 NM 2008 10 29 AALA200802487 1 20080925 A 5240 ANGLE BOEING 737 737823 13844CB NM SERVICE DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CREASE ANGLE AT FORWARD SERVICE DOOR HAS LARGE AREA OF CORROSION. REPAIRED PER SRM 51-70-11-02. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 USAA920081871 1 20081011 A 5311 65C32394 FRAME BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03C10753038/006 FUSELAGE FRAME CRACKED ON INNER CHORD AT BS 601, S17R, WL 202, RBL 66. REPAIRED FUSELAGE FRAME INNER CHORD AT BS 601, S17R, WL 202, RBL 66 IAW EA NR 100688. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 2008UALA06194 1 20081020 A 3320 RELAY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 644UA 25094 RELAYS K417 AND K383 IN P-19 PANEL SHOW SIGNS OF OVERHEATING. REMOVED AND REPLACED RELAYS. PERFORMED A GOOD OPS CHECK OF THE NS-FSB SIGNS AND OPS CHECK OF L-1 DOOR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081029 NM 2008 10 29 2008UALA06204 1 20081021 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 771UA 26932 SEAT 2E AFT EEL LIGHT INOP. REPLACED LAMP, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081029 NM 2008 10 29 2008UALA06206 1 20081017 A 5320 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 BS 500 BETWEEN STR 25L & 26L HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING REPAIR & INSTALLED NEW REPAIR PER EVA 72035. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 CALA0800979 1 20081023 A 5315 141T5107 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 68155 30434 BODY STATION 303 FLOOR SUPPORT FOUND CORRODED BETWEEN LBL 22 - 40. BODY STATION 303 FLOORBEAM BETWEEN LBL 6 LBL 63 REPA IRED PER SRM 53-00-51, REPAIR 1, FIG 201, AND HFEC NIL CRACK FOUND. 2 L 7 2 4F RT A1NM 20081029 NM 2008 10 29 CALA0800981 1 20081023 A 5315 141T5146 STIFFENER BOEING 767 767224 1385170 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 68155 30434 E AND E COMPARTMENT M/D FLOORBEAM STATION 246 LBL 40 VERTICAL STIFFENER FOUND CRACKED. MAIN DECK FLOOR BEAM STATION 246 LBL 40 VERTICAL STIFFENER REPAIRED PER ECRA 5310-04854 PART 1. HFEC NIL CRACKS FOUND. REF L/P 7984436 53-DIP, 90691, DIP ISSUED TO PERFORM REPEAT INSPECTION PER ECRA5310-04854. LOG CLOSED, DIP REF TO L/P 7984436. 2 L 7 2 4F RT A1NM 20081029 EA 2008 10 29 ASOA1223 1 20080926 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA ASD UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED & REPLACED FWD AND AFT ASD ANCHOR FITTINGS. R&R FWD/AFT ANCHOR FITTING, OP'S CHECK GOOD & RIGGING 52-11-17. RE PLACED FWD/AFT SERATED PLATE. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081029 NM 2008 10 29 SWAA085807 1 20081027 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085808 1 20081027 A 5311 6546533 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500, BETWEEN STR 27R TO STR 28R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085809 1 20081027 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 727E, STR 18R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085810 1 20081027 A 5315 BAC1509100146 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767 STR 27R. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085811 1 20081027 A 5754 65C26686 WEDGE BOEING 737 7373H4 1384600 NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND LT WING L/E NR 3 SLAT INBOARD UPPER WEDGE DELAMINATED. REPAIRED WEDGE PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085812 1 20081027 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085813 1 20081027 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 303, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085818 1 20081027 A 5754 65C26686 WEDGE BOEING 737 7373H4 1384600 NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 24Y CHECK, FOUND LT WING LEADING EDGE NR 3 SLAT I/B UPPER WEDGE DELAMINATED. REPAIRED WEDGE PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085819 1 20081027 A 5752 6546455 TAB BOEING 737 7373H4 1384600 NM LT AILERON CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 24Y CHECK, FOUND LT AILERON TAB CORRODED AT HINGE DOUBLER UPPER SURFACE. REMOVED AND REPLACED TAB PER MM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085820 1 20081027 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 24Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 1016, STR 6L. REPAIRED WEB PER AAR EA. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085821 1 20081027 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 784SW 29810 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 39 TO LBL 42. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081030 EA 2008 10 30 ASOA200801190 1 20080918 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REPAIRED PAX DOOR AFT DRAG ANGLE IAW BOMBARDIER REO 601R-52-11-513. PAINTED PAX DOOR DRAG ANGLE IAW BOMBARDIER REO 601R -52-11-513. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081030 NM 2008 10 30 AALA200802265 1 20080903 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 EMERGENCY LIGHT AT SEAT 34C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 34C. SYSTEM GROUND CHECKED NORMAL OP ERATION. (K) 2 L 7 2 4F RT T00001SE 20081030 WP 2008 10 30 AALA200802268 1 20080904 A 2560 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 458AA 49563 EMERGENCY FLASH LIGHT AT AFT GALLEY INOPERATIVE. REPLACED BULB, BATTERY AND STRAP. SYSTEM GROUND CHECKED NORMAL OPERATIO N. (K) 2 L 7 2 4F A6WE 20081030 NM 2008 10 30 KCSA081505 1 20080930 A 5411 FRAME BOEING 747 747249F 1384849 NM NR 3 PYLON CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 NR 3 PYLON NAC STA 221.9 BULKHEAD LT FWD FRAME WEB CORRODED. (K) 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 KCSA081496 1 20080927 A 5330 SKIN BOEING 747 747249F 1384849 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 FUSELAGE SKIN IS CORRODED AT STA 2362, BETWEEN STR 40L AND 46L. (K) 2 L 7 4 4F RT A20WE 20081017 2008 10 17 DL76G081334 4 20081006 A 3413 INDICATOR BOEING 767 767332 1382001 NM VSI INOPERATIVE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 1605 30198 F/O TA VSI INOP. REPLACED F/O TA VSI. 2 L 7 2 4F RT A1NM 20081017 WP 2008 10 17 08FDEA04266 1 20081008 A 5312 AEA01613 PRESSURE PANEL DOUG MD10 MD1010F 3022112 WP MLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 556FE 46710 CENTER LANDING GEAR SPACE LT WALL UPPER AFT CORNER HAS A CRACK ALONG UPPER EDGE ACROSS THREE RIVETS ENDING AT STIFFENE R, FWD OF PNEUMATIC DUCT. (VERIFIED CRACK USING LFEC) REPAIRED CRACK AS REQ., REF. EA 8-5310-118303. SEE JPF WORK STEP SIGNOFFS. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 CALA0800970 1 20081013 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59630 27534 CABIN STATION 867 BETWEEN S8R AND S9R PSU SUPPORT BRACKET TO FRAME CRACKED. REMOVED DAMAGED FRAME WEB AND INSTALLED REP AIR ANGLES REF EA 5310-04498 OP 2. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 08FDEA04292 1 20081009 A 5311 65163161 FRAME BOEING 727 727233 138408A NM ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 221FE 20932 9G BULKHEAD CONTACTING FRAME AT STA 344 AND STR 5L. TRIMMED OUT FRAME AND FABRICATED FRAME REPAIR, INSTALLED FRAME REPAI R IAW B727 SRM 51-30-2, 53-10-2 FIG 3 AND SRM 53-10-4 FIG2. 2 L 7 3 4F RT A3WE 20081017 2008 10 17 2008UALA06055 4 20081010 A 3442 RADAR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE WEATHER RADAR FAILED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 WX RADAR FAILURE. RTFL. WX RADAR IS INTERMITTENT. REPLACED TRANSCEIVER (PRECAUTIONARY). PER CREW WX RADAR ACTED NORMAL LY THE LAST TWO HOURS OF FLIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 20081017 NM 2008 10 17 2008UALA06058 1 20081010 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 AFT GALLEY LWR LEFT TWO EEL LIGHTS INOP. REPLACED DAMAGED SUPPLY WIRE DUE. OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081017 NM 2008 10 17 2008UALA06059 1 20081010 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 FLOOR EEL LIGHTS INOP SEAT 45 TO 53 ABC. REPLACED BAD AND WET SUPPLY WIRE FOR EEL LIGHT SYS. OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081017 EU 2008 10 17 08FDEA04302 1 20080909 A 5330 A53812632201 SKIN AIRBUS 300 A300B4622R 3930312 EU ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 725FD 572 SKIN DAMAGE LOCATED AT FR46/47 S41L. REPAIRED AS PER EA 6-5330-121701. 2 L 7 2 4F RT A35EU 20081017 EU 2008 10 17 08FDEA04278 1 20081008 A 2750 532A000003 LIMITER AIRBUS 300 A300F4605R 3930327 EU TE FLAPS TORQUE MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 650FE 726 FLAPS STUCK AT 20 DEG. WOULD NOT RETRACT. FOLLOWED RED TABS FLAPS DID EXTEND TO 30/40 ON LANDING FLAPS RETRACTED AFTER LANDING. BOTH SYS 1 AND SYS 2 FLAP FAULT LIGHT ON IN FLT. PERFORMED SERVICING OF RT WING JACKSCREWS AND TORQUE LIMITER PER AMM 12-13-27-0. ALL FLUIDS CLEAN WITH MINIMAL SERVICING REQUIRED. R&R FLAP TORQUE LIMITER IAW MM 27-54-12-4. PER FORMED OPERATIONAL TEST OF FLAP SYSTEM AND NO DEFECTS FOUND. REINSTALLED INBD NR 1 JACKSCREW ACCESS PANEL. PER VERBAL, MTSI STEP 4 FLAP SYSTEM LUBE ACCOMPLISHED. PERFORMED VISUAL INSPECTION OF ALL CARRIAGES, BEARINGS, ROLLERS, JACKSCREWS, TRACKS, NO DEFECTS FOUND. 2 L 7 2 4F RT A35EU 20081017 NM 2008 10 17 08FDEA04332 1 20081014 A 5744 ARC050214 HINGE DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 RIGHT WING OUTBOARD FLAP INBOARD HINGE (WINGSIDE) LOWER ATTACHMENT OUTBOARD HOLE FORWARD SPOTFACE FOUND SURFACE CORROS ION. SPOTFACE CORROSION REPAIRED AS PER E.A. 1-5750-122592, SHIM FABRICATED AND INSTALLED AS PER CMM 57-44-08. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081017 NM 2008 10 17 08FDEA04333 1 20081014 A 5744 ARC050312 HINGE DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 RIGHT WING OUTBOARD FLAP OUTBOARD HINGE (WING SIDE) LOWER INBOARD BORE HOLE FOUND WITH CORROSION. REPAIRED AS PER E.A. 1-5750-122590, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081105 WP 2008 11 5 AALA200802563 1 20080922 A 5320 STRUCTURE DOUG DC9 DC983 3022083 WP BS 214 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 RT SUBFLOOR CRACKED AT STATION 214. CRACK LENGTH IS 1 INCH. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH AARD 53-20-00- 16. 2 L 7 2 4F RT A6WE 20081017 EU 2008 10 17 08FDEA04338 1 20080916 A 5753 SPAR AIRBUS 300 A300B4622R 3930312 EU LT WING TE FLAP WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 725FD 572 LEFT WING FLAP INBD W/ HOLES OVALIZED AT FRONT SPAR OF RIB 7 THE FRONT SPAR WAS REPAIRED IAW EA 6-5750-121702. 2 L 7 2 4F RT A35EU 20081017 NM 2008 10 17 KNNA20080034 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 639, STR 4L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080035 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 639, STR 3R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080036 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 639, STR 4R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 UPS08553558 1 20080930 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 CORROSION FOUND ALONG UPPER I/B SURFACE OF SEAT TRACK AT FASTENER HOLES BS 1138 RBL 25 WL 208. REMOV ED AND REPLACED PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081017 NM 2008 10 17 UPS08553559 1 20081001 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 LONGITUDINAL BEAM BS 1040-1180 BL 0 WL 208 IS CORRODED AT NUT PLATES AND ON FASTENERS. REMOVED AND R EPLACED PER SRM 51-40-02 (SEAT TRACK). 2 L 7 2 4F RT A2NM 20081022 NM 2008 10 22 EIAA2008101600058 1 20081015 A 5730 SKIN BOEING 747 747230B 1384889 NM LT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 23286 LEFT WING FWD OF SPAR RABBIT JOINT 8 FT FROM TIP CORRODED. REMOVED CORROSION, NDT AREA, FABBED AND INSTALLED REPAIR PER ECRA 487-57-047-2. 2 L 7 4 4F RT A20WE 20081022 NM 2008 10 22 EIAA2008101600059 1 20081015 A 5210 SKIN BOEING 747 747230B 1384889 NM L1 DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 23286 L1 DOOR SKIN CRACK AT 2 FASTENERS AND ONE FASTENER COMMON TO LWR DOOR FRAME. REMOVED DAMAGE, NDT AREA, FABBED AND INSTA LLED REPAIR PER B747 SRM 52-10-02 FIG 9. 2 L 7 4 4F RT A20WE 20081022 CE 2008 10 22 YADA100708 1 20081007 A 3240 MS287410226 LINE BEECH 1900 1900C 1154161 CE LT BRAKE RUPTURED E YADA K NONE S AFFECT SYSTEMS NR NOT REPORTED 1 AL 03 115AX UC02 PILOT REPORTED LEFT BRAKE "FLAT". REPLACED SEEPING FLEXIBLE BRAKE LINE - DATE CODE 2Q06. 2 L 7 2 4T RT A24CE 20081022 EA 2008 10 22 TRAX200801258 1 20081001 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA BS 559 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 LT FS 559 CAP ANGLE LBL 18 HAS AN INDICATION NOTED APPROX .5" IN LENGTH 90% FULL SCREEN HEIGHT FAILED NDT INSP. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 ASOA200801344 1 20081016 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 836AS 7263 PAX DOOR INNER HANDLE HAS CRACK. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 ASOA200801345 1 20081015 A 2560 SIGN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 826AS 7210 PAX DOOR EXIT SIGN BROKE. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 ASOA200801346 1 20081015 A 5312 ANGLE CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 934EV 8028 CARGO CENTER BULKHEAD ANGLE IS CRACKED. REPAIRED PANEL CTR BULKHEAD AND ANGLE IAW CMM 25-52-21. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 ASOA200801355 1 20081015 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 908EV 7654 MAIN CABIN DOOR DIFFICULT TO CLOSE. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 ASOA200801357 1 20081016 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 PAX DOOR FWD INNER HANDLE CRACKED AT TORQUE TUBE ATTACH POINT. REMOVED ASD INNER HANDLE PER AMM 52-11-00. DRILLED AND REAMED HANDLE IAW MM 52-11-00. INSTALLED NEW ASD INNER HANDLE IAW SRM 52-11-02. INSTALLED, REMOVED AND REPLACED BETA L IGHT IAW AMM 52-11-02. 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 SIMA200829402 1 20081018 A 3350 BATTERY CNDAIR CL600 CL6002C10 1390015 EA E&E BAY DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 509AE 10078 ON FLIGHT 4113 CREW REPORTED CABIN EMERGENCY LIGHT SWITCH LEFT ON ALL LIGHTS INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE . REPLACED NR 1, 2, 3 AND AVIONICS BAY EMERGENCY LIGHT BATTERIES. OPERATION CHECKED GOOD. AIRCRAFT RETURNED TO SERVIC E. 2 L 7 2 4F RT A21EA 20081022 NM 2008 10 22 DHLA2008745528 1 20081015 A 5320 6516279 SUPPORT BEAM BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 CORROSION ON AND AROUND LONGITUDINAL SUPPORT BEAM AT BS 760 TO 848.95, LBL 45, OVER CENTER WING FUEL CELL. REMOVED CORR ODED UPPER CHORD, FABRICATED NEW CHORD MEMBER, AND INSTALLED IAW B727 SRM 51-30-2, 51-10-1, AND BOEING DWG 65-16279 REV D DATED 07/08/80. REF N/R 4987-2-423. 2 L 7 3 4F A3WE 20081022 SO 2008 10 22 SIMA200829403 1 20081020 A 3350 20131A BATTERY PACK EMB 135 EMB135KL 3260302 SO CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 801AE 145469 ON FLIGHT 4606 CREW REPORTED SEVERAL EMERGENCY LIGHTS NOT WORKING. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 BATTERY POWER SUPPLY PACK IAW EMB AMM 33-50-04, OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081022 NM 2008 10 22 DHLA2008745529 1 20081015 A 5320 6516279 SUPPORT BEAM BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 CORROSION ON AND AROUND LONGITUDINAL SUPPORT BEAM AT BS 740 TO 870, RBL 45, OVER CENTER WING FUEL CELL. REMOVED CORRODE D UPPER CHORD, FABRICATED NEW CHORD MEMBER, AND INSTALLED IAW B727 SRM 51-30-2, 51-10-1, AND BOEING DWG 65-16279 REV D D ATED 07/08/80. REF N/R 4987-2-223. 2 L 7 3 4F A3WE 20081022 SO 2008 10 22 SIMA200829404 1 20081018 A 3230 LANDING GEAR EMB 135 EMB135LR 3260305 SO MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 703MR 145173 ON FLIGHT 9802 CREW REPORTED AFTER TAKEOFF LANDING GEAR HANDLE UP, YELLOW IN TRANSIT LIGHTS FOLLOWED BY LANDING GEAR LEV ER DISAGREEMENT. CREW UNABLE TO RETRACT GEAR. AIRCRAFT RETURN FOR LANDING CREW REPORTED GEAR IN DOWN POSITION 3 GREEN. AIRCRAFT REMOVED FROM SERVICE. C/W GEAR EXTENSION AND RETRACTION NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081022 EA 2008 10 22 CHQA200800204 1 20081018 A 2710 601R5122623 TRIM PANEL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE COCKPIT FAULTY A CHQA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 11 702BR 7462 GEE872885 FLIGHT 5601, IAH TO JAX. DURING CLIMB, THE FLIGHT CREW EXPERIENCED AN AILERON TRIM RUN-AWAY. THE QRH WAS FOLLOWED AND THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AILERON/RUDDER TRIM PANEL AND THE AI LERON TRIM SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 20081022 NM 2008 10 22 SWAA085565 1 20081012 A 3350 101331 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED MV2 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081022 EA 2008 10 22 CHQA200800205 1 20081018 A 8097 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 1 STARTER CHAFED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 647BR 7399 GEE872717 FLIGHT 5622, SDF TO IAH. DURING TAKEOFF AT APPROXIMATELY 400FT THE FLIGHT CREW RECEIVED A L ENGINE START STATUS MESSAGE AND CYCLED ON AND OFF EVERY 5 TO 10 SECONDS. THE FLIGHT LEVELED OFF AT 10,000FT AND THE FLIGHT CREW RAN THROUGH THE QR H CHECKLISTS. AFTER COMPLETING THE QRH LIST THE INDICATION CONTINUED CYCLING. THE FLIGHT THEN LANDED BACK AT SDF WITHO UT INCIDENT. MAINTENANCE FOUND A WIRE CHAFED AT CONNECTOR P24EZ ON THE E1 AIR TURBINE STARTER. THE WIRE WAS REPAIRED A ND THE SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 20081022 NM 2008 10 22 SWAA085566 1 20081012 A 3350 311500 LENS BOEING 737 7373H4 1384600 NM L1 DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 382SW 26588 FOUND L1 DOOR EGRESS LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085574 1 20081013 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED 18Y CHECK, FOUND EQUIPMENT COOLING EXHAUST SKIN CUTOUT CRACKED AT BS 379, LBL 1.5. REPAIRED SKIN PER A AR EA. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085575 1 20081014 A 5320 69172861 ANGLE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND ANGLE CORRODED BETWEEN BS 219 TO BS 203, LBL 14, WL 156. REMOVED AND REPLACED ANGLE P ER SRM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 SWAA085564 1 20081014 A 3397 W998592920 WIRE BOEING 737 7373H4 1384600 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT IDENTIFIER WIRES PULLED OUT OF SPLICES. RESPLICED WIRES P ER WDM. 2 L 7 2 4F RT A16WE 20081022 NM 2008 10 22 2008UALA05865 1 20080923 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 127UA 28813 RIGHT OVERWING FWD LIGHT ASSY FWD LAMP IS INOP. FOUND LAMP INOPERATIVE. REPLACED LIGHT ASSEMBLY. CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081022 EU 2008 10 22 2008UALA05873 1 20080923 A 5210 FE1740011 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 427UA 512 DOOR 2L 1300 PSI - LOW. SERVICED DOOR 2L TO PROPER PRESSURES. 2 L 7 2 4F 4 F RT A28NM E40NE 20081022 NM 2008 10 22 2008UALA06063 1 20081010 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY CEILING LIGHT AFT OF DOOR 1 LEFT INOP. LAMPED FOUND INOPERATIVE. REPLACED LAMP, OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081022 NM 2008 10 22 2008UALA06073 1 20081013 A 3397 80541 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 181UA 25278 FOUND AFT GALLEY EMERGENCY LIGHT WIRE BROKEN. REPLACED AFT GALLEY LOWER SIDE WALL EMERGENCY LIGHT AND SECURED RIBBON CA BLE. EMERGENCY EMERGENCY LIGHTS OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081022 EA 2008 10 22 ASOA200801197 1 20080919 A 3230 PULLEY CNDAIR CL600 CL6002B19 1900309 EA MLG RELEASE LOOSE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED PULLEY FOR LANDING GEAR MANUAL RELEASE CABLE FOR ACCESS BY UNBOLTING PULLEY. REMOVED AND REPLACED CABIN FLOOR S UPPORT STRUCUTRE FS 280 LBL 9.0 CLIP O/B WITH NEW PART IAW SRM 51-42-13 AND 51-42-21. RE-INSTALLED PULLEY FOR LANDING G EAR MANUAL RELEASE CABLE IAW AMM 20-21-00-910-801. OPS CHECK OF THE MANUAL GEAR RELEASE SYS DUE. OPS CHECK OF LANDING GEAR MANUAL RELEASE SYSTEM GOOD IAW AMM 32-34-00-710-801. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 ASOA200801229 1 20080926 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REPAIRED REAR PRESSURE BULKHEAD WEB THAT SURROUNDS LINTEL ATTACHMENT FITTING IAW BOMBARDIER REO 601R-53-61-1230 REV D. FUSELAGE EXTERIOR REQUIRES PAINT. PAINTED LINTEL EXTERIOR REPAIR IAW CRJ SRM 51-25-01. REPAIR PER EC/TC REO 601R-53-61 -1230 HAS BEEN COMPLETE AND THE REPAIR COMPLIES WITH THE REQUIREMENTS OF EC/TC AND BOMBARDIER REO 601R-53-61-1230, REV D . SUPPLEMENTAL SDR CLOSED 10/15/08. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 ASOA20081242 1 20080929 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED AND REPLACED LT UPPER OBLIQUE ANGLE AT FS 621.0 TO 625.0 IAW SRM 51-40-11, 51-42-06, 51-42-21. SUPPLEMENTAL SDR CLOSED 10/15/08. 2 L 7 2 4F RT A21EA 20081023 CE 2008 10 23 DJFA2008074 1 20081013 A 2612 WARNING SYSTEM RAYTHN DH125 HAWKER800XP 7150012 CE CARGO BAY MALFUNCTIONED E DJFA K NONE N FALSE WARNING AP APPROACH 1 EA 23 805LX 258374 CREW REPORTED FIRE LIGHT IN BAGGAGE COMPARTMENT ILLUMINATED INTERMITTENTLY DURING FINAL APPROACH. NO SMOKE WAS SEEN OR SMELLED. MAINTENANCE INSPECTED AND TESTED THE SYSTEM BUT WAS UNABLE TO DUPLICATE THE PROBLEM. 2 L 7 2 4F RT A3EU 20081023 EA 2008 10 23 N6WA200810092 1 20081009 A 5220 COVER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT UNSECURE A N6WA K NONE O OTHER UK UNKNOWN 1 CE 03 164GJ 10256 RIGHT COVER FOR EMERGENCY EXIT ROW HANDLE FALLING DOWN. RE-SECURED COVER IAW M/M 51-22-61. 2 L 7 2 4F RT A21EA 20081023 SW 2008 10 23 QML2008F00012 1 20080911 A 5310 PANEL BELL 407 407 1182206 SW FUSELAGE LEAKING E QMLA L ABORTED APPROACH B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 03 408AM 53445 ON SHORT FINAL ABORT, SMOKE, SPARKS, BRIGHTER THAN NORMAL OVERHEAD LIGHTING AND A STRONG ODOR CAME FROM THE OVERHEAD PAN EL. ON TOUCHDOWN THE INSTRUMENT PANEL LIGHTS RHEOSTAT SWITCH ADJUSTED TO OFF POSITION - SMOKE, SPARKS, AND BRIGHTER THAN NORMAL LIGHTING STOPPED IMMEDIATELY. WATER DRIPPING FROM THE OVERHEAD PANEL. NORMAL SHUTDOWN COMPLETED. MAINT CALLED. MAINT COMMENT- RAINWATER ENTERED WHERE AN ANTENNA COAX PASSES THRU THE DECK, AND RAN DOWN A TRIM PANEL TO THE CIRCUIT B REAKER PANEL. THE LIGHTED PANEL IS ATTACHED TO THE LOWER SIDE OF THE CIRCUIT BREAKER PANEL AND WATER COLLECTED ON TO AND ENTERED THE LIGHTED PANEL. THIS PANEL IS MODIFIED FOR NVG LIGHTING. NOTE: THIS IS THE SECOND OR POSSIBLY THE THIRD PANE 1 G 7 1 3U O H2SW 20081017 EU 2008 10 17 F3LA200800507 1 20080717 A 5321 D5367307300000 FLOOR PANEL AIRBUS A318 A318111 3940019 EU CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 807FR 2276 LINE MAINTENANCE NOTED THE AFT CARGO PIT TRANSITION PANEL 151FG HAS PUNCTURE DAMAGE IN THREE PLACES ON UPPER SKIN. MAIN TENANCE REPAIRED DAMAGE IN ACCORDANCE WITH A318 SRM 53-02-00, FIGURE 205. 2 L 7 2 4F RT 20081017 NM 2008 10 17 F3LA200800578 1 20080820 A 5321 D5367313600000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 928FR 2236 DURING C3 C-CHECK, INSPECTION NOTED THE FORWARD PIT PANEL 132EG WAS DAMAGED. MAINTENANCE REPAIRED PUNCTURED DAMAGE TO F LOOR PANEL IN ACCORDANCE WITH A319 SRM 53-02-00, FIGURE 204. 2 L 7 2 4F RT A28NM 20081017 NM 2008 10 17 2008UALA05755 1 20080916 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCONNECTED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 655UA 25393 EMERGENCY EXIT LIGHTING STRIP DISCONNECTED NEAR SEATS 10E. LIGHT STRIP FOUND DISCONNECTED. SECURED LOOSE LIGHT STRIP. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081017 NM 2008 10 17 DL757081338 1 20081001 A 5313 143N311087 STRINGER SPLICE BOEING 757 757232 1384965 NM GE CF6 CF680C2B6F 30025 NE FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 609DL 22816 706619 FWD CARGO CORROSION NOTED ON STRINGER SPLICE RADIUS STA 605 LBL 15. REPAIRED IAW SRM 53-00-03 FIG 201. 2 L 7 2 4F 4 F RT A2NM E13NE 20081017 NM 2008 10 17 SWAA085540 1 20081011 A 5743 115A5211 TRUNNION BOEING 737 7377H4 1384404 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 DURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING CORRODED. REPAIRED PER FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 SWAA085545 1 20081013 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP DAMAGED AT BS 277, STR 7R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081017 2008 10 17 SWAA085555 4 20081011 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR UNWANTED DEPLOY A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 740SW 29276 R1 EMERGENCY EXIT DOOR SLIDE INADVERTANTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 SWAA085556 1 20081009 A 3350 BAC27DEX64791 CHARGER BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 783SW 29809 DURING SCHEDULED 8Y CHECK, FOUND LT EMERGENCY EXIT HATCH LIGHT INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 SWAA085557 1 20081012 A 3350 8210248801 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 914WN 36622 DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING DOOR EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 SWAA085558 1 20081012 A 3350 417A56014 SIGN BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 296WN 36613 DURING SCHEDULED MV2 CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED SIGN PER MM. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 CALA0800975 1 20081013 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59630 27534 LEFT FUSELAGE FRAME IS CRACKED AT PSU RAIL SUPPORT BRACKET MOUNT RIVET LOCATED BETWEEN STRINGERS 8 AND 9 AT STATION 400. REPAIRED LEFT FUSELAGE, FRAME STATION 400 BETWEEN S8L AND S9L PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 08FDEA04342 1 20081014 A 5313 65562451 STRINGER BOEING 727 727227 1384078 NM BS 950F-1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 491FE 21529 CORROSION INSIDE OF STR 27L, STA 950F TO STA 1110. REMOVED CORROSION AND FOUND OUT OF LIMITS, REMOVED STRINGER SECTION FOR ACCESS AND REMOVED DAMAGED STRINGER SECTION, FABRICATED NEW STRINGER SECTION, FABRICATED REPAIR SPLICE. INSTALLED R EPAIR PARTS AND STRINGER SECTION REMOVED FOR ACCESS IAW SRM 53-10-1, 51-10-6, 53-10-3, 53-10-2. 2 L 7 3 4F A3WE 20081017 NM 2008 10 17 08FDEA04344 1 20081014 A 5330 65545734 SKIN BOEING 727 727227 1384078 NM BS 640 S28R CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 491FE 21529 FWD CARGO HAS CRACK AROUND RIVETS BACK TAIL AT STR 28R, STA 640. CUT OUT DAMAGED AREA AND REMOVED PREVIOUS SPLICE AS RE QUIRED, FABRICATED REPAIR HAT SECTION AND ONE SPLICE AND INSTALLED REPAIR PARTS IAW SRM 53-10-3, 53 10-2, 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 20081017 EU 2008 10 17 08FDEA04345 1 20081014 A 5320 A5398111320000 CUSP WEB AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 MAIN CARGO DECK LT CUSP 4 INCHES AFT OF FRAME 79, WEB IS BENT & CRACKED. REMOVED CRACKED WEB IAW SRM 51-40-21 & INSTALL ED NEW WEB IAW DWG NR A53981113. 2 L 7 2 4F RT A35EU 20081017 EU 2008 10 17 08FDEA04346 1 20081014 A 5320 A5398111320100 CUSP WEB AIRBUS 300 A300B4622R 3930312 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 MAIN CARGO DECK RT CUSP 4 INCHES AFT OF FRAME 79, WEB IS CRACKED. REMOVED CRACKED WEB IAW SRM 51-40-21 & INSTALLED A N EW WEB IAW SRM 51-40-21 & DWG A53981113. 2 L 7 2 4F RT A35EU 20081017 EU 2008 10 17 08FDEA04347 1 20081014 A 5753 A579603050000 SKIN AIRBUS 300 A300B4622R 3930312 EU LT WING TE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 LEFT CENTER FLAP L/E HAS A GOUGE IN THE EXTERNAL SURFACE LOCATED APPROX MIDWAY BETWEEN NR 3 & 4 FLAP TRACKS. REPAIRED L EFT CENTER FLAP L/E FROM RIB 16 TO RIB 17 IAW SRM 57-50-00. 2 L 7 2 4F RT A35EU 20081017 NM 2008 10 17 KNNA20080077 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 787, STR 7R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080080 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 807, STR 4R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080081 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 807, STR 5R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080083 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 807, STR 8R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080086 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 827, STR 6L. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080088 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM 3 CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 827, STR 5R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080089 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 827, STR 6R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 ASAA0843568 1 20080911 A 5311 654653969 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 BODY STATION 616 LT SIDE INNER CHORD IS CRACKED AT WL 200 (REF SECTION 5 OF EO 5310 0528). CUT OUT DAMAGED AREA, FABRIC ATED FILLER STIFFENING ANGLE LOCATED DRILLED AND INSTALLED IAW EO 5310 02528. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 ASAA0843578 1 20080917 A 5313 654657959 STRINGER BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 APU TORQUE BOX BOTTOM STRINGER CORRODED. REMOVED APU TORQUE BOX BOTTOM STRINGERS LOCATED DRILLED AND INSTALLED REPLACEM ENT STRINGERS IAW B737 400 SRM 51 40 02 PG 2-5. 2 L 7 2 4F RT A16WE 20081017 NM 2008 10 17 ASAA0843581 1 20080917 A 5313 6546579619 STRINGER BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 APU TORQUE BOX TOP BULB FRAME STRINGER CORRODED. REMOVED DAMAGED FRAME STRINGER, LOCATED DRILLED AND INSTALLED A REPLAC EMENT STRINGER IAW B737 400 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081017 SO 2008 10 17 N93A1386-101308 1 20081013 A 5320 TORQUE BOX GULSTM G1159 GIV 3980115 SO FUSELAGE CORRODED E N93A K NONE O OTHER IN INSP/MAINT 1 SO 13 486QS 8079 1386 CENTER FUSELAGE TORQUE BOX ASSEMBLY UPPER SKIN IS CORRODED. 2 L 7 2 4F RT A12EA 20081017 NM 2008 10 17 KNNA20080090 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 827, STR 10R. 2 L 7 2 4F A16WE 20081017 NM 2008 10 17 KNNA20080091 1 20080918 A 5340 STRINGER CLIP BOEING 737 737291 138448W NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 CRACKED STRINGER CLIP AT STA 847, STR 10R. 2 L 7 2 4F A16WE 20081017 EU 2008 10 17 UPS08153555 1 20080926 A 5321 B5327086400200 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR MAIN CARGO FLOORBOARD 221FG IS CRACKED ON EACH SIDE. REPAIRED MAIN CARGO FLOORBOARD 221FG REF A300 -600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081020 WP 2008 10 20 AALA200802281 1 20080906 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7540A 49994 MSP EMERGENCY LIGHT AT SEAT ROW 2D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 2D. SYSTEM GROUND CHECKE D NORMAL OPS. 2 L 7 2 4F A6WE 20081020 EA 2008 10 20 QXEA200800685 1 20080612 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 573-675 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK NUMEROUS CORROSION SPOTS ON LT SIDE SEAT RAIL FS 573 TO FS 675. REMOVED CORROSION FROM SEAT TRACK AT FS 57 3 TO FS 675. .010 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013 AND CRJ SRM 51-21-16. 2 L 7 2 4F RT A21EA 20081020 NM 2008 10 20 AALA200802314 1 20080908 A 3350 PBS73 BATTERY PACK BOEING 767 767323 1385205 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 377AN 25446 JFK EMERGENCY LIGHT EXIT SIGN AT LT OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT EXIT SIGN AT LT OVE RWING. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081020 NM 2008 10 20 AALA200802306 1 20080908 A 3350 LAMP BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 912AN 29513 TPA EMERGENCY LIGHT AT SEAT 7D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMA L OPS. 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 NOC2008F00004 1 20080920 A 3350 LAMP BOEING 767 767324 1385203 NM EMERGENCY LIGHTS INOPERATIVE A NOCA O OTHER O OTHER NR NOT REPORTED 1 EA 15 767NA 27569 SEAT 9 AB E PATH LIGHT OUT ACTION RELAMPED LIGHT ASSY IAW 33-51-10. 2 L 7 2 4F RT A1NM 20081020 WP 2008 10 20 AALA200802277 1 20080906 A 2910 ADK4327501 TUBE DOUG DC9 DC982 3022082 WP HYD SYSTEM BROKEN A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 70529 49921 ORD INFLIGHT T333/06SEP. CREW REPORTED LOSS OF RT HYDRAULIC SYSTEM. LANDED ORD WITHOUT INCIDENT. FOUND RT TAIL COMPAR TMENT HYDRAULIC PRESSURE LINE BROKEN. REPLACED TUBE ASSEMBLY FOR RT TAIL COMPARTMENT HYDRAULIC PRESSURE LINE. SYSTEM G ROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081020 WP 2008 10 20 AALA200802289 1 20080906 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7547A 53029 DFW EMERGENCY LIGHTS AT OVERHEAD AFT SERVICE DOOR AND TAIL CONE AREA INOPERATIVE. REPLACED BATTERY PACK AT AFT LAVATORY FOR EMERGENCY LIGHTS AT OVERHEAD AFT SERVICE DOOR AND TAIL CONE AREA. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081020 NM 2008 10 20 USAA920081661 1 20080908 A 5311 FRAME BOEING 737 7374B7 1384702 NM BS 616 S17L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 FUSELAGE FRAME CRACKED ON INNER CHORD STRAP AT LOWER END BS 616, S17L. REPAIRED FUSELAGE FRAME ON INNER CHORD STRAP AT L OWER END BS616, S17L IAW AMM 2015-05 AND REPAIR 53-62-01. (K) 2 L 7 2 4F RT A16WE 20081020 NM 2008 10 20 USAA920081665 1 20080907 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 1384595 NM BS 380 S9R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 STRINGER CLIP CRACKED AT BS 380, 9R. REPAIRED STRINGER CLIP AT BS 380, 9R IAW SRM 51-40-01-0G. (K) 2 L 7 2 4F RT A16WE 20081020 SO 2008 10 20 SIMA200826101 1 20080911 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 696AE 14500874 DURING MBV INSPECTION, FOUND CARGO DOOR SILL UPPER AND LOWER SURFACES CORRODED. MAINT REPLACED CARGO DOOR SILL IAW SRM 51-40-02. ACFT WAS RETURNED TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081020 EA 2008 10 20 MAS2008F00081 1 20080909 A 3350 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 921FJ 15021 CREW REPORTED EMERGENCY EXIT LIGHT AT 16A AND AN EMERGENCY EXIT LIGHT AT ROW 7 INOPERATIVE. MX RELAMPED. (K) 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 MAS2008F00082 1 20080910 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHTS INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 911FJ 15011 FLOOR EMERGENCY EXIT SIGN AT ROW 16A AND 16F INOPERATIVE. MX RELAMPED. (K) 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 MAS2008F00083 1 20080910 A 5270 WARNING MESSAGE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR FALSE ACTIVATION A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 510MJ 10101 IN FLIGHT, MAIN CABIN DOOR OUTER HANDLE CAUTION MESSAGE. OPS CHECK GOOD. NO FAULTS FOUND. (K) 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 A6WA200840590 1 20080918 A 7931 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* 30015 NE RT ENGINE FLUCTUATES A A6WA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 31 457AW 7854 ON REACHING CRUISE ALTITUDE, EICAS SHOWN RT ENGINE OIL LOP MASTER WARNING OIL PRESSURE FLUX BETWEEN 38-53 PSI UNTIL JUST BEFORE LANDING WHEN AGAIN RECEIVED RT ENGINE LOP. CORRECTIVE ACTION IN PROGRESS. (K) 2 L 7 2 4F 4 F RT A21EA 20081020 EU 2008 10 20 USAA920081663 1 20080908 A 3251 C202163392E34 CONTROL UNIT AIRBUS 320 A320214 3930316 EU NLG STEERING FAULTY A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 112US 26809 1134 EMERGENCY LANDING- FLIGHT DEPARTED WITH BSCU SYS, BRK/STEER MEL 32-42-03A. WHILE ENROUTE, SECOND CHANNEL WAS LOST. CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. MAINT REMOVED AND REPLACED THE BRAKE/STEERING CONTROL UNIT IAW MM 32- 42-34. OPS CHECK WAS NORMAL. (K) 2 L 7 2 4F RT A28NM 20081020 SO 2008 10 20 SIMA200826103 1 20080912 A 5320 14525480603 FLOOR SUPPORT EMB 135 EMB135KL 3260302 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 837AE 145647 DURING A MBV INSPECTION. A PREV REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAI R AND CLEANED THE AREA. FABRICATED A DOUBLER, FILLER, PLATE AND TWO SHIMS. MARKED, DRILLED AND CLEANED REPAIR PARTS. RE PAIR DONE IAW SRM145/1142, REF 40, CHAPTER 53-00-10, FIGURE 201. (K) 2 L 7 2 4F RT T00011AT 20081030 NM 2008 10 30 KCSA081498 1 20080927 A 5311 FRAME BOEING 747 747249F 1384849 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 AFT BILGE FUSELAGE FRAME UPPER CHORD IS CORRODED AT STA 1880, RBL 18. (K) 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 DHL2008F00034 1 20080917 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN AT BS 500 BETWEEN STRINGER 16R AND 17R FRAME WITH DENT. REPAIRED FUSELAGE FRAME SECTION AT BS 5 00 BETWEEN STRINGER 16R AND STRINGER 17R DUE TO DENT IAW SRM 51-40-3, FIG 1. (K) 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 DHL2008F00039 1 20080912 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN AT BS 720C STRINGER 8R FRAME WITH DOUBLE HOLES. REPAIRED FUSELAGE FRAME SECTION AT BS 720C BETW EEN STRINGER 7 AND 9 RT SIDE, DUE TO DOUBLE HOLES IAW SRM 53-10-4, FIG 2. (K) 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 DHL2008F00045 1 20080926 A 3350 1000677 LIGHT BOEING 727 727200 138407E NM CABIN INOPERATIVE A DHLA O OTHER O OTHER NR NOT REPORTED 1 GL 05 741DH 704 21931 COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-50-93. OP CHECK GOOD. A CFT GROUNDED. (K) 2 L 7 3 4F RT A3WE 20081030 NM 2008 10 30 DL757081418 1 20081022 A 5315 146N5391 FLOORBEAM BOEING 757 757232 1384965 NM BS 1523 LBL 3 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 CORROSION AROUND NUTPLATE HOLE BS 1523 LBL 3 FLOOR SUPPORT RAIL. REMOVED DAMAGED SECTION OF FLOOR SUPPORT RAIL BS 1523 LBL 3. FABRICATED REPAIR PARTS, ALODINED, PRIMED, AND INSTALLED WET WITH SEALANT. WORK DONE IAW SRM 53-60-53D FIG 206. 2 L 7 2 4F RT A2NM 20081030 EA 2008 10 30 A6WA200840586 1 20080904 A 4930 O-RING CNDAIR CL600 CL6002B19 1900309 EA APU FUEL SYS DETERIORATED A A6WA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 31 444ZW 7788 FUEL LEAK BELOW APU. FOUND APU FUEL SUPPLY LINE O-RING DETERIORATED. REMOVED AND REPLACED APU FUEL LINE O-RING IAW AMM 4 9-31-01-420-001. NO LEAKS. OK FOR SERVICE. (K) 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 A6WA200840587 1 20080908 A 3320 BALLAST CNDAIR CL600 CL6002B19 1900309 EA CABIN FAULTY A A6WA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 426AW 7669 STRONG ELECTRICAL SMELL PRESENT IN CABIN BETWEEN ROWS 4 AND 9 EXCLUSIVE. (DISCOVERED ON GROUND) REMOVED AND REPLACED NR 4 RT SIDEWALL LIGHT BALLAST IAW AMM 33-21-10. CONFIRMED BALLAST WAS CAUSE OF SMELL. (K) 2 L 7 2 4F RT A21EA 20081030 NM 2008 10 30 DL757081420 1 20081014 A 5320 146N539157 FLOOR SUPPORT BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE BS 1486-1530 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 728754 CORROSION ON FLOOR TO SIDEWALL SUPPORT AT NUTPLATE LOCATIONS BS 1510-1530 RBL 17. REPLACED DAMAGED SECTION OF FLOOR TO SIDEWALL SUPPORT PLATE BS 1486-1530. FABRICATED AND INSTALLED NEW SPLICE PLATE AT BS 1486 RBL 17. 2 L 7 2 4F 4 F RT A2NM E17NE 20081030 NM 2008 10 30 DL757081421 1 20081014 A 5320 146N539151 FLOOR SUPPORT BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE BS 1530 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 728754 CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE AT BS 1530 RBL 25 IS OUT OF LIMITS. REPLACED DAMAGED SECTION OF FLOOR TO S IDEWALL SUPPORT PLATE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081030 NM 2008 10 30 DL757081422 1 20081019 A 5320 453N185318 BRACKET BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE CARGO DOORWAY DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 728754 FWD CARGO BAY CARGO SYSTEM STOP FITTING SUPPORT IS DENTED, FOUND ALSO TO BE CORRODED. REMOVED AND REPLACED STOP FITTING 2 L 7 2 4F 4 F RT A2NM E17NE 20081030 NM 2008 10 30 K11A2008102372214 1 20080820 A 5311 FITTING BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 FRAME TIE CORRODED, 9 INCHES IN LENGTH. 2 L 7 3 4F RT A3WE 20081030 SO 2008 10 30 SIMA200830301 1 20081024 A 3320 BR900022 BALLAST EMB 145 EMB145LR 3260212 SO CABIN FAULTY A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 635AE 145158 FLIGHT 3982 - CREW NOTICED A BURNING SMELL IN GALLEY. AIRCRAFT REMOVED FROM SERVICE. FOUND CEILING BALLAST FOR ROW 2 A ND 3 TO BE THE SOURCE OF THE SMELL. REMOVED AND REPLACED ROW 2 AND 3 CEILING BALLASTS AND ASSOCIATED HARNESS IAW EMB 14 5 MM 33-21-05. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081030 CE 2008 10 30 GUUA10220801 1 20081022 A 3260 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE NR 2 OUT OF ADJUST A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 29 45AR UE12 FLIGHT 6505 - MCO/FLL - DURING FLIGHT LANDING GEAR HANDLE LIGHT ILLUMINATES INTERMITTENTLY WITH GEAR UP. ADJUSTED NUMBE R TWO UPLOCK SWITCH. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A24CE 20081030 EA 2008 10 30 SIMA200830102 2 20081023 A 7200 AE3007A1 ENGINE EMB 145 EMB145LR 3260212 SO RROYCE AE3007 AE3007A1 54165 EA NR 1 MALFUNCTIONED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 664MS 13093 145779 CAE312137 FLIGHT 4292 - ON CLIMBOUT CREW OBSERVED SMOKE IN THE CABIN AND COCKPIT. CREW ELECTED TO RETURN TO CMH. AIRCRAFT LANDED AND TAXIED SAFELY TO THE GATE WITHOUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER ON E ENGINE IAW WORK CARD 71-000-00. GROUND OPERATIONAL AND LEAK CHECKS GOOD AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081030 CE 2008 10 30 GUUA10170801 1 20081017 A 5210 CAM BEECH BEECH 1900 1900D 1154162 CE ASD OUT OF ADJUST A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 53545 UE185 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED AIRSTAIR DOOR DIFFICULT TO OPEN AND CLOSE. RE-ADJUSTED AIRSTAIR DOOR CA M. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081030 WP 2008 10 30 WRLA2008090 1 20081022 A 5210 ADA27376513 CABLE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE L4 DOOR MISRIGGED A WRLA K NONE L NO TEST IN INSP/MAINT 1 SO 11 14075 46922 DURING MAINTENANCE L4 DOOR FAILED TO OPEN WITH DOOR ARMED, EMERGENCY MODE. REMOVED LININGS, RIGGED AIR RELEASE CABLE AN D ARMING ROD IAW DC10 MM 52-12-00. OPS CHECK GOOD. SERVICED DOOR OPENING RESERVOIR IAW DC10 MM 52-12-00. REPLACED L4 DOOR AND SURROUND LININGS IAW DC10 MM 25-61-01. 2 L 7 3 4F 4 F A22WE E23EA 20081030 NM 2008 10 30 EIAA2008102800064 1 20081027 A 5320 FLOOR SUPPORT BOEING 747 747273C 1384896 NM BS 1990-2010 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 BULK CARGO STA 2000 RBL 50 FLOOR SUPPORT CRACKED. REMOVED FASTENERS AT CRACKED FLOOR SUPPORT, STA 1990 TO STA 2010 RBL 50, AS PER SRM 51-30-02. REMOVED DAMAGE, NDT AREA, FABRICATED NEW SUPPORT PER BOEING DRAWING 65B06261, HEAT TREATED, AL ODINED AND PRIMED INSTALLED NEW SUPPORT PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 EIAA2008102800066 1 20081027 A 3350 S1356B37 LIGHT BOEING 747 747273C 1384896 NM ZONE 200 NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487EV 20653 UPPER DECK EMERGENCY LIGHT TEST FOUND UPPER DECK CABIN CEILING LIGHT BURNT OUT. REPLACED UPPER DECK LIGHT ASSY, OPS CHE CKED NORMAL IAW B747 MM 33-51-00. 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 EIAA2008102800067 1 20081027 A 3350 S1356B37 LIGHT BOEING 747 747273C 1384896 NM ZONE 100 NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481EV 23286 MAIN DECK CEILING MOUNTED EMERGENCY LIGHT FOUND INOP, STA 580. REPLACED MD CEILING MOUNTED EMERGENCY LT ASSY, OPS CHECK NORMAL PER 33-51-00. 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 08FDEA04616 1 20081029 A 5311 651593456 FRAME BOEING 727 7272D4 138407U NM ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 FWD PIT BS 620 FRAME CRACKED RBL 2 TO RBL 3 WL 155, BELOW FLOOR SUPPORT. REPAIRED IAW SRM 51-40-3. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081030 EU 2008 10 30 08FDEA04617 1 20081029 A 5315 A53275349200 FLOORBEAM AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 668FE 772 GUIDE BROKE AT POS 9L WITH FLOOR DAMAGE REMOVED DAMAGED SECTION AT FLOORBEAM FRAME 64 BETWEEN SEAT TRACK NR 3 LT AND NR 4 LT AND REPAIRED IAW FEDEX EA 6-5310-117443, RELEASE DATE 11/14/07. 2 L 7 2 4F RT A35EU 20081030 NM 2008 10 30 08FDEA04618 1 20081029 A 5414 311N504634 SKIN BOEING 757 757236 1384971 NM NR 1 NACELLE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 NR 1 PYLON INBD AFT 311N5046-34 SKIN PANEL ASSY HAS CORROSION ON INNER SURFACE. FOUND SKIN ASSY CORRODED OUT OF LIMITS IAW SRM 54-50-01 (L= 1.5 INCH, W= 2.0 INCH, D= .028 INCH). ROUTED SKIN PANEL ASSY FOR REPAIR ON AMII WORK ORDER NR 7434 , DATED 07/14/08 AGAINST W/C T F-5450-122806 AND EA F-5450-122806, REV "A", DATED 07/17/08. INSTALLED NR1 PYLON INBD RE PAIRED SKIN PANEL ASSY IAW DRAWING 311N5002. THIS REPAIR IS CLASSIFIED AS A CATEGORY "A" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20081030 NM 2008 10 30 DL757081453 1 20081026 A 5321 453N761121 SPLICE BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE FLOOR PANEL CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 727893 CORROSION FWD CARGO BAY FLOOR PANEL SPLICE AT BS 748, RBL 13-20. REMOVED AND REPLACED SPLICE DUE TO CORROSION OUT OF LI MITS IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E24NE 20081030 NM 2008 10 30 DL757081454 1 20081016 A 5330 146N361010 SKIN BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 727893 WHILE ACCESSING AFT LAV SERVICE PAN FOUND SKIN UNDER LIP OF PAN TO HAVE CORROSION, OUT OF LIMITS. REPAIRED PER ER/A 465 409-14 REV ORG. 2 L 7 2 4F 4 F RT A2NM E24NE 20081030 NM 2008 10 30 DL757081458 1 20081027 A 5320 146N365016 CHANNEL BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS1690 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 727893 SUPPORT CHANNEL INBD OF AFT DUMP VALVE CORRODED ALL THE WAY THROUGH BS 1690 RBL 10. REMOVED AND REPLACED CHANNEL DUE TO OUT OF LIMITS CORROSION. 2 L 7 2 4F 4 F RT A2NM E24NE 20081030 NE 2008 10 30 USAA EMB08018 2 20081028 A 7200 ENGINE EMB ERJ190 ERJ190100IGW 3260408 NM GE CF34 CF3410E6 30023 NE NR 2 CONTAMINATED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 956UW 19000156 FLIGHT 1711, CLT-ORF - APPROXIMATELY 100 FEET AFTER TAKEOFF THE FLIGHT ATTENDANT NOTIFIED THE CAPTAIN THAT THERE WAS SMO KE/FUMES IN THE AFT GALLEY. THE CAPTAIN REQUESTED TO RETURN TO CLT AND THE EMERGENCY EQUIPMENT STAND BY. THE CAPTAIN S TATED THE SMOKE AND FUMES DISSIPATED PRIOR TO LANDING AND TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE NOTICED THE NR 2 ENGINE HAS AN ODOR OF DE-ICING FLUID. THERE WAS ALSO A FAINT ODOR OF DE-ICING FLUID IN THE CABIN. MAINTENANCE PER SONNEL RAN BOTH ENGINES, BOTH PACKS AND PRESSURIZED THE CABIN. AFTER APPROXIMATELY 30 MINUTES THE ODOR CLEARED. 2 L 7 2 4F 4 F RT A57NM E00070EN 20081030 NM 2008 10 30 DL757081459 1 20081027 A 5320 146N36501 CHANNEL BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 1690 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 727893 SUPPORT CHANNEL AFT OF AFT DUMP VALVE IS CORRODED BS 1690 RBL 24. REMOVED AND REPLACED SUPPORT CHANNEL DUE TO OUT OF LI MITS CORROSION. 2 L 7 2 4F 4 F RT A2NM E24NE 20081030 NM 2008 10 30 DL777081460 1 20081028 A 4920 ENGINE BOEING 777 777232 1385232 NM APU MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 866DA 15462 P1297 29738 REMOVED AND REPLACED APU DUE TO METAL ON CHIP DETECTOR. POST MTC IN-FLT START IN FLT RELEASE. FOUND EXCESSIVE METAL ON MAIN CHIP DET. REMOVED AND REPLACED APU PER M/M OPS GOOD. 2 L 7 2 4F RT T00001SE 20081030 NM 2008 10 30 QXEA2008291001099 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4 - RT INBD SEAT TRACK HAS SCRATCHES AND CHAFING ALONG CHANNEL AND TOP FROM APPROX STA X435 - X441. BLENDED CORR OSION AND FOUND TO BE WITHIN LIMITS PER RD8/4-53-884. HFEC INSPECTED IAW 1-84-7A, PT 6, 51-00-02, NO CRACKS NOTED. APP LIED ACID ETCH AND ALODINE IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 QXEA2008102901100 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4 - LT INBD SEAT TRACK HAS CHAFING AND SCRATCHES ALONG CHANNEL AND TOP FROM APPROX STA X435 - X441. BLENDED OUT CHAFE AND SCRATCHES, FOUND TO BE WITHIN LIMITS PER RD8/4-53-884. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01 NO CRACK S NOTED. ETCHED AND ALODINED IAW RD 8/4-53-884. 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 QXEA2008102901102 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX-C4- LT INBD SEAT TRACK HAS CHAFING AND SCRATCHES ALONG CHANNEL AND TOP FROM APPROX STA X359 - X374. BLENDED CHAFE A ND SCRATCHES AND FOUND TO BE WITHIN LIMITS PER RD8/4-53-884. HFEC INSPECTED IAW -8 Q400 NDTM PART 6, 51-00-01. NO CRAC KS NOTED. ETCHED AND ALODINED IAW RD 8/4-53-884. 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 QXEA2008102901103 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX-C4- LT INBD SEAT TRACK HAS CHAFING AND SCRATCHES ALONG CHANNEL AND TOP FROM APPROX STA X325 - X343. BLENDED CORROSI ON AND FOUND TO BE WITHIN LIMITS PER RD 8/4-53-884. HFEC INSPECTED IAW 1-84-7A PART 6, 51-00-02, NO CRACKS NOTED. ALOD INE AREA IAW RD 8/4-53-884 PARA 6 GENERAL NOTES 4 AND 6. 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 DL757081429 1 20081017 A 5315 146N54587 FLOORBEAM BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE BS 1480 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 728754 FLOOR SUPPORT BRACKET AT BS 1480 RBL 11 CORRODED. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-30-01, DWG 146N5458, SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E17NE 20081030 NE 2008 10 30 DL76L081430 2 20081024 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 MALFUNCTIONED A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 181DN 34618 25986 727893 AFTER LEVEL OFF AT FL 364 THE LEFT ENGINE SPOOLED BACK ON ITS OWN FOLLOWED BY NUMEROUS EEC AND ENGINE OUT MESSAGES. T/S PER FIM INSPECTION FUEL SAMPLES PLUS NR 1 ENG FUEL FILTER FOR CONTAMINATION. FILTER PLUS FUEL SAMPLE FOUND CLEAN C/W E NG FU SUCTION FEED OPS TEST PER M/M. NR 1 ENG OPS NORMAL. REMOVED PLUS INSPECTION L FWD PLUS AFT BOOST PUMPS. CHKS NO RMAL. INST BOOST PUMPS PER M/M. REPLACED N1 ENG FUEL PUMP PLUS FMU PER M/M. 2 L 7 2 4F 4 F RT A1NM E24NE 20081030 NM 2008 10 30 DL757081431 1 20081013 A 5320 146N54444 STRUCTURE BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 1510 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 727893 CORROSION ON Z STRINGER LOWER SURFACE NUTPLATE LOCATION RBL 7.5 BS 1510, OUT OF LIMITS. REMOVED AND REPLACED PART IAW S RM 51-40-02, DRD 53-60-53. 2 L 7 2 4F 4 F RT A2NM E24NE 20081030 NM 2008 10 30 DL757081432 1 20081019 A 5320 143N534639 FLOOR SUPPORT BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 791-818 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 727893 CORROSION IN AND AROUND FASTENER AND HOLES AT BS 791-818 RBL 7 FLOOR STRINGER. FLOOR STRINGER REMOVED AND REPLACED DUE TO CORROSION OUT OF LIMITS IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E24NE 20081030 NM 2008 10 30 08FDEA04619 1 20081029 A 2121 GASPER FAN BOEING 727 727233 138408A NM CABIN MALFUNCTIONED A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 21 220FE 20934 AT FL 350 A SLIGHT ELECTRICAL ODOR WAS DETECTED APPROACHING MEMPHIS. TURNED OFF GASPER FAN. ODOR WAS STILL DETECTED AN D BECOMING STRONGER. DONNED OXYGEN MASKS RAN QRH SMOKE, FUMES, ODORS CHECKLIST. DECLARED ATC EMERGENCY AND LANDED. AT GATE SHUTDOWN ACFT UNTIL ALL POWER OFF, LEFT ACFT. FLT ENGINEER REPORTS VISUAL SMOKE NEAR FIRST OFFICERS LIDO BAG AFTE R RUNNING QRH CHECKLIST. POSSIBLE OUT OF GASPER VENT BY LANDING SMOKE CLEARED. AT CREW DEPARTURE STILL COULD DETECT SM OKE/WIRE/INSULATION BURN. GASPER FAN CAME APART, R/R GASPER FAN IAW 21-23-001-4 2 L 7 3 4F RT A3WE 20081030 EA 2008 10 30 S9BA2008030 1 20081025 A 2430 A701D RELAY DHAV DHC6 DHC6300 2802606 EA ELECTRICAL SYS FAULTY A S9BA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 29 533 373 373 533 ON FIRST START, LEFT ENGINE DID NOT SPOOL UP. DURING SECOND ATTEMPT STRONG ELECTRICAL SMELL AND CABIN SMOKE DEVELOPED. START WAS ABORTED. FOUND CABLE TERMINAL END BURNT AT REVERSE CURRENT RELAY (RCR) POST. REPLACED TERMINAL END AND RCR REPLACED WITH NEW. OPS CHECK SATISFACTORY, NO ODOR OR HEAT DETECTED. 1 H 7 2 3T RT A9EA 20081030 2008 10 30 DL75E081434 4 20081024 A 8300 GEARBOX BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE NR 2 ENGINE MAKING METAL A DALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 706TW 25955 28165 728754 RIGHT ENGINE SHUTDOWN BY ITSELF. FOUND METAL ON GEARBOX CHIP DETECTOR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081030 NM 2008 10 30 DL76G081436 1 20081025 A 2910 O-RING BOEING 767 767332 1382001 NM HYD SYSTEM LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 176DZ 29697 ON FLIGHT 30 ATB TO JFK DUE TO CTR SYS HYD QTY LOSING FLUID. FOUND NR 10 SPOILER PCA PLUS LEADING REF IPC FOR SPOILER P ITEM 425. REMOVED AND REPLACED DAMAGED O-RING PER AMM. OPS 2 LEAK CHK OK. ACFT RETURNED TO NML CONFIG ACFT OK FOR SE RVICE. CTR HYDS SVCD T FULL. 2 L 7 2 4F RT A1NM 20081030 NM 2008 10 30 EIAA2008102800068 1 20081027 A 5330 SKIN BOEING 747 747273C 1384896 NM BS 2130 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 BULK CARGO STA 2160 STRINGER 46R SKIN ADJ AREA CRACKED. REMOVED FASTENERS, CUT SKIN FABRICATED REPAIR AND NEW SHEAR TIE , HEAT TREATED, ALODINED AND PRIMED, INSTALLED REPAIR. COI RAISED TO ACCOMPLISH REINSPECTION IAW WITH SRM. 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 EIAA2008102800069 1 20081027 A 5315 FLOORBEAM BOEING 747 747230B 1384889 NM BS 700 DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 487EV 20653 FWD CARGO STA 700 RBL 50 FLOORBEAM FOUND DENTED. REMOVED CENT AREA. PERFORMED NDT OF AREA, NO CRACKS NOTED. FABRICATE D REPAIR, ALODINED AND PRIMED REPAIR. REPAIR INSTALLED PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 EIAA2008102800070 1 20081027 A 5320 FLOOR SUPPORT BOEING 747 747273C 1384896 NM CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 BULK CARGO STA 2100, BL 0 FLOOR SUPPORT FOUND CRACKED. REMOVE FLOOR SUPPORT NDTD AREA, NO CRACKS NOTED. FABRICATED NEW FLOOR SUPPORT PER BOEING DRAWING 65B06261. HEAT TREATED, ALODINED AND PRIMED, INSTALLED REPAIR PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 EIAA2008102800071 1 20081027 A 5347 S1356B37 SEAT TRACK BOEING 747 747273C 1384896 NM BS 1900 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 AFT CARGO LT AFT FIXED STOP TIE-DOWN TRACK CRACKED STA 1900 LBL44, SEAT TRACK REMOVED. NEW SEAT TRACK FABRICATED ALODIN ED AND PRIMED. INSTALLED NEW SEAT TRACK PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 DHLA2008745565 1 20080907 A 5313 STRINGER BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 NR 1-322 LOWER FUSELAGE AFT CARGO COMPARTMENT FROM BS 1050 TO BS 1130 S-29R WITH CORROSION. REPAIRED FUSELAGE STRINGER 29 RIGHT FROM BS 1010 TO BS 1128 IAW B727SRM 53-10-3 FIG 1 DETAIL 1. 2 L 7 3 4F A3WE 20081020 NM 2008 10 20 NSV2008F00026 1 20080918 A 7602 CONDITION LEVER BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A NSVA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 27 187WQ 4187 DURING INITIAL CLIMB PEC NR 1 AND NR 2 CAUTION LIGHT ILLUMINATED AFTER INADVERTENT MOVEMENT OF CONDITION LEVERS PAST 850 MIN POSITION. CONDITION LEVERS IMMEDIATELY RESET TO 850, PROP RPM REMOVED STEADY AT 1060 THROUGH REMAINDER OF FLIGHT. R ETRIEVED FADEC CODE IAW Q400-AMM 45-00-79-742-801 FAULT CODES SET NR1 FADEC 260, 236, NR 2 FADEC 280, 236 DETERMINED DUE TO CONDITION LEVERS DROPPED BELOW MIN 850. CLEARED FAULT CODES IAW Q400 AMM 45-00-73-743-801. POWERPLANT MESSAGE DEILL UMINATED. (K) 2 H 7 2 4T RT A13NM 20081020 NM 2008 10 20 UPS08M53512 1 20080518 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A RT WING O/B FLAP O/B FWD HINGE UPPER MOUNT FWD SPOTFACE CORRODED. RT WING O/B FLAP O/B FWD HINGE UP PER MOUNT FWD SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09. 2 L 7 3 4F RT A22WE 20081020 NM 2008 10 20 UPS08M53513 1 20080518 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A RT WING O/B FLAP I/B FWD HINGE BARREL NUT UPPER BORE CORRODED. RT WING O/B FLAP I/B FWD HINGE BARRE L NUT UPPER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08. 2 L 7 3 4F RT A22WE 20081020 EA 2008 10 20 ASOA200801187 1 20080918 A 3350 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED AND INSTALLED A SERVICEABLE EMERGENCY EXIT FLOODLIGHT CAVE AND BASE ON AFT LOWER SIDE OF WARDROBE IAW AMM 33-51- 13-400-801. OPS CHECK DUE. OPS TEST OF WARDROBE EMERGENCY LIGHT IS GOOD IAW AMM TASK 33-51-00-710-801. SUPPLEMENTAL S DR CLOSED 10/15/08. 2 L 7 2 4F RT A21EA 20081020 EA 2008 10 20 ASOA20081216 1 20080925 A 5210 ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 COMPLIED WITH STEPS 1 AND 2 OF REO 670-52-11-072. CUT OF DAMAGED ANGLE AND REMOVAL OF ALL BURRS. PERFORMED EDDY CURRE NT INSPECTION OF CUT LINES ON AIRSTAIR DOOR AFT DRAG ANGLE IAW REO 670-52-11-072 PER CRJ 700 NDTM 51-20-006. NO DEFECTS NOTED. 09/30/08 VTJ7010159, COMPLIED WITH STEPS 4 THRU 13 PER REO 670-52-11-072. SM7017032 JOB COMPLETE. SUPPLEMENT AL SDR CLOSED 10/15/08. 2 L 7 2 4F RT A21EA 20081020 NM 2008 10 20 UPS08M53524 1 20080516 A 5753 HINGE DOUG MD11 MD11F 3023600 NM RT WING TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A RT WING O/B FLAP I/B AFT HINGE UPPER MOUNTING CENTER BORE CORRODED. RT WING O/B FLAP I/B AFT HINGE UPPER MOUNTING CENTER BORE CORROSION REMOVED AS PER BSOPM 20-11-02 AND FOUND WITHIN DWG ARC 1984 LIMIT. 2 L 7 3 4F RT A22WE 20081020 EU 2008 10 20 F3LA200800624 1 20080925 A 5321 D5367520200600 FLOOR PANEL AIRBUS A318 A318111 3940019 EU FUSELAGE DEBONDED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 808FR 29 3038 DURING C1 C-CHECK, INSPECTION NOTED THE TOP SKIN OF FLOOR PANEL 151DH WAS DISBONDED FROM THE CORE. DAMAGE WAS FOUND TO BE BEYOND REPAIRABLE LIMITS. MX REMOVED AND REPLACED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 AMM 53-42-14-400-001. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT 20081020 EU 2008 10 20 F3LA200800627 1 20080925 A 5321 D5367520200400 FLOOR PANEL AIRBUS A318 A318111 3940019 EU FUSELAGE DEBONDED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 808FR 29 3038 DURING C1 C-CHECK, INSPECTION NOTED THE TOP SKIN OF FLOOR PANEL 151CH WAS DISBONDED FROM THE CORE. DAMAGE WAS FOUND TO BE BEYOND REPAIRABLE LIMITS. MX REMOVED AND REPLACED THE FLOOR PANEL IAW THE REQUIREMENTS OF A318 AMM 53-42-14-400-001. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT 20081021 NM 2008 10 21 USAA920081746 1 20080910 A 5311 65C323941 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT - MAJOR REPAIR, CRACK ON FUSELAGE FRAME INNER CHORD AT LOWER END BS 601, 17R. REPAIRED FUSELAGE FRAME INNER CHORD B S 601, 17R IAW US AIRWAYS EA 100637 & B737 SRM 53-62-01. 2 L 7 2 4F RT A16WE 20081021 NM 2008 10 21 USAA920081766 1 20080825 A 5311 90526911 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN - MAJOR REPAIR - C18 CHECK, CRACKED FRAME, BS 500A, S9L AND S9R. REPAIRED FRAME, BS 500A, S9L AND S9R IAW US AIRWAY S TASK CARD M1C53002. 2 L 7 2 4F RT A16WE 20081022 EA 2008 10 22 ASOA200801226 1 20080926 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED AND REPLACED PASSENGER DOOR EXIT, TO OPEN, OPEN, RED ARROW AND RED STRIPE PLACARDS IAW CRJ 200 AMM 11-30-00-400- 801. SUPPLEMENTAL SDR CLOSED 10/15/08. 2 L 7 2 4F RT A21EA 20081022 WP 2008 10 22 DHLA200800113 1 20081015 A 2822 11230311 PUMP DOUG DC8 DC873 302199C WP GE CFM56 CFM562C 13802 NE NR 1 FAILED A DHLA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 GL 05 873SJ 5496 2216 46091 AT 45 MINUTES FROM SJU AT FL370 NR 1 ENGINE QUIT DURING DESCENT. AT FL250 DID AN INFLIGHT ENGINE RESTART. RESOLUTION D ESCRIPTION: COMPLIED WITH T/S AS PER CFMI M/M 71-00-00 FAULT 51. NO DEFECTS NOTED. PERFORMED MAX ASSURANCE RUN IAW AS TAR JRH CHAP 11. ALL PARAMETERS WITHIN SPEC'S. SEE ITEM NR 2D LOG A022268 FOR RELATED WORK. ITEM 2D LOG A022268: REF DMI 33864 DURING ENG START AFTER BLOCKOUT NR 1 ENG FEED PUMP PRESS LIGHT ILLUMINATED. ALL 3 C/B'S POPPED SHORTLY AFTER . ABNORMAL PROCEDURES ACCOMPLISHED. RESOLUTION DESCRIPTION FOR ITEM 2D: REMOVED AND REPLACED NR 1 FEED PUMP IAW DC-8 MM 28-10-6 T/R 28-114 OPS CHECK GOOD THIS CLEARS DMI 33864. 2 L 7 4 4F 4 F RT 4A25 E2GL 20081022 NM 2008 10 22 ABXA200810160251 1 20080917 A 5711 114T0222 SPAR BOEING 767 767281 1385109 NM LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 793AX 23143 LEFT WING LOWER L/E WING SPAR WAS CORRODED I/B OF TAI DUCT, APPROXIMATELY WS 433. WING SPAR WAS REPAIRED IAW REA B657-5 7753. 2 L 7 2 4F RT A1NM 20081022 EA 2008 10 22 COMA0860383 1 20080907 A 5330 SB601R53615063 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 430CA 7461 LT INTERNAL BONDED DOUBLER SKIN CRACKED AT STA 640. REPAIRED IAW REO 601R-53-61-506 AT ST 640 BETWEEN STR 8L AND STR 13 L. (K) 2 L 7 2 4F RT A21EA 20081022 EA 2008 10 22 TRAX200801247 1 20080930 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 976EV 7601 ASD UPPER TOP STEP CRACKED ON AFT SIDE. R&R ASD UPPER TOP STEP IAW 52-11-00. 2 L 7 2 4F RT A21EA 20081022 NM 2008 10 22 SWAA085588 1 20081013 A 3350 300432 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 923WN 36627 DURING SCHEDULED MV2 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 USAABB08160 1 20081014 A 3350 20121 CHARGER BOEING 767 767201 1385125 NM CABIN FAULTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 249AU 23901 BCN - THE EMERGENCY PATH LIGHTING WAS FOUND INOPERATIVE BETWEEN SEATS 1B AND 8B. MAINTENANCE REPLACED THE BATTERY CHARG ER. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A1NM 20081023 NM 2008 10 23 HALA0800812 1 20081016 A 3610 SWITCH BOEING 767 7673G5 1385126 NM BLEED AIR SYS MALFUNCTIONED A HALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 585HA 24257 ETOPS SIGNIFICANT SYSTEM - AFTER ENGINE START L ISN VALVE EICAS & OVERHEAD LIGHT ON. RTN TO GATE. PER FIM 36-10-00 RES ET SW AND OPS CHECKED OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20081023 NM 2008 10 23 NOC2008F00005 1 20080921 A 2400 BUSS BOEING 757 75728A 1384976 NM OVERHEATED A NOCA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 15 750NA 26277 ACFT DIVERTED TO STL, SMOKE IN COCKPIT EMERGENCY DECLARED CAPT REPORTS THE RT ACFT BUSS OVERHEATED ITEM REMAINS OPEN. (K ) 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 HALA0800813 1 20081006 A 5347 SEAT TRACK BOEING 767 7673CB 1385187 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 592HA 33468 LEVEL 2 CORROSION ON SEAT TRACKS BS 1208 - 1428, RBL 88.5. REMOVED CORROSION IAW SRM 51-10-02, REV 11, CORROSION OUTSID E LIMITS PER 53-00-02 FIG 101. 2 L 7 2 4F RT A1NM 20081023 NM 2008 10 23 UIEA200800309 1 20080916 A 5311 146U7756U2 FRAME BOEING 747 747230B 1384889 NM BS 1780 CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 512MC 21220 MAIN DECK CARGO COMPARTMENT SIDEWALL FRAME AT BS 1780 AT S12R HAS A 6.0 INCH CRACK, TOTAL WIDTH OF FRAME. INTERIM REPAI R ACCOMPLISHED IAW SRM 51-30-02 EO NR 4753B208 AND FORM 8110-3. REQUIRES INITIAL AND REPEAT INSPECTIONS AT EVERY C-CHEC K INTERVALS. (K) 2 L 7 4 4F RT A20WE 20081017 EU 2008 10 17 UPS08153556 1 20080926 A 5321 B5327086300200 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU CARGO BAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 154UP 0840 INSPECTION TYPE:5 YR MAIN CARGO FLOORBOARD 221BG IS CRACKED ON EACH SIDE. REPAIRED MAIN CARGO FLOORBOARD 221BG REF A300 -600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081023 EA 2008 10 23 COMA0860391 1 20080915 A 3297 17300205 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 940CA 7048 RECEIVED GEAR DISAGREE MSG ON T/O. NLG DID NOT RETRACT. PERFORMED QRH FOR GEAR DISAGREE. EMERGENCY DECLARED, A/C RETURNE D BACK AND LANDED SAFELY. REMOVED AND REPLACED NLG WOW NR 2 WIRE HARNESS. (K) 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 UIEA200800333 1 20081011 A 2612 51224001 ELEMENT BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE NR 2 ENGINE FALSE ACTIVATION A UIEA F B A ACTIVATE FIRE EXT. EMER. DESCENT UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 540MC 22508 517353 DURING CLIMBOUT AT 17000 FEET NR 2 ENGINE FIRE WARNING BELL AND LIGHT CAME ON. ACCOMPLISHED CHECKLIST, BOTH FIRE BOTTLE S WERE DISCHARGED, HYD PUMP SUPPLY OFF FOR 1 HOUR AND 30 MINUTES NR 2 FIRE WARNING LIGHT AND NACELLE TEMP STAYED AT 7.9 AND 8.9 AFTER BLOCK IN. TROUBLESHOT TO HARD FAULTS ON STRUT AREA FORWARD DETECTOR ELEMENT, REPLACED ELEMENTS AND REPLAC ED FIRE BOTTLES. ALL OPS CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E23EA 20081023 NE 2008 10 23 EGI2008F00003 1 20080925 A 2612 FIRE DETECTOR SKRSKY S76 S76C 8143008 NE CARGO BAY FALSE INDICATION E EGIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 09 760EH 760709 DURING TRAINING FLT, DURING TAXI, CARGO BAY FIRE LIGHT ILLUMINATED TWO TIMES AND EXTINGUISHED. DURING NORMAL TAKEOFF C ARGO BAY FIRE LIGHT ILLUMINATED WITH SMOKE IN COCKPIT AND CABIN. LANDED AND IMMEDIATELY NOTIFIED MX. MFG TECH TROUBLE SHOOTING, DISCREPANCIES FOUND. ACFT ALLOWED TO SIT OVERNIGHT AT ENGINEERING SUGGESTION. ACFT GROUND RUN NEXT MORNING FOR 30 MINUTES AT FULL OPERATING RPM WHILE CYCLING AIR CONDITIONER OFF AND ON, COULD NOT DUPLICATE. ACFT FLOWN 1.2 HOUR S WITH NO DEFECTS NOTED. ACFT RELEASED FOR SERVICES MFG ENGINEERING RECOMMENDATIONS. (K) 1 G 7 2 3U NC H1NE 20081023 EA 2008 10 23 COMA0860386 1 20080911 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS MALFUNCTIONED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 720SW 7297 EMERGENCY LIGHTS AFT OF ROW 8 WILL NOT ILLUMINATE. REPLACED LIGHT AFT OF ROW 8 AND REPLACED ASSOCIATED POWER CONNECTOR. NO FURTHER DEFECTS. (K) 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 UIEA200800308 1 20080916 A 5754 65B393001 SKIN BOEING 747 747230B 1384889 NM KRUEGER FLAP CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 512MC 21220 LT WING LEADING EDGE KRUEGER FLAP LOWER IB SIDE PANEL AT WING STA 323.00 TO 330.00 HAS A 7.0 INCH COMPOSITE CRACK. PERMA NENT REPAIR ACCOMPLISHED IAW SRM 51-40-09, FIG 3, SHEETS 1, 4 AND 8, PREPEG 250 DEGREES F CURE IAW SRM 51-40-12. ALSO, R EFERENCE EO NR 4757A464. 2 L 7 4 4F RT A20WE 20081023 NM 2008 10 23 USA2008F00032 1 20080915 A 3397 WIRE BOEING 737 7374B7 138449C NM EMERGENCY LIGHTS BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 452UW 24979 MAINT REPORTED THE SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 20 TO 25 INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE. SPLICED WIRES TOGETHER. OPERATIONAL CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 UPS08553576 1 20080930 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 CORROSION FOUND ALONG UPPER I/B SURFACE OF SEAT TRACK AT FASTENER HOLES, BS 1200 - BS 1180, RBL 25. REMOVED CORROSION, BLENDOUTS WENT OUT OF LIMITS. REPAIRED SEAT TRACK PER ER 757-5340-30805-A AND ATS ER 08-3105. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 UPS08553596 1 20080930 A 5347 SEAT TRACK BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 CORROSION FOUND ALONG UPPER O/B SURFACE OF SEAT TRACK AT FASTENER HOLES BS 1184-1197 RBL 45 WL 208. REPAIRED PER ATS ER 08-3097 DATED 13OCT08. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 UPS08553607 1 20080930 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 CORROSION FOUND ALONG UPPER SURFACE OF FLOORBEAM AT FASTENER HOLES BS 1200 RBL 15 INSTALLED NESTE D ANGLES REPAIR IAW ATS ER 08-3101. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 UPS08553609 1 20080930 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 CORROSION FOUND ALONG UPPER SURFACE OF FLOORBEAM AT FASTENER HOLES BS 1200 RBL 48 TO RBL 51. FLAP PE ENED, ALODINE, PRIME, APPLIED SEALANT IAW ATS ER 08-3101. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 UPS08553611 1 20081001 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 FLOORBEAM AT BS 1100 BL 0 - LBL 65 WL 208 IS CORRODED AT NUT PLATE HOLES. REPAIRED PER ATS ER 08-310 3 DATED 14OCT08. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 UPS08553612 1 20081001 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 425UP 25370 INSPECTION TYPE:C2 FLOORBEAM AT BS 1200 BL 0 TO LBL 65 WL 208 IS CORRODED AT NUT PLATES. FLAP PEENED, ALODINED, PRIMED, APPLIED SEALANT IAW ATS ER 08-3101. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 UPS08M53600 1 20081007 A 5712 RIB DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:1C RT WING FIXED L/E RIB XOS 1113 CRACKED LWR AFT END. STOP DRILLED, FABBED AND INSTALLED REPAIR DOUBLE R IAW SRM 57-00-01 FIG 3, VOL 1 57-00-1 PG 9, SRM VOL 2. 51-21-01 PG 1, VOL 2, 51-33-01 PG 29. 2 L 7 3 4F RT A22WE 20081023 NM 2008 10 23 UPS08M53602 1 20081007 A 5730 SPLICE DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:1C LT WING L/E SKIN SPLICE STRAP XFS 791 CRACKED. FABBED AND INSTALLED REPAIR DOUBLER IAW, SRM, 51-33-0 1 VOL 2 PG 1, DWG ARB3954, 51-33-01 PG 29. 2 L 7 3 4F RT A22WE 20081023 NM 2008 10 23 USA2008F00033 1 20080910 A 2560 MV10 MEGAPHONE BOEING 737 7373G7 138447J NM AFT CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 155AW 23777 MAINT REPORTED THE AFT CABIN MEGAPHONE INOPERATIVE. MAINT REMOVED AND REPLACED THE AFT CABIN MEGAPHONE. OPS CHECK GOOD . (K) 2 L 7 2 4F RT A16WE 20081023 EA 2008 10 23 COMA0860388 1 20080914 A 3234 7455025 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA MLG FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 21 932CA 11705 7038 ON CLIMBOUT, LANDING GEAR WOULD NOT RETRACT, WITH IB A SKID AND P-BRAKE CAUTION MSG`S. EMERGENCY DECLARED A/C RETURNED BACK AND LANDED SAFELY. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE. (K) 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 RYN2008F00022 1 20081001 A 5410 NOSE COWL BOEING 727 727232 1384082 NM NR 3 NACELLE DENTED A RYNA O OTHER O OTHER NR NOT REPORTED 1 GL 31 727NY 20646 NR 3 ENGINE NOSE COWL HAS DENT AT 5 OCLOCK POSITION, LEADING EDGE. REMOVED DENTED AREA AND ACCOMPLISHED NOSE COWL LEADIN G EDGE LIP SKIN REPAIR IAW SRM 54-30-1, 54-30-3, AND 51-30-2, 51-20-00, 51-31-00. (K) 2 L 7 3 4F A3WE 20081023 NM 2008 10 23 RYN2008F00023 1 20081001 A 5510 STRUCTURE BOEING 727 727232 1384082 NM HORIZONTAL STAB CORRODED A RYNA O OTHER O OTHER NR NOT REPORTED 1 GL 31 727NY 20646 RT HORIZONTAL STABILIZER TRAILING EDGE UPPER CHORD HAS CORROSION AT STABILIZER STA 189.68. REPLACED UPPER CHORD AT RT HO RIZONTAL STABILIZER TRAILING EDGE IAW SRM 51-10-1 AND 51-30-3. (K) 2 L 7 3 4F A3WE 20081023 NM 2008 10 23 2008UALA06117 1 20081014 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 EMERGENCY BATTERIES DISCHARGE QUICKLY AT DOOR 1 LT AND DOOR 1 RT. BATTERIES ARE DEFECTIVE. REPLACED BATTERY PACKS, OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081023 NM 2008 10 23 UPS08M53637 1 20081016 A 3010 DUCT DOUG MD11 MD11F 3023600 NM LT WING LEAKING A IPXA J A DUMP FUEL UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 275UP 48774 INSPECTION TYPE:N/A DIVERSION - LT WING ANTI ICE DISAGREE. *SUPPLEMENTAL SDR* PERFORMED TROUBLESHOOT AS PER FIM 30-11- 01 & FOUND AIR LEAK FROM LT WING TELESCOPE DUCT AT WING SIDE. INSTALLED MISSING BOLT, NUT, WASH, SLIPPER SEAL, PACKING & RING AS PER AMM 30-11-01-4. OPS & LEAK CHECKS OK. PRECAUTIONARY CHECKED RT WING TELESCOPE DUCT, FOUND ALL BOT & NUT ARE SECURED. 2 L 7 3 4F RT A22WE 20081023 EA 2008 10 23 SWIA200820180 1 20080609 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 461SW 7811 RT FS 640 FRAME AFT SIDE CRACKED IN BEND RADIUS BELOW STR 9R (C-CHECK). REPLACED IN CONJUNCTION WITH SB 601R-53-059 MOD IFICATION. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 SWIA200820181 1 20080609 A 5230 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 461SW 7811 CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED (C-CHECK). REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 2008UALA06124 1 20081014 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 FWD PIT STA 660 FRAME DENTED ABOUT STR 245. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME & INSTALLED DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081023 NE 2008 10 23 IXX2008F00096 2 20080916 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE NR 2 FLAMED OUT A IXXA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 11 823BX 46064 DURING CRUISE AT 36,000 FT WITH POWER REDUCTION NR 2 ENGINE FLAMED OUT, WITH 1-2 PSI OIL PRESSURE ATTEMPTED INFLIGHT RES TART, NO FUEL FLOW AND NO IGNITION. THE CREW PERFORMED INFLIGHT ENGINE SHUTDOWN PROCEDURE. THE CREW LANDED WITHOUT FURT HER INCIDENT. OPEN (K) 2 L 7 4 4F 4 F RT 4A25 E2GL 20081023 WP 2008 10 23 EIA2008049 1 20080913 A 5312 PRESSURE PANEL DOUG DC3 DC3 3021401 WP LT MLG WW CORRODED A EIAA O OTHER O OTHER NR NOT REPORTED 1 NM 19 490 1954 LT MAIN GEAR W/N FWD WALL LOWER IB EDGE HAS CORROSION, ANGLE HOLDING STEAL HAS 100 PERCENT MATERIAL LOSS. WEB CORRODED A T BS 1253 LBL 16- LBL 46. WEB REPAIRED IAW SUPPLEMENTAL WORKSHEET. CORRODED SEAL RETAINER REPLACED SRM 51-30-42 REF NRC NR 112 AND SUPPLEMENTAL WORKSHEET. (K) 2 L 7 2 4R A669 20081023 NM 2008 10 23 KCSA081485 1 20080922 A 5347 SEAT TRACK BOEING 747 747221F 1384868 NM BS 1910 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 748CK 21744 AFT PIT SEAT TRACK CRACKED AT BS 1910, RBL 46. (K) 2 L 7 4 4F RT A20WE 20081029 NM 2008 10 29 08FDEA04554 1 20081026 A 5330 651821849 SKIN BOEING 727 727233 138408A NM ZONE 200 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 221FE 20932 REPAIR AT STA 440 STR 10L NOT IAW SRM. REMOVED PREVIOUS REPAIR AND CUTOUT DAMAGED AREA DIMS 12" BY 9" IAW WITH EA 7-533 0-126855 HFEC INSPECTED EDGE OF CUTOUT AND .040 INSURANCE CUT AND EXISTING HOLES FREE OF CRACK INDICATIONS IAW NDTM 51-0 0-00. FABRICATED DOUBLER REPAIR, TRIPLER, FILLER, & 3 EACH SHIMS. INSTALLED REPAIR PARTS IAW EA 7-5330-126885. 2 L 7 3 4F RT A3WE 20081029 NM 2008 10 29 08FDEA04555 1 20081026 A 5330 651842011 SKIN BOEING 727 727227 1384078 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 491FE 21529 DENT STA 324 STR 23L EVALUATED DENT AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA DIMS 7/8 INCH B Y 7/8 INCH. FABRICATED FILLER USING 2024-T3 .040 DIMS 7/8" BY 7/8" AND DOUBLER AND INSTALLED REPAIR PARTS IAW SRM 53-30 -3 FIG 13 AND 51-30-2. 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 08FDEA04557 1 20081026 A 5313 STRINGER BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 AFT LOWER CARGO COMPARTMENT STA 950F, 4 INCHES STR 27L, STRINGER CORRODED AT FASTENER. REMOVED DAMAGED SECTION OF STRIN GER, INSTALLED STRINGER REPAIR SPLICE SRM 51-10-1 AND 53-10-03 AND 51-30-02. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081029 EA 2008 10 29 ASOA200801213 1 20080922 A 5220 HINGE FITTING CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED AND REPLACED RT HINGE ARM ON CREW ESCAPE HATCH IAW CRJ 200 AMM 52-22-00-820-801 STEP B1A-E. PRESSURE AND TOLERA NCE CHECKS DUE ON CREW ESCAPE HATCH. PRESSURE TOLERANCE CHECKS GOOD IAW CRJ 200 MM 21-32-00-863-801 AND 52-22-00-220-80 2. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081029 NM 2008 10 29 08FDEA04560 1 20081027 A 5720 651928715 ANGLE BOEING 727 7272D4 138407U NM ZONE 600 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 PANEL RACK-PANEL 8805 CRACKED RIGHT WING OB AILERON REMOVED SEAL ANGLE, TRANSFERRED HOLES TO NEW ANGLE P/N 65-19287-15. INSTALLED ANGLE REF SRM 51-30-2 PG 1-10. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081029 WP 2008 10 29 08FDEA04562 1 20081027 A 5347 6044987075T651 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 68050 47804 MCDECK SEAT TRACK AT STA 1089 LBL 48 IS DAMAGED, REMOVED FLOORBOARDS FOR ACCESS. REMOVED SEAT TRACK, FABRICATED NEW TRA CK. INSTALLED NEW TRACK AND REINSTALLED FLOORBOARDS IAW SRM 51-31-01, SRM 53-70-00 AND MAE TRAVELER T8/766008. MAJOR R EPAIR AND RII. 2 L 7 3 4F RT A22WE 20081029 WP 2008 10 29 08FDEA04563 1 20081027 A 5347 6044987075T65 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 373FE 46611 CABIN FLOOR SEAT TRACK AT STA 1119-1180, LBL 47 HAVE SEVERAL GOUGES AROUND CROWN HOLES EDGE BLENDED AREAS FOUND 1129 T HROUGH 1180 IN LIMITS. TREATED AND PRIMED IAW SRM 53-70-00 FIG 5 AND SRM 51-21-01. FOUND AREAS AT 1119 THROUGH 1129 OU T OF LIMITS. REMOVED AND REINSTALLED FLOOR PANEL FOR ACCESS. REMOVED SEAT TRACK SECTION AND INSTALLED NEW SEAT TRACK W ITH SPLICES ALL IAW SRM 53-70-00 FIG 5, SRM 51-31-01 AND MAE TRAVELERS T8/763092 AND T8/763091. MAJOR REPAIR RII 2 L 7 3 4F RT A22WE 20081029 WP 2008 10 29 08FDEA04565 1 20081027 A 5347 601096418 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 373FE 46611 MCD SEAT TRACK RBL 28 STA 615 GOUGED AT CROWN REMOVED AND REINSTALLED 5 FLOOR PANEL FOR ACCESS. REMOVED AND REPLACED SE AT TRACK AND SPLICES AT STA 575 THROUGH 630 AT RBL 28 ALL IAW AMM 53-21-08-2, SRM 51-31-01, SRM 53-70-00 FIG 5, MAE TRAV ELERS T8/763440 AND T8/763461. MAJOR REPAIR RII. 2 L 7 3 4F RT A22WE 20081029 EU 2008 10 29 08FDEA04568 1 20081027 A 5321 B5327052000200 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 CABIN FLOOR PANEL BETWEEN FRAMES 31 - 34 AND LBL 78 - 97 HAS HOLES ON THE BOTTOM. FABBED NEW PANEL 241 EF USING THE OLD PANEL AS A TEMPLATE. LOCATED & COUNTER BORED THE HOLES; POTTED; CURED & SANDED THE EDGES. POTTED & CURED THE INSER TS. PART MARKED & APPLIED NON-SKID TAPE IAW DWG SRZ 25-005. 2 L 7 2 4F RT A35EU 20081029 EU 2008 10 29 08FDEA04570 1 20081027 A 5321 B5327000400400 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 CABIN FLOOR PANEL BETWEEN RBL 85 - 78 AND FRAMES 45-46 HAS A HOLE IN THE BOTTOM. FABBED NEW PANEL 242 XJ USING THE OLD PANEL AS A TEMPLATE. LOCATED & COUNTER BORED THE HOLES; POTTED; CURED & SANDED THE EDGES. POTTED & CURED THE INSE RTS. PART MARKED & APPLIED NON-SKID TAPE IAW FEDEX DWG A300-600 SRZ 25-005; REV" G ". 2 L 7 2 4F RT A35EU 20081029 NM 2008 10 29 08FDEA04495 1 20081023 A 5753 ARC0503503 HINGE BRACKET DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER ATTACH OUTBOARD HOLE AFT MATING SURFACE FOUND WITH CORROSION . CORROSION REPAIRED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081029 EU 2008 10 29 08FDEA04572 1 20081027 A 5321 B5327062400000 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 FLOOR PANEL 241 RJ IS CRACKED. LOCATED & COUNTER BORED PANEL. POTTED, CURED & SANDED THE EDGES. POTTED & CURED INSER TS. PART MARKED & APPLIED THE NON-SKID TAPE IAW DWG SRZ 25-005. 2 L 7 2 4F RT A35EU 20081029 WP 2008 10 29 08FDEA04573 1 20081027 A 5347 601096418 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 373FE 46611 MCD SEAT TRACK AT RBL 46 STA 1341 IS GOUGED. REMOVED AND REPLACED SEAT TRACK AT RBL 46 STA 1331 THROUGH 1351 WITH SPLIC ES IAW SRM 53-70-00 FIG 5, SRM 51-31-01, AND MAE TRAVELERS T8/763348 AND T8/763347. MAJOR REPAIR RII. 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 08FDEA04574 1 20081027 A 5330 SKIN BOEING 727 727227 1384078 NM BS 180 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 491FE 21529 DENT AROUND FASTENER STA 180 FWD OF LWR NOSE COMPT CUT-OUT. REMOVED FASTENER AT STA 180 LWR NOSE IAW SRM 51-30-2, FOUND AREA TO HAVE OIL CAN CONDITION AND OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUT OUT DAMAGE AREA, DIM 1 INCH BY 1 INCH IAW SRM 53-30-3 FIG 13. FABRICATED FILLER AND DOUBLER IAW SRM 53-30-3 FIG 13. TREATED AND PRIMED AREA AND DOUBLER REPAIR I AW SRM 51-10-20. INSTALLED DOUBLER REPAIR IAW SRM 53-30-3 FIG 13 AND 51-30-2. 2 L 7 3 4F A3WE 20081029 WP 2008 10 29 08FDEA04575 1 20081027 A 5347 601096418 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 373FE 46611 MAIN DECK FLOOR SEAT TRACK HAS 4 GOUGES ON UPPER CROWN AT STA 675 LBL 47. REMOVED AND REINSTALLED FLOOR PANELS FOR ACCE SS. REMOVED AND REPLACED SEAT TRACK AND SPLICES AT STA 665 THROUGH 685 LBL 47 AL IAW SRM 53-70-00 FIG 5, SRM 51-31-01, AMM 53-21-08-2 AND MAE TRAVELERS T8/763463 AND T8/763462. MAJOR REPAIR RII. 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 2008UALA06246 1 20081022 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 AFT CARGO COMPT, FRAME AT BS 1500 LT AND STR 25L HAS A DENT AT INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMA GED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 EU 2008 10 29 2008UALA06248 1 20081022 A 2622 BA21758 FIRE BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AFT LAVATORY UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 410UA 463 AFT LAV WALL FIRE EXTINGUISHER FELL OUT OF BRACKET. SECURED BOTTLE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081029 NM 2008 10 29 2008UALA06249 1 20081022 A 3350 20131A BATTERY PACK BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 924UA 26645 EMERGENCY LIGHTS FLOOR ROW 9-15 EXIT INOPERATIVE. REPLACED M1577 BATTERY PACK AND EMERGENCY LIGHTS CHECK NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20081029 NM 2008 10 29 2008UALA06250 1 20081023 A 5320 SPLICE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 820UA 898 BEAM 170 AT AFT SPLICE HAS CORROSION. REMOVED BEAM NR 170. NEW BEAM FASTENED TO ACFT FRAME. NEED TO INSTALL AFT SPLIC ES. COMPLETED INSTALLATION OF BEAM 170. 2 L 7 2 4F 4 F RT A28NM E40NE 20081029 NM 2008 10 29 2008UALA06251 1 20081023 A 5320 BEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 820UA 898 BEAM 175 CORRODED, NEEDS REPLACEMENT. REMOVED BEAM NR 175. GALLEY MOUNT BRACKETS WERE TRANSFERRED TO NEW BEAM. BEAM I S FASTENED TO ACFT FRAME. NEED TO INSTALL FWD AND AFT SPLICES. COMPLETED INSTALLATION OF BEAM 175. 2 L 7 2 4F 4 F RT A28NM E40NE 20081029 NM 2008 10 29 DL757081400 1 20081021 A 5321 143N53663 FLOOR PANEL BOEING 757 757232 1384965 NM BS 635-650 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 FWD CARGO BAY BILGE FIXED FLOOR PANEL UPPER SURFACE CORROSION AT STATION 635 TO 650 LBL 19. REPAIRED ON NR 00065 PER DE LTA ERA 470939-14 AND ATS ER 08 3281. 2 L 7 2 4F RT A2NM 20081029 NM 2008 10 29 DL76L081401 1 20081021 A 2160 VALVE BOEING 767 767332 1382001 NM CABIN TEMP MALFUNCTIONED A DALA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 174DN 24802 RTB - DUE FWD CABIN TEMP CONTROL EICAS MSG. TEMP CONTROL FWD CABIN INOP LIGHT ILLUMINATED. NO MEL RELIEF BY FCP/C MTC CLOSED FWD TRIM VALVE AND RELEASED PER MEL 21-61-04A. 2 L 7 2 4F RT A1NM 20081029 NM 2008 10 29 DL757081402 1 20081013 A 5320 FLOOR SUPPORT BOEING 757 757232 1384965 NM BS 1510 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 CORROSION ON Z STRINGER LOWER SURFACE AT NUTPLATE LOCATION LBL 7.5 B/S 1510. REPAIRED ON CUSTOMER CARD 00069. 2 L 7 2 4F RT A2NM 20081029 NM 2008 10 29 CALA0800976 1 20081016 A 5320 65C3397035 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 INTERCOSTAL BETWEEN STATION 344 TO STATION 360 LBL 10 CRACKED AROUND FASTENER HOLES. REMOVED AND REPLACED ANGLE AT STA 344 TO STA 360 LBL 10 PER B737 SRM 51-40-02 AND 53-10-51. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0801005 1 20081022 A 5330 65C323593 SKIN BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59630 27534 AIR CONDITONING ACCESS CUTOUT DAMAGED ON FUSELAGE, 1 INCH CRACK ON LEFT SIDE AND COMING LOOSE AT PREVIOUS DOUBLER ON AFT SIDE. INSTALLED INTERIM REPAIR TO FUSELAGE SKIN AT STATION 540 S-28R PER ECRA 5331-01427 AND INITIATED A DIP WHICH REA DS BEFORE THE ACCUMULATION OF 79,053 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM AN INSPECTION PER PART 2 OF ECRA 5331-01427. 53-DIP, CNTL 90817. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 UPS08653755 1 20081026 A 5753 113T3000 SKIN BOEING 767 76734AF 1385212 NM TE FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 304UP 27242 INSPECTION TYPE:N/A RT O/B FLAP LWR SKIN DELAMINATION D368856. REPAIRED IAW SRM 51-70-10-2R. 2 L 7 2 4F RT A1NM 20081029 WP 2008 10 29 UPS08853563 1 20080923 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV FLUSH REPAIR BS 151, 8 INCHES BELOW L21L HAS CLOSE FASTENER SPACING. ACCOMPLISHED IAW DALFORT AVIATI ON REPAIR XEA X8-53-706 AND REFERENCE DC8-73F SRM 53-2-0 FIG 1C PG 10 10 OF 14. 2 L 7 4 4F RT 4A25 20081029 WP 2008 10 29 UPS08853623 1 20081005 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV RT WING LEADING EDGE LOWER DOUBLER I/B SIDE OF NR 4 PYLON NEED VALIDATION AT STA XFS 500. DOES NOT M EET CRITERIA IN APPENDIX H STEP 5. 894-W4- 32 AREA PREVIOUSLY REPAIRED FEF SRM 57-3-1 T/R 57-83. 2 L 7 4 4F RT 4A25 20081029 EA 2008 10 29 ASOA1252 1 20080930 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 INSTALLED PAX DOOR PROX SW PX-25. ADJUSTED AND OPS CHECK GOOD PER CRJ 700 AMM 52-70-04-820-802-AO2. REMOVED MID CAP IA W CRJ 700 SRM CH 51-42-00. REMOVED PAX DOOR PROX SWITCH. REMOVED & REPLACED FLOOR SUPPORT FWD CAP IAW SRM 51-42-06 CRJ 700. INSTALLED FLOOR SUPPORT MIDCAP IAW CRJ 700 SRM 51-42-00. INSTALLED PAX DOOR PROX SW PX-25 ADJUSTED AND OPS CK GO OD PER CRJ 700 AMM 52-70-04-820-802-A02. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 ASOA200801156 1 20080910 A 5320 REPAIR CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REPAIRED FS 559 CAP ANGLES, AND WEB FROM LBL 18 TO LBL 9 AND RBL 18 TO RBL 9 IAW REO 601R-53-41-260 AND REO 601R-53-41-7 82 DEVIATION ON RT SIDE. C/W ASA ECTC'S REO 601R-53-41-782 AND 601R-53-41-260 BY ACCOMPLISHING BOMBARDIER REO'S 601R-53 -41-782 AND 601R-53-41-260. /25/08 (9/26/08 RM) ASA RII C/W BY 5300044. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 ASOA200801176 1 20080916 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REPAIRED LT FS 621.00 FLOOR SUPPORT ANGLE IAW BOMBADIER REO 601R-53-61-117 REV C. ALL STEPS OF REO ARE COMPLETE. FASTE NERS THRU LT FS 621.00 FLOOR SUPPORT ANGLE AND BULKHEAD REQUIRE PRESSURIZATION LEAK CHECK. LEAK CHECK GOOD AT FS 621.00 . BULKHEAD IAW CRJ 200 AMM 21-32-00-863-801. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081030 NM 2008 10 30 QXEA200801022 1 20080924 A 3010 DEICE SYSTEM DHAV DHC8 DHC8202 2809007 NM HORIZ STAB MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 19 352PH 494 FLIGHT 2078. DIVERTED TO RDM FOR LT HORIZONTAL STABILIZER DE-ICE CAUTION LIGHT. DIVERSION DUE TO PENDING CLOUDS AND ICE CONDITIONS. MAINTENANCE REPLACED THE LEADING EDGE 332CL. CHECKS GOOD. RETURNED TO SERVICE. (K) 2 H 7 2 4T RT A13NM 20081030 WP 2008 10 30 08FDEA04607 1 20081029 A 3234 HANDLE DOUG DC10 DC1030F 3023504 WP MLG MALFUNCTIONED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 21 310FE 48299 ON DEPARTURE FROM MEM, GEAR HANDLE WOULD NOT MOVE TO UP POSITION. RAN QRH PROCEDURE FOR GEAR HANDLE WILL NOT MOVE TO UP POSITION UNABLE TO RAISE GEAR HANDLE, RETURNED TO MEM. 2 L 7 3 4F RT A22WE 20081030 WP 2008 10 30 08FDEA04596 1 20081028 A 5320 AFA71321C SUPPORT FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 373FE 46611 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 HOLES "C" AND "D" INDICATED CRACKED DURING HFEC INSPECTION REMOVED AND R EINSTALLED FRAME , INTERCOSTALLS, BRACKET AND WEB. REMOVED AND REPLACED FITTING. FABRICATED AND INSTALLED BUSHINGS AND REPAIR DOUBLER ALL IAW SRM 51-31-01, SRM 53-50-00 FIG 17, SRM 53-12-01 AND MAE TRAVELER T8/764446. MAJOR REPAIR RII. 2 L 7 3 4F RT A22WE 20081030 NM 2008 10 30 08FDEA04597 1 20081028 A 5753 652167229 ANGLE BOEING 727 7272D4 138407U NM ZONE 500 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 LEFT WING OTBD L/E, CRACKS IN INBD AND OTBD REINFORCEMENT ANGLES AT FWD FASTENERS LOCATIONS ABOVE NR 2 SLAT ACTUATOR LWR FAIRING. REMOVED INBD AND OTBD REINFORCEMENT ANGLES, MFG NEW ANGLES REF DWG 65-21672 PGS 1- 3 USING A63549 FOR ANGLE M ATERIAL PRIMED AND INSTALLED ANGLES REF SRM 51-30-02 AND SRM 51-10-2. REINSTALLED SLAT ACTUATOR FAIRING NR 2 REF SRM 51 -30-2 PG 1-7. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081030 WP 2008 10 30 08FDEA04598 1 20081028 A 5414 AUB70363 PANEL DOUG MD10 MD1010F 3022112 WP NR 3 NACELLE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 NR 3 PYLON PANEL 488 GL IS CHAFED IN SEVERAL AREAS. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01. FABRICATED REPAIR DOUBLERS IAW SRM 54-00-01. TREATED & PRIMED REPAIR DOUBLERS IAW SRM 51-21-01. INSTALLED REPAIR DOUBLERS IAW SR M 51-31-01. 2 L 7 3 4F RT A22WE 20081030 NM 2008 10 30 08FDEA04599 1 20081028 A 5310 655614815 CREASE BEAM BOEING 727 7272D4 138407U NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 PNL RACK, MAIN DECK CREASE BEAM WEB UPPER SURFACE BS 1000-1006 LBL 68 HAS CORROSION. REMOVED DAMAGED PARTS PER REF SR M 51-30-02, FABRICATED NEW PARTS REF DWG 65-56148-15 AND -23. TREATED AND PRIMED PER REF SRM 51-10-3. INSTALLED NEW PART S PER REF SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 08FDEA04609 1 20081029 A 5320 FLOOR SUPPORT BOEING 727 7272D4 138407U NM ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 LOWER FWD CARGO PIT, FLOOR SUPPORT STRINGER IS BENT WITH A CRACK ON SIDE STA 720C 10", LBL 8 INCH. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 08FDEA04611 1 20081029 A 5315 6520827171 FLOORBEAM BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 UPPER LOBE FLOORBEAM 520, RBL 45 LOWER LEG CORRODED REMOVED CORROSION REF: SRM 51-10-1, P1-27. MATERIAL REMOVED IS BEYO ND LIMITS: REF; P- F SRM 53-10-1, PAGE 6. FABRICATED REPAIR PARTS, REF: P/F SRM 53-10-8, PAGES 8-17. TREATED AND PRIM ED REPAIR PARTS, REF:SRM 51-10-2. INSTALLED REPAIR PARTS, REF, SRM 51-30-2, P.1-27. THIS IS CLASSIFIED AS A MAJOR REPA IR. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 EIAA2008102800073 1 20081027 A 5313 STRINGER BOEING 747 747132 1384882 NM CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 20653 BODY SKIN FOUND BULGED UP AT BS 2150 TO 2170 S49R AND STRINGER CRACKED. REMOVED DAMAGED STRINGER. REPAIR FABRICATED, A LODINED AND PRIMED. INSTALLED PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 DL757081426 1 20081017 A 5320 146N5456 CHANNEL BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE BS 1460-1480 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 728754 WEB AT BS RBL CORRODED. REMOVED AND REPLACED WEB PN 146N5456-2, CHANNEL AT BS 1460 PN 146N5458-6, CHANNEL BS 1480 PN 14 6N5458-5 IAW SRM 51-40-02, SRM 51-30-01, DWG 146N5458. 2 L 7 2 4F 4 F RT A2NM E17NE 20081030 NM 2008 10 30 DL757081427 1 20081017 A 5315 146N54588 FLOORBEAM BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE BS 1460 RBL 11 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 728754 FLOOR SUPPORT BRACKET AT BS 1460 RBL 11 CORRODED. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-02, SRM 51-30-01, DWG 146N5458. 2 L 7 2 4F 4 F RT A2NM E17NE 20081030 NM 2008 10 30 DL757081428 1 20081017 A 5322 146N54584 SHEAR TIE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE BS 1460 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 728754 FLOOR SUPPORT BRACKET AT BS 1460 RBL 11-15 IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT BRACKET IAW SRM 51-40-02, DW G 146N5458, SRM 51-30-01. 2 L 7 2 4F 4 F RT A2NM E17NE 20081030 NM 2008 10 30 K11A2008102772201 1 20080821 A 5322 SHEAR TIE BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 FRAME SHEAR TIE 2 INCHES BY 2 INCHES CORROSION STA 950D, BETWEEN STR 26L AND 27L FRAME SHEAR TIE. 2 L 7 3 4F RT A3WE 20081030 EA 2008 10 30 SWIA200820230 1 20080616 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 625 S13 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 492SW 7168 STRINGER CLIP AT STA 625 BETWEEN STRINGER 14 CRACKED. C-CHECK, REPLACED CLIP. 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 SWIA200820231 1 20080616 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 492SW 7168 PASSENGER DOOR AFT ANCHOR FITTING CRACKED. C-CHECK, REPLACED FITTING. 2 L 7 2 4F RT A21EA 20081030 WP 2008 10 30 AALA200802619 1 20080926 A 5340 39521721 MOUNT DOUG DC9 DC983 3022083 WP GALLEY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON MOUNT AT GALLEY NUMBER TWO. AREA OF DISCREPANCY IS 1.5 INCHES WIDE BY 5 INCHES LONG. INSTALLED MOUN T IN ACCORDANCE WITH SRM 51-01. 2 L 7 2 4F RT A6WE 20081030 WP 2008 10 30 AALA200802620 1 20080926 A 5340 993653U57 FITTING DOUG DC9 DC983 3022083 WP ZONE 900 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON GALLEY NUMBER TWO TIE DOWN FITTING INBOARD OF SEAT TRACK NR 4. AREA OF DISCREPANCY WAS 3 INCHES BY 1 INCH. REPLACED TIE DOWN FITTING IN ACCORDANCE WITH SRM 51-01. 2 L 7 2 4F RT A6WE 20081030 WP 2008 10 30 AALA200802622 1 20080925 A 5310 TAB DOUG DC9 DC983 3022083 WP DOOR FRAME CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CRACK FOUND ON TAB ON FORWARD ENTRY DOOR JAMB STRAP AT LONGERON 11 LEFT. AREA OF DISCREPANCY IS ONE INCH BY ONE INCH. CRACK LENGTH IS 0.5 INCH. INSTALLED REPAIR STRAP OVER CUT OUT OF DAMAGED TAB IN ACCORDANCE WITH AARD 53-10-00-11. 2 L 7 2 4F RT A6WE 20081030 EA 2008 10 30 SWIA200820236 1 20080622 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA BS 409 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 439SW 7578 VERTICAL BEAM AT FS 409 LBL 27 CRACKED AT INBOARD LOWER RADIUS. C-CHECK, REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 SWIA200820237 1 20080622 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 439SW 7578 LEFT FS 625 OBLIQUE ANGLE CRACKED. C-CHECK, REPLACED ANGLE. 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 SWIA200820238 1 20080622 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 439SW 7578 CRACKED WEB ON FLOOR ANGLE AT FS 280 LBL 9 LOWER FLANGE. C-CHECK, REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 SWIA200820239 1 20080622 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 439SW 7578 FS 280 FLOORBEAM ATTACH CLIPS AT LBL 9 ARE CRACKED. C-CHECK, REPLACED CLIPS. 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 SWIA200820240 1 20081024 A 3350 AD20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCHARGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 862AS 9415 9415 7476 FLT 3870 - SEVERAL EMERGENCY CABIN LIGHTS INOP. REPLACED NR 1 EMERGENCY LIGHTING BATTERY, PN AD-2013-1A SN ON 60763 SN OFF 43074. 2 L 7 2 4F RT A21EA 20081030 NM 2008 10 30 EIAA2008102800061 1 20081027 A 5347 SEAT TRACK BOEING 747 747273C 1384896 NM BS 520 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 MAIN DECK STATION 520, RBL11, WL 200 SEAT TRACK FOUND CRACKED. SEAT TRACK REMOVED AS PER SRM 51-30-02 CRACKED SEAT TRAC K TRIMMED OUT AS PER SRM 51-10-01 NDT CHECK CARRIED OUT AS PER 51-00-00 FIG 23. NO CRACKS REMAIN, NEW SEAT TRACK SPLICE FABRICATED AND INSTALLED PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 DL757081439 1 20081026 A 3350 20131A BATTERY PACK BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 613DL 22820 723843 FOUND SEVERAL EMERGENCY LIGHTS INOP IN PASSENGER COMPARTMENT. REMOVED AND REPLACED L-2 DOOR EMERGENCY LIGHTS BATTERY P ACK, AND RELAMPED SEVERAL EMERGENCY LIGHTS PER AMM 33-51-07-902-001 AND PERFORMED SATISFACTORY OPS CHECK PER AMM 33-51-0 0-715-075. 2 L 7 2 4F 4 F RT A2NM E24NE 20081030 EA 2008 10 30 SWIA200820241 1 20081022 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 702SK 10136 FLT 5931 - CEILING EMERGENCY LIGHT, SECOND FROM BACK, INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081030 SO 2008 10 30 SWIA200820242 1 20081020 A 3260 SENSOR EMB 120 EMB120ER 3260203 SO RT MLG MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 226SW 120296 FLT 5706 - AFTER TAKEOFF, GEAR WOULD NOT RETRACT. REPLACED RIGHT MLG "WOW" SENSOR. 2 L 7 2 4T RT A31SO 20081030 EA 2008 10 30 SWIA200820248 1 20081022 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 806SK 15070 FLT 3912 - EMERGENCY OVERHEAD LIGHT NR 7 IS INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081030 WP 2008 10 30 AALA200802623 1 20080926 A 5340 993061293 FITTING DOUG DC9 DC983 3022083 WP GIRT BAR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON FORWARD GIRT BAR SUPPORT BRACKET AT AFT SERVICE DOOR AT LONGERON 18 LEFT. AREA OF DISCREPANCY WAS TH REE INCHES BY THREE INCHES. INSTALLED NEW FITTING IN ACCORDANCE WITH SRM 51-01. 2 L 7 2 4F RT A6WE 20081030 NM 2008 10 30 DHLA2008745566 1 20081015 A 5315 STRAP BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE AFT CARGO COMPARTMENT FROM BS 1110 TO BS 1130 AT RBL 25 AND RBL 45 STABILIZER STRAP WITH CORROSION. REPL ACED FUSELAGE STABILIZER STRAPS FROM BS 1074 TO BS 1130 AT RBL 25 AND RBL 45 IAW B727 SRM 51-10-1 PARA 7. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 QXEA2008132801097 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4 - RT INBD SEAT TRACK HAS CHAFING FROM APPROX STA X310-X345 IN CHANNEL AND TOP. REMOVED CHAFING FROM TRACK IAW RD 8/4-53-884, FOUND WITHIN LIMITS PER RD 8/4-53-884. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. APPLIED ACID ETCH AND ALODINE IAW RD 8/4-53-884. 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 QXEA20081029 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4 - NR 5 CABIN SEAT TRACK INBD FLANGE IS CORRODED AT STA X70-X72. BLENDED CORROSION AND FOUND TO BE OUT OF LIMIT S. REMOVED AND INSTALLED NEW TRACK REF Q400 SRM 51-40-15 AND 51-42-05. 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 F3LA2008102700695 1 20081027 A 5320 D53470340208 PROFILE AIRBUS A319 A319111 3930336 NM ZONE 100 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE AFT CARGO COMPARTMENT ON PROFILE LOCATED AT BUTT LINE 0, BETWEEN FRAME 56 AND FRAME 57. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2. 2 L 7 2 4F RT A28NM 20081030 EU 2008 10 30 F3LA2008102700685 1 20081027 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU EMERGENCY LIGHTS FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 21 910FR 1781 LINE MAINTENANCE NOTED THAT MULTIPLE EMERGENCY LIGHTS FAILED TO ILLUMINATE IN CABIN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT AT POSITION 11WL IN ACCORDANCE WITH AMM 33-51-38-400-001. ALL EMERGENCY LIGHTS WORK NOR MALLY. 2 L 7 2 4F RT A28NM 20081030 NM 2008 10 30 F3LA2008102700688 1 20081024 A 5320 D5397496600000 PROFILE AIRBUS A319 A319111 3930336 NM ZONE 100 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE AFT CARGO COMPARTMENT LOCATED ON PROFILE AT FRAME 61 BETWEEN STR INGER 38 LEFT AND 38 RIGHT. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2. 2 L 7 2 4F RT A28NM 20081030 NM 2008 10 30 F3LA2008102700694 1 20081024 A 5320 D5397497200200 PROFILE AIRBUS A319 A319111 3930336 NM ZONE 100 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK , INSPECTION NOTED CORROSION IN THE AFT CARGO COMPARTMENT ON PROFILE LOCATED AT FRAME 56 BETWEEN ST RINGER 38 LEFT AND 41 RIGHT. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2 . 2 L 7 2 4F RT A28NM 20081030 NM 2008 10 30 QXEA2008102901113 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4 - NR 12 SEAT TRACK HAS CORROSION FROM STA X201.5 - X200.0. BLENDED OUT CORROSION AND FOUND ALL BLENDS WITHIN L IMITS IAW RD8/4-53-884. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ETCHED AND ALODINED IAW RD8/4- 53-884. 2 H 7 2 4T RT A13NM 20081029 SO 2008 10 29 SWIA200820226 1 20081022 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 586SW 120354 FLT 5773 - ROW 3 OVERHEAD EMERGENCY LIGHT OUT. RELAMPED. 2 L 7 2 4T RT A31SO 20081029 EA 2008 10 29 SWIA200820228 1 20081020 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A SWIA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 07 936SW 7726 FLT 5969 - GEAR DISAGREE WARNING ON SHORT FINAL AFTER GO AROUND, NOSE GEAR FELL DOWN AND LOCKED AFTER ABOUT FOUR MINUTES . REPLACED NOSE GEAR SELECTOR VALVE, PN 750006000 SN ON 0242T SN OFF 2093. 2 L 7 2 4F RT A21EA 20081029 WP 2008 10 29 AALA200802589 1 20080930 A 5350 FRAME DOUG DC9 DC982 3022082 WP TAILCONE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 581AA 53158 CANTED FRAME IN AFT ACCESSORY AT TAIL CONE ALIGNMENT PIN BELOW MAINTENANCE LIGHT SWITCH WAS CRACKED. INSTALLED DOUBLER IN ACCORDANCE WITH ESO 80559 DATED 30 SEP 2008. 2 L 7 2 4F A6WE 20081029 NM 2008 10 29 AALA200802591 1 20080926 A 5320 WEB BOEING 737 737823 13844CB NM BS 992 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 FLOOR STRUCTURE WEB FOUND CORRODED. AREA OF DISCREPANCY IS 1 INCH BY 1 INCH. INSTALLED DOUBLER IN ACCORDANCE WITH SRM 51-70-13-2R. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 DHLA2008745563 1 20080902 A 5230 SKIN BOEING 727 727224 1384076 NM CARGO DOOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 NR 1-45 LOWER FUSELAGE AFT CARGO COMPARTMENT DOOR NR 2 OUTER SKIN WITH DOUBLE HOLES AT BS 950F PLUS 8 INCH BETWEEN UPPER FRAME AND BEAM NR 1. REPAIRED LOWER FUSELAGE AFT CARGO COMPARTMENT DOOR NR 2 OUTER SKIN IAW B727SRM 52-00-3 FIG 4. 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 AALA200802594 1 20080922 A 5311 FRAME BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CRACK FOUND ON FRAME AT LEFT STRINGER AT STATION 480. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH ECO J1159AA. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 DHLA2008745564 1 20080907 A 5340 STRINGER CLIP BOEING 727 727224 1384076 NM ZONE 100 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 NR 1-299 LOWER FUSELAGE AFT CARGO COMPARTMENT BS 1033 STRINGER 25 RT CLIP CRACKED. REPLACED STRINGER CLIP AT BS 1033 S- 25R IAW B727 SRM 51-10-1NPARA 7. 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 AALA200802596 1 20080922 A 5311 FRAME BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CRACK FOUND ON FRAME AT LEFT STATION 867 BETWEEN STRINGER 8 AND 9. INSTALLED DOUBLER REPAIR PER ECO J1159AA. 2 L 7 2 4F RT A16WE 20081029 WP 2008 10 29 UPS08853565 1 20081003 A 5720 STRUCTURE DOUG DC8 DC873F 302199F WP WING MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV, L/E STATION XFS 88 DOUBLER DOES NOT MEET CRITERIA FOR APPENDIX H. REPAIR PREVIOUSLY ACCOMPLISHED PE R DC8 73F SRM 57-2-1 FIG 2H CLASS B. 2 L 7 4 4F RT 4A25 20081029 EA 2008 10 29 SWIA200820190 1 20081013 A 2910 HOSE CNDAIR CL600 CL6002C10 1390015 EA HYD SYSTEM LEAKING A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 07 613SK 10038 FLT 4101 - DURING FLAP RETRACTION AFTER DEPARTURE, NR 2 HYD LOW PRESSURE WARNING. REPLACED SYSTEM NR 2 PRESSURE LINE IN RT PYLON. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA200801382 1 20081022 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 559 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 LT SIDE PRESSURE FLOOR SEAL HAS CORROSION INTERMITTANT FROM FS 409+128 TO FS 559 LBL 36 TO LBL 47. FOUND CORROSION TO B E ONLY LIGHT SURFACE CORROSION WHICH IS WITHIN REPAIR LIMITS IAW SRM 53-61-43. REMOVED CORROSION, PREPPED, PRIMED & PAI NTED DOORS IAW SRM 51-21-06. INVESTIGATED, MAPPED & BLENDED LT SIDE PRESSURE FLOOR SILL CORROSION AREAS IAW REO 601R-53 -41-666. AREA FAILS DIMENSIONAL LIMITS OF EO DUE TO LOCATIONS OF FASTENER HOLES & SPACE BETWEEN AREAS OF CORROSION. EN GINEERING DISPOSITION REQUIRED. REPAIRED CORROSION DAMAGE TO PRESSURE FLOOR PANEL & ANGLES IAW REO 601R-53-41-805. EC/ TC REQUIRED. WORK PERFORMED IAW EC/TC REO 601R-53-41-805. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA200801384 1 20081022 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FS 589-605 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 CARGO BAY FLOOR SUPPORT AT LBL 27 HAS CORROSION (INTERGRANULAR) ON O/B FLANGE FROM FS 589 TO FS 605. FOUND CORROSION TO BE BEYOND ALLOWABLE LIMITS. ANGLE ON FLOOR SUPPORT REQUIRES REPLACEMENT. REMOVED CARGO BAY FLOOR SUPPORT. LOCATED FA STENER LOCATIONS AND INSTALLED NEW SERVICEABLE FLOOR SUPPORT IAW EC/TC 601R-53-61-2883. PRIMED AND PAINTED REPAIRED AR EA IAW SRM 51-25-00. REMOVED AND INSTALLED SAME SERVICEABLE INSULATION IN APPLICABLE AREAS IAW AMM 25-81-02-400-801. 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 EIA2008053 1 20080905 A 5210 SKIN BOEING 747 747132 1384882 NM L3 DOOR CRACKED A EIAA O OTHER O OTHER NR NOT REPORTED 1 NM 19 479EV 19898 L3 DOOR LOWER FWD. CORNER BS 1275 CRACKS IN SKIN FASTENER HOLES. REMOVED DAMAGE, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 479-53-225-2. (K) 2 L 7 4 4F RT A20WE 20081023 EA 2008 10 23 COMA0860390 1 20080912 A 3297 TR17300600000014 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA RT MLG FAILED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 962CA 7123 ON CLIMBOUT, RECEIVED ANTI-SKID CAUTION MSG. EMERGENCY DECLARED, A/C RETURNED BACK AND LANDED SAFELY. REMOVED AND REPLAC ED RT MLG OB ANTI-SKID WIRE HARNESS. (K) 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 USAA920081668 1 20080910 A 5311 BOEING FRAME BOEING 737 7374B7 138449C NM BS 601 S17R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 FUSELAGE FRAME CRACKED ON INNER CHORD AT BS601, S17R. REPAIRED FUSELAGE FRAME INNER CHORD AT BS 601, S17R IAW TYPICAL R EPAIR 53-62-01. (K) 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 USAA920081672 1 20080825 A 5320 654580730 STIFFENER BOEING 737 7373G7 138447J NM BS 289 S11R CRACKED A USAA O OTHER O OTHER NR NOT REPORTED 1 EA 19 311AW 24712 ANGLE STIFFENER CRACKED AT BS 289, S11R, WL253 BELOW R1 DOOR CUT OUT. REPLACED ANGLE STIFFENER AT BS 289, S11R, WL253 B ELOW R1 DOOR CUTOUT IAW EA 13011. (K) 2 L 7 2 4F RT A16WE 20081023 2008 10 23 GLB2008F00032 2 20080915 A 7321 38827309 FCU EMB 120 EMB120ER 3260203 SO ENGINE LEAKING A GLBA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 03 297UX 1172 120297 FUMES, ENROUTE , PILOTS REPORTED A STRONG FUEL ODOR IN THE COCKPIT. MAINT PERFORMED A LEAK CHECK OF THE ENGINE AND APU WITH NO DEFECTS NOTED. MAINT PLACED THE ISSUE ON MEL 49-00-0. PN NR OFF 3882730-9/ SN OFF. D441. LEAK CHECK WAS SUCCESSF UL. (K) 2 L 7 2 4T RT A31SO 20081023 NM 2008 10 23 EIA2008052 1 20080905 A 5240 SKIN BOEING 747 747132 1384882 NM R3 DOOR CRACKED A EIAA O OTHER O OTHER NR NOT REPORTED 1 NM 19 479EV 19898 R3 DOOR LOWER FWD CORNER BS 1275 CRACKS IN SKIN FASTENER HOLES. REMOVED DAMAGE, NOT AREA, FABBED AND INSTALLED REPAIR IA W ECRA 479-53-225-2. 2 L 7 4 4F RT A20WE 20081023 NM 2008 10 23 USA2008F00031 1 20080915 A 3397 WIRE BOEING 737 7373G7 138447J NM EMERGENCY LIGHTS BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 MAINT REPORTED THE EMERGENCY ESCAPE PATH LIGHT ON SEAT ROW 22, LT SIDE, INOPERATIVE. MAINT TROUBLESHOT AND FOUND A BROK EN WIRE. OPERATIONAL CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 20081023 EA 2008 10 23 COMA0960384 1 20080909 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCHARGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 720SW 11812 9679 7297 FLOOR EMERGENCY LIGHTING AFT OF ROW 9 INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK NR 4. (K) 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 YENA2008087 1 20080908 A 2120 UNKNOWN EMB ERJ190 ERJ190100IGW 3260408 NM CABIN ODOR A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 184JB 19000008 STRONG PLASTIC BURNING ODOR, AFTER TAKEOFF UNTIL 3000 FEET. ODOR RETURNED ON DOWN WIND AT 3000 FEET UNTIL TOUCHDOWN. PE RFORMED FIM TASK 21-20-00-801A. NO FURTHER DEFECT NOTED. RAN AIR CONDITIONER (CREW) CAN NOT DUPLICATE ON THE GROUND. AC FT OK TO CONTINUE. (K) 2 L 7 2 4F RT A57NM 20081023 EU 2008 10 23 YENA2008090 1 20080918 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU CABIN ODOR A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 562JB 1948 PASSING 8000 FEET ON CLIMB OUT, PASSENGER AND CREW DETECTED AN ODOR ORIGINATING IN THE AREA OF ROW 4, ODOR WAS NOTICED F ROM FLIGHT DECK TO ROW 20. AIRCRAFT RETURNED FOR INSPECTION. ODOR DECREASED AFTER LANDING. LANDING WEIGHT 138,000 LBS . PERFORMED TASK 24-00-00-810-823 AND TASK 23-39-810-801. NO DEFECTS NOTED. REPLACED RECIRCULATION FILTER PRECAUTIONA RY IAW AMM 21-21-41. NO OTHER DEFECTS NOTED AIRCRAFT OK FOR SERVICE. (K) 2 L 7 2 4F RT A28NM 20081023 NM 2008 10 23 KCSA081487 1 20080922 A 5320 SUPPORT ANGLE BOEING 747 747122 1384872 NM BS 1640 S23R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FUSELAGE FRAME SUPPORT T-DAMAGED AT BS 1640, STR 23R. (K) 2 L 7 4 4F RT A20WE 20081023 NM 2008 10 23 USAA920081670 1 20080825 A 5320 654580724 STIFFENER BOEING 737 7373G7 138447J NM BS 289 S13R CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 ATTACH ANGLE CRACKED ABOVE WEB AT R-1 DOOR CUTOUT AT BS 289, S13R, WL 235. REPLACED ATTACH ANGLE ABOVE WEB AT R-1 DOOR CUTOUT AT BS 289, S13R, WL 235 IAW EA NR 130111. (K) 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 USAA920081675 1 20080909 A 2560 P2070003001 FLASHLIGHT BOEING 737 7373G7 138447J NM ZONE 200 INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 FORWARD FLIGHT ATTENDANT FLASH LIGHT IN-OP. REPLACED FORWARD FLIGHT ATTENDANT FLASH LIGHT. (K) 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 USA2008F00029 1 20080913 A 3397 WIRE BOEING 737 7374B7 138449C NM EMERGENCY LIGHT BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 MAINTENANCE REPORTED THE EMERGENCY ESCAPE PATH LIGHTING FROM SEAT ROWS 19 TO 25, LT SIDE, INOPERATIVE. MAINT REPAIRED WIRING AT SEAT ROW 25 IAW STANDARD PRACTICES. EMERGENCY LIGHTING OPERATIONALLY CHECKS SATISFACTORY. (K) 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 QXEA200801014 1 20080921 A 3260 401020101 PROXIMITY SENSOR BOMBDR DHC8 DHC8402 1390042 NM MLG MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 19 425QX 4039 SEA FLIGHT 2387 YYJ-SEA. ENROUTE RECEIVED A LG INDICATION MALFUNCTION. PERFORMED A ALTERNATE GEAR EXTENSION AND UNEVENT FUL LANDING. REPLACED THE PROX SENSOR. CHECKS GOOD. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081023 NM 2008 10 23 AALA200802433 1 20080923 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 DFW EMERGENCY LIGHT AT SEAT 40C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 40C. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT T00001SE 20081023 WP 2008 10 23 AALA200802435 1 20080924 A 4900 GTCP8598DHF APU DOUG DC9 DC983 3022083 WP APU BAY LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 9620D 53591 INFLIGHT T4XG/24SEP CREW REPORTED NOXIOUS FUMES IN CABIN AND COCKPIT. COCKPIT CREW USED OXYGEN MASKS. RETURNED TO MCI AND LANDED WITHOUT INCIDENT. REPLACED AUXILIARY POWER UNIT (APU) AND PERFORMED PACK BURN OUT. SYSTEM GROUND CHECKED NO RMAL OPS. 2 L 7 2 4F RT A6WE 20081023 EA 2008 10 23 TRAX200801246 1 20080930 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 PAX DOOR HARD TO OPEN. LUBRICATED PAX DOOR. CHECKS GOOD. REF AMM 52-11-13. PAX DOOR WHEEL WAS STIFF. CKS GOOD AT TH IS TIME. 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 AALA200802373 1 20080916 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 DFW EMERGENCY LIGHT EXIT SIGN AT LT NR 3 DOOR HAS 1 LAMP INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT EXIT SIGN AT LT NR 3 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081023 NM 2008 10 23 AALA200802412 1 20080922 A 7711 L954007 PROBE BOEING 757 757223 1384957 NM NR 1 ENGINE DAMAGED A AALA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 21 690AA 25696 LAX INFLIGHT T824/22SEP. CREW REPORTED NR 1 ENGINE PRESSURE RATIO PROBLEMS AFTER TAKEOFF. RETURNED TO LAX AND LANDED W ITHOUT INCIDENT. FOUND PROBE MOUNT FLANGE BROKEN AND PNEUMATIC TUBE AND MOUNT BROKEN. ALSO FOUND NOSE COWL CRACKED. R EPLACED PROBE SENSOR AND MOUNTING PLATE, PNEUMATIC TUBE AND MOUNT, AND NOSE COWL. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 AALA200802425 1 20080923 A 3350 LAMP BOEING 737 737823 13844CB NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 974AN 30098 DFW EMERGENCY LIGHT AT RT FORWARD OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHTS AT RT FORWARD OVERWING. SYS TEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081023 2008 10 23 USAA920081856 4 20081010 A 2565 LANYARD AIRBUS 320 A320214 3930316 EU ESCAPE SLIDE MISROUTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 113UW 1141 PIT A12 EES LT AFT DOOR HAS IMPROPER ROUTING OF WHITE AND YELLOW LANYARDS ON ESCAPE SLIDE RAFT. PIT. RE-ROUTED LANYARD S ON LT AFT DOOR IAW US AIRWAYS JOB CARD 26L00025011. 2 L 7 2 4F RT A28NM 20081023 WP 2008 10 23 AALA200802369 1 20080915 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 580AA 53157 DFW EMERGENCY LIGHT AT SEAT ROW 21 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 21. SYSTEM GROUND CHECK ED NORMAL OPS. 2 L 7 2 4F A6WE 20081023 NM 2008 10 23 QXEA200800926 1 20080817 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 410QX 4053 PDX C4 CHECK LOWER FUSELAGE EXTERNAL SKIN HAS NICK AT STA X11.0 BETWEEN STRINGERS 24R. BLENDED OUT DAMAGE WITH SCOTCH B RITE PAD. HFEC INSP IAW Q400 NDTM PT 6, 51-00-01, NO CRACKS NOTED. MAX MATERIAL REMOVED .006. OUT OF LIMITS IAW RD8/4 -53-505. MAPPED FOR ENGINEERING. BLENDED AREA IS WITHIN LIMITS IAW RD 8/4-53-2455. PAINTED IAW 400 SRM 51-25-05. 2 H 7 2 4T RT A13NM 20081023 WP 2008 10 23 AALA200802370 1 20080915 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 580AA 53157 DFW EMERGENCY LIGHT AT SEAT ROW 21 MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 21. SYSTEM GROUND C HECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081023 NM 2008 10 23 AALA200802424 1 20080923 A 3350 LAMP BOEING 737 737823 13844CB NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 974AN 30098 DFW EMERGENCY LIGHT AT LT FORWARD OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHTS AT LT FORWARD OVERWING. SYS TEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 QXEA200800915 1 20080817 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 410QX 4053 PDX C4 CHECK. RT INBD SEAT TRACK NR 14 IS CORRODED BETWEEN X584 AND X590. BLENDED CORROSION REF RD8/4-53-884 PG 6 NOTE 1. MAX MATERIAL REMOVED INNER CHANNEL .021", UPPER CLAW SURFACE NEGLIGIBLE PER RD 8/4-53-884 PG 2 FIG A-A. HFEC INSPE CTED IAW RD 8/4-53-884 NOTE 2 AND D8 400 NDTM PT 6, 51-00-01, NO CRACKS NOTED. ALODINED PER RD 8/4-53-884 PG 3. 2 H 7 2 4T RT A13NM 20081023 NM 2008 10 23 QXEA200800925 1 20080817 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 410QX 4053 PDX C4 CHECK. LOWER FUSELAGE EXTERNAL SKIN HAS NICK AT STA X1.0 BETWEEN STRINGERS 31R AND 32R. BLENDED OUT DAMAGE WITH SCOTCH BRITE PAD. HFEC INSP IAW Q400 NDTM PT 6, 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECK IAW Q400 NDTM PT 1, 51- 00-04 HI .060" LO .057. OUT OF LIMITS IAW RD8/4-53-505. MAPPED FOR ENGINEERING. INSPECTED BLENDED AREA FOUND TO BE WI THIN LIMITS IAW RD 8/4-53-666. PAINTED IAW 400 SRM 51-25-05. 2 H 7 2 4T RT A13NM 20081023 NM 2008 10 23 AALA200802413 1 20080922 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 187AN 32381 DFW EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. REPLACED DAMAGED PIN AT SIDEWALL CONNECTOR FOR EMERGENCY LIGHT AT SEAT 26D . SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081023 EA 2008 10 23 TRAX200801249 1 20080930 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 L/H 280 FLOOR SUPPORT BEAM CORRODED. 2 L 7 2 4F RT A21EA 20081023 EU 2008 10 23 MAL2008F00044 1 20080926 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 389 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 340B424 DURING THE 2Y AND N4K NOTED DENT IN RT FUSELAGE AT STA 389. REPAIRED IAW EO# S53009. 2 L 7 2 4T RT A52EU 20081023 WP 2008 10 23 AALA200802368 1 20080915 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 580AA 53157 DFW EMERGENCY LIGHT AT SEAT ROW 21 MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 21. SYSTEM GROUND CHECK ED NORMAL OPS. 2 L 7 2 4F A6WE 20081023 NM 2008 10 23 USAA920081851 1 20081009 A 5315 6546810 FLOORBEAM BOEING 737 7374B7 138449C NM BS 208 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03C10853029/005 LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM T-CAP AT BS208 LBL29 THRU RBL29. RE PAIRED FLOORBEAM T-CAP AT BS208 LBL29 THRU RBL29 REPAIR NR 53-10-05B. 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 AALA200802432 1 20080923 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 DFW EMERGENCY LIGHT AT SEAT 31C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31C. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT T00001SE 20081023 EA 2008 10 23 TRAX200801253 1 20080930 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 BS 280 WEB CORRODED. 2 L 7 2 4F RT A21EA 20081023 EU 2008 10 23 MAL2008F00042 1 20080926 A 5220 SKIN SAAB SF340 340B 7860101 EU EMERGENCY EXIT DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 340B424 DURING THE 2Y AND N4K NOTED 2 DENTS NOTED IN RT OVERWING EXIT EXTERIOR SKIN. REPAIRED IAW EO S52028 & S52139. 2 L 7 2 4T RT A52EU 20081023 WP 2008 10 23 AALA200802422 1 20080923 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 556AA 53086 LGA EMERGENCY LIGHT AT SEAT 4D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 4D. SYSTEM GROUND CHECKED NORMA L OPS. 2 L 7 2 4F A6WE 20081023 NM 2008 10 23 AALA200802415 1 20080922 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 187AN 32381 DFW EMERGENCY LIGHT EXIT SIGN AT LT NR 7 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT EXIT SIGN AT LT NR 7 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081023 NM 2008 10 23 KCSA081509 1 20081002 A 5730 SKIN BOEING 747 747122 1384872 NM LT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 LT WING STA 700 NR 4 AFT BOOST PUMP CUT OUT CORRODED. 2 L 7 4 4F RT A20WE 20081023 NM 2008 10 23 AALA200802427 1 20080923 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 792AN 30253 DFW EMERGENCY LIGHT AT SEAT 21G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT T00001SE 20081023 NM 2008 10 23 ASAA0843602 1 20081014 A 5210 6552873525 HINGE BOEING 737 7374Q8 138447Q NM L2 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 765AS 25102 F/A'S REPORT L2 HARD TO OPEN. LUBRICATED L2 DOOR GUIDE PLATES & DOOR HINGES AS REQUIRED. L2 DOOR CHECKS NORMAL, REFERE NCE MM 12 25 11. 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 ASAA0843594 1 20081001 A 5320 652072637 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 FWD CARGO BAY RT INTERCOSTAL STR 25R STA 500 500A CRACKED AT NUT PLATE HOLE. REMOVED INTERCOSTAL, LOCATED, DRILLED NEW INTERCOSTAL, INSTALLED NEW INTERCOSTAL IAW B737 400 SRM 51 40 02 05. 2 L 7 2 4F RT A16WE 20081023 NM 2008 10 23 WX0A070240 1 20081001 A 3350 2031A BATTERY PACK DOUG MD80 MD83 3023681 NM CABIN DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 876G 53469 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETUR NED TO SERVICE. 2 L 7 2 4F RT 20081023 NM 2008 10 23 WX0A070241 1 20081001 A 3350 AD4002 BATTERY DOUG MD80 MD83 3023681 NM CABIN DISCHARGED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 876G 53469 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETUR NED TO SERVICE. 2 L 7 2 4F RT 20081023 EA 2008 10 23 MASA2008101700734 1 20081017 A 5240 PIN CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BROKEN A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 37342 7342 ASH FLT 1004 OFF-HNL. SERVICE DOOR PIN BROKEN. MX REPLACED SERVICE DOOR PIN AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 MASA2008101700735 1 20081017 A 3350 1317 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 513MJ 10111 ASH FLT 7146 SAV. ONE CEILING EMERGENCY FLOOD LIGHTS INOP ON RIGHT AND LEFT SIDE. MX RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 MASA2008101700736 1 20081017 A 3350 BATTERY CNDAIR CL600 CL6002D24 1390016 EA CABIN DISCHARGED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 924FJ 15024 ASH 2656 ATL-CLT. CAPT FOUND EMERGENCY LIGHTS WEAK UPON FIRST START UP OF THE DAY. CHARGED EMERGENCY LIGHTS WITH AIRCR AFT POWER, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081023 EA 2008 10 23 MASA2008101800737 1 20081018 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 27314 7314 ASH FLT 7301 IAD-ROC. EMERGENCY FLOOR PATH LIGHTING INOPERATIVE AT ROW 2. MAINTENANCE REPLACED LIGHT STRIP. 2 L 7 2 4F RT A21EA 20081023 NM 2008 10 23 MASA2008101900738 1 20081019 A 3350 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 988HA 426 ASH 2897 DRO-PHX. CAPTAIN REPORTED AFTER LANDING THAT NR 3 FLOOR EMERGENCY LIGHT STRIPS INOP. MX RELAMPED EMERGENCY LI GHT. 2 H 7 2 4T RT A13NM 20081027 NE 2008 10 27 M7KA0815084417 2 20080901 A 7261 0292817460 LABYRINTH SEAL UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENGINE LEAKING D M7KA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 19 853MH 190 4417 46027 ENGINE SMOKING FOLLOWING REDUCTION OF POWER TO FLIGHT IDLE WAS THE OBSERVED SYMPTOM. CLOSER INSPECTION REVEALED TRACES O F OIL STREAKING FROM POWER TURBINE BLADE ROOTS. A SERVICEABLE LABYRINTH RING ASSEMBLY HAS BEEN INSTALLED. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 EU 2008 10 27 M7KA0812084142 1 20080901 A 6310 SEAL UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE FREEWHEEL UNIT LEAKING E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 822MH 3430 3729B 4142 23179 FOUND LEAKING EXCESSIVELY BOTH STATICALLY AND IN OPERATION DURING ROUTINE INSPECTION. INSTALLED NEWLY OVERHAULED FREE WH EEL SHAFT ASSY WITH NO FURTHER LEAKAGE NOTED. TEAR DOWN OF REMOVED ASSY REVEALED SEAL LIP HAD BEEN DAMAGED DURING ASSY. AS THE SHAFT WAS REPORTED TO BE INSTALLED FOR TEST CELL ENGINE. RUNS IT SEEMS ODD THE LEAK WAS NOT DISCOVERED AT THE OVE RHAUL FACILITY. THIS IS THE SECOND TIME A NEWLY OVERHAULED ENGINE WAS INSTALLED THAT HAD A DAMAGED SEAL WHEN RECEIVED FR OM THE FACTORY. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 EU 2008 10 27 M7KA0730084173 1 20080901 A 3340 CIRCUIT BOARD UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE EXTERIOR LIGHTS FAILED E M7KA O OTHER O OTHER NR NOT REPORTED 1 WP 19 824MH 306 P020629 4173 23209 POSITION LIGHTS FAILED TO ILLUMINATE WITH CIRCUIT BREAKER IN CLOSED POSITION AND NO APPARENT OPENS OR SHORTS IN THE WIRE HARNESS. INVESTIGATION REVEALED THAT THE PCB TRACE FOR THE POSITION LIGHT SWITCH POWER HAD MELTED MUCH AS A FUSE BLOWS. THIS IS NOT AN UNCOMMON PROBLEM FOR THIS PART. SUGGEST A CLOSE LOOK AT THE CURRENT PATH FOR THIS CIRCUIT TO SEE WHY THE CIRCUIT BREAKER PROTECTION FAILS TO PROTECT THE SWITCH PANEL PERHAPS A MORE ROBUST CIRCUIT TRACE IS REQUIRED ON THE PCB FOR THIS CIRCUIT. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20081027 EA 2008 10 27 SWIA200820191 1 20081018 A 3213 AXLE CNDAIR CL600 CL6002B19 1900309 EA LT MLG CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 LEFT MLG AXLE REQUIRES REPLACEMENT DUE TO CORROSION. C-CHECK, INSTALLED LEFT MLG AXLE. 2 L 7 2 4F RT A21EA 20081027 NM 2008 10 27 DL757081350 1 20081012 A 5311 FAILSAFE BOEING 757 757232 1384965 NM FS 900 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 604DL 22811 FOUND FAILSAFE STRAP ON THE RT SIDE OF THE FS 900 BULKHEAD CORRODED. REMOVED AND REPLACED DAMAGED STRAP PER BLUEPRINT. 2 L 7 2 4F RT A2NM 20081027 NM 2008 10 27 DL75E081354 1 20081010 A 2910 HYDRAULIC SYSTEM BOEING 757 7572Q8 1384972 NM RIGHT SYS OVERSERVICED A DALA D RETURN TO BLOCK W J INADEQUATE Q C WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 704X 28163 ON TAXI OUT R HYD SYSTEM PRESSURE AND BRAKE SOURCE EICAS LIGHT ILLUMINATED AND R SYS PRESS OVERHEAD LIGHT ILLUMINATED AL L BRAKE PRESSURE INDICATE NORMAL. FOUND RT HYD SYS OVER SERVICED. DRAINED RT HYD SYS TO PROPER LEVEL. REMOVED AND REP LACED RT HYD SYS PRESSURE SWITCH S32 PER AMM LEAK CHK GOOD RT HYD PRESSURE LIGHT AND SYS NOW CHK NML. 2 L 7 2 4F RT A2NM 20081027 WP 2008 10 27 08FDEA04442 1 20081020 A 7830 BRACKET DOUG MD10 MD1010F 3022112 WP THRUST REVERSER BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 NR 1 ENGINE INBD T/R UPPER FWD STOP BRACKET IS BROKEN. REMOVED BUMPER & BRACKET IAW CF-6 ENGINE MANUAL 78-32-03; PG 40 9; 405. LOCATED & DRILLED UP BUMPER P/N 3111M84P001A & P/N 3110M30P001A IAW ENGINE MANUAL 78- 32-03; FIG 405; PG 40 9. INSTALLED BUMPER & BRACKET IAW ENGINE MANUAL 78-32- 03; FIG 405; PG 409. 2 L 7 3 4F RT A22WE 20081027 EU 2008 10 27 USAA920081731 1 20080922 A 3397 CONNECTOR AIRBUS A319 A319112 3930323 EU CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 742PS 1275 FLT NR 1210 - DFW-PHX, EMERGENCY EXIT SIGN ABOVE THE LEFT PAX EXIT DOES NOT ILLUMINATE. FOUND CONNECTOR DISCONNECTED. RECONNECTED CONNECTOR 7245VC TO THE POWER SUPPLY. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081027 NM 2008 10 27 QXEA200800949 1 20080820 A 5330 DOUBLER BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 410QX 4053 PDX - C CHECK, CORROSION ON DOUBLER WHERE VHF NR 3 ANTENNA IS MOUNTED STA X331 TO LOWER FUSELAGE. DOUBLER CORROSION OUT OF LIMITS. REMOVED DOUBLER IAW Q400 SRM51-40-07. MATCH DRILLED NEW DOUBLER ALODINED HOLES AND INSTALLED REF Q400 SRM 51-42-05 AND 51-23-00. PREPPED PRIMED AND PAINTED IAW 8-400 SRM 51-25-10 AND 51-25-15. 2 H 7 2 4T RT A13NM 20081027 NM 2008 10 27 USAA920081729 1 20080915 A 5315 654583469 STRAP BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - C18 - MAJOR REPAIR, FLOORBEAM STABILIZER STRAP CRACKED AT BS 312, LBL11.10. REPAIRED FLOORBEAM STABILIZER STRAP A T BS 312, LBL 11.10 IAW B737 SRM 53-10-51-2R4 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 QXEA2008102201068 1 20081002 A 5320 PANEL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX-C4-CORROSION AROUND SOME OF THE FASTENERS FOR CARGO BAY PANEL 144GZ. REMOVED MINOR SURFACE CORROSION PER Q400 SRM 5 1-14-00. ALODINED AND PRIMED AREA IAW SRM 51-25-10 AND 51-21-10. 2 H 7 2 4T RT A13NM 20081028 NM 2008 10 28 QXEA2008102201069 1 20081002 A 5320 PANEL BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX-C4- CORROSION AROUND SOME FASTENERS FOR CARGO BAY PANEL 144HZ. REMOVED MINOR SURFACE CORROSION PER Q400 SRM 51-14-0 0. ALODINED AND PRIMED AREA IAW Q400 SRM 51-21-10 AND 51-25-10. 2 H 7 2 4T RT A13NM 20081028 NM 2008 10 28 QXEA2008102201070 1 20081002 A 5320 PANEL BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX-C4- CORROSION AROUND SOME OF THE FASTENERS FOR CARGO BAY PANEL 144JZ. BLENDED OUT CORROSION PER Q400 SRM 51-14-00, ALODINED PER SRM 51-21-00. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01 NO CRACKS NOTED. PRIMED AREA IAW Q400 SRM 51- 25-10. 2 H 7 2 4T RT A13NM 20081028 NM 2008 10 28 QXEA2008102201071 1 20081002 A 5320 STRUCTURE BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX-C4- BLENDED OUT CORROSION PER Q400 SRM 51-14-00, ALODINED PER Q400 SRM 51-21-10. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. PRIMED AREA AT BLENDS IAW Q400 SRM 51-25-10. 2 H 7 2 4T RT A13NM 20081028 NM 2008 10 28 QXEA2008102201073 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 LT INBOARD SEAT TRACK HAS CORROSION INSIDE THE CHANNEL FROM STA X644 TO X688. BLENDED OUT CORROSION REF RD 8/4-53-884. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ETCHED ALODINED AREAS IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 20081028 EU 2008 10 28 USAA920081894 1 20081011 A 5753 SKIN AIRBUS 320 A320231 3930325 EU RT WING TE FLAP DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 620AW 052 PHX-RON MAJOR REPAIR. RT WING TRAILING EDGE WEDGE DISBONDED APPROX 3 INCHES FROM TRAILING EDGE AND 40 INCHES FROM INBD EDGE. REPAIRED RT WING TRAILING EDGE IAW A320 SRM 57-53-00, PAGE 253, PARAGRAPH M. FIGURE 211. 2 L 7 2 4F RT A28NM 20081028 NM 2008 10 28 USAA920081864 1 20081010 A 2121 EVT3454HC FAN AIRBUS A319 A319132 3930340 NM FAILED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 824AW 27456 27456 1490 FLT 440 PHX-DCA BURNING ODOR. DURING CRUISE, HEARD A LOUD RUMBLING NOISE ALONG WITH ELECTRICAL ODOR. SHUT OFF BLOWER F AN TO OVERRIDE. NOISE AND ODOR STOPPED. POPS BLOWER FAN CIRCUIT BREAKER BEHIND FIRST OFFICER. SWAPPED BLOWER FAN WITH EXTRACT FAN. R & R COOLING EXTRACT FAN. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081028 NM 2008 10 28 USAA920081895 1 20080909 A 5340 693535214 STRINGER CLIP BOEING 737 7373G7 138447J NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN C18 MAJOR REPAIR NR 6131871. STRINGER CLIP CRACKED AT BS 867, S9L. REPLACED STRINGER CLIP AT BS 867, S9L IAW B737 SRM 51-40-02-OG. 2 L 7 2 4F RT A16WE 20081028 EA 2008 10 28 QXEA200800903 1 20080728 A 5522 SKIN CNDAIR CL600 CL6002C10 1390015 EA RT ELEVATOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK. RT ELEVATOR UPPER SKIN ON AFT OTBD CORNER REQUIRES A PERMANENT REPAIR. REMOVED DAMAGE AS REQUIRED PER RE O 670-55-21-058. HFEC INSPECTED IAW REO 670-55-21-058 NOTE 4 AND NDTM PT 1, 51-20-006. NO CRACKS NOTED. FABRICATED UP PER AND LOWER REPAIR DOUBLERS AND PACKERS. LOCATED, DRILLED AND COUNTERSUNK DOUBLERS, PACKERS AND WEDGE FILLER. ALODIN ED AND PRIMED IAW REO 670-55-21-058. INSTALLED REPAIR IAW REO 670-55-21-058. 2 L 7 2 4F RT A21EA 20081028 NM 2008 10 28 AALA200802481 1 20080919 A 5743 115A52119 TRUNNION BOEING 737 737823 13844CB NM LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 TUL LT MLG TRUNNION FITTING CORRODED AT UPPER INBD HOLE OUTER FACE. AREA OF DISCREPANCY IS 2 INCHES BY 2 INCHES WITH A .119 INCH DEPTH. REMOVED CORROSION, TREATED, PRIMED, AND INSTALLED NEW BUSHING PER SRM 57-20-90-R2-2. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 AALA200802480 1 20080919 A 5743 115A521110 TRUNNION BOEING 737 737823 13844CB NM RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 TUL RT MLG TRUNNION FITTING CORRODED AT LOWER INBD HOLE OUTER FACE. AREA OF DISCREPANCY IS 2 INCHES BY 2 INCHES WITH A .120 INCH DEPTH. REMOVED CORROSION, TREATED, PRIMED, AND INSTALLED NEW BUSHING PER SRM 57-20-90-R2-2. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 USAA200802485 1 20080919 A 5743 115A52119 TRUNNION BOEING 737 737823 13844BZ NM LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 TUL LT MLG TRUNNION FITTING CORRODED AT LOWER OTBD HOLE OUTER FACE. AREA OF DISCREPANCY IS 2 INCHES BY 2 INCHES WITH A .042 INCH DEPTH. REMOVED CORROSION, TREATED, PRIMED, AND INSTALLED NEW BUSHING PER SRM 57-20-90-R2-2. 2 L 7 2 4F RT A16WE 20081028 WP 2008 10 28 AALA200802514 1 20080924 A 5320 S2932222 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 176 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 TUL FLOORBOARD SUPPORT IS WORN AND CRACKED AT STATION 176. AREA OF DISCREPANCY IS 2 INCHES BY 26 INCHES WITH A DEPTH OF 20 PERCENT PLUS. CRACK LENGTH OF 1 INCH. REPLACED FLOORBOARD SUPPORT PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081028 NM 2008 10 28 AALA200802486 1 20080919 A 5743 115A521110 TRUNNION BOEING 737 737823 13844CB NM RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 RT MLG TRUNNION FITTING CORRODED AT UPPER INBD HOLE OUTER FACE. AREA OF DISCREPANCY IS 2 INCHES BY 2 INCHES WITH A .127 INCH DEPTH. REMOVED CORROSION, TREATED, PRIMED AND INSTALLED NEW BUSHING PER SRM 57-20-90-R2-2. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0843619 1 20080916 A 5330 65C337533 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 DURING HEAVY MAINTENANCE WHILE ACCOMPISHING INSPECTIONS OF R1 DOOR LOWER CUTOUTS PER EM 5330 02085 TWO FASTENER HOLES WE RE FOUND ELONGATED. FABRICATED FREEZE PLUGS FOR HOLE REPAIR FABRICATED REPLACEMENT STIFFENER ANGLE FILLER TAPERED FILLE R AND SINGLE REPAIR DOUBLER. INSTALLED IAW AAR EA 12932 AND ASA EA 5310 02827. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0843621 1 20080923 A 5751 654652031 HINGE FITTING BOEING 737 7374Q8 138447Q NM LT AILERON GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 UPON REMOVAL OF LT WING AILERON FOUND NR 1 HINGE LUG ON FITTING GOUGED IN 2 PLACES. REMOVED NR 1 HINGE FITTING DAMAGE F OUND TO BE OUT OF LIMITS. LOCATED, DRILLED AND INSTALLED A REPLACEMENT FITTING IAW B737 400 SRM 51 40 02 AND AAR EA 129 69 ASA EA 5750 02509. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0843611 1 20080913 A 5754 65C26603191 SKIN BOEING 737 7374Q8 138447Q NM LE SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 LT WING NR 3 SLAT LOWER SURFACE I/B CORNER CHAFED. REMOVED DAMAGED AREA OF SKIN, FABRICATED FILLER SKIN AND DOUBLER BON DED IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0843603 1 20080911 A 5754 65C2631017 SKIN BOEING 737 7374Q8 138447Q NM LE SLAT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 LT WING I/B MID FLAP TRAILING EDGE WEDGE DENTS ON LOWER SURFACE. REMOVED DAMAGED AREA, FABRICATED SKIN AND DOUBLER BOND ED IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 2008UALA06151 1 20081016 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1640 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 CORROSION ON UPPER T-CAP WHERE IT ATTACHES TO RT CUSP AT BS 1640. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION AND FOU ND TO BE OUT OF LIMITS. FABRICATED & INSTALLED A NEW SECTION OF T-CAP. 2 L 7 2 4F 4 F RT A2NM E17NE 20081028 NM 2008 10 28 2008UALA06157 1 20081017 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHT INOPERATIVE 38 LT. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 20081028 NM 2008 10 28 2008UALA06159 1 20081017 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHT INOP CEILING ROW 16. RELAMPED EMERGENCY LIGHT. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081028 NM 2008 10 28 ASAA0843608 1 20080918 A 5753 65C2632017 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 LT WING O/B MID FLAP LOWER SURFACE CHAFED O/B OF NR 1 FLAP TRACK. REMOVED DAMAGED AREA OF SKIN, FABRICATED REPAIR PARTS AND BONDED IAW B737 400 SRM 51 70 10 PG 254. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 2008UALA06161 1 20081017 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHT INOP CEILING ABOVE LAV 104. RELAMPED EMERGENCY LIGHT, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081028 NM 2008 10 28 ASAA0843612 1 20080907 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 1 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 LT WING NR 1 SPOILER DENTED 2 INCHES FROM LEADING EDGE 10 INCHES FROM O/B EDGE. CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER BONDED IAW B737 400 SRM 51 70 01 REPAIR 4. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0853634 1 20081019 A 3610 32895625 CONTROL VALVE BOEING 737 737890 1384527 NM NR 1 ENGINE FAULTY A ASAA K NONE O OTHER CL CLIMB 1 NM 02 570AS 6612 35185 UPON DEPARTURE FROM HNL AIRFLOW FROM GASPERS WAS EXCESSIVELY HIGH NOISE LEVEL WAS 120 DBT AND TEMPERATURE IN CABIN WAS V ERY COLD. AFTER APPROX 5 MIN AIRFLOW DB LEVEL AND TEMPERATURE RETURNED TO NORMAL. SUSPECT THAT A 9TH STAGE BLEED VALVE STUCK OPEN. NO OTHER DISCREPANCIES. PERFORMED FIM TASK 36 10 00 810 809 AND FOUND PRECOOLER CONTROL VALVE ON THE NR 1 ENGINE BAD. REMOVED AND REPLACED NR 1 PRECOOLER VALVE. OP CHECK GOOD REF MM 36 12 02 PRECOOLER VALVE VERIFIED BY SEAM C MARK. BITE ON PACK CONTROLLERS PRODUCED NO FAULTS. PERFORMED ENGINE BLEED CROSSOVER OP TEST, CK'D GOOD. VERIFICATIO N FLIGHT SATISFACTORY. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873653 1 20081003 A 5320 141A5410U12 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 FWD PASSENGER CABIN INTERCOSTAL AT BS 328 344 LBL 47 IS CRACKED. FWD PASSENGER CABIN INTERCOSTAL REPLACED WITH NEW PART P/N 141A5410U12, PO 122205 AT BS 328 344 LBL 47 IAW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 2008UALA06160 1 20081017 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHT INOP CEILING ROW 18. RELAMPED EMERGENCY LIGHT, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081028 NM 2008 10 28 ASAA0873638 1 20081001 A 5321 453A16102 FLOOR PANEL BOEING 737 737790 13844CN NM CARGO BAY DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 FWD CARGO PIT MID FLOOR PANEL BS 428 500 LBL 24 RBL 24 HAS MULTIPLE DENTS. FWD CARGO PIT MID FLOOR PANEL BS 428 500 LBL 24 RBL 24 DENT FOUND TO BE BEYOND LIMITS. FLOOR BOARD REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53 00 53. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873641 1 20081001 A 5320 146A9401 SPLICE BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 AFT CARGO PIT CORROSION ON FLOOR SUPPORT SPLICE BS 887 LBL 10 RBL 21. CORROSION ON FLOOR SUPPORT SPLICE FOUND TO BE BEY OND LIMIT. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53 00 53. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 QXEA2008102301140 1 20081020 A 2932 7G773 PRESSURE SWITCH DHAV DHC8 DHC8202 2809007 NM HYDRAULIC SYS MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 19 349PH 486 PDX- NR 2 ENG HYD PUMP CAUTION ILLUMINATED. CAUTION REMAINED ILLUMINATED THROUGHOUT LANDING. TAXI AND PARKING. NO LOSS OF HYD PRESS OR QTY. PERFORMED ALTERNATE GEAR EXTENTION. UNEVENTFUL LANDING. REMOVED AND REPLACED NR 2 HYD PRESSURE SWITCH, GROUND RAN NR 2 ENGINE. OPS CHECK AND LEAK CHECK GOOD. NO DEFECTS NOTED. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081028 NM 2008 10 28 QXEA2008102301141 1 20080921 A 3260 SENSOR BOMBDR DHC8 DHC8402 1390042 NM LANDING GEAR OUT OF RIG A QXEA O OTHER J WARNING INDICATION CR CRUISE 1 NM 19 403QX 4037 LAS - IN CRUISE AND DESCENT LEFT AND RIGHT MAIN GEAR DOORS OPENED. HEARD AND FELT THUMP AS WELL AS LT & RT GEAR UNSAFE LIGHTS. AIRSPEED WAS 255K USED ALT GEAR EXTENSION TO LOWER GEAR. UNEVENTFUL LANDING. TOWED AIRCRAFT FROM THE RUNWAY. FERRY TO PDX FOR REPAIR. FOUND FAULT LGDRCL RIGGING GAP TOO LARGE. RIGGED SENSOR S17. CLEARED FAULT HISTORY. PERFOR MED OPERATIONAL CHECK FLIGHT WITH NO DEFECTS. EXTENSION RETRACTION CHECK OF GEAR GOOD. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081028 EA 2008 10 28 MASA2008102100742 1 20081021 A 3620 GG670800053 SENSOR CNDAIR CL600 CL6002C10 1390015 EA BLEED AIR SYS FAULTY A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 510MJ 4031 10101 ASH FLT 7051 PWM-ORD. RT PACK AUTO FAIL FOLLOWED BY SMOKE IN THE CABIN. MX REMOVED AND REPLACED RT BLEED TEMP SENSOR. 2 L 7 2 4F RT A21EA 20081028 NE 2008 10 28 HALA2008102300825 2 20081023 A 7261 O-RING BOEING 717 717200 1383700 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DETERIORATED A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM - NR 1 ENGINE OIL CONSUMPTION RATE HIGH. T/S PER FIM 71-05-00 & 71-08-00-101 FOUND OIL TANK SE RVICE CAP O-RING DETERIORATED REPLACED O-RING AND GRD ENGINE RUN LEAK CHECK GOOD. 2 L 7 2 4F 4 F TR A6WE E24NE 20081028 EU 2008 10 28 MALA080184 1 20081002 A 5542 SKIN SAAB SF340 340B 7860101 EU RUDDER DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 340B428 DENT NOTED ON LT SIDE OF RUDDER ASSY, 5.25 AFT OF FRONT SPAR AT WL 164.55. REPAIRED IAW EO S57226. 2 L 7 2 4T RT A52EU 20081028 EA 2008 10 28 ASOA200801256 1 20081001 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REPLACED RT FS 484.00 FLOOR SUPPORT INTERCOSTAL ANGLE RBL 27 IAW CRJ SRM 51-42-06. SUPPLEMENTAL SDR CLOSED 10/15/08. 2 L 7 2 4F RT A21EA 20081028 EA 2008 10 28 ASOA1225 1 20080926 A 5534 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 PERFORMED EDDY CURRENT INSPECTION OF FORWARD AND AFT V/STAB TO FUSELAGE DRAG ANGLES, RIGHT SIDE. FORWARD AND AFT DRAG A NGLES VERIFIED CRACKED, FORWARD DRAG ANGLE IS MARKED AT THE END OF CRACK. REMOVED RT AFT DRAG ANGLE MADE TEMPLATE FOR A FT RT DRAG ANGLE (IN THE BEND). DRILLED UP FASTENER HOLES FOR RT AFT DRAG ANGLE. PLUGGED DISCREPANT HOLE WITH RIVET. REMOVED 2 SCREWS THAT WERE DRILLED OFF. INSTALLED AFT DRAG AND APPLIED PRIMES TO SURFACE. FAY SEALED RT AFT DRAG ANGLE . APPLIED A023 FINISH TO RT AFT DRAG ANGLE. PERFORMED EDDY CURRENT INSPECTION OF FORWARD AND AFT V/STAB TO FUSELAGE DR AG ANGLES, LEFT SIDE. FORWARD AND AFT DRAG ANGLES VERIFIED CRACKED, FORWARD DRAG ANGLE IS MARKED AT END OF CRACK. REMO 2 L 7 2 4F RT A21EA 20081028 EA 2008 10 28 ASOA1289 1 20081002 A 5534 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVAL & REPLACEMENT OF RT AFT DRAG ANGLE. CUT AWAY DAMAGED AREA. FURTHER DAMAGE FOUND TO AREA UNDERNEATH REMOVED ARE A. REMOVED DAMAGE. REMOVED TOOLING MARKS IN UPPER FLANGE TO A DEPTH OF .002 AND .015 DEPTH SUBMIT TO BOMBARDIER FOR FU RTHER DISPOSITION. FABRICATED REPAIR FILLER & DOUBLER. COMPLIED WITH NDT, NO DEFECTS NOTED. INSTALLED REPAIR FILLER & DOUBLER TO REPAIR AREA. REMOVED & REPLACED AFT DRAG ANGLE ON VERTICAL STAB LEFT SIDE FAY SEALED & APPLIED FINISH TO AR EA. PERFORMED EDDY CURRENT INSPECTION OF FORWARD & AFT V/STAB TO FUSELAGE DRAG ANGLES, RIGHT SIDE. FORWARD & AFT DRAG ANGLES VERIFIED CRACKED. REMOVED RT AFT DRAG ANGLE MADE TEMPLATE FOR AFT RT DRAG ANGLE (IN THE BEND). DRILLED UP FASTE 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA200801385 1 20081022 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FS 621 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.0 INCH. REMOVED AND REPLACED CARGO DOOR SUPPORT BEAM LOWER ANGL E WITH NEW IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA200801075 1 20080831 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED AND REPLACED PAX DOOR OUTER HANDLE IAW AMM 52-11-03. OPS CHECK GOOD. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081029 NM 2008 10 29 SWAA085825 1 20081026 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A BETWEEN STR 28L TO STR 28R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085826 1 20081027 A 3350 6574550 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 6 ABC. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085796 1 20081027 A 5340 6527314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 15L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085799 1 20081027 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081030 EA 2008 10 30 ASOA200801387 1 20081022 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 LT / RT FS 559.0 BULKHEAD WEB HAS INDICATIONS NOTED LT WEB WL 52.10 O/B OF LBL 9 .2 INCH IN LENGTH RT WEB WL 58.70 I/B O F RBL 18 APPROX 1 INCH IN LENGTH WL 58.70 O/B RBL 9. .3 INCH IN LENGTH AND WL 54.10 O/B RBL 9 1INCH IN LENGTH. ALL THES E AREAS FAILED NDT MARK ON WEBS. REPAIRED LT AND RT FS 559.0 BULKHEAD WEB IAW BOMBARDIER REO 601R-53-41-802. WORK PERF ORMED IAW ASA EC/TC 601R-53-41-802. 2 L 7 2 4F RT A21EA 20081030 WP 2008 10 30 AALA200802270 1 20080806 A 2560 3913359583 RELEASE CABLE DOUG DC9 DC983 3022083 WP TAILCONE FRAYED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9304C 49530 TAIL CONE EMERGENCY RELEASE CABLE FROM OUTSIDE HANDLE TO LT SIDE CABLE BLOCK ASSY IS FRAYED. REPLACED TAIL CONE EMERGENC Y RELEASE CABLE. (K) 2 L 7 2 4F RT A6WE 20081030 WP 2008 10 30 AALA20802271 1 20080806 A 2560 3913359545 RELEASE CABLE DOUG DC9 DC983 3022083 WP TAILCONE FRAYED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9304C 49530 LT TAIL CONE EMERGENCY RELEASE CABLE FROM TRIANGLE BRACKET TO LWR LT LATCH ASSY IS FRAYED. REPLACED TAIL CONE EMERGENCY RELEASE CABLE. (K) 2 L 7 2 4F RT A6WE 20081030 WP 2008 10 30 AALA200802272 1 20080806 A 2560 3951072503 RELEASE PIN DOUG DC9 DC983 3022083 WP TAILCONE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9304C 49530 TAIL CONE EMERGENCY RELEASE PIN HAS AFT SLOT DAMAGE. REPLACED TAIL CONE RELEASE PIN. (K) 2 L 7 2 4F RT A6WE 20081030 NM 2008 10 30 AALA200802273 1 20080905 A 3397 CONNECTOR BOEING 777 777223 1385213 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 EMERGENCY LIGHTS AT SEAT ROWS 4A TO LAVATORY NR 2, INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT ROWS 4A TO LAVATORY NR 2. SYSTEM GROUND CHECKED NORMAL OPERATION. (K) 2 L 7 2 4F RT T00001SE 20081030 NM 2008 10 30 KCSA081499 1 20080930 A 5414 SKIN BOEING 747 747259B 1384804 NM PYLON DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 NR PYLON OTBD SKIN LOWER FASTERNER HOLES DAMAGED AT NAC 221.9. (K) 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 DHL2008F00042 1 20080924 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN AT BS 720D BETWEEN STRINGER 13L AND 14L FRAME WITH DOUBLE HOLES. REPAIRED UPPER FUSELAGE BODY F RAME SECTION AT BS 720D BETWEEN STRINGER 11 AND 14 LEFT SIDE DUE TO DOUBLE HOLES IAW SRM 53-10-4, FIG 1, DETAIL 1. (K) 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 DHL2008F00043 1 20080918 A 5230 SKIN BOEING 727 727224 1384076 NM CARGO DOOR DAMAGED A DHLA K NONE O OTHER NR NOT REPORTED 1 GL 05 745DH 20665 LOWER FUSELAGE AFT CARGO COMPARTMENT DOOR NR 2 OUTER SKIN WITH DOUBLE HOLES AT BS 950F + 8 BETWEEN UPPER FRAME AND BEAM NR 1. REPAIRED LOWER FUSELAGE AFT CARGO COMPARTMENT DOOR NUMBER 2 OUTER SKIN SECTION FROM BS 950F+3.5 TO BS 950F + 10.5 BETWEEN UPPER FRAME AND BEAM NUMBER 1 DUE TO SKIN WITH DOUBLE HOLES IAW SRM 52-00-3, FIG 4. (K) 2 L 7 3 4F A3WE 20081030 CE 2008 10 30 GUUA10130801 1 20081013 A 5210 12951408723 DAMPENER BEECH 1900 1900D 1154162 CE ASD CRACKED A GUUA O OTHER O OTHER IN INSP/MAINT 1 SO 29 69549 UE194 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED AIRSTAIR DOOR COUNTER BALANCE SUPPORT ASSEMBLY DAMPENER CRACK. REPLACED AIRSTAIR DOOR COUNTER BALANCE UPPER SUPPORT ASSEMBLY DAMPENER. 2 L 7 2 4T RT A24CE 20081030 SO 2008 10 30 SIMA200830101 1 20081024 A 2160 M835362024M RELAY EMB 135 EMB135KL 3260302 SO TEMP CONTROL FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 21 835AE 145634 FLIGHT 4886 - CREW REPORTED WHEN ANTI-ICE TURNS ON IT GETS VERY HOT IN THE COCKPIT WITH A SMELL OF MELTING PLASTIC AND U NABLE TO BRING TEMP DOWN TILL ANTI-ICE TURNS OFF. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RELAYS K0186 CAP T RECIRC AND K0321 CKPT REICR AS PER TROUBLESHOOTING MANUAL. OPERATIONAL CHECK OF TEMP CONTROL SYSTEM GOOD IAW AMM 21-6 0-00. NO FURTHER DEFECTS NOTED AT THIS TIME. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081030 CE 2008 10 30 GUUA10260801 1 20081026 A 5220 HANDLE BEECH 1900 1900D 1154162 CE EMERGENCY EXIT LACK OF LUBE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 17541 UE203 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT EMERGENCY EXIT DIFFICULT TO OPEN. LUBRICATED LEFT EMERGENCY EXIT H ANDLE. 2 L 7 2 4T RT A24CE 20081030 EA 2008 10 30 MASA2008102400748 1 20081024 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA ROW 8 INOPERATIVE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 75998 7336 ASH FLT 7315 ORD-RON - EMERGENCY FLOOR LIGHT STRIP AT ROW 8 INOPERATIVE. MX RESECURED LIGHT. 2 L 7 2 4F RT A21EA 20081030 NM 2008 10 30 MASA2008102400750 1 20081024 A 3350 COVER DHAV DHC8 DHC8202 2809007 NM EMERGENCY LIGHT MISSING A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 988HA 426 ASH 2805 PHX - CREW REPORTED HAVING AN EMERGENCY EXIT LIGHT COVER MISSING. MX REPLACED LENS. 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 F3LA2008102700692 1 20081024 A 5320 D5347047520600 PROFILE AIRBUS A319 A319111 3930336 NM ZONE 100 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION AND CRACKS IN THE AFT CARGO COMPARTMENT ON PROFILE LOCATED AT STRINGER 38 LEFT BETWEEN FRAME 52 AND FRAME 56. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PA GE 1 AND 2. 2 L 7 2 4F RT A28NM 20081030 NM 2008 10 30 F3LA2008102700693 1 20081024 A 5320 D5347047920400 PROFILE AIRBUS A319 A319111 3930336 NM ZONE 100 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE AFT CARGO COMPARTMENT ON PROFILE LOCATED AT STRINGER 38 LEFT BET WEEN FRAME 59 AND FRAME 63. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2. 2 L 7 2 4F RT A28NM 20081030 NM 2008 10 30 QXEA2008102901112 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4 - NR 17 SEAT TRACK HAS CORROSION IN THE BASE BETWEEN APPROX STA X94.800 - XX196.00. BLENDED OUT CORROSION AND FOUND TO BE WITHIN LIMITS PER RD8/4-53-884. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01. NO CRACKS NOTED. ETCHED AN D ALODINED IAW RD 8/4-53-884. 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 DHLA2008745574 1 20080911 A 5753 RIB BOEING 727 727224 1384076 NM RT WING TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 RT WING OTBD MID FLAP LOWER AFT SECTION AT WBL 492 RIB CRACKED. REPLACED RIB AT RT WING OTBD MID FLAP IAW B727 SRM 51-1 0-1 PARA 7. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 DHLA2008745575 1 20081008 A 5240 FRAME BOEING 727 727224 1384076 NM ZONE 800 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE CABIN FWD GALLEY DOOR UPPER SECTION FRAME WITH HOLE. REPLACED FRAME SECTION BETWEEN DOOR BEAM NR 2 AND D OOR BEAM NR 5 IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 DHLA2008745576 1 20080904 A 5241 FRAME BOEING 727 727224 1384076 NM GALLEY DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE FWD GALLEY DOOR FWD UPPER CORNER EXTERNAL FRAME CRACKED. REPAIRED FWD GALLEY DOOR FWD UPPER FRAME SECTIO N BETWEEN DOOR BEAM NR 1 AND DOOR BEAM NR 3 IAW S/B 727-52-114 DTD FEB 24, 1978 SECT 3 PART 3 PARA E DWG 69-69977 REV B DTD 1/19/77. 2 L 7 3 4F A3WE 20081030 WP 2008 10 30 AALA200802630 1 20081001 A 5313 LONGERON DOUG DC9 DC983 3022083 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CRACK FOUND ON LONGERON 2 LEFT AT STATION 160. CRACK LENGTH WAS 1 INCH. REPLACED LONGERON SECTION BETWEEN STATIONS 148 AND 170 IN ACCORDANCE WITH SRM 53-02-00. 2 L 7 2 4F RT A6WE 20081030 NM 2008 10 30 DLM88081406 1 20081023 A 5350 10090013 RADOME DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA O OTHER C F.O.D. LD LANDING 1 SO 27 937DL 49810 BIRD STRIKE ON NOSE OF RADOME. C/W BIRDSTRIKE INSPECTION PER AMM FOUND RADOME CRACKED. REPLACED RADOME PER AMM. 2 L 7 2 4F RT A6WE 20081030 NM 2008 10 30 DL738081408 1 20081023 A 5340 DOOR BOEING 737 737832 13844CF NM FUSELAGE OPEN A DALA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 27 3739P 30541 TWO SMALL CRACKS ON LIP OF EXT PWR DOOR OPENING. MADE TIME LIMITED REPAIR PER ERA 471288-14. EXT PWR DOOR TAP CLOSED P ER ERA. WILL NEED PERM REPAIR WITHIN 50 FLT HRS. 2 L 7 2 4F RT A16WE 20081030 SO 2008 10 30 FDKA2008102200280 1 20081022 A 5210 ROLLER EMB 145 EMB145LR 3260212 SO PAX DOOR LOOSE A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 853MJ 145464 FRL FLT 8906 JFK-ORF. MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. MX SECURED DOOR ROLLERS. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081030 SO 2008 10 30 FFKA134 1 20081022 A 3221 95551023 MOUNT PIPER PA34 PA34200T 7103406 SO NLG BROKEN E FFKA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 05 286BW 10400 173 347970182 DURING TAXI OPERATIONS THE PILOT REPORTED HAVING DIFFICULTY MAKING LEFT TURNS. AFTER INVESTIGATING IT WAS FOUND THAT TH E NOSE LANDING GEAR MOUNT HAD BROKEN AT THE MOUNTING POINT FOR PIPER P/N 95395-000 (ARM ASSEMBLY-STEERING). THIS CAUSED THE ROLLER ASSEMBLY P/N 95387-000 TO COME OUT OF THE NOSE WHEEL CENTERING TRACK P/N 95394-000. THE AIRCRAFT HAD RECENT LY BEEN TOWED AND TAXIED BY MAINTENANCE PERSONNEL AND SUSPECT THAT THE NOSE GEAR HAD BEEN OVER STEERED BREAKING THE SMAL L TAB OFF OF THE MOUNT. 1 L 7 2 3O A7SO 20081030 NE 2008 10 30 YENA200810240101 2 20081023 A 7200 ENGINE EMB ERJ190 ERJ190100IGW 3260408 NM GE CF34 CF3410E6 30023 NE NR 1 BIRD INGESTION A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 192JB 19000014 JFK-PIT, STRONG UNKNOWN FUMES IN COCKPIT AND CABIN DURING INITIAL CLIMB. COMPLETED CABIN /SMOKE FUMES QRH AND RETURNED TO JFK. FUMES DISSIPATED INFLIGHT PRIOR TO LANDING. ACCOMPLISHED FIM TASK 21-20-00-810-801-A SMOKE AND /OR ABNORMAL SM ELL IN PASSENGER CABIN AND/OR ABNORMAL SELL IN PASSENGER CABIN AND/OR COCKPIT. FOUND FOUL SMELL DURING ENGINE NR 1 OPER ATION DUE TO ENGINE NR 1 BIRD INGESTION. ENGINE WAS BORESCOPED AND CLEANED, NO ABNORMALITIES NOTED. PERFORMED ELECTRIC AL ODOR INSPECTION PER LTV MM 44-20-10. NO ABNORMALITIES NOTED. LTV OPS NORMAL. 2 L 7 2 4F 4 F RT A57NM E00070EN 20081030 NM 2008 10 30 USAASB08085 1 20080921 A 3230 65446915 MODULE BOEING 737 7374B7 138449C NM RT MLG WW FAULTY A USAA A UNSCHED LANDING O OTHER AP APPROACH 1 EA 19 443US 57431 5704 24842 IAD - FLT 1282 - ENROUTE FROM PBI TO DCA, CREW ENCOUNTERED A LANDING GEAR PROBLEM WHEN EXTENDING THE GEAR. CAPTAIN REP ORTED THE RT MLG WOULD NOT EXTEND WITH THE HANDLE IN THE DOWN POSITION. GEAR WAS STUCK IN THE WHEEL WELL WHICH WAS VERI FIED BY OPS TOWER. FIRST INDICATION WAS 2 GREEN AND 1 RED, AFTER MANUAL GEAR EXTENSION, CREW RECEIVED 3 GREEN. FLT DIV ERTED TO IAD AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. MX R&R THE RT MLG MODULAR PACKAGE PER TAS K 32-32-61-4. GEAR OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 USAASB08084 1 20080919 A 2560 P4010021 BATTERY BOEING 737 7373G7 138447J NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 307AW 24634 IAH - MX REPORTED THE FWD FLT ATTENDANT FLASHLIGHT INOPERATIVE. MX REMOVED AND REPLACED THE BATTERY. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 20081030 CE 2008 10 30 DJFA2008076 1 20081021 A 2170 CLAMP RAYTHN DH125 HAWKER800XP 7150012 CE WATER SEPARATOR LOOSE E DJFA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 23 809LX 258432 DURING CLIMBOUT CREW REPORTED REAR BAY OVERHEAT LIGHT ILLUMINATED. MAINTENANCE IS INSPECTING. FOUND THE WATER SEPARATO R CLAMP LOOSE. THE CLAMP WAS SECURED. 2 L 7 2 4F RT A3EU 20081030 CE 2008 10 30 DJFA2008077 1 20081022 A 4930 DRAIN LINE RAYTHN DH125 HAWKER800XP 7150012 CE APU DISCONNECTED E DJFA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 23 791TA 258291 CREW REPORTED FUEL ODOR WHEN STARTING THE APU AFTER LANDING. MAINTENANCE FOUND THE APU PURGE TANK OVERBORAD DRAINLINE D ISCONNECTED. MAINTENANCE RE-INSTALLED THE DRAIN LINE. 2 L 7 2 4F RT A3EU 20081030 SO 2008 10 30 FDKA2008102700282 1 20081027 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA K NONE L NO TEST NR NOT REPORTED 1 SW 07 838MJ 145384 FRL FLT 8927 ALB-JFK. FWD EMERGENCY LIGHT STRIP INOP AND OVERHEAD EMERGENCY SIGN. MX RESECURED CONNECTOR. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081030 SO 2008 10 30 C2XA08TY128 1 20081028 A 2197 GROUND WIRE EMB 145 EMB145XR 3260214 SO CABIN BURNED A C2XA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 27 11192 14500936 TYS - AIR RETURN - LAV SMOKE INDICATION ON CLIMBOUT. ONCE ON GROUND F/A REPORTED, THERE WAS A LOT OF HEAT COMING FROM B EHIND THE EXIT ROW, BUT NO VISIBLE SMOKE. MX FOUND AND REPAIRED A BROKEN GROUND WIRE ON THE THERMAL DISTRIBUTION SWITCH IAW EMB 145XR WM 20-21-00 AND OPS CHECKED GOOD IAW EMB 145XR AMM 21-20-00 AND EMB 145XR AMM 26-14-00. A SATISFACTORY T EST FLIGHT WAS ALSO PERFORMED AND THE A/C WAS RELEASED BACK TO SERVICE. 2 L 7 2 4F RT 20081030 NM 2008 10 30 KCSA081547 1 20081028 A 5320 STIFFENER BOEING 747 747212B 1384886 NM NLG WW CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 NOSE WHEEL WELL TOP PANEL WEB STIFFENER CRACKED AT BS 310 LBL 10 .500 INCH. 2 L 7 4 4F RT A20WE 20081031 SO 2008 10 31 RAIA2008102800001 1 20081026 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 847HK 14500857 PRE FLIGHT INSPECTION REVEALED THAT THE GALLEY EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE RESEATED THE CONNECTOR AT THE LIGHT ASSEMBLY. LIGHT OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081031 SO 2008 10 31 RAIA2008102800003 1 20081025 A 3350 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 809HK 145187 DURING PRE FLIGHT INSPECTION THE OVERHEAD EMERGECNY EXIT LIGHT AT ROW 12 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE LIGHT. 2 L 7 2 4F RT T00011AT 20081031 WP 2008 10 31 ABXA200810280255 1 20081003 A 3231 CABLE DOUG DC9 DC941 302207N WP NLG DOOR BROKEN A ABXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 23 958AX 47760 AFTER TAKEOFF, UPON GEAR RETRACTION, LOUD BANG HEARD IN NOSE WHEEL AREA FOLLOWED BY VIBRATION SOUND. RECYCLED GEAR. WH EN GEAR WAS UP AGAIN, SAME VIBRATION SOUND WAS HEARD. EXTENDED GEAR AND RETURNED TO AIRPORT WITH NORMAL GEAR INDICATION . FOUND STOP CABLE ON RIGHT NOSE GEAR DOOR BROKEN. REPLACED CABLE ASSEMBLY IAW DC9 AMM 32-22-01. 2 L 7 2 4F A6WE 20081031 NM 2008 10 31 ASAA0843676 1 20081007 A 5754 SKIN BOEING 737 737490 1384715 NM LE SLAT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 NR 2 SLAT HAS A DENT ON THE UPPER SUFACE 3.5 INCHES FROM T/E AND 34 INCHES FROM OUTBOARD END. PREPPED DAMAGED AREA, FAB BED DOUBLER AND BONDED THE REPAIR IAW B737 400 SRM 51 70 10 REP 2. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 ASAA0843671 1 20081008 A 5753 SKIN BOEING 737 737490 1384715 NM MIDFLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 LT WING INBOARD MID FLAP WEDGE UPPER SURFACE HAS A DENT. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, AND BONDED TH E REPAIR IAW B737 400 SRM 51 70 10 REP 2. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 ASAA0843673 1 20081007 A 5753 SKIN BOEING 737 737490 1384715 NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 LT INBOARD AFT FLAP HAS MULTIPLE DENTS ON THE UPPER SURFACE. REMOVED DAMAGED AREAS, FABBED FILLERS AND DOUBLER, AND BON DED REPAIRS 2 EA IAW B737 400 SRM 51 70 10 REP 4. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 ASAA0853666 1 20081025 A 3040 8300005604 CONTROL UNIT BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA K NONE J WARNING INDICATION DE DESCENT 1 NM 02 559AS 8292 35178 RIGHT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED DURING DESCENT. FOLLOWED QRH PROCEDURE LIGHT EXTINGUISHED. PERFORMED BITE ON WINDOW HEAT CONTROL UNIT AND P5 9 OVERHEAT TEST PASSED OPS CHECK GOOD REF AMM 30 41 00. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 ASAA0853657 1 20081021 A 8010 66002849 SWITCH BOEING 737 737890 1384527 NM COCKPIT MALFUNCTIONED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 587AS 35684 SHORT TERM MAINT MESSAGE NR 73 20311 START SWITCH ARINC BUS DATA DISAGREE FOUND ON LEG NR 2 WHILE ACCOMPLISHING TC 78273 00 ON NR 1 ENG PERFORMED FIM TASK 73 24 00 810 813 F00 SYSTEM CK'S GOOD, NO HISTORY IN 90 DAYS PER SEAMC ED GROUND VERIF ICATION SUCCESSFUL. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 ASAA0853658 1 20081021 A 7910 41P5025 O-RING BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE OIL TANK DEFORMED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 558AS YT014643 35177 NR 1 ENG OIL TANK CAP O-RING IS DEFORMED. REMOVED & REPLACED O-RING SEAL REF MM 79 11 01 300 801 F00. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081031 NM 2008 10 31 ASAA0843679 1 20081008 A 5330 655298865 SKIN BOEING 737 737490 1384715 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 FUSELAGE SKIN IS DENTED AT STA 1002 AND STR 14L 2.5 INCHE ABOVE LAP 6 INCHES FROM CUTOUT 2 INCHES FROM REPAIR. REMOVED SKIN PANEL, FABBED NEW SKIN PANEL AND BONDED DOUBLER TO IT AND INSTALLED REPLACEMENT SKIN PANEL ASSEMBLY IAW B737 400 SR M 51 40 02. 2 L 7 2 4F RT A16WE 20081028 EA 2008 10 28 ASOA200801298 1 20081004 A 5320 PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED DAMAGED PORTION OF SIDE PNL. REQUIRED NDT. COMPLIED WITH (HFEC) OF THE PAX DOOR AFT SKIN REPAIR. NO INDICATIO NS NOTED AT THIS TIME. FABBED REPAIR ITEMS AND INSTALLED TO AFT SIDE WEB. EDGE SEALED REPAIR. ALSO PAINTED REPAIR. C UT OUT DAMAGED PORTION OF SIDE PNL. REQUIRED NDT. COMPLIED WITH (HFEC) OF THE PAX DOOR FWD SKIN REPAIR. NO INDICATION S NOTED AT THIS TIME. FABBED REPAIR ITEMS AND INSTALLED. REPAIR REQUIRED EDGE SEAL & PAINT. EDGE SEALED REPAIR. ALS O PAINTED REPAIR. REMOVED DAMAGED CARGO DOOR SUPPORT BEAM LOWER ANGLE & INSTALLED A NEW SERVICABLE ANGLE. REPAIRED REA R PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT. REPAIR PER EC/TC REO 601R-53-61-1230 HAS BEEN COMPLETED. 2 L 7 2 4F RT A21EA 20081028 EA 2008 10 28 ASOA200801251 1 20080930 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 BLENDED SILL FOUND TO BE OUT OF LIMITS PER CRJ 700 SRM 51-21-06. REMOVED, FABRICATED, AND REPLACED -3 FILLER IN REF TO REO670-53-21-139 PER CRJ 700 SRM 51-42-06 AND 51-42-21. SUPPLEMENTAL SDR CLOSED 10/15/08. 2 L 7 2 4F RT A21EA 20081028 NM 2008 10 28 ASAA0843664 1 20081010 A 5753 SKIN BOEING 737 7374Q8 138447Q NM MIDFLAP DENTED A ASAA K NONE N FALSE WARNING IN INSP/MAINT 1 NM 02 764AS 25101 LT INBOARD MID FLAP T/E WEDGE HAS MULTIPLE DENTS ON A PREVIOUS REPAIR ON THE LOWER SURFACE. REMOVED DAMAGED DOUBLER, FA BBED REPLACEMENT DOUBLER AND BONDED THE REPAIR IAW B737 400 SRM 51 70 10 REP 4. 2 L 7 2 4F RT A16WE 20081028 EA 2008 10 28 ASOA200801293 1 20081002 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REPAIRED LT SIDE FLOOR SUPPORT ANGLE AT FS 621 LBL 40, WL 73 IAW BOMBARDIER REO 601R-53-61-117. REQUIRES INSTALLATION O F TWO NUT PLATES. APPLICATION OF FILLET SEAL AND TOPCOAT. INSTALLED 2 EA NUT PLATES, FILLET SEAL AND TOPCOAT IAW BOMBA RDIER REO 610R-53-61-117. C/W ASA ECTC REO 601R-53-61-117. SUPPLEMENTAL SDR CLOSED 10/20/08. 2 L 7 2 4F RT A21EA 20081028 EA 2008 10 28 ASOA200801271 1 20081002 A 5320 SUPPORT ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REPAIRED RT SIDE FS 621 SUPPORT ANGLE RBL 4 WL 73 IAW BOMBARDIER REO 601R-53-61-117 REV C. SUPPLEMENTAL SDR CLOSED 10/2 0/08. 2 L 7 2 4F RT A21EA 20081028 NM 2008 10 28 SWAA085734 1 20081023 A 5312 6517853 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 DURING SCHEDULED SPV CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 5.7 LOWER AFT CORNER. REPAIRED WEB P ER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085735 1 20081023 A 5312 6517853 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 DURING SCHEDULED SPV CHECK, FOUND FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 5.7 FWD LOWER CORNER. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085736 1 20081023 A 5312 6517853 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 619SW 28035 DURING SCHEDULED SPV CHECK, FOUND FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 5.7. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085737 1 20081023 A 5330 6545766 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 510, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085740 1 20081023 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 27R TO STR 27L, WL 148. REMOVED AND REPLAC ED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085741 1 20081023 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085742 1 20081019 A 3350 411A2212 LENS BOEING 737 7377H4 1384404 NM R1 DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 704SW 27838 FOUND R1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085747 1 20081022 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 385SW 26600 FOUND FWD O/B EMERGENCY EXIT FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081028 2008 10 28 SWAA085749 4 20081023 A 2565 6556685 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 FOUND L1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085750 1 20081021 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 DURING SCHEDULED 6Y CHECK, FOUND FLOORBEAM CORRODED AT BS 700, LBL 8. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085751 1 20081021 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 DURING SCHEDULED 6Y CHECK, FOUND FLOORBEAM CORRODED AT BS 700, LBL 3. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 DL757081412 1 20081013 A 5320 CHANNEL BOEING 757 757232 1384965 NM BS 1440-1480 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 C CHANNEL BS 1440-1480 RBL 19 IN ACB IS CORRODED. REMOVED AND REPLACED CHANNEL IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081031 NM 2008 10 31 DL757081413 1 20081012 A 5320 654B0244128 SUPPORT BOEING 757 757232 1384965 NM BS 1440 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 CORROSION ON FLOOR TO SIDEWALL SUPPORT AT THE AFT INBD CORNER OF THE ACB THRESHOLD BS 1440. REPLACED SUPPORT. 2 L 7 2 4F RT A2NM 20081031 NM 2008 10 31 DL757081449 1 20081026 A 5330 143N35219 SKIN BOEING 757 757232 1384965 NM BS 690 BL 0 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 DURING THE AGING AIRCRAFT INSPECTION, CORROSION WAS FOUND ON THE EXTERNAL SURFACE OF THE SKIN UNDERNEATH THE DME ANTENNA MOUNT AT STA 690 BETWEEN S-28L AND S-28R. THE CORROSION WAS REMOVED AND REPAIRED PER BOEING INSTRUCTIONS. 2 L 7 2 4F RT A2NM 20081031 NM 2008 10 31 DL757081451 1 20081016 A 5320 143N536681 FLOOR SUPPORT BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 655 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 727893 FWD CARGO COMPARTMENT STA 655 BL, RBL 19, LOWER SIDE OF FLOOR SUPPORT CORRODED. REMOVED AND REPLACED SUPPORT IAW SRM 51 -40-02, SRM 51-40-05. 2 L 7 2 4F 4 F RT A2NM E24NE 20081031 NM 2008 10 31 DL757081452 1 20081019 A 5315 143N53861 FLOORBEAM BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 739 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 727893 CORROSION IN AND AROUND FASTENER HOLE AT BS 739, RBL 9 FLOORBEAM, OUT OF LIMITS. REPAIRED PER DELTA ER/A 465406-14 REV ORIG. 2 L 7 2 4F 4 F RT A2NM E24NE 20081031 WP 2008 10 31 ABXA080243 1 20080924 A 3246 TIE BOLT DOUG DC9 DC941 302207N WP WHEEL ASSY LOOSE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX JULY79295 47759 LOOSE TIE BOLTS. WHEEL SCRAPPED. (K) TIE BOLT NUTS LOOSE REQUIRES REPAIR. INSPECTED, REPAIRED IAW ABX SPEC WORKSHEET B S421B DATED 12-21-07 AND THE ABX WHEEL AND TIRE MANUAL, REV 17. 2 L 7 2 4F A6WE 20081031 EU 2008 10 31 COEA0804742 1 20080925 A 2820 HOSE FOKKER F27 F27MK600 4990706 EU FUEL SYSTEM LEAKING A COEA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 13 742FE 10349 AIR TURN BACK. DURING CLIMB OUT AT APPROXIMATELY 7500 FT AGL, THE CREW NOTICED THE ODOR OF FUEL IN THE COCKPIT. AIR FLOW FROM THE AIR CONDITIONING SYSTEM WAS TURNED OFF. THE CREW MENTIONED THE ODOR DID NOT GET ANY WORSE AFTER THE A/C SYSTEM WAS TURNED OFF. MAINT FOUND A SMALL FUEL LEAK FROM THE HOSE CONNECTION TO THE FUEL HEATER OF THE RT ENG. TIGHTENED FUE L HOSE TO FUEL HEATER ON RT ENG. (K) 2 H 7 2 4T A817 20081031 SO 2008 10 31 RAIA00809027 1 20080926 A 3230 CONNECTOR EMB 145 EMB145 3260210 SO NLG SOLENOID VLV DISCONNECTED A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 807HK 145119 NOSE LANDING GEAR DOOR WOULD NOT CLOSE. MAINT INSP AND FOUND THE CONNECTOR PLUG ON THE NLG DOOR SOLENOID VALVE LOOSE. R EINSTALLED THE CONNECTOR AND PERFORMED SEVERAL SUCCESSFUL OPS CHECKS. (K) 2 L 7 2 4F RT T00011AT 20081031 CE 2008 10 31 DXTA200803289 1 20080926 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE RT MLG WEAK E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 337QS 5600437 RT SIDE BRAKES DID NOT FUNCTION, LT SIDE REQUIRED HEAVY PRESSURE. (K) 2 L 7 2 4F RT A22CE 20081031 SO 2008 10 31 RAIA00809025 1 20080924 A 3260 PROXIMITY SWITCH EMB 145 EMB145 3260210 SO NLG MALFUNCTIONED A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 804HK 145082 CREW RECEIVED AN AIR/GROUND SYSTEM FAIL INDICATION ON THE EICAS DURING CRUISE. MAINT REMOVED AND REPLACED THE NLG PROXIM ITY SWITCH SYSTEM. OPS CHECKED GOOD. (K) 2 L 7 2 4F RT T00011AT 20081030 EA 2008 10 30 ASOA200801023 1 20080802 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 PERFORMED EDDY CURRENT OF FS 202 BULKHEAD O/B HYDRAULIC LINE SUSPECTED AREA IAW CRJ 200 NDTM 51-20-06. NO INDICATIONS N OTED AT THIS TIME. FS 202 BULKHEAD IS CRACKED AT PARK BRAKE, REQUIRES REPAIR. DISCONNECTED PARK BRAKE AND PULLED THRU FS 202 BULKHEAD. REPAIRED FS 202 BULKHEAD AT PARK BRAKE PASS THRU CUTOUT. ALL WORK PERFORMED. ALSO PARK BRAKE REQ REC ONNECTION. COMPLIED WITH STEP 10 OF BOMBARDIER REO 601R-53-11-563. PARKING BRAKE REQUIRES RECONNECTION. PARKING BRAKE CABLE RECONNECTED. OPERATION TEST GOOD. COMPLIED WITH ASA EC/TC EO 600-53-217 C/W. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081030 NM 2008 10 30 F3LA2008102300679 1 20081023 A 2797 27921918AND27927 WIRE AIRBUS A319 A319111 3930336 NM RUDDER PEDAL BROKEN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 921FR 2010 MAINTENANCE FOUND WIRES 2792-1918 AND 2792-7407 BROKEN IN CONDUIT AT RUDDER PEDAL FORCE TRANSDUCER UNIT. CAUSE OF BREAK AGE WAS DETERMINED TO BE WIRE ROUTING. MAINTENANCE REPAIRED WIRES IN ACCORDANCE WITH THE ELECTRICAL STANDARDS PRACTICES MANUAL 20-53-22, 20-53-21, 20-48-11, 20-48-21 AND PERFORMED ELECTRONIC FLIGHT CONTROL MESSAGE GROUND SCAN IN ACCORDANCE WITH AMM 27-96-00-740-001. NO FAULTS RECORDED. MAINTENANCE AND INSPECTION FELT THAT THIS SHOULD BE REPORTED TO ALERT AIRBUS AND/OR THE FAA OF THIS ISSUE OCCURRING ON OTHER AIRCRAFT WITH ASSOCIATED FLIGHT CONTROL MESSAGES. 2 L 7 2 4F RT A28NM 20081030 WP 2008 10 30 AALA200802263 1 20080903 A 2560 MS24693C277 SCREW DOUG DC9 DC982 3022082 WP GIRT BAR BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 LT NR (1) SLIDE GIRT BAR FWD RETAINER CLIP BROKEN. REPLACED ATTACH SCREW IN FWD SLIDE GIRT BAR SUPPORT BRACKET. SYSTEM G ROUND CHECKED NORMAL OPERATION. (K) 2 L 7 2 4F A6WE 20081030 NM 2008 10 30 KCSA081504 1 20080930 A 5411 FRAME BOEING 747 747249F 1384849 NM PYLON CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 NR PYLON NAC STA 221.9 BULKHEAD RT FWD FRAME WEB CORRODED. (K) 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 DHL2008F00044 1 20080924 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER NR NOT REPORTED 1 GL 05 745DH 20665 UPPER FUSELAGE CARGO CABIN, FRAME WITH DOUBLE HOLE AT BS 1070 BETWEEN STRINGER 5L AND 6L. REPAIRED UPPER FUSELAGE BODY F USELAGE BODY FRAME SECTION AT BS 1070 BETWEEN STRINGER 4 AND 6 LEFT SIDE DUE TO DOUBLE HOLES IAW SRM 53-10-4, FIG 1. (K) 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 08FDEA04587 1 20081028 A 3040 HEATER BOEING 727 7272D4 138407U NM WINDOW INOPERATIVE A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 21 288FE 21850 L1 WINDOW HEAT FAILED EN ROUTE. TURNED OFF AND BACK ON SEVERAL TIMES BUT WINDOW HEAT CONTINUED TO FAIL. CHECKED/RESET BOTH L1 AC AND DC CONTROL PER MOCC. NO HELP. WINDOW VERY COLD. RELEASED FOR SERVICE PER MEL/CDL: 30-15-A CATEGORY: C EXPIRATION: 07NOV08 "MEL 30-15-A: L1 WINDOW HEAT, INOP. ACFT RESTRICTED FROM OPERATING INTO ICING CONDITIONS. DO NOT EXCEED 250 KIAS BELOW 10,000 MSL." 2 L 7 3 4F A3WE 20081030 EU 2008 10 30 08FDEA04589 1 20081028 A 5347 A53274786212 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 427FE 362 SEAT TRACK 5 RT CRACKED AT FR 60. REMOVED DAMAGED SECTION OF TRACK AND INSTALLED REPAIR SPLICE AT SEAT TRACK 5 RT BETWE EN FR 58 AND FR 62 IAW A310-200 SRM 53-10-16, FIG 208A, PG 250, SHT 2. 2 L 7 2 4F RT A35EU 20081030 WP 2008 10 30 08FDEA04590 1 20081028 A 5320 AFA71321C SUPPORT FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 373FE 46611 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 HOLES "C" AND "B" INDICATED CRACKED DURING HFEC INSPECTION AND HOLE "D" HAS CORROSION. REMOVED AND REINSTALLED SIDEWALL GRILLS, PANELS, STRAPS, CLIPS, ANGLE AND WEB FOR ACCESS. REMOVED AND R EPLACED FITTING. FABRICATED AND INSTALLED REPAIR BUSHINGS AND REPAIR DOUBLER ALL IAW SRM 51-31-01, SRM 53-50-00 FIG 17, SRM 53-00-01, SRM 53-12-01, SRM 51-21-02 AND MAE TRAVELER T8/764409. MAJOR REPAIR RII. 2 L 7 3 4F RT A22WE 20081030 WP 2008 10 30 08FDEA04591 1 20081028 A 5320 AFA71321C SUPPORT FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 373FE 46611 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 HOLES "A", "C" AND "D" INDICATED CRACKED DURING HFEC INSPECTION. REMOVE D AND REINSTALLED STRAPS, WEBS, CLIPS AND ANGLES. REMOVED AND REPLACED FITTING. FABRICATED AND INSTALLED BUSHINGS ALL IAW SRM 53-50-00 FIG 17, SRM 51-31-01 AND MAE TRAVELER T8/764410. MAJOR REPAIR RII. 2 L 7 3 4F RT A22WE 20081030 NM 2008 10 30 08FDEA04604 1 20081029 A 5315 65863561 FLOORBEAM BOEING 727 7272D4 138407U NM ZONE 200 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 UPPER LOBE INTERIOR STATION 804 LBL 68 INCH FLOORBEAM LOWER CHORD CORRODED. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 08FDEA04606 1 20081029 A 5320 656057115 FLOOR SUPPORT BOEING 727 7272D4 138407U NM ZONE 200 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 MAIN DECK FLOOR SUPPORT INTERCOSTAL IS CORRODED BS 1067, LBL 12 WL 208. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW S RM 53-10-1. REMOVED & REPLACED FLOOR SUPPORT IAW SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 DL757081440 1 20081014 A 5330 143N34714 SKIN BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 535 BL 0 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 723843 CORROSION AFTER ANTENNA REMOVAL FOUND ON SKIN AT BS 535 BL 0. REMOVED CORROSION AND REPAIRED IAW ER 08-3328/ER/A 465407 -14 DATED 10/24/08. 2 L 7 2 4F 4 F RT A2NM E24NE 20081030 NM 2008 10 30 DL757081441 1 20081013 A 5320 453N161123 STRAP BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 1510 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 723843 CORROSION AT BS 1510, LBL 17 THRU RBL 17 ON FLOOR PANEL SPLICE, OUT OF LIMITS AND REMOVED AND REPLACED IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E24NE 20081030 NM 2008 10 30 DL757081442 1 20081014 A 5320 2651216 VALVE BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE AFT CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 723843 CORROSION AFT DUMP VALVE INNER FLANGE IS CORRODED AND FASTENERS ARE PULLED THRU. REMOVED AND REPLACED AFT DUMP VALVE DU E TO CORROSION OUT OF LIMITS IAW AMM 20-11-00-201. 2 L 7 2 4F 4 F RT A2NM E24NE 20081030 NM 2008 10 30 DL757081443 1 20081019 A 5313 143N534639 STRINGER BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 814-840 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 723843 CORROSION IN AND AROUND FASTENERS AND HOLES AT BS 814-BS 840 RBL 16 FLOOR STRINGER. REMOVED AND REPLACED DUE TO CORROSI ON OUT OF LIMITS IAW SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E24NE 20081030 NM 2008 10 30 DL76G081445 1 20081026 A 2421 729825E IDG BOEING 767 7673P6 1385105 NM NR 1 ENGINE INTERMITTENT A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 156DL 25354 UKN RTB DUE WHILE TAXIING FOR TAKEOFF THE LEFT ENGINE GEN DRIVE LIGHT CAME ON INTERMITTENLY WITH THE ASSOCIATED LEFT GEN DRI VE EICAS MESSAGE. REPLACED NR 1 ENG IDG AS PER AMM OP AND LEAK CKS OK MFG P/N 729825E. 2 L 7 2 4F RT A1NM 20081030 NE 2008 10 30 DL75E081447 2 20081025 A 7200 PW2037RTC ENGINE BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE NR 1 MALFUNCTIONED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 718TW 41284 28486 727156 REJECTED TAKEOFF RWY 13R KJFK FOR LOSS OFF EPR INDICATION LEFT ENG ALL OTHER INDICATIONS NORMAL. RTO INITIATED 50 KTS G S, LOW SPEED REJECT. CONSULTED W/JFK MTC DISPATCH. RESTARTED ENG ALL INDICATIONS NORMAL. EPCS MSGS NR 1 ENG P2 RESET ALSO S DCI DC2 EPR IND FWD TO MCO PER MEL 77-11-01. PLACARD INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081030 EA 2008 10 30 SWIA200820249 1 20081022 A 3350 BATTERY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT DISCHARGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 746SK 10202 FLT 6564 - EMERGENCY EXIT SIGN LEFT SIDE INOP. REPLACED CHARGER AND BATTERY. 2 L 7 2 4F RT A21EA 20081030 NM 2008 10 30 08FDEA04581 1 20081027 A 5311 70750063C FRAME BOEING 757 75723A 1384967 NM BS 800 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 AFTER REMOVAL DOUBLER FROM TV MONITOR SUPPORT AT BS 800, FOUND SEVERAL HOLES ON FRAME. REMOVED DAMAGE AT BS 800 FROM S4R TO 4L IAW SRM 53-00-07. FABRICATED NEW ZEE FRAME PER MAE TRAVELER T8/763342. FABRICATED NEW SPLICES PER MAE TRAVEL ER T8/761971. DRILLED REPAIR PARTS IAW SRM 53-00-07 . TREATED AND PRIMED REPAIR PARTS IAW SRM 53-00-07. INSTALLED REP AIR PARTS AT BS 800 IAW SRM 53-00-07. DO A HFEC INSPECTION EVERY 12,000 FLT CYCLES AS GIVEN IN NDT 6,51-00-01 REPEAT TH IS INSPECTION AT EVERY 12,000 FLT CYCLES INTERVALS AS ALTERNATIVE DO A DETAILED VISUAL INSPECTION EVERY 9,000 FLT CYCLES AFTER INITIAL INSPECTION. THIS IS A CAT "B" REPAIR . 2 L 7 2 4F RT A2NM 20081030 WP 2008 10 30 AALA200802628 1 20080930 A 5320 7075T6 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON BOTTOM SIDE OF RIGHT CUSP AT MID CARGO. AREA OF DISCREPANCY WAS 11.5 INCHES BY 3.5 INCHES. INSTALLE D DOUBLER IN ACCORDANCE WITH AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081030 SO 2008 10 30 CHQA200800211 1 20081026 A 3222 1170C000006 STRUT EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL NLG OVERSERVICED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 370SK 13192 13192 145515 CAE311281 FLIGHT 3034, CMH TO DCA. DURING CLIMBOUT, THE FLIGHT CREW RECEIVED LG AIR/GND FAIL FOLLOWED BY E1-E2 THRUST REVERSER DI SAGREE ON EICAS. THE CREW BURNED OFF FUEL TO LAND UNDER WEIGHT AND LANDED WITHOUT INCIDENT IN CMH. MAINTENANCE FOUND C MC MESSAGES FOR NLG PROX SWITCH FAIL AND L/G T/R LOGIC. THE NOSE STRUT WAS INSPECTED AND WAS FOUND TO BE OVER SERVICED. THE NOSE STRUT WAS DRAINED AND RE-SERVICED PER AMM 32-20-01. THE GEAR WAS THEN SWUNG WITH NO DEFECTS NOTED AND NO CMC MESSAGES NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081028 NM 2008 10 28 SWAA085752 1 20081023 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EXTERIOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 DURING SCHEDULED 6Y CHECK, FOUND LT OVERWING EXTERNAL EMERGENCY EXIT LIGHT COVER CRACKED. REMOVED AND REPLACED COVER PE R MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085753 1 20081022 A 3350 8200048801 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 476WN 32475 DURING SCHEDULED MV2 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085760 1 20081022 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 DURING SCHEDULED HC2 CHECK, FOUND RT EMERGENCY EXIT LIGHT LENS LOOSE. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085761 1 20081022 A 5512 182A1500 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 796SW 27889 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER IN SPAR SKIN CRACKED AT BS 101, AFT OF FRONT SPAR. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081027 EA 2008 10 27 QXEA200800887 1 20080728 A 5520 HINGE CNDAIR CL600 CL6002C10 1390015 EA LT ELEVATOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK ELEVATOR LT MOUNT LUG. THE HINGE ASSY HAS DAMAGE THE ANTI ROTATION LUG RAISED AND SMOKING METAL. REMOVED HSTAB HINGE BOLT AND ANTI ROTATION COLLARD, BLENDED OUT DAMAGE IAW REO 670-55-11-099 REV B AND REO 670-55-11-112 REV A. HFEC IAW NDTM PT 6, 51-20-006 AND REO670-55-11-099 STEP 4. NO CRACKS NOTED. ROTOPEENED AREA IAW 670-55-11-099 REV B S TEP 5. INSPECTED PIN IAW REV A. ALODINED AND PRIMED AREA IAW REO 670-55-11-099 REV B. INSPECTED. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 QXEA200800914 1 20080817 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK LT INBD SEAT TRACK NR 7 HAS LIGHT CORROSION AT X388, X428 AND X449. BLENDED CORROSION REF 8/4-53-884 PG 6 STEP 1. MAX MATERIAL REMOVED .017, .015 AND .025" RESPECTIVELY. BLENDS WITHIN LIMITS. HFEC INSP IAW RD 8/4-53-884, D8 -400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. TREATED BLENDED AREA REF RD8/4-53-884. 2 L 7 2 4F RT A21EA 20081027 EA 2008 10 27 QXEA200800892 1 20080728 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK LT OTBD SEAT TRACK HAS CORROSION AT STA X797. BLENDED CORROSION IAW REO 670-53-00-013 SHT 2 STEPS 1-2. MA X MATERIAL REMOVED WAS .010". BLEND IS WITHIN LIMITS IAW REO 670-53-00-013 TABLE 1. ALODINED IAW SRM 51-21-11. 2 L 7 2 4F RT A21EA 20081027 NM 2008 10 27 KCSA081530 1 20081012 A 5712 RIB BOEING 747 747146 1384905 NM LT WING CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 LEFT WING L/E RIB CRACKED AT FWD END AT FS 415. 2 L 7 4 4F RT A20WE 20081027 NM 2008 10 27 KCSA081531 1 20081012 A 5210 FITTING BOEING 747 747249F 1384849 NM L1 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 L1 MAIN ENTRY DOOR AFT TOP CORNER FITTING CRACKED. 2 L 7 4 4F RT A20WE 20081027 EA 2008 10 27 QXEA200800913 1 20080817 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK RT INBD SEAT TRACK NR 13 HAS LIGHT CORROSION AT X419. BLENDED CORROSION REF 8/4-53-884 PG 6 STEP 1. MAX M ATERIAL REMOVED .024". BLEND WITHIN LIMITS. HFEC INSP IAW RD 8/4-53-884. D8-400 NDTM PART 6, 51-00-01, NO CRACKS NOTE D. TREATED BLENDED AREA REF RD 8/4-53-884. 2 L 7 2 4F RT A21EA 20081027 NM 2008 10 27 KCSA081529 1 20081012 A 5712 RIB BOEING 747 747146 1384905 NM LT WING CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 LT WING L/E RIB CRACKED AT AFT END, AT THE WING FRONT SPAR FSS 415. 2 L 7 4 4F RT A20WE 20081027 EU 2008 10 27 USAA920081712 1 20080921 A 5315 D5347218820400 FLOORBEAM AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 PIT - S4 -MAJOR REPAIR, LEVEL 2 EXFOLIATION CORROSION ON UPPER SURFACE OF FLOORBEAM AT FR 69 TO FR 70, S23L. REPLACED FLOORBEAM AT FR 69 TO FR 70, S23L IAW A319 SRM 51-42-11. 2 L 7 2 4F RT A28NM 20081027 NM 2008 10 27 USAA920081721 1 20080901 A 5311 6546529 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 SAL - C17 -MAJOR REPAIR, FRAME AT BS 440 HAS A .431 INCH CRACK BETWEEN S8L & S9L AND A .471 INCH CRACK BETWEEN S8R & S9R . REPAIRED FRAME AT BS 440 BETWEEN S8L & S9L, ALSO BETWEEN S8R & S9R IAW AMERICA WEST AIRLINES TASK CARD NR M1C53002. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873646 1 20081003 A 5315 147A5506 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 AFT PASSENGER CABIN CORROSION ON FLOORBEAM AT BS 986 RBL 12. CORROSION ON FLOORBEAM BLENDED OUT BLEND AREA FOUND TO BE BEYOND LIMIT. FLOORBEAM REPAIRED IAW B737 700 SRM 53 00 51 FIG 203 REPAIR 1. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873648 1 20081003 A 5315 141A5502 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 CORROSION FOUND ON FLOORBEAM BS 294.5 RBL 10 52. CORROSION ON FLOORBEAM BS 294.5 RBL 10 52 BLENDED OUT. BLEND AREA FOU ND TO BE BEYOND ALLOWABLE DAMAGE LIMIT. FLOORBEAM REPAIRED IAW B737 ERO 8715 AND EA. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873649 1 20081003 A 5315 141A550313 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 CORROSION FOUND ON FLOORBEAM BS 312 LBL 11 TO LBL 30. CORROSION ON FLOORBEAM BS 312 LBL 11 TO LBL 30 BLENDED OUT. BLEN D AREA FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMIT. FLOORBEAM REPAIRED IAW ERO 8711 AND EA. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085758 1 20081022 A 5330 6545778 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 526SW 26568 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081028 2008 10 28 SWAA085759 4 20081022 A 2565 6556685 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 605SW 27956 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085710 1 20081019 A 3350 101331 LENS BOEING 737 737301 1384611 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 660SW 23230 FOUND RT EMERGENCY EXIT LIGHT LENS LOOSE. REPAIRED LENS PER SWA EA. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085715 1 20081021 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 435, STR 1. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085716 1 20081020 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085717 1 20081021 A 3350 65C27095 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 404WN 27892 DURING SCHEDULED HC2 CHECK, RT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085691 1 20081021 A 5315 6546804 FLOORBEAM BOEING 737 7375H4 138449D NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 514SW 25153 DURING SCHEDULED 18Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 47, WL 208. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085692 1 20081018 A 5330 6945765 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 425, STR 1R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085699 1 20081020 A 3350 81000 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 263WN 32520 DURING SCHEDULED HC1 CHECK, FOUND EEPLS LENS LOOSE AT FWD SECTION. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085704 1 20081022 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR LOWER HINGE CUTOUT FUSELAGE SKIN CRACKED AT BS 303, WL 238. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081029 2008 10 29 SWAA085706 4 20081020 A 2565 6556685 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802497 1 20080926 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM UPPER FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 TUL CORROSION ON UPPER SURFACE OF FLOORBEAM BEYOND LIMITS. REPAIRED PER ESO 61000 DATED 22 SEP 08. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 USAA920081883 1 20080919 A 5311 6546555 FRAME BOEING 737 7373G7 138447J NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN C18 MAJOR REPAIR NR 6131828 FRAME CRACKED AT BS867, BETWEEN S8L AND S9L. REPAIRED FRAME AT BS867, BETWEEN S8L AND S 9L IAW TASK CARD NR M1C53002. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 2008UALA06173 1 20081017 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 548UA 25396 DURING EMERGENCY LIGHT TEST, FOLLOWING BULLNOSE LIGHTS INOP, 4AB, 6AB, 10CD, 13 CD, 14 AB, 15 AB, 20 CD, 21 AB, 23 CD, 2 7 CD, AND 29 AB. RELAMPED ALL LISTED LOCATIONS. ALSO REPLACED BATTERY PACK M10568, OPS CHECKS GOOD REF MM 33-51-07 AND 33-51-05. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 2008UALA06176 1 20081017 A 5753 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FOREFLAP CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 RIGHT WING INBOARD FORE FLAP OUTBOARD END UPPER SURFACE HAS CHAFED REPAIR. REMOVED DAMAGED REPAIR AND BONDED ON NEW REP AIR REO G12468, REV B. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 WP 2008 10 29 AALA200802509 1 20080923 A 5340 SUPPORT BRACKET DOUG DC9 DC982 3022082 WP GIRT BAR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 TUL AFT SERVICE DOOR GIRT BAR AFT SUPPORT FITTING AT STATION 1165 CORRODED. AREA OF DISCREPANCY IS 4 INCHES BY 5 INCHES . INSTALLED NEW AFT SERVICE DOOR GIRT BAR BRACKET PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081029 NM 2008 10 29 AALA200802490 1 20080925 A 5320 FLOOR SUPPORT BOEING 737 737823 13844CB NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION ON FLOOR SUPPORT IN AFT CARGO BEYOND LIMITS. AREA OF DISCREPANCY IS 10 INCHES BY 1 INCH. REPLACED FLOOR SUPP ORT PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 2008UALA06178 1 20081017 A 2560 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 548UA 25396 DOOR 2R SLIDE ANNUNCIATOR ALWAYS ON EVEN WHEN DOOR NOT ARMED. REPLACED DOOR 2R GIRT BAR SENSOR S10220. OPS CHECKS GOOD . 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 USAA920081874 1 20081004 A 5340 69353521 STRINGER CLIP BOEING 737 7373G7 138447J NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN C18 MAJOR REPAIR NR 6132460 STRINGER CLIP CRACKED AT BS400, S10R. REPLACED STRINGER CLIP AT BS400, S10R IAW SRM 51- 40-02-OG. 2 L 7 2 4F RT A16WE 20081029 2008 10 29 2008UALA06180 4 20081018 A 2564 B14056907 O-RING AIRCRUISERS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LIFE RAFT LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 11992991 25396 LIFE RAFT AT AFT LOWERED CEILING PANEL, CYLINDER PRESSURE FAILED. LOW BOTTLE PRESSURE. LEAKING AT GAUGE TO VALVE O-RIN G. REMOVED & REPLACED O-RING. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 WP 2008 10 29 AALA200802504 1 20080929 A 5347 1D00268 CARGO TRACK DOUG DC9 DC982 3022082 WP BS 1003-1221 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 CORROSION ON LT TIE DOWN TRACK IN AFT CARGO NUMEROUS PLACES. INSTALLED TIE DOWN TRACK SINGLE PIECE FROM STATION 1003 TO 1221 PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081029 NM 2008 10 29 2008UALA06181 1 20081019 A 3320 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN IMPROPER PART A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 555UA 26647 OVERHEAD READING LIGHT ROW 26ABC OVERHEATED CAUSING BURNING SMELL IN CABIN. DEADHEADING FLT CREW REMOVED BULB AND SMELL DISSIPATED. THE REMOVED BULB IS IN COCKPIT, MAINT TO RETRIEVE BULB AND VERIFY PART NUMBER. FLT ATTENDANT REPORTED AFT CABIN FWD LAV DOME LIGHT, THAT CAUSED OVERHEAD SMELL AT 26ABC. THE 26ABC READING LIGHTS NEVER REMOVED. REPLACED LAV D OME LIGHT 1591 REF IPC33-26-52-010, TESTED GOOD. PCN 028-4739. INFO ONLY, FOUND WRONG BULB WAS INSTALLED, AND FLT CREW S REMOVED A BAD ELECTRICAL SMELL HEADSET AT 26ABC SEAT. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 AALA200802488 1 20080925 A 5320 INTERCOSTAL BOEING 737 737823 13844CB NM BS 943 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION ON TOP OF INTERCOSTAL. REPAIRED PER SRM 51-10-02-OG. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 USAA920081876 1 20080919 A 5311 6546526 FRAME BOEING 737 7373G7 138447J NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN C18 MAJOR REPAIR NR 6131828 FRAME HAS A .250 INCH CRACK AT BS 400, BETWEEN S8L AND S9L, ALSO A .500 INCH CRACK BETWE EN S8R AND S9R. REPAIRED FRAME AT BS 400, BETWEEN S8L AND S9L, ALSO BETWEEN S8R AND S9R. IAW TASK CARD NR M1C53002. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802499 1 20080926 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM BS 947 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 TUL CORROSION ON UPPER SURFACE OF FLOORBEAM BEYOND LIMITS. REPAIRED PER ESO 61000 DATED 22 SEP 08. 2 L 7 2 4F RT A16WE 20081029 EA 2008 10 29 QXEA200800885 1 20080728 A 5100 FASTENER CNDAIR CL600 CL6002C10 1390015 EA STRUCTURE MISSING A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK 2 MISSING FASTENERS AT BL 9R, FS281 AND FS283. INSTALLED FASTENERS IAW CRJ SRM 51-42-13. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 QXEA200800893 1 20080728 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK LT OTBD SEAT TRACK HAS CORROSION AT STA X-810 TO X-824. BLENDED CORROSION IAW REO 670-53-00-013 SHT 2 STEP S 1-2. MAX MATERIAL REMOVED WAS .004". BLEND IS WITHIN LIMITS IAW REO 670-53-00-013 TABLE 1. ALODINED IAW SRM 51-21-1 1. 2 L 7 2 4F RT A21EA 20081029 NM 2008 10 29 AALA200802491 1 20080925 A 5320 FLOOR SUPPORT BOEING 737 737823 13844CB NM BS 787 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 TUL CORROSION ON FLOOR SUPPORT IN AFT CARGO BEYOND LIMITS. AREA OF DISCREPANCY IS 4 INCHES BY 1 INCH. REPLACED FLOOR S UPPORT PER SRM 53-00-53. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 2008UALA06190 1 20081020 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT SEAT 5J INOP. REPLACED EEL LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 20081029 NM 2008 10 29 2008UALA06193 1 20081020 A 2497 6F16620501 WIRE HARNESS BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU POWER CORRODED A UALA K NONE M OVER TEMP IN INSP/MAINT 1 WP 29 644UA 25094 APU POWER CABLE (W236-006-1-0) HAS A CORRODED SPLICE CAUSING OVERHEAT AT BS 1783-1800 IN EMPENNAGE COMPARTMENT BELOW HOR IZ STAB RIGHT SIDE. REMOVED AND REPLACED HARNESS ASSY. INSTALLED ASSOCIATED SPLICES FOR HARNESS. OPS CHECK OF APU GEN ERATOR GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081029 NM 2008 10 29 2008UALA06201 1 20081021 A 3350 767 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA L ABORTED APPROACH W K INADEQUATE Q C FLUID LOSS IN INSP/MAINT 1 WP 29 347UA 24251 LEFT OVERWING SLIDE EEL LIGHT INOP. RELAMPED, OPS CHECK OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 20081030 NM 2008 10 30 SWAA085838 1 20081026 A 3350 PL22300L STRIP BOEING 737 7373H4 1384600 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND LT EEPLS STRIP DELAMINATED. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085839 1 20081026 A 3350 PL22300L STRIP BOEING 737 7373H4 1384600 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND RT EEPLS STRIP DELAMINATED. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085842 1 20081027 A 3350 MS25237 LIGHT BOEING 737 7373H4 1384600 NM L2 DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 655WN 28400 FOUND L2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER MM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085843 1 20081027 A 3350 MS25237 LIGHT BOEING 737 7373H4 1384600 NM L2 DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 655WN 28400 FOUND RT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER MM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085844 1 20081026 A 5754 6573714 SLAT BOEING 737 737317 138447P NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND RT WING NR 4 L/E SLAT DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085860 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085861 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 22L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085862 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 23L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085863 1 20081028 A 3350 PL22300L LIGHT BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED 14Y CHECK, FOUND LT EEPLS CRACKED AT ROW 20 ABC. REMOVED AND REPLACED EEPLS PER MM. 2 L 7 2 4F RT A16WE 20081031 EU 2008 10 31 NSV2008F00028 1 20080929 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN NONE A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 347CJ 340B347 EMERGENCY LIGHTS ARE ON WITH SWITCH IN THE ARM POSITION AND ACFT POWERED FROM BATTERIES. PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM IAW AMM 33-50-00 AND WC 33-50-016. NO FAULT FOUND. NOTE: EMERGENCY LIGHTS SYSTEM IS DESIGN ED TO ILLUMINATE IF ARMED WITHOUT RT MAIN BUSS POWERED. SYSTEM OPERATING AS DESIGNED. (K) 2 L 7 2 4T RT A52EU 20081031 SO 2008 10 31 RAIA00809026 1 20080924 A 3350 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 834HK 145269 AIRSTAIR HANDRAIL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE HANDRAIL. OPS CHECKED GO OD. (K) 2 L 7 2 4T RT T00011AT 20081031 EA 2008 10 31 VNAA0809008 1 20080809 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 250PS 7929 CREW REPORTED A FLAPS FAIL AT 8 DEGREES AFTER TAKEOFF AND FLAPS FAILED TO RETRACT. CREW DECLARED AN EMERGENCY. CREW ELEC TED TO RETURN TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINT INSPECTED ACFT AND PERFORMED CHECKS. NO DEFECTS WERE NOTED . ACFT RELEASED FOR SERVICE. (K) 2 L 7 2 4F RT A21EA 20081031 NM 2008 10 31 NSV2008F00029 1 20080927 A 5240 SEAL BOMBDR DHC8 DHC8402 1390042 NM SERVICE DOOR LACK OF LUBE A NSVA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 27 214WQ 4214 RT AFT SERVICE DOOR ILLUMINATED THE FUSELAGE DOORS LIGHT INFLIGHT. PERFORMED OPS CHECK AT RT AFT SERVICE DOOR IAW AMM 5 2-41-00-710-801. OPS CHECK GOOD. COULD NOT DUPLICATE FAULT. LUBRICATED DOOR SEALS IAW RIL 84-12-003. (K) 2 H 7 2 4T RT A13NM 20081031 EA 2008 10 31 ASOA200801211 1 20080919 A 3200 BPSU CNDAIR CL600 CL6002B19 1900309 EA MLG INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED AND REPLACED LT O/B BPSU IAW AMM 32-43-26, OPS CHECK GOOD AND RII C/W PER SP-607. 2 L 7 2 4F RT A21EA 20081031 NM 2008 10 31 08FDEA04586 1 20081028 A 5753 ARB0029509 STRAP DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 607FE 48547 LEFT WING, OUTBOARD FLAP INBOARD HINGE (WINGSIDE) TENSION STRAP FITTING FOUND CRACKED. R & R AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081031 NM 2008 10 31 ASAA0843681 1 20081012 A 5320 DOUBLER BOEING 737 737490 1384715 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 L1 DOOR HINGE CUTOUT FOUND DOOR DOUBLER CRACKED AT LOWER HINGE. REPAIRED DOUBLER IAW ASA EA 5330 02402 BY INSTALLING DO UBLER AND TRIPLER. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 ASAA0843678 1 20081007 A 5753 SKIN BOEING 737 737490 1384715 NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 LT TRAILING EDGE FLAP LOWER SURFACE DENT AT 42 INCHES FROM INBOARD AND 3.5 INCHES FWD OF TRAILING EDGE. PREPPED DAMAGED AREA AND BONDED THE REPAIR IAW B737 400 SRM 51 70 16 REP 11. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 ASAA0843680 1 20081008 A 5753 SKIN BOEING 737 737490 1384715 NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 LEFT INBD AFT FLAP LOWER SURFACE HAS MULTIPLE DENTS. PREPPED DAMAGED AREA AND BONDED THE REPAIR IAW B737 400 SRM 51 70 16 REP 11 IN THE SRM. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 ASAA0843670 1 20081007 A 5330 6546881 SKIN BOEING 737 737490 1384715 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 DENT FOUND ON BELLY SKIN AT BS 1020 RBL 13.5, DENT IS WITHIN 3 INCHES OF SKIN SPLICE. REMOVED DAMAGED AREA, FABBED FILL ER AND DOUBLER AND INSTALLED REPAIR PARTS IAW B737 400 SRM 53 80 01 REP 2. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 CALA0801013 1 20081028 A 3350 D71701100 BATTERY PACK BOEING 737 737724 13844BY NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13750 28941 FORWARD ENTRY AND FLIGHT DECK EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY BATTERY PACK, OPERAT ION CHECKS GOOD. 2 L 7 2 4F RT A16WE 20081031 EA 2008 10 31 CHQA200800212 1 20081027 A 3040 16591 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE COCKPIT DEFECTIVE A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 650BR 69 69 7418 GEE872770 FLIGHT 5585, CLE TO RDU. DURING CRUISE THE FLIGHT CREW RECEIVED A RIGHT WINDOW HEAT EICAS MESSAGE. THE QRH PROCEDURE W AS FOLLOWED BUT THE MESSAGE REMAINED. THE FLIGHT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE MEASURE THE RESISTANCE OF THE WINDOW AND ALL RESISTANCES WERE WITHIN LIMITS. THE TEMP CONTROLLER WAS THEN REPLACED AND THE WINDOW H EAT CHECKED GOOD. ON THE 29TH THE FAULT RETURNED AND BOTH THE RIGHT HAND WINDOW AND WINDSHIELD WERE REPLACED. THE WIND OW HEAT CHECKED GOOD AFTER THE TEMP CONTROLLER WAS REPLACED AGAIN. 2 L 7 2 4F 4 F RT A21EA E15NE 20081031 EA 2008 10 31 ASOA200801043 1 20080822 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED AND REPLACED 625 OBLIQUE ANGLES ON LT AND RT SIDES IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 20081031 CE 2008 10 31 DXTA2008102803323 1 20081027 A 2920 HYDRAULIC SYSTEM CESSNA 750 750 2076810 CE B SYSTEM LEAKING E DXTA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 GL 07 977QS 7500077 B-HYDRAULIC SYSTEM LOST FLUID EN ROUTE TO DISTINATION. EMERGENCY DECLARED. 2 L 7 2 4J RT T00007WI 20081031 CE 2008 10 31 DXTA2008103003328 1 20081029 A 3020 WARNING SYSTEM CESSNA 750 750 2076810 CE ANTI-ICE SYSTEM ACTIVATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 946QS 7500195 ENG ANTI-ICE HOT R CAS MESSAGE APPEARED DURING T/O ROLL, ABORTED T/O. 2 L 7 2 4J RT T00007WI 20081031 2008 10 31 DXTA2008102903324 4 20081028 A 2210 WARNING SYSTEM CESSNA 750 750 2076810 CE COCKPIT ACTIVATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 950QS 7500050 ON TAKEOFF ROLL AT 65 KTS, MASTER CAUTION "YD OFF LWR" EICAS MESSAGE. ABORTED T/O. 2 L 7 2 4J RT T00007WI 20081031 CE 2008 10 31 DXTA2008102903325 1 20081028 A 2120 UNKNOWN CESSNA 560 560XL 2076702 CE CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 07 654QS 5605611 DURING PREFLT WITH APU RUNNING SMOKE FILLED THE CABIN. (KLUK) 2 L 7 2 4F RT A22CE 20081031 WP 2008 10 31 U2RA872CWO1839 1 20081024 A 5720 STRAP DOUG DC8 DC871F 302199D WP RT WING CRACKED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 872SJ 83402 2078 46040 DURING C-CHECK, FOUND RT WING XFS 6.225 CENTER LEADING EDGE INTERIOR LOWER STRAP HAS 5 INCH CRACK. 2 L 7 4 4F RT 4A25 20081031 NM 2008 10 31 2008UALA06265 1 20081024 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 61 LEFT. REPLACED LAMP ASSY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081031 NM 2008 10 31 2008UALA06273 1 20081024 A 5753 ATTACH FITTING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE TE FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 LT WING OUTBOARD FLAP, OUTBOARD, AUX TRACK ATTACH FITTING TO RS, IS CRACKED. REPLACED FITTING. 2 L 7 2 4F 4 F RT A1NM E24NE 20081031 NM 2008 10 31 2008UALA06278 1 20081025 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 122UA 29168 EEL LIGHTS SEAT 4A AND 2J HANGING OFF SEAT AND NOT SECURE. SECURED EEL LIGHTS TO SEATS SIDE PANELS. 2 L 7 4 4F 4 F RT A20WE E24NE 20081031 NM 2008 10 31 2008UALA06263 1 20081024 A 3397 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EXIT EEL LIGHT INOP JUST AFT OF SEAT 8GH BELOW COAT CLOSET. SECURED CONNECTOR, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081031 2008 10 31 2008UALA06279 4 20081025 A 2350 MICROPHONE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 594UA 28145 CAPT OXYGEN MASK MIC INOP. CLICKS WITH PTT, BUT NO SOUND. SWAPPED FIRST OBS MASK TO CAPT POSITION AND CAPT O2 MASK TO FIRST OBS. MASK WORKS EXCEPT FOR MIC. INSTALLED NEW O2 MASK AT 1ST OBSERVERS POSITION. MIC OPS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081031 CE 2008 10 31 Z5FA102308N617CS 1 20081023 A 3233 99146763 ACTUATOR CESSNA 680 680SOV 2076811 CE NLG FAILED E Z5FA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 63 617CS 2058 6800102 NOSE GEAR DID NOT RETRACT WHEN LANDING GEAR WAS SELECTED UP. NOSE GEAR DOWN AND LOCKED INDICATOR REMAINED ON. NOSE LAN DING GEAR ACTUATOR REPLACED. OPERATIONAL CHECK GOOD, AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RC T00012WI 20081031 EA 2008 10 31 ASOA200801395 1 20081025 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 906EV 7642 NOSE DOOR AND GEAR DISAGREE WARNING MSG. A/C RETURNED TO MDT AFTER T/O, EMERGENCY DECLARED. FLT 5204 CX. 2 L 7 2 4F RT A21EA 20081031 EA 2008 10 31 ASOA200801400 1 20081025 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 FLIGHT ATTENDANT REPORTS DIFFICULTY CLOSING MAIN CABIN DOOR. FLT 4941 DEL 23 MINS. 2 L 7 2 4F RT A21EA 20081031 NM 2008 10 31 HALA2008102500828 1 20081025 A 2720 CONTROL SYSTEM BOEING 717 717200 1383700 NM RUDDER MALFUNCTIONED A HALA K NONE S AFFECT SYSTEMS CR CRUISE 1 WP 13 596HA 23276 ETOPS SIGNIFICANT SYSTEM - RUDDER RATIO INOP IN FLT. PERFORMED FIM 27-21-00 FIG 104, NO FAULTS NOTED. OK FOR SERVICE. 2 L 7 2 4F TR A6WE 20081031 NM 2008 10 31 HALA2008102900830 1 20081029 A 2910 FITTING BOEING 767 7673G5 1385126 NM LT MLG WW LOOSE A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEMS - ON ETOPS1 CK FOUND ADP MODULE IN LT WHEEL WELL LEAKING AT UNION. RE-TORQUED UNION AND B-NUT , LEAK CHECK GOOD. SERVICED HYD, OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20081031 NE 2008 10 31 2008UALA06295 2 20081028 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 FIRE A UALA O OTHER A FLAME/FIRE IN INSP/MAINT 1 WP 29 449UA 851 V10470 NR 1 ENG - FIRE IN TAIL PIPE AFTER SHUTDOWN. SUSPECT OIL LEAK. 2 L 7 2 4F 4 F RT A28NM E40NE 20081031 NM 2008 10 31 2008UALA06290 1 20081027 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EEL LIGHTS INOP DOOR 5R SILL, EXIT, OVERHEAD. REPLACED BATTERY. CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081031 NM 2008 10 31 2008UALA06292 1 20081026 A 3397 7846243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EEL LIGHT INOP SEAT 58 ABC. FOUND LAMP INOPERATIVE. SECURED EEL LIGHT ASSY CONNECTOR. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081031 NM 2008 10 31 2008UALA06293 1 20081028 A 2421 745329F IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 655UA 25393 LEFT IDG RISE SHOWS 0 TEMP, RIGHT IDG SHOWS 17. CLEANED AND SECURED L IDG CONNECTORS. INSTALLED NEW GCU WITH NO HELP. R EINSTALLED OLD GCU. REPLACED NR 1 ENGINE IDG. IDG OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081031 NM 2008 10 31 2008UALA06283 1 20081025 A 5320 SHEAR PLATE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 820UA 898 SHEAR PLATE AFT OF DOOR SILL 2 LEFT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED PLATE. FWD HI-LOKS IN PLATE NEED TO BE INSTALLED. COMPLETED INSTALLATION. 2 L 7 2 4F 4 F RT A28NM E40NE 20081031 NE 2008 10 31 AALA200802386 2 20080920 A 7200 ROTOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE SEIZED A AALA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 21 9404V 53140 725493 ORD INFLIGHT T779/20SEP. AT APPROX 2000 FEET NR 1 ENGINE LOST ALL POWER. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE ON 20 SEP AT ORD DUE TO ROTOR SEIZED. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F 4 F RT A6WE E9NE 20081031 WP 2008 10 31 AALA200802532 1 20080919 A 5320 BRACKET DOUG DC9 DC982 3022082 WP BS 1193 L29R CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70504 49798 CORROSION FOUND ON L BRACKET IN AFT CARGO AT STATION 1193 LONGERON 29 RT. AREA OF DISCREPANCY IS 1/2 INCH BY 1 INCH WIT H A DEPTH OF .060 INCH. INSTALLED NEW L BRACKET IN AFT CARGO AT STATION 1193 LONGERON 29 RT PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081031 NM 2008 10 31 AALA200802330 1 20080808 A 5313 141T3001 STRINGER BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 332AA 22331 AFW STRINGER WAS CORRODED FROM STATION 425 TO 443. REPAIRED PER SRM 53-00-03-2R2 WITH EXCEPTIONS PER MRB 767 3272. 2 L 7 2 4F RT A1NM 20081031 NM 2008 10 31 AALA200802384 1 20080920 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 793AN 30255 NRT EMERGENCY LIGHT AT FIRST CLASS CLOSET BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FIRST CLASS CLOSET. S YSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081029 NM 2008 10 29 2008UALA06203 1 20081021 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 771UA 26932 SEAT 1E AFT EEL LIGHT INOP. REPLACED LAMP. TESTED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081029 NM 2008 10 29 2008UALA06205 1 20081021 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 771UA 26932 SEAT 2F FORWARD EEL LIGHT INOP. REPLACED LAMP, CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081029 NM 2008 10 29 2008UALA06223 1 20081021 A 5712 RIB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 LT WING O/B LEADING EDGE CAVITY, LWR RIB FWD END CRACKED AT OFSS 688. MAJOR REPAIR ACCOMPLISHED. REMOVED RIB, INSTALLE D NEW RIB AND LOWER STRUT. 2 L 7 2 4F 4 F RT A1NM E24NE 20081029 NM 2008 10 29 2008UALA06168 1 20081017 A 3350 3071BPEGPL LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 781UA 26945 SEAT 36G EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT, TESTED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081029 NM 2008 10 29 2008UALA06222 1 20080908 A 2121 65772 FAN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EQUIP COOLING FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 398UA 24673 CREW REPORT: ALT EQUIP COOLING FAN INTERMITTENT AT FL250 SAMC TEXT: PACKS AND CABIN PRESSURIZATION NORMAL, ALT EQUIP C OOLING EXHAUST FAN 'OFF' LIGHT FLICKERING ON INTERMITTANTLY. FOUND EXHAUST DUCT FORWARD OF MUFFLER CLOGGED WITH DUST AN D DIRT RESTRICTING EXHAUST AIRFLOW PAST SENSOR M100. REPLACED SENSOR PRECAUTIONARY AND BLEW THE DUCT FREE OF DUST AND D IRT. FLOW FOUND SATISFACTORY. ALL ELECTRICAL CHECKS OF THE FANS NORMAL AND ALTERNATE WERE FOUND NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20081029 EU 2008 10 29 2008UALA06191 1 20081020 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 471UA 1432 EEL LIGHTS AT ROWS 8 AND 9 SEATS ABC ARE INOP. RELAMPED EMERGENCY LIGHTS, NO HELP. FOUND CONNECTOR AT BOTTOM OF SEAT L OOSE. CLEANED CONNECTOR AND SECURED. EEL LIGHT WORK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081029 NM 2008 10 29 2008UALA06209 1 20081019 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 548UA 25396 DOOR 4R EMERGENCY LIGHT OUT, OUTSIDE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 EU 2008 10 29 2008UALA06210 1 20081021 A 5520 D55280001000 ELEVATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LEFT DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 408UA 457 OUTBOARD 3FT OF LEFT ELEVATOR DAMAGED. ELEVATOR REMOVED. NEW ELEVATOR INSTALLED. SAFETIED AND RIGGED AND TESTED LT ELEV ATOR. OPS CHECKS OK. NO LEAKS NOTED FROM ACTUATORS. 2 L 7 2 4F 4 F RT A28NM E40NE 20081029 NM 2008 10 29 2008UALA06211 1 20081022 A 2421 745329F IDG BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LEFT LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 666UA 29238 EICAS MSG L GEN DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUM. GEN DRIVE DISCONNECTED. CREW COMMENTS: L T ENG DRIVE LIGHT CA ME ON AFTER T/O AND WENT OUT AFTER TWO MINUTES WITH NO CREW ACTION. FUEL OIL COOLER LEAKING AND IDG DRY. REPLACED NR 1 ENGINE IDG & NR 1 ENG FUEL OIL COOLER & BYPASS VALVE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081029 NM 2008 10 29 2008UALA06212 1 20081022 A 3010 ANTI-ICE SYSTEM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 654UA 25392 CREW REPORT: WING ANTI ICE DISAGREEMENT L-R. 2 L 7 2 4F 4 F RT A1NM E24NE 20081029 NM 2008 10 29 CALA0800982 1 20081023 A 5315 141T5108 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 68155 30434 BODY STATION 325 FLOOR SUPPORT FOUND CORRODED BETWEEN LBL 26 -59. BODY STATION 325 FLOORBEAM LBL 13 - LBL 62 REPAIRED P ER SRM 53-00-51 REPAIR 1, FIG 201. HFEC NO CRACK FOUND. 2 L 7 2 4F RT A1NM 20081029 NM 2008 10 29 CALA0800983 1 20081023 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 BODY STATION 400R FRAME CRACKED AT AIR CONDITION (A/C) BRACKET BETWEEN S-8 AND S-9. CUT OUT DAMAGE ON FRAME AT STATION 400 BETWEEN STR 8R AND 9R, REPAIRED SAME IAW EA 5310-04498. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0800988 1 20081023 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 BODY STATION 440 RT SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S8 AND S9. CUT OUT DAMAGE ON FRAME AT STATION 440 BETWEEN S8R AND S9R REPAIRED SAME IAW EA 5310-04498. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0800990 1 20081023 A 5311 65C34355 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 BODY STATION 482 RT SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. CUT OUT DAMAGE ON FRAME A T STATION 482 BETWEEN S8R AND S9R, REPAIRED SAME IAW EA 5310-04498. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0800991 1 20081023 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 BODY STATION 827R FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED BODY STATION FRAME 827 RIGHT AT S8R AND S9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0800992 1 20081023 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 BODY STATION 907R FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED BODY STATION 907 RIGHT FRAME AT S8R AND S9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0800993 1 20081023 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 BODY STATION 787R FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. REPAIRED BODY STATION 787 RIGHT FRAME AT S8R AND S9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0800998 1 20081023 A 5320 141A5211U1 INTERCOSTAL BOEING 737 737924 13848A1 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 30401 30118 CONTROL CABIN AFT CENTER FLOOR INTERCOSTAL CORRODED BETWEEN STATION 259 AND 268 AT BL 0 AND WL 207. REMOVED OLD INTERCO STAL AND INSTALLED NEW PART (141A5211U1) PER SRM 53-10-51 AND INSTALLED FASTENERS PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0800999 1 20081023 A 5315 147A5506 FLOORBEAM BOEING 737 737924 13848A1 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 30401 30118 FLOORBEAM AT STATION 986.5 UPPER FLANGE BLENDED OUT OF LIMITS. REPAIRED FLOORBEAM 986.5 AT RBL 11 PER SRM 53-00-51 REPA IR 1. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 08FDEA04549 1 20081025 A 5310 65561533 CREASE BEAM BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 R-1 DOOR CREASE BEAM WEB CRACKED AT FWD END OF CUT-OUT. REMOVED AND REPLACED RT CREASE BEAM WEB REF DWG 65-56153 AND SR M 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 CALA0801001 1 20081023 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 BODY STATION 400L FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S8 AND S9. REPAIRED FRAME AT BODY STATION 400 L BETWEEN S-8 AND S-9 IAW EA 5310-04498. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 08FDEA04550 1 20081025 A 2697 8956831 SWITCH DOUG MD11 MD11F 3023600 NM FIRE DETECTOR DAMAGED A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 21 605FE 48514 "CRG FIRE LWR AFT" LEVEL 3 ALERT AND AURAL WARNING ON TAKEOFF ROLL. ABORTED TAKEOFF AND DISCHARGED BOTH FIRE BOTTLES. PERFORMED AFT AND FWD CARGO COMPT INSPECTION, NO DAMAGED OR FIRE CONDITION FOUND. VERIFY WITH FLT CREW THAT THEY DISCHA RGED AGENT 1 (THE BIG BOTTLE) ONLY. MSC FAULT REVIEW SHOWN 'MSC' NO OTHER RELATED FAULT. REMOVED AGENT 1 FIRE BOTTLE PER AMM 26-22-01-4 AND FOUND P1-2286 CONNECTOR BROKEN OFF. SUPP, R & R LOWER CARGO FIRE EXTINGUISHER CONTAINER NR 1 PER MM 26-22-01-4, FOUND FWD & AFT AGENT 1 LOW PRESS LIGHT ON. T/S FIM 26-22-01 FOUND LOW PRESS SWITH AT FAULT ,PRESSURE SWITCH PIN "A" & "B" IN CLOSED. 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 08FDEA04551 1 20081026 A 5320 65575703 PANEL BOEING 727 7272D4 138407U NM ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 PANEL RACK, EDGE PANEL STA 1030 TO STA 1166 RBL 19 TO 28 AFT PLATE OB EDGE BROKEN AND CORRODED UPPER SURFACE BLENDED COR ROSION ORG "T" .040, MATERIAL LOSS OF .005 AT DEEPEST POINT WITHIN LIMITS. REF SRM 53*-10-1 FIG 7 TOOL NR AAR20278 CAL DUE 12-11-08. REPAIRED EDGE CRACK WITH WEB REPAIR REF SRM 51-40-2. REPAIR CLASSIFIED AS MINOR. 2 L 7 3 4F A3WE 20081028 SO 2008 10 28 GUU2008F00060 1 20080915 A 3350 BATTERY PACK EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS INOPERATIVE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 268AS 120202 DURING SCHEDULED ROUTINE MAINT DISCOVERED NR 3 EMERGENCY LIGHT BATTERY PACK INOPERATIVE. RECHARGED NR 3 EMERGENCY LIGHT BATTERY PACK. (K) 2 L 7 2 4T RT A31SO 20081028 CE 2008 10 28 TIMA20080005 1 20081002 A 2910 115811026 FITTING BEECH 99 C99 1154006 CE HYD POWERPACK MISSING E TIMA O OTHER S AFFECT SYSTEMS LD LANDING 1 NM 07 216CS 22435 U216 LANDING GEAR FAILED TO EXTEND WHEN SELECTED. GEAR WAS PUMPED DOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. INVESTIGATION REVEALED THAT THE C-CLIP ON THE HYDRAULIC POWERPACK COUPLING WAS MISSING AND ALLOWED THE COUPLING TO MIGRATE ON THE SHAF T UNTIL IT NO LONGER CONNECTED THE MOTOR TO THE PUMP. 1 L 7 2 3T A14CE 20081028 EU 2008 10 28 USAA920081859 1 20080927 A 5320 D53112609200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C7 MAJOR REPAIR NR 6109614. CORROSION ON FLOOR SUPPORT BETWEEN FR12 TO FR20, Y1380. REPLACED FLOOR SUPPORT BETWEEN FR 12 TO FR20, Y1380 IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081028 SO 2008 10 28 RAIA2008102300006 1 20081021 A 5210 DOOR EMB 145 EMB145LR 3260212 SO PAX DOOR MALFUNCTIONED A RAIA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 03 822HK 145069 DURING INSPECTION, THE PASSENGER DOOR WAS DIFFICULT TO OPERATE. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE MAIN D OOR AND LOAD TEST OF THE INTERNAL HANDLE. ALL CHECKS WERE FOUND TO BE WITHIN LIMITS. DOOR OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081028 NM 2008 10 28 2008UALA06156 1 20081017 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHT INOP DOOR 2L FWD SILL. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 20081028 NM 2008 10 28 2008UALA06163 1 20081015 A 5220 BACC2A4D00134JJ CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE AFT RT OVERWING FRAYED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 644UA 25094 AFT RT OVERWING HATCH STEP AFT CABLE FRAYED. REPLACED CABLE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081028 NM 2008 10 28 ASAA0843623 1 20081015 A 3397 MS2524415 LIGHT BOEING 737 7374Q8 138447Q NM CARGO BAY MISWIRED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 CABIN MAIN CARGO LIGHT 15AMP CIRCUIT BREAKER C9001 FAIL TO TRIP WHEN FWD UPPER CARGO LIGHT WAS MISWIRED ALLOWING POSITIV E TO GROUND CAUSING J10 BOX TO BURN UNTIL ELECTRICAL CIRCUIT OPENED. REFERENCE PEMCO WDM 33 30 02 PAGE 3 SHEET 1. REPA IRED IAW AAR EA 12982 AND ASA EA 3330 01021. REBUILT J 10 BOX INSPECTED AND REPLACED DAMAGED WIRING. INSPECTED AND REP AIRED AS REQUIRED ADJACENT WIRE RUNS FROM J10 BOX TO CARGO OVERHEAD LIGHTING. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873625 1 20081003 A 5320 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE SCRATCHED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 FWD PASSENGER CABIN SCRATCHES ON FLOORBOARD SUPPORT BS 312 TO BS 328 RBL 10. FLOORBOARD SUPPORT BEAM AT BS 312 TO BS 32 8 RBL 10 REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873628 1 20081003 A 5320 141A83125 SILL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 FWD PASSENGER CABIN RT FWD DOOR SILL CHORD HAS MINOR CORROSION AT BS 328 RBL 62. REPLACED DAMAGED PART WITH NEW PART. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873630 1 20081001 A 5320 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 AFT CARGO PIT CORROSION FOUND ON FLOOR SUPPORT AT BS 767+6 RBL 3. AFT CARGO PIT CORROSION ON FLOOR SUPPORT BLENDED OUT AND FOUND BEYOND LIMITS AND REPAIR ACCOMPLISHED IAW B737 700 SRM 53 00 53 REPAIR 2 FIG 201. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873631 1 20081001 A 5320 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 AFT CARGO PIT CORROSION FOUND ON FLOOR SUPPORT AT BS 767 + 6 LBL 3. AFT CARGO PIT CORROSION ON FLOOR SUPPORT BLENDED OU T AND FOUND TO BE BEYOND LIMITS AND REPAIR ACCOMPLISHED IAW B737 700 SRM 53 00 53 REPAIR 2 FIG 201. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873632 1 20081001 A 5320 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 AFT CARGO PIT CORROSION FOUND ON FLOOR SUPPORT AT BS 767 + 6 LBL 8.1. AFT CARGO PIT CORROSION ON FLOOR SUPPORT BLENDED OUT AND FOUND TO BE BEYOND LIMITS AND REPAIR ACCOMPLISHED IAW B737 700 SRM 53 00 53 REPAIR 2 FIG 201. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873633 1 20081001 A 5320 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 AFT CARGO PIT CORROSION FOUND ON FLOOR SUPPORT AT BS 767 + 6 LBL 17.24. AFT CARGO PIT CORROSION ON FLOOR SUPPORT BLENDE D OUT AND FOUND TO BE BEYOND LIMITS AND REPAIR ACCOMPLISHED IAW B737 700 SRM 53 00 53 REPAIR 3 FIG 201. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873650 1 20081005 A 5330 146A81271 SHIELD BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE N FALSE WARNING IN INSP/MAINT 1 NM 02 624AS 30778 AFT CARGO PIT DOOR SURROUND FWD SHIELD HAS SURFACE CORROSION FROM BS 767 TO BS 795 STR 25R. AFT CARGO PIT SHIELD CORROS ION BLENDED OUT. BLEND AREA FOUND TO BE BEYOND LIMIT. SHIELD REPLACED WITH REPAIR PART IAW B737 700 SRM 53 60 15 AND 5 1 40 02. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873656 1 20081001 A 5321 453A26102 FLOOR PANEL BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 AFT CARGO PIT FLOOR PANEL AT BS 767 TO 887 HAS CORROSION ON UPPER EDGES AND NUMEROUS GOUGES ON THE SIDE. AFT CARGO PIT FLOOR PANEL AT BS 767 TO 887 CORROSION BLENDED OUT. BLEND AREA FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMIT AND GOUGES FOU ND TO BE BEYOND LIMITS. FLOOR PANEL REPLACED IAW B737 700 SRM 51 40 05. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873642 1 20081001 A 5320 146A9401 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 AFT CARGO PIT CORROSION ON FLOOR SUPPORT TRACK BS 787 TO BS 847 + 6 RBL 14. FLOOR SUPPORT TRACK FOUND TO BE BEYOND LIMI T. REPLACED WITH MADE REPAIR PART IAW DWG 146A7501 AND SRM B737 700 51 40 02. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085748 1 20081022 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 362SW 26573 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT DOOR SIDEWALL LAMP INOP. REMOVED AND REPLACED LAMP PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085766 1 20081023 A 5330 6545771 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 638SW 27711 DURING SCHEDULED 12Y CHECK, FOUND RT MAIN WHEEL WELL LOWER CHORD SKIN CRACKED AT BS 679. REMOVED AND REPLACED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085687 1 20081019 A 3350 PL2230LH0 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 446WN 29842 DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS INOP. REPAIRED TRACK LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085688 1 20081017 A 3350 PL2230LH0 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 449WN 32469 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS COVER MISSING AT ROW 1 ABC. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085689 1 20081016 A 3350 65C3330484 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 461WN 32465 FOUND RT OVERWING EMEGENCY EXIT DOOR SIDEWALL LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085767 1 20081026 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 784SW 29810 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 30. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085768 1 20081026 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 784SW 29810 DURING SCHEDULED 8Y CHECK, FOUND LT EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085770 1 20081025 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 275WN 36153 DURING SCHEDULED MV2 CHECK, FOUND AFT RT EMERGENCY EXIT SIGN LENS COVER MISSING. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081103 SO 2008 11 3 C2XA08IA226 1 20081016 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145XR 3260214 SO LAVATORY FALSE ACTIVATION A C2XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 27 11176 10564 14500881 IAW FLIGHT 2703 DURING CRUISE THE CREW REPORTED A LAV SMOKE INDICATION ON EICAS. THE ACFT RETURNED TO IAW WHERE IT LAND ED WITHOUT INCIDENT. MX INSPECTED THE ACFT WITH NO EVIDENCE OF SMOKE FOUND, R&R THE LAV SMOKE DETECTOR. OPS CHECKED WI TH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081030 EA 2008 10 30 MASA2008102400749 1 20081024 A 5210 SEAL CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR LEAKING A MASA O OTHER O OTHER CR CRUISE 1 SW 07 923FJ 15023 ASH FLT 2829 PHX-TUS - PILOT REPORTED THAT THE MAIN CABIN DOOR WAS SQUEALING IN FLIGHT. MX REPOSITIONED THE DOOR SEAL A ND LEAK CHECKED IT. 2 L 7 2 4F RT A21EA 20081030 SO 2008 10 30 LR7A08119 1 20081015 A 5350 SKIN LKHEED 382 382G 526414U SO FAIRING CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 713 4763 DURING SCHEDULED B-3 CHECK, PER HB5301 JOB CARD FOUND LT MLG BOTTOM SKIN FAIRING CRACKED AT FS 597, LBL40, WL129 ATTACHM ENT TO BELLY AREA. REPAIRED IAW SMP583 FIG 51-140-12. 2 H 7 4 4T A1SO 20081030 WP 2008 10 30 AALA200802616 1 20080929 A 5320 99367183 INTERCOSTAL DOUG DC9 DC983 3022083 WP ZONE 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON INTERCOSTAL BETWEEN LEFT STATIONS 1309 AND 1322. AREA OF DISCREPANCY IS 12 INCHES BY 6 INCHES. REPL ACED INTERCOSTAL IN ACCORDANCE WITH SRM 51-10-1. 2 L 7 2 4F RT A6WE 20081030 NM 2008 10 30 DHLA200800118 1 20081029 A 3397 CIRCUIT BREAKER BOEING 727 727264 138408M NM EMERGENCY LIGHTS TRIPPED A DHLA O OTHER O OTHER CL CLIMB 1 GL 05 763AT 22983 DURING THE CLIMB-OUT OF KILN, EMERGENCY EXIT CONTROL RT C/B POPPED. COCKPIT EMERGENCY EXIT LIGHTS OPERATE NORMAL. 2 L 7 3 4F A3WE 20081030 WP 2008 10 30 AALA200802625 1 20080930 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON RIGHT CUSP MEMBRANE BETWEEN STATIONS 484 AND 503. AREA OF DISCREPANCY WAS 3 INCHES BY 15 INCHES. IN STALLED DOUBLER REPAIR ON RIGHT CUSP AT STATION 495 TO 502 IN ACCORDANCE WITH AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081030 NM 2008 10 30 DHLA2008745577 1 20080903 A 5241 FRAME BOEING 727 727224 1384076 NM GALLEY DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE CABIN FWD GALLEY DOOR AFT UPPER CORNER FRAME WITH CRACK. REPAIRED FWD GALLEY DOOR AFT UPPER FRAME SECTIO N BETWEEN DOOR BEAM NR 1 AND DOOR BEAM NR 3 IAW S/B 727-52-114 DTD FEB 24,1978 SECT 3 PART 3 PARA F DWG 69-69978 REV B D TD 1/18/77. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 L19A2008102400050 1 20081019 A 2742 500N72181 ADAPTER DOUG MD900 MD900 3027375 NM VERTCAL STAB BROKEN E L19A A UNSCHED LANDING F FLT CONT AFFECTED AA AIR AMBULANCE 1 SW 13 902NM 60 90000105 THE HELICOPTER WAS IN CRUISE FLIGHT AND THE VSCS ADAPTER BROKE IN TWO. THIS CAUSED THE A CONTROL PROBLEM WITH THE HELIC OPTER UNTIL IT SLOWED BELOW 100 KTS. THE AIRCRAFT CAME BACK TO THE AIRPORT AND LANDED WITH NO PROBLEMS. THERE IS NOW A NEW AD ON THIS MATTER. (SEE AD2008-22-53). 1 G 7 2 3U NC H19NM 20081030 SO 2008 10 30 GLBA200810242 1 20081023 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO LT WING CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 71GL 120071 MAJOR REPAIR - DURING SCHEDULED MAINTENANCE THE NR 8 STRINGER WAS FOUND CRACKED ON THE LOWER WING SKIN JUST INBOARD OF R IB NR 5 AT APPROXIMATELY WS 1380. APPROXIMATE CRACK LENGTH 2 INCHES. MAINTENANCE INSTALLED SPLICE. RII INSPECTION COM PLIED PER TASKCARD 8.2.1. 2 L 7 2 4T RT A31SO 20081030 SO 2008 10 30 C2XA08IA229 1 20081020 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13995 145295 PREFLIGHT INSPECTION THE CREW REPORTED AN AISLE PATH LIGHT STRIP TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE AISLE PATH LIGHTING WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081030 NM 2008 10 30 KCSA081546 1 20081026 A 3350 SIGN BOEING 747 747221F 1384868 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 748CK 21744 UPPER DECK EMERGENCY EXIT SIGN IS INOPERATIVE. 2 L 7 4 4F RT A20WE 20081030 CE 2008 10 30 DJFA2008078 1 20081024 A 3310 12838008117 PANEL BEECH MU300 400A 1155402 CE COCKPIT DEFECTIVE E DJFA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 23 454LX RK327 DURING FLIGHT CREW REPORTED STRONG ELECTRICAL SMELL IN THE AIRCRAFT. MAINTENANCE FOUND A DEFECTIVE ELECTROLUMINSCENT PA NEL. THE FAILED EL PANEL WAS REPLACED. 2 H 7 2 4F RT A16SW 20081030 SO 2008 10 30 C2XA08IA230 1 20081026 A 3234 7455503 CONTROL LEVER EMB 145 EMB145XR 3260214 SO COCKPIT DEFECTIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16112 17638 17638 145660 FLIGHT 4917, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE WARNING DURING RETRACTION. THE AIRCRAFT RETURNED TO IAH WH ERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER, OPERATIONALLY TESTED WITH NO D EFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081030 SO 2008 10 30 CHQA200800209 1 20081022 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 267SK 145268 CAE311659 FLIGHT 5912, CLE TO CMH. THE EMERGENCY LIGHT ABOVE THE FLIGHT ATTENDANTS SEAT WAS FOUND TO BE INOP. THE EMERGENCY LIGH T INVERTER WAS REPLACED AND THE SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081030 EA 2008 10 30 CHQA200800210 1 20081023 A 2613 26212000 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NR 1 ENGINE MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 638BR 7311 GEE872506 FLIGHT 5601, IAH TO JAX. DURING CLIMB THE FLIGHT CREW RECEIVED AN L JETPIPE OVHT FAIL CAUTION MESSAGE. THE MESSAGE APP EARED AND EXTINGUISHED SEVERAL TIMES. THE QRH CHECKLISTS WERE FOLLOWED AND A L JETPIPE OVERHEAT MESSAGE APPEARED ALONG WITH THE TRIPLE CHIME. THE POWER WAS REDUCED ON E1 AND THE FLIGHT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MA INTENANCE REPLACED BOTH THE A AND B JET PIPE OVERHEAT LOOPS AND THE SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 20081030 NM 2008 10 30 SWAA085827 1 20081025 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CRACKED AT R1 DOOR. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085828 1 20081028 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND AFT EMERGENCY EXIT FLASHLIGHT INOP. REMOVED AND REPLACED BATTERIES PER MM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085830 1 20081027 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER PAE EA. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085831 1 20081027 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER PAE EA. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085836 1 20081026 A 3350 6573709 LIGHT BOEING 737 7373H4 1384600 NM COCKPIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 389SW 26592 FOUND COCKPIT CONTROL EMERGENCY EXIT LIGHT INDICATOR INOP. REMOVED AND REPLACED KORRY LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081030 GL 2008 10 30 SWAA085837 2 20081027 A 7532 121762 SHAFT BOEING 737 7373H4 1384600 NM CFMINT CFM56 CFM563B1US GL NR 1 ENGINE SHEARED A SWAA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 29 601WN 27695 AIR TURNBACK - NR 1 ENGINE UNABLE TO MAINTAIN CLIMB POWER. FOUND NR 1 ENG VBV FLEX SHAFT SHEARED. REMOVED AND REPLACED VBV MOTOR & SHAFT PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 20081030 2008 10 30 SWAA085849 4 20081028 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM CABIN LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 407WN 29817 R2 DOOR EMERGENCY EXIT SLIDE LOW PRESSURE INDICATOR. REMOVED AND REPLACED SLIDE ASSY PER MT. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085852 1 20081028 A 3350 8210248801 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 494WN 33868 DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085853 1 20081028 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 504SW 24181 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 435, STR 1. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085854 1 20081028 A 3260 6558206 SENSOR BOEING 737 7373H4 1384600 NM RT MLG LOOSE A SWAA K NONE N FALSE WARNING CL CLIMB 1 SW 29 636WN 27709 AFTER GEAR HANDLE AT UP POSITON, RT MLG UNSAFE LIGHT INDICATED. RECYCLED GEAR LEVER. INDICATION NORMAL. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085855 1 20081028 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, BETWEEN STR 18R TO STR 17R. REPAIRED SKIN PER SWA EA . 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 ASAA0843668 1 20081019 A 5210 652999413 GUIDE ARM BOEING 737 737490 1384715 NM L1 DOOR WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 793AS 28888 L1 DOOR GUIDE ARM BINDING AND POPPING UPPER HINGE LOWER CAM PLATE WORN. INITIATED MIG2C 227000. REPLACED UPPER HINGE L OWER GUIDE PLATE GUIDE ARM ASSY, OPS CHECK GOOD REF MM 52 11 41 AND MM 52 11 00. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 DHLA200800119 1 20081030 A 2120 UNKNOWN BOEING 727 727247 138408F NM COCKPIT ODOR A DHLA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 05 793DH 21393 DURING CLIMB-OUT A STRONG KEROSENE ODOR WAS IN THE COCKPIT FOR TWO TO THREE MINUTES AND THEN WENT AWAY. RESOLUTION, GRO UND RUN OF APU IAW 49-00-00 AND GROUND RUN OF LEFT AND RIGHT PACKS IAW MM 21-55-00 COULD NOT ODOR KEROSENE OR ANY OTHER ABNORMAL ODORS, NO NOTED DEFECTS. 2 L 7 3 4F A3WE 20081031 NM 2008 10 31 DL757081411 1 20081014 A 5320 214N500222 FLOOR SUPPORT BOEING 757 757232 1384965 NM BS 848-860 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 CORROSION AT FASTENERS HOLE ON PANEL SUPPORT BS 848-860, WL 154, ABOVE STRINGER 28L. REMOVED AND REPLACED PANEL SUPPORT . 2 L 7 2 4F RT A2NM 20081031 NM 2008 10 31 PCSA2008093001 1 20080930 A 2782 269002911 ACTUATOR BOEING 727 727233 138408A NM NR 7 LE SLAT LEAKING A PCSA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 29 395AJ 21100 LOST A HYDR SYS AFTER FLAP RETRACTION DEPARTING. ON APPROACH TO POS NR 7 L/E SLAT FAILED TO EXTEND. LANDING GEARS WERE EXTENDED MANUALLY, THE AC LANDED SAFELY AND WAS TOWED FROM THE RUNWAY. MAINT DISCOVERED THE NR 7 L/E ACTUATOR BODY HAD FAILED CAUSING A LOSS OF A SYS HYDR FLUID, A SYS FAILURE AND CONSEQUENT LOSS OF NOSE WHEEL STEERING. (K) 2 L 7 3 4F RT A3WE 20081031 NE 2008 10 31 DXTA2008102703321 2 20081026 A 7200 ENGINE BEECH MU300 400A 1155402 CE PWA JT15 JT15D5 52112 NE LT & RT POWER LOSS E DXTA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 07 161QS RK435 LT & RT ENGINE FAILED TO DEVELOP TAKEOFF THRUST. 2 H 7 2 4F 4 F RT A16SW E25EA 20081031 NE 2008 10 31 2008UALA06270 2 20081026 A 7200 BLADE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ENGINE DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 648UA 25285 NUMEROUS FAN BLADES HAVE SMALL NICKS & DENTS ON BOTH NR 1 & NR 2 ENGINES. 2 L 7 2 4F 4 F RT A1NM E24NE 20081031 EA 2008 10 31 ASOA200801394 1 20081003 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 846AS 7328 DURING EDDY CURRENT INSPECTION ON THE 621 BULKHEAD FWD FACE, AN INDICATION WAS NOTED AT LBL 48.00, WL 106, .500 IN LENGT H. 2 L 7 2 4F RT A21EA 20081031 NM 2008 10 31 HALA2008102300831 1 20081023 A 5314 KEELBEAM BOEING 767 76733A 1385209 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 CORROSION ON KEEL BEAM AT PANEL FIXING ANCHOR NUT AT BS 933. CORROSION BLENDED IAW SRM 53-50-12 FIG 101 SHEET 10. WORK ED AREA, ROTO PEENED IAW SRM 51-20-06 & PAINTED IAW SRM 51-20-01. 2 L 7 2 4F RT A1NM 20081031 NM 2008 10 31 HALA2008102300832 1 20081023 A 5314 KEELBEAM BOEING 767 76733A 1385209 NM FUSELAGE CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 580HA 28140 CORROSION ON KEEL BEAM AT PANEL FIXING ANCHOR NUT AT BS 933. CORROSION BLENDED IAW SRM 53-50-12 FIG 101, SHEET 10. WOR KED AREA, ROTO PEENED IAW SRM 51-20-06 & PAINTED IAW SRM 51-20-01. 2 L 7 2 4F RT A1NM 20081031 NM 2008 10 31 2008UALA06298 1 20081027 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN EXPOSED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 WIRES EXPOSED ON EMERGENCY FLOOR LIGHTS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081031 NM 2008 10 31 2008UALA06285 1 20081027 A 3350 FU305 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BATTERY CHARGER INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 RIGHT OVERWING 2 AFT EMERGENCY LIGHTS INOP. REPLACED FUSE IN BATTERY CHARGER. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081031 2008 10 31 2008UALA06282 4 20081027 A 2565 655298878 O-RING BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EVAC SLIDE DEFECTIVE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 195UA GI1085 26899 LOW BOTTLE. LEAKING AROUND GAUGE ELBOW O-RING. REMOVED & REPLACED O-RING. 2 L 7 4 4F 4 F RT A20WE E24NE 20081031 NM 2008 10 31 2008UALA06284 1 20081027 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 820UA 898 FLOORBEAM 95 NEEDS TO BE REPLACED. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM 95. 2 L 7 2 4F 4 F RT A28NM E40NE 20081031 NM 2008 10 31 AALA200802328 1 20080723 A 5313 141T3001 STRINGER BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 339AA 22336 AFW FORWARD CARGO STRINGER WAS CORRODED. AREA OF DISCREPANCY WAS 21 INCHES IN LENGTH. REPAIRED PER SRM 53-00-03 2R2 WI TH EXCEPTIONS PER MRB 767 3256. 2 L 7 2 4F RT A1NM 20081103 SO 2008 11 3 C2XA08CL116 1 20081019 A 3230 355022002 ELECTRONIC UNIT EMB 145 EMB145XR 3260214 SO MLG FAULTED A C2XA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 27 11181 9986 14500904 DAY FLIGHT NR 4922. THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MSG ON THE ECIAS DURING PREFLIGHT. MX INSPECTED AN D REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPS CHECKS WERE GOOD. 2 L 7 2 4F RT 20081103 WP 2008 11 3 AALA200802524 1 20080918 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP BS 1250-1287 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70504 49798 RT CUSP SHEET IS CORRODED. AREA OF DISCREPANCY IS 12 INCHES BY 37 INCHES. INSTALLED NEW CUSP SHEET PER AARD 53-20-00-16 . 2 L 7 2 4F A6WE 20081103 WP 2008 11 3 AALA200802530 1 20080919 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP BS 226 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70504 49798 LT CUSP IS CRACKED AT STATION 226. CRACK LENGTH IS 3 INCHES. REPLACED LT CUSP PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081103 NM 2008 11 3 USAA920081896 1 20081015 A 3397 WIRE AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 821AW 1406 LOGPAGE NR 4427709 FLT NR 542 PHX DFW EMERGENCY LIGHT PASSENGER SEAT 3L EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED BROK EN WIRE TO PASSENGER SEAT 3L PER SWPM 20-10. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081103 EU 2008 11 3 USAA920081899 1 20080927 A 5320 D5747228400200 FLOOR SUPPORT AIRBUS 320 A320231 3930325 EU ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C9 MAJOR REPAIR NR 6062491 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR64 AND FR66, Y465. REPLACED FLOOR SUPPORT BETWEEN FR64 AND FR66, Y465 IAW A320 SRM 53-41-14 AND SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081103 NM 2008 11 3 USAA920081900 1 20081014 A 5311 6546540 FRAME BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03C20053004/004 FRAME CRACKED AT BS 639, S17L, WL 200. REPAIRED FRAME AT BS 639, S17L, WL 200 IA W TYPICAL REPAIR NR 53-62-01 AND EA NR 100695. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081919 1 20081012 A 5310 CREASE BEAM BOEING 767 767201 1385125 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245AY 23897 BFM MAJOR REPAIR C3 CHECK NR 6013042, CORROSION ON CREASEBEAM, BS 1502, BS 1518, RBL 84. REPAIRED CREASEBEAM, BS 1502, BS 1518, RBL 84 IAW EA 134030. 2 L 7 2 4F RT A1NM 20081103 WP 2008 11 3 AALA200802538 1 20080922 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 274AA 49271 EMERGENCY LIGHT BATTERY PACK AT STATION 225 WEAK. REPLACED BATTERY PACK AT STATION 225. SYSTEM GROUND CHECKED NORMAL O PS. 2 L 7 2 4F A6WE 20081103 WP 2008 11 3 AALA200802542 1 20080916 A 5320 PAN DOUG DC9 DC982 3022082 WP BS 370-427 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70524 49916 CORROSION FOUND ON FORWARD CARGO DOOR THRESHOLD PAN. AREA OF DISCREPANCY IS 1 INCH BY 57 INCHES WITH A DEPTH OF .030 IN CH. REPLACED LOWER SECTION OF PAN IN ACCORDANCE WITH SRM 53-05-00. 2 L 7 2 4F A6WE 20081103 NM 2008 11 3 USAA920081956 1 20081017 A 5311 FRAME BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT MAJOR REPAIR Q3 CHECK NR 03C10753039/013, CRACKED FRAME AT BS 867, S9R. REPAIRED FRAME AT BS 867, S9R IAW TYPICAL R EPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081962 1 20081025 A 5740 654544555 ATTACH ANGLE BOEING 737 7374B7 138449C NM ZONE 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03052980086/002 CRACK ON LT WING LOWER SKIN ATTACH ANGLE AT WBL 135.5, 6 INCHES FORWARD OF REAP S PAR. REPAIRED LT WING LOWER SKIN ATTACH ANGLE AT WBL 135.5, 6 INCHES FORWARD OF REAR SPAR IAW US AIRWAYS EA NR 100682. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081964 1 20081024 A 5330 6545774 SKIN BOEING 737 7373S3 138449H NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW 23713 PHX RON MAJOR REPAIR NR 4427814 CRACK IN LT FUSELAGE AFT OF EMERGENCY EXIT LIGHT AFT OF WING TO BODY FAIRING. REPAIRED LT FUSELAGE AFT OF EMERGENCY EXIT LIGHT IAW SRM 53-00-01-2R. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 AALA200802331 1 20080815 A 5313 141T3001 STRINGER BOEING 767 767223 1385123 NM BS 434-456 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 332AA 22331 AFW STRINGER WAS CORRODED AT STATION 451 DUE TO PREVIOUS REPAIR AT STATION 434. STATION 434 WILL NEED TO BE REPLACED TO ALLOW A REPAIR AT STATION 451. REPAIRED PER SRM 53-00-03-2R2 WITH EXCEPTIONS PER MRB 767 3278. 2 L 7 2 4F RT A1NM 20081103 NM 2008 11 3 AALA200802332 1 20080815 A 5313 141T3001 STRINGER BOEING 767 767223 1385123 NM BS 424-446 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 332AA 22331 AFW STRINGER WAS CORRODED FROM STATION 424 TO 446. REPAIRED PER SRM 53-00-03-2R2 WITH EXCEPTIONS PER MRB 767 3281. 2 L 7 2 4F RT A1NM 20081103 NM 2008 11 3 AALA200802333 1 20080819 A 5330 143T3510 SKIN BOEING 767 767223 1385123 NM BS 532 S32R DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 332AA 22331 AFW FUSELAGE SKIN APPROXIMATELY 10 INCHES FORWARD OF FORWARD CARGO DOOR AT STRINGER 32 RT HAD A GOUGE BLENDED BEYOND SRM LIMITS. AREA OF DISCREPANCY IS 2 INCHES BY 1 INCH WITH A DEPTH OF .050 INCH. MATERIAL REMAINING IS .156 INCH. HIGH F REQUENCY EDDY CURRENT INSPECTION FOR CRACKS WITH NO FINDINGS. REPAIRED PER SRM 53-00-01-1A WITH EXCEPTIONS PER MRB 767 3276. 2 L 7 2 4F RT A1NM 20081103 NM 2008 11 3 USAA920081972 1 20081025 A 5311 65C22908 FRAME BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03C20853011/008 CRACK IN FRAME STIFFENER AT LIGHTNING HOLE AT BS500B BETWEEN S20L AND S21L. REPA IRED FRAME STIFFENER AT LIGHTNING HOLE AT BS500B BETWEEN S20L AND S21L. IAW SRM 53-00-07, EA NR 100705. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 AALA200802387 1 20080920 A 3350 LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 355AA 24036 DFW EXTERIOR EMERGENCY LIGHT AT AFT LT INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT AFT LT. SYSTEM GROUN D CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081103 NM 2008 11 3 AALA200802394 1 20080920 A 3350 BATTERY PACK BOEING 737 737823 13844CB NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 944AN 29535 DFW EMERGENCY LIGHTS AFT OF SEAT ROW 21 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AFT OF SEAT ROW 21. SYS TEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081103 WP 2008 11 3 NWAA084679760 1 20081018 A 2780 SUPPORT DOUG DC9 DC941 302207N WP OUT OF ADJUST A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 760NW 47288 AFTER TAKEOFF THE SLATS WERE SELECTED TO RETRACT BUT THE AMBER SLAT DISAGREEMENT LIGHT ILLUMINATED AND THE ACFT EXPERIEN CED A VERY SLIGHT ABNORMAL ROLLING TENDENCY TO THE LT. THE COM PROCEDURES WERE COMPLIED WITH AND THE FLIGHT RETURNED TO A SAFE LANDING BACK AT EWR. MX FOUND THE RT T-DUCT SUPPORT PADS WERE OUT OF ADJUSTMENT. THE T-DUCT AND SUPPORT PADS W ERE ALL REALIGNED PER AMM AND FUNCTIONALLY CHECKED. THE ACFT HAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 20081103 NM 2008 11 3 NWAA084695644 1 20081021 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM EMERGENCY LIGHTS MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 544US 26491 DURING AN OVERNIGHT LINE CHECK, 3 EMERGENCY ESCAPE PATH LIGHTS AND AN OVER WING SLIDE ILLUMINATION LIGHT WERE FOUND TO B E INOPERATIVE. MX FOUND THE EMERGENCY LIGHT POWER SUPPLY AT STATION 1090 ON THE ACFT LT TO BE DEFECTIVE AND REPLACED IT . OPS CHECK GOOD AFTER REPLACEMENT. 2 L 7 2 4F RT A2NM 20081103 NM 2008 11 3 USAA920081837 1 20081008 A 5312 BULKHEAD BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 450UW 24933 PIT - MAJOR REPAIR, 3 CRACKS ON RT VERTICAL WE OF BS 178 BULKHEAD, WL 234 TO 220, RBL 17. REPAIRED RT VERTICAL WEB OF B S 178 BULKHEAD, WL 234 TO 220, RBL 17 IAW B737 SRM 53-10-08 REPAIR 12. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081843 1 20080822 A 5315 6546811 FLOORBEAM BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 SAL - C19 - MAJOR REPAIR, CORROSION ON FLOORBEAM UPPER CHORD AT BS 986.5, BETWEEN LBL 44 TO RBL 42. REPAIRED FLOORBEAM UPPER CHORD AT BS 986.5, BETWEEN LBL 44 TO RBL 42 IAW B737 SRM 53-00-51. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081849 1 20081004 A 5320 65C27021 ATTACH BRACKET BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, PSU FRAME RAIL ATTACH BRACKET CRACKED AT BS 827, BETWEEN S8L & S9L. REPAIRED FRAME AT BS 827, BETWEEN S8L & S9L IAW US AIRWAYS TYPICAL REPAIR NR 53-10-20E. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081850 1 20081008 A 5320 BRACKET BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, BRACKET CRACKED AT INBD CORNER ON FRAME AT BS 706, S11R. REPLACED BRACKET AT INBD CORNER ON FR AME AT BS 706, S11R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 WRLA2008085 1 20081006 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHECK, MX FOUND M/D SEAT TRACK CORROSION AT Y465, X-27.5. REMOVED CORROSION PER MD-11F SRM 51-33-01 VOL 2 REV 40, REPAIRED SEAT TRACK PER MD-11F SRM 53-70-00 VOL 1 REV 40, REPLACED FASTENERS PER MD-11F SRM 51-33-01 VOL 2 REV 40. 2 L 7 3 4F RT A22WE 20081103 NM 2008 11 3 WRL2008F00009 1 20081006 A 5311 FRAME DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHECK, MX FOUND FUSELAGE FRAME AND LONGERON TO HAVE HEAT DAMAGE AT STA Y 6-90 TO Y 1139, L27L. OPEN 2 L 7 3 4F RT A22WE 20081103 NM 2008 11 3 WRLA2008083 1 20081006 A 5410 FRAME DOUG MD11 MD11F 3023600 NM NR 3 NAC DOOR CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHECK, MX FOUND NR 3 ENGINE LT CORE COWL AFT FRAME CRACK AT 7 O’CLOCK POSITION. REPAIRED CRACK IAW ENGINE ERING INSTRUCTION W2008A54B-1082 REV 00. 2 L 7 3 4F RT A22WE 20081103 NM 2008 11 3 WRLA2008080 1 20081006 A 5350 SKIN DOUG MD11 MD11F 3023600 NM TAILCONE MISREPAIRED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHECK, MX FOUND TAILCONE SKIN RT FWD EDGE IMPROPER TRIM OUT AT STA Y2245. REPAIRED DAMAGED AREA IAW ENGIN EERING INSTRUCTION W2008A53-119 REV 00 AND EI W2008A53B-119 REV 01. 2 L 7 3 4F RT A22WE 20081103 NM 2008 11 3 HNAA0800304 1 20080812 A 5320 85320686101 THRESHOLD DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 931HA 51228 132 PAX DOOR THRESHOLD CORRODED. REPLACED PAX DOOR THRESHOLD IAW SRM 51-40-00. 2 H 7 2 4T RT A13NM 20081103 NM 2008 11 3 HNAA0800307 1 20080903 A 5320 FITTING DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 931HA 51228 132 FWD EMERGENCY DOOR AREA, BELTFRAME AT STA X254 FOUND CORRODED AND SURFACE CORROSION ON DOOR SILL. AT STA X259 BLENDED B ELTFRAME IAW SRM 53-00-16. CLEAT, THRESHOLD, STRAP AND BRACKET LOCALLY FABRICATED IAW DRAWINGS 8532075, 85320594, 85321 705, 853206070. 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 DL76G081407 1 20081023 A 2150 3964621 VALVE BOEING 767 767332 1382001 NM RT A/C PACK INTERMITTENT A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 173DZ 29692 DURING TAXI OUT OF BCN RT PACK VALVE WOULD NOT OPEN AFTER TURNED OFF FOR ENG START. RTB, SWAPPED PACK CONTROL CARDS NO HELP. RESEATED FCV CONNECTOR. NOW OPN NORMAL. 2 L 7 2 4F RT A1NM 20081030 NM 2008 10 30 USAA920081740 1 20080902 A 5311 65C22909 FRAME BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT - Q1 - MAJOR REPAIR, FRAME CRACKED AT BS 500E BETWEEN S20L AND S21L. REPAIRED FRAME AT BS 500E BETWEEN S20L AND S21 L IAW US AIRWAYS EA 100631. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 SWAA085868 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727, STR 2R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 SWAA085869 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081031 EA 2008 10 31 SWIA200820229 1 20080616 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 492SW 7168 FS 280 FLOORBEAM LOWER FLANGE IS CRACKED AT RBL12. C-CHECK, REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081031 NM 2008 10 31 DL757081448 1 20081024 A 5330 SKIN BOEING 757 757232 1384965 NM BS 536-630 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 DURING AN AGING AIRCRAFT INSPECTION, CORROSION WAS FOUND ON THE EXTERNAL SKIN UNDERNEATH THE ANTENNA MOUNTS AT STA 536 A ND 630 BETWEEN S-28L AND S-28R. REPAIR WAS MADE PER BOEING INSTRUCTIONS. 2 L 7 2 4F RT A2NM 20081031 NM 2008 10 31 CALA0801015 1 20081028 A 3350 D71701100 BATTERY PACK BOEING 737 737924 13848A1 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 32404 30121 RIGHT AFT GALLEY EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED ASSOCIATED BATTERY PACK. ALL EMERGENCY EX ITS LIGHTS OPERATE NORMAL. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 CALA0801012 1 20081028 A 5315 141T5107 FLOORBEAM BOEING 767 767424ER 1385270 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76054 29449 CABIN BODY STATION 303 LBL 18 - LBL 48 FLOOR SUPPORT FOUND CORRODED. CABIN BODY STATION 303 LBL 37 - LBL 48 FLOORBEAM C ORROSION REMOVED PER SRM 51-10-02 AND PROTECTED PER SRM 51-20-01. BLEND AREA LENGTH 1" X WIDTH 0.7" X DEPTH 0.003" IS W ITHIN SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. LBL 44 - LBL 37 FLOORBEAM REPAIRED PER SRM 53-00-51 REPAIR 1 FIG 201. CABIN BODY STATION 303 LBL 37- LBL 48 FLOORBEAM CORROSION REMOVED PER SRM 51-10-02 AND PROTECTED PER SRM 51-20-01 BLEND AREA LENGTH 1" X WIDTH 0.7" X DEPTH 0.003" IS WITHIN SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND LBL 4 - LBL 37 FLOORBEAM REPAIR EDAS PER SRM 53-00-51 REPAIR 1 FIG 201. 2 L 7 2 4F RT A1NM 20081031 EA 2008 10 31 A6WA200840014 1 20080118 A 2750 860D10018 CONTROL UNIT CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 31 438AW 11096 7748 FLAPS FAILED AT 0 DEGREES ON APPROACH. REMOVED AND REPLACED FECU REF AMM 27-51-05. OP CHECKS GOOD REF BLOCK 3 DURING TR OUBLESHOOTING FOUND FAULT CODES TO SHOW LOGIC PROBLEM IN THE FECU. (K) 2 L 7 2 4F RT A21EA 20081031 SO 2008 10 31 C2XA08SH132 1 20081026 A 5310 14523779001 DOOR FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16981 145208 SHV DURING C CHECK THE BAGGAGE DOOR UPPER FRAME WAS FOUND TO BE CORRODED. MX PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5230-01198. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081028 NM 2008 10 28 SWAA085771 1 20081023 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 300SW 22940 DURING SCHEDULED MV4 CHECK, FOUND KEEL BEAM CRACKED FWD BS 727. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085707 1 20081019 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 495WN 33869 FOUND FWD EEPLS LIGHT LOOSE. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085776 1 20081026 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 455WN 32462 FOUND EGRESS LENS MISSING AT OVERWING EMERGENCY EXIT. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081028 2008 10 28 SWAA085777 4 20081024 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 458WN 33857 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085778 1 20081024 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 458WN 33857 DURING SCHEDULED HC1 CHECK, FOUND EEPLS LIGHT STRIP CRACKED AT OVERWING EXIT. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085779 1 20081025 A 3350 101114 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 503SW 24180 DURING SCHEDULED MV1 CHECK, FOUND RT AFT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085782 1 20081024 A 5330 6545775 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 528SW 26570 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 870, STR 23R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085783 1 20081024 A 3350 6573709 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 654SW 28399 DURING SCHEDULED MV1 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 6. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085784 1 20081024 A 5330 6545774 SKIN BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085785 1 20081024 A 5330 6545774 SKIN BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 793, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085789 1 20081024 A 5312 6545409 PRESSURE PANEL BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM PRESSURE DECK WEB CRACKED AT BS 664, LBL 24. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081029 WP 2008 10 29 AALA200802506 1 20080929 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP BS 1212-1231 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 CORROSION LT TIE DOWN TRACK IN AFT CARGO IN NUMEROUS PLACES. INSTALLED NEW SPLICE ON LT TIE DOWN TRACK BETWEEN STATION 1212 AND 1231 PER SRM 51-10-03. 2 L 7 2 4F A6WE 20081029 NM 2008 10 29 SWAA085693 1 20081018 A 3350 101331 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 602SW 27953 DURING SCHEDULED MV1 CHECK, FWD EMERGENCY EXIT LIGHT LENS COVER FELL OFF. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085725 1 20081021 A 5210 141A61604 SKIN BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR SKIN CRACKED AT LOWER AFT END. REMOVED AND REPLACED L1 DOOR PER MM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 2008UALA06171 1 20081017 A 3350 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 548UA 25396 INSTALL JIFFY SPLICES ON EMERGENCY EXIT SWITCH, FWD F/A CALL INDICATORS AND DOOR SLIDE LIGHTS. INSTALLED JIFFY SPLICES ALL LOCATIONS PER BOEING SWPM 20-90-14. FOUND SWITCH S10219 BAD, REPLACED PER AND TEST GOOD PER MM 25-66-11. FOUND MID CABIN EMERGENCY TEST SWITCH BAD, REPLACED AND OPS CHECKS GOOD PER B757 WDM 33-51-13. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 USAA920081882 1 20080919 A 5311 6546552 FRAME BOEING 737 7373G7 138447J NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN C18 MAJOR REPAIR NR 6131828 FRAME CRACKED AT BS827, BETWEEN S8R AND S9R. REPAIRED FRAME AT BS827, BETWEEN S8R AND S 9R. IAW TASK CARD NR M1C53002. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 USAA920081872 1 20081008 A 5320 WEB BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03055380105/001 FUSELAGE WEB CRACKED AT BS 180, WL 228, LBL17. REPAIRED FUSELAGE WEB AT BS 180, WL 228, LBL17 IAW SRM 53-10-08, REPAIR 12, DETAIL V. 2 L 7 2 4F RT A16WE 20081029 EA 2008 10 29 QXEA200800902 1 20080728 A 5320 STIFFENER CNDAIR CL600 CL6002C10 1390015 EA BS 280 BULKHEAD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK X280 BEAM BULKHEAD STIFFENER AT Y26R JUST BELOW CABIN FLOOR LEVEL AND ON FWD SIDE OF BULKHEAD IS CRACKED. REMOVED STIFFENER, FABRICATED NEW STIFFENER REF CRJ 700 SRM 53-11-10-003-A01 PAGE 16 ITEM 81 FOR MATERIAL SPEC. TREATED AND APPLIED PRIMER AND PAINT. INSTALLED NEW ANGLE IAW CRJ SRM 51-42-06. 2 L 7 2 4F RT A21EA 20081029 WP 2008 10 29 AALA200802505 1 20080929 A 5347 1D00268 CARGO TRACK DOUG DC9 DC982 3022082 WP BS 1003-1155 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 CORROSION ON RT TIE DOWN TRACK IN AFT CARGO IN NUMEROUS PLACES. INSTALLED RT TIE DOWN TRACK FROM STATION 1003 TO 1155 P ER SRM 51-01-00. 2 L 7 2 4F A6WE 20081029 NM 2008 10 29 2008UALA06182 1 20081019 A 3350 78941 STRIP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26877 THE 4F AFT PEEL STRIP BROKEN OFF. 2 L 7 4 4F 4 F RT A20WE E24NE 20081029 NM 2008 10 29 USAA920081880 1 20080919 A 5311 65C25229 FRAME BOEING 737 7373G7 138447J NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN C18 MAJOR REPAIR NR 6131828 FRAME HAS A .300 INCH CRACK AT BS 727D, BETWEEN S8L AND S9L AND A .5 INCH CRACK BETWEEN S8R AND S9R. REPAIRED FRAME AT BS 727D BETWEEN S8L AND S9L, ALSO BETWEEN S8R AND S9R IAW TASK CARD NR M1C53002. 2 L 7 2 4F RT A16WE 20081029 EA 2008 10 29 QXEA200800895 1 20080728 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK LT OTBD SEAT TRACK HAS CORROSION AT STA X-853. BLENDED CORROSION IAW REO 670-53-00-013 SHT 2 STEPS 1-2. M AX MATERIAL REMOVED WAS .012", BLEND IS WITHIN LIMITS IAW REO 670-53-00-013 TABLE 1. ALODINED IAW SRM 51-21-11. 2 L 7 2 4F RT A21EA 20081029 NE 2008 10 29 2008UALA06192 2 20081020 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE STALLED A UALA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 651UA 25389 724651 TWO ENGINES STALLED AT FL380. 2 L 7 2 4F 4 F RT A1NM E24NE 20081029 NM 2008 10 29 08FDEA04514 1 20081024 A 2780 106081917 SWITCH BOEING 727 727225 1384077 NM LE FLAPS FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 464FE 21288 ON DEPARTURE WHEN FLAPS RAISED FROM 5 TO O GOT AN LED DISAGREE LIGHT WITH NR 2 LE FLAP LED INDICATING NOT IN PROPER POS ITION. REMOVED NR 2 LE FLAP SWITCH AND PIGGY BACKED ONTO NR 1 LE FLAP POSITION AND PROBLEM FOLLOWED. REINSTALLED CONNE CTOR ON ORIGINAL NR 1 SWITCH. REPLACED NR 2 LE FLAP SWITH AND CYCLED FLAPS SEVERAL TIMES PER MM 27-82-001-4, OPS CHECK GOOD. 2 L 7 3 4F A3WE 20081029 WP 2008 10 29 08FDEA04505 1 20081023 A 5313 AYB70202 FITTING DOUG MD10 MD1010F 3022112 WP BS 1501-1521 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 THE CENTER LANDING GEAR SPAC, LONGERON FITTING, RIGHT SIDE FROM STA 1501 TO 1521 IS CORRODED. REMOVED FITTINGS IAW SRM 51-33-01. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01. REMOVED CORROSION & FOUND OUT OF LIMITS IAW S RM 53-00-01. MACHINED FITTING IAW DWG AYB7020. REMOVED CORRODED SECTION, FABBED NEW LONGERON SECTION & REPAIR SPLICES IA W DWG AYB 7013 & SRM 53-00-01. INSTALLED LONGERON SECTION, REPAIR SPLICES & END FITTINGS IAW SRM 53-00-01 & 51-31-01. 2 L 7 3 4F RT A22WE 20081029 EU 2008 10 29 08FDEA04540 1 20081025 A 5753 A57960007200 SKIN AIRBUS 300 A300F4605R 3930327 EU RT WING TE FLAP CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 677FE 791 RT WING INBD FLAP UPPER SURFACE 12 INCHES AFT OF FWD SPAR AND 1 INCH OTBD OF RIB 12 HAS 2 CHAFED AREA, 2 SQ INCHES CUT O UT DAMAGED AREA AND INSTALLED FLAPS, SKIN PATCH REPAIR DOUBLER ON RT WING INBD FLAP UPPER SKIN AT RIB 12 IAW A300-600 SR M 57-50-00, FIG 205, PAGE 219. 2 L 7 2 4F RT A35EU 20081029 EU 2008 10 29 08FDEA04541 1 20081025 A 7830 491B131300239 FRAME AIRBUS 300 A300F4605R 3930327 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 668FE 772 NR 1 ENG OTBD T/R FWD FLANGE FOR MOUNTING RING LATCH ASSY HAS 2.25 IN CRACK AT 12 O'CLOCK POS REMOVED CRACK AND REPAIRED NR 1 OTBD T/R FWD FLANGE IAW FEDEX EA 6-7830-124134, RELEASE DATE 8 OCTOBER, 2008. 2 L 7 2 4F RT A35EU 20081029 NM 2008 10 29 08FDEA04546 1 20081025 A 5311 651634786 FRAME BOEING 727 7272D4 138407U NM ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 AFT PIT BS 1130 FRAME UPPER CHORD HAS TRIPLE DRILLED HOLE INBD OF TIE DOWN FITTING AT S27R. CUTOUT DAMAGE, REMOVED FAST ENERS FROM FRAME AT REPAIR AREA. FABRICATED REPAIR ANGLE & HEAT TREATED TO T6 CONDITION. TREATED, PRIMED, & INSTALLED FRAME REPAIR ANGLE. REF: SRM 51-40-3, FIG. 1 / SRM 51-30-2, PG. 8 / SRM 51-10-2, PG. 1-2 / SHOP REPAIR NON ROUTINE CARD NO. N00953. THIS IS CLASSIFIED AS A MAJR REPAIR 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 08FDEA04548 1 20081025 A 5320 652082621 BEAM BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FUSELAGE UPPER LOBE INTERIOR STRUCTURE CORROSION ON FWD SHEAR DECK STA 382 RBL 46-55. REPAIRED FLOORBEAM REF EA 7-5310- 123808 AND DWG SR27-53-034 REV F REPAIR 5. THIS IS CLASSIFIED AS A MAJOR REPAIR. (ORIGINAL MATERIAL THICKNESS .125, MAT ERIAL LOSS .027, REMAINING .098 OUT OF LIMITS) 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 08FDEA04553 1 20081026 A 5720 651735639 BULKHEAD BOEING 727 7272D4 138407U NM ZONE 500 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 LEFT WING INBD L/E CAVITY, SUPPORT BRACKET CRACKED AT FWD FIXED L/E 3 INCH OTBD NR 1 FLAP INBD HINGE. REMOVED SUPPORT BRACKET ASSY REF: SRM 51-30-02. CRACKS FOUND .25 INCH AND 1 INCH LONG ON PARTS 65-17356-39 AND -87, OUT OF LIMITS. FAB RICATED -39 AND -87 REF, DWG 65-17356, SRM 51-30-05 ID MATERIAL -39 BULKHEAD 2024T3 .032 ATAG 69787, -87 2024 .063 ATAG A33090 REF: DWG 65-17356, TREATED SOPM 20-43-03P3, PRIMED 20-44-04P3, INSTALLED ASSY REF SRM 51-30-02P1. THIS REPAIR IS CLASSIFIED AS MINOR. 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 2008UALA06230 1 20081021 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ODOR A UALA A UNSCHED LANDING W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 556UA 26650 BURNING ODOR REPORTED. RFTL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 EA 2008 10 29 ASOA200801212 1 20080922 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 REMOVED AND REPLACED NR 1 BATTERY PACK CHARGER ASSY IAW CRJ 200 AMM 33-51-05. OP'S CHECK GOOD. DMIL CLEARED PLACARD RE MOVED. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081031 SO 2008 10 31 C2XA08SH133 1 20081026 A 5610 14523775001 DOOR FRAME EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16981 145208 SHV DURING C CHECK THE BAGGAGE DOOR LOWER FRAME WAS FOUND TO BE CORRODED. MX PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5230-01198. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081031 NM 2008 10 31 2008UALA06165 1 20081017 A 5210 285W0955102 BATTERY PACK BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE R2 DOOR FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 781UA 26945 DOOR 2R EPAS BATTERY TEST FAILED. BATTERY FAILED TEST. REPLACED BATTERY PACK. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081031 NM 2008 10 31 2008UALA06272 1 20081024 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 820UA 898 FLOORBEAM 80 HAS CORROSION. STARTED REMOVAL OF FLOORBEAM. CONNECTOR AND FORWARD END OF FLOORBEAM NEED TO BE REMOVED. REMOVED FLOORBEAM 80 AND BEGAN INSTALLING BRACKETS ON FLOORBEAM. INSTALLED ALL BRACKETS AND JOINED FLOORBEAMS 150 AND 8 0 TOGETHER. READY TO INSTALL ON ACFT. REPLACED FLOORBEAM 80. 2 L 7 2 4F 4 F RT A28NM E40NE 20081031 NM 2008 10 31 2008UALA06262 1 20081024 A 3397 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 8GH. SECURED CONNECTOR, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081103 SO 2008 11 3 C2XA08IA228 1 20081017 A 2120 AE3007A1E UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN SMOKE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 18120 15310 145681 MCI FLIGHT 2484. SHORTLY AFTER TAKEOFF THE CREW REPORTED OPAQUE SMOKE IN THE CABIN WITH ELECTRICAL SMOKE. THE ACFT RET URNED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MX R&R THE NR 2 ENGINE, OPS CHECKED WITH NO DEFECTS AND THE ACFT WAS APP ROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081103 NM 2008 11 3 USAA920081890 1 20081013 A 5754 SKIN BOEING 737 737301 1384611 NM LE SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 0224 23739 CLT Q3 MAJOR REPAIR NR 5030880 AND 03C40257009/011 NR 4 SLAT DELAMINATED AT INBD END OF TRAILING EDGE WEDGE. REPLACED N R 4 SLAT IAW TASK CARD NR 03C40227004. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081965 1 20080919 A 5320 654587545 THRESHOLD BOEING 737 7373G7 138447J NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN C18 MAJOR REPAIR NR 6131857 EXFOLIATION CORROSION ON R1 DOOR THRESHOLD AT BS294.5 TO BS344, S17R, WL208, RBL75. REP LACED R1 DOOR THRESHOLD IAW SRM 51-40-02-OG. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 AALA200802389 1 20080920 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 186AN 32380 DFW EMERGENCY LIGHT AT SEAT 18A INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 18A. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT A2NM 20081103 NM 2008 11 3 USAA920081848 1 20081008 A 5340 STRINGER CLIP BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, STRINGER TIE CLIP CRACKED AT FRAME BS 706, S2L. REPLACED STRINGER TIE CLIP AT FRAME BS 706, S2 L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 HNAA0800306 1 20080903 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 931HA 132 CORROSION FOUND ON BOTTOM SKIN OF COCKPIT STA X123, LT STRINGER 31. REPAIRED CORROSION ON BOTTOM SKIN IAW SRM 53-20-21. 2 H 7 2 4T RT A13NM 20081103 WP 2008 11 3 P4Y2008F00003 2 20080813 A 7250 31021706 TURBINE WHEEL CASA C212 C212200 2410304 EU GARRTT TPE331 TPE331* 01514 WP NR 1 ENGINE DAMAGED E P4YA O OTHER Y ENGINE STOPPAGE AP APPROACH 1 EA 39 962BW 10781 1887 290 P36122C DURING FLT, ON APPROACH CREW REPORTED THE NR ONE ENGINE MADE A LOUD NOISE FOLLOWED BY SHUTDOWN AND FEATHERING OF THE PRO P. MX FOUND THE PROP TO PULL THROUGH WITH LITTLE EFFORT AND THE ENTIRE ROTATING GROUP TURNS. FURTHER INSPECTION REVEAL ED PIECES MISSING FROM THE THIRD TURBINE WHEEL. MX REPLACED THE ENGINE AND RETURNED THE AIRCRAFT TO SERVICE. NO EXTERN AL DAMAGE TO THE ENGINE OR AIRCRAFT STRUCTURE OCCURRED. TEARDOWN OF THE ENGINE INDICATED THE FIRST STAGE WHEEL HAD A BL ADE FRACTURE CAUSING SIGNIFICANT DAMAGE IN THE HOT SECTION AND HAS ALSO CAUSED THE MAIN SHAFT TO WHIP, CAUSING DAMAGE TO THE COMPRESSOR SECTION ALSO. THE FAILED BLADE AND REQUESTED PARTS HAVE BEEN SENT TO HONEYWELL FOR INVESTIGATION. 2 H 7 2 4T 3 T RT A43EU E2WE 20081103 NM 2008 11 3 HNAA0800305 1 20080812 A 5320 STRUCTURE DHAV DHC8 DHC8102 2809003 NM FUSELAGE DENTED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 931HA 51228 132 PROTRUDING DENT FOUND AT STATION X183.35 BETWEEN 24P AND 26P. REPAIRED DENT IAW RD 8-53-2181, HIGH FREQ EDDY CURRENT PE RFORMED, NO DEFECT NOTED. 2 H 7 2 4T RT A13NM 20081104 CE 2008 11 4 MTNA1008003 1 20081024 A 3243 26820011 MASTER CYLINDER CESSNA 208 208B 2073701 CE BRAKE SYSTEM DEFECTIVE E MTNA E ENGINE SHUTDOWN O OTHER UK UNKNOWN 1 EA 68 853FE 1746 0170 DURING TAXI-OUT THE PILOT NOTED THAT THE LEFT BRAKE LOST PRESSURE AS THE PLANE TURNED ONTO THE MAIN RUNWAY. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS TOWED BACK TO THE RAMP. MAINTENANCE DETERMIND THE AIRCRAFT NEEDED A BRAKE MASTER CYL INDER. 1 H 7 1 3T A37CE 20081104 WP 2008 11 4 UPS08853651 1 20081001 A 5310 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV EXT DOUBLER AFT LOWER DOOR CUTOUT BS 50.5 TO 55 L30L TO 1 INCH BELOW L 29L NEED VALIDATION FOR REPAIR . REPAIRED SRM 53-02-00 FIG 13. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853670 1 20081003 A 5753 FLAP DOUG DC8 DC873F 302199F WP RT WING MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV RT INBOARD FLAP LOWER I/B EDGE DOUBLER IN STA 0.00 NEEDS VALIDATION, FAILED APPENDIX H STEP 5. REMOV ED DOUBLER, FABBED AND INSTALLED NEW DOUBLER IAW DC8 SRM 57-2-05 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 20081104 EA 2008 11 4 COMA0860424 1 20081019 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA FS625 RT CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 809CA 21560 7366 CRACKED STRINGER CLIP AT FS 625 STR 14 RT SIDE AFT EQUIPMENT COMPARTMENT. REPLACED CLIP IAW REO601R-53-61-100 AND SR99- 5140-0001. 2 L 7 2 4F RT A21EA 20081104 WP 2008 11 4 AALA200802397 1 20080920 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9302B 49528 SFO EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS WILL NOT TURN OFF. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEAD FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081104 WP 2008 11 4 UPS08853671 1 20081003 A 5753 FLAP DOUG DC8 DC873F 302199F WP LT WING MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-28 LT BS XW5.0 I/B FLAP WEB REPAIR DOES NOT MEET CRITERIA FOR APPENDIX H. FLA P REPLACED ON NR 188423. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 AALA200802381 1 20080919 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 436AA 49454 DFW EMERGENCY LIGHTS AT AISLE OVERHEAD SEAT ROWS 22 TO 28 INOPERATIVE. REPLACED BATTERY PACK AT STATION 1100 FOR EMERGE NCY LIGHTS AT AISLE OVERHEAD SEAT ROWS 22 TO 28. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081104 WP 2008 11 4 AALA200802580 1 20080923 A 5320 PAN DOUG DC9 DC983 3022083 WP BS 370-427 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 DOOR PAN AT FORWARD CARGO HAS CORROSION OUT OF LIMITS AT STATION 370 TO 427. AREA OF DISCREPANCY IS 3 INCHES BY 4 INCHE S. INSTALLED DOUBLER IN ACCORDANCE WITH ESO 80559 DATED 18 SEP 2008. 2 L 7 2 4F RT A6WE 20081104 NM 2008 11 4 AALA200802377 1 20080919 A 2611 FIRE DETECTOR BOEING 757 757223 1384957 NM MLG WW FALSE ACTIVATION A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 687AA 25695 LAX INFLIGHT T253/19 SEP. CREW REPORTED WW FIRE WARNING INDICATION WITH HORN. ACCOMPLISHED CHECKLIST AND INDICATION WE NT OUT. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. INSPECTED ACFT WITH NO FAULTS OR DAMAGE NOTED. SYSTEM CHECKED NO RMAL OPS. 2 L 7 2 4F RT A2NM 20081104 EA 2008 11 4 COMA0860426 1 20081011 A 5210 601R31902 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 685BR 7712 PAX DOOR INNER SKIN IS DAMAGED AT DOOR DATUM 6, FS329.5. REPAIRED IAW EA 10-5210-02377. 2 L 7 2 4F RT A21EA 20081104 WP 2008 11 4 UPS08853673 1 20081007 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV RT WING L/E LOWER RIB CRACKED AT XFS 829. STOP DRILLED CRACK IAW SRM 57-2-0 DC8. FABBED AND INSTALL ED REPAIR IAW DC8 SRM 51-03-00-0, AND SRM 51-01-20D-0 DC8. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 AALA200802395 1 20080920 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9302B 49528 SFO EMERGENCY LIGHTS AT AFT OVERWING INOPERATIVE. REPLACED BATTERY PACK AT STATION 900 FOR EMERGENCY LIGHT AT AFT OVERW ING. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081104 EA 2008 11 4 COMA0860434 1 20081024 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 781CA 7312 FUEL DRAIN INSIDE FUEL ACCESS PANELS 510AB FWD AND AFT DRAIN ATTACH HOLES ARE DAMAGED. REAMED AND INSTALLED SERVICEABLE FREEZE PLUGS AT FUEL DRAIN FWD AND AFT ATTACH HOLES PER COMAIR EA 10-5721-02382. 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 COMA0860431 1 20081024 A 5320 601R3103023 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 589-605 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 588SW 7069 CORROSION FOUND ON TOP FLOOR STRUCTURE AT LBL27 BETWEEN FS 589 AND 605. R&R FLOOR STRUCTURE AT LBL27 BETWEEN FS 589 AND 605 IAW REO 601R-53-00-027 AND 601R-53-00-045. 2 L 7 2 4F RT A21EA 20081104 WP 2008 11 4 AALA200802576 1 20080923 A 5311 9919603 FRAME DOUG DC9 DC983 3022083 WP BS 1231 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 TUL CORROSION FOUND ON BELL FRAME AT STATION 1231. AREA OF DISCREPANCY IS 2 INCHES BY 1 INCH. INSTALLED DOUBLER IN ACC ORDANCE WITH SRM 51-70-05. 2 L 7 2 4F RT A6WE 20081104 NM 2008 11 4 AALA200802544 1 20080916 A 5310 143T82043 FAILSAFE BOEING 767 767323 1385205 NM BS 504-590 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AA 24036 CORROSION FOUND ON LOWER CARGO DOOR LOWER SILL FAIL SAFE STRAP IN 2 PLACES. REPLACED STRAPS AND REPAIRED FASTENER HOLES IN ACCORDANCE WITH MRB 767 3302. 2 L 7 2 4F RT A1NM 20081104 WP 2008 11 4 AALA200802586 1 20080929 A 5320 7075T6032 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7538A 49992 CRACK ON CUSP MEMBRANE BELOW G1 GALLEY DRAIN PAN AT STATION 160. CRACK LENGTH IS 2 INCHES. INSTALLED DOUBLER IN ACCORD ANCE WITH AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081104 WP 2008 11 4 UPS08853679 1 20081015 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV (REPAIR STA -45 LBL 33 DOUBLE FILLER) REPAIR PER DAC DWG SR0830026 REF UPS NRC 188379. REPLACED FING ER AND SPLICE DOUBLERS IAW SR 08530026 REV A. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853680 1 20080921 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN 89420061026. ORIG NR 994522 L33R STA 1 160 TO STA 1220 UPPER WEB HAS HEAVY CORROSION IN SEVERAL PLACES. REMOVED, FABBED, AND INSTALLED NEW DOUBLER AND FASTENERS IAW REO G12470. 2 L 7 4 4F RT 4A25 20081104 CE 2008 11 4 L412008F00001 1 20081011 A 5620 58109595 WINDOW CESSNA 500 500CESSNA 2076602 CE LT PAX NOISY A L41A O OTHER O OTHER NR NOT REPORTED 1 EA 61 320LA 000016 POPPING NOISE COMING FROM THE VICINITY OF LT PAX WINDOW. 1 L 7 2 4F A22CE 20081029 NM 2008 10 29 DL757081395 1 20081021 A 5320 STIFFENER BOEING 757 757232 1384965 NM BS 660 RBL 45 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 WEB STIFFENER CRACKED AT STATION 660 RBL 45. REPAIRED PER SRM 51-40-01 ON NR 00098. 2 L 7 2 4F RT A2NM 20081029 NM 2008 10 29 DL757081396 1 20081021 A 5340 415N400217 MOUNT BOEING 757 757232 1384965 NM GALLEY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 G1A GALLEY AFT OUTBOARD GALLEY MOUNT CORRORED. REPAIRED ON NR 00142 PER 51-40-02. 2 L 7 2 4F RT A2NM 20081029 NM 2008 10 29 DL757081397 1 20081021 A 5340 415N400217 MOUNT BOEING 757 757232 1384965 NM GALLEY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 G1A GALLEY INBD MOUNT CORRODED. REPAIRED PER 51-30-01 ON NR 00136. 2 L 7 2 4F RT A2NM 20081029 NM 2008 10 29 2008UALA06242 1 20081022 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 AFT PIT BS 1400, LT SIDE STR 24L, FRAME INBOARD FLANGE DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF F RAME AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 2008UALA06244 1 20081022 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR OUT OF TOLERANCE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 DOOR R2 REQUIRES DOUBLER AT UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 2008UALA06245 1 20081022 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 AFT PIT, BS 1440LT, STR 23-25L, FRAME INBOARD FLANGE DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED FRAME SECTION AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 WP 2008 10 29 UPS08853586 1 20080927 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV BATH TUBE FITTINGG AT L33R-L34R IS CRACKED. REPAIR AS PER IAW DC8 SRM 51-03-02. 2 L 7 4 4F RT 4A25 20081029 EA 2008 10 29 SWIA200820186 1 20081016 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMEREGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 607SK 10251 FLT 3705 - THIRD AFT CEILING EMERGENCY LIGHT OUT. RELAMPED. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 SWIA200820218 1 20080624 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 772SK 10235 LT FS 280 FLOORBEAM CORRODED. C-CHECK, REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20081028 NM 2008 10 28 ASAA0843620 1 20080912 A 5311 6546534502 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 FWD CARGO BAY STA 520 FRAME CORRODED AT STA 520 BETWEEN STR 27R AND STR 28R PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR DO UBLER AND SHEAR TIE, FABRICATED, LOCATED, DRILLED AND INSTALLED A REPLACEMENT SHEAR TIE AND DOUBLER IAW B737 400 SRM 53 00 07 FIG 201. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873639 1 20081001 A 5320 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE N FALSE WARNING IN INSP/MAINT 1 NM 02 624AS 30778 AFT CARGO PIT CORROSION FOUND ON FLOOR SUPPORT AT BS 767 + 6 RBL 13.84. AFT CARGO PIT FLOOR SUPPORT AT BS 767 + 6 RBL 1 3.84 CORROSION BLENDED OUT. BLEND AREA FOUND TO BE BEYOND LIMIT IAW B737 700 SRM 53 00 53 REF MIGS 5106709 FOR REPAIR D ETAILS ITEM 7 PARTIAL WORK. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873643 1 20081001 A 5320 143A8122 SILL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 FWD CARGO DOOR SILL CORRODED IN MULTIPLE SPOTS. DOOR SILL FOUND TO BE BEYOND LIMIT. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 51 30 01. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873651 1 20081001 A 5320 146A81236 SILL BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 624AS 30778 AFT CARGO PIT DOOR SILL AT BS 807 TO BS 847 RBL 25 CORROSION FOUND. AFT CARGO PIT DOOR SILL CORROSION BLENDED OUT. BLE ND AREA FOUND TO BE BEYOND LIMIT. NEW PART INSTALLED IAW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 ASAA0873640 1 20081001 A 5320 147A7501 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE N FALSE WARNING IN INSP/MAINT 1 NM 02 624AS 30778 AFT CARGO PIT CORROSION AROUND ANCHOR NUTS ON FLOOR SUPPORT CHANNEL AT BS 927 947 RBL 14. CORROSION AROUND ANCHOR NUTS ON FLOOR SUPPORT CHANNEL AT BS 927 947 FOUND TO BE BEYOND LIMIT. SUPPORT CHANNEL REPLACED WITH MADE REPAIR PART IAW B73 7 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081028 EU 2008 10 28 MALA080182 1 20081002 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 340B428 SEAT TRACK HAS CORROSION LBL 18.3 FROM STA 294 AND STA 373. REPAIRED IAW EO S53060. 2 L 7 2 4T RT A52EU 20081028 EU 2008 10 28 MALA080183 1 20081002 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 428XJ 340B428 SEAT TRACK HAS CORROSION BL 0.0 FROM STA 294 AND STA 373. REPAIRED IAW EO S53060. 2 L 7 2 4T RT A52EU 20081028 EA 2008 10 28 ASOA200801284 1 20081003 A 5320 POST CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED 5 CLAMPS FROM HYD LINES (1 JUST FWD OF 409+128, 2 AT 409+128 AND 2 JUST AFT OF 409+128) TO ACCESS FOR AT RBL 27 IAW CRJ 200 SRM 51-41-02. COMPLIED WITH BOMBARDIER REO 601R-53-41-056, REPAIR TO POSTS AT FS 409+128 BULKHEAD. RE-INST ALLED SAME SERVICEABLE CLAMPS (5 EACH) FOR HYD LINES AT RBL 29 AT FS 409+128 IAW CRJ 200 SRM 51-41-02. NEEDS EC/TC. AS A EC/TC REO 601R-53-41-056 COMPLIED WITH. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081028 EA 2008 10 28 ASOA200801283 1 20081003 A 5320 POST CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 FS 559, RBL 9 POST WAS REPLACED ON FS 559 REPAIR REO 601R-53-41-260 JOB 8752815, OP 68. SUPPLEMENTAL SDR CLOSED 10/21/0 8. 2 L 7 2 4F RT A21EA 20081029 NM 2008 10 29 SWAA085705 1 20081022 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR UPPER HINGE CUTOUT FUSELAGE SKIN CRACKED AT BS 303, WL 258. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085724 1 20081017 A 3350 417N5213 COVER BOEING 737 73776Q 13845AA NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 551WN 30280 DURING SCHEDULED MV2 CHECK, FOUND EGRESS TRACK COVER MISSING AT SEAT 11 ABC. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085723 1 20081020 A 5330 6552988 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BETWEEN BS 967 TO BS 986, STR 20L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 USAA920081884 1 20080919 A 5311 6546550 FRAME BOEING 737 7373G7 138447J NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN C18 MAJOR REPAIR NR 6131828, FRAME CRACKED AT BS787 BETWEEN S8R AND S9R. REPAIRED FRAME AT BS787, BETWEEN S8R AND S 9R. IAW TASK CARD NR M1C53002. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 2008UALA06179 1 20081018 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 848UA 1647 EPSU AFT LT INTERIOR LIGHT FAULT ON 3SV EMERGENCY LIGHT CHECK. REPLACED AFT LEFT POWER SUPPLY AND BATTERY. LIGHTS CHEC KED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20081029 WP 2008 10 29 AALA200802507 1 20080929 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1117-1155 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 TUL CORROSION ON FLOOR BOARD SUPPORT ZEE ANGLE ON LT TRACK IN AFT CARGO. INSTALLED NEW ZEE ANGLE ON LT TIE DOWN TRACK B ETWEEN STATION 1117 AND 1155 PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081029 NM 2008 10 29 USAA920081875 1 20080919 A 5311 6546525 FRAME BOEING 737 7373G7 138447J NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN C18 MAJOR REPAIR NR 6131828 FRAME CRACKED AT BS380, BETWEEN S8R & S9R. REPAIRED FRAME AT BS380, BETWEEN S8R & S9R I AW TASK CARD NR M1C53002. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 2008UALA06183 1 20081019 A 3397 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 797UA 26924 SEATS 1E AND 3F 1EA SEAT EEL LIGHTS INOP. SECURED CONNECTOR ON SEAT 1, REPLACED LAMP ASSY ON SEAT 3, OPS CHECK. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081029 NM 2008 10 29 2008UALA06185 1 20081019 A 4940 EXCITER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE APU DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 672UA 30027 APU NO START. REPLACED EXCITOR BOX. APU OPS CHECKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081029 2008 10 29 2008UALA06199 4 20081020 A 2565 D30654122U1 SLIDE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 544UA 25322 DOOR 1L SLIDE PRESSURE NEEDLE INDICATES LOW. PRESSURE BELOW DISPATCH LIMITS. REPLACED SLIDE ASSEMBLY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 2008UALA06202 1 20081021 A 3397 WIRE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 818UA 882 CABIN EMERGENCY LIGHTS AT SEAT 10 ABC NOT ILLUMINATING. REPAIRED WIRE, TESTS OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081029 NM 2008 10 29 2008UALA06169 1 20081017 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 781UA 26945 SEAT 24G EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT, TESTED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081029 NM 2008 10 29 2008UALA06170 1 20081017 A 3350 3071BPEGPL LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 781UA 26945 EMERGENCY LIGHTS OUT AFT GALLEY RT WALL BY FLOOR ACROSS FROM DOOR 4R, 2 AFT LIGHTS NOT WORKING. RELAMPED EMERGENCY LIGH TS, TESTED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081029 NM 2008 10 29 2008UALA06218 1 20081004 A 2121 BLOWER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU MALFUNCTIONED A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 386UA 24661 STRONG ELECTRICAL ODOR IN FWD PART OF AIRCRAFT. REPLACED NORM EXHAUST BLOWER. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20081029 NM 2008 10 29 2008UALA06224 1 20081021 A 5712 RIB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 LT WING O/B LEADING EDGE CAVITY LWR RIB FWD END CRACKED AT OFSS 547. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED DOUBLER T RIMMED DAMAGE AND INSTALLED DOUBLER. 2 L 7 2 4F 4 F RT A1NM E24NE 20081029 NM 2008 10 29 2008UALA06225 1 20081021 A 2560 GIRT BAR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOOR OUT OF RIG A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 818UA 882 PRESSURE CHECK DOOR 2R FOR LEAKS AND MIGRATION OF SLIDE ARMED HANDLE, ACCOUNT OF SCUFF PLATES REPLACED AND GIRT BAR RIGG ED. PRESSURE CHECKED DOOR AT 4 LBS, DOOR ARMED HANDLE GOOD, NO DOOR LEAKS. 2 L 7 2 4F 4 F RT A28NM E40NE 20081029 NM 2008 10 29 2008UALA06213 1 20081021 A 5753 6546435274A SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU TE FLAP DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 327UA 24147 RT OUTBOARD TRAILING EDGE FLAP OUTBOARD LOWER SURFACE DELAMINATED APPROX 72 SQ INCHES. REPLACED DAMAGED OUTBOARD AFT FL AP ON RT WING. OP CHECKED GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081029 EU 2008 10 29 08FDEA04499 1 20081023 A 5347 A5381314400100 TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 668FE 772 RT NR 5 (-Y1959) AFT DUMMY TRACK AT FRAME 54.1 HAS 6 FASTENERS IMPROPERLY INSTALLED AND 1 HOLE IS ELONGATED ON INBD AF T FLANGE OF DUMMY TRACK. REPAIRED RT NR 5 (-Y1959) AFT DUMMY TRACK AT FRAME 54.1 IAW A300-600 FREIGHTER SRM 53-10-16 FI G 202. 2 L 7 2 4F RT A35EU 20081029 EA 2008 10 29 ASOA1227 1 20080926 A 5300 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED AND REPLACED CARGO DOOR SUPPORT BEAM LOWER ANGLE IAW CRJ 200 SRM 51-42-21. PRESSURE CHECK DUE. PRESSURE CHECK GOOD OF CARGO DOOR IAW AMM 21-32-00-863-801. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081029 NM 2008 10 29 2008UALA06232 1 20081022 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 550UA 25398 DOOR 4R LWR GATE CORRODED AND MISSING PIECES. REPLACED LOWER GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 WP 2008 10 29 08FDEA04504 1 20081023 A 5330 AYB70301 SKIN DOUG MD10 MD1010F 3022112 WP BS 1501-1521 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 THE CENTER LANDING GEAR SPACE, BELLY SKIN, RIGHT SIDE FROM STA 1501 TO 1521 IS CORRODED. REMOVED CORROSION AND FOUND SK IN TO BE OUT OF LIMITS IAW SRM 53-00-01. REPAIRED DAMAGED SKIN IAW EA 8-5330-123511. 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 2008UALA06233 1 20081022 A 3510 MC1019151 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 564UA 26666 CAPT O2 MASK HAS CONSTANT FLOW WHEN IN USE. FOUND MASK LEAKING. REPLACED CAPT OXYGEN MASK. LEAK & OPS TEST OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 WP 2008 10 29 08FDEA04506 1 20081023 A 5322 AEA027319 SHEAR TIE DOUG MD10 MD1010F 3022112 WP BS 1501 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 THE CENTER LANDING GEAR SPACE, SHEAR TIE AT FRAME 1501, RIGHT SIDE IS CORRODED. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01. REMOVED DAMAGED SHEAR TIE SECTION IAW SRM 53-30-00. FABBED SHEAR TIE & SPLICE IAW SRM 53-30- 00 & DWG AEA 0273. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED SHEAR TIE & SPLICE IAW SRM 51-33-01. 2 L 7 3 4F RT A22WE 20081029 WP 2008 10 29 08FDEA04507 1 20081023 A 5330 AEA027311 SHEAR TIE DOUG MD10 MD1010F 3022112 WP BS 1481 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 THE CENTER LANDING GEAR SPACE, RIGHT SIDE BELLY AT STA 1481, FROM SHEAR TIE IS CORRODED. REMOVED CORROSION & FOUND TO B E OUT OF LIMITS IAW SRM 53-00-01. REMOVED DAMAGED SHEAR TIE SECTION IAW SRM 53-30-00. FABBED SHEAR TIE & SPLICE IAW S RM 53-30-00 & DWG AEA 0273. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED SHEAR TIE & SPLICE IAW SRM 51-33-01. 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 2008UALA06235 1 20081022 A 5210 PLATE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 820UA 898 DOOR 2R AFT SHEAR PLATE SUPPORT HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: REMOVED SHEAR PLATE SUPPORT. REPLACED SHEAR P LATE SUPPORT. 2 L 7 2 4F 4 F RT A28NM E40NE 20081029 NM 2008 10 29 2008UALA06238 1 20081022 A 3350 1619 LAMP BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 923UA 26643 RT WING OVERWING EXIT EMERGENCY LIGHT INOP. REPLACED RT WING EMERGENCY LIGHT, OP CHECKS GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081029 NM 2008 10 29 AALA200802598 1 20080922 A 5311 FRAME BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CRACK FOUND ON FRAME AT RIGHT STATION 400 BETWEEN STRINGER 8 AND 9. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH ECO J11 59AA. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802604 1 20080922 A 5311 FRAME BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CRACK FOUND ON FRAME AT RIGHT STATION 727B BETWEEN STRINGERS 8 AND 9. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH ECO J 1159AA. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802605 1 20080924 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM ZONE 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION FOUND ON AFT GALLEY AREA FLOORBEAM AROUND NUT CLIP HOLES ON UPPER FLANGE. AREA OF DISCREPANCY IS 1 INCH BY 45 INCHES. CUT OFF TOP OF BEAM FROM RIGHT BUTTLINE 6 TO LEFT OUTBOARD END. INSTALLED T CAP REPAIR IN ACCORDANCE WITH SRM 53-70-51. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802606 1 20080924 A 5315 FLOORBEAM BOEING 737 737823 13844BZ NM ZONE 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION FOUND ON FLOORBEAM AT STATION 986.5 AT RIGHT BUTTLINE 17. REMOVED CORROSION AND REPAIRED IN ACCORDANCE WITH S RM 53 70 51 AND 53 00 51 2R. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802607 1 20080924 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM ZONE 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION FOUND ON FLOORBEAM AT STATION 986.5 AT RIGHT BUTTLINE 23. REMOVED CORROSION AND REPAIRED IN ACCORDANCE WITH S RM 53-70-51 AND 53-00-51 2R. 2 L 7 2 4F RT A16WE 20081029 EA 2008 10 29 SWIA200820208 1 20081018 A 5610 601R3303312 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT FRACTURED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 427SW 2 2 7497 FLT 3768 - AT FL350, RIGHT WINDOW SHATTERED. REPLACED RIGHT SIDE WINDOW, PN ON NP-139322-12, PN OFF 601R33033-12, SN ON 08029H1712, SN OFF 00339H5276. 2 L 7 2 4F RT A21EA 20081029 NM 2008 10 29 AALA200802612 1 20080929 A 5320 PANEL BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION FOUND IN FOUR PLACES ON AFT CARGO FLOORBOARD SUPPORT SIDEWALL TRANSITION PANEL BETWEEN LEFT STATIONS 787 AND 8 27. AREA OF DISCREPANCY WAS 4 INCHES BY 40 INCHES. REPLACED FLOORBOARD SUPPORT TRANSITION PANEL. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802614 1 20080930 A 5320 INTERCOSTAL BOEING 737 737823 13844CB NM BS 320 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 FOUND CRACK ON INTERCOSTAL AT NUT PLATE HOLE AT STATION 320. REPLACED INTERCOSTAL. 2 L 7 2 4F RT A16WE 20081029 EA 2008 10 29 SWIA200820210 1 20080610 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 766SK 10232 FS 280 FLOORBEAM CRACKED. C-CHECK, REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 SWIA200820211 1 20080610 A 5712 RIB CNDAIR CL600 CL6002C10 1390015 EA WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 766SK 10232 ATTACHING RIB BETWEEN 195DL AND 196DR CRACKED. C-CHECK, REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 SWIA200820212 1 20081017 A 5344 HINGE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR WORN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 705SK 10145 FLT 5884 - MAIN CABIN DOOR UNUSUALLY DIFFICULT TO CLOSE, HINGE WORN. REPLACED DOOR HINGE. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 SWIA200820213 1 20081020 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 738SK 10195 FLT 5810 - SECOND FROM LAST CEILING LEVEL EMERGENCY FLOOD LIGHT INOP. OPS CHECKS NORMAL. 2 L 7 2 4F RT A21EA 20081029 NM 2008 10 29 DHLA2008745561 1 20080903 A 5320 WEB BOEING 727 727224 1384076 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN FROM STA 1130 TO STA 1172 FLOOR PANELS SHEAR WEB HAS CORROSION ON BOTH SIDES AND AROUND NUTPLAT ES. REPAIRED FUSELAGE SHEAR WEB SECTION FROM STA 1130 TO STA 1151 BETWEEN LBL16 AND LBL 69.750 IAW B727 SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 20081029 WP 2008 10 29 UPS08853567 1 20080929 A 5320 CUSP WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV REMOVE AND REPLACE ORIGINAL N/R 534909 LEFT LOWER CUSP MEMBRANE CRACKED, DENTED AND CORRODED BETWEEN FS 400-420. UPON INVESTIGATION FOUND DAMAGE WAS REMOVED AND VALIDATED REPAIR WAS A ACCOMPLISHED REF DC8 SRM 53-02-00 FI G 25. 2 L 7 4 4F RT 4A25 20081029 NE 2008 10 29 SWIA200820187 2 20081016 A 7261 CARBON SEAL CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B 30069 NE LT ENGINE LEAKING A SWIA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 455SW 7760 FLT 3799 - AFTER TAKEOFF AIRCRAFT FILLED WITH SMOKE AND WE RECEIVED THE TOILET SMOKE CAUTION. FOUND NR 3 CARBON SEAL LE AK LEFT ENGINE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 20081029 WP 2008 10 29 UPS08853598 1 20080929 A 5320 CUSP WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV REMOVE AND REPLACE EFN 89419971055 ORGINIAL N/R 534204 LEFT CUP MEMBRANE CRACKED AT LBL 45 BETWEEN FS 1580-1600. VERFIED REPAIR COMPLIES WITH SRM 53-02-00 FIG 23. 2 L 7 4 4F RT 4A25 20081029 WP 2008 10 29 UPS08853603 1 20081003 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-20 LT INBOARD FLAP UPPER SURFACE AT STA XW89 DOES NOT MEET CRITERIA OF APPENDI X H. FLAP REPAIR MEETS CRITERIA TO BE IAW DC8 SRM 57-02-01-0 FIG 002Q. 2 L 7 4 4F RT 4A25 20081029 WP 2008 10 29 UPS08853619 1 20081005 A 5420 SKIN DOUG DC8 DC873F 302199F WP NR 3 PYLON MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV RT LOWER LEADING EDGE DOUBLER I/B SIDE NR 3 PYLON AT STA XFS 225 DOES NOT MEET CRITERIA APPENDIX H ST EP 5. 894-W4-31 AREA PREVIOUSLY REPAIRED FEF DC8 SRM 57-2-1 TR 57-83 FIG 14A. 2 L 7 4 4F RT 4A25 20081029 NM 2008 10 29 UPS08M53724 1 20081025 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 260UP 48418 INSPECTION TYPE:1C RT WING SLAT TRACK 312 CUTOUT LWR O/B CORNER CRACKED. HFEC AREA NO CRACK FOUND, HOWEVER FOUND DAMAGE D. CUT OUT DAMAGE IAW SRM VOL 1 57-10-00. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM VOL 1 57-10-00 PG 58. 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 CALA0801008 1 20081027 A 5754 65C26602311SP SKIN BOEING 737 737524 1384721 NM LE SLAT DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 LEFT WING NUMBER 2 SLAT INBOARD AND OUTBOARD WEDGE SEALANT DAMAGED, NEED TO CHECK FOR DELAMINATION. REMOVED AND REPLACE D DELAMINTED SKIN AND CORE ON LEFT WING NUMBER 2 SLAT PER SRM 51-70-10 AND APPLIED PROTECTIVE FINISH PER CAL ECRA 5100 5 00128 REV Q. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0801009 1 20081023 A 3350 D71701100 BATTERY PACK BOEING 737 737824 13844BZ NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 33294 34000 FIRST CLASS EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY EXIT LIGHTS REF MM 33-51-06. 2 L 7 2 4F RT A16WE 20081029 2008 10 29 CALA0801011 4 20081025 A 2565 65C1990115 CABLE BOEING 737 7373T0 1384582 NM EVAC SLIDE FRAYED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14320 23371 ESCAPE SLIDE LATCH CABLE HAS BROKEN STRANDS ON (L-2) AFT ENTRY DOOR. INSTALLED NEW CABLE REF AMM 25-61-35. 2 L 7 2 4F RT A16WE 20081029 EA 2008 10 29 ASOA200801374 1 20081020 A 3211 TRUNNION PIN CNDAIR CL600 CL6002C10 1390015 EA RT MLG CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 RT MLG SHOCK STRUT UPPER (FWD) ATTACHMENT TRUNNION PIN SHOWS SIGN OF CORROSION. AFTER FURTHER INSPECTION FOUND RESIDUE TO BE DRIED CORROSION INHIBITING COMPOUND. REMOVED BOLT, CLEANED AREA AND REINSTALLED BOLT WITH CORROSION INHIBITING CO MPOUND PER AMM 32-00-05. RII SATISFACTORY FOR THE INSTALLATION OF THE FWD TRUNNION PIN ATTACH BOLT PER CRJ 700 AMM 32-1 1-05 AND SP 607. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA200801376 1 20081021 A 5347 SH670321591 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 ALL CABIN FLOOR SEAT TRACKS HAVE CORROSION AS MARKED. R & R SEAT TRACK AS PER MM 53-00-49. BLENDED AREA FOUND TO BE OU T OF LIMITS PER SRM 53-51-49. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA200801377 1 20081021 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 RIGHT WALL SEAT TRACK SECOND SEGMENT FROM FRONT OF AIRCRAFT HAS CORROSION AS MARKED. REMOVED AND REPLACED RIGHT SIDE WA LL SEAT TRACK IAW SRM 51-41-02. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA200801391 1 20081024 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN FAILED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 761ND 10213 WITH EMERGENCY LIGHTS SW IN ON POSITION LIGHTS COME ON THEN FADE WITHIN 15-20 SECONDS. FLT 5083 DEL 136 MINS. FLT 4926 ,4927 CX. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA1235 1 20080928 A 5320 STRAP CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 BLENDED CORROSION IN BELLY AT FS 280.00 LOWER STRAP IAW CRJ 700 SRM 51-21-06 MO 7025667. REWORKED AREA NEEDS THK'S CHE CK. PERFORMED THICKNESS MEASUREMENT OF BLEND AREA ON LOWER STRAP AT FS 280.00, INTERNALLY IAW CRJ 700 NDTM 51-20-004. MINIMUM THICKNESS IS .075". INSTALLED FASTENERS IAW CRJ 700 SRM 51-42-06 AND PAINTED SURFACES IAW CRJ 700 SRM 5125-01. APPLIED CIC TO FUSELAGE STRAP DOUBLER JUST AFT FS 280 PER CRJ 700 SRM 51-21-11. PERFORMED ET INSPECTION OF THE BLENDED AREA PER REO 670-53-21-396 IAW CRJ 700 NDTM 51-20-006. NO DEFECTS NOTED. THE DAMAGE ON THIS REPAIR WAS BLENDED, MEASU RED AND REPORTED TO BOMBARDIER. THE ABOVE WORK DONE IAW REO 670-53-21-396. RII COMPLETED SATISFACTORY PER SP 607. SUP 2 L 7 2 4F RT A21EA 20081029 NM 2008 10 29 SWAA085803 1 20081027 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, BETWEEN STR 23L TO STR 22L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085804 1 20081027 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 986, STR 20L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085805 1 20081027 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085806 1 20081027 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085795 1 20081027 A 5340 6527314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 365SW 26576 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 16L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085718 1 20081021 A 3350 65C27095 BATTERY BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 404WN 27892 DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT LIGHT BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081028 NM 2008 10 28 SWAA085690 1 20081018 A 3350 411A2212 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 474WN 33861 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT LENS MISSING NEAR AFT SERVICE DOOR. INSTALLED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085697 1 20081020 A 5312 6545409 PRESSURE PANEL BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED HC1 CHECK, FOUND RT MLG W/W PRESSURE DECK WEB CRACKED AT BS 665 RBL 40. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085698 1 20081019 A 5330 6552988 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR LOWER FWD FUSELAGE SKIN CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085726 1 20081020 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 705SW 27839 DURING SCHEDULED MV2 CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT LENS BROKEN. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081029 EA 2008 10 29 QXEA200800884 1 20080728 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA BS 626.5 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 PDX C4 CHECK LT SEAT TRACK HAS GOUGE INSIDE THE TRACK AT APPROX STA FS626.500. BLENDED OUT GOUGE IAW 670-53-00-013 SHT 2 STEPS 1-2. .005" MAX MATERIAL REMOVED. BLEND IS WITHIN LIMITS IAW REO 670-53-00-013 TABLE 1. FPI IAW HORIZON NDTM S ECT 8 NO CRACKS NOTED. ALODINED AREA IAW SRM 51-21-11. 2 L 7 2 4F RT A21EA 20081029 NM 2008 10 29 AALA200802496 1 20080926 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM BS 947 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 TUL CORROSION ON UPPER SURFACE OF FLOORBEAM BEYOND LIMITS. REPAIRED PER ESO 61000 DATED 22 SEP 08. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802498 1 20080926 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM BS 947 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 TUL CORROSION ON UPPER SURFACE OF FLOORBEAM BEYOND LIMITS. REPAIRED PER ESO 61000 DATED 22 SEP 08. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 USAA920081877 1 20080919 A 5311 6546529 FRAME BOEING 737 7373G7 138447J NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN C18 MAJOR REPAIR NR 6131828 FRAME HAS A .250 INCH CRACK AT BS 440, BETWEEN S8R AND S9R ALSO BETWEEN S8L AND S9L. RE PAIRED FRAME AT BS 440, BETWEEN S8R AND S9R ALSO BETWEEN S8L AND S9L. IAW TASK CARD NR M1C53002. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802489 1 20080925 A 5320 FLOOR SUPPORT BOEING 737 737823 13844CB NM BS 760 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION ON FLOOR SUPPORT IN AFT CARGO BEYOND LIMITS. REPLACED FLOOR SUPPORT PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 2008UALA06188 1 20081020 A 3350 POWER SUPPLY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 569UA 26677 EMERGENCY LIGHT PROBLEM DISCOVERED ON 1SV. REPLACED POWER SUPPLY M10818, M10817 AND BATTERY PACKS FOR BOTH POWER SUPPLI ES. 2 L 7 2 4F 4 F RT A2NM E17NE 20081029 NM 2008 10 29 2008UALA06198 1 20081020 A 2913 731966 PUMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HYDRAULIC SYS LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 779UA 26941 AFTER AIRCRAFT WAS DELIVERED TO GATE, FOUND CENTER (C2) HYDRAULIC PUMP LEAKING. REPLACED PUMP. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081029 NM 2008 10 29 2008UALA06200 1 20081021 A 3397 362624 CONNECTOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 314UA 23675 EMERGENCY EXIT LIGHT STRIP HAS SEGMENT THAT DOES NOT ILLUMINATE BY 2B AND STRIP BY AFT GALLEY BROKEN. SECURED LOOSE CO NNECTIONS AT LIGHT STRIPS. BOTH TEST NORMAL. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081029 NM 2008 10 29 2008UALA06208 1 20081020 A 3350 30234112 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 228UA 30556 DOOR 3R EXTERNAL EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT, OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081029 NM 2008 10 29 CALA0800980 1 20081023 A 5315 141T52822 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 68155 30434 E AND E COMPARTMENT M/D FLOORBEAM STATION 246 LBL 25 VERTICAL STIFFENER FOUND CRACKED. M/D FLOORBEAM STATION 246 LBL 25 VERTICAL STIFFENER REPLACED PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081029 NM 2008 10 29 CALA0800985 1 20081023 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16650 28911 BODY STATION 867 LT SIDE FRAME CRACKED AT AIR CONDITIONING (A/C) BRACKET BETWEEN S-8 AND S-9. CUT OUT DAMAGE ON FRAME A T BODY STATION 867L BETWEEN S8 AND S9. FABRICATED REPAIR PARTS AND INSTALLED PER EA5310-04498. 2 L 7 2 4F RT A16WE 20081029 GL 2008 10 29 08FDEA04576 2 20081027 A 7230 9690M04 BLADE DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL ZONE 400 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 NR 3 ENGINE S/N 451539 10TH STAGE COMPRESSOR BLADE T/E TIP AREA HAS A DING 0.036 INCH WITH 0.020 TEAR ON THE CONVEX SIDE . BLENDED BLADE TIP AND REMOVED THE DAMAGED AREAS AND PERFORMED AN INSPECTION TO ENSURE DEFECTS HAVE BEEN REMOVED IAW M D-10-10 AMM 72-36-00-2. 2 L 7 3 4F 4 F RT A22WE E23EA 20081104 CE 2008 11 4 L412008F00002 1 20081011 A 3150 WARNING LIGHT CESSNA 500 500CESSNA 2076602 CE ILLUMINATED A L41A O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 61 320LA 000016 DOOR MASTER WARNING ON IN FLT. 1 L 7 2 4F A22CE 20081104 WP 2008 11 4 UPS08853682 1 20080930 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV EXT DOUBLER BS 1279.5 TO 1299.5 AT L35R CENTERLINE NEED VALIDATION FOR REPAIR REF SEQ 894-FA-57. RE MOVED, FABBED AND REPLACED DOUBLER IAW BOEING ROD SKETCH 99-01-20-004 REV IR AND UPS EO DC8-53-20422. 2 L 7 4 4F RT 4A25 20081031 CE 2008 10 31 26N2008F00005 1 20080804 A 2700 70611107 SELECTOR CESSNA 510 510 2076617 CE AILERONS UNKNOWN E 26NA O OTHER O OTHER NR NOT REPORTED 1 EA 05 1693L 5100026 CREW REPORTED AILERONS FROZE AFTER FLYING THROUGH MOISTURE. 07/25/2008 AC REPOSITIONED TO SERVICE CENTER FOR FURTHER EVA LUATION AND RESOLUTION. MFG HEAVILY INVOLVED WITH THIS ISSUE. (K) 1 L 7 2 4F RT A00014WI 20081031 CE 2008 10 31 DXTA2008102703320 1 20081026 A 2720 RUDDER CESSNA 680 680CE 2076811 CE LOCKED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED TO TAKEOFF 1 GL 07 370QS 6800099 ON TAKEOFF RUDDER FELT LIKE IT WAS HANGING UP. WHEN AIRCRAFT WAS AIRBORNE RUDDER COMPLETELY LOCKED UP. 2 L 7 2 4F RC T00012WI 20081031 NM 2008 10 31 2008UALA06259 1 20081023 A 3350 20131A POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 646UA 25283 DURING TAXI IN, F/A REPORTED ESCAPE PATH LIGHTING CYCLING OFF AND ON. REPLACED M1557 BATTERY PWR SUPPLY. GOOD OP CHECK . 2 L 7 2 4F 4 F RT A1NM E24NE 20081031 NM 2008 10 31 2008UALA06271 1 20081024 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 820UA 898 BEAM 150 NEEDS REPLACEMENT. MAJOR REPAIR ACCOMPLISHED. BEGAN REMOVAL OF BEAM 150. REMOVED FLOORBEAM 150 AND BEGAN INS TALLING BRACKETS ON BEAM. INSTALLED ALL BRACKETS AND JOINED FLOORBEAMS 150 AND 80 TOGETHER. REPLACED FLOORBEAM 150. 2 L 7 2 4F 4 F RT A28NM E40NE 20081031 2008 10 31 HALA2008102500827 4 20081025 A 3417 4040800911 ADC BOEING 767 767332 1382001 NM RIGHT FAULTY A HALA K NONE O OTHER CR CRUISE 1 WP 13 594HA 16017 16017 23275 ETOPS SIGNIFICANT SYSTEM - F/O ALTIMETER IN ERROR, IT READS 33850. CAPT ALTIMETER READS 34000. STBY ALT READS 34300, S ELECTING ALTN AIR DATA CORRECTS FAULT. REPLACED RT ADC. OPS CHECK OK PER MM 34-12-01. PERFORMED MCDP TEST 30 TO RETAI N A/C LMP STATUS IN LAND 3. TEST 30 PASSED. 2 L 7 2 4F RT A1NM 20081103 EA 2008 11 3 C2XA08CL115 2 20081016 A 7261 LINER EMB 145 EMB145XR 3260214 SO RROYCE AE3007 AE3007A1E 54169 EA NR 0 BEARING OUT OF POSITION A C2XA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 18120 145681 CAE312251 MCI FLIGHT NR 2484 THE CREW REPORTED SMOKE IN THE CABIN SHORTLY AFTER TAKE OFF FROM MCI. THE ACFT RETURNED TO MCI AND L ANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE NR 2 ENGINE. OPS CHECKS WERE GOOD. INVESTIGATION CLOSE-OUT FROM MANUFACTURER INDICATED THE NR 0 BEARING LINER SHIFTED. THIS ALLOWED OIL TO ESCAPE THE FAN BEARING HOUSING AND SUBSEQUE NTLY GET INTO THE CORE FLOW OF THE ENGINE. THE PFI IS THEREFORE THE FAN BEARING HOUSING. 2 L 7 2 4F 4 F RT TE6CH 20081103 NM 2008 11 3 KCSA081537 1 20081016 A 5347 SEAT TRACK BOEING 747 747249F 1384849 NM BS 998 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 SEAT TRACK CRACKED AT STA 998 ON MAIN DECK LBL75. 2 L 7 4 4F RT A20WE 20081103 EU 2008 11 3 USAA920081897 1 20081015 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 633AW 54526 398 82 LOG PAGE 4408275 FLT NR 232 PHX-LAS EMERGENCY LIGHT FORWARD LT EMERGENCY POWER SUPPLY UNIT INTERNAL LOADS FAULT. MX R&R THE FORWARD EMERGENCY POWER SUPPLY UNIT PER AIRBUS MM 33-51-38. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081103 EU 2008 11 3 USAA920081906 1 20081004 A 5315 D5347209400200 FLOORBEAM AIRBUS 320 A320231 3930325 EU ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C7 MAJOR REPAIR NR 6109453 GALVANIC CORROSION ON FLOORBEAM AT FR66 Y512. REPLACED FLOORBEAM AT FR66, Y512 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081103 NM 2008 11 3 USAA920081910 1 20081016 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 813AW 1223 LOG PAGE NR 8351550 FLT 683 BOI-PHX EMERGENCY LIGHT FLASHLIGHT A JUMPSEAT INOPERATIVE. R&R JUMPSEAT FLASHLIGHT A BATTER Y. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081103 NM 2008 11 3 USAA920081916 1 20081020 A 5312 BULKHEAD BOEING 737 7373B7 138447F NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 24479 PIT MAJOR REPAIR FPBH INSPECTION NR 4371880. FORWARD PRESSURE BULKHEAD FORWARD FACE CRACKED AT BS 178, RBL 10, WL 234 A T RIVET HOLE. REPAIRED FORWARD PRESSURE BULKHEAD FORWARD FACE CRACKED AT BS 178, RBL 10, WL 234 IAW SRM 53-10-08 FIGURE 201. 2 L 7 2 4F RT A16WE 20081103 EU 2008 11 3 USAA920081963 1 20080927 A 5320 D53475565210 SILL AIRBUS 320 A320231 3930325 EU ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C7 MAJOR REPAIR NR 6060490 CORROSION ON LOWER SILL BETWEEN FR52A AND FR 56, S39R AMD S41R AFT CARGO COMPARTMENT. RE PAIRED LOWER SILL BETWEEN FR52A AND FR56, S39R AND S41R AFT CARGO COMPARTMENT IAW EA NR 132087. 2 L 7 2 4F RT A28NM 20081103 NM 2008 11 3 USAA920081973 1 20081024 A 5320 6913383 WEB BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03C20353004/003 WEB CRACKED AT BS 243.7, WL 208, LBL 18 AT LIGHTNING HOLE. REPLACED WEB AT BS 24 3.7, WL 208, LBL 18 IAW DRAWING NR 69-1338. 2 L 7 2 4F RT A16WE 20081103 SW 2008 11 3 QML2008F00016 1 20081016 A 6321 40004244 BRAKE BELL 222 222U 1182140 SW MAIN ROTOR OUT OF ADJUST E QMLA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 NM 03 402MA 47540 ON REPOSITION FLIGHT, APPROX 6 MILES FROM LANDING, ROTOR BREAK AND MASTER CAUTION ILLUMINATED. THIS IS A LAND AS SOON A S POSSIBLE EVENT. CONSULTED THE CHECKLIST. VERIFIED POSITION OF ROTOR BREAK HANDLE. THE HANDLE WAS SECURE. IN ADDITI ON, VERIFIED TRANSMISSION TEMPERATURE INDICATORS, RPMR, TORQUE, LISTENED FOR UNUSUAL GRINDING OR SCOURING SOUNDS IN THE TRANSMISSION AREA AND TURNED THE ACFT TO CHECK FOR INDICATIONS OF SMOKE. NONE OF THESE INDICATORS WERE PRESENT. TERRAI N BELOW WAS NOT PERMISSIVE FOR LANDING. CONTINUED TO DESTINATION, NOTIFIED LIFECOM DISPATCH CENTER, MX AND MANAGEMENT. INSPECTION REVEALED NO UNUSUAL WEAR, ODORS, BURNING INDICATIONS OR DAMAGE TO THE ROTOR BRAKE. ADJUSTED ROTOR BRAKE. 1 G 7 2 3U H9SW 20081104 WP 2008 11 4 UPS08853649 1 20080921 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV EVALUATION AND DISPOSITION EFN 89419971107 ORGINIAL N/R 534711 R-1 DO OF FORWARD DOOR JAMB REPAIR FOR ELONGATED HOLES. REPAIRED BY ANGLE AND WEB REF DC8 51--21 EO DC8 5310-11728B AND DWG 53 DC8 53A-011-REV A. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853652 1 20080930 A 5310 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV EXT WINDOW DOUBLER BS 1400 TO 1421 1.5 ABOVE L14R TO 1.5 BELOW L17R NEEDS VALIDATION FOR REPAIR. REP AIRED BY SRM 51-3-0 AND EO DC 5320-31585. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853728 1 20081002 A 5712 RIB DOUG DC8 DC871F 302199D WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATE AND DISPOSITION EFN 70219911059 ORIGINAL NRC 188671 RIB CRACKED AT OUTBOARD FORWARD CORNER O F ACCESS PANEL 522B. REPAIRED IAW 57-02-00 PG 1 FIG 002. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853729 1 20081002 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATE EFN 70219901052 ORIGINAL NRC 158580 CORRODED PATCH ON C-CROSS DOOR AT FS 1182, L33R. SPLICE MEETS DOUGLAS DRAWING BSH4868. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853730 1 20081002 A 5520 STRUCTURE DOUG DC8 DC871F 302199D WP LT ELEVATOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATE EFN 70220081043 ORIGINAL NR 123529 DAMAGE COUNTERSINKS ON INBOARD AFT CORNER OF LEFT ELEVATO R. REPAIR IAW 55-02-00 FIG 002. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853741 1 20081002 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:S/V EVALUATE REPAIR EFN 70219911007 ORIGINAL NRC 289089 HEAVY CORROSION ON FWD SIDE OF CANTED BELT FRAME STA 1723 L35 L35R. REPAIR FOUND TO BE VALID DWG 5772706. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853742 1 20081002 A 5220 DOOR FRAME DOUG DC8 DC871F 302199D WP EMERGENCY EXIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATE REPAIR EFN 7021991074 ORIGINAL NRC 289037 LEFT AFT EMERGENCY DOOR CRACKED ON FRAME FLANGE RA DIUS FORWARD CORNER. REPAIRED SRM 52-02-00 FIG 002. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853749 1 20081002 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATE EFN 70219961032 ORIGINAL N/R 445992 WEB NEEDS TO BE CUT AND REMOVED BETWEEN FS 1190 AND 121 0. PREVIOUSLY REPAIRED SRM 53-02-00. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853750 1 20081002 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATION OF REPAIR EFN 70220081026 N/R 123643 REPAIR DOUBLER IS GOUGED IN C PIT TORQUE BOX AT FS 11 90 L33R. REPAIR PREVIOUSLY DC8 SRM 53-02-00 FIG 001B. 2 L 7 4 4F RT 4A25 20081104 NM 2008 11 4 KCSA081516 1 20081007 A 5330 SKIN BOEING 747 747249F 1384849 NM BS 2715 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 SKIN, BS 2715 TOP OF FUSELAGE DENTED. (K) 2 L 7 4 4F RT A20WE 20081104 NM 2008 11 4 KCSA081524 1 20081009 A 5330 SKIN BOEING 747 747249F 1384849 NM BS 2412 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 DENT IN SKIN AT STA-2412 INBD OF JACK PAD AT RBL-65R. (K) 2 L 7 4 4F RT A20WE 20081104 NM 2008 11 4 WX0A070233 1 20080904 A 3350 AD4002 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 892GA 49826 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSP, MAINT REPORTED A PROTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD N OT TEST. MAINT REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATION AL CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. (K) 2 L 7 2 4F RT 20081104 NM 2008 11 4 USA2008F00040 1 20081003 A 3297 17073804903 WIRE HARNESS EMB ERJ190 ERJ190100IGW 3260408 NM NLG STEERING DAMAGED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 957UW 19000161 THE CREW WAS UNABLE TO RETRACT THE LANDING GEAR UPON TAKEOFF. THE FLIGHT RETUREND TO THE FIELD WITHOUT INCIDENT. MAINTEN ANCE REPLACED THE LANIDNG CONTROL LEVER AND THE PROXIMITY SENSOR MODULE. HOWEVER, ON THE FIRST FLIGHT OUT, THE HANDLE TO RETRACT THE GEAR WOULD NOT MOVE PREVENTING THE GEAR FROM RETRACTING. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED UNEV ENTFULLY. MAINTENANCE REPLACED THE NOSE LANDING GEAR WEIGHT ON WHEEL SENSOR/STEERING SENSOR FEEDBACK ELECTRICAL HARNESS. (K) 2 L 7 2 4F RT A57NM 20081104 NM 2008 11 4 WRLA2008077 1 20081002 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE WORN A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHECK, MECHANIC FOUND MAIN CABIN SEAT TRACK WORN AT STA Y-635, X-8.5. REPAIRED DAMAGE SEAT TRACK PER MD- 11 SRM 53-70-00 FIG.1 VOL.1 REV.40. 2 L 7 3 4F RT A22WE 20081104 EU 2008 11 4 COEA0804919 1 20081003 A 5210 S52176300204 SKIN AEROSP ATR42 ATR42300 8680920 EU PAX DOOR CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 919FX 266 DAMAGE TO AFT LT PASSENGER. DOOR SKIN DENTED AND CRACKED BEYOND SRM LIMITS. ATR SRAS DO/TS-3648.08, 4803 ISSUED TO REPAI R DOOR. DOOR SKIN DAMAGED AREA CUT OUT AND A DOUBLER INSTALLED. DOUBLER INSTALLED USING SRAS DO/TS-3648/08-10619 INSTRUC TIONS. (K) 2 H 7 2 4T RT A53EU 20081104 CE 2008 11 4 DXTA200803294 1 20081004 A 3240 BRAKE SYS CESSNA 500 560CESSNA 2076750 CE MLG FAILED E DXTA O OTHER J WARNING INDICATION LD LANDING 1 GL 07 336QS 5600336 BOTH BRAKES ON BOTH SIDES FAILED ON LANDING. (K) 2 L 7 2 4F RT A22CE 20081104 NM 2008 11 4 KCSA081519 1 20081007 A 5753 SPAR BOEING 747 747122 1384872 NM LT WING TE FLAP DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 LT OTBD MID FLAP AFT SPAR HAS TOOLING DAMAGE. UNDER WBL 815 ACCESS PLATE. (K) 2 L 7 4 4F RT A20WE 20081104 NM 2008 11 4 KCSA081514 1 20081006 A 5322 SHEAR TIE BOEING 747 747122 1384872 NM BS 1740 S11R DAMAGED A KCSA O OTHER O OTHER NR NOT REPORTED 1 GL 23 712CK 19754 STA 1740 STR 11R SHEAR TIE HAS ELONGATED HOLES. (K) 2 L 7 4 4F RT A20WE 20081104 NM 2008 11 4 KCSA081522 1 20081009 A 5330 SKIN BOEING 747 747249F 1384849 NM BS 2595 S46R DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 DENT IN SKIN AT STA-2595 AT STR-46R. (K) 2 L 7 4 4F RT A20WE 20081104 NM 2008 11 4 KCSA081523 1 20081009 A 5330 SKIN BOEING 747 747249F 1384849 NM BS 2610 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 DENT IN SKIN AT STA-2610 BETWEEN STR-42R AND STR-46R. (K) 2 L 7 4 4F RT A20WE 20081104 WP 2008 11 4 WXOA070232 1 20080903 A 3350 AD4002 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS FAILED A WXOA K NONE L NO TEST IN INSP/MAINT 1 WP 19 878GA 53487 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSP, MAINT REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOUL D NOT TEST. MAINT REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERAT IONAL CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (K) 2 L 7 2 4F RT A6WE 20081104 NM 2008 11 4 USA2008F00041 1 20081006 A 3350 1012721 LIGHT BOEING 737 7373G7 138447J NM ROW 4 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 154AW 23776 MAINTENANCE REPORTED THE EMERGENCY EXIT PATH LIGHT AT SAT ROW 4, LT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSY. OPS CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 20081104 NM 2008 11 4 KCSA081525 1 20081009 A 5347 SEAT TRACK BOEING 747 747249F 1384849 NM BS 320 WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 CAPTAINS INBD SEAT TRACK WORN LBL-36, STA-320. (K) 2 L 7 4 4F RT A20WE 20081104 EA 2008 11 4 ASOA200801402 1 20081025 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 750EV 10161 RT SIDE OVERWING EXTERIOR EXIT EMERGENCY LIGHT IS INOP. 2 L 7 2 4F RT A21EA 20081104 NM 2008 11 4 KCSA081517 1 20081007 A 5347 SEAT TRACK BOEING 747 747249F 1384849 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 CAPTAINS AFT SEAT TRACK IS CRACKED .250 INCH. (K) 2 L 7 4 4F RT A20WE 20081104 EA 2008 11 4 ASOA200801403 1 20081026 A 7830 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA THRUST REVERSER MALFUNCTIONED A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 835AS 7258 IN FLIGHT RETURN, RT THRUST REV UNLOCK MSG AT 22000FT, UNCOMMANDED YAW. RT ENGINE SHUTDOWN IN FLIGHT. EMERGENCY DECLAR ED. A/C RETURNED TO ATL AFTER T/O. REMOVED AND REPLACED BALL SCREW ACTUATOR IAW AMM 78-3201, OPS CHECK GOOD. CLEARED , PLACARD REMOVED. 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 ASOA200801404 1 20081026 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 880AS 7606 PAX DOOR DIFFICULT TO CLOSE. 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 ASOA200801405 1 20081026 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 861AS 7445 PAX DOOR BOTTOM STEP BROKEN. 2 L 7 2 4F RT A21EA 20081104 CE 2008 11 4 DXTA2008110303334 1 20081101 A 2730 WARNING SYSTEM CESSNA 750 750 2076810 CE COCKPIT ACTIVATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 900QS 7500123 PITCH FEEL FAIL" CAS MESSAGE ILLUMINATED IN FLIGHT. 2 L 7 2 4J RT T00007WI 20081104 WP 2008 11 4 UPS08853768 1 20081024 A 5753 SKIN DOUG DC8 DC871F 302199D WP TE FLAP DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV REF UPS EO APPENDIX H STEP A (7) REPAIR FAILS. SURVEY SEQUENCE 715-W3-27. INSTALLED DOUBLER IAW DC8 SRM 57-02-01-0. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853770 1 20081013 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV SURVEY SEQUENCE NUMBER 702-F1-46 DOES NOT MEET SRM CRITERIA. REPAIRED IAW DC8 SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 20081104 NE 2008 11 4 IXXA080029O 2 20081029 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE NR 3 FLAMED OUT A IXXA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 SW 11 821BX 40894 7207 45811 693218 AFTER LEVEL OFF AT 37,000 FT DURING THROTTLE REDUCTION NUMBER THREE ENGINE FLAMED OUT. THE CREW PERFORMED INFLIGHT STAR T AT 22,000 FT, RESTART NORMAL. THE CREW LANDED IN KTOL WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED CFM FAULT 51, TROUBLESHOT TREE, CLEANED WEEP HOLE ON CDP TUBE, CHECKED CHIP DETECTOR, SPECIFIC GRAVITY .82, FLIGHT IDLE 74 N2-FF 6000P PH AT 75 PERCENT N1. EGT 683, FUEL PRESSURE 31PSI PUMP OFF. OPERATIONAL CHECK GOOD IAW CFM MAINTENANCE MANUAL 71-00-00 . AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT 4A25 E2GL 20081104 NM 2008 11 4 TSAA0878027 1 20081028 A 7897 PIN BOEING 737 7372X6C 1384552 NM CONNECTOR BACKED OUT A TSAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 840A 23124 FLT 917, NR 1 THRUST REVERSER LIGHT FLICKERED DURING TAXI OUT. RETURNED TO BLOCK. MEL’D NR 1 T/R IAW MEL 78-1-1, VERIF IED NR 1 T/R CLOSED AND LOCKED. PLACARD INSTALLED. MAINTENANCE FOUND PIN 16 ON CONNECTOR D4856P PUSHED OUT. INSTALLED PIN 16 INTO SPARE PIN NR 10 ON CONNECTOR D4856P AND D4856J. OPS CHECK OF NR 1 T/R PER AMM 78-32-01, PG 501 GOOD. MEL CLEARED, PLACARDS REMOVED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A16WE 20081104 NM 2008 11 4 USAASB08104 1 20081030 A 3350 20121 CHARGER BOEING 737 7374B7 138449C NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 458UW 25022 FLL - MAINTENANCE REPORTED THE LOW LEVEL EMERGENCY LIGHTING, FROM SEAT ROWS 12 THRU 17, INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20081104 EA 2008 11 4 QXEA2008103000750 1 20080711 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 612QX 10042 PDX - C4 - LT OUTBOARD SEAT TRACK HAS CORROSION ON TRACK AT APPROX FS 708.00. BLENDED OUT CORROSION AND FOUND TO BE OUT OF LIMITS PER REO 670-53-00-013. REMOVED TRACK IAW CRJ 700 MM 53-00-49-000-801-A02 PARA 3A-D (1) (B). INSTALLED NEW T RACK IAW CRJ 700 AMM 53-00-49-400-801A02 PARA 6A-D (1) (B) & E (1). 2 L 7 2 4F RT A21EA 20081104 NM 2008 11 4 DHLA2008745582 1 20080910 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN BS 328 LBL 45 FLOORBEAM UPPER CHORD CORRODED. REPAIRED UPPER FUSELAGE FLOORBEAM UPPER CHORD S ECTION AT BS 328 BETWEEN LBL 38.5 AND LBL 51.5 IAW B727 SRM 53-10-8 FIG 9. 2 L 7 3 4F A3WE 20081104 SO 2008 11 4 FDKA2008102800283 1 20081028 A 5210 DOOR EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 825MJ 145179 FRL FLT 6243 IAD-JFK. MAIN CABIN DOOR HARD TO OPEN. MX LUBED DOOR, OPS GOOD. 2 L 7 2 4T RT T00011AT 20081104 SO 2008 11 4 FDKA2008102900284 1 20081028 A 5210 DOOR EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF RIG A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FDM FLT 8904 CVG-MEM. MAIN CABIN DOOR WILL NOT CLOSE. MX ADJUSTED RIGGING ON DOOR. 2 L 7 2 4T RT T00011AT 20081104 SO 2008 11 4 FDKA2008102900285 1 20081029 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A FDKA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 853MJ 145464 FRL FLT 6227 JFK. HEAVY BURNING SMELL IN CABIN. MX INSPECTED AIRCRAFT AND NO DEFECTS FOUND. 2 L 7 2 4T RT T00011AT 20081104 WP 2008 11 4 AALA200802631 1 20081001 A 5320 BEAM DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON MID CARGO DOOR BEAM. AREA OF DISCREPANCY IS 3 INCHES BY 12 INCHES WITH AT DEPTH OF .112 INCH. INSTA LLED DOUBLER IN ACCORDANCE WITH AARD 53 10 00 3. 2 L 7 2 4F RT A6WE 20081104 WP 2008 11 4 AALA200802632 1 20081002 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON RIGHT TIE DOWN TRACK IN AFT CARGO. AREA OF DISCREPANCY IS 3 INCHES BY 111 INCHES. REPLACED RIGHT TI E DOWN TRACK IN ACCORDANCE WITH SRM 51 10 3. 2 L 7 2 4F RT A6WE 20081104 WP 2008 11 4 AALA200802633 1 20081001 A 5347 SPLICE DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION ON LEFT TIE DOWN TRACK SPLICE AT AFT CARGO. AREA OF DISCREPANCY IS 1 INCH BY 6 INCHES. REPLACED LEFT TIE DOW N TRACK SPLICE IN ACCORDANCE WITH SRM 51 10 1. 2 L 7 2 4F RT A6WE 20081104 EA 2008 11 4 SWIA200820250 1 20080625 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 773SK 10236 FLOORBEAM CRACKED AT FS 280 LEFT AND RIGHT SIDES (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081104 WP 2008 11 4 AALA200802643 1 20081002 A 5311 FRAME DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON BALL FRAME AT STATION 1309 LONGERON 30. AREA OF DISCREPANCY WAS 12 INCHES BY 2 INCHES. CUT OUT DAMA GED AREA AND INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53 10 00 17 AND ESO 80559 DATED 01 OCT 2008. 2 L 7 2 4F RT A6WE 20081104 WP 2008 11 4 AALA200802644 1 20081002 A 5313 S27779223 LONGERON DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CRACK FOUND ON LONGERON 4 LEFT BETWEEN STATIONS 170 AND 228. CRACK LENGTH WAS 60 INCHES. ACCOMPLISHED SPLICE REPAIR IN ACCORDANCE WITH SRM 53 02 00. 2 L 7 2 4F RT A6WE 20081104 WP 2008 11 4 AALA200802645 1 20081002 A 5320 STRUCTURE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON SUB FLOOR INBOARD OF FORWARD SERVICE DOOR. AREA OF DISCREPANCY IS 10 INCHES BY 10 INCHES. REMOVED D AMAGE AND INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53 20 00 16. 2 L 7 2 4F RT A6WE 20081103 SO 2008 11 3 C2XA08CL114 1 20081016 A 3350 78812 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13553 145585 CLE FLIGHT NR 2927 THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTING INOPERATIVE BY THE EXIT ROW. MX REPLACED THE AIS LE PATH LIGHT STRIP. OPS CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20081103 SO 2008 11 3 C2XA08CL117 1 20081017 A 7931 OIL SYSTEM EMB 145 EMB145LR 3260212 SO RROYCE AE3007 AE3007A1P 54571 EA NR 1 ENGINE FLUCTUATES A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 13968 145138 CAE311209 EWR FLIGHT NR 2142 THE CREW REPORTED DURING TAKEOFF ROLL AND INITIAL CLIMBOUT THE OIL PRESSURE REMAINED ABOVE 115 PSI FO R 2 MIN ON THE NR 1 ENGINE. ALSO BELOW 13000 FT THE NR 1 ENGINE OIL PRESSURE WOULD ENTER THE AMBER RANGE WITH THRUST IN DESCENT. MX INSPECTED AND REPLACED THE NR 1 ENGINE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081103 WP 2008 11 3 AALA200802525 1 20080918 A 5310 952000815 BEAM DOUG DC9 DC982 3022082 WP BS 644-684 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70504 49798 DOUBLER ON MID CARGO DOOR BEAM IS CORRODED. AREA OF DISCREPANCY IS 32 INCHES BY 4 INCHES. INSTALLED DOUBLER ON MID CAR GO DOOR BEAM PER AARD 53-10-00-03. 2 L 7 2 4F A6WE 20081103 EU 2008 11 3 COEA0806917 1 20081011 A 5754 SKIN AEROSP ATR42 ATR42300 8680920 EU LT WING SLAT DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 917FX 354 FOUND AT COE LT WING FWD UPPER LEADING EDGE SLAT HAS MECHANICAL DAMAGE. AWAITING DISPOSITION FROM ATR. 2 H 7 2 4T RT A53EU 20081103 2008 11 3 USAA920081898 4 20081015 A 2565 60592101 RESERVOIR AIRBUS A319 A319112 3930323 EU SLIDE PRESSURE LOW A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 766US 17826 2537 1378 LOG PAGE 8107178 FLT NR 1817. DCA-CLT EMERGENCY EQUIPMENT CIDS FAULT. RT EMERGENCY SLIDE PRESSURE LOW. R&R RT OFF WIN G ESCAPE SLIDE RESERVOIR PER MM 25-62-46. 2 L 7 2 4F RT A28NM 20081103 NM 2008 11 3 USAA920081901 1 20081017 A 5340 6935352Y1 STRINGER CLIP BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03055380358/002 STRINGER CLIP CRACKED AT BS 616, S4R. REPLACED STRINGER CLIP AT BS 616, S4R IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081103 WP 2008 11 3 AALA200802533 1 20080922 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP BS 148-151 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70504 49798 CORROSION FOUND ON RT CUSP DIAPHRAGM AT FORWARD CABIN STATION 148 TO 151. AREA OF DISCREPANCY IS 12 INCHES BY 14 INCHES . INSTALLED DOUBLER IN RT FORWARD CABIN AT STATION 148 TO 151 PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081103 WP 2008 11 3 AALA200802535 1 20080929 A 5340 FITTING DOUG DC9 DC982 3022082 WP BS 895 S17L DELAMINATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 33502 49739 TUL FITTINGS AT STRINGER 17 STATION 895 LT SIDE DELAMINATED WITH FUEL LEAKING BELOW FITTINGS. REPLACED BOTH FITTINGS AT KEELBEAM STATION 895 LT SIDE IN ACCORDANCE WITH SRM DRAWING 5930569. 2 L 7 2 4F A6WE 20081103 NM 2008 11 3 USAA920081954 1 20081009 A 5240 6545849169 WEB BOEING 737 7374B7 138449C NM ZONE 800 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT MAJOR REPAIR Q5 CHECK NR 03C10652003/007. CRACKED WEB ON THE AFT SERVICE DOOR AT THE 4TH STOP CUT OUT FROM THE BOTT OM. REPAIRED AFT SERVICE DOOR WEB AT THE 4TH STOP CUT OUT FROM THE BOTTOM IAW TYPICAL REPAIR 52-10-11. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081955 1 20081023 A 5311 FRAME BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT MAJOR REPAIR Q5 CHECK NR 03C20853011/007, CRACKED FRAME AT BS 500C, S20L - S21L. REPAIRED FRAME AT BS 500C, S20L - S21L IAW B737 SRM 53-00-07. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081957 1 20081022 A 5240 65458492 HOUSING BOEING 737 737301 1384611 NM ZONE 800 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT MAJOR REPAIR Q3 CHECK NR 03C11252008/001. AFT SERVICE DOOR TORQUE TUBE HOUSING CRACKED. REPLACED AFT SERVICE DOOR TORQUE TUBE HOUSING. 2 L 7 2 4F RT A16WE 20081103 SW 2008 11 3 QML2008F00015 1 20081009 A 6700 407375024101 PCU BELL 407 407 1182206 SW FAILED E QMLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 408GA 8349 53392 ON TAKEOFF, PEDAL STOP FAILED TO ENGAGE AND PEDAL STOP CAUTION 1 LIGHT ILLUMINATED. ACFT WAS APPROX 4 NM FROM AIRPORT. PERFORMED EMERGENCY PROCEDURES AND DECIDED TO FLY ACFT TO AIRPORT. NORMAL LANDING WAS MADE AND MECHANIC WAS NOTIFIED. THE PEDAL RESTRICTOR CONTROL UNIT (PRCU) WOULD NOT RELEASE DURING SLOWER SPEEDS OF 55 +- 5 KNOTS, WHICH CAUSED THE PILO T TO PULL MANUAL RELEASE. THE PEDALS THEN RETURN TO FULL RANGE OF CONTROL. TROUBLESHOOTING GUIDES IN THE BHT407MM8 CHA PTER 67. FOUND THAT THE PRCU HAD FAILED. INSTALLED NEW PRCU P/N 407-375-024-101 SN 1026. FUNCTION CHECK FOUND TO BE S ERVICEABLE. 1 G 7 1 3U O H2SW 20081103 NM 2008 11 3 AALA200802545 1 20080917 A 5730 SKIN BOEING 757 757223 1384957 NM LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 624AA 24582 CORROSION FOUND ON LT WING SKIN AT THE EMERGENCY WALKWAY. REPAIRED IN ACCORDANCE WITH ESO 90309 DATED 17 SEP 2008. 2 L 7 2 4F RT A2NM 20081103 2008 11 3 USAA920081840 4 20081009 A 2565 SAFETY WIRE AIRBUS A321 A321211 3930370 EU EVAC SLIDE BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 189UW 8736 1425 PIT - C11, SAFETY WIRE BROKEN ON BOTTOM REAR OF PACK. THE SAFETY WIRE HOLDS THE PAWL IN PLACE, HOLDING THE RETAINING PI NS OF THE SLIDE. REPLACED SLIDE WITH BROKEN PAWL SAFETY WIRE WITH A NEW SLIDE. INSTALLED BY ROUTINE JOB CARD RT AFT PA X /CREW DOOR LOBE AND OPERATIONAL CHECKS. 2 L 7 2 4F RT A28NM 20081103 EU 2008 11 3 USAA920081841 1 20080927 A 5315 D5372190202 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL - C7 - MAJOR REPAIR, CORROSION ON FLOORBEAM HARD POINT AT FR64+7 TO FR66, Y765. REPLACED FLOORBEAM AT FR64+7 TO FR6 6, Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081103 EU 2008 11 3 USAA920081842 1 20081003 A 5315 D531126002000 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL - C7 - MAJOR REPAIR, CORROSION ON FLOORBEAM IN PAX CABIN BETWEEN FR12 & FR16, Y498. REPLACED FLOORBEAM ASSEMBLY BET WEEN FR12 & FR16, Y498 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081103 SO 2008 11 3 C2XA08RI151 1 20081001 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 12142 145735 FLT 2276 - EWR - FLT CREW REPORTED RT EXIT IDENTIFIER UPPER AT EMERGENCY EXIT INOPERATIVE. MX R&R NR 5 EMERGENCY LIGHT INVERTER AND PERFORMED OPS CHECK SUCCESSFULLY. AC WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081103 NM 2008 11 3 HNA2008F00056 1 20080903 A 5311 BELTFRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 931HA 51228 132 FWD EMERGENCY DOOR AREA, BELTFRAME AT STA X254 FOUND CORRODED AND SURFACE CORROSION ON DOOR SILL. AT STA X259 BLENDED B ELTFRAME IAW SRM 53-00-16. CLEAT, THRESHOLD, STRAP AND BRACKET LOCALLY FABRICATED IAW DRAWINGS 8532075, 85320594, 85321 705, 853206070. 2 H 7 2 4T RT A13NM 20081029 EU 2008 10 29 08FDEA04577 1 20081027 A 7120 A5461121960000 MOUNT AIRBUS 300 A300F4605R 3930327 EU NR 1 ENGINE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 NR 1 ENGINE FWD ENGINE MOUNT IN SPIGOT HOLE HAS RUST. REMOVED SPIGOT FITTING IAW DWG 41A54612646; REV "B". REPAIRED D AMAGED BORE HOLE IAW SRM 54-51-81; FIG 101. CAD PLATED IAW SRM 51-21-10. PRIMED IAW SRM 51-21-10. RE-INSTALLED SPIGOT FITTING IAW DWG 41A54612646 AND SRM 51-40-00. 2 L 7 2 4F RT A35EU 20081029 NM 2008 10 29 DL757081398 1 20081021 A 5321 143N53472 FLOOR PANEL BOEING 757 757232 1384965 NM BS 635-650 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 FWD CARGO BAY BILGE FIXED FLOOR PANEL UPPER SURFACE CORRODED AT STATION 635-650 AT RBL 19. REPAERED PER ERA 470940-14 R EV ORG ON NR CARD 00063. 2 L 7 2 4F RT A2NM 20081029 WP 2008 10 29 UPS08853552 1 20080926 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV FLUSH SKIN REPAIR CUT BS 88 TO 14 BETWEEN L31L AND L27L NEEDS VALIDATION. REPAIR PREVIOUSLY ACCOMPLI SHED PER DC8 73F SRM 53-02-01 FIG 007. 2 L 7 4 4F RT 4A25 20081029 SO 2008 10 29 SWIA200820189 1 20081010 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS DAMAGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 218SW 120287 FLT 5562 - EMERGENCY EXIT SIGN ROW 6A UNINTELLIGIBLE. REPLACED SIGN ASSEMBLY. 2 L 7 2 4T RT A31SO 20081029 WP 2008 10 29 UPS08853568 1 20080929 A 5320 CUSP WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV REMOVE AND REPLACE WITH SRM REPAIR ORGINIAL N/R 534146 RIGHT CUSP MEMBRANE CRACK EXTENDING FROM STOP DRILL TO AFT OF FS 1600. INSTALLED DOUBLER AS PER SRM 51-21-01. 2 L 7 4 4F RT 4A25 20081029 WP 2008 10 29 UPS08853585 1 20080929 A 5320 CUSP WEB DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV REMOVE REPAIR AND REPLACE WITH SRM REPAIR EFN 89419971080 ORIGINAL N/R 534358 CUSP MEMBRANE CRACKED BETWEEN LIGHTENING HOLES FS 80. UPON INVESTIGATION FOUND REPAIR MISSING ONE ROW OF FASTENERS, ADDED ROW 3 RIVETS AS IAW SRM 53-02-00. FOUND TO MEET ALL REQUIREMENTS OF OF DC8 SRM 53-02-00 FIG 25. 2 L 7 4 4F RT 4A25 20081029 NM 2008 10 29 SWAA085814 1 20081027 A 3350 65C27095 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 395SW 27689 DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085815 1 20081027 A 5311 65C22908 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085816 1 20081027 A 5240 6552863516 HINGE FITTING BOEING 737 7373H4 1384600 NM L2 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND L2 DOOR LOWER HINGE FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085817 1 20081027 A 3350 6574550 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 5 DEF. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 EIAA2008102800063 1 20081027 A 5210 WEB BOEING 747 747273C 1384896 NM ZONE 800 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 L-2 DOOR LOWER HINGE FWD CUT OUT WEB FOUND CRACKED. L-2 DOOR LOWER HINGE FWD CUT OUT WEB REPAIRED PER EA 52-0061. 2 L 7 4 4F RT A20WE 20081030 EA 2008 10 30 ASOA200801194 1 20080919 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REPLACED ANGLE IAW REO 601R-53-41-059. REPLACED LEFT FS 484.00, LBL 27.0 FLOOR SUPPORT STRUCTURE CLIP IAW REO 601R-53-4 1-059. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 ASOA200801389 1 20081023 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 PAX DOOR WILL NOT OPEN. 2 L 7 2 4F RT A21EA 20081030 NM 2008 10 30 08FDEA04583 1 20081027 A 5311 70750063C FRAME BOEING 757 75723A 1384967 NM BS 1320 S4L/R DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 AFTER REMOVAL DOUBLER FROM TV MONITOR SUPPORT AT STA 1320. FOUNDED SEVERAL HOLES ON FRAME. REMOVED DAMAGE AT STA 1320 FROM STR 4L-4R IAW SRM 53-00-07. FABRICATED ZEE FRAME FROM MAE TRAVELER T8/763299. FABRICATED SPLICES PER MAE TRAVELER T8/761975. DRILLED REPAIR PARTS IAW SRM 53-00-07. TREATED AND PRIMED REPAIR PARTS IAW SRM 53-00-07 REPAIR NR 3. INST ALLED REPAIR PARTS IAW SRM 53-00-07 FIG 201 REPAIR NR 3 AT STA 1320. DO A HFEC INSPECTION EVERY 12,000 FLIGHT CYCLES AS GIVEN IN NDT PART 6,51-00-01. REPEAT THIS INSPECTION AT EVERY 12,000 FIGHT CYCLES INTERVALS, AS AN ALTERNATIVE, DO A ( DVI) INSPECTION AT 9,000 FLIGHT CYCLES INTERVALS AFTER INITIAL INSPECTION PER NOTES D53-00-07. THIS IS A CT "B' REPAIR. 2 L 7 2 4F RT A2NM 20081030 NM 2008 10 30 QXEA200801019 1 20080924 A 4940 4951070 EXCITER BOMBDR DHC8 DHC8402 1390042 NM APU FAILED A QXEA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 NM 19 421QX 2191 4149 FLIGHT 2215. APU FAILED TO START, FLAME CAME OUT OF THE TAIL ON START ATTEMPT. PLACED THE APU ON MEL 49-00-1. CLEARED O N 9/28 BY REPLACING THE APU EXCITER AND IGNITER "B". OPERATIONAL CHECKS GOOD. RETURNED TO SERVICE. (K) 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 F3LA2008102400681 1 20081024 A 5320 D53913790200 PROFILE AIRBUS A319 A319111 3930336 NM ZONE 100 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE FORWARD CARGO COMPARTMENT ON PROFILE AT FRAME 28 BETWEEN STRINGE R 38 LEFT AND 38 RIGHT. MAINTENANCE REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2. 2 L 7 2 4F RT A28NM 20081104 CE 2008 11 4 DXTA2008102903327 1 20081028 A 3240 WARNING SYSTEM CESSNA 680 680CE 2076811 CE BRAKE SYSTEM ACTIVATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 301QS 6800010 DURING T/O ROLL AT 60-70 KTS THE RED "NO TAKEOFF" AND AMBER PARKING BRAKE LOW PRESSURE CAS MSG ILLUMINATED. T/O WAS ABO RTED. 2 L 7 2 4F RC T00012WI 20081104 WP 2008 11 4 UPS08853660 1 20080923 A 5753 DOUBLER DOUG DC8 DC873F 302199F WP TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV SURVEY SEQ NO 894-W4-24 RT WING INBOARD FLAP UPPER EXT SURFACE SKIN REPAIR DOUBLER EXT SURFACE GOUGED . REMOVED AND REPLACED DOUBLER IAW DC8 SRM 57-2-05 FIG 2. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853661 1 20080923 A 5753 DOUBLER DOUG DC8 DC873F 302199F WP TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV SURVEY SEQ 894-W4-23 RT WING INBOARD FLAP UPPER EXT SURFACE SKIN REPAIR DOUBLER EXT SURFACE GOUGED IN BOARD OF BOILER PANEL AT STA XF 211. REMOVED AND REPLACED DOUBLER IAW DC-8 SRM 57-02-05 FIG 2. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853668 1 20080921 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN89419971256 ORIG NR 535436 PREVIOUS REPAIR DOUBLER AND TRIPLER ON LONG 33L ARE CORRODED STA 1185-1295. REMOVED AND INSTALLED REPAIR DOUBLER IAW ROD SKETCH 97-05-06-006 AND SRM 51-30-01-00. ACTUAL REPAIR FOUND TO BE AT 33L STA 1185-1200. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 AALA200802396 1 20080920 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9302B 49528 SFO EMERGENCY LIGHTS AT TAILCONE WILL NOT TURN OFF. REPLACED BATTERY PACK AT AFT LAVATORY FOR EMERGENCY LIGHTS AT TAILC ONE. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081104 EA 2008 11 4 COMA0860425 1 20081015 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 436CA 7482 DURING HMV4 LT WING PLANK INSPECTION NDT FOUND CRACK INDICATION AT FUEL DRAIN MOUNT HOLES WS 12 AND WS 60. DAMAGE REMOV ED BY OVERSIZING HOLES AND INSTALLING FREEZE PLUGS PER EA 10-5721-02374. 2 L 7 2 4F RT A21EA 20081104 WP 2008 11 4 AALA200802577 1 20080923 A 5311 9919603 FRAME DOUG DC9 DC983 3022083 WP BS 1231 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 TUL CORROSION FOUND ON BELL FRAME AT STATION 1231. AREA OF DISCREPANCY IS 2 INCHES BY 1 INCH. INSTALLED DOUBLER IN ACC ORDANCE WITH SRM 51-70-05. 2 L 7 2 4F RT A6WE 20081104 NM 2008 11 4 AALA200802581 1 20080905 A 5522 SKIN BOEING 767 767323 1385205 NM LT ELEVATOR DELAMINATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 344AN 33083 OTBD ELEVATOR LT UPPER SURFACE HAS DELAMINATION AT ELEVATOR STATION 151.499. APPROXIMATELY 16 INCHES FROM EDGE AND 1.5 INCHES INBD OF RIB. ACCOMPLISHED REPAIR IAW SRM 51-70-04 AND MRB 767-3289. 2 L 7 2 4F RT A1NM 20081104 SO 2008 11 4 C2XA08TY119 1 20081006 A 7120 MOUNT EMB 145 EMB145LR 3260212 SO ENGINE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 21805 145180 AC CURRENTLY INA C-CHECK STATUS AND THE NR 2 ENGINE INLET MOUNTING FLANGE BOLT HOLES HAD SEVERAL HOLE`S THAT WERE FOUND CORRODED. MAINT REPAIRED THE INLET BOLTHOLES IAW EC5420-01161. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. (K) 2 L 7 2 4T RT T00011AT 20081104 NM 2008 11 4 WX0A070235 1 20080919 A 3350 AD4002 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 892GA 49826 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSP, MAINT REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOUL D NOT TEST. MAINT REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERAT IONAL CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. (K) 2 L 7 2 4F RT 20081104 SO 2008 11 4 C2XA08TY121 1 20081007 A 5751 PE64042K6028027 BUSHING EMB 145 EMB145LR 3260212 SO LT AILERON WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 21805 145180 ACFT CURRENTLY IN A C-CHECK STATUS WAS FOUND WITH THE LT AILERON PCA BRACKET WITH MIGRATING BUSHINGS IAW EC5740-01152 AN D WILL BE RELEASED AT THE END OF THE CHECK. (K) 2 L 7 2 4T RT T00011AT 20081104 SO 2008 11 4 C2XA08TY122 1 20081007 A 5751 14564009410SD FITTING EMB 145 EMB145LR 3260212 SO RT AILERON WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13978 145180 RT AILERON PCA FITTING OTBD LUG (ON AILERON) MISSING HAT BUSHING. REMOVED AND REPLACED FITTING IAW EC5750-01177, REV B. AIRCRAFT CURRENTLY IN C-CHECK. (K) 2 L 7 2 4T RT T00011AT 20081104 CE 2008 11 4 DXTA200803296 1 20081005 A 3260 WARNING LIGHT BEECH MU300 400A 1155402 CE MLG INOPERATIVE E DXTA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 101QS RK484 ON LANDING APPROACH, WE DID NOT GET A LT GEAR SAFE INDICATION. (K) 2 H 7 2 4F RT A16SW 20081104 CE 2008 11 4 DXTA200803295 1 20081005 A 2720 CONTROL SYSTEM CESSNA 750 750 2076810 CE RUDDER FAILED E DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 944QS 7500144 STANDBY RUDDER SYSTEM FAIL IN FLIGHT. (K) 2 L 7 2 4J RT T00007WI 20081104 WP 2008 11 4 AALA200802588 1 20080926 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1485 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7538A 49992 CRACK IN CANTED FRAME WEB AT AFT ACCESSORY AT STATION 1485. CRACK LENGTH IS .5 INCH. INSTALLED DOUBLER IN ACCORDANCE W ITH AARD 53-10-00-32. 2 L 7 2 4F A6WE 20081104 WP 2008 11 4 AALA200802587 1 20080925 A 5311 9911843516 FRAME DOUG DC9 DC982 3022082 WP BS 1510 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7538A 49992 CRACK IN CANTED FRAME AT LONGERON 23 RT AT STATION 1510. CRACK LENGTH IS 1 INCH. INSTALLED DOUBLER IN ACCORDANCE WITH ESO 80559 DATED 25 SEP 2008. 2 L 7 2 4F A6WE 20081104 NM 2008 11 4 USAA EMB08019 1 20081027 A 3243 389575001 SHUTOFF VALVE EMB ERJ190 ERJ190100IGW 3260408 NM BRAKE SYSTEM MALFUNCTIONED A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 962UW 792 19000188 FLIGHT 948, SAV-CLT - WHILE ON APPROACH TO CLT, DESCENDING TO 2000 FEET EICAS DISPLAYED BOTH LEFT AND RIGHT BRAKE FAULTS . THE CREW BROKE OF THE APPROACH, REDUCED THE BRAKING AUTHORITY TO HALF AND REQUESTED THE LONGEST RUNWAY AND EMERGENCY EQUIPMENT DEPLOYED. THE CAPTAIN REPORTED THE MESSAGES WENT AWAY ON SECOND APPROACH AND THE FLIGHT LANDED WITHOUT FURTHE R INCIDENTS. MAINTENANCE ACCOMPLISHED FIM TASKS AND FOUND NO FAULTS. ON FIRST FLIGHT OUT OF CLT THE EICAS DISPLAYED LE FT AND RIGHT BRAKE FAULT IN AIR AT 1500 FEET ABOVE GROUND LEVEL. GO AROUND ON GEAR DOWN THE BRAKE FAULT CLEARED AND THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE SHUT OFF VALVE. FOR TROUBLESHOOTING BRAKE CONTROL VALVE AND 2 L 7 2 4F RT A57NM 20081104 SO 2008 11 4 C2XA08RI163 1 20081028 A 3230 355022002MOD2 CONTROL UNIT EMB 145 EMB145LR 3260212 SO LANDING GEAR INOPERATIVE A C2XA K NONE J WARNING INDICATION AP APPROACH 1 SW 27 15986 20074 145254 FLIGHT 2866 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE WHEN GEAR IS IN TRANSIT DOWN. EWR MX REMO VED AND REPLACED THE LANDING GEAR ELECTRONIC CONTROL UNIT AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS AP PROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081104 EA 2008 11 4 QXEA2008103101047 1 20080923 A 5730 SKIN CNDAIR CL600 CL6002C10 1390015 EA WING DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 611QX 10041 PDX - C4 - PERMANENT REPAIR FOR DENT TO RT FIXED LEADING EDGE SKIN AT SS156.28. CUT OUT DAMAGE REF REO 670-57-41-154/3. HFEC IAW CRJ 700 NDTM PART 1, 51-20-006 AT CUTOUT, NO CRACKS NOTED. FABRICATED REPAIR DOUBLER FROM .063" 2024T3 AND R EPAIR SHIM FROM .032 2024T3 REF REO 670-57-41-154/3. INSTALLED REPAIR REF REO 670-57-41-154/3. 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 MASA2008103000757 1 20081030 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002D24 1390016 EA COCKPIT MALFUNCTIONED A MASA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 07 930LR 15030 ASH FLT 2779 MEM-PHX. PASSENGER DOOR WARNING MESSAGE. MX RESET THE SYSTEM, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081105 WP 2008 11 5 AALA200802555 1 20080924 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 1474 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 SKIN CRACKED AT CANTED FRAME AT STATION 1474. INSTALLED DOUBLER IN ACCORDANCE WITH SRM 53-01-00. 2 L 7 2 4F RT A6WE 20081105 WP 2008 11 5 AALA200802647 1 20081003 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION ON CUSP ANGLE TANG AT STATION 168. AREA OF DISCREPANCY IS 10 INCHES BY 5 INCHES. REPAIRED CUSP ANGLE IN ACCO RDANCE WITH ESO 80559 DATED 03 OCTOBER 2008. 2 L 7 2 4F RT A6WE 20081105 WP 2008 11 5 AALA20802648 1 20081001 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 973TW 53623 LGA - EMERGENCY LIGHT AT OVERHEAD SEAT ROWS 19 TO 24 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT OVERHEA D SEAT ROWS 19 TO 24. SYSTEM GROUND CHECKED NORMAL OPERATON. 2 L 7 2 4F RT A6WE 20081105 WP 2008 11 5 AALA200802642 1 20081002 A 5510 3912033512 HINGE FITTING DOUG DC9 DC983 3022083 WP HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON HORIZONTAL STABILIZER RIGHT OUTBOARD HINGE PLATE LUG NUMBER 4. AREA OF DISCREPANCY 2 INCHES BY 2 INC HES. REPLACED RIGHT OUTBOARD LUG IN ACCORDANCE WITH WORKCARD 55 94 05. 2 L 7 2 4F RT A6WE 20081105 SO 2008 11 5 C2XA08RI162 1 20081027 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14542 23249 2964 145547 FLIGHT 2747 - EWR - FLIGHT CREW REPORTED 2 EMERGENCY LIGHTS WOULD NOT STAY ILLUMINATED. EWR MX REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081105 NM 2008 11 5 HNAA0800311 1 20081021 A 2760 H188C INDICATOR DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTIONED A HNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 07 807EX 29620 1114 292 DURING TAKEOFF ROLL, POWERED FLIGHT CONTROL SYSTEM INDICATOR SHOWED THE LEFT WING SPOILERS NOT RETRACTED. TAKEOFF WAS A BORTED BELOW 30 KTS. MAINTENANCE CHANGED THE PFCS INDICATOR. OPS CHECKS WERE GOOD AND AIRCRAFT WAS THEN RELEASED BACK INTO SERVICE. 2 H 7 2 4T RT A13NM 20081105 WP 2008 11 5 UPS08853774 1 20081008 A 5522 SKIN DOUG DC8 DC871F 302199D WP ELEVATOR MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV SURVEY SEQ NO 702-S2-11 RT ELEV TIP EXT DOUBLER AT 312.500 FASTENER SPACING AND EDGE DISTANCE OUT OF LIMIT REF STEP 1, 2 APPEN-D. VERIFIED THE REPAIR IS IN THE INTENT AND GUIDELINES IAW DC8 SRM 51-1-21, TR 51-134 FIG 33. 2 L 7 4 4F RT 4A25 20081105 WP 2008 11 5 UPS08853777 1 20081002 A 5511 RIB DOUG DC8 DC871F 302199D WP HORIZ STAB MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATION AND DISPOSITION EFN 70219911047 ORIGINAL NR 288533 RIB CRACKED AT LOWER AFT END AT XFS 53. EVALUATED REPAIR FOUND ADDED FASTENERS TO BE INCORRECT, REPLACED FASTENERS TO CONFORM WITH DC8 SRM 55-02-00-0 PG 2 ITE M 6 USING HL326 HI-LOKS. 2 L 7 4 4F RT 4A25 20081105 WP 2008 11 5 UPS08853786 1 20081020 A 5753 DOUBLER DOUG DC8 DC871F 302199D WP TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV LT WING OUTBOARD FLAP TOP SKIN HAS A REPAIR DOUBLER THAT IS GOUGED. REMOVED, FABRICATED AND INSTALLE D NEW DOUBLER IAW DC8 SRM 57-2-0 TR57- 84. 2 L 7 4 4F RT 4A25 20081105 EA 2008 11 5 QXEA2008103101040 1 20080923 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 611QX 10041 PDX - C4 - RT IN FLOOR SEAT TRACK AT STN 353.0 IS PITTED. BLENDED OUT PITTING FROM TRACK AND FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK IAW CRJ 700 AMM 53--00-49-000-801-A02 PARA 2A-C (1) AND D(2)(A). INSTALLED NEW TRACK IAW CRJ 700 A MM 53-00-49-400-801-A02 PARA 6A-C, D (2)(A) AND E (1). 2 L 7 2 4F RT A21EA 20081105 NM 2008 11 5 SWAA085909 1 20081029 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085884 1 20081029 A 5310 6546529 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND FWD CARGO DOOR CUTOUT FWD FRAME CRACKED AT BS 440, STR 23R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085885 1 20081029 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085886 1 20081029 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 24L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085887 1 20081029 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 20L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085890 1 20081029 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085871 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085872 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085873 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085874 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081103 2008 11 3 C2XA08RI152 4 20081002 A 3417 ADC EMB 145 EMB145LR 3260212 SO NR 1 MALFUNCTIONED A C2XA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 27 13958 145085 FLT 2199 - BNA - FLT CREW REPORTED AIR DATA COMPUTER NR 1 FAILURE AND TOTAL FUEL DASHING OUT. FLT CREW PERFORMED AIR RE TURN ANEVENTFULLY. FLT CREW PROCEEDED WITH SYSTEM RESET AND RESET WAS SUCCESSFUL. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081104 WP 2008 11 4 UPS08853677 1 20081005 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV RT LWR LEADING EDGE DOUBLER STA XFS 524 NEEDS VALIDATION. DOES NOT MEET CRITERIA APPENDIX H STEP 5. 894-W4-19 AREA PREVIOUSLY REPAIRED & AND ADDED EXTRA ROW OF FASTENERS IAW DC8 SRM 57-2-1 TR 57-95 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 20081104 NM 2008 11 4 UPS08M53758 1 20081027 A 5730 ARB7766511 FAIRING DOUG MD11 MD11F 3023600 NM LT WINGLET DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP 48417 INSPECTION TYPE:N/A LT WINGLET UPPER T/E FAIRING DAMAGED. REPAIRED IAW EO MD11-5730-90798-B. 2 L 7 3 4F RT A22WE 20081104 EU 2008 11 4 ASOA200801410 1 20081028 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 EMERGENCY LIGHTS CAME ON BY THEMSELF AND WILL NOT TURN OFF. 2 H 7 2 4T RT 20081104 EA 2008 11 4 ASOA200801412 1 20081029 A 5210 MECHANISM CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FAULTY A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 PASSENGER AIRSTAIR DOOR LATCHING MECHANISM IS EXTREMELY HARD TO ACTUATE. 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 ASOA200801413 1 20081029 A 3350 SIGN CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 867AS 7463 ROW 8 OVERHEAD CEILING LIGHT EXIT SIGN FACING FWD INOP. FLT 5400 CX. 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 ASOA200801415 1 20081030 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 CORROSION ON 280 FRAME AT LBL 9. REMOVED AND REPLACED FRAME. REMOVED MINOR CORROSION ON FRAME. BEGAN REMOVAL OF 280 B EAM LT PER SB670BA-53-026. 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 ASOA200801418 1 20081030 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 CORROSION ON RT 280 WEB. REMOVED AND REPLACED RT 280 WEB PER CRJ 700 SRM 51-42-06 AND 51-42-13. REMOVED AND REPLACED 4 EA ATTACH ANGLES CUT RT 280 WEB. CC670-34117-5 WAS PRE-FAB REMAINING ATTACH ANGLES IAW CRJ 700 SRM DWG CC670-34-100 AN D 51-24-16. COMPLIED WITH FP 1 OF FABBED PARTS IAW NDTM 51-20-08. FABRICATED RT SPLICE PLATE (P/N CC670-34251-2 ) IAW CRJ 700 SRM 51-24-16 AND 700 SRM 53-11-10. INSTALLING RT WEB AND ATTACH ANGLES PER CRJ 700 SRM 51-42-06 AND 51-42-13. S UPPLEMENTAL-SDR CLOSED 11/17/2008. 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 QXEA200800782 1 20080719 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 610QX 10033 C4 CHECK - LT FLOOR SEAT RAIL IS CORRODED, PITTED AND GOUGED AT FS 418.0 TO 420.0. BLENDED TO REMOVE SEAT RAIL CORROSIO N PITTING AND GOUGE IAW REO 670-53-00-013. PERFORMED FPI NDTM CHAP 8 NO CRACKS NOTED. ETCHED, ALODINED AREAS IAW REO 67 0-53-00-013. (K) 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 QXEA200800779 1 20080719 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 610QX 10033 C4 CHECK - LT FLOOR SEAT RAIL IS GOUGED AT FS 454.0 TO 458.0 BLENDED TO REMOVE SEAT RAIL GOUGE IAW REO 670-53-00-013. MA X MATERIAL REMOVED FOR DIMENSION T IS .009 INCH, DIMENSION U IS .010 INCH, NOTED. ETCHED, ALODINED AREAS IAW REO 670-53- 00-013. (K) 2 L 7 2 4F RT A21EA 20081030 NM 2008 10 30 KCSA081497 1 20080927 A 5730 SKIN PANEL BOEING 747 747122 1384872 NM RT WING BULGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 RT WING UPPER T/E PANEL HAS BULGE ABOVE REAR SPAR AT WBL 241. (K) 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 DHL2008F00035 1 20080912 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN AT BS 700 BETWEEN STRINGER 16R AND 17R FRAME WITH DENT. REPAIRED FUSELAGE FRAME SECTION AT BS 7 00 BETWEEN STRINGER 16 AND 17 RT SIDE DUE TO DENT IAW SRM 51-40-3, FIG 1. (K) 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 DHL2008F00036 1 20080916 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN AT BS 720B STRINGER 13L AND 14L FRAME WITH DOUBLE HOLES. REPAIRED FUSELAGE FRAME SECTION AT BS 720B BETWEEN STRINGER 11 AND 14 LEFT SIDE DUE TO DOUBLE HOLES IAW SRM 53-10-4, FIG 1 DETAIL 1. (K) 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 DHL2008F00037 1 20080917 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN AT BS 660 BETWEEN STRINGER 16R AND 17R FRAME WITH DENT. REPAIRED FUSELAGE FRAME SECTION AT BS 6 60 BETWEEN STRINGER 16 AND 17 RT SIDE DUE TO DENT IAW SRM 51-40-3, FIG 1. (K) 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 DHL2008F00038 1 20080912 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN AT BS 720B STRINGER 8R FRAME WITH DOUBLE HOLES. REPAIRED FUSELAGE FRAME SECTION AT BS 720B BETW EEN STRINGER 7 AND 9, RT SIDE, DUE TO DOUBLE HOLES IAW SRM 53-10-4. (K) 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 DHL2008F00040 1 20080913 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN AT BS 460 BETWEEN STRINGER 16R AND 17R FRAME WITH DENT. REPAIRED FUSELAGE FRAME SECTION AT BS 4 60 BETWEEN STRINGER 16 AND 17 RT SIDE, DUE TO DENT IAW SRM 51-40-3, FIG 1. (K) 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 DHL2008F00041 1 20080912 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN AT BS 680 BETWEEN STRINGER 16R AND 17R FRAME WITH DENT. REPAIRED FUSELAGE FRAME SECTION AT BS 680 BETWEEN STRINGER 16 AND 17 RIGHT SIDE, DUE TO DENT IAW SRM 51-40-3, FIG 1. (K) 2 L 7 3 4F A3WE 20081030 NE 2008 10 30 DL75E081419 2 20081024 A 7210 ENGINE BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE NR 2 SHUTDOWN A DALA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 27 706TW 25962 28165 728754 RT ENGINE IFSD. REMOVED AND REPLACED MAIN AND ANGLE GEAR BOXES. REMOVED AND REINSTALLED IDG LUBE PUMP STARTER AND VALV E HYD PUMP PER PA W 2037 EMM, 475658. PERFORMED ENGINE RUN PER MM CHECKS NORM OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081030 EA 2008 10 30 A6WA200840589 1 20080914 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA NLG & MLG UNKNOWN A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 443AW 7781 ON GEAR RETRACTION, GEAR DISAGREE WARNING MESSAGE. SUSPECT NOSE GEAR FAULT. LANDED AT 41,000 LBS AND BRAKING WAS NORMAL. SERVICED MLG AND NLG IAW AMM 12-12-32, PERFORMED GEAR EXTENSION AND RETRACTION CHECK AS REQUIRED. OPS CHECK GOOD. (K) 2 L 7 2 4F RT A21EA 20081030 NM 2008 10 30 DL757081423 1 20081014 A 5322 1440N200210 SHEAR TIE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE BS 1701 S28-29R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 728754 SHEAR TIE IS CORRODED AT BS 1701 BETWEEN STRINGER 29R AND 28R. OUT OF LIMITS, REMOVED AND FABRICATED AND INSTALLED NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081030 NM 2008 10 30 DL757081424 1 20081019 A 5320 143N537027 FLOOR SUPPORT BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE BS 701 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 728754 CORROSION IN AND AROUND FASTENER HOLE AT BS 701 RBL 16 FLOOR STRINGER. CORROSION WAS OUT OF LIMITS. REPAIRED BY SPLICI NG IN NEW STRINGER FROM BS 670 TO FACTORY SPLICE AT BS 705 IAW AMM 53-87-01-801. 2 L 7 2 4F 4 F RT A2NM E17NE 20081030 NM 2008 10 30 USAASB08102 1 20081027 A 4930 36177501 FUEL CONTROL BOEING 737 7374B7 138449C NM APU FAULTY A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 434US 24556 EN ROUTE FROM ORD TO PHL, DURING CRUISE, THE APU GENERATOR FELL OFF LINE. CREW WAS UNABLE TO GET IT BACK ON LINE. SINC E THE NR 1 ENGINE GENERATOR WAS ALREADY ON MEL, THE FLIGHT DIVERTED TO PIT WHERE THE FLIGHT LANDED WITHOUT FURTHER INCID ENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE APU FUEL CONTROL UNIT PER MM 49-31-11-4. APU OPE RATIONAL TEST GOOD PER MM 49-11-00. AS FOR THE NR 1 ENGINE GENERATOR, MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE GCU PER MM 24-21-84-1. OPERATIONAL TEST GOOD. 2 L 7 2 4F RT A16WE 20081030 EA 2008 10 30 S9BA2008029 2 20081022 A 7250 P3015000 TURBINE DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA RT ENGINE DAMAGED A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 562CP 3316 562 PCE40031 RIGHT ENGINE MAKES NOISE WHEN PROP MOVED BY HAND. REMOVED AND REPLACED RIGHT ENGINE AND PROPELLER AS A QEC ASSEMBLY. S PLIT ENGINE AT C-FLANGE AND FOUND POWER TURBINE RUB. 1 H 7 2 3T 4 T RT A9EA E4EA 20081030 NM 2008 10 30 EIAA2008102800065 1 20081027 A 3350 900835AB BATTERY PACK BOEING 747 747273C 1384896 NM EMERGENCY LIGHTS NO TEST A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 470EV 20653 UPPER DECK EMERGENCY LIGHT TEST FOUND DOOR EXIT SIGN INOP. REPLACED BATTERY PACK ASSY AND OPS CHECK NORMAL PER 33-51-00 . 2 L 7 4 4F RT A20WE 20081030 CE 2008 10 30 GUUA10130802 1 20081013 A 5210 1294000321 DOOR BEECH 1900 1900D 1154162 CE CABIN DOOR MALFUNCTIONED A GUUA K NONE O OTHER TX TAXI/GRND HDL 1 SO 29 38537 UE158 FLIGHT 9154 - MCO/MIA - PILOT REPORTED CHECK FORWARD CABIN DOOR FOR PROPER OPERATION APPEARS TO JAM. INSPECTED FORWARD CABIN DOOR. NO DEFECTS NOTED. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081030 NM 2008 10 30 USAABB08162 1 20081023 A 2740 6224591511 COMPUTER BOEING 757 757225 1384959 NM HORIZ STAB MALFUNCTIONED A USAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 19 921UW 22201 FLT 1752. THE CREW REPORTED THAT THE HORIZONTAL STABILIZER TRIM RAN TO FULL NOSE UP UNCOMMANDED, RESULTING IN DIFFICULT Y IN KEEPING THE NOSE OF THE AIRCRAFT DOWN DURING LANDING ROLL OUT. MAINTENANCE REPLACED THE RIGHT FLT CONTROL COMPUTER (FCC). CAT SYSTEM TESTED SATISFACTORY. 2 L 7 2 4F RT A2NM 20081030 NM 2008 10 30 QXEA2008102901097 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4 - RT INBD SEAT TRACK HAS CHAFING FROM APPROX STA X310-X345 IN CHANNEL AND TOP. REMOVED CHAFING FROM TRACK AND FOUND TO BE WITHIN LIMITS IAW RD8/4-53-884. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01. NO CRACKS NOTED. APPLIED E TCH AND ALODINE IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 QXEA2008102901098 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 RT INBD SEAT TRACK HAS CHAFING AND SCRATCHES ALONG TOP AND IN CHANNEL FROM APPROX STA X390 - X407. BLENDED CORROSION AN D FOUND WITHIN LIMITS IAW RD8/4-53-884. HFEC INSPECTED IAW 1-84-7A PART 6, 51-00-02, NO CRACKS NOTED. APPLIED ETCH AND ALODINE IAW RD 8/4-53-884. 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 QXEA2008102901101 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX -C4- LT INBD SEAT TRACK HAS CHAFING AND SCRATCHES ALONG CHANNEL AND TOP FROM APPROX STA X390 - X406. BLENDED OUT CH AFE AND SCRATCHES AND FOUND TO BE WITHIN LIMITS PER RD8/4-53-884. HFEC INSPECTED IAW Q400 NDTM PART 6, 51-00-01, NO CRA CKS NOTED. ETCHED AND ALODINED IAW RD 8/4-53-884. 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 DL757081433 1 20081014 A 5330 143N34714 SKIN BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 630 BL 0 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 727893 CORROSION AFTER REMOVAL OF ANTENNA, FOUND SKIN CORROSION AT BS 630 BL 0. REMOVED CORROSION AND REPAIRED IAW ATS ER 8-33 28, DELTA ER/A 465407-14 DATED 24 OCT 2008. 2 L 7 2 4F 4 F RT A2NM E24NE 20081030 NM 2008 10 30 USAASB08100 1 20081025 A 2410 CSD BOEING 737 7374B7 138449C NM NR 2 ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 435US 24557 SHORTLY AFTER TAKEOFF FROM PIT, EN ROUTE TO FLL, THE NR 2 ENGINE GENERATOR CSD HIGH OIL TEMPERATURE LIGHT ILLUMINATED AN D THE LOW OIL PRESSURE LIGHT WAS FLASHING. CREW DISCONNECTED CSD PER QUICK REFERENCE HANDBOOK PROCEDURES AND BROUGHT AP U ON LINE. APU THEN FAILED AT ALTITUDE AND FAILED TO RESTART. DUE TO SINGLE POWER SOURCE, FLIGHT DIVERTED TO CLT AND LA NDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE STARTED APU SEVERAL TIMES AND NOTED NO FAULTS OR HISTORY FOR PAST 30 DAYS. AS FOR THE NR 2 ENGINE CSD AND GENERATOR, MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE C SD AND GENERATOR PER MM 24-11-11 AND 24-21-11. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A16WE 20081030 NE 2008 10 30 DLM90081435 2 20081025 A 7200 ENGINE DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 2 BIRD INGESTION A DALA C ABORTED TAKEOFF C J F.O.D. WARNING INDICATION TO TAKEOFF 1 SO 27 904DA 53384 20025 HIT BIRD AT ABOUT 135 KTS. HIGH SPEED ABORT ACCOMPLISHED AND PARKED WITH HOT BRAKES. RT ENGINE FLUCTUATED AND HAD NOTI CABLE POWER LOSS WITH THE BIRD STRIKE. BRAKE TEMP REACHED 650. REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F RT A6WE E40NE 20081030 NM 2008 10 30 EIAA2008102800072 1 20081027 A 5320 FLOOR SUPPORT BOEING 747 747273C 1384896 NM CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 BULK CARGO STA 2025 LBL25 FLOOR SUPPORT ANGLE CRACKED. FLOOR SUPPORT REMOVED. NEW SUPPORT FABRICATED. HEAT TREATED, A LODINED AND PRIMED, AREA NDTD. NO CRACKS FOUND, INSTALLED REPAIR PER SRM 51-30-02. 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 DLM88081437 1 20081022 A 5310 5912494 DOOR FRAME DOUG MD88 MD88 3023688 NM CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 929DL 49716 20025 C1 CARGO JAMB WAS FOUND CORRODED BEYOND LIMITS AND REPAIRED PER SRM 53-05D FIG 804. 2 L 7 2 4F RT A6WE 20081029 NM 2008 10 29 08FDEA04556 1 20081026 A 5311 65163165 FRAME BOEING 727 727227 1384078 NM ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 491FE 21529 FRAME AT STA 344 AND STR 5L CONTACTING 9G BULKHEAD. TRIMMED OUT FRAME AND FOUND OUT OF LIMITS IAW SRM 53-30-1 FIG 1. F ABRICATED REPAIR IAW SRM 53-10-2 FIG 3 AND 53-10-4 FIG 2. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR A T FRAME STA 344 STR 5L IAW SRM 53-10-4 FIG 2. 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 08FDEA04558 1 20081026 A 5240 65216386 FRAME BOEING 727 727227 1384078 NM ZONE 800 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 491FE 21529 E/E COMPT DOOR CRACKED AT AFT FRAME. REMOVED INNER SKIN AND CRACKED FRAME, FABRICATED NEW FRAME. INSTALLED NEW FRAME A ND SKIN IAW SRM 51-20-1, 52-40-1 FIG 2 AND 51-30-2. 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 08FDEA04559 1 20081027 A 5340 69455141 STRINGER CLIP BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 FWD PIT BS 560 STR 27R STRINGER CLIP CORRODED. REMOVED DAMAGED STRINGER CLIP, AND REPLACED IAW SRM 51-30-2. DWG 65-5610 0. THIS IS CLASSIFIED AS A MAJOR REPAIR REF GMM 6-2-100 PG 2-3. 2 L 7 3 4F A3WE 20081029 EA 2008 10 29 ASOA200801214 1 20080922 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED AND REPLACED CREW ESCAPE HATCH OUTER HANDLE IAW CRJ 200 SRM 51-42-06. REQUIRES PAINT. PAINTED REPAIR IAW CRJ S RM 51-25-01. REQUIRES LEAK CHECK. LEAK CHECK GOOD IAW CRJ 200 MM 21-32-00-863-801. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081029 WP 2008 10 29 08FDEA04561 1 20081027 A 5350 AKC70031 FRAME DOUG MD10 MD1010F 3022112 WP TAILCONE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 TAIL CONE RIGHT FRAME HAS A CRACK WITH A PREVIOUS STOP DRILL HOLE AT STA 2199 AT THE UPPER LONGERON. FORMED ANGLE PER S RM 53-30-00. FABBED, LOCATED, & DRILLED HOLES PER SRM 53-30-00. ALODINED & PRIMED PER SRM 51-21-01. INSTALLED PER SRM 51-35-01. 2 L 7 3 4F RT A22WE 20081029 EU 2008 10 29 08FDEA04564 1 20081027 A 5321 B532706000120 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 FLOOR PANEL 242 QJ IS CRACKED THROUGH THE UPPER SURFACE. FABBED NEW PANEL 242 QJ USING THE OLD PANEL AS A TEMPLATE. L OCATED & COUNTER BORED THE HOLES; POTTED; CURED & SANDED THE EDGES. POTTED & CURED THE INSERTS. PART MARKED & APPL IED NON-SKID TAPE IAW DWG SRZ 25-005. 2 L 7 2 4F RT A35EU 20081029 EU 2008 10 29 08FDEA04566 1 20081027 A 5321 B5327061300200 FLOORBOARD AIRBUS 300 A300F4605R 3930327 EU ZONE 200 BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 MAIN CABIN FLOOR BOARD 241 HK IS BROKEN. FABBED NEW FLOOR PANEL 241 HK BY USING THE OLD PANEL AS A TEMPLATE. LOCATED & COUNTER BORED HILES. POTTED, CURED & SANDED THE EDGES. POTTED & CURED INSERTS. PART MARKED & APPLIED THE NON-SKID T APE IAW DWG SRZ 25-005. 2 L 7 2 4F RT A35EU 20081029 WP 2008 10 29 08FDEA04567 1 20081027 A 5347 601096418 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 373FE 46611 MCD SEAT TRACK AT RBL 28 STA 755 IS GOUGED REMOVED AND REINSTALLED 3 FLOOR PANELS FOR ACCESS. REMOVED AND REPLACED SEAT TRACK AT STA 725 THROUGH 850 RBL 28 WITH SPLICES AND FABRICATED TRACK AND SPLICES ALL IAW AMM 53-21-08-2, SRM 51-31-01, SRM 53-70-00 FIG 5 AND MAE TRAVELERS T8/763383 AND T8/763382. MAJOR REPAIR RII. 2 L 7 3 4F RT A22WE 20081029 WP 2008 10 29 08FDEA04569 1 20081027 A 5347 601096418 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 373FE 46611 MCD SEAT TRACK AT RBL 46 STA 795 IS GOUGED REMOVED AND REPLACED SEAT TRACK AT STA 765 THROUGH 819 AT RBL 46 IAW SRM IAW SRM 51-31-01, SRM 53-70-00 FIG 5 AND MAE TRAVELER T8/763465. MAJOR REPAIR RII. 2 L 7 3 4F RT A22WE 20081029 EU 2008 10 29 08FDEA04571 1 20081027 A 5321 B5327061800200 FLOOR PANEL AIRBUS 300 A300F4605R 3930327 EU FUSELAGE BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 FLOOR PANEL 242 SF IS BROKEN. LOCATED & COUNTER BORED PANEL. POTTED, CURED & SANDED THE EDGES. POTTED & CURED INSER TS. PART MARKED & APPLIED THE NON-SKID TAPE IAW DWG SRZ 25-005. 2 L 7 2 4F RT A35EU 20081029 NM 2008 10 29 08FDEA04494 1 20081023 A 5744 ARC0503503 HINGE BRACKET DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 LEFT WING, OUTBOARD FLAP OUTBOARD FORWARD HINGE AFT LOWER ATTACH OUTBOARD HOLE FORWARD MATING SURFACE FOUND WITH CORRO SION. CORROSION REPAIRED IAW EA 1-5750-122600. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 08FDEA04496 1 20081023 A 5313 A5A70301 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 CENTER CARGO, BETWEEN LT STA 5-32 TO 5-53 LONGERON 46 FOUND CORRODED. REPAIR CARRIED OUT IAW EA 1-5310-122603. CORROSI ON REMOVED AND FOUND EXCEED LIMITS IAW SRM 53-00-01. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081029 NM 2008 10 29 08FDEA04497 1 20081023 A 5340 69455141 STRINGER CLIP BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FWD PIT BS 620 STR 27R STRINGER CLIP CORRODED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2. THIS IS CLASSIFIED A S A MAJOR REPAIR IAW GMM 6-2-100. 2 L 7 3 4F A3WE 20081029 EU 2008 10 29 2008UALA06247 1 20081022 A 3530 89151114 OXYGEN BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 410UA 463 THE O2 BOTTLE LOW AT FIRST CLASS LOCATION. REPLACED O2. 2 L 7 2 4F 4 F RT A28NM E40NE 20081029 NM 2008 10 29 2008UALA06252 1 20081022 A 3350 BPS73 BATTERY PACK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 311UA 23672 EEL LIGHTS OUT FROM ROW 15 BACK. SUSPECT FAULTY POWER STRIP AND POWER PACK. REPLACED POWER STRIP AND BATTERY PACK OP C HECKED GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081029 NM 2008 10 29 DL757081404 1 20081014 A 5320 WEB BOEING 757 757232 1384965 NM BS 1510 LBL 12 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 CRACK FOUND ON WEB DURING REMOVAL OF PAINT B/S 1520 LBL 12 COMMON TO Z STRINGER. REPAIRED ON CUST CARD 00126. 2 L 7 2 4F RT A2NM 20081029 NM 2008 10 29 CALA0801006 1 20081023 A 3350 D71702030 CHARGER BOEING 737 737724 13844BY NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13750 28941 THE EMERGENCY LIGHTS COME ON IN THE ARM POSITION, ALSO THE EMERGENCY CHARGER CIRCUIT BREAKER POPPED. THIS IS THE SECOND TIME THE CIRCUIT BREAKER POPPED, FOUND BATTERY POWER SUPPLY M1675 WITH ELECTRICAL ODOR. REMOVED AND REPLACED M1675, M1 674 AND BATTERY PACKS. OPERATIONAL CHECKS OK PER B737 AMM 33-51-06-960-806 /805. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 CALA0801007 1 20081022 A 5312 65C37590 BULKHEAD BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 59630 27534 STATION 178 BULKHEAD INSPECTION: REMOVED RT, LT SIDE WEBS AND CENTER WEB FOR INSPECTION REF EA 5310-03040 WHERE CRACKS WERE FOUND. INTERIM REPAIR COMPLETED AT BODY STATION 178 BULKHEAD PER ECRA 5310-04858 AND INITIATED A DIP WHICH READS A CCOMPLISH A PERMANENT REPAIR WITHIN 24 MONTHS FROM 21-OCT-08. PLANNING TO CONTACT ENGINEERING AFTER 21-AUG-10 BUT BEFOR E 21-SEP-10 FOR PERMANENT REPAIR. 2 L 7 2 4F RT A16WE 20081029 WP 2008 10 29 UPS08853553 1 20081003 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV RT FLAP UPPER EXT SURFACE BOILER PANEL DOUBLER REPAIR NEEDS VALIDATION. UPON FURTHER INVESTIGATION R EPAIR DOES MEET CRITERIA OF EO DC8-5100-304 18 APPENDIX H STEP 5, NO FURTHER ACTION REQUIRED. 2 L 7 4 4F RT 4A25 20081029 WP 2008 10 29 UPS08853618 1 20081005 A 5720 STRUCTURE DOUG DC8 DC873F 302199F WP RT WING MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV RT WING LOWER L/E DOUBLER REPAIR NEEDS VALIDATION FOR REPAIR AT STA XFS 747.600. DOES NOT MEET CRITE RIA IN APPENDIX H STEP 1 SURVEY SEQ 89 4-W4-17. PREVIOUSLY REPAIRED IAW DC8 SRM 57-2-1 FIG 2H PG 15. 2 L 7 4 4F RT 4A25 20081029 WP 2008 10 29 UPS08853622 1 20080923 A 5320 REPAIR DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV LOWER FUSE-INT, BATHTUB FITTING REPAIR ANGLE HAS CORROSION AT FS 1180, BETWEEN L33R-L34R JUST INBOAR D OF AFT CARGO DOOR CUTOUT LOWER EDGE. REPLACED REPAIR ANGLE IAW DC8 SRM 51-30-00-0-1 AND 53-02-00-0 FIG 002D. 2 L 7 4 4F RT 4A25 20081029 EA 2008 10 29 ASOA1257 1 20081001 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REPAIRED RT FS 484 FLOOR SUPPORT INTERCOSTAL RBL 36 IAW REO 601R-53-41-059 AND ASA ECTC REO 601R-53-41-059. LEAK CHECK DUE. LEAK CHECK OF FS 484 GOOD IAW AMM 21-32-00-863-801. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA1275 1 20081003 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 TROUBLESHOT IAW CRJ 200 WDM 33-51-00 AND 33-52-00 RANG WIRING, NO DEFECT NOTED. LO POWER AT LAMP SLAVED IN KNOWN GOOD N R 1 CHARGER ASSY OPS CHECK GOOD. NR 1 BATTERY CHARGER ASSY REQUIRES REPLACEMENT AND BATTERY REQUIRES TOP CHARGE. REMOV ED AND REPLACED FWD CEILING EMERGENCY FLOODLIGHT BATTERY CHARGER IAW CRJ 200 AMM 33-51-05. REQUIRES OP CHECK AND BATTER Y TOP CHARGE. BATTERY TOP CHARGED IAW CMM 33-21-70. OPS TEST GOOD IAW CRJ AMM 33-51-00-710-801. SUPPLEMENTAL SDR CLOS ED 10/21/08. 2 L 7 2 4F RT A21EA 20081030 NM 2008 10 30 SWAA085794 1 20081027 A 5311 6546533 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 302SW 22942 DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500 BETWEEN STR 27R TO STR 28R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081030 EA 2008 10 30 ASOA200801120 1 20080905 A 5320 REPAIR CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 DRILLED OFF, REMOVED OLD PREVIOUS REPAIR LT FLOOR SUPPORT ANGLE AT FS 621. DRILLED UP, COUNTERSUNK AND ALODINED NEW REP AIR PARTS 601R-53-61-117-1 ANGLE, -3 REPAIR ANGLE AND -5 STRAP FROM 2024-T3 .090. INSTALLED ALL REPAIR PARTS WET USING PR1422B½ SEALNT. PRIMED AND PAINTED FASTENERS AND REPAIR PARTS. ALL STEPS OF REO ARE COMPLETE. REPAIR AT LT 621 FLOOR SUPPORT REQ'S DINITROL. APPLIED DINATROL TO REPAIR AREA. LT 621 FLOOR SUPPORT REPAIR REQ'S PRESURIZATION LEAK CHECK. WORK PERFORMED. LT 621 FLOOR SUPPORT REPAIR REQ'S PRESS CHECK. PERFORMED LEAK CHECK OF THE LT 621 FLOOR SUPPORT REPAI R. NO LEAK NOTED. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081030 NM 2008 10 30 F3LA2008102400683 1 20081024 A 5320 D53974968004 PROFILE AIRBUS A319 A319111 3930336 NM ZONE 100 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE AFT CARGO COMPARTMENT ON PROFILE LOCATED AT FRAME 58 BETWEEN STR INGER 38 LEFT AND 38 RIGHT. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2. 2 L 7 2 4F RT A28NM 20081030 NM 2008 10 30 DL757081417 1 20081022 A 5320 FLOOR SUPPORT BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 CORROSION AROUND NUTPLATE HOLE BS 1519 LBL 8 FLOOR SUPPORT RAIL. REMOVED DAMAGED SECTION OF FLOOR SUPPORT RAIL BS 1519 LBL 8. FABRICATED REPAIR PARTS, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH SEALANT. WORK DONE IAW SRM 53-60 -53D FIG 206. 2 L 7 2 4F RT A2NM 20081030 NM 2008 10 30 DL757081425 1 20081016 A 5321 146N539147 FLOOR PANEL BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 728754 CORROSION NOTED ON FIXED FLOOR PANEL STA 1470-1510 AT NUTPLATE LOCATION APPROX AREA LBL 19. CORROSION REMOVED AND REPAI RED IAW ER 08-3376, DAL ER/A 456405-14 REV ORG. 2 L 7 2 4F 4 F RT A2NM E17NE 20081030 WP 2008 10 30 08FDEA04594 1 20081028 A 5320 AFA71321C SUPPORT FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 373FE 46611 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 HOLE "A" INDICATED CRACKED DURING HFEC INSPECTION REMOVED AND REINSTALLE D CLIP, STRAPS AND WEBS. REMOVED AND REPLACED FITTING. FABRICATED AND INSTALLED BUSHING ALL IAW SRM 51-31-01, SRM 53-5 0-00 FIG 17 AND MAE TRAVELER T8/764443. MAJOR REPAIR RII. 2 L 7 3 4F RT A22WE 20081030 WP 2008 10 30 08FDEA04595 1 20081028 A 5320 AFA71321C FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 373FE 46611 MAIN CARGO DOOR LOWER JAMB FITTING NR 6 HOLES "A" AND "C" INDICATED CRACKED DURING HFEC INSPECTION REMOVED AND REINSTALL ED WEB, INTERCOSTALS AND FRAME. REMOVED AND REPLACED FITTING. FABRICATED AND INSTALLED BUSHINGS ALL IAW SRM 51-31-01, SRM 53-50-00 FIG 17 AND MAE TRAVELER T8/764445. MAJOR REPAIR RII. 2 L 7 3 4F RT A22WE 20081030 NM 2008 10 30 08FDEA04600 1 20081028 A 5220 50797824 RETAINER BOEING 727 7272D4 138407U NM ZONE 800 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 EMERGENCY ESCAPE HATCH LT FWD, SEAL RETAINER ATTACH FLANGE IS CRACKED AND WORN IN SEVERAL AREAS. REPLACED UPPER AND LOW ER SEAL RETAINERS REF SRM 51-30-2 P. 3&4 AND SRM 51-30-5 P.5 THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 08FDEA04601 1 20081028 A 5220 50797824 RETAINER BOEING 727 7272D4 138407U NM ZONE 800 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 RT FWD EMERGENCY EXIT HATCH, SEAL RETAINER ATTACH FLANGE IS CRACKED IN SEVERAL PLACES. REPLACED RETAINERS IAW SRM 51-30 -2 AND SRM 51-30-5. THIS IS CLASSIFIED AS A MINOR REAPAIR. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 08FDEA04608 1 20081029 A 5320 656724511 SUPPORT BOEING 727 7272D4 138407U NM FUSELAGE CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 EDGE SUPPORT PANEL BS950 TO 95C LBL 19 TO LBL 28 UPPER AND LOWER SURFACE CORRODED. FABRICATED NEW Z-ANGLE AND STIFFENER , INSTALLED NUT PLATE AND SPLICE OLD STIFFENER W/NEW REPAIR PART & SPLICED BOTH HALVES OF Z-ANGLE REF.DWG 65-57568 & DWG 65-67245 ITEM 12 & SRM 51-40-04 PG 14-17 (CLASSIFIED AS A MINOR REPAIR) 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 08FDEA04610 1 20081029 A 5320 BAC15171507 FLOOR SUPPORT BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 LOWER FWD CARGO PIT, CORROSION ON UNDERSIDE AT NUT PLATES OF FLOOR SUPPORT STRINGER STA 700 15 INCH, RBL 8. CUT DAMAGE SECTION OUT. FABRICATED NEW SECTION AND SPLICE TARTS REF SRM 51-40-4. PRIMED ALL PARTS AND MATING SURFACES REF SRM 51-1 0-3. INSTALLED REPAIR PARTS REF SRM 51-30-2 AND 51-40-4. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081030 WP 2008 10 30 08FDEA04612 1 20081029 A 5414 AUB710813 PANEL DOUG MD10 MD1010F 3022112 WP NR 1 NACELLE CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 NR 1 PYLON PANEL 437 FR IS CHAFED. BLENDED AREA IAW SRM 54-00-01. BOTH FOUND TO BE OUT OF LIMITS IAW 54-00-01 & DWG 71 08. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED IAW SRM 51-35-01 & 51-41-01. 2 L 7 3 4F RT A22WE 20081030 NM 2008 10 30 08FDEA04613 1 20081029 A 5311 651766351 FRAME BOEING 727 7272D4 138407U NM ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 FWD PIT FRAME BS 580 RBL2 WL 155, UPPER FLANGE CRACKED UNDER FLOOR SUPPORT AS SEEN FROM LOWER SIDE. INSTALLED REPAIR CO MPLETED REF SRM 51-30-2. CUT OUT DAMAGED AREA. NDT'D TO VERIFY TERMINATION OF CRACK, NO DEFECTS NOTED REF SRM 51-40-2, N DT MANUAL. 51-00-00. REPAIRED FRAME PER SRM 51-40-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 08FDEA04614 1 20081029 A 5311 651766351 FRAME BOEING 727 7272D4 138407U NM ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 FWD PIT FRAME BS 580 RBL2 WL 155, UPPER FLANGE CRACKED UNDER FLOOR SUPPORT AS SEEN FROM LOWER SIDE. SDR OPENED IN ERROR DUPLICATE OF SDR 08-4613, FAA PLEASE DELETE THIS SDR. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 08FDEA04602 1 20081028 A 5311 6516348 FRAME BOEING 727 7272D4 138407U NM ZONE 200 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 1148 FRAME DAMAGED FROM GILL LINER ATTACH FRAME, FS 1148, LBL 65, WL 254. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 08FDEA04603 1 20081028 A 5311 655611415 FRAME BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 LOWER FWD CARGO PIT, CORROSION ON FRAME SHEAR TIE AT AFT SIDE OF STA 720B, STR 26-R. REMOVED & REINSTALLED ZEE ANGLE, S TRINGER CLIP AND TIE DOWN FITTING REF SRM 51-30-2. REMOVED CORROSION REF SRM 53-10-1. FOUND TO BE OUT OF LIMITS. MEASUR ED REF NDT MAN PART 4.51-00-00 FIG 2. REPAIRED REF SRM 53-10-4 FIG 13. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081030 EU 2008 10 30 08FDEA04615 1 20081029 A 7830 2215127509 STRUCTURE AIRBUS 300 A300B4622R 3930312 EU THRUST REVERSER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 NR 2 ENGINE INBD T/R, CORE COWL SECTION HAS A CRACK AT THE AFT UPPER SECTION ABOVE THE LOCK HANDLE. MATERIAL ID PER P/ W CMM 78-32-34, 0.050, PO 607468.1. HEAT TREAT IAW TPS 1003; REV "A" (HT102408.2). STOP DRILL THE CRACK TO 0.0625 PER P/W CMM 78-32-34. LOCATED, DRILLED AND INSTALLED SPLICE PLATE PER P/W CMM 78-32-34. ALODINED AND PRIMED PER P/W SRM 5 4-02-03. 2 L 7 2 4F RT A35EU 20081030 NM 2008 10 30 USAASB08099 1 20081022 A 2560 P4010021 BATTERY BOEING 737 7374B7 138449C NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 445US 24863 PIT - MAINTENANCE REPORTED THE FORWARD CABIN EMERGENCY FLASHLIGHT RED INDICATOR WAS NOT BLINKING. MAINTENANCE REMOVED A ND REPLACED THE BATTERY IN FLASHLIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 K11A2008102472201 1 20080908 A 5320 INTERCOSTAL BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722C 20948 MAIN DECK FLOOR INTERCOSTAL UPPER CHORD AND WEB CORRODED (INTERCOSTAL FRAME). 2 L 7 3 4F RT A3WE 20081030 NM 2008 10 30 K11A2008102372202 1 20080924 A 5311 FRAME BOEING 727 7272H3 138368N NM FUSELAGE CRACKED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 FRAME 1110 LT SIDE AT LBL 30 CRACKED AND DENTED. 2 L 7 3 4F RT A3WE 20081030 WP 2008 10 30 AALA20080218 1 20080926 A 2560 BRACKET DOUG DC9 DC983 3022083 WP GIRT BAR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION ON AFT GIRT BAR SUPPORT AT AFT SERVICE DOOR. INSTALLED NEW FITTING IN ACCORDANCE WITH SRM 51 01. 2 L 7 2 4F RT A6WE 20090114 WP 2009 1 14 AALA200802621 1 20081201 A 3230 ROD DOUG DC9 DC982 3022082 WP ZONE 700 BROKEN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 492AA 49730 ABQ INFLIGHT. CREW REPORTED LT MAIN LANDING GEAR UNSAFE INDICATION. RETURNED TO ABQ AND LANDED WITHOUT INCIDENT. FOUN D LT MAIN LANDING GEAR BUNGEE ROD END SHREARED OFF. REPLACED LEFT MAIN LANDING GEAR BUNGEE ROD. SYSTEM GROUND CHECKED NO RMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 20081030 EA 2008 10 30 SWIA200820232 1 20080616 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 492SW 7168 FS 280 RBL9 INBOARD AND OUTBOARD CLIPS CRACKED. C-CHECK, REPLACED CLIPS. 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 SWIA200820233 1 20080616 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 492SW 7168 ONE AFT PRESSURE BULKHEAD ISOLATOR CRACKED. C-CHECK, REPLACED ISOLATOR. 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 SWIA200820234 1 20080616 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 492SW 7168 FS 280 FLOORBEAM CORRODED ON TOP FROM LBL 2.0 TO RBL 2.0. C-CHECK, REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 SWIA200820235 1 20080622 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 439SW 7578 AFT CAP ANGLE ATTACHED TO FS 280 IS CRACKED AT OUTBOARD SIDE OF LBL9 AND RBL9. C-CHECK, REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081030 NM 2008 10 30 DL76P081438 1 20081025 A 7921 LINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE OIL COOLER LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 1402A 61846 25989 723843 AIRCRAFT ATB FOR NR 2 ENG LOSS OF OIL QTY AND OIL PRESSURE. CREW SHUT DOWN ENGINE PRIOR TO LANDING. T/S IN PROGRESS AIR /OIL COOLER OIL RETURN LINE FOUND CRACKED. REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081030 NM 2008 10 30 EIAA2008102800062 1 20081027 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM BS 228 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 MAIN DECK STA 228 UPPER CHORD AT BL L11 TO R33 FOUND CRACKED, MAIN DECK BS 228 FLOORBEAM UPPER CHORD AT LBL11 TO RBL33. REPAIRED AS PER TAECO EA 53-0062. 2 L 7 4 4F RT A20WE 20081030 EA 2008 10 30 SWIA200820244 1 20081024 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 919SW 7657 FLT 6717 - NR 2 CEILING LEVEL EMERGENCY FLOODLIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 SWIA200820245 1 20081011 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 916SW 7634 FLT 1492 - FLAPS FAIL CAUTION MESSAGE DISPLAYED DURING FLAP RETRACTION. SET FLAP LEVER TO 8° AND RESET CBP1 F4 AND CBP 2 F4. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 MASA2008102400747 1 20081024 A 3350 1317 LIGHT CNDAIR CL600 CL6002D24 1390016 EA ROW 17 INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 904FJ 15004 ASH FLT 2709 CLT-DTW - CAPTAIN REPORTS THE OVERHEAD EMERGENCY FLOOD LIGHT AT ROW 17 INOP. MX REMOVED AND REPLACED LIGHT . 2 L 7 2 4F RT A21EA 20081030 NM 2008 10 30 MASA2008102500751 1 20081025 A 3350 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 449YV 449 ASH FLT 2767 MRY - ALL EMERGENCY LIGHTS WILL SHUT OFF. MX RESET SYSTEM WITH THE CREW. 2 H 7 2 4T RT A13NM 20081030 EA 2008 10 30 SWIA200820247 1 20081020 A 3350 BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS DISCHARGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 927SW 7693 FLT 6526 - FLOOR EMERGENCY LIGHTS FROM ROW 2 THROUGH 5 INOP. REPLACED NR 1 BATTERY POWER SUPPLY. 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 MASA2008102700753 1 20081027 A 2750 855D10013 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS SYS NONE A MASA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 SW 07 715SF 7313 7115 ASH 7320 - MSN-ORD - CREW DECLARED AND EMERGENCY ON LANDING DUE TO A FLAP FAIL. MX REMOVED AND REPLACED BPSU AND COMPLI ED WITH PART A AND B. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081030 SO 2008 10 30 LR7A08118 1 20081006 A 5230 SKIN LKHEED 382 382G 526414U SO CARGO DOOR PUNCTURED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 713 4763 EN ROUTE TO SCHEDULED B-3 CHECK, FOUND 1/4 INCH HOLE IN CARGO DOOR SKIN AT FS 877, LBL 10, WL 201. AIRCRAFT FERRIED TO WSSL FOR B CHECK AND REPAIR. REPAIRED IAW SMP583 FIG 51-140-10. 2 H 7 4 4T A1SO 20081030 SO 2008 10 30 LR7A08120 1 20081015 A 5340 342593L FITTING LKHEED 382 382G 526414U SO FS 858 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 404LC 713 4763 DURING SCHEDULED B-3 CHECK, PER HB5302 JOB CARD, FOUND AFT FUSELAGE INTERIOR STRUT TO SLOPING LONGERON TEE FITTING CRACK ED AT FS 858. REPLACED FITTING IAW SMP583 CHAP 51-70. 2 H 7 4 4T A1SO 20081030 WP 2008 10 30 AALA200802615 1 20080925 A 5320 PAN DOUG DC9 DC983 3022083 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 FOUND WINDOW CRACKED AT FORWARD LOWER WINDOW AT RIGHT STATION 845. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH AARD 53 10 00 25. 2 L 7 2 4F RT A6WE 20081030 WP 2008 10 30 AALA200802617 1 20080926 A 5347 74529527 SEAT TRACK DOUG DC9 DC983 3022083 WP ZONE 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON SEAT TRACK 4. REPAIRED SEAT TRACK 4 PER AARD 53-20-00-10. 2 L 7 2 4F RT A6WE 20081030 NM 2008 10 30 QXEA2008102901104 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX- C4- LT INBD SEAT TRACK HAS CHAFING AND SCRATCHES ALONG CHANNEL AND TOP FROM APPROX STA X262 - X266. BLENDED CHAFE AND SCRATCHES IAW RD8/4-53-884. HFEC INSPECTED IAW 1-84-7A PT 6, 51-00-02, NO CRACKS NOTED. ALODINED BLENDED AREA IAW RD 8/4-53-884, PAGE 6 NOTES 4 AND 6. 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 F3LA2008102700686 1 20081024 A 5320 D5347047700800 PROFILE AIRBUS A319 A319111 3930336 NM ZONE 100 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN AFT CARGO COMPARTMENT ON PROFILE LOCATED AT STRINGER 38 LEFT BETWEEN FRAME 56 AND FRAME 58. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2. 2 L 7 2 4F RT A28NM 20081030 NM 2008 10 30 F3LA2008102700687 1 20081024 A 5320 D53974971002 PROFILE AIRBUS A319 A319111 3930336 NM ZONE 100 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE AFT CARGO COMPARTMENT LOCATED AT FRAME 53 BETWEEN STRINGER 38 LE FT AND 38 RIGHT. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2. 2 L 7 2 4F RT A28NM 20081030 NM 2008 10 30 F3LA2008102700690 1 20081024 A 5320 D5391550320010 PROFILE AIRBUS A319 A319111 3930336 NM ZONE 100 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE FORWARD CARGO COMPARTMENT ON PROFILE LOCATED AT FRAME 31 BETWEEN STRINGER 38 LEFT AND 38 RIGHT. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AN D 2. 2 L 7 2 4F RT A28NM 20081030 NM 2008 10 30 DHLA2008745570 1 20080904 A 5347 CARGO TRACK BOEING 727 727224 1384076 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN FROM STA 950 TO STA 1136 LBL 25 CARGO TRACK WITH CORROSION INCLUDING AROUND ANCHOR NUTS. REPA IRED CARGO TRACK FROM BS 1094 TO 1137 LBL 25 IAW B727 SRM 53-10-5 FIG 1. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 08FDEA04578 1 20081027 A 5730 PANEL DOUG MD11 MD11F 3023600 NM ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 LEFT WING ANTI-ICE TELESCOPIC ACCESS PANEL FOUND CHAFED. REMOVED AND REPLACED IAW AMM 30-11-01-4. ADJUSTMENT CARRIED OUT IAW AMM 30-11-01-4, FOUND SATISFACTORY. 2 L 7 3 4F RT A22WE 20081030 NM 2008 10 30 08FDEA04579 1 20081027 A 5330 2024T3063C SKIN BOEING 757 75723A 1384967 NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 EXTERNAL LOWER FUSELAGE SKIN, LIGHTNING STRIKES BS 500- BS 520 STR 28R- 27R. CHECKED LIMITS IAW SRM 53-00-01 FIGURE 201 REPAIR 6, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIGURE 201 REPAIR 16, FIGURE 101. REMOVED DAMAGE IAW SRM 50-00-01 , REPAIR 16, NFEC CUTOUT IAW NTW 51-00-19 PT.6 NO DEFECTS. MADE REPAIR DOUBLER AND DRILLED IAW SRM 53-00-01 REPAIR 16. TREATED AND PRIMED AREA IAW SRM 51-20-01. INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIGURE 201 REPAIR 16. THIS IS A C AT "B" INSPECTION THRESHOLD 37,000 TOTAL FLIGHTS WITH REPEAT INSPECTION ALTERNATIVES HFEC EVERY 6,000 OR HFEC EVERY 3, 000 IAW SRM 53-00-01 TABLE V. 2 L 7 2 4F RT A2NM 20081030 NM 2008 10 30 08FDEA04580 1 20081027 A 5311 70750063C FRAME BOEING 757 75723A 1384967 NM BS 760 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 AFTER REMOVAL DOUBLER FROM TV MONITOR SUPPORT AT STA 760 FOUND SEVERAL HOLES ON FRAME. REMOVED DAMAGE FRAME STA 760 B TW STR 5R AND 4L IAW 53-00-07. FABRICATED NEW ZEE FRAME PER MAE TRAVELER T8/763343. FABRICATED NEW SPLICES PER MAE TRA VELER T8/76190. TREATED AND PRIMED REPAIR PARTS IAW SRM 53-00-07. DRILLED REPAIR PARTS IAW SRM 53-00-07. INSTALLED RE PAIR PARTS AT STA 760 IAW SRM 53-00-07 FIG 201 REPAIR NR 3. DO A HFEC INSPECTION EVERY 12,000 FLIGHT CYCLES IN NDT PART 6, 51-00-01 REPEAT THIS INSPECTION EVERY 12,000 FLIGHT CYCLES INTERVALS AS ALTERNATIVE DO A DETAILED VISUAL INSPECTION AT 9,000 FLIGHT CYCLES AFTER THE INITIAL INSPECTION. THIS IS A CATEGORY "B" REPAIR. 2 L 7 2 4F RT A2NM 20081030 NM 2008 10 30 QXEA2008102901107 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX- C4- LT INBD SEAT TRACK HAS CORROSION INSIDE CHANNEL FROM APPROX STA X356 - X360. BLENDED OUT CORROSION FOUND TO B E WITHIN LIMITS IAW RD8/4-53-884. HFEC INSPECTED IAW DASH 8 Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ETCHED AND AL ODINED IAW RD8/4-53-884. 2 H 7 2 4T RT A13NM 20081029 EA 2008 10 29 SWIA200820222 1 20080611 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 768SK 10234 FS 280 FLOORBEAM CRACKED AT LBL9 AND RBL9. C-CHECK, REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 SWIA200820223 1 20080623 A 5210 WEB CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 817SK 15107 PASSENGER DOOR AFT WEB CRACKED AT ZONES 2 AND 3. C-CHECK, REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 SWIA200820224 1 20080623 A 5210 WEB CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 817SK 15107 PASSENGER DOOR FORWARD WEB CRACKED AT ZONE 2. C-CHECK, REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 SWIA200820225 1 20081022 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 763SK 10228 FLT 6366 - FORWARD CEILING EMERGENCY FLOOD LIGHT OUT. RELAMPED. 2 L 7 2 4F RT A21EA 20081029 SO 2008 10 29 SWIA200820227 1 20081022 A 2612 DETECTION SYS EMB 120 EMB120ER 3260203 SO MALFUNCTIONED A SWIA K NONE N FALSE WARNING IN INSP/MAINT 1 NM 07 565SW 120340 FLT 5752 - FIRE BELL INTERMITTENTLY RINGS IN FLIGHT, NO LIGHT ASSOCIATED WITH IT. RESET FIRE SYSTEM, CHECKS NORMAL. 2 L 7 2 4T RT A31SO 20081029 WP 2008 10 29 AALA200802590 1 20080930 A 5350 FRAME DOUG DC9 DC982 3022082 WP TAILCONE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 581AA 53158 CANTED FRAME CRACKED AT TAIL CONE ALIGNMENT PIN AT 9 O`CLOCK POSITION. INSTALLED DOUBLER IN ACCORDANCE WITH ESO 80559 D ATED 30 SEP 2008. 2 L 7 2 4F A6WE 20081029 NM 2008 10 29 AALA200802592 1 20080922 A 5311 FRAME BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CRACK FOUND ON FRAME AT LEFT STRINGER 8. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH ECO 1159AA. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 DHLA2008745562 1 20080906 A 5320 STRAP BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 1130 LBL25 STABILIZER STRAP WITH CORROSION. REPLACED FUSELAGE STABILIZER STR AP SECTION FROM BS 1090 TO BS 1130 LBL 25 DUE TO CORROSION IAW B727SRB 51-10-1 PARA 7. 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 AALA200802593 1 20080922 A 5311 FRAME BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CRACK FOUND ON FRAME AT LEFT STRINGER AT STATION 400. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH ECO J1159AA. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 AALA200802595 1 20080922 A 5311 FRAME BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CRACK FOUND ON FRAME AT STATION 500A AND LEFT STRINGER 8. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH ECO J1159AA. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 DHLA2008745559 1 20080905 A 5753 STRAP BOEING 727 727224 1384076 NM LT WING TE FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LT WING INBD MID FLAP INBD SECTION STRAP WITH CORROSION AT WBL 132. REPLACED LT WING INBD MID FLAP I/B SECTION STRAP IA W B727SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081029 NM 2008 10 29 DHLA2008745560 1 20080905 A 5347 CARGO TRACK BOEING 727 727224 1384076 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE CABIN FROM STA 500 TO STA 590 LBL 45 CARGO TRACK WITH CORROSION AT UPPER SECTION AND CRACKED AT STA 522 L OWER SECTION. REPLACED CARGO TRACK AT LBL45 STA 480 TO STA 590 IAW B737 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081029 EA 2008 10 29 ASOA200801381 1 20081022 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 LT 280 WEB HAS MINOR CORROSION DAMAGE. BLENDED OUT MINOR CORROSION ON LT FS 280 WEB. DAMAGE IS FOUND TO BE WITH IN LIM ITS IAW SRM 53-11-00. MAT'L REMOVED .003 IN OUT OF .005 IN MAX ALLOWED. RESTORED A044 FINISH. RESTORED A023 FINISH ON REWORKED AREA IAW SRM 51-21-16. REINSTALLED ALL FASTENERS IN REWORKED AREA AT LT 280 WEB IAW SRM 51-42-06 BM7024222 JO B COMPLETE. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA200801383 1 20081022 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 409 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 RT SIDE PRESSURE FLOOR SEAL HAS CORROSION INTERNITTANT FROM FS 409+128 TO FS 559 RBL 36 TO RBL 47. FOUND CORROSION TO B E ONLY LIGHT SURFACE CORROSION WHICH IS WITHIN ALLOWABLE REPAIR LIMITS IAW SRM 53-61-43. REMOVED CORROSION, PREPPED, PR IMED & PAINTED AREAS IAW SRM 51-21-06. INVESTIGATED, MAPPED AND BLENDED RT PRESSURE FLOOR SILL CORROSION AREAS IAW REO 601R-53-41-666. AREAS FAIL DIMENSIONAL LIMITS OF EO DUE TO LOCATIONS OF FASTENER HOLES & SPACE BETWEEN AREAS OF CORROSI ON. ENGINEERING DISPOSITION REQUIRED. REPAIRED CORROSION DAMAGE TO PRESSURE FLOOR PANEL & ANGLES IAW REO 601R-53-41-80 5. EC/TC REQUIRED. WORK PERFORMED IAW EC/TC REO 601R-53-41-805. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA200801386 1 20081022 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 828AS 7213 REAR PRESSURE BULKHEAD WEB THAT SURROUNDS LINTEL FITTING HAS AN INDICATION NOTED APPROX 1 INCH IN LENGTH 90 PERCENT FULL SCREEN HEIGHT. FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD WEB IAW REO 601R-53-61-1230, STEPS 1 THRU 24. REPAIR OF THE REAR PRESSURE BULKHEAD WEB WAS ACCOMPLISHED IAW REO 601R-53-61-1230. 2 L 7 2 4F RT A21EA 20081029 EA 2008 10 29 ASOA200801390 1 20081024 A 2910 HYDRAULIC SYSTEM CNDAIR CL600 CL6002B19 1900309 EA NR 3 FAILED A ASOA K NONE J WARNING INDICATION CL CLIMB 1 SO 27 877AS 7579 HYDRAULIC SYSTEM 3 FAILURE. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 20081104 NM 2008 11 4 UPS08553764 1 20081027 A 5420 BRACE BOEING 757 75724APF 1384969 NM NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 451UP 27739 INSPECTION TYPE:MOD NR 1 PYLON UNDERWING FAIRING STRUCTURE, LT SUPPORT BRACE P/N 313N5004U13 IS CRACKED AT THE VERTICAL FASTENER HOLE PPS 185.35. REMOVED AND REPLACED NR 1 PYLON SUPPORT BRACE. 2 L 7 2 4F RT A2NM 20081104 CE 2008 11 4 GUUA10030802 1 20081003 A 5320 STRUCTURE BEECH 1900 1900D 1154162 CE FUSELAGE CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81546 UE187 AT SCHEDULED INSPECTION DISCOVERED A .5 INCH CRACK LEFT AIRCRAFT FUSELAGE BELLY LBL 29.06. STOP DRILLED CRACK AND INSTA LLED REPAIR DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 53-90-18. 2 L 7 2 4T RT A24CE 20081104 NM 2008 11 4 K11A2008103172201 1 20081029 A 5311 FRAME BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 CORROSION ON BS 1110 FUSELAGE FRAME BETWEEN STR 17R AND STR 18R. CORROSION 2 X 2 INCHES. 2 L 7 3 4F RT A3WE 20081104 SO 2008 11 4 CHQA200800213 1 20081028 A 3350 100865 BATTERY PACK EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CABIN DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 564RP 1363 692 145524 CAE312502 DURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOP WHEN TESTED. THE NR 4 EMERGENCY LIGHT BATTERY WAS REPLACED, AND THE EMERGENCY LIGHTS OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081104 2008 11 4 NSVA2008039 4 20081030 A 3445 6226523213 CONTROL UNIT SAAB SF340 340B 7860101 EU TCAS DEFECTIVE A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 311CJ 214 TCAS TRANSPONDER WILL NOT POWER UP. SMOKE REPORTED. FOUND FAULTY CONTROL UNIT IAW SAAB AMM 34-54-00 & 34-00-00. 2 L 7 2 4T RT A52EU 20081105 WP 2008 11 5 AALA200802564 1 20080923 A 5320 STRUCTURE DOUG DC9 DC983 3022083 WP BS 180 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 TUL RT SUBFLOOR CORRODED AT STATION 180. AREA OF DISCREPANCY IS 2 INCHES BY 2 INCHES. INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081105 NM 2008 11 5 SWAA085879 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 6L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085895 1 20081029 A 5754 65C26686 WEDGE BOEING 737 737317 138447P NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND NR 2 SLAT T/E WEDGE DELAMINATED AT UPPER SURFACE. REPAIRED WEDGE PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085896 1 20081029 A 5330 6545768 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, STR 15L. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085897 1 20081029 A 5330 6562212 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085898 1 20081029 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 18R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081105 EA 2008 11 5 SWIA200820251 1 20080629 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 913SW 7597 INTERCOSTAL TO FRAME CLIP CRACKED AT RT FS 625 (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081105 EA 2008 11 5 SWIA200820253 1 20080629 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 913SW 7597 OUTBOARD CLIP UNDER PANEL 262DRF AT FS 484 IS CRACKED (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081105 EA 2008 11 5 SWIA200820256 1 20081027 A 3234 CONTROL HANDLE CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A SWIA K NONE O OTHER CL CLIMB 1 NM 07 913SW 7597 ON ROTATION AND GEAR UP, GEAR DID NOT RETRACT UNTIL FL100. FLT 6252. REPLACED LANDING GEAR CONTROL HANDLE ASSEMBLY. 2 L 7 2 4F RT A21EA 20081105 EA 2008 11 5 SWIA200820258 1 20081025 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DIRTY A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 955SW 7817 EXIT ROW EMERGENCY LIGHTS INOP. FLT 6653. CLEANED CONNECTORS. 2 L 7 2 4F RT A21EA 20081105 EA 2008 11 5 SWIA200820259 1 20081025 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 955SW 7817 EXIT ROW EMERGENCY LIGHT RIGHT SIDE INOP. FLT 6653. OPS CHECKS NORMAL. 2 L 7 2 4F RT A21EA 20081105 EA 2008 11 5 SWIA200820260 1 20081026 A 3350 INVERTER CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 955SW 7817 EMERGENCY EXIT LIGHTS FROM ROWS 6 THROUGH 8 INOP. FLT 5966. REPLACED INVERTER NR 2. 2 L 7 2 4F RT A21EA 20081105 NM 2008 11 5 SWAA085945 1 20081030 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 2008 11 5 SWAA085950 4 20081030 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 400WN 27891 DURING SCHEDULED MV2 CHECK, FOUND L2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085955 1 20081030 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 457WN 33856 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085956 1 20081030 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 457WN 33856 DURING SCHEDULED HC1 CHECK, FOUND EEPLS LENS MISSING AT ROW 11 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 08FDEA04673 1 20081103 A 5754 652171311 ANGLE BOEING 727 7272D4 138407U NM LT WING LE SLAT CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 LT WING OTBD LE APPROX CLOSE OUT WEB UPPER ANGLE IS CRACKED REMOVED DAMAGED ANGLE. INSTALLED NEW ANGLE, IAW SRM 51-30-2 . THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081105 WP 2008 11 5 08FDEA04676 1 20081103 A 5320 ABA72039 WEB DOUG DC10 DC1030F 3023504 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 FLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL, FOUND CRACK ON HORIZONTAL WEB FLOOR. 2 L 7 3 4F RT A22WE 20081105 EU 2008 11 5 08FDEA04678 1 20081103 A 5321 A2557158700200 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 BULK CARGO FLOOR PANEL IS DELAMINATED AND PUNCTURES. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED A NEW PANEL IAW FEDE X DWG SRZ 25-005. PART MARKED IAW GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20081105 EU 2008 11 5 08FDEA04679 1 20081103 A 5321 A2557158600200 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU FUSELAGE PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 BULK CARGO FLOOR PANEL DELAMINATED AND PUNCTURED. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED NEW PANEL. FABRICATED IAW DWG SRZ 25-005. PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-35-1. 2 L 7 2 4F RT A35EU 20081105 EU 2008 11 5 08FDEA04683 1 20081103 A 5321 A2557157100200 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 BULK CARGO FLOOR PANEL IS DELAMINATED. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED NEW PANEL. FABRICATED TOP SHEET I AW DWG SRZ 25-011. PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-35-4. 2 L 7 2 4F RT A35EU 20081105 EU 2008 11 5 08FDEA04684 1 20081103 A 5321 A2557158300200 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 BULK CARGO FLOOR PANEL IS DELAMINATED. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED NEW PANEL IAW DWG SRZ 25-005. FAB RICATED TOP SHEET IAW DWG SRZ 25-011. PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-35-4. 2 L 7 2 4F RT A35EU 20081105 EU 2008 11 5 08FDEA04685 1 20081103 A 5321 A2557996800000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 BULK PIT FLOOR PANEL IS DELAMINATED. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED NEW PANEL IAW DWG SRZ 25-005. FABRI CATED TOP SHEET IAW DWG SRZ 25-011. PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-35-4. 2 L 7 2 4F RT A35EU 20081105 WP 2008 11 5 08FDEA04687 1 20081103 A 5414 AUB703833 PANEL DOUG MD10 MD1010F 3022112 WP NR 3 PYLON CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 NR 3 PYLON PANEL 487 EL IS CHAFED AT THE FWD END. BLENDED CHAFED AREA. FOUND TO BE OUT OF LIMITS IAW SRM 54-00-01. FA BRICATED IAW SRM 51-21-01. ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED IAW SRM 51-35-01. 2 L 7 3 4F RT A22WE 20081105 NM 2008 11 5 SWAA085957 1 20081030 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 457WN 33856 DURING SCHEDULED HC1 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081105 2008 11 5 SWAA085958 4 20081030 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 506SW 24183 L1 DOOR EMERGENCY EXIT SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081105 WP 2008 11 5 08FDEA04660 1 20081031 A 5711 SPAR CAP DOUG MD10 MD1010F 3022112 WP LT WING DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 388FE 46622 COMPLY WITH LT WING REAR SPAR LOWER CAP SPLICE-LIFE LIMITED REPAIR, STA XORS 395 TO 446 PER EA 8-5710-118517 REV NR POS , SEQ NR 000007. COMPLIED WITH E.A. 8-5710-118917 WING-REAR SPAR LOWER CAP SPLICE-LIFE LIMITED REPAIR. 2 L 7 3 4F RT A22WE 20081105 NM 2008 11 5 08FDEA04661 1 20081101 A 5320 652617212 FLOOR SUPPORT BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 MAIN DECK FLOOR SUPPORT INTERCOSTAL IS CORRODED BS 304-312, LBL 30, WL 230 REMOVED CORROSION ON INTERCOSTAL AT BS 304-31 2 ORIGINAL THICKNESS .062, MATERIAL LOSS .012 REMAINING MATERIAL .050 OUT OF LIMITS. REMOVED INTERCOSTAL AND FABRICATED NEW INTERCOSTAL INSTALLED NEW INTERCOSTAL AND SHIM. REF BOEING DRW 65-26173, SRM 51-30-2 PG 1-3. 2 L 7 3 4F A3WE 20081105 NM 2008 11 5 SWAA085913 1 20081029 A 5311 65548927SW FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 323, STR 20L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085914 1 20081029 A 5320 BAC15171487 STRUCTURE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND CHORD CORRODED AT BS 270, BETWEEN LBL 12 TO RBL 12, WL 208. REMOVED AND REPLACED CHOR D PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 2008UALA05699 1 20080912 A 3350 SWITCH BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT DEFECTIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 FOUND EMERGENCY LIGHT TOGGLE SWITCH ON P5 PANEL TO BE DEFECTIVE, MISSING PLUNGER FOR MICRO SWITCH IN CIRCUIT FOR NOT ARM ED LIGHT WITH SWITCH IN OFF POSITION. INSTALLED NEW SWITCH ON THE P5 PANEL. 2 L 7 2 4F 4 F RT A16WE E21EU 20081104 WP 2008 11 4 UPS08853731 1 20081002 A 5500 RIB DOUG DC8 DC871F 302199D WP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATION OF N/R288527 RIB CRACKED AT TOP AFT END AT XFS 185. REPAIRED 55-02-00 FIG 2. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853737 1 20080930 A 5320 RUB STRIP DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV LT FILLER LOWER RUB STRIPS CORRODED. REPAIRED IAW SRM 51-1-11. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853738 1 20081008 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV REPAIR AT BS 99 TO 104 L31L-L33R HAS ONLY 2 ROWS OF FASTENERS. REPAIRED AS IAW 53-2-0 FIG 10. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853739 1 20080930 A 5350 SUPPORT ANGLE DOUG DC8 DC871F 302199D WP FILLET FAIRING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV RT UPPER WING TO FUSELAGE FILLET FAIRING 292B SUPPORT ANGLE CRACKED. REPAIRED DWG 5769482 SRM 51-1-0 8. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853740 1 20081002 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATE EFN 70219901008 ORIGINAL NRC 158466 LOWER FLOOR WEB CRACKED. REPAIRED IAW 53-2-0 FIG 25. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853746 1 20081002 A 5320 CUSP WEB DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATE EFN 7021997113 NRC 750487 RIGHT CUSP MEMBRANE AT CARGO TRACK CRACKED FS 1430 TO FS 1580. RE PAIRED IAW 53-2-0 FIG 25. 2 L 7 4 4F RT 4A25 20081104 NM 2008 11 4 DXTA2008102803322 1 20081027 A 2780 SLAT GULSTM 200 200 4500308 NM WING MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 758QS 178 KRUEGERS DEPLOYED UNCOMMANDED IN FLIGHT. 2 L 7 2 4F RT A53NM 20081104 EA 2008 11 4 N6WA200810235 1 20081023 A 5220 DOOR CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT NOT SEATED A N6WA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 151GJ 10216 RIGHT EMERGENCY DOOR MESSAGE ON LANDING. RESEATED EMERGENCY DOOR, NO DEFECTS NOTED. OP'S CHECK GOOD. 2 L 7 2 4F RT A21EA 20081105 2008 11 5 SWAA085902 4 20081029 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 405WN 27893 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085903 1 20081029 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 424WN 29828 FOUND EEPLS COVER MISSING AT ROW 8 ABC. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085904 1 20081029 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN PEELING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 623SW 27933 DURING SCHEDULED MV2 CHECK, FOUND OVERHEAD AISLE EMERGENCY EXIT LIGHT LENS RED LETTERING PEELING OFF. REMOVED AND REPLA CED LENS PER MM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085905 1 20081028 A 3350 65C27095 BATTERY BOEING 737 737301 1384611 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR LOWER INTERIOR EMERGENCY EXIT LIGHT INOP. SECURED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085915 1 20081029 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 23R. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085920 1 20081029 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 26R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085929 1 20081030 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 15L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085931 1 20081030 A 5311 65C25228 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 732, STR 4R. REPAIRED FRAME PER SWA ACO. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085932 1 20081030 A 5311 6520725 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085933 1 20081030 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085934 1 20081030 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085939 1 20081030 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER PAE EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085940 1 20081030 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 08FDEA04635 1 20081030 A 5311 651766351 FRAME BOEING 727 7272D4 138407U NM ZONE 100 DAMAGED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 LOWER FWD CARGO PIT, STA 600 RBL 2 INCH WL 155 FLOOR SUPPORT STRINGER IS CORRODED. REPAIRED LOWER FWD CARGO PIT FLOOR S UPPORT STRINGER STA 600 RBL 2 WL 155 REF SRM 51-40-3 PGS 1-6. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081105 EU 2008 11 5 08FDEA04671 1 20081101 A 2611 CG7G0 SMOKE DETECTOR AIRBUS 300 A300B4622R 3930312 EU CARGO BAY MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 721FD 13225 10357 477 AT 8000 AFTER TAKEOFF FROM EGSS GOT SMOKE/FUME ALERT FROM MAIN DECK SMOKE DETECTOR MID 2A. STAYED ON FOR ABOUT 8 MINS, WENT OFF JUST BEFORE LANDING. REACTIVATED ALL MDC LOOPS ALREADY DEFERRED (AFT A, MID 1B AND MID 2B). NO MORE FAULT DI SPLAYED ON MDC SMOKE DETECTION PANEL. CARRIED OUT MDC SMOKE. R & R SMOKE DETECTOR 10 WU AS PER AMM, 26-19-12 P401. PER FORMED TEST AS PER PREVIOUS AMM REF, TEST PASSED. 2 L 7 2 4F RT A35EU 20081105 NM 2008 11 5 08FDEA04670 1 20081102 A 5347 652363753 SEAT TRACK BOEING 727 7272D4 138407U NM BS 600-620 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FUSELAGE UPPER LOBE INTERIOR STRUCTURE, SEAT TRACK AT STA 600-620 LBL 24 CORROSION. REPLACED SEAT TRACK REF S.R.M. 51 -10-2 AND 51-30-2 THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081105 NM 2008 11 5 2008UALA05867 1 20080924 A 8011 35054367 STARTER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 ENGINE CRACKED A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 673UA 29241 OIL LEAK NR 2 ENGINE. FOUND STARTER DRIVE GEARBOX BEARING HOUSING ASSY CRACKED AND LEAKING. REPLACED NR 2 ENG STARTER HOUSING ASSY & STARTER. ALSO REPLACED STARTER DRIVE OIL SEAL. RAN ENG, NO LEAKS NOTED. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081105 NM 2008 11 5 2008UALA05889 1 20080925 A 2612 FIRE LOOP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU APU TAILPIPE FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 339UA 24243 APU FIRE BELL & HANDLE ILLUMINATE DURING TEST. APU FIRE DETECTOR FOUND FAULTY. REPLACED APU TAILPIPE OVERHEAT FIRE LOO P. APU FIRE DETECTION SYSTEM OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 20081105 NM 2008 11 5 2008UALA06300 1 20081028 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 653UA 25391 MID CABIN EEL CROSS-AISLE LIGHT IS INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20081105 NM 2008 11 5 2008UALA06302 1 20081028 A 2432 018550000 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU DISCHARGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 565UA 26669 APU WON`T START TRIED TWO TIMES. APU BATTERY ZERO VOLTS. REPLACED SHIP'S APU BATTERY. ALL START-RUN-CHARGE FUNCTIONS OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081105 NM 2008 11 5 2008UALA06303 1 20081028 A 5230 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FWD CARGO DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 FWD CARGO PIT DOOR SKIN AFT LWR CORNER IS CRACKED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF SKIN. INSTAL LED DOUBLER & FILLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081105 NM 2008 11 5 2008UALA06304 1 20081028 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 CRACK ON FRAME, FWD OF R-2 DOOR CUTOUT, BS 665, STR 11R. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED NEW WEB (P/ N 143N8388). 2 L 7 2 4F 4 F RT A2NM E17NE 20081105 NE 2008 11 5 2008UALA06305 2 20081028 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE UNKNOWN A UALA O OTHER J W WARNING INDICATION INADEQUATE Q C NR NOT REPORTED 1 WP 29 672UA 30027 IDLE DISAGREE: IN AIR MODE LEFT ENG WILL ONLY MATCH RIGHT ENG WITH FLAPS AT 25 AND-OR ENG TAI SW ON. 2 L 7 2 4F 4 F RT A1NM E24NE 20081106 NM 2008 11 6 DHLA2008745584 1 20080926 A 5330 SKIN BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE FROM BS 385 TO BS 391.5 BETWEN S-1L AND S-2L SKIN WITH DOUBLE HOLES AT GPS ANTENNA AREA. REPAIRED FUSELA GE SKIN SECTION FROM BS 367.75 TO BS 395 BETWEEN S-3L AND S-2R DUE TO SKIN WITH DOUBLE HOLES IAW COOPESA EO COO-253-337- 08 DTD 10/05/08 DOCUMENTED ON FAA FORM 8110-3. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 DHLA200800120 1 20081101 A 3350 LIGHT BOEING 727 7272M7 138407S NM CABIN LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 750DH 21951 PILOT REPORT, EMERGENCY EXIT LIGHTS ILLUMINATE PERIODICALLY WITH SWITCH IN THE ARMED POSITION. RESOLUTION, CONFIRMED. RESEATED COCKPIT EMERGENCY EXIT LIGHT. OPS CHECKS GOOD IAW MM 33-50-01. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 DHLA2008745604 1 20080904 A 5320 WEB BOEING 727 727224 1384076 NM ZONE 100 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN WING CENTER SECTION AT BS 825.95 LBL50 WL204 STUB BEAM WEB CRACKED. REPAIRED FUSELAGE WEB SEC TION AT BS 825.95 FROM LBL 49 TO LBL 57 IAW EO COO-2-53-274-08 DTD 9/16/08 DOCUMENTED ON FAA FORM 8110-3. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 DHLA2008745605 1 20081012 A 5313 STRINGER BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE CARGO CABIN S-4R WITH ELONGATED HOLES BS 720E. REPAIRED S-4R FROM BS 720E TO BS 740 IAW SRM 53-10-3 FIG 3. 2 L 7 3 4F A3WE 20081106 WP 2008 11 6 AALA200802653 1 20081001 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 463AA 49593 LGA - EMERGENCY LIGHT AT OVERHEAD RIGHT LAVATORY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD RIGHT LAVAT ORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081106 WP 2008 11 6 AALA200802654 1 20081001 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 463AA 49593 LGA - EMERGENCY LIGHT AT OVERHEAD AFT BULKHEAD DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD AFT BULK HEAD DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081106 NM 2008 11 6 AALA200802655 1 20081001 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 678AN 29428 LAX - EMERGENCY LIGHT AT SEAT 33D BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 33D. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081106 NM 2008 11 6 DHLA2008745583 1 20080905 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM ZONE 200 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT BS 783.45 WL 202 RBL 54 FLOORBEAM WEB CRACKED. REPAIRED FUSELAGE WEB SECTION AT BS 783 WL2 02 FROM RBL 45.5 TO RBL 49.5 DUE TO CRACK IAW EO COO-2-53-267008 DTD 9/9/08 DOCUMENTED ON FAA FORM 8110-3. 2 L 7 3 4F A3WE 20081106 WP 2008 11 6 AALA200802664 1 20081002 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 574AA 53151 TUL - EMERGENCY LIGHT BATTERY PACK AT FORWARD CABIN INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AT FORWARD CABIN . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081106 WP 2008 11 6 AALA200802667 1 20081003 A 3350 LIGHT DOUG DC9 DC982 3022082 WP EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33414 49325 LGA - LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR EXTERIOR LEFT EMERGENCY LIGHT. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F A6WE 20081106 NM 2008 11 6 08FDEA04666 1 20081101 A 5712 640834219 RIB BOEING 727 7272S2F 1384O81 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 LT WING LE RIB LWR CHORD IS CRACKED FSS 119, 17 INCH FROM SPAR REMOVED CRACKED AREA OF RIB FLANGE, FABRICATED AND INSTAL LED REPAIR ANGLE REF SRM 51-40-3 FIG 1. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 08FDEA04669 1 20081102 A 5347 652363725 SEAT TRACK BOEING 727 7272D4 138407U NM BS 690 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 SEAT TRACK HAS CORROSION UNDER O/B FLANGE BS 690 LBL-2, UNDER SEAT TRACK SPLICE ANGLE. REPLACED DAMAGED SECTION OF SE AT TRACK REF SRM 53-10-5. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081106 EU 2008 11 6 AALA200802672 1 20081004 A 2797 WIRE AIRBUS 300 A300B4605R 3930308 EU SLAT SYSTEM BROKEN A AALA O OTHER F P FLT CONT AFFECTED NO WARNING INDICATION LD LANDING 1 SW 21 11060 470 GYE - CREW REPORTED SLAT LOCKOUT AT 5 DEGREES. NO ECAM OR WARNINGS OR FAULT INDICATIONS. LANDED GYE WITHOUT INCIDENT. FOUND BROKEN WIRES ON CONNECTOR TO POSITION PICK OFF UNIT 4CN. REPLACED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT A35EU 20081029 NM 2008 10 29 SWAA085822 1 20081027 A 4920 38007021 APU BOEING 737 7377H4 1384404 NM LEAKING A SWAA D RETURN TO BLOCK K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 29 912WN 36621 AIR TURNBACK / DECLARED EMERGENCY. APPROX 4 MINS. AFTER TAKEOFF BOTH LAV SMOKE ALARMS SOUNDED. FLT ATTENDANTS REPORTE D A SLIGHT ODOR & HAZE IN CABIN. FAINT ODOR IN COCKPIT. RETURNED TO DAL. REMOVED AND REPLACED APU PER MM AND MT. 2 L 7 2 4F RT A16WE 20081029 2008 10 29 SWAA085823 4 20081020 A 2565 416A2100 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 230WN 34592 FOUND R2 DOOR EMERGENCY EXIT SLIDE PARTIALLY OUT OF POSITION. REPOSITIONED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081029 NM 2008 10 29 SWAA085824 1 20081026 A 3350 6574550 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND LT OVERHEAD BULLNOSE LIGHT LOOSE AT ROW 13 ABC. SECURED LIGHT PER SRM. 2 L 7 2 4F RT A16WE 20081030 NE 2008 10 30 SWAA085793 2 20081024 A 7230 874788 COMPRESSOR BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE NR 2 ENGINE STALLED A SWAA B EMER. DESCENT R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 29 726SW 27858 874108 AIR TURNBACK / DECLARED EMERGENCY. COMPRESSOR STALL IN THE NR 2 ENGINE AT 1,100 FT. WHILE REDUCING POWER TO CLIMB THRU ST. REMOVED AND REPLACED NR 2 ENGINE PER MT. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081030 EA 2008 10 30 ASOA200801177 1 20080916 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REPAIRED RT FS 621.00 FLOOR SUPPORT ANGLE IAW BOMBARDIER REO 601R-53-61-117 REV C. ALL STEPS OF REO ARE COMPLETE. FAST ENERS THRU RT FS 621.00 FLOOR SUPPORT ANGLE AND BULKHEAD REQUIRE PRESSURIZATION LEAK CHECK. LEAK CHECK GOOD FOR FASTENE RS AT RT FS 621 FLOOR SUPPORT ANGLE & BULKHEAD IAW CRJ 200 AMM 21-32-00-790-801. SUPPLEMENTAL SDR CLOSED 10/21/08. 2 L 7 2 4F RT A21EA 20081030 EA 2008 10 30 ASOA200801388 1 20081023 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 908EV 7654 PAX DOOR DIFFICULT TO CLOSE. FLT 5624 DEL 312 MINS. 2 L 7 2 4F RT A21EA 20081030 NM 2008 10 30 F3LA2008102400682 1 20081024 A 5320 D53476460000 PROFILE AIRBUS A319 A319111 3930336 NM ZONE 100 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE AFT CARGO COMPARTMENT ON PROFILE LOCATED AT STRINGER 38 (RIGHT) BETWEEN FRAME 52 AND FRAME 55A. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AN D 2. 2 L 7 2 4F RT A28NM 20081030 WP 2008 10 30 AALA200802266 1 20080904 A 4920 5940405503 APU DOUG DC9 DC982 3022082 WP LEAKING A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 242AA 49255 CREW REPORTED SMOKE IN CABIN. RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. FOUND AUXILIARY POWER UNIT (APU) OIL LE AKAGE WITH POSITIVE INDICATIONS OF INGESTION INTO APU INTAKE. REPLACED APU AND PERFORMED PACK BURN. SYS GROUND CHECKED N ORMAL OPERATION. (K) 2 L 7 2 4F A6WE 20081030 WP 2008 10 30 AALA200802267 1 20080903 A 3397 WIRE HARNESS DOUG DC9 DC983 3022083 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 948TW 49575 EMERGENCY LIGHT AT SEAT 15D INOPERATIVE. SECURED WIRE HARNESS FOR EMERGENCY LIGHT AT SEAT 15D. SYSTEM GROUND CHECKED NOR MAL OPERATION. (K) 2 L 7 2 4F RT A6WE 20081030 WP 2008 10 30 AALA200802269 1 20080904 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 458AA 49563 EMERGENCY LIGHT AT OVERHEAD AFT GALLEY AISLE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD AFT GALLEY AISLE . SYSTEM GROUND CHECKED NORMAL OPERATION. (K) 2 L 7 2 4F A6WE 20081030 NM 2008 10 30 AALA200802274 1 20080905 A 3397 CONNECTOR BOEING 777 777223 1385213 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 EMERGENCY LIGHTS AT SEAT ROWS 4J TO 8H INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHTS AT SEAT ROWS 4J TO 8H. SYSTE M GROUND CHECKED NORMAL OPERATION. (K) 2 L 7 2 4F RT T00001SE 20081030 NM 2008 10 30 AALA200802275 1 20080905 A 3350 0201804001 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 761AJ 31478 EMERGENCY LIGHTS AT SEAT 20G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHTS AT SEAT 20G. SYSTEM GROUND CHECKED NORMAL OPERATION. (K) 2 L 7 2 4F RT T00001SE 20081030 NM 2008 10 30 KCSA081500 1 20080930 A 5414 SKIN BOEING 747 747236B 1384804 NM NR 2 PYLON DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 701CK 21730 NR 2 PYLON INBD LOWER SKIN DAMAGED AT NAC STA 194. (K) 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 KCSA081501 1 20080930 A 5411 FRAME BOEING 747 747249F 1384849 NM NR 3 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 NR 3 PYLON NAC STA 221.9, BULKHEAD RT AFT FRAME WEB CRACKED AT (2) SPOTS. 750 AND .250. (K) 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 KCSA081502 1 20080930 A 5411 FRAME BOEING 747 747249F 1384849 NM NR 3 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 NR 3 PYLON NAC STA 221.9 BULKHEAD LT AFT FRAME WEB CRACKED. (K) 2 L 7 4 4F RT A20WE 20081030 NM 2008 10 30 KCSA081503 1 20080930 A 5411 DOUBLER BOEING 747 747249F 1384849 NM NR 3 PYLON CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 NR 3 PYLON NAC STA 221.9 BULKHEAD FWD FRAME WEB DOUBLERS CORRODED. (K) 2 L 7 4 4F RT A20WE 20081107 NM 2008 11 7 2008UALA06352 1 20081102 A 5210 DOOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR OBSTRUCTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 585UA 26709 DOOR 3R WILL NOT ARM. CLEARED D RING STRAP FROM DOOR SILL, ARMS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081106 NM 2008 11 6 08FDEA04649 1 20081031 A 5311 FRAME BOEING 757 75723A 1384967 NM BS 720 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 FWD CARGO PIT, BS 720, AT S-23L, FRAME IS DENTED ON TOP SIDE. REPAIRED BS 720 FRAME AT S-23L, IAW SRM 53-00-07, REPAIR N R 5. REPAIR PARTS FABRICATED ON MAE TRAVELER T8/763002 AND INSTALLED IAW SRM 51-40-02 AND 53-00-07, REPAIR NR 5. THIS REPAIR IS CLASSIFIED AS A CATEGORY 'B" MAJOR REPAIR WITH THE FOLLOWING FOLLOW UP TRACKING REQUIREMENTS: INITIAL AT 37,50 0 FC AFTER REPAIR INSTALL OR 50,000 FC, WHICHEVER OCCURS FIRST; THEREAFTER EVERY 12,000 FC. 2 L 7 2 4F RT A2NM 20081106 WP 2008 11 6 AALA200802665 1 20081002 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 574AA 53151 TUL - EMERGENCY LIGHT BATTERY PACK AT AFT CABIN INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK AT AFT CABIN. SYSTE M GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081106 SO 2008 11 6 C2XA08IA218 1 20080929 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16951 145063 DURING SCHEDULED MAINT THE GALLEY EMERGENCY EXIT IDENTIFIER LIGHT WAS FOUND TO BE INOPERATIVE. MAINT REMOVED AND REPLACE D NR2 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED THE SYS AND CLEARED THE DISCREPANCY. (K) 2 L 7 2 4T RT T00011AT 20081106 SO 2008 11 6 C2XA08IA233 1 20081025 A 2822 2C74 PUMP EMB 145 EMB145XR 3260214 SO FUEL SYSTEM FAILED A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 12201 6881 6881 14500959 IAH - FLIGHT 2196, THE CREW ABORTED TAKEOFF AT 60KIAS DUE TO E2 LOW FUEL PRESSURE MESSAGE ON EICAS. MAINTENANCE PLACED THE FUEL PUMPS ON MEL 28-21-01 CAT C CTL 157306, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 10/28/08 THE A IRCRAFT RETURNED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED ELECTRIC FUEL PUM 2C, OPERATIONALLY CHECKED WITH NO DEFEC TS, CLEARED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081106 NM 2008 11 6 CALA0801020 1 20081103 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 FRAME CRACKED AT STATION 747 ABOVE S-9L. REPAIRED PER EA 5310-04498 OP 2, INSTALLED REPAIR ANGLES ON FRAME STATION 747, S-9L. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 CALA0801021 1 20081103 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 FRAME CRACKED AT STATION 787 ABOVE S-9L. INSTALLED REPAIR ANGLE AT STATION 787, S-9L PER EA 5310-04498 OP 2. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 CALA0801023 1 20081103 A 5311 143A1110 BELTFRAME BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34222 28931 CRACK FOUND AT FASTENER, BELT-FRAME AT STATION 380 BETWEEN S-8R S-9R AT OVERHEAD BIN MOUNT RAIL ATTACHMENT. REPAIRED FR AME PER EC/RA 5310-04863. 2 L 7 2 4F RT A16WE 20081106 SO 2008 11 6 C2XA08RI148 1 20080921 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO ODOR A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13913 145438 FLIGHT CREW REPORTED BURNING ODOR IN CABIN DURING TAXI OUT. MX PERFORMED OPS CHECK OF AIR CONDITIONING, ELECTRICAL AND B LEED SYSTEMS AND COULD NOT DUPLICATE THE ODOR. ACFT WAS APPROVED TO RETURN TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081106 EA 2008 11 6 MASA2008110200760 1 20081102 A 3230 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR MALFUNCTIONED A MASA K NONE O OTHER CR CRUISE 1 SW 07 37178 19913 7178 ASH FLT 2923 PHX-ICT. CAPTAIN RETURNED TO FIELD DUE TO A GEAR DISAGREE AFTER RETRACTION FOLLOWED BY NOSE GEAR DOOR WARN ING. MX REMOVED AND REPLACED PSEU. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 MASA2008110100759 1 20081101 A 3350 20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA CABIN DISCHARGED A MASA K NONE L NO TEST NR NOT REPORTED 1 SW 07 154SF 7154 ASH FLT 7300 GSP-IAD. LEFT AND RIGHT EXTERIOR FORWARD EMERGENCY LIGHT INOP. MX REMOVED AND REPLACED BATTERY. 2 L 7 2 4F RT A21EA 20081106 NM 2008 11 6 QXEA2008110501132 1 20081018 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 418QX 4143 PDX - C1 - FWD FUSELAGE EXTERIOR ROOF SKIN HAS LIGHTNING STRIKE AT RIVET EDGE AND SKIN AT APPROX FS X-31.000 AND STR LT 3. DRILLED OUT RIVET, NO DAMAGE TO SKIN FOUND. PERFORMED HFEC AROUND REMOVED RIVET FOR CRACKS IAW Q400 NDTM PART 6, 51 -00-01, NO CRACKS NOTED. INSTALLED SOLID RIVET IAW SRM 51-42-05. PRIMED AND PAINTED REF Q400 SRM 51-25-05. 2 H 7 2 4T RT A13NM 20081106 EA 2008 11 6 QXEA2008110401155 1 20081031 A 2130 PRESSURE SYSTEM CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 19 601QX 10009 SEA- "AUTO PRESS" CAUTION MESSAGE AFTER T/O. SELECTED "MAN PRESS." AT THAT TIME WE GOT AN "AUTO PRESS 1/2 FAIL". RETURN ED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. FOUND "CPC PNL FAILED" FAULT IN THE MDC. MDC STATES THAT THE CAB IN PRESS CONTROL PANEL IS NOT ABLE TO PROVIDE CABIN PRESS DATA. THIS WAS NOTED ON DATA LINE 350 BIT 13 "CPCP PRESS SNSR FAIL." CYCLED SHIP POWER. FAULT DID NOT RETURN. COMPLIED WITH CRJ700 FIM TASK 21-33-01-810-804-A01. FAULT DID NOT R ETURN. COMPLIED WITH OPS TEST OF THE CABIN PRESSURE CONTROL PANEL IAW CRJ-700 MM TASK 21-33-01-710-801-A01. FAULT DID NOT RETURN. OPS CHECK GOOD. PRESSURIZED AIRCRAFT IN MANUAL MODE. NO FAULTS INDICATED. CHECKS GOOD. NO PARTS REPLACE 2 L 7 2 4F RT A21EA 20081106 NM 2008 11 6 SWAA085982 1 20081031 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN UNSECURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 283WN 36610 FOUND LT EEPLS LIGHT UNSECURED. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081105 WP 2008 11 5 AALA200802652 1 20081001 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 463AA 49593 LGA - EMERGENCY LIGHT AT LEFT OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081105 WP 2008 11 5 AALA200802638 1 20081002 A 5510 3912033504 HINGE FITTING DOUG DC9 DC983 3022083 WP HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON HORIZONTAL STABILIZER LEFT INBOARD HINGE PLATE LUG NUMBER 4. AREA OF DISCREPANCY 2 INCHES BY 2 INCHE S. REPLACED LEFT INBOARD LUG IN ACCORDANCE WITH WORKCARD 55 94 05. 2 L 7 2 4F RT A6WE 20081105 SO 2008 11 5 SWIA200820262 1 20081028 A 6120 78249046 PCU EMB 120 EMB120ER 3260203 SO RIGHT DEFECTIVE A SWIA K NONE O OTHER CR CRUISE 1 NM 07 236SW 13041 120312 IN ALL PHASES OF FLIGHT, AND AT SEVERAL DIFFERENT TORQUE SETTINGS, IF CONDITION LEVERS ARE MAX RPM, NP IS 101.5 PERCENT TO 102.5 PERCENT RT SIDE. FLT 7768. REPLACED RIGHT PCU. P/N: 782490-46, S/N ON: 981074, S/N OFF: 950741. 2 L 7 2 4T RT A31SO 20081105 NM 2008 11 5 UIEA200800335 1 20081030 A 5753 65B155183 FAIRING BOEING 747 7472D3B 1384805 NM TE FLAP DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 506MC 21252 LT WING NR 1 CANOE FAIRING AT WBL 743.828 WAS DAMAGE ON CARGO LOADING. CANOE WAS REMOVED PER ATLAS DMI M08-227. AREAS OF CANOE AT FAIRING STA 147.766 LOWER SIDE, STA 124.5 & 135.5 INSIDE OF CANOE, STA 152.766, 159.766, 167.766 ON OUTBOARD SIDE, SMALL HOLES 3.0 INCH DIAMETER WITH DELAMINATION AND STA 126.766 LOWER SIDE AREA OF DELAMINATION 12.0 IN. X 7.5 I N. WERE PERMANENT REPAIRED AS PER B747-200 SRM 51-40-09 FIG 6 SHEETS 1 THRU 3 TABLE 1, 250* CURE PER SRM 51-40-12. CANO E TAIL CONE AREA WAS REMOVED AND REPLACED AS PER B747-200 SRM 51-30-02 AND CANOE WAS RE-INSTALLED AS PER B747-200 AMM 27 -51-31. 2 L 7 4 4F RT A20WE 20081105 NM 2008 11 5 CALA0801018 1 20081030 A 5315 255T1241 STIFFENER BOEING 767 767424ER 1385270 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76054 29449 BODYSTATION 246 FLOORBEAM FORWARD SIDE ONE STIFFENER FOUND CRACKED AT RBL 8. BODYSTATION 246 FLOORBEAM FORWARD SIDE RBL 8 STIFFENER REPLACED PER SRM 51-10-02 AND FASTENER INSTALLED PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081105 NM 2008 11 5 08FDEA04634 1 20081030 A 5315 651631468 FLOORBEAM BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 FUSELAGE UPPER LOBE INTERIOR STRUCTURE CORROSION STA 310 LBL 3, ON FLOORBEAM. REMOVED CORROSION, FOUND TO BE OUT OF LIM ITS, FABRICATED REPAIR ANGLE, HFEC BLEND OUT AREA AND TO ALL FASTENER HOLES IN FLOOR BEAM. INSTALLED REPAIR. REF EA 7 -5310-123807 STEP 1 THRU 13. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081105 NM 2008 11 5 08FDEA04640 1 20081030 A 5720 WEB BOEING 727 7272D4 138407U NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 RT WING LE, ANTI-ICE DUCT BOX WEB AT NR 4 KRUEGER FLAP POS, IS CRACKED AND HAS SEVERAL IMPROPERLY INSTALLED FASTENERS. REPLACED LOOSE AND WORN FASTENERS, FABRICATED AND INSTALLED DOUBLER FOR CRACK IN PANEL, REF SRM 51-30-02 PG 1-12 AND SRM 51-40-02 2 L 7 3 4F A3WE 20081105 EU 2008 11 5 08FDEA04643 1 20081030 A 5347 A5383202020400 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK SEAT TRACK AT RBL 38 HAS CORROSION 12.0 INCH FWD OF FR 43. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-4 0-21. 2 L 7 2 4F RT A35EU 20081117 NM 2008 11 17 KCSA081577 1 20081113 A 5313 STRINGER BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 STR 46R DAMAGED AT BS 2160. 2 L 7 4 4F RT A20WE 20081105 NM 2008 11 5 08FDEA04636 1 20081030 A 5322 69445661 SHEAR TIE BOEING 727 727227 1384078 NM BS 950F CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 491FE 21529 AFT CARGO COMPT SHEAR TIE AT BS 950F BETWEEN STR 28L AND 29L IS CRACKED. REMOVED SHEAR TIE IAW SRM 51-30-2. FAB NEW SH EAR TIE FROM 7075-O 0.080 INCH IAW SRM 53-10-2 FIG 5 AND 53-10-4 FIG 15. HEAT TREAT SHEAR TIE IAW FAS ENGINEERING REPOR T NR 2-37153-807 REV A, TREAT AND PRIME NEW SHEAR IAW SRM 51-10-2. INSTALLED NEW SHEAR TIE AT BS 950F BETWEEN STR 28L A ND 29L IAW SRM 51-30-2 AND 53-10-4 FIG 15. 2 L 7 3 4F A3WE 20081105 NM 2008 11 5 08FDEA04637 1 20081030 A 5322 69445667 SHEAR TIE BOEING 727 727227 1384078 NM BS 970 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 491FE 21529 CORROSION AT SHEAR TIE STR 30R AND STA 970 REMOVED DAMAGE SHEAR TIE IAW SRM 53-10-4 FIG 15. FAB NEW SHEAR TIE IAW SRM 5 3-10-4 FIG 15 AND 53-10-2 FIG 5. HEAT TREAT SHEAR TIE IAW FAS ENGINEERING REPORT NR 2-37153-801 REV A. TREAT AND PRIME D IAW SRM 51-10-2. INSTALLED SHEAR TIE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20081105 NM 2008 11 5 08FDEA04626 1 20081030 A 5315 6516318113 FLOORBEAM BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 FUSELAGE UPPER LOBE INTERIOR STRUCTURE, CORROSION ON FWD SHEAR DECK STA 360 RBL 30-37. FASTENERS REMOVED FROM FLOORBEAM STA 360 RBL 30-37 REF SRM 51-30-02. ACCOMPLISHED EA 7-5310-123806 FASTENERS INSTALLED IT FLOORBEAM REF SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081105 NM 2008 11 5 08FDEA04627 1 20081030 A 5220 65C80678107 ANGLE BOEING 727 7272D4 138407U NM ZONE 800 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 LT AFT EMERGENCY HATCH, SEAL RETAINER ATTACH FLANGE IS CRACKED IN SEVERAL PLACES. MATCH DRILLED NEW SEAL RETAINER REF S RM 51-30-5 P 1/5. REMOVAL AND INSTALLATION COMPLETED ON NON ROUTINE NR N11265 ITEM NR 3/4. THIS IS CLASSIFIED AS A MIN OR REPAIR. 2 L 7 3 4F A3WE 20081105 NM 2008 11 5 SWAA085980A 1 20081102 A 3350 70036611 SIGN BOEING 737 7377H4 1384404 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 240WN 32503 DURING SCHEDULED MV1 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN INOP. R&R SIGN PER MM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085980 1 20081028 A 5312 6516300 WEB BOEING 737 7373H4 1384600 NM BS 188 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND WEB CRACKED AT BS 188, RBL 45. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 08FDEA04667 1 20081101 A 5320 65162794 FLOOR SUPPORT BOEING 727 7272D4 138407U NM ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 UPPER LOBE INTERIOR STATION 760 TO 850 RBL 45 INCH, 24' FLOOR BOARD ATTACH ANGLE HAS WEAR IN SEVERAL AREAS. REMOVED NUT PLATE 8 SRM 51-30-02, BLENDED WEAR MARKS STA 760 - 850 RBL 24 REF SRM 51-10-1 ORIG "T'' .088, WORST "T" REMOVED .035 INCH. REMAINING "T' .053 INCH STA 808 RBL 24, OUT OF LIMITS. REPAIR REF EA 7-5310-118309, STA 760 - 850 RBL45 WEAR MAR KS THROUGH PAINT, CLEANED, TREATED AND PRIMED REF MM 20 151 7. TREATED AND PRIMED STA 760 - 802/817 - 850 RBL 24 SOPM 2 0-43-05, SOPM 20-44-04, HFEC PER EA 7-5310-118309 STEP 3 PART. NO CRACKS DECTECTED, ROTO PEENED STA 808-RBL 24. TREAT ED AND PRIMED, FILLED BLEND WITH SEALANT APPLIED CORROSION INHIBITOR REF EA NR 7-5310-118309 PG 2 ITEM 3-7. 2 L 7 3 4F A3WE 20081106 WP 2008 11 6 AALA200802666 1 20081001 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 574AA 53151 TUL - OVERHEAD EMERGENCY LIGHTS IN MID CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN MID CABIN. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081106 NM 2008 11 6 KCSA081554 1 20081103 A 5320 FITTING BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 STA 2360 BATHTUB FITTING AT STR 51R CORRODED. 2 L 7 4 4F RT A20WE 20081030 CE 2008 10 30 GUUA10200801 1 20081020 A 5220 MECHANISM BEECH 1900 1900D 1154162 CE EMERGENCY EXIT DIRTY A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 16540 UE172 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED EMERGENCY EXIT DOOR 6A WILL NOT OPEN. CLEANED AND LUBRICATED EMERGENCY EXIT DOOR 6A LATCH MECHANISM. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081030 NM 2008 10 30 USAASB08103 1 20081028 A 3350 CONTACT BOEING 737 73733A 1384673 NM EXTERIOR DIRTY A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 166AW 23627 PHX MAINTENANCE REPORTED THE L1 DOOR EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE CLEANED THE L1 DOOR BULB CON TACTS. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 F3LA2008102800699 1 20081027 A 3213 201522255 BEARING AIRBUS A319 A319111 3930336 NM MLG CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON LEFT MAIN LANDING GEAR LOWER BEARING. MAINTENANCE REMOVED AND REPLA CED LOWER BEARING ASSEMBLY IN ACCORDANCE WITH ENGINEERING AUTHORIZATION A9-32R-30744 AND A9-32R-30742. 2 L 7 2 4F RT A28NM 20081030 SO 2008 10 30 SWIA200820246 1 20081027 A 6120 78249046 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PROPELLER OVERSPEED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 567SW 16760 4846 120342 FLT 5549 - RIGHT PROPELLER NP CONTINUALLY SURGED FROM 103 PERCENT TO 95 PERCENT ON CLIMB. REPLACED RIGHT ENGINE PCU, P/ N 782490-46, S/N ON, 931245 S/N OFF, 980912. 2 L 7 2 4T RT A31SO 20081030 NM 2008 10 30 QXEA2008102901106 1 20081002 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4- NR 5 CABIN SEAT TRACK INBD FLANGE IS CORRODED AT STA X70 - X72. BLENDED OUT CORROSION AND FOUND TRACK TO BE O UT OF LIMITS IAW RD8/4-53-884. REMOVED OLD TRACK AND INSTALLED NEW TRACK REF Q400 SRM 51-40-15 AND 51-42-05. 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 QXEA2008102901114 1 20081002 A 5320 THRESHOLD BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4 - MAIN CABIN DOOR THRESHOLD HAS CORROSION ON UPPER SURFACE AROUND RIVET HEADS. FOUND THRESHOLD TO BE OUT OF LI MITS PER RD8/4-53-1660. REMOVED THRESHOLD MEMBER PER DHC8 Q400 SRM 51-40-07 AND INSTALLED NEW THRESHOLD WITH RUB STRIP IAW SRM 51-42-05. 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 QXEA2008102901115 1 20081002 A 5320 SILL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4 - MAIN CABIN DOOR LOWER SILL PLATE HAS CORROSION ON LOWER SURFACE UNDER NUTPLATES. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER RD8/4-53-1660. REMOVED AND SILL PLATE PER Q400 SRM 51-40-07 AND INSTALLED NEW SILL PLATE IAW 5 1-42-05, 51-42-90 AND 51-23-00. 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 QXEA2008102901116 1 20081002 A 5320 FLOOR SUPPORT BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4- MAIN CABIN ENTRY FLOOR SUPPORT STRUCTURE HAS CORROSION ON BRACKET AT STA X27.00. REMOVED TWO RIVETS FROM LOWE R SECTION OF BRACKET IAW SRM 51-40-07. REMOVED BRACKET AND FABRICATED NEW AS PER ORIGINAL REF SPEC IN DHC8 Q400 SRM 53- 20-23 ITM 35. INSTALLED NEW BRACKET AT X27.00 WITH RIVETS REF DHC8 Q400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 DHLA2008745572 1 20080905 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN SEAT TRACK FROM BS 344 TO BS 600 RBL 45 HAS CORROSION. REPLACED SEAT TRACK SECTION AT RBL 45 FROM BS 480 TO BS 690 IAW B727 SRM 51-10-1 PARA 7. 2 L 7 3 4F A3WE 20081030 WP 2008 10 30 AALA200802626 1 20080930 A 5347 5936663U503 CARGO TRACK DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON LEFT FLOOR TIE DOWN TRACK IN AFT CARGO. AREA OF DISCREPANCY WAS 8 FEET BY 4 INCHES. REPLACED LEFT T IE DOWN TRACK IN ACCORDANCE WITH SRM 51-10-1. 2 L 7 2 4F RT A6WE 20081030 WP 2008 10 30 AALA200802629 1 20081001 A 5313 LONGERON DOUG DC9 DC983 3022083 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CRACK FOUND ON LONGERON 3 LEFT AT STATION 160. LENGTH OF CRACK WAS .025 INCH. REPLACED APPROXIMATELY A 22 INCH SECTION OF LONGERON FROM STATION 148 TO 170 IN ACCORDANCE WITH SRM 53-02-00 FIGURE 18. 2 L 7 2 4F RT A6WE 20081030 SO 2008 10 30 SIMA200829801 1 20081023 A 3350 78241 INVERTER EMB 135 EMB135KL 3260302 SO CABIN INOPERATIVE A SMIA K NONE L NO TEST UK UNKNOWN 1 SW 21 858AE 145754 FLIGHT 3852 - CREW REPORTED CABIN EMERGENCY LIGHTING FLOOR STRIP AT SEATS 1 AND 2 INOPERATIVE AT THE MOST FORWARD STRIP. CREW RESET AIRCRAFT POWER NO CHANGE. AIRCRAFT REMOVED FROM SERVICE. REMOVED & REPLACED NR 2 BATTERY POWER SUPPLY IAW EMB AMM 33-50-04, NO FIX. REMOVED & REPLACED NR 2 EMERGENCY LIGHT INVERTER IAW EMB AMM 33-50-11, EMERGENCY LIGHTS OPER ATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081030 SO 2008 10 30 FDKA2008102100279 1 20081021 A 2750 3634001021 SHAFT EMB 145 EMB145LR 3260212 SO TE FLAP UNKNOWN A FDKA B EMER. DESCENT F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 07 844MJ 2986 145481 FRL FLT 6198 SYR-JFK. DECLARED EMERGENCY IN BOUND TO JFK FOR FLAP FAIL AT ZERO DEGREES. MX REMOVED AND REPLACED BOTH I /B FLEX SHAFTS, LT VELOCITY SENSOR AND RIGGED FLAPS. 2 L 7 2 4T RT T00011AT 20081030 EU 2008 10 30 YENA200810240100 1 20081022 A 2621 34600017 PRESSURE SWITCH AIRBUS 320 A320232 3930326 EU FIRE BOTTLE FAULTY A YENA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 658JB 5687 3148 AFTER 1 HOUR INTO FLIGHT, CREW OBSERVED A CARGO DISCHARGE 1 LIGHT ILLUMINATED. NO CORRESPONDING ECAM OR SMOKE IND ON CA RGO PANEL. FLIGHT DIVERTED TO DENVER. TROUBLESHOT AND VERIFIED NR 1 BOTTLE LOW PRESSURE SW AT FAULT. REPLACED NR 1 BOT TLE IAW AMM 26-23-41-04. OPS TEST NORMAL. 2 L 7 2 4F RT A28NM 20081030 NM 2008 10 30 YENA200810240102 1 20081023 A 2120 UNKNOWN EMB ERJ190 ERJ190100IGW 3260408 NM CABIN & COCKPIT ODOR A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 193JB 190000017 BURNING ODOR DETECTED IN COCKPIT & CABIN, RETURNED TO JFK. AS PER FIM 21-20-00-210-201-A OPERATION & ISOLATED PACKS & I NSPECTED PASSENGER CABIN FOR ABNORMAL SMELL. OPERATED ENGINE & ISOLATED BLEED SYSTEMS. INSPECTED CABIN, NO ABNORMALITI ES NOTED. ACCOMPLISHED FIM TASK 21-20-00-819-801-A SMOKE AND/OR ABNORMAL SMELL IN PASSENGER CABIN AND/OR COCKPIT. ACCO MPLISHED STATIC TORQUE CK OF LT & LT ACM'S IAW AMM 21-51-05. NO DEFECTS AT THIS TIME. OPS CHECK OK. 2 L 7 2 4F RT A57NM 20081030 2008 10 30 PNSA100802 4 20081022 A 3445 6228971120 WARNING SYSTEM SAAB SF340 340B 7860101 EU TCAS MALFUNCTIONED A PNSA O OTHER N FALSE WARNING CL CLIMB 1 AL 03 675PA 33012 6517 340B206 YELLOW TCAS ALERT SHORTLY AFTER TURN RED ALERT. PULLED C/B AND RESET THE TCAS, WENT TO A NORMAL MODE. TESTED OK, CONTI NUED THE FLIGHT. 2 L 7 2 4T RT A52EU 20081030 NM 2008 10 30 USAA920081741 1 20080912 A 5754 BAC15063692 TEE FITTING BOEING 737 7373G7 138447J NM LE SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 160AW 23782 SAL - C19 - NR 5 SLAT TEE CHORD CRACKED AT SLAT A STATION 124 TO 254.4. REPLACED TEE CHORD ON NR 5 SLAT STATION 124 TO 254.4 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 USAASB08086 1 20080922 A 3350 20121 POWER SUPPLY BOEING 737 7374B7 138449C NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 458UW 25022 BOS - MX REPORTED THE AFT CABIN EMERGENCY LIGHTS INOPERATIVE. MX R&R THE AFT LT BATTERY PACK AND CHARGER PER MM 33-51-5 1. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 20081030 SO 2008 10 30 FDKA2008102400281 1 20081024 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO EXTERIOR INOPERATIVE A FDKA K NONE L NO TEST NR NOT REPORTED 1 SW 07 856MJ 145626 FRL FLT 6220 IAD-OVERNIGHT. RT EXTERIOR EMERGENCY LIGHT INOP. MX RELAMPED THE LIGHT. 2 L 7 2 4T RT T00011AT 20081030 NM 2008 10 30 KCSA081549 1 20081028 A 5320 ANGLE BOEING 747 747212B 1384886 NM NLG WW CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 NOSE WHEEL WELL VERTICAL BEAM ANGLE CRACKED .500 INCH AT BS 300 RBL 32 WL 150. 2 L 7 4 4F RT A20WE 20081031 NM 2008 10 31 SWAA085865 1 20081028 A 5322 6546546 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 907, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 SWAA085867 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081031 SO 2008 10 31 RAIA2008102800002 1 20081024 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 844HK 14500838 DURING PRE FLIGHT INSPECTION, THE LT OVERWING EMERGENCY EXIT FLOOD LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE BULB AT THE AFFECTED LIGHT. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081031 NE 2008 10 31 ABXA200810270254 2 20080926 A 7200 CF680A2 ENGINE BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE NR 1 DEFECTIVE A ABXA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 23 749AX 3451 22226 580124 LEFT FAN ENGINE VIBRATION HIGH 4.7. OTHER VIBRATION INDICATIONS WERE: AIRPLANE VIBRATION, AUDIBLE NOISE, VIBRATION FOLL OWS THRUST CHANGE. REPLACED NR 1 ENGINE PER WORK CARD NR 7010. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E13NE 20081031 NM 2008 10 31 ABXA200810280256 1 20081006 A 3697 TERMINAL BOEING 767 767232 1385132 NM BLEED AIR SYS BROKEN A ABXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 741AX 22215 WITH RIGHT HP BLEED CLOSED PER MEL PROCEDURES, CONTINUED TO GET A BLEED VALVE OFF EICAS MSG. CREW FOLLOWED THE ENGINE B LEED VALVE NON NORMAL PROCEDURES. RETURNED TO AIRPORT. FOUND TERMINAL BROKEN AT NR 1 HIGH STAGE VALVE POSITION, REPAIR ED TERMINAL IAW 20-00-00. 2 L 7 2 4F RT A1NM 20081031 WP 2008 10 31 ABXA200810180257 1 20081014 A 5610 LOCK DOUG DC9 DC941 302207N WP WINDOW OUT OF POSITION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 FIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT OPEN. FOUND UPPER LOCK OFF THE TRACK. REPOSITIONED WINDOW LOCK MECHANISM. OPS CHECK GOOD IAW DC9 AMM 56-10-00. 2 L 7 2 4F A6WE 20081031 NM 2008 10 31 ASAA0873669 1 20081027 A 5210 571411 LATCH BOEING 737 737790 13844CN NM L1 DOOR DIRTY A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 618AS NG000519 30543 L1 DOOR HOLD OPEN LATCH WILL NOT UNLOCK. CLEANED AND LUBED L1 DOOR HOLD OPEN LATCH, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 QXEA2008102901117 1 20081002 A 5320 FLOOR SUPPORT BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 416QX 4083 PDX - C4- CABIN FLOOR SUPPORT HAS CORROSION AT UPPER SURFACE X33.00 Z100.00 Y32L. REMOVED CORROSION BY BLENDING AND FOU ND BLEND TO BE OUT OF LIMITS PER Q400 SRM 51-21-00 AND 51-14-00. FABRICATED NEW "TEE" CABIN FLOOR SUPPORT AS PER SRM 53 -20-43 AND USING ORIGINAL AS TEMPLATE. MATCH DRILL HOLES TO EXISTING STRUCTURE IAW DHC8 Q400 SRM 51-40-07. INSTALLED C ABIN FLOOR SUPPORT AND NUTPLATES TO THE SUPPORT WITH SOLID RIVETS PER Q400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 20081031 NM 2008 10 31 DL757081414 1 20081023 A 5320 146N539151 FLOOR SUPPORT BOEING 757 757232 1384965 NM BS 1510-1530 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 1510 THRU 1530 RT. REPLACED FLOOR SIDEWALL SUPPORT IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081031 NM 2008 10 31 DL757081416 1 20081009 A 5320 146N5391 FLOOR SUPPORT BOEING 757 757232 1384965 NM BS 1540 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 CORROSION ON LOWER SURFACE OF FLOOR SUPPORT RAIL BS 1540 RBL 3 AT NUTPLATE LOCATION. REMOVED DAMAGED SECTION OF FLOOR S UPPORT RAIL BS 1540 RBL3. FABRICATED REPAIR PARTS, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH SEALANT. DONE IAW SRM 53-60-53D FIG 206. 2 L 7 2 4F RT A2NM 20081031 WP 2008 10 31 ABXA080244 1 20080926 A 3246 TIE BOLT DOUG DC9 DC941 302207N WP WHEEL ASSY DAMAGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX OCT831144 47499 LOOSE TIE BOLTS. WHEEL SCRAPPED. (K) WHEEL BOLTS LOOSE. INSPECTED, REPAIRED IAW ABX SPEC WORKSHEET BS421B DATED 12-21-0 7 AND THE ABX WHEEL AND TIRE MANUAL, REV 17. 2 L 7 2 4F A6WE 20081031 WP 2008 10 31 ABXA080242 1 20080919 A 3246 BOLT DOUG DC9 DC941 302207N WP WHEEL ASSY LOOSE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX SEP891797 47510 LOOSE TIE BOLTS. WHEEL SCRAPPED. (K) BOLTS BACKED OFF. REQUIRES OVERHAUL. OVERHAULED IAW ABX SPEC WORKSHEET BS421A D ATED 12/21/07 AND THE ABX WHEEL AND TIRE MANUAL, REV 18. 2 L 7 2 4F A6WE 20081031 EA 2008 10 31 A6WA200840588 1 20080911 A 3297 17300233 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING DAMAGED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 31 401AW 7280 DEPARTING, RETRACTIVE GEAR AND NOSE WHEEL STEERING INOP CAUTION. COMPLIED WITH QRH PROCEDURE. PERFORMED SHORT TO GROUND TEST WITH MEGGER OF NOSE WHEEL STEERING HARNESS ON GEAR FOUND MULTIPLE SHORT TO GROUND ON 500V SETTING. REPLACED HARNESS FROM CONNECTOR P4EC TO PIVOT RVDT AND SERVO VALVE IAW AMM 23-61-65. SWUNG NLG AND PERFORMED OPS CHECK OF NWC IAW 32-51- 00, OPS CHECK GOOD. (K) 2 L 7 2 4F RT A21EA 20081031 SO 2008 10 31 RAIA00809028 1 20080927 A 5210 DOOR EMB 145 EMB145LR 3260212 SO MAIN PAX STIFF A RAIA O OTHER O OTHER NR NOT REPORTED 1 CE 03 847HK 14500857 PASSENGER DOOR STIFF TO SWING OPEN. MAINT CYCLED THE DOOR SEVERAL TIMES WITH NO DEFECTS NOTED. (K) 2 L 7 2 4T RT T00011AT 20081030 NM 2008 10 30 QXEA200801021 1 20080924 A 3230 SEQUENCE VALVE BOMBDR DHC8 DHC8402 1390042 NM NLG MALFUNCTIONED A QXEA O OTHER O OTHER AP APPROACH 1 NM 19 405QX 4047 NOSE LANDING GEAR DOORS DID NOT CYCLE CLOSED AFTER GEAR SELECTED DOWN. DID NOT EXCEED SPEED LIMITS. LANDING UNEVENTFUL. FERRIED FOR REPAIRS. REPLACED THE NLG SOLENOID SEQUENCE VALVE AND FLUSHED THE HYDRAULIC LINES. CHECKS GOOD. RETURNED TO SERVICE. (K) 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 QXEA200801020 1 20080923 A 2120 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 19 405QX 4047 RAMP REPORTS ELECTRICAL SMELL IN AFT CARGO COMPARTMENT. MAINTENANCE PERFORMED GVI OF COMPARTMENT WITH NO DEFECTS NOTED. RAN APU AND BLEED AIR WITH NO SMELL NOTED. COULD NO DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED. (K) 2 H 7 2 4T RT A13NM 20081030 NM 2008 10 30 AALA200802264 1 20080903 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 EMERGENCY LIGHT AT SEAT 22C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORMAL O PERATION. (K) 2 L 7 2 4F RT T00001SE 20081030 NM 2008 10 30 08FDEA04585 1 20081027 A 5411 SPAR BOEING 757 75723A 1384967 NM NR 1 NACELLE MISINSTALLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 920FD 24289 NR 1 PYLON, WHEN THE 311N5220-52 BATHTUB FITTING WAS LOCATED AND DRILLED C/M TO THE INBD LOWER SPAR 3 HOLES WERE MISLOCA TED CAUSING A MISALIGNMENT C/M TO THE LWR SPAR. REAMED OTBD HOLE "A' TO 0.3267 DIA AND INSTALLED 1 BACB30US5K(*) X BOLT . REAMED OTBD HOLE "B" TO 0.4067 AND INSTALLED 1 BACB30US6K(*) Y BOLT AND BACW10CA SELF, ALIGNING WASHERS UNDER BOLT H EAD AND NUT. BOTH FASTENERS IN HOLE "A" AND HOLE "B" WERE REAMED. INSTALLED AND TORQUED PER EA 757-5450-16-A1812 REV - , OCT 21,2008. COMPLIED WITH EA F-5450-124026 OCT 22, 2008. 2 L 7 2 4F RT A2NM 20081030 EU 2008 10 30 08FDEA04588 1 20081028 A 5347 A53812923000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK SEAT TRACK RBL 38 HAS CORROSION 9.0 INCH FWD OF FRAME 42. REMOVED SEAT TRACK IAW SRM 51-40-21. LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-44. INSTALLED SEAT TRACK IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20081030 WP 2008 10 30 08FDEA04592 1 20081028 A 5320 AFA71321C SUPPORT FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 373FE 46611 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 HOLE "D" INDICATED TWO CRACKS DURING HFEC INSPECTION. REMOVED AND REINS TALLED STRAPS, WEBS, CLIPS AND ANGLES. REMOVED AND REPLACED FITTING. FABRICATED AND INSTALLED BUSHINGS ALL IAW SRM 51- 31-01, SRM 53-50-00 FIG 17 AND MAE TRAVELER T8/764441. MAJOR REPAIR RII. 2 L 7 3 4F RT A22WE 20081030 WP 2008 10 30 08FDEA04593 1 20081028 A 5320 AFA71321C SUPPORT FITTING DOUG MD10 MD1010F 3022112 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 373FE 46611 MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 HOLES "A" AND "D" INDICATED CRACKED AND HOLE "C" HAS CORROSION. REMOVED AND REINSTALLED STRAPS, CLIP AND WEB. REMOVED AND REPLACED FITTING MANUFACTURED AND INSTALLED BUSHINGS ALL IAW SRM 51- 31-01, SRM 53-50-00 FIG 17 AND MAE TRAVELER T8/764442. MAJOR REPAIR RII. 2 L 7 3 4F RT A22WE 20081030 NM 2008 10 30 08FDEA04605 1 20081029 A 5320 65317835 THRESHOLD BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 FUSELAGE UPPER LOBE INTERIOR STRUCTURE-LEFT FWD ENTRY DOOR THRESHOLD CORROSION ON "L" ANGLE AND ONE ELONGATED HOLE AND ONE FASTENER HOLE WITH "0" EDGE DISTANCE. REMOVED DAMAGED CHANNEL AND REPLACED WITH NEW 65-31787-5. REINSTALLED DOOR GUTTER ASSY. AND SEALED IAW SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 DL757081455 1 20081020 A 5320 146N36502 PAN BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE LAVATORY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 727893 AFT LAV PAN CRACKED AROUND RIGHT DUMP VALVE T HANDLE CUTOUT. REPAIRED PER ER/A 465404-14 REV ORG. 2 L 7 2 4F 4 F RT A2NM E24NE 20081030 NM 2008 10 30 DL757081456 1 20081016 A 5320 146N545111 INTERCOSTAL BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 1500-1508 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 727893 CORROSION NOTED ON INTERCOSTAL SURFACE AND AT LOWER ANGLE AROUND FASTENERS AT STA 1500-1508 RBL 4. BLENDED CORROSION ON INTERCOSTAL, BLEND EXCEEDED ALLOWABLE LIMITS. REMOVED AND REPLACED INTERCOSTAL IAW DELTA SRM 51-40-02. 2 L 7 2 4F 4 F RT A2NM E24NE 20081030 NM 2008 10 30 DL757081457 1 20081027 A 5320 146N365014 CHANNEL BOEING 757 757232 1384965 NM PWA 4060 PW4060 52119 NE BS 1685 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 727893 CORROSION SUPPORT CHANNEL FWD OF AFT DUMP VALVE IS CORRODED BS 1685, RBL 14-24. REMOVED AND REPLACED SUPPORT CHANNEL DU E TO OUT OF LIMITS CORROSION. 2 L 7 2 4F 4 F RT A2NM E24NE 20081030 NM 2008 10 30 DL76G081461 1 20081029 A 4910 DOOR BOEING 767 767332 1382001 NM APU BAY OPEN A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 1602 34349 29694 RTB - APU DOOR LIGHT ILLUMINATED ON TAXI OUT. ACFT RELEASED AS PER MEL 49-15-01A APU INTAKE DOOR CLOSED. 2 L 7 2 4F RT A1NM 20081030 NM 2008 10 30 DL764081444 1 20081026 A 2750 FLAP SYSTEM BOEING 767 767432ER 1385134 NM PWA 4060 PW4060 52119 NE TE FLAPS MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 834MH 29707 723843 RTB DUE TO T/E FLAP DISAGREE MSG ON TAXI. FLAP SELECTED 15 W/ONLY SLAT MOVEMENT. T/S PER FIM. RAN FLAP/SLATS. NO FAU LTS. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081030 NM 2008 10 30 DL757081446 1 20081027 A 5330 146N361010 SKIN BOEING 757 757232 1384965 NM FS 1690 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 FUSELAGE SKIN CORRODED AT AFT LAV SVC CUTOUT FS 1690, S-26R. SKIN BLENDED AND REINFORCED WITH AN EXTERNAL DOUBLER. 2 L 7 2 4F RT A2NM 20081030 EA 2008 10 30 MASA2008102600752 1 20081026 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS MISSING A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 17231 7231 ASH 2711 PHX - CREW REPORTED A RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. MX REPLACED THE LENS. 2 L 7 2 4F RT A21EA 20081030 NM 2008 10 30 F3LA2008102700684 1 20081026 A 2140 753C000001 HEAT EXCHANGER AIRBUS A319 A319111 3930336 NM ZONE 100 ODOR A F3LA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 21 906FR 18 1684 FLIGHT CREW MADE AN UNSCHEDULED LANDING DUE TO A STRONG ELECTRICAL SMELL THROUGHOUT THE AIRCRAFT CABIN ON CLIMB-OUT. MA INTENANCE INSPECTED AIRCRAFT AND FOUND THAT ALL AIRCRAFT BAY HEAT EXCHANGERS WERE REPLACED THE NIGHT BEFORE DURING SCHED ULED OVERNIGHT MAINTENANCE, WITHOUT SUFFICIENT RUN TIME. CABIN FILTERS WERE REMOVED AND REPLACED IN ACCORDANCE WITH ATS M 21-00-00810-802 AND SIL 21-132. APU BLEED AND ENGINE BLEED SYSTEMS RAN UNTIL SMELL DECREASED IN ACCORDANCE WITH AMM 2 1-21-41-PB401. 2 L 7 2 4F RT A28NM 20081030 NM 2008 10 30 F3LA2008102700689 1 20081024 A 5320 D53974967000 PROFILE AIRBUS A319 A319111 3930336 NM ZONE 100 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE AFT CARGO COMPARTMENT ON PROFILE LOCATED AT FRAME 59 BETWEEN STR INGER 38 LEFT AND 38 RIGHT. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 AND 2. 2 L 7 2 4F RT A28NM 20081030 NM 2008 10 30 DHLA2008745571 1 20080905 A 5347 CARGO TRACK BOEING 727 727224 1384076 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN FROM STA 600 TO STA 690 RBL 25 CARGO TRACK CORRODED. REPLACED SEAT TRACK FROM STA 600 TO STA 690 RBL 25 IAW B727SRM 51-10-1. 2 L 7 3 4F A3WE 20081030 WP 2008 10 30 IXX2008F00098 1 20080923 A 2910 HYDRAULIC SYSTEM DOUG DC8 DC871F 302199D WP LOW A IXXA K NONE O OTHER CR CRUISE 1 SW 11 825BX 45978 DURING CRUISE FROM KSJC TO KRFD, FLT ENGINEER NOTICED HYDRAULIC QUANTITY INDICATOR WAS AT THE BOTTOM OF NORMAL QUANTITY, DID NOT DROP ANY FURTHER DURING THE REST OF THE FLT. THE CREW LANDED IN KTOL WITHOUT FURTHER INCIDENT. MX SERVICED HY DRAULIC SYS, OPS CHECK GOOD IAW DACO DC8 MM 29-00-00. AC WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 20081030 NM 2008 10 30 KCSA081548 1 20081028 A 5320 STIFFENER BOEING 747 747212B 1384886 NM NLG WW CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 NOSE WHEEL WELL TOP PANEL WEB STIFFENER CRACKED AT BS 310 RBL 10, 1 INCH. 2 L 7 4 4F RT A20WE 20081030 2008 10 30 SWAA085840 4 20081025 A 2565 6556685 SLIDE BOEING 737 7375H4 138449D NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY ESCAPE SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081030 2008 10 30 SWAA085841 4 20081026 A 2565 6556685 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 FOUND L2 DOOR EMERGENCY ESCAPE SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085845 1 20081027 A 5322 6546546 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085846 1 20081027 A 5310 6545815 DOOR FRAME BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE L1 DOOR FRAME CRACKED BETWEEN 5TH TO 7TH STOP FITTINGS. REPAIRED FRAME PER S RM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085847 1 20081025 A 5754 65C26686 WEDGE BOEING 737 7373T0 1384582 NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT AFT WEDGE DELAMINATED. REPAIRED WEDGE PER SRM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085848 1 20081028 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FWD EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERIES PER MM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085859 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 13L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085864 1 20081028 A 5322 6546546 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 SWAA085857 1 20081028 A 5512 65C25727 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT BS 147, AFT OF L/E. REPAIRED S KIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 HNAA0800310 1 20081023 A 3610 BLEED AIR SYS DHAV DHC8 DHC8102 2809003 NM CONTAMINATED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 808EX 41453 41453 299 AN ODOR WAS DETECTED WHEN THE BLEED SYSTEM DUCT TEMP EXCEEDS 20C. THE APU AND ENGINE BLEEDS WERE RUN ON THE GROUND AND ODOR DISSIPATED. SUSPECT RESIDUAL DE-ICE FLUID CONTAMINATION OF APU DURING MORNING DE-ICEING OF AIRCRAFT. AIRCRAFT WAS RELEASED FOR SERVICE WITH NO FURTHER DIFFICULTIES REPORTED. 2 H 7 2 4T RT A13NM 20081031 NM 2008 10 31 ASAA0853665 1 20081025 A 2150 3989083 CONTROL VALVE BOEING 737 737890 1384527 NM LT PACK MALFUNCTIONED A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 559AS 6257 35178 LEFT PACK LIGHT ILLUMINATES DURING RECALL. TROUBLE SHOT PER FIM 21 53 TASK 803. BITE CHECK SHOWS LT PACK TEMP CONTROL VALVE FAULT. REPLACED TCV PER M/M 23 51 10 801. GROUND VERIFICATION SUCCESSFUL. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 DL757081410 1 20081017 A 5320 SILL BOEING 757 757232 1384965 NM FS 610 RBL 23 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 FWD CARGO DOOR SILL STA 610 RBL 23 AT FWD SIDE OF AFT FITTING CORRODED. 2 L 7 2 4F RT A2NM 20081031 GL 2008 10 31 RAIA00809023 2 20080920 A 7532 23070418 BLEED VALVE EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007C 03047 GL COMP ACCELERATOR MALFUNCTIONED A RAIA O OTHER M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 CE 03 816HK 145055 ENG 2 ITT RISE ABOVE 900 IN AMBER WHILE THRUST LEVER IN DETENT. MAINT REMOVED AND REPLACED THE NR 2 ENG COMPRESSOR ACCEL ERATION BLEED CONTROL VALVE. ENG RUN OPS CHECKED GOOD. (K) 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081031 CE 2008 10 31 COEA0801788 1 20080927 A 7331 99103386 TRANSDUCER CESSNA 208 208B 2073701 CE FUEL FLOW FLUCTUATES A COEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 13 788FE 208B0286 UNSCHEDULED LANDING, WHILE ENROUTE, THE FUEL FLOW GAGE BEGAN TO FLUCTURATE BETWEEN 150 AND 300 PPH. THE PAR (POWER ANAL YZING RECORDER) WAS ALSO SHOWING THE SAME FLUCTUATION. THE FUEL FLOW TRANSDUCER WAS REMOVED AND REPLACED. (K) 1 H 7 1 3T A37CE 20081031 SO 2008 10 31 RAIA00809029 1 20080927 A 3297 WIRE EMB 145 EMB145ER 3260211 SO NLG WOW BROKEN A RAIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 CE 03 808HK 145157 LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS. MAINT FOUND A BROKEN WIRE AT THE NLG WOW SWITCH. WIRES WERE REPAIRED AND OPS CHECK PROVED GOOD FIX. (K) 2 L 7 2 4F RT T00011AT 20081031 CE 2008 10 31 GUUA10160801 1 20081016 A 5260 1294000321 DOOR BEECH 1900 1900D 1154162 CE AIRSTAIR STIFF A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 53545 UE185 FLT 9254- PILOT REPORTED AIRSTAIR DOOR DIFFICULT TO CLOSE. PERFORMED OPERATIONAL CHECK OF AIRSTAIR DOOR. OPERATIONAL C HECK GOOD. 2 L 7 2 4T RT A24CE 20081031 NE 2008 10 31 22AA20081004 2 20081025 A 7200 CF50C2 ENGINE DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 1 MALFUNCTIONED A 22AA A UNSCHED LANDING A Y FLAME/FIRE ENGINE STOPPAGE CL CLIMB 1 SO 19 526MD 46998 517608 AFTER TAKEOFF HEARD LOUD NOISE. TOWER ADVISED, FLAMES COMING FROM AIRCRAFT AND NR 1 ENGINE EGT WENT TO RED LINE. ENGIN E SHUTDOWN ON ITS OWN. ENGINE CHANGE IN PROGRESS. 2 L 7 3 4F 4 F RT A22WE E23EA 20081031 NM 2008 10 31 ASAA0843675 1 20081007 A 5753 SKIN BOEING 737 737490 1384715 NM FOREFLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 RT OUTBOARD FORE FLAP IS CHAFED ON THE OUTBOARD LEADING EDGE. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, AND INST ALLED IAW B737 400 SRM 57 53 01. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 ASAA0843672 1 20081010 A 5755 SKIN BOEING 737 737490 1384715 NM NR 5 SPOILER DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 NR 5 SPOILER FOUND DELAMINATED ON UPPER AND LOWER SURFACE. THREE REPAIRS. REMOVED DELAMINATED SKIN, FABBED FILLERS AND DOUBLERS, AND BONDED REPAIRS IAW B737 400 SRM 51 70 10 REP 4 ON 3 EA REPAIRS. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 ASAA0843677 1 20081008 A 5330 655298878 SKIN BOEING 737 737490 1384715 NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 SKIN DENTED AT STA 1000 AND STR 14L JUST BELOW THE LAP. REMOVED DAMAGED AREA, FABBED FILLER DOUBLER AND TRIPLER AND INS TALLED REPAIR PARTS IAW B737 400 SRM 53 00 01 REP 31. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 CALA0801016 1 20081028 A 5312 61736 BULKHEAD BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 BULKHEAD VERTICAL WEB AT RBL 17.1 CRACKED AT FASTENER HOLE APPROXIMATELY AT WL 226. REPLACED CRACKED WEB AS REQUIRED PE R SRM 51-10-2. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 CALA0801017 1 20081028 A 3350 D71701100 BATTERY PACK BOEING 737 737924 13848A1 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 79402 30119 BATTERY PACK M1670 WILL NOT ILLUMINATE FLOOR LIGHTS AT WING SECTION. PACK LOCATED AT ROW 21 LT SIDE REMOVED AND REPLACE D EMERGENCY LIGHT BATTERY PACK LOCATED AT ROW 21 LEFT M1670 AND OPS CHECKED EMERGENCY LIGHTS GOOD REF AMM 33-51-06. 2 L 7 2 4F RT A16WE 20081031 CE 2008 10 31 DXTA2008102703317 1 20081024 A 3260 WARNING SYSTEM CESSNA 560 560XL 2076702 CE COCKPIT ACTIVATED E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 645QS 5605145 WITH GEAR HANDLE IN UP, NOSE GEAR GREEN LIGHT INDICATED GEAR DOWN. 2 L 7 2 4F RT A22CE 20081031 NM 2008 10 31 DXTA2008102703318 1 20081024 A 2120 UNKNOWN AMD FALC50 FALCON2000 2730170 NM CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 277QS 177 WITH APU RUNNING AND BLEED AIR IN AUTO THERE IS A STRONG ODOR OF OIL. 2 L 7 2 4F RT A50NM 20081031 2008 10 31 DXTA2008102703319 4 20081025 A 3460 COMPUTER CESSNA 750 750 2076810 CE NR 2 FAILED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 947QS 7500047 FGC 2 FAIL IN FLIGHT. 2 L 7 2 4J RT T00007WI 20081031 EU 2008 10 31 NSVA2008037 1 20081024 A 2120 UNKNOWN SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE COCKPIT SMOKE A NSVA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 27 341CJ 340B341 SMOKE IN COCKPIT DURING DESCENT. NO ABNORMAL INDICATIONS AND FLIGHT ATTENDANT DID NOT SMELL THE SMOKE. CHECKED RT & LT ENG FOR OBVIOUS DAMAGE, NO FAULT FOUND. CHECKED BOTH RT & LT ACM OILS, FOUND FULL. CHECKED FOR POPPED C/B, NONE FOUND . RAN RT ENG FOR APPROX 20 MIN WITH BLEED AIR ON, ACM RUNNING WAS A SLIGHT SMOKE/WARM AIR SMELL. RESIDUAL FROM DISCREP ANCY NR 8 LOG PAGE 168096. (ENG CHANGE) RAN LT ENG, NO FAULTS NOTED. RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 20081031 NM 2008 10 31 2008UALA06269 1 20081026 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 830UA 1243 CABIN EMERGENCY LIGHT TEST FAILED. REPLACED POWER SUPPLY, OPS CHECKED NORMAL. CABIN EMERGENCY LIGHT TEST PASSED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081031 EU 2008 10 31 2008UALA06275 1 20081023 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 457UA 1146 FRAME 67 TO FRAME 71 AND FROM STR 42R TO STR 42L HAS DAMAGE. REPAIR WAS MADE FROM FRAME 67 TO FRAME 71 AND FROM STR 42R TO STR 42L. RAS-DAHAM-4800505-2008 ISSUE C RELEASED 25SEP08 APPROVING THIS REPAIR AS PERMANENT. 2 L 7 2 4F 4 F RT A28NM E40NE 20081031 NM 2008 10 31 2008UALA06277 1 20081025 A 7931 41816054 TRANSMITTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE FAULTY A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 590UA 28708 726725 CREW REPORTS: ENG 1 OIL PRESSURE FLUCTUATES 166-120 PSI, ALL OTHER INDICATION NORMAL. FOUND FAULTY TRANSMITTER. REPLA CED TRANSMITTER. LEAK CHECKS GOOD. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081031 NE 2008 10 31 2008UALA06280 2 20081026 A 7311 1043V0300 BYPASS VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OIL SYSTEM LEAKING A UALA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 546UA 25367 LEFT GENERATOR EICAS ON TAKEOFF ROLL. IDG REQUIRED 3 PINTS OF OIL TO SVC TO FULL. RAN ENG FOUND FUEL-OIL HEAT EXCHANGE R BYPASS VALVE LEAKING AT DRAIN TRAP AT 10 DROPS PER MIN. INDICATED NO FAULTS AND DELTA P WAS NOT POPPED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081031 EA 2008 10 31 ASOA200801397 1 20081025 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 MAIN AVIONICS BAY FLOORBOARD SUPPORT ANGLE ATTACHED TO AFT SIDE OF FS 280 FRAME HAS CORROSION DAMAGE (MARKED). REMOVED AND BLENDED AVIONICS BAY FLOORBEAM ANGLE. BLENDED OUT OF LIMITS PER SRM 51-21-06. TRANSFERRED HOLES FROM OLD ANGLE TO TEMPLET AND FROM TEMPLET TO NEW SUPPORT ANGLE IAW SRM 51-40-11. RIVETED NEW ANGLE IN PLACE USING SOLID RIVETS AND LOCK FASTENERS IAW SRM 51-42-06 AND 51-42-20. 2 L 7 2 4F RT A21EA 20081031 EA 2008 10 31 ASOA200801398 1 20081025 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 750EV 10161 RT SIDE OVERWING EXTERIOR EXIT EMERGENCY LIGHT IS INOP. 2 L 7 2 4F RT A21EA 20081031 EA 2008 10 31 ASOA200801399 1 20081025 A 3260 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 906EV 7642 NOSE DOOR AND GEAR DISAGREE WARNING MSG. A/C RETURNED TO MDT AFTER T/O, EMERGENCY DECLARED. FLT 5204 CX. 2 L 7 2 4F RT A21EA 20081031 EA 2008 10 31 ASOA200801401 1 20081025 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 MAIN AVIONICS BAY FLOORBEAM ATTACHED TO AFT SIDE OF FS 280 FRAME HAS CORROSION DAMAGE (MARKED). REMOVED AND BLENDED AVI ONICS BAY FLOORBEAM. BLENDED OUT OF LIMITS PER SRM 51-21-06. TRANSFERRED HOLES FROM OLD ANGLE TO TEMPLET AND FROM TEMP LET TO NEW SUPPORT ANGLE IAW SRM 51-40-11. 2 L 7 2 4F RT A21EA 20081031 NM 2008 10 31 2008UALA06294 1 20081028 A 3610 7732887810 SHUTOFF VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BLEED AIR SYS MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 644UA 25094 RT BLEED FAULT. RTFL. REPLACING PRSOV. RIGHT ENGINE BLEED LIGHT ILLUMINATED WITH BLEED SWITCH ON. REPLACED PRSOV. AC COMPLISHED IDLE RUN, BLEED PRESSURE NORMAL. BLEED SWITCH-NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E24NE 20081031 NM 2008 10 31 2008UALA06296 1 20081025 A 2432 263BA1011 BATTERY BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE APU FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 785UA 26954 APU BATTERY AND APU CHARGER STATUS MESSAGE. REPLACED APU BATTERY & CHARGER. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081031 NM 2008 10 31 2008UALA06297 1 20081028 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHTS INOP AT ROWS 55HJK THROUGH 61HJK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081031 NM 2008 10 31 2008UALA06287 1 20081027 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EEL LIGHT INOP SEAT 3A AFT. LAMP FOUND DEFECTIVE. REPLACED LAMP, OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081031 NM 2008 10 31 2008UALA06288 1 20081026 A 3350 P40100021 BATTERY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FLASHLIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 773UA 26929 F/A FLASHLIGHT IN FWD GALLEY AREA INOP. REPLACED FLASHLIGHT AND BATTERY, OPS OK. REPLACED SEAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081031 NM 2008 10 31 2008UALA06289 1 20081027 A 8011 35054367 STARTER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT ENGINE FAULTY A UALA D RETURN TO BLOCK W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 671UA 30026 LEFT ENGINE START VALVE CLOSED EARLY DURING ENGINE START. PUSH CREW REPORTED SPARKS COMING FROM ENGINE. REPLACED NR 1 ENGINE STARTER & START VALVE. OPS & AIR LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081106 NM 2008 11 6 KCSA081556 1 20081103 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 706CK 21937 LT SLIDE LIGHT HAS ONE LAMP INOP. 2 L 7 4 4F RT A20WE 20081106 EA 2008 11 6 MASA2008110200761 1 20081102 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC SYS MALFUNCTIONED A MASA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 SW 07 77278 19821 7278 ASH 1025 KOA-HNL. CAPTAIN DECLARED AN EMERGENCY WHEN UPON GEAR EXTENSION AIRCRAFT EXPERIENCED A GEAR DISAGREE. AIRCRAF T LANDED WITHOUT INCIDENT AND MX CHANGED 3A HYD PUMP AND CHANGED MLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 20081106 NM 2008 11 6 2008UALA06310 1 20081029 A 2822 568129115004 PUMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUEL BOOST FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 769UA 26921 FUEL PUMP R FWD RIGHT FORWARD (BOOST) FUEL PUMP SWITCH ON AND PUMP OUTPUT PRESSURE LOW. STATUS MSG01- ACTIVE CLIMB MODE DEPENDENT; RELAY (R FWD FUEL BST PMP SWITCH) IN P110 IS NOT IN COMMANDED POSITION. DB- ELMS P110 ELECTRONICS UNIT MSG- 2811007 ACTIVE CL MODE. FOUND FAULTY BOOST PUMP. REPLACED RIGHT FWD BOOST PUMP. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081106 EU 2008 11 6 08FDEA04650 1 20081031 A 2421 735874D IDG AIRBUS 300 A300F4605R 3930327 EU UNDERSERVICED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 21 659FE 757 ON TAKEOFF, ROLL REJECTED AT 50 KTS FOR GEN1 FAULT ECAM ALERT. ACCOMPLISHED REJECTED AND ECAM PROC TAXIED CLEAR, TO RAM P FOR EXTRA FUEL. ACN RELEASED FOR SERVICE PER MEL/CDL: 24-11-01-A CAT: B EXP: 03NOV08 "MEL 24-11-01-A: GEN (IDENTIFY 1 OR 2) INOP APU GEN MUST BE USED TO POWER AFFECTED BUSS THROUGHOUT FLIGHT. VERIFY AND RECORD IN AML/EAML THAT OIL QTY O F IDG IN DISCONNECT MODE, REMAINING OPERATIVE IDG, AND APU GEN ARE CHECKED ONCE EACH FLIGHT DAY. "MX SERVICED IDG NR 1 AND VERIFIED IT IS DISCONNECTED. MX SERVICE IDG NR 2 AND FUEL WAS ADDED FOR THE FLIGHT TO MEM. R & R IDG1 OPS CK NORMA L REF AMM 24-11-11-4-01. 2 L 7 2 4F RT A35EU 20081106 EU 2008 11 6 08FDEA04651 1 20081031 A 5330 A5397821820200 SKIN AIRBUS 300 A300F4605R 3930327 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 AFT CARGO DOOR, FWD LOWER DOOR JAMB IS GOUGED. FOUND TO BE OUT OF LIMITS PER SRM 53-17-12. REPAIRED PER SRM 53-17-12. TREATED ALL AREAS PER 51-21-10. APPLY LUBRICANT CORROSION INHIBITOR PER 51-23-00. 2 L 7 2 4F RT A35EU 20081106 EU 2008 11 6 08FDEA04652 1 20081031 A 5320 A5397333620000 STRAP AIRBUS 300 A300F4605R 3930327 EU FUSELAGE UNKNOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 AFT CARGO DOOR CUT-OUT AT STRINGER 41R; FRAME 59A; STRAP P/N/A5397333620000 HAS A PREVIOUS BLEND OUT ON THE AFT END OF T HE STRAP. REMOVED & REPLACED PER SRM 51-40-23. 2 L 7 2 4F RT A35EU 20081106 WP 2008 11 6 08FDEA04653 1 20081031 A 5320 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 46631 MAIN CARGO DOOR LOWER JAMB NR 2 FITTING HAS CORROSION IN HOLES "B" AND "C". REMOVED & REPLACED AFA 7131-1 FITTING & REP AIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00 FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 20081106 WP 2008 11 6 08FDEA04658 1 20081031 A 5320 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP NR 7 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 46631 MAIN CARGO DOOR LOWER JAMB NR 7 FITTING HAS CORROSION IN HOLES "A"; "C" AND "D". REMOVED & REPLACED AFA 7132-1 FITTING & REPAIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00 FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 20081106 EA 2008 11 6 COMA0860436 1 20081024 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 781CA 7312 FUEL DRAIN FWD OF ACCESS PANELS 610AB FWD AND AFT DRAIN ATTACH HOLES ARE DAMAGED. REAMED AND INSTALLED FREEZE PLUGS AT FUEL DRAIN FWD AND AFT ATTACH HOLES PER COMAIR EA NR 10-5721-02382. 2 L 7 2 4F RT A21EA 20081106 WP 2008 11 6 AALA200802575 1 20080923 A 5340 59524211 BRACKET DOUG DC9 DC983 3022083 WP GALLEY MOUNT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 TUL RT GALLEY MOUNT BRACKET CORRODED AT STATION 160. AREA OF DISCREPANCY IS 1 INCH BY 1 INCH. REPLACED RT GALLEY MOUNT BRACKET IN ACCORDANCE WITH SRM 51-10. 2 L 7 2 4F RT A6WE 20081106 NM 2008 11 6 F3LA2008110300703 1 20081030 A 5320 D53480043205 SILL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 932FR 18 2258 DURING C3 C-CHECK, INSPECTION NOTED R2 DOOR SILL, AFT OF GIRT BAR FITTING, AFT OUTBOARD NUT PLATE HOLE HAS SIGNS OF CORR OSION. MAINTENANCE REMOVED NUT PLATE IN ACCORDANCE WITH A319 SRM 51-42-11, ENLARGED HOLE TO CLEAN CORROSION, PRIMED AND PAINTED IN ACCORDANCE WITH A319 SRM 51-75-12 AND ENGINEERING AUTHORIZATION A9-53R-30726. 2 L 7 2 4F RT A28NM 20081106 2008 11 6 HALA2008110300839 4 20081103 A 3442 WARNING SYSTEM BOEING 767 7673CB 1385187 NM WEATHER RADAR MALFUNCTIONED A HALA K NONE N FALSE WARNING CR CRUISE 1 WP 13 590HA 33467 ETOPS SIGNIFICANT SYSTEM - WEATHER SYS STATUS INDICATION. RESET WX RADAR SYS STATUS MESSAGE. PERFORMED OPERATIONAL TES T WEATHER RADAR IAW AMM 34-43-00-715-001. OPS CHECK SATISFACTORY. CHECKED FOR FAULT STATUS, NO FAULT DISPLAYED. 2 L 7 2 4F RT A1NM 20081106 NM 2008 11 6 HALA2008110300837 1 20081103 A 7920 OIL FILTER BOEING 767 76733A 1385209 NM PWA 4090 PW4090 52119 NE OIL SYSTEM UNKNOWN A HALA K NONE J WARNING INDICATION CR CRUISE 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM - L OIL FILTER ADVISORY LIGHT EICAS MESSAGE L OIL FILTER. DISAPPEARED WITH THRUST REDUCTION, A DVISORY REMAINED. ACCMP FIM TASK 79-35-00, REPLACED THE MAIN OIL FILTER, RAN ENG OPER NORMAL. LEAK CHECKED OK PER AMM 79-21-05/401. 2 L 7 2 4F 4 F RT A1NM E46NE 20081106 NM 2008 11 6 HALA2008110300838 1 20081103 A 2612 89873202 CIRCUIT CARD BOEING 767 7673G5 1385126 NM FIRE DETECTION FAULTY A HALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM - AT PUSHBACK STATUS MSG, "APU FIRE LP 1" RETURNED TO GATE. PERFORMED FIM 26-15-00 FIG 103 TES T PASS. PERFORMED AMM 26-15-00 715-001 APU FIRE DETECTION SYS, OPS CHECKS GOOD. REPLACED APU FIRE DETECTION CARD PER A MM 26-10-01, OPS CHECKS GOOD. 2 L 7 2 4F RT A1NM 20081106 NM 2008 11 6 HALA2008103100833 1 20081031 A 2421 727810C GENERATOR BOEING 767 76733A 1385209 NM APU MALFUNCTIONED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 582HA 6415 6415 28139 ETOPS SIGNIFICANT SYSTEM - PER FLT CREW APU GEN FELL OFF LINE. REMOVED & REPLACED APU GENERATOR PER MM 24-21-01-424-002 REF LOG PAGE 272631 ITEM 94 FOR VERIFICATION FLT. 2 L 7 2 4F RT A1NM 20081106 NM 2008 11 6 KCSA081557 1 20081105 A 5330 SKIN BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 RT SIDE OF EMPENNAGE SKIN EXTERIOR HAS A 3 INCH CRACK AT BS 2658 WL 295.5. 2 L 7 4 4F RT A20WE 20081106 NM 2008 11 6 KCSA081559 1 20081105 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 UPPER DECK FLOORBEAM WEB CRACKED .750 INCH AT STA 343 RBL 6 TOP SIDE. 2 L 7 4 4F RT A20WE 20081106 NM 2008 11 6 PIDA08034 1 20081030 A 3350 6104789 BATTERY PACK BOEING 737 7372K5 138448X NM CABIN DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 249TR 22598 EXTERNAL EMERGENCY LIGHTS INOP AT THE L2 AND R2 DOORS. REPLACED BATTERY PACK IN THE RIGHT AFT CARGO COMPARTMENT AND OPS CHECKED LIGHTS PER MM 33-51-51. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 QXEA2008110401157 1 20081030 A 5210 HANDLE BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 420QX 4147 SEA - THE AFT PAX DOOR EXTERIOR HANDLE INTERMITTENTLY CATCHES ON THE EXTERIOR DOOR SKIN SURFACE WHEN THE DOOR IS CLOSED AND LOCKED FROM THE INTERIOR HANDLE. WHEN THIS HAPPENS THE EXTERIOR HANDLE REMAINS SLIGHTLY POPPED OUT BUT THE COCKPIT INDICATION SHOWS CLOSED AND LOCKED. FERRY TO PDX FOR REPAIRS. VERIFIED RIG OF VENT DOOR MECHANISM IAW 52-00-00-830-801 , NO DEFECTS NOTED. CHECKED HANDLE FORCE IAW 52-00-00-830-802, NOTED A SLIGHT DRAG ON HANDLE SHAFT. LUBRICATED HANDLE MECHANISM IAW 12-20-01-640-806 TR 12-085. DOOR OPS CHECKED GOOD IAW 52-12-00-710-802. CHECKED ADJUSTMENT OF HANDLE PRO X SENSOR IAW 52-71-01-830-804, NO DEFECTS NOTED. NO PARTS REPLACED. RETURN TO SERVICE. 2 H 7 2 4T RT A13NM 20081106 EA 2008 11 6 QXEA2008110401052 1 20080923 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 611QX 10041 PDX - C4- CORROSION O BELLY SKIN FOR LOWER TCAS ANTENNA AROUND COAX CUT OUT. BLENDED AREA OF DAMAGE IAW CRJ SRM 51-21-0 6 AND FOUND TO BE OUT OF LIMITS. MAPPED AREA OF BLEND FOR ENGINEERING. HFEC INSPECTED IAW CRJ700 NDTM PART 1, 51-20-06 , NO CRACKS NOTED. REMOVED TCAS ANTENNA INTERNAL DOUBLER FROM BELLY SKIN AND REMOVED STRINGER SECTION JUST FWD OF DOUBL ER BY DRILLING OUT RIVETS. CUT OUT SKIN DAMAGE, FABRICATED AND DRILLED UP REPAIR PARTS IAW CRJ 700 REO 670-53-21-384. SIZED UP AND DEBURRED SKIN CUTOUT TO ENSURE GAP BETWEEN PACKER AND SKIN. REF REO 670-53-21-384 SHEET 4. REMAINING BLEN DED AREA WITHIN LIMITS OF REO 670-53-21-284 SHEET 3. HFEC INSPECTED IAW REO 670-53-21-384 SHEET 4 STEP 3, NO CRACKS NOT 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 QXEA2008110401053 1 20080923 A 2752 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA TE FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 611QX 10041 PDX - C4 - L INBOARD FLAP OUTBOARD VANE ACTUATOR IS WORN ON THE SHAFT AT 4 PLACES (UPPER & LOWER SURFACES APPROX .200"LX .100"WX .002" DEEP. MAPPED AREA FOR ENGINEERING. REMOVED DAMAGE FROM AFFECTED AREA REF REO 670-57-52-116 STEP 1. FPI BLENDED AREA FOR CRACKS IAW CRJ 700 NDTM PART 1, 51-20-008 AND HORIZON AIR NDTM SEC 8, NO CRACKS NOTED. COMPLETED REO 670-57-52-116 BY C/W STEP 4. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 COMA0860437 1 20081024 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 781CA 7312 FUEL DRAIN FWD OF ACCESS PANELS 640AB AFT DRAIN ATTACH HOLE IS DAMAGED. REAMED AND INSTALLED FREEZE PLUG AT FUEL DRAIN AFT ATTACH HOLE PER COMAIR EA NR 10-5721-02382. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 QXEA2008110401058 1 20080923 A 2752 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA TE FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 611QX 10041 PDX - C4 - RH WING I/B FLAP 2ND FROM I/B, VANE ACTUATOR SHAFT HAS CHAFING ON UPPER SURFACE. MAPPED AREA FOR ENGINEERING , REMOVED DAMAGE FROM AFFECTED AREA PER REO 670-57-52-116 SHEET 3 STEP 1. FPI BLENDED AREA FOR CRACKS IAW CRJ 700 NDTM PART 1, 51-20-008 AND HORIZON AIR NDTM SEC 8, NO CRACKS NOTED. COMPLETED REO 670-57-52-116 BY COMPLETING STEP 34. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 QXEA2008110401059 1 20080923 A 2752 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA TE FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 611QX 10041 PDX - C4 - RT WING I/B FLAP THIRD FROM I/B, VANE ACTUATOR SHAFT HAS CHAFING ON UPPER SURFACE. MAPPED AREA FOR ENGINEERI NG REMOVED DAMAGED FROM AFFECTED AREA REF REO 670-57-52-116 STEP 1. FPI BLENDED AREA FOR CRACKS IAW CRJ 700 NDTM PART 1 , 51-20-008 AND HORIZON AIR NDTM SEC 8, NO CRACKS NOTED. COMPLETED REO 670-57-52-116 BY COMPLETING STEP 4. 2 L 7 2 4F RT A21EA 20081106 NM 2008 11 6 QXEA2008110501142 1 20081018 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 418QX 4143 PDX C1- POSSIBLE LIGHTNING STRIKE DAMAGE ON UPPER FUSELAGE AT APPROX STA X34.5 4.5 INCH LEFT OF STRINGER 1. REMOVED LIG HTNING STRIKE DAMAGE BY BLENDING IAW RD 8/4-53-666 FOUND TO BE BEYOND LIMITS PER RD 8/4-53-666. MAPPED FOR ENGINEERING. HFEC IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. REMOVED DAMAGE AND CUT INTO INTERNAL STRAP, FABRICATED PACKER AN D DOUBLER, REPAIRED SKIN COUNTERSINKS ALODINED AND PRIMED PARTS AND BARE METAL IAW RD8/4-53-2517/3 GENERAL NOTES 3,4,6-1 0 AND 12. HFEC AREA IAW -8 Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. FINISHED REPAIR IAW RD 8/4-53-2517/3 STEP 13-1 6. 2 H 7 2 4T RT A13NM 20081106 EA 2008 11 6 SWIA200820268 1 20081028 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 956SW 7825 OVERHEAD EMERGENCY LIGHTS NR 3 AND NR 4 INOP (FLT 6504). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 SWIA200820270 1 20081027 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 953SW 7813 EMERGENCY EXIT SIGN BY MAIN CABIN DOOR BURNED OUT (FLT 6589). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081106 SO 2008 11 6 SWIA200820283 1 20081024 A 3320 BALLAST EMB 120 EMB120ER 3260203 SO LAVATORY LEAKING A SWIA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 07 218SW 120287 AFTER TAKEOFF, SMELL OF SMOKE IN FLIGHT DECK; LAV SMOKE DETECTOR ACTIVATED (FLT 5538). REPLACED LEAKING LAV LIGHT BALLA ST. 2 L 7 2 4T RT A31SO 20081106 EA 2008 11 6 SWIA200820284 1 20081029 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 954SW 7815 AFT REARWARD FACING EXTERIOR EMERGENCY WING LIGHT ON RIGHT SIDE IS INOP (FLT 5805). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081105 SO 2008 11 5 C2XA08SH128 1 20080911 A 3000 ANTI-ICE SYSTEM EMB 135 EMB135LR 3260305 SO MALFUNCTIONED A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 27 12530 145533 BLEED 2 LOW TEMP INOP IN ICING CONDITION. MX RELEASED ON MEL IAW 36-11-05. IAW MX VERIFIED NORMAL OPERATION OF BLEED SYS TEM AND ICE AND RAIN PROTECTION TEST REF EMB 135, AMM 30-00-00. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. (K) 2 L 7 2 4F RT T00011AT 20081105 NM 2008 11 5 08FDEA04622 1 20081030 A 5313 A5A70301 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 WHILE ACCOMPLISHING REPAIR ON LT LONGERON 46 AS PER SNRM NR N00694 FOUND LONGERON END CORRODED AT STA 5 -70, AFTER SPL ICE REMOVED FOR ACCESS. REPAIR CARRIED OUT AS PER E.A. 1-5310-122603. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-1 00. 2 L 7 3 4F RT A22WE 20081105 EU 2008 11 5 08FDEA04624 1 20081030 A 7120 A546109260000 FITTING AIRBUS 310 A310222 3930315 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 418FE 343 AFT MOUNTING MATING SURFACE ON NR 1 ENGINE PYLON RUSTED. PERFORMED REPAIR AS PER EA 6-5450-125471 PART 2. 2 L 7 2 4F RT A35EU 20081105 WP 2008 11 5 08FDEA04625 1 20081030 A 5512 ALC72281 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 DURING U/S INSP OF HORIZONTAL STAB, FOUND UPPER INTERIOR SKIN PANELS P/N 7229-1, P/N 7228-1 (POSITION 7 AND 11) WITH CRA CK IN FLYABLE LIMITS, 2 L 7 3 4F RT A22WE 20081105 NM 2008 11 5 SWAA085944 1 20081030 A 5330 6545778 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085946 1 20081030 A 5311 6546533 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 EU 2008 11 5 08FDEA04682 1 20081103 A 5321 A2557157200200 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 BULK CARGO FLOOR PANEL IS DELAMINATED. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED NEW PANEL. FABRICATED TOP SHEET I AW DWG SRZ 25-011. PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL 161 BF IAW AMM 53-10-35-4. 2 L 7 2 4F RT A35EU 20081105 NE 2008 11 5 SWAA085963 2 20081029 A 7230 9513M97PO1 BUSHING BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE NR 1 ENGINE MISSING A SWAA D RETURN TO BLOCK O OTHER CL CLIMB 1 SW 29 701GS 27836 889590 AIR TURNBACK/DECLARED EMERGENCY. DURING CLIMB NR 1 ENG POPPED AND BANGED AT 10,000 FT. FOUND RT VSV ACTUATOR BELLCRANK TO 3RD STG ARM NUT BUSHING MISSING. INSTALLED BUSHING & HARDWARE PER MM. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081105 NM 2008 11 5 SWAA085964 1 20081030 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085965 1 20081030 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085966 1 20081030 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085974 1 20081030 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085975 1 20081030 A 5311 65C25230 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727E, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085976 1 20081030 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085977 1 20081030 A 5311 6546554 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085947 1 20081030 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR CUTOUT, BS 303 TO BS 305, WL 236 TO WL 258. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085921 1 20081030 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085922 1 20081030 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085928 1 20081030 A 3350 65C27095 BATTERY BOEING 737 7373T0 1384582 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 684WN 23941 DURING SCHEDULED SPV CHECK, FOUND AFT CENTER OVERHEAD EMERGENCY EXIT LIGHT INOP. SECURED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085923 1 20081030 A 5311 6520722 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 DHLA2008745595 1 20080907 A 5330 SKIN BOEING 727 727224 1384076 NM ZONE 100 CRACKED A DHLA O OTHER O OTHER NR NOT REPORTED 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT ON LOWER FASTENER ROW OF LAP JOINT S-26L BS 546.5 TO BS 550.5 LOWER SKIN WITH CRACK . REPAIRED FUSELAGE SKIN SECTION FROM BS 543 TO BS 554.75 BETWEEN S-25L AND S-27L IAW B727 SRM 53-30-3 FIG 14 DETAIL II . 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 DHLA2008745593 1 20080917 A 5340 FITTING BOEING 727 727224 1384076 NM ZONE 100 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE AFT CARGO COMPARTMENT BS 950 WL 175 RBL 50 BULKHEAD LATERAL FITTING CRACKED. REPLACED SPLICE FITTING AT BS 950 BULKHEAD WL 175 RBL 50 IAW B727SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 DHLA2008745585 1 20080903 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN STA 1110 BETWEEN RBL 15 AND LBL 63 FLOORBEAM UPPER CHORD WITH CORROSION SEVERAL PLACES. REPAI RED FUSELAGE FLOORBEAM UPPER CHORD SECTION AT BS 1110 FROM LBL 13.750 TO RBL 70 IAW EO COO-2-53-272-08 DTD 9/14/08 DOCUM ENTED ON FAA FORM 8110-3. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 08FDEA04668 1 20081101 A 5315 BAC1505100617 FLOORBEAM BOEING 757 757236 1384971 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 MAIN CABIN STA 345 LBL14 FLOOR SUPPORT HAS AREA OF CORROSION AROUND FASTENER HOLES. REMOVED THE DAMAGED AND FABRICATED PARTS ON MAE TRAVELERS NR T8/755777, T8/755776, T8/748077, T8/748078. INSTALLED REPAIR PARTS AND UPPER T-CHORD ON STA 3 45 LBL 52 TO RBL18 IAW SRM 53-00-51 FIGURE 20 REPAIR 3. THIS IS CATEGORY A REPAIR. 2 L 7 2 4F RT A2NM 20081106 EU 2008 11 6 08FDEA04648 1 20081031 A 5753 A5796011420400 WEB AIRBUS 300 A300B4622R 3930312 EU LT WING TE FLAP DAMAGED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 722FD 479 LEFT WING INBD FLAP AT RIB 25A, WEB PLATE IS CRACKED AND MISDRILLED. REMOVED & REPLACED THE WEB PLATE IN REF TO SRM 51 -40-21& DWG A57960114. 2 L 7 2 4F RT A35EU 20081106 SO 2008 11 6 C2XA08IA232 1 20081025 A 2822 2C74 PUMP EMB 145 EMB145XR 3260214 SO FUEL SYSTEM FAILED A C2XA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 27 12201 6881 6881 14500959 IAH - FLIGHT 2196, THE CREW ABORTED TAKEOFF AT 60KIAS DUE TO E2 LOW FUEL PRESSURE MESSAGE ON EICAS. MAINTENANCE PLACED THE FUEL PUMPS ON MEL 28-21-01 CAT C CTL 157306, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ON 10/28/08 THE A IRCRAFT RETURNED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED ELECTRIC FUEL PUMP 2B, OPERATIONALLY CHECKED WITH NO DEFE CTS, CLEARED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081106 NM 2008 11 6 CALA0801022 1 20081103 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 FRAME CRACKED AT STATION 867 ABOVE S-9L. INSTALLED REPAIR ANGLE AT STATION 867, S-9L PER EA 5310-04498 OP 2. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 2008UALA06313 1 20081029 A 3350 1317 LAMP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT INOP, CEILING ROW 13. REPLACED EMERGENCY LAMP. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081106 NM 2008 11 6 2008UALA06315 1 20081029 A 3350 582233 BATTERY BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 FLOOR EEL INOP, RT SIDE LAV 112. REPLACED BATTERY. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081106 NM 2008 11 6 2008UALA06322 1 20081030 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY CEILING LIGHT ABOVE SEAT 39 LT. RELAMPED EMERGENCY LIGHT. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081106 NM 2008 11 6 2008UALA06324 1 20081030 A 5220 CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE HATCH FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 RT OVERWING ESCAPE HATCH (S) OFFWING MANUAL BACKUP CABLE CHECK FAILED. REPLACED RT OVERWING EXIT PRESSURE BOTTLE MANUAL BACKUP CABLE AND ADJUSTED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081106 NM 2008 11 6 2008UALA06325 1 20081030 A 5347 SPLICE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 CABIN: STA 365, RBL 25 SEAT TRACK SPLICE STRAP CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRAP AND FILLER. 2 L 7 2 4F 4 F RT A2NM E17NE 20081106 NM 2008 11 6 2008UALA06327 1 20081030 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 DENT ON FUSELAGE SKIN AT STA 1711 BETWEEN S15R AND S16R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081106 NM 2008 11 6 USAABB08164 1 20081031 A 2424 734284A GCU BOEING 757 7572S7 1384962 NM NR 1 LOOSE A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 905AW 81918 5362 23567 PHX - FLT 45 PHX TO KOA. UPON ROTATION, THE LEFT AC BUS TRIPPED OFF AND COULD NOT BE RESET, OR POWERED BY ANOTHER GENE RATOR. THE FLIGHT RETURNED TO PHX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE BITE CHECKED THE BUS PROTECTION CON TROL UNIT (BPCU) AND FOUND "NO RESPONSE FROM CONTROL" MESSAGE. THE NUMBER ONE GENERATOR CONTROL UNIT (GCU) WAS INSPECTE D AND FOUND LOOSE IN ITS RACK. THE NUMBER ONE GCU WAS REPLACED. OPERATIONAL CHECKS WERE FOUND OK. 2 L 7 2 4F RT A2NM 20081031 NM 2008 10 31 2008UALA06291 1 20081026 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EEL LIGHT INOP SEAT 40 HJK. FOUND LAMP INOP. REPLACED EEL LIGHT ASSY ON SEAT. OPERATES OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081031 NM 2008 10 31 2008UALA06286 1 20081025 A 2612 STATUS MESSAGE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE WARNING ACTIVATED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 595UA 28748 L ENG FIRE LOOP 1 STATUS MSG. 2 L 7 2 4F 4 F RT A2NM E17NE 20081031 NM 2008 10 31 2008UALA06281 1 20081027 A 2421 GENERATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CR CRUISE 1 WP 29 662UA 27159 LOST RT GENERATOR AND APU. FLIGHT DIVERTED. NR 2 ENGINE GENERATOR REPLACED. (OFF: P/N 745329C, S/N G0796) 2 L 7 2 4F 4 F RT A1NM E24NE 20081031 NM 2008 10 31 AALA200802329 1 20080808 A 5311 148T2740 FRAME BOEING 767 767223 1385123 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 332AA 22331 AFW WHILE ACCOMPLISHING MX NDT FOUND INDICATIONS OF CRACKING AT RT OUTER CHORD AT LOWER AFT FASTENER AT 12A. HOLE REAME D TO .2807 INCH TO REMOVE CRACKING. REPLACED WITH OVERSIZED FASTENER PER MRB 767 3273. 2 L 7 2 4F RT A1NM 20081031 NM 2008 10 31 AALA200802391 1 20080920 A 3350 BATTERY PACK BOEING 737 737823 13844CB NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 944AN 29535 DFW EMERGENCY LIGHT AT RT NR 1 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RT NR 1 DOOR. SYSTEM GRO UND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081031 WP 2008 10 31 AALA200802529 1 20080918 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70504 49798 CUSP IS CRACKED. AREA OF DISCREPANCY IS 18 INCHES BY 8 INCHES. CRACK LENGTH IS 1 INCH. INSTALLED DOUBLER PER AARD 53- 20-00-16. 2 L 7 2 4F A6WE 20081103 EA 2008 11 3 C2XA08TY127 2 20081023 A 7200 23078008 FLANGE EMB 145 EMB145LR 3260212 SO RROYCE AE3007 AE3007A12 54164 EA NR 1 ENGINE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13913 18649 145438 16576 ACFT WAS IN FOR A 3C INSPECTION AND THE NR 1 ENGINE FORWARD BOLT FLANGE WAS FOUND CORRODED. 2 BOLT HOLES AT NR 29 AND N R 45 WERE FOUND IF REPAIRED WOULD RESULT IN BEING BEYOND THE MM LIMITS AND REPAIR OF THE HOLES WOULD RESULT IN A THINWAL L CONDITION. ALL OTHER CORROSION WAS WITHIN LIMITS. THE BOLT HOLES WERE REPAIRED BY PERFORMING A KEYHOLE REPAIR AND IN STALLING REINFORCEMENT PLATES PER SERVICE BULLETIN AE3007A-72-247. ALL WORK WAS ACCOMPLISHED IN REFERENCE TO THE SB AND WILL BE RELEASED AT THE END OF THE CHECK. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081103 SO 2008 11 3 C2XA08TY124 1 20081009 A 5610 163500112 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT MELTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 27 16999 9635 145307 ACFT WAS ON APPROACH INTO BNA WHEN SMOKE WAS SEEN COMING OUT FROM UNDERNEATH THE F/O DASH. MX R&R THE RT W/S IAW EMB 14 5 AMM 56-10-01. PRESSURIZATION CHECK/LEAK CHECK GOOD. IAW EMB 145 AMM 21-31-00. ACFT RELEASED AFTER ALL CHECKS BACK T O SERVICE. 2 L 7 2 4T RT T00011AT 20081103 SO 2008 11 3 C2XA08TY125 1 20081017 A 3350 744412 LIGHT EMB 145 EMB145LR 3260212 SO AFT GALLEY INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16951 145063 AFT GALLEY EMERGENCY LIGHT INOP. R&R LIGHT IAW EMB AMM 33-50-14. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 20081030 NM 2008 10 30 F3LA2008102700698 1 20081027 A 5320 D53916355200 PROFILE AIRBUS A319 A319111 3930336 NM ZONE 100 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE FORWARD CARGO COMPARTMENT ON PROFILE LOCATED AT STRINGER 38 RIGH T, BETWEEN FRAME 28 AND FRAME 31. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 AND 51- 42-11. 2 L 7 2 4F RT A28NM 20081030 NM 2008 10 30 DHLA2008745567 1 20080901 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE CARGO CABIN FRAME WITH DOUBLE HOLE AT B/S 1070 BETWEEN S-5L AND S-6L. REPAIRED FRAME SECTION AT BS 1070 BETWEEN S-4L AND S-6L IAW B727 SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 DHLA2008745568 1 20080902 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE PAX CABIN AT B/S 720C S-8R FRAME WITH DOUBLE HOLE. REPAIRED FUSELAGE FRAME SECTION AT BS 720C BETWEEN S- 7R AND S-9R IAW B727 SRM 53-10-4 FIG 2. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 DHLA2008745569 1 20080904 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE CABIN BS 720E S-8R FRAME WITH HOLE. REPAIRED FRAME SECTION AT BS 720E BETWEEN S-7R AND S-9R IAW B727 SRM 53-10-4 FIG 2. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 F3LA2008102700696 1 20081027 A 5320 D53916354200 PROFILE AIRBUS A319 A319111 3930336 NM ZONE 100 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE FORWARD CARGO COMPARTMENT ON PROFILE LOCATED AT STRINGER 38 LEFT , BETWEEN FRAME 28 AND FRAME 31. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 A ND 2. 2 L 7 2 4F RT A28NM 20081030 NM 2008 10 30 F3LA2008102700697 1 20081027 A 5320 D53974977000 PROFILE AIRBUS A319 A319111 3930336 NM ZONE 100 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CRACKED PROFILE AT FRAME 55A, UPPER SIDE OF AFT CARGO COMPARTMENT. MAINTENANCE R EMOVED AND REPLACED CRACKED PROFILE FROM FRAME 55A TO FRAME 52 IN ACCORDANCE WITH A319 SRM 51-72-11 PAGES 1 AND 2. 2 L 7 2 4F RT A28NM 20081106 NM 2008 11 6 USAABB08167 1 20081102 A 2560 P2070003001 FLASHLIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 939UW 27303 SEA - THE AFT FLIGHT ATTENDANT, OUTBOARD POSITION FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE AFT FLIGHT ATTEN DANT, OUTBOARD POSITION FLASHLIGHT. 2 L 7 2 4F RT A2NM 20081106 NM 2008 11 6 USAASB08106 1 20081103 A 3350 20131ASMI BATTERY PACK BOEING 737 737401 138449B NM CABIN FAULTY A USAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 19 419US 23986 DURING TAXI OUT, THE AFT CABIN EMERGENCY EXIT LIGHTS ILLUMINATED AND COULD NOT BE EXTINGUISHED. AIRCRAFT RETURNED TO TH E GATE. PHL MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 USAABB08166 1 20081101 A 2560 P4010021 BATTERY PACK BOEING 757 757225 1384959 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 915AW 22209 PHX - THE AFT FLIGHT ATTENDANT FLASHLIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE AFT FLIGHT ATTENDANT FLASHLIGHT BATT ERY PACK. 2 L 7 2 4F RT A2NM 20081106 NM 2008 11 6 USAASB08105 1 20081102 A 3350 1012721 LIGHT BOEING 737 737401 138449B NM CABIN FAULTY A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 419US 23986 PILOT REPORTED THE FLOOR LEVEL EMERGENCY EXIT LIGHTING BETWEEN SEAT ROWS 22 TO 24 ILLUMINATED FOR A FEW MINUTES AND THEN WENT OFF. PIT MAINTENANCE REMOVED AND REPLACED THE FLOOR LEVEL LIGHT AT SEAT ROW 24. OPERATIONAL CHECK OF EMERGENCY L IGHTING SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A16WE 20081106 2008 11 6 HALA2008110400840 4 20081104 A 3445 WARNING SYSTEM BOEING 767 76733A 1385209 NM TCAS MALFUNCTIONED A HALA K NONE N FALSE WARNING CL CLIMB 1 WP 13 593HA 33424 ETOPS SIGNIFICANT SYSTEM - DURING CLIMB OUT TCAS FAIL LIGHT ILLUMINATED WENT OUT APPROX 2HRS LATER WORKED FINE FOR REST OF FLIGHT. PERFORMED BITE CHECK PER FIM 34-45-00, SYSTEM CHECKS OK TO CONTINUE. 2 L 7 2 4F RT A1NM 20081106 NM 2008 11 6 HALA2008110300841 1 20081103 A 4990 OIL SYSTEM BOEING 767 767332 1382001 NM APU LOW A HALA K NONE O OTHER LD LANDING 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM - "APU FAULT" EICAS, APU WILL NOT START AFTER LANDING. INSPECTED APU FOUND OIL CAP SECURE BUT OIL LEVEL LOW. SERVICED 3PT OIL. SECURED OIL CAP PER ETOPS 2 PROCEDURE & RAN APU. NO LEAKS NOTED. BITE CHECK PER 49- 11-00/101 FIG 103 OK. 2 L 7 2 4F RT A1NM 20081106 NM 2008 11 6 USAA920081980 1 20081027 A 5330 6552988 SKIN BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 442US 24841 CLT RON MAJOR REPAIR NR 8213467 AND 4371386 LT FUSELAGE SKIN CRACKED AT BS 967, 24L. REPAIRED LT FUSELAGE SKIN AT BS967 , 24L IAW US AIRWAYS EA NR 100715. 2 L 7 2 4F RT A16WE 20081106 2008 11 6 HALA2008110100834 4 20081101 A 2565 D29982225 SLIDE BOEING 717 717200 1383700 NM ZONE 200 UNWANTED DEPLOY A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 481HA 3018 3018 55126 SERVICE DOOR ESCAPE SLIDE INADVERTENTLY DEPLOYED. FOUND SLIDE NOT PROPERLY DEACTIVATED. REMOVED & REPLACED FWD SERVICE DOOR SLIDE PACK IAW AMM 25-61-03. 2 L 7 2 4F TR A6WE 20081106 EA 2008 11 6 SWIA200820263 1 20080707 A 7120 BEARING CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 915SW 7615 LT FORWARD ENGINE MOUNT YOKE LINK ASSEMBLY CORRODED ON UPPER BEARING (C-CHECK). REPLACED MOUNT. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 SWIA200820271 1 20080629 A 7120 SPHERICAL BEARIN CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 913SW 7597 LEFT ENGINE FORWARD MOUNT UPPER LINK SPHERICAL BEARING IS CORRODED (C-CHECK). REPLACED BEARING. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 SWIA200820273 1 20080629 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 913SW 7597 RIGHT ENGINE REAR MOUNT THRUST FITTING BALL END CORRODED (C-CHECK). REPLACED BALL END. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 SWIA200820278 1 20081031 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST NR NOT REPORTED 1 NM 07 746SK 10202 NR 4 CEILING LEVEL EMERGENCY FLOODLIGHT INOP (FLT 5818). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 SWIA200820282 1 20081030 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST NR NOT REPORTED 1 NM 07 492SW 7168 THIRD AFT EMERGENCY LIGHT IN MAIN CABIN INOP (FLT 3802). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 VNAA2008110400012 1 20081029 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A VNAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 05 213PS 7879 CREW REPORTED FLAPS FAIL AMBER CAS MESSAGE WHEN FLAPS WERE SELECTED TO 30 DEGREES ON FINAL APPROACH. CREW COMPLIED WITH QRH. AIRCRAFT LANDED WITHOUT INCIDENT WITH FLAPS AT 20 DEGREES. MAINTENANCE INSPECTED AND PERFORMED CHECKS. NO DEFEC TS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 VNAA2008110300011 1 20081029 A 5230 HANDLE CNDAIR CL600 CL6002C10 1390015 EA CARGO DOOR POPPED A VNAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 05 710PS 10167 CREW REPORTED AN AFT CARGO DOOR AMBER CAUTION ON TAKEOFF. CREW ELECTED TO RETURN TO OAJ. AIRCRAFT LANDED WITHOUT INCID ENT. MAINTENANCE INSPECTED AND FOUND THE AFT CARGO DOOR HANDLE WAS POPPED. MAINTENANCE INSPECTED THE AFT BAGGAGE BAY DOOR, PERFORMED CHECKS AND SECURED THE DOOR CLOSED. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081106 EU 2008 11 6 YENA200811030103 1 20081031 A 3234 215TS07Y00 CONTROL HANDLE AIRBUS 320 A320232 3930326 EU COCKPIT FAILED A YENA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 509JB 7232 64 1270 FLIGHT 908, ORD-JFK, RETURN TO ORD, LANDING GEAR HANDLE WILL NOT MOVE. HANDLE LOCKED IN DOWN POSITION AFTER TAKEOFF. R EMOVED AND REPLACED LANDING GEAR LEVER CONTROL (6GA) IAW 32-31-11-000-001, PERF LG BITE TEST IAW AMM 32-69-00-740-001 AN D NORMAL BRAKING ADJ/TEST IAW AMM 32-42-00-710-001, ALL TEST OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081106 EU 2008 11 6 YENA200811050104 1 20081104 A 3350 321430 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN FAILED A YENA K NONE L NO TEST IN INSP/MAINT 1 EA 15 582JB 20719 1216 2147 ON WEEKLY CHECK, FOUND RT EMERGENCY EXIT EPSU BATTERY FAILED. REMOVED & REPLACED RT EMERGENCY EPSU IAW MM 33-51-38. OP S CHECK NORMAL. 2 L 7 2 4F RT A28NM 20081106 SW 2008 11 6 QMLA1027200808047 1 20081027 A 3310 RCR32G820JS RHEOSTAT BELL 206 206L3 1182108 SW COCKPIT BURNED E QMLA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 220LL 51039 PILOTS REPORT, THE AIRCRAFT LANDED AT EMMETSBURG HOSPITAL AS PART OF THE ORIENTATION TRAINING FOR NEW PILOT. THE ENGINE S WENT TO IDLE AND THE PILOT GOT OUT OF THE AIRCRAFT TO TALK TO THE POLICEMAN SECURING THE LZ. WHEN THE PILOT GOT BACK IN THE AIRCRAFT, SMOKE BEGAN POURING OUT OF THE OVERHEAD CIRCUIT PANEL. THE ENGINE WAS ALREADY AT IDLE, SO THE AIRCRAFT WAS SHUT DOWN AND THE PILOT EXITED THE AIRCRAFT WITH THE FIRE EXTINGUISHER. MECHANICS REPORT, DETERMINED THE CAUSE WAS THE INSTRUMENT LIGHT RHEOSTAT. EVEN THOUGH THE INSTRUMENTS ARE AN MEL ITEM, THE AIRCRAFT WAS LEFT OVERNIGHT. THE MECH ANIC WANTED TO VERIFY THAT THERE WERE NO ADDITIONAL ISSUES BEFORE RELEASING THE AIRCRAFT FOR FLIGHT. 1 G 7 1 3U H2SW 20081106 EU 2008 11 6 MALA080190 1 20081021 A 5522 SKIN SAAB SF340 340B 7860101 EU RT ELEVATOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425XJ 340B425 DENT NOTED IN RT ELEVATOR UPPER SKIN. REPAIRED IAW EO S51031. 2 L 7 2 4T RT A52EU 20081106 WP 2008 11 6 UPS08853843 1 20081022 A 5230 SKIN DOUG DC8 DC871F 302199D WP CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV FLUSH DOUBLER C3 DOOR SKIN BS 1228 L23R NEEDS VALIDATION FOR REPAIR SEQ 715-F1-55. REPAIRED 52-02-00 FIG 4 SHEET 3 AND 52-04-01. 2 L 7 4 4F RT 4A25 20081106 WP 2008 11 6 UPS08853844 1 20081022 A 5230 HOOK DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV FWD PIT DOOR LATCH HOOK CRACKED. INSTALLED NEW LATCH 52-31-01-5 AND 51-01-21. 2 L 7 4 4F RT 4A25 20081106 WP 2008 11 6 UPS08853845 1 20081102 A 2697 CONNECTOR DOUG DC8 DC871F 302199D WP FIRE BOTTLE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV LEFT WING LEADING EDGE INBOARD FIRE BOTTLE QTY CONNECTOR WIRE BROKEN. REPLACE CONNECTOR 20-31-09. 2 L 7 4 4F RT 4A25 20081106 NE 2008 11 6 UPS08M53826 2 20081101 A 7200 ENGINE DOUG MD11 MD11F 3023600 NM PWA 4460 PW4460 NE NR 2 OVERTEMP A IPXA F ACTIVATE FIRE EXT. M E OVER TEMP VIBRATION/BUFFET AP APPROACH 1 SO 01 279UP 48573 AT 2600FT NR 2 ENGINE EGT CLIMBED TO 668 DEGREES FOR 30 SECONDS. VIBRATION FELT IN THE AIRFRAME. PERFORMED ENG OPERATI ONAL OVERLIMITS INSPECTION AFTER EGT OVERTEMP IAW AMM 70-00-04-6-2. NO PHYSICAL DAMAGE NOTED. RAN ENGINE AT FLIGHT IDLE, ALL PATAMETERS CHECKED NORMAL ON THE GROUND IAW AMM 71-00-00. 2 L 7 3 4F 4 F RT A22WE E24NE 20081106 EA 2008 11 6 ASOA200801435 1 20081029 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 933EV 8022 CARGO BAY FLOORBEAM FLOOR PANEL ATTACH FLANGE IS CORRODED AT LBL 27 OUTBOARD FLANGE FS 589. CORROSION APPEARS MINOR AND ISOLATED. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 ASOA200801422 1 20081029 A 3350 STRIP CNDAIR CL600 CL6002B19 1900309 EA CABIN CRACKED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 933EV 8022 FOUR EACH EMER PHOTOLUMINESCENT FLOODLIGHT STRIPS ARE CRACKED. 2 L 7 2 4F RT A21EA 20081107 NE 2008 11 7 PCSA2008103101 2 20081031 A 7261 GARLOCK SEAL BOEING 727 7272J7 138400E NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE LEAKING A PCSA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 17 PCSA 20879 688711 ENGINE 2 OIL TEMPERATURE RED BAND INDICATION, OIL QUANTITY NORMAL 3 GALLONS, ENGINE INSTRUMENT PARAMETERS NORMAL. ENGIN E SHUT DOWN PER ALTERNATE AND ABNORMAL PROCEDURES. WINDMILL AFTER SHUTDOWN 20 MINUTES, OIL PRESSURE 15 PSI. DIVERTED T O SDQ AND PERFORMED UNSCHEDULED LANDING. MAINTENANCE DISCOVERED OIL LEAK AT STARTER GARLOCK SEAL. REPLACED SEAL AND OP ERATIONAL TESTED. FOUND FUEL DE-ICING VALVE INTERMITTENT. REPLACED FUEL DE-ICING VALVE, FUEL OIL COOLER AND OIL TEMPER ATURE BULB AND CONTAMINATED ENGINE OIL FILTER. 2 L 7 3 4F 4 F A3WE E2EA 20081107 EA 2008 11 7 ASOA200801424 1 20081029 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 933EV 8022 LT SIDE FLOOR SUPPORT IS CRACKED 1.0 INCH AT FS 621, WL 73, LBL 40. REPAIRED THE LT FS 621 FLOOR ANGLE IAW BOMBARDIER R EO 601R-53-61-117, REV C ASA EC/TC 601R-53-61-117, INCORPORATED. SUPPLEMENTAL-SDR CLOSED 11/17/2008. 2 L 7 2 4F RT A21EA 20081107 EA 2008 11 7 ASOA200801425 1 20081029 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 933EV 8022 FS 484.0 RBL 36 WL 73.0 INTERCOSTAL FLANGE CRACKED IN RADIUS. 2 L 7 2 4F RT A21EA 20081107 WP 2008 11 7 AALA200802674 1 20081004 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 76200 53290 LGA - EMERGENCY LIGHT AT OVERHEAD AFT GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD AFT GALLEY. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081107 WP 2008 11 7 AALA200802675 1 20081004 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 76200 53290 LGA - FORWARD EMERGENCY LIGHT ON AFT VENTRAL STAIR SIDEWALL INOPERATIVE. REPLACED BATTERY PACK FOR FORWARD EMERGENCY LI GHT ON AFT VENTRAL STAIR SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081106 NM 2008 11 6 DHLA2008745594 1 20080914 A 5313 STRINGER BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT FROM BS 640 TO BS 660 S-26L HAS CORROSION. REPLACED FUSELAGE STRINGER SECTION FROM BS 480 TO BS 680 S-26L IAW B727 SRM 51-10-1. REPAIRED FUSELAGE STRINGER FROM BS 680 TO BS 718 S-26L IAW B727 SRM 53-10 -3 FIG 1 DETAIL 1. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 DHLA2008745589 1 20081022 A 5322 SHEAR TIE BOEING 727 727224 1384076 NM ZONE 100 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 640 BETWEEN S26L AND S27L SHEAR TIE CRACKED. REPLACED FUSELAGE SHEAR TIE SEC TION AT BS 640 BETWEEN S26L AND S-27L IAW B727SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 DHLA2008745592 1 20081010 A 5330 SKIN BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE EXISTING REPAIR DOUBLER DEFORMED AND CORROSION FROM BS 680 TO BS 690 BETWEEN S26L AND S26R. REPAIRED FUS ELAGE SKIN SECTION FROM BS 680 TO BS 693.5 BETWEEN S25L AND S25R DUE TO REPAIR DOUBLER DEFORMED AND CORROSION OUT OF LIM ITS IAW SRM 53-30-3 FIG 12 DETAIL X. 2 L 7 3 4F A3WE 20081106 2008 11 6 M2Z2008F00001 4 20081021 A 2562 BATTERY RKWELL 700 700 7630520 SW ELT DISCHARGED B M2ZR O OTHER O OTHER NR NOT REPORTED 1 GL 19 700CG 35644 70025 BATTERY PACK LEAKING. PREMATURE DEAD BATTERY. DESTROYED ELT. DEFECTIVE BATTERY AND/OR IMPROPER MFG PROCESS OF BATTERY PA CK. (K) 1 L 7 2 3O A12SW 20081106 SO 2008 11 6 C2XA08IA219 1 20080929 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO EMERGENCY EXIT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16951 145063 DURING SCHEDULED MAINT THE EXTERNAL EMERGENCY EXIT LOCATER LIGHT WAS FOUND TO BE INOPERATIVE. MAINT REMOVED AND REPLACED THE LIGHT ASSY, OPERATIONALLY TESTED THE SYSTEM AND CLEARED THE DISCREPANCY. (K) 2 L 7 2 4T RT T00011AT 20081106 EA 2008 11 6 QXEA200801049 1 20081002 A 5230 670BA52030K1 HANDLE CNDAIR CL600 CL6002C10 1390015 EA CARGO DOOR BROKEN A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 19 608QX 10026 GROUND AGENT REPORTS MCD OUTER HANDLE BROKE OFF. FERRIED, RREMOVED AND REPLACED MCD OUTER HANDLE IAW T/C SB670BA-52-030, WO 68578. OPS TEST GOOD GROUND VALVE REACTIVATED. PREFORMED OPS TEST OF GROUND VALVE IAW AMM TASK 21-24-18-710-801-A01. OPS TEST GOOD. (K) 2 L 7 2 4F RT A21EA 20081106 NM 2008 11 6 SWAA085987 1 20081102 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 797MX 27890 FOUND FWD EEPLS COVER LOOSE AT ROW 1 TO ROW 2. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 SWAA085988 1 20081102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 28L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 SWAA085999 1 20081031 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 881, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 SWAA085998 1 20081030 A 5311 6546554 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, NR 5 STOP PAD. REPAIRED FRAME PER SWA ACO. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 SWAA085989 1 20081102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 28L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 SWAA085990 1 20081102 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 SWAA085991 1 20081102 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 782SA 29808 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 43. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 SWAA085992 1 20081101 A 3350 1010421 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 FOUND LT EMERGENCY EXIT BULLNOSE LIGHT COVER MISSING AT ROW 17. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 SWAA085981 1 20081102 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 263WN 32520 FOUND FWD CABIN EEPLS LIGHT LOOSE. REMOVED AND REPLACED EEPLS ASSY PER MM. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 SWAA085993 1 20081102 A 3350 65C27095 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 F3LA2008110300702 1 20081031 A 5313 D53472090010 LONGERON AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 932FR 18 2258 DURING C3 C-CHECK, INSPECTION NOTED LONGERON Y1292 FORWARD OF FRAME 68 HAS CORROSION ON FORWARD INBOARD NUT CLIP HOLE. MAINTENANCE REMOVED CORROSION IN ACCORDANCE WITH A319 SRM 53-00-14, FIGURE 102. ROTO-PROBED HOLES WITH NO DEFECTS NOTED IN ACCORDANCE WITH NTM 51-10-01. ALL WORK ACCOMPLISHED PER ENGINEERING AUTHORIZATION A9-53R-30725. 2 L 7 2 4F RT A28NM 20081106 2008 11 6 M2Z2008F00000 4 20081021 A 2562 BATTERY PACK CESSNA 150 A152 2071836 CE LYC O235 O235* 41505 EA ELT LEAKING B M2ZR O OTHER K FLUID LOSS NR NOT REPORTED 1 GL 17 4958A 47473 A1520916 BATTERY PACK LEAKING. PREMATURE DEAD BATTERY. DESTROYED ELT. DEFECTIVE BATTERY AND/OR IMPROPER MFG PROCESS OF BATTERY PA CK. (K) 1 H 7 1 3O 3 O 3A19 E223 20081106 NM 2008 11 6 QXEA200801061 1 20081003 A 6123 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 19 431QX 4164 AUTO FEATHER FAILED TO ARM ON TAKEOFF. ABORTED TAKEOFF AT 80 KNOTS. MAINT FOUND 64,70,494 ON ENG 1 CHAN A AND CODE 494 O N CHAN B. CLEARED PEC CODES IAW Q400AMM TASK 61-20-36-070-801 FOR BOTH ENGINES. PERFORMED OPS TEST OF AUTOFEATHER SYSTEM IAW AMM TASK 61-20-00-710-801. OPS TEST GOOD - TEST PASSED. GROUND RAN ACFT TO RATING PWR AND AUTO FEATHER ARMED AS REQ UIRED. CHECKED CDS FOR CODES, NO CODES POSTED. RETURN TO SERVICE NO PARTS REPLACED. (K) 2 H 7 2 4T RT A13NM 20081107 WP 2008 11 7 AALA200802677 1 20081003 A 3350 LENS DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 466AA 49596 DFW - EMERGENCY LIGHT AT SEAT ROW 12DEF HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 12DEF. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081107 EA 2008 11 7 ASOA200801427 1 20081029 A 5320 ATTACH ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 933EV 8022 FS 484.0 RBL 27.0 WL 73.0 INTERCOSTAL ATTACH ANGLE CRACKED IN RADIUS. 2 L 7 2 4F RT A21EA 20081107 NE 2008 11 7 USAA920081989 2 20081029 A 7200 8080504062 EEC AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE FAILED A USAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 19 662AW 35863 12122 1274 FLT NR 245 BWI-PHX EMERGENCY LANDING CREW REPORTED LOSS OF POWER EXPERIENCED ON NR 2 ENGINE SEVERAL TIMES. ECAM INDICAT ED ENG 2 STALL. THERE WAS NO ASSOCIATED NOISE OR FAILURE. CREW DECLARED AN EMERGENCY AND RETURNED TO BWI LANDING WITHO UT INCIDENT. ECAM INDICATION FOR ENG 2 SENSOR FAIL AFTER LANDING AND CLASS 2 ENG 2 FADEC FAULT AFTER SHUTDOWN. MX R&R THE ELECTRONIC ENGINE CONTROL AND THE LPC BLEED MASTER ACTUATOR. THE REASON FOR REMOVAL OF THE ACTUATOR COULD NOT BE CO NFIRMED BY THE VENDOR. 2 L 7 2 4F 4 F RT A28NM E40NE 20081107 NM 2008 11 7 USAA920081985 1 20081029 A 5230 SKIN BOEING 737 7374B7 138449C NM ZONE 800 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 1636 24554 CLT MAJOR REPAIR Q5 CHECK NR 03C21952009/002, AFT CARGO DOOR SKIN CRACKED, AFT OF HANDLE. REPLACED AFT CARGO DOOR IAW T ASK CARD 03C21952008. 2 L 7 2 4F RT A16WE 20081107 WP 2008 11 7 AALA200802574 1 20080923 A 5343 3917446505 SUPPORT BRACKET DOUG DC9 DC983 3022083 WP MLG CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 TUL RT DOOR STRUT SUPPORT BRACKET CRACKED 12 INCHES ABOVE HINGE IN WW AT STATION 101. REPLACED RT STRUT SUPPORT IN ACCO RDANCE WITH SRM 51-30-05. 2 L 7 2 4F RT A6WE 20081107 EA 2008 11 7 COMA0860435 1 20081024 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 781CA 7312 FUEL DRAIN FWD OF ACCESS PANELS 640AB AFT DRAIN ATTACH HOLE IS DAMAGED. REAMED AND INSTALLED FREEZE PLUG AT FUEL DRAIN AFT ATTACH HOLE PER COMAIR EA NR 10-5721-02382. 2 L 7 2 4F RT A21EA 20081107 NM 2008 11 7 USAA920081982 1 20081010 A 5347 BAC1520792 SEAT TRACK BOEING 737 7373G7 138447J NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL MAJOR REPAIR C21 CHECK NR 6139598 CORROSION ON CABIN SEAT TRACK AT BS 907 - BS 947, RBL 24.75, WL 208. REPAIRED CAB IN SEAT TRACK AT BS 907 - BS 947, RBL 24.75, WL 208 IAW B737 53-00-52-2R3. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 USAA920081981 1 20081028 A 5512 61C27494 SKIN BOEING 737 7374B7 138449C NM ZONE 300 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT RON MAJOR REPAIR LOG NR 4371367 RT HORIZONTAL STABILIZER LOWER SURFACE HAS A CRACK FORWARD OF CENTER ELEVATOR BALANC E PANEL AT AFT SPAR. REPAIRED RT HORIZONTAL STABILIZER LOWER SURFACE IAW US AIRWAYS TYPICAL REPAIR NR 55-10-07 REV D. 2 L 7 2 4F RT A16WE 20081107 EA 2008 11 7 COMA0860441 1 20081024 A 5311 6013600121 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 640 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 781CA 7312 LT FS 640 FRAME DOUBLER AND BONDED SKIN DOUBLER ARE CRACKED. REMOVED DAMAGED PARTS AND COMPLIED WITH MODIFICATION K601R 36009-3 ON LT FS 640 FRAME AND DOUBLER PER S/B601R-53-061 KIT DRWG. K601R36009 REV B, 601R-53-61-506 REV C AMD 601R53-6 1-569. 2 L 7 2 4F RT A21EA 20081107 EA 2008 11 7 COMA0860440 1 20081024 A 5330 601R32026337 SKIN PANEL CNDAIR CL600 CL6002B19 1900309 EA FS 559 RBL 9-18 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 781CA 7312 FS 559 WEB RT SIDE IS CRACKED BY AILERON BELLCRANK UPPER O/B BOLT HOLE. REMOVED DAMAGE AND INSTALLED A PERMANENT REPAIR DOUBLER ON FS559 BULKHEAD WEB BETWEEN RBL9 AND RBL18. 2 L 7 2 4F RT A21EA 20081107 EU 2008 11 7 MAL2008F00051 1 20081022 A 2613 PUMP SAAB SF340 340B 7860101 EU HYD SYSTEM MALFUNCTIONED A MALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 15 445XJ 340B445 FLIGHT CALLED AROUND THE MBS AREA WITH A MAIN HYDRAULIC PUMP PROBLEM. MAIN HYDRAULIC ACCUMULATOR PRESSURE DROPS FROM 30 00 TO 2000 PSI EVERY 35 SECONDS IN FLIGHT. CREW TALKED TO DISPATCH MXC AND RETURNED TO DTW. WORKED UP NRS FOR FLIGHT T O RETURN TO DTW. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. SYSTEM APPEARS NORMAL ON THE GROU ND. AUTO FUNCTION SEEMS NORMAL. EMERGENCY IB AND OB ACCUMULATOR PRESSURE CAN START AT 3000 PSI. HYDRAULIC QUANTITY VA RIED BETWEEN 80-120 CN IN UPON LANDING WE SMELLED HYDRAULIC FLUID. R&R NLG ACTUATOR IAW JOBCARD NR 323110. OPS CHECK G OOD. 2 L 7 2 4T RT A52EU 20081107 WP 2008 11 7 IXX2008F00099 1 20080805 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK INSPECTION, FOUND AFT LOWER FUSELAGE AFT AND BELOW L-2 AND R-2 DOORS HAS IMPROPER REPAIR AT STA F S 1695, LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRI CATED NEW SKIN. REPAIR DOUBLER, INTERNAL FINGER DOUBLER, AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-2-1, FIGURE 7 SHEETS 1 AND 4 , SRM 53-5-1, FIG 1 ITEM "E", AND DC8 SRM 51-1-8B. (K) 2 L 7 4 4F RT 4A25 20081107 WP 2008 11 7 UPS08853853 1 20081022 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV EXT DOUBLER NOSE GEAR DOOR CUTOUT BS 6.5 TO BS 11 NEEDS VALIDATION. REPAIRED TO SRM 53-02-01 FIG 7. 2 L 7 4 4F RT 4A25 20081107 WP 2008 11 7 UPS08853854 1 20081022 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV EXT DOUBLER BS 8 TO BS 3 L33R CORNER OF NOISE LANDING GEAR DOOR. REPAIRED AS PER 53-03-01. 2 L 7 4 4F RT 4A25 20081107 NM 2008 11 7 SWAA086011 1 20081102 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 503C, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 F3LA2008102700691 1 20081024 A 5320 D5392059220000 PROFILE AIRBUS A319 A319111 3930336 NM ZONE 100 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 920FR 48 1997 DURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION IN THE FORWARD CARGO COMPARTMENT ON PROFILE LOCATED AT STRINGER 38 LEFT BETWEEN FRAME 24A AND FRAME 28. MAINTENANCE REMOVED AND REPLACED PROFILE IN ACCORDANCE WITH A319 SRM 51-72-11 PAGE 1 A ND 2. 2 L 7 2 4F RT A28NM 20081030 NM 2008 10 30 08FDEA04527 1 20081024 A 5210 50794516 WEB BOEING 727 7272D4 138407U NM PAX DOOR CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 MED FWD LWR CORNER INTERIOR SURFACE OF THE LOWER DOOR WEB IS CRACKED. REMOVED LOWER PORTION OF INNER SKIN FOR ACCESS RE F SRM51-30-2 PG 32. REMOVED LWR FWD STOP FITTING REF SRM 51-30-2 PG 8 HAD WEB NDT'ED, AND NO CRACK WAS FOUND, TOOL NR I N22-0043 WAS USED CAL DUE 3/26/09. REINSTALLED INNER SKIN REF SRM 51-30-2 PG 4. REINSTALLED LWR FWD STOP FITTING REF S RM 51-30-2 PG 8. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081030 NM 2008 10 30 08FDEA04582 1 20081027 A 5311 70750063C FRAME BOEING 757 75723A 1384967 NM BS 980 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 AFTER REMOVAL DOUBLER FROM TV MONITOR SUPPORT AT STA 980 SEVERAL HOLES ON FRAME. REMOVED DAMAGE BTW STR 5L AND 5R IAW S RM 53-00-01 REPAIR NR 3. FABRICATED NEW ZEE FRAME REPAIR PER MAE TRAVELER T8/763340. FABRICATED NEW SPLICES PER MAE TR AVELER T8/761973. LOCATED AND DRILLED REPAIR PARTS IAW SRM 53-00-07 REPAIR NR 3 B. FIG 201. DO A HFEC INSPECTION EVERY 12,000 FLIGHT CYCLES AS GIVEN IN NDT PART 6, 51-00-01. REPEAT THIS INSPECTION AT EVERY 12,000 FLIGHT CYCLES INTERVAL S, AS AN ALTERNATIVE, DO A (DVI) INSPECTION AT 9,000 FLIGHT CYCLES INTERVALS AFTER THE INITIAL INSPECTION. THIS IS A CA T "B" REPAIR . 2 L 7 2 4F RT A2NM 20081030 WP 2008 10 30 AALA200802624 1 20080930 A 5320 593666067 FLOOR SUPPORT DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON AFT CARGO FLOORBOARD SUPPORT AT TOP. AREA OF DISCREPANCY WAS 57 INCHES BY 2 INCHES. REPLACED FLOORB OARD SUPPORT IN ACCORDANCE WITH SRM 51-10-1. 2 L 7 2 4F RT A6WE 20081030 SO 2008 10 30 GLBA200810241 1 20081023 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO LT WING CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 71GL 120071 MAJOR REPAIR - DURING SCHEDULED MAINTENANCE THE NR 8 STRINGER WAS FOUND CRACKED ON THE LOWER WING SKIN JUST INBOARD OF R IB NR 9 NEAR WS 2593. MAINTENANCE INSTALLED SPLICE PER EMB SRM 57-20-03. RII INSPECTION COMPLIED PER TASKCARD 8.2.1. 2 L 7 2 4T RT A31SO 20081030 SO 2008 10 30 GLBA200810243 1 20081023 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO LT WING CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 71GL 120071 MAJOR REPAIR - DURING SCHEDULED MAINTENANCE THE NR 10 STRINGER WAS FOUND CRACKED ON THE LOWER WING SKIN JUST INBOARD OF RIB NR 9 AT APPROXIMATELY WS 2443. MAINTENANCE INSTALLED SPLICE IAW SRM 57-20-03. RII INSPECTION COMPLIED PER TASKCARD 8.2.1. 2 L 7 2 4T RT A31SO 20081030 CE 2008 10 30 HSYA20081002 1 20081022 A 3240 BRAKE SYS CESSNA 208 208B 2073701 CE MLG MALFUNCTIONED E HSYA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 05 933FE 208B0033 DURING AN ATTEMPTED LEFT HARD TURN OFF OF THE TAXI WAY ONTO THE RUNWAY THE CREW REPORTED THE AIRCRAFT CONTINUED IN A STR AIGHT LINE AND LOST BRAKING. THE CREW WAS ABLE TO STOP THE AIRCRAFT WITH NO INCIDENT. MAINTENANCE TOWED THE AIRCRAFT T O THE HANGAR. AFTER CYCLING THE BRAKES SEVERAL TIMES THE CREW AND MAINTENANCE PERFORMED TAXI CHECKS. TAXI CHECK GOOD W ITH NO OTHER INCIDENTS. 1 H 7 1 3T A37CE 20081030 CE 2008 10 30 DJFA2008075 1 20081021 A 2120 UNKNOWN BEECH MU300 400A 1155402 CE CABIN ODOR E DJFA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 23 454LX RK327 CREW REPORTED A BURNING SMELL COMING FROM THE FWD EVAP. MAINTENANCE INSPECTED THE AIRCRAFT AND COULD NOT DUPLICATE THE DISCREPANCY. 2 H 7 2 4F RT A16SW 20081030 SO 2008 10 30 C2XA08CL119 1 20081027 A 3232 21180100401 ACTUATOR EMB 145 EMB145XR 3260214 SO NLG DOOR SLOW A C2XA K NONE J WARNING INDICATION AP APPROACH 1 SW 27 14180 11507 4021 0900 CLE FLIGHT 2141 - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE WHEN PUTTING LANDING GEAR DOWN DURING APPROAC H INTO CLE. MAINTENANCE INSPECTED AND REPLACED THE NOSE GEAR DOOR LEFT ACTUATOR. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT 20081030 NM 2008 10 30 SWAA085829 1 20081025 A 5340 0822368 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947D, STR 22L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085832 1 20081027 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER PAE EA. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085833 1 20081027 A 5311 6516301 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 188, STR 17R. REMOVED AND REPLACED FRAME PER PAE EA. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085834 1 20081027 A 5320 6546529 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND COCKPIT FLOOR WEB CRACKED AT BETWEEN BS 188 TO BS 197 STR 17R. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081030 2008 10 30 SWAA085835 4 20081026 A 2565 6949956 CABLE BOEING 737 7373H4 1384600 NM EVAC SLIDE FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND L2 DOOR EMERGENCY SLIDE GIRT BAR CABLE FRAYED. REMOVED AND REPLACED CABLE PER SRM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085850 1 20081028 A 3350 8210248801 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 FOUND LT MID CABIN EMERGENCY EXIT LIGHT COVER MISSING. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085851 1 20081028 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 413WN 29819 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR ESCAPE SLIDE GIRT BAR FWD HOOK LOOSE. SECURED HOOK PER MM. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085856 1 20081028 A 5512 65C25727 SKIN BOEING 737 7373Q8 1384670 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN RIB STA 147 TO RIB STA 157. REPAI RED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081030 NM 2008 10 30 SWAA085858 1 20081028 A 5512 65C25727 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT BS 175, AFT OF L/E. REPAIRED S KIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 SWAA085866 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 DL757081415 1 20081009 A 5320 146N539151 FLOOR SUPPORT BOEING 757 757232 1384965 NM BS 1523 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 CORROSION AROUND NUTPLATE HOLE BS 1523 LBL3 FLOOR SUPPORT RAIL. REPAIRED SUPPORT IAW SRM 53-60-53 FIG 206. 2 L 7 2 4F RT A2NM 20081031 2008 10 31 USAABB08163 4 20081017 A 3497 2TC4725 CIRCUIT BREAKER BOEING 757 7572S7 1384962 NM CDU MALFUNCTIONED A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 905AW 23567 FLT 119 IN CRUISE, EICAS MESSAGES "L GEN OFF" AND "L AC BUS OFF". DISPLAYED WITH THE CORRESPONDING "L GEN OFF" AND "L BUS OFF" LIGHTS ILLUMINATED. A GENERATOR RESET DID NOT CORRECT THE CONDITION. ATTEMPTS TO POWER THE L AC BUSS FROM THE OTHER POWER SOURCES WERE NOT SUCCESSFUL. FLT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED GROUND POWER E XTERNAL CONTACTOR K114, CURRENT TRANSFORMERS T112 & T127, AND BUSS TIE BREAKER C902, WITH NO EFFECT. ALSO, PERFORMED FI M 24-22-00. NO FAULTS FOUND. MX FOUND WHAT WAS BELIEVED TO BE A SHORTED AFT GALLEY FEEDER WIRE, W3538-0005. WIRE STOW ED IN PREPARATION FOR A FERRY FLT WITH THE WIRES DISCONNECTED, THE AC BUSS ISOLATION STILL OCCURRED. PROBLEM ISOLATED T 2 L 7 2 4F RT A2NM 20081031 SO 2008 10 31 CHQA2800207A 1 20081021 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL ZONE 700 FAILED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 294SK 145497 CAE311674 FLIGHT 7790, YOW TO IAD. AFTER TAKEOFF THE FLIGHT CREW RECEIVED A LG AIR/GRND FAIL MESSAGE ON EICAS AND THE LANDING GEA R WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO YOW AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED THE CMC FOR MESSAGE S AND FOUND A PROX SWITCH FAIL CMC MESSAGE. THROUGH FURTHER TROUBLESHOOTING THE NOSE LANDING GEAR WEIGHT ON WHEELS PROX SWITCH WAS FOUND TO BE AT FAULT. THE PROX SWITCH WAS REPLACED AND THE SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081031 EA 2008 10 31 ASOA200801396 1 20081025 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 FLIGHT ATTENDANT REPORTS DIFFICULTY CLOSING MAIN CABIN DOOR. FLT 4941 DEL 23 MINS. 2 L 7 2 4F RT A21EA 20081031 NM 2008 10 31 HALA2008102600829 1 20081026 A 2432 32669001 BATTERY BOEING 767 76733A 1385209 NM APU UNKNOWN A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 582HA 1472 1472 28139 ETOPS SIGNIFICANT SYSTEM - UPON PUSHBACK BEFORE ENG START APU AUTO SHUT DOWN. REMOVED & REPLACED APU BATTERY PER AMM24- 31-04. OPS CHECK OK. PERFORMED APU ECU BITE CK. NO FAULTS NOTED. OK FOR SERVICE. FOUND NO APU ELECTRICAL. REPLACED APU GCU PER AMM24-22-02. NO FAULTS NOTED. PERFORMED FIM 24-20-00 FIG 101. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20081031 NM 2008 10 31 AALA200802334 1 20080820 A 5330 146T32212 SKIN BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 332AA 22331 AFW FUSELAGE SKIN AT STATION 1084 TO 1088 BETWEEN STRINGER 37 LT AND 38 LT HAD CORROSION ON THE OUTER SKIN SURFACE. ARE A OF DISCREPANCY IS 2.4 INCHES BY 4.6 INCHES. REPAIRED PER MRB 767 3274. 2 L 7 2 4F RT A1NM 20081031 WP 2008 10 31 AALA200802541 1 20080922 A 5755 5936832505 FITTING DOUG DC9 DC983 3022083 WP SPOILER CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 76202 53292 GROUND SPOILER FITTING ASSEMBLY AT FORWARD INBD CORNER WING STATION 91 CRACKED. LENGTH OF CRACK IS 1.5 INCH. REPLACED CASTING. 2 L 7 2 4F RT A6WE 20081103 WP 2008 11 3 AALA200802526 1 20080918 A 5311 5936597525 FRAME DOUG DC9 DC982 3022082 WP BS 1060 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70504 49798 TUL FRAME IN AFT CARGO IS CORRODED. AREA OF DISCREPANCY IS 1 INCH BY 2 INCHES WITH A DEPTH OF .072 INCHES. INSTALLED D OUBLER ON FRAME IN AFT CARGO PER ESO 80559 DATED 17 SEP 2008. 2 L 7 2 4F A6WE 20081103 WP 2008 11 3 AALA200802527 1 20080918 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 160-190 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70504 49798 FLOORBOARD SUPPORT IS CORRODED. AREA OF DISCREPANCY IS 1 INCH BY 30 INCHES. REPLACED FLOORBOARD SUPPORT PER SRM 51-01- 00. 2 L 7 2 4F A6WE 20081103 WP 2008 11 3 AALA200802528 1 20080918 A 5320 PAN DOUG DC9 DC982 3022082 WP BS 370-427 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70504 49798 FORWARD CARGO DOOR PAN IS CORRODED. AREA OF DISCREPANCY IS 57 INCHES BY 8 INCHES. REPLACED FORWARD CARGO DOOR PAN PER SRM 53-05-00. 2 L 7 2 4F A6WE 20081103 NM 2008 11 3 KCSA081538 1 20081016 A 5230 DOUBLER BOEING 747 747249F 1384849 NM ACCESS PANEL CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 C2 DOOR ACCESS PANEL HAS CORROSION ON DOUBLER. 2 L 7 4 4F RT A20WE 20081103 NM 2008 11 3 P5CA0801578 1 20081014 A 8012 START VALVE BOEING 747 74746NF 13848BT NM NR 1 ENGINE INOPERATIVE A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 453PA 30811 NR 1 ENGINE START VALVE FAILED. DEFERRED ITEM PER DISPATCH DEVIATIONS GUIDE PROCEDURE ITEM 80-11-1 CAT C, ALLOWING TO D ISPATCH THE ACFT WITH NR 1 ENGINE START VALVE INOP. MANUAL START REQUIRED. 2 L 7 4 4F RT A20WE 20081103 EU 2008 11 3 RMX2008F00005 1 20081015 A 5302 RING UROCOP EC135 EC135P2 5620027 EU TAILBOOM CRACKED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 135CH 3397 0346 WITH THE RELEASE OF EASB EC135-53A-022, A VISUAL INSPECTION REVEALED A CRACK IN THE TAILBOOM TO FENESTRON JUNCTION RING FRAME AFT. THIS EASB HAS NOW ALSO BEEN A SUBJECT OF AN EMERGENCY AD 2008-22-51. 1 G 7 2 3U H88EU 20081103 NM 2008 11 3 USAA920081902 1 20081015 A 5311 6546557 FRAME BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753039/014 CRACK IN FRAME AT BS 887, ABOVE S9R. REPAIRED FRAME AT BS 887, ABOVE S9R IAW TYP ICAL REPAIR NR 53-10-20E. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081903 1 20081015 A 5311 6546554 FRAME BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753039/012 CRACK IN FRAME AT BS 847, ABOVE S9R. REPAIRED FRAME AT BS 847, ABOVE S9R IAW TYP ICAL REPAIR NR 53-10-20E. 2 L 7 2 4F RT A16WE 20081103 WP 2008 11 3 AALA200802537 1 20080929 A 3231 59164605509 VALVE DOUG DC9 DC982 3022082 WP MLG DOORS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 33502 49739 INFLIGHT T9610/29 SEP FCF. AFTER TEST OF ALTERNATE GEAR EXTENSION, GEAR DOOR INDICATION DID NOT GO OUT ON GEAR EXTENSIO N. LANDED TUL WITHOUT INCIDENT WITH RT MLG DOORS OPEN. REPLACED THE LG CONTROL VALVE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081103 WP 2008 11 3 AALA200802539 1 20080922 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 274AA 49271 EMERGENCY LIGHT BATTERY PACK IN CABIN WEAK. REPLACED EMERGENCY LIGHT BATTERY PACK IN CABIN. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F A6WE 20081103 WP 2008 11 3 AALA200802540 1 20080923 A 5311 991184356 FRAME DOUG DC9 DC983 3022083 WP BS 1510 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 76202 53292 LT CANTED FRAME AT TAIL CONE STATION 1510 CRACKED. LENGTH OF CRACK IS 3/4 INCH. INSTALLED DOUBLER IN ACCORDANCE WITH E SO 80559 DATED 22 SEP 2008. 2 L 7 2 4F RT A6WE 20081103 NM 2008 11 3 USAA920081953 1 20081023 A 5414 SKIN BOEING 737 7374B7 138449C NM ZONE 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT MAJOR REPAIR Q5 CHECK NR 03C50754003/011 LT PYLON STRUT SKIN CRACKED AT ACCESS PANEL OPENING 5724. REPAIRED THE LT PYLON STRUT SKIN AT ACCESS PANEL OPENING 5724 IAW US AIRWAYS TYPICAL REPAIR 54-50-07 PART 2 FIGURE 3. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081966 1 20080919 A 5320 65C320747 INTERCOSTAL BOEING 737 7373G7 138447J NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN C18 MAJOR REPAIR NR 6131810 CORROSION ON INTERCOSTAL AT BS986.5, RBL38, WL208. REPLACED INTERCOSTAL IAW SRM 51-40-0 2-OG. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081967 1 20081023 A 5753 6546431280 SKIN BOEING 737 737301 1384611 NM RT WING TE FLAP WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C40727023/007 AND LOG NR 5030908 RT OTBD FOREFLAP HAS NUMEROUS WORKING FASTENERS ALONG LEADING EDGE. REPLACED RT OTBD FOREFLAP. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081968 1 20081025 A 5311 65C22910 FRAME BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03055380546/002 CRACK IN FRAME/SIDE FRAME AT BS 500D AT FASTENER JUST BELOW S13L. REPAIRED FRAME /SIDE FRAME AT BS 500D AT FASTENER JUST BELOW S13L IAW TYPICAL REPAIR NR 53-10-21A. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081969 1 20081024 A 5320 65C10592155 INTERCOSTAL BOEING 737 737301 1384611 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10853028/020 LEVEL 2 EXFOLIATION CORROSION AROUND HOLES ON INTERCOSTAL BETWEEN BS 947 TO BS 96 4, RBL 40. REPLACED INTERCOSTAL BETWEEN BS 947 TO BS 964, RBL 40 IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081970 1 20081023 A 5311 65C22910 FRAME BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03C20853011/005 CRACK IN FRAME AT LIGHTNING HOLE AT BS 500D BETWEEN S20R TO S21R. REPAIRED FRAME AT LIGHTNING HOLE AT BS 500D BETWEEN S20R TO S21R IAW SRM 53-00-07. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081971 1 20081025 A 5311 65C32351 FRAME BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03C20853011/012 CRACK AT FRAME 500E BETWEEN S20L AND S21L. REPAIRED FRAME 500E BETWEEN S20L AND S21L IAW SRM 53-00-07, REPAIR 13. 2 L 7 2 4F RT A16WE 20081103 WP 2008 11 3 AALA200802336 1 20080910 A 3397 WIRE HARNESS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 255AA 49287 LGA EMERGENCY LIGHT AT SEAT 21D INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT SEAT 21D. SYSTEM GROUND CHECKED NO RMAL OPS. 2 L 7 2 4F A6WE 20081103 NM 2008 11 3 AALA200802385 1 20080920 A 2822 PUMP BOEING 737 737823 13844CB NM FUEL SYSTEM INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 972AN 30097 TPA INFLIGHT T465/20SEP MIA TO DFW. WHEN FUEL CENTER PUMPS WERE TURNED ON LOW PRESSURE INDICATION FOR BOTH PUMPS ILLUMI NATED. CENTER TANK PUMPS WOULD NOT OPERATE DURING FLIGHT. LANDED TPA WITHOUT INCIDENT. FOUND LT CENTER FUEL PUMP NOT TRANSFERRING FUEL. FOUND NR 2 AND CENTER FUELING SWITCH OPEN ON FUELING PANEL ON ARRIVAL. ACFT FUELED TO 14000 POUNDS AND PRIMED CENTER PUMPS. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 AALA200802393 1 20080920 A 3350 BATTERY PACK BOEING 737 737823 13844CB NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 944AN 29535 DFW EMERGENCY LIGHT AT LT NR 2 DOOR INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 NWAA084633130 1 20081015 A 3350 NWAD321430 BATTERY PACK AIRBUS A319 A319114 3930350 NM EMERGENCY LIGHTS FAULTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 330NB 1549 RT EMERGENCY EGRESS BATTERY SHOWS BATTERY FAULT DURING TEST. REPLACED RT BATTERY. CHECKS OK. 2 L 7 2 4F RT A28NM 20081103 EU 2008 11 3 NWAA084613306 1 20081015 A 3350 BATTERY PACK AIRBUS 330 A330323 3940030 EU EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 806NW 0578 BATTERY EPSU 12WL DOOR 1 FAILED CAPACITY CHECK, REPLACED BATTERY AND TESTS OK. 2 L 7 2 4F RT A46NM 20081103 EU 2008 11 3 NWAA084663304 1 20081018 A 3350 NWAD321430 BATTERY PACK AIRBUS 330 A330323 3940030 EU EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 804NW 0549 BATTERY EPSU 14WL MSG DURING TEST. REPLACED BATTERY AND TESTS OK. 2 L 7 2 4F RT A46NM 20081103 WP 2008 11 3 NWAA084659865 1 20081018 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 774NC 47776 DURING LINE CHECK MX FOUND THAT THE EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MX R&R THE BATTERY PACK AND THE LIG HTS RETURNED TO AN OPS CONDITION. 2 L 7 2 4F RT A6WE 20081103 EU 2008 11 3 NWAA084683236 1 20080929 A 5340 ATTACH ANGLE AIRBUS 320 A320212 3930322 EU FUSELAGE CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 336NW 355 DURING H CHECK FOUND CORROSION ON ATTACH FLANGE OF RT AFT PAX DOOR SILL PLATE. REPAIRED PER EA 32-214374. 2 L 7 2 4F RT A28NM 20081103 EU 2008 11 3 NSVA08038 1 20081027 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU ZONE 100 DISCHARGED A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 344CJ 344 ONE GROUP OF INTERIOR EMERGENCY LIGHTS WILL NOT TEST. REPLACED POWER SUPPLY 22LN BATTERY WAS EVIDENTLY DEAD. 2 L 7 2 4T RT A52EU 20081103 NM 2008 11 3 USAA920081845 1 20081008 A 5320 INTERCOSTAL BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, INTERCOSTAL ANGLE CRACKED AT BS 291 BETWEEN S9R & S10R OF FWD SERVICE DOOR. REPAIRED INTERCOST AL ANGLE AT BS 291 BETWEEN S9R & S10R OF FWD SERVICE DOOR IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081846 1 20081008 A 5320 INTERCOSTAL BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, INTERCOSTAL ANGLE CRACKED AT BS 294 BETWEEN S10R & S11R OF FWD SERVICE DOOR. REPAIRED INTERCOS TAL ANGLE AT BS 294 BETWEEN S10R & S11R OF FWD SERVICE DOOR IAW B737 SRM 51-70-11 & BOEING DRAWING NR 6545807. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081847 1 20081008 A 5340 STRINGER CLIP BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, STRINGER TIE CLIP CRACKED AT FRAME BS 727B, S4L. REPLACED STRINGER TIE CLIP AT FRAME BS727B, S 4L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 WRLA2008087 1 20081006 A 5730 SKIN DOUG MD11 MD11F 3023600 NM CENTER WING SKIN CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHECK, MX FOUND CENTER WING TANK UPPER SKIN SURFACE CORROSION AT STA Y1229, X-100- -120. REPAIRED THE CEN TER WING TANK UPPER SKIN CORROSION IAW EI W2008A57B-1061 REV.00 2 L 7 3 4F RT A22WE 20081103 NM 2008 11 3 WRLA2008086 1 20081006 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHECK, MX FOUND M/D SEAT TRACK CORROSION AT STA Y466 TO Y470, X-58.5. REPAIR SEAT TRACK CORROSION IAW ENG INEERING INSTRUCTION W2008A53B-1092 REV 00, W2008A53B-1092 REV 01, AND W2008A53-1092 REV 02. 2 L 7 3 4F RT A22WE 20081103 NM 2008 11 3 WRAL2008082 1 20081006 A 7110 FRAME DOUG MD11 MD11F 3023600 NM NR 3 COWLING CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHECK, MX FOUND NR 3 ENGINE LT CORE COWL AFT FRAME CRACK AT 9 O’CLOCK POSITION. OPEN 2 L 7 3 4F RT A22WE 20081103 NM 2008 11 3 WRLA2008081 1 20081006 A 5730 SKIN DOUG MD11 MD11F 3023600 NM CENTER WING TANK CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHECK, MX FOUND CENTER WING TANK LT UPPER SKIN SURFACE CORROSION AT STA Y1159-1239, X27-120. REPAIRED IAW ENGINEERING INSTRUCTION W2008A57B-106 REV 00. 2 L 7 3 4F RT A22WE 20081103 NM 2008 11 3 WRLA2008079 1 20081006 A 5730 SKIN DOUG MD11 MD11F 3023600 NM CENTER WING TANK CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHECK, MX FOUND CENTER WING TANK RT UPPER SKIN SURFACE CORROSION AT STA Y1150-1239, X-8 TO -120. REPAIRED CENTER WING TANK UPPER SKIN CORROSION AREA IAW ENGINEERING INSTRUCTION W2008A57B-1061 REV 00. 2 L 7 3 4F RT A22WE 20081030 WP 2008 10 30 AALA200802627 1 20080930 A 5330 7024T3 SKIN DOUG DC9 DC983 3022083 WP BS 1380 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CRACK FOUND IN AIRCRAFT SKIN ABOVE LEFT ENGINE PYLON. CRACK LENGTH 2/32 INCH. INSTALLED DOUBLER IN ACCORDANCE WITH AAR D 53-30-00-02. 2 L 7 2 4F RT A6WE 20081030 NM 2008 10 30 DLM88081409 1 20081023 A 5330 99115311 SKIN DOUG MD88 MD88 3023688 NM FS 560-655 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 917DL 49573 LIGHTNING STRIKES ON WINDOW BELT AT WINDOWS 19L, 20L, AND 23L FS 560-655. 2 L 7 2 4F RT A6WE 20081031 SO 2008 10 31 RAIA2008102800004 1 20081024 A 3010 ANTI-ICE SYSTEM EMB 145 EMB145 3260210 SO MALFUNCTIONED A RAIA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 807HK 145119 DURING CRUISE, CREW REPORTED RECEIVING A WING ANTI-ICE FAIL MESSAGE ON THE EICAS WHILE FLYING IN ICING CONDITIONS. MAIN TENANCE PERFORMED AN OPERATIONAL CHECK OF THE ANTI-ICING SYSTEM WITH NO DEFECTS NOTED. DISCREPANCY COULD NOT BE DUPLICA TED. 2 L 7 2 4F RT T00011AT 20081031 NM 2008 10 31 HNAA0800309 1 20081024 A 5697 CONNECTOR PPG DHAV DHC8 DHC8102 2809003 NM WINDSHIELD SHORTED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 07 808EX 2671 2671 07046H5849 299 DURING DESCENT A BURNING ODOR WAS DETECTED IN THE COCKPIT. UPON INVESTIGATION, THE L1 CONNECTOR ON THE CO-PILOTS WINDSH IELD WAS FOUND TO BE BURNT. THE WINDSHIELD WAS REMOVED AND REPLACED AND OPS CHECKED GOOD. AIRCRAFT WAS THEN RELEASED F OR SERVICE. 2 H 7 2 4T RT A13NM 20081031 NM 2008 10 31 ASAA0843667 1 20081026 A 5210 65299913 GUIDE ARM BOEING 737 7374Q8 138447Q NM L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 773AS 25106 L1 DOOR DOES NOT CLOSE. ADJUSTED GUIDE ARM ONE FLAT TO PARALLEL DOOR CLOSING. OPS CHECK NORMAL REF 52 11 21. 2 L 7 2 4F RT A16WE 20081031 NE 2008 10 31 DL76L081450 2 20081027 A 7510 80217010 SHUTOFF VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE FAULTED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 181DN 25986 727893 LEFT ENG ANTI-ICE AFTER TAXI. FOUND HPSOV AT FAULT. FWD TO MEL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081031 NM 2008 10 31 ASAA0843674 1 20081007 A 5753 SKIN BOEING 737 737490 1384715 NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 767AS 27081 RT INBOARD AFT T/E FLAP UPPER SURFACE HAS 2 EA DENTS 3 INCHES OUTBOARD OF INBOARD EDGE. PREPPED DAMAGED AREAS, FABBED D OUBLER AND BONDED THE REPAIR IAW B737 400 SRM 51 70 10 REP 2. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 CALA0801014 1 20081028 A 5315 141T51479 FLOORBEAM BOEING 767 767424ER 1385270 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76054 29449 BODY STATION 246 FLOORBEAM LBL 40 UPPER MID CHORD FOUND CRACKED. BODY STATION 246 FLOORBEAM LBL 40 UPPER MID CHORD REPA IRED PER EC/RA 5310-04859. 2 L 7 2 4F RT A1NM 20081031 CE 2008 10 31 DXTA2008102903326 1 20081028 A 3260 WARNING LIGHT CESSNA 560 560XL 2076702 CE COCKPIT ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 630QS 5605130 GEAR "UNLOCK" LIGHT ILLUMINATED AFTER TAKEOFF. 2 L 7 2 4F RT A22CE 20081031 SO 2008 10 31 C2XA08SH131 1 20081026 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CRACKED A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 16981 145208 SHV DURING C CHECK THE LT OMEGA BEAM WAS FOUND TO BE CRACKED AT RIVETS AT FRAMES 21 AND 22. MX PERFORMED A DOUBLER REPA IR IAW CONTINENTAL EXPRESS EC5320-01426. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081031 NM 2008 10 31 AALA200802392 1 20080920 A 3350 BATTERY PACK BOEING 737 737823 13844CB NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 944AN 29535 DFW EMERGENCY LIGHT AT RT NR 2 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RT NR 2 DOOR. SYSTEM GRO UND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081103 SO 2008 11 3 C2XA08IA227 1 20081016 A 3260 23092900401 UPLOCK EMB 145 EMB145LR 3260212 SO NLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13964 22989 145123 BTR FLIGHT 2789. THE CREW REPORTED A LG LEVER DISAGREE MSG IN FLIGHT AND THE NOSE GEAR WOULD NOT RETRACT. THE ACFT RET URNED TO BTR WHERE IT LANDED WITHOUT INCIDENT. THE ACFT WAS FERRIED TO IAH WHERE MX R&R THE NLG UPLOCK BOX. OPS CHECKE D WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081103 CE 2008 11 3 FFSA200800006 1 20081015 A 3240 BRAKE SYS BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA HARTZL HCB5M HCB5MP3 GL PILOTS MALFUNCTIONED A FFSA O OTHER O OTHER NR NOT REPORTED 1 AL 01 575P UC95 PILOT’S RT BRAKE PEDAL WENT TO THE FLOOR WITH LITTLE OR NO BRAKING ACTION UPON LANDING. CO-PILOT’S BRAKE OPERATION WAS NORMAL. PRESSURE TESTED SYSTEM NO LEAKS NOTED. SERVICED HYDRAULIC RESERVOIR AND BLED BRAKE SYSTEM. BRAKE SYSTEM OPS C HECK SATISFACTORY. 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P44GL 20081103 NM 2008 11 3 USAA920081892 1 20081014 A 5744 65C344837 SPINDLE BOEING 737 7374B7 138449C NM ZONE 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 450UW 24933 PIT FPBH MAJOR REPAIR LOG NR 4352180 AND 03T30757001 OTBD LT SPINDLE SHOWS CRACK 60% AT 35 THRU GATE VERTICALLY TO 40% A T 50 HORIZONTALLY. REPLACED SPINDLE IAW B737 MM 27-51-44-404-006. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081904 1 20081015 A 5311 6546552 FRAME BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753039/011 CRACK IN FRAME AT BS 827 BETWEEN S8R AND S9R. REPAIRED FRAME AT BS 827 BETWEEN S 8R AND S9R IAW TYPICAL REPAIR NR 53-10-20E. 2 L 7 2 4F RT A16WE 20081103 WP 2008 11 3 AALA200802531 1 20080919 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP BS 1003-1155 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70504 49798 CORROSION FOUND ON RT CARGO TIE DOWN TRACK IN AFT CARGO. AREA OF DISCREPANCY IS 1 INCH BY 4 INCHES WITH A DEPTH OF .090 INCH. INSTALLED NEW RT CARGO TIE DOWN TRACK IN AFT CARGO PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081103 EU 2008 11 3 USAA920081952 1 20081023 A 3350 1013083 LIGHT AIRBUS 320 A320231 3930325 EU ZONE 200 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 633AW 82 LOG PAGE 4451328 FLT NR 605 LAS - PHX EMERGENCY LIGHT SINGLE RED WALL MOUNTED EMERGENCY LIGHT ON LT WINDSCREEN INOPERATI VE. MX R&R THE WALL MOUNTED LIGHT ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081103 NM 2008 11 3 USAA920081958 1 20081022 A 5320 65C10592151 INTERCOSTAL BOEING 737 737301 1384611 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT MAJOR REPAIR Q3 CHECK NR 03C10853028/007 LEVEL 2 CORROSION ON INTERCOSTAL AT BS 955, LBL 51. REPLACED INTERCOSTAL A T BS 955, LBL 51 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081103 NE 2008 11 3 AALA200802388 2 20080920 A 7323 FFG022AD GOVERNOR BOEING 757 757223 1384957 NM RROYCE RB211 RB211535* NE NR 1 ENGINE INOPERATIVE A AALA A UNSCHED LANDING R F J PARTIAL RPM/PWR LOSS FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 21 690AA 25696 31116 LAX INFLIGHT T285/20SEP. AT ABOUT 18000 FT ACFT YAWED TO THE LT AND ENGINE INSTRUMENTS SHOWED REDUCED POWER ON NR 1 ENG INE. FUEL FLOW WAS 3000 LBS. LESS ON NR 1 ENGINE. NR 1 ENGINE WOULD NOT PRODUCE FULL POWER WITH LT THROTTLE PUSHED TOW ARDS FULL FORWARD. CREW COULD NOT CONTROL YAW. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED FUEL FLOW GOVERN OR FOR NR 1 ENGINE. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F 4 F RT A2NM E12EU 20081103 EU 2008 11 3 NSVA08038A 1 20081025 A 3350 6013211 BATTERY SAAB SF340 340B 7860101 EU ZONE 100 DISCHARGED A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 369PX 295 DURING OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM ON A LINE CHECK 3 FLOOR PROXIMITY AND 3 EMERGENCY COVE LIGHTS WER E FOUND NOT TO BE ILLUMINATING. EMERGENCY LIGHT POWER SUPPLY 22LN WAS REPLACED IAW COLGAN AIR WORK CARD 33-50-02S AND S YSTEM CHECKED SATISFACTORILY. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 20081103 NM 2008 11 3 USAA920081844 1 20081008 A 5320 65528942 FLOOR SUPPORT BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, FLOOR SUPPORT CRACKED AT BS 540, RBL 2. REPLACED FLOOR SUPPORT AT BS 540, RBL 2 IAW SRM 51-10- 02. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 WRLA2008084 1 20081006 A 5313 LONGERON DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHECK, MX FOUND FUSELAGE FRAME AND LONGERON TO HAVE HEAT DAMAGE AT STA Y 6-90 TO Y 1139, L27L. REPAIRED IAW ENGINEERING INSTRUCTION W2008A53B-984 REV 00, W2008A53-984 REV 01, W2008A53B-984 REV 02, AND W2008A53B-984 REV 03 TO CLARIFICATION THE HEAT DAMAGED PARTS HAVE BEEN CONSIDERED AS SERVICEABLE AND CONTINUED USE. 2 L 7 3 4F RT A22WE 20081103 NM 2008 11 3 HNA2008F00052 1 20080812 A 5347 85320490136SP SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 931HA 51228 132 SEVERAL SPOTS OF MINOR CORROSION FOUND ON RT INBD SEAT TRACK FROM STA X259 TO X597. REMOVED CORROSION IAW RD8-53-1339 F ROM X426 TO X526, R&R SEAT RAIL FROM X182 TO X425 AND X526 IAW SRM 51-40-00. 2 H 7 2 4T RT A13NM 20081103 NM 2008 11 3 HNAA0800303 1 20080812 A 5347 85330469001 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 931HA 51228 132 SEVERAL SPOTS OF MINOR CORROSION FOUND ON RT INBD SEAT TRACK FROM STA X259 TO X597. REMOVED CORROSION IAW RD8-53-1339 F ROM X426 TO X526, R&R SEAT RAIL FROM X182 TO X425 AND X526 IAW SRM 51-40-00. 2 H 7 2 4T RT A13NM 20081104 NM 2008 11 4 UPS08553759 1 20081016 A 5420 SUPPORT BOEING 757 75724APF 1384969 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 451UP 27739 INSPECTION TYPE:MOD FAIRING SUPPORT STRUCTURE SEAL SUPPORT CRACKED. REPLACED SEAL SUPPORT PER SRM. 2 L 7 2 4F RT A2NM 20081104 WP 2008 11 4 UPS08853645 1 20081016 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV INSTALL EXTERNAL SKIN DOUBLERS AT STA -88 TO -50 AND -29 TO 7 L21R. INSTALLED DOUBLERS IAW SRM DC-8 53-02-01 FIG 007. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853646 1 20080921 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV EVALUATION ESN 89420041016 N/R 721564 FOWARD ENTRY DOOR AFT LOWER JAMB REPAIR FOR ELONGATED HOLES. F AB NEW WEB IAW DC8 SRM 53-02-00 FIG 25 AND DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853648 1 20081002 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV STA-53 TO -89 RBL TO RBL 42 DOUBLER NEEDS VALIDATION FOR REPAIR 894-F 3-11. REPAIRED BY SR08530026 A ND SRM 53-2-1. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853650 1 20081005 A 5730 DOUBLER DOUG DC8 DC873F 302199F WP RT WING UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV RT UPPER LEADING DOUBLER NEEDS VALIDATION AT STA XFS627 FAIL APP H ST STEP 5 894-W4-12 REPAIRED I AW 57-2-1 AND 51-01-04. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853654 1 20081015 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV STA 904 OCTAGON DOUBLER REINSTALL DOUBLER. INSTALLED DOUBLER 51-01-08 AND DALFORT XEA X8-53-298. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853655 1 20080921 A 5310 DOOR FRAME DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN89419971106 ORIG NR 534710 R-1 DOOR AFT DOOR JAMB REPAIR FOR ELONGATED HOLES (FUSELAGE FRAME). EXISTING REPAIR ACCOMP IAW DWG UPS DC8-53A-011A. RFTS N894UP-12-2027. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853656 1 20080921 A 5320 WEB DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN 89419911026. ORIGINAL NR 303033. CORROSION REPAIR TO WEB AND ANGLE AT AFT PASS DOOR FS 1615-1625. REPAIR SATISFIES INTENT AND GUIDELINES OF DC8 SRM 53-2-0 FIG 001D. RF TS 894UP-20-20265 . 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853658 1 20080917 A 5720 3751686501 FLANGE DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV RT WING LEADING EDGE AUX TANK AFT INBOARD SIDE VENT TUBE FLANGE CRACKED. REMOVED, REPAIRED, REINSTAL LED FLANGE IAW DCI MM 20-12-00-2. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 AALA200802383 1 20080919 A 3350 OL1098BPEGPL LAMP DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 436AA 49454 DFW EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT A6WE 20081104 NM 2008 11 4 AALA200802582 1 20080910 A 5522 SKIN BOEING 767 767323 1385205 NM RT ELEVATOR DELAMINATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 344AN 33083 OTBD ELEVATOR RT LOWER SURFACE HAS DELAMINATION AT ELEVATOR STATION 229. AREA OF DISCREPANCY IS 1 INCH. ACCOMPLISHED R EPAIR IN ACCORDANCE WITH SRM 51-70-04 AND MRB 767-3289. 2 L 7 2 4F RT A1NM 20081104 WP 2008 11 4 AALA200802382 1 20080919 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 436AA 49454 DFW EMERGENCY LIGHT EXIT SIGNS AT AFT OVERWING LT AND RT INOPERATIVE. REPLACED BATTERY PACK AT STATION 900 FOR EMERGENC Y LIGHT EXIT SIGNS AT AFT OVERWING LT AND RT. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081104 NE 2008 11 4 COMA0870028 2 20081026 A 7200 ENGINE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE LEFT VIBRATION A COMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 371CA 11480 10082 965444 LT ENGINE N2 VIB ON CLIMBOUT FROM CVG. ACFT RETURNED TO CVG. LANDED SAFELY. R&R LT ENGINE. 2 L 7 2 4F 4 F RT A21EA E00063EN 20081211 WP 2008 12 11 AALA200802380 1 20080919 A 3350 0202226001 SHROUD DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 DFW EMERGENCY LIGHT AT SEAT 22D HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHEC KED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081104 EA 2008 11 4 COMA0860433 1 20081026 A 5720 CHANNEL CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 588SW 7069 DURING HMV 7 LT WING PLANK INSPECTION NDT FOUND CRACK INDICATION AT FUEL DRAIN MOUNT HOLE, FWD HOLE OF BOOST PUMP DRAIN ASSY, BETWEEN WS 0.00 AND WS 22.5, STR 5 AND STR 7. DAMAGE REMOVED BY OVERSIZING HOLE AND INSTALLING FREEZE PLUG PER EA 10-5721-02400. 2 L 7 2 4F RT A21EA 20081104 WP 2008 11 4 UPS08853674 1 20081005 A 5280 STOP DOUG DC8 DC873F 302199F WP NLG DOOR MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV LT FWD NLG DOOR BUFFER STOP MISSING. REPLACED FWD NLG DOOR BUFFER STOP IAW DC8 MM 32-22-01-5. 2 L 7 4 4F RT 4A25 20081104 EA 2008 11 4 COMA0860430 1 20081023 A 2916 73031 RESERVOIR CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 518CA 25629 7816 AFTER TAKE OFF NOSE GEAR DID NOT RETRACT. RECEIVED GEAR DISAGREE AND RED HASH MARKS FOR NOSE. COMPLIED WITH QRH, ALL G EAR EXTENDED, RETURNED YYZ AND LANDED WITHOUT INCIDENT. REPLACED NR 3 HYDRAULIC RESERVOIR. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 20081104 WP 2008 11 4 AALA200802578 1 20080922 A 5755 SUPPORT FITTING DOUG DC9 DC983 3022083 WP RT WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 TUL RT OTBD SIDE OF GROUND SPOILER SUPPORT FITTING CRACKED. REPLACED SUPPORT FITTING IN ACCORDANCE WITH SRM 51-30-05. 2 L 7 2 4F RT A6WE 20081104 WP 2008 11 4 AALA200802579 1 20080919 A 2560 BRACKET DOUG DC9 DC983 3022083 WP GIRT BAR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 GIRT BAR BRACKET AT AFT SERVICE DOOR HAS CORROSION. AREA OF DISCREPANCY IS 4 INCH BY 4 INCH WITH A DEPTH OF .030 INCH. REPLACED BRACKET IN ACCORDANCE WITH SRM 51-01. 2 L 7 2 4F RT A6WE 20081104 NM 2008 11 4 AALA200802583 1 20080911 A 5320 146T80811 SILL BOEING 767 767323 1385205 NM BS 1343 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 344AN 33083 AFW OUTER CHORD AT AFT CARGO DOOR CUTOUT LOWER MAIN SILL HAD CORROSION AT STATION 1343. AREA OF DISCREPANCY IS 1 INCH B Y 1 INCH. ACCOMPLISHED REPAIR IN ACCORDANCE WITH SRM 51-00-06 AND MRB 767-3288. 2 L 7 2 4F RT A1NM 20081104 WP 2008 11 4 AALA200802584 1 20080926 A 5313 LONGERON DOUG DC9 DC983 3022083 WP BS 1418 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 970TW 53620 LONGERON 2 RT HAS 1 INCH CRACK AT STATION 1418. ACCOMPLISHED SPLICE REPAIR IN ACCORDANCE WITH AARD 53-30-00-2. 2 L 7 2 4F RT A6WE 20081104 WP 2008 11 4 AALA200802585 1 20080926 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7538A 49992 CORROSION ON CUSP MEMBRANE BELOW G1 GALLEY DRAIN PAN BETWEEN STATIONS 160 TO 168. AREA OF DISCREPANCY IS 6 INCHES BY 8 INCHES. INSTALLED DOUBLER UNDER G1 GALLEY DRAIN PAN IN ACCORDANCE WITH AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081104 NM 2008 11 4 AALA200802378 1 20080919 A 2750 FSEU BOEING 767 767323 1385205 NM TE FLAPS INOPERATIVE A AALA O OTHER J WARNING INDICATION DE DESCENT 1 SW 21 351AA 24032 HNL INFLIGHT T5/19SEP. CREW REPORTED FLAPS WOULD NOT EXTEND DURING DESCENT. LANDED HNL WITHOUT INCIDENT. REPLACED FLA P SLAT ELECTRONICS UNIT (FSEU). SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081104 WP 2008 11 4 UPS08853725 1 20081021 A 5320 WEB DOUG DC8 DC871F 302199D WP FUSELAGE PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV FLOOR WEB AT STA 620-640 LBL 45 HAS SMALL PUNCTURE. INSTALLED DOUBLER SRM 53-02-00. 2 L 7 4 4F RT 4A25 20081104 SW 2008 11 4 QML2008F00018 1 20081004 A 2910 212076153001 LINE BELL 412 412 1182202 SW HYD SYSTEM LEAKING E QMLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 NM 03 405LN 33025 RECEIVED A MASTER CAUTION LIGHT WITH AN ASSOCIATED HYD CAUTION LIGHT. NR 2 HYD PRESSURE GAUGE INDICATED 0 PRESSURE. REF ERRED TO CHECKLIST AND MANEUVERED ACFT FOR LANDING. AFTER COMPLETING ALL IMMEDIATE ACTION AND CHECKLIST STEPS, WEATHER, TERRAIN AND DISTANCE TO NEAREST FACILITY CONSIDERED, WE PERFORMED A PRECAUTIONARY LANDING AND NOTIFIED MX AND MANAGEME NT. MX WAS ABLE TO IDENTIFY THAT A HYDRAULIC LINE ASSY HAD A SLOW LEAK, DEPLETING HYD SYSTEM TO APPROXIMATELY 3/4 QUART . SYSTEM FELL OFFLINE. TORQUED LINE ASSY AND RESERVICED SYS. GROUND RUN FOR 30 MINUTES, OPS CHECKED & LEAK CHECKED, F OUND SERVICEABLE. 1 G 7 2 4U H4SW 20081104 WP 2008 11 4 UPS08853726 1 20081002 A 5720 STRUCTURE DOUG DC8 DC871F 302199D WP WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATE EFN 7022004 ORIGINAL NRC 750568. REPAIRED PER SRM 57-02-00. 2 L 7 4 4F RT 4A25 20081031 CE 2008 10 31 DXTA2008102703316 1 20081024 A 3220 LANDING GEAR CESSNA 750 750 2076810 CE NLG MALFUNCTIONED E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 943QS 7500043 HIGH SPEED ABORT ABOUT 102 KTS; HAD NOSE WHEEL SHIMMY. 2 L 7 2 4J RT T00007WI 20081107 NM 2008 11 7 SWAA086012 1 20081102 A 5330 6545772 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 731C TO 733C, STR 4R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086017 1 20081102 A 3350 079123 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 EEPLS LENS MISSING AT FWD END. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086025 1 20081104 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN AT L1 DOOR LOWER HINGE CUTOUT CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086026 1 20081104 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN AT L1 DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086027 1 20081104 A 5313 6562276 ANGLE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE STRINGER ANGLE CRACKED AT BS 301, STR 10L. REPAIRED ANGLE PER SRM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086018 1 20081101 A 5330 6546765 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 511SW 24188 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 1. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086019 1 20081103 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 4L. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086036 1 20081104 A 3350 20121 RETAINER BOEING 737 7373H4 1384600 NM BATTERY CHARGER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED SPV CHECK, FOUND RT EMERGENCY LIGHT BATTERY CHARGER RETAINER BROKEN. REMOVED AND REPLACED RETAINER PER MM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086038 1 20081102 A 3350 101331 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT ROW 12. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086001 1 20081102 A 3350 3003432 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 223WN 32492 DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR EXTERNAL EMERGENCY EGRESS LIGHT INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086008 1 20081103 A 5322 65C38654 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SHEAR TIE CRACKED AT BS 520, BETWEEN STR 21R AND STR 22R. REPAIRED SHEAR TIE PER SRM & BAC DRAWING. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 2008UALA06332 1 20081102 A 3030 ANTI-ICE SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE PITOT HEAT MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 837UA 1474 PITOT HEAT & AUTO PILOT PROBLEMS. FLIGHT DIVERTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081107 NM 2008 11 7 2008UALA06333 1 20081103 A 2120 UNKNOWN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY SMOKE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 182UA 25279 SMOKE IN THE GALLEY. RTFL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081107 NM 2008 11 7 2008UALA06334 1 20081031 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 GALLEY BETWEEN DOORS 5R AND 5L RIGHT SIDE CROSS EEL LIGHT INOPERATIVE. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 20081107 NM 2008 11 7 2008UALA06335 1 20081031 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 SEATS 46 THRU 54L EEL LIGHT INOP. REPAIRED SHORT AT 54L. 2 L 7 4 4F 4 F RT A20WE E24NE 20081106 NM 2008 11 6 2008UALA06312 1 20081028 A 2560 P2070003100 FLASHLIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 585UA 26709 HIGH INTENSITY FLASHLIGHT AT DOOR 2, LT SIDE IS INOP, PER FLIGHT ATTENDENT. REPLACED AND CHECKED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081106 EU 2008 11 6 UPS08153827 1 20081030 A 5330 SKIN AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 122UP 0807 INSPECTION TYPE:N/A LIGHTNING STRIKE TO FASTENER 1 INCH FWD OF FRAME 11. REPAIRED PER EO A300-5330-31036-A. 2 L 7 2 4F RT A35EU 20081106 EU 2008 11 6 UPS08153846 1 20081031 A 3350 LENS AIRBUS A300 A300F4622R 3930360 EU CABIN BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 126UP 0810 INSPECTION TYPE:N/A EMERGENCY LIGHT LENS BROKEN RED D387788. REMOVED AND REPLACED LENS ASSY PER M/M 33-51-17-04. 2 L 7 2 4F RT A35EU 20081106 EU 2008 11 6 MALA080186 1 20081021 A 3222 BOLT SAAB SF340 340B 7860101 EU NLG MISSING A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425XJ 340B425 NLG UPPER TORQUE LINK PIN BOLT MISSING HEAD. REPLACED BOLT P/N NAS1304-25D. 2 L 7 2 4T RT A52EU 20081106 EU 2008 11 6 MALA080187 1 20081021 A 5220 DOOR SAAB SF340 340B 7860101 EU EMERGENCY EXIT DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425XJ 340B425 DENTS NOTED IN RT EMERGENCY EXIT DOOR. REPAIRED IAW EO S52147 AND S52028. 2 L 7 2 4T RT A52EU 20081106 EU 2008 11 6 MALA080189 1 20081021 A 5753 SKIN SAAB SF340 340B 7860101 EU TE FLAP GOUGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 425XJ 340B425 GOUGE NOTED IN LT FLAP UPPER SKIN. REPAIRED IAW EO S51031. 2 L 7 2 4T RT A52EU 20081106 EA 2008 11 6 ASOA200801433 1 20081101 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR JAMMED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 PASSENGER BOARDING DOOR JAMS CLOSED AND LOCKED AT TIMES IS TO UNLOCK AND OPEN FROM BOTH INSIDE AND OUTSIDE. FLT 5276 DE L 59 MINS. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 ASOA200801434 1 20081030 A 5320 MOUNT BRACKET CNDAIR CL600 CL6002C10 1390015 EA LT ENGINE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 LT ENG SHUT-OFF VALVE MOUNTING BRACKET CLIP CRACKED. 2 L 7 2 4F RT A21EA 20081107 NM 2008 11 7 SWAA086010 1 20081103 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 25R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086020 1 20081103 A 5330 6545775 SKIN BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 670SW 23784 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 19R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086006 1 20081103 A 5311 6545815 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 344, STR 3R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 2008UALA06355 1 20081102 A 8011 35054367 STARTER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE NR 2 ENGINE FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 671UA 30026 DURING RIGHT ENGINE START, START SWITCH IN GND POSITION WITH N2 READING 6 PERCENT START. STARTER IS DEFECTIVE. REPLACE D NR 2 ENGINE STARTER & STARTER. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081107 WP 2008 11 7 IXX2008F00100 1 20080805 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK INSPECTION, FOUND LT FWD FUSELAGE AFT AND BELOW EMERGENCY EXIT DOOR HAS IMPROPER REPAIR AT FS 447 LOGN 25.5 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, EXTERNAL DOUBLER, INTERNAL FINGER DOUBLERS AND FILLER. CLEANED TREATED AND PRIMED AREA AND REPAIR PARTS. INS TALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-1-11, SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1, SRM 53-2-1, SRM 51-1-21, S RM 53-4-1 & SRM 51-1-8B. (K) 2 L 7 4 4F RT 4A25 20081107 NE 2008 11 7 2008UALA06356 2 20081102 A 7261 ACC434F65 OIL FILTER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE NR 2 ENGINE FAULTY A UALA D RETURN TO BLOCK J WARNING INDICATION IN INSP/MAINT 1 WP 29 666UA 29238 NR 2 ENGINE OIL FILTER MESSAGE DISPLAYED. MESSAGE DISAPPEARED WHEN THRUST REDUCED. OIL FILTER IS FAULTY. REPLACED NR 2 ENG OIL FILTER. LEAK AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081107 NM 2008 11 7 2008UALA06357 1 20081102 A 2421 729825M IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE FAULTY A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 596UA 28749 RT IDG DRIVE LIGHT AND MESSAGE ON TAXI OUT. DISCONNECTED IDG PER SAM. RETURN TO GATE. IDG IS OUT OF TOLERANCE. REPLA CED RT ENGINE IDG. OP CHK'D GOOD ON ENGINE RUN. NO LEAKS, NO FAULTS. 2 L 7 2 4F 4 F RT A2NM E17NE 20081107 NM 2008 11 7 2008UALA06361 1 20081103 A 4960 CONTROLLER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 213UA 30219 APU BLEED AIR APUC DETECTED LOSS OF ABILITY TO PNEUMATICALLY LOAD APU. MESSAGE IS TRIGGERED BY IGV OR SURGE CONTROL SYS TEM FAULTS. STATUS MSG01- NOT ACTIVE ENGINE START MODE DEPENDENT; SURGE CONTROL VALVE (PNEUMATIC CLUSTER) DOES NOT FOLL OW COMMAND. DB- APU CONTROLLER (APUC)MSG-4911180 INACTV ES MODE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081107 NM 2008 11 7 2008UALA06344 1 20081101 A 5320 STRUCTURE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 RT SIDE FUSELAGE DAMAGE FROM STA 1131 TO 1175 STRINGERS 18R TO 20R. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED REPAIR DOU BLER TRIPLER AND FILLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081107 NM 2008 11 7 2008UALA06345 1 20081101 A 5310 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 550UA 25398 LT FORWARD OVERWING ESCAPE HATCH CUTOUT CORRODED AT LOWER FORWARD CORNER. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION AND FOUND MATERIAL REMAINING IS OUT OF LIMITS. REMOVED DAMAGE AND FABRICATED REPAIR DOUBLER AND INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081107 NM 2008 11 7 2008UALA06347 1 20081101 A 3350 582240 POWERPACK BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 677UA 30029 RIGHT AISLE EEL PATH LIGHTS INOP AT ROW 20 - 26. FOUND BOTH PWR SUPPLIES ARE DISCONNECTED AT ROW 24, WIRING NEEDS TO BE SECURED UNDER THE SEATS. SECURED WIRING. REPLACED EEL LIGHT PWR PACK LOCATED ON FLOOR BEHIND AIR GRILL BETWEEN SEATS 23HJ AND 24HJ EEL LTS. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081107 2008 11 7 DXTA2008110403335 4 20081103 A 2210 AUTOPILOT SYS CESSNA 500 560CESSNA 2076750 CE COCKPIT MALFUNCTIONED E DXTA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 07 803QS 5600775 AUTOPILOT CAME OFF 3 TIMES INFLIGHT. 2 L 7 2 4F RT A22CE 20081107 NE 2008 11 7 DL76P081475 2 20081030 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 DEFECTIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 143DA 66057 25991 724139 FAILED EA 51-470869-12 REV B MGB OIL NOZZLES INSP. REPLACING NR 1 ENGINE. REPLACED NR 1 ENG PER TRANS 1T148AD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081110 NM 2008 11 10 USAA920081988 1 20081029 A 5414 SKIN BOEING 737 737301 1384611 NM ZONE 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT MAJOR REPAIR Q3 CHECK NR 03975480042, CRACKED NR 1 ENGINE PYLON SKIN AT ACCESS OPENING 5727L. REPAIRED NR 1 ENGINE PYLON SKIN AT ACCESS OPENING 5727L. IAW US AIRWAYS TYPICAL REPAIR 54-30-07. 2 L 7 2 4F RT A16WE 20081110 WP 2008 11 10 AALA200802552 1 20080925 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 3 CRACKS FOUND ON AFT FUSELAGE SKIN AT STATION 1437 BETWEEN LONGERONS 3 RT AND 4 RT. INSTALLED DOUBLER IN ACCORDANCE WI TH AARD 53-30-00-02. 2 L 7 2 4F RT A6WE 20081110 WP 2008 11 10 AALA200802569 1 20080917 A 5315 3925819U2 FLOORBEAM DOUG DC9 DC983 3022083 WP BS 927 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 FLOORBEAM CRACKED AT STATION 927. CRACK LENGTH IS 1 INCH. REPLACED FLOORBEAM IN ACCORDANCE WITH SRM 51-01. 2 L 7 2 4F RT A6WE 20081110 SO 2008 11 10 N93A20081103 1 20081031 A 5720 BEAM GULSTM GV GV 3980116 SO LT WING CRACKED E N93A K NONE O OTHER IN INSP/MAINT 1 SO 13 509QS 8104 637 CRACK LOCATED ON WING REAR BEAM BEHIND FLIGHT SPOILER ACTUATOR BRACKET. LT AND RT PER CUSTOMER BULLETIN THIS IS A RESUL T OF IMPROPER RIGGING OF THE FLIGHT SPOILERS. 2 L 7 2 4F RT A12EA 20081110 NM 2008 11 10 C8GA20080031 1 20081028 A 2780 SLAT BOEING 727 727223 1384074 NM WING MALFUNCTIONED A C8GA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 29 708AA 22465 FLT 715 FROM MEM TO TOL. DURING CLIMB OPERATION ON FLAP RETRACTION THE NR 7 LEADING EDGE DEVICE WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO MEM WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION OF THE NR 7 LEADING EDGE POSITION SW ITCH WAS PERFORMED AND THE LEADING EDGE DEVICES WERE OPERATIONALLY CHECKED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETU RNED TO SERVICE. 2 L 7 3 4F A3WE 20081110 SO 2008 11 10 RAIA2008110400001 1 20081103 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 829HK 145281 DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHT OVER THE GALLEY SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE LIGHT BULB. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081110 SO 2008 11 10 FDKA2008110300287 1 20081103 A 3350 INVERTER EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA K NONE L NO TEST NR NOT REPORTED 1 SW 07 846MJ 145507 FRL JFK 6265. EMERGENCY AFT CEILING LOCATOR SIGN OUT. MX REMOVED AND REPLACED NR 4 INVERTER, OPS GOOD. 2 L 7 2 4T RT T00011AT 20081110 EA 2008 11 10 SWIA200820265 1 20080707 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 915SW 7615 FS 625 CLIPS CRACKED LEFT AND RIGHT SIDES (C-CHECK). REPLACED CLIPS PER REO. 2 L 7 2 4F RT A21EA 20081110 NM 2008 11 10 USAA920081974 1 20081028 A 5320 6517582 BEAM BOEING 737 7373G7 138447J NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN C18 MAJOR REPAIR NR 6132076 VERTICAL BEAM CRACKED AT BS184, WL232, RBL17. REPAIRED VERTICAL BEAM AT BS184, WL232, R BL17 IAW BOEING 737 SRM 53-10-08. 2 L 7 2 4F RT A16WE 20081110 NM 2008 11 10 ASM2008F00006 1 20080930 A 5730 112N61012 ACCESS PANEL BOEING 737 737* NM RT WING TANK LEAKING W ASMF O OTHER O OTHER NR NOT REPORTED 1 SW 23 852AM 33787 DURING FUEL SUPPLY SERVICE MX PERSONNEL DETECTED A FUEL LEAK UNDER THE RT WING. THE MAIN TANK ACCESS DOOR 632EB AND ITS RUDDER DOOR SEAL WERE REPLACED AND TESTED IAW MM 28-11-11, TASK 28-11-00-790-801 ALL CORRECT. 2 L 7 2 4F RT A16WE 20081110 EA 2008 11 10 SWIA200820275 1 20080629 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 913SW 7597 INTERCOSTAL TO FRAME CLIP AT LFS625 STR 14 CRACKED (C-CHECK). REPLACED PER REO. 2 L 7 2 4F RT A21EA 20081110 NM 2008 11 10 08FDEA04712 1 20081104 A 5420 311N50406 WEB BOEING 757 757200 1384950 NM NR 2 PYLON DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 NR 2 PYLON UPPER WEB AT PPS 146-154 HAS WORN AREA CAUSED BY LOOSE SUPPORT BRACKETS. BLENDED DAMAGED WORN AREA AND FOUN D TO BE OUT OF LIMITS PER SRM 54-50-01 FIG. 101 DETAIL III . COMPLIED WITH FED EX E.A. F-5450-123904A DATED 09/03/08. THIS IS A CAT. "A" REPAIR. "MAJOR REPAIR" 2 L 7 2 4F RT A2NM 20081110 NM 2008 11 10 08FDEA04713 1 20081104 A 5420 311N50406 WEB BOEING 757 757200 1384950 NM NR 2 PYLON DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 NR 2 PYLON CENTER WEB BETWEEN PPS 146-154 HAS HEAT DAMAGE. PREFORMED HARDNESS TEST ON NR 2 PYLON CENTER WEB PER SRM 51-2 0-02 FIG.3 AND FOUND TO BE ABOVE LIMITS. COMPLIED WITH F-5450-123904A DATED 09/03/08. THIS IS CAT "A" REPAIR . "MAJO R REPAIR" 2 L 7 2 4F RT A2NM 20081110 NM 2008 11 10 08FDEA04723 1 20081105 A 5230 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 593FE 48551 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 5 FOUND WI TH CRACK INDICATION AT HOLE D. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50- 00, FIGURE 10, VOLUME I. REAPIR CLASSIFIE D MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081110 NM 2008 11 10 08FDEA04725 1 20081105 A 5230 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 593FE 48551 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 6 FOUND WI TH CRACK INDICATIONS AT HOLES B AND D. CARRIED OUT BUSHING REPAIR AS PER SRM 53-50- 00, FIGURE 10, VOLUME I. REPAIR C LASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081110 EA 2008 11 10 MAS2008F00097 1 20080925 A 5270 WARNING LIGHT CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT FALSE ACTIVATION A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 926LR 15026 FLT 2781 - LT FWD OVERWING EMERGENCY DOOR CAUTION MESSAGE APPEARED AFTER LANDING. TROUBLESHOT AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 MAS2008F00095 1 20080926 A 5270 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT DIRTY A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 509MJ 10094 FLT 7048 - LT EMERGENCY EXIT CAUTION MESSAGE ON LANDING. MX CLEANED THE DOOR PROXIMITY SWITCH AND RESEATED DOOR. OPS CH ECKED GOOD. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 MAS2008F00096 1 20080926 A 5210 DOOR CNDAIR CL600 CL6002D24 1390016 EA MAIN PAX STIFF A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 903FJ 15003 FLT 2766 - MAIN PAX DOOR DIFFICULT TO CLOSE. MX PERFORMED OPS CHECK AND FOUND OPS NORMAL. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 MAS2008F00098 1 20080925 A 3320 1317 LAMP CNDAIR CL600 CL6002D24 1390016 EA CABIN LIGHTS INOPERATIVE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 921FJ 15021 FLT 2719 - AFT CEILING LIGHT INOPERATIVE. MX RELAMPED. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 ASOA200801230 1 20080927 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 331CA 10061 FLT 4185 - EMERGENCY LIGHT MISSING AT RT SIDE OF ACFT. REPLACED MISSING LIGHT, OK FOR SERVICE IAW AMM 33-51-01. 2 L 7 2 4F RT A21EA 20081110 NM 2008 11 10 USAA920081834 1 20080919 A 5320 6545834255 STIFFENER BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - C18 - MAJOR REPAIR, CORROSION ON FLOOR STIFFENER AT BS 294.5 TO BS 312, RBL 11, WL 208. REPLACED FLOOR STIFFENER AT BS 294.5 TO BS 312, RBL 11, WL 208 IAW B737 SRM 51-40-02-0G FIGURE 12. 2 L 7 2 4F RT A16WE 20081110 NM 2008 11 10 USAA920081833 1 20080919 A 5320 6517688125 STRUCTURE BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - C18 - MAJOR REPAIR, CORROSION ON FLOOR CHORD AT BS 312 TO BS 350, S17L, WL 208. REPLACED CHORD AT BS 312 TO BS 35 0, S17L, WL 208 IAW B737 SRM 51-40-02-OG FIGURE 3, 8, & 12. 2 L 7 2 4F RT A16WE 20081110 NM 2008 11 10 USAA920081824 1 20081001 A 5320 6935352Y1 TIE CLIP BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, STRINGER TIE CLIP CRACKED AT BS 907, S8L. REPLACED STRINGER TIE CLIP AT BS 907, S8L IAW B737 S RM 51-10-02. 2 L 7 2 4F RT A16WE 20081110 NM 2008 11 10 USAA920081823 1 20081005 A 5320 693535214 TIE CLIP BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, STRINGER TIE CLIP CRACKED AT BS 727C, S4R. REPLACED STRINGER TIE CLIP AT BS 727C, S4R IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081110 NM 2008 11 10 EIA2008056 1 20081007 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486EV 20888 UPPER DECK AFT EMERGENCY LIGHT INOP. REPLACED UPPER DECK AFT EMERGENCY LIGHT, OPS CK NORMAL PER MM 33-51-00. 2 L 7 4 4F RT A20WE 20081110 SO 2008 11 10 C2XA008TY123 1 20081008 A 3610 8166248 THERMOSTAT EMB 145 EMB145XR 3260214 SO BLEED AIR SYS MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 11137 15855 15855 145721 ENROUTE FROM IAH TO ORF WHEN THE CREW RECEIVED SEVERAL EICAS MESSAGES FROM BLEED NR 1 OVERTEMP FOLLOWED BY BLEED NR 2 O VERTEMP THROUGHOUT DESCENT TO EXIT, IN ADDITION TO ANTI-ICE FAIL AND ICE CONDITIONS. DIVERTED TO TYS, WHERE MX REMOVED R&R BOTH FWD FAN AIR THERMOSTATS. OPS CHECKS GOOD. WORK WAS IAW AMM 36-11-06 AND WAS RELEASED TO SERVICE. 2 L 7 2 4F RT 20081110 NM 2008 11 10 USAA920081835 1 20081007 A 5312 BULKHEAD BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 450UW 24933 PIT - FPBH - MAJOR REPAIR, 4 CRACKS FOUND ON LT VERTICAL BEAM WEB OF BS 178 BULKHEAD, WL 234 TO WL 220, LBL 17. REPAIRE D LT VERTICAL BEAM WEB OF BS 178 BULKHEAD, WL 234 TO WL 220, LBL 17 IAW B737 SRM 51-10-08. 2 L 7 2 4F RT A16WE 20081110 NM 2008 11 10 USAA920081822 1 20081003 A 5311 65C32395 FRAME BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, FRAME CRACKED AT BS 727F, S8R & S9R. REPAIRED FRAME AT BS 727F, S8R & S9R IAW US AIRWAYS TYPIC AL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 20081031 NM 2008 10 31 2008UALA06274 1 20081025 A 2421 745329F IDG BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LEFT FAILED A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION NR NOT REPORTED 1 WP 29 677UA 30029 EICAS MSG L GEN OFF DISPLAYED. GEN OFF LIGHT ILLUM & FAILED TO RESET. GENERATOR FOUND FAULTY. REPLACED LEFT IDG. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081031 NM 2008 10 31 2008UALA06276 1 20081025 A 3350 767 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 559UA 26657 THREE RT MED EXTERIOR EMERGENCY LIGHT INOP. REPLACED LAMP, OPS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081031 NM 2008 10 31 2008UALA06264 1 20081024 A 3397 794640 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 119UA 28812 EMERGENCY EXIT EEL LIGHT INOP ACROSS LAV 102 LOWER WALL EEL. SECURED CONNECTOR, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081031 NM 2008 10 31 HALA2008102300826 1 20081027 A 2432 BA3601 BATTERY BOEING 717 717200 1383700 NM E&E BAY FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 475HA 55121 BATTERY CHARGER FAIL LIGHT ON CLIMBOUT. REPLACED ALL 3 BATTERIES PER AMM 24-34-01. 2 L 7 2 4F TR A6WE 20081031 NM 2008 10 31 AALA200802327 1 20080723 A 5313 141T3001 STRINGER BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 339AA 22336 AFW FORWARD CARGO STRINGER WAS CORRODED. AREA OF DISCREPANCY WAS 22 INCHES IN LENGTH. REPAIRED PER SRM 53-00-03 2R2 WI TH EXCEPTIONS PER MRB 767 3260. 2 L 7 2 4F RT A1NM 20081103 CE 2008 11 3 10172008N303CS 1 20081014 A 3233 99124655 ACTUATOR CESSNA 500 550 2076604 CE LT MLG MALFUNCTIONED E Z5FA O OTHER J WARNING INDICATION LD LANDING 1 EA 63 303CS 5500814 WHEN LANDING SELECTED DOWN, LT LG DID NOT INDICATE DOWN, NO GREEN LIGHT. PROBLEM TROUBLESHOT TO LT SIDE BRACE ACTUATOR . ACTUATOR REPLACED AND ACFT RETURNED TO SERVICE. 1 L 7 2 4F A22CE 20081103 WP 2008 11 3 AALA200802536 1 20080921 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 33502 49739 EMERGENCY LIGHT AT FORWARD OVERWING EXIT STAY ON. ADJUSTED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081103 EU 2008 11 3 USAA920081960 1 20080925 A 5347 D5323046420000 SEAT TRACK AIRBUS 320 A320231 3930325 EU ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL MAJOR REPAIR C7 CHECK NR 6062562. CORROSION ON SEAT TRACK AT FR 24 - FR 35 Y765. REPLACED SEAT TRACK AT FR 24 - FR 35 Y765 IAW SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081103 NM 2008 11 3 AALA200802326 1 20080723 A 5313 141T3001 STRINGER BOEING 767 767223 1385123 NM BS 421-443 S36R CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 339AA 22336 AFW FORWARD CARGO STRINGER WAS CORRODED. AREA OF DISCREPANCY WAS 22 INCHES IN LENGTH. REPAIRED PER SRM 53-00-03 2R2 WI TH EXCEPTIONS PER MRB 767 3258. 2 L 7 2 4F RT A1NM 20081103 NM 2008 11 3 AALA200802335 1 20080910 A 3350 18539202 SWITCH BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA O OTHER O OTHER CR CRUISE 1 SW 21 783AN 30004 EZE INFLIGHT T943/10SEP. CREW REPORTED EMERGENCY LIGHTS THROUGHOUT ACFT WERE INTERMITTENTLY BLINKING ON AND OFF. LAND ED EZE WITHOUT INCIDENT. REPLACED EMERGENCY LIGHT SWITCH AT LT NR 1 DOOR PANEL. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081103 EU 2008 11 3 NWAA084643255 1 20081015 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320212 3930322 EU EMERGENCY LIGHTS FAULTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 355NW 4561 807 RT EMERGENCY EGRESS LIGHT POWER SUPPLY UNIT FAULT. REPLACED RT POWER SUPPLY UNIT. CHECKS GOOD. 2 L 7 2 4F RT A28NM 20081103 EU 2008 11 3 USAA920081839 1 20081008 A 5220 D5337046320000 ROD AIRBUS 320 A320214 3930316 EU EMEGENCY EXIT BENT A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 111US 1114 FLT NR 9244 ARA-CLT, LT OVERWING EMERGENCY HATCH DOES NOT SHOW ARMED. MX FOUND ACTUATING ROD FOR SWITCH 5WN1 BENT AND N OT ACTUATING. REPLACED LT FWD OVERWING ACCESS ACTUATING ROD AND ADJUSTED SWITCH 5WN1 TO WITHIN LIMITS. ALL INDICATIONS CHECK NORMAL. 2 L 7 2 4F RT A28NM 20081104 EU 2008 11 4 UPS08153756 1 20081025 A 7830 32142368 SHUTOFF VALVE AIRBUS A300 A300F4622R 3930360 EU THRUST REVERSER MALFUNCTIONED A IPXA K NONE J WARNING INDICATION CL CLIMB 1 SO 01 137UP 0820 INSPECTION TYPE:N/A ATB - NR 1 ENG REVERSER UNLOCK LIGHT ILLUMINATED. REMOVED & REPLACED THRUST REVERSER PRSOV FOR TSM 78-31-40 BLOCK 22 PER AMM 78-31-05-04. PERFORMED OPS CHECK PER AMM 78-32-11-05. NR 1 ENG REVERSER SYSTEM HAS NO DEFECT S NOTED. 2 L 7 2 4F RT A35EU 20081104 WP 2008 11 4 UPS08853647 1 20081005 A 5730 DOUBLER DOUG DC8 DC873F 302199F WP RT WING UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV RIGHT LEADING EDGE DOUBLER NEEDS VALIDATION AT STA XFS 455 FAILED APPH STEP 5 894-W4-07. REPLACED DO UBLER IAW DC8 SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 20081104 EU 2008 11 4 QML2008F00019 1 20081005 A 3110 1179203107 CONTROL UNIT BOLKMS 117 BK117B2 5626013 EU INSTRUMENT PANEL SHORTED E QMLA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 154AM 7154 AFTER STARTING ENGINE NR 1 NOTICED AN ELECTRICAL ODOR AND INSTRUMENT PANEL LIGHT CIRCUIT BREAKER POPPED. ACFT SHUTDOWN, MX. LIGHT INTENSITY CONTROL UNIT P/N 117-92031-07 SHORTED OUT CAUSING BURNED ELECTRICAL ODOR IN COCKPIT. SHORTED UNIT CAUSED INSTRUMENT LIGHTS TO BECOME INOPERATIVE AND THEN POPPED THE INSTRUMENT LIGHT CIRCUIT BREAKER. 1 G 7 2 3U NC H13EU 20081110 EA 2008 11 10 SWIA200820287 1 20080630 A 5210 WEB CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 820SK 15108 PASSENGER DOOR AFT WEB CRACKED AT ZONES 2 AND 3. (C-CHECK)REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 SWIA200820292 1 20080711 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 916SW 7634 LT SIDE FS 621 TO FS 625 OBLIQUE ANGLE IS CRACKED. (C-CHECK)REPLACED. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 SWIA200820293 1 20080712 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 957SW 7829 PASSENGER DOOR AFT WEB CRACKED AT DOOR COUNTERBALANCE SPRING UPPER BOLT CUTOUT. (C-CHECK)REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 SWIA200820294 1 20080712 A 5230 ANGLE CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 957SW 7829 CARGO DOOR SUPPORT LOWER ANGLE CRACKED. (C-CHECK)REPLACED. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 SWIA200820302 1 20081102 A 2421 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 LOW A SWIA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 NM 07 923SW 7664 ON CLIMBOUT NR 2 GEN WENT OFF LINE. DURING RESET PROCEDURE ADG INADVERTENTLY DEPLOYED. (FLT 6532)SERVICED IDG. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 SWIA200820303 1 20081101 A 3610 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE MALFUNCTIONED A SWIA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 NM 07 913EV 7731 LEFT 14TH STAGE DUCT WARNING MESSAGE ON DESCENT, SECURED ENGINE. (FLT 4785)REPLACED LEFT PRSOV AND 14TH STAGE VALVES. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 SWIA200820304 1 20081103 A 5210 PIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR LACK OF LUBE A SWIA K NONE O OTHER NR NOT REPORTED 1 NM 07 498CA 7792 FA UNABLE TO OPEN MAIN CABIN DOOR. (FLT 2523)LUBED CABIN DOOR LATCH PINS. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 SWIA200820305 1 20081104 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 910EV 7727 LAST OVERHEAD EMERGENCY LIGHT INOP. (FLT 4416)RELAMPED. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 SWIA200820310 1 20081030 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 957SW 7829 SECOND TO LAST OVERHEAD EMERGENCY LIGHT INOP. (FLT 5939)RELAMPED. 2 L 7 2 4F RT A21EA 20081110 NM 2008 11 10 USAA920081820 1 20081002 A 5311 6546526 FRAME BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, FRAME CRACKED AT BS 400, S8L & S9L. REPAIRED FRAME AT BS 400, S8L & S9L IAW US AIRWAYS TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 20081112 NM 2008 11 12 AALA200802320 1 20080714 A 3350 D14101100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 920AN 29521 AFT EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK. GROUND CHECKED NORMAL. 2 L 7 2 4F RT A16WE 20081106 EA 2008 11 6 ASOA200801432 1 20081102 A 2781 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA SLAT SYSTEM ACTIVATED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 707EV 10057 SLATS FAIL CAUTION ON FLAPS 8 DEG SELECTION. SLATS 0 DEG, FLAPS 45 DEG. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 20081107 NM 2008 11 7 AALA200802681 1 20081004 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 778AN 29587 DFW - EMERGENCY LIGHTS AT SEAT ROWS 30 TO 45 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 30 TO 45. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081107 NM 2008 11 7 SWAA086030 1 20081104 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER EA. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086035 1 20081104 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER EA. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086009 1 20081103 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 20R. REMOVED AND REPLACED STR CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081107 EU 2008 11 7 2008UALA06354 1 20081101 A 4990 LINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE APU OIL SYS LEAKING A UALA O OTHER W K B INADEQUATE Q C FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 447UA 836 ACRID SMELL RETURNED ON TAKEOFF AND CLIMB GOT BETTER AT ALTITUDE NOW JUST MILD. SMELL GETS BETTER WITH CABIN FANS OFF A ND PACK IN HIGH FLOW. FOUND BRAIDED OIL LUBE LINE AFT SIDE OF GEARBOX ON APU LEAKING OIL INTO AREA OF APU INLET, AND CA USING OIL SMELL. ACCOMPLISHED PACK BURN OUT ENG RUN, SMELL GONE. CLEANED APU INLET. RESIDUAL OIL SMELL IS STILL REMAI NING IN AC. SMELL HAS NOT DISSIPATED ENTIRE FLIGHT. REPLACED RECIRCULATION FILTERS. 2 L 7 2 4F 4 F RT A28NM E40NE 20081107 2008 11 7 DL76G081477 4 20081030 A 2330 RDFA312401 ELECTRICAL BOX BOEING 767 7673P6 1385105 NM CABIN MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 155DL 25269 ELECTRICAL ODOR NEAR SEATS 2F/G. FOUND SEB AT 2A/B (NOT 2F/G) AT FAULT. MOVED SEB TO SEATS 5A/B. FWD TO MCO AND MEL P ER 25-25-02A. SEATS 2A/B NOW GOOD. REMOVED AND REPLACED DC SEB P/N RD-FA 3124-07. REMOVED AND REPLACED SPM P/N RD-FA 3621-01 AND R SAC CONTROL BOX P/N PS4-52222-52. ALL IFE AND SEAT FUNCTION OPS NORMAL AT 5 A/B. REMOVED PLACARD. 2 L 7 2 4F RT A1NM 20081110 NM 2008 11 10 USAA920081975 1 20081014 A 5315 6546810501 FLOORBEAM BOEING 737 7373G7 138447J NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL C21 MAJOR REPAIR NR 6136443 CORROSION ON FLOORBEAM UPPER CHORD AT BS967, WL208, LBL18. REPAIRED FLOORBEAM UPPER CHO RD AT BS967, WL208, LBL18 IAW B737 SRM 53-00-51-2R. 2 L 7 2 4F RT A16WE 20081110 SO 2008 11 10 N93A 1 20081101 A 5720 BEAM GULSTM GV GV 3980116 SO LT WING CRACKED E N93A K NONE O OTHER IN INSP/MAINT 1 SO 13 508QS 7790 631 CRACK LOCATED ON WING REAM BEAM BEHIND FLIGHT SPOILER ACTUATOR BRACKETS. (LT AND RT) PER CUSTOMER BULLETIN THIS IS A RE SULT OF IMPROPER RIGGING OF THE FLIGHT SPOILERS. 2 L 7 2 4F RT A12EA 20081110 WP 2008 11 10 AALA200802566 1 20080919 A 5340 FITTING DOUG DC9 DC983 3022083 WP BS 1140 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 AFT SERVICE DOOR FORWARD GIRT BAR FITTING DOUBLER CRACKED AT STATION 1140. AREA OF DISCREPANCY IS 3 INCHES BY 3 INCHES. CRACK LENGTH IS .25 INCH. INSTALLED DOUBLER FOR AFT SERVICE DOOR FORWARD GIRT BAR FITTING IN ACCORDANCE WITH AARD 53- 20-00-16. 2 L 7 2 4F RT A6WE 20081110 NM 2008 11 10 08FDEA04717 1 20081105 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 593FE 48551 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOUND WI TH CRACK INDICATIONS AT HOLES A, B AND D. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. BUSHING REPAIR CARRIED O UT AT BOLT HOLES AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081110 NM 2008 11 10 08FDEA04720 1 20081105 A 5230 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 593FE 48551 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FOUND WI TH CRACK INDICATIONS AT HOLES C AND D. CARRIED OUT REPAIR AS PER SRM 53-50-00, VOLUME I, FIGURE 10. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081110 NM 2008 11 10 08FDEA04728 1 20081105 A 2750 40173 SWITCH BOEING 727 727225 1384077 NM LE FLAPS MISALIGNED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 464FE 21288 NR 2 LED/FLAP DID NOT RETRACT. FOUND SWITCH INTERNALLY BINDING. REPLACED SWITCH PER 27-82-001-4, OP CHECKS NORMAL, GOOD FOR SERVICE. PREMATURE REMOVAL/INSTALLATION. REMOVED AND REPLACED NR 2 LEADING EDGE FLAP SWITCH AMM 27-82-001-4 2 L 7 3 4F A3WE 20081110 EA 2008 11 10 MAS2008F00087 1 20080930 A 2560 LATCH CNDAIR CL600 CL6002C10 1390015 EA SEAT BELT MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 506MJ 10073 FLT 7335- FWD AND AFT FA SEAT BELT RELEASE HARD TO OPERATE. MX ADJUSTED SEAT BELT AND RETURN SPRING. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 MAS2008F00090 1 20080929 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT INOPERATIVE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 501MJ 10047 FLT 7123-LT AND RT EMERGENCY DOOR EXIT SIGNS BULBS BURNED OUT. RELAMPED, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 SWIA200820312 1 20081030 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 449SW 7699 LEFT WING AFT EMERGENCY LIGHT INOP. (FLT 3852)RELAMPED. 2 L 7 2 4F RT A21EA 20081110 2008 11 10 COEA0803917 4 20081006 A 6113 7901761 SPINNER AEROSP ATR42 ATR42300 8680920 EU LT PROPELLER CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 917FX 354 MAJOR REPAIR, LT ENGINE PROPELLER SPINNER IS CRACKED AT 3 BOLT HOLES AND OTHER HOLES SHOW SIGNS OF WEAR. FOUND AT COE M AJOR REPAIR LT ENGINE PROPELLER SPINNER IS CRACKED AT 3 BOLT HOLES AND OTHER HOLES SHOW SIGNS OF WEAR. CUT OUT 3 CRACKE D CORNERS AND MADE REPLACEMENT CORNER PIECES. INSTALLED THE 3 CORNERS WITH REINFORCEMENT STRIPS DOUBLERS ON THE SPINNER . INSTALLED A 4TH REINFORCEMENT STRIP AS A COUNTER BALANCE ON THE SPINNER. 2 H 7 2 4T RT A53EU 20081112 NM 2008 11 12 AALA200802319 1 20080714 A 3350 D71701100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 920AN 29521 MID EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK. GROUND CHECKED NORMAL. 2 L 7 2 4F RT A16WE 20081112 NM 2008 11 12 AALA200802322 1 20080714 A 3350 D17101100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 920AN 29521 AFT EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK. GROUND CHECKED NORMAL. 2 L 7 2 4F RT A16WE 20081112 NM 2008 11 12 AALA200802325 1 20080715 A 3350 D71701100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 920AN 29521 FWD EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK. GROUND CHECKED NORMAL. 2 L 7 2 4F RT A16WE 20081112 EU 2008 11 12 DHLA200800106 1 20080930 A 3350 312101 POWER SUPPLY AIRBUS 300 A300B4203 3930306 EU EMERGENCY LIGHTS INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 GL 05 367DH 645 381 265 ON PRE-DEPARTURE CHECK, EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE, ACFT GROUNDED. R&R POWER SUPPLY IAW MM 33-51-14. OPS CHECKED GOOD IAW 33-51-00. 2 L 7 2 4F RT A35EU 20081112 EU 2008 11 12 USAA920081796 1 20081001 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 3930316 EU EMERGENCY LIGHTS DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 113UA 1141 FLT 870, EMERGENCY LIGHT POWER SUPPLY FAILED BITE CHECK. MX R&R IAW 33-51-38-04. OPS CHECKED GOOD. 2 L 7 2 4F RT A28NM 20081112 EA 2008 11 12 VTZ2008F00000 1 20080928 A 2421 M832481216 O-RING CNDAIR CL600 CL6002B19 1900309 EA NR 2 IDG CUT A VTZA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 27 667BR 7535 FLT 5703 - WHILE CLIMBING THROUGH 600 FT, FLT CREW RECEIVED AN NR 2 OIL PRESSURE MESSAGE. ENGINE INDICATIONS FOR NR 1 NO RMAL, ALL OTHER INDICATIONS FOR NR 2 NORMAL. OIL PRESSURE FLUCTUATING BETWEEN 25 AND 35 PSI. POWER PULLED BACK ON NR 2 T O IDLE TO MONITOR ENGINE. EMERGENCY DECLARED, RTB AND LANDED WITHOUT FURTHER INCIDENT. MX RAN ENGINE AND FOUND THE IDG ON NR 2 LEAKING OIL. IDG REPLACED AND ENGINE OPERATED NORMAL. ENGINE REPEATED PROBLEM AND FOUND NR 2 IDG SHAFT SEAL CUT AND LEAKING. O-RING REPLACED, LEAK AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081112 WP 2008 11 12 AALA200802338 1 20080910 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 472AA 49647 EMERGENCY LIGHT AT SEAT 15D MISSING SHROUD. REPLACED SHROUD. GROUND CHECKED NORMAL. 2 L 7 2 4F A6WE 20081112 NM 2008 11 12 KCSA081506 1 20081001 A 5310 DOOR FRAME BOEING 747 747122 1384872 NM BS 1668 S25R CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 R4 DOOR FRAME CRACKED AT BS 1668, S25R. OTBD OR DOOR FITTING. 2 L 7 4 4F RT A20WE 20081112 NM 2008 11 12 AALA200802323 1 20080714 A 3350 D71701100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 920AN 29521 COACH EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK. GROUND CHECKED NORMAL. 2 L 7 2 4F RT A16WE 20081112 NM 2008 11 12 DHLA2008745655 1 20080902 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE FROM BS 1323 TO BS 1342.4 S-19L SKIN WITH LOOSE RIVETS. REPAIRED FUSELAGE SKIN SECTION FROM BS 1321 TO B S 1342.4 BETWEEN S-19L AND S-21L IAW COOPESA EC COO-2-53-290-08. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745657 1 20080901 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT BS 700 AT S-8L FRAME WITH DOUBLE HOLE. REPAIRED FUSELAGE FRAME SECTION AT BS 700 BETWEEN S -6L AND S-9L IAW B727 SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745663 1 20081015 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 640 S-28R FRAME CRACKED AT UPPER SECTION. REPAIRED FRAME UPPER SECTION AT BS 640 BETWEEN S-27R AND S-28L IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DLM88081464 1 20081028 A 5330 593600419 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 929DL 49716 23843 CRACK AND CORROSION IN BELLY SKIN AT POTABLE WATER DRAIN, FS 593.6, BTW L-29R AND L-30. CUT OUT DAMAGED AREA AND INSTAL LED EXTERNAL DOUBLER. 2 L 7 2 4F RT A6WE 20081112 NM 2008 11 12 DL757081467 1 20081028 A 5321 FLOOR PANEL BOEING 757 757232 1384965 NM AFT CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 613DL 22820 23843 ACB FLOOR PANEL BS 1330 TO 1460 HAS CORROSION ON TOP AND BOTTOM SURFACE. REMOVED AND REPLACED ACB FLOOR PANEL BS 1330-1 460 IAW AMM. 2 L 7 2 4F RT A2NM 20081112 NM 2008 11 12 DL757081469 1 20081028 A 5320 149N712215 TEE FITTING BOEING 757 757232 1384965 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 23843 T-CLIP CRACKED IN RADIUS BS 800 LOWER BBL 0 COMMON TO FAIRING FORMER. REMOVED AND REPLACED FORMER. 2 L 7 2 4F RT A2NM 20081112 NM 2008 11 12 DL757081470 1 20081022 A 5320 SUPPORT BEAM BOEING 757 757232 1384965 NM AFT CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 23843 CORROSION ON THE THRESHOLD SUPPORT BEAM IN THE AFT CARGO DOOR CUTOUT BS 1380-1440 RBL 21. SUPPORT BEAM WAS REPLACED ON CUST CARD 00126. 2 L 7 2 4F RT A2NM 20081112 NE 2008 11 12 DL76L081472 2 20081030 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 DEFECTIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 184DN 67810 723834 27111 723834 ENG FAILED EA 51-470869-12 REV B MGB OIL NOZZLES INSP. REPLACING NR 1 ENG. REPLACED NR 1 ENGINE PER TRANS 1T148. 2 L 7 2 4F 4 F RT A1NM E24NE 20081112 WP 2008 11 12 DHLA200800123 1 20081106 A 2697 CONNECTOR DOUG DC8 DC873 302199C WP FIRE LOOP LOOSE A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 05 802DH 46076 DURING CRUISE FLT 370 ENG FIRE NR 4 IND/ FOLLOWED EMERGENCY PROCEDURES PER AOM / LANDED AT ATL / A&B LOOPS WERE CHK'D B LOOP STEADY IND / A LOOP INTERMITTENT. DEFERRED PER MEL 26-2-3 DMI 34020 ASSIGNED PLACARD INSTALLED REF: LG PG A02579 ITEM 1. NR 4 ENG FIRE IND ON B LOOP & A LOOP INTERMITTENT ON A LOOP FOUND LOOSE CONNECTER, SECURED & RAN NR 4 ENG PER J RH 11.8 & OP'S CK PER MM 26-10-0, OP'S NORMAL. 2 L 7 4 4F RT 4A25 20081112 SO 2008 11 12 C2XA08IA231 1 20081031 A 3320 7287501539 LIGHT EMB 145 EMB145XR 3260214 SO CABIN DEFECTIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 11199 14500953 IAH - FLIGHT 2166, THE CREW REPORTED A BURNING ODOR IN THE CABIN NEAR ROW 12. THE AIRCRAFT LANDED AT IAH WITH NO INCIDE NTS. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE LAMP AT ROW 12BC, OPERATIONALLY CHECKED WITH NO DEFEC TS. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081112 2008 11 12 USAA920081832 4 20081007 A 2213 C12850AC02 FCU AIRBUS 320 A320214 3930316 EU AUTOPILOT SYS DEFECTIVE A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 104UW 22707 96 0863 FLT 1180 PDX-PHL, APPROXIMATELY 5 MINUTES AFTER TAKEOFF, SMOKE STARTED COMING OUT OF CENTER GLARESHIELD PANEL (AUTOPILOT PANEL). WE TURNED OFF BACKGROUND LIGHTS AND RETURNED TO PDX. SMOKE STOPPED SHORTLY AFTER TURNING OFF BACKGROUND LIGHT S. MX R&R THE FLT CONTROL UNIT. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081104 EA 2008 11 4 COMA0860432 1 20081024 A 5320 601R3521017 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FS 654.5 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 588SW 7069 FOUND CRACK ON INTERCOSTAL FOR APU DOOR ACTUATOR. REPAIRED CRACK ON INTERCOSTAL FOR APU DOOR ACTUATOR IAW EA 10-5362-02 391. 2 L 7 2 4F RT A21EA 20081104 WP 2008 11 4 UPS08853743 1 20081002 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATION REPAIR EFN 70219961018. REPAIRED 53-02-03 FIG 8A. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853754 1 20081013 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATION REPAIR AT BS 702-BS 688N L16R AND L17R REPAIR DOES INCORPORATE FASTENER ROW AFT OF REPAIR. REPAIR IS IAW 53-02-00 FIG 22A. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853762 1 20081028 A 3350 CIRCUIT BREAKER DOUG DC8 DC873F 302199F WP COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT CONTROL C/B OPENED DURING ENGINE START. RESET C/B. PERFORMED OPS CHECK OF EME RGENCY LIGHTING SYSTEM SEVERAL TIMES. SYSTEM CHECKS NORMAL. NOTED BY MAINTENANCE. NO FURTHER ACTION REQUIRED REF AMM 33-50-00. 2 L 7 4 4F RT 4A25 20081104 EU 2008 11 4 USAA920081809 1 20081005 A 2560 P2070003001 FLASHLIGHT AIRBUS A319 A319112 3930323 EU ZONE 200 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 838AW 2615 AFT F/A STATION FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT. OPS CHECK WAS GOOD. (K) 2 L 7 2 4F RT A28NM 20081104 NM 2008 11 4 KCSA081512 1 20081006 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 210 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 RT FRAME CRACKED AT STR CUT OUT STA 210 ABOUT 2 INCHES LONG. (K) 2 L 7 4 4F RT A20WE 20081104 NM 2008 11 4 KCSA081510 1 20081004 A 5710 STRUCTURE BOEING 747 747122 1384872 NM LT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 LT WING STA-680 BOOST PUMP CUT OUT CORRODED. (K) 2 L 7 4 4F RT A20WE 20081104 NM 2008 11 4 KCSA081518 1 20081007 A 5347 SEAT TRACK BOEING 747 747249F 1384849 NM FUSELAGE WORN A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 CAPTAINS FORWARD INBD SEAT TRACK, WORN. (K) 2 L 7 4 4F RT A20WE 20081104 SO 2008 11 4 CHQA200800191 1 20081002 A 2910 12303012401 HOSE EMB 135 EMB135KL 3260302 SO ALLSN AE3007 AE3007A 03030 GL HYDRAULIC SYS LOOSE A CHQA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 376SK 145578 CAE311852 ON INITIAL CLIMBOUT, THE FLIGHT CREW RECEIVED A HYD SYS 1 LO QTY EICAS MESSAGE. THE HYDRAULIC PAGE WAS BROUGHT UP ON THE MFD AND THE HYDRAULIC SYS 1 INDICATED IN THE AMBER RANGE AND THE PRESSURE WAS FALLING. WHILE FOLLOWING THE QRH IT WAS N OTED THAT THE NOSE GEAR DOORS OPENED AND A HYD SYS 1 FAIL MESSAGE APPEARED ON EICAS. THE QRH CHECKLISTS WERE COMPLETED AND THE ACFT LANDED WITHOUT INCIDENT. MAINT INSP THE ACFT AND FOUND THE HYDRAULIC PRESSURE LINE GOING TO THE RT NOSE LA NDING GEAR DOOR ACTUATOR WAS LOOSE AND LEAKING FLUID. THE LINE WAS TIGHTENED AND HYDRAULIC SYSTEM 1 WAS SERVICED AND THE NR 1 EDP WAS REPLACED AND THERE WERE NO FURTHER DEFECTS NOTED. (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081104 EA 2008 11 4 VNAA0809009 1 20080927 A 3000 GG690800123 DETECTOR CNDAIR CL600 CL6002C10 1390015 EA ANTI ICE SYS FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 05 712PS 57 10168 CREW REPORTED DUCT MON WARNING VALVES CLOSED, AC WOULD NOT MAINTAIN PRESSURAZATION. CREW ELECTED TO RETRUN TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINT REMOVED AND REPLACED THE ANTI-ICE AND LEAK DETECTION UNIT. NO OTHER DEFECTS NOTED AND ACFT WAS RELEASED FOR SERVICE. (K) 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 VNAA0809010 1 20080930 A 5200 DOOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE GROUND POWER OPEN A VNAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 05 251PS 7931 CREW ELECTED TO RETURN TO DEPARTURE WITH A SUSPTECTED GROUND POWER DOOR OPEN. ACFT LANDED WITHOUT INCIDENT. MAINT REMOVE D AND REPLACED THE AFT LATCH SPRING ON THE GROUND POWER DOOR. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERV ICE. (K) 2 L 7 2 4F 4 F RT A21EA E15NE 20081104 NM 2008 11 4 KCSA081515 1 20081006 A 3350 BULB BOEING 747 747146 1384905 NM EMERGENCY LIGHTS INOPERATIVE A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 702CK 20332 BOTH EMERGENCY LIGHTS INOPERATIVE IN CEILING ABOVE L-5 DOOR. (K) 2 L 7 4 4F RT A20WE 20081104 NM 2008 11 4 KCSA081521 1 20081009 A 5310 DOOR FRAME BOEING 747 747249F 1384849 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 L-5 DOOR FORWARD LOWER CORNER VERTICAL FRAME CRACKED .5 INCHES. (K) 2 L 7 4 4F RT A20WE 20081104 NM 2008 11 4 KCSA081511 1 20081004 A 5710 STRUCTURE BOEING 747 747122 1384872 NM RT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 RT WING STA-680 BOOST PUMP CUT OUT CORRODED. (K) 2 L 7 4 4F RT A20WE 20081104 NM 2008 11 4 KCSA081520 1 20081009 A 5210 BEAM BOEING 747 747249F 1384849 NM L5 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 L-5 DOOR FORWARD LOWER CORNER HORIZONTAL BEAM CRACKED .5 INCH. (K) 2 L 7 4 4F RT A20WE 20081104 NM 2008 11 4 UPS08M53761 1 20081003 A 5230 SKIN DOUG MD11 MD11F 3023600 NM CARGO DOOR DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 279UP 48573 INSPECTION TYPE:C REF D-374482: AFT BULK CARGO DOOR, DOOR SKIN DENT (DEFERRAL TRANSFER ITEM). EXISTING REPAIR DOUBLER R EMOVED PER SRM 51-31-01VIIR40. DISCREPANT LWR SKIN TRIM-OUT PER EN1386-08 & REPROTECTED PER SRM 51-21-01VII R40. HFEC INSP C/O PER DAC NDTSPM REV13 06-10-01.001 ON TRIM-OUT AREA, NO CRACK EVIDENT. NEW SKIN, REPAIR DOUBLER & INTERNAL DOUB LER FAB. FAB SKIN & DOUBLERS INSTALLED PER EN1386-08. 2 L 7 3 4F RT A22WE 20081104 SO 2008 11 4 SIMA200828002 1 20081003 A 2121 4611028900 FAN EMB 145 EMB145LR 3260212 SO CABIN FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 21 664MS 145779 CREW REPORTS THAT ON APPROACH, THE CABIN WAS FILLING UP WITH A HAZY SMOKE. UPON GATE ARRIVAL THE CABIN WAS QUITE HAZY. A PU ON UNTIL AFTER LANDING AND THERE WAS NO CHANGE IN THE CABIN. ACFT REMOVED FROM SERVICE. C/A REMOVED AND REPLACED BOTH RECIRC FANS AND EXHAUST, OPERATION CHECKED GOOD. ACFT RETURNED TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081104 WP 2008 11 4 WX0A070234 1 20080907 A 3350 AD4002 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 877GA 53467 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSP, MAINT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING S YS WOULD NOT TEST. MAINT REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTOR Y OPERATIONAL CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (K) 2 L 7 2 4F RT A6WE 20081104 CE 2008 11 4 DXTA2008103103329 1 20081029 A 4920 APU CESSNA 560 560XL 2076702 CE FAILED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 694QS 5605194 APU FAILED WHILE RUNNING ON THE RAMP, APU FAIL LIGHT ON. APU INOP. COCKPIT FILLED WITH SMOKE. 2 L 7 2 4F RT A22CE 20081104 CE 2008 11 4 DXTA2008110303330 1 20081031 A 2130 PRESSURE SYSTEM CESSNA 500 560CESSNA 2076750 CE MALFUNCTIONED E DXTA G O2 MASK DEPLOYED O OTHER CR CRUISE 1 GL 07 366QS 5600466 AT FL340 LOST PSI'T AT 2000 FPM TO MAX CAB ALT OF 12000. EMERGENCY ACTION TAKEN. 2 L 7 2 4F RT A22CE 20081104 CE 2008 11 4 DXTA2008110303331 1 20081031 A 3260 WARNING LIGHT RAYTHN DH125 HAWKER800XP 7150012 CE COCKPIT ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 815QS 258705 RIGHT GEAR RED LIGHT CAME ON IN FLIGHT. 2 L 7 2 4F RT A3EU 20081104 NM 2008 11 4 DXTA2008110303332 1 20081031 A 7931 WARNING SYSTEM AMD FALC50 FALCON2000 2730170 NM COCKPIT ACTIVATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 230QS 59 ON TAKEOFF ROLL AT 90KTS THE NR 1 ENGINE LOW OIL RED CAS MESSAGE CAME ON AND THE OIL PRESSURE GAUGE DROPPED BELOW 20 PSI . 2 L 7 2 4F RT A50NM 20081104 CE 2008 11 4 DXTA2008110303333 1 20081101 A 2840 WARNING SYSTEM CESSNA 750 750 2076810 CE COCKPIT ACTIVATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 949QS 7500049 ON TAKEOFF BELOW 80 KTS, RECEIVED AN AMBER "FUEL FILTER BYPASS R". TAKEOFF WAS ABORTED. 2 L 7 2 4J RT T00007WI 20081104 NM 2008 11 4 UPS08553779 1 20081028 A 3350 LIGHT BOEING 757 75724APF 1384969 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 471UP 28842 INSPECTION TYPE:N/A EMERGENCY EGRESS LIGHT INOP. RELAMPED EMERGENCY EGRESS LIGHT. OPS CHECK GOOD PER MM 33-50-00. 2 L 7 2 4F RT A2NM 20081104 WP 2008 11 4 UPS08853769 1 20081018 A 5753 DOUBLER DOUG DC8 DC871F 302199D WP TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV REPAIR DOUBLER GOUGED. REF SURVEY SEQUENCE 715-W3-28. INSTALLED DOUBLER IAW DC8 SRM 57-02-01-0. 2 L 7 4 4F RT 4A25 20081104 NM 2008 11 4 K11A20080817001 1 20080817 A 5315 FLOORBEAM BOEING 727 7272H3 138368N NM FUSELAGE GOUGED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 FLOORBEAM STA 380, RBL 45 HAS GOUGES ON BOTH SIDES ON LOWER SURFACE OF UPPER CHORD AND ON UPPER WEB. 2 L 7 3 4F RT A3WE 20081104 NM 2008 11 4 K11A2008103072202 1 20081021 A 5320 STRUCTURE BOEING 727 7272H3 138368N NM FUSELAGE CRACKED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 AFT AIRSTAIRS LT WING BS 1250 APPROX WL 190 CRACKED AT LIGHTENING HOLE .5 INCH CRACK. 2 L 7 3 4F RT A3WE 20081104 NM 2008 11 4 DHLA2008745578 1 20080903 A 5241 DOOR FRAME BOEING 727 727224 1384076 NM GALLEY DOOR CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE CABIN FWD GALLEY DOOR FWD LOWER SECTION FRAME CRACKED. REPAIRED FWD GALLEY DOOR FWD LOWER FRAME SECTION BETWEEN DOOR BEAM NR 4 AND DOOR BEAM NR 6 IAW S/B 727-52-114 DTD FEB 24, 1978 SECTION 3 PART 3 PARA C DWG 69-69940 REV B 11-11-77. 2 L 7 3 4F A3WE 20081104 NM 2008 11 4 DHLA2008745580 1 20081008 A 5320 STRAP BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 680 BETWEEN S-27R AND S-27L INTERNAL STRAP WITH MISSING SECTION. REPLACED ST RAP AT BS 680 BETWEEN S-27L AND S-27R IAW B727 SRM 51-10-1 PARA 7. 2 L 7 3 4F A3WE 20081104 NM 2008 11 4 DHLA2008745581 1 20080905 A 5347 CARGO TRACK BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN SEAT TRACK FROM BS 344 TO BS 600 RBL 45 CORRODED. REPLACED SEAT TRACK SECTION AT RBL 45 FROM BS 480 TO BS 690 IAW B727 SRM 51-10-1 PARA 7A AND IAW VENTURA AEROSPACE 9G CARGO BARRIER INSTALLATION B727-100-200 STRUC TURAL REPAIR MANUAL REPORT 2489 REV A DTD 9/17/2007 PARA 5-4. 2 L 7 3 4F A3WE 20081104 CE 2008 11 4 GUUA10030801 1 20081003 A 5320 STRUCTURE BEECH 1900 1900D 1154162 CE FUSELAGE CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81546 UE187 AT SCHEDULED INSPECTION DISCOVERED A .5 INCH CRACK RIGHT AIRCRAFT FUSELAGE BELLY RBL 29.06. STOP DRILLED CRACK AND INST ALLED REPAIR DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 53-90-18. 2 L 7 2 4T RT A24CE 20081104 NM 2008 11 4 F3LA2008103000700 1 20081029 A 3397 087021673 WIRE HARNESS AIRBUS A319 A319111 3930336 NM CABIN DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 932FR 18 2258 DURING C3 C-CHECK, INSPECTION NOTED THE PATH LIGHT PLUG IN FOR ROW 8, SEATS ABC, WAS PULLED OFF. MAINTENANCE REMOVED AN D REPLACED THE EMERGENCY LIGHT WIRING AND PLUG IN ACCORDANCE WITH ASM 33-51-00 SCH 04 P 105, FIGURE 2 AND AMM 33-51-00-7 10-009. MAINTENANCE PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH AMM 33-51-00-710-009. 2 L 7 2 4F RT A28NM 20081104 2008 11 4 VNAA2008103000010 4 20081025 A 3418 C16258AA TRANSDUCER CNDAIR CL600 CL6002C10 1390015 EA AOA FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 719PS 13 10177 CREW REPORTED RECEIVING A STALL FAIL MESSAGE ON DEPARTURE. CREW ELECTED TO RETURN TO CLT. AIRCRAFT LANDED WITHOUT INCI DENT. MX INSPECTED AND FOUND THE LT AOA BAD. MX REMOVED AND REPLACED THE LT AOA TRANSDUCER. CHECKS WERE PERFORMED. N O FURTHER DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081104 CE 2008 11 4 GUUA09270801 1 20080927 A 5730 SKIN BEECH 1900 1900D 1154162 CE LT WING CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81546 UE187 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT OUTBOARD WING UPPER SKIN TRAILING EDGE HAD CORROSION AND DEBOND BET WEEN WS 121 THROUGH 194.85. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER. 2 L 7 2 4T RT A24CE 20081104 CE 2008 11 4 GUUA09300802 1 20080930 A 5410 118120036603 KEELBEAM BEECH 1900 1900D 1154162 CE LT NACELLE CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81546 UE187 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT NACELLE INBOARD KEEL HAS .75 INCH CRACK FORWARD AND ABOVE LANDING G EAR BOLT. REMOVED AND REPLACED INBOARD KEEL. 2 L 7 2 4T RT A24CE 20081104 CE 2008 11 4 CIEA200800008 1 20081028 A 5220 115430100161 DOOR BEECH B300 B300 1159232 CE EMERGENCY EXIT COCKED E CIEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 350JB 3853 FL213 LOUD NOISE HEARD FROM AREA OF RIGHT FUSELAGE MID-CABIN. DEBRIEFED CREW, CREW INFORMED POPPED SOUND CAME FROM EMERGENCY AREA DOOR OF RIGHT SIDE. REMOVED RIGHT EMERGENCY EXIT DOOR AND INSPECTED IN ACCORDANCE WITH HAWKER BEECHCRAFT KING AIR B300 MAINTENANCE MANUAL CHAPTER 52-20-00. WORK WAS PREVIOUSLY DONE ON WORK ORDER 2284,ITEM 1.1 WHICH REQUIRED REMOVAL A ND RE-INSTALLATION OF RIGHT CABIN EMERGENCY EXIT DOOR. SERVICED/LUBE EMERGENCY EXIT DOOR IN ACCORDANCE WITH HAWKER BEEC HCRAFT KING AIR B300 MAINTENANCE MANUAL CHAPTER 12-20-00 AND REINSTALLED RIGHT EMERGENCY EXIT DOOR AS REQUIRED. PERFORM ED GROUND ENGINE RUNS AND PRESSURIZED THE AIRCRAFT TO SEA LEVEL NO DEFECTS, LEAKS, NOISE OR ANOMALIES WERE PRESENT IN AC 2 L 7 2 4T RT A24CE 20081104 NM 2008 11 4 R61A 20080032 1 20081028 A 2780 SLAT EMB ERJ170 ERJ170100SU 3260403 NM WING OUT OF RIG A R61A L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 11 804MD 17000016 CREW RECEIVED A FLAP/SLAT FAIL MESSAGE ON EICAS DIVERTED FLIGHT TO IAD AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DIS PATCHED TO AIRCRAFT, PERFORMED RERIGGING OF THE LEADING EDGE SLATS SYSTEM, OPERATIONAL CHECK GOOD RETURNED AIRCRAFT TO S ERVICE. 2 L 7 2 4F RT A56NM 20081104 NM 2008 11 4 ASAA0853683 1 20081028 A 2421 59880 INDICATOR BOEING 737 737890 1384527 NM NR 2 IDG ACTIVATED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 585AS AAAH004526 35683 NR 2 ENG IDG DIFFERENTIAL PRESSURE INDICATOR EXTENDED. VERIFIED FAULT TO BE NUISANCE IAW FIM TASK 24 11 00 810 803. RE PLACED FILTERS AND OIL FOR NR 2 ENG IDG AND OPTS. CK IAW T/C 78424000. INSTALLED DPI COUNTER DECAL IAW MM 24 11 41 210 005. NO LEAKS NOTED. 2 L 7 2 4F RT A16WE 20081104 NM 2008 11 4 ASAA0853682 1 20081028 A 4940 38880587 EXCITER BOEING 737 737890 1384527 NM APU DEFECTIVE A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 579AS 1390 35187 FAULT LIGHT ILLUMINATED WHEN STARTING APU. TROUBLESHOT REF FIM 49 40 00 810 802 NO IGNITION. REMOVED AND REPLACED EXCI TER IGNITION UNIT REF M/M 49 41 31. OPS CHECK OK NORMAL START NOTED. 2 L 7 2 4F RT A16WE 20081104 NM 2008 11 4 ASAA0843684 1 20081027 A 5210 6545800732 DOUBLER BOEING 737 737490 1384715 NM L1 DOOR MISREPAIRED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 767AS 558 27081 GATE AGENT REPORTS UPPER L1 DOOR RUBBING INIT MIG 2C 212173 98040. L1 DOOR UPPER HINGE LWR CAM PLATE BOLTS REPLACED AND TORQUED TO REMOVE LOOSENESS. L1 DOOR GUIDE ARM LOCKPLATE ATTACH BOLT/NUT TORQUED TO REMOVE LOOSENESS. REF CLOSED MIG 2C 212173 FOR WORK ACCOMPLISHED. TRIMMED L1 DOOR UPPER AND LOWER HINGE CUTOUTS DOUBLER AND TRIPLER RADIUS TO RELIEVE IN TERFERENCE. REF AAR EA 12977. REPLACED UPPER HINGE COVER PER MM 20 50 11. DOOR RIG ADJ CK OK PER MM 52 11 0. 2 L 7 2 4F RT A16WE 20081104 NM 2008 11 4 ASAA0843685 1 20081028 A 5210 571411 RELEASE MECH BOEING 737 737490 1384715 NM L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 768AS 549 27082 L1 DOOR SAFETY RELEASE STUCK IN OPEN POSITION. LUBRICATED LATCH RELEASE, OP'S NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20081104 WP 2008 11 4 AALA200802634 1 20081001 A 5320 BEAM DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON MID CARGO DOOR BEAM. AREA OF DISCREPANCY WAS 3 INCHES BY 12 INCHES WITH A DEPTH OF .113 INCH. INSTA LLED DOUBLER IN ACCORDANCE WITH AARD 51 10 00 5. 2 L 7 2 4F RT A6WE 20081103 NM 2008 11 3 USAA920081905 1 20081015 A 5312 BULKHEAD BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03055380105/001, 03055380105/002, 030553080105/003 AND 03055380105/004. 4 CRACKS IN WEB FORWARD FLANGE AT BS 178 LBL17 AT 4TH, 5TH, 6TH AND 8TH FASTENER DOWN FROM WL 234. REPAIRED WEB FORWARD FLANGE AT BS 178, LBL 1 7, AT 4TH, 5TH, 6TH AND 8TH FASTENERS DOWN FROM WL 234 IAW SRM 53-10-08 REPAIR 12. 2 L 7 2 4F RT A16WE 20081103 WP 2008 11 3 AALA200802534 1 20080922 A 5320 991007813 CUSP WEB DOUG DC9 DC982 3022082 WP BS 148 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70504 49798 CORROSION FOUND BEYOND LIMITS ON RT CUSP TEE AT CABIN FLOOR STATION 148. SPLICED IN NEW SECTION IN RT CABIN FLOOR IN AC CORDANCE WITH ESO 80559 DATED 19 SEP 2008. 2 L 7 2 4F A6WE 20081103 NM 2008 11 3 USAA920081920 1 20081013 A 5754 SKIN BOEING 767 767201 1385125 NM ZONE 600 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245AY 23897 BFM MAJOR REPAIR C3 CHECK NR 6013566 RT WING NR 8 SLAT UPPER SURFACE DELAMINATED 2 INCHES FROM INBD TRAILING EDGE WEDGE. REPAIRED RT WING NR 8 SLAT UPPER SURFACE 2 INCHES FROM INBD TRAILING EDGE WEDGE IAW B767 SRM 57-43-01. 2 L 7 2 4F RT A1NM 20081103 NM 2008 11 3 USAA920081959 1 20081022 A 5320 6545834259 INTERCOSTAL BOEING 737 737301 1384611 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT MAJOR REPAIR Q3 CHECK NR 03C10753005/013 LEVEL 2 CORROSION ON INTERCOSTAL AT BS 312 - BS 328, RBL 11. REPLACED INTE RCOSTAL AT BS 312 - BS 328, RBL 11 IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 USAA920081961 1 20081024 A 3350 WIRE AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 807AW 1064 LOGPAGE 4427823 FLT NR 0678 PHX BOI EMERGENCY LIGHT ROW 6 LT EMERGENCY LIGHT INOPERATIVE. FOUND WIRE CONNECTOR UNDER SE AT PULLED OUT. REPAIRED WIRE AT ROW 6. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081224 EU 2008 12 24 AALA200802390 1 20081023 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 18066 509 MIA - EMERGENCY LIGHT AT SEAT ROWS 1G TO 5G INOPERATIVE. CHARGED BATTERY LIGHTING SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081103 EU 2008 11 3 NWAA084603216 1 20081012 A 2913 PUMP AIRBUS 320 A320211 3930320 EU HYD SYSTEM FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 316US 192 GREEN RESERVOIR LO LEVEL OCCURRED IN CRUISE. COMPLIED WITH COM, LG GRAVITY EXTENDED PRIOR TO LANDING. ACFT LANDED UNEV ENTFULLY AND WAS TOWED TO GATE. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP. CHECKS OK. 2 L 7 2 4F RT A28NM 20081103 NM 2008 11 3 USAA920081838 1 20081008 A 5312 BULKHEAD BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 450UW 24933 PIT - MAJOR REPAIR, CRACK THRU INSULATION PIN HOLE OF WEB AT BS 178 BULKHEAD, WL 234, RBL 17. REPAIRED WEB AT BS 178 BU LKHEAD, WL 234, RBL 17 IAW B737 SRM 53-10-08 REPAIR 12. 2 L 7 2 4F RT A16WE 20081103 NM 2008 11 3 HNA2008F00055 1 20080903 A 5320 BRACKET DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 931HA 51228 132 FWD EMERGENCY DOOR AREA, BELTFRAME AT STA X254 FOUND CORRODED AND SURFACE CORROSION ON DOOR SILL. AT STA X259 BLENDED B ELTFRAME IAW SRM 53-00-16. CLEAT, THRESHOLD, STRAP AND BRACKET LOCALLY FABRICATED IAW DRAWINGS 8532075, 85320594, 85321 705, 853206070. 2 H 7 2 4T RT A13NM 20081103 NM 2008 11 3 HNA2008F00054 1 20080903 A 5320 STRAP DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 931HA 132 FWD EMERGENCY DOOR AREA, BELTFRAME AT STA X254 FOUND CORRODED AND SURFACE CORROSION ON DOOR SILL. AT STA X259 BLENDED B ELTFRAME IAW SRM 53-00-16. CLEAT, THRESHOLD, STRAP AND BRACKET LOCALLY FABRICATED IAW DRAWINGS 8532075, 85320594, 85321 705, 853206070. 2 H 7 2 4T RT A13NM 20081103 NM 2008 11 3 HNA2008F00053 1 20080903 A 5320 THRESHOLD DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 931HA 51228 132 FWD EMERGENCY DOOR AREA, BELTFRAME AT STA X254 FOUND CORRODED AND SURFACE CORROSION ON DOOR SILL. AT STA X259 BLENDED B ELTFRAME IAW SRM 53-00-16. CLEAT, THRESHOLD, STRAP AND BRACKET LOCALLY FABRICATED IAW DRAWINGS 8532075, 85320594, 85321 705, 853206070. 2 H 7 2 4T RT A13NM 20081104 WP 2008 11 4 UPS08853664 1 20080923 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV FUSELAGE EXTERIOR SKIN STA 50 L21R BULGING AND FASTENER HEAD SHEARED. REMOVED FASTENERS STA FS 70 TO FS 50 L19R TO L21R AND FS 50 TO FS 30 IAW DC 8 SRM 51-1-21. REMOVED DOUBLER FROM STA 7 TO STA 70 L20R-L21R. FABBED AN D INSTALLED DOUBLER IAW DC8 SRM 53-03-03-0, DWG 5613861, AND SRM DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853665 1 20080922 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV SURVEY SEQ NO 894-W3-03 LT WING L/E LOWER SURFACE SKIN REPAIR DOUBLER A HAS 5EA FASTENER HEADS PROTRU DING AT XFS 462.000 AFT OF SLOT DOOR. RE-COUNTERSINK HOLES AND INSTALLED SCREWS IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853666 1 20080922 A 5730 FASTENER DOUG DC8 DC873F 302199F WP LT WING BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV SURVEY SEQ NO 894-W3-01 LT WING L/E LOWER SURFACE SKIN REPAIR DOUBLER HAS 1EA FASTENER HEAD BROKEN AT XFS 404.000 BETWEEN NR 1 AND NR 2 ENG. REPLACED FASTENER IAW UPS DC8 SRM 51-03-00. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853667 1 20080922 A 5730 FASTENER DOUG DC8 DC873F 302199F WP LT WING LOOSE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV SURVEY SEQ NO 894-W3-13 LT WING L/E ABOVE NR 2 PYLON AT XFS 275 SKIN REPAIR DOUBLER HAS 4 FASTENERS L OOSE AND 1 FASTENER PULLED THROUGH. REMOVED AND INSTALLED 5 NEW FASTENERS IAW DC8 SRM 51-3-0 FIG 52A. 2 L 7 4 4F RT 4A25 20081104 2008 11 4 AALA200802376 4 20080919 A 2565 SLIDE AIRBUS 300 A300B4605R 3930308 EU DOOR MALFUNCTIONED A AALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 21 90070 513 SJU FLIGHT ATTENDANT REPORTED LT NR 1 DOOR DIFFICULT TO ARM. CREW OPENED DOOR CAUSING SLIDE TO PARTIALLY DEPLOY. RESER VICED ASSIST BOTTLE AND REPLACED DOOR SLIDE AT LT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A35EU 20081104 WP 2008 11 4 AALA200802379 1 20080919 A 3350 LENS DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 DFW EMERGENCY LIGHT BETWEEN RT SEAT ROWS 6 AND 7 MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT BETWEEN RT SEAT ROWS 6 AND 7. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081104 WP 2008 11 4 AALA200802543 1 20080916 A 5311 9911842129 FRAME DOUG DC9 DC982 3022082 WP BS 1485 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 450AA 49476 CRACK IN WEB OF CANTER FRAME AT STATION 1485. CRACK LENGTH IS 1.5 INCHES. INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53 -10-00-32. 2 L 7 2 4F A6WE 20081104 WP 2008 11 4 UPS08853695 1 20080930 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV BS 659 TO 719.5 L35L TO L35R EXT DOUBLER LOWER BELLY NEED VALIDATION FOR REPAIR. REPAIRED IAW EO DC8 -5300-3I587. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853753 1 20081008 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV REPAIR AT BS 50-56 L28L -L29L DOES MATCH SRM 53-02-00 FIG 13. REPAIR TO 53-2-00 FIG 13. 2 L 7 4 4F RT 4A25 20081104 NM 2008 11 4 KCSA081526 1 20081009 A 5330 SKIN BOEING 747 747249F 1384849 NM BS 2612 S51R DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 DENT IN SKIN AT STA-2612 AT STR-51R. (K) 2 L 7 4 4F RT A20WE 20081104 NM 2008 11 4 WRLA2008078 1 20081002 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 DURING BRIDGE CHECK, MECHANIC FOUND RT NR 1 DOOR LOWER SEAT TRACK CORROSION AT STA Y-430 TO Y-449. REMOVED CORROSION AN D MEASURED REWORK AREA THICKNESS REF JOB CARD NO.300318. REPAIRED IAW ENGINEERING INSTRUCTION NR W2008A53B-1185 REV.01 2 L 7 3 4F RT A22WE 20081104 SO 2008 11 4 CHQA200800190 1 20081002 A 2700 TRIM SYSTEM EMB 135 EMB135KL 3260302 SO MALFUNCTIONED A CHQA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 11 382SK 145624 AFTER ROTATION ON TAKE-OFF, THE FLIGHT CREW RECEIVED A MAIN PATCH TRIM INOPERATIVE MESSAGE ON EICAS. THE BACK TRIM SYS F UNCTIONED NORMALLY AND TERE WAS NO RUN-AWAY TRIM SITUATION. THE QRH WAS FOLLOWED BUT THE MAIN TRIM WOULD NOT OPERATE. T HE AIRCRAFT LANDED BACK AT EWR WITHOUT INCIDENT. MAINT RESET THE TRIM SYSTEM AND THE MAIN TRIM SYS FUNCTIONED NORMALLY. (K) 2 L 7 2 4F RT T00011AT 20081104 NM 2008 11 4 KCSA081513 1 20081006 A 5711 SPAR BOEING 747 747122 1384872 NM WS 530 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 CORROSION ON FITTING AT WS 530 ON AFT SPAR WEB. (K) 2 L 7 4 4F RT A20WE 20081104 NM 2008 11 4 WX0A070236 1 20080928 A 3350 AD4002 BATTERY PACK DOUG MD88 MD88 3023688 NM EMERGENCY LIGHTS FAILED A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 402NV 49763 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSP, MAINT REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOUL D NOT TEST. MAINT REMOVED AND REPLACED THE APPROPRIATE BATTERIESIN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATI ONAL CHECK WAS ACCOMPLISHED IAW AMM 33-50-00. THE ACFT HAS RETURNED TO SERVICE. (K) 2 L 7 2 4F RT A6WE 20081104 WP 2008 11 4 UPS08853773 1 20081021 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV SURVEY SEQUENCE 702-W4-15, RT LEADING EDGE ACCESS PNL DOUBLER LOCATION 477.750 NOT IN COMPLIANCE WITH SRM (NO SRM REPAIR). VERIFIED DOUBLER MEETS SRM 57-02-00 FIG 2A & TR 57-84. 2 L 7 4 4F RT 4A25 20081104 NM 2008 11 4 DHLA2008745579 1 20080901 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT STA 440 BETWEEN S-2L AND S-3L FRAME WITH DOUBLE HOLE. REPAIRED FUSELAGE FRAME SECTION AT B S 440 BETWEEN S-2L AND S-5L IAW B727 SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 20081104 WP 2008 11 4 IXXA080030O 1 20081029 A 3230 UPLOCK DOUG DC8 DC873F 302199F WP LT MLG DEFECTIVE A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 SW 11 603AL 99733 1590 46003 DURING CLIMBOUT FROM BGTL DOOR NOT LATCH LIGHT ILLUMINATED AFTER RAISING MAIN LANDING GEAR. THE CREW ACCOMPLISHED COM P ROCEDURE AND THE LIGHT STAYED ON. BOTH ALTERNATING MAIN LANDING GEAR LIGHTS WERE OUT AND TESTED GOOD. THE CREW LANDED IN KTOL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT UPLATCH CYLINDER. JACKED AIRCRAFT AND SWUNG GEAR NUMEROUS TIMES. OPERATIONAL CHECK GOOD IAW DACO MAINTENANCE MANUAL 32-30-0. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 20081104 NM 2008 11 4 QXEA2008103001143 1 20081024 A 5420 STRUCTURE BOMBDR DHC8 DHC8402 1390042 NM NR 2 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 413QX 4060 PDX- NR 2 ENGINE NACELLE HAS A CRACKED "SPINE" CLEAT. REPLACED CLEAT IAW RD8/4-71-032. 2 H 7 2 4T RT A13NM 20081104 NM 2008 11 4 QXEA2008103001150 1 20081028 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR DIRTY A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 19 424QX 4006 BOI - F/A REPORTS AFT PAX DOOR HARD TO OPEN. CLEANED AND LUBED C/W OPS CHECK, OPS CHECK NORMAL. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081104 NM 2008 11 4 QXEA2008103001151 1 20081029 A 2920 AE7128852 HYDRAULIC LINE BOMBDR DHC8 DHC8402 1390042 NM NLG LEAKING A QXEA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 NM 19 403QX 4037 PDX - DURING FLIGHT FROM SEA-RNO THERE WAS A HYDRAULIC LEAK OF NR 2 MAIN SYSTEM. OVER RDM QUANTITY REACHED 30 PERCENT. DIVERTED TO PDX AND ACCOMPLISHED A UNEVENTFUL LANDING. FOUND NR 2 HYD SYSTEM READING LOW (2 QUARTS). FOUND HYD FLUID LEAKING FROM RT FLEX LINE THAT ATTACHES TO NLG LOCK ACTUATOR. REMOVED AND REPLACED RT FLEX LINE. REF Q400 AMM TASK 20- 20-11-400-801. BLEED RT FLEX LINE. CYCLED GEAR, NO LEAKS NOTED. SERVICED NR 2 HYD SYSTEM TO CORRECT LEVEL. NO OTHER DEFECTS NOTED. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081104 EA 2008 11 4 MASA2008103000754 1 20081030 A 5210 ROD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DEFECTIVE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 7305V 7305 ASH FLT 2733 TUS-PHX. PASSENGER DOOR FLAPPER DOOR WILL NOT CLOSE. MX REMOVED AND REPLACED FLAPPER DOOR ROD ASSY. 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 MASA2008103000755 1 20081030 A 5210 MECHANISM CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR OBSTRUCTED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 505MJ 10070 ASH FLT 7324 ORD-BHM. PASSENGER DOOR WILL NOT CLOSE. MX REMOVED FOD FROM DOOR INTERIOR, OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 MASA2008102900756 1 20081029 A 5270 SENSOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT OUT OF ADJUST A MASA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 07 926LR 15026 ASH FLT 2926 PHX-RON. LT FWD AND AFT EMERGENCY DOORS INTERMITTENT CAUTION MESSAGES. MX ADJUSTED FWD AND AFT OVERWING D OOR SENSORS. 2 L 7 2 4F RT A21EA 20081104 WP 2008 11 4 AALA200802646 1 20081003 A 5344 39174465 SUPPORT DOUG DC9 DC983 3022083 WP NLG DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CRACK FOUND ON LEFT NOSE LANDING GEAR DOOR FORWARD HINGE SUPPORT ARM. CRACK LENGTH IS .025 INCH. REPLACED SUPPORT ARM AND DOOR RIGGED IN ACCORDANCE WITH MM 32 22 01 2. 2 L 7 2 4F RT A6WE 20081105 WP 2008 11 5 AALA200802558 1 20080923 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP BS 1212 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 TUL CORROSION FOUND ON RT TIE DOWN TRACK SPLICE AT STATION 1212. AREA OF DISCREPANCY IS 6 INCHES BY 2 INCHES. REPLACED SPLICE AT STATION 1212 IN ACCORDANCE WITH SRM 51-10-01. 2 L 7 2 4F RT A6WE 20081105 WP 2008 11 5 AALA200802562 1 20080923 A 5313 S2279223 LONGERON DOUG DC9 DC983 3022083 WP BS 200 L2L CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 LONGERON 2 LT WAS CRACKED AT INBD SIDE AT STATION 200. CRACK LENGTH IS 1/4 INCH. INSTALLED SPLICE REPAIR IN ACCORDANCE WITH SRM 53-02-00 FIGURE 18. 2 L 7 2 4F RT A6WE 20081105 WP 2008 11 5 AALA200802559 1 20080923 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP BS 616-619 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 TUL-CORROSION FOUND ON LT CUSP AT STATION 616 TO 619. AREA OF DISCREPANCY IS 3 INCHES BY 2 INCHES. INSTALLED DOUBLER I N ACCORDANCE WITH AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081105 WP 2008 11 5 AALA200802650 1 20081001 A 3350 0201720003 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 460AA 49565 LGA - EMERGENCY LIGHT AT SEAT 32D INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 32D. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F A6WE 20081105 NM 2008 11 5 AALA200802651 1 20081001 A 3610 DUCT BOEING 757 757223 1384957 NM NR 1 ENGINE LEAKING A AALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SW 21 173AN 32399 LAX - ON CLIMB THROUGH 1000 OVERHEAT LIGHT ILLUMINATED. CREW TURNED OFF ENGINE BLEED SYSTEM AND LIGHT EXTINGUISHED. RE TURNED TO LAX AND LANDED WITHOUT INCIDENT. ON LANDING FOUND NUMBER ONE ENGINE ACCESS PANELS OPEN. REPLACED NUMBER ONE ENGINE HIGH PRESSURE NUMBER 6 DIFFUSER DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081105 WP 2008 11 5 AALA200802635 1 20081002 A 5510 3912033511 HINGE FITTING DOUG DC9 DC983 3022083 WP HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON HORIZONTAL STABILIZER LEFT OUTBOARD HINGE PLATE LUG NUMBER 1. AREA OF DISCREPANCY 2 INCHES BY 2 INCH ES. REPLACED LEFT OUTBOARD LUG IN ACCORDANCE WITH WORKCARD 55 94 05. 2 L 7 2 4F RT A6WE 20081105 WP 2008 11 5 AALA200802639 1 20081002 A 5510 3912033503 HINGE FITTING DOUG DC9 DC983 3022083 WP HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON HORIZONTAL STABILIZER RIGHT INBOARD HINGE PLATE LUG NUMBER 1. AREA OF DISCREPANCY 2 INCHES BY 2 INCH ES. REPLACED RIGHT INBOARD LUG IN ACCORDANCE WITH WORKCARD 55 94 05. 2 L 7 2 4F RT A6WE 20081105 WP 2008 11 5 AALA200802640 1 20081002 A 5510 3912078502 HINGE FITTING DOUG DC9 DC983 3022083 WP HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON HORIZONTAL STABILIZER RIGHT INBOARD OUTBOARD HINGE PLATE LUG NUMBER 2. AREA OF DISCREPANCY 2 INCHES BY 2 INCHES. REPLACED RIGHT INBOARD OUTBOARD LUG IN ACCORDANCE WITH WORKCARD 55 94 05. 2 L 7 2 4F RT A6WE 20081105 SO 2008 11 5 C2XA08RI161 1 20081025 A 5610 163500111 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT SHORTED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 27 14972 8568 145151 FLIGHT 2354 - EWR - FLIGHT CREW REPORTED ELECTRICAL SMELL COMING OUT OF THE GLARESHIELD/FRONT AVIONICS PANEL ON APPROACH . EWR MX REMOVED AND REPLACED LT WINDSHIELD AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RET URN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081105 NM 2008 11 5 HNAA0800312 1 20081020 A 2931 54271158010 INDICATOR DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A HNAA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 07 806EX 27028 30 263 DURING THE TAKEOFF ROLL, THE NR 2 HYDRAULIC SYSTEM INDICATOR WENT TO ZERO. CAUTION LIGHT DID NOT ILLUMINATE AND QUANTIT Y REMAINED STEADY. TAKEOFF WAS ABORTED AT 75 KNOTS IAS. MAINTENANCE REPLACED THE HYDRAULIC PRESSURE INDICATOR. OPS CH ECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 20081105 WP 2008 11 5 UPS08853778 1 20081002 A 5511 RIB DOUG DC8 DC871F 302199D WP HORIZ STAB MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATION AND DISPOSITION EFN 70219911048 ORIGINAL NR 288532 RIB CRACKED AT LOWER END AT XFS 47. EV ALUATED REPAIR FOUND FASTENERS ADDED. FASTENERS TO BE INCORRECT REPLACED WITH HL 926 IAW DC8 SRM 55-02-00-0 FIG 2 ITEM 6. 2 L 7 4 4F RT 4A25 20081105 WP 2008 11 5 UPS08853797 1 20081011 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN 71520041070 ORIG NR 735729 FRAME STA 7 81 AND X20 (CRACK). REPAIR WA S ACCOMPLISHED WITH DC8 SRM 53-02-00 FIG 001B REV 78. 2 L 7 4 4F RT 4A25 20081105 NM 2008 11 5 UPS08M53781 1 20081008 A 5720 SPLICE DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:1C LT WING FIXED L/E SPLICE FOUND CRACKED AT STA 775 COMPARTMENT AREA. REMOVED, FABRICATED, AND INSTALL ED SPLICE IAW DWG ARB3954 AND MD-11 SRM 51-33-01. 2 L 7 3 4F RT A22WE 20081105 NM 2008 11 5 UPS08M53782 1 20081015 A 5754 SKIN DOUG MD11 MD11F 3023600 NM LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 INSPECTION TYPE:1C CRACK FOUND ON LT WING DROOP L/E UPPER SKIN O/B SIDE. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG 30. 2 L 7 3 4F RT A22WE 20081105 EA 2008 11 5 QXEA2008103101034 1 20080923 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 611QX 10041 PDX - C4 - LT IN FLOOR SEAT TRACK AT STN 557.0 IS GOUGED ON TOP SURFACE. BLENDED GOUGE IN TRACK IAW CRJ 700 REO 670-53- 00-013. FPI INSPECTED IAW CRJ 700 NDTM PART 1, 51-20-08, NO CRACKS NOTED. ALODINED AND ID TRACK IAW REO 670-53-00-013. 2 L 7 2 4F RT A21EA 20081105 NM 2008 11 5 SWAA085907 1 20081029 A 5330 654577881 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 960, BETWEEN STR 17R TO STR 18R. REPAIRED SKIN PER SWA EA . 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085908 1 20081029 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085910 1 20081029 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085882 1 20081029 A 3097 16922 WIRE BOEING 737 7375H4 138449D NM COCKPIT DAMAGED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 29 522SW 26564 ON DEPARTURE COWL ANTI ICE VALVE LIGHT ILLUMINATED AND ENG TO COWL C/B POPPED, ACCOMPANIED WITH ACRID SMELL. WHILE ATTE MPTING TO CLOSE VALVE ACRID SMELL RETURNED AND ENG TO WING CONTROL C/B POPPED. NO MORE RESETS WERE ATTEMPTED. FOUND WI RING DAMAGED AT DISCONNECT ATTACHED TO COWL WING ANTI ICE OVERHEAD MODULE. REPAIRED WIRING AND REMOVED AND REPLACED O/H MODULE PER MM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085883 1 20081029 A 3397 DD3016DC GROUND STUD BOEING 737 7373H4 1384600 NM CABIN DEFECTIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FIRST RT OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED EXIT LIGHT ELECTRIC GROUND STUD PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085888 1 20081029 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085889 1 20081029 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 18R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085891 1 20081029 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085892 1 20081029 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 640SW 27713 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085870 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 4L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085875 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 3L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085876 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081104 WP 2008 11 4 UPS08853636 1 20081005 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING UNKNOWN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV RT UPPER LEADING EDGE DOUBLER NEEDS VALIDATION AT STA 325 FAILS APPEN DIX "H" STEP 5 SURVEY SEQ 894- W4-5. REMOVED AND REPLACED REPAIR PER DC 8 SRM 57-2-1 FIG 38 TR 57-85. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853675 1 20081007 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV RT WING OUTBOARD L/E LOWER RIB CRACKED AT XFS 835. STOP DRILLED CRACK IAW SRM 57-2-0 DC8. MANUF AND INSTALLED REPAIR IAW DC8 SRM 51-1-8AND SRM DC8 SRM 51-01-20D-0. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853676 1 20081006 A 5753 FASTENER DOUG DC8 DC873F 302199F WP TE FLAP DEFORMED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-28 LT WING INBOARD FLAP INBOARD EDGE WEB EXT REPAIR DOUBLER HAS 2EA DEFORMED F ASTENER. REPLACED FASTENERS IAW DC8 SRM 51-01-21. 2 L 7 4 4F RT 4A25 20081104 EU 2008 11 4 QML2008F00017 1 20081006 A 6340 CONNECTOR AGUSTA A109 A109 0260109 EU XMSN PRESS IND INTERMITTENT E QMLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 2MF 7277 DEPARTED HOME BASE ON AN IFR FLT. SWITCHED TO DEPARTURE FREQUENCY, TURNED ON THE INITIAL HEADING AND SAW TRANSMISSION P RESSURE GAUGE FLUCTUATING BELOW MINIMUMS. CANCELLED THE CLEARANCE WITH ATC AND RETURNED FOR A NORMAL LANDING PER THE E MERGENCY PROCEDURES. GAUGE CONTINUED TO FLUCTUATE BELOW MINIMUMS THROUGHOUT SHUTDOWN. REPLACED TRANSMISSION OIL PRESS TRANSDUCER AND CONNECTOR. ACFT GROUND RUN AND TRANSMISSION SHOWED NORMAL OPS PRESSURE. 1 G 7 2 3U H7EU 20081104 NM 2008 11 4 UPS08B53763 1 20081026 A 3350 LIGHT BOEING 747 74744AF 13848B2 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 575UP 35664 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR ON MAIN DECK INOP (CEILING LIGHTS). RELAMPED WITH A SERVI CEABLE LAMP IAW BOEING 747-400 AMM 33-51-07-2. OPS CHECK NORMAL. 2 L 7 4 4F RT A20WE 20081104 EA 2008 11 4 ASOA200801406 1 20081027 A 3250 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A ASOA K NONE J WARNING INDICATION CL CLIMB 1 SO 27 870AS 7530 STEERING MSGS CAUTION MESSAGE UPON GEAR RETRACTION. EMERGENCY VEHICLES REQUESTED TO BE ON STANDBY AS A PRECAUTION. 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 ASOA200801407 1 20081027 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 845AS 7324 RIGHT SIDE, FWD OVERWING EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 ASOA200801408 1 20081028 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 PAX DOOR DIFFICULT OPENING FROM INSIDE. FLT 5514 DEL 54 MINS. 2 L 7 2 4F RT A21EA 20081112 SO 2008 11 12 C2XA08RI149 1 20080924 A 3320 BR90002 BALLAST EMB 145 EMB145LR 3260212 SO CABIN FAULTY A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14959 145091 FLT 2325 - EWR - FLT CREW REPORTED BURNING SMELL IN CABIN. EWR MX R&R LIGHT BALLAST AT 5A AND 16A SEAT AREAS. PERFORME D OPS CHECK SUCCESSFULLY. AC WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081112 EA 2008 11 12 COMA0860406 1 20081005 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 967CA 30355 7134 NLG CUTOUT IS CRACKED IN RADIUS ON LT SIDE. REPAIRED PER REO 601R 53-11-048. 2 L 7 2 4F RT A21EA 20081112 EU 2008 11 12 USAA920081807 1 20081004 A 5315 D5347219020300 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL - C7 - MAJOR REPAIR, CORROSION ON FLOORBEAM IN PAX CABIN AT FR 64+10.5 INCHES, BL -Y765. REPLACED FLOORBEAM IN PAX CABIN AT FR 64+10.5 INCHES, BL -Y765 IAW A320SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081112 EU 2008 11 12 USAA920081814 1 20080925 A 5347 D53371112005 SEAT TRACK AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL - C7 - MAJOR REPAIR, CORROSION ON SEAT TRACK(4PLACES) LOCATED BETWEEN FR 41 TO FR 47, -Y1292. REPLACED SEAT TRACK L OCATED BETWEEN FR 41 TO FR 47, -Y1292 IAW A320 SRM 51-72-17. 2 L 7 2 4F RT A28NM 20081112 EA 2008 11 12 COMA0860407 1 20081006 A 5330 601R35004311 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 967CA 30355 7134 STA 640 LT SIDE BONDED DOUBLER IS CRACKED. REPAIRED STA 640 LT SIDE BONDED SKIN PER CRJ REO 601-53-61-506. 2 L 7 2 4F RT A21EA 20081112 EA 2008 11 12 COMA0860410 1 20081005 A 5210 601R31902455 DOOR FRAME CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 967CA 30355 7134 CABIN DOOR FRAME AT STA 380 IS CRACKED. REPAIRED PER CRJ REO 601R-52-11-402 REV H. 2 L 7 2 4F RT A21EA 20081112 EA 2008 11 12 COMA0860409 1 20081005 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 967CA 30355 7134 LT WING FUEL ACCESS HOLE AT 540BB FLANGE HAS FRETTING CORROSION. REPAIRED AREA OF FUEL ACCESS PANEL CUTOUT PER CRJ REO 601R-57-21-030 REV D. 2 L 7 2 4F RT A21EA 20081112 EU 2008 11 12 USAA920081816 1 20081003 A 5320 D53112224201 SUPPORT BRACKET AIRBUS A319 A319112 3930323 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 701UW 0890 PIT - S4 - MAJOR REPAIR, LEVEL 2 EXFOLIATION CORROSION ON SUPPORT BRACKET AT LOWER AFT CORNER OF R1 DOOR CUTOUT. REPLAC ED SUPPORT BRACKET AT LOWER AFT CORNER OF R1 DOOR CUTOUT IAW A319 SRM 51-72-11 . 2 L 7 2 4F RT A28NM 20081112 NM 2008 11 12 DHLA200800122 1 20081105 A 2120 UNKNOWN BOEING 727 727247 138408F NM COCKPIT ODOR A DHLA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 05 793DH 21393 PIREP: KEROSENE SMELL AFTER TAKEOFF IN ILN. DOWNLOADED A/C VISUALLY INSPECTED MAIN CARGO DECK & FWD & AFT PITS NO EVID ENCE OF LEAKS OR SMELL IAW BMM 5-51-0 & 12-40. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745614 1 20080925 A 5330 DOUBLER BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE FROM BS 373 TO BS 383 BETWEEN S-17L AND S-19L DOUBLER REPAIR WITH RIVETS DEFORMED AND RIVET SPACING GREAT ER THAN 8 RIVET DIAMETERS. REPAIRED FUSELAGE SKIN SECTION FROM BS 368 TO BS 386 BETWEEN S-16L AND S-19L IAW COOPESA EO COO-2-53-323-08 DTD 09/29/08. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745615 1 20080925 A 5330 DOUBLER BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE FROM BS 421 TO BS 432 BETWEEN S-17L AND S-19L DOUBLER REPAIR WITH DENT AND RIVETS DEFORMED. REPAIRED FUS ELAGE SKIN SECTION FROM BS 416.5 AND BS 435.5 BETWEEN S-16L AND S-19L IAW B737 SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745617 1 20081008 A 5322 SHEAR TIE BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 580 BETWEEN S-26R AND S-27R SHEAR TIE WITH CORROSION. REPLACED FUSELAGE SHEA R TIE SECTION AT BS 580 BETWEEN S-26R AND S-27R AFT SECTION IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081107 EA 2008 11 7 REX2008F00050 1 20081029 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA OUT OF RIG A REXA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 25 8907A 7907 FLAPS FAILED ON APPROACH WHEN SELECTED TO 30 DEGREES. VREF ADJUSTED AND APPROACH CONTINUED WITH UNEVENTFUL LANDING. RE SET FLAPS AND PERFORMED RIG CHECK PER BOMBARDIER AMM. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081107 WP 2008 11 7 AALA200802547 1 20080918 A 5320 PAN DOUG DC9 DC982 3022082 WP GALLEY DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7527A 49919 CORROSION FOUND ON FORWARD SERVICE DOOR AT GALLEY DRAIN PAN AT STATION 160. AREA OF DISCREPANCY WAS 8.5 INCHES BY 9 INC HES. INSTALLED DOUBLER IN ACCORDANCE WITH SRM 52-20-00-16. 2 L 7 2 4F A6WE 20081107 NM 2008 11 7 SWAA086041 1 20081030 A 3350 65C27095 BATTERY PACK BOEING 737 737317 138447P NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 698SW 23176 FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086031 1 20081104 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER EA. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086037 1 20081104 A 3350 20121 RETAINER BOEING 737 7373H4 1384600 NM BATTERY CHARGER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY LIGHT BATTERY CHARGER RETAINER BROKEN. REMOVED AND REPLACED RETAINER PER MM. 2 L 7 2 4F RT A16WE 20081107 GL 2008 11 7 SWAA086000 2 20081103 A 7261 J221P147 GARLOCK SEAL BOEING 737 7373H4 1384600 NM CFMINT CFM56 CFM563B1US GL NR 1 ENGINE LEAKING A SWAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 29 369SW 26580 DIVERSION, NR 1 ENG OIL QUANTITY LOSS INDICATION. FOUND OIL LEAK AT NR 1 ENG FUEL PUMP. REMOVED AND REPLACED GARLOCK S EAL PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 20081107 NM 2008 11 7 SWAA086007 1 20081103 A 5534 6547450 DRAG ANGLE BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STAB FITTING DRAG ANGLES CORRODED. REMOVED AND REPLACED DRAG ANGLES PER SRM. 2 L 7 2 4F RT A16WE 20081110 NM 2008 11 10 UPS08M53852 1 20081104 A 5753 NCR6055507 SKIN DOUG MD11 MD11F 3023600 NM TE FLAP DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 286UP 48453 INSPECTION TYPE:N/A RIVETS PULLED THROUGH UPPER SKIN OF INBOARD FLAP LT WING. REPAIR IAW EO MD11-5750-31055-B. 2 L 7 3 4F RT A22WE 20081110 EA 2008 11 10 SWIA200820272 1 20080629 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 913SW 7597 LEFT ENGINE REAR MOUNT THRUST FITTING SPHERICAL BALL END CORRODED (C-CHECK). REPLACED BALL END. 2 L 7 2 4F RT A21EA 20081110 WP 2008 11 10 AALA200802553 1 20080923 A 5320 ANGLE DOUG DC9 DC983 3022083 WP BS 826 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 LT ANGLE CRACKED AT TOP OF CENTER AUXILIARY FUEL TANK BELOW SEAT TRACK NR 5 AT STATION 826. INSTALLED STACK DOUBLERS IN ACCORDANCE WITH ESO 80559 DATED 24 SEP 2008. 2 L 7 2 4F RT A6WE 20081110 WP 2008 11 10 AALA200802567 1 20080918 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP BS 219 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 CORROSION FOUND ON RT CABIN FLOOR CUSP MEMBRANE AT STATION 219. AREA OF DISCREPANCY IS 4 INCHES BY 6 INCHES WITH A DEPT H OF .015 INCH. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081110 WP 2008 11 10 AALA200802554 1 20080923 A 5320 ANGLE DOUG DC9 DC983 3022083 WP BS 826 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 RT ANGLE CRACKED AT TOP OF CENTER AUXILIARY FUEL TANK AT STATION 826. INSTALLED STACK DOUBLERS IN ACCORDANCE WITH ESO 8 0559 DATED 24 SEP 2008. 2 L 7 2 4F RT A6WE 20081110 NM 2008 11 10 08FDEA04714 1 20081105 A 5730 SKIN BOEING 757 75723A 1384967 NM ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 RT WING O/B MAIN FLAP O/B L/E CORNER HAS 4 INCH CHAFF MARK (FROM LOWER WING PANEL). DEFECT REPAIRED IAW EA F-5750-120571 . REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 2 4F RT A2NM 20081110 EA 2008 11 10 SWIA200820285 1 20080708 A 5210 WEB CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 821SK 15109 AFT PASSENGER DOOR CRACKED IN ZONE 2 WEB. (C-CHECK)REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081110 EU 2008 11 10 08FDEA04730 1 20081105 A 5542 SKIN AIRBUS 310 A310 EU RUDDER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 420FE HF1005 339 THERMOGRAPHY INSPECTION OF RUDDER S/N HF1005 SHOWS 3 AREAS OF POSSIBLE DEFECTS, LT SIDE- CONFIRMED BY ULTRASONIC INS P. DEFECTS AT NEAR FASTENERS 9,13 AND 20 COUNTED FROM TOP OF RUDDER REMOVED DAMAGED AREAS AND REPAIRED LT SIDE OF RUDD ER IAW EA 6-5540-118122. 2 L 7 2 4F RT A35EU 20081110 CE 2008 11 10 MAS2008F00102 1 20080930 A 3240 BRAKE ASSY RAYTHN DH125 HAWKER800XP 7150012 CE MLG WEAK A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 872QS 258472 LEFT BRAKE ON POLOTS SIDE HAS NO BRAKE PRESSURE. 2 L 7 2 4F RT A3EU 20081110 NM 2008 11 10 USAA920081825 1 20081004 A 5320 6935352Y1 TIE CLIP BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, STRINGER TIE CLIP CRACKED AT BS 807, S4L. REPLACED STRINGER TIE CLIP AT BS 807, S4L IAW B737 S RM 51-10-01 & BOEING DRAWING 69-35352. 2 L 7 2 4F RT A16WE 20081112 WP 2008 11 12 AALA200802339 1 20080910 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 472AA 49647 EMERGENCY LIGHT AT SEAT 15D MISSING LENS. REPLACED LENS. GROUND CHECKED NORMAL. 2 L 7 2 4F A6WE 20081112 NM 2008 11 12 DHLA2008745647 1 20081012 A 5322 SHEAR TIE BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT SHEAR TIE WITH CORROSION AT BS 700 BETWEEN S-25L AND S-26L. REPLACED SHEAR TIE AT BS 700 BETWEEN S-25L AND S-26L IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081112 NE 2008 11 12 DL76P081462 2 20081025 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 FAILED A DALA E A ENGINE SHUTDOWN UNSCHED LANDING B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS CR CRUISE 1 SO 27 1402A 35579 25989 23843 OIL LOSS IN FLIGHT AND IFSD. REPLACED RT ENG PER TRANSMITTAL 1T149AD9. 2 L 7 2 4F 4 F RT A1NM E24NE 20081112 NM 2008 11 12 DHLA2008745606 1 20080905 A 5753 SKIN BOEING 727 727224 1384076 NM TE FLAP CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 RT WING I/B MID FLAP L/E INNER SKIN WITH CORROSION AT WBL 136. REPAIRED RT WING INBOARD MID FLAP LEADING EDGE SKIN SECT ION FROM WBL 134 TO WBL 140 IAW COOPESA EO COO-2-57-321-08 DTD 09/29/08. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 USAA920081817 1 20080905 A 5320 65479573 WEB BOEING 737 7373G7 138447J NM CARGO BAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 SAL - C17 - MAJOR REPAIR, CRACKS ON WEB AT AFT CARGO COMPARTMENT FLOOR STRUCTURE BETWEEN BS 787 TO BS 847 S25R TO 26R. REPLACED WEB AT AFT CARGO COMPARTMENT FLOOR STRUCTURE BETWEEN BS 787 TO BS 847 S25R TO 26R IAW B737 SRM 51-10-0G AND BOE ING DRAWING 6547-957. 2 L 7 2 4F RT A16WE 20081112 NM 2008 11 12 USAA920081812 1 20080922 A 5312 6416300 BULKHEAD BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - MAJOR REPAIR - C18 CHECK, CRACKED BULKHEAD WEB SKIN, BS 178, RBL 5.7, WL 212. REPAIRED BULKHEAD WEB SKIN, BS 178, RBL 5.7, WL 212 IAW B737 SRM 53-10-08-2R10 FIGURE 201. 2 L 7 2 4F RT A16WE 20081112 NM 2008 11 12 DHLA2008745616 1 20081008 A 5313 STRINGER BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 482.5 S-27L WITH CORROSION. REPAIRED FUSELAGE STRINGER 27L FROM BS 476 TO BS 517 IAW B727 SRM 53-10-3 FIG 1 DETAIL 1. 2 L 7 3 4F A3WE 20081113 EA 2008 11 13 TRAX200801301 1 20081002 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 PAX DOOR FORWARD SIDE SKIN IS CRACKED AT HANDRAIL STOP/SUPPORT BRACKET. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 TRAX200801302 1 20081002 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 JOB 8752811 OP 357 PAX DOOR OUTER HANDLE IS CRACKED. RESOLVED ON W/O 101539 TASKCARD NR 00442. PAX DOOR OUTER HANDLE BEING REPLACED UNDER 8752815/5771. REF 8752815/5771 FOR MX ACTION. 2 L 7 2 4F RT A21EA 20081113 2008 11 13 DXTA2008110603338 4 20081105 A 3120 CIRCUIT BREAKER CESSNA 500 560CESSNA 2076750 CE COCKPIT POPPED E DXTA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 806QS 5600614 DURING FLIGHT THE RIGHT CLOCK CIRCUT BREAKER POPPED FOLLOWED BY A BURNING SMELL THAT LASTED FOR 5-10 SECONDS. 2 L 7 2 4F RT A22CE 20081113 NM 2008 11 13 DHLA2008745644 1 20080906 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER TX TAXI/GRND HDL 1 GL 05 745DH 20665 LOWER FUSELAGE AFT CARGO COMPARTMENT BS 970 BETWEEN S-26L AND 27L FRAME CRACK. REPAIRED FRAME SECTION AT BS 970 BETWEEN S-24L AND S-28L IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 QXEA2008110601168 1 20081101 A 6123 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 19 410QX 4053 GEG - AUTOFEATHER FAILED TO ARM ON TAKEOFF ROLL. ABORTED TAKEOFF. RETURNED TO GATE. PERFORMED OPERATIONAL TEST OF THE PROP AUTOFEATHER AND UPTRIM SYSTEM IAW Q400 AMM TASK 61-20-00-710-801. OPS CHECK GOOD. A/C OK FOR SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081113 NM 2008 11 13 QXEA2008110601170 1 20081104 A 2913 6617303 PUMP BOMBDR DHC8 DHC8402 1390042 NM HYDRAULIC SYS FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 19 408QX 8982 4050 SEA - NR 1 ENG HYD PUMP, NR 1 HYD ISO VLV, AND ASSOCIATED CAUTION LIGHTS ILLUMINATED FOLLOWING TAKEOFF AND AFTER THE AFT ER TAKEOFF CHECKLIST WAS ACCOMPLISHED TURNING OFF ALL HYDRAULIC PUMPS. DIVERTED TO SEA. NR 1 ENG EDP REMOVED AND REPLA CED, NR 1 HYD SYSTEM FILTERS REMOVED AND REPLACED. NR 1 HYD SYSTEM FLUSHED. GROUND RUNS OPS AND LEAK CHECKS GOOD. RET URNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081113 NM 2008 11 13 KCSA081562 1 20081107 A 5534 ANGLE BOEING 747 747212B 1384886 NM VERTICAL STAB CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 VERTICAL STAB, FIN STA 586 HAS A 5 INCH CRACK IN AN ANGLE THAT ATTACHES INTO THE FRONT SPAR WEB AT BL 0 TO RBL 5. 2 L 7 4 4F RT A20WE 20081113 WP 2008 11 13 ABXA11070258 1 20081028 A 2510 2925379523ABX1 SEAT DOUG DC9 DC941 302207N WP COCKPIT LACK OF LUBE A ABXA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 23 959AX 832 47761 ON DEPARTURE ROLL FROM BHM CAPT'S SEAT SLID FULL AFT. ABORTED T/O AT 110 KTS. LUBED CAPTAIN SEAT MECH & LINKAGE OPS CH ECK GOOD PER AMM 25-00. PER MAINT CONTROL REQUEST FOR FOLLOW-UP MAINTENANCE, CAPTAIN'S SEAT WAS VERIFIED TO LOCK IN SEL ECTED POSITION AND OPS CHECKED GOOD IAW DC9 MM 25-00-00. 2 L 7 2 4F A6WE 20081113 EU 2008 11 13 AALA200802684 1 20081005 A 3350 P401049 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 70054 461 JFK - EMERGENCY PATH LIGHTS ON SEATS 7C TO 18C ARE DIM IN TEST MODE. REPLACED BATTERY PACK FOR DIM EMERGENCY PATH LIGHT S. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081113 WP 2008 11 13 AALA200802686 1 20081007 A 3320 BALLAST DOUG DC9 DC983 3022083 WP CABIN FAULTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 562AA 49344 DEN - INFLIGHT STL TO LAX. CREW REPORTED STRONG ELECTRICAL SMELL IN AFT CABIN. FLIGHT ATTENDANT REPORTED BURNING EYES AND PASSENGERS GETTING NAUSEOUS. LANDED DEN WITHOUT INCIDENT. FOUND OVERHEAD LIGHT AT SEAT 29 FAULTED AND BALLAST GIVI NG OFF ELECTRICAL SMELL. REPLACED BALLAST AND SHORT HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081113 WP 2008 11 13 AALA200802687 1 20081007 A 2560 1001191 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7519A 49896 LAX - EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED PORTABLE EMERGENCY LIGHT. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081113 NM 2008 11 13 AALA200802689 1 20081008 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM CABIN LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 797AN 30012 NRT - EMERGENCY FLOOR LIGHTING FORWARD OF LEFT NUMBER ONE CLOSET DOOR AT FIRST CLASS GALLEY LOOSE. REPOSITIONED FLOOR L IGHT ASSEMBLY FORWARD OF LEFT NUMBER ONE CLOSET DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081113 NM 2008 11 13 AALA200820002 1 20081007 A 5320 146N52468 SUPPORT BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 670AA 52802 25335 RT THRESHOLD DRAIN PAN, SUPPORT IS CORRODED. 2 L 7 2 4F RT A2NM 20081113 NM 2008 11 13 AALA200820003 1 20081007 A 5320 146N27131 SUPPORT BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 670AA 52802 25335 SUPPORT IS CORRODED. 2 L 7 2 4F RT A2NM 20081113 NM 2008 11 13 AALA200820000 1 20081007 A 5320 146N52465 SUPPORT BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 670AA 52802 25335 LT THRESHOLD GUTTER DRAIN, SUPPORT IS CORRODED AT STATION 1640 TO STATION 1680. 2 L 7 2 4F RT A2NM 20081107 NM 2008 11 7 2008UALA06346 1 20081101 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 677UA 30029 SEAT MOUNTED EMERGENCY LAMP STRIP AT 26HJ IS INOP. TRIED A NEW STRIP LAMP ASSY, NO HELP. REPAIRED LOOSE PLUG UNDER SEA T. OP'S CHECKED GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081110 CE 2008 11 10 GUUA11030801 1 20081103 A 3230 UNKNOWN BEECH 1900 1900D 1154162 CE NLG NOISY A GUUA O OTHER O OTHER TO TAKEOFF 1 SO 29 81536 UE152 FLIGHT 5403 MIA/FLL - AFTER TAKEOFF RETRACTING LANDING GEAR A "CLUNK AND THUD" IS HEARD FROM NOSE WHEEL, GEAR FUNCTIONS NORMALLY AND VISUAL INSPECTION DOES NOT LOOK ABNORMAL. PERFORMED LANDING GEAR OPERATIONAL CHECK. NO DEFECTS NOTED. 2 L 7 2 4T RT A24CE 20081110 NM 2008 11 10 UPS08M53855 1 20081020 A 5720 STRAP DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:3C RT WING L/E SKIN SPLICE STRAP XFS 669 CRACKED. REMOVED, FABRICATED, AND INSTALLED SPLICE STRAP IAW D WG ARB 3954. 2 L 7 3 4F RT A22WE 20081110 NM 2008 11 10 USAA920081977 1 20081023 A 5311 65C22908 FRAME BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03C20853011/019 CRACK AT FRAME BS500B, BETWEEN S20L AND S21L. REPAIRED FRAME AT BS500B, BETWEEN S20L AND S21L IAW B737 SRM 53-00-07 REPAIR 13. 2 L 7 2 4F RT A16WE 20081110 WP 2008 11 10 I5HA0858005F 1 20080717 A 5320 340311020757 CHANNEL CVAC 340 34031 2422704 WP ALLSN 501D 501D13 03004 GL ALLSN A6441 A6441FN606 GL DAMAGED A I5HA O OTHER O OTHER NR NOT REPORTED 1 GL 25 581P 29 DURING A STORM ON APRIL 6, 2008 A CARGO CAN (ULB) WAS THROWN INTO THE RT SIDE OF ACFT. THE RT PROPELLER WAS ALSO STRUCK A GLANCING BLOW. THERE WAS SIGNIFICANT DAMAGE TO THE SKIN AND SUPPORT STRUCTURE BENEATH THE SKIN. THERE WAS DAMAGE TO WI RING IN THE AREA. THE NOSE STEERING ACTUATOR WAS ALSO DAMAGED. DAMAGE AREA WAS BETWEEN FUSELAGE STATIONS 72 TO 125 AT AP PROXIMATELY BETWEEN STRINGERS 11 AND 3. THE PROPELLER AND REDUCTION GEARBOX WERE REMOVED AND INSPECTED. NO DAMAGE TO EIT HER. ACFT WAS REPAIRED AND THE ACFT TEST FLOWN ON JULY 3, 2008. THE AIRCRAFT WAS RETURNED TO SERVICE JULY 8, 2008. 2 L 7 2 4R 4 T 6A6 E282 6 C P898 20081110 WP 2008 11 10 08FDEA04721 1 20081105 A 5755 NRC6050507 SKIN DOUG DC10 DC1030F 3023504 WP NR 4 SPOILER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 LT WING NR 4 SPOILER FOUND CRACK ON UPPER SURFACE SPOILER. 2 L 7 3 4F RT A22WE 20081110 NM 2008 11 10 08FDEA04659 1 20081031 A 5311 BAC1503100028 FRAME BOEING 727 7272D4 138407U NM BS 520 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FWD PIT LEFT SIDE FRAME, BS 520 AT STR 24L , UPPER FLANGE HAS 2 EA.DENTS WITIN 3". INSTALLED FRAME REPAIR AFTER REMOVI NG DAMAGE FROM FRAME. (CLASSIFIED AS A MAJOR REPAIR) REF SRM 51-40-06 PG 1-6 2 EA. DENTS REMOVED BY CUTOUT. FABRICATED NEW FRAME REPAIR, ALODINE, PRIMED PART. INSTALLED REPAIR AS REQUIRED. NO OTHER DEFECTS NOTED THIS IS CLASSIFIED AS A MAJOR REPAIR 2 L 7 3 4F A3WE 20081110 NM 2008 11 10 08FDEA04722 1 20081105 A 5230 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 593FE 48551 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 4 FOUND WI TH CRACK INDICATION AT HOLE C. CARRIED OUT BUSHING REPAIR AS PER SRM 53- 50-00, FIGURE 10, VOLUME I. REPAIR CLASSIFIE D MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081110 SO 2008 11 10 SWIA200820295 1 20080924 A 5320 FITTING EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 227SW 120304 FLOOR SUPPORT CLIP ON INTERIOR FS 38 CORRODED. (C-CHECK)REPLACED. 2 L 7 2 4T RT A31SO 20081110 EA 2008 11 10 SWIA200820313 1 20081030 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 449SW AFT CEILING EMERGENCY LIGHT INOP. (FLT 3852)RELAMPED. 2 L 7 2 4F RT A21EA 20081110 EU 2008 11 10 COEA0802917 1 20081018 A 5320 FLOOR SUPPORT AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CRACKED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 917FX 354 MAJOR REPAIR, LT FLOOR SUPPORT BEAM THAT RUNS FROM FR 20 TO 25 IS CRACKED. OPEN 2 H 7 2 4T RT A53EU 20081112 NE 2008 11 12 EIA2008F00010 2 20080929 A 7200 ENGINE BOEING 747 747212B 1384886 NM PWA JT9 JT9* 52054 NE NR 2 SURGES A EIAA E A ENGINE SHUTDOWN UNSCHED LANDING R E J PARTIAL RPM/PWR LOSS VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 NM 09 485EV 20712 689564 DURING CRUISE, ENCOUNTERED HEAVY SURGE IN NR 2 ENGINE ALONG WITH VIBRATION, EPR DROPPED TO BOTTOM OF SCALE, EGT REACHED YELLOW BAND, REDUCED POWER TO IDLE, VIBRATION PERSISTED, SHUTDOWN NR 2 ENGINE, WINDMILLED OIL PRESSURE AT 28 PSI. 2 L 7 4 4F 4 F RT A20WE E20EA 20081112 EU 2008 11 12 DHLA200800108 1 20080930 A 3350 311701 BATTERY PACK AIRBUS 300 A300B4203 3930306 EU EMERGENCY LIGHTS INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 GL 05 367DH 265 ON PRE-DEPARTURE CHECK, EMERGENCY LIGHT OVER R1 DOOR INOPERATIVE, ACFT GROUNDED. R&R POWER SUPPLY IAW MM 33-51-14. OPS CHECKED OK IAW 33-51-00. 2 L 7 2 4F RT A35EU 20081112 NM 2008 11 12 DHLA2008745634 1 20080902 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT BS 520 BETWEEN S-16R AND 17R FRAME WITH DENT. REPAIRED FRAME SECTION AT BS 520 BETWEEN S-1 6R AND S-17R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745635 1 20080902 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT BS 500 BETWEEN S-16R AND S-17R FRAME WITH DENT. REPAIRED FRAME SECTION AT BS 500 BETWEEN S -16R AND S-17R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745636 1 20080902 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT BS 460 BETWEEN S-16R AND S-17R FRAME WITH DENT. REPAIRED FRAME SECTION AT BS 460 BETWEEN S -16R AND S-17R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DL757081468 1 20081028 A 5350 SUPPORT BOEING 757 757232 1384965 NM FAIRING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 23843 WHILE WORKING CUSTOMER CARD 00068 FOUND FAIRING SUPPORT STRUCTURE CRACKED AT BS 780-800 BL 0. REMOVED AND REPLACED FAIR ING SUPPORT STRUCTURE BS 780-800 BL 0 IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081112 NM 2008 11 12 DL764081471 1 20081029 A 2530 OVEN BOEING 767 767432ER 1385134 NM AFT GALLEY MALFUNCTIONED A DALA F A ACTIVATE FIRE EXT. UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 845MH 29719 23843 DURING CLIMB F/A NOTICED A BLUEISH HAZE AND ODOR IN AFT CABIN. NR 3 AND 4 OVENS IN AFT GALLEY VERY HOT. COULD NOT TURN OFF NR 3 OVEN AND DISCHARGED HALON BOTTLE. REPORTED AFT CABIN LIGHTS COMING ON AND BRIGHT ON THEIR OWN LIKE A POWER SU RGE. UNABLE TO CONTROL THEM. MTC IN PROGRESS. OPERATED NR 3 OVEN AND CHECKS NORMAL. OPERATED LIGHTS AND CHECKS NORMAL . MTC STILL T/S. DEACVT NR 3 AND 4 OVENS AS PRECAUTION. PERFORMED HIGH PWR ENG RUN TO ASSURE NO SMOKE/ODOR FROM PNEU SYS. 2 L 7 2 4F RT A1NM 20081112 CE 2008 11 12 HDNA200811030001 1 20081101 A 7110 1019100251 COWLING BEECH 200 B200 1152922 CE PWA PT6 PT6A41 52043 EA HARTZL HCB3T HCB3TN3 GL NR 1 ENGINE DEPARTED E HDNA A UNSCHED LANDING E D P VIBRATION/BUFFET INFLIGHT SEPARATION NO WARNING INDICATION CR CRUISE 1 SW 03 315MS 11674 180 BB404 PCE80866 BUA26739 DURING CRUISE FLIGHT, THE AIRCRAFT SHUDDERED LIGHTLY AND THE PILOT SAW A FLASH OF WHITE. THE NR 1 ENGINE TOP FORWARD CO WLING DISENGAGED FROM THE AIRPLANE. INITIAL THOUGHT WAS A BIRD STRIKE, BUT THERE WAS NO VISIBLE EVIDENCE. THE ENGINE I NSTRUMENTS WERE MONITORED CLOSELY AND NO ABNORMAL ENGINE INDICATIONS WERE NOTED. POWER AND AIRSPEED WAS REDUCED AND AN UNEVENTFUL LANDING WAS MADE BACK AT THE HOME BASE. UPON INSPECTION AFTER LANDING IT WAS NOTED THAT BOTH OUTBOARD LOCKIN G LATCHES WERE IN THE LOCKED POSITION. THE INBOARD AFT LOCKING LATCH WAS IN THE LOCKED POSITION WITH THE COWLING SIDE L ATCH COMPONENTS STILL ATTACHED. THE INBOARD FORWARD LATCH WAS NOT IN THE LOCKED POSITION AND WAS HANGING LOOSELY. THE 1 L 7 2 4T 4 T A24CE E4EA 6 C P15EA 20081112 EA 2008 11 12 COMA0860411 1 20081005 A 5311 60036030 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 967CA 30355 7134 FRAME AT FS 718 LT SIDE BETWEEN STR 10L AND 11L IS CRACKED. PERFORMED REPAIR IAW SERVICE BULLETIN 601R-53-055 AND AE10- 5361-02357. 2 L 7 2 4F RT A21EA 20081112 SO 2008 11 12 C2XA08RI150 1 20080927 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 16919 145393 FLT 3077 - EWR - FLT CREW REPORTED EMERGENCY LIGHTS INOPERATIVE. EWR MX RESET EMERGENCY LIGHT SYSTEM AND PERFORMED OPS CHECK SUCCESSFULLY. AC WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081113 NM 2008 11 13 DHLA2008745622 1 20080904 A 5313 STRINGER BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT BS S-5L WITH CRACK. REPLACED FUSELAGE S-5L FROM BS 350 TO BS 360 IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745624 1 20080906 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT BS 312 BETWEEN S-13R AND 14R FRAME WITH CRACK. REPAIRED FRAME SECTION AT BS 312 BETWEEN S- 10R AND S-14R IAW B727 SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 USAA920081936 1 20081022 A 5330 SKIN BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03C00053006/001 FUSELAGE SKIN AT EXTERNAL POWER RECEPTICAL LOWER LATCH IS CRACKED ON INSIDE AT BS 219, S23R. REPAIRED FUSELAGE SKIN AT EXTERNAL POWER RECEPTICAL LOWER LATCH ON INSIDE AT BS219, S23R IAW US AIRWAYS EA N R 100686. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 USAA920081947 1 20081022 A 3350 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 833AW 1844 LOGPAGE 8342523 FLT NR 158 PHX-STL EMERGENCY LIGHT FLIGHT ATTENDANT FORWARD FLASHLIGHT INOPERATIVE. R&R BATTERY. OPS C HECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081113 NM 2008 11 13 DHLA2008745645 1 20080906 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 520 BETWEEN S-25R AND S-26R FRAME WITH DOUBLE HOLES AND CORROSION. REPAIRED FRAME SECTION AT BS 520 BETWEEN S-21R AND S-28R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20081113 EA 2008 11 13 ASOA200801454 1 20081104 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 CARGO COMPARTMENT DOOR BEAM AFT LOWER ANGLE AT REAR PRESSURE BULKHEAD IS CRACKED. REMOVED AND REPLACED CRACKED ANGLE AT CARGO COMPARTMENT DOOR BEAM AT LOWER AFT PRESSURE BULKHEAD IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801455 1 20081104 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 RIGHT FS 484.00 ANGLE AT RBL 27 IS CRACKED .5 INCH LONG IN UPPER RADIUS. 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 ASOA200801409 1 20081029 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 861AS 7445 PAX DOOR WOULD NOT CLOSE. 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 ASOA200801411 1 20081028 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA ASD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 927EV 7844 ASD BOTTOM STEP IS CRACKED. 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 ASOA200801414 1 20081029 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 PAX DOOR STILL DIFFICULT TO OPEN FROM INSIDE. 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 ASOA200801416 1 20081030 A 5311 FRAME CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 CORROSION ON 280 FRAME AT RBL 9. CORROSION OUT OF LIMITS. REMOVED AND REPLACED FRAME. 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 ASOA200801417 1 20081030 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 CORROSION ON FWD FLOOR SUPPORT AT STA 280. CORROSION ON FWD FLOOR SUPPORT AT STA 280 IS OUT OF LIMITS. REMOVED CORRODE D SUPPORT, LOCATED DRILL AND INSTALLED NEW SUPPORT PER CRJ 700 SRM 51-40-00, 51-42-06 AND 51-44-00. SUPPLEMENTAL-SDR CL OSED 11/17/2008. 2 L 7 2 4F RT A21EA 20081104 EA 2008 11 4 ASOA200801419 1 20081030 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 CORROSION ON LT 280 WEB. REMOVED AND REPLACED LT 280 WEB PER CRJ 700 SRM 51-42-06 AND 51-42-13. FINISHED REMOVING REMA INING FASTENERS AND UNINSTALLED LT WEB AND WEB STRAP AT FS 280 IAW CRJ 700 SRM 51-42-06 AND 51-52-21. FABRICATED NEW LT SPLICE PLATE (P/N CC670-34251-1) IAW CRJ 700 SRM 51-24-16 AND 700 SRM 53-11-10. INSTALLED LT WEB AND ATTACH ANGLES PER CRJ 700 SRM 51-42-06 + 51-42-13. SUPPLEMENTAL-SDR CLOSED 11/17/2008. 2 L 7 2 4F RT A21EA 20081104 EU 2008 11 4 ASOA200801420 1 20081030 A 3350 LIGHT AEROSP ATR72 ATR72 EU CABIN MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 636AS 375 EMERGENCY LIGHTS WILL NOT TURN OFF. 2 H 7 2 4T RT 20081104 EA 2008 11 4 ASOA200801421 1 20081030 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 834AS 7254 MAIN PAX DOOR HARD TO PULL CLOSE LAST 2 FEET. 2 L 7 2 4F RT A21EA 20081104 NM 2008 11 4 K11A2008103172202 1 20081030 A 5343 STIFFENER BOEING 727 7272H3 138368N NM NLG CRACKED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 LT FORWARD EDGE ON NLG TRUNNION SUPPORT VERTICAL STIFFENER IS CRACKED 3 INCHES STA 320, LBL 16, WL 149. 2 L 7 3 4F RT A3WE 20081104 EA 2008 11 4 QXEA2008103101044 1 20080923 A 5320 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 611QX 10041 PDX - C4 - CORROSION ON TOP OF CROSSBEAM AT FS 280 FROM APPROX RBL 15 TO LBL 15. REMOVED DAMAGED AREA OF 280 BEAM, DRIL LED UP AND CUT NEW BEAM, FABRICATED NEW SPLICE DOUBLERS FROM .040 2024-T3 IAW REO 670-53-11-047. INSTALLED NEW 280 BEAM WITH SOLID RIVETS, CHERRY MAX AND HI LITE FASTENERS REF REO 670-53-11-047 AND CRJ SRM 51-42-06. 2 L 7 2 4F RT A21EA 20081105 WP 2008 11 5 AALA200802560 1 20080923 A 5320 99365801 INTERCOSTAL DOUG DC9 DC983 3022083 WP BS 769-786 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 INTERCOSTAL CRACKED IN MID CARGO CEILING AT STATION 769 TO 786. CRACK LENGTH IS 2 INCHES. REPLACED INTERCOSTAL IN ACCO RDANCE WITH AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081105 NM 2008 11 5 SWAA085877 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085878 1 20081028 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 6L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085880 1 20081029 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085881 1 20081029 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085894 1 20081029 A 5313 6551698 STRINGER SPLICE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 25R. REMOVED AND REPLACED SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20081113 EA 2008 11 13 ASOA200801456 1 20081105 A 5230 TRACK CNDAIR CL600 CL6002B19 1900309 EA CARGO TRACK CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 CARGO DOOR FWD TRACK TO COAMING CLIP IS CRACKED AT MID TRACK SUPPORT. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801457 1 20081106 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 717EV 10088 EMERGENCY LIGHT WILL NOT ILLUMINATE DURING COCKPIT CHECK. 2 L 7 2 4F RT A21EA 20081113 WP 2008 11 13 ABXA200811120263 1 20081106 A 3350 60030451 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 967AX 688 47509 COCKPIT EMERGENCY LIGHTS DIM. DEFERRED: 62445 REMOVED AND REPLACED 1.2 VDC BATTERIES IAW 33-53-02-4. OPS CHECK GOOD. BATTERY PACK NEED REPLACED WITHIN 3 FLT DAYS. DEFERRED FOR TRACKING PER AMM 33-53-00-8 & GMM 07.04. MPCW. PLACARD IN STALLED. CODE 2. CLEARED DI 62445 REMOVED AND REPLACED EMERGENCY POWER BATTERY SUPPLY IAW DC9 MM 33-53-02-4, SYS CHECK S GOOD IAW 33-53-00-5 - PLACARD REMOVED. 2 L 7 2 4F A6WE 20081113 NM 2008 11 13 ABXA200811070262 1 20081105 A 3350 BATTERY BOEING 767 767281 1385109 NM CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 786AX 23019 EMERGENCY LIGHTS INOP. DEFERRED DI 62414 SPARE EMERGENCY LIGHT BATTERY DEFERRED FOR MAINT TRACKING IAW ABX GMM 01.07.04 REPLACE WITHIN 7 DAYS DEFERRED PER B767 AMM 33-51-07-2 PLACARD INSTALLED MBCB 11-22-08. CLEAR DI 62414 REMOVED BOTH BA TTERYS, CHECK BOTH BATTERY CHARGER, BOTH OPERATE NORMALLY, REINSTALLED PRIMARY BATTERYS, INSTALLED NEW BATTERY IN SECOND ARY POSITION, CHECK SYSTEM PER 33-51-07-2, OPS CKS NORMALLY. 2 L 7 2 4F RT A1NM 20081113 WP 2008 11 13 ABXA200811130264 1 20081024 A 3350 60030451 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 957AX 277 47759 EMERGENCY LIGHTS INOP SWITCH LEFT ON. REPLACED EMERGENCY LIGHT BATTERY PACK AS PER DC9 MM 33-53-0. 2 L 7 2 4F A6WE 20081113 NM 2008 11 13 ABXA200811130265 1 20081024 A 3350 20131A BATTERY PACK BOEING 767 767231 1385131 NM CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 708AX 22571 ON SERVICE CHECK, FOUND EMERGENCY LIGHTS INOP. DEFERRED NR 62289, SWAPPED EMERGENCY BATTERY PACKS P/N 2013-1A, S/N 6078 1 AND LOWER S/N 61030 AS REQUIRED. OPS CHECK NORMAL. DEFERRED FOR TRACKING IAW 767 GMM 07.04 PLACARD INSTALLED CODE 11 . CLEARING DI 62289. REMOVED AND REPLACED LOWER EMERGENCY LIGHTING BATTERY PACK. OPS CHECKS GOOD IAW B767 AMM 33-51-0 0. PLACARD REMOVED. NOTE: PART REMOVED WAS 'F' CLASS. 2 L 7 2 4F RT A1NM 20081113 WP 2008 11 13 ABXA080250 1 20080929 A 3246 BOLT DOUG DC9 DC941 302207N WP WHEEL LOOSE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 952AX SAPR8827 47615 NR 1 MLG TIRE REQUIRED CHANGE PER PEA 34100014-001. REMOVED AND REPLACED NR 1 MLG TIRE ASSY IAW DC9 AMM 32-40-01-2. WH EEL BOLTS LOOSE. INSPECTED, REPAIRED IAW ABX SPEC WORKSHEET BS421B DATED 12-21-07 AND THE ABX WHEEL AND TIRE MANUAL, RE V 17. 2 L 7 2 4F A6WE 20081113 EA 2008 11 13 ASOA200801480 1 20081106 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 LEFT FS 484 FLOOR SUPPORT ANGLE CRACKED AT LBL 9.0. REMOVED ANGLE IAW SRM 51-42-06. FABRICATED REPAIR ANGLE IAW 51-40- 11 AND 51-42-06 SRM. REPLACED ANGLE ON FLOOR SUPPORT IAW SRM 51-24-36 AND 51-31-59. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801481 1 20081106 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 LEFT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED AT LBL 27.0. REPLACED FLOOR SUPPORT INTERCOSTAL ANGLE IAW REO 601R- 53-41-059 STEPS 8-13. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801471 1 20081106 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 LEFT FS 409.0+128 VERTICAL BEAM CRACKED .1 INCH LONG O/B SIDE LBL 9 AT BOTTOM OF BEAM. ACCOMPLISHED REPAIR TO FS 409+12 8 VERTICAL BEAM O/B SIDE OF LBL 9 IAW BOMBARDIER REO 601R-53-41-237. ASA ECTC REQUIRES COMPLIANCE. COMPLIED WITH ECTC REO 601R-53-41-237 IAW BOMBARDIER REO 601R-53-41-237 REV A. ASA RII COMPLIED WITH: 5300194. SUPPLEMENTAL-SDR CLOSED 11 /17/2008. 2 L 7 2 4F RT A21EA 20081113 NM 2008 11 13 SWAA086156 1 20081111 A 5754 65C26686 SKIN BOEING 737 7373Q8 1384670 NM LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED SPV CHECK, FOUND LT LOWER NR 5 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081113 2008 11 13 SWAA086157 4 20081111 A 2565 D31354 SLIDE BOEING 737 7373T5 1384608 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086133 1 20081111 A 3350 81000 STRIP BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED MV2 CHECK, FOUND EEPLS STRIP MISSING AT MID CABIN. INSTALLED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086150 1 20081111 A 3350 20121 CHARGER BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY EXIT LIGHT BATTERY CHARGER BROKEN. REMOVED AND REPLACED CHARGER PER MM. 2 L 7 2 4F RT A16WE 20081113 EU 2008 11 13 YENA200810110109 1 20081108 A 2700 3945128102 COMPUTER AIRBUS 320 A320232 3930326 EU NR 2 ELAC FAILED A YENA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 15 599JB 28016 548 2336 FLT 1119, BUF-FLL, ACCELERATING ABOVE 10000FT THE AIRCRAFT BANK 4-5 DEGREES LEFT IN LEVEL FLIGHT. NO FUEL IMBALANCED NO TED, BUT THE LEFT AILERON FLOATING UP ABOVE THE DOUBLE TICK MARKS & THE RUDDER INPUT WAS 2.5 DEGREES RIGHT. DIVERTED TO IAD. DECLARED EMERGENCY WITH ATC, NOTICED BELOW 10000FT WITH SPEED 250 KTS AND LOWER THE AILERON BANKING DISAPPEARED. PERFORMED VISUAL INSPECTION OF LT AILERON SERVO CONTROL. NO DEFECTS NOTED IAW AMM 27-14-00. PERFORMED VISUAL INSPECTI ON OF ALL SPOILERS SURFACES. NO DEFECT NOTED WITH IRW AMM 27-64-00. REMOVED AND REPLACED NR 1 ELAC (2CE1) AND NR 2 ELA C (2CE2) IAW AMM 27-93-34, PERFORMED ELAC NR 1 & NR 2 TEST IAW AMM 27-93-34. NO DEFECTS NOTED AT THIS TIME. OK TO CONT 2 L 7 2 4F RT A28NM 20081113 NM 2008 11 13 ASAA0853729 1 20081108 A 2150 32145525 SHUTOFF VALVE BOEING 737 737890 1384527 NM RIGHT PACK MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 02 579AS 4373 35187 RIGHT "BLEED TRIP OFF" LIGHT CAME ON AT 41,000FT. RESET LIGHT AND LIGHT WENT OUT, LIGHT CAME BACK ON SHORTLY AFTER RESE T. ON T/S FOUND PRSOV SLUGGISH AND WOULD NOT RETURN, CLOSED DURING WRENCH CHECK AND APU AIR CHECK. REPLACED PRSOV IAW MM REF 36 11 04 000 801 AND 36 11 04 400 801. OPS CHECK NORMAL DURING WRENCH CHECK AND APU AIR CHECK. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0893710 1 20081026 A 5320 146A750219 SUPPORT BOEING 737 737990 NM BS 727A-727E CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 SEVERAL AREAS OF CORROSION ON LT FLOOR TO SIDEWALL SUPPORT BS 727A TO 727I. 2 L 7 4 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843733 1 20081012 A 5753 6546435340 SKIN BOEING 737 737490 1384715 NM RT WING TE FLAP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 RT OUTBOARD AFT FLAP PREVIOUS REPAIR IS DELAMINATED ON INSIDE UPPER SURFACE. REMOVED DAMAGED AREA, FABRICATED REPAIR PA RTS AND BONDED REPAIR IAW B737 400 SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081113 EA 2008 11 13 ASOA200801222 1 20080926 A 5242 HANDLE CNDAIR CL600 CL6002C10 1390015 EA E/E DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED DAMAGED DOOR HANDLE AND REPLACED WITH NEW HANDLE ON MAIN AVONICS DOOR IAW SRM 51-42-00. REMOVED MAIN AVIONICS B AY DOOR IAW AMM 52-42-00. MAIN AVIONICS BAY DOOR SURFACE RESTORED IAW SRM 51-25-01. REINSTALLED AVIONICS BAY MAIN DOOR IAW AMM 52-42-00. COMPLIED WITH OPS CHECK OF MAIN AVIONICS DOOR AS PER MM 52-42-00. 2 L 7 2 4F RT A21EA 20081113 NE 2008 11 13 ASAA0853708 2 20081107 A 7320 RP23500 PROBE BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE NR 2 ENGINE MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 02 586AS FFFB0742 35189 NR 2 ENG N1 FLUCTUATION RAPIDLY FORM 91.2 TO 100.1 BETWEEN ABOUT 2500FT TO 6000FT ON CLIMBOUT, AUTOTHROTTLE WAS FOLLOWIN G. ALL OTHER ENGINE PARAMETERS APPEAR NORMAL. ABOVE 6KFT ALL NORMAL. NR 2 ENG EEC LOGGED FAULTS 73-30902-T12 SIGNALS D ISAGREE 73-21702 ADIRU TAT DATA AND T12 SIGNAL DISAGREE 73 20812 T12 SIGNAL OUT OF RANGE. NR 1 ENGINE NO FAULTS LOGGED. NR 2 REMOVED T12 SENSOR IN REF 73-21-05-000-801-F00 AND REPLACED T12 SENSOR IN REF 73-21-05-400-801-F00. OPS CHECK NO RMAL IN REF 73-21-00-700-804-F00. ACCOMPLISHED REPAIR CONFIRMATION PERFORMED HIGH POWER ENGINE RUN, OPS CHECK GOOD REF FIM 73-06-00-810-09. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081113 SO 2008 11 13 FDKA2008110300288 1 20081103 A 3297 WIRE HARNESS EMB 145 EMB145LR 3260212 SO MLG DAMAGED A FDKA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SW 07 848MJ 145530 FDL FLT 6231 BUF TO JFK RETURNED TO FIELD DUE TO L/G DISAGREE ON RETRACTION. EMERGENCY DECLARED. FLIGHT LANDED SAFELY. MX FOUND NR 3 MLG TREAD SEPARATED AND FOUND RT FLAP DAMAGED. MX CURRENTLY INSTALLING HARNESS. 2 L 7 2 4T RT T00011AT 20081113 SO 2008 11 13 FDKA2008110400289 1 20081104 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT DIRTY A FDKA K NONE O OTHER IN INSP/MAINT 1 SW 07 838MJ 145384 FRL FLT 6225 JFK. AFT EMERGENCY CEILING EXIT LOCATOR WILL NOT ILLUMINATE. MX CLEANED CONNECTOR, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081113 NM 2008 11 13 ASAA0843718 1 20081029 A 5340 66235744 STRINGER CLIP BOEING 737 7374Q8 138447Q NM BS 706 S10R CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 CABIN FRAME STA 706 STRINGER CLIP CRACKED AT STA 10R. REMOVED DAMAGED CLIP, LOCATED DRILLED NEW CLIP AND INSTALLED IAW B737 400 SRM 51 40 03. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843736 1 20081029 A 5753 6546434370 SKIN BOEING 737 737490 1384715 NM RT WING TE FLAP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 RIGHT INBOARD AFT FLAP UPPER SURFACE DELAMINATED ON OUTBOARD END. REMOVED DAMAGED AREA. BOND REPAIRED WITH REPAIR PART S PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0853687 1 20081102 A 2160 6228145 CONTROLLER BOEING 737 737890 1384527 NM CABIN TEMP MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 570AS 6802 35185 ON RECALL CONT CABIN ZONE TEMP LIGHT ILLUMINATES, LIGHT EXTINGUISHES WITH MC RESET. COULD NOT DUPLICATE. ACCOMPLISHED FIM 21 62 00 810 842. NO FAULTS. FAULT WAS INTERMITTENT. ACCOMPLISHED BITE TEST AND NO FAULT FOUND. NO HISTORY 90 DA YS. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843686 1 20081103 A 3233 65C329564 ACTUATOR BOEING 737 737490 1384715 NM RT MLG BYPASSING A ASAA O OTHER P NO WARNING INDICATION AP APPROACH 1 NM 02 797AS 35495 28892 AFTER GEAR EXTENSION ON FINAL, DID NOT GET A GREEN LIGHT ON THE RIGHT MAIN. WENT TO FLAPS 15 AND HAD GEAR HORN. RAN TH E CHECKLIST AND DID A MANUAL GEAR EXTENSION. THIS WORKED, RECEIVED A GREEN LIGHT AND LANDED. JACKED A/C. CYCLED GEAR, RT MAIN DOES NOT FULLY RETRACT OR EXTEND. SUSPECT TRANSFER CYLINDER OR MAIN ACTUATOR DEFECTIVE. SWAPPED THE LT & RT T RANSFER CYLINDERS, NO HELP. SWAPPED CYLINDERS BACK, LEAK/OPS CHECK OK REF MM 32 32 71. REMOVED & REPLACED THE RT MLG A CTUATOR AND RT MLG BEAM HANGAR. OPS/LEAK CHECKED OK. PERFORMED MAIN LANDING GEAR OPERATIONAL TEST. TEST PASSED GEAR R ETRACTS/EXTENDS NORMALLY AND ALL INDICATIONS ARE NORMAL. DE JACKED A/C. REF MM 32 32 11, MM 32 32 93, MM 32 32 00. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843719 1 20081030 A 5322 651768484 SHEAR TIE BOEING 737 7374Q8 138447Q NM BS 303 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 SHEAR TIE STA 303.1 STR 15L IS GOUGED. REMOVED DAMAGED SHEAR TIE, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE IAW B7 37 400 SRM 51 30 01 AND BOEING DRAWING 65 17684. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843738 1 20081028 A 5753 65C3570339 SKIN BOEING 737 737490 1384715 NM FOREFLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 LEFT INBOARD FOREFLAP HAS CLUSTER OF DENTS ON LOWER SURFACE OUTBOARD OF INBOARD TRACK. REMOVED DAMAGED AREA. REPAIRED WITH DOUBLER FILLER AND BOND REPAIR PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843739 1 20081029 A 5753 6546434370 SKIN BOEING 737 737490 1384715 NM RT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 RIGHT INBOARD AFT FLAP LOWER SURFACE HAS CLUSTER OF DENTS. BOND REPAIRED DAMAGED AREA PER SRM 51 70 06. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843740 1 20081028 A 5753 65C2631025 SKIN BOEING 737 737490 1384715 NM MIDFLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 LEFT INBOARD MIDFLAP UPPER SURFACE CHAFED AT INBOARD END 15 INCHES FORWARD OF TRAILING EDGE. REMOVED DAMAGED AREA. INS TALLED DOUBLER FILLER AND BOND REPAIR PER SRM 57 53 01 AND 51 70 10. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843741 1 20081029 A 5753 65C3570330 SKIN BOEING 737 737490 1384715 NM FOREFLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 RIGHT OUTBOARD FOREFLAP PREVIOUS REPAIR CHAFED ON UPPER SURFACE AT INBOARD END. REMOVED DAMAGED AREA. INSTALLED DOUBLE R FILLER AND BOND REPAIR PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843722 1 20081105 A 5754 65C26603192 SKIN BOEING 737 7374Q8 138447Q NM NR 4 SLAT DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NR 4 SLAT T/E WEDGE UPPER SURFACE IS DENTED. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085899 1 20081029 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 FOUND EMERGENCY EXIT LIGHT ON BULLNOSE MISSING COVER AT ROW 15 DEF. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085900 1 20081029 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 450, RBL 1. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085901 1 20081029 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 396SW 27690 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 377, STR 28R. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081105 EA 2008 11 5 SWIA200820252 1 20080629 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 913SW 7597 FS 280 RIGHT SIDE TOP OUTBOARD CLIP IS CRACKED (C-CHECK). REPLACED CLIP. 2 L 7 2 4F RT A21EA 20081105 SO 2008 11 5 SWIA200820254 1 20081025 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 291SW 120318 EMERGENCY EXIT LIGHT AT ENTRY DOOR INOP (FLT 7788). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4T RT A31SO 20081105 2008 11 5 SWIA200820255 4 20081028 A 3160 D980000158 DISPLAY EMB 120 EMB120ER 3260203 SO COCKPIT MALFUNCTIONED A SWIA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 07 271YV 8371 120271 ELECTRICAL SMOKE SMELL IN COCKPIT CORRESPONDING TO AVIDYNE FLIGHTMAX DISPLAY GOING BLANK. PULLED C/B AND SMELL STOPPED. FLT 7782. REPLACED FLIGHTMAX SCREEN. P/N: D98-0000-1-58-G, S/N ON: 1583, S/N OFF: 1562. 2 L 7 2 4T RT A31SO 20081105 EA 2008 11 5 SWIA200820257 1 20081027 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 957SW 7829 FORWARD FLOOR EMERGENCY LIGHT ROW 7C INOP. FLT 6718. REPLACED FLOOR EMERGENCY STRIP. 2 L 7 2 4F RT A21EA 20081105 EA 2008 11 5 SWIA200820261 1 20081026 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN LOOSE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 748SK 10203 RIGHT SIDE EXIT ROW LOWER EMERGENCY LIGHT INOP. FLT 6204. RESEATED BULB. 2 L 7 2 4F RT A21EA 20081105 EA 2008 11 5 TIMA20080006 2 20081027 A 7200 ENGINE BEECH 99 99 1154002 CE PWA PT6 PT6A27 52043 EA LEFT SEIZED E TIMA O OTHER A Y FLAME/FIRE ENGINE STOPPAGE CR CRUISE 1 NM 07 95WA 36671 518 U6 PCE40783 PILOT FELT A POWER SURGE AND SAW FLAMES OUT THE LEFT ENGINE EXHAUST FOR A MOMENT. LEFT PROPELLER STOPPED TURNING. PILO T SECURED ENGINE, CONTINUED ON AND LANDED WITHOUT INCIDENT. INVESTIGATION REVEALED THAT THE PT BLADES WERE MOSTLY GONE. CT BLADES ARE OK. SUSPECT BEARING FAILURE IN POWER SECTION. 1 L 7 2 3T 4 T A14CE E4EA 20081105 NM 2008 11 5 08FDEA04620 1 20081030 A 5311 707500063C FRAME BOEING 757 75723A 1384967 NM BS 760 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 FWD CARGO PIT STA 760 STR -24L FRAME UPPER J ANGLE DENTED. REPAIRED FRAME STA 760 STR -24L IAW SRM 53-00-07,51-40-02. SUBSEQUENT INSPECTIONS ARE REQUIRED PER SRM 53-00-07, PAGE 208, REPAIR 5, DETAIL III AND PAGE 210, TABLE II. THIS IS A CLASS "B" REPAIR WITH FOLLOW UP INSPECTIONS REQUIRED. HFEC AND DETAILED INSPECTION REQUIRED EVERY 12,000 FLIGHT CYCLES REF 53-00-01, FIG 201, SHEET 10 OF 15,TABLE II. 2 L 7 2 4F RT A2NM 20081105 NM 2008 11 5 SWAA085941 1 20081030 A 5340 69353502 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085948 1 20081030 A 5743 6552235 FITTING BOEING 737 7373H4 1384600 NM LT MLG CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND LT MLG FITTING CRACKED AT D-HOLE. REPAIRED FITTING PER PAE ER. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085949 1 20081030 A 5720 6545402 STRUCTURE BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND LT WING UPPER CHORD CRACKED AT WBL 114, STR 2. REPAIRED CHORD PER PAE ER. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085951 1 20081030 A 5512 65C25727 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 432WN 33715 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABLIZER ELEVATOR SKIN CRACKED AT BS 101, AFT OF LEADING EDGE. REPAIRE D SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085952 1 20081030 A 5512 65C25727 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 432WN 33715 DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABLIZER ELEVATOR SKIN CRACKED AT BS 129, AFT OF LEADING EDGE. REPAIRE D SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085953 1 20081030 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 442WN 32459 DURING SCHEDULED HC2 CHECK, FOUND EEPLS INOP AT OVERWING EXIT. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085954 1 20081030 A 3350 81000 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 456WN 32463 FOUND EEPLS COVER LOOSE AT FWD ENTRY. REMOVED AND REPLACED EEPLS PER MM. 2 L 7 2 4F RT A16WE 20081105 WP 2008 11 5 08FDEA04674 1 20081103 A 5320 ABA72033 WEB DOUG DC10 DC1030F 3023504 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 FLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL, FOUND CRACK ON HORIZONTAL WEB FLOOR. 2 L 7 3 4F RT A22WE 20081105 WP 2008 11 5 08FDEA04675 1 20081103 A 5320 ABA72033 WEB DOUG DC10 DC1030F 3023504 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 FLIGHT COMPARTMENT (COCKPIT) AFTER REMOVAL FLOOR PANEL, FOUND CRACK ON HORIZONTAL WEB FLOOR. 2 L 7 3 4F RT A22WE 20081105 EU 2008 11 5 08FDEA04677 1 20081103 A 2560 379103C15 STRAP AIRBUS 310 A310324 3930206 EU ESCAPE ROPE BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 F/O'S FWD EMERGENCY ESCAPE ROPE TAMPER RESISTANT STRAPS, UPPER AND LOWER ARE BROKEN. REMOVED & REPLACED F/O'S FWD EMERG ENCY DESCENT DEVICE PER AMM 25-61-13-4. 2 L 7 2 4F RT A35EU 20081105 EU 2008 11 5 08FDEA04680 1 20081103 A 5321 A2557158800000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 BULK CARGO FLOOR PANEL IS DELAMINATED. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED NEW PANEL. FABRICATED TOP SHEET I AW DWG SRZ 25-011. PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-35-4. 2 L 7 2 4F RT A35EU 20081105 EU 2008 11 5 08FDEA04681 1 20081103 A 5321 A2557157300200 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 BULK CARGO FLOOR PANEL IS DELAMINATED. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED NEW PANEL. FABRICATED TOP SHEET I AW DWG SRZ 25-011. PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-35-4. 2 L 7 2 4F RT A35EU 20081105 EU 2008 11 5 08FDEA04686 1 20081103 A 5321 A2557996700000 FLOOR PANEL AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 BULK PIT FLOOR PANEL IS DELAMINATED. REMOVED PANEL IAW AMM 53-10-35-4. FABRICATED NEW PANEL IAW FEDEX DWG SRZ 25-005. FABRICATED TOP SHEET IAW DWG SRZ 25-011. PART MARKED IAW GMM 7-0-1000. INSTALLED PANEL IAW AMM 53-10-35-4. 2 L 7 2 4F RT A35EU 20081105 NM 2008 11 5 SWAA085959 1 20081030 A 5330 6545767 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 435, STR 1. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085960 1 20081029 A 3350 8210248801 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 706SW 27840 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085924 1 20081030 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085911 1 20081029 A 5340 65C27314 STRINGER CLIP BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 255WN 32513 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 20R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085912 1 20081029 A 5311 6545874 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 294, R1 DOOR MIDDLE CUTOUT. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 2008UALA03170 1 20080603 A 5753 SPAR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU RT MIDFLAP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 FOUND RT MID FLAP L/E SPAR DAMAGED. FOUND RT MID FLAP L/E SPAR DAMAGED. CONNECTING LINKAGE FOR EXHAUST GATE CAME LOOSE AND DAMAGED CUTOUT SECTION THAT ROD GOES THROUGH. REMOVED FLAP. INSTALLED NEW MID FLAP. FLAP ASSY INSTALLED. TEST F LT OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 20081105 NE 2008 11 5 2008UALA05754 2 20080917 A 7220 INLET BULLET BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 CRACK AND DELAMINATION FOUND ON INLET CONE (SPINNER) ON RT ENGINE. SPINNER FOUND CRACKED/DELAMINATED. ASSY SENT TO SHO P. REPLACED INLET CONE. NO FAN BLADE DAMAGE FOUND. AFTER VERIFICATION FLIGHT, A/C DETERMINED OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081105 NE 2008 11 5 2008UALA05860 2 20080924 A 7321 7911004111 EEC BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE NR 1 ENGINE FAULTY A UALA D RETURN TO BLOCK J WARNING INDICATION IN INSP/MAINT 1 WP 29 666UA 29238 L ENG CONT EICAS AND L ENG CONT STATUS. REPLACED NR 1 ELECTRICAL ENGINE CONTROL. ACCOMPLISHED OPS CHECK. CHECKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081104 WP 2008 11 4 UPS08853733 1 20081008 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV REPAIR AT STA BS 35 TO 42 L28L L29L DOES NOT MATCH REPAIR IN SRM 53-2-00 FIG 13. REPAIRED TO SRM 53- 02-00 FIG 13. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853734 1 20081008 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV REPAIR AT BS 50-55 L29L L30L DOES NOT MATCH SRM REPAIR 53-02-00 FIG 13. REPAIR PER 53-02-00 FIG 13. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853735 1 20081002 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATE EFN 70219911038 SEAT TRACK FS 160. REPAIRED SRM 53-02-03 FIG 008A. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853736 1 20080925 A 5230 REPAIR DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV PERMANENT REPAIR TO PIT 32 DOOR INNER PAN CRACKED. REPAIRED 52-02-00. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853744 1 20081002 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATION REPAIR EFN 70220001109 ORIGINAL NRC 042313 CORROSION ON FLOOR BLANK FS 160 TO 180. INSPEC TED PREVIOUSLY REPAIR AND REMOVED CORROSION 53-2-03 FIG 9. 2 L 7 4 4F RT 4A25 20081104 WP 2008 11 4 UPS08853745 1 20081002 A 5320 CUSP WEB DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATE EFN 70219971129 ORIGINAL 750504 CUSP MEMBRANE AT FS 1580 LATERAL LOCATION ID AS CARGO TRACK C. REPAIRED PREVIOUSLY SRM 53-02-00. 2 L 7 4 4F RT 4A25 20081104 EU 2008 11 4 MTNA100804 1 20081030 A 5720 RETAINER AEROSP ATR42 ATR42320 8680930 EU WING CORRODED A MTNA K NONE O OTHER IN INSP/MAINT 1 EA 68 907FX 286 DURING A GENERAL VISUAL INSPECTION, NOTICED THERE IS EXFOLIATION CORROSION OF THE WING PRESSURE DECK SEAL RETAINER LOCAT ED AT REAR SPAR (FUSELAGE FRAME 27) BETWEEN RIBS 1LT - 1RT. 2 H 7 2 4T RT A53EU 20081104 2008 11 4 YYFA200800003 4 20080922 A 2340 6224096002 PA SYSTEM DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE COCKPIT INOPERATIVE A YYFA F ACTIVATE FIRE EXT. O OTHER UK UNKNOWN 1 SO 29 905TA 8760 49905 AIRCRAFT RETURNED TO THE GATE DUE TO P/A SYSTEM INOPERATIVE. 2 L 7 2 4F 4 F A6WE E9NE 20081105 WP 2008 11 5 AALA200802556 1 20080924 A 5531 SPAR DOUG DC9 DC983 3022083 WP VERTICAL STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 RT VERTICAL STABILIZER FORWARD SPAR TANG CRACKED ON AFT SIDE OF CANTED FRAME AT STATION 1388. INSTALLED REPAIR ANGLE IN ACCORDANCE WITH AARD 55-30-00-08. 2 L 7 2 4F RT A6WE 20081105 WP 2008 11 5 AALA200802637 1 20081002 A 5510 3912078501 HINGE FITTING DOUG DC9 DC983 3022083 WP HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON HORIZONTAL STABILIZER LEFT INBOARD OUTBOARD HINGE PLATE LUG NUMBER 3. AREA OF DISCREPANCY 2 INCHES B Y 2 INCHES. REPLACED LEFT INBOARD OUTBOARD LUG IN ACCORDANCE WITH WORKCARD 55 94 05. 2 L 7 2 4F RT A6WE 20081105 WP 2008 11 5 AALA200802641 1 20081002 A 5510 3912034502 HINGE FITTING DOUG DC9 DC983 3022083 WP HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON HORIZONTAL STABILIZER RIGHT OUTBOARD INBOARD HINGE PLATE LUG NUMBER 3. AREA OF DISCREPANCY 2 INCHES BY 2 INCHES. REPLACED RIGHT OUTBOARD INBOARD LUG IN ACCORDANCE WITH WORKCARD 55 94 05. 2 L 7 2 4F RT A6WE 20081105 WP 2008 11 5 UPS08853791 1 20081011 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN 71520081041 ORIG NR 198845 MAIN CABIN STA 240 LBL 45 SEAT TRACK PLUG. NO SEAT TRACK PLUG AT STA 240 LBL 45. SEAT TRACK SPLICE IAW DCI SRM 53-02-03-0 FIG 006A REV 78. 2 L 7 4 4F RT 4A25 20081105 NM 2008 11 5 SWAA085916 1 20081029 A 5311 6546541 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 2R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085917 1 20081029 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 947 TO BS 996. REMOVED AND REPLACED WEB PER SR M. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085918 1 20081029 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 21L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085919 1 20081029 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 336, STR 21L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085893 1 20081028 A 3350 65C27095 BATTERY BOEING 737 737301 1384611 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR LOWER INTERIOR EMERGENCY EXIT LIGHT INOP. SECURED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085930 1 20081030 A 5313 65617777 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 1L. REMOVED AND REPLACED SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085935 1 20081030 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER PAE EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085936 1 20081030 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER PAE EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085937 1 20081030 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER PAE EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085938 1 20081030 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER PAE EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085942 1 20081030 A 5340 69353502 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 16R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 08FDEA04639 1 20081030 A 5311 FRAME BOEING 757 75723A 1384967 NM BS 1320 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 AFT CARGO COMPT, BS 1320, S-26L, IS CORRODED. REPAIRED FRAME, BS 1320, S-26R, IAW SRM 53-00-07, REPAIR NR 5. INSTALLED REPAIR IAW SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CATEGORY "B" MAJOR REPAIR WITH THE FOLLOWING FOLLOW UP TRACKIN G REQUIREMENTS: INITIAL AT 37,500 FC FROM REPAIR INSTALLATION; THEREAFTER EVERY 12,000 FC. 2 L 7 2 4F RT A2NM 20081105 NM 2008 11 5 08FDEA04672 1 20081103 A 5720 652171317 WEB BOEING 727 7272D4 138407U NM ZONE 500 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 LEFT WING OTBD LE, CRACK IN CLOSE OUT WEB AT TIP INBD EDGE, AT OTBD END OF NR 1 SLAT WEDGE WHEN EXTENDED REMOVED CLOSEOU T WEB. INSTALLED NEW WEB, IAW SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081105 NM 2008 11 5 SWAA085961 1 20081030 A 5322 69353656 SHEAR TIE BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 750SA 29802 DURING SCHEDULED MV1 CHECK, FOUND SHEAR TIE CRACKED AT BS 380, STR 17L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081105 2008 11 5 SWAA085962 4 20081030 A 2565 63550107 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 766SW 29806 FOUND R1 DOOR SLIDE LOW PRESSURE. REMOVED AND REPLACED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 2008UALA06254 1 20081023 A 5270 TARGET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR CONTAMINATED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 547UA 25368 LEFT WING SLIDE INDICATION. FLIGHT DIVERTED. MECHANICS STATED THAT THERE WERE PAINT OVER-SPRAY ON THE TARGET AND SWITC H. AFTER REMOVAL OF THE OVER-SPRAY, A SLIGHT ADJUSTMENT TO THE DOOR SWITCH TO ENSURE WITHIN LIMITS, AND OPS CHECKING TH E DOOR SEVERAL TIME TO ENSURE THE MESSAGE WENT AWAY THIS ITEM HAS BEEN SIGNED OFF. 2 L 7 2 4F 4 F RT A2NM E17NE 20081105 NM 2008 11 5 2008UALA06299 1 20081028 A 2400 ELECTRICAL SYS BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 218UA 30222 FLIGHT REPORTED ELECTRICAL PROBLEM. FLIGHT DIVERTED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081105 NM 2008 11 5 2008UALA06301 1 20081028 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 653UA 25391 FWD EEL CROSS-AISLE LIGHT IS INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20081105 NM 2008 11 5 2008UALA06306 1 20081028 A 5230 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FWD CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 FWD CARGO PIT DOOR HAS DAMAGE TO LOWER AFT CORNER. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED FRAME CORNER & INSTALLED NEW FRAME CORNER (P-N 143N6618). 2 L 7 2 4F 4 F RT A2NM E17NE 20081106 NM 2008 11 6 DHLA2008745597 1 20080903 A 5330 SKIN BOEING 727 727224 1384076 NM ZONE 100 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE SKIN WITH RIVETS WITHOUT EDGE MARGIN FROM BS 720E+2 TO BS 720E+7.5 BETWEEN S-21L AND S-22L. REPAIRED FUS ELAGE EXTERNAL SKIN SECTION FROM BS 720D+17.5 TO BS 720E+17.5 BETWEEN S-20L AND S-23L IAW B727 SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 DHLA2008745599 1 20080917 A 5322 SHEAR TIE BOEING 727 727224 1384076 NM ZONE 100 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT BS 720C BETWEEN S-28L AND S-28R SHEAR TIE WITH DOUBLE HOLES. REPAIRED FUSELAGE SHE AR TIE SECTION AT BS 720C BETWEEN S-28L AND S-28R IAW B727 SRM 53-10-4 FIG 11 DETAIL 1. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 DHLA2008745600 1 20081008 A 5322 SHEAR TIE BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 660 BETWEEN S-28R AND S-28L SHEAR TIE WITH CORROSION. REPAIRED FUSELAGE SHEA R TIE AT SKIN ATTACHMENT BS 660 BETWEEN S28L AND S28R IAW SRM 53-10-4 FIG 15. 2 L 7 3 4F A3WE 20081106 WP 2008 11 6 AALA200802656 1 20081002 A 2170 5953625521 DUCT DOUG DC9 DC982 3022082 WP WATER SEPARATOR LEAKING A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 236AA 49251 DFW - CREW REPORTED TAIL COMPARTMENT OVERHEAT INDICATION DURING CLIMBOUT. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED WATER SEPARATOR DUCT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081106 WP 2008 11 6 AALA200802659 1 20081002 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 262AA 49290 LGA - EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 18B, 20B, 20D, AND 21B INOPERATIVE. SECURED LOOSE BATTERIES IN EMERGENCY B ATTERY PACK AT SEAT ROW 19. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081106 WP 2008 11 6 AALA200802661 1 20081001 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 581AA 53158 TUL - SKIN CRACKED AT CANTED FRAME IN AFT FUSELAGE AT STATION 1474. LENGTH OF CRACK IS 2 INCHES. INSTALLED DOUBLER IN ACCORDANCE WITH SRM 53 01 00. 2 L 7 2 4F A6WE 20081106 NM 2008 11 6 DHLA2008745602 1 20081015 A 5320 STRAP BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE AFT CARGO COMPARTMENT FROM BS 1130 AT LBL45 STABILIZER STRAP WITH CORROSION. REPLACED STABILIZER STRAP S ECTION FROM BS 1070 TO 1130 AT RBL 45 IAW SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 DHLA2008745603 1 20080903 A 5310 WINDOW FRAME BOEING 727 727224 1384076 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE EXTERIOR FUSELAGE CARGO CABIN WINDOW CUT-OUT NR 36 RIGHT SIDE WINDOW FRAME WITH CORROSION. REPLACED FUSE LAGE WINDOW FRAME FROM BS 970 TO BS 990 BETWEEN S-10R AND S-14R IAW B727SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 DHLA2008745587 1 20080903 A 5310 DOOR FRAME BOEING 727 727224 1384076 NM ZONE 800 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN FWD GALLEY DOOR AFT SECTION BEAM AREA STOP FITTING CUT OUT WITH CRACK. REPAIRED FUSELAGE FWD GALLEY DOOR LOWER AFT FRAME SECTION BETWEEN DOOR BEAM NR 4 AND DOOR BEAM NR 6 IAW SB 727-52-114 DTD 2/24/78 SECT 3 PART 3 PARA D. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 DHLA2008745588 1 20080901 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 200 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT STA 490 BETWEEN S14L AND S16L FRAME WITH WEAR. REPLACED FRAME SECTION AT BS 490 BETWEEN S- 14L AND LOWER BEAM IAW DWG AE 4899 REV J DTD 12/15/99. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 08FDEA04664 1 20081101 A 5320 6517592 STRAP BOEING 727 7272S2F 1384O81 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 MAIN DECK FLOORBEAM STABILIZER STRAP IS CRACKED BS 344 LBL 23 WL 200 STOP DRILLED CRACK. INSTALLED REPAIR DOUBLER REF S RM 53-10-08 PG 36, FIG 6. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081106 WP 2008 11 6 AALA200802668 1 20081003 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 33414 49325 LGA - EMERGENCY FLASHLIGHT AT AFT RIGHT LAVATORY HAS STRAP BROKEN. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT RIGHT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081106 NM 2008 11 6 08FDEA04665 1 20081101 A 5320 6517592 STRAP BOEING 727 7272S2F 1384O81 NM FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 UPPER MAIN DECK FLOORBEAM STABILIZER STRAP CRACKED AT STA 324 LBL 23 WL 200. STOP DRILLED CRACK, INSTALLED REPAIR DOUBL ER REF SRM 53-10-08 PG 36 FIG 6. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 AALA200802669 1 20081003 A 3350 BPS73 BATTERY PACK BOEING 767 767223 1385123 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AA 22327 JFK - EMERGENCY EXIT SIGN AT MID GALLEY LEFT SIDE INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN AT LEFT MI D GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081106 NM 2008 11 6 AALA200802670 1 20081003 A 3397 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 343AN 33082 SFO - EMERGENCY EXIT LIGHTS AT SEAT ROW 33 TO 41HJ INOPERATIVE. REPLACED CONNECTOR AT SEAT 33HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081106 NM 2008 11 6 08FDEA04646 1 20081030 A 2780 106081918 LINKAGE BOEING 727 727227 1384078 NM LE FLAP LOOSE A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CE 21 490FE 21493 NUMBER 4 LE FLAP ON RIGHT SIDE DID NOT RETRACT AFTER TAKEOFF DURING FLAP/SLAT RETRACTION. RAN QRH. EXTENDED NORMALLY AND DID NOT RETRACT SECOND TIME. FOUND LOOSE LINKAGE ON NR 4 LE FLAP SWITCH. SECURED LINKAGE, OPERATED FLAPS AND OPS C HECKED GOOD IAW MM 27-82-000-1. ACFT OK FOR FLIGHT. SWITCH REF. IPC ITEM 085, PART NUMBER 10-60819-18, IPC REF 27-80 -00-14. LOOSE LINKAGE TO SWITCH FOUND, SECURED IAW AMM 27-82-000-1, OPS CHECK GOOD. 2 L 7 3 4F A3WE 20081106 2008 11 6 AALA200802662 4 20081002 A 2565 100503109 HANDLE DOUG DC9 DC982 3022082 WP EVAC SLIDE FRAYED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 574AA 53151 TUL - TAIL CONE SLIDE LIFT HANDLE IS FRAYED AND NOT READABLE AT AFT ACCESSORY STATION 1500. REPLACED SLIDE. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081106 SO 2008 11 6 C2XA08IA217 1 20080929 A 3350 66367 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16951 145063 DURING SCHEDULED MAINT, THE NR 3 EMERGENCY AISLE LIGHT WAS FOUND TO BE INOPERATIVE. MAINT REMOVED AND REPLACED THE NR 3 EMERGENCY LIGHT STRIP, OPERATIONALLY TESTED THE SYSTEM AND CLEARED THE DISCREPANCY. (K) 2 L 7 2 4T RT T00011AT 20081106 NM 2008 11 6 KCSA081550 1 20081103 A 5320 FITTING BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 STA 2360 BATHTUB FITTING AT STR 46R CORRODED. 2 L 7 4 4F RT A20WE 20081106 NM 2008 11 6 KCSA081551 1 20081103 A 5320 FITTING BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 STA 2360 BATHTUB FITTING AT STR 49R CORRODED. 2 L 7 4 4F RT A20WE 20081106 NM 2008 11 6 KCSA081555 1 20081103 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 706CK 21937 EMERGENCY LIGHT AT STA 460 ABOVE STAIRS IN UPPER DECK INOP. 2 L 7 4 4F RT A20WE 20081106 NM 2008 11 6 QXEA200801006 1 20080912 A 5410 FRAME BOMBDR DHC8 DHC8402 1390042 NM LT NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 413QX 4060 C4-CHECK - LT NACELLE TAIL PANEL, 414AR THE THIRD FRAME AFT FROM THE FWD EDGE IS CHAFED SEVERELY AT THE UPPER END. BLEND ED OUT MINOR CHAFE IAW D8 Q400 SRM 51-14-00, PG 201, PARA 1-5B, STEP 2. MEASURED, BLEND MATERIAL REMOVED. ALODINED AND P RIMED IAW D8 Q400 SRM 51-21-10 AND 51-25-10. (K) 2 H 7 2 4T RT A13NM 20081106 EA 2008 11 6 QXEA200801062 1 20081003 A 2120 A/C PACK CNDAIR CL600 CL6002C10 1390015 EA RIGHT OVERTEMP A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 19 618QX 10205 SMOKE FROM AIR CONDITIONING AND PACK DISCHARGE TEMP RISING WHEN RT PACK ON. MAINT PLACED ON MEL 21-51-1B. RETURNED TO SE RVICE. (K) 2 L 7 2 4F RT A21EA 20081106 NM 2008 11 6 QXEA200801051 1 20081001 A 5280 PIVOT ASSY BOMBDR DHC8 DHC8402 1390042 NM MLG DOOR LOOSE A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 19 406QX 4048 AFTER T/O AT GEAR UP, THE RT MAIN GEAR CAUTION LIGHT REMAINED ILLUMINATED THEN WENT OUT. POST FLIGHT INDICATED RT MAIN G EAR DOORS LOOSE. FERRY FOR REPAIRS. REPLACED RT GEAR PIVOT ARM ASSY AND LINK FRE MM 32-31-31-440-801, CHECK GOOD. RETURN ED TO SERVICE. (K) 2 H 7 2 4T RT A13NM 20081106 NM 2008 11 6 USA2008F00042 1 20081005 A 2560 P4010021 BATTERY BOEING 737 7373S3 138449H NM FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 F/A REPORTED THE EMERGENCY FLASHLIGHT CHARGING INDICATOR INOPERATIVE. MAINT REMOVED AND REPLACED THE BATTERY. OPS CHECK NORMAL. (K) 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 QXEA2008110501137 1 20081018 A 5420 DIAPHRAGM BOMBDR DHC8 DHC8402 1390042 NM LT NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 418QX 4143 PDX - C1 - LT NACELLE INTERCOSTAL DIAPHRAGM IS CRACKED. REMOVED DIAPHRAGM P/N 85414131 AND P/N 85414117. LOCATED AND D RILLED HOLES IN DIAPHRAGMS. INSTALLED DIAPHRAGMS REF Q400 SRM 51-40-15. 2 H 7 2 4T RT A13NM 20081106 NM 2008 11 6 QXEA2008110401156 1 20081030 A 5210 85217741011 CAM BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 420QX 4147 SEA - THE AFT PASSENGER DOOR INTERLOCK CAM (REF D8-400 IPC 52-12-11-1-90) IS WORN AND INTERMITTENTLY NOT ENGAGING THE DO OR FRAME STRIKER PLATE TO ALLOW DOOR HANDLE ROTATION FOR CLOSING. FERRIED TO PDX. REMOVED DAMAGED INTERLOCK CAM IAW 52 -12-11-000-801 PARA 4.E. REPLACED CAM IAW 52-12-11-400-801 PARA 4.J. REMOVED AND REPLACED DAMAGED AFT LATCH ROLLER TRA CK, POSITIONED TRACK IAW 52-00-00-820-801 PARA 4.C.(4). OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 20081106 NM 2008 11 6 QXEA2008110501130 1 20081018 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 418QX 4143 PDX - C1 - FWD FUSELAGE EXTERIOR ROOF SKIN HAS A LIGHTNING STRIKE ON RIVET HEAD AT APPROX X-55.000 AND STR LT 5. DRILLE D OUT RIVET, ENLARGED COUNTERSINK TO REMOVE DAMAGE FROM SKIN REF RD 8/4-53-1039. HFEC INSPECTED IAW Q400 NDTM PART 6, 5 1-00-01, NO CRACKS NOTED. INSTALLED SOLID RIVET IAW SRM 51-42-05. PRIMED AND PAINTED REF Q400 SRM 51-25-05. 2 H 7 2 4T RT A13NM 20081106 NM 2008 11 6 SWAA085983 1 20081031 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN UNSECURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 283WN 36610 FOUND RT EEPLS LIGHT UNSECURED. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 SWAA085984 1 20081031 A 3350 300432 LIGHT BOEING 737 7377H4 1384404 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 288WN 36611 DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 SWAA085985 1 20081102 A 5753 6573731 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20081106 SO 2008 11 6 C2XA08RI147 1 20080919 A 2131 912R0301 CONTROLLER EMB 145 EMB145LR 3260212 SO CABIN PRESSURE INOPERATIVE A C2XA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 27 13988 145265 FLIGHT CREW REPORTED AUTO PRESSURIZATION FAILED DURING TAXI OUT. MX REMOVED AND REPLACED PRESSURIZATION MANUAL CONTROLLE R AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081106 NM 2008 11 6 QXEA200801007 1 20080912 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 413QX 4060 C4 CHECK, CHAFE DAMAGE ON SKIN LOCATED 6 INCHES FROM SIDE OF TOILET SERVICE ACCESS DOOR BLENDED CHAFE REF SRM 51-14-00 M ETHOD 4 PG 203. HFEC INSP IAW NDTM PART 6,, 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECKED IAW NDTM PART 1 51-00-04 HI. 054 INCH LOW .053 INCH. CHAFE FOUND WITHIN LIMITS IAW SRM 53-00-00 PG 203 TABLE 201. ALODINED AREA REF SRM 51-21-10 PG 2 03 PARA D. PRIMED, PAINTED, REF SRM 51-25-10 AND 51-25-15. (K) 2 H 7 2 4T RT A13NM 20081106 NM 2008 11 6 QXEA200801008 1 20080912 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 413QX 4060 C4-CHECK-CHAFE DAMAGED ON EXTERNAL DOUBLER AT AFT SIDE OF TOILET SERVICE ACCESS DOOR 7 INCHES DOWN FROM TOP AFT CORNER O F DOUBLER. BLENDED CHAFE REF Q400, SRM 51-14-00 METHOD 4, PG 203. HFEC INSP IAW D8 Q400 NDTM PART 6,51-00-01 NO CRACKS N OTED. UT THICKNESS CHECK IAW D8 Q400 NDTM PART 1,51-00-04, HI .063 INCH LOW .061 INCH. CHAFE WITHIN LIMITS REF Q400 SRM 51-14-00, PG 204, PARA C. ALODINED, PRIMED, PAINTED REF Q400 SRM 51-21-10, 51-25-10 AND 51-25-15. (K) 2 H 7 2 4T RT A13NM 20081113 SO 2008 11 13 FDKA2008110700290 1 20081107 A 2560 FLASHLIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 858MJ 145767 FRL FLT 6207 JFK-CLT. CAPTAIN'S EMERGENCY FLASHLIGHT WAS INOP. MX REPLACED THE FLASHLIGHT. 2 L 7 2 4T RT T00011AT 20081113 SO 2008 11 13 FDKA2008110800291 1 20081108 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 FRL FLT 6268 CVG. EMERGENCY OVERHEAD LIGHT OUT AT ROW 12. MX PERFORMED OPS CHECKS, OPS GOOD. 2 L 7 2 4T RT T00011AT 20081112 NM 2008 11 12 USAABB08157 1 20080930 A 3350 BCREF5985 LIGHT BOEING 757 7572S7 1384962 NM CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 906AU 23598 L4 DOOR EXIT LIGHT FOUND INOPERATIVE. MX REPLACED THE ASSY. OPS CHECKED OK. 2 L 7 2 4F RT A2NM 20081112 NM 2008 11 12 USAABB08158 1 20080930 A 2150 A/C PACK BOEING 757 757225 1384959 NM LEFT MALFUNCTIONED A USAA B G EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 EA 19 917UW 22193 FLT 1100 - FL 350, WITH LT PACK ON MEL, FLT RECEIVED AN EICAS WARNING "CAB ALT". RT PACK INDICATED NORMAL. BEGAN DESCE NT DONNED O2 MASKS AND DECLARED AN EMERGENCY. CABIN O2 MASKS NOT DEPLOYED. DESCENDED TO 10,000 FT. TURNED ON LT PACK AN D RECEIVED NORMAL CABIN PRESSURE. FLT CONTINUED AT 15,000 FT AND LANDED WITHOUT FURTHER INCIDENT. MX PERFORMED A SINGLE PACK CONFIDENCE CHECK. OPS CHECKED GOOD. 2 L 7 2 4F RT A2NM 20081112 NM 2008 11 12 DHLA2008745654 1 20080905 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE FROM BS 703 TO BS 710.5 BETWEEN S-1L AND S-2L EXTERNAL SKIN DAMAGED. REPAIRED FUSELAGE SKIN SECTION FROM BS 701 TO BS 716 BETWEEN S-2L AND S-3L IAW COOPESA EO COO-2-53-287-08. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745656 1 20080906 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT BS 600 BETWEEN S-26R AND S-27R SHEAR TIE AND FRAME WITH CORROSION. REPLACED SHEAR TIE SECTION AT BS 600 BETWEEN S-26R AND S-27R IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745646 1 20081002 A 5754 RIB BOEING 727 727224 1384076 NM LE SLAT WORN A DHLA O OTHER O OTHER UK UNKNOWN 1 GL 05 745DH 20665 RT WING NR 7 SLAT STA 246, 262, 268.5, 292.5, 299, 306 AND 313 INTERNAL RIBS WITH MISSING MATERIAL. REPLACED INTERNAL R IBS AT RT WING NR 7 SLAT IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DXTA2008110403336 1 20081103 A 2720 RUDDER GULSTM 200 200 4500308 NM VIBRATES E DXTA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 07 730QS 120 RUDDER SHAKES INFLIGHT INTERMITTENTLY FROM FL410 DOWN UNTIL AC SLOWED TO 250KTS. 2 L 7 2 4F RT A53NM 20081113 NM 2008 11 13 DHLA2008745625 1 20080923 A 5313 STRINGER BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE AT BS 320 S-12R WITH CRACK. REPAIRED S-12R FROM BS 312 TO BS 329 IAW B727 SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745633 1 20080902 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT BS 580 BETWEEN S-16R AND 17R FRAME WITH DENT. REPAIRED FRAME SECTION AT BS 580 BETWEEN S-1 6R AND S-17R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 HNAA20080300318 1 20081031 A 2751 44281508010 INDICATOR DHAV DHC8 DHC8102 2809003 NM FLAP POSITION DEFECTIVE A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 330EN 41024 8863 274 TAKEOFF WAS ABORTED WHEN THE TAKEOFF WARNING HORN SOUNDED. MAINTENANCE CYCLED THE CONDITION LEVER AND SYSTEM OPERATED N ORMALLY. THE FLAP POSITION INDICATOR WAS CHANGED OUT AND SYSTEM CHECK WAS PERFORMED. NO DEFECTS WERE NOTED AT THAT TIM E AND AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 20081113 NM 2008 11 13 USAASB08107 1 20081108 A 2150 ACM BOEING 737 7374B7 138449C NM RIGHT PACK BAY OVERSERVICED A USAA A UNSCHED LANDING W B J INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 19 430US 24552 DURING CLIMBOUT FROM PHL, EN ROUTE TO MCO, CREW REPORTED A SOUR ODOR HAD FILLED THE CABIN ATMOSPHERE CAUSING THE FORWARD LAVATORY SMOKE DETECTOR TO SOUND. SMELL DISSIPATED EN ROUTE BUT RETURNED ON FINAL APPROACH TO MCO. FLIGHT LANDED WITH OUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT AIR CYCLE MACHINE OVERSERVICED. DRAINED OIL TO PROPER LEVEL. RAN EN GINES AND AIR CONDITIONING SYSTEMS. NO ODOR AT THIS TIME. AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20081113 EA 2008 11 13 ASOA200801444 1 20081103 A 5260 STEP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 926EV 7843 PAX DOOR BOTTOM STEP BROKEN. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801445 1 20081103 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 933EV 8022 FS 484.0 LBL 36 INTERCOSTAL FLANGE CRACKED IN RADIUS. NOT PREVIOUSLY REPAIRED. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801446 1 20081103 A 3350 LENS CNDAIR CL600 CL6002C10 1390015 EA CABIN MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 759EV 10211 OVERWING EMERGENCY EXIT SIGN; RED EMERGENCY LIGHT LENS MISSING. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801447 1 20081103 A 5320 GUSSET CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 841AS 7300 CRACK FOUND IN GUSSETT AT FS 461.5 OF LT INBOARD SEAT TRACK SUPPORT BEAM. 2 L 7 2 4F RT A21EA 20081105 WP 2008 11 5 AALA200802561 1 20080923 A 5313 S22779223 LONGERON DOUG DC9 DC983 3022083 WP BS 160 L2L CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 LONGERON 2 LT WAS CRACKED AT INBD SIDE AT STATION 160. CRACK LENGTH IS 1/4 INCH. INSTALLED SPLICE REPAIR IN ACCORDANCE WITH SRM 53-02-00 FIGURE 18. 2 L 7 2 4F RT A6WE 20081105 SO 2008 11 5 SIMA200830501 1 20080929 A 3260 PROXIMITY SWITCH EMB 135 EMB135KL 3260302 SO RT MLG FAULTY A SIMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 21 853AE 145742 ON FLIGHT 3116 CREW REPORTED AFTER RETRACTING LANDING GEAR CAPTAIN AND FLIGHT ATTENDANT FELT AND HEARD LOUD THUMPING NOI SE 4 TIMES. CREW ALSO NOTED LEFT RUDDER PEDAL VIBRATED. CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO FIELD. AI RCRAFT REMOVED FROM SERVICE. PERFORMED TROUBLESHOOTING IN REF TO AMM 32-61-01 AND CMC DOWNLOAD IAW AMM 45-45-00 AND DET ERMINED RIGHT MAIN LANDING GEAR UP LOCK PROX SWITCH TO BE FAULTY. REMOVED AND REPLACED PROX SWITCH AND PERFORMED VIBRAT ION WORK CARD IAW W/C 12-200-01, NO DISCREPANCIES WERE FOUND. AIRCRAFT AWAITING FCF. 2 L 7 2 4F RT T00011AT 20081105 WP 2008 11 5 AALA200802649 1 20081001 A 3350 0201720003 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 460AA 49565 LGA - EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F A6WE 20081105 WP 2008 11 5 AALA200802636 1 20081002 A 5510 3912034501 HINGE FITTING DOUG DC9 DC983 3022083 WP HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON HORIZONTAL STABILIZER LEFT OUTBOARD INBOARD HINGE PLATE LUG NUMBER 2. AREA OF DISCREPANCY 2 INCHES B Y 2 INCHES. REPLACED LEFT OUTBOARD INBOARD LUG IN ACCORDANCE WITH WORKCARD 55 94 05. 2 L 7 2 4F RT A6WE 20081105 NM 2008 11 5 SWAA085906 1 20081029 A 5610 571761 WINDOW BOEING 737 7373A4 1384585 NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 677AA 23289 DURING CRUISE AT FL 330 R1 COCKPIT WINDOW ARCHED AND CRACKED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 20081105 CE 2008 11 5 TIMA20080007 1 20081028 A 3230 H111541 LIMIT SWITCH BEECH 1900 1900C 1154161 CE LANDING GEAR BROKEN E TIMA K NONE P NO WARNING INDICATION AP APPROACH 1 NM 07 197GA UB16 THE LANDING GEAR DID NOT EXTEND WHEN SELECTED. THE PILOT MANUALLY PUMPED THE GEAR DOWN AND LANDED. INVESTIGATION REVEA LED THAT THE LT UP-LIMIT ELECTRICAL SWITCH HAD PHYSICALLY BROKEN, OPENING THE CIRCUIT TO THE LANDING GEAR CONTROL. 2 L 7 2 4T RT A24CE 20081105 NM 2008 11 5 SWAA085943 1 20081030 A 5753 6573731 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND RT WING I/B FORE FLAP T/E DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20081105 EU 2008 11 5 08FDEA04642 1 20081030 A 5311 A53775400258 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS GOUGE ON FRAME SPLICE AT FR 29 3.5 INCH BELOW STR 12. REMOVED AND REPLACED FRAME SPLICE IAW SRM 51- 40-21, LOCATED AND DRILLED IAW SRM 51-40-44. TREATED AND PRIMED IAW SRM 51-21-10. SPLICE FABRICATED ON TRAVELER T8/765 592. 2 L 7 2 4F RT A35EU 20081105 EU 2008 11 5 08FDEA04644 1 20081030 A 5347 A5381292300000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK SEAT TRACK RBL 38 HAS CORROSION 7.0 INCH FWD OF FR 49. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-21 . 2 L 7 2 4F RT A35EU 20081105 NM 2008 11 5 08FDEA04630 1 20081030 A 5320 25FX12531 ATTACH BRACKET BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 UPPER LOBE INTERIOR STATION 760 RIGHT, BELOW WINDOW AT DOOR CUTOUT, CILL LINER ATTACH BRACKET IS CRACKED. REMOVED CRACK ED BRACKET VERIFIED MATERIAL FOR BRACKET AND FABRICATED NEW BRACKET. TREATED AND PRIMED INSTALLED NEW BRACKET IDENTIFI ED P/N ON BRACKET IN REF TO GMM 7-0-1000 PG 2 SRM 51-30-2 PG 1-13 AND DWG BY 25FX1432. THIS IS CLASSIFIED AS A MINOR RE PAIR. 2 L 7 3 4F A3WE 20081105 NM 2008 11 5 08FDEA04631 1 20081030 A 5315 656097140 FLOORBEAM BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 CORROSION ON BOTTOM AFT OF FLOORBEAM, FS 1034, LBL 13 TO LBL16, WL 208. REMOVED CORROSION ORIGINAL THICKNESS .100 .083 REMAINING OUT OF LIMITS FLOORBEAM REMOVED. NEW FLOOR SUPPORT LOCATED, DRILLED AND INSTALLED REF SRM 51-30-2 PG 13-16. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081105 EU 2008 11 5 08FDEA04632 1 20081030 A 5753 A5794217400200 CARRIAGE AIRBUS 300 A300B4622R 3930312 EU LT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 LEFT WING CENTER FLAP NR 3 TRACK CARRIAGE UPPER FLANGE ASSY IS CORRODED AT THE LUGS. REMOVED AND REPLACED THE LEFT NR 3 FLAP TRACK FWD CARRIAGE UPPER BRIDGE REF A300-600 AMM 27-54-27-4. 2 L 7 2 4F RT A35EU 20081105 NM 2008 11 5 08FDEA04638 1 20081030 A 5311 FRAME BOEING 757 75723A 1384967 NM BS 760 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 FWD CARGO COMPT, BS 760, S-24L, FRAME UPPER J-ANGLE IS DENTED. REPAIRED FRAME, BS 760, S-24L, FWD CARGO COMPT, IAW SRM 53-00-07, REPAIR NR 5. INSTALLED REPAIR PARTS IAW SRM 51-40-02. THIS REPAIR I CLASSIFIED AS A CATEGORY 'B" MAJOR REP AIR WITH THE FOLLOWING FOLLOW UP TRACKING REQUIREMENTS: INITIAL AT 37,500 FC FROM REPAIR INSTALLATION; THEREAFTER EVERY 12,000 FC. 2 L 7 2 4F RT A2NM 20081105 EU 2008 11 5 08FDEA04623 1 20081030 A 7120 A546109260000 MOUNT AIRBUS 310 A310222 3930315 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 418FE 343 AFT MOUNTING MATING SURFACE ON NR 2 ENGINE PYLON RUSTED. PERFORMED REPAIR AS PER EA NR 6-5450-125471 PART 2. 2 L 7 2 4F RT A35EU 20081105 EU 2008 11 5 08FDEA04628 1 20081030 A 5311 A53775400258 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS GOUGE ON FRAME SPLICE ON FRAME 29 2.5 INCH BELOW STR 12 L. REMOVED AND REPLACED SPLICE IAW SRM 51-4 0-21. NEW SPLICE FABRICATED ON TRAVELER T8/765594 MAT.2024-0 .063C BATCH NR 3976. LOCATED AND DRILLED IAW SRM 51-40-45 . TREATED AND PRIMED IAW SRM 51-21-10. 2 L 7 2 4F RT A35EU 20081105 EU 2008 11 5 08FDEA04629 1 20081030 A 5311 A53775400260 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS GOUGE ON FRAME SPLICE ON FRAME 30 2.5 INCH BELOW STR 12. REMOVED AND REPLACED FRAME SPLICE IAW SRM 51-40-21. NEW SPLICE FABRICATED ON TRAVELER T8/ 765593. LOCATED AND DRILLED IAW SRM 51-40-44. TREATED AND PRIMED IAW SRM 51-21-10. 2 L 7 2 4F RT A35EU 20081001 SO 2008 10 1 SWIA200820032 1 20080616 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 296SW 120325 LT IB WING STRINGER NR 10 CRACKED. C-CHECK, RE-WORKED STRINGER "RAMPS" FABRICATED AND INSTALLED. 2 L 7 2 4T RT A31SO 20081001 SO 2008 10 1 SWIA200820033 1 20080909 A 2720 ACTUATOR EMB 120 EMB120ER 3260203 SO RUDDER JAMMED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 217SW 120286 ON CLIMB, RIGHT RUDDER WAS JAMMED AFTER ABOUT 1 INCH OF TRAVEL. REPLACED BLUE RUDDER ACT PER MM 27-22-00, P/N: 308140-1 003, S/N ON, 0153 S/N OFF, 0494. 2 L 7 2 4T RT A31SO 20081001 NM 2008 10 1 08FDEA03201 1 20080731 A 5330 SKIN BOEING 757 75723A 1384967 NM BS 860 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 919FD 24636 AT BS 860, STR 7L. DAMAGE REPAIR CARRIED OUT IAW SRM 53-00-01 REV 93, FIG 201, REPAIR 6, SECT I PARA 3. REPAIR IS CL ASSIFIED AS MAJOR PER GMM 6-2-100 CRITERIA. 2 L 7 2 4F RT A2NM 20081001 EU 2008 10 1 2008UALA05696 1 20080913 A 3510 MF20010 MASK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 445UA 826 CREW REPORT: CAPT O2 MASK LEAKING AT O2 HOSE CONNECTION. ALSO 2ND O/B'S OXYGEN HARNESS FAILS TO INFLATE IS LEAKING. R EPLACED O2 MASK AT CAPTAIN'S, FIRST OBSERVER'S & SECOND OBSERVERS POSITION. 2 L 7 2 4F 4 F RT A28NM E40NE 20081002 SO 2008 10 2 C2XA08RI142 1 20080926 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13975 145163 RIC - MX - DURING ROUTINE MAINTENANCE RIC MX FOUND SERVICE DOOR EMERGENCY LIGHT NOT ILLUMINATING. MX FOUND ONE WIRE DIS CONNECTED FROM THE SPLICE. MX RECONNECTED WIRE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081002 SO 2008 10 2 C2XA08RI143 1 20080920 A 3350 375901 SIGN EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 13997 145298 FLIGHT 2064 - EWR - FLIGHT CREW REPORTED EMERGENCY EXIT ROW 12 B/C AFTERWARD SIGN INOPERATIVE. EWR MX REMOVED AND REPLA CED EMERGENCY SIGN AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081002 NM 2008 10 2 2008UALA05536 1 20080830 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 THE A-ZONE LT COLUMN EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, OP CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081002 NM 2008 10 2 2008UALA05549 1 20080831 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 180UA 25224 UPPER DECK CEILING EMERGENCY LIGHT, SEAT 16 INOP. *S/D* LIGHT FAULTY. RELAMPED, OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081002 NM 2008 10 2 2008UALA05556 1 20080831 A 5320 STIFFENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE STA 246 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 STA 246 FLOORBEAM FWD SIDE VERT STIFFENER CRACKED AT LBL 26. MAJOR REPAIR ACCOMPLISHED. REMOVED AND INSTALLED NEW STIF FENER. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 2008UALA05557 1 20080831 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1518 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 MAIN CABIN FLOORBEAM T-CAP CORRODED UNDER STEEL SUBFLOOR AT BS 1518 AT BL 0. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE D T-CAP SECTION. FABRICATED AND INSTALLED A NEW T-CHORD, SPLICE ANGLES & SPLICE STRAPS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 2008UALA05560 1 20080901 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 628 S26-27L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 DENT IN FUSELAGE AT BS 628 AND BETWEEN STR 26L-27L. *S/D* MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN. FABRICATE D AND INSTALLED A REPAIR DOUBLER. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 2008UALA05561 1 20080901 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY LIGHT INOP AT 49ABC. FAULTY LAMP. REPLACED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 20081002 NM 2008 10 2 2008UALA05582 1 20080903 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1430 S29R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 STR 29R AT STA 1430 REQUIRES RPR DUE TO PREVIOUS DAMAGE. MAJOR REPAIR ACCOMPLISHED. REMOVED & REPLACED STRINGER WITH N EW STRINGER SECTION (P/N 146N3300-183). 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 2008UALA05583 1 20080903 A 5313 STRINGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1430 S30R DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 STR 30R AT STA 1430 REQUIRES REPAIR DUE TO PREVIOUS DAMAGE. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF STRI NGER. FABRICATED & INSTALLED A NEW STRINGER SECTION & SPLICE PLATE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 2008UALA05585 1 20080903 A 5240 DOOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R2 OUT OF ADJUST A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 826UA 989 CREW REPORT: IN FLIGHT, DOOR 2R SHOWS DISARMED ON DOORS PAGE. DOOR INDICATES ARMED AT DOOR. FOUND DOOR OUT OF ADJUSTM ENT. PERFORMED DOOR ADJUSTMENT, ALL OPERATIONS ARE NORMAL.. NO REPEATS SINCE ORIGINAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081002 NM 2008 10 2 CALA0800857 1 20080905 A 5311 143A1120 FRAME BOEING 737 737724 13844BY NM BS 480 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27722 28789 CABIN STA 480 FRAME CRACKED BETWEEN S8-9R. INSTALLED REPAIR PER EC/RA 5310-04824 REV A. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 2008UALA05898 1 20080926 A 3350 LAMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 331UA 24192 AFT 15 FT OF CABIN FLOOR MOUNTED EMERGENCY ESCAPE PATH LIGHTING IS INOP. REMOVED, DRIED & REINSTALLED AFT THREE LAMPS. OP CHKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20081002 NM 2008 10 2 UPS08553282 1 20080813 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 560 S7R DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 FRAME DENTED BS 560 4 INCHES ABOVE STR 7R. ACCOMPLISHED REPAIR PER SRM 53-00-07-2R1. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 UPS08553283 1 20080813 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 440 S12L GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 BS 440 FRAME GOUGED STR 12L FWD SIDE. REPAIRED BS 440 FRAME WITH CHANNELS & FILLER IAW SRM 53-00-07- 2R. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 UPS08553284 1 20080813 A 5311 FRAME BOEING 757 75724APF 1384969 NM BS 940 S15R GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 BS 940 FRAME INNER CHORD IS GOUGED ON THE AFT SIDE AT STR 15R. BLENDED OUT GOUGED PER ATS ER 08-2721 DATED AUG 28 08. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 UPS08553285 1 20080813 A 5230 SKIN BOEING 757 75724APF 1384969 NM CARGO DOOR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 AFT CARGO DOOR FWD EDGE OF OUTER SKIN IS DAMAGED 7 INCHES UP FROM LWR EDGE. BLENDED OUT GOUGE PER AT S ER 08-2776 DATED 28AUG08. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 UPS08553291 1 20080815 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM BS 440 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 MAIN CARGO FLOORBEAM UPPER SURFACE IS CORRODED BL 0 - RBL 65 WL 208 BS 440. BLENDED OUT CORROSION PE R ATS ER08-2754 DATE 08AUG08. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 2008UALA05890 1 20080925 A 2421 756589A GENERATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU INOPERATIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 776UA 26937 APU GENERATOR INOP. REPLACED GENERATOR. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081002 NM 2008 10 2 UPS08553292 1 20080816 A 5315 FLOORBEAM BOEING 757 75724APF 1384969 NM BS 1320 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 416UP 23903 INSPECTION TYPE:C3 CORROSION ON UPPER SURFACE OF FLOORBEAM AT STA 1320 RBL 25-65 WL 208. BLENDED OUT CORROSION PER ATS ER08-2738 DATED 28AUG08. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 2008UALA05888 1 20080925 A 3397 58783 CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 593UA 28144 EEL STRIP LIGHTING FROM ROW 9 THRU 15 BLINK INTERMITTANTLY. REPLACED CABLE RIBBON FROM SEAT 12 THRU 15. OPS CHECKS GOO D. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 UPS08553299 1 20080904 A 3350 BULB BOEING 757 75724APF 1384969 NM EMERGENCY LIGHT NO TEST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 461UP 28265 EXTERIOR EMERGENCY LIGHT FAILED TO TEST. REMOVED AND REPLACED GE767 BULB & OPS CHECKED PER MM 33-51-06. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 UPS08M53293 1 20080820 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C1 FOUND CORROSION IN NR 1 RIGHT BARREL NUT BORE HOLE. REPAIRED HORIZONTAL BARREL NUT HOLE NR 1 RT REF EO MD11-5510-30459-A AND EA 0 11-5510-A1499. 2 L 7 3 4F RT A22WE 20081002 NM 2008 10 2 UPS08M53294 1 20080808 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C1 FOUND CORROSION IN NR 29 LT BARREL NUT HOLE. REPAIRED HORZ STAB BARREL NUT HOLE NR 29 LT REF EO MD11 -5510-30462-A AND EA 011-5510-01-A1462. 2 L 7 3 4F RT A22WE 20081002 NM 2008 10 2 UPS08M53295 1 20080808 A 5510 STRUCTURE DOUG MD11 MD11F 3023600 NM HORIZONTAL STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:C1 FOUND CORROSION IN NR 1 LT BARREL NUT BORE HOLE. REPAIRED HORZ STAB CENTER BOX HOLE NR 1 LT REF EO M D11-5510-30452-A AND EA 011-5510-01-A1491. 2 L 7 3 4F RT A22WE 20081002 NM 2008 10 2 2008UALA05886 1 20080924 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 MAIN CABIN T-CAP AT BS 1640, RBL 58 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF T-CAP FROM RBL 0 TO RBL 64. FABBED AND INSTALLED NEW SECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 2008UALA05883 1 20080924 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 MAIN CABIN T-CAP AT BS 365, RBL 10 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF T-CAP RBL 0 TO R BL 64. INSTALLED NEW SECTION. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 2008UALA05881 1 20080924 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 AFT PIT STA 1540 FRAME DENTED BETWEEN STR 22L AND 23L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED FRAME SECTION AND IN STALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 2008UALA05876 1 20080924 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 LEFT OVERWING FWD 2 EMERGENCY LIGHT ASSY INOP. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081008 EA 2008 10 8 TRAX200801116 1 20080905 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 980EV 7759 JOB 8775921 OPERATION 153 FLOOR SUPPORT BEAM LBL 27 HAS MINOR CORROSION NUTPLATES FROM FS 621 TO FS 574. SUP 9/11/2008 - AFTER FURTHER INVESTIGATION FOUND ALL CORROSION N LBL 27, FS 574-621 AROUND NUTPLATES TO BE WITHIN REPAIRABLE LIMITS E XCEPT 1 AREA AT FS 615. BLENDED ALL OTHER AREAS TO REMOVED CORROSION. APPLIED ALODINE, PRIME AND PAINT. ALL WORK PERF ORMED IAW REO 601R-53-00-005. REPLACEMENT OF AFT FITTING AT LBL 27 FS 605-621 DUE TO DAMAGE BEYOND REAPAIRABLE LIMITS. (K) 2 L 7 2 4F RT A21EA 20081002 NM 2008 10 2 UPS08553388 1 20080926 A 5320 DEFLECTOR BOEING 757 75724APF 1384969 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 424UP 25369 INSPECTION TYPE:C2 LIGHTNING STRIKE ON THE LT SIDE OF THE AIR DEFLECTOR UNDER THE APU EXHAUST. BLENDED DAMAGE PER UPS E O B757-5300-30642-A/ATS ER 08-2995. 2 L 7 2 4F RT A2NM 20081002 EU 2008 10 2 2008UALA05601 1 20080828 A 3230 VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE MLG INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 437UA 655 LANDING GEAR EXT DELAY T-S: REPLACE LANDING GEAR SAFTEY VALVE 49GA. REPLACED LANDING GEAR SAFTEY VALVE 49GA PER MM32-3 1-17 THRU STEP 3.C. PG 411. NEED TO COMPLETE INSTALLATION FROM STEP 4.D. PG 412 THRU TO END. CONT OF AMIS ITEM 7342001 . 2 L 7 2 4F 4 F RT A28NM E40NE 20081008 EA 2008 10 8 TRAX200801117 1 20080905 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B16 1900305 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 980EV 7759 JOB 8775921 OPERATION 144 PAX DOOR AFT DRAG ANGLE IS CRACKED. RESOLVED ON W/O 98579 TASKCARD NR 00181. C/A REPAIRED PA X DOOR AFT DRAG ANGLE IAW BOMBARDIER REO 601R-52-11-513. SEAL AND PAINT REQUIRED. SEALED PNL IAW CRJ 200 MM 51-23-00. PAINTED IAW CRJ 200 SRM 51-25-01. WORK PERFORMED IAW ASA EC/TX REO 601R-52-11-513. 2 L 7 2 4F RT A21EA 20081002 NM 2008 10 2 CALA0800862 1 20080905 A 5312 148A2232 BULKHEAD BOEING 737 737724 13844BY NM BS 304 CANNING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27722 28789 PER EA 5310-04639 REV A STEP 3.1, AFT PRESURE BULKHEAD HAS ONE OIL CAN SPOT STATION 1016 BETWEEN STR 0L AND 2L AT WATER LINE STATION 304. FABRICATED AND INSTALLED REPAIR PER ECRA 5311-01420. DIP WRITEN TO ACCOMPLISH A PERMANENT REPAIR WIT HIN 12 MONTHS FROM SEPTEMBER 4, 2008. PLANNING SHOULD CONTACT ENGINEERING AFTER JULY 4, 2009 BUT BEFORE AUGUST 4, 2009 FOR PERMANENT REPAIR. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 2008UALA05852 1 20080923 A 4990 OIL SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 549UA 25397 FOUND OIL LEAKING FROM BOTTOM OF PNEUMATIC SUPPLY DUCT COMING OFF APU IN APU COMPARTMENT WHILE ACCOMPLISHING SERVICE TIP , APU HOC. NO OTHER OIL LEAKAGE NOTED. REMOVED & REPLACED APU. 2 L 7 2 4F 4 F RT A2NM E17NE 20081001 NM 2008 10 1 SWAA085174 1 20080924 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CORRODED AT BS 312, STR 28L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 08FDEA04052 1 20080926 A 5230 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 613FE 48749 HFEC INSPECTION CARRIED OUT ON DIAMETER 0.460 INCH HOLES AT MAIN DECK CARGO DOOR NR 4 SPOOL FITTING, FOUND CRACK INDICAT ION ON HOLE A, C AND D. REMOVED AND REPLACED AS PER SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081002 NM 2008 10 2 CALA0800849 1 20080904 A 5320 69759963 FLOOR SUPPORT BOEING 737 7373T0 1384582 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 G2 GALLEY RIGHT FORWARD FLOOR MOUNT HAS CORROSION. REMOVED MOUNT AND REPLACED THE MOUNT WITH NEW PART IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 2008UALA04375 1 20080822 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 4A MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 107UA 26900 A 4A AFT EEL STRIP MISSING. *S/D* FOUND MISSING LIGHT STRIP. REPLACED LIGHT STRIP, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20081002 NM 2008 10 2 2008UALA05494 1 20080826 A 3350 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 EMERGENCY LIGHT INOP ON BULL NOSE AT SEAT 9D AND 13D. *S/D* FOUND FAULTY LIGHT. REPLACED DOOR 2L BATTERY. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 EU 2008 10 2 2008UALA05546 1 20080831 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 451UA 865 BEAM 255 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM. BEGAN INSTALLING FLOORBEAM 255 IN A/C. COMPLETED IN STALLATION OF FLOORBEAM 255. INSPECTED INSTALLATION OF BEAM 255 FOR SAFETY AND SECURITY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081002 NM 2008 10 2 2008UALA05570 1 20080902 A 5420 WEB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 NR 1 PYLON STA 156 WEB AT OUTBOARD DRAIN HOLE IS CRACKED, MIGRATED BEYOND EXISTING STOP DRILL. MAJOR REPAIR ACCOMPLISHE D. FOUND 2 CRACKS AT INBOARD DRAIN HOLE. STOP DRILLED CRACKS. FABRICATED & INSTALLED A DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 2008UALA05578 1 20080903 A 2611 SMOKE DETECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE E/E BAY FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 771UA 26932 CHANNEL 1 E&E SMOKE DETECTOR EICAS MESSAGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081002 NM 2008 10 2 2008UALA05579 1 20080903 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 1F BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 AFT EMERGENCY LIGHT AT SEAT 1F BROKEN. REPLACED EMERGENCY LIGHT ASSY. OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081002 NM 2008 10 2 2008UALA05580 1 20080903 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SEAT 1E MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 AFT EMERGENCY LIGHT AT SEAT 1E MISSING. REPLACED EMERGENCY LIGHT. OPS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081002 SO 2008 10 2 C2XA08RI146 1 20080926 A 3350 INVERTER EMB 145 EMB145LR 3260212 SO CABIN FAILED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 16954 145072 FLIGHT 2717 - EWR - FLIGHT CREW REPORTED EMERGENCY LIGHT ABOVE GALLEY INOPERATIVE. EWR MX REMOVED AND REPLACED EMERGENC Y LIGHT INVERTER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081002 NM 2008 10 2 ZZDA2008156 1 20080901 A 5330 SKIN BOEING 717 717200 1383700 NM BS 256-275 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 920AT 55083 GROUND DAMAGE LT SIDE A/C AT BS 256 AND L17 AND BS 275 LONGERON. CUT OUT DAMAGED AREA, FABBED AND INSTALLED DOUBLER REP AIR PER SRM 53-00-01 REPAIR 1 NDT OF CUT OUT AREA PERFORMED PER NDT SPM 06-10-01-001, NO CRACKS NOTED AT AAR W/O 28385 N /R 3777 AND 3780. 2 L 7 2 4F TR A6WE 20081002 2008 10 2 2008UALA05589 4 20080903 A 2565 5A29011 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE ESCAPE SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 676UA 30028 ASPIRATOR LEAKING. REPLACED ASPIRATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 2008 10 2 2008UALA05590 4 20080904 A 2565 5A29011 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE ESCAPE SLIDE UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 ASPIRATOR LEAKING ON TOP TUBE. BAD SEAL. REPLACED ASPIRATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 2008UALA05591 1 20080904 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 AFT MAIN GALLEY WALL EMERGENCY LIGHT FWD OF GALLEY AND LT SIDE INOP. 2 L 7 4 4F 4 F RT A20WE E24NE 20081002 NM 2008 10 2 2008UALA05592 1 20080904 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY LIGHT SEAT 4A AFT INOP. FOUND FAULTY LAMP. RELAMPED, OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081002 NM 2008 10 2 2008UALA05593 1 20080904 A 2120 UNKNOWN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 556UA 26650 WHILE DESCENDING TO FL 350 AT FL 390 F/A REPORTED SMOKE ALARMS SOUNDED IN LAVS 2L AND FWD-AFT. ALSO A LIGHT HAZE WAS NO TICED IN THE AFT CABIN. NO ODOR OF OIL OR ELECTRICAL BURNING. UPON REACHING FL350 HAZE CLEARED. SMOKE ALARMS WERE RES ET AND DID NOT RESOUND. ALL PACK OPERATIONS APPEARED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 CALA0800925 1 20080926 A 5320 6545834U551 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16649 28910 FWD WET AREA CROSS BRACE CRACKED AT FLOORBOARD ATTACH HOLES BETWEEN STA 340-360 LBL 46. REMOVED AND REPLACED INTERCOSTA L AT LBL 46 BS 328 TO BS 344 REF 737-500 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085116 1 20080918 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085115 1 20080918 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085114 1 20080918 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 7L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085133 1 20080917 A 2612 727SW FIRE DETECTOR BOEING 737 7373H4 1384600 NM APU FAULTY A SWAA K NONE N FALSE WARNING CL CLIMB 1 SW 29 357SW 26594 AT FL 8000 APU FIRE WARNING LIGHT ILLUMINATED AND WARNING SOUNDED, DISCHARGED FIRE BOTTLE AND LIGHT EXTINGUISHED. REMOV ED AND REPLACED OVERHEAT DETECTOR PER MM. 2 L 7 2 4F RT A16WE 20081002 2008 10 2 SWAA085132 4 20080917 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 351SW 24572 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0853475 1 20080905 A 2160 693732478 MODULE BOEING 737 737890 1384527 NM CABIN TEMP FAULTED A ASAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 02 585AS 4077 35683 CONT CABIN ZONE TEMP LIGHT COMES ON WHEN RECALLED GOES OUT WITH MASTER CAUTION RESET HARD FAULT ON ZONE TEMP CONTROLLER NR 1 FOR "SELECTOR FLT DECK" NEED TEMP SELECTOR 4 2160 9 4035. TRIED RESEATING CONNECTOR, NO HELP. VERIFIED DISCREPANC Y & HARD FAULT ON BITE CK NR 1 CONTROLLER. REMOVED AND REPLACED TEMP CONTROL MODULE REF MM 21 61 15. REPAIR CONFIRMED FIXED. 2 L 7 2 4F RT A16WE 20081002 2008 10 2 ASAA0873478 4 20080907 A 2565 5A33075 SLIDE BOEING 737 737790 13844CN NM L2 DOOR OBSTRUCTED A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 609AS 1273 29752 L2 DOOR SLIDE CATCHING ON DOOR. REMOVED & REPLACED SLIDE REF MM 25 66 01 000 801. 2 L 7 2 4F RT A16WE 20081002 2008 10 2 SWAA085129 4 20080918 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 221WN 34259 L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0843477 1 20080907 A 5210 571411 GUST LOCK BOEING 737 737490 1384715 NM L1 DOOR STIFF A ASAA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 02 796AS 28891 F/A REPORTS L1 DOOR GUST LOCK IS DIFFICULT TO RELEASE. OPS CHECK OF L1 DOOR GUST LOCK GOOD. LUBRICATED AND NO DEFECTS FOUND. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085124 1 20080918 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 15L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085123 1 20080918 A 5322 6546529 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 21R - 22R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0853514 1 20080915 A 2840 125334D1 WARNING SYSTEM BOEING 737 737890 1384527 NM FUEL SYSTEM MALFUNCTIONED A ASAA K NONE N FALSE WARNING CL CLIMB 1 NM 02 577AS 5958 35186 ON CLIMBOUT 2000LBS OF FUEL FROM NR 1 TANK TRANSFERRED INTO CENTER TANK. FUEL IMBAL LIGHT ON UPPER DEU FUEL QUANTITY IL LUMUNATED. FUEL X FEED WORKED NORMAL INFLIGHT. FUEL IMBALANCE WAS VERIFIED BY REQUIREMENT OF RUDDER AND AILERON TRIM. PERFORMED SCAVENGE PUMP FIM TEST PER MM 28 21 00 810 803. NO DEFECTS NOTED. PERFORMED OPERATIONAL CHECK OF THE FUEL C ROSSFEED VALVE PER MM 28 22 00 730 802. NO DEFECTS NOTED. ACCESSED FUEL PANEL 532RB FOR VISUAL CHECK OF LEFT WING VENT FLOAT VALVE ASSEMBLY. NO DEFECTS NOTED OR EVIDENCE OF DAMAGE. CLOSED FUEL PANEL 532RB IAW MM 28 11 11 400 801. RELEA SED JET FOR ETOPS FCF. ACCOMPLISHED FCF PER MIG 56 AND FOUND TO BE SATISFACTORY. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ZZDA2008157 1 20080915 A 3350 8039251 BATTERY PACK BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 936AT 55058 DURING OVERNIGHT SERVICE CHECK FOUND EMERGENCY SEAT LIGHTS ROW 21-25 INOP. REPLACED BATTERY PACK ASSEMBLY AT SEAT 3DF A ND OPS CHECK GOOD PER AMM 33-51. 2 L 7 2 4F TR A6WE 20081002 WP 2008 10 2 UPS08853334 1 20080814 A 5330 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 FUSELAGE EXTERIOR SKIN REPAIR DOUBLER IS CRACKED AT L1 DOOR HOLD OPEN PIN RECEPT 8. REMOVED, FABRICA TED, AND INSTALLED REPAIR DOUBLER AT L1 DOOR HOLD OPEN PIN RECEPT IAW DC8 SRM 51-1-21, 51-1-8. 2 L 7 4 4F RT 4A25 20081002 EU 2008 10 2 UPS08153309 1 20080910 A 5753 FAIRING AIRBUS A300 A300F4622R 3930360 EU NR 4 FLAP DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 131UP 0815 INSPECTION TYPE:N/A, NR 4 MOVEABLE FLAP FAIRING DENTED OUT OF LIMTS. DETERMINED DAMAGE TO BE THREE DENTS. DENTS MEASUR E AS FOLLOWS: DENT FWD IS 1.3" X 1.0, CENTER DENT IS 2.2" X 1.6" & AFT DENT IS .6" X 1.4". INSPECTED AND TAPED DENTS P ER EO A300-5720-30525-A. TRANSFERRED TO DMI LOG D384264. PERMANENT REPAIR WITHIN 30 DAYS. 2 L 7 2 4F RT A35EU 20081002 NM 2008 10 2 ASAA0873510 1 20080909 A 5754 114A50104 SKIN BOEING 737 737790 13844CN NM NR 8 SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 NR 8 SLAT LOWER SURFACE T/E IS CHAFED AT THE ACTR. REMOVED DAMAGE, FABBED FILLER AND DOUBLER, BONDED THE REPAIR IAW B73 7 700 SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873497 1 20080828 A 5321 453A2601017 FLOOR PANEL BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 AFT CARGO PIT FLOORBOARD STA 767 887 HAS CORROSION WOUND EDGE ORIGINAL PANEL WAS BEYOND ALLOWABLE LIMITS IAW ASA EA 2550 01425. FLOOR PANEL REPLACED WITH REPAIR PART IAW B737 700 SRM 51 40 05 AND 51 40 06 AND 51 40 08. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873496 1 20080827 A 5321 453A161031 FLOOR PANEL BOEING 737 737790 13844CN NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 FWD CARGO PIT FLOOR PANEL FOUND DENTED AT DIFFERENT LOCATIONS BS 495 TO 500D. FLOOR PANEL REPLACED AT BS 495 500D IN FW D CARGO PIT IAW B737 700 SRM 53 30 53 AND 51 40 05. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 2008UALA05622 1 20080906 A 5210 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 L-2 DOOR UPPER HINGE CUTOUT REQUIRES A REPAIR DOUBLER PER MM 52-11-87. HFEC INSPECTION COMPLETE PER NDT 6- 51-00-19, AN D NO CRACKS NOTED. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 2008UALA05623 1 20080906 A 5730 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT WING DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 543UA 25698 LEFT WING UPPER SURFACE SKIN DENTED OUTBOARD END BETWEEN WS 780 AND WS 810. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE AND INSTALLED CORE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 ASAA0873487 1 20080828 A 5320 146A81237 INTERCOSTAL BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 AFT CARGO RT SUPPORT INTERCOSTAL AT BS 767 TB CORRODED. AFT CARGO RT SUPPORT INTERCOSTAL AT BS 767 AND 6 REPLACED WITH NEW PART. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873486 1 20080828 A 5312 111A1141 BULKHEAD BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 WHEEL WELL AREA BULKHEAD AT BS 663 FOUND CRACK AT RBL 14. REPAIRED IAW B737 700 SRM CH 51 70 04 REPAIR 10. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085080 1 20080916 A 5311 6546552 FRAME BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 827, STR 25L TO STR 26L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085079 1 20080916 A 5315 BAC1509100146 FLOORBEAM BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 773, LBL 8. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085074 1 20080916 A 5311 6558280 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085073 1 20080916 A 5340 6545815 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, RBL 65. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085072 1 20080916 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800905 1 20080916 A 3350 D71702030 CHARGER BOEING 737 737924 13848A1 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 27 73406 30123 RIGHT FORWARD EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED RIGHT FORWARD EMERGENCY LIGHT POWER SUPPLY AN D BATTERY IAW AMM TASKS 33-51-06-960-805 AND 33-51-06-960-806, OPERATION CHECKS NORMAL. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800904 1 20080916 A 5315 141T52822 STIFFENER BOEING 767 767224 1385170 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69154 30433 BS 246 FLOORBEAM FWD SIDE ONE STIFFENER FOUND CRACKED AT LBL 25. FLOORBEAM LBL 25" FWD SIDE STIFFENER REPLACED PER SRM 51-10-02 AND FASTENER INSTALLED PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081002 NM 2008 10 2 2008UALA05630 1 20080907 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT PULLED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 182UA 25279 EEL LIGHT WIRES PULLED 55C. LIGHT DEFECTIVE & OUT OF POSITION. REPLACED EMERGENCY LIGHT. OP CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20081002 NM 2008 10 2 2008UALA05631 1 20080907 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 118UA 28811 THE 4F FWD LIGHT STRIP BROKEN OFF. 2 L 7 4 4F 4 F RT A20WE E24NE 20081002 2008 10 2 2008UALA05638 4 20080906 A 2300 ACP2788AB04 AUDIO PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 340UA 24244 UNABLE TO TRANSMIT ON ANY ACP SELECTIONS FROM CAPTAIN'S SIDE. RTFL. REPLACED THE CAPT'S ACP AND THE REMOTE ELECTRONICS UNIT. 2 L 7 2 4F 4 F RT A16WE E21EU 20081002 NM 2008 10 2 2008UALA05644 1 20080907 A 8011 8110503 STARTER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 1 ENGINE INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 223UA 30224 NR 1 ENG STARTER INOP. FOUND STARTER INOP. REPLACED STARTER. ENG DRY MOTOR & LEAK CHECKED NORMAL. OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081002 NM 2008 10 2 2008UALA05645 1 20080907 A 8011 35054367 STARTER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE NR 1 ENGINE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 ENG SLOW TO ACCELERATE AFTER STARTER CUTOUT APPROX 50 PERCENT. COMPLETED FIM 73-21-00 TO BLOCK 7. ALL NORMAL. FOUND F AULTY STARTER. REPLACED STARTER. ENGINE STARTS WITHIN LIMITS. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 CALA0800892 1 20080916 A 5311 6546536 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 559 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. REMOVED BRACKET IAW EA531 0-04498, CUT OUT DAMAGE IAW EA5310-04498. INSPECTED IAW 737 NOTM PT65100-00 FIG 23, NO DEFECTS NOTED, FABRICATED PARTS ALODINED, PRIMED PARTS AND CUTOUT IAW EA5310-04498 INSTALLED REPAIR PARTS AND BRACKET IAW EA5310-04498. 2 L 7 2 4F RT A16WE 20081105 EU 2008 11 5 08FDEA04645 1 20081031 A 5311 A53775400260 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS GOUGE ON FRAME SPLICE 2.5 INCH BELOW STR 12 L ON FR 32. REMOVED AND REPLACED FRAME SPLICE IAW SRM 5 1-40-21, LOCATED AND DRILLED IAW SRM 51-40-45. TREATED AND PRIMED IAW SRM 51-21-10. FABRICATED NEW SPLICE ON TRAVELER T8/765595. 2 L 7 2 4F RT A35EU 20081106 WP 2008 11 6 AALA200802663 1 20081002 A 5755 5936832505 FITTING DOUG DC9 DC982 3022082 WP SPOILER CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 574AA 53151 TUL - CRACK FOUND ON LEFT GROUND SPOILER FITTING AT INBOARD FORWARD CORNER. CRACK LENGTH IS .5 INCH. REPLACED FITTING IN ACCORDANCE WITH AARD 57 20 00 15. 2 L 7 2 4F A6WE 20081106 NM 2008 11 6 DHLA2008745598 1 20080907 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT BS 660 BETWEEN S-25R AND S-26R SHEAR TIE AND FRAME CORRODED. REPLACED FUSELAGE SHE AR TIE TEE SECTION AT B/S 660 BETWEEN S-25R AND S-26R IAW B727SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 DHLA2008745591 1 20081008 A 5313 STRINGER BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 497 S28L WITH CORROSION. REPAIRED FUSELAGE S28L SECTION FROM BS 482 TO 536 I AW SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081106 WP 2008 11 6 AALA200802658 1 20081002 A 3350 P4010051111 MODULE DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7543A 53025 LGA - EMERGENCY AISLE PATH LIGHTS FROM FIRST CLASS THROUGH MID CABIN INOPERATIVE. REPLACED MODULE ASSEMBLY AT FIRST CLAS S OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081106 NM 2008 11 6 CALA0801024 1 20081103 A 5311 143A1113 BELTFRAME BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34222 28931 CRACK FOUND IN BELT-FRAME AT STATION 440 AT FASTENER BETWEEN S-8R AND S-9R AT OVERHEAD BIN MOUNT RAIL ATTACHMENT. REPAI RED FRAME PER EC/RA 5310-04863. 2 L 7 2 4F RT A16WE 20081106 EA 2008 11 6 MASA2008103100758 1 20081031 A 5270 PROXIMITY SWITCH CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT OUT OF ADJUST A MASA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 926LR 15026 ASH FLT 2622 CLT-GSO. LT AFT EMERGENCY EXIT DOOR CAUTION ON TAXI. MX ADJUSTED PROXIMITY SWITCH. 2 L 7 2 4F RT A21EA 20081106 NM 2008 11 6 QXEA2008110501131 1 20081018 A 5414 SKIN BOMBDR DHC8 DHC8402 1390042 NM NR 1 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 418QX 4143 PDX - C1 - UPPER OUTBOARD SKIN OF THE NR 1 NACELLE IS CRACKED. ROUTED OUT CRACK AND RESTORED FINISH REF RD 8/4-54-157. 2 H 7 2 4T RT A13NM 20081106 NM 2008 11 6 SWAA085994 1 20081031 A 3350 417A56014 SIGN BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 401WN 29813 FOUND FWD MID CABIN EMERGENCY EXIT SIGN MISSING. REPLACED SIGN PER MM. 2 L 7 2 4F RT A16WE 20081106 2008 11 6 SWAA085995 4 20081031 A 2565 6567380 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 407WN 29817 DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EXIT SLIDE LENS COVER LOOSE. REMOVED AND REPLACED COVER PER EA. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 USA2008F00043 1 20081004 A 2150 A/C PACK BOEING 737 7374B7 138449C NM ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 434US 24556 AFTER TAKEOFF, CAPTAIN REPORTED, RECEIVED A SINGLE CHANNEL PACK FAULT AND A ODOR IN THE COCKPIT AND FWD CABIN. THE SMELL WAS REPORTED AS BEING A MECHANICAL ODOR, NOT SMOKE. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT . NO EMERGENCY WAS DECLARED. MAINT PERFORMED OPS CHECK OF PACK SYS IAW MM 21-51-00-5. WITH BOTH ENGINES RUNNING AT POWER SETTINGS AND WITH APU, MAINT COULD NOT DUPLICATE PROBLEM. LEFT PACK FAULTS WERE RESET AND DID NOT RETURN. BITE CHECK OF CONTROLLER SHOWS NO FAULTS AFTER RESET. (NOTE: ACFT FRESH OUT OF HEAVY MAINT. NEW INTERIOR LEATHER INSTALLED.) (K) 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 SWAA085996 1 20081031 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 407WN 29817 DURING SCHEDULED HC2 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081106 2008 11 6 SWAA085997 4 20081101 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 447WN 33720 FOUND R1 DOOR EMERGENCY EXIT SLIDE LOOSE. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081106 NM 2008 11 6 2008UALA06307 1 20081029 A 3800 WATER SYSTEM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 777UA 26916 LOSS OF ALL WATER PRESSURE. FLIGHT DIVERTED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081106 NE 2008 11 6 2008UALA06308 2 20081028 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE OIL CONSUMPTION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 674UA 29242 724365 HIGH OIL CONSUMPTION. 2 L 7 2 4F 4 F RT A1NM E24NE 20081106 EU 2008 11 6 2008UALA06309 1 20081030 A 2120 UNKNOWN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN ODOR A UALA A UNSCHED LANDING W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 480UA 1555 ELECTRICAL SMELL IN CABIN. FLIGHT DIVERTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081002 NM 2008 10 2 2008UALA05647 1 20080909 A 7500 BLEED AIR SYS BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE APU INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 791UA 26933 APU BLEED AIR SYSTEM INOP. OIL FOUND IN APU INLET PLENUM ASSY. REPLACED APU ASSY. REPLACED IGV ACTUATOR. OPS NORMAL 2 L 7 2 4F 4 F RT T0001SE E46NE 20081002 NM 2008 10 2 CALA0800890 1 20080916 A 5311 6546538 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 597 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. REMOVED BRACKET IAW5310-0 4498, CUT OUT DAMAGE IAW EA5310-04498. INSPECTED CUTOUT IAW 737 NDTMPT65100-00 FIG 23, NO DEFECT NOTED. FABRICATED PAR TS, ALODINED, PRIMER PARTS AND CUT OUT IAW EA5310-004498 INSTALLED REPAIR ANGLES AND AIR CONDITIONING (AC) BRACKET IAW E A5310-04498 E. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084964 1 20080909 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 410WN 27897 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084965 1 20080909 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 425LV 29829 DURING SCHEDULED 6Y CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT ASSY CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084966 1 20080909 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 513D S10L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 FUSELAGE SKIN CRACKED AT BS 513D, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084967 1 20080909 A 5315 BAC1509100146 FLOORBEAM BOEING 737 737301 1384611 NM BS 860 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 860, RBL 8. REPAIRED FLOORBEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084970 1 20080909 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 360 S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 22L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084975 1 20080909 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 400 S27L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 27L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084976 1 20080910 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 520 S22R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 22R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084977 1 20080910 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM BS 907 S24L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 24L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084978 1 20080910 A 5311 6517685 FRAME BOEING 737 7373H4 1384600 NM BS 360 S14L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 360, STR 14L. REPAIRED FRAME WEB PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085140 1 20080921 A 5311 6546550 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787 STR 26R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 ASAA0843518 1 20080921 A 5210 507945310 GUIDE ARM BOEING 737 737490 1384715 NM L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 709AS BN001319 28896 L1 DOOR EXTREMELY DIFFICULT WILL NOT LATCH ADJUST FORWARD L1 DOOR GUIDE ARM. REF AMM 52 11 21 401, OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 20081001 2008 10 1 ASAA0853517 4 20080919 A 2310 8220990004 TRANSCEIVER BOEING 737 737890 1384527 NM HF COMM FAILED A ASAA K NONE O OTHER UK UNKNOWN 1 NM 02 570AS 6329 35185 HF RADIO NR 1 INOP VERIFIED MALFUNCTION BITE CHECK PER MM 23 11 00 SHOW TRANCEIVER NR 1 FAILURE. REMOVED AND REPLACED N R 1 HF TRANCEIVER. OPERATIONAL TEST GOOD PER MM 23 11 21, SYSTEM CHECKS GOOD. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085113 1 20080917 A 5753 65C30462 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 645SW 28330 DURING SCHEDULED SPV CHECK, FOUND LT WING INBOARD FORE FLAP DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20081001 EU 2008 10 1 2008UALA05547 1 20080901 A 3510 REGULATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OXY SYS LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 441UA 751 CREW OXYGEN SYSTEM LOW. RECORD PRESSURE PRIOR TO SERVICING. FOUND O2 REGULATOR - TRANSMITTER LEAKING AT FILL PORT. RE PLACED REGULATOR - TRANSMITTER. FOUND LOOSE B-NUT AT 1ST OBSERVER'S 02 BOX. SECURED LINE. SERVICED O2 TO 1890 PRIOR T O DEPARTURE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081001 NM 2008 10 1 2008UALA05551 1 20080831 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 180UA 25224 SEAT 5F AFT FLOOR EMERGENCY LIGHT INOP. FOUND FAULTY LAMP STRIP. REPLACED LAMP STRIP, OP CHECK GOOD. AC OK FOR SERVIC E. 2 L 7 4 4F 4 F RT A20WE E24NE 20081001 NM 2008 10 1 2008UALA05554 1 20080831 A 2120 SENSOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 EQUIP COOLING CTRL R RIGHT ECC REPORTS FAILED FOR 10 SECONDS AND POWER IS AVAILABLE FOR THE ECC. STATUS MSG-2117112 INA CTV ER MODE, MSG-2117112 LATCHD ER MODE, MSG-2117132 LATCHED ER HARD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081001 2008 10 1 UPS08M53241 2 20080829 A 7200 UNKNOWN DOUG MD11 MD11F 3023600 NM UNKNOWN A IPXA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 SO 01 251UP 48744 ENG FLAME OUT - WHILE OPERATING FSC IN MANUAL WHILE IN CRUISE, NR 2 ENGINE FLAMED OUT. NR 2 FUEL BOOST PUMP SHUT OFF UN COMMANDED. RESTARTED ENGINE AND CONTINUED TO DESTINATION. REMOVED AND REPLACED FSC AFSC & ESCP IAW 28-08-01-2, 28-08-0 3-4 AND 28-08-02-2, RTS TEST C/O & ALL PASSED. ENG RUN IDLE POWER ACCOMPLISHED IAW AMM 71-00-00-5-1. FOUND ALL PARAMET ERS & BOOST PUMPS NORMAL. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 UPS08M53264 1 20080822 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:1C RT WING FIXED L/E TELESCOPE CUTOUT CRACKED ON INBOARD CORNER UPPER SURFACE. REMOVED DAMAGE, FABRICAT ED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG 43 SHEET 2, 51-33-01, 51-21-01. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 CALA0800847 1 20080902 A 3350 ADD71701100 BATTERY PACK BOEING 737 737824 13844BZ NM EMERGENCY LIGHT FAILED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 13248 28808 EMERGENCY BATTERY PACKS WON`T CHARGE ROW 19F, 19A, 11A, 11F, L2 DOOR GALLEY PER CHECK CARD 29-3350-1-7100. REPLACED BAT TERY PACKS PER CHECK CARD 29-3350-1-7100 ROW 19F, 19A, 11A, 11F, L2 DOOR GALLEY OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 ASAA0843456 1 20080824 A 5753 6546486149 SKIN BOEING 737 7374Q8 138447Q NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 778AS 25110 LEFT INBOARD MIDFLAP T/E WEDGE HAS DENTS NEXT TO A PREVIOUS REPAIR. REMOVED DAMAGE, FABBED FILLER AND DOUBLER, BONDED T HE REPAIR IAW B737 400 SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 ASAA0843458 1 20080823 A 5753 6546430129 SKIN BOEING 737 7374Q8 138447Q NM LT WING TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 778AS 25110 LEFT INBOARD FOREFLAP LOWER SURFACE HAS MULTIPLE SHARP DENTS. PREPPED DAMAGED AREA, FABBED DOUBLER AND BONDED REPAIR IA W B737 400 SRM 51-70-10 REPAIR 2. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 ASAA0843461 1 20080823 A 5754 65C26602311A SKIN BOEING 737 7374Q8 138447Q NM NR 2 SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 778AS 25110 NR 2 SLAT T/E LOWER SURFACE IS DELAMINATED AT OUTBOARD CORNER. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, INSTALL ED REPAIR IAW B737 400 SRM 51-70-10 FIG 4. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 ASAA0843464 1 20080824 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 7 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 778AS 25110 NR 7 SPOILER UPPER SURFACE HAS PROTRUDING DENT 5 INCHES AFT OF L/E. PREPPED DAMAGED AREA, FABBED DOUBLER AND INSTALLED THE REPAIR IAW 57-70-01. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 UPS08653343 1 20080914 A 5315 707500071IN STIFFENER BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 332UP 32843 INSPECTION TYPE:C MEC CABIN FLOORBEAM STA 246 LBL 20 VERT STIFFENER CRACK (CRACK LENGTH 1 INCH). VERT STIFFENER REPLACE D AS PER SRM 53-10-51-2R FIG 201 REPAIR 3. UPS MPI P19868 RAISED FOR REPEAT DVI AT 3000 CYCLES OR 24 MONTHS WHICHEVER C OMES FIRST. 2 L 7 2 4F RT A1NM 20081001 EU 2008 10 1 UPS08153337 1 20080916 A 3411 PITOT SYSTEM AIRBUS A300 A300F4622R 3930360 EU CAPTAINS CONTAMINATED A IPXA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 01 125UP 0809 INSPECTION TYPE:N/A RTO (X2) SPLIT BETWEEN CAPTAIN AND STANDBY AIRSPEED AFTER 1ST RTO. MX ACCOMPLISHED ADC TEST ON BOTH ADC'S & PITOT CK ON BOTH PITOT SYS PER AMM. DRIED WATER FOUND IN CAPT'S PITOT DRAIN. BOTH SYS CHECK NORMAL SPLIT WAS AT 100 & 80 KTS, A/C OOS FOR T/S AFTER 2ND RTO. ACCOMPLISHED ADC TEST ON NR 1 & 2 ADC'S PER M/M 34 18 00 00 BOTH CKS NO RMAL. T/S TO WATER & CAPT PITOT DRAIN. DRIED WATER, ACCOMPLISHED PITOT CHECK ON BOTH NR 1 & 2 PITOT SYSTEMS PER M/M 34 -10-00-05. BOTH WENT UP AND DOWN TOGETHER IN AIRSPEED. ACCOMP PITOT LEAK TEST AT 310 KTS PER M/M 34 10 00 05. NO LEAK S NOTED. ACCOMP AFS LAND TEST NO FAULT. 2 L 7 2 4F RT A35EU 20081001 NM 2008 10 1 SWAA085121 1 20080918 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 9L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 2008UALA05495 1 20080826 A 3350 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 539UA 25223 ENTIRE FIRST CLASS EMERGENCY LIGHTS INOP TO MID LAV. REPLACED DOOR 2R BATTERY. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 2008UALA05559 1 20080831 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 284 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 CABIN FLOORBEAM FRAME CORRODED STA 284 RBL 17. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION OF FLOORBEAM TEE AND FABRICATED A NEW TEE REPAIR ANGLE. DAMAGED T-CAP REMOVED BETWEEN RBL 17 - RBL 22 AND WL 208. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 UPS08553274 1 20080804 A 5320 ANGLE BOEING 757 75724APF 1384969 NM APU INLET DUCT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 453UP 25474 INSPECTION TYPE:C3 APU INLET HAS CORROSION EMINATING FROM NUT PLATES AT INLET PERIPHERY 148N3138-8000 WAS REPAIRED PER E O B757-5310-30434/ER 08-7685 AND THE 148N3138-2, -20 AND 148N3152-2 AND -1 WERE REPLACED PER ER 08-2685 AND SRM 51-40-02 -0G, 51-10-02-0G, 53-00-01-1A, 51-40-05-0G, 51-40-08-0G, 51-10-02, 51-20-01-0G, MM 49-15-06-4, 49-15-05-4, 49-15-08LH, 4 9-15-01-4, 49-61-14, AND SOPM 20-30-12. 2 L 7 2 4F RT A2NM 20081106 EU 2008 11 6 2008UALA06319 1 20081029 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 441UA 751 FOUND LIGHTNING STRIKE HOLE THROUGH SKIN ABOVE F/O STATIC PORT, REQUIRES PLUG REPAIR. STRINGER HAS DAMAGE WILL REQ REPL ACEMENT. 2 L 7 2 4F 4 F RT A28NM E40NE 20081106 EU 2008 11 6 2008UALA06320 1 20081029 A 2611 PPA120300 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 474UA 1475 SMOKE LAV & CARGO DET FAULT MESSAGE PRESENT ON UPPER ECAM BY. REPLACED DETECTOR 1WQ, VERIFIED NO FAULTS, OP CHECKS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20081106 NM 2008 11 6 2008UALA06321 1 20081030 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 120UA 29166 EMERGENCY LIGHT DOOR 1L ENTRY LIGHT INOP. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081106 WP 2008 11 6 08FDEA04654 1 20081031 A 5310 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP DOOR FRAME CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 46631 MAIN CARGO DOOR LOWER JAMB NR 3 FITTING HAS CORROSION IN HOLES "A" AND "D". REMOVED & REPLACED AFA 7132-1 FITTING & REP AIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00 FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 20081106 WP 2008 11 6 08FDEA04655 1 20081031 A 5320 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP NR 4 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 46631 MAIN CARGO DOOR LOWER JAMB NR 4 FITTING HAS CORROSION IN HOLES "A"; "B" AND "D". REMOVED & REPLACED AFA 7132-1 FITTING & REPAIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00 FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 20081106 WP 2008 11 6 08FDEA04656 1 20081031 A 5320 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP NR 5 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 46631 MAIN CARGO DOOR LOWER JAMB NR 5 FITTING HAS CORROSION IN HOLES "C" AND "D". REMOVED & REPLACED AFA 7132-1 FITTING & RE PAIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00 FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 20081106 WP 2008 11 6 08FDEA04657 1 20081031 A 5320 AFA71321 FITTING DOUG MD10 MD1010F 3022112 WP NR 6 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 46631 MAIN CARGO DOOR LOWER JAMB NR 6 FITTING HAS CORROSION IN HOLES "A"; "B"; "C" AND "D". REMOVED & REPLACED AFA 7132-1 F ITTING & REPAIRED THE LOWER JAMB IN REF TO DC/MD-10 SRM 53-50-00; FIG 17 VOL I & DC/MD-10 SRM 51-33-01 VOL II. 2 L 7 3 4F RT A22WE 20081106 NM 2008 11 6 USAA920081978 1 20081023 A 5311 65C32351 FRAME BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03C20853011/017 AND 03C20853011/016 FRAME STIFFENER CRACKED AT BS 500E BETWEEN S20L - S21L AND S2 0R - S21R. REPAIRED FRAME STIFFENER AT BS 500E BETWEEN S20L - S21L AND S20R - S21R IAW B737 SRM 53-00-07 REPAIR 13. 2 L 7 2 4F RT A16WE 20081106 SO 2008 11 6 C2XA08IA234 1 20081104 A 4940 23080013A STARTER GEN EMB 145 EMB145XR 3260214 SO APU MALFUNCTIONED A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 12201 6570 169 14500959 IAH - FLIGHT 3020, THE CREW REPORTED A BURNING SMELL AFTER THE APU START. THE APU THEN FAILED AND WOULD NOT RESTART. T HE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE PLACED THE APU ON MEL 49-00-00 CAT - C CTL NUMBER 157685, AND THE AIR CRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT RETURNED TO IAH ON 11/04/08 WHERE MAINTENANCE REMOVED AND REPLAC ED THE APU STARTER GENERATOR, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081106 SO 2008 11 6 C2XA08IA235 1 20081104 A 2530 500064001 COFFEEMAKER EMB 145 EMB145XR 3260214 SO GALLEY SMOKE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14153 145761 IAH - FLIGHT 2459 THE CREW REPORTED THAT THE NUMBER ONE COFFEEMAKER SMOKES WHEN TURNED ON. MAINTENANCE INSPECTED THE AI RCRAFT AND PLACED THE NUMBER ONE COFFEEMAKER ON NEF GL-01 CAT D CTL 157681, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SDR FILED OPEN AWAITING FINAL COPRRECTIVE ACTION. 2 L 7 2 4F RT 20081106 NM 2008 11 6 F3LA2008110300707 1 20081101 A 5320 D53480043204 SILL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 932FR 18 2258 DURING C3 C-CHECK, INSPECTION NOTED L2 DOOR SILL, AFT OF GIRT BAR FITTING, AFT OUTBOARD NUT PLATE HOLE HAS SIGNS OF CORR OSION. MAINTENANCE REMOVED NUT PLATE IN ACCORDANCE WITH A319 SRM 51-42-11, ENLARGED HOLE TO CLEAN CORROSION, PRIMED AND PAINTED IN ACCORDANCE WITH A319 SRM 51-75-12 AND ENGINEERING AUTHORIZATION A9-53R-30723. 2 L 7 2 4F RT A28NM 20081106 NM 2008 11 6 HALA200811020083 1 20081102 A 2612 FIRE WARNING BOEING 767 7673G5 1385126 NM COCKPIT MALFUNCTIONED A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM - APU FIRE LOOP 1 ON STATUS PAGE. TESTED APU FIRE LOOP SYSTEM PER FIM 26-15-00 / 101 FIG 104. NO FAULTS NOTED. MESSAGE CLEARED. 2 L 7 2 4F RT A1NM 20081106 NM 2008 11 6 KCSA081558 1 20081105 A 5320 STIFFENER BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 STA 2120 AT RBL 48 STIFFENER CRACKED ONE INCH ON AFT SIDE OF FRAME. 2 L 7 4 4F RT A20WE 20081106 NM 2008 11 6 KCSA081560 1 20081105 A 5320 FITTING BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 STA 2360 LOWER FORWARD CHORD BATHTUB FITTING CORRODED AT STR 40L. 2 L 7 4 4F RT A20WE 20081106 NM 2008 11 6 QXEA2008110401158 1 20081030 A 2910 82920010307 HYDRAULIC LINE DHAV DHC8 DHC8202 2809007 NM HYDRAULIC SYS FAILED A QXEA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 NM 19 349PH 486 PDX - ON DOING DAILY CHECKS, PERFORMED PTU TEST AND LOST ALL HYD ON THE NR 2 SYSTEM. HYDRAULIC FLUID IS ALL OVER ROWS 3 /4/5 SEATS. ENGINE SHUTDOWN WITH IN 1 MIN. REPLACED CRACKED NOSE GEAR DOWN LINE, CHECK GOOD. PERFORMED EDP HYD FLUID LOSS INSP IAW MM 05-50-33-280-801, NO DEFECTS. CLEANED AIRCRAFT AND INSTALLED NEW SEAT COVERS, OVERHEAD BINS, PSU'S, AN D OTHER INTERIOR EQUIPMENT AS REQUIRED. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081106 NM 2008 11 6 QXEA2008110401159 1 20081101 A 5240 85217752002 FASTENER BOMBDR DHC8 DHC8402 1390042 NM R2 DOOR BROKEN A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 19 400QX 4030 SEA - F/A REPORTS UNABLE TO OPEN R2 DOOR. REPLACED MISSING & BROKEN HARDWARE ON GUIDE ROLLER LATCH ASSEMBLIES AS NEEDED . TIGHTENED LOOSE HARDWARE ON LATCH ASSEMBLIES. MAINTENANCE HAD NO AFFECT ON RIG OF LATCHING ASSEMBLIES. R2 DOOR OP'S CHECK GOOD. A/C OK FOR CONTINUED SERVICE. 2 H 7 2 4T RT A13NM 20081106 EA 2008 11 6 QXEA2008110401054 1 20080923 A 2752 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA TE FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 611QX 10041 PDX - C4 - LT INBOARD FLAP OUTBOARD MIDDLE VANE ACTUATOR IS WORN ON THE SHAFT AT 3 PLACES (UPPER) SURFACE APPROX .400"L X .300W X .002 DEEP. MAPPED AREA FOR ENGINEERING. REMOVED DAMAGE FROM AFFECTED AREA PER REO 670-57-52-116 SHEET 3 STEP 1. FPI BLENDED AREA FOR CRACKS IAW CRJ NDTM PART 1, 51-20-008 AND HORIZON AIR NDTM SEC 8, NO CRACKS NOTED. COMPLETED REO 670-57-52-116 BY C/W STEP 4. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 QXEA2008110401055 1 20080923 A 2752 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA TE FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 611QX 10041 PDX - C4 - LT INBOARD FLAP INBOARD-MIDDLE VANE ACTUATOR IS WORN ON THE SHAFT AT 2 PLACES (LOWER) SURFACE APPROX .050"L X .200"W X .002" DEEP. MAPPED AREA FOR ENGINEERING. REMOVED DAMAGE FROM AFFECTED AREA PER REO 670-57-52-116 SHEET 3 STE P 1. FPI BLENDED AREA FOR CRACKS IAW CRJ 700 NDTM PART 1, 51-20-008 AND HORIZON AIR NDTM SEC 8, NO CRACKS NOTED. COMPL ETED REO 670-57-52-116 BY C/W STEP 4. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 QXEA2008110401060 1 20080923 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 611QX 10041 PDX - C4 - CORROSION AT RT LOWER BULKHEAD AT FS 280 RBL 9 TO RBL 18. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS PER R EO 670-53-11-052. REMOVED RT LOWER WEB PER REO 670-53-11-05 REPAIR NR 2, DRILLED AND DEBURRED NEW WEB REF REO 670-53-11 -05 REPAIR NR 2. INSTALLED LOWER WEB IAW REO 670-53-11-052. INSTALLED UPPER WEB IAW CRJ700 SRM 51-42-06, 51-42-13 AND REO 670-53-11-052. INSTALLED SPLICE STRAP REF REO 670-53-11-052 AND CRJ 700 SRM 51-42-06 AND 51-42-13. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 QXEA2008110401056 1 20080923 A 2752 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA TE FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 611QX 10041 PDX -C4 - LT INBOARD FLAP, INBOARD VANE ACTUATOR IS WORN ON THE SHAFT AT 2 PLACES (LOWER) SURFACE APPROX .050"L X .200"W X .002" DEEP. MAPPED AREA FOR ENGINEERING. REMOVED DAMAGE FROM AFFECTED AREA PER REO 670-57-52-116 SHEET 3 STEP 1. F PI BLENDED AREA FOR CRACKS IAW CRJ 700 PART 1, 51-20-008 AND HORIZON AIR NDTM SEC 8, NO CRACKS NOTED. COMPLETED REO 670- 57-52-116 BY C/W STEP 4. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 QXEA2008110401057 1 20080923 A 2752 ACTUATOR CNDAIR CL600 CL6002C10 1390015 EA TE FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 611QX 10041 PDX - C4 - RT WING I/B FLAP I/B VANE ACTUATOR SHAFT HAS CHAFING ON UPPER SURFACE. MAPPED AREA FOR ENGINEERING, REMOVED DAMAGE FROM SHAFT REF REO 670-57-52-116 STEP 1. FPI BLENDED AREA FOR CRACKS IAW CRJ 700 NDTM PART 1, 51-20-008 AND HORI ZON AIR NDTM SEC 8, NO CRACKS NOTED. COMPLETED REO 670-57-52-116 BY COMPLETING STEP 4. 2 L 7 2 4F RT A21EA 20081106 NM 2008 11 6 QXEA2008110501128 1 20081018 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 418QX 4143 PDX -C1-POSSIBLE LIGHTNING STRIKE DAMAGE ON UPPER FUSELAGE AT APPROX STA X13.0 LEFT OF STR 1 ON TOP OF DOUBLER. REMOVED RIVET BY DRILLING, ENLARGED HOLE AND COUNTERSINK TO REMOVE DAMAGE TO SKIN REF RD8/4-53-1039. HFEC AREA IAW Q400 NDTM P ART 6, 51-00-01, NO CRACKS NOTED. INSTALL SOLID RIVET IAW SRM 51-42-05. PRIMED AND PAINTED REF Q400 SRM 51-25-05. 2 H 7 2 4T RT A13NM 20081106 NM 2008 11 6 QXEA2008110501129 1 20081018 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 418QX 4143 PDX - C1- POSSIBLE LIGHTNING STRIKE DAMAGE ON UPPER FUSELAGE AT APPROX STA 71.5, 5.5 INCHES LEFT OF STRINGER NR 1. DRI LLED OUT RIVET THAT WAS DAMAGED AND COUNTERSUNK TO REMOVE DAMAGE IAW Q400 RD 8/4-53-1039. HFEC AREA IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. INSTALLED SOLID RIVET IAW SRM 51-42-05, PRIMED AND PAINTED REF SRM 51-25-05. 2 H 7 2 4T RT A13NM 20081106 EA 2008 11 6 SWIA200820267 1 20081029 A 2611 SMOKE WARNING CNDAIR CL600 CL6002B19 1900309 EA LAVATORY ACTIVATED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 909SW 7558 ON CLIMB, SMOKE TOILET CAUTION MESSAGE APPEARED FOR 2-3 MINUTES (FLT 6664). ACCOMPLISHED ENGINE GROUND RUNS WITH BOTH P ACKS RUNNING. NO SMOKE MESSAGES, NO SMOKE IN LAVATORY. 2 L 7 2 4F RT A21EA 20081105 WP 2008 11 5 08FDEA04688 1 20081103 A 5414 NTL6012507 SKIN DOUG MD10 MD1010F 3022112 WP NR 2 NACELLE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 NR 2 ENGINE FAN COWL EXTERIOR SURFACE DENTED APPROX 10 INCH FROM THE L/E; 3' FROM THE TOP. EVAULATED THE DENT AND FOUND TO BE OUT OF LIMITS IAW SRM 51-80-01. DENTED AREA IS DELAMINATED. REPAIRED DELAMINATED AREA BY REMOVING DAMAGE, FABRI CATED DETAILS, PREPPED AND CLEANED FOR BOND, LAYED UP, VAC BAGGED CURED REPAIR, SANDED FLUSH, ALODINED, SEALED, PRIMED AND PAINTED REPAIR AREA IAW SRM 54-00-01, 51-71-00 AND SRM 54-32-01. 2 L 7 3 4F RT A22WE 20081105 NM 2008 11 5 08FDEA04689 1 20081103 A 5720 652165823 CHANNEL BOEING 727 7272D4 138407U NM ZONE 600 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 RT WING TE FLAP WELL LOWER FIXED PANEL CHANNEL IS CRACKED AT DIAGONAL STRUT ATTACHMENT WS 521 REMOVED CHANNEL REF SRM 51-30-02. FORMED NEW CHANNEL REF DWG 65-21658 ITEM 23. INSTALLED NEW CHANNEL REF SRM 51-30-02, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081105 NM 2008 11 5 SWAA085967 1 20081030 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085968 1 20081030 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085969 1 20081030 A 5311 6546554 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 847, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085925 1 20081030 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085970 1 20081030 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085971 1 20081030 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085972 1 20081030 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SLAT UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085973 1 20081030 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085978 1 20081030 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085979 1 20081030 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085926 1 20081030 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 SWAA085927 1 20081030 A 5315 BAC1609100688 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 DURING SCHEDULED 6Y CHECK, FOUND FLOORBEAM CORRODED AT BS 770, LBL 12. REPAIRED BEAM PER AAR EA. 2 L 7 2 4F RT A16WE 20081105 NM 2008 11 5 08FDEA04662 1 20081101 A 5320 65242972 FLANGE BOEING 727 7272S2F 1384O81 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 MAIN DECK FLOOR E/E RACK STANTION SUPPORT INTERCOSTAL VERT FLANGE IS CRACKED BS 371 RBL 2 WL 199. REMOVED ANGLE VERIFIE D MATERIAL ID FABRICATED NEW ANGLE INSTALLED NEW ANGLE AND WIRE BUNDLE CLAMP, REF SRM 51-30-2 PG 2, REF DWR 65-24297, RE F MM 51-20-151 PG 1- 6, REF SRM 51-30-2 PG 8, 13-14. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081105 NM 2008 11 5 08FDEA04663 1 20081101 A 5320 6526173 INTERCOSTAL BOEING 727 7272S2F 1384O81 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 MAIN DECK FLOOR INTERCOSTAL IS CORRODED BS 312-328, LBL 30, WL 208. REMOVED CORROSION AND INTERCOSTAL AT STA 312 ORIGIN AL THICKNESS .075 MATERIAL LOSS .025 REMAINING MATERIAL .050, FOUND OUT OF LIMITS. FABRICATED NEW INTERCOSTAL, INSTALLE D NEW INTERCOSTAL AND SHIM REF BOEING DWR 65-26173, SRM 51-30-2 PG 1-3. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 DHLA2008745590 1 20081014 A 5322 SHEAR TIE BOEING 727 727224 1384076 NM ZONE 100 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT SHEAR TIE WITH CRACK AT BS 540 BETWEEN S25R AND S26R. REPLACED FUSELAGE SHEAR TIE SECTION AT BS 540 BETWEEN S25R AND S26R IAW SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081106 NM 2008 11 6 DHLA2008745601 1 20081010 A 5313 STRINGER BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 680 S-28L WITH IMPROPER SPLICE. REPLACED FUSELAGE STRINGER SECTION AT BS 683 TO BS 720+4 S-28L AND REPLACED SPLICE SECTION FROM BS 673.5 TO BS 688 DUE TO IMPROPER SPLICE IAW SRM 51-10-1 PARA 7A AN D IAW SRM 51-30-2 PARA 4B AND PARA 7D. 2 L 7 3 4F A3WE 20081106 2008 11 6 AALA200802671 4 20081003 A 3422 GYRO DOUG DC9 DC982 3022082 WP NR 1 MALFUNCTIONED A AALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SW 21 420AA 49332 DFW - HEADING FLAG CAME ON AFTER TAKEOFF AND NUMBER ON COMPASS DRIFTED OFF 45 DEGREES. AUTOPILOT FAILED. BOTH FLIGHT D IRECTORS FAILED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE DIRECTIONAL GYRO. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081106 NM 2008 11 6 CALA0801025 1 20081103 A 5315 141T5146 STIFFENER BOEING 767 767424ER 1385270 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76054 29449 BODY STATION 246 FLOORBEAM FORWARD SIDE, ONE STIFFENER FOUND CRACKED AT LBL 40. BODY STATION 246 FLOORBEAM FORWARD SIDE ONE STIFFENER LBL 40 REPAIRED PER ECRA 5310-04859, HFEC NO CRACK FOUND. ITEM 1-9 ACCOMPLISHED. ISSUED DIP TO PERFORM A DETAILED INSPECTION PER PART 2 OF ECRA 5310-04859 AT 246 AT OR BEFORE 3000 CYCLES FROM 10/30/08, ACCOMPLISH A PERMANEN T REPAIR PER PART 3 AT THE NEXT 8C-CHECK, 48,000 FLIGHT HOURS, 24,000 CYCLES OR 144-MONTHS WHICHEVER OCCURS FIRST. 2 L 7 2 4F RT A1NM 20081106 NM 2008 11 6 KCSA081542 1 20081103 A 5320 FITTING BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 STA 2360 BATHTUB FITTING AT STR 50L IS CORRODED. 2 L 7 4 4F RT A20WE 20081106 NM 2008 11 6 2008UALA06314 1 20081029 A 3350 582233 BATTERY BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 SEAT EEL INOP, ROWS 32, 33, 34 RT. REPLACED BATTERY. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081106 NM 2008 11 6 2008UALA06316 1 20081029 A 3350 582233 BATTERY BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY EXIT SIGN INOP, DOOR 3 RT AFT SIDE. REPLACED BATTERY. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081106 NM 2008 11 6 2008UALA06317 1 20081029 A 3350 582233 BATTERY BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 FLOOR EEL INOP, BETWEEN MID LAVS 111 & 112. REPLACED BATTERY. OPS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081106 NM 2008 11 6 2008UALA06323 1 20081030 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 670UA 29240 THE 6B EMERGENCY EXIT LIGHT BROKEN OFF. FWD SEAT MOUNTED ELECTRO LUMINESCENT LIGHT STRIP BROKEN OFF. ALL ADJACENT LIGH TS OPERATIVE. SEAT LOCATION 6B. REPLACED LIGHT ASSY SAFETY, SECURITY AND OPERATION OF LIGHT STRIP 10B OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081106 NM 2008 11 6 2008UALA06326 1 20081030 A 5315 FLOORBEAM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 CABIN STA 365, RBL 45 FLOOR SUPPORT BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION. FABRICATED & INSTALL ED DOUBLER AND SHIM REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081106 NM 2008 11 6 2008UALA06328 1 20081031 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 DOOR 4R SILL LIGHT INOP. RELAMPED DOOR SILL LIGHT, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081106 NM 2008 11 6 2008UALA06329 1 20081031 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 AFT GALLEY 2 LEFT SIDEWALL EEL LIGHTS INOP. FEEDER FOUND DEFECTIVE. REPLACED FEEDER CABLE. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081106 NM 2008 11 6 2008UALA06330 1 20081030 A 8012 35054367 START VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE RT ENGINE FAULTY A UALA D RETURN TO BLOCK W INADEQUATE Q C IN INSP/MAINT 1 WP 29 670UA 29240 STARTER VALVE DID NOT OPEN ON RIGHT ENGINE DURING START. FOUND FAULTY START VALVE. REPLACED NR 2 ENG START VALVE & STA RTER. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081106 NM 2008 11 6 2008UALA06331 1 20081029 A 5230 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FWD CARGO DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 FWD CARGO PIT DOOR SKIN AFT LWR CORNER IS CRACKED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF SKIN. INSTAL LED DOUBLER & FILLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081106 NM 2008 11 6 USAABB08165 1 20081101 A 3350 BPS73 BATTERY PACK BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 915AW 22209 PHX - THE EMERGENCY EXIT LIGHT AT THE L3 DOOR WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE MID, AFT, LEFT BATTERY PA CK ASSEMBLY. OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A2NM 20081106 NM 2008 11 6 F3LA2008110300701 1 20081031 A 5315 D53472090010 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 932FR 18 2258 DURING C3 C-CHECK, INSPECTION NOTED LONGERON Y1292 BETWEEN FRAME 66 AND FRAME 68 HAS CORROSION IN NUMEROUS NUT CLIP HOLE S. MAINTENANCE REWORKED 4 HOLES TO REMOVE ALL CORROSION IN ACCORDANCE WITH A319 SRM 53-00-14 FIGURE 102. ROTO-PROBED H OLES WITH NO DEFECTS NOTED. TREATED, PRIMED AND PAINTED IN ACCORDANCE WITH ENGINEERING AUTHORIZATIONS A9-53R-30730 AND A9-53R-30731. 2 L 7 2 4F RT A28NM 20081106 NM 2008 11 6 F3LA2008110300705 1 20081101 A 5321 D5367180500400 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 932FR 18 2258 DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 261FF HAS CORROSION ON THE LOWER SURFACE. MAINTENANCE REPLACED FLOOR PA NEL WITH NEW IN ACCORDANCE WITH A319 AMM 53-42-12-400-002. 2 L 7 2 4F RT A28NM 20081106 NM 2008 11 6 F3LA2008110300706 1 20081101 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CABIN CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 932FR 18 2258 DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 262FF HAS CORROSION ON THE LOWER SURFACE. MAINTENANCE REPLACED FLOOR PA NEL WITH NEW IN ACCORDANCE WITH A319 AMM 53-42-12-400-002. 2 L 7 2 4F RT A28NM 20081106 EA 2008 11 6 SWIA200820266 1 20080707 A 5320 TIE CLIP CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 915SW 7615 FS 484 LT BL 36 TIE CLIP CRACKED (C-CHECK). REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 SWIA200820276 1 20081031 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA NLG FAULTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 701SK 10133 NOSE DOOR OPEN WARNING MESSAGE AND PROX SYSTEM 1 FAULT AFTER TAKEOFF (FLT 5942). REPLACED PROX SENSOR PX30. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 SWIA200820277 1 20081029 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 948SW 7789 CABIN EMERGENCY LIGHT INOP (FLT 6664). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 SWIA200820280 1 20081027 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST NR NOT REPORTED 1 NM 07 943SW 7762 FORWARD OVERHEAD EMERGENCY EXIT LIGHT NOT WORKING (FLT 6039). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 SWIA200820281 1 20081029 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 910SW 7566 NR 3 CEILING LEVEL EMERGENCY FLOOD LIGHT INOP (FLT 6043). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081106 WP 2008 11 6 UPS08853831 1 20081020 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV LT WING CENTER L/E UPPER AFT EDGE HAS A STEEL REPAIR DOUBLER INSTALLED AT STA XFS 396-404. INSTALLED CONICAL WASHER REPAIR DOUBLER AND FILLER 4 EA IAW DC8 SRM 57-2-1 REV 78. 2 L 7 4 4F RT 4A25 20081106 WP 2008 11 6 UPS08853832 1 20081024 A 5753 SKIN DOUG DC8 DC871F 302199D WP TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV APPENDIX D SURVEY SEQ 715-W4-03 EXTERNAL DOUBLER AT STA XF 240 RT WING FLAP UPPER SURFACE IS GOUGED. INSTALLED DOUBLER IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 20081106 WP 2008 11 6 UPS08853833 1 20081024 A 5753 DOUBLER DOUG DC8 DC871F 302199D WP TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV APPENDIX D SURVEY SEQUENCE 715-W4-02 EXTERNAL DOUBLER ON RT WING FLAP UPPER SURFACE AT STA XF 255 IS GOUGED. INSTALLED DOUBLER IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 20081106 EU 2008 11 6 QMLA1028200808046 1 20081028 A 2120 UNKNOWN SNIAS 350 AS350B2 8680813 EU CABIN ODOR E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 97LG 2917 ABOUT TWO MINUTES AFTER TAKEOFF, THE FLIGHT NURSE REPORTED SMELLING SOMETHING. MOMENTS LATER THE PILOT SMELLED SOMETHIN G LIKE BURNING RUBBER COMING OUT OF THE VENTS. TURNED BACK AND LANDED AT HOSPITAL. PATIENT WAS TRANSPORTED BY ANOTHER HELICOPTER. THE MECHANIC AND PILOT MADE A THOROUGH CHECK, AND A MAINTENANCE FLIGHT, FOUND NOTHING UNUSUAL. ON THE MAIN TENANCE FLIGHT INTO THE SAME AREA AN ODOR OF BURNING GARBAGE WAS NOTICED BY PILOT. 1 G 7 1 3U H9EU 20081106 WP 2008 11 6 UPS08853842 1 20081024 A 5730 FASTENER DOUG DC8 DC871F 302199D WP RT WING IMPROPER PART A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SVN/ SEQ 715-W4-100 RIGHT WING STA XRS 366.300 UPPER LEADING EDGE DOUBLER HAS BLIND FASTENERS NOT CALLED OUT IN SRM. REPLACED FASTENERS AS IAW 57-02-01 FIG 38. 2 L 7 4 4F RT 4A25 20081106 WP 2008 11 6 UPS08853848 1 20081020 A 3350 601233 BATTERY PACK DOUG DC8 DC873F 302199F WP COCKPIT UNSERVICEABLE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:N/A EMERGENCY LIGHTS UNSERVICEABLE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ASSY IAW AMM 33-5 0-01-02 AND FOUND SERVICEABLE. 2 L 7 4 4F RT 4A25 20081106 NM 2008 11 6 UPS08M53828 1 20081030 A 5210 SKIN DOUG MD11 MD11F 3023600 NM L1 DOOR BENT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 L1 DOOR FWD UPPER CORNER SKIN IS BENT. MAJOR REPAIR - REPAIR DOUBLER INSTALLED REF EO 5210-31026-A. REMOVED DAMAGE PER SRM 52-10-00 VOL 1 FIG 10. PERFORMED HFEC ON AREAS NO CRACKS NOTED. COMPLETED FABRICATION OF SKIN FILLER & REPAIR DOUBL ER REF EO MD11-5210-31026. COMPLETED INSTALL OF REPAIR REF MD11-5210-31026. 2 L 7 3 4F RT A22WE 20081106 EA 2008 11 6 ASOA200801439 1 20081102 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 718EV 10095 F/A ADVISES THE OPEN EXIT STICKERS ON MAIN CABIN DOOR NEED REPLACING. 2 L 7 2 4F RT A21EA 20081106 EA 2008 11 6 ASOA200801423 1 20081029 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 933EV 8022 LT AND RT FS 621.00 TO 625.00 OBLIQUE ANGLES IN AFT EQUIPMENT COMPARTMENT ARE CRACKED 2 INCHES LONG ON AFT RADIUS. 2 L 7 2 4F RT A21EA 20081107 NM 2008 11 7 AALA200802678 1 20081004 A 3350 SHROUD BOEING 737 737823 13844BZ NM LIGHT ASSEMBLY BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 946AN 30600 DFW - EMERGENCY LIGHT AT SEAT ROW 15DEF HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 15DEF. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 AALA200802679 1 20081004 A 3350 SHROUD BOEING 737 737823 13844BZ NM LIGHT ASSEMBLY BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 946AN 30600 DFW - EMERGENCY LIGHT AT SEAT ROW 16DEF HAS BROKEN SHROUD. REPLACED SHROUD AT SEAT ROW 16DEF. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 AALA200802680 1 20081004 A 3350 SHROUD BOEING 737 737823 13844BZ NM LIGHT ASSEMBLY BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 946AN 30600 DFW - EMERGENCY LIGHT AT SEAT ROW 22DEF HAS BROKEN SHROUD. REPLACED SHROUD AT SEAT ROW 22DEF. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A16WE 20081107 WP 2008 11 7 AALA200802682 1 20081005 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAILCONE BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 498AA 49736 DFW - EMERGENCY LIGHT AT OVERHEAD TAIL CONE HAS BROKEN TWIST LOCK TERMINAL WIRE L795ZD14. REPLACED TWIST LOCK TERMINAL WIRE AT OVERHEAD TAIL CONE AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081107 WP 2008 11 7 AALA200802676 1 20081003 A 3350 SHROUD DOUG DC9 DC982 3022082 WP LIGHT ASSEMBLY BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 466AA 49596 DFW - EMERGENCY LIGHT AT SEAT ROW 12DEF HAS BROKEN SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 12DEF. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081105 NM 2008 11 5 2008UALA05862 1 20080923 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN SHORTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 AFT CEILING LIGHT IN AFT AUX GALLEY SHORTED OUT CAUSING BURN MARKS ON CEILING. LIGHT SHORTED OUT. REPLACED LIGHT ASSY. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081106 NM 2008 11 6 DHLA2008745596 1 20080907 A 5322 SHEAR TIE BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT BS 720A BETWEEN S-25L AND S-26L SHEAR TIE WITH CORROSION. REPLACED FUSELAGE SHEAR TIE SECTION AT BS 720A BETWEEN S-25L AND S-26L IAW B727SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081106 WP 2008 11 6 AALA200802657 1 20081002 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 588AA 53251 MIA - EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A6WE 20081106 NM 2008 11 6 DHLA2008745586 1 20080902 A 5330 SKIN BOEING 727 727224 1384076 NM ZONE 200 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LOWER FUSELAGE AT BS 357 BETWEEN S-17L AND S-18L. REPAIRED FUSELAGE SKIN SECTION FROM BS 351 TO BS 360 BETWEEN S-16L AN D S-18L DUE TO DENT IAW COOPESA EO COO-2-53-271-08 DTD 9/12/08 DOCUMENTED ON FAA FORM 8110-3. 2 L 7 3 4F A3WE 20081106 WP 2008 11 6 AALA200802660 1 20081002 A 3350 60030451 BATTERY DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 262AA 49290 LGA - EMERGENCY LIGHTS AT OVERHEAD SEATS 28B, 30B, 30D, AND OVER GANTRY STEPS INOPERATIVE. SECURED LOOSE BATTERIES IN E MERGENCY BATTERY PACK AT SEAT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081106 NM 2008 11 6 CALA0801019 1 20081030 A 5315 141T5108 FLOORBEAM BOEING 767 767424ER 1385270 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76054 29449 BODYSTATION 325 LBL 10 LBL 60 FLOOR SUPPORT FOUND CORRODED AFT FLOOR PANEL REMOVED. BODYSTATION 325 LBL 10 LBL 60 FLOOR BEAM UPPER CHORD REPAIRED PER SRM 53-00-51 REPAIR 1 FIG 201. HFEC NO CRACK FOUND. 2 L 7 2 4F RT A1NM 20081106 NM 2008 11 6 KCSA081553 1 20081103 A 5320 FITTING BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 STA 2360 BATHTUB FITTING AT STR 48L CORRODED. 2 L 7 4 4F RT A20WE 20081106 NM 2008 11 6 QXEA2008110501138 1 20081018 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 418QX 4143 PDX - C1 - FWD FUSELAGE EXTERIOR ROOF SKIN HAS LIGHTNING STRIKE AT RIVET EDGE AND SKIN AT APPROX FS X38.000 AND STR LT 6 . DRILLED OUT RIVET, ENLARGED COUNTERSINK TO REMOVE DAMAGE FROM SKIN REF RD 8/4-53-1039. HFEC AROUND FASTENER FOR CRAC KS IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. INSTALLED SOLID RIVET IAW SRM 51-42-05. PRIMED AND PAINTED REF Q4 00 SRM 51-25-05. 2 H 7 2 4T RT A13NM 20081106 NM 2008 11 6 QXEA200801063 1 20081003 A 5310 BLOWOUT PANEL BOMBDR DHC8 DHC8402 1390042 NM BULKHEAD DISLODGED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 19 424QX 4006 LOSS OF CABIN PRESSURIZATION AT FL240. STARTED WORKING AGAIN AFTER RUNNING THROUGH THE CHECKLIST. CREW USED OXYGEN AND A CCOMPLISHED AN UNEVENTFUL LANDING. NO PASSENGER ISSUES. FERRY FOR REPAIRS. INSPECTED AFT BAG PIT DOOR SEAL. CHECKS OK, F OUND CANTED BULKHEAD BLOW OUT PANEL NOT SEATED IN OPENING, RESECURED BLOW-OUT PANEL IN SPRING LATCHES. CHECKS OK. RETURN ED TO SERVICE. NO PARTS REPLACED. (K) 2 H 7 2 4T RT A13NM 20081106 SO 2008 11 6 FDK2008F00012 1 20080927 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DIRTY A FDKA K NONE O OTHER IN INSP/MAINT 1 SW 07 825MJ 145179 GALLEY EMERGENCY LIGHTS INOPERATIVE. MX CLEANED THE CONNECTOR. OPS CHECKED GOOD. (K) 2 L 7 2 4T RT T00011AT 20081106 NM 2008 11 6 QXEA200801050 1 20081001 A 2620 4739511 EXTINGUISHER BOMBDR DHC8 DHC8402 1390042 NM APU BAY LOW A QXEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 19 413QX 4060 INTERMITTENT MASTER WARNING ALONG WITH CHECK FIRE DETECTOR AND APU BLT LOW LIGHT IN OVERHEAD PANEL. REMOVED AND REPLACED APU FIRE EXTINGUISHING BOTTLE IAW DHC-8/400 AMM 26-23-01-000-801/ 400/801. OPERATIONAL CHECK GOOD IAW 26-13-00-710-801. (K) 2 H 7 2 4T RT A13NM 20081106 2008 11 6 SWAA085986 4 20081031 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 FOUND R2 DOOR EMERGENCY EXIT SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081106 SO 2008 11 6 C2XA08SH134 1 20081105 A 5512 14532235401 RIVET EMB 145 EMB145LR 3260212 SO HORIZ STAB CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14952 145067 DURING C-CK LT HORIZONTAL STAB L/E HAS NUMEROUS RIVETS WITH CORROSION UPPER AND LOWER SURFACE. MX REMOVED AND REPLACED AFFECTED RIVETS ON LT HORIZONTAL STAB L/E UPPER AND LOWER SURFACE IAW EC5510-01192. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 20081106 NM 2008 11 6 F3LA2008110300704 1 20081030 A 5315 D53472090010 FLOORBEAM AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 932FR 18 2258 DURING C3 C-CHECK, INSPECTION NOTED LONGERON -Y1292 BETWEEN FRAME 66 AND FRAME 68 HAS CORROSION ON NUMEROUS NUT CLIP HOL ES. MAINTENANCE REMOVED DAMAGED BEAM IN ACCORDANCE WITH A319 SRM 51-42-11 PARAGRAPHS 6 AND 7. MAINTENANCE INSTALLED NE W FLOORBEAM IN ACCORDANCE WITH A319 SRM 51-42-11 PARAGRAPH 5. 2 L 7 2 4F RT A28NM 20081106 NM 2008 11 6 QXEA200801009 1 20080912 A 5330 DOUBLER BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 413QX 4060 CHAFE DAMAGE ON INTERNAL DOUBLER AT AFT SIDE OF TOILET SERVICE ACCESS DOOR 4.5 INCH DOWN FROM TOP AFT EDGE OF INTERNAL D OUBLER. BLENDED AREA OF CHAFE REF Q400, SRM 51-14-00, METHOD 4, PG 203. INSP IAW D8 Q400 NDTM PART 6, 51-00-01 NO CRACK S NOTED. UT THICKNESS CHECK IAW D8 Q400 NDTM PART 1,51-00-04, HI .080 INCH LO .078 INCH. CHAFE WITHIN LIMITS IAW RD8/4-5 3-347. ALODINED PRIMED AND PAINTED REF Q400 SRM 51-21-10, 51-25-10, AND 51-25-15. (K) 2 H 7 2 4T RT A13NM 20081106 SO 2008 11 6 RTA2008F00000 2 20081022 A 7414 BRUSHES CIRRUS SR SR20 05628AJ GL CONT O360 IO360ES SO HARTZL HCJ3Y PHCJ3YF1 GL MAGNETO FAILED E RTAA K NONE O OTHER IN INSP/MAINT 1 SW 11 431SR 389 0608208 1754 360271 FP5130B DURING ROUTINE INSPECTION, LT MAGNETO WOULD NOT TIME, REMOVED, OPENED TO CHECK POINTS, FOUND SEVERE ARCHING FROM BRUSH T O THE POINT OF BEARING BAR FAILURE. SN FROM BOTH MAGNETOS AFFECTED BY SB3-08A, BOTH MAGNETOS FAILED INSP AND REPLACED. D OWN SIDE, REPLACEMENT (NEW) MAGNETOS ARE STILL AFFECTED, REQUIRING INSPECTION WITHIN 25 HRS. (K) 1 L 7 1 3O 3 O NT A00009CH E1CE 5 C P36EA 20081106 2008 11 6 QMLA1101200808048 4 20081101 A 2210 117884141 COMPUTER BOLKMS 117 BK117A4 5626017 EU AUTOPILOT SYS INTERMITTENT E QMLA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 03 68AM 7111 PILOT REPORT - DURING A FLIGHT TO SAINT FRANCIS HOSPITAL, THE AIRCRAFT BEGAN TO HAVE VERY STRONG UNCOMMANDED YAW INPUTS. THE PILOT DISENGAGED THE YAW CSAS BUT STILL FELT WHAT HE THOUGHT WAS UNCOMMANDED YAW INPUTS. BOTH ENGINES INDICATED N ORMAL. THE PILOT THEN MADE A PRECAUTIONARY LANDING AND NOTIFIED MAINTENANCE. MAINTENANCE REPORT - WHEN THE MECHANIC MA DE A VISUAL INSPECTION OF THE TAIL ROTOR AND CONTROLS. THE MECHANIC ALSO CLEANED AND REINSTALLED THE YAW CSAS COMPUTER ELECTRICAL CONNECTORS. THE AIRCRAFT WAS THEN FLOWN IN THE LOCAL AREA AND HAD NO PROBLEMS. THE AIRCRAFT WAS RETURNED TO SERVICE AND FLOWN BACK TO THE BASE. APPROXIMATELY TWO HOUR LATER, THE NEXT DUTY PILOT EXPERIENCED THE SAME UNCOMMANDED 1 G 7 2 3U H13EU 20081107 WP 2008 11 7 AALA200802673 1 20081004 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 76200 53290 LGA - EXTERIOR EMERGENCY LIGHTS AT LEFT AND RIGHT INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 25. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081002 WP 2008 10 2 UPS08853275 1 20080814 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1540 L30R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 D PIT CARGO COMP STA 1540, L30R HAS EXFOLATED CORROSION AT L30. REMOVED AND REPLACED LONGERON SECTIO N IAW SRM 51-1-8, 53-4-1, 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 20081113 EA 2008 11 13 ASOA200801469 1 20081106 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 LT SIDE PRESSURE FLOOR SILL PLATE HAS CORROSION FROM FS 409+128 TO FS 559, LBL 36 TO LBL 44. REMOVED CORROSION ON LT PR ESSURE FLOOR SILL PLATE IAW REO 601R-53-41-666. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801474 1 20081106 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 FS 621-625 UPPER RT OBLIQUE ANGLE CRACKED IN RADIUS. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801476 1 20081106 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA LT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 LT BATTERY RIB ASSY AT WS 53.60 IS CRACKED AROUND A FASTENER. TRIMMED AWAY DAMAGE FROM LT BATTERY RIB. REMOVED NUT PLA TES AND FABRICATED ALL REPAIR PARTS. ALL WORK PERFORMED IAW BOMBARDIER AEROSPACE REO 601R-57-51-046 STEPS 1-4 REPAIR 2. REPAIR ITEMS REQUIRE INSTALL. INSTALLED ALL REPAIR PARTS & NUT PLATES IAW BOMBARDIER AEROSPACE REO 601R-57-51-046 STE PS 5-8. C/W ASA ECTC REO 601R-57-51-046. SUPPLEMENTAL-SDR CLOSED 11/17/2008. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801477 1 20081106 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 RIGHT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED AT RBL 9.0. REPLACED ANGLE AT RT FS 484 FLOOR SUPPORT RBL 9.0 IAW SRM 51-42-06 AND 51-40-11. SUPPLEMENTAL-SDR CLOSED 11/17/2008. 2 L 7 2 4F RT A21EA 20081113 NM 2008 11 13 DHLA2008745665 1 20080910 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 580 BETWEEN S-27R AND S-28R SHEAR TIE WITH CORROSION. REPAIRED FUSELAGE FRAM E SECTION AT BS 580 BETWEEN S-26R AND S-28R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745662 1 20080901 A 5320 FITTING BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT STA 480 S-6L, S-7L, AND S-8L CLIPS WITH CRACK. REPLACED CLIPS AT BS 480 S-6L, S-7L, AND S- 8L IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745664 1 20080909 A 5311 ANGLE BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE BS 294.5 BETWEEN S-24L AND S-27L FRAME ANGLE WITH CORROSION. REPAIRED FRAME ANGLE SECTION AT BS 294.5 BE TWEEN S-26L AND S-27L IAW B727 SRM 51-40-4 FIG 1. 2 L 7 3 4F A3WE 20081113 2008 11 13 SWAA086138 4 20081107 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086139 1 20081111 A 2560 65C16820 FITTING BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR SLIDE GIRT BAR FWD CLIP LOOSE. SECURED CLIP PER MM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086154 1 20081111 A 5754 5C327003 SLAT BOEING 737 737317 138447P NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND LT WING NR 3 L/E SLAT CRACKED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086147 1 20081111 A 3350 20131 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY EXIT LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086144 1 20081111 A 5340 6935352U14 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 867, STR 8L. REPAIRED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086145 1 20081111 A 5210 6562212 SKIN BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR SKIN CRACKED AT UPPER HINGE, BS 304, WL 257. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086146 1 20081111 A 5210 6562212 SKIN BOEING 737 7373H4 1384600 NM L1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR SKIN CRACKED AT LOWER HINGE BS 303, WL 303. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086155 1 20081111 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 21R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086128 1 20081111 A 5242 6545830 SKIN BOEING 737 7373H4 1384600 NM E&E BAY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED SPV CHECK, FOUND E/E DOOR EXTERNAL SKIN CRACKED AT RT EDGE. REMOVED AND REPLACED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086129 1 20081111 A 5340 694515602 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086130 1 20081111 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 17R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086131 1 20081111 A 5311 6546545 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 685, STR 15L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086132 1 20081111 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 203WN 32483 DURING SCHEDULED MV1 CHECK, FOUND FWD EEPLS INOP. REMOVED AND REPLACED EEPLS PER MM. 2 L 7 2 4F RT A16WE 20081113 SO 2008 11 13 C2XA08RI165 1 20081028 A 3610 4800104 SWITCH EMB 145 EMB145LR 3260212 SO BLEED AIR SYS DEFECTIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14543 145553 FLIGHT 2473 - EWR - FLIGHT CREW REPORTED NR 2 BLEED FAIL INDICATION ON CLIMBING. CREW PERFORMED AIR RETURN AND LANDED A IRCRAFT UNEVENTFULLY. EWR MX REMOVED AND REPLACED BLEED PUSHBUTTON AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCR AFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081113 NM 2008 11 13 ASAA0843721 1 20081025 A 5755 654645262A SKIN BOEING 737 7374Q8 138447Q NM NR 4 SPOILER PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NR 4 SPOILER LOWER SURFACE DENTED AND PUNCTURED AT WBL 114. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBL ER IAW B737 400 SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 TSAA0832028 1 20081107 A 3260 ROD END BOEING 737 7372X6C 1384552 NM SQUAT SWITCH DISCONNECTED A TSAA O OTHER O OTHER CL CLIMB 1 WP 13 840AL 23124 FLT 912, LIH-HNL: LANDING GEAR LEVER WOULD NOT GO TO THE UP POSITION AFTER TAKEOFF. ALL SIX GEAR INDICATOR LIGHTS WERE ILLUMINATED. DECLARED EMERGENCY, CONTINUED TO HNL AND LANDED WITHOUT INCIDENT. MAINTENANCE: RECONNECTED THE SQUAT SW ITCH CABLE ROD END. OPS CHECK, GEAR SWING, AND EMERGENCY GEAR SWING OK. RIG CHECK OKAY REF 27-62-51. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 YENA200811100107 1 20081109 A 2780 SLAT SYSTEM EMB ERJ190 ERJ190100IGW 3260408 NM LE SLATS FAILED A YENA O OTHER F FLT CONT AFFECTED DE DESCENT 1 EA 15 265JB 190000049 FLT 1718, SDQ-MCO, SLAT FAIL ON APPROACH WHEN SELECTING FLAPS 5. COMPLETED QRH. FLAPS OPERATE NORMALLY, SLATS FAILED B ETWEEN 3 AND FULL. PERFORMED OPS CHECK OF SLAT IAW FIM 27-81-00-810-803. OPS CHECK OK. 2 L 7 2 4F RT A57NM 20081113 SO 2008 11 13 C2XA08SH146 1 20081113 A 5320 14521713005 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11192 145936 SHV-DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED BEAM IAW EMB 145XR SRM 51-40-02 AND EC5320-01137. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081113 SO 2008 11 13 C2XA08SH148 1 20081113 A 5540 12033817005 HINGE BRACKET EMB 145 EMB145XR 3260214 SO RUDDER WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11192 145936 SHV-DURING C-CHECK THE RUDDER CENTER UPPER HINGE BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MA INTENANCE REMOVED AND REPLACED THE AFFECTED HINGE BRACKET IAW EMB 145XR SRM 55-40-02. THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. 2 L 7 2 4F RT 20081113 SO 2008 11 13 C2XA08SH149 1 20081113 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11192 145936 SHV-DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 17. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01417. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081114 NM 2008 11 14 GTIA0800080 1 20081011 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM ZONE 900 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 507NK 2560 AFT GALLEY FLOORBEAM HAS CORROSION AT Y765 BETWEEN FR 64 AND FR 66. 2 L 7 2 4F RT A28NM 20081114 NM 2008 11 14 CALA0801043 1 20081107 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 FRAME CORRODED STATION 907 AT S-27R. ROUTED OUT CORROSION FROM S-27R TO BL 0 STA 907 AND INSTALLED REPAIR PER SRM 53-00 -07 FIG 201, REPAIR 10. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801048 1 20081108 A 5320 147A57122 WEB BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 73259 30803 WEB AT STATION 1016 RBL 36 CRACKED. REMOVED DAMAGE AND PERFORMED TYPICAL WEB REPAIR PER SRM 51-70-13. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801049 1 20081108 A 5315 147A5506 FLOORBEAM BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 73259 30803 CABIN FLOORBEAM AT STATION 986.5 THE ENTIRE WIDTH HAS AREAS OF CORROSION LBL 50 - RBL 50 FLOORBEAM 986.5 CAP. REPLACED CORRODED FLOORBEAM PER ECRA 5321-01584 AND SRM TR 53-02 / 53-70-51 FOR ASSEMBLY INSTALLATIONS. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801050 1 20081109 A 5315 141T5108 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 67157 30436 CABIN BODY STATION 325 FLOOR SUPPORT FOUND CORRODED BETWEEN LBL 27-56. BODY STATION 325 FLOORBEAM SUPPORT BETWEEN LBL 6 TO LBL 64 REPAIRED PER SRM 53-00-51 REPAIR 1, FIG 201. HFEC NO CRACK FOUND. 2 L 7 2 4F RT A1NM 20081114 NM 2008 11 14 SWAA086163 1 20081112 A 5534 6547450 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER LT O/B FWD LUG FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086175 1 20081112 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 747, STR 26L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086176 1 20081112 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS. 827, STR 26L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801029 1 20081103 A 5320 141A8315U4 ANGLE BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34222 28931 R-1 DOOR L ANGLE HAS CORROSION AT STATION 300 TO 328. REMOVED AND REPLACED CHORD AT R-1 DOOR PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801030 1 20081103 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 FRAME CRACKED AT STATION 827 ABOVE S-9L. REPAIRED FRAME PER EC/RA 5311-01431. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801031 1 20081103 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 FRAME CRACKED AT STATION 380 ABOVE S-9R. REPAIRED FRAME PER EA 5310-04498, OP 2. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801033 1 20081103 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 FRAME CRACKED AT STATION 440 ABOVE S-9R. REPAIRED FRAME PER EA 5310-04498, OP2. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 DHLA2008745623 1 20080905 A 5347 CARGO TRACK BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN FROM BS 690 TO BS 720E RBL 25 CARGO TRACK WITH CORROSION. REPAIRED FUSELAGE CARGO TRACK AT RB L 25 FROM BS 690 TO BS 720C IAW B727 SRM 53-10-5 FIG 1 AND VENTURA AEROSPACE 9G CARGO BARRIER INSTALLATION B727-100/200 STRUCTURAL REPAIR MANUAL REPORT 2489 REV A DTD 09/13/07 PARA 5.4. 2 L 7 3 4F A3WE 20081113 EA 2008 11 13 TRAX200801303 1 20081005 A 5240 HANDLE CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 900EV 7608 SERVICE DOOR REALLY HARD TO CLOSE. LUBED SERVICE DOOR HANDLE IAW CRJ200, AMM 52-41-01. 2 L 7 2 4F RT A21EA 20081113 NM 2008 11 13 USAA920081931 1 20080917 A 5340 69773671 TEE FITTING BOEING 737 7373G7 138447J NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN C18 MAJOR REPAIR NR 6131670 R1 DOOR CUTOUT AFT FRAME INTERCOSTAL IS CRACKED AT STOP FITTING AT BS 332.1, S8R, WL270. REPAIRED R1 DOOR CUTOUT AFT FRAME INTERCOSTAL STOP FITTING AT BS 332.1, S8R, WL270 IAW US AIRWAYS EA NR 130127. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 USAA920081934 1 20081021 A 5754 114N4002103M PCU BOEING 757 757225 1384959 NM NR 1 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918UW 22196 CLT C3 MAJOR REPAIR NR 19C51057012/004 NR 1 SLAT COVE PANEL CRACKED AT OTBD SLAT TRACK 27 INCHES FROM OTBD END. REPAIRE D NR 1 SLAT COVE PANEL AT OTBD SLAT TRACK IAW BOEING DRAWING NR 114NO75-11. 2 L 7 2 4F RT A2NM 20081113 NM 2008 11 13 USAA920081944 1 20081021 A 2560 P2070003001 FLASHLIGHT AIRBUS A319 A319132 3930340 NM ZONE 200 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 822AW 1410 LOG PAGE 8357407 FLT NR 511 PHX-OMA EMERGENCY LIGHT FLIGHT ATTENDANT FORWARD FLASHLIGHT INOPERATIVE. R&R FLASHLIGHT. O PS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081113 NM 2008 11 13 USAA920081945 1 20081022 A 3397 CONNECTOR AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 820AW 1397 LOG PAGE 4329007 FLT NR 536 SEA-PHX EMERGENCY LIGHTS AT 18L ARE INOPERATIVE. FOUND BULKHEAD CONNECTOR DISCONNECTED. RE CONNECTED CANNON PLUG. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081113 CE 2008 11 13 DXTA2008110603339 1 20081105 A 2120 UNKNOWN CESSNA 500 560CESSNA 2076750 CE CABIN SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 07 348QS 5600348 WITH GPU ON AND FREON AIR ON FOR LESS THAN 10 MIN, THERE WAS CONSIDERABLE AMOUNT OF SMOKE COMING OUT OF THE HELL HOLE. 2 L 7 2 4F RT A22CE 20081113 NM 2008 11 13 ABXA200811070259 1 20081029 A 3350 20131A BATTERY PACK BOEING 767 767281 1385109 NM CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 793AX 23143 EMERGENCY LIGHTS ARE INOPERATIVE AT ENTRANCE DOOR COCKPIT AND GROUND EXTERIOR LIGHT OK SWAPPED EMERGENCY LIGHTS POWER SU PPLY IAW B767 MM 33-51-07-2. CHECKS GOOD AS PER SAME. SPARE EMERGENCY LIGHTS BATTERY PACK USED. DEFERRED DI 62333 SPA RE EMERGENCY LIGHTS BATTERY PACK DEFERRED FOR MAINT TRACKING IAW ABX GMM CHAP 1 SEC 07.04. REPLACED THE SPARE EMERGENCY LIGHT BATTERY WITH 7 DAYS. THE SPARE EMERGENCY LIGHT BATTERY PACK WILL BE REPLACED ON OR BEFORE NOV. 5, 2008 ALL PER B7 67 MM 33-51-07-2. CLEAR DI 62333, REMOVED SPARE EMERGENCY LIGHT BATTERY PACK AND BATTERY CHARGER ASSY IAW 33-61-02-2 DI CLEARED PLACARD REMOVED. 2 L 7 2 4F RT A1NM 20081113 EA 2008 11 13 ASOA200801483 1 20081106 A 5210 DRAG ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 PAX DOOR AFT DRAG ANGLE IS CRACKED. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801479 1 20081106 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 RIGHT FS 460 FLOOR SUPPORT FITTING P/N 600-31068-19 CRACKED 1 INCH LONG OUTBOARD SIDE RBL 9. REMOVED RT FS 460 FLOOR SU PPORT FITTING IAW CRJ 200 SRM 51-42-06 AND 51-42-21. LOCATED FASTENER HOLES IN NEW SERVICEABLE FITTING IAW CRJ 200 SRM 51-40-11. FITTING REQUIRES INSTALL. INSTALLED RT FS 460 FLOOR SUPPORT FITTING IAW CRJ 200 SRM 51-42-06 AND 51-42-21. SUPPLEMENTAL-SDR CLOSED 11/17/2008. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801466 1 20081106 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 VERTICAL BEAM ON FRAME AT FS 409+128, LBL 18 O/B SIDE IS CRACKED APPROX 0.250 INCH LONG FROM BOTTOM. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801467 1 20081106 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 VERTICAL BEAM ON FRAME AT FS 409+128 IS CRACKED AT LBL 27 I/B SIDE FROM BOTTOM .500 INCH. REPAIRED VERTICAL BEAM ON FRA ME AT FS 409+128 AT LBL 27 I/B SIDE IAW BOMBARDIER REO 601R-53-41-056 AND BOMBARDIER REO 601R-53-41-809. COMPLIED WITH EC/TC REO 601R-53-41-056 IAW REO 601R-53-41-056 REV E. COMPLIED WITH TC REO 601R-53-41-809 REV A AND MET ALL ITS REQUIR EMENTS. SUPPLEMENTAL-SDR CLOSED 11/17/2008. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801468 1 20081106 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 VERTICAL BEAM ON FRAME AT FS 409+128 IS CRACKED AT RBL 27 I/B SIDE AT BOTTOM RIVET HOLE APPROX .250 INCH. 2 L 7 2 4F RT A21EA 20081113 NM 2008 11 13 KCSA081572 1 20081111 A 5347 SEAT TRACK BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 UPPER DECK SEAT TRACK CORRODED ALONG BS 550 TO BS 570 RBL 11. 2 L 7 4 4F RT A20WE 20081113 NM 2008 11 13 KCSA081567 1 20081110 A 5320 FITTING BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 BS 2360 LOWER FWD CHORD BATHTUB FITTING CORRODED AT STR 50R. 2 L 7 4 4F RT A20WE 20081113 NM 2008 11 13 QXEA2008111001015 1 20080912 A 5347 CARGO TRACK BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 413QX 4060 PDX - C4 - THE LT INBOARD CARGO COMPARTMENT TRACK 9 HAS CORROSION ALONG THE OUTBOARD FLOOR FLANGE FROM STATION X720 TO X 782. BLENDED CORRODED AREA IAW RD 8/4-53-884 AND FOUND BLEND TO BE OF LIMITS. REMOVED SEAT TRACK IAW Q400 SRM 51-40-15 AND 51-42-05. INSTALLED NEW TRACK IAW Q400 SRM 51-21-10, 51-40-07, 51-42-05 AND 51-40-00. 2 H 7 2 4T RT A13NM 20081113 NM 2008 11 13 QXEA2008111201152 1 20081025 A 5350 FAIRING BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 421QX 4149 PDX - C1 - FUSELAGE FAIRING PANEL 261CT HAS CHAFING ALONG FWD EDGE UNDERSIDE MATING SURFACE. BLENDED DAMAGED AREA MAX M ATERIAL REMOVED .003" , IAW RD 8/4-53-521 STEP 1-2. HFEC AREA IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ALODINE D AND PRIMED REPAIR AREAS IAW RD 8/4-53-521 STEP 4-8. 2 H 7 2 4T RT A13NM 20081113 NM 2008 11 13 QXEA2008111201153 1 20081025 A 5350 FAIRING BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 421QX 4149 PDX - C1 - FUSELAGE FAIRING PANEL 261FT HAS CHAFING ALONG FWD EDGE UNDERSIDE MATING EDGE. BLENDED OUT DAMAGE MAX MATERI AL REMOVED .003" IAW RD 8/4-53-521 STEP 1-2. HFEC INSPECTED AREA IAW Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. ALOD INED AND PRIMED AREA IAW RD 8/4-53-521 STEPS 4-8. 2 H 7 2 4T RT A13NM 20081114 NM 2008 11 14 GTIA0800082 1 20081011 A 5320 53472192200 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 507NK 2570 AFT GALLEY FLOORBEAM HAS CORROSION AT Y765 BETWEEN FR 67 AND FR 70. 2 L 7 2 4F RT A28NM 20081114 NM 2008 11 14 SWAA086164 1 20081112 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 273WN 32528 FOUND FWD EEPLS LIGHT LOOSE. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086165 1 20081112 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 593, STR 9R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 ASAA0843690 1 20081104 A 5315 654680362 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 764AS 25101 SEAT TRACK AT BS 480 BS 520 RBL 20 FOUND FLOORBEAM HAVING ADDITIONAL FASTENER HOLE AT BS 500 FROM PREVIOUS INSTALLATION AND HOLE WOULD FALL DIRECTLY UNDER SEAT TRACK. REPAIRED ADDITIONAL FASTENER HOLE AT BS 500 FROM PREVIOUS INSTALLATION D IRECTLY UNDER SEAT TRACK RBL 25 PER ASA EA 400 53EA 00161. PERMANENT REPAIR TO SUBJECT BEAM ACCOMPLISHED AT NEXT HEAVY CHECK NO LATER THAN 18 MONTHS FROM 05 NOV 2008. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 ASAA0873692 1 20081031 A 5320 141A54103 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 PAX CABIN FWD FLOOR INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801056 1 20081110 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 BODY STATON 400 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR-8L AND STR-9L. REPAIRED BODY STATION 400 LEFT SIDE FRAME AT (AC) RAIL BRACKET BETWEEN S-8L AND S-9L PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081107 EA 2008 11 7 ASOA200801428 1 20081030 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 933EV 8022 CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED .3 INCH IN LENGTH. 2 L 7 2 4F RT A21EA 20081107 EA 2008 11 7 ASOA200801431 1 20081031 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DETERIORATED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 832AS 7243 PAX DOOR OPEN AND EXIT PLACARDS DETERIORATED. 2 L 7 2 4F RT A21EA 20081107 NM 2008 11 7 USAA920081986 1 20081029 A 5311 FRAME BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT MAJOR REPAIR Q5 CHECK NR 03C20853011/018, CRACKED FRAME AT BS 500C, S20R - S21R. REPAIRED FRAME AT BS 500C, S20R - S21R. IAW EA 100716. 2 L 7 2 4F RT A16WE 20081107 WP 2008 11 7 AALA200802548 1 20080918 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP BS 160-207 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7527A 49919 CORROSION FOUND ON RT CUSP BELOW GALLEY AT STATION 160 TO 207. AREA OF DISCREPANCY WAS 8.5 INCHES BY 6.5 INCHES. INSTA LLED DOUBLER IN ACCORDANCE WITH SRM 52-20-00-16. 2 L 7 2 4F A6WE 20081107 WP 2008 11 7 AALA200802546 1 20080918 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1418 L2R CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7527A 49919 CRACK FOUND AT LONGERON 2 RT AFT OF BS 1418. REPAIRED IN ACCORDANCE WITH AARD 53-30-00-2. 2 L 7 2 4F A6WE 20081107 WP 2008 11 7 AALA200802571 1 20080923 A 5312 BULKHEAD DOUG DC9 DC983 3022083 WP BS 110 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 RT LOWER SIDE PRESSURE BULKHEAD CRACKED AT STATION 110. CRACK LENGTH IS .5 INCH. INSTALLED DOUBLER WITH FINGERS IN ACC ORDANCE ESO 80559 DATED 19 SEP 2008. 2 L 7 2 4F RT A6WE 20081107 WP 2008 11 7 AALA200802572 1 20080924 A 5340 9936533057 BRACKET DOUG DC9 DC983 3022083 WP BS 211 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 TUL GALLEY INBD TIE DOWN BRACKET CORRODED BEYOND LIMITS AT STATION 211. REPLACED TIE DOWN BRACKET IN ACCORDANCE WITH AA RD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081107 EA 2008 11 7 COMA0860438 1 20081024 A 5315 60034017595 FLOORBEAM CNDAIR CL600 CL6002B16 1900305 EA FS 280 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 781CA 7312 FS 280 FLOOR ANGLE 600-34017-595 IS CRACKED AT LBL9 IN THE LWR FLANGE. CUT OUT DAMAGE AND INSTALLED PERMANENT REPAIR DO UBLER PER REO 601R-53-11-171. 2 L 7 2 4F RT A21EA 20081107 NM 2008 11 7 USAA920081984 1 20081029 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 825AW 1527 LOGPAGE 8313778 FLT NR 202 PHX-ABQ EMERGENCY LIGHT FLASHLIGHT AT DIRECT VIEW JUMPSEAT IS INOPERATIVE. R&R BATTERY PACK IN FLASHLIGHT. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081107 NM 2008 11 7 USAA920081979 1 20081028 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 812AW 1178 LOGPAGE 8349619 FLT NR 548 LAS-PHX EMERGENCY LIGHT FORWARD FLIGHT ATTENDANT FLASHLIGHT RED LIGHT IS NOT BLINKING. R&R F LASHLIGHT BATTERY IN FORWARD FLIGHT ATTENDANT FLASHLIGHT. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081107 EA 2008 11 7 CHQA200800214 1 20081104 A 2824 2421132 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE APU FUEL SYSTEM FAILED A CHQA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 11 653BR 27830 16222 7438 GEE872823 FLIGHT 5505, CMH TO IAH. DURING CRUISE THE FLIGHT CREW RECEIVED AN APU CROSS FLOW FAIL MESSAGE FOLLOWED BY A FUEL IMBAL ANCE. THE AIRCRAFT CONTINUED TO TRANSFER FUEL TO THE NR 2 TANK AND THE FLIGHT DIVERTED TO SDF WHERE IT LANDED WITHOUT I NCIDENT. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE APU FUEL CROSS FLOW SHUT-OFF VALVE WAS AT FAULT. THE VALVE W AS REPLACED AND THE FUEL SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 20081107 NE 2008 11 7 M7K2008F00147 2 20080804 A 7200 ENGINE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE MAKING METAL E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 812MH 3956 PRIOR TO OPS CHECK, FLIGHT TAKEOFF ENGINE CHIP LIGHT ILLUMINATED. FLIGHT WAS ABORTED. ALL DEFECTIVE INSPECTED AND METAL RECEIVED. RUNS COMPLETED. NO LIGHT . EVEN THOUGH FOLLOWING SUCCESSFUL PENALTY RUNS AND NO LIGHT AFTER 1.5 HOURS OF FLI GHT CHECK IT WAS APPARENT THAT METAL WAS CONTINUED TO BE GENERATED. METAL ON MODULE 5 CHIP DETECTOR AND PICKUPS FOUND MO DULE 5 REPLACED. NO FURTHER DEFECT NOTED. METAL GENERATION SO SHORTLY AFTER OVERHAUL IS A BIT UNUSUAL BUT WITH THIS MODU LE, MAKING METAL IS EASILY IDENTIFIED BY METAL COLLECTING ON THE HIGHLY MAGNETIC PICKUPS AS WELL AS THE CHIP DETECTOR. ( K) 1 G 7 2 3U 3 U H9EU E00054EN 20081107 NM 2008 11 7 UPS08M53850 1 20081022 A 5720 STIFFENER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:3C RT WING L/E STIFFENER XFS 600 CRACKED. REMOVED STIFFENER, FABRICATED AND INSTALLED STIFFENER IAW DWG ARB2933 AND MD-11 SRM 51-21-01, 51-33-01. 2 L 7 3 4F RT A22WE 20081107 NM 2008 11 7 UPS08B53859 1 20081101 A 3350 LIGHT BOEING 747 74744AF 13848B2 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 573UP 35662 INSPECTION TYPE:N/A EMERGENCY LIGHT AT BOTTOM OF CREW STAIRS INOP. RELAMPED PER MM 33-51-07-2. OK FOR SERVICE. 2 L 7 4 4F RT A20WE 20081107 NM 2008 11 7 SWAA086040 1 20081031 A 3350 8200048801 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 655WN 28400 FOUND LT OVERWING EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER EA. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086013 1 20081102 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 385 TO 387, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081114 EU 2008 11 14 08FDEA04757 1 20081105 A 5230 A5237416020800 SKIN AIRBUS 300 A300B4622R 3930312 EU CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 AFT CARGO DOOR INTERIOR SKIN IS CORRODED AT THE AFT LOWER CORNER. REMOVED CORROSION IAW SRM 51-74-01. FOUND TO BE OUT OF LIMITS IAW SRM 52-30-00. ORIGINAL MATERIAL 0.063. REMAINING MATERIAL 0.052. MATERIAL REMOVED 0.011. THE SKIN WA S REPLACED ON WORK CARD N00380. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 CALA0801057 1 20081110 A 5311 6546525 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 BODY STATION 380 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR-8R AND STR-9R. REPAIRED BODY STATION 3 80 FRAME CRACK BETWEEN S-8R AND S-9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081114 EU 2008 11 14 08FDEA04759 1 20081105 A 5311 A53770545 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA O OTHER O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS GOUGE ON FRAME 28, 2.125 INCH BELOW STR 18L, REPAIR COMPLIED WITH ON EA 6-5310-123938. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 CALA0801058 1 20081110 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 BODY STATION 787 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8R AND STR 9R. ACCOMPLISHED EA5310-044 98 ON BODY STATION 787 FRAME AT STR 8R - STR 9R. 2 L 7 2 4F RT A16WE 20081114 EA 2008 11 14 SWIA200820325 1 20081109 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 976SW 7952 FLT 6590 - CEILING LEVEL AFT EMERGENCY FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081114 EA 2008 11 14 SWIA200820314 1 20081104 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 698BR 7799 FLT 6621 - AFT EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081114 EA 2008 11 14 SWIA200820315 1 20081106 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 698BR 7799 FLT 6621 - FLOOR LEVEL EMERGENCY FLOOD LIGHT INOP. REPLACED BATTERY CHARGER AND LIGHT ASSEMBLY. 2 L 7 2 4F RT A21EA 20081114 NM 2008 11 14 CALA0801059 1 20081110 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 BODY STATION 440 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8L AND STR 9L. REPAIRED BODY STATION 440 LEFT HAND SIDE FRAME BETWEEN S-8L AND S-9L PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081114 EU 2008 11 14 08FDEA04692 1 20081104 A 5310 A53770903210 SPLICE AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS DAMAGE ON FRAME 22 TRUSS SPLICE BETWEEN STR 8R AND STR 9R WITH SHEARED RIVETS ON STR 9R. REMOVED AN D REPLACED PROFILE AND SPLICE IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 08FDEA04694 1 20081104 A 5340 69445595 STRINGER CLIP BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 LOWER AFT CARGO AREA, CORROSION ON STRINGER CLIP AT KEEL BEAM CHORD STA 950E 3. REMOVED STRINGER CLIP, LOCATED AND DRIL LED TO SIZE, TREATED AND PRIMED BARE METAL ON KEEL BEAM. INSTALLED NEW STRINGER CLIP REF SRM 51-30-2 PG 1, 51-10-2 PG 1 . THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081114 EU 2008 11 14 08FDEA04738 1 20081105 A 5311 A53770545 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS GOUGE ON FR 28, 1 INCH ABOVE STR 20L. REPAIR COMPLIED WITH ON EA6-5310-123938. 2 L 7 2 4F RT A35EU 20081114 EU 2008 11 14 08FDEA04702 1 20081104 A 5311 A53773288200 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK FR 20 HAS GOUGE 2.5 INCHES BELOW STR 12R. REPAIR COMPLIED WITH ON EA 6-5310-124032. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 08FDEA04703 1 20081104 A 5322 6516340 SHEAR TIE BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 LOWER AFT CARGO AREA, CORROSION ON SHEAR TIE AT RBL 11 BS 990, REMOVED CORROSION REF SRM 51-10-6 PG 5. MEASURED ORIGINA L "T" .043, .038 REMAINING REF NDT PART 4 51-00-00 FIG 2. REMOVED .005 OUT OF LIMITS REF SRM 53-10-1 DETAIL IV. REMOVE D DAMAGE, FABRICATED SHEAR TIE REF SRM 53-10-4 DETAIL I. HEAT TREATED SHEAR TIE TO THE T-6 CONDITION. TREATED AND PRIM ED REF SRM 51-10-2 PG 7 AND MM 51-20-151-7. INSTALLED SHEAR TIE REF SRM 51-51-10-4 PG 58-60. THIS IS CLASSIFIED AS A M AJOR REPAIR. 2 L 7 3 4F A3WE 20081114 EU 2008 11 14 08FDEA04704 1 20081104 A 5311 A53773289204 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS 2 GOUGES ON FR 24 2.75 INCH BELOW STR13R AND 2.5 INCHES BELOW STR 14. REMOVED AND REPLACED FRAME SE CTION BETWEEN STR 13R AND 21R IAW SRM 51-40-21. FABRICATED FRAME SECTION ON TRAVELER T8/ 765475. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 08FDEA04705 1 20081104 A 5320 6558352273 FLOOR SUPPORT BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 LOWER FWD CARGO PIT, CORROSION AT NUT PLATE HOLE UPPER AND LOWER SURFACE OR FLOOR SUPPORT STA. 720C 3 INCHES, LBL 2.5. REMOVED CORROSION ORIG T= .064 RE= .009, LOSS OUT OF LIMITS REF SRM 51-10-1 PG 5. INSTALLED REPAIR STA 720C REF SRM 53- 10-5 FIG 4. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 ASAA0843698 1 20081029 A 5340 654652587 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 CABIN STRINGER CLIP CRACKED AT STA 380 STR 8. REMOVED DAMAGED CLIP, LOCATED DRILLED AND INSTALLED REPLACEMENT STRINGER CLIP IAW B737 400 SRM 51 40 02 PG 2 AND 4. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 ASAA0843699 1 20081029 A 5340 65C229086 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 CABIN STRINGER CLIP CRACKED AT STA 500B STR 16R. REMOVED DAMAGED CLIP, LOCATED DRILLED AND INSTALLED REPLACEMENT STRING ER CLIP IAW B737 400 SRM 51 40 02 PG 2 AND 4 AND 51 40 05. 2 L 7 2 4F RT A16WE 20081114 EU 2008 11 14 08FDEA04751 1 20081105 A 5311 A53770545 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS GOUGE ON FRAME 28, 1 INCH ABOVE STR17 L. REPAIR COMPLIED WITH ON EA 6-5310-123938. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 ASAA0893700 1 20081026 A 5320 146A7502 SUPPORT BOEING 737 737990 NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 SEVERAL AREAS OF CORROSION ON LT FLOOR TO SIDEWALL SUPPORT BS 727A TO 727I. REMOVED CORROSION OUT OF LIMITS, REPLACED F LOOR TO SIDEWALL SUPPORT. 2 L 7 4 4F RT A16WE 20081114 NM 2008 11 14 ASAA0843728 1 20081029 A 5320 654681231 STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FLOOR STRAP CORRODED STA 1016 LBL 2. REMOVED CORRODED STRAP, INSTALLED REPLACEMENT STRAP IAW B737 400 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 ASAA0843723 1 20081024 A 5755 SKIN BOEING 737 7374Q8 138447Q NM NR 4 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NR 4 SPOILER HAS DENTS ON LOWER SURFACE IN LINE WITH ACTUATOR. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR AN D DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 ASAA0843743 1 20081031 A 5755 SKIN BOEING 737 737490 1384715 NM SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 RIGHT INBOARD GROUND SPOILER LOWER SURFACE HAS MULTIPLE DENTS WITH DELAMINATION ON INBOARD TRAILING EDGE. REMOVED DAMAG ED AREA. INSTALLED DOUBLER FILLER AND BOND REPAIR PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 2008UALA06367 1 20081103 A 2612 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FIRE WARNING INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 366UA 24535 ENG 2 FIRE LIGHT DID NOT LIGHT UP. RELAMPED FIRE LIGHT, ALSO REPLACED PIT DETECTOR PANEL. CHECKED OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 20081114 NM 2008 11 14 2008UALA06368 1 20081103 A 3350 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS FAULTY A UALA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 29 569UA 26677 AFTER ENG START AND TAXI FOLLOWING EMERGENCY EXIT LIGHTS CAME ON WITH SW ARMED: EEL ROW 16-24, RANDOM STOW BIN LIGHTS F ROM ROW 16-33, & DOOR 3 LT &RT SIGNS. NOTHING FWD OF OVERWING EXITS TO COCKPIT CAME ON. FOUND ABOVE LIGHTS WERE PART O F AFT EMER TEST LT SW CIRCUIT. REPLACED DOOR 3L EMER LT TEST SW S 10295, ALL EMER LIGHTS TEST OK. RAN ENGS AND ACCOMPL ISHED TAXI TEST, UNABLE TO DUPLICATE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 NM 2008 11 14 2008UALA06369 1 20081103 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 548UA 25396 EMERGENCY LIGHT STRIP IN FRONT OF F/C CLOSET IS LOOSE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 NM 2008 11 14 2008UALA06371 1 20081104 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 776UA 26937 SEAT 3E AFT EMERGENCY LIGHT INOP. LIGHT CHECKS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081114 NM 2008 11 14 2008UALA06374 1 20081104 A 5210 ROLLER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE PAX DOOR DIRTY A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 RT UPPER DECK DOOR WILL NOT ARM FOR DEPARTURE. CLEANED ROLLERS AND SLIDE OF ARMING TEE. CLEANED ARMING FORK. CYCLED D OOR AND ARMING IS NOW NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081114 2008 11 14 ZZDA2008170 4 20081111 A 2330 ENTERTAIN SYS BOEING 717 717200 1383700 NM ROW 12-14 SHORTED A ZZDA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 37 985AT 55090 PAX IN ROW 12 AND 14 AC LEFT SAW SPARKS AND ODOR SMOKE. F/A CONFIRM ODOR BUT NOT NO SPARKS. CONFIRMED SPARK THAT WAS REPORTED BY PAX IN ROW 12 AC. FOUND C/B ZONE 5 POPPED FOR XM SYSTEM IN THE E&E. COLLARED C/B FOR ZONE 5. PULLED AND COL LARED XM SYSTEM C/B IN COCKPIT D3,4,5 AND E5. 2 L 7 2 4F TR A6WE 20081114 NM 2008 11 14 SWAA086180 1 20081112 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 20L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086181 1 20081112 A 5312 6545771 PRESSURE PANEL BOEING 737 7373H4 1384600 NM RT MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND RT MAIN WHEEL WELL LOWER CHORD SKIN CRACKED AT BS 679. REMOVED AND REPLACED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086182 1 20081112 A 5753 6573731 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20081114 2008 11 14 ZZDA2008169 4 20081104 A 2565 3964899501 LANYARD BOEING 717 717200 1383700 NM L1 DOOR SLIDE BROKEN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 932AT 55073 ESCAPE SLIDE AT L-1 DOOR WIRE LANYARD BROKEN. R&R WIRE LANYARD IAW REF MM 25-61 2 L 7 2 4F TR A6WE 20081114 CE 2008 11 14 Z5FA110708N322CS1 1 20081107 A 3233 99124854 ACTUATOR CESSNA 500 550 2076604 CE NLG INTERMITTENT E Z5FA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 63 322CS 3977 5501052 NOSE GEAR DOWN INDICATION FAILED TO ILLUMINATE WHEN GEAR WAS EXTENDED. CREW ABORTED APPROACH TO WORK AFM CHECK LIST FOR GEAR PROBLEM. AFTER GEAR WAS BLOWN DOWN, NOSE GEAR DOWN IDICATION WAS GOOD. SEVERAL MOMENTS LATER, NOSE GEAR DOWN INDIC ATION FAILED AGAIN. CREW DECLARED EMERGENCY AND PROCEDED TO LAND, NOSE GEAR DOWN INDICATION CAME BACK ON PRIOR TO TOUCH -DOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND DEFECTIVE NOSE GEAR ACTUATOR. ACTUATOR REPLACED , GEAR RETRACTION FUNCTIONAL CHECK SATISFACTORY, AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 4F A22CE 20081114 EA 2008 11 14 VNAA2008111300001 1 20081110 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ODOR A VNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 05 206PS 7860 CREW REPORTED AFTER SWITCHING BLEEDS TO THE ENGINES, HAD STRANGE ODOR IN THE COCKPIT AND CABIN. CREW ELECTED TO RETURN TO DAY. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND GROUND RAN THE AIRCRAFT AT HIGH POWER SETTING IN ACCOR DANCE WITH AMM 71-00-00-868-806. NO FURTHER DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE. SUSPECT SMELL CAUSED BY RES IDUE FROM ENGINE WASH PERFORMED DURING PREVIOUS OVERNIGHT MAINTENANCE. THERE HAVE BEEN NO SUBSEQUENT WRITE-UPS FOR THIS CONDITION. 2 L 7 2 4F RT A21EA 20081114 NM 2008 11 14 UIEA200800337 1 20081027 A 2130 DOOR BOEING 747 747481 NIR NM CABIN PRESSURE FAILED A UIEA K NONE J WARNING INDICATION CR CRUISE 1 EA 15 429MC 24833 LOWER PRESSURE RELIEF DOOR STATUS MESSAGE DISPLAYED WITH PACK 2 MESSAGE. DEACTIVATED LOWER PRESSURE RELIEF DOOR AND PLA CED ON MEL 21-32-1 2 L 7 4 4F RT A20WE 20081114 NM 2008 11 14 R61A20080034 1 20081101 A 2780 SLAT SYSTEM EMB ERJ170 ERJ170100SU 3260403 NM WARNING LIGHT A R61A O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 804MD 17000016 CREW REPORTED DURING APPROACH THEY RECEIVED A SLAT/FLAP FAIL MESSAGE THEY DECLARED AN EMERGENCY AND LANDED WITH OUT INCI DENT. CREW TAXIED AIRCRAFT TO GATE MAINTENANCE WAS CALLED AND PERFORMED TROUBLE SHOOTING AND COMPLETED OPERATIONAL CHECK S SYSTENM OPERATIONAL CHECK GOOD NO DEFECTS NOTED AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A56NM 20081114 NM 2008 11 14 R61A20080035 1 20081102 A 2780 SLAT SYSTEM EMB ERJ170 ERJ170100SU 3260403 NM MALFUNCTIONED A R61A O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 804MD 17000016 ON APPROACH CREW RECEIVED A FLAP/SLAT FAIL MESSAGE DECLARED AN EMERGENCY AND LANEDED WITH OUT INCIDENT. MAINTENAN WAS DI SPATCHED TO A/C PRFORMED TROUBLE SHOOTING. MANINTENANCE REMOVED AND REPLACED SLAT NR 5 ACTUATOR SYSTEM OPS CHECK GOOD. A IRCRAFT OPS CHECK FLT COMPLETD AND SYSTEM CHECK GOOD. ACFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A56NM 20081114 NM 2008 11 14 SWAA086186 1 20081112 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 12L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086189 1 20081112 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BETWEEN BS 785 TO BS 823, STR 26L. REMOVED AND REPLACED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086190 1 20081112 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086192 1 20081104 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 344SW 24152 DURING SCHEDULED RON CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086197 1 20081112 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED BETWEEN BS 772 TO BS 774, RBL 3. REPAIRED FLOOR SUPP ORT PER EA. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086198 1 20081112 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED BS 727D + 6. REPAIRED FLOOR SUPPORT PER EA. 2 L 7 2 4F RT A16WE 20081113 EU 2008 11 13 YENA200811110108 1 20081108 A 2700 3945128102 COMPUTER AIRBUS 320 A320232 3930326 EU NR 1 ELAC FAILED A YENA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 EA 15 599JB 19343 6242 2336 FLT 1119, BUF-FLL, ACCELERATING ABOVE 10000FT THE AIRCRAFT BANK 4-5 DEGREES LEFT IN LEVEL FLIGHT, NO FUEL IMBALANCED NOT ED, BUT THE LEFT AILERON FLOATING UP ABOVE THE DOUBLE TICK MARKS & THE RUDDER INPUT WAS 2.5 DEGREES RIGHT. DIVERTED TO IAD. DECLARED EMERGENCY WITH ATC, NOTICE BELOW 10000FT WITH SPEED 250 KTS AND LOWER THE AILERON BANKING DISAPPEARED. P ERFORMED VISUAL INSPECTION OF LT AILERON SERVO CONTROL. NO DEFECTS NOTED WITH IRW AMM 27-14-00. PERFORMED VISUAL INSPE CTION OF ALL SPOILERS SURFACES, NO DEFECT NOTED IRW AMM 27-64-00. REMOVED AND REPLACED NR 1 ELAC (2CE1) AND NR 2 ELAC ( 2CE2) IRW AMM 27-93-34. PERFORMED ELAC NR 1 & NR 2 TEST IRW AMM 27-93-34. NO DEFECTS NOTED AT THIS TIME. OK FOR CONTI 2 L 7 2 4F RT A28NM 20081113 NM 2008 11 13 KCSA081565 1 20081110 A 5320 FITTING BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 BS 2360 LOWER FWD CHORD BATHTUB FITTING CORRODED AT STR 36R. 2 L 7 4 4F RT A20WE 20081114 EA 2008 11 14 SWIA200820327 1 20081110 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 954SW 7815 FLT 5877 - CEILING LEVEL EMERGENCY FLOODLIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081114 NM 2008 11 14 CALA0801040 1 20081107 A 5531 65476414 RIB BOEING 737 737524 1384721 NM VERTICAL STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 VERTICAL STABILIZER LEADING EDGE RIB AT STATION 292.07 IS CRACKED ON RIGHT SIDE. INSTALLED REPAIR PER SRM 51-40-02 AND SRM 51-70-11. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086014 1 20081102 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 432 TO 434, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086028 1 20081104 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 739, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086029 1 20081031 A 3350 101114 COVER BOEING 737 7375H4 138449D NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 527SW 26569 FOUND RT EMERGENCY EXIT LIGHT LENS COVER AT ROW 13 DEF MISSING. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086032 1 20081104 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER EA. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086021 1 20081103 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CRACKED AT BS 788, STR 16R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086034 1 20081104 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 28L. REPAIRED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086022 1 20081101 A 5754 65C26686 SKIN BOEING 737 7375H4 138449D NM LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081107 SO 2008 11 7 FDKA2008110100286 1 20081101 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHTS DIRTY A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 FRL 6175 IAD. ROW 12 AFT CEILING PANEL EMERGENCY LIGHT INOP. MX CLEANED CONNECTOR, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081107 NM 2008 11 7 SWAA086039 1 20081101 A 3350 101331 SIGN BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 626SW 27702 DURING SCHEDULED MV1 CHECK, FOUND FWD EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086002 1 20081101 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500A, STR 17R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086004 1 20081101 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 436, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086005 1 20081101 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 2008UALA06340 1 20081031 A 3530 OXYGEN BOTTLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN MISINSTALLED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 510UA 24780 ALL PORTABLE O2 CYLINDERS IMPROPERLY STOWED. STRAPS ARE CAUGHT UNDER CLAMPS. SECURED O2 BOTTLES. 2 L 7 2 4F 4 F RT A2NM E17NE 20081107 NM 2008 11 7 2008UALA06341 1 20081101 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 34C BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 121UA 29167 WIRE HARNESS HANGING DOWN UNDER SEAT 34C HAS A WIRE PULLED AWAY FROM CONNECTOR WHICH IS ALSO HANGING DOWN. REPLACED BRO KEN EEL WIRE. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081106 NM 2008 11 6 2008UALA06311 1 20081028 A 2621 342004051U1 FIRE BOTTLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO BAY FAULTY A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 203UA 24718 CARGO FIRE DETECT BOTH BOTTLES ARMED LIGHTS INOP, NO TEST. REPLACE 2 EA FIRE BOTTLES. REPLACE METERING VLV. REPLACE D IVERTER VALVE. REPLACE 2 EA LINE FILTERS. INSTALL 2 SQUIBS IN EXTINGUISHER BOTTLES. TEST OK. 2 L 7 2 4F 4 F RT A16WE E21EU 20081106 WP 2008 11 6 UPS08853820 1 20081011 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV EVALUATE AND DISPOSITION REPAIR EFN 71520081063 ORIGINAL NON-ROUTINE 1 99042, FORWARD CARGO COMPARTME NT RT SUPPORT ANGLE ATTACHED TO FLOOR SUPPORT BEAM FOUND CRACKED. INSTALLED SUPPORT ANGLE IAW DC8 SRM 51-1-21 REV 78. 2 L 7 4 4F RT 4A25 20081106 WP 2008 11 6 UPS08853829 1 20081027 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE:SP COMPLY WITH ATTACHED WAN NR 1421616 REGARDING CRACK ON L24L. NDT'D NEW CRACKS AND STOP DRILLED, INST ALLED REPAIR DOUBLER AND TAPERED SHIMS IAW SRM, EA 008-10-01-A1544, 51-1-20D, 51-1-8, UPS EO M-5100-27 80-E. 2 L 7 4 4F RT 4A25 20081106 WP 2008 11 6 UPS08853830 1 20081020 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV LT WING CENTER L/E UPPER AFT EDGE HAS A STEEL REPAIR DOUBLER INSTALLED AT STA XFS 297-299. INSTALL C ONICAL WASHERS, REPAIR DOUBLER FILLER 4EA IAW DC8 SRM 57-2-1 REV 78. 2 L 7 4 4F RT 4A25 20081106 EA 2008 11 6 ASOA200801440 1 20081102 A 1100 PLACARD CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR LOOSE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 355CA 10067 EXIT SIGN ON PASSENGER DOOR IS COMING LOOSE. 2 L 7 2 4F RT A21EA 20081107 EA 2008 11 7 ASOA200801426 1 20081029 A 5310 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 933EV 8022 LT EMER EXIT DOOR CUTOUT 6 O'CLOCK POSITION, DOOR LANDING MISSING A 7 INCH LONG SECTION OF MATERIAL THAT IS BONDED TO FU SELAGE SKIN THAT MAKES DOOR LANDING. REPAIRED LT EMERGENCY EXIT LANDING IAW BOMBARDIER AEROSPACE PROCESS SPECIFICATION 157-028. PRESSURE LEAK CHECK OF LT OVERWING EMERGENCY EXIT GOOD IAW CRJ 200 AMM 21-32-00-863-801. SUPPLEMENTAL-SDR CLO SED 11/17/2008. 2 L 7 2 4F RT A21EA 20081107 EA 2008 11 7 ASOA200801429 1 20081030 A 5210 ANCHOR FITTING CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 933EV 8022 FWD/AFT PAX DOOR ANCHOR FITTING ARE CRACKED AND HAVE CORRODED HARDWARE. REMOVED LT WINDSCREEN IAW AMM 25-24-04-000-801. REMOVED AND REPLACED FWD AND AFT PAX DOOR ANCHOR FITTINGS ASSY AND CORRODED HARDWARE WITH SERVICEABLE PARTS IAW EO 600 -52-66 C/W. INSTALLED LT WINDSCREEN IAW AMM 25-24-04-400-801. 2 L 7 2 4F RT A21EA 20081107 WP 2008 11 7 UPS08853860 1 20081105 A 5230 DOOR SEAL DOUG DC8 DC873F 302199F WP CARGO DOOR OBSTRUCTED A IPXA O OTHER C F.O.D. CL CLIMB 1 SO 01 805UP 46117 INSPECTION TYPE:N/A ON CLIMB WITH CABIN PRESSURE DIFFERENTIAL BETWEEN 1.5 - 3.5 PSI THERE WAS A LOUD AIR LEAK FROM CABIN DOOR AREA. NOISE LEVEL WAS SUCH THAT COCKPIT COMMUNICATIONS WERE LIMITED. ACCOMPLISHED AIR TURNBACK. REMOVED LOOSE S EALANT AT MAIN CARGO DOOR UPPER FORWARD SEAL AREA. RESEALED AND PRESSURIZED PER MM 21-31-00-2. NO LEAKS NOTED. 2 L 7 4 4F RT 4A25 20081107 NM 2008 11 7 SWAA086015 1 20081102 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 495 TO 437, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 2008UALA06337 1 20081031 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 SEATS 54 THRU 60 RIGHT EEL LIGHTS INOP. REPAIRED SHORT AT 60JK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081107 NM 2008 11 7 2008UALA06353 1 20081102 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN MISSING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 595UA 28748 THE 34C EXIT STRIP MISSING. REPLACED EEL STRIP AT SEAT 34C. 2 L 7 2 4F 4 F RT A2NM E17NE 20081107 NM 2008 11 7 2008UALA06358 1 20081104 A 2120 4100941C FAN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 211UA 30217 ODOR OF SMOKE IN COCKPIT. FOUND FAN BEARING BAD ALSO BLACK SMOKE AT FAN BLADES. REPLACED EQ COOLING FAN. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081107 NM 2008 11 7 2008UALA06359 1 20081103 A 2613 WARNING SYSTEM BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU OVERHEAT SYS ACTIVATED A UALA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 WP 29 935UA 26663 WING BODY OVERHEAT LIGHT. RTFL DUE TO INCLEMENT WEATHER AT PLANNED DESTINATION. FAULT RECURRED ON NEXT FLIGHT OUT. 2 L 7 2 4F 4 F RT A16WE E21EU 20081107 NM 2008 11 7 2008UALA06360 1 20081104 A 2910 HYDRAULIC SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE UNKNOWN A UALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 29 547UA 25368 LOSS OF HYDRAULICS. FLIGHT DIVERTED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081107 NM 2008 11 7 2008UALA06348 1 20081101 A 5240 582240 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN NO TEST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 CREW REPORT LT UPPER DECK DOOR BATTERY LIGHT TEST FAIL. BATTERY FAILED TEST. REPLACED BATTERY. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081107 NM 2008 11 7 2008UALA06349 1 20081102 A 3510 89151114 OXYGEN SYSTEM BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW O2 LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 198UA 28716 CREW OXYGEN SYSTEM-LOW. *S/D* SERVICED CREW OXYGEN SYSTEM. 2 L 7 4 4F 4 F RT A20WE E24NE 20081107 NM 2008 11 7 2008UALA06350 1 20081102 A 3350 20131A BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 515UA 24840 EEL LIGHTS INOP ROWS 1-6. REPLACED EMERGENCY BATTERY M732, OPS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081107 NM 2008 11 7 2008UALA06351 1 20081102 A 3350 20131A LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 515UA 24840 EMERGENCY EXIT LIGHTS INOP ROWS 9 AND 13. REPLACED EMERGENCY BATTERY M732, OPS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081107 NE 2008 11 7 DL76L081473 2 20081030 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 DEFECTIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 198DN 51934 28455 724740 FAILED EA 51-470869-12 REV B MGB OIL NOZZLES INSP. REPLACING NR 1 ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081107 NM 2008 11 7 DL757081476 1 20081031 A 5412 BULKHEAD BOEING 757 757232 1384965 NM NR 1 PYLON CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 DURING HMV AT SAA, THE NR 1 PYLON AFT BULKHEAD LOWER OUTBOARD FLANGE AT NAC STA 203 WAS FOUND CHAFED WHILE ACCOMPLISHING THE PYLON MOD PER SB-757-0034. THE BULKHEAD WAS REPAIRED PER BOEING INSTRUCTIONS. 2 L 7 2 4F RT A2NM 20081110 NM 2008 11 10 DL75E081478 1 20081102 A 2530 COFFEEMAKER BOEING 757 7572Q8 1384972 NM MID GALLEY DIRTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 706TW 28165 BURNING SMELL FROM MID GALLEY, F/O SIDE COFFEE POT HAD TO PULL C/B. CHECKED COFFEEMAKER LOCATED ON MID GALLEY F/O SIDE. OPS NORMAL. FOUND SMELL DUE TO DIRTY HOTPLATE. CLEANED SAME, OPS NORMAL. 2 L 7 2 4F RT A2NM 20081110 WP 2008 11 10 AALA200802568 1 20080918 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 578-579 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 TANGS ARE CRACKED ON NR 6 SEAT TRACK BETWEEN STATIONS 578 AND 579. AREA OF DISCREPANCY IS 41 INCH BY 1 INCH. REPAIRED WITH PLUG AND BACKING PLATE IN ACCORDANCE WITH AARD 53-20-00-10. 2 L 7 2 4F RT A6WE 20081110 NM 2008 11 10 UPS08M53856 1 20081024 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:3C RT WING TELESCOPING DUCT CUTOUT UPPER CORNERS CRACKED. REMOVED DAMAGE, FABRICATED, AND INSTALLED REP AIR DOUBLER IAW MD-11 SRM 57-10-00 FIG 43, 51-33-01 ITEM 16, 51-35-01 ITEM 7. 2 L 7 3 4F RT A22WE 20081110 EA 2008 11 10 SWIA200820264 1 20080707 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 915SW 7615 ENGINE SUPPORT BEAM ANGLE LT SIDE FS 625 TO FS 640 UPPER AREA CRACKED (C-CHECK). REPLACED ANGLE. 2 L 7 2 4F RT A21EA 20081110 2008 11 10 AALA200802549 4 20080918 A 2565 HOOK AND LOOP DOUG DC9 DC982 3022082 WP ESCAPE SLIDE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7527A 49919 HOOK AND LOOP ON GIRT BAR FLAP FOR EMERGENCY EXIT SLIDE AT AFT SERVICE DOOR FAILS TO ADHERE TOGETHER PROPERLY. REPLACED SLIDE AT AFT SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081110 NM 2008 11 10 USAA920081976 1 20081010 A 5315 6546810501 FLOORBEAM BOEING 737 7373G7 138447J NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL C21 MAJOR REPAIR NR 6139586 CORROSION ON FLOORBEAM UPPER CHORD AT BS967, WL208, LBL 18 TO RBL 18. REPAIRED FLOORBEA M UPPER CHORD AT BS967, WL208, LBL 18 TP RBL 18 IAW B737 SRM 53-00-51-2R. 2 L 7 2 4F RT A16WE 20081110 WP 2008 11 10 AALA200802565 1 20080922 A 5320 ANGLE DOUG DC9 DC983 3022083 WP BS 168 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 RT CUSP ANGLE CORRODED AT STATION 168. AREA OF DISCREPANCY IS 1 INCH BY 1 INCH WITH A DEPT OF .033 INCH. BLENDED OUT C ORROSION AND INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH ESO 80559 DATED 19 SEP 2008. 2 L 7 2 4F RT A6WE 20081110 CE 2008 11 10 Z5F2008F00006 1 20081003 A 3260 622EN2266 SQUAT SWITCH CESSNA 680 680CE 2076811 CE LANDING GEAR OUT OF ADJUST E Z5FA O OTHER N FALSE WARNING CL CLIMB 1 EA 63 630CS 551 81 6800170 AFTER TAKEOFF, WHEN LANDING GEAR WAS SELECTED UP THE LANDING GEAR CYCLED UP AND DOWN 3 OR 4 TIMES. LANDING GEAR WAS SELE CTED DOWN AND LANDING GEAR REMAINED DOWN AND LOCKED. FOUND NOSE LANDING GEAR SQUAT SWITCH OUT OF ADJUSTMENT. ADJUSTED S QUAT SWITCH AND OPS CHECK WAS SATISFACTORY. (K) 2 L 7 2 4F RC T00012WI 20081110 EA 2008 11 10 SWIA200820279 1 20081101 A 3260 BRACKET CNDAIR CL600 CL6002B19 1900309 EA NLG BENT A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 946SW 7776 GEAR DISAGREE MESSAGE, NOSE GEAR DID NOT RETRACT, MAIN GEAR RETRACTED (FLT 5899). REPLACED BENT NOSE CENTERING PROXIMIT Y SENSOR BRACKET. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 SWIA200820269 1 20081028 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 956SW SECOND AFT EMERGENCY LIGHT IN CEILING INOP (FLT 5868). RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081110 NM 2008 11 10 08FDEA04711 1 20081104 A 5311 FRAME BOEING 757 757200 1384950 NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 MAIN CABIN AT STA. 1600 BETWEEN STR2-5L HAS TOOLMARKS. REPAIRED FRAME BS 1600 S2-5L IAW SRM 53-00-07 REPAIR NR 1.THIS IS CATEGORY A REPAIR WITH NO FOLLOW-UP. 2 L 7 2 4F RT A2NM 20081110 EA 2008 11 10 SWIA200820286 1 20080708 A 5210 WEB CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR CRACKED A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 821SK 15109 FORWARD PASSENGER DOOR CRACKED IN ZONE 2 WEB. (C-CHECK)REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081110 WP 2008 11 10 08FDEA04724 1 20081105 A 5730 NRB6219 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 LH WING L/E FOUND CRACK ON SKIN L/E. 2 L 7 3 4F RT A22WE 20081110 NM 2008 11 10 08FDEA04726 1 20081105 A 5230 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 593FE 48551 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 7 FOUND WI TH CRACK INDICATIONS AT HOLES A, B AND D. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II. BUSHING REPAIR AT BOLT H OLES CARRIED OUT AS PER SRM 53-50-00, FIGURE 10, VOLUME I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081110 NM 2008 11 10 08FDEA04727 1 20081105 A 5720 6521656225 RETAINER BOEING 727 7272D4 138407U NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 LEFT WING INBD T.E., CORROSION ON SEAL RETAINER OF LWR. SURFACE PANEL AT REAR SPAR CHORD, 16" O.B. OF WING ROOT AND BE LOW T/T ANGLE GEARBOX REMOVED DAMAGED PARTS. SEAL RETAINER AND ZEE ANGLE RETAINERS. FABRICATED SEAL RETAINER. FABRICATE D ZEE ANGLE RETAINER NDT. ALODINED AND PRIMED PARTS. CLEANED AND PROTECTED AREA. INSTALLED SEAL RETAINER AND ZEE ANGLE R ETAINER IAW SRM 51-30-2 PG 1-10, SRM 51-10-2. DWG 65-21656 THIS IS CLASSIFIED AS A MINOR REPAIR GMM 6-2-100 PG 2-3 2 L 7 3 4F A3WE 20081110 EA 2008 11 10 ASOA20081231 1 20080927 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA BS 559 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 981EV 7768 VERTICAL BEAM AT BS 559 RBL 9 CRACKED .05. OPEN 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 QXEA200834 1 20080728 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 609QX 10031 C4 CHECK, FUSELAGE SKIN CORRODED AROUND LOWER TCAS ANTENNA CUTOUT. BLENDED CORROSION AND FOUND OUT OF LIMITS. IAW SRM 5 3-21-01-002-A01. HFEC INSPECTION IAW NDTM 53-00-000-250-A01. NO CRACKS NOTED. BLEND WITH LIMITS IAW REO 670-53-21-374. 2 L 7 2 4F RT A21EA 20081110 NM 2008 11 10 MAS2008F00088 1 20080930 A 5210 DOOR DHAV DHC8 DHC8202 2809007 NM MAIN PAX STIFF A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 988HA 426 FLT 2860-GOURND CREW CAN NOT GET MAIN CABIN DOOR OPEN. MX OPENED DOOR WITH NO FAULTS. 2 H 7 2 4T RT A13NM 20081110 EA 2008 11 10 MAS2008F00089 1 20080930 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN MALFUNCTIONED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 506MJ 10073 FLT 7335-OVERWING EMERGENCY LIGHTS INOPERATIVE ON AFT SIDE. MX TROUBLESHOT AND FOUND NO FAULTS. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 MAS2008F00093 1 20080928 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM FAILED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 75994 FLT 7262 - NOSE GEAR DISAGREE, PILOT DELARED AND EMERGENCY. MX REMOVED AND REPLACED 3A PUMP, OPS AND LEAK CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 MAS2008F00100 1 20080925 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA MAIN PAX STUCK A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 651ML 7139 FLT 7137 - MAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. MX OPENED DOOR. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 MAS2008F00099 1 20080924 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17231 7231 FLT 2986 - EMERGENCY LIGHT INOPERATIVE. MX INSPECTED AND PERFORMED SYSTEMS OPS CHECK. OPS CHECKED NORMAL. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 MAS2008F00101 1 20080924 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS UNSECURE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 17175 7175 FLT 7210 - EMERGENCY LIGHT INOPERATIVE. RESECURED CONNECTOR. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081110 WP 2008 11 10 NWAA084449997 1 20080930 A 3397 WIRE DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8933E 47142 DURING LINE CHECK, MAINTENANCE FOUND EMERGENCY LIGHTS FOR CATWALK IN TAIL COMPARTMENT INOPERATIVE. MX FOUN BROKEN WIRE, REPAIRED AND REPLACED BATTERY PACK. OPS CHECK OK. 2 L 7 2 4F A6WE 20081110 EU 2008 11 10 MAL2008F00052 1 20081001 A 3397 WIRE SAAB SF340 SF340A 7850100 EU EMERGENCY LIGHT LOOSE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 110XJ 110 DURING INSPECTION EMERGENCY FLOOD LIGHT FOUND INOPERATIVE. FOUND DEFECTIVE SOLDER JOINT ON LAMP ASSY. 2 L 7 2 4T RT A52EU 20081110 EA 2008 11 10 MAS2008F00094 1 20080928 A 5220 COVER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 512MJ 10109 FLT 7204 - LT EMERGENCY EXIT DOOR HANDLE COVER LOOSE. MX RESECURED COVER. 2 L 7 2 4F RT A21EA 20081110 NM 2008 11 10 USAA920081828 1 20081001 A 5320 6935352Y1 STRINGER CLIP BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 -MAJOR REPAIR, STRINGER TIE CLIP CRACKED AT BS 847, S4R. REPLACED STRINGER TIE CLIP AT BS 847, S4R IAW B737 SR M 51-10-02. 2 L 7 2 4F RT A16WE 20081110 NM 2008 11 10 USAA920081827 1 20081001 A 5320 6935352Y1 STRINGER CLIP BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, STRINGER TIE CLIP CRACKED AT BS 807, S4R. REPLACED STRINGER TIE CLIP AT BS807, S4R IAW B737 SR M 51-10-02. 2 L 7 2 4F RT A16WE 20081110 NM 2008 11 10 USAA920081831 1 20081001 A 5320 6545807U30 ANGLE BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, INTERCOSTAL ANGLE CRACKED AT BS 290 BETWEEN S11R & S12R. REPLACED INTERCOSTAL ANGLE AT BS 290 BETWEEN S11R & S12R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081110 EA 2008 11 10 SWIA200820288 1 20080711 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 916SW RT FS460 RBL9 FLOOR SUPPORT FITTING CRACKED. (C-CHECK)REPLACED. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 SWIA200820289 1 20080711 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 916SW LT FS484 LBL27 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED AT FLOOR BEAM. (C-CHECK)REPLACED. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 SWIA200820290 1 20080711 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 916SW LT FS484 LBL36 FLOOR SUPPORT INTERCOSTAL CRACKED AT FLOOR BEAM. (C-CHECK)REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 SWIA200820291 1 20080711 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 916SW 7634 RT SIDE FS 621 TO FS 625 OBLIQUE ANGLE CRACKED. (C-CHECK)REPLACED. 2 L 7 2 4F RT A21EA 20081110 SO 2008 11 10 SWIA200820300 1 20081101 A 3320 LIGHT EMB 120 EMB120ER 3260203 SO CABIN SHORTED A SWIA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 07 568SW 120343 FA REPORTS BURNING ELECTRICAL SMELL NEAR FRONT OF CABIN. (FLT 5729)RELAMPED CEILING LIGHT AT 4A. 2 L 7 2 4T RT A31SO 20081110 EA 2008 11 10 SWIA200820301 1 20081105 A 3230 TARGET CNDAIR CL600 CL6002B19 1900309 EA NLG OUT OF ADJUST A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 946SW 7776 AFTER TAKE OFF NOSE GEAR WOULD NOT RETRACT. (FLT 6491)ADJUSTED CENTERING TARGET ON NOSE STRUT. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 SWIA200820306 1 20081101 A 3397 SPLICE CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A SWIA K NONE L NO TEST NR NOT REPORTED 1 NM 07 926SW 7687 EMERGENCY FLOOR LIGHTS INOP FROM EMERGENCY ROW AFT. (FLT 6351)RESECURED FLOOR SPLICE. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 SWIA200820307 1 20081101 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE L NO TEST UK UNKNOWN 1 NM 07 953SW 7813 AFT EMERGENCY CEILING FLOODLIGHT INOP. (FLT 6050)RELAMPED. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 SWIA200820309 1 20081101 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA RIGHT MALFUNCTIONED A SWIA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 07 909SW 13492 10866 7558 ON CLIMB OUT SMOKE TOILET MESSAGE. (FLT 6752)REPLACED RIGHT ACM PN 782790-15 SN ON 200404155 SN OFF 200211021. 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 SWIA200820311 1 20081030 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA AC BAY DIRTY A SWIA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 NM 07 909SW 7558 SMOKE TOILET WARNING ON TAKEOFF. (FLT 6690)REPLACED COALESCER BAGS ON LT AND RT WATER SEPARATORS. RAN ENGINES AT POWER , NO WARNINGS DISPLAYED. 2 L 7 2 4F RT A21EA 20081112 NM 2008 11 12 AALA200802324 1 20080715 A 3350 D71701100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 920AN 29521 COACH EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK. GROUND CHECKED NORMAL. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086016 1 20081103 A 3350 BR1320 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 421LV 32452 EEPLS COVER BROKEN AT 1 ABC. REMOVED AND REPLACED EEPLS COVER PER MM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086024 1 20081031 A 5330 6545765 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BETWEEN BS 431 TO BS 434, STR 1L. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086033 1 20081104 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER EA. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 SWAA086003 1 20081101 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 426, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 2008UALA06338 1 20081031 A 3350 LAMP BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 795UA 26927 EMERGENCY EVAC LIGHT ON SEAT 1E DANGLING LOOSE. REPLACED LAMP, OPS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081114 NM 2008 11 14 CALA0801046 1 20081108 A 5320 147A5712 SHEAR WEB BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 73259 30803 SHEAR WEB AT STATION 986.5 RBL 48 CRACKED. FABRICATED REPAIR PER ECRA 5321-01585 AND INSTALLED PER SRM 51-40-02 FOR SHE AR WEB AT STATION 986.5 RBL 48. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 ASAA0873691 1 20081030 A 5320 BAC1515531 ANGLE BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 RT BEAM CHORD HAS CORROSION. REMOVED AND REPLACED SECTION OF CHORD. 2 L 7 2 4F RT A16WE 20081114 EU 2008 11 14 08FDEA04732 1 20081105 A 5311 A53973019202 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK FR 59 BENT BELOW STR 13L 2 INCH TO 4 INCH. REWORKED THE UPPER FLANGE SECTION IAW SRM 51-26-00, PERFORM ED HFEC INSPECTION IAW NTM 51-10-08 PT 6. NO CRACK INDICATIONS NOTED. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 CALA0801066 1 20081111 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8L AND STR 9L. REPAIRED FRAME BODY STATION 787 AT STR 8 L AND STR 9L AT AC RAIL BRACKET PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 UIEA200800339 1 20081109 A 2133 7644762 OUTFLOW VALVE BOEING 747 747230B 1384889 NM CABIN PRESSURE FAILED A UIEA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 512MC 21220 AIR TURN BACK . ACFT WOULD NOT PRESSURIZE AFTER TAKEOFF. NR 1 PACK DEFERRED ALREADY. NR 3 PACK VALVE SWITCH OPEN. CABIN ALTITUDE WARNING HORN SOUNDED CABIN AT 10,000 FT. A/C MODE SELECT SWITCH IN AUTO. BOTH OUTFLOW VALVES CLOSED. DUCT PRES SURE 42 PSI, CABIN CLIMBS WITH AIRCRAFT, DIFF PRESS "0". WHEN NR 3 PACK SELECTED THERE WAS NO CHANGE IN DUCT PRESSURE OR CABIN VERTICAL SPEED. FOUND NR 3 PACK FLOW CONTROL AND SHUTOFF VALVE WOULD NOT OPEN WHEN COMMANDED. REPLACED VALVE PER MM 21-51-1 OPS CHECKED NORMAL. 2 L 7 4 4F RT A20WE 20081114 2008 11 14 UIEA200800336 4 20081015 A 2210 COMPUTER BOEING 747 7472D7B 1384803 NM AUTO PILOT FAILED A UIEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 523MC 21782 WHEN "A" AUTOPILOT ENGAGED AIRCRAFT STARTED UNCOMMANDED LEFT ROLL. DISENGAGED "A". "B" WOULD NOT ENGAGE. CYCLED YOKE SWI TCHES AND YOKES NEITHER WOULD ENGAGE. FINALLY GOT "B" TO ENGAGE BUT IT WOULD NOT FOLOW ANY COMMANDS. REPLACED "A" CHANNE L CCA IAW 22-13-02. RESEATED PUSHED BACK PINS 14, 15, 16 ON "B" CHANNEL CCA IAW 20-61-00. REPLACED AUTOPILOT ACC BOX NR 2 PER MM 22-11-03. ACCOMPLISHED CHECKS ON BOTH A & B A/P CHANNELS BOTH CHECK OK. 2 L 7 4 4F RT A20WE 20081114 NM 2008 11 14 SWAA086191 1 20081112 A 5312 6546576 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 1016, BETWEEN STR 5L TO STR 6L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 UIEA200800340 1 20081113 A 7997 CONNECTOR BOEING 747 7472D7B 1384803 NM GE CF6 CF650E2 30018 NE TEMP SENSOR DEFECTIVE A UIEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 15 524MC 21784 517532 AIR TURN BACK. NR 1 ENGINE OIL TEMP OFF SCALE HIGH FOR AT LEAST 10 MINUETS . ENGINE SHUT DOWN. WIRING CHECKS ACCOMPLISH ED AND FOUND NR 1 OIL TEMP SENSOR CONNECTOR DEFECTIVE . CONNECTOR REPLACED AND ALL OPERATIONS NORMAL. ENGINE RUN UP NORM AL. NR 1 ENGINE OIL TEMP SENSOR REPLACED AS PRECAUTION AND ENGINE RUNUP. LEAK CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E23EA 20081114 EU 2008 11 14 F3LA2008111000709 1 20081106 A 3520 21214001 SOLENOID AIRBUS A318 A318111 3940019 EU OXYGEN SYSTEM FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 808FR 31 3038 REFERENCE NON-ROUTINE 104852. DURING COMPLIANCE OF ENGINEERING ORDER A8-25EO-20453, BE AEROSPACE 120 PASSENGER SEAT CABI N CONFIGURATION, THE OXYGEN CONTAINER AT THE FIFTEENTH ROW OF SEATS ON THE LEFT FAILED DROP TEST. MAINTENANCE REMOVED AN D REPLACED THE OXYGEN CONTAINER PER AMM 35-21-10-000-001 AND AMM 35-21-41-400-001. OPERATIONAL CHECK PERFORMED WITH SATI SFACTORY RESULTS IN ACCORDANCE WITH AMM 35-23-00-710-001. 2 L 7 2 4F RT 20081114 EU 2008 11 14 F3LA2008111000710 1 20081106 A 3520 21214001 SOLENOID AIRBUS A318 A318111 3940019 EU OXYGEN SYSTEM FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 808FR 31 3038 REFERENCE NON-ROUTINE 104853. DURING COMPLIANCE OF ENGINEERING ORDER A8-25EO-20453, BE AEROSPACE 120 PASSENGER SEAT CABI N CONFIGURATION, THE OXYGEN CONTAINER AT THE TWELFTH ROW OF SEATS ON THE LEFT FAILED DROP TEST. MAINTENANCE REMOVED AND REPLACED THE OXYGEN CONTAINER PER AMM 35-21-10-000-001 AND AMM 35-21-41-400-001. OPERATIONAL CHECK PERFORMED WITH SATISF ACTORY RESULTS IN ACCORDANCE WITH AMM 35-23-00-710-001. 2 L 7 2 4F RT 20081114 NM 2008 11 14 F3LA2008111000711 1 20081109 A 5210 D5211071720000 BUSHING AIRBUS A319 A319111 3930336 NM L1 DOOR OUT OF POSITION A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 939FR 10 2448 REFERENCE LOG PAGE 420725. PILOT REPORTED THE FORWARD ENTRY DOOR L1 GUST LOCK WILL NOT ENGAGE. MAINTENANCE REINSTALLED B USHING IN THE FORWARD ENTRY DOOR GUST LOCK MECHANISM IN ACCORDANCE WITH A319 AMM 52-11-11-730-050. 2 L 7 2 4F RT A28NM 20081114 SO 2008 11 14 SIMA200831002 1 20081031 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 908AE 5000 14500897 DURING AN IMBV INSPECTION. THE BAGGAGE DOOR LOWER CENTER SILL WAS FOUND TO BE CORRODED. REMOVED CORRODED CENTER SILL. I NSTALLED NEW SILL 145-25480-603. REPAIR DONE IAW SRM 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081114 SO 2008 11 14 SIMA200831003 1 20081028 A 5310 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 642AE 5000 145193 DURING A MBV INSPECTION. THE LT OMEGA BEAM AT FRAME 29 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE LT OMEGA BEAM TO REMOVE THE DAMAGE. PREPARED A REPAIR DOUBLE, FILLER AND TWO SHIMS. MARKED, DRILLED, CLEANED AND TREATED REPAIR PART. REPAIR DONE IAW SRM 53-00-10, FIGURE 202. ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081114 SO 2008 11 14 SIMA200831502 1 20081107 A 3230 2309290041 UNLOCK CYLINDER EMB 135 EMB135KL 3260302 SO MLG MALFUNCTIONED A SIMA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 21 815AE 145545 ON FLIGHT 4662 CREW REPORTED THAT GEAR FAILED TO RETRACT DURING TAKE OFF. AIRCRAFT RETURNED TO FIELD. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED UNLOCK BOX IAW EMB AMM B32-33-10. PERFORMED EXTENSION AND RETRACTION IAW AMM 32-30-00, OP ERATIONAL CHECK GOOD NO FURTHER DEFECTS NOTED. ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081114 NM 2008 11 14 NSVA2008040 1 20081104 A 3260 WARNING LIGHT BOMBDR DHC8 DHC8402 1390042 NM MLG ILLUMINATED A NSVA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 187WQ 4187 UNSAFE GEAR INDICATION ON APPROACH INTO EWR / GEAR MANUALLY EXTENDED / AIRCRAFT LANDED SAFELY AND WAS TOWED TO GATE. 2 H 7 2 4T RT A13NM 20081114 NM 2008 11 14 QXEA2008111201172 1 20081106 A 2421 11522184 GENERATOR BOMBDR DHC8 DHC8402 1390042 NM AC SYSTEM MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 19 430QX 3969 4163 YKM- RECEIVED A NR 1 AC GENERATOR CAUTION LIGHT PRIOR TO 60 KNOTS ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO THE GATE. REMOVED AND REPLACED NR 1 AC GEN IAW TC 6242101.OPS CHECKED GOOD PER Q-400 AMM TASK 24-21-00-710-801. RETURNED TO SERV ICE. 2 H 7 2 4T RT A13NM 20081114 EU 2008 11 14 QMLA1104200808051 1 20081104 A 2140 350A72027102 NOZZLE SNIAS 350 AS350B2 8680813 EU VENTILATION COLLAPSED E QMLA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 03 561AM 184 4381 TOOK OFF AT 22:45 FROM A LOCAL HOSPITAL TRANSFERRING AN ELDERLY PATIENT. THE PATIENT WAS COLD AND ASKED THE MEDICAL CRE W IF THE PILOT COULD TURN ON THE HEAT. THE PATIENT ALREADY HAD SEVERAL BLANKETS ON TO KEEP WARM. SEVERAL MINUTES AFTER TAKE OFF, THE PILOT TURNED ON THE HEAT AND THE DEMISTER TO WARM THE CABIN. A COUPLE OF MINUTES LATER, A URINE TYPE SME LL WAS STRONG IN THE CABIN AND THERE WAS WHAT LOOKED LIKE A SMOKY HAZE. THE HEAT AND DEMIST WERE TURNED OFF AND THE AIR CRAFT WAS TURNED TOWARD THE NEAREST AIRPORT AND WE MADE A CALL TO DISPATCH TO LET THEM KNOW OF OUR SITUATION. SINCE THE SMOKY HAZE AND SMELL WAS STARTING TO GO AWAY, THE PILOT DID NOT OPEN THE WINDOWS TO AIR OUT THE CABIN AND REDUCE THE TE 1 G 7 1 3U H9EU 20081114 NM 2008 11 14 2008UALA06376 1 20081104 A 2722 S252T7016 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RUDDER LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 646UA 25283 FOUND MIDDLE RUDDER PCA LEAKING HYDRAULIC FLUID. REPLACED MIDDLE RUDDER PCA. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081114 2008 11 14 2008UALA06377 4 20081105 A 2565 B14056904 O-RING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 562UA 0503 26664 LOW SLIDE PRESSURE. CAUSE: LEAKING AT GAUGE O-RING. REMOVED & REPLACED O-RING. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 NM 2008 11 14 2008UALA06380 1 20081105 A 3350 BATTERY BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 942UA 26679 LEFT OVERWING EXTERNAL EMERGENCY SLIDE LIGHT INOP. OPS CHECK OK AFTER RECHARGING. 2 L 7 2 4F 4 F RT A16WE E21EU 20081114 NM 2008 11 14 2008UALA06381 1 20081105 A 3350 POWER STRIP BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 942UA 26679 CABIN FLOOR EEL INOP FROM ROW 11 TO ROW 14. SPLICED EEL POWER STRIP AT ROW 11. 2 L 7 2 4F 4 F RT A16WE E21EU 20081114 NM 2008 11 14 2008UALA06386 1 20081106 A 4900 DUCT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU WORN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 781UA 26945 APU PRESSURE DUCT FOUND WORN BEYOND LIMITS, BY CONTACT WITH STRUCTURE CUTOUT AT STA 2360 FRAME. REMOVED DUCT, WELD REPA IRED. REINSTALLED AND LEAK CHECKED. REPLACED SUPPORT NYLON SLEEVE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081114 NM 2008 11 14 08FDEA04821 1 20081109 A 5414 311N504631 SKIN BOEING 757 75723A 1384967 NM NR 1 PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 NR 1 STRUT OTBD SIDE SKIN CORRODED INSIDE ACCESS PANEL 433CL. REMOVED AND REPLACED WITH NEW SKIN P/N 311N5046-31 IAW SR M 51-40-02 AND DWG 311N5002, "A" MAJOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED. 2 L 7 2 4F RT A2NM 20081114 NM 2008 11 14 08FDEA04512 1 20081023 A 5313 AFA77751 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 CENTER CARGO BETWEEN LT STA 5-123 TO 1541 LONGERON 48 HAS CORROSION. REMOVED AND FOUND EXCEED LIMITS AS PER SRM 53-00-0 1 FIGURE 4 VOLUME I. ORIGINAL THICKNESS = 0.130", MATERIAL REMOVED = 0.060 INCH, MATERIAL REMAINING = 0.070 INCH, LON GERON FABRICATED AS PER DRAWING NR AFA7755, LONGERON 48 LEFT CARRIED REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I AND SR M 51-33-01 VOLUME II. FABRICATED LONGERON 48 LEFT FROM STA 5-123 TO 1541 REMOVED AND REPLACED AS PER SRM 53-10-00 FIGUR E 2 VOLUME I AND SRM 51-33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081114 NM 2008 11 14 08FDEA04513 1 20081023 A 5313 AFA77551 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 CENTER CARGO, LEFT STA 1531 TO 1541 LONGERON 40 FOUND CRACKED. CENTER CARGO LEFT STA 1531 TO 1541 LONGERON 40 CARRIED O UT REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I. LONGERON 40 LEFT FABRICATED AS PER DRAWING NR AFA7755. LONGERON 40 LE FT FROM STA 1531 TO 1551 REMOVED AND REPLACED AS PER SRM 53-10-00 FIGURE 2 VOLUME I AND SRM 51-33-01 VOLUME II. THIS RE PAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081114 NM 2008 11 14 08FDEA04518 1 20081024 A 5322 AGA000919 SHEAR TIE DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 AFT CARGO, STA 1902 BETWEEN LONGERON 51 LEFT TO 51 RIGHT FOUND SHEAR CLIP CORRODED. AFT CARGO STA 1902 BETWEEN LONGER ON 51 LEFT TO 51 RIGHT SHEAR CLIP CORROSION REMOVED AND FOUND EXCEED LIMITS AS PER SRM 53-00-01 FIGURE 4 VOLUME I. ORIG INAL THICKNESS = 0.071 INCH, MATERIAL REMOVED = 0.030 INCH, MATERIAL REMAINING = 0.041 INCH. SHEAR CLIP FABRICATED AS PER DOUGLAS DRAWING NR AGA0009. SHEAR CLIP REMOVED AND REPLACED AS PER SRM 51-35-01 VOLUME II. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081114 NM 2008 11 14 08FDEA04519 1 20081024 A 5313 A6A70031 LONGERON DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 CRACK INDICATION FOUND DURING X-RAY INSPECTION AT STA 6-0, LONGERON - 1 LEFT AFT SECTION EDGE AS MARKED. CRACK LENGTH A PPROXIMATELY 0.5 INCH STA 6-0, LONGERON, 1 LEFT CARRIED OUT REPAIR WITH FABRICATED INTERCOSTAL AS PER EA NR 1-5310-122 615 (TITLE; FUSELAGE - MAIN FRAME - LONGERON 1 LEFT SPLICE REPAIR AT STA 6-00 TO 6-10). REPAIR LONGERON FABRICATED AS P ER DOUGLAS DRAWING A6A7003 AND SRM 53-10-00 FIGURE 2 VOLUME I. ALL REPAIR PARTS INSTALLED AS PER SRM 53-10-00 FIGURE 2 VOLUME I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081114 NM 2008 11 14 08FDEA04824 1 20081109 A 5330 65545776 SKIN BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 LOWER FWD CARGO PIT BILGE, CORROSION SPOT ON FUSE SKIN AT AFT SIDE OF STA 700, BL 0". REMOVED DAMAGE FABRICATED REPAIR DOUBLER ANDINSTALLED REPAIR PER REF SRM'S 51-10-6,51-10-2, 51-30-02 AND 53-30-3 FIG1 . THIS IS CLASSIFIED AS A MAJOR RE PAIR. CATEGORY "B" REPAIR 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04826 1 20081110 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 593FE 48551 UPON REMOVAL OF FLOOR PANEL FOR AUX TANK UPPER SURFACE CORROSION REMOVAL ACCESS FOUND SEAT TRACK ATTACHMENT HOLE AT STAT ION 1219, X=-75 CORRODED. 2 L 7 3 4F RT A22WE 20081114 NM 2008 11 14 08FDEA04827 1 20081110 A 5347 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 593FE 48551 UPON REMOVAL OF FLOOR PANEL FOR AUX TANK UPPER SURFACE CORROSION REMOVAL ACCESS FOUND SEAT TRACK AT STATION 1184, X=-75 CORRODED. 2 L 7 3 4F RT A22WE 20081114 EU 2008 11 14 08FDEA04829 1 20081110 A 5510 A5517781120200 FITTING AIRBUS 310 A310324 3930206 EU ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 LEFT HORIZONTAL ACCESS 333 BB REAR HOIST POINT FITTING IS CRACKED. REMOVED INBD REAR HOIST POINT FITTING IAW SRM 51-40- 21. INSTALLED REPAIR PLUG IAW EO 6-5510-7-5001. INSTALLED FITTING IAW SRM 51-40-21. SEALED FITTING FASTENERS IAW SRM 5 1-74-00. INSTALLED COVER PLUG IAW EO 6-5510-7-5001. 2 L 7 2 4F RT A35EU 20081114 SO 2008 11 14 C2XA08SH135 1 20081106 A 5751 14569005410 BUSHING EMB 145 EMB145XR 3260214 SO RT AILERON MIGRATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11192 14500936 SHV - DURING C-CHECK RT AILERON CENTER O/B BRACKET HAS MIGRATING HAT BUSHING. MX REMOVED AND REPLACED RT AILERON CENTER O/B BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4F RT 20081114 CE 2008 11 14 DJFA2008079 1 20081102 A 2130 WARNING SYSTEM BEECH MU300 400A 1155402 CE CABIN PRESSURE MALFUNCTIONED E DJFA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 EA 23 429LX RK265 CLIMBING THROUGH FL 340 CABIN PRESS LOW LIGHT ILLUMINATED WITH CABIN AT 9000 FT AND CLIMBING. CREW PERFORMED AN EMERGEN CY DESCENT, DECLARED AN EMERGENCY AND LANDED SAFELY. SDR WILL BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION. 2 H 7 2 4F RT A16SW 20081114 NM 2008 11 14 K11A2008111272202 1 20080918 A 5311 FRAME BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 FRAME WEB HAS CORROSION ON AFT SIDE ABOVE STRINGER 24L AT STA 303.9 LBL 37. CORROSION 2 X 2 INCHES. 2 L 7 3 4F RT A3WE 20081114 NM 2008 11 14 K11A2008111272203 1 20080818 A 5311 FRAME BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 UPPER CHORD OF FRAME CORRODED BELOW SUB FLOOR AT STA 304, ABOVE STR 24L, LBL 38. CORROSION 2 X 1 INCHES. 2 L 7 3 4F RT A3WE 20081114 NM 2008 11 14 2008UALA06366 1 20081103 A 2612 G7185095 CONTROL PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 366UA 24535 CARGO FIRE LIGHT DID NOT LIGHT UP. SUSPECT FAULTY FIRE CONTROL PANEL. REPLACED CARGO FIRE CONTROL PANEL CHECKD OKAY. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081114 NM 2008 11 14 2008UALA06401 1 20081106 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT PIT FRAME DENTED STA 1340, STR 25L TO 24L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED FRAME SECTION AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 NM 2008 11 14 08FDEA04509 1 20081023 A 5730 ARB74021 SKIN DOUG MD11 MD11F 3023600 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 08 FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HFEC INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS = 690 AND STA XORS = 700. LEFT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS = 690 AND STA XORS = 700, 08 EACH FASTENER HOLES CARRIED OUT REPAIR AS PER EA NR 1-5710-122604 PART 1. TITLE, AD 2007-07-04, WINGS, LT LO WER SKIN PLANK CUT OUT AT 536AB, EIGHT ACCESS DOOR ATTACHMENT BORES WITH CRACK INDICATIONS PSE 57.23.01 ALI - REPAIR. T HIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081114 NE 2008 11 14 08FDEA04854 2 20081111 A 7200 ENGINE DOUG MD11 MD11F 3023600 NM GE CF6 CF680 30025 NE NR 3 FLAMED OUT A FDEA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 CE 21 584FE 48436 704338 ENGINE NR 3 FLAMED OUT DURING DESCENT AT APPROX HIGH 20'S. ON DEBRIEF CREW REPORTED RESTART WAS NORMAL AND ENGINE OPERA TED NORMAL REMAINDER OF FLIGHT, TROUBLESHOOTING NOW IN PROGRESS. 2 L 7 3 4F 4 F RT A22WE E13NE 20081114 NM 2008 11 14 08FDEA04838 1 20081110 A 5414 311N504631 SKIN BOEING 757 75723A 1384967 NM NR 1 PYLON MISREPAIRED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 WHILE REAMING THE -31 OTBD SKIN AND OTBD BATHTUB FITTING FOR THE NR 1 PYLON SIP MOD F- 5450-7-5003 A4 PT.5 1 HOLE WAS O VERSIZED TO 0.390 DIA AND COUNTERUNK FOR A BACB30NW12K(*) X FASTENER. COMPLIED WITH FEDEX EA NR F-5450-124034 11/07/08 AND REPAIRED OVERSIZED HOLE PER MAE EA NR 757-5451-16-A1814 REV, NOV 5,2008. NO FOLLOW UP ACTION REQUIRED. "MAJOR REP AIR". 2 L 7 2 4F RT A2NM 20081114 NM 2008 11 14 2008UALA06390 1 20081106 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 ROWS 45 - 55 LEFT SEAT EEL LIGHT INOP. REPLACED BATTERY. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081114 NM 2008 11 14 2008UALA06391 1 20081106 A 3397 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 AFT GALLEY FWD AND LEFT EMERGENCY LIGHTS INOP. REPLACED FEEDER CABLE. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081114 NM 2008 11 14 2008UALA06409 1 20081107 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHT INOP CEILING ROW 17. LAMP IS INOP. REPLACED LAMP. ALL CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20081114 NM 2008 11 14 2008UALA06411 1 20081105 A 3610 32153024 SHUTOFF VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE BLEED AIR SYS FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 215UA 30221 WITH RIGHT ENGINE BLEED SELECTED DO NOT GET GREEN BAR ON AIR PAGE TO OPERATE PACKS. PRSOV VALVE OPENS ONLY. STATUS MES SAGE R PRSOV BLEED. MAT MESSAGE 36-10380. FOUND R PRSOV MUSCLE LINE GALLED. REPLACED R PRSOV AND R PRSOV CONTROLLER. ENGINE RUN RIGHT BLEED OPENS AND CLOSES, PACKS DO NOT COME ON WITH RIGHT ENGINE BLEED. REPLACED MANIFOLD DUAL TEMP SENS OR (P/N 1150322-1). 2 L 7 2 4F 4 F RT T0001SE E46NE 20081114 2008 11 14 2008UALA06258 4 20081024 A 2565 S416T203153 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN BLOWN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 RT OFF-WING SLIDE DEPLOYED DURING RE-ACTIVATION PROCEDURE. FOUND RIGHT OFF WING SLIDE SPOILER OVERRIDE ACTUATOR BLOWN. REPLACED INFLATION CYLINDER. 2 L 7 2 4F 4 F RT A1NM E24NE 20081114 NM 2008 11 14 2008UALA06260 1 20081024 A 5610 5717623097 SLIDING WINDOW BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT CRACKED A UALA G O2 MASK DEPLOYED W INADEQUATE Q C DE DESCENT 1 WP 29 328UA 24148 CAPTAINS L2- SLIDING WINDOW CRACKED AT TOP OF DESCENT. REPLACED SLIDING WINDOW. TROUBLESHOT WINDOW HEAT. FOUND NO POW ER TO THE WINDOW. FOUND AND CORRECTED MIS-WIRED CAPTAIN'S SLIDER WINDOW. CORRECTED PER WD.30-41-00. OPS NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20081114 NM 2008 11 14 2008UALA06261 1 20081024 A 5320 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 820UA 898 DOOR 2R SILL REMOVED FOR CORROSION. MAJOR REPAIR ACCOMPLISHED. BEGAN PICKING UP HOLES ON NEW SILL PLATE DOOR 2R. FINI SHED INSTALLATION OF SILL PLATE FASTENER. 2 L 7 2 4F 4 F RT A28NM E40NE 20081114 NM 2008 11 14 SWAA086199 1 20081113 A 5610 589354314 WINDOW BOEING 737 7377H4 1384404 NM COCKPIT ARCED A SWAA K NONE O OTHER AP APPROACH 1 SW 29 230WN 34592 COCKPIT R1 WINDOW ARCED ON APPROACH. R&R R1 WINDOW PER MM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 USAA EMB08020 1 20081113 A 2510 1805003000 CABLE EMB ERJ190 ERJ190100IGW 3260408 NM FO SEAT OUT OF ADJUST A USAA K NONE O OTHER LD LANDING 1 EA 19 960UW 19000173 FLIGHT 1613, CLT-MSY - THE FIRST OFFICER'S SEAT DOES NOT LATCH IN PLACE AND SLIDES FORWARD WITHOUT RESTRAINT. MAINTENAN CE ADJUSTED THE LONGITUDINAL CABLE. 2 L 7 2 4F RT A57NM 20081114 NM 2008 11 14 USAA920081798 1 20080922 A 5312 6516300 BULKHEAD BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 C-18 CHECK, NR 6132091, CRACKED WEB, BS 178, LBL 15, WL 234. REPAIRED WEB, BS 178, LBL 15, WL 234 IAW B737SRM 53-10-08- 2R9, FIG 201. (K) 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 USAA920081805 1 20080918 A 5320 654580733 ANGLE BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 C-18 CHECK - NR 6131761, CRACKED ANGLE, BS 290, S11R. REPLACED ANGLE, BS290, S11R IAW SRM 51-40-02. (K) 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 USAA2008111492060 1 20081009 A 5311 6546551 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL - MAJOR REPAIR - C21 CHECK - NR 6062844, LEVEL 2 CORROSION ON FRAME AT BS 827, LBL 5, IN THE AFT CARGO COMPARTMENT. REPAIRED FRAME AT BS 827, LBL 5 IN THE AFT CARGO COMPARTMENT IAW B737 SRM 53-00-07-2R 8 FIGURE 201. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 USAA2008111492061 1 20081009 A 5330 65C35777 SKIN BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL - MAJOR REPAIR - C21 CHECK - NR 6139576, CORROSION ON FUSELAGE SKIN INTERIOR SURFACE AT BS 947.5, S19L. REPAIRED FU SELAGE SKIN AT BS 947.5, S19L IAW B737 SRM 53-00-01-2R 31. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 USAA2008111392055 1 20081113 A 5330 SKIN BOEING 737 737401 138449B NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 23885 CLT - MAJOR REPAIR - C4 CHECK - CRACKED FUSELAGE SKIN AT BS 745, S25L. REPAIRED FUSELAGE SKIN AT BS 745, S25L I/A/W B73 7 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 20081114 EA 2008 11 14 MASA2008111000767 1 20081110 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH 2939 PHX. CREW REPORTED THE AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING INOP. MX RESECURED A LOOSE CONNECTOR. 2 L 7 2 4F RT A21EA 20081117 EA 2008 11 17 MASA2008110300762 1 20081103 A 5270 PROXIMITY SWITCH CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT OUT OF ADJUST A MASA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 07 926LR 15026 ASH 2714 SBA-PHX. CAPTAIN REPORTED A RT FORWARD OVERWING EMERGENCY EXIT CAUTION AFTER LANDING. MX INSPECTED DOOR AND A DJUSTED PROXIMITY SWITCH. 2 L 7 2 4F RT A21EA 20081117 EA 2008 11 17 MASA2008110500764 1 20081105 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002D24 1390016 EA CABIN DISCHARGED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 925FJ 15025 ASH FLT 2649 BHM-CLT. ROW 15 L/R FLOOR LEVEL EMERGENCY LIGHTS & RT EXTERIOR 2ND EMERGENCY LIGHT INOP. MX REMOVED AND R EPLACED BATTERY PACK. 2 L 7 2 4F RT A21EA 20081117 SO 2008 11 17 C2XA08TY132 1 20081112 A 3397 7287580505 WIRE EMB 145 EMB145LR 3260212 SO LIGHT STRIP BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16911 145446 NR 1 EMERGENCY LIGHT STRIP ON THE FLOOR HAD BROKEN WIRES. REMOVED AND REPLACED LIGHT STRIP IAW EMB 145 AMM 33-50-12. A IRCRAFT STILL IN C-CHECK. 2 L 7 2 4T RT T00011AT 20081117 SO 2008 11 17 C2XA08TY129 1 20081109 A 3397 WIRE EMB 145 EMB145LR 3260212 SO COCKPIT CHAFED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14573 145638 EWR-CVG - COCKPIT READING LIGHTS CIRCUIT BREAKER POPPED WHEN USING CA SIDE YOKE LIGHT THAT CAUSED A SMOKE SMELL IN COCKP IT. MX FOUND A CHAFED WIRE ON CAPTAINS YOKE READING LIGHT. A/C WAS RELEASED IAW NEF CB 02 CAT D CONTROL NR 157869. 2 L 7 2 4T RT T00011AT 20081117 SO 2008 11 17 C2XA08SH143 1 20081111 A 5320 14530644401 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14952 145067 SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 38. MAINTENANCE REMOVED THE CORROSION A ND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10 FIG 202, STEP 2. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . 2 L 7 2 4T RT T00011AT 20081117 SO 2008 11 17 C2XA08SH139 1 20081108 A 5320 14523171003 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14952 145067 SHV - DURING C-CHECK CORRODED NUT PLATE HOLE ON OMEGA BEAM LAV AREA BETWEEN FRAME 60 AND 61 LT SIDE. REPAIRED LT OMEGA BEAM BETWEEN FR 60-61 AT NUT PLATE ARE IAW EC 5320-01430. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 20081117 SO 2008 11 17 C2XA08SH140 1 20081108 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14952 145067 SHV - DURING C-CHECK CORROSION ON LT OMEGA BEAM JUST ABOVE FR 20 CARBON CROSS BEAM. MX REPAIRED LT OMEGA BEAM AT FR 20 IAW EMB 145 SRM 53-00-10 FIG 201. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 20081117 NM 2008 11 17 KCSA081580 1 20081114 A 5347 SEAT TRACK BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 MAIN DECK SEAT TRACK FLANGE IS CORRODED AT STA 455, RBL 66. 2 L 7 4 4F RT A20WE 20081117 NM 2008 11 17 KCSA081575 1 20081113 A 5730 SKIN BOEING 747 747212B 1384886 NM RT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 RT WING LOWER SKIN CORRODED AT BOOST PUMP CUTOUT AT WS 682. 2 L 7 4 4F RT A20WE 20081117 NM 2008 11 17 KCSA081576 1 20081113 A 5320 CHANNEL BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 FLT DECK FLOOR CHANNEL CORRODED AT BS 273, LBL 24. 2 L 7 4 4F RT A20WE 20081114 NM 2008 11 14 CALA0801038 1 20081105 A 5347 146T5217 SEAT TRACK BOEING 767 767424ER 1385270 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76054 29449 CABIN BODY STATION 1241-1417 RBL 88 SEAT TRACK CROWN SLIP FOUND CORRODED. CABIN BODY STATION 1208-1428 RBL 88 SEAT TRAC K REPAIRED PER EC/RA 5320-01911. 2 L 7 2 4F RT A1NM 20081114 NM 2008 11 14 CALA0801039 1 20081106 A 5531 6547634502 RIB BOEING 737 737524 1384721 NM VERTICAL STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 VERTICAL STABILIZER LEADING EDGE RIB AT STATION 189.09 IS CRACKED ON RIGHT SIDE. REMOVED AND REPLACED CRACKED RIB AT ST ATION 189.09 PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801041 1 20081107 A 5531 65476404 RIB BOEING 737 737524 1384721 NM VERTICAL STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 VERTICAL STABILIZER LEADING EDGE RIB AT STATION 273.35 IS CRACKED ON RIGHT SIDE. INSTALLED REPAIR PER SRM 51-40-02 AND SRM 51-70-11. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801051 1 20081109 A 5315 141T5107 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 67157 30436 CABIN BODY STATION 303 FLOOR SUPPORT FOUND CORRODED BETWEEN LBL 17-41. BODY STATION 303 FLOORBEAM SUPPORT BETWEEN LBL 1 1 TO LBL 64 REPLACED PER SRM 53-00-51, REPAIR 1, FIG 201. HFEC NO CRACK FOUND. 2 L 7 2 4F RT A1NM 20081114 NM 2008 11 14 SWAA086173 1 20081112 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND CARGO BAY FLOOR SUPPORT BEAM CORRODED AT BETWEEN BS 772 TO BS 774, LBL 8. REPAIRED BE AM PER SWA EA. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086174 1 20081112 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND CARGO BAY FLOOR SUPPORT BEAM CORRODED AT BETWEEN BS 772 TO BS 774, RBL 8. REPAIRED BE AM PER SWA EA. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801028 1 20081103 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 FRAME CRACKED AT STATION 440 ABOVE S-9L. REPAIRED FRAME PER EA 5310-04498, OP 2. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 ASAA0843720 1 20081029 A 5320 654587545 SILL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 R1 DOOR CUTOUT INNER CHORD MOP SILL IS CORRODED. REMOVED CORRODED MOP SILL AND INSTALLED NEW MOP SILL IAW B737 400 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 08FDEA04697 1 20081104 A 5310 65595341 BEAM BOEING 727 7272D4 138407U NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 LOWER FUSELAGE DELTA BEAM LT LOWER CHORD IS CRACKED ON LOWER INBD FLANGE AT BS 740 TO 743 LBL 6 INCHES. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 CALA0801064 1 20081111 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 BODY STATION 747 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8L AND STR 9L. REPAIRED FRAM E BODY STATION 747 AT AC RAIL BRACKET BETWEEN STR 8L AND STR 9L PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 ASAA0873693 1 20081031 A 5320 141A541012 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 PAX CABIN FWD FLOOR INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 08FDEA04746 1 20081105 A 5753 692288221 BRACKET BOEING 727 7272S2F 1384O81 NM FLAP TRACK CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 NR 4 FLAP TRACK FAIRING BRACKET CLIP IS CRACKED LOCATED ON OTBD SIDE, 20 INCHES FROM FWD END VERIFIED MATERIAL AS 7075-T 6-.063 REF DWR 69- 22882. REPLACEMENT MATERIAL SAME AS ORIGINAL, FABRICATED BRACKET FOR OTBD SIDE OF NR 4 FLAP TRACK PE R DWR 69-22882. TREATED BRACKET REF MM 51-20-021-7 AND PRIMED REF MM 51-20-031-7 AND INSTALLED BRACKET ON FLAP TRACK RE F SRM 51-30-2. MARKED BRACKET WITH FX 69-22882-21 REF GMM 7-0-001. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 SWAA086187 1 20081112 A 5311 6547958 FRAME BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STUB FRAME CORRODED AT BS 793, STR 27R. REPAIRED STUB FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081114 SO 2008 11 14 RAIA2008111200001 1 20081107 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 836HK 145695 DURING PREFLIGHT INSPECTION, A SMALL PIECE OF THE EMERGENCY LIGHTING STRIP CAME LOOSE. MAINTENANCE RESECURED THE LOOSE S TRIP OF EMERGENCY LIGHTING. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081114 SO 2008 11 14 RAIA2008111200003 1 20081110 A 7500 DUCT EMB 145 EMB145LR 3260212 SO BLEED AIR LOOSE A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 815HK 145048 DURING TAXI TO THE GATE, CREW REPORTED A BURNING ODOR IN THE CABIN AND COCKPIT. MAINTENANCE RESECURED A BLOWN PACK NR 2 SUPPLY DUCT UNDER THE CABIN FLOOR AND PERFORMED SEVERAL OPS CHECKS OF THE AIR CONDITIONING SYSTEM WITH NO ADDITIONAL DEF ECTS NOTED. MAINTENANCE ALSO PERFORMED ADDITIONAL OPS CHECKS OF THE WINDSHIELD HEATING SYSTEM, RECIRCULATION FANS, AND T HE CABIN LIGHTING WITH NO ADDITIONAL DEFECTS. 2 L 7 2 4T RT T00011AT 20081114 NM 2008 11 14 2008UALA06398 1 20081106 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 DOOR 4L, LWR GATE CORRODED. INSTALLED NEW GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 EU 2008 11 14 08FDEA04853 1 20081111 A 5321 A5327996300200 FLOOR PANEL AIRBUS 310 A310324 3930206 EU CARGO BAY DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 BULK CARGO PIT FLOOR PANEL NR 161 GF IS DAMAGED. FABRICATED NEW PANEL IAW DWG. SRZ 25-005. FABBED TOP SHEET IAW SRZ DW G. 25-005. ATTACHED TOP SHEET IAW DWG SRZ 25-005. PART MARKED IAW GMM 7-0-1000. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 08FDEA04793 1 20081107 A 5330 651842016 SKIN BOEING 727 727225 1384077 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 469FE 21581 PREVIOUS REPAIR AT STA 188 STR 26L HAS 1 DENT AND NUMEROUS IMPROPERLY INSTALLED FASTENERS. REMOVED DOUBLER, FABRICATED NEW DOUBLER AND FILLER AND INSTALLED REPAIR PARTS IAW SRM 51-30-5, 53-30-2 AND 53-30-3. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04798 1 20081108 A 5340 65C1612910 MOUNT BOEING 727 7272S2F 1384O81 NM E/E BAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 FWD ELECTRONIC BAY WEATHER RADAR MOUNT SHELF, LT AFT ATTACH BRACKET CRACKED VERIFIED MATERIAL ID. FABRICATED DOUBLER AN D NEW LIGHT SWITCH BRACKET. REMOVED ELECTRONIC BAY LIGHT SWITCH BRACKET, STOP DRILLED CRACKS, TREATED, PRIMED AND PAINT ED DOUBLER AND NEW LIGHT SWITCH BRACKET. INSTALLED DOUBLER AND NEW LIGHT SWITCH BRACKET, REF SRM 51-20-1 PG 13, SRM 51- 40-3 PG 1/4, SRM 51-30-2 PG 8/14, REF DOC 66-14849-2, DOC 65C16129-10, REF MM 51-20-151 PG 1, REF SRM 51-10-1 PG 13 REF NDT MAN PART 6, 51-00-00 FIG 23 THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04799 1 20081108 A 5720 691676512 WEB BOEING 727 7272S2F 1384O81 NM ZONE 300 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 VERTICAL STRAP UPPER END, ELEVATOR FEEL CONTROL UNIT MOUNT PLATFORM LEFT AND RIGHT VERTICAL WEBS CRACKED AT L/E FASTENER S. VERIFIED VERT WEBS CRACKED. REMOVED LT AND RT VERTICAL WEBS, FABRICATED, TREATED, PRIMED AND INSTALLED LT AND RT NE W VERTICAL WEBS, REF SRM 51-10-2 PG 2, SRM 51-30-2 PG 1-4, BOEING DWG 69-16765 ID:0001, THIS IS CLASSIFIED AS A MINOR RE PAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04800 1 20081108 A 5720 6521795324 SKIN BOEING 727 7272S2F 1384O81 NM TRACK FAIRING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 NR 6 FLAP TRACK HINGE FAIRING CRACKED ON LOWER SKIN AT L/E. FABRICATED DOUBLER AND FILLER FOR NR 6 FLAP TRACK PER DWG 6 5-21795 PG 1 2024-T3 .040 FILLER 2024-T3 .050. DOUBLER INSTALLED, TREATED AND PRIMED AND PAINTED REF SRM 51-10-2 PG 2 -7. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04801 1 20081108 A 5712 640834219 RIB BOEING 727 7272S2F 1384O81 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 RT WING LE RIB LWR CHORD IS CRACKED IS CRACKED FSS 119, 4 INCHES-18 INCHES FROM SPAR VERIFIED MATERIAL ID FOR REPAIR ANG LE AND FILLER. CUT OUT DAMAGE. FABRICATED REPAIR ANGLE AND FILLER. LOCATED, DRILLED AND TRIMMED REPAIR ANGLE. HEAT T REATED REPAIR ANGLE. TREATED AND PRIMED REPAIR ANGLE AND FILLER. INSTALLED FILLER, REPAIR ANGLE AND RELATED PARTS, REF SRM 51-30-2, DWG 64-08342-19, REF SRM 51- 10-1 PG 1, REF SRM 51-40-3 PG 3-13 REF MM 51-20-151-7 PG1. THIS IS CLASSIFI ED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04806 1 20081108 A 5315 655756718 FLOORBEAM BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 UNDERSIDE OF AFT PIT FLOOR SUPPORT CORRODED AT STA 1166 RBL 11-12. SPLICED IN NEW SUPPORT SECTION REF SRM 53-10-5 AND 5 1-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04808 1 20081108 A 5315 655756774 FLOORBEAM BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 AFT PIT FLOOR SUPPORT CORRODED ON UNDERSIDE AROUND NUTPLATE STA 1166 LBL 3-4. SPLICED IN NEW SUPPORT SECTION REF SRM 53 -10-5 AND 51-30-2. THIS IS CLASSIFIOED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04809 1 20081108 A 5315 655756716 FLOORBEAM BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 AFT PIT FLOOR SUPPORT CORRODED ON UNDERSIDE AROUND NUTPLATE STA 1166 RBL 3-4. SPLICED IN NEW SUPPORT SECTION REF SRM 53 -10-5 AND 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04810 1 20081108 A 5315 655756729 FLOORBEAM BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 AFT PIT FLOOR SUPPORT CORRODED ON UNDERSIDE AROUND NUTPLATE STA 1166 RBL 7-8. SPLICE IN NEW SUPPORT SECTION REF SRM 53- 10-5 AND 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04811 1 20081108 A 5315 65575716 FLOORBEAM BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 AFT PIT FLOOR SUPPORT ON UNDERSIDE AROUND NUTPLATE STA 1166, NO CENTER LINE. SPLICED IN NEW SUPPORT SECTION REF SRM 53- 10-5 AND 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04813 1 20081108 A 5315 652084010 FLOORBEAM BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 AFT FLOORBEAM CORRODED RBL 27 AND RBL 43 NUTPLATES STA 1166 WL 208. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04816 1 20081109 A 5712 640834219 RIB BOEING 727 7272D4 138407U NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 RT WING L/E RIB UPPER CHORD HAS SEVERAL CRACKS ALONG EXISTING REPAIRS AT 9 INCHES-20 INCHES FROM SPAR, FSS 122. REMOVED REPAIR, FABRICATED REPAIR DOUBLER REF SRM 51-40-3 FIG 1. INSTALLED RT WING LF RIB CHORD REPAIR REF SRM 51-40-3 FIG 1. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04818 1 20081109 A 5320 6523638 STRAP BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FUSELAGE UPPER LOBE INTERIOR STRUCTURE FRAME SUPPORT BETWEEN STA 500 AND STA 520 RBL 45 CORRODED. REMOVED OUTBOARD BLOW OUT PANEL FRAME SEGMENT TO ACCESS CORROSION UNDER THE NUT PLATES, ALSO REMOVED ALL NUT PLATES ON FRAME SUPPORT STRAP FR OM STA 520 TO STA 552, REF SRM 51-30-2, P1-27. REMOVED CORROSION FROM UNDER ALL NUT PLATES, REF SRM 51-10-1,P1-16. FOU ND CORRODED OUT OF LIMITS AT STA 520, USED POINT MIKE NR IN17-0112 CAL DUE DATE 12-11-08. REF: SRM 53-10-2, P.42G AND P. 40E. FABRICATED REPAIR PART REF: SRM 51-40-2,P.5. TREATED, PRIMED REPAIR. REF: SRM 51-10-2. INSTALLED REPAIR. REF SR M 51-30-2, P.1-27, STA 520 FLOORBEAM REPAIR TRANSFERED TO NR N00701. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04819 1 20081109 A 5712 640834220 RIB BOEING 727 7272S2F 1384O81 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 A86-2470, RT WING LE RIB UPPER CHORD IS CRACKED AT EXISTING REPAIR FSS 119, 8 INCHES-18 INCHES FROM SPAR (MKD). INSTALL ED AND FABRICATED RT WING LE UPPER CHORD AND SPLICE AT FSS 119. REFS BOEING DWG 64-08342-20, SRM 51-40-03, SRM 51-30-02 . TREATED AND PRIMED PARTS REF SRM 51-10-2 PGS 1, 2. CLASSIFIED MAJOR REPAIR. 2 L 7 3 4F A3WE 20081114 SO 2008 11 14 C2XAO8RI164 1 20081023 A 2611 WARNING SYSTEM EMB 145 EMB145XR 3260214 SO SMOKE WARNING MALFUNCTIONED A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 27 11176 14500881 FLIGHT 2761 - EWR - FLIGHT CREW REPORTED LAV SMOKE INDICATION ON EICAS DURING FLIGHT. EWR MX PERFORMED OPERATIONAL CHEC K OF LAVATORY SMOKE INDICATION SYSTEM AND COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081114 NM 2008 11 14 K11A2008111272205 1 20080918 A 5311 FRAME BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 STA 312 FRAME UPPER CHORD ASSY UPPER AND LOWER SURFACE CORRODED WHERE NLG STEERING CABLE PULLEY BRACKET ATTACHES AT LBL 32. CORROSION 2 X 2 INCHES. 2 L 7 3 4F RT A3WE 20081114 NM 2008 11 14 2008UALA06399 1 20081106 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 DOOR 2L NEEDS REPAIR DOUBLER AT UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 NM 2008 11 14 2008UALA06388 1 20081106 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 SEAT 20 RIGHT EMERGENCY LIGHT INOP. FOUND LIGHT INOP. REPLACED SEAT 20 RIGHT EMERGENCY LIGHT. OPS CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20081114 NM 2008 11 14 2008UALA06389 1 20081106 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 EMERGENCY LIGHT ROW 41 RT INOP. FOUND LIGHT INOP. REPLACED SEAT 41 RIGHT EMERGENCY LIGHT. OPS CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20081114 NM 2008 11 14 USAA920081802 1 20080925 A 5320 69366564 INTERCOSTAL BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 C18-CHECK - NR 6127756, CRACKED INTERCOSTAL, BS927 - BS947, BL 0. REPLACED INTERCOSTAL, BS927-BS947, BL 0 IAW SRM 51-40 -02. (K) 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 USAA920081804 1 20080918 A 5320 6544580734 ANGLE BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 C-18 CHECK - NR 6131710, CRACKED ANGLE, BS 290, S10R. REPLACED ANGLE, BS 290, S10R IAW SRM 51-40-02. (K) 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 MASA2008111300770 1 20081113 A 3350 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 454YV 454 ASH 7177 DEN. MX REPORTED CENTER AISLE CEILING EMERGENCY LIGHT IS INOPERATIVE. MX REMOVED AND REPLACED BATTERY POWER S UPPLY. 2 H 7 2 4T RT A13NM 20081117 NM 2008 11 17 KCSA081574 1 20081113 A 5320 TEE FITTING BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 FUSELAGE CREASE BEAM OUTER TEE CHORD CRACKED AT AFT SIDE OF BS 980 FRAME, STR 5R. 2 L 7 4 4F RT A20WE 20081117 NM 2008 11 17 KCSA081582 1 20081116 A 5313 STRINGER BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 STR 2L CORRODED AT BS 2040. 2 L 7 4 4F RT A20WE 20081117 NM 2008 11 17 KCSA081585 1 20081116 A 5712 RIB BOEING 747 747212B 1384886 NM LT WING CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 LT WING RIB LOWER CHORD CRACKED AT WS 1516, 23 INCHES AFT OF FRONT SPAR. 2 L 7 4 4F RT A20WE 20081117 NM 2008 11 17 SWAA086200 1 20081113 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 203WN 32483 FOUND FWD EEPLS COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086201 1 20081113 A 2560 P4010021 BATTERY PACK BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED MV2 CHECK, FOUND FWD O/B FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086208 1 20081113 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 2008UALA06339 1 20081031 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 778UA 26940 EEL STRIP AT SEAT 2E IS LOOSE WITH WIRES SHOWING. SECURED LIGHT, CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081107 WP 2008 11 7 I5HA0858005G 1 20080717 A 5320 3403110207 CHANNEL CVAC 340 34031 2422704 WP ALLSN 501D 501D13 03004 GL ALLSN A6441 A6441FN606 GL FUSELAGE DAMAGED A I5HA O OTHER O OTHER NR NOT REPORTED 1 GL 25 581P 29 DURING A STORM A CARGO CAN (ULB) WAS THROWN INTO THE RT SIDE OF ACFT. THE RT PROPELLER WAS ALSO STRUCK A GLANCING BLOW. THERE WAS SIGNIFICANT DAMAGE TO THE SKIN AND SUPPORT STRUCTURE BENEATH THE SKIN. THERE WAS DAMAGE TO WIRING IN THE AREA. THE NOSE STEERING ACTUATOR WAS ALSO DAMAGED. DAMAGE AREA WAS BETWEEN FUSELAGE STATIONS 72 TO 125 AT APPROXIMATELY BETWE EN STRINGERS 11 AND 3. THE PROPELLER AND REDUCTION GEARBOX WERE REMOVED AND INSPECTED. NO DAMAGE TO EITHER. ACFT WAS REP AIRED AND THE ACFT TEST FLOWN. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4R 4 T 6A6 E282 6 C P898 20081107 NE 2008 11 7 DL76L081474 2 20081030 A 7200 PW40603 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 DEFECTIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 180DN 66252 25985 724314 FAILED EA 51-470869-12 REV B MGB OIL NOZZLES INSP. REPLACING NR 1 ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081110 WP 2008 11 10 AALA200802550 1 20080925 A 5310 BEAM DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 CRACK FOUND ON LT J BEAM REPAIR DOUBLER IN NG WW. REPLACED REPAIR DOUBLER IN ACCORDANCE WITH AARD 53-10-00-04. 2 L 7 2 4F RT A6WE 20081110 NM 2008 11 10 ASM2008F00007 1 20081022 A 5753 ARC1984502 HINGE DOUG MD11 MD11 3023602 NM RT TE FLAP CORRODED W ASMF O OTHER O OTHER NR NOT REPORTED 1 SW 23 742BC 48758 AFTER REWORK OF RT OB FLAP, IB AFT HINGE PN ARC 1984-502, OB PIVOT LUG BORE HAS BEEN FOUND OUT OF LIMITS PER CMM 57-52-0 4 PAGE 624 AND 625. FOUND 1.162" INSTEAD OF 1.150". NR 1-1032193304-2 APPROVE TO INSTALL AN OS BUSHING. 2 L 7 3 4F RT A22WE 20081110 WP 2008 11 10 AALA200802551 1 20080925 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 1437 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 CRACK FOUND ON AFT FUSELAGE SKIN AT STATION 1437 BETWEEN LONGERONS 2 RT AND 3 RT. INSTALLED DOUBLER IN ACCORDANCE WITH AARD 53-30-00-02. 2 L 7 2 4F RT A6WE 20081110 EA 2008 11 10 SWIA200820274 1 20080629 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 913SW 7597 INBOARD AND OUTBOARD CLIPS AT STA 484 UNDER PANEL 261DLF CRACKED (C-CHECK). REPLACED PER REO. 2 L 7 2 4F RT A21EA 20081110 WP 2008 11 10 08FDEA04718 1 20081105 A 5754 NRB6225507 ANGLE DOUG DC10 DC1030F 3023504 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 LH WING SLATS FOUND CRACK ON ANGLE OUTBOARD SIDE NR 2 SLAT. 2 L 7 3 4F RT A22WE 20081110 NM 2008 11 10 08FDEA04719 1 20081105 A 5230 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 593FE 48551 DURING OPEN-HOLE HFEC INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 2 FOUND WI TH CRACK INDICATIONS AT HOLES A, B, C AND D. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II. BUSHING REPAIR CARRI ED OUT AT BOLT HOLES AS PER SRM 53-50-00, FIGURE 10, VOLUME I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081110 EA 2008 11 10 MAS2008F00092 1 20080929 A 5420 BAFFLE CNDAIR CL600 CL6002D24 1390016 EA LT NACELLE DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 924FJ 15024 LT LOWER TRANCOWL BAFFLE BROKEN. REPLACED TRANSLATING COWL. 2 L 7 2 4F RT A21EA 20081110 EU 2008 11 10 SIM2008F00029 1 20081003 A 5311 REPAIR SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 384AE 340B384 DURING A HMBV INSP, AN OLDER REPAIR ON THE GALLEY FRAME AT FS 258 WAS FOUND TO BE CORRODED. REMOVED THE PREVIOUS REPAIR FILLER. FABRICATED A NEW FILLER. DRILLED, CLEANED AND TREATED NEW PART. REPAIR DONE IAW SAAB SRM (79LKS 3079 REV 50) CHAPTER 53-70-30. AC RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 20081110 NM 2008 11 10 USAA920081829 1 20080929 A 5330 6518420 SKIN BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, FUSELAGE SKIN CRACKED AT LT COCKPIT WINDOW POST BS 219. REPAIRED FUSELAGE SKIN AT LT COCKPIT W INDOW POST BS 219 IAW B737 SRM 53-10-01 REPAIR 10. 2 L 7 2 4F RT A16WE 20081110 CE 2008 11 10 COEA0801728 1 20081006 A 3610 1H1014 CONTROL VALVE CESSNA 208 208B 2073701 CE BLEED AIR SYS FAILED E COEA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B P SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION CL CLIMB 1 NM 13 728FX 2536 208B0471 FLT NR 7699 SEA TO BLI, DURING CLIMB OUT AT APPROXIMATELY 1000FT AGL THE BLEED AIR HEAT SYSTEM WAS SELECTED ON. AFTERWA RD THE COCKPIT STARTED FILLING WITH BLACK SMOKE ALONG WITH A BURNT RUBBER ODOR. THE PILOT PIT ON HIS OXYGEN MASK AND TU RNED OFF THE BLEED AIR HEAT. NEITHER THE CREW NOR THE FIRE WARNING SYSTEM DETECTED ANY FIRE. THE AC RETURNED TO SEA SA FELY. TROUBLESHOOTING FOUND THE PROBLEM ORIGINATED FROM THE BLEED AIR FLOW CONTROL VALVE. R&R THE BLEED AIR FLOW CONTR OL VALVE. 1 H 7 1 3T A37CE 20081112 WP 2008 11 12 DHLA200800105 1 20080930 A 3350 5708458505 BATTERY PACK DOUG DC8 DC873 302199C WP EMERGENCY LIGHTS INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 GL 05 803DH 4499 1442 46123 EMERGENCY LIGHTS WILL NOT TEST ON PREFLT, ACFT GROUNDED. R&R BATTERY PACK ASSY, OPS CHECKED GOOD IAW 33-50-1. 2 L 7 4 4F RT 4A25 20081112 WP 2008 11 12 AALA200802341 1 20080909 A 3233 ACTUATOR DOUG DC9 DC982 3022082 WP NLG MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 584AA 53247 INFLT T564, DURING CLIMB. CREW REPORTED UNSAFE NLG INDICATION ON RETRACTION. RECYCLED AND RECEIVED 3 GREEN LIGHT FOR NLG DOWN. ON RETRACTION RECEIVED UNSAFE LIGHT AGAIN. LANDED WITHOUT INCIDENT. REPLACED NLG UP PROXIMITY SENSOR ELECTRO NIC UNIT AS PRECAUTION. REPLACED NLG SHOCK STRUT AND NLG RETRACTION ACTUATOR. GROUND CHECKED NORMAL. 2 L 7 2 4F A6WE 20081117 NM 2008 11 17 SWAA086209 1 20081113 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086211 1 20081112 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND AFT CABIN CENTER EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086212 1 20081113 A 5311 6546540 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STUB FRAME CRACKED AT BS 639, LBL 45, WL, 206. REPAIRED STUB FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086213 1 20081113 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 4R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086214 1 20081113 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND RT CREASE BEAM CORRODED AT BS 291. REPAIRED CREASE BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086238 1 20081113 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 30544 DURING SCHEDULED HC1 CHECK, LT AFT GALLEY BATTERY PACK FAILED CAPACITY TEST 16. REMOVED AND REPLACED BATTERY PACK PER M M. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086239 1 20081113 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 30544 DURING SCHEDULED HC1 CHECK, RT AFT GALLEY BATTERY PACK FAILED CAPACITY TEST 16. REMOVED AND REPLACED BATTERY PACK PER M M. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 UPS08M53873 1 20081108 A 5320 AJC70135 TORQUE BOX DOUG MD11 MD11F 3023600 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 255UP 48404 INSPECTION TYPE:N/A WHILE ACCOMPLISHING EO MD-11-2820-14180-K, A CRACK 0.75 INCHES WAS DISCOVERED AT STATION 2014.987 ON UPPER TORQUE BOX WEB. CRACK OUT OF LIMITS PER SRM 53-40-00 VOLUME 1 FIGURE 24. REPAIRED CRACK PER EO MD11-5310-31131- A. REPAIR WAS MAJOR REPAIR. 2 L 7 3 4F RT A22WE 20081117 EU 2008 11 17 UPS08153874 1 20081028 A 5321 B5327077900000 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 142UP 0825 INSPECTION TYPE:1C3C MAIN CARGO DECK FLOOR PANEL 251SJ HAS FIELD REPAIRS. REPAIRED MAIN CARGO DECK FLOOR PANEL 251SJ RE F A300-600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081117 EU 2008 11 17 UPS08153875 1 20081028 A 5321 B5327077400300 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 142UP 0825 INSPECTION TYPE:1C3C MAIN CARGO DECK FLOOR PANEL 252QJ HAS FIELD REPAIRS. REPAIRED MAIN CARGO DECK FLOOR PANEL 252QJ RE F A300-600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081117 EU 2008 11 17 UPS08153865 1 20081028 A 5753 A57960306200 DOUBLER AIRBUS A300 A300F4622R 3930360 EU TE FLAP CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 142UP 0825 INSPECTION TYPE:1C3C LT WING T/E CTR FLAP UPPER SKIN INBOARD. REPAIR DOUBLER CHAFED AS MARKED. REMOVED, FABRICATED AND REPLACED LEFT WING T/E CENTER FLAP UPPER SKIN I/B REPAIR DOUBLER REF A300-600 SRM 57-50-00 PARA 4E AND FIG 205. 2 L 7 2 4F RT A35EU 20081117 WP 2008 11 17 UPS08853863 1 20081002 A 5320 CUSP WEB DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV EVALUATION AND DISPOSITION REPAIR EFN 70219971240 ORIGINAL NR 750802 CUSP MEMBRANE AT TRACK I AND AT A FUSELAGE STATION NOT DEFINED ON THE NON-ROUTINE IT MAY BE A REPAIR LOCATED BETWEEN THE REPAIR AT FS 1050 AND 1250. IN STALLED DOUBLER IAW DC8 SRM 53-02-00 FIG 25. 2 L 7 4 4F RT 4A25 20081118 EA 2008 11 18 ASOA200801496 1 20081113 A 2760 WARNING SYSTEM CNDAIR CL600 CL6002C10 1390015 EA SPOILER SYS ACTIVATED A ASOA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SO 27 741EV 10155 OUTBOARD SPOILERON MESSAGE, O/B FLT SPOILER CAUTION MESSAGE. EMERGENCY DECLARED. FLT 5610 DEL 107 MINS. 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 ASOA200801498 1 20081113 A 5230 ANGLE CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 927EV 7844 CARGO DOOR BEAM AFT BOTTOM ANGLE AT THE REAR PRESSURE BULKHEAD IS CRACKED .5 INCH LONG IN O/B RADIUS. REMOVED CRACKED B RACKET FROM CARGO DOOR BEAM/AFT BULKHEAD. LOCATED, DRILLED & INSTALLED NEW SERVICEABLE BRACKET. ALL WORK PERFORMED IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 ASOA200801499 1 20081113 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 927EV 7844 FS 280 LBL 9 O/B CLIP CRACKED. REPLACED O/B CLIP FS 280, RBL 9 IAW CRJ 200 SRM 51-40-11 AND SRM 51-42-21. 2 L 7 2 4F RT A21EA 20081118 NM 2008 11 18 2008UALA06416 1 20081107 A 3350 78671 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 502UA 24623 EMERGENCY LIGHTS AT SEAT 15C AND 18C ARE INOP. REMOVED BOTH LIGHTS FROM THE SEATS. REPLACED 2EA LIGHT ASSYS. 2 L 7 2 4F 4 F RT A2NM E17NE 20081112 NM 2008 11 12 AALA200802321 1 20080714 A 3350 D71701100 BATTERY PACK BOEING 737 737823 13844BZ NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 920AN 29521 AFT EMERGENCY LIGHT BATTERY PACK FAILED FUNCTIONAL TEST. REPLACED BATTERY PACK. GROUND CHECKED NORMAL. 2 L 7 2 4F RT A16WE 20081112 NM 2008 11 12 DHLA2008745639 1 20080905 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN FLOORBEAM UPPER CHORD WITH CORROSION AT BS 400 RBL 10. REPAIRED FLOORBEAM UPPER CHORD AT BS 4 00 BETWEEN RBL 2 AND RBL 19 IAW B727 SRM 53-10-8 FIG 8. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745643 1 20080902 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT BS 720A AT S-8R FRAME WITH DOUBLE HOLES. REPAIRED FRAME SECTION AT BS 720A BETWEEN S-7R AN D S-9R IAW B727 SRM 53-10-4 FIG 2. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745670 1 20080906 A 5730 SKIN BOEING 727 727224 1384076 NM RT WING CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 RT WING REAR SPAR SECTION LOWER SKIN WITH CORROSION BETWEEN WS 470 TO WS 480. REPAIRED RT WING LOWER SKIN AT REAR SPAR AND STIFFENER 4 FROM WS 472 TO WS 491 IAW COOPESA EO COO-2-57-324-08. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745671 1 20080913 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE E/E COMPARTMENT CHORD AND FRAME AT INTERSECTION WITH NLG WHEEL WELL LT SIDE ON STA 294.5 BETWEEN S-26L AN D S-27L ANGLES WITH LIGHT CORROSION. REPAIRED FUSELAGE FRAME ANGLE SECTION AT BS 294 BETWEEN S-26L AND S-27L DUE TO COR ROSION IAW B727 SRM 51-40-1 FIG 1. REPLACED FUSELAGE LEFT SIDE CHORD SECTION FROM BS 282 TO BS 360 WL 150 S-27L IAW BOE ING DWG 65-18415 REV U DTD 12/15/77 AND 65-18420 REV M DTD 10/22/81. 2 L 7 3 4F A3WE 20081112 EA 2008 11 12 COMA0860412 1 20081005 A 5311 601R53612827 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 967CA 30355 7134 FRAME AT FS 718 LT SIDE BETWEEN STR 10R AND 11R IS CRACKED. REPAIRED IAW SERVICE BULLETIN 601R-53-055 AND REO 601R-53-6 1-2827. 2 L 7 2 4F RT A21EA 20081112 NM 2008 11 12 USAA920081811 1 20080918 A 5320 654580730 ANGLE BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN - MAJOR REPAIR - C18 CHECK, CRACKED ANGLE, BS 290, S12R. REPLACED ANGLE, BS 290, S12R IAW B737 SRM 51-40-02 AND BOI ENG DWG 65-45807. 2 L 7 2 4F RT A16WE 20081112 EU 2008 11 12 USAA920081810 1 20081005 A 2160 D2127405700600 DUCT AIRBUS 320 A320232 3930326 EU CABIN TEMP MALFUNCTIONED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 642AW 584 FLT 0468 CMH-PHX, AFTER TAKEOFF, CABIN TEMPERATURE CLIMBED TO 105 DEGREES (FORWARD) & 102 DEGREES (AFT). A/C PACKS TEMP ERATURE WERE NORMAL. SELECTED HOT AIR TO OFF & NO CHANGE. FLT ATTENDANT SMELLED ELECTRICAL TYPE ODOR. AC RETURNED TO CMH. MAINTENANCE REMOVED AND REPLACED DUCT NEAR RECIRCULATION FAN CHECK VALVE. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081112 EA 2008 11 12 COMA0860408 1 20081006 A 5330 601R3500469 DOUBLER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 967CA 7134 STA 640 RT SIDE BONDED DOUBLER IS CRACKED. REPAIRED STA 640 RT SIDE BONDED SKIN PER CRJ REO 601-53-61-506. 2 L 7 2 4F RT A21EA 20081112 NM 2008 11 12 I5P2008F00000 1 20081003 A 3411 BAC1130BC060174 STATIC LINE BOEING 727 727212 138407G NM PITOT/STATIC SYS KINKED D I5PA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 15 86425 21459 AC DEPARTED AT 1530L AND AIR RETURNED AT 1557L DUE TO CAPTS AND STANDBY A/S INDICATOR 40 TO 50 KNOTS LESS THAN COPILOTS (VERY SLOW TO RESPOND). UPON FURTHER TROUBLE SHOOTING, FOUND KINKED STATIC LINE BEHIND CAPTS VSI WHICH LINKS TO THE CA PT AND STANDBY A/S INDICATOR. REPOSITIONED AND STRAIGHTENED LINE AND R&R CADC AS PRECAUTION, CHECK GOOD. AFTER REVIEW FROM THE CAPTAIN AND FE ACFT WAS CLOSED OUT AND DEPARTED AT 0435L. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 USAA920081836 1 20081007 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST UK UNKNOWN 1 EA 19 823AW 1463 FLT 295 - LAS-MSP, BOTH FLASHLIGHTS ON FLT ATTENDANT SEAT ARE INOPERATIVE. R&R BOTH BATTERIES. OPS CHECKS WERE GOOD. 2 L 7 2 4F RT A28NM 20081112 NM 2008 11 12 DHLA2008745609 1 20080912 A 5711 SPAR BOEING 727 727224 1384076 NM RT WING CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 RT WING SPAR AT WBL 164.5 LOWER CHORD WITH CORROSION. REPAIRED RIGHT WING FRONT SPAR LOWER CHORD IAW B727 SRM 57-10-6 F IG 2 DETAIL II. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745611 1 20080907 A 5322 SHEAR TIE BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT BS 720F BETWEEN S-25R AND S-27R SHEAR TIE WITH CORROSION. REPLACED SHEAR TIE AT BS 720F BETWEEN S-25R AND S-26R IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745618 1 20081012 A 5313 STRINGER SPLICE BOEING 727 727224 1384076 NM FUSELAGE MISREPAIRED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 680 S-27L WITH IMPROPER SPLICE. REPLACED FUSELAGE SLICE SECTION AT S-27L AT BS 680 IAW B727 SRM 51-10-1 PARA 7A. REPAIRED S-27L FROM BS 680 TO BS 720+16 IAW B727 SRM 53-10-3 FIG 1 DETAIL 1. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745619 1 20081017 A 5320 STRAP BOEING 727 727224 1384076 NM AFT CARGO BAY CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 200665 LOWER FUSELAGE AFT CARGO COMPARTMENT STABILIZER STRAP WITH CORROSION FROM BS 1110 TO BS 1130 BL 0. REPLACED STABILIZER STRAP FROM BS 1010 TO BS 1166 BL 0 IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081107 EA 2008 11 7 ASOA200801430 1 20081031 A 5210 INTERCOSTAL CNDAIR CL600 CL6002C10 1390015 EA ASD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 INTERCOSTAL CRACKED INSIDE ASD AFT ACCESS PANEL 832BR. REMOVED AND REPLACED INTERCOSTAL IN ACCESS PANEL 832BR IAW CRJ 7 00 SRM 51-42-06 AND 51-42-21. SUPPLEMENTAL-SDR CLOSED 11/17/2008. 2 L 7 2 4F RT A21EA 20081107 EA 2008 11 7 REX2008F00051 1 20081029 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA OUT OF RIG A REXA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 25 8907A 7907 FLAPS FAILED ON APPROACH WHEN SELECTED TO 30 DEGREES. VREF ADJUSTED AND APPROACH CONTINUED WITH UNEVENTFUL LANDING. RE SET FLAPS AND PERFORMED RIG CHECK PER BOMBARDIER AMM. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081107 WP 2008 11 7 AALA200802573 1 20080924 A 5340 9936533057 BRACKET DOUG DC9 DC983 3022083 WP GALLEY TIE DOWN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 TUL GALLEY INBD TIE DOWN BRACKET CORRODED BEYOND LIMITS AT STATION 217. REPLACED TIE DOWN BRACKET IN ACCORDANCE WITH AA RD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081107 NM 2008 11 7 UPS08M53849 1 20081024 A 5720 STRUCTURE DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:3C LT WING TELESCOPING DUCT CUTOUT UPPER O/B CORNER CRACKED. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG 43 SHEET 5. 2 L 7 3 4F RT A22WE 20081107 WP 2008 11 7 UPS08853857 1 20081004 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK PER DC8 MM 33-50-01-2. OPS CHECKS GOOD. 2 L 7 4 4F RT 4A25 20081107 NM 2008 11 7 SWAA086023 1 20081101 A 5754 65C26686 SKIN BOEING 737 7375H4 138449D NM LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 DURING SCHEDULED SPV CHECK, FOUND RT WING NR 6 SLAT OUTER SKIN CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081107 NM 2008 11 7 2008UALA06336 1 20081031 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 SEATS 46 AND 47 RIGHT EEL LIGHTS INOP. LIGHTS INOPERATIVE. REPLACED LAMPS. ALL CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081107 NM 2008 11 7 2008UALA06362 1 20081102 A 2751 TRANSMITTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAP FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 550UA 25398 IN ALTERNATE FLAPS - INDICATORS SPLIT AT FLAPS 1. LT INDICATION MOVES TO 1 NORMALLY, RT INDICATOR JUMPS TO ABOUT 15 THE N NEEDLES STAY SPLIT UNTIL LEADING EDGES AND TRAILING EDGES GET TO POSITION 1, THEN INDICATIONS ARE WITHIN LIMITS. 2 L 7 2 4F 4 F RT A2NM E17NE 20081107 NM 2008 11 7 2008UALA06343 1 20081101 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 550UA 25398 AFT FUSELAGE DENTED STA 1710, STR 13-14R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED AREA AND FABRICATED A REPAIR DOUB LER AND FILLER. 2 L 7 2 4F 4 F RT A2NM E17NE 20081110 NM 2008 11 10 DL75E081479 1 20081101 A 2432 CIRCUIT BREAKER BOEING 757 757231 1384950 NM POPPED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 722TW 29385 APU DOOR STATUS MSG AFTER APU SHUTDOWN. RETURN TO GATE. FOUND APU BATT C/B POPPED. RESET SAME DOOR, OPN NOW NORMAL. 2 L 7 2 4F RT A2NM 20081110 NM 2008 11 10 UPS08M53851 1 20081022 A 5420 ANGLE DOUG MD11 MD11F 3023600 NM NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 278UP 48577 INSPECTION TYPE:3C NR 1 PYLON APPROX STA YN344 1 EA ANGLE BRACKET FOUND CRACKED. REMOVED, FABRICATED, AND INSTALLED ANG LE IAW DWG AVB7533 AND MD-11 SRM 51-21-01, 51-31-01. 2 L 7 3 4F RT A22WE 20081110 WP 2008 11 10 AALA200802570 1 20080917 A 5320 PAN DOUG DC9 DC983 3022083 WP BS 905 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 571AA 49353 RT WINDOW PAN CRACKED AT STATION 905. CRACK LENGTH IS .5 INCH. INSTALLED DOUBLER IN ACCORDANCE AARD 53-10-00-25. 2 L 7 2 4F RT A6WE 20081110 NM 2008 11 10 ASM2008F00008 1 20081017 A 5753 ARC1984501 HINGE DOUG MD11 MD11 3023602 NM TE FLAP CORRODED W ASMF O OTHER O OTHER NR NOT REPORTED 1 SW 23 742BC 48758 AFTER REWORK OF OB FLAP, IB AFT HINGE PN ARC 1984-501, IB PIVOT LUG BORE HAS BEEN FOUND OUT OF LIMITS PER CMM 57-52-04 P AGE 624 AND 625. FOUND 1.172" INSTEAD OF 1.150". BOECOM NR 1-1024128699-4 APPROVE TO INSTALL AN OS BUSHING. 2 L 7 3 4F RT A22WE 20081110 SO 2008 11 10 SIM2008F00028 1 20081003 A 2121 4611028900 FAN EMB 145 EMB145LR 3260212 SO SMOKE A SIMA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 21 664MS 11721 145779 ON FLIGHT 4433, CREW REPORTS THAT ON APPROACH,, THE CABIN WAS FILLING UP WITH A HAZY SMOKE. UPON GATE ARRIVAL THE CABIN WAS QUITE HAZY. APU ON UNTIL AFTER LANDING AND THERE WAS NO CHANGE IN THE CABIN. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH RECIRC FANS AND EXHAUST, OPERATION CHECKED GOOD. ACFT RETURNED TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081110 EA 2008 11 10 TRAX200801130 1 20080907 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA FS 280 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 980EV 7759 FS 280 BEAM IS CRACKED OTBD OF RBL 9 BLEOW BOTTOM (2) FASTENERS THAT CONNECT FS 280 BEAM TO RBL 11 VERTICAL BEAM. (K) 2 L 7 2 4F RT A21EA 20081110 EA 2008 11 10 TRAX200801129 1 20080902 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA ROW 10 INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 909EV 7658 CEILING EMERGENCY FLOOD LIGHT OVER ROW 10 INOPERATIVE. RELAMPED CEILING EMERGENCY FLOOD LIGHT OVER ROW 10 IAW CRJ200 AM M33-51-16. OPS CHECK GOOD. (K) 2 L 7 2 4F RT A21EA 20081110 NM 2008 11 10 08FDEA04729 1 20081105 A 5320 BAC1493577 SUPPORT BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FUSELAGE UPPER LOBE INTERIOR STRUCTURE- CORROSION ON FRAME SUPPORT BETWEEN BS 620-640 RBL 48 REMOVED DAMAGED AREA, INSER TION REPAIR REQUIRED. REF SRM 51-30-02, P1-27. FABBED REPAIR PARTS FOR INSERTION REPAIR AND ALSO END PLATE SPLICE. REF S RM 51-40-3 AND SRM 53-10-8. TREATED & PRIMED REPAIR PARTS. REF: SRM 51-10-2. ASSEMBLED REPAIR PARTS. REF: SRM 51-30-2. INSTALLED ASSEMBLED PARTS. REF: SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081110 EA 2008 11 10 MAS2008F00091 1 20080928 A 2751 601R930571 SENSOR CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A MASA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 07 154SF 29362 26216 7154 FLT 7082-CREW DECLARED AN EMERGENCY DUE TO FLAP FAIL FAULT IN FLT AT 0. MX COMPLIED WITH PARTS A & B OF MTC FOR FLAP FAI L REPORTS. TROUBLE SHOT THE FAULT TO THE RT OTBD SKEW SENSOR AND REPLACED THE UNIT. SYSTEM OPS CHECK WITH NO DEFECTS NOT ED. 2 L 7 2 4F RT A21EA 20081110 NM 2008 11 10 USA2008F00044 1 20080928 A 2842 FG1006AA07 CONTROL UNIT BOEING 767 767201 1385125 NM FUEL TANK FAILED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 249AU 23901 FLT 758 - ENROUTE, IN CRUISE FLT, THE FUEL TOTALIZER AND CENTER FUEL TANK INDICATORS BECAME INOPERATIVE. RETURNED AND LA NDED WITHOUT FURTHER INCIDENT. MX REPLACED TANK UNIT ASSY NR 3. OPS AND LEAK CHECKED OK. 2 L 7 2 4F RT A1NM 20081110 SO 2008 11 10 SWIA200820308 1 20081103 A 5230 DOOR EMB 120 EMB120ER 3260203 SO MCD LACK OF LUBE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 297SW 120327 MCD HARD TO OPEN FROM INSIDE. (FLT 5441)LUBED DOOR. 2 L 7 2 4T RT A31SO 20081112 NM 2008 11 12 DHLA2008745642 1 20080902 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT BS 720E BETWEEN S-13L AND 14L FRAME WITH DOUBLE HOLES. REPAIRED FRAME SECTION AT BS 720E B ETWEEN S-11L AND S-14L IAW B727 SRM 53-10-4 FIG 1 DETAIL 1. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DL75E081480 1 20081101 A 2425 WARNING SYSTEM BOEING 767 7672Q8 1385157 NM PWA 2037 PW2037 NE COCKPIT ACTIVATED A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 703TW 27620 727206 AFTER STARTING RT ENGINE GOT STEADY RT GEN DRIVE LIGHT. IDG GEN OIL SERVICED AND INSPECTED RUN UP REFORMED AND PROBLEM CONTINUE. FWD TO MEL 24-00-01. APU OIL CHECKED SERVICED TO FULL. CONFIRMED NO FAULT HISTORY LAST 20 DAYS. REP PLA IN STALLED. 2 L 7 2 4F 4 F RT A1NM E17NE 20081112 NM 2008 11 12 DHLA2008745649 1 20080924 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE FROM BS 950E+3 TO BS 950E+19 BEWTEEN S-25L AND S-26L DOUBLER REPAIR WITH CORROSION AND WEAR. REPAIRED FU SELAGE SKIN SECTION IN LT AFT WING TO BODY FAIRING AREA FROM BS 950D+14 TO BS 950F+5.5 BETWEEN S-24L AND S-27L IAW COOPE SA EO-C00-2-53-336-08. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DL757081463 1 20081029 A 5330 143N35219 SKIN BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 23843 DURING AN AGING AIRCRAFT INSPECTION, CORROSION WAS FOUND ON THE INNER SURFACE OF THE GROUND AIR CONDITIONING CUTOUT AT S TA 869. THE CORROSION DAMAGE WAS REPAIRED PER BOEING INSTRUCTIONS. 2 L 7 2 4F RT A2NM 20081112 NM 2008 11 12 DHLA200800124 1 20081106 A 2810 FUEL TANK BOEING 727 727247 138408F NM NR 2 LEAKING A DHLA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 05 793DH 21393 KEROSENE SMELL WHEN TURNING ON PACKS AFTER T/O. FOUND FUEL LEAK NR 2 TANK. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DL757081482 1 20081103 A 5320 146N545121 WEB BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 WEB AT STATION 1500-1520 AT LBL 3 CORRODED. REPAIRED PER 51-40-01 BY REPLACEMENT ON NR 00039. 2 L 7 2 4F RT A2NM 20081112 EA 2008 11 12 COMA0860414 1 20081006 A 5320 6013600130 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 967CA 30355 7134 STA 640 RT SIDE REINFORCEMENT ANGLE IS CRACKED. COMPILED WITH MOD K601R360093 ON RT SIDE OF FS 640 IAW SB 601R-53-061. 2 L 7 2 4F RT A21EA 20081112 EA 2008 11 12 COMA0860413 1 20081006 A 5320 6013600129 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 967CA 30355 7134 STA 640 LT SIDE REINFORCEMENT ANGLE IS CRACKED. COMPILED WITH MOD K601R360093 ON LT SIDE OF FS 640 IAW SB 601R-53-061. 2 L 7 2 4F RT A21EA 20081112 NM 2008 11 12 USAA920081818 1 20081002 A 5311 65C25229 FRAME BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, FRAME CRACKED AT BS 727D, S8L & S9L. REPAIRED FRAME AT BS 727D, S8L & S9L IAW US AIRWAYS TYPIC AL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 20081112 NM 2008 11 12 DHLA2008745610 1 20080902 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE AT BS 335 BETWEEN S-20L AND S-21L SKIN WITH DENT. REPAIRED FUSELAGE SKIN SECTION AT BS 332.25 TO BS 336 BETWEEN S-20L AND S-21L IAW B727 SRM 53-30-3 FIG 13. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745612 1 20080908 A 5320 WEB BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 DELTA BEAM LOWER WEB LOWER SKIN AND ATTACHMENT HARDWARE ARE CORRODED AT BS 741 BS 770 BS 780 BS 800. REPAIRED FUSELAGE WEB SECTIONS DELTA BEAM AREA FROM BS 740 TO BS 750 BETWEEN LBL 5 AND RBL 5 FROM BS 795 TO BS 804 BETWEEN LBL 1 AND RBL 5 IAW B727 SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745613 1 20080909 A 5322 SHEAR TIE BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE BS 272 BETWEEN S-25L AND S-26L SHEAR TIE WITH CORROSION. REPLACED SHEAR TIE SECTION AT BS 272 BETWEEN S- 24L AND S-27L IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745621 1 20080903 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 CARGO CABIN AT BS 1166 S-6R FRAME DOUBLER WITH HOLE IN RADIUS. REPLACED FRAME DOUBLER AT BS 1166 BETWEEN S-5R AND S-7R IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081113 SO 2008 11 13 I06B20081030001 1 20081030 A 5280 DOOR EMB 135 EMB135ER 3260203 SO RROYCE AE3007 AE3007A13 54166 EA NLG DAMAGED I I06B K NONE O OTHER CL CLIMB 1 WP 25 926FM 145466 14K FT NOTICED A FLASH OF LIGHT THAT APPEARED TO BE BELOW THE AIRCRAFT. THE CREW REPORTED NO AIRCRAFT ANOMALIES AS A RE SULT OF THE SUSPECTED NEAR LIGHTNING STRIKE. FO PERFORMED THE POST FLT INSP AND IMMEDIATELY NOTICED A PIN HOLE IN THE N OSE GEAR DOOR. CAPTAIN CONFIRMED AIRCRAFT HAD BEEN STRUCK BY LIGHTNING. THE REMOVAL OF THE AILERON WAS INITIATED. THE ALTERNATIVE TO MOVE THE PART TO THE UNITED AIRLINES COMPOSITE REPAIR SHOP IN SFO WAS EXECUTED. REPAIRS WHERE MADE PER THE STRUCTURAL REPAIR MANUAL, AND AN ASG MECHANIC REMAINED IN THE AREA TO TRANSPORT THE REPAIRED PARTS TO MHR. THE AIRC RAFT HAD ALL OF THE BELLY REWORK ACCOMPLISHED DURING THE SAME TIME PERIOD. REINSTALLATION WAS ACCOMPLISHED AND THE REQU 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081113 NM 2008 11 13 DHLA2008745626 1 20080920 A 5730 SKIN BOEING 727 727224 1384076 NM RT WING CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 RT WING UPPER SKIN WITH CORROSION AT WS 619 REAR SPAR SECTION. REPAIRED RT WING UPPER SKIN AT REAR SPAR AT WS 619 IAW B OEING MESSAGE 1-1000735864-2 DTD 10/2/08 AND COOPESA EO COO-2-57-330-08. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745627 1 20080904 A 5310 DOOR FRAME BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN FWD RT DOOR CUTOUT FWD FRAME LOWER SECTION WITH CORROSION. REPAIRED FRAME AT BS 377 BETWEEN S -16R AND S-17R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 USAA920081951 1 20081014 A 5330 65C33756 SKIN BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753006/004 CRACK AT FORWARD SERVICE DOOR AFT BOTTOM CUTOUT IN RADIUS. REPAIRED FORWARD SERV ICE DOOR AFT BOTTOM CUTOUT IAW B737 SRM 53-10-01. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 USAA920081932 1 20080917 A 5320 69773611 INTERCOSTAL BOEING 737 7373G7 138447J NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN C18 MAJOR REPAIR NR 6131670 R1 DOOR CUTOUT AFT FRAME INTERCOSTAL IS CRACKED AT STOP FITTING AT BS 332.1, S8R, WL270. REPAIRED R1 DOOR CUTOUT AFT FRAME INTERCOSTAL STOP FITTING AT BS 332.1, S8R, WL270 IAW US AIRWAYS EA NR 130127. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 DHLA2008745628 1 20080902 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT BS 700 BETWEEN S-16R AND S-17R FRAME WITH DENT. REPAIRED FRAME SECTION AT BS 700 BETWEEN S -16R AND S-17R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 QXEA20081106O1122 1 20081011 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 419QX 4145 PDX - C1- CORROSION ON TOP PF SEAT TRACK 9 STA X704-X706. BLENDED OUT CORROSION AND FOUND BLEND TO BE OUT OF LIMITS IAW RD 8/4-53-884. MAPPED FOR ENGINEERING. REMOVED SEAT TRACK BY DRILLING OUT RIVETS AND REMOVING BOLTS AT FRAME. MATCH DRILLED NEW NR 9 SEAT TRACK IAW DHC8 Q400 SRM 51-40-07. INSTALLED NR 9 SEAT TRACK IAW DHC8 Q400 SRM 51-42-05 AND 51-40- 15. 2 H 7 2 4T RT A13NM 20081113 NM 2008 11 13 QXEA2008110601144 1 20081025 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 421QX 4149 PDX - C1 - LT INBOARD SEAT TRACK HAS CORROSION BETWEEN STA X664 AND X 666. BLENDED CORROSION AND FOUND TO BE OUT OF LIM ITS REF RD 8/4-53-884. REMOVED NR 8 SEAT TRACK IAW Q400 SRM 51-40-07. MATCH DRILLED NEW SEAT TRACK AND INSTALLED SEAT TRACK IAW -8 Q400 SRM 51-40-07, 51-40-15 AND 51-42-05. 2 H 7 2 4T RT A13NM 20081113 EA 2008 11 13 ASOA200801438 1 20081102 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 908EV 7654 PAX DOOR DIFFICULT TO OPEN. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 QXEA2008110601167 1 20081102 A 5240 PLUNGER CNDAIR CL600 CL6002C10 1390015 EA DOOR HANDLE MALFUNCTIONED A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 19 612QX 10042 LAX - SERVICE DOOR EXIT IS HARD TO OPEN AND CLOSE. OPEN MIDDLE ACCESS PNL ON SERVICE DOOR EXIT, FOUND AND RESET CENTER PLUNGER ON DOOR HANDLE. OPS CHECK GOOD. CLOSED MIDDLE ACCESS PNL. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS. 2 L 7 2 4F RT A21EA 20081113 2008 11 13 QXEA2008110601169 2 20081102 A 7497 WIRE HARNESS BOMBDR CNDAIR CL600 CL6002C10 1390015 EA STATIC INVERTER CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 PDX - WIRE HARNESS TO STATIC INVERTER ON AFT RT SIDE OF REAR PRESSURE HAS CHAFED THRU HYDRAULIC LINE AND DAMAGED WIRES T O STATIC INVERTER. REPAIRED WIRE RHB0878-20 AT STATIC INVERTER BY SPLICING IAW CRJ 700 WM 74-00-01. INSTALLED STATIC I NVERTER WITH A SERVICEABLE PART FROM STOCK IAW CRJ 700 AMM TASK 74-31-03-400-801-A01. OP'S CHECKED GOOD. RETURNED TO S ERVICE. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 QXEA2008110601171 1 20081105 A 5210 LATCH CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR DIRTY A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 19 603QX 10011 LAX - F/A REPORTS PASSENGER DOOR HANDLE DIFFICULT TO OVER DETENT WHEN OPENING AND CLOSING. INSPECTED DOOR WITH NO DEFEC TS, CLEANED & LUBED DOOR LATCHES, DOOR OPERATES NORMAL. RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801441 1 20081103 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 PAX DOOR COULD NOT BE OPENED BY F/A AT THE END OF THE FLIGHT. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801449 1 20081103 A 5320 PANEL CNDAIR CL600 CL6002B19 1900309 EA CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 PANEL 282AZ HAS 2 CRACKS. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801450 1 20081102 A 5320 SUPPORT CNDAIR CL600 CL6002C10 1390015 EA LT MLG WW CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 LT WHEEL WELL FWD OUTBOARD BIN ATTACH SUPPORT IS CRACKED. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801442 1 20081103 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MISSING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 683BR 7692 OPEN PLACARD MISSING ON PAX DOOR. GATE RETURN 2 L 7 2 4F RT A21EA 20081113 WP 2008 11 13 22AA20081006 1 20081027 A 5754 SLAT DOUG DC10 DC1030F 3023504 WP RT WING DAMAGED A 22AA K NONE O OTHER IN INSP/MAINT 1 SO 19 450ML 47831 ON SERVICE CHECK, RT WING SLAT NR 8 LEADING EDGE DAMAGE. FOUND BIRD STRIKE ON RT WING SLAT NR 8 LEADING EDGE; INSPECTED RT WING SLAT NR 8 LEADING EDGE IN ACCORDANCE WITH DC10 M/M 05-62-00. PERFORMED TEMPORARY REPAIR IN ACCORDANCE WITH ENG INEERING AUTHORIZATION 5740-N450ML-FVCI. 2 L 7 3 4F RT A22WE 20081113 EU 2008 11 13 AALA200802685 1 20081007 A 2750 JACKSCREW AIRBUS 300 A300B4605R 3930308 EU TE FLAP MALFUNCTIONED A AALA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SW 21 91050 423 MIA - CREW REPORTED FAULT FOR FLAP SYSTEM NUMBER ONE AND TWO. FLAPS DID NOT EXTEND. ABORTED APPROACH AND FLEW AROUND F OR SECOND APPROACH. SLATS AND FLAPS WORKED NORMAL. LANDED MIA WITHOUT INCIDENT. ACCOMPLISHED SPECIAL ITEMS CARD 5705 FLAP JACKSCREW DRAIN AND SERVICE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081113 NM 2008 11 13 AALA200802688 1 20081007 A 3350 LENS BOEING 737 737823 13844BZ NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 976AN 30099 DFW - EMERGENCY EXIT SIGN AT LEFT AFT OVERWING EXIT MISSING LENS. REPLACED EMERGENCY EXIT IDENTIFIER LIGHT ASSEMBLY. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20081113 WP 2008 11 13 AALA200802690 1 20081008 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 59523 49915 LGA - EMERGENCY EXIT LIGHT AT LOWER FORWARD GALLEY INOPERATIVE. REPAIRED BROKEN WIRE FOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081113 WP 2008 11 13 AALA200802691 1 20081008 A 3397 TERMINAL DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 59523 49915 LGA - EMERGENCY LIGHTS AT TAIL CONE COMPARTMENT INOPERATIVE. REPAIRED BROKEN TERMINAL AT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081113 WP 2008 11 13 AALA200802692 1 20081008 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 982TW 53632 LGA - OVERHEAD EMERGENCY LIGHT AT AFT GALLEY SERVICE DOOR INOPERATIVE. INSTALLED LAMP FOR OVERHEAD EMERGENCY LIGHT AT A FT GALLEY SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081113 WP 2008 11 13 AALA200802693 1 20081008 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 982TW 53632 LGA - EMERGENCY LIGHT AT OVERHEAD AFT GALLEY SERVICE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVE RHEAD AFT GALLEY SERVICE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081113 NM 2008 11 13 AALA200820004 1 20081007 A 5320 146N5300199 FLOOR SUPPORT BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 670AA 52802 25335 FLOOR SUPPORT IS CORRODED. 2 L 7 2 4F RT A2NM 20081113 NM 2008 11 13 AALA200802683 1 20081005 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 636AM 24594 DFW - EMERGENCY SEAT MOUNTED AND EXIT DOOR SIGN LIGHTS AT AFT CABIN DIM. REPLACED BATTERY PACK FOR DIM EMERGENCY LIGHTS . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081107 NM 2008 11 7 2008UALA06342 1 20081030 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 677UA 30029 SEAT 4H FWD EEL LIGHT MISSING. LIGHT IS OUT-OF-POSITION. REPLACED EEL LIGHT. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081107 NM 2008 11 7 2008UALA00955 1 20080220 A 3610 7732887810 CHECK VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BLEED AIR SYS FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 649UA 25286 NR 1 ENGINE HAS THE L BLEED OFF EICAS MSG AND L-BLEED OFF LIGHT ON WITH BLEED SELECTED. REPLACED ISOLATION BYPASS CHECK VALVE. FOUND DIRECT SHORT AT PRSOV CONNECTOR. FOUND D22 CONNECTOR ON PRSOV BAD. REPLACED SAME. OPS CHECKED GOOD. R EPLACED PRSOV. LEAK & OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081110 CE 2008 11 10 GUUA11040801 1 20081104 A 3297 WIRE BEECH 1900 1900D 1154162 CE LT MLG BROKEN A GUUA O OTHER O OTHER AP APPROACH 1 SO 29 17541 UE203 FLIGHT 5201 MIA/FLL - DURING APPROACH LEFT LANDING GEAR INDICATION LIGHTS DOES NOT SHOW LOCKED. CONTINUED TO FLL. LAND ED WITHOUT INCIDENT. REPAIRED BROKEN WIRE AT LEFT MAIN LANDING GEAR CONNECTOR P273. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081110 CE 2008 11 10 AXS2008F00000 1 20080925 A 7100 50910275267 COWLING BEECH 99 99A 1154003 CE RT ENG DAMAGED E AXSA O OTHER E VIBRATION/BUFFET DE DESCENT 1 EA 65 197WA U130 DEPARTED AND LEVELED OFF AT 9000 FT. DURING DECENT THROUGH 7800 FT THE PILOT NOTED A "LOADING NOISE" AND THE ACFT YAWED FROM THE ASSIGNED HEADING. THE ACFT EXPERIENCED A CONSTANT BUFFETING AND VIBRATION COULD BE FELT THROUGH THE AIRCRAFT. A FTER 5-6 SECONDS THE VIBRATIONS CEASED BUT THE YAW TENDENCIES CONTINUED AND DID OCCASIONAL BUFFETING. THE PILOT DECLARED AND EMERGENCY AS THE ISSUE COULD NOT BE IDENTIFIED. THE PILOT SLOWED THE AIRCRAFT TO 140KTS. THE PILOT TURNED ON ALL L IGHTS AS THE FLIGHT WAS CLEAR FOR IMMEDIATE LANDING AND THE ICE LIGHT ON THE RT SIDE ILLUMINATED THE OUTLINE OF A DISTOR TED AFT UPPER ENGINE COWLING WHICH APPEAR TO BE FIXED AND NOT MOVING. WHEN LANDING WAS ASSURED THE PILOT SECURED THE RT 1 L 7 2 3T A14CE 20081110 NM 2008 11 10 USAA920081821 1 20081003 A 5311 6546529 FRAME BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, FRAME CRACKED AT BS 440, S8L & S9L. REPAIRED FRAME AT BS 440, S8L & S9L IAW US AIRWAYS TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 20081110 NM 2008 11 10 USAA920081830 1 20081006 A 5340 69468314 STRINGER CLIP BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, STRINGER TIE CLIP CRACKED AT BS 360, S5L. REPLACED STRINGER TIE CLIP AT BS 360, S5L IAW BOEING SERVICE BULLETIN 737-53-1268-00. 2 L 7 2 4F RT A16WE 20081110 SO 2008 11 10 SWIA200820296 1 20080921 A 5320 FITTING EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 227SW 120304 FS37 & FS38 ABOVE APU BLEED DUCT LINE CORRODED. (C-CHECK)REPLACED CORRODED CLIPS. 2 L 7 2 4T RT A31SO 20081110 SO 2008 11 10 SWIA200820297 1 20080918 A 5311 FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 227SW 120304 COCKPIT LT FRAME 10 CRACKED AT STEERING TILLER AREA. (C-CHECK)REPAIRED PER SRM. 2 L 7 2 4T RT A31SO 20081110 SO 2008 11 10 SWIA200820298 1 20080918 A 5320 ANGLE EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 227SW 120304 COCKPIT LEFT FRAME FS10 TOP ANGLE CRACKED BY MIDDLE OF DIRECT VISION WINDOW. (C-CHECK)REPLACED PER SRM. 2 L 7 2 4T RT A31SO 20081110 SO 2008 11 10 SWIA200820299 1 20081103 A 6120 PCU EMB 120 EMB120ER 3260203 SO LEFT MALFUNCTIONED A SWIA K NONE O OTHER AP APPROACH 1 NM 07 236SW 120312 NP CONTINUOUS L 102.0, R 101.6-101.3 ON APPROACH, 30% TORQUE. (FLT 7762)REPLACED LEFT PROPELLER CONTROL UNIT. 2 L 7 2 4T RT A31SO 20081112 EU 2008 11 12 DHLA200800107 1 20080930 A 3350 311701 BATTERY PACK AIRBUS 300 A300B4203 3930306 EU EMERGENCY LIGHT INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 GL 05 367DH 265 ON PRE-DEPARTURE CHECK, EMERGENCY LIGHT OVER R1 DOOR INOPERATIVE, ACFT GROUNDED. R&R POWER SUPPLY IAW MM 33-51-14. OPS CHECKED OK IAW 33-51-00. 2 L 7 2 4F RT A35EU 20081112 NM 2008 11 12 DHLA2008745641 1 20080904 A 5714 SKIN BOEING 727 727224 1384076 NM CENTER WING CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN WING CENTER SECTION UPPER SKIN CORRODED FROM BS 782 TO BS 785 BETWEEN RBL 60 AND RBL 65. REPA IRED UPPER SKIN AT WING CENTER SECTION AT BS 782 TO BS 785 BETWEEN RBL 45 AND RBL 70 IAW COOPESA EO COO-2-57-319-08. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DL757081481 1 20081103 A 5322 146N10131 SHEAR TIE BOEING 757 757232 1384965 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 AFT CARGO STATION 1439 AT STRINGER 30 TO 29 RIGHT SHEAR TIE DEFORMED BY TOOLING DAMAGE. REPAIRED BY REPLACEMENT ON NR 0 0053. 2 L 7 2 4F RT A2NM 20081112 NM 2008 11 12 DHLA2008745648 1 20081008 A 5322 SHEAR TIE BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 640 BETWEEN S-27R AND S-28R SHEAR TIE FRAME WITH CRACK. REPLACED SHEAR TIE A ND TEE AT BS 640 BETWEEN S-27R AND S-28R IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DL757081466 1 20081028 A 5321 FLOOR PANEL BOEING 757 757232 1384965 NM AFT CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 23843 CORROSION AFT CARGO BAY AFT FLOOR PANEL FROM BS 1510 TO 1640 IS CORRODED ON BOTTOM SURFACE AT THE FASTENER HOLES. REMOV ED AND REPLACED ACB FLOOR PANEL BS 1510-1640 IAW AMM 25, 50-04-004-001, AMM 25-50-04-404-004, SRM 51-40-02, 51-40-05, AN D 51-40-08. 2 L 7 2 4F RT A2NM 20081112 EU 2008 11 12 USAA920081813 1 20080927 A 5315 D53472190211 FLOORBEAM AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL - C7 - MAJOR REPAIR, CORROSION ON FLOORBEAM HARD POINT AT FLOOR STRUCTURE IN PAX CABIN LOCATED -Y1292 FR 64 TO FR 66 +1. REPLACED FLOORBEAM IN PAX CABIN LOCATED -Y1292 FR 64 TO FR 66+1 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081112 NM 2008 11 12 USAA920081819 1 20081002 A 5311 6546529 FRAME BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT - Q5 - MAJOR REPAIR, FRAME CRACKED AT BS 440, S8R & S9R. REPAIRED FRAME AT BS 440, S8R & S9R IAW US AIRWAYS TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 20081112 NM 2008 11 12 DHLA2008745607 1 20080905 A 5714 SKIN BOEING 727 727224 1384076 NM CENTER WING CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN WING CENTER SECTION UPPER SKIN CORRODED AT STA 867 LBL 66. REPAIRED UPPER SKIN WING CENTER SE CTION FROM BS 867 TO BS 834 BETWEEN LBL 49 AND LBL 70 IAW COOPESA EO COO-2-57-286-08 DTD 09/18/08. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 USAA920081946 1 20081022 A 3397 WIRE HARNESS AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHTS DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 831AW 1576 LOG PAGE 4427795 FLT NR 363 PHX-SMF EMERGENCY LIGHT AT 18 LT SEAT MOUNTED IS INOPERATIVE. FOUND SEAT HARNESS DISCONNECT ED. SECURED AND RECONNECTED HARNESS. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081113 NM 2008 11 13 USAA920081935 1 20081023 A 5320 6565710 CHANNEL BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03C21853024/005 HAT CHANNEL CRACKED AT BS 727D, BLO IN AFT CARGO COMPARTMENT. REPLACED HAT CHANN EL AT BS 727D, BLO IN AFT CARGO COMPARTMENT IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081113 EA 2008 11 13 ASOA200801436 1 20081102 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 821AS 7194 PAX DOOR DIFFICULT TO CLOSE. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801437 1 20081102 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR BINDING A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 824AS 7203 CATERING REPORTS GALLEY SERVICE DOOR WILL NOT OPEN FROM OUTSIDE. 2 L 7 2 4F RT A21EA 20081113 NM 2008 11 13 KCSA081561 1 20081107 A 5210 DOOR FRAME BOEING 747 747212B 1384886 NM R5 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 R5 DOOR AT BS 2239 FORWARD LOWER CORNER VERTICAL FRAME CRACKED IN RADIUS 2.5 INCH LONG, WL 209. 2 L 7 4 4F RT A20WE 20081113 EA 2008 11 13 ASOA200801458 1 20081106 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 722EV 10127 EMERGENCY LIGHT JUST AFT OF SERVICE DOOR HAS SEVERAL INOP BULBS. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801459 1 20081106 A 3320 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 878AS 7590 TOP AND MIDDLE AFT EQUIPMENT BAY SERVICE LIGHTS INOP. 2 L 7 2 4F RT A21EA 20081113 NM 2008 11 13 AALA200820001 1 20081007 A 5320 146N25466 SUPPORT BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 670AA 52802 25335 RT DRAIN PAN SUPPORT IS CORRODED. 2 L 7 2 4F RT A2NM 20081113 WP 2008 11 13 ABXA200811070261 1 20081104 A 3350 60030451 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 900AX 841 47380 DURING PREDEPARTURE FOUND EMERGENCY LIGHTING SYSTEM INOP. DEFERRED: 62393 REMOVED AND REPLACED EMERGENCY BATTERIES IAW DC9 AMM 33-03-00-8; DEFERRED PER DC9 AMM 33-53-00-3 AND GMM 07.04 FOR TRACKING MBCB 3 FLYT DAYS. CODE 2 CLEARED DI 623 93 REMOVED & REPLACED EMERGENCY LIGHTING BATTERY POWER PACK ASSY AS REQUIRED. 2 L 7 2 4F A6WE 20081113 EA 2008 11 13 ASOA200801482 1 20081106 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 LEFT FS 484 FLOOR SUPPORT INTERCOSTAL PREVIOUS REPAIR ANGLE AT LBL 36.0 CRACKED. REPLACED ANGLE AT LT FS 484 FLOOR SUPP ORT LBL 36.0 IAW REO 610R-53-41-059, STEPS 5-12 AND 14. PRESSURE LEAK CHECK DUE. PRESSURIZATION CHECKS GOOD IAW AMM 21 -32-00-863-801. C/W EC/TC REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801484 1 20081108 A 5260 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA ASD CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 744EV 10157 BOTTOM ASD STEP CORRODED WHERE BOTTOM FOLDING STEP ATTACHES. 2 L 7 2 4F RT A21EA 20081113 NM 2008 11 13 DHLA2008745653 1 20080907 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT BS 720C+2" BETWEEN S-27R AND S-28R SKIN WITH LIGHT CORROSION. REPAIRED FUSELAGE SK IN SECTION FROM BS 720C-8" TO BS 720C+8" BETWEEN S-27R AND S-27L IAW EO COO-2-53-328-08. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745669 1 20080903 A 5313 STRINGER BOEING 727 727224 1384076 NM RT MLG WW CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE RT MAIN WHEEL WELL BS 940 S-18A CRACKED. REPAIRED FUSELAGE S-18A RIGHT SIDE AND FUSELAGE SKIN SECTION FR OM BS 930 TO BS 966 IAW COOPESA EO COO-2-53-285-08. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745651 1 20080909 A 5320 BEAM BOEING 727 727224 1384076 NM NLG WW CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE NOSE WHEEL WELL RT HORIZONTAL WALKWAY BEAM WITH CORROSION. REPLACED SIDE CHORD SECTION NOSE WHEEL WELL F ROM BS 282 TO BS 360 WL 150 S-27R IAW BOEING DWG 65-18420 REV M DTD 07/22/81 AND BOEING DWG 65-18415 REV U DTD 11/15/72. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745652 1 20080924 A 5330 SKIN PANEL BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER EXTERNAL FUSELAGE SKIN PANEL FROM BS 480 TO BS 680 BETWEEN S-26L AND S-26R WITH SEVERAL EXISTING REPAIRS. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745668 1 20080919 A 5322 SHEAR TIE BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE NOSE COMPARTMENT TORQUE BOX AT BS 303 BETWEEN S-24L AND S-27L SHEAR TIE WITH CORROSION. REPAIRED FUSELAG E SHEAR TIE AT BS 303 BETWEEN S-25L AND S-27L IAW B727 SRM 53-10-4 FIG 11. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 HALA2008111100843 1 20081111 A 5347 SEAT TRACK BOEING 767 76733A 1385209 NM FUSELAGE DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 THE B-ZONE, SEAT TRACK AT RBL 11 STN 545 HAS DAMAGE TO TOP OF TRACK BEYOND REPAIR LIMITS. DEPTH MEASURED AFTER BLEND AT 0.052 INCH (SRM LIMIT 0.020). DAMAGED SECTION OF TRACK CUT & REMOVED IAW SRM 53-00-52 FIG 201 REPAIR 1. REPAIR PARTS FABRICATED IAW SRM 53-00-52 FIG 201 REPAIR 1 & INSTALLED. FPI OF SEAT TRACK SATIS IAW SOPM 20-20-02. REPAIR PART ALODI NED IAW BAC5719. REPAIRED PARTS PRIMED W/BMS 10-11 TYPE 1 IAW SOPM 20-41-02. SEAT TRACK PAINTED IAW SOPM 20-41-04. 2 L 7 2 4F RT A1NM 20081113 NE 2008 11 13 HALA2008111100844 2 20081111 A 7230 9267M28P09 FAN BLADE BOEING 767 767332 1382001 NM GE CF6 CF680A 30025 NE NR 1 ENGINE DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 58318 UPON ARRIVAL FOUND NR 1 ENGINE HAD 2 1ST STAGE FAN BLADES WITH DAMAGE OUT OF LIMITS. ALSO 8-9 BLADES NEED TO BE BLENDED . REMOVED & REPLACED NR 1 ENGINE 1ST STAGE FAN BLADES PER AMM 72-31-02, OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E13NE 20081113 NM 2008 11 13 HALA2008110500842 1 20081105 A 3697 WIRE BOEING 767 7673G5 1385126 NM BLEED AIR SYS OPEN A HALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 13 586HA 24259 ETOPS SIGNIFICANT SYSTEM - ATB/ LT ENG HPSOV EICAS, WITH LT BLEED AIR ON STEADY. FOUND OPEN WIRE ON CONNECTOR D4208P PI N 10. REPLACED WIRE PER SWPM, RESECURED CONNECTOR, UNLOCKED HPSOV VALVE, REMOVED SHORTING PLUG, PER MEL PROCEDURES CHEC KED HPSOVON ENG HIGH PWR RUN, OPS CHECK GOOD. NO DEFECTS NOTED. 2 L 7 2 4F RT A1NM 20081113 NM 2008 11 13 QXEA2008111001016 1 20080912 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 413QX 4060 PDX - C4 - LT SEAT TRACK NR 5 HAS CORROSION AROUND 7 RIVETS AT STA 12.00 (APPROX). BLENDED HEAVY CORROSION AND FOUND T O BE OUT OF LIMITS PER RD 8/4-53-2336. REMOVED NR 5 SEAT TRACK AND INSTALLED NEW TRACK REF DASH8 Q400 SRM 51-42-05, 511 -40-15, 51-42-05 AND 51-42-45. 2 H 7 2 4T RT A13NM 20081113 NM 2008 11 13 QXEA2008111201162 1 20081101 A 5720 PANEL BOMBDR DHC8 DHC8402 1390042 NM WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 420QX 4147 PDX - C1 - THE 261LT PANEL LAND ON FRONT SPAR HAS 2 AREAS OF LIGHT FRETTING. BLENDED FWD RT LANDING STRIP PER RD 8/4-53 -451. HFEC INSPECTED IAW -8 Q400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. APPLIED ALODINE AND PRIMER IAW RD 8/4-53-451 STEPS 5&6. APPLIED TEFLON TAPE PER RD 8/4-53-451. 2 H 7 2 4T RT A13NM 20081118 NM 2008 11 18 2008UALA06418 1 20081107 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT PIT FRAME DENTED STA 1400, STR 25L TO 24L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALL ED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 2008UALA06419 1 20081107 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT PIT FRAME DENTED STA 1520 AT STR 21L - 22L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED FRAME SECTION AND INSTALLE D DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 2008UALA06421 1 20081107 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT PIT FRAME DENTED STA 1580, STR 26R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOU BLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 2008 11 18 2008UALA06423 4 20081107 A 2565 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 585UA 26709 DOOR 1R DIFFICULT TO ARM -"ARMED" LIGHT STAYS ON. PROPERLY STOWED LANYARD THAT WAS TANGLED IN GIRT BAR. OPERATED ARMIN G HANDLE SEVERAL TIMES, ALL OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 08FDEA04886 1 20081115 A 5320 65282885 SUPPORT BOEING 727 7272D4 138407U NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FUSELAGE UPPER LOBE INTERIOR STRUCTURE, CORROSION ON GILL LINER SUPPORT AT STA 1180, RBL68, AT STRINGER R9. REMOVED COR ROSION AND INSTALLED REPAR DOUBLER AND FILLER REF SRM 1-40-23 FIG 1. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 ASAA0843726 1 20081029 A 5320 65196033 SHEAR WEB BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 SHEAR WEB CORRODED AT STA 370 LT SIDE. REMOVED CORRODED AREA OF WEB, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 4 00 SRM 51 70 13. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 GTIA0800083 1 20081011 A 5320 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM ZONE 900 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 507NK 2560 AFT GALLEY FLOORBEAM CORRODED AT Y765 BETWEEN FR 64 AND FR 66 2 L 7 2 4F RT A28NM 20081114 SO 2008 11 14 SWIA200820332 1 20081107 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 270YV 120270 FLT 5482 - WHITE FLOOR EMERGENCY LIGHT ADJACENT TO SEAT 4A INOP. RELAMPED. 2 L 7 2 4T RT A31SO 20081114 EU 2008 11 14 08FDEA04762 1 20081105 A 5311 A53770545 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS GOUGE ON FRAME 28, 4.5 INCHES ABOVE STR 22L. REPAIR COMPLIED WITH ON EA 6-5310-123938. 2 L 7 2 4F RT A35EU 20081002 WP 2008 10 2 UPS08853276 1 20080814 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1540 L30R CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 D PIT CARGO COMPT STA 1540 RT LONG 30 HAS EXFOLIATING CORROSION. CUT OUT DAMAGED SECTION OF LONGERON AND SPLICED IN REPAIR SECTION OF LONGERON IAW SRM 53-02-02 FIG 10. 2 L 7 4 4F RT 4A25 20081002 NM 2008 10 2 CALA0800854 1 20080905 A 5311 146A1133 FRAME BOEING 737 737724 13844BY NM BS 787 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27722 28789 CRACK IN BELT FRAME BS 787 S8-9R AT FASTENER FOR OVERHEAD BIN MOUNT. INSTALLED REPAIR PER EC/RA 5310-04824 REV A. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800855 1 20080905 A 5311 143A1113 FRAME BOEING 737 737724 13844BY NM BS 440 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27722 28789 CABIN STA 440 FRAME CRACKED BETWEEN S8-9R. INSTALLED REPAIR PER EC/RA 5310-04824 REV A. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800928 1 20080929 A 5210 507945178 SKIN BOEING 737 7373T0 1384582 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 L-1 DOOR SKIN IS CRACKED AT 5TH STOP FROM TOP. TRIMMED OUT CRACK AND INSTALLED REPAIR DOUBLER PER ECRA 5210-02035. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800872 1 20080905 A 5320 65C3397335 INTERCOSTAL BOEING 737 737524 1384721 NM BS 312-328 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 INTERCOSTAL CRACKED FROM BS 312-328 AT LBL 44. REMOVED AND REPLACED INTERCOSTAL PER B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 2008UALA03110 1 20080531 A 8011 35054367 STARTER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 1 ENGINE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 676UA 30028 NO ENG ROTATION WHEN LEFT START SW TO GND. GROUND CREW REPORTED SPARKS FROM LEFT ENG. FOUND FAULTY STARTER. REPLACED STARTER & STARTER VALVE. CHECKS OKAY FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 2008UALA05571 1 20080830 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 1 FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 799UA 26926 NR 1 IDG HAS 'BLOCKED' MESSAGE ON CH24 MFD PAGE. DISCONNECTED IDG AFTER START. *S/D* FOUND FAULTY IDG. REPLACED NR 1 IDG. OPS CHECK NORMAL. NO FURTHER MSGS OR LEAKS NOTED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081002 NM 2008 10 2 2008UALA05602 1 20080905 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1446 S30 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 CORROSION ON FUSELAGE SKIN WHERE AFT AIRFONE MOUNTS, BS 1446 AT STR 30. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING DO UBLER, CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 2008UALA05603 1 20080905 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 630 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 EXT FUSELAGE STA 630, FWD OF L-2 DOOR, FUSELAGE DOUBLER DENTED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SKIN AND IN STALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 2008UALA05608 1 20080905 A 5320 WEB BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 174UA 24381 UPPER DECK FLOORBEAM WEB IS DAMAGED, AS VIEWED FROM GALLEY AT DOOR 2 IN ELEVATOR COMPARTMENT AT TOP FWD SIDE OF COMPARTM ENT. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED STIFFENER. REMANUFACTURED NEW STIFFENER FROM LIKE MATERIAL. BLENDED ALL DAMAGE, FOUND WITHIN LIMITS EXCEPT SMALL GOUGE WHICH WAS REPAIRED PER 53-00-51 NOTE "C". ALL AREAS AND PARTS TREATE D, PRIMED, INSTALLED WITH SEALANT AND PAINTED. 2 L 7 4 4F 4 F RT A20WE E24NE 20081002 NE 2008 10 2 2008UALA05610 2 20080906 A 7532 PROBE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE BLEED VALVE OUT OF TOLERANCE A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 206UA 30212 RIGHT ENG 2.9 STAB BLEED VALVE TC PROBE CHANNEL-B SIGNAL OUT OF RANGE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081002 NM 2008 10 2 2008UALA05613 1 20080906 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1219 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 AFT PIT AT STA 1219, LBL 4 - RBL 4, CORROSION ON ANGLE AT FRAME ATTACH TO SKIN. *S/D* MAJOR REPAIR ACCOMPLISHED. FABR ICATED & INSTALLED NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 SWAA084981 1 20080910 A 5312 6517853 STRUCTURE BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED SPV CHECK, FOUND VERTICAL CHORD CRACKED AT BS 178, LBL 5.5. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084982 1 20080910 A 5340 6557463 FITTING BOEING 737 7373K2 13844BA NM FUSELAGE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084983 1 20080910 A 5754 SKIN BOEING 737 7373K2 13844BA NM NR 3 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 3 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085246 1 20080926 A 3350 8210248801 LENS BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 263WN 32520 DURING SCHEDULED RON CHECK, R2 DOOR EMERGENCY LIGHT LENS FELL OFF. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM. 2 L 7 2 4F RT A16WE 20081002 2008 10 2 SWAA085245 4 20080925 A 2565 65C34691 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 226WN 32494 FOUND L1 DOOR SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085233 1 20080925 A 5313 BAC1498 STRINGER BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 360, STR 14L. REPAIRED STRINGER PER EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085239 1 20080919 A 5322 6546546 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND BELTFRAME SHEAR TIE CORRODED AT BS 767, STR 27R TO STR 26R. REMOVED AND REPLACED SHE AR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084988 1 20080909 A 2612 4735975 FIRE DETECTOR BOEING 737 7377H4 1384404 NM AFT CARGO BAY FAULTY A SWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 29 484WN 33841 DIVERSION/DECLARED EMERGENCY. AFT CARGO FIRE WARNING LIGHT ILLUMINATED AND BELL SOUNDED AT ALTITUDE. DISCHARGED SUPPRE SSION SYSTEM. ON ARRIVAL NO VISUAL INDICATION OF FIRE. REMOVED AND REPLACED AFT A2 DETECTOR, CARGO DETECTOR ELECTRONIC UNIT AND FIRE BOTTLE PER MM. 2 L 7 2 4F RT A16WE 20081002 2008 10 2 SWAA084989 4 20080910 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 791SW 27886 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084991 1 20080911 A 5754 SKIN BOEING 737 7375H4 138449D NM NR 1 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED 18Y CHECK, FOUND LT WING NR 1 L/E SLAT AFT INBOARD CORNER DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084992 1 20080911 A 5753 SKIN BOEING 737 7375H4 138449D NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED 18Y CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP INBOARD END DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 UPS08553420 1 20080925 A 2560 SEAL BOEING 757 75724APF 1384969 NM CABIN BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 455UP 25476 INSPECTION TYPE:N/A 2ND, 3RD, 4TH, FROM FWD EMERGENCY DESCENT DEVICE HAS BOTH SEALS BROKEN. REMOVED AND REPLACED EMERGE NCY DESCENT DEVICES PER MM 25-61-00-4. 2 L 7 2 4F RT A2NM 20081003 NM 2008 10 3 UPS08553418 1 20080930 A 2560 SEAL BOEING 757 75724APF 1384969 NM COCKPIT BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 470UP 25486 INSPECTION TYPE:N/A FWD EMERGENCY DESCENT DEVICE HAS ONE SEAL BROKEN. REMOVED AND REPLACED DESCENT DEVICE REF MM 25-61- 02-2. 2 L 7 2 4F RT A2NM 20081003 NM 2008 10 3 SWAA084994 1 20080911 A 5311 6546550 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA084999 1 20080911 A 5753 6546435336 FLAP BOEING 737 737317 138447P NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP P ER MM. 2 L 7 2 4F RT A16WE 20081003 2008 10 3 UPS08853318 4 20080911 A 2565 SLIDE DOUG DC8 DC873F 302199F WP EMERGENCY EXIT UNWANTED DEPLOY A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 808UP 46008 INSPECTION TYPE:N/A JUMP SEATER OPENED DOOR WITH RAFT ATTACHED. REPACKED EMERGENCY DOOR SLIDE AND SECURED. CHECK OK . 2 L 7 4 4F RT 4A25 20081003 NM 2008 10 3 2008UALA03346 1 20080612 A 3350 20131A BATTERY PACK BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 330UA 24191 CREW REPORTS, THE EMERGENCY EXIT LIGHTS ARE ON WITH THE DISARM SWITCH IN THE DISARM POSITION. REPLACED S7 EMERGENCY EXI T LIGHT SWITCH ON P5 OVERHEAD PANEL,REPLACED 2 EACH BATTERY PACKS AT FWD GALLEY OVERHEAD AREA, REF WDM 33-51-11. OP CHE CKS OK REF MM 33-51-02. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081003 NM 2008 10 3 2008UALA05566 1 20080902 A 3510 60B008791 OXYGEN BOTTLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW O2 LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 203UA 24718 CREW O2 LOW. FOUND FAULTY O2 BOTTLE SUSPECT FAULTY O-RING. REPLACED O2 BOTTLE. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081003 2008 10 3 DXT2008F00005 4 20080905 A 2210 TRIM SYSTEM GULSTM 200 200 4500308 NM AUTOPILOT FAILED E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 716QS 148 AUTO PILOT PITCH TRIM FAILED. (K) 2 L 7 2 4F RT A53NM 20081003 2008 10 3 2008UALA05600 4 20080905 A 2565 D31516109 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR UNSERVICEABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 428UA 523 EMERGENCY LIGHT TEST FAILED WITH MSG, EXTERNAL LOAD FWD LEFT. REPLACED PSU 10WL AND BATTERY, NO HELP. RE-INSTALLED ORI GINAL. SWAPPED L FWD AND R FWD SLIDES, ALSO NO HELP. RE-INSTALLED ORIGINAL. REPLACED DOOR 1LT SLIDE. CHECKS NORMAL. ALL EMERGENCY TEST FUNCTIONS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05624 1 20080907 A 3350 58673 INVERTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 595UA 28748 CENTER SECTION BY FWD CTR EMERGENCY EXIT WILL NOT ILLUMINATE DURING TEST, FOUND INVERTER FOR ASSOCIATED AREA COLD. SUSP ECT INVERTER FAILURE. REPLACED INVERTER. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081003 NM 2008 10 3 2008UALA05665 1 20080909 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 FLOORBEAM 145 HAS LOOSE RIVET(MARKED). MAJOR REPAIR ACCOMPLISHED. BEAM OUT AND ON BENCH WORKING. FOUND CORRODED BEAM REPLACED. ACP INSP OF BEAM 145. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 SO 2008 10 3 C2X2008F00025 1 20080902 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO CABIN ODOR A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16963 145116 THE CREW REPORTED SMOKE OR ELECTRICAL, ODOR IN THE CABIN AND FLIGHTDECK DURING TAXI. THE AC RETURNED TO THE GATE WITHOU T FURTHER INCIDENT. MAINT INSPECTED CONTACTORS, RELAYS AND ELECTRICAL CONNECTIONS IN THE COCKPIT. CHECKED OPERATION FO T HE LAV AND CABIN LIGHTS, BALLASTS AND SOCKETS. INSPECTED ENG NR 1 AND NR 2 AND APU FOR LEAKS AND BLEED VALVE OPERATION. NO DEFECTS FOUND. PERFORMED ENGINE RUNS AND APU OPERATION AND NO FAULTS OR EVIDENCE OF SMOKE OR ELECTRICAL FAILURES WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081003 2008 10 3 ANC2008F00002 4 20080901 A 3160 4608000306 DISPLAY DOUG MD80 MD83 3023681 NM ALTITUDE INOPERATIVE W ANCF A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 23 583AN 53183 AIR TURN BACK, AFTER LIFT OFF CAPT AND F/O PRIMARY DISPLAY AND NAV DISPLAY WENT BLANK, AIRSPEED INDICATOR, ALTIMETER SHO WED FLAGS. GONE AHRS DISPLAYED. CAPT`S VSI AND CAPT`S RMI SHOW HDG FLAG AND VSI AND RA FLAGS. FTR AND RTS WERE ACCOMPLI SHED AT BOTH DFGC SHOWED GO IAW AMM 22-01-05, PAG 204. OPERATIONAL TEST ADC AMM: 34-16-01 PAG 02 ITEM 7 AND ACCORDING AM M: 34-21-10 PAG 201. BOTH ATTITUDE AND HEADING REFERENCE UNIT WERE REPLACED, TEST SATISFACTORY IAW AMM 34-14-01 VSI OPER ATIONAL TEST WAS ACCOMPLISHED AND AMM 22-01-05 DFGS TEST ACCOMPLISHED WERE FOUND SATISFACTORY. (K) 2 L 7 2 4F RT 20081003 NM 2008 10 3 NSV2008F00021 1 20080913 A 3220 LOCK BOMBDR DHC8 DHC8402 1390042 NM NLG MALFUNCTIONED A NSVA O OTHER J WARNING INDICATION NR NOT REPORTED 1 EA 27 202WQ 4202 NOSE GEAR DID NOT RETRACT IN FLIGHT. RESET GROUND LOCK IAW AMM 9-10-00, OPS CHECK GOOD. (K) 2 H 7 2 4T RT A13NM 20081002 NM 2008 10 2 2008UALA05548 1 20080831 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 180UA 25224 CEILING EMERGENCY LIGHT ABOVE DOOR 1R INOP. FAULTY LAMP. RELAMPED, OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081002 NM 2008 10 2 2008UALA05568 1 20080902 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 630 S16L DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 EXT FUSELAGE STA 630 FWD OF L-2 DOOR, STR 16L HAS DENTED FASTENER HOLES. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED DAM AGED STRINGER SECTION. FABRICATED & INSTALLED A NEW SECTION AND SPLICE ANGLES. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 CALA0800856 1 20080905 A 5311 146A1141 FRAME BOEING 737 737724 13844BY NM BS 827 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27722 28789 CRACK IN BELT FRAME AT STA 827, BETWEEN S8-9R AT FASTENER FOR OVERHEAD BIN MOUNT. INSTALLED REPAIR PER EC/RA 5310-04824 REV A. 2 L 7 2 4F RT A16WE 20081002 SO 2008 10 2 C2XA08IA216 1 20080925 A 3320 BALLAST EMB 145 EMB145LR 3260212 SO CABIN FAULTY A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 13955 145075 IAH - FLT 2001, DURING PREFLIGHT INSPECTION THE CREW REPORTED A STRONG SMELL OF ELECTRICAL COMPONENTS COMING FROM THE CA BIN. MX REMOVED AND REPLACED BALLAST FROM SEAT 12BC. OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081002 NM 2008 10 2 2008UALA05896 1 20080925 A 5414 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 STRUT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 NR 2 STRUT, ONBOARD AFT SKIN CRACKED AT PANEL CUTOUT RADIUS, FORWARD OF AFT BULKHEAD. MAJOR REPAIR ACCOMPLISHED. STOP- DRILLED CRACK. VERIFIED HFEC. INSTALLED -1 & -3 DOUBLERS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 2008UALA05874 1 20080924 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 SEAT 2F FWD EEL LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 20081002 NM 2008 10 2 ASAA0873489 1 20080828 A 5320 146A81271 FLOOR SUPPORT BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 AFT CARGO FLOOR SUPPORT WEB BS 767 790 CORRODED. AFT CARGO CORRODED FLOOR SUPPORT WEB AT LS 767 790 REPLACED WITH NEW P ART IAW B737 700 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873483 1 20080828 A 5320 149A81189 FLOOR SUPPORT BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 AFT CARGO FLOOR SUPPORT ANGLE CORRODED BS 947 LBL 13 TO RBL 22. REPLACED WITH NEW PART. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873503 1 20080904 A 5320 143A75035 INTERCOSTAL BOEING 737 737790 13844CN NM CARGO BAY CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 FWD CARGO INTERCOSTAL AT LBL 22 STA 500A TO 500B FOUND CRACKED. UPON INSTALLATION OF ZEE ANGLE CRACKED INTERCOSTAL AT L BL 22 FWD CARGO STA 500A TO 500B REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53 30 53 AND BOEING DRAWINGS 143A7510. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873502 1 20080904 A 5320 143A75035 INTERCOSTAL BOEING 737 737790 13844CN NM CARGO BAY CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 FWD CARGO INTERCOSTAL AT LBL 22 STA 500B TO 500 C FOUND CRACKED. ON INSTALLATION OF ZEE ANGLE CRACKED INTERCOSTAL AT FW D CARGO LBL 22 STA 500B TO 500 C REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53 30 53 AND BOEING DRAWING 143A7510. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873500 1 20080828 A 5320 453A26113 CHANNEL BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 AFT CARGO LT ZEE CHANNEL BS 707 TO 847 CORRODED. REPAIRED PART LT ZEE CHANNEL AT AFT CARGO BS 727 847 IAW B737 700 SRM 51 40 05. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873499 1 20080903 A 5320 143A751015 INTERCOSTAL BOEING 737 737790 13844CN NM CARGO BAY CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 FWD CARGO INTERCOSTAL AT LBL 22 SR26L BETWEEN STA 500 AND 500A FOUND CRACKED UPON INSTALLATION OF ZEE ANGLE. CRACKED IN TERCOSTAL AT LBL 22 STR 26L BETWEEN STA 500 AND 500A REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53 30 53 AND BOEING DRAWING 143A7570. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873491 1 20080828 A 5347 146A75035 CARGO TRACK BOEING 737 737790 13844CN NM CARGO BAY DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 AFT CARGO PIT MISDRILLED HOLES ON CARGO TRACK ET BS 7270 T10 LBL 7. AFT CARGO PIT MISDRILLED HOLES ON CARGO TRACK AT BS 727+10 LBL 7 REPAIRD IAW B737 700 SRM 53 00 53 REPAIR 2. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873490 1 20080828 A 5347 146A750125 CARGO TRACK BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 AFT CARGO PIT RT TIE DOWN TRACK FOUND CORRODED AT BS 767TB. REPLACED TIE DOWN TRACK 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 2008UALA05618 1 20080906 A 2997 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HYD PUMP DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 RIGHT ACMP CONNECTOR D486P, PIN 'B' IS BURNED, SHOWS SIGNS OF ARCING. REPLACED RIGHT ACMP CONNECTOR D486P PIN "B". OPS CHKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 2008UALA05619 1 20080906 A 5320 ANGLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1394 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 AFT PIT STA 1394, BL 0, CORROSION ON ANGLE AT FRAME ATTACH TO SKIN. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR T IE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 2008UALA05620 1 20080906 A 5347 SEAT TRACK BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 795 LBL 62 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 CORROSION ON SHORT SEAT TRACK AT BS 795, LBL 62. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SEAT TRACK SECTION. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 2008UALA05625 1 20080907 A 2910 520850 GENERATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYD SYSTEM LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 595UA 28748 HMG TEST FAILED WITH ONLY PARTIAL VOLTAGE SHOWING ON EICAS. REPLACED HMG PER MM 24-25- 01. PERFORMED OPERATIONAL TEST AND LEAK CHECK. FOUND HYDRAULIC FLUID LEAKING FROM MAIN BODY PARTING SURFACES. RE-INSTALLED ORIGINAL HMG, OPS CHECK GO OD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 CALA0800903 1 20080916 A 5210 146N6100671 SKIN BOEING 757 75733N 1384931 NM L4 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 57869 32593 L4 DOOR INNER SKIN IS CRACKED AT THE UPPER HINGE CUTOUT AREA. REPAIRED PER ECRA 5210-02031. DIP WRITTEN TO ACCOMPLISH PERMANENT REPAIR WITHIN 12 MONTHS FROM SEP 15 2008 PLANNING TO CONTACT ENGINEERING AFTER 10 MONTHS BUT BEFORE 11 MONTHS FOR A PERMANENT REPAIR. DIP CTL 090286. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 CALA0800902 1 20080916 A 5312 65465684524 BULKHEAD BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 AFT PRESSURE BULKHEAD WEB FROM FLOOR LEVEL TO Y-CORD FROM APPROXIMATELY LBL 6 TO APPROXIMATELY LBL 20 HAS OVERHEAT DAMAG E. REMOVED AFT PRESSURE BULKHEAD WEB FROM CENTER RING TO Y-CHORD AND REPLACED BULKHEAD WEB (P/N-65-46568Y524) AND DOUBL ER (P/N-65-46568-696) PER BOEING DWG 65-46568.B737-300 SRM 51-40-02, 51-20-01, AND 51-20-05. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800898 1 20080916 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 867 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. INSTALLED REPAIR ANGLES O N FRAME 867 BETWEEN STR 8R AND 9R PER EA5310-04498. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800895 1 20080916 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 400 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET LT SIDE BETWEEN STRINGER 8L AND 9L. REPAIRED IN ACCORD ANCE WITH EA5310-04498 REMOVED A/C RAIL BRACKET, CUT OUT DAMAGED AREA, PERFORMED HFEC, FABRICATED AND INSTALLED REPAIR P ARTS IAW EA5310-04498. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800893 1 20080916 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 400 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. REMOVED A/C RAIL BRACKET, CUT OUT DAMAGE IN FRAME. PERFORMED HFEC. FABRICATED AND INSTALLED REPAIR PARTS IAW EA5310-04498. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085234 1 20080927 A 5240 141A65162 BOLT BOEING 737 7377H4 1384404 NM R1 DOOR DISCONNECTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 924WN 36628 R1 DOOR WOULD NOT OPEN. CONNECTED BOLT PER MT. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800930 1 20081001 A 5230 6547952U133 WEB BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 C2 DOOR WEB CRACKED ON UPPER FORWARD SIDE UNDER PULLEY BRACKET OF COUNTER BALANCE. INSTALLED NEW FRAME PER 51-40-02. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085280 1 20080930 A 3350 300432 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED SPV CHECK, FOUND EXTERNAL LT EMERGENCY EXIT LIGHT INOP AT AFT LOWER WING TO BODY FAIRING. REPLACED LIG HT PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085300 1 20080930 A 3350 65C27095 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND R1 EMERGENCY EXIT OVERHEAD DOOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM . 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085299 1 20080930 A 3350 65C27095 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT OVERWING EXIT. REMOVED AND REPLACED BATTERY PACK PER MM . 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085293 1 20080930 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND AFT RT CREASE BEAM CORRODED BETWEEN BS 943 AND BS 1006. REMOVED AND REPLACED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085290 1 20080930 A 2560 PH22300L GLOWSTRIP BOEING 737 7373Y0 1384671 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED 22Y CHECK, FOUND PHOTOLUMINESCENT STRIP CRACKED BETWEEN BS 336 TO BS 947. REPLACED STRIP PER SWA DWG. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085288 1 20080930 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 747, STR 27L TO STR 27R. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086148 1 20081111 A 3350 20131 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED SPV CHECK, FOUND RT EMERGENCY EXIT LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086136 1 20081111 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 453WN 29847 DURING SCHEDULED MV3 CHECK, FOUND EGRESS LIGHT COVER MISSING AT ROW 19. INSTALLED LIGHT COVER PER MM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086153 1 20081111 A 5754 6573714 SLAT BOEING 737 737317 138447P NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND RT WING L/E NR 4 SLAT O/B DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086134 1 20081111 A 5754 65C26002312A WEDGE BOEING 737 7373H4 1384600 NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE DELAMINATED AT O/B EDGE. REPAIRED WEDGE PER MM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 TSAA0852029 1 20081109 A 2130 CABIN PRESSURE BOEING 737 737210C 1384459 NM FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 834AL 20917 FLT 940, HNL-KOA: AFTER TAKEOFF WITH PRESSURIZATION SYSTEM IN NORMAL AUTO MODE, THE CABIN PRESSURE CLIMBED. WITH THE A IRCRAFT SWITCHED TO STANDBY, HAD SAME RESULTS. OUTFLOW VALVE WAS FULLY CLOSED; SAME RESULTS. RETURNED TO HNL, NO EMERG ENCY DECLARED. UNEVENTFUL LANDING. SDR STATUS - OPEN 2 L 7 2 4F A16WE 20081113 NM 2008 11 13 ASAA0843717 1 20081030 A 5320 65C2640212 WEB BOEING 737 7374Q8 138447Q NM BS 755 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 RT SHEAR WEB IS SCRATCHED STA 755. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 51 70 13. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843727 1 20081029 A 5310 6545855103 STRUCTURE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 INNER CHORD AT R2 DOOR WAY IS CORRODED. REMOVED CORRODED INNER CHORD FABRICATED AND INSTALLED INNER CHORD IAW SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843732 1 20081029 A 5755 654645170 SKIN BOEING 737 737490 1384715 NM SPOILER DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 RT OUTBOARD GROUND SPOILER HAS PROTRUSION ON UPPER SURFACE AT O/B END ABOVE LOWER BLADE SEAL RETAINER. PREPPED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND BONDED DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843734 1 20081029 A 5755 654645268A SKIN BOEING 737 737490 1384715 NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 NR 5 SPOILER UPPER SURFACE HAS MULTIPLE DENTS IN CLUSTERS. PREPPED DAMAGED AREA, FABRICATED REPAIR PARTS BONDED THE REP AIR IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20081113 EA 2008 11 13 ASOA0801222 1 20080922 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA ESCAPE HATCH DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED AND REPLACED CREW ESCAPE HATCH OUTER HANDLE IAW SRM 51-42-06. REQUIRES PAINT. PAINTED REPAIR IAW SRM 51-25-01. REQUIRES LEAK CHECK. LEAK CHECK GOOD IAW MM 21-32-00-863-801. 2 L 7 2 4F RT A21EA 20081113 NM 2008 11 13 ASAA0843735 1 20081028 A 5755 654645268A SKIN BOEING 737 737490 1384715 NM NR 4 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 NR 4 SPOILER HAS A DENT ON LOWER SURFACE 2 INCHES O/B OF I/B END 8.5 INCHES FWD OF TRAILING EDGE. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, AND BONDED THE REPAIR IAW SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0853725 1 20081108 A 2131 71211997101AC CONTROLLER BOEING 737 737890 1384527 NM CABIN PRESSURE MALFUNCTIONED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 577AS 6566 35186 AUTO FAIL LIGHT AND ALTN LIGHT ILLUMINATED WITH PRESSURIZATION MODE CONTROL SWITCH IN AUTO POSITION. PERFORMED TASK 21 31 00 700 802 ON PRESSURIZATION CONTROL. OPS CHECK NORMAL SYSTEM RESET. VERIFICATION FLIGHT SUCCESSFUL. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843715 1 20081106 A 5522 65C25746141A SKIN BOEING 737 7374Q8 138447Q NM LT ELEVATOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 CRACK IN LT ELEVATOR UPPER SKIN O/B OF TAB CONTROL ROD. REMOVED DAMAGED AREA OF SKIN, PREPPED AREA AND REPAIR, INSTALLE D REPAIR PLIES IAW 737 400 SRM 51 70 10 REPAIR 1. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843714 1 20081109 A 5753 07311P0002 NUT BOEING 737 7374Q8 138447Q NM TE FLAPS LACK OF LUBE A ASAA O OTHER O OTHER LD LANDING 1 NM 02 765AS 11132 25102 FLAPS WOULD NOT EXTEND PAST 15 DEG, NO SPLIT OBSERVED. CREW REPORTS NO "NEEDLE SPLIT" & NO ABNORMAL ROLL CONTROL INPUTS REQUIRED. CONDUCTED VISUAL INSPECTION OF FLAP TRACK & DRIVE MECHANISM. FOUND SEVERAL DRY JACK SCREWS. LUBED SCREWS & BALL NUTS REF MM 12 22 51. ACCOMPLISHED ASYMMETRY TEST PER MM 27 51 00. CYCLED FLAPS MANY TIMES NO ABNORMAL FUNCTION OR INDICATION NOTED. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0873731 1 20081111 A 5610 69713271 SPRING BOEING 737 737790 13844CN NM COCKPIT WINDOW DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 649AS 30663 F/O EMERGENCY ESCAPE WINDOW DOES NOT LOCK IN AFT POSITION AUTOMATICALLY. ADJUSTED BELLCRANKS (FOUND JAM NUT LOOSE) PER MM 65 12 11 400 801. INSPECTED DITCHING LOCK ASSEMBLY PER MM 65 12 11 400 801 AND FOUND SPRINGS HAD FALLEN OFF. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843744 1 20081023 A 5730 65C27024 SKIN BOEING 737 737490 1384715 NM RT WING LE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 RIGHT WING INBOARD LEADING EDGE DENTED. REMOVED DAMAGED AREA. INSTALLED DOUBLER AND FILLER PER SRM 57 41 01. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085287 1 20080930 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND FRAME CRACKED AT BS 328, STR 20R TO STR 21R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085282 1 20080930 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 360 TO BS 380, STR 17R. REMOVED AND REPLACED BEAM PER S RM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085281 1 20080930 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 750, STR 25R. REMOVED AND REPLACED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085298 1 20080929 A 5311 6546551 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 807, STR 27L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 UPS08553422 1 20080925 A 2560 SEAL BOEING 757 75724APF 1384969 NM CABIN BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 455UP 25476 INSPECTION TYPE:N/A FWD EMERGENCY DESCENT DEVICE HAS BOTH SEALS MISSING/BROKEN. REMOVED AND REPLACED DESCENT DEVICE PER MM 25-61-00-4. 2 L 7 2 4F RT A2NM 20081003 NM 2008 10 3 UPS08553421 1 20080926 A 2560 SEAL BOEING 757 75724APF 1384969 NM CABIN BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 455UP 25476 INSPECTION TYPE:N/A 5TH & 6TH FROM FWD EMERGENCY DESCENT DEVICE HAS SEALS BROKEN. REMOVED AND REPLACED DESCENT DEVICE P ER AMM 25-61-00-4 IN 5TH & 6TH POSITION. 2 L 7 2 4F RT A2NM 20081003 NM 2008 10 3 CALA0800874 1 20080912 A 5320 FLOOR SUPPORT BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19136 29285 AFT BAG BIN CARGO FLOOR SUPPORT STRINGER CORRODED AT FS 1470 RBL 7.55. REPAIRED AS PER ECRA 5321-01567. 2 L 7 2 4F RT A2NM 20081003 NM 2008 10 3 CALA0800875 1 20080912 A 5320 FLOOR SUPPORT BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19136 29285 AFT BAG BIN CARGO FLOOR SUPPORT STRINGER CORRODED AT FS 1470 RBL 10.45. REPAIRED AS PER ECRA 5321-01567. 2 L 7 2 4F RT A2NM 20081003 NM 2008 10 3 G8G2008F00000 1 20080528 A 3110 6560214106 ACCESSORY UNIT BOEING 727 727200 138407E NM INSTRUMENT PANEL MALFUNCTIONED A G8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 713AA 22469 DURING CRUISE OPERATION CAPTAIN’S RMI CARD AND FO`S HSI CARD STOPPED TURNING IN FLIGHT, BOTH RMI NEEDLES FROZE IN POSITI ON. AC RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THE FLIGHT INSTRUMENT AC CY UNIT AT FAULT. REMOVED AND REPLACED FLIGHT INSTRUMENT ACCY UNIT, OPS CHECK GOOD. NO OTHER DEFECTS WERE NOTED. AIRCRAF T WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F RT A3WE 20081003 CE 2008 10 3 JNE2008F00000 1 20080821 A 8011 65556624V STARTER CESSNA 337 T337G 2075726 CE CONT O360 TSIO360CB 17025 SO ENGINE FAILED E JNEA O OTHER O OTHER NR NOT REPORTED 1 WP 21 1ZJ P3370267 824817R INSTALLED TWO FACTORY ENGINES. AFTER SEVERAL TEST RUNS , THE FRONT STARTER SOLENOID FAILED ON. REPLACED THE SOLENOID WI TH AN NEW MFG SOLENOID. ON A TEST FLIGHT ELECTRICAL FAILURE OCCURRED. IT HAPPENED BECAUSE OF AN OVERLOAD OF THE BATTER Y AND ELECTRICALSYSTEM . AFTER MANUALLY PUMPING THE LANDING GEAR DOWN, LANDED WITHOUT INCIDENT. AFTER TROUBLESHOOTING, FOUND THE NEW STARTER SOLENOID FAILED AND STARTER WAS ENGAGED. CALLED MFG PILOT ASSOCIATION AND THEY EXPLAINED THAT MFG USES A NEW STARTER THAT USES 400 AMPS AND THE MFG SOLENOID IS ONLY RATED 200 AMPS. THE SOLENOID MAY FAIL ON THE FIRST U SE OR ANY USES THERE AFTER. THEY ALSO MENTIONED MFG KNOWS ABOUT THE PROBLEM AND IS UNWILLING TO CORRECT IT. AFTER CAL 1 H 7 2 3O 3 O A6CE E9CE 20081003 NM 2008 10 3 UPS08M53326 1 20080913 A 3350 OM77839 LIGHT DOUG MD11 MD11F 3023600 NM CREW REST INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 273UP 48574 INSPECTION TYPE:PS5 EMERGENCY LIGHT IN FORWARD CREW REST MODULE ABOVE BUNK INOP. RELAMPED AND TESTED PER MM 33-50-00-5. 2 L 7 3 4F RT A22WE 20081003 NM 2008 10 3 SWAA085026 1 20080913 A 3246 162A11204 BEARING BOEING 737 7377H4 1384404 NM NLG FAILED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 29 290WN 36632 DECLARED EMERGENCY. AFTER NORMAL LANDING, GROUND ADVISED NOSE TIRES SMOKING. INSPECTED NLG FOUND LT NLG TIRE INNER BEA RING FAILED. REMOVED AND REPLACED NLG STRUT INNER CYLINDER PER MM. 2 L 7 2 4F RT A16WE 20081003 2008 10 3 SWAA085027 4 20080912 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085028 1 20080912 A 5753 6546434368 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP P ER MM. 2 L 7 2 4F RT A16WE 20081003 CE 2008 10 3 AJC2008F00001 1 20080914 A 2611 SMOKE DETECTOR CESSNA 525 525 2076601 CE CARGO BAY FALSE ACTIVATION E AJCA O OTHER N FALSE WARNING DE DESCENT 1 EA 65 12GS 0122 IN THE DESCENT FROM ALTITUDE FL430, THE BAGGAGE SMOKE LIGHT ILLUMINATED (RED). ACTION TAKEN BY CAPTAIN WAS REQUEST FOR P RIORITY HANDLING TO A SAFE LANDING IN MINUTES WITHOUT INCIDENT. PERFORMED VISUAL INSPECTION OF THE FWD AND AFT BAGGAGE C OMPARTMENTS FOUND NO EVIDENCE OF SMOKE OR FIRE PRESENT. THIS IS A KNOWN ISSUE WITH MFG. THE FWD COMPARTMENT IS PRONE T O CONDENSATION WHICH TRIGGERS A BAGGAGE SMOKE ALERT. PREFORMED A BAGGAGE COMPARTMENT FIRE DETECTION TEST, SYSTEM TESTS N ORMAL. (K) 1 L 7 2 4F RT A1WI 20081003 NM 2008 10 3 C8G2008F00013 1 20080611 A 7722 152BL801E INDICATOR BOEING 727 727225 1384077 NM PWA JT8 JT8D15 52051 NE EGT FAULTY A C8GA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 SO 29 801EA 22432 DURING TAKEOFF ROLL THE NR 2 ENGINE EGT INDICATOR WENT TO ZERO INDICATION. THE TAKEOFF WAS ABORTED, WHERE THE AC RETURNE D TO BLOCKS WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED NR 2 ENGINE EGT INDICATOR AT FAULT. THE NR 2 ENGINE EGT IN DICATOR WAS REMOVED AND REPLACED. OPS GOOD. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F 4 F A3WE E2EA 20081003 NM 2008 10 3 KPV2008F00002 1 20080911 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8103 1386005 NM AFT CARGO BAY FALSE ACTIVATION A KPVA O OTHER N FALSE WARNING AP APPROACH 1 WP 13 808WP 026 ON APPROACH, "SMOKE" WARNING LIGHT CAME ON, REMAINED ON FOR 3 SECONDS THEN WENT OUT. AFTER LANDING LIGHT CAME ON AGAIN T HEN WENT OUT AFTER A FEW SECONDS. VISUALLY INSPECTED NR 1 AND NR 2 SMOKE DETECTORS, NO DEFECTS NOTED. PERFORMED OPS CHEC K OF SMOKE DETECTION SYSTEM GOOD IAW MM 26-12-00, PG 201. (K) 2 H 7 2 4T RT A13NM 20081003 NM 2008 10 3 SWAA085030 1 20080912 A 5755 654645268A SPOILER BOEING 737 7373H4 1384600 NM RT WING LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 GROUND SPOILER HAS LATERAL MOVEMENT. REMOVED AND REPLACED SPOILER PER MM . 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085037 1 20080911 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 DURING SCHEDULED HC1 CHECK, FOUND AFT SERVICE DOOR SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085038 1 20080914 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827 STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085039 1 20080914 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085042 1 20080914 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085043 1 20080914 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085053 1 20080914 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 20081003 EA 2008 10 3 COMA086375 1 20080829 A 5210 601R31902 SKIN CNDAIR CL600 CL6002B16 1900305 EA PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 420CA 7451 PAX DOOR INNER SKIN IS CRACKED AT DOOR DATUM 1 BETWEEN FS 338.90 TO 3490. REPAIRED PER EA 10-5210-02307. 2 L 7 2 4F RT A21EA 20081003 EA 2008 10 3 COMA086381 1 20080902 A 2621 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA FIRE WARNING ACTIVATED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 914CA 7012 EN ROUTE FROM CVG TO AVP RECEIVED CARGO BOTTLE LOW CAUTION MSG IN FLT. ACFT DIVERTED TO PIT AND LANDED SAFELY. DEFERRE D PER MEL 26-25-01. 2 L 7 2 4F RT A21EA 20081003 EA 2008 10 3 HNAA0800252 1 20080612 A 5210 GOOSENECK ASSY DHAV DHC8 DHC8311 1386006 EA PAX DOOR CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 335EN 32270 375 CORROSION PAX DOOR GOOSENECK FOUND CORRODED FWD AND AFT. REPLACED PAX DOOR GOOSENECK. 2 H 7 2 4T RT A13NM 20081003 EA 2008 10 3 HNAA0800278 1 20080907 A 2163 BYLF51514 SENSOR DHAV DHC8 DHC8311 1386006 EA COCKPIT FAILED A HNAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 337EN 34413 284 WHEN FLIGHT CREW POWERED ACFT UP FOR PRE-FLIGHT CHECKS, A NOISE WAS HEARD BEHIND THE CAPTAINS SEAT AND AN ODOR OF RUBBER WAS DETECTED. MX FOUND THE ZONE TEMP SENSOR FAN BEHIND CAPTAINS SEAT TO BE THE SOURCE OF THE ODOR. SYSTEM WAS DEACTIV ATED AT THAT TIME. WHEN ACFT REACHED A MX BASE, THE TEMP SENSOR UNIT WAS CHANGED. OPS CHECKS WERE GOOD AND SYSTEM WAS REACTIVATED. ACFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 20081003 EU 2008 10 3 2008UALA03113 2 20080602 A 7261 3353112040 CARBON SEAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 ENGINE LEAKING A UALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 29 329UA 52 24149 860242 LOSS OF OIL NR 1 ENGINE CAUSED FLIGHT DIVERSION UNDER AMBER ALERT. OIL LEAK. REPLACED THE STARTER CARBON SEAL AND SEAL SEAT. 2 L 7 2 4F 4 F RT A16WE E21EU 20081003 NM 2008 10 3 2008UALA05458 1 20080825 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 519UA 24872 EXTERIOR EEL LIGHT AT DOOR 2L IS INOP. BULB INOP/OUT. RELAMPED, OP CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081003 NM 2008 10 3 2008UALA05736 1 20080915 A 3397 80172424 CABLE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN DISCONNECTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 791UA 26933 EMERGENCY LIGHT AT SEAT 38C WILL NOT WORK. FOUND CABLE DISCONNECTED. RE-SECURED CABLE. TESTS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081003 NM 2008 10 3 2008UALA05737 1 20080915 A 3350 1317 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 791UA 26933 EMERGENCY CEILING LIGHT IN AFT GALLEY WILL NOT WORK. LIGHT FOUND INOP. REPLACED LAMP. TESTS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081003 NM 2008 10 3 2008UALA05738 1 20080915 A 3350 8100035701 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 791UA 26933 EMERGENCY LIGHT IN AFT GALLEY FLOOR LEVEL LT SIDE WILL NOT WORK. FOUND DEFECTIVE LAMP. REPLACED LAMP. TESTS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081003 NM 2008 10 3 2008UALA05740 1 20080915 A 5210 CYLINDER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE R1 DOOR LOW PRESSURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 834UA 1420 DOOR 1 RIGHT EMERGENCY OPERATION CYLINDER PRESSURE IS LOW. SERVICED CYLINDER. SERVICED CYLINDER, NO LEAKS NOTED AT TIM E OF SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 2008 10 3 2008UALA05741 4 20080914 A 2565 GASKET BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ESCAPE SLIDE FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 574UA 26686 FOUND LT OFFWING SLIDE INFLATION HOSE GASKET BROKEN. REPLACED INFLATION GASKET. 2 L 7 2 4F 4 F RT A2NM E17NE 20081003 NM 2008 10 3 2008UALA05742 1 20080911 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 817UA 873 FWD GALLEY OUTBOARD "B" FLOORBEAM HAS ONE FOOT SECTION WITH CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED BRACKETS. INSTALLED MFG'ED BEAM. INSTALLED ALL WIRE BUNDLES AND SECURED ALL CLAMPS BEAM. FINAL INSTALLATION IS COMPLETE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05743 1 20080915 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 817UA 873 BEAM UNDER FLOORBOARD AT DOOR 1 RIGHT HAS CORROSION ON IT. FIRST BEAM INBOARD OF SILL. MAJOR REPAIR ACCOMPLISHED. INST ALLED BEAM JUST INBOARD OF 2R SILL. BEAM IS B-BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05750 1 20080917 A 2121 4100943C FAN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT LAVATORY DAMAGED A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 777UA 26916 CABIN AND FLIGHT DECK TEMP PROBLEMS. FOUND RT LAV GALLEY VENTILATION FAN HAD NO BLADES. REPLACED RT LAV GALLEY VENTILA TION FAN. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081003 NM 2008 10 3 2008UALA05880 1 20080925 A 2421 729825G IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT FAULTY A UALA C ABORTED TAKEOFF W INADEQUATE Q C TO TAKEOFF 1 WP 29 546UA 25367 L GEN TRIPPING OFF. IDG FOUND FAULTY. REPLACED LT IDG. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081003 NM 2008 10 3 2008UALA05900 1 20080927 A 2820 S343T00339 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUEL SYSTEM MALFUNCTIONED A UALA D RETURN TO BLOCK W INADEQUATE Q C TX TAXI/GRND HDL 1 WP 29 652UA 25390 FUEL SHUTOFF VALVE PROBLEM. RTBL. REPLACED SPAR VALVE ACTUATOR. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081003 NM 2008 10 3 2008UALA05901 1 20080928 A 5730 PANEL BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU RT WING DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 912UA 25290 RIGHT WING INBOARD LWR FIXED T/E PANEL NEXT TO BODY FAIRING DAMAGED AT WBL 71.26. REPLACED PANEL. 2 L 7 2 4F 4 F RT A16WE E21EU 20081002 NM 2008 10 2 CALA0800865 1 20080905 A 5320 6517684634 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 303 S16L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 INTERCOSTAL CRACKED AT INBOARD AFT FLANGE LOCATED AT BODY STATION 303.9 AND S16L. REPLACED INTERCOSTAL AT BODY STATION 303.9 AND S16L PER EC/RA 5310-04826. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800867 1 20080905 A 5330 6545800 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 R1 DOOR CUTOUT CRACKED AT LOWER AFT CORNER OF CUTOUT. CUT OUT DAMAGED AREA AND REPAIRED SAME PER SRM 53-10-01 REPAIR 2. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873508 1 20080909 A 5754 114A50204 SKIN BOEING 737 737790 13844CN NM L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 NR 7 SLAT INBOARD CORNER LOWER SURFACE CHAFED. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED THE REPAIR IAW B 737 700 SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873505 1 20080903 A 5321 453A261031 FLOOR PANEL BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 AFT CARGO PIT FLOOR PANEL BS 727 D TO 767 + 5 CORRODED. REPLACED WITH MADE REPAIR PART IAW B737 700 SRM 53 60 53, FOUND BEYOND LIMIT IAW B737 700 SRM 53 60 53 AND EA 2550 01425. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873498 1 20080903 A 5320 143A750111 ANGLE BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 FWD CARGO LT ZEE ANGLE BETWEEN STA 490 AND 500D FOUND CORRODED TRANSFERRED FROM MIG 5 NR 5101846 FOR REPAIR. FWD CARGO LT ZEE ANGLE BETWEEN STA 490 AND 500D REPLACED WITH MADE REPAIR PART IAW B737 700. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085091 1 20080916 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 439WN 29834 DURING SCHEDULED HC2 CHECK, LT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843745 1 20081023 A 5754 65C27024 SKIN BOEING 737 737490 1384715 NM NR 4 K FLAP DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 RIGHT FIXED LEADING EDGE DAMAGED, NO SPECIFICS AT NR 4 K FLAP ACTUATOR LOWER EDGE. REMOVED DAMAGED AREA. INSTALLED DOU BLER AND FILLER PER SRM 57 41 01. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843716 1 20081024 A 5753 6546430150 SKIN BOEING 737 7374Q8 138447Q NM RT WING FLAP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 RT WING I/B FORE FLAP LOWER SURFACE HAS VARIOUS DENTS WBL 73-93. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR SKIN AND DOUBLER IAW B737 400 SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081113 SO 2008 11 13 FDKA2008110800292 1 20081108 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT UNSECURE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 850MJ 145568 FRL FLT 6189 JFK-RIC. ROW 12 FWD CEILING EMERGENCY LIGHT INOP. MX RE-SECURED LIGHT ASSY CONNECTORS, OPS CK GOOD. 2 L 7 2 4T RT T00011AT 20081112 WP 2008 11 12 AALA200802337 1 20080910 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 255AA 49287 EMERGENCY LIGHT AT LT GALLEY AISLE INOPERATIVE. REPLACED LAMP. GROUND CHECKED NORMAL. 2 L 7 2 4F A6WE 20081112 WP 2008 11 12 AALA20082340 1 20080910 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 472AA 49647 EMERGENCY LIGHT AT SEAT 24D INOPERATIVE. REPLACED LAMP. GROUND CHECKED NORMAL. 2 L 7 2 4F A6WE 20081112 NM 2008 11 12 DHL2008F00046 1 20081001 A 5754 85C8067819 BRACKET BOEING 727 727223 1384074 NM LT WING SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 780DH 22006 NR 4 SLAT ACTUAROT MOUNT BRACKET CRACKED AT BOTTOM SIDE LWS 410. R&R MOUNT BRACKET IAW SRM 51-10-1 AND 51-30-2. OPS AND LEAK CHECKED OK IAW MM 27-81-32 & 28-11-21. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745637 1 20080908 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 950F BETWEEN S-23L AND S-24L FRAME DENTED. REPAIRED FRAME SECTION AT BS 950F BETWEEN S-21L AND S-25L IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745638 1 20081005 A 5754 SKIN BOEING 727 727224 1384076 NM LE SLAT CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 RT WING NR 7 SLAT SKIN WITH CRACK LOWER SECTION AT SLAT STA 328. REPAIRED RT WING NR 7 SLAT LOWER SKIN BETWEEN SLAT STA 323.5 TO STA 333.5 IAW COOPESA EO COO-2-57-345-08 DTD. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745640 1 20080905 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT STA 720C BETWEEN S-12L AND S-13L FRAME I/B FLANGE HAS DOUBLE HOLE. REPAIRED FRAME SECTION AT BS 720C BETWEEN S-11L AND S-14L IAW B727 SRM 53-10-4 FIG 1 DETAIL 1. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DL757081465 1 20081009 A 5321 SPLICE BOEING 757 757232 1384965 NM FLOOR PANEL CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 614DL 22821 23843 CORROSION ON FLOOR PANEL SPLICE BS 1510 LBL 19 THRU RBL 19. FLOOR PANEL SPLICE REPLACED. 2 L 7 2 4F RT A2NM 20081112 NM 2008 11 12 DHLA2008745608 1 20080903 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER EXTERNAL FUSELAGE BS 178 LBL 3 EDGE SKIN WITH MISSING MATERIAL. REPLACED FUSELAGE EXTERNAL DOUBLER FROM BS 178 TO BS 194 BETWEEN LBL 8 AND RBL 8 IAW BOEING DWG 65-45800 REV F DTD 04/23/97. 2 L 7 3 4F A3WE 20081112 NM 2008 11 12 DHLA2008745620 1 20080901 A 5311 FRAME SPLICE BOEING 727 727224 1384076 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN FRAME SPLICE WITH DOUBLE HOLE AT BS 1130 BETWEEN S-13L AND S-14L. REPLACED FRAME SPLICE SECTI ON AT BS 1130 BETWEEN S-13L AND S-14L IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745629 1 20080902 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT BS 680 BETWEEN S-16R AND S-17R FRAME DENT. REPAIRED FRAME SECTION AT BS 680 BETWEEN S-16R AND S-17R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745630 1 20080902 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT BS 600 BETWEEN S-16R AND 17R FRAME WITH DENT. REPAIRED FRAME SECTION AT BS 660 BETWEEN S-1 6R AND S-17R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745631 1 20080902 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT BS 640 BETWEEN S-16R AND 17R FRAME WITH DENT. REPAIRED FRAME SECTION AT BS 640 BETWEEN S-1 6R AND S-17R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745632 1 20080902 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN AT BS 600 BETWEEN S-16R AND 17R FRAME WITH DENT. REPAIRED FRAME SECTION AT BS 600 BETWEEN 16R AND 17R IAW B727SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 USAAB08107 1 20081112 A 2560 P4010021 BATTERY BOEING 737 7374B7 138449C NM FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 451UW 24934 DCA - MAINTENANCE REPORTED THE AFT EMERGENCY FLASHLIGHT HAS A DEAD BATTERY. MAINTENANCE REMOVED AND REPLACED THE BATTER Y IN THE AFT EMERGENCY FLASHLIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20081113 EA 2008 11 13 ASOA200801448 1 20081103 A 5320 PANEL CNDAIR CL600 CL6002B19 1900309 EA CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 PANEL 281HZ HAS 4 CRACKS. 2 L 7 2 4F RT A21EA 20081113 NM 2008 11 13 USAA920081949 1 20081016 A 5310 6546561509 DOOR FRAME BOEING 737 737301 1384611 NM ZONE200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10853030/001CRACK AT RT AFT SERVICE DOOR CUTOUT INTERIOR STRUCTURE UPPER FORWARD LATCH SUPPORT . REPAIRED RT AFT SERVICE DOOR CUTOUT INTERIOR STRUCTURE UPPER FORWARD LATCH SUPPORT IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081113 EA 2008 11 13 ASOA200801464 1 20081106 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 RT FUSELAGE EXTERIOR SKIN 3.5" FWD OF FS 559+96 AND AT STR 24R HAS MINOR SURFACE CORROSION. REMOVED 16 RIVETS AND CORRO SION, THEN INSTALLED 16 NEW SERVICEABLE RIVETS AT RT FUSELAGE EXT SKIN 3.5 INCHES FWD OF FS 559+96 & AT STR 24R IAW CRJ 200 SRM 51-21-06, 51-42-06, 53-51-31. AREA NEEDS PAINT. TOUCHED UP REPAIR IAW CRJ SRM 51-25-16. MAX MATERIAL REMOVED .003. SUPPLEMENTAL-SDR CLOSED 11/17/2008. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801470 1 20081106 A 5320 PLATE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 RT SIDE PRESSURE FLOOR SILL PLATE HAS CORROSION FROM FS 409+128 TO FS 559, RBL 36 TO RBL 44. REMOVED CORROSION ON R PRE SSURE FLOOR SILL PLATE. REQUIRES REO 601R-53-41-666, STEPS 2.2 C THRU F COMPLIANCE. PERFORMED EDDY CURRENT INSPECTION ON BLENDED AREAS. NO INDICATIONS FOUND AT THIS TIME. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801472 1 20081106 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 LEFT FS 409.0+128 VERTICAL BEAM CRACKED .1 INCH LONG O/B SIDE LBL 18 AT BOTTOM OF BEAM. REPAIRED LT FS 409.0+128 VERTIC AL BEAM LBL 18 O/B IAW BOMBARDIER REO 601R-53-41-056. REQUIRES ECTC. COMPLIED W/ECTC REO 601R-53-41-056 IAW REO 601R-5 3-41-056 REV E. SUPPLEMENTAL-SDR CLOSED 11/17/2008. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801473 1 20081106 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 FS 621-625 UPPER LT OBLIQUE ANGLE CRACKED IN RADIUS. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801475 1 20081106 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 RIGHT FS 280 FLOOR SUPPORT ANGLE CRACKED .3 INCH LONG I/B RBL 9.0. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801478 1 20081106 A 5712 RIB CNDAIR CL600 CL6002B19 1900309 EA RT WING CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 905EV 7632 RT WING BAT WEB AT FS 53.6 CRACKED BETWEEN 2 FASTENERS. REPAIRED RT WING BAT WEB AT WS 53.6 IAW REO 601R-57-51-0046. C /W ASA ECTC REO 601R-57-51-046. SUPPLEMENTAL-SDR CLOSED 11/17/2008. 2 L 7 2 4F RT A21EA 20081113 NM 2008 11 13 DHLA2008745667 1 20080903 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM FUSELAGE CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE MAIN CABIN STA 1130 LBL 8 WL 201 FLOORBEAM LOWER CHORD CRACKED. REPAIRED FUSELAGE FLOORBEAM UPPER CHORD SECTION AT BS 1130 FROM LBL 5 TO LBL 54 AND LOWER CHORD SECTION FROM LBL 67 TO RBL 67 DUE TO CORROSION AND CRACK IAW COO PESA EO COO-2-53-269-08. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745666 1 20080924 A 5730 SKIN BOEING 727 727224 1384076 NM RT WING CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 RT WING AT WBL 446 BETWEEN REAR SPAR AND S-5 WING LOWER SKIN, LOWER SURFACE WITH CORROSION. REPAIRED RT WING LOWER SKIN SECTION AT REAR SPAR AND STIFFENER 5 AT WBL 442 DUE TO CORROSION IAW COOPESA EO COO-2-57-354-08. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745658 1 20080908 A 5311 FRAME BOEING 727 727224 1384076 NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE AFT CARGO COMPARTMENT BS 950B BETWEEN S-23L AND S-24L FRAME DENTED. REPAIRED FRAME SECTION AT BS 950B BE TWEEN S-21L AND S-25L IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745659 1 20080924 A 5240 SKIN BOEING 727 727224 1384076 NM SERVICE DOOR CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE FWD SERVICE DOOR OUTER SKIN FROM BS 386 TO BS 391 BETWEEN DOOR BEAM NR 4 AND LOWER DOOR BEAM REPAIR DOUBL ER DEFORMED AND CORROSION. REPAIRED FUSELAGE FWD SERVICE DOOR OUTER SKIN SECTION FROM BS 380 TO BS 396 BETWEEN DOOR BEA M NR 3 AND LOWER BEAM IAW B727 SRM 52-00-3 FIG 4. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745660 1 20081007 A 2810 VENT LINE BOEING 727 727224 1384076 NM LT WING WORN A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LT WING FUEL VENT TUBE WITH WEAR AT WS 574. REPAIRED FUEL VENT TUBE AT WS 574 IAW COOPESA EO COO-2-28-320-08. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745661 1 20080907 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 UPPER FUSELAGE EXTERIOR FUSELAGE FROM BS 950+5" TO BS 970 S-14R SKIN WITH CORROSION. REPAIRED FUSELAGE SKIN SECTION FRO M BS 350 TO BS 1030 BETWEEN S-13R AND S-15R IAW COOPESA EO COO-2-53-322-08. 2 L 7 3 4F A3WE 20081113 NM 2008 11 13 DHLA2008745650 1 20080906 A 5322 SHEAR TIE BOEING 727 727224 1384076 NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 745DH 20665 LOWER FUSELAGE FWD CARGO COMPARTMENT BS 560 BETWEEN S-26L AND S-27L FRAME AND SHEAR TIE HAS CORROSION. REPLACED SHEAR T IE AT BS 560 BETWEEN S-26L AND S-27L IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081113 2008 11 13 SWAA086137 4 20081107 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086140 1 20081111 A 3350 417S5500 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 701GS 27836 DURING SCHEDULED HC2 CHECK, FOUND RT OVERWING EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086141 1 20081111 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086142 1 20081111 A 5311 6520722 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086143 1 20081111 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086127 1 20081111 A 5753 6546486 WEDGE BOEING 737 7373H4 1384600 NM TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED SPV CHECK, FOUND RT WING I/B TRAILING EDGE FLAP WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER SRM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086149 1 20081111 A 3350 20121 CHARGER BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 616SW 27699 DURING SCHEDULED SPV CHECK, FOUND RT EMERGENCY EXIT LIGHT BATTERY CHARGER BROKEN. REMOVED AND REPLACED CHARGER PER MM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086135 1 20081107 A 3350 P2070001214 FLASHLIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 410WN 27897 FOUND AFT RT FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 SWAA086151 1 20081102 A 3350 MS25237 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 622SW 27932 DURING SCHEDULED MV2 CHECK, FOUND RT EMERGENCY EXIT LIGHT INOP AT ROW 12. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081113 2008 11 13 SWAA086152 4 20081111 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 USAASB08108 1 20081112 A 2560 P4010021 BATTERY BOEING 737 7374B7 138449C NM FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 451UW 24934 DCA - MAINTENANCE REPORTED THE AFT EMERGENCY FLASHLIGHT HAS A DEAD BATTERY. MAINTENANCE REMOVED AND REPLACED THE BATTER Y IN THE AFT EMERGENCY FLASHLIGHT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 ASAA0843742 1 20081029 A 5755 SKIN BOEING 737 737490 1384715 NM GROUND SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 RIGHT INBOARD GROUND SPOILER IS DENTED ON LOWER INBOARD SURFACE 6 INCHES FROM INBOARD END. REMOVED DAMAGED AREA. INSTA LLED DOUBLER FILLER AND BOND REPAIRED PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081113 EU 2008 11 13 YENA200811100106 1 20081109 A 2910 4502310000 SWITCH AIRBUS 320 A320232 3930326 EU HYD SYSTEM LEAKING A YENA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 15 613JB 14319 2449 FLT 705, JFK-SJU, HYD BLUE LOW DURING CLIMBOUT, AIR RETURN TO JFK. FOUND BLUE PUMP PRESS SWITCH LEAKING. REMOVED AND R EPLACED BLUE ELECTRICAL PUMP PRESSURE SWITCH AS PER MM 29-12-17, OPS CHECK AND LEAK CHECK OK, SERVICE BLUE HYD SYSTEM TO LIMITS. 2 L 7 2 4F RT A28NM 20081113 2008 11 13 ABXA080231 4 20080808 A 3444 00301560 CIRCUIT BOARD DOUG DC9 DC941 302207N WP TAWS COMPUTER SHORTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 951AX 53 554 47616 GPWS FAIL LIGHT AND TERR INOP LIGHT ON TAWS CIRCUIT BRAKE TRIPPED. NR 1 ADC AND NR 1 GS C/B TRIPPED. DEFERRED 61397 FOUN D TAWS COMPUTER INOP. CAPPED AND STOWED WIRES TW9020 FROM S30-6 (55) TW9056A FROM S30-16 (32) AND TW9014A22 FROM S30-6 ( 52) IAW REA D934-57692. DEFERRED TAWS SYSTEM IAW MEL 34-29. MAINT PROCEDURES COMPLIED WITH. PLACARD INSTALLED. RESEATED NR 1 ADC AND NR 1 GS CIRCUIT BRAKERS, CHECKED OK CODE 1. REMOVED AND REPLACED TAWS COMPUTER AND REINSTALLED REA D934- 5762. OPS CHECK GOOD IAW DC9 AMM 34-15-00. TEARDOWN RESULTS FROM R/O 501584251. ARINC RECEPTACLE/FILTER BOARD SCRAPPE D TO ENGINEERING FOR ANALYSIS. ENGINEERING RESULTS FOR S/N A040501281 FOUND PIN A31 SHORTED TO BOTH 28V AND GROUND. 2 L 7 2 4F A6WE 20081113 SO 2008 11 13 C2XA08CL120 1 20081104 A 2150 8152403 ACM EMB 145 EMB145LR 3260212 SO AC BAY FAULTY A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 16911 18193 145446 CLE FLIGHT 2368 THE CREW REPORTED SMOKE IN THE CABIN WHILE ON THE GROUND WITH THE APU RUNNING AND PACKS ON. MAINTENANCE INSPECTED AND REPLACED THE RIGHT AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20081113 SO 2008 11 13 C2XA08SH147 1 20081113 A 5320 14525480603 BEAM EMB 145 EMB145XR 3260214 SO CARGO BAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11192 145936 SHV-DURING C-CHECK THE CARGO DOOR LOWER CUT-OUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFF ECTED BEAM IAW EMB 145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081114 NM 2008 11 14 GTIA0800081 1 20081011 A 5320 D53472196200 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM ZONE 900 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 507NK 2560 AFT GALLEY FLOORBEAM CORRODED AT Y254 BETWEEN FR 68 AND FR 70. 2 L 7 2 4F RT A28NM 20081114 EA 2008 11 14 SWIA200820328 1 20081105 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A SWIA O OTHER O OTHER NR NOT REPORTED 1 NM 07 614SK 10051 FLT 4719 - SECOND AFT OVERHEAD EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081114 NM 2008 11 14 CALA0801037 1 20081106 A 5311 654655159 FRAME BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 FRAME CORRODED AT STATION 807, S-25L TO S-27R. REMOVED AND REPLACED BOTTOM FRAME AT STATION 807 FROM STR 25 RT TO STR 2 3 LEFT PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801042 1 20081107 A 5531 65476374 RIB BOEING 737 737524 1384721 NM VERTICAL STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 VERTICAL STABILIZER LEADING EDGE RIB AT STATION 235.90 IS CRACKED ON RIGHT SIDE. INSTALLED REPAIR PER SRM 51-40-02 AND SRM 51-70-11. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801045 1 20081108 A 5315 147A5506 FLOORBEAM BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 73259 30803 FLOORBEAM VERTICAL FLANGE AT STATION 986.5 HAS CRACK FROM CUT-LINE TO FASTENER HOLE AT LBL 50. LBL 50 VERTICAL FLANGE O F FLOORBEAM 986.5. REPAIRED PER ECRA 5321-01584 AND REASSEMBLED PER SRM 53-70-51. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086166 1 20081112 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 573, STR 10L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086167 1 20081112 A 5753 6546435 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 335SW 23939 DURING SCHEDULED HC1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086168 1 20081112 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 450WN 32470 FOUND R1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086172 1 20081112 A 2560 65C16820 FITTING BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 725SW 27857 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR GIRT BAR AFT RETAINING CLIP LOOSE. SECURED CLIP PER MM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086158 1 20081112 A 5311 6545808 FRAME BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 786SW 29811 DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SUB FRAME CRACKED AT BS 294, STR 17R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086159 1 20081112 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 786SW 29811 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 38 TO RBL 5. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086160 1 20081112 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BETWEEN BS 294 TO BS 299, STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801027 1 20081103 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 FRAME CRACKED AT STATION 867 ABOVE S-9R. REPAIRED FRAME PER EA 5310-04498, OP 2. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801032 1 20081103 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 FRAME CRACKED AT STATION 400 ABOVE S-9R. REPAIRED FRAME PER EA 5310-04498, OP 2. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801036 1 20081104 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 FRAME CRACKED AT STATION 360 ABOVE S-9L. REPAIRED FRAME PER EC/RA 5311-01430. 2 L 7 2 4F RT A16WE 20081113 NM 2008 11 13 USAA920081933 1 20081021 A 5754 114N4002103M PANEL BOEING 757 757225 1384959 NM NR 1 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918UW 22196 CLT C3 MAJOR REPAIR NR 19C51057012/001 NR 1 SLAT COVE PANEL CRACKED AT OTBD SLAT TRACK 30 INCHES FROM OTBD END. REPAIRE D NR 1 SLAT CLOVE PANEL AT OTBD SLAT TRACK IAW BOEING DRAWING NR 114N075-11. 2 L 7 2 4F RT A2NM 20081113 NM 2008 11 13 USAA920081950 1 20081016 A 5310 6545871523 DOOR FRAME BOEING 737 737301 1384611 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10652003/012 CRACK AT FORWARD SERVICE DOOR STOP FITTING CUTOUT, 2ND FROM TRAILING EDGE. REPAI RED FORWARD SERVICE DOOR STOP FITTING CUTOUT IAW EA NR 100689 AND TYPICAL REPAIR NR 52-10-11. 2 L 7 2 4F RT A16WE 20081113 EU 2008 11 13 ASOA200801443 1 20081103 A 2910 HYDRAULIC SYSTEM AEROSP ATR72 ATR72 EU BLUE SYSTEM MALFUNCTIONED A ASOA K NONE J WARNING INDICATION CR CRUISE 1 SO 27 636AS 375 LOST BLUE HYDRAULIC PRESSURE AND LOW LEVEL ILLUMINATED. AIRCRAFT RETURNED TO ATL AFTER T/O, EMERGENCY DECLARED & REQUES TED EMERGENCY VEHICLES. FLT 5200 DEL 181 MINS. 2 H 7 2 4T RT 20081113 EA 2008 11 13 ASOA200801451 1 20081101 A 5320 MOUNT BRACKET CNDAIR CL600 CL6002C10 1390015 EA AFT EQUIP BAY CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 712EV 10074 LT HYD SHUT OFF VALVE MOUNTING BRACKET CRACKED (AFT EQUIP BAY). 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801452 1 20081104 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 ENGINE SUPPORT BEAM FWD WEB SHOWS SIGNS OF CRACK AT LBL 9. PERFORMED EDDY CURRENT INSPECTION ON ENGINE SUPPORT BEAM FWD WEB. NO CRACKS FOUND AT THIS TIME IAW NDTM 51-20-06. RESTORE FINISH IS REQUIRED. APPLIED TOP COAT FWD WEB AT ENG SUP PORT BEAM IAW CRJ SRM 51-25-01. 2 L 7 2 4F RT A21EA 20081113 EA 2008 11 13 ASOA200801453 1 20081104 A 5320 PANEL CNDAIR CL600 CL6002B19 1900309 EA CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 PANEL 281AZ HAS CRACK ON FWD TOP EDGE. FABBED A REPAIR DOUBLER FOR FWD TOP EDGE OF PANEL 281AZ. INSTALLED DOUBLER IAW REO 601R-25-53-005. 2 L 7 2 4F RT A21EA 20081113 NM 2008 11 13 ABXA200811070260 1 20081104 A 3350 2012 POWER SUPPLY BOEING 767 767281 1385109 NM CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 793AX 23143 EXIT IDENTIFIER LIGHT AT L1 DOOR INOP. REMOVED AND REPLACED POWER SUPPLY, AND BATTERY PER 767 MM 33-41-07-2, REMOVED AN D REPLACED LIGHT ASSY PER 767 MM 33-51-03-002-802, OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 20081113 EA 2008 11 13 ASOA200801465 1 20081106 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 RT FUSELAGE EXTERIOR SKIN 3 INCHES FWD OF FS 559+96 AT STR 23R HAS MINOR SURFACE CORROSION. REMOVED 7 RIVETS, THEN REMO VED CORROSION AND INSTALLED 7 NEW SERVICEABLE RIVETS IAW CRJ 200 SRM 51-21-06, 53-51-31, AND 51-42-06 AT RT FUSELAGE EXT ERIOR SKIN 3 INCHES FWD OF FS 559+96 & AT STR 23R. AREA NEEDS PAINT. TOUCHED UP REPAIR AREA IAW CRJ SRM 51-25-16. MAX MATERIAL REMOVED .003. SUPPLEMENTAL-SDR CLOSED 11/17/2008. 2 L 7 2 4F RT A21EA 20081113 NM 2008 11 13 KCSA081566 1 20081110 A 5320 FITTING BOEING 747 747212B 1384886 NM FSUELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 BS 2360 LOWER FWD CHORD BATHTUB FITTING CORRODED AT STR 48R. 2 L 7 4 4F RT A20WE 20081113 NM 2008 11 13 KCSA081573 1 20081111 A 5320 FITTING BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 STA 2360 LOWER FORWARD CHORD BATH TUB FITTING CORRODED AT STR 6R. 2 L 7 4 4F RT A20WE 20081113 NM 2008 11 13 KCSA08072 1 20081107 A 2700 UNKNOWN BOEING 747 747209B 138489B NM FLIGHT CONTROL MALFUNCTIONED A KCSA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 23 715CK 22447 APPROXIMATELY 2:20 INTO FLIGHT, A/P DID NOT FOLLOW ROLL COMMAND IN INS OR HDG MODES. AFTER A/P DISCONNECT, UNABLE TO RO LL AIRCRAFT TO CHANGE HEADING MANUALLY WITH AILERONS. SPEED BRAKES WOULD NOT EXT. 2 L 7 4 4F RT A20WE 20081113 NM 2008 11 13 KCSA081570 1 20081110 A 5320 FITTING BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 BS 2360 LOWER FWD CHORD BATHTUB FITTING CORRODED AT STR 38L. 2 L 7 4 4F RT A20WE 20081113 NM 2008 11 13 KCSA081568 1 20081110 A 5320 FITTING BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 BS 2360 LOWER FWD CHORD BATHTUB FITTING CORRODED AT STR-51L. 2 L 7 4 4F RT A20WE 20081113 NM 2008 11 13 KCSA081569 1 20081110 A 5320 FITTING BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 BS 2360 LOWER FWD CHORD BATHTUB FITTING CORRODED AT STR 49L. 2 L 7 4 4F RT A20WE 20081113 NM 2008 11 13 KCSA081571 1 20081111 A 5347 SEAT TRACK BOEING 747 747212B 1384886 NM FUSELAGE DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 SEAT TRACK DAMAGED UPPER DECK FLOOR BS 730 RBL 47. 2 L 7 4 4F RT A20WE 20081113 NM 2008 11 13 QXEA2008111201154 1 20081025 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 421QX 4149 PDX - C1 - RT INBOARD SEAT TRACK HAS CORROSION BETWEEN STA X665 AND STA X668. BLENDED OUT CORROSION, MAX MATERIAL REMOV ED .026", FOUND TO BE OUT OF LIMITS PER RD 8/4-53-884. REMOVED SEAT TRACK REF Q400 SRM 51-40-15 AND 51-42-05. INSTALLE D NEW SEAT TRACK REF Q400 SRM 51-40-15 AND 51-42-05. 2 H 7 2 4T RT A13NM 20081114 EA 2008 11 14 SWIA200820323 1 20081107 A 2120 UNKNOWN CNDAIR CL600 CL6002C10 1390015 EA CABIN ODOR A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 726SK 10190 FLT 6369 - STRONG BURNING ODOR WHENEVER AT REDUCED THRUST AND IDLE. ACCOMPLISHED PACK BURN OUT. 2 L 7 2 4F RT A21EA 20081114 2008 11 14 GTIA0800084 4 20081110 A 2565 D30665309 SLIDE AIRBUS A319 A319132 3930340 NM L2 DOOR LOW PRESSURE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 509NK 2603 L2 SLIDE PACK PRESSURE LOW. REPLACED L2 SLIDE PACK. 2 L 7 2 4F RT A28NM 20081114 NM 2008 11 14 GTIA0800078 1 20081011 A 5320 D53472189202 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM ZONE 900 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 507NK 2560 AFT GALLEY FLOORBEAM HAS CORROSION AT 1292 BETWEEN FR 68 AND FR 69. 2 L 7 2 4F RT A28NM 20081114 EA 2008 11 14 SWIA200820329 1 20081104 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS SHORTED A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 955SW 7817 FLT 6276 - EMERGENCY EXIT LIGHTS WILL NOT WORK. CLEANED AND DRIED ALL FLOOR LEVEL CONNECTIONS. 2 L 7 2 4F RT A21EA 20081114 NM 2008 11 14 SWAA086170 1 20081112 A 2560 65C16820 FITTING BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 725SW 27857 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR GIRT BAR FWD RETAINING CLIP LOOSE. SECURED CLIP PER MM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086171 1 20081112 A 2560 65C16820 FITTING BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 725SW 27857 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR GIRT BAR AFT RETAINING CLIP LOOSE. SECURED CLIP PER MM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086162 1 20081112 A 5534 6547450 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER RT O/B FWD LUG FITTING CORRODED. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801034 1 20081103 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 FRAME CRACKED AT STATION 827 ABOVE S-9R. REPAIRED FRAME PER EC/RA 5311-01431 AND EA 5310-04498. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801035 1 20081104 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 FRAME CRACKED AT STATION 907 ABOVE S-9R. REPAIRED FRAME PER EA.5310-04498, OP 2. 2 L 7 2 4F RT A16WE 20081114 EA 2008 11 14 SWIA200820330 1 20081108 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA RIGHT SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 932SW 7714 FLT 6038 - "SMOKE TOILET" MESSAGE AFTER TAKEOFF. REPLACED RIGHT ACM. 2 L 7 2 4F RT A21EA 20081114 NM 2008 11 14 CALA0801052 1 20081110 A 5730 65E26272 SKIN BOEING 737 737524 1384721 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 RIGHT WING NUMBER 4 SLAT LEADING EDGE SKIN AT ACTUATOR CUTOUT APPEARS TO BE CRACKED. REMOVED ACTUATOR DOOR SEAL ASSEMBL Y IAW B737 SRM 57-41-01, STOP DRILLED CRACK IAW B737 SRM 57-41-01. MATERIAL ID 301 1/2 HARD, .040", IC 0649022 IAW B737 SRM 57-41-01, FABRICATED REPAIR DOUBLER IAW B737 SRM 57-41-01. PRIMED REPAIR DOUBLER IAW B737 SRM 51-20-01, INSTALLED REPAIR DOUBLER IAW B737 SRM 52-41-01. REINSTALL ACTUATOR DOOR SEAL. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801053 1 20081110 A 5320 65C3397047 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 BODY STATION 312 - 328 RBL 12 INTERCOSTAL HAS CORROSION ON TOP SURFACE. REMOVED AND REPLACED DAMAGED INTERCOSTAL AT BOD Y STATION 312 - 328 RBL 12 PER B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801055 1 20081110 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 BODY STATION 440 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR-8R AND STR-9R. REPAIRED BODY STATION 4 40 FRAME CRACK BETWEEN S-8R AND S-9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081114 EU 2008 11 14 08FDEA04758 1 20081105 A 5311 A53770545 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA O OTHER O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS GOUGE ON FRAME 28, 3 INCHES ABOVE STR 18L. REPAIR COMPLIED WITH ON EA 6-5310-123938. 2 L 7 2 4F RT A35EU 20081114 EU 2008 11 14 08FDEA04761 1 20081105 A 5311 A53770545 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS GOUGE ON FRAME 28, 1 INCH BELOW STR 19L. REPAIR COMPLIED WITH ON EA 6-5310-123938. 2 L 7 2 4F RT A35EU 20081114 EA 2008 11 14 SWIA200820316 1 20081103 A 3230 533407 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA MLG FAILED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 702SK 10136 FLT 6732 - GEAR DISAGREE CAUTION WHEN SELECTING GEAR DOWN. REPLACED LANDING GEAR SELECTOR VALVE, PN: 53340-7, SN ON: 13 42/04, SN OFF: 1289/03. 2 L 7 2 4F RT A21EA 20081114 EA 2008 11 14 SWIA200820317 1 20081104 A 2530 COFFEEMAKER CNDAIR CL600 CL6002D24 1390016 EA GALLEY SMOKE A SWIA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 07 804SK 15067 FLT 4680 - COFFEEMAKER HAD BURNING SMELL, SET OFF LAVATORY SMOKE ALARM. REPLACED COFFEEMAKERS. 2 L 7 2 4F RT A21EA 20081114 EA 2008 11 14 SWIA200820318 1 20081105 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 947SW 7786 FLT 6655 - FORWARD MOST CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081114 EA 2008 11 14 SWIA200820319 1 20081106 A 3350 AD20131A BATTERY CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCHARGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 970SW 3810 3810 7881 FLT 6517 - FORWARD EMERGENCY LIGHTS DIM. REPLACED BATTERY PACK, PN AD-2013-1A, SN ON 79469, SN OFF 69315. 2 L 7 2 4F RT A21EA 20081114 EA 2008 11 14 SWIA200820320 1 20081106 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT INOPERATIVE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 970SW 7881 FLT 5891 - FIRST OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY CHARGER. 2 L 7 2 4F RT A21EA 20081114 NM 2008 11 14 CALA0801060 1 20081110 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 BODY STATION 747 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8R AND STR 9R. ACCOMPLISHED EA 5310-04 498 ON BODY STATION 747 FRAME AT STR-8R AND STR-9R. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 08FDEA04737 1 20081105 A 5320 6515940 STRAP BOEING 727 7272S2F 1384O81 NM ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 MAIN CARGO FLOOR, CHAFING ON "I" BEAM FLOORBEAM AT STA 740 FROM BL 0 TO BL 50. REPLACED STRAP AT 740, LBL 50 TO RBL 50 REF EA 7-5310-118310, WORKED WITH N/R N00390, THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 CALA0801062 1 20081111 A 5320 141A541022 FLOOR SUPPORT BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34222 28931 MAIN DECK FLOOR SUPPORT STATION 344 - 360 LBL 12 CRACKED. REPAIRED INTERCOSTAL PER ECRA 5321-01586. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801063 1 20081111 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 BODY STATION 827 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR-8L AND STR-9L. REPAIRED FRAME BODY STA TION 827 AT AC RAIL BRACKET BETWEEN STR 8L AND STR 9L PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801065 1 20081111 A 5320 65C33970400 INTERCOSTAL BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 BODY STATION 328 - 344 LBL 12 INTERCOSTAL HAS CORROSION ON TOP SURFACE. REMOVED AND REPLACED DAMAGED INTERCOSTAL AT BOD Y STATION 328 - 344 LBL 12 PER B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081114 EU 2008 11 14 08FDEA04706 1 20081031 A 5753 A5796011421800 WEB AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 LEFT WING INBD FLAP AT RIB 25A THE WEB PLATE IS CRACKED. REMOVED AND REPLACED -218 WEB PLATE IN REF TO A300-600 SRM 51 -40-21, PARA 7, PARA 14 AND FOKKER DWG A57960114, ISSUE E. 2 L 7 2 4F RT A35EU 20081002 NM 2008 10 2 CALA0800907 1 20080916 A 5320 694962415 ANGLE BOEING 737 7373T0 1384582 NM CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 SURFACE CORROSION ON TRANSITION ANGLE AT STATION 767 STR 24R. REMOVED BAD SECTION OF TRANSITION ANGLE, FABRICATED NEW A NGLE, ALODINED, PRIMED AND INSTALLED NEW SECTION OF ANGLE PER SRM 51-40-02, SRM 51-40-05, AMM51-20-00. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800906 1 20080916 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 440 LT SIDE FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGER 8L AND 9L. REMOVED DAMAGE AND A BRACKET AT FS 440 LT SIDE FRAME AT 8L TO 9L AND REPAIRED IAW EA 5310-04498. 2 L 7 2 4F RT A16WE 20081002 EU 2008 10 2 2008UALA05636 1 20080907 A 4920 APU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SMOKE A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 413UA 470 GROUND CREW REPORTED SMOKE FROM APU EXHAUST AREA. FIRE DEPARTMENT RESPONDED. OPENED APU COMPARTMENT. NO OIL ON THE EX TERIOR. APU EXHAUST IS OK. PER FIRE DEPARTMENT NO FIRE AGENT REQUIRED, SMOKE ONLY. CLOSED APU COMPARTMENT. NO OIL IN SIT E GLASS. REPLACED APU AS PRECAUTIONARY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081002 NM 2008 10 2 2008UALA05639 1 20080905 A 2432 893003 CHARGER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE MAIN BATTERY INOPERATIVE A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 675UA 29243 MAIN BATTERY CHARGER STATUS MESSAGE. FOUND FAULTY BATTERY/CHARGER. REPLACED BATTERY & CHARGER. OP CHECKS OKAY FOR SER VICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NE 2008 10 2 2008UALA05640 2 20080905 A 7261 ACC434F65 OIL FILTER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 656UA 25394 R OIL FILTER BYPASS LIGHT ON FOR 1 MIN AFTER START. R OIL FILTER STATUS MSG REMAINS ON. REPLACED MAIN OIL FILTER. LEAK CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 2008UALA05643 1 20080908 A 2150 A/C PACK AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 826UA 989 HARD CONT TEMP PACK 1 WILL NOT GO TO HIGH FLOW. OPERATED NR 1 PACK THROUGH ALL PARAMETERS AND GROUND CHECKS NORMAL. PAC K WENT TO HIGH FLOW WITH NO DELAY OR MESSAGES. 2 L 7 2 4F 4 F RT A28NM E40NE 20081002 NM 2008 10 2 SWAA085090 1 20080916 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 439WN 29834 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085088 1 20080916 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085087 1 20080916 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085086 1 20080916 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 23R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085085 1 20080916 A 5311 6549564 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED CHECK, FOUND FUSELAGE FRAME U-CHANNEL CORRODED AT BS 540, STR 26L. REPAIRED FRAME CHANNEL PER ACO. 2 L 7 2 4F RT A16WE 20081114 EA 2008 11 14 SWIA200820324 1 20081110 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA O OTHER O OTHER CR CRUISE 1 NM 07 941SW 7750 FLT 5981 - RIGHT WINDOW CRACKED IN FLIGHT. REPLACED RIGHT WINDOW 2 L 7 2 4F RT A21EA 20081114 EA 2008 11 14 SWIA200820326 1 20081104 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 944SW 7764 FLT 6378 - FORWARD CENTER EMERGENCY FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081114 NM 2008 11 14 CALA0801061 1 20081110 A 5754 65C26602312A SKIN BOEING 737 737524 1384721 NM SLAT DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 RIGHT WING NUMBER 5 SLAT OUTBOARD EDGE ON TRAILING EDGE WEDGE SEALANT MISSING, CHECK FOR DELAMINATION. REPAIRED DAMAGE AT OUTBOARD TRAILING EDGE WEDGE NUMBER 5 SLAT PER B737-500 SRM 51-70-10. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 ASAA0843697 1 20081029 A 5340 654655837 STRINGER CLIP BOEING 737 7374Q8 138447Q NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 CABIN STRINGER CLIP CRACKED STA 907 STR 8R. REMOVED DAMAGED CLIP, LOCATED DRILLED AND INSTALLED REPLACEMENT STRINGER CL IP IAW B737 400 SRM 51 40 02 PG 2 AND 4. 2 L 7 2 4F RT A16WE 20081114 EU 2008 11 14 08FDEA04756 1 20081105 A 5414 A5461175000000 SKIN AIRBUS 310 A310324 3930206 EU NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 NR 2 PYLON LOWER SPAR, LOWER SIDE; 12 INCHES FWD OF THE AFT ATTACH BEAM, SKIN IS CRACKED. COMPLIED WITH EA E 6-5410-7-3 000 A5 PTPT 4. 2 L 7 2 4F RT A35EU 20081114 2008 11 14 UHLA2008110700002 4 20081021 A 2565 4A40304 SLIDE EMB ERJ170 ERJ170100SU 3260403 NM L1 DOOR NO TEST A UHLA K NONE L NO TEST IN INSP/MAINT 1 GL 11 654RW 7532 879 17000104 WHILE ACCOMPLISHING JOB CARD S25-65-01-710-801AQ-1; L1 DOOR SLIDE FAILED OPS CHECK. DURING OPS CHECK THE FORWARD EDGE TH AT DEPLOYS TOWARDS THE GROUND DID NOT CLEAR THE YELLOW STRAP ON THE FORWARD SIDE RESULTING IN A LARGE BUMP IN THE CENTER OF THE SLIDE WHEN DEPLOYED, RESULTING IN THE SLIDE NOT SITTING LEVEL WITH THE GROUND. 2 L 7 2 4F RT A56NM 20081114 NE 2008 11 14 UHLA2008110700003 2 20081104 A 7200 ENGINE EMB ERJ170 ERJ170100SE 3260406 NM GE CF34 CF348E5 30061 NE NR 2 MALFUNCTIONED A UHLA E L ENGINE SHUTDOWN ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 11 864RW 17000117 GEE193359 FLIGHT 5952 ATL-HPN ON FINAL APPROACH WITH GEAR DOWN AND FLAPS AT NR 5 POS, NR 2 ENG SPOOLED UP TO 80% UN-COMMANDED. CRE W SHOT MISSED APPROACH. ON SECOND APPROACH AND SAME THING HAPPENED. CREW SHUT DOWN ENGINE. CREW DID NOT RECEIVE ANY MESS AGES IN AIR OR ON GROUND. MAINTENANCE INSPECTED ENGINE, VG ACTUATORS AND SHAFTS, NO CHECKED HISTORY. RAN ENGINES, COUL D NOT DUPLICATE. 2 L 7 2 4F 4 F RT A56NM E00063EN 20081114 NM 2008 11 14 SWAA086188 1 20081112 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO FLOOR SUPPORT CORRODED AT BETWEEN BS 772 TO BS 774, LBL 13. REPAIRED FLOOR SUPPORT PER SWA EA. 2 L 7 2 4F RT A16WE 20081114 EU 2008 11 14 F3LA2008111000708 1 20081106 A 3520 21214001 SOLENOID AIRBUS A318 A318111 3940019 EU OXYGEN SYSTEM FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 808FR 31 3038 REFERENCE NON-ROUTINE 104851. DURING COMPLIANCE OF ENGINEERING ORDER A8-25EO-20453, BE AEROSPACE 120 PASSENGER SEAT CABI N CONFIGURATION, THE OXYGEN CONTAINER AT THE SECOND ROW OF SEATS ON THE RIGHT FAILED DROP TEST. MAINTENANCE REMOVED AND REPLACED THE OXYGEN CONTAINER PER AMM 35-21-10-000-001 AND AMM 35-21-41-400-001. OPERATIONAL CHECK PERFORMED WITH SATISF ACTORY RESULTS IN ACCORDANCE WITH AMM 35-23-00-710-001. 2 L 7 2 4F RT 20081114 EU 2008 11 14 QMLA1112200808053 1 20081112 A 5300 STRUCTURE BOLKMS 117 BK117A4 5626017 EU FUSELAGE CRACKED E QMLA K NONE O OTHER IN INSP/MAINT 1 NM 03 587MC 7086 1" CRACK FOUND IN LEFT UPPER NOSE COMPARTMENT. 1 G 7 2 3U H13EU 20081114 NM 2008 11 14 2008UALA06379 1 20081104 A 5210 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE R1 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 642UA 25092 DOOR 1R OUTER SKIN LOWER EDGE DAMAGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR AT LOWER EDGE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081114 NM 2008 11 14 2008UALA06383 1 20081105 A 2560 140N276218 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 DOOR DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 539UA 25223 DOOR 3L DOES NOT ARM. CHECKED GIRT AND CLEANED AND LUBED GIRT BAR AREA AND ARMING LEVER PIVOT. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 NM 2008 11 14 2008UALA06408 1 20081107 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHT INOP CEILING ROW 14 FWD. LAMP FOUND DEFECTIVE. REPLACED LAMP. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081114 NM 2008 11 14 2008UALA06400 1 20081106 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 DOOR 2R NEEDS REPAIR DOUBLER UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 2008 11 14 2008UALA06410 4 20081107 A 2565 ATTACH FITTING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EVAC SLIDE DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 401UA 435 FOUND DOOR 1L SLIDE UPPER AFT ATTACH FITTING DISCONNECTED (SPRING TYPE). REPLACED FITTING. 2 L 7 2 4F 4 F RT A28NM E40NE 20081114 WP 2008 11 14 08FDEA04842 1 20081111 A 5720 ARB291712 INTERCOSTAL DOUG DC10 DC1030F 3023504 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 RT WING L/E FOUND CRACK ON INTERCOSTAL. 2 L 7 3 4F RT A22WE 20081114 EU 2008 11 14 08FDEA04843 1 20081110 A 5712 A57151605201 RIB AIRBUS 310 A310222 3930315 EU ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 452FE 313 N16 MLG RT GEAR RIB 5, LUG WITH CORROSION UPON REMOVAL OF BUSHES E AND F. THE LUG BORE AND FACES WERE REPAIRED AS PER F EDEX EA 6-5710-126457. 2 L 7 2 4F RT A35EU 20081219 NM 2008 12 19 SWAA087197 1 20081216 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 22R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 08FDEA04855 1 20081111 A 5311 FRAME BOEING 757 75723A 1384967 NM BS 1480 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 AFT CARGO COMPT, BS 1480, S-23R - S-24R, BEAM HAS DEEP GOUGES. REPAIRED FRAME/BEAM, BS 1480, S-23R - S-24R, AFT CARGO C OMPT, IAW SRM 53-00-07, REPAIR NR 5, DETAIL 3. THIS REPAIR IS CLASSIFIED AS A CATEGORY "B" MAJOR REPAIR WITH THE FOLLOW ING FOLLOW UP TRACKING REQUIREMENTS: INITIAL AT 37,500 FC; THEREAFTER EVERY 12,000 FC. 2 L 7 2 4F RT A2NM 20081114 NM 2008 11 14 08FDEA04860 1 20081112 A 5340 66148482 SUPPORT BRACKET BOEING 727 7272D4 138407U NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 RADAR R/T SHELF CENTER LT SUPPORT BRACKET IS CRACKED REMOVED DAMAGED ANGLE. FABRICATED NEW ANGLE PER REF SRM 51-30-02, AND DRW NR 66-14848. INSTALLED NEW ANGLE REF SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04861 1 20081112 A 5347 651960214 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 469FE 21581 CORROSION ON SEAT TRACK STA 970 TO 1030 LBL 45. FOUND CORROSION OUT OF LIMITS. CUT OUT DAMAGED AREA FROM BS 960 TO 106 0 DIMS 101". FABRICATED SEAT TRACK USING BAC1590-792 7178T65 PO NR 9006020. INSTALLED REPAIR PARTS IAW SRM 53-10-5. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04510 1 20081023 A 5730 ARB74022 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 04 FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HFEC INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUT OU T BETWEEN STA XORS = 690 AND STA XORS = 700. RIGHT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS = 690 AND STA X ORS = 700, 04 FASTENER HOLES CARRIED OUT REPAIR AS PER EA NR 1-5710-122605 PART 1. TITLE, AD 2007-07-04, WINGS, RIGHT LOWER SKIN PLANK CUT OUT AT 636AB, FOUR ACCESS DOOR ATTACHMENT BORES WITH CRACK INDICATIONS PSE 57.23.01 ALI - REPAIR. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081114 NM 2008 11 14 08FDEA04511 1 20081023 A 5313 AEA76531 LONGERON SPLICE DOUG MD11 MD11F 3023600 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 CENTER CARGO, BETWEEN LEFT STA 5-53 TO 5-73 LONGERON 48 SPLICE FOUND CORRODED. CENTER CARGO BETWEEN LEFT STA 5-53 TO 5-73 LONGERON 48 SPLICE CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIGURE 4 VOLUME I. ORIGINAL THICK NESS = 0.125 INCH, MATERIAL REMOVED = 0.075 INCH, MATERIAL REMAINING = 0.050 INCH. SPLICE REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. THIS REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081114 NM 2008 11 14 08FDEA04764 1 20081106 A 5340 25FX12539 ATTACH ANGLE BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 MAIN CARGO BAY-GILL LINER MOUNT FRAME ATTACH ANGLE CRACKED ON 1148 FRAME, FS 1148, BRL 54, WL 273 REMOVED DAMAGED CLIP R EF SRM 51-30-2. FABRICATED NEW CLIP REF DWG 25FX1253 AND SRM 51-20-1. INSTALLED ANGLE CLIP REF SRM 51-30-2 PGS 1-17. IDENIFIED ANGLE CLIP REF GMM 7- 0-1001 PGS 1-2 THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04765 1 20081106 A 5340 25FX12539 ATTACH BRACKET BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 MAIN CARGO BAY-GILL LINER MOUNT FRAME ATTACH BRACKET CRACKED AT 1110 FRAME, FS 1110, RBL 44, WL 287. REMOVED DAMAGED CL IP REF SRM 51-30-2. FABRICATED NEW CLIP REF DWG 25FX1253, SRM 51-20-1. INSTALLED ANGLE CLIP REF SRM 51-30-2 PGS 1-17. IDENTIFIED ANGLE CLIP REF GMM 7-0-1001 PG 1-2, THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04766 1 20081106 A 5320 651759360 INTERCOSTAL BOEING 727 7272S2F 1384O81 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 FORWARD LAVATORY BELOW FLOOR WATERLINE 208 APPROX STA 294-312 AND APPROX 41 INCHES INTERCOSTAL WEB BETWEEN FLOORBEAMS IS CRACKED, JUST INBD OF LAV DUMP TUBE. REMOVED INTERCOSTAL FOR REPAIR REF SRM 51-10-2, REPAIRED INTERCOSTAL REF SRM 51-4 0-03 FIG 1. TREATED PRIMED AND PAINTED, REF SOPM 20-43-03 PG3, SOPM 20-44-04 PG3. INSTALLED NEW INTERCOSTAL AT STA 294 -312, RBL 41, WL 208 REF SRM 51-30 02 PG 1-12. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 WP 2008 11 14 08FDEA04767 1 20081106 A 5320 ANB70513 SUPPORT DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 PANEL NR 151ET SUPPORT CRACKED IN HALF, STA 1241, TOP OF LT WING. REMOVED CRACKED ANGLE IAW MD/DC 10 SRM 51-31-01 VOL I I. MAT ID FOR ANGLE 7075-0 .063 PO NR 629531.1 AND FABRICATED IAW DAC DWG NR ANB 7051 REV C. ALODINED AND PRIMED IAW MD /DC 10 SRM 51-21-01 VOL II PG 21-24. INSTALLED IAW DAC DWG ANB7051 REV C AND MD/DC 10 SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 20081114 NE 2008 11 14 2008UALA06256 2 20081024 A 7421 AA134S1476493477 IGNITER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 547UA 25368 RIGHT ENGINE DID NOT LIGHT OFF WITH IGNITION SELECTED TO NR 2 SYSTEM. LIGHT OFF OK IN "BOTH". DUE TO HISTORY REPLACED BOTH IGNITER PLUGS. REPLACED LEADS BOTH. REPLACED EXCITER BOX BOTH. TESTED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 NM 2008 11 14 USAA2008111492063 1 20081113 A 3397 CONNECTOR AIRBUS A319 A319132 3930340 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 805AW 1049 LOGPAGE:4327505 - FLT#700 - PHX-SEA - EEL - AISLE EMERGENCY LIGHT AT ROW 10R IS INOPERATIVE. FOUND EMERGENCY LIGHT AT R OW 10R TO BE UNPLUGGED. RECONNECTED PLUG. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081114 NM 2008 11 14 USAA2008111492062 1 20081108 A 5347 D5311278220201 SEAT TRACK AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 804AW 1043 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON CABIN SEAT TRACK AT FR 19 + 19", -Y765. REPLACED CABIN SEAT TRACK AT FR 19 + 19", -Y765 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081117 NM 2008 11 17 KCSA081583 1 20081116 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 AFT PIT FLOORBEAM (FRAME) CRACKED AT CUTOUT AT BS 1960, LBL 22. 2 L 7 4 4F RT A20WE 20081117 EU 2008 11 17 UPS08153886 1 20081028 A 5753 A57960306200 DOUBLER AIRBUS A300 A300F4622R 3930360 EU TE FLAP CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 142UP 0825 INSPECTION TYPE:1C3C LEFT WING T/E CENTER FLAP UPPER SKIN OUTBOARD REPAIR DOUBLER CHAFED. REMOVED, FABRICATED AND REPLA CED LEFT WING T/E CENTER FLAP UPPER SKIN OUTBOARD. REPAIR DOUBLER REF A300-600 SRM 57-50-00 PARA 4E AND FIG 205. 2 L 7 2 4F RT A35EU 20081117 NM 2008 11 17 SWAA086243 1 20081113 A 5610 5893543129 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 641SW 27714 DURING SCHEDULED MV1 CHECK, COCKPIT L1 WINDOW ARCED. REMOVED AND REPLACED L1 WINDOW ASSY PER MM. 2 L 7 2 4F RT A16WE 20081117 WP 2008 11 17 UPS08853864 1 20081028 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV SURVEY SEQUENCE 715-W4-28 STA XFS 310.750 RT WING LEADING EDGE DOUBLER IS STAINLESS STEEL AND IS NOT IN COMPLIANCE WITH SRM APP G. REPAIRED PER EO DC8 5720-31062A. 2 L 7 4 4F RT 4A25 20081118 EA 2008 11 18 ASOA200801486 1 20081109 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 724EV 10138 OVERHEAD EMERGENCY LIGHT ROW 4. 2 L 7 2 4F RT A21EA 20081118 NM 2008 11 18 2008UALA06422 1 20081107 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT PIT FRAME DENTED AT STA 1500, STR 25L TO 24L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF PIT FRAME AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 EU 2008 11 18 08FDEA04875 1 20081113 A 5553 A55371301208 FITTING AIRBUS 310 A310222 3930315 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 453FE 267 VERTICAL STABILIZER ATTACH FITTING AT RIB 14 HAS CORROSION. 2 L 7 2 4F RT A35EU 20081118 NM 2008 11 18 08FDEA04878 1 20081114 A 5320 655610010 WEB BOEING 727 7272D4 138407U NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FWD PIT DOOR CUTOUT FWD FRAME CLOSER WEB LOWER CORNER CRACKED, BS 560 RBL 26, WL 158. REMOVED DAMAGED WEB. FABRICATE N EW WEB. TREATED, PRIMED AND INSTALLED WEB REF: SRM 51-30-02 PG 1-12, SRM 51-1-2, PG 1-7. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081118 EU 2008 11 18 2008UALA06425 1 20081107 A 5210 SHEAR PLATE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 404UA 450 LT TRAY AFT OF DOOR 2L CRACKED AND MARKED. MAJOR REPAIR ACCOMPLISHED. FINISHED DRILLING NEW SHEAR PLATE AND STARTED IN STALLING. INSTALLED REMAINING FASTENERS LT TRAY AFT OF DOOR 2L. ACCOMPLISHED INSPECTION OF FASTENER INSTALLATION. 2 L 7 2 4F 4 F RT A28NM E40NE 20081118 EU 2008 11 18 2008UALA06430 1 20081108 A 5320 SUPPORT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 404UA 450 RT AFT SHEAR PLATE SUPPORT HAS CORROSION ON BOTTOM SIDE. SUPPORT NEEDS REPLACED. MAJOR REPAIR ACCOMPLISHED. REPLACED RT AFT SHEAR PLATE SUPPORT. 2 L 7 2 4F 4 F RT A28NM E40NE 20081118 2008 11 18 2008UALA06431 4 20081108 A 2310 8220330001 TRANSCEIVER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE NR 2 HF RADIO FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 674UA 29242 NUMBER 2 HF RADIO WON'T TEST. TRANSCEIVER IS DISCREPANT. REPLACED RIGHT TRANSCEIVER. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081118 EU 2008 11 18 2008UALA06433 1 20081108 A 3350 COVER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MISSING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 419UA 487 THE 6ABC EMERGENCY EXIT PATH LIGHT COVER MISSING. REPLACED LENS COVER FOR SEAT 6C EMERGENCY EXIT PATH LIGHT. 2 L 7 2 4F 4 F RT A28NM E40NE 20081118 NM 2008 11 18 2008UALA06438 1 20081108 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT PIT FRAME DENTED STA 1540 STR 22R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF PIT FRAME AND INSTALLED D OUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 2008UALA06439 1 20081108 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT PIT FRAME DENTED STA 1540 AT STR 25R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED D OUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 2008UALA06442 1 20081109 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY EXIT LIGHT INOP ABOVE DOOR 5L. REPLACED BATTERY PACK, OP CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081118 NM 2008 11 18 2008UALA06443 1 20081109 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 DOOR MOUNTED EMERGENCY EXIT LIGHTS INOP AT 3L & 5L. REPLACED BATTERY PACK FOR DOOR 3L. REPLACED LIGHT FOR DOOR 5L. OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081118 2008 11 18 2008UALA06494 4 20081112 A 2565 D31516121 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R1 DOOR DEFECTIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 415UA 475 EMERGENCY LIGHT TEST FAILED EXT LOAD L, TESTED AND FOUND DOOR 1R SLIDE PACK AT FAULT. REMOVED DOOR 1R SLIDE. REPLACED SLIDE. STILL HAVE ORIGINAL PROBLEM FAILED EXT LOAD L. VERIFIED ALL EMERGENCY LIGHTS ARE OPERATIVE EXCEPT DOOR 1R SLIDE LIGHTS. ACCMP EMERGENCY LIGHT TEST, NO FAULTS. ALL EMERGENCY LIGHTS WORK OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081118 NE 2008 11 18 2008UALA06507 2 20081113 A 7261 OIL SYSTEM BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE RT ENGINE LOW A UALA O OTHER W K INADEQUATE Q C FLUID LOSS IN INSP/MAINT 1 WP 29 217UA 30550 RIGHT ENG TOOK 10 QUARTS OF OIL ON ARRIVAL. BOROSCOPED NR 3 WEEP TUBE, FOUND CLEAN NO OIL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081118 NM 2008 11 18 08FDEA04775 1 20081106 A 5313 STRINGER BOEING 757 757236 1384971 NM BS 1000-1020 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 INTERNAL STRUCTURE S 8L BS 1000-1020 STRINGER HAS SEVERAL NICKS. REPAIRED STRINGER 8 L BS-1000-1020 IAW SRM 53-00-03 RE PAIR NR 1 "A" MAJOR REPAIR, NO FOLLOW-UP INSP REQUIRED. 2 L 7 2 4F RT A2NM 20081118 NM 2008 11 18 08FDEA04776 1 20081106 A 5320 WEB BOEING 757 757236 1384971 NM BS 1681 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 DECK PLATE WEB AT STA 1681 RBL 13 CORRODED. REPAIRED CORRODED DECK PLATE WEB AT STA 1681 RBL 13 IAW SRM 53-60-51 REPAIR NR 2 "A" MAJOR REPAIR. NO FOLLOW-UP INSPECTION REQUIRED (TRANSFERED FROM N00582 ). 2 L 7 2 4F RT A2NM 20081118 NM 2008 11 18 2008UALA06452 1 20081110 A 5210 ROLL PIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 571UA 26681 NR 1 RIGHT MAIN ENTRY DOOR EMERGENCY POWER TRIGGER LOOSE. REPLACED ROLL PIN. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NE 2008 11 18 2008UALA06454 2 20081110 A 7321 4300702 STATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EEC DEFECTIVE A UALA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 WP 29 643UA 25093 727875 NR 2 ENGINE FLAME OUT PER CREW. FLIGHT DIVERTED. ON NR 2 ENG MCD AND OIL FILTER RE-CHECK FOUND NR 4 BEARING MCD TO HAV E A LONG CHIP AND MAIN OIL FILTER TO HAVE FLAKES. NEED TO REMOVE ENG S/N 727875 (NR 2 POS) DUE TO PMA GEARBOX DEBRIS. ACP ENG REMOVAL. REPLACED EEC ALTERNATOR (N2 TRANSDUCER) STATOR, EEC ROTOR GEN & EEC ALTERNATOR DRIVE SHAFT AND BEARING . OPS CHECK NORMAL. NO EICAS OR STATUS MESSAGES. 2 L 7 2 4F 4 F RT A1NM E24NE 20081118 NM 2008 11 18 2008UALA06455 1 20081107 A 3610 79027013 SHUTOFF VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 660UA 27115 CREW COMMENTS: AFTER ENG START R ENG HPSOV ON WITH BLEED OFF. HPSOV FOUND FAULTY. REPLACED HPSOV. PROBLEM STILL PERS ISTS. HP VALVE LOCKED OUT & W3510-017-18 WAS MOVED FROM TERMINAL 1 TO TERMINAL 2. RECONFIGURED RIGHT HPSOV. REPLACED AIR SUPPLY BITE MODULE. RAN NR 2 ENGINE TO 70 PERCENT N2 OPERATING TAI. NO RIGHT ENGINE BLEED LIGHT OR EICAS MESSAGE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081118 NM 2008 11 18 2008UALA06458 1 20081109 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 EEL LIGHT AT 4AB BROKEN AND WIRE HANGING OUT. REPLACED LIGHT ASSY, TEST OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081118 NM 2008 11 18 2008UALA06462 1 20081109 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 EEL LIGHT INOP AT AFT GALLEY LEFT SIDE. REPLACED FEEDER ASSY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081118 NM 2008 11 18 2008UALA06464 1 20081109 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 EEL LIGHT INOP BETWEEN VIDEO CLOSET AND SEAT 1H RT SIDE. REPAIRED FEEDER ASSY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081118 NM 2008 11 18 2008UALA06465 1 20081109 A 3350 767 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 EEL LIGHT INOP RT SIDE EXTERIOR MID. REPLACED LAMP. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 2008 10 2 2008UALA05646 4 20080908 A 2565 D31516121 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R1 DOOR LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 418UA 485 FLIGHT ATTENDANT REPORTED, SLIDE PRESSURE ON 1R IS LOW. PRESSURE FOUND LOW. SERVICED TO NORMAL LEVEL. OKAY FOR SERVI CE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081002 NM 2008 10 2 CALA0800891 1 20080916 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 787 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. REPAIRED CRACKED FRAME AT STATION 787 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081002 2008 10 2 2008UALA05648 4 20080908 A 2565 SLIDE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE L2 DOOR LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 854UA 1731 DOOR 2L SLIDE PRESSURE IN RED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081002 NM 2008 10 2 CALA0800889 1 20080916 A 5311 6546545 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 706 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. REMOVED BRACKET PER EA 53 10-04498, CUT OUT DAMAGE PER EA 5310-04498, HEEL CUT OUT PER NDTM PTG 51-00-00 FIG 23, NO DEFECTS NOTED. FABRICATED REP AIR ANGLE C, D. TREATED AND PRIMED PART C, D PER EA 5310-04498. INSTALLED REPAIR PART C, D EA 5310-04498. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800888 1 20080916 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 787 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. INSTALLED REPAIR ANGLES A T STA 787 BETWEEN STR 8R AND 9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 UPS08653308 1 20080909 A 5610 BRACKET BOEING 767 76734AF 1385212 NM R2 WINDOW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 306UP 27759 INSPECTION TYPE:N/A R2 WINDOW CARRIAGE ASSEMBLY BRACKET CRACKED. REMOVED AND REPLACED BALL SCREW ASSEMBLY AND CARRIAGE ASSEMBLY PER MM 56-11-04-4. 2 L 7 2 4F RT A1NM 20081002 NM 2008 10 2 SWAA084962 1 20080909 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM BS 827 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084963 1 20080909 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 374SW 26582 RIGHT OVERWING EMERGENCY EXIT LIGHT ASSY LOOSE. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084968 1 20080909 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 787 S20R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084969 1 20080909 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 747 S21R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 21R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084971 1 20080909 A 5320 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM BS 1006 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 8L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084972 1 20080909 A 5311 65C22908 FRAME BOEING 737 7373A4 1384585 NM BS 500B S20L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 20L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084973 1 20080909 A 5754 SKIN BOEING 737 7373T0 1384582 NM NR 2 SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 684WN NS0070 23941 DURING SCHEDULED 22Y CHECK, FOUND LT WING NR 2 L/E SLAT INBOARD END DELAMINATED. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084974 1 20080909 A 3350 20131A BATTERY PACK BOEING 737 7373Y0 1384671 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED 22Y CHECK, FOUND RT FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085141 1 20080921 A 5311 6546551 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 807 STR 27L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 SWAA085112 1 20080917 A 5315 6545833 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 354SW 25219 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 178, LBL 27. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081118 NM 2008 11 18 2008UALA06466 1 20081110 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EEL INOP: ROW 43L. RELAMPED EEL, CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081118 NM 2008 11 18 2008UALA06467 1 20081110 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY LT INOP: DOOR 2R CEILING. RELAMPED EMERGENCY LIGHT, CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081118 NM 2008 11 18 2008UALA06514 1 20081114 A 3350 20131A CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 OVERWING EMERGENCY LIGHT LT 2 TOP LIGHTS INOP. REPLACED BATTERY CHARGER. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081118 NM 2008 11 18 2008UALA06515 1 20081114 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT ROW 22 LT AFT INOP. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081114 EU 2008 11 14 08FDEA04831 1 20081110 A 5510 A5517781120000 FITTING AIRBUS 310 A310324 3930206 EU HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 RIGHT HORIZONTAL STABILIZER, OTBD FWD HOIST POINT IS CRACKED. REMOVED OUTBD FWD HOIST POINT FITTING IAW SRM 51-40-21. INSTALLED REPAIR PLUG IAW EO 6-5510-7-5001. INSTALLED FITTING IAW SRM 51-40-21. SEALED FITTING FASTENERS IAW SRM 51-74 -00. INSTALLED COVER PLUG IAW EO 6-5510-7-5001. 2 L 7 2 4F RT A35EU 20081114 WP 2008 11 14 08FDEA04836 1 20081110 A 5510 SUPPORT BRACKET DOUG MD10 MD1010F 3022112 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 LEFT HORIZONTAL STAB INBD L/E REMOVED SECTION, MOST INBD, HAS A CRACKED OTBD LOWER SUPPORT BRACKET. REMOVED TEE CAP IAW SRM 51-35-01. LOCATED, DRILLED & DEBURRED IAW DWG ALC 7273 ALODINED & PRIMED IAW SRM 51-21-01. INSTALLED NEW TEE CAP IAW SRM 51-35-01 & EA 8-5510-123667. 2 L 7 3 4F RT A22WE 20081114 EU 2008 11 14 08FDEA04837 1 20081110 A 5712 A57151605200 RIB AIRBUS 310 A310222 3930315 EU ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 452FE 313 LT GEAR RIB 5, CORROSION FOUND UPON REMOVAL OF BUSH E AND F. A REPAIR IN ACCORDANCE WITH EA 6-5710-126452 WAS ACCOMPLIS HED. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 K11A2008111272204 1 20080918 A 5320 WEB BOEING 727 7272H3 138368N NM NLG WW CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 NLG WHEEL WELL WEB INNER SURFACE HAS CORROSION AT STA 292, LBL 148-153. CORROSION 1 X 1 INCH. 2 L 7 3 4F RT A3WE 20081114 EU 2008 11 14 2008UALA06403 1 20081106 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 448UA 842 FUSE STR 43RT AT FR67 + 2 HAS EXCESSIVE MAT'L LOSS FROM GRINDING. MAJOR REPAIR. STRINGER TO BE REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081114 NM 2008 11 14 2008UALA06396 1 20081106 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 DOOR 2L LWR GATE CORRODED. INSTALLED NEW GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 NM 2008 11 14 USAA920081799 1 20080918 A 5320 654580731 ANGLE BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 C-18 CHECK - CRACKED ANGLE, BS 290, S11R. REPLACED ANGLE, BS 290, S11R IAW SRM 51-40-02. (K) 2 L 7 2 4F RT A16WE 20081117 EA 2008 11 17 MASA2008110600765 1 20081106 A 7110 22850081141 COWLING CNDAIR CL600 CL6002B19 1900309 EA NR 1 ENGINE MISSING A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 7264V 7264 ASH FLT 2743 PHX-RON. NR 1 ENGINE LOWER TRANSLATING COWL FOUND MISSING ON POST FLIGHT WALK AROUND. MX INSPECTED DAMAGE AND INSTALLED NR 1 LOWER FAN COWL. 2 L 7 2 4F RT A21EA 20081117 SO 2008 11 17 C2XA08SH138 1 20081108 A 5320 14530637004 SUPPORT EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14952 145067 SHV - DURING C-CHECK RT UPPER SEAT TRACK SUPPORT HAS CORROSION AROUND RIVETS AT FR 45,46 AND 50. MX REPAIRED LT UPPER S EAT TRACK SUPPORT AT FR 45, 46 AND 50 IAW EC 5320-01429. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 20081117 SO 2008 11 17 C2XA08SH141 1 20081111 A 5320 14530643401 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14952 145067 SHV - DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. MAINTENANCE REMOVED THE C ORROSION AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10, FIG 203, STEP 4. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081117 SO 2008 11 17 C2XA08TY131 1 20081114 A 3350 3104404 FUSE EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BLOWN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 15910 145455 LEFT FORWARD FUSELAGE EMERGENCY LIGHT WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY FUSE IAW HONEYWELL VCMM 33-50-74, OPS CHECK GOOD AND WAS RELEASED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081117 NM 2008 11 17 KCSA081584 1 20081116 A 5311 FRAME BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 AFT PIT FLOORBEAM (FRAME) CRACKED AT CUTOUT AT BS 2080, LBL 24. 2 L 7 4 4F RT A20WE 20081117 WP 2008 11 17 UPS08853883 1 20081013 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV SURVEY ESQ NUMBER 702-F1-61 DOES NOT MEET SRM REQUIREMENTS FS 1469. REPAIRED AS PER 53-02-01 FIG 7 A ND TR 53-203 FIG 7 SHEET 24. 2 L 7 4 4F RT 4A25 20081117 WP 2008 11 17 IXX2008F00102 1 20080805 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK, FOUND LWR FWD FUSELAGE BELLY AFT OF FWD BASKET DOOR HAS IMPROPER REPAIR AT STA FS403, LONGERON 3 5.5 LT. REMOVED FASTNERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. FABRICA TED NEW SKIN, REPAIR DOUBLER, INTERNAL FINGER DOUBLERS, AND FILLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. IN STALLED NEW FASTNERS AND REPAIR PARTS IAW SRM. (K) 2 L 7 4 4F RT 4A25 20081117 WP 2008 11 17 IXX2008F00111 1 20080806 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK INSP, FOUND FWD LWR FUSELAGE AFT OF AFT ADF ANTENNA HAS IMPROPER REPAIR AT STA FS 172 LONGERON 35 .5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT I NSP. NO CRACK AND NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, FILLER, INTERNAL FINGER DOUBLERS. CLEANED, TREATED, AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS. 2 L 7 4 4F RT 4A25 20081117 WP 2008 11 17 IXX2008F00101 1 20080806 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK, FOUND DOUBLER FWD OF A-PIT DOOR ON LWR CENTERLINE, HAS IMPROPER REPAIR AT FS220, LONGERON 36. R EMOVED FASTNERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP, NO CR ACK, NO CORROSION FOUND. FABRICATED NEW SKIN, DOUBLER REPAIR, FILLER, INTERNAL FINGER DOUBLERS, CLEANED, TREATED AND PR IMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM. (K) 2 L 7 4 4F RT 4A25 20081117 WP 2008 11 17 IXX2008F00103 1 20080805 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING DENTED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK INSP, FOUND RT WING INBD L/E UPPER SKIN DENTED AT STA SFS 120.000. REMOVED FASTENERS AS NEEDED T O PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, DOUBLER, ANGLES, FILLER, AND FAIRING. PERFORMED HEAT TRE ATMENT TO REPAIR ANGLES. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW S RM. (K) 2 L 7 4 4F RT 4A25 20081117 WP 2008 11 17 IXX2008F00108 1 20080705 A 5753 SKIN DOUG DC8 DC871F 302199D WP TE FLAP BROKEN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK INSPECTION, FOUND LT WING OTBD FLAP UPPER SKIN BROKEN AT STA XF 169.000-213.000. REMOVED FASTENE RS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAI R PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 57-7-1, FIG 4 TR 57-94 DATED 10/01/02, SRM. (K) 2 L 7 4 4F RT 4A25 20081117 WP 2008 11 17 IXX2008F00109 1 20080818 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK INSPECTION, FOUND LOWER AFT FUSELAGE BELLY FWD OF AFT BASKET DOOR HAS IMPROPER REPAIR AT STA FS11 42 LONGERON 35.5 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. P ERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED EXTERNAL DOUBLER, EXTERNAL TRIPLER, FILLER AND FINGE R DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM. (K) 2 L 7 4 4F RT 4A25 20081117 WP 2008 11 17 IXX2008F00112 1 20080807 A 5753 SKIN DOUG DC8 DC871F 302199D WP TE FLAP MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK INSP, FOUND RT OTBD FLAP LOWER SKIN HAS IMPROPER REPAIR AT STA XF 238.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR P ARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM. (K) 2 L 7 4 4F RT 4A25 20081117 WP 2008 11 17 IXX2008F00113 1 20080805 A 5753 SKIN DOUG DC8 DC871F 302199D WP TE FLAP MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK INSP, FOUND LT OTBD FLAP UPPER SKIN HAS IMPROPER REPAIR AND AT STA XF420.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR, REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CL EANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM. (K) 2 L 7 4 4F RT 4A25 20081117 WP 2008 11 17 IXX2008F00114 1 20080807 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK INSP, FOUND LT AFT CORNER OF A PIT DOOR OPENING HAS IMPROPER REPAIR AT STA FS340, LONGERON 31 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND P RIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FORM 8100-9. (K) 2 L 7 4 4F RT 4A25 20081118 NM 2008 11 18 08FDEA04879 1 20081114 A 5330 6518220 SKIN BOEING 727 7272S2F 1384O81 NM ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 LT EXTERIOR FUSELAGE BS 720D 12 STR 19L SKIN LAP JUST FWD OF WING LE, SKIN HAS WEAR REPAIRED FUSE SKIN AT STA 720D 12 STR 19L REF SRM 53-30-3 FIG 5. DISPLACED LEFT INBD LEADING EDGE FOR REPAIR AND REINSTALLED REF SRM 51-30-2 PG 1-5. DIS CONNECTED LEADING EDGE PNEUMATIC DUCT AND REINSTALLED AND LEAK CHECKED REF MM 36-13-00-4 PG4. THIS IS CLASSIFIED AS A M AJOR REPAIR. 2 L 7 3 4F A3WE 20081118 NM 2008 11 18 2008UALA06444 1 20081109 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY EXIT LIGHTS INOP UPPER DECK CEILING BS 360, 570, & 670. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081118 NM 2008 11 18 08FDEA04774 1 20081106 A 5313 STRINGER BOEING 757 757236 1384971 NM BS 730-780 S5L DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 INTERNAL STRUCTURE, STRINGER 5L HAVE SEVERAL SCRATCHES BS 750-BS 770. REPAIRED IAW SRM 53-00-03, REPAIR NR 1, ENTIRE ST RINGER SECTION REPLACED BS 730-780 AT S-5L CAT "A" MAJOR REPAIR NO FOLLOW-UP REQUIRED. 2 L 7 2 4F RT A2NM 20081118 NM 2008 11 18 08FDEA04781 1 20081107 A 5550 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM EMPENNAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 593FE 48551 EMPENNAGE, AFT FUSELAGE COMPARTMENT PRESSURE BULKHEAD UPPER AFT SURFACE QUANTITY 01 SUPPORT FITTING AT STATION 2007, X=- 31.930 FOUND CRACKED. 2 L 7 3 4F RT A22WE 20081118 EU 2008 11 18 08FDEA04783 1 20081107 A 5311 A53771694201 FRAME SPLICE AIRBUS 300 A300F4605R 3930327 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS DAMAGE ON FRAME 21 TRUSS SPLICE BETWEEN STR 8R AND STR 9R WITH SHEARED RIVETS ON STR 9R. REMOVED AN D REPLACED TRUSS SPLICE AT FRAME 21 STR 8, STR 9, AND STR 13 IAW SRM 51-40-21. FABRICATED PARTS ON TRAVELERS T8/765472, T8/765399, T8/765471, T8/765400. 2 L 7 2 4F RT A35EU 20081118 EU 2008 11 18 08FDEA04848 1 20081111 A 5330 A53778736208 SKIN AIRBUS 300 A300B4605R 3930308 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 LOWER FUSELAGE HAS LIGHTNING STRIKE ON STR 54L 4TH FASTENER FWD OF FR 34. CUT-OUT DAMAGE IAW SRM 53-10-12 FIG 207, PERF ORMED HFEC OF CUT-OUT AREA IAW NTM 51-10-08 PT6. NO CRACK INDICATIONS NOTED. FABRICATED DOUBLER FROM 2024-T3 .071C IAW SRM 53-10-12 FIG 207. TREATED, PRIMED, TOP COATED, AND INSTALLED REPAIR PARTS IAW SRM 51-21-10, 51-75-10, AND 53-10-12 FIG 207. 2 L 7 2 4F RT A35EU 20081118 EU 2008 11 18 08FDEA04850 1 20081111 A 2421 735874D IDG AIRBUS 300 A300F4605R 3930327 EU NR 2 LEAKING A FDEA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CE 21 672FE 779 DURING TAKEOFF ROLL AT 70 KTS, RGT ENG IDG 2 LOW PRESS AND NR 2 GEN FAULT, ABORTED TAKEOFF. RESET GEN REST OFF LIGHT NO RMAL KMEM. NR 2 IDG 2 QTS LOW SERVICED PER MM 24-11-00, RAN ENG PER JRH, FOUND SERVICE PORT LEAKING 1 DROP EVERY 2 SEC . REMOVED AND REPLACED SERVICE PORT PER MM 24-11-11. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 20081118 NM 2008 11 18 08FDEA04839 1 20081110 A 5414 311N504631 SKIN BOEING 757 75723A 1384967 NM NR 1 PYLON DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 WHILE DRILLING THE 311N5046-31 NR 1 PYLON OTBD SKIN 2 NUTPLATE ATTACH HOLES WERE OVERSIZED TO .250 DIAMETER AT APPROX PP S 132 AND 1 HOLE WAS ELONGATED AT APPROX PPS 205.65 AND 2 HOLES DAMAGED IN LOWER CHORD AT PPS 174.30. COMPLIED WITH FED EX EA NR F-5450-124034 11/07/08 AND MAE EA NR 757-16-A1814 REV-NOV 5,2008. NO FOLLOW UP ACTION REQUIRED. "MAJOR REPAI R". 2 L 7 2 4F RT A2NM 20081118 EU 2008 11 18 2008UALA06473 1 20081111 A 5210 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 404UA 450 RT SHEAR TRAY HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. TRAY REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081118 EU 2008 11 18 2008UALA06474 1 20081111 A 5320 BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 404UA 450 BEAM 205 HAS CORROSION AT FRAME 68. MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM. REMOVED BRACKETS AND TRANSFER DRILLED ON TO NEW BEAM. CONNECTED BEAM 205 TO BEAM 200. READY TO INSTALL IN AC. INSTALLED BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081118 NM 2008 11 18 2008UALA06475 1 20081109 A 8011 35054367 STARTER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE NR 2 ENGINE UNDERSERVICED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 675UA 29243 DURING STARTER SERVICE, FOUND ENG 2 STARTER EMPTY OF OIL AND MAG PLUG COVERED WITH METAL. STARTER FOUND UNDER SERVICED. REPLACED STARTER, OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081118 NM 2008 11 18 2008UALA06477 1 20081110 A 3350 20131A582233 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 642UA 25092 AFT EMERGENCY LIGHTS AT R-4 AND L-4, EXIT SIGNS INOP. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER. OPS CHECK GOOD . 2 L 7 2 4F 4 F RT A1NM E24NE 20081217 NM 2008 12 17 SWAA087042 1 20081211 A 5330 6562212 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081118 EA 2008 11 18 SWIA200820356 1 20080731 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 917SW 7641 C-CHECK, LEFT ENGINE FORWARD YOKE MOUNT LINK BEARING CORRODED. REPLACED. 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 SWIA200820360 1 20080731 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 917SW 7641 C-CHECK, RIGHT OUTBOARD CLIP AT RBL 9 FS 280 CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 SWIA200820335 1 20080731 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 698BR 7799 C-CHECK, PASSENGER DOOR AFT WEB CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 SWIA200820337 1 20080801 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 668CA 10162 C-CHECK, PASSENGER DOOR AFT DRAG ANGLE CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081118 NM 2008 11 18 2008UALA06484 1 20081107 A 3510 MXP4023 OXYGEN SYSTEM BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE COCKPIT MALFUNCTIONED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 786UA 26938 F/O OXYGEN MASK TEST DOES NOT TEST. REPLACED O2 BOX. OPS OKAY, LEAK CHECKED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081118 EU 2008 11 18 08FDEA04744 1 20081105 A 5321 R532B375200000 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 FLOOR PANEL 241 WH IS CRACKED. FABRICATED NEW PANEL FROM STOCK MATERIAL, INSTALLED INSERTS, POTTED EDGES, APPLIED NONSK ID, PART ID MARKED, IAW SRZ25-005 REV G. 2 L 7 2 4F RT A35EU 20081118 NM 2008 11 18 2008UALA06486 1 20081110 A 3510 OXYGEN SYSTEM BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW O2 LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 365UA 24534 CREW O2 LEAK. 2 L 7 2 4F 4 F RT A16WE E21EU 20081118 NM 2008 11 18 2008UALA06487 1 20081110 A 5330 DOUBLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 REPAIR DOUBLER AT BS 610 IS DENTED BETWEEN STR 16L AND STR 17L. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED AREA, FABRI CATED REPAIR, AND INSTALLED. REPAIR MADE IAW MM 53-30-92 PG 801. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 WP 2008 11 18 08FDEA04695 1 20081104 A 5730 ARB25103 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 500 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 LEFT WING INBD L/E PANEL 516 HB IS CHAFED. BLENDED AREA IAW SRM 57-00-01 VOL I, CHECKED LIMITS, FOUND TO BE OUT OF LIM ITS, ORIG THICKNESS .090 BLEND LIMITS 20 PERCENT OR .072 WAS .067 IAW SRM 51-31- 01 VOL II FIG 1. FABRICATED DOUBLER IA W SRM 57-00-01 VOL I FIG 4 PG 12. ALODINED AND PRIMED IAW SRM 51-21-01 VOL II. INSTALLED DOUBLER IAW SRM 57-00-01 VO L I FIG 4 PG 12. 2 L 7 3 4F RT A22WE 20081118 EU 2008 11 18 08FDEA04868 1 20081112 A 5540 A55471611000 ATTACH FITTING AIRBUS 310 A310222 3930315 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 453FE 267 RUDDER, NR 1 ATTACH FITTING HAS CORROSION. 2 L 7 2 4F RT A35EU 20081118 NM 2008 11 18 2008UALA03132 1 20080601 A 2730 4885501002 CONTROL UNIT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE LT ELAVATOR FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 217UA 30550 ACTUATOR CONFIDENCE FAILED. MSG 27-10110, ELEVATOR POWER CONTROL UNIT (LEFT OUTBOARD) BLOCKING SOLENOID OPERATED VALVE IS NOT IN COMMANDED POSITION. AFTER EXTENSIVE TROUBLESHOOTING FOUND FAULTY L1 ACE. REPLACED L1 ACE, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081118 EA 2008 11 18 SWIA200820341 1 20080712 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 440SW 7589 C-CHECK, UPPER INBOARD CORNER LINTEL ATTACHMENT FITTING CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 SWIA200820346 1 20081111 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 932SW 7714 FLT 6719 - RIGHT WING FORWARD EMERGENCY EXIT LIGHT INOP, RELAMPED. 2 L 7 2 4F RT A21EA 20081118 CE 2008 11 18 O2G2008F00001 1 20081016 A 2422 PC15H STATIC INVERTER CESSNA 500 550 2076604 CE NR 2 FAILED E O2GA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 63 823NA 5500236 AC INVERTER FAILED, TROUBLESHOT INVERTER AND COULD NOT DUPLICATE. AS A PRECAUTION, REPLACED INVERTER AND IT CHECKED GOO D. ON NEXT FLIGHT INVERTER FAILED, REPLACED WITH NEW INVERTER. (K) 1 L 7 2 4F A22CE 20081118 SW 2008 11 18 MT92008F00007 1 20081104 A 2797 202021AB22 WIRE SWRNGN SA227 SA227AC 8780603 SW FLAP CONTROL BROKEN E MT9A A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 05 592BA AC592 ON TUESDAY 11/4/08, FLIGHT RETURNED TO RAMP AFTER DEPARTURE. PILOT IN COMMAND STATED THAT AFTER ROTATION AND STANDARD D EPARTURE, HE SELECTED FLAPS UP. NO CHANGE IN ACFT CONFIGURATION WAS NOTED AND NO MOVEMENT ON THE FLAP INDICATOR. HYDR PRESSURE AND ALL CIRCUIT BREAKERS WERE CHECKED AND FOUND NORMAL. PILOT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT AND DID NOT DECLARE AN EMERGENCY. INSP BY MAINT, FOUND A FLAP CONTROL WIRE BROKEN AT THE TERMINAL STRIP LOCATED UNDER THE HYDR POWER PACK. THE WIRE WAS REPAIRED AND OPS CHECKED GOOD. (K) 2 L 7 2 4T RT A8SW 20081118 NM 2008 11 18 08FDEA04852 1 20081111 A 5320 69471112 ANGLE BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 LWR EXTERIOR FUSELAGE INSIDE DELTA BEAM BS 740 LBL 5 TO RBL 5 WL 149, FWD LOWER CHORD HAS CORROSION AROUND FASTENERS. R EMOVED CORROSION FROM TEE ANGLE STA 740 LBL 5 TO RBL 5, FOUND OUT OF LIMITS. REMOVED TEE ANGLE STA 740, FABRICATED NEW TEE ANGLE TREATED AND PRIMED. INSTALLED NEW TEE ANGLE STA 740 TORQUED BOLTS AT STS 740. INSTALLED WEB AT STA 743 TO 7 88 BL 0 AND INSTALLED COAXIAL DME CABLE STA 740-800 REF SRM 51-30-2 PG 4/5 FASTENERS, 51-10-6 PG 1-4 CORROSION, 53-10-1 PG 2 LIMITS, 51-10-2 PG 1-7. MAJOR REPAIR. 2 L 7 3 4F A3WE 20081118 2008 11 18 MT92008F00008 4 20081104 A 3455 TRANSISTOR CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE ADF BURNED E MT9A K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 05 4687B 208B0167 PCE17326 THE PILOT REPORTED SMOKE IN THE COCKPIT TO ATC, DECLARED AN EMERGENCY, AND RETURNED TO DEPARTURE. THE SMOKE THAT WAS SE EN BY THE PILOT APPEARED TO BE COMING FROM UNDER THE GLARE SHIELD ABOVE THE FUEL FLOW AND FUEL QUANTITY INDICATORS. THE PILOT SAID THERE WAS NOT A LOT OF SMOKE, BUT JUST ENOUGH TO BE SEEN AS IF SOMEONE HAD LIT A CIGARETTE. CHECKED ALL AVI ONICS AND FOUND THAT THE ADF HAD A SMOKE SMELL. REMOVED THE ADF AND FOUND THAT A TRANSISTOR INSIDE THE ADF DISPLAY HAD BURNED UP. DID NOT HAVE THE PARTS TO FIX THE ADF SO THE ADF WAS DEFERRED IAW MEL. THE ADF MEL IS 120 DAYS. A SERVICEA BLE ADF HAS BEEN SHIPPED, WHERE THE ADF RECEIVER WILL BE REPLACED. FOUND AN EXPOSED WIRE ON THE FUEL FLOW INDICATOR WI 1 H 7 1 3T 3 T A37CE E4EA 20081118 EU 2008 11 18 08FDEA04747 1 20081105 A 5321 R532B375900000 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 FLOOR PANEL 241 AJ IS CRACKED. FABRICATED NEW PANEL FROM STOCK MATERIAL, INSTALLED INSERTS, POTTED EDGES, APPLIED NONSK ID, PART ID MARKED IAW SRZ 25-005 REV G. 2 L 7 2 4F RT A35EU 20081118 EU 2008 11 18 08FDEA04869 1 20081112 A 2720 A2721206000060Z BELLCRANK AIRBUS 310 A310222 3930315 EU RUDDER SERVO CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 453FE 267 NR 1 RUDDER SERVO ACTUATOR BELLCRANK AT RIB 12 HAS CORROSION. 2 L 7 2 4F RT A35EU 20081118 NM 2008 11 18 08FDEA04870 1 20081113 A 5311 6520827135 FRAME BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FUSELAGE UPPER LOBE INTERIOR STRUCTURE CORROSION AT STA 600 RBL 51 "I" FRAME BOTTOM FLANGE. REPAIRED FRAME IAW EA 7-531 0-123811 SEE JPF FOR PARTIAL WORK ACCOMPLISHED, REPAIR CLASSIFIED AS MAJOR. 2 L 7 3 4F A3WE 20081118 EU 2008 11 18 08FDEA04872 1 20081113 A 7160 3110416 NOSE COWL AIRBUS 300 A300F4605R 3930327 EU ZONE 400 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 NR V 1 NOSE COWL HAS A MINOR SCRATCH AT 10 O'CLOCK POSITION LEADING EDGE. REMOVED DAMAGED SKIN AREA IAW SRM 54-10-00 RE PAIR NR 9. FABRICATED SKIN PATCH AND DOUBLER IAW SRM 54-10-00, LOCATED AND DRILLED PATCH AND DOUBLER IAW SRM 51-40-44. HEAT TREATED PATCH DOUBLER IAW AMS 2070H, ALODINED AND PRIMED PATCH, DOUBLER, AND SKIN IAW SRM 54-02-03. INSTALLED PA TCH AND DOUBLER IAW SRM 54-10-10. 2 L 7 2 4F RT A35EU 20081118 EU 2008 11 18 08FDEA04873 1 20081113 A 5553 A55371291208 ATTACH FITTING AIRBUS 310 A310222 3930315 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 453FE 267 VERTICAL STABILIZER ATTACH FITTING AT RIB 12 HAS CORROSION. 2 L 7 2 4F RT A35EU 20081118 EU 2008 11 18 08FDEA04789 1 20081107 A 5311 A53834138205 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS GOUGE ON FRAME 47 3 INCH BELOW STR 12R BLENDED AREA IAW SRM 51-73-10, FOUND TO BE WITHIN LIMITS. PE RFORMED HFEC IAW NTM 51-10-08 PT6, NO CRACK INDICATIONS NOTED. TREATED AND PRIMED IAW SRM 51-23-20. 2 L 7 2 4F RT A35EU 20081001 NM 2008 10 1 SWAA085111 1 20080917 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 405, STR 27L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 2008UALA05518 1 20080828 A 3320 81841 BALLAST BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GALLEY LIGHTS ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 502UA 24623 NOTICED ODOR FROM MID GALLEY OVERHEAD LIGHTS. TURNED OFF SWITCH ODOR DISSIPATED. REPLACED 2EA BALLAST. OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081001 NM 2008 10 1 2008UALA05550 1 20080831 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENYC LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 180UA 25224 SEAT 2J AFT EMERGENCY LIGHT FLOOR INOP. FOUND FAULTY LAMP. REPLACED LAMP STRIP, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20081001 NM 2008 10 1 2008UALA05552 1 20080831 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 180UA 25224 SEAT 5J FWD FLOOR EMERGENCY LIGHT INOP. FOUND FAULTY LAMP STRIP. REPLACED LAMP STRIP, OP CHECK GOOD. AC OK FOR SERVIC E. 2 L 7 4 4F 4 F RT A20WE E24NE 20081001 NM 2008 10 1 2008UALA05553 1 20080831 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 DOOR 4L DOOR MOUNTED EMERG EVAC LIGHT ONLY STAYS ON FOR A FEW SECONDS. FOUND FAULTY LAMP. REPLACED LAMP, OP CHECK GOOD . AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20081001 NM 2008 10 1 2008UALA05565 1 20080902 A 3350 LAMP BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 675UA 29243 DOOR 2L EXTERIOR EMERGENCY LIGHT INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20081001 NM 2008 10 1 2008UALA05567 1 20080902 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 569UA 26677 AFT OF WING LT EMERGENCY LIGHT INOP. FOUND LAMP INOPERATIVE. RELAMPED- OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081001 NM 2008 10 1 UPS08M53119 1 20080816 A 2430 UNKNOWN DOUG MD11 MD11F 3023600 NM COCKPIT FAILED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 288UP 48540 EMERGENCY POWER TEST FAIL. RESET CIRCUIT BREAKERS. OPS CHECK NORMAL. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 UPS08M53268 1 20080826 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP 48745 INSPECTION TYPE:1C LEFT WING L/E STRINGER CRACKED XFS 669. REMOVED, FABRICATED, AND INSTALLED STRINGER IAW DWG ARB1180 AND MD-11 SRM 51-35-01 TABLE 1, 51-33-01 PARAGRAPH 6. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 UPS08M53269 1 20080829 A 5720 STIFFENER DOUG MD11 MD11F 3023600 NM LEFT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP 48745 INSPECTION TYPE:1C LEFT WING L/E STIFFENER XFS 587 CRACKED. REMOVED, FABRICATED, AND INSTALLED STIFFENER IAW DWG ARB291 8, MD-11 SRM 51-35-01. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 UPS08M53270 1 20080829 A 5730 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP 48745 INSPECTION TYPE:1C RT WING L/E SKIN STRAP XFS 901 CRACKED. REMOVED, FABRICATED, AND INSTALLED SKIN STRAP IAW DWG ARB395 4 AND MD-11 SRM 51-33-01, 51-31-01. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 UPS08M53271 1 20080830 A 5730 SPLICE DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP 48745 INSPECTION TYPE:1C RT WING L/E SKIN SPLICE STRAP XFS 791 CRACKED. REMOVED, FABRICATED, AND INSTALLED SPLICE STRAP IAW D WG ARB 3954 AND MD-11 SRM 51-35-01, 51-33-01. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 UPS08M53272 1 20080828 A 5730 SPLICE DOUG MD11 MD11F 3023600 NM LEFT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP 48745 INSPECTION TYPE:1C LEFT WING L/E SKIN SPLICE XFS 791 CRACKED. REMOVED, FABRICATED, AND INSTALLED SKIN SPLICE STRAP IAW DWG ARB3954 AND MD-11 SRM 51-31-01, 51-33-01. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 UPS08M53273 1 20080827 A 5754 SLAT TRACK DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP 48745 INSPECTION TYPE:1C RIGHT WING SLAT TRACK 16 CRACKED. REMOVED, REPLACED, AND INSTALLED FITTING IAW MD-11 SRM 51-33-01, 5 1-31-01. 2 L 7 3 4F RT A22WE 20081001 NM 2008 10 1 ASAA0843454 1 20080823 A 5754 65C26603201A SKIN BOEING 737 7374Q8 138447Q NM NR 3 SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 778AS 25110 NR 3 SLAT LOWER SURFACE T/E INBOARD END IS CHAFED. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER. BONDED REPAIR IAW B737 400 SRM 51-70-10. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 ASAA0843455 1 20080823 A 5753 65C26601389A SKIN BOEING 737 7374Q8 138447Q NM NR 1 SLAT DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 778AS 25110 NR 1 SLAT LOWER T/E SURFACE IS DELAMINATED AT THE OUTBOARD CORNER. REMOVED DELAM SKIN AND CORE FABBED REPLACEMENT CORE, SKIN AND DOUBLER. BONDED REPAIR IAW B737 400 SRM 51 70 10 8. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 ASAA0843462 1 20080824 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 7 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 778AS 25110 NR 7 SPOILER UPPER SURFACE HAS PROTRUDING DENT 5 INCHES AFT OF L/E. REMOVED DAMAGED AERA, FABBED DOUBLER AND INSTALLED REPAIR IAW B737 400 SRM 57 70 01. 2 L 7 2 4F RT A16WE 20081001 NM 2008 10 1 UPS08653344 1 20080914 A 5720 SUPPORT BRACKET BOEING 767 76734AF 1385212 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 332UP 32843 INSPECTION TYPE:C LT WING NR 6 SLAT LWR LIP NR 5, 7 & 8 SUPPORT BRACKET CRACK (CRACK LENGTH .5 INCH). THREE EA SUPPORT BRACKET REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081002 NM 2008 10 2 2008UALA05503 1 20080827 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1420 S26L DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 BS 1420 STR 26L FRAME HAS DAMAGE. *S/D* MAJOR REPAIR ACCOMPLISHED. REMOVED PREVIOUS REPAIR INCLUDING STRINGER CLIPS A ND PRODUCTION SPLICE. FABRICATED & INSTALLED A REPAIR ANGLE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 EU 2008 10 2 2008UALA05521 1 20080829 A 2611 PPA120300 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LAVATORY INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 483UA 1586 LAV SMOKE DETECTOR INOP. REPLACED LAV 'D' SMOKE DETECTOR. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081002 NM 2008 10 2 CALA0800851 1 20080905 A 5311 143A1113 FRAME BOEING 737 737724 13844BY NM BS 440 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27722 28789 CABIN STA 440 FRAME CRACKED BETWEEN S8-9L. INSTALLED REPAIR PER EC/RA 5310-04824 REV A. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800852 1 20080805 A 5311 143A1110 FRAME BOEING 737 737724 13844BY NM BS 380 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27722 28789 CABIN STA 380 FRAME CRACKED BETWEEN S8-9L. INSTALLED REPAIR PER EC/RA 5310-04824 REV A. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800853 1 20080905 A 5311 143A1111 FRAME BOEING 737 737724 13844BY NM BS 400 S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27722 28789 CABIN STA 400 FRAME CRACKED BETWEEN S8-9L. INSTALLED REPAIR PER EC/RA 5310-04824 REV A. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 2008UALA05897 1 20080926 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 DOOR 3 RT AREA EMERGENCY LIGHT HAS QUICK DISCHARGE. REPLACED BATTERY PACK AND FUSE. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081002 NM 2008 10 2 UPS08M53298 1 20080822 A 5754 SKIN DOUG MD11 MD11F 3023600 NM NR 2 SLAT DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 290UP 48456 INSPECTION TYPE:C RT WING NR 2 SLAT LEADING EDGE DENT. DENT SKIN REMOVED PER SRM 57-10-00 FIG 37 VIR 40 & CUT OUT PROTE CTED PER SRM 51-21-01 VII R40. HFEC INSP C/OUT PER NDTSPM R.13 06-10-01.001 FOUND NO CRACK ON TRIMMED OUT AREA. REP FI LLER & DOUBLER FABRICATED PER SRM 57-10-00 FIG 37 V1. R40. ALL REPAIR PARTS REPROTECTED PER SRM 51-21-0 1 VII R40. OK TO INSTALL REPAIR PARTS. 2 L 7 3 4F RT A22WE 20081002 NM 2008 10 2 2008UALA05424 1 20080823 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 117UA 28810 DOOR 3 LEFT SILL EMERGENCY LIGHT IS INOP. FOUND BURNED OUT LAMP. REPLACED LAMP, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20081002 2008 10 2 2008UALA05491 4 20080827 A 2565 O-RING AIRCRUISERS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 498UA 1865 DOOR 2R SLIDE PRESSURE BOTTLE LOOKS LOW. O-RING LEAKING FROM CENTER BALL SHAFT. REMOVED & REPLACED O-RING. 2 L 7 2 4F 4 F RT A28NM E40NE 20081002 NM 2008 10 2 2008UALA05875 1 20080924 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 196UA 28715 SEAT 4A FWD EEL LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 20081002 NM 2008 10 2 CALA0800870 1 20080905 A 5531 65505753 SPAR BOEING 737 7373T0 1384582 NM VERTICAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 VERTICAL STABILIZER HAS CORROSION AT FIN STATION 163.90 - 191.50 LEFT-SIDE AT REAR SPAR. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER EC/RA 5530-01510. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800871 1 20080905 A 5320 6545834V551 INTERCOSTAL BOEING 737 737524 1384721 NM BS 328-344 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 INTERCOSTAL CRACKED FROM BODY STATION 328-344 AT LBL 44. REMOVED AND REPLACED INTERCOSTAL PER B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800873 1 20080905 A 5320 65C3459713 INTERCOSTAL BOEING 737 737524 1384721 NM BS 927-947 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 INTERCOSTAL FOUND CRACKED UNDER FLOORBOARD IN AFT CABIN BETWEEN BODY STATION 947.5 AND 927 AT RBL 25". REMOVED DAMAGE F ROM INTERCOSTAL BETWEEN BODY STATION 947.5 AND 927 AT RBL 25" UNDER FLOORBOARD IN AFT CABIN PER B737 SRM 51-70-11. FABR ICATED REPAIR FROM 7075-T6 .050 ALUM SHEET PO 56315A PER B737 SRM 51-70-11, INSTALLED PER B737 51-40-02. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 2008UALA05519 1 20080827 A 3510 89151114 OXYGEN BOTTLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 127UA 28813 CREW OXYGEN SYSTEM LOW. CREW COMMENTS: CREW O2 NEEDS SERVICING. *S/D* SUSPECT PRE FLIGHT CHECKS. SERVICED SYSTEM TO FULL. AC OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20081002 NM 2008 10 2 2008UALA05607 1 20080908 A 2421 1701768 IDG BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LEFT FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 214UA 30220 ELEC BACKUP GEN L DISPLAYED ON EICAS AND STATUS PAGE. FOUND FAULTY BUG. REPLACED LEFT BACKUP GENERATOR. OK FOR SERVIC E. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081002 NM 2008 10 2 2008UALA05614 1 20080906 A 5311 FRAME BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1197 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 AFT PIT STA 1197+66 FRAME CAP HAS FLAKED PAINT AND LIGHT SURFACE CORROSION FROM LBL 48 - RBL 10. MAJOR REPAIR ACCOMPLIS HED. INSTALLED NEW FRAME CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 2008UALA05615 1 20080906 A 5310 STRUCTURE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 AFT PIT, UPPER CHORD FOR WEB AT STR 33L CORRODED ON THE LOWER SURFACE. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW ANGLE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 2008UALA05616 1 20080906 A 5300 STRUCTURE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1197 S33L CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 AFT PIT CORROSION ON FRAME CAP LOWER SURFACE AT BS 1197+110 AND STR 33L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED "T " CAP. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 SWAA084979 1 20080910 A 5310 6547952 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO DOOR AFT FRAME CRACKED AT LOWER END. REMOVED AND REPLACED FRAME PER BOEING DRAWING AND SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084980 1 20080910 A 5310 6547952 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO DOOR AFT FRAME CRACKED AT UPPER END. REMOVED AND REPLACED FRAME PER BOEING DRAWING AND SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085254 1 20080927 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 729E TO BS 739E, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085253 1 20080927 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED SC CHECK, FOUND SKIN CRACKED AT BS 307, BELOW STR 18R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085227 1 20080923 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 10R. REPAIRED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085226 1 20080923 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND FRAME CORRODED AT BS 500A BETWEEN STR 28L AND STR 28R. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085243 1 20080919 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CORRODED AT BS 785, STR 26R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085242 1 20080919 A 5320 6567740 STIFFENER BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND MLG W/W BS 663 VERTICAL STIFFENER CRACKED AT LBL 6.15. REMOVED AND REPLACED STIFFENE R PER ACO. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085241 1 20080919 A 5314 6545866 KEELBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND LT FWD KEEL BEAM CORRODED AT BS 500D. REMOVED AND REPLACED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085240 1 20080919 A 5322 6546546 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND BELTFRAME SHEAR TIE CORRODED AT BS 767, STR 26R TO STR 25R. REMOVED AND REPLACED SHE AR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085238 1 20080905 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP DAMAGED AT BS 767, STR 25R AND STR 26R. REPAIRED PER SWA EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085237 1 20080905 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CRACKED AT BS 485, STR 28R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085236 1 20080928 A 2150 22064002 ACM BOEING 737 7377H4 1384404 NM A/C BAY OVERHEATED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 29 425LV 29829 F/A'S REPORTED FUMES IN FWD PART OF CABIN. REMOVED AND REPLACED ACM, WATER SEPARATOR BAGS AND HEPA FILTER PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085235 1 20080927 A 3230 69141067 ACTUATOR BOEING 737 7377H4 1384404 NM NLG FAULTY A SWAA K NONE O OTHER CL CLIMB 1 SW 29 725SW 27857 DURING CLIMB NLG EXTENDED WITHOUT COMMAND WHEN GEAR HANDLE MOVED TO OFF POSITION. REMOVED AND REPLACED NLG LOCK ACTUATO R PER MM. 2 L 7 2 4F RT A16WE 20081002 2008 10 2 SWAA084984 4 20080910 A 2565 D31354418 SLIDE BOEING 737 7373K2 13844BA NM L2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 345SA 23786 DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE INDICATED OUT OF LIMITS. REMOVED AND REPL ACED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081002 2008 10 2 SWAA084985 4 20080910 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084986 1 20080910 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 480 S7R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA084987 1 20080910 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 480 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081002 2008 10 2 SWAA084990 4 20080910 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 791SW 27886 R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081003 SO 2008 10 3 C2X2008F00044 1 20080906 A 3230 355022002 ELECTRONIC UNIT EMB 145 EMB145EP 3260221 SO MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15932 22073 145015 THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AC RETURNED WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONICS UNIT, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AC WAS APPROVED FOR RETURN TO SERVICE. (K) 2 L 7 2 4F RT T00011AT 20081003 NM 2008 10 3 UPS08M53410 1 20080919 A 5720 STIFFENER DOUG MD11 MD11F 3023600 NM RT WING BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 287UP 48539 INSPECTION TYPE:1C BROKEN STIFFENING RIB INSIDE RT WING I/B LEADING EDGE PANEL 616EB, ON UPPPER PANEL PART NUMBER ARB238 6-402PFD PANEL 616ET. REMOVED 2 EACH STIFFENER RIBS, FABRICATED, AND INSTALLED STIFFENER RIBS IAW DWG ARB2440, MD-11 SR M 51-21-01, 51-41-01. 2 L 7 3 4F RT A22WE 20081003 NM 2008 10 3 UPS08653415 1 20081001 A 5754 PANEL BOEING 767 76734AF 1385212 NM L/E SLAT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 331UP 000043 27757 LEFT INBOARD L/E SLAT CLOSURE PANEL DAMAGED BEYOND LIMITS. REPAIRED NR 6 L/E SLAT CLOSURE PANEL TORN OFF AREA IAW SRM 5 7-43-01-2R, REPAIR 3 TABLE 1 WET LAYUP 200DF CURE METHOD. SLAT OPERATION TEST SATISFACTORY IAW AMM 27-81-00-05. ACFT OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20081003 NM 2008 10 3 SWAA084995 1 20080911 A 5312 6545819 PRESSURE PANEL BOEING 737 7373Y0 1384671 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED BRDG CHECK, FOUND NLG W/W LT CEILING PANEL CUTOUT WEB CRACKED. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA084996 1 20080911 A 5312 6545819 PRESSURE PANEL BOEING 737 7373Y0 1384671 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED BRDG CHECK, FOUND NLG W/W RT CEILING PANEL CUTOUT WEB CRACKED. REPAIRED WEB PER ACO. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA084997 1 20080911 A 5322 6546948 SHEAR TIE BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED BRDG CHECK, FOUND SHEAR TIE CRACKED AT BS 967, STR 7L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA084998 1 20080911 A 5753 6546430190 SKIN BOEING 737 737317 138447P NM FOREFLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 698SW 23176 DURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD FORE FLAP DELAMINATED AT LOWER SURFACE. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20081003 WP 2008 10 3 UPS08853314 1 20080905 A 5713 STRINGER DOUG DC8 DC871F 302199D WP WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C2 4ALT- STRINGER 51 CRACKED BETWEEN XM 408 AND XRS 463 ACESS THRU 505B. REMOVED AND REPLACED STRINGER SECTION IAW SRM 51-1-20D, 57-2-2 FIG 3D, 51-3-0. 2 L 7 4 4F RT 4A25 20081003 NM 2008 10 3 UPS08M53312 1 20080831 A 5720 STRUCTURE DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 250UP 48745 INSPECTION TYPE:1C RIGHT WING TELESCOPING DUCT CUTOUT UPPER I/B CORNER AND O/B CORNER CRACKED. REMOVED CRACK, FABRICATE D AND INSTALLED FILLER AND DOUBLER IAW MD-11 SRM 57-10-00 FIG 43. 2 L 7 3 4F RT A22WE 20081003 NM 2008 10 3 2008UALA05612 1 20080906 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 795UA 26927 SEAT 2E EMERGENCY LIGHT INOP WHEN TESTED. FOUND LIGHTS INOP. REPLACED BOTH EMERGENCY LIGHTS AT SEAT 2E. BOTH OP CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081003 NM 2008 10 3 2008UALA05660 1 20080906 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 FLOORBEAM 140 HAS CORROSION ON ENTIRE LENGTH. MAJOR REPAIR ACCOMPLISHED. BEAM OUT AND ON BENCH WORKING. FAB'D SPLICES FOR BEAMS FORE AND AFT PRIMED, SEALED & INSTALLED AFT END TO BEAM 145, FWD READY TO INSTALL. INSTALLED SPLICE TO BEAM 80. REPLACED BEAM AND COMPLETED WITH FASTENERS. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05662 1 20080908 A 5322 SHEAR TIE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 AFT RT SHEAR TIE CORRODED BETWEEN FRAME 69 & 70. MAJOR REPAIR ACCOMPLISHED. FABRICATED NEW SHEAR TIE. INSTALLED SHEA R PLATE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05663 1 20080909 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 FLOORBEAM -Y1292 HAS CORROSION JUST AFT OF FR66. MAJOR REPAIR ACCOMPLISHED. REPLACED BEAM & SECURED WITH FASTENERS. A CP BEAM INSTALLATION FOR Y1292 FWD OF BEAM 140. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05669 1 20080910 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT ROW 46 RT INOP. FOUND FAULTY LAMP. REPLACED LAMP. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081003 SO 2008 10 3 C2X2008F00023 1 20080902 A 3230 23092005003 LANDING GEAR EMB 145 EMB145LR 3260212 SO MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 13979 145181 AC WAS ENROUTE WHEN THEY GOT A LG AIR/GND FAIL MESSAGE. AC DIVERTED WHERE MAINT PERFORMED MULTIPLE GEAR RETRACTIONS AND THE GEAR RETRACTED NORMALLY. NO INDICATIONS. AC RELEASED TO SERVICE IAW EMB 32-30. (K) 2 L 7 2 4T RT T00011AT 20081003 NM 2008 10 3 2008UALA05488 1 20080826 A 2130 CHECK VALVE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE FAULTY A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 376UA 24641 PRESSURIZATION PROBLEM. RTFL. FAULTY CHECK VALVE. REPLACED CHECK VALVE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081002 NM 2008 10 2 UPS08553239 1 20080829 A 3020 CIRCUIT BREAKER BOEING 757 75724APF 1384969 NM RIGHT ENGINE TRIPPED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 460UP 25481 CREW LOST AUTO THROTTLES AND RIGHT ENGINE THRUST MGMT COMPUTER PARAMETERS DISPLAY. SUBSEQUENTLY, THE EEC LIGHT AND TAT PROBE LIGHT ILLUMINATED. FLIGHT RETURNED TO MIA. FOUND C/B GL24 POPPED, RESET C/B. ACCOMPLISHED TAT PROBE HEAT TEST P ER AMM 30-33-00-5. OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 20081002 NM 2008 10 2 2008UALA05882 1 20080924 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 547UA 25368 AFT PIT STA 1500 FRAME DENTED BETWEEN STR 24L AND 26L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER FRAME REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 SWAA085127 1 20080918 A 5315 6546811 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 781WN 30601 DURING SCHEDULED 8Y CHECK, FOUND UPPER FLOORBEAM CORRODED AT BS 986.5 BETWEEN RBL 32 TO RBL 44. REMOVED AND REPLACED BE AM PER SWA EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873493 1 20080903 A 5320 146A9401 SPLICE PLATE BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 CORROSION FOUND ON AFT CARGO PIT FLOOR PANEL T-SPLICE PLATE AT BS 767. CORROSION FOUND ON AFT CARGO PIT FLOOR PANEL IAW SPLICE PLATE FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMIT. TEE SPLICE PLATE WAS REPLACED IAW B737 700 SRM 53 00 53 AND DW G 146A9401. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873492 1 20080903 A 5320 146A9401 SPLICE PLATE BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 CORROSION ON AFT CARGO PIT FLOOR PANEL TEE SPLICE PLATE AT BS 727D. CORROSION FOUND ON AFT CARGO PIT FLOOR PANEL TEE SP LICE WAS INVESTIGATED AND REPLACED IAW B737 700 SRM 53 00 53 AND DWG 146A9401. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873482 1 20080901 A 5320 146A81275 FLOOR SUPPORT BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 AFT CARGO FLOOR SUPPORT WEB AT BS 847 867 RBL 22 FOUND CORRODED. CORRODED SUPPORT WEB AT AFT CARGO PIT BETWEEN 847 867 RBL 22 FOUND TO BE BEYOND ALLOWABLE DAMAGE LIMIT. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873501 1 20080828 A 5320 453A26113 ANGLE BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 AFT CARGO PIT ZEE ANGLE FOUND CORRODED AT BS 867 - 947 RBL 23 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 2008UALA05626 1 20080907 A 3350 362624 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 556UA 26650 EXTERIOR EMERGENCY EXIT LIGHT INOP AT LT NR 1 DOOR. LIGHT FOUND INOP. REPLACED LAMP. OP CKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 2008UALA05627 1 20080907 A 3350 362624 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 556UA 26650 EXTERIOR EMERGENCY EXIT LIGHT AT DOOR NR 4 RT. LIGHT FOUND DEFECTIVE. REPLACED LAMP. OPS CHK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081002 NM 2008 10 2 CALA0800901 1 20080916 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 747 FRAME IS CRACKED AT AIR CONDITIONING (AC) BRACKET BETWEEN STRINGERS 8R AND 9R. INSTALLED REPAIR ANGLES AT STATIO N 747 BETWEEN STR 8R AND 9R PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800900 1 20080916 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 867 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. REMOVED A/C RAIL BRACKET IAW EA 5310-04498, CUT OUT 2 EA HOLES IN FRAME IAW EA 5310-04498. HFEC INSPECTED IAW 737 NDTM PT6 51-00-00, FIG 23. NO DEFECTS NOTED. FABRICATED REPAIR ANGLES, TREATED AND PRIMED IAW EA 5310-04498. INSTALLED REPAIR ANGLES AND A/C RAIL B RACKET IAW EA 5310-04498. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800899 1 20080916 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 907 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L & 9L. REPAIRED CRACKED FRAME AT S TATION 907 PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800897 1 20080916 A 5311 65C33511 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 440 FRAMED CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. REPAIRED CRACKED FRAME AT S TA 440 BETWEEN STR 8R AND 9R PER EA5310-04498. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800896 1 20080916 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 907 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. REMOVED BRACKET IAW EA531 0-04498 CUT OUT DAMAGE IAW EA5310-04498 INSPECTED CUTOUT IAW 737 NOTM P T65100-00 FIG 23, NO DEFECTS NOTED. FABRICATED PARTS, ALODINED AND PRIMED PARTS AND CUTOUT IAW EA5310-04498. INSTALLED REPAIR ANGLES AND BRACKET IAW EA5310-04498. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800894 1 20080916 A 5311 6546525 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 380 FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8R AND 9R. REMOVED A/C RAIL BRACKET, CUT OUT DAMAGE TO FRAME. PERFORMED HFEC. FABRICATED AND INSTALLED REPAIR PARTS IAW EA5310-04498. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 CALA0800929 1 20081001 A 5330 65C32362 SKIN BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 17356 23942 FUSELAGE SKIN CREASED AFT OF PREVIOUS REPAIR, STATION 847 AT S-4L. REPAIRED PER SRM 53-00-01 FIG 201, PAGE 23. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085269 1 20080930 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 673, LBL 24.8. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085303 1 20080930 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 390, LBL 4. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085302 1 20080930 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 430, RBL 2. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085301 1 20080930 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 410, RBL 2. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085294 1 20080930 A 5313 6917286 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 367SW 26578 DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR LOWER FUSELAGE STRINGER CORRODED AT BS 208, STR 26L. REMOVED AND REPLACED STR INGER PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085285 1 20080930 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 380, STR 15L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085284 1 20080930 A 5322 6546569 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 927, STR 24R TO STR 25R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085297 1 20080929 A 5311 6546549 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 656SW 28401 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 767, STR 27L. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 2008UALA05413 1 20080822 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 545UA 25323 LOWER GATE CORRODED R-4 DOOR. REPLACED LOWER GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081003 NM 2008 10 3 2008UALA05650 1 20080909 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 182UA 25279 LAV 100 & LAV 101 FWD CORNERS HAVE EVAC LIGHT ASSY THAT ARE LOOSE. SECURED EVAC LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081003 NM 2008 10 3 2008UALA05671 1 20080910 A 5320 TORQUE BOX BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 AFT PIT, PITTING CORROSION IN TOP SURFACE OF TORQUE BOX STA 1345, RBL 8. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION & FOUND TO BE OUT OF LIMITS. REMOVED WEB. FABRICATED & INSTALLED NEW WEB. 2 L 7 2 4F 4 F RT A1NM E24NE 20081003 NM 2008 10 3 2008UALA05659 1 20080908 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 FLOORBEAM 195 HAS CORROSION ALONG LENGTH (MARKED). MAJOR REPAIR ACCOMPLISHED. STARTED REMOVING FASTENERS. REMOVED SEV ERAL FASTENERS FROM BEAM 190 TO REMOVE BEAM 195. BEAM REMOVED. INSTALLED 8 NUT PLATES ON BEAM 195 FOR PNL 261FF. SECU RED NUT PLATES FOR FLOORBOARD HOLES. INSTALLATION IS COMPLETE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05661 1 20080908 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 FLOORBEAM 190 HAS CORROSION AFT OF FR68 (MARKED). MAJOR REPAIR ACCOMPLISHED. STARTED REMOVING FASTENERS. BEAM REMOVED . STARTED INSTALLATION OF BEAMS 190 AND 195. SECURED NUT PLATES FOR FLOORBOARD. INSTALLATION IS COMPLETE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05668 1 20080911 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 FLOORBEAM - Y765 HAS CORROSION FWD OF FR68. MAJOR REPAIR ACCOMPLISHED. BEAMS REMOVED AND BRACKETS TRANSFERRED (BEAM 95 AND 150) BEAMS NEED TO BE SPLICED TOGETHER AND INSTALLED. SPLICE INSTALLED AND BEAMS 95 AND 150 INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081114 EU 2008 11 14 08FDEA04707 1 20081031 A 5753 A5796011422000 WEB AIRBUS 300 A300B4622R 3930312 EU ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 LEFT WING INBD FLAP AT RIB 25A, WEB PLATE IS CRACKED. REMOVED AND REPLACED THE -220 WEB PLATE IN REF TO A300-600 SRM 51 -40-21; PARA 7; PARA 14 AND FOKKER DWG A57960114, ISSUE E. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 ASAA0873694 1 20081031 A 5320 141A541016 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 PAX CABIN FWD FLOOR INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 ASAA0873695 1 20081028 A 5347 1A2260205 SEAT TRACK BOEING 737 737790 13844CN NM COCKPIT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 CAPTAIN O/B SEAT TRACK IS CHAFED AT AFT RADIUS. REMOVED AND REPLACED SEAT TRACK. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 08FDEA04710 1 20081104 A 5311 7075T60630 FRAME BOEING 757 757236 1384971 NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 MAIN CABIN AT STA 1620 STR 5L HAS TOOLMARK. REPAIRED FRAME BS 1620 S5L IAW SRM 53-00-07 REPAIR NR 1. REMOVED AND REINS TALLED SHEAR TIES FOR ACCESS. CATEGORY A REPAIR, NO FOLLOW-UP REQUIRED. 2 L 7 2 4F RT A2NM 20081114 NM 2008 11 14 08FDEA04750 1 20081105 A 5753 692288221 BRACKET BOEING 727 7272S2F 1384O81 NM TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 NR 5 FLAP TRACK FAIRING BRACKET CLIP IS CRACKED LOCATED ON INBD SIDE, 20 INCHES FROM FWD END VERIFIED MATERIAL AS 7075-T 6-.063 REF DWR 69-22882. REPLACEMENT MATERIAL SAME AS ORIGINAL, FABRICATED BRACKET FOR INBD SIDE OF NR 5 FLAP TRACK PER DWR 69-22882. TREATED BRACKET REF MM 51-20-021-7 AND PRIMED REF MM 51-20-031-7 AND INSTALLED BRACKET ON FLAP TRACK REF SRM 51-30-2. MARKED BRACKET WITH FX 69-22882-21 REF GMM 7-0-1001. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04753 1 20081105 A 5320 6529548 ANGLE BOEING 727 7272S2F 1384O81 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 DITCHING PAN ANGLE, JUST OTBD OF AIRSTAIR DOOR, LEFT SIDE IS CRACKED AT ALL FASTENER HOLES. REPLACED ANGLE REF DWR 65 -29548. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081118 NM 2008 11 18 08FDEA04790 1 20081107 A 5340 ATTACH FITTING BOEING 727 7272D4 138407U NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 LT LWR FUSE TO BODY FAIRING SUPPORT (STA 870) HAS A CRACKED CLIP. REMOVED AND REPLACED CRACKED ANGLE CLIP STA 870 LT WI NG TO BODY FAIRING SUPPORT CLIP ALL WORK ACCOMPLISHED REF DRW 66-47181-3 AND SRM 51-30-02 AND 51-10-3. THIS IS CLASSIFI ED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081118 NM 2008 11 18 08FDEA04791 1 20081107 A 5720 6521655616 SUPPORT BOEING 727 727227 1384078 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 487FE 21490 APU EXHAUST DUCT MOUNT FLANGE AT UPPER WING PANEL, AFT Z ANGLE SUPPORT CORRODED. REPLACED FLANGE SUPPORT/STIFFENER RE F SRM 51-30-02 PG 2 AND 5. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081118 SO 2008 11 18 C2XA08SH129 1 20081014 A 5720 14567605001 BRACE EMB 145 EMB145XR 3260214 SO WING CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 11193 14500938 SHV DURING C CHECK LT FWD SIDE BRACE WING FITTING BEARING HOUSING HAS SCRATCHES ON INTERNAL SURFACE AND PITTING CORROSIO N. MX R&R LT FWD SIDE BRACE WING FITTING. IAW EC5750-01369. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081118 EU 2008 11 18 QML2008F00022 1 20081024 A 5312 1172233803 BULKHEAD BOLKMS 117 BK117A4 5626017 EU FUSELAGE CRACKED E QMLA K NONE O OTHER IN INSP/MAINT 1 NM 03 485UH 12230 7036 WHILE PERFORMING NON RELATED MX ON N125EC SN 7065 A CRACK WAS DISCOVERED IN THE LT AFT 5600 BULKHEAD IN THE AREA OF THE MOUNTED VACUUM PUMP. THE ACFT WAS GROUNDED AND MX NOTIFIED. CHOSE TO DO A PRECAUTIONARY CHECK OF OUR OTHER 3 ACFT ON S IGHT AND FOUND CRACKS IN THE SAME AREA ON N485UH SN 7036. 1 G 7 2 3U H13EU 20081118 EA 2008 11 18 TRAX200801242 1 20080929 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 LT UPPER OBLIQUE ANGLE (INTERCOSTAL) IN AFT EQUIPMENT BAY, FS 621 TO FS 625 IS CRACKED IN RADIUS. (K) 2 L 7 2 4F RT A21EA 20081117 NM 2008 11 17 SWAA086202 1 20081113 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 4L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086203 1 20081113 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 3L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086219 1 20081113 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND LT CREASE BEAM WEB CORRODED AT BETWEEN BS 867 TO BS 887. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086220 1 20081113 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086221 1 20081113 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086222 1 20081113 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086227 1 20081113 A 5320 BAC1508 FITTING BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 741SA 29277 DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, RBL 15. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086228 1 20081113 A 5320 BAC1508 FITTING BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 741SA 29277 DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, RBL 6. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086229 1 20081113 A 5320 BAC1508 FITTING BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 741SA 29277 DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 6. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086230 1 20081113 A 5320 BAC1508 FITTING BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 741SA 29277 DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 15. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086231 1 20081113 A 5320 BAC1508 FITTING BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 741SA 29277 DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 32. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 ZZDA2008168 1 20081101 A 5311 FRAME BOEING 717 717200 1383700 NM BS 1178 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 972AT 55033 FROM N/R N1300620--AFT ACCY. COMPARTMENT FOUND 2 CRACKS IN FRAME ONE CRACK IS 3" LONG AT THE 4 O'CLOCK POSITION SECOND C RACK IS LOCATED 2" ABOVE AND IS 13/4" IN LENGTH STATION 1178 REAR SPAR INSTALLATION CANTED. REMOVED TAIL CONE AND LT PY LON T/E TO ACCESS AREA PER AMM &SRM 53-52-01 AND 51-10-4.REPAIRED LT CANTED FRAME BS 1178 BETWEEN L16 & 17 LT IAW SRM 51 -70-11 INSTALLED TAIL CONE & LT PYLON T/E IAW AMM & SRM 53-52-01, 51-10-4 ON W/O 28476-2 NRWC 4661 AND 4660. STRUCTURAL REPAIR REPORT SUBMITTED TO ENGINEERING. 2 L 7 2 4F TR A6WE 20081114 CE 2008 11 14 Z5FA103108N610CS1 1 20081031 A 5610 991438012 WINDSHIELD CESSNA 680 680SOV 2076811 CE COCKPIT CRACKED E Z5FA O OTHER N FALSE WARNING CR CRUISE 1 EA 63 610CS 2145 6800092 AT FL 410 WHEN WINDSHIELD HEAT FAIL LIGHT ILLUMINATED, CREW FOLLOWED CHECKLIST, WAITED APPROX 5 MINUTES AND RESET BREAKE R. W/S HEAT FAIL LIGHT REMAINED EXTINGUISHED AT THIS TIME. APPROX 30 SECONDS LATER, CREW HEARD A LOUD POP AND WITNESSE D COPILOTS WINDSHIELD SPIDERWEBBED. CREW DECLARED AN EMERGENCY AND DIVERTED TO GJT. REMOVED AND REPLACED CO-PILOTS WIN DSHIELD, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RC T00012WI 20081114 NE 2008 11 14 V2JA145103108 2 20081031 A 7200 ENGINE PIAGIO P180 P180 6960204 EU PWA PT6 PT6A66 52043 NE LEFT POWER LOSS E V2JA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 15 145SL 4201 116 1093 RK0114 CREW NOTICED LOSS OF TORQUE AND OIL PRESSURE ON LT ENGINE. OIL PRESSURE LIGHT CAME ON. PER MANUAL, CREW CONTINUED WITH SECURING PROCEDURES AND SHUT DOWN LT ENGINE. AIRCRAFT LANDED WITH NO INCIDENT. 1 H 7 2 3O 4 T RT A59EU E26NE 20081114 EA 2008 11 14 S9BA2008031 1 20081105 A 5740 CLAMP DHAV DHC6 DHC6300 2802606 EA FUEL CELL LOOSE A S9BA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 29 288SA 74 74 573 ON PREFLIGHT FUEL ODOR NOTICED IN CABIN. FOUND CLAMP AT FWD RT FUEL CELL NIPPLE LOOSE. TIGHTENED CLAMP AND CHECKED FOR L EAKS. NO LEAKS NOTED. REQUEST CHECK FLIGHT TO CHECK FOR FUEL SMELL IN CABIN. CHECK FLIGHT WAS SATISFACTORY. 1 H 7 2 3T RT A9EA 20081114 EA 2008 11 14 S9BA2008032 1 20081108 A 7921 AN90112A GASKET DHAV DHC6 DHC6300 2802606 EA OIL COOLER FAILED A S9BA O OTHER K FLUID LOSS CR CRUISE 1 SO 29 573SA 573 LOST NR 2 OIL PRESSURE AND TORQUE PRESSURE OIL ON ENGINE COWLING AND RIGHT FLOAT. FOUND OIL COOLER RETURN LINE GASKET L EAKING. REMOVED AND REPLACED GASKET, SERVICED ENGINE WITH 4 QUARTS OF OIL. LEAK CHECK SATISFACTORY. PROPELLER WAS FEAT HERED AND ENGINE WAS SHUTDOWN IN FLIGHT 1 H 7 2 3T RT A9EA 20081114 NM 2008 11 14 SWAA086183 1 20081112 A 5312 6546568 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD WEB CRACKED AT BS 1016, STR 5L. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086184 1 20081112 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM TEE CAP CRACKED AT BS 294, LBL 52. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086185 1 20081112 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 13L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086194 1 20081112 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081114 EU 2008 11 14 2008UALA06375 1 20081105 A 5315 FLOORBEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 404UA 450 BEAM 235 HAS CORROSION AT AFT END OF FRAME 68. REMOVED FASTENERS BEAM STILL NEEDS REMOVED. REMOVED BEAM 235. NEW BEAM IS ON BENCH AND IS DRILLED OUT, MOUNTS ARE HELD IN PLACE. PLACED SEALANT AND HARDWARE BY BEAM. REPLACED BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081113 EU 2008 11 13 HDNA200811072008 1 20081106 A 2612 CONTACTOR PWC UROCOP EC135 EC135P1 8680990 EU FIRE DETECTOR CONTAMINATED E HDNA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 03 911KB 0013 BB0067 DURING TAKEOFF, THE NR 1 ENGINE FIRE DETECTOR LIGHT ILLUMINATED ON THE WARNING PANEL. THE AIRCRAFT RETURNED TO THE HELI PAD WITHOUT INCIDENT. DURING THE INSPECTION OF THE SYSTEM IT WAS FOUND THAT THE FIRE DETECTOR CONTACTORS WERE WET FROM A PREVIOUS RAIN STORM. THE CONTACTORS WERE CLEANED AND THE SYSTEM WAS OPERATING WITHIN LIMITS. 1 G 7 2 3U O H88EU 20081113 NM 2008 11 13 HNAA2008110800317 1 20081009 A 5330 85320300281 DOUBLER DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 827EX 33979 33979 390 DURING C-CHECK, THE LAVATORY SERVICE DOOR CUTOUT ON THE RIGHT SIDE OF THE FUSELAGE BELOW AND FORWARD OF THE RIGHT SIDE E MERGENCY EXIT WAS FOUND TO HAVE CORROSION ON THE SKIN DOUBLER. THE CORROSION WAS LOCATED ON THE AFT CORNER, BOTTOM EDGE OF THE LAVATORY SERVICE DOOR OPENING. APPROXIMATE LOCATION WAS X216.0 BY Y93.0. CORRODED AREA WAS CUT OUT AND AREA CH ECKED USING HFEC. NO DEFECTS WERE FOUND. REPAIR WAS THEN COMPLETED USING DEHAVILLAND RD8-53-2103. 2 H 7 2 4T RT A13NM 20081113 NM 2008 11 13 HNAA2008110300319 1 20081103 A 3242 21565 BRAKE DHAV DHC8 DHC8102 2809003 NM NR 1 SMOKE A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 826EX 9466 182 389 THE NR 1 BRAKE ASSEMBLY APPEARED TO BE SMOKING DURING TAXI. MAINTENANCE JACKED THE AIRCRAFT AND INSPECTED THE BRAKE ASS EMBLY. THE BRAKE WAS COLD TO THE TOUCH AND WEAR PINS INDICATED A NEWER BRAKE ASSEMBLY. THE BRAKE ASSEMBLY WAS CHANGED AS A PRECAUTION. LEAK AND OPS CHECKS WERE GOOD AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 20081113 NM 2008 11 13 KCSA081563 1 20081107 A 5753 PLATE BOEING 747 747249F 1384849 NM TE FLAP CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 LT TRAILING EDGE INBOARD MID-FLAP HAS CORROSION ON TIE PLATE AT WBL 235.20. 2 L 7 4 4F RT A20WE 20081113 NM 2008 11 13 KCSA712A 1 20081110 A 5313 STRINGER BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 CORROSION ON STR 46R AT BS 560. 2 L 7 4 4F RT A20WE 20081114 NM 2008 11 14 CALA0801044 1 20081108 A 5320 148A852016 BRACKET BOEING 737 737724 13844BY NM APU BAY WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 38727 28797 LEFT BRACKET ATTACHED TO INBOARD SIDE OF WEB ABOVE APU INLET DUCT HAS WEAR MARKS. REPAIRED LEFT BRACKET PER EC/RA 5311- 01432 AND ISSUED DIP TO READ, ACCOMPLISH PERMANENT REPAIR WITHIN 12 MONTHS FROM 6 NOV 08. PLANNING TO CONTACT ENGINEERI NG AFTER 10 MONTHS BUT BEFORE 11 MONTHS FOR A PERMANENT REPAIR. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801026 1 20081103 A 5311 BAC15171470 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 FRAME CRACKED AT STATION 907 S-9L. REPAIRED FRAME PER EA 5310-04498, OP2. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 CALA0801047 1 20081108 A 5320 147A5712 SHEAR WEB BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 73259 30803 SHEAR WEB AT STATION 986.5 LBL 48 CRACKED. FABRICATED REPAIR PER ECRA 5321-01585 AND INSTALLED PER SRM 51-40-02 FOR SHE AR WEB AT STATION 986.5 LBL 48. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086177 1 20081112 A 5320 BAC14902831 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND CARGO BAY FLOOR SUPPORT BEAM COORDED AT BS 729E, LBL 3. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 ASAA0843724 1 20081029 A 5320 65469563 SHEAR WEB BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 SHEAR WEB CORRODED LT STA 400. REMOVED CORRODED AREA OF WEB, FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 5 1 70 13. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 08FDEA04760 1 20081105 A 5414 311N504634 SKIN BOEING 757 75723A 1384967 NM NR 1 PYLON CORRODED A FDEA O OTHER O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 NR 1 PYLON INBD AFT 311N5046-34 SKIN PANEL ASSY HAS CORROSION ON INNER SURFACE. REMOVED AND INSTALLED REPAIRED NR 1 PYL ON INBD AFT SKIN PANEL ASSY IAW DWG 311N5002 AND SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING REQUIREMENTS. 2 L 7 2 4F RT A2NM 20081114 NM 2008 11 14 08FDEA04739 1 20081105 A 5320 6515940 STRAP BOEING 727 7272S2F 1384O81 NM ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 MAIN CABIN FLOOR CHAFING ON "I" BEAM FLOORBEAM AT STA 740 FROM BL 0 TO RBL 50. REMOVED DAMAGED STRAP REF 51-30-02, FABR ICATED REPLACEMENT STRAP REF EA 7-5310-118310. TREATED AND PRIMED REF AMM 51-20-151. INSTALLED NEW STRAP REF EA 7-5310 -118310, WORKED WITH N/R N00389. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04740 1 20081105 A 5320 69205885 INTERCOSTAL BOEING 727 7272S2F 1384O81 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 COCKPIT FLOOR SUPPORT INTERCOSTAL IS CRACKED BS 304, LBL 10, WL 208. REMOVED FIRE EXTINGUISHER BRACKET TO FOM REF SRM 5 1-30-2 P. 1. REMOVED DAMAGED INTERCOSTAL REF SRM 51-30-2. INSTALLED REPLACEMENT INTERCOSTAL REF SRM 51-30-2. REINST ALLED FIRE EXTINGUISHER BRACKET. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 EU 2008 11 14 08FDEA04743 1 20081105 A 5311 A55770545 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS GOUGE ON FR 28, 2.5 INCH ABOVE STR 14L. REPAIR COMPLIED WITH ON EA 6-5310-123938. 2 L 7 2 4F RT A35EU 20081114 2008 11 14 08FDEA04699 4 20081104 A 2210 WARNING LIGHT AIRBUS 300 A300B4622R 3930312 EU AUTOLAND SYS FALSE ACTIVATION A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CE 21 728FD 581 AT 250' ON AN ACTUAL CAT3 APPROACH GOT RED AUTOLAND FLASHING LIGHT ALL PARAMETERS APPEARED NORMAL. EXECUTED A GO AROU ND. PERFORMED A FAULT ISOLATION PROCEDURE AND A AFS LAND TEST PER AMM 22-42-00-0. NO FAULTS WERE RECORDED ON DISPLAY O R TRIFOLD FAILURE RECORD INDICATOR. AFS LAND TEST PASSED WITH NO FAULTS. 2 L 7 2 4F RT A35EU 20081114 EU 2008 11 14 08FDEA04700 1 20081104 A 5311 A53773288200 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK FR 20 HAS GOUGE 3.5 INCHES BELOW STR 12R. REPAIR COMPLIED WITH ON EA6-5310-124032. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 ASAA0873696 1 20081030 A 5320 BAC1515531 ANGLE BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 RIGHT O/B FLOOR PANEL ANGLE AT BS 636 TO BS 638 HAS CORROSION. REMOVED AND REPLACED FLOOR PANEL ANGLE FROM BS 627-674. 2 L 7 2 4F RT A16WE 20081114 EU 2008 11 14 2008UALA06370 1 20081104 A 3350 20131A BATTERY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 427UA 512 FAILED EMERGENCY LIGHT SYSTEM TEST REF MM 33-51-00-710-001. MESSAGE: EMER SYSTEM ATA 33-51-38 BATTERY EMER R. REPLACE D BATTERY FOR RIGHT MID CABIN. OP'S CHECK GOOD. EMER LIGHT SYS TEST PASSED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081114 NM 2008 11 14 SWAA086179 1 20081112 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 UIEA200800338 1 20081105 A 2721 CONTROLLER BOEING 747 747243B 1384830 NM RUDDER RATIO FAILED A UIEA O OTHER J WARNING INDICATION CL CLIMB 1 EA 15 517MC 23300 RUDDER RATIO LIGHT CAME ON IN CLIMB PASSING THROUGH 5000FT. PROCEEDED AS PER FHB 3-27-24. REMOVED AND REPLACED LOWER REP LACED LOWER RUDDER RATIO CHANGER AND PERFORMED REQUIRED CHECKS PER MM 27-21-00 2 L 7 4 4F RT A20WE 20081114 SO 2008 11 14 SIMA200831001 1 20081105 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO READING LIGHT DAMAGED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 657AE 145744 ON FLIGHT 3693 CREW REPORTED THAT THEIR WAS A READING LIGHT THAT WAS FLICKERING AND THEN BEGAN TO EMIT AN ODOR OR SMOKE WHILE IN FLIGHT AIRCRAFT REMOVED FROM SERVICE. UPON INVESTIGATION FOUND CONNECTORS TO BE DAMAGED ON LIGHT ASSEMBLY. R EMOVED AND REPLACED LIGHT ASSEMBLY NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081114 NM 2008 11 14 NSVA2008041 1 20081108 A 3244 TIRE BOMBDR DHC8 DHC8402 1390042 NM NLG FAILED A NSVA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 EA 27 188WQ 4188 ON TAKE-OFF, LOUD POP / VIBRATION NOTICED ON NOSEGEAR AFTER V1, VIBRATION / NOISE CONTINUED, RETURNED TO BUF, NOSE GEAR TIRE BLOWN, DOOR DAMAGED. REMOVED AND REPLACED NOSE TIRES, AND REMOVED DAMAGED GEAR DOORS. ACFT WAS FERRIED TO ALB FOR FURTHER REPAIRS. 2 H 7 2 4T RT A13NM 20081117 NM 2008 11 17 SWAA086232 1 20081113 A 5320 BAC1508 FITTING BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 741SA 29277 DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, LBL 40. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086233 1 20081113 A 5320 6545833 WEB BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 741SA 29277 DURING SCHEDULED 10Y CHECK, FOUND COCKPIT FLOOR WEB CORRODED AT BETWEEN BS 249 TO BS 259, LBL 11 TO RBL 11. REPAIRED WE B PER SRM. 2 L 7 2 4F RT A16WE 20081117 EU 2008 11 17 UPS08153876 1 20081028 A 5321 B5327079800000 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 142UP 0825 INSPECTION TYPE:1C3C MAIN CARGO DECK FLOOR PANEL 242QM HAS FIELD REPAIRS. REPAIRED MAIN CARGO DECK FLOOR PANEL 242QM RE F A300-600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081117 EU 2008 11 17 UPS08153877 1 20081028 A 5321 B5327079800100 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 142UP 0825 INSPECTION TYPE:1C3C MAIN CARGO DECK FLOOR PANEL 241QM HAS FIELD REPAIRS. REPAIRED MAIN CARGO DECK FLOOR PANEL 241QM RE F A300-600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081118 NM 2008 11 18 2008UALA06420 1 20081107 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT PIT FRAME DENTED STA 1420, STR 25L TO 24L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALL ED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 08FDEA04780 1 20081107 A 5754 ARB75822 SKIN DOUG MD11 MD11F 3023600 NM NR 3 SLAT RT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 593FE 48551 RIGHT WING, NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUTOUT REPAIR DOUBLER INBOARD AND OUTBOARD SIDE LEADING EDGE SURFAC E FOUND CHAFING. CHAFE MARK SMOOTHED AS PER SRM 51-21-01, VOLUME II AND REPAIR CARRIED OUT AS PER EA 1-5740-122632. RE PAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. NR 3 SLAT ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-10-5 FOUND SATI SFACTORY. 2 L 7 3 4F RT A22WE 20081118 EA 2008 11 18 SWIA200820334 1 20080731 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 698BR 7799 C-CHECK, LEFT ENGINE THRUST FITTING CORRODED, REPLACED. 2 L 7 2 4F RT A21EA 20081118 EU 2008 11 18 08FDEA04735 1 20081105 A 5321 R532B373600000 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 FLOOR PANEL 231 QH IS CRACKED. FABRICATED NEW PANEL FROM STOCK MATERIAL, INSTALLED INSERTS, POTTED EDGES, APPLIED NONSK ID, PART ID MARKED, IAW SRZ 25-005 REV G. 2 L 7 2 4F RT A35EU 20081118 EA 2008 11 18 SWIA200820354 1 20081031 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 447SW 7677 FLT 3780 - CRACK IN RIGHT SIDE REINFORCEMENT ANGLE BETWEEN STR 9 AND STR 12. REPAIRED PER SB AND REO. 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 SWIA200820355 1 20081021 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 FLT 6559 - NR 2 CEILING EMERGENCY FLOODLIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081118 NM 2008 11 18 08FDEA04884 1 20081115 A 5320 6523638 STRAP BOEING 727 7272S2F 1384O81 NM FLOORBEAM CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 AREAS OF CORROSION ON FWD CARGO PIT UPPER FLOORBEAM STABILITY STRAP AS MARKED. REMOVED CORROSION FOUND OUT OF LIMITS RE F SRM 53-10-01. FABRICATED STRAP AND SPLICE PLATE REF DWG 65-23638 AND 66-14865. TREATED, PRIMED AND INSTALLED STABILI TY STRAP AND SPLICE BS 620-720C RBL 48 REF SRM 51-10-2 AND MM 51-20-151-7 AND 51-30-2. THIS IS CLASSIFIED AS A MINOR RE PAIR. 2 L 7 3 4F A3WE 20081118 EU 2008 11 18 08FDEA04871 1 20081113 A 5321 A30N40735039003 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 FWD CARGO PIT FLOOR PANEL NR 131QF IS DAMAGED FABRICATED NEW PANEL FWD CARGO PIT FLOOR PNL 131QF PER DWG SRZ 25-005 REV G AND AMM 20-31-00-0 PG 58. 2 L 7 2 4F RT A35EU 20081118 NM 2008 11 18 08FDEA04896 1 20081116 A 5330 65175301 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 213FE 22935 SKIN AT STA 1290 STR 20R HAS TOOLING MARKS, FASTENERS WITH IMPROPER ED AND THE SKIN IS BULGING. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-02. CUT-OUT DAMAGE PER B727 SRM 51-10-01, FABRICATED REPAIR DOUBLER IAW B727 SRM 53-30-3 & 53-30-2 FIG 3. FABRICATED TRIPLER IAW B727 SRM 53-30-3 & 53-30-2 FIG 3. TREATED AND PRIMED DOUBLERS IAW B727 SRM 51-10-2. I NSTALLED REPAIR DOUBLERS IAW B727 SRM 51-30-2 & 53-30-03 FIG 5. 2 L 7 3 4F A3WE 20081118 EU 2008 11 18 08FDEA04897 1 20081117 A 5321 B5323361300200 FLOOR PANEL AIRBUS 310 A310324 3930206 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 FLOOR PANEL 232 TG IS CRACKED. FABBED NEW FLOOR PANEL 232 TG USING THE OLD PANEL AS A TEMPLATE. POTED & CURED INSERTS; POTTED; CURED & SANDED THE EDGES. APPLIED NON-SKID TAPE & PART MARKED PANEL IAW FEDEX DWG SRX 25-005; REV "G". 2 L 7 2 4F RT A35EU 20081118 EA 2008 11 18 TRAX200801131 1 20080907 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 980EV PAX DOOR AFT WEB IS CRACKED IN ZONES 2,3. REMOVED CRACKED SUCTIONS OF AFT WEB PAX DOOR AND REPAIRED IAW REO. AREA REAU IRES SEALANT AND PAINT. SEALED AND CLEANED IAW REO 601R-52-11-702, REV A STEPS 11 AND 12. PAINTED IAW SRM 51-25-01. ( K) 2 L 7 2 4F RT A21EA 20081119 WP 2008 11 19 NWAA084579987 1 20081012 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1059 L18L CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 987US 47458 DURING OVERNIGHT CHECK FOUND CRACK IN AFT LT FUSELAGE SKIN AT BS 1059 ABOVE L18. REPAIRED PER EA 99-214064 SECT I. SEC TION II REQUIRES A BOEING DAMAGE TOLERANCE ANALYSIS AND INSPECTION NO LATER THAN 10/11/10. 2 L 7 2 4F A6WE 20081119 SO 2008 11 19 C2XA08IA221 1 20081006 A 3350 20131A BATTERY PACK EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 23139 2289 145731 IAH DURING MX INSPECTION THE EMERGENCY EXIT SIGN AT ROW 12 WAS FOUND TO BE INOP. MX R&R THE NR 4 BATTERY PACK. OPS CHE CKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081119 NE 2008 11 19 2008UALA06495 2 20081111 A 7321 CONTROL SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT EEC MALFUNCTIONED A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION IN INSP/MAINT 1 WP 29 651UA 25389 THE 'L ENG EEC MODE' EICAS MSG DISPLAYED. NOW OPERATING IN N1 MODE. REPLACED NR 1 EEC IAW MM 73- 21-04 FOR TS (L ENG E EC MODE) CAUTION MSG DISPLAYED ON UPPER EICAS. REPLACED LEFT DADC, LEFT ENG EEC CONTROL SWITCH, RAN BOTH ENGINES. COUL D NOT DUPLICATE PROBLEM OR GET ANY STATUS MESSAGES. 2 L 7 2 4F 4 F RT A1NM E24NE 20081119 EU 2008 11 19 2008UALA06497 1 20081111 A 5320 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 404UA 450 RT TRAY (AFT OF DOOR 2R) IS CRACKED AND MARKED. FABRICATED TRAY FROM 2024T3.063 THICK. INSTALLED TRAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081119 NM 2008 11 19 CALA0801068 1 20081111 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 BODY STATION 867 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8R AND STR 9R. BODY STATION 867 FRAME REPAIRED BETWEEN STR 8R AND STR 9R PER CO EA 5310-04498. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 CALA0801069 1 20081111 A 5311 6546596 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 BODY STATION 727B LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8L AND STR 9L. REPAIRED BOD Y STATION 727B FRAME AT AC RAIL BRACKET BETWEEN STR 8L AND STR 9L PER EA5310-04498. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 CALA0801074 1 20081113 A 5311 141A83716 FRAME BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34222 28931 R-1 DOOR STUB FRAME AT STATION 294.5 IS CRACKED JUST ABOVE CREASE BEAM WEB. REPAIRED CRACK PER ECRA 5311-01433. 2 L 7 2 4F RT A16WE 20081118 NM 2008 11 18 08FDEA04887 1 20081115 A 5320 65282885 SUPPORT BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FUSELAGE UPPER LOBE INTERIOR STRUCTURE CRACKED ON GILL LINER SUPPORT AT STA 1180, RBL 68, STRINGER R 11. REPLACED SUPPO RT STRUCTURE REF SRM 51-40-03 PG 1-5. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081118 NM 2008 11 18 2008UALA06428 1 20081108 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EELS INOP ROW 54 TO 60, LT & RT AISLES. REPLACED BATTERY PACK, OP CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081118 EU 2008 11 18 2008UALA06432 1 20081108 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 419UA 487 EMERGENCY EXIT LIGHTING INOP SEAT ROWS 12, 13 AND 14. BROKEN WIRE FOUND AT 13ABC. REPAIRED BROKEN WIRE. OP CHECKS GOO D. 2 L 7 2 4F 4 F RT A28NM E40NE 20081118 NM 2008 11 18 08FDEA04894 1 20081115 A 5744 ARC050214 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 600 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 593FE 48551 RIGHT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE) SIDE LOAD MOUNTING SURFACE FOUND CORRODED. CORROSION REMOVED ON SID E LOAD MOUNTING SURFACE AT RIGHT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) AND FOUND WITHIN LIMIT AS PER CMM 57-44-08 . EXISTING THICKNESS =0.422 INCH, REMAINING THICKNESS = 0.405 INCH, MATERIAL REMOVED = 0.017 INCH. SHIM MACHINED AND BONDED AS PER EA 1-5750-122635, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081118 NM 2008 11 18 2008UALA06445 1 20081109 A 5330 SKIN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 174UA 24381 FWD CARGO COMPT BILGE AREA SKIN HAS SMALL AREA OF CORROSION, BS 740 BETWEEN STR 44R - 45R. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED SKIN, INSTALLED SKIN DOUBLER. 2 L 7 4 4F 4 F RT A20WE E24NE 20081118 NM 2008 11 18 08FDEA04777 1 20081106 A 5315 FLOORBEAM BOEING 757 757236 1384971 NM BS 1681 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 FLOORBEAM CORRODED AT STA 1681 RBL 13. REPAIRED CORRODED FLOORBEAM AT STA 1681 RBL 13 IAW SRM 53-00-51. REPAIR NR 2, " A" MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED . 2 L 7 2 4F RT A2NM 20081118 NM 2008 11 18 2008UALA06450 1 20081109 A 3350 S1356B37 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 174UA 24381 UPPER DECK BS 900 LT, EMERGENCY EXIT LIGHT BATTERY PACK WEAK. REPLACED BATTERY PACK. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081118 NM 2008 11 18 2008UALA06453 1 20081109 A 5320 WEB BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 174UA 24381 CORROSION ON CANTED DECK SKIN BS 1265-1480, LBL 33.99-R BL 11.33. AFTER CORROSION REMOVAL FOUND EXCESSIVE MATERIAL LOSS AT BS 1265-1308 BL 0 TO LBL 33.99, AND BS 1377-1398 LBL 11.33 - LBL 33.99. MAJOR REPAIR ACCOMPLISHED. BS 1265-1308, C UT OUT DAMAGED WEB. SPLICED IN NEW WEB SECTION WITH LONG DOUBLER FROM BS 1265-1313, OUTBOARD OF LBL 11.33 AND TRANSVERS E DOUBLER AT BS 1310 BL 0- OUTBOARD OF LBL 11.33. FOR BS 1377-1398, CUT OUT DAMAGED WEB, SPLICED IN NEW WEB SECTION WITH 1 LONG DOUBLER INBOARD 094372 OF LBL 11.33 BEAM, 1 LONG DOUBLER INBOARD OF THE LBL 33.99 BEAM, 1 TRANSVERSE DOUBLER AT BS 137.5, AND 1 TRAN DOUBLER AT APPROX BS 1410. 2 L 7 4 4F 4 F RT A20WE E24NE 20081118 EU 2008 11 18 08FDEA04902 1 20081117 A 5320 YGF2557100002 GUIDE AIRBUS 300 A300F4605R 3930327 EU ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 667FE 771 COMPLY WITH EA NR 2550-116540, "EQUIPMENT/FURNISHINGS, MAIN DECK CARGO COMPARTMENT, CARGO SYSTEM, REMOVAL OF AFT "Y" G UIDES. COMPLIED WITH EA 6-2550-116540 "EQUIPMENT/FURNISHINGS, MAIN DECK CARGO COMPARTMENT, CARGO SYSTEM, REMOVAL OF "AF T" GUIDES. 2 L 7 2 4F RT A35EU 20081118 EU 2008 11 18 08FDEA04733 1 20081105 A 5321 R532B382900200 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 FLOOR PANEL 252 YG IS CRACKED. FABRICATED NEW PANEL FROM STOCK MATERIAL, INSTALLED INSERTS, POTTED EDGES, APPLIED NONSK ID, PART ID MARKED IAW FEDEX DWG SRZ 25-00-05 REV G. 2 L 7 2 4F RT A35EU 20081118 EA 2008 11 18 SWIA200820366 1 20081114 A 5610 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER TX TAXI/GRND HDL 1 NM 07 938SW 7741 FLT 5836 - CAPTAIN'S SIDE WINDOW CRACKED. REPLACED WINDOW. 2 L 7 2 4F RT A21EA 20081118 NM 2008 11 18 2008UALA06489 1 20081111 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 216UA 30549 SEAT 32E EEL LIGHT INOP. REPLACED LIGHT ASSY, OPS TEST GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081118 EA 2008 11 18 SWIA200820344 1 20080724 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 958SW 7833 C-CHECK, FS 280 RBL9 LOWER FLOOR SUPPORT CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 SWIA200820347 1 20081111 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE ACTIVATION A SWIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 07 909SW 7558 FLT 5808 - ABORTED TAKEOFF FOR "SMOKE TOILET" CAUTION MSG. RAN ENGINES AND APU BLEEDS, OPERATED PACKS AT FULL HOT, UNAB LE TO DUPLICATE. 2 L 7 2 4F RT A21EA 20081118 SO 2008 11 18 SWIA200820349 1 20081102 A 2710 AILERON EMB 120 EMB120 3260201 SO OBSTRUCTED A SWIA H DEACTIVATE SYST/CIRCUITS C S F F.O.D. AFFECT SYSTEMS FLT CONT AFFECTED AP APPROACH 1 NM 07 216SW 120285 FLT 5450 - ON APPROACH, AILERONS JAMMED. REMOVED DEBRIS BELOW TORQUE TUBE. 2 L 7 2 4T RT A31SO 20081118 WP 2008 11 18 08FDEA04788 1 20081107 A 5320 NJC6040 STIFFENER DOUG DC10 DC1030F 3023504 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 AFT FUSELAGE COMPT INTERNAL FOUND CRACK ON STIFFENER ABOVE. 2 L 7 3 4F RT A22WE 20081118 EU 2008 11 18 08FDEA04749 1 20081105 A 5321 R532B388100000 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 MAIN DECK FLOOR PANEL AT FRAME 75 TO FRAME 77, LBL 76 TO LBL 64 IS BROKEN. FABRICATED NEW PANEL FROM STOCK MATERIAL, IN STALLED INSERTS, POTTED EDGES, APPLIED NONSKID, PART ID MARKED IAW SRZ 25-005 REV G. 2 L 7 2 4F RT A35EU 20081118 NM 2008 11 18 08FDEA04792 1 20081107 A 5330 SKIN BOEING 727 727225 1384077 NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 469FE 21581 SKIN DENTED AT LAP SEAM STA 1115 STR 20R. EVALUATED DENT AND FOUND OUT OF LIMITS, REMOVED DAMAGED SKIN DIMS 3.3 INCH BY 1.8 INCH. FABRICATED FILLER 3.3 INCH BY 1.8 INCH, DOUBLER 12.250 INCH BY 8.5 INCH IAW SRM 53-30-3 FIG 24. INSTALLED REPAIR PARTS IAW SRM 53-30-3 FIG 24. 2 L 7 3 4F A3WE 20081119 SO 2008 11 19 C2XA08IA220 1 20081006 A 3350 20131A BATTERY PACK EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 23139 3174 145731 IAH DURING MX INSPECTION THE EMERGENCY EXIT SIGN AT ROW 12 WAS FOUND TO BE INOP. MX R&R THE NR 3 BATTERY PACK. OPS CHE CKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081119 NM 2008 11 19 CALA0801067 1 20081111 A 5311 6546558 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 BODY STATION 907 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8R AND STR 9R. BODY STATION 907 FRAME REPAIRED BETWEEN STR 8R AND STR 9R PER CO EA 5310-04498. 2 L 7 2 4F RT A16WE 20081119 2008 11 19 CALA0801084 4 20081114 A 2397 WIRE BOEING 767 767424ER 1385270 NM OXGEN MASK BROKEN A CALA G O2 MASK DEPLOYED O OTHER IN INSP/MAINT 1 SW 27 66056 12871 29451 DISCOVERED F/O OX2 MASK COMM WIRE BROKEN, UNABLE TO COMMUNICATE ON. REMOVED AND REPLACED A/C AEROSPACE MASK PER AMM 35- 11-51. OPS CHECK OK. P/N 174692N7 TK, ON-1187028, S/N OFF-12871. ROTABLE PARTS CHANGE WAS INDICATED - TT 1187028 S/N OFF 01287 MASK, OXYGEN, C OFF 64-3511-9-9001 2871, ON 64-3511-9-9001 2465. 2 L 7 2 4F RT A1NM 20081119 NM 2008 11 19 SWAA086120 1 20081108 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 921WN 36626 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086122 1 20081110 A 3350 PL2230LH0 STRIP BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 332SW 23696 FOUND EEPLS STRIP MISSING AT MID CABIN. INSTALLED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086103 1 20081109 A 3350 PL2230LH0 STRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 746SW 29798 FOUND EEPLS STRIP LOOSE BETWEEN ROW 9 ABC TO ROW 10 ABC. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086104 1 20081110 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 16R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086123 1 20081109 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 456WN 32463 FOUND FWD EGRESS LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086069 1 20081030 A 3350 81000 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 456WN 32463 FOUND EEPLS COVER LOOSE AT FWD ENTRY AREA. REMOVED AND REPLACED EEPLS PER MM. 2 L 7 2 4F RT A16WE 20081119 2008 11 19 SWAA086079 4 20081105 A 2565 5A33075 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 498WN 32480 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086084 1 20081109 A 5315 6546804 FLOORBEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM TEE CAP CORRODED AT BS 1006, LBL 9, WL 208. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081119 2008 11 19 SWAA086086 4 20081031 A 2565 D31354 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 795SW 30606 FOUND R2 DOOR EMERGENCY EXIT SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086087 1 20081102 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 797MX 27890 FOUND EEPLS COVER LOOSE AT ROW 1 TO ROW 2. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086244 1 20081113 A 5743 654654318 LUG BOEING 737 7373Q8 1384670 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED MV2 CHECK, FOUND RT MLG LOWER FITTING LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086246 1 20081113 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 748, STR 23L. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086281 1 20081114 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST AT ROW 16. REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086102 1 20081110 A 5711 6552235 SPAR BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND LT WING UPPER T/E SPAR CHORD CRACKED AT MLG BEAM TO SPAR FITTING. REPAIRED CHORD PER PAE ER. 2 L 7 2 4F RT A16WE 20081119 2008 11 19 SWAA086095 4 20081105 A 2565 63551101 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 FOUND R2 DOOR EMERGENCY EVAC SLIDE LOW PRESSURE. REMOVED AND REPLACED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086097 1 20081106 A 3350 417A5601 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 FOUND RT OVERWING EMERGENCY EXIT LIGHT COVER MISSING. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086254 1 20081113 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 926WN 36629 DURING SCHEDULED MV3 CHECK, FOUND EEPLS LIGHT END CAP MISSING. INSTALLED END CAP PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086255 1 20081117 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 867, STR 26R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086256 1 20081117 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 907, BETWEEN STR 9R TO STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086113 1 20081107 A 3350 8210248801 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 489WN 33855 FOUND LT OVERWING EEPLS LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081119 CE 2008 11 19 NWAA084589881 1 20081010 A 2913 FUSE BEECH 90 C90 1152913 CE PWA JT8 JT8D17A 52049 NE HYD PUMP FAILED A NWAA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 01 767MC LJ595 709387 AFTER THE ACFT WAS PUSHED BACK FOR DEPARTURE AND FOLLOWING ENGINE START, THE RT HYDRAULIC SYSTEM LOST ALL FLUID. COM PR OCEDURES WERE COMPLIED WITH AND THE ACFT RETURNED TO THE GATE. MX FOUND THE RT SIDE LOWER HYDRAULIC FUSE HAD FAILED. A HYDRAULIC SYSTEM RT SIDE RETURN LINE, THE FAILED FUSE, THE ELECTRICAL AUXILIARY HYDRAULIC PUMP, THE ENGINE DRIVEN HYDRA ULIC PUMP NR 2 ENGINE AND ALL APPLICABLE HYDRAULIC SYSTEM FILTERS WERE REPLACED. NO DEBRIS WAS FOUND IN ANY FILTER OR P UMP HOUSING. LEAK CHECK AND OPS CHECK WERE GOOD AND THE ACFT WAS RETURNED TO SERVICE. 1 L 7 2 3T 4 F 3A20 E2EA 20081119 NM 2008 11 19 SWAA086262 1 20081117 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED AT BS 667, BL 0. REPAIRED CHORD PER SI. 2 L 7 2 4F RT A16WE 20081119 EA 2008 11 19 ASOA200801506 1 20081114 A 5311 FRAME CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 860AS 7433 RT BS 210 FRAME CRACKED. REMOVE FRAME AND INSTALLED NEW FRAME P/N 600-34011-1 PER SRM 51-42-06. 2 L 7 2 4F RT A21EA 20081119 NM 2008 11 19 SWAA086263 1 20081117 A 5315 6545410 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED AT BS 665, BL 0. REPAIRED CHORD PER SI. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086272 1 20081117 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 465, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086273 1 20081117 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 349SW 24408 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 474, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081119 2008 11 19 SWAA086274 4 20081117 A 2565 63350 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 408WN 27895 R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081119 EA 2008 11 19 ASOA200801500 1 20081113 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 927EV 7844 LEFT FS 484 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED .1 INCH LONG AT LBL 27. REPLACED ANGLE AT LT FS 484 LBL 27 IAW REO 601R-53-411-059, STEPS 8-11 AND 14. COMPLIED WITH ASA EC/TC REO 601R-53-41-059. 2 L 7 2 4F RT A21EA 20081119 EA 2008 11 19 ASOA200801501 1 20081113 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 927EV 7844 FS 280 LBL 9 O/B CLIP CRACKED. THIS SDR WILL REMAIN OPEN PENDING MTC DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. 2 L 7 2 4F RT A21EA 20081119 EA 2008 11 19 ASOA200801503 1 20081113 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 927EV 7844 FS 280 RBL 9 I/B CLIP CRACKED. REMOVED AND REPLACED FS 280 RBL 9 INBOARD CLIP IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 20081119 WP 2008 11 19 AALA200810002 1 20081111 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70529 49921 LEFT CUSP CRACKED AT LIGHTING HOLES. CUSP AREA REPAIRED PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081119 WP 2008 11 19 AALA200810138 1 20081027 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 LEFT CUSP TORN AND CORRODED SEVERAL AREAS BETWEEN STATION 503 AND 518. INSTALLED REPAIR DOUBLER TO LEFT CUSP FROM STATI ON 503 TO 522 PER AMERICAN AIRLINES REPAIR DOCUMENT 53-20-00-16. MAJOR STRUCTURAL REPAIR NUMBER 016606. 2 L 7 2 4F A6WE 20081119 EU 2008 11 19 AALA200802694 1 20081008 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 25071 514 JFK - EMERGENCY DOWN SPOT LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER ONE DOOR EMERGENCY L IGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081118 NM 2008 11 18 2008UALA06504 1 20081113 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 SEAT ROW 19 ABC EMERGENCY LIGHT IS INOP. REPLACED LAMP, OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081118 NM 2008 11 18 2008UALA06506 1 20081113 A 2780 SWITCH BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE LE SLAT OUT OF LIMITS A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 676UA 30028 L/E SLAT ASYM. FOUND THE S284 SW FOR THE NR 3 INBOARD L/E SLAT OUT OF LIMITS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081118 NM 2008 11 18 2008UALA03130 1 20080601 A 5320 STRUCTURE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 907UA 25007 STR 10L STA 296 FOUND CRACKED DURING L1 DOOR. MAJOR REPAIR ACCOMPLISHED. REPAIRED PER UA-EVA-71626 AND REO-L01081. FI RST STAGE APPROVAL ONLY. NEW BOEING 8100-9 MUST BE RECEIVED ON OR BEFORE 31MAY2008 OR AIRCRAFT MUST BE REMOVED FROM SER VICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081118 NM 2008 11 18 2008UALA03131 1 20080601 A 5313 STRINGER SPLICE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 907UA 25007 LT AT FS 360 STRINGER 16L SPLICE CHANNEL CRACKED. MAJOR REPAIR ACCOMPLISHED. CF 9041 CAN BE CLEARED. EC 955313099SD & AMM 53-13-99 CREATED TO INSPECT REPAIR EVERY 6000 CYCLES. MONITORED BY EQ. OK TO CLEAR PER ABOVE INFO. 2 L 7 2 4F 4 F RT A16WE E21EU 20081118 EU 2008 11 18 2008UALA06472 1 20081111 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 404UA 450 DOOR 2R SILL PLATE HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REPLACED DOOR 2R SILL PLATE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081118 EA 2008 11 18 SWIA200820357 1 20080731 A 7120 BEARING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 917SW 7641 C-CHECK, RIGHT ENGINE FORWARD YOKE MOUNT LINK BEARING CORRODED. REPLACED. 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 SWIA200820361 1 20081105 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 452SW 7716 C-CHECK, RIGHT SIDE REINFORCEMENT ANGLE AT FS 640 CRACKED. REPAIRED PER SB 601R-53-061. 2 L 7 2 4F RT A21EA 20081118 NM 2008 11 18 08FDEA04885 1 20081115 A 5320 BAC1493577 SUPPORT BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FUSELAGE UPPER LOBE INTERIOR STRUCTURE FRAME SUPPORT CORROSION AT STA 600 - 620, RBL 47 UPPER AND LOWER SURFACE REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND NEW STRAP, TREATED AND PRIMED AND INSTALLED. CLASSIFIED AS A MINO R REPAIR. 2 L 7 3 4F A3WE 20081118 WP 2008 11 18 MU12008F00000 1 20081009 A 3246 WHEEL DOUG DC9 DC983 3022083 WP NLG VIBRATION B MU1Z C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 23 160BS 53463 REJECTED TAKE OFF. DURING TAKE OFF ROLL AFTER A/T ENGAGE AND TO POWER WAS ADJUSTED (EPR 2.04) REACHING 60 KTS THERE WAS A VERY STRONG VIBRATION, LOW SPEED REJECTED TAKE OFF WAS PERFORMED. DURING VIBRATION BRAKES DID NOT WORK UNTIL REACHIN G 30 TO 49 KTS. TOGW 132600 FLAPS. 6.2 ASSUMING 28` CELSIUS. IAW AMM 32-40-02 PAGE 204 RT AND LT NOSE WHEELS REPLACED , IAW 05-51-10 PAGE 601, MLG VIBRATION CHECK WAS PERFORMED. ALSO IAW AMM 32-42-01 PAGE 205. BLEED BRAKES PROCEDURES WE RE DONE. 2 L 7 2 4F RT A6WE 20081119 NM 2008 11 19 2008UALA06496 1 20081110 A 3020 ANTI-ICE VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 651UA 25389 THE L ENG ANTI-ICE VALVE HAS TO BE CYCLED EVERY TIME THE SWITCH IS TURNED OFF. 2 L 7 2 4F 4 F RT A1NM E24NE 20081119 NM 2008 11 19 CALA0801071 1 20081112 A 5311 6546549 FRAME BOEING 737 737524 1384721 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 62631 27535 FRAME CORRODED AT STATION 767 FROM S-27L TO S-26R. CUT OUT DAMAGED AREA AND INSTALLED SHEAR TIE REPAIR PER SRM 53-00-07 , REPAIR 10. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 CALA0801076 1 20081114 A 5311 6558280 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 BS 360 LEFT SIDE FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8L AND STR 9L. ACCOMPLISHED EA 5310-04 498 ON BS 360 LEFT FRAME AT STR 8L AND STR 9L. ACCOMPLISHED EC/RA 5310-04867 ON CLIP REPLACEMENT AT BS 360 AT STR 8L. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 CALA0801079 1 20081116 A 5320 141A541012 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 79279 31597 INTERCOSTAL BETWEEN STA 312 AND 328 AT LBL 45 IS CRACKED AT FASTENER HOLE. REMOVED DAMAGED INTERCOSTAL, INSTALLED NEW I NTERCOSTAL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086068 1 20081104 A 3350 3071BPEGL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 411WN 29821 DURING SCHEDULED MV3 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 13 SEAT D. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086073 1 20081104 A 5310 6547978 CREASE BEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 785SW 30602 DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM CHORD CORRODED AT BETWEEN BS 291 TO BS 328, RBL 54. REMOVED AND REPLACED B EAM PER SRM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086109 1 20081107 A 3397 81000 CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 417WN 29822 DURING SCHEDULED MV1 CHECK, FOUND EGRESS LIGHT INOP BETWEEN ROW 9 TO ROW 10. SECURED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086245 1 20081113 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 21R. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086101 1 20081028 A 5512 65C25727 SKIN BOEING 737 7373Q8 1384670 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED HC1 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT BS 161.9. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086257 1 20081117 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 747, BETWEEN STR 9R TO STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081114 EU 2008 11 14 NSVA2008042 1 20081111 A 2613 WARNING LIGHT SAAB SF340 340B 7860101 EU TAIL PIPE FALSE ACTIVATION A NSVA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 EA 27 9CJ 224 DURING TAKE-OFF ROLL LEFT ENGINE TAIL-PIPE HOT LIGHT ILLUMINATED AND SUBSEQUENTLY ABORTED TAKE-OFF. OPS CHECK IAW AMM 2 6-11-00-05, PROCEDURE 1, NO DEFECTS NOTED. 2 L 7 2 4T RT A52EU 20081114 EA 2008 11 14 QXEA2008111201173 1 20081106 A 5610 NP13932210 WINDOW CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 CRACKED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 19 611QX 10041 ONT- LARGE CRACKS IN THE FIRST OFFICER'S SIDE WINDOW. REPLACED R/H SIDE WINDOW IAW MM TASK 56-12-01-000-801-A01 TR 56-00 23 AND 56-12-01-400-801-A01 TR-0022, AND REMOVAL AND REPLACEMENT WITH NEW AS A PRECAUTIONARY MEASURE PER MTX CONTROL OF R/H SIDE WINDOW TEMP CONTROLLER IAW MM TASKS 30-41-06-000-801-A01 AND 30-41-06-400-801-A01. LEAK AND OP CHECK GOOD. RETU RNED TO SERVICE. 2 L 7 2 4F RT A21EA 20081114 NM 2008 11 14 2008UALA06413 1 20081106 A 2997 BMS1360T11C02G18 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYDRAULIC SYS FAULTY A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 543UA 25698 LT HYD QTY "LOW" PRESSURE DISPLAYED ON HYDRAULIC PAGE ALONG WITH OVERHEAD "RSVR" LIGHT ILLUMINATED. FOUND LEAKING CAP A T PRESSURIZATION MODULE. REPLACED CAP, LEAK CHECK GOOD WITH APU BLEED AND ENG BLEED. REPLACED LEFT SIDE HYDRAULIC RESE RVOIR. OPS OKAY. FOUND WIRE WITH HIGH RESISTANCE. REMOVED & REPLACED WIRE. WILL NEED TO PRESSURIZE RESERVOIR TO CONF IRM FIX. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 2008 11 14 2008UALA06378 4 20081105 A 2565 MECHANISM BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EVAC SLIDE MISINSTALLED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 667UA 29239 INADVERTANTLY BLOWN DURING INSTALLATION. CAUSE: IMPROPER INSTALLATION. RESET PACKBOARD RELEASE MECHANISM. 2 L 7 2 4F 4 F RT A1NM E24NE 20081114 NM 2008 11 14 2008UALA06382 1 20081105 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 595UA 28748 EEL STRIP INOP AT SEAT ROW 14ABC. REPLACED EEL SEGMENT, OPS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 EU 2008 11 14 2008UALA06405 1 20081106 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 426UA 510 DAMAGE FOUND AT FRAME 69 STRINGER 20 DIMENSION ARE D=.030 A=.500 B=.311 OF STRINGER 20. CREASE IS ON STRINGER. SIZE OF DENT IS 2 INCH BY 2 INCH BY .030 DEEP. THIS IS AFT OF DOOR 2LT. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER 20 NEAR FRAME 69. ACP HFEC INSP OF SKIN AND FASTENER HOLES AFTER OLD STRINGER WAS REMOVED. NO CRACKS FOUND. 2 L 7 2 4F 4 F RT A28NM E40NE 20081114 NM 2008 11 14 2008UALA06407 1 20081107 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 107UA 26900 EMERGENCY LIGHT INOP DOOR 2R AFT SILL. LIGHT IS INOPERABLE. REPLACED LAMP. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081114 SO 2008 11 14 C2XA08SH136 1 20081108 A 5312 14526850401 FIREWALL EMB 145 EMB145LR 3260212 SO APU CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14952 145067 DURING C-CHECK APU FIREWALL HAS CHAFING DAMAGE A 6 O`CLOCK POSITION. MX REPAIRED APU FIREWALL AT FR 81 IAW EC 5310-0135 9. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 20081114 SO 2008 11 14 C2XA08SH137 1 20081108 A 5347 14530637003 SUPPORT EMB 145 EMB145LR 3260212 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14952 145067 SHV - DURING C-CHECK LT UPPER SEAT TRACK SUPPORT HAS CORROSION AROUND RIVETS AT FR 45, 46 AND 50. MX REPAIRED LT UPPER SEAT TRACK SUPPORT AT FR 45, 46 AND 50 IAW EC 5320-01429. THE AIRCRAFT WAS APPROVED TO RETURN FOR MAINTENANCE. 2 L 7 2 4T RT T00011AT 20081114 NM 2008 11 14 08FDEA04822 1 20081109 A 5414 311N504633 SKIN BOEING 757 75723A 1384967 NM ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 NR 2 NACELLE STRUT INTERNAL, INBD SKIN EXFOLIATED AT PP STA 166 APPROXIMATELY AND HAS CORROSION FROM PP STA 174-100 AT A CCESS DOORS CUT-OUTS. REMOVED AND REPLACED WITH A NEW SKIN PANEL P/N 311N5046-33 "A" MAJOR REPAIR. NO FOLLOW-UP INSPE CTION REQUIRED. 2 L 7 2 4F RT A2NM 20081114 NM 2008 11 14 08FDEA04516 1 20081024 A 5753 ARC050213 BRACKET DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 LEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE BRACKET AFT LOWER ATTACH INBOARD HOLE FOUND WITH CORROSION. CORROSION A T LEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE AFT LOWER ATTACH INBOARD HOLE REWORKED AND CORROSION REMOVED AS PER EA N R 1-5750-122606. TITLE: WINGS, LEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE BRACKET (WING SIDE) CORROSION, REPAIR. RE PAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081114 NM 2008 11 14 08FDEA04517 1 20081024 A 5753 ARC050213 BRACKET DOUG MD11 MD11F 3023600 NM LT WING TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 578FE 48458 LEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE BRACKET AFT LOWER ATTACH OUTBOARD HOLE FOUND WITH CORROSION. CORROSION AT LEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE BRACKET AFT LOWER ATTACH OUTBOARD HOLE REWORKED AND CORROSION REMOVED A S PER EA NR 1-5750-122606. TITLE WINGS - LEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE BRACKET (WING SIDE) CORROSI ON, REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081114 WP 2008 11 14 08FDEA04535 1 20081024 A 5350 ALC7068502 FRAME DOUG MD10 MD1010F 3022112 WP TAIL CONE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 TAIL CONE RIGHT UPPER FRAME IS GOUGED, 3 PLACES. REMOVED RIGHT UPPER SUPPORT PER DC/MD-10 SRM 51-35-01; VOL II. FABRIC ATED, LOCATED AND DRILLED HOLES PER DAC DWG AKC7068; REV "T". INSTALLED SUPPORT PER DC/MD-10 SRM 51-33-01; VOL II AND DC/MD-10 SRM 51-35-01, VOL II. 2 L 7 3 4F RT A22WE 20081114 EU 2008 11 14 08FDEA04823 1 20081108 A 3230 DAMPENER AIRBUS 300 A300B4622R 3930312 EU UNKNOWN A FDEA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 CE 21 742FD 613 GEAR WOULD NOT RETRACT AFTER TAKEOFF. PERFORMED ECAM AND QRH DIRECTIVES. CHECKED THE MEMORY DISPLAY OF THE PSEU AND IT SHOWS FAULT CODE "BR". REMOVED AND REPLACED RT PITCH DAMPER. ATTEMPTED TO LUBE BOTH BOGIE BEAMS, NEITHER WOULD TAKE GREASE. THE BOGIE WILL NOT RETURN TO NEUTRAL WITH THE PITCH DAMPER SERVICED OR NOT, EVEN WITH IT REMOVED. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 08FDEA04825 1 20081109 A 5322 691487112 SHEAR TIE BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 LOWER FWD CARGO PIT, CORROSION ON FRAME SHEAR TIE, AFT SIDE OF STA 700, LBL 5 INCH. REPLACED SHEAR TIE IAW DRAWING 69-1 4871 AND SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081114 EU 2008 11 14 08FDEA04828 1 20081110 A 5311 A53970203 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS GOUGE ON FRAME 47, 3 INCHES BELOW STR 12L REPAIR COMPLIED WITH ON EA 6-5310-133939. 2 L 7 2 4F RT A35EU 20081114 SO 2008 11 14 C2XA08IA236 1 20081106 A 2120 151137 SLEEVE HAMLTN EMB 145 EMB145XR 3260214 SO A/C BAY BLOWN A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 12172 200404054 14500864 IAH - FLIGHT 2962, THE CREW REPORTED A BLEED 1 CLOSED EICAS MESSAGE FOLLOWED BY PACK 1 CLOSED EICAS MESSAGE APPEARING RE PEATEDLY, THE APU WAS USED FOR PRESSURIZATION, AND A CABIN HIGH ALT WARNING WAS RECEIVED. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED A SLEEVE ON THE NUMBER ON E ACM, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081114 NM 2008 11 14 K11A2008111272201 1 20080812 A 5311 FRAME BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 EVIDENCE OF CORROSION ON LOWER WEB OF SUB FLOOR FRAME ON AFT SIDE BETWEEN STRINGERS 26L AND 27L BY NOSE GEAR WELL BULKHE AD AT STA 304, LBL 16, WL 146. 2 L 7 3 4F RT A3WE 20081114 NM 2008 11 14 K11A2008110472201 1 20080908 A 5315 FLOORBEAM BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 722CK 20948 MAIN DECK, CORROSION ON BS 1110 FLOORBEAM UPPER CHORD AT RBL 62. CORROSION 2 X 1 INCHES. 2 L 7 3 4F RT A3WE 20081114 NM 2008 11 14 NOCA08208 1 20081104 A 2611 PU90499R3 SMOKE DETECTOR BOEING 767 76736N 1385152 NM LAVATORY DEFECTIVE A NOCA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 15 768NA 29898 SMOKE ALARM KEEPS GOING OFF IN LAV R4. REMOVED AND REPLACED LAV SMOKE DETECTOR AS PER MM 26-13-01, OPS CHECK OK. 2 L 7 2 4F RT A1NM 20081114 WP 2008 11 14 08FDEA04537 1 20081024 A 5311 ACA72306 FRAME DOUG MD10 MD1010F 3022112 WP ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 MAIN CARGO DOOR AREA AT STA 663.542, LONGERON 28, UPON SPOOL BACK UP FITTING REMOVAL, REPAIR BUSHINGS WERE FOUND IN FRAM E P/N ACA 7230-6 AND ANGLE P/N ACA 7230-8. REPAIRED FRAME, ANGLE AND SHEAR TIE IAW FEDEX EA 8-5310-123514 TITLE "FUSELA GE STA 663.542 MCD SILL REAME OVERSIZE HOLES - REPAIR". 2 L 7 3 4F RT A22WE 20081114 NM 2008 11 14 2008UALA06415 1 20081106 A 7931 21SN04459 PRESSURE SWITCH BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE LT ENGINE FAILED A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 798UA 26928 ENGINE OIL FILTER SENSOR L THE PRESSURE SWITCH FOR DETECTING IMPENDING OIL FILTER BYPASS ON THE LEFT ENGINE HAS FAILED. STATUS MSG-7960861 ACTIVE ERROR MODE MSG-7960861 ACTIVE ER MODE. ACPD LEFT ENG OIL TANK MASTER CHIP DETECTOR FOR CONTA MINATION. CHIP DETECTOR CONDITION CHECK OK. RECOMMEND REPLACE OIL FILTER DIFFERENTIAL PRESSURE SWITCH. REPLACED OIL F ILTER DIFF PRESSURE SWITCH. ACCOMPLISHED OIL FILTER PRESSURE SWITCH CHECK FOR NR 1 ENG DURING IDLE. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081114 NM 2008 11 14 2008UALA03168 1 20080603 A 2910 211C223211 RELAY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HYDRAULIC SYS FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 661UA 27158 RIGHT HYD INOP INDICATION. FLT DIVERTED. *S/D* REPLACED RELAY K127 IN P33 PER 29-00-03 AND CLEANED S32 AND S30 PRESSU RE SWITCHES AND PERFORMED ACMP AND EDP TESTS PER JRH 2-6-8. OPERATED DEMAND PUMP IN AUTO AND ON WHILE ENG RUN AND ALL L TS OPERATION NORMAL. DUE TO HISTORY OF FAULTY RIGHT HYD SYSTEM LOW PRESSURE WARNING REPLACED BOTH THE RIGHT ACMP CONTRO L PRESSURE SWITCH (S32) & PACKING, AND THE BRAKE ALTERNATE VALVE SELECT PRESSURE SWITCH (S415). 2 L 7 2 4F 4 F RT A1NM E24NE 20081114 NM 2008 11 14 2008UALA06412 1 20081106 A 2750 MODULE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE WING FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 671UA 30026 LEADING EDGE SLAT DISAGREE GOING FROM FLAPS 20 TO 25. REPLACED FLAP-SLAT SOV MODULE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081114 NM 2008 11 14 2008UALA06392 1 20081106 A 3350 FU305 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CHARGER FAULTY A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 DOOR 1 RIGHT BOTH SILL LIGHTS INOP AND OVER DOOR EXIT SIGN INOP. REPLACED FUSE IN CHARGER. CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081114 NM 2008 11 14 2008UALA06394 1 20081106 A 3397 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 ZONE-D RIGHT SIDE SEAT EMERGENCY LIGHTS INOP (SEATS 33 - 43). RESECURED EMERGENCY LIGHT CONNECTOR, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081114 NM 2008 11 14 2008UALA06414 1 20081106 A 2910 272W4592180 HYDRAULIC LINE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE RT MLG WW LEAKING A UALA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 29 798UA 26928 RT MLG WHEEL WELL HYD LEAK. FOUND TUBING THAT IS LEAKING. REMOVED LEAKING HYDRAULIC LINE FROM AIRCRAFT AND ROUTED TO T UBE SHOP FOR MANUFACTURING OF NEW LINE. NEW LINE WILL BE READY AROUND 2100. INSTALLED NEW DOOR LOCK LOWER HYD LINE FRO M ACTUATOR TO TEE FITTING. PRESSURE CHECKED, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081114 NM 2008 11 14 2008UALA06387 1 20081106 A 2120 FILTER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FWD CARGO BAY UNKNOWN A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 784UA 26951 ALL FLIGHT ATTENDANTS FROM BUS CLASS AFT REPORT STALE STUFFY AIR QUALITY. FLT CREW REPORTED MORE THAN 10 F/A'S FELL ILL WITH EFFECTS OF DIZZINESS AND LIGHTHEADED. ONE FLT CREW FELT SAME EFFECTS WHEN TRAVELING TO BACK OF CABIN. F/A'S FROM MID CABIN FELT ILL FIRST AND THEN AFT CABIN F/A'S. THEY ALL FELT BETTER AFTER USING PORTABLE O2. REPLACED 4 EA RECIRC FAN FILTERS IN FWD PIT. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081114 NM 2008 11 14 2008UALA06365 1 20081103 A 5720 287T1030124 STRUCTURE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RT WING DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 673UA 29241 DURING A CHECK, FOUND RIGHT WING RACEWAY INSTL WING T/E WIRE PROVISION CRACKED AT 2 PLACES. REPLACED WIRE BUNDLE RACEWA Y. 2 L 7 2 4F 4 F RT A1NM E24NE 20081114 NM 2008 11 14 2008UALA06395 1 20081106 A 2612 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE WARNING INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 583UA 26705 RT FIRE LIGHT DOES NOT ILLUMINATE DURING FIRE TEST. RELAMPED FIRE LIGHT. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 2008 11 14 2008UALA06402 4 20081106 A 2565 D31517109 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 433UA 589 EMERGENCY LIGHTS FAILS TEST. FAULTS EXT LOAD AFT L. REPLACED DOOR 2L SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081114 NE 2008 11 14 2008UALA06266 2 20081024 A 7261 1B30517913 SCAVENGE PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE LEAKING A UALA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 29 596UA 28749 726696 FOUND OIL LEAKED FROM LUBE SCAVENGE PUMP HOUSING ON NR 1 ENG. FOUND OIL LEAKING FROM PUMP. REPLACED LUBE-SCAVENGE PUMP . 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 NM 2008 11 14 2008UALA06267 1 20081023 A 5270 81020401 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 DOOR DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 518UA 24871 THE 3L DOOR, NO DOOR SLIDE LIGHT. CLEANED SENSOR. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 NM 2008 11 14 USAA920081801 1 20080919 A 5320 6517582 WEB BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 C18 CHECK - NR 6132033, CRACKED VERTICAL BEAM WEB, BS 180, LBL 5.7, WL 178. REPAIRED VERTICAL BEAM WEB, BS 180, LBL 5.7 , WL 178 IAW SRM 53-10-08-2R 12 FIG 201. (K) 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 USAA920081800 1 20081001 A 5330 SKIN BOEING 737 7373B7 138447F NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 530AU 24412 RON - NR 4370173, CRACKED FUSELAGE SKIN, BS929 - B931, S25R. REPAIRED FUSELAGE SKIN, BS 929-BS 931, S25R. REPAIRED FUSE LAGE SKIN, BS 929-BS 931, S25R IAW B737 SRM53-00-01, REPAIR 31. (K) 2 L 7 2 4F RT A16WE 20081114 2008 11 14 USAAEMB08021 4 20081113 A 2565 STITCHING EMB ERJ190 ERJ190100IGW 3260408 NM EVAC SLIDE LOOSE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 946UW 3768 19000072 ORF - MAINTENANCE FOUND THE FORWARD PASSENGER DOOR EVACUATION SLIDE LACING CORD UNRAVELED. MAINTENANCE - REMOVED AND RE PLACED THE SLIDE. 2 L 7 2 4F RT A57NM 20081114 NM 2008 11 14 USAA2008111392058 1 20081009 A 5320 65479573 WEB BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL - MAJOR REPAIR - C21 CHECK - CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL WEB, AT BS 794.3 - BS 847, S 25R. REPLACED AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL WEB, AT BS 794.3 - BS 847, S25R IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 USAA920081803 1 20080919 A 5320 65C3267723 WEB BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 C-18 CHECK - NR 6131686, CRACKED FLOOR WEB, BS 980, RBL 43. REPLACED FLOOR WEB, BS 980, RBL 43 IAW SRM 51-40-02AND DWG 65C32677. (K) 2 L 7 2 4F RT A16WE 20081114 EA 2008 11 14 MASA2008111200769 1 20081112 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 75987 7405 ASH FLT 7345 MHT-IAD. CAPT COULD NOT OPEN THE MAIN PASSENGER DOOR FROM THE OUTSIDE. MX COULD NOT DUPLICATE AND OPENED THE DOOR NORMALLY. 2 L 7 2 4F RT A21EA 20081114 EA 2008 11 14 MASA2008110800766 1 20081108 A 5610 601R3303310 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A MASA B EMER. DESCENT O OTHER CR CRUISE 1 SW 07 37178 13936 7178 ASH FLT 2716 PHX-FAT. FO'S WINDSHIELD CRACKED. CREW DECLARED EMERGENCY, LANDING WAS UNEVENTFUL AND PASSENGERS WERE NOT BRACED. MX REMOVED AND REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 20081117 SO 2008 11 17 C2XA08TY030A 1 20081111 A 3620 110415041 SENSOR EMB 145 EMB145XR 3260214 SO ZONE 500 DEFECTIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 18101 17210 17210 145590 FLT 2543 - DIVERTED TO TYS FROM ERW EN ROUTE TO MEM WHEN THE CREW RECEIVED A MESSAGE OF NR 1 ENGINE BLEED LEAK. MAINTEN ANCE REMOVED AND REPLACED THE OVER THE WING THERMAL SWITCH IAW EMB 145XR 36-20-02. OPS CHECK GOOD. ACFT RELEASED TO SE RVICE. 2 L 7 2 4F RT 20081117 SO 2008 11 17 C2XA08SH142 1 20081111 A 5320 14530642403 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14952 145067 SHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 34. MAINTENANCE REMOVED THE CORROSION A ND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-00-10 FIG 202, STEP 3. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . 2 L 7 2 4T RT T00011AT 20081117 SO 2008 11 17 C2XA08SH144 1 20081111 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14952 145067 SHV - DURING C-CHECK THE CARGO DOOR LOWER CUTOUT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AF FECTED SILL IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081117 SO 2008 11 17 C2XA08SH145 1 20081111 A 5544 12007254607 ATTACH BRACKET EMB 145 EMB145LR 3260212 SO RUDDER WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14952 145067 SHV - DURING C-CHECK THE RUDDER UPPER CENTER ATTACHMENT BRACKET WAS FOUND TO BE WORN AND THE HAT BUSHINGS MIGRATED. MAI NTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 55-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. 2 L 7 2 4T RT T00011AT 20081114 NM 2008 11 14 GTIA0800079 1 20081011 A 5320 D53472189202 FLOOR SUPPORT AIRBUS A319 A319132 3930340 NM ZONE 900 CORRODED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 507NK 2560 AFT GALLEY FLOORBEAM HAS CORROSION AT Y1292 BETWEEN FR 68 AND FR 69. 2 L 7 2 4F RT A28NM 20081114 NM 2008 11 14 SWAA086169 1 20081112 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 519SW 25318 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 762, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086161 1 20081112 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500C, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME PER SRM . 2 L 7 2 4F RT A16WE 20081114 EU 2008 11 14 08FDEA04731 1 20081105 A 5311 A53973018234 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS BENT FRAME 58 FROM STR 13L 4.5 INCH TOWARD STR 14L. REWORKED THE UPPER FLANGE SECTION IAW SRM 51-26 -00, PERFORMED HFEC INSPECTION IAW NTM 51-10-08 PT 6. NO CRACK INDICATION NOTED. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 08FDEA04693 1 20081104 A 5712 651727611 RIB BOEING 727 7272D4 138407U NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 LEFT WING OTBD L/E NR 4 SLAT S/N BN605, 2 CRACKED INTERNAL BRACKET TABS ON AFT WEB BELOW EACH SIDE OF ACTUATOR BOLT HEAD AND NUT. REPLACED 2 CRACKED RIBS REF SRM 51-30-02 PG 1-5. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081114 EU 2008 11 14 08FDEA04698 1 20081104 A 5311 A53773289202 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS 2 GOUGES ON FR 22, 1 IS 4.25 INCHES BELOW STR 13R AND 1 IS 2.75 INCH BELOW STR 14R. REMOVED AND REP LACED FRAME PROFILE BETWEEN STR 12R AND STR 15R IAW SRM 51-40-21. FABRICATED NEW SECTION ON TRAVELER T8/765537. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 08FDEA04701 1 20081104 A 5320 69154431 WEB BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 LT MLG WHEEL WELL AFT BULKHEAD BS 950 LBL 30, REINFORCEMENT WEB HAS LIGHT CORROSION. REMOVED CORROSION, ORIGINAL MATE RIAL THICKNESS .050 MATERIAL LOSS OF .020. REMAINING MATERIAL .030, FOUND OUT OF LIMITS REF SRM 53-10-1 PG 2. INSTALL ED NEW WEB P/N 69-15443-1 REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081114 WP 2008 11 14 08FDEA04709 1 20081104 A 5414 SKIN DOUG MD10 MD1010F 3022112 WP NACELLE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 46631 AFT NACELLE, FIREWALL SEAL PLANE AT FS Y2166 AND LEFT SIDE OF THE TRAILING EDGE OF THE DIVERTER, HAS WORN SKIN. 2 L 7 3 4F RT A22WE 20081114 2008 11 14 ASAA0853689 4 20081103 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM E&E BAY MALFUNCTIONED A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 579AS 6610 35187 FMC DISAGREE ON THE GROUND. RESET PER FMC DISAGREE CHECK LIST. UNABLE TO DUPLICATE PROBLEM. FMS OPS NORMAL REF MM 34 61 TASK 801. NOTE FMC 10.7 SOFTWARE INSTALLED. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 ASAA0853688 1 20081102 A 4990 38810521 INDICATOR BOEING 737 737890 1384527 NM APU OIL FILTER ACTIVATED A ASAA O OTHER J WARNING INDICATION IN INSP/MAINT 1 NM 02 579AS P7808 35187 RED BUTTON ON APU OIL FILTER INDICATOR HAS EXTENDED ACCOMPLISHED OIL FILTER INDICATOR SERVICING. REF AMM TASK 49 91 13 PB 301. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086196 1 20081112 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 394SW 27380 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081114 SO 2008 11 14 SIMA200831501 1 20081106 A 2560 FLASHLIGHT EMB 135 EMB135LR 3260305 SO CABIN ODOR A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 716AE 145264 ON FLIGHT 4728 CREW REPORTED THAT SHORTLY AFTER TAKE OFF CREW NOTICED STRONG ELECTRICAL SMELL ON FLIGHT DECK AND FLIGHT ATTENDANT SEAT. AFTER 30 SECONDS ODOR DISSIPATED BUT FLIGHT ATTENDANT NOTICED ODOR A FEW MIN LONGER. AFTER LANDING ALL O DORS WERE GONE. ACFT REMOVED FROM SERVICE, NO FAULTS FOUND THAT WOULD CAUSE THE ELECTRICAL ODOR. REMOVED AND REPLACED TH E FLASHLIGHT. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT T00011AT 20081114 SO 2008 11 14 RAIA2008111200002 1 20081109 A 2750 3631101005 SELECTOR EMB 145 EMB145EP 3260221 SO TE FLAPS MALFUNCTIONED A RAIA B EMER. DESCENT J WARNING INDICATION LD LANDING 1 CE 03 808HK 2382 145157 DURING LANDING PHASE OF THE FLIGHT, THE CREW RECEIVED A FLAP FAIL MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION SELECTOR LEVER AND PERFORMED AN OPERATIONAL CHECK OF THE FLAP SYSTEM WITH NO DEFECTS NOTED. 2 L 7 2 4F RT T00011AT 20081114 SO 2008 11 14 RAIA2008111300001 1 20081111 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT LOOSE A RAIA O OTHER L NO TEST TX TAXI/GRND HDL 1 CE 03 847HK 14500857 DURING PRE-FLIGHT INSPECTION, THE GALLEY WALL EMERGENCY EXIT LOCATOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE RESE CURED THE CONNECTOR TO THE LIGHT ASSEMBLY. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081114 NM 2008 11 14 2008UALA06384 1 20081105 A 3350 20131A362624 BATTERY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 513UA 24810 EMERGENCY EEL LIGHT STRIP SECTION INOP AFT OF ROW 27. REPLACED BATTERY PACK AND ONE EEL LIGHT STRIP. OP CKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 NM 2008 11 14 08FDEA04794 1 20081108 A 5320 65294586 PAN BOEING 727 7272D4 138407U NM BS 1183 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 PASSENGER CABIN, BULKHEAD 1183 DITCH PAN, LBL 28 CRACKED REPLACED DITCHING PAN 1183 BLKHD LBL 28 REF BOEING DWG 65-29567 AND SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NE 2008 11 14 08FDEA04795 2 20081108 A 7200 ENGINE DOUG MD10 MD1030F 3024020 NM GE CF6 CF650C2 30018 NE MALFUNCTIONED A FDEA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 CE 21 304FE 64399 46992 517630 AT 2 00 INTO FLIGHT GOT EGT FLUCTUATING UP TO 1065 DEGREES CELSIUS TO VALUE S AT OR BELOW NORMAL. RETARDED THROTTLE TO IDLE AND RAN CHECKLIST EGT STILL FLUCTUATING WILDLY SO WE PERFORMED ENG SHUTDOWN. NO OTHER INDICATIONS OF SEVERE DAMAGE , BUT WITH EGT STILL CYCLING ABOVE RED LINE WE TREATED IT AS SEVERE DAMAGE AND RAN THAT CHECKLIST AS WELL, TO INCLUDE FI RING FIRE BOTTLE. AFTER 1 MINUTE, STILL SHOWED HI EGT, SO FIRED 2ND BOTTLE AND DIVERTED TO KFLL. SHORTLY AFTER FIRING 2ND BOTTLE EGT SETTLED DOWN TO 25C, IN WORK. 2 L 7 3 4F 4 F RT A22WE E23EA 20081114 NM 2008 11 14 08FDEA04796 1 20081108 A 5330 65253372 SKIN BOEING 727 7272S2F 1384O81 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 LOWER FUSELAGE SKIN, STA 720A, STR 18R, LIGHTNING STRIKE IN SKIN REPAIRED LIGHTING STRIKE IN SKIN STA 720A STR 18R IN AC CORDANCE WITH SRM 53-30-3 FIG 3 REPAIR CLASSIFIED A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04797 1 20081108 A 5322 69436685 SHEAR TIE BOEING 727 7272S2F 1384O81 NM ZONE 100 MISINSTALLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 216FE 22937 SHEAR TIE AT STA 720A, STR 18 R HAS NO EDGE MARGIN AT FASTENER HOLE REPLACED SHEAR TIE AT STA 720 STR 18R IN ACCORDANCE WITH SRM 51-30-02 AND DRAWING 69-43668. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04802 1 20081108 A 5330 6554581 SKIN BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 LOWER AFT CARGO AREA, CORROSION ON SKIN AT STA 950E TO 950F AT LEFT KEEL BEAM. REMOVED CORROSION AND FOUND OUT OF LIMIT S. REMOVED FLOOR SUPPORTS, REMOVED, DRILLED, COUNTERSUNK, AND TRIMMED DOUBLER, TREATED AND PRIMED DOUBLER AND SKIN, INST ALLED DOUDLER, INSTALLED FLOOR SUPPORTS REF SRM 53-10-1 AND 51-30-2, 53-30-2, 53-30-1. THIS IS CLASSIFIED AS A MAJOR REP AIR 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04803 1 20081108 A 5315 53FX14971 FLOORBEAM BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 UPPER LOBE INTERIOR STATION 776 LBL 2 INCH FLOORBOARD ATTACH ANGLE CRACKED. REPAIRED ATTACH ANGLE REF SRM 51-40-03 FIG 1 PG 1-6. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04804 1 20081108 A 5312 6557172 BULKHEAD BOEING 727 7272S2F 1384O81 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 FWD CARGO PIT, AFT BULKHEAD LWR BEAM PRESSURE PANEL IS CORRODED APPROXIMATELY 6 INCHES LBL ON UNDER SIDE, AND IN SEVERAL OTHER AREAS OF LWR BEAM AROUND NUTPLATE HOLES. REMOVED CORROSION ON LOWER BEAM FOR BULKHEAD PRESSURE PANELS ON AFT B ULKHEAD IN FWD CARGO PIT LBL 6 AND SEVERAL OTHER AREAS, LEFT SEGMENT AREA 1" X 1.75" X .029 REMAINING MATERIAL .035, R IGHT SEGMENT AREA 1" X 1" X .019 REMAING MATERIAL .045 ORIGINAL THICKNESS .064, BOTH AREAS FOUND OUT OF LIMITS IAW SRM 53-10- 1. REPLACED LOWER BEAM IAW DRAWING 65-57172 AND SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04805 1 20081108 A 5320 65295489 ANGLE BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 DITCHING PAN AFT ANGLE AT STA 1183 RBL 53 IS CRACKED. REMOVED DAMAGED ANGLE, FABRICATED HEAT TREATED NEW ANGLE. INSTAL LED AND SEALED NEW ANGLE CLASSIFIED AS A MINOR REPAIR, REF DWG 65-29567, SRM 51-40-02. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04807 1 20081108 A 5315 655756717 FLOORBEAM BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 AFT PIT FLOOR SUPPORT CORRODED ON UNDERSIDE AROUND NUTPLATE STA 1166 LBL 11-12. SPLICED IN NEW SUPPORT SECTION REF SRM 53-10-5 AND 51-30-2. CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04812 1 20081108 A 5315 652083938 FLOORBEAM BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 STA 1148 FLOORBEAM UPPER FLANGE CORRODED RBL 45-45 AFT SIDE AND 44-47 FWD SIDE WL 208. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04814 1 20081108 A 5414 311N504634 SKIN BOEING 757 75723A 1384967 NM NR 1 PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 NR 1 STRUT CORROSION ON INNER AFT SKIN INBD SIDE. REMOVED AND REPLACED INBD SIDE SKIN PANEL ASS'Y IAW DRAWING N311N5002 AND SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081114 NM 2008 11 14 08FDEA04815 1 20081109 A 5315 6558352274 FLOORBEAM BOEING 727 7272D4 138407U NM BS 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 LOWER FWD CARGO PIT, CORROSION ON UNDERSIDE AT NUTPLATES OF FLOOR SUPPORT STRINGER STA 700 15 INCH, RBL 2.5. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04817 1 20081109 A 5712 640834219 RIB BOEING 727 7272D4 138407U NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 RT WING L/E RIB UPPER CHORD HAS SEVERAL CRACKS ALONG EXISTING REPAIRS AT 9 INCHES-20 INCHES FROM SPAR, FSS 122. REMOVED REPAIR, FABRICATED REPAIR DOUBLER REF SRM 51-40-3 FIG 1. INSTALLED RT WING LF RIB CHORD REPAIR REF SRM 51-40-3 FIG 1. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04820 1 20081109 A 5414 311N504632 SKIN BOEING 757 75723A 1384967 NM NR 2 PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 NR 2 NACELLE STRUT, OTBD INTERNAL SKIN HAVE CORRODED SPOTS ALONG PYLON. REMOVED AND REPLACED NEW SKIN P/N 311N5446-32 "A" MAJOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED. 2 L 7 2 4F RT A2NM 20081114 2008 11 14 2008UALA06363 4 20081104 A 2565 D31591478 BOTTLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU EVAC SLIDE LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 381UA 24656 LOW BOTTLE. RUPTURE DISK HAS SLOW LEAK. REMOVED & REPLACED RUPTURE DISK. 2 L 7 2 4F 4 F RT A16WE E21EU 20081114 NM 2008 11 14 USAA920081806 1 20080918 A 5320 654580728 ANGLE BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 C-18 CHECK - NR 6131764, CRACKED ANGLE, BS 290, S13R. REPLACED ANGLE, BS 290, S13R IAW SRM 51-40-02. (K) 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 KCSA081578 1 20081113 A 5210 DOOR FRAME BOEING 747 747212B 1384886 NM R5 DOOR DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 R5 MAIN ENTRY DOOR INTERIOR FRAME DAMAGED AT BOTTOM CENTER OF DOOR BS 2260. 2 L 7 4 4F RT A20WE 20081117 NM 2008 11 17 KCSA081581 1 20081114 A 5313 ANGLE BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 LEFT OVERWING LONGERON L-ANGLE CORRODED AT STA 1255 LBL 130. 2 L 7 4 4F RT A20WE 20081117 NM 2008 11 17 SWAA086206 1 20081113 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081117 2008 11 17 SWAA086210 4 20081112 A 2565 6557463 MOUNT BRACKET BOEING 737 7373H4 1384600 NM R2 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 326SW 23690 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR SLIDE AFT MOUNTING BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086237 1 20081113 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 30544 DURING SCHEDULED HC1 CHECK, LT BATTERY PACK FAILED CAPACITY TEST AT ROW 16. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081117 2008 11 17 SWAA086240 4 20081113 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 30544 DURING SCHEDULED HC1 CHECK, R1 DOOR SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081117 EU 2008 11 17 UPS08153913 1 20081111 A 2820 ISOLATION VALVE AIRBUS A300 A300F4622R 3930360 EU FUEL SYSTEM UNKNOWN A IPXA K NONE J WARNING INDICATION CL CLIMB 1 SO 01 143UP 0826 INSPECTION TYPE:N/A ATB - ON CLIMBOUT, SINGLE CHIME YELLOW CAUTION LIGHT. ECAM SHOWED TRIM TANK SYSTEM FAULT COULD NOT REMOVE TRIM TANK FUEL. RETURNED TO SDF. CAN NOT DUPLICATE, SYS CKS NORMAL. REPLACED TRIM TANK ISOLATION VALVE ACT 48QB AND RELAY 54QB FOR PRECAUTIONARY AMM 28-22-55-04. CKS NORMAL AMM 31-46-00-05. PLACARDS REMOVED. 2 L 7 2 4F RT A35EU 20081117 WP 2008 11 17 IXX2008F00107 1 20080730 A 5347 S2772660 SEAT TRACK DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK INSPECTION, FOUND P-1-5 SEAT TRACK DAMAGED. REMOVED DAMAGED TRACK SEGMENT. FABRICATED SPLICES. CLEANED, TREATED, AND PRIMED AREA AND SPLICES. INSTALLED NEW TRACK SEGMENT AND SPLICES IAW SRM 53-7-1, FIG 4, SHEET 1 ITEM C, SRM 51-2-0, FIG 50 SHEET 73. (K) 2 L 7 4 4F RT 4A25 20081118 EU 2008 11 18 08FDEA04874 1 20081113 A 5553 A55371296208 FITTING AIRBUS 310 A310222 3930315 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 453FE 267 VERTICAL STABILIZER ATTACH FITTING AT RIB 13 HAS CORROSION. 2 L 7 2 4F RT A35EU 20081114 EA 2008 11 14 SWIA200820331 1 20081107 A 3320 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A SWIA K NONE O OTHER CR CRUISE 1 NM 07 406SW 7030 FLT 4797 - AT FL340, HAD A STRONG ODOR OF BURNING NYLON. REPLACED GALLEY LIGHT ASSEMBLY. 2 L 7 2 4F RT A21EA 20081114 NM 2008 11 14 CALA0801054 1 20081110 A 5311 65C33509 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 BODY STATION 400 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR-8R AND STR-9R. REPAIRED CRACK BETWEEN S-8R AND S-9R AT BODY STATION 400 FRAME PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081114 EA 2008 11 14 SWIA200820322 1 20081018 A 3230 CONTROL PANEL CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 418SW 7446 FLT 4128 - GEAR WOULD NOT COME UP AFTER TAKEOFF. REPLACED GEAR LEVER PANEL ASSEMBLY. 2 L 7 2 4F RT A21EA 20081114 SO 2008 11 14 SWIA200820321 1 20081109 A 6120 PCU EMB 120 EMB120ER 3260203 SO LT PROPELLER MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 07 578SW 120346 FLT 5603 - EEC IN MANUAL, LEFT NP FLUCTUATES BETWEEN 101.6 AND 96.9 WITH CLIMB TORQUE AND PROPS MAX. REPLACED LEFT ENGI NE PCU. 2 L 7 2 4T RT A31SO 20081114 NM 2008 11 14 08FDEA04690 1 20081103 A 5347 SEAT TRACK BOEING 757 757236 1384971 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 MAIN CABIN FLOOR STA 640 RBL 45 SEAT TRACK CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52 REPAIR NR 1. THIS REPAIR IS CATEGORY "A" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20090121 NM 2009 1 21 ASAA0853730 1 20081108 A 3040 141A481024 WINDOW BOEING 737 737890 1384527 NM FLT DECK OVERHEATED A ASAA O OTHER J WARNING INDICATION CR CRUISE 1 NM 02 558AS 9819 35177 45 MINUTES INTO FLIGHT AT FL 35 000. LT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. QRH PROCEDURES WERE ACCOMPLISHED AND LIG HT REMAINS ON WHEN SWITCH WAS TURNED BACK ON. GROUNDED YES. R&R THE LT SLIDING WINDOW PER MM 56 12 11. OPS CHECKS OK. REMOVED C/N 6608314 PLACARD. SEAMC TIM NOTIFIED. GROUND VERIFICATION SUCCESSFUL. 2 L 7 2 4F RT A16WE 20081114 EU 2008 11 14 08FDEA04741 1 20081105 A 5311 A53770545 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS GOUGE ON FRAME 28, 2.5 INCH ABOVE STR 21L. REPAIR COMPLIED WITH ON EA 6-5310-123938. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 2008UALA06372 1 20081104 A 3350 1158291 SIGN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN UNSECURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 534UA 25129 EMERGENCY EXIT SIGN AT LT OVERWING EXIT FELL OFF. SECURED SIGN. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 NM 2008 11 14 2008UALA06373 1 20081104 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 528UA 25018 FLIGHT ATTENDANT REPORT EEL TRACK COVER BROKE. FOUND EEL LIGHT OUT BETWEEN ROW 14ABC TO 20ABC. REPLACED MISSING EEL SE GMENT AND SECURED LOOSE CONNECTORS. REPLACED BROKEN COVER. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 NM 2008 11 14 SWAA086178 1 20081112 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, STR 25L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086264 1 20081117 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND KEEL BEAM CORRODED BETWEEN BS 663 TO BS 727. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 AALA200802695 1 20081008 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 643AA 24601 DFW - EMERGENCY SEAT MOUNTED LIGHTS AND EDIT MARKER LIGHTS ARE DIM FROM SEAT ROW 26 TO AFT OF CABIN. REPLACED BATTERY P ACK FOR DIM EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081119 WP 2008 11 19 AALA200802699 1 20081008 A 2560 STRAP DOUG DC9 DC983 3022083 WP FLASHLIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 593AA 53256 LGA - EMERGENCY FLASHLIGHT AT AFT JUMPSEAT HAS TWO STRAPS MISSING. REPLACED TWO STRAPS FOR EMERGENCY FLASHLIGHT AT AFT JUMPSEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081119 NM 2008 11 19 AALA200802702 1 20081008 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 664AA 25298 DFW - EMERGENCY LIGHTS IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT STATION 1665 FOR INOPERATIVE EMERGENCY LIGHTS IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081119 NM 2008 11 19 AALA200802704 1 20081008 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 664AA 25298 DFW - EMERGENCY LIGHT AT LEFT FORWARD OVERHEAD EXIT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT FORWARD OVER HEAD EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081119 WP 2008 11 19 AALA200810140 1 20081027 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 UNDERSIDE OF LEFT CUSP CORRODED AT STATION 695 - 699. INSTALLED DOUBLER PER AMERICAN AIRLINES REPAIR DOCUMENT 53-20-00- 16. 2 L 7 2 4F A6WE 20081119 WP 2008 11 19 AALA200810142 1 20081027 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 LEFT CUSP GOUGED AT STATION 387. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081119 WP 2008 11 19 AALA200810012 1 20081009 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 RIGHT CUSP WEB CRACKED AT STATION 788. INSTALLED CUSP REPAIR PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081119 NM 2008 11 19 AALA200820005 1 20081008 A 5320 DOUBLER BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 670AA 52802 25335 REPAIR DOUBLER FOUND CORRORED, INSTALLED NEW DOUBLER ALUM 2024-T3 PER SRM 53-60-51-2R. 2 L 7 2 4F RT A2NM 20081119 EA 2008 11 19 CHQA200800219 1 20081107 A 3620 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE BLEED AIR SYS MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 639BR 7313 GEE872507 FLIGHT 5710, ATL TO CLE, DURING CLIMB THE FLIGHT CREW RECEIVED A 14TH STAGE DUCT MESSAGE. THE QRH WAS FOLLOWED BUT THE MESSAGE REMAINED. THE AIRCRAFT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE SYSTEM PER CRJ FIM 3 6-10-00 AND RAN THE ENGINES WITH THE CREW WITH NO FURTHER DEFECTS NOTED. 2 L 7 2 4F 4 F RT A21EA E15NE 20081120 EU 2008 11 20 08FDEA04863 1 20081111 A 2701 MO46Z1402 SENSOR AIRBUS 310 A310324 3930206 EU ZONE 300 FAILED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 21 815FD 638 DURING T/O ROLL RECEIVED ECAM WARNING OF PITCH TRIM NOT IN T/O RANGE, REJECTED T/O. AFTER CONFIRMING PITCH TRIM PROPER LY SET (VIA PERFORMING COMPUTER NUMBERS) TESTED T/O CONFIG TEST AND STILL RECEIVED SAME WARNING ON ECAM. PITCH TRIM SH OWS IN GREEN BAND ON TROM WHEEL BUT OUT OF GREEN RANGE ON ECAM FLT CONTROL PAGE. REMOVED AND REPLACED THS POSITION SENS OR 11CT IAW A310-300 MM 27-45-11-4 AND MM 27-45-00-5, OPS CKS NORMAL. PERFORMED THS TAKEOFF WARNING TEST IAW A310-300 M M 27-00-00, OPS CKS NORMAL. A/C OK FOR SERVICE. CREATED OIL TO RECHECK 11CT SENSOR AT NEXT 'A' CK. WITH TEST SET 31- 590-100 (NOT AVAIL IND). 2 L 7 2 4F RT A35EU 20081120 EU 2008 11 20 F3LA2008111800716 1 20081117 A 5210 D5211009820000 HOOK AIRBUS A318 A318111 3940019 EU ZONE 800 WORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 801FR 1939 DURING C4 C-CHECK, INSPECTION NOTED THAT DURING INSTALLATION OF THE ESCAPE SLIDE THE L2 DOOR HANDLE WAS ABLE TO MOVE INT O THE CLOSED POSITION BEFORE THE DOOR WAS CLOSED. MAINTENANCE REMOVED AND REPLACED THE DOOR HOOK IN ACCORDANCE WITH AMM 52-13-21-420-052. 2 L 7 2 4F RT 20081120 EU 2008 11 20 F3LA2008111800717 1 20081118 A 3350 321430 BATTERY AIRBUS A318 A318111 3940019 EU EMERGENCY LIGHTS FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 801FR 1939 DURING C4 C-CHECK, INSPECTION NOTED THAT THE EMERGENCY LIGHT TEST THROUGH THE CENTRALIZED FAULT DISPLAY UNIT FAILED OPER ATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT BATTERY IN ACCORDANCE WITH AMM 33-51-38 -000-001. 2 L 7 2 4F RT 20081120 WP 2008 11 20 IXXA08SMN157S 1 20080418 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN CRACKED AT STATION XFS 335.000 - XFS 3 41.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08244 DATED 05/08/08, SEMAN DRAWING NUMBER ED-4767 DATED 04/25/08, SRM 51-1-21, 51-1-20D, NDT SPM PART 06-10-01-001, SRM 51-1-8B, SRM 51-1-11, 51-3-0, AND 51-3-1. 2 L 7 4 4F RT 4A25 20081120 NM 2008 11 20 DHLA2008745689 1 20081114 A 5320 STRUCTURE BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LWR FUSE, NLG W/WELL HORIZONTAL WALKWAY LOWER LT CHORD CORRODED BETWEEN BS 294.5 AND 348.2. REMOVED, FABRICATED NEW CHO RD MEMBER PER BAC DWG 65-18415 REV U DATED 12/15/77, BAC DWG 65-18420 REV M DATED 10/22/81, AND ASTAR EC-01167-001, AND INSTALLED PER SRM 51-30-2 AND BAC 5300-1. 2 L 7 3 4F A3WE 20081120 EA 2008 11 20 SWIA200820377 1 20080805 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 771SK 10244 C-CHECK, COCKPIT FLOOR SUPPORT CRACKED AT FS 280. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081120 WP 2008 11 20 IXXA08SMN172S 1 20080419 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP LOWER SKIN CRACKED BETWEEN STATION XF 375.000 - 404.000. RE MOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN FABRICATED NEW SKIN, DOUBLER. BONDED PARTS AS NEEDED . CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW 57-7-1 FIGURE 4 TR 5 7-94 DATED 10-01-2002, SRM 57-1-0 PAGE 1, SRM 51-1-21, SRM 57-7-1 FIGURE 4 TR 57-94 ITEM "U" AND "Q", SRM 51-1-9 TR 51-1 42, SRM 51-1-9A TR 51-141, SRM 51-1-8B, AND SRM 51-1-11. 2 L 7 4 4F RT 4A25 20081120 EA 2008 11 20 CHQA200800222 1 20081114 A 3250 16735109 RVDT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NLG STEERING OUT OF ADJUST A CHQA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 11 645BR 7383 GEE872681 FLIGHT 5531, SDF TO IAH - DURING CRUISE, THE FLIGHT CREW RECEIVED A STEERING INOP CAUTION MESSAGE ON EICAS. THE CREW FO LLOWED THE QRH CHECKLISTS BUT THE MESSAGE REMAINED. THE AIRCRAFT LANDED AT SDF WITHOUT INCIDENT AND WAS TOWED TO THE GA TE. DURING TROUBLESHOOTING MAINTENANCE SLAVED IN A TILLER, ECU AND SERVO ALL NO FIX. THE PSEU FAULT CODES POINTED TO R VDT FAILURES, AND BOTH RVDT'S WERE ADJUSTED AND THE STEERING SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 20081119 SO 2008 11 19 C2XA08IA223 1 20081006 A 3200 UNKNOWN EMB 145 EMB145EP 3260221 SO MLG UNKNOWN A C2XA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 27 14933 145018 IAH FLIGHT 3123 THE CREW REPORTED A LOUD THUMPING NOISE 3 OR 4 TIMES AFTER GEAR RETRACTION. THE ACFT RETURNED TO IAH WH ERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT, OPS CHECKED THE LANDING GEAR EXTENSION AND RETRACTION MULTIPLE T IMES WITH NO DEFECTS NOTED AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20081119 NM 2008 11 19 KCSA081544 1 20081023 A 5347 SEAT TRACK BOEING 747 747249F 1384849 NM BS 1035 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 MAIN DECK SEAT TRACK CORRODED AT BS 1035, RBL 98.58. 2 L 7 4 4F RT A20WE 20081119 NM 2008 11 19 SWAA086072 1 20081104 A 5754 65C26686 SKIN BOEING 737 7373Q8 1384670 NM LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED SPV CHECK, FOUND NR 3 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086085 1 20081110 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 20Y CHECK, FOUND RT FWD CARGO KEEL BEAM CORRODED AT BS 524. REPAIRED KEEL BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086112 1 20081107 A 3350 8210248801 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 489WN 33855 FOUND RT OVERWING EEPLS LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086096 1 20081106 A 3350 417A5601 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 FOUND LT OVERWING EMERGENCY EXIT LIGHT COVER MISSING. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 KCSA081542A 1 20081023 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 960 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 BS 960 FUSELAGE FRAME CRACKED AT STR 39L 2 L 7 4 4F RT A20WE 20081119 2008 11 19 SWAA086265 4 20081117 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 495WN 33869 FOUND R1 DOOR SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. INSTALLED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086269 1 20081115 A 3350 411A2212 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 FOUND FWD ENTRY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086114 1 20081107 A 5330 6585988 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 524SW 26566 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086115 1 20081108 A 3350 PL2230LH0 STRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 FOUND EEPLS STRIP LOOSE BETWEEN ROW 6 TO ROW 7. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086280 1 20081114 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 DURING SCHEDULED HC1 CHECK, RT OVERWING EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081119 WP 2008 11 19 AALA200810007 1 20081014 A 5320 MEMBRANE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 585AA 53248 SUB FLOOR HAS 1 INCH AREA OF CORROSION AT G1 GALLEY STATION 154 TO 160. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER P ER ESO 80559 DATED 10-13-2008 AND AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081119 NM 2008 11 19 AALA200810004 1 20081002 A 5315 FLOORBEAM BOEING 737 737823 13844BZ NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION AND TOOLING MARKS TOP OF 328 BEAM. REPAIRED FLOORBEAM PER ESO 61000 DATED 10-02-2008. 2 L 7 2 4F RT A16WE 20081119 WP 2008 11 19 AALA200802707 1 20081009 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 963TW 53613 LGA - EXTERIOR EMERGENCY LIGHTS AT OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR INOPERATIVE EXTERIOR EMERGENCY LIGHT S. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081119 WP 2008 11 19 AALA200810143 1 20081028 A 5310 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 SEVERAL AREAS OF CORROSION ON HORIZONTAL AND VERTICAL LEGS OF AFT CARGO DOOR BEAM STATION 1156 TO 1212. REMOVED CORROSI ON, TREATED AND PRIMED. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3. 2 L 7 2 4F A6WE 20081120 EA 2008 11 20 SWIA200820378 1 20081113 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 959SW 7840 FLT 6484 - CEILING LEVEL EMERGENCY FLOODLIGHT OVER ROW 2 INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081120 EA 2008 11 20 SWIA200820379 1 20081113 A 3350 SWITCH CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS MALFUNCTIONED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 495CA 7774 FLT 2674 - EMERGENCY LIGHTS ON WITH FIGHT DECK SWITCH ARMED AND FA SWITCH OFF. CYCLED COCKPIT EMERGENCY LIGHT SWITCH. 2 L 7 2 4F RT A21EA 20081120 EA 2008 11 20 SWIA200820380 1 20081111 A 3350 INVERTER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS SHORTED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 FLT 6656 - LAST TEN FEET OF EMERGENCY FLOOR LIGHTING INOP. REPLACED NR 4 INVERTER. 2 L 7 2 4F RT A21EA 20081120 SO 2008 11 20 SWIA200820381 1 20081110 A 3397 RELAY EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS FAULTY A SWIA O OTHER O OTHER AP APPROACH 1 NM 07 560SW 120334 FLT 7811 - EMERGENCY LIGHTS CAME ON JUST BEFORE THE LANDING CHECK AND STAYED ON UNTIL TURNING OFF RUNWAY. REPLACED RELA Y K0201. 2 L 7 2 4T RT A31SO 20081120 SO 2008 11 20 LR7A08123 1 20081107 A 5330 SKIN LKHEED 382 382G 526414U SO FS 1039 DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 405LC 5025 DURING CARGO OFF LOAD, SKIN AT FS 1039, WL265, BL 9LT TO BL 9RT WAS DAMAGED. REPAIRED SKIN IAW LAC MEA 382-53-08-060 AN D DRAWING NR R08-033-01. 2 H 7 4 4T A1SO 20081120 SO 2008 11 20 CHQA200800220 1 20081109 A 7500 8166248 THERMOSTAT EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL BLEED SYSTEM FAULTY A CHQA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 11 573RP 10879 10879 145837 CAE312348 FLIGHT 6006, CVG TO MKE, DURING CLIMB IN ICING CONDITIONS THE FLIGHT CREW RECEIVED AN E1 BLEED OVERTEMP WARNING ON EICAS . THE QRH WAS FOLLOWED AND THE AIRCRAFT RETURNED TO CVG AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 FAN AIR VALVE FILTER AND THE NR 1 FAN AIR THERMOSTAT AND THE BLEED SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081120 EA 2008 11 20 QXEA2008111401184 1 20081110 A 3230 533407 SELECTOR VALVE CNDAIR CL600 CL6002C10 1390015 EA MLG MALFUNCTIONED A QXEA O OTHER E VIBRATION/BUFFET CR CRUISE 1 NM 19 604QX 13392 10019 PDX - WHILE CRUISING AT FL360, FELT A VIBRATION UNDER THE CREW'S FEET (LIKE A MOTOR RUNNING) FOR ABOUT 5 SECONDS FOLLOWE D BY A "CLUNK". SIMULTANEOUSLY RECEIVED A "PROX SYS FAULT" STATUS MESSAGE AND GEAR UP INDICATION FOR APPROXIMATELY 5 SE CONDS AND 30 SECONDS RESPECTIVELY. SPEED WAS 260 KIAS (M .77). REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW AM M TASKS 32-32-10-000-801-A01 AND 32-32-10-400-801-A01. LANDING GEAR EXT/RETRACT SYSTEM OPS CK GOOD. VALVE LEAK CHECK G OOD. NO STATUS MSG NOTED, PROX SYS FAULT. RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 20081120 NM 2008 11 20 08FDEA04922 1 20081119 A 5347 SEAT TRACK BOEING 727 7272S2F 1384O81 NM BS 1148-1176 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 SEAT TRACK CORRODED, MAIN DECK AT RBL 24 BS 1148 TO 1176. 2 L 7 3 4F A3WE 20081120 NM 2008 11 20 08FDEA04923 1 20081119 A 5320 6518636323 STIFFENER BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 LT MLG WHEEL WELL APU AIR INLET MOUNT FLANGES CORRODED REMOVED CORROSION REF SRM 51-10-1 ORIGINAL THICKNESS .150', REMOV ED .018', REMAINING THICKNESS, .132' OUT OF LIMITS REF SRM 53-10-1 FIG 1. REPLACED 323 STIFFENER REF DWG 65-18636, AND SRM 51-30-2 PG 1-10. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081120 NM 2008 11 20 08FDEA04924 1 20081119 A 5320 65C1612933 CHANNEL BOEING 727 7272D4 138407U NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 RADAR R/T SHELF, RT SIDE HAT CANNEL ON UPPER SIDE OF SHELF IS CRACKED. REPLACED RT SIDE HAT CHANNEL ON RADAR R/T SHELF IN ACCORDANCE WITH BOEING DRAWING 65C16129 AND SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR 2 L 7 3 4F A3WE 20081120 WP 2008 11 20 IXXA08SMN165S 1 20080419 A 5340 FITTING DOUG DC8 DC871F 302199D WP ZONE 200 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT UPPER SURFACE OF CUSP EXTRUSION AFT FITTING CRACKED AT STATION 702.875 LO NGERON 19 RIGHT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION F OUND. CLEANED TREATED AND PRIMED FITTING AND AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, REPAIR SPECIFICATION NUMBER 2003-05 DRAWING 3779874, DPS 4.707, SRM 51-1-8B, AND 51-3-1. 2 L 7 4 4F RT 4A25 20081120 2008 11 20 DL76G081483 4 20081031 A 2330 PS45222252 ELECTRICAL BOX BOEING 767 7673P6 1385105 NM 2 A/ 2B OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 155DL 25269 DUE TO FUMES THE IFE SYSTEM WAS SHUTDOWN. REMOVED AND REPLACED DC SEB P/N RD-FA 3124-07. REMOVED AND REPLACED SPM P/N RD-FA 3621-01 AND R SAC CONTROL BOX P/N PS4-52222-52. ALL IFE AND SEAT FUNCTION OPS NORMAL AT 5 A/B. 2 L 7 2 4F RT A1NM 20081120 NM 2008 11 20 DL757081485 1 20081104 A 5410 STRUT BOEING 757 757232 1384965 NM NR 2 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 DURING THE PYLON MOD, THE NR 2 PYLON LT SIDE STRUT WAS FOUND WITH SEVEN OVERSIZE HOLES. SIX OF THE HOLES WERE CLEANED U P FOR OVERSIZE FASTENERS AND ONE HOLE WAS BUSHED TO THE ORIGINAL HOLE SIZE PER BOEING INSTRUCTIONS. 2 L 7 2 4F RT A2NM 20081120 NM 2008 11 20 DL757081486 1 20081104 A 5320 146N545120 WEB BOEING 757 757232 1384965 NM BS 1520-1540 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 WEB AT STATION 1520 -1540 RBL 12 CORRODED. REPAIRED ON NR 00040 PER 51-30-01 STEP 8 AND 51-40-02 FIG 1. 2 L 7 2 4F RT A2NM 20081114 2008 11 14 UHLA2008110700004 4 20081015 A 3497 CONNECTOR EMB ERJ170 ERJ170100SE 3260406 NM TAT PROBE BURNED A UHLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 855RW 160 17000077 FLIGHT 7624 ORD TO HPN CREW RECEIVED EICAS MESSAGES "AOA FAIL" AND "TAT1 FAIL AND REPORTED A STRANGE ODOR BUT NOTED NO S MOKE OR NOXIOUS VAPORS WERE PRESENT IN THE COCKPIT. CREW DECLARED AN EMERGENCY AND DIVERTED INTO CLE. MAINTENANCE REPLAC ED NR 2 TAT PROBE CONNECTOR AND THE NR 4 ADSP. 2 L 7 2 4F RT A56NM 20081114 NM 2008 11 14 UHLA2008110700001 1 20081028 A 2780 SLAT SYSTEM EMB ERJ170 ERJ170100SE 3260406 NM MALFUNCTIONED A UHLA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 865RW 17000122 FLIGHT 5986 ATL TO DCA ON APPROACH FLAPS WERE SELECTED TO "1" AND CREW RECEIVED A "SLAT FAIL" AND "SHAKER ANTICIPATED" E ICAS MESSAGES. CREW FOLLOWING THE QRH; SLATS REMAINED AT 0 BUT FLAPS COULD BE EXTENDED TO 2. EMERGENCY WAS DECLARED AND LANDING UNEVENTFUL. MAINTENANCE CLEARED INHIBITS AND RESET SYSTEM; OPS CHECK GOOD. THIS DISCREPANCY HAS NOT REPEATED. 2 L 7 2 4F RT A56NM 20081114 NM 2008 11 14 SWAA086193 1 20081112 A 5753 6573732 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 SWAA086195 1 20081112 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 392SW 27379 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081114 NM 2008 11 14 R61A20080033 1 20081106 A 3246 WHEEL EMB ERJ170 ERJ170200LR 3260121 NM NLG VIBRATION A R61A O OTHER O OTHER LD LANDING 1 GL 11 124HQ 17000200 CREW REPORTED VIA ACARS AFTER TAKE OFF THE CREW HAD A NOSE WHEEL VIABRATION AND A BURNING ODOR IN COCKPIT. CREW HAD TOWE R VIRIFY NOSE GEAR HAD BOTH NOSE WHEELS INDY TOWER DECLARED A EMERGENCY AFTER A GO AROUND CRE LANDED ACFT WITHOUT INCIDE NT AND PROCEEDED TO THE GATE. MAINTENANCE WAS DISPATCHED TO AIRCRAFT INSPECTED NOSE WHEEL TIRES SEEN WEAR AND REMOVED AN D REPLACED BOTH NOSE WHEEL ASSEMBLIES. ACFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A56NM 20081114 SW 2008 11 14 QMLA1101200808049 1 20081101 A 5302 206020110103 STINGER BELL 407 407 1182206 SW TAILBOOM BENT E QMLA O OTHER O OTHER LD LANDING 1 NM 03 409UH 53422 WHILE IN A STABILIZED HOVER, ABOVE THE HOSPITAL LANDING PAD, THE PILOT REACHED UP TO SWITCH TO A DIFFERENT RADIO AND THE AIRCRAFT PITCHED TAIL DOWN AND THE TAIL STINGER IMPACTED THE CONCRETE PAD. THE PILOT LANDED THE AIRCRAFT AND CONDUCTED A NORMAL SHUTDOWN. THE PILOT IMMEDIATELY CALLED DISPATCH, TOOK THE AIRCRAFT OUT OF SERVICE, AND CALLED MAINTENANCE AND REQUESTED AN INSPECTION. MAINTENANCE INSPECTED THE AIRCRAFT AND RETURNED IT TO SERVICE. THE PILOT FLEW THE AIRCRAFT B ACK TO THE HANGER AT KSLC AT THE END OF THE PILOTS SHIFT [ON THE FIRST OF NOVEMBER] AND FLEW IT TO AND FROM TIMPANOGOS [ OREM BASE] THE NEXT DAY [NOVEMBER SECOND]. MAINTENANCE DETERMINED [ON NOVEMBER THIRD] THAT THE TAIL STINGER APPEARED TO 1 G 7 1 3U O H2SW 20081114 EU 2008 11 14 QMLA1110200808052 1 20081110 A 2435 150SG122Q STARTER GEN SNIAS 350 AS350B2 8680813 EU FAILED E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 124LN 510 248 4130 DURING FLIGHT THE CREW SMELLED SMOKE WITH THE ILLUMINATION OF GEN LIGHT, FUEL P LIGHT AND WITH A DROP OF FUEL PRESSURE T O 0 BARS. PILOT MADE PRECAUTIONARY LANDING. MECHANIC WAS NOTIFIED. STARTER GENERATOR WAS REPLACED AND ACFT WAS RETURNED TO SERVICE. 1 G 7 1 3U H9EU 20081114 EU 2008 11 14 2008UALA06406 1 20081107 A 5320 BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 404UA 450 BEAM 200 HAS CORROSION AT FRAME 67. MAJOR REPAIR ACCOMPLISHED. REMOVED BEAM. REMOVED BRACKETS AND TRANSFER DRILLED ON TO NEW BEAM. CONNECTED BEAM 200 TO BEAM 205. READY TO INSTALL IN ACFT. INSTALLED BEAM 200 TO ACFT. 2 L 7 2 4F 4 F RT A28NM E40NE 20081114 WP 2008 11 14 08FDEA04841 1 20081111 A 5720 ARB11646 INTERCOSTAL DOUG DC10 DC1030F 3023504 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 RT WING FOUND CRACK ON INTERCOSTAL. 2 L 7 3 4F RT A22WE 20081114 EU 2008 11 14 08FDEA04844 1 20081111 A 5347 A53812944000 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK SEAT TRACK RBL 58 HAS CORROSION 7 INCH FWD OF FRAME 49. REMOVED AND REPLACED SEAT TRACK FROM FR 45 TO F R 54 IAW SRM 51-40-21- AND 51-40-44. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 08FDEA04859 1 20081112 A 5330 651842018 SKIN BOEING 727 727225 1384077 NM BS 251 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 469FE 21581 SKIN AT STA 251 STR 20R HAS NUMEROUS TOOL MARKS. REMOVED PREVIOUS DOUBLER REPAIR. FABRICATED NEW DOUBLER REPAIR USING 2024-T3 .050 PO NR 9007753 DIMS 13 1/2 INCH BY 13 5/8 INCH. INSTALLED DOUBLER REPAIR IAW SRM 53-30-3. 2 L 7 3 4F A3WE 20081114 NM 2008 11 14 08FDEA04763 1 20081105 A 5311 FRAME BOEING 757 75723A 1384967 NM ZONE 200 DAMAGED A FDEA O OTHER O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 AFTER REMOVAL OF DOUBLER FROM TV MONITOR SUPPORT AT BS 1000, FOUND SEVERAL HOLES IN FRAME. REMOVED DAMAGED SECTION OF F RAME, FABBED REPAIR PARTS AND INSTALLED REPAIR PARTS, BS 1000, S-5L - S-5R, IAW SRM 53-00-07, REPAIR NR 3. THIS REPAIR IS CLASSIFIED AS A CAT "B" MAJOR REPAIR WITH THE FOLLOWING FOLLOW UP TRACKING: INITIAL INSPECTION 12,000 FC; THEREAFTER EVERY 12,000 FC AS AN ALTERNATIVE, DO AN DVI INSPECTION EVERY 9,000 FC. 2 L 7 2 4F RT A2NM 20081114 WP 2008 11 14 08FDEA04768 1 20081015 A 5420 AJC72868 ANGLE DOUG MD10 MD1010F 3022112 WP ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 RT SIDE OF NR 2 ENG INLET STRUCTURE APPROX STA YID 328.413 UPPER FRAME CAP HAS CORROSION AND NUTPLATES CORRODED, APPROX MIDWAY BETWEEN FRONT CENTER SPAR AND REAR CENTER SPAR BENEATH PANEL NR 364JR. REMOVED CORRODED CAP ANGLE PER SRM 51-31- 01 VOL II. CAP ANGLE CORROSION FOUND TO BE OUT OF LIMITS. TOTAL MATERIAL LOSS, IAW MD/DC 10 SRM 54-00-01 VOL I. FORME D AND FABRICATED NEW CAP ANGLE P/N AJC7286-8 PER DAC DWG AJC7286 REV F. INSTALLED NEW CAP ANGLE PER DAC DWG AJC7286 REV F AND MD/DC 10-10 SRM 51-35-01 PG 5 VOL II. 2 L 7 3 4F RT A22WE 20081114 EU 2008 11 14 08FDEA04769 1 20081106 A 5311 B53770316200 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS DAMAGE ON FRAME 24 TRUSS SPLICE BETWEEN STR 8R AND STR 9R. REMOVED DAMAGED SPLICE IAW SRM 51-40-21A ND REWORKED IAW SRM 51-26- 00, PERFORMED NDT CRACK TEST IAW NTM 51-10-08 PT 6. NO CRACK INDICATION NOTED, TREATED AND PRIMED IAW SRM 51-21-10. INSTALLED SPLICE IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 08FDEA04846 1 20081111 A 5320 655612950 INTERCOSTAL BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 LOWER AFT CARGO AREA CORROSION ON INTERCOSTAL AT STA 950E 3 RBL 12. REMOVED INTERCOSTAL, REMOVED CORROSION, ORIGINAL "T " .040, REMOVED .010, REMAINING .030, FOUND TO BE OUT OF LIMITS. FABRICATED NEW DOUBLER FOR INTERCOSTAL, INSTALLED NEW INTERCOSTAL AND DOUBLER REF SRM 51-10-2 PG 2, SRM 51-30-2 PG 1-4, SRM 53-10-1 FIG 1, BOEING DWR 69-47773 ID 001 FRAM E 1. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081114 EU 2008 11 14 08FDEA04856 1 20081111 A 5320 R538D104820200 ADAPTER AIRBUS 310 A310203 3930313 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 427FE 362 MDCC CLS ADAPTER AT FRAME 46 BETWEEN SEAT TRACK 2 RT AND 3 RT HAS 1 CRACK 3 INCHES LONG. REMOVED AND REPLACED 1 CLS ADA PTER AT FR 46 BETWEEN SEAT TRACK 2 RT AND 3 RT IAW A310-200 SRM 51-40-21. 2 L 7 2 4F RT A35EU 20081114 NM 2008 11 14 2008UALA06393 1 20081106 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 181UA 25278 DOOR 4 RIGHT AFT SILL LIGHT INOP. RELAMPED, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081114 NM 2008 11 14 2008UALA06364 1 20081103 A 3350 78941 LAMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 777UA 26916 EMERGENCY ESCAPE PATH LIGHTS AT SEAT 1F AFT AND 3E FWD ARE INOP OR MISSING. REPLACED EMERGENCY LIGHT ASSY. OPS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081114 NM 2008 11 14 USAA2008111492059 1 20081014 A 5320 6517684107 WEB BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL - MAJOR REPAIR - C21 CHECK - NR# 6136447, CRACKED WEB AT BS 303.9, S16L. REPLACED WEB AT BS 303.9, S16L I/A/W US A IRWAYS TASK CARD M1C53001. 2 L 7 2 4F RT A16WE 20081114 EA 2008 11 14 MASA2008111100768 1 20081111 A 3350 1317 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 518LR 10259 ASH FLT 7178 CLT-IAD. AFT CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. MX RELAMPED THE LIGHT OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081117 NM 2008 11 17 KCSA081579 1 20081113 A 5320 FITTING BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 BS 2360 LOWER FWD BATHTUB FITTING CORRODED AT STR 22L. 2 L 7 4 4F RT A20WE 20081117 NM 2008 11 17 SWAA086236 1 20081113 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 30544 DURING SCHEDULED HC1 CHECK, RT OVERWING EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081117 WP 2008 11 17 UPS08853870 1 20081013 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE:SV REPAIR AT STA BS 8 L32R L33.5R HAS ONLY 2 ROWS OF RIVETS SRM CALLS FOR 3. REPAIRED AS IAW 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 20081117 NM 2008 11 17 SWAA086241 1 20081113 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, BETWEEN STR 9R TO STR 8R. REPAIRED FRAME PER SWA EA . 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086242 1 20081113 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, BETWEEN STR 9R TO STR 8R. REPAIRED FRAME PER SWA EA . 2 L 7 2 4F RT A16WE 20081117 EU 2008 11 17 UPS08153887 1 20081110 A 3350 BATTERY AIRBUS A300 A300F4622R 3930360 EU COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 122UP 0807 INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT TEST. REPLACED EMERGENCY LIGHT BATTERY PER 33-51-0, OPS CHECKS OK. 2 L 7 2 4F RT A35EU 20081117 NM 2008 11 17 ASAA0853707 1 20081106 A 4920 CH31769 IGNITER BOEING 737 737890 1384527 NM APU FAILED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 579AS 35187 APU WON'T START. FAULT LIGHT ILLUMINATES. APU HAS HISTORY OF NO STARTS. ADDED 1 QT OIL, CLEARED FAULT. REMOVED AND R EPLACED APU IGNITER PLUG AND LEAD REF MM 49 41 52, APU OPS CHECKED GOOD 4 STARTS. APU HAS HISTORY OF NO STARTS. PRIORIT Y 1. REMOVED AND REPLACED APU IGNITER PLUG AND LEAD REF 49 41 52 APU OPS CHECK GOOD 4 STARTS. PARTS VERIFIED PER JERRY S EAMC. TSR CLEARED 2 L 7 2 4F RT A16WE 20081118 WP 2008 11 18 08FDEA04876 1 20081114 A 5347 6045067075T651 SEAT TRACK DOUG MD10 MD1010F 3022112 WP ZONE 200 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 68050 47804 MAIN CARGO DECK SEAT TRACK AT STA 879 TO 919 LBL 107 HAS SEVERAL FASTENER HOLES DAMAGED ON THE OTBD LOWER LEG FROM PREVI OUS REWORK. REMOVED AND REPLACED SEAT TRACK, FAB NEW SEAT TRACK SECTION AND SPLICES IAW SRM 51-31-01, 53-70-00 FIG 1 SH EET 1 AND MAE TRAVELER T8/767563 AND T8/767564. MAJOR REPAIR RII. 2 L 7 3 4F RT A22WE 20081118 NM 2008 11 18 2008UALA06424 1 20081107 A 2560 CIRCUIT BREAKER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY ESCAPE BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 551UA 25399 CIRCUIT BREAKER P6C5 "EMER ESCAPE SYS" IS BROKEN. REPLACED P6 C5 CIRCUIT BREAKER FOR EMERGENCY ESCAPE SYSTEM. CONTINUI TY CHECKS GOOD. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 2008UALA06434 1 20081108 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 796UA 26931 AFT EEL STRIP MISSING AT SEAT 3F. REPLACED EEL ASSY AND CHECKED OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081118 NM 2008 11 18 2008UALA06436 1 20081109 A 5514 STRUCTURE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE HORIZ STAB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 174UA 24381 RT HORIZONTAL STABILIZER AFT UPPER CHORD, STA 2590, RBL 43.5 A FASTENER HOLE WAS FOUND DAMAGED DURING COA 850111. OVER- SIZED HOLE TO APPROX 0.469 INCHES & INSTALLED BOLT WITH NUT. 2 L 7 4 4F 4 F RT A20WE E24NE 20081120 NM 2008 11 20 DL757081487 1 20081104 A 5340 141N516010 MOUNT BOEING 757 757232 1384965 NM G1 GALLEY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 G1 GALLEY LEFT GALLEY MOUNT PAD CORRODED. REPAIRED PER 51-40-02 BY REPLACEMENT ON NR 00079. 2 L 7 2 4F RT A2NM 20081120 NM 2008 11 20 DL757081488 1 20081104 A 5340 415N40015 MOUNT BOEING 757 757232 1384965 NM G1 GALLEY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 G1 GALLEY MOUNT LEFT FORWARD CORRODED. REPIARED BY REPLACEMENT PER 51-40-02 ON NR 00078. 2 L 7 2 4F RT A2NM 20081120 NM 2008 11 20 DL757081490 1 20081104 A 5320 146N545121 WEB BOEING 757 757232 1384965 NM BS 1500-1520 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 AFT CARGO BAY WEB AT STATION 1500- 1520 RBL 3 CORRODED. REPAIRED ON NR 00039 PER 51-20-01. 2 L 7 2 4F RT A2NM 20081120 NM 2008 11 20 DL757081491 1 20081104 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM FS 620 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 617DL 22907 DENT OUT OF ALLOWABLES SKIN. CUTOUT THE DENT AND INSTALL SINGLE REPAIR DOUBLER FOR BOTH DAMAGE AREAS. 2 L 7 2 4F RT A2NM 20081120 NM 2008 11 20 DHLA2008745673 1 20081110 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 CABIN FRAME HAS HOLES ON INBD FLANGE THAT ARE WITHIN THE MINIMUM ED OF THE RADIUS AND FLANGE EDGE AT BS 848.95, BETWEEN STR 16L AND 17L. REPAIRED FRAME INBD CHORD PER EO COO-2-53-292-08 DATED 10/14/08, BAC MSG 1-980377061-3 DATED 10/18/08, BAC MSG 1-980377061-9 DATED 10/13/08, AND EVA B253-00129. REPAIR AUTHORIZED BY FAA FORM 8100-9 DATED 11/4/2008. REF N /R 2-110. 2 L 7 3 4F A3WE 20081120 NM 2008 11 20 DHLA2008745674 1 20081110 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 CABIN FRAME HAS DOUBLE DRILLED HOLES ON INBD FLANGE AT BS 783.95, BETWEEN STR 16R AND 17R. REPAIRED FRAME INBD CHORD PE R EO COO-2-53-292-08 DATED 10/14/08, BAC MSG 1-980377061-3 DATED 10/18/08, BAC MSG 1-980377061-9 DATED 10/13/08, AND EVA B253-00129. REPAIR AUTHORIZED BY FAA FORM 8100-9 DATED 11/4/2008. REF N/R 2-104. 2 L 7 3 4F A3WE 20081120 NM 2008 11 20 DHLA2008745675 1 20081007 A 5330 SKIN BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 EXTERNAL FUSELAGE EXISTING REPAIR IS DEFORMED AND HAS MISSING FASTENERS, AT BS 235.5, BETWEEN WL 212 AND WL 220. REMOVE D EXISTING REPAIR, FABRICATED NEW DOUBLER REPAIR, AND INSTALLED PER SRM 53-30-3 FIG 1. THIS IS A CAT "B" REPAIR AND SUB JECT TO SSID F-21. REF EC-01251 FOR RE-INSPECTION TRACKING. 2 L 7 3 4F A3WE 20081120 WP 2008 11 20 IXXA08SMN166S 1 20080419 A 5751 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD AILERON UPPER SKIN HAS IMPROPER REPAIR AT STATION XA 542.000 - 60 3.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, BONDED DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. PERFORMED WEIGHT AND BALANCE. FOUND WITHIN TOLERANCE MOMENT= 3320 INCH-POUNDS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 57-1-0 PAGE 1, SRM 51-1-21, SRM 57 -8-1 FIGURE 1 ITEM "B" AND "K", DRAWING 5705334, SRM 51-1-9 TR 51-142, SRM 51-1-9A TR 51-141, SRM 51-1-8B, AND SRM 51-4- 1 PAGES 1-3. 2 L 7 4 4F RT 4A25 20081120 SO 2008 11 20 CHQA200800224 1 20081114 A 2611 23073567 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL NR 1 ENGINE LEAKING A CHQA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 11 570RP 145821 CAE312065 FLIGHT 6050, AVP TO LGA - ON SHORT FINAL, THE FLIGHT CREW RECEIVED A LAV SMOKE INDICATION ON EICAS. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FAULT AND FOUND THAT THE MESSAGE WAS PRESENT ONLY WHEN OPERATING OFF OF THE NR 1 BLEED SYSTEM. THE AIRCRAFT WAS THEN FERRIED TO CMH WHERE THE ZERO CARBON SEAL WAS REPLACED AND THERE WERE NO F URTHER INDICATIONS. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081120 NM 2008 11 20 QXEA2008111701190 1 20081115 A 5260 HANDLE BOMBDR DHC8 DHC8402 1390042 NM AIRSTAIR DOOR STIFF A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 19 433QX 4210 SEA - FLIGHT ATTENDANT ADVISES INSIDE HANDLE ON MAIN CABIN DOOR IS EXTREMELY HARD TO LIFT WHEN OPENING DOOR. PERFORMED FUNCTIONAL CHECK OF AIRSTAIR DOOR IAW TASK NR 52-11-00-720-802. DOOR UNLOCKING LOAD FRONT INTERIOR HANDLE IS 45 LBS AFT ER LUBING DOOR IAW TASK NR 52-11-00-640-801. NO DEFECTS NOTED, COULD NOT DUPLICATE. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081120 NM 2008 11 20 QXEA2008111701191 1 20081114 A 3350 58401A2B5C5F4L30 SWITCH BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY LIGHTS MALFUNCTIONED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 19 400QX 4030 SEA - EMERGENCY LIGHTS FLASH ON AND OFF INTERMITTENTLY WHEN IN ARM POSITION. REMOVED AND REPLACED FWD FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH PERFORMED OPERATIONAL CK OF THE EMERGENCY LIGHT SYSTEM REF Q400 AMM TASK NR 33-51-00-710-801. O PS CK'S GOOD, NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081120 EU 2008 11 20 F3LA2008111700712 1 20081115 A 5755 D5775002000118A HINGE FITTING AIRBUS A318 A318111 3940019 EU NR 3 SPOILER GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 801FR 1939 DURING C4 C-CHECK, INSPECTION NOTED THE RIGHT NR 3 SPOILER ANTI-ROTATION WEB FLAT WAS GOUGED. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH ENGINEERING AUTHORIZATION A8-57R-30776. 2 L 7 2 4F RT 20081120 CE 2008 11 20 AJC2008F00002 1 20081013 A 2611 47359717 SMOKE DETECTOR CESSNA 525 525B 2076616 CE CARGO BAY FALSE ACTIVATION E AJCA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 65 12GS 525B0122 ON DESCENT, `BAGGAGE SMOKE` ANNUNCIATOR ILLUMINATED. RAN ABNORMAL CHECKLIST, MAINTENANCE PERFORMED VISUAL INSP OF FWD A ND AFT BAGGAGE COMPARTMENTS AND FOUND NO EVIDENCE OF SMOKE OR FIRE. MINOR CONDENSATION WAS FOUND AND WAS DRIED. THIS I S A KNOWN ISSUE. THE FWD BAGGAGE COMPARTMENT IS PRONE TO CONDENSATION WHICH TRIGGERS A BAGGAGE SMOKE ALERT. SYS TESTED NORMAL. (K) 1 L 7 2 4F RT A1WI 20081120 EU 2008 11 20 COEA0801901 1 20081008 A 5610 NP1588011 WINDSHIELD AEROSP ATR42 ATR42320 8680930 EU COCKPIT CRACKED A COEA H D DEACTIVATE SYST/CIRCUITS RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 13 901FX 172 SMOKE AND ELECTRICAL ARCING IN COCKPIT AND RETURN TO BLOCKS FLT. DURING TAXI OUT THE CREW SELECTED WINDSHIELD HEAT ON, SHORTLY AFTER SEVERAL CRACKS FORMED WITH ARCING AND SMOKING FROM THE RT WINDSHIELD. THE CRACKING IS BELIEVED TO HAVE OR IGINATED FROM A SMALL (WITHIN ACCEPTABLE LIMITS) CRACK IN THE OUTER GLASS PLY, WHICH WAS FOUND BY THE GROUND CREW AFTER THE PREVIOUS FLIGHT. THE CREW TURNED THE WINDOW HEAT SYSTEM OFF AND SAFELY RETURNED TO BLOCKS. REMOVED AND REPLACED RT FWD WINDSHIELD. (K) 2 H 7 2 4T RT A53EU 20081120 SO 2008 11 20 FDK2008F00018 1 20081003 A 3350 2013A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 837MJ 145367 EMERGENCY FLOOR PATH LIGHTING OUT AT ROW 12. MX REPLACED NR 4 EMERGENCY BATTERY. OPS GOOD. (K) 2 L 7 2 4T RT T00011AT 20081120 SO 2008 11 20 FDK2008F00016 1 20081005 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 ROW 12 OVERHEAD EMERGENCY LIGHT INOPERATIVE. MX OPS CHECKED THE SYS, NORMAL AFTER RESET. (K) 2 L 7 2 4T RT T00011AT 20081120 SO 2008 11 20 FDK2008F00017 1 20081011 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 832MJ 145310 EMERGENCY LIGHTS OUT AT ROW 8 AND ROW 9. MX REPLACED LIGHT STRIP. (K) 2 L 7 2 4T RT T00011AT 20081119 NM 2008 11 19 SWAA086119 1 20081108 A 3350 81000 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 910WN 36618 FOUND EEPLS LENS BROKEN AT R1 DOOR. REMOVED AND REPLACED EEPLS ASSY PER MM. 2 L 7 2 4F RT A16WE 20081119 2008 11 19 SWAA086121 4 20081110 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 237WN 34632 FOUND R2 DOOR SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086070 1 20081104 A 5314 6545771 KEELBEAM BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED HC1 CHECK, FOUND KEEL BEAM CRACKED AT BS 699, STR 27R. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086071 1 20081104 A 3350 101331 LENS BOEING 737 7373Q8 1384670 NM L1 DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 663SW 23256 FOUND L1 DOOR EMERGENCY EXIT LENS UNSECURED. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086078 1 20081103 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 421LV 32452 DURING SCHEDULED RON CHECK, FOUND EEPLS COVER BROKEN AT ROW 1, SEAT ABC. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086094 1 20081111 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 277, STR 8L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081119 EA 2008 11 19 ASOA200801146 1 20081104 A 5320 PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 FABBED A REPAIR DOUBLER FOR FWD TOP EDGE OF PNL 281AZ USING AMS 5510 .032 PO 94453. INSTALLED DOUBLER USING RTV106 AND CR3523-4-3 FASTENERS PO 95946 IAW BOMBARDIER REO 601R-25-53-005. SUPPLEMENTAL-SDR CLOSED 11/17/2008. 2 L 7 2 4F RT A21EA 20081119 NM 2008 11 19 SWAA086275 1 20081117 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 421LV 32452 FOUND FWD EEPLS BROKEN. REMOVED AND REPLACED EEPLS PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 AALA200810005 1 20081003 A 5320 FLOOR SUPPORT BOEING 737 737823 13844BZ NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 903AN 29505 CORROSION ON FLOOR SUPPORT ANGLE RIGHT SIDE STATION 767 TO 787 ABOVE STRINGER 25. REPLACED FLOOR SUPPORT ANGLE PER ESO 61000 DATED 10/02/2008. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 AALA200802697 1 20081008 A 3350 LIGHT BOEING 757 757223 1384957 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 643AA 24601 DFW - EXTERIOR EMERGENCY LIGHT AT LEFT OVERWING INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LEFT OVERWIN G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081119 NM 2008 11 19 AALA200802696 1 20081008 A 3350 LIGHT BOEING 757 757223 1384957 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 643AA 24601 DFW EXTERNAL EMERGENCY SLIDE LIGHT AT LEFT NUMBER FOUR DOOR IS INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY SLIDE LIGHT AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081119 NM 2008 11 19 AALA200820008 1 20081009 A 5320 146N5318 STRUCTURE BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 672AA 52528 25337 MAIN DECK FLOOR STRUCTURE IS CORRODED. REMOVED CORROSION AND INSTALLED DOUBLER IAW SRM 53-60-51-2R2. 2 L 7 2 4F RT A2NM 20081120 EA 2008 11 20 CHQA200800223 1 20081114 A 3150 WARNING MESSAGE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FALSE ACTIVATION A CHQA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 11 653BR 7438 GEE872823 FLIGHT 5756, IAH TO SDF - DURING CRUISE, THE FLIGHT CREW RECEIVED AN E1 14TH STAGE DUCT MESSAGE AND DIVERTED TO AEX WHER E IT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED THE DUCT TEST WITH NO DEFECTS NOTED AND INSPECTED THE PYLON AND COW L DUCTS WITH NO DEFECTS NOTED. THE ENGINES WERE RUN WITH NO FURTHER MESSAGES AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20081120 NM 2008 11 20 DHLA2008745676 1 20081110 A 5330 SKIN BOEING 727 727224 1384076 NM ZONE 200 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 FUSELAGE SKIN, FASTENER ROW AT STR 4R LAP SEAM FROM BS 691.5 TO 693.5 HAS CRACK INDICATIONS. DURING ACCESS, FOUND FRAME CRACKED AT BS 740, BETWEEN STR 3R AND 5R. ACCOMPLISHED SKIN REPAIR AT LAP SEAM, BS 680 TO BS 740, PER SB 727-53A0222 R EV 1, SECT 3, PART II. REPAIRED FRAME SECTION PER COOPESA EO COO-2-53-317-08 DATED 10/24/08, BAC MSG 1-981723679-5 DATE D 10/23/08, AND ASTAR EVA B253-00116. APPROVAL DOCUMENTED ON FAA FORM 8100-9. REF COOPESA N/R'S 2-146, 2-147, 2-148, 2 -149, 2-150, AND 2-151. 2 L 7 3 4F A3WE 20081120 SO 2008 11 20 SWIA200820382 1 20081116 A 6120 78249046 PCU EMB 120 EMB120ER 3260203 SO RT PROPELLER FAILED A SWIA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 NM 07 295UX 31317 8008 120295 ON TAKEOFF, RIGHT NP DROPPED TO 99 PERCENT AND DID NOT RECOVER, ABORTED TAKEOFF. REPLACED RIGHT PCU, P/N 782490-46 S/N ON 980810 S/N OFF 890455. 2 L 7 2 4T RT A31SO 20081120 SO 2008 11 20 SWIA200820388 1 20081111 A 5280 LATCH EMB 120 EMB120ER 3260203 SO MLG DOOR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 270YV 120270 FLT 5590 - ON DEPARTURE, LEFT MAIN GEAR UNSAFE LIGHTS REMAINED ILLUMINATED W/GEAR HANDLE IN THE UP POSITION. REPLACED L EFT INBOARD MAIN GEAR DOOR LATCH ASSEMBLY. 2 L 7 2 4T RT A31SO 20081120 SO 2008 11 20 SWIA200820389 1 20081113 A 3234 MODULE EMB 120 EMB120ER 3260203 SO MLG SELECTOR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 236SW 120312 FLT 5495 - LANDING GEAR DID NOT RETRACT AFTER TAKEOFF. REPLACED LANDING GEAR HANDLE SELECTOR CONTROL PANEL MODULE. 2 L 7 2 4T RT A31SO 20081120 EU 2008 11 20 F3LA2008111700714 1 20081115 A 3350 BR964424 LAMP AIRBUS A318 A318111 3940019 EU EMERGENCY LIGHT INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 805FR 39 1660 LINE MAINTENANCE NOTED THAT THE SEAT MOUNTED EMERGENCY EXIT LIGHT AT ROW 5ABC WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED SEAT MOUNTED EMERGENCY EXIT LIGHT AND PERFORMED OPERATIONAL TEST IN ACCORDANCE WITH A318 AMM 33-51-19 PB 40 1. 2 L 7 2 4F RT 20081120 EU 2008 11 20 F3LA2008111700715 1 20081116 A 3350 2LA00546901 CONTROL PANEL AIRBUS A318 A318111 3940019 EU EMERGENCY LIGHT FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 21 806FR 2218 PILOT REPORTED THE LEFT OVERWING EXIT SHOWS OPEN ON LOWER ECAM. MAINTENANCE PERFORMED TROUBLESHOOTING AND FOUND LEFT OV ERWING LIGHT TO BE AT FAULT. THE WARNING LIGHT PANEL WAS REMOVED, REPLACED AND CHECKED IN ACCORDANCE WITH A318 AMM 52-7 3-21 PB 401. 2 L 7 2 4F RT 20081120 2008 11 20 QXEA2008111401187 4 20081111 A 6122 697072003 GOVERNOR BOMBDR DHC8 DHC8402 1390042 NM NR 2 PROPELLER FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 418QX 7 4143 SEA - NR 2 PROP WOULD NOT COME OUT OF FEATHER. REMOVED OVERSPEED GOVERNOR IAW Q400 AMM TASK 61-20-26-000-801 AND INSTAL LED A NEW FROM STOCK OSG IAW Q400 AMM TASK 61-20-26-400-801. OPS AND LEAK CHECK GOOD. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081120 WP 2008 11 20 IXXA08SMN177S 1 20080419 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1580 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FRAME FLANGE CRACKED AT STATION 1580.000 LONGERON 20 LEF T TO LONGERON 21 LEFT. REMOVED DAMAGED SEGMENT OF FRAME. FABRICATED SEGMENT OF FRAME, ANGLES. PERFORMED HEAT TREATMEN T TO REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW SRM 53-2-0 FIGURE 2 S HEETS 1, 4 AND 6, SRM 53-4-1 FIGURE 51 ITEM "A", 53-2-0 FIGURE 2 SHEET 7, 8 TR NUMBER 53-110 DATED 11-10-00, 53-2-0 FIGU RE 2 SHEET 5 TR NUMBER 53-125 DATED 08-31-01, SRM 51-1-1 PAGES 1, 13 AND 17, SRM 51-1-8B, SRM 51-1-20, AND 51-3-1. 2 L 7 4 4F RT 4A25 20081120 EA 2008 11 20 SWIA200820367 1 20080715 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 368CA 10075 C-CHECK, FS 280 COCKPIT FLOOR SUPPORT ANGLE CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081120 EA 2008 11 20 SWIA200820368 1 20080715 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 368CA 10075 C-CHECK, FS 280 CROSSBEAM CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081120 WP 2008 11 20 NWAA084559869 1 20081011 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 778NC 48100 DURING LINE CHECK, MX FOUND THAT THE EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MX REPLACED THE POWER SUPPLY AND T HE LIGHTS RETURNED TO AN OPS CONDITION. 2 L 7 2 4F RT A6WE 20081120 EU 2008 11 20 NWAA084543303 1 20081003 A 3350 EPSU AIRBUS 330 A330323 3940030 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 803NW 23257 0542 DURING TEST EPSU 11WL DOOR 1 FAULTED AND SEATS 1AB, 2AB AND 3AB EMERGENCY AISLE LIGHTS INOP. REPLACED THE EPSU 11WL AND TESTED OK. 2 L 7 2 4F RT A46NM 20081120 NM 2008 11 20 NWAA084536624 1 20081009 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 624US 21706 DURING OVERNIGHT CHECK, FOUND EMERGENCY LIGHT EXIT SIGN AT 45C, 51C AND ABOVE 4L DOOR INOP. MX R&R BATTERY PACK. OPS C HECKED GOOD AND ACFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20081120 WP 2008 11 20 NWAA084499851 1 20080918 A 5312 STIFFENER DOUG DC9 DC951 3022051 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NC 47708 DURING H CHECK FOUND CRACK IN OTBD END OF UPPER AFT PRESSURE BULKHEAD HORIZONTAL STIFFENER. REPAIRED PER EA 98-213643. 2 L 7 2 4F RT A6WE 20081121 NE 2008 11 21 DLM88081573 2 20081117 A 7510 DUCT DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 NACELLE DAMAGED A DALA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 27 988DL 44433 53339 725774 ON CLIMB-OUT AT LEVEL OFF THE RT ENGINE THROTTLE WAS BOUND. UNUSUAL RESISTANCE TO MOVING TO IDLE. AFTER BRINGING THE E NGINE BACK TO IDLE THE THROTTLES OPERATED NORMALLY. FOUND THE NUMBER 2 ENG COWL ANTI-ICE DUCT BLOWN WHICH CAUSED DAMAGE TO THE UPPER ENGINE COWL. 2 L 7 2 4F 4 F RT A6WE E9NE 20081121 NM 2008 11 21 DL757081574 1 20081112 A 5347 CARGO TRACK BOEING 757 757232 1384965 NM BS 1520 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 CORROSION ON TIE DOWN SUPPORT LOWER SURFACE BS 1520 RBL 22 BILGE AREA. FOUND CORROSION ON DOUBLER FOR TIE DOWN FITTING OUT OF LIMITS, REMOVED AND REPLACED DOUBLER IAW SRM 51-40-02, SRM 51-20-01. 2 L 7 2 4F RT A2NM 20081121 NE 2008 11 21 DL76G081580 2 20081117 A 7230 BLADES BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE ENGINE FAN DAMAGED A DALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 27 1612T 31905 30575 704747 RIGHT ENGINE BIRD INGESTION, ENGINE VIBS, DIVERTED TO DKR 3 FAN BLADES ARE DAMAGED BORO WAS GOOD. REPLACED FANBLADE SET S. 2 L 7 2 4F 4 F RT A1NM E13NE 20081121 CE 2008 11 21 GLBA200811121 1 20081103 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE DENTED A GLBA K NONE O OTHER TX TAXI/GRND HDL 1 NM 21 257GL UE257 MAJOR REPAIR - DURING ROUTINE DAILY LINE ENVIRONMENT CONDITIONS A TUG COLLIDED WITH THE AIRCRAFT LEAVING FOUR DENTS BELO W THE CARGO DOOR BETWEEN FS 447.0 TO APPROXIMATELY FS 472.7 BETWEEN STRINGER 11L & 12L. MAINTENANCE REPAIRED AFT FUSELA GE SKIN BETWEEN FS 447.0 TO APPROXIMATELY FS 472.7 BETWEEN STRINGER 11L & 12L IAW BEECH 1900D SRM 51-70. REPAIR AREA AP PROXIMATELY 21.8 INCH BY 8.3 INCH 2024 T3 ALUMINUM, RIVETS CR3212, CR3213, Z0426 & Z0470AD. 2 L 7 2 4T RT A24CE 20081118 NM 2008 11 18 2008UALA06440 1 20081108 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 525UA 24978 FUSELAGE DAMAGE BY CABIN SERVICE TRUCK LEFT OF OUTFLOW VALVE. MAJOR REPAIR ACCOMPLISHED. SHEAR TIES BEING MFG IN SFO. RECEIVED STRINGER, DRILLING. CONT TO MFG DOUBLER & TRIPLER. ACCOMPLISHED REPAIR AT FRAME 1600 AND 1620 AND BETWEEN ST RINGER 27L AND 28L. PERFORMED PERMANENT REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 2008UALA06441 1 20081108 A 3020 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ENGINE ANTI-ICE FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 544UA 25322 EICAS MSG ENG ANTI-ICE DISPLAYED AND ENG ANTI-ICE VALVE LIGHT REMAINED ILLUM WITH SWITCH OFF. POSITION 2. CREW COMMENT S: VALVE LIGHT TOOK 30 SEC TO EXTINGUISH. VALVE DID CLOSE. REPLACED NR 2 ENG TAI VALVE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 EU 2008 11 18 08FDEA04891 1 20081115 A 3411 PITOT LINE AIRBUS 310 A310324 3930206 EU OBSTRUCTED A FDEA C ABORTED TAKEOFF P NO WARNING INDICATION TO TAKEOFF 1 CE 21 813FD 500 REJECTED TAKEOFF, NO AIRSPEED ON F/O'S PFD (60KTS). REMOVED LINE AT F/O'S PITOT PROBE AND PRESSURIZED WITH NITROGEN. THERE WAS A BLOCKAGE AT FIRST THEN IT CLEARED, WAS NOT ABLE TO DETERMINE WHAT THE BLOCKAGE WAS, BUT F/O'S PITOT PROBE IS NOW CLEAR. RECONNECTED LINE. SYSTEM OPS CHECKS NORMAL PER M/M 34-11-34-4. PERFORMED LEAK CHECK OF F/O'S PITOT SY STEM, LEAK WAS GOOD PER M/M 34-10-10-501. 2 L 7 2 4F RT A35EU 20081118 2008 11 18 08FDEA04892 4 20081115 A 3417 4045053914 ADC AIRBUS 310 A310324 3930206 EU NR 2 FAILED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 21 813FD 12 12 500 ON TAKEOFF ROLL, F/O HAD NO AIRSPEED INDICATION, PERFORMED REJECT (70KTS). PERFORMED ALL OTHER PARAMETERS THAT COME FRO M ADC ARE NORMAL. THE ON ISSUE IS THE SEED. PER FLIGHT CREW THE SPEED STOP AND THERE WAS DIFFERENCE FROM THE CAPTAIN'S AND THE F/O'S. DURING FLIGHT FROM OAK TO BUR, FLIGHT CREW DID MENTION THAT THEY SWITCHED OVER FROM NR 2 SGU TO NR 3 A ND THE RESULTS WERE NO JOY. BAGGED F/O'S PITOT PROBE AND BACK PRESSURIZED PITOT LINE, NO DEBRIS FOUND, RECONNECTED ALL LINES. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER. PERFORMED F/O'S PITOT LEAK CHECK WITH BARFIELD TESTER, LEAK CHEC KS NORMAL. SYSTEM OPS CHECKS NORMAL PER M/M 34-11-34-4. 2 L 7 2 4F RT A35EU 20081118 NM 2008 11 18 08FDEA04893 1 20081115 A 5330 SKIN BOEING 727 7272D4 138407U NM BS 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 39962 21849 LOWER FWD CARGO PIT BILGE, CORROSION SPOT ON FUSE SKIN AT AFT SIDE OF STA 700, BL- 0" REF DUPLICATE SDR #08-4824. FAA PLEASE DELETE THIS SDR- ADMINISTRATOR 2 L 7 3 4F A3WE 20081118 NM 2008 11 18 08FDEA04895 1 20081115 A 5744 ARC050213 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 593FE 48551 LEFT WING, OUTBOARD FLAP INBOARD HINGE (WING SIDE) SIDE LOAD MOUNT SURFACE FOUND CORROSION. CORROSIONS REMOVED ON SIDE LOAD MOUNT AT LT WING OUTBOARD FLAP INBOARD HINGE (WING SIDE) AND FOUND WITHIN LIMIT AS PER EA 1-5750-122634, REPAIR CL ASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081118 EU 2008 11 18 08FDEA04857 1 20081111 A 5753 A5797130100600 VANE AIRBUS 310 A310203 3930313 EU LT WING TE FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 427FE 362 LT OTBD FLAP UPPER SURFACE HAS 9 INCH GOUGE APPROX .020 IN DEEP LOCATED 54 INCHES FROM OTBD END AND 21 INCHES FROM T/E . REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW EA 6-5750-124167, RELEASE DATE4 NOVEMBER, 2008. 2 L 7 2 4F RT A35EU 20081118 WP 2008 11 18 08FDEA04770 1 20081104 A 5310 AYB70301 SKIN DOUG MD10 MD1010F 3022112 WP BS 1501-1521 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 46631 CENTER LANDING GEAR WHEEL WELL, FS 1501 TO FS 1521 AT STR R50 TO L48 HAS CORROSION AND BARE METAL. REMOVED CORROSION IAW SRM 51-21-01 PG. 28 VOL. II. ORIGINAL THICKNESS ON SKIN IS .125 IAW DWG AYB7030 REV E. FOUND TO BE OUT OF LIMITS IA W SRM 53-00-01 PG. 6 VOL. I. CUTOUT DAMAGED SECTION OF SKIN. FABRICATED REPAIR DOUBLER, TRIPLER, FILLER, & INSTALLED FI NAL E.A. TO BE ACCOMPLISHED ON FEDEX N/R N00465 EA 8-5330-123517 FUSE- UNDERWING CENTER BELLY SKIN CORROSION. 2 L 7 3 4F RT A22WE 20081118 WP 2008 11 18 08FDEA04771 1 20081104 A 5310 AYB70301 SKIN DOUG MD10 MD1010F 3022112 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 46631 CENTER LANDING GEAR WHEEL WELL, FS 1481 TO FS 1501 BETWEEN STR R50 TO L49 HAS CORROSION ON SKIN. REMOVED CORROSION IAW SRM 51-21-01 PG 28 A VOL II. SKIN ORIG THICKNESS 0.125 IAW DWG AYB 7030; REV "E". REMAINING MATERIAL THICKNESS 0.090. MATERIAL REMOVED 0.035. FOUND TO BE OUT OF LIMITS; MORE THAN 20% MATERIAL LOSS IAW SRM 53-00-01 PG 6 VOL I. CUT OUT DAMAGED SKIN. FABRICATED REPAIR DOUBLER TRIPPLER, FILLER AND INSTALLED FROM IAW EA 8-5330-123517. 2 L 7 3 4F RT A22WE 20081118 EU 2008 11 18 08FDEA04772 1 20081106 A 5753 A57960007200 SKIN AIRBUS 300 A300B4622R 3930312 EU TE FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 722FD 479 LT WING INBD FLAP AT RIB 25A, UPPER SKIN IS CRACKED. FABRICARED SKIN P/N A57960007200 & DOUBLER P/N A57960007202 IN REF TO FEDEX EA 6-5750-123671. 2 L 7 2 4F RT A35EU 20081118 NM 2008 11 18 08FDEA04880 1 20081114 A 5321 6523638 FLOOR PANEL BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 MAIN CARGO FLOOR CORROSION ON SEAT TRACK AT STA 740 LBL46 REMOVED BEYOND LIMITS CORRODED SEAT TRACK REF SRM 51-30-2. FA BRICATED REPLACEMENT SEAT TRACK REF SRM 53-10-5. FABRICATED TRACK SPLICE REF SRM 53-10-5. INSTALLED SEAT TRACK AND SPL ICE REF SRM 53-10-5, TREATED AND PRIMED REF SRM 51-10-2 PG 3. FABRICATED -3 SPLICE STRAP REF SRM 53-10-5 PG3 HEAT TREAT SPLICE REF 8130 NR 418721, CADIUM PLATE STRAP REF NR N00957, PRIMED STRAP REF 51-10-2. INSTALLED STRAP SPLICE REF SRM 53-10-5 P3. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081118 NM 2008 11 18 2008UALA06508 1 20081113 A 3610 CONTROLLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BLEED AIR SYS MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 598UA 28751 WHILE REACTIVATING NR 2 ENG HS-PILOT FOUND OVERPRESSURE INDICATOR POPPED. RESET, RAN ENG AT IDLE. PRESSURE INDICATING 18 PSI. REF MEL 3611D BY- 118169. ACP'D PNEUMATIC HEALTH CK ON NR 2 ENG ON H-S PILOT, HPSOV, PRC, AND PRSOV. PRSOV CO NTROLLER FAILED REF PRESSURE, PRESS EXCEEDED LIMIT. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 2008UALA06510 1 20081113 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 551UA 25399 TWO EEL EXIT IDENTIFIERS HAVE BROKEN WIRES. REPLACED 2 EA EEL IDENTIFIERS, 1 EA SEAT ROW 15 LT AND RT. OPS CHECKS GOO D. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 2008UALA06447 1 20081109 A 3350 COVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN LOOSE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 596UA 28749 EMERGENCY FLOOR LIGHTING STRIP AT 13C IS PEELING BACK. SECURED LOOSE PLASTIC COVER ON TRACK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 2008UALA06448 1 20081109 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 174UA 24381 UPPER DECK CEILING EMERGENCY EXIT LIGHT DIM, BS 945 BL 0. RELAMPED, OP CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081121 SO 2008 11 21 GN0A-1 1 20081031 A 2797 W602000522B WIRE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE FLAP ACTUATOR BROKEN E GN0A O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 15 650CT 120198 FLIGHT KFRG-KACY, CREW REVIEWED FLAP CONTROL FAULT WHEN FLAPS SELECTED FOR LANDING AT KACY. COULD NOT RE-SET FAULT. DE CLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. FOUND BROKEN WIRE GOING TO RIGHT INBOARD FLAP ACTUATOR APPROX 12 INCHES FROM ACTUATOR ELECTRICAL CONNECTOR P0652. WIRE WAS REPAIRED AND SYSTEM CHECKED GOOD. AIRCRAFT RETURNED TO SERVI CE. 2 L 7 2 4T 4 T RT A31SO E20NE 20081121 NM 2008 11 21 DLM88081536 1 20081112 A 4990 SEAL DOUG MD88 MD88 3023688 NM APU OIL CAP WORN A DALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 963DL 49982 SMOKE IN CABIN AND COCKPIT. RTB - SMOKE DISSIPATED ON LANDING FOUND APU INLET CONTAMINATED WITH ENG OIL 042620, PERFORM ED OP 5088. FOUND APU OIL CAP SEAL WORN. REPLACED SAME. RAN APU LEAKS NOTED. PERFORMED OP 5089. PNEUMATIC SYS DUCT BURN. 2 L 7 2 4F RT A6WE 20081121 NM 2008 11 21 DL757081547 1 20081008 A 5753 PANEL BOEING 757 757232 1384965 NM RT INBD FLAP GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 RT INBD FLAP CENTER L/E PANEL IS GOUGED ON LOWER SURFACE INBD SIDE. BLENDED DAMAGED AREA IAW AMM 57-53-00. REMAINING S KIN THICKNESS .073. ORIGINAL IS .080, WITHIN LIMITS. 2 L 7 2 4F RT A2NM 20081121 CE 2008 11 21 GUUA11160802 1 20081116 A 3240 BRAKE SYS BEECH 1900 1900D 1154162 CE RIGHT CONTAMINATED A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 81533 UE137 FLIGHT 9272 EYW/FLL - PILOT REPORTED RIGHT BRAKE INOPERATIVE. PERFORMED BRAKE BLEEDING ON RIGHT BRAKE ASSEMBLY. OPERAT IONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081121 CE 2008 11 21 GUUA11160803 1 20081116 A 3240 BRAKE SYS BEECH 1900 1900D 1154162 CE RIGHT CONTAMINATED A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 81533 UE137 FLIGHT 9207PNS/TPA - PILOT REPORTED RIGHT BRAKE INOPERATIVE, THE PEDAL GOES ALL THE WAY DOWN. BLED RIGHT BRAKES. OPERA TIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081121 NM 2008 11 21 DL764081556 1 20081115 A 4900 38006081 APU BOEING 767 767432ER 1385134 NM APU BAY MALFUNCTIONED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 834MH 16455 29707 REPLACED APU, IN-FLIGHT APU START REQUEST LOADED IN GHGD. 2 L 7 2 4F RT A1NM 20081121 NM 2008 11 21 DL757081557 1 20081011 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 365.25 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 MAIN CABIN FLOORBEAM END CAP STA 365.25 RBL 10 CORRODED. REMOVED END CAP IAW SRM 51-40-02 FIG 8 PG 31. INSTALLED REPLA CEMENT CAP IAW SRM 51-40-02 PG 4 AND 7. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081559 1 20081112 A 5340 6945579Y30 FITTING BOEING 757 757232 1384965 NM BS 1400 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 AFT CARGO BAY DOOR WAY THRESHOLD SUPPORT FITTING IS CORRODED BS 1400 RBL 28. REMOVED AND REPLACED FITTING DUE TO CORROS ION OUT OF LIMITS. 2 L 7 2 4F RT A2NM 20081121 WP 2008 11 21 AALA200810151 1 20081106 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1497 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 459AA 49564 RIGHT FRAME 1497 WORN. INSTALLED DOUBLER ON 1497 FRAME PER SRM 53-10-00-15. 2 L 7 2 4F A6WE 20081121 WP 2008 11 21 AALA200810106 1 20081027 A 5320 STRUCTURE DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA * 49736 CABIN SUBFLOOR CRACKED, 1/2 INCH IN LENGTH. INSTALLED NEW CUSP SECTION PER 51-30-02 AND 51-30-5, 8 INCH BY 16 INCH. 2 L 7 2 4F A6WE 20081121 NM 2008 11 21 08FDEA04916 1 20081118 A 5311 FRAME BOEING 757 75723A 1384967 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 AFT CARGO COMPT, FRAME 1360, AT S-26L, IS CORRODED AND GOUGED. REPAIRED FRAME, AFT CARGO COMPT, BS 1360, AT S-26L, IAW SRM 53-00-07, REPAIR NR 5. THIS REPAIR IS CLASSIFIED AS A CAT "B" MAJOR REPAIR WITH THE FOLLOWING FOLLOW UP REQUIRE MENTS, INITIAL AT 37,500 FC, THEREAFTER EVERY 12,000 FC. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081548 1 20081011 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 1640 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 MAIN CABIN FLOORBEAM STA 1640 BL "0" TO RBL 12 UPPER SURFACE OF FLOORBEAM IS CORRODED HEAVILY. REPAIRED IAW SRM 53-00-5 1, REPAIR 3 FIG 201. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL77L081562 1 20081116 A 3150 WARNING LIGHT BOEING 777 777232 1385232 NM FALSE ACTIVATION A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 701DN 29740 RTB DUE TO FLT CONTROL EICAS MESSAGE CAME ON DURING FLT CONTROL CHECK. MTC MESSAGE 27-10223. PERFORMED GROUND TEST PER FIM. TEST PASSED. OK FOR SERVICE. 2 L 7 2 4F RT T00001SE 20081121 NM 2008 11 21 DL76G081563 1 20081116 A 7330 PRESSURE SWITCH BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE NR 2 FUEL FILTER FAILED A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 1609 36375 30574 704749 INTERMITTENT RIGHT ENGINE FUEL FILTER LIGHT. REMOVED AND REPLACED RT ENG FILTER PER M/M. INSPECTED NTF REMOVED AND REP LACED FUEL FILTER PRESSURE SW PER M/M RAN ENG MSG DID NOT RETURN. 2 L 7 2 4F 4 F RT A1NM E13NE 20081121 NM 2008 11 21 DL764081564 1 20081114 A 3150 WARNING LIGHT BOEING 767 767432ER 1385134 NM ILLUMINATED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 828MH 29699 FWD EQUIP OVERHEAT EICAS WITH OVERHEAT LIGHT. FWD TO MCO AND PLACARD PER MEL M21-58-08. 2 L 7 2 4F RT A1NM 20081121 NM 2008 11 21 DL76G081502 1 20081015 A 4900 491003096 APU BOEING 767 767332 1382001 NM UNKNOWN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1602 31203 29694 P1191* REPLACED APU DUE START HISTORY. APU REPLACED. 2 L 7 2 4F RT A1NM 20081118 NM 2008 11 18 2008UALA06456 1 20081107 A 2710 550030019 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE AILERON FAULTY A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 660UA 27115 THE "AIL LOCK" LT ON AT LOW SPEED. EICAS MSG AILERON LOCKOUT DISPLAYED. RECEIVED AILERON LOCKOUT MSG. REPLACED LEFT A ILERON LOCKOUT ACTUATOR. MESSAGE CLEARED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081118 NM 2008 11 18 2008UALA06457 1 20081110 A 5754 PANEL BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LE SLAT DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 668UA 30024 NR 1 L/E SLAT INBOARD SECTION OF FIBERGLASS CLOSURE PANEL MISSING APPROX 30 INCHES. PANEL RECEIVED, NEED 8 HOURS TO INS TALL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081118 2008 11 18 2008UALA06459 4 20081109 A 2565 69B528083 HOUSING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 642UA 25092 LT OVER WING SLIDE CABLE DISCONNECT HOUSING BROKEN. REMOVED AND REPLACED DISCONNECT HOUSING. 2 L 7 2 4F 4 F RT A1NM E24NE 20081118 NM 2008 11 18 2008UALA06460 1 20081109 A 3350 BACS16X3A SOCKET BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EXTERIOR DIRTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 642UA 25092 EXTERIOR EMERGENCY LIGHT AT L-2 DOOR IS INOP. CLEANED LIGHT SOCKET AND OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081118 NM 2008 11 18 2008UALA06461 1 20081109 A 3397 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 EEL LIGHT INOP AT LEFTSIDE MID LAV. REPAIRED FEEDER ASSY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081118 NM 2008 11 18 2008UALA06463 1 20081109 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 EEL LIGHT INOP AT SEAT 25H. REPLACED EEL LIGHT, OP CHECK IS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081118 NM 2008 11 18 2008UALA06468 1 20081110 A 3350 9F19948501 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 175UA 24382 EMERGENCY LIGHT INOP: DOOR 1R SLIDE ILLUM. REPLACED LIGHT ASSEMBLY, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081118 NM 2008 11 18 2008UALA06471 1 20081110 A 2131 7102048 CONTROLLER BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE MALFUNCTIONED A UALA B A EMER. DESCENT UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 935UA 26663 PRESSURIZATION PROBLEM. FLIGHT DIVERTED. 2 L 7 2 4F 4 F RT A16WE E21EU 20081118 NM 2008 11 18 2008UALA06511 1 20081112 A 3350 36262478671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 178UA 24385 EEL LIGHT BROKEN AT 45C, 35H, 38H. REPLACED EEL AT 45C, CHECKS OKAY. REPLACED EEL STRIP AT SEAT 35H & 38H. OPS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081118 NM 2008 11 18 2008UALA06512 1 20081112 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 204UA 28713 THE 2E EXIT PATH LIGHT ON SEAT IS FALLING OFF. SECURED LIGHT ASSY, CHECKED OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081118 NM 2008 11 18 2008UALA06513 1 20081114 A 3350 CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 OVERWING EMERGENCY LIGHT RT 2 BOTTOM LIGHT INOP. REPLACED BATTERY CHARGER. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081114 NM 2008 11 14 2008UALA06397 1 20081106 A 5210 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 DOOR 4R LWR GATE CORRODED. INSTALLED NEW GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081114 NM 2008 11 14 2008UALA06404 1 20081107 A 2781 PROXIMITY SENSOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LE SLAT FAULTY A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 670UA 29240 EICAS MSG L/E SLAT ASYM DISPLAYED, LEADING EDGE LIGHT ILLUM WITH THE FLAP LEVER IN 1. BOTH FLAP POINTERS ARE CORRECT. REPLACED PROX SENSOR S-286 FOR INBOARD NR 5 L/E SLAT, CONDITION NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081114 NM 2008 11 14 2008UALA06385 1 20081105 A 3397 CONNECTOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 942UA 26679 CABIN FLOOR EEL INOP FROM ROW 4 TO ROW 11. CHECKED CONNECTIONS TO EEL FLOOR STRIP AND BATTERY PACK PWR SUPPLY, OPS CHEC K EMERG LIGHTS, TEST OK. 2 L 7 2 4F 4 F RT A16WE E21EU 20081114 EU 2008 11 14 08FDEA04830 1 20081110 A 5510 A5517781120200 FITTING AIRBUS 310 A310324 3930206 EU HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 RIGHT HORIZONTAL STAB, OTBD AFT HOIST POINT IS CRACKED. REMOVED INBD REAR HOIST POINT FITTING IAW SRM 51-40-21. INSTAL LED REPAIR PLUG IAW EO 6-5510-7-5001. INSTALLED FITTING IAW SRM 51-40-21. SEALED FITTING FASTENERS IAW SRM 51-74-00. INSTALLED COVER PLUG IAW EO 6-5510-7-5001. INSTALLED FITTING IAW SRM 51-40-21. SEALED FITTING FASTENERS IAW SRM 51-74- 00. INSTALLED COVER PLUG IAW EO 6-5510-7-5001; PARA 12. 2-B. 2 L 7 2 4F RT A35EU 20081114 EU 2008 11 14 08FDEA04832 1 20081110 A 5347 A538202020 SEAT TRACK AIRBUS 300 A300F4605R 3930327 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK SEAT TRACK RBL 18 HAS CORROSION 3 INCHES FWD OF FRAME 42. REMOVED AND REPLACED SEAT TRACK FROM FR 40 T O FR 44 IAW SRM 51-40-41AND 51-40-44. 2 L 7 2 4F RT A35EU 20081114 EU 2008 11 14 08FDEA04833 1 20081110 A 5210 A5217633320300 FAILSAFE AIRBUS 310 A310324 3930206 EU PAX DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 RIGHT AFT PAX DOOR FAIL/SAFE RING LOWER SECTION HAS CORROSION ON THE SKIN AROUND THE FASTENER HEADS. REMOVED LIGHT SU RFACE CORROSION AS REQUIRED ON R/H AFT ENTRY DOOR FRAME, FAILSAFE RING IAW SRM 53-18-12 FIG. 102 & 5140-47. ALODINE & PR IME APPLICATION REFER TO W/C 41X5067ALI J.P.F. STEP 7 - 10. 2 L 7 2 4F RT A35EU 20081114 EU 2008 11 14 08FDEA04834 1 20081110 A 5210 A5217633320200 FAILSAFE AIRBUS 310 A310324 3930206 EU PAX DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 LEFT AFT PASSENGER DOOR EXTERNAL SKIN IN THE SCUFF PLATE AREA AND FAIL/SAFE RING HAS SEVERAL AREAS OF CORROSION. REMOVE D LIGHT SURFACE CORROSION AS REQUIRED FROM SCUFF PLATE AREA & FAILSAFE RING IAW SRM 51-74-10. ALODINE AND PRIME ACCOMPLI SHED ON W/C 41X5067ALI. 2 L 7 2 4F RT A35EU 20081114 EU 2008 11 14 08FDEA04835 1 20081110 A 5313 AEA027313 STRINGER AIRBUS 310 A310324 3930206 EU BS 1401 S25 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 449 CENTER LANDING GEAR WHEEL WELL AT FS 1401 AND STRINGER 52 HAS CORROSION. REMOVED AND REPLACED FRAME IAW SRM 51-31-01. FABRICATED A NEW FRAME IAW DWG AEA 0273. ALODINED AND PRIMED IAW SRM 51-21-01. PART MARKED IAW GMM 7-0-1001. 2 L 7 2 4F RT A35EU 20081117 EA 2008 11 17 MASA2008110500763 1 20081105 A 2750 860D10018ABCD ECU CNDAIR CL600 CL6002B19 1900309 EA TE FLAP MALFUNCTIONED A MASA B EMER. DESCENT J WARNING INDICATION LD LANDING 1 SW 07 715SF 18489 7115 ASH 7093 ORD-CLE. CREW DECLARED AND EMERGENCY ON LANDING DUE TO A FLAP SYSTEM FAILED. AIRCRAFT FERRIED TO CAE WHERE MA INTENANCE COMPLIED WITH PART A/PART B AND REMOVED AND REPLACED FECU. 2 L 7 2 4F RT A21EA 20081117 SO 2008 11 17 C2XA08IA237 1 20081112 A 2120 UNKNOWN EMB 145 EMB145EP 3260221 SO GALLEY ODOR A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 14933 145018 IAH - FLIGHT 3059 THE CREW REPORTED A BURNING SMELL IN THE GALLEY DURING TAXI. THE AIRCRAFT RETURNED TO THE GATE WITHOU T INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, PERFORMED ENGINE RUNS, AND OPERATIONALLY CHECKED THE COFFEEMAKERS, ALL WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20081117 NM 2008 11 17 SWAA086205 1 20081113 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 2L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081117 WP 2008 11 17 IXX2008F00104 1 20080808 A 5512 SKIN DOUG DC8 DC871F 302199D WP HORIZ STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK INSP, FOUND RT HORIZ STABILIZER AFT PANEL CORRODED AT STA XF 195.963. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTNERS AS NEEDED TO PERFORM REPAIR. REMOVED CORRODED SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PART AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTNERS AND REPAIR PARTS IAW SRM. (K) 2 L 7 4 4F RT 4A25 20081117 WP 2008 11 17 IXX2008F00105 1 20080805 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK INSPECTION, FOUND RT WING UPPER SKIN CRACKED AT STRINGER 8 STA XW 408.00. REMOVED FASTENERS AS N EEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFOMRED NDT INSP. NO CRACK AND NO CORROSION FOUND. FABRICATED REPAI R DOUBLER, AND FILLER PLUG. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PART S IAW SRM. (K) 2 L 7 4 4F RT 4A25 20081117 WP 2008 11 17 IXX2008F00106 1 20080730 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK, FOUND FWD OF FLAT AFT PRESSURE BULKHEAD HAS IMPROPER REAPIR AT LONGERON 28. REMOVED FASTENERS A S NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRA CK, NO CORROSION. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. CLEANED, TREATED, AND PRIMED AEA AND REPAIR PART S. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SB. (K) 2 L 7 4 4F RT 4A25 20081117 WP 2008 11 17 IXX2008F00110 1 20080805 A 5320 FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT SPLICE FITTING CRACKED AT STA 1040.000-1060.000 LONGERON 31 LT. REMOVED CRACKED SPLICE FITTING. FABRICATED SPLICE FITTING. PERFORMED NDT INSP. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED, AND PRIMED AREA AND SPLICE FITTING. INSTALLED NEW SPLICE FITTING SRM. (K) 2 L 7 4 4F RT 4A25 20081117 WP 2008 11 17 IXX2008F00115 1 20080806 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK INSP, FOUND AFT LOWER FUSELAGE AFT OF OUTFLOW VALVE HAS IMPROPER REPAIR AT STA FS1688, LONGERON 3 5.75 RT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, TRIPLER, FILLER, INTERNAL DOUBLER. CLEANED TREATED, A ND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM. 2 L 7 4 4F RT 4A25 20081117 WP 2008 11 17 IXX2008F00116 1 20080807 A 5753 SKIN DOUG DC8 DC871F 302199D WP TE FLAP MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK INSPECTION, FOUND RT OTBD FLAP EXHAUST GATE LOWER SKIN HAS IMPROPER REPAIR. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED TREATED AND PRIMED AREA AND REPAIR PA RT. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM. (K) 2 L 7 4 4F RT 4A25 20081117 WP 2008 11 17 IXX2008F00117 1 20080805 A 5320 FITTING DOUG DC8 DC871F 302199D WP CARGO BAY CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 830BX 45973 DURING ROUTINE C-CHECK INSP, FOUND AFT CARGO COMPARTMENT SPLICE FITTING CRACKED AT STA 1040.00-1060.000 LONGERON 31 RIGH T. REMOVED CRACKED SPLICE FITTING. FABRICATED SPLICE FITTING. PERFORMED NDT INSP. NO CRACK, NO CORROSION FOUND. CLE ANED, TREATED AND PRIMED AREA AND SPLICE FITTING. INSTALLED NEW SPLICE FITTING IAW SRM. (K) 2 L 7 4 4F RT 4A25 20081118 EA 2008 11 18 ASOA200801485 1 20081109 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 753EV 10169 CABIN OVERHEAD EMERGENCY LIGHTS OUT. 2 L 7 2 4F RT A21EA 20081118 NM 2008 11 18 2008UALA06417 1 20081107 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT PIT FRAME DENTED STA 1360, STR 25R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED A DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 08FDEA04890 1 20081115 A 5320 6557570 SUPPORT BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 EDGE SUPPORT PANEL, BS 1030 TO BS 1166, LBL 19 TO LBL28, UPPER AND LOWER SURFACES CORRODED EDGE SUPPORT FOUND TO BE OUT OF LIMITS REF SRM 53-10-1 PGS 30-31. FABRICATED NEW EDGE SUPPORT REF 65-57570 65-57568. TREATED AND PRIMED NEW EDGE SU PPORT REF SRM 51-10-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081118 EU 2008 11 18 2008UALA06429 1 20081108 A 5320 SHEAR PLATE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 404UA 450 RIGHT AFT SHEAR PLATE CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. REPLACED RT AFT SHEAR PLATE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081118 NM 2008 11 18 08FDEA04773 1 20081106 A 5320 141N517030 FLOOR SUPPORT BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 FWD MAIN CABIN LT, INTERCOSTAL PLATE ABOVE FLIGHT CONTROL PULLEYS AT LBL 24.75 BS 333.45 AND STA 350.00 IS CORRODED. RE MOVED AND REPLACED FLOOR SUPPORT P/N 141N5170-30 IAW SRM 51-40-02 FROM STA 324.0 - 345.0 LBL 24.75 "A" MAJOR REPAIR NO F OLLOW-UP REQUIRED. 2 L 7 2 4F RT A2NM 20081118 2008 11 18 2008UALA06509 4 20081114 A 2310 HF COMM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE INTERFERENCE A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 663UA 27160 HF INTERFERENCE FAULTS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081118 NM 2008 11 18 2008UALA06446 1 20081109 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 EMERGENCY EXIT LIGHTS INOP UPPER DECK CEILING BS 660 CL & BS 690 RT. REPLACED BATTERY PACKS, OP CHECK OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081118 NM 2008 11 18 2008UALA06449 1 20081109 A 3397 80172424 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN LOOSE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 227UA 30555 EEL LIGHTS ON SEATS 41C&G, 42C&G, 43C&G ARE INOPERATIVE DURING TEST OF LIGHTING. CONNECTED LOOSE CONNECTOR, CHECKS OKA Y. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081118 NM 2008 11 18 2008UALA06469 1 20081107 A 3030 RELAY BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE PITOT HEAT FAILED A UALA D RETURN TO BLOCK J WARNING INDICATION IN INSP/MAINT 1 WP 29 794UA 26953 HEAT PITOT C MSG AFTER START. STATUS MSG - HEAT PITOT C - MAINT MSG 30-36122. REPLACED PROBE HEAT SENSOR RELAY. CHECK ED OPS OKAY. NO STATUS MSG ON EICAS. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081118 EU 2008 11 18 2008UALA06470 1 20081109 A 5210 THRESHOLD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 404UA 450 RT DOOR 2R THRESHOLD CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. STARTED REMOVING FASTENERS. REMOVED DOOR SILL AND STARTED TO MFG NEW SILL. INSTALLING FASTENERS. CONTINUED INSTALLING FASTENERS AND MFG NEW FWD SPLICE ANGLES. INS TALLING FASTENERS, STILL. COMPLETED INSTALLING NEW THRESHOLD PAN. 2 L 7 2 4F 4 F RT A28NM E40NE 20081118 NM 2008 11 18 08FDEA04784 1 20081107 A 5320 652273535 WEB BOEING 727 7272D4 138407U NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 PASSENGER CABIN FLOOR WEB BS 1110 - 1130 LBL 69 FWD OUTBOARD FASTENER HAS CORROSION AROUND IT FABRICATED NEW FLOOR WEB IAW DWG 65-22735-35. INSTALLED NEW FLOOR WEB IAW SRM 51-30-02 PG 5. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081118 EU 2008 11 18 08FDEA04785 1 20081107 A 5311 A53833131204 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS GOUGE ON FRAME 54 3 INCHES BELOW STR 12R. BLENDED AREA IAW SRM 51-73-10, FOUND WITHIN LIMITS. HFEC IAW SRM 51-10-08 PT6, NO CRACKS FOUND. TREATED AND PRIMED IAW SRM 51-23-20. 2 L 7 2 4F RT A35EU 20081118 NM 2008 11 18 08FDEA04847 1 20081111 A 5347 65C26010 SEAT TRACK BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 MAIN CABIN FLOOR CORROSION ON SEAT TRACK FLANGE AROUND FASTENER HOLES STA 560-640 LBL 23 REMOVED CORROSION AT BS 560, RE MOVED .030 AREA 1 INCH BY 1 INCH, BS 610 REMOVED .047 AREA 1 INCH BY 1 INCH AND BS 620 REMOVED .045 AREA 1 INCH BY 1 INC H ORIGINAL MATERIAL THICKNESS .100" FOUND OUT OF LIMITS IN ALL 3 AREAS OF MAIN SEAT TRACK FLANGE LBL 23 IAW SRM 53-10-1 DETAIL V. REPLACED SEAT TRACK BS 530-690 LBL 25 IAW SRM 51-30-02 AND DRAWING 65C26010. THIS IS CLASSIFIED AS A MAJOR R EPAIR. 2 L 7 3 4F A3WE 20081118 NM 2008 11 18 08FDEA04523 1 20081024 A 5322 69208132 SHEAR TIE BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 AFT PIT BS 1130 SHEAR TIE HAS CORROSION ON LOWER FLANGE BETWEEN S27L AND 28L. FABRICATED SHEAR TIE. REMOVED AND REPLAC ED SHEAR TIE REF DWG 69-20813, SRM 51-30, OLD SHEAR TIE WAS BLENDED OUT OF LIMITS. ORIG "T" .050', .042 INCH REMAINING .008' MAT LOSS. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081118 NM 2008 11 18 08FDEA04524 1 20081024 A 5340 69441043 STRINGER CLIP BOEING 727 7272D4 138407U NM ZONE 100 CRACKED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 AFT PIT BS 1130 S27L STRINGER CLIP SPLIT REMOVED, FABRICATED, TREATED, PRIMED AND INSTALLED STR CLIP REF SRM 51-30-02, 5 1-10-2 AND BOEING DWG 69-44104. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081118 NM 2008 11 18 DHLA2008745672 1 20081107 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 100 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 FRAME CRACKED IN FWD/LWR CARGO COMPARTMENT AT BS 600, BETWEEN STR 27R AND 28R. REMOVED, FABRICATED NEW FRAME SECTION, A ND INSTALLED PER SRM 53-10-2 FIG 3, 51-10-1, AND 51-30-2, REF N/R 1-242. 2 L 7 3 4F A3WE 20081118 NM 2008 11 18 08FDEA04900 1 20081117 A 5340 69488512 SUPPORT BRACKET BOEING 727 7272D4 138407U NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 MLG WW KEEL BEAM INTERIOR, UPPER BLEED DUCT RT SUPPORT BRACKET IS CRACKED BS 950. REPLACED UPPER BLEED DUCT RT SUPPORT BRACKET BS 950 MLG WW KEEL BEAM INTERIOR IN ACCORDANCE WITH BOEING DRAWING 69-48851 AND SRM 51-20-01 AND 51-30-02. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081118 NM 2008 11 18 2008UALA06476 1 20081110 A 5420 ANGLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 PYLON DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 642UA 25092 NR 1 PYLON MIDSPAR FITTING CLOSE-OUT ANGLE, 2 EACH INBOARD FASTENER HOLES ARE ELONGATED IN PREVIOUS REPAIR AREA. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING REPAIR ANGLES AND FABRICATED A NEW REPAIR DOUBLER AND TRIPLER ANGLE. BOTH HOLES MEASURE .531 INCH AND WITHIN LIMITS OF THIS REPAIR CRITERIA. 2 L 7 2 4F 4 F RT A1NM E24NE 20081118 NM 2008 11 18 08FDEA04862 1 20081112 A 5320 65672313 STIFFENER BOEING 727 7272D4 138407U NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FWD PIT DOOR CUTOUT FWD FRAME CLOSURE WEB FWD LOWER ANGLE STIFFENER CRACKED AT 4 LOWER INTERCOSTAL CUTOUTS BS 555. RE MOVED CRACKED STIFFENER, FABRICATED NEW STIFFENER, BACK DRILLED TRIMMED TO FIT. ALSO, FABRICATED NEW FRAME CLIP FOR NEW STIFFENER, CLASSIFIED AS A MINOR REPAIR. ALSO, FABRICATED DOUBLER FOR NEW END OF STIFFENER FOR ALIGNMENT OF HOLES, R EF DWG 65-67231, DWG 69-4745-3, AND SRM 51-40-3P 2-6. 2 L 7 3 4F A3WE 20081118 WP 2008 11 18 08FDEA04865 1 20081112 A 5711 SPAR CAP DOUG MD10 MD1010F 3022112 WP RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 46631 APPROX 2.75 INCH CRACK EXISTS IN RT WING LOWER SPAR CAP (PSE 57.10.008 ) AT XORS = 411. CRACK RUNS FROM AFT EDGE OF SPA R CAP AFT TANG, FWD APPROX 1.625 INCH TO RADIUS, THEN UPWARDS AND INBOARD APPROX 1.125 INCH AND TERMINATES AT VERTICAL L EG FASTENER AT APPROX = 410. 2 L 7 3 4F RT A22WE 20081118 EA 2008 11 18 SWIA200820333 1 20080731 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 698BR 7799 DURING C-CHECK, RIGHT ENGINE THRUST MOUNT CORRODED, REPLACED. 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 SWIA200820362 1 20081107 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 448SW 7678 FLT 4762 - RIGHT SIDE REINFORCEMENT ANGLES AT FS 640 CRACKED. REPAIRED PER SB 601R-53-061. 2 L 7 2 4F RT A21EA 20081118 NM 2008 11 18 08FDEA04851 1 20081111 A 5321 656724516 FLOOR PANEL BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 PANEL RACK, AFT PIT FLOOR PANEL SPLICE AT BS 1035 BOTTOM SURFACE CORRODED BLENDED CORROSION. ORIGINAL MATERIAL .125 MA TERIAL LOSS OF .030 REMAINING .095, FOUND OUT OF LIMITS REF SRM 53-10-1 PG 30-3. FABRICATED NEW SPLICE PLATE P/N BAC151 1-3795 2024-T3. TREATED AND PRIMED REF BOEING DWG 65-67245, SRM 51-10-2 AND MM 51-20-151-7. THIS IS CLASSIFIED AS A MI NOR REPAIR. 2 L 7 3 4F A3WE 20081118 NM 2008 11 18 08FDEA04691 1 20081104 A 5315 651634567 FLOORBEAM BOEING 727 7272D4 138407U NM ZONE 200 CORRODED A FDEA O OTHER O OTHER NR NOT REPORTED 1 CE 21 287FE 21849 PASSENGER CABIN FRAME STA 1090-LBL 68-1 1/2 INCH UP FROM FLOOR CORRODED. REMOVED FRAME CORROSION, FOUND OUT OF LIMITS. ORIGINAL "T" 0.063, LOSS .035, REMAINING .028. FABRICATE REPAIR PARTS, ANGLE AND FILLER AND SUPPORT ANGLE (CLIP), ALOD INED AND PRIMED PARTS. REPAIR ANGLE, RADIUS FILLER AND SUPPORT ANGLE. INSTALLED REPAIR FRAME AND SUPPORT ANGLE (CLIP) REF SRM 51-30-2, 53-10-1, 53-10-2, 51-40-3 DWG 65-58636. THIS IS CLASSIFIED AS A MAJOR REPAIR GMM 6-2-100 PG 2-3. 2 L 7 3 4F A3WE 20081118 EA 2008 11 18 SWIA200820336 1 20080801 A 5210 INTERCOSTAL CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 668CA 10162 C-CHECK, PASSENGER DOOR AFT INTERCOSTAL CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081118 NE 2008 11 18 08FDEA04881 2 20081010 A 7200 ENGINE AIRBUS 310 A310 EU PWA JT9 JT9D* NE NR 2 FAILED A FDEA F A ACTIVATE FIRE EXT. UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 CE 21 453FE 47009 267 715410 ENG NR 2 FAILURE DURING CLIMB-OUT. CLIMB POWER PASSING 1800 FT, FELT SHUDDER, HEARD A BANG, HAD YAW. COMPLETED SINGLE ENGINE LANDING. NO SMOKE OR FIRE. PULLED NR 2 ENG FIRE HANDLE AND AGENT 1 DISCHARGED. EGT SPIKE TO 780. R AND I NR 2 ENGINE AND PERFORMED ADJUSTMENT AND TEST PER MM 71-00-00-4 FOUND SATISFACTORY. R AND I NR 2 ENG FIREX AGENT 1 BOTTLE P ER MM 26-21-15-4 AND TEST OK. PERFORMED ENG RUN PER A310 JRH ALL PARAMETERS NML. 2 L 7 2 4F 4 F RT A35EU E20EA 20081118 EA 2008 11 18 SWIA200820338 1 20080801 A 5300 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 668CA 10162 C-CHECK, RADIUS CRACKED ON STRUCTURE NEXT TO ADG PUMP. REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20081118 EU 2008 11 18 08FDEA04734 1 20081105 A 5321 R532B366400000 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 FLOOR PANEL 231 NH IS CRACKED. FABRICATED NEW PANEL FROM STOCK MATERIAL, INSTALLED INSERTS, POTTED EDGES, APPLIED NONSK ID, PART ID MARKED IAW SRZ 25-005 REV G. 2 L 7 2 4F RT A35EU 20081118 EU 2008 11 18 2008UALA06483 1 20081111 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DENTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 423UA 504 APPROX STA 1325 FRAME 74 + 5 INCHES, 10 INCHES TO THE RIGHT OF THE BELLY CENTER LINE IS DENTED. DRESSED OUT DENT, NDT I NSP FOR FURTHER DAMAGE INSIDE AND OUTSIDE OF SKIN, NO CRACKS DETECTED. PAINT TO MATCH REWORK AREA. 2 L 7 2 4F 4 F RT A28NM E40NE 20081118 EU 2008 11 18 08FDEA04736 1 20081105 A 5321 R532B372400200 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 FLOOR PANEL 241 NK IS CRACKED. FABRCATED NEW PANEL FROM STOCK MATERIAL, INSTALLED INSERTS, POTTED EDGES, APPLIED NONSKI D, PART ID MARKED IAW SRZ25-005 REV G. 2 L 7 2 4F RT A35EU 20081118 NM 2008 11 18 08FDEA04889 1 20081115 A 5320 65282885 ANGLE BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 MAIN CARGO BAY, GILL LINER MOUNT FRAME CRACKED AT AFT BULKHEAD TOP RT CORNER, FS 1176, 27, WL 292. FABRICATED AND INSTA LLED NEW ANGLE REF DRW 25FX1253, SRM 51-30-02 PG 1-12, SRM 51-10-2 PG 7, MM 51-20-151-7 PG 1, THIS IS CLASSIFIED AS A MI NOR REPAIR. 2 L 7 3 4F A3WE 20081118 WP 2008 11 18 08FDEA04787 1 20081107 A 5320 AJC73727 ANGLE DOUG DC10 DC1030F 3023504 WP ZONE 200 CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 AFT FUSELAGE COMPT INTERNAL FOUND CRACK ON ANGLE. 2 L 7 3 4F RT A22WE 20081118 EU 2008 11 18 08FDEA04742 1 20081105 A 5321 R532B375800005 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 FLOOR PANEL 241 LK IS CRACKED. FABRICATED NEW PANEL FROM STOCK MATERIAL, INSTALLED INSERTS, POTTED EDGES, APPLIED NONSK ID, PART ID MARKED IAW SRZ 25-005 REV G. 2 L 7 2 4F RT A35EU 20081118 NE 2008 11 18 2008UALA06485 2 20081110 A 7200 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 MALFUNCTIONED A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 598UA 28751 727116 STRONG ODOR - OIL SMELL ON TAKEOFF DISSIPATED ON CLIMBOUT. REPLACED NR 2 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 2008UALA06488 1 20081109 A 2421 729825M IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE FAULTY A UALA D RETURN TO BLOCK W INADEQUATE Q C NR NOT REPORTED 1 WP 29 547UA 25368 R GEN DRIVE FAULTY. REPLACED RIGHT ENGINE IDG. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 2008UALA03158 1 20080602 A 2913 6613304 PUMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HYDRAULIC SYS MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 777UA 26916 HYD PRESS PRI C1 LOW CENTER SYSTEM HYDRAULIC PRIMARY PUMP NR 1 PRESSURE OR PUMP SWITCHED OFF. ADVISORY MSG-2912015 LATC HED ER MODE MSG-2912015 LATCHED ERR MODE -. REPLACED C1 PUMP. REPLACED & CONNECTED DM29304A & PINS, CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081118 EU 2008 11 18 08FDEA04745 1 20081105 A 5321 R532B372700200 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 FLOOR PANEL 241 QJ IS CRACKED. FABRICATED NEW PANEL FROM STOCK MATERIAL, INSTALLED INSERTS, POTTED EDGES, APPLIED NONSK ID, PART ID MARKED IAW SRZ 25-005 REV G. 2 L 7 2 4F RT A35EU 20081003 NM 2008 10 3 2008UALA05682 1 20080912 A 4920 CONTACTOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE APU DAMAGED A UALA O OTHER W INADEQUATE Q C DE DESCENT 1 WP 29 670UA 29240 APU NO ROTATION NO EGT NO START ABOVE FL300 AND NO START AT FL200 EITHER. REPLACED APU CRANK CONTACTOR AND APU ECU. 2 L 7 2 4F 4 F RT A1NM E24NE 20081003 2008 10 3 ASAA0853481 4 20080909 A 2210 POSITION SENSOR BOEING 737 737890 1384527 NM SPOILER OUT OF ADJUST A ASAA K NONE N FALSE WARNING IN INSP/MAINT 1 NM 02 583AS 35681 AUTOPILOT HAD SPOIL 4 SIQ FAILURE INDICATION. ADJUSTED SPOILER POSITION SENSOR. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 ASAA0853479 1 20080907 A 4940 28B5457 STARTER GEN BOEING 737 737890 1384527 NM APU MALFUNCTIONED A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 584AS 1385 35682 MAINTENANCE ANNUNCIATOR ILLUMINATED UPON APU SHUTDOWN. REPLACED STARTER GENERATOR AND STARTER POWER UNIT. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 KPV2008F00001 1 20080911 A 2611 3023145 SMOKE DETECTOR DHAV DHC8 DHC8103 1386005 NM PWA 120 PW120 NE AFT CARGO BAY MALFUNCTIONED A KPVA O OTHER O OTHER NR NOT REPORTED 1 WP 13 808WP 026 ON APPROACH, "SMOKE" WARNING LIGHT CAME ON, REMAINED ON FOR 3 SECONDS THEN WENT OUT. AFTER LANDING LIGHT CAME ON AGAIN T HEN WENT OUT AFTER A FEW SECONDS. VISUALLY INSPECTED NR 1 AND NR 2 SMOKE DETECTORS, NO DEFECTS NOTED. PERFORMED OPS CHEC K OF SMOKE DETECTION SYSTEM GOOD IAW MM 26-12-00, PG 201. (K) 2 H 7 2 4T 4 T RT A13NM E20NE 20081003 NM 2008 10 3 CALA0800878 1 20080911 A 5311 6546552 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 827 FRAME IS CRACKED AT AC SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. REPAIRED FRAME PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 CALA0800879 1 20080911 A 5311 6546548 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 747 FRAME IS CRACKED AT AC SUPPORT BRACKET BETWEEN STRINGERS 8L & 9L. REPAIRED PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081003 WP 2008 10 3 MWE2008F00038 1 20080827 A 3397 WIRE DOUG DC9 DC981 3022081 WP EMERGENCY LIGHT BROKEN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 803ME 48029 EMERGENCY FLOOR LEVEL LIGHTS OUT ROW 5-8. FOUND BROKEN WIRE AND REPAIRED. (K) 2 L 7 2 4F A6WE 20081003 NM 2008 10 3 SWAA085033 1 20080914 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 25R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085040 1 20080914 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 344, STR 5L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085046 1 20080914 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787 STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085047 1 20080914 A 5340 65C27314 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CORRODED AT BS 787, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085050 1 20080914 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 16R. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085051 1 20080914 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 540, STR 26L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085052 1 20080914 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 15R. REMOVED AND REPLACED STRINGER CLIP PER SR M. 2 L 7 2 4F RT A16WE 20081003 EA 2008 10 3 COMA0880015 1 20080903 A 5240 DOOR CNDAIR CL600 CL6002D24 1390016 EA EXTERNAL POWER OPEN A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 678CA 15125 AFTER T/O LOUD NOISE COMING FROM NOSE AREA, SUSPECTED EXTERNAL ACCESS PANEL LEFT OPEN. EMERGENCY DECLARED, A/C RETURNED BACK TO IAH AND LANDED SAFELY. INSPECTED A/C AND FOUND EXT PWR RECEPTACLE DOOR OPEN. INSPECTED DOOR NO DEFECTS NOTED, CLOSED DOOR. 2 L 7 2 4F RT A21EA 20081003 EA 2008 10 3 COMA086382 1 20080903 A 3234 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 27 926CA 29515 7027 ON APPROACH INTO EWR SELECTED GEAR DOWN AND RECEIVED GEAR DISAGREE WARNING MSG FOR NOSE GEAR. EMERGENCY DECLARED, FOLLO WED QRH PROBLEM RESOLVED. ACFT LANDED SAFELY. R&R NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 20081003 EA 2008 10 3 HNAA0800256 1 20080612 A 2540 82540016101 ANGLE DHAV DHC8 DHC8311 1386006 EA LAVATORY CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 335EN 32270 375 CORROSION FOUND ON THE RT SIDE OF LAV, BOTTOM ANGLE. REPLACED ANGLE. 2 H 7 2 4T RT A13NM 20081003 NM 2008 10 3 2008UALA03115 1 20080602 A 2750 FLAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU WING MALFUNCTIONED A UALA A UNSCHED LANDING W F INADEQUATE Q C FLT CONT AFFECTED CR CRUISE 1 WP 29 318UA 23950 FLAP RETRACT PROBLEM CAUSED DIVERSION. UNABLE TO DUPLICATE. ADJUSTED CABLE TENSION AND SERVICED NR 7 FLAP TRANSMISSION . 2 L 7 2 4F 4 F RT A16WE E21EU 20081003 NM 2008 10 3 2008UALA05628 1 20080907 A 2432 263BC1012 CHARGER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE APU INOPERATIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 799UA 26926 STATUS MESSAGE APU. APU BATTERY AND CHARGER INOP, NEEDS REPLACEMENT. CHARGER NOT CHARGING. FOUND APU BATTERY & CHARGE R INOP. REPLACED APU BATTERY & APU BATTERY CHARGER. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081003 NM 2008 10 3 2008UALA05673 1 20080910 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 BULK CARGO COMPARTMENT AT STA 1562 BETWEEN STR 39R AND 39L, SHEAR TIE HAS CORROSION AROUND DRAIN HOLE AFT SIDE. MAJOR R EPAIR ACCOMPLISHED. REPLACED SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081003 NM 2008 10 3 2008UALA05735 1 20080915 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 791UA 26933 EMERGENCY LIGHT AT SEAT 25C WILL NOT WORK. LIGHT FOUND INOP. REPLACED LAMP. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081003 EU 2008 10 3 2008UALA05744 1 20080916 A 2820 6441009 VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUEL SYSTEM MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 446UA 834 TRIM & FUEL BALANCE PROBLEM. FLIGHT DIVERTED. FOUND AIR RELEASE VALVE AT FAULT. PERFORMED SEVERAL FUEL TRANSFER CHECK S, CHECKED ALL FLIGHT CONTROL ROD ENDS, REPLACED AIR RELEASE VALVE, ALL TESTS CAME BACK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 SO 2008 10 3 C2XA08RI145 1 20080922 A 3320 BR90002 BALLAST EMB 145 EMB145LR 3260212 SO CABIN BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 13964 145123 FLIGHT 3053 - EWR - FLIGHT CREW REPORTED A STRONG ELECTRICAL/HOT PLASTIC SMELL NEAR SEAT 1A ASSOCIATED WITH OVERHEAD PAN EL. EWR MX REMOVED AND REPLACED BALLAST AT ROW 1A AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081003 NM 2008 10 3 2008UALA05902 1 20080929 A 2612 8243 FIRE LOOP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 3 ENGINE FAULTY A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 120UA 29166 ENG 3 FIRE LOOP-B MSG. REPLACED NR 3 ENGINE UPPER AFT FIRE LOOP A&B ASSY TS681. FIRE TEST PASSES NO FAULTS. 2 L 7 4 4F 4 F RT A20WE E24NE 20081003 NM 2008 10 3 2008UALA05903 1 20080928 A 5754 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L/E FLAP DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 572UA 26682 METAL SKIN PEELING BACK ON UPPER SURFACE OF L/E FLAP JUST INBOARD OF RIGHT PYLON. REMOVED AND REPLACED SLAT NR 6 WITH S ERVICEABLE UNIT. 2 L 7 2 4F 4 F RT A2NM E17NE 20081121 NM 2008 11 21 DL76G081503 1 20081106 A 2130 3209953 VALVE BOEING 767 767332 1382001 NM WARNING LIGHT A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 173DZ 29692 P1191* AFTER SECOND ENGINE START NR 2 ENG, FWD EQUIPT VAL EICAS MSG WITH ASSOCIATED VALVE LIGHT ON EQUIPMENT COOLING PANEL. WEN T TO STANDBY, NO HELP. RETURN TO GATE. VALVE LIGHT AND EICAS MSG WENT OUT WHEN NR 1 ENG SHUT DOWN. FWD TO MCO AND PLA CARD PER MEL 21-58-07. VALVE LOCKED CLOSED T/S FWD EQUIP VALVE MSG PER FIM. NO FAULTS FOUND. EQUIPMENT COOLING SYS CK S GOOD. 2 L 7 2 4F RT A1NM 20081121 NM 2008 11 21 SWAA086288 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B STR 9R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086299 1 20081118 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 UALA2008111302712 1 20080511 A 4930 388250017 FCU BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU FAULTY A UALA D RETURN TO BLOCK W J INADEQUATE Q C WARNING INDICATION IN INSP/MAINT 1 WP 29 647UA 25284 RTBL WITH A AUXILIARY POWER UNIT DOOR MESSAGE. RECURRED ON FLT 0907-11. REPLACED FUEL CONTROL UNIT. ACCOMPLISHED INSP ECTION AS PER MM. ALL OPS AND INDICATIONS NORMAL, LEAK CHECK GOOD. ACCMP VERIFICATION FLIGHT. 2 L 7 2 4F 4 F RT A1NM E24NE 20081121 NM 2008 11 21 UALA2008111302896 1 20080519 A 5512 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HORIZ STAB DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 213UA 30219 LIGHTNING STRIKES LT HORIZ STAB UPPER SURFACE, INBOARD END. FOUND LIGHTNING STRIKES. ACCOMPLISHED PERMANENT REPAIR PER SRM 51-20-06. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081121 WP 2008 11 21 IXXA08SMN154S 1 20080418 A 5542 SKIN DOUG DC8 DC871F 302199D WP ZONE 300 CANNING A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND LT RUDDER SKIN OIL CANNING AT STATION ZR 168.656. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, BONDED DOUBLER. BONDED BOTH PARTS AS NEEDED. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE. FOUND WITHIN TOLERANCE, MOMENT=2549.7 INCH/POUNDS. INSTA LLED NEW FASTENERS AND REPAIR PARTS IAW SRM 55-6-1 FIGURE 1, SRM 55-1-0 PAGE 1 AND 51-1-21, SRM 55-6-1 FIGURE 1 ITEM "A" , SRM 51-1-9 T/R NUMBER 51-142, 51-1-9A T/R NUMBER 51-141, 51-1-8B, SRM 51-1-11, 51-1-21, AND SRM 51-4-5 PAGES 1-5. 2 L 7 4 4F RT 4A25 20081121 WP 2008 11 21 IXXA08SMN155S 1 20080418 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 1755 LONGERON 35.5 RT. REMOVED FASTENERS AS NEED ED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND CORROSION FOUND. FABRICATED REPAIR DOUBLER, FILLER, FINGER DOUBLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS . INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08197 DATED 04/25/08, SEMAN DRAWING ED-4775 DATED 04/22/08, SRM 51-1-21, 51-1-20D, NDT SPM PART 06-10-01-001, SRM 51-1-8B, SRM 51-1-11, AND 51-3-1. 2 L 7 4 4F RT 4A25 20081121 SO 2008 11 21 CHQA200800218 1 20081107 A 3350 RPS1B BATTERY PACK EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL EMERGENCY LIGHTS DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 292SK 15797 12478 145488 CAE311794 DURING INSPECTION THE AFT EMERGENCY LIGHTS WERE FOUND TO BE INOP. THE NR 4 EMERGENCY LIGHT BATTERY WAS REPLACED AND THE EMERGENCY LIGHTS FUNCTIONED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081119 WP 2008 11 19 AALA200810139 1 20081027 A 5313 LONGERON DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 LONGERON L2 CRACKED AFT OF STATION 1418. INSTALLED LONGERON SPLICE REPAIR PER AMERICAN AIRLINES REPAIR DOCUMENT 53-30-0 0-2. 2 L 7 2 4F A6WE 20081119 NM 2008 11 19 AALA200802705 1 20081008 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 664AA 25298 DFW - EMERGENCY LIGHTS AT SEAT ROWS 27 TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR INOPEATIVE EMERGENCY LIGHTS AT SEAT ROWS 27 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081003 SO 2008 10 3 F2P2008F00001 1 20080924 A 8011 HOUSING PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2B 41979 EA HARTZL HCE3Y HCE3YR2 GL STARTER CRACKED E F2PA K NONE O OTHER IN INSP/MAINT 1 SO 19 684JJ 174 317952194 L270168A DJ8842A RT ENGINE FAILED TO START ON GROUND. FOUND REAR OF STARTER MOTOR HOUSING WITH 2 INCH X 2 INCH HOLE LOCATED AT THE BRUSH HOUSING. (K) 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 20081003 NM 2008 10 3 2008UALA05654 1 20080908 A 5330 SKIN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 815UA 867 PREVIOUS SKIN BLEND AT FRAME 2 STR 23R OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05672 1 20080910 A 5420 WEB BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 NACELLE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 NR 2 PYLON NAC STA 180 (APPROX) RIGHT SIDE, UPPER WEB CRACKED INTO RIVET HOLE. MAJOR REPAIR ACCOMPLISHED. REMOVED OLD DOUBLER. INSTALLED NEW DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081003 NM 2008 10 3 2008UALA05676 1 20080910 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT ROW 58 LT INOP. FOUND LAMP INOP. REPLACED LAMP, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081003 NM 2008 10 3 2008UALA05666 1 20080907 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT ENGINE FAULTY A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION IN INSP/MAINT 1 WP 29 213UA 30219 RIGHT IDG HAS BLOCKED MESSAGE ON EICAS CHAPTER 24 MAINTENANCE PAGE. IDG FOUND FAULTY. REPLACED IDG. OP CHECK & LEAK C HECK GOOD. RESERVICED RT IDG. OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081003 WP 2008 10 3 UPS08853324 1 20080910 A 2120 CLAMP DOUG DC8 DC873F 302199F WP A/C BAY DISCONNECTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:N/A UNABLE TO MAINTAIN PRESSURIZATION. FOUND LEFT CLAMP PACK DISCONNECTED PERFORMED DECAY CHECK PER AMM 21-31-00-2. ALSO PERFORMED COOLING PACK ADJUSTMENT TEST 21-55-00-5. 2 L 7 4 4F RT 4A25 20081003 NM 2008 10 3 UPS08M53325 1 20080911 A 3620 WARNING SYSTEM DOUG MD11 MD11F 3023600 NM COCKPIT ACTIVATED A IPXA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 01 260UP 48418 INSPECTION TYPE:N/A ATB - IFSD - CREW OBSERVED A LEVEL 3 ALERT "AIR MANIFOLD 2 FAIL AND QRH/AOM PROCEDURES REQUIRED REDU CING ENGINE TO IDLE. DECLARED EMERGENCY AND RETURNED TO ALA. PERFORMED ESC READOUT; TAIL PYLON Z15OVHT FIM 36-23-03-02 STAP 1;4;6;7. PERFORMED LEAK CHECK Z15. NO LEAKS. DECAY CHECK MAN 2 PERFORMED CHECK FAULT AMM 36-00-01. RTS PERFORM ED AT ESC, MFS PSC 1/2 PASSED. A/C DISP PER MEL 36-23-1-0-1. 2 L 7 3 4F RT A22WE 20081003 NM 2008 10 3 SWAA085029 1 20080912 A 2761 6567179 FITTING BOEING 737 7373H4 1384600 NM NR 5 SPOILER LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 GROUND SPOILER OUTBOARD ACTUATOR FITTING LOOSE. REPAIRED FITTING PER SWA EA. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085032 1 20080914 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 908, STR 20R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085054 1 20080914 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 15L. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 2008UALA05906 1 20080927 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EMERGENCY EXIT EEL LIGHTS INOP ALL RIGHT SIDE OF FIRST CLASS SEATS. LIGHT INOPERATIVE. REPLACED BATTERY. EEL LIGHTS O PS CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081003 NM 2008 10 3 2008UALA05908 1 20080927 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EMERGENCY EXIT EEL LIGHT INOP ACROSS DOOR 1 RIGHT LOWER WALL EEL. LIGHT INOPERATIVE. REPLACED BATTERY. OPS CHECKS NOR MAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081003 NM 2008 10 3 2008UALA05909 1 20080927 A 3350 20131A POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 LEFT OVERWING EXTERIOR EMERGENCY LIGHTS INOP TWO MOST FWD LIGHT ASSY'S. LIGHTS FOUND INOP. REPLACED POWER SUPPLY ASSY. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081003 EU 2008 10 3 2008UALA05910 1 20080927 A 3350 20131A BATTERY PACK AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 490UA 1728 EMERGENCY LIGHT TEST FAULTS FWD BATTERY PACK. BATTERY PACK FOUND FAULTY. REPLACED BATTERY PACK. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05911 1 20080927 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 UPPER FUSELAGE AT STA 1197 + 88 SHEAR TIE BETWEEN STR 1L AND STR 1R HAS DOUBLED DRILLED HOLE. MAJOR REPAIR ACCOMPLISHED . REMOVED DAMAGED SHEAR TIE. FABRICATED & INSTALLED A NEW SHEAR TIE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081003 NM 2008 10 3 2008UALA05916 1 20080927 A 5420 ATTACH ANGLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 STRUT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 646UA 25283 NR 2 STRUT AFT STRUT BULKHEAD INBOARD ATTACH ANGLE CRACKED. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED ANGLE. FABRICA TED & INSTALLED NEW ANGLE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081003 NM 2008 10 3 2008UALA05917 1 20080927 A 5210 F1314 SPRING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE R2 DOOR WEAK A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 646UA 25283 DOOR R2 DOOR DEPLOYMENT BAR GAS SPRING WEAK. SPRING FOUND INADEQUATE. REPLACED GAS SPRING. OPS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081003 NM 2008 10 3 2008UALA05918 1 20080927 A 5210 F1314 SPRING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE R1 DOOR WEAK A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 646UA 25283 DOOR R1 DEPLOYMENT BAR GAS SPRING WEAK. GAS SPRING DEFECTIVE. REPLACED DEPLOYMENT BAR GAS SPRING. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081003 NM 2008 10 3 2008UALA05919 1 20080927 A 2997 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HYDRAULIC SYS ARCED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 646UA 25283 CENTER SYS NR 1 ACMP CONNECTOR D482 SHOWS SIGNS OF ARCHING AND HAS A RECESSED PIN. REPLACED CONNECTOR D482P. OPS CHECK S GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081003 NM 2008 10 3 2008UALA05921 1 20080927 A 7920 ACC434F65 OIL FILTER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT ENGINE DEFECTIVE A UALA E ENGINE SHUTDOWN J WARNING INDICATION IN INSP/MAINT 1 WP 29 674UA 29242 CREW REPORTS: LEFT ENG OIL FILTER STS MSG AFTER START, AT 26C. BEFORE ENGINE START. ACCOMPLISHED OIL FILTER AND MAG PLU GS INSPECTION AND NO METAL FOUND. REPLACED MAIN OIL FILTER, MOTORED ENG, NO LEAKS FOUND. RAN ENGINE AND OIL FILTER MSG DID NOT APPEAR. OIL PRESS GOOD, SVC ENG OIL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081002 NM 2008 10 2 CALA0800866 1 20080905 A 5230 6546921528 SKIN BOEING 737 7373T0 1384582 NM FWD CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76355 23593 FORWARD CARGO DOOR SKIN FOUND CRACKED UNDER DOOR LINER AT EDGE OF LIGHTENING HOLE 21" FROM TOP 21.5" FROM FORWARD EDGE. REMOVED CRACK AND REPAIRED FORWARD CARGO DOOR INNER SKIN AT LIGHTENING HOLE 21" FROM TOP AND 21.5" FROM FORWARD EDGE PE R SRM 52-30-01 AND SRM 51-70-13. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873509 1 20080909 A 5754 114A54104 SKIN BOEING 737 737790 13844CN NM L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 NR 8 SLAT OUTBOARD END LOWER SURFACE IS CHAFED. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED THE REPAIR IAW B737 700 SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873507 1 20080909 A 5754 114A50404 SKIN BOEING 737 737790 13844CN NM L/E SLAT CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 615AS 30344 NR 5 SLAT LOWER SURFACE IS CHAFED AT INBOARD UPPER CORNER. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED THE REPAIR IAW B737 700 SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0873504 1 20080828 A 5320 FLOOR SUPPORT BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 622AS 30165 AFT CARGO PIT FLOOR SUPPORT T FOUND CORRODED AT BS 887 LBL 9 RBL 22. CORROSION IN AFT CARGO PIT ON FLOOR SUPPORT T BLEN DED OUT AND FOUND BEYOND LIMIT. NEW PART INSTALLED IAW B737 700 SRM 20 50 11. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 ASAA0853488 1 20080913 A 3610 1074847 REGULATOR BOEING 737 737890 1384527 NM NR 1 ENGINE FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 577AS 2562 35186 NR 1 ENGINE HIGH STAGE REGULATOR FAILED ENGINE BLEED AIR SYSTEM HEALTH CK. REMOVED AND REPLACED HIGH STAGE REF IAW 737N G MM 36 11 07 000 801 STEP B&C W MM 36 11 07 400 801 STEP E. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085094 1 20080916 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 439WN 29834 DURING SCHEDULED HC2 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PE R MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085093 1 20080916 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 439WN 29834 DURING SCHEDULED HC2 CHECK, MID CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085092 1 20080916 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 439WN 29834 DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085089 1 20080916 A 5512 182A4001 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 439WN 29834 DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 111. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085084 1 20080915 A 2612 65557055 FIRE DETECTOR BOEING 737 7377H4 1384404 NM MLG W/W FAULTY A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 29 282WN 32534 AIR TURNBACK, AT FL 260 FIRE WARNING LIGHT ILLUMINATED AND FIRE WARNING HORN SOUNDED, WITH W/W FIRE WARNING LIGHT ILLUMI NATED. REMOVED AND REPLACED MLG W/W FIRE DETECTOR PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085083 1 20080916 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 201LV 29854 DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085082 1 20080916 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 699SW 23826 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 765, STR 19R. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085081 1 20080916 A 5310 6545833 CREASE BEAM BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED BRDG CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 324 TO BS 340, LBL 70. REMOVED AND REPLACED WEB PER S RM. 2 L 7 2 4F RT A16WE 20081003 2008 10 3 C8G2008F00017 2 20080903 A 7321 74360205 FCU BOEING 727 727225 1384077 NM NR 1 ENGINE UNSERVICEABLE A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 801EA 22432 SHORTLY AFTER TAKEOFF DURING CLIMB OPERATION THE NR 1 ENGINE SPREAD 28 HIGH AND ALL ENGINE INDICATORS BEGAN TO DECREASE INDICATING A FAILURE. THE ENGINE THEN RELIT DUE TO CONTINUOUS IGNITION BEING ENGAGED. 2 OR 3 MINUTES LATER THE SAME EVEN T OCCURRED. THE AC RETURNED TO ELP WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED. THE NR 1 FUEL CONTROL UNIT, ENGINE DRIVEN FUEL PUMP AND THE P&D VALVE WERE REMOVED AND REPLACED, OPS CHECKS GOOD. NO OTHER DEFECTS WE RE NOTED. AC WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F A3WE 20081003 WP 2008 10 3 CNM2008F00000 1 20080723 A 2910 NAS161210 O-RING DOUG DC10 DC1030 3023501 WP TRANSMITTER DAMAGED A CNMA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 07 620AX 48319 LOST NR 3 HYD SYS FLUID WITH A HYD SYSTEM 3 ELEV OFF LIGHT. FOUND DAMAGED O-RING ON NR 3 PRESS TRANSMITTER REMOVED AND REPLACED O-RING IAW MM 2900. OPS CHECK GOOD. (K) 2 L 7 3 4F A22WE 20081003 SO 2008 10 3 C2X2008F00045 1 20080906 A 3320 BR90002 BALLAST EMB 145 EMB145LR 3260212 SO CABIN LIGHTS SHORTED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 27 12564 145618 DURING APPROACH, THE F/A REPORTED A FAINT ELECTRICAL SMOKE ODOR IN THE FRONT OF THE CABIN. THE AC LANDED WITHOUT INCIDEN T WHERE MAINT INSPECTED THE ACFT AND REMOVED AND REPLACED THE FIRST AND SECOND LIGHT BALLASTS ABOVE SEAT 1A, OPERATIONAL LY CHECKED WITH NO DEFECTS NOTED. AND THE AC WAS APPROVED FOR RETURN TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081003 EU 2008 10 3 2008UALA05923 1 20080928 A 2920 680203037 RAM AIR TURB AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE HYDRAULIC SYS FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 454UA 1104 RAT FAILED RETRACT TEST WITH BLADES TURNED SIDEWAYS. CLEANED BOTH CONNECTORS AND LUBRICATED PLUNGER MECHANISM. THE STOW FUNCTION NOW OPS NORMAL. WILL NOT RETRACT WITH BLADE TURNED. INSPECTION VERIFIED STOW FUNCTION. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 EU 2008 10 3 2008UALA05928 1 20080927 A 2610 DETECTION SYS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO BAY FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 438UA 678 SMOKE - FIRE TEST FAILS FOR CARGO SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05929 1 20080928 A 3510 MC1019101 OXYGEN MASK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 569UA 26677 OXYGEN PRESSURE 480. FOUND LEAK AT FIRST OBSERVER'S O2 MASK. REPLACED & LEAK CHECKED OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081003 EU 2008 10 3 2008UALA05930 1 20080930 A 2910 HYDRAULIC SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN SYS FAILED A UALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 29 473UA 1469 GREEN HYD SYSTEM FAILURE. FLIGHT DIVERTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 WP 2008 10 3 AALA200801929 1 20080722 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9621A 53592 AUS OVERHEAD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 102 FOR OVERHEAD EMERGENCY LIGHTS IN CA BIN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A6WE 20081006 NM 2008 10 6 AALA200802012 1 20080802 A 2934 TRANSMITTER BOEING 767 767323 1385205 NM HYDRAULIC SYSTEM INOPERATIVE A AALA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 397AN 29604 ORD INFLIGHT T96102AUG. CREW REPORTED DURING LANDING GEAR RETRACTION NR 2 CENTER ELECTRIC HYDRAULIC PUMP PRESSURE LIGH T ILLUMINATED. LANDING GEAR WAS SLOW TO RETRACT FOLLOWED BY LT MAIN GEAR DOORS DOWN INDICATION AND GEAR DISAGREE INDICA TIONS. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED HYDRAULIC QUANTITY TRANSMITTER AND MONITOR UNIT. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20081006 NM 2008 10 6 F3LA200800606 1 20080912 A 5330 D5367314400000 PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 930FR 2241 REFERENCE NON-ROUTINE C050859. DURING C3 C-CHECK. INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151FE WAS DAMAGED. MAIN TENANCE REPAIRED DAMAGED FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPA IR. IT WAS INSPECTED AND FOUND ACCEPTABLE. (K) 2 L 7 2 4F RT A28NM 20081006 NM 2008 10 6 AALA200801997 1 20080729 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 696AN 26976 LAX EMERGENCY LIGHTS AT SEAT ROW 26 INOPERATIVE. REPAIRED SHORTED WIRE FOR EMERGENCY LIGHTS AT SEAT ROW 26. SYSTEM GRO UND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20081006 NM 2008 10 6 USAA920081587 1 20080817 A 5311 655287448 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN C19 MAJOR REPAIR NR 6124540 L2 DOORWAY LOWER FORWARD STUB FRAME CRACKED AT BS 957. WL216. LBL60. REPLACED L2 DOORWA Y LOWER FORWARD STUB FRAME AT BS 957, WL216, LBL60 IAW B737 SRM 51-40-02-0G. 2 L 7 2 4F RT A16WE 20081006 2008 10 6 USAA920081577 4 20080704 A 2565 D30665109 SLIDE RAFT AIRBUS A319 A319112 3930323 EU LEFT MALFUNCTIONED A USAA K NONE O OTHER TX TAXI/GRND HDL 1 EA 19 723UW 38462 633 1109 LOG PAGE 8094629 FLT 1897 PIT CLT SLIDE DEPLOYMENT AFTER GATE ARRIVAL IN CLT THE LT REAR SLIDE WAS INADVERTENTLY DEPLOYE D. THE SLIDE DID NOT DEPLOY PROPERLY AND WAS UNUSABLE FOR EVACUATION. ONLY ATTACHED BY ELECTRICAL WIRES. MX R&R THE L T REAR DOOR SLIDE ASSEMBLY. 2 L 7 2 4F RT A28NM 20081006 NM 2008 10 6 USAA920081586 1 20080819 A 5754 65C26601197A SKIN BOEING 737 7373B7 1384580 NM L/E SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 4437 2280 24479 CLT MAJOR REPAIR C4 CHECK NR 5030564 AND 03C0057002/022, LT WING NR 1 SLAT SKIN CRACKED AT INBOARD AUXILIARY TRACK R&R T HE LT WING NR 1 SLAT IAW 737 AMM 27-81-21. 2 L 7 2 4F RT A16WE 20081006 NM 2008 10 6 USAA920081596 1 20080829 A 2560 P2070003001 FLASHLIGHT AIRBUS A319 A319132 3930340 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 802AW 0924 LOGPAGE 8039279 FLT NR 230 MCI PHX EEL AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R&R AFT GALLEY EMERGENCY FLASHLIGHT . OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081006 NM 2008 10 6 USAA920081597 1 20080829 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 819AW 1395 LOGPAGE 8047440 FLT NR 4 ORD PHX EEL OUTBOARD FORWARD FLIGHT ATTENDANT FLASHLIGHT NOT BLINKING. R&R BATTERY. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081006 EU 2008 10 6 USAA920081603 1 20080809 A 5753 6546434301 SKIN AIRBUS 320 A320214 3930316 EU T/E FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 102UW 0844 MCN C19 MAJOR REPAIR NR 6126557 & 6126556 LT HAND INBOARD AFT FLAP DELAMINATED IN 2 PLACES. WBL117 ON LOWER SURFACE, AN D WBL 107 ON UPPER SURFACE. REPAIRED LT HAND INBOARD AFT FLAP IN 2 PLACES. WBL 117 ON LOWER SURFACE, AND WBL 107 ON UP PER SURFACE IAW B737 SRM 51-70-10-2R4. 2 L 7 2 4F RT A28NM 20081006 NM 2008 10 6 USAASB08075 1 20080831 A 3260 PRINTED CKT BOAR BOEING 737 7374B7 1384702 NM LANDING GEAR FAULTY A USAA L A ABORTED APPROACH UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 449US 24893 PIT FLT 1991 ENROUTE PHL TO ORD. ON GEAR RETRACTION THE NOSE GEAR RED LIGHT ILLUMINATED. THE FLIGHT DIVERTED TO PIT. DURING APPROACH, UPON GEAR EXTENSION, THERE WAS INITIALLY A 3 GREEN, DOWN AND LOCKED INDICATION. A FEW MOMENTS LATER, T HE NOSE GEAR GREEN INDICATION EXTINGUISHED, AND THE GEAR HORN SOUNDED. HOWEVER, THE RED GEAR INDICATION DID NOT ILLUMIN ATE. THE FLIGHT DID A FLY BY OF THE TOWER AND AFTERWARDS PROCEEDED TO LAND WITHOUT FURTHER INCIDENT. MX REPLACED PRINT ED CIRCUIT CARDS M983 AND M1214. PERFORMED SEVERAL GEAR SWINGS. OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 20081006 CE 2008 10 6 DXT2008F00006 1 20080912 A 2720 LIMITER CESSNA 750 750 2076810 CE RUDDER MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 901QS 7500102 IN FLIGHT GOT RUDDER LIMIT FAIL B AMBER CAS MESSAGE. CONTROL PAGE SHOWED RUDDER LIMITED TO 44 PERCENT. 2 L 7 2 4J RT T00007WI 20081006 NE 2008 10 6 GLB2008F00023 2 20080904 A 7310 B-NUT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE FUEL LINE LOOSE A GLBA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 21 219GL UE219 PS0072 PILOTS REPORTED IN CRUISE AND DESCENT A STRONG FUEL ODOR IN THE COCKPIT AND CABIN AREA. MAINTENANCE TIGHTENED A LOOSE "B " NUT IN THE FUEL PURGE AREA ON THE NR (1) ENGINE IAW MM 28-20. CLEANED CHECK VALVES ON THE FUEL PURGE SYSTEMS FOR THE RT ENGINE AND LT ENGINE IAW MM 71-70. NO NEW ODORS WERE PRESENT. (K) 2 L 7 2 4T 4 T RT A24CE E26NE 20081006 NM 2008 10 6 F3LA200800607 1 20080912 A 5320 D53673020000000 PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 930FR 15706 REFERENCE NON-ROUTINE C050860. DURING C3-C-CHECK, INSPECTION NOTED THE AFT PIT TRANSITION PANEL 151BE WAS DAMAGED. MAINT ENANCE REPAIRED DAMAGED FLOOR PANEL IAW THE REQUIREMENTS OF A319 SRM 53-02-00, FIGURE 204. UPON COMPLETION OF THE REPAIR , IT WAS INSPECTED AND FOUND ACCEPTANCE. (K) 2 L 7 2 4F RT A28NM 20081006 SO 2008 10 6 C2X2008F00048 1 20080910 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13118 145675 DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT ON THE AFT GALLEY WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLAC ED THE EMERGENCY LIGHT BATTERY AND INVERTER. OPERATIONAL CHECKS WERE GOOD. (K) 2 L 7 2 4F RT 20081006 EA 2008 10 6 C2X2008F00049 2 20080702 A 7250 23074650 ROTOR CESSNA 182 182P 2075816 CE RROYCE AE3007 AE3007A1E 54169 EA HP TURBINE ERODED A C2XA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 27 21145 14192 18261444 CAE312423 THE CREW REPORTED ENGINE NR 1 HP INDICATION IN YELLOW RANGE AFTER TAKEOFF, THE ACFT RETURNED TO DEPARTURE AND LANDED WIT HOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD. SUPPLEMENT TO FOLLOW: C ONDITION REPORT FROM MFG INDICATED HOT SECTION DETERIORATED. THE HIGH PRESSURE TURBINE MODULE EXHIBITED SULFIDATION AND EROSION OF AIRFOILS AS WELL AS A CRACKED COMBUSTION LINER. THE 1ST STAGE HPT VANES EXHIBITED COATING LOSS ON THE AIRFOIL S AND EROSION/CRACKING ON THE AIRFOIL TRAILING EDGES. (BURN-THROUGH) (K) 1 H 7 1 3O 4 F NT TA13 TE6CH 20081006 NM 2008 10 6 DHL2008F00032 1 20080911 A 3150 UNKNOWN BOEING 727 727247 138408F NM OVERSPEED WARN UNKNOWN A DHLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 793DH 21393 DURING TAKEOFF ROLL OVERSPEED WARNING SOUND AT 70 KTS . DEFERRED IAW MEL 34-4-3 PULLED IAW CREW REQUEST. AIRCRAFT WAS G ROUNDED. (K) 2 L 7 3 4F A3WE 20081006 NM 2008 10 6 NWAA084215517 1 20080911 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 517US 23205 DURING THE EMERGENCY LIGHT CHECK AS A PART OF AN OVERNIGHT LINE CHECK, THE ESCAPE SLIDE ILLUMINATION LIGHT AT DOOR 3L FA ILED. MAINTENANCE REPLACED BATTERY PACK POWER SUPPLY M735, ALL OPERATIONS WERE NORMAL AFTER REPLACEMENT OF THE BATTERY P ACK. (K) 2 L 7 2 4F RT A2NM 20081006 NM 2008 10 6 USAA920081605 1 20080808 A 5313 65457768 STRINGER BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT Q6 MAJOR REPAIR NR 03C10853057/002 LEVEL 2 EXFOLIATION CORROSION ON STUB STRINGER AT BS 1008, S27R. REPLACED STUB STRINGER AT BS 1008, S27R IAW B737 SRM 51-10-02 & SRM 51-40. 2 L 7 2 4F RT A16WE 20081006 CE 2008 10 6 GLB2008F00026 1 20080903 A 5320 STIFFENER BEECH 1900 1900D 1154162 CE RT MLG WW KEEL CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 21 211GL UE211 DURING STRUCTURAL CHECK MAINT DISCOVERED A CRACK ON THE RT WHEEL WELL OB KEEL TAB TO OB FENDER STIFFENER 1" AT THE BOTTO M END OF STIFFENERS TO KEEL AREA. " SUPPLEMENTAL INFORMATION WILL BE PROVIDED UPON COMPLETION OF THE REPAIR". (K) 2 L 7 2 4T RT A24CE 20081006 NM 2008 10 6 USAA920081615 1 20080830 A 5512 SKIN BOEING 737 7374B7 1384702 NM HORIZ STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 444US 24862 CLT MAJOR REPAIR LOG NR 4393607 LT HAND HORIZONTAL STABILIZER LOWER SKIN CRACKED ALONG REAR SPAR 64 INCHES FROM ROOT. R EPAIRED LT HAND HORIZONTAL STABILIZER LOWER SKIN ALONG REAR SPAR 64 INCHES FROM ROOT IAW TYPICAL REPAIR 55-10-08. ***SUP P*** SUPPLEMENTAL INFORMATION WILL BE ADDED UPON RECEIPT & REVIEW OF MAJOR REPAIR FORM. 2 L 7 2 4F RT A16WE 20081006 NM 2008 10 6 QXEA200800401 1 20080418 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK ZONE 144 SUBFLOOR IS CORRODED AT Y565 AND Y25L-Y27L. REMOVED CORROSION IAW CPM CHAP 4. REMOVED .002 MATER IAL FROM ORIGINAL THICKNESS, .043 MATERIAL REMAINING WITHIN LIMITS IAW -8 200 SRM 51-20-11 STEP 3. HFEC INSP. IAW -8 20 0 NDTM PT 6, 51-00-01 NO CRACKS NOTED. ALODINED PRIMED PAINTED IAW -8 200 SRM 51-20-16, 51-20-36 PG 6 PARA F(1) AND 51- 20-26 PG 8 PARA B(1-6). 2 H 7 2 4T RT A13NM 20081006 WP 2008 10 6 I5H2008F00003 1 20080815 A 7921 862501 OIL COOLER CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13 03004 GL RT ENGINE LEAKING A I5HA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 25 584E 24 CAE500021 WHILE IN FLIGHT, THE CREW OBSERVED THE OIL QUANTITY ON THE RT ENGINE DECREASING. AS THE OIL QUANTITY CONTINUED TO DECREA SE, THE CREW ELECTED TO SHUTDOWN THE ENGINE AS A PRECAUTIONARY MEASURE. THE CREW MADE AN UNEVENTFUL LANDING. MAINTENAN CE INSP REVEALED A LEAK IN THE RT OIL COOLER. THE OIL COOLER WAS REPAIRED IAW MM AND THE ACFT RETURNED TO SERVICE. (K) 2 L 7 2 4R 4 T 6A6 E282 20081006 NM 2008 10 6 QXEA200800414 1 20080418 A 5320 FLOOR SKIN DHAV DHC8 DHC8202 2809007 NM CARGO BAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK CARGO PIT LOWER FLOOR DECK SKIN HAS CORROSION ALONG RIVET ROW AT STA X600 BETWEEN Y10L AND Y24L. REMOVED C ORROSION IAW CPM CHAP 4. UT THICKNESS CHECK IAW -8 200 NDTM PT 1, 51-00-04 HI.040 LO.038. HFEC INSP. IAW -8 200 NDTM P T 6, 51-00-01 NO CRACKS NOTED. BLEND WITHIN LIMITS IAW -8 200 SRM 51-20-11 C.3 F. ALODINED AND PRIMED IAW SRM -8 200 5 1-20-16. 2 H 7 2 4T RT A13NM 20081006 NM 2008 10 6 QXEA200800945 1 20080828 A 3260 327 LIGHT BOMBDR DHC8 DHC8402 1390042 NM COCKPIT INOPERATIVE A QXEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 NM 19 425QX 4039 SEA FLIGHT 2344 (SUN-SEA). ON APPROACH TO SEATTLE, RECEIVED A GEAR INDICATION ON GEAR EXTENSION. PERFORMED MISSED APPR OACH. GEAR EXTENDED NORMALLY. LANDED WITHOUT INCIDENT. MX REPLACED THE LAMP. CHECKS GOOD. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081006 EA 2008 10 6 TRAX200801071 1 20080829 A 3350 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 1900309 EA COCKPIT MALFUNCTIONED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 885AS 7521 FAA STATES THAT EMERGENCY LIGHTS FOR EXIT DID NOT ILLUMINATE DURING APPROACH. CONFIRMED ON GROUND THAT LIGHTS DID NOT I LLUMINATE IN THE ARMED POSITION. RESET CIRCUIT BREAKER C2 ON PANEL NR 4. PERFORMED OPS CHECK OF EMERGENCY LIGHTS. OPS CHECK GOOD. IAW CRJ 200 AMM 33-50-00. 2 L 7 2 4F RT A21EA 20081002 NM 2008 10 2 SWAA085266 1 20080930 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 20R. REMOVED AND REPLACED STRINGER SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085265 1 20080930 A 3350 6042221 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND R1 EMERGENCY EXIT DOOR LOWER LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085264 1 20080930 A 3350 6042221 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 659SW 23229 DURING SCHEDULED 24Y CHECK, FOUND L1 EMERGENCY EXIT DOOR LOWER LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085263 1 20080926 A 3350 8210248801 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 919WN 36625 FOUND EMERGENCY EXIT FLOOR LIGHT LENS COVER MISSING. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085258 1 20080925 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 748, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085257 1 20080925 A 5330 6545774 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED AT BS 803, STR 19L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085256 1 20080927 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 780, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085255 1 20080927 A 5330 6545774 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED MV3 CHECK, FOUND SKIN CRACKED AT BS 769 19L TO BS 770, STR 18L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085250 1 20080927 A 3350 300432 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 465WN 33829 FOUND AFT GALLEY RT EGRESS LIGHT ASSEMBLY BROKEN. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085247 1 20080927 A 3350 10107451 LENS BOEING 737 7373H4 1384600 NM EXIT SIGN DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 FOUND EMERGENCY EXIT SIGN LEFT SIDE LENS DETACHED. SECURED SIGN PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085244 1 20080923 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 780SW 27885 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, BL 0. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 UPS08553419 1 20080927 A 2560 SEAL BOEING 757 75724APF 1384969 NM COCKPIT BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 450UP 25472 INSPECTION TYPE:N/A EMERGENCY ESCAPE DEVICE SEAL BROKEN. REMOVED AND REPLACED EMERGENCY ESCAPE DEVICE AS PER MM 25-61-0 2-2. 2 L 7 2 4F RT A2NM 20081003 NM 2008 10 3 SWAA084993 1 20080911 A 5311 6546548 FRAME BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 509SW 24186 DURING SCHEDULED 18Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085000 1 20080911 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM L2 DOOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 325SW 23689 L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK BROKEN. REMOVED AND REPLACED HOOK PER MT. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085031 1 20080914 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 520, STR 10L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085045 1 20080912 A 5755 654645262A FITTING BOEING 737 7373H4 1384600 NM NR 4 SPOILER LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED MV2 CHECK, FOUND LT WING NR 4 GROUND SPOILER INBOARD FITTING LOOSE. REMOVED AND REPLACED SPOILER PER M M. 2 L 7 2 4F RT A16WE 20081003 SO 2008 10 3 C2X2008F00046 1 20080903 A 3260 WARNING LIGHT EMB 145 EMB145LR 3260212 SO MLG ILLUMINATED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14977 145175 THE CREW REPORTED A LANDING GEAR LEVER DISAGREE ON EICAS AFTER TAKEOFF. THE AC RETURNED TO DEPARTURE WHERE IT LANDED WIT HOUT INCIDENT. MAINTENANCE PERFORMED MULTIPLE GEAR EXTENSION AND RETRACTION OPERATIONAL CHECKS ALL WITH NO DEFECTS FOUND , AND THE AC WAS APPROVED FOR RETURN TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081003 NM 2008 10 3 2008UALA05656 1 20080908 A 5320 SILL AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 THE 2R DOOR SILL CORRODED AT FWD SPLICE OUTBOARD SIDE, AT NUT CLIP HOLE. MAJOR REPAIR ACCOMPLISHED. STARTED TO REMOVE FASTENERS, INBOARD AND OUTBOARD ANGLES, NEW ANGLES FOR REPAIR IN WORK AREA. ACCOMPLISHED REPAIR PER MT 53-025. INSPECT ED REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05679 1 20080909 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 584UA 26706 EMERGENCY LIGHT STRIP, LAST FEW FEET BROKEN OFF. REPAIRED EMERGENCY LIGHT WIRING AND REPLACED TRACK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081003 NM 2008 10 3 SWAA085025 1 20080912 A 2560 P2070001 FLASHLIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 288WN 36611 FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085034 1 20080914 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 987, STR 20R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085035 1 20080914 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 26R. REMOVED AND REPLACED STRINGER CLIP PER SRM . 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 2008UALA05904 1 20080929 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT & CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 522UA 24931 CREW REPORT: EMERGENCY LIGHTS ON WHEN ALL SWITCHES IN COCKPIT AND CABIN ARE OFF. NOW LIGHTS ARE INOP FROM ROWS 9-15. RESET SYSTEM AND RE-TESTED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081003 2008 10 3 2008UALA05905 4 20080927 A 2565 SLIDE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU R1 DOOR OUT OF POSITION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 334UA 24229 DOOR 1R SLIDE GAUGE NOT VISIBLE. FOUND SLIDE IN PACK MISALIGNED. REMOVED SLIDE, REALIGNED SLIDE IN PACK SO GAUGE VISIB LE. REINSTALLED SLIDE. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081003 NM 2008 10 3 2008UALA05907 1 20080927 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 194UA 26892 EMERGENCY EXIT EEL LIGHT SIGN INOP JUST AFT OF DOOR 1 RIGHT. EXIT SIGN FOUND INOP. REPLACED BATTERY. OPS CHECKS NORMA L. 2 L 7 4 4F 4 F RT A20WE E24NE 20081003 NM 2008 10 3 2008UALA05912 1 20080927 A 3397 CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 RIGHT AFT LIGHT BAR INOP. FOUND BROKEN RIBBON CABLE FROM POWER SUPPLY. REPLACED WITH NEW LIGHT BAR. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081003 NM 2008 10 3 2008UALA05913 1 20080927 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 EEL LIGHT BARS INOP AT AFT LT LAV. FOUND EEL LIGHT BAR WITH CUT WIRES AND POOR SPLICES. REPLACED PER MM33-51-10, AND O PS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081003 NM 2008 10 3 2008UALA05914 1 20080927 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 EEL LIGHT BARS INOP AT MID LEFT AND RIGHT LAVS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081003 NM 2008 10 3 2008UALA05915 1 20080927 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 646UA 25283 EEL LIGHT BAR AT RT FWD G2 GALLEY IS INOP. 2 L 7 2 4F 4 F RT A1NM E24NE 20081003 NM 2008 10 3 2008UALA05924 1 20080928 A 2611 SMOKE DETECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LAVATORY FAULTY A UALA O OTHER W N INADEQUATE Q C FALSE WARNING NR NOT REPORTED 1 WP 29 855UA 1737 LAVATORY DET FAULT DISPLAYED ON UPPER ECAM SCREEN - SMOKE. REPLACED SMOKE DETECTOR FWD AFT LAVATORY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05926 1 20080929 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN OUT OF POSITION A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 546UA 25367 EMERGENCY LIGHT STRIP ON FLOOR BETWEEN ROWS 21 & 23 LIFTING UP OFF THE FLOOR. SECURED LOOSE TRACK COVER. 2 L 7 2 4F 4 F RT A2NM E17NE 20081003 NM 2008 10 3 2008UALA05927 1 20080929 A 2750 S256T0058 BYPASS VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE T/E FLAP FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 666UA 29238 ALTERNATE T/E FLAP DRIVE ELECTRIC MOTOR RUNS BUT DOES NOT TURN GEARBOX TO EXTEND FLAPS. REPLACED T/E FLAP BYPASS VALVE. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081006 NM 2008 10 6 AALA200802023 1 20080804 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 784AN 29588 DFW EMERGENCY LIGHT AT LT NR 1 DOOR CLOSET DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LT NR 1 DOOR CLOSET . SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT T00001SE 20081006 NE 2008 10 6 AALA200802022 2 20080804 A 7250 TURBINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED A AALA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 21 592AA 53255 70853 JFK INFLIGHT T2393/04AUG. LGA TO ATL. NR TWO ENGINE SEIZED ON TAKE OFF ROTATION. ALL INDICATIONS WENT TO ZERO. LANDE D JFK WITHOUT INCIDENT. SINGLE ENGINE TIME 13 MINUTES. REPLACED NR TWO ENGINE DUE TO TURBINE FAILURE ON 05AUG AT JFK. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F 4 F RT A6WE E9NE 20081006 WP 2008 10 6 AALA200802020 1 20080804 A 3350 SHROUD DOUG DC9 DC983 3022083 WP CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9618A 53565 DFW EMERGENCY LIGHT SHROUD AT SEAT 22D DAMAGED. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A6WE 20081006 NM 2008 10 6 AALA200802019 1 20080803 A 3350 SHROUD BOEING 737 737823 13844BZ NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 907AN 29509 DFW EMERGENCY LIGHT SHROUD AT SEAT 16D DAMAGED. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A16WE 20081006 NM 2008 10 6 AALA200802018 1 20080803 A 2560 FIRST AID KIT BOEING 737 737823 13844BZ NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 DFW FIRST AID KIT AT FIRST CLASS CABIN OPEN. REPLACED FIRST AID KIT AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A16WE 20081006 NM 2008 10 6 AALA200802017 1 20080803 A 3350 SHROUD BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 DFW EMERGENCY LIGHT SHROUD AT SEAT ROW 14DEF BROKEN. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 14DEF. SYSTEM GRO UND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A16WE 20081006 NM 2008 10 6 AALA200801999 1 20080729 A 3350 LIGHT BOEING 737 737823 13844BZ NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 917AN 29518 DFW EMERGENCY LIGHT AT RT HAND EXTERIOR OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RT AND EXTERIOR OVER WING. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A16WE 20081006 WP 2008 10 6 AALA200801998 1 20080729 A 2612 474007 CONTROL PANEL DOUG DC9 DC982 3022082 WP FIRE DETECTION FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 955U 49427 ORD FORWARD COMPARTMENT BOTTLE NR 2 SQUIB FAILED DURING TEST OF CARGO FIRE SUPPRESSION. REPLACED CARGO FIRE SUPPRESSION CONTROL PANEL. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F A6WE 20081006 WP 2008 10 6 AALA200801996 1 20080729 A 3510 2766005 REGULATOR DOUG DC9 DC983 3022083 WP CREW O2 DEFECTIVE A AALA A UNSCHED LANDING O OTHER UK UNKNOWN 1 SW 21 563AA 49345 LAS INFLIGHT T1041/29JUL. CREW REPORTED CREW OXYGEN BOTTLE LOW. LANDED LAS WITHOUT INCIDENT. REPLACED CREW OXYGEN BOT TLE AND REGULATOR. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A6WE 20081006 NM 2008 10 6 AALA200802033 1 20080805 A 2751 SENSOR BOEING 737 737823 13844BZ NM T/E FLAP OUT OF ADJUST A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 924AN 29525 LAX INFLIGHT T1330/05AUG SNA TO DFW. CREW REPORTED FLAP ASYMMETRY INDICATION. LANDED LAX WITHOUT INCIDENT. ADJUSTED N R 6 SKEW SENSOR. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A16WE 20081006 NM 2008 10 6 AALA200802030 1 20080805 A 3350 LENS BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 676AN 29426 DFW EMERGENCY LIGHT AT SEAT 31C BULLNOSE MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 31C BULLNOSE. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20081006 2008 10 6 USAA920081592 4 20080828 A 2565 SLIDE AIRBUS 320 A320214 3930316 EU LEFT MALFUNCTIONED A USAA K NONE J WARNING INDICATION NR NOT REPORTED 1 EA 19 111US 1114 LOG PAGE 7734293 FLT NR 1521 CLT DEN EMERGENCY EQUIPMENT CIDS CAUTION ON FORWARD FLIGHT ATTENDANT PANEL. MX R&R LT OFF WING ESCAPE SLIDE ASSEMBLY PER AIRBUS MX MANUAL 25-62-46. CIDS BITE CHECK GOOD. ***SUPP*** TO BE ISSUED UPON DETERMINA TION OF PART INFORMATION. 2 L 7 2 4F RT A28NM 20081006 2008 10 6 USAA920081598 4 20080829 A 2370 Z030H0005110 DEU AIRBUS A319 A319132 3930340 NM CABIN UNSERVICEABLE A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 830AW 10108 10108 1565 LOGPAGE 8163459 FLT NR 0156 SFO PHX SMOKE FLIGHT ATTENDANTS REPORT A SMELL OF SMOKE AROUND ROW 5 IN CABIN. CONFIRMED BY 2 FLIGHT ATTENDANTS AND A FEW PASSENGERS. NO SMOKE NOTED ON LANDING. R&R DEU AT ROW 5 ACFT RIGHT. 2 L 7 2 4F RT A28NM 20081006 NM 2008 10 6 USAA920081604 1 20080831 A 5230 658099875 SKIN BOEING 737 7373B7 1384580 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT Q6 MAJOR REPAIR NR 03C21952009/013 2 CRACKS ON FORWARD CARGO DOOR INNER SKIN. REPAIRED FORWARD CARGO DOOR INNER SKI N IAW US AIRWAYS EA NR 100614. 2 L 7 2 4F RT A16WE 20081006 CE 2008 10 6 GUU2008F00048 1 20080909 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE COCKPIT ODOR A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 29 87550 UE205 DURING FINAL APPROACH BOTH PILOTS OBSERVED BURNING ODOR. INSPECTED COCKPIT INSTRUMENTS NO DEFECTS NOTED, PERFORMED OPERA TIONAL CHECK OF ENVIRONMENTAL SYSTEM COULD NOT DUPLICATE. (K) 2 L 7 2 4T RT A24CE 20081006 EU 2008 10 6 HXS2008F00006 1 20080929 A 6720 350A21136324 BRACKET SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE RUDDER PEDALS CRACKED E HXSA O OTHER O OTHER NR NOT REPORTED 1 AL 05 149TH 9071 ON THE BOTTOM SIDE OF THE FOOT PEDAL CONTROLS, ON THE RT PILOT SIDE, THE BRACKET THAT IS PART OF THE BELLCRANK ASSY, BRA CKET PN 350A21-13636-24, HAS A CRACK IN IT. REMOVED BRACKET AND REPLACED WITH A SERVICEABLE BRACKET AND RETURNED AC TO S ERVICE. THIS AC HAS BEEN PREVIOUSLY CONVERTED TO LT PILOT IN CHARGE IAW MFG MODIFICATION. THIS BRACKET IS WHAT HOLDS THE CENTERING ROD OR THE FOOT PEDAL BELLCRANK IN THE FOOT PEDAL FLIGHT CONTROLS. (K) 1 G 7 1 3U 3 U H9EU E19EU 20081006 NM 2008 10 6 R612008F00010 1 20080904 A 3231 ROD EMB ERJ170 ERJ170100SU 3260403 NM NLG DOOR SHEARED A R61A A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 11 817MD 11360 7912 17000038 CREW RECEIVED LANDING GEAR NOSE DOOR OPEN INDICATION IN EICAS. CREW DECLARED EMERGENCY FOLLOWED QRH PROCEDURES AND LANDE D WITHOUT INCIDENT. MAINT WAS DISPATCHED TO THE AC FOUND NOSE LANDING GEAR DOOR ROD ASSY LOCKING TABS SHEARED OFF. AC WA S FERRIED AND MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR DOOR ROD ASSY AND RETURNED THE AC TO SERVICE. (K) 2 L 7 2 4F RT A56NM 20081006 EU 2008 10 6 HXS2008F00007 1 20080929 A 6720 350A21136324 BRACKET SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D1 60053 NE RUDDER PEDALS CRACKED E HXSA O OTHER O OTHER NR NOT REPORTED 1 AL 05 141TH 1167 ON THE BOTTOM SIDE OF THE FOOT PEDAL CONTROLS, ON THE RT PILOT SIDE, THE BRACKET THAT IS PART OF THE BELLCRANK ASSY, BRA CKET PN 350A21-13636-24, HAS A CRACK IN IT. REMOVED BRACKET AND REPLACED WITH A SERVICEABLE BRACKET AND RETURNED AC TO S ERVICE. THIS AC HAS BEEN PREVIOUSLY CONVERTED TO LT PILOT IN CHARGE IAW MFG MODIFICATION. THIS BRACKET IS WHAT HOLDS THE CENTERING ROD OR THE FOOT PEDAL BELLCRANK IN THE FOOT PEDAL FLIGHT CONTROLS. (K) 1 G 7 1 3U 3 U H9EU E19EU 20081006 NM 2008 10 6 USAABB08142 1 20080831 A 3350 BPS73 POWER SUPPLY BOEING 757 7572S7 1384962 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 906AW 23568 PHX ALL SEAT MOUNTED LIGHTS AFT OF AFT LAVATORIES WERE FOUND INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT POWER SUPPLY AT AFT GALLEY, LEFT HAND SIDE. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 20081006 CE 2008 10 6 AWK2008F00001 1 20080912 A 2822 99144251 PUMP CESSNA 750 750 2076810 CE RROYCE AE3007 AE3007C1 54168 EA LT FUEL BOOST INOPERATIVE E AWKA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 25 786XJ 7500286 CAE330593 LT BOOST ON CAS MESSAGE WITH ASSOCIATED LOW FUEL PRESS CAS MESSAGE CALLED IN BY THE CREW AT 1800. THEN AT 1815 CREW CALL ED IN WITH OIL QTY DOWN TO 9 QTS LOW AND AT THAT TIME THEY GOT THE LOW OIL PRESSURE. CREW THEN PERFORMED EMERGENCY PROCE DURES FOR THE LOW OIL PRESSURE AND DIVERTED. ACFT LANDED WITHOUT SHUTTING DOWN THE ENGINE UNTIL AFTER THEY WERE TAXIING INTO THE FBO WHEN OIL PRESSURE DROPPED INTO THE RED BELOW 34 PSI. AFTER SECURING THE ACFT THE CREW NOTED OIL COMING FRO M THE ENGINE UPON A VISUAL INSPECTION. NO OIL WAS NOTED IN THE OIL TANK SIGHT GLASS. TECHNICIANS PULLED THE MOTIVE FLOW FUEL PUMP (MFP) AND NOTED THAT THE SHAFT WAS TURNING FREELY ON THE MFP, INDICATING A FAILED MFP. METAL WAS FOUND ON THE 2 L 7 2 4J 4 F RT T00007WI TE6CH 20081006 SO 2008 10 6 N932008F00003 1 20080901 A 3250 1159SCL50051 ACTUATOR GULSTM GIVX GIVXG450 3980205 SO NLG STEERING UNSERVICEABLE E N93A O OTHER J WARNING INDICATION AP APPROACH 1 SO 13 440QS 4025 AFTER GEAR WAS EXTENDED, NOSE WHEEL STEERING FAIL CAS MESSAGE ILLUMINATED. MX FOUND NOSE STEERING ACTUATOR, FAILED. (K ) 2 L 7 2 4F RT A12EA 20081006 NM 2008 10 6 QXEA200800418 1 20080418 A 5320 INTERCOSTAL DHAV DHC8 DHC8202 2809007 NM BS 190-201 S31L CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 C4-CHECK - SUSPECT CORROSION ON AVIONICS BAY INTERCOSTAL AT BELLY SKIN, JUST OB OF STRINGER 31P FROM STA X190 TO X201. R EPAIRED IAW SRM. (K) 2 H 7 2 4T RT A13NM 20081006 NM 2008 10 6 MWE2008F00037 1 20080828 A 2460 762904E PCDU DOUG MD88 MD88 3023688 NM ELEC BAY INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 822ME 49759 LT DC BUSS INOPERATIVE, C/B TRIPPED. NORMAL CRUISE FL350. LT GEN WOULD NOT RESET. FOUND NUMEROUS FAULTS DISPLAYED IN COC KPIT. RESET LT PCDU C/B WITH POWER ON ACFT. REMOVED AND REPLACED PCDU RESET C/B. (K) 2 L 7 2 4F RT A6WE 20081006 NM 2008 10 6 USAA920081607 1 20080808 A 5320 6545834227 INTERCOSTAL BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT Q6 MAJOR REPAIR NR 03C10753005/017 LEVEL 2 CORROSION ON INTERCOSTAL AT BS330, RBL10. REPLACED INTERCOSTAL AT BS330. RBL10 IAW B737 SRM 51-10-2. 2 L 7 2 4F RT A16WE 20081006 EA 2008 10 6 QXEA200800542 1 20080529 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 601QX 10009 PDX C4 CHECK AT APPROX STA FS541 ON THE RT IB SEAT TRACK THERE ARE AREAS OF CORROSION ON THE UPPER EDGES OF THE TRACK. BLENDED AREAS OF CORROSION ON BOTH SIDE OF THE TOP OF TRACK AREA APPROX 0.5" X 3.0". MAX MATERIAL REMOVED .009" WITHIN LIMITS AS PER REO 670-53-00-13. COMPLETED COMPLIANCE WITH REO 670-53-00-013 PG 2 STEPS 3-9. 2 L 7 2 4F RT A21EA 20081006 NM 2008 10 6 QXEA200800400 1 20080418 A 5320 STRUCTURE DHAV DHC8 DHC8202 2809007 NM CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK ZONE 144 SUBFLOOR TOP SURFACE IS CORRODED AT Y580-X581 AND Y24L-Y26L. REMOVED CORROSION IAW CPM CHAP 4. R EMOVED .002 MATERIAL FROM ORIGINAL THICKNESS. .043 MATERIAL REMAINING WITHIN LIMITS IAW -8 200 SRM 51-20-11 STEP 3. HF EC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. C/W CPM CHAP 5 FOR SURFACE TREATMENT. PRIMED AND PAINTED IAW SRM 51-20-26 PARA 5A. 2 H 7 2 4T RT A13NM 20081006 NM 2008 10 6 QXEA200800408 1 20080418 A 5753 FLAP DHAV DHC8 DHC8202 2809007 NM RT WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK RT O/B FLAP HAS A CHAFFED AREA AT THE O/B END APPROX 10" FROM THE TRAILING END. BLENDED ARE OF CHAFE, FOUN D OUT OF LIMITS IAW -8 200 SRM 57-50-16. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01. NO CRACKS NOTED. UT THICKNESS CHE CK IAW -8 200 NDTM PT 1, 51-00-04 HI .025, LO .017. MAPPED FOR ENG. FOUND WITHIN LIMITS PER RD8-57-3923. UT DISBONDING CHECK IAW -8 200 NDTM PT 1, 51-00-04, NO DISBOND NOTED. ALODINE PRIMED, PAINTED IAW -8 200 RD8-57-3923 NOTES 5 AND 6. 2 H 7 2 4T RT A13NM 20081006 NM 2008 10 6 QXEA200800411 1 20080418 A 5347 SUPPORT BRACKET DHAV DHC8 DHC8202 2809007 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK LT O/B SEAT TRACK SUPPORT BRACKET ON FWD SIDE OF FRAME AT STA X333.3 HAS DAMAGED HOLE, 2ND HOLE AFT TOP. R EMOVED LT O/B SEAT TRACK SUPPORT BRACKET FWD SIDE FRAME AT STA X3333.3. INSTALLED NEW BRACKET FROM STOCK AT LT O/B SEAT TRACK ON FWD SIDE OF FRAME AT STA 333.3 IAW -8 200 SRM 51-40-11. 2 H 7 2 4T RT A13NM 20081006 NM 2008 10 6 QXEA200800412 1 20080418 A 5230 DOOR DHAV DHC8 DHC8202 2809007 NM CARGO BAY GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK CARGO DOOR HAS SEVERAL GOUGES ON CENTER FWD LOWER SIDE. REMOVED DAMAGE IAW -8 200 51-20-11. HFEC INSP IAW -8 200 NDTM PT6, 51-00-01 NO CRACKS NOTED. WITHIN LIMITS PER -8 200 52-00-16. ALODINED PRIMED IAW SRM 51-20-36. 2 H 7 2 4T RT A13NM 20081006 NM 2008 10 6 QXEA200800947 1 20080827 A 5240 DOOR BOMBDR DHC8 DHC8402 1390042 NM SERVCIE DOOR DIRTY A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 19 432QX 4166 PDX FLIGHT ATTENDANT REPORTS SERVICE DOOR HARD TO OPEN AND CLOSE. MX CLEANED AND LUBRICATED. OPS CHECK GOOD. ACFT RET URNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081006 NM 2008 10 6 QXEA200800946 1 20080827 A 2621 4739511 FIRE BOTTLE BOMBDR DHC8 DHC8402 1390042 NM APU DEFECTIVE A QXEA K NONE J WARNING INDICATION NR NOT REPORTED 1 NM 19 432QX 4166 SEA MASTER WARNING FOR THE FIRE DETECTION WARNING AND APU BOTTLE LOW LIGHT ILLUMINATED FOR 2 MINUTES. MX REPLACED THE A PU FIRE BOTTLE. CHECKS GOOD. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081003 EU 2008 10 3 2008UALA05721 1 20080913 A 3260 664700500A4D CONTROL UNIT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 430UA 568 NLG WOULD NOT RETRACT. RTFL. POSSIBLE LGCIU INTERMITTANT SHORT AND PROX SENSORS 24GA,25GA OUT OF ADJUSTMENT. REPLACED NR 1 LGCIU. ADJUSTED 24GA & 25GA NLG PROX SENSORS TARGET CLEARANCE. ACCMP FUNCTIONAL TEST NORMAL EXTENTION & RETRACTION OF NLG. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05728 1 20080914 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 SEAT 4J FWD EMERGENCY LIGHT INOP. LIGHT FOUND DEFECTIVE. REPLACED LAMP. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081003 NM 2008 10 3 2008UALA05729 1 20080914 A 3397 7945243 CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 SEAT 4A BOTH EMERGENCY LIGHTS INOP. CABLE FOUND DEFECTIVE. REPLACED UNDERSEAT CABLE. CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081003 NM 2008 10 3 2008UALA05920 1 20080927 A 7160 314N301025A NOSE COWL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 DELAMINATED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 553UA 25277 WHILE PROCESSING THE AC FOR PAINT, A DELAM INATED AREA WAS FOUND AT THE 10 O'CLOCK POSITION ON THE INBOARD SIDE OF THE N R 2 NOSE COWL. COMPLETELY UN-NOTICABLE VISUALLY FROM THE OUTSIDE. AREA IS 18 INCHES BY 18 INCHES. THERE ARE NO DEPRES SIONS, OR ANY OTHER VISUAL DEFECTS. ASSUME THE HONEYCOMB LAYER HAS DISBONDED FROM THE OUTER SKIN. REPLACED NR 2 ENG N OSE COWL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081003 NM 2008 10 3 AALA200801985 1 20080727 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 636AM 24594 DFW SEAT MOUNTED EMERGENCY LIGHTS AFT OF FIRST CLASS TO SEAT ROW 15D INOPERATIVE. REPLACED BATTERY PACK M10799 FOR EMER GENCY LIGHTS AFT FIRST CLASS TO SEAT ROW 15D. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20081003 WP 2008 10 3 AALA200801930 1 20080722 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9621A 53592 AUS OVERHEAD EMERGENCY LIGHTS IN CABIN INOPERATIVE. REPLACED BATTERY PACK AT B5 103 FOR OVERHEAD EMERGENCY LIGHTS IN CA BIN. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A6WE 20081006 NM 2008 10 6 AALA200802003 1 20080730 A 2421 IDG BOEING 777 777223 1385213 NM RT ENGINE FAILED A AALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SW 21 770AN 29578 MIA INFLIGHT T869/30JUL. CREW REPORTED LT INTEGRATED DRIVE GENERATOR FILTER BLOCK MESSAGE. DISCONNECTED LT INTEGRATED DRIVE GENERATOR. RT INTEGRATED DRIVE GENERATOR DROPPED OFF LINE. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACE D LT AND RT HAND INTEGRATED DRIVE GENERATORS AND LT HAND INTEGRATED DRIVE GENERATOR OIL COOLER. SYSTEM GROUND CHECKED N ORMAL OPS. (CLOSED) 2 L 7 2 4F RT T00001SE 20081006 2008 10 6 USAA920081594 4 20080829 A 2565 D31517317 SLIDE AIRBUS 320 A320232 3930326 EU L2 DOOR LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656AW 19023 2110 1079 LOG PAGE 4420383 FLT NR 192 BOS PHX EMERGENCY EQUIPMENT L2 DOOR SLIDE PRESSURE GAUGE IN LOWER RED BAND RANGE. MX R&R L2 DOOR SLIDE. 2 L 7 2 4F RT A28NM 20081006 NM 2008 10 6 USAA920081599 1 20080829 A 5330 6545775 SKIN BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 23876 CLT C5 MAJOR REPAIR 03C10025001/001 CRACK IN FUSELAGE SKIN BETWEEN BS727D & BS727E, S25R. REPAIRED FUSELAGE SKIN BETWEE N BS727D & BS727E, S25R IAW B737 SRM 53-00-01, R31, TEMPORARY REVISION 53-27. 2 L 7 2 4F RT A16WE 20081006 NM 2008 10 6 USAASB08074 1 20080831 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 427US 24549 PVD THE RT HAND OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. MX REPLACED THE BATTERY PACK. OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 20081006 CE 2008 10 6 GLB2008F00024 1 20080902 A 5311 FRAME BEECH 1900 1900D 1154162 CE FS 177.3 S9AR CRACKED A GLBA O OTHER O OTHER NR NOT REPORTED 1 NM 21 211GL UE211 DURING STRUCTURAL INSPECTION MAINTENANCE FOUND FRAME CRACKED AT STRINGER CUTOUT FS 177.3 AT STRINGER 9AR. LENGTH OF CRAC K APPROXIMATELY .750". MAINTENANCE REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW SRM 51-70 AT FS 177.3 AT STRINGER 9 AR. REPAIR APPROXIMATELY 5 INCH BY 2.5". 2024-T3. RII INSPECTION COMPLIED IAW TASKCARD 8.2.1. (K) 2 L 7 2 4T RT A24CE 20081006 SO 2008 10 6 FDK2008F00010 1 20080827 A 2560 CONNECTOR EMB 145 EMB145LR 3260212 SO FLASHLIGHT CHARG DISCONNECTED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 826MJ 145214 AFT FLASHLIGHT INOPERATIVE. MX RESECURED THE CONNECTION. (K) 2 L 7 2 4T RT T00011AT 20081006 NM 2008 10 6 QXEA200800416 1 20080418 A 5320 FLOOR SKIN DHAV DHC8 DHC8202 2809007 NM CARGO BAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK CORROSION AT CARGO PIT DECK SKIN I/B AND BELOW CORNER FITTING STA X597.5, Y40.95. REMOVED CORROSION USING SCOTCH BRITE PAD IAW -8 200 SRM 51-40-11 AND CPM CHAP 4 PG25-26. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NO TED. UT THICKNESS CHECK IAW -8 200 NDTM PT 1, 51-00-04, HI.063 AND LOW .058. WITHIN LIMITS IAW -8 200 SRM 51-20-11. A LODINED PRIMED IAW -8 200 SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 20081006 EA 2008 10 6 TRAX200800988 1 20080808 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 738EV 10146 PAX DOOR THRESHOLD FLOOR SUPPORT ANGLE HAS CORROSION DAMAGE (MARKED) (RESOLVED ON W/O: 97397 TASKCARD: N/R 00173) WORK COMPLETED IN ACCORDANCE WITH: ITEM 1 R&R FLOOR SUPPORT ANGLE IAW CRJ 700 SRM 51-40-00 AND SRM 51-40-11. DH 7025983 ITEM 2 ADJUSTED AND SAFETIED PROX SWITCH PX 25 IAW CRJ 700 AMM 52-70-04. MV7022816 08-16-08. 2 L 7 2 4F RT A21EA 20081006 EA 2008 10 6 TRAX200801052 1 20080824 A 5210 SKIN CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 970EV 7527 JOB 8752721 OPERATION 299 PAX DOOR AFT SIDE SKIN IS CRACKED BETWEEN STEPS 3 AND 4. REPAIRED PAX DOOR AFT SIDE SKIN IAW BOMBARDIER REO 601R-52-11-702 AND REO 601R-52-11-1541 AND C/W ASA EC/TC NR REO 601R-52-11-702. DEVIATION TO GREO 601R-5 2-11-702 PER REO 601-52-11-1541 IS COMPLETED AND MEETS WITH THE REQUIREMENTS ASA EC/TC REO 601R-52-11-1541. 2 L 7 2 4F RT A21EA 20081006 EA 2008 10 6 TRAX200801058 1 20080825 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 932EV 8016 JOB 8801621 OPERATION 159 RH INBD AND OTBD 280 CLIPS ARE CRACKED AT RBL 9. THIS SDR WILL REMAIN OPEN PENDING MX DETERMIN ATION OF AN APPROPRIATE CORRECTIVE ACTION. REMOVED CRACKED ANGLES (INBD AND OTBD). INSTALLED NEW ANGLES PN 601R3113-58 I AW CRJ 200, SRM 51-42-06/ -21. SUP CLOSED 9/11/2008 (K) 2 L 7 2 4F RT A21EA 20081006 NM 2008 10 6 QXEA200800954 1 20080831 A 3242 216052 BRAKE BOMBDR DHC8 DHC8402 1390042 NM NR 3 FAULTY A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 19 404QX 4046 PDX WHILE BRAKING ON LANDING ON TAXI, THE RT SIDE BRAKES SEEM TO GRAB AND THE ANTI-SKID IS RELEASED TOO EARLY CAUSING S TOPPING TO BE JERKY. MX REPLACED THE NR 3 BRAKE AND THE NR 3 WHEEL SPEED TRANSDUCER. CHECKS GOOD. RETURNED TO SERVICE . 2 H 7 2 4T RT A13NM 20081006 EU 2008 10 6 TRAX200801072 1 20080829 A 5240 LATCH AEROSP ATR72 ATR72212 8680945 EU SERVICE DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 632AS 338 SVC DOOR LATCH INOP. FLT 4265 DEL 300 MINS. PERFORMED FUNCTIONAL TEST OF SERVICE DOOR LATCHING AND LOCKING MECHANISM. VERIFIED CORRECT OPERATION OF HOLD OPEN HOOK. NO DEFECTS NOTED IAW ATR 72 JIC 52-42-00 FUT 10000. 2 H 7 2 4T RT A53EU 20081002 NM 2008 10 2 CALA0800887 1 20080916 A 5311 6546596 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 11651 28912 FS 727B FRAME IS CRACKED AT AIR CONDITIONING (AC) SUPPORT BRACKET BETWEEN STRINGERS 8L AND 9L. REPAIRED CRACKED FRAME A T STA 727B PER EA 5310-04498. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 2008UALA05745 1 20080914 A 2421 CSD BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NR 1 OVERSERVICED A UALA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CL CLIMB 1 WP 29 934UA 26662 OIL TEMP INDICATION BOTH ENGINES. RTFL. FOUND NR 1 AND 2 CSD OIL LEVEL HIGH. DRAINED OIL TO PROPER LEVELS. REPLACED N R 1 OIL TEMP INDICATOR AND NR 2 CSD. 2 L 7 2 4F 4 F RT A16WE E21EU 20081002 NM 2008 10 2 SWAA085267 1 20080930 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND AFT CARGO BAY SHEAR TIE CORRODED AT BS 747, STR 19R TO STR 20R. REPAIRED SHEAR TIE PE R ER. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085262 1 20080926 A 3350 3071BPEGPL LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 788SA 30603 DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHT AT SEAT 3D INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085261 1 20080926 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM COCKPIT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 782SA 29808 DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT LIGHT FAILED FUNCTION TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081002 2008 10 2 SWAA085260 4 20080919 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 FOUND L1 DOOR SLIDE PARTIALLY PULLED OUT OF CASE. INSTALLED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085259 1 20080926 A 5330 6545774 SKIN BOEING 737 7373T5 1384608 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 692SW 23062 DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT BS 863, STR 25L. REPAIRED PER SWA EA. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085252 1 20080927 A 3350 20121 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 621SW 28037 DURING SCHEDULED MV2 CHECK, FOUND L1 EMERGENCY EXIT ESCAPE SLIDE LIGHT INOP. REMOVED AND REPLACED BATTERY ASSY PER MM. 2 L 7 2 4F RT A16WE 20081002 2008 10 2 SWAA085251 4 20080926 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 474WN 33861 FOUND R2 EMERGENCY EXIT DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085249 1 20080927 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 927, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081002 NM 2008 10 2 SWAA085248 1 20080927 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 370SW 26597 DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500C + 4, STR 15R. REPAIRED PER SWA EA. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 2008UALA05657 1 20080907 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 FLOORBEAM 175 HAS CORROSION ALONG LENGTH BETWEEN FR68 AND FR70. MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM. INSTALL ED LAV AND GALLEY MOUNT FITTINGS TO NEW FLOORBEAM. DRILLED AND INSTALLED BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05658 1 20080908 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 FLOORBEAM 185 HAS CORROSION AT FR68 (MARKED). MAJOR REPAIR ACCOMPLISHED. REMOVED FLOORBEAM. BEAM OUT AND ON BENCH WOR KING. STARTED INSTALLATION OF BRACKETS. RIVETING OF STANDOFF BRACKETS IS WHAT IS LEFT. DRILLED AND INSTALLED NEW BEAM 185. ALL BRACKETS RE-INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05670 1 20080911 A 2697 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE FIRE DETECTOR CHAFED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 127UA 28813 APU FIRE WARNING INDICATION. RTFL. CREW SAID THAT AT TOP OF CRUISE APPROX 1HR 30 MIN INTO FLT THEY HEARD CLICKING FROM THE FIRE PANE L FOLLOWED BY APU FIRE MSG AND AND HANDLE LITE, FIRED BOTTLE, LITE WENT OUT BUT CLICKING FROM PANEL CONTI NUED FOR ANOTHER 30 MINUTES BEFORE STOPPING. LANDING WEIGHT WAS 929.7 AND FUEL ON BOARD WAS 142.1 AT THE GATE. FOUND WI RES CHAFING UNDER CLAMP IN APU COMPARTMENT FOR T1814 'A' LOOP. REPLACED W720-451- 18 AND W720-452-18 PER WDM 26-15-11. T EST NORMAL. NO EVIDENCE OF FIRE NOTED. 2 L 7 4 4F 4 F RT A20WE E24NE 20081006 EA 2008 10 6 TRAX200801066 1 20080827 A 5210 HINGE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR DIRTY A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 708EV 10060 PAX DOOR VERY DIFFICULT TO OPEN AND CLOSE. CLEANED PAX DOOR HINGES AND LUBRICATE HINGES AND LOCK MECHANISM. OPS CHECK IAW CRJ AMM 52-11-00. NO DEFECT NOTED. 2 L 7 2 4F RT A21EA 20081006 EA 2008 10 6 TRAX200801068 1 20080828 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 682BR 7691 RT AFT EXT EMERGENCY LIGHT INOP. RESOLVED ON W/O 98667 TASKCARD N/R 00006. R/R AFT BATTERY PACK NR 4 IAW CRJ 200 AMM 3 3-51. OP CK GOOD. 2 L 7 2 4F RT A21EA 20081006 EA 2008 10 6 TRAX200801070 1 20080828 A 2150 ACM CNDAIR CL600 CL6002B19 1900309 EA A/C BAY MALFUNCTIONED A ASOA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 849AS 7347 SMOKE IN COCKPIT AND CABIN ON TAXI OUT FOLLOWED QRH FOR PASSENGER EVACUATION. EMERGENCY TRUCKS ROLLED AS A PRECAUTION. FLT 4899 DEL 30 MINS. AIR CONDITIONING PACK LT SIDE. R&R LT ACM IAW AMM 21-51-10 OPS AND LEAK CHK GOOD IAW AMM 21-51 -00 DML CLEARED PLACARD REMOVED. 2 L 7 2 4F RT A21EA 20081006 EA 2008 10 6 TRAX200801041 1 20080822 A 5230 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 970EV 7527 JOB 8752725 OPERATION 78 CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 3" IN LENGTH. REMOVED CRACKED ANGLE. IN STALLED NEW ANGLE P/N 601R35050-109 IAW CRJ 700 SRM 51-42-21. 2 L 7 2 4F RT A21EA 20081006 SO 2008 10 6 C2XA08CL098 1 20080824 A 3040 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 12135 145718 CLE FLIGHT NR 2285 THE CREW REPORTED A BURNING SMELL IN THE COCKPIT WHEN THE WINDSHIELD HEAT COMES ON AND GOES AWAY WHEN WINDSHIELD HEAT IS TURNED OFF. MX INSPECTED AND PERFORMED OPS CHECKS AND COULD NOT DUPLICATE BURNING SMELL. THE NR 1 WINDSHIELD GROUND WIRE WAS RETORQUED BUT NO DAMAGE WAS FOUND TO EITHER NR 1 OR NR 2 WINDSHIELD HEAT WIRING. 2 L 7 2 4F RT 20081006 SO 2008 10 6 C2XA08CL099 1 20080824 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO COCKPIT ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 12135 145718 CLE FLIGHT NR 2641 THE CREW REPORTED A STRONG BURNING SMELL EVERYTIME THRUST WAS REDUCED TO IDLE IN FLIGHT. THE SMELL W ENT AWAY WHEN THRUST WAS INCREASED. MX INSPECTED AND PERFORMED ENGINE GROUND RUNS AT VARIOUS POWER SETTINGS AND PACK SE TTINGS AND COULD NOT DUPLICATE BURNING SMELL. OPS CHECKS WERE GOOD. 2 L 7 2 4F RT 20081006 EA 2008 10 6 C2XA08RI123 2 20080826 A 7261 23073567 CARBON SEAL EMB 145 EMB145XR 3260214 SO RROYCE AE3007 AE3007A1E 54169 EA NR 1 ENGINE LEAKING A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 27 14117 145674 FLIGHT 2034 EWR FLIGHT CREW REPORTED STRANGE SMELL COMING FROM PACKS. UPON TOUCH DOWN IN EWR, FOLLOWED BY LAV SMOKE WAR NING AND A CLOUDY APPEARANCE IN THE CABIN. EWR MX R&R ENGINE NR 1 CARBON SEAL AND PERFORMED OPS CHECK SUCCESSFULLY. AC FT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 20081006 SO 2008 10 6 C2XA08RI120 1 20080801 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 26545 145558 FLIGHT 1296 EWR FLIGHT CREW REPORTED EMERGENCY LIGHTS OVER THE WING INOPERATIVE. EWR MX R&R NR 4 EMERGENCY LIGHT POWER SUPPLY AND BATTERY ASSEMBLY AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081006 SO 2008 10 6 C2XA08RI119 1 20080801 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13964 145123 EWR MX DURING ROUTINE MX EWR MX FOUND LT OVER WING EMERGENCY LIGHT INOPERATIVE. MX R&R LIGHT BULB AND PERFORMED OPS CHE CK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081006 SO 2008 10 6 C2XA08RI118 1 20080823 A 3320 7281000501 CONTROL MODULE EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 13123 145688 FLIGHT 2123 EWR FLIGHT CREW REPORTED SMELL OF SMOKE NEAR SEAT 1A. EWR MX R&R LIGHT CONTROL MODULE IAW EMB 145 AMM 33-21 -01 AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081006 EU 2008 10 6 VQI2008F00003 1 20080823 A 2760 31077100 CONTROLLER AIRBUS 320 A320214 3930316 EU CFMINT CFM56 CFM565B4 NE LT NR 5 SPOILER FAILED A VQIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 WP 15 626VA 2830 FLIGHT PHASE 6 CLIMB DEPARTED JFK AT 1127 Z - RETURNED TO FIELD AT 1200 Z. CREW REPORTED A NORMAL DEPARTURE WITH NO ABN ORMALITIES UNTIL AROUND 10,000 FT WHEN THEY NOTICED AN AIRFRAME VIBRATION. CHECKING WITH THE FLT TEAM, THEY CONFIRMED T HAT A CREW REPORTED A NORMAL DEPARTURE WITH NO ABNORMALITIES UNTIL AROUND 10,000 FT WHEN THEY NOTICED AN AIRFRAME VIBRAT ION. CHECKING WITH THE IN FLIGHT TEAM, THEY CONFIRMED THAT A LT NR 5 SPOILER HAD PARTIALLY DEPLOYED. THE AC RETURNED T O DEPARTURE WITH AN UNEVENTFUL LANDING. THE NR 5 SPOILER HAD MEL 27-64-01-2 APPLIED PRIOR TO DEPARTURE. THE NR 5 SPOIL ERS WERE LOCKED OUT IAW MEL MAINT PROCEDURE. AFTER RETURN, THE LT SPOILER SERVO CONTROL WAS REPLACED. THE ORIGINAL FAU 2 L 7 2 4F 4 F RT A28NM E38NE 20081006 SO 2008 10 6 C2XA08SH113 1 20080829 A 5312 14526850401 FIREWALL EMB 145 EMB145LR 3260212 SO APU CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13979 145181 SHV DURING C-CHECK APU FIREWALL CRACKED AT LT UPPER, RT LOWER APU MOUNTS. MX REPAIRED APU FIREWALL LT UPPER, RT LOWER A PU MOUNTS IAW EC5330-01838. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081006 SO 2008 10 6 C2XA08IA200 1 20080828 A 3350 LIGHT EMB 135 EMB135LR 3260305 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14522 145383 ICT FLIGHT 2327 DURING PREFLIGHT INSPECTION THE CREW REPORTED THE FORWARD HALF OF THE OVERHEAD EMERGENCY LIGHT TO BE INO PERATIVE. MX PERFORMED A SYSTEM RESET. OPS CHECKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20081006 NM 2008 10 6 WRLA2008072 1 20080826 A 5320 BOLT DOUG DC10 DC10 N/A-SDR NM GE CF6 CF650C2 30018 NE FUSELAGE SHEARED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 139WA 46583 DURING C-CHECK INSPECTION FOUND 1 BOLT SHEARED AND RUSTED, AND 1 BOLT RUSTED AT RT WING ROOT FUSELAGE ANGLE. FUSELAGE S TA 1371. REAMED HOLES, EDDY CURRENT INSPECTION ACCOMPLISHED, MFG AND INSTALLED TAPERED WASHERS, TREAT, PRIME, SEAL AND PAINT IAW ENGINEERING REPAIR. (K) 2 L 7 3 4F 4 F RT A22WE E23EA 20081006 EA 2008 10 6 REX2008F00046 1 20080822 A 2750 85D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A REXA O OTHER J WARNING INDICATION AP APPROACH 1 CE 21 8506C 17114 7506 ON APPROACH WHEN SELECTING FLAPS 8 RECEIVED FLAP FAIL WHEN FLAPS REACHED 8 QRH FOLLOWED EMERGENCY DECLARED WITH UNEVENTF UL LANDING. TROUBLESHOT FLAP SYSTEM PER BOMBARDIER FAULT ISOLATION MANUAL (FIM) R&R THE LT BPSU (BRAKE POSITION SENSING UNIT) IAW BOMBARDIER AMM. 2 L 7 2 4F RT A21EA 20081006 NM 2008 10 6 USAASB08072 1 20080829 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 445US 24863 FLL MX REPORTED THE EMERGENCY LIGHTS FROM SEAT ROWS 6 THROUGH 9 AND THE OVERHEAD SIGNS AT ROW 12 AND RT FORWARD OVERWING EXIT WOULD NOT REMAIN ILLUMINATED. MX REPLACED THE BATTERY PACK AT STATION 527L. OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 20081006 EU 2008 10 6 NWAA084083254 1 20080829 A 3231 BYPASS VALVE AIRBUS 320 A320212 3930322 EU RT MLG DOOR MALFUNCTIONED A NWAA K NONE O OTHER CR CRUISE 1 GL 01 354NW 801 HYD G RSVR LO LVL DISPLAYED ON ECAM. FOLLOWED COM PROCEDURES. GREEN HYDRAULIC SYSTEM WAS DEPLETED FOR 3 MINUTES BEFORE EDP WAS SHUT OFF. LANDING GEAR GRAVITY EXTENDED, LANDING UNEVENTFULLY, AND TOWED TO GATE. REPLACED RH MAIN LANDING GE AR DOOR GROUND OPENING BYPASS VALVE. LEAK CHECKS GOOD. 2 L 7 2 4F RT A28NM 20081006 NM 2008 10 6 DHL2008F00031 1 20080826 A 3350 1000679 LIGHT BOEING 727 7272M7 138407S NM CABIN INOPERATIVE A DHLA K NONE L NO TEST IN INSP/MAINT 1 GL 05 750DH 2408 21951 L1 DOOR EMER EXIT LIGHT INOP. R&R EMER EXIT LIGHT ASSY OPS CHECK GOOD IAW MM 33-50-71. ACFT WAS GROUNDED. FLIGHT NR 82 0. 2 L 7 3 4F A3WE 20081006 NM 2008 10 6 MWE2008F00034 1 20080830 A 3350 316 LAMP BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE EMERGENCY LIGHTS BURNED OUT A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 925ME 55191 EMERGENCY LIGHT AFT CEILING AREA IN AFT ACCESSORY IS INOPERATIVE. RELAMPED. (K) 2 L 7 2 4F 4 F TR A6WE E00061EN 20081006 WP 2008 10 6 MWE2008F00035 1 20080830 A 2620 8981501 FIRE BOTTLE DOUG DC9 DC981 3022081 WP APU DISCHARGED A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 13 805ME 48031 NR 2 FIRE BOTTLE AGENT LOW LIGHT NR 2 LIGHT ILLUMINATED. FOUND NR 2 FIRE BOTTLE HAD DISCHARGED INTO THE APU COMPARTMENT . REMOVED AND REPLACED FIRE BOTTLE. (K) 2 L 7 2 4F A6WE 20081006 EA 2008 10 6 A6WA200840559 1 20080806 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A A6WA K NONE F FLT CONT AFFECTED AP APPROACH 1 GL 31 448AW 7804 FLAPS FAIL AT 30 DEGREES ON APPROACH REF PREVIOUS WRITE UP. COMPLIED WITH FLAP RESET PROCEDURE IAW AWAC SUPP 98-018B ST EPS 1.3 AND 1.4 FLAP SYSTEM RESET OK. 2 L 7 2 4F RT A21EA 20081006 NM 2008 10 6 AALA200802141 1 20080819 A 3350 LIGHT BOEING 737 737823 13844BZ NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 948AN 30086 DFW EXTERIOR EMERGENCY LIGHT AT RT AFT OVERWING INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RT AFT OVERW ING. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081006 NM 2008 10 6 AALA200802071 1 20080811 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 938AN 29533 DFW EMERGENCY EXIT LIGHT AT RT AFT OVERWING INOPERATIVE. REPLACED LAMP FOR EMERGENCY EXIT LIGHT AT RT AFT OVERWING. SY STEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081006 WP 2008 10 6 AALA200802047 1 20080809 A 2910 HYDRAULIC LINE DOUG DC9 DC982 3022082 WP HYDRAULIC SYSTEM LEAKING A AALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 21 7508 49802 ORD INFLIGHT T336/09AUG. CREW REPORTED LANDING GEAR RETRACTION WAS SLOW FOLLOWED BY RT HYDRAULIC FLUID QUANTITY AT ZERO . LOWERED GEAR MANUALLY AND RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND LEAKING HYDRAULIC RETURN LINE ON RT SID EWALL OF AFT CARGO. REPLACED HYDRAULIC LINE. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081007 NM 2008 10 7 YENA2008082 1 20080826 A 2150 A/C PACK EMB ERJ190 ERJ190100IGW 3260408 NM NR 2 CONTAMINATED A YENA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION IN INSP/MAINT 1 EA 15 249JB 19000045 FLT NR 1191, JFK-ACK, AIR TURN BACK TO JFK, AFTER ROTATION BOTH PILOTS SMELLED ELCE. SMOKE. BOTH NOTED SMOKE HAZE IN CO CKPIT. INFLIGHT CALLED ON INTERCOM & STATED THERE WAS SMOKE IN THE CABIN. SMOKE WAS COMING FROM FWD LAV AT ABOUT 1000` AGL. THE RED FWD LAV SMOKE CAS POSTED. OPS CHECKED LAVS SMOKE DET. PER AMM 26-14-00.01. OPS CHECKED THE OPERATION TRU `S PER AMM 24-31-00. ALSO INSPECTED BOTH PACKS FOR DEBRIS, FOUND NR 2 PACK HAD COFFEE GROUNDS & COFFEE STAINS IN INTAKE . CLEANED DEBRIS, RAN BOTH PACKS. THEY OPS CHECKED OK PER AMM 21-51-05. ALSO PERFORMED FIM TASK FOR SMOKE PER 21-20-0 0-810-A. ALSO RAN BOTH ENGINES AT CLIMB 2 POWER WITH RECIRC. FAN ON/OFF & NO ABNORMAL SMELL PER 71-80-01. ALL TASKS C 2 L 7 2 4F RT A57NM 20081007 EU 2008 10 7 F3LA200800587 1 20080825 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319112 3930323 EU CABIN FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 21 903FR 1560 REFERENCE NON ROUTINE 104231. DURING EXIT CHECK, INSPECTION NOTED LT FORWARD EMERGENCY POWER SUPPLY UNIT FAILED EMERGEN CY LIGHTS TEST. MX R&R LT FORWARD EMERGENCY POWER SUPPLY UNIT IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 33-51-38- 400-001. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081007 NM 2008 10 7 F3LA200800586 1 20080821 A 5320 D53480043205 SILL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 928FR 2236 REFERENCE NON ROUTINE CO50131. DURING C3 C-CHECK, INSPECTION NOTED NUT PLATE HOLE ON R-2 DOOR SILL, AFT AND OUTBOARD OF R-2 AFT GIRT BAR ATTACH FITTING WAS CORRODED. MX INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH THE REQUIREMENTS OF ENGIN EERING AUTHORIZATION NR A9-53R-30582. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081007 NM 2008 10 7 KCSA081428 1 20080827 A 5412 BULKHEAD BOEING 747 7472B4B 138481B NM NR 4 PYLON CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 NR 4 PYLON AT NAC STA-221.9 BULKHEAD WEB CHAFFED AT HYD PRESSURE LINE. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081431 1 20080827 A 2810 SKIN BOEING 747 747249F 1384849 NM CENTER FUEL TANK CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 STA-1241 LBL-1 TO LBL-14 CENTER TANK UPPER SKIN HAS CORROSION. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081433 1 20080828 A 5330 SKIN BOEING 747 7472B4B 138481B NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 FUSELAGE SKIN CORRODED AT STA-2480 STR-49R. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081440 1 20080902 A 5314 ATTACH BRACKET BOEING 747 747122 1384872 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 KEELBEAM ATTACH BRACKET CRACKED AT BS 1267, LBL-9, WL-116. 2 L 7 4 4F RT A20WE 20081007 EA 2008 10 7 MAS2008F00066 1 20080820 A 5270 SENSOR CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY EXIT OUT OF ADJUST A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 906FJ 15006 ASH FLT 2611 CLT-IAH. LH AFT EMERGENCY EXIT CAUTION ON GROUND. MX ADJUSTED SENSOR. 2 L 7 2 4F RT A21EA 20081003 NM 2008 10 3 2008UALA05678 1 20080911 A 2421 1701766 GENERATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RIGHT LEAKING A UALA O OTHER W K INADEQUATE Q C FLUID LOSS IN INSP/MAINT 1 WP 29 213UA 30219 RIGHT BACK UP GENERATOR OFF OR FAILED. RIGHT BUG WILL NOT HOLD OIL LEAKING ON ENG RUN. NR 2 ENGINE BUG FOUND UNDERSERV ICED. SERVICED UNIT RAN ENGINE, WITHIN 2 MINUTES OIL COULD BE SEEN EVACUATING FROM OVERFILL DRAIN. REMOVED BUG. INSTA LLED REPLACEMENT BACK UP GENERATOR. OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081003 NM 2008 10 3 CALA0800876 1 20080912 A 5320 FLOOR SUPPORT BOEING 757 757224 1384958 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19136 29285 AFT CARGO PIT FLOOR SUPPORT STRINGER CORRODED OUT OF LIMIT STA 1470 LBL 2.90. REPLACED AS PER ECRA 5321-01567. 2 L 7 2 4F RT A2NM 20081003 NM 2008 10 3 SWAA085036 1 20080914 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 328SW 23692 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 812, STR 18L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085049 1 20080914 A 2560 65C16820 FITTING BOEING 737 7373A4 1384585 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 679AA 23291 DURING SCHEDULED BRDG CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20081003 EA 2008 10 3 HNAA0800276 1 20080907 A 6120 3V19 SWITCH DHAV DHC8 DHC8311 1386006 EA COCKPIT DEFECTIVE A HNAA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 07 333EN 35035 221 AT AN ALTITUDE OF APPROXIMATELY 100 FEET AND AFTER THE LANDING GEAR WAS SELECTED UP, THE NR 1 ENGINE BETA LOCKOUT FAILED . PROP SPEED DROPPED TO 990 RPM AND FLUCTUATED UP TO 1080 RPM. THE EMERGENCY CHECKLIST WAS PERFORMED AND THE ACFT WAS RETURNED TO THE ORIGINATING FIELD. AN EMERGENCY WAS NOT DECLARED. WHILE TRYING TO DEACTIVATE THE BETA SYSTEM, THE PROP WOULD STILL CYCLE IN AND OUT OF BETA RANGE. MX TROUBLESHOOTING DISCOVERED THE POWER LEVER MICRO-SWITCH 6141-S3 TO BE D EFECTIVE. THE SWITCH WAS CHANGED AND SYSTEM RE-ACTIVATED. THE SYSTEM WAS THEN OPS CHECKED WITH APPLICABLE WORKCARD AND CHECKED GOOD. ACFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 20081003 2008 10 3 2008UALA05690 4 20080911 A 2565 B14056015 O-RING AIRCRUISERS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE BLOWN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 503UA 0425 24624 LOW BOTTLE. O-RING ON FILLER VALVE BLOWN OUT. REMOVED & REPLACED ALL EXTERNAL O-RINGS PER JD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081003 NM 2008 10 3 2008UALA05722 1 20080914 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 187UA 26877 FOUND AT SEAT 5A EEL BROKEN. LIGHT FOUND BROKEN. REPLACED EEL. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081003 NM 2008 10 3 2008UALA05723 1 20080914 A 3350 BR8164005 COVER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 845UA 1585 EMERGENCY EXIT LIGHT COVER MISSING FROM FWD CLOSET BULKHEAD AT DOOR 1L. DISCOVERED COVER IS MISSING. REPLACED LIGHT AS SY. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05727 1 20080914 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 SEAT 5F EMERGENCY LIGHT INOP. LIGHT FOUND INOP. REPLACED LAMP. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081003 NM 2008 10 3 AALA200801941 1 20080723 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 391AA 27451 MIA EMERGENCY LIGHTS AT SEAT ROWS 20B, 25B, AND 28B INOPERATIVE. CHARGED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 20B, 25B, AND 28B. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A1NM 20081003 WP 2008 10 3 AALA200801990 1 20080727 A 3260 PROXIMITY SENSOR DOUG DC9 DC983 3022083 WP NLG INOPERATIVE A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 961TW 53611 DFW INFLIGHT T472/27 JUL (REPEAT). CREW REPORTED NOSE LANDING GEAR WARNING INDICATION AND LANDING GEAR AURAL WARNING ON APPROACH. LANDED DFW WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR DOWNLOCK PROXIMITY SENSOR. SYSTEM GROUND CHECKED N ORMAL OPS. (CLOSED) 2 L 7 2 4F RT A6WE 20081003 NM 2008 10 3 AALA200801988 1 20080727 A 2120 UNKNOWN BOEING 757 757223 1384957 NM CABIN ODOR A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 661AA 25295 IAD INFLIGHT T2009/27JUL JFK TO UVF. CREW REPORTED CABIN SMOKE DETECTORS SOUNDED DURING FLIGHT THEN STOPPED FOLLOWED BY ELECTRICAL BURNING SMELL. LANDED IAD WITHOUT INCIDENT. NO SIGN OF SMOKE OR SMELL. COULD NOT DUPLICATE. SYSTEM GROUN D CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20081006 WP 2008 10 6 AALA200802028 1 20080805 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 561AA 53091 LGA EMERGENCY FLASH LIGHT AT FORWARD ENTRY DOOR HAS BROKEN STRAP. REPLACED STRAP FOR EMERGENCY FLASH LIGHT AT LT AT FOR WARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F A6WE 20081006 EU 2008 10 6 USAA920081595 1 20080901 A 3350 321454 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 633AW 58701 13892 82 LOG PAGE 4436163 FLT NR 605 PHX EEL EMERGENCY LIGHT TEST FAILS BATTERY FORWARD LT. COMM FWD L MSG ON CIDS. MX R&R THE POWER SUPPLY UNIT AT FORWARD LT POSITION. EMERGENCY LIGHT SYSTEM TESTS GOOD. 2 L 7 2 4F RT A28NM 20081006 NM 2008 10 6 USAASB08073 1 20080830 A 3350 1012721 LIGHT BOEING 737 7373G7 1384595 NM CABIN DEFECTIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 154AW 23776 PHX THE EMERGENCY ESCAPE PATH LIGHTING WAS DIM AT ROWS 5-9 AND INOPERATIVE AT ROW 10. MX REPLACED THE LIGHT ASSEMBLY AT ROW 10. OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 20081006 NM 2008 10 6 USAA920081606 1 20080809 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT Q6 MAJOR REPAIR NR 03C10853057/006 LEVEL 2 CORROSION ON FLOOR BEAM T CAP AT BS986, BLO. REPAIRED T CAP UPPER FLANGE IAW B737 TYPICAL REPAIR NR 53-60-01 REV A. 2 L 7 2 4F RT A16WE 20081006 EA 2008 10 6 TRAX200801022 1 20080820 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 970EV 7527 JOB 8752721 OPERATION 104 LT FS 625 OBLIQUE ANGLE CRACKED. DUPLICATE WRITE YP REF MWC 8752721 OP 253 FOR REPLACEMENT. 2 L 7 2 4F RT A21EA 20081006 NE 2008 10 6 EXD2008F00000 2 20080821 A 7314 9234A7 PUMP AMD FALC20 FALCOND 2720304 EU GE CF700 CF7002D2 30010 NE LT ENGINE FAILED E EXDA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 19 961AA 205 245U092B THE FLIGHT CREW REPORTED APPROXIMATELY (1) HOUR INTO THE FLIGHT, THE LT ENGINE SHUT DOWN WITH NO WARNING OR PRIOR INDICA TION OF A PROBLEM. THE TREND MONITORING WAS COMPLETED PRIOR TO THE ENGINE PARAMETERS WERE NORMAL. THE FLIGHT CREW PROMPT LY NOTIFIED ATC AND LANDED WITHOUT FURTHER INCIDENT. MECHANIC WAS DISPATCHED WITH PARTS. AC FLIGHT LOG PAGE NR 1655, THE LT FUEL CONTROL UNIT AND THE LT FUEL PUMP WERE REMOVED AND REPLACED WITH SERVICEABLE UNITS, OPS AND LEAK CHECK GOOD AND THE ENGINE POWER RUNS WERE PERFORMED IAW MM CHAPTER 72. NO DEFECTS NOTED. AC WAS RETURNED TO SERVICE. (K) 2 L 7 2 4F 4 F A7EU E7EA 20081006 EA 2008 10 6 TRAX200801045 1 20080823 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 846AS 7328 CLIP CRACKED AT FS605 AT CARGO DOOR SILL AND INTERCOSTAL ATTACHMENT (RESOLVED ON W/O 96197 TASKCARD N/R 00022) JOB COMPL ETE ITEM 1. DRILLED UP NEW CLIP IAW CRJ 200 51-40-11RAP 7025969. ITEM 2. 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 SWIA200820345 1 20080724 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 958SW 7833 C-CHECK, PASSENGER DOOR AFT WEB CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081118 WP 2008 11 18 08FDEA04708 1 20081104 A 5414 AJC741595 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 46631 AFT NACELLE, FIREWALL SEAL PLANE AT FS Y2166 AND RIGHT SIDE OF THE TRAILING EDGE OF THE DIVERTER; HAS WORN SKIN AND IS C RACKED. REMOVED AND FABRICATED NEW SKIN SECTION IAW SRM 51-35-01 VOL II AND DWG AJC7415 REV BK, ALODINED AND PRIMED IAW SRM 51-21-01 VOL I PG1. INSTALLED NEW SKIN SECTION IAW SRM 51-35-01 VOL II PG 1 AND DWG AJC 7415 REV BK. 2 L 7 3 4F RT A22WE 20081118 SO 2008 11 18 SWIA200820350 1 20081109 A 3350 LAMP EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 FLT 5527 - FLOOR EMERGENCY LIGHT STRIP FORWARD RED LIGHT INOP. RELAMPED. 2 L 7 2 4T RT A31SO 20081118 EA 2008 11 18 VNA2008F00008 1 20081007 A 2751 601R930303 TRANSMITTER CNDAIR CL600 CL6002B19 1900309 EA TE FLAP FAILED A VNAA O OTHER O OTHER DE DESCENT 1 GL 05 220PS 11119 7887 CREW REPORTED IN DESCENT AT 290 KTS W/ AUTOPILOT ON, UCA AND FLAP INDICATORS DEPLOYED ON EICAS PAGE. FLAP INDICATOR SHO WED GREEN BAR MOVEMENT AND READOUT MOVED TO 2 DEG. ACFT HAD PITCH OSCILLATIONS OF APPROX 3 DEG NOSE UP AND DOWN. MAINT REMOVED AND REPLACED THE FLAP TRANSMITTER. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE. (K) 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 SWIA200820351 1 20081108 A 2150 SENSOR CNDAIR CL600 CL6002B19 1900309 EA RT A/C PACK FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 934SW 7722 FLT 6550 - "SMOKE TOILET" MESSAGE AFTER TAKE OFF. REPLACED RIGHT PACK TEMPERATURE SENSOR. 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 SWIA200820352 1 20081031 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA BS 640 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 447SW 7677 FLT 3780 - CRACK AT UPPER WEB OF ENGINE SUPPORT BEAM MID SECTION AT FS 640. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 SWIA200820353 1 20081031 A 5346 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 447SW 7677 FLT 3780 - CRACK AT UPPER WEB OF BOX BEAM MID SECTION. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081118 NM 2008 11 18 08FDEA04883 1 20081115 A 5347 BAC15201430 SEAT TRACK BOEING 727 7272D4 138407U NM ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FUSELAGE UPPER LOBE STRUCTURE, SEAT TRACK HAS LONG CHAFE AT STA 520, RBL 64 BLENDED CHAFED AREA. MAPPED OUT AND SENT T O EG FOR BLEND ALLOWABLE LIMITS. BLEND IS WITHIN LIMITS. REF EA 7-5310-118317, ALODINED AND PRIMED REF SRM 51-10-02. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081118 EU 2008 11 18 08FDEA04752 1 20081105 A 5321 R532B385600400 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 MAIN DECK FLOOR PANEL AT FRAME 55, LBL 36 IS BROKEN. FABRICATED NEW PANEL FROM STOCK MATERIAL, INSTALLED INSERTS, POTT ED EDGES, APPLIED NONSKID, PART ID MARKED IAW SRZ 25-005 REV G. 2 L 7 2 4F RT A35EU 20081118 SO 2008 11 18 C2XA08CL113 1 20081012 A 3350 82311 SIGN EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11150 145756 DURING ROUTINE MX THE AFT EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE AFT EMERGENCY EXIT S IGN. OPS CHECKS WERE GOOD. 2 L 7 2 4F RT 20081118 EU 2008 11 18 QML2008F00020 1 20081011 A 3397 WIRE BOLKMS 117 BK117B2 5626013 EU SEARCH LIGHT SHORTED E QMLA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 03 911KD 7237 PRIOR TO LIFTOFF WITH TRANSPORT TEAM THE PILOT DETECTED AN ACRID ODOR IN COCKPIT. THE PILOT THOUGHT THIS WAS ENVIRONMEN TAL IN NATURE AND ODOR DISSIPATED WITHIN 10 SECONDS. THE PILOT COMPLETED THE FLIGHT WITHOUT INCIDENT. THE PILOT NOTICE D THE SEARCHLIGHT INOPERATIVE. UPON TROUBLESHOOTING, I REALIZED THE ODOR MAY HAVE COME FROM RECENT WORK ON COLLECTIVE H EAD/SEARCH LIGHT SWITCH. MX WAS ABLE TO IDENTIFY BURNED WIRES ON THE SEARCHLIGHT WIRING BUNDLE AS THE SOURCE OF THE ODO R. THE WIRES ON THE SEARCHLIGHT SHORTED ON A CLAMP HOLDING PITOT TUBE ACCUMULATOR IN PLACE. WIRES WERE BURNED AND INSU LATION MELTED. A SERVICEABLE SEARCHLIGHT FROM ANOTHER ACFT WAS USED AND THE ORIGINAL WIRE HARNESS WAS REPAIRED AND REUS 1 G 7 2 3U NC H13EU 20081118 EA 2008 11 18 TRAX200801132 1 20080907 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 980EV 7759 PAX DOOR FWD WEB IS CRACKED IN ZONE 2. REMOVED CRACKED SUCTIONS OF FWD WEB PAX DOOR AND REPAIRED IAW REO 601R-52-11-702 , REV A STEPS 1-10, 15. STEPS 13, 14 AND 17 ARE N/A. AREA REQUIRES SEALANT AND PAINT. SEALED AND CLEANED IAW REO 601R- 52-702. 2 L 7 2 4F RT A21EA 20081117 NM 2008 11 17 KCSA081586 1 20081116 A 5414 SKIN BOEING 747 747212B 1384886 NM NR 3 PYLON CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 NR 3 PYLON O/B SKIN CRACKED AT LOWER EDGE NAC STA 221.9. 2 L 7 4 4F RT A20WE 20081117 NM 2008 11 17 KCSA081587 1 20081116 A 5712 RIB BOEING 747 747212B 1384886 NM LT WING CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 LT WING RIB LOWER CHORD CRACKED AT WS 1516, 35 INCHES AFT OF FRONT SPAR. 2 L 7 4 4F RT A20WE 20081117 NM 2008 11 17 SWAA086204 1 20081113 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 3L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086215 1 20081113 A 5313 6551698 STRINGER SPLICE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CORRODED AT BETWEEN BS 420 TO BS 440, STR 28R. REMOVED AND REPLACED S PLICE PER SRM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086216 1 20081113 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND RT CREASE BEAM WEB CORRODED BETWEEN BS 380 TO BS 400. REMOVED AND REPLACED WEB PER SR M. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086217 1 20081113 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 440 TO BS 460. REMOVED AND REPLACED WEB PER SR M. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086218 1 20081113 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086223 1 20081113 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 501SW 24178 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 894, STR 25R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086224 1 20081113 A 5310 6547978 CREASE BEAM BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND LT DOOR CREASE BEAM CORRODED BETWEEN BS 312 TO BS 360. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086225 1 20081113 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 967, STR 27L. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086226 1 20081113 A 5320 BAC1508 FITTING BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 741SA 29277 DURING SCHEDULED 10Y CHECK, FOUND SHEAR FITTING CRACKED AT BS 540, RBL 40. REMOVED AND REPLACED FITTING PER SRM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086234 1 20081113 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 30544 DURING SCHEDULED HC1 CHECK, FWD LT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081117 NM 2008 11 17 SWAA086235 1 20081113 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 759GS 30544 DURING SCHEDULED HC1 CHECK, LT OVERWING EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081117 EA 2008 11 17 ASOA200801494 1 20081112 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 820AS 7188 LT FUSELAGE EMERGENCY LIGHT FWD OF WING INOP. 2 L 7 2 4F RT A21EA 20081117 EA 2008 11 17 ASOA200801495 1 20081113 A 7931 OIL SYSTEM CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE MALFUNCTIONED A ASOA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 27 886AS 7531 RT ENG OIL PRESSURE MSG IN FLT. OIL PRESSURE FLUX BETWEEN 40-24 PSI, FOLLOWED QRH EMERGENCY, 1-13 OIL PRESS WENT TO 24 PSI, IN FLT ENG SHUTDOWN PER QRH. EN ROUTE TO ATL A/C DIVERTED TO MCI DUE TO MTC - EMERGENCY DECLARED. REMOVED AND REP LACED NR 2 ENG IDG, EDP AND STARTER CARBON SEALS IAW CRJ 200 AMM 72-60-00. OPS CHECKS GOOD, NO DEFECTS NOTED AT THIS TI ME. 2 L 7 2 4F RT A21EA 20081117 EU 2008 11 17 UPS08153878 1 20081028 A 5321 B5327075300000 FLOOR PANEL AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO BAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 142UP 0825 INSPECTION TYPE:1C3C MAIN CARGO DECK FLOOR PANEL 241LJ HAS FIELD REPAIRS. REPAIRED MAIN CARGO DECK FLOOR PANEL 241LJ RE F A300-600 SRM 53-10-20 TABLE 201 PARA 8A. 2 L 7 2 4F RT A35EU 20081118 EA 2008 11 18 ASOA200801487 1 20081109 A 3350 COVER CNDAIR CL600 CL6002B19 1900309 EA CABIN OUT OF POSITION A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 927EV 7844 EMERGENCY LIGHT COVER BY PAX DOOR FELL OFF, KNOCKED OFF DURING DEPLANING. 2 L 7 2 4F RT A21EA 20081118 EU 2008 11 18 08FDEA04877 1 20081112 A 5230 A5237807900000 FITTING AIRBUS 310 A310324 3930206 EU CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 BULK CARGO DOOR FITTING UNDERNEATH SPRING MECHANISM IS CRACKED. REMOVED CRACKED FITTING IAW A310-300 SRM 51-72-10. LO CATED; DRILL & INSTALLED NEW FITTING P/N A5237807900000 IAW A310-300 SRM 51-72-10. 2 L 7 2 4F RT A35EU 20081118 NM 2008 11 18 2008UALA06426 1 20081107 A 3010 CIRCUIT CARD BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ANTI-ICE SYSTEM FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 779UA 26941 ANTI-ICE WING EICAS MESSAGE. REPLACED ACIPS CARD. OPS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081118 NM 2008 11 18 08FDEA04849 1 20081111 A 5320 69205761 CHANNEL BOEING 727 7272D4 138407U NM ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 PASSENGER CABIN GILL LINER "Z" CHANNEL STA 1148 STR 14L CHAFED INTO FRAME SPLICE BLENDED CHAFED AREA FRAME SPLICE STA 11 48 STR 14L REF SRM 53-10-1 ORIG "T" .112 LOSS .040 OUT OF LIMITS REF SRM 53-10-1 P1-2. REPLACED FRAME SPLICE REF SRM 51 -30-2, P2 THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081118 NM 2008 11 18 08FDEA04888 1 20081115 A 5320 655850438 SUPPORT ANGLE BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 LWR FUSELAGE ANTENNA SUPPORT ANGLES AT FASTENER HOLES HAVE CORROSION, BS 740-760, RBL 6 TO LBL 6. REMOVED CORROSION AT LWR FUSELAGE ANTENNA SUPPORT ANGLES STA 740 - 760, RBL 6 TO LBL 6, REF SRM 51-10-6, MATERIAL LOSS 50 PERCENT OFF, FOUND TO BE OUT OF LIMITS REF SRM 53-10-1 FIG 1. FABRICATED NEW ANGLES REF BOEING DWG 65-32330, 69-25418. TREATED AND PRIM ED AND INSTALLED REF SRM 51-10-2 PG 1-7, MM 51-20-151-7, 51-30-02 PG 2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081118 EA 2008 11 18 SWIA200820359 1 20080731 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 917SW 7641 C-CHECK, UPPER RIGHT FLOOR SUPPORT ANGLE AT FS 280 CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 SWIA200820363 1 20081112 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 411SW 7067 FLT 4859 - AFT CEILING LEVEL EMERGENCY FLOODLIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081118 EU 2008 11 18 08FDEA04786 1 20081107 A 5311 A53833131204 FRAME AIRBUS 300 A300F4605R 3930327 EU ZONE 200 GOUGED A FDEA O OTHER O OTHER IN INSP/MAINT 1 CE 21 654FE 738 MAIN CARGO DECK HAS GOUGE ON FRAME 54 3 INCH BELOW STR.12L BLENDED AREA IAW SRM 51-73-10, FOUND TO BE WITHIN LIMITS. PE RFORMED HFEC IAW NTM 51-10-08 PT6, NO CRACK INDICATIONS NOTED, TREATED AND PRIMED IAW SRM 51-23-20. 2 L 7 2 4F RT A35EU 20081118 NM 2008 11 18 2008UALA06480 1 20081110 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 UPPER DECK DOOR LIGHT NOT TESTING. RELAMPED LT DOOR SLIDE TEST LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 20081118 NM 2008 11 18 2008UALA06481 1 20081111 A 2130 CABIN PRESSURE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE MALFUNCTIONED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 676UA 30028 CREW UNABLE TO PRESSURIZE DURING CLIMB. RTFL. ACCMP PRESSURIZATION CHECK. DID DECAY CHECK, ALSO WITHIN TOLERANCE. CH ECKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081118 EU 2008 11 18 2008UALA06482 1 20081111 A 5320 BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 404UA 450 RT BEAM LABELED - Y1292 HAS CORROSION AT FR66 AND IS MARKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED BEAM TO AIRCRAFT. N EEDS SUPPORTS BETWEEN FR64 - FR65 INSTALLED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081118 EA 2008 11 18 SWIA200820342 1 20080712 A 5312 ISOLATOR CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 440SW 7589 C-CHECK, THREE ISOLATORS CRACKED AT REAR PRESSURE BULKHEAD FORWARD FACE, REPLACED. 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 SWIA200820343 1 20080724 A 5312 ISOLATOR CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 958SW 7833 C-CHECK, SIX ISOLATORS CRACKED ON AFT BULKHEAD FS 621, REPLACED. 2 L 7 2 4F RT A21EA 20081118 EU 2008 11 18 08FDEA04882 1 20081114 A 3260 GA558614 HOUSING AIRBUS 310 A310203 3930313 EU MLG SWITCH CRACKED A FDEA O OTHER N FALSE WARNING LD LANDING 1 CE 21 411FE 359 ON ARRIVAL, NOSE GEAR INDICATED UNSAFE ON BOTH SYSTEM 1 AND 2. COMPLIED WITH QRH AND USED MLG GRAVITY EXTEND CHECKLIST. WHEN COMPLETED UNSAFE WARNING REMAINED, VISUALLY CHECKED. INDICATED DOWN AND LOCKED. LANDED WITH INDICATION. FOUND SW ITCH 40 GB HOUSING BROKEN. REMOVED & REPLACED HOUSING AND SWITCH IAW MM 32-00-00-4. COMPLIED WITH NOSE GEAR SWING IAW MM 32-31-00-5. ALL INDICATIONS NORMAL. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 20081118 EU 2008 11 18 08FDEA04898 1 20081117 A 5321 B5323362600000 FLOOR PANEL AIRBUS 310 A310324 3930206 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 FLOOR PANEL 232 LG IS CRACKED. FABBED NEW FLOOR PANEL 231 LG USING THE OLD PANEL AS A TEMPLATE. POTED & CURED INSERTS; POTTED; CURED & SANDED THE EDGES. APPLIED NON-SKID TAPE & PART MARKED PANEL IAW FEDEX DWG SRX 25-005; REV "G". 2 L 7 2 4F RT A35EU 20081118 EU 2008 11 18 08FDEA04899 1 20081117 A 7120 A54611219600 MOUNT AIRBUS 300 A300F4605R 3930327 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 NR 1 PYLON ENGINE PYRAMID MOUNT ALIGNMENT PIN HOLE IS PITTED. CHECKED ALLOWABLE LIMITS OF SPIGOT FITTING IAW SRM 54-51 -81. ORIGINAL HOLE DIAMETER OF 1.350. FOUND TO BE OUT OF LIMITS DIAMETER WAS 1.371. REAMED HOLE IN STEPS OF 1.389-1.4 10, TO 1.409-1.428 WITH FINAL OF 1.429. CAD PLATED IAW SRM 51-21-10 THEN INSTALLED NEW BUSHING. 2 L 7 2 4F RT A35EU 20081118 SO 2008 11 18 JIK2008F00005 1 20081014 A 7810 LW16697AWL EXHAUST DUCT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2B NE LT ENGINE CRACKED E JIKA A UNSCHED LANDING Y A ENGINE STOPPAGE FLAME/FIRE CL CLIMB 1 WP 01 3BT 253 317752172 L930361A AFTER DEPARTURE, AT ABOUT 1000 FEET AGL, THE PILOT REPORTED THAT THE LT ENGINE MANIFOLD PRESSURE DROPPED SUDDENLY, THE E NGINE SURGED AND THEN QUIT RUNNING. THE PILOT RETURNED TO DEPARTURE SAFELY. UPON EXAMINATION, IT WAS FOUND THAT THE EXH AUST FLANGE AT THE WASTE GATE HAD CRACKED AND BROKEN OFF. THE RESULTING BLAST OF HEAT FROM THE EXHAUST MELTED PART OF THE WASTE GATE CONTROLLER, SPILLING OIL AND CAUSING AN INFLIGHT FIRE. THE DAMAGE FROM THE FIRE WARPED THE SKINS ON THE BOTTOM OF THE WING, BURNED THE OUTER SKIN OFF THE LT MLG DOOR AND BURNED LARGE HOLES IN THE FLAP. IT IS HIGHLY RECOMME NDED TO PAY CLOSE ATTENTION TO THE FLANGES AND WELDS ON THESE PMA ASSEMBLIES, AS FAILURE OF THE EXHAUST PIPES COULD CAUS 1 L 7 2 3O 3 O A20SO E14EA 20081118 SO 2008 11 18 JIK2008F00006 1 20081016 A 7810 LW10161AWL EXHAUST DUCT PIPER PA31 PA31350 7103110 SO ENGINE CRACKED E JIKA K NONE O OTHER IN INSP/MAINT 1 WP 07 35805 1505 318052090 DURING INSPECTION ON JUNE 26, 2008 IT WAS NOTED THAT THERE WAS A CRACK THAT WENT AROUND THE CIRCUMFERENCE OF THE NR 7 EX HAUST FLANGE. A NEW MANIFOLD ASSY WAS ORDERED AND INSTALLED. WHILE REMOVING THE CRACKED ONE, IT WAS DISCOVERED THAT TH ERE HAD BEEN COMPLETE SEPARATION. THIS EXHAUST MANIFOLD IS A PMA PART FOR THE ENGINES, AND WAS INSTALLED NEW AT OVERHAU L 1505 HOURS PRIOR. IT WAS NOTED THAT A NEW WELDING TECHNIQUE HS BEEN USED RECENTLY IN THE FLANGE AREA. (K) 1 L 7 2 3O A20SO 20081118 SO 2008 11 18 JIK2008F00004 1 20081017 A 7810 LW16697AWL EXHAUST DUCT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2B NE ENGINE CRACKED E JIKA K NONE O OTHER IN INSP/MAINT 1 WP 01 27426 300 317752175 L709761A ON 9/11/08 DURING AN INSP, IT WAS FOUND THAT THE EXHAUST FLANGE WHERE THE MANIFOLD IS CLAMPED TO THE WASTE GATE HOUSING, THERE WAS A CRACK IN THE FLANGE RADIUS THAT RAN APPROXIMATELY .3333 OF THE WAY AROUND THE PIPE. THE MANIFOLD ASSY WAS R EPLACED WITH A NEW ASSY. IT IS HIGHLY RECOMMENDED TO PAY CLOSE ATTENTION TO THE FLANGES AND WELDS ON THESE PMA ASSEMBLI ES, AS FAILURE OF THE EXHAUST PIPES COULD CAUSE CONSIDERABLE DAMAGE TO THE AIRCRAFT. IT MUST BE NOTED THAT THE MFG WELD PROCESS IN THIS AREA HAS RECENTLY CHANGED. (K) 1 L 7 2 3O 3 O A20SO E14EA 20081118 EA 2008 11 18 TRAX200801239 1 20080929 A 5210 SPRING STRUT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DEFECTIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 973EV 7575 MAIN DOOR IS NOT LOCKING CLOSE. REMOVED AND REPLACED FWD PAX DOOR GAS SPRING STRUT IAW AMM 52-11-14. OPS CHECK GOOD, A CFT OK FOR SERVICE. (K) 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 TRAX200801133 1 20080907 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 980EV 7759 CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.5 INCHES. REMOVED CRACKED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET IAW SRM 51-92-21. (K) 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 TRAX200801240 1 20080929 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 909EV 7658 EXIT PLACARD ON MAIN CABIN DOOR PARTIALLY MISSING ALONG WITH EMERGENCY DIRECTIONAL ARROW. FLT 4250 DEL 15 MINS. REPLAC ED EXIT AND ARROW ON PAX DOOR IAW AMM. (K) 2 L 7 2 4F RT A21EA 20081119 NM 2008 11 19 2008UALA03128 1 20080601 A 5320 ATTACH FITTING BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 907UA 25007 CRACKS FOUND AT ATTACH CLIP STA 360 STR 11L, STRINGER SPLICE CHANNEL STA 360 STR 15L, INTERCOSTAL WEB STRAP STA 360 STR 16L AND INTERCOSTAL ATTACH ANGLE STA 348 STR 15L. MAJOR REPAIR ACCOMPLISHED. AREAS REPAIRED PER UA-EVA- 71614 AND REO- 01077, TO BE REINSPECTED WITHIN 6000 CYCLES AND EVERY 6000 CYCLES THEREAFTER. CURRENT PTC 30113. FIRST REINSPECT AT 36 113 CYCLES. PER SB737-53A1204 (AD 2005-20-03) 2 L 7 2 4F 4 F RT A16WE E21EU 20081119 NM 2008 11 19 2008UALA06492 1 20081109 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 LT OVERWING EMERGENCY EXIT LIGHTS INOP, FWD & AFT POSITIONS. RELAMPED EMERGENCY LIGHT, OP CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081119 NM 2008 11 19 NWAA084565520 1 20081012 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM EMERGENCY LIGHT DEFECTIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 520US 23208 DURING AN OVERNIGHT LINE CHECK THE EMERGENCY ESCAPE PATH LIGHTING IN THE AFT SECTION OF THE PAX CABIN WAS FOUND TO BE IN OPERATIVE. MX FOUND THE ASSOCIATED BATTERY PACK TO BE DEFECTIVE AND REPLACED IT. ALL OPS CHECKED GOOD AFTER REPLACEMEN T. 2 L 7 2 4F RT A2NM 20081119 NM 2008 11 19 2008UALA06499 1 20081112 A 2497 WIRE HARNESS BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE IDG SHORTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 786UA 26938 NR 2 ENG IDG WILL NOT DISCONNECT. SWAPPED NR 1 AND NR 2 IDG DISCONNECT SWITCH ON OVERHEAD, NO HELP. REMOVED ALL IDG EL ECTRICAL CONNECTORS, NO BENT PINS OR DEFECTS NOTED. SUSPECT BAD IDG FROM STOCK. NEW IDG ON ORDER. REPLACED IDG PER MM 24-11-01-401, NO HELP. GCU BITE TEST OK. CHECKED PWR & GND AT CONN DM24001A, CKS OK. SOLENOID CHECKS OK. RAN ENG 4 TIMES, GOT IDG TO DISCONNECT ONE TIME. NEED A HEA (PAR (PARTIAL) REPLACED IDG, NO HELP. FOUND BAD HARNESS, SHORTED TO GROUND. REPLACED HARNESS. IDG DISCONNECT CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081119 NM 2008 11 19 2008UALA06500 1 20081110 A 3350 BR964421 COVER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN MISSING A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 836UA 1460 SEAT 2B EMERGENCY EXIT LIGHT COVER MISSING. REPLACED EMERGENCY EXIT LIGHT COVER. 2 L 7 2 4F 4 F RT A28NM E40NE 20081119 NM 2008 11 19 2008UALA06502 1 20081113 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 SEAT ROW 45HJK EMERGENCY LIGHT IS INOP. REPLACED LAMP. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081119 NM 2008 11 19 2008UALA06503 1 20081113 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 SEAT ROW 24ABC EMERGENCY LIGHT IS INOP. REPLACED LAMP, OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081119 NM 2008 11 19 CALA0801073 1 20081113 A 5320 111A72024 STRUCTURE BOEING 737 737824 13844BZ NM FUSELAGE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 34222 28931 INBOARD FLANGE OF THE LOWER CHORD FOR THE HIGH PRESSURE DOOR JUST FORWARD OF STRIKER PLATE IS WORN. FABRICATED AND INST ALLED REPAIR PER ECRA 5351-01069. 2 L 7 2 4F RT A16WE 20081118 NM 2008 11 18 2008UALA06427 1 20081108 A 2751 WARNING SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAP MALFUNCTIONED A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 550UA 25398 FLAP DISAGREE ON APPROACH. FLAPS STUCK ON 20 UNITS. SFOLM TUNG INSPECTED ALL OVERLOAD INDICATORS ON FLAP TRANSMISSION GEAR BOXES AND FOUND OK. OPS CHECKED GOOD IN NORMAL AND ALTERNATE MODE INCLUDING FSEU TEST. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 2008UALA06435 1 20081108 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 788UA 26942 SEATS 1E AFT, 2E BOTH AND 1F FWD EEL LIGHTS INOP. REPAIRED 1E AND 1F. CURRENTLY 2E EEL LIGHTS STILL INOP. NEED INVER TER LOCATED ON 3E STOWAGE BOX. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081118 NM 2008 11 18 2008UALA06437 1 20081108 A 5210 142N273611 FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR CRACKED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 551UA 25399 MAIN CABIN L-4 DOOR TORQUE BOX AREA, AT BS 1645 AND STR 11L, EMERGENCY POWER ASSIST CABLE MECHANISM FITTING CRACKED. RE PLACED EMERGENCY POWER ASSIST CABLE MECHANISM FITTING. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 2008UALA06451 1 20081109 A 3350 S1356B37 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 174UA 24381 UPPER DECK, BS 945 CENTER, EMERGENCY EXIT LIGHT BATTERY PACK WEAK. REPLACED BATTERY PACK. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081118 NM 2008 11 18 08FDEA04779 1 20081107 A 5754 ARB75821 SKIN DOUG MD11 MD11F 3023600 NM NR 3 SLAT CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 593FE 48551 LEFT WING, NR 3 LEADING EDGE SLAT TELESCOPIC DUCT CUTOUT REPAIR DOUBLER INBOARD AND OUTBOARD SIDE LEADING EDGE SURFACE FOUND CHAFING. CHAFE MARK SMOOTHED AS PER SRM 51-21-01, VOLUME II AND REPAIR CARRIED OUT AS PER EA 1-5740-122631. R EPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. SLAT ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-10-5 FOUND 'SATIS'. 2 L 7 3 4F RT A22WE 20081118 NM 2008 11 18 08FDEA04782 1 20081107 A 3260 MS250081 SWITCH BOEING 727 727227 1384078 NM MLG FAILED A FDEA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 CE 21 494FE 21532 "NOSE GEAR DOWN AND LOCKED LIGHT" AND NOSE GEAR UNSAFE LIGHT" ILLUMINATED WHEN LANDING GEAR HANDLE WAS MOVED TO OFF POSI TION FOLLOWING GEAR RETRACTION. BOTH LIGHTS THEN REMAINED ILLUMINATED WHEN LANDING GEAR HANDLE WAS MOVED TO "UP" POSIT ION. JACKED ACFT IAW MM 07-11-000-2 AND RETRACTED NOSE GEAR AND FOUND S92 CONTROL LEVER POSITION SWITCH INTERMITTENT. REMOVED AND REPLACED SWITCH IAW MM 32-61-012-4. SWITCH OPS CHECKS GOOD PER SAME. 2 L 7 3 4F A3WE 20081118 NM 2008 11 18 2008UALA06478 1 20081110 A 2560 P2070003100 FLASHLIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN INOPERATIVE A UALA O OTHER L NO TEST IN INSP/MAINT 1 WP 29 370UA 24539 FWD F/A FLASHLIGHT NOT BLINKING. REPLACED FLASHLIGHT. 2 L 7 2 4F 4 F RT A16WE E21EU 20081118 EA 2008 11 18 SWIA200820358 1 20080731 A 5210 LOCK CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 917SW 7641 C-CHECK, PASSENGER DOOR LATCH-LOCK BOX OUTBOARD LEVER ASSEMBLY FORWARD ATTACH PIN CORRODED. REPLACED PIN. 2 L 7 2 4F RT A21EA 20081118 2008 11 18 2008UALA06479 4 20081110 A 2565 D31517121 MOUNT FITTING AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EVAC SLIDE CRACKED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 805UA 783 R2 DOOR SLIDE LOWER FWD MOUNT FITTING IS CRACKED. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081118 EA 2008 11 18 SWIA200820364 1 20081113 A 3350 CHARGER CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT MALFUNCTIONED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 956SW 7825 FLT 6406 - FLOOR LEVEL EMERGENCY LIGHT STRIP, FORWARD SECTION INOP. RESET BATTERY CHARGER. 2 L 7 2 4F RT A21EA 20081118 WP 2008 11 18 08FDEA04696 1 20081104 A 5414 AUB710826 PANEL DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 NR 3 PYLON PANEL 487 ER IS WORN. NR 3 PYLON PANEL 487ER WAS WORN BEYOND ALLOWABLE LIMITS IAW SRM 54-00-01 VOL I PG 5. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 54-00-01 VOL I PG 11. ALODINED AND PRIMED DOUBLER AND FILLER IAW SRM 51-21 -01 VOL II. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 51-31-01 VOL II. 2 L 7 3 4F RT A22WE 20081118 EA 2008 11 18 SWIA200820340 1 20080712 A 5210 WEB CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 440SW 7589 C-CHECK, PASSENGER DOOR AFT WEB CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081118 NM 2008 11 18 2008UALA06490 1 20081111 A 3397 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN CONTAMINATED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 SEAT EEL INOP FROM SEAT 45ABC TO 53ABC. REPLACED BATTERY PACK (M6011) ABOVE DOOR 4L, NO HELP. FOUND EEL CONNECTOR UNDE R GALLEY MAT SOAKING WET, DRIED OUT WIRING AND SECURED. 2 L 7 4 4F 4 F RT A20WE E24NE 20081118 NM 2008 11 18 2008UALA06491 1 20081112 A 3350 COVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 541UA 25253 ROW 19 DAMAGED FLOOR EMERGENCY EXIT LIGHTING. REPLACED 15 FT SECTION OF LIGHT COVER. LIGHTING TEST OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 EU 2008 11 18 08FDEA04748 1 20081105 A 5321 R532B375400000 FLOOR PANEL AIRBUS 310 A310324 3930206 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 809FD 449 FLOOR PANEL 241 UJ IS CRACKED. FABRICATED NEW PANEL FROM STOCK MATERIAL, INSTALLED INSERTS, POTTED EDGES, APPLIED NONSK ID, PART ID MARKED IAW SRZ 25-005 REV G. 2 L 7 2 4F RT A35EU 20081118 SO 2008 11 18 C2XA08IA224 1 20081010 A 3320 BR90002 BALLAST EMB 145 EMB145LR 3260212 SO LAVATORY LIGHTS INOPERATIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 11551 145411 IAH DURING MX INSPECTION A BURNING ODOR IN THE LAV WAS DISCOVERED. MX R&R THE LT LIGHT BALLAST IN THE LAV. OPS CHECKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081119 NM 2008 11 19 KCSA081541 1 20081023 A 5311 FRAME BOEING 747 747249F 1384849 NM BS 880 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 BS 880 FUSELAGE FRAME CRACKED BETWEEN STR 39R AND STR 40R. 2 L 7 4 4F RT A20WE 20081119 NM 2008 11 19 KCSA081543 1 20081023 A 5347 SEAT TRACK BOEING 747 747249F 1384849 NM BS 320 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 F/O`S FWD O/B SEAT TRACK CRACKED. 2 L 7 4 4F RT A20WE 20081119 NM 2008 11 19 CALA0801072 1 20081112 A 5711 112T20077 SPAR BOEING 767 767224 1385170 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 67157 30436 LEFT WING LEADING EDGE FRONT SPAR WEB FOUND CRACKED AT OFSS 1027 APPROXIMATELY 1 X 1 INCH L SHAPE. LEFT WING FRONT SPAR WEB AT OFSS 1027 REPAIRED PER ECRA 5710-02152. 2 L 7 2 4F RT A1NM 20081119 NM 2008 11 19 CALA0801075 1 20081114 A 5542 65C2596144 SKIN PANEL BOEING 737 737524 1384721 NM RUDDER SCRATCHED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 RUDDER BETWEEN ATTACH POINT 4 AND 5 SCRATCH ON RIGHT SIDE CLOSE TO TRAILING EDGE. ACCOMPLISHED REPAIR OF RT RUDDER SKIN PANEL PER CO EC/RA 5540-01257. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 CALA0801078 1 20081112 A 5534 65538343 DRAG ANGLE BOEING 737 737524 1384721 NM VERTICAL STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 VERTICAL STABILIZER AFT LEFT ATTACH LUG AREA, FWD DRAG ANGLE FITTING HAS CORROSION INSIDE O/B HOLE. REMOVED LT VERTICAL STABILIZER AFT I/B AND O/B ATTACH BOLTS, REMOVED AND REPLACED LT DRAG ANGLE PER B737 SRM 51-40-02. REINSTALLED LT VERT ICAL STABILIZER AFT I/B AND O/B ATTACH BOLTS PER B737 SRM 55-30-00 AND CO WORK CARD 24-55-30-1-2600 SEQ 342. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 CALA0801080 1 20081116 A 5320 141A5410U3 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 79279 31597 INTERCOSTAL BETWEEN STA 277 AND 294.5 AT BL 0 IS CRACKED. REMOVED INTERCOSTAL, INSTALLED NEW INTERCOSTAL PER BOEING DRA WING DOC 141A5400 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 CALA0801082 1 20081117 A 5320 141A541022 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 79279 31597 INTERCOSTAL BETWEEN STA 344 AND 360 AT LBL 11 IS CRACKED AT FASTENER HOLE. REMOVED AND REPLACED CRACKED INTERCOSTAL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 CALA0801083 1 20081117 A 5320 141A541023 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 79279 31597 INTERCOSTAL BETWEEN STA 344 AND 360 AT BL 0 CRACKED AT FASTENER HOLE. REMOVED AND REPLACED CRACKED INTERCOSTAL PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086124 1 20081107 A 3350 81000 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 489WN 33855 FOUND OVERWING EEPLS LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086125 1 20081107 A 3397 411A2212 CONNECTOR BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 782SA 29808 DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. SECURED CONNECTOR PER MM. 2 L 7 2 4F RT A16WE 20081119 2008 11 19 SWAA086067 4 20081030 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 400WN 27891 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086074 1 20081104 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 797MX 27890 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 3 SEAT C. REPAIRED EEPLS PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086080 1 20081105 A 3097 601SW CABLE BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 620SW 28036 FOUND CAPT SLIDING WINDOW ANTI ICE POWER CABLE ARCED. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086083 1 20081105 A 2560 P4010021 BATTERY BOEING 737 7377H4 1384404 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 756SA 27872 FOUND FWD EMERGENCY EXIT FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086106 1 20081104 A 3350 1010731 HOUSING BOEING 737 7373H4 1384600 NM CABIN DEFECTIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED HC1 CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT BATTERY PACK HOUSING INOP. REMOVED AND REPLACED HOUSING P ER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086107 1 20081104 A 5753 6546430130 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 350SW 24409 DURING SCHEDULED HC1 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086108 1 20081107 A 2560 P2070001214 FLASHLIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 410WN 27897 FOUND RT AFT FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086248 1 20081113 A 5330 6545776 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 945, STR 25R. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086249 1 20081115 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION UPPER LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086250 1 20081115 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION LOWER LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086088 1 20081110 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CHORD CORRODED AT BS 673, RBL 24. REPAIRED CHORD PER EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086089 1 20081110 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED AT BS 669, LBL 24. REPAIRED CHORD PER EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086090 1 20081110 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED AT BS 665, LBL 24. REPAIRED CHORD PER EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086251 1 20081117 A 5322 6546536 SHEAR TIE BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 741SA 29277 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 32. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086093 1 20081111 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 4L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086110 1 20081107 A 3350 PL2230LH0 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 426WN 29830 FOUND EEPLS LIGHT INOP BETWEEN ROW 3 TO ROW 4. REMOVED AND REPLACED EEPLS PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086111 1 20081107 A 3350 81000 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 426WN 29830 FOUND EEPLS LIGHT LENS MISSING BETWEEN ROW 1 TO ROW 2. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086118 1 20081107 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 785SW 30602 DURING SCHEDULED 8Y CHECK, FOUND EMERGENCY EXIT LIGHT LENS COVER LOOSE AT AFT GALLEY. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086252 1 20081115 A 5754 114A50104 SKIN BOEING 737 7377H4 1384404 NM LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 748SW 29800 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 8 SLAT OUTER SKIN CRACKED AT FASTENER HOLE. REMOVED AND REPLACED SLAT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086253 1 20081116 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 901WN 32545 DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086258 1 20081117 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 480, BETWEEN STR 9R TO STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086098 1 20081106 A 3350 284A01216 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 435WN 32455 DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086260 1 20081117 A 5311 6546595 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 727A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086261 1 20081117 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 8R. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081119 EA 2008 11 19 ASOA200801507 1 20081114 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA CABIN DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 884AS 7513 CABIN DOOR WILL NOT CLOSE. 2 L 7 2 4F RT A21EA 20081119 NM 2008 11 19 SWAA086266 1 20081115 A 3320 101331 LIGHT BOEING 737 7373T5 1384608 NM CABIN INOPERATIVE A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 29 692SW 23062 FLT ATTENDANTS REPORTED ELECTRICAL SMOKE SMELL AT ROW 12 TO ROW 14. CEILING LIGHTS INOP IN SAME ROW. RELAMPED LIGHTS P ER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086117 1 20081107 A 3350 8210248801 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 785SW 30602 DURING SCHEDULED 8Y CHECK, FOUND EMERGENCY EXIT LIGHT LENS LOOSE AT FWD LAV. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086278 1 20081114 A 5512 65C25727 SKIN BOEING 737 7377H4 1384404 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER SKIN CRACKED AT BS 138. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086279 1 20081114 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 459WN 32497 DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED AT ROW 2. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081119 EA 2008 11 19 ASOA200801502 1 20081113 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 927EV 7844 FS 280 LBL 9 I/B STRINGER CLIP CRACKED. REMOVED INBOARD STRINGER CLIP IAW SRM 51-42-21. INSTALLED NEW SERVICEABLE STRI NGER CLIP IAW SRM 51-42-21. 2 L 7 2 4F RT A21EA 20081118 NM 2008 11 18 2008UALA06505 1 20081113 A 2421 729825M IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE FAULTY A UALA A UNSCHED LANDING W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 WP 29 598UA 28751 RIGHT IDG MSG AND LIGHT. RTFL. RAN ENGINES FOUND DC-A 23 FOR NR 1 AND 13 FOR NR 2. AFTER DISCONNECTING APU GEN, NR 2 TRIPPED OFF AND WOULD NOT RESET. TRIED SWAPPING GCU'S BUT GEN WOULD NOT COME ONLINE SWAPPING BACK GCU'S GEN NR 2 CAME O NLINE BUT TRIPPED BEFORE TRYING TO TRANSFER POWER. TRIED NEW GPCU, BUT GEN NR 2 AGAIN DID NOT COME ONLINE AND WOULD NOT RESET. REPLACED NR 2 IDG, OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081118 NM 2008 11 18 08FDEA04778 1 20081107 A 5320 STIFFENER DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 593FE 48551 EMPENNAGE, AFT FUSELAGE COMPARTMENT PRESSURE BULKHEAD AFT SURFACE VERTICAL STIFFENER AT STATION 2007, X=-15.250 FOUND CR ACKED AT UPPER CORNER AREA. 2 L 7 3 4F RT A22WE 20081118 NM 2008 11 18 2008UALA03126 1 20080601 A 5320 FITTING BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 907UA 25007 FOUND CRACKED INTERCOSTAL CLIP S-11L AFT OF STA 294.5, CRACK IN TEE ATTACHMENT ANGLE STR-11L BETWEEN 294.5 & 303.9 STA, CRACK IN CLIP FRAME TO STRINGER S-11 FWD OF STA 294.5, CRACKED INTERCOSTAL WEB S-12L BETWEEN STA 294.5 & 303.9. AND CRAC K IN INTERCOSTAL WEB S-16L BETWEEN STA.294.5 AND STA 303.9. MAJOR REPAIR ACCOMPLISHED. AREAS REPAIRED PER REO-L01 076 AND UA-EVA-71613, TO BE REINSPECTED WITHIN 6000C AND EVERY 6000C THEREAFTER. CURRENT PTC 30113. FIRST REINSPECT AT 361 13C. PER SB 737-53A1204 (AD 2005-20-03) 2 L 7 2 4F 4 F RT A16WE E21EU 20081118 NM 2008 11 18 2008UALA03127 1 20080601 A 5320 STRUCTURE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 907UA 25007 LT FS 294 HAS A 1 INCH CRACK AT STRINGER 11, JUST FWD OF WEB ATTACHMENT HOLES. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAI RED PER UA-EVA-71611 AND REO-L01080, HAVE RECEIVED FIRST STAGE APPROVAL ONLY. BOEING MUST ISSUE A NEW FORM 8100-9 ON OR BEFORE 27MAY09. THIS REPAIR IS APPROVED FOR 12 MONTHS ONLY. AIRCRAFT MUST BE REMOVED FROM SERVICE ON 27MAY09 UNLESS A NEW 8100-9 IS RECEIVED. 2 L 7 2 4F 4 F RT A16WE E21EU 20081118 NM 2008 11 18 2008UALA03129 1 20080601 A 5320 WEB BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 907UA 25007 INTERCOSTAL WEB CORROSION FOUND AT WEB BS 351.2 & BS 360 STR 11L,12L,14L AND 16L. MAJOR REPAIR ACCOMPLISHED. AREAS REP AIRED PER UA-EVA- 71614 AND REO-01077, TO BE REINSPECTED WITHIN 6000 CYCLES AND EVERY 6000 CYCLES THEREAFTER. CURRENT P TC 30113. FIRST REINSPECT AT 36113 CYCLES. PER SB737-53A1204 (AD 2005-20-03) 2 L 7 2 4F 4 F RT A16WE E21EU 20081118 EU 2008 11 18 08FDEA04901 1 20081117 A 3411 PITOT TUBE AIRBUS 310 A310203 3930313 EU OBSTRUCTED A FDEA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 CE 21 434FE 355 ABORTED TAKEOFF AT 60KIAS DUE TO NO F/O'S AIRSPEED INDICATION. CLEANED DEBRIS FROM F/O'S PITOT TUBE PROBE IAW 34-10-00. OPS CHECK GOOD IAW 34-12-00. 2 L 7 2 4F RT A35EU 20081118 SO 2008 11 18 SWIA200820365 1 20081112 A 3233 ACTUATOR EMB 120 EMB120ER 3260203 SO NLG BYPASSING A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 236SW 120312 FLT 5509 - LANDING GEAR VERY SLOW TO RETRACT. REPLACED NOSE GEAR ACTUATOR. 2 L 7 2 4T RT A31SO 20081118 EA 2008 11 18 SWIA200820339 1 20080801 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 668CA 10162 C-CHECK, FS 280 BEAM CORRODED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081118 NM 2008 11 18 2008UALA03139 1 20080531 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 318UA 23950 FUSELAGE SECTION 46 SKIN DENT AT AFT DOOR 2L. MAJOR REPAIR ACCOMPLISHED. REF EVA 71590 B, FUSELAGE SKIN AND STRINGER R EPAIR BETWEEN BS 996 AND BS 1016, S10L TO S16 HAS RECEIVED FIRST STAGE APPROVAL FOR STATIC STRENGTH ONLY, AND IS TIME LI MITED UNTIL 5-30-2009. 2 L 7 2 4F 4 F RT A16WE E21EU 20081118 WP 2008 11 18 08FDEA04647 1 20081031 A 5512 NLC6031504 SKIN DOUG MD10 MD1010F 3022112 WP HORIZONTAL STAB DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 390FE 46624 RIGHT HORIZONTAL STAB UPPER SURFACE HAS A DENT. CHECKED THE DEPTH OF THE DENT. FOUND TO BE 0.059 DEEP WITH NO CRACKS. DENT IS IN LIMITS PER SRM 51-80-01; PG 2; PARA 1; VOL II. ALODINED, PRIMED AND PAINTED PER SRM 51-21-01, PGS 21-24, VO L II AND SRM 51-21-02, PG 8, VOL II. 2 L 7 3 4F RT A22WE 20081118 EA 2008 11 18 SWIA200820348 1 20081106 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE INDICATION A SWIA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 07 413SW 7102 FLT 6607 - "SMOKE TOILET" CAUTION MESSAGE AND ALARM, NO SMOKE OR FIRE PRESENT. RESET SMOKE DETECTOR. 2 L 7 2 4F RT A21EA 20081118 NM 2008 11 18 08FDEA04754 1 20081105 A 5330 6554583205 SKIN BOEING 727 7272S2F 1384O81 NM FUSELAGE MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 216FE 22937 FOUND EXTERNAL FUSELAGE REPAIR LOCATED AT APPROX BS 1164-1178 STR 17R- STR 18R. REPAIR REQUIRES EVALUATION FOR MAJOR/MI NOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REMOVED OLD REPAIR REF SRM 51-30-2 PG 1-6. FABRICATED REPAIR DOUBLER REF SRM 53-30-2 FIG 3. TREATED AND PRIMED REF SRM 51-10-2 PG 1-6. INSTALLED REF SRM 53-30 -3 FIG 1. PAINTED TO MATCH REF MM 51-20-151-7 (CLASSIFIED AS A MAJOR REPAIR). 2 L 7 3 4F A3WE 20081118 EA 2008 11 18 TRAX200801241 1 20080929 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT DEFECTIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 BETA LIGHT PLACARDS ON LT/ RT EMER EXIT DOOR INTERIOR HANDLE COVERS FAILED INTENSITY TEST. (K) 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 TRAX200801264 1 20081002 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 RT FLOOR SEAT RAIL FROM FS 581.00 TO FS 683.00 CORRODED REMOVED AND REPLACED FLOOR SEAT RAIL FROM FS581 - FS 683 IAW MM 53-00-49. (K) 2 L 7 2 4F RT A21EA 20081118 EA 2008 11 18 TRAX200801238 1 20080927 A 5260 STEP CNDAIR CL600 CL6002C10 1390015 EA CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 710EV 10071 LOWER STEP CRACKED FWD SIDE. (K) 2 L 7 2 4F RT A21EA 20081119 NM 2008 11 19 2008UALA06493 1 20081112 A 3350 COVER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 663UA 27160 EMERGENCY LIGHT STRIP LOOSE AT 14B. SECURED EMERGENCY LIGHT PLASTIC COVER AT SEAT 14B. OPS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081119 NM 2008 11 19 SWAA086284 1 20081115 A 3350 PL22300L COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 FOUND EEPLS LIGHT COVER MISSING AT FWD ENTRY DOOR. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086066 1 20081109 A 5534 6546872 FITTING BOEING 737 7373H4 1384600 NM VERTICAL STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 20Y CHECK, FOUND VERTICAL STABILIZER LT OUTBOARD REAR LUG FITTING CORRODED. REPAIRED FITTING PER EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086075 1 20081105 A 3350 MS25237 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 310SW 22949 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081119 2008 11 19 SWAA086076 4 20081031 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 FOUND L2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086247 1 20081113 A 5330 6545774 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 695SW 23506 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D + 12, STR 23. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086116 1 20081109 A 3350 PL2230LH0 STRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 746SW 29798 FOUND EEPLS STRIP LOOSE BETWEEN ROW 9 TO ROW 10. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086276 1 20081114 A 3350 417N5212 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 441WN 29837 DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS LENS LOOSE. REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086277 1 20081115 A 3350 284A01216 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 443WN 29838 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081119 WP 2008 11 19 AALA200810008 1 20081008 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 AFT UPPER CORNER OF WINDOW PAN IS CRACKED AT STATION 1041 LEFT SIDE. INSTALLED DOUBLER PER AARD 53-10-00-25. 2 L 7 2 4F A6WE 20081119 WP 2008 11 19 AALA200810001 1 20081011 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70529 49921 CRACK IN CUSP AT STATION 223 RIGHT SIDE LIGHTING HOLE. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081119 WP 2008 11 19 AALA200810000 1 20081006 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7526A 49918 SMALL CRACK ON CANT FRAME 1510. REPAIR ACCOMPLISHED WITH A 3 INCH BY 9 INCH DOUBLER IAW ESO 80559 DATED 10/6/08. 2 L 7 2 4F A6WE 20081119 WP 2008 11 19 AALA200810011 1 20081009 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 RIGHT CUSP CORRODED AT STATION 826 TO 845. CUT OUT CORROSION AND INSTALLED CUSP REPAIR DOUBLER PER AARD 53-20-00-16/ 2 L 7 2 4F A6WE 20081119 NM 2008 11 19 AALA200802698 1 20081008 A 3350 SOCKET BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 643AA 24601 DFW EMERGENCY LIGHT AT AFT SEAT 16D INOPERATIVE. SECURED SOCKET IN SEAT HARNESS CONNECTOR FOR EMERGENCY LIGHT AT AFT S EAT 16D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081119 WP 2008 11 19 AALA200802701 1 20081008 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 593AA 53256 LGA - EXTERIOR EMERGENCY LIGHTS AT LEFT AND RIGHT OVERWING INOPERATIVE. RESEATED CONNECTOR ON CHARGER FOR LEFT AND RIGH T EXTERIOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081119 WP 2008 11 19 AALA200810144 1 20081028 A 5310 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 AFT CARGO DOOR BEAM WEB UPPER SURFACE CORRODED STATION 1155 TO 1212. REMOVED CORROSION, TREATED AND PRIMED. INSTALLED REPAIR DOUBLER PER SRM 51-70-04 51-10-3 51-30-5. 2 L 7 2 4F A6WE 20081119 WP 2008 11 19 AALA200810013 1 20081013 A 5310 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE OUT OF LIMITS A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 MID CARGO DOOR LAMB BEAM DAMAGE OUT OF LIMITS. INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3. 2 L 7 2 4F A6WE 20081119 WP 2008 11 19 AALA200802700 1 20081008 A 2560 STRAP DOUG DC9 DC983 3022083 WP FLASHLIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 593AA 53256 LGA - EMERGENCY FLASHLIGHT AT STRAP MISSING AT AFT GALLEY. REPLACED STRAP FOR EMERGENCY FLASHLIGHT AT AFT GALLEY. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081119 NM 2008 11 19 AALA200820006 1 20081010 A 5754 SKIN BOEING BOEING 757 757223 1384957 NM LE SLAT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 670AA A10297 25335 CORROSION AROUND FASTENER HEAD, 29 INCH FROM INBOARD END OF NR 1 SLAT 5 INCH FORWARD OF UPPER TRAILING EDGE OF LEADING E DGE SKIN. REMOVED DAMAGED SKIN AND INATALLED FLUSH DOUBLER REPAIR IN ACCORDANCE WITH SRM 57-43-01 2 L 7 2 4F RT A2NM 20081120 NM 2008 11 20 ASMF 20081101 1 20081117 A 5610 5893543149 WINDSHIELD BOEING 737 737* NM COCKPIT CRACKED W ASMF A UNSCHED LANDING O OTHER CL CLIMB 1 SW 23 851AM 15147 29363 AIRCRAFT RETURNED DUE TO THE LT WINDOW NR 1 CRACKED. MAINT REPLACED THE LT WINDSHIELD ASSY NR 1 AND WINDOW HEAT CONTROL UNIT IAW AMM 56-11-11 AND AMM 30-41-11, TESTED CORRECT. THE OVERWEIGHT INSPECTION WAS NOT NECESSARY DUE TO THE ACFT LAND ED WITH 52,961 KG AND THE MAXIMUM LANDING WEIGHT IS 58,059 KG. 2 L 7 2 4F RT A16WE 20081120 EA 2008 11 20 ASOA200801462 1 20081106 A 5310 BEAM CNDAIR CL600 CL6002B19 1900309 EA CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 7196 VERTICAL BEAM ON FRAME 559.0 AT LBL 9 O/B IS CRACKED FROM BOTTOM UP TO FIRST RIVET HOLE. 2 L 7 2 4F RT A21EA 20081120 NM 2008 11 20 08FDEA04866 1 20081112 A 5347 691570916 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 469FE 21581 CORROSION ON SEAT TRACK FLANGES AND ATTACH FASTENERS RBL 45 STA 1030 TO 1110. FOUND CORROSION OUT OF LIMITS, FABRICATED NEW SEAT TRACK USING BAC1520-792 PO# 9006020 DIMS 100" INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-10-5. 2 L 7 3 4F A3WE 20081120 NM 2008 11 20 DHLA2008745677 1 20081103 A 5730 SKIN BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 WING CENTER SECTION, AS ACCESSED THROUGH CABIN, UPPER SKIN CORRODED AT BS 823, BL 0 TO RBL 25. REPAIRED WING CENTER SEC TION SKIN DAMAGE AND SPANWISE BEAM BETWEEN RBL 6.5 TO RBL 25 PER EO COO-2-57-284-08 DATED 10/16/08. REFERENCE FAA FORM 8110-3 DATED 10/29/2008, AND ASTAR EVA B257-00113 FOR REPAIR APPROVAL. DOCUMENTED ON N/R 2-214. 2 L 7 3 4F A3WE 20081120 NM 2008 11 20 DHLA2008745678 1 20081103 A 5754 SKIN BOEING 727 727224 1384076 NM ZONE 600 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 966 20665 NR 5 L/E SLAT SKIN CRACKED AT TRACK, SLAT STA 90.25 ACCOMPLISHED REPAIR TO NR 5 SLAT SKIN PER EO COO-2-57-344-08 DATED 10/08/08. REFERENCE FAA FORM 8110-3 DATED 10/12/08 AND EVA B257-00136 FOR REPAIR APPROVAL. DOCUMENTED ON N/R 6-327 2 L 7 3 4F A3WE 20081120 NM 2008 11 20 DHLA2008745679 1 20081108 A 5322 SHEAR TIE BOEING 727 727224 1384076 NM ZONE 100 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 FRAME SHEAR TIE CRACKED IN NLG W/WELL TORQUE BOX AT BS 328, BETWEEN STR 26L AND 27L. REPAIRED FRAME SHEAR TIE PER SRM 5 3-10-4 FIG 15. DOCUMENTED ON N/R 1-683. 2 L 7 3 4F A3WE 20081007 EA 2008 10 7 MAS2008F00067 1 20080821 A 3350 BATTERY CNDAIR CL600 CL6002D24 1390016 EA CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 906FJ 15006 ASH FLT 2836 PHX-BUR. EMERGENCY LIGHTS WILL NOT STAY ILLUMINATED. MX CHARGED BATTERIES. 2 L 7 2 4F RT A21EA 20081003 NM 2008 10 3 C8G2008F00009 1 20080805 A 2797 CONNECTOR BOEING 727 727227 1384078 NM NR 8 SLAT DIRTY A C8GA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 29 308AS 22002 AFTER TAKEOFF, DURING CLIMB, OPERATION, THE NR 8 SLAT WOULD NOT RETRACT. POST FLIGHT INSP WAS PERFORMED AND THE NR 8 S LAT ACTUATOR CONNECTOR WAS CLEANED AND SYSTEM WAS OPERATIONAL CHECKED WITH NO DEFECTS. NO OTHER DEFECTS WERE NOTED. AC W AS RETURNED TO SERVICE. (K) 2 L 7 3 4F A3WE 20081003 NM 2008 10 3 2008UALA05687 1 20080911 A 5754 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 6 SLAT DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 567UA 26673 ON INBOUND RECEIVING INSPECTION, A TEAR WAS FOUND ON THE NR 6 SLAT, RT INBOARD IN THE UPPER INBOARD CORNER OF THE TRAILI ING EDGE WEDGE. THE TEAR GOES FROM THE TRAILING EDGE 3.3 INCHES INTO THE WEDGE. THE TEAR GOES COMPLETELY THROUGH THE W EDGE, BOTH FACES AND THE HONEYCOMB. REPLACED NR 6 SLAT. INSPECTED NR 6 SLAT FOR SAFETY AND SECURITY. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081003 NE 2008 10 3 2008UALA05688 2 20080912 A 7200 ENGINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 MALFUNCTIONED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 403UA 442 V11114 UPON ARRIVAL AT GATE NR 1 ENGINE WAS SMOKING HEAVILY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 CALA0800877 1 20080913 A 5321 146N5391110 FLOOR PANEL BOEING 757 757224 1384958 NM CARGO BAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 19136 29285 AFT CARGO FLOOR RT SIDE PANEL CORRODED FROM FS 1470 TO FS 1500. REMOVED AND REPLACED PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081003 NM 2008 10 3 UPS08653329 1 20080914 A 3220 UNKNOWN BOEING 767 76734AF 1385212 NM NLG NOISY A IPXA K NONE O OTHER CR CRUISE 1 SO 01 324UP 27750 INSPECTION TYPE:N/A 30 SECS AFTER GEAR RETRACTION THERE WAS A NOISE UNDER C/P SIMILAR TO A COMPRESSOR STALL WITH NO OTHE R INDICATIONS. DURING DESCENT FROM FL 390 PASSING FL 390 PASSING FL 250 SAME SOUND WAS HEARD THROTTLES AT IDLE. CREW R EQUESTED EMERGENCY EQUIPMENT BE STANDING BY PERFORMED DVI OF NOSE AREA PNEUMATIC DUCT WORK & ASSOCIATED AREAS, NO DEFECT S NOTED. PRESSURIZED A/C TO ALLOWABLE GROUND LIMITS IAW B767 MM 05-51-24-2. REPEATED SEVERAL TIMES. COULD NOT DUPLICA TE ON GROUND AT THIS TIME. OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A1NM 20081003 NM 2008 10 3 SWAA085044 1 20080912 A 3350 20131A BATTERY PACK BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 507SW 24184 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 2008UALA05686 1 20080910 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN MISSING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 776UA 26937 SEAT 2E MISSING FLOOR PROX EMERGENCY PATH MARKING LIGHT. DISCOVERED LIGHT MISSING. NEW LIGHT ASSY INSTALLED. OK FOR S ERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081003 NM 2008 10 3 2008UALA05689 1 20080912 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE CABIN EXPOSED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 673UA 29241 WIRES STICKING OUT AT SEAT 13B. FOUND INADEQUATE WIRING. REPLACED EEL LT ASSY, OPS CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081003 NM 2008 10 3 2008UALA05730 1 20080914 A 2421 729825G IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 546UA 25367 LEFT IDG DRIVE LIGHT ON AFTER TAKEOFF. FOUND DEFECTIVE IDG. REPLACED LEFT ENG IDG. IDG OPS AND LEAK CHECK GOOD. SAFE TIED LEFT GENERATOR DISCONNECT SWITCH GUARD. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081003 NE 2008 10 3 2008UALA05731 2 20080914 A 7520 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 655UA 25393 724465 NR 2 ENG, TURBINE CASE COOLING ACTUATOR IS LEAKING FUEL AT A RATE OF 30 DROPS PER MINUTE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081003 NM 2008 10 3 C8G2008F00011 1 20080708 A 2497 CONNECTOR BOEING 727 7272A1 138407F NM CSD LOOSE A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 287SC 21345 AFTER TAKEOFF DURING CLIMB OUT THE NR 1 GENERATOR EXPERIENCED A SPEED FAULT WITH THE NR 3 GENERATOR PREVIOUSLY DEFERRED. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION WAS PERFORMED. NR NR 1 CSD A S PEED SWITCH CONNECTOR WAS RESEAT, RECRACKED GENERATOR CONTROL PANEL AND RESEAT CURRENT BREAKER. OPERATED ENGINE AND PERF ORMED OPS CHECKS, CHECKED GOOD. O OTHER DEFECTS WERE NOTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F A3WE 20081003 EU 2008 10 3 ZJ62008F00000 1 20080905 A 3060 SMR6890 BOOT BAG JETSTM JETSTM3101 1500215 EU PROP BLADE MISSING E ZJ6A O OTHER O OTHER NR NOT REPORTED 1 EA 11 16EN 743 NR 1 ENGINE VIBRATION IN FLIGHT, DEICE BOOT MISSING. 2 L 7 2 4T RT A21EU 20081003 NM 2008 10 3 CALA0800931 1 20081001 A 5320 14T5107 FLOOR SUPPORT BOEING 767 767224 1385170 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76156 30435 CABIN FLOOR SUPPORT FOUND CORRODED AT BODY STATION 303 BETWEEN LBL 31- 41. CABIN FLOOR SUPPORT REPAIRED PER SRM 53-00-5 1, REPAIR 1, FIG 201. 2 L 7 2 4F RT A1NM 20081003 NM 2008 10 3 CALA0800932 1 20081001 A 5315 141T5146 STIFFENER BOEING 767 767224 1385170 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76156 30435 E&E COMPARTMENT LEFT STATION 246 CABIN FLOORBEAM LBL 40 VERTICAL STIFFENER FOUND CRACKED. E&E COMPARTMENT LEFT STATION 246 CABIN FLOORBEAM LBL 40 VERTICAL STIFFENER REPAIRED PER ECRA 5310-04844. 2 L 7 2 4F RT A1NM 20081003 NM 2008 10 3 CALA0800933 1 20081001 A 5315 141T5147 FLOORBEAM BOEING 767 767224 1385170 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76156 30435 E&E COMPARTMENT STATION 246 LBL 40 CABIN FLOOR MID CHORD FOUND CRACKED. E&E COMPARTMENT STATION 246 LBL 40 CABIN FLOOR MID CHORD REPAIRED PER SRM 53-10-51, REPAIR 2 FIG 201 AND ECRA 5310-04844. 2 L 7 2 4F RT A1NM 20081006 NM 2008 10 6 AALA200802014 1 20080802 A 3350 SHROUD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 631AA 24589 ORD EMERGENCY LIGHT SHROUD AT SEAT 5E DAMAGED. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED N ORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20081006 CE 2008 10 6 GLB2008F00025 1 20080902 A 5311 FRAME BEECH 1900 1900D 1154162 CE BS 164 S9R CRACKED A GLBA O OTHER O OTHER NR NOT REPORTED 1 NM 21 211GL UE211 DURING STRUCTURAL INSPECTION MAINT FOUND FRAME CRACKED AT STRINGER CUTOUT AT FS 164.4 STRINGER 9AR. LENGTH OF CRACK APPR OXIMATELY .5". MAINT REPAIRED FRAME CRACK AT STRINGER RELIEF HOLE IAW SRM 51-70 AT FS 164.4 REPAIR APPROXIMATELY 5 INCH BY 2.5 INCH. 2024-T3. RLL INSPECTION COMPLIED IAW TASKCARD 8.2.1. (K) 2 L 7 2 4T RT A24CE 20081006 CE 2008 10 6 GAJ2008F00000 1 20080825 A 2700 S17011 PULLEY CESSNA 210 T210M 2073451 CE FROZEN E GAJA K NONE O OTHER IN INSP/MAINT 1 NM 11 7067Z 12000 21062572 THE COPILOT RETRACTABLE STEP MALFUNCTIONED DUE TO PULLEYS FREEZING. FWD PULLEY IS HARD TO SEE ON AFT NOSE GEAR WELL AND IS IN A VERY DIRTY ENVIRONMENT. THE REAR PULLEY IS IMPOSSIBLE TO SEE. THE REAR PULLEY STOPPED ROTATING (FROZE) CAUSING S EVERE WEAR TO THE CABLE AND PULLEY. THE RETRACTABLE STEP WOULD NOT COME OUT. THE STEP WAS LUBED AND THE STEP STARTED WOR KING HOWEVER THE WEAR AND DAMAGE TO THE CABLE AND PULLEYS WAS ALREADY DONE. SUGGEST THAT THE RETRACTABLE STEP AND ACTUAT ING SYS BE PRESSURE WASHED AND LUBED EVERY 10000 HRS. THE AC THAT THIS RETRACTABLE STEP IS INSTALLED ON HAS OVER 12000 H RS TTAF, RESEARCH OF THE LOGBOOKS SHOWS NO MAINT OR PARTS REPLACEMENT SINCE THE AC WAS NEW. (K) 1 H 7 1 3O 3A21 20081006 2008 10 6 USAA920081610 4 20080830 A 2565 SLIDE AIRBUS A319 A319112 3930323 EU RIGHT DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 741UW 1269 LOGPAGE 4393997 FLT NR RON CLT EMERGENCY EQUIPMENT RT HAND OFFWING ESCAPE SLIDE RESERVOIR REQUIRES REPLACEMENT DUE TO OP S TEST OF ESCAPE SLIDE. PER DATA SHEET, SLIDE DEPLOYED BUT TOP OUTBOARD LIGHT DID NOT ILLUMINATE. REPLACED RESERVOIR W ITH SERVICEABLE UNIT. """SUPP"** WILL BE SUBMITTED UPON RECEIPT OF INFORMATION ON REMOVED ESCAPE SLIDE. 2 L 7 2 4F RT A28NM 20081006 WP 2008 10 6 U2R2008F00009 1 20080825 A 5330 SKIN DOUG DC8 DC871F 302199D WP FS 8 L21R CORRODED A U2RA O OTHER O OTHER NR NOT REPORTED 1 GL 23 872SJ 83402 46040 DURING C-CHECK INSP, FOUND FUSELAGE EXTERIOR FS 8.000, L-21R SKIN WITH BULGING AND CHERRY MAX RIVETS. (K) 2 L 7 4 4F RT 4A25 20081006 CE 2008 10 6 GLB2008F00018 1 20080828 A 6123 SWITCH BEECH 1900 1900D 1154162 CE AUTOFEATHER OUT OF ADJUST A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 21 881SK UE88 SUSPECTED AUTOFEATHER EVENT. DURING CRUISE, THE PILOTS REPORTED THAT THE LT AUTOFEATHER DISARMED IN FLIGHT AND NEVER REA RMED AT ANY POWER SETTING. MAIT ADJUSTED THE LT POWER LEVER SWITCH. OPS CHECK OF THE AUTOFEATHER SYS GOOD IAW MM 61-20- 00. (K) 2 L 7 2 4T RT A24CE 20081006 EA 2008 10 6 TRAX200801061 1 20080826 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 932EV 8016 JOB 8801621 OPERATION 196 LT FS 621 FLOOR SUPPORT ANGLE IS CRACKED, APPROX .25" LONG. THIS SDR WILL REMAIN OPEN PENDING MX DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. 2 L 7 2 4F RT A21EA 20081006 EA 2008 10 6 TRAX200801073 1 20080830 A 5210 DOOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 845AS 7324 F/A REPORTS MAIN CABIN DOOR DIFFICULT TO OPEN FROM INSIDE. C/W OPERATIONAL CK OF PASSENGER DOOR IAW CRJ 200 AMM 52-11-0 0 NO DEFECTS NOTED OK FOR SERVICE. 2 L 7 2 4F RT A21EA 20081006 SO 2008 10 6 C2XA08IA198 1 20080825 A 3610 40303920 O-RING EMB 145 EMB145EP 3260221 SO BLEED AIR SYS BLOWN A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14940 145033 JAN FLIGHT 3021. THE CREW REPORTED A BLEED 1 LEAK ON CLIMBOUT FROM BHM AT APPROXIMATELY 10,000 FEET. THE CREW SHUT DOW N THE NR 1 ENGINE AND DIVERTED TJAN WHERE IT LANDED WITHOUT INCIDENT. MX PLACED THE NR 1 BLEED SYSTEM ON MEL 36-11-05 C TL NR 153327 AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. THE ACFT RON`D AT IAH WHERE MX R&R THE O-RINGS IN THE AFT PAX COMPARTMENT NR 1 BLEED SYSTEM. OPS AND LEAK CHECK WITH NO DEFECTS, THE MEL WAS REMOVED AND THE ACFT WAS APPROVED F OR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20081006 SO 2008 10 6 C2XA08ON175 1 20080827 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 11551 2909 145411 FLT MX ONT WHILE PERFORMING PRELIMINARY INSPECTION ON ACFT 551 SCHEDULE 4A CHECK INSPECTOR FOUND EMERGENCY PROXIMITY LIG HT OUT BTW ROWS 8 AND 12. MX PERSONNEL R&R NR 3 EMERGENCY LIGHT BATTERY. OPS CHECK SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 20081006 SO 2008 10 6 C2XA08ON174 1 20080826 A 2611 SMOKE WARNING EMB 145 EMB145XR 3260214 SO LAVATORY MALFUNCTIONED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 27 12175 14500878 FLT 7786 LAX FLIGHT CREW REPORTED LAV SMOKE INDICATION AND PERFORMED AN AIR RETURN. MX PERSONNEL PERFORMED HIGH POWER R UNS AND COULD NOT DUPLICATE LAV SMOKE INDICATION MSG. OPS CHECK SATISFACTORY AND AIRCRAFT WAS RELEASED TO RETURN FOR SE RVICE. 2 L 7 2 4F RT 20081006 SO 2008 10 6 NTB2008F00000 2 20080808 A 7414 IMPULSE COUPLING PIPER PA28 PA28R201T 7102813 SO CONT O360 TSIO360F 17025 SO MAGNETO BROKEN E NTBA K NONE O OTHER IN INSP/MAINT 1 NM 05 5880V 14 D07HA271R 28R7703158 834910R IMPULSE COUPLING SPRING BROKEN. EVIDENCE OF PRE-EXISTING CRACK AND CORROSION. VERY LOW TIME IN SERVICE. MAG TO ENGINE TIMING LOST. BOTH MAGS EXPERIENCED THE SAME FAILURE ALMOST SIMULTANEOUSLY. (K) 1 L 7 1 3O 3 O 2A13 E9CE 20081006 EA 2008 10 6 REX2008F00045 1 20080822 A 2750 855D10011 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A REXA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 8631E 14788 7631 FLAP FAIL MESSAGE IN CRUISE. FLAP ELECTRONIC CONTROL UNIT (FECU) INTERROGATED FAULT CODES LOGGED 1. RT BPSU (BRAKE POS ITION SENSING UNIT) 2. FECU 3. WIRING RT BPSU. 12 1B AND 12 2B. R&R THE RT BPSU PER BOMBARDIER AMM OPS CHECK PERFORMED ALONG WITH A FUNCTIONAL CHECK FLIGHT NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 MAS2008F00069 1 20080821 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 75993 7372 ASH FLT 7135 CLE-IAD. CEILING EMERGENCY LIGHT NR 2 WAS INOP. MX RELAMPED. 2 L 7 2 4F RT A21EA 20081007 NM 2008 10 7 EIA2008038 1 20080828 A 5313 STRINGER BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE FUSELAGE CRACKED A EIAA O OTHER O OTHER NR NOT REPORTED 1 NM 19 485EV 20712 STATION 750 TO 760 STRINGER R-23 CRACKED. SPLICED AND REPAIRED PER 51-30-02. 2 L 7 4 4F 4 F RT A20WE E20EA 20081007 NM 2008 10 7 EIA2008033 1 20080828 A 5720 STRUCTURE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE RT WING CRACKED A EIAA O OTHER O OTHER NR NOT REPORTED 1 NM 19 485EV 20712 RT WING L/E DEVICE FAIRING AFT WEB ADJACENT UPPER CHORD AND LOWER CHORD CRACK AT 1 LES 1127. REPLACED PER SRM 57-20-03. 2 L 7 4 4F 4 F RT A20WE E20EA 20081007 NM 2008 10 7 EIA2008032 1 20080828 A 5411 FRAME BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE NR 4 PYLON CRACKED A EIAA O OTHER O OTHER NR NOT REPORTED 1 NM 19 485EV 20712 PYLON NR 4 AFT ENG MOUNT, RT (1/B) AFT FRAME, 1 HOLE CRACKED PER NDT REPORT. MFGR NEW FRAME PER DRW NR 65B90310 INSTALL ED PER 51-30-02 - 51-24-11 - BAL5119. 2 L 7 4 4F 4 F RT A20WE E20EA 20081007 NM 2008 10 7 EIA2008030 1 20080828 A 5720 STRUCTURE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE LT WING CRACKED A EIAA O OTHER O OTHER NR NOT REPORTED 1 NM 19 485EV 20712 LTW L/E DEVICE FAIRING AFT WEB ADJACENT LOWER CHORD AND UPPER CHORD. CRACK AT ILES 1127. REPAIRED PER 51-40-04 AND 57- 20-03 SRM 2 L 7 4 4F 4 F RT A20WE E20EA 20081007 SO 2008 10 7 RAIA00808020 1 20080822 A 3397 WIRE EMB 145 EMB145 3260210 SO CABIN DETACHED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 802HK 145066 PRE FLT NR 3505 RIC EMERGENCY LIGHT INOPERATIVE. MX REATTACHED A WIRE TO THE EMERGENCY LIGHT. SYSTEM OPS CHECKED GOOD AS PER AMM PROCEDURES. 2 L 7 2 4F RT T00011AT 20081007 SO 2008 10 7 RAIA00808027 1 20080826 A 7830 THRUST REVERSER EMB 145 EMB145LR 3260212 SO NR 2 MALFUNCTIONED A RAIA K NONE J WARNING INDICATION CR CRUISE 1 CE 03 816HK 145055 FLT NR 5558 BNA DURING CRUISE CREW RECEIVED A NR 2 T/R MESSAGE ON THE EICAS. MX DEFERRED THE NR 2 T/R SYSTEM AS PER THE MEL PROCEDURES. 2 L 7 2 4T RT T00011AT 20081007 SO 2008 10 7 RAIA00808026 1 20080826 A 2932 APTE2410005000 TRANSDUCER EMB 145 EMB145 3260210 SO HYDRAULIC SYSTEM LEAKING A RAIA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 03 801HK 145053 FLT NR 3505 PIT DURING FLIGHT CREW RECEIVED A HYDRAULIC SYSTEM NR 1 FAIL MESSAGE ON THE EICAS. MX INSPECTED AND FOUND T HE NR 1 HYDRAULIC PRESSURE TRANSDUCER LEAKING AND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP LEAKING PRESSURE LINE LEAKING. THE TRANSMITTER AND THE HOSE WERE R&R IN ACCORDANCE WITH AMM PROCEDURES. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 20081007 NE 2008 10 7 VNAA0808012 2 20080823 A 7260 6014T81G32 GEARBOX CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT ENGINE FAILED A VNAA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 GL 05 237PS 10488 7906 E950027 CREW REPORTED THE LT ENGINE FAILED ON CLIMBOUT. CREW ELECTED TO DIVERT TO IAD LANDING WITHOUT INCIDENT. MX INSPECTED E NGINE AND FOUND THE LT GEARBOX FAILED. GEARBOX WAS R&R. CHECKS WERE COMPLETED AND NO DEFECTS NOTED. ACFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20081007 EA 2008 10 7 VNAA0808013 1 20080823 A 2752 601R9310419 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE T/E FLAP FAILED A VNAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 05 249PS 10210 7926 CREW REPORTED A FLAPS FAIL AT 45 DEG. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MX INSPECTED ACFT AND R& R LT OUTBOARD ACTUATOR. CHECKS WERE MADE AND NO OTHER DEFECTS WERE NOTED. ACFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20081007 EA 2008 10 7 A6WA200840562 1 20080810 A 8010 SHAFT CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE STARTER SHEARED A A6WA O OTHER O OTHER UK UNKNOWN 1 GL 31 461AW 7870 STARTER ON ENGINE NR 1 WILL NOT STAY ENGAGED. NO ROTATION N1 OR N2. STARTER SHAFT SHEARED. R&R NR 1 ENG ATS PER MM 80 -11-01. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 20081007 EA 2008 10 7 A6WA200840563 1 20080811 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS MALFUNCTIONED A A6WA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 31 448AW 7814 FLAP FAIL ON TAXI OUT AFTER SHORT TURN. ATTEMPT TO RESET PER FIM DID NOT CLEAR MESSAGE. FLAPS AT ZERO. LT BPSU REPLAC ED IAW AMM 27-51-10-400-801. RIGGING CARRIED OUT AND OPS CHECK CARRIED OUT IAW 27-51-10-220-802. OPS CHECK GOOD. OK F OR SERVICE. 2 L 7 2 4F RT A21EA 20081007 SO 2008 10 7 RAIA00809002 1 20080903 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 811HK 145256 PRE FLT 5535 STL - EMERGENCY EXIT LIGHT INOP IN THE CABIN AT THE FORWARD CENTER LOCATION. MX RE-SECURED THE CONNECTOR T O THE LIGHT ASSEMBLY. OPS CHECKED GOOD IAW AMM PROCEDURES. 2 L 7 2 4T RT T00011AT 20081007 GL 2008 10 7 HEF2008F00000 2 20080903 A 7200 2544198 BEARING BELL 206 206L4 1182110 SW ALLSN 250C 250C30 03013 GL SPOOL FAILED B HEFR O OTHER O OTHER NR NOT REPORTED 1 WP 01 410RL 3056 52310 895274 UPPER BEARING, (PN 2525465) INSIDE OF SPOOL BEARING ASSY FAILED (CAME APART). LOWER SPOOL BEARING, (PN 2525468) IS STILL INTACT, BUT NO LONGER ROTATES FREELY. (K) 1 G 7 1 3U 3 U NC H2SW E1GL 20081007 NM 2008 10 7 USAA920081630 1 20080904 A 5311 6546525 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03C10753039/005 - FRAME CRACKED AT BS380, BETWEEN S8L & S9L. REPAIRED FRAME AT BS380, BETWEEN S8 L & S9L. IAW US AIRWAYS TYPICAL REPAIR NR 53-10-20E. 2 L 7 2 4F RT A16WE 20081007 NM 2008 10 7 USAA920081631 1 20080903 A 5311 6546548 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03C10753039/006 - FRAME CRACKED AT BS747, BETWEEN S7R & S8R. REPAIRED FRAME AT BS747, BETWEEN S7 R & S8R IAW US AIRWAYS TYPICAL REPAIR NR 53-10-20E. 2 L 7 2 4F RT A16WE 20081007 NM 2008 10 7 USAA920081632 1 20080812 A 5315 65498852 FLOORBEAM BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN C19 MAJOR REPAIR NR 6124249 - EXFOLIATION CORROSION ON TRANSVERSE BEAM AT BS986.5, WL208, RBL16. REPAIRED TRANSVERS E BEAM AT BS986.5, WL208, RBL16 IAW US AIRWAYS EA NR 130100. 2 L 7 2 4F RT A16WE 20081120 NM 2008 11 20 QXEA2008111401188 1 20081113 A 3230 464161 SPRING BOMBDR DHC8 DHC8402 1390042 NM ZONE 700 BROKEN A QXEA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 19 404QX 4046 MSO - OVERCENTER GEAR SPRING FOUND BROKEN ON PRE-FLIGHT ON RIGHT SIDE LANDING GEAR. REMOVED OUTBOARD STABILIZER-BRACE L OCK, SPRING ASSY REF Q400 AMM TASK NR 32-11-16-000-802. REMOVED AND REPLACED STABILIZER, BRACE LOCK, SPRING PIN RE-INST ALLED OUTBOARD STABILIZER-BRACE LOCK-SPRING ASSY AND INSTALLED NEW INBOARD STABILIZER-BRACE LOCK-SPRING ASSY REF Q400 AM M TASK NR 32-11-16-400-802 ON RT MLG. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081120 WP 2008 11 20 IXXA08SMN175S 1 20080419 A 5753 SKIN DOUG DC8 DC871F 302199D WP ZONE 600 MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD FLAP TRAILING EDGE LOWER SKIN IMPROPER REPAIR AT STATION XF 370. 000 - 404.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, AND DOUBL ER. BONDED PARTS AS NEEDED. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PART S IAW SRM 57-7-1 FIGURE 4 TR 57-94 DATED 10-01-02, SRM 57-1-0 PAGE 1, SRM 51-1-21, SRM 57-7-1 FIGURE 4 TR 57-94 ITEM U A ND Q, SRM 51-1-9 TR 51-1-42, SRM 51-1-9A TR 51-1-41, SRM 51-1-8B, AND SRM 51-1-11. 2 L 7 4 4F RT 4A25 20081120 EA 2008 11 20 SWIA200820375 1 20080725 A 5514 STIFFENER CNDAIR CL600 CL6002C10 1390015 EA BULKHEAD CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 776SK 10241 C-CHECK, INBOARD HORIZONTAL BULKHEAD ANGLE STIFFENERS CRACKED IN RADIUS WL111.5 ON LEFT SIDE OF FS 280 BULKHEAD. REPAIR ED PER REO. 2 L 7 2 4F RT A21EA 20081120 NM 2008 11 20 08FDEA04919 1 20081119 A 5311 6947200I FRAME SPLICE BOEING 727 7272D4 138407U NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 AFT CARGO PIT STATION 1030 FRAME SPLICE AT APPROX STRINGER 24L IS DAMAGED. REPLACED FRAME SPLICE REF SRM 51-30-02 AND D RAWING 69-47200. THIS IS CLASSIFIED AS A MAJOR REPAIR 2 L 7 3 4F A3WE 20081120 NM 2008 11 20 08FDEA04910 1 20081118 A 5311 DOUBLER BOEING 757 75723A 1384967 NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 LT FUSELAGE FRAME RE-INFORCING ANGLE (DOUBLER) HAS A CRACK BS-700, LBL 65 WL-200. REMOVED FRAME RE-INFORCING ANGLE/DOUB LER IAW SRM 51-40-02, RECEIVED NEW ANGLE/DOUBLER AND INSTALLED IAW SRM 51-40-02 AND DWG NR 143N1014 MAJOR REPAIR. NO FO LLOW-UP INSPECTION REQUIRED. 2 L 7 2 4F RT A2NM 20081120 NM 2008 11 20 QXEA2008111401180 1 20081109 A 3230 464161 SPRING BOMBDR DHC8 DHC8402 1390042 NM ZONE 700 BROKEN A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 19 406QX 4048 RNO - SPRING IN RIGHT MAIN WHEEL WELL BROKEN. REMOVED AND REPLACED THE INBD STABILIZER-BRACE LOCK SPRING ON THE NR 2 GE AR IAW AMM TASKS 32-11-16-000/400-802. ACFT IS OK FOR SERVICE. 2 H 7 2 4T RT A13NM 20081120 NM 2008 11 20 08FDEA04911 1 20081118 A 5311 651634112 FRAME BOEING 727 7272D4 138407U NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 AFT CARGO PIT STATION 1010 FUSELAGE FRAME DAMAGED AT STRINGER 26L. REPAIRED FRAME REF SRM 51-40-03 FIG1 AND FABRICATED CHANNEL ANGLE REF DWG 65-84827-8 SRM 51-30-02 PG 1-5 2 L 7 3 4F A3WE 20081120 EA 2008 11 20 QXEA2008111401181 1 20081109 A 5270 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA FALSE ACTIVATION A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 19 603QX 10011 SFO - JUST AT THRUST APPLICATION FOR TAKEOFF PAX DR OUTER HANDLE CAUTION MESSAGE. ABORTED TAKEOFF AND RETURNED TO THE G ATE. INSPECTED PASSENGER DOOR FOR ANY OBVIOUS DEFECTS, NO DEFECTS NOTED. COMPLIED WITH OPS CHECK PASSENGER DOOR TASK 5 2-11-00-710-801-A02. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 20081120 NM 2008 11 20 QXEA2008111401182 1 20081109 A 5610 80260008 WINDSHIELD BOMBDR DHC8 DHC8402 1390042 NM COCKPIT FAILED A QXEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 19 410QX 489 4053 SMF - ON FLIGHT 2420 AT FL 250 IN CRUISE, THE FIRST OFFICER'S FRONT WINDOW FAILED. DIVERTED TO SMF AND ACCOMPLISHED A U NEVENTFUL LANDING. REMOVED AND REPLACED FO'S FRONT WINDSHIELD IAW MM TASK 56-10-01-000-801 AND 56-10-01-400-801. ALSO, REPLACED FOS ANTI-ICE CONTROLLER IAW MM TASK 30-41-01-000-801 AND 30-41-01-400-801. OPS CHECK GOOD. RETURNED TO SERVI CE. 2 H 7 2 4T RT A13NM 20081120 NM 2008 11 20 QXEA2008111401183 1 20081111 A 3397 CIRCUIT BREAKER BOMBDR DHC8 DHC8402 1390042 NM TRIPPED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 19 416QX 4083 SEA - AFT FLIGHT ATTENDANT GALLEY WORK LIGHT CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER IAW GPM 9.2.4. OPERATED WOR K LIGHT SEVERAL TIMES. C/B REMAINED CLOSED. OPS CHECK GOOD. NO FURTHER DEFECTS. RETURNED TO SERVICE. NO PARTS REPLA CED. 2 H 7 2 4T RT A13NM 20081120 NM 2008 11 20 DHLA2008745690 1 20081114 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 100 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 FUSELAGE FRAME AT BS 188, OTBD CHORD CRACKED AT WL 208 AND LBL 36. REMOVED, FABRICATED, AND INSTALLED FRAME OTBD CHORD AND WEB SECTION PER SRM 51-10-1, 51-20-1, AND 51-30-2. DOCUMENTED ON N/R 2-387. 2 L 7 3 4F A3WE 20081120 NM 2008 11 20 08FDEA04920 1 20081119 A 5330 65545803 SKIN BOEING 727 7272S2F 1384O81 NM ZONE 100 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 LOWER RIGHT EXTERIOR FUSELAGE SKIN IS CHAFED AT AFT CARGO PIT DOOR CUTOUT FWD LWR CORNER STA 950E, STR 26-R. REPAIRED F WD LOWER CORNER OF FUSELAGE SKIN AT AFT CAGO DOOR CUT OUT REF EA 7-5330-123818. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081120 NM 2008 11 20 08FDEA04921 1 20081119 A 5347 SEAT TRACK BOEING 727 7272S2F 1384O81 NM BS 1176-1183 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 MAIN DECK SEAT TRACK AT LBL 24 BS 1176 TO 1183 IS CORRODED. 2 L 7 3 4F A3WE 20081120 WP 2008 11 20 IXXA08SMN159S 1 20080418 A 5730 SKIN DOUG DC8 DC871F 302199D WP ZONE 500 MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD FLAP LOWER SKIN IMPROPER REPAIR AT STATION XF 375.000 - STATION XF 404.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, DOUBLER. BO NDED PARTS AS NEEDED. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 57-7-1 FIGURE 4 TR 57-94 DATED 10-01-2002, SRM 57-1-0 PAGE 1, SRM 51-1-21, SRM 57-7-1 FIGURE 4 TR 57-94 ITEM "U" AN D "Q", SRM 51-1-9 TR 51-142, SRM 51-1-9A TR 51-1-41, SRM 51-1-8B, AND SRM 51-1-11. 2 L 7 4 4F RT 4A25 20081120 NM 2008 11 20 DHLA2008745686 1 20081112 A 5743 FITTING BOEING 727 727224 1384076 NM ZONE 600 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 MODIFICATION OF LMLG TRUNNION SUPPORT BEAM OTBD FITTING, ON REAR SPAR, REQUIRED IN CONJUNCTION WITH FITTING BORE RE-WORK . ACCOMPLISHED MODIFICATION TO FITTING IAW SB 727-57-0153 REV 4 SECTION 3, PART II, DATED 9/10/92. DOCUMENTED ON COOPE SA N/R 1-686. 2 L 7 3 4F A3WE 20081120 NM 2008 11 20 DHLA2008745687 1 20081106 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 CABIN FLOORBEAM CORRODED, BS 1130, BETWEEN RBL 34 AND LBL 50, ON UPPER AND LOWER CHORDS. ACCOMPLISHED FLOORBEAM REPAIR TO UPPER CHORD FROM LBL 5.7 TO LBL 54.5, AND TO LOWER CHORD FROM RBL 67 TO LBL 67 DUE TO CORROSION AND POST ACCESS CRACK S DISCOVERED, IAW EO COO-2-53-269-08 DATED 10/13/2008. REFERENCE FAA FORM 8110-3 DATED 10/29/2008 AND EVA B253-00115 FO R REPAIR APPROVAL. DOCUMENTED ON N/R 2-155. 2 L 7 3 4F A3WE 20081007 NM 2008 10 7 USAA920081620 1 20080819 A 5210 652399711 LINK BOEING 737 7373G7 1384595 NM AFT ENTRY DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 SAL C17 MAJOR REPAIR NR 6090106 MOUNTED BRACKET OF SNUBBER CRACKED ON AFT ENTRY DOOR. REPLACED LINK ASSEMBLY FOR LOWER HINGE MOUNTED SNUBBER AT AFT ENTRY DOOR IAW B737 AMM 52-13-41. 2 L 7 2 4F RT A16WE 20081007 NM 2008 10 7 USAABB08146 1 20080903 A 3233 273N20071 ACTUATOR BOEING 757 7572S7 1384962 NM LT MLG MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 904AW 82076 23566 PHL FLT 798 ENROUTE PHL TO AMS. THE STANDBY ATTITUDE INDICATOR FAILED ABOUT 45 MINUTES AFTER DEPARTURE. THE DECISION W AS MADE TO RETURN TO PHL. THE FLIGHT RETURNED WITHOUT FURTHER INCIDENT. MX REPLACED THE LT MAIN GEAR UP-LOCK ACTUATOR. OPS CHECK OK. 2 L 7 2 4F RT A2NM 20081007 NM 2008 10 7 USAABB08147 1 20080903 A 3350 036000570010 FUSE BOEING 757 7572S7 1384962 NM BATTERY PACK BLOWN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 906AW 23568 PHX THE LT HAND SEATS, ROWS 27 THROUGH 35, SEAT MOUNTED EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX REPLACED FUSE NR 1 IN BATTERY PACK SUPPLY. OPS CHECKS OK. 2 L 7 2 4F RT A2NM 20081007 NM 2008 10 7 USAA920081647 1 20080825 A 5340 69353501 STRINGER CLIP BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN C18 MAJOR REPAIR NR 6124317 STRINGER TIE CRACKED AT BS380, S15L. REPLACED STRINGER TIE AT BS380, S15L IAW B737 SRM 51-40-05-OG. 2 L 7 2 4F RT A16WE 20081007 NM 2008 10 7 USAA920081646 1 20080906 A 5753 6546435278MC FLAP BOEING 737 7374B7 1384702 NM RT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03C40727023/010 & NR 5030682. RT OTBD AFT FLAP DELAMINATED UPPER & LOWER SURFACE OF INBD END CAP . REPLACED RT OTBD AFT FLAP IAW B737 SRM 51-70-10. 2 L 7 2 4F RT A16WE 20081007 NM 2008 10 7 USAA920081641 1 20080902 A 5315 6545834 STRAP BOEING 737 7374B7 1384702 NM FLOORBEAM CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03C20553006/001. STRAP CRACKED ON LOWER PORTION OF FLOORBEAM AT BS312. BLO. REPLACED STRAP ON LO WER PORTION OF FLOORBEAM AT BS312, BLO IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081007 NM 2008 10 7 SCN2008F00000 1 20080802 A 3246 FUSIBLE PLUG BOEING 737 7378BK 13844FG NM WHEEL BLOWN A SCNA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 15 811SY B7280 29660 DURING TAXI-IN, CREW REPORTED LT OB MAIN WHEEL ASSY/ BRACE DRAGGING. MAINT DISCOVERED NR 1 WHEEL ASSY FUSE PLUG BLOWN. R EMOVED AND REPLACED NR 1 WHEEL/TIRE ASSY AND NR 1 BRAKE ASSY. (K) 2 L 7 2 4F RT A16WE 20081007 2008 10 7 C8G2008F00010 4 20080722 A 3442 20675680501 ANTENNA BOEING 727 727225 1384077 NM WX RADAR SYSTEM INOPERATIVE A C8GA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 29 808EA 22439 FLT 1204, AFTER TAKEOFF, THE RADAR WAS SPOOKING AND WOULD NOT PAINT KNOWN BAD WEATHER . THE AIRCRAFT RETURNED, WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED THE RADAR ANTENNA AT FAULT. REMOVED AND REPLACED RADAR ANTENNA PERFO RMED OPERATIONAL CHECKS GOOD. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F A3WE 20081007 NM 2008 10 7 C8G2008F00012 1 20080717 A 2611 77401 SMOKE DETECTOR BOEING 727 727225 1384077 NM CARGO BAY INOPERATIVE A C8GA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 29 808EA 22439 DURING CLIMB OUT OPERATION, THE MAIN DECK FIRE WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO DEPARTURE WHERE IT LA NDED WITHOUT INCIDENT. POST FLIGHT INSPECTION REVEALED THAT THE LT WARNING LIGHT ILLUMINATED STEADY. VERIFIED THAT NO SM OKE OR FIRE WAS PRESENT. LIGHT EXTINGUISHED AFTER RESEATING THE NR 8 SMOKE DETECTOR. REMOVED AND REPLACED THE NR 8 SMOKE DETECTOR AS PRECAUTION REMOVED AND REPLACED THE NR2, NR 4, NR 6, NR 10, NR 12 ON THE LT SIDE AND NR 9 ON THE RT. ALL OP ERATIONAL CHECKS GOOD. NO OTHER DEFECTS WERE NOTED AIRCRAFT WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F A3WE 20081007 EA 2008 10 7 SIMA200824605 2 20080831 A 7200 AE30007A13 ENGINE EMB 135 EMB135LR 3260305 SO RROYCE AE3007 AE3007A13 54166 EA LEFT MALFUNCTIONED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 721HS 145283 CAE311907 ON FLIGHT 4782 CREW REPORTED DURING TAXIING THAT THEY NOTED A STRONG ODOR OF BURN-ENGINE OIL IN COCKPIT AND CABIN. ACFT REMOVED FROM SERVICE. ACFT PULLS TO THE LT WHILE TAXIING WITH BOTH ENGINES RUNNING. R&R LT ENGINE. IAW EMB WORK CARD NR 71-000-00. OPS CHECKED GOOD AND LEAK CHECK GOOD. ACFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081007 EA 2008 10 7 TRAX200801050 1 20080823 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 846AS 7328 RT INBD FLOOR. SHORT SEAT TRACK AT 559.96 CORRODED (RESOLVED ON W/O 96197 TASKCARD N/R 00025) JOB COMPLETE ITEM 1. R&R R T INBD SHORT SEAT TRACK FROM FS559.96. PER CRJ200 SRM 51-41-00 KR17389 JOB COMPLETED 2 L 7 2 4F RT A21EA 20081007 SO 2008 10 7 C2X2008F00038 1 20080907 A 3350 2013BR BATTERY PACK EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHTS DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16151 145758 FWD EMERGENCY LIGHT INOPERATIVE. AND REPLACED NR 1 & NR 2 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04. OPS CHECK GOOD. NOTE : AC HAS BEEN IN C-CHECK SINCE 8/26. (K) 2 L 7 2 4F RT 20081007 SO 2008 10 7 C2X2008F00039 1 20080907 A 5510 STRUCTURE EMB 145 EMB145LR 3260212 SO RT HORZ STAB ERODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18982 145223 RT HORZ STAB L/E ERODED. POLISHED L/E AND REIDENTIFIED L/E IAW EC 5530-01116. AC STILL IN C-CHECK. (K) 2 L 7 2 4T RT T00011AT 20081007 SO 2008 10 7 C2X2008F00041 1 20080904 A 3350 602043 LIGHT EMB 145 EMB145LR 3260212 SO CABIN BURNED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 14923 19622 145318 AC WAS IN FOR A SERVICE/ ROUTINE CHECK AND THE LOWER SERVICE DOOR EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-50-09. OPS CHECK GOOD AND WAS RELEASED TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081007 SO 2008 10 7 C2X2008F00042 1 20080830 A 3350 7287580501 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13956 145078 DURING PREFLIGHT INSPECTION, THE CREW REPORTED (2) EMERGENCY LIGHT STRIPS TO BE INOPERATIVE. MAINT REMOVED AND REPLACED THE AFFECTED LIGHT STRIPS, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AC WAS APPROVED FOR RETURN TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081007 WP 2008 10 7 NWAA084129866 1 20080830 A 3397 PIN DOUG DC9 DC951 3022051 WP CABIN PULLED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 775NC 47785 DURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 9-13 OF THE CABIN WERE INOPERATIVE. INVESTIGATIO N REVEALED THAT A PIN HAD BEEN PULLED FROM THE WALL DISCONNECT PLUG. MX REPAIRED IT BY RE-INSERTING THE PIN. ALL CHECK S WERE GOOD. 2 L 7 2 4F RT A6WE 20081119 NM 2008 11 19 KCSA081540 1 20081022 A 3350 SIGN BOEING 747 747209B 138489B NM EMERGENCY LIGHT INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 715CK 22447 UPPER DECK EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. 2 L 7 4 4F RT A20WE 20081119 NM 2008 11 19 2008UALA06498 1 20081110 A 3510 802642 INDICATOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CREW O2 FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 912UA 25290 CREW OXYGEN PRESSURE INDICATOR INOP. CREW COMMENTS: FLUCTUATING 0 TO 1600. CONFIRMED PRESSURE AT BOTTLES OKAY. REPL ACED COCKPIT CREW OXYGEN INDICATOR, READS NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20081119 NM 2008 11 19 2008UALA06501 1 20081112 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 666UA 29238 EMERGENCY ESCAPE LIGHTING LOOSE IN FLOOR AT SEAT 3B. LIGHT FOUND UNSECURE. REPLACED THE EEL LIGHT AT SEAT 3B AS REQUIR ED. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081119 NM 2008 11 19 CALA0801070 1 20081111 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 16648 28909 BODY STATION 867 FRAME CRACKED AT AIR CONDITIONING (AC) RAIL BRACKET BETWEEN STR 8L AND STR 9L. REPAIRED BODY STATION 8 67 AT AC RAIL BRACKET BETWEEN STR 8L AND STR 9L PER CO EA5310-04498. 2 L 7 2 4F RT A16WE 20081119 2008 11 19 SWAA086077 4 20081031 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 357SW 26594 FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086081 1 20081104 A 3350 101331 LENS BOEING 737 7373L9 1384470 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 658SW 23332 FOUND LT OVERWING EXIT LIGHT LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086082 1 20081105 A 5313 6551698 STRINGER SPLICE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 360, STR 28L. REMOVED AND REPLACED SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086267 1 20081117 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 20L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 AALA200802708 1 20081009 A 2710 2828001011 ACTUATOR BOEING 767 767323 1385205 NM AILERON FAILED A AALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SW 21 350AN 33089 JFK INFLIGHT ORD TO BRU - BOTH AILERON FLOATING IN FLIGHT. RIGHT INBOARD AILERON WOULD NOT GO BELOW NEUTRAL. LEFT INBO ARD AILERON OVER COMPENSATING FOR THE RIGHT SIDE. DIVERTED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED LEFT AND RIGHT INBOARD AND OUTBOARD ACTUATORS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081119 WP 2008 11 19 AALA200810003 1 20081011 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70529 49921 CRACK IN CUSP AT STATION 223 RIGHT SIDE LIGHTING HOLE. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081119 WP 2008 11 19 AALA200810137 1 20081026 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 NR 1 SEAT TRACK CORROSION AT STATION 1234 - 1238. INSTALLED NEW SEAT TRACK FROM STATION 1174 - 1309 AT NR 1 SEAT TRACK. 2 L 7 2 4F A6WE 20081119 NM 2008 11 19 AALA200820007 1 20081010 A 5754 SKIN BOEING BOEING 757 757223 1384957 NM LE SLAT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 670AA A10297 25335 NUMEROUS PREVIOUS BLENDOUTS ON NR 1 SLAT IN AREA 30 INCH FROM OUTBOARD END OF SLAT. REPAIRED DAMAGED SKIN IAW SRM 57-43 -01. 2 L 7 2 4F RT A2NM 20081120 NM 2008 11 20 DHLA200800127 1 20081115 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN MALFUNCTIONED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 752DH 22466 L1 DOOR EMERGENCY EXIT LIGHT REMAINS ON WHEN SWITCH IS IN THE OFF POSITION. 2 L 7 3 4F A3WE 20081120 SO 2008 11 20 CHQA200800221 1 20081111 A 7500 7276045 FILTER ELEMENT EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL BLEED SYSTEM 1 CLOGGED A CHQA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 11 257JQ 145812 CAE311677 FLIGHT 3016, IND TO LGA - THE FLIGHT CREW RECEIVED A BLEED 1 OVERTEMP MESSAGE DURING CLIMB WHILE IN ICING CONDITIONS WIT H THE ANTI-ICE SYSTEM ON. THE CREW FOLLOWED THE APPROPRIATE CHECKLISTS AND DIVERTED TO CMH WHERE IT LANDED WITHOUT INCI DENT. MAINTENANCE TROUBLESHOT THE FAULT PER FIM TASK 36-11-00-810-803A WHICH LED TO THE REPLACEMENT OF THE FAN AIR VALV E FILTER. AFTER REPLACEMENT, THE SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081120 WP 2008 11 20 IXXA08SMN168S 1 20080419 A 5340 FITTING DOUG DC8 DC871F 302199D WP ZONE 200 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT CUSP EXTRUSION UPPER SURFACE FORWARD FITTING CRACKED AT STATION 742.250 LO NGERON 19 LEFT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 20081120 WP 2008 11 20 IXXA08SMN161S 1 20080419 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN HAS CORROSION AT STATION FS 505.000 LONGERON 33 RIGHT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECT ION. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, FILLERS. CLEANED, TREATED AND PRIMED AR EA AND REPAIR PARTS, SRM 51-1-8B. ORIGINALS DOCUMENTS ENTERED ON N/R NR100296 IAW FAA FORM 8100-9 DATED 05-22-08, AD 20 05-18-0-7, S/B DC8-53-078, DRAWING SR08530019 AND 5750776, MESSAGE 1-821382564-7 DATED 05-09-08, ND 1-842846685-2 DATED 05-22-08, SRM 51-1-8 PAGES 17-18, SRM 53-2-0 PAGE 2P, SRM 51-3-0, 51-1-21, 51-1-20D, REPAIR SKETCH 1-821382564, ED-SEMAN 2 L 7 4 4F RT 4A25 20081007 CE 2008 10 7 DXT2008F00004 1 20080904 A 4920 APU CESSNA 560 560XL 2076702 CE ODOR E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 652QS 5605152 DURING THE TAXI WE STARTED THE APU, ONCE THE APU BLEED WAS TURNED ON SMELLED A SLIGHT OILY SCENT. (K) 2 L 7 2 4F RT A22CE 20081007 WP 2008 10 7 NWAA084139884 1 20080901 A 3350 FUSE DOUG DC9 DC951 3022051 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 677MC 47756 DURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 14-18 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE ASSOCIATED FUSE. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A6WE 20081007 NM 2008 10 7 HALA0800762 1 20080905 A 5340 STRINGER CLIP BOEING 767 767332 1382001 NM FUSELAGE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 598HA 23278 EMPENNAGE STR 3 RT HAD TIE CLIPS AT STA 1654.5 AND STA 1678 CRACKED. 2 L 7 2 4F RT A1NM 20081007 NM 2008 10 7 QXEA200800420 1 20080418 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK. SURFACE CORROSION ON SEAT TRACK NR 7 BETWEEN STA X220 AND X226. REMOVED NR 7 SEAT TRACK IAW -8 200 SRM 5 1-40-11. DRILLED UP AND INSTALLED NEW TRACK IAW -8 200 SRM 51-40-00, 51-40-11 AND RD8-53-1102. 2 H 7 2 4T RT A13NM 20081007 NM 2008 10 7 QXEA200800421 1 20080418 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK. CORROSION ON SEAT TRACK NR 4 CAMLOCK RECEP. STA X222. REMOVED NR 4 SEAT TRACK IAW -8 200 SRM 51-40-11. DRILLED UP AND INSTALLED NEW TRACK IAW -8 200 SRM 51-40-00, 51-40-11 AND RD8-53-1102. 2 H 7 2 4T RT A13NM 20081007 EA 2008 10 7 TRAX200801039 1 20080821 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 970EV 7527 JOB 8752725 OPERATION 63 RH FS 559 BULKHEAD WEB HAS AN INDICATION NOTED AT O/B RBL 9, WL 58.7 3 IN LENGTH 50% FULL SCREE N HEIGHT FAILED NDT INSPECTION . REPAIRED FS 559 FROM LBL 18 TO LBL 9 AND RBL 18 TO RBL 9. ALSO CAP ANGLES ON LH/RH SI DE IAW REO 601R-53-41-260 AND GENERIC REO 601R-53-41-260. C DEVIATION. C/W EC/TC REO 601R-53-41-771 IAW BOMBARDIER RE O 601R-53-41-771. C/W REO 601R-53-41-260 ASA EC/TC REO 601R-53-41-260. ASA RII C/W 5300043. 2 L 7 2 4F RT A21EA 20081008 NM 2008 10 8 QXEA200800440 1 20080418 A 3213 STRUT DHAV DHC8 DHC8202 2809007 NM RT MLG STRUT CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK RT MLG SHOCK STRUT HAS CHAFE ON FWD SURFACE AT STRUT FAIRING UPPER ATTACH HOLE. POLISHED CHAFFED AREA IAW -8/200 MESSIER/DOWTY CMM 32-10-01 PG 6015 PARA 6A4. HFEC INSP. IAW -8/200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. PERFOR MED FPI IAW -8/200 VENDOR CMM 32-10-01 PG 6009 PARA 5A3 AND HORIZON NDTM CHP 8 NO CRACKS NOTED. PEENED IAW -8/200 CMM 3 2-10-01 STEP 6A2 AND FIG 601. ALODINED IAW MESSIER/DOWTY CMM 32-10-01 PG 6009 PARA 5B2A PRIMED PAINTED IAW 2 H 7 2 4T RT A13NM 20081008 NM 2008 10 8 QXEA200800442 1 20080418 A 3213 STRUT DHAV DHC8 DHC8202 2809007 NM RT MLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK RT MLG SHOCK STRUT HAS CHAFE AT LOWER O/B SURFACE WHERE O/B WOW HARNESS CONDUIT HAS CONTACTED. POLISHED CH AFFED AREA IAW -8/200 MESSIER/DOWTY CMM 32-10-01 PG 6015 PARA 6A4. HFEC INSP. IAW -8/200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. PERFORMED FPI IAW -8/200 VENDOR CMM 32-10-01 PG 6009 PARA 5A3 AND HORIZON NDTM CHP 8 NO CRACKS NOTED. PEENED IA W -8/200 CMM 32-10-01 STEP 6A2 AND FIG 601. ALODINED IAW MESSIER/DOWTY CMM 32-10-01 PG 6009 PARA 5B2A. 2 H 7 2 4T RT A13NM 20081008 NM 2008 10 8 AALA200802054 1 20080809 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW EMERGENCY LIGHT AT SEAT 25C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 2008 10 8 J7E2008F00001 4 20080917 A 3460 CDU LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE731* 01518 WP FMS FAILED A J7EA O OTHER O OTHER NR NOT REPORTED 1 WP 07 411AJ 1208 1047 2011 INITIALLY THE FMS WOULD NOT PASS THE SELF TEST. SCREEN WAS TELLING THE TECH THAT THE CDU/RAM FAILURE. REMOVED FMS INST ALLED OVERHAULED FMS. THIS WOULD INITIALIZE PROPERLY. FMS DOWNLOADED NAV DATABASE PROPERLY. WHEN PERFORMANCE DATABASE WAS INSTALLED, IT WAS SAYING NO DISK INSTALLED. FOUND THAT THERE WAS AN INCORRECT FMS INSTALLED. ACFT SHOULD HAVE SCN 802.5 INSTALLED. THIS OVERHAULED FMS WAS A SCN 801.5, FMS SCN 802.3 INSTALLED BOTH NAVIGATION, AND PERFORMANCE. OPS CHECK WAS SATISFACTORY COMPLETED. NO OTHER DEFECTS WERE NOTED. (K) 2 L 7 2 4F 4 F RT T00008WI E6WE 20081008 EA 2008 10 8 CVG2008F00001 1 20080818 A 5610 600330301 WINDOW CNDAIR CL600 CL6002B16 1900305 EA COCKPIT CRACKED E CVGA O OTHER O OTHER CR CRUISE 1 GL 05 497DM 5359 DURING CRUISE AT FL380, PILOTS SIDE WINDOW OUTER PANE CRACKED. AC DEPARTED. REMOVED DEFECTIVE LT WINDOW AND INSTALLED A NEW WINDOW. POST INSTALLATION OPERATIONAL TEST OF COCKPIT SIDE WINDOW ANTI-ICING SYS AND LEAK TESTS WERE COMPLETED WITH SATISFACTORY RESULTS. (K) 2 L 7 2 4F RT A21EA 20081008 NM 2008 10 8 AALA200802049 1 20080809 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW EMERGENCY LIGHT AT SEAT 21C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 SPA2008F00002 1 20080917 A 3350 110049 BATTERY PACK BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15 52051 NE EMERGENCY LIGHT INOPERATIVE A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 07 712S 23038 LOWER EMERGENCY EXIT LIGHT AT R1 AND L1 DOOR POSITIONS WILL NOT ILLUMINATE. REPLACED EMERGENCY LIGHT BATTERY PACK IAW MA NUAL 33-21-27. FUNCTIONAL CHECK SATISFACTORY. (K) 2 L 7 2 4U 4 F RT A16WE E2EA 20081003 NM 2008 10 3 2008UALA05922 1 20080927 A 5320 FLOOR SUPPORT AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 804UA 759 CORROSION ON FLOOR SUPPORT RT SIDE FR 70 STR 22-23. REMOVED CORROSION. FABRICATED & INSTALLED NEW FITTING. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 2008 10 3 2008UALA05931 4 20080929 A 3414 INDICATOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AIRSPEED MALFUNCTIONED A UALA C ABORTED TAKEOFF W INADEQUATE Q C TO TAKEOFF 1 WP 29 336UA 24240 ABORTED T/O AT AROUND 100 KTS AT 110K LBS, ACCOUNT OF FLAG IN VIEW ON F/O'S AIRSPEED INDICATOR. 2 L 7 2 4F 4 F RT A16WE E21EU 20081003 EU 2008 10 3 2008UALA05933 1 20080929 A 3830 TOILET AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LAVATORY INTERMITTENT A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 455UA 1105 LAVATORY TOILET BOWL FLUSH SYSTEM INOPERATIVE AT AFT CABIN LIGHT AFT LAV. CREW COMMENTS: BOTH AFT LAV TOILETS FLUSH SY STEMS ARE INTERMITTENT. 2 L 7 2 4F 4 F RT A28NM E40NE 20081120 NM 2008 11 20 DL757081484 1 20081104 A 5753 113N21007 CARRIAGE BOEING 757 757232 1384965 NM LT WING TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 DURING HMV, FOUR ELONGATED BOLT HOLES WERE FOUND IN THE LT WING INBOARD MAIN FLAP INBOARD CARRIAGE ASSEMBLY. THE ELONGA TED HOLES WERE REAMED TO ROUND HOLES AND OVERSIZE BOLTS WERE INSTALLED PER BOEING INSTRUCTIONS. 2 L 7 2 4F RT A2NM 20081120 NM 2008 11 20 DL757081489 1 20081104 A 5315 146N54443 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 AFT CARGO BAY STATION 1510 LBL 7 FLOORBEAM CORRODED. REPAIRED PER 53-60-53D ON NR 00035. 2 L 7 2 4F RT A2NM 20081120 WP 2008 11 20 IXXA08SMN131S 1 20080411 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 1350 LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND CORROSION FOU ND. FABRICATED REPAIR DOUBLER, FILLER, FINGER DOUBLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08198 DATED 04/25/08, DRAWING ED-4760 DATED 04/24/08, SRM 51- 1-21, 51-1-20D, 51-3-0, NDT SPM PART 06-10-01-001, SRM 51-1-8B, SRM 51-1-11, AND 51-3-1. 2 L 7 4 4F RT 4A25 20081120 WP 2008 11 20 IXXA08SMN132S 1 20080411 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 545 LONGERON 35.75 LEFT. REMOVED FASTENERS AS NE EDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND CORROS ION FOUND. FABRICATED REPAIR DOUBLER, FILLER, AND FINGER DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08188 DATED 04/23/08, SEMAN DRAWING ED-4758 DATED 04 /19/08, DC8 SRM 51-1-21, 51-1-20D, 51-3-0, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND 51-3-1. 2 L 7 4 4F RT 4A25 20081120 EA 2008 11 20 SWIA200820384 1 20081111 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 465SW 7845 FLT 6020 - FIRST EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081120 EA 2008 11 20 SWIA200820385 1 20081111 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 429SW 7518 FLT 4559 - FIRST EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081120 EA 2008 11 20 SWIA200820386 1 20081113 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 804SK 15067 FLT 4522 - EMERGENCY CEILING FLOOD LIGHTS INOP AT ROW 20. RELAMPED. 2 L 7 2 4F RT A21EA 20081120 SO 2008 11 20 SWIA200820387 1 20081111 A 5610 WINDOW EMB 120 EMB120ER 3260203 SO COCKPIT STUCK A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 586SW 120354 FLT 5743 - CREW UNABLE TO OPEN FO DIRECT VISION WINDOW. LUBRICATED FO'S WINDOW. 2 L 7 2 4T RT A31SO 20081120 EU 2008 11 20 COEA0805917 1 20081013 A 5312 S53174000202 STIFFENER AEROSP ATR42 ATR42300 8680920 EU BULKHEAD CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 917FX 354 MAJOR REPAIR AND LEVEL 2 CORROSION. FWD BULKHEAD EXTRUDED STIFFENER HAS SURFACE CORROSION AROUND ATTACHMENT RIVETS. CO RROSION BLEND-OUT WAS BEYOND ACCEPTABLE LIMITS. FOUND AT COE MAJOR REPAIR AND LEVEL 2 CORROSION. FWD BULKHEAD EXTRUDED STIFFENER HAS SURFACE CORROSION AROUND ATTACHMENT RIVETS. CORROSION BLEND OUT WAS BEYOND ACCEPTABLE LIMITS. BLENDED O UT DAMAGED AREA ON THE VERTICAL STIFFENER AND LEFT AS IS. R&R FASTENERS IN AREA OF CORROSION AND INSPECTED HOLES FOR CR ACKS. 2 H 7 2 4T RT A53EU 20081120 CE 2008 11 20 COEA0801899 1 20081007 A 7331 UNKNOWN CESSNA 208 208B 2073701 CE FUEL FLOW MALFUNCTIONED A COEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 13 899FE 208B0235 DURING CLIMB OUT AT APPROXIMATELY 1500 FT AGL THE FUEL FLOW DROPPED TO 75 PPH. THE PARS UNIT CONFIRMED A 75 PPH FUEL FL OW. THE AC RETURNED TO SAFELY. TROUBLESHOOT ON THE GROUND WITH ENGINE RUNS COULD NOT DUPLICATE THE PROBLEM. THE FUEL FLOW INDICATOR WAS REPLACED FOR ADDITIONAL TROUBLESHOOTING AFTER THE GROUND RUNS COULD NOT DUPLICATE THE PROBLEM. THERE HAS NOT BEEN ANY REPORTED PROBLEM WITH THE FUEL FLOW INDICATIONS SYSTEM FROM THE LAST 2 SUBSEQUENT FLIGHTS. REMOVED AN D REPLACED THE FUEL FLOW INDICATOR FOR TROUBLESHOOTING. (K) 1 H 7 1 3T A37CE 20081120 SO 2008 11 20 FDK2008F00013 1 20081004 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA O OTHER O OTHER NR NOT REPORTED 1 SW 07 846MJ 145507 OVERHEAD EMERGENCY ROW LIGHTS INOP. MX RESET SYS. (K) 2 L 7 2 4T RT T00011AT 20081120 SO 2008 11 20 FDK2008F00014 1 20081007 A 2913 971808 PUMP EMB 145 EMB145LR 3260212 SO HYDRAULIC SYS FAILED A FDKA O OTHER J G WARNING INDICATION MULTIPLE FAILURE NR NOT REPORTED 1 SW 07 825MJ 145179 DECLARED AN EMERGENCY DUE TO HYDR 2 PRESSURE AND QUANTITY WENT TO ZERO. ALSO, HAD AILERON 2 AND RUDDER 2 FAIL IN FLIGHT . MX REMOVED AND REPLACED EDP 2 AND SERVICED HYD. OPS CHECKED MACH 2. (K) 2 L 7 2 4T RT T00011AT 20081120 SO 2008 11 20 FDK2008F00015 1 20081004 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA K NONE O OTHER IN INSP/MAINT 1 SW 07 836MJ 145359 RT ROW 12 EMERGENCY SIGN INOP. MX RE-SECURED LIGHT ASSY OPS CK GOOD. (K) 2 L 7 2 4T RT T00011AT 20081119 SO 2008 11 19 C2XA08CL111 1 20081009 A 3240 429515 CONTROL UNIT EMB 145 EMB145LR 3260212 SO BRAKE FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 48901 145501 CLE FLIGHT NR 2626 THE CREW REPORTED A NR 1 T/R DISAGREE AND A SPOILER FAIL MSG IN FLIGHT. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE BRAKE CONTROL UNIT AND RELAYS KO479 AND K1202. OPS CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20081119 NM 2008 11 19 CALA0801081 1 20081116 A 5320 141A5410U12 INTERCOSTAL BOEING 737 737824 13844BZ NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 79279 31597 INTERCOSTAL BETWEEN STA 312 AND 328 AT RBL 31 IS CRACKED AT FASTENER HOLE. REMOVED INTERCOSTAL, INSTALLED NEW INTERCOST AL PER BOEING DOC 141A5400 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086282 1 20081114 A 3350 81000 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 482WN 29852 FOUND EEPLS LOOSE AT ROW 1. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086283 1 20081114 A 3350 81000 STRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 488WN 33853 FOUND EEPLS STRIP LOOSE AT ROW 1. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086105 1 20081110 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FLOORBEAM CHORD CRACKED AT BS 665, LBL 24. REPAIRED CHORD PER EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086126 1 20081109 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 904WN 36616 FOUND FWD EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086091 1 20081110 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED AT BS 661, LBL 24. REPAIRED CHORD PER EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086092 1 20081106 A 3350 65C27095 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED CV CHECK, FOUND EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 3 TO ROW 4. REMOVED AND REPLACED BATTER Y PACK PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086259 1 20081117 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 400, BETWEEN STR 9R TO STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086268 1 20081114 A 3350 307ABPEGPL LIGHT BOEING 737 737705 13844SC NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 270WN 29089 DURING SCHEDULED MV1 CHECK, FOUND RT EMERGENCY EXIT SIDE WALL LAMP INOP. REMOVED AND REPLACED LAMP PER MM. 2 L 7 2 4F RT A16WE 20081119 NM 2008 11 19 SWAA086270 1 20081117 A 5340 693532U14 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP DAMAGED AT BS 420, STR 4R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081119 2008 11 19 SWAA086099 4 20081106 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 508SW 24185 FOUND L2 EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081119 2008 11 19 SWAA086100 4 20081105 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081119 EA 2008 11 19 ASOA200801504 1 20081113 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 849AS 7347 EMERGENCY FLOOR TRACK LIGHTING FROM 3CD-4CD INOP. 2 L 7 2 4F RT A21EA 20081119 EA 2008 11 19 ASOA200801505 1 20081113 A 5312 ISOLATOR CNDAIR CL600 CL6002B19 1900309 EA BULKHEAD BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 927EV 7844 FS 621.00 REAR PRESSURE BULKHEAD FWD FACE HAS TWO ISOLATORS BROKEN. REPLACED ISOLATORS AT FS 621.00 REAR PRESSURE BULK HEAD FWD FACE IAW SRM 51-42-10. 2 L 7 2 4F RT A21EA 20081119 WP 2008 11 19 AALA200810009 1 20081008 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 AFT UPPER CORNER OF WINDOW PANE IS CRACKED. DOUBLER INSTALLED PER AARD 53-10-00-25. 2 L 7 2 4F A6WE 20081119 WP 2008 11 19 AALA200810010 1 20081008 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 FORWARD LOWER SIDE OF WINDOW PAN IS CRACKED AT AFT SIDE OF STATION 1022 RIGHT SIDE. INSTALLED REPAIR ANGLE PER AARD 53- 40-00-25. 2 L 7 2 4F A6WE 20081119 NM 2008 11 19 AALA200802703 1 20081008 A 3350 PBS73 BATTERY PACK BOEING 757 757223 1384957 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 664AA 25298 DFW - EMERGENCY LIGHTS AT RIGHT FORWARD AND AFT OVERWING EXIT HANDLES INOPERATIVE. REPLACED BATTERY PACK AT STATION 985 FOR RIGHT FORWARD AND AFT OVERWING EXIT HANDLE LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081120 EA 2008 11 20 ASOA200801282 1 20081003 A 5230 BRACKET CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED CRACKED BRACKET IAW CRJ 200 SRM 51-42-21. LOCATED HOLES IN NEW SERVICEABLE BRACKET IAW SRM 51-40-11. INSTALLED BRACKET IAW SRM 51-42-21. AFT PRESSURE BULKHEAD AT FS 621.00 DUE LEAK CK, FOR FASTENERS REPLACED. PRESSURIZATION CHEC K GOOD IAW CRJ 200 AMM 21-32-00-863-801. SUPPLEMENTAL-SDR CLOSED 11/13/2008. 2 L 7 2 4F RT A21EA 20081120 NM 2008 11 20 08FDEA04912 1 20081118 A 5311 651634235 FRAME BOEING 727 7272D4 138407U NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 AFT CARGO PIT STATION 1030 FUSELAGE FRAME DAMAGED AT STR 26L. REMOVED FRAME DAMAGE STA 1030 STR 26L REF SRM 51-40-3 FIG 1 PGS 1-6. FORMED DOUBLER REF SRM 51-20-1 PG 1 HEAT TREAT DOUBLER TRACKING 2008-11-129. REMOVED INTERCOSTAL STA 103 0, INSTALALED INTERCOSTAL STA 1030 STR 24-26L REF SRM 51-30-2 PGS 1-17. FABRICATED REPAIR DOUBLER REF SRM 51-40-3 FIG 1. TREATED PRIMED REPAIR DOUBLER REF SRM 51-10-2 MM 51-30-151-7. INSTALLED REPAIR DOUBLER REF SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20081120 NM 2008 11 20 QXEA2008111401174 1 20081110 A 3213 PIN BOMBDR DHC8 DHC8402 1390042 NM STRUT BACKED OUT A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 19 417QX 4086 SEA - ON DEPARTURE WOW CAUTION ILLUMINATED AND AURAL TONE HEARD AT HIGH POWER SETTINGS. RETURNED TO THE FIELD AND ACCOM PLISHED A UNEVENTFUL LANDING. FOUND THE SHOCK STRUT PIVOT ARM PIN BACKED OUT 1.5 INCH APPROX. INSPECTED PIN WITH NO DA MAGE FOUND, REINSTALLED PIN IAW 32-21-03-400-801. GVI PERFORMED ON GEAR AND DOORS WITH NO DEFECTS FOUND. LUBRICATED PIV OT ARM. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081120 WP 2008 11 20 IXXA08SMN135S 1 20080418 A 5343 3646956U502 FITTING DOUG DC8 DC871F 302199D WP BS 940 L24R CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR WHEEL WELL FITTING CRACKED AT STATION 940.000 LONGERON 24. REMOVED CRACKED FRAME FITTING. FABRICATED SPLICES, DOUBLER, FILLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FITTING AND REPAIR PARTS IAW DC8 SRM 53-2-0 FIGURE 8 SHEETS 1, 2, 5 AND 6, DC8 SRM 53-1-0 PAGE 1, 51-1-20D, DC8 AND SRM 51-1-8B. 2 L 7 4 4F RT 4A25 20081120 EU 2008 11 20 F3LA2008111700713 1 20081115 A 5755 D5775002100118A HINGE FITTING AIRBUS A318 A318111 3940019 EU NR 4 SPOILER GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 801FR 1939 DURING C4 C-CHECK, INSPECTION NOTED THE RIGHT NR 4 SPOILER ANTI-ROTATION WEB FLAT WAS GOUGED. MAINTENANCE REPAIRED THE DAMAGE IN ACCORDANCE WITH ENGINEERING AUTHORIZATION A8-57R-30776. 2 L 7 2 4F RT 20081120 WP 2008 11 20 IXXA08SMN147S 1 20080418 A 5330 SKIN DOUG DC8 DC871F 302199D WP ZONE 100 MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 45.000 LONGERON 29LT. REMOVED FASTENERS AS NEEDE D TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 53-2-0 FIGURE 13 SHEET 1 TR NUMBER 53-16 9 SHEET 5 DATED 09-20-03, SRM 51-1-20D, SRM 53-2-0 FIGURE 13 SHEET 1 VIEW A (7001) ITEM 1, SRM 53-3-1 FIGURE 1 ITEM C, S RM 51-1-8B, SRM 51-1-11, 51-1-21, 51-1-20D AND 51-3-1. 2 L 7 4 4F RT 4A25 20081120 WP 2008 11 20 IXXA08SMN176S 1 20080419 A 5347 CARGO TRACK DOUG DC8 DC871F 302199D WP CARGO BAY DETERIORATED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 5 TRACK LUGS DETERIORATED BETWEEN STATION 70.000 AND STATION 210.000. REMOVED DAMAGED SEGMENT OF TRACK AND EXISTING SPLICES. CLEANED, TREATED AND PRIMED AREA AND EXIST ING SPLICES. INSTALLED NEW SEGMENT OF TRACK AND REINSTALLED SPLICES IAW DC8 SRM 53-2-3 FIGURE 14 SHEET 1 PAGES 49-50, D C8 SRM 51-3-0, DC8 SRM 51-1-8B, 51-1-20D, AND 51-3-1. 2 L 7 4 4F RT 4A25 20081120 NM 2008 11 20 QXEA2008111401189 1 20081114 A 3231 CONNECTING ROD BOMBDR DHC8 DHC8402 1390042 NM MLG DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 405QX 4047 GEG - DURING POST FLIGHT INSPECTION, NOTED RT GEAR DOORS SAGGING OPEN 1 1/2 INCHES, AFT DOORS THAT ARE NORMALLY CLOSED. REMOVED AND REPLACED RT MLG AFT OTBD DOOR CONNECTING ROD ASSY WITH NEW FROM STOCK AND RIGGED RT MLG AFT DOORS IAW Q400 AMM TASKS 32-12-06-000-801 TR NR32-250, 32-12-06-400-801 TR NR 32-250 AND 32-12-01-830-801. OPS CKS GOOD. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081120 NM 2008 11 20 DHLA2008745688 1 20081113 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 CABIN FLOORBEAM AT BS 1070 LOWER CHORD CORRODED FROM LBL 10 TO RBL 55. ACCOMPLISHED REPAIR TO LOWER CHORD FROM LBL 19 T O RBL 10 PER B727 SRM 53-10-8 FIG 8. ALL OTHER CORROSION CLEANED UP WITHIN SERVICE LIMITS. DOCUMENTED ON N/R 2-164. 2 L 7 3 4F A3WE 20081120 EU 2008 11 20 E0X2008F00007 1 20081025 A 2720 RUDDER BRAERO 1000 BAE1251000 1500287 EU LOCKED E E0XA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 39 505LR 259005 AFTER DEPARTED, GOING THROUGH APPROX 800 FT AGL THE F/O NOTED THAT THE RUDDER HAD LOCKED UP IN THE NEUTRAL POSITION. TH E OAT AT THE TIME WAS +9C. ACFT CONTINUED TO CLIMB AND CAPTAIN INFORMED ATC THAT WOULD BE RETURNING TO DEPARTURE. ACFT WAS ABOVE MAX LANDING WEIGHT SO FLIGHT CREW REQUESTED A DELAY IN LANDING UNTIL ACFT BURNED OFF FUEL BELOW MAX LANDING WE IGHT. FLIGHT CREW DID NO DECLARE AN EMERGENCY AND NO PASSENGERS WERE ON ACFT. THE WINDS WERE CALM AND THE APPROACH AND LANDING WAS WITHOUT INCIDENT. ONCE ON GROUND THE RUDDER RETURNED TO NORMAL WITHOUT ANY INPUT FROM FLIGHT CREW. ANTI-I CE SYSTEMS WERE IN FORMAL OPERATION DURING FLIGHT, YAW DAMP AND AUTO-PILOT WERE NEVER ENGAGED DURING FLIGHT. CONTACTED 2 L 7 2 4F RT A3EU 20081121 SO 2008 11 21 GLBA200810008088 1 20081008 A 5310 WINDOW POST EMB 120 EMB120ER 3260203 SO FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 21 71GL 120071 SUPPLEMENTAL INFORMATION - MAJOR REPAIR. CRACK IN RT FWD DV WINDOW POST. C/W EO 04-716L-01 ON RT DV WINDOW IAW THE INC LUDED INSTRUCTIONS AND SB 120-53-0072. SCHEDULED MAINTENANCE INSPECTION IT WAS DISCOVERED THAT THIS REPAIR DOES NOT CON FORM TO GIVEN DOCUMENTATION. 10/22/08- NO FURTHER ACTION REQUIRED. RELIEF FOR AFFECTED AREA OBTAINED FROM EMBRAER 10/22 /08. REFERENCE EMBRAER IC2008-120/07962. IWO 96192. 2 L 7 2 4T RT A31SO 20081121 NM 2008 11 21 DL738081578 1 20081117 A 2751 18173810 TRANSMITTER BOEING 737 737832 13844CF NM LEFT FLAP MALFUNCTIONED A DALA O OTHER N FALSE WARNING DE DESCENT 1 SO 27 3747D 29665 FLAPS STUCK AT 25 DEGREES ON LANDING. WOULD NOT SELECT TO 30 DEGREES OR BACK TO 15 DEGREE AFTER LANDING WITH HANDLE IN 15 POSITION FLAPS MOVED TO 15 DEGREES AND THEN RETRACTED TO UP WHEN HANDLE MOVED TO UP. REPLACED LT FLAP TRANSMITTER CH ECKS OK. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 DL757081581 1 20081011 A 5311 FRAME BOEING 757 757232 1384965 NM BS 395 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 MAIN CABIN FRAME STA 395 LT SIDE FWD CABIN 2 DENTS. BLENDED GOUGES, FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 PG 103 DETAIL II. INSTALLED REPAIR PARTS AT FRAME 395 IAW ERA 461183-14 STEP 8. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081568 1 20081116 A 5320 146N539155 FLOOR SUPPORT BOEING 757 757232 1384965 NM BS 1465 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 FLOOR SUPPORT STRINGER BS 1465 LBL 16 IS CORRODED AT THE NUTPLATE. REPAIRED FLOOR SUPPOR IAW MM 53-87-01-801. 2 L 7 2 4F RT A2NM 20081121 SO 2008 11 21 GLBA200809251 1 20080925 A 5330 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE PUNCTURED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 21 71GL 120071 SUPPLEMENTAL INFORMATION - MAJOR REPAIR. DURING SCHEDULED MAINTENANCE A HOLE IN THE FUSELAGE IN AN AREA CLOSE TO THE CA RGO DOOR PULLEY AREA AT FS 15000.0 BETWEEN STRINGER 2L & 3L APPROXIMATELY .5 INCH BY .750 INCH WAS DISCOVERED. MAINTENA NCE REPAIRED .5 INCH BY .750 INCH HOLE IN AFT LEFT AT APPROXIMATELY FS 15000.0 BETWEEN STRINGER 2L & 3L IAW EMB 120 SRM 53-00. REPAIR APPROXIMATELY 3.7 INCH BY 3.750 INCH. 2024 T-3, .063 INCH, FILLER MATERIAL 2024 T-3 .063 INCH. BRFZ AD R IVETS UTILIZED. 2 L 7 2 4T RT A31SO 20081121 NM 2008 11 21 DL757081569 1 20081111 A 5315 146N543131 FLOORBEAM BOEING 757 757232 1384965 NM BS 1530 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 CORROSION AROUND NUTPLATES BS 1530 RBL 22 COMMON TO FLOOR TO SIDE WALL SPLICE LOWER SURFACE OF SPLICE, BULDGED. REPLACE D SPLICE IAW 51-40-02. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081570 1 20081114 A 5321 146N539155 FLOOR PANEL BOEING 757 757232 1384965 NM BS 1530 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 652DL 24392 CORROSION ON LOWER SURFACE OF FLOOR TO SIDEWALL BS 1530, RBL 16 - RBL 20, PANEL REPLACED ON CUSTOMER CARD NR 00033 DUE T O CORROSION OUT OF LIMITS IAW 51-40-02. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081533 1 20081112 A 5311 146N103072 FRAME BOEING 757 757232 1384965 NM FS 1540 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 DURING AGING AIRCRAFT INSPECTIONS ON THE SUBJECT AIRCRAFT, VISUAL INSPECTIONS NOTED CORROSION ON THE FORWARD SIDE OF THE 1540 BOTTOM FRAME BETWEEN S-29L AND S-30L. THE CORROSION WAS UNDER THE ATTACHING SHEAR TIE. SUBJECT CORROSION WAS REM OVED PER SRM GUIDELINES, WITH THE EXCEPTION OF THE PROXIMITY TO NEAREST FASTENER. AS A RESULT, BOEING WAS CONTACTED FOR APPROVAL TO LEAVE THE BLEND AS IS NEAR THE SUBECT FASTENERS. BOEING APPROVED AND INFO IS DOCUMENTED IN ER/A 471250-14. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL75E081537 1 20081113 A 2161 CONTROLLER BOEING 757 7572Q8 1384972 NM LT A/C PACK INOPERATIVE A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 707TW 27625 LT PACK TEMP CONTROL INOP. RE- RACKED LT PACK TEMP CONTROL PER BITE. NO FAULTS. LT PACK OPS NML. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081542 1 20081011 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 MAIN CABIN FLOORBEAM STA 350 BL "0"-LBL 13 CORRODED. FABRICATED, LOCATED, AND DRILLED ANGLES, TREATED AND PRIMED IAW SR M 53-10-51D FIG 203 PG 212 AND 51-40-05 PG 1 AND 51-20-01 PG 1. INSTALLED 2 REPAIR ANGLES IAW 53-10-51D FIG 203 PG 212. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081544 1 20081011 A 5315 BEAM BOEING 757 757232 1384965 NM BS 324 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 MAIN CABIN FLOORBEAM STA 324 RBL 3 CORRODED. REMOVED DAMAGED AREA AND INSTALLED NEW SECTION IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081549 1 20081011 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 355 LBL 34 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 MAIN CABIN FLOOR CONNECTING CHANNEL 5 INCHES FWD STA 350 LBL 34 CORRODED. REMOVED AND REPLACED DAMAGED SUPPORT IAW SRM 51-40-02 PG 2 PARA 4. 2 L 7 2 4F RT A2NM 20081121 CE 2008 11 21 GUUA11010801 1 20081101 A 5220 DOOR BEECH 1900 1900D 1154162 CE EMERGENCY EXIT LACK OF LUBE A GUUA O OTHER O OTHER IN INSP/MAINT 1 SO 29 87551 UE206 DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED EMERGENCY DOOR AT SEAT 6F STIFF TO OPEN. LUBRICATED EMERGENCY DOOR. OP ERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081121 CE 2008 11 21 GUUA11160804 1 20081116 A 3240 BRAKE SYS BEECH 1900 1900D 1154162 CE RIGHT CONTAMINATED A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 81533 UE137 FLIGHT 9158 TPA/EYW - PILOT REPORTED RIGHT BRAKE INOPERATIVE RIGHT PEDAL GOES ALL THE WAY DOWN. BLED RIGHT BRAKE. OPER ATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081121 NM 2008 11 21 DL757081571 1 20081114 A 5321 146N539155 FLOOR PANEL BOEING 757 757232 1384965 NM BS 1480-1520 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 652DL 24392 CORRODED FASTENER HOLES COMMON TO SIDEWALL SUPPORT, BS 1480 THRU BS 1520 RT PANEL WAS REPLACED DUE TO CORROSION OUT OF L IMITS ON CUSTOMER CARD ATS NR 00033 IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081121 CE 2008 11 21 GUUA11060803 1 20081116 A 3240 BRAKE SYS BEECH 1900 1900D 1154162 CE RIGHT CONTAMINATED A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 81533 UE137 FLIGHT 9207 PNS/TPA - PILOT REPORTED RIGHT BRAKE INOPERATIVE THE PEDAL GOES ALL THE WAY DOWN BLED RIGHT BRAKES. OPERATI ONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081121 NM 2008 11 21 DL757081538 1 20081014 A 5412 BULKHEAD BOEING 757 757232 1384965 NM NR 1 PYLON CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 NR 1 PYLON BLKHD (AFT) LWR OUTBD CORNER IS CHAFED. PYLON REPAIRED IAW ERA 471168-14 AD REV 0. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081541 1 20081113 A 3350 SOCKET BOEING 757 757232 1384965 NM EMERGENCY LIGHTS DIRTY A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 650DL 24390 EXTERNAL EMERGENCY LIGHTS INOP. REMOVED, CLEANED, AND REINSTALLED SOCKETS IAW AMM 33-51-06-962-049. REPLACED LAMPS IAW AMM 33-51-06-962-042. OPS CHECK GOOD IAW AMM 33-51-00-715-075. 2 L 7 2 4F RT A2NM 20081121 WP 2008 11 21 AALA200810105 1 20081027 A 5320 STRUCTURE DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 CABIN SUBFLOOR CORROSION, 8 INCH BY 16 INCH, INSTALLED NEW SUBFLOOR DOUBLER PER 53-20-00-16. 2 L 7 2 4F A6WE 20081121 NM 2008 11 21 DL757081560 1 20081112 A 5320 65C80678180 SUPPORT BOEING 757 757232 1384965 NM BS 1400 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 SUPPORT COMMON TO FITTING CORRODED BS 1400 RBL 28. REMOVED AND REPLACED SUPPORT IAW SRM 51-40-02, DRW 146N8560. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081561 1 20081112 A 5340 415N400217 MOUNT BOEING 757 757232 1384965 NM G1A GALLEY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 CORROSION ON OTBD AFT GALLEY MOUNT BS 322 RBL 38 WL 209. REMOVED AND REPLACED GALLEY FITTING IAW SRM 51-40-02, SRM 51-4 0-03, SRM 51-40-04. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 SWAA086318 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 4R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 WP 2008 11 21 AALA200810104 1 20081023 A 5320 STRUCTURE DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 CABIN SUBFLOOR CORRODED, STATION 160-200 RIGHT. REMOVED AND REPLACED SUBFLOOR PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081121 NM 2008 11 21 DL757081501 1 20081105 A 5320 146N5480 ANGLE BOEING 757 757232 1384965 NM BS 1480-1500 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 652DL 24392 AFT CARGO ANGLE CORRODED AT 1480 TO 1500 STRINGER 26 LT. REPAIRED PER 53-00-04 ON ATS NR 00088. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 08FDEA04928 1 20081119 A 5340 652427638 FITTING BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 AFT PIT STRINGER BULKHEAD FITTING STA 1183 STR 19R CORRODED. REMOVED AND REPLACED CORRODED FITTING, REF SRM 51-30-2 PG 1-4,8 THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081121 NM 2008 11 21 08FDEA04929 1 20081119 A 5320 6519606164 WEB BOEING 727 7272S2F 1384O81 NM ZONE 100 MISALIGNED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 MAIN CABIN SHEAR DECK AT BS 1148 TO 1166 RBL 8-19 NEEDS FABRICATED, SHEAR DECK WILL NOT BE ABLE TO BE INSTALLED AFTER FL OORBEAM REPAIR ON SNRM N00512. NEW DECK WILL BE FABRICATED FROM REF 65-19602. FABRICATED MAIN CABIN SHEAR DECK AT 1148 TO 1166 RBL 8-19 REF DWR 65-19606, SRM 51-10-2. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081121 NM 2008 11 21 SWAA086300 1 20081118 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 UALA2008111300794 1 20080212 A 2751 1817389 TRANSMITTER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU TE FLAP FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 337UA 24241 FLIGHT DIVERTED DUE TO A FLAP ASYMMETRY PROBLEM. FAULTY FLAP POSITION TRANSMITTER. REPLACED LT FLAP POSITION TRANSMITT ER. 2 L 7 2 4F 4 F RT A16WE E21EU 20081121 NM 2008 11 21 UALA2008111302618 1 20080502 A 4997 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU DIRTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 647UA 25284 APU AUTO SHUT DOWN. REMOVED & CLEANED FUEL CONTROL UNIT CONNECTOR. APU STARTS AND RUNS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081121 NM 2008 11 21 UALA2008111303630 1 20080630 A 2751 01812996 INDICATOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C 13802 EU COCKPIT FAULTY A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 928UA 26651 FLAPS WOULD NOT RETRACT AFTER TAKEOFF. CYCLED INDICATOR CB, NO HELP. RTFL. SUSPECT FAULTY INDICATOR. CYCLED FLAP IND ICATOR CB AND FLAPS BEGAN TO OPERATE. REPLACED INDICATOR, OP CHECKS OK. ACMP FCC INTERFERENCE TEST OF FLAP TRANSMITTER S. ALL VALUES NORMAL. 2 L 7 2 4F 4 F RT A16WE E21EU 20081121 WP 2008 11 21 IXXA08SMN153S 1 20080418 A 5310 DOOR FRAME DOUG DC8 DC871F 302199D WP ZONE 100 WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND "B" CARGO DOOR FORWARD LOWER JAMB CORNER SKIN WORN AT STATION 520.000 LONGERON 30 RIGHT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, FILLERS, CLEANED. TREATED AN D PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FAA FORM 8100-9 DATED 05-22-08, AD 2005-18-0-7 S/B DC8-53-07 8, DRAWING SR08530019, 5750776, MESSAGE 1-821382564-7 DATED 05-09-08 ND 1-842846685-2 DATED 05-22-08, SRM 51-1-8 PAGES 17-18, SRM 53-2-0 PAGE 2P, SRM 51-3-0, 51-1-21, 51-1-20D, REPAIR SKETCH 1-821382564, NDT SPM PART 06-10-01-001, AND SRM 2 L 7 4 4F RT 4A25 20081121 SO 2008 11 21 CHQA200800217 1 20081107 A 3260 8005701 PROXIMITY SENSOR EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL LT MLG OUT OF LIMITS A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 561RP 145447 CAE311826 FLIGHT 6046, CMH TO JFK, AFTER LIFT-OFF, THE FLIGHT CREW RECEIVED A L/G AIR/GND FAIL MESSAGE ON EICAS, AND THE GEAR LEVE R COULD NOT BE MOVED TO THE UP POSITION. THE QRH WAS FOLLOWED AND THE AIRCRAFT LANDED BACK AT CMH WITHOUT INCIDENT. MA INTENANCE FOUND THE WEIGHT-ON-WHEELS PROXIMITY SWITCH GAPS WERE OUTSIDE LIMITS. THE GAPS WERE ADJUSTED BACK INTO TOLERA NCE AND THE PROX SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081119 NM 2008 11 19 AALA200802706 1 20081008 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 187AN 32381 DFW - EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP AT LEFT NUMBER FOUR DOOR. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081119 WP 2008 11 19 AALA200810141 1 20081027 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 CORROSION ON LEFT CUSP AT STATION 695. INSTALLED CUSP REPAIR DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081120 EA 2008 11 20 ASOA200801285 1 20081003 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REPAIRED FS 409+128 LBL 27 INBOARD SIDE IAW REO 601R-53-41-056 STEPS 1-16. PRESSURE CHECK REQUIRED. PRESSURE CHECK GOO D IAW CRJ 200 AMM 21-32-00-863-801. ASA ECTC REO 601R-53-056 REQUIRED. ASA EC/TC REO 601R-53-056 INCORPORATED. SUPPLE MENTAL-SDR CLOSED 11/13/2008. 2 L 7 2 4F RT A21EA 20081120 SO 2008 11 20 CHQA200800215 1 20081104 A 3350 66367 LIGHT EMB 145 EMB145EP 3260221 SO ALLSN AE3007 AE3007A 03030 GL CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 978RP 145169 CAE312632 DURING INSPECTION WHILE TESTING THE EMERGENCY LIGHTING, THE FLOOR STRIPS AT SEATS 10, 11, 14, 15, AND 16 WERE FOUND TO B E INOP. THE EMERGENCY FLOOR LIGHT STRIPS WERE REPLACED AND THE EMERGENCY LIGHTING SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081120 WP 2008 11 20 IXXA080031O 1 20081105 A 5310 ACCESS PANEL DOUG DC8 DC871F 302199D WP COCKPIT MISINSTALLED A IXXA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 11 821BX 89259 381 45811 DURING CLIMB-OUT FROM KBDL, THE CREW HEARD LOUD NOISE OF AIR FROM CAPT'S SIDE. THE CREW RETURNED TO KBDL WITHOUT FURTHE R INCIDENT. MAINTENANCE FOUND EMERGENCY ACCESS PANEL TO CAPT CLEARVIEW WINDOW HAD COME OUT AND FELL DOWN INTO FUSELAGE. MAINTENANCE REINSTALLED PANEL IAW DACO DC8 MAINTENANCE MANUAL 6-11-1. 2 L 7 4 4F RT 4A25 20081120 NM 2008 11 20 08FDEA04858 1 20081111 A 5753 652163013 SKIN BOEING 727 727227 1384078 NM RT WING FLAP GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 495FE 21669 RT INBD FOREFLAP L/E O/B CORNER IS GOUGED ON PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR IAW B727 SRM 51-30-2. FABRICATED NEW REPAIR PART, MAT USED 2024T3 .063 PO NR 9007835, DIMENSION 4 INCH BY 3 3/4 INCH IAW B727 57-50-4 FIG 1. TREATED AND PRIMED AREA AND PART IAW B 727 SRM 51-10-2. INSTALLED NEW DOUBLER IAW B 727 SRM 51-30-2. 2 L 7 3 4F A3WE 20081120 EU 2008 11 20 COEA0804917 1 20081009 A 5751 S57610187203 SKIN AEROSP ATR42 ATR42300 8680920 EU AILERON CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 917FX 354 MAJOR REPAIR AND LEVEL 2 CORROSION. RT WING AILERON TRAILING EDGE HAS SURFACE CORROSION, JUST OB OF THE TRIM TAB. CORR OSION BLEND-OUT WAS BEYOND ACCEPTABLE LIMITS. FOUND AT COE MAJOR REPAIR AND LEVEL 2 CORROSION. RT WING AILERON TRAILIN G EDGE HAS SURFACE CORROSION, JUST OTBD OF THE TRIM TAB. CORROSION BLEND OUT WAS BEYOND ACCEPTABLE LIMITS. CUT OUT DAM AGED AREA ON CHANNEL. INSTALLED A SPLICE OVER THE CHANNEL WITH FILLER. (K) 2 H 7 2 4T RT A53EU 20081120 NE 2008 11 20 MU12008F00004 2 20081022 A 7220 ACOUSTIC PANEL AIRBUS 330 A330243 3930330 EU RROYCE RB211 RB211TRENT77 NE ENGINE DAMAGED B MU1Z K NONE O OTHER IN INSP/MAINT 1 SO 23 948AC 0948 ENGINE FOREING OBJECT DAMAGE. MX REPORT DURING TRANSIT CHECK IN BOG ENG N1 WAS FOUND FOD EVIDENCE. BOROSCOPIC INSPECTI ON ON HP AND HI COMPRESSOR IAW TASK 72-00-00-200-812 AND PENETRANT LIQUID INSPECTION ON LEADING EDGE OGV IAW TASK 70-20- 02-230-804. NO DAMAGES WERE FOUND. IAW AMM TASK 72-21-41-000-803 2 ICE IMPACT/REAR ACOUSTIC PANELS WERE REPLACED. IAW AMM TASK 72-21-41-400-802. 5 OGV ANNULUS FORMER PANELS WERE REPLACED. 2 L 7 2 4F 4 F RT A46NM E39NE 20081121 NM 2008 11 21 DL757081582 1 20081117 A 5311 141N13217 FRAME BOEING 757 757232 1384965 NM BS 395 S11L GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 DURING HMV, TWO GOUGES WERE FOUND IN THE WEB OF THE STA 395 FRAME BETWEEN S11L AND S13L. A NEW FRAME SECTION WAS SPLICE D IN BETWEEN S10L AND S11L PER BOEING REPAIR INSTRUCTIONS. 2 L 7 2 4F RT A2NM 20081121 CE 2008 11 21 GUUA11050801 1 20081105 A 5210 1294000321 DOOR BEECH 1900 1900D 1154162 CE PAX DOOR MALFUNCTIONED A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 81536 UE152 FLIGHT 9181 PNS/TPA - PILOT REPORTED CABIN DOOR EXTREMELY DIFFICULT TO CLOSE FROM INSIDE CABIN. CLOSED DOOR PROPERLY MU LTIPLE TIMES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081121 CE 2008 11 21 GUUA11160801 1 20081116 A 3230 LANDING GEAR BEECH 1900 1900D 1154162 CE MALFUNCTIONED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 29 87557 UE246 FLIGHT 9260 MIA/TPA - PILOT REPORTED NOSE LANDING GEAR TAKES EXTREMELY LONG TIME TO RETRACT AND EXTEND. PERFORMED LANDI NG GEAR SYSTEM OPERATIONAL CHECK. NO DEFECTS NOTED. 2 L 7 2 4T RT A24CE 20081121 CE 2008 11 21 GUUA11170801 1 20081117 A 2910 HYDRAULIC SYSTEM BEECH 1900 1900D 1154162 CE CONTAMINATED A GUUA O OTHER O OTHER AP APPROACH 1 SO 29 87557 UE246 FLIGHT 9193 FLL/TLH - DURING APPROACH TRIED TO EXTEND THE LANDING GEAR AND THE LANDING GEAR CIRCUIT BREAKER POPPED. RES ET THE CIRCUIT BREAKER AND THE GEAR EXTENDED. CONTINUED TO TLH LANDED WITHOUT INCIDENT. INSPECTED THE LANDING GEAR SYS TEM BLED AIR FROM THE SYSTEM. PERFORMED LANDING GEAR EXTENSION AND RETRACTION. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081121 CE 2008 11 21 GUUA11100801 1 20081110 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 49543 UE181 AT SCHEDULED INSPECTION DISCOVERED EXFOLIATION AT LOWER FUSELAGE SKIN AT FS 250.750 STRINGER 15L. REMOVED DAMAGED SKIN AND INSTALLED REPAIR DOUBLER PER BEECH STRUCTURAL REPAIR MANUAL 51-70-06. 2 L 7 2 4T RT A24CE 20081121 NM 2008 11 21 SWAA086307 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 2L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086308 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 4L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086309 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 5R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086301 1 20081118 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086302 1 20081118 A 5322 6546546 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086293 1 20081118 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B, STR 4R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086294 1 20081118 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086295 1 20081118 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086311 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 4R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086312 1 20081118 A 3350 101073 HOUSING BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR EMERGNECY EXIT LIGHT HOUSING BROKEN. REMOVED AND REPLACED LIGHT HOUSING PER M M. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086313 1 20081118 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, STR 10R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086327 1 20081115 A 3350 65C28060 LENS BOEING 737 7373T5 1384608 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 694SW 23061 DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE LIGHT LENS MISSING AT ROW 4. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086328 1 20081118 A 3350 411A2212 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 708SW 27842 DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR EGRESS LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086285 1 20081118 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND SHEAR TIE CRACKED AT BS 420, RBL 5. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086310 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 4R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 2008 11 21 DL76G081506 4 20081106 A 3416 ALTIMETER BOEING 767 767332 1382001 NM COCKPIT MALFUNCTIONED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 173DZ 29692 ATB - DUE TO ALTIMETER SPLITS. 2 L 7 2 4F RT A1NM 20081121 NM 2008 11 21 DL757081509 1 20081107 A 5320 146N5432 STIFFENER BOEING 757 757232 1384965 NM BS 333 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 P1191* TOOLING MARKS ON STIFFENER AT STATION 333 RBL 5. REPLACED STIFFENER ON NR 00073 PER 51-40-02 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081512 1 20081107 A 5312 BAC1505100581 FLOOR PANEL BOEING 757 757232 1384965 NM CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 652DL 24392 AFT CARGO BAY FLOOR PANEL SPLICE CORRODED. REPAIRED BY REPLACEMENT PER 51-40-02 ON NR 00034. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081513 1 20081107 A 5321 146N5431 FLOOR PANEL BOEING 757 757232 1384965 NM BS 1510-1535 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 652DL 24392 P1191* STATION 1510 TO 1535 FLOOR PANEL CORRODED. REPAIRED ON NR 00035 PER 53-00-53. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081514 1 20081107 A 5313 BAC15172226 STRINGER BOEING 757 757232 1384965 NM BS 1468 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 652DL 24392 P1191* STRINGER CORRODED AT 1468 RBL 11. REPAIRED PER 53-00-53 ON ATS NR 00095. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081515 1 20081107 A 5320 145N5335 WEB BOEING 757 757232 1384965 NM BS 596 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 652DL 24392 FWD CARGO WEB CRACKED AT STATON 596 LBL 3. REPAIRED PER 53-20-02 ON ATS 00046. 2 L 7 2 4F RT A2NM 20081121 2008 11 21 DL76G081517 4 20081107 A 2330 RECEPTACLE BOEING 767 7673P6 1385105 NM AUDO SYSTEM DAMAGED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 27 155DL 25269 ACRID ODOR AY SEAT 2A AND 2B. FOUND AUDIO JACK AT SEAT 2B EXTREMELY HOT AND PARTIALLY MELTED. REPLACED AUDIO JACK, NO HEAT AND AUDIO OPS CK GOOD. AUDIO QUARANTINE PER TOPP 20-60-02. 2 L 7 2 4F RT A1NM 20081121 NM 2008 11 21 DL757081519 1 20081108 A 5321 654H02441033 FLOOR PANEL BOEING 757 757232 1384965 NM BS 1510-1538 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 AFT CARGO BAY AT STATION 1510 - 1538 LBL 17 FIXED FLOOR PANEL CORRRDED. REPAIRED ON NR 00033 PER 53-20-02. 2 L 7 2 4F RT A2NM 20081121 EU 2008 11 21 MALA080191 1 20081111 A 5320 ANGLE SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 340B427 SIX CHAFE SPOTS FOUND ON CABIN FRAME INNER FLANGES OR INNER FLANGE REINFORCEMENT ANGLES. REPAIRED IAW EO NR S53635 AND S53152. 2 L 7 2 4T RT A52EU 20081121 EU 2008 11 21 MALA080192 1 20081114 A 5753 SKIN SAAB SF340 340B 7860101 EU LT WING TE FLAP DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 340B427 SEVEN DENTS NOTED IN THE LT FLAP UPPER SKIN PANEL 541AT. REPAIRED IAW EO NR S57231. 2 L 7 2 4T RT A52EU 20081121 EU 2008 11 21 MALA080193 1 20081109 A 5310 PANEL SAAB SF340 340B 7860101 EU FUSELAGE DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 340B427 DENT NOTED IN PANEL 193AL. REPAIRED IAW EO NR S51031. 2 L 7 2 4T RT A52EU 20081121 EU 2008 11 21 MALA080194 1 20081112 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297-330 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 340B427 REPLACED FWD SEAT TRACK SPLICE BETWEEN STA 297 AND STA 330, LBL18.3 DUE TO CORROSION. REPAIRED IAW EO NR S53060. 2 L 7 2 4T RT A52EU 20081121 NM 2008 11 21 UALA2008111305497 1 20080826 A 3350 LENS BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 675UA 29243 OVERWING EMERGENCY LIGHT LENS MISSING. LENS OUT OF POSITION. REPLACED MISSING LENS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081121 NM 2008 11 21 DHLA2008745680 1 20081111 A 5312 BULKHEAD BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 NLG W/WELL TORQUE BOX AREA, BULKHEAD WEB AT BS 351.2 CORRODED BETWEEN LBL 2 AND LBL 4, WL 169. ACCOMPLISHED REPAIR TO W EB PER COOPESA EO COO-2-53-389-08 DATED 10/28/2008. REF FAA FORM 8110-3 DATED 11/6/2008 AND ASTAR EVA B253-00165 FOR RE PAIR APPROVAL. DOCUMENTED ON COOPESA N/R 1-687. 2 L 7 3 4F A3WE 20081121 NM 2008 11 21 UALA2008111305512 1 20080829 A 3510 B-NUT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CREW O2 LOOSE A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 335UA 24230 CREW O2 AT 1550 PSI AND DROPPING. FOUND LOOSE B-NUT. FOUND AND REPAIRED THREE LEAKS ON HIGH PRESS SIDE. REPLACED 90 D EGREE ELBOWS AT BOTH ENDS OF HARD LINE FROM CROSS FITTING TO FILL VALVE. SECURED LEAKING B-NUT AT CROSS FITTING TO STEP DOWN REG SVCED SYSTEM. OPENED AND SAFTIED BOTTLE VALVE. SYSTEM WAS SERVICED TO 1800 PSI & RECHECKED WITH NO LOSS OF P RESSURE FOUR HOURS LATER. 2 L 7 2 4F 4 F RT A16WE E21EU 20081121 WP 2008 11 21 08FDEA04908 1 20081118 A 5310 AEA01122 DOOR FRAME DOUG DC10 DC1030F 3023504 WP ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 MAIN CABIN FOUND A CRACK ON WEB JAMB DOOR. 2 L 7 3 4F RT A22WE 20081121 NM 2008 11 21 08FDEA04909 1 20081118 A 5315 FLOORBEAM BOEING 757 75723A 1384967 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 CABIN FLOORBEAM STA 1661, LBL 58 TO RBL 58 HAS CORROSION AT SEVERAL PLACES. REMOVED AND REPLACED FLOORBEAM UPPER CAP AT STA 1661 LABL 58-RBL 58 IAW SRM 51-40-02, MAJOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED. 2 L 7 2 4F RT A2NM 20081121 WP 2008 11 21 AALA200810146 1 20081029 A 5330 SKIN DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 CRACK IN FUSELAGE SKIN BELOW AIRSTAIR DOOR. CUTOUT CRACK, INSTALLED DOUBLER PER ESO 80559 DATED 10/21/08 AND DRAWING NR SR09530219. 2 L 7 2 4F A6WE 20081121 WP 2008 11 21 AALA200810147 1 20081029 A 5311 FRAME DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 CORROSION IN AFT CARGO COMPARTMENT AT STATION 1309 FRAME AFT SIDE AT LONGERON 29R TO 30. REMOVED CORROSION AND INSTALLE D DOUBLER PER AARD 53-10-00-14 FIG 1. 2 L 7 2 4F A6WE 20081121 NM 2008 11 21 08FDEA04918 1 20081118 A 5730 654N0244466 SKIN BOEING 757 75723A 1384967 NM ZONE 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 PREVIOUSLY INSTALLED REPAIR, WS 823, WBL 740, TANK INTERNAL, RT WING, LOWER SURFACE, IDENTIFIED AS A TIME-LIMITED REPA IR. COMPLY WITH ATTACHMENT "B" OF EO F-5100-7-5100, PART 1. COMPLIED WITH ATTACHMENT "B" OF EO F-5100-7-5001, PART 1. REPLACED RT WING, LOWER SKIN, P/N 654N0244-466, AT WS 823, WBL 740, IAW SRM 51-40-02 AND DWG 12N4501, 112N4106, 112N200 1, 112N1660 AND 112N5026. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 AALA200810157 1 20081023 A 5340 BOSS BOEING 737 737823 13844BZ NM ZONE 100 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 HOLES DRILLED INTO TIE DOWN BOSS. REPLACED THE SECTION OF FLOOR BOARD SUPPORT FROM STATION 727F + 11" TO 727F +10 RBL14 PER SRM 53-00 AND 53-02. 2 L 7 2 4F RT A16WE 20081121 WP 2008 11 21 AALA200810124 1 20081022 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 CORROSION ON NR 3 SEAT TRACK AT STATION 302 TO 306. INSTALLED PLUG PER AARD 53-20-00-10. 2 L 7 2 4F A6WE 20081121 NM 2008 11 21 AALA200810161 1 20081030 A 5315 FLOORBEAM BOEING 737 737823 13844BZ NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 CORROSION ON FLOORBEAM, FRAME 986 AT RBL43. INSTALLED "T" CAP REPAIR PER SRM 53-70-51 FROM RBL2 TO RBL49. 2 L 7 2 4F RT A16WE 20081121 WP 2008 11 21 AALA200810125 1 20081022 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 CORROSION ON NR 1 SEAT TRACK AT STATION 307. INSTALLED REPAIR PLUG PER AARD 53-20-00-10. 2 L 7 2 4F A6WE 20081121 EA 2008 11 21 COMA0860428 1 20081009 A 5320 STIFFENER CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 436CA 7482 OTBD LBL 9 VERTICAL STIFFENER AT FS 559 IS CRACKED ON LOWER SIDE. REPAIRED OTBD VERTICAL POST AT LBL 9 PER REO 601R-53- 41-057. 2 L 7 2 4F RT A21EA 20081121 EA 2008 11 21 COMA0860429 1 20081009 A 5320 WEB CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 436CA 7482 FS 559 WEB AND CAP ANGLES, FOUND LT SIDE CAP ANGLE CRACKED UNDER POSTS AT LBL 18. REPAIRED PER REO 601R-53-41-793. 2 L 7 2 4F RT A21EA 20081003 NM 2008 10 3 SWAA085274 1 20080928 A 5322 6516323 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085275 1 20080928 A 5322 6516323 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 360 BETWEEN STR 27L TO STR 28L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085276 1 20080928 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 325SW 23689 DURING SCHEDULED 18Y CHECK, FOUND AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085277 1 20080929 A 5310 6545815 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND R1 DOOR AFT CUTOUT FRAME CRACKED AT SECOND STOP FITTING. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081003 2008 10 3 SWAA085289 4 20080929 A 2565 D31354 SLIDE BOEING 737 737301 1384611 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 659SW 23229 FOUND R2 DOOR EMERGENCY EXIT ESCAPE SLIDE SIGHT GAUGE OUT OF POSITION. POSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085291 1 20080928 A 3350 100031 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED MV3 CHECK, FOUND R1 EMERGENCY EXIT LOWER LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085292 1 20080930 A 3350 079123 LENS BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 255WN 32513 FOUND FIRST ROW EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20081006 NM 2008 10 6 AALA200802026 1 20080805 A 2120 UNKNOWN BOEING 757 757223 1384957 NM CABIN SMOKE A AALA G A O2 MASK DEPLOYED UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 192AN 32386 LAX INFLIGHT T31/05AUG. CREW REPORTED SMOKE FILLING CABIN. DROPPED OXYGEN MASKS. RETURNED TO LAX AND LANDED WITHOUT I NCIDENT. DEPLOYED SIX SLIDES FOR EMERGENCY EVACUATION. FLIGHT ATTENDANTS REPORTED RT NR FOUR DOOR WOULD NOT COMPLETELY OPEN. FERRIED AIRCRAFT TO TUL FOR EVALUATION AND REPAIR OF RT NR FOUR DOOR. INSPECTED DOOR RIG AND POWER ASSIST SYSTE M. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20081006 WP 2008 10 6 AALA200802007 1 20080731 A 2410 696233B CSD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LT ENGINE INOPERATIVE A AALA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER UK UNKNOWN 1 SW 21 7531A 49923 709980 ELP INFLIGHT T1540/31JUL TUS TO DFW. CREW REPORTED LT GENERATOR CLICKED OFF AND ON SEVERAL TIMES. UNABLE TO DISCONNEC T CONSTANT SPEED DRIVE. SHUT DOWN NR 1 ENGINE AND LANDED ELP WITHOUT INCIDENT. ENGINE WINDMILL TIME 15 MINUTES. SYSTE M GROUND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F 4 F A6WE E9NE 20081006 NM 2008 10 6 USAA920081585 1 20080826 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 23885 PIT MAJOR REPAIR FPBH INSP NR 4352158. 0.5" CRACK VERTICAL BEAM WEB, AT BS178, WL227, RBL17. REPAIRED BEAM AT BS178, WL 227, RBL17. IAW SRM 53-10-08 FIG. 201 DETAIL 6. 2 L 7 2 4F RT A16WE 20081006 NM 2008 10 6 USAA920081601 1 20080830 A 5753 6546431279 FLAP BOEING 737 737401 1384701 NM LT WING DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 23876 CLT C5 MAJOR REPAIR NR 03C10025001/002 LT HAND OUTBOARD FORE FLAP DELAMINATED. REPLACED LT HAND OUTBOARD FORE FLAP IAW B737 SRM 57-53-01 & B737 AMM 27-51-37. 2 L 7 2 4F RT A16WE 20081006 NM 2008 10 6 USAABB08143 1 20080830 A 2751 60231002 ACTUATOR BOEING 767 7672B7 1385107 NM LT SPOILER DEFECTIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AY 76507 25257 PHL THE LT SPOILER OVER RIDE ACTUATOR WAS FOUND WITH OIL INSIDE. MX REPLACED THE LT SPOILER OVER RIDE ACTUATOR. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20081006 NM 2008 10 6 QXEA200800406 1 20080418 A 5313 STRINGER DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK CORROSION ON STR 23S (X387 TO X392) AND CONNECTING CLIP TO FRONT SPAR MAIN FRAME ON AFT SIDE AT X387.35. R EMOVED LIGHT SURFACE FROM STRINGER AND CONNECTING CLIP USING SCOTCH BRITE PAD. ALODINED EXPOSED ALUM. IAW -8 200 CPM CH AP 4 AND 5. NEGLIGIBLE MATERIAL REMOVED. PRIMED IAW 51-20-36PG 6 PARA F1. 2 H 7 2 4T RT A13NM 20081006 NM 2008 10 6 QXEA200800415 1 20080418 A 5320 FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK FITTING CORRODED JUST AFT OF CARGO DOOR FUSELAGE CUTOUT, LOWER AFT CORNER. REMOVED CORRODED FITTING AT AF T LOWER CORNER IAW -8 200 SRM 51-40-11. INSTALLED NEW FITTING IAW -8 200 SRM 51-40-11 AND RD8-51-102. 2 H 7 2 4T RT A13NM 20081006 CE 2008 10 6 YRR2008F00000 1 20080903 A 2121 78008013 BLOWER LEAR 60 60LEAR 5170707 CE PWC PW306 PW306A 52165 NE CABIN AIR FAILED B YRRR A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 05 360AN 7236 137 THE ACFT WAS LEVELING OFF AT CRUISE ALTITUDE OF FL400 AFTER DEPARTING AND ENROUTE, WHEN THE CREW NOTED THE ODOR OF SMOKE AND SMOKE COULD BE SEEN COMING FROM THE AFT SECTION OF THE CABIN. THE CREW DECLARED AN EMERGENCY AND BEGAN A DESCENT W HILE COMPLETING THE EMERGENCY CHECK LIST. ATC THEN GAVE THE CREW VECTORS TO WHERE AN UNEVENTFUL LANDING WAS MADE WITH F IRE CREWS STANDING BY. THE CREW NOTED THAT DURING THE DESCENT AT FL250 THE SMOKE HAD DISSIPATED FROM THE CABIN. AFTER T HE LANDING THE ACFT WAS INSPECTED AND THE CREW DETERMINED THERE WAS NO FIRE AND TAXIED THE ACFT TO A STANDING AREA FOR F URTHER INSPECTIONS WERE CARRIED OUT FOR PROBABLE CAUSE OF SMOKE AS WELL AS AN INSPECTION FOR OVERWEIGHT LANDING. THE CAU 2 L 7 2 4F 4 F RT A10CE E35NE 20081006 WP 2008 10 6 U2R2008F00008 1 20080825 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP BS 560 CRACKED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 872SJ 83402 46040 DURING C-CHECK INSP, FOUND LWR CARGO COMPARTMENT, STA 560.000 RT CUSP EXTRUSION WITH 2 INCH CRACK. (K) 2 L 7 4 4F RT 4A25 20081006 CE 2008 10 6 GUU2008F00045 1 20080826 A 5210 12951405933 CABLE BEECH 1900 1900D 1154162 CE PAX DOOR BROKEN A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87554 UE227 PILOT REPORTED UNABLE TO OPEN CABIN DOOR, FOUND UPPER FWD DOOR CABLE BROKEN. REPLACED UPPER FWD DOOR CABLE. (K) 2 L 7 2 4T RT A24CE 20081006 EA 2008 10 6 TRAX200801060 1 20080826 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 857AS 7411 LT OVER WING EMERGENCY LIGHT INOP. RELAMPED LT OVER WING EMERGENCY LIGHT IAW CRJ200AMM 33-51-21. OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 20081006 CE 2008 10 6 GUU2008F00046 1 20080825 A 5210 CAM BEECH 1900 1900D 1154162 CE PAX DOOR OBSTRUCTED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87557 UE246 CABIN DOOR RT SIDE SECOND CAM FROM TOP IS RUBBING ON CAM LOCK MAKING DOOR HARD TO OPEN AND CLOSE. CLEANED EXCESSIVE GREA SE AND GUM OUT OF CAM. (K) 2 L 7 2 4T RT A24CE 20081006 SO 2008 10 6 C2XA08IA195 1 20080819 A 3350 78241 BALLAST EMB 145 EMB145EP 3260221 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13929 145009 LCH DURING MX INSPECTION THE OVERWING CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX R&R THE NR 6 EMERGENCY LI GHT BALLAST, OPS CHECK WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20081006 SW 2008 10 6 WGE2008F00002 1 20080902 A 2697 WIRE ECLIPS EA500 ECLIPSEEA500 3350000 SW OVERHEAT SENSOR DAMAGED D WGEA K NONE O OTHER IN INSP/MAINT 1 EA 27 141DJ 000055 REPAIRED FIRE OVERHEAT SENSOR HIGH WIRE ENGINE R0612-22 IAW EA 500 WIRING REPAIR MANUAL SECTION 3.27 FOR OPS CHECK C/W F IRE DETECTION WIRE ADJUSTMENT/ TEST IAW EA500, AMM 26-10-00-071-801. OPS CHECK GOOD. REFERENCE LOG PAGE 0875, DIS NR 2. (K) 1 L 7 2 4J RT A00002AC 20081006 NM 2008 10 6 KNN2008F00000 1 20080822 A 2731 BOLT BOEING 737 737232 1384475 NM TRIM TAB HINGE WORN A KNNA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 25 326DL 23098 IN FLIGHT AGGRESSIVE VIBRATION FELT AT VARIOUS AIRSPEEDS 190 KTS-290 KTS, ALTITUDE STARTING AT 10,300 FT NOT RELENTING U NTIL WELL BELOW 190 KTS. (K) 2 L 7 2 4F RT A16WE 20081007 SO 2008 10 7 CHQ2008F00005 1 20080831 A 3350 LIGHT EMB 135 EMB135KL 3260302 SO ALLSN AE3007 AE3007A 03030 GL CABIN MALFUNCTIONED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 297SK 145522 CAE311245 2 FLOOR LEVEL LIGHT STRIPS WERE REPORTED TO NOT ILLUMINATE WHEN TESTED. MX OPS CHECKED THE LIGHTS IN ACCORDANCE WITH EM B AMM 33-50-00 WITH NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081007 EU 2008 10 7 MAL2008F00030 1 20080822 A 5210 SKIN SAAB SF340 340B 7860101 EU PAX DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 402XJ 340B402 5 DENTS IN PAX DOOR OUTER SKIN. DENTS NR 1, 2, 3, 4 ARE ACCEPTED AS IS AND DENT NR 5 WAS REPAIRED. 2 L 7 2 4T RT A52EU 20081007 NM 2008 10 7 USAA920081584 1 20080827 A 5320 146N873815 WEB BOEING 757 7572G7 1384963 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 909AW 24522 MCN C3 MAJOR REPAIR NR 6122889 WEB CRACKED AT BS 1620 S10L. REPLACED WEB AT BS 1620 S10L IAW SRM 51-40-02-OG. 2 L 7 2 4F RT A2NM 20081007 CE 2008 10 7 DXTA200803255 1 20080830 A 2741 WARNING SYSTEM CESSNA 560 560XL 2076702 CE COCKPIT ACTIVATED E DXTA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 689QS 5605659 DURING APPROACH LOWERED FLAPS TO 15` AND STAB MISCOMPARE CAUTION LT ILLUMINATED. 2 L 7 2 4F RT A22CE 20081007 NM 2008 10 7 KCSA081423 1 20080827 A 5330 SKIN BOEING 747 747249F 1384849 NM FUSELAGE CHAFED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 EXTERNAL FUSELAGE SKIN IS CHAFFED AT STA 990, STR 39R. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081439 1 20080902 A 5314 ATTACH BRACKET BOEING 747 747122 1384872 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 KEELBEAM ATTACH BRACKET CRACKED AT BS 1267, RBL-9, WL-116. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081442 1 20080903 A 5320 TENSION TIE BOEING 747 747122 1384872 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STA-1740 ABOVE STR-36L FRAME TENSION TIE DENTED. 2 L 7 4 4F RT A20WE 20081007 EA 2008 10 7 MAS2008F00068 1 20080821 A 5270 PROXIMITY SWITCH CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR OUT OF ADJUST A MASA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 07 715SF 7115 ASH FLT 7319 IAD-CLT-SAV. PAX DOOR OUTER HANDLE CAUTION MESSAGE IN FLIGHT. MX ADJUSTED PROX SWITCH PS1MB. OPS CHECK G OOD. 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 MAS2008F00070 1 20080822 A 4930 69254517 SOLENOID VALVE CNDAIR CL600 CL6002B19 1900309 EA APU DEFECTIVE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 77181 122 7181 ASH FLT 7168 GRB-ORD. FUEL SMELL IN FLIGHT DECK ON GROUND IN ORD. MX REPLACED FUEL SOL VALVE. 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 MAS2008F00071 1 20080821 A 5270 WARNING SYSTEM CNDAIR CL600 CL6002B19 1900309 EA COCKPIT ACTIVATED A MASA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 07 75994 7367 ASH FLT 7185 IAD-CLE. RT OVERWING EMERGENCY EXIT CAUTION MSG IN FLIGHT. MX CHECKED THE DOOR SENSORS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 MAS2008F00077 1 20080823 A 5270 PSEU CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A MASA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 07 75994 7367 ASH FLT 7202 IAD. PAX DOOR WARNING MESSAGE AND PAX DOOR OUTER HANDLE CAUTION MESSAGE IN FLIGHT. MX R&R PSEU AND PERFOR MED RIGGING AND INSPECTION OF DOOR. NO DEFECTS NOTED. 2 L 7 2 4F RT A21EA 20081007 SO 2008 10 7 RAIA00808024 1 20080824 A 2133 2097K011100 OUTFLOW VALVE EMB 145 EMB145LR 3260212 SO CABIN PRESSURE MALFUNCTIONED A RAIA K NONE O OTHER CL CLIMB 1 CE 03 829HK 15973 145281 FLT NR 5500 STL DURING CLIMB ACFT AUTO AND MANUAL PRESSURIZATION FAILED. MX R&R THE DIGITAL CONTROLLER. OPS CHECKED GO OD ON THE GROUND. 2 L 7 2 4T RT T00011AT 20081007 NM 2008 10 7 ASM2008F00004 1 20080909 A 5730 112N61012 ACCESS PANEL BOEING 737 737* NM RT FUEL TANK LEAKING W ASMF O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 23 852AM 33787 DURING WALK AROUND CAPTAIN FOUND A FUEL LEAK UNDER THE RIGHT WING AND ENGINE FUEL DRAIN. MAINT CONFIRMED THE FUEL LEAK T HEN REMOVED AND REPLACED MAIN TANK RIGHT WING ACCESS PANEL SEAL. 112N51012, DOOR ASSY ON RIGHT SIDE AND TESTED IAW MM 2 8-11-11M ALL CORRECT. (K) 2 L 7 2 4F RT A16WE 20081007 EA 2008 10 7 TRAX200801082 1 20080822 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 970EV 7527 JOB 8752721 OPERATION 239. FLOORBEAM OTBD FLANGE AT FS 574 TO FS 621, LBL 27 HAS CORRODED NUTPLATE HOLES. REMOVED FILL ER STRIP TO ACCESS BEAM CAP REMOVAL IAW CRJ 200 SRM 51-41-02. REMOVED HARDWARE. 7 BOLTS FROM LT ELEV PULLEY BRACKET JU ST FWD OF FS 621 BULKHEAD TO ALLOW MOVEMENT OF PULLEY BRACKET. CABLES WERE NOT DETENSIONED. REMOVED FLOORBEAM CAP AT L BL 27 BETWEEN FS 621 AND 574 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. OK TO INSTALL LBL 27 FS 574-621. 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 TRAX200801084 1 20080828 A 5230 FITTING CNDAIR CL600 CL6002B19 1900309 EA CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 932EV 8016 JOB 8801621 OPERATION 230 AFT LOWER CLIP ON CARGO DOOR SUPPORT BEAM IS CRACKED AT FS 621. RESOLVED ON W/O 98367 TASKCAR D NR 00329. C/A R&R CRACKED LOWER AFT CLIP FROM CARGO DOOR SUPPORT BEAM WITH NEW PART IAW CRJ 200 SRM 5J1-42-21. 2 L 7 2 4F RT A21EA 20081007 NM 2008 10 7 P5CA0801575 1 20080831 A 3600 SHUTOFF VALVE BOEING 747 74746NF 13848BT NM GE CF6 CF680 30025 NE NR 1 ENGINE DEFECTIVE A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 15 452PA 30810 NR 1 ENGINE AUTO START FAILED. TROUBLESHOT AND FOUND NR 1 PRSOV DEFECTIVE AMM36-11-04. (K) 2 L 7 4 4F 4 F RT A20WE E13NE 20081007 NM 2008 10 7 G8G2008F00001 1 20080611 A 7900 439563 FITTING BOEING 727 727223 1384074 NM BYPASS SWITCH FAULTY A G8GA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 29 708AA 22465 DURING CLIMB, THE NR 2 ENGINE LOW OIL PSI LIGHT ILLUMINATED AND OIL QUANTITY WENT TO EMPTY. THE NR 2 ENGINE WAS SHUT DOW N, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. POST FLIGHT INSPECTION FOUND OIL FILTER BYPASS SW ITCH GEARBOX FITTING AT FAULT. REPAIRED GEARBOX PERFORMED OPS AND LEAK CHECKS GOOD. NO OTHER DEFECTS. AIRCRAFT WAS RETUR NED TO SERVICE. (K) 2 L 7 3 4F A3WE 20081007 EA 2008 10 7 NW62008F00000 1 20080827 A 3397 CONNECTOR CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS LOOSE A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 160GJ 10239 EMERGENCY EXIT ROW LIGHT IS OUT ON SIDE 12 A/B INSPECTED, FOUND PIN ON POWER SUPPLY CONNECTOR BY ROW 10 TO BE LOOSE. RE SECURED PIN IAW SWPM 20-33-00. OPS CHECK GOOD IAW AMM 33-61-00. (K) 2 L 7 2 4F RT A21EA 20081007 EU 2008 10 7 NSV2008F00022 1 20080827 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY FALSE INDICATION A NSVA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 27 202SR 340B202 AVIONICS SMOKE LIGHT ILLUMINATED. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR (PN 72-111211-000) SN A4091, SN ON A5414 , DONE IAW 26-13-06-04, OPS CHECK GOOD. (K) 2 L 7 2 4T RT A52EU 20081007 NM 2008 10 7 QXEA200800426 1 20080418 A 5320 FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK. TENSION FITTING LOCATED AT FRAME X201 STR 31S HAS CORROSION. REMOVED TENSION FITTING AND INSTALLED NEW F ITTING IAW 8 200 SRM 51-40-11, 51-20-36. 2 H 7 2 4T RT A13NM 20081007 NM 2008 10 7 QXEA200800439 1 20080413 A 5713 FORMER BOMBDR DHC8 DHC8402 1390042 NM WING GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 412QX 4059 PDX C4 CHECK SEVERAL GOUGES ON OTBD SIDE OF LT LEADING EDGE FORMER AT APPROX STA YW 48. BLENDED GOUGES AND PREPPED AND PRIMED SURFACE IAW Q400 SRM 51-14-00 STEP 1-5.B4C. 2 H 7 2 4T RT A13NM 20081007 EA 2008 10 7 QXEA200800443 1 20080421 A 5210 ANGLE CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 608QX 10026 RFD C4 CHECK MINOR CORROSION ON PAX DOOR MID CAP ANGLE. REMOVED CORROSION ON PAX MID CAP ANGLE. REMOVED .002 INCH WITH IN LIMITS. IAW SRM 53-21-23. TREATED EXPOSED METAL AREAS IAW SRM 51-21-11 APPLIED EPOXY PRIMER TO AERA IAW SRM 51-25-0 6 APPLIED TOPCOAT IAW SRM 51-25-16. 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 QXEA200800554 1 20080502 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 613QX 10045 RFD C4 CHECK LT FS 280 LOWER BULKHEAD CORRODED. BLENDED CORROSION, ALL BLENDS WITHIN LIMITS, BLENDED .003 FROM LOWER BU LKHEAD IAW CRJ 700 SRM 53-11-10. ETCHED ALODINE PRIMED IAW CRJ 700 SRM 51-21-11 AND 51-25-06, APPLIED TOP COAT IAW SRM 51-25-01. 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 QXEA200800555 1 20080502 A 5312 BULKHEAD CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 613QX 10045 RFD C4 CHECK RT FS 280 LOWER BULKHEAD CORRODED. BLENDED CORROSION. BLENDED .003 MATERIAL FROM LOWER BULKHEAD IAW CRJ 7 00 SRM 53-11-10. ETCHED ALODINE PRIMED IAW CRJ 700 SRM 51-21-11 AND 51-25-06. APPLIED TOP COAT IAW SRM 51-25-01. 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 QXEA200800556 1 20080502 A 5320 ANGLE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 613QX 10045 RFD C4 CHECK FORWARD FS 280 CENTER FLOOR BOARD ANGLE CORRODED. REMOVED FWD CTR FLOOR BOARD ANGLE IAW CRJ 700 SRM 51-42- 06. LOCATED HOLES IN NEW ANGLE AND INSTALLED IAW CRJ 700 SRM 51-40-11, 51-23-02, 51-42-07 AND 51-42-14. 2 L 7 2 4F RT A21EA 20081007 NM 2008 10 7 AALA200802068 1 20080811 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 765AN 32879 DFW EMERGENCY LIGHT AT SEAT 21C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT T00001SE 20081121 NM 2008 11 21 USAA920081922 1 20080910 A 5312 65405409306 PRESSURE PANEL BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN C18 MAJOR REPAIR NR 6131676 MLG WW PRESSURE WEB CRACKED AT BS 663.75. WL204, LBL40. REPAIRED MLG WW PRESSURE WEB AT BS 663.75, WL204, LBL40 IAW US AIRWAYS EA NR 130128. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 USAA920081917 1 20081008 A 5522 SKIN BOEING 737 7374B7 138449C NM ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT MAJOR REPAIR Q5 CHECK NR 03C10000029/028, LT ELEVATOR UPPER SURFACE DELAMINATED, 3" FORWARD OF TRIM TAB CONTROL ROD CUT OUT. REPAIRED LT ELEVATOR UPPER SURFACE, 3" FORWARD OF TRIM TAB CONTROL ROD CUT OUT IAW US AIRWAYS EA 100676. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 USAA920081914 1 20081015 A 5311 6546551 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753039/005 FRAME CRACKED AT BS 807 ABOVE S9L. REPAIRED FRAME AT BS 807 ABOVE S9L IAW US AIR WAYS TYPICAL REPAIR NR 53-10-20. 2 L 7 2 4F RT A16WE 20081120 NM 2008 11 20 08FDEA04926 1 20081118 A 2750 FLAP SYSTEM DOUG MD11 MD11F 3023600 NM TE FLAPS STUCK A FDEA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 CE 21 579FE 48470 ACFT HAD AN ATB FOR FLAPS SLOW TO RETRACT AND ON GROUND FLAPS ARE STUCK AT 28 DEG. 2 L 7 3 4F RT A22WE 20081120 NM 2008 11 20 08FDEA04927 1 20081119 A 5313 65258111 STRINGER BOEING 727 7272D4 138407U NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 AFT PIT S27L LONGERON/FITTING HAS CORROSION AT BS 1130 REMOVED FASTENERS, REMOVED CORROSION, NDT (HFEC) BLENDOUT AREA AN D FASTENER HOLES. ALODINED AND CIC, D AREA. WITH NO LIMITS REF EA 7-5310-123810, THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081120 NM 2008 11 20 08FDEA04913 1 20081118 A 5311 651634363 FRAME BOEING 727 7272D4 138407U NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 AFT CARGO PIT STATION 1050 FUSELAGE FRAME DAMAGED AT STR 26L. REMOVED DAMAGE ON STA 1050 AT STR 26R. REF SRM 51-40-05 P G1 FABRICATED AND INSTALLED DOUBLER FOR FRAME. REF SRM 51-20-1 PG 1 SRM 51-30-02 PG 1-12 FABRICATED AND INSTALLED NEW EN D ATTACH ANGLE FOR INTERCOSTAL FWD OF 1050 AT STR 26L. REF. SRM 51-40-02 PG 1-6 SRM 51-30-02 PG 1-6. THIS IS CLASSIFIE D AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081120 GL 2008 11 20 CHQA200800216 2 20081105 A 7261 CARBON SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL NR 2 ENGINE LEAKING A CHQA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 278SK 19676 11223 145370 CAE311503 FLIGHT 5997, PHL TO CLE - DURING INITIAL CLIMB AT ABOUT 2,000 FT, THE FLIGHT CREW RECEIVED A LAVATORY SMOKE INDICATION. THE FLIGHT ATTENDANT REPORTED THAT THERE WAS A BURNING RUBBER ODOR COMING FROM THE BACK OF THE ACFT AND LAV. THE FLT R ETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE RAN THE ENGINES AND WAS UNABLE TO DUPLICATE THE FAULT AND THE LAV SMOK E INDICATION WAS DEFERRED. THE ACFT WAS THEN FERRIED TO CLE FOR AN UNRELATED MAINTENANCE ISSUE AND FURTHER TROUBLESHOOT ING WAS PERFORMED. DURING ENGINE RUNS THE ODOR OF OIL WAS NOTED WHEN OPERATING ON THE E2 BLEED SYSTEM. E2 WAS THEN INS PECTED FOR LEAKAGE OF THE ZERO CARBON SEAL WITH NO LEAKS NOTED. THE AIRCRAFT WAS THEN FERRIED TO CMH FOR FURTHER TROUBL 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081120 NM 2008 11 20 DL757081493 1 20081105 A 5330 453N761127 PANEL BOEING 757 757232 1384965 NM BS 1470 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 AFT CARGO BAY STATION 1470 PANEL SPLICE HAD SURFACE CORROSION. REPAIRED ON NR 00051 PER 53-00-53. 2 L 7 2 4F RT A2NM 20081120 NM 2008 11 20 USAA920081938 1 20081021 A 5311 6546558 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753039/007 FRAME CRACKED AT BS907 JUST ABOVE S9L. REPAIRED FRAME AT BS907 JUST ABOVE S9L IA W US AIRWAYS TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 20081120 NM 2008 11 20 USAA920081925 1 20081002 A 3397 W15006722 WIRE BOEING 737 7373G7 138447J NM CABIN DAMAGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 308AW 24710 SAL C17 EEL NR 6092122 EMERGENCY OVERWING LIGHT RT SIDE DOESN`T COME ON. REPAIRED ELECTRICAL WIRING BUNDLE WL 50-067-22 IAW B737 WSPM 20-10-13 AND WDM 33-51-21. 2 L 7 2 4F RT A16WE 20081120 NM 2008 11 20 USAA920081940 1 20081020 A 5311 65C25230 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753039/004 FRAME CRACKED AT BS727E JUST ABOVE S9L. REPAIRED FRAME AT BS727E JUST ABOVE S9L IAW US AIRWAYS TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 20081120 EU 2008 11 20 USAA920081930 1 20080926 A 5320 D53480054223 FITTING AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C7 MAJOR REPAIR NR 6062336 CORROSION ON SHEAR TEAR CLIP AT FR65 BETWEEN S43L AND S43R. REPLACED SHEAR TEAR CLIP AT FR65 BETWEEN S43L AND S43R IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081120 NM 2008 11 20 DL757081494 1 20081105 A 5320 143N5366Y54 SUPPORT BOEING 757 757232 1384965 NM BS 620 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 CORROSION AT FLOOR TO SIDE WALL SUPPORT BS 620 AT RBL 23. REPIARED ON NR 00061 PER 51-40-02. 2 L 7 2 4F RT A2NM 20081120 NM 2008 11 20 DL757081495 1 20081105 A 5320 453N161123 SPLICE BOEING 757 757232 1384965 NM BS 1510 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 AFT CARGO BAY STATION 1510 PANEL SPLICE CORRODED. REPAIRED ON NR CARD 00037 PER 53-00-53. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081539 1 20081011 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 350-365.25 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 MAIN CABIN BL "0" FLOORBEAM STRAP STA 350-365.25 MULTIPLE SPOTS CORRODED. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-40- 02. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081555 1 20081115 A 5320 140N35051 ANGLE BOEING 757 757232 1384965 NM BS 660 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 FOUND UPPER WEB ANGLE CRACKED WL 208, BS 660 RBL 24. 2 L 7 2 4F RT A2NM 20081007 NM 2008 10 7 AALA200802066 1 20080810 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 DFW EMERGENCY LIGHT AT SEAT 25D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081007 NM 2008 10 7 AALA200802063 1 20080810 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 760AN 31477 DFW EMERGENCY LIGHT AT SEAT 26G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081007 NM 2008 10 7 AALA200802060 1 20080809 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW EMERGENCY LIGHT AT SEAT 40G MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 40G. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081007 NM 2008 10 7 AALA200802059 1 20080809 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW EMERGENCY LIGHT AT SEAT 40G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 40G. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081007 NM 2008 10 7 AALA200802057 1 20080809 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW EMERGENCY LIGHT AT SEAT 36C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 36C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802046 1 20080809 A 3350 BPS73 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 391AA 27451 JFK EMERGENCY LIGHT AT OVERHEAD SEAT ROW 20B INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT OVERHEAD ROW 20B . SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081008 NM 2008 10 8 SPA2008F00003 1 20080917 A 3350 110049 POWER SUPPLY BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15 52051 NE EMERGENCY LIGHT FAILED A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 07 712S 23038 LOWER EMERGENCY EXIT LIGHTS AT DOORS L2 AND R2 WILL NOT ILLUMINATE. REPLACED POWER SUPPLY IAW MM 33-21-27. FUNCTIONAL C HECK SATISFACTORY. (K) 2 L 7 2 4U 4 F RT A16WE E2EA 20081008 NM 2008 10 8 AALA200802041 1 20080808 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 772AN 29580 MIA EMERGENCY LIGHT AT LT NR 1 DOOR BROKEN. REPLACED LIGHT ASSEMBLY AT LT NR 1 DOOR FOR INOPERATIVE EMERGENCY LIGHT. S YSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802037 1 20080806 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 199AN 32393 LAX SEAT MOUNTED EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK M10801 FOR INOPERATIVE EMERGENCY LIGH TS AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 EU 2008 10 8 RMX2008F00003 1 20080923 A 5330 1172250401 SKIN BOLKMS 117 BK117A4 5626017 EU FUSELAGE DAMAGED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 171MU 9946 7138 DURING A SCHEDULED INSPECTION, 3 AREAS OF THE PRIMARY FUSELAGE SKIN HAD CORROSION DAMAGE THAT WAS COMPLETELY THROUGH THE SKIN THICKNESS. DAMAGE AREA WAS APPROX 1 SQ INCH AT EACH DAMAGE LOCATION. THE AREAS WERE LOCATED AT : 1 EA AREA UNDER T HE REFUELING GROUND CLIP LT FUSELAGE SKIN AT STA 5100MM, WL 1600MM. 2EA AREAS; ONE ON BOTH LT AND RT FUSELAGE SKINS AT T HE AFT ENGINE COWLING LATCH PLATE. FUSELAGE STA 5800 MM, WL 2600 MM. (K) 1 G 7 2 3U H13EU 20081008 NM 2008 10 8 KCS2008F00008 1 20080914 A 5320 ANGLE BOEING 747 747122 1384872 NM BS 1352 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STA 1352, RBL125, WL 118 ANGLE CORRODED. (K) 2 L 7 4 4F RT A20WE 20081008 NM 2008 10 8 KCS2008F00009 1 20080914 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2678 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FASTENER HEAD MISSING AND SKIN CRACKED UPPER AFT CORNER OF APU INLET OPENING. (K) 2 L 7 4 4F RT A20WE 20081006 EA 2008 10 6 TRAX200801021 1 20080820 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 970EV 7527 JOB 8752721 OPERATION 103 RT FS 625 OBLIQUE ANGLE CRACKED. DUPLICATE WRITE UP REF MWC 8752721 OP 253 FOR REPLACEMENT. 2 L 7 2 4F RT A21EA 20081006 SO 2008 10 6 C2XA08RI122 1 20080823 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 27 16147 145749 FLIGHT 2074 EWR FLIGHT CREW REPORTED EMERGENCY EXIT IDENTIFIER ABOVE FORWARD FLIGHT ATTENDANT SEAT INOPERATIVE. EWR MX R&R NR 1 EMERGENCY LIGHT INVERTER IAW EMB 145 AMM 33-50-11 AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO R ETURN TO SERVICE. 2 L 7 2 4F RT 20081006 NM 2008 10 6 NWAA084055640 1 20080827 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 540US 26487 DURING OVERNIGHT MX THE ESCAPE PATH LIGHTING IN ROWS 28 THROUGH 33 WERE FOUND TO BE INOPERATIVE. THE BATTERY PACK ASSOC IATED WITH THESE LIGHTS WAS FOUND TO BE INOPERATIVE. MX REPLACED POWER SUPPLY K735. ALL OPS WERE NORMAL AFTER REPLACEM ENT OF THE POWER SUPPLY. 2 L 7 2 4F RT A2NM 20081006 NM 2008 10 6 NWAA084045809 1 20080827 A 3350 BATTERY PACK BOEING 757 757351 1384991 NM CABIN FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 589NW 32989 DURING EMERGENCY LIGHT BATTERY PACK DEEP CYCLE CHECK, ALL 15 EMERGENCY LIGHT BATTERY PACKS FAILED THE TEST. MX REPLACED THE BATTERY PACKS AND ALL OPS WERE NORMAL AFTER REPLACEMENT. 2 L 7 2 4F RT A2NM 20081121 WP 2008 11 21 NWAA084519929 1 20081007 A 3010 DUCT DOUG DC9 DC931 3022065 WP ANTI-ICE SYS DEFECTIVE A NWAA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 GL 01 8923E 45838 ON APPROACH INTO YYZ AFTER FLIGHT CREW SET THE LEADING EDGE SLATS TO EXTEND, FLAPS AT ZERO, THE AMBER SLAT DISAGREEMENT LIGHT ILLUMINATED AND AN UNCOMMANDED ROLL OF THE ACFT TO THE LT OCCURRED. THE SLATS WERE RETRACTED WITHOUT DIFFICULTY, THE FLAPS EXTENDED TO 40 AND THE ACFT COMPLETED A NO SLAT LANDING WITHOUT FURTHER DIFFICULTIES. MX FUNCTIONALLY CHECKED THE SYSTEM AND REPLACED THE LT SIDE T-DUCT AS A RESULT. LEAK CHECK OF THE AIRFOIL ANTI-ICE SYSTEM AND FUNCTIONAL CHECK S OF THE SLAT AND FLAP SYSTEMS WERE ALL GOOD AND THE ACFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 20081121 WP 2008 11 21 AALA200810126 1 20081024 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 UNDERSIDE OF RIGHT CUSP CORRODED AT STATION 530-534. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081121 WP 2008 11 21 AALA200810115 1 20081029 A 5313 STRINGER DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 251AA 49270 NR 20 LEFT STRINGER CRACKED AT STATION 995. INSTALLED DOUBLER PER AARD 53-10-00-18. 2 L 7 2 4F A6WE 20081121 NM 2008 11 21 AALA200810154 1 20081020 A 5315 FLOORBEAM BOEING 737 737823 13844BZ NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AA 29506 CORROSION ON CABIN FLOOR SUPPORT AT STATION 962 AT RBL 16. REMOVED AND REPLACED FLOOR SUPPORT. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 AALA200810155 1 20081020 A 5320 FLOOR SUPPORT BOEING 737 737823 13844BZ NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 CORROSION ON CABIN FLOOR SUPPORT AROUND NUTPLATE HOLES AT STATION 312 TO 328 RBL 10. INSTALLED NEW FLOOR SUPPORT. 2 L 7 2 4F RT A16WE 20081121 WP 2008 11 21 AALA200810018 1 20081013 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 NUMBER 3 SEAT TRACK CORRODED AT STATION 1176 TO 1180. INSTALLED SEAT TRACK SPLICE PER 53-05-00. 2 L 7 2 4F A6WE 20081121 NM 2008 11 21 USAA920081923 1 20081017 A 5312 BULKHEAD BOEING 737 7373B7 138447F NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 24479 PIT FPBH MAJOR REPAIR LOG NR 4371426 CRACK ON 178 BULKHEAD WEB BETWEEN WL234 AND WL 225, BL17R. REPAIRED 178 BULKHEAD W EB BETWEEN WL234 AND WL225, BL17R. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 USAA920081915 1 20081016 A 5310 6545871523 STOP FITTING BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C100652003/011 AND 03C10652003/010 R1 DOOR STOP FITTINGS CRACKED 3RD AND 4TH FROM TOP/TRAILING EDGE. REPAIRED R1 DOOR STOP FITTINGS 3RD AND 4TH FROM TOP/TRAILING EDGE IAW US AIRWAYS TYPICAL REPAIR NR 51-10-11. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 USAA920081912 1 20081019 A 5312 BULKHEAD BOEING 737 7373B7 138447F NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 24479 CLT RON MAJOR REPAIR NR 4371427 4 CRACKS ON LT VERTICAL BEAM AT 178 BULKHEAD BL17L, BETWEEN WL234 TO WL225. REPAIRED LT VERTICAL BEAM AT 178 BULKHEAD BL17L, BETWEEN WL234 TO WL225 IAW B737 SRM 53-10-08. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 USAA920081913 1 20081017 A 5340 6953207U501 STRINGER CLIP BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03-055380358/003 STRINGER TIE CLIP CRACKED AT BS 663, S4R. REPLACED STRINGER TIE CLIP AT BS 663, S4R IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081121 EU 2008 11 21 USAA920081928 1 20081021 A 3350 P2070003001 FLASHLIGHT AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 633AW 82 LOG PAGE 8342213 FLT NR 343 ORD PHX EMERGENCY EQUIPMENT FORWARD FLIGHT ATTENDANT FLASHLIGHT NEEDS REPLACEMENT. MX R&R T HE FORWARD FLIGHT ATTENDANT FLASHLIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081121 WP 2008 11 21 NWAA084749880 1 20081024 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 675MC 47651 DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 9-13 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE BATTERIES. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A6WE 20081121 NM 2008 11 21 NWAA084875519 1 20081103 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM CABIN FAULTY A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 519US 23207 DURING AN OVERNIGHT LINE CHECK THE EMERGENCY EXIT SIGNS IN THE CEILING AT DOORS 2 AND 3 WOULD NOT ILLUMINATE. THE BATTE RY PACKS WERE FOUND TO BE FAULTY AND THEY WERE REPLACED. OPS WERE NORMAL AFTER THE BATTERY PACKS WERE REPLACED. 2 L 7 2 4F RT A2NM 20081124 WP 2008 11 24 AALA200810135 1 20081027 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 CORROSION ON NR 2 SEAT TRACK FROM STATION 1303 TO 1309. INSTALLED NEW SEAT TRACK FROM STATION 1260 TO 1309 PER SRM 53-0 5-00 FIG 4F. 2 L 7 2 4F A6WE 20081124 NE 2008 11 24 UALA2008111305934 2 20080930 A 7261 ACC434F65 OIL FILTER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE DEFECTIVE A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 652UA 25390 THE 'R OIL FILTER' STATUS MSG DISPLAYED. REPLACED MAIN OIL FILTER & ENGINE OIL SCREEN. ENG RUN PERFORMED. NO LEAKS NO TED AND NO FURTHER MSG DISPLAYED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 WP 2008 11 24 AALA200810127 1 20081024 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 INTERCOSTAL IN AFT CARGO CRACKED, CEILING AREA AT STATION 1287-1309. INSTALLED NEW INTERCOSTAL PER SRM 51-10-1. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 AALA200810156 1 20081022 A 5330 SKIN BOEING 737 737823 13844BZ NM ZONE 100 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 DENT AND CREASE IN FUSELAGE SKIN AT STATION 500B+13 BETWEEN STRINGER 18L AND 19L. INSTALLED REPAIR PER SRM 53-00-01-2 R EPAIR NR 3. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 AALA200810160 1 20081016 A 5320 INTERCOSTAL BOEING 737 737823 13844BZ NM ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 INTERCOSTAL CRACKED AT NUTPLATE HOLE. REPLACED INTERCOSTAL PER SRM 51-10-02-0. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 AALA200810166 1 20081029 A 5315 FLOORBEAM BOEING 737 737823 13844BZ NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 CORROSION ON FLOOR FRAME. INSTALL FILLER STRAP AND ANGLES PER SRM 53-00-51. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 UALA2008111306301 1 20081028 A 3397 794640 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 653UA 25391 FWD EEL CROSS-AISLE LIGHT IS INOP. SECURED RIBBON CONNECTOR. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 NM 2008 11 24 AALA200820009 1 20081009 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 672AA 52528 25337 AFT MAIN DECK PLATE IS CORRODED. DOUBLER INSTALLED IAW SRM 53-60-51-2R2. 2 L 7 2 4F RT A2NM 20081006 EA 2008 10 6 TRAX200801047 1 20080823 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 860AS 7433 SERVICE DOOR EXTER. EMER. LIGHT INOP. RELAMPED SERVICE DOOR EXTER. EMER. LIGHT IAW CRJ200AMM 33-51-21. OP CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 20081006 EA 2008 10 6 TRAX200801051 1 20080823 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR LACK OF LUBE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 971EV 7528 PAX SERVICE DOOR IS VERY HARD TO OPEN FROM OUTSIDE. LUBE SERVICE DOOR OK FOR SERVICE. 2 L 7 2 4F RT A21EA 20081006 EA 2008 10 6 TRAX200801059 1 20080825 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 932EV 8016 JOB 8801621 OPERATION 160 LT INBD AND OTBD 280 CLIPS AT LBL 9 ARE CRACKED. THIS SDR WILL REMAIN OPEN PENDING MX DETERMI NATION OF AN APPROPRIATE CORRECTIVE ACTION. 2 L 7 2 4F RT A21EA 20081006 EA 2008 10 6 TRAX200801064 1 20080826 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 846AS 7328 INTERCOASTAL AT FS 589 BETWEEN LBL 36 AND CARGO DOOR SILL CRACKED AT SILL ATTACHMENT. THIS SDR WILL REMAIN OPEN PENDING MX DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. 2 L 7 2 4F RT A21EA 20081006 EA 2008 10 6 TRAX200801065 1 20080827 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 921EV 7819 RT AFT EXTERIOR EMER LIGHT INOP. RELAMPED RT AFT EXTERIOR EMER LIGHT IAW CRJ 200 AMM 35-51-21. 2 L 7 2 4F RT A21EA 20081006 SO 2008 10 6 C2XA08IA197 1 20080826 A 3397 M812P1 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13990 145277 IAH DURING A CHECK INSPECTION THE EMERGENCY LIGHT ON THE GALLEY SERVICE DOOR SWING ARM WAS FOUND TO BE INOPERATIVE. MX RECONNECTED A LOOSE PLUG CONNECTED TO THE LIGHT, OPS CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SE RVICE. 2 L 7 2 4T RT T00011AT 20081006 SO 2008 10 6 C2XA08RI121 1 20080825 A 3320 7281000501 CONTROL MODULE EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 12564 145618 FLIGHT 2251 EWR FLIGHT CREW REPORTED SIDE ROW LIGHTS OUT AND BURNING SMELL FROM CONTROL MODULE. EWR MX R&R CONTROL MODU LE IAW EMB 145 AMM 33-20 AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081006 SO 2008 10 6 C2XA08SH114 1 20080829 A 5210 14525302007 DOOR FRAME EMB 145 EMB145LR 3260212 SO MAIN DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15912 145439 SHV DURING C-CHECK MAIN DOOR LOWER NUTPLATE HOLES HAS CORROSION MX REPAIRED MAIN DOOR LOWER BOTTOM NUTPLATE AREA IAW EC 5210-01154. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081006 SO 2008 10 6 C2XA08SH115 1 20080829 A 5320 14530642401 FLOOR SUPPORT EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 15912 145439 SHV DURING C-CHECK LT OMEGA BEAM HAS CORROSION AT CROSSBEAM AT FR29. MX REPAIRS LT OMEGA BEAM AT FR 29 IAW EMB 145 SRM 53-00-10 FIG 202 ST 2 THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081006 SO 2008 10 6 C2XA08ON173 1 20080823 A 5200 14533413401 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR OUT OF ADJUST A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 26549 14816 145571 FLT 0053 RNO FLIGHT CREW REPORTED AFTER LANDING IN RNO PAX DOOR DIFFICULT TO OPEN FROM INSIDE. REPO ACFT 188 ONT RNO TO COVER FLIGHT 53 AND ROUTE MECHANICS AND PARTS TO REPAIR 549. MX PERSONNEL ADJUSTED PAX DOOR INTERNAL HANDLE. OPS CHEC K SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. 2 L 7 2 4T RT T00011AT 20081006 SO 2008 10 6 C2XA08CL100 1 20080827 A 3350 110049 CHARGER EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 34111 145659 DURING ROUTINE MX THE AFT OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MX INSPECTED AND REPLACED THE NR 4 EMERGENC Y LIGHT BATTERY CHARGER. OPS CHECKS WERE GOOD. 2 L 7 2 4F RT 20081006 SO 2008 10 6 C2XA08CL101 1 20080827 A 2840 WARNING SYSTEM EMB 145 EMB145LR 3260212 SO COCKPIT ACTIVATED A C2XA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 27 14953 145071 DSM FLIGHT NR 2636 THE CREW REPORTED A FUEL 1 LOW LEVEL MSG IN FLIGHT. THE FLIGHT DIVERTED IN DSM AND LANDED WITHOUT IN CIDENT. THE FUEL QUANTITY INDICATOR WAS ACCURATE. THE SYSTEM WAS PLACED ON MEL SUPPLEMENT TO FOLLOW. 2 L 7 2 4T RT T00011AT 20081006 SO 2008 10 6 C2XA08CL102 1 20080831 A 3297 14521495403 WIRE HARNESS EMB 145 EMB145LR 3260212 SO NLG DEFECTIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13968 145138 CLE FLIGHT NR 2320 THE CREW REPORTED AN AIR/GROUND FAIL MESSAGE IN FLIGHT. THE GEAR WOULD NOT RETRACT. THE ACFT RETURN ED TO CLE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE NOSE GEAR WOW HARNESS AND PROXIMITY SWITCH. OPS C HECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20081006 SO 2008 10 6 C2XA08IA199 1 20080826 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 21154 145772 IAH FLIGHT 2073 THE CREW REPORTED THAT THE RT EMERGENCY LIGHT STRIP WAS INOPERATIVE. MX R&R THE NR 4 INVERTER. OPS CHE CKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081006 NM 2008 10 6 WRLA2008070 1 20080822 A 5320 AE06261 DOUBLER DOUG MD11 MD11F 3023600 NM PWA 4462 PW4462 NE CLG WW CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 279WA 48756 DURING INSPECTION FOUND CRACK ON CENTER LANDING GEAR WHEEL WELL FORWARD BULKHEAD LT & RT AROUND LATERAL CONTROL MIXER. CORRECTIVE ACTION: INSTALLED ANGLE REF ROD SKETCH 91-09-09-002. 2 L 7 3 4F 4 F RT A22WE E24NE 20081006 NM 2008 10 6 WRLA2008073 1 20080826 A 5330 SKIN DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 272WA 48437 DURING INSPECTION FOUND FUSELAGE SKIN AND REINFORCING DOUBLER CORRODED AT AFT LAV EXHAUST PORT STA 1959 BETWEEN LONGERON S LS9R AND L40R. CORRECTIVE ACTION: REF. DELTA ERA 47026114 REMOVED DAMAGED AREA, PERFORMED HF EDDY CURRENT INSPECTION AS REQUIRED, FABRICATED REPAIR PARTS, TREATED, PRIMED AND SEALED REPAIRED AREA. 2 L 7 3 4F 4 F RT A22WE E24NE 20081006 EA 2008 10 6 REX2008F00044 1 20080825 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A REXA O OTHER J WARNING INDICATION CR CRUISE 1 CE 21 8587E 16135 7587 IN CRUISE AT FL 220 RECEIVED A FLAP FAIL CAUTION MESSAGE QRH FOLLOWED DECLARED EMERGENCY, DIVERT TO DTW FROM LEX LANDED WITHOUT INCIDENT IN DTW. TROUBLESHOT FLAP SYSTEM IAW BOMBARDIER FAULT ISOLATION MANUAL (FIM) AND ACFT MX MANUAL (AMM) R &R RT BRAKE POSITION SENSING UNIT (BPSU) DUE TO WOULD NOT MAINTAIN RIG. 2 L 7 2 4F RT A21EA 20081006 NM 2008 10 6 USAASB08069 1 20080826 A 3350 036000570010 FUSE BOEING 737 737401 1384701 NM BATTERY CHARGER BLOWN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 424US 23991 PHL MX REPORTED THE BULL NOSE EMERGENCY LIGHT AT STATION 850L, ABOVE THE AISLE AT SEAT 24A, INOPERATIVE. MX R&R THE FUS E IN POWER SUPPLY BATTERY CHARGER M1435, ABOVE RT HAND CEILING PANEL AT STATION 753. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 20081006 2008 10 6 USAASB08070 4 20080826 A 3497 WIRE BOEING 737 7373S3 1384711 NM E&E BAY CHAFED A USAA O OTHER F N FLT CONT AFFECTED FALSE WARNING CR CRUISE 1 EA 19 315AW 23734 PHX FLT409 DURING FLIGHT, ENROUTE FROM SFO TO PHX AUTO THROTTLES WENT TO FULL POWER UNCOMMANDED. AUTOPILOT COMMANDED NO SE OVER BEFORE DISCONNECT. FLIGHT FAULT REVIEW REVEALED PROBLEM WITH CAPTAINS AOA VANE GIVING FALSE STALL INDICATIONS T O COMPUTERS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MX FOUND WIRE NR W005910222R ON E1-1 RACK CHAFED. REPLACED SHIELDED CABLE WOO5910222R ALONG WITH SHIELDED CABLE WOO59100R/9101B-22. RETERMINATED SPLICES SM 351, SM352, SM353 PER WDM 22-12-31. ALSO, FOUND WIRE NR WOO523522R AND 236-22B CHAFED 6 INCHES BEHIND D00309A. REPLACE D SHIELD PAIR WOO523522R/236-22B PER WDM 22-23-12. CONTINUITY CHECKS GOOD. REPLACED CAPTAINS AOA VANE AND FOS PITOT TU 2 L 7 2 4F RT A16WE 20081006 NM 2008 10 6 USAASB08071 1 20080828 A 3260 WARNING SYSTEM BOEING 737 73733A 1384673 NM COCKPIT ACTIVATED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 166AW 23627 DFW FLT 550 AFTER TAKEOFF FROM DFW CREW RECEIVED A RT MAIN LANDING RED LIGHT AFTER GEAR WAS SELECTED UP. FLIGHT RETURNE D TO FIELD AT DFW AND LANDED WITHOUT FURTHER INCIDENT. MX ACTION PENDING. 2 L 7 2 4F RT A16WE 20081006 EU 2008 10 6 NWAA084013217 1 20080822 A 2910 O-RING AIRBUS 320 A320211 3930320 EU HYDRAULIC SYSTEM DEFECTIVE A NWAA K NONE O OTHER AP APPROACH 1 GL 01 317US 197 Y HYD RSVR LO LVL DISPLAYED. COMPLIED WITH COM. ACFT LANDED UNEVENTFULLY TOWED TO GATE. REPLACED O-RING AND BACK-UP R ING ON NR 2 ENGINE DRIVEN HYDRAULIC PUMP FITTING. CHECKS OK. 2 L 7 2 4F RT A28NM 20081006 WP 2008 10 6 DHL200800093 1 20080813 A 2697 87823802 CONNECTOR DOUG DC8 DC873F 302199F WP FIRE WARNING MALFUNCTIONED A DHLA K NONE N FALSE WARNING NR NOT REPORTED 1 SO 01 805DH 46125 FIRE WARNING LIGHT ON AND FIRE BELL RINGING NR 3 ENG. SWITCHED TO B LOOP LIGHT AND BELL WENT OUT. DEFERRED NR 3 ENG A LOOP PER EML 26-2-3 CAT C PLACARD ISN`T DMI 33371. A/C WAS GROUNDED FLIGHT 445. P/N CHANGED CONNECTOR 878238-02. 2 L 7 4 4F RT 4A25 20081006 NM 2008 10 6 MWE2008F00039 1 20080827 A 5330 594115853 DOUBLER BOEING 717 717200 1383700 NM BS 994 L28R CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 919ME 55181 AFT CARGO BAY STAR DOUBLER AT STA 994 LONGERON 28R IS EXFOLIATED AROUND SCREW HOLE. REMOVED AND REPLACED STAR DOUBLER. 2 L 7 2 4F TR A6WE 20081006 NE 2008 10 6 AALA200802124 2 20080818 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 2 MALFUNCTIONED A AALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 489AA 49682 718267 MSY INFLIGHT T2224/18AUG DFW TO PBI. CREW REPORTED NR 2 ENGINE OIL LOW PRESSURE INDICATION AT FLIGHT LEVEL 330. CREW S HUT DOWN ENGINE AND LANDED MSY WITHOUT INCIDENT. SINGLE ENGINE TIME 17 MINUTES. REPLACED NR 2 ENGINE ON 20 AUG AT MSY DUE TO OIL PRESSURE OUT OF LIMITS. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F 4 F A6WE E9NE 20081007 NM 2008 10 7 DHLA200800095 1 20080903 A 7711 EPR SYSTEM BOEING 727 727227 1384078 NM NR 3 ENGINE FAULTY A DHLA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 781DH 21996 WHEN SETTING T/O THRUST, NR 3 ENGINE PARAMETERS WERE SIGNIFICANTLY LOWER WITH EPR READINGS MATCHED. T/O REJECTED AT 80 KTS, TEMP 27, PA 3925 GW 160K. NR 3 ENG EPR SYSTEM DEFERRED REF B737 MEL 77-1-1. CAT A DDD 3.6.09. ALL ASSOCIATED ENG INDICATIONS NORMAL. CONTROL NR 33529. PLACARD INSTALLED. FLIGHT NR 119. ACFT WAS GROUNDED. 9/12/2008 FOUND CONTAMIN ATION IN NR 3 PT2 LINE BLOWOUT AND REINSTALL LINE IAW B727, MM 77-11-0 RUN ENG IAW JRH 5.2. OPS CHECK GOOD. (K) 2 L 7 3 4F A3WE 20081007 EU 2008 10 7 MAL2008F00031 1 20080825 A 2161 CONTROLLER SAAB SF340 340B 7860101 EU CABIN TEMP INOPERATIVE A MALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 442XJ 340B442 RT HAND DUCT OVERTEMP ILLUMINATED AFTER TAKEOFF. RT BLEED AUTOMATICALLY CLOSED. FLIGHT ATTENDANT REPORTED SEEING SMOKE AND EXTREME HEAT IN THE CABIN. RETURNED TO LAND AT MEMPHIS AFTER DECLARING EMERGENCY. CND RT DUCT OVERTEMP. FOUND FL IGHT DECK TEMP SENSOR BLOWER INOP AND CABIN AUTO TEMP INOP. R&R CABIN AUTO TEMP CONTROLLER AND F DECK TEMP SENSOR. ALL CHECKS GOOD IAW SF340 AMM CHP. 21-60-00-05. TEMP SENSOR P/N ON & OFF BYLF51175 IAW 21-61-15-04. TEMP CONTROLLER P/N O N & OFF 754661-8, S/N ON 98022638, S/N OFF 96121815. 2 L 7 2 4T RT A52EU 20081006 NM 2008 10 6 NWAA084066731 1 20080822 A 5411 FRAME BOEING 747 747251B 1384892 NM NR 4 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 631NW 23111 DURING L CHECK FOUND CRACK IN NR 4 PYLON REAR ENGINE MOUNT BULKHEAD FORWARD FRAME AT NAC STA 222.90. REPAIRED PER EA 67 -213556. 2 L 7 4 4F RT A20WE 20081006 NM 2008 10 6 NWAA084076315 1 20080901 A 3397 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 675NW 33001 DURING OVERNIGHT CHECK FOUND EMERGENCY LIGHTS FROM ROWS 51 TO 66 LT SIDE INOP. MX RESECURED LOOSE CONNECTOR. OPS CHECK GOOD AND ACFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20081008 NM 2008 10 8 AALA200802143 1 20080819 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 798AN 30797 DFW EMERGENCY LIGHT AT RT NR 4 GALLEY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 10G. SYSTEM GROUND CHECK ED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802150 1 20080820 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 750AN 30259 DFW EMERGENCY LIGHT AT SEAT 26G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802151 1 20080821 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 794AN 30256 EZE EMERGENCY LIGHT AT SEAT 23G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23G. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 2008UALA05726 1 20080914 A 3397 80582 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 STAIRWELL EMERGENCY LIGHTS INOPERATIVE. FOUND DEFECTIVE FEEDER CABLE. REPLACED FEEDER CABLE. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081008 WP 2008 10 8 AALA200802136 1 20080819 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9409F 53121 LGA EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 18D. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT A6WE 20081008 NM 2008 10 8 AALA200802137 1 20080819 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 948AN 30086 DFW EMERGENCY LIGHT AT SEAT ROW 23 INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 23. SYSTEM GRO UND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 AALA200802138 1 20080819 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 948AN 30086 DFW EMERGENCY LIGHT AT SEAT ROW 27 INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 27. SYSTEM GRO UND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 AALA200802139 1 20080819 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 948AN 30086 DFW EMERGENCY LIGHT AT SEAT ROW 9 INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 9. SYSTEM GROUN D CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 AALA200802142 1 20080819 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 770AN 29578 DFW EMERGENCY LIGHT AT SEAT 10G MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 10G. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 WP 2008 10 8 AALA200802159 1 20080821 A 2410 CSD DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RT ENGINE OVERHEATED A AALA A UNSCHED LANDING M H J OVER TEMP ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SW 21 450AA 49476 717881 ABQ INFLIGHT T1760/21AUG PHX TO DFW. RT ENGINE CONSTANT SPEED DRIVE OVER TEMP INDICATION. AUXILIARY POWER UNIT PLACARD INOPERATIVE. LANDED ABQ WITHOUT INCIDENT. REPLACED CONSTANT SPEED DRIVE AND GENERATOR. REPLACED TUBE. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F 4 F A6WE E9NE 20081008 WP 2008 10 8 AALA200802163 1 20080822 A 2530 8291110000D OVEN DOUG DC9 DC983 3022083 WP GALLEY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 9618A 53565 STL INFLIGHT T1419/22AUG. FIRST CLASS GALLEY OVEN SMOKING AFTER TAKE OFF. RETURNED TO STL AND LANDED WITHOUT INCIDENT. FOUND RESIDUE IN OVEN. REPLACED FIRST CLASS GALLEY OVEN AND OVEN CONTROLLER. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081008 WP 2008 10 8 AALA200802170 1 20080822 A 4920 5940405503 APU DOUG DC9 DC982 3022082 WP APU BAY MALFUNCTIONED A AALA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 7522A 49899 DFW INFLIGHT T351/22AUG. AFTER TAKE OFF FLIGHT ATTENDANTS REPORTED BLUE HAZE COMING FROM AIR CONDITIONING. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED AUXILIARY POWER UNIT (APU) DUE TO OIL SATURATING APU COMPARTMENT. SYSTEM GR OUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081008 WP 2008 10 8 AALA200802172 1 20080822 A 3350 LENS DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 466AA 49596 DFW EMERGENCY LIGHT AT SEAT 7D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMA L OPS. 2 L 7 2 4F A6WE 20081008 EU 2008 10 8 COEA0801913 1 20080915 A 2421 800326 COVER AEROSP ATR42 ATR42300 8680920 EU RT ENGINE LOOSE E E9LA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 EA 05 913FX 250 ABORTED TAKE OFF. ON TAKE OFF RT ENGINE POWER LEVER RESISTANCE FELT AT APPROXIMATELY 55% OF POWER LEVER ANGLE. INSPECT ION OF THE POWER LEVER SYSTEM FOUND THE ALTERNATOR TERMINAL COVER LOOSE, WHICH OBSTRUCTED POWER LEVER MOVEMENT AT THE PR OPELLER GOVERNOR. REINSTALLED THE TERMINAL COVER. C/W ATR SL 42-24-5011, TIGHTENING TORQUE VALUES. 2 H 7 2 4T RT A53EU 20081007 EU 2008 10 7 MAL2008F00032 1 20080825 A 3350 CIRCUIT BREAKER SAAB SF340 340B 7860101 EU POPPED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 424XJ 340B424 CB L8 POPPED, PREVIOUSLY RESET ONCE PER POM CB POLICY. RESET CB L8. 2 L 7 2 4T RT A52EU 20081007 NM 2008 10 7 YENA2008084 1 20080902 A 2150 A/C PACK EMB ERJ190 ERJ190100IGW 3260408 NM NR 2 CONTAMINATED A YENA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 EA 15 198JB 19000021 FLT NR 68, JFK-SYR, AIR RETURN TO JFK, CABIN CREW REPORTED SMOKE IN CABIN. REMOVED NR 1 AND NR 2 PACK EXT PNLS. INSPEC TED FOUND COFFEE DEBRIS IN NR 2 PACK, NR 1 PACK OK. AMM 21-51-05. CLEANED OUT NR 2 PACK AND SECURED NR 1 AND 2 EXT PNL S. OPS CHECK OF NR 1 AND NR 2 PACKS. OKAY. INSPECTED FWD/MID E & E BAY RECIRC FANS. OPS CHK OK AMM 21-26-00/01. RAN OPERATED ENG NR 1 & NR 2 BLEED CHECK OK. NO DEFECTS NOTED AMM 71-60-01. COMPLETED FIM 21-20-00-810-801A. PERFORMED L TV SMOKE IN CABIN INSPECTION PER LTV MM 44-20-10. NO FAULTS NOTED LTV SYS. OPS CHK NML PER LTV MM 44-20-10. 2 L 7 2 4F RT A57NM 20081007 NM 2008 10 7 UIEA200800322 1 20081002 A 5330 SKIN BOEING 747 7472D7B 1384803 NM ZONE 200 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 BS 740 TO 999.9 AT S6L/R LAP JOINT SCRIBE LINE DAMAGED. REPAIRED IN ACCORDANCE WITH SERVICE REQUEST 1-750626371 APPROVED BY FAA FORM 8100-9 DATED 2 OCT 2008, DETAILS OF WORK KEPT IN EO-473B205 & EO-4753B113. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 UIEA200800319 1 20080930 A 5330 SKIN BOEING 747 7472D7B 1384803 NM ZONE 200 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 FUSELAGE STA 520 TO STA 740 AT S-23L/R LAP JOINT SCRIBE LINE DAMAGED. REPAIRED IN ACCORDANCE WITH SERVICE REQUEST 1-750 634474 APPROVED BY FAA FORM 8100-9 DATED 2 OCT 2008, DETAILS OF WORK KEPT AT EO-4753B203 & EO-4753B114. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 UIEA200800320 1 20081002 A 5330 SKIN BOEING 747 7472D7B 1384803 NM ZONE 200 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 FUSELAGE STA 520 TO STA 740 AT S-23L/R LAP JOINT SCRIBE LINE DAMAGED. REPAIRED IN ACCORDANCE WITH SERVICE REQUEST 1-75 0634474 APPROVED BY FAA FORM 8100-9 DATED 2 OCT 2008, DETAILS OF WORK KEPT AT EO-4753B203 & EO-4753B114. 2 L 7 4 4F RT A20WE 20081007 EA 2008 10 7 TRAX200801046 1 20080823 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA BS 605 CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 846AS 7328 INTERCOSTAL AT FS 605 BETWEEN LBL 36 AND CARGO DOOR SILL CRACKED AT SILL ATTACHMENT (RESOLVED ON W/O 96197 TASKCARD: N/ R 00021) JOB COMPLETE ITEM 1. REFER TO ATTACHED M-234 FORMS FOR WORK ACCOMPLISHED. ITEM 2. 2 L 7 2 4F RT A21EA 20081007 NM 2008 10 7 KCSA081427 1 20080827 A 5315 FLOORBEAM BOEING 747 747122 1384872 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 AFT BILGE FLOOR BEAM UPPER CHORD IS CRACKED AT STA 2100, RBL 23. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081441 1 20080902 A 5210 DOOR FRAME BOEING 747 747122 1384872 NM R1 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 R1 MAIN ENTRY DOOR FWD VERT FRAME CRACKED AT LOWER CORNER. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 MAS2008F00064 1 20080823 A 5755 SPOILER BOEING 737 737* NM NR 7 DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 855AM 33792 DURING TRANSIT CHECK, MX PERSONNEL DETECTED A PERFORATION OUT OF LIMITS IN THE INBOARD GROUND SPOILER NR 7 SO THE SPOILE R WAS REPLACED IAW MM 27-62-12. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 ASAA0853480 1 20080909 A 2421 761574B IDG BOEING 737 737890 1384527 NM NR 2 ENGINE MALFUNCTIONED A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 558AS 8573 35177 NUMBER 2 GENERATOR ANNUNCIATION AT GATE. REPLACED IDG. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085024 1 20080911 A 3350 417A5701 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 274WN 32529 EEPLS LENS MISSING AT ROW 2 ABC. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085041 1 20080914 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 339SW 24090 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED STRINGER CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085048 1 20080914 A 2560 65C16820 FITTING BOEING 737 7373Y0 1384671 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 664WN 23495 DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING CORRODED. REMOVED AND REPLACED FITT ING PER SRM. 2 L 7 2 4F RT A16WE 20081003 EA 2008 10 3 HNAA0800254 1 20080612 A 5311 FRAME DHAV DHC8 DHC8311 1386006 EA FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 335EN 32270 375 CORROSION SURFACE FOUND ON FRAMES STA 434.5 TO 445.5 RT STRINGER 31. SURFACE CORROSION REMOVED IAW EO8-53-08-3218 LPI A CCOMPLISHED. 2 H 7 2 4T RT A13NM 20081003 EA 2008 10 3 HNAA0800255 1 20080612 A 5320 85320596111 FITTING DHAV DHC8 DHC8311 1386006 EA FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 335EN 32270 375 CORROSION FOUND AT STR 31 RT AT FRAME 424.12. FITTING REPLACED WITH NEW PART. 2 H 7 2 4T RT A13NM 20081003 NE 2008 10 3 HNAA0800280 3 20080907 A 6140 WARNING SYSTEM DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF7 NE COCKPIT MALFUNCTIONED A HNAA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 07 815EX 321 DURING TAKEOFF ROLL THE NR 1 ENGINE MANUAL LIGHT ILLUMINATED. ACFT WAS RETURNED TO THE FIELD. MX CYCLED THE BETA LOGIC CIRCUIT BREAKER AND GROUND RAN THE ACFT. NO DEFECTS WERE NOTED AT THAT TIME. THE ENGINE CONDITION PANEL WAS ALSO CHEC KED AND NO FLAGS WERE NOTED AT THAT TIME. ACFT THEN CONTINUED IN SERVICE. 2 H 7 2 4T RT A13NM 6 C P7NE 20081003 NM 2008 10 3 2008UALA05732 1 20080914 A 2530 3510003201U2 COFFEEMAKER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FWD GALLEY DEFECTIVE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 799UA 26926 SMOKE AND ELECTRICAL SMELL IN FORWARD GALLEY. DEFECT FOUND IN COFFEEMAKER. REPLACED COFFEEMAKER. NO STRUCTURAL DAMAGE TO GALLEY. SYSTEM OP CHECKS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081003 NM 2008 10 3 2008UALA05733 1 20080914 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 817UA 873 FWD GALLEY FLOORBEAM "A" HAS CORROSION AT FR16. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 2008UALA05925 1 20080929 A 2611 PPA120300 SMOKE DETECTOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE LAVATORY FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 826UA 989 SMOKE LAVATORY DETECTOR FAULT. REPLACED LAV 'A' DETECTOR. 2 L 7 2 4F 4 F RT A28NM E40NE 20081003 NM 2008 10 3 SWAA085296 1 20080930 A 3350 65C27095 HOUSING BOEING 737 7373H4 1384600 NM BATTERY PACK DEFECTIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 633SW 27936 DURING SCHEDULED SPV CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY WOULD NOT SECURE TO CHARGER AT BS 927 LT. REMOVED AND RE PLACED BATTERY PACK HOUSING PER MM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 CALA0800934 1 20081001 A 5315 141T5282 STIFFENER BOEING 767 767224 1385170 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 76156 30435 E&E COMPARTMENT LEFT STATION 246 CABIN FLOORBEAM LBL 25 VERTICAL STIFFENER FOUND CRACKED. E&E COMPARTMENT LEFT STATION 246 CABIN FLOORBEAM LBL 25 VERTICAL STIFFENER REPLACED PER SRM 51-10-02 AND FASTENERS INSTALLED PER SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081003 EU 2008 10 3 UPS08153413 1 20080930 A 2421 GENERATOR AIRBUS A300 A300F4622R 3930360 EU NR 1 MALFUNCTIONED A IPXA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 01 164UP 005 INSPECTION TYPE:N/A ATB - AFTER TAKEOFF NR 1 GEN FAULTED. APU GEN FAULTED ALSO UPON START UP REF LOG PAGE 964332. GPCU SHOWED GEN 1 GCU AT FAULT. REPLACED NR 1 GCU IAW AMM 24-22-12-04. REPLACED GPCU IAW AMM 24-41-11-04. OPS CHECK GOOD. GROUND RAN ENG NR 1, IDG OPERATES NORMALLY IAW AMM 24-11-11-04. 2 L 7 2 4F RT A35EU 20081006 NM 2008 10 6 AALA200802016 1 20080803 A 3350 SHROUD BOEING 737 737823 13844BZ NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 DFW EMERGENCY LIGHT SHROUD AT SEAT ROW 17DEF BROKEN. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT ROW 17DEF. SYSTEM GRO UND CHECKED NORMAL OPS. (CLOSED) 2 L 7 2 4F RT A16WE 20081006 NM 2008 10 6 AALA200802031 1 20080805 A 3350 LENS BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 676AN 29426 DFW EMERGENCY LIGHT AT SEAT 10D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 10D. SYSTEM GROUND CHECKED NOR MAL OPS. (CLOSED) 2 L 7 2 4F RT A2NM 20081006 NM 2008 10 6 USAASB08076 1 20080901 A 3350 20131ASMI BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 443US 24842 FLL THE EMERGENCY EXIT LIGHTS WERE INOPERATIVE FROM ROW 12 THROUGH 19. MX REPLACED THE BATTERY CHARGER AT STATION 807. OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 20081006 CE 2008 10 6 GUU2008F00051 1 20080831 A 3240 BRAKE ASSY BEECH 1900 1900D 1154162 CE MLG MALFUNCTIONED A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 29 81533 UE137 PILOT REPORTED NO BRAKES AND NO STEERING AT THE END OF LANDING ROLL. PERFORMED PRESSURE POT BLEEDING OF BRAKE SYSTEM. OP ERATIONAL CHECK OF BRAKES AND STEERING NORMAL. (K) 2 L 7 2 4T RT A24CE 20081006 NM 2008 10 6 NSV2008F00025 1 20080908 A 3246 WHEEL BOMBDR DHC8 DHC8402 1390042 NM NLG VIBRATION A NSVA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 EA 27 202WQ 4202 AIR RETURN, NOSE WHEEL VIBRATION ON TAKEOFF, DECLARED AN EMERGENCY. RETURNED TO FIELD, LANDED SAFELY. (K) 2 H 7 2 4T RT A13NM 20081006 WP 2008 10 6 U2R2008F00005 1 20080825 A 5713 STRINGER DOUG DC8 DC871F 302199D WP RT WING CRACKED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 872SJ 83402 46040 DURING C-CHECK INSP, FOUND RT WING X RS 202 NR 4 MAIN FUEL TANK STRINGER 67 HAS 2 INCH CRACK BY ACCESSORY PANEL NR 5050. (K) 2 L 7 4 4F RT 4A25 20081006 SO 2008 10 6 C2XA08RI117 1 20080823 A 2131 22250NO30201 CONTROLLER EMB 145 EMB145XR 3260214 SO CABIN PRESSURE INOPERATIVE A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 41104 3534 145646 FLIGHT 1228 EWR FLIGHT CREW REPORTED ACFT NO PRESSURIZING IN CLIMBING. AIR CREW PERFORMED AIR RETURN AND LANDED UNEVENT FULLY. EWR MX R&R DIGITAL PRESSURIZATION CONTROLLER AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081006 CE 2008 10 6 FPI2008F00001 1 20080814 A 3230 505530401 CABLE CESSNA 210 210M 2073450 CE CONT O520 IO520* 17032 SO NLG BROKEN E FPIA O OTHER O OTHER NR NOT REPORTED 1 SO 15 8427M 21062043 MFG SERVICE KIT, PN SK210-174 CABLE ASSEMBLY BROKE AT THREADED END AFTER THE STOP NUT FIVE WEEKS AFTER INSTALLATION APPE ARS THREAD WALL IS TOO THIN LEADING TO FATIGUE. (K) 1 H 7 1 3O 3 O 3A21 E5CE 20081007 EA 2008 10 7 MAS2008F00073 1 20080824 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA ACM CONTAMINATED A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 154SF 7154 ASH 7290 ORD FUEL ODOR IN THE COCKPIT. MX REPLACED CONTAMINATED ACM COALESSER BAGS. 2 L 7 2 4F RT A21EA 20081007 NE 2008 10 7 EIA2008042 2 20080828 A 7200 ENGINE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE NR 2 MALFUNCTIONED A EIAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 NM 19 485EV 20712 IN FLIGHT SHUT DOWN NR 2 ENGINE. C CRUISE RAIN, FL 4.0 WITH MODERATE TURB. NO THROTTLE MOVEMENT AND NOTED COMPRESSOR S TALL. 2 L 7 4 4F 4 F RT A20WE E20EA 20081008 CE 2008 10 8 COEA0802876 1 20080913 A 2421 200SGL119Q2 GENERATOR CESSNA 208 208B 2073701 CE ENGINE TRIPPED E E9LA D RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 EA 05 876FE 208B0207 RETURN TO BLOCKS. FLT NR 8774 ABQ TO DRO. DURING TAXI TO THE RUNWAY THE GENERATOR TRIPPED TO STANDBY AND WOULD NOT RES ET. PILOT TAXIED A/C BACK TO BLOCKS. REMOVED AND REPLACE THE GENERATOR. (K) 1 H 7 1 3T A37CE 20081008 WP 2008 10 8 08FDEA03640 1 20080829 A 7830 SKIN GE DOUG MD10 MD1010F 3022112 WP THRUST REVERSER GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 NR 3 ENGINE INBD THRUST REVERSER OUTER SKIN IS GOUGED. 2 SPOTS CHECKED LIMITS & FOUND 1 DENT WITHIN LIMITS AND 1 OUT OF LIMITS IAW MM 78-32-01. REMOVED THE DAMAGED AREA. FABRICATED FILLER, BONDED FILLER. CURED & SANDED FLUSH IAW MM 78-3 2-01. CLEANED PRIMED & PAIMTED SRM 51-21-01 & SRM 51-21-01 VOL II. 2 L 7 3 4F RT A22WE 20081008 NM 2008 10 8 KCSA081471 1 20080916 A 3350 LIGHT BOEING 747 747246F 1384850 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 707CK 21681 DOOR L1 FWD CEILING EMERGENCY LIGHT INOP. 2 L 7 4 4F RT A20WE 20081008 SO 2008 10 8 C2XA08IA208 1 20080915 A 3397 72875775 CONNECTOR EMB 145 EMB145XR 3260214 SO CABIN DISCONNECTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14204 14500968 IAH FLIGHT 2039 DURING PREFLIGHT INSPECTION THE CREW REPORTED FWD EXIT LICATION SIGN ASSEMBLY INOP. RESECURED CANNON PL UG AT FWD EXIT LICATION SIGN ASSEMBLY. OPS TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081008 SO 2008 10 8 C2XA08IA210 1 20080918 A 2840 366927001 INDICATOR EMB 145 EMB145LR 3260212 SO COCKPIT INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 18982 21085 145223 SAV FLIGHT 2517. THE CREW REPORTED A FUEL 1 TO LEVEL WARNING CLIMBING THROUGH 12000. THE ACFT RETURNED TO SAV WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE ACFT AND PLACED THE FUEL SYSTEM ON MEL 28-40-00/1 CAT B CTL NR 154609 AND TH E ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081008 SO 2008 10 8 C2XA08IA209 1 20080916 A 5210 14531948401 DOOR TRACK EMB 145 EMB145XR 3260214 SO PAX DOOR OUT OF ADJUST A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 13133 145712 IAH FLIGHT 2035. THE CREW REPORTED THAT THE CABIN DOOR WAS HARD TO CLOSE. MX INSPECTED THE DOOR AND ADJUSTED THE FOLDI NG FLAP. OPS CHECKED WITH NO DIFFICULTIES AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081008 NM 2008 10 8 USAA920081694 1 20080914 A 5322 SHEAR TIE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03C21853024/012 LEVEL 2 EXFOLIATION CORROSION ON SHEAR TIE AT BS 787, S27R. REPLACED SHEAR TIE A T BS 787, S27R IAW B737 SRM 53-00-07. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 AALA200802178 1 20080824 A 3350 SIGN BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AM 24579 DFW EMERGENCY LIGHT EXIT SIGN AT LT NR 1 DOOR DAMAGED. REPLACED SIGN ASSEMBLY FOR EMERGENCY LIGHT EXIT SIGN AT LT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 NM 2008 10 8 AALA200802182 1 20080824 A 3350 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AM 24579 DFW EMERGENCY LIGHT EXIT SIGN DECAL AT RT NR 3 DOOR DAMAGED. REPLACED DECAL FOR EMERGENCY LIGHT EXIT SIGN AT RT NR 3 DO OR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 EU 2008 10 8 AALA200802130 1 20080818 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 8067A 510 JFK EMERGENCY LIGHT AT SEAT 13G BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 13G. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A35EU 20081008 2008 10 8 AALA200802123 4 20080818 A 2565 PIN DOUG DC9 DC982 3022082 WP EVAC SLIDE PULLED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 77421 49333 ATL FORWARD ENTRY DOOR SLIDE PINS WERE PULLED. REPLACED SLIDE AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081008 WP 2008 10 8 AALA200802120 1 20080816 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9628W 53598 LGA EMERGENCY LIGHT EXIT SIGN ACROSS FROM FIRST CLASS LAVATORY INOPERATIVE. REPAIRED CONNECTOR FOR INOPERATIVE EMERGENC Y LIGHT EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081008 NM 2008 10 8 AALA200802117 1 20080816 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39356 24037 DFW EMERGENCY LIGHT AT SEAT 6B INOPERATIVE. REPAIRED BROKEN WIRE TO LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 6B. SYS TEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081008 EU 2008 10 8 AALA200802111 1 20080815 A 3350 BR964814 FIXTURE AIRBUS 300 A300B4605R 3930308 EU CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 80058 466 JFK EMERGENCY LIGHT AT SEAT 24C MISSING FIXTURE. REPLACED FIXTURE FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECK ED NORMAL OPS. 2 L 7 2 4F RT A35EU 20081008 EA 2008 10 8 TRAX200801087 1 20080901 A 2560 BATTERY CNDAIR CL600 CL6002C10 1390015 EA MEGAPHONE DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 750EV 10161 MEGAPHONE INOP. R&R MEGAPHONE BATTERY. OPS CHECK GOOD. IAW CRJ 700 AMM 25-61-14. A/C OK FOR SERVICE. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801094 1 20080903 A 5210 SKIN CNDAIR CL600 CL6002C10 1390015 EA ASD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 ASD INNER SKIN CRACKED AT FWD CORNER UNDER UPPER STEP. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801095 1 20080903 A 5210 SKIN CNDAIR CL600 CL6002C10 1390015 EA ASD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 ASD INNER SKIN CRACKED AT AFT CORNER UNDER UPPER STEP. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801101 1 20080904 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 RT SIDE OF 280 BEAM CORRODED. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801106 1 20080904 A 5534 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 RT AFT V/STAB TO FUSELAGE DRAG ANGLE CRACKED AT 67.5% REAR SPAR DATUM. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801119 1 20080905 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 980EV 7759 JOB 8775921 OPERATION 166 FOUND INBD AND OTBD CLIP ANGLES AT FS 280 AND LBL 9 CRACKED. SUP - REMOVED INBD AND OTBD CLIP S AT FS 280 IAW CRJ 200 SRM 51-42-21 AND 51-42-06. INSTALLED NEW SERVICEABLE CLIP ON OTBD SIDE OF LBL 9 IAW CRJ 200 SRM 51-42-21. CLIP ANGLE ON INBD SIDE OF LBL 9 REQURIES INSTALL. INSTALLED NEW ANGLE ON INBD SIDE OF LBL 9 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. (K) 2 L 7 2 4F RT A21EA 20081008 WP 2008 10 8 WRLA2008075 1 20080909 A 5320 INTERCOSTAL DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 303WL 46917 DURING INSPECTION FOUND CORROSION RT MLG WW. STA 1505 AT LONGERON 31R, INTERCOSTAL SKIN ATTACH. REF DELTA NR40. 2 L 7 3 4F 4 F RT A22WE E23EA 20081008 SO 2008 10 8 CHQA200800175 1 20080907 A 2133 MO30014450964 SEAL EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL OUTFLOW VALVE MISSING A CHQA O OTHER O OTHER CR CRUISE 1 GL 11 564RP 145524 CAE312502 FLIGHT 6142, CMH TO JFK. DURING CRUISE AT FL330, THE CABIN ALTITUDE RAPIDLY ROSE TO APPROXIMATELY 12,000FT. THE FLIGHT CREW FOLLOWED THE QRH CHECKLISTS AND DESCENDED. THE FLIGHT ATTENDANT REPORTED THAT A HISSING NOISE WAS COMING FROM THE MAIN ENTRY DOOR. THE ACFT DIVERTED TO AVP AND LANDED WITHOUT INCIDENT. MX LOCKED OUT THE PRESSURIZATION VALVES AND DE FERRED THE PRESSURIZATION SYSTEM AND THE ACFT WAS FLOWN TO CMH FOR FURTHER TROUBLESHOOTING. MX ADJUSTED THE BOTTOM THRE SHOLD FOR THE MAIN ENTRY DOOR TO ELIMINATE THE HISSING NOISE FROM THE DOOR. WHEN THE ELECTRO-PNEUMATIC OUTFLOW VALVE WA S INSPECTED, IT WAS FOUND THAT A SEAL WAS MISSING THAT SEALED IT TO THE MOUNTING FLANGE. THE VALVE WAS REPLACED AND A N 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081009 NM 2008 10 9 USAABB08148 1 20080905 A 2150 6806404 ACM BOEING 757 757225 1384959 NM A/C BAY DAMAGED A USAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 19 916UW 53753 22192 TPA FLT 1089 ENROUTE CLT TO TPA. DURING DESCENT THE LT AIR CONDITIONING PACK WENT TO FULL HOT WITH A BURNING ODOR. WHE N THE LT PACK WAS SHUT OFF, THE ODOR DISSIPATED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE LT PACK A IR CYCLE MACHINE DUE TO FOD. OPS AND LEAK CHECKS OK. 2 L 7 2 4F RT A2NM 20081009 NM 2008 10 9 2008UALA05576 1 20080903 A 2400 734285E CONTROL UNIT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FAILED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 652UA 25390 EICAS MSG (L,R) UTIL BUSS OFF DISPLAYED. UTILITY BUSS OFF LGT ILLUM. SYS FAILED TO RESET. BUSS PCU FAILURE. REPLACED B USS POWER CONTROL UNIT.TESTS OKAY. RAN BOTH ENGINES & RAN ALL ELECTRICAL POWER SYSTEMS USING ALT BUSSES ALL INDICATION & OPS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081009 NM 2008 10 9 USAA920081638 1 20080905 A 5312 BULKHEAD BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 23379 PIT FPBH MAJOR REPAIR LOG NR 4353301. 2 CRACKS ON 178 BULKHEAD AT RIVET FASTENERS AT WL234, RBL8, ON FORWARD SIDE. REP AIRED 178 BULKHEAD AT RIVET FASTENERS AT WL 234, RBL8 IAW B737 SRM 53-10-08. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 AALA200802099 1 20080813 A 3397 CONNECTOR BOEING 737 737823 13844BZ NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 928AN 29528 MIA EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 20D. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081009 WP 2008 10 9 AALA200802096 1 20080813 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7512A 49806 MSP EMERGENCY LIGHT AT SEAT 7D LIGHT ASSEMBLY MISSING PARTS. REPLACED HARNESS AND LAMP FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081009 NM 2008 10 9 AALA200802093 1 20080813 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 785AN 30005 DFW EMERGENCY LIGHT IN MID CABIN MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT IN MID CABIN. SYSTEM GROUND CHECKED N ORMAL OPS. 2 L 7 2 4F RT T00001SE 20081009 NM 2008 10 9 AALA200802089 1 20080813 A 3241 MANIFOLD BOEING 737 737823 13844BZ NM ANTI-SKID SYS DAMAGED A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 950AN 30087 IAD INFLIGHT T1060 13 AUG DFW TO DCA. CREW REPORTED ANTI SKID INDICATION INTERMITTENT. LANDED IAD WITHOUT INCIDENT. R EPLACED NR 4 MANIFOLD. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 USAA920081653 1 20080811 A 5330 6545769 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN C19 MAJOR REPAIR NR 6123258 FUSELAGE SKIN CRACKED AT AFT SATELLITE HOLE FOR RADIO ANTENNA MOUNT BS410, LBL1.5, BETWE EN S28R & S28L. REPAIRED FUSELAGE SKIN AT BS410, LBL1.5, BETWEEN S28R & S28L IAW AMERICA WEST AIRLINES TASK CARD NR M2A 53001. 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 QXEA200800659 1 20080609 A 5340 STRINGER CLIP BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK CORROSION ON FUSELAGE FRAME TO STRINGER CLIP AT STA X234.475 AND RT STR 29. REMOVED CLIP TO ACCESS CORROSI ON REMOVAL. FABRICATED NEW CLIP FROM .040 7075 T6 ALUM. PER DHC8 400 SRM 53-20-15 PG 13 ITEM 186 AND USING ORIGINAL AS TEMPLATE. MATCH DRILLED. ALODINED NEW CLIP IAW DHC8-400 SRM 51-21-10, PRIMED IAW DHC8-400 SRM 51-25-10. HFEC INSP. BE ND RAD. IAW -8 400 NDTM PART 6, 51-00-01 NO CRACKS NOTED. INSTALLED NEW CLIP IAW Q400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 20081009 EA 2008 10 9 QXEA200800680 1 20080612 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK NUMEROUS CORROSION SPOTS ON RT SIDE SEAT RAIL FS 861 TO 985. REMOVED CORROSION FROM SEAT TRACK AT FS 861 T O 985. .010 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 QXEA200800677 1 20080612 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK NUMEROUS CORROSION SPOTS ON RT SIDE SEAT RAIL FS 675 TO 713. REMOVED CORROSION FROM SEAT TRACK AT FS 675 T O 713. .010 MATERIAL REMOVED IAW REO 670-53-00-013. TREATED IAW REO 670-53-00-013. 2 L 7 2 4F RT A21EA 20081009 NM 2008 10 9 QXEA200800635 1 20080609 A 5320 INTERCOSTAL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK INTERCOSTAL SUPPORT FOR RT ELEVATOR QUADRANT HAS CORROSION ON LOWER FLANGE AROUND RIVET ENTIRE LENGTH OF IN TERCOSTAL BETWEEN FS X-64.400 AND 54 JUST IB OF STR 29R. REMOVED RIVETS ALONG INTERCOSTAL REF Q400 SRM 51-40-07 AND 51- 42-05. BLENDED CORROSION REF Q400 SRM 51-21-00. UT THICKNESS CHECK IAW -8 400 NDTM PT 1, 51-00-04. HFEC INSPECTED IAW -8 400 NDTM PT 6, 51-00-10 NO CRACKS NOTED. ALODINED, INSTALLED RIVETS AND APPLIED PRIMER AND PAINT. 2 H 7 2 4T RT A13NM 20081009 EA 2008 10 9 TRAX200801165 1 20080912 A 3350 COVER CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 908EV 7654 LIGHT COVER TO MAIN PAX DOOR EMERGENCY LIGHT EXIT IS BROKEN. REPAIRED LIGHT COVER TO MAIN PAX DOOR EMERGENCY LIGHT PER CRJ-200 33-51-01 A/C OK FOR SERVICE. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 TRAX200801166 1 20080912 A 3350 PLATE CNDAIR CL600 CL6002B19 1900309 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 826AS 7210 JOB 8721025 OPERATION 118 WARDROBE EMERGENCY EXIT FLOOR LEVEL FLOOR LIGHT BASE PLATE BROKEN. 2 L 7 2 4F RT A21EA 20081009 CE 2008 10 9 DXTA200803284 1 20080922 A 3240 PEDAL RAYTHN DH125 HAWKER800XP 7150012 CE BRAKE SYSTEM FAULTY E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 872QS 258472 LT BRAKE PEDAL ON PILOTS SIDE HAS NO PRESSURE GOES TO FLOOR WITH NO BRAKING AUTHORITY. 2 L 7 2 4F RT A3EU 20081009 CE 2008 10 9 DXTA200803281 1 20080921 A 2120 UNKNOWN CESSNA 500 560CESSNA 2076750 CE ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 07 345QS 5600445 ON TAKEOFF HAD STRONG ODOR OF HOT WIRE OR RUBBER. 2 L 7 2 4F RT A22CE 20081009 NM 2008 10 9 2008UALA05609 1 20080905 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE SEAT 1F MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 229UA 30557 SEAT 1F MISSING AFT EMERGENCY PATH EXIT LIGHT ASSY. REPLACED LIGHT ASSY, OPS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081009 NM 2008 10 9 2008UALA05611 1 20080906 A 3350 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 542UA 25276 NR 4 DOOR LT EMERGENCY EXTERIOR LIGHT INOP. RELAMPED, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081009 NM 2008 10 9 QXEA200800654 1 20080609 A 5311 ANGLE BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK FUSELAGE FRAME ANGLE HAS CORROSION AROUND 1 RIVET AT OTBD END LOCATED AT FS 98.000. REMOVED RIVETS AS NECE SSARY AND BLENDED CORROSION IAW Q400 SRM 51-42-05, 51-21-00, AND RD8/4-53-2344 STEPS 1&2. HFEC INSP IAW D8-Q400 NDTM PA RT 6 51-00-01, NO CRACKS NOTED. THICKNESS CHECK IAW NDTM PART 1 51-00-01, FOUND TO BE OUT OF LIMITS. MAPPED FOR ENGINE ERING. FOUND WITHIN LIMITS IAW RD8/4-53-2382. ALODINE PRIMED, INSTALLED RIVETS AND PAINTED IAW SRM 51-42-05. 2 H 7 2 4T RT A13NM 20081009 EA 2008 10 9 TRAX200801189 1 20080918 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 931EV 8015 JOB 8801521 OPERATION 152 PAX DOOR OUTER HANDLE IS CRACKED. RESOLVED ON W/O 100587 TASKCARD NR 00227 C/A PAX DOOR OUTER HANDLE BEING REPLACED UNDER 8801525/5771. REF THIS CARD FOR MTC ACTION. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 TRAX200801192 1 20080922 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 922EV 7822 LT SIDE EXT EMERGENCY LIGHTS FWD CENTER FUSELAGE INOP. RESOLVED ON W/O 101005 TASKCARD NR 00002. WORK COMPLETED IN COM PLIANCE WITH AMM R&R LT SIDE EMERGENCY LIGHT FWD CENTER OF FUSELAGE IAW CRJ 200 AMM 33-51-21. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 TRAX200801195 1 20080919 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 683BR 7692 JOB 8769211 OPERATION 193 RT FS 484, RBL 27 FLOOR SUPPORT STRUCTURE CLIPS ARE CRACKED 1/4". 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 TRAX200801198 1 20080919 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 931EV 8015 JOB 8801521 OPERATION 191 LT & RT 625 OBLIQUE ANGLES AREA CRACKED. RESOLVED ON W/O 100587 TASKCARD NR 00276. C/A REMOV ED DAMAGED RT & LT OBLIQUE ANGLES AND INSTALLED NEW SERVICEABLE RT & LT OBLIQUE ANGLES IAW CRJ 200 SRM 51-42-21. 2 L 7 2 4F RT A21EA 20081009 NM 2008 10 9 KCSA081490 1 20080925 A 5315 FLOORBEAM BOEING 747 747249F 1384849 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 MAIN DECK FLOORBEAM UPPER CHORD CORRODED AT BS 640, LBL 103. 2 L 7 4 4F RT A20WE 20081009 WP 2008 10 9 DHLA200800098 1 20080923 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A DHLA K NONE L NO TEST IN INSP/MAINT 1 GL 05 801DH 46033 EMERG LTS BATTERY DISCHARGED. REPLACED BATTERY PACK FOR EMER LTS PER MM 33-50-01 CHECKS SERV. NO FLT NR. ACFT WAS GRO UNDED. 2 L 7 4 4F RT 4A25 20081009 EA 2008 10 9 TRAX200801151 1 20080910 A 5320 PANEL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 682BR 7691 JOB 8769121 OPERATION 91 PANEL 281HZ HAS A CRACK 4" LONG. RESOLVED ON W/O 99838 TASKCARD NR 00273. C/A REMOVED THE 4 I N LONG CRACK ON PNL 281HZ USING AMS5510.032SS. INSTALLED REPAIR DOUBLER USING RTV106 AND CR3524-4 FASTENERS IAW REO 601 R-25-53-005. UPON FURTHER INVESTIGATION, FOUND 2 MORE AREAS OF COMPOSITE DAMAGE. REPAIRED THE 2 DAMAGED AREAS USING AM S5510.032SS. INSTALLED BOTH REPAIRED DOUBLERS USING RTV106 AND CR3524-4 FASTENERS IAW REO 601R-25-53-005. 2 L 7 2 4F RT A21EA 20081009 NM 2008 10 9 HNAA0800286 1 20080905 A 5610 STUD PPG DHAV DHC8 DHC8102 2809003 NM WINDSCREEN LOOSE A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 814EX 128 D899H1833 318 AT APPROX 16,000`, BURNING SMELL AND VISIBLE SMOKE COMING FROM RT SIDE OF MASTER CAUTION PANEL. CONTRACT MX FOUND WIRE AT L1 POSITION ON F/O`S WINDSCREEN BURNT. FOUND TERMINAL STUD LOOSE. DEACTIVATED W/S HEAT AND ISSUED MEL. ROA R&R F/O `S WINDSHIELD IAW WORKCARD 56-00-00R. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 20081009 NM 2008 10 9 HNAA0800287 1 20080922 A 3397 M2275916229 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A HNAA O OTHER O OTHER NR NOT REPORTED 1 EA 07 975HA 176 EMERGENCY LIGHT AT ROW 1F IS INOP. REPAIRED BROKEN WIRES AT RT FWD EMERGENCY DOOR LIGHT. OPS CHECK GOOD. OK FOR SERVI CE. 2 H 7 2 4T RT A13NM 20081009 EA 2008 10 9 HNAA0800291 1 20080915 A 3150 HA1555 WARN PANEL DHAV DHC8 DHC8311 1386006 EA COCKPIT FAULTY A HNAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 331EN 42599 279 SLIGHT SMELL OF BURNING WIRE INSULATION NOTED UPON ENGINE SHUT DOWN THAT LINGERS FOR 2 TO 3 MIN, THEN DISSIPATES. R&R C AUTION PANEL IAW 33-12-00 AFTER INSPECTING AREA OF SMELL. FOUND ODOR COMING FROM CAUTION PANEL, NO HIDDEN DAMAGE NOTED. ACFT OK FOR SERVICE. 2 H 7 2 4T RT A13NM 20081006 WP 2008 10 6 AALA200802121 1 20080816 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9628W 53598 LGA EMERGENCY LIGHT EXIT SIGN AT AIRSTAIRS SIDEWALL INOPERATIVE. SECURED CONNECTOR FOR INOPERATIVE EMERGENCY LIGHT EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081006 WP 2008 10 6 AALA200802116 1 20080816 A 2611 301840103 SMOKE DETECTOR DOUG DC9 DC982 3022082 WP CARGO BAY DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 440AA 49459 STL INFLIGHT T720/16AUG DFW TO LGA. CREW REPORTED AFT CARGO FIRE LIGHT ON ANNUNCIATOR. MASTER WARNING ON 1 TO 2 SECOND S THEN EXTINGUISHED. LANDED STL AS PRECAUTIONARY WITHOUT INCIDENT. REPLACED CARGO FIRE MX UNIT AND AFT CARGO SMOKE DET ECTORS. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081006 WP 2008 10 6 AALA200802119 1 20080816 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9628W 53598 LGA OVERHEAD EMERGENCY LIGHTS FROM AFT GALLEY TO SEAT 30D INOPERATIVE. REPLACED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS FROM AFT GALLEY TO SEAT 30D. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081007 GL 2008 10 7 CHQ2008F00004 2 20080830 A 7321 23063131 FUEL CONTROL EMB 135 EMB135KL 3260302 SO ALLSN AE3007 AE3007A 03030 GL NR 2 ENGINE FAILED A CHQA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 GL 11 379SK 17332 145606 CAE311971 FLIGHT 5346, STL TO MSY. WHILE ON DESCENT INTO MSY, AT APPROXIMATELY FL285 THE FLIGHT CREW NOTICED ABNORMAL INDICATIONS ON EICAS FROM E2. THE N1 INDICATIONS WERE INCREASE AND DECREASING RAPIDLY BUT WERE STAYING WITHIN LIMITS AS WELL AT TH E ITT. IT WAS ALSO NOTED THAT THE FADEC CHANNELS WERE COMMANDING IGNITION. AS THE FLIGHT CREW ATTEMPTED TO VERIFY THE CAUSE OF THE PROBLEM THERE WAS A FLAMEOUT ON E2, AT WHICH TIME ENG 2 OUT WAS DISPLAYED ON EICAS. THE APU WAS STARTED AN D QRH WAS FOLLOWED AND E2 WAS SUCCESSFULLY RESTARTED. THERE WERE NO FURTHER ABNORMALITIES DURING THE OPERATION OF E2 A ND THE ACFT LANDED WITHOUT INCIDENT. ON CALL MX AT MSY INSPECTED THE FADEC HARNESSES WITH NO FAULTS FOUND AND RAN THE E 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081007 NM 2008 10 7 YENA2008083 1 20080828 A 2782 1703909 ACTUATOR EMB ERJ190 ERJ190100IGW 3260408 NM L/E SLAT FAILED A YENA O OTHER O OTHER LD LANDING 1 EA 15 229JB 6357 19000032 FLT NR 293, SEA-LGB, SLAT FAIL ON APPROACH TO LGB, FOUND LT NR 5 SLAT ACTUATOR TRIPPED. R/R LT SLAT ACTUATOR IAW AMM 27 -81-01. PERFORMED SLAT CTL MECH RIGGING PER 27-80-00-820-801 & SLAT CTL ELEC RIGGING PER 27-80-00-820-802A/200. NO FAU LTS NOTED. OPS TEST OF SLAT CTL SYS CKS NORMAL AT THIS TIME. ACFT OK FOR SERVICE. 2 L 7 2 4F RT A57NM 20081007 NM 2008 10 7 UIEA200800324 1 20080926 A 5330 SKIN BOEING 747 7472D7B 1384803 NM ZONE 100 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 FUSELAGE STA 520 TO 740 AT STR 34L LAP JOINT SCRIBE LINE DAMAGE. REPAIRED IAW SERVICE REQUEST 1-963742727 APPROVED BY F AA FORM 8100-9 DATED 02 OCT 08 DETAILS OF WORK EO4753B206 & EO 4753B114. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 UIEA200800321 1 20080930 A 5330 SKIN BOEING 747 7472D7B 1384803 NM ZONE 200 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 BS 2181-2360 AT S12L/R LAP JOINT SCRIBE LINE DAMAGED. REPAIRED IN ACCORDANCE WITH SERVICE REQUEST 1-750626156 APPROVED BY FAA FORM 8100-9 DATED 30 SEP 2008, DETAILS OF WORK KEPT AT EO-4753B202 & EO-4753B114. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 DXTA200803252 1 20080828 A 3620 WARNING SYSTEM GULSTM 200 200 4500308 NM BLEED AIR SYS ACTIVATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 728QS 116 TAKE OFF ABORTED DUE TO RED BLEED AIR EICAS MESSAGE AND MASTER WARNING LIGHTS. 2 L 7 2 4F RT A53NM 20081007 NM 2008 10 7 KCSA081430 1 20080827 A 2810 SKIN BOEING 747 747249F 1384849 NM CENTER FUEL TANK CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 CORROSION ON CENTER TANK UPPER SURFACE STA-1160 RBL-80. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081432 1 20080827 A 5310 DOOR FRAME BOEING 747 747122 1384872 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STA-1315 STR-22R TO STR-25R DOOR FRAME CORRODED. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081438 1 20080901 A 3350 LIGHT BOEING 747 7472B4B 138481B NM CABIN DEFECTIVE A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 CENTER DOME EMERGENCY LIGHT COMES ON AND GOES BACK OUT AFTER 3 SEC. 2 L 7 4 4F RT A20WE 20081007 EA 2008 10 7 MAS2008F00072 1 20080823 A 4930 FUEL LINE CNDAIR CL600 CL6002B19 1900309 EA APU LOOSE A MASA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 154SF 7154 ASH FLT 7206 GSO. CAPTAIN REPORTED SMELL OF FUEL ON GROUND IN ORD WITH APU RUNNING. MX RE-SECURED LOOSE FUEL LINES. 2 L 7 2 4F RT A21EA 20081007 NM 2008 10 7 USAA920081640 1 20080904 A 5522 65C25746132A SKIN BOEING 737 7373B7 1384580 NM ELEVATOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT Q6 MAJOR REPAIR NR 03C71227004/001 AND NR 5030650. CRACK ON LOWER SURFACE OF RT ELEVATOR AT ELEVATOR STATION 24.90. REPLACED RT ELEVATOR IAW US AIRWAYS JOB CARD NR 03C71227004 AND 03C71127003. 2 L 7 2 4F RT A16WE 20081007 NM 2008 10 7 EIA2008041 1 20080828 A 5330 SKIN BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE FUSELAGE DAMAGED A EIAA O OTHER O OTHER NR NOT REPORTED 1 NM 19 485EV 20712 FUSELAGE AT BS 460-480 TOP BL O TO 5-IL, ANTENNA LOCATION SURFACE SKIN SUNK. REPAIRED PER SRM 51-30-02. 2 L 7 4 4F 4 F RT A20WE E20EA 20081007 NM 2008 10 7 EIA2008037 1 20080828 A 5320 FLOOR SUPPORT BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE FUSELAGE CRACKED A EIAA O OTHER O OTHER NR NOT REPORTED 1 NM 19 485EV 20712 MAIN DECK STATION 940 RBL 120 FLOOR PANEL SUPPORT CRACK. FABRICATED AND REPLACED IAW SRM 51-30-02. 2 L 7 4 4F 4 F RT A20WE E20EA 20081007 NM 2008 10 7 EIA2008035 1 20080828 A 5420 ANGLE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE NR 1 PYLON CRACKED A EIAA O OTHER O OTHER NR NOT REPORTED 1 NM 19 485EV 20712 NR 1 PYLON AT A7 NAL STATION 22/LOWER SURFACE OF MID SPAR WEB LT 1 EA ANGLE CRACKED. FAB NEW ANGLE PER DRW 65B90387. H EAT TREAT AND NDT. INSTALLED PER SRM 51-30-02. 2 L 7 4 4F 4 F RT A20WE E20EA 20081007 NM 2008 10 7 EIA2008034 1 20080828 A 3350 LIGHT BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE CABIN INOPERATIVE A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 19 485EV 20712 DURING EMG LT OPS TEST, FOUND V/D AFT CEILING EMERG. LT. INOP. REPLACED PER MM 33-51-00. 2 L 7 4 4F 4 F RT A20WE E20EA 20081007 SO 2008 10 7 RAIA00808022 1 20080824 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 841HK 145382 PRE FLT NR 7889 MKE CABIN EMERGENCY LIGHT INOPERATIVE. MX RESEATED THE CONNECTOR AT THE LIGHT ASSEMBLY. OPS CHECKED AS PER AMM PROCEDURES. 2 L 7 2 4T RT T00011AT 20081007 EA 2008 10 7 VNAA0808011 1 20080823 A 2130 VALVE CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF343B1 30070 NE CABIN PRESSURE MALFUNCTIONED A VNAA A UNSCHED LANDING O OTHER TO TAKEOFF 1 GL 05 723PS 10181 CREW REPORTED ACFT WOULD NOT MAINTAIN PRESSURE. CREW ELECTED TO RETURN TO DTW AND LANDED WITHOUT INCIDENT. MX INSPECTE D ACFT AND SECURED CLOSED GROUND VALVE. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20081007 2008 10 7 VNAA0808015 4 20080826 A 3451 S6553667L ANTENNA CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE DME SYSTEM UNSERVICEABLE A VNAA O OTHER O OTHER UK UNKNOWN 1 GL 05 703PS 10137 DURING SCHEDULED MX DAMAGE CAUSED BY POSSIBLE LIGHTNING STRIKE WAS NOTED. DME ANT WAS R&R ALONG WITH DAMAGE TO FUSELAGE REPAIRED. NO OTHER DAMAGE WAS NOTED AND THE ACFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E00063EN 20081007 EA 2008 10 7 VNAA0808016 1 20080829 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE WING MALFUNCTIONED A VNAA A UNSCHED LANDING F FLT CONT AFFECTED UK UNKNOWN 1 GL 05 250PS 7929 CREW REPORTED A FLAPS FAIL AT 20 DEG MESSAGE. CREW ELECTED TO RETURN TO JAN AND LANDED WITHOUT INCIDENT. MX INSPECTED ACFT AND NO DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20081007 EA 2008 10 7 VNAA0808014 1 20080826 A 5520 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE ELEVATOR DAMAGED A VNAA K NONE O OTHER UK UNKNOWN 1 GL 05 249PS 7926 CREW REPORTED A POSSIBLE LIGHTNING STRIKE AFTER LANDING AT XNA. MX INSPECTED AND REPAIRED DAMAGE TO THE ELEVATOR. NO O THER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20081007 SO 2008 10 7 RAIA00809001 1 20080902 A 3297 CONNECTOR EMB 145 EMB145 3260210 SO NLG BROKEN A RAIA K NONE J WARNING INDICATION CL CLIMB 1 CE 03 801HK 145053 FLT 3503 IND GEAR WOULD NOT RETRACT ALONG WITH AN AIR/GND FAIL MESSAGE ON THE EICAS. MX REPAIRED WIRING AT THE NOSE PRO XIMITY SWITCH CONNECTOR IAW AMM PROCEDURES. OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 20081007 NM 2008 10 7 USAA920081616 1 20080903 A 5330 6545775 SKIN BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 440US 24811 CLT MAJOR REPAIR LOG NR 4365477 - CRACK IN FUSELAGE SKIN AT BS727E, S24R. REPAIRED FUSELAGE SKIN AT BS727E, S24R, IAW B 737 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 20081007 NM 2008 10 7 USAA920081617 1 20080812 A 5312 6546568515 BULKHEAD BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN C19 MAJOR REPAIR NR 6124120 - CRACK IN DOME WEB AT BS 1016, S6L. REPAIRED DOME WEB AT BS 1016, S6L IAW EA NR 130098 . 2 L 7 2 4F RT A16WE 20081007 NM 2008 10 7 USAA920081618 1 20080812 A 5330 6552988 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 306AW 24633 MCN C19 MAJOR REPAIR NR 6124118 - CRACK IN FUSELAGE SKIN AT BS961, S17L. REPAIRED FUSELAGE SKIN AT BS961, S17L IAW B737 SRM 53-00-01-2R-32. 2 L 7 2 4F RT A16WE 20081007 EU 2008 10 7 USAA920081619 1 20080827 A 5540 D5537131800200 HINGE FITTING AIRBUS 320 A320232 3930326 EU RUDDER WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 660AW 1234 SAL BC6 MAJOR REPAIR NR 6091887 EXCESSIVE PLAY ON NR 3 RUDDER HINGE FITTING. REPLACED NR 3 RUDDER HINGE FITTING IAW A32 0 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081007 CE 2008 10 7 JBG2008F00003 1 20080904 A 2121 76008013 BLOWER LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE CABIN FAILED C JBGA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 11 360AN 7238 137 CA0109 THE ACFT WAS LEVELING OFF AT CRUISE ALTITUDE OF FL400 AFTER DEPARTING AND ENROUTE, WHEN THE CREW NOTED THE SMELL OF SMO KE AND SMOKE COULD BE SEEN COMING FROM THE AFT SECTION OF THE CABIN. THE CREW DECLARED AN EMERGENCY AND BEGAN A DECENT WHILE COMPLETING THE EMERGENCY CHECK LIST. ATC THEN GAVE THE CREW VECTORS, WHERE AN UNEVENTFUL LANDING WAS MADE WITH FIR E CREWS STANDING BY. THE CREW NOTED THAT DURING THE DESCENT AT FL250 THE SMOKE HAD DISSIPATED FROM THE CABIN. AFTER THE LANDING THE AC WAS INSPECTED AND THE CREW DETERMINED THERE WAS NO FIRE AND TAXIED THE AC TO A STANDING AREA FOR FURTHER INSPECTIONS WERE CARRIED OUT FOR PROBABLE CAUSE OF SMOKE AS WELL AS AN INSPECTION FOR OVERWEIGHT LANDING. THE CAUSE OF T 2 L 7 2 4F 4 F RT A10CE E35NE 20081007 2008 10 7 USAABB08144 4 20080902 A 3416 H150AKM1 INDICATOR BOEING 757 7572B7 1384964 NM COCKPIT INOPERATIVE A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 206UW 42339 27808 PHL FLT 798 ENROUTE PHL TO AMS. THE STANDBY ALTITUDE INDICATOR FAILED ABOUT 45 MINUTES AFTER DEPARTURE. THE DECISION W AS MADE TO RETURN TO PHL. THE FLIGHT RETURNED WITHOUT FURTHER INCIDENT. MX REPLACED THE STANDBY ALTITUDE INDICATOR. O PS CHECKS OK. 2 L 7 2 4F RT A2NM 20081007 NM 2008 10 7 USAA920081645 1 20080906 A 5754 6526602224 WEDGE BOEING 737 7374B7 1384702 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03C40257009/011 & 03C40257009/015 - NR 5 SLAT LOWER WEDGE DELAMINATED AT INBD AND OTBD END. REPA IRED NR 5 SLAT LOWER WEDGE AT INBD AND OTBD END IAW B737 SRM 51-70-10. 2 L 7 2 4F RT A16WE 20081007 NM 2008 10 7 USAA920081644 1 20080906 A 5320 6545812 ATTACH ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03C10753060/014 - WEB ATTACH ANGLE IS CRACKED AT BS328, RBL33. REPAIRED WEB ATTACH ANGLE AT BS32 8, RBL33 IAW B373 SRM 51-40-02 AND BOEING DRAWING NR 65-45812. 2 L 7 2 4F RT A16WE 20081007 NM 2008 10 7 USAA920081643 1 20080905 A 5311 65C25229 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03C10753039/007. FRAME CRACKED AT BS727D, BETWEEN S8R AND S9R. REPAIRED FRAME AT BS727D, BETWEE N S8R AND S9R IAW US AIRWAYS TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 20081007 NM 2008 10 7 USAA920081642 1 20080905 A 5320 65528941 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03C10753073/039 FLOOR SUPPORT CRACKED AT BS540, BLO TO LBL24. REPLACED FLOOR SUPPORT AT BS540, B LO TO LBL24 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081007 CE 2008 10 7 D382008F00000 1 20080829 A 2434 ALB20AS1 THRU BOLT CESSNA 421 421A 2076012 CE CONT O520 GTSIO520C 17032 SO RT ALT CASE HALF BROKEN E D38A O OTHER O OTHER NR NOT REPORTED 1 WP 27 421RM 22 421A0069 22.2 HOURS AFTER INSTALLING AN OVERHAULED (ALV9510) ALTERNATOR, THE PILOT CAME TO ME ABOUT A THRU BOLT THAT WAS COMING O UT OF THE ALTERNATOR CASE. THERE WAS ONE THRU BOLT STICKING OUT OF THE CASE AND ANOTHER HAD COME OUT AND WAS GONE. THE A LTERNATOR WAS CHARGING THE ELECTRICAL SYSTEM AND THERE WERE FOUR THRU BOLTS STILL IN PLACE. ALSO, THE OIL SEAL APPEARED TO HAVE FAILED. THERE WAS SOME OIL NOTED INSIDE THE ALTERNATOR CASE. THERE WAS NO DAMAGE INCURRED BY THE AC AND WARRANT Y REPLACEMENT ALTERNATOR WAS INSTALLED. (K) 1 L 7 2 3O 3 O A7CE E7CE 20081007 SO 2008 10 7 C2XA08TY090 1 20080825 A 5530 14540881001 BEARING EMB 145 EMB145XR 3260214 SO VERTICAL STAB CORRODED A C2XA K NONE O OTHER CR CRUISE 1 SW 27 16149 7569 145753 A/C WAS IN FOR A C-CHECK WHEN CORROSION WAS FOUND ON THE LT SPHERICAL BEARING. MX REMOVED THE CORROSION REMOVED SPHERI CAL HOUSING AND REAM TO THE 1ST OVERSIZE TO INSTALL A NEW BUSHION. REPLACED THE BEARING. INSTALL THE SPHERICAL BEARING AND PERFORMED ALL CHECKS. A/C WAS RELEASED AT THE CLOSE OF THE C-CHECK. ALL WORK WAS ACCOMPLISHED IAW EMB 145XR SRM 5 5-37-00, 55-30-02. 2 L 7 2 4F RT 20081007 NM 2008 10 7 NWAA084145640 1 20080902 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM CABIN DEFECTIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 540US 26487 DURING AN OVERNIGHT LINE CHECK THE EMERGENCY ESCAPE PATH LIGHTS FROM ROW 29 ON THE RT SIDE TO ROW 33 ON THE RT SIDE WERE INOPERATIVE. MX FOUND BATTERY PACK M10699 TO BE DEFECTIVE AND REPLACED IT. ALL OPS CHECKED NORMAL AFTER REPLACEMENT. 2 L 7 2 4F RT A2NM 20081007 WP 2008 10 7 NWAA084159997 1 20080903 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8933E 47142 DURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 11-13 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 2 L 7 2 4F A6WE 20081007 NM 2008 10 7 QXEA200800422 1 20080418 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK. CORROSION ON SEAT TRACK NR 1 AT APPROX. STA X360. REMOVED NR 4 SEAT TRACK IAW -8 200 SRM 51-40-00. DRIL LED UP AND INSTALLED NEW TRACK IAW -8 200 SRM 51-40-00, 51-40-11. 2 H 7 2 4T RT A13NM 20081007 NM 2008 10 7 QXEA200800419 1 20080418 A 5347 SEAT TRACK DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK. LT SEAT TRACK NR 2 HAS CORROSION AT APPROX STA 438 STA 466.5, STA 485, AND STA 498. REMOVED SEAT TRACK I AW -8 200 SRM 51-40-11. DRILLED UP AND INSTALLED NEW TRACK IAW -8 200 SRM 51-40-00, 51-40-11. 2 H 7 2 4T RT A13NM 20081008 NM 2008 10 8 AALA200802072 1 20080811 A 5610 WINDOW BOEING 737 737823 13844BZ NM COCKPIT CRACKED A AALA A UNSCHED LANDING O OTHER UK UNKNOWN 1 SW 21 913AN 29514 PLS INFLIGHT T1290/11 AUG STX TO MIA. CREW REPORTED LT NR 1 WINDOW CRACKED. LANDED PLS WITHOUT INCIDENT. REPLACED LT NR 1 WINDOW. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081008 2008 10 8 MWE2008F00042 4 20080924 A 2565 D29982225 SLIDE BOEING 717 717200 1383700 NM GALLEY AREA UNWANTED DEPLOY A MWEA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 GL 13 903ME 55167 FWD SERVICE DOOR EMERGENCY SLIDE IN UNARMED POSITION FROM BEING SECURED IN DOOR/COVER BRACKETS. FOUND EMERGENCY SLIDE D EPLOYED. REMOVED AND REPLACED EMERGENCY SLIDE. (K) 2 L 7 2 4F TR A6WE 20081008 WP 2008 10 8 AALA200802043 1 20080808 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 411AA 49322 LGA EMERGENCY LIGHTS AT OVERHEAD SEAT ROW 20 AND AFT LAVATORY INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD SEAT ROW 2 0 FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081003 NM 2008 10 3 2008UALA05932 1 20080929 A 2560 140N276218 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 553UA 25277 GIRT BAR DOOR 3R BROKE. INSTALLED NEW GIRT BAR. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081003 NM 2008 10 3 SWAA085268 1 20081001 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 338SW 23960 DURING SCHEDULED BRDG CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 667, LBL 24.8. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085270 1 20080928 A 3350 65C27093 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 286WN 32471 DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REPLAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085271 1 20080928 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500C + 16, STR 8R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085272 1 20080928 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 25L TO 26L. REPAIRED SHEAR TIE PER ER. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085273 1 20080928 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 309SW 22948 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 25L TO 26L. REPAIRED SHEAR TIE PER ER. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085278 1 20081001 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 450 LT TO 495 LT. REMOVED AND REPLACED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085279 1 20081001 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 500A + 6 RT. REMOVED AND REPLACED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085283 1 20080927 A 5240 65C26331 SKIN BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED OTS, FOUND R1 OUTER DOOR SKIN CRACKED ABOVE LOWER GUIDE ARM. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085286 1 20080928 A 3350 101114 LENS BOEING 737 7373H4 1384600 NM CABIN DETACHED A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 366SW 26577 DURING FLT EMERGENCY EXIT SIGN LEFT SIDE LENS DETACHED. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20081003 NM 2008 10 3 SWAA085295 1 20080930 A 3350 100031 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 483WN 32472 DURING SCHEDULED MV2 CHECK, FOUND L2 EMEGENCY EXIT DOOR LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081006 NM 2008 10 6 USAA920081588 1 20080819 A 5320 FLOOR SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 309AW 24711 MCN CORROSION MAJOR REPAIR NR 4420136 & 6124059 CORROSION ON FLOOR SUPPORT AT BS967, RBL8. REPLACED FLOOR SUPPORT AT BS 967, RBL8 IAW B737 SRM 51-40-02-0G. 2 L 7 2 4F RT A16WE 20081006 NM 2008 10 6 UDSS920081591 1 20080826 A 5754 65C26601168 SKIN BOEING 737 7373B7 1384580 NM L/E SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT Q6 MAJOR REPAIR NR 03C40257009/001 AREA OF DELAMINATION ON RT WING NR 6 SLAT TRAILING EDGE WEDGE LOWER SURFACE. REP LACED RT WING NR 6 SLAT IAW US AIRWAYS TASK CARD 03C40227004. 2 L 7 2 4F RT A16WE 20081006 NM 2008 10 6 ANCF200800019 1 20080818 A 4990 APU BOEING 767 767283ER 1385149 NM MALFUNCTIONED W ANCF A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SO 23 728CG 24728 AIR TURN BACK, EICAS MSG 02 "R GEN OFF" DISPLAYED, R GEN OFF LIGHT ILLUMINATED. GENERATOR SWITCH RESET DID NOT CORRECT C ONDITION. APU WAS TRANSFERRED TO DMI N. 247 BY MAINT REPORT P4264038-X3. : "APU FAIL". PERFORMED BPCU BITE TEST IAW FIM PROCEDURE 24-20-00, PG 180K. ACCOMPLISHED BOTH ENGINES RUN UP, ALL ELECTRICAL PARAMETERS WERE NORMAL. RT ENGINE IDG IS CONSIDERED OPERATIVE. SERVICED APU OIL TANK AS REQUIRED IAW AMM 12-13-04 PAGE 301, ACCOMPLISHED ERASE BITE PROCEDURE IAW FIM 49-11-01, PAGE 401. CHECKED APU OPERATION. WORKING PROPERLY. (K) 2 L 7 2 4F RT A1NM 20081006 NM 2008 10 6 C8G2008F00014 1 20080529 A 2150 2040751 ACM BOEING 727 727223 1384074 NM LEFT INOPERATIVE A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 29 715AA 22470 DURING CLIMB OPERATION, THE AC WAS UNABLE TO MAINTAIN CABIN ALTITUDE BELOW 10000 FEET WITH ONE PACK OPERATION. AC RETURN ED TO DEPARTURE, WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED LT ACM INOPERATIVE. REMOVED AND REPLACED LT ACM AND LT PACK SHUTOFF VALVE, OPS CHECK GOOD. NO OTHER DEFECTS NOTED. AC WAS RETURNED TO SERVICE 2 L 7 3 4F A3WE 20081006 NM 2008 10 6 QXEA200800403 1 20080418 A 5311 FRAME DHAV DHC8 DHC8202 2809007 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK SUSPECT CORROSION OF FRA X201 AT STR 31S. REMOVED CORROSION IAW CPM CHAP 4 PARA 9A-B(1-6(A)). UT THICKNES S CHECK IAW -8 200 NDTM PT 1, 51-00-04 HI .032 LOW .029. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01 NO CRACKS NOTED. AL ODINED PRIMED IAW -8 200 SRM 51-20-16, 51-20-36. 2 H 7 2 4T RT A13NM 20081006 EA 2008 10 6 QXEA200800944 1 20080827 A 5270 CC670322129 FITTING CNDAIR CL600 CL6002C10 1390015 EA NLG DOOR FAILED A QXEA O OTHER D INFLIGHT SEPARATION AP APPROACH 1 NM 19 611QX 10041 BUR FLIGHT 2559. ON APPROACH TO BUR, DURING GEAR EXTENSION THE CREW HEARD 3 LOUD BANGS. ACCOMPLISHED UNEVENTFUL LANDIN G. MX FOUND THE AFT NOSE GEAR DOOR DAMAGED AND HANGING BY THE BONDING STRAPS. THE AFT PIVOT BOLT LEFT SIDE SHEARED OFF AND THE RIGHT SIDE LOOSE. REMOVED DOOR AND FERRIED TO PDX FOR REPAIRS. BLENDED & REPAIRED DAMAGE. HFEC SHOWS NO CRAC KS. REPLACED LH FITTING AND DOOR. CHECKS GOOD. RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 20081006 CE 2008 10 6 26N2008F00003 1 20080929 A 2710 70611107 CONTROL CABLE CESSNA 510 510 2076617 CE AILERONS FROZEN E 26NA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 05 83EM 5100026 ON CLIMB OUT, AT 20,000 FT THE AILERONS FROZE WITH AN OAT OF 0 DEGREES C. PILOT WAS GETTING THE AMBER AP LIGHT. HE WOULD TURN THE AP "OFF" AND FREE UP THE CONTROLS ABOUT EVERY 15 TO 20 MINUTES BY EXERTING A LOSS OF FORCE TO FREE THE ICING. AT 33,000 FT WITH AN OAT OF -22 DEGREES, AND THE AP ENGAGED, THE ELEVATOR FROZE. PILOT SAID IT TOOK AN UNBELIEVABLE AMOU NT OF FORCE TO GET THE AC TO RESPOND. JUST LIKE BEFORE, HE WAS CONTROLLING THE AC WITH ENGINES AND TRIM. AT 6,000 FT, O N APPROACH, HE WAS USING ELEVATOR TRIM TO CONTROL THE AC AND ALMOST MAX'D IT OUT. AC IS AT SERVICE CENTER AND ARE LOOKIN G FOR THE POSSIBLE CAUSES OF THE FREEZING. WE ARE FOCUSING ON WATER INTRUDING THE TAILCONE AND GETTING ON THE AILERON AN 1 L 7 2 4F RT A00014WI 20081006 EA 2008 10 6 TRAX200801057 1 20080825 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 932EV 8016 JOB 8801621 OPERATION 63 RH 621 OBLIQUE ANGLE CRACKED. THIS SDR WILL REMAIN OPEN PENDING MX DETERMINATION OF AN APPROPRI ATE CORRECTIVE ACTION. 2 L 7 2 4F RT A21EA 20081006 2008 10 6 COEA0803912 4 20080905 A 3440 457400TB0811 INDICATOR AEROSP ATR42 ATR42300 8680920 EU VSI/TCAS FAILED A COEA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 NM 13 912FX 047 AIR TURN BACK, ENROUTE, THE CAPT`S VSI FLASHED MOMENTARILY CAUSING A TCAS FAIL AND RESOLUTION ALERT, THEN WENT BLANK. SI NCE THE COPILOT`S SYSTEM WAS OPERATING NORMALLY. A DECISION TO RETURN TO DEPARTURE WAS MADE SINCE PARTS WERE AVAILABLE T HERE AND MAINTENANCE ALSO COULD BE ACCOMPLISHED. REMOVED AND REPLACED CAPT`S VSI/TCAS INDICATOR. (K) 2 H 7 2 4T RT A53EU 20081006 NM 2008 10 6 KNN2008F00002 1 20080909 A 5312 BULKHEAD BOEING 737 737291 138448W NM BS 178 CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 977UA 21508 WHILE COMPLYING WITH AD 2000-05-29 PARA (A) DURING THE CURRENT C-CHECK, WE FOUND MULTIPLE CRACKS ON THE FWD PRESSURE BUL KHEAD AT STA 178. DAMAGE WAS CUTOUT AND REPAIRED IAW SRM 53-10-10 FIG 1. (K) 2 L 7 2 4F A16WE 20081006 EA 2008 10 6 TRAX200801062 1 20080826 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 932EV 8016 JOB 8801621 OPERATION 197 RH FS 621 FLOOR SUPPORT ANGLE IS CRACKED, APPROX .25" LONG. THIS SDR WILL REMAIN OPEN PENDING MX DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. 2 L 7 2 4F RT A21EA 20081006 EA 2008 10 6 TRAX200801067 1 20080828 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 710EV 10071 BOTH AFTMOST CEILING EMERGENCY LIGHTS INOP. RESOLVED ON W/O 98211 TASKCARD N/R 00006. RELAMPED BOTH AFT MOST CABIN CEI LING EMERGENCY LIGHTS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20081006 WP 2008 10 6 IXX2008F00091 1 20080829 A 2910 AE2463532J0970 HOSE DOUG DC8 DC871F 302199D WP HYD SYSTEM LEAKING A IXXA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 11 825BX 45978 AT TOP OF DECENT, THE ACFT LOST HYDRAULIC FLUID DOWN TO THE STAND PIPE. MAINT INSPECTED AND FOUND NR 3 ENGINE HYDRAULIC PUMP HOSE LEAKING, REPLACED NR 3 ENGINE HYDRAULIC PUMP HOSE. OPS CHECK GOOD IAW MM 29-16. AC WAS RETURNED TO SERVICE. (K) 2 L 7 4 4F RT 4A25 20081006 EU 2008 10 6 COEA0803919 1 20080822 A 5330 S53671205204 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DAMAGED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 919FX 266 MAJOR REPAIR: DAMAGE TO AFT LT DOOR AND FUSELAGE. IMPACT DAMAGE TO LT AFT FUSELAGE SKIN DOUBLER PLATE AFT OF AFT PASSEN GER DOOR. FUSELAGE SKIN DENTED WITH CRACKING FOUND AT ONE FASTENER. FUSELAGE SKIN DAMAGED AREA CUT OUT AROUND CRACKED FA STENER HOLE AND DOUBLER. (K) 2 H 7 2 4T RT A53EU 20081006 NM 2008 10 6 KCSA081447 1 20080907 A 3350 LIGHT BOEING 747 747221F 1384868 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 748CK 21744 UPPER DECK EMERGENCY LIGHT INOPERATIVE ABOVE STAIRS. WILL NOT GO OUT. (K) 2 L 7 4 4F RT A20WE 20081006 2008 10 6 GLB2008F00021 4 20080826 A 6122 CONNECTOR BEECH 1900 1900D 1154162 CE PCB LOOSE A GLBA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 21 211GL UE211 SUSPECTED AUTOFEATHER EVENT, UPON APPROACH, PILOTS REPORTED THAT RT AUTOFEATHER ACTUATED (AS IT NORMALLY DOES DURING TES TING) ON APPROACH AFTER A MINOR POWER INCREASE. MAINT REMOVED AND REPLACED THE OVERSPEED GOVERNOR IAW MM 61-20. OPS CHE CK WAS GOOD, HOWEVER, IT DID NOT FIX THE DISCREPANCY. MAINT REMOVED AND REPLACED THE PRESSURE SWITCH PN 50-389121-4 IAW MM 61-21. SWITCH OPS CHECK GOOD, BUT DID NOT FIX THE DISCREPANCY. MX FOUND LOOSE SOCKET ON PCB A123 CONNECTOR. SECURED SOCKET, SYSTEM OPERATIONALLY CHECKED GOOD IAW MM 61-20. OPS CHECK FLIGHT WAS PERFORMED AND WAS SATISFACTORY. (K) 2 L 7 2 4T RT A24CE 20081006 2008 10 6 C8G2008F00016 2 20080826 A 7310 LINE BOEING 727 727227 1384078 NM ENGINE FUEL LEAKING A C8GA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 29 308AS 22002 ON ROTATION THE NR 3 ENGINE FAILED. THE CREW PERFORMED APPROPRIATE CHECKLIST. AN EMERGENCY WAS DECLARED AND THE AC RETUR NED WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED, IT WAS NOTED THAT THE FUEL FEED LINE TO THE P & D VALVE WAS LEAKING. THE PACKING WAS REPLACED AND THE LINE SECURED. OPERATIONAL AND LEAK CHECKS WERE PERFORMED SATISFACTOR ILY. NO OTHER DEFECTS WERE NOTED. AC WAS RETURNED TO SERVICE. (K) 2 L 7 3 4F A3WE 20081006 SO 2008 10 6 C2X2008F00022 1 20080902 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 16987 145261 DURING ROUTINE MAINT THE EMERGENCY EXIT SIGN ON AFT GALLEY WALL WAS FOUND INOPERATIVE. MAINT INSPECTED AND REPLACED THE NR 2 INVERTER. OPERATIONAL CHECKS WERE GOOD. (K) 2 L 7 2 4T RT T00011AT 20081007 NM 2008 10 7 UIEA200800323 1 20081002 A 5330 SKIN BOEING 747 7472D7B 1384803 NM ZONE 100 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 526MC 22337 FUSELAGE SCRIBE LINE OVERLAPPED SKIN BETWEEN BS 520-560 AT S34R DAMAGED. REPAIRED IN ACCORDANCE WITH SERVICE REQUEST 1- 751139526 APPROVED BY FAA FORM 8100-9 DATED 02 OCT 2008, DETAILS OF WORK KEPT IN EO-4753B204 & EO-4753B114. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081437 1 20080901 A 5320 TENSION TIE BOEING 747 747122 1384872 NM FUSELAGE BUCKLED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STA 1520-1540 ABOVE STR 36R FRAME TENSION TIE BUCKLED. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081436 1 20080901 A 5330 SKIN BOEING 747 747122 1384872 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 CORROSION ON RT SIDE OF EMPENNAGE SKIN, BS 2484, WL 216. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 MAS2008F00062 1 20080821 A 7830 THRUST REVERSER BOEING 777 7772Q8 1385238 NM RT ENGINE DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 745AM 32718 DURING TRANSIT CHECK WAS DETECTED THE OUTBOARD REVERSER OF THE RT ENGINE WITH EXTENDED DAMAGE ON FAN DUCT INNER WALL WIT H MATERIAL MISSING OF 70 X 60 INCH BY IMPACT OF THE BOROSCOPE L PLUG, THE ACFT WAS SENT TO HANGAR FOR REVERSER REPLACEME NT WHICH WILL BE SENT AS A SUPPLEMENT. 2 L 7 2 4F RT T00001SE 20081007 EA 2008 10 7 MAS2008F00074 1 20080824 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 17231 7231 ASH 2704 PHX LOWER OVERWING EXIT LT INOP. MX RESECURED A LOOSE CONNECTOR ONT HE LIGHT ASSY. 2 L 7 2 4F RT A21EA 20081007 SO 2008 10 7 RAIA00080829 1 20080825 A 2810 2810051104 RELIEF VALVE EMB 145 EMB145LR 3260212 SO LT WING LEAKING A RAIA K NONE K FLUID LOSS CL CLIMB 1 CE 03 823HK 4074 145475 FLT NR 7878 STL DURING CLIMB CREW MADE REPORT THAT FUEL WAS LEAKING FROM THE LT WING FUEL VENT. MX R&R THE LEFTHAND VEN T RELIEF VALVE AS PER AMM PROCEDURES. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081007 SO 2008 10 7 RAIA00808023 1 20080824 A 2131 22250N030201 CONTROLLER EMB 145 EMB145LR 3260212 SO CABIN PRESSURE MALFUNCTIONED A RAIA K NONE O OTHER CL CLIMB 1 CE 03 829HK 16287 145281 FLT NR 5500 STL DURING CLIMB ACFT AUTO AND MANUAL PRESSURIZATION FAILED. MX R&R THE DIGITAL CONTROLLER. OPS CHECKED GO OD ON THE GROUND. 2 L 7 2 4T RT T00011AT 20081007 NM 2008 10 7 MWE2008F00041 1 20080908 A 2611 CBAB110001 SMOKE DETECTOR BOEING 717 717200 1383700 NM LT LAVATORY FAILED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 919ME 55181 LT LAVATORY SMOKE DETECTOR DID NOT WORK DURING FUNCTION TEST. REMOVED AND REPLACED SMOKE DETECTOR. (K) 2 L 7 2 4F TR A6WE 20081007 EU 2008 10 7 USAA920081625 1 20080903 A 3350 1012887 BRACKET AIRBUS A321 A321211 3930370 EU CABIN BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 177US 1517 FLT NR 780 SPO-CLT-EEL BRACKET IS BROKEN ON SEAT 9D FLOOR LEVEL EMERGENCY LIGHT. MX REINSTALLED LOOSE BRACKET AND REPLA CED BROKEN EMERGENCY LIGHT FIXTURE. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081007 EA 2008 10 7 TRAX200801083 1 20080822 A 5315 STRIP CNDAIR CL600 CL6002B19 1900309 EA FLOORBEAM BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 970EV 7527 JOB 8752721 OPERATION 251 LBL 27 FLOOR BEAM FILLER STRIP BETWEEN FS 574 TO FS 621 IS BROKEN IN SEVERAL PLACES. REMOVED BROKEN LBL 27 FLOOR BEAM FILLER STRIP BETWEEN FS 576 TO 621 AND INSTALLED NEW SERVICEABLE FILLER STRIP IAW CRJ 200 SRM 5 1-41-04. 2 L 7 2 4F RT A21EA 20081007 CE 2008 10 7 V0J2008F00001 1 20080909 A 7120 8912149 SUPPORT CESSNA 680 680CE 2076811 CE PWC PW306 PW306C 52169 NE ENGINE DAMAGED E V0JA O OTHER O OTHER NR NOT REPORTED 1 EA 03 227DH 6800086 ELECTRICAL ARC FROM GROUNDING STUD ON ENGINE SUPPORT FRAME TO SUPPORT FRAME ITSELF. THE SUPPORT FRAME WAS REPLACED WITH NEW IMPROPER BONDING BETWEEN LUG AND SUPPORT FRAME APPEARS TO BE THE CAUSE OF THE ARCING DAMAGE TO THE FRAME. (K) 2 L 7 2 4F 4 F RC T00012WI E35NE 20081007 2008 10 7 C8G2008F00015 4 20080823 A 3442 20412151101 INDICATOR BOEING 727 727225 1384077 NM WX RADAR INOPERATIVE A C8GA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 29 755DH 21857 AFTER TAKEOFF FOUND RADAR UNSUITABLE FOR FLIGHT OPERATIONS INTO KNOWN CONVECTIVE ACTIVITY. ON ROTATION WX RADAR DOES NOT STABILIZE REGARDLESS OF PITCH KNOB SELECTION, RADAR SHOWS COMPLETELY COVERS SCREEN. DURING CRUISE RADAR INDICATES FALSE TARGETS ON ALL PITCH SETTINGS. AC RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFOR MED. REMOVED AND REPLACED NR 2 VERTICAL GYRO, RADAR ANTENNA AND RADAR INDICATOR. OPS CHECKS WERE SATISFACTORY. AC WAS RE TURNED TO SERVICE. NO OTHER DEFECTS WERE NOTED. (K) 2 L 7 3 4F A3WE 20081007 NM 2008 10 7 C772008F00001 1 20080828 A 5210 17068393001 COUNTERBALANCE EMB ERJ170 ERJ170200LR 3260121 NM LT PASS DOOR INOPERATIVE A C77A O OTHER O OTHER NR NOT REPORTED 1 EA 27 602CZ 2889 17000171 L1 DOOR WAS FOUND TO BE HARD TO OPEN AFTER FLT 2068 ON 8/27//2008. FOUND COUNTERBALANCE RODS WEAK IN L1 DOOR. WILL BE RE PLACING WITH NEW ONE. (K) 2 L 7 2 4F RT A56NM 20081007 WP 2008 10 7 BKA2008F00000 2 20080827 A 7200 31021802 ENGINE MTSBSI MU2 MU2B60 5780460 CE GARRTT TPE331 TPE33110 01514 WP RIGHT SHUTDOWN E BKAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 13 8083A 3007 739SA P20086C DEPARTING , THE RT ENGINE BETA LIGHT CAME ON SHORTLY AFTER TAKEOFF. LOSS OF OIL PRESSURE WAS NOTED, THE OIL PRESSURE DID NOT DROP BELOW THE RED LINE BUT WAS IN THE YELLOW ARC. IAW EMERGENCY CHECK LIST RT ENGINE WAS SHUT DOWN, DECLARED EMERG ENCY AND RETURNED TO DEPARTURE. (K) 1 H 7 2 3T 4 T RT A10SW E4WE 20081007 NM 2008 10 7 QXEA200800424 1 20080418 A 5230 CASTING DHAV DHC8 DHC8202 2809007 NM CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK. FWD CORNER CASTING ON MCD HAS CORROSION AROUND NUTPLATE, TOP AND BOTTOM. REMOVED FWD CORNER MCD CASTINGS AND INSTALL NEW CASTING REF -8 200 SRM 51-40-00 AND 51-40-11. 2 H 7 2 4T RT A13NM 20081007 EA 2008 10 7 QXEA200800444 1 20080421 A 5320 CROSSBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 608QX 10026 PFD C4 CHECK FOUND LIGHT CORROSION ON 280 CROSSBEAM. REMOVED LIGHT CORROSION ON 280 CROSSBEAM. REMOVED .002 INCH WITHI N LIMITS IAW REO 670-53-11-046. PRIMED EXPOSED AERAS IAW SRM 51-25-06 APPLIED TOPCOAT PAINT IAW SRM 51-25-16. 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 QXEA200800445 1 20080421 A 5320 ANGLE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 608QX 10026 PFD C4 CHECK FORWARD ANGLE FOUND TO BE CORRODED AT FS 280. REMOVED FORWARD ANGLE AT FS 280 IAW 51-42-06. LOCATED HOLES ON NEW ANGLE FWD AT FS 280 IAW SRM 51-40-11. INSTALL FWD ANGLE IAW SRM 51-42-06. PRIMED RIVETS IAW SRM 51-25-06 AND AP PLIED PAINT TO RIVETS IAW SRM 51-25-16. 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 QXEA200800446 1 20080421 A 5730 PANEL CNDAIR CL600 CL6002C10 1390015 EA WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 608QX 10026 RFD C4 CHECK PANEL 584ET HAS CHAFFING. BLENDED PANEL 584ET FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 57-52-02. REMOVED .005 MATERIAL FROM PANEL 584ET IAW CRJ 700 SRM 57-52-02. PRIMED PANEL 584ET IAW CRJ 700 SRM 51-25-06, PAINTED PANEL WI TH 8003/B707 IAW CRJ 700 SRM 51-25-01. 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 QXEA200800447 1 20080421 A 5730 PANEL CNDAIR CL600 CL6002C10 1390015 EA WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 608QX 10026 RFD C4 CHECK PANEL 584HT HAS CHAFFING. BLENDED PANEL 584HT FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 57-52-02. REMOVED .004 MATERIAL FROM PANEL 584HT IAW CRJ 700 SRM 57-52-02. PRIMED PANEL 584HT IAW CRJ 700 SRM 51-25-06, PAINTED PANEL WI TH 8003/B707 PAINT IAW CRJ 700 SRM 51-25-01. 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 QXEA200800558 1 20080502 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 613QX 10045 RFD C4 CHECK RT FS 280 BEAM CORRODED. REMOVED LT FS 280 BEAM IAW CRJ 700 SRM 51-42-06 AND 51-42-13. PERFORMED LPI ON L T 280 CROSSBEAM IAW CRJ 700 NDTM 51-20-008 NO DEFECTS NOTED. LOCATED HOLES IN NEW BEAM AND INSTALLED BEAM IAW CRJ 700 S RM 51-40-11, 51-42-07, 51-42-14, 51-42-22, 51-42-21 AND 51-23-02. 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 QXEA200800559 1 20080502 A 5210 SEAL CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 613QX 10045 RFD CR CHECK LOWER FWD STRIKER SEAL FOR PAX DOOR SCRATCHED. BLENDED DAMAGE IAW REO 670-53-21-348. PERFORMED EDDY CURRE NT IAW REO 670-53-21-348. ALODINE PRIMED AND PAINTED IAW CRJ 700 SRM 51-21-11, 51-25-06 AND 51-25-01. 2 L 7 2 4F RT A21EA 20081007 NM 2008 10 7 QXEA200800956 1 20080902 A 3260 401020101 UPLOCK SENSOR BOMBDR DHC8 DHC8402 1390042 NM RT MLG FAULTY A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 19 401QX 4031 PDX FLIGHT 2427. ON DESCENT AT 265 KNOTS THE RT MAIN GEAR DOOR AND UNSAFE LIGHTS ILLUMINATED FOR A MOMENT. THERE WAS A YAWING MOTING ASSOCIATED WITH THE INDICATION. MX REPLACED THE RT UPLOCK PROX SENSOR AND ADJUSTED THE LT UPLOCK PROX SE NSOR. CHECKS GOOD. ACFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081007 EU 2008 10 7 NWAA084163247 1 20080826 A 5320 BUTTSTRAP AIRBUS 320 A320212 3930322 EU FUSELAGE DENTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 347NW 408 DURING GROUND OPS FR 24 BUTT SPLICE STRAP WAS DENTED AT S35L. REPAIRED PER EA 32-213810. 2 L 7 2 4F RT A28NM 20081007 NM 2008 10 7 AALA200802067 1 20080810 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 DFW EMERGENCY LIGHT AT SEAT 25D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 25D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081007 NM 2008 10 7 AALA200802065 1 20080810 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 DFW EMERGENCY LIGHT AT SEAT 23D MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081007 NM 2008 10 7 AALA200802064 1 20080810 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 DFW EMERGENCY LIGHT AT SEAT 23D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081007 NM 2008 10 7 AALA200802062 1 20080810 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 760AN 31477 DFW EMERGENCY LIGHT AT SEAT 26G MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081007 NM 2008 10 7 AALA200802058 1 20080809 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW EMERGENCY LIGHT AT SEAT 36C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 36C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081007 NE 2008 10 7 CNM2008F00002 2 20080921 A 7230 COMPRESSOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650* 30018 NE NR 3 ENGINE STALLED A CNMA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 07 270AX 48318 517234 DURING CRUISE AT FL 300 NR 3 ENG COMPRESSOR STALLED N1 DROPPED TO APPROXIMATELY 70 PERCENT VIBRATION FELT IN NR 3 THROTT LE/ FUEL LEVEL/ FIRE HANDLE AS WELL AS AIRFRAME. (K) 2 L 7 3 4F 4 F A22WE E23EA 20081008 NE 2008 10 8 AALA200802042 2 20080808 A 7260 GEARBOX DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 2 ENGINE FAILED A AALA A UNSCHED LANDING E Y VIBRATION/BUFFET ENGINE STOPPAGE CR CRUISE 1 SW 21 464AA 49594 708176 TUL INFLIGHT T1009/08AUG SDF TO DFW. CREW REPORTED NR 2 ENGINE VIBRATIONS AND ENGINE PRESSURE RATION FLUCTUATION FOLLOW ED BY NR 2 ENGINE UNCOMMENTED SHUTDOWN. LANDED TOOL WITHOUT INCIDENT. REPLACED NR 2 ENGINE ON 10 AGUE AT TOOL DUE TO G EAR BOX FAILURE. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F 4 F A6WE E9NE 20081008 WP 2008 10 8 AALA200802040 1 20080808 A 3233 39281375001 RETRACT CYLINDER DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 21 458AA 49563 DFW INFLIGHT T1032/08AUG. CREW REPORTED NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED TO DFW AND LANDED WITHOUT INCIDE NT. REPLACED RETRACT CYLINDER AND BUNGEE CYLINDER. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081008 NM 2008 10 8 AALA200802038 1 20080807 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 378AN 25447 DFW EMERGENCY LIGHT AT SEAT 36B INOPERATIVE. REPLACED LAMP FOR INOPERATIVE EMERGENCY LIGHT AT SEAT 36B. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081008 NM 2008 10 8 KCS2008F00010 1 20080913 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 L-5 DOOR SILL EMERGENCY EXIT LIGHTS INOPERATIVE. (K) 2 L 7 4 4F RT A20WE 20081006 EA 2008 10 6 TRAX200801044 1 20080823 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 713EV 10081 LOWER EXIT LIGHT AFT OF SERVICE DOOR HAS SEVERAL INOP BULBS. (RESOLVED ON W/O 98983 TASKCARD: N/R 00010) RELAMPED LOWER EMERGENCY EXIT LIGHT ASSY IAW CRJ 700 AMM 33-51-05. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20081006 CE 2008 10 6 GLB2008F00019 1 20080902 A 5311 FRAME BEECH 1900 1900D 1154162 CE FS 164.4 S9AR CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 21 211GL 26807 UE211 DURING STRUCTURAL INSPECTION MAINT FOUND FRAME CRACKED AT STRINGER CUTOUT AT FS 164.4 STRINGER 9AR. LENGTH OF CRACK APPR OXIMATELY .5 INCH. OPEN (K) 2 L 7 2 4T RT A24CE 20081006 WP 2008 10 6 U2R2008F00004 1 20080825 A 5713 STRINGER DOUG DC8 DC871F 302199D WP RT WING CRACKED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 872SJ 83402 46040 DURING C-CHECK INSP, FOUND RT WING X RS NR 4 MAIN FUEL TANK STRINGER 58 HAS 2 INCH TRANSVERSAL CRACK BY ACCESSORY PANEL NR 5050. (K) 2 L 7 4 4F RT 4A25 20081006 SO 2008 10 6 C2X2008F00043 1 20080907 A 3397 7287500603 WIRE HARNESS EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 13936 145025 DURING PREFLIGHT INSP THE CREW REPORTED A SMOKE ODOR COMING FROM SEATS 3 & 4A. THE ACFT WAS RELEASED ON MEL 33-20-00 CAT C CTL NR 153947. THE AC LANDED, WHERE MAINT REMOVED AND REPLACED THE LIGHT SOCKET HARNESS ASSY AT ROW 4A, OPERATIONALLY CHECKED WITH NO DEFECTS, REMOVED THE MEL, AND THE AC WAS APPROVED FOR RETURN TO SERVICE. (K) 2 L 7 2 4F RT T00011AT 20081007 NM 2008 10 7 USAA920081639 1 20080903 A 5330 654576987 SKIN PANEL BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CLT Q6 MAJOR REPAIR NR 03-0553-8-0364/008 AND NR 5030674. CRACK IN FUSELAGE SKIN AT BS520, WL 198.5. REPAIRED FUSELAGE SKIN AT BS520, WL198.5 IAW US AIRWAYS EA NR 100609. 2 L 7 2 4F RT A16WE 20081007 NM 2008 10 7 USAA920081633 1 20080904 A 5755 654645170A SKIN BOEING 737 7374B7 1384702 NM NR 6 SPOILER DELAMINATED A USAA K NONE O OTHER NR NOT REPORTED 1 EA 19 456UW 25020 CLT C4 MAJOR REPAIR NR 03C30057003/043 NR 6 SPOILER DELAMINATED ON UPPER SURFACE. REPLACED NR 6 SPOILER IAW B737 AMM 27 -61-11. 2 L 7 2 4F RT A16WE 20081007 NM 2008 10 7 USAA920081614 1 20080829 A 5313 654988628 STRINGER BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 311AW 24712 MCN C18 MAJOR REPAIR NR 6124275 STRINGER CRACKED AT BS380, S15L. REPAIRED STRINGER AT BS380, S15L OAW B737 SR, 53-30-03 -2R1. 2 L 7 2 4F RT A16WE 20081007 NM 2008 10 7 ABXA080232 1 20080819 A 2510 824250611 SEAT BOEING 767 767232 1385132 NM COCKPIT DEFECTIVE A ABXA K NONE O OTHER LD LANDING 1 GL 23 739AX 1113 22216 CAPTAINS ELECTRICAL SEAT UNOP. FORE AND AFT, UP AND DOWN, SEAT LOCK RELEASED WHEN APPLYING BRAKES ALLOWING SEAT TO SLID E AFT UNCONTROLLABLY. REPLACED CAPTAINS SEAT WITH SERVICEABLE UNIT. OPS CHECK OK. IAW B767 MM 25-11-02. 2 L 7 2 4F RT A1NM 20081007 2008 10 7 ABXA080233 4 20080821 A 3421 258733512 VERTICAL GYRO DOUG DC9 DC932 3022066 WP E&E BAY DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 900AX 5695 47380 A COUPLE OF MINUTES AFTER GYRO FLAG, THERE WAS A STRONG ELECTRICAL HOT SMELL IN THE COCKPIT. REPLACED NR 2 VERTICAL GYR O IAW DC9 MM 34-27-00-2. INSPECTED WIRING AND CANNON PLUGS. NO EVIDENCE OF OVERHEAT CONDITION. RAN V.G. FOR 2 MINUTES WITH NO EVIDENCE OF ELECTRICAL OR HOT SMELL. 2 L 7 2 4F A6WE 20081007 NE 2008 10 7 SIMA200824101 2 20080826 A 7320 23063131 FMU SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE NR 1 ENGINE MALFUNCTIONED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 240DS 340B240 ON FLIGHT 3576 CREW REPORTED ENGINE 1 POWER FLUX N1 ITT, N2, IGNITION A&B AUTO RELIGHT AND FADEC TRANSFER IN FLIGHT FOR ABOUT 39 SECONDS. THRUST SURGED UP/DOWN CONTINUED FROM ABOVE TRUST LEVERS AT FLT IDLE. ENGINE 1 STABILIZED. NO ABNORM AL INDICATIONS AFTERWARDS. NO EICAS MESSAGES. ACFT REMOVED FROM SERVICE. C/A R&R FPMU AND OPS CHECKED GOOD. FCF PASS ED. ACFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 20081007 EA 2008 10 7 SIMA200824602 2 20080829 A 7200 AE3007A13 ENGINE EMB 135 EMB135LR 3260305 SO RROYCE AE3007 AE3007A13 54166 EA LEFT MALFUNCTIONED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 701MH 6650 145162 CAE312893 ON FLIGHT 4739 CREW REPORTED DURING CRUISE AND DESCENT THE SMELL OF BURNING OIL COMING FROM PACKS. ACFT REMOVED FROM SE RVICE. R&R LT ENGINE. IAW EMB WORK CARD NR 71-000-00. OPS CHECKED GOOD AND LEAK CHECK GOOD. ACFT RETURNED TO SERVICE . 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081007 NM 2008 10 7 F3LA200800592 1 20080904 A 5321 D5367402000000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 929FR 26 2240 REFERENCE NON ROUTINE C050372. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL I51FF WAS PUNCTURED. MX REPAIRED C ARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081007 NM 2008 10 7 F3LA200800594 1 20080904 A 5321 D5367303600000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 929FR 26 2240 REFERENCE NON ROUTINE C050375. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL 161CF WAS PUNCTURED. MX REPAIRED C ARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081007 NM 2008 10 7 F3LA200800595 1 20080904 A 5321 D5367313300000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 929FR 26 2240 REFERENCE NON ROUTINE C050457. DURING C3 C-CHECK INSPECTION NOTED TRANSITION PANEL 131EG WAS PUNCTURED. MX REPAIRED CA RGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION O F THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081007 NM 2008 10 7 F3LA200800596 1 20080904 A 5321 D5367301100000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 929FR 26 2240 REFERENCE NON ROUTINE C050458. DURING C3 C-CHECK INSPECTION NOTED TRANSITION PANEL 131CF WAS PUNCTURED. MX REPAIRED CA RGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION O F THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081007 NM 2008 10 7 FELA200800597 1 20080904 A 5321 D5367180500400 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 929FR 26 2240 REFERENCE NON ROUTINE C050515. DURING C3 C-CHECK INSPECTION NOTED FLOOR PANEL 261FF HAS CORROSION ON LOWER SURFACE. MX R&R FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-12 PB 401. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081007 EA 2008 10 7 TRAX200801078 1 20080831 A 5312 ISOLATOR CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 932EV 8016 JOB 8801625 OPERATION 57 AFT PRESSURE BULKHEAD FS 621 HAS A BROKEN ISOLATOR AT LBL9, WL93. RESOLVED ON W/O 98370 TASKC ARD: NR 00336. REMOVED BROKEN ISOLATOR AND INSTALLED NEW SERVICEABLE ISOLATOR IAW CRJ 200 SRM 51-42-06. 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 TRAX200801079 1 20080831 A 5210 STRAP CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR STUCK A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 923EV 7826 PAX DOOR WILL NOT OPEN. HANDLE STRAP STUCK IN LOCKED POSITION. FREED STRAP AND DOOR OPENED NORMALLY. NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A21EA 20081007 NM 2008 10 7 NWAA084096302 1 20080902 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK FOUND RT UPPER DECK EMERGENCY BATTERY PACK INOPERATIVE. R&R BATTERY PACK PER AMM 52-23-14. OPS CHECK GOOD. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 ANC2008F00001 1 20080828 A 5280 39567851 LINK DOUG MD80 MD83 3023681 NM NLG DOOR UNKNOWN W ANCF A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 23 EICEP 53122 AIR TURN BACK. WHEN LANDING GEAR HANDLE WAS MOVED UP AFTER TAKEOFF, A VERY STRONG VIBRATION WAS FELT ON THE NOSE LANDING GEAR. REMOVED AND REPLACED RT FWD DOOR LINK IAW AMM 32-22-01, PAGE 201. OPS CHECK OK. PN 39567851, SN OFF EFS26043. SN ON LIN5301. (K) 2 L 7 2 4F RT 20081006 EA 2008 10 6 TRAX200801024 1 20080820 A 3350 LENS CNDAIR CL600 CL6002B19 1900309 EA CABIN CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 970EV 7527 JOB 8752721 OPERATION 162 FLOOR EMER FLOODLIGHT LOCATED ON WARDROBE UNIT HAS A CRACKED LENS AND BASE. REMOVED DAMAGED L ENS AND BASE IAW CRJ 200 AMM 33-51-19-000-801. INSTALLED SERVICEABLE LENS AND BASE IAW CRJ 200 AMM 33-51-19-400-801. O PS TEST DUE OPS TEST EMERGENCY FLOOD LIGHT ON WARDROBE IAW CRJ 200 AMM 33-51-00-710-801. 2 L 7 2 4F RT A21EA 20081006 NM 2008 10 6 NWAA084006310 1 20080824 A 3350 BATTERY BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING OVERNIGHT CHECK FOUND EMERGENCY EXIT SIGN INOP AT DOOR 3 RT AFT. MX R&R POWER SUPPLY AND BATTERY. OPS CHECKED G OOD AND ACFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20081008 NM 2008 10 8 KCS2008F00016 1 20080904 A 5310 DOOR FRAME BOEING 747 747249F 1384849 NM BS 281 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 STA 281, RBL-50, W/L-312 CARGO DOOR FRAME CRACKED. (K) 2 L 7 4 4F RT A20WE 20081008 NM 2008 10 8 KCS2008F00017 1 20080912 A 5347 SEAT TRACK BOEING 747 747249F 1384849 NM BS 620 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 SEAT TRACK AT STA-620 AT LBL-70 CORRODED. (K) 2 L 7 4 4F RT A20WE 20081008 NM 2008 10 8 2008UALA05713 1 20080913 A 3350 767 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 508UA 24744 DOOR 2L SLIDE ARMING LIGHT INOP. FOUND SLIDE LIGHT INOP. DOOR VERIFIED TO BE ARMED. RELAMPED ARMING LIGHT, CHECKS OKAY . 2 L 7 2 4F 4 F RT A2NM E17NE 20081008 NM 2008 10 8 2008UALA05724 1 20080914 A 3397 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 ROW 60 LEFT EMERGENCY LIGHT INOP. SECURED CONNECTOR AT ASSY. OP CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081008 NM 2008 10 8 2008UALA05725 1 20080914 A 3350 9F19948501 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 116UA 26908 DOOR 1R SLIDE ILLUMINATION LIGHT INOP. FOUND LIGHT INOPERATIVE. REPLACED LAMP. OP CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20081008 NM 2008 10 8 AALA200802133 1 20080819 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 794AN 30256 ORD EMERGENCY LIGHT AT SEAT 20C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802134 1 20080819 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 794AN 30256 ORD EMERGENCY LIGHT AT SEAT 36C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 36C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802154 1 20080730 A 5311 148T2740 FRAME BOEING 767 767223 1385123 NM FUSELAGE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 328AA 22328 AFW RT OUTER CHORD AT STATION 1809 HAD HOLES REAMED TO 0.285 INCH AND 0.280 INCH. REPAIRED PER MRB 767 3264. 2 L 7 2 4F RT A1NM 20081008 NM 2008 10 8 AALA200802155 1 20080818 A 5330 148T32813 SKIN BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 328AA 22328 AFW FUSELAGE SKIN AT SECTION 48 HAS LIGHT CORROSION BETWEEN STRINGER 30 AND 32 LT AND BETWEEN STATION 1809 AND 1832. AR EA OF DISCREPANCY IS 4.8 INCHES BY 20 INCHES. REPAIRED PER MRB 767 3283. 2 L 7 2 4F RT A1NM 20081008 NM 2008 10 8 AALA200802156 1 20080805 A 5531 173T10221 FITTING BOEING 767 767223 1385123 NM VERTICAL STAB DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 328AA 22328 AFW VERTICAL STABILIZER RIB FITTING AT RUDDER STATION 380.769 WAS DAMAGED FROM STATIC DISCHARGE. REPAIRED PER MRB 767 3 269. 2 L 7 2 4F RT A1NM 20081008 NM 2008 10 8 AALA200802167 1 20080822 A 3350 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AA 24585 DFW LT AFT EMERGENCY LIGHT EXIT IDENTIFIER PLACARD IS DAMAGED. REPLACED PLACARD FOR LT AFT EMERGENCY LIGHT EXIT IDENTIF IER. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 NM 2008 10 8 AALA200802168 1 20080822 A 3350 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 627AA 24585 DFW RT AFT EMERGENCY LIGHT EXIT IDENTIFIER PLACARD IS DAMAGED. REPLACED PLACARD FOR RT AFT EMERGENCY LIGHT EXIT IDENTIF IER. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 NM 2008 10 8 AALA200802174 1 20080823 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 772AN 29580 JFK EMERGENCY LIGHT AT SEAT 21G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 21G. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 KCSA081484 1 20080920 A 5343 ATTACH FITTING BOEING 747 747123 1384873 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 RT BODY GEAR ACTUATOR ATTACH FITTING OTBD LUG IS CRACKED 2 INCHES AT STA 1480. 2 L 7 4 4F RT A20WE 20081007 WP 2008 10 7 U2R2008F00001 1 20080825 A 5522 SKIN DOUG DC8 DC871F 302199D WP RT ELEVATOR DENTED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 872SJ 83402 46040 DURING C-CHECK INSP, FOUND RT ELEVATOR XE117-594 LOWER SURFACE DENTED. (K) 2 L 7 4 4F RT 4A25 20081007 WP 2008 10 7 U2R2008F00006 1 20080825 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 872SJ 83402 46040 DURING C-CHECK INSP, FOUND FWD CARGO COMPARTMENT F3 8.00 BTW L-24R FRAME WITH CORROSION. (K) 2 L 7 4 4F RT 4A25 20081007 WP 2008 10 7 U2R2008F00007 1 20080825 A 5320 STRAP DOUG DC8 DC871F 302199D WP DOOR FRAME CRACKED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 872SJ 83402 46040 DURING C-CHECK INSPECTION, FOUND AFT SERVICE DOOR (R2) AFT UPPER JAMB CORNER WITH CRACK OF 0.800 LENGTH ON BEAR STRAP (A FTER ACCOMPLISHED X-RAY INSPECTION). (K) 2 L 7 4 4F RT 4A25 20081007 CE 2008 10 7 GUU2008F00047 1 20080826 A 5210 12951405933 CABLE BEECH 1900 1900D 1154162 CE PAX DOOR BROKEN A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87554 UE227 PILOT REPORTED UNABLE TO OPEN CABIN DOOR, FOUND UPPER FWD DOOR CABLE BROKEN. REPLACED UPPER FWD DOOR CABLE. (K) 2 L 7 2 4T RT A24CE 20081007 SW 2008 10 7 WGE2008F00001 1 20080826 A 2752 EM41165 ACTUATOR ECLIPS EA500 ECLIPSEEA500 3350000 SW NR 1 FLAP FAILED E WGEA K NONE O OTHER IN INSP/MAINT 1 EA 27 139DJ 000054 REF MX LOG PAGE NR 2805, NR 1 FLAP FAIL CAS MESSAGE AT 1030Z ON APPROACH. WO2557, TASKCARD NR-00002. REMOVED AND REPLA CED RT IB FLAP ACTUATOR IAW EA500 AMM 27-51-11. PERFORMED A FLAP ADJUSTMENT/TEST IAW EA500 AMM 27-50-00. CHECKED GOOD. R EPLACED LT IB FLAP ACTUATOR WITH NEW UNIT IAW EA500 AMM, CH 27-51-11. PERFORMED ADJUSTMENT/ TEST IAW EA500 AMM CH 27-50 -00. (K) 1 L 7 2 4J RT A00002AC 20081007 2008 10 7 YEN2008F00018 4 20080922 A 2210 221104501 ACTUATOR EMB ERJ190 ERJ190100IGW 3260408 NM AUTO PILOT SERVO BINDING A YENA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 265JB 19000049 CLIMBING THROUGH 8,000 MSL AT 250 KTS, NOTICED AILERONS WERE MORE DIFFICULT TO MOVE THAN NORMAL, AS WE CLIMBED AND INCRE ASED AIRSPEED TO 290 KTS THE AILERON CONTROLS GRADUALLY BECAME HARDER TO MOVE AT APPROX 20,000 MSL AND 290 KTS AILERONS BINDING FEEL AND WHEN TRIED TO RETURN TO CENTER YOKE SNAPPED BACK TO CENTER WITH ROUGHLY 2 INCHES OF TRAVEL IN YOKE. THI S WAS EXPERIENCED WITH BOTH CAPTAIN AND FO`S YOKE. IN DESCENT THESE CONDITIONS GRADUALLY REVERSED TO NORMAL AILERON CONT ROL WITH THE YOKE. PERFORMED TSM TASK 27-10-00-810-803-A AND FOUND AUTO PILOT SERVO ACTUATOR BINDING. REMOVED AND REPLAC ED AUTO PILOT SERVO ACTUATOR IAW AMM 22-11-04, OPS CHECK NORMAL. PERFORMED AILERON ELECTRONIC RIGGING IAW AMM 27-03-02, 2 L 7 2 4F RT A57NM 20081007 NM 2008 10 7 YEN2008F00019 1 20080903 A 5270 ROLLER EMB ERJ190 ERJ190100IGW 3260408 NM PAX DOOR BENT A YENA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 238JB 19000039 "DOOR PAX AFT OPEN" RED CAS MESSAGE DURING CLIMB OUT. ALL DOOR INDICATION GREEN. CABIN ALT AT 7700` AND CLIMBING WITH AC ALTITUDE AT FLT 190. OUTFLOW VALVE STAYED AT .2500 OPEN. HIGHEST CABIN ALT RATE OF CLIMB WAS 1100 FPM. FMS ENTERED CRU ISE AL WAS FL350. UNDER WEIGHT LANDING PERFORMED. PERFORMED TEST OF CPCS IAW AMM 21-30-720-801, NO DEFECTS NOTED. PERFOR MED PRESSURIZATION TEST IAW AMM 21-30-00-720-802. NO DEFECTS NOTED. INSPECTED PACK OUTLET DUCTS IAW AMM 21-51-21. NO DE FECTS NOTED. DURING ABOVE OPS CHECKS. L-2 PAX DOOR SHOWED OPEN. FOUND RT LATCH INDICATOR ROLLER BENT AND PIN BROKEN. PLA CED DOOR ON MEL 52-70-00 MDDR NR 34140 ( DOOR INDICATION ON MFD AND ASSOC EICAS). 2 L 7 2 4F RT A57NM 20081007 NM 2008 10 7 YEN2008F00020 1 20080902 A 2120 UNKNOWN EMB ERJ190 ERJ190100IGW 3260408 NM CABIN SMOKE A YENA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 EA 15 198JB 19000021 CABIN CREW REPORTED SMOKE IN CABIN, REMOVED NR 1 AND NR 2 EXT PNLS. INSPECTED FOUND COFFEE DEBRIS IN NR PACK (NR 1 PACK OK) AMM 21-51-05. CLEANED OUT NR 2 PACK AND SECURED NR 1 AND NR EXT PNLS. OPS CHECK OF NR AND NR 2 PACKS. OK INSPECTED F WD/MID E/E BAY RECIRC FANS. OPS CHECK OK. AMM 21-26-00/01. ALSO INSPECTED TR`S, CONDITION AND OPS CHECK OK AMM 24-31-01/ 00. INSPECTED LAV`S NO DEFECTS NOTED. AMM 26-14-00/01. RAN (OPERATED) ENG NR 1 AND NR 2 BLEED CHECK OK. NO DEFECTS NO TED AMM 71-60-01. COMPLETED FIM 21-20-810-801A. PERFORMED LTV SMOKE IN CABIN INSPECTION IAW LTV MM 44-20-10. NO FAULTS NOTED LTV SYS. OPS CHECK NML IAW LTV MM 44-20-10. (K) 2 L 7 2 4F RT A57NM 20081007 SO 2008 10 7 C2X2008F00026 1 20080904 A 7160 14575001409 INLET EMB 145 EMB145LR 3260212 SO NR 1 ENGINE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18982 21000 145223 AC IS CURRENTLY IN C-CHECK AND CORROSION WAS FOUND ON THE NR 1 ENGINE INLET ATTACH FLANGE MOUNTING HOLES. MAINTENANCE RE PAIRED THE NR 1 ENGINE INLET IAW EC5420-01145. AC WILL BE RELEASED AT THE END OF THE CHECK. (K) 2 L 7 2 4T RT T00011AT 20081007 SO 2008 10 7 C2X2008F00027 1 20080904 A 7160 14575001405 INLET EMB 145 EMB145LR 3260212 SO NR 2 ENGINE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18982 21000 145223 AC IS CURRENTLY IN C-CHECK AND CORROSION WAS FOUND ON THE NR 2 ENGINE INLET ATTACH FLANGE MOUNTING HOLES. MAINTENANCE RE PAIRED THE NR 2 ENGINE INLET IAW EC542001146/ AC WO; BE RELEASED AT THE END OF THE CHECK. (K) 2 L 7 2 4T RT T00011AT 20081007 SO 2008 10 7 C2X2008F00028 1 20080904 A 4910 450412 FIREWALL EMB 145 EMB145LR 3260212 SO APU DENTED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 18982 145223 AC IS CURRENTLY IN C-CHECK AND THE APU FIREWALL WAS FOUND CHAFED AT THE LOWER BEND (STR 21L/ 21R) EXTERIOR SURFACE. MAIN TENANCE REPAIRED THE DAMAGE AREA IAW EC5310-01359. AC WILL BE RELEASED AT THE END OF THE CHECK. (K) 2 L 7 2 4T RT T00011AT 20081007 SO 2008 10 7 C2X2008F00030 1 20080904 A 5751 14574000416 BONDING STRAP EMB 145 EMB145XR 3260214 SO RT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16151 7507 145758 AC IS CURRENTLY IN C-CHECK AND THE RT AILERON SHROUD BONDING STRAPS WERE FOUND CORRODED. MAINT REMOVED AND REPLACED THE BONDING STRAP PLATE IAW EC 575001315. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. (K) 2 L 7 2 4F RT 20081007 SO 2008 10 7 C2X2008F00031 1 20080812 A 3350 20131A BATTERY EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12163 14500811 DURING ROUTINE MAINT, MX FOUND LT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED EMERGENCY LIGHT BATT ERY NR 4 AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. (K) 2 L 7 2 4F RT 20081007 EA 2008 10 7 N6W2008F00001 1 20080905 A 5270 SENSOR CNDAIR CL600 CL6002C10 1390015 EA DOOR WARNING MALFUNCTIONED A N6WA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 151GJ 10216 REAR EMERGENCY DOOR CAUTION MESSAGE ON/OFF SEVERAL TIMES AFTER LANDING AND DURING TAXI. GLEANED PROX SENSOR IN UPPER R E MERGENCY DOOR FRAME AND TESTED IAW CRJ700 82-21-00. ALL OPS AND INDICATIONS NORMAL. VERIFIED DOOR IS SECURE. 2 L 7 2 4F RT A21EA 20081007 NM 2008 10 7 AALA200802077 1 20080812 A 3397 WIRE BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 DFW EMERGENCY LIGHT AT FORWARD GALLEY LT HAND SIDE INOPERATIVE. FOUND BROKEN WIRE. REPLACED LIGHT ASSEMBLY FOR EMERGEN CY LIGHT AT FORWARD GALLEY LT HAND SIDE. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081007 NM 2008 10 7 AALA200802076 1 20080812 A 3397 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 39365 24046 ORD EMERGENCY LIGHT AT MID GALLEY LT HAND SIDE INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT MID GALLEY LT HAND SIDE. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081007 NM 2008 10 7 UIE2008F00029 1 20080918 A 5313 BAC1498143 STRINGER BOEING 747 74747UF 1384812 NM GE CF6 CF680C2B6F 30025 NE BS 2588 S46R CORRODED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 418MC 32840 FOUND RT FUSELAGE INNER STRINGER CORROSION AT STA 2580, S46R. REPAIRED RT FUSELAGE INNER STRINGER AT STA 2588, S-46R, IA W 747-400F SRM 53-00-03, FIG 201 REV 48 AND EO NR 4463A209. (K) 2 L 7 4 4F 4 F RT A20WE E13NE 20081007 NM 2008 10 7 UIE2008F00031 1 20080918 A 5330 146U70053 SKIN BOEING 747 74747UF 1384812 NM GE CF6 CF680C2B6 30025 NE FUSELAGE DENTED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 418MC 32840 DENT WAS FOUND AT THE AFTER LOWER CORNER OF BULK CARGO DOOR. INSPECTED IAW SRM 51-10-00 AND SR ID NR 1949639862. (K) 2 L 7 4 4F 4 F RT A20WE E13NE 20081007 NM 2008 10 7 UIE2008F00032 1 20080918 A 5414 2242302545 SKIN BOEING 747 74747UF 1384812 NM GE CF6 CF680C2B6 30025 NE NR 3 NACELLE CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 418MC 32840 FOUND NR 3 ENGINE RT CORE COWL LOWER FACE CRACKED. 0.3 INCH AT NAC STA 288. REPAIRED IAW FORM NR E8207.4. (K) 2 L 7 4 4F 4 F RT A20WE E13NE 20081007 NM 2008 10 7 UIE2008F00033 1 20080918 A 5420 3234538733 FAIRING BOEING 747 74747UF 1384812 NM GE CF6 CF680C2B6 30025 NE NR 4 NACELLE DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 418MC 32840 FOUND NR 4 ENGINE SKIRT FAIRING SUPPORT BRACKET ATTACHED BOLT IB SIDE HOLE ENLARGED NEAR FAIRING DOOR NR 4 HINGE. REPAIR ACCOMPLISHED IAW SR ID NR 1945402461 AND EO NR 4464A066. (K) 2 L 7 4 4F 4 F RT A20WE E13NE 20081008 NM 2008 10 8 QXEA200800441 1 20080418 A 3213 STRUT DHAV DHC8 DHC8202 2809007 NM RT MLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK RT MLG SHOCK STRUT HAS CHAFE ON FWD SURFACE AT STRUT FAIRING MID ATTACH HOLE. POLISHED CHAFFED AREA IAW -8 /200 MESSIER/DOWTY CMM 32-10-01 PG 6015 PARA 6A4. HFEC INSP IAW -8/200 NDTM PT 6, 51-00-01. NO CRACKS NOTED. PERFORM ED FPI IAW -8/200 VENDOR CMM 32-10-01 PG 6009 PARA 5A3 AND HORIZON NDTM CHP 8 NO CRACKS NOTED. PEENED IAW -8/200 CMM 32 -10-01 STEP 6A2 AND FIG 601. ALODINED IAW MESSIER/DOWTY CMM 32-10-01 PG 6009 PARA 5B2A. PRIMED PAINTED IAW 2 H 7 2 4T RT A13NM 20081008 SO 2008 10 8 CVG2008F00000 1 20080905 A 5610 1159SCB310214 WINDSHIELD GULSTM G1159 GIV 3980115 SO COCKPIT CRACKED E CVGA O OTHER O OTHER NR NOT REPORTED 1 GL 05 72BD 2370 1420 DURING A FLIGHT, WITH ONE PASSENGER ON BOARD, FROM SJC TO AGC, RT FWD WINDSHIELD OUTER PANE CRACKED DUE TO HEATING ELEME NT FAILURE. AC DIVERTED TO IRK WITHOUT INCIDENT. THE WINDSHIELD WAS DEFERRED AT IRK AND THE AIRCRAFT REPOSITIONED TO AT W FOR REPAIRS. THE WINDSHIELD WAS REPLACED WITH A NEW PART AT ATW. OPS AND PRESSURIZATION CHECKS WERE PERFORMED WITH SA TISFACTORY RESULTS. (K) 2 L 7 2 4F RT A12EA 20081008 GL 2008 10 8 WVX2008F00000 2 20080911 A 7250 23069745 TURBINE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL ENGINE DESTROYED A WVXA A UNSCHED LANDING X T ENGINE FLAMEOUT ENGINE CASE PENETRATION HO HOVERING 1 WP 13 58251 15480 581 880317D CAE833089 AIRCRAFT WAS IN A 70 FOOT HOVER AND HAD JUST PLACED A SLING LOAD ON THE GROUND WHEN A LOUD BANG OCCURRED THE LOUD BANG W AS THE TURBINE EXPLODING. AT THIS TIME, THE PILOT LOWERED THE COLLECTIVE AND ENTERED AN AUTO ROTATION. AIRCRAFT TOUCHED DOWN IN A LEVEL ATTITUDE WITH MINOR DAMAGE TO AIRFRAME. SUBSEQUENT INSPECTION REVEALED THAT THE NR4 TURBINE WHEEL BURST. (K) 1 G 7 1 3U 3 U H3WE E4CE 20081008 NM 2008 10 8 SPA2008F00001 1 20080917 A 3350 20131A BATTERY PACK BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15 52051 NE EMERGENCY LIGHTS INOPERATIVE A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 07 712S 23038 LOWER EMERGENCY LIGHTS AT DOORS L2 AND R2 WILL NOT ILLUMINATE. REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-21-27. F UNCTIONAL CHECK SATISFACTORY. (K) 2 L 7 2 4U 4 F RT A16WE E2EA 20081008 WP 2008 10 8 AALA200802044 1 20080808 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 411AA 49322 LGA SEAT MOUNTED EMERGENCY LIGHTS AT SEAT ROW 20 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 20 FOR INOPERATIVE SEAT MOUNTED EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081008 NM 2008 10 8 KCS2008F00014 1 20080913 A 5311 FRAME BOEING 747 747221F 1384868 NM BS 2231 S21-22L CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 748CK 21744 MAIN DECK L5 DOOR REVEAL IS CRACKED (2") AT STA 2231 BETWEEN STR 21L AND 22L. (K) 2 L 7 4 4F RT A20WE 20081008 WP 2008 10 8 AALA200802035 1 20080806 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7517A 49894 LGA EMERGENCY LIGHTS AT OVERWING INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD ROW 24 FOR INOPERATIVE EMERGENCY LIGHTS AT OVERWING. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081008 SO 2008 10 8 CHQ2008F00006 1 20080909 A 2120 UNKNOWN EMB 135 EMB135KL 3260302 SO ALLSN AE3007 AE3007A 03030 GL COCKPIT SMOKE A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 375SK 145569 WHILE CLIMBING THROUGH 8,000 FT THE FLIGHT CREW WAS INFORMED OF SMOKE OR STEAM COMING FROM THE FLOOR OF THE CABIN BY THE F/A. THE QRH CHECKLISTS WERE COMPLIED WITH AND THE AC LANDED BACK AT RDU WITHOUT INCIDENT. MAINTENANCE WAS ABLE TO DUP LICATE THE FAULT WHEN THE PACKS WERE TURNED ON AND A HEAVY MIST WOULD COME OUT OF THE FLOOR VENTS. THE WATER COLLECTORS WERE ON THE PACKS WERE INSPECTED AND IT WAS FOUND TO BE WATER VAPOR DUE TO THE LOCAL WEATHER CONDITIONS. (K) 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081008 EA 2008 10 8 VNAA0809005 1 20080913 A 3234 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE NLG FAILED A VNAA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 05 207PS 11227 7873 CREW REPORTED A NOSE GEAR DISAGREE INDICATION FOR 1.5 MINUTES ON TAKE OFF. THE ACFT LANDED IN RIC WITHOUT INCIDENT. MX INSPECTED AND R&R THE NOSE LANDING GEAR SELECTOR VALVE ASSEMBLY. NO OTHER DEFECTS WERE NOTED. THE ACFT WAS RELEASED F OR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20081008 NM 2008 10 8 UIE2008F00038 1 20080914 A 5310 DOOR FRAME BOEING 747 7472D7B 1384803 NM FUSELAGE CRACKED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 523MC 21782 LT NR 1 MAIN ENTRY DOOR FWD FRAME UPPER HINGE CUTOUT AREA CRACKED. REPAIRED IAW MFG SERVICE REQUEST 1-948230971 APPROVED BY FORM 8100-9 DATED 4 SEP, 2008, DETAILS OF WORK KEPT AT EO-4752A153. (K) 2 L 7 4 4F RT A20WE 20081007 2008 10 7 USAA920081621 4 20080903 A 2565 D31591479 SLIDE BOEING 737 7373B7 1384580 NM PAX DOOR LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 516AU 23702 CTO Q6 EES LOG NR 4390815 FORWARD MAIN ENTRY DOOR SLIDE HAS LOW PRESSURE. REPLACED FORWARD MAIN ENTRY DOOR SLIDE IAW JO B CARD 03C10552008. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 USAA920081699 1 20080909 A 5312 STRUCTURE BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03-0553-8-0349/001. CRACK ON VERTICAL CHORD OF 178 BULKHEAD AT WL 184, LBL5.7. REPAIRED VERTICA L CHORD OF 178 BULKHEAD AT WL 184, LBL5.7 IAW B737 SRM 53-10-08 REPAIR NR 5. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 USAA920081700 1 20080916 A 5320 65458078 INTERCOSTAL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03C10753006/001. CRACK IN RADIUS OF INTERCOSTAL BS277, S14R. REPAIRED INTERCOSTAL BS277, S14R I AW B737 SRM 51-10-02 & BOEING DRAWING NR 65-45807. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 USAA920081702 1 20080919 A 5312 6517583504 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 23879 PIT FPBH MAJOR REPAIR JOB CARD NR EIA53032. 2 CRACKS ON VERTICAL WEB AT BS 178, WL184, RBL5.7. REPAIRED VERTICAL WEB A T BS 178, WL184, RBL5.7 IAW B737 SRM 53-10-08 AND US AIRWAYS EA NR 111653. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 AALA200802179 1 20080824 A 3350 SIGN BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AM 24579 DFW EMERGENCY LIGHT EXIT SIGN AT RT FORWARD OVERWING EXIT DOOR DAMAGED. REPLACED SIGN ASSEMBLY FOR EMERGENCY LIGHT EXIT SIGN AT RT FORWARD OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 NM 2008 10 8 AALA200802186 1 20080824 A 3350 LENS BOEING 767 767223 1385123 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 335AA 22333 JFK EMERGENCY LIGHT AT SEAT 19B MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 19B. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A1NM 20081008 NM 2008 10 8 AALA200802053 1 20080809 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW EMERGENCY LIGHT AT SEAT 25C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802183 1 20080824 A 3350 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AM 24579 DFW EMERGENCY LIGHT EXIT SIGN DECAL AT RT OVERWING EXIT DOOR DAMAGED. REPLACED DECAL FOR EMERGENCY LIGHT EXIT SIGN AT R T OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 NM 2008 10 8 USAA920081689 1 20080828 A 5320 65479767 SHEAR WEB BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 SAL C17 MAJOR REPAIR NR 6093420 CORROSION ON SHEAR WEB BETWEEN BS827 TO BS847, S17L. REPLACED SHEAR WEB BETWEEN BS827 T O BS847, S17L IAW B737 SRM 51-10-02-OG. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 AALA200802122 1 20080817 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 784AN 29588 DFW EMERGENCY LIGHT AT LT NR 4 DOOR CROSS AISLE INOPERATIVE. REPLACED LAMP FOR INOPERATIVE EMERGENCY LIGHT. SYSTEM GRO UND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802115 1 20080815 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INCORRECT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 197AN 32391 DFW EMERGENCY LIGHT AT SEAT 25D HAS WRONG LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 EU 2008 10 8 AALA200802110 1 20080815 A 3350 BR964814 FIXTURE AIRBUS 300 A300B4605R 3930308 EU CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 80058 466 JFK EMERGENCY LIGHT AT SEAT 21C MISSING FIXTURE. REPLACED FIXTURE FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECK ED NORMAL OPS. 2 L 7 2 4F RT A35EU 20081008 EA 2008 10 8 TRAX200801121 1 20080906 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP OUT OF RIG A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 852AS 7369 FLAPS FAIL MSG AT 20 DEGREES ON FINAL APPROACH. COMPLIED WITH QRH. EMERGENCY DECLARED. CK`D RIGGING OF BPSU`S. FOUND LT AND RT BPSU`S OUT OF RIG. RIGGED BPSU`S IAW CRJ 200 AMM 27-51-10-830-801. OPS CK GOOD. 2 L 7 2 4F RT A21EA 20081008 NE 2008 10 8 TRAX200801123 2 20080907 A 7321 FADEC CNDAIR CL600 CL6002C10 1390015 EA GE CF34 CF348C1 30049 NE RT ENGINE MALFUNCTIONED A ASOA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 27 761ND 10213 0605 DURING DESCENT FROM 22500 TO 12000 @ 300KIAS GOT R FADEC MSG RAN QRH & MONITORED ENGINE INDICATIONS. R ITT WENT TO 932 C. SHUTDOWN R ENGINE. RAN SINGLE ENGINE PROCEDURES CHECK AND LANDED WITH ALL CHECK LIST NO HOT ICON GAUGE TURNED RED. EMERGENCY DECLARED. R&R FUEL METERING UNIT AND FADEC IAW CRJ 700 AMM 733-21-07, 73-21-03 ALL OPS CHECK OK. 2 L 7 2 4F 4 F RT A21EA E00063EN 20081008 EA 2008 10 8 TRAX200801088 1 20080902 A 3297 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA NLG LOOSE A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 868AS 7474 NOSE DOOR OPEN RED MSG AFTER TAKE OFF. ACFT RETURNED TO BNA AFTER T/O, EMERGENCY DECLARED. FLT 4992 DEL 75 MINS. NC. F LT 4992 CX. FOUND CANNON PLUG LOOSE ON NLG DOOR SELECTOR VALVE. RESECURED IAW CRJ200 AMM 32-22-20. DOORS OPS CHECK NO RMAL. ON GROUND WITH MTC SWITCH. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801091 1 20080903 A 5210 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA ASD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 ASD AFT SIDEWALL CRACKED AT SECOND STEP RISER. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801093 1 20080903 A 5210 HANDLE CNDAIR CL600 CL6002C10 1390015 EA ASD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 ASD EXTERNAL HANDLE CRACKED. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801100 1 20080904 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 LT SIDE OF 280 BEAM CORRODED 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801103 1 20080904 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 RT 280 WEB CORRODED. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801112 1 20080905 A 5330 DOUBLER CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 CORROSION ON SEVERAL LOCATIONS OF THE BELLY SKIN DOUBLER JUST AFT OF FS 280 BETWEEN STR 25L AND 25R. 2 L 7 2 4F RT A21EA 20081008 2008 10 8 DXTA200803269 4 20080908 A 2210 WARNING SYSTEM CESSNA 750 750 2076810 CE AUTOPILOT SYS ACTIVATED E DXTA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 931QS 7500064 DURING DESCENT AUTOPILOT STAB TRIM FAIL AMBER CAS MSG CAME ON. 2 L 7 2 4J RT T00007WI 20081008 NM 2008 10 8 KCSA081458 1 20080910 A 5347 SEAT TRACK BOEING 747 747122 1384872 NM FUSELAGE CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 CARGO FLOOR SEAT TRACK CRACKED AT BS 1840, LBL 24. 2 L 7 4 4F RT A20WE 20081008 NM 2008 10 8 KCSA081459 1 20080910 A 5315 FLOORBEAM BOEING 747 747122 1384872 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 BS 1820 FLOORBEAM UPPER CHORD DENTED BETWEEN LBL 1 AND RBL 3. 2 L 7 4 4F RT A20WE 20081008 SO 2008 10 8 CHQA200800176 1 20080908 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CABIN INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 279SK 145379 CAE311424 DURING INSPECTION, THE RT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOP. THE BULB FOR THE RT OVER WING EMERGENCY LIGHT WAS REPLACED IAW EMB 145 AMM 33-50-07-4. THE EMERGENCY LIGHTING SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081009 NM 2008 10 9 2008UALA05573 1 20080901 A 3510 A3008120M0 TRANSDUCER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE OXYGEN SYSTEM FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 580UA 26698 THE O2 PRESSURE DECREASES FROM 1600 TO 160 WHEN TESTED ON BOTH CAPT - F/O POSITIONS. TRANSDUCER FOUND FAULTY. REPLACED PRESSURE TRANSDUCER.OPS CHECKS OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081009 NM 2008 10 9 2008UALA05575 1 20080902 A 2120 S161N3001 FILTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RECIRC SYS FAULTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 551UA 25399 MUSTY SMELL IN CABIN. WHILE TROUBLESHOOTING FOUND LEFT FILTER NEW AND ALL DUCTS CLEAN. RIGHT RECIRC FILTER IS FAULTY. REPLACED RT RECIRC FILTER. 2 L 7 2 4F 4 F RT A2NM E17NE 20081009 WP 2008 10 9 AALA200802104 1 20080814 A 2560 STRAP DOUG DC9 DC982 3022082 WP FLASHLIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 573AA 53092 LGA EMERGENCY FLASH LIGHT STRAP AT FORWARD CABIN BROKEN. REPLACED STRAP FOR EMERGENCY FLASH LIGHT AT FORWARD CABIN. SY STEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081009 WP 2008 10 9 AALA200802102 1 20080814 A 2822 PUMP DOUG DC9 DC982 3022082 WP FUEL SYSTEM FAILED A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 426AA 49338 ABQ INFLIGHT T1968/14AUG SLC TO DFW. CREW REPORTED CENTER TANK FUEL UNUSABLE. LANDED ABQ WITHOUT INCIDENT. REPLACED B OTH CENTER TANK FUEL PUMPS. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081009 WP 2008 10 9 AALA200802097 1 20080813 A 3350 101191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7538A 49992 LGA PORTABLE EMERGENCY LIGHT ASSEMBLY AT FIRST CLASS CABIN INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR PORTABLE EMERGENCY LIGHT AT FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081009 NM 2008 10 9 2008UALA05584 1 20080903 A 2161 8102003 CONTROLLER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE LT CABIN TEMP MALFUNCTIONED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 791UA 26933 STRONG ODOR IN CABIN. SUSPECT FAULTY CONTROLLER. REPLACED LEFT CABIN TEMPERATURE CONTROLLER. CHECKS OKAY & NO ODOR ON DEPARTURE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081009 NM 2008 10 9 QXEA200800643 1 20080609 A 5320 FITTING BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK FRAME CLIPS UNDER CENTER FLOOR AT STA X101 ARE CORRODED IN SEVERAL LOCATIONS. REMOVED CORROSION IAW RD8/4- 53-2344. HFEC INSPECTED IAW -8 400 NDTM PT 6, 51-00-01, NOT CRACKS NOTED. UT THICKNESS CHECK IAW -8 400 NDTM PT 1, 51- 00-04. APPLIED ALODINE PRIMED AND PAINTED IAW Q400 SRM 51-21-10, 51-25-10 AND 51-25-15. 2 H 7 2 4T RT A13NM 20081009 EA 2008 10 9 QXEA200800674 1 20080612 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK. NUMEROUS CORROSION SPOTS ON RT SIDE SEAT RAIL FS 379 TO FS 483. REMOVED CORROSION FROM SEAT TRACK AT FS 379 TO 483. .15 MATERIAL REMOVED IAW REO670-53-00-013. TREATED IAW REO 670-53-00-013. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 QXEA200800673 1 20080612 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 614QX 10049 RFD C4 CHECK CORROSION FOUND UNDER UPPER TCAS ANTENNA ON STRUCTURE. REMOVED ANTENNA IAW CRJ 700 AMM 34-43-04-000-801. BLENDED CORROSION, .013 MATERIAL REMOVED IAW REO670-53-21-362. PERFORMED ECI NO DEFECTS NOTED IAW REO 670-53-21-362. T REATED AREA AND INSTALLED ANTENNA IAW REO 670-53-21-362 AND CRJ AMM 34-43-04-400-801. 2 L 7 2 4F RT A21EA 20081009 EA 2008 10 9 TRAX200801163 1 20080912 A 3350 COVER CNDAIR CL600 CL6002C10 1390015 EA CABIN BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 354CA 10064 CEILING LIGHT COVER AT 15AB BROKEN. LIGHT LENS/COVERS, INCLUDING EMERGENCY LIGHT. REPLACED LIGHT COVER AT SEAT 15AB IA W CRJ 700 AMM 33-21-00. DML CLEARED. 2 L 7 2 4F RT A21EA 20081009 2008 10 9 DXTA200803279 4 20080919 A 2210 AUTOPILOT SYS CESSNA 500 560CESSNA 2076750 CE COCKPIT MALFUNCTIONED E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 814QS 5600776 AUTO PILOT KICKS OFF WHEN IN CLIMB OR TURN. 2 L 7 2 4F RT A22CE 20081009 CE 2008 10 9 DXTA200803283 1 20080922 A 3200 UNKNOWN CESSNA 750 750 2076810 CE LANDING GEAR MALFUNCTIONED E DXTA O OTHER O OTHER AP APPROACH 1 GL 07 942QS 7500024 ON APPROACH TO LANDING, SELECTED GEAR DOWN, RECEIVED NO NOSE GEAR INDICATION. 2 L 7 2 4J RT T00007WI 20081009 2008 10 9 DXTA200803282 4 20080922 A 2210 AUTOPILOT SYS BEECH MU300 400A 1155402 CE COCKPIT MALFUNCTIONED E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 108QS RK382 A/P PITCH TRIM FAILURE IN FLIGHT. 2 H 7 2 4F RT A16SW 20081009 NM 2008 10 9 QXEA200800636 1 20080609 A 5320 INTERCOSTAL BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK INTERCOSTAL SUPPORT FOR LT ELEVATOR QUADRANT HAS CORROSION ON LOWER FLANGE AROUND RIVET ENTIRE LENGTH OF IN TERCOSTAL BETWEEN FS X-64.400 AND 54.00 JUST IB OF STR 29L. REMOVED RIVETS ALONG INTERCOSTAL REF Q400 SRM 51-40-07 AND 51-42-05. BLENDED CORROSION REF Q400 SRM 51-21-00. UT THICKNESS CHECK IAW -8 400 NDTM PT 1, 51-00-04. HFEC INSPECTED IAW -8 400 NDTM PT 6, 51-00-10 NO CRACKS NOTED. ALODINED, INSTALLED RIVETS AND APPLIED PRIMER AND PAINT IAW Q400. 2 H 7 2 4T RT A13NM 20081009 NM 2008 10 9 QXEA200800658 1 20080609 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 424QX 4006 PDX C4 CHECK THERE ARE LARGE AREAS OF PITTING ALONG SEAT TRACK NR 13 INCLUDES BOTH SIDES FROM FS 224 TO FS 570 RT INBD T RACK. R&R NR 13 SEAT TRACK IAW DHC8 -400 SRM 51-42-05 AND SRM 51-40-15. 2 H 7 2 4T RT A13NM 20081009 EA 2008 10 9 TRAX200801154 1 20080910 A 5220 SEAL CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY EXIT LACK OF LUBE A ASOA O OTHER O OTHER NR NOT REPORTED 1 SO 27 826AS 7210 JOB 8721021 OPERATION 169 LT OVERWING EMERGENCY EXIT FAILED TO OPEN AT 30 10 LBF. RESOLVED ON W/O 98649 TASKCARD NR 002 19. C/A CLEANED AND APPLIED LUBE DC33 TO SEAL AND PINS ON LT OVERWING EMER EXIT. PERFORMED FUNC TEST OF EXIT IAW CRJ 2 00 AMM 52-21-00-720-801. FOUND HANDLE OPERATING WITHIN LIMITS AT THIS TIME. ASA RII C/W 53000 2 L 7 2 4F RT A21EA 20081009 2008 10 9 08FDEA03522 2 20080820 A 7314 PUMP BOEING 727 727200 138407E NM NR 1 MALFUNCTIONED A FDEA O OTHER E X J VIBRATION/BUFFET ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 CE 21 281FE 22348 AT FL 350 IN STEADY CRUISE FLT, FELT SLIGHT VIBRATION FOLLOWED BY NR 1 EPR ROLL BACK, NR 1 N1,N2 EGT ROLLBACK. N1 STABI LIZED AT 26 PERCENT, EGT 180 DEG NR 1 GEN BREAKER LIGHT ON AND NR 1 LOW OIL PRESSURE LIGHT ON. THRUST LEVEL BOUGHT TO I DLE AND DESCENT STARTED. PASSING FL 300 AND 320 KIAS NR 1 ENG PARAMETERS RETURNED TO NORMAL. ENG OPERATED NORMAL FOR REMAINED OF FLIGHT. RAN QRH FOR NR 1 GEN RESET AND COULD NOT RESET GENERATOR BREAKER. VOLTS AND FREQS NORMAL AND ESSE NTIAL POWER OK WHEN NR 1 GEN SELECTED. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP AND FUEL CONTROL UNIT OPS AND LK CHEC KED GOOD PER MM 73-11-01 AND 73-21-01.. 2 L 7 3 4F RT A3WE 20081009 EA 2008 10 9 TRAX200801194 1 20080919 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 683BR 7692 JOB 8769211 OPERATION 192 LT FS 484, LBL 27 FLOOR SUPPORT STRUCTURE CLIPS ARE CRACKED 1/2". 2 L 7 2 4F RT A21EA 20081009 NM 2008 10 9 2008UALA05555 1 20080831 A 3350 LAMP BOEING 737 737322 1384676 NM EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 314UA 23675 AFT SECTION OF CABIN FLOOR EMERGENCY LIGHTS INOP. FOUND FAULTY LAMP, REPLACED LAMP. OP CHECK GOOD. ACFT OK FOR SERVICE . 2 L 7 2 4F RT A16WE 20081009 NM 2008 10 9 2008UALA05562 1 20080901 A 2560 65659733 GIRT BAR BOEING 737 737322 1384676 NM L2 DOOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 329UA 24149 GIRT BAR LOCKS ARE LOOSE AT 2L. FOUND LOOSE GIRT BAR LOCKS. SECURED FLOOR LOCKS OP CHECK GOOD. ACFT OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20081009 CE 2008 10 9 GLB2008F00028 1 20080924 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 03 100UX UE100 MAJOR REPAIR CONFORMITY CHECK OF REPAIR ABOVE AIRSTAIR DOOR PERFORMED. MX FOUND STOP DRILLED CRACKS AROUND 2 RIVETS BOT H 1.25 FROM LT AND RT CENTERLINE OF STRINGER 1 AT 163.975. MX REMOVED OLD PATCH, REMOVED DAMAGED AREAS BY CUTTING OUT . 75" SKIN IN BOTH AREAS. MX INSTALLED SHIM MADE FROM ORIGINAL SKIN MATERIAL, THEN INSTALLED COVER PATCH IAW BEECH 1900 S RM 51-70-06. COVER PATCH MADE FROM NEW FACTORY SKIN MATERIAL 6.2" BY 4.1". RII INSPECTION COMPLIED WITH AT STATION 163 .975 PER TASKCARD 8.2.1 MX PERFORMED A PRESSURIZATION CHECK THAT WAS REQUIRED FOR MAJOR REPAIR OF FUSELAGE SKIN IN AW B MM 21-30. ALL CHECKS FOUND TO BE WITHIN LIMITS. 2 L 7 2 4T RT A24CE 20081009 NM 2008 10 9 HNAA0800288 1 20080905 A 2910 82910009159 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM NLG LEAKING A HNAA O OTHER K FLUID LOSS CL CLIMB 1 EA 07 808EX 299 NR2 HYDRAULIC SYSTEM DROPPED TO 1 QUART AFTER TAKE-OFF. RUDDER ISO KICKED IN, WITH NO LOSS OF PRESSURE. FOUND NLG UP L OCK HYDRAULIC LINE LEAKING. INSTALLED TEMP FLEX LINE, BLED AND SERVICED HYDRAULIC SYSTEM. LEAK CHECK GOOD ON GROUND. REMOVED FLEX LINE AND INSTALLED RIGID LINE. 2 H 7 2 4T RT A13NM 20081006 NM 2008 10 6 MWE2008F00036 1 20080830 A 3350 6011779 BATTERY PACK BOEING 717 717200 1383700 NM EMERGENCY LIGHT INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 910ME 55174 BOTH LT AND RT EXTERIOR EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY BATTERY PACK. (K) 2 L 7 2 4F TR A6WE 20081006 NE 2008 10 6 DHLA200800094 2 20080829 A 7220 NOSE BULLET BOEING 727 7272Q9 138448M NM PWA JT8 JT8D17R 52049 NE NR 1 ENGINE CONTAMINATED A DHLA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 01 741DH 21931 WHEN TAKE OFF THRUST WAS APPLIED ENG NR 1 AND NR 3 AT 2.19 EPR SHOWED 88% N1 520* EGT. 90% N2. FAILED TO MAKE TAKE OFF OFF THRUST. REMOVED DEBRIS WITH DRY NITROGEN OUTWARD THROUGH NOSE DOME ON NR 1 & NR 3 ENG. NOSE DOME NOT REMOVED. PT 2 LINES RESECURED. PERFORMED ENG RUNS ON NR 1 & NR 3 ENGINES. OPS CK GOOD REF B727 JRH CHPT 5.2 COWLINGS SECURED. A/C OK TO CONTINUE. FLIGHT NR 119. ACFT WAS GROUNDED. 2 L 7 3 4F 4 F RT A3WE E2EA 20081006 EA 2008 10 6 A6WA200840560 1 20080810 A 2750 BPSU CNDAIR CL600 CL6002B19 1900309 EA T/E FLAP MALFUNCTIONED A A6WA O OTHER F FLT CONT AFFECTED DE DESCENT 1 GL 31 429AW 7711 FLAPS FAIL CAUTION MESSAGE. FLAPS FAILED AT 8 DEGREES IN FLIGHT. R&R RT BPSU AND RE-RIGGED FLAPS IAW AMM 27-50. 2 L 7 2 4F RT A21EA 20081006 WP 2008 10 6 AALA200802118 1 20080816 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9628W 53598 LGA SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 21D TO 32D INOPERATIVE. REPAIRED BROKEN WIRE TO CONNECTOR AT SEAT 29D FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081007 NM 2008 10 7 F3LA200800580 1 20080822 A 5321 D5367151300000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 928FR 2236 REFERENCE NON ROUTINE C049995. DURING C3 C-CHECK INSPECTION NOTED THE FORWARD OUTBOARD CORNER WAS DAMAGED ON FLOOR PANEL 242LF. MX REPAIRED DAMAGE TO PANEL 242LF IN ACCORDANCE WITH THE REQUIREMENTS OF ENGINEERING AUTHORIZATION NR A9-53R-30 577. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081007 NM 2008 10 7 F3LA200800588 1 20080826 A 5321 D5367175604800 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 928FR 2236 REFERENCE NON ROUTINE CO50125. DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 261PF HAS A CORRODED INSERT ON THE LT HA ND SIDE AND DELAMINATION IN THE SAME AREA. MX REPAIRED PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF ENGINEERING AUTHORI ZATION NR A9-53R-30588. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081007 CE 2008 10 7 DXT2008F00001 1 20080826 A 3240 BRAKE SYS CESSNA 500 560CESSNA 2076750 CE DEFECTIVE E DXTA O OTHER O OTHER NR NOT REPORTED 1 GL 07 398QS 5600522 INITIAL BRAKE CHECK ON F/O SIDE UPON LEAVING CHOCKS IS SATISFACTORY. HOWEVER, AFTER FLIGHT THE F/O BRAKES ARE COMPLETEL Y INEFFECTIVE. 2 L 7 2 4F RT A22CE 20081007 CE 2008 10 7 DXT2008F00002 1 20080827 A 3240 BRAKE SYS CESSNA 500 560CESSNA 2076750 CE INOPERATIVE E DXTA O OTHER O OTHER LD LANDING 1 GL 07 398QS 5600522 BRAKING UPON TOUCHDOWN WAS NONEXISTENT FOR APPROX 2-3 SECONDS FOLLOWING TOUCHDOWN. 2 L 7 2 4F RT A22CE 20081007 NM 2008 10 7 DXT2008F00003 1 20080828 A 3230 UNKNOWN AMD FALC50 FALCON2000 2730170 NM LANDING GEAR MALFUNCTIONED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 253QS 153 AFTER SELECTING GEAR UP, THE GEAR RETRACTION APPEARED TO BE VERY SLOW. WE THEN HAD 3 RED GEAR LIGHTS AND FLASHING GEAR HANDLE. 2 L 7 2 4F RT A50NM 20081007 NM 2008 10 7 KCSA081424 1 20080827 A 5311 FRAME BOEING 747 747122 1384872 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FUSELAGE FRAME IS DENTED AT STA 1800, STR 10R. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081425 1 20080827 A 5311 FRAME BOEING 747 747122 1384872 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FUSELAGE FRAME IS DENTED AT STA 1760, STR 11R. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081426 1 20080827 A 5311 FRAME BOEING 747 747122 1384872 NM FUSELAGE DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FUSELAGE FRAME IS DENTED AT STA 1740, STR 11R. 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081434 1 20080828 A 5330 SKIN BOEING 747 747122 1384872 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STA-2484 AT WL-216 AT LBL-60 SKIN HAS CORROSION 24" BELOW HOR. STAB. 2 L 7 4 4F RT A20WE 20081007 NE 2008 10 7 MAS2008F00063 2 20080823 A 7200 ENGINE DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE RIGHT MALFUNCTIONED A MASA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 07 803ML 49726 ACFT REJECTED TAKE OFF 70 KNOT DUE TO RT ENGINE DID NOT ACCELERATE (EPR 1.14). MX PERSONNEL CHECKED THE RT ENGINE IAW M M 72-00-00 PAGE 501, ALL CORRECT. ADDITIONALLY, A HIGH ENERGY STOP INSPECTION WAS PERFORMED IAW MM 05-57-00, NO DAMAGES WERE FOUND. DURING OVERNIGHT CHECK, MX PERSONNEL PERFORMED SLOW ACCELERATION TROUBLE SHOOTING IAW 72-00-04, ALL CORREC T. 2 L 7 2 4F 4 F RT A6WE E9NE 20081007 NE 2008 10 7 MAS2008F00065 2 20080823 A 7530 PRBC DOUG DC9 DC987 3022087 WP PWA JT8 JT8D219 52053 NE RT ENGINE MALFUNCTIONED A MASA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 07 803ML 35810 49726 ACFT REJECTED TAKE OFF AT 70 KNOTS DUE TO RT ENGINE DID NOT ACCELERATE. MX PERSONNEL REPLACED PRBC`S IAW MM 75-31-01 AN D FCU IAW 73-20-01. ADDITIONALLY THE PS3 WAS VERIFIED AND CLEANED, THE BLEED VALVES WERE LUBRICATED IAW 75-31-05 AND TR IM BOTH ENGINES WAS PERFORMED IAW MM 71-00-00, ALL CORRECT. AS A COMPLIMENTARY ACTION, A HIGH ENERGY STOP INSPECTION WA S PERFORMED IAW MM 05-57-00, NO DAMAGES WERE FOUND. 2 L 7 2 4F 4 F RT A6WE E9NE 20081007 EA 2008 10 7 MAS2008F00076 1 20080824 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA CABIN LOOSE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 AIRSHUTTLE 2997 IN PHX THE CREW REPORTED THE FLOOR PATH LIGHTING FWD OF ROW 5 INOP. MX RESECURED A LOOSE CONNECTOR ON T HE FLOOR PATH LIGHTING STRIP. 2 L 7 2 4F RT A21EA 20081007 NM 2008 10 7 EIA2008040 1 20080828 A 3350 SIGN BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE CABIN DEFECTIVE A EIAA O OTHER O OTHER NR NOT REPORTED 1 NM 19 485EV 20712 EXIT SIGN OVER CREW STAIR FOUND BELOW 100 M/L. REPLACED PER AMM 20-51-01. 2 L 7 4 4F 4 F RT A20WE E20EA 20081007 NM 2008 10 7 EIA2008039 1 20080828 A 5330 SKIN BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE FUSELAGE CRACKED A EIAA O OTHER O OTHER NR NOT REPORTED 1 NM 19 485EV 20712 FUSELAGE BOTTOM SKIN AT BS 2061 5-45R CRACKED APPROX 2 INCHES. REPAIRED PER SRM 53-30-03 FIG 1. 2 L 7 4 4F 4 F RT A20WE E20EA 20081007 NM 2008 10 7 EIA2008036 1 20080828 A 5330 SKIN BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE FUSELAGE CRACKED A EIAA O OTHER O OTHER NR NOT REPORTED 1 NM 19 485EV 20712 FUSELAGE BS 740 TOP AFT OF VHF BL 0 SURFACE SKIN CRACKED. REPAIRED PER SRM 53-30-03 FIG 48. 2 L 7 4 4F 4 F RT A20WE E20EA 20081007 WP 2008 10 7 ARW2008F00001 1 20080827 A 5610 NBA6045501OFF WINDSHIELD DOUG DC10 DC1030 3023501 WP COCKPIT CRACKED A ARWA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 29 524MD 46999 CAPTAIN`S WINDSHIELD ARCED; IT APPEARS TO HAVE AN APPROXIMATELY 6 INCH CRACK ON OUTER PANEL. PERFORMED ATT PROCEDURE "WI NDSHIELD OR CLEARVIEW WINDOW CRACKED OR ARCING; FLIGHT RETURNED TO DEPARTURE IAW COMPANY`S REQUEST. REMOVED CAPTAIN`S W INDSHIELD IAW AMM 56-11-00. INSTALLED LT CAPTAIN`S WINDSHIELD WINDOW IAW MM 56-11-00. (K) 2 L 7 3 4F A22WE 20081007 2008 10 7 Z3O2008F00000 4 20080817 A 6122 DRIVE GEAR HARTZL PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA HARTZL HCE3Y HCE3YR2A GL GOVERNOR BROKEN E Z3OA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION NR NOT REPORTED 1 EA 03 27956 1644 D2966TJ 317952064 L115568A DJ9323A PILOT REPORTS RT ENGINE WENT INTO FEATHER AND SHUT DOWN DURING FLIGHT, AFTER INSPECTION, FOUND RT GOVERNOR DRIVE GEAR SH EARED FROM GOVERNOR, THE THREE JOINTS THAT ATTACH THE DRIVE GEAR TO THE GOVERNOR HAD BEEN BROKEN OFF ALLOWING GEAR TO CO ME OUT. AFTER REVIEW OF THE THREE PIECES, IT LOOKED LIKE THEY HAD BEEN PARTIALLY BROKEN FOR A WHILE. (K) 1 L 7 2 3O 3 O A20SO E14EA 5 C P33EA 20081007 NM 2008 10 7 USAA920081634 1 20080904 A 5755 654645170A SPOILER BOEING 737 7374B7 1384702 NM NR 8 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 456UW 25020 CLT C4 MAJOR REPAIR NR 03C40057003/015 NR 8 SPOILER DELAMINATED ALONG TRAILING EDGE. REPLACED NR 8 SPOILER IAW B737 AMM 27-62-91. 2 L 7 2 4F RT A16WE 20081007 NM 2008 10 7 ABXA080236 1 20080904 A 3350 20131A BATTERY BOEING 767 767281 1385109 NM E&E BAY DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 773AX 22788 EMERGENCY LIGHT INOPERATIVE. SWAPPED EMERGENCY BATTERY WITH SPARE BATTERY. IAW B767 AMM 33-51-00. 2 L 7 2 4F RT A1NM 20081007 WP 2008 10 7 ABXA080234 1 20080825 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 959AX 47761 COCKPIT EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES. IAW DC9 AMM 33-53-00-8. 2 L 7 2 4F A6WE 20081007 EA 2008 10 7 SIM2008F00021 1 20080823 A 3350 20131A BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 523AE 10152 ON FLIGHT 3939 CREW REPORTED ON PRE FLIGHT EMERGENCY LIGHTS INOPERATIVE C/A. R&R BATTERY PACK IAW AMM 33-51-17. ACFT R ETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 20081007 SO 2008 10 7 SIM2008F00022 1 20080822 A 3350 20131A BATTERY PACK EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 654AE 145437 ON FLIGHT 4123 CREW REPORTED EMERGENCY LIGHTS INOPERATIVE. ACFT REMOVED FROM SERVICE C/A. R&R NR 1 BATTERY PACK. OPS CHECKS GOOD. ACFT RETURNED TO SERVICE 2 L 7 2 4T RT T00011AT 20081007 SO 2008 10 7 UG82008F00002 1 20080908 A 2742 ACTUATOR GULSTM G1159 GIV 3980115 SO VERTICAL STAB MALFUNCTIONED E UG8A O OTHER O OTHER NR NOT REPORTED 1 GL 23 5113 4013 INCIDENT OCCURRED AFTER DEPARTURE FROM DTW AND DURING CLIMBOUT AT 11000 FT WITH AUTOPILOT ENGAGED IN SMOOTH AIR, CONTROL WHEEL JOLTED FWD BRIEFLY AND "UNCOMMANDED STAB" AMBER ICAS MESSAGE ILLUMINATED. NO FURTHER UNCOMMANDED INPUTS TO STAB O CCURRED. AIRCREW COMPLIED WITH APPROPRIATE CHECKLIST REQUIREMENTS. AC RETURNED WITHOUT FURTHER INCIDENT. (K) 2 L 7 2 4F RT A12EA 20081007 EA 2008 10 7 SIMA200824601 2 20080828 A 7200 AE3007A13 ENGINE EMB 135 EMB135LR 3260305 SO RROYCE AE3007 AE3007A13 54166 EA RIGHT MALFUNCTIONED A SIMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 713AE 10712 145249 CAE311378 ON FLIGHT 4629 CREW REPORTED DURING CLIMB OUT THAT THEY RECEIVED A LAV SMOKE WARNING AND REPORTED A SMELL. CREW RETURNE D TO RDU WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R&R RT ENGINE IAW EMB WORK CARD NR 71-000-00. OPS CHECKED GOOD AND LEAK CHECK GOOD. ACFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081007 SO 2008 10 7 SIMA200824603 1 20080829 A 3260 PROXIMITY SWITCH EMB 135 EMB135LR 3260305 SO MLG OUT OF ADJUST A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 728AE 145328 ON FLIGHT 4700 CREW REPORTED AFTER TAKEOFF LG AIR GRND FAIL CAUTION CAME ON. COULD NOT RETRACT LANDING GEAR. COMPLIED AOM VOL 1. RETURNED TO AIRPORT. NORMAL LANDING WAS MADE LANDING WAS NOT OVERWEIGHT. LESS THAN 300 FEET PER MINUTE WEI GHT WAS 38000 LBS. C/A. R&R RADIO ALTIMETER COAX CABLES AND ALTIMETER ANTENNAS. RESET ALL GAPS ON ALL WEIGHT ON WHEEL S PROX SWITCHES AND PERFORMED ALL OPS CHECKS. OPS CHECKS GOOD. FCF WAS PERFORMED SATISFACTORY. ACFT RETURNED TO SERVI CE. 2 L 7 2 4F RT T00011AT 20081007 NM 2008 10 7 F3LA200800598 1 20080904 A 5321 D5367180500500 FLOOR PANEL AIRBUS A319 A319111 3930336 NM FUSELAGE CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 929FR 26 2240 REFERENCE NON ROUTINE C050516. DURING C3 C-CHECK, INSPECTION NOTED FLOOR PANEL 262FF HAS CORROSION ON LOWER SURFACE. M X R&R FLOOR PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 AMM 53-42-12 PB 401. UPON COMPLETION OF THE REPAIR, IT WA S INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081007 NM 2008 10 7 F3LA200800589 1 20080904 A 5321 D5367301800100 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 929FR 26 2240 REFERENCE NON ROUTINE C050366. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL I52UG WAS PUNCTURED. MX REPAIRED C ARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081007 NM 2008 10 7 F3LA200800590 1 20080904 A 5321 D5367301900000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 929FR 26 2240 REFERENCE NON ROUTINE C050368. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL I51TG WAS PUNCTURED. MX REPAIRED C ARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081007 NM 2008 10 7 F3LA200800591 1 20080904 A 5321 D5367301800000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 929FR 26 2240 REFERENCE NON ROUTINE C050370. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL I51UG WAS PUNCTURED. MX REPAIRED C ARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081007 NM 2008 10 7 F3LA200800593 1 20080904 A 5321 D5367303801000 FLOOR PANEL AIRBUS A319 A319111 3930336 NM CARGO BAY PUNCTURED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 929FR 26 2240 REFERENCE NON ROUTINE C050374. DURING C3 C-CHECK, INSPECTION NOTED TRANSITION PANEL 161BF WAS PUNCTURED. MX REPAIRED C ARGO COMPARTMENT TRANSITION PANEL IN ACCORDANCE WITH THE REQUIREMENTS OF A319 SRM 53-02-00 FIGURE 204. UPON COMPLETION OF THE REPAIR, IT WAS INSPECTED AND FOUND ACCEPTABLE. 2 L 7 2 4F RT A28NM 20081007 EA 2008 10 7 TRAX200801075 1 20080831 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 856AS 7404 PAX DR OUTER HANDLE BROKEN 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 TRAX200801076 1 20080831 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BROKEN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 853AS 7374 PAX DOOR HANDLE BROKEN COMPLETELY SHEARED OFF. GATE RETURN. R&R PAX DOOR OUTER HANDLE IAW AMM 52-11-03. 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 TRAX200801077 1 20080831 A 5320 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 932EV 8016 UNDER FLOOR INTERCOSTAL ATTACH CLIP IS CRACKED AT THE O/B SIDE OF LBL 27, FS 484, WL 73. C/A REMOVED CRACKED CLIP AT FS 484 LBL 27. LOCATED, DRILLED AND INSTALLED NEW CLIP. ALL WORK PERFORMED IAW BOMBARDIER REO 601R-53-41-059. REPAIRED COMPLIED WITH IAW ASA ECTC 601R-53-41-059. ASA RII COMPLIED WITH 5300041. 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 TRAX200801080 1 20080831 A 5210 SETSCREW CNDAIR CL600 CL6002B16 1900305 EA PAX DOOR OUT OF ADJUST A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 923EV 7826 CREW REPORTS PAX DOOR HARD TO OPEN. ADJUSTED PAX DOOR INNER HANDLE SET SCREW OPS CHECK GOOD AT THIS TIME. PER CRJ200 A MM 52-11-00. 2 L 7 2 4F RT A21EA 20081007 EA 2008 10 7 TRAX200801081 1 20080831 A 1100 PLACARD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT TORN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 932EV 8016 JOB 8801625 OPERATION 70 CREW ESCAPE HATCH EMERGENCY EXIT PLACARD IS TORN. RESOLVED ON W/O 98370 TASKCARD NR 00349. C/ A APPLIED NEW SILKSCREEN IAW CRJ 200 MM 11-10-03-400-801. 2 L 7 2 4F RT A21EA 20081007 WP 2008 10 7 NWAA084109865 1 20080831 A 2161 CONTROLLER DOUG DC9 DC951 3022051 WP CABIN TEMP DEFECTIVE A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 774NC 47776 DURING CLIMB AS THE ACFT DEPARTED MSP THE FLIGHT ATTENDANT REPORTED A BURNING SMELL THROUGHOUT THE CABIN. NO MENTION OF COM COMPLIANCE BUT THE FLIGHT CREW DID DECLARE A YELLOW EMERGENCY AND RETURNED TO AN UNEVENTFUL LANDING BACK AT MSP. P ASSENGERS DEPLANED NORMALLY THROUGH THE JET BRIDGE AT THE GATE. MX PERFORMED MINIMUM WORK SCOPE FOR SMOKE IN THE CABIN AND FOUND THE NR 2 AUTO-TEMP CONTROL WAS FAULTING. TEMP CONTROLLER AND BOTH WATER SEPARATORS WERE REPLACED. SYSTEM WAS LEAK CHECKED. 2 L 7 2 4F RT A6WE 20081007 WP 2008 10 7 NWAA084119865 1 20080829 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 774NC 47776 DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE VENTRAL STAIRWAY WAS INOPERATIVE. MX REPLACED TH E BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 2 L 7 2 4F RT A6WE 20081007 CE 2008 10 7 Z5F2008F00004 1 20080828 A 3240 215881 BRAKE CESSNA 500 550 2076604 CE LT MLG WORN E Z5FA K NONE O OTHER LD LANDING 1 EA 63 342CS 571 461 5501101 UPON LANDING, LT MAIN TIRE BLEW. SHORTLY THERE AFTER, THE RT MAIN TIRE ALSO BLEW. AIRCRAFT CAME TO A STOP ON THE RUNWAY . BOTH BRAKES AND BOTH MAIN WHEELS AND TIRES REPLACED. ANTI SKID SYSTEM CHECKED NORMAL, BRAKES BLED, TAXI CHECK PERFORME D OK, AND AC RETURNED TO SERVICE. (K) 1 L 7 2 4F A22CE 20081007 WP 2008 10 7 U2R2008F00002 1 20080825 A 5740 BRACKET DOUG DC8 DC871F 302199D WP BOOST PUMP CRACKED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 872SJ 46040 DURING C-CHECK INSP, FOUND LT WING NR 1 ALTERNATE FUEL TANK INTERIOR BOOST PUMP BRACKET FITTING (2) CRACKS. (K) 2 L 7 4 4F RT 4A25 20081007 WP 2008 10 7 U2R2008F00003 1 20080825 A 5720 SUPPORT ANGLE DOUG DC8 DC871F 302199D WP LT WING CRACKED A U2RA K NONE O OTHER IN INSP/MAINT 1 GL 23 872SJ 83402 46040 DURING C-CHECK INSP, FOUND LT WING X RS 71, 5-52 NR 2 MAIN FUEL TANK INTERIOR LOWER SUPPORT ANGLE CRACKED. (K) 2 L 7 4 4F RT 4A25 20081007 CE 2008 10 7 GLB2008F00020 1 20080902 A 5311 FRAME BEECH 1900 1900D 1154162 CE FS 177 S9AR CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 21 211GL 26826 UE211 DURING STRUCTURAL INSP MAINT FOUND FRAME CRACKED AT STRINGER CUTOUT FS 177.3 AT STRINGER 9AR. LENGTH OF CRACK APPROXIMAT ELY .750. (K) 2 L 7 2 4T RT A24CE 20081007 SO 2008 10 7 C2X2008F00029 1 20080904 A 5751 14574000420 BONDING STRAP EMB 145 EMB145XR 3260214 SO LT AILERON CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16151 7507 145758 AC IS CURRENTLY IN C-CHECK AND THE LT AILERON SHROUD BONDING STRAPS WERE FOUND CORRODED. MAINT REMOVED AND REPLACED THE BONDING STRAP PLATE IAW EC 5750-01315. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. (K) 2 L 7 2 4F RT 20081007 SO 2008 10 7 C2X2008F00032 1 20080812 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12163 14500811 DURING ROUTINE MAINTENANCE, MX FOUND EXIT ROW IDENTIFIER LIGHT OUT AT ROW 12A INOPERATIVE. MX REMOVED AND REPLACED EMERG ENCY LIGHT POWER SUPPLY ASSY AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AC WAS APPROVED TO RETURN TO SERVICE. (K) 2 L 7 2 4F RT 20081007 SO 2008 10 7 C2X2008F00033 1 20080828 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13988 145265 DURING ROUTINE MAINTENANCE, MX FOUND SEAT 12 BC OVERHEAD SQUARE EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED LIG HT BULB AND PERFORMED OPERATIONAL SUCCESSFULLY. AC WAS APPROVED TO RETURN TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081007 SO 2008 10 7 C2X2008F00034 1 20080827 A 3320 7281000501 CONTROL MODULE EMB 145 EMB145LR 3260212 SO CABIN LIGHTS ODOR A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 12564 145618 FLIGHT CREW REPORTED BURNING SMELL IN FWD CABIN AND ELECTRICAL ODOR AS WELL. EWR MX FOUND POOR GROUND AT GS 8008DC. THEN AREA WAS CLEANED AND GROUND RESECURED. MX ALSO REMOVED AND REPLACED CABIN LIGHT CONTROL MODULE. MX PERFORMED OPERATION AL CHECK SUCCESSFULLY. AC WAS APPROVED TO RETURN TO SERVICE. (K) 2 L 7 2 4T RT T00011AT 20081007 SO 2008 10 7 C2X2008F00035 1 20080829 A 3320 7281000501 CONTROL MODULE EMB 145 EMB145XR 3260214 SO CABIN LIGHTS ODOR A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 11150 145756 FLIGHT CREW REPORTED LT SIDE CABIN LIGHT INOPERATIVE AND BURNING SMELL IN CABIN. EWR MX REMOVED AND REPLACED CONTROL MOD ULE FOR SIDE LIGHTS. CLEANED GROUND STUD FOR PINK FOR THE MODULE. (K) 2 L 7 2 4F RT 20081007 NM 2008 10 7 QXEA200800423 1 20080418 A 5310 STOP FITTING DHAV DHC8 DHC8202 2809007 NM FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 355PH 500 PDX C4 CHECK. MCD SURROUND STOP FITTINGS ALL HAVE SIGNS OF WEAR. BLENDED FITTINGS IAW -8 200 RD8-53-3933 PG 4, PARA 1. 2. WITHIN LIMITS. INSPECTED AS PER RD8-53-3933 NO CRACKS NOTED. COLD GALV. PRIMED STOP FITTINGS IAW -8 200 RD8-53-393 3 PG 4, PARA 4-7. 2 H 7 2 4T RT A13NM 20081007 NM 2008 10 7 AALA200802075 1 20080812 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 343AN 33082 DFW EMERGENCY LIGHT AT OVERHEAD FORWARD GALLEY RT HAND SIDE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD F ORWARD GALLEY RT HAND SIDE. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081007 NM 2008 10 7 UIE2008F00030 1 20080918 A 5320 7075T6020 WEB BOEING 747 74747UF 1384812 NM GE CF6 CF680C2B6F 30025 NE BS 1800 CANNING A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 418MC 32840 AFT CARGO COMPARTMENT FOUND FRAME WEB ALL CAN AT STA 1800, LBL 17 INCHES, S:60L. REPAIRED FRAME WEB OIL CAN AREA AT AFT CARGO COMPARTMENT STA 1800, LBL 16 TO LBL 20S:50L, FABRICATED IAW SRM 63-00-07, REV 48 AND SRM 51-40-02 REV 48 AND EO N R 4453A207. (K) 2 L 7 4 4F 4 F RT A20WE E13NE 20081007 NM 2008 10 7 UIE2008F00034 1 20080918 A 5330 86B07662162 SKIN BOEING 747 74747UF 1384812 NM GE CF6 CF680C2B6 30025 NE BS 380-440 DAMAGED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 418MC 32840 DURING PFM J/C: MCIA016, REPLACE 6 BLIND FASTENER FOUND DEVIATION FOR STA 380, 440, S-1R MISS DRILLING HOLE. ACCOMPLISHE D THE SEA DOUBLER HOLES ON SKIN COMMON TO THE STRAP AT BS 380, 440, AND 480 BETWEEN S1R AND A2R. (K) 2 L 7 4 4F 4 F RT A20WE E13NE 20081007 NM 2008 10 7 UIE2008F00035 1 20080918 A 5320 SHIM BOEING 747 74747UF 1384812 NM RT MLG WW MIGRATED A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 418MC 32840 SHIM MIGRATION AT RT BODY GEAR W/W FUSELAGE LONGERON STRUCTURE STATION 1468-1480. SHIM REPLACED IAW SRM 51-20-08, REV 48 , SR ID NR 1-937881538 AND EO NR 4453A203. (K) 2 L 7 4 4F RT A20WE 20081007 2008 10 7 RYN2008F00013 4 20080901 A 3442 ANTENNA BOEING 757 7572G5 1384912 NM WX RADAR SYS FAILED A RYNA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 31 929RD 23929 AIR TURN BACK DUE TO WEATHER RADAR FAILED BEFORE ENTERING ETOPS AIRSPACE. REMOVED WATER FROM THE ANTENNA RESET THE SYSTE M OPS CHECKED NORMAL. (K) 2 L 7 2 4F RT A2NM 20081008 NM 2008 10 8 QXEA200800955 1 20080902 A 3260 WARNING SYSTEM BOMBDR DHC8 DHC8402 1390042 NM COCKPIT ACTIVATED A QXEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 19 417QX 4086 GTF FLIGHT 2322 SEA-GTF. ON SHORT APPROACH THE GREEN NOSE GEAR LIGHT WENT OUT AND THE AMBER NOSE LIGHT CAME ON. THEN A CLUNK WAS HEARD. PERFORMED A MISSED APPROACH AND AN ALTERNATE GEAR EXTENSION. ALL INDICATIONS WERE GREEN AND ACCOMPLI SHED A UNEVENTFUL LANDING. ACFT WAS TOWED FROM THE RUNWAY. ACFT FERRIED FROM GTF TO PDX FOR REPAIRS. 2 H 7 2 4T RT A13NM 20081008 NM 2008 10 8 AALA200802055 1 20080809 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW EMERGENCY LIGHT AT SEAT 33C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 33C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802052 1 20080809 A 3350 LAMP BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW EMERGENCY LIGHT AT SEAT 24C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802051 1 20080809 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW EMERGENCY LIGHT AT SEAT 24C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802050 1 20080809 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW EMERGENCY LIGHT AT SEAT 21C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 21C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 SPA2008F00000 1 20080901 A 3350 900835 BATTERY PACK BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D15 52051 NE EMERGENCY LIGHT FAILED A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 07 712S 23038 MID CABIN CEILING EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. REPLACED BATTERY PACK AND POWER SUPPLY IAW MM 33-51-81. FUN CTIONAL CHECK SATISFACTORY. (K) 2 L 7 2 4U 4 F RT A16WE E2EA 20081008 2008 10 8 AALA200802045 4 20080808 A 2565 D30654122 SLIDE BOEING 757 757223 1384957 NM NR 1 DOOR FAILED A AALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 673AN 29423 SEA SLIDE WAS UNSUCCESSFULLY DEPLOYED FROM LT NR 1 DOOR WHEN OPENED FROM OUTSIDE. SLIDE PULLED OUT OF HARDPACK AND HANG ING FROM GIRTH BAR. REPLACED SLIDE AND DOOR ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 NM 2008 10 8 KCS2008F00015 1 20080913 A 5330 SKIN BOEING 747 747249F 1384849 NM BS 1960-2180 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 FUSELAGE SKIN HAS CORROSION AROUND FASTENER HEADS AT STA 1960 TO 2180, STR 46R. (K) 2 L 7 4 4F RT A20WE 20081008 WP 2008 10 8 AALA200802036 1 20080806 A 3233 39281375001 RETRACT CYLINDER DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 573AA 53092 STL INFLIGHT T2028/06AUG. CREW REPORTED UNSAFE NOSE GEAR LIGHT. NOSE LANDING GEAR WOULD NOT RETRACT. RETURNED TO STL AND LANDED WITHOUT INCIDENT. REPLACED RETRACT CYLINDER AND BUNGEE CYLINDER. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081008 CE 2008 10 8 NSV2008F00024 1 20080904 A 5210 SEAL BEECH 1900 1900D 1154162 CE PAX DOOR BROKEN A NSVA O OTHER O OTHER NR NOT REPORTED 1 EA 27 191CJ UE19 ACFT OVER SCUPP AT 12,000 FEET THE PAX DOOR SEAL BROKE. THE CREW DECLARED AN EMERGENCY AND DESCENDED BELOW 10,000 FEET. THE ACFT LANDED WITHOUT INCIDENT IN BOSTON 2 L 7 2 4T RT A24CE 20081008 EA 2008 10 8 VNAA0809004 1 20080912 A 3234 7455025 HANDLE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE COCKPIT FAILED A VNAA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 05 244PS 10511 7912 CREW REPORTED LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. ANTI-SKID INBD AMBER AND PARKING BRAKE SOV AMBER MSG DISPL AYED. AFTER 3 MINUTES, MSG WENT AWAY AND LANDING GEAR RETRACTED. THE ACFT LANDED IN CLT WITHOUT INCIDENT. MX INSPECTE D THE ACFT, PERFORMED ANTI-SKID TESTS AND R&R THE LANDING GEAR HANDLE ASSEMBLY. NO OTHER DEFECTS WERE NOTED. THE ACFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20081008 WP 2008 10 8 AALA200802147 1 20080820 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 73444 49470 LGA EMERGENCY LIGHT AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD CABIN. SYSTEM G ROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081007 NM 2008 10 7 MWE2008F00040 1 20080905 A 2611 CBAB110001 SMOKE DETECTOR BOEING 717 717200 1383700 NM LT LAV FAILED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 13 914ME 55177 LT LAVATORY SMOKE DETECTOR TEST FAILED. REMOVED AND REPLACED SMOKE DETECTOR. (K) 2 L 7 2 4F TR A6WE 20081007 NM 2008 10 7 MAS2008F00075 1 20080824 A 3350 20412 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 456YV 1151 456 ASH FLT 7092 MTG-GJT. ALL 4 EMERGENCY LIGHTS WERE INOP. MX REPLACED NR 3 EMERGENCY LIGHT BATTERY AND OPS CHECK WAS GOO D. 2 H 7 2 4T RT A13NM 20081007 NM 2008 10 7 USAASB08077 1 20080902 A 2560 P2070003001 BATTERY BOEING 737 737401 1384701 NM FLASHLIGHT DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 405US 23885 CLT MX REPORTED A LOW BATTERY IN FLASHLIGHT AT FORWARD FLIGHT ATTENDANT STATION. MX R&R THE FLASHLIGHT. OPS CHECK NORM AL. 2 L 7 2 4F RT A16WE 20081007 2008 10 7 USAABB08145 4 20080809 A 3425 B254ADM1 INVERTER BOEING 757 7572B7 1384964 NM COCKPIT INOPERATIVE A USAA A UNSCHED LANDING I FLT. ATTITUDE INST. CR CRUISE 1 EA 19 206UW 46203 27808 PHL FLT 798 ENROUTE PHL TO AMS. THE STANDBY ATTITUDE INDICATOR FAILED ABOUT 45 MINUTES AFTER DEPARTURE. THE DECISION W AS MADE TO RETURN TO PHL. THE FLIGHT RETURNED WITHOUT FURTHER INCIDENT. MX REPLACED THE STANDBY HORIZON INVERTER. OPS CHECKS OK. 2 L 7 2 4F RT A2NM 20081007 2008 10 7 CNM2008F00001 2 20080903 A 7200 ENGINE DOUG DC10 DC1030 3023501 WP NR 1 ENGINE OVERHEATED A CNMA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 531AX 48316 DURING CLIMB THRU 15000 FT N2 103.4 TAT +20 NACELLE TEMP WAS 240 DEGREE C PREV SUPPLY SELECTED OFF AXCELL TEMP DECREASED 10 DEGREES C STILL 40 DEGREE C ABOVE QRH CHARTED VALVE (NR 1 ENG). (K) 2 L 7 3 4F A22WE 20081007 NE 2008 10 7 EIA2008F00003 2 20080904 A 7200 CF650E2 ENGINE BOEING 747 747230B 1384889 NM GE CF6 CF650E2 30018 NE NR 3 STALLED A EIAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 19 488EV 94761 23287 517736 DURING TAKEOFF EGT`S WERE PEAK 934,908,908,913 ON ENG`S ONE THRU FOUR. AUTO THROTTLES WERE ON. AFTER REDUCTION TO CLIMB POWER, PASSING THRU 1800`, IN LEFT TURN WE HEARD A LOUD BANG ACCOMPANIED WITH AN AIRCRAFT SHUDDER. NOTICED NR 3 N1 ROLL ING BACK WITH N2 ROLLING BACK. NOTICED EGT DECREASING THRU 930 C. EGT GAGE OVERTEMP NEEDLE STOPPED AT 955 C. SHUTDOWN NR 3 ENGINE. DECLARED AN EMERGENCY, DUMPED FUEL TO GW OF 630,000. RETURNED TO DEPARTURE FOR UNEVENTFUL LANDING ON RWY 36. FUEL DUMPED. REMOVED AND REPLACED ENGINE IAW WITH EIA WORK CARD F7201-CF6. (K) 2 L 7 4 4F 4 F RT A20WE E23EA 20081007 NM 2008 10 7 EIA2008F00008 1 20080831 A 5240 SKIN BOEING 747 747132 1384882 NM R3 DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 R3 DOOR SKIN CRACKED AT NUMEROUS FASTENER HOLES AT LOWER CENTER DOOR FRAME. REMOVED DAMAGE, NDT AREA AND FABRICATED AND INSTALLED REPAIR IAW SRM 52-10-02, FIG 9 SHEETS 1-4. (K) 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 EIA2008F00009 1 20080818 A 5313 STRINGER BOEING 747 747409 13848AU NM BS 480 S10R CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 780BA 24310 BODY STATION 480, STRINGER 10 RT CRACKED. REPAIRED STRINGER IAW SB 747-63A2484, FIG 24. (K) 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081446 1 20080905 A 3350 LIGHT BOEING 747 747146 1384905 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 702CK 20332 RT EMERGENCY EXIT LIGHT INOPERATIVE ON THE UPPER DECK STA 590. (K) 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081479 1 20080907 A 5730 SKIN BOEING 747 747122 1384872 NM LT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 LT WING UPPER SKIN CORRODED AT FRONT SPAR, WS 380 TO 450. (K) 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081482 1 20080907 A 5512 SPLICE PLATE BOEING 747 747122 1384872 NM HORIZONTAL STAB CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 HORIZONTAL STAB CENTER SECTION LT SIDE SPLICE PLATE CRACKED IN FASTENER HOLE, AFT FASTENER HOLE OF THE 2ND ROW IB OF LBL 43.5, COMMON TO THE UPPER REAR SPAR CHORD. (K) 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081444 1 20080904 A 5320 WEB BOEING 747 747249F 1384849 NM BS 264 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 STA-264 UPPER DECK FLOOR WEB CRACKED "1 INCH WL-306. (K) 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081449 1 20080907 A 5730 SKIN BOEING 747 747122 1384872 NM LT WING CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 LT WING UPPER SKIN CORRODED AT FRONT SPAR, WS 380 TO 450. (K) 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081450 1 20080907 A 5315 FLOORBEAM BOEING 747 747122 1384872 NM BS 1720 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 BS 1720, BBL-0 FLOORBEAM UPPER T-CHORD DENTED. (K) 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081451 1 20080907 A 5340 STRINGER CLIP BOEING 747 747122 1384872 NM BS 2020 S48R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STRINGER CLIP DAMAGED AT BS 2020, STR-48R. (K) 2 L 7 4 4F RT A20WE 20081007 WP 2008 10 7 NWAA084179929 1 20080904 A 3397 CONNECTOR DOUG DC9 DC931 3022065 WP CABIN CORRODED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8923E 45838 DURING LINE CHECK MX FOUND THAT 2 OF THE 3 EMERGENCY PATHWAY LIGHTS IN THE VENTRAL STAIRWAY WERE INOPERATIVE. MX FOUND THE CATWALK LIGHTS CONNECTOR BETWEEN THE SECOND AND THIRD EEPL WAS CORRODED. AFTER IT WAS CLEANED AND SECURED THE LIGHT S TESTED AS FUNCTIONAL. 2 L 7 2 4F A6WE 20081007 NM 2008 10 7 NWAA084186302 1 20080904 A 3350 BATTERY BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK FOUND EMERGENCY EXIT SIGN UPPER DECK AFT INOP. MX R&R POWER SUPPLY AND BATTERY. OPS CHECKED GOOD AND ACFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20081007 CE 2008 10 7 Z5F2008F00005 1 20080905 A 2910 99121942 SWITCH CESSNA 525 525 2076601 CE HYD FLOW FAILED E Z5FA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 63 417CS 2102 525B0090 DURING CLIMB THROUGH FL 270, RT HYDRAULIC FLOW LIGHT ILLUMINATED. DIVERTED, DURING DECENT RT HYD FLOW LIGHT WENT OUT. R EMOVED DEFECTIVE RT FLOW SWITCH AND INSTALLED NEW SWITCH. HYDR INDICATION CHECKS NORMAL, AND AC RETURNED TO SERVICE. (K ) 1 L 7 2 4F RT A1WI 20081007 SO 2008 10 7 FFK2008F00002 2 20080902 A 7414 6314 CAM PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360EB 17025 SO LT MAGNETO WORN E FFKA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SO 05 3570M 498 347870117 PILOT REPORTED A "POPPING" SOUND COMING FROM THE LT ENGINE, AFTER INVESTIGATION MAINT FOUND THAT THE LT ENGINE LT MAGNET O CAM FOLLOWER EXCESSIVELY WORN. REPLACED MAGNETO AS NEEDED NO FURTHER PROBLEMS NOTED. (K) 1 L 7 2 3O 3 O A7SO E9CE 20081007 NM 2008 10 7 AALA200802087 1 20080812 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 750AN 30259 MIA EMERGENCY LIGHT AT FIRST CLASS GALLEY LT SIDE MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT FIRST CLASS GALLEY LT SIDE. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081007 NM 2008 10 7 AALA200802086 1 20080812 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 750AN 30259 MIA EMERGENCY LIGHT AT SEAT 20C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 20C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081007 NM 2008 10 7 AALA200802085 1 20080812 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 DFW EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT T00001SE 20081007 NM 2008 10 7 AALA200802084 1 20080812 A 3397 CONNECTOR BOEING 777 777223 1385213 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 776AN 29582 DFW EMERGENCY LIGHT AT SEAT 9G INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 9G. SYSTEM GROUND CHECKED NO RMAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 WRLA2008071 1 20080822 A 5312 AEA05282 DOUBLER DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE CENTER MLG WW CRACKED A WRLA O OTHER O OTHER NR NOT REPORTED 1 SO 11 277WA 48743 CENTER MLG WW RT BULKHEAD CUTOUT DOUBLER CRACKED AT RT FWD CORNER. 2 L 7 3 4F 4 F RT A22WE E24NE 20081008 2008 10 8 QXEA200800957 3 20080907 A 6140 WARNING SYSTEM BOMBDR DHC8 DHC8402 1390042 NM COCKPIT MALFUNCTIONED A QXEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 NM 19 401QX 4031 EAT - FLIGHT 2159. AFTER ADVANCING THE POWER LEVERS TO TAKEOFF A POWERPLANT MESSAGE WAS RECEIVED. ABORTED TAKEOFF AT 3 0 KNOTS AND RETURNED TO THE GATE. MX FOUND FAULT CODE 224A, NR 2 PROP. CLEARED BY AMM TASK 61-20-36-070-801. ACFT RET URNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081008 SO 2008 10 8 CHQA200800173 1 20080901 A 3231 22250100003 SOLENOID EMB 135 EMB135KL 3260302 SO ALLSN AE3007 AE3007A 03030 GL NLG FAULTY A CHQA O OTHER O OTHER NR NOT REPORTED 1 GL 11 295SK 145513 CAE312373 FLIGHT 5325 ICT TO STL. THE FLIGHT CREW REPORTED A LOUD AIR SOUND FROM THE NLG AREA DURING FLIGHT. THE ACFT LANDED WIT HOUT INCIDENT. MX INSPECTED THE ACFT AND FOUND THE NLG DOOR COMMAND CIRCUIT BREAKER TRIPPED. THROUGH FURTHER TROUBLESH OOTING, IT WAS FOUND THAT THE NLG CONTROL SOLENOID WAS AT FAULT. THE SOLENOID WAS REPLACED AND THE NOSE GEAR DOORS OPER ATED NORMALLY. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081008 NM 2008 10 8 AALA200802073 1 20080811 A 3241 429352 CONTROL UNIT BOEING 737 737823 13844BZ NM ANTI-SKID SYS FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 950AN 30087 IAD INFLIGHT T2192/11AUG MIA TO DCA. CREW REPORTED ANTI SKID LIGHT ILLUMINATED. LANDED IAD WITHOUT INCIDENT. REPLACED ANTI SKID AUTOBRAKE CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 AALA200802039 1 20080808 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 795AN 30257 JFK SEAT MOUNTED EMERGENCY LIGHTS AT FORWARD COACH CABIN INOPERATIVE. REPLACED BATTERY PACK AT RT NR 3 DOOR FOR INOPERA TIVE SEAT MOUNTED EMERGENCY LIGHTS AT FORWARD COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081008 SO 2008 10 8 RAIA00808025 1 20080824 A 3297 CONNECTOR EMB 145 EMB145LR 3260212 SO PROX SENSOR LOOSE A RAIA O OTHER N FALSE WARNING CL CLIMB 1 CE 03 839HK 14500829 FLT NR 7978 RIC LANDING GEAR AIR/GND DISAGREE MESSAGE ON THE EICAS AND THE GEAR WOULD NOT RETRACT. MX INSPECTED AND FO UND THAT THE NLG WOW PROXIMITY SENSOR CONNECTOR WAS LOOSE AND THAT THE RH MLG AIR/GND PROXIMITY SWITCH WAS OUT OF ADJUST MENT. CORRECTIONS WERE MADE AND THE SYSTEM CHECKED GOOD AS PER AMM PROCEDURES. 2 L 7 2 4T RT T00011AT 20081008 NM 2008 10 8 AALA200802132 1 20080819 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 794AN 30256 ORD EMERGENCY LIGHT AT SEAT 24C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802152 1 20080722 A 5313 141T3001 STRINGER BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 328AA 22328 AFW STRINGER 37 RT WAS CORRODED FROM STATION 424 TO STATION 445. REPAIRED IN ACCORDANCE WITH SRM 53-00-03-1R2 AND MRB 7 57 3259. 2 L 7 2 4F RT A1NM 20081008 NM 2008 10 8 AALA200802161 1 20080821 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 JFK EMERGENCY LIGHTS AT RT SEAT ROWS 30 TO AFT CABIN INOPERATIVE. REPLACED SHORTED LAMP AT SEAT 32G FOR EMERGENCY LIGHT S AT RT SEAT ROW 30 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802169 1 20080822 A 3350 SIGN BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 343AN 33082 ORD LT AISLE OVERHEAD EMERGENCY EXIT SIGN AT SEAT ROW 20 IS DAMAGED. REPLACED EXIT SIGN LIGHT ASSEMBLY FOR LT HAND AISL E EMERGENCY LIGHT AT SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081008 WP 2008 10 8 AALA200802171 1 20080822 A 3350 SHROUD DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 466AA 49596 DFW EMERGENCY LIGHT AT SEAT 7D MISSING SHROUD. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 7D. SYSTEM GROUND CHECKED N ORMAL OPS. 2 L 7 2 4F A6WE 20081008 NM 2008 10 8 KCSA081483 1 20080920 A 5210 STOP FITTING BOEING 747 747123 1384873 NM R3 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 R3 DOOR NR 3 STOP FITTING HAS A 3 INCH CRACK AT STA 1264, WL225. 2 L 7 4 4F RT A20WE 20081008 NM 2008 10 8 USAA920081688 1 20080909 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 23879 PIT FPBH MAJOR REPAIR NR 4353372 CRACK IN WEB OF RT VERTICAL BEAM OF 178 BULKHEAD AT RBL17, WL230. REPAIRED WEB OF RT V ERTICAL BEAM OF 178 BULKHEAD AT RBL17, WL230 IAW B737 SRM 53-10-08. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 USAA920081693 1 20080917 A 5310 6520723 DOOR FRAME BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 23879 PIT FPBH MAJOR REPAIR JOB CARD NR 03T20953001. CRACK IN FORWARD CARGO DOOR CUTOUT AFT FRAME BS492, S24R. REPAIRED FORW ARD CARGO DOOR CUTOUT AFT FRAME BS492, S24R IAW US AIRWAYS ER NR 111638. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 USAA920081698 1 20080916 A 5311 65C22908 FRAME BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03C20853011/002 FRAME CRACKED AT BS500B BETWEEN S20L & S21L. REPAIRED FRAME AT BS500B BETWEEN S2 0L & S21L IAW B737 SRM 51-10-02 & 51-70-11. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 USAA920081701 1 20080914 A 5320 INTERCOSTAL BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03C10753006/017 INTERCOSTAL CRACKED AT BS303, S10L. REPAIRED INTERCOSTAL AT BS303, S10L IAW B737 SRM 51-10-02 & 51-40-02. 2 L 7 2 4F RT A16WE 20081008 WP 2008 10 8 AALA200802177 1 20080824 A 2150 ACM DOUG DC9 DC982 3022082 WP A/C BAY SEIZED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 7542A 49996 TUS INFLIGHT T1540/24AUG. CREW REPORTED BURNING SMELL IN CABIN AND COCKPIT AND FLIGHT ATTENDANT REPORTED LIGHT SMOKE IN SIDE AFT STAIR AREA. RETURNED TO TUS AND LANDED WITHOUT INCIDENT. FOUND RT AIRCONDITIONING PACK AIR CYCLE MACHINE HAD SEIZED. REPLACED RT PACK AIR CYCLE MACHINE. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081008 NM 2008 10 8 2008UALA05649 1 20080906 A 5330 SKIN BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE BS 633-641 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 219UA 30551 BS 633-641 BETWEEN S27-28L MATERIAL REMOVED AND DENT IN SKIN AND IN SHEAR TIE BEYOND SRM LIMITS. INSTALLED DOUBLER REP AIR. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081008 NM 2008 10 8 2008UALA05651 1 20080908 A 3350 767 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 578UA 26694 SLIDE LIGHT INOP AT DOOR 2R. LAMP INOPERATIVE. REPLACED LAMP. CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081008 NM 2008 10 8 AALA200802180 1 20080824 A 3350 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AM 24579 DFW EMERGENCY LIGHT EXIT SIGN DECAL AT RT NR 1 EXIT DOOR DAMAGED. REPLACED DECAL FOR EMERGENCY LIGHT EXIT SIGN AT RT NR 1 EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 NM 2008 10 8 AALA200802181 1 20080824 A 3350 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AM 24579 DFW EMERGENCY LIGHT EXIT SIGN DECAL AT RT NR 2 EXIT DOOR DAMAGED. REPLACED DECAL FOR EMERGENCY LIGHT EXIT SIGN AT RT NR 2 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 EA 2008 10 8 VNAA0809007 1 20080915 A 5350 601R33038963 RADOME CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE FUSELAGE DELAMINATED A VNAA O OTHER C F.O.D. LD LANDING 1 GL 05 258PS 5109 7941 CREW REPORTED DURING LANDING A BIRD STRIKE TO THE NOSE OF THE ACFT. MX FOUND DELAMINATION ON THE RADOME. THE RADOME WA S R&R. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20081008 NM 2008 10 8 AALA200802145 1 20080820 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 368AA 25195 MIA EMERGENCY LIGHT OVERHEAD SEAT 24B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 24B. SYSTEM GROU ND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081008 NM 2008 10 8 AALA200802127 1 20080818 A 3350 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AM 24491 DFW EMERGENCY LIGHT ARROW IDENTIFIER AT LT NR 2 EXIT NOT READABLE. REPLACED PLACARD FOR EMERGENCY LIGHT ARROW IDENTIFIE R AT LT NR 2 EXIT. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 NM 2008 10 8 AALA200802125 1 20080818 A 3350 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AM 24491 DFW EMERGENCY LIGHT PLACARD AT LT FORWARD OVERWING EXIT SIGN COMING OFF. REPLACED PLACARD FOR EMERGENCY LIGHT AT LT FOR WARD OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 NM 2008 10 8 AALA200802112 1 20080815 A 3350 LIGHT BOEING 767 767323 1385205 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 347AN 33086 DFW EXTERIOR EMERGENCY LIGHT AT RT AFT TRAILING EDGE INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RT AFT TRAILING EDGE. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081008 WP 2008 10 8 08FDEA03761 1 20080908 A 5720 ARL050144 CHANNEL DOUG MD10 MD1010F 3022112 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 RIGHT WING OUTBD UPPER FUEL TANK ACCESS OPENING 634 CT HAS FUEL LINE CLAMP ATTACH BRACKET IS CRACKED XORS 538; FWD AND O UTBD OF ACCESS OPENING. REMOVED & INSTALLED THE INTERCOSTAL IN REF TO SRM 51-31-01; VOL II. FABRICATED INTERCOSTAL P/ N ARL 0501-44 IN REF TO DWG ARL 0501; REV "AY". ALODINED IN REF TO SRM 51-21-01; VOL II. PART MARKED ARL 0501-44 I N REF TO GMM 7-0-1000. 2 L 7 3 4F RT A22WE 20081008 WP 2008 10 8 08FDEA03767 1 20080908 A 5720 ARL050021 ATTACH BRACKET DOUG MD10 MD1010F 3022112 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 550FE 46521 LEFT WING FUEL TANK FWD MOST FUEL LINE CLAMP ATTACH BEACKET IS CRACKED AT XORS 683; ACCESS 536 AB. REMOVED & INSTALLE D THE INTERCOSTAL IN REF TO SRM 51-31-01; VOL II. FABRICATED INTERCOSTAL P/N ARL 0500-21IN REF TO DWG ARL 0500, REV "BU". ALODINED IN REF TO SRM 51-21-01; VOL II. PART MARKED IAW GMM 7-0-1000. 2 L 7 3 4F RT A22WE 20081008 EA 2008 10 8 TRAX200801086 1 20080904 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 980EV 7759 JOB 8775921 OPERATION 43 LT AND RT FS 621 TO 625 OBLIQUE ANGLES IN THE AFT EQUIPMENT BAY ARE CRACKED 1 IN LONG IN AFT RA DIUS. REMOVED CRACKED LT AND RT FS 621.00 TO 625.00, OBLIQUE ANGLES AND INSTALLED NEW SERVICEABLE LT AND RT OBLIQUE ANGL ES IAW CRJ 200 SRM 51-42-21. SUP CLOSED 9/11/08. (K) 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801089 1 20080903 A 5240 LATCH CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 875AS 7559 SERVICE DOOR LATCH WILL NOT RELEASE DOOR TO CLOSE. C/N/D DOOR (SERVICE) WORKS PROPERLY NOT DEFECT FOUND AT THIS TIME OK FOR SERVICE. IAW 52-45-01. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801090 1 20080903 A 5210 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA ASD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 ASD AFT SIDEWALL DRAG ANGLE CRACKED. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801092 1 20080903 A 5210 STRUCTURE CNDAIR CL600 CL6002C10 1390015 EA ASD CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 ASD FWD SIDEWALL CRACKED AT SECOND STEP RISER. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801098 1 20080903 A 5240 SERVICE DOOR CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 836AS 7263 SERVICE DOOR WILL NOT CLOSE FROM INSIDE. DOOR OPS OK PER 52-40-01. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801104 1 20080904 A 5320 ANGLE CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 FWD ANGLE OF 280 BEAM (COCKPIT FLOOR LAND) BADLY CORRODED. SUP - REMOVED FWD ANGLE OF THE 280 BEAM ( COCKPIT LAND) IAW CRJ 700 SRM 51-42-06. CB 7015474 DRILLED NEW FWD ANGLE TO NEW FS 280 BEAM IAW CRJ 700 SRM 51-42-06 AND 51-42-13. (K) 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801120 1 20080905 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 980EV 7759 JOB 8775921 OPERATION 155 FS 621 FLOOR SUPPORT ANGLE ON LT SIDE AT LBL 36 HAS A 1" CRACK. 2 L 7 2 4F RT A21EA 20081121 NM 2008 11 21 DL757081572 1 20081112 A 5320 146N54562 WEB BOEING 757 757232 1384965 NM AFT CARGO CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 CORROSION AFT CARGO BAY, FLOOR WEB CORRODED FS 1460-1480 S28R. REPLACED WEB IAW SRM 51-40-02, SRM 51-40-03, SRM 51-20- 01. 2 L 7 2 4F RT A2NM 20081121 2008 11 21 DL738081540 4 20081114 A 2210 65528202 ACCESSORY UNIT BOEING 737 737832 13844CF NM INTEGRATED FLT FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 3752 29670 F/O FLT DIR WOULD NOT DISPLAY PITCH BAR EVEN W/CA SIDE INFO CA'S OK. FOUND C/B AFCS SYS B SNSR EXC AC BREAKER POPPED. RESET C/B PERFORMED TEST PER MM ON IFSAU. ACC TEST NORMAL REPLACED INTEGRATED FLT SYS ACC UNIT SYSTEM TEST NORMAL AS PR ECAUTIONARY MEASURE REPLACED FCC PER MM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 DL757081543 1 20081011 A 5410 STRUCTURE BOEING 757 757232 1384965 NM NR 2 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 NR 2 ENG PYLON INBD LOWER CHORD STA 128 6 FASTENERS AT 5/16 STANDARD SIZE AND 1 AT 3/8 STANDARD SIZE. NOT PER DRAWING, INCOMING DEFECT. FABRICATED FREEZE PLUG REFERENCE ERA 471169-14, STEP 4. INSTALLED FREEZE PLUGS AND FASTENERS IAW ERA 471169-14 STEPS 1, 2, 3, AND 7. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 SWAA086319 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 7R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086320 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 7R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086321 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 6R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086326 1 20081118 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 08FDEA04930 1 20081119 A 5347 65C260114 SEAT TRACK BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 MAIN CABIN FLOOR, CORROSION ON SEAT TRACK FROM STA 567-639 LBL 46 REMOVED CORROSION FROM SEAT TRACK ORIGINAL MATERIAL TH ICKNESS TEE .094 AFTER BLENDING .010 MATERIAL. REMOVED REMAINING .084 AND IS OUT OF LIMITS REF SRM 53-10-1. REMOVED SE AT TRACK REF SRM 51-30-2. FABRICATED NEW TRACK REF SRM 51-10-2. INSTALLED NEW TRACK REF SRM 53-10-2. THIS IS CLASSIFIE D AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081121 NM 2008 11 21 08FDEA04931 1 20081119 A 5315 FLOORBEAM BOEING 727 7272S2F 1384O81 NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 MAIN DECK 1130 FLOORBEAM UPPER TEE CAP HAS A DOUBLE DRILLED 1/4 INCH RBL 57.5 INCH. 2 L 7 3 4F A3WE 20081121 NM 2008 11 21 DL76L081520 1 20081109 A 3030 0856LU5 PITOT HEAD BOEING 767 767332 1382001 NM LEFT WARNING LIGHT A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 181DN 25986 CAPTS PITOT HEAT LIGHT ILLUMINATED AFTER PUSHBACK. REMOVED AND REPLACED CAPTS PITOT PROBE. 2 L 7 2 4F RT A1NM 20081121 NM 2008 11 21 DL757081521 1 20081109 A 5320 146N54513 WEB BOEING 757 757232 1384965 NM BS 1533 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 CRACK ON FLOOR SUPPORT WEB AT STATON 1533 LBL 33 AFT CARGO COMPARTMENT. REPAIRED ON NR 00100 PER 53-20-04. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081522 1 20081109 A 5320 146N539110 THRESHOLD BOEING 757 757232 1384965 NM CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 AFT CARGO BAY THRESHOLD CORRODED ON UPPER SURFACE. REPAIRED ON NR 00059 PER ERA 471251-14 REV ORG. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DLM88081524 1 20081109 A 5310 BEAM DOUG MD88 MD88 3023688 NM BS 636-693 L28R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 968DL 53161 DURING HMV CORROSION WAS FOUND ON LWR BEAM AFT MID CARGO COMPARTMENT BTW STA Y=636 TO 693 AND LONGERON 28 RT. AREA WAS REPAIRED IAW SRM 53-05 FIG 123. 2 L 7 2 4F RT A6WE 20081121 NM 2008 11 21 DLM88081525 1 20081109 A 5310 BEAM DOUG MD88 MD88 3023688 NM BS 370-408 L28R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 968DL 53161 DURING HMV CORROSION WAS FOUND ON LWR BEAM AFT FWD CARGO COMPARTMENT BTW STA Y=370 TO 408 AND LONGERON 28 RT. AREA WAS REPAIRED IAW RM 53-05D FIG 804. 2 L 7 2 4F RT A6WE 20081121 NM 2008 11 21 DLM88081527 1 20081109 A 5230 FRAME DOUG MD88 MD88 3023688 NM CARGO DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 968DL 53161 DURING HMV A CRACK WAS FOUND ON AFT OTBD FRAME BTW BEAMS 3 TO 4 AT FWD CARGO DOOR C1. FRAME WAS REPAIRED IAW SRM 52-05D FIG 50. 2 L 7 2 4F RT A6WE 20081121 EA 2008 11 21 ASOA200801463 1 20081106 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 RT FUSELAGE EXTERIOR SKIN 8" FWD OF FS 559+112 AND AT STR 24R HAS MINOR SURFACE CORROSION. REMOVED RIVETS AT RT FUSELAG E EXT SKIN 8" FWD OF FS 559+112 AND AT STR 24R IAW CRJ 200 SRM 51-42-06. INSTALLED 8 NEW SERVICEABLE RIVETS IAW CRJ 200 SRM 51-42-06. UPON FURTHER INVESTIGATION FOUND 3 LOCATIONS TO BE BEYOND SERVICEABLE LIMITS. CORROSION WAS ON DOUBLER P/N 601R39000-59, REQUIRES REPAIR. BLENDED CORROSION IN 3 LOCATIONS IAW BOMBARDIER REO 601R-53-51-081 STEPS 1 & 2. THR EE EA RIVETS NEED INSTALLED. INSTALLED RIVETS REF CRJ SRM 51-42-06. PERFORMED EDDY CURRENT INSPECTION ON NEWLY BLENDED AREAS OF RT FUSELAGE SKIN. NO CRACKS FOUND AT THIS TIME. REPORT ATTACHED IAW STEP 4 OF BOMBARDIER REO 601R-53-51-081 A 2 L 7 2 4F RT A21EA 20081124 WP 2008 11 24 AALA200810170 1 20081107 A 5311 FRAME DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 587AA 53250 FRAME CRACKED AT 4 O`CLOCK POSITION STATION 1510, AT TAIL CONE ALIGNMENT PIN. INSTALLED DOUBLER PER ESO 80559 DATED 11/ 07/08. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA2008132 1 20081027 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP BS 1168 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 LEFT CUSP CORRODED AROUND AREA UNDER GIRT BAR AT STATION 1168. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 UALA2008111306177 1 20081017 A 5210 LOCK NUT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR MISALIGNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 DOOR 2L EMERGENCY POWER ASSIST PRESSURE RESERVOIR RED BAND ON EMERGENCY POWER SPRING CYLINDER ALIGNED IMPROPERLY. ADJUS TED CABLE TERMINAL LOCK NUT TO ACHIEVE DIMENSION. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 NM 2008 11 24 UALA2008111306300 1 20081028 A 3397 794640 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 653UA 25391 MID CABIN EEL CROSS-AISLE LIGHT IS INOP. SECURED RIBBON CONNECTOR. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 NM 2008 11 24 UALA2008111706519 1 20081114 A 3350 767 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 772UA 26930 EXTERIOR EMERGENCY LIGHTS ON DOORS 3 AND 4 LT INOP. RELAMPED EMERGENCY LIGHTS ON DOORS 3 AND 4 LEFT, OPS CHECK OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081124 WP 2008 11 24 AALA200810169 1 20081110 A 5311 FRAME DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 587AA 53250 CRACK IN RADIUS ON FRONT SIDE OF FRAME 1418 AT LONGERON 2R. REPAIRED 1418 2R FRAME CRACK PER ESO 80559 DATED 11/10/08. 2 L 7 2 4F A6WE 20081124 SO 2008 11 24 C2XA08RI154 1 20081010 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO RUDDER SYSTEM DEFECTIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 29917 14927 145414 FLIGHT 2316 EWR FLIGHT CREW REPORTED RUDDER SYSTEM 1/2 INOP MSG ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNE VENTFUL. EWR MX R&R LT AND RT RUDDER PRESSURE SWITCH AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETUR N TO SERVICE. 2 L 7 2 4T RT T00011AT 20081124 SO 2008 11 24 C2XA08RI156 1 20081012 A 3260 0132AFU SENSOR EMB 145 EMB145LR 3260212 SO NR 2 BRAKE DEFECTIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 19961 24187 145153 FLIGHT 3009 EWR FLIGHT CREW REPORTED NR 2 BRAKE TEMPERATURE INDICATION WENT INTO THE AMBER ON TAKEOFF. FLIGHT CREW PERF ORMED AIR RETURN AND LANDED ACFT UNEVENTFULLY. EWR MX R&R NR 2 BRAKE SENSOR AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081124 SO 2008 11 24 C2XA08RI155 1 20081010 A 2720 15793101 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO RUDDER SYSTEM DEFECTIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 29917 14927 145414 FLIGHT 2316 EWR FLIGHT CREW REPORTED RUDDER SYSTEM 1/2 INOP MSG ON EICAS. CREW PERFORMED AIR RETURN AND LANDED ACFT UNE VENTFUL. EWR MX R&R RT RUDDER PRESSURE SWITCH AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SE RVICE. 2 L 7 2 4T RT T00011AT 20081124 EU 2008 11 24 UALA2008111806544 1 20081117 A 2120 FILTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E&E BAY DIRTY A UALA A UNSCHED LANDING W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 423UA 504 ELECTRICAL BURNING ODOR IN COCKPIT. RTFL. AFTER CONFER WITH CAPT, REMOVED CAPTS SIDE PFD & ND, CHECKED AREA FOR ELECT BURN ODOR & DAMAGE, NONE FOUND, EQUIPT COOLING NORMAL. REPLACED AND TESTED CRTS, CKS GOOD. FOUND AVIONICS COOLING FILT ER HEAVILY SOILED. REPLACE AVIONICS COOL INLET FILTER. AEVC CFDS TESTS CKS PASSED. PRECAUTIONARY REPLACED BOTH THE LT & RT RECIRC FILTERS. CHECKED RECIRC SYSTEM, BOTH FANS OPERATE & NO ODORS PRESENT. ACP'D CABIN PRESS TO 5.3 DP FOR 57 MIN DURATION PRECAUTIONARY, NO ABNORMALITIES NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081124 NM 2008 11 24 UALA2008111806552 1 20081117 A 2761 332150012 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 8 SPOILER UNKNOWN A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 543UA 25698 SCM 2L INDICATES PCA 8 FAULT. INSTALLED -200 SERIES SCM AT 2L. CLEANED CONNECTORS (D655 SPL 8 M313) AND (D649 SPL 5 M3 10). RANG WIRES FROM SCM 2L TO NR 5 & 8 PCA. RESISTANCE WITHIN LIMITS. SLUGGED GEARS TO PUT IN AIR MODE. ACP'D SYS T EST ON SCM 2L IN AIR AND GND MODE, SYS TEST GOOD. NO EXISTING FAULTS FOUND, NO FAULT BALLS SHOWING ON REMAINING -100 SE RIES SCM'S. RERACKED SCM 2L. INTERROGATED SCM 2L HISTORY AND FOUND ONLY PCA 5 FAULT WHICH WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 2008 11 24 UALA2008111806553 4 20081114 A 2565 5A29011 ASPIRATOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EVAC SLIDE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 675UA PF0090 29243 ASPIRATOR LEAKING FROM BARREL. REPLACED ASPIRATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 NM 2008 11 24 UALA2008111806558 1 20081118 A 3350 FU305 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BATTERY PACK BLOWN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 DOOR 3R OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK FUSE, OP CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111806559 1 20081118 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT LIGHT INOP SEAT ROW 10 RIGHT FWD LIGHT ASSY. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111806563 1 20081118 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT EEL LIGHT INOP DOOR 2 LEFT AFT EXIT SIGN. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111806564 1 20081118 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT LIGHT INOP DOOR 2 LEFT CEILING ENTRY LIGHT. REPLACED LAMP. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111806565 1 20081118 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT EEL LIGHT INOP SEAT ROW 39 LEFT. REPLACED LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 EU 2008 11 24 UALA2008111306191 1 20081020 A 3397 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 471UA 1432 EEL LIGHTS AT ROWS 8 AND 9 SEATS ABC ARE INOP. RELAMPED EMERGENCY LIGHTS, NO HELP. FOUND CONNECTOR AT BOTTOM OF SEAT L OOSE. CLEANED CONNECTOR AND SECURED. EEL LIGHT WORK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081124 NE 2008 11 24 UALA2008111306295 2 20081028 A 7261 SEAL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE DEFECTIVE A UALA O OTHER A FLAME/FIRE IN INSP/MAINT 1 WP 29 449UA 851 V10470 NR 1 ENGINE REPORTED FIRE IN TAIL PIPE AFTER SHUTDOWN. SUSPECT OIL LEAK AS SOURCE OF IGNITION. REPLACED NR 1 ENGINE. REPLACED SEAL NR 5 BEARING/ASSY. REPLACED NR 5 BEARING COMPARTMENT PULLER/COVER. 2 L 7 2 4F 4 F RT A28NM E40NE 20081124 NM 2008 11 24 UALA2008112006573 1 20081120 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 779UA 26941 EMERGENCY LIGHTS INOP AT SEATS 22C AND 39C. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081124 CE 2008 11 24 DXTA2008111403354 1 20081113 A 3260 WARNING SYSTEM RAYTHN 900 HAWKER900XP 4220011 CE COCKPIT ACTIVATED E DXTA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 07 848QS HA0031 ON TAKEOFF THE LEFT GEAR DID NOT COME UP + LOCKED, ONLY THE RED UNSAFE LIGHT WAS ON. 1 L 7 2 4F RT A3EU 20081124 SO 2008 11 24 C2XA08IA225 1 20081013 A 3350 2013BR BATTERY EMB 145 EMB145EP 3260221 SO EMERGENCY LIGHTS DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 16944 7285 145045 IAH DURING A CHECK INSPECTION THE AFT 3 AISLE PATH LIGHTS WERE FOUND TO BE INOPERATIVE. MX R&R THE NR 4 EMERGENCY LIGHT BATTERY. OPS CHECKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT T00011AT 20081124 SO 2008 11 24 C2XA08CL112 1 20081013 A 3350 110049 POWER SUPPLY EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26545 145558 DURING ROUTINE MX THE OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE ON BOTH SIDES. MX INSPECTED AND REPLACED THE NR 4 BATTERY POWER SUPPLY. OPS CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20081124 SO 2008 11 24 C2XA08IA222 1 20081003 A 3610 40303925 O-RING EMB 145 EMB145XR 3260214 SO NR 2 BLEED WORN A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 34110 145658 IAH FLIGHT 2160 THE CREW REPORTED A BLEED 2 LEAK MSG DURING CRUISE. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT IN CIDENT. MX R&R BLEED O-RINGS UNDER THE CARGO COMPARTMENT FLOOR. OPS AND LEAK CHECKED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081124 CE 2008 11 24 DXTA2008111703357 1 20081114 A 2931 WARNING SYSTEM CESSNA 560 560XL 2076702 CE COCKPIT ACTIVATED E DXTA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 07 630QS 5605130 GEAR UNLOCK HYD PRESS REMAINED ILLUMINATED AFTER GEAR AND FLAP RETRACTION. 2 L 7 2 4F RT A22CE 20081124 CE 2008 11 24 DXTA2008111703360 1 20081116 A 2120 UNKNOWN CESSNA 750 750 2076810 CE COCKPIT ODOR E DXTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 903QS 7500162 AT FL 450, LEVEL FLIGHT, HAD STRONG ODOR IN COCKPIT (SMELLED LIKE BURNED PLASTIC ). 2 L 7 2 4J RT T00007WI 20081124 CE 2008 11 24 DXTA2008111003341 1 20081107 A 5270 WARNING SYSTEM CESSNA 560 560XL 2076702 CE COCKPIT ACTIVATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 660QS 5605647 TAIL ACCESSORY DOOR OPEN PANEL LIGHT CAME ON DURING TAKEOFF. 2 L 7 2 4F RT A22CE 20081124 CE 2008 11 24 DXTA2008111803362 1 20081117 A 3260 WARNING SYSTEM CESSNA 500 560CESSNA 2076750 CE COCKPIT ACTIVATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 367QS 5600367 AT GEAR RETRACTION THE THREE GREEN LIGHTS EXTINGUISHED, BUT THE RED GEAR UNLOCKED LIGHT REMAINED ON. 2 L 7 2 4F RT A22CE 20081124 CE 2008 11 24 DXTA2008111003344 1 20081107 A 3240 BRAKE SYS CESSNA 500 560CESSNA 2076750 CE FAILED E DXTA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 810QS 5600625 LO BRAKE PRESSURE/ANTISKID ANNUNCIATOR ILLUMINATED FOLLOWED BY A COMPLETE BRAKE FAILURE. 2 L 7 2 4F RT A22CE 20081124 CE 2008 11 24 DXTA2008111003346 1 20081109 A 2930 WARNING SYSTEM CESSNA 560 560XL 2076702 CE HYDRAULIC SYS ACTIVATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 698QS 5605653 LOW HYD FLOW RT ANNUNCIATOR ILLUMINATED WHEN POWER APPLIED FOR T/O. T/O ABORTED. 2 L 7 2 4F RT A22CE 20081124 CE 2008 11 24 DXTA2008111003347 1 20081109 A 2700 UNKNOWN CESSNA 750 750 2076810 CE OUT OF TRIM E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 999QS 7500203 AFTER LEVELING OFF AT 10,000FT, AIRCRAFT WAS SEVERLY OUT OF TRIM. 2 L 7 2 4J RT T00007WI 20081124 CE 2008 11 24 DXTA2008111903364 1 20081119 A 3260 LIGHT CESSNA 500 560CESSNA 2076750 CE COCKPIT MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 344QS 5600344 LT GEAR INDICATION LIGHT FAILED TO ILLUMINATE AFTER GEAR EXTENSION. 2 L 7 2 4F RT A22CE 20081124 CE 2008 11 24 DXTA2008111003348 1 20081109 A 3230 LANDING GEAR CESSNA 560 560XL 2076702 CE LT MLG STUCK E DXTA O OTHER O OTHER AP APPROACH 1 GL 07 601QS 5605301 MAIN LEFT LANDING GEAR BECAME STUCK IN THE UP LOCK POSITION WHEN SELECTED GEAR DOWN. 2 L 7 2 4F RT A22CE 20081124 NM 2008 11 24 DXTA2008110503337 1 20081104 A 2120 UNKNOWN AMD FALC50 FALCON2000 2730170 NM ODOR E DXTA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 07 298QS 98 STRONG SMELL OF AN ELECTRICAL TYPE BURNING ODOR AFTER TAKEOFF AND AGAIN AFTER LANDING. 2 L 7 2 4F RT A50NM 20081124 NM 2008 11 24 IU6R240813 1 20081105 A 3240 511531 HOUSING BOEING 737 737* NM CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 PART WAS FOUND CRACKED DURING BENCH MAINTENANCE. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 IU6R240784 1 20081105 A 3240 511531 HOUSING BOEING 737 737* NM CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 PART WAS FOUND CRACKED DURING BENCH MAINTENANCE. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 KNNA200800098 1 20081119 A 5340 STRINGER CLIP BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 465AT 21528 STRINGER CLIP CRACKED AT STA 685, STRINGER 3R. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 KNNA200800100 1 20081119 A 5340 STRINGER CLIP BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 465AT 21528 STRINGER CLIP WAS CRACKED AT STA 616, STRINGER 3R. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 KNNA200800095 1 20081119 A 5340 STRINGER CLIP BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 465AT 21528 STRINGER CLIP WAS CRACKED AT STA 727B, STR 3L. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 KNNA200800101 1 20081119 A 5340 STRINGER CLIP BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 KNNA 21528 FOUND STRINGER CLIP CRACKED AT STA 616, STRINGER 3R. 2 L 7 2 4F RT A16WE 20081124 WP 2008 11 24 AALA200810171 1 20081107 A 5755 CASTING DOUG DC9 DC982 3022082 WP GROUND SPOILER CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 587AA 53250 GROUND SPOILER ACTUATOR MOUNT CASTING IS CRACKED AT FORWARD INBOARD END. REMOVED AND REPLACED CASTING. 2 L 7 2 4F A6WE 20081124 2008 11 24 UALA2008111706522 4 20081114 A 2350 MICROPHONE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE OXYGEN MASK FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 466UA 1343 CAPT OXYGEN MASK MIKE IS WEAK, UNREADABLE ACCORDING TO ATC. REPLACED O2 MASK. 2 L 7 2 4F 4 F RT A28NM E40NE 20081124 WP 2008 11 24 AALA200810149 1 20081101 A 5210 BRACKET DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 449AA 49475 BRACKET CRACKED BY INSIDE DOOR HANDLE IN CORNER OF FWD PASSENGER DOOR. INSTALLED ANGLE DOUBLER PER SRM 52-05-00. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 AALA200820016 1 20081013 A 5320 2024T3 FLOOR SUPPORT BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 672AA 52528 25337 FLOOR SUPPORT CORRODED FOR G1B GALLEY. REPLACED SUPPORT IAW SRM 53-00-00-0G. 2 L 7 2 4F RT A2NM 20081124 EA 2008 11 24 SWIA200820370 1 20080715 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 368CA 10075 C-CHECK, PASSENGER DOOR FORWARD WEB CRACKED AT ZONE 2. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 SWIA200820372 1 20080715 A 3210 BOLT CNDAIR CL600 CL6002C10 1390015 EA LT MLG CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 368CA 10075 C-CHECK, LEFT AND RIGHT MAIN LANDING GEAR OUTBOARD PINTLE PIN SLEEVE BOLTS CORRODED, REPLACED. 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 SWIA200820373 1 20080723 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 767SK 10233 C-CHECK, FS 280 CROSSBEAM CRACKED, REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 SWIA200820374 1 20080725 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 776SK 10241 C-CHECK, FS 280 CROSSBEAM CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081124 NM 2008 11 24 DHLA2008745685 1 20081113 A 5330 SKIN BOEING 727 727224 1384076 NM ZONE 200 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 FUSELAGE SKIN LAP SEAM AT STR 4L HAD CRACK INDICATIONS AT LOWER FASTENER ROW FROM AT BS 391.5, 395, 409, 410, 415.5, 442 .5, AND 450, CRACK INDICATIONS DOCUMENTED ON COOPESA N/R'S 2-184, 2-185, AND 2-186. COMPLETE REPAIR DOCUMENTED ON 2-186 ONLY. ACCOMPLISHED SKIN REPAIR FROM BS 360 TO BS 460, STR 3L TO 5L, PER SB 727-53A0222 REV 1 DATED 3/15/2001, SECT 3, PART II, AND BAC DWG 65C38441 REV A DATED 2/7/2000. REPAIRED SECT 43 AT LAP SEAM AND MCD DOUBLER MODIFICATION INTERSECT ION, BS 460 AND STR 4L, PER EO COO-2-53-275-08 DATED 9/17/2008. REF FAA FORM 8110-3 DATED 10/15/2008, SIE-ICAW-318-32-2 0665 REV IR DATED 10/15/08, AND EVA B253-00112 FOR REPAIR APPROVAL. 2 L 7 3 4F A3WE 20081124 NM 2008 11 24 DL76L081529 1 20081110 A 2910 ACTUATOR BOEING 767 767332 1382001 NM HYD SYSTEM LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 184DN 27111 CENTER HYDRAULIC SYSTEM WAS LOSING FLUID, ATB TO SVO. FOUND LCCA LEAKING. 2 L 7 2 4F RT A1NM 20081124 NM 2008 11 24 DL757081531 1 20081111 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 1516 RBL 12 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 AFT CARGO BAY FLOORBEAM 1516 AT RBL 12 CORRODED. REPAIRED PER 51-40-02 ON NR 00044. 2 L 7 2 4F RT A2NM 20081124 NM 2008 11 24 DL757081532 1 20081111 A 5321 146N539151 FLOOR PANEL BOEING 757 757232 1384965 NM BS 1470-1510 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 AFT CARGO BAY FIXED FLOOR PANEL CORRODED AT STATION 1470 TO 1510 RBL 17. REPAIRED PER 51-40-02 ON NR 00086. 2 L 7 2 4F RT A2NM 20081124 NM 2008 11 24 UALA2008111706531 1 20081115 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT EEL LIGHT INOP ACROSS LAV 104 LOWER WALL EEL. REPLACED WALL EEL LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111306202 1 20081021 A 3350 WIRE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 818UA 882 CABIN EMERGENCY LIGHTS AT SEAT 10 ABC NOT ILLUMINATING. REPAIRED WIRE, TESTS OKAY. 2 L 7 2 4F 4 F RT A28NM E40NE 20081124 NM 2008 11 24 KNNA2000800093 1 20081119 A 5330 DOUBLER BOEING 737 7372L9 1384497 NM FUSELAGE DELAMINATED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 465AT 21528 FOUND BONDED DOUBLER WITH DELAM BETWEEN STA 727-727A AND STR 15R TO 17R. DELAM WAS REPAIRED IAW SRM 53-30-3 FIG 17. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 KNNA20080092 1 20081110 A 5311 654654020 FRAME BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 465AT 52209 21528 DURING C-CHECK FOUND FRAME CRACKED AT STA 639 BETWEEN STR 14R AND 15R. REPAIRED FRAME IAW SKY KING ACO-085357. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 KNNA200800103 1 20081119 A 5340 STRINGER CLIP BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 465AT 21528 FOUND STRINGER CLIP CRACKED AT STA 616, STRINGER 0. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 KNNA200800106 1 20081119 A 5340 STRINGER CLIP BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 465AT 21528 FOUND STRINGER CLIP CRACKED AT STA 787, STRINGER 4R. 2 L 7 2 4F RT A16WE 20081124 2008 11 24 UALA2008112006584 4 20081119 A 2397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN EXPOSED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 534UA 25129 CREW REPORT: EXPOSED WIRE AT SEAT 5A THIS IS A LIVE ELECTRICAL WIRE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 NM 2008 11 24 UALA2008112006585 1 20081118 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT PIT FRAME DENTED STA 1520, RBL 8 TO RBL 9. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALL ED J-ANGLE DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 NM 2008 11 24 UALA2008112006586 1 20081118 A 2997 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 WIRE BUNDLES AND COAX HAVE CHAFING, 1 EA BROKEN WIRE, NOT SECURED UNDER MAIN CABIN FLOOR STA 996 TO 1180, LBL 48. SECUR ED WIRE BUNDLES AND COAX UNDER MAIN CABIN FLOOR AT BS 996-1180, LBL 48 PER BSWPM 20-10-42. OPS CHECK OF HYDRAULIC RESER VOIR TEMP GOOD AND OPS CHECK OF SPOILER CONTROL MODULE 3R WIRING GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 NM 2008 11 24 UALA2008112006587 1 20081118 A 2611 SMOKE DETECTOR BOEING 767 767222 1385122 NM PWA 2037 PW2037 NE LAVATORY FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 LAV K SMOKE DETECTOR WILL NOT RESET. 2 L 7 2 4F 4 F RT A1NM E17NE 20081124 2008 11 24 UALA2008112006574 4 20081029 A 2210 AUTOLAND SYS BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE COCKPIT MALFUNCTIONED A UALA K NONE O OTHER AP APPROACH 1 WP 29 218UA 30222 NO LAND 3 DEGRADATION IN AUTO LAND SYSTEM PRIOR TO APPROACH (BEFORE LAND 3 AUTO LAND STATUS ANNUNCIATION). AUTO LAND SYS TEM IS NO LONGER FAIL-OPERATIONAL. ADVISORY MSG01- ACTIVE CRUISE MODE DEPENDENT; BUS ISOLATION IS NOT AVAILABLE. DB- AUTOPILOT FLIGHT DIRECTOR COMPUTER (RIGHT) MSG02- ACTIVE CRUISE HARD; POWER BUS (L AC FRO BUS) IN P100 IS NOT POWERED. DB- ELMS P110 ELECTRONICS UNIT MSG03- NOT ACTIVE CRUISE INTERMITTENT; TRANSFORMER-RECTIFIER UNIT (TRUE L) IS INOPERATIVE . DB- ELMS P310 ELECTRONICS UNIT MSG04- ACTIVE CRUISE INTERMITTENT; MULTI-MODE RECEIVER (LEFT) HAS NO OUTPUT ON ANY BUS . MSG-2213620 ACTIVE ERR MODE MSG-2411101 ACTIVE ERR HARD MSG-2413051 INACTIVE ERR INTER MSG-3453801 ACTIVE ERR INTE 2 L 7 2 4F 4 F RT T0001SE E46NE 20081124 NM 2008 11 24 UALA2008112006575 1 20081119 A 3350 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 795UA 26927 SEAT 2E REAR EEL LIGHT STRIP INOP. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081202 NM 2008 12 2 UALA2008112406615 1 20081119 A 2432 263BA1011 BATTERY BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE MAIN FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 787UA 26939 STATUS MSG BATTERY CHARGER MAIN. REPLACED MAIN BATTERY CHARGER AND BATTERY, NO HELP. SWAPPED APU BATTERY WITH MAIN BAT TERY AND CHECKS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081202 EU 2008 12 2 UALA2008112406617 1 20081121 A 5330 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 448UA 842 MAJOR REPAIR. REPLACE BELLY SKIN FR 64-70 STR 40R-31L ACCT TAIL STRIKE ON LANDING. MAJOR REPAIR ACCOMPLISHED. REMOVED AFT POTABLE WATER SERVICE PANEL. REMOVED & REPLACED DAMAGED SKIN WITH HEAT TREATED FASTENERS WHERE REQUIRED. 11/24/20 08 REINSTALLED POTABLE WATER SERVICE PANEL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081124 NM 2008 11 24 UALA2008112006600 1 20081118 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INTERMITTENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY FLOOR LIGHTING INBOARD SIDE AISLE BUSINESS LEFT SIDE INTERMITTENT. EMERGENCY LIGHT OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008112006601 1 20081118 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY LIGHTS AT DOOR 2L INOP. DOOR 2L EMERGENCY LIGHT, OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008112006602 1 20081120 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INTERMITTENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 EXIT PATH LIGHT OPPOSITE LAV 100 FLICKERING. PATH LIGHT ON-OFF CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081202 NM 2008 12 2 UALA2008111306368 1 20081103 A 3350 10295 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAULTY A UALA D RETURN TO BLOCK W L INADEQUATE Q C NO TEST TX TAXI/GRND HDL 1 WP 29 569UA 26677 AFTER ENG START AND TAXI FOLLOWING EMERGENCY EXIT LIGHTS CAME ON WITH SW ARMED: EEL ROW 16-24, RANDOM STOW BIN LIGHTS F ROM ROW 16-33, & DOOR 3L&R SIGNS. NOTHING FWD OF OVERWING EXITS TO COCKPIT CAME ON. FOUND ABOVE LIGHTS WERE PART OF AF T EMER TEST LIGHT SW CIRCUIT. REPLACED DOOR 3L EMER LIGHT TEST SWS 10295, ALL EMER LIGHTS TEST OK. RAN ENGS AND ACCOMP LISHED TAXI TEST, UNABLE TO DUPLICATE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081202 NM 2008 12 2 UALA2008112406622 1 20081122 A 5220 BACC2A4D00134JJ CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY EXIT KINKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 LT AFT EMERG EXIT HATCH STEP FWD AND AFT CABLES ARE KINKED. REPLACED CABLES. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 NM 2008 11 24 UALA2008112006594 1 20081101 A 5754 PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LE SLAT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 512UA 24809 NR 1 AND NR 2 LEADING EDGE SLAT AND UNDER WING PANEL 521MB DAMAGE BY AIRSTAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 2008 11 24 UALA2008112006595 4 20081026 A 2565 SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 AFTER RT OVERWING SLIDE DEPLOYMENT, FOUND FWD RT OVERWING EXIT DOOR AUTO ARM AND AUTO FIRE SWITCHES NOT IN THE FULLY DOW N POSITION. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 EA 2008 11 24 REX2008F00052 1 20081007 A 4920 38004883 APU CNDAIR CL600 CL6002B19 1900309 EA APU BAY FAILED A REXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 21 8877A 9254 310 7877 ON TAXI OUT, APU FAILED WHICH RESULTED IN SMOKE IN THE CABIN. FLIGHT CREW DECLARED AN EMERGENCY AND CALLED. NO EVIDENC E OF FIRE WAS FOUND AND THE SMOKE CLEARED. CFR CLEARED AIRCRAFT TO TAXI BACK TO THE GATE. MAINT DEFERRED THE APU AND T HE AIRCRAFT WAS RELEASED FOR SERVICE. (K) 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 REX2008F00054 1 20080912 A 2697 601R575261 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA OVERHEAT SYS FAULTY A REXA O OTHER N FALSE WARNING AP APPROACH 1 CE 21 8506C 7506 ON APPROACH, RECEIVED GEAR OVERHEAT WARNING WHEN GEAR EXTENDED, QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED L T AND RT MLG BAY DETECTION LOOP HARNESS IAW AMM. (K) 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 REX2008F00053 1 20080912 A 2697 601R575251 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA OVERHEAT SYS FAULTY A REXA O OTHER N FALSE WARNING AP APPROACH 1 CE 21 8506C ON APPROACH, RECEIVED GEAR OVERHEAT WARNING WHEN GEAR EXTENDED. QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED LT AND RT MLG BAY DETECTION LOOP HARNESS IAW AMM. (K) 2 L 7 2 4F RT A21EA 20081124 WP 2008 11 24 MWEA080132 1 20081116 A 2422 GO000222 INVERTER DOUG DC9 DC981 3022081 WP ELECTRICAL SYS FAULTY A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 804ME 48030 BAS A/C EMERGENCY BUS COMES ON WHEN EMERGENCY POWER IS SELECTED ON. REPLACED EMERGENCY INVERTER. (K) 2 L 7 2 4F A6WE 20081124 EA 2008 11 24 MAS2008F00106 1 20081005 A 3230 4622 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 27191 7191 CREW REPORTED A GEAR DISAGREE CAUTION MESSAGE. MX REMOVED AND REPLACED NLG PRIORITY VALVE. (K) 2 L 7 2 4F RT A21EA 20081124 NM 2008 11 24 MAS2008F00107 1 20081001 A 3350 1317 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA O OTHER O OTHER NR NOT REPORTED 1 SW 07 991HA 431 FWD AND AFT EMERGENCY FLOOD LIGHTS IN CEILING INOPERATIVE. MX RELAMPED. OPS CHECKED GOOD. (K) 2 H 7 2 4T RT A13NM 20081124 NM 2008 11 24 SWAA086369 1 20081119 A 5240 6545871 DOOR FRAME BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND R1 DOOR FRAME CRACKED AT BS AFT BOTTOM STOP PIN FITTING. REPAIRED FRAME ASSY PER SRM. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 SWAA086345 1 20081118 A 5322 6546569 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BETWEEN STR 27R TO STR 25R. REMOVED AND REPLACED SHEAR TIE PER AAR EA. 2 L 7 2 4F RT A16WE 20081007 NM 2008 10 7 KCSA081429 1 20080827 A 5311 FRAME BOEING 747 747249F 1384849 NM FUSELAGE GOUGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 FRAME WEB GOUGED AT STA-220 BL-O AT WL-177. 2 L 7 4 4F RT A20WE 20081007 EU 2008 10 7 SIMA200824604 1 20080830 A 7712 UNKNOWN SAAB SF340 340B 7860101 EU UNKNOWN A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 902AE 340B269 ON FLIGHT 3248 CREW REPORTED ON ABORTED TAKE OFF DUE TO NO TORQUE INDICATING ON NR 2 ENGINE, NO BOTTOM GOVERNING AND PRO P RPM WILL NOT COME ABOVE 1000 RPM. ACFT REMOVED FROM SERVICE. PERFORMED GROUND RUN IAW SAAB AND GE MM NO FAULTS FOUND ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 20081007 NM 2008 10 7 EIA2008F00004 1 20080822 A 5313 STRINGER BOEING 747 747409 13848AU NM BS 480-499 S10L CRACKED A EIAA O OTHER O OTHER NR NOT REPORTED 1 NM 19 780BA 24310 BS 480-499 STRINGER 10 LT STRINGER IS CRACKED. REPAIRED CRACKED STRINGER AT BS 480 & 500 IAW SB747-53A2484, FIG 18 AND 2 0. (K) 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 EIA2008F00006 1 20080822 A 5330 SKIN BOEING 747 747409 13848AU NM BS 2640 DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 780BA 24310 FUSELAGE SKIN BS 2640 LBL 16, DENT OUT OF LIMITS. REMOVED DAMAGED AREA, NDT AREA, FABRICATED AND INSTALLED REPAIR DOUBLE R AND FILLER IAW SRM 400 LCF 53-30-01 PG 3 ITEM 7, 53-00-01 REPAIR 6PG 201-204 51-30-50, PG 5, 51-10-02 PG 6-7. (K) 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 EIA2008F00007 1 20080818 A 5330 SKIN BOEING 747 747409 13848AU NM BS 220-260 DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 780BA 24310 (2) DENTS IN FUSELAGE SKIN BS 220-260, STRINGER 30 RT-32 RT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AN D FILLER IAW SRM 53-00-01 PG 201-211, REPAIR 1 DETAIL, FIG 201. (K) 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081478 1 20080907 A 5343 DRAG ANGLE BOEING 747 747249F 1384849 NM LT MLG TRUNNION CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 LT BODY GEAR TRUNNION SUPPORT, DRAG ANGLE CORRODED AT BS 1482, STR-42R. (K) 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081480 1 20080907 A 5315 FLOORBEAM BOEING 747 747122 1384872 NM BS 1720 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STA 1720 BB L 0.00, FLOORBEAM UPPER "T" CHORD DENTED. (K) 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081481 1 20080907 A 5340 STRINGER CLIP BOEING 747 747122 1384872 NM BS 2020 S48R DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STRINGER CLIP DAMAGED AT STR 48R STA 2020. (K) 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081443 1 20080904 A 5322 SHEAR TIE BOEING 747 747122 1384872 NM BS 1640 S36 DENTED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 STA-1640 ABOVE STR-36, FRAME TENSION TIE DENTED. (K) 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081445 1 20080904 A 5320 WEB BOEING 747 747249F 1384849 NM BS 264 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 STA-264, UPPER DECK FLOOR WEB CRACKED 1 INCH WL-306. (K) 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081448 1 20080907 A 5343 DRAG ANGLE BOEING 747 747249F 1384849 NM LT MLG TRUNNION CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 706CK 21827 LT BODY GEAR TRUNNION SUPPORT, DRAG ANGLE CORRODED AT BS 1482, STR-42. (K) 2 L 7 4 4F RT A20WE 20081007 NM 2008 10 7 KCSA081452 1 20080907 A 5512 SPLICE PLATE BOEING 747 747122 1384872 NM HORIZONTAL STAB CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 HORZ STAB CENTER SECTION LT SIDE SPLICE PLATE CRACKED IN AFT FASTENER HOLE OF THE 2ND ROW IB OF LBL-43.5. COMMON TO THE UPPER REAR SPAR CHORD. (K) 2 L 7 4 4F RT A20WE 20081007 EA 2008 10 7 TRAX200801085 1 20080825 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 932EV 8016 JOB 8801621 OPERATION 159 RT INBD AND OTBD 280 CLIPS ARE CRACKED AT RBL 9. W/O 98367 TASKCARD NR 00190. REMOVED CRACKE D ANGLES INBD AND OTBD. INSTALLED NEW ANGLES P/N 601R3113-58 IAW CRJ 200 SRM 51-42-06/-21. 2 L 7 2 4F RT A21EA 20081007 SO 2008 10 7 CHQA200800172 1 20080901 A 3222 1170C000003 STRUT EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL NLG UNDERSERVICED A CHQA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 11 279SK 20148 145379 CAE311424 FLIGHT 3080, SDF TO LGA. WHEN THE CREW SELECTED THE LANDING GEAR DOWN THEY HEARD A THUD FROM THE NOSE AREA AND RECEIVED LG AIR/GND FAIL AND T/R DISAGREE MESSAGES ON EICAS. UPON LANDING THEY RECEIVED A STEERING INOP MESSAGE ON EICAS. AFT ER STOPPING THE ACFT ON THE RUNWAY THE TILLER WAS ENGAGED SUCCESSFULLY AND THE STEERING MESSAGE CLEARED. MX INSPECTED T HE NOSE LANDING GEAR AND FOUND THE STRUT WAS LOW AND ALSO INSPECTED THE LANDING GEAR PROXIMITY SWITCHES ON THE NOSE AND MAIN LANDING GEAR WITH NO DEFECTS NOTED. THE 7 DEGREE SWITCH WAS CLEANED AND THE NOSE STRUT WAS SERVICED AND THE STEERI NG AND PROXIMITY SYSTEMS OPS CHECKED GOOD. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081007 NM 2008 10 7 AALA200802083 1 20080812 A 3350 LENS DOUG MD80 MD83 3023681 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 951TW 53470 LGA EMERGENCY LIGHT AT SEAT 5E MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NORMA L OPS. 2 L 7 2 4F RT 20081007 NM 2008 10 7 AALA200802082 1 20080812 A 3350 LIGHT DOUG MD80 MD83 3023681 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 951TW 53470 LGA EMERGENCY LIGHT AT SEAT 5E MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NORMA L OPS. 2 L 7 2 4F RT 20081124 NM 2008 11 24 SWAA086441 1 20081120 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 706, STR 8L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 SWAA086368 1 20081119 A 5322 6546563 SHEAR TIE BOEING 737 7373Q8 1384670 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 685SW 23401 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 967, BETWEEN STR 27R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 AALA200820017 1 20081013 A 5320 141N516279 FLOOR SUPPORT BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 672AA 52528 25337 FLOOR SUPPORT CORRODED FOR G1B GALLEY. REPLACED SUPPORT IAW SRM 51-00-51-0G. 2 L 7 2 4F RT A2NM 20081124 WP 2008 11 24 AALA200810097 1 20081015 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 FLOOR BOARD SUPPORT CRACKED AT LOWER FWD SIDE BELOW SEAT TRACK NR 5. INSTALLED NEW SUPPORT. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 SWAA086371 1 20081119 A 5322 6546546 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727B, BETWEEN STR 25L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086372 1 20081119 A 5322 6546546 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 867B, BETWEEN RBL 1 TO RBL 4. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 HALA2008111700864 1 20081117 A 5730 SKIN BOEING 767 76733A 1385209 NM RT WING DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 582HA 28139 FRETTING DAMAGE ON RT WING AT RBBL 97.42 LOWER SPLICE PLATE. FRETTING DAMAGE BLENDED IAW 767 SRM 57-20-90/1AO1, THEN RO TO-PEEING 767 CM 20-10-03. SURFACE ALODINED AND PRIMED, SEALENT RE-APPLIED TO EDGES. 2 L 7 2 4F RT A1NM 20081125 WP 2008 11 25 AALA200810025 1 20081015 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 CUSP ANGLE CORRODED STATION 160 RIGHT. REPLACED CUSP ANGLE FROM STATION 144 TO 227 PER SRM 53-05-00 AND ESO 80559 DATED 10/13/08. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810089 1 20081017 A 5313 LONGERON DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 AFT CARGO, CORROSION ON LONGERON 23L AT STATION 1287. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 51-10-1. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 SWAA086374 1 20081119 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 4R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 EA 2008 11 25 SWIA200820423 1 20080818 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 441SW 7602 C-CHECK, FS 280 FLOOR SUPPORT BEAM LBL 9 INBOARD CLIP CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081125 EA 2008 11 25 SWIA200820425 1 20080818 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 441SW 7602 C-CHECK, LEFT ENGINE THRUST FITTING BEARING AND BALL WORN AND CORRODED, REPLACED. 2 L 7 2 4F RT A21EA 20081124 EU 2008 11 24 AALA200820014 1 20081016 A 3350 BR964814 LIGHT AIRBUS 300 A300B4605R 3930308 EU SEAT 17G BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 40064 52743 0507 EMERGENCY PATH LIGHT ASSY IS BROKEN AT ROW 17 SEAT G. REPLACED LIGHT FIXTURE ASSY IAW ESPM 20-52-10. 2 L 7 2 4F RT A35EU 20081124 WP 2008 11 24 AALA200810168 1 20081106 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7547A 53029 3/8 INCH HOLE IN CUSP LEFT SIDE, AFT OF FRAME 864, APPROXIMATE 10 INCH AFT AND INBOARD 6 3/4 INCH. INSTALLED DOUBLER P ER SRM 53-01-00 IN CABIN FLOOR CUSP. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 UALA2008111306273 1 20081024 A 5753 FITTING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE TE FLAP CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 647UA 25284 LT WING OUTBOARD FLAP, OUTBOARD, AUX TRACK ATTACH FITTING TO RS, IS CRACKED. REPLACED FITTING. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 WP 2008 11 24 AALA200810019 1 20081013 A 5310 BEAM DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 AFT DOOR BEAM CORRODED. INSTALLED DOUBLER PER AARD 53-10-00-03. 2 L 7 2 4F A6WE 20081007 NM 2008 10 7 AALA200802081 1 20080812 A 3350 LIGHT DOUG MD80 MD83 3023681 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 951TW 53470 LGA EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 11D. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F RT 20081007 NM 2008 10 7 AALA200802080 1 20080812 A 3350 LIGHT DOUG MD80 MD83 3023681 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 951TW 53470 LGA EXTERIOR EMERGENCY LIGHT AT AFT RT HAND INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RT HAND AFT. SY STEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT 20081007 NM 2008 10 7 AALA200802079 1 20080812 A 3350 BRACKET BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 394AN 29431 JFK EMERGENCY EXIT SIGN LIGHT AT RT NR 1 DOOR HAS DAMAGED BRACKET. REPAIRED BRACKET FOR EMERGENCY EXIT SIGN LIGHT AT RT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081007 NM 2008 10 7 AALA200802078 1 20080812 A 3350 LAMP BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 DFW EMERGENCY LIGHT AT SEAT 24C INOPERATIVE. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 24C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802056 1 20080809 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 754AN 30262 DFW EMERGENCY LIGHT AT SEAT 33C MISSING LAMP. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 33C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802070 1 20080811 A 3350 LIGHT BOEING 737 737823 13844BZ NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 938AN 29533 DFW EMERGENCY SLIDE LIGHT AT LT NR 1 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY SLIDE LIGHT AT LT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20081008 WP 2008 10 8 AALA200802048 1 20080809 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 493AA 49731 SFO EMERGENCY LIGHT AT OVERHEAD FIRST CLASS CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 2 FOR EMERGENCY LIGHT AT OVERHEAD FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081008 EU 2008 10 8 RMX2008F00004 1 20080923 A 5330 1172250402 SKIN BOLKMS 117 BK117A4 5626017 EU FUSELAGE DAMAGED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 171MU 9946 7138 DURING A SCHEDULED INSPECTION, 3 AREAS OF THE PRIMARY FUSELAGE SKIN HAD CORROSION DAMAGE THAT WAS COMPLETELY THROUGH THE SKIN THICKNESS. DAMAGE AREA WAS APPROX 1 SQ INCH AT EACH DAMAGE LOCATION. THE AREAS WERE LOCATED AT; 1 EA AREA UNDER T HE REFUELING GROUND CLIP LT FUSELAGE SKIN AT STA 5100MM, WL 1600MM. 2 EA AREAS; ONE ON BOTH LT AND RT FUSELAGE SKINS AT THE AFT ENGINE COWLING LATCH PLATE. FUSELAGE STA 5800, WL2600MM. (K) 1 G 7 2 3U H13EU 20081008 NM 2008 10 8 KCS2008F00011 1 20080913 A 3350 LIGHT BOEING 747 747123 1384873 NM CABIN INOPERATIVE A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 MAIN DECK STA 2290 OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. (K) 2 L 7 4 4F RT A20WE 20081008 NM 2008 10 8 KCS2008F00012 1 20080913 A 5315 FLOORBEAM BOEING 747 747122 1384872 NM BS 600 DAMAGED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 FORWARD BILGE FLOORBEAM UPPER CHORD IS DAMAGED AT STA 600, RBL 21. (K) 2 L 7 4 4F RT A20WE 20081008 NM 2008 10 8 KCS2008F00013 1 20080913 A 5311 FRAME BOEING 747 747122 1384872 NM BS 1820, RBL 11 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 19754 AFT BILGE FRAME WEB IS CRACKED AT STA 1820, RBL 11. (K) 2 L 7 4 4F RT A20WE 20081008 EA 2008 10 8 VNAA0809003 1 20080910 A 3250 16650101 MODULE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE COCKPIT FAILED A VNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 05 249PS 10311 7926 CREW REPORTED ON TAKE OFF ACFT PULLED HARD LT NEEDED FULL RT RUDDER AND TILLER TO MAINTAIN RUNWAY HEADING. TAKE OFF ABO RTED AT UNKNOWN SPEED. ACFT RETURNED TO GATE WITHOUT INCIDENT. MX INSPECTED ACFT AND R&R THE HAND CONTROL MODULE. NO OTHER DEFECTS WERE NOTED. ACFT RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20081008 NM 2008 10 8 AALA200802148 1 20080820 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 750AN 30259 DFW EMERGENCY LIGHT AT SEAT 12D MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 12D. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802149 1 20080820 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 750AN 30259 DFW EMERGENCY LIGHT AT FIRST CLASS GALLEY MISSING LENS. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FIRST CLASS GALL EY. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802131 1 20080819 A 3350 WIRE BOEING 777 777223 1385213 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 794AN 30256 ORD EMERGENCY LIGHT AT SEAT 13D INOPERATIVE. REPAIRED WIRE PULLED FROM CONNECTOR FOR EMERGENCY LIGHT AT SEAT 13D. SYST EM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802153 1 20080722 A 5315 141T5113 FLOORBEAM BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 328AA 22328 AFW FLOOR BEAM AT STATION 325 HAD CORROSION REMOVAL ON UPPER SURFACE OF HORIZONTAL FLANGES. AREA OF DISCREPANCY IS 2.0 INCH BY 1.5 INCH WITH A DEPTH OF 0.027 INCH AND 0.028 INCH. REPAIRED PER MRB 767 3254. 2 L 7 2 4F RT A1NM 20081008 NM 2008 10 8 AALA200802158 1 20080821 A 3350 LIGHT BOEING 767 767323 1385205 NM EXTERIOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 378AN 25447 DFW EXTERIOR EMERGENCY LIGHT AT RT NR 1 DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A1NM 20081008 NM 2008 10 8 AALA200802162 1 20080821 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 799AN 30258 JFK EMERGENCY LIGHTS AT LT SEAT ROWS 30 TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK M33401 FOR EMERGENCY LIGHTS AT LT SEAT ROW 30 TO AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802165 1 20080822 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 662AA 25296 DFW EMERGENCY LIGHTS AT OVERHEAD BULLNOSE SEAT 2E INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHTS AT OVERHEAD BULLNOSE SEAT 2E. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 NM 2008 10 8 KCSA081470 1 20080916 A 5311 FRAME BOEING 747 747123 1384873 NM FUSELAGE CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 717CK 20325 CHORD CORRODED AT STA 1241, RBL 95, WL 160. NEXT TO TOOTH FITTING STIFFENER. 2 L 7 4 4F RT A20WE 20081008 SO 2008 10 8 C2XA08RI130 1 20080906 A 3230 22250100003 SEQUENCE VALVE EMB 145 EMB145LR 3260212 SO NLG MALFUNCTIONED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 13566 15066 145622 FLIGHT 2825 EWR FLIGHT CREW REPORTED THAT DURING CLIMBING OUT OF EWR THEY HEARD A SOUND LIKE GEAR WAS STILL DOWN WITH GE AR LEVER UP AND GEAR INDICATION SHOWING UP POSITION. CREW RECYCLE GEAR TWICE AT AIR SPEED UNDER 200 KT. NOISE ONLY SLI GHTLY CHANGED WHEN GEAR WENT UP. FLIGHT CREW AIR RETURNED TO EWR UNEVENTFULLY. EWR MX R&R NLG SEQUENCE VALVE. R&R NLG RT DOOR AND THIRD UPPER LOCK BOX PROXIMITY SW. EWR MX PREFORMED LEAK AND OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081008 NM 2008 10 8 USAA920081685 1 20080916 A 5312 BULKHEAD BOEING 737 737401 1384701 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 409US 23879 CLT FPBH MAJOR REPAIR NR 4352195 & 4353371 PITTING CORROSION ABOVE & BELOW HORIZONTAL STIFFENER ON BULKHEAD WEB AT BS178 , WL218. ALSO CRACK AT BS218, LBL10. REPAIRED PITTING CORROSION ABOVE & BELOW HORIZONTAL STIFFENER AND CRACK ON BULKHE AD WEB AT BS178, WL218 LBL 10 IAW B737 SRM53-10-08. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 USAA920081686 1 20080915 A 5320 6517688U165 ANGLE BOEING 737 7374B7 1384702 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 NR 03C10753006/013 LEVEL 2 GALVANIC CORROSION ON Z ANGLE AT BS294.5 TO BS360, LBL17. REPLACED Z ANGLE AT BS 294. 5 TO BS360, LBL17 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 USAA920081682 1 20080828 A 5320 65C105922 SUPPORT BOEING 737 7373G7 1384595 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 SAL C17 MAJOR REPAIR NR 6091621 CORROSION ON SUPPORT BS947 5 INCHES, RBL8. REPLACED SUPPORT BS947 5 INCHES, RBL8 IAW B7 37 SRM 51-10-02-OG. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 2008UALA05652 1 20080908 A 3350 767 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 578UA 26694 SLIDE LIGHT INOP AT DOOR 4R. FOUND LAMP INOPERATIVE. REPLACED LAMP. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081008 EU 2008 10 8 2008UALA05653 1 20080908 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 417UA 483 EMERGENCY LIGHTS FAILED TEST, FAULTING L AFT EXTERNAL LOAD. REPLACED 2R EMERGENCY ESCAPE SLIDE. ACCOMPLISHED EMERGENCY LIGHT TEST. NO DEFECTS NOTED. INSPECTED SLIDE AT 2R, FOUND SECURED ON DOOR, CABLE ROUTED CORRECTLY, EMERGENCY LIGHT T ESTS OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20081008 2008 10 8 2008UALA05655 4 20080908 A 2300 8220330001 TRANSCEIVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT DEFECTIVE A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 590UA 28708 LEFT HF DOES NOT TRANSMIT ON 8843. SUSPECT LEFT COUPLER. REPLACED LT TRANSCEIVER. REPLACED LT COUPLER. OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081008 NM 2008 10 8 AALA200802184 1 20080824 A 3350 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 621AM 24579 DFW EMERGENCY LIGHT EXIT SIGN DECAL AT LT OVERWING EXIT DOOR DAMAGED. REPLACED DECAL FOR EMERGENCY LIGHT EXIT SIGN AT L T OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 WP 2008 10 8 AALA200802185 1 20080824 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 982TW 53632 LGA SEAT MOUNTED EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20081008 NM 2008 10 8 USAA920081629 1 20080903 A 5320 65528942 FLOOR SUPPORT BOEING 737 7374B7 1384702 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 CLT Q1 MAJOR REPAIR NR 03C10753073/038 FLOOR SUPPORT CRACKED AT BS540, BLO TO RBL24. REPLACED FLOOR SUPPORT AT BS540, B LO TO RBL24 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081008 WP 2008 10 8 ABXA080235 1 20080902 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 963AX 47780 EMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES. IAW DC9 AMM 33-53-00-8. 2 L 7 2 4F A6WE 20081008 WP 2008 10 8 AALA200802173 1 20080823 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 580AA 53157 DFW INFLIGHT T1841/23AUG. CREW REPORTED NLG WOULD NOT RETRACT AND SPOILER INDICATION ILLUMINATED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOUND NLG FLAT WITH NO EVIDENCE OF FLUID LEAKING. REPLACED NLG STRUT, PISTON SEALS AND SCHRAD ER VALVE. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20081008 NM 2008 10 8 USAA920081684 1 20080827 A 5311 6546550 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 308AW 24710 SAL C14 MAJOR REPAIR NR 6097545 GALVANIC CORROSION ON FRAME AT BS787. BETWEEN S24L TO S25L. REPAIRED FRAME AT BS787 BE TWEEN S24L TO S25L IAW B737 SRM 51-70-11-OG. UPON FURTHER EVALUATION FOUND THIS DISCREPANCY TO BE LEVEL 2 CORROSION. 2 L 7 2 4F RT A16WE 20081008 NM 2008 10 8 AALA200802088 1 20080812 A 3350 LENS BOEING 757 757223 1384957 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 646AA 24604 JFK EMERGENCY LIGHT AT AFT FIRST CLASS GALLEY FLOOR MISSING LENS. REPLACED DAMAGED LIGHT ASSEMBLY FOR EMERGENCY LIGHT A T FIRST CLASS GALLEY FLOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 NM 2008 10 8 2008UALA05739 1 20080915 A 3397 78941 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE EMERGENCY LIGHTS DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 791UA 26933 EMERGENCY LIGHT AT SEAT 2F AFT LIGHT WILL NOT WORK. FOUND UNPLUGGED. RECONNECTED. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081008 NM 2008 10 8 2008UALA05664 1 20080909 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 FLOORBEAM Y254 HAS CORROSION BETWEEN FR65 AND FR66 (MARKED). REPLACED BEAM 160. REPLACED FLOORBEAM 160. 2 L 7 2 4F 4 F RT A28NM E40NE 20081008 NM 2008 10 8 2008UALA05667 1 20080910 A 5711 STIFFENER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NLG WW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 816UA 871 STIFFENER IN NOSE WHEEL WELL LEFT SIDE IS CRACKED ON THE RISER. REPAIRED STIFFENER PER SRM 57-11-16. 2 L 7 2 4F 4 F RT A28NM E40NE 20081008 EU 2008 10 8 2008UALA05674 1 20080910 A 5210 FE1740011 BOTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR LOW A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 465UA 1341 DOOR 2L PRESSURE ASSIST BOTTLE LOW. READING 800 PSI. BOTTLE READS LOW. SERVICED BOTTLE. NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081008 NM 2008 10 8 AALA200802126 1 20080818 A 3350 PLACARD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 615AM 24491 DFW EMERGENCY LIGHT PLACARD AT LT AFT OVERWING EXIT SIGN COMING OFF. REPLACED PLACARD FOR EMERGENCY LIGHT AT LT AFT OVE RWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 NM 2008 10 8 2008UALA05675 1 20080910 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR SLIDE OUT OF ALIGNMENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 553UA 25277 DOOR 3R ARMING LIGHT WILL NOT ILLUMINATE. FOUND GIRT BAR OUT OF ALIGNMENT. REALIGNED GIRT BAR. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081008 NM 2008 10 8 2008UALA05677 1 20080910 A 3397 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT AT BOTTOM OF WALL NEAR DOOR 3 LAV 111 INOP. FOUND CONNECTOR UNSECURE. RESECURED EMERGENCY LIGHT CONNEC TOR. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081008 NM 2008 10 8 AALA200802114 1 20080815 A 3350 LIGHT BOEING 757 757223 1384957 NM CARGO BAY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 197AN 32391 DFW EMERGENCY LIGHT AT AFT CARGO DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT AFT CARGO DOOR. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 NM 2008 10 8 AALA200802109 1 20080815 A 3350 LENS BOEING 777 777223 1385213 NM CABIN INCORRECT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 767AJ 33539 DFW EMERGENCY LIGHT AT RT SEAT ROW 26 HAS WRONG LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RT SEAT ROW 26. SYSTEM GROU ND CHECKED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802108 1 20080815 A 3350 LENS BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 779AN 29955 DFW EMERGENCY LIGHT AT SEAT 26C MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802107 1 20080815 A 3350 LIGHT BOEING 777 777223 1385213 NM CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 779AN 29955 DFW EMERGENCY LIGHT AT SEAT 26C MISSING LAMPS. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 26C. SYSTEM GROUND CHECKED N ORMAL OPS. 2 L 7 2 4F RT T00001SE 20081008 NM 2008 10 8 AALA200802106 1 20080815 A 2910 HYDRAULIC LINE BOEING 757 757223 1384957 NM NLG WW LEAKING A AALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 21 699AN 27051 POS INFLIGHT T1818/15AUG. DURING CLIMB CREW REPORTED LT HYDRAULIC FLUID LOSS. RETURNED TO POS AND LANDED. DURING LAND ING 3 BRAKES SEIZED. REPLACED BROKEN FLEX HYDRAULIC HOSE FROM NOSE WHEEL DOORS. REPLACED NR 2, 6 AND 8 BRAKES DUE TO O VERHEAT. ALSO REPLACED NR 2 AND 4 MAIN TIRES. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20081008 EA 2008 10 8 TRAX20801125 1 20080906 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE DOOR MALFUNCTIONED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 820AS 7188 SERVICE DOOR WILL NOT STAY OPEN AND LOCKED. COULD NOT DUPLICATE. OK FOR SERVICE. NO FAULT FOUND. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801096 1 20080903 A 5534 DRAG ANGLE CNDAIR CL600 CL6002C10 1390015 EA VERTICAL STAB CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 709EV 10068 CRACKED DRAG ANGLE LT LOWER VERT STAB. MARKED. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801107 1 20080904 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 RT 280 WEB CORRODED. SUP CLOSED 9/15/2008 - BLENDED OUT CORROSION ON RT WEB. TOOK NO MORE THEN 004 OF MATERIAL IAW REP AIR NR 1 OF REO 670-53-11-052. ALODINE PRIME AND PAINT ON BLENDED AREAS IAW REO 670-53-11-052. 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801108 1 20080904 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 LT 280 WEBB CORRODED. SUP - 9/15/2008 - REMOVED LT WEB IAW REO 670-53-11-052. (K) 2 L 7 2 4F RT A21EA 20081008 EA 2008 10 8 TRAX200801109 1 20080904 A 5320 BEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 740EV 10151 RT 280 BEAM CORRODED. SUP 9/15/2008. INSTALLED DRIP TRAYS IAW SB670BA-53-026. (K) 2 L 7 2 4F RT A21EA 20081121 NM 2008 11 21 DLM88081579 1 20081117 A 5320 59360215 DOUBLER DOUG MD88 MD88 3023688 NM FS 1307 L21 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 980DL 53267 INTERNAL SURROUND DOUBLER FOR THE AFT LAV PAN WAS CORRODED ALONG THE LOWER EDGE. THE CORROSION WAS CUT OUT, AND AND EXT ERNAL REPAIR DOUBLER WAS INSTALLED. 2 L 7 2 4F RT A6WE 20081121 NM 2008 11 21 DL757081534 1 20081112 A 5530 175N11005 STRUCTURE BOEING 757 757232 1384965 NM VERTICAL STAB DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 DURING AGING AIRCRAFT INSPECTION, FOUR AREAS OF TOOLING DAMAGE WERE FOUND ON THE VERTICAL STABILIZER CHORD. BOEING WAS CONTACTED FOR APPROVAL TO LEAVE THE BLENDED MARKS AS IS. THE REPAIR IS DOCUMENTED IN ER/A 471254-14. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081546 1 20081009 A 5240 NUT PLATE BOEING 757 757232 1384965 NM R2 DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 R2 DOOR HAS 5 CORRODED NUT PLATES INSIDE FRAME AT CENTER OF DOOR, TWO FRAMES BELOW DOOR HANDLE. REPLACED CORRODED NUTPL ATE IAW SRM 52-10-02. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 SWAA086322 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086323 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP BROKEN AT BS 807, STR 26R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086324 1 20081118 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 27L TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081121 2008 11 21 SWAA086325 4 20081117 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 495WN 33869 FOUND R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081121 WP 2008 11 21 08FDEA04907 1 20081118 A 5310 ACA72241 DOOR FRAME DOUG DC10 DC1030F 3023504 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 318FE 46837 UPPER CARGO DOOR FOUND CORROSION ON UPPER EXT FACE OF LWR JAMB. REPAIRED AREA IAW EA NR 8-5310-125423. 2 L 7 3 4F RT A22WE 20081121 NM 2008 11 21 DLM88081523 1 20081109 A 5310 BEAM DOUG MD88 MD88 3023688 NM BS 1155-1212 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 968DL 53161 DURING HMV3 CORROSION WAS FOUND ON LWR BEAM AT AFT CARGO COMPARTMENT BTW STA Y=1155 TO1212 AND LONGERON 28 RT. AREA WAS REPAIRED IAW SRM 53-05 FIG 123. 2 L 7 2 4F RT A6WE 20081121 NM 2008 11 21 DLM88081526 1 20081109 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 332-351 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 968DL 53161 DURING HMW LIGHTNING STRIKE WAS FOUND ON FUSELAGE SKIN BTW LONGERON 26-27 RT AND STA Y=332-351. AREA WAS REPAIRED IAW S RM 53-04D FIG 12C. 2 L 7 2 4F RT A6WE 20081121 EA 2008 11 21 SWIA200820369 1 20080715 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 368CA 10075 C-CHECK, PASSENGER DOOR AFT WEB CRACKED AT ZONE 2 AND 3. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081121 WP 2008 11 21 AALA200810123 1 20081023 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 CORROSION ON RIGHT CUSP AT STATION 864 - 886. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 UALA2008111306381 1 20081105 A 3350 58781 POWER STRIP BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 942UA 26679 CABIN FLOOR EEL INOP FROM ROW 11 TO ROW 14. SPLICED EEL POWER STRIP AT ROW 11. OP CHECKS OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 20081124 WP 2008 11 24 AALA200810134 1 20081027 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 LEFT CUSP CORRODED AT STATION 1250 TO 1309. INSTALLED NEW CUSP SHEET FROM STATION 1250 TO 1309. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810113 1 20081028 A 5311 FRAME DOUG DC9 DC982 3022082 WP ZONE 100 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 251AA 49270 DOUBLER ON FORWARD SIDE OF FRAME STATION 1380 HAS HOLE WORN IN IT. REPLACED DOUBLER PER AARD 53-10-00-28. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 UALA2008111706534 1 20081115 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 204UA 28713 EEL LIGHT ON SEAT 13G FWD LIGHT INOP. RELAMPED, OPS CHECK OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081124 NM 2008 11 24 UALA2008111303275 1 20080608 A 2150 8102142 VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE AC BAY FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 206UA 30212 PACK MODE R RIGHT PACK AIR CYCLE MACHINE HAS FAILED, OR RIGHT ECONOMY COOLING VALVE FAILED OPEN, OR BOTH RIGHT CONDENSOR INLET TEMP SENSORS FAILED. RIGHT PACK IS OPERATING IN A NON-NORMAL MODE (HEAT EXCHANGER ONLY COOLING MODE). ADVISORY CREW COMMENTS: PACK MODE R. FOUND LOW LIMIT VALVE FAULTY. REPLACED LOW LIMIT VALVE. OP CHECK GOOD. AC OK FOR SERVIC E. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081124 NM 2008 11 24 UALA2008111303782 1 20080708 A 2797 D4367J CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DEFECTIVE A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 653UA 25391 VIBRATION FELT IN CONTROL COLUMN. FLIGHT DIVERTED. FOUND DEFECTIVE CONTACTS ON CONNECTOR 4367J AND REPAIRED. PERFORME D SINGLE SYSTEM ELEVATOR TEST GOOD. PERFORMED SINGLE SYSTEM RUDDER TEST GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 EA 2008 11 24 MAL2008F00053 1 20081003 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY MALFUNCTIONED A MALA O OTHER N FALSE WARNING CL CLIMB 1 GL 15 8943A 7943 AT 2000 FT GOT `SMOKE TOILET` EICAS MESSAGE AND DID AIR RETURN TO MSP. FLIGHT 3272 RETURNED TO MSP AFTER DEPARTURE DUE TO A LAVATORY SMOKE DETECTOR WARNING. THE CREW CALLED AFTER LANDING AND ACTUALLY SAID IT WAS A LAV SMOKE MESSAGE THAT W AS DISPLAYED RT AFTER T.O. THE CREW STAYED IN PATTERN, DECLARED AN EMERGENCY AND RETURNED TO MSP WITHOUT INCIDENCE. F/ A VERIFIED NO SMOKE. REPLACED DETECTOR. (K) 2 L 7 2 4F RT A21EA 20081125 WP 2008 11 25 AALA200510032 1 20081017 A 5320 DIAPHRAGM DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 CORROSION ON DIAPHRAGM UNDER G-1 GALLEY DRAIN PAN. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 HALA2008110900852 1 20081109 A 2841 HG1057AA07 PROCESSOR BOEING 767 767332 1382001 NM INOPERATIVE A HALA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, RT FUEL QUANTITY INDICATOR BLANK, TOTALIZER BLANK. NO EICAS MSG. ACCOMPLISHED FUEL QTY TEST IAW DELTA FIM 28-41-00 FIG 103. TEST OK PERFORMED FQIS BITE FAULTED B8, A8, C3, C6, 81, 82, 83 AND 88. REMOVED AND REP LACED FQIS PROCESSOR IAW DELTA AMM 28-41-08. BITE CK, NO FAULTS. A/C DIVERTED TO LAX FROM LAS, WHERE AN UNEVENTFUL LAN DING WAS MADE. 2 L 7 2 4F RT A1NM 20081125 EA 2008 11 25 SWIA200820422 1 20080818 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 441SW 7602 C-CHECK, FS 280 FLOOR SUPPORT BEAM INBOARD AND OUTBOARD CLIPS CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081125 EA 2008 11 25 SWIA200820430 1 20080821 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 962SW 7859 C-CHECK, FS 625 LEFT INTERCOSTAL CLIP CRACKED AT STRINGER 14. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081125 WP 2008 11 25 AALA200810030 1 20081016 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 SEAT TRACK NR 6 HAS CORROSION, STATION 214-220 RIGHT. INSTALLED NR 6 SEAT TRACK SPLICE PER SRM 53-05-00. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810032 1 20081117 A 5320 DIAPHRAGM DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 CORROSION ON DIAPHRAGM UNDER G-1 GALLEY DRAIN PAN. INSTALLED DOUBLER REPAIR PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 SWAA086329 1 20081118 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086330 1 20081118 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086331 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086379 1 20081119 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE DAMAGED AT BS 520, BETWEEN STR 16R TO STR 17R. REMOVED AND REPLACED SHEAR T IE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086332 1 20081118 A 5313 6551698 STRINGER SPLICE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086380 1 20081119 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 23R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086435 1 20081120 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FRAME PER PAE ER. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086436 1 20081120 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BETWEEN BS 500A TO BS 500B, STR 19L. REMOVED AND REPLACED CL IP PER SRM. 2 L 7 2 4F RT A16WE 20081125 EA 2008 11 25 SWIA200820401 1 20080808 A 7120 BUSHING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 443SW 7638 C-CHECK, RIGHT ENGINE FORWARD MOUNT YOKE FLANGED BUSHINGS CORRODED, REPLACED. 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 SWAA086416 1 20081120 A 2560 6557463 BRACKET BOEING 737 7375H4 138449D NM GIRT BAR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 FOUND R2 DOOR SLIDE GIRT BAR CLIP BROKEN. REMOVED AND REPLACED BRACKET PER MM. 2 L 7 2 4F RT A16WE 20081125 EA 2008 11 25 SWIA200820402 1 20080808 A 7120 BUSHING CNDAIR CL600 CL6002B19 1900309 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 443SW 7638 C-CHECK, LEFT ENGINE FORWARD MOUNT YOKE FLANGED BUSHING CORRODED, REPLACED. 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 HALA2008111300847 1 20081113 A 5350 SUPPORT ANGLE BOEING 767 76733A 1385209 NM FAIRING CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 FAIRING 139C SUPPORTING CROSSMEMBER CORRODED AROUND SWAGE NUTS, CROSSMEMBER (P/N:145T8629-2). REPLACED, PAINT AND CPC A PPLICATION PRIOR TO RE-INSTALLATION. 2 L 7 2 4F RT A1NM 20081125 EA 2008 11 25 SWIA200820408 1 20080813 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 963SW 7865 C-CHECK, FS 280 FLOOR SUPPORT CAP ANGLE CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 SWAA086353 1 20081118 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086424 1 20081120 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086425 1 20081120 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 2008 11 25 SWAA086417 4 20081120 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086406 1 20081119 A 3230 BACC2C4A05561FG CABLE BOEING 737 7373H4 1384600 NM LANDING GEAR FOD A SWAA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 29 608SW 27928 AIR TURNBACK, AFTER T/O HAD TO USE TRIGGER TO RETRACT LANDING GEAR. CONFIGUATION WARNING HORN SOUNDED CONTINUOUSLY AFTE R GEAR RETRACTION. FOUND FOD ON TELEFLEX CABLE. REMOVED AND REPLACED CABLE PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086356 1 20081118 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 WP 2008 11 25 AALA200810042 1 20081015 A 5311 FRAME DOUG DC9 DC982 3022082 WP ZONE 100 CUT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 241AA 49254 BELLFRAME STATION 1338 CUT AT LONGERON 6 RIGHT. REMOVED SECTION FROM LONGERON 6 RIGHT TO LONGERON 18 RIGHT FOR OTHER MA INTENANCE. SPLICED IN REPAIR PER ESO 80559 DATED SEPT 29-08 IN AFT CABIN. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 HALA2008111200850 1 20081112 A 2620 LAMP BOEING 767 76733A 1385209 NM TEST SWITCH INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 580HA 28140 ETOPS SIGNIFICANT SYSTEM, APU SQUIB WOULD NOT TEST. RELAMPED APU SQUIB TEST SWITCH. OPS OK, TEST OK. 2 L 7 2 4F RT A1NM 20081125 EA 2008 11 25 SWIA200820409 1 20080813 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 963SW 7865 C-CHECK, FS 280 FORWARD FACE ANGLE CRACKED, REPLACED. 2 L 7 2 4F RT A21EA 20081125 WP 2008 11 25 AALA200810065 1 20081001 A 5340 ATTACH ANGLE DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 RIGHT WHEEL WELL TRAP FITTING UPPER FORWARD ATTACH ANGLE HAS CORROSION AT VERTICAL ATTACH BOLTS ABOVE BRAKE ACCUMULATOR. REMOVED CORRODED ANGLE AND INSTALLED SERVICEABLE REPLACEMENT ANGLE. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 SWAA086337 1 20081118 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 305, WL 261. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081125 WP 2008 11 25 08FDEA04938 1 20081120 A 5730 ARC1111502 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 317FE 46835 DURING INSPECTION RT WING LWR SURFACE FOUND SCRATCH 22 INCHES LONG AND DEEP DENT 3 INCHES BY 3 INCHES DEEP .161 INCH ON LWR SKIN OF OUTBD AILERON. DAMAGE IS "NOT/FLIGHT AIRCRAFT STRIKE DAMAGE". 2 L 7 3 4F RT A22WE 20081124 EU 2008 11 24 AALA200820015 1 20081014 A 5310 FAILSAFE AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 40064 0507 FAIL/SAFE RING FASTENERS CORRODED. REMOVED CORROSION IAW EA A300-53-004721 DATED 13 OTC 2008. 2 L 7 2 4F RT A35EU 20081124 NM 2008 11 24 UALA2008111306414 1 20081106 A 2910 272W4592180 HYDRAULIC LINE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE RT MLG WW LEAKING A UALA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 29 798UA 26928 RIGHT MLG WHEEL WELL HYD LEAK. FOUND TUBING THAT IS LEAKING. REMOVED LEAKING HYDRAULIC LINE FROM AIRCRAFT AND ROUTED T O TUBE SHOP FOR MANUFACTURING OF NEW LINE. NEW LINE WILL BE READY AROUND 2100. INSTALLED NEW DOOR LOCK LOWER HYD LINE FROM ACTUATOR TO TEE FITTING. PRESSURE CHECKED, NO LEAKS NOTED. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081124 WP 2008 11 24 AALA200810112 1 20081027 A 5322 SHEAR TIE DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 251AA 49270 SHEAR TIE CRACKED AT STATION 1437 AFT SIDE. REPLACED SHEAR TIE AT STATION 1437 PER SRM 53-01. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 UALA2008111306461 1 20081109 A 3397 794640 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 EEL LIGHT INOP AT LEFTSIDE MID LAV. REPAIRED FEEDER ASSY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 WP 2008 11 24 AALA200810020 1 20081014 A 5321 FLOOR PANEL DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 CORROSION ON SUBFLOOR FORWARD OF NR 6 SEAT TRACK. CORROSION REMOVED AND INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 UALA2008111406513 1 20081114 A 3350 582233 CHARGER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 OVERWING EMERGENCY LIGHT RT 2 BOTTOM LIGHT INOP. REPLACED BATTERY CHARGER. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111706517 1 20081114 A 3397 794640 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 663UA 27160 EEL EMERGENCY LIGHT STRIPS INOP ON LEFT AISLE IN THE VICINITY 1AB THRU 5AB. SECURED CONNECTOR, TEST OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 NM 2008 11 24 UALA2008111706518 1 20081114 A 3397 80172424 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN NOT SEATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 772UA 26930 AFT EEL LIGHT ON SEAT 3E INOP. RESEATED CONNECTOR, OPS CHECK OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081124 SO 2008 11 24 LR7A08122 1 20081101 A 3610 1511623101 DUCT LKHEED 382 382G 526414U SO NR 3 BLOWN A LR7A E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CL CLIMB 1 AL 03 401LC 153 4606 DURING CLIMB, FLIGHT CREW NOTED NR 3 ENGINE NACELLE OVERHEAT ANNUNCIATION AND PERFORMED ENGINE SHUTDOWN IAW AFM AT 14:28 Z. REPLACED UPPER BLEED AIR MANIFOLD ON NR 3 ENGINE, LEAK CHECK GOOD PER SMP581 CH 36-10. 2 H 7 4 4T A1SO 20081124 WP 2008 11 24 AALA200810172 1 20081107 A 5311 FRAME DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 587AA 53250 CRACK APPROXIMATELY 1 INCH IN LENGTH AT TOP OF OPENING FOR LEFT FORWARD OVERWING EXIT DOOR, FORWARD OF LATCH. STOP DRIL LED AND DOUBLER INSTALLED PER SRM 53-05-00 FIGURE 32, SHEET 1. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 AALA200810164 1 20081029 A 5320 WEB BOEING 737 737823 13844BZ NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 CORROSION ON FLOOR WEB. INSTALLED DOUBLER PER SRM 51-70-13. 2 L 7 2 4F RT A16WE 20081124 EU 2008 11 24 MALA080196 1 20081109 A 5311 FRAME SAAB SF340 340B 7860101 EU BS 294 DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 340B427 FRAME DAMAGED AT STA 294 BETWEEN SL1617 AND SL1618. REPAIRED IAW EO NR S53152. 2 L 7 2 4T RT A52EU 20081124 NM 2008 11 24 08FDEA04933 1 20081119 A 5347 53FX976500 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 200 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 469FE 21581 FOUND CORROSION ON SEAT TRACK STA 1130 TO 1180 BL0. FOUND CORROSION OUT OF LIMITS, REMOVED SEAT TRACK, FABRICATED SEAT TRACK AND INSTALLED SEAT TRACK IAW DWG 53FX976. 2 L 7 3 4F A3WE 20081124 NM 2008 11 24 NWAA084806308 1 20081102 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 668US 24223 DURING OVER NIGHT CHECK FOUND DOOR 1 RT EXIT SIGN LIGHT INOP. MX R&R EMERGENCY LIGHT BATTERY AND POWER SUPPLY. OPS CHE CKED GOOD, AND ACFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20081124 SO 2008 11 24 C2XA08RI158 1 20081018 A 3350 1317 BULB EMB 145 EMB145LR 3260212 SO EMERGENCY LIGHT BURNED OUT A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13956 145078 RIC MX DURING ROUTINE MX, FOUND LT OVER WING EMERGENCY LIGHT TO BE INOPERATIVE. MX R&R EMERGENCY BULB AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081124 SO 2008 11 24 C2XA08RI160 1 20081018 A 2150 8152402 ACM EMB 145 EMB145LR 3260212 SO NR 2 SMOKE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 27 12957 24626 145080 FLIGHT 2994 EWR FLIGHT CREW REPORTED ACFT CABIN FILLED WITH SMOKE WHILE PACK NR 2 DURING PREFLIGHT. EWR MX R&R NR 2 PAC K AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081124 NM 2008 11 24 UALA2008111303975 1 20080726 A 2424 GCU BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT ENGINE MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 668UA 30024 LEFT GENERATOR FAILURE. FLT DIVERTED. BELIEVED TO BE A POWER TRANSFER PROBLEM. REPLACED L ENG GCU. CHECKS OK ON B PC U. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 NM 2008 11 24 UALA2008111304042 1 20080728 A 5297 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CARGO DOOR LOOSE A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 651UA 25389 FWD CARGO DOOR EICAS ALONG WITH OVERHEAD CARGO DOOR LIGHT. RTFL. FOUND LOOSE CONNECTOR ON FWD CARGO DOOR WIRE HARNESS. SECURED CONNECTOR & DOOR INDICATION OPS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 NM 2008 11 24 UALA2008111305409 1 20080822 A 5210 624EN338R SWITCH BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L4 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 DOOR 4L SLIDE PACK ARM MODE SELECTOR SWITCH FAILED TEST PER JC 283507211. NO CONTINUITY ON DOOR ARMING CONDUIT. FOUND FAULTY SWITCH. REPLACED DOOR OPEN SWITCH, OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081124 EU 2008 11 24 UALA2008111305933 1 20080929 A 3830 TOILET AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LAVATORY INTERMITTENT A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 455UA 1105 LAVATORY TOILET BOWL FLUSH SYSTEM INOPERATIVE AT AFT CABIN LIGHT AFT LAV. CREW COMMENTS: BOTH AFT LAV TOILETS FLUSH SY STEMS ARE INTERMITTENT. WASTE TANK SERVICED. RESET PWR TO LAVS. ALL LAVS FLUSH NORMALLY. NO HISTORY IN AMIS. 2 L 7 2 4F 4 F RT A28NM E40NE 20081124 2008 11 24 UALA2008111806555 4 20081118 A 2565 BOTTLE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE EVAC SLIDE LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 805UA 783 DOOR 1R SLIDE BOTTLE PRESSURE IS LOW. ACCOMPLISHED CHECK OF SLIDE PRESSURE. SLIDE PRESSURE GAUGE IN LOWER LIMITS OF GR EEN BAND. 2 L 7 2 4F 4 F RT A28NM E40NE 20081124 NM 2008 11 24 UALA2008111806556 1 20081117 A 5210 RESERVOIR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 551UA 25399 DOOR 2L EMERGENCY POWER RESERVOIR PRESSURE IS LOW. REMOVED AND REPLACED THE L -2 DOOR EMERGENCY POWER RESERVOIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 NM 2008 11 24 UALA2008111806557 1 20081118 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 DOOR 2R & 4R EVAC SLIDE LIGHTS INOP. RELAMPED, OP CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111806560 1 20081118 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT SIGN INOP AT DOOR 3 RIGHT UPPER SIGN. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111806561 1 20081118 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT LIGHT INOP DOOR 3 RIGHT BUSTLE LIGHT. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111806562 1 20081118 A 3350 582233 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT LIGHT INOP DOOR 3 RIGHT CEILING ENTRY LIGHT. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NE 2008 11 24 UALA2008111306036 2 20081008 A 7532 BLEED VALVE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE NR 1 ENGINE BROKEN A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 811UA 847 ENG 1 BLEED FAULT. RTFL. AIR CREW COMMENTS: ON CLIMBOUT THRU 3K FEET ECAM AIR ENG NR 1 BLEED FAULT; UNABLE TO RETURN NORMAL. FOUND CONNECTOR FOR VALVE 4001HA ON NR 1 ENGINE BROKEN. RE-ACTIVATED HPV. CREATED NEW ITEM FOR BLEED PRESS RE G VALVE 4001HA RPL AND CONNECTOR REPAIR. REPLACED CONNECTOR BACKSHELL ON CONNECTOR THAT CONNECTS TO NR 1 BLEED PRESSURE REGULATOR. PRESSURE REG BLEED VALVE REMOVED. UNABLE TO INSTALL NEW VALVE DUE TO BROKEN CONNECTOR. INSTALLED NEW VALV E. ACCOMPLISH OP TEST OF BLEED PRESS-REG VALVE WITH ENG IN OPERATION. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081124 EU 2008 11 24 UALA2008111306255 1 20081023 A 3260 848401 SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT MLG FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 487UA 1669 LANDING GEAR SYS DISAGREE ON UPPER ECAM. RTFL. THE RT MLG EXTEND SENSOR 20GA HAS FAILED. REMOVED AND REPLACED RT MLG EXTEND SENSOR. OPS TEST NORMAL. BITE TEST NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081124 NM 2008 11 24 UALA2008112006572 1 20081120 A 2120 3010000801 OVEN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 778UA 26940 CREW REPORTS AFTER DESCENT AND LEVEL AT APPROX 12K FT, SMELLED A BURNING ELECTRIC ODOR WHICH DISSIPATED AFTER A FEW MINU TES. CONTINUED APPROACH AND GEAR WAS SELECTED DOWN AND POWER INCREASED THE ODOR RETURNED UNTIL LANDING. CREW ALSO STAT ES THAT ODOR WAS ONLY NOTICED IN FLT DECK AND NOTHING IN MAIN CABIN IN ANY ZONE. R031 POPPED BREAKER. REPLACED OVEN. RAN FOR 20 MINUTES. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081124 2008 11 24 UALA2008111806566 4 20081118 A 2565 SHIM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 523UA 24932 LEFT OFF-WING SLIDE PACK INFLATION HOSE ADAPTOR FITTING HAS A BROKEN MICARDA SHIM. REPLACED SHIM. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 NM 2008 11 24 UALA2008111806567 1 20081118 A 5210 DOOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L3 DOOR LACK OF LUBE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 582UA 26702 DOOR 3L WILL NOT ARM. LUBED DOOR, REMOVED SMALL AMOUNT OF ICING. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 NM 2008 11 24 UALA2008111806568 1 20081115 A 2560 81020401 PROXIMITY SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 573UA 26685 DOOR 3R SLIDE LIGHT IS OUT. REPLACED DOOR 3R AFT GIRT BAR PROXIMITY SWITCH. OPS CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 NM 2008 11 24 UALA2008111806569 1 20081114 A 5753 SUPPORT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAP DEFECTIVE A UALA K NONE W INADEQUATE Q C NR NOT REPORTED 1 WP 29 550UA 25398 FOUND "T/E FLAP TT SPRT" INBOARD BRG OUTER RACE SPINNING DURING OPS CHECK, LOCATED BETWEEN NR 5 AND NR 6 XMISSION. REPL ACED TORQUE TUBE BEARING SUPPORT ASSY WITH NEW, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 2008 11 24 UALA2008111806571 4 20081115 A 2310 HF COMM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 663UA 27160 HF SYSTEM FAULTY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 CE 2008 11 24 DXTA2008111803361 1 20081117 A 3230 LANDING GEAR CESSNA 680 680CE 2076811 CE MALFUNCTIONED E DXTA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 357QS 6800155 AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. 2 L 7 2 4F RC T00012WI 20081124 CE 2008 11 24 DXTA2008111203350 1 20081111 A 3240 WARNING SYSTEM CESSNA 560 560XL 2076702 CE COCKPIT ACTIVATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 667QS 5605365 DURING T/O ROLL LO BRAKE PRESS AND ANTI SKID INOP ANNUNCIATORS, ILLUMINATED. T/O ABORTED. 2 L 7 2 4F RT A22CE 20081120 NM 2008 11 20 QXEA2008111401185 1 20081111 A 3250 STEERING SYS BOMBDR DHC8 DHC8402 1390042 NM NLG MALFUNCTIONED A QXEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NM 19 427QX 4156 SEA - NOSE STEERING CAUTION LIGHT ILLUMINATED ON FINAL APPROACH BEFORE GEAR DOWN. CYCLED STEERING SWITCH AS PER CHECK L IST, BUT CAUTION LIGHT REILLUMINATED. ABORTED APPROACH. PERFORMED NORMAL GEAR EXTENSION AND LANDING. PERFORMED SCU IN TERROGATION PER AMM TASK NR 32-51-01-742-801. CLEARED SCU NVM PER AMM TASK NR 32-51-01-743-801. ALL FAULTS CLEARED. P ERFORMED NWS OPS CHECK PER AMM TASK NR 32-51-00-710-801. OPS CHECK GOOD. NO SCU FAULTS OR NWS CAUTION RE-OCCURRING. R ETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081120 NM 2008 11 20 QXEA2008111401186 1 20081112 A 7500 8209712 SHUTOFF VALVE BOMBDR DHC8 DHC8402 1390042 NM NR 1 BLEED MALFUNCTIONED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 19 416QX 7263 3319 4083 SEA - EXHAUST ODOR FROM BLEEDS SEEMS MORE PRONOUNCED FROM BLEED NR 1, NR 1 ENG BLEED OP INCREASES FUEL FLOW 70 NR ITT. REMOVED AND REPLACED NR 1 HPSOV IAW AMM 36-11-09 PG 401-405. OPS CHECKED GOOD. NO ODOR PRESENT. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081120 SO 2008 11 20 SWIA200820383 1 20081107 A 2120 UNKNOWN EMB 120 EMB120ER 3260203 SO CABIN SMOKE A SWIA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 NM 07 564SW 120339 FLT 5734 - AFTER POWER REDUCTION IN DESCENT, AIRCRAFT FILLED WITH SMOKE. SMOKE LIGHT ON MAP ASSOCIATED WITH LAV DETECTO R. INSPECTED RT AND LT ENGINES, RT AND LT PACKS, APU, NO DEFECTS FOUND. RAN ENGS AND APU IN MULTIPLE BLEED CONFIGURATI ONS, COULD NOT DUPLICATE. 2 L 7 2 4T RT A31SO 20081120 NM 2008 11 20 08FDEA04925 1 20081119 A 2782 651781823 ACTUATOR BOEING 727 727225 1384077 NM NR 7 SLAT FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 468FE 4081 38 21452 NR 7 LED FAILED TO RETRACT AFTER TAKEOFF. WHEN GOING FROM 2 DEG TO 0 DEG, RAN QRH LED DID NOT RETRACT FLIGHT CONTROLS I NPUTS INDICATE THE LED WAS ACTUALLY EXTENDED. REMOVED AND REPLACED NR 7 SLAT ACTUATOR PER M/M 27-81-032-4. OPS CKS AND LEAK CKS NML. 2 L 7 3 4F A3WE 20081120 NM 2008 11 20 08FDEA04904 1 20081117 A 5415 311N51932 SKIN BOEING 757 757236 1384971 NM ZONE 400 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 915FD 24120 WHILE DRILLING THE NR 1 PYLON INBD FWD 311N5193-2 SKIN PANEL NUMEROUS FASTENER HOLES WERE OVERSIZED AND ELONGATED. THE NUMEROUS FASTENER HOLES THAT WERE OVERSIZED AND ELONGATED WERE REPAIRED AND A NEW 311N5193-2 SKIN PANEL INSTALLED PER MAE EA NR 757-5452-16-A1808 REV A. COMPLIED WITH FEDEX EA NR F-5450-124028 REV A ON NR 1 PYLON INBOARD SKIN. 2 L 7 2 4F RT A2NM 20081120 NE 2008 11 20 EIA2008055 2 20080929 A 7200 ENGINE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE NR 2 MAKING METAL A EIAA O OTHER O OTHER CR CRUISE 1 NM 19 485EV 20712 689564 DURING CRUISE ENCOUNTERED HEAVY SURGE NR 2 ENG ALONG WITH VIBRATION EPR DROPPED TO BOTTOM OF SCALE EGT REACHED YELLOW BA ND, REDUCED POWER TO IDLE, VIBRATION PERSISTED, SHUT NR 2 ENGINE DOWN ENG WINDMILL OIL PRESS AT 28PSI. ANGLE GEARBOX AN D MAIN GEARBOX CHIP DETECTORS REMOVED. METAL FOUND AT LOWER RT 3.5 BLEED PORT. REPLACED ENGINE IAW WORK CARD F7201-JT9 . (K) 2 L 7 4 4F 4 F RT A20WE E20EA 20081120 CE 2008 11 20 EWC2008F00000 1 20081001 A 7331 57847 PRESSURE SENSOR CESSNA 525 525 2076601 CE RT ENGINE FAULTY E EWCA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 39 44CK 2416 5250401 AFTER DEPARTURE, THE CREW NOTICED THE ANNUNCIATOR WARNING LIGHT COME ON FOR THE RT ENGINE FUEL FILTER BYPASS. THE CREW NOTIFIED ATC, DECLARED AN EMERGENCY, AND WERE ROUTED FOR LANDING, AFTER ARRIVING SAFELY AND CONFERRING WITH THE MFG ON F IELD, THE RT FUEL FILTER WAS REPLACED AND THE BYPASS PRESSURE SENSOR WAS ALSO REPLACED CORRECTING THE PROBLEM. THE RT F UEL FILTER SHOWED NO SIGNS OF CONTAMINATION. (K) 1 L 7 2 4F RT A1WI 20081121 NM 2008 11 21 DL757081575 1 20081111 A 5321 453N117070 FLOOR PANEL BOEING 757 757232 1384965 NM FWD CARGO BAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 FWD CARGO BAY, BS 550 - 650 LBL 19 - RBL 19, FLOOR PANEL MATING SURFACES HAVE AREAS OF SURFACE CORROSION. FABRICATED AN D REPLACED FLOOR PANEL IAW SRM 51-40-02, SRM 53-30-53. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081583 1 20081117 A 5320 146N852251 SILL BOEING 757 757232 1384965 NM BS 1360 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 DURING HMV, TWO FASTENER HOLES WERE MISDRILLED IN THE INNER CHORD OF THE LOWER SILL OF THE AFT CARGO DOOR CUTOUT AT STA 1360. THE OVERSIZE HOLES WERE PLUGGED AND A REPAIR ANGLE WAS INSTALLED PER REPAIR INSTRUCTIONS. 2 L 7 2 4F RT A2NM 20081121 CE 2008 11 21 GUUA11070801 1 20081107 A 3233 11238002223 ACTUATOR BEECH 1900 1900D 1154162 CE NLG CRACKED A GUUA O OTHER K FLUID LOSS AP APPROACH 1 SO 29 69547 9213 UE189 FLIGHT 9294 FKL/DUJ - DURING APPROACH HEARD A BANG NOISE DURING THE LANDING GEAR EXTENSION. DID NOT NOTICE ANYTHING UNU SUAL OR ABNORMAL AS A RESULT OF THE NOISE. OBTAINED POSITVIE INDICATION THAT THE LANDING GEAR WAS DOWN AND LOCKED. CON TINUED TO DUJ LANDED WITHOUT INCIDENT. DURING POST FLIGHT NOTICED NOSE GEAR HYDRAULIC FLUID LEAKING ON THE GROUND. REP LACED NOSE LANDING GEAR ACTUATOR. LANDING GEAR OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081121 CE 2008 11 21 GUUA11020801 1 20081102 A 3230 1143640683 PRINTED CKT BOAR BEECH 1900 1900D 1154162 CE LANDING GEAR DEFECTIVE A GUUA O OTHER O OTHER CL CLIMB 1 SO 29 81546 UE187 FLIGHT 5202 FLL/FLL - AFTER TAKEOFF LANDING GEAR SELECTED UP DISCOVERED LANDING GEAR CIRCIUT BREAKER POPPED. REPLACED T IME DELAY RELAY PCB. OPERATIONAL CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081121 NM 2008 11 21 SWAA086304 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 5R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086305 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 2R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086306 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 5L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 DL757081558 1 20081113 A 2520 PANEL BOEING 757 757232 1384965 NM ROWS 2CD & 26ABC STUCK A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 ROW 2 CD AND ROW 26 ABC OXYGEN PANEL WILL NOT DROP. DOOR LATCH ACTUATORS FOUND STICKING. ACTUATORS EXERCISED. NO DEFE CTS NOTED IAW SOPM 20-00-00 PAR 1D. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 SWAA086303 1 20081118 A 2560 6551463 MOUNT BOEING 737 7373H4 1384600 NM GIRT BAR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND R2 DOOR GIRT BAR FLOOR MOUNT DAMAGED. REMOVED AND REPLACED MOUNT PER MM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086289 1 20081118 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 492, STR 16R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086290 1 20081118 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086291 1 20081118 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081124 WP 2008 11 24 AALA200810022 1 20081014 A 5322 SHEAR TIE DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 SHEAR TIE CORRODED IN AFT CARGO AT STATION 1287 LONGERON 29 LEFT. INSTALLED SHEAR TIE AND DOUBLER PER SRM 53-03-00. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810114 1 20081029 A 5755 CASTING DOUG DC9 DC982 3022082 WP GROUND SPOILER CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 251AA 49270 GROUND SPOILER WING MOUNTED CASTING CRACKED AT INBOARD FORWARD END. REPLACED GROUND SPOILER CASTING. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810016 1 20081012 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 3 INCH CRACK IN LEFT CUSP BETWEEN NR 1 AND NR 2 SEAT TRACK AT STATION 1295. NEW LEFT CUSP INSTALLED AT STATION 1250 TO 1309 PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810077 1 20081016 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 CORROSION ON CUSP AT STATION 1136 TO 1174. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 DL757081552 1 20081010 A 5320 SILL BOEING 757 757232 1384965 NM BS 697 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 R2 DOOR SILL FWD SUPPORT FRAME HAS CORROSION AROUND FASTENER HOLE AT FS 697 RBL 46. BLENDED OUT CORROSION. FOUND TO BE IN LIMITS IAW SRM 53-10-15 DETAIL VI SECTION B-B. TREATED AND PRIMED IAW SRM 51-20-01 PG 1. 2 L 7 2 4F RT A2NM 20081124 NM 2008 11 24 DL757081553 1 20081010 A 5320 SILL BOEING 757 757232 1384965 NM BS 700-723 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 R2 DOOR SILL SUPPORT ANGLE HAS NUMEROUS FASTENER HOLES WITH CORROSION FROM STA 700-723. BLENDED CORROSION AND FOUND WIT HIN LIMITS IAW SRM 53-10-15 DETAIL VI SECTION B-B. TREATED AND PRIMED IAW SRM 51-20-01 PG 1. 2 L 7 2 4F RT A2NM 20081124 NM 2008 11 24 DL757081554 1 20081005 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1640 S29R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 LOWER FUSELAGE HAS DENT ON STR 29R STA 1640. CUT OUT DAMAGE IAW SRM 53-00-01 PG 201 DETAIL 1. INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 PG 201 REPAIR 2. 2 L 7 2 4F RT A2NM 20081124 NM 2008 11 24 UALA2008111706523 1 20081114 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT PIT FRAME DENTED STA 1460, STR 25L TO 24L. MAJOR REPAIR ACCOMPLISHED. CUTOUT DAMAGED SECTION OF PIT FRAME AND INST ALLED DOUBLER REPAIR. THIS ALSO INCLUDES DAMAGE NEAR STR 26L-25L. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 NM 2008 11 24 UALA2008111706524 1 20081114 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 AFT PIT FRAME UPPER FLANGE DENTED BETWEEN STR 26L AND 25L AT STA 1460. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECT ION OF PIT FRAME AND INSTALLED DOUBLER REPAIR. THIS ALSO INCLUDES DAMAGE NEAR STR 26L-25L. REPAIRED WITH SMC022. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 NM 2008 11 24 UALA2008111706529 1 20081115 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 47 RIGHT. REPLACED LIGHT ASSY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111706532 1 20081115 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 3J AFT LIGHT ASSY. REPLACED LAMP, OP CHECKS GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111706533 1 20081115 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 823UA 952 EMERGENCY SEAT LIGHTS INOP SEATS 15-16, 19-20, 23-24. REPLACED FAULTY POWER SUPPLY UNIT AND BATTERY, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 20081124 NM 2008 11 24 UALA2008111706539 1 20081117 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EEL LIGHT INOP GALLEY AT DOOR 2, MID LOWER WALL LIGHT. RELAMPED EMERGENCY LIGHT, CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111706540 1 20081117 A 2560 CONTROL PANEL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 UPPER DECK AFT FLT ATTENDANT STATION, EMERGENCY EVAC CONTROL PANEL "EVAC" LIGHT INOP. REPLACED EVAC CONTROL PANEL, OP C HECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111706541 1 20081117 A 5330 REPAIR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 551UA 25399 SKIN REPAIR DENTED STA 610, STA 620, STR 15L TO 16L. MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING REPAIR DOUBLER AND AC P'D SCRIBE LINE INSPECTIONS PER 757-53A0092 S/B AND ACP'D HFEC PER 757 NDT 6-51-00-19 AND 6-51-00-16, NO INDICATIONS NOT ED. FABRICATED A NEW SKIN, DOUBLERS, TRIPLERS, FILLERS, AND STRUCTURAL FILLERS PER TIMCO REO-G12490 REV A AND UAL EVA 7 2120. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 EU 2008 11 24 UALA2008111706542 1 20081116 A 3260 WARNING SYSTEM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE COCKPIT ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 409UA 462 GEAR NOT UPLOCKED DISPLAYED ON UPPER ECAM SCREEN - L-G. 2 L 7 2 4F 4 F RT A28NM E40NE 20081124 2008 11 24 UALA2008111806543 4 20081117 A 3417 ADC BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE E&E BAY FAILED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 663UA 27160 ADC FAILURE. RTFL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 EA 2008 11 24 COMA0860423 1 20081019 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA FS 625 S14L CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 809CA 21560 7366 CRACKED CLIP AT FS 625 STR 14 LT SIDE AFT EQUIPMENT COMPARTMENT. REPLACED CLIP IAW REO 601R-53-61-100 AND SR 99-5140-00 01. 2 L 7 2 4F RT A21EA 20081124 NM 2008 11 24 UALA2008111806549 1 20081118 A 2432 BATTERY BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE MAIN READS LOW A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION IN INSP/MAINT 1 WP 29 664UA 29236 EICAS MSG MAIN BATTERY CHARGER. 2 L 7 2 4F 4 F RT A1NM E24NE 20081219 2008 12 19 SWAA087171 4 20081216 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 16Y CHECK, FOUND R2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087214 1 20081216 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST UK UNKNOWN 1 SW 29 491WN 33867 FWD EEPLS LIGHT INOP AT ROW 2. REMOVED AND REPLACED EEPLS PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087222 1 20081216 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 784SW 29810 EEPLS LIGHT STRIP LOOSE AT ROW 8. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 QXEA2008121601246 1 20081214 A 5230 502213 SEAL BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR FAILED A QXEA O OTHER O OTHER NR NOT REPORTED 1 NM 19 401QX 4031 UNABLE TO PRESSURIZE. SAME RESULT IN MANUAL MODE; SAME RESULT W/ALL ITEMS IN EIA CHECKLIST; F/A REPORTS LOUD AIR NOISE FROM AFT PAX DOOR; NO "FAULT" ON PRESS CONTROLLER. REMOVED AND REPLACED AFT CARGO DOOR SEAL IAW AMM TASK 52-31-26-000-8 01 AND TASK 52-31-26-400-801. FUNCTIONAL CHECK GOOD. PRESSURIZATION TEST PER AMM TASK 21-00-00-863-801. PRESSURIZATIO N CHECKED GOOD. NO DEFECTS NOTED. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081219 2008 12 19 HALA2008121400891 4 20081214 A 3497 CONNECTOR BOEING 767 76733A 1385209 NM STDBY ATTITUDE LOOSE A HALA O OTHER O OTHER CL CLIMB 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM, STANDBY ALTIMETER HANGS UP PASSING ZERO ON CLIMB/DESCENT THEN JUMPS 300-500 FT. STANDBY ALTIM ETER TESTS GOOD PER AMM 34-13-06. CLEANED AND RE-SEATED CONNECTOR. VIBRATOR OPS CK GOOD. 2 L 7 2 4F RT A1NM 20081219 NM 2008 12 19 SWAA087232 1 20081217 A 2560 65C16820 FASTENER BOEING 737 7373L9 1384470 NM GIRT BAR HOOK LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND L1 DOOR ESCAPE SLIDE FWD LOWER GIRT BAR HOOK LOOSE. REMOVED AND REPLACED FASTENER PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087233 1 20081217 A 2560 65C16820 FASTENER BOEING 737 7373L9 1384470 NM GIRT BAR HOOK LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR ESCAPE SLIDE FWD LOWER GIRT BAR HOOK LOOSE. REMOVED AND REPLACED FASTENER PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087183 1 20081216 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087146 1 20081216 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED AT R2 DOOR BETWEEN BS 996 TO BS 947. REMOVED AND REPLACED BEAM P ER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087217 1 20081217 A 5753 6546434301 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED HC1 CHECK, FOUND LT WING AFT I/B FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 UALA2008121506881 1 20081213 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 554UA 26644 AFT PIT FRAME DENTED BS 1420 AND STR 26L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DO UBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081219 NM 2008 12 19 UALA2008121506889 1 20081212 A 3020 21SN415A600U SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENG TAI PRESS FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 644UA 25094 RIGHT ENG TAI PROBLEM. REPLACED RT ENG TAI PRESSURE SWITCH S525. RAN ENGINE AND OPS CHECK NORMAL. REACTIVATED SYSTEM. 2 L 7 2 4F 4 F RT A1NM E24NE 20081121 NM 2008 11 21 SWAA086292 1 20081118 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 4R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086296 1 20081118 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086297 1 20081118 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086298 1 20081118 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086314 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 2R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086315 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086316 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 6R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086317 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 5R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086286 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 328, STR 21L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 SWAA086287 1 20081118 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 DL764081504 1 20081106 A 2730 162900100 COMPUTER BOEING 767 767432ER 1385134 NM ELEVATOR FEEL MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 837MH 24 29710 P1191* ELEV FEEL EICAS MSG 1 HOUR INTO CRUISE. RETURNED TO ATL. FOUND FLUID IN DRAIN LINES. REPLACED THE ELEV FEEL COMPUTER PER AMM. 2 L 7 2 4F RT A1NM 20081121 NM 2008 11 21 DL76L081505 1 20081107 A 8010 774860A4 STARTER BOEING 767 767332 1382001 NM LEFT FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 191DN 28448 AFTER PUSH NR N2 RISE ON ENGINE START. REPLACED NR 1 ENG STARTER PER AMM 80-11-01. SERVICED OIL. CRANKED ENG AND LEAK CHECK PERFORMED OPS CK NORMAL. STARTER MFG 774860A4 S/N 960225. 2 L 7 2 4F RT A1NM 20081121 NM 2008 11 21 DL757081507 1 20081105 A 5320 146N54511 INTERCOSTAL BOEING 757 757232 1384965 NM BS 1520 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 P1191* INTERCOSTAL AT STATION 1520 LBL 11 CORRODED. REPAIRED PER 53-00-04 ON ATS NR 00101 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081508 1 20081107 A 5347 146N54584 CARGO TRACK BOEING 757 757232 1384965 NM BS 1460 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 P1191* AFT TIE DOWN FITTING CORRODED AT STATION 1460 RBL 14. REPAIRED PER 51-40-02 ON NR 00049. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081510 1 20081107 A 5321 146N539151 FLOOR PANEL BOEING 757 757232 1384965 NM BS 1510-1540 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 AFT CARGO FIXED FLOOR PANEL CORRODED AT 1510 TO 1540 RBL 17. REPAIRED PER ERA 47249-14 REV ORIGINAL ON NR 00033. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081511 1 20081107 A 5322 140N20021024 SHEAR TIE BOEING 757 757232 1384965 NM BS 1701 S29R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 CORROSION AT SHEAR TIE STATION 1701 STRINGER 29R. REPAIRED BY REPLACEMENT PER 51-40-02 ON NR 00112. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081516 1 20081107 A 5320 146N54507 WEB BOEING 757 757232 1384965 NM BS 1520 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 652DL 24392 AFT CARGO WEB CORRODED AT 1520 LBL 3.5. REPAIRED ON NR 00040 PER 53-20-02. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081518 1 20081108 A 5330 146N3531 SKIN BOEING 757 757232 1384965 NM BS 1510 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 652DL 24392 SKIN CORROSION UNDER RT AIR PHONE ATTENNA AT BS ANTENNA BS 1510 RBL 10. REPAIRED ON NR 00067 PER 530001. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 UALA2008111304333 1 20080818 A 3020 8106012 ANTI-ICE VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE LT ENGINE FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 204UA 28713 ANTI ICE VALVE FAILURE. FOUND 1FT OF AIR LINE MISSING ABOVE LEFT ENGINE ANTI-ICE VALVE. REPLACED MISSING LINE. REPLAC ED EAI VLV. OP CHECKS GOOD, NO MESSAGES NOTED. REPLACED EAI VLV CONTROLLER. OPS CHECK GOOD WITH NO MESSAGES NOTED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081121 NE 2008 11 21 IXXA080032O 2 20081105 A 7261 OIL SYSTEM DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE LEAKING A IXXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 11 799AL 58677 6769 45922 671365 DURING CRUISE, NR 4 ENGINE OIL PRESSURE WAS FLUCTUATING & OIL PRESSURE LIGHT FLICKERING, OIL QUANTITY READ 0. CREW RAN ABNORMAL OIL PRESSURE CHECKLIST FOLLOWED BY EMERGENCY SHUTDOWN CHECKLIST. WINDMILL OIL PRESSURE 14 PSI. RESTORED FUEL TO FUEL CONTROL EVERY HOUR. MX REPLACED GEARBOX RELIEF VALVE & INSPECTED NR 4 ENGINE INLET & EXHAUST FOR OIL WETTING, N ONE FOUND. INSPECTED OIL TANK FOR SERVICE LEVEL, REQUIRED 16 QTS. INSPECTED LUBE SYS FOR LEAKS & FOUND ONLY MINOR SEEP S, RETORQUED FITTINGS. RAN ENGINE AT IDLE FOR 40 MIN TO LEAK CHECK FUEL/OIL COOLER, NONE NOTED. PERFORMED 10 MIN POWER RUN UP TO INCLUDE TAKEOFF POWER NO LEAKS. OIL TANK REMAINED FULL, INSPECTED MAIN OIL FILTER, FILTER CLEAN REINSTALLED F 2 L 7 4 4F 4 F 4A25 1E8 20081121 EU 2008 11 21 MALA080195 1 20081112 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 294-326 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 427XJ 340B427 REPLACED SECTION OF RT INBD AISLE SEAT TRACK 31 5/8 LONG BEGINNING AT STA 294 TO STA 326 DUE TO CORROSION. REPAIRED IAW EO NR S53060. 2 L 7 2 4T RT A52EU 20081121 NM 2008 11 21 DHLA2008745681 1 20081111 A 5313 STRINGER BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 FUSELAGE CABIN STR 14R HAS ELONGATED FASTENER HOLES FROM BS 950A TO 950C. ACCOMPLISHED STR 14R SPLICE REPAIR PER EO COO -2-53-369-08 DATED 10/16/2008. REFERENCE FAA FORM 8110-3 DATED 11/6/2008 AND EVA B253-00150 FOR REPAIR APPROVAL. DOCUM ENTED ON N/R 2-476. 2 L 7 3 4F A3WE 20081121 NM 2008 11 21 DHLA2008745682 1 20081111 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 FUSE FRAME AT BS 1090 HAS DOUBLE DRILLED HOLE OVER STR 8R. ACCOMPLISHED FRAME REPAIR BETWEEN STR 7R AND 9R PER EO COO-2 -53-379-08 DATED 10/24/2008. REF FAA FORM 8110-3 DATED 11/6/2008 AND EVA B253-00162 FOR REPAIR APPROVAL. DOCUMENTED ON N/R 2-53. 2 L 7 3 4F A3WE 20081121 WP 2008 11 21 AALA200810109 1 20081029 A 3350 BAT5014 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 461AA 49566 EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 20081121 NM 2008 11 21 UALA2008111305565 1 20080902 A 3350 767 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 675UA 29243 DOOR 2L EXTERIOR EMERGENCY LIGHT INOP. FOUND LIGHT INOPERATIVE. REPLACED LAMP. OK CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081121 WP 2008 11 21 AALA200810110 1 20081029 A 3350 BAT5014 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 461AA 49566 EMERGENCY LIGHT BATTERY PACK WEAK. REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 20081121 NM 2008 11 21 08FDEA04932 1 20081119 A 5330 6554583125 SKIN BOEING 727 727225 1384077 NM ZONE 100 MISREPAIRED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 21 469FE 21581 ON SKIN, IMPROPER FASTENERS USED ON REPAIR AT STA 1183 STR 21L TO 22L. REMOVED PREVIOUS REPAIR DOUBLER, FABRICATED NEW DOUBLER AND INSTALLED REPAIR PARTS IAW SRM 53-30-3 AND 51-40-2. 2 L 7 3 4F A3WE 20081121 WP 2008 11 21 IXXA08SMN156S 1 20080418 A 5740 FITTING DOUG DC8 DC871F 302199D WP ZONE 500 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND LT WING TRAILING EDGE FITTING CRACKED BETWEEN STATION XRS 337.000 TO XRS 351.00 0. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. CLEA NED, TREATED AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATION NUMBER 2 003-05, ED-SEMAN 4785, DACO DPS 4.707, DC8 SRM 51-1-8B, AND DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 20081121 WP 2008 11 21 AALA200810014 1 20081012 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 CORROSION ON RIGHT CUSP AT STATION 1155 TO 1174. CORROSION REMOVED AND DOUBLER INSTALLED PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081121 WP 2008 11 21 AALA200810015 1 20081011 A 5330 SKIN DOUG DC9 DC982 3022082 WP ZONE 100 SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 SCRATCHES IN SKIN AFT OF AFT CARGO DOOR MEASURING 8 INCHS BY 1.25 INCHES. INSTALLED EXTERNAL FUSELAGE DOUBLER AND FILLE R PER SRM 53-05, FIG 80. 2 L 7 2 4F A6WE 20081121 NM 2008 11 21 DL757081545 1 20081008 A 5720 PANEL BOEING 757 757232 1384965 NM RT INBD FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 RT INBD FLAP L/E PANEL IS CRACKED JUST INBD OF TRUNNION. REPAIRED PANEL IAW SRM 57-53-01. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL76L081565 1 20081117 A 2797 CONNECTOR BOEING 767 767332 1382001 NM GE CF6 CF680C2B6F 30025 NE TRIM MODULE LOOSE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 176DN 25061 704749 RTB - ON TAXI OUT RUDDER TRIM INOP. NO MEL RELIEF, MTC RESEATED CONNECTOR ON RUDDER TRIM MODULE SYSTEM. OPS CK OK. 2 L 7 2 4F 4 F RT A1NM E13NE 20081121 NM 2008 11 21 DL757081566 1 20081114 A 3520 PANEL BOEING 757 757232 1384965 NM OXYGEN SYSTEM INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 OXYGEN DOORS AT ROWS 21 DEF, 26 DEF AND 28 ABC DO NOT DROP WHEN FUNCTIONAL CHECK IS PERFORMED. SOLENOIDS DO DISENGAGE. CLEANED AND ADJUSTED DOOR LATCH ACTUATOR ON 21 DEF, 26 DEF AND 28 ABC IAW AMM 35-21-06-404-007. OPS CHECK GOOD IAW AMM 35-21-00-705-0766. 2 L 7 2 4F RT A2NM 20081121 WP 2008 11 21 AALA200810120 1 20081023 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 PUNCTURED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 HOLE PUNCTURED IN LEFT CUSP AT STATION 1183. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081121 EU 2008 11 21 NWAA084483216 1 20081007 A 3350 EPSU AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 316US 5698 192 EMERGENCY EGRESS PATH LIGHTING INOP BETWEEN ROWS 1 AND 8. REPLACED EPSU 10WL, CHECKS OK. 2 L 7 2 4F RT A28NM 20081121 NM 2008 11 21 USAA920081918 1 20081008 A 5320 65528941 FLOOR SUPPORT BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT MAJOR REPAIR Q5 CHECK NR 03C10753038/003. CRACKED FLOOR SUPPORT AT BS540, LBL2. REPLACED FLOOR SUPPORT AT BS540, L BL2 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 USAA920081924 1 20081002 A 3397 W15006722 WIRE BOEING 737 7373G7 138447J NM CABIN SHORTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 308AW 24710 SAL C17 EEL NR 6097753 EMERGENCY EXIT LIGHT AT SEAT NR 21 LT DOES NOT WORK PROPERLY. REPAIRED WIRING ON ELECTRICAL BUND LE W150-067-22 IAW SWPM 20-10-13 AND WDM 33-51-21. 2 L 7 2 4F RT A16WE 20081120 EU 2008 11 20 08FDEA04905 1 20081118 A 2720 353152003 CONTROL UNIT AIRBUS 310 A310324 3930206 EU RUDDER INOPERATIVE A FDEA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 21 812FD 467 2ND REJECTED TAKEOFF DUE TO BLUE RUDDER SERVO CTL JAM, ECAM WARNING CAME ON AT 40-50 PERCENT N1. NO FAULT FOUND ON 1ST RTO, RAN ENG AND CHECKED ALL FLT CONTROL OPERATION (WRI 27-20/2731). REPLACED JAMMING DETECTION CONTROL UNIT PER AMM 27 -14-17-4 PRE CAUTIONARY REMOVED AND REPLACED BLUE SYSTEM RUDDER SERVO JAM DETECTION SWITCH, 22CB, PER AMM 27-24-12-4. OP S CHECKS GOOD. REMOVED & REPLACED BLUE SYSTEM RUDDER ACTUATOR IAW AMM 27-24-11-4. 2 L 7 2 4F RT A35EU 20081120 EU 2008 11 20 08FDEA04906 1 20081118 A 5753 A57960418203 SKIN AIRBUS 300 A300F4605R 3930327 EU RT WING TE FLAP DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 654FE 738 RT WING CENTER FLAP T/E HAS DAMAGE REMOVED DAMAGED SKIN IAW SRM 57-50-00 FIG 206. PERFORMED HFEC IAW NTM 51-10-08 PT6, NO CRACK INDICATION NOTED. FABRICATED REPAIR DOUBLER IAW SRM 57-50-00 FIG 206. TREATED REPAIR PARTS IAW SRM 51-21-10. PRIMED REPAIR PARTS IAW SRM 51-21-10. INSTALLED REPAIR PARTS IAW SRM 57-50-00 FIG 206. RESTORED TOP COAT IAW SRM 51-5 7-10. ACCOMPLISHED FLAP ATTACHMENTS INSPECTION, NO DEFECTS NOTED. 2 L 7 2 4F RT A35EU 20081120 EU 2008 11 20 F3LA2008111900718 1 20081118 A 5340 D5311247400000 FITTING AIRBUS A318 A318111 3940019 EU GIRT BAR OUT OF ADJUST A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 801FR 1939 DURING C4 C-CHECK, INSPECTION NOTED THE R2 DOOR ARMED HANDLE WAS SPONGY WHEN IN THE ARMED POSITION. MAINTENANCE ADJUSTE D THE R2 GIRT BAR FITTING AND PERFORMED OPERATION CHECK IN ACCORDANCE WITH A318 AMM 52-13-00-820-001. 2 L 7 2 4F RT 20081120 WP 2008 11 20 DHLA200800128 1 20081118 A 2121 50075381 FAN DOUG DC8 DC873 302199C WP CABIN BURNED A DHLA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 05 806DH 2707 46002 SMOKE IN CABIN AFT OF CABIN AFTER LANDING. REMOVED AND REPLACED CABIN AIR RECIRC FAN INSTALLED CABIN FAN TRANSFERED TO DMI LOG PER MEL21-16, PLACARD INSTALLED. A/C WAS GROUNDED. 2 L 7 4 4F RT 4A25 20081120 2008 11 20 DLM8K081492 2 20081105 A 7200 ENGINE DOUG MD88 MD88 3023688 NM NR 1 ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 915DE 53420 IMMEDIATELY UPON ROTATION, ALL F/A STATION AND COCKPIT SMELLED A VERY ACRID, HEAVY ODOR. APU WAS OFF A/C FLIGHT RETURNE D TO LAND THERE WAS NO SMOKE PRESENT. MTC IN PROGRESS. FOUND LT ENGINE AS SOURCE OF ODOR. REMOVED AND REPLACED NR 1 P ER TRANSMITTAL. CHECKS GOOD OK FOR SERVICE. RUN UP CK ALL GOOD. 2 L 7 2 4F RT A6WE 20081120 NM 2008 11 20 USAA920081926 1 20081010 A 5314 SUPPORT BOEING 767 767201 1385125 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245AY 23897 BFM C3 MAJOR REPAIR NR 6113987 KEEL BEAM PANEL SUPPORT CORRODED AT BS 900, WL 108, BLO. REPLACED KEEL BEAM PANEL SUPPOR T AT BS 900, WL 108, BLO IAW B767 SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081120 NM 2008 11 20 USAA920081939 1 20081022 A 5311 6546554 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753039/006 FRAME CRACKED AT BS847 BETWEEN S8L AND S9L. REPAIRED FRAME AT BS847 BETWEEN S8L AND S9L IAW US AIRWAYS TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 20081120 EU 2008 11 20 USAA920081929 1 20080929 A 3213 D3215303000200 PIN AIRBUS 320 A320231 3930325 EU RT MLG CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C7 MAJOR REPAIR NR 6109431 CORROSION ON REAR PINTLE PIN OF RT MLG. REPLACED REAR PINTLE PIN OF RT MLG IAW AMERICA W EST AIRLINES TASK CARD R4M32304. 2 L 7 2 4F RT A28NM 20081120 EU 2008 11 20 USAA920081927 1 20081021 A 3350 32145410 POWER SUPPLY AIRBUS A321 A321211 3930370 EU CABIN NO TEST A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 165US 27755 3609 1431 LOG PAGE 4284226 FLT NR 1753 CLT TPA EEL WHILE ACCOMPLISHING JC 26C00033004, FORWARD EMERGENCY POWER SUPPLY UNIT WOULD N OT TEST. MX R&R THE FORWARD EMERGENCY POWER SUPPLY UNIT 10WL PER AIRBUS MX MANUAL 33-51-38-04. OPS TEST GOOD. 2 L 7 2 4F RT A28NM 20081120 NM 2008 11 20 DL757081496 1 20081105 A 5315 146N54461 FLOORBEAM BOEING 757 757232 1384965 NM BS 1510 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 652DL 24392 FLOOR SUPPORT CORRODED AT 1510 LBL 12. REPAIRED ON NR 00030 PER 53-60-53. 2 L 7 2 4F RT A2NM 20081120 NM 2008 11 20 DL757081497 1 20081105 A 5315 146N54443 FLOORBEAM BOEING 757 757232 1384965 NM BS 1510 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 652DL 24392 AFT CARGO FLOOR SUPPORT CORRODED AT 1510 LBL 7. REPAIRED ON NR 00031 PER 53-60-53. 2 L 7 2 4F RT A2NM 20081222 NM 2008 12 22 USAA2008121692242 1 20081208 A 5754 65C26601196 SKIN BOEING 737 7374B7 138449C NM LE SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - NR 6 SLAT SKIN TRAILING EDGE DELAMINATED ON LOWER OUTBOARD SIDE. REPAIRED NR 6 SLAT SKIN TRAI LING EDGE IAW B737 SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081222 EA 2008 12 22 A6WA200840623 1 20081204 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 413AW 7585 MWC 6 FS 621 PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING IS CRACKED APPROX 1" LONG. PERFORMED A REPAIR BY CUTTING OUT SECTION OF WEB, FABRICATING AND INSTALLING REPAIR PARTS IAW BOMBARDIER, INC REO 601R-53-61-1230 RE V D. 2 L 7 2 4F RT A21EA 20081222 WP 2008 12 22 UPS08854157 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-100 AT STA 1521 L27L HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER, FABRI CATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 10. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854158 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-99 AT STA 1529 L23L HAS NO SRM REF. REMOVED FLUSH REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER AND FILLER IAW UPS EO DC8-5330-31419-A AND FVCI DWG 53-08540-17. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854129 1 20081110 A 5730 5769467 SKIN DOUG DC8 DC871F 302199D WP LT WING MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:SV LT WING OUTBOARD L/E HAS A REPAIR DOUBLER INSTALLED THAT DOES NOT MEET SRM SURVEY SEQ 729-W3-10 XFS 7 01. REPAIRED IAW DC8 SRM 57-2-1 FIG 2H SHT 1 REV 78. 2 L 7 4 4F RT 4A25 20081222 EU 2008 12 22 UPS08154191 1 20081212 A 3350 321431 LIGHT AIRBUS A300 A300F4622R 3930360 EU CABIN MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 130UP 0814 INSPECTION TYPE:N/A EMERGENCY LAMPS COME ON IN THE DISARM POSITION. RESEATED C/O ON THE PSU, OPS CHECK GOOD PER MM 33-5 1-14-04. REMOVED AND REPLACED BATTERY PRECAUTIONARY. 2 L 7 2 4F RT A35EU 20081222 WP 2008 12 22 UPS08854175 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-59 AT STA 1294-1305 L14-17L HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND IN STALLED REPAIR DOUBLER IAW DC-8 SRM 53-02-00 FIG 22A. 2 L 7 4 4F RT 4A25 20081222 NM 2008 12 22 SWAA087248 1 20081218 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 SWAA087251 1 20081218 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 463WN 32467 DURING SCHEDULED HC1 CHECK, FOUND RT EEPLS LIGHT COVER CRACKED. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 SWAA087256 1 20081218 A 5311 6546593 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500A, LBL 17. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 SWAA087257 1 20081218 A 5330 6552988 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED HC2 CHECK, FOUND SKIN CRACKED AT L2 DOOR, FWD LOWER CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 SWAA087258 1 20081218 A 5754 65C2660298 SLAT BOEING 737 7373A4 1384585 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 669SW 23752 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT O/B END DELAMINATED. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 SWAA087241 1 20081218 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081222 EA 2008 12 22 COMA2008121750033 1 20081212 A 5346 601350061 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 785CA 23029 7326 ENGINE CENTER SUPPORT BEAM IS CRACKED AT RBL 8.5 AT SENSING LOOP SUPPORT BRACKET. REPAIRED ENGINE SUPPORT BEAM PER CRJ REO 601R-53-61345 REV F. 2 L 7 2 4F RT A21EA 20081222 EA 2008 12 22 COMA2008121750034 1 20081216 A 3010 355483255 SENSING ELEMENT CNDAIR CL600 CL6002B19 1900309 EA ZONE 100 FAILED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 807CA 7364 ON CLIMBOUT FROM BOS RECEIVED ANTI-ICE DUCT WARNING MSG, (LEFT FUSELAGE) WITH ANTI-ICE SYSTEM OFF. EMERGENCY DECLARED, A/C RETURNED TO BOS LANDED SAFELY. REMOVED AND REPLACED LEFT MLG SENSING ELEMENT (A41WK). 2 L 7 2 4F RT A21EA 20081222 SO 2008 12 22 FDKA2008121800317 1 20081218 A 5210 DOOR EMB 145 EMB145LR 3260212 SO PAX DOOR LACK OF LUBE A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 852MJ 145567 FRL FLT 6271 CVG-IND. MAIN CABIN DOOR HARD TO OPEN. MX CLEANED AND LUBED THE DOOR. 2 L 7 2 4T RT T00011AT 20081120 NM 2008 11 20 DL738081498 1 20081105 A 2750 18173810 TRANSMITTER BOEING 737 737832 13844CF NM RT WING TE FLAP MALFUNCTIONED A DALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 27 3741S 30487 ON APPROACH WHEN FLAPS MOVED FROM 1 TO 5 FLAPS STUCK AT APPROX 2 DEG, PER QRH FLAPS MOVED TO 15 BY ALT FLAPS SWITCH, WOR KED OK. INSTALLED NEW RT POS FLAP TRANSMITTER PER MM. PERFORMED MANUAL EXTENSION PER MM TO ACHIEVE FINE RIG MARK ON BO TH WINGS. PERFORMED REPAIR CONFIRMATION PER FIM 27-51-00-801-820. NO FAULTS NOTED. 2 L 7 2 4F RT A16WE 20081120 NM 2008 11 20 DL76L081499 1 20081105 A 2150 A/C PACK BOEING 767 767332 1382001 NM LEFT INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 175DN 24803 L PACK TEMP EICAS MESSAGE WITH LEFT PACK INOP LIGHT RESET PER QRH WITH SAME RESULT. NO AUTO EVEN GENERATED. BITE PACK CONTROLLER NO FAULTS OPENED PACK BAY AND INSPECTED AREA FOR DUCT LEAKS WHILE OPERATING PACK. PACKS OPERATE NORMAL COULD NOT REPRODUCE PROBLEM NO HISTORY. 2 L 7 2 4F RT A1NM 20081120 NM 2008 11 20 DL757081500 1 20081105 A 5340 231107002 PLATE BOEING 757 757232 1384965 NM BS 1510 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 652DL 24392 AFT CARGO BAY STATION 1510 LBL 10 ATENNA MOUNT PLATE CORRODED. REPAIRED PER 53-00-01 -201 ON NR 00038. 2 L 7 2 4F RT A2NM 20081121 WP 2008 11 21 AALA200810148 1 20081024 A 5311 FRAME DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 CRACK IN 905 FRAME AT LONGERON 18L. INSTALLED NEW FRAME AT STATION 905 PER ADK 3290AC. 2 L 7 2 4F A6WE 20081121 NM 2008 11 21 DL757081576 1 20081011 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 365.25 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 MAIN CABIN FLOORBEAM CAP 4 INCHES AFT STA 365.25 RBL 54 CORRODED. REPLACED DAMAGED FLOORBEAM CAP AT STA 365.25 TO 395 R BL 54 IAW SRM 51-40-02 FIG 8 PG 31 AND SRM 51-40-02 PG 7 PARA 7D. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081577 1 20081011 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 365.25 RBL18 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 MAIN CABIN FLOORBEAM STA 365.25 RBL 18 CORRODED. REMOVED DAMAGED FLOOR BEAM IAW SRM 51-40-02 FIG 8 PG 31. REINSTALLED REPAIR PIECE IAW SRM 51-40-05 PG 4 PARA 4. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 DL757081535 1 20081112 A 5311 146N103072 FRAME BOEING 757 757232 1384965 NM BS 1540 LBL5 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 AFT CARGO BAY FRAME CORRODED AT STA 1540 LBL 5. REPAIRED PER ERA 471250-14REV ORG ON NRC 00043. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 UALA2008111305591 1 20080904 A 3350 80541 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA O OTHER L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 AFT MAIN GALLEY WALL EMERGENCY LIGHT FWD OF GALLEY AND LT SIDE INOP. REPLACED TWO LIGHTS & TWO FEEDERS. OP CHECKS NORM AL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081121 NM 2008 11 21 UALA2008111305783 1 20080918 A 4920 SEAL BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE APU DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 675UA 60259 29243 APU OIL CONSUMPTION ABOVE LIMIT. APU IS INADEQUATE. FOUND GEARBOX, DRIVEN COMPRESSOR LEAKING AT GEARBOX TO COMPRESSOR MATING SURFACE. SUSPECT SEAL NEEDS REPLACEMENT. NO OTHER LEAKS NOTED. REPLACED APU. 2 L 7 2 4F 4 F RT A1NM E24NE 20081121 WP 2008 11 21 AALA200810121 1 20081023 A 5320 BRACKET DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 AFT CARGO AREA, T BRACKET AT STATION 1155 IS CORRODED. INSTALLED NEW T BRACKET PER SRM 51-10-01. 2 L 7 2 4F A6WE 20081121 NM 2008 11 21 AALA200810158 1 20081027 A 5320 WEB BOEING 737 737823 13844BZ NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 CORROSION ON WEB AT STATION 990. AREA REPAIRED PER SRM 51-70-13-2. 2 L 7 2 4F RT A16WE 20081121 WP 2008 11 21 AALA200810122 1 20081023 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 UNDERSIDE OF RIGHT CUSP CORRODED AT STA 544 - 548. INSTALLED DOUBLER PER AARD 53-20-00-3. 2 L 7 2 4F A6WE 20081121 WP 2008 11 21 AALA200810017 1 20081012 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP BS 1250-1309 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 BOTTOM OF CUSP CORRODED AT STATION 1308 TO 1309 LONGERON 18 RIGHT. CUSP SHEET REPLACED FROM STATION 1250 TO 1309 PER AA RD 53-20-00-16. 2 L 7 2 4F A6WE 20081121 NM 2008 11 21 USAA920081937 1 20081020 A 5311 6546551 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753039/010 FRAME CRACKED AT BS807 JUST ABOVE S9R. REPAIRED FRAME AT BS807 JUST ABOVE S9R IAW US AIRWAYS TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 20081121 NM 2008 11 21 USAA920081942 1 20081016 A 5311 6546526 FRAME BOEING 737 737301 1384611 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753039/002 FRAME CRACKED AT BS400 JUST ABOVE S9L. REPAIRED FRAME AT BS400 JUST ABOVE S9L IA W US AIRWAYS TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 20081121 EU 2008 11 21 USAA920081911 1 20080927 A 5320 D5347048500200 WEB AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C7 MAJOR REPAIR NR 6062290 CORROSION ON WEB BETWEEN FR56 AND FR57 AT S38R AFT CARGO COMPARTMENT. REPLACED WEB BETWE EN FR56 AND FR57 AT S38R AFT CARGO COMPARTMENT IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081121 WP 2008 11 21 NWAA084769881 1 20081025 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 676MC 47652 DURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE O R TOO DIM TO BE FUNCTIONAL. MX CHARGED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OP CONDITION. 2 L 7 2 4F RT A6WE 20081121 WP 2008 11 21 NWAA084759941 1 20081025 A 3350 SIGN DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3324L 47103 DURING LINE CHECK THE LT AFT OVERWING EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSEMBLY A ND FUNCTIONALLY CHECKED IT. 2 L 7 2 4F A6WE 20081121 NM 2008 11 21 NWAA084725649 1 20081025 A 3350 BATTERY PACK BOEING 757 757251 1384970 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 549US 26496 DURING AN OVERNIGHT LINE CHECK THE EMERGENCY ESCAPE PATH LIGHTS AT ROWS 4AB THROUGH 6AB WERE INOPERATIVE. MX FOUND THE ASSOCIATED BATTERY PACK TO BE DEFECTIVE, THE BATTERY PACK WAS REPLACED AND OPS WERE NORMAL AFTER THE BATTERY PACK WAS RE PLACED. 2 L 7 2 4F RT A2NM 20081121 NM 2008 11 21 NWAA084736308 1 20081026 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 668US 24223 DURING OVERNIGHT CHECK FOUND OVER WING EMERGENCY LIGHTS LT SIDE, AFT LIGHT INOP. MX R&R POWER SUPPLY. OPS CHECKED GOOD , AND ACFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20081124 WP 2008 11 24 AALA200810136 1 20081026 A 5310 BEAM DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 MID CARGO DOOR BEAM CORRODED FROM 636 TO 693. INSTALLED DOUBLER PER AARD 53-10-00-3. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810128 1 20081024 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 INTERCOSTAL IN AFT CARGO CRACKED AT CEILING AREA STATION 1271-1287. INSTALLED NEW INTERCOSTAL PER SRM 51-10-1. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810174 1 20081110 A 5322 SHEAR TIE DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70529 49921 SHEAR TIE CRACKED AFT SIDE AT 1451 LONGERON 2R. REPLACED SHEAR TIE. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 AALA200810163 1 20081029 A 5320 WEB BOEING 737 737823 13844BZ NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 CORROSION ON FLOOR WEB. INSTALLED DOUBLER PER SRM 51-70-13. 2 L 7 2 4F RT A16WE 20081124 WP 2008 11 24 AALA200810116 1 20081027 A 3220 GUIDE DOUG DC9 DC982 3022082 WP ZONE 700 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7530 49922 DURING ECO3332AB A CHECK, CRACK WAS FOUND ON THE NOSE LANDING GEAR WHEEL WELL RIGHT DEFLECTOR STOP GUIDE WHEN REMOVED. A STAINLESS STEEL REPAIR WAS ACCOMPLISHED AND LOCK FASTENERS INSTALLED PER ECO AND SRM AND PER FMR NR 53053 E 4B3. FABR ICATED DOUBLER FROM CDK2670-1 SIZE AS REQUIRED TO HAVE A SINGLE ROW FASTENERS AROUND TRIMMED OUT, PER ESO80559 DATED 27O CT 08. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810129 1 20081028 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 CORROSION ON LOWER SIDE OF LEFT CUSP STATION 427-503. REMOVED DAMAGED CUSP AND INSTALLED NEW CUSP SHEET PER SRM 51-10-0 1. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 AALA200810165 1 20081029 A 5315 FLOORBEAM BOEING 737 737823 13844BZ NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 CORROSION ON FLOOR FRAME. INSTALLED FILLER STRAP AND ANGLES 1 AND 2. 2 L 7 2 4F RT A16WE 20081124 WP 2008 11 24 AALA200810130 1 20081028 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 CORROSION AT ATTACH BOLTS, AFT CARGO, LEFT TIEDOWN TRACK AT STATION 1220 TO 1322. INSTALLED NEW TIEDOWN TRACK FROM STAT ION 1220 TO 1322. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810131 1 20081028 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 AFT CARGO RIGHT TIEDOWN TRACK CORRODED AT MOUNT HOLES STATION 1211-1322. INSTALLED NEW TIEDOWN TRACK FROM 1211 TO 1322. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 AALA200810167 1 20081029 A 5315 FLOORBEAM BOEING 737 737823 13844BZ NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 CORROSION ON FLOOR FRAME. INSTALLED FILLER STRAP AND ANGLES PER SRM 53-00-51. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 AALA200820010 1 20081009 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 672AA 52528 25337 AFT MAIN DECK IS CORRODED. DOUBLER INSTALLED IAW SRM 53-60-51-2R2. 2 L 7 2 4F RT A2NM 20081124 WP 2008 11 24 AALA200810173 1 20081108 A 5313 LONGERON DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 587AA 53250 CRACK IN LONGERON RADIUS IN AFT ACCESSORY COMPARTMENT STATION 1418. INSTALLED LONGERON REPAIR SPLICE PER AARD 53-30-00- 2. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810117 1 20081021 A 5340 BRACKET DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 AFT BULKHEAD DOORWAY RIGHT MID DOOR STOP BRACKET CRACKED AT UPPER FASTENER (STA 1338). INSTALLED NEW BRACKET PER SRM 51 -01. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810118 1 20081022 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP ZONE 100 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 GOUGES IN THE BOTTOM OF NR 4 SEAT TRACK PLUG AT STATION 900 - 901. INSTALLED SEAT TRACK PLUG AT STATION 900 - 901 PER A ARD 53-20-00-10. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810150 1 20081104 A 5310 BEAM DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 FWD ENTRY DOOR NUMBER 2 BEAM CRACKED AT FORWARD END. INSTALLED DOUBLER REPAIR PER SRM 52-05-00 FIG 31 AND ESO 80172. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810119 1 20081022 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 CRACK IN LEFT CUSP AT STATION 222. INSTALLED DOUBLER ON CUSP AT STA 222 PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 UALA2008111306462 1 20081109 A 3397 794640 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 EEL LIGHT INOP AT AFT GALLEY LEFT SIDE. REPLACED FEEDER ASSY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 NM 2008 11 24 UALA2008111706520 1 20081114 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY LIGHT ROW 44 LT INOP. FOUND EMERGENCY LIGHT ASSY BROKEN OFF AT SIDE OF SEAT. REPLACED LIGHT ASSY. OPS CHECK GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 EA 2008 11 24 SWIA200820376 1 20080802 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 464SW 7827 C-CHECK, CRACK IN UPPER RADIUS OF INTERCOSTAL UNDER PANEL 832BR, REPLACED. 2 L 7 2 4F RT A21EA 20081124 NM 2008 11 24 AALA200820012 1 20081009 A 5321 146N5318 FLOOR PANEL BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 672AA 52528 25337 AFT MAIN DECK FLOOR STRUCTURE IS CORRODED. REPAIRED IAW SRM 53-60-51-2R2. 2 L 7 2 4F RT A2NM 20081124 NM 2008 11 24 DL757081567 1 20081005 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1720 S30 BULGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 FUSELAGE LOWER SKIN IS BULGING DUE TO HEAVY CORROSION UNDERNEATH SKIN AT STA 1720 STR 30. CUT OUT DAMAGE SKIN IAW SRM 5 3-00-01 FIG 201 DETAIL I REPAIR 3. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-00-01 FIG 201 DETAIL I REPAIR 3. IN STALLED REPAIR DOUBLER, FILLER AND ID TAG IAW SRMS 53-00-01 FIG 201, 51-40-02 FIG 8 PG 31 AND 51-40-02 PG7 PARA 7D. 2 L 7 2 4F RT A2NM 20081124 EU 2008 11 24 DHLA200800130 1 20081115 A 3350 311701 BATTERY PACK AIRBUS 300 A300B42C 3930106 EU EMERGENCY LIGHT FAILED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 362DH 084 LT EMERGENCY LIGHT INOP AT ENTRANCE AREA. TROUBLESHOT LT EMERGENCY LIGHT AND FOUND 3 BATTERIES PACKS DEFECTIVE. REMOVE D AND REPLACED ALL 3 BATTERIES PACKS AND EMERGENCY LIGHT RT AND LT ENTRANCE AREA CHECKED NORMAL IAW A300 AMM 33-51-14, P N OFF 3117-01 S/N'S 013571, 013554, 013558. A/C WAS GROUNDED. 2 L 7 2 4F RT A35EU 20081124 NM 2008 11 24 UALA2008111706525 1 20081114 A 3350 LIGHT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN LOOSE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 327UA 24147 EMERGENCY FLOOR LIGHTS LOOSE NEAR ROW 6 ABC. SECURED EMERGENCY LIGHTS. 2 L 7 2 4F 4 F RT A16WE E21EU 20081124 NM 2008 11 24 UALA2008111706526 1 20081115 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT LIGHT INOP AT ROW 13 CEILING LIGHT. RELAMPED EMERGENCY LIGHT, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111706530 1 20081115 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT LIGHT INOP BY LAV 102 CEILING LIGHT. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111706535 1 20081115 A 2611 PU90471WR1 SMOKE DETECTOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FWD LAVATORY FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 204UA 28713 ALL TEST FAULTED OUTBOARD FWD LAV SMOKE DETECTOR. REPLACED SMOKE DETECTOR. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081124 NM 2008 11 24 UALA2008111706537 1 20081117 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 CEILING EEL LIGHTS INOP ROWS 9 THRU 24 R&L. REPLACED BATTERIES, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111706538 1 20081117 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FALSE ACTIVATION A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 173UA 24380 EXIT LIGHTS AT DOOR 2L AND BY F-C GALLEY FLOOR FLASHING CONSTANTLY. ACCOMPLISHED DATA BASE RELOAD AND NO ACCESS INTO PA NASONIC EQT, GROUND TEST EMERGENCY LIGHT WITH FLIGHT DECK SW, OP CHECK NORMAL ON GROUND. INSTALL DATA BASE AND EMERGENC Y LIGHT OPS CHECKED NORMAL ON GROUND. CONFERRED WITH CABIN CREW & RESET EMERGENCY LIGHT POWER SWITCH, TEST OK. NOT ABL E TO DUPLICATE OR OBSERVE MALFUNCTION. ITEM HAS PRIOR HISTORY, FUNCTIONAL AT THIS TIME. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 EU 2008 11 24 UALA2008111806550 1 20081117 A 5320 PLATE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN CORRODED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 424UA 506 SKID PLATES FOUND FLOOR PANELS DELAMINATED. CORROSION FOUND UNDER FLOOR PANELS. 2 L 7 2 4F 4 F RT A28NM E40NE 20081219 2008 12 19 SWAA087213 4 20081216 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR LOOSE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 469WN 33859 R2 DOOR EMERGENCY EVAC SLIDE LOOSE. RE-INSTALLED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 QXEA2008121601245 1 20081213 A 5320 BLOWOUT PANEL BOMBDR DHC8 DHC8402 1390042 NM LOOSE A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 19 430QX 4163 DEPARTING BLI AT 1500 FT, HEARD A MUFFLED THUMP (AFT FA DESCRIBED A LOUD METALLIC THUMP). ACFT THEN DEPRESSURIZED. CAB IN CLIMB FOLLOWED ACFT CLIMB RATE TO 7000 FT. FINISHED AFTER TAKEOFF FLOW AND WHEN SELECTING BLEED CONTROL FROM MIN TO NORM. THE CABIN STARTED TO RAPIDLY REPRESSURIZE AFTER 2 MINUTES, PRESSURIZATION RATE WAS NORMAL. REMAINED IN LEVEL FL T 7000. PRESSURIZATION WAS NORMAL ON DESCENT TO SEA. ON GROUND IN BLI BEFORE FLIGHT, THE A/C WAS PARKED WITH 40 KNOT D IRECT TAILWIND. FOUND AFT CARGO BAY AFT BLOW OUT PANEL OUT OF POSITION. RESECURED AS NECESSARY PRESSURIZED ACFT (REF A MM TASK NR 21-00-00-863-801) TO 5 DIFF + HELD FOR 5 MIN WITH NO DEFECTS OR LEAKS NOTED. DEPRESSURIZED A/C (REF AMM TASK 2 H 7 2 4T RT A13NM 20081219 NM 2008 12 19 SWAA087237 1 20081217 A 5312 6545402 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD HORIZONTAL FLANGE CRACKED AT BS 663, LBL 6. REPAIRED BULKHEAD PER DWG. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087187 1 20081216 A 5330 6562212 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081124 CE 2008 11 24 DXTA2008111903363 1 20081119 A 3260 WARNING SYSTEM CESSNA 500 560CESSNA 2076750 CE COCKPIT ACTIVATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 367QS 5600367 AT GEAR RETRACTION, THE GREEN LIGHTS WENT OUT BUT THE RED GEAR UNLOCKED LIGHT REMAINED ILLUMINATED. 2 L 7 2 4F RT A22CE 20081124 EU 2008 11 24 J1QA20081019002 1 20081109 A 7700 30707223 MONOPOLE AMD FALC50 FALCON50MYST 2730106 EU GARRTT TFE731 TFE731* 01518 WP ENGINE DEFECTIVE E J1QA E B A ENGINE SHUTDOWN EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 752JC 590 590 028 P77416C AIRCRAFT DEPARTED KEGE, DURING CLIMBOUT AT APPROXIMATELY 11,000FT MSL THE NR 2 ENGINE STARTED SURGING +/- 10% N1 ROTATIO N, FOLLOWED BY A NR 2 ENGINE COMPUTER LIGHT. THE CREW FOLLOWED THE AIRCRAFT CHECKLIST AND RESET THE ENGINE COMPUTER. T HE ENGINE STABILIZED FOR APPROXIMATELY 2-3 MINUTES, THEN THE ENGINE ROLLED BACK AND SHUTDOWN UN-COMMANDED. THE FLIGHT C REW THEN RAN THE AIRCRAFT CHECKLIST FOR AN ENGINE FAILURE AND ENGINE SHUT DOWN PROCEDURES. THE CREW PROCEEDED TO KDEN A ND LANDED UNEVENTFULLY. 2 L 7 3 4F 4 F A46EU E6WE 20081124 NM 2008 11 24 J1QA20081019001 1 20081019 A 2431 11561 SENSOR GULSTM 200 200 4500308 NM PWC PW306 PW306A 52165 NE BATTERY TEMP FAILED E J1QA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 272J 3888 2105 054 AIRCRAFT DEPARTED KPSP, DURING CLIMB OUT AT 14,000 FEET THE AMBER "EMERGENCY BATTERY OVERHEAT" LIGHT CAME ON. CREW CHEC KED THE BATTERY TEMPURATURE AND THE READING WAS 140 DEGREES F AND CLIMBING. THE CREW PER THE CHECKLIST TURNED OFF THE " EMERGENCY BATTERY". THE CREW LEVELED OFF THE AIRCRAFT OFF AT 15,000 FEET AND THE "EMERGENCY BATTERY OVERHEAT" LIGHT TUR NED TO RED. TEMPERATURE OF THE BATTERY WAS 160 DEGREES F AND CLIMBING. CREW CHECKLIST SAYS TO LAND AS SOON AS POSSIBLE THE CREW RETURNED TO KPSP AND LANDED. ON THE GROUND THE "EMERGENCY BATTERY WAS CHECKED AND DETERMINED NOT TO BE NON-EM ERGENCY SITUATION. MAINTENANCE FOUND A FAILED BATTERY TEMPERATURE SENSOR, REPLACED BATTERY TEMPERATURE SENSOR WITH NEW. 2 L 7 2 4F 4 F RT A53NM E35NE 20081124 WP 2008 11 24 AALA200810062 1 20080929 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 469AA 49734 INTERCOSTAL UNDER FLOORBOARD C-18 BETWEEN STATION 1271-1287 CRACKED AT MOUNT HOLES TO FLOORBOARD. INSTALL NEW INTERCOST AL 1271 -1287 STATION PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081124 CE 2008 11 24 DXTA2008111703356 1 20081114 A 2933 WARNING SYSTEM CESSNA 560 560XL 2076702 CE COCKPIT ACTIVATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 698QS 5605653 DURING TAKEOFF AT APPROX 60KTS, THE RIGHT HYD LOW FLOW ANNUNCIATOR ILLUMINATED. 2 L 7 2 4F RT A22CE 20081124 NM 2008 11 24 DXTA2008111703358 1 20081115 A 2751 WARNING SYSTEM AMD FALC50 FALCON2000 2730170 NM COCKPIT ACTIVATED E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 268QS 168 DURING CRUISE AT FL410 THE "FLAP ASYM" MASTER CAUTION LIGHT FLASHED OFF AND ON. 2 L 7 2 4F RT A50NM 20081124 CE 2008 11 24 DXTA2008111703359 1 20081116 A 3220 LANDING GEAR CESSNA 500 560CESSNA 2076750 CE NLG VIBRATION E DXTA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 802QS 5600706 EXPERIENCED VIOLENT NOSE WHEEL SHIMMY DURING TAKEOFF ROLL. ABORTED TAKEOFF. 2 L 7 2 4F RT A22CE 20081124 2008 11 24 DXTA2008111003342 4 20081107 A 2210 YAW DAMPER CESSNA 560 560XL 2076702 CE MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 GL 07 605QS 5605321 FL390 AP/FAIL, ATT FAIL, HDG FAIL COPILOTS SIDE STBY HSI FAIL. YAW DAMP WOULD NOT RE-ENGAGE. 2 L 7 2 4F RT A22CE 20081124 CE 2008 11 24 DXTA2008111003343 1 20081107 A 3240 BRAKE SYS CESSNA 500 560CESSNA 2076750 CE RIGHT MALFUNCTIONED E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 393QS 5600393 AT END OF LANDING ROLL OUT RIGHT SEAT PILOT LOST BRAKE PRESSURE WITH PEDALS PRESSED 3/4 THROW. 2 L 7 2 4F RT A22CE 20081124 2008 11 24 DXTA2008111003345 4 20081108 A 3414 UNKNOWN CESSNA 500 560CESSNA 2076750 CE COCKPIT MALFUNCTIONED E DXTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 07 314QS 5600441 NO AIRSPEED ON CAPTAIN PFD. ABORTED AT 75 KTS. 2 L 7 2 4F RT A22CE 20081124 EA 2008 11 24 ASOA200801460 1 20081106 A 5320 BEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 VERTICAL BEAM ON FRAME AT FS 409+128 IS CRACKED AT LBL 9 O/B SIDE FROM BOTTOM TO FIRST RIVET APPROX .300"L. 2 L 7 2 4F RT A21EA 20081124 CE 2008 11 24 DXTA2008111203351 1 20081111 A 3230 LANDING GEAR RAYTHN DH125 HAWKER800XP 7150012 CE MALFUNCTIONED E DXTA O OTHER O OTHER TO TAKEOFF 1 GL 07 817QS 258517 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. 2 L 7 2 4F RT A3EU 20081124 CE 2008 11 24 DXTA2008111403355 1 20081024 A 5511 65320XXXXX RIB CESSNA 500 560CESSNA 2076750 CE HORIZ STAB CRACKED E DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 330QS 5600329 WHILE COMPLETING A LUBRICATION SEVERAL CRACKS HAVE BEEN FOUND IN HORZ STAB RIBS, P/N 65320XX-XXX. 2 L 7 2 4F RT A22CE 20081124 CE 2008 11 24 DXTA2008110603340 1 20081105 A 3240 BRAKE SYS BEECH MU300 400A 1155402 CE RIGHT MALFUNCTIONED E DXTA O OTHER O OTHER LD LANDING 1 GL 07 114QS RK469 UPON LANDING RT BRAKE PEDAL IN BOTH PILOT & COPILOTS POSITION WAS APPLIED TO FULLY DEPRESSED POSITION & RESPONDED WITH N EGATIVE BRAKING EFFECT ON BOTH POSITIONS. 2 H 7 2 4F RT A16SW 20081124 GL 2008 11 24 15HA0858011 2 20081105 A 7321 3300588 FUEL CONTROL CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13 03004 GL RT ENGINE DAMAGED A I5HA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 GL 25 588X 2398 2398 29 702591 WY12145 WHILE EN ROUTE, THE CREW OBSERVED THE RT ENGINE LOOSING POWER. THE CREW ELECTED TO SHUT DOWN THE ENGINE AND DIVERTED, M ADE AN UNEVENTFUL SINGLE ENGINE LANDING. A MX CREW WAS DISPATCHED TO INVESTIGATE. AFTER TROUBLESHOOTING THE PROBLEM, T HE MX CREW DISCOVERED THE RT FUEL CONTROL DRIVE SHAFT SHEARED. THE FUEL CONTROL WAS REMOVED AND REPLACED AND THE AIRCRA FT RETURNED TO SERVICE. 2 L 7 2 4R 4 T 6A6 E282 20081124 NM 2008 11 24 KNNA200800094 1 20081119 A 5340 STRINGER CLIP BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 465AT 21528 STRINGER CLIP WAS CRACKED AT STA 767, STR 4R. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 KNNA200800107 1 20081119 A 5340 STRINGER CLIP BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 465AT 21528 STRINGER CLIP WAS CRACKED AT STA 827, STRINGER 5L. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 KNNA200800099 1 20081119 A 5340 STRINGER CLIP BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 465AT 21528 CRACKED STRINGER CLIP AT STA 685, STRINGER 8L. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 KNNA200800096 1 20081119 A 5340 STRINGER CLIP BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 465AT 21528 FOUND STRINGER CLIP CRACKED AT STA 706, STR 0. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 KNNA200800097 1 20081119 A 5340 STRINGER CLIP BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 465AT 21528 FOUND STRINGER CLIP CRACKED AT STA 706, STR 9L. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 AALA200810162 1 20081030 A 5320 WEB BOEING 737 737823 13844BZ NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 CORROSION ON WEB STATION 986.5 RBL32 FORWARD OF RIGHT FORWARD OF G4 MOUNT. INSTALLED REPAIRED PER SRM 51-70-13. 2 L 7 2 4F RT A16WE 20081124 WP 2008 11 24 AALA200810175 1 20081110 A 5320 FRAME DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70529 49921 FRAME CRACKED AT STATION 1510, LOWER RIGHT TAIL CONE ALIGNMENT PIN. INSTALLED DOUBLER PER ESO 80559 DATED, 10 NOV 08. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810133 1 20081027 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 LEFT CUSP CORRODED AT AREA UNDER GIRT BAR AT STATION 1140. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 AALA200820011 1 20081009 A 5320 STRUCTURE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 672AA 52528 25337 AFT MAIN DECK FLOOR STRUCTURE IS CORRODED. REPAIRED IAW SRM 53-60-51-2R2. 2 L 7 2 4F RT A2NM 20081124 NM 2008 11 24 AALA200820013 1 20081015 A 5320 69455559 SUPPORT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 686AA 51188 25343 SILL TIE DOWN SUPPORT CORRODED. REPLACED SUPPORT IAW SRM 51-10-02. 2 L 7 2 4F RT A2NM 20081124 EA 2008 11 24 SWIA200820371 1 20080715 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 368CA 10075 C-CHECK, RIGHT SIDE FORWARD SEAT TRACK RAIL CORRODED, REPLACED. 2 L 7 2 4F RT A21EA 20081222 SO 2008 12 22 FDKA2008122000318 1 20081220 A 3397 JUMPER EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 856MJ 145626 FRL FLT 6228 JFK. EMERGENCY FLOOR LIGHT STRIP OUT AT ROW 12. MX RESECURED JUMPER, OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081222 SO 2008 12 22 FDKA2008122100320 1 20081221 A 5210 HANDLE EMB 145 EMB145LR 3260212 SO PAX DOOR DIRTY A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 858MJ 145767 FRL FLT 6190 CVG-CAE. MAIN CABIN DOOR INNER DOOR HANDLE HARD TO LOCK, AND DOOR HARD TO CLOSE. MX CLEANED AND LUBED, OP S CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081222 SO 2008 12 22 FDKA2008121700316 1 20081217 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO ODOR A FDKA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 831MJ 145273 FRL FLT 6209 JFK-IAD. STRONG FUEL ODOR AFTER APU START. MX COULD NOT DUPLICATE AND FOUND NO FUEL LEAKS. 2 L 7 2 4T RT T00011AT 20081223 NM 2008 12 23 UALA2008111300653 1 20080204 A 3040 HEATER BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT WINDOW MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 203UA 24718 FLIGHT DIVERTED DUE TO CAPTAIN'S WINDOW HEAT PROBLEM. REPLACED 1LT WINDOW. AWAITING SHOP FINDINGS. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 SWAA087259 1 20081221 A 3350 417S5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 214WN 32486 EGRESS LIGHT TRACK COVER CRACKED AT ROW 11. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081223 EU 2008 12 23 COEA0803903 1 20081114 A 5311 S53572502220 FRAME AEROSP ATR42 ATR42320 8680930 EU ZONE 100 CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 903FX 179 MAJOR REPAIR & LEVEL 2 CORROSION. LT LOWER FRAME 24 SEGMENT IS CORRODED BELOW RECIRCULATION DUCT SUPPORT. S/D CUT THE FRAME ASSY WITH A STEPPED CUT FROM STRINGER 16L TO 16R AND FROM STRINGER 17L TO 17R. SPLICED IN NEW FRAME ASSEMBLY WI TH SPLICES AT STRINGERS 16 & 17 L & R. 2 H 7 2 4T RT A53EU 20081223 NM 2008 12 23 SWAA087281 1 20081220 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT WING TE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 615SW 966 27698 DURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20081223 2008 12 23 SWAA087282 4 20081220 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 733SA 27865 DURING SCHEDULED RON CHECK, FOUND L1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081223 EA 2008 12 23 MASA2008121800747 1 20081218 A 3230 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA LANDING GEAR MALFUNCTIONED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 77181 20199 7181 ASH FLT 7135 CLR-IAD. CREW REPORTED GETTING A GEAR DISAGREE WITH NOSE DOOR MESSAGES IN FLIGHT. MX REPLACED PSEU AND PE RFORMED GEAR SWINGS. OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081223 NE 2008 12 23 MASA2008121800748 2 20081218 A 7310 5050T37G01 ACTUATOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* 30015 NE GUIDE VANE MALFUNCTIONED A MASA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 77278 20331 7278 ASH FLT 1040 HNL-ITO. CREW REPORTED FUEL ODOR IN CABIN DURING FLIGHT DUE TO FUEL LEAKING FROM NR 2 ENGINE EXHAUST DRAIN . MX REMOVED AND REPLACED VG ACTUATORS. 2 L 7 2 4F 4 F RT A21EA 20081223 NM 2008 12 23 SWAA087294 1 20081221 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 397 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 397, RBL 70, WL 208. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087283 1 20081221 A 5743 115A5211 TRUNNION BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION BEARING LUGS CORRODED. REPAIRED LUGS PER SWA EA. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 UALA2008111300855 1 20080216 A 2913 PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYD SYSTEM LOW PRESSURE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 517UA 24861 RTFL DUE TO LEFT ENGINE HYD PUMP LOW PRESSURE. REPLACED ENGINE DRIVEN HYD PUMP. ACP ENG RUN-UP, NO LEAKS FOUND. OK FO R SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081223 EA 2008 12 23 COMA200812185003 1 20081217 A 3010 355493255 LOOP CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE DUCT FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 807CA 7364 DURING CLIMBOUT OF BOS RECEIVED AN ANTI-ICE DUCT CAUTION MESSAGE, FLIGHT RETURNED TO THE FIELD. REPLACED THE ANTI-ICE D UCT LOOP IN FRONT OF AFT BULKHEAD TO WHEEL BIN. 2 L 7 2 4F RT A21EA 20081223 NM 2008 12 23 UHLA2008110700007 1 20081207 A 3350 LIGHT EMB ERJ170 ERJ170200LR 3260121 NM CABIN MALFUNCTIONED A UHLA K NONE J WARNING INDICATION IN INSP/MAINT 1 GL 11 206JQ 17000249 AFT CABIN EMERGENCY LIGHTS WERE ON AND CREW HAD EMERGENCY BATTERY FAULT ON EICAS. MAINTENANCE RESET EMERGENCY LIGHT SYS TEM FAULT CLEARED. NO HISTORY AND HAS NOT REPEATED THIS DATE 12/12/2008. 2 L 7 2 4F RT A56NM 20081223 NM 2008 12 23 UALA2008111300892 1 20080215 A 3260 INDICATOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU MLG MISALIGNED A UALA O OTHER N FALSE WARNING CL CLIMB 1 WP 29 382UA 24657 AFTER TAKEOFF THE NLG DID NOT RETRACT, WITH THE GEAR HANDLE UP THE GREEN NOSE GEAR LIGHT WENT OFF BUT THE RED NOSE GEAR LIGHT STAYED ON. LOOKING THROUGH THE NOSE GEAR VIEWER, THE NOSE GEAR WAS STILL DOWN AND THE TWO RED ARROWS WERE STILL A LIGNED. THE GEAR HANDLE OPERATION WAS NORMAL. VISUALLY INSPECTED NLG AND WHEEL WELL. NO DEFECTS NOTED. PERFORMED OPS CHECK OF NLG. OPS CHECK IS GOOD. REMOVED 3 EACH GEAR PINS. NO FAULT FOUND. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 UALA2008121806917 1 20081217 A 2432 893003 CHARGER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE MAIN BATTERY FAILED A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 530UA 25043 MAIN BATTERY CHARGER EICAS MSG PRESENT. REPLACED MAIN BATTERY CHARGER UNIT. OP TESTED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081223 EA 2008 12 23 COMA2008121650027 1 20081212 A 3150 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA BLEED DUCT ILLUMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 934CA 7042 ON CLIMBOUT FROM MHT RECEIVED ANTI-ICE DUCT WARNING MSG. PERFORMED QRH, SYSTEM OFF, MSG CLEARED. ACFT RETURNED TO MHT LANDED SAFELY. INSPECTED 14TH STAGE BLEED AIR SYSTEM, AND PERFORMED OPERATIONAL TEST OF WING ANTI-ICE SYSTEM. NO DEFEC TS NOTED. 2 L 7 2 4F RT A21EA 20081223 NM 2008 12 23 UALA2008121806918 1 20081218 A 2421 729825M IDG BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RIGHT FAILED A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 596UA 28749 THE R GEN DRIVE LIGHT ON WITH ASSOCIATED EICAS DURING TAXI OUT. VERIFIED GEN BAD. GEN OIL SMELLED BURNED. REPLACED RT ENG IDG. OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081223 EA 2008 12 23 COMA2008121650026 1 20081212 A 2841 7680941 COMPENSATOR CNDAIR CL600 CL6002B19 1900309 EA FUEL SYSTEM FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 914CA 7012 EN ROUTE FROM DCA TO HSV RECEIVED FUEL IMBALANCE MSG. EMERGENCY DECLARED, A/C DIVERTED TO CHA, LANDED SAFELY. REMOVED AND REPLACED RIGHT FUEL COMPENSATOR. 2 L 7 2 4F RT A21EA 20081223 EA 2008 12 23 COMA2008121750036 1 20081215 A 3010 32144424 SHUTOFF VALVE CNDAIR CL600 CL6002B19 1900309 EA ZONE 200 FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 713CA 30796 7245 ON CLIMBOUT FROM CVG RECEIVED WING OVERHEAT WARNING MSG WITH SYSTEM ON, AND IN STANDBY. ACFT RETURNED TO CVG LANDED SAF ELY. REMOVED AND REPLACED LEFT ANTI-ICE MODULATING SHUTOFF VALVE. 2 L 7 2 4F RT A21EA 20081223 NE 2008 12 23 UALA2008111302047 2 20080408 A 7320 7911004111 EEC BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE RT ENGINE MALFUNCTIONED A UALA O OTHER O OTHER LD LANDING 1 WP 29 668UA 57616 613 30024 724634 RIGHT ENG NO N1 READING ON TOUCHDOWN. REPLACED ELECTRONIC ENGINE CONTROL (EEC). 2 L 7 2 4F 4 F RT A1NM E24NE 20081223 NE 2008 12 23 UALA2008111302048 2 20080408 A 7397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT ENGINE DIRTY A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 667UA 33998 16570 29239 727816 CREW REPORT: LEFT ENGINE FUEL FILTER LIGHT ON MOMENTARILY IN DESCENT. RECEIVED STATUS LIGHT, CLEARED IT. FOUND CONNEC TOR D10996 DIRTY. CLEANED CONNECTOR & RAN ENGINE - OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081223 EU 2008 12 23 UALA2008111302182 1 20080414 A 2710 A880082 SERVO AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT AILERON MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 401UA 435 LT AILERON FAULT DISPLAYED ON UPPER ECAM SCREEN. CHRONIC A/C. MX WANTS TO WATCH THE LATEST FIX BEFORE CLOSING. REPLAC ED L B AILERON SERVO. ALL OPS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081223 2008 12 23 UALA2008111301328 4 20080310 A 3445 INDICATION SYS COLLINS BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU TCAS MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 351UA 1286 24319 FLIGHT DIVERTED DUE TO INOP TCAS. *S/D* TCAS INOPERATIVE. REPLACED TCAS. WAITING ON SHOP FINDINGS. 2 L 7 2 4F 4 F RT A16WE E21EU 20081222 SO 2008 12 22 FDKA2008121300311 1 20081213 A 3350 BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 836MJ 145359 FRL FLT 6254 IND - EMERGENCY EXIT LOCATOR AND OVERWING IDENTIFIERS OUT ON LT AND RT SIDE OF CABIN. MX ALLOWED EMERGENCY BATTERIES TO CHARGE. OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081222 NM 2008 12 22 USAA2008121592224 1 20081204 A 5322 143N534413 SHEAR TIE BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 CLT - C1 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON SHEAR TIE AT BS 660, BL0. REPLACED SHEAR TIE AT BS 660, B L 0 IAW BOEING DRAWING 143N5344. 2 L 7 2 4F RT A2NM 20081222 NM 2008 12 22 USAA2008121692235 1 20081215 A 5330 6545774 SKIN BOEING 737 7373B7 138447F NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 527AU 23862 CLT - RON - MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT BS 727D, LBL 24. REPAIRED FUSELAGE SKIN AT BS 727D, LBL 24 IAW B73 7 SRM 53-00-01 REPAIR 31. 2 L 7 2 4F RT A16WE 20081222 CE 2008 12 22 GUUA94532121208A 1 20081212 A 3260 MS24171D1 RELAY BEECH 1900 1900D 1154162 CE MLG SHORTED A GUUA O OTHER O OTHER AP APPROACH 1 SO 29 53545 UE185 FLIGHT NR 9201 EYW/FLL DURING APPROACH UPON LANDING GEAR EXTENSION LANDING GEAR CIRCUIT BREAKER POPPED. NOSE GEAR LOCKE D INDICATION DID NOT APPEAR. MANUALLY PUMPED NOSE GEAR DOWN. REPLACED K3 LANDING GEAR MOTOR RELAY. OPS CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081222 NM 2008 12 22 USAA2008121692247 1 20081213 A 3350 20137A BATTERY PACK BOEING 737 7373G7 138447J NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 307AW 24634 SAL - C17 - EEL - EMERGENCY EXIT LIGHT INOP AT PASSENGER SEAT ROW 18 LEFT TO SEAT ROW 23 LEFT. REPLACED AFT LEFT EMERGE NCY BATTERY PACK IAW B737 AMM 33-51-51. 2 L 7 2 4F RT A16WE 20081222 NE 2008 12 22 USAA2008121592222 2 20081212 A 7230 COMPRESSOR AIRBUS A319 A319112 3930323 EU CFMINT CFM565 CFM565B6 13802 NE LT ENGINE STALLED A USAA A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 19 750UW 1315 575387 FLT 2131 - BOS-LGA - EMERGENCY LANDING - THREE LOUD BANGS WERE HEARD WITHIN TWO MINUTES BELOW LEFT WING AND VIBRATION WA S FELT AT FLIGHT LEVEL 16000. CAPTAIN DECLARED EMERGENCY AND RETURNED TO BOSTON. AIRCRAFT LANDED NORMALLY AND TAXIED T O THE GATE. REPLACED LEFT ENGINE DUE TO COMPRESSOR STALLS PER WORK CARD 26L40071001. ADDITIONAL INFORMATION WILL BE SU BMITTED UPON REVIEW OF VENDOR TEAR DOWN REPORT. 2 L 7 2 4F 4 F RT A28NM E37NE 20081124 WP 2008 11 24 AALA200810107 1 20081029 A 2560 LIG5363 LIGHT DOUG DC9 DC982 3022082 WP PORTABLE INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 461AA 59931 49566 PORTABLE EMERGENCY LIGHT AT EPC, CHARGE LIGHT IS INOP. REMOVED AND REPLACED PORTABLE EMERGENCY BELT RACK. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 DHLA2008745683 1 20081111 A 5311 FRAME BOEING 727 727224 1384076 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 FUSE FRAME AT BS 1090 HAS DOUBLE DRILLED HOLES AT STR 8L, 11L, AND 14L. ACCOMPLISHED NECESSARY FRAME REPAIRS BETWEEN ST R 7L AND 9L, AND BETWEEN STR 10L AND 12L PER EO COO-2-53-385-08 DATED 10/27/2008. REF FAA FORM 8110-3 DATED 11/6/2008 A ND EVA B253-00163 FOR REPAIR APPROVAL. DOCUMENTED ON N/R 2-23. 2 L 7 3 4F A3WE 20081124 NM 2008 11 24 DHLA2008745684 1 20081111 A 5312 PRESSURE PANEL BOEING 727 727224 1384076 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 NLG W/WELL SKIN/WEB CORRODED AT BS 326.5, LBL 17.5. ACCOMPLISHED SKIN REPAIR PER EO COO-2-53-375-08 DATED 10/22/2008. REF FAA FORM 8110-3 DATED 11/6/2008 AND EVA B253-00161 FOR REPAIR APPROVAL. DOCUMENTED ON N/R 1-666. 2 L 7 3 4F A3WE 20081124 WP 2008 11 24 AALA200810108 1 20081029 A 3350 BAT5014 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT WEAK A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 461AA 49566 EMERGENCY LIGHT BATTERY PACK WEAK. REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 AALA200810152 1 20081028 A 5315 FLOORBEAM BOEING 737 737823 13844BZ NM ZONE 100 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 AFT CARGO FLOORBEAM HAS 2 HOLES DRILLED THROUGH TOP FLANGE AT STATION 787 RIGHT BODY LINE 8.10. BLENDED DAMAGED AREA AN D ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-53 IAW ESO 61000 AT STATION 787 AND 788 RIGHT BODY LINE 8.10. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 DLM88081528 1 20081109 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 968DL 53161 DURING HMV A MISSING ID TAG WAS FOUND ON FUSELAGE REPAIR AT STA Y=113 LONGERON 23 LT. SKIN WAS REPAIRED IAW SRM 53-04 F IG 12C. 2 L 7 2 4F RT A6WE 20081124 NE 2008 11 24 DL77L081530 2 20081111 A 7200 GE90110B ENGINE BOEING 777 777232 1385232 NM GE GE90 GE90110B1 30046 NE NR 1 MALFUNCTIONED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 702DN 3232 29741 906440 PERFORMED EA 54-41523-14 ORIG REMOVED STARTER GEARSHAFT AND TGB REMOVED AND REPLACED. REMOVED AND REPLACED NEC TUBES AN D BRACKETS FOR ACCESS. PERFORMED TEST NO FAULTS DRY MOTOR NO LEAKS COMPLETED EA 54-471523-14 ORG OPERATED NR 1 ENG PER 71-00-00-700-805 TEST 6 CKS GOOD. 2 L 7 2 4F 4 F RT T00001SE E00049EN 20081124 NM 2008 11 24 DL757081550 1 20081010 A 5330 SKIN BOEING 757 757232 1384965 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 CORROSION ON RIGHT AIRPHONE ANTENNA FUSELAGE SKIN. CUT OUT DAMAGE IAW SRM 53-00-01 FIG 201. INSTALLED REPAIR DOUBLER I AW SRM 53-00-01 FIG 201 REPAIR 3. 2 L 7 2 4F RT A2NM 20081124 NM 2008 11 24 UALA2008111706528 1 20081115 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT EEL LIGHT INOP AT SEAT 4F FWD LIGHT ASSY. REPLACED LIGHT ASSY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111706536 1 20081116 A 3397 80172424 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 206UA 30212 SEAT 1E BOTH EEL LIGHTS INOP. SECURED CONNECTOR, CHECKS OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081124 NE 2008 11 24 UALA2008111806547 2 20081117 A 7421 IGNITER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT ENGINE INOPERATIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 211UA 30217 L ENG IGNITOR 1 INOPERATIVE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081124 NM 2008 11 24 UALA2008111806548 1 20081117 A 4990 OIL FILTER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE APU CLOGGED A UALA O OTHER J WARNING INDICATION UK UNKNOWN 1 WP 29 204UA 28713 APU APUC DETECTED FAULT THAT WOULD CAUSE AUTOMATIC SHUTDOWN OF APU IN UNATTENDED MODE OPERATION, OR COMPLETE LOSS OF APU C BUS ACTIVITY (BOTH L AND R 629) FOR 3 SECONDS AFTER THE APU MASTER CONTROL SWITCH HAS BEEN IN THE ON POSITION FOR TEN SECONDS. STATUS MSG-4910270 INACTV TA MODE. REPLACED APUC. AFTER APUC WAS INSTALLED, FAULT MSG, 49-12990 APPEARED - O IL FILTER ELEMENT CLOGGED. REPLACED OIL FILTER ELEMENT. ALL FAULTS CLEARED. APU OPS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081124 NM 2008 11 24 UALA2008111306207 1 20081020 A 2120 UNKNOWN AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 822UA 948 F/A REPORTED PLASTIC BURNING ODOR NEAR DOOR 2L. SMELL GONE AFTER 5 MINUTES. REMOVED COFFEEMAKERS, RAN CHILLERS, CHECKE D AFT LAVS AND AFT LAV HEATERS, CHECKED AFT CARGO COMPARTMENT. NO PLASTIC OR BURNING SMELL NOTED. RE-INSTALLED COFFEEM AKERS. 2 L 7 2 4F 4 F RT A28NM E40NE 20081124 NM 2008 11 24 UALA2008111306217 1 20081005 A 5315 FLOORBEAM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 818UA 882 BEAM 95 CORRODED. REMOVED FLOORBEAM 95. REMOVED BRACKETS AND DRILLED NEW BEAM. ALL BRACKETS AND ATTACH FITTINGS INSTA LLED. BEAM INSTALLED, ATTACHMENT COMPLETE AT FRAME 64, NEEDS BOLTS AT FRAME 66 AND 65. COMPLETED INSTALLATION OF BEAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081124 NM 2008 11 24 KNNA200800102 1 20081119 A 5340 STRINGER CLIP BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 465AT 21528 FOUND STRINGER CLIP CRACKED AT STA 616, STRINGER 1L. 2 L 7 2 4F RT A16WE 20081222 2008 12 22 ZZDA2008183 4 20081211 A 2565 64210103 SLIDE BOEING 717 717200 1383700 NM TAILCONE UNWANTED DEPLOY A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 894AT 55046 TAIL CONE SLIDE INADVERTENTLY DEPLOYED BY MAINTENANCE. REPLACED TAIL CONE SLIDE ASSEMBLY PER B717 MM 25-61-02. REINSTA LLED TAIL CONE ASSEMBLY PER B717 MM 53-52-01. 2 L 7 2 4F TR A6WE 20081222 2008 12 22 C2XA08RI180 2 20081215 A 7532 4800104 SWITCH EMB 145 EMB145LR 3260212 SO BLEED VALVE INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14952 145067 FLIGHT 2306 - EWR - DURING CLIMBING FLIGHT CREW REPORTED THE FOLLOWING MSGS ON EICAS: PACK 2 CLSD AND BLD 2 CLSD. CREW RESET THE SYSTEM BUT FAILED AGAIN AND WHEN TRIED AN ANTI ICE TEST GOT BLD 2 FAIL MSG. CREW PERFORMED AIR RETURN AND LAND ED UNEVENTFULLY. MX R&R NR 2 BLEED VALVE PUSH BUTTON SWITCH AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081222 WP 2008 12 22 UPS08854183 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR 803-F1-53, STA 1278-1285, L5R-L7R, HAS NO SRM REFERENCE AND REQUIRES EO APPX F. REMOVED EXIST ING REPAIR. FABRICATED AND INSTALLED REPAIR REF EO DC8- 5330-31400-A AND DWG FVCI 53-08540-24. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854184 1 20081014 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-41 FS 1120-1135 L1-L4L HAS SRM REF 53-02-01 FIG 7 SHEET 11 IS A CAT B REPAIR. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-9 SRM 53-02-01 FIG 7 SHEET 10. 2 L 7 4 4F RT 4A25 20081222 NM 2008 12 22 UPS08M54195 1 20081215 A 3397 WIRE DOUG MD11 MD11F 3023600 NM CABIN NOT SEATED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 295UP 48475 INSPECTION TYPE:N/A INTERIOR EMERGENCY LIGHTS INOP. RESEATED WIRE NUMBER B315-12-20 AT BLOCK 53-692, BLOCK 2. EMERGENC Y LIGHTS SYSTEM OPS CHECKED NORMAL REF MM 33-50-00-5. 2 L 7 3 4F RT A22WE 20081222 EU 2008 12 22 UPS08154210 1 20081216 A 2612 FIRE LOOP AIRBUS A300 A300F4622R 3930360 EU MID CABIN FAILED A IPXA K NONE N FALSE WARNING CR CRUISE 1 SO 01 124UP 0808 INSPECTION TYPE:N/A DIVERSION - CAPTAIN OBSERVED AN ECAM MESSAGE STATING "LAND ASAP" FOR MID CABIN FIRE LOOP FAIL. CREW DIVERTED TO FWA. DEFERRED PER MEL 26-17-01-1. PERFORMED MAIN CARGO DECK SMOKE DETECTION ADJ/TEST PER MM 26-19-00-05. NO DEFECTS NOTED. 2 L 7 2 4F RT A35EU 20081222 WP 2008 12 22 UPS08854176 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-56 AT STA 1157-1166 L27L HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTA LLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 13. 2 L 7 4 4F RT 4A25 20081222 NM 2008 12 22 SWAA087246 1 20081218 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 559, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 SWAA087250 1 20081218 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 463WN 32467 DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS LIGHT COVER CRACKED. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081222 EA 2008 12 22 COMA2008121750035 1 20081216 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 784CA 7319 ON APPROACH INTO FSD RECEIVED FLAPS FAIL CAUTION MSG WHEN SELECTING FLAPS TO 8 DEG. EMERGENCY DECLARED, A/C LANDED SAFE LY. COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW UP MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 20081223 NM 2008 12 23 UALA2008111300890 1 20080215 A 5320 INTERCOSTAL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CARGO DOORWAY CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 AFT CARGO DOOR CUTOUT LOWER FWD SIDE HAS INTERCOSTAL CORRODED AT FASTENER HOLES. REMOVED CORROSION. FOUND WITHIN LIMIT S. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 UALA2008121706911 1 20081217 A 3350 20131A BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 EEL LIGHTS AFT OF ROW 31 INOP. EXIT SIGN INOP OVER DOOR 4R. AISLE LIGHTS INOP ROWS 27 & 31, SLIDE LIGHT INOP DOOR 4R. REPLACED BATTERY PACK & POWER SUPPLY AT POSITION M10817. 2 L 7 2 4F 4 F RT A2NM E17NE 20081223 NM 2008 12 23 CALA2008122201160 1 20081220 A 5311 6546596 FRAME BOEING 737 737524 1384721 NM BS 727B S8-9L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24633 27901 FRAME CRACKED AT STATION 727B BETWEEN STRINGER 8 AND 9 LEFT. CUT OUT DAMAGED AREA FROM FRAME STA 727B BETWEEN STR 8 AND 9 LT INSTALLED REPAIR ANGLES PER EA5310-04498 OP2. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 CALA2008122201161 1 20081220 A 5311 6546525 FRAME BOEING 737 737524 1384721 NM BS 380 S8-9R CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24633 27901 FRAME CRACKED AT STATION 380 BETWEEN STR 8 AND 9 RIGHT. CUT OUT DAMAGED AREA FROM FRAME AT STATION 380 BETWEEN STRINGER S 8 AND 9 RIGHT. INSTALLED REPAIR ANGLES PER EA5310-04498 OP2. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087288 1 20081221 A 5310 6546822 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 807-827 S17L CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BETWEEN BS 807 TO BS 827, STR 17L. REMOVED AND REPLACED W EB PER SRM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087289 1 20081221 A 5310 6546822 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 727E-747 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 16Y CHECK, FOUND RT CREASE BEAM WEB CORRODED AT BETWEEN BS 727E TO BS 747. REMOVED AND REPLACED WEB PE R SRM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087291 1 20081221 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM BS 520 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087292 1 20081221 A 5340 65C27314 STRINGER CLIP BOEING 737 7375H4 138449D NM BS 881 S25R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED 18Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 881, STR 25R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087293 1 20081221 A 5310 6552874951 DOOR FRAME BOEING 737 7373H4 1384600 NM L2 DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME CRACKED AT L2 DOOR LOWER AFT ENTRY CUTOUT. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 UALA2008111301538 1 20080318 A 4930 170101 FUEL NOZZLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU APU LOOSE A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 313UA 23674 STRONG FUEL ODOR DETECTED IN CABIN. LOWER FUEL NOZZLE AT 6 O'CLOCK POSITION MISSING BOLT. THREADED INSERT IS STRIPPED CANNOT SECURE BOLT. RAN APU AND FOUND FUEL LEAK AT FUEL HEATER AFT CHECK VALVE UNION AREA. DIFFICULT TO SEE IF LEAK IS DUE TO SEALS OR UNIONS. APU NEEDS TO BE DROPPED TO REPLACE CHECK VALVE AND APPROPRIATE SEALS. MAY NEED TO CHANGE HEAT ER AS PRECAUTIONARY. REMOVED APU AND ROUTED TO SHOP FOR REPAIR AND TEST CELL RUN. REPLACED APU AND FUEL HEATER CHECK V ALVE AND SEALS. OPS AND LEAKS CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NE 2008 12 23 UALA2008111301584 2 20080319 A 7320 7911004111 EEC BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 644UA 63616 2713 25094 717676 NR 2 ENG 'ENG CONTROL' MESSAGE APPEARED ON EICAS WITH EEC IN NORMAL MODE. RECURRED ON SUBSEQUENT FLIGHT. *S/D* REPLACE D NR 2 ENGINE EEC ALTERNATOR, EEC AND N1 TRANSDUCER. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081224 NM 2008 12 24 AALA200820101 1 20081210 A 5340 146N52832 FITTING BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 609AA 45862 27447 LAVATORY MOUNT FITTING CORRODED. REPLACED MOUNT FITTING IAW SRM 51-10-02. 2 L 7 2 4F RT A2NM 20081224 WP 2008 12 24 AALA200810528 1 20081205 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 RIGHT CUSP CRACKED AT STATION 810. REPAIRED PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081224 WP 2008 12 24 AALA200810529 1 20081206 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 CORROSION ON RIGHT TIE DOWN TRACK IN AFT CARGO STATION 1041 TO 1155. INSTALLED SERVICEABLE TIE DOWN TRACK. 2 L 7 2 4F A6WE 20081224 NM 2008 12 24 USAA2008121792250 1 20081207 A 5330 6552988 SKIN BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - CRACK ON FUSELAGE SKIN AT LOWER HINGE CUTOUT OF L2 DOOR BS 947, S14L. REPAIRED FUSELAGE SKIN AT LOWER HINGE CUTOUT IAW TYPICAL REPAIR 53-60-10. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121792253 1 20081215 A 5320 ANGLE BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - ANGLE CRACKED AT BS 270, S10L. REPAIRED ANGLE AT BS 270, S10L IAW BOEING DRAWING 65-17684-65. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121992277 1 20081218 A 5311 6545834U552 FRAME BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - FRAME WEB CRACKED AT BS 328, LBL 50. REPLACED FRAME WEB AT BS 328, LBL 50 IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 MZZA2008122200012 1 20081219 A 5320 147A8540U8 SILL BOEING 737 737824 13844BZ NM BS 964 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 SW 27 14228 28792 CORROSION FOUND ON R2 SERVICE DOOR SILL, BODY STATION 964 RBL 43 NEXT TO AFT DRAIN AREA. R2 DOOR SILL CHORD REMOVED AND REPLACED IAW SRM 51-10- 02, HOLES PICKED UP PER SRM 51-40-05 REV 34. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 MZZA2008122200014 1 20081220 A 5320 5321DB11727 INTERCOSTAL BOEING 737 737824 13844BZ NM BS 294-312 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 SW 27 14228 28792 CABIN FLOOR SUPPORT INTERCOSTAL CRACKED ABOUT 2.0 INCH RBL45 AND BETWEEN BODY STATION 294.5 TO BODY STATION 312. INTERC OSTAL REMOVED, FABRICATED PER EC/RA 5321-01524, HOLES PICKED-UP PER SRM 51-40-05 AND INSTALLED PER SRM 51-10-02 REV 34. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 MZZA2008122200015 1 20081220 A 5320 5321DB11727 INTERCOSTAL BOEING 737 737824 13844BZ NM BS 312-328 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 SW 27 14228 28792 CABIN FLOOR SUPPORT INTERCOSTAL CRACKED ABOUT 0.20 INCH, STATION 312 TO 328 LBL 50. INTERCOSTAL REMOVED, FABRICATED IAW EC/RA 5321-01524, HOLES PICKED-UP PER SRM 51-40-05 AND INSTALLED PER SRM 51-10-02 REV 34. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121892270 1 20081031 A 5320 6517583504 VERTICAL BEAM BOEING 737 7373G7 138447J NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 SAL - C17 - MAJOR REPAIR - VERTICAL BEAM WEB CRACKED AT BS 178, WL 183, RBL 5 TO RBL 7. REPAIRED VERTICAL BEAM WEB AT B S 178, WL 183, RBL 5 TO RBL 7 IAW US AIRWAYS EA 132168. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008122292291 1 20081122 A 5320 141T5814 SUPPORT ANGLE BOEING 767 7672B7ER 1385107 NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 253AY 24894 BFM - C4 - MAJOR REPAIR - CABIN FLOORBEAM SUPPORT ANGLE IS CRACKED AT BS 246, LBL 36. REPAIRED FLOORBEAM SUPPORT ANGLE IS AT BS 246, LBL 36 IAW SRM 51-40-02. 2 L 7 2 4F RT A1NM 20081224 NM 2008 12 24 USAA2008121892266 1 20081124 A 5320 69434771 CHANNEL BOEING 737 7373G7 138447J NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - CORROSION ON SUPPORT CHANNEL BETWEEN BS 767 TO BS 787, S25R. REPLACED SUPPORT CHANNEL BETWEE N BS 767 TO BS 787, S25R IAW SRM 51-40-02-0G. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121892269 1 20081217 A 5320 WEB BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - CRACK ON FUSELAGE WEB AT BS 277, S14R FORWARD OF R1 DOOR. REPLACED FUSELAGE WEB AT BS 277, S1 4R IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 UALA2008111302330 1 20080420 A 2697 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FIRE BOTTLE UNSTABLE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 WHILE ACCOMPLISHING EG8515 FOR CARGO PIT FIRE BOTTLE CHECK, NOTICED THAT WHEN DISC SWITCH IS PUSHED THAT VOLTAGE AT SQB CONN SPIKES TO 24.96 VDC FOR A SPLIT SECOND THEN GOES BACK TO APPROX ZERO AND STAYS ZERO UNTIL 20 MINS WHEN IT GOES TO A PPROX 24 VDC AS STATED IN MM. SHOULD NOT HAVE THAT INITIAL SPIKE OF 24.96 VDC AT BOTTLE 2C. ACCOMP WITH FIRE EXTINGUIS HER SYSTEM TESTING KIT. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081224 NM 2008 12 24 USAA2008121792254 1 20081216 A 5712 RIB BOEING 737 7374B7 138449C NM ZONE 600 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - RIGHT WING RIB WEB LOWER CHORD CRACKED AT WBL 135.5, 7 INCHES FORWARD OF AFT SPAR AT LOWER SKI N. REPAIRED RIGHT WING RIB WEB LOWER CHORD CRACKED AT WBL 135.5, IAW US AIRWAYS EA 100777. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086385 1 20081119 A 5322 6546569 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BETWEEN STR 15R TO 16R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086407 1 20081120 A 3350 417N5212 CAP BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 221WN 34259 DURING SCHEDULED HC1 CHECK, FOUND FWD EEPLS END CAP BROKEN. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086408 1 20081118 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BETWEEN BS 707 TO BS 714, BL 0. REPAIRED WEB PER PAE ER. 2 L 7 2 4F RT A16WE 20081125 2008 11 25 SWAA086401 4 20081118 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081125 WP 2008 11 25 AALA200810053 1 20081006 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 RIGHT CUSP CRACKED AT STATION 1245. REMOVED DAMAGE AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 20081125 WP 2008 11 25 AALA200810039 1 20081022 A 5310 SPAR DOUG DC9 DC982 3022082 WP ZONE 300 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 03 PLANK BOLTS SEALANT LOOSE AND EMITTING RUST AT CENTER SPAR BOX RIGHT TOP SIDE. REMOVED 05 BOLTS, FOUND CORROSION IN BORES. REAMED HOLES TO REMOVE CORROSION. TREATED AND PRIMED BORES. MANUFACTURED AND INSTALLED 05 BUSHINGS IN ACCORDAN CE WITH ESO 80559 DATED 10-14-08. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810054 1 20081007 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 CRACK IN INTERCOSTAL AT CENTERLINE BETWEEN FLOORBEAMS 1271-1287. INSTALLED NEW INTERCOSTAL. 2 L 7 2 4F RT A6WE 20081125 WP 2008 11 25 AALA200810094 1 20081016 A 5310 BEAM DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 AFT CARGO DOOR BEAM CORRODED AT STATION 1155-1211. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER AARD 53-10-00-3. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810038 1 20081016 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 CORROSION ON TOP OF SUBFLOOR CUSP FORWARD OF NR 6 SEAT TRACK. INSTALLED CUSP REPAIR DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 HALA2008111300848 1 20081113 A 5512 SKIN BOEING 767 76733A 1385209 NM HORIZONTAL STAB CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 HORIZONTAL STABILIZER CENTER SECTION LOWER SKIN EXTERNAL SURFACE CORRODED AT LBL 3.3 AND RBL 6.5 AT REAR SPAR. BLEND RE PAIR IAW SRM 55-10-01 FIG 101 AND ANZ TI 190119901-0001. 2 L 7 2 4F RT A1NM 20081125 NM 2008 11 25 HALA2008111700861 1 20081117 A 2612 FIRE DETECTOR BOEING 767 767332 1382001 NM CARGO BAY FALSE ACTIVATION A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 594HA 22375 "AFT CARGO DET 2" "FWD CARGO DET 2" STATUS PAGE. CHECKED COND AND SECURITY OF FWD AND AFT PIT NO DEFECTS NOTED. PERFOR MED OPS CHECK OF FAULT DET SYSTEM, LIGHTS DID NOT RETURN REF AMM 26-16-00. 2 L 7 2 4F RT A1NM 20081125 WP 2008 11 25 AALA200810055 1 20081009 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP ZONE 100 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 DAMAGE ON LEFT TIE DOWN TRACK IN AFT CARGO FROM STATION 1110 TO 1220. INSTALLED NEW TIE DOWN TRACK. 2 L 7 2 4F RT A6WE 20081125 WP 2008 11 25 AALA200810102 1 20081022 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 CORROSION ON RIGHT CUSP AT STATION 160-168. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810103 1 20081022 A 5320 PAN DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 CORROSION ON BOTTOM SIDE OF G1 GALLEY DRAIN PAN STATION 148-160 RIGHT SIDE OF CABIN. REMOVED CORROSION INSTALLED DOUBLE R PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810072 1 20081013 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 CRACK AT BELT BOTTOM CORNER ON WINDOW FRAME STATION 1098 RIGHT. INSTALLED DOUBLER PER AARD 53-10-00-25. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810074 1 20081015 A 5320 STRUCTURE DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 SUBFLOOR CRACKED OUTBOARD SIDE OF NUMBER 2 SEAT TRACK AT STATION 218. INSTALLED DOUBLER PER SRM 53-20-00-16. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 SWAA086426 1 20081120 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086438 1 20081120 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086386 1 20081119 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 179, RBL 5.7, WL 184. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081125 EA 2008 11 25 COMA0860457 1 20081106 A 5311 6013600130 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 640 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 783CA 7315 RT FS 640 FRAME DOUBLER IS CRACKED BETWEEN STR 9 AND 12. REMOVED DAMAGED PARTS AND COMPLIED WITH MODIFICATION K601R3600 9-4 ON RT FS 640 FRAME AND DOUBLER PER SB601R-53-061 KIT DRWG. K601R36009 REV B AND 601R5361569 REV A. 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 SWAA086390 1 20081119 A 5754 6573714 SLAT BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT O/B SIDE DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086410 1 20081120 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED MV1 CHECK, FOUND STRINGER CRACKED AT BS 487 + 14, STR 18L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 USAA920081948 1 20081019 A 5322 SHEAR TIE BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03-0553-8-0546/004 SHEAR TIE CRACKED AT BS 520, BETWEEN S13L AND S14L. REPAIRED SHEAR TIE AT BS 520 BETWEEN S13L AND S14L IAW SRM 53-00-01 REPAIR 25 DETAIL VII. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086461 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 25R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086462 1 20081121 A 5340 69353526114 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 25R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 NWAA084865810 1 20081103 A 3350 POWER SUPPLY BOEING 757 757351 1384991 NM EMERGENCY LIGHT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 590NW 32990 DURING AN OVERNIGHT LINE CHECK THE LT OVER WING SLIDE ILLUMINATION LIGHT WOULD NOT TEST. MX FOUND POWER SUPPLY M11383 T O BE DEFECTIVE AND REPLACED IT. OPS WAS NORMAL AFTER REPLACEMENT OF THE BATTERY PACK. 2 L 7 2 4F RT A2NM 20081125 2008 11 25 COMA0860451 4 20081103 A 3418 COMPUTER CNDAIR CL600 CL6002B19 1900309 EA STALL WARNING MALFUNCTIONED A COMA L ABORTED APPROACH N FALSE WARNING DE DESCENT 1 SO 27 811CA 7380 STALL FAIL CAUTION MSG INFLIGHT, ACFT LANDED SAFELY IN YUL. NO FAULTS LISTED IN MDC. RESET STALL PROTECTION COMPUTER, SYSTEM OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20081124 NM 2008 11 24 UALA2008111806551 1 20081117 A 4930 38760263 ECU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 543UA 25698 APU FAULT WILL NOT START. REPLACED ECU DUE TO NO RESPONSE. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 EU 2008 11 24 UALA2008111305928 1 20080927 A 2612 VALVE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FIRE DETECTION FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 438UA 678 SMOKE-FIRE TEST FAILS FOR CARGO SYSTEM. SMOKE-FIRE TEST FAILS FOR CARGO SYSTEM. REPLACED AFT CARGO VALVE 33HN. 2 L 7 2 4F 4 F RT A28NM E40NE 20081124 EU 2008 11 24 UALA2008111305930 1 20080930 A 2910 HYDRAULIC LINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN SYSTEM LEAKING A UALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 29 473UA 1469 GREEN HYD SYSTEM FAILURE. FLIGHT DIVERTED. REPLACED LEFT ENGINE HYD PUMP DUE TO RUNNING DRY, LEAK DUE TO LEAKING HYD L INE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081124 EA 2008 11 24 SWIA200820392 1 20080807 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 778SK 10242 C-CHECK, PASSENGER DOOR AFT WEB CRACKED AT UPPER COUNTERBALANCE ATTACH POINT. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 SWIA200820394 1 20080819 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710SK 10242 C-CHECK, CROSSBEAM AT FS 280 CRACKED AT RBL11 AND LBL11. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 SWIA200820395 1 20080819 A 5320 STIFFENER CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710SK 10170 C-CHECK, FS 280 RBL26 WL-3 STIFFENER CRACKED. REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 SWIA200820397 1 20080716 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 442SW 7609 C-CHECK, FS 280 LBL9 LOWER FLOOR SUPPORT CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 SWIA200820418 1 20081117 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 452SW 7716 FLT 4383 - AFT CEILING LEVEL EMERGENCY LIGHT INOP, RELAMPED. 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 SWIA200820419 1 20081117 A 3350 BATTERY PACK CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT DISCHARGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 928SW 7701 FLT 6678 EMERGENCY FLOOR LIGHTS BETWEEN ROWS 2 AND 5 INOP. REPLACED INVERTERS AT BATTERY PACKS 2 AND 4. 2 L 7 2 4F RT A21EA 20081124 WP 2008 11 24 AALA200810028 1 20081016 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 CORROSION ON CUSP STATION 218 UNDER G-2 GALLEY MOUNT. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810084 1 20081016 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 CORROSION UNDER LEFT CUSP AT STATION 489. REMOVED CORROSION. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810081 1 20081016 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 RIGHT HAND CUSP CORRODED AT STATION 1155-1174 IN PASSENGER CABIN. REMOVED CORROSION PER SRM 51-10-3, INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810023 1 20081014 A 3222 CYLINDER DOUG DC9 DC982 3022082 WP NLG DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 RETRACK CYLINDER STRUCK NOSE LANDING GEAR CASTING. INSTALLED NEW NOSE LANDING GEAR RETRACK CYLINDER. 2 L 7 2 4F A6WE 20081125 NE 2008 11 25 HALA2008111200851 2 20081112 A 7240 COMBUST CHAMBER BOEING 767 7673G5 1385126 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 585HA 24257 729124 ETOPS SIGNIFICANT SYSTEM, DUE TO (3) AXIAL CRACKS EXTENDING THROUGH (3) LOUVERS IN THE COMBUSTION CHAMBER LINING (‘NOT P ERMITTED’ PER BOROSCOPE PAPERWORK AND AMM) WHICH WAS DISCOVERED DURING THE NR 2 ENGINE BOROSCOPE, ACFT WILL BE UNDERGOIN G A NR 2 ENGINE REPLACEMENT. INSTALLED SERVICEABLE ENGINE ON NR 2 POSITION PER HAL M275-767 GRD RUN UPS AND LEAK CHECKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081125 NM 2008 11 25 SWAA086373 1 20081119 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 EA 2008 11 25 SWIA200820424 1 20080818 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 441SW 7602 C-CHECK, RIGHT ENGINE AFT THRUST FITTING BALL CORRODED, REPLACED. 2 L 7 2 4F RT A21EA 20081125 WP 2008 11 25 AALA200810031 1 20081017 A 5320 DIAPHRAGM DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 CORROSION ON SUB FLOOR DIAPHRAM BETWEEN STATION 160-200. INSTALLED DOUBLER/DIAPHRAM DOUBLER BETWEEN STATION 160-200, RB L 42-57,PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810044 1 20081006 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 LEFT CUSP CRACKED AT STATION 227. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16 2 L 7 2 4F RT A6WE 20081125 NM 2008 11 25 SWAA086442 1 20081120 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 600WN 27694 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, STR 8R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086443 1 20081120 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 HALA2008111900860 1 20081119 A 5330 SKIN BOEING 767 76733A 1385209 NM BS 1777 PUNCTURED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 589HA 33422 OPEN - HOLE PUNCHED IN BELLY OF FUSELAGE AT STA 1777 BETWEEN STRINGERS S-36L AND S-36R. HOLE MEASURES 4" LONG BY 3" WID E. OK TO CONTINUE PER HALM105 FILE NR 589034. 2 L 7 2 4F RT A1NM 20081125 WP 2008 11 25 AALA200810033 1 20081017 A 5340 MOUNT DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 CORROSION TOP OF FORWARD OUTBOARD GALLEY TIE DOWN FITTING. REPLACED FORWARD OUTBOARD OUTBOARD GALLEY MOUNT PER SRM 51-0 0-00. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810064 1 20081001 A 5322 SHEAR TIE DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 SHEAR TIE IS CRACKED BETWEEN LONGERON 1 AND 2 RIGHT AFT SIDE OF FRAME. REPAIRED PER ESO 80559 DATED 10/1/08. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 SWAA086339 1 20081118 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 304, WL 259. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086409 1 20081118 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 520, O/B OF LT KEEL BEAM. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086362 1 20081118 A 5511 6573721 RIB BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND LT HORIZONTAL STABILIZER L/E OUTBOARD RIB UPPER AFT CORNER CRACKED. REMOVED AND REPLA CED RIB PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086342 1 20081118 A 5310 6545768 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED SPV CHECK, FOUND FWD CARGO DOOR CUTOUT AFT FRAME CRACKED AT LOWER STOP FITTING. REMOVED AND REPLACED F RAME SECTION PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086419 1 20081120 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 735SA 27867 DURING SCHEDULED HC2 CHECK, FOUND EEPLS STRIP INOP AT ROW 11. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086468 1 20081121 A 5330 6545778 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081125 EU 2008 11 25 USAA920081991 1 20081030 A 3397 CONNECTOR AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHT DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AW 076 FLT NR 347 LAS-PHX EMERGENCY LIGHT ESCAPE PATH LIGHT AT ROW 1L INOPERATIVE. RECONNECTED CONNECTOR AT WALL 1L. OPS CHEC K WAS GOOD. 2 L 7 2 4F RT A28NM 20081125 NM 2008 11 25 USAA920081999 1 20081008 A 5340 6935350 STRINGER CLIP BOEING 737 7373G7 138447J NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL C21 MAJOR REPAIR NR 6062377 TIE CLIP CRACKED AT BS 400, S28L. REPLACED TIE CLIP AT BS 400, S28L IAW B737 SRM 51-40- 02 AND BOEING DRAWING NR 6546526. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086471 1 20081121 A 5330 6545775 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR SKIN CUTOUT CRACKED AT BS 794, RBL 49. REPAIRED SKIN PER ACO. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 NWAA084816308 1 20081027 A 5330 SKIN BOEING 747 747451 1384940 NM BS 2090 S36R CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK FOUND CRACK IN SKIN AT LAVATORY VACUUM EXHAUST HOLE AT BS 2090 S36R. REPAIRED PER EA 63-214334. 2 L 7 4 4F RT A20WE 20081125 NM 2008 11 25 SWAA086472 1 20081121 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727B, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM . 2 L 7 2 4F RT A16WE 20081125 EU 2008 11 25 NWAA084883304 1 20081031 A 3350 BATTERY PACK AIRBUS 330 A330323 3940030 EU EMERGENCY LIGHT FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 804NW 0549 BATTERY EPSU 17WL DOOR 4L FAILED CAPACITY CHECK, REPLACED BATTERY AND TESTS OK. 2 L 7 2 4F RT A46NM 20081125 EU 2008 11 25 COEA0805742 1 20081016 A 7997 CONNECTOR FOKKER F27 F27MK600 4990706 EU OIL PRESS XMITER DIRTY A COEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 NM 13 742FE 10349 RETURN TO BLOCKS. FLIGHT NR 7757 MAF TO LBB. DURING TAXI OUT TO THE RUNWAY, THE RT ENG OIL PRESSURE GAGE BEGAN TO FLUC TUATE THEN DROPPED INTO THE RED. ACFT WAS SAFELY TAXIED BACK TO BLOCKS. MX FOUND THE CONNECTIONS AT THE OIL PRESS TRAN SMITTER DIRTY. CLEANED CONNECTIONS AT THE RT ENGINE OIL PRESSURE TRANSMITTER. 2 H 7 2 4T A817 20081125 WP 2008 11 25 NWAA084859873 1 20081103 A 3397 CONNECTOR DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT DAMAGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 782NC 48107 DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 19-22 OF THE CABIN AND IN THE TAIL COMPARTMENT W ERE INOPERATIVE. MX REPAIRED THE CONNECTOR FOR THE WIRE HARNESS AT THE SIDEWALL AND FUNCTIONALLY CHECKED THE SYSTEM. 2 L 7 2 4F RT A6WE 20081125 NM 2008 11 25 SWAA086478 1 20081121 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086479 1 20081121 A 5310 655227134 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND LT CREASE BEAM WEB CORRODED BETWEEN BS 500B TO BS 500C, WL 208. REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086483 1 20081121 A 5330 6545775 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND AFT CARGO DOOR EXTERNAL SKIN CRACKED AT UPPER AFT CORNER CUTOUT. REPAIRED SKIN PER SW A EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086484 1 20081121 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086485 1 20081121 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086494 1 20081120 A 5755 LUG BOEING 737 7373H4 1384600 NM SPOILER BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 646SW MA3202 28331 DURING SCHEDULED MV2 CHECK, FOUND RT WING I/B GROUND SPOILER LUG BROKEN. REMOVED AND REPLACED SPOILER PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086495 1 20081121 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 500B, STR 27L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086496 1 20081121 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 480 + 10, STR 26L. REMOVED AND REPLACED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 USAA920081997 1 20081021 A 5754 SKIN BOEING 737 737301 1384611 NM ZONE 600 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 229 23739 CLT Q3 MAJOR REPAIR NR 03C40257009/009 DELAMINATED AREA ON NR 5 SLAT TRAILING EDGE WEDGE OTBD END. REPAIRED NR 5 SLAT T RAILING EDGE IAW B737 SRM 51-70-10, REPAIR NR 4. 2 L 7 2 4F RT A16WE 20081125 EA 2008 11 25 COMA0860454 1 20081106 A 5330 60034014 SKIN CNDAIR CL600 CL6002B19 1900309 EA BS 235 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 783CA 7315 RT FUEL SKIN IS CRACKED AT FS 235 IN THE RT AFT RADIUS OF THE NLG CUTOUT. REMOVED DAMAGED SKIN AND INSTALLED PERMANENT REPAIR PER BOMBARDIER AEROSPACE REO 601R-53-11-048. 2 L 7 2 4F RT A21EA 20081125 EA 2008 11 25 COMA0860456 1 20081106 A 5210 601R31902455 FRAME CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 783CA 7315 PAX DOOR AFT INNER FRAME AT FS 338.9 IS CRACKED. REMOVED DAMAGED PORTION OF FRAME AT FS 338.9, FABRICATED AND INSTALLED SERVICEABLE REPAIR PARTS PER CRJ REO 601R-52-11-402 REV H. 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 USAA920081994 1 20081031 A 5320 6545807 SUPPORT ANGLE BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753006/002 FUSELAGE FRAME SUPPORT ANGLE CRACKED AT BS291.5 ABOVE S16R. REPAIRED FUSELAGE FR AME SUPPORT ANGLE AT BS291.5 ABOVE S16R IAW B737 SRM 51-40-02 AND BOEING DRAWING NR 6545807. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 USAA920081996 1 20081031 A 5311 65C22908 FRAME BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03-0553-8-0546/001 FUSELAGE FRAME/SIDE FRAME CRACKED AT BS 500C BELOW S13L. REPAIRED FUSELAGE FR AME/SIDE FRAME AT BS500C BELOW S13L IAW US AIRWAYS TYPICAL REPAIR NR 53-10-21A. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 USAA920081943 1 20081023 A 5311 6546534 FRAME BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03-0553-8-0546/003 CRACK IN FRAME/SIDE FRAME AT BS520 BELOW S13L. REPAIRED FRAME/SIDE FRAME AT B S520 BELOW S13L IAW US AIRWAYS TYPICAL REPAIR 51-10-21A. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086504 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 5L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086508 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 USAA920081921 1 20081013 A 5754 SKIN BOEING 767 767201 1385125 NM NR 3 SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245AY 23897 BFM MAJOR REPAIR C3 CHECK NR 6013567 LT WING NR 3 SLAT UPPER SURFACE DELAMINATED OTBD END. REPAIRED LT WING NR 3 SLAT U PPER SURFACE OTBD END IAW B767 SRM 57-43-01. 2 L 7 2 4F RT A1NM 20081125 NM 2008 11 25 2ARF 20081101 1 20080920 A 2421 GENERATOR DOUG MD80 MD83 3023681 NM RIGHT MALFUNCTIONED W 2ARF B A EMER. DESCENT UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SW 23 838AM 49397 ACFT RETURNED, DUE TO ACFT CROSS TIE AND RT GENERATOR FAILED. CAPTAIN REPORTED THAT THE LANDING WAS WITH EMERGENCY POWER AND WITHOUT FLAPS/SLATS EXTENDED, MAINT PERFORMED AC CROSS TIE AND RT GENERATOR TEST IAW AMM 24-20-00, ALL CORRECT. FLA PS/SLATS CONTROL SYS WAS TESTED IAW AMM 27-50-00 ALL CORRECT. THE OVERWEIGHT INSP WAS PERFORMED IAW AMM 05-51-04, NO DAM AGES WERE FOUND. 2 L 7 2 4F RT 20081125 NM 2008 11 25 SWAA086509 1 20081121 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BETWEEN BS 847 TO BS 867, RBL 65, WL 207. REPAIRED WEB PE R SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086512 1 20081121 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FLOOR SUPPORT BEAM CORRODED AT BS 859, RBL 3. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086514 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 807, STR 26R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 PCSA2008111101 1 20081111 A 7932 3910201001 TRANSMITTER BOEING 727 7272F9 138407D NM PWA JT8 JT8D17A 52049 NE NR 3 ENGINE FAILED A PCSA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 SO 17 199AJ 21426 715306 ON DESCENT IN SDQ OIL QUANTITY GAUGE NR 3 BLED SLOWLY DOWN TO ZERO QUANTITY. OIL PRESSURE AND TEMPERATURE NORMAL BUT WE RE VERY LIGHT SO A PRECAUTIONARY ENGINE SHUTDOWN WAS DONE. A NORMAL LANDING WAS PERFORMED. AFTER LANDING OIL QUANTITY CHECKED FULL. ENGINE WINDMILL TIME 20 MINUTES AT 22 PSI OIL PRESSURE. MAINTENANCE CHECKED THE MAIN OIL FILTER AND CHIP DETECTORS, NO METAL FOUND. REPLACED OIL QUANTITY TRANSMITTER OPERATED ENGINE OIL PRESSURE TEMPERATURE AND QUANTITY IND ICATIONS WERE NORMAL. 2 L 7 3 4F 4 F RT A3WE E2EA 20081124 2008 11 24 UALA2008112006596 4 20081120 A 3425 S231T1106 INDICATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT FAILED A UALA K NONE O OTHER UK UNKNOWN 1 WP 29 661UA 27158 STBY ATTITUDE INDICATOR INOP. FLT DIVERTED. STBY ADI IS DRIFTING AWAY FROM PROPER ATTITUDE. REPLACED STANDBY ATTITUDE INDICATOR. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 2008 11 24 UALA2008112006597 4 20081118 A 3417 0856LU5 PROBE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEFT FAILED A UALA K NONE O OTHER TO TAKEOFF 1 WP 29 663UA 27160 LT ASI DURING TAKEOFF ROLL WENT TO ZERO KNOTS. REPLACED LT PITOT STATIC PROBE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 CE 2008 11 24 Z5F2008F00007 1 20081009 A 2611 SMOKE WARNING CESSNA 525 525B 2076616 CE CARGO BAY MALFUNCTIONED E Z5FA K NONE N FALSE WARNING CL CLIMB 1 EA 63 418CS 525B0108 CLIMBING THROUGH FL250, BAGGAGE SMOKE LIGHT CAME ON. STAYED ON THROUGH LANDING. DIVERTED PERFORMED FUNCTIONAL CHECK OF BOTH FWD AND AFT SMOKE DETECTORS, THEY CHECKED GOOD. REMOVED INSPECTED AND REINSTALLED BOTH SMOKE DETECTORS, INSPECTED WIRING ADJACENT TO BOTH DETECTORS NO DEFECTS NOTED. SMOKE DETECTION SYSTEMS CHECKS NORMAL AND AIRCRAFT RETURNED TO SERV ICE. (K) 1 L 7 2 4F RT A1WI 20081124 CE 2008 11 24 YAA2008F00000 1 20081105 A 7810 K12502632 COLLECTOR CESSNA 207 207A 2073604 CE EXHAUST CRACKED E YAAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 AL 03 6470H 824 20700534 PILOT REPORTED SMOKE IN COCKPIT AFTER TAKEOFF, HE LANDED ACFT SAFELY AND TAXIED TO MAINT HANGER. MAINT FOUND HOLE AND C RACK IN EXHAUST NEAR HEATER MUFFLER. REMOVED AND REPLACED LT EXHAUST COLLECTOR, RAN UP ENGINE, FOUND OK FOR SERVICE AL L AD`S ON EXHAUST ARE CURRENT, NORMAL EXHAUST FAILURE THAT WOULD HAVE BEEN CAUGHT AT NEXT 100 HR INSP. ACFT WAS 30 HRS AWAY FROM NEXT 100 HR. (K) 1 H 7 1 3O A16CE 20081124 WP 2008 11 24 WRLA2008089 1 20080827 A 5330 SKIN DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 139WA 46583 DURING C1 INSPECTION FOUND FASTENER HOLE CORRODED AT STA 2160 BETWEEN LONGERON 13L-14L. REAMED HOLE TO REMOVE DAMAGE, E DDY CURRENT INSPECTION ACCOMPLISHED, MFG AND INSTALLED BUSHINGS AND REPAIR DOUBLER, TREAT, PRIME, SEAL AND PAINT IAW ENG INEERING REPAIR. (K) 2 L 7 3 4F A22WE 20081124 WP 2008 11 24 WRL2008F00010 1 20080827 A 5330 SKIN DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 139WA 46583 DURING C1 INSPECTION FOUND FASTENER HOLE CORRODED AT STA 2160 BETWEEN LONGERON 13L - 14L. REAMED HOLE TO REMOVE DAMAGE, EDDY CURRENT INSPECTION ACCOMPLISHED, MFG AND INSTALLED BUSHINGS AND REPAIR DOUBLER, TREAT, PRIME, SEAL AND PAINT IAW E NGINEERING REPAIR. (K) 2 L 7 3 4F A22WE 20081124 NM 2008 11 24 UIEA200800328 1 20081012 A 5320 PANEL BOEING 747 747228F 1384895 NM NLG WW CRACKED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 NOSE WHEEL WELL LT SIDE AT STA 273.0, WATER LINE 160 HAS A 0.250 INCH CRACK DETECTED WITH HFEC INSPECTION. INTERM REPAI R WAS ACCOMPLISHED IAW SRM 53-10-04, FIG 116, SHEETS 1 THRU 6. INITIAL AND REPEAT INSPECTION TO BE ACCOMPLISHED AT 15,0 00 FC AND THERE AFTER AT 4,000 FC. EO NR 4753B214. (K) 2 L 7 4 4F RT A20WE 20081125 WP 2008 11 25 AALA200810075 1 20081016 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 LEFT CUSP HAS CORROSION AT STATION 505 TO 509. REMOVED CORROSION, INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810086 1 20081016 A 5340 BRACKET DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 AFT CARGO DOOR LOWER FORWARD CORNER CORROSION ON BRACKET AT STATION 1155. INSTALLED NEW BRACKET PER SRM 51-10-01. 2 L 7 2 4F A6WE 20081125 EA 2008 11 25 SWIA200820403 1 20080808 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 443SW 7638 C-CHECK, RIGHT ENGINE THRUST FITTING CORRODED, REPLACED. 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 SWAA086437 1 20081120 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 385SW 26600 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086354 1 20081118 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086355 1 20081118 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086338 1 20081118 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 305, WL 262. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081125 2008 11 25 SWAA086418 4 20081120 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086387 1 20081119 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CRACKED AT BETWEEN BS 430 TO BS 440, STR 28R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086470 1 20081121 A 5330 6545775 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND AFT CARGO DOOR SKIN CUTOUT CRACKED AT BS 794, BETWEEN STR 21R TO STR 26R. REPAIRED SK IN PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086473 1 20081121 A 5712 6545455 RIB BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND LT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 TO STR 3. REPAIRED RIB PE R ACO. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086486 1 20081121 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086497 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 27L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086501 1 20081121 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT O/B TRAILING EDGE UPPER SURFACE DELAMINATED. REMOVED AND REPLACED S LAT PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086503 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 4R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086511 1 20081121 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FLOOR SUPPORT BEAM CORRODED AT BS 859, RBL 8. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086519 1 20081121 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND R1 DOOR FUSELAGE SKIN CRACKED AT BS 290. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086520 1 20081121 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT O/B TRAILING EDGE UPPER SURFACE DELAMINATED. REMOVED AND REPLACED S LAT PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086522 1 20081121 A 3350 65C34691 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND RT BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 8. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081125 EU 2008 11 25 VQI2008F00005 1 20081030 A 2120 UNKNOWN AIRBUS 320 A320214 3930316 EU CABIN ODOR A VQIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 15 632VA 3155 FLT DIVERTED DUE TO ODOR IN CABIN AROUND SEAT ROWS 4 TO 7. AT ABOUT 10,000 FT & CLIMBING ODOR FIRST NOTICED BY FLT TEAM MEMBER & THEN DISAPPEARED. LATER, AT ABOUT 30,000 FT ODOR RETURNED. REPORTED IT TO BE LIKE ELECTRIC OR PLASTIC ODOR & THAT IT WAS STRONG. CAPTAIN TO DIVERTED FOR INVESTIGATION. ODOR AGAIN DISAPPEARED BEFORE ARRIVAL. ACCOMPLISHED VISUAL INSPECTION OF E&E BAY, FWD CARGO BIN, CABIN CEILING PANELS AND PSU`S IN AFFECTED AREA. NO FINDINGS REF AMM 25-23-41-04 , TSM 24-00-00-810-823. ACCOMPLISHED CABIN TEMP CONT SYS TEST. OPS OK IAW 21-63-00-710-004. PLACED IFE SYS INOP AS PR ECAUTION. ACFT RETURNED TO SERVICE & WITH NO FURTHER OCCURRENCE. FURTHER INSP & CHECKS CARRIED OUT, NO DEFECTS FOUND. 2 L 7 2 4F RT A28NM 20081125 NM 2008 11 25 SWAA086523 1 20081121 A 2560 65C16820 HOOK BOEING 737 7373H4 1384600 NM GIRT BAR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR SLIDE AFT GIRT BAR HOOK LOOSE. REMOVED AND REPLACED HOOK PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086527 1 20081121 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086528 1 20081121 A 5311 6546538 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 597, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086529 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND STRNGER CLIP CRACKED AT BS 827, STR 6. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086427 1 20081120 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STR 26L CORRODED AT BS 936. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081125 EA 2008 11 25 ASOA200801278 1 20081003 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REPAIRED RT FS 280 FLOOR SUPPORT ANGLE AT RBL 9.0 IAW ASA REO 601R-53-11-926. NO FURTHER ACTION REQUIRED. SUPPLEMENTAL -SDR CLOSED 11/13/2008. 2 L 7 2 4F RT A21EA 20081125 EA 2008 11 25 ASOA200801279 1 20081003 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REPAIRED FS 280 FLOOR SUPPORT ANGLE P/N 600-34017-595 AT LBL 9.0 IAW ASA REO 601R-53-11-926. NO FURTHER ACTION REQUIRED . SUPPLEMENTAL-SDR CLOSED 11/13/2008. 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 SWAA086451 1 20081121 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BETWEEN BS 847 TO BS 867, RBL 65. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086452 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 6R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086453 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 420, STR 7R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121792255 1 20081216 A 5312 BULKHEAD BOEING 737 737401 138449B NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 23876 PIT - FPBH - MAJOR REPAIR - FORWARD PRESSURE BULKHEAD CRACKED ON FORWARD FACE BS 178, WL 234, RBL 9. REPAIRED FORWARD P RESSURE BULKHEAD AT BS 178, WL 234, RBL 9 IAW B737 SRM 53-10-08 & ENGINEERING ORDER 5300153. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121992274 1 20081218 A 5320 6545834107 STRAP BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - LOWER STABILIZER STRAP CRACKED AT BS 344, LBL 44. REPLACED LOWER STABILIZER STRAP AT BS 344, LBL 44 IAW SRM 51-10-02 & DRAWING 65-45834. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 UALA2008111301965 1 20080405 A 3150 WARNING MESSAGE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE ILLUMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 772UA 26930 FOUND FLT CONTROL SYS STATUS MESSAGE LATCHED WITH NO CORRELATED MESSAGES. FOUND MESSAGE 31-54102. RPL IOM M004, NO HEL P. SUSPECT ARINC 629 COUPLER B31208 IN P212 PANE. *NOTE* TURNED ON ALL HYD SYS PER MT 27-005-R1, NO HELP. *NOTE* MS G CAN BE CLEARED BY DOING RT AIMS M004 RESET, BUT, FLT CONTROL SYS STATUS MESSAGE DOES NOT CLEAR. REPLACED ROBBED ADIRU AND UPDATED SOFTWARE, NO HELP. SWAPPED COUPLER B31208 AND RT AIMS M004 WITH LT AIMS M004, NO HELP. RANG OUT WIRING IN BETWEEN COUPLER AND RT AIMS. ALL OK. MSG STILL ACTIVE WITH NO CORRELATED FAULT. PUT SWAPPED AIMS UNIT BACK TO NORMAL . TRIED NEW FCDC BATTERY, SWAPPED LT AND CENTER PRIMARY FLIGHT COMPUTERS, NEW PSA, PROBLEM SEEMS TO BE ON CENTRAL BUSS 2 L 7 2 4F 4 F RT T0001SE E46NE 20081224 EA 2008 12 24 COMA2008122250042 1 20081222 A 5320 601R5341260 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 927CA 35573 7031 CRACK FOUND IN RADIUS OF ANGLE AT FS 559.00 LBL 18.00. REPAIRED IAW REO 601R-53-41-260. 2 L 7 2 4F RT A21EA 20081224 NM 2008 12 24 UPS08554215 1 20081218 A 3231 26702887 DOOR BOEING 757 75724APF 1384969 NM NLG INOPERATIVE A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 403UP 23725 INSPECTION TYPE:N/A ATB - AFTER TAKEOFF CREW REPORTED GEAR WOULD NOT RETRACT. GEAR DISAGREE & GEAR DOOR LIGHT ILLUMINAT ED (AIRFRAME VIBRATION) LEVEL OFF AT 5000. GEAR RETRACTS AT 5000 WITH LIGHTS EXTINGUISHED. GEAR DEPLOYED NORMALLY UPON LANDING. REPLACED NOSE GEAR DOOR. 2 L 7 2 4F RT A2NM 20081224 NM 2008 12 24 SWAA087264 1 20081221 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM BS 727D S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 SWAA087265 1 20081221 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE DOUBLER. REMOVED AND REPLACED SKIN PER S RM. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 SWAA087266 1 20081220 A 3350 8200048901 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 288WN 36611 DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY LIGHT LENS MISSING AT ROW 1. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 SWAA087267 1 20081220 A 3350 65C27093 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 303SW 22943 DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081222 CE 2008 12 22 GUUA93332121408B 1 20081214 A 3240 BRAKE BEECH 1900 1900D 1154162 CE MLG INOPERATIVE A GUUA O OTHER S AFFECT SYSTEMS TX TAXI/GRND HDL 1 SO 29 81533 UE137 FLIGHT NR 9246 MHH/FLL AFTER LANDING RT BRAKE INOPERATIVE. BOTH CAPTAIN AND FIRST OFFICER RT BRAKE HAS NO RESISTANCE. PEDAL GOES STRAIGHT TO THE FLOOR. PERFORMED BRAKE BLEEDING. OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 20081222 2008 12 22 DXTA2008121603403 4 20081215 A 2210 AUTOPILOT SYS CESSNA 680 680CE 2076811 CE MALFUNCTIONED E DXTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 372QS 6800201 AFTER DEPARTING CMH THE AP FAIL B MSG FLICKERED THEN ILLUMINATED SOLID. 2 L 7 2 4F RC T00012WI 20081222 NM 2008 12 22 UPS08554199 1 20081215 A 5321 143N545714 FLOOR PANEL BOEING 757 75724APF 1384969 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 466UP 25482 INSPECTION TYPE:N/A 2ND PANEL FROM RT SIDE 17 INCHES FROM AFT OF PANEL STA 440 SEC 43 POS 4 DAMAGE CONSIDERED AS ONE 4 I NCH DIA TOP SKIN AND CORE. REPLACED PANEL. 2 L 7 2 4F RT A2NM 20081222 EA 2008 12 22 COMA2008121650028 1 20081208 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING MALFUNCTIONED A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 27 806CA 7359 ON APPROACH INTO YUL RECEIVED FLAPS FAIL CAUTION MSG AT 0 DEG WHEN SELECTING 8 DEG. EMERGENCY DECLARED, A/C LANDED SAFE LY. COMPLIED WITH TASK CARD SI-2-27I0001, FLAPS FAIL FIRST EVENT MAINTENANCE ACTION. 2 L 7 2 4F RT A21EA 20081223 2008 12 23 HALA2008121400883 4 20081214 A 2310 9640452012 TRANSCEIVER BOEING 767 76733A 1385209 NM HF SYSTEM MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, TRANSMISSIONS ON RT HF INTERMITTENT AT ALL STATIONS. REMOVED AND REPLACED NR 2 HF TRANSCEIVER GRND CHK OK PER AMM 23-11-03. 2 L 7 2 4F RT A1NM 20081223 EA 2008 12 23 MASA2008121600745 1 20081216 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR FALSE ACTIVATION A MASA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 650ML 7137 ASH FLT 7110 MLI-ORD. CREW REPORTED GETTING THE PASSENGER DOOR WARNING MESSAGE IN FLIGHT AFTER TAKEOFF WITH NO PRESSURI ZATION ISSUES. CONTRACT MX PERFORMED PSEU TEST AND PRESSURIZATION CHECK OF THE DOOR AND INDICATION SYSTEM WITH NO FAULT S FOUND. 2 L 7 2 4F RT A21EA 20081223 EA 2008 12 23 MASA2008121600746 1 20081216 A 5270 SENSOR CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR MALFUNCTIONED A MASA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 650ML 7137 ASH FLT 7148 TVC. PASSENGER DOOR WARNING IN FLIGHT, CREW REPORTED MESSAGE CLEARED ON GROUND WITH NO PRESSURIZATION ISSU ES IN FLIGHT. MX REMOVED AND REPLACED DOOR SENSORS. 2 L 7 2 4F RT A21EA 20081223 WP 2008 12 23 ABXA200812190271 1 20081215 A 3350 41B004AD07G3 BATTERY PACK DOUG DC9 DC941 302207N WP EMERGENCY LIGHTS DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 953AX 47608 DURING PRE-DEPARTURE CHECK, FOUND COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 AMM 33-53-02-4. 2 L 7 2 4F A6WE 20081223 NM 2008 12 23 UALA2008121706912 1 20081216 A 2710 550030019 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE AILERONS FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 652UA 25390 THE "AIL LOCK" LT ON AT LOW SPEED. EICAS MSG AILERON LOCKOUT DISPLAYED. REPLACED RIGHT WING AILERON LOCKOUT ACTUATOR. REPLACED RT WING AILERON LOCKOUT ACTUATOR. TESTED NORMAL. RECEIVED SAME EICAS SEVERAL FLIGHT SEGMENTS LATER. REPLACE D RIGHT SAM AND RT ADC (P/N S242T210-211). MCDP TEST 30 AND 65 CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081223 NM 2008 12 23 SWAA087275 1 20081221 A 3397 81000 WIRE BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT EXPOSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 473WN 33832 FWD EEPLS WIRE EXPOSED AT ROW 1. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087276 1 20081220 A 3350 417N5212 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 491WN 33867 FWD CABIN EEPLS LIGHT LENS BROKEN. REMOVED AND REPLACED END CAP PER MM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087277 1 20081221 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM BS 760 S22L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 510SW 24187 DURING SCHEDULED MV3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087278 1 20081221 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087280 1 20081220 A 3350 3005931 LENS BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081223 EA 2008 12 23 COMA2008121750032 1 20081212 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA ZONE 500 DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 785CA 23029 7326 LT WING LOWER DRAIN ATTACHMENT HOLE JUST FWD OF PANEL 540 AB, AT WS 67.75 AFT SCREW HOLE IS DAMAGED. REPAIRED DAMAGE PE R EA 10-57-02437. 2 L 7 2 4F RT A21EA 20081224 WP 2008 12 24 AALA200810523 1 20081203 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 CORROSION ON NUMBER 1 SEAT TRACK STATION 1278. INSTALLED REPAIR PLUG PER SRM 53-05-4A. 2 L 7 2 4F A6WE 20081224 WP 2008 12 24 AALA200810531 1 20081206 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 RIGHT CUSP CRACKED STATION 800. INSTALLED A SERVICEABLE CUSP SHEET PER SRM 51-01. 2 L 7 2 4F A6WE 20081224 NM 2008 12 24 USAA2008121792252 1 20081211 A 5320 VERTICAL BEAM BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - CRACK IN VERTICAL BEAM WEB AT BS 184.0321, LBL 17, WL 233. REPAIRED VERTICAL BEAM WEB AT BS 18 4.0321, LBL 17, WL 233 IAW B737 SRM 53-10-08 & ENGINEERING ORDER 5312-01008. 2 L 7 2 4F RT A16WE 20081224 EU 2008 12 24 USAA2008121992279 1 20081204 A 5340 D53112798201 FITTING AIRBUS 320 A320232 3930326 EU ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - C8 - MAJOR REPAIR - GALVANIC CORROSION ON FITTING BETWEEN FR16 TO FR20, WL -Z520. REPLACED FITTING BETWEEN FR16 T O FR20, WL -Z520 IAW SRM 51-72-17. 2 L 7 2 4F RT A28NM 20081224 NM 2008 12 24 USAA2008121892268 1 20081210 A 5320 VERTICAL BEAM BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - CRACKS IN VERTICAL BEAM WEB AT BS 179, WL 227, RBL 17. REPAIRED VERTICAL BEAM WEB AT BS 179, WL 227, RBL 17 IAW B737 SRM 53-10-08. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 UALA2008111302518 1 20080430 A 3233 65446104 LINE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NLG ACTUATOR FAULTY A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 375UA 24640 PER CAPTAIN NOSE GEAR DID NOT RETRACT. MAIN IND WAS GREEN AND NOSE WAS RED. CYCLED GEAR, NO HELP. SUSPECT AN INTERNAL PROBLEM WITH "NOSE GEAR MODULE PACKAGE". ATTACH BOLTS REMOVED AND LINES "BROKEN" ON MODULE, READY FOR REPLACEMENT REPL ACED NOSE GEAR MODULE AND SELECTOR VALVE, NO HELP. REPLACED NOSE GEAR ACTUATOR AND NOSE GEAR RETRACT PRESSURE FUSE. OP S CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E21EU 20081224 NM 2008 12 24 UALA2008111302584 1 20080504 A 5320 CHANNEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 360 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 STR CLIP STA 360 AT 14L,10L, 8L-STA 360 STR 15L CHANNEL STA 348 STR 16L TIE STA 294 STR 13L,11L CLIP STA 294 STR 7L INTE RCOSTAL WEB AND STA 294 STR 7L AUX INTERCOSTAL CRACKED. MAJOR REPAIRS. ALL REPAIRS ACP PER REO-L01068 AND UA-EVA-71520 . TO BE REINSPECTED WITHIN 6000 CYCLES AND EVERY 6000 CYCLES THEREAFTER. REPAIRS APPROVED VIA BOEING 8100-9. 2 L 7 2 4F 4 F RT A16WE E21EU 20081224 NM 2008 12 24 UALA2008111302585 1 20080503 A 5340 STRINGER CLIP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 360 S9 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 312UA 23673 CRACKED CLIPS AT S-9L, BS 360 AND AT S-10L, BS 360. THE INTERIM REPAIR IS APPROVED BY AD 2005-20-03 BY FAA FORM 8100-9. THE REPAIR STRUCTURE WILL BE RE-INSPECTED PER SB 737-53A1204 STARTING AT 38,165 PTC AND REPEATED EVERY 6,000 FLIGHT CY CLES THEREAFTER. REPAIRED REF SRM 51-40-02 AND EVA 71519 ON NR K4083G AND K4082G. 2 L 7 2 4F 4 F RT A16WE E21EU 20081124 NM 2008 11 24 KNNA200800104 1 20081119 A 5340 STRINGER CLIP BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 465AT 21528 STRINGER CLIP WAS CRACKED AT STA 639, STRINGER 1L. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 KNNA200800105 1 20081119 A 5340 STRINGER CLIP BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A KNNA K NONE O OTHER IN INSP/MAINT 1 WP 25 465AT 21528 FOUND STRINGER CLIP CRACKED AT STA 639, STRINGER 3L. 2 L 7 2 4F RT A16WE 20081124 EA 2008 11 24 N6WA200811091 1 20081109 A 5270 WARNING LIGHT CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY EXIT INTERMITTENT A N6WA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 03 152GJ 10218 LEFT EMERGENCY DOOR LIGHT INTERMITTENT EICAS CAUTION. DEFERRED DOOR INDICATION SYSTEM PER MEL 52-70-03. 2 L 7 2 4F RT A21EA 20081124 NM 2008 11 24 UALA2008112006583 1 20081120 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN BROKEN A UALA K NONE O OTHER UK UNKNOWN 1 WP 29 782UA 26948 SEAT 1F EMERGENCY LIGHT BROKEN. REPLACED LIGHT ASSY & CHECKS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081124 NM 2008 11 24 UALA2008112006588 1 20081118 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 551UA 25399 LAV K FLOOR PATH LIGHT STRIP INOP. REPLACED FLOOR PATH LIGHT STRIP. 2 L 7 2 4F 4 F RT A2NM E17NE 20081216 NM 2008 12 16 UALA2008111305408 1 20080821 A 3260 SWITCH BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RT MLG FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 669UA 30025 RIGHT MAIN GEAR INDICATOR LIGHT INOP WILL ILLUMINATE WHEN WIGGLED. REPLACED RIGHT GEAR DOWN INDICATOR LIGHT KORRY SWITC H, CONDITION NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081202 NM 2008 12 2 UALA2008111306395 1 20081106 A 2612 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FIRE WARNING INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 583UA 26705 RT FIRE LIGHT DOES NOT ILLUMINATE DURING FIRE TEST. REPLACED LAMP. 2 L 7 2 4F 4 F RT A2NM E17NE 20081202 EU 2008 12 2 UALA2008111306403 1 20081106 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 448UA 842 FUSELAGE STR 43RT AT FR67 + 2 HAS EXCESSIVE MAT'L LOSS FROM GRINDING. MAJOR REPAIR. STRINGER TO BE REPLACED. REPLACE BELLY SKIN FRAME 64-70 STR 40R-31L. REMOVED DAMAGED STRINGER & REPLACED WITH NEW. 2 L 7 2 4F 4 F RT A28NM E40NE 20081124 NM 2008 11 24 UALA2008112006581 1 20081118 A 5210 JAM-NUT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR LOOSE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 514UA 24839 NR 1 RT PASSENGER DOOR - COCKING PUSHROD ROD END JAM NUT LOOSE - REQUIRES ADJUSTMENT. RED DANGER TAG ATTACHED FROM PREV IOUS VISIT WARNING TO ADJUST AND SAFETY. ROD END LOCATED FWD OF INTERNAL DOOR HANDLE MECHANISM. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 NM 2008 11 24 UALA2008112006598 1 20081119 A 3350 276005 FUSE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BATTERY CHARGER INTERMITTENT A UALA K NONE O OTHER CR CRUISE 1 WP 29 643UA 25093 EMERGENCY EXIT LIGHTS ON INTERMITTENTLY AROUND DOOR 1L MAINT TEXT: VERBAL REPORT FROM FLT ATTENDANT, ONLY THE LWR EXIT SIGN AT DOOR 1L AND THE TWO ESCAPE LIGHTING RIBBONS ILLUMINATED FOR A BRIEF TIME, TWICE IN FLT. REPLACED FUSE IN BATTER Y CHARGER. CHECKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 NM 2008 11 24 UALA2008112006599 1 20081027 A 3350 FUSE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 RT OVERWING 2 AFT EEL LIGHTS INOP. REPLACED FUSE IN BATTERY CHARGER. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008112006603 1 20081120 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INTERMITTENT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 173UA 24380 EXIT LIGHT BELOW PROTECTION HANDLE AFT OF 2L FLICKERS. EXIT LIGHT ON-OFF CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008112006590 1 20081118 A 3510 214C401110 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CREW O2 FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 THE O2 SYSTEM FAILS ALTITUDE SWITCH, OPS CHECKS. REPLACED ALTITUDE PRESSURE SWITCH, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 NM 2008 11 24 UALA2008112006591 1 20081119 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 AFT PIT AT STA 1520, STR 26L FRAME DENTED AT INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED FRAME SECTION AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 NM 2008 11 24 UALA2008112006593 1 20081118 A 3510 MXP147 OXYGEN SYSTEM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE O2 BOX FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 87UA 26713 CAPT O2 RESET - TEST SLIDE STICKS IN TEST POSITION. REPLACED O2 BOX PER MM 35-11-51. 2 L 7 2 4F 4 F RT A2NM E17NE 20081224 NM 2008 12 24 USAA2008121792260 1 20081123 A 5320 655287812 ANGLE BOEING 737 7373G7 138447J NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - CRACK ON SUPPORT ANGLE OF FLOOR STRUCTURE BETWEEN BS 967 TO BS 986.5, LBL 68.6 AT L2 DOOR ARE A. REPLACED SUPPORT ANGLE OF FLOOR STRUCTURE IAW SRM 51-40-02-0G. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121792262 1 20081216 A 5312 BULKHEAD BOEING 737 737401 138449B NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 23876 PIT - FPBH - MAJOR REPAIR - CRACK IN FORWARD PRESSURE BULKHEAD AT BS 178, WL 234, LBL 9. REPAIRED FORWARD PRESSURE BULK HEAD AT BS 178, WL 234, LBL 9 IAW SRM 53-10-08 & EO 5300153. 2 L 7 2 4F RT A16WE 20081224 WP 2008 12 24 AALA200802393A 1 20081025 A 3297 WIRE HARNESS DOUG DC9 DC982 3022082 WP ANNUN PANEL BROKEN A AALA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SW 21 7514A 49891 DFW INFLIGHT. LANDING GEAR INDICATIONS INOPERATIVE DURING APPROACH. PERFORMED GO-AROUND TO CONFIRM LANDING GEAR DOWN A ND LOCKED. LANDED DFW WITHOUT INCIDENT. FOUND BROKEN WIRE ON ANNUNCIATOR PANEL IN COCKPIT FOR LANDING GEAR INDICATION. REPAIRED WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081224 WP 2008 12 24 AALA200802387A 1 20081024 A 2560 P4010021 BATTERY DOUG DC9 DC982 3022082 WP FLASHLIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 422AA 49334 LGA - AFT GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY FOR AFT GALLEY EMERGENCY FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081224 NM 2008 12 24 ANCF200800030 1 20081210 A 3246 WHEEL BOEING 757 757236 1384971 NM MLG DAMAGED W ANCF K NONE O OTHER IN INSP/MAINT 1 SO 23 522NA 25133 DURING TAXI OUT RT MAIN GEAR GOT STUCK INTO THE PAVED AREA UNABLE TO CONTINUE TAXI. IAW AIRPLANE RECOVERY DOCUMENT 4-10 -3 AIRPLANE WAS TOWING OUT OF SOFT GND IAW AMM 32-00-10 PG 601. LANDING GEAR INNER CYLINDER CHROME INSPECTION CHECK ACC OMPLISHED AND FOUND NO DAMAGE OR EVIDENCE OF OIL LEAKS IAW AMM 32-41-10 PG 601. INSPECTION OF MAIN GEAR WHEEL BRAKE ACC OMPLISHED SATISFACTORY, AXLE FOUND NORMAL ON RT MLG AND NLG IAW AMM 32-45-01 PG 401. WHEEL NR 7 AND 8 WERE REPLACED AND FOUND WITH DEEP CUTS PRESS READS 180 PSI, RT MAIN LANDING GEAR LOWER COVER AFT INBOARD LAMP IS BROKEN: DUE NO STOCK THI S ITEM IS DEFERRED TO DMI4-15 ASPER MEL NEF X-7 CAT "D". RT MAIN LANDING GEAR AFT CONDUIT OF THE HARNESS ANTI SKID IS 2 L 7 2 4F RT A2NM 20081224 NM 2008 12 24 ASAA0874024 1 20081111 A 5720 115A29307 SUPPORT BRACKET BOEING 737 737790 13844CN NM LT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 R&R CRACKED SUPPORT BRACKET AT UPPER TRAILING FIXED PANEL RSS 261. 2 L 7 2 4F RT A16WE 20081224 2008 12 24 ASAA0854046 4 20081214 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM EE BAY WARNING MESSAGE A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 557AS 19965 35176 FMC DISAGREE ON GROUND FOLLOWED QRH. THE GROUND POWER CART HAD DROPPED OFF A COUPLE OF TIMES BEFORE THIS HAPPENED. GRO UNDED YES. COULD NOT DUPLICATE. PERFORMED FIM: 34 61 00/835 FMC RT & LT BITE CK NML & NO FAULTS LOGGED. NO HISTORY 60 DAYS & SEAMC ROB NOTIFIED GROUND VERIFICATION SUCCESSFUL. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 ASAA0874044 1 20081208 A 5720 115A2179Y4 SUPPORT BOEING 737 737790 13844CN NM RT WING DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 RT WING UPPER TE PANEL LWR SUPPORT FITTING AT RSS 277 HAS ELONGATED HOLES. REPLACED TE LOWER SUPPORT BEAM PER SRM 51-40 -05 AND REPAIRED DEFLECTION CONTROL RIB UPPER FLANGE PER SRM 57-51-02. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 ASAA0854048 1 20081126 A 7797 3250453010 CONNECTOR BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 2 ENGINE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 559AS 35178 876334 FOUND CONNECTOR DP1204 THREADS DAMAGED CONN. WILL NOT STAY ENGAGED AND FALLS OFF NR 2 ENG. HYDRAULIC PUMP. GROUNDED Y ES. VERIFIED DAMAGED CONNECTOR WILL REQUIRE NEW HARNESS PN 325 045 301 0. R&R WIRE HARNESS MW 312 FOR NR 2 ENGINE . R EF AMM 71 51 03/401. EEC TEST AND ACTUATORS TEST NR 12 PASS NO FAULTS. REF AMM 73 21 00/501 AND AMM 71 00 00/501. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081224 EA 2008 12 24 A6WA200840628 1 20081203 A 5320 BRACKET CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 414ZW 7586 CRACK FOUND ON BRACKET FS 280 LBL 9 INBD CRACK LENGTH IS .250. BRACKET AT FS 280 LBL 9 REMOVED IAW SRM 51-54-13 AND 51- 42-21. NEW BRACKET ST FS 280 LBL INSTALL IAW SRM 51-42-20. 2 L 7 2 4F RT A21EA 20081224 NM 2008 12 24 ASAA0844062 1 20081216 A 2750 FLAP SYSTEM BOEING 737 7374Q8 138447Q NM RT WING MALFUNCTIONED A ASAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 02 763AS 25100 DURING ARRIVAL INTO OTZ FLAPS EXTENDED TO JUST SHORT OF 10 WITH A GREEN LIGHT ON THE LEADING EDGE. FLAPS COULD NOT BE E XTENDED PAST 10 WITH NORMAL OR ALTERNATE FLAP EXTENSION. RAN APPROPRIATE CHECK LIST AND LANDED IN OTZ. RELEASED PER CDL 57 53 1 PLACARD INSTALLED & DOOR REMOVED MIDFLAP TORQUE SHAFT CLEARANCE RT. OPS CHECK FLAP CHECKS NORMAL ED NOTIFIED C N 1217001 RH 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 ASAA0854061 1 20081216 A 8011 STARTER BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 1 ENGINE INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 557AS 35176 892792 NR 1 ENGINE NO START. R&R NR 1 ENGINE STARTER ASSY. REF. MM 80-11-01. OPS LEAK CHECKS NORMAL. (OFF STARTER HAD NO EVID ENCE OF CHIPS IN ITS MCD). ETOPS PART NR 1 ENGINE STARTER 3505945-10 SN GRTA3903C VERIFIED GOOD. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081224 2008 12 24 ASAA0854039 4 20081211 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM EE BAY MALFUNCTIONED A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 559AS 8736 35178 FMC DISAGREE ON GRD PRIOR TO T/O. PERFORMED FMC DISAGREE QRH PROCEDURE. GROUNDED YES. PERFORMED FIM 34 61 TASK 835 W/ NO DEFECTS NOTED. ACFT REMAINS ETOPS QUALIFIED ETOPS CONTROLLER. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 ASAA0874026 1 20081215 A 5320 143A94836 GUSSET BOEING 737 737790 13844CN NM BS 500D CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 GUSSET CRACKED STA 500D STR 19 LT. REMOVED FABRICATED INSTALLED NEWLY FABRICATED GUSSET STA 500D S19L PER SRM 51-40-02- 51-30-1 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 ASAA0874027 1 20081211 A 5320 143A812210 WEB BOEING 737 737790 13844CN NM BS 438-495 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION AROUND NUTPLATE HOLES FWD CARGO DOOR SAB THRESHOLD WEB. REMOVED CORROSION AROUND NUTPLATE HOLES IN FWD CARGO D OOR SUB THRESHOLD WEB AREA 52 SQUARE INCHES X MAX .009 IN SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15 FIG 103. R&R WEB IAW 51-40-02. 2 L 7 2 4F RT A16WE 20081229 SO 2008 12 29 C2XA08CL133 1 20081217 A 3610 8166102 VALVE EMB 145 EMB145XR 3260214 SO NR 1 FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 11176 11012 14500881 CLE FLIGHT NR 2986 THE CREW REPORTED A BLEED 1 OVER TEMP WARNING DURING CLIMB IN ICING CONDITIONS. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE NR 1 FAN AIR VALVE. OPS CHECKS WERE GOOD. 2 L 7 2 4F RT 20081229 NM 2008 12 29 SWAA087336 1 20081222 A 5312 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 179, LBL 17.5, WL 227. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087324 1 20081223 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081229 2008 12 29 SWAA087325 4 20081221 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 200WN 32482 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087327 1 20081223 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 333SW 23697 FWD GALLEY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087330 1 20081222 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 462WN 32466 DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVERS CRACKED. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 AALA200820102 1 20081210 A 5340 65B5783942 MOUNT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 609AA 45862 27447 LAVATORY MOUNT FITTING CORRODED, REPLACED MOUNT FITTING IAW SRM 51-10-02. 2 L 7 2 4F RT A2NM 20081229 NM 2008 12 29 AALA200820103 1 20081210 A 5340 65B5783992 MOUNT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 609AA 54862 27447 AFT LAVATORY MOUNT CORRODED, REPLACED LAVATORY MOUNT FITTING IAW SRM 51-10-02. 2 L 7 2 4F RT A2NM 20081229 NM 2008 12 29 AALA200810519 1 20081218 A 5347 CARGO TRACK BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CORROSION ON CARGO TRACK TIE DOWN STATION 807 TO 847. INSTALLED A SERVICEABLE TRACK FROM STATION 807 TO 887 PER SRM 53- 00-53-2R. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087300 1 20081222 A 5312 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND VERTICAL WEB CRACKED AT BS 180, LBL 17, WL 230. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081229 WP 2008 12 29 AALA200810538 1 20081208 A 5320 FITTING DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 CORROSION ON LOWER FORWARD CORNER FITTING IN AFT CARGO DOOR CUTOUT STATION 1155. INSTALLED A SERVICEABLE FITTING PER SR M 51-30. 2 L 7 2 4F A6WE 20081229 WP 2008 12 29 AALA200810539 1 20081208 A 5320 FITTING DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 CORROSION LOWER AFT CORNER FITTING IN AFT CARGO DOOR CUTOUT STATION 1212. INSTALLED A SERVICEABLE FITTING PER SRM 51-30 . 2 L 7 2 4F A6WE 20081229 WP 2008 12 29 AALA200810541 1 20081208 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 RIGHT CUSP CRACKED AT STATION 220. INSTALLED A SERVICEABLE CUSP SHEET FROM STATION 218 TO 237. 2 L 7 2 4F A6WE 20081229 NM 2008 12 29 ASAA0844023 1 20081211 A 5320 654659242 SUPPORT BOEING 737 7374Q8 138447Q NM BS 867-947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON FLOOR TO SIDEWALL SUPPORT BS 867 947 RBL 25 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 UALA2008111302764 1 20080513 A 3610 CLAMP BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NR 1 PYLON LEAKING A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 934UA 26662 RTFL DUE TO A WING/BODY OVERHEAT INDICATION. NORMAL LANDING. FOUND PNEUMATIC LEAK JUST INBOARD OF NR 1 ENG PYLON AT CL AMP. REPLACED CLAMP, NO LEAK NOTED. RUNUP CREW RAN BOTH ENGS AT HIGH THRUST SETTINGS FOR SEVERAL MINUTES WITH NO OVERH EAT WARNING. A/C OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081229 NE 2008 12 29 UALA2008122206954 2 20081222 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 1 FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 225UA 30554 222056 LEFT ENGINE BURNS 400 TO 600 LBS MORE FUEL THAN RIGHT ENGINE AT CRUISE. REMOVED AND REPLACED NR 1 ENGINE.THIS ENGINE WAS A PLANNED REMOVAL DUE TO PERFORMANCE DETERIORATION. IT WAS A HIGH TIME ENGINE - 17520 TSO - AND EXHIBITED HOT SECTION DISTRESS TYPICAL OF AN ENGINE WITH THIS TSO. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081229 NM 2008 12 29 UALA2008122206956 1 20081221 A 2421 767146A IDG BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE RT ENGINE FAULTY A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 206UA 30212 CREW REPORTED RIGHT GENERATOR DROPPED OFF LINE. REPLACED IDG. RAN NR 2 ENG, OP CHECKED OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081124 2008 11 24 U5Q2008F00002 4 20080922 A 3460 6229926221 FMC LEAR 60 60LEAR 5170707 CE NR 2 FAILED D U5QA A UNSCHED LANDING O OTHER TO TAKEOFF 1 GL 07 923SK 050 ACFT WAS CONDUCTING A PART 91 FLIGHT. SHORTLY AFTER TAKEOFF, THEY LOST THE FLIGHT DIRECTOR AND THE FMS ON PIOTS SIDE. THE CREW ATTEMPTED TO RESET THE SYS, STILL UNABLE TO BRING THE FLIGHT DIRECTOR BACK UP. THE CREW MADE THE DECISION TO R ETURN TO DEPARTURE. THEY LANDED WITHOUT INCIDENT. MG SWAPPED NR 1 AND NR 2 FLIGHT CONTROL COMPUTERS (FCC) AND PERFORME D SATISFACTORY FUNCTIONAL TEST. FOUND NR 2 FLIGHT MANAGEMENT COMPUTER (FMC) BAD. INSTALLED NEW FMC AND PERFORMED SATIS FACTORY FUNCTIONAL TEST. (K) 2 L 7 2 4F RT A10CE 20081124 EA 2008 11 24 REX2008F00055 1 20080921 A 2611 47359719 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY MALFUNCTIONED A REXA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 21 8598B 7598 ON TAXI OUT RECEIVED A SMOKE CARGO WARNING. STOPPED AC RAN THE QRH TO PREPARE TO FIRE BOTTLES REQUESTED RAMP VERIFICATI ON BY CFR, FOUND NO FIRE OR SMOKE, RETURNED TO THE GATE. REMOVED AND REPLACED THE NR 1 SMOKED DETECTOR IAW AMM. (K) 2 L 7 2 4F RT A21EA 20081124 NM 2008 11 24 PIDA08033 1 20081006 A 2560 P4010021 BATTERY BOEING 737 737228 13844AG NM FLASHLIGHT DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 EA 39 251TR 23792 EMERGENCY FLASHLIGHT AT L-1 DOOR INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-60-00. OPS CHECK GOOD. (K) 2 L 7 2 4F RT A16WE 20081124 EA 2008 11 24 MAS2008F00104 1 20081004 A 5210 SWITCH CNDAIR CL600 CL6002D24 1390016 EA PAX DOOR STUCK A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 927LR 15027 PASSENGER DOOR HARD TO OPEN AND KEEP OPEN. MX FOUND THE F/A PASSENGER DOOR ASSIST MOTOR SWITCH STUCK IN. MX CLEANED SW ITCH. OPS CHECKED GOOD. (K) 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 MAS2008F00103 1 20081002 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 7264V 7264 THE CREW REPORTED LT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MX RELAMPED. OPS CHECKED GOOD. (K) 2 L 7 2 4F RT A21EA 20081124 NM 2008 11 24 MAS2008F00105 1 20081002 A 3232 3261K14 RELAY DHAV DHC8 DHC8202 2809007 NM NLG FAILED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 455YV 455 NLG FAILED TO EXTEND NORMALLY. MX REPLACED LDG DOOR ACTUATOR AND RELAY OPS CHECKED GOOD. (K) 2 H 7 2 4T RT A13NM 20081124 NM 2008 11 24 SWAA086370 1 20081119 A 5320 6546546 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 727A, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 SWAA086414 1 20081119 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 369SW 26580 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 SWAA086421 1 20081120 A 5610 141A481018 WINDOW BOEING 737 7377H4 1384404 NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 29 757LV 29850 R2 WINDOW ARCED IN COCKPIT. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 SWAA086432 1 20081120 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR CUTOUT BS 291. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081124 WP 2008 11 24 AALA200810034 1 20081017 A 5320 ATTACH ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 LEFT LOUVER BOX INBOARD FORWARD UPPER CORNER ATTACH ANGLE CRACKED. INSTALLED REPAIR DOUBLER ON ATTACH ANGLE PER SRM 53- 01-00. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810040 1 20081023 A 5320 PAN DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 567AM 53293 DOOR PAN CORRODED AROUND FORWARD STOP STATION 389. REPAIRED PER ESO 80559 DATED 21 OCT 2008. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810091 1 20081020 A 5320 SPLICE PLATE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 AFT CARGO SPLICE PLATE CORRODED ON LEFT TIE DOWN TRACK AT STATION 1213. INSTALLED NEW SPLICE PLATE PER AARD 51-00-012. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810059 1 20081008 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 CORROSION ON INTERCOSTAL UNDER RIGHT TIE DOWN TRACK AFT CARGO BAY STATION 1309-1322. REPLACED DEFECTIVE INTERCOSTAL WIT H SERVICEABLE PART PER SRM 51-30-5. 2 L 7 2 4F RT A6WE 20081125 WP 2008 11 25 AALA200810024 1 20081014 A 5343 BOLT DOUG DC9 DC982 3022082 WP NLG MIGRATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 BOLT FOR NOSE LANDING GEAR RETRACK CYLINDER SCORED DUE TO MIGRATING EYE BOLT BUSHINGS. REPLACED BOLT AND BUSHINGS PER 3 2-32-06. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810083 1 20081016 A 5340 BRACKET DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 AFT CARGO AREA, TEE BRACKET CORRODED STATION 1155 LOWER FORWARD CORNER OF DOOR OPENING. REMOVED AND REPLACED TEE BRACKE T AT STATION 1155 PER SRM 51-10-1. 2 L 7 2 4F A6WE 20081229 NM 2008 12 29 UALA2008122206946 1 20081220 A 2710 550030019 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT AILERON FAULTY A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 WP 29 655UA 25393 AILERON LOCKOUT EICAS AND OVERHEAD LIGHT CAME ON AROUND 300 KTS. CREW ADVISED BOTH O/B AILERONS APPEAR TO BE LOCKED OUT IN CRUISE. RT AIL LOCKOUT MODULE FAULT BALL DISPLAYED, RT AIL LOCKOUT ACTUATOR REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081229 NM 2008 12 29 UALA2008122206938 1 20081220 A 2611 2156556HS SMOKE DETECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW REST AREA SHORTED A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 198UA 28716 SMOKE DETECTOR PROBLEM. FLIGHT DIVERTED. FOUND DETECTOR 1A SHORTED. REPLACED DETECTOR. OPERATIONAL TESTED GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 20081229 NM 2008 12 29 UALA2008122306977 1 20081223 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 FWD GALLEY EMERGENCY CEILING LIGHT INOP. RELAMP EMERGENCY LIGHT, OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081229 NM 2008 12 29 UALA2008120506769 1 20081205 A 2751 WARNING SYSTEM BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE COCKPIT MALFUNCTIONED A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 665UA 29237 THE 'T-E FLAP DISAGREE' EICAS MSG DISPLAYED WITH FLAPS AT 20 UNITS. ACCOMPLISHED BITE TEST OF FSEU AT GATE IN SFO WITH FLAPS STILL AT 20 UNITS. FSEU IS THE OLD NON-DIGITAL TYPE. SHOWED FAULTS FOR M548 AND M603. PERFORMED BITE TEST PER M M 27-51-00-FIG 104, FLAPS AT RETRACTED POSITION ENDED AT BLOCK 4 THE FSEU COMPONENTS AND WIRING ARE OK. CREW REPORTED M SG APPEARED WHEN FLAP HANDLE WAS MOVED FROM 1 UNIT POS TO THE 5 UNIT POS. FLAPS WERE LOWERED TO 20 UNITS IN ALTERNATE. NOTHING UNUSUAL FELT OR NOTICED BY CREW. PERFORMED BITE TEST. TEST OK. ALSO RAN SLATS FLAPS IN EACH POSITION FROM 1 TO 25 UNITS, NO FAULTS OR EICAS MESSAGE, ALSO PERFORMED THE BITE TEST AGAIN ON FSEU NO FAULTS INDICATED. NO RECURRENCE 2 L 7 2 4F 4 F RT A1NM E24NE 20081229 NM 2008 12 29 SWAA087307 1 20081222 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087308 1 20081222 A 5315 141A5170 FLOORBEAM BOEING 737 7373H4 1384600 NM COCKPIT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND COCKPIT FLOORBEAM CHORD CORRODED AT BS 270, BETWEEN LBL 10 TO RBL 10, WL 208. REMOVED AND REPLACED CHORD PER SRM. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 SWAA087247 1 20081218 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 SWAA087240 1 20081218 A 5310 6545874 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 16Y CHECK, FOUND R1 DOOR AFT FRAME CRACKED AT UPPER STOP FITTING. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 HALA08121400883A 1 20081214 A 4940 211734220 CONTROLLER BOEING 767 767332 1382001 NM APU MALFUNCTIONED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, APU AUTO SHUTDOWN. REPLACED APU CONTROL UNIT DUE TO SUSPECT BAD PART FROM STOCK. OPS CHECKED APU AND CONTOLLER OK IAW AMM 49-61-05. 2 L 7 2 4F RT A1NM 20081223 NM 2008 12 23 HNAA2008121000349 1 20081213 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM LAVATORY MALFUNCTIONED A HNAA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 07 808EX 299 LAV SMOKE DETECTOR ALARM SOUNDS WITH NO EVIDENCE. TURNED APU BLEED ON, RAN ENGINE WITH BLEED SELECTED ON, LAV SMOKE DET ECTOR DOES NOT SOUND, NO EVIDENCE OF SMOKE AND FUMES. 2 H 7 2 4T RT A13NM 20081223 NM 2008 12 23 UHLA2008110700009 1 20081208 A 2130 WARNING LIGHT EMB ERJ170 ERJ170200LR 3260121 NM CABIN PRESSURE ILLUMINATED A UHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 958WH 17000248 CREW RECEIVED HIGH ALTITUDE EICAS MESSAGE. CREW DECLARED EMERGENCY AND RETURNED TO FIELD. MAINTENANCE CHECKED PRESENT LEG MESSAGES AND HAD A WARNING FOR "CABIN ALT HIGH" WITH NO LRU'S AT FAULT AND NO CORRELATED MX MESSAGES. MAINTENANCE R EPOWERED THE ACFT AND PERFORMED A GROUND RUN TO PRESSURIZE THE CABIN; SYSTEM OPS CHECK NORMAL. MAINTENANCE WAS UNABLE T O DUPLICATE DISCREPANCY ON GROUND. THERE IS NO PRIOR HISTORY AND DISCREPANCY HAS NOT REPEATED THIS DATE 12-12-2008. 2 L 7 2 4F RT A56NM 20081223 NM 2008 12 23 UALA2008111300838 1 20080214 A 5510 CLEVIS BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HORIZONTAL STAB CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 HORIZONTAL STABILIZER CENTER SECTION REAR SPAR LT UPPER CLEVIS HAS CORROSION ON AFT SIDE OF THE AFT CLEVIS AND FWD SIDE OF THE FWD CLEVIS AROUND THE BUSHING. *S/D* REAMED THE BORES AND SPOTFACED BOTH SIDES OF THE FWD AND AFT CLEVIS TO REM OVE CORROSION. ALL WITHIN LIMITS OF SRM 55-10-10 ALLOWABLE DAMAGE 5. ACP'D HFEC WITH NO DEFECTS NOTED. INSTALLED OVER SIZED BUSHING REF SRM 55-10-10 ALLOWABLE DAMAGE 5. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 UALA2008111301396 1 20080312 A 4930 FUEL NOZZLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU APU FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 313UA 922248 23674 FUEL SMELL WITH APU IN USE, SMOKE ALSO NOTED AT TAIL. FOUND FUEL NOZZLE LINE B-NUT AT 2 O'CLOCK POS BACKED OFF WHICH AL LOWED FUEL LEAK. DIFFICULT ACCESS, MAY REQUIRE DROP APU. DROPPED AND REPAIRED FUEL NOZZLES. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 CALA2008121901153 1 20081218 A 5754 65C26603 SKIN BOEING 737 7373T0 1384582 NM NR 3 SLAT DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69348 23586 LEFT WING NR 3 SLAT INBOARD END SKIN IS DELAMINATED. REPAIRED LEFT WING NR 3 SLAT TRAILING EDGE WEDGE PER SRM 51-70-10. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 CALA2008122201156 1 20081219 A 5330 2024T3 SKIN BOEING 737 7373T0 1384582 NM BS 747 S22L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 DURING C SCAN INSPECTION FOUND 1 INCH LONG CRACK ON STRINGER 22L 7 INCHES FWD OF STATION 747. REPAIRED IN ACCORDANCE WI TH SRM 53-00-01, PROCEDURE 5, REPAIR 31. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 CALA2008122201157 1 20081219 A 5330 2024T3 SKIN BOEING 737 7373T0 1384582 NM BS 727E CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 LEFT FUSELAGE STATION 727E HAS A CRACK IN THE SKIN. REPAIRED PER SRM 53-00-01, PROCEDURE 5, REPAIR 31. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 CALA2008122201159 1 20081220 A 5754 65C26602108 SKIN BOEING 737 7373T0 1384582 NM NR 5 SLAT DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69348 23586 RIGHT WING NR 5 SLAT TRAILING EDGE WEDGE INBOARD AND OUTBOARD PROTECTIVE FINISH FOUND DELAMINATION ON OUTBOARD TRAILING EDGE. FABRICATED REPAIR DOUBLER AND REPLACED DAMAGED HONEYCOMB. BONDED REPAIR DOUBLER AND CORE, SEALED INBOARD AND OUT BOARD TRAILING EDGE WEDGE SEALANT IAW SRM 51-70-10. RESTORED PROTECTIVE FINISH TO NR 5 SLAT PER CAL SPEC 5100 S00128, R EV Q. 2 L 7 2 4F RT A16WE 20081224 WP 2008 12 24 AALA200810530 1 20081202 A 5340 ATTACH ANGLE DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 ATTACH ANGLE CRACKED BELOW RIGHT HAND TIE DOWN TRACK STATION 237 FORWARD CARGO. INSTALLED SERVICEABLE ANGLE. 2 L 7 2 4F A6WE 20081224 EU 2008 12 24 USAA2008121792248 1 20081204 A 5315 D5347217220290 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 500 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - C8 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT FR66, Y1292. REPLACED FLOORBEAM AT FR66, Y1292 IAW SRM 51- 72-11. 2 L 7 2 4F RT A28NM 20081224 NM 2008 12 24 USAA2008122292286 1 20081113 A 5320 143N536715 WEB BOEING 757 7572B7 1384964 NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 941UW 27806 MCN - C1 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON WEB BETWEEN BS 648 TO BS 651, LBL 8. REPLACED WEB BETWEEN BS 648 TO BS 651, LBL 8 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081224 NM 2008 12 24 USAA2008122292288 1 20081209 A 5320 143N54102 SUPPORT BOEING 757 7572B7 1384964 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 941UW 27806 MCN - C1 - MAJOR REPAIR - CORROSION ON FLOORBEAM AREA GUTTER SUPPORT AT R2 DOOR BETWEEN BS 720 TO BS 740, RBL 65. REPLA CED GUTTER SUPPORT AT R2 DOOR BETWEEN BS 720 TO BS 740, RBL 65 IAW B757 SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081224 NM 2008 12 24 USAA2008122292289 1 20081221 A 3350 276005 FUSE BOEING 737 7373G7 138447J NM EMERGENCY LIGHT INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REPLACED LOAD FUSE AT EMERGENCY LIGHT BATTERY PACK M1137 IAW B737 WDM 33-51 -31. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 MZZA2008122200017 1 20081220 A 5315 BAC14902887 FLOORBEAM BOEING 737 737824 13844BZ NM BS 986 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 SW 27 14228 28792 CORROSION FOUND ON CABIN FLOORBEAM BODY STATION 986 RBL 43. REPAIR CARRIED OUT IAW EC/RA 5321-01429 REPAIR A. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 PIDA08037 1 20081220 A 3350 REFLECTOR BOEING 757 757200 1384950 NM EMERGENCY LIGHT INOPERATIVE A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 801DM 26240 DURING OPS CK ON EMERGENCY LIGHTS L-4 EXTERIOR SLIDE LIGHT INOP. REPLACED REFLECTOR ASSY, OPS CK GOOD REF MM 33-51-00. 2 L 7 2 4F RT A2NM 20081224 EA 2008 12 24 COMA2008122250041 1 20081222 A 5320 601R5341260 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 927CA 35573 7031 CRACK FOUND IN RADIUS OF ANGLE AT FS 559.00 RBL 18.00. REPAIRED IAW REO 601R-53-41-260. 2 L 7 2 4F RT A21EA 20081224 NM 2008 12 24 SWAA087270 1 20081221 A 3350 LAMP BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 22Y CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121992282 1 20081203 A 5740 6567172017 SUPPORT FITTING BOEING 737 7373G7 138447J NM ZONE 500 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 SAL - C17 - MAJOR REPAIR - CORROSION ON STABILIZER BEAM AFT SUPPORT FITTING AT LT MAIN LANDING GEAR. REPLACED STABILIZE R BEAM AFT SUPPORT FITTING IAW AMM 57-15-00-4. 2 L 7 2 4F RT A16WE 20081224 WP 2008 12 24 NWAA085639865 1 20081217 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 774NC 47776 DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAILED. MX REPLACED 3 BATTERY PACKS AND 1 POWER SUPPLY TO GET THE LIGHTS TO RETURN TO AN OP CONDITION. 2 L 7 2 4F RT A6WE 20081229 NM 2008 12 29 ASAA0874025 1 20081207 A 5320 146A9401U21 SPLICE BOEING 737 737790 13844CN NM FLOOR PANEL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION AROUND NUTPLATE HOLES ON FLOOR PANEL SPLICE STRAP STA 886 RBL 16 LBL 15. R&R FLOOR PANEL SPLICE. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087312 1 20081222 A 5311 6546540 ANGLE BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 515SW 25154 DURING SCHEDULED 18Y CHECK, FOUND FRAME SUPPORT ANGLE CRACKED AT BS 639, LBL 48. REMOVED AND REPLACED ANGLE PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087316 1 20081222 A 5310 6519603 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 377, RBL 70, WL 208. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087319 1 20081222 A 5311 6546533 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED 24Y CHECK, FWD CARGO COMPT FRAME CORRODED AT BS 500, BETWEEN STR 27L TO STR 28L. REPAIRED FRAME PER SR M. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087320 1 20081222 A 5322 6546536 SHEAR TIE BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 739GB 29275 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 540, LBL 54. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 UALA2008122206944 1 20081220 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT ROW 36L INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY EXIT EMERGENCY LIGHT INOP AT SEAT ROW 36 LEFT. REPLACED EMERGENCY LIGHT AND CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081229 NM 2008 12 29 UALA2008122206945 1 20081220 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT ROW 22L INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY EXIT LIGHT INOP AT SEAT ROW 22 LEFT. REPLACED EMERGENCY LIGHT AND CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081229 NM 2008 12 29 UALA2008122306969 1 20081222 A 3397 58781 FEEDER CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 554UA 26644 G2A GALLEY EMERGENCY LIGHT FEEDER CABLE DAMAGED. REPAIRED G2A GALLEY EMERGENCY LIGHT FEEDER CABLE AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081229 NM 2008 12 29 UALA2008111302849 1 20080518 A 3620 11503221 SENSOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE BLEED AIR SYS FAULTY A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 773UA 26929 BLEED OFF ENG L LEFT ENGINE BLEED VALVE CLOSED FOR SYSTEM FAULT OR SWITCH OFF, AND THE ENGINE IS NOT SHUTDOWN. ADVISORY MSG-3610500 LATCHD ER MODE MSG-3610500 LATCHD ER MODE. REPLACED DUAL TEMP SENSOR. RAN MAT TEST CHECK GOOD, AND LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081229 2008 12 29 UALA2008120106697 4 20081128 A 2330 J15J16 CIRCUIT BREAKER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BUFFER BOX TRIPPED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 641UA 25091 BURNING ELECTRICAL SMELL IN FWD CABIN NEAR VIDEO CONTROL EQUIPMENT WITH BUFFER BOX CB`S J15 AND J16 REPORTED TRIPPED BY FLT CREW. RESET J15 & J16 CB'S ON BUFFER BOX OPS CK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081229 NM 2008 12 29 UALA2008122306971 1 20081223 A 2913 65057 PUMP BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT ENGINE LEAKING A UALA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 29 665UA 29237 EDP HYD OVERHEAT LGT ILLUM. EICAS MSG (L, R) PRIM HYD OVERHEAT DISPLAYED. PUMP WAS DEACTIVATED, POS 1 (01=L,02=R). FO UND L ENG HYD PUMP LEAKING. REPLACED PUMP. ACP'D SYSTEM FLUSH, REPLACED CASE DRAIN AND PRESSURE FILTERS 3 TIMES. SERV ICED L HYD SYS TO FULL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081229 WP 2008 12 29 AALA200810510A 1 20081216 A 3350 5763 LIGHT DOUG DC9 DC982 3022082 WP PORTABLE INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7533A 49987 PORTABLE EMERGENCY LIGHT B5-29 ARM LIGHT DOES NOT COME ON. INSTALLED SERVICEABLE LIGHT. 2 L 7 2 4F A6WE 20081229 NM 2008 12 29 UALA2008122206926 1 20081220 A 2730 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ELEVATOR FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 548UA 25396 EICAS MESSAGE 'ELEV ASYM' IS DISPLAYED. REPLACED ASSY LIMITER ACTUATOR. CHECKS OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081229 NM 2008 12 29 UALA2008122206929 1 20081219 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 554UA 26644 EXT FUSE STA 560 TO STA 600 BELLY SKIN (LBL 10 TO RBL 10) HAS NUMEROUS ARCHIVED DENTS. MAJOR REPAIR ACCOMPLISHED. CUTO UT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081229 NM 2008 12 29 UALA2008122206930 1 20081219 A 2497 D71072 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE ELECTRICAL SYS LOOSE A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 217UA 30550 ELEC GEN SYS R MSG. REPLACED IDG, NO HELP. FOUND LOOSE CONNECTOR D71072. REMOVED CONNECTOR CHECKED PINS AND SOCKETS A LL OK. SECURED CONNECTOR. CLEARED MSG. RAN ENGINE, OPS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081229 NM 2008 12 29 ASAA0844091 1 20081218 A 5753 6546434336 SKIN BOEING 737 737490 1384715 NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 794AS 28889 RT IB AFT FLAP IS DENTED ON UPPER SURFACE 1" AFT OF FWD SPAR AND 7" IB OF OB END. REPAIRED DENT DAMAGE ON UPPER SURFACE OF RT IB AFT FLAP 1" AFT OF FWD SPAR AND 7" IB OF OB END IAW SRM 51 70 10 REPAIR 4 PG 201. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 ASAA0844068 1 20081211 A 5320 654659242 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON FLOOR TO SIDEWALL SUPPORT. BS 867 947 RBL 25. R&R FLOOR TO SIDEWALL SUPPORT. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 ASAA0844069 1 20081207 A 5320 69434562 STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON LOWER SUPPORT STRAP BS 782 800 RBL 25 WL 155. LOWER SUPPORT STRAP WILL BE REPLACED ON CARD 5140637. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 ASAA0874064 1 20081217 A 5320 141A83107 SUPPORT ANGLE BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION ON THRESHOLD SUPPORT ANGLE BS 310 TO BS 344 WL 208 RBL 50. THRESHOLD SUPPORT ANGLE FOUND OUT OF LIMITS AND WAS R&R. DAMAGE REMOVAL WAS .080 FROM .090 AT BS 310 REMAINING. 2 L 7 2 4F RT A16WE 20081230 2008 12 30 UALA2008122607007 4 20081225 A 2330 RDAX443110 ELECTRICAL BOX AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN MALFUNCTIONED A UALA K NONE O OTHER UK UNKNOWN 1 WP 29 828UA 1031 ELEC BURNING ODOR NOTED VICINITY OF SEATS 6 D, E, F. ODOR UNDER SEATS 2ABC. ISOLATED TO SEB AT 2ABC. REPLACED PER MM 23-33-46. 2 L 7 2 4F 4 F RT A28NM E40NE 20081230 NM 2008 12 30 UALA2008122607010 1 20081226 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 674UA 29242 THE 1H EXIT OFF PATH LIGHT BROKEN. REPLACED FWD EMERGENCY LIGHT ASSY, TESTS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081230 NM 2008 12 30 UALA2008122306978 1 20081223 A 3350 58673 INVERTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 542UA 25276 AFT LOWER EXIT SIGNS AND 2 AISLE ILLUMINATION LIGHTS FAIL TO ILLUMINATE DURING TEST. NEEDS INVERTER, LOCATED ABOVE AFT GALLEY CEILING AFT OF MID FLORESCENT LIGHT AND 2 BAD LAMPS. CK'D GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081230 NM 2008 12 30 UALA2008122306981 1 20081221 A 7932 S332T00613 TRANSMITTER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE RT ENGINE FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 671UA 30026 717695 B4 ENGINE START RT ENGINE OIL QTY READS 1 QT. CHECKED OIL QTY AND FOUND FULL. REPLACED NR 2 ENGINE OIL QUANTITY TRANSM ITTER. 2 L 7 2 4F 4 F RT A1NM E24NE 20081230 NM 2008 12 30 UALA2008111302679 1 20080507 A 5280 DOOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NLG CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 226UA 30226 RT AFT NLG DOOR AFT LOWER CORNER CRACKED APPROX 3 X 1 INCH AREA. SUSPECT GROUND EQUIPMENT DAMAGE. INTERIM REPAIR PER E VA-71532. ** MF2588 CREATED TO MONITOR. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081224 WP 2008 12 24 AALA200810526 1 20081203 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 VERTICAL FLOORBEAM SUPPORT CRACKED STATION 927 UNDER SEAT TRACK NUMBER 2. INSTALLED A SERVICABLE SUPPORT. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 SWAA086460 1 20081121 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 440, NR 1 STOP PAD FITTING. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086411 1 20081120 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086412 1 20081120 A 5753 6546436334 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 360SW 26571 DURING SCHEDULED HC1 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086344 1 20081118 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BETWEEN BS 500D + 1 TO 500D + 3, STR 12R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086454 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 440, STR 6R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 2008 11 25 SWAA086400 4 20081118 A 2565 6557463 MOUNT BRACKET BOEING 737 7373H4 1384600 NM EVAC SLIDE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR SLIDE MOUNT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086459 1 20081121 A 5310 6520723 DOOR FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FWD CARGO DOOR FRAME CUTOUT CRACKED AT LOWER CORNER OF LOWER STOP FITTING. REPAIRED F RAME PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 ASAA0893706 1 20081024 A 5230 146A611028 SKIN BOEING 737 737990 NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 DENT ON AFT CARGO DOOR EXT SKIN 18 INCHES FWD OF AFT EDGE 14 INCHES DOWN. REMOVED AND REPLACED EXTERIOR SKIN AFT CARGO DOOR PER ER 08 5453. 2 L 7 4 4F RT A16WE 20081126 NM 2008 11 26 2ARF 20081102 1 20081025 A 2750 AYG70305513 CONTROL VALVE DOUG MD80 MD83 3023681 NM ZONE 100 LEAKING W 2ARF O OTHER K FLUID LOSS LD LANDING 1 SW 23 838AM 25355 25355 49397 DURING TAXING, THE CAPTAIN REPORTED FLAPS DISAGREE BETWEEN INSTRUMENT POSITION. MAINT DETECTED A HYD LEAK IN THE FLAP C ONTROL VALVE AND IT WAS REPLACED AND TESTED IAW AMM 27-52-01 ALL CORRECT. DURING OVERNIGHT CHECK, MAINT PERFORMED VERIFY FLAP CONTROL VALVE IAW AMM 27-50-00, ALL CORRECT. 2 L 7 2 4F RT 20081126 NM 2008 11 26 ASAA0853763 1 20081110 A 2421 7588429101 FILTER BOEING 737 737890 1384527 NM NR 1 IDG DIRTY A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 570AS AAH004860 35185 FOUND ON WALKAROUND NR 1 ENG DPI INDICATOR POPPED OUT. REPLACED SCAVENGE FILTER CHANGE PER FIM 21 11 00 810 803, RAN NR 1 ENG 5 MIN, NO OIL LEAKS AND DPI INDICATOR OK. CONFIRM FILTER SCAVENGE CHECK PER FIM 24 11 41 200. 801. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0893704 1 20081110 A 5420 115A29532 BRACKET BOEING 737 737990 NM NR 2 PYLON CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AT RSS 261 RIGHT JUST AFT OF NR 2 PYLON AFT BRACKET CRACKED AT FIXED TRAILING EDGE. REMOVED CRACKED BRACKET AND REPLACE D WITH SERVICEABLE PER SRM 51 40 02 ITEM 9. 2 L 7 4 4F RT A16WE 20081126 NM 2008 11 26 ASAA0853766 1 20081114 A 3040 8300005604 CONTROL UNIT BOEING 737 737890 1384527 NM WINDOW HEAT MALFUNCTIONED A ASAA K NONE J WARNING INDICATION NR NOT REPORTED 1 NM 02 558AS 32763 35177 THE L SIDE WINDOW 'OVERHEAT' LIGHT ILLUMINATED AND PER CHECK LIST WOULD NOT RESET (380 53SAT NORMAL WARM TO TOUCH). FOU ND C/B C392 POPPED. PERFORMED FIM TASK 30 41 00 810 806. REPLACED CIRCUIT BREAKER C392 REF WDM 30 41 12. VERIFIED LEF T SIDE WINDOW HEAT OPERATED NORMAL ON THE GROUND. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0893705 1 20081108 A 5420 115A298210 BRACKET BOEING 737 737990 NM NR 2 PYLON CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AT RSS 261 RIGHT JUST AFT OF NR 2 PYLON AFT BRACKET CRACKED AT FIXED TRAILING EDGE. REMOVED CRACKED BRACKET AND REPLACE D WITH SERVICEABLE PER SRM 51 40 02 ITEM 9. 2 L 7 4 4F RT A16WE 20081126 NM 2008 11 26 ASAA0853753 1 20081107 A 3040 8300005604 CONTROL UNIT BOEING 737 737890 1384527 NM WINDOW HEAT FAULTY A ASAA K NONE J WARNING INDICATION CR CRUISE 1 NM 02 558AS 313 35177 LEFT SIDE WINDOW HEAT "OVERHEAT" LIGHT ILLUMINATED IN CRUISE AT FL 400. FOLLOWED AND TURNED OFF FOR 5 MIN. TURNED BACK ON STILL ILLUMINATED. SWITCHED BACK OFF. SHOOK LT SLIDING WINDOW COIL CORD. UNABLE TO DUPLICATE. DUE TO HISTORY REM OVED LT WINDOW HEAT CONTROL UNIT PER FIM 30 41 11 000 801. INSTALLED WHCU PER FIM 30 41 11 400 801. OPS CHECK GOOD ON GROUND. VERIFIED ETOPS PART INSTALLED PER IPC. 2 L 7 2 4F RT A16WE 20081126 NE 2008 11 26 HAEA200800205A 2 20081110 A 7320 9234A7 PUMP LEAR 25 25 5170506 CE GE CJ610 CJ6106 30006 NE RT ENGINE FUEL FAILED E HAEA E A ENGINE SHUTDOWN UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 SW 05 525TW 1966 1966 25011 240379 ENGINE RPM ROLLED BACK FL430 PLUS 30 MINUTES. AIRCRAFT DESCENDED TO FL 150 AND DIVERTED TO GSP. MAINTENANCE DISCOVERED ENGINE DRIVEN FUEL PUMP FAILED. REPLACED FUEL CONTROL/FUEL PUMP ASSY. NO FURTHER DEFECTS. 2 L 7 2 4J 4 J A10CE 1E16 20081126 NM 2008 11 26 ASAA0873870 1 20081121 A 5320 143A812210 WEB BOEING 737 737790 13844CN NM BS 440-492 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON DOOR STRUCTURE BS 440-492 UNDER THRESHOLD AND SCUFF PLATE ON SUPPORTING WEB. REMOVED WEB FABRICATED NEW WE B AND INSTALLED. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843770 1 20081024 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 1 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NUMBER 1 SPOILER LOWER SURFACE DENTED. INSTALLED REPAIR DOUBLER PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0893847 1 20081123 A 5720 115A29531 SUPPORT BRACKET BOEING 737 737990 NM LT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 LT WING FWD SUPPORT BRACKET FITTING AT RSS 261 AFT FITTING IS CRACKED. REMOVED AND REPLACED LT WING SUPPORT BRACKET AFT FITTING AT RSS 261. 2 L 7 4 4F RT A16WE 20081126 WP 2008 11 26 IXXA08SMN179S 1 20080419 A 5730 SKIN DOUG DC8 DC871F 302199D WP LT WING MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 821BX 88878 2984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT AND RIGHT INNER WING TRAILING EDGE STRUCTURE HAS IMPROPER REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. INSTALLED REPAIR PART KIT ON LT AND RT INNER WING TRAILING EDGE STRUCTURE. CL OSED MLG DOORS AND RAISED FLAPS IAW AD 90-16-05, DACO SB 57-58 DATED 01-19-08, DOUGLAS DRAWING 5758978, 5643410, DC8 SRM 51-1-21, 51-1-20D, DACO SRM 51-1-11, 51-1-21, 51-1-20D, AND 51-3-1, DC8 MM 27-27-1, AND 32-1-4. 2 L 7 4 4F RT 4A25 20081126 NM 2008 11 26 QXEA2008112101192 1 20081120 A 5210 DOOR BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR STUCK A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 19 428QX 4160 SEA - FLIGHT ATTENDANT REPORTS AFT REAR ENTRY DOOR WILL NOT OPEN. FOUND THAT THE AFT PAX DOOR WAS SLIGHTLY MISALIGNED. AFTER DOOR OPENED, INSPECTED ALL THE DOOR TRACKS AND ROLLERS AND DOOR SEAL. NO DAMAGE FOUND. CLEANED DOOR SEAL, ROLLE RS, AND TRACKS AND LUBRICATED TRACKS AS NECESSARY. PERFORMED OPS CHECK IAW Q400 AMM TASK 52-12-00-710-802. DOOR OPENS AND CLOSES SMOOTHLY. NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081126 NM 2008 11 26 ASAA0843822 1 20081028 A 5320 65479574 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 767-787 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 AFT CARGO PIT CORRODED INTERCOSTAL STA 767 TO STA 787 RBL 24. REMOVED DAMAGED INTERCOSTAL LOCATED DRILLED INSTALLED REP LACEMENT INTERCOSTAL IAW B737 400 SRM 51 40 02 AND 51 40 05. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843828 1 20081026 A 5753 6546430150 SKIN BOEING 737 7374Q8 138447Q NM FOREFLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 RT INBD FOREFLAP UPPER SURFACE DENTED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843829 1 20081023 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 3 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 33 SPOILER UPPER SURFACE HAS DENT. PREPPED DAMAGED AREA FABRICATED AND INSTALLED REPAIR AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843760 1 20081104 A 5210 69174132 PLATE BOEING 737 7374Q8 138447Q NM R1 DOOR FAULTY A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 783AS 002137 25114 R1 DOOR UPPER AND LOWER HINGE ARM ATTACH BOLTS CONTACTING CAM PLATE & STOP PLATE. REMOVED R1 DOOR FROM A/C SHIMMED R1 D OOR & BODY SIDE TORQUE TUBE PER MM 52 41 41 524 048. REMOVED R1 DOOR UPPER HINGE LOWER CAMPLATE RE AMM 20 50 11. INSTA LLED NEW UPPER HINGE LOWER CAMPLATE AND BEARING FOR R1 DOOR REF BOEING DWG 65 45807 AND MM 20 50 11. REINSTALLED R1 DOO R & ADJUSTED RIG & ACCOMPLISHED OPERATIONAL TEST, TESTED GOOD. RE-INSTALLED DOOR LINER PRESSURIZED LEAK CK GOOD REF AMM 52 41 524 048 52 41 00 404 012 52 41 00 501 52 41 31 404 006 BOO & 52 41 00 705 001 BOO & 52 41 00 705 041 BOO. CLEARA NCE GOOD ON CAM PLATE & STOP PLATE. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 USAA920082006 1 20081101 A 5210 65458492 MECHANISM BOEING 737 737301 1384611 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C11252009/001 AND 5030988 AFT SERVICE DOOR MECHANISM BOX HAS A CRACK IN THE HOUSING. REPLACED AFT SERVICE DOOR IAW US AIRWAYS TASK CARD NR 03C11252008. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 USAA920082009 1 20081101 A 5320 100T14403 TEE FITTING BOEING 767 7672B7 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 BFM MONITOR MAJOR REPAIR NR 6056565 CORROSION ON TEE FITTING AT BS955 TO 977, S22L TO 23L, RBL90. REPAIRED TEE FITTING AT BS955 TO 977, S22L TO 23L, RBL90 IAW US AIRWAYS EA NR 134048. 2 L 7 2 4F RT A1NM 20081126 NM 2008 11 26 USAA920082001 1 20081010 A 5347 6546815 SEAT TRACK BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL C21 MAJOR REPAIR NR 6139600 CORROSION ON SEAT TRACK BETWEEN BS887 TO BS947.5, WL208, LBL 24.75. REPAIRED SEAT TRACK BETWEEN BS887 TO BS947.5, WL208, LBL 24.75 IAW B737 SRM 53-00-52-2R. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 USAA920082004 1 20081010 A 5347 6546815 SEAT TRACK BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL C21 MAJOR REPAIR NR 6139601 CORROSION ON SEAT TRACK UPPER AND LOWER FLANGE BETWEEN BS907 TO BS947.5, WL208.1, LBL45. 50. REPAIRED SEAT TRACK UPPER AND LOWER FLANGE BETWEEN BS907 TO BS947.5, WL208.1, LBL45.50 IAW B737 SRM 53-00-52-2R. 2 L 7 2 4F RT A16WE 20081125 EA 2008 11 25 SWIA200820400 1 20080716 A 7120 BUSHING CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 442SW 7609 C-CHECK, LEFT ENGINE YOKE BUSHING CORRODED, REPLACED. 2 L 7 2 4F RT A21EA 20081125 WP 2008 11 25 AALA200810087 1 20081016 A 5230 BRACKET DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 CORROSION ON BRACKET ON AFT CARGO DOOR, LOWER AFT CORNER AT STATION 1212. INSTALLED NEW BRACKET PER SRM 51-10-01. 2 L 7 2 4F A6WE 20081125 EA 2008 11 25 SWIA200820410 1 20080813 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 963SW 7865 C-CHECK, FS 280 INBOARD AND OUTBOARD FLOOR SUPPORT CLIPS AT RBL9 CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 08FDEA04936 1 20081120 A 5311 651872080 FRAME BOEING 727 727227 1384078 NM FWD CARGO PIT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 495FE 21669 CORROSION ON THE FWD CARGO BILGE AREA AT ST 480 BETWEEN STR 27R AND STR 26R. CUT OUT DAMAGE AREA SHEAR TIE IAW SRM 53-1 0-4 FIG 15. FAB SHEAR TIE IAW SRM 53-10-2 FIG 3. HEAT TREAT PART IAW ENGINEERING REPORT NR 2-37153-801 REV A. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED SHEAR TIE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20081125 WP 2008 11 25 AALA200810043 1 20081020 A 5320 PAN DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 576AA 53153 AFT LAV SERVICE PANEL PAN HAS CORROSION AT OUTBOARD RADIUS OF PAN STATION 1322. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-30-00-7. 2 L 7 2 4F A6WE 20081125 EA 2008 11 25 SWIA200820411 1 20080813 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 963SW 7865 C-CHECK, RIGHT ENGINE AFT THRUST FITTING ASSEMBLY CORRODED IN BEARING AREA, REPLACED. 2 L 7 2 4F RT A21EA 20081125 EA 2008 11 25 SWIA200820412 1 20080820 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 603SK 10248 C-CHECK, FS 280 CROSSBEAM CRACKED AT LBL9. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081125 2008 11 25 HALA2008111400849 2 20081114 A 7260 70R065 ADAPTER BOEING 767 76733A 1385209 NM RT ENGINE CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 10781 10781 28141 RT ENGINE GEAR BOX STARTER MOTOR ADAPTER PLATE CRACKED HORIZONTALLY IN TWO POSITIONS ACROSS TOP AND BOTTOM OF ADAPTER. POSSIBLE FATIGUE CAUSED BY IMBALANCE OF STARTER FAILURE. REPLACED IAW ENGINE MANUAL, SUBTASK 72-61-00-430-061. 2 L 7 2 4F RT A1NM 20081125 WP 2008 11 25 AALA200810050 1 20081006 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 SEAT TRACK NUMBER 4 HAS CORROSION AT STATION 1215. INSTALLED PLUG REPAIR PER AARD 53-20-00-10. 2 L 7 2 4F RT A6WE 20081125 WP 2008 11 25 AALA200810052 1 20081006 A 5320 STIFFENER DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 STIFFENER CASING IS CRACKED ON INBOARD WALL OF LEFT LAV APPROXIMATELY 24 INCHES FROM FLOOR FORWARD OF PRESSURE BULKHEAD. INSTALLED SERVICEABLE STIFFNER CASTING PER SRM 51-01. 2 L 7 2 4F RT A6WE 20081125 EA 2008 11 25 SWIA200820413 1 20080820 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 603SK 10248 C-CHECK, FS 280 RIGHT WEB CORRODED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081125 WP 2008 11 25 AALA200810066 1 20080929 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 CABIN CUSP DAMAGED LEFT HAND SIDE. INSTALLED DOUBLER ON CUSP PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810067 1 20080929 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 NR 3 SEAT TRACK CORRODED, STATION 1295-1300. SPLICED IN NEW SEAT TRACK PER SRM 53-05-00. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 SWAA086361 1 20081118 A 3350 PL22300L STRIP BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND EEPLS STRIP MISSING AT ROW 8. INSTALLED EEPLS PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086469 1 20081121 A 5311 6545805 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 277, BETWEEN STR 9R TO STR 10R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086513 1 20081121 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FLOOR SUPPORT BEAM CORRODED AT BS 859, LBL 3. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0853752 1 20081105 A 3040 8300005604 CIRCUIT BREAKER BOEING 737 737890 1384527 NM WINDOW HEAT TRIPPED A ASAA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 02 558AS 296 35177 WINDOW HEAT "LEFT SIDE" OVERHEAT LIGHT ON. FOUND P6 12 "B7" C/B "LT SIDE WINDOW HEAT" OPEN RESET SAME PER SP CHAPTER 20 61 00. TESTED WINDOW HEAT ELEMENT FILM RESISTANCE AND SENSOR VALUES FOR CORRECT VALUES, NO FAULTS NOTED. COMPLETED FI M TASK AFTER C/B RESET PER 30 41 00 810 801. NO FAULTS NOTED, GROUND VERIFICATION SUCCESSFUL FOR ONE HOUR. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 USAA920082011 1 20081103 A 5330 145T34219 SKIN BOEING 767 7672B7 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 BFM MONITOR MAJOR REPAIR NR 6056548 CORROSION ON INTERNAL SKIN AT BOLT HOLES COMMON TO TEE FITTING BS960, S23R, WL178. REPAIRED INTERNAL SKIN AT BOLT HOLES COMMON TO TEE FITTING BS960, S23R, WL178 IAW US AIRWAYS EA NR 6056548. 2 L 7 2 4F RT A1NM 20081126 EU 2008 11 26 USAA920082016 1 20081001 A 5320 D53480043207 SILL AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C7 MAJOR REPAIR NR 6060306 CORROSION ON LOWER SILL AREA FR66, -Y1732. REPLACED LOWER SILL AREA FR66, -Y1732 IAW A32 0 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081126 EU 2008 11 26 USAA920082018 1 20081107 A 3397 CONNECTOR AIRBUS A319 A319112 3930323 EU CABIN DISCONNECTED A USAA K NONE L NO TEST UK UNKNOWN 1 EA 19 710UW 1019 LOGPAGE 8309802 FLT NR 954 FLL-PHL EMERGENCY EXIT SIGN OVER L2 DOOR INOPERATIVE. FOUND CANNON PLUG DISCONNECTED. RECON NECTED CONNECTOR. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081126 EU 2008 11 26 USAA920082017 1 20081107 A 2560 P4010021 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 677AW 2430 LOGPAGE 4452017 FLT NR 143 CMH-PHX EMERGENCY EQUIPMENT AFT FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT ON AND NOT INSTALL ED CORRECTLY. MX R&R THE AFT FLIGHT ATTENDANT FLASHLIGHT BATTERY AND INSTALLED FLASHLIGHT CORRECTLY. OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 20081126 EU 2008 11 26 08FDEA04954 1 20081121 A 5347 R5327049020000 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 429FE 364 MAIN DECK NR 2 RT SEAT TRACK AT FR 46 HAS 2 ELONGATED SCALLOPS. REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED SEA T TRACK SPLICE REPAIR BETWEEN FR 45 AND FR 54 AT TRACK NR 2 RT IAW A310 SRM 53-10-16, FIG 202. 2 L 7 2 4F RT A35EU 20081126 NM 2008 11 26 USAA920082019 1 20081107 A 2560 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 828AW 1552 LOGPAGE 8342494 FLT NR 464 PIT-SFO FLIGHT ATTENDANT FLASHLIGHT UNDER FORWARD JUMP SEAT NOT CHARGING. R&R FLASHLIGHT BAT TERY. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081126 NM 2008 11 26 USAA920082022 1 20081105 A 5330 6545774 SKIN BOEING 737 7373S3 138449H NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 313AW 23712 PHX RON MAJOR REPAIR LOG NR 4458497 FUSELAGE SKIN CRACK AT BS727D, S23L AT AFT EDGE OF EXISTING REPAIR. REPAIRED FUSELA GE SKIN AT BS727D, S23L IAW B737 SRM 53-00-01-2R-31. 2 L 7 2 4F RT A16WE 20081126 EU 2008 11 26 USAA920082007 1 20081101 A 5313 D5348004720201 STRINGER AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C7 MAJOR REPAIR NR 6060305 CORROSION ON STRINGER 26R BETWEEN FR65 AND FR66. REPLACED STRINGER 26R BETWEEN FR65 AND FR66 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081126 NM 2008 11 26 AALA200802717 1 20081010 A 3397 CONNECTOR BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 639AA 24597 MIA EMERGENCY LIGHT AT SEAT 16D INOPERATIVE. SECURED CONNECTOR PLUG FOR EMERGENCY LIGHT AT SEAT 16D. SYSTEM GROUND CHE CKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A2NM 20081126 WP 2008 11 26 AALA200802718 1 20081011 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 931TW 49527 LGA EMERGENCY EXIT SIGN LIGHT AT AFT OVERWING INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 20 OVERHEAD BIN FOR EMERG ENCY EXIT SIGN LIGHT AT AFT OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A6WE 20081126 WP 2008 11 26 AALA200802719 1 20081011 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 931TW 49527 LGA EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 18 TO 21 INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD BIN SEAT ROW 20 FOR EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 18 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A6WE 20081126 WP 2008 11 26 AALA200802720 1 20081011 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14551 53033 LGA EMERGENCY LIGHTS AT OVERHEAD SEAT ROWS 6 TO 9 INOPERATIVE. REPLACED BATTERY PACK AT OVERHEAD BIN 6F FOR EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 20081126 WP 2008 11 26 AALA200802721 1 20081011 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 14551 53033 LGA EMERGENCY LIGHTS AT OVERHEAD COCKPIT INOPERATIVE. REPLACED BATTERY PACK AT FIRST CLASS OVERHEAD ELECTRICAL BAY FOR EMERGENCY LIGHTS AT OVERHEAD COCKPIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 20081126 NM 2008 11 26 AALA200802722 1 20081011 A 3350 8110133801 LENS BOEING 777 777223 1385213 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 774AN 29581 LHR EMERGENCY LIGHT AT GALLEY NEXT TO FIRST CLASS CLOSET HAS BROKEN LENS. REPLACED LENS FOR EMERGENCY LIGHT AT GALLEY NEXT TO FIRST CLASS CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT T00001SE 20081126 WP 2008 11 26 AALA200802723 1 20081011 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7540A 49994 LGA EMERGENCY LIGHTS IN FIRST CLASS CABIN INOPERATION. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS IN FIRST CLASS CABIN . SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 20081126 WP 2008 11 26 AALA200810095 1 20081010 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 CORROSION ON RIGHT HAND CUSP STATION 1179 TO 1189. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081126 WP 2008 11 26 AALA200810096 1 20081015 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 "J" ANGLE DOUBLER CRACKED. INSTALLED NEW J ANGLE DOUBLER. 2 L 7 2 4F A6WE 20081126 NM 2008 11 26 USAA920082042 1 20081022 A 5320 6546812198 INTERCOSTAL BOEING 737 737301 1384611 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q5 MAJOR REPAIR NR 03C10853028/022 LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL AT BS967 TO BS986.5, LBL17. REPLACE D INTERCOSTAL AT BS967 TO BS986.5, LBL17 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 DHLA2008745691 1 20081115 A 5743 SUPPORT BEAM BOEING 727 727224 1384076 NM RT MLG CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 RT MLG TRUNNION SUPPORT BEAM OTBD ATTACH LUG BORE AND ATTACH FITTING BORE CORRODED AND SCRATCHED. REPAIRED RT MLG BEAM OTBD LUG BORE AND ATTACH FITTING (REAR SPAR) BORE IAW COOPESA EO COO-2-57-376-08 DATED 10/23/08 AND BOEING MESSAGE 1-986 112769-7 DATED 10/22/08. REF FAA FORM 8100-9 DATED 10/27/08 AND ASTAR EVA B257-00058 FOR REPAIR APPROVAL. DOCUMENTED O N COOPESA N/R 1-539. 2 L 7 3 4F A3WE 20081126 NM 2008 11 26 DHLA2008745695 1 20081115 A 5754 LUG BOEING 727 727224 1384076 NM LT WING LE FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LT WING, NR 2 L/E FLAP, OTBD BULLNOSE ACTUATING MECHANISM, LOWER ROD BEARING LOOSE. ACCOMPLISHED REPAIR TO FLAP BULLNOS E O/B BEARING LUG, DUE TO CORROSION, IAW COOPESA EO COO-2-57-343-08 DATED 10/9/08 AND BAC MSG 1-1006665684-2 DATED 10/7/ 08. REF FAA FORM 8100-9 DATED 11/12/08 AND ASTAR EVA B257-00148 FOR REPAIR APPROVAL. DOCUMENTED ON COOPESA N/R 5-64. 2 L 7 3 4F A3WE 20081126 NM 2008 11 26 DHLA2008745697 1 20081115 A 5743 SUPPORT BEAM BOEING 727 727224 1384076 NM LT MLG CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 LT MLG TRUNNION SUPPORT BEAM OTBD ATTACH LUG BORE CORRODED AND ATTACH FITTING BORE'S SCRATCHED AND CORRODED. ACCOMPLISH ED REPAIR TO TRUNNION BEAM BORE AND ATTACH FITTING BORES IAW COOPESA EO COO-2-57-376-08 DATED 10/23/08 AND BAC MSG 1-986 112769-7 DATED 10/23/08. REF FAA FORM 8100-9 DATED 10/27/08 AND ASTAR EVA B257-00058 FOR REPAIR APPROVAL. DOCUMENTED O N COOPESA N/R 1-538. 2 L 7 3 4F A3WE 20081126 WP 2008 11 26 AALA20081027001 1 20081027 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 CORROSION ON UPPER OUTBOARD FLANGE ON NUMBER 5 SEAT TRACK AT STATION 200 TO 218. REPLACED SEAT TRACK PER SRM 53-05-00 F IG 4F. 2 L 7 2 4F A6WE 20081126 NM 2008 11 26 AALA200820020 1 20081016 A 5754 SKIN BOEING BOEING 757 757223 1384957 NM LE SLAT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 686AA 51188 25343 NR 10 SLAT ASSY SKIN CORRODED. REPAIR DOUBLER INSTALLED IAW ECO B757-57-004757 DATED 10/16/2008. 2 L 7 2 4F RT A2NM 20081126 WP 2008 11 26 AALA20081008001 1 20081008 A 5320 STRAP DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 STATION 1193 IN AFT CARGO, WEB STRAP HAS CORROSION AT LONGERON 28R TO 29R. INSTALLED NEW STRAP PER SRM 51-30 2 L 7 2 4F RT A6WE 20081126 NM 2008 11 26 ASAA0843771 1 20081024 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 1 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NUMBER 1 SPOILER LOWER SURFACE DENTED. INSTALLED REPAIR DOUBLER PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081126 SO 2008 11 26 SWIA200820438 1 20081030 A 2530 COFFEEMAKER EMB 120 EMB120ER 3260203 SO GALLEY SMOKE A SWIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 07 567SW 120342 FLT 5446 - BURNING ELECTRICAL ODOR ON FLIGHT DECK. FOUND GALLEY HOT JUGS ARCING. REPLACED. 2 L 7 2 4T RT A31SO 20081126 EA 2008 11 26 QXEA2008112401197 1 20081120 A 7710 M210D4N RELAY CNDAIR CL600 CL6002C10 1390015 EA LT ENGINE MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 19 613QX 10045 PDX - RECEIVED A LEFT ENG DEGRADED CAUTION MESSAGE. REMOVED AND REPLACED JB 11, PCB 3 RELAYS K19 AND K21 REF 20-42-0-96 0-801-A02 OPERATIONAL CHECK GOOD REF 24-06-07-710-801-C01. NO DEFECTS NOTED STATUS AND CAUTION MESSAGES CLEARED. RETUR NED TO SERVICE. 2 L 7 2 4F RT A21EA 20081126 NM 2008 11 26 AALA200820021 1 20081016 A 5754 SKIN BOEING BOEING 757 757223 1384957 NM LE SLAT CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 686AA 25343 NR 10 SLAT ASSY SKIN CRACKED. REPAIR DOUBLER INSTALLED IAW AARD 57-43-00-04 2 L 7 2 4F RT A2NM 20081126 WP 2008 11 26 AALA200810176 1 20081114 A 5311 FRAME DOUG DC9 DC982 3022082 WP FUSELAGE CHAFED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 584AA 53247 AFT ACCESSORY AREA, FRAME 1361 HAS HOLE FROM BRAIDED LINE CHAFING AT LONGERON 19L. INSTALLED SPLICE REPAIR PER SRM 53-0 3-00. 2 L 7 2 4F A6WE 20081126 EA 2008 11 26 ASOA200801532 1 20081118 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 27 920EV 7810 FLT 5448 - FLAP FAIL AT ZERO DEGREES. EN ROUTE TO AVP A/C DIVERTED TO ABE DUE TO MTC. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 20081126 EA 2008 11 26 ASOA200801534 1 20081118 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA EXTERIOR INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 871AS 7537 LT AFT FUSELAGE EMERGENCY LIGHT INOP ON EXTERIOR FUSELAGE. 2 L 7 2 4F RT A21EA 20081126 NM 2008 11 26 ASAA0843782 1 20081107 A 5755 654645262A SKIN BOEING 737 7374Q8 138447Q NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NUMBER 5 SPOILER LOWER SURFACE DENTED. REMOVED DAMAGED AREA AND INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843783 1 20081024 A 5753 6546430150 SKIN BOEING 737 7374Q8 138447Q NM FOREFLAP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 RIGHT INBOARD FOREFLAP DENTED AND PUNCTURED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843823 1 20081026 A 5320 652072629 WEB BOEING 737 7374Q8 138447Q NM BS 452-489 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FWD CARGO PIT DOOR THRESHOLD WEB CORRODED STA 452 TO STA 489 RBL 26 TO RBL 29. REMOVED DAMAGED THRESHOLD WEB LOCATED DR ILLED INSTALLED REPLACEMENT WEB IAW B737 400 SRM 51 40 02 FIG 9 PG 31 33. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 08FDEA04945 1 20081120 A 5320 6944880 INTERCOSTAL BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 LOWER AFT CARGO AREA- CORROSION ON WEB RBL 18 STA 950F 4 WL 148 BLENDED OUT CORROSION REMOVED .025 FROM ORIGINAL .040, R EMAINING THICKNESS .015. FOUND OUT OF LIMITS IAW SRM 53-10-1. REMOVED INTERCOSTAL WEB STA 950F- 970 RBL 18 WL 148 AN D FABRICATED REPLACEMENT AND INSTALLED IAW SRM 51-30-2 AND BOEING DRAWING 69-44880. THIS IS CLASSIFIED AS A MINOR REP AIR. 2 L 7 3 4F A3WE 20081126 2008 11 26 ASAA0853820 4 20081119 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM EE BAY MALFUNCTIONED A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 558AS 9320 35177 FMC DISAGREE DISPLAYED ON TAXI IN CUN FOLLOWED QRH PROCEDURES DUAL FMC RESTORED. PERFORMED FIM TASK 34 61TASK 835 PER S TEP D2 FAULT WAS INTERMITTENT W/NO OTHER OCCURRENCES LAST 30 DAYS. OK FOR CONTINUED SERVICE. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0873852 1 20081120 A 5320 141A5410U12 INTERCOSTAL BOEING 737 737790 13844CN NM CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 INTERCOSTAL CRACKED BS 312 328 LB 40. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843833 1 20081105 A 5753 6546486156 SKIN BOEING 737 7374Q8 138447Q NM RT IB MID FLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 RT INBD MID FLAP T/E WEDGE CHAFED. REMOVED AND REPLACED T/E WEDGE IAW B737 400 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0873853 1 20081118 A 5320 FLOOR SUPPORT BOEING 737 737790 13844CN NM BS 772 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON FLOOR SUPPORT AFT CARGO BAY. FABRICATED AND INSTALLED NEW FLOOR SUPPORT. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086557 1 20081120 A 2560 6557463 FITTING BOEING 737 7375H4 138449D NM GIRT BAR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 523SW 26565 FOUND R2 DOOR AFT GIRT BAR CLIP BROKEN. R&R BRACKET PER MM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086530 1 20081123 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CLIP CRACKED AT BS. 500B, STR 8L. R&R CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0893803 1 20081118 A 5320 143A751020 INTERCOSTAL BOEING 737 737990 NM BS 500I GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 SIDEWALL SUPPORT INTERCOSTAL GOUGED AT FASTENER HOLES. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT INTERCOSTAL. 2 L 7 4 4F RT A16WE 20081126 NM 2008 11 26 SWAA086531 1 20081123 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS. 520, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 WP 2008 11 25 AALA200810090 1 20081019 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CUT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 CUT IN LEFT CUSP SHEET AT STATION 895 TO 905. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081125 2008 11 25 HALA2008112000865 2 20081120 A 7320 EEC BOEING 767 76733A 1385209 NM LT ENGINE FAILED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 591HA 33423 ETOPS SIGNIFICANT SYSTEM, STATUS MESSAGE LT ENG EEC C1 DISPLAYED. PIMU BITE SHOWS EEC CH-A/B B25 FD-BK FAIL. PERFORMED CORRECTIVE ACTION PIMU MSG INDEX AND FIM 73-21-00. REMOVED CONNECTOR FROM 2.5 BLEED VALVE AND CHECKED PINS NO TROUBLE FOUND. RESEATED CONNECTOR AND RAN PIMU BITE. BITE SHOWS NO FAULT AND NO STATUS MSGS. PER REPAIR CONFIRMATION ACFT OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20081125 WP 2008 11 25 AALA200810035 1 20081017 A 5340 MOUNT DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 CORROSION ON TOP OF INBOARD GALLEY TIE DOWN. REPLACED INBOARD GALLEY MOUNT PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810076 1 20081016 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 LEFT CUSP CORRODED AT STATION 1155 TO 1174. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 UALA2008111306365 1 20081103 A 5720 STRUCTURE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RT WING CRACKED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 673UA 29241 DURING A CHECK FOUND RIGHT WING RACEWAY INSTL WING T/E WIRE PROVISION CRACKED AT 2 PLACES. REPLACED WIRE BUNDLE RACEWAY . 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 NM 2008 11 24 UALA2008111306464 1 20081109 A 3397 794640 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 668UA 30024 EEL LIGHT INOP BETWEEN VIDEO CLOSET AND SEAT 1H RT SIDE. REPAIRED FEEDER ASSY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 NE 2008 11 24 UALA2008111706521 2 20081117 A 7321 7911004111 EEC BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE OUT OF ADJUST A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 651UA 25389 NR 1 ENG 'ENG EEC MODE' MESSAGE APPEARED ON EICAS ALONG WITH ALTN LIGHT. NR 1 ENG EEC REPLACED. ENGINE REPLACED DUE TO REPEATED EEC HITS. NO FAULT FOUND WITH ENGINE. PROBLEM PERSISTED ON THE AIRPLANE AFTER THE ENGINE WAS REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 WP 2008 11 24 AALA200810111 1 20081028 A 3350 BAT5061 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INOPERATIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 461AA 49566 EMERGENCY LIGHT BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 DL757081551 1 20081013 A 5311 FRAME BOEING 757 757232 1384965 NM BS 1560 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 650DL 24390 AFT CARGO COMP STA 1560 HAS CORROSION ON FRAME ABOVE L27. BLENDED AREA IAW SRM 53-00-07 PG 103 FIG 101. FOUND OUT OF LIMITS. INSTALLED REPAIR DOUBLER IAW SRM 51-40-07 PG 4 PARA 7. 2 L 7 2 4F RT A2NM 20081124 NM 2008 11 24 UALA2008111706527 1 20081115 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 199UA 28717 EMERGENCY EXIT LIGHT INOP AT DOOR 1 RIGHT CEILING ENTRY. RELAMPED EMERGENCY LIGHT, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081124 NM 2008 11 24 UALA2008111806545 1 20081117 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 551UA 25399 LWR FUSELAGE SKIN IS DENTED NUMEROUS PLACES, STA 233 - 236, STR 24L TO 26L. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SKIN AND FABRICATED A REPAIR DOUBLER AND INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081124 NM 2008 11 24 UALA2008111806554 1 20081117 A 2761 154260019 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 SPOILER LEAKING A UALA O OTHER W K INADEQUATE Q C FLUID LOSS IN INSP/MAINT 1 WP 29 663UA 27160 FOUND NR 2 SPOILER ACTUATOR POURING HYD FLUID FROM PCU. NR 2 SPOILER ACTUATOR LEAKING. REPLACED ACTUATOR. VERIFIED RI G AND OPS CHECKS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081125 NM 2008 11 25 HALA2008111300846 1 20081113 A 5314 KEELBEAM BOEING 767 76733A 1385209 NM BS 920 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 CORRISION ON KEEL BEAM STA 920. REMOVED IAW SRM 53-50-12, OPEN HOLE INSPECTION FPI, ROTO REEMED, PAINT CPC. 2 L 7 2 4F RT A1NM 20081125 EA 2008 11 25 SWIA200820426 1 20080821 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 962SW 7859 C-CHECK, FS 280 RBL9 LOWER FRAME CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081125 EA 2008 11 25 SWIA200820427 1 20080821 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 962SW 7859 C-CHECK, FS 280 RBL9 AND LBL9 UPPER FLOOR SUPPORT CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081125 EA 2008 11 25 SWIA200820428 1 20080821 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 962SW 7859 FS 280 LBL9 LOWER FLOOR SUPPORT CRACKED AT RADIUS. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081125 EA 2008 11 25 SWIA200820429 1 20080821 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 962SW 7859 C-CHECK, FS 280 COCKPIT FLOOR SUPPORT ANGLE CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 SWAA086375 1 20081119 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 5R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086377 1 20081119 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 WP 2008 11 25 AALA200810085 1 20081017 A 5310 BEAM DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 MID CARGO DOOR BEAM CORRODED AT STATION 636-693. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-10-00-3. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 SWAA086347 1 20081118 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086348 1 20081118 A 5311 6546533 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086349 1 20081118 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086350 1 20081118 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086333 1 20081118 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 305, WL 258. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086351 1 20081118 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086381 1 20081119 A 5322 6546569 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 987, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086382 1 20081119 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 986, STR 26R. REMOVED AND REPLACED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081125 WP 2008 11 25 AALA200810093 1 20081019 A 5311 FRAME DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 CRACK AT LEFT OVERWING FRAME RADIUS STATION 905. REMOVED AND REPLACED FRAME PER BOEING SERVICE REWORK DRAWING SRO953028 2-7013. 2 L 7 2 4F A6WE 20081125 2008 11 25 SWAA086415 4 20081120 A 2565 D31354 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 L1 DOOR SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. INSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081125 NE 2008 11 25 HALA2008111700855 2 20081117 A 7200 FAN BLADE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DISTORTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, FOUND NR 1 ENGINE FAN BLADE 18 IS DISTORTED 1ST STAGE FAN. INSPECTED NR 1 ENGINE 1ST STAGE FA N BLADE 18. DISTORTION IS WITHIN LIMITS PER AMM 72-31-02-226-007-G00 SECTION U RAN ENGINE ALL PARAMETERS WITHIN TOLERAN CE NO EXCESSIVE VIBE. OK FOR SEREVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081126 2008 11 26 SWAA086563 4 20081121 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 781WN 30601 L1 DOOR EMERGENCY EXIT SLIDE FELL OUT, DID NOT DEPLOY. SECURED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081211 NM 2008 12 11 DU4R2008244 1 20081118 A 5315 147A550408 FLOORBEAM BOEING 737 7378Q8 13844BX NM BS 947 CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION, FOUND CORROSION ON FLOORBEAM AFT CABIN BS 947 LBL 53. 2 L 7 2 4F RT A16WE 20081211 NM 2008 12 11 DU4R2008255 1 20081120 A 5320 141A5505 FLOOR SUPPORT BOEING 737 7378Q8 13844BX NM BS 344 BL0-10R CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION, FOUND CORROSION ON FLOOR SUPPORT AT BS 344 BL 0 TO BL 10R. 2 L 7 2 4F RT A16WE 20081211 NM 2008 12 11 DU4R2008252 1 20081120 A 5310 144A591010 STRUCTURE BOEING 737 7378Q8 13844BX NM BS 685-727 CORRODED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 171LF 30637 DURING SCHEDULED INSPECTION, FOUND CORROSION ON INNER CHORD AT LT OB FLOOR STRUCTURE AT BS 685-727. 2 L 7 2 4F RT A16WE 20081211 NM 2008 12 11 DU42008F00000 1 20081118 A 5330 148N3213 SKIN BOEING 757 75723APF 1384966 NM FS 1739.5 S29R CRACKED A DU4R K NONE O OTHER IN INSP/MAINT 1 EA 39 868AN 24868 DURING SCHEDULED INSPECTION, FOUND 1/8" LONG CRACK RUNNING FWD AND AFT FROM FASTENER HOLE ON REPAIR FILLER AT BS 1739-5 S-29R. EXISTING EO REPAIR FAT EO 757-53-0118. 2 L 7 2 4F RT A2NM 20081211 NM 2008 12 11 AALA200820071 1 20081119 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 56842 24599 AFT MAIN DECK PLATE CORRODED. REPAIRED IAW SRM 53-60-51-2R2. 2 L 7 2 4F RT A2NM 20081211 EA 2008 12 11 VNAA2008120900004 1 20081206 A 2421 IDG CNDAIR CL600 CL6002B19 1900309 EA NR 2 MALFUNCTIONED A VNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 05 253PS 7934 CREW REPORTED AN ABORTED TAKEOFF IN MGM FOR NR 2 IDG CAS MESSAGE. THE AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED AND DEFERRED THE NR 2 IDG. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. AT ANOTHER STATION, THE I DG WAS SERVICED AND THE DEFERRAL WAS CLEARED. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801681 1 20081206 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 FLOORBEAM CAP HAS CORROSION AT LBL 9 BETWEEN FS 645.00 AND FS 661.00. BLENDED FLOORBEAM CAP LBL 9 BETWEEN FS 645.00 & F S 661.00 IAW CRJ 700 SRM 51-21-06. LBL 9 FLOORBEAM REPLACED DUE TO OUT OF LIMITS CORROSION. REFER TO W/O 105591 N/R-00 395 FOR BEAM REPLACEMENT. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801630 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LT SIDEWALL SEAT RAIL FS 708.00 TO FS 761.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .013, WITHI N LIMITS PER SRM 53-41-49. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801632 1 20081204 A 5347 SEAT TRACK CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 LT SIDEWALL SEAT RAIL FS 785.15.00 TO FS 863.00 HAS CORROSION DAMAGE (MARKED). BLENDED OUT CORROSION MAX DEPTH .010 WIT HIN LIMITS PER SRM 53-41-49. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 ASOA200801667 1 20081206 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 680BR 7679 FLAP FAIL AT 0 DEGREES AT 200 KIAS. EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 DU4R2008268 1 20081207 A 5312 PRESSURE PANEL BOEING 757 75723APF 1384966 NM RT MLG WW CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 868AN 24868 DURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND CORROSION IN RT WHEEL WELL ON LOWER SURFACE OF CEILING ARE A AT BS 1120 S-17R ALONG FASTENERS RBL 60 - 70 AT PRESSURE DECK. 2 L 7 2 4F RT A2NM 20081211 NM 2008 12 11 UPS08454081 1 20081126 A 3350 LIGHT BOEING 747 747212B 1384886 NM CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT ON CEILING OF MAIN CARGO DECK JUST INSIDE MAIN ENTRY DOOR DAMAGED. REPLACED LI GHT ASSY PER MM 31-51-07, OPS NORMAL. THIS CLEARS M389505. PLACARD REMOVED. 2 L 7 4 4F RT A20WE 20081211 2008 12 11 QXEA2008121001206 2 20081125 A 7210 MOUNT BOMBDR DHC8 DHC8402 1390042 NM RGB CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 412QX 4059 PDX - C4 - NR 1 ENGINE REDUCTION GEARBOX HAS PITTING CORROSION AT TOP CENTER MOUNT ATTACH POINT BETWEEN MOUNT AND GEARBO X MATING SURFACE AROUND ALL 4 MOUNT BOLTS. REMOVED FWD TOP ISOLATER MOUNT IAW Q400 AMM 71-21-11-000-801, LOOSENED LT AN D RT FWD ISOLATOR ASSYS. REMOVED LT NACELLE DOORS. MAPPED FOR ENGINEERING. REPAIRED MATING SURFACE OF 31 ENG FWD TOP ISOLATOR MOUNT IAW D8 400 AMM 71-21-11-400-801. 2 H 7 2 4T RT A13NM 20081211 WP 2008 12 11 AALA200802377S 1 20081021 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 955U 49427 LGA - EMERGENCY LIGHT AT AFT TAIL COMPARTMENT WALK WAY MISSING LENS. REPLACED LENS FOR THE AFT EMERGENCY LIGHT AT AFT T AIL COMPARTMENT WALK WAY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081211 WP 2008 12 11 AALA200802370V 1 20081021 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP ZONE 200 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 955U 49427 LGA - FORWARD AND AFT SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 6E INOPERATIVE. RESET CONNECTOR AT SEAT 6E FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081211 WP 2008 12 11 AALA200802376S 1 20081021 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 955U 49427 LGA - SEAT MOUNTED FORWARD EMERGENCY LIGHT HAS DAMAGED SHROUD AT SEAT 6E. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 6 E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081211 EU 2008 12 11 UPS08154089 1 20081130 A 3350 321491U POWER SUPPLY AIRBUS A300 A300F4622R 3930360 EU CREW ENTRY DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 147UP 0830 INSPECTION TYPE:N/A CREW ENTRY DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED AUTONOMOUS PWR SUPPLY UNIT IAW AMM 52-73 -18-04. 2 L 7 2 4F RT A35EU 20081211 EA 2008 12 11 COMA2008120850021 1 20081206 A 3250 16736105 SERVO VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 920CA 13570 7022 ON APPROACH INTO JFK RECEIVED NOSE WHEEL STEERING FAILED CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED A ND REPLACED EHSV. 2 L 7 2 4F RT A21EA 20081211 NE 2008 12 11 DL777081650 2 20081126 A 7200 TRENT892 ENGINE BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 2 FLUCTUATES A DALA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SO 27 862DA 23175 29734 051150 RT ENG PARAMETERS FLUCTUATED AND ENG PWR SHORTFALL AT FL390 WITH ENG RESPONSE EICAS MSG. PERFORMED QRH 7.25 AND DESCEND ED TO FL310. CORRECTED PROBLEM. FUEL TEMP WAS -22 AND OAT -56. MTC IN PROGRESS. 2 L 7 2 4F 4 F RT T00001SE E00050EN 20081212 NM 2008 12 12 HNAA2008120600339 1 20081206 A 2611 PU90461S SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM LAVATORY MALFUNCTIONED A HNAA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 07 908HA 59605 59605 015 DURING OPERATIONS, THE LAVATORY SMOKE DETECTOR BEGAN SOUNDING CONTINUOUSLY. THE TEST SWITCH WAS CYCLED AND THE UNIT OPE RATED NORMALLY. THE AIRCRAFT WAS NOT TAKEN OUT OF SERVICE. 2 H 7 2 4T RT A13NM 20081212 WP 2008 12 12 UPS08854071 1 20081118 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV EXTERNAL REPAIR AT BS 29 TO BS 34 DOES NOT MEET SRM 729-F1-03. REPAIRED PREVIOUSLY IAW SRM 53-02-00. 2 L 7 4 4F RT 4A25 20081212 WP 2008 12 12 UPS08854076 1 20081125 A 5321 FLOOR PANEL DOUG DC8 DC871F 302199D WP COCKPIT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV COCKPIT SEAT TRACK FLOOR PANEL STA 70 REQUIRES EVALUATION. REPAIRED SRM 53-2-0 FIG 001B SH 2 REV 78. 2 L 7 4 4F RT 4A25 20081212 EU 2008 12 12 UPS08854080 2 20081202 A 7200 ENGINE DOUG DC8 DC873F 302199F WP CFMINT CFM56 CFM563C 13802 EU NR 3 FLAMED OUT A IPXA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 SO 01 802UP 46100 INSPECTION TYPE:N/A NR 3 ENGINE FLAMED OUT. ENGINE RELIT ON IT'S OWN. PERFORMED FIRST FOUR STEPS OF DC-8 M/M 71-00-00- 1 FIG 139 UP TO INSPECT FUEL FILTER. FILTER KIT ON ORDER. REPLACED NR 3 FUEL FILTER PER AMM 73-10-02-4. LEAK CHECK OK . ACCOMPLISHED STEPS 5 THRU 15. ENGINE RUN SUCCESSFUL. A/C RETURNED TO SERVICE. 2 L 7 4 4F 4 F RT 4A25 E21EU 20081212 NM 2008 12 12 USAASB08123 1 20081207 A 3350 20131ASMI BATTERY PACK BOEING 737 737301 138447R NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 574US 23739 CLT - MAINTENANCE REPORTED THE FORWARD RIGHT AND FIRST CLASS EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT STA 326R PER MM 33-51-51. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086923 1 20081207 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086924 1 20081207 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 490, STR 16L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086888 1 20081206 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT COVER CRACKED. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086935 1 20081207 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST UK UNKNOWN 1 SW 29 456WN 32463 FOUND EEPLS LIGHT INOP AT ROW 1. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086925 1 20081207 A 5330 6545772 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 691, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086926 1 20081209 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 911, BELOW STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081212 2008 12 12 SWAA086887 4 20081206 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086422 1 20081120 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 907, STR 4L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 WP 2008 11 25 AALA200810041 1 20081022 A 5340 SUPPORT BRACKET DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 567AM 53293 SUPPORT AT STATION 1210 IS CORRODED AT AFT CARGO DOOR. REPLACED SUPPORT BRACKET PER SRM 53-01-00 AND 51-01-00. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 SWAA086433 1 20081120 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 410, RADIO ALTIMETER CUTOUT OPENING. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086334 1 20081118 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 303, WL 258. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081125 WP 2008 11 25 AALA200810100 1 20081121 A 5520 ANGLE DOUG DC9 DC982 3022082 WP ZONE 300 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 494AA 49732 SUPPORT ANGLE IN STRUCTURAL RIB CRACKED OUTBOARD OF ANTI FLOAT TAB PUSH ROD CRANK IN RIGHT ELEVATOR. REPLACED CRACKED R IB AND CLIP. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 SWAA086383 1 20081119 A 5322 6546569 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 947, BETWEEN STR 27L TO 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086423 1 20081120 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086444 1 20081120 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086445 1 20081120 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086384 1 20081119 A 5322 6546569 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 947, BETWEEN STR 26R TO 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081125 WP 2008 11 25 AALA200810101 1 20081021 A 5320 PAN DOUG DC9 DC982 3022082 WP ZONE 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 FWD CARGO DOOR PAN CORRODED, STATION 370-427. INSTALLED NEW DOOR PAN SECTION FROM STATION 370 TO 427 PER SRM 53-05-00 F IG 44 SHEET 14. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810046 1 20081005 A 5320 PAN DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 FORWARD LAV SERVICE PAN HAS CORROSION LOWER EDGE. INSTALLED DOUBLER PER ESO 80559 DATED 10-5-08. 2 L 7 2 4F RT A6WE 20081125 WP 2008 11 25 AALA200810048 1 20081006 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 LEFT CUSP CORRODED AT STATION 872. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081125 WP 2008 11 25 AALA200810049 1 20081006 A 5340 FITTING DOUG DC9 DC983 3022083 WP GIRT BAR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 CORROSION BELOW AFT GIRT BAR FITTING AT AFT SERVICE DOOR STATION 1098. REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081125 NM 2008 11 25 08FDEA04935 1 20081119 A 5754 65216823 SKIN BOEING 727 727227 1384078 NM ZONE 500 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 495FE 21669 LT WING NR 2 SLAT UPPER T/E LIP DAMAGED AT INBD UP STOP HOOK. TRIMMED OUT DAMAGE AREA IAW SRM 57-50-1, REMOVED SLAT HOO K IAW SRM 51-30-2, FAB REPAIR PLATE IAW SRM 57-50-3. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED COUNTERSINK WASHER S IAW SRM 51-30-8 FIG 4. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2. REINSTALLED HOOK IAW SRM 51-30-2. 2 L 7 3 4F A3WE 20081125 NM 2008 11 25 SWAA086336 1 20081118 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 302, WL 261. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086934 1 20081207 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 456WN 32463 FOUND EMERGENCY EXIT LIGHT COVER MISSING AT ROW 2. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086889 1 20081205 A 5330 6552988 SKIN BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR FWD LOWER CORNER. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086936 1 20081206 A 5753 6546435278 FLAP BOEING 737 7373H4 1384600 NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED MV2 CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121992271 1 20081218 A 3350 1012881 LIGHT AIRBUS A319 A319132 3930340 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 816AW 1350 FLT 0700 - ROW 14 LEFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED ROW 14 LEFT EMERGENCY EXIT SEAT MOUNTED LIGHT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081224 NM 2008 12 24 USAA2008121992276 1 20081218 A 5311 6546548 FRAME BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - FUSELAGE FRAME CRACKED AT BS 747, BETWEEN S8L & S9L. REPAIRED FUSELAGE FRAME AT BS 747, BETWE EN S8L & S9L TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008122292287 1 20081206 A 5340 6545810517 STRINGER CLIP BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - STRINGER TIE CLIP CRACKED AT BS 312, S18R. REPAIRED STRINGER TIE CLIP AT BS 312, S18R IAW BOE ING DRAWING 65-45810 & B737 SRM 51-40-05. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008122292290 1 20081221 A 5311 6520722 FRAME BOEING 737 737401 138449B NM BS 440 S24L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 23876 PIT - FPBH - MAJOR REPAIR - CRACK IN FORWARD CARGO DOOR OPENING IN FORWARD FRAME AT LOWER DOOR STOP FITTING ON LOWER EDG E AT BS 440, S24L. REPAIRED DOOR FRAME IAW US AIRWAYS EA 112037. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 UALA2008111302631 1 20080505 A 5754 WEDGE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NR 2 SLAT DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 913UA 25291 NR 3 SLAT T/E WEDGE ASSEMBLY HAS DAMAGE. *S/D* METAL OVERLAY PIECE IS LOCATED IN THE FLIGHT DECK. PERFORMED REPAIR OF SLAT 3 TRAILING EDGE WEDGE BOND ASSEMBLY. PRIMED AND PAINTED AREA. 2 L 7 2 4F 4 F RT A16WE E21EU 20081224 NM 2008 12 24 UPS08554216 1 20081218 A 2560 SEAL BOEING 757 75724APF 1384969 NM COCKPIT PBE LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 443UP E0601478 27388 PBE VACUUM SEAL COMPROMISED. REMOVED AND REPLACED PBE. 2 L 7 2 4F RT A2NM 20081224 NM 2008 12 24 ASAA0844052 1 20081216 A 5320 654795113 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 787-795 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON INTERCOSTAL WEB BETWEEN FRAMES AT BS 787-795 RBL 24. R&R INTERCOSTAL. 2 L 7 2 4F RT A16WE 20090115 NM 2009 1 15 ASAA0844053 1 20081216 A 5320 WEB SHEAR WEB BOEING 737 7374Q8 138447Q NM BS 787-794 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 WHILE WORKING CARD 5140578 FOUND SHEAR WEB CORRODED. STA. 787-794 WL 156 RBL 25 REPLACED 2 L 7 2 4F RT A16WE 20081224 SO 2008 12 24 C2XA08RI182 1 20081218 A 3610 320C62315M CLAMP EMB 145 EMB145LR 3260212 SO BLEED AIR SYS DEFORMED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 14952 145067 FLIGHT 2775 - EWR - FLIGHT CREW REPORTED ENG NR 1 BLEED LEAK INDICATION ON EICAS IN FLIGHT. CREW PERFORMED AIR RETURN A ND LANDED UNEVENTFULLY. EWR MX R&R BLEED V-CLAMP AND PERFORMED OPX CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081224 2008 12 24 ASAA0854038 4 20081212 A 2310 8220990004 TRANSCEIVER BOEING 737 737890 1384527 NM HF SYSTEM INOPERATIVE A ASAA O OTHER O OTHER CR CRUISE 1 NM 02 585AS 5130 35683 NR 1 HF TRANSMIT INTERMITTENTLY INOP GROUNDED YES. PERFORMED FIM TASK 23 11 00 810 801 NO DEFECTS NOTED. AS PRECAUTION ARY REPLACED NR 1 HF TRANSCEIVER IAW AMM 23 11 21 400 801. NR 1 HF FLIGHT VERIFICATION SATISFACTORY. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 ASAA0874035 1 20081214 A 5310 141A33131 DOOR FRAME BOEING 737 737790 13844CN NM BS 295 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 WHILE WORKING NRC5144956 FWD SER DOOR FRAME FOUND 2 EA HOLES W/PARTIAL PILOT HOLES 51295 WL 269 RT SIDE. REPAIRED HOLES PER EA700 53EA 00342. 2 L 7 2 4F RT A16WE 20081229 NE 2008 12 29 ASAA0854040 2 20081213 A 7261 ENGINE BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 1 OIL CONSUMPTION A ASAA K NONE J WARNING INDICATION IN INSP/MAINT 1 NM 02 558AS 9589 35177 894148 SEAMC REPORTS NR 1 ENGINE EXCEEDED ETOPS OIL CONSUMPTION RATE NR 1 ENGINE CURRENT CONSUMPTION AT .0.71 QUARTS PER HOUR. ACFT GROUNDED. RAN NR 1 ENGINE AT IDLE FOR APPROX. 5 MINUTES. NO LEAKS DETECTED. ACFT RELEASED FOR ETOPS SERVICE. N R 1 ENGINE WITHIN OIL RATE LIMITS AND CONSUMPTION RATE LIMITS. TASK CARD COMPLIED WITH. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081229 NM 2008 12 29 SWAA087337 1 20081222 A 5312 6517582 WEB BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 630WN 27705 DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 180, LBL 17.5 WL 228. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 08FDEA04937 1 20081120 A 5330 6517510200 SKIN BOEING 727 727227 1384078 NM ZONE 200 CANNING A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 495FE 21669 EVIDENCE OF SKIN OIL CANNING AT BS 1347.65 BETWEEN STR 6 R AND STR 7R. CUT OUT DAMAGE AREA IAW SRM 53-30-5 FIG 26. FAB REPAIR PART IAW SRM 53-30-3 FIG 26 AND 54-30-2 FIG 4. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR IAW SRM 51 -30-2. 2 L 7 3 4F A3WE 20081125 WP 2008 11 25 AALA200810057 1 20081009 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 CORROSION AROUND UPPER NUT CLIP HOLE ON LEFT TIE DOWN TRACK FROM SPLICE STATION 1220 TO AFT END OF TRACK. INSTALLED NEW TIE DOWN TRACK PER SRM 53-05-00 FIG 4G. 2 L 7 2 4F RT A6WE 20081125 NM 2008 11 25 SWAA086341 1 20081118 A 3350 101331 LIGHT BOEING 737 7373H4 1384600 NM EXTERIOR BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081125 2008 11 25 AALA200810069 4 20081022 A 2565 PIN AIRCRUISERS DOUG DC9 DC983 3022083 WP ESCAPE SLIDE LOOSE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9677W 1710 53627 SLIDE PACK CONTAINMENT PIN PULLED LOOSE AND FRANGIBLE LINK (STRING) BROKEN. REPLACED SLIDE. 2 L 7 2 4F RT A6WE 20081125 WP 2008 11 25 AALA200810070 1 20081023 A 5322 SHEAR TIE DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9677W 53627 SHEAR TIE CRACKED AFT SIDE OF 1451 FRAME, AFT OF LONGERON 2 LEFT. INSTALLED NEW SHEAR TIE. 2 L 7 2 4F RT A6WE 20081125 WP 2008 11 25 AALA200810071 1 20081013 A 5310 STRUCTURE DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 FORWARD LOWER TANG CRACKED ON LT WINDOW PAN. INSTALLED DOUBLER PER AARD 53-10-00-25. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810037 1 20081010 A 5340 MOUNT DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 GALLEY TIE DOWN MOUNT CORRODED. REPLACED GALLEY FLOOR MOUNT. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA2008 1 20081015 A 5320 ANGLE DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 LEFT NOSE LANDING GEAR DOOR JAM BEAM J ANGLE DOUBLER CRACKED AT STA 47. INSTALLED NEW J ANGLE DOUBLER. 2 L 7 2 4F A6WE 20081125 EA 2008 11 25 SWIA200820414 1 20080820 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA CORRODED CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 603SK 10248 C-CHECK, FS 280 LEFT WEB CORRODED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081125 EA 2008 11 25 SWIA200820415 1 20081111 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 1900309 EA RIGHT SMOKE A SWIA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 NM 07 934SW 13653 13653 7722 FLT 6514 - SMOKE TOILET MESSAGE AND SMOKE IN CABIN. REPLACED RIGHT ACM, 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 SWAA086402 1 20081120 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 787, STR 22R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086403 1 20081120 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 9L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086404 1 20081120 A 5230 6545768 SKIN BOEING 737 7373A4 1384585 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED HC1 CHECK, FOUND FWD CARGO DOOR SKIN CRACKED AT DOOR HANDLE CUTOUT. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20081125 2008 11 25 SWAA086405 4 20081119 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086391 1 20081119 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 461WN 32465 DURING SCHEDULED HC1 CHECK, FOUND LT OVERWING EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BA TTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086447 1 20081120 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 618WN 28034 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086392 1 20081119 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 461WN 32465 DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BA TTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081125 EU 2008 11 25 NWAA084893304 1 20081031 A 3350 BATTERY AIRBUS 330 A330323 3940030 EU EMERGENCY LIGHTS NO TEST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 804NW 0549 BATTERY EPSU 13WL DOOR 2L FAILED CAPACITY CHECK, REPLACED BATTERY AND TESTS OK. 2 L 7 2 4F RT A46NM 20081125 EA 2008 11 25 COMA0860455 1 20081106 A 5330 601R32026337 SKIN CNDAIR CL600 CL6002B19 1900309 EA FS 559 RBL 9-18 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 783CA 7315 PERMANENT REPAIR REQUIRED DUE TO TEMP REPAIR THAT WAS DONE AT FS 559 WEB BETWEEN RBL 9-18. REMOVED TEMP REPAIR AND INST ALLED A PERMANENT REPAIR DOUBLER ON FS 559 BULKHEAD WEB. 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 SWAA086463 1 20081121 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM . 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086465 1 20081121 A 5315 BAC1509100146 SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND AFT CARGO BAY FLOORBEAM SUPPORT CORRODED AT BS 727D + 6, LBL 3. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 UALA2008111305468 1 20080826 A 2120 UNKNOWN BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE AC SYSTEM CONTAMINATED A UALA A UNSCHED LANDING W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 665UA 29237 HEAVY ODOR (BURNING SMELL) IN CABIN. RTFL. AC SYSTEM OIL CONTAMINATION REMOVAL. ENGINE RUN TO REMOVE OIL ODORS. SIX QUARTS OIL REMOVED FROM OIL TANK. ALL OIL SMELL HAS DISSIPATED FROM NR 1 ENG BLEED SYSTEM. NO ODORS PRESENT AT END OF PACK BURN. 2 L 7 2 4F 4 F RT A1NM E24NE 20081124 NM 2008 11 24 UALA2008111305469 1 20080825 A 5730 116W2501 SKIN PANEL BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT WING CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 774UA 26936 LT WING SKIN PANEL HAS 10 INCH CRACK AND DELAMINATION. SUSPECT MOISTURE CONTAMINATION. REMOVED PANEL AND ROUTED TO SH OP FOR REPAIR. RE-INSTALLED REPAIRED PANEL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081124 CE 2008 11 24 DXTA2008111303353 1 20081112 A 2120 UNKNOWN CESSNA 750 750 2076810 CE COCKPIT ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 07 903QS 7500162 DIVERTED EN ROUTE DUE TO DETECTION OF AN UNUSUAL ODOR OF UNKNOWN SOURCE OR ORIGIN IN COCKPIT AND CABIN. 2 L 7 2 4J RT T00007WI 20081124 WP 2008 11 24 AALA200810088 1 20081017 A 5230 WEB DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 AFT CARGO, CORROSION ON DOOR WEB AT STATION 1155-1174. INSTALLED WEB REPAIR PER AARD 53-10-00-24. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810026 1 20081015 A 5320 ANGLE DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 CORROSION ON UNDERSIDE OF CUSP ANGLE BETWEEN STATION 204-218. REPLACED CUSP ANGLE. 2 L 7 2 4F A6WE 20081124 EA 2008 11 24 SWIA200820416 1 20081117 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 742SK 10197 FLT 6253 - PASSENGER DOOR, 2 EMERGENCY LIGHTS INOP. SERVICE DOOR, 1 EMERGENCY LIGHT INOP, RELAMPED. 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 SWIA200820390 1 20080807 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 778SK 10242 C-CHECK, FS 280 CROSSBEAM CRACKED AT LBL9 AND RBL9. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 SWIA200820391 1 20080807 A 5210 WEB CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 778SK 10242 C-CHECK, PASSENGER DOOR AFT WEB CRACKED AT SECOND AND THIRD STEP. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 SWIA200820393 1 20080819 A 5320 WEB CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710SK 10170 C-CHECK, LT WEB CORRODED AT FS 280. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 SWIA200820396 1 20080716 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 442SW 7609 C-CHECK, FORWARD FLOOR SUPPORT CRACKED AT BOTH RADIUS CORNERS. REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 SWIA200820398 1 20080716 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 442SW 7609 C-CHECK, FLOORBEAM FS 280 LBL9 AND RBL9 CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081229 NM 2008 12 29 SWAA087341 1 20081223 A 5311 65C22908 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 500B, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 AALA200820094 1 20081119 A 5340 146N872216 TEE FITTING BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 56842 24599 TEE FITTING CORRODED, REPLACED FITTING IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20081229 NM 2008 12 29 AALA200820095 1 20081205 A 5543 178W00615 TAB BOEING 777 777223 1385213 NM RUDDER DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 761AJ 27651 31478 RT RUDDER TAB HAS TWO INCH LONG CREASE 17.5 INCH FROM LEADING EDGE AND 6.5 INCH FROM BOTTOM SIDE OF TAB. RT RUDDER TAB REPAIRED IAW SRM 51-70-04-2R AND EA COMP NUMBER 5T-005062 CURED PER FIG 211. 2 L 7 2 4F RT T00001SE 20081229 WP 2008 12 29 AALA200810536 1 20081207 A 5310 BEAM DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 CORROSION ON MID CARGO DOOR BEAM STATION 636 TO 693. REPAIRED PER AARD 53-10-00-3. 2 L 7 2 4F A6WE 20081229 WP 2008 12 29 AALA200810548 1 20081208 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 CORROSION ON CUSP STATION 135 TO 155. INSTALLED DOUBLER. 2 L 7 2 4F A6WE 20081229 NM 2008 12 29 ASAA0854059 1 20081216 A 2840 INDICATION SYS BOEING 737 737890 1384527 NM FUEL SYSTEM FALSE INDICATION A ASAA O OTHER N FALSE WARNING CR CRUISE 1 NM 02 585AS 5169 35683 CRUISE FLT MASTER CAUTION AND FUEL LIGHTS ILLUMINATED WITH ALL PUMPS INDICATING NORMALLY. QUANTITIES=8.44, 8.80, 8.69 ( INTERMITTENT) GROUNDED YES. WITH FUEL IN ALL 3 TANKS / ALL PUMPS RUNNING UNABLE TO DUP / VERIFY DISCREP. DUE TO HISTORY R&R PRECAUTIONARY FUEL SYSTEM MODULE P5 2 REF. MM 28-22-43-020-801. OPS TEST FUEL SYSTEM MODULE P5 2 GOOD REF. 28-22-43 . DISCONNECTED AND RECONNECTED PLUG DP1207 REF. MM: 28-22-43 STEP 216 P5 2 FUEL MODULE OPS NML REF. 28-33-43. VERIFICA TION FLT SATISFACTORY. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 UALA2008122206947 1 20081220 A 3350 COVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 593UA 28144 EEL STRIP COVER FROM ROW 25 TO BACK OF ACFT CHEWED UP AND BROKEN. REPLACED COVER STRIP. 2 L 7 2 4F 4 F RT A2NM E17NE 20081229 NM 2008 12 29 UALA2008111303580 1 20080624 A 2751 INDICATION SYS BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE TE FLAP MALFUNCTIONED A UALA D RETURN TO BLOCK N FALSE WARNING LD LANDING 1 WP 29 646UA 25283 EICAS MESSAGES T/E FLAP DISAGREE & T/E FLAP SHUTDOWN DISPLAYED. CREW COMMENTS: FLAPS DISAGREE FROM 20 TO 25. RAN L/E AND T/E DEVICES THRU SEVERAL CYCLES AND OPERATED IN RAPID FLAP POSITION CHANGES. OPERATION APPEARS NORMAL. FSEU BITE=N O FAULTS. MESSAGE CLEARED AND DID NOT RE-APPEAR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081229 NM 2008 12 29 SWAA087317 1 20081222 A 5311 6546533 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED 24Y CHECK, FOUND FWD CARGO COMPARTMENT FRAME CORRODED AT BS 500, BETWEEN STR 28L TO STR 28R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087318 1 20081222 A 5330 6562212 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 UALA2008111303171 1 20080602 A 2841 INDICATOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE COCKPIT UNRELIABLE A UALA K NONE W INADEQUATE Q C CR CRUISE 1 WP 29 667UA 29239 FUEL BURN IS EXCESSIVE. UPON ARRIVAL PRIOR TO RE-FUEL DRIP AND CONFIRM FUEL QTY'S FOR ACCURACY. THEN AFTER FUELING STI CK AND RECONFIRM INDICATION FOR ACCURACY. ACP'D, FUELERS DRIPPED BEFORE AND AFTER FUELING AND NO DISCREPANCY FOUND. CR EW COMMENTS: HAVE REASON TO SUSPECT THE CENTER FUEL QUANTITY GAUGE IS UNRELIABLE. ACCOMPLISHED BITE TEST. CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081229 WP 2008 12 29 AALA200802396B 1 20081025 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 471AA 49601 LGA - FORWARD SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 20DEF. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F A6WE 20081229 NE 2008 12 29 AALA200802396A 2 20081025 A 7230 COMPRESSOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE STALLED A AALA E A ENGINE SHUTDOWN UNSCHED LANDING R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CL CLIMB 1 SW 21 976TW 53626 708521 ORD INFLIGHT - CREW REPORTED SUSPECTED NUMBER ONE ENGINE COMPRESSOR STALL DURING CLIMB THROUGH 25000 FEET. FELT AND HEA RD BANG N1 ENGINE PRESSURE RATIO RAPID FLUCTUATION. CREW BROUGHT ENGINE TO IDLE. FLIGHT ATTENDANTS REPORTED EXTREME VI BRATION ON LEFT SIDE OF AIRCRAFT. CREW SHUT ENGINE DOWN AND VIBRATION STOPPED. LANDED ORD WITHOUT INCIDENT. REPLACED NUMBER ONE ENGINE ON 27 OCT AT ORD DUE TO BOROSCOPE FINDINGS. 2 L 7 2 4F 4 F RT A6WE E9NE 20081229 WP 2008 12 29 AALA200802397A 1 20081025 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP ZONE 200 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 471AA 49601 LGA - FORWARD SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081229 NM 2008 12 29 AALA200802398A 1 20081025 A 2560 BATTERY BOEING 767 767323 1385205 NM FLASHLIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 343AN 33082 SFO - FIRST CLASS LEFT CENTER FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT AT FIRST CLASS LEFT CENTER. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081124 EA 2008 11 24 SWIA200820399 1 20080716 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA LT NACELLE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 442SW 7609 C-CHECK, LEFT THRUST FITTING CORRODED, REPLACED. 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 SWIA200820417 1 20081116 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 708SK 10156 FLT 6510 - ONE CEILING LEVEL EMERGENCY FLOOD LIGHTS INOP, RELAMPED. 2 L 7 2 4F RT A21EA 20081124 EA 2008 11 24 SWIA200820420 1 20081113 A 3397 CONNECTOR CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS LOOSE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 928SW 7701 FLT 6678 - EMERGENCY LIGHT STRIP OUT BETWEEN EMERGENCY EXIT AND LAV ON RT SIDE. RESECURED CONNECTOR. 2 L 7 2 4F RT A21EA 20081124 WP 2008 11 24 AALA200810027 1 20081015 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 RIGHT CUSP CORRODED. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810029 1 20081016 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 CRACK IN CUSP STATION 219 RIGHT OUTBOARD OF NR 6 SEAT TRACK. INSTALLED NEW CUSP AT STATION 218 TO 237 RIGHT, PER AARD 5 3-20-00-16. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810078 1 20081016 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 AFT CARGO COMPARTMENT, INTERCOSTAL BETWEEN FLOORBEAMS AT STATION 1287-1309 UPPER LEG HAS CORROSION AFT END IS CRACKED. INSTALLED NEW INTERCOSTAL PER AARD 51-00-012 AT STATION 1287. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810079 1 20081016 A 5322 SHEAR TIE DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 AFT CARGO AREA, CORROSION AFT LOWER ANGLE STATION 1211 AT LONGERON 30R TO 29R. INSTALLED SERVICEABLE SHEAR TIE AT STATI ON 1211 PER SRM 51-10-1. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810080 1 20081016 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 AFT CARGO FLOORBOARD SUPPORT CORRODED STATION 1212 AT LONGERON 28L TO 29L. REMOVED AND REPLACED FLOORBOARD SUPPORT PER SRM 51-10-1. 2 L 7 2 4F A6WE 20081124 WP 2008 11 24 AALA200810082 1 20081015 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 CORROSION ON DOUBLER LEFT CUSP AT STATION 664-668. INSTALLED NEW CUSP DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081124 NM 2008 11 24 UALA2008111806570 1 20081117 A 2997 BACC63BP12A3S10L CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DAMAGED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 647UA 25284 CREW REPORT AIR DEMAND PUMP OVERHEAT LIGHT ILLUMINATED. LIGHT STAYED ON WITH PUMP SWITCHED OFF. CREW REPORT THAT C HYD DEM PUMP EICAS MSG FINALLY APPEARED 5 HOURS AFTER TURNING THE SWITCH ON. ALSO OVHT LIGHT STILL ON. FOUND DAMAGED CONN ECTOR (D2216) TO TEMP SWITCH AND DAMAGED CONNECTOR (D464) TO S28. REPLACED D2216 AT S317, SYSTEM CKS OK. ALL INDICATIO N NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081125 WP 2008 11 25 AALA200810073 1 20081013 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 CRACK AT FORWARD LOWER END OF FLOORBEAM SUPPORT, STATION 927 BELOW NR 2 SEAT TRACK. REPLACED FLOORBEAM SUPPORT PER SRM 51-01 2 L 7 2 4F A6WE 20081125 EA 2008 11 25 SWIA200820431 1 20080821 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 962SW 7859 C-CHECK, FS 625 RIGHT INTERCOSTAL CLIP CRACKED AT STRINGER 14. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 SWAA086378 1 20081119 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE DAMAGED AT BS 500D, BETWEEN STR 16R TO STR 17R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086352 1 20081118 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086434 1 20081120 A 5330 6545769 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 430, RADIO ALTIMETER CUTOUT OPENING. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081125 EA 2008 11 25 SWIA200820407 1 20080808 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 443SW 7638 C-CHECK, FS 280 LOWER FLOOR SUPPORT CRACKED AT LBL9.. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081125 2008 11 25 HALA2008111700856 2 20081117 A 7200 FAN BLADE BOEING 767 767332 1382001 NM NR 1 ENGINE DISTORTED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 594HA 23275 ETOPS SIGNIFICANT SYSTEM, FOUND NR 1 ENGINE FAN BLADE 17 IS DISTORTED 1ST STAGE FAN. INSPECTED NR 1 ENGINE 1ST STAGE FA N BLADE 17. DISTORTION IS WITHIN LIMITS PER AMM 72-31-02-226-007-G00 SECTION U. RAN NR 1 ENGINE ALL PARAMETERS WITHIN TOLERANCE NO EXCESSIVE VIBE. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20081125 NM 2008 11 25 SWAA086446 1 20081120 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 HALA2008111600858 1 20081116 A 4990 1589352 BYPASS VALVE BOEING 767 767332 1382001 NM APU OIL COOLER FAILED A HALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 13 598HA 23278 ETOPS SIGNIFICANT SYSTEM, APU HAD AUTO SHUTDOWN, FAULT LIGHT ILLUMINATED AND EICAS MSG APU FAULT DISPLAYED. TROUBLESHOT PER FIM 49-11-00 FIG 110. FOUND BAD OIL COOLER BYPASS VALVE. REMOVED AND REPLACED VALVE PER AMM 49-27-10, OPS AND LEA K CKS GOOD. 2 L 7 2 4F RT A1NM 20081125 WP 2008 11 25 AALA200810098 1 20081020 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 RIGHT CUSP VERTICAL ANGLE CORRODED AT STATION 200. INSTALLED NEW VERTICAL ANGLE. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810047 1 20081006 A 5320 STRAP DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 STATION 1193 IN AFT CARGO, WEB STRAP HAS CORROSION AT LONGERON 28R TO 29R. INSTALLED NEW STRAP PER SRM 51-30. 2 L 7 2 4F RT A6WE 20081125 NM 2008 11 25 SWAA086358 1 20081118 A 5311 6558280 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086389 1 20081119 A 3350 PL22300L STRIP BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 405WN 27893 DURING SCHEDULED MV2 CHECK, FOUND EEPLS STRIP LOOSE AT ROW 1. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081125 EA 2008 11 25 COMA0860452 1 20081029 A 3230 864808 PSEU CNDAIR CL600 CL6002B19 1900309 EA AVIONICS BAY FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 518CA 25993 7816 GEAR DISAGREE ON CLIMBOUT FROM RDU. NOSE GEAR DID NOT RETRACT. ACFT RETURNED BACK TO RDU, LANDED SAFELY. R&R PSEU. 2 L 7 2 4F RT A21EA 20081125 EU 2008 11 25 USAA920081993 1 20081101 A 2560 P4010021 BATTERY AIRBUS 320 A320231 3930325 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 631AW 77 FLT NR 625 PHX-OAK EMERGENCY EQUIPMENT FORWARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MX R&R FORWARD FLIGHT ATTENDANT FLASHLIGHT BATTERY. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081125 NM 2008 11 25 USAA920081998 1 20081031 A 5311 6546534 FRAME BOEING 737 7374B7 138449C NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03C20853011/010 FUSELAGE FRAME CRACKED AT BS 520 BETWEEN S20L AND S21L. REPAIRED FUSELAGE FRAME AT BS 520 BETWEEN S20L AND S21L IAW SRM 53-00-07 REPAIR 13. 2 L 7 2 4F RT A16WE 20081125 WP 2008 11 25 NWAA084829853 1 20081030 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 762NC 47710 DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE VENTRAL STAIRWAY WAS INOPERATIVE. MX REPLACED TH E BATTERIES. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A6WE 20081125 NM 2008 11 25 USAA920081990 1 20081010 A 5320 65C3184725 WEB BOEING 737 7373G7 138447J NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL MAJOR REPAIR C21 CHECK NR 6139596 CORROSION ON SHEAR WEB AT BS 1016 - BS 1032, BL 0 - RBL 34, WL 208.1. REPLACED SH EAR WEB AT BS 1016 - BS 1032, BL 0 - RBL 34, WL 208.1 IAW B737 SRM 51-10-02-09. 2 L 7 2 4F RT A16WE 20081125 EU 2008 11 25 COEA0808917 1 20081020 A 5730 S57110926200 PANEL AEROSP ATR42 ATR42300 8680920 EU RT CENTER WING CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 917FX 354 FOUND AT COE MAJOR REPAIR AND LEVEL 2 CORROSION. CORROSION ON CENTER WING UPPER SKIN, ON THE CUTOUT FLANGE FOR PANEL 62 2CT. 2 H 7 2 4T RT A53EU 20081125 NM 2008 11 25 SWAA086477 1 20081121 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 WP 2008 11 25 NWAA084839853 1 20081030 A 3397 WIRE DOUG DC9 DC951 3022051 WP EMERGENCY LIGHT BROKEN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 762NC 47710 DURING LINE CHECK, MX FOUND THAT THE LAST EMERGENCY PATHWAY LIGHTING IN THE VENTRAL STAIRWAY WAS INOPERATIVE. MX FOUND A BROKEN WIRE AND REPAIRED IT. 2 L 7 2 4F RT A6WE 20081125 NM 2008 11 25 SWAA086480 1 20081121 A 3350 PL22300 STRIP BOEING 737 7373H4 1384600 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND LT EEPLS STRIP DELAMINATED. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 AALA200802399A 1 20081025 A 2560 BATTERY BOEING 767 767323 1385205 NM FLASHLIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 343AN 33082 SFO - BUSINESS CLASS LEFT FORWARD FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT AT BUSINESS CLASS LEFT FORWARD. SYSTEM G ROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081229 NM 2008 12 29 AALA200802401A 1 20081025 A 3350 LIGHT BOEING 737 737823 13844CB NM ZONE 200 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 923AN 29524 DFW - EMERGENCY LIGHT EXIT IDENTIFIER AT RIGHT NUMBER TWO DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RIGHT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 AALA200802407A 1 20081026 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 192AN 32386 DFW - EMERGENCY BULL NOSE LIGHTS AT SEAT ROW 18C INOPERATIVE. REPLACED LAMP AT SEAT ROW 18C. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 20081229 NM 2008 12 29 AALA200802409A 1 20081026 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 192AN 32386 DFW - EMERGENCY BULL NOSE LIGHTS AT SEAT ROW 20C INOPERATIVE. REPLACED LAMP AT SEAT ROW 20C. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 20081230 NM 2008 12 30 UALA2008122607008 1 20081225 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 174UA 24381 THE 21H EMERGENCY LIGHT ON SIDE OF SEAT IS DAMAGED. EMERGENCY LIGHT ASSY REPLACED. CHECKED OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081230 NM 2008 12 30 UALA2008122607009 1 20081225 A 2497 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CONTROL PANEL BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 641UA 25091 FWD CARGO COMPARTMENT P35 POPPING CB`S AS FOLLOW: C171, C173, C167, C168 & C169. FOUND 24 WIRES BURNED OUT UNDER PNL PD U 7L. ALL WIRES ISOLATED AND AFFECTED PDU'S ELECT PLUGS REMOVED AND ISOLATED. FWD CARGO HDG SYS INOP. STARTED TO IDEN TIFY WIRES WITH LABELS. REPAIRED AND OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081230 NM 2008 12 30 UALA2008122206960 1 20081220 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 EMERGENCY PATH LIGHT STRIP INOP RT AISLE, FWD GALLEY. EMERGENCY LIGHT STRIP WIRING GOES UNDER SEAT CONSOLE 1H. REPAIRE D LIGHT WIRING. REPLACED BATTERY. OP CHKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081230 NM 2008 12 30 UALA2008122206961 1 20081220 A 3397 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 EMERGENCY EXIT SIGN LIGHT INOP DOOR 1R. LOWER LEFT SIGN LIGHT. FLOOR SIGN INOP UPPER SIGN WORKS NEEDS FURTHER TROUBLES HOOTING. REPLACED LIGHT EXIT SIGN, NO HELP. SUSPECT BAD POWER SUPPLY: M1552. REPLACED ECT WIRING TO THE LIGHT. OP CHE CKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081230 NM 2008 12 30 UALA2008122306963 1 20081220 A 3610 2780539107 ISOLATION VALVE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RIGHT FAULTY A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 673UA 29241 THE 'R ISLN VALVE' ILLUMINATED. ASSOCIATED BLD ISLN VLV EICAS MSG IS DISPLAYED. REPLACED R ISOLATION VALVE. CHECKS GO OD, NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081230 2008 12 30 UALA2008122306968 4 20081222 A 2565 62774421 SLIDE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE L4 DOOR FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 769UA 26921 THE 4L ENTRY DOOR WILL NOT OPEN GIRT BAR JAMS ON FLOOR. REMOVED SLIDE. INSTALLING NEW SLIDE AT DOOR 4L. INSTALLED GIR T BAR. COMPLETED INSTALLATION OF SLIDE AT DOOR 4L. CHECKED DOOR OPENING AND CLOSING AND ARMING AND DISARMING, CHECKS G OOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081230 NM 2008 12 30 UALA2008122206935 1 20081219 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 554UA 26644 FWD CARGO COMPT, FRAME HAS SEVERAL DENTS AT LT BS 540 AND BETWEEN STR 24L-25L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMA GED SECTION OF FRAME AND INSTALLED J-DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081230 2008 12 30 UALA2008122406983 4 20081222 A 2565 31104200 BARREL BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EVAC SLIDE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 664UA PA1309 29236 LEAKING ASPIRATOR BARREL NOT SEALING. REPLACED BARREL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081230 EU 2008 12 30 UALA2008122406984 1 20081223 A 3397 BR963165 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 479UA 1538 SEAT MOUNTED EMERGENCY LIGHTS AT ROW 10 AND 11 LEFT HAVE BROKEN WIRES. LIGHTS ARE OVERWING EXIT-NOT DEFERRABLE. REPLAC ED UNDER SEAT CABLE P/N 565-2099 ON BOTH ROWS REF IPC 33-51-09, ALL EMERGENCY LIGHTS ALL ROWS OPS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081230 NM 2008 12 30 ASAA0844087 1 20081220 A 5311 65E329621 FRAME BOEING 737 7374Q8 138447Q NM BS 727B CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON FRAME AT BS 727B LBL 15 WL 155. REPAIRED FRAME PER SRM 53-00-07 REPAIR 4 2 L 7 2 4F RT A16WE 20081230 EU 2008 12 30 UALA2008122406985 1 20081223 A 3350 BR964421 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 479UA 1538 SEAT 18 EMERGENCY LIGHT IS INOP. REPLACED EMERGENCY LIGHT ON SEAT ROW END CAP AT POSITION 18C, OPS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081230 NM 2008 12 30 ASAA0844088 1 20081220 A 5347 655384410 CARGO TRACK BOEING 737 7374Q8 138447Q NM BS 947.5-577 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON AFT CARGO TRACK BS 945 RT RBL 13. REPLACED AFT CARGO BAY FLOOR TIE DOWN TRACK FROM BS 847 945 RBL 13. 2 L 7 2 4F RT A16WE 20081230 EU 2008 12 30 UALA2008122406992 1 20081223 A 5320 SILL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 406UA 454 L2 DOOR SILL HAS CORROSION AT AFT GIRT FITTING. MAJOR REPAIR. INSTALLED ANGLE REPAIR. 2 L 7 2 4F 4 F RT A28NM E40NE 20081230 NM 2008 12 30 AALA200802418A 1 20081027 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 771AN 29579 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 25C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25C. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081230 NM 2008 12 30 AALA200802419A 1 20081027 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AA 24486 DFW - EMERGENCY LIGHT AT SEAT ROW 12ABC MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 12ABC. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081230 NM 2008 12 30 AALA200802422A 1 20081028 A 7932 DRIVE SHAFT BOEING 757 757223 1384957 NM RROYCE RB211 RB211535E4 54555 NE NR 1 ENGINE LEAKING A AALA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 649AA 1227 24607 31009 MIA INFLIGHT - NR 1 ENGINE OIL PRESSURE ND QUANTITY LOSS DURING CRUISE. CREW SHUT DOWN NR 1 ENGINE. RETURNED TO MIA AN D LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME 50 MINUTES. REPLACED NR 1 ENGINE ON 28 OCT AT MIA DUE TO LEAK FROM RADIA L DRIVE SHAFT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A2NM E12EU 20081230 WP 2008 12 30 AALA200802423A 1 20081028 A 3350 LAMP DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9404V 53140 LGA - OVERHEAD EMERGENCY EXIT LIGHT AT FIRST CLASS LAVATORY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT FIRST CLA SS LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081230 EU 2008 12 30 UPS08154227 1 20081219 A 3397 CONNECTOR AIRBUS A300 A300F4622R 3930360 EU CABIN LOOSE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 156UP 0845 INSPECTION TYPE:N/A ARM REPORTS EXIT LIGHTING DU GR ENTRY DOOR INTERMITTENT. FOUND LOOSE CONNECTOR ON EXIT MODULE, RESE CURED. OPS CHECK NORMAL IAW MM 33-51-13-04. 2 L 7 2 4F RT A35EU 20081230 WP 2008 12 30 UPS08854234 1 20081212 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQ 803-F1-126 FS 1703 L24-26L ROUND FLUSH REPAIR 1.0 INCH DIA. HAS NO SRM. REF PER APPX G A ND REQUIRES ENGINEERING. REMOVED 2 EXISTING REPAIRS, FABBED AND INSTALLED DOUBLER, FILLER, AND IA FINGER DOUBLER IAW EA 008-5330-01-A1577 AND EO DC8-5330-31577-A. 2 L 7 4 4F RT 4A25 20081230 WP 2008 12 30 UPS08854235 1 20081212 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP SEQ 803-W3-23 LT O/B FLAP STA 340 SKIN PLATING EO DC8-5100-30418C APP X H STEP 1 MARKED NO REQUIRES E NGINEERING EVAL. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW SAA EA 008-5730-01-A 1578 AND EO3 DC8-5730-31635-A. 2 L 7 4 4F RT 4A25 20081230 WP 2008 12 30 UPS08854236 1 20081212 A 5720 FUEL TANK DOUG DC8 DC873F 302199F WP RGIHT AUX DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR 803-W4-23 RT AUX TANK, LOWER, XFS53, HAS NO SRM REF AND REQUIRES ENGINEERING DISPOSITION. REM OVED EXISTING REPAIR. FABRICATED AND INSTALLED REPAIR WITH UPS EO DC8-5730-31576-A. 2 L 7 4 4F RT 4A25 20081230 NM 2008 12 30 UPS08554233 1 20081222 A 5270 INDICATION SYS BOEING 757 75724APF 1384969 NM FWD ENTRY MALFUNCTIONED A IPXA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 01 423UP 25325 INSPECTION TYPE:N/A EICAS MSG L FWD ENT DOOR DISPLAYED & ENTRY DOORS OPEN LIGHT ILLUMINATED WITH DOOR CLOSED. ***SDR FI LED OPEN*** DEFERRED PER MEL 52-71-1 M-391356. VERIFIED L1 DOOR CLOSED & LOCKED. OK FOR SERVICE. DEFERRAL REMAINS. 2 L 7 2 4F RT A2NM 20081230 WP 2008 12 30 UPS08854218 1 20081012 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR 803-F1-22, STA 490-510, L23R-L25R, HAS NO SRM REFERENCE AND REQUIRES EO APPX F. REMOVED EXIST ING REPAIR. FABRICATED AND INSTALLED NEW REPAIR REF DC-8 SRM 53-02-01 FIG 7 SHT 4. 2 L 7 4 4F RT 4A25 20081224 NM 2008 12 24 USAA2008121792261 1 20081125 A 5340 65353642 STRINGER CLIP BOEING 737 7373G7 138447J NM BS 986.5 S25L CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - STRINGER TIE CLIP CRACKED AT BS 986.5, S25L. REPLACED STRINGER TIE CLIP AT BS 986.5, S25L I AW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081224 NE 2008 12 24 ASAA0854060 2 20081216 A 7200 CFM567B27 ENGINE BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 2 SURGES A ASAA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 NM 02 577AS 6943 35186 894542 ON CLIMBOUT OF OAK THROUGH FL 370 THE NR 2 ENGINE BEGAN TO SURGE FOR A FEW SECONDS. N1 EXCEEDED LIMIT (105.0). AUTO TH ROTTLES DISENGAGED AND NR 2 THRUST LEVER REDUCED TO NR 2 N1 OF 98.0. THIS BROUGHT ALL INDICATIONS TO NORMAL. FLIGHT CO NDITIONS WERE CLEAR AND SMOOTH AIR. REMOVED NR 2 ENG SN 894542 IAW T/C 78471000. ASA TECH 94411. REPLACED NR 2 ENG WI TH SN 896771 PN CFM56 7B27/3 PER T/C 78471001 W/O NR 6637. ENG SN THAT WAS REMOVED IS 894542. SYSTEMS PERFORMED SATISFAC TORILY VERIFICATION FLIGHT WAS SATISFACTORY. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081230 NM 2008 12 30 HNAA2008121000344 1 20081211 A 7797 30005000047 TORQUE SENSOR DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE CONTAMINATED A HNAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 07 938HA 29767 9080 152 ON TAKEOFF NR 1 ENGINE TORQUE DROP TP 40 PERCENT IN FLUX THE INCREASED OVER 108 PERCENT FOR 15 SECOND PROPELLER RPM DROP TO 350. REMOVED TORQUE SENSOR CONTROL UNIT NR 1 ENGINE. FOUND MOISTURE IN CONNECTOR. REPLACED TORQUE SENSOR CONTROL UNIT. 2 H 7 2 4T RT A13NM 20081230 NM 2008 12 30 HNAA2008121000346 1 20081213 A 3350 OL3071BPEGPL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 912HA 58428 58428 040 FIRST FLOOR EMERGENCY LIGHT INOP. RELAMPED 1ST EMERGENCY LIGHT BULB. 2 H 7 2 4T RT A13NM 20081230 EA 2008 12 30 COMA2008122670007 1 20081226 A 3040 165911 CONTROLLER CNDAIR CL600 CL6002C10 1390015 EA WINDOW HEAT FAULTY A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 658CA 12250 10148 EN ROUTE ATL-YYZ RECEIVED A LEFT WINDOW HEAT CAUTION MESSAGE, FLGIHT DIVERTED TO CVG. REPLACED THE LEFT WINDOW HEAT CON TROLLER. 2 L 7 2 4F RT A21EA 20081230 EA 2008 12 30 COMA2008122750048 1 20081227 A 2613 OVERHEAT LOOP CNDAIR CL600 CL6002B19 1900309 EA RT PYLON OUT OF POSITION A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 916CA 7014 EN ROUTE PHL-BOS RECEIVED A RIGHT 14TH STAGE DUCT MESSAGE, FLIGHT RETURNED TO PHL. REPOSITIONED THE RIGHT PYLON HEAT DE TECTION LOOP. 2 L 7 2 4F RT A21EA 20081230 NM 2008 12 30 HNAA2008122000352 1 20081220 A 2424 51539008D GCU DHAV DHC8 DHC8102 2809003 NM COCKPIT ODOR A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 807EX 31310 6 292 ELECTRICAL SMELL ABOUT CABIN CIRCUIT BRAKER PANEL. INSPECT CABIN CIRCUIT BRAKER PANEL NO DEFECT FOUND. FOUND NUMBER 1 G ENERATOR CONTROL UNIT BURNED SMELL. REMOVED AND REPLACE GENERATOR CONTROL UNIT AND STARTER GENERATOR REFERENCE HA 300 S EQUENCE 5. REMOVED AND REPLACE BUS TIE RELAY FOR NON FUNCTIONING. REFERENCE SEQUENCE 6 HA 300. ALL GROUND RUN COMPLET ED SATISFACTORY. 2 H 7 2 4T RT A13NM 20081230 NM 2008 12 30 HNAA200082300360 1 20081218 A 3350 8241162003 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM COCKPIT FAULTY A HNAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 07 810EX 41233 41233 308 FLOOR EMERGENCY LIGHT INITIALLY ILLUMINATED WHILE ENGINES ARE RUNNING. GROUND RAN AIRCRAFT, CANNOT DUPLICATE, REMOVED A ND REPLACED EMERGENCY LIGHT CONTROL BOX, OPS CHECK GOOD IAW 33-52-00. 2 H 7 2 4T RT A13NM 20081230 NM 2008 12 30 HNAA2008122300361 1 20081222 A 3234 574205A SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A HNAA O OTHER O OTHER LD LANDING 1 EA 07 815EX 35230 10012 321 NOSE GEAR FAILED TO EXTEND BY NORMAL PROCEDURE, REQUIRED ALTERNATE EXTENSION. REMOVED AND REPLACED GEAR SELECTOR VALVE IN REFERENCE MAINTENANCE MANUAL 32-30-41. REMOVED AND REPLACED GEAR HANDLE SELECTOR VALVE IN ACCORDANCE WITH MAINTENAN CE MANUAL 32-30-41. CYCLED GEAR SEVERAL TIMES, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 20081230 NM 2008 12 30 HNAA2002120800351 1 20081208 A 2120 UNKNOWN DHAV DHC8 DHC8102 2809003 NM COCKPIT ODOR A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 936HA 145 DURING OPERATIONS, AN OIL ODOR WAS NOTICED IN THE COCKPIT WITH BLEEDS SELECTED ON. OIL LEVELS IN BOTH ENGINES AND THE A CM UNIT WERE CHECKED AND FOUND TO BE GOOD. BOTH ENGINE NACELLES WERE INSPECTED FOR EVIDENCE OF OIL LEAKS, WITH NONE BEI NG FOUND. ENGINES WERE RUN ON THE GROUND WITH BLEEDS SELECTED ON WITH NO ODORS BEING DETECTED. THE AIRCRAFT WAS THEN R ELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 20081230 NM 2008 12 30 ASAA0844079 1 20081210 A 5320 CARGO TRACK BOEING 737 7374Q8 138447Q NM CARGO BAY DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 MECHANICAL DAMAGE DOUBLE HOLES ON CARGO TIE DOWN STRAP. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 ASAA0844081 1 20081209 A 5751 FITTING BOEING 737 737490 1384715 NM RT AILERON GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 794AS 28889 RT AILERON O/B CORNER FWD EDGE FITTING IS GOUGED. REMOVED GOUGED FITTING INSTALLED REPLACEMENT FITTING IAW B737 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 AALA200802480A 1 20081108 A 3350 LIGHT BOEING 757 757223 1384957 NM SEAT 29D BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 698AN 26980 DFW - EMERGENCY LIGHT AT SEAT 29D IS BROKEN. REPLACED LIGHT ASSEMBLY FOR SEAT 29D. SYSTEM GROUND CHECKED NORMAL OPERAT ION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802481A 1 20081108 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 698AN 26980 DFW - EMERGENCY EXIT MARKER LIGHT ASSEMBLY AFT OF RIGHT AFT PASSENGER DOOR IS BROKEN. REPLACED LIGHT ASSEMBLY AFT OF RI GHT AFT PASSENGER DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802482A 1 20081108 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 698AN 26980 DFW - EXTERIOR EMERGENCY SLIDE LIGHT AFT OF THE LEFT AFT PASSENGER DOOR INOPERATIVE. SECURED LAMP FOR EXTERIOR EMERGENC Y SLIDE LIGHT AFT OF THE LEFT AFT PASSENGER DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802498A 1 20081109 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 671AA 25336 DFW - EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. SECURED LOOSE CONNECTOR AS SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F RT A2NM 20081231 WP 2008 12 31 AALA200802451A 1 20081101 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 259AA 49289 LGA - OVERHEAD EMERGENCY LIGHTS AT SEAT ROW 24 INOPERATIVE. REPLACED BATTERY AND CHARGER AT SEAT ROW 25DEF. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081231 WP 2008 12 31 AALA200802452A 1 20081101 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 259AA 49289 LGA - EMERGENCY LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081231 WP 2008 12 31 AALA200802453A 1 20081101 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 259AA 49289 LGA - EMERGENCY LIGHTS AT AFT GALLEY DROP DOWN PANEL INOPERATIVE. REPLACED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHT S. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 SWAA086481 1 20081121 A 3350 PL22300 STRIP BOEING 737 7373H4 1384600 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND RT EEPLS STRIP DELAMINATED. REMOVED AND REPLACED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086482 1 20081121 A 3350 6575342 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND OVERWING EMERGENCY EXIT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086487 1 20081121 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086488 1 20081121 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086490 1 20081121 A 5754 6573714 SKIN BOEING 737 7373H4 1384600 NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND LT WING SLAT I/B UPPER SURFACE DELAMINATED. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086491 1 20081121 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 EA 2008 11 25 COMA0860458 1 20081106 A 5311 6013600129 FRAME CNDAIR CL600 CL6002B19 1900309 EA FS 640 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 783CA 7315 LT FS 640 FRAME DOUBLER IS CRACKED BETWEEN STR 9 AND 12. REMOVED DAMAGED PARTS AND COMPLIED WITH MODIFICATION K601R3600 9-3 ON LT FS 640 FRAME AND DOUBLER PER SB601R-53-061 KIT DRWG. K601R36009 REV B AND 601R5361569 REV A. 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 USAA920081992 1 20081028 A 5320 6552870501 FITTING BOEING 737 7373S3 138449H NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 316AW 23713 MCN DROP IN MAJOR REPAIR NR 6134962 FORWARD UPPER SEAL FITTING FOR R2 DOOR CUT-OUT IS CRACKED BS951, S10R. REPLACED FOR WARD UPPER SEAL FITTING FOR R2 DOOR CUT-OUT AT BS951, S10R IAW B737 SRM 51-40-02-0G. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 USAA920081995 1 20081031 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753006/007 FUSELAGE FRAME SUPPORT CRACKED AT BS294.5 AT S7L. REPAIRED FUSELAGE FRAME SUPPOR T AT BS294.5 AT S7L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081125 EA 2008 11 25 COMA0860460 1 20081106 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 783CA 7315 LT WING 540BB FUEL PANEL CUTOUT HAS FRETTING CORROSION. REPAIRED LT WING FUEL ACCESS PANEL CUTOUT 540BB AT WS 54.897 AS PER CRJ REO 601R-57-21-030 REV. G FIG 6 DETAIL III. 2 L 7 2 4F RT A21EA 20081125 EA 2008 11 25 COMA0860459 1 20081106 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 783CA 7315 RT WING 640BB FUEL PANEL CUTOUT HAS FRETTING CORROSION. REPAIRED RT WING FUEL ACCESS PANEL CUTOUT 640BB AT WS 54.897 AS PER CRJ REO 601R-57-21-030 REV. G FIG 6 DETAIL III. 2 L 7 2 4F RT A21EA 20081125 2008 11 25 COEA0802788 4 20081016 A 2350 6114302 SWITCH CESSNA 208 208B 2073701 CE CONTROL WHEEL INOPERATIVE A COEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 13 788FE 208B0286 RETURN TO BLOCKS. FLT NR 8690 PDX TO MFR. ACFT TAXIED TO RUNWAY RUN UP AREA. WITH ENGINE RUNS COMPLETED, ATTEMPTS TO C ONTACT CLEARANCE DELIVERY FOUND NO VOICE BEING TRANSMITTED FROM EITHER NR 1 OR NR 2 RADIOS. ACFT WAS TAXIED BACK SAFELY TO BLOCKS FOR MX. R&R THE PILOTS PUSH TO TALK SWITCH. 1 H 7 1 3T A37CE 20081125 NM 2008 11 25 SWAA086505 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 520, STR 2L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 EA 2008 11 25 COMA0860453 1 20081107 A 5740 601R102371 FITTING CNDAIR CL600 CL6002B19 1900309 EA LT MLG ACTUATOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 784CA 7319 LT MLG SIDE STAY ACTUATOR UPPER FITTING CRACKED. R&R SERVICEABLE LT SIDE STAY ACTUATOR UPPER FITTINGS. 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 SWAA086510 1 20081121 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND AFT CARGO FLOOR SUPPORT BEAM CORRODED AT BS 767 + 7, LBL 8. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081124 NM 2008 11 24 UALA2008112006582 1 20081119 A 2130 AS150528A0032 DUCT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN PRESSURE DAMAGED A UALA A UNSCHED LANDING O OTHER UK UNKNOWN 1 WP 29 523UA 24932 PRESSURIZATION PROBLEM. RTFL. REPLACED BLOWN FLEX DUCT. 2 L 7 2 4F 4 F RT A2NM E17NE 20081231 WP 2008 12 31 AALA200802455A 1 20081101 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 437AA 49455 SFO - EMERGENCY BATTERY PACK AT SEAT ROW 8 INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 8. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A6WE 20081231 NM 2008 12 31 AALA200802456A 1 20081101 A 2782 5006397R ACTUATOR BOEING 757 757223 1384957 NM NR 2 SLAT FAULTED A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 618AA 24526 BOS INFLIGHT - LEADING EDGE SLAT DISAGREE INDICATION WHEN FLAPS SELECTED TO ONE AT 21 KNOTS. LANDED BOS WITHOUT INCIDEN T. FOUND NUMBER ONE SLAT AND NR 2 ROTARY ACTUATOR TRIPPED. REPLACED NR 2 SLAT ROTARY ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802457A 1 20081102 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 772AN 29580 NRT - EMERGENCY LIGHT LENS AT FIRST CLASS CLOSET DOOR MISSING. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT FIRST CLA SS CLOSET DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 AALA200802460A 1 20081103 A 2910 B-NUT BOEING 767 767323 1385205 NM HYD LINE LEAKING A AALA J A DUMP FUEL UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 349AN 33088 JFK INFLIGHT MIA TO CDG - LEFT HYDRAULIC QUANTITY LOW INDICATION. LANDED JFK WITHOUT INCIDENT. FOUND RUDDER AREA WET A ND LEAKING B NUT FITTING AT HYDRAULIC BLOCK IN VERTICAL FIN. REPLACED SEAL AND SECURED B NUT. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 AALA200802507A 1 20081111 A 3397 CONTACT BOEING 767 767323 1385205 NM EMERGENCY LIGHT DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 344AN 33083 SFO - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR INOPERATIVE. CLEANED CONTACTS FOR EXTERIOR EMERGENCY LIGHT AT LE FT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 AALA200802508A 1 20081111 A 3397 CONTACT BOEING 767 767323 1385205 NM EMERGENCY LIGHT DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 344AN 33083 SFO - EMERGENCY LIGHT AT LEFT AFT LOWER FUSELAGE INOPERATIVE. CLEANED CONTACTS FOR EMERGENCY LIGHT AT LEFT AFT LOWER FU SELAGE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 AALA200802509A 1 20081106 A 5330 SKIN BOEING 767 767323 1385205 NM BS 437 S36 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 366AA 25193 AFW - FUSELAGE SKIN AT STATION 437 AT STRINGER 36 JUST AFT OF THE SECTION 41/43 BUTT SPLICE AND ABOVE A SKIN LAP JOINT H AS CORROSION BLENDED. MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIRED IN ACCORDANCE WITH MRB 767 3337. 2 L 7 2 4F RT A1NM 20081231 SO 2008 12 31 C2XA08IA265 1 20081221 A 3260 8005701 PROXIMITY SWITCH EMB 145 EMB145EP 3260221 SO NLG FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15926 145005 FLIGHT 4920 - THE AIR/GROUND FAIL MESSAGE ILLUMINATED DURING CLIMB AND THE CREW ELECTED TO RETURN TO IAH. MAINTENANCE R EMOVED AND REPLACED THE NOSE LANDING GEAR PROXIMITY SWITCH TO CORRECT THE DISCREPANCY, PERFORMED SUCCESSFUL LANDING GEAR EXTENSION/RETRACTION TESTS AND CLEARED THE DISCREPANCY. 2 L 7 2 4F RT T00011AT 20081231 NM 2008 12 31 AALA200802558A 1 20081122 A 3350 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 MIA - EMERGENCY LIGHTS FROM SEAT ROW 30 TO AFT BOTH AISLES INOPERATIVE. REPLACED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 AALA200802559A 1 20081122 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 MIA - EMERGENCY LIGHT AT SEAT 18C MISSING LAMP. REPLACED LAMP AT SEAT 18C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 AALA200802565A 1 20081122 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 785AN 30005 MIA - EMERGENCY LIGHT AT SEAT 41C MISSING LAMP. REPLACED LAMP AT SEAT 41C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 AALA200802484A 1 20081108 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 24599 LGA - EMERGENCY LIGHT AT R3 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT R3 DOOR. SYSTEM GROUND CHECKED NORM AL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802435A 1 20081029 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 194AA 32388 DFW - EMERGENCY LIGHT AT LEFT DOOR INOPERATIVE. RESET LAMP FOR EMERGENCY LIGHT AT LEFT DOOR. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802502A 1 20081110 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 760AN 31477 MIA - SEAT MOUNTED EMERGENCY LIGHT LENS IS MISSING AT SEAT 22C. REPLACED LENS AT SEAT 22C. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 AALA200802500A 1 20081110 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 760AN 31477 MIA - SEAT MOUNTED EMERGENCY LIGHT LENS IS MISSING AT SEAT 21C. REPLACED LENS AT SEAT 21C. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT T00001SE 20081231 WP 2008 12 31 AALA200802463A 1 20081104 A 7930 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 2 LOW PRESSURE A AALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 592AA 724 53255 718507 INFLIGHT - ABOUT 160 MILES OUT OF DFW NUMBER TWO ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED ALONG WITH ZERO OIL PRESSURE READING. OIL TEMPERATURE AT 30C. CREW SHUT DOWN NR 2 ENGINE. LANDED DFW WITHOUT INCIDENT. REPLACED NR 2 ENGINE ON 4 NOV AT DFW DUE TO OIL PRESSURE OUT OF LIMITS AND REQUIRED OIL SYSTEM COMPONENT INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A6WE E9NE 20081231 NM 2008 12 31 AALA200802464A 1 20081105 A 3350 OL3071BPEGPL LAMP BOEING 767 767323 1385205 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 381AN 25450 JFK - EMERGENCY LIGHT AT SEAT 23B MISSING LAMP. REPLACED LAMP AT SEAT 23B. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 AALA200802465A 1 20081106 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 195AN 32389 DFW - EMERGENCY LIGHT AT SEAT ROW 18DEF MISSING LENS. REPLACED LENS AT SEAT ROW 18DEF. SYSTEM GROUND CHECKED NORMAL OP ERATION. 2 L 7 2 4F RT A2NM 20081231 EA 2008 12 31 MASA2008122200752 1 20081222 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY MALFUNCTIONED A MASA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SW 07 75987 7405 ASH 7065 IAD-EWR. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD DUE TO A LAV SMOKE WARNING. MX FOUND LAV FAN C/ B POPPED, RESET C/B AND FAN OPS NORMAL. MX PERFORMED POWER RUNS WHILE ISOLATING PACKS AND OPERATING LAV FAN. NO SMELL OR VISUAL SMOKE PRESENT. 2 L 7 2 4F RT A21EA 20081231 EU 2008 12 31 AALA200802467A 1 20081106 A 3350 BR964814 LIGHT AIRBUS 300 A300B4605R 3930308 EU SEAT 7C BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14065 508 JFK - EMERGENCY LIGHT ASSEMBLY AT SEAT 7C BROKEN. REPLACED LIGHT ASSEMBLY AT SEAT 7C. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F RT A35EU 20081231 EU 2008 12 31 AALA200802470A 1 20081106 A 3350 BR964814 LIGHT AIRBUS 300 A300B4605R 3930308 EU SEAT 12G BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 14065 508 JFK - EMERGENCY LIGHT ASSEMBLY AT SEAT 12G BROKEN. REPLACED LIGHT ASSEMBLY AT SEAT 12G. SYSTEM GROUND CHECKED NORMAL O PERATION. 2 L 7 2 4F RT A35EU 20081231 NM 2008 12 31 NOCA09408 1 20081220 A 2610 033688 BLOWER BOEING 767 767324 1385203 NM NR 1 MALFUNCTIONED A NOCA K NONE J WARNING INDICATION UK UNKNOWN 1 EA 15 767NA 27569 REF CI 26-08 EICAS MAINT MSG "AFT DET FAN" ON MAINT PAGE. REPLACED AFT NR 1 DETECTOR P/N 2166-604A, S/N 23154B, NO HELP ACCOMPLISHED FIM 26-16-00 FIG 105, BLOWER NR 1 M718 AND RELAY K332 P/N BACR13CE2, NO S/N FOR AFT CARGO. EICAS MSG CLE ARED IAW 26-16-02. 2 L 7 2 4F RT A1NM 20081231 WP 2008 12 31 AALA200802474A 1 20081108 A 2910 HOSE DOUG DC9 DC983 3022083 WP HYD SYSTEM LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 9619V 53566 DFW INFLIGHT - RIGHT MAIN LANDING GEAR RED LIGHT ON WITH GEAR UP. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLAC ED HYDRAULIC FLEX LINE FOR RIGHT MAIN LANDING GEAR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081231 NM 2008 12 31 AALA200802528A 1 20081117 A 2913 PUMP BOEING 757 757223 1384957 NM HYDRAULIC SYS FAILED A AALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 21 699AN 27051 INFLIGHT - CREW REPORTED CENTER HYDRAULIC SYSTEM QUANTITY LOSS. LANDED DFW WITHOUT INCIDENT. REPLACED NUMBER TWO CENTE R HYDRAULIC PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802541A 1 20081120 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 781AN 29586 DFW - EMERGENCY LIGHT AT SEAT 26C INOPERATIVE. REPLACED LAMP AT SEAT 26C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 2008 12 31 AALA200802544A 4 20081121 A 8300 SEAL BOEING 767 767323 1385205 NM GE CF6 CF680C2B6 30025 NE NR 2 ENG GEARBOX LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 357AA 14 24038 690306 INFLIGHT FCF - APPROXIMATELY FIVE MINUTES AFTER LEVEL OFF AT 40000 FEET OIL QUANTITY INDICATION ILLUMINATED OR NUMBER TW O ENGINE THEN WENT RAPIDLY TO ZERO. OIL PRESSURE BEGAN TO DROP AND OIL TEMPERATURE BEGAN TO RISE. REDUCED ENGINE TO ID LE. ON DESCENT OIL QUANTITY BEGAN TO RISE AND OIL PRESSURE AND TEMPERATURE NORMALIZED. OIL TEMPERATURE OR PRESSURE NEV ER WENT TO AMBER BAND. NO EICAS MESSAGE ON OIL QUANTITY. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE ON 25 NOV AT JFK DUE TO INLET GEARBOX SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A1NM E13NE 20081231 NM 2008 12 31 AALA200802552A 1 20081121 A 3350 SHROUD BOEING 757 757223 1384957 NM EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 635AA 24593 DFW - EMERGENCY LIGHT SHROUD AT AFT SEAT 28D IS BROKEN. REPLACED SHROUD AT AFT SEAT 28D. SYSTEM GROUND CHECKED NORMAL O PERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802554A 1 20081122 A 3350 MODULE BOEING 757 757223 1384957 NM EMERGENCY LIGHT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 679AN 29589 DFW - EMERGENCY LIGHTS AT FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER ASSEMBLY. SYSTEM GROUND CHECKED N ORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802555A 1 20081122 A 3350 BATTERY PACK BOEING 737 737823 13844CB NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 976AN 30099 DFW - EMERGENCY LIGHT AT RIGHT FORWARD OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20081231 WP 2008 12 31 AALA200802556A 1 20081122 A 8012 9794104 START VALVE DOUG DC9 DC983 3022083 WP NR 2 ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 9621A 53592 INFLIGHT ORD TO LAX - RIGHT START VALVE OPEN INDICATION ILLUMINATED AT FL300. REDUCED NUMBER TWO ENGINE TO IDLE. LIGHT FLICKERED ON AND OFF THROUGH DESCENT AND LANDING. LANDED MCI WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE START VALVE . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20090105 EA 2009 1 5 SWIA200820712 1 20081224 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 367CA 10069 FLT 4583 - NR 4 EMERGENCY FLOODLIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820713 1 20081121 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 468CA 7649 C-CHECK, DURING LEFT FS 484 INTERCOSTAL ANGLE AT LBL36 CRACKED IN UPPER RADIUS. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081124 WP 2008 11 24 WRLA2008088 1 20080827 A 5330 SKIN DOUG DC10 DC1030 3023501 WP FUSELAGE CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 139WA 46583 DURING C1 INSPECTION FOUND FASTENER HOLE CORRODED AT STA 2160 BETWEEN LONGERON 13R - 14R. REAMED HOLE TO REMOVE DAMAGE, EDDY CURRENT INSPECTION ACCOMPLISHED. MFG AND INSTALLED BUSHINGS AND REPAIR DOUBLER, TREAT, PRIME, SEAL AND PAINT IAW ENGINEERING REPAIR. (K) 2 L 7 3 4F A22WE 20081124 NM 2008 11 24 UIEA200800329 1 20081012 A 5730 SKIN PANEL BOEING 747 747228F 1384895 NM RT WING DEBONDED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 809MC 20887 RT WING UPPER SURFACE L/E PANEL AT ILES 328.5 HAS A PREVIOUS REPAIR AREA 7.0 BY 6.0 INCHES DISBONDING AND CRACKING. PER MANENT REPAIR ACCOMPLISHED IAW SRM 51-40-09, FIG 18, SHEETS 2 AND 5, PREPREG 250 DEGREE F CURE IAW SRM 51-40-12. ALSO, REF EO NR 4757A465. 2 L 7 4 4F RT A20WE 20081125 NM 2008 11 25 HALA2008111400853 1 20081114 A 2840 TOTALIZER BOEING 767 76733A 1385209 NM FUEL INDICATOR READS HIGH A HALA O OTHER N FALSE WARNING CR CRUISE 1 WP 13 581HA 28141 TOTALIZER FUEL DISAGREES WITH CALCULATED FUEL ON BOTH CDU'S. CALCULATED FUEL SHOWS HIGHER AND INCREASES AS FLIGHT PROGR ESSED. CDU TOTALIZER FUEL AGREES W/FUEL GAUGE. PERFORMED FIM 28-41-00 SYS IS OK. 2 L 7 2 4F RT A1NM 20081125 NM 2008 11 25 HALA2008111300845 1 20081113 A 5314 KEELBEAM BOEING 767 76733A 1385209 NM BS 965 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 581HA 28141 CORRISION, TOP SURFACE OF KEELBEAM RT INNER FAIRING ATTACHMENT FLANGE AT STA 965. CORRISION REMOVED IAW SRM 53-50-12 FP I, OPEN HOLE INSPECTION, ROTO REEMED, PART AND CPC APLICATION. 2 L 7 2 4F RT A1NM 20081125 EA 2008 11 25 SWIA200820421 1 20081113 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN MALFUNCTIONED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 957SW 7829 FLT 6586 - EMERGENCY FLOOR LIGHTING AT ROW 6, 7, 8 INOP. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20081125 WP 2008 11 25 AALA200810092 1 20081020 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 AFT CARGO, CORROSION ON OUTBOARD LEG AND CLIPNUT HOLES OF RIGHT TIE DOWN TRACK AT STATION 1211-1309. REMOVED AND REPLAC ED TIE DOWN TRACK PER SRM 51-30-1. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 HALA2008111700854 1 20081117 A 2997 CONNECTOR BOEING 767 76733A 1385209 NM HYD PUMP LOOSE A HALA B EMER. DESCENT N FALSE WARNING TX TAXI/GRND HDL 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, RT HYD PRIME PUMP ANNUNCIATED ON EICAS ASSOC SWITCHED LIGHT (PRESS) ILLUMINATED BTB. C/W FIM 29-11-00, SECURED RT ENG HYD PUMP CONNECTOR D10980, OPERATED RT ENG PER MM 71-00-00, R ENG PRIMARY PRESS LIGHT EXTINGUIS HED, NO MESSAGE ON EICAS, SYSTEM PRESS NORMAL, NO LEAKS ON RT ENG PUMP NOTED. NO OTHER DEFECTS NOTED, OK FOR SVC. 2 L 7 2 4F RT A1NM 20081125 WP 2008 11 25 AALA200810036 1 20081016 A 5340 FITTING DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 510AM 49804 CORROSION ON GALLEY TIE DOWN FITTING. REPLACED GALLEY TIE DOWN FITTING PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081125 EA 2008 11 25 SWIA200820404 1 20080808 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 443SW 7638 C-CHECK, FS 280 RBL9 SUPPORT CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 SWAA086335 1 20081118 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 324SW 23414 DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 303, WL 261. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 HALA2008111500857 1 20081115 A 4990 SEAL BOEING 767 767332 1382001 NM APU OIL CAP WORN A HALA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 596HA 23276 ETOPS SIGNIFICANT SYSTEM, STATUS MESSAGE "APU OIL QTY" ON TAXI IN. APU RUNNING WHEN SHUT DOWN, MSG WENT AWAY. OIL QUAN TITY LOW. RESERVICED OIL OPS CHECK GOOD NO LEAKS NOTED PER REF 49-11-00 FIG 116. FOUND OIL CAP RING WORN AND COCKED AN D NOT SECURED PROPERLY, RE-SECURED AND REPLACED SEAL. 2 L 7 2 4F RT A1NM 20081125 NM 2008 11 25 HALA2008111600859 1 20081116 A 3222 STRUT BOEING 717 717200 1383700 NM NLG DISCHARGED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 483HA 55128 ATB - NOSE DID NOT RETRACT AFTER TAKEOFF. FOUND NOSE STRUT COMPRESSED NO LEAKS NOTED. REPLACED AIR CHARGING VALVE SERV ICED STRUT PER MM32-21-01, RETRACTION CK GOOD. 2 L 7 2 4F TR A6WE 20081125 NM 2008 11 25 SWAA086357 1 20081118 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 WP 2008 11 25 AALA200810063 1 20080930 A 5320 ANGLE DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 496AA 49734 LEFT TORQUE TUBE VERTICAL ANGLE CRACKED AT CENTER AREA, AFT ACCESSORY. INSTALLED SERVICEABLE ANGLE. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 08FDEA04934 1 20081119 A 5710 65216562 SUPPORT BEAM BOEING 727 727227 1384078 NM ZONE 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 495FE 21669 FASTENERS LOOSE LWR SIDE OF NR 7 SPOILER FITTING. UPON FURTHER EVALUATION FOUND IMPROPER REPAIR IAW DRAWING SR27-57-038 . REPAIRED LT WING INBD SPOILER SUPPORT BEAM IAW DRAWING SR 27-57-038 REV C, SEE WO NR 00042909, N/R N00197, JPF FOR DE TAILS. 2 L 7 3 4F A3WE 20081125 WP 2008 11 25 AALA200810056 1 20081009 A 5330 SKIN DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 469AA 49599 CRACK AT FASTENER HOLE STATION 191 LONGERON 22 LEFT. DAMAGE CUTOUT AT REPAIRED PER ESO 80559 DATED 10/3/08 AND BOEING S ERVICE REWORK DRAWING SRO9530219. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 SWAA086388 1 20081119 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 355SW 25250 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 294, LBL 52. REPAIRED WEB PER EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086476 1 20081121 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086492 1 20081121 A 5311 6546557 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 601WN 27695 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 2008 11 25 SWAA086498 4 20081120 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C3 CHECK, FOUND L2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086500 1 20081120 A 3211 6552235 SUPPORT FITTING BOEING 737 7373A4 1384585 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C3 CHECK, RT MLG SIDE STRUT SUPPORT FITTING FWD AND AFT LUG BORE CORRODED. REPAIRED FITTING PER SWA EA . 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086515 1 20081121 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086518 1 20081121 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND EMERGENCY EXIT SIGN LENS MISSING AT BS 930. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086524 1 20081121 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27L TO STR 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 ABXA200811140266 1 20081029 A 7120 310T10203 MOUNT BOEING 767 767232 1385132 NM ENGINE RUSTED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 746AX 22223 AFT ENGINE MOUNT WAS RUSTED AT LOWER RIGHT LUG. REMOVED AND REPLACED AFT MOUNT ASSEMBLY IAW B767 AMM 71-21-02-4. ENGIN E REMOVED AND REINSTALLED ON JOB CARD 7010. 2 L 7 2 4F RT A1NM 20081125 EA 2008 11 25 ASOA200801064 1 20080826 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 7328 REMOVED (2) TWO CARGO DOOR TIE DOWN BRACKETS AND LOOSENED CARGO DOOR COMING (LOWER) IAW CRJ 200 SRM 51-42-06/51-41-04. REPAIRED DAMAGED INTERCOSTAL IAW BOMBARDIER REO 601R-53-61-2767. REINSTALLED (2) TWO CARGO TIE DOWN BRACKETS & LOOSENED CARGO DOOR COAMING IAW CRJ 200 SRM 51-42-06 & 51-42-040, 51-42-21. SUPPLEMENTAL-SDR CLOSED. 2 L 7 2 4F RT A21EA 20081125 EA 2008 11 25 ASOA200801266 1 20081001 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED PAINT FROM AREA SPECIFIED IAW CRJ AMM TASK 51-26-00-150-803. REQUIRES INVESTIGATION. REMOVED AND REPLACED 19 H I-LITES IAW CRJ 200 SRM 51-42-21. ONE EACH RIVET REQUIRES INSTALLATION AT FS 559.32 AT STA 26L. INSTALLED ONE EACH RIV ET AT FS 559.32 AT STA 26L IAW SRM 51-42-06. REQUIRES RESTORATION OF ORIGINAL FINISH. COMPLIED WITH STEPS 6 & 7 OF BOM BARDIER REO 601R-53-51-078. REPAIRED FUSELAGE LOWER SKIN AT FS 559 + 30 IAW REO 601R-53-51-078. ASA EC/TC REQUIRED. A SA EC/TC REO 601R-53-51-078 INCORPORATED. SUPPLEMENTAL-SDR CLOSED 11/13. 2 L 7 2 4F RT A21EA 20081125 NM 2008 11 25 SWAA086420 1 20081120 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 735SA 27867 DURING SCHEDULED HC2 CHECK, LT AFT GALLEY EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PA CK PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086364 1 20081119 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086365 1 20081119 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086366 1 20081119 A 5322 6546546 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086367 1 20081119 A 5313 6551698 STRINGER SPLICE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086413 1 20081120 A 5322 6546529 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 364SW 26575 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER PAE ER. 2 L 7 2 4F RT A16WE 20081125 2008 11 25 SWAA086399 4 20081118 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 627SW 27935 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086455 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 5R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086456 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 480, STR 4R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086457 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 6R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086458 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500A, STR 7R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843750 1 20081026 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 7 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NR 7 SPOILER UPPER SURFACE DENTED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 40 0 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0893702 1 20081108 A 5420 115A29829 BRACKET BOEING 737 737990 NM NR 1 PYLON CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AT RSS 261 LEFT JUST AFT OF NR 1 PYLON FORWARD BRACKET CRACKED AT FIXED UPPER TRAILING EDGE. REMOVED AND REPLACED CRACK ED BRACKET WITH NEW PER SRM 51 40 02 STEP 4B 4C AND SOPM 20 10 1 STEP 2. 2 L 7 4 4F RT A16WE 20081126 NM 2008 11 26 ASAA0893703 1 20081108 A 5420 115A29531 BRACKET BOEING 737 737990 NM NR 1 PYLON CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 319AS 33679 AT RSS 261 LEFT JUST AFT OF NR 1 PYLON AFT BRACKET CRACKED AT FIXED UPPER TRAILING EDGE. REMOVED CRACKED BRACKET AND RE PLACED WITH SERVICEABLE PER SRM 51 40 02 ITEM 9. 2 L 7 4 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843777 1 20081030 A 5315 62C3394116 FLOORBEAM BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 FLOORBEAM CORRODED. REPLACED BEAM CHORD PER SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843776 1 20081106 A 5320 69407653 SPLICE PLATE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 L1 DOOR CUTOUT INNER CHORD SPLICE PLATE IS CORRODED. REPLACED SPLICE PLATE PER SRM 51 40 05. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843757 1 20081107 A 5241 STRUCTURE BOEING 737 7374Q8 138447Q NM R1 DOOR CORRODED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 755AS 54270 002291 25096 R1 DOOR INSIDE HANDLE IS LOOSE MIG 2C 240086 INITIATED FOUND R1 DOOR TORQUE BOX BEARING BORES CORRODED FOR LATCHING CRAN K ASSY. REMOVED AND REPLACED R1 DOOR REF MM 52-41-00. 2 L 7 2 4F RT A16WE 20081126 NE 2008 11 26 ASAA0853755 2 20081105 A 7200 CFM567B27 ENGINE BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE NR 1 MALFUNCTIONED A ASAA K NONE M OVER TEMP IN INSP/MAINT 1 NM 02 577AS 6520 35186 894540 GE REMOTE DIAGNOSTICS NR 1 ENGINE TREND DATA CONTINUES TO SHOW A GREATER THAN NORMAL EGT MARGIN LOSS. PRIORITY 2 NOTE E TOPS SIGNIFICANT. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081126 NM 2008 11 26 ASAA0843826 1 20081026 A 5753 6546430150 SKIN BOEING 737 7374Q8 138447Q NM FOREFLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 RT INBD FOREFLAP UPPER SURFACE DENTED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087210 1 20081217 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 402WN 29814 EEPLS LIGHT COVER BROKEN BETWEEN ROW 1 TO ROW 3. REPAIRED COVER PER MM. 2 L 7 2 4F RT A16WE 20081219 SO 2008 12 19 CHQA200800244 1 20081211 A 3240 15851 PRESSURE SWITCH EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL MLG BRAKE FALSE INDICATION A CHQA O OTHER N FALSE WARNING CR CRUISE 1 GL 11 273SK 145331 CAE311926 FLIGHT 6123, ORF TO CVG - DURING CRUISE FLIGHT THE CREW REPORTED THAT THE BRAKE ON LIGHT FOR THE EMERGENCY BRAKE ILLUMIN ATED AND STAYED ON FOR THE DURATION OF THE FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE EMER GENCY PARKING BRAKE PRESSURE SWITCH AND TAXI CHECKED THE AIRCRAFT WITH NO FURTHER DEFECTS NOTED. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081219 EA 2008 12 19 CHQA200800245 1 20081211 A 2751 855D10011 POSITION SENSOR CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS FALSE INDICATION A CHQA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 11 467CA 11166 11166 7637 GEE873361 FLIGHT 5652, IAH TO ATL - IN CRUISE FLIGHT THE FLIGHT CREW RECEIVED A FLAPS FAIL EICAS MESSAGE. THE FLIGHT CONTROL SYNO PTIC PAGE INDICATED THE FLAPS WERE OUTLINED IN YELLOW SHOWING ZERO DEGREES OF EXTENSION. THE AIRCRAFT LANDED BACK AT IA H WITHOUT INCIDENT. MAINTENANCE PULLED FECU CODES FOR THE RIGHT BRAKE POSITION SENSING UNIT AND THE FECU. THE RIGHT BR AKE POSITION SENSING UNIT WAS REPLACED AND THE FLAP SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 20081219 NM 2008 12 19 UALA2008121506880 1 20081213 A 3350 60243 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE G2B GALLEY DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 554UA 26644 G2B GALLEY EEL LIGHT DAMAGED. REPAIRED 2 EA EEL LIGHTS FOR G2B GALLEY, OPS CHECKS GOOD. BOTH HAD BROKEN PIN. 2 L 7 2 4F 4 F RT A2NM E17NE 20081219 NE 2008 12 19 UALA2008121506890 2 20081213 A 7200 UNKNOWN BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 ENGINE UNKNOWN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 217UA 30550 222178 NR 2 ENGINE HOC. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081219 EA 2008 12 19 MASA2008121300743 1 20081213 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN SMOKE A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 519LR 10260 ASH FLT 7258 IAD-LGA - CREW RETURNED TO THE FIELD DUE TO SMOKE IN CABIN. MX PERFORMED HIGH POWER ENGINE RUNS AND OPS CH ECKED GOOD. 2 L 7 2 4F RT A21EA 20081222 NM 2008 12 22 UALA2008121506894 1 20081214 A 5754 PANEL BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LE SLAT DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 663UA 27160 LEFT WING NR 4 OUTBOUND SLAT LINKAGE PANEL HANGING DOWN. REPLACED LEFT WING NR 4 OUTBOARD SLAT LINKAGE PANEL, OPERATED SLATS, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081222 NE 2008 12 22 UALA2008121506895 2 20081214 A 7412 38882677 EXCITER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 ENGINE UNRELIABLE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 223UA 30224 ENG IGNITER R1. REPLACED UPPER EXCITER AND CABLE ON NR 2 ENGINE. OPERATIONAL TEST IS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081222 NM 2008 12 22 USAA2008121592226 1 20081212 A 5755 654645170BG SPOILER BOEING 737 7374B7 138449C NM NR 3 SPOILER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 450UW 24933 MCO - PILOT REPORT - MAJOR REPAIR - NR 3 SPOILER DELAMINATED. REPLACED NR 3 SPOILER IAW B737 AMM 27-61-11. 2 L 7 2 4F RT A16WE 20081222 EU 2008 12 22 USAA2008121592229 1 20081204 A 5315 D53472193200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - C8 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 4.5 INCHES TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 + 4.5 INCHES TO FR70, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081222 NM 2008 12 22 USAA2008121692236 1 20081204 A 5311 6546525 FRAME BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - FUSELAGE FRAME CRACKED ON UPPER FLANGE AT BS 380, ABOVE S21L & S22L. REPAIRED FUSELAGE FRAME ON UPPER FLANGE AT BS 380, ABOVE S21L & S22L IAW B737 SRM 51-20-01 & US AIRWAYS TYPICAL REPAIR 53-60-07A. 2 L 7 2 4F RT A16WE 20081222 EA 2008 12 22 VNAA2008121600006 1 20081211 A 3250 16735109 RVDT CNDAIR CL600 CL6002B19 1900309 EA NLG STEERING FAILED A VNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 05 202PS 11838 7858 CREW REPORTED AN ABORTED TAKEOFF AT ABOUT 80 KNOTS AND RETURN TO GATE IN CLT FOR NOSE WHEEL STEERING PULLING RIGHT. MAI NTENANCE INSPECTED AIRCRAFT AND REPLACED THE RT RVDT. OPERATION CHECKS ACCOMPLISHED WITH NO OTHER DEFECTS. AIRCRAFT WA S RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081222 WP 2008 12 22 UPS08854182 1 20081013 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-19 AT FS 663-677 L36 HAS SRM REF 53-02-01 FIG 7 SHEET 11 IS A CAT B REPAIR. R EMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO DC8-5330-31489-A AND FVCI DWG 53-08540-23. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854213 1 20081217 A 3242 ROD DOUG DC8 DC873F 302199F WP BRAKE SYSTEM BROKEN A IPXA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 01 819UP 46019 F/O MADE UNEVENTFUL LANDING WITH NORMAL BRAKING. EXITED RUNWAY & HAD NO BRAKES AT 55 KTS. NOSE WHEEL STEERING WORKED, BUT HAD TO USE EMERGENCY AIR BRAKES. R&R NOSE STEERING CABLE GUIDE, REF MM 29-10-0. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854169 1 20081013 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-29 AT FS 160-180 L29-31R HAS SRM REF 53-02-01 FIG 7 SHEET 11 IS CAT B REPAIR. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEE T 15. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854177 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-77 FS 1530-1540 L16-18R HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTAL LED REPAIR DOUBLER IAW DC-8 SRM 53-02-00 FIG 22A. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854179 1 20081028 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-78 AT FS 1585 L24R HAS SRM 53-02-01 FIG 7 SHEET 11 IS A CAT B REPAIR. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11. 2 L 7 4 4F RT 4A25 20081222 NM 2008 12 22 SWAA087253 1 20081217 A 5330 6545800 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 257, WL 181. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 SWAA087243 1 20081218 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 SWAA087242 1 20081218 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 SWAA087239 1 20081218 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 348, STR 16R. REPAIRED STRINGER PER AAR EA. 2 L 7 2 4F RT A16WE 20081222 EA 2008 12 22 COMA2008121670006 1 20081214 A 3020 54011485 ANTI-ICE VALVE CNDAIR CL600 CL6002C10 1390015 EA LT COWLING FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 669CA 11142 10176 ON CLIMBOUT FROM CVG, RECEIVED LEFT COWL ANTI-ICE CAUTION MSG. EMERGENCY DECLARED, A/C RETURNED TO CVG LANDED SAFELY. REMOVED AND REPLACED LEFT COWL ANTI-ICE VALVE. 2 L 7 2 4F RT A21EA 20081222 EA 2008 12 22 COMA2008121750030 1 20081212 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 785CA 23029 7326 RT WING LOWER DRAIN ATTACHMENT HOLE JUST FWD OF PANEL 640 DB AT WS 85.50 AFT SCREW HOLE IS DAMAGED. REPAIRED DAMAGE PER EA10-57-02437. 2 L 7 2 4F RT A21EA 20081223 NM 2008 12 23 SWAA087268 1 20081221 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Q8 1384670 NM BS 727E S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 727E, STR 16L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087271 1 20081221 A 3350 101073 LENS BOEING 737 7373K2 13844BA NM EMERGENCY LIGHTS MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 340LV 23738 L1 DOOR EMERGNECY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087260 1 20081219 A 3350 417A56014 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 245WN 32506 L1 DOOR EMERGENCY EXIT SIGN LIGHT LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081223 EU 2008 12 23 COEA0804903 1 20081117 A 5330 S53571501200 SKIN AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A COEA K NONE O OTHER IN INSP/MAINT 1 NM 13 903FX 179 MAJOR REPAIR & LEVEL 2 CORROSION. LT LOWER BELLY SKIN INNER SURFACE IS CORRODED BELOW RECIRCULATION DUCT SUPPORT ON FRA ME 24. S/D ATR SRAS (STRUCTURAL REPAIR APPROVAL SHEET) WITH REPAIR INSTRUCTION DO/TS-4977/08-10961 ISSUED FOR DAMAGE REMOVAL & REPAIR. CORROSION REMOVED BY BLENDING. REWORKED AREA CONTOUR RESTORED WITH FILLER COMPOUND. 2 H 7 2 4T RT A53EU 20081223 NM 2008 12 23 HNAA2008122200354 1 20081217 A 2530 180140 COFFEEMAKER DHAV DHC8 DHC8102 2809003 NM GALLEY SMOKE A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 815EX 41450 41450 321 HOT ODOR COMING FROM NUMBER ONE HOT JUG AREA. PERFORMED HIDDEN DAMAGE INSPECTION ON NUMBER ONE HOT JUG SOCKET (IN ACCOR DANCE WITH SPECIAL PROCEDURE 33.1) NO DAMAGE NOTED. PULLED AND COLLARED NUMBER ONE HOT JUG CIRCUIT BREAKER. ITEM ON MEL 25-7, SEE SEQUENCE ONCE, THIS LOG PAGE. 2 H 7 2 4T RT A13NM 20081223 2008 12 23 HNAA2008122200355 2 20081217 A 7300 CONTROL UNIT DHAV DHC8 DHC8102 2809003 NM ENGINE MALFUNCTIONED A HNAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 07 931HA 132 NR 2 ELECTRONIC CONTROL UNIT FAILED IN FLIGHT. RESET NR 2 ELECTRONIC CONTROL UNIT & BETA LOCKOUT CIRCUIT BREAKERS GROUN D RUN AIRCRAFT, OPS CHECK GOOD OK FOR SERVICE. 2 H 7 2 4T RT A13NM 20081223 NM 2008 12 23 SWAA087295 1 20081221 A 3397 W145000920 WIRE BOEING 737 7373H4 1384600 NM EMERGENCY LIGHTS INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND FWD GALLEY EMERGENCY EXIT SIGN INOP. REPAIRED WIRE PER MM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087296 1 20081221 A 5311 6546525 FRAME BOEING 737 7373L9 1384470 NM BS 380 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087284 1 20081221 A 5743 115A5211 TRUNNION BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 734SA 27866 DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION BEARING LUGS CORRODED. REPAIRED LUGS PER SWA EA. 2 L 7 2 4F RT A16WE 20081223 2008 12 23 SWAA087285 4 20081219 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 917WN 36624 R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF IT'S CONTAINER, DID NOT DEPLOY. REINSTALLED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087286 1 20081221 A 5311 6545875 FRAME BOEING 737 7373H4 1384600 NM BS 348 S16L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 348, STR 16L. REMOVED AND REPLACED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 UALA2008111300841 1 20080214 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU BS 794-865 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FUSELAGE SKIN INTERNAL BEAR STRAP HAS 3 EA SMALL AREAS OF CORROSION AFT OF AFT PIT CARGO THRESHOLD BS 855-865 & AT FWD S IDE OF THRESHOLD BETWEEN BS 794-807 JUST BELOW STR 25R LAP JOINT. MAJOR REPAIR ACP'D, THE AFT AREAS WERE BLENDED THE FW D AREA REPAIRED WITH EXTERNAL FUSELAGE DOUBLER. SUSPECT MOISTURE CONTAMINATION. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 UHLA2008110700008 1 20081210 A 2780 SLAT SYSTEM EMB ERJ170 ERJ170100SE 3260406 NM NR 1 SLAT MALFUNCTIONED A UHLA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 11 647RW 17000067 ON APPROACH CREW RECEIVED SLAT FAIL WHEN SELECTING SLAT 1. CREW ABORTED APPROACH, PERFORMED CHECKLIST AND DID A NO-FLAP LANDING. MAINTENANCE CLEARED INHIBITS, RAN FLAPS MULTIPLE TIMES WITH NO FAULTS. HAS NOT REPEATED THIS DATE 12/12/2008 . 2 L 7 2 4F RT A56NM 20081223 NM 2008 12 23 UALA2008111300445 1 20080125 A 2913 424244 PUMP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 309UA 23670 RTFL DUE TO NR 1 ENGINE HYDRAULIC PUMP FAILURE. NR 1 ENGINE DRIVEN PUMP FOUND FAULTY. REPLACED NR 1 ENGINE DRIVEN PUMP . REPLACED NR 1 HYD EDP CASE DRAIN FILTER. NO METAL FOUND IN FILTER. CHANGED FILTER (P/N FLA161001144) PRECAUTIONARY, NO LEAKS NOTED ON ENG RUN. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 UALA2008111303783 1 20080708 A 2421 21E841 OIL COOLER BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RT IDG FAULTY A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 669UA 30025 THE 'R IDG VALVE' EICAS MSG DISPLAYED. REPLACED NR 2 ENG IDG AIR OIL COOLER. REPLACED IDG AIR-OIL HEAT EXCHANGER AND V ALVE (P/N 51G760-600U). REPLACED IDG OVERRIDE PRESSURE SWITCH - PRECAUTIONARY (P/N 51G160). OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081223 EA 2008 12 23 COMA2008122250039 1 20081220 A 2130 CABIN PRESSURE CNDAIR CL600 CL6002B19 1900309 EA MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 938CA 7046 ON CLIMBOUT FROM CVG, ACFT WOULD NOT PRESSURIZE. EMERGENCY DECLARED, ACFT RETURNED TO CVG LANDED SAFELY. INSPECTED BOT H OUTFLOW VALVES, PERFORMED BITE TEST OF CPAN 1 AND 2 NO DEFECTS NOTED. PRESSURIZED ACFT ON GROUND WITH NO DEFECTS NOTE D. 2 L 7 2 4F RT A21EA 20081223 NM 2008 12 23 UALA2008121806915 1 20081217 A 7921 1043V0300 BYPASS VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE OIL LEAKING A UALA O OTHER K FLUID LOSS CR CRUISE 1 WP 29 589UA 28707 717940 NR 1 ENGINE HOC. FOUND NR 1 ENG FUEL-OIL HEAT EXCHANGER LEAKING OIL- INTO FUEL. REPLACED NR 1 FOX & BYPASS VALVE ASSY. OP CHECKED GOOD ON HIGH POWER RUN, NO LEAKS NO FAULTS. 2 L 7 2 4F 4 F RT A2NM E17NE 20081223 EA 2008 12 23 COMA2008121650024 1 20081211 A 3010 14463101 DUCT CNDAIR CL600 CL6002B19 1900309 EA ZONE 500 CRACKED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 940CA 34102 7048 RECEIVED LEFT WING ANTI-ICE DUCT WARNING MSG. RETURNED TO YYZ. LANDED WITHOUT INCIDENT. FOUND LEFT WING OUTBOARD ANTI -ICE DUCT CRACKED. REPLACED DUCT WITH SERVICEABLE DUCT. NO FURTHER DEFECTS. 2 L 7 2 4F RT A21EA 20081223 EA 2008 12 23 COMA2008121650025 1 20081211 A 2421 6047T55P02 ALTERNATOR CNDAIR CL600 CL6002B19 1900309 EA ZONE 400 FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 721CA 5243 7259 ON CLIMBOUT FROM CVG, NR 2 ENGINE N2 SHOWS 0 RPM. A/C RETURNED TO CVG LANDED SAFELY. REMOVED AND REPLACED NR 2 ENGINE ALTERNATOR STATOR. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20081223 NM 2008 12 23 UALA2008111301969 1 20080406 A 2597 3510003201U2 WIRE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COFFEEMAKER FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 906UA 25006 FLIGHT ATTENDANT NOTICED HOT ODOR AT FWD GALLEY. SMELL WAS ELECTRIC. THEN SPARK OCCURRED FROM COFFEEMARKER GRILL (HOT P LATE) THEN ARC AND PUFF OF SMOKE. FOUND BURNED WIRE ON FORWARD GALLEY COFFEEMAKER. REPLACED COFFEEMAKER. AWAITING SHO P FINDINGS. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 UALA2008121906921 1 20081219 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BS 1660 DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 585UA 26709 EXTERNAL FUSELAGE SKIN DENTED AT STA 1660 AND BETWEEN STR 26L-27L AT LAV SERVICE DOOR CUTOUT. MAJOR REPAIR ACCOMPLISHED . CUT OUT DAMAGE. FABRICATED AND INSTALLED FILLER, DOUBLER AND TRIPLER. 2 L 7 2 4F 4 F RT A2NM E17NE 20081223 NM 2008 12 23 UALA2008121906922 1 20081219 A 3350 582233 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 EMERGENCY ESCAPE PATH LIGHTS IN 1ST CLASS CABIN CYCLING ON AND OFF IN FLIGHT. REPLACED EMERGENCY LIGHT BATTERY. OPS CH ECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081223 2008 12 23 UALA2008111301035 4 20080225 A 2565 PIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L2 DOOR SLIDE MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 376UA 24641 DOOR 2L SLIDE PACK MISSING SAFETY PIN. NOT LOCATED INSIDE THE POUCH WHEN THE SLIDE WAS REMOVED. *S/D* FOUND SAFETY PI N MISSING. INSTALLED NEW SAFETY PIN & FLAG. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 UALA2008111301383 1 20080313 A 5520 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT ELEVATOR CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 310UA 23671 FOUND A CRACK ON THE LT ELEV FWD OF TRIM TAB (DMG) APPROX 8 TO 10 INCHES LONG. *S/D* FOUND SCRAPE IN LT ELEVATOR. REP AIRED & REPLACED LT ELEVATOR. ELEVATOR INSTALLED. RIGGED & OPS DONE & SOLD. CLOSING UP. TEST FLT ACCOMPLISHED. 2 L 7 2 4F 4 F RT A16WE E21EU 20081219 SO 2008 12 19 C2XA08IA253 1 20081212 A 2530 500064001 COFFEEMAKER EMB 145 EMB145XR 3260214 SO GALLEY DIRTY A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 14143 17176 10929 145739 IAH - FLIGHT 2924, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL FROM BOTH COFFEEMAKERS. MX PLACED THE COFFEEMAKERS ON NEF NR GL01 D CTL NR 160100, AND THE ACFT WAS RETURNED TO SERVICE. ON 12/14/08 THE DISCREPANCY REPEATED AND MX INSPECTED THE COFFEEMAKERS, FOUND THEM TO BE DIRTY ON THE HEATERS, CLEANED THE HEATERS, OPS CHECKED WITH NO DEF ECTS, REMOVED THE NEF, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20090105 EA 2009 1 5 SWIA200820714 1 20081121 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 468CA 7649 C-CHECK, RIGHT FS 484 INTERCOSTAL ANGLE AT RBL 36 CRACKED IN UPPER RADIUS. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820715 1 20081121 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 468CA 7649 DURING C-CHECK, FLOOR SUPPORT CLIP AT FS 280 LBL9 INBOARD CRACKED. REPLACED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820724 1 20081226 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 806SK 15070 FLT 4382 - EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820726 1 20081230 A 5610 NP13932114 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 935SW 3319 3319 7725 FLT 6070 - RIGHT WINDSHIELD CRACKED. REPLACED RIGHT WINDSHIELD P/N OFF, NP139321-14, S/N OFF, 05220H8098. 2 L 7 2 4F RT A21EA 20090105 SO 2009 1 5 SWIA200820727 1 20081218 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 218SW 120287 FLT 5732 - EMERGENCY OVERHEAD LIGHT AT ROW 9BC INOP. RELAMPED. 2 L 7 2 4T RT A31SO 20090105 EA 2009 1 5 SWIA200820729 1 20081226 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 468CA 7649 FLT 2669 - PASSENGER DOOR FLOOR LEVEL EMERGENCY SIGN HAS TWO BULBS OUT. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EU 2009 1 6 FDEA200812135138 1 20081213 A 2897 WIRE AIRBUS 300 A300F4605R 3930327 EU FUEL SYSTEM DAMAGED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 21 668FE 772 DURING CLIMB THRU 18K, LOW FUEL QTY DECREASING AT APPX 500-1000 LBS/MIN, THIS WAS ON THE ECAM & OVHD PANEL. REF QRH, "P OSSIBLE FUEL LEAK" PULLED FQI CHAN SUPPLY 1 2 C/B'S. WHEN FQI RETURNED LOW RESUMED IT'S STEADY DECREASE. AFTER LANDING , ALL FUEL IND'S RETURNED TO NORMAL. ACFT RELEASED FOR SERVICE PER MEL/CDL: 28-42-01-01 RELEASED FOR SERVICE. BITE TES T OF CGCC & FUEL QTY COMPUTER NORMAL. DEPINNED SHIELDED WIRE PIN -W FOR INSPECTION & TWO SHIELD WIRES THAT WERE PIGGY-B ACKED TO IT PULLED OUT OF THE SOLDER. RETERMINATED SOCKET FOR CENTER CONDUCTOR AND REASSEMBLED SOLDER SLEEVE FOR SHIELD & TWO PIGGY-BACKED WIRES. 2 L 7 2 4F RT A35EU 20090106 NM 2009 1 6 FDEA200812165183 1 20081216 A 5320 6517510119 WEB BOEING 727 727233 138408A NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 AFT AIR STAIRS, LT LOWER TORQUE BOX INBD VERTICAL WEB IS CRACKED AT LIGHTNING HOLE BETWEEN STA 1263-1283. TRIMMED OUT D AMAGED AREA IAW SRM 51-40-2, FIG 1. FABRICATE REPAIR IAW SRM 51-40 -2 FIG 1, AND 53-10-2 FIG 6. TREATED AND PRIMED IAW S RM 51-10-2. INSTALLED REPAIR PART IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 20090106 SO 2009 1 6 C2XA08IA277 1 20081230 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13161 14500805 IAH - DURING MX INSPECTION THE EXIT ROW OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX R&R THE NR 4 INVE RTER, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20090106 EA 2009 1 6 MASA2008123000763 1 20081230 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN/LAVATORY SMOKE A MASA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 27173 7173 ASH 7187 CAE-ORD. CREW RETURNED TO THE FIELD AND DECLARED AN EMERGENCY DUE TO SMOKE IN THE LAV AND AFT CABIN. THE SMOK E DISSIPATED AFTER SECURING BOTH ACM'S 2 L 7 2 4F RT A21EA 20090106 NM 2009 1 6 K11A2009010272304 1 20080409 A 5210 FITTING BOEING 727 7272H3 138368N NM DOOR CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 723CK 20545 DOOR BACK UP FITTING CORRODED. 2 L 7 3 4F RT A3WE 20090106 EA 2009 1 6 MASA2008123000762 1 20081230 A 3350 COVER CNDAIR CL600 CL6002B19 1900309 EA CABIN MISSING A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 77331 7331 FLT 7155 ORD. FWD FA EMER LIGHT COVER MISSING. MX CALLED OUT AND REPLACED LENS COVER. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 MASA2008122900760 1 20081229 A 5730 WINGLET CNDAIR CL600 CL6002C10 1390015 EA LT WING DAMAGED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 513MJ 10111 PERMANENT REPAIR ON LT WINGLET DUE TO LIGHTNING STRIKE DAMAGE. 2 L 7 2 4F RT A21EA 20090106 NE 2009 1 6 FDEA200811114854 2 20081111 A 7321 441790 HMU DOUG MD11 MD11F 3023600 NM GE CF6 CF680 30025 NE NR 3 ENGINE FAILED A FDEA E ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 CE 21 584FE 48436 704338 ENGINE NR 3 FLAMED OUT DURING DESCENT AT APPROX HIGH 20'S. ON DEBRIEF CREW REPORTED RESTART WAS NORMAL AND ENGINE OPERA TED NORMAL REMAINDER OF FLIGHT. T/S NOW IN PROGRESS. REMOVED AND REPLACED NR 3 HMU PER MM 73-21-01-4, ALL LEAK CHECKS ON. FUEL AND OIL CHECKED GOOD. RAN NR 3 ENG PER JRH 7-1 AND OP'S NORMAL, ALL COWLING SECURED CLOSED. ACFT OK FOR SERV ICE. 2 L 7 3 4F 4 F RT A22WE E13NE 20090106 NM 2009 1 6 FDEA200811284994 1 20081128 A 5730 ARB75822 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CHAFED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 RIGHT WING LEADING EDGE SURFACE FOUND CHAFED AT BOTH SIDE OF WING ANTI-ICE TELESCOPIC DUCT CUT OUT AREA. RT WING LEADIN G EDGE CHAFED SURFACE AT BOTH SIDE OF WING ANTI-ICE TELESCOPIC DUCT CUT OUT AREA REPAIR CARRIED OUT AS PER EA NO 1-5740- 122639 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090106 EA 2009 1 6 SWIA200820737 1 20081121 A 5322 SHEAR TIE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 C-CHECK, RIGHT WINDSHIELD SIDE POST SUPPORT BOTTOM SHEAR TIE CRACKED. REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20081222 NM 2008 12 22 UALA2008121606903 1 20081215 A 3010 2780537104 ANTI-ICE VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT WING FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 547UA 25368 AFTER HIGH POWER RUN FOUND RIGHT WING ANTI ICE VALVE FAILED TO OPEN CORRECTLY. REPLACED RT WING ANTI ICE VALVE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081222 NM 2008 12 22 UALA2008121506897 1 20081212 A 3610 2790598101 SHUTOFF VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 596UA 28749 LEFT ENGINE BLEED VALVE WILL NOT CLOSE WHEN SWITCH IS MOVED TO THE OFF POSITION. DUCT PRESS RISES WHEN THROTTLES WERE A DVANCED. REMOVED AND REPLACED PRSOV. OP CHECKS AND LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081222 EU 2008 12 22 USAA2008121592233 1 20081212 A 3350 321430 BATTERY AIRBUS 320 A320232 3930326 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 642AW 584 FLT 219 - BOS-PHX - EEL - EMERGENCY LIGHT TEST FAILED OPERATIONAL CHECK. REMOVED AND REPLACED THE EMERGENCY POWER SUPPL Y UNIT BATTERY ON LEFT OVERWING. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081222 WP 2008 12 22 UPS08854153 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-115 AT STA 1607-1613 L22-23L HAS NO SRM REF. REMOVED REPAIR DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 13. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854154 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-112 AT STA 1607.5-1625.75 L14-15L HAS NO SRM REF. REMOVED REPAIR DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11. 2 L 7 4 4F RT 4A25 20081222 NM 2008 12 22 KCSA081615 1 20081214 A 5322 SHEAR TIE BOEING 747 747212B 1384886 NM ZONE 100 CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 B.S.540 FUSELAGE FRAME SHEAR TIE CRACKED AT STR-40R. 2 L 7 4 4F RT A20WE 20081222 WP 2008 12 22 UPS08854143 1 20081014 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-55 FS 1358 - 1366 L11R - L12R HAS SRM REF 53-02-01 FIG 7 IS A CAT B REPAIR. R EMOVED REPAIR DOUBLER AND FILLER. FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW UPS EO DC8-5330-31 486-A AND FVCI DWG 53-08540-20. 2 L 7 4 4F RT 4A25 20081222 NM 2008 12 22 UPS08554188 1 20081213 A 5753 113N380089H FLAP BOEING 757 75724APF 1384969 NM WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 455UP 25476 INSPECTION TYPE:N/A LT OUTBOARD AFT FLAP T/E LWR SURFACE INTERIM REPAIR. REPAIRED FLAP PER B757-5750-31551-A. 2 L 7 2 4F RT A2NM 20081222 WP 2008 12 22 UPS08854181 1 20081013 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-15 FS 355-418 L25-27L HAS SRM REF 53-02-01 FIG 7 SHEET 11 IS A CAT B REPAIR. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER AND FINGER DOUBLERS IAW DC-8 SRM 53-02-01 FIG 7 SHEET 5. 2 L 7 4 4F RT 4A25 20081222 NM 2008 12 22 UALA2008121106853 1 20081211 A 3350 767 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 567UA 26673 NR 4 RT MAIN ENTRY DOOR (EXT) EMERGENCY EXIT LIGHT INOP. RELAMPED EMERGENCY LIGHT. OPERATES NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081222 NM 2008 12 22 UALA2008121106855 1 20081211 A 2421 S281T00137 GENERATOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE APU INOPERATIVE A UALA O OTHER O OTHER CL CLIMB 1 WP 29 672UA 30027 APU GENERATOR WENT INOP. REPLACING APU GEN. 2 L 7 2 4F 4 F RT A1NM E24NE 20081222 NM 2008 12 22 HALA2008120600878 1 20081206 A 4940 211734220 ECU BOEING 767 767332 1382001 NM APU FAILED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 597HA 23277 ETOPS SIGNIFICANT SYSTEM, APU FAILED TO START AFTER LANDING. APU FAULT "EICAS" ILLUMINATED. REMOVED AND REPLACED APU E CU PER AMM 49-61-00 FIG 103. NO DEFECTS NOTED, OK FOR SVC. 2 L 7 2 4F RT A1NM 20081222 WP 2008 12 22 UPS08854211 1 20081111 A 5730 57695895 SKIN DOUG DC8 DC871F 302199D WP LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:SV LT WING CENTER L/E LWR SKIN HAS 2 FLUSH REPAIRS AT STA XFS 422. REPAIRED IAW UPS EO DC8-5720-31609-A . 2 L 7 4 4F RT 4A25 20081222 NM 2008 12 22 UPS08M54203 1 20081215 A 5320 AJC7013 WEB DOUG MD11 MD11F 3023600 NM UPPER TORQUE BOX CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 258UP 48416 INSPECTION TYPE:N/A A .5 INCH CRACK RT UPPER TORQUE BOX WEB. REPAIRED PER EO MD11-5310-31565-A AND SRM 53-40-00 FIG 24. 2 L 7 3 4F RT A22WE 20081222 NM 2008 12 22 SWAA087255 1 20081217 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 625SW 27701 DURING SCHEDULED MV1 CHECK, FOUND LT KEEL BEAM CRACKED AT BS 700, LBL 1. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081222 EA 2008 12 22 COMA2008121750031 1 20081212 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 785CA 23029 7326 LT WING LOWER DRAIN ATTACHMENT HOLE JUST AFT OF PANEL 510 AB, BETWEEN WS 0.00 AND WS 22.50, AFT SCREW HOLE IS DAMAGED. REPAIRED DAMAGE PER EA 10-57-02437. 2 L 7 2 4F RT A21EA 20081222 SO 2008 12 22 FDKA2008122000319 1 20081220 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 FRL FLT 6208 CVG-JFK. OVERHEAD EMERG LIGHT ROW 12 INOP. MX RESET SYSTEM, OPS GOOD. 2 L 7 2 4T RT T00011AT 20081223 NM 2008 12 23 HNAA2008121000348 1 20081213 A 2520 1010818M PSU DHAV DHC8 DHC8102 2809003 NM CABIN SMOKE A HNAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 07 809EX 42345 42345 302 PSU AT ROW 4 DF SMOKED. PERFORM HIDDEN DAMAGE INSPECTION, DEACTIVATED UNIT PER SP 23.3 2 H 7 2 4T RT A13NM 20081223 NM 2008 12 23 UHLA2008110700012 1 20081217 A 2752 C1548162 ACTUATOR EMB ERJ170 ERJ170100SE 3260406 NM NR 3 TE FLAP DEFECTIVE A UHLA O OTHER J WARNING INDICATION LD LANDING 1 GL 11 648RW 10428 17000068 CREW SELECTED FLAPS 1 AND RECEIVED FLAPS FAIL MESSAGE ON EICAS. CREW DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. M AINTENANCE REMOVED AND REPLACED THE RT NR 3 FLAP ACTUATOR. 2 L 7 2 4F RT A56NM 20081223 NM 2008 12 23 UALA2008111300302 1 20080117 A 5630 58935721 WINDOW BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU L4 DOOR CRACKED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 364UA 24533 FLIGHT DIVERTED TO DUE CRACKED L4 WINDOW. WAITING FOR SHOP FINDINGS. REPLACED WINDOW. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 EA 2008 12 23 MASA2008121900750 1 20081219 A 5240 DOOR CNDAIR CL600 CL6002B19 1900309 EA SERVICE OBSTRUCTED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 37342 7342 ASH FLT 1032 HNL-OGG. AIRCRAFT SERVICE DOOR WILL NOT CLOSE. MX TIGHTENED HARDWARE ON DOOR HANDLE AND OPS CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081223 EA 2008 12 23 COMA2008121670005 1 20081214 A 2133 OUTFLOW VALVE CNDAIR CL600 CL6002C10 1390015 EA CABIN PRESSURE OBSTRUCTED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 669CA 10176 ON CLIMBOUT FROM CVG, ACFT WOULD NOT PRESSURIZE. ACFT RETURNED TO CVG LANDED SAFELY. REMOVED SECTION OF LOOSE INSULATI ON FROM OUTFLOW VALVE. PRESSURIZED A/C, OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20081223 NM 2008 12 23 UHLA2008110700011 1 20081211 A 2752 ACTUATOR EMB ERJ170 ERJ170100SE 3260406 NM TE FLAPS LACK OF LUBE A UHLA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 644RW 17000061 ON APPROACH CREW SELECTED FLAPS 2 AND RECEIVED A "FLAP FAIL" EICAS MESSAGE. CREW DECLARED AN EMERGENCY AND LANDED WITHO UT INCIDENT. MAINTENANCE LUBED AND RESET ACTUATORS. OPS CHECKED SEVERAL TIMES WITHOUT A FAULT. 2 L 7 2 4F RT A56NM 20081223 EA 2008 12 23 COMA2008122250038 1 20081216 A 3010 CLAMP CNDAIR CL600 CL6002B19 1900309 EA ANTI ICE DUCT LOOSE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 940CA 7048 ON CLIMBOUT FROM CVG RECEIVED ANTI-ICE DUCT WARNING MSG. EMERGENCY DECLARED, A/C RETURNED TO CVG LANDED SAFELY. INSPEC TED ACFT, FOUND CLAMP AT LEFT I/B PICCOLO TUBE LOOSE. RETORQUED CLAMP, OPS AND LEAK CHECKS GOOD. 2 L 7 2 4F RT A21EA 20081223 NM 2008 12 23 UALA2008111300478 1 20080128 A 2612 655449932 MODULE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU FIRE WARNING MALFUNCTIONED A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 906UA 25006 CREW REPORTS ON PREFLT, GET NO BELL DURING FIRE TEST. APU HORN IN WHEEL WELL DOES COME ON. FOUND FAULTY AURAL WARNING MODULE. REPLACED AURAL WARNING MODULE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 UALA2008111301384 1 20080312 A 5610 5717623097 WINDOW BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT CRACKED A UALA O OTHER O OTHER AP APPROACH 1 WP 29 941UA 26676 CREW REPORT: L2 WINDOW CRACKED AND ARCED ON APPROACH INTO YYZ AT 2000 MSL. TURNED OFF WINDOW HEAT. *S/D* REPLACED TH E 2L WINDOW. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 CALA2008122201162 1 20081222 A 5320 693874OU2 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 227 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69348 23586 FUSELAGE FRAME, SKIN AND SURROUNDING STRUCTURE CORRODED STATION 227.8 FROM LBL-12 TO RBL-12 (BILGE). REMOVED CORROSION FROM HORIZONTAL CHORD, FOUND TO BE WITHIN LIMITS, AND FOUND INTERCOSTAL TO BE OUT OF LIMITS. CLEANED AREA AND INSTALLED NEW INTERCOSTAL PER B737 SRM 51-10-2 AND 51-4. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087287 1 20081221 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 747 S26-27R CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 16Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087290 1 20081221 A 5311 6546525 FRAME BOEING 737 7373H4 1384600 NM BS 380 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081223 EU 2008 12 23 UALA2008111302207 2 20080417 A 7200 ENGINE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 LEAKING A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 339UA 53272 24243 722218 HEAVY "WET SOCKS" ODOR DURING TAKEOFF AND CLIMB. ENGINE HAS BEEN DETERMINED AS SOURCE OF ODOR. REMOVED & REPLACED NR 1 ENGINE ON ACCOUNT OF OIL WETTING AT HPC BLADES STAGES 1 THRU 3. SECURED CONNECTOR THAT WAS REMOVED TO COMPLY WITH 4950 C. APU IS OPERATIVE FOR SVC. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 UALA2008121906923 1 20081219 A 2421 745329F IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE INOPERATIVE A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 655UA 25393 L GEN OFF EICAS & L GEN CONT OFF LIGHT ILLUMINATED. COMPLIED WITH MEL - NR 1 ENG GENERATOR DISCONNECTED. GENERATOR HAS UNDER VOLTAGE PER BPCU MSG. SWAPPED GCU'S, NO HELP. REPLACED LEFT IDG. GROUND RAN, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081223 EU 2008 12 23 UALA2008111301673 1 20080324 A 2700 3945128206 COMPUTER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ELAC FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 436UA 638 ELAC 1 FAULT DISPLAYED ON UPPER ECAM SCREEN, - F-CTL. ELAC 1 FAILURE. REPLACED ELAC 1. ACCOMPLISHED OPS TESTS, OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20081223 NM 2008 12 23 UALA2008111302236 1 20080417 A 5310 STRUCTURE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LAV SVC PANEL DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 366UA 24535 ACFT HAS DENT AFT OF FWD LAV SERVICE PNL. MAJOR REPAIR ACCOMPLISHED. VERTICAL LEADING EDGE WAS REMOVED AND SENT TO THE SHEET METAL SHOP. DOUBLERS RPR'S COMPLETED ON DENT AFT OF FWD SERVICE PANEL. 2 L 7 2 4F 4 F RT A16WE E21EU 20081224 WP 2008 12 24 AALA10521 1 20081203 A 5320 ANGLE DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 VERTICAL ANGLE CRACKED BELOW LONGERON 1 STATION 1338. REPAIRED PER AARD 53-10-00-15. 2 L 7 2 4F A6WE 20081224 WP 2008 12 24 AALA200810522 1 20081203 A 5320 SUPPORT BRACKET DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 VERTICAL FLOORBEAM SUPPORT BRACKET CRACKED STATION 927 UNDER NUMBER 5 SEAT TRACK. INSTALLED A SERVICEABLE SUPPORT BRACK ET PER SRM 51-01. 2 L 7 2 4F A6WE 20081224 WP 2008 12 24 AALA200810524 1 20081203 A 5340 MOUNT DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 FORWARD GALLEY OUTBOARD MOUNT CORRODED STATION 160. INSTALLED SERVICEABLE MOUNT. 2 L 7 2 4F A6WE 20081224 WP 2008 12 24 AALA200810525 1 20081203 A 5340 MOUNT DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 FORWARD GALLEY INBOARD MOUNT CORRODED STATION 160. INSTALLED A SERVICABLE MOUNT. 2 L 7 2 4F A6WE 20081224 NM 2008 12 24 USAA2008121792251 1 20081209 A 5311 6546532 FRAME BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - FRAME CRACKED BETWEEN BS 480, S8R & S9R. REPAIRED FRAME BETWEEN BS 480, S8R & S9R IAW TYPICAL REPAIR 53-10-20E. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121792257 1 20081123 A 5347 6546815 SEAT TRACK BOEING 737 7373G7 138447J NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON SEAT TRACK BETWEEN BS 907 TO BS 927, RBL 45.5. REPAIRED SEAT TRACK BET WEEN BS 907 TO BS 927, RBL 45.5 IAW SRM 53-00-52-2R. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121792258 1 20081123 A 5347 6546815 SEAT TRACK BOEING 737 7373G7 138447J NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON SEAT TRACK BETWEEN BS 907 TO BS 927, LBL 47. REPAIRED SEAT TRACK BETWEE N BS 907 TO BS 927, LBL 47 IAW SRM 53-00-52-2R. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121792259 1 20081124 A 5320 6547957 STRAP BOEING 737 7373G7 138447J NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - CORROSION ON STRAP BETWEEN BS 847 TO BS 867, S25R. REPAIRED STRAP BETWEEN BS 847 TO BS 867, S25R IAW DRAWING 6547957 & SRM 51-90-02. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121992275 1 20081218 A 5754 65026601197A SKIN BOEING 737 7374B7 138449C NM NR 1 SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - NR 1 SLAT SKIN CRACKED AT RIVET HOLES AT INBOARD AUXILIARY TRACK. REPAIRED NR 1 SLAT SKIN IAW SRM 57-43-01. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121992278 1 20081218 A 5320 654580731 ANGLE BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - ANGLE CRACKED AT BS 294, BETWEEN S11R & S12R FORWARD OF R2 DOOR. REPLACED ANGLE AT BS 294, BE TWEEN S11R & S12R FORWARD OF R2 DOOR IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121992281 1 20081108 A 5320 65528942 ANGLE BOEING 737 7373G7 138447J NM ZONE 100 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 SAL - C17 - MAJOR REPAIR - ANGLE ON FLOOR SUPPORT CRACKED AT BS 540, BL 0. REPLACED ANGLE ON FLOOR SUPPORT AT BS 540, B L 0 IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081224 WP 2008 12 24 AALA200810532 1 20081207 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 CORROSION ON LEFT CUSP BETWEEN STATION 1250 AND 1304. REPAIRED PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081224 WP 2008 12 24 AALA200810533 1 20081207 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 CORROSION ON LEFT TIE DOWN TRACK STATION 1041 TO 1220, AFT CARGO. INSTALLED A SERVICEABLE TIE DOWN TRACK PER SRM 53-01. 2 L 7 2 4F A6WE 20081224 NM 2008 12 24 MZZA2008122200013 1 20081220 A 5320 5321DB11727 INTERCOSTAL BOEING 737 737824 13844BZ NM BS 277-294 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 SW 27 14228 28792 CABIN FLOOR SUPPORT INTERCOSTAL CRACKED ABOUT 0.20 INCH BL 0, BODY STATION 277 TO BODY STATION 294.5. INTERCOSTAL REMOV ED, FABRICATED IAW EC/RA 5321-01524, HOLES PICKED-UP PER SRM 51-40-05 AND INSTALLED PER SRM 51-10-02 REV 34. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 MZZA2008122200016 1 20081220 A 5320 BAC14902887 FLOOR SUPPORT BOEING 737 737824 13844BZ NM BS 986 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 SW 27 14228 28792 CORROSION FOUND ON CABIN FLOORBEAM BODY STATION 986 LBL 43. REPAIR CARRIED OUT IAW EC/RA 5321-01429 REPAIR A. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121892264 1 20081218 A 3350 20121 BATTERY PACK BOEING 757 7572B7 1384964 NM ZONE 200 DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 941UW 27806 EMERGENCY LIGHT BATTERY PACK ABOVE LEFT EMERGENCY DOOR NR 3 DOES NOT CHARGE. REPLACED EMERGENCY LIGHT BATTERY PACK ABOV E LEFT EMERGENCY DOOR NR 3 IAW B757 AMM 33 33-51-07. 2 L 7 2 4F RT A2NM 20081224 NM 2008 12 24 USAA2008121892265 1 20081121 A 5320 65C320747 INTERCOSTAL BOEING 737 7373G7 138447J NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - CORROSION ON UPPER FLANGE OF INTERCOSTAL BETWEEN BS 986.5 TO BS 1006, LBL 29. REPLACED INTER COSTAL BETWEEN BS 986.5 TO BS 1006, LBL 29 IAW B737 SRM 51-40-02-0G. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121892263 1 20081217 A 3397 CONNECTOR AIRBUS A319 A319132 3930340 NM EMERGENCY LIGHT DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 829AW 1563 FLT 535 - AISLE EMERGENCY EXIT LIGHT ON ROW 10 RIGHT SIDE INOPERATIVE. RECONNECTED AISLE EMERGENCY EXIT LIGHT CONNECTOR AT ROW 10 RIGHT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081224 NM 2008 12 24 UALA2008111301695 1 20080325 A 2730 ELEVATOR SYSTEM BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE MALFUNCTIONED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 221UA 30552 PER CREW WHEN ONLY ELEVATOR MOVEMENT, HAD TOO MUCH RESISTANCE. WHEN ONLY AILERON MOVEMENT, RIGHT SIDE TOO MUCH RESISTAN CE. WITH SPOILERS DEPLOYED AILERONS OK. ELEVATORS ALWAYS HAD TOO MUCH RESISTANCE. NO UNUSUAL AILERON FORCES NOTED. H EAVY ELEV FORCES ARE PRESENT. RT HYD SYS CUTTING OUT AND RT SYS QTY DROPPING WITH NO EVIDENCE OF EXTERNAL LEAKAGE. QTY ON RTBL .94, QTY AFTER OPS CHECKS - .66. NO STATUS MSGS OR OTHER DEFECTS NOTED. ACCMP'D ELEV AND FORCE CHKS. SVC'D R HYDS. ALL CHECKS GOOD. NO HYD LOSS. EDP GOOD. COULD NOT DUPLICATE PROBLEM. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081224 NM 2008 12 24 USAA2008121992272 1 20081218 A 5320 6545834256 INTERCOSTAL BOEING 737 7374B7 138449C NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION ON INTERCOSTAL AT BS 328, RBL 12. REPLACED INTERCOSTAL AT BS 328, RBL 12 IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081224 EU 2008 12 24 USAA2008122292283 1 20081219 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320214 3930316 EU EMERGENCY LIGHT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 110UW 24468 3598 1112 FLT 1162 PIT-BOS - EEL - RIGHT OVERWING EMERGENCY POWER SUPPLY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RIGHT OVER WING EMERGENCY POWER SUPPLY PACK. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 20081224 EU 2008 12 24 USAA2008122292284 1 20081219 A 3350 32145510 POWER SUPPLY AIRBUS A321 A321211 3930370 EU EMERGENCY LIGHTS INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 192UW 27965 4322 1496 FLT 1522 DEN-CLT - EEL - DURING EMERGENCY LIGHT SYSTEM TEST, EMERGENCY POWER SUPPLY UNIT MID LEFT FAULTED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT MID LEFT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A28NM 20081224 NM 2008 12 24 USAA2008122292285 1 20081218 A 2133 2079002AC OUTFLOW VALVE AIRBUS A319 A319132 3930340 NM CABIN PRESSURE INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 806AW 29679 10135 1056 FLT 358 PIT-PHX - EMERGENCY LANDING - CREW REPORTED CABIN PRESSURIZATION INOPERATIVE DURING CLIMB. WILL NOT WORK WITH C ABIN PRESSURE CONTROLLER 1 OR 2 MANUAL SYSTEM. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PIT. MAINTENANCE REMOVED AND REPLACED THE OUTFLOW VALVE. OPERATIONAL CHECK OF AUTO AND MANUAL PRESSURE CONTROL AND MONITORING SYSTEM GO OD. 2 L 7 2 4F RT A28NM 20081224 EU 2008 12 24 USAABA08032 1 20081209 A 3233 C248311004 UPLOCK AIRBUS 330 A330323 3940030 EU MLG FAULTED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 277AY 36945 8873 0380 PHL FLT 734 PHL TO MAN. ON TAKEOFF AND LANDING GEAR RETRACTION, THE NOSE GEAR DOORS DID NOT CLOSE. THE CREW RECYCLED THE GEAR AND THE DOORS INDICATED PROPERLY CLOSED. DUE TO THE FOLLOW ON MAINTENANCE ACTION REQUIRED UPON LANDING IN MAN , AN OPERATIONAL DECISION WAS MADE TO RETURN TO PHL THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MA INTENANCE PERFORMED SEVERAL GEAR SWINGS AND COULD NOT DUPLICATE THE PROBLEM. AFTER ADDITIONAL TROUBLESHOOTING, A FAULT WAS FOUND WITH THE RIGHT MAIN GEAR UPLOCK ASSEMBLY. MAINTENANCE REPLACED THE RIGHT MAIN GEAR UPLOCK ASSEMBLY. 2 L 7 2 4F RT A46NM 20081224 2008 12 24 SWAA087273 4 20081220 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM L1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 389SW 26592 L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. INSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20090129 EA 2009 1 29 A6WA200840626 1 20081205 A 5530 VISOR CNDAIR CL600 CL6002B19 1900309 EA HORIZONTAL STAB CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 414ZW 7586 VERTICAL STAB. LT UPPER VISOR CRACKED AND BENT. CRACK .250 LONG. VERTICAL STAB LT UPPER VISOR REPLACED IAW CRJ 200 2 L 7 2 4F RT A21EA 20081222 NM 2008 12 22 UPS08554201 1 20081215 A 5321 143N545736 FLOOR PANEL BOEING 757 75724APF 1384969 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 466UP 25482 INSPECTION TYPE:N/A 3RD PANEL FROM RT SIDE DAMAGE 12 INCHES FROM AFT OF PANEL STA 440 SEC 43 8 INCH DIA AREA TOP SKIN AN D CORE. REPLACED PANEL. 2 L 7 2 4F RT A2NM 20081222 EU 2008 12 22 UPS08154193 1 20081212 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU CREW DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 160UP 0005 INSPECTION TYPE:N/A LAMP INOP IN CREW DOOR EMERGENCY EXIT LIGHT SIGN. RELAMPED, OPS CHECKED GOOD. 2 L 7 2 4F RT A35EU 20081222 WP 2008 12 22 UPS08854126 1 20081008 A 5720 STRUCTURE DOUG DC8 DC873F 302199F WP RT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-W4-25 RT WING NR 3 PYLON STUB WING HAS REPAIR DOUBLER WITH 1 SPINNING SCREW AND 1 0 OVERSIZED FASTENER HOLES WITH DIMPLE WASHERS INSTALLED O/B END AT SLOT VANE. REMOVED REPAIR DOUBLER, FABRICATED AND I NSTALLED REPLACEMENT REPAIR DOUBLER IAW DC-8 SRM 57-02-00 FIG 2A AND 57-03-03 FIG 10. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854172 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-71 AT FS 1396 L20-21L HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTALLE D REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 10. 2 L 7 4 4F RT 4A25 20081222 NM 2008 12 22 SWAA087244 1 20081218 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081222 EA 2008 12 22 COMA2008121750029 1 20081212 A 5730 601R10045 SKIN CNDAIR CL600 CL6002B19 1900309 EA LT WING DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 785CA 23029 7326 LT WING LOWER DRAIN ATTACHMENT HOLES JUST FWD OF PANEL 540AB AT WS.0.00, FWD AND AFT SCREW HOLES ARE DAMAGED. REPAIRED DAMAGE PER EA10-57-02437. 2 L 7 2 4F RT A21EA 20081223 2008 12 23 UALA2008121106844 4 20081210 A 2565 COVER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE DOOR 2L SLIDE UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 658UA 27113 L2 DOOR SLIDE COVER LACING NOT SECURED. RESECURED L2 DOOR SLIDE LACING CABLE BALL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081223 NM 2008 12 23 UALA2008121106845 1 20081210 A 2421 756589A GENERATOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE APU FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 782UA 26948 APU GENERATOR FOUND WITH ONE TERMINAL BLOCK LOOSE AND SIGNS OF OVERHEAT - FOUND DURING FAILED STARTER TROUBLESHOOTING. SUPPLEMENTAL DATA UPDATE NEEDS NEW APU GENERATOR. REPLACED APU GENERATOR. OP CKS GOOD. NO FAULTS. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081223 NM 2008 12 23 UHLA2008110700010 1 20081208 A 2752 C1548122 ACTUATOR EMB ERJ170 ERJ170100SE 3260406 NM ZONE 500 FAULTY A UHLA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 644RW 10935 17000061 DURING APPROACH CREW RECEIVED A "FLAP FAIL" EICAS MESSAGE. THE CREW CYCLED THE FLAPS AND THEY FAILED TO EXTEND ON BOTH ATTEMPTS. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEARED INHIBITS AND RELEASED BRAKE, ALL TRIP INDICATORS CHECK ED GOOD. DISCREPANCY REPEATED 12-11-2008 FLAP FAIL ON DESCENT AFTER SELECTING FLAPS 2. MAINTENANCE LUBED AND RESET ACT UATORS AND OPS CHECKED SEVERAL TIMES WITHOUT A FAULT. MAINTENANCE IS SCHEDULED TO REPLACE THE LT AND RT NR 3 FLAP ACTUA TORS. 2 L 7 2 4F RT A56NM 20081223 NM 2008 12 23 UALA2008121806916 1 20081218 A 7921 1043V0300 BYPASS VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUEL/OIL COOLER FAULTY A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 545UA 25323 726570 NR 2 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT. DUE TO INCREASE IN OIL CONSUMPTION & NO LEAKS REPORTED DURING HIGH POWER R EPLACED FCOC & BYPASS VALVE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081223 NM 2008 12 23 SWAA087262 1 20081221 A 5311 6963820 FRAME BOEING 737 7373H4 1384600 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND RT CHORD CRACKED AT BS 178, RBL 28, WL 207. REPAIRED CHORD PER ACO. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087269 1 20081221 A 3350 0L3071BPLSGPL BULB BOEING 737 7373H4 1384600 NM EMERGENCY LIGHT INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 22Y CHECK, FOUND L1 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB PER MM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087272 1 20081220 A 5340 65C27317 STRINGER CLIP BOEING 737 7373H4 1384600 NM BS 380 S8L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087274 1 20081221 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 402WN 29814 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY LIGHT COVER BROKEN AT BETWEEN ROW 1 TO ROW 3. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 SWAA087279 1 20081221 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM BS 520 S8R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 609SW 27929 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 8R. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 UALA2008111301002 1 20080225 A 2133 7110033 OUTFLOW VALVE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN PRESSURE FROZEN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 302UA 23643 FLIGHT DIVERTED WITH A PRESSURIZATION PROBLEM. OUTFLOW VALVE FREEZING UP. REPLACED OUTFLOW VALVE AND HEAT GASKET. AWAI TING SHOP FINDINGS. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NE 2008 12 23 UALA2008121706913 2 20081216 A 7510 2790583108 ANTI-ICE VALVE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE RT ENGINE FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 669UA 30025 RT ENGINE TAI PROBLEM. REPLACED COWL ANTI-ICE VALVE AND PRESSURE SWITCH. OP CHECKS NORMAL ON ENGINE RUNS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081223 2008 12 23 UALA2008121706914 4 20081215 A 2310 8220330001 TRANSCEIVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT HF SYSTEM FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 543UA 25698 RIGHT HF WILL RECEIVE BUT WILL NOT TRANSMIT. REPLACED NR 2 HF TRANSCEIVER. 2 L 7 2 4F 4 F RT A2NM E17NE 20081224 WP 2008 12 24 AALA200810527 1 20081205 A 5313 LONGERON DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 LONGERON 2L CRACKED AT STATION 160. REPAIRED LONGERON 2L FROM 148 TO 168 PER SRM 53-02-00 FIG 18. 2 L 7 2 4F A6WE 20081224 NM 2008 12 24 USAA2008121792256 1 20081212 A 5315 143N50651 FLOORBEAM BOEING 757 7572B7 1384964 NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 941UW 27806 SAL - C1 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT BS 740, WL 208, BETWEEN RBL 49 TO RBL 61. REPAIRED FLOORBEAM AT BS 740, WL 208, BETWEEN RBL 49 TO RBL 61 IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20081224 EU 2008 12 24 USAA2008121992280 1 20081204 A 5315 D53112782200 FLOORBEAM AIRBUS 320 A320232 3930326 EU ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - C8 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR20, -Y1292. REPLACED FLOORBEAM BETWEEN FR12 TO FR20, -Y1292 IAW SRM 51-74-00. 2 L 7 2 4F RT A28NM 20081224 NM 2008 12 24 WRLA2008082 1 20081006 A 5410 STRUCTURE DOUG MD11 MD11F 3023600 NM NR 3 NACELLE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 384WA 48435 CORROSION - DURING BRIDGE CHECK, EGAT MECHANIC FOUND NR 3 ENG LT CORE COWL AFT FRAME CRACK AT 9 O’CLOCK POSITION. (REFE R TO EGAT NRC U05049). REPAIRED IAW EI W2008A54B-1056 REV 00, AND EI 2008A54B-1056 REV 01. 2 L 7 3 4F RT A22WE 20081224 NM 2008 12 24 USAA2008121892267 1 20081123 A 5347 6546815 SEAT TRACK BOEING 737 7373G7 138447J NM ZONE 200 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 303AW 24010 SAL - C19 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN BS 907 TO BS 927, LBL 26. REPAIRED SEAT TRACK BETWEEN BS 907 TO BS 927, LBL 26 IAW SRM 53-00-52-2R. 2 L 7 2 4F RT A16WE 20081224 NE 2008 12 24 UALA2008111301950 2 20080404 A 7397 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FMU DIRTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 783UA 13346 13346 26950 222223 ENG FUEL VALVE L LEFT HIGH PRESSURE (HP) FUEL SHUTOFF VALVE POSITION DISAGREES WITH COMMANDED POSITION. ACP'D FMU ELECT WIRES AND CONNECTORS SECURITY, CLEANED CONNECTORS AT FUEL METERING UNIT AND ENG START CHK OK. A/C OKAY FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081224 NM 2008 12 24 USAA2008121992273 1 20081218 A 5320 6545834259 INTERCOSTAL BOEING 737 7374B7 138449C NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON INTERCOSTAL BETWEEN BS 328 TO BS 344, LBL 12. REPLACED INTERCOS TAL BETWEEN BS 328 TO BS 344, LBL 12 IAW SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAABB08175 1 20081215 A 2133 1036423 OUTFLOW VALVE BOEING 757 7572S7 1384962 NM ZONE 200 MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 902AW 63819 14 23322 PHX FLT 42 PHX TO DCA. THE AIRCRAFT WAS UNABLE TO MAINTAIN CABIN PRESSURE AT FL 370. DURING THE RETURN TO PHX, AS TH E FLIGHT DESCENDED TO FL200, THE AIRCRAFT MAINTAINED A CABIN PRESSURE ALTITUDE OF 7,000 FEET WITH THE OUTFLOW VALVE CLOS ED, AND LEFT AND RIGHT DUCT PRESSURE AT 40 PSI. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE U PPER CABIN PRESSURE RELIEF VALVE. 2 L 7 2 4F RT A2NM 20081224 NM 2008 12 24 SWAA087263 1 20081221 A 5311 6963820 FRAME BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND LT CHORD CRACKED AT BS 178, RBL 28, WL 207. REPAIRED CHORD PER ACO. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 AALA200802394A 1 20081025 A 3350 0202365001 LIGHT BOEING 777 777223 1385213 NM ZONE 200 BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 753AN 30261 LHR - EMERGENCY AISLE LIGHT BY FIRST CLASS COAT CLOSET AT LEFT NR 1 DOOR IS BROKEN. REPLACED LIGHT ASSEMBLY FOR EMERGEN CY LIGHT AT FIRST CLASS COAT CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081224 NM 2008 12 24 AALA200802388A 1 20081024 A 3350 D71702001 BATTERY PACK BOEING 777 777223 1385213 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 785AN 30005 LHR - EMERGENCY LIGHTS AT AFT COACH CLASS LEFT AND RIGHT AISLE FLOOR INOPERATIVE. REPLACED BATTERY PACK AT R4 DOOR. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081224 NM 2008 12 24 NWAA085573117 1 20081214 A 3230 VALVE AIRBUS A319 A319114 3930350 NM MLG MALFUNCTIONED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 317NB 1324 DURING CLIMB OUT OF MSP, AROUND 17,000` HAD A LOW GREEN PRESS ON ENGINE NR 1 PUMP, THEN GREEN RESERVOIR LO LEVEL WARNING . COMPLIED WITH COM PROCEDURES. LANDING GEAR GRAVITY EXTENDED, LANDING UNEVENTFULLY, WITH TOW TO GATE. REPLACED LANDI NG GEAR SAFETY VALVE 49GA. LEAK CHECKS OK. 2 L 7 2 4F RT A28NM 20081224 EA 2008 12 24 A6WA200840629 1 20081208 A 5753 VANE CNDAIR CL600 CL6002B19 1900309 EA LT WING TE FLAP GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 414ZW 7586 LT WING INBD FLAP, VANE LEADING EDGE GOUGED AT 3 PLACES. 1ST GOUGE AT FLAP STA 57.00 WIDTH .500", LENGTH 1", DEPTH .030 ". 2ND GOUGE AT FLAP STA 105 WIDTH .500", LENGTH 1.00", DEPTH .007". 3RD GOUGE AT FLAP STA 141 WIDTH .500" LENGTH 1.00 ", DEPTH .010". LT WING INBD FLAP VANE L/E AT FLAP STA 57 FOUND OUT OF LIMIT IAW REO 601R-57-52-004 REV C AND REPLACED IAW SRM 51-42-13. FLAP VANE L/EDGE AT FLAP STA 105 AND 141. PERMANENT REPAIR PERFORMED IAW REO 601R-57-52-004 REV C. 2 L 7 2 4F RT A21EA 20081224 EA 2008 12 24 A6WA200840635 1 20081202 A 5210 LEVER CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 414ZW 7586 GOUGE FOUND ON PAX DOOR PULL IN LEVER, FWD UPPER PACK DOOR PULL IN LEVER REPLACED IAW AMM 20-21-00-910-801. 2 L 7 2 4F RT A21EA 20081224 NM 2008 12 24 ASAA0874041 1 20081210 A 5320 146A75023 ANGLE BOEING 737 737790 13844CN NM BS 779-849 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION ON FLOOR TO SIDEWALL SUPPORT AROUND NUTPLATE HOLES STA 779 849 LBL 20. R&R NEW FLOOR TO SIDEWALL SUPPORT BS 7 57 BS 849 LBL 20 WL 160 IAW SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 ASAA0844045 1 20081210 A 5754 65C26601389A SKIN BOEING 737 737490 1384715 NM NR 1 SLAT CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 794AS 28889 LT WING NR 1 SLAT CRACK ON LOWER TE AT RIVET 19" FROM OB OF ACTUATOR MARKED. REPAIRED LT WING NR 1 SLAT IAW B737 400 SR M 57 43 01 FIG 201. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 ASAA0874057 1 20081216 A 5321 147A5810137 FLOOR PANEL BOEING 737 737790 13844CN NM BS 947-986 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 FLOOR PANEL AT L2 DOOR SEALED TO STRUCTURE AND DAMAGED UPON REMOVAL. REMOVED AND FABRICATED NEW FLOOR PANEL. 2 L 7 2 4F RT A16WE 20081224 SO 2008 12 24 C2XA08IA256 1 20081215 A 2120 14527547407 DUCT EMB 145 EMB145XR 3260214 SO AIR CON PACK BLOWN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 11140 145732 IAH - FLIGHT 2843, THE CREW REPORTED PAC1-2 VLV CLSD MSGS WITH THE NR 1 PACK ON MEL. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX R&R A BLOWN DUCT ON THE NR 2 PAC, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081224 NM 2008 12 24 ASAA0854037 1 20081213 A 2160 3989083 VALVE BOEING 737 737890 1384527 NM RT A/C PACK FAULTED A ASAA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 583AS 2923 35681 ON MASTER CAUTION RECALL GOT MASTER CAUTION AIR COND AND RT PACK LIGHT. IT EXTINGUISHES ON RESET GROUNDED YES. PERFORM ED PACK/ZONE TEMP CONTROL BITE TEST PER FIM TASK 21-62 TASK 801. FOUND FAULT WITH TRIM CONTROL VALVE RT. R&R RT TRIM VA LVE PER FIM TASK 21-62 TASK 828. CONFIRMED PROPER ETOPS PN W/ ROB. PERFORMED PACK/ZONE TEMP CONTROL TEST SECOND TIME. NO FAULTS NOTED. OK FOR ETOPS. NO LEAKS NOTED. 2 L 7 2 4F RT A16WE 20081224 SO 2008 12 24 C2XA08SH158 1 20081218 A 5350 C510 PANEL EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 48901 501 SHV DURING C-CHECK PANEL 191EL WAS FOUND TO HAVE CORRODED BONDING PLATES. MX R&R BONDING PLATES ON PANEL 191EL IAW EC 5 750-01315 REV "E". THE ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081224 SO 2008 12 24 C2XA08SH159 1 20081218 A 5720 C510 PLATE EMB 145 EMB145LR 3260212 SO ZONE 600 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 48901 501 SHV DURING C-CHECK RT AILERON UPPER SHROUD HAD CORRODED BONDING PLATE. MX REPAIRED RT UPPER AILERON SHROUD IAW EC 5750- 01315 (E). THE ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081229 SO 2008 12 29 C2XA08SH161 1 20081218 A 5320 NUT PLATE EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 48901 501 SHV DURING C-CHECK SERVICE DOOR LOWER NUTPLATE HOLES HAD CORROSION. MX REPAIRED SERVICE DOOR LOWER NUTPLATE HOLES BY RE MOVING CORROSION AND FINDING SERVICE DOOR LOWER NUT PLATE HOLES TO BE WITHIN LIMITS IAW EMB SRM 51-10-03 AND EC 5210-011 54. MX THEN TREATED, PRIMED AND PAINTED SERVICE DOOR LOWER NUTPLATE HOLES IAW EMB 145 CPM 51-21-06 AND EC 5210-01154. THE ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081229 SO 2008 12 29 C2XA08CL134 1 20081217 A 7500 8166243 THERMOSTAT EMB 145 EMB145LR 3260212 SO BLEED SYSTEM FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 16918 18567 145397 CLE FLIGHT NR 2293 THE CREW REPORTED A BLEED 1 OVERTEMP MSG ON CLIMB IN ICING CONDITIONS. THE ACFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND REPLACED THE NR 1 FAN AIR VALVE CONTROL THERMOSTAT. OPS CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20081229 NM 2008 12 29 ASAA0874031 1 20081211 A 5240 411A2129321 BRACKET BOEING 737 737790 13844CN NM L2 DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 L2 DOOR LOWER DUST SKIRT BRACKET ON AFT END IS CRACKED. R&R L2 DOOR LOWER SKIRT BRACKET IAW SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 ASAA0874033 1 20081214 A 5320 654A000497 SCUFF PLATE BOEING 737 737790 13844CN NM CARGO DOORWAY CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 AFT CARGO DOOR FWD CORNER THRESHOLD SCUFF PLATE CRACKED. R&R CORNER THRESHOLD SCUFF PLATE. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087323 1 20081223 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087340 1 20081223 A 5753 6546531279 FLAP BOEING 737 7373Y0 1384671 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED 24Y CHECK, FOUND LT WING O/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087328 1 20081223 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED HC2 CHECK, FOUND FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087329 1 20081222 A 3350 417A56014 SIGN BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 460WN 32464 DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM. 2 L 7 2 4F RT A16WE 20081229 2008 12 29 SWAA087332 4 20081222 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 462WN 32466 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081229 WP 2008 12 29 AALA200810512 1 20081211 A 3350 5016 BATTERY DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS WEAK A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 463AA 49593 EMERGENCY LIGHTING BATTERY PACK TESTED WEAK (AMM 33-60-98-4). INSTALLED A SERVICEABLE BATTERY PACK. 2 L 7 2 4F A6WE 20081229 WP 2008 12 29 AALA200810544 1 20081208 A 5330 DOUBLER DOUG DC9 DC982 3022082 WP ZONE 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 CORROSION ON DOUBLER AT FORWARD SERVICE DOOR STATION 180 TO 200. REMOVED AND REPLACED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081229 WP 2008 12 29 AALA200810535 1 20081205 A 5310 BEAM DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 CORROSION ON VERTICAL LEG OF AFT CARGO DOOR BEAM AT STATION 1163. INSTALLED FULL BEAM DOUBLER PER SRM 51-10-3 AND AARD 53-10-00-3. 2 L 7 2 4F A6WE 20081229 WP 2008 12 29 AALA200810545 1 20081209 A 5313 LONGERON DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 CORROSION ON LONGERON 22L STATION 1286 TO 1295. REPAIRED PER SRM 53-02-00 FIG 18. 2 L 7 2 4F A6WE 20081229 GL 2008 12 29 SWAA087303 2 20081223 A 7320 8901274 SENSOR BOEING 737 7375H4 138449D NM CFMINT CFM56 CFM563B1US GL NR 1 ENGINE FAULTY A SWAA D RETURN TO BLOCK O OTHER CL CLIMB 1 SW 29 528SW 26570 AIR TURNBACK - BETWEEN 10K & 15K FT ON CLIMB NR 1 N1 WAS 80 PERCENT OR 12 LESS THAN NR 2 N1. MOVED NR 1 THRUST LEVER TO STOP, NO DIFFERENCE, TURNED PMC NR 1 OFF NO DIFFERENCE. REMOVED AND REPLACED NR 1 ENGINE CIT SENSOR PER MM. 2 L 7 2 4F 4 F RT A16WE E2GL 20081229 WP 2008 12 29 AALA200810546 1 20081209 A 5313 LONGERON DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 STATION 1260 LONGERON 22L, SPLICE CRACKED AT AFT END. INSTALLED SERVICEABLE LONGERON SPLICE PER SRM 51-02-00. 2 L 7 2 4F A6WE 20081229 WP 2008 12 29 AALA200810547 1 20081208 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7506 49800 CORROSION ON NUMBER 5 SEAT TRACK STATION 200 TO 205. SPLICED IN NEW SEAT TRACK FROM STATION 200 TO 242 PER SRM 53-05-00 . 2 L 7 2 4F A6WE 20081229 NM 2008 12 29 ASAA0874022 1 20081211 A 5347 146A7503 CARGO TRACK BOEING 737 737790 13844CN NM BS 727E DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 HOLE IN CARGO FLOOR SUPPORT IS LOCATED IN THE RADIUS OF THE SUPPORT. REPAIRED CARGO TRACK PER SRM 53 00 53 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 UALA2008122206962 1 20081220 A 2612 8244 FIRE LOOP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE FAILED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 643UA 25093 L ENG FIRE LOOP 1 - LOWER EICAS. RANG OUT EACH LOOP FOUND LWR AFT LOOP BAD, REPLACED LOOP ASSY. OP CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081229 NM 2008 12 29 UALA2008111303845 1 20080707 A 2842 1833KTU01 PROBE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FUEL TANK FAULTY A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 798UA 26928 FUEL IMBALANCE MSG DISPLAYED. LEFT TANK FUEL QTY INDICATOR IS FAILING. SHOWED 3.5 LOW, HAS HISTORY. IDENTIFIED SEVERA L PROBES WITH POSSIBLE FAULTS. PROBES REPLACED (REPLACED NR 1, 3 & 6 LEFT CENTER TANK UNITS), CLOSING UP & LEAK CHECKIN G. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081229 NM 2008 12 29 ASAA0874028 1 20081210 A 5320 146A75021 SUPPORT BOEING 737 737790 13844CN NM BS 765-774 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION WHILE WORKING CUST CARD 5155571 FOUND CORROSION ON FLOOR TO SIDEWALL SUPPORT SPLICE BS 765 LBL 20. R&R FLOOR TO SIDEWALL SUPPORT SPLICE BS 774 BS 765. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 UALA2008111302865 1 20080518 A 5320 STRAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 305UA 23666 THE FOLLOWING CRACKS WERE AT VERTICAL STRAP STA 348 STR 16L, INTERCOSTAL CLIP STA 360 STR 11L, INTERCOSTAL CLIP STA 294. 5 STR 11L AND INTERCOSTAL WEB STA 294.5 STR 11L. MAJOR REPAIRS. REPAIRED PER UA-EVA-71568 AND UA-EVA-71569, REO'S L-01 075 AND REO L-01074 TO BE REINSPECTED WITHIN 6000 CYCLES AND EVERY 6000 CYCLES THEREAFTER. CURRENT PTC 35815. RECEIVED 8100-9. PER SB 737-53A1204. 2 L 7 2 4F 4 F RT A16WE E21EU 20081229 NM 2008 12 29 UALA2008120506767 1 20081204 A 5320 STRUCTURE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FUSELAGE DAMAGED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 783UA 26950 LIGHTNING STRIKE, FOUND 11 HITS INSIDE RT RVSM AREA. REPAIRED AS REQUIRED PER SRM 53-00-01-RPR 8. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081229 NM 2008 12 29 SWAA087304 1 20081222 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081222 WP 2008 12 22 UPS08854178 1 20081027 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-10 AT FS 190-198 L24-25L HAS SRM REF 53-02-01 FIG 7 SHEET 11 IS A CAT B REPAIR . REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11. 2 L 7 4 4F RT 4A25 20081222 NM 2008 12 22 SWAA087245 1 20081218 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 SWAA087249 1 20081217 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 444WN 29839 FWD EEPLS STRIP LIGHT COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 SWAA087252 1 20081218 A 3350 8200048801 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 481WN 29853 R2 DOOR EMERGENCY EXIT LIGHT LENS BASE BROKEN. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 SWAA087254 1 20081217 A 5330 6545800 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 502SW 24179 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 257, WL 182. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 SWAA087238 1 20081217 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 288WN 36611 FWD CABIN EEPLS LIGHT LOOSE. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 HNAA2008121900353 1 20081219 A 7697 SWITCH DHAV DHC8 DHC8102 2809003 NM POWER LEVER DIRTY A HNAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 07 980HA 376 WHEN ADVANCING POWER LEVER FOR TAKEOFF AT APPROXIMATELY 30 PERCENT TORQUE NUMBER 2 PROPELLER FEATHERED. INSPECT ENGINE CONTROL PANEL NO FLAG NOTED. CLEANED POWER LEVER SWITCHES 6126-S6 THRU S 13. COMPLY WITH WORK CARD 61-20-03Q AND 61-20 -04Q. 2 H 7 2 4T RT A13NM 20081223 NM 2008 12 23 SWAA087261 1 20081221 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM BS 484 S23R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND STRINGER CRACKED AT BS 484, STR 23R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081223 EA 2008 12 23 MASA2008121900749 1 20081219 A 3230 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA MLG UNKNOWN A MASA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 SW 07 27314 7314 ASH FLT 7270 IAD-CHO. CREW DECLARED AND EMERGENCY DUE TO THE GEAR WOULD NOT RETRACT ON MISSED APPROACH. CREW CYCLED GE AR AND IT RETRACTED. MX REMOVED AND REPLACED PRIORITY VALVE AND NLG HARNESS BRACKET. OPS AND LEAK CHECKED GOOD. 2 L 7 2 4F RT A21EA 20081223 NM 2008 12 23 UALA2008111300839 1 20080214 A 5520 CRANK ASSY BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT ELEVATOR DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 ELEVATOR BUSS ASSY (NO SERIAL NUMBER) LT SIDE OF CRANK ASSEMBLY BOLT IS DAMAGED. MAJOR REPAIR ACCOMPLISHED. REWORKED D AMAGED BOLT HOLE. INSTALLED BOLT & WASHER. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 2008 12 23 UALA2008111300446 4 20080126 A 2210 65528179 ACCESSORY UNIT BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU AUTOPILOT MALFUNCTIONED A UALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 29 338UA 24242 LANDED UNDER AMBER ALERT DUE TO A TRIM PROBLEM. EXTENSIVE TROUBLESHOOTING PERFORMED. FOUND FAULTY AUTOPILOT ACCESSORY UNIT. REPLACED THE AUTOPILOT ACCESSORY UNIT. 2 L 7 2 4F 4 F RT A16WE E21EU 20081223 NM 2008 12 23 UALA2008112606678 1 20081125 A 4990 38760483 SWITCH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CONTROLLER FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 654UA 126 25392 APU SHUTDOWN AGAIN, FAULT LIGHT ON UNSUCCESSFUL RESTART. REPLACED APU CONTROLLER. REPLACED GEN OIL FLTR DELTA P SWITCH , TWICE (24NOV AT IAD & 26NOV AT ORD). 2 L 7 2 4F 4 F RT A1NM E24NE 20081223 NE 2008 12 23 UALA2008111301456 2 20080314 A 7230 FAN BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE LT ENGINE VIBRATION A UALA O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 29 228UA 40720 8526 30556 222050 LEFT ENGINE HAS PRONOUNCED VIBRATION AT 76 PERCENT N2 ABOVE 2.0. *S/D* LUBED FAN BLADES AND TRIM BALANCED. VIBRATION IS NOW WITHIN LIMITS. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081223 NM 2008 12 23 CALA2008121901152 1 20081218 A 5315 6545812 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 328 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69348 23586 FLOORBEAM BS 328 LBL 12 UPPER TEE CAP CRACKED SL-7 69. REPAIRED CRACKED FLOORBEAM AT BS 328 LBL 12 UPPER TEE CAP PER SR M 53-10-51 FIG 201. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 CALA2008122201155 1 20081219 A 5330 2024T3 SKIN BOEING 737 7373T0 1384582 NM BS 727E S24L CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 12319 23370 DURING C SCAN INSPECTION FOUND 1 INCH LONG CRACK ON STRINGER 24L 3 INCHES AFT OF STATION 727E. REPAIRED CRACK PER SRM 5 3-00-01, PROCEDURE 5, REPAIR 31. 2 L 7 2 4F RT A16WE 20081223 NM 2008 12 23 CALA2008122201158 1 20081220 A 5311 143A820132 FRAME BOEING 737 737924ER 13848A3 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 27421 37094 DAMAGE TO RIGHT FUSELAGE, FORWARD AND AFT OF FORWARD CARGO DOOR, INCLUDING DOOR, ANTENNA, AND NLG TIRES. REPAIRED FUSEL AGE PER SRM 53-00-01, ECRA 5331-01434 AND ECRA 5230- 01808. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 USAA2008121792249 1 20081213 A 5754 65C26603101 SKIN BOEING 737 7374B7 138449C NM NR 3 SLAT DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - DISBOND AREA ON NR 3 SLAT AT UPPER INBOARD EDGE. REPAIRED NR 3 SLAT IAW B737 SRM 51-70-10. 2 L 7 2 4F RT A16WE 20081224 EA 2008 12 24 COMA2008122250040 1 20081222 A 5312 601R5311563 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA ZONE 100 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 927CA 35573 7031 FORWARD PRESSURE BULKHEAD CRACKED WHERE PARKING BRAKE CABLE PASSES THROUGH. REPAIRED IAW REO 601R-53-11-563. 2 L 7 2 4F RT A21EA 20081224 NM 2008 12 24 UALA2008121906919 1 20081219 A 2170 COALESCER BAG BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN AIR DIRTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 933UA 26659 STRONG ENGINE OIL ODOR NOTICED IN COCKPIT DURING INITIAL CLIMB AFTER TAKEOFF. WITH PACKS OFF NR 1 ENGINE RUNNING, RIGHT AFTER NR 2 ENGINE START, GOT STRONG OIL SMELL IN COCKPIT. PACKS STILL OFF. RAN PACKS AND OIL ODOR WENT AWAY. NOTE: BEFORE ENGINE RUN, RAN PACKS, NO ODOR NOTED IN AIR CON. ACCOMPLISHED HIGH POWER RUN TO CLEAN OUT OIL IN SYSTEM AND REPL ACED BOTH COALESCER BAGS. 2 L 7 2 4F 4 F RT A16WE E21EU 20081224 NM 2008 12 24 ASAA0874042 1 20081211 A 5320 143A750310 BAFFLE BOEING 737 737790 13844CN NM CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 BAFFLE CRACKED BS 500C TO 500D WL 156 RBL 20. R&R BAFFLE PER SRM 53 30 53 51 40 02 51 20 01. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 ASAA0844054 1 20081210 A 5320 69353622 INTERCOSTAL BOEING 737 7374Q8 138447Q NM BS 747-767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON INTERCOSTAL BETWEEN FRAMES BS 747 TO BS 767 RBL 24. REPLACED INTERCOSTAL. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 ASAA0844055 1 20081216 A 5315 69457571 FLOORBEAM BOEING 737 7374Q8 138447Q NM BS 795 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON AFT CARGO FLOOR BEAM. BS 795 RBL 15 RBL 19 LOWER SURFACE AT NUTPLATE HOLE. R&R SUPPORT CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087314 1 20081222 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT RT R1 DOOR LOWER HINGE CUTOUT, BS 304, WL 257. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087315 1 20081222 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 304, WL 234. REPAIRED SKIN PE R ER. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087321 1 20081222 A 5322 6546536 SHEAR TIE BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 739GB 29275 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CORRODED AT BS 540, RBL 40. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087322 1 20081222 A 5320 141A5170 WEB BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 739GB 29275 DURING SCHEDULED 10Y CHECK, FOUND FLOOR WEB CORRODED AT BS 285, BL 0, WL 208. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 UALA2008122206940 1 20081220 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 EMERGENCY EXIT LIGHT INOP AT ROW 4 LT CEILING. RELAMPED EMERGENCY LIGHT, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081229 NM 2008 12 29 AALA200802382A 1 20081010 A 5320 STRUCTURE BOEING 767 767223 1385123 NM ZONE 100 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AA 22320 AFW - RIGHT CHORD AT STATION 1809, STRINGER 12 RIGHT HAS ELONGATED FASTENER HOLE IN SPLICE FITTING. REPAIRED PER MRB 76 7 3321. 2 L 7 2 4F RT A1NM 20081229 NM 2008 12 29 UALA2008111302602 1 20080504 A 4997 WIRE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU APU BURNED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 367UA 24536 FOUND GENERATOR LEAD WIRES BURNT AND ARCING ON OIL PUMP, NEEDS REPLACEMENT. UNDER INVESTIGATION 5/19/08. REPLACED APU FEEDER CABLES. REMOVED AND REPLACED OIL PUMP ASSEMBLY. REPLACED APU GENERATOR AND OIL COOLER AND REPLACED GENERATOR FE EDER CABLE. PER MM 49-11-00 -401, OPS CK'S GOOD, NO FAULTS STARTED AND RAN APU WITH FULL ELEC LOAD AND GENERATOR OPERATE D NORMAL. SHUT DOWN AND REPEATED THE CHECK WITH SAME RESULT. OK FOR SERVICE. REOPENED ON 03MAY08 DUE TO APU GEN INOP AGAIN. 2 L 7 2 4F 4 F RT A16WE E21EU 20081229 NM 2008 12 29 UALA2008111303097 1 20080529 A 2897 DV28108 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FUEL SYSTEM DEFECTIVE A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 218UA 30222 THE LT OUTBOARD REFUEL VLV INOP. REPLACED CONNECTOR DV28108 REF WD 28-21-21 ON ACCOUNT OF INTERNALLY SHORTED WIRES 2 AN D 5. REPLACED REFUEL VALVE CONTROL UNIT. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081229 NM 2008 12 29 UALA2008111303278 1 20080606 A 2620 G718505 CONTROL PANEL BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT DAMAGED A UALA O OTHER W C INADEQUATE Q C F.O.D. NR NOT REPORTED 1 WP 29 318UA 23950 COFFEE SPILLED ON CENTER CONSOLE IN COCKPIT. FLUID GOT ONTO CARGO FIRE SUPPRESSION PANEL ONLY AND DOES NOT TEST. BOTH CARGO FIRE BOTTLES ARE BLOWN. REPLACED CONTROL PANEL, NO HELP. REPLACED BOTH CARGO PIT FIRE SUPPRESSION BOTTLES, DIVER TER VALVE, METERING VALVE, SQUIBS, AND FILTERS. OPS CHECKED NORMAL. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A16WE E21EU 20081229 NM 2008 12 29 ASAA0844095 1 20081216 A 5330 6546881142 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 780AS 25112 FUSELAGE SKIN DENT AT STA 1057 ABOVE STR 24R. REMOVED DAMAGED AREA FABBED FILLER AND DOUBLER AND INSTALLED REPAIR IAW E A 13083. 2 L 7 2 4F RT A16WE 20081229 NE 2008 12 29 ASAA0854093 2 20081221 A 7200 CFM567B27 ENGINE BOEING 737 737890 1384527 NM GE CFM56 CFM567B24 NE NR 2 OIL CONSUMPTION A ASAA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 02 557AS 9790 35176 894103 NR 2 ENG OIL USAGE AT .66 REQUIRES REMOVAL FROM ETOPS STATUS PER SEAMC BILL. ON TOP DEFERRAL. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081229 NM 2008 12 29 ASAA0874066 1 20081211 A 5320 146A75021 SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION ON FLOOR TO SIDEWALL SUPPORT STA 727B 727D + 5 LBL 20. REMOVED FABRICATED AND NEW SUPPORT AND INSTALLED . 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 ASAA0874067 1 20081211 A 5340 68434863 STRINGER CLIP BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION ON STR CLIP BS 794 STR 27 RT. R&R STRINGER CLIP. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 ASAA0854082 1 20081218 A 2163 412A160041 SENSOR BOEING 737 737890 1384527 NM CABIN DIRTY A ASAA K NONE O OTHER CR CRUISE 1 NM 02 577AS 35186 ROW 6 9 REPORTED VERY HOT SEEMED TO BE UNCONTROLLABLE FROM COCKPIT. GROUNDED YES. BITE TEST BOTH ZONE TEMP. CONTROLS. R EF. M.M. 21 61 00. NO FAULTS FOUND. BOTH CABIN TEMPERATURE SENSOR ASSY FILTERS CLOGGED WITH DUST. CLEANED FILTERS. R EF. M.M. 21 61 06 100 801. PERFORMED CABIN TEMPERATURE CONTROL AND INDICATION OPS TEST ALL INDICATIONS NORMAL. REF. M.M . 21 61 00 700 807 002. CONTROLLABLE ON ALL SWITCHES ON CABIN TEMP PANEL. (FWD CAB AFT CAB & CONT CAB). 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 UALA2008122607003 1 20081224 A 3260 WARNING SYSTEM AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE COCKPIT ACTIVATED A UALA K NONE J WARNING INDICATION CL CLIMB 1 WP 29 833UA 1401 AFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT MOVE TO UP POSITION WITH LG SHOCK ABSORBER FAULT ECAM. 2 L 7 2 4F 4 F RT A28NM E40NE 20081230 NM 2008 12 30 UALA2008122607005 1 20081224 A 7500 77328915 CONTROLLER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT ENGINE FAULTY A UALA K NONE J WARNING INDICATION CL CLIMB 1 WP 29 675UA 29243 LT ENG BLEED LGT & LT ENG HPSOV EICAS MSG DURING TAKEOFF CLIMB, WITH ENG BLEED SW ON, & ENG RUNNING. BITE OF PNEUMATIC CONTROL BOX FOUND FAULT OF: LEFT ENGINE 'HPC'. REPLACED LEFT ENGINE HIGH PRESSURE CONTROLLER. 2 L 7 2 4F 4 F RT A1NM E24NE 20081230 EU 2008 12 30 UALA2008122607006 1 20081224 A 2612 FIRE WARNING AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE MALFUNCTIONED A UALA K NONE N FALSE WARNING UK UNKNOWN 1 WP 29 456UA 1128 FIRE LOOP-B FAULT DISPLAYED ON UPPER ECAM SCREEN - ENG 2. CREW COMMENTS: ECAM APPEARS INTERMITTENTLY PERFORMED CFDS B ITE CK OF FDU. TEST OK. PERFORMED FIRE TEST. TESTS OK. NO MESSAGES. 2 L 7 2 4F 4 F RT A28NM E40NE 20081230 NM 2008 12 30 UALA2008122607013 1 20081226 A 2120 3010000801 OVEN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FWD GALLEY ODOR A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 29 644UA 25094 ELECTRICAL ODOR REPORTED IN AFT GALLEY. NO ODOR WITH GALLEY POWER OFF. CHECKED IN CEILING ABOVE AFT GALLEY ALL OK. FO UND WARMING OVEN W51 HAD MELTED PLASTIC INSIDE AND STRONG BURNED ODOR. CLEANED OVEN. RAN FOR SEVERAL HOURS. CHECKED O K. 2 L 7 2 4F 4 F RT A1NM E24NE 20090108 EU 2009 1 8 FDEA200812315323 1 20081231 A 3230 3212338 DAMPER AIRBUS 310 A310324 3930206 EU LANDING GEAR MALFUNCTIONED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 21 808FD 439 LANDING GEAR WOULD NOT RETRACT ON TAKEOFF ALTHOUGH AUTO THROTTLES WAS ENGAGED IT WAS INOP IN THE INITIAL CLIMB AUTO THR OTTLE WORKED AGAIN ONCE SLATS WERE EXTENDED. PERFORMED BITE CHECK ON PROX BOX AT HGR RAMP AND CAME UP WITH (LB) FAULT A T THIS TIME. NO OTHER FAULTS NOTED. CPN 3212338 QTY 1 DAMPER MSN 1116800. REPLACED RT PITCH TRIM CYLINDER REF AMM 32 -11-15-4. REQUIRES SERVICING AND HARDWARE TO BE SEALED. REMOVED PIVOT PIN PER MM 32-11-14 CLEANED BEARING RACES AND PIN. FOUND OUTBOARD WASHER ITEM 270 IPC 32-16-13-05A. DAMAGED AND NEEDS REPLACED. INSTALLED NEW PROX SENSORS PRECAUTIONA RY, DUE TO BEING REMOVED. REF AMM 32-11-14-4. 2 L 7 2 4F RT A35EU 20081230 2008 12 30 UALA2008122206948 4 20081220 A 2310 8220330001 TRANSCEIVER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HF COMM FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 597UA 28750 SECOND TIME RECEIVE INOP HF RIGHT RADIO FREQ 5574. RETUNE, NO HELP. REPLACED RT HF TRANSCEIVER AND F/O'S AUDIO SELECT PANEL. OPS CHECK FOR RT HF NOW TESTS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081230 NM 2008 12 30 UALA2008122206958 1 20081220 A 3350 582233 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 EMERGENCY EXIT CEILING AISLE LIGHTS ARE INOP AT RIGHT AISLE ROWS 29, 32, 35, 38 AND ON THE LOWER CEILING PANEL AFT OF RO W 38. EMERGENCY EXIT SIGN LIGHT IS ALSO INOP ON THE SAME LOWER CEILING PANEL AFT OF ROW 38. FOUND BATTERY NOT SECURED TO POWER SUPPLY ASSY. SECURED AND OPS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081230 NM 2008 12 30 UALA2008122306965 1 20081220 A 3397 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 EMERGENCY PATH LIGHT INOP AT ROW 34AB. SECURED FEEDER CONNECTOR, CHECKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081230 EU 2008 12 30 UALA2008111303292 2 20080609 A 7200 ENGINE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 MAKING METAL A UALA D RETURN TO BLOCK X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 WP 29 399UA 24674 721621 NR 1 ENGINE FLAMEOUT ON TAXI OUT. THE NR 1 ENGINE WAS REPORTED TO HAVE FLAMEOUT DURING TAXI OUT FOR A MAINTENANCE TEST FLIGHT. UPON RETURN TO THE BASE, METAL WAS FOUND IN THE TAIL PIPE AND THE ENGINE WAS REPORTED SEIZED. THE ENGINE WAS R EPLACED. NO ADDITIONAL INFORMATION HAS BEEN PROVIDED AND NONE IS EXPECTED DUE TO DOWN SIZING OF THE FLEET. 2 L 7 2 4F 4 F RT A16WE E21EU 20081230 NM 2008 12 30 UALA2008122206949 1 20081221 A 5320 PANEL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU BAY DELAMINATED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 554UA 26644 APU COMPARTMENT RT INTERIOR PANEL DELAMINATED. FABRICATED A CORE PLUG, INNER SKINS AND DOUBLER AND INSTALLED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081230 NM 2008 12 30 UALA2008122206950 1 20081221 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 554UA 26644 AFT PIT FRAME DENTED BS 1440, STR 26L. MAJOR REPAIR ACCOMPLISHED. REPAIRED FRAME DENT AT STA 1440 WITH FABRICATED J-AN GLE REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081224 2008 12 24 ASAA0854047 4 20081214 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM EE BAY INTERMITTENT A ASAA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 584AS 5350 35682 MAP FLAG VISIBLE ON F/O'S DISPLAY AND SINGLE FMC OPERATION ANNUNCIATED ON SCRATCH PAD. GROUNDED YES. PERFORMED FIM 34 61TASK801 FMC CK'S GOOD. PER SEAMC ED GROUND VERIFICATION SUCCESSFUL. 2 L 7 2 4F RT A16WE 20081224 NM 2008 12 24 ASAA0874050 1 20081113 A 5720 115A29307 SUPPORT BRACKET BOEING 737 737790 13844CN NM RT WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 647AS 33012 CRACKED SUPPORT BRACKET AT UPPER TRAILING EDGE PANEL RSS 261. R&R. 2 L 7 2 4F RT A16WE 20090106 EA 2009 1 6 SWIA200820684 1 20081215 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 705SK 10145 FLT 5822 - FIVE BULBS INOP ON EXIT SIGN IN GALLEY. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820685 1 20081216 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 705SK 10145 FLT 5822 - EXIT LIGHTING ON CEILING INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820686 1 20081212 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DISCHARGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 765SK 10231 FLT 6075 - FIVE EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED BATTERY. 2 L 7 2 4F RT A21EA 20090106 SO 2009 1 6 SWIA200820687 1 20081222 A 5280 UPLOCK HOOK EMB 120 EMB120ER 3260203 SO MLG DOOR MISRIGGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 298SW 120328 FLT 5739 - GEAR DISAGREEMENT INDICATION ILLUMINATED. RIGGED UPLOCK HOOK AND ROLLER. 2 L 7 2 4T RT A31SO 20090106 EA 2009 1 6 SWIA200820650 1 20081211 A 3297 WIRE HARNESS CNDAIR CL600 CL6002B19 1900309 EA NLG WOW SHORTED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 403SW 19908 17790 7028 FLT 2670 - 'GEAR DISAGREE' DISPLAYED AFTER TAKEOFF. REMOVED AND REPLACED NLG WOW NR 2 ELECTRICAL HARNESS, PN 750006000, SN ON 1976, SN OFF 1353. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820651 1 20081211 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 953SW 7813 FLT 6719 - RIGHT WING FORWARD EMERGENCY EXIT LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820652 1 20081215 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 432SW 7548 FLT 4729 - NR 3 OVERHEAD EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820653 1 20081208 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 866AS 7517 FLT 4852 - CABIN EMERGENCY CEILING LEVEL FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 NM 2009 1 6 YENA200812230131 1 20081219 A 2913 5116403 PUMP EMB ERJ190 ERJ190100IGW 3260408 NM HYDRAULIC SYS LEAKING A YENA O OTHER K FLUID LOSS CR CRUISE 1 EA 15 178JB 3560 190000004 FLT NR 1433, LGB-SFO, LOST HYD NR 2 EDP IN FLIGHT ALONG WITH LOSS OF ALL HYD QTY IN FLIGHT. DUE TO LOSS OF HYD NR 2 QTY, GEAR WAS MANUALLY LOWERED, GEAR REF QRH PROCEDURE. R&R NR 2 ENG DRIVEN HYDRAULIC PUMP, RAN ENGINE LEAK CHECK OK. NO L EAK NOTED. 2 L 7 2 4F RT A57NM 20090106 SO 2009 1 6 SWIA200820702 1 20081224 A 3350 FUSE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BLOWN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 226SW 120296 FLT 5479 - FORWARD CEILING EMERGENCY LIGHT INOP. REPLACED FUSE. 2 L 7 2 4T RT A31SO 20090106 EA 2009 1 6 SWIA200820704 1 20081222 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 944SW 7764 FLT 6052 - CEILING LEVEL EMERGENCY FLOODLIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820705 1 20081220 A 3411 PITOT HEAD CNDAIR CL600 CL6002B19 1900309 EA OBSTRUCTED A SWIA O OTHER C F.O.D. CR CRUISE 1 NM 07 865AS 7507 FLT 4836 - 150 FT DIFFERENCE BETWEEN PFD1 AND PFD 2 ALTITUDE INDICATIONS. CLEANED DEBRIS FROM RIGHT PITOT TUBE AND LEAK CHECKED SYSTEM. 2 L 7 2 4F RT A21EA 20090106 NM 2009 1 6 WX0A070249 1 20081106 A 3350 AD4002 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHTS INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 891GA 49401 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETUR NED TO SERVICE. 2 L 7 2 4F RT 20090106 NM 2009 1 6 WX0A070250 1 20081123 A 3350 AD4002 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 891GA 49423 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETUR NED TO SERVICE. 2 L 7 2 4F RT 20090106 EA 2009 1 6 SWIA200820658 1 20081029 A 5210 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 479CA 7675 DURING C-CHECK, PASSENGER DOOR FORWARD FILLET CRACKED IN STEP RADIUS AT HANDRAIL SUPPORT AND MID STEP RADIUS. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820659 1 20081029 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 479CA 7675 C-CHECK, LEFT AND RIGHT OBLIQUE ANGLES AT FS 625 CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820642 1 20081206 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 750SK 10207 FLT 6564 - EMERGENCY CEILING LIGHTS 4 AND 5 INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820643 1 20081208 A 3350 RELAY CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DEFECTIVE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 701SK 10133 FLT 5807 - EMERGENCY LIGHTS FLASH ON AND OFF IN ARMED (NORMAL) POSITION. REPLACED RELAY K35. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820717 1 20081121 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 468CA 7649 C-CHECK, RIGHT ENGINE THRUST FITTING CORRODED. REPLACED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820662 1 20081214 A 3220 LANDING GEAR CNDAIR CL600 CL6002C10 1390015 EA NOSE FROZEN A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 712SK 10172 FLT 5834 - NOSE GEAR FAILED TO RETRACT. USED GROUND AIR CONDITION CART TO THAW NLG. CYCLED NLG 5 TIMES, CHECKS NORMAL. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820663 1 20081214 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 471CA 7655 FLT 2631 - THIRD CABIN EMERGENCY FLOODLIGHT FROM THE FRONT OF CABIN BURNED OUT. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820664 1 20081214 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 915EV 7754 FLT 4577 - THE SECOND OVERHEAD EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820665 1 20081215 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN NO TEST A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 862AS 7476 FLT 4643 - EMERGENCY LIGHTS WOULD NOT WORK. TURNED ON EMERGENCY LIGHTS. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820692 1 20081221 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 763SK 10228 FLT 6669 - SECOND TO LAST OVERHEAD EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820694 1 20081220 A 5610 601R3303318 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 961SW 9 9 7857 FLT 5900 - FIRST OFFICERS WINDSHIELD CRACKED. REPLACED RIGHT WINDSHIELD. 2 L 7 2 4F RT A21EA 20090106 CE 2009 1 6 GUUA93853121708A 1 20081217 A 5330 SKIN BEECH 1900 1900D 1154162 CE BS 327 CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81538 UE199 DURING SCHEDULED ROUTINE MAINT, DISCOVERED SURFACE CORROSION ON FUSELAGE BELLY AT FS 327.630. REMOVED DAMAGED SKIN FABR ICATED AND INSTALLED AN EXTERNAL DOUBLER. 2 L 7 2 4T RT A24CE 20090106 NM 2009 1 6 FDEA200812215254 1 20081221 A 5330 65545732 SKIN BOEING 727 727233 138408A NM BS 650 BULGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 257FE 20939 SKIN BULGE STA 650 STR 29R. CUT OUT STR DAMAGE AND REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 53-30-1. CUTOUT DAM AGED SKIN, FABRICATED REPAIR DOUBLER , FABRICATED STR REPAIR AND SPLICE, INSTALLED REPAIR PARTS IAW SRM 51-30-2, 53-30-3 AND 53-10-3. 2 L 7 3 4F RT A3WE 20090106 2009 1 6 FDEA200812215255 4 20081221 A 2230 AUTOTHROTTLE SYS AIRBUS 300 A300B4622R 3930312 EU MALFUNCTIONED A FDEA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 21 730FD 659 ABORTED T/O DUE TO LARGE SPLIT IN THROTTLE LEVERS ( APROX 2 KNOBS WIDTH) NORMAL ACCELERATION ON NR 1. NR 2 LAGGED BEHIND WITH ENG INDICATORS ON NR 2 ALSO SLOW AND BEHIND NR 1. ABORTED T/O AT APPROX 60 KTS. RETURNED FOR TAKEOFF THIS TIME W ITH TOGA ENGAGED. THE SAME THING STARTED TO OCCURE SO WE IMMEDIATELY SELECTED AUTO THROTTLES OFF AND MANUALLY SET T/O P OWER. ACFT RELEASED FOR SERVICE IAW MEL/CDL: 22-30-01-B. 2 L 7 2 4F RT A35EU 20090106 NM 2009 1 6 USAA EMB08025 1 20081229 A 2510 POWER CABLE EMB ERJ190 ERJ190100IGW 3260408 NM COCKPIT OUT OF POSITION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 956UW 19000156 CLT - THE CAPTAIN'S SEAT FWD AND AFT LOCKING MECHANISM IS INOPERATIVE. THE SEAT MOVES FORWARD AND AFT FREELY. MAINTENAN CE - THE ELECTRIC POWER CORD WAS FOUND CAUGHT UP UNDER THE LATCH. OPERATIONAL TEST OF SEAT IS SATISFACTORY. 2 L 7 2 4F RT A57NM 20090106 EU 2009 1 6 USAA2009010290003 1 20081231 A 3350 32145410 CHARGER AIRBUS A321 A321211 3930370 EU CABIN DEFECTIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 184US 22108 415 1651 TPA - EEL - A03 CHECK - NR 8286691, AFT RIGHT EMERGENCY LIGHT BATTERY CHARGER FOUND BAD DURING TEST OF CABIN EMERGENCY L IGHTING. REMOVED, REPLACED AND OPERATIONAL CHECKED AFT RIGHT EMERGENCY LIGHT BATTERY CHARGER IAW A321 AMM 33-51-38. 2 L 7 2 4F RT A28NM 20090106 NE 2009 1 6 CLCA080802 2 20080815 A 7200 TUBE DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 3 DAMAGED A CLCA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 SO 29 614GC 59838 46931 455343 NR (3) ENG FIRE WARNING CAME ON DURING CLIMB THROUGH 22KFT. ENG WAS SHUTDOWN IAW AOM PROCEDURE E-12, ACFT FUEL WAS DUMPE D, AND ACFT RETURNED TO DEPARTURE. UPON EXTERIOR INSP OF THE ENG, DISCOVERED THE SEALS TO THE HIGH PRESSURE TURBINE (HPT ), COOLING TUBE WAS MISSING/BLOWN OUT. ENGINE BOROSCOPE REVEALED INTERNAL DAMAGE TO THE HPT AREA. METAL WAS FOUND IN THE TAIL PIPE. ENGINE WAS REMOVED AND REPLACED. ENG TSLSV: 4773:16 ENG CSLSV:1571 ENG TSI:921:19 ENG CSI: 285 2 L 7 3 4F 4 F RT A22WE E23EA 20090106 EA 2009 1 6 DATA200800011 2 20081224 A 7200 PT6A45R ENGINE STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA HARTZL HCB5M HCB5MP3 GL ZONE 400 FIRE E DATA A UNSCHED LANDING A FLAME/FIRE CL CLIMB 1 GL 13 336MV 16884 SH3018 PCE84060 EVA2279 DURING CLIMB, PILOT REPORTS FLAME FROM ENGINE EXHAUST. NO FIRE WARNING OR DAMAGED NOTED ON ACFT. AIR TURNBACK TO DEPARTU RE. ACFT LANDED WITHOUT INCIDENT. 2 H 7 2 4T 4 T A41EU E4EA 6 C P44GL 20081224 NM 2008 12 24 ASAA0874056 1 20081211 A 5320 146A75032 FLOOR SUPPORT BOEING 737 737790 13844CN NM BS 727E-747 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 RIVET HOLE IN CARGO FLOOR SUPPORT IS LOCATED IN THE RADIUS OF SUPPORT. REPAIRED CARGO TRACK PER SRM 53-00-53 REPAIR 4. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 ASAA0874032 1 20081214 A 5320 146A83418 SCUFF PLATE BOEING 737 737790 13844CN NM CARGO DOORWAY CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 AFT CARGO DOOR AFT CORNER THRESHOLD SCUFF PLATE CRACKED. R&R CORNER THRESHOLD SCUFF PLATE. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 SWAA087339 1 20081223 A 3350 101331 LENS BOEING 737 7373A4 1384585 NM CABIN MISSING A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 679AA 23291 RT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 AALA20820097 1 20081205 A 5543 178W00615 TAB BOEING 777 777223 1385213 NM RUDDER DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 761AJ 27651 31478 LT SIDE OF RUDDER TAB HAS DAMAGE 14 INCHES FROM LEADING EDGE AND 5 INCHES ABOVE BOTTOM OF TAB, DIAMETER .5 INCHES, REPA IRED IAW SRM 51-70-04-2R FIGURE 201-6 CURED PER FIG 211 SHEET 1. 2 L 7 2 4F RT T00001SE 20081229 NM 2008 12 29 AALA200820104 1 20081210 A 5330 146N3780 SKIN BOEING 757 757223 1384957 NM ZONE 100 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 609AA 45862 27447 FUSELAGE SKIN HAS DENT, REPAIRED DENT IAW SRM 53-00-01-2R. 2 L 7 2 4F RT A2NM 20081229 NM 2008 12 29 UALA2008122206924 1 20081222 A 4940 5198588 STARTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 596UA 28749 APU FAILED TO START. FAULT LGT ILLUM AND EICAS MSG. APU FAULT DISPLAYED. ADDITIONAL START ATTEMPTS UNSUCCESSFUL. CRE W COMMENTS: 4 ATTEMPTS UNSUCCESSFUL. EGT ROSE TO 790 RPM 21. AUTO SHUTDOWN. REMOVED & REPLACED APU STARTER. OP CHEC KS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081229 NM 2008 12 29 UALA2008111302942 1 20080519 A 2910 O-RING BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU HYDRAULIC SYS LEAKING A UALA O OTHER K FLUID LOSS CR CRUISE 1 WP 29 385UA 24660 THE "B" SYSTEM HYDRAULIC PRESSURE DECREASING. CREW REPORTS 'B' SYS HAS LEAK. REPLACED O-RING ON ELEC 'B' PUMP OUTPUT U NION. SERVICED 'B' SYSTEM HYDRAULICS AND LEAK CHECKED. FOUND OKAY. 2 L 7 2 4F 4 F RT A16WE E21EU 20081229 NM 2008 12 29 UALA2008122206941 1 20081220 A 3350 1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 179UA 25158 UPPER DECK EMERGENCY EXIT LIGHT INOP ACROSS FWD LAVS LOWER WALL EMERGENCY LIGHT. REPLACED LIGHT ASSY, OPS CHECKS NORMAL . 2 L 7 4 4F 4 F RT A20WE E24NE 20081229 NM 2008 12 29 AALA200802408A 1 20081026 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 192AN 32386 DFW - EMERGENCY BULL NOSE LIGHTS AT SEAT ROW 19C INOPERATIVE. REPLACED LAMP AT SEAT ROW 19C. SYSTEM GROUND CHECKED NOR MAL OPERATION. 2 L 7 2 4F RT A2NM 20081229 NM 2008 12 29 ASAA0844092 1 20081212 A 5753 65C348101 FLAP TRACK BOEING 737 737490 1384715 NM TE FLAP CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 794AS 28889 NR 1 FLAP TRACK CRACKED ON IB UPPER FLANGE. REMOVED CRACKED FLAP TRACK INSTALLED REPLACEMENT TRACK IAW B737 400 MM 27 5 1 49. 2 L 7 2 4F RT A16WE 20081229 NM 2008 12 29 AALA200802410A 1 20081026 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 192AN 32386 DFW - EMERGENCY LIGHTS AT LEFT OVERWING INOPERATIVE. REPLACED LAMPS AT LEFT OVERWING EMERGENCY LIGHT. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081230 NM 2008 12 30 UALA2008122206951 1 20081222 A 7931 PRESSURE SWITCH BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE LT ENGINE FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 798UA 38851 26928 222099 ENGINE OIL FILTER SENSOR L THE PRESSURE SWITCH FOR DETECTING IMPENDING OIL FILTER BYPASS ON THE LEFT ENGINE HAS FAILED. STATUS MSG01- ACTIVE CRUISE MODE DEPENDENT; SWITCH POSITION SIGNAL FROM OIL FILTER DIFFRNTL PRESS SW (L ENG) CHANNEL A AND B DO NOT AGREE. DB- ELECTRONIC ENGINE CONTROL (L ENG, CH A) MSG02- ACTIVE CRUISE MODE DEPENDENT; SWITCH POSITION S IGNAL FROM OIL FILTER DIFFERENTIAL PRESS SW (L ENG) CHANNEL A AND B DO NOT AGREE. MSG-7960861 ACTIVE ER MODE MSG-796086 1 ACTIVE ER MODE. ACP'D FIM 79-35 801-802. NO ACTIVE MESSAGE PRESENT. DPI DID NOT POP, INSPECTED & REPLACED MAIN OIL FILTER (P/N ACC434F65). 2 L 7 2 4F 4 F RT T0001SE E46NE 20081230 NM 2008 12 30 UALA2008122206952 1 20081222 A 2120 CD01109F2 FILTER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU FAULTY A UALA A UNSCHED LANDING W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 780UA 26944 FUMES IN CABIN & COCKPIT. RTFL. REPLACED AIR RECIRCULATION FAN FILTERS AND OZONE CONVERTERS RUN PACKS. NO FUMES NOTED. FURTHER TROUBLESHOOTING FOUND APU PNEUMATIC DUCT CONTAMINATED WITH OIL CAUSING FUMES IN CABIN/COCKPIT. NEED NEW APU. RE PLACED APU. PERFORMED DUCT & PACK BURNOUT AFTER APU REPLACEMENT. VERIFICATION FLIGHT CONFIRMED FUNCTIONALITY OF APU. ACF T OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081230 NM 2008 12 30 UALA2008122206959 1 20081220 A 3350 582240 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 EEL PATH LIGHTS INOP RT AISLE ROWS 27-34. REPLACED BATTERY AND BATTERY CHARGER ASSY AT ROW 32JK, NO HELP. HAND OVER HA ND OF WIRE FROM POWER SUPPLY TO SEAT 34 CHECKS OK. THIS POWER SUPPLY IS NOT LABELED AND MAY BE DISCREPANT. REPLACED PO WER SUPPLY M99080 AGAIN AND LIGHTS OP OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081230 NM 2008 12 30 UALA2008122306964 1 20081221 A 2822 32C171 VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE NR 2 BOOST PUMP FAULTY A UALA E ENGINE SHUTDOWN W INADEQUATE Q C NR NOT REPORTED 1 WP 29 675UA 29243 NR 2 ENG FAILS FUEL SUCTION FEED OP CK ON OUTBOUND CARD. AFTER APPROX 1.5 MINUTES AND ALL FUEL PUMPS OFF, ENG STARTS TO SURGE, N2 DROPS OFF, ENG VALVE LIGHT ON PEDESTAL (BE LOW FUEL CUTOFF) FLICKERS, ENG WAS SHUT DOWN AT THAT POINT. MADE SECOND ATTEMPT WITH EXACT SAME RESULTS. ALL IDLE RUNS PRIOR TO THIS WERE NORMAL. REPLACED NR 2 BOOST PUMP BYPASS CHECK VALVE. LEAK EXISTS IN THE FUEL FEED LINE IN THE R MAIN TANK. AFTER BYPASS VLV TO MANI-FOLD LINE O-RING REPLACED IN RT TANK, NR 2 ENG PASSED FUEL SUCT FEED JC OPS CK; RAN FOR 5 MIN, OPS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081230 NM 2008 12 30 UALA2008122306966 1 20081220 A 3350 767 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 643UA 25093 DOOR 2L EMERGENCY EXIT SLIDE LIGHT IS INOP. RELAMPED EMERGENCY LIGHT, CHECKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081230 NE 2008 12 30 UALA2008122206957 2 20081221 A 7532 32144882 BLEED VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 595UA 28748 THE L ENG BLEED WON'T CLOSE WITH SWITCH OFF. CYCLE LEFT END START SW AND APU BLEED OPENED. ALL INDICATIONS NORMAL. REPL ACED RELAY K10282 LT AIR SUPPLY ENGINE START RELAY. REPLACED AIR GROUND SYS 2 RELAY K10201. OP CHECKS GOOD ON ENGINE RUN . 2 L 7 2 4F 4 F RT A2NM E17NE 20081230 NM 2008 12 30 UALA2008122406986 1 20081223 A 5313 STRINGER AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FUSELAGE CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 807UA 798 CORROSION ON STRINGER 42L BETWEEN FR 59 AND 60. MAJOR REPAIR. REMOVED DAMAGE AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081230 NM 2008 12 30 UALA2008122406987 1 20081223 A 3213 CYLINDER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT MLG CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 549UA 25397 LT MLG OUTER CYLINDER IS CORRODED. OUTER CYLINDER CORROSION REPAIRED. REPLACED STRUT SEALS. PRESSURE CHECKED OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081230 NM 2008 12 30 AALA200802526A 1 20081028 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 680AN 29590 DFW - EMERGENCY LIGHT AT SEAT 16DEF INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 16DEF. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081126 NM 2008 11 26 ASAA0843827 1 20081026 A 5753 6546430150 SKIN BOEING 737 7374Q8 138447Q NM FOREFLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 RT INBD FOREFLAP UPPER SURFACE CHAFED ON INBD END. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUB LER IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 08FDEA04941 1 20081120 A 5330 65545812 SKIN BOEING 727 727227 1384078 NM BS 950F-970 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 495FE 21669 AFT CARGO COMP BS 950F - 970 OUTBD OF STR 28L HAS SURFACE CORROSION RUNNING AFT BEHIND INTERCOSTAL. REMOVED FLOOR SUPPO RT AND INTERCOSTAL FOR ACCESS IAW SRM 51-30-2. CUT OUT DAMAGE AREA. FABBED DOUBLER REPAIR AND 2 FILLER IAW SRM 53-30-3 FIG 3 AND 53-30-2 FIG 2. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PARTS AND INTERCOSTAL AND FLOOR SUPPORT IAW SRM 51-30-2. INSTALLED COUNTER SINK WASHER IAW SRM 51-30-8. 2 L 7 3 4F A3WE 20081126 NM 2008 11 26 ASAA0873761 1 20081106 A 5210 MS16562216 PIN BOEING 737 737790 13844CN NM L1 DOOR MIGRATED A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 618AS NG000519 30543 L1 DOOR GUST LOCK DIFFICULT TO OPERATE. FOUND PIN (205 IPC REF 52 11 21 01 FIG C) MIGRATED. REPOSITIONED PIN GUST LOCK , OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843759 1 20081108 A 5754 65C26602311A SKIN BOEING 737 737490 1384715 NM LE SLAT GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 792AS 28887 NUMBER 2 SLAT LOWER TRAILING EDGE GOUGED. REMOVED DAMAGED SECTION. INSTALLED DOUBLER FILLER AND BOND REPAIR PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 USAA920082003 1 20081023 A 5311 6546593 FRAME BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 24554 CLT Q5 MAJOR REPAIR NR 03C20853011/014 AND 4262806 FRAME CRACKED AT 500B BETWEEN S20L AND S21L. REPAIRED FRAME AT 500B BETWEEN S20L AND S21L IAW US AIRWAYS EA NR 100705. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 USAA920082013 1 20081010 A 5320 653184725 WEB BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL C21 MAJOR REPAIR NR 6139595 CORROSION ON WEB BETWEEN BS1016 TO BS1032, WL208.1, BLO TO LBL34. REPLACED WEB BETWEEN BS1016 TO BS1032, WL208.1, BLO TO LBL34 IAW BOEING DRAWING NR 65C31847 AND B737 SRM 51-40-02-0G. 2 L 7 2 4F RT A16WE 20081126 EU 2008 11 26 USAA920082015 1 20081001 A 5320 D5348004220701 FITTING AIRBUS 320 A320231 3930325 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 626AW 65 SAL C7 MAJOR REPAIR NR 6060309 CORROSION ON CORNER FITTING ON LOWER SILL AREA FR68, -Y1732. REPLACED CORNER FITTING ON LOWER SILL AREA FR68, -Y1732 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081126 EU 2008 11 26 USAA920082021 1 20081105 A 4990 GEARBOX AIRBUS A319 A319112 3930323 EU APU LEAKING A USAA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 EA 19 715UW 1051 LOGPAGE NR 8393492 FLT NR 2036 DCA-BOS OTHER CABIN ODOR IS MAKING PASSENGERS SICK. APU LEAKING OIL AT GEARBOX / COMPRES SOR FLANGE. 2 L 7 2 4F RT A28NM 20081126 NM 2008 11 26 USAA920082005 1 20081009 A 5320 6547957 WEB BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL C21 MAJOR REPAIR NR 6062846 CORROSION ON WEB BETWEEN BS787 TO BS847, RBL21 IN AFT CARGO COMPARTMENT. REPLACED WEB B ETWEEN BS787 TO BS847, RBL21 IAW B737 SRM 51-10-02-0G. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086376 1 20081119 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086346 1 20081118 A 5315 6545801512 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 348SW 24375 DURING SCHEDULED 20Y CHECK, FOUND LOWER CHORD CORRODED AT BS 227, BETWEEN BL 0 TO RBL 5. REPAIRED CHORD PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 EA 2008 11 25 SWIA200820405 1 20080808 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 443SW 7638 C-CHECK, FS 280 FORWARD FLOOR SUPPORT CRACKED AT RADIUS, REPLACED. 2 L 7 2 4F RT A21EA 20081125 EA 2008 11 25 SWIA200820406 1 20080808 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 443SW 7638 C-CHECK, FS 280 RBL9 LOWER FLOOR SUPPORT CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081125 WP 2008 11 25 AALA2008200810045 1 20081006 A 5320 STIFFENER DOUG DC9 DC983 3022083 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 BRACKET STIFFENER IS CRACKED ON FORWARD SIDE AT AFT PRESSURE BULKHEAD TOP END AT LONGERON 1 STATION 1338. INSTALLED REP AIR DOUBLER PER AARD 53-10-00-15. 2 L 7 2 4F RT A6WE 20081125 NM 2008 11 25 SWAA086340 1 20081118 A 5711 6582764 SPAR BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 341SW 24091 DURING SCHEDULED 20Y CHECK, FOUND RT WING REAR SPAR WEB CRACKED AT FWD MLG BEAM FITTING. REPAIRED WEB PER PAE ER. 2 L 7 2 4F RT A16WE 20081125 WP 2008 11 25 AALA200810060 1 20080929 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 469AA 49599 CRACK IN CEILING INTERCOSTAL AT STATION 1297 AFT CARGO. REPLACED INTERCOSTAL FROM STATION 1297- 1309 AT CENTER FLOORBOA RD. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810061 1 20080929 A 5313 LONGERON DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 469AA 49599 CORROSION IN LONGERON 29 RIGHT. REPLACED LONGERON AND SPLICED IN NEW PART PER 53-02-00. 2 L 7 2 4F A6WE 20081125 WP 2008 11 25 AALA200810099 1 20081017 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AA 49736 CUSP HAS CORROSION AT STATION 664. INSTALLED DOUBLER PER SRM 53-20-00-16. 2 L 7 2 4F A6WE 20081125 NM 2008 11 25 HALA2008111900862 1 20081119 A 3231 893602 CONTROLLER BOEING 717 717200 1383700 NM PSEU MALFUNCTIONED A HALA O OTHER O OTHER AP APPROACH 1 WP 13 476HA 55118 MOMENTARY "GEAR DOOR OPEN" ALERT ON APPROACH. CHECKED LT AND RT GEAR DOOR SENSORS PER FIM 62-60 TASK 802. BOTH CHECK' S GOOD 33OHMS. BITE CHECKED PSEU NO FAULTS. FOUND INDUCTANCE CHECKS GOOD PER AMM 32-61-00. REPLACED PSEU CONTROL BOS PER 32-61-01. OPS CHECKED PER 32-61-01 CHECKED GOOD. 2 L 7 2 4F TR A6WE 20081125 NM 2008 11 25 SWAA086359 1 20081118 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 376SW 26584 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 HALA2008111900863 1 20081119 A 3260 WARNING LIGHT BOEING 717 717200 1383700 NM MLG DOOR FALSE ACTIVATION A HALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 13 476HA 55118 OPEN - MOMENTARY GEAR DOOR OPEN ALERT. OKAY TO CONTINUE PER AMM 32-34-01. 2 L 7 2 4F TR A6WE 20081125 WP 2008 11 25 AALA200810051 1 20081005 A 5330 SKIN DOUG DC9 DC983 3022083 WP ZONE 100 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 DENT WITH SCRATCH IN FUSELAGE SKIN AT STATION 275 AT LONGERON 24L. INSTALLED DOUBLER PER SRM 53-04 FIG 12B. CLASS II R EPAIR. 2 L 7 2 4F RT A6WE 20081125 WP 2008 11 25 AALA200810068 1 20081023 A 5313 LONGERON DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 9677W 53627 LONGERON 2 RIGHT CRACKED AFT OF STATION 1418. REPLACED LONGERON AND SPLICE, INSTALLED PER AARD 53-30-00-2. 2 L 7 2 4F RT A6WE 20081125 NM 2008 11 25 SWAA086360 1 20081118 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086475 1 20081121 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 379SW 26586 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081125 2008 11 25 SWAA086499 4 20081120 A 2565 D31354 SLIDE BOEING 737 7373A4 1384585 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 677AA 23289 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086506 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 1. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086507 1 20081121 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 706, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081125 NM 2008 11 25 SWAA086525 1 20081121 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0873780 1 20081117 A 5210 14A60752 GUIDE ARM BOEING 737 737790 13844CN NM L1 DOOR WORN A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 02 618AS NG000519 30543 F/A REPORTS AT 1435Z THAT MAIN CABIN DOOR OPEN LOCK WILL NOT RELEASE. CLEANED AND LUBED GUST LOCK LEVER OPS CHECK GOOD HOWEVER IT IS REPORTED INTERMITTENT. FOUND MECHANISM BINDING DUE TO WORN BUSHINGS AND GENERAL DETERIORATION. REMOVED F WD GUIDE ARM ASSY AND INSTALLED NEW GUIDE ARM ASSY PER MM 52 11 21 000 802 AND MM 52 11 21 400 802. DOOR OPERATES SMOOT HLY AND NEW GUST LOCKS AND RELEASES NORMALLY. OKAY FOR CONTINUED SERVICE. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 USAA920082012 1 20081103 A 5311 145T252422 STRAP BOEING 767 7672B7 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 BFM MONITOR MAJOR REPAIR NR 6056556 MINOR CORROSION ON RT FAIL SAFE STRAP BS955, S17.25R. REPAIRED RT FAIL SAFE STRAP B S955, S17.25R IAW US AIRWAYS EA NR 134035. 2 L 7 2 4F RT A1NM 20081126 NM 2008 11 26 ASAA0873851 1 20081120 A 5320 141A5410U16 INTERCOSTAL BOEING 737 737790 13844CN NM CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 INTERCOSTAL CRACKED BS 328 340 LBL 40. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 08FDEA04953 1 20081121 A 5311 6516339 FRAME BOEING 727 7272S2F 1384O81 NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 C-2 PIT FLOOR FRAME SHEAR TIE AT FS 970, RBL9 TO RBL15, WL 139 HAS CORROSION ON AFT TO BOTTOM SIDE. INSTALLED NEW SHEAR TIE REF SRM 53-10-4. THIS IS CLASSIFIED AS A MAJOR REPAIR. 2 L 7 3 4F A3WE 20081126 NM 2008 11 26 QXEA2008112401194 1 20081119 A 6120 697072004 GOVERNOR BOMBDR DHC8 DHC8402 1390042 NM OVERSPEED MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 19 406QX 13752 1379 4048 RDD - NR 1 ENGINE WILL NOT COME OUT OF FEATHER. REMOVED AND REPLACED NR 1 OVERSPEED GOVERNOR IAW 61-20-26-000-801 AND 6 1-20-26-400-801. OPS AND LEAK CHECKS GOOD. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081126 NM 2008 11 26 USAA920082010 1 20081101 A 5320 100T14404 TEE FITTING BOEING 767 7672B7 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 BFM MONITOR MAJOR REPAIR NR 6056529 CORROSION ON TEE FITTING AT BS955 TO BS977, S22R TO S23R, RBL90. REPAIRED TEE FITTI NG AT BS955 TO BS977, S22R TO S23R, RBL90 IAW US AIRWAYS EA NR 134048. 2 L 7 2 4F RT A1NM 20081126 NM 2008 11 26 USAA920082008 1 20081103 A 5320 145T8754 STIFFENER BOEING 767 7672B7 1385107 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 24764 BFM MONITOR MAJOR REPAIR NR 6056532 SLOPE PANEL STIFFENER CRACKED AT AFT END BS955 TO BS977, WL180, RBL 75. REPAIRED SL OPE PANEL STIFFENER IAW US AIRWAYS EA NR 134024. 2 L 7 2 4F RT A1NM 20081126 NM 2008 11 26 USAA920082020 1 20081108 A 3350 P4010021 BATTERY AIRBUS A319 A319132 3930340 NM FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 806AW 1056 LOGPAGE 8360315 FLT NR 310 LAS-CLT FLASHLIGHT AT FORWARD FLIGHT ATTENDANT STATION NEEDS REPLACEMENT. R&R FORWARD FLIGHT ATTENDANT FLASHLIGHT BATTERY. OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081126 NM 2008 11 26 USAA920082002 1 20081103 A 5330 6545774 SKIN BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 426US 24548 CLT RON MAJOR REPAIR LOG NR 8218827 CRACK IN FUSELAGE SKIN AT BS727E, S22L. REPAIRED FUSELAGE SKIN AT BS727E, S22L IAW B737 SRM 53-00-01. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 USAA920082014 1 20081010 A 5320 65C3184725 WEB BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL C21 MAJOR REPAIR NR 6139589 CORROSION ON WEB BETWEEN BS986.5 TO BS1006, WL208.1, RBL43. REPLACED WEB BETWEEN BS986. 5 TO BS1006, WL208.1, RBL43 IAW BOEING DRAWING NR 65C31847 AMD B737 SRM 51-40-02-0G. 2 L 7 2 4F RT A16WE 20081126 NE 2008 11 26 DXTA2008111303352 2 20081112 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWC JT15 JT15D5D 52192 NE RIGHT MALFUNCTIONED E DXTA O OTHER X ENGINE FLAMEOUT LD LANDING 1 GL 07 302QS 5600402 RIGHT ENGINE QUIT ON LANDING ROLL OUT. 2 L 7 2 4F 4 F RT A22CE E45NE 20081126 NE 2008 11 26 DXTA2008111203349 2 20081111 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE PWC JT15 JT15D5D 52192 NE RIGHT SHUTDOWN E DXTA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 GL 07 302QS 5600402 RIGHT ENGINE QUIT ON LANDING APPROACH ABOUT 100 AGL THROTTLES AT IDLE. 2 L 7 2 4F 4 F RT A22CE E45NE 20081126 WP 2008 11 26 AALA20081010001 1 20081010 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 585AA 53248 2 EACH CRACKS IN LEFT HAND CUSP BETWEEN STATION 229 AND 237. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081126 WP 2008 11 26 AALA200802724 1 20081011 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7540A 49994 LGA EMERGENCY LIGHTS BETWEEN AFT LAVATORIES INOPERATIVE. RESET BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS BETWEEN A FT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 20081126 NM 2008 11 26 AALA20081028001 1 20081028 A 5320 FLOOR SUPPORT BOEING 737 737823 13844BZ NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 904AN 29506 CORROSION ON FLOOR SUPPORT BEAM STATION 970-975 AT LEFT HAND BODY LINE 16. 2 L 7 2 4F RT A16WE 20081126 2008 11 26 QXEA2008112401195 2 20081120 A 7532 311669101 BLEED VALVE DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 19 345PH 81 476 PDX - NR 2 TORQUE INCREASED EXCESSIVELY. TAKEOFF ABORTED AT LOW SPEED (BELOW 60KTS) AIRCRAFT YAWED ACCORDING TO DIFFERE NTIAL POWER. RETURNED TO THE GATE. REPLACED NR 2 ENG IBV IAW MTC 9720024, OPS TEST GOOD. ALSO REPLACED THE NR 1 ENG TSCU IAW MM 72-01-10 PAGE 420 THRU 424 PARA 7 A THRU 7.B.(2)(J). OPS TEST IAW MTC 9720019, OPS TEST GOOD, NO DEFECTS N OTED. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081126 NM 2008 11 26 AALA200802713 1 20081010 A 3350 0201720101 LIGHT BOEING 777 777223 1385213 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 794AN 30256 LHR EMERGENCY LIGHT AT SEAT 11G FORWARD INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 11G. SYSTEM G ROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT T00001SE 20081126 EU 2008 11 26 AALA200802714 1 20081010 A 3350 OL3229BPE LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 18066 509 JFK - EMERGENCY LIGHT AT SEAT 13C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 13C. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A35EU 20081126 WP 2008 11 26 AALA200810145 1 20081027 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 499AA 49737 CORROSION ON UPPER OUTBOARD FLANGE ON NR 5 SEAT TRACK AT STATION 200 TO 218. REPLACED SEAT TRACK PER SRM 53-05-00 FIGUR E 4F. 2 L 7 2 4F A6WE 20081126 NM 2008 11 26 AALA200820018 1 20081013 A 5320 141N516257 FLOOR SUPPORT BOEING 757 757223 1384957 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 672AA 52528 25337 FLOOR SUPPORT CORRODED BELOW G1B GALLEY. REPLACED FLOOR SU[PPORT IAW SRM 53-60-51 2 L 7 2 4F RT A2NM 20081126 EU 2008 11 26 USAA920082032 1 20081110 A 3397 CONNECTOR AIRBUS 320 A320231 3930325 EU EMERGENCY LIGHTS MISINSTALLED A USAA K NONE L W NO TEST INADEQUATE Q C IN INSP/MAINT 1 EA 19 629AW 076 LOG PAGE 4519069 FLT NR 541 PHX-EEL BOTH OVERWING LIGHTS LT SIDE INOPERATIVE. MX FOUND CONNECTORS FOR 5WN1 AND 6WN1 AT ROW 11 LT SWAPPED. CORRECTED AND OPS CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081126 NM 2008 11 26 USAA920082023 1 20081009 A 5315 654961612 FLOORBEAM BOEING 737 7373G7 138447J NM ZONE 100 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 158AW 23780 SAL C21 MAJOR REPAIR NR 6062842 CORROSION ON ANGLE LOCATED AT BS947.5 BETWEEN LBL21 AND RBL21. REPAIRED ANGLE LOCATED A T BS947.5 BETWEEN LBL21 AND RBL21 IAW SRM 51-10-02-0G. 2 L 7 2 4F RT A16WE 20081126 EA 2008 11 26 ASOA200801530 1 20081119 A 2560 FLASHLIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 833AS 7246 F/A FLASHLIGHT DOES NOT WORK. 2 L 7 2 4F RT A21EA 20081126 EA 2008 11 26 SWIA200820434 1 20081113 A 7120 BUSHING CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910EV 7727 RIGHT ENGINE FORWARD MOUNT YOKE UPPER LINK BUSHINGS CORRODED, AD INSP, REPLACED. 2 L 7 2 4F RT A21EA 20081126 EA 2008 11 26 SWIA200820436 1 20081112 A 5340 STRINGER CLIP CNDAIR CL600 CL6002B19 1900309 EA BS 624 S14R CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910EV 1390008 STRINGER CLIP AT FRAME 624 TO STRINGER 14 RIGHT SIDE CRACKED. AD INSP, REPLACED. 2 L 7 2 4F RT A21EA 20081126 EA 2008 11 26 SWIA200820437 1 20081111 A 5343 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 910EV 7727 ENGINE SUPPORT BEAM CRACKED. AD INSP, REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081126 NM 2008 11 26 ASAA0893871 1 20081121 A 5320 147A571246 WEB BOEING 737 737990 NM BS 1016 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 320AS 33680 CORROSION SHEAR WEB BS 1016 RBL 28 WL 208.1. REPAIRED PER EA 900 53EA 00246, BLENDED AND TREATED. 2 L 7 4 4F RT A16WE 20081126 NM 2008 11 26 DHLA2008745693 1 20081116 A 5740 ATTACH FITTING BOEING 727 727224 1384076 NM ZONE 500 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 20665 NR 1 T/E FLAP TRACK FWD ATTACH FITTING OTBD LUG CORRODED. ACCOMPLISHED REPAIR TO LUG BORE IAW COOPESA EO COO-2-57-335-0 8 DATED 10/04/08 AND BOEING MSG 1-1000885726-2 DATED 10/02/08. REF FAA FORM 8100-9 DATED 11/5/08 AND ASTAR EVA B257-001 44 FOR REPAIR APPROVAL. DOCUMENTED ON COOPESA N/R 5-502. 2 L 7 3 4F A3WE 20081126 EU 2008 11 26 AALA200802725 1 20081011 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 41063 506 MIA - EMERGENCY LIGHT AT LEFT SEAT ROWS 29C TO 37C INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT LEFT SEAT ROWS 29C TO 37C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081126 NM 2008 11 26 AALA200802726 1 20081011 A 3350 BATTERY PACK BOEING 737 737823 13844BZ NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 910AN 29512 MIA - EMERGENCY LIGHTS AT AFT LEFT CABIN INOPERATIVE. RESET EMERGENCY LIGHT BATTERY PACK FOR AFT LEFT CABIN. SYSTEM GR OUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20081126 2008 11 26 ASAA0853848 4 20081120 A 3460 1762000101 FMC BOEING 737 737890 1384527 NM EE BAY FAILED A ASAA O OTHER O OTHER NR NOT REPORTED 1 NM 02 557AS 9476 35176 LEFT FMC FAILURE BOTH ON RIGHT OPS GOOD. VERIFIED LEFT FMC INOP. TRIED REBOOT NO HELP. REMOVED AND REPLACED LEFT FMC COMPUTER REF MM 34 61 02. OPS NORMAL SAME. VERIFIED IPC PART NUMBER. VERIFIED GOOD GROUND OPERATIONAL CHECK. 2 L 7 2 4F RT A16WE 20081126 EA 2008 11 26 SWIA200820439 1 20080823 A 3200 BRACKET CNDAIR CL600 CL6002C10 1390015 EA LT MLG CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 715SK 10179 C-CHECK, LEFT MLG RETRACT ACTUATOR BRACKET ASSEMBLY CORRODED. REPLACED. 2 L 7 2 4F RT A21EA 20081126 WP 2008 11 26 AALA200810058001 1 20081009 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 RIGHT TIE DOWN CORRODED FROM STATION 1211-1287 ABOVE LONGERON 27 RIGHT. INSTALLED NEW RIGHT HAND TIE DOWN TRACK PER AAR D 51-00-00-012. 2 L 7 2 4F RT A6WE 20081126 WP 2008 11 26 AALA200810058 1 20081008 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 569AA 49351 CORROSION ON INTERCOSTAL UNDER RIGHT HAND TIE- DOWN TRACK AFT CARGO BAY STATION 1309-1322. REPLACED INTERCOSTAL WITH SE RVICEABLE PART, PER SRM 51-30-5. 2 L 7 2 4F RT A6WE 20081208 NM 2008 12 8 UALA2008120406753 1 20081204 A 3510 B198201 VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CREW O2 FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 799UA 26926 CREW O2 LEAK. RTFL. CREW O2 BOTTLE READING 1800 PSI. REPLACED 02 BLEED VALVE, PRESSURE TRANSDUCER AND RELAY K35005 BL EED VALVE CONTROL. RAN ENGINE TO VERIFY NO DROP IN O2 PRESSURE ON EICAS. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081126 EA 2008 11 26 ASOA200801533 1 20081118 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 914EV 7752 PAX DOOR AND SERVICE DOOR EMERGENCY EXIT LIGHTS INOP. 2 L 7 2 4F RT A21EA 20081126 EA 2008 11 26 ASOA200801536 1 20081119 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 445-462 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 THE RT PRESSURE FLOOR SILL IS CORRODED AT FS 445-462 THE SILL PNL AT FS 452 RBL 44 IS BEYOND REO LIMITS AT .039 IAW REO 601R-53-41-666. THE FLOOR ANGLE AT FS 461 RBL 44 IS BEYOND LIMITS AT .063 REMAINING THICKNESS. DAMAGED AREAS ARE CLOSE R THAN 5 INCHES APART AND 1 AREA AT FS 459 IS GREATER THAN 2 INCHES WIDE. 2 L 7 2 4F RT A21EA 20081126 EA 2008 11 26 ASOA200801538 1 20081119 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA BS 499 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 823AS 7196 THE PRESSURE FLOOR SILL IS CORRODED AT LT FS 499, LBL 43-45. BEYOND BLENDABLE LIMITS OF BOMBARDIER REO 601R-53-41-666 S HEETS 5 AND 6. REMAINING THICKNESS IS .060 AND .063. 2 L 7 2 4F RT A21EA 20081126 NM 2008 11 26 ASAA0843774 1 20081024 A 5755 654645170 SKIN BOEING 737 7374Q8 138447Q NM NR 2 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NUMBER 2 SPOILER LOWER SURFACE IS DENTED. INSTALLED REPAIR DOUBLER PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 08FDEA04947 1 20081120 A 5320 44221227 PANEL BOEING 727 7272D4 138407U NM ZONE 100 PUNCTURED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FWD CARGO COMPARTMENT, PFM BOX, PUNCTURE JUST BELOW PFM DOOR REPAIRED PUNCTURE IN PFM BOX REF SRM 51-40-20 PAR'S 7, 14, 15, 19, 20, AND FIG'S 8, 211, SRM 51-20-4 AND AMM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081126 NM 2008 11 26 ASAA0843784 1 20081024 A 5753 6546435278 SKIN BOEING 737 7374Q8 138447Q NM TE FLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 RIGHT OUTBOARD AFT FLAP LOWER SURFACE DENTED. REMOVED DAMAGED SECTION AND INSTALLED REPAIR DOUBLER PER SRM 51 70 10. 2 L 7 2 4F RT A16WE 20081126 NE 2008 11 26 ASAA0853876 2 20081121 A 7297 3250453010 WIRE HARNESS BOEING 737 737890 1384527 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 587AS 35684 875857 DURING OPERATIONAL CK OF HYDRAULIC PUMP ON NR 2 ENGINE FOUND THAT HYD PRESS WAS ZERO WITH PUMP SWITCH ON FOUND ENG HYD P UMP CONNECTOR DP1204 WORN. REPLACED MW0312 HARNESS REF IPC 71 51 03 01 AND AMM 71 51 03. OPS NML REF AMM 71 00 00 AND 73 21 00. ENG HYD PUMP TEST NML REF AMM 29 11 11 PRESSURE INDICATION NML WITH SWITCH ON. GROUND VERIFICATION OF ETOPS SIGNIFICANT SYSTEM SUCCESSFUL. 2 L 7 2 4F 4 F RT A16WE E2GL 20081126 NM 2008 11 26 ASAA0893835 1 20081121 A 3610 1074847 REGULATOR BOEING 737 737990 NM NR 1 ENGINE MALFUNCTIONED A ASAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 02 302AS 52200 30017 LT BLEED TRIP 31000 CLIMB-OUT OF ANC RESET TRIPPED AGAIN. REPLACED HIGH STAGE REGULATOR. 2 L 7 4 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843824 1 20081028 A 5320 65479573 WEB BOEING 737 7374Q8 138447Q NM BS 800-847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 AFT CARGO PIT DOOR SILL WEB CORRODED AROUND NUT PLATES ON LOWER SIDE STA 800 TO 847 RBL 20 TO RBL 28. REMOVED DAMAGED S ILL WEB LOCATED DRILLED INSTALLED REPLACEMENT SILL WEB IAW SRM 51-40-02 PG 3 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 ASAA0843834 1 20081025 A 5755 654645262A SKIN BOEING 737 7374Q8 138447Q NM NR 5 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 760AS 25098 NR 5 SPOILER LOWER SURFACE DENTED. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4. 2 L 7 2 4F RT A16WE 20090106 CE 2009 1 6 DBCA20081219678EQ 1 20081210 A 3210 MS35206230 SCREW CESSNA CESSNA 650 650 2076802 CE BRACKET SHEARED E DBCA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 13 678EQ 6507008 ACFT DEPARTED, ON CLIMBOUT THE LANDING GEAR WOULD NOT RETRACT. ACFT RETURNED TO DEPARTURE. LANDING WAS UNEVENTFUL. MX INSPECTED LANDING GEAR AND FOUND NLG SQUAT SWITCH BRACKET DETACHED FROM TORQUE KNEE. BRACKET ATTACH SCREWS HAD FAILED. SUSPECT ICE PREVENTED NORMAL ACTUATOR ARM MOVEMENT WHICH RESULTED IN FASTENER FAILURE. REINSTALLED SQUAT SWITCH BRACK ET AND COMPLETED RETRACT/EXTENSION TESTS. ALL OPS NORMAL. 2 L 7 2 4F A9NM 20090106 NM 2009 1 6 AALA200810553 1 20081207 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM ZONE 100 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 GOUGES ON BOTTOM SIDE OF CABIN FLOORBEAMS AT STA 655. REPAIRED IAW AARD 53-20-00-21. 2 L 7 2 4F RT A16WE 20090106 NM 2009 1 6 FDEA200812245281 1 20081224 A 5322 65584241 SHEAR TIE BOEING 727 727233 138408A NM BS 344-346 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 MISDRILLED STRINGER SHEAR TIE AT 9G BULKHEAD AND STR 12R REMOVED STR SHEAR TIE ON 9G BULKHEAD, STR12R IAW SRM 51-30-2. FABRICATED PART OF STRINGER TIE FROM 2024T3, 0.032 AND FRAME REPAIR PART FROM 7075O AND HEAT TREATED TO 7075T6 IAW SRM 51-20-1, 51-10-3 AND 53-10-4 FIG 2, 53-10-2 FIG3. TREATED AND PRIMED REAPIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR P ARTS IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 20090106 NM 2009 1 6 2009F00004 1 20081231 A 2913 123412 COVER SMITHSIND BOEING 737 737 UTILSYS NM CRACKED B IU6R K NONE O OTHER IN INSP/MAINT 1 NM 01 7711 COVER FOUND CRACKED DURING SHOP MX, THIS IS A COMMON OCCURANCE. 2 L 7 2 4F RT A16WE 20090106 WP 2009 1 6 I5HA0824013 1 20081218 A 5730 2401410009812 WING CVAC 240 240* 2422601 WP PWA R2800 R2800* 52026 NE HAMSTD 43E 43E60 NE LEFT DENTED A I5HA K NONE O OTHER LD LANDING 1 GL 25 150PA 278 DURING THE LANDING FLARE, A BIRD STRUCK THE OTBD L/E OF THE LT WING. THE CREW LANDED THE ACFT WITHOUT FURTHER INCIDENT. THE LEADING EDGE WAS REMOVED AND REPLACED AND THE ACFT RETURNED TO SERVICE. 2 L 7 2 4R 4 R A793 5E8 6 C P871 20090106 SO 2009 1 6 C2XA09IA001 1 20081229 A 2611 FAU751A4 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY MALFUNCTIONED A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 27 13538 145527 THE CREW REPORTED A LAV SMOKE WARNING ION EICAS AFTER TAKEOFF. THE CREW PERFORMED QRH WITH NO SMOKE NOTED. THE ACFT LAND ED WITHOUT INCIDENT WHERE MX REMOVED AND REPLACED THE LAV SMOKE DETECTOR PANEL, OPERATIONALLY TESTED WITH NO DEFECTS, AN D THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20090107 EU 2009 1 7 FDEA200812245291 1 20081224 A 5322 A5377341420151 SHEAR TIE AIRBUS 310 A310 EU BS 2029 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 FWD PIT BILGE FRAME NR 37 BETWEEN STRINGER 51L AND STRINGER 52L SHEAR TIE HAS CORROSION ON THE AFT SURFACE. REMOVED SHEA R TIE FROM FRAME 37 IAW SRM 51-40-21. REMOVED CORROSION IAW SRM 51-73-10. ORIGINAL MATERIAL 0.055 IAW SRM 53-14-13. REMAINING MATERIAL 0.042 IAW DWG 6-17-09. FOUND TO BE OUT OF LIMITS IAW SRM 53-73-10. LOCATED AND DRILLED NEW SHEA R TIE IAW SRM 51-40-40. ALODINED IAW SRM 51-21-00. PRIMED IAW SRM 51-24-00. INSTALLED IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20090107 NE 2009 1 7 UALA2008122607011 2 20081226 A 7230 COMPRESSOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 1 ENGINE DAMAGED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 204UA 28713 222067 SILENT SURGE DETECTED - NR 1 ENGINE. MM BORESCOPED ENGINE AND FOUND NUMEROUS STAGE-8 AND STAGE-9 HP COMPRESSOR BLADES D AMAGED, WITH PIECES MISSING AND BENT AIRFOILS. THE ENGINE WAS REPLACED PRIOR TO FURTHER FLIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 20090107 NM 2009 1 7 FDEA200812265296 1 20081226 A 5310 AFA71321 SUPPORT FITTING DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 5 SUPPORT FITTING AT HOLE D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090107 NM 2009 1 7 FDEA200812265297 1 20081226 A 5310 AFA71321 SUPPORT FITTING DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JA MB NR 6 SUPPORT FITTING AT HOLES A, B AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAI R CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090106 2009 1 6 YENA200812300132 4 20081225 A 3416 066011534001 ALTIMETER EMB ERJ190 ERJ190100IGW 3260408 NM NR 2 FAILED A YENA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 15 239JB 6207 190000040 FLT NR 52, JFK-BTV, AIR RETURN TO JFK, LANDING GEAR ORAL WARNING IN COULD NOT INHIBIT. R&R RADAR ALTIMETER NR 2 IAW AMM 34-31-01, OPS TEST AND CHECK GOOD. 2 L 7 2 4F RT A57NM 20090106 NM 2009 1 6 YENA200812300134 1 20081228 A 2150 10007004 ACM EMB ERJ190 ERJ190100IGW 3260408 NM NR 2 FAILED A YENA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 197JB 7886 190000020 FLT NR 434, MCO-BOS, AIR RETURN TO MCO, FUMES OF UNKNOWN ORIGIN REPORTED IN CABIN AFTER TAKE OFF. COMPLETED QRH FUMES D ISSIPATED. COMPLETED SMOKE REMOVAL. QRH AND FUMES RETURNED WHEN PACKS RESELECTED ON RETURN TO PACKS OFF CONFIG AND FUM ES DISSIPATED AGAIN. (AIR CONDITIONING PACKS-SINGLE) R&R NR 2 AIR CYCLE MACHINE IAW 21-51-05. OPS CHECK NORMAL, NO ODOR PRESENT. 2 L 7 2 4F RT A57NM 20090106 NM 2009 1 6 FDEA200812245280 1 20081224 A 5311 53FXU561 FRAME BOEING 727 727233 138408A NM ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 276FE 22041 GOUGED FRAME ON STA 580, STR 3L REMOVED FASTENERS IAW SRM 51-30-2, BLENDED OUT DAMAGE AREA IAW SRM 51-10-1. UT AREA IAW NDTM 51-00-00 FIG 2 PT 4. HFEC AREA IAW NDTM 51-00-00 FIG 23 PT 6. NO DEFECTS NOTED. FOUND TO BE OUT OF LIMITS IAW FD X SRM 53-10-1 FIG 1A. FABRICATED REPAIR ANGLE AND HEAT TREATED TO 7075 T6 IAW FAS REPORT NR2 -37153-801 REV A AND EA NR 7-5310-12688. LOCATED, DRILLED, AND DEBURRED REPAIR ANGLE IAW SRM 51-30-5 AND EA NR 7-5310-12688. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2 AND EA NR 7-5310-12688 AND INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND EA NR 7-5310-12688. 2 L 7 3 4F RT A3WE 20090106 NM 2009 1 6 USAA2008123092338 1 20081230 A 5330 SKIN BOEING 737 7373B7 138447F NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 527AU 23862 CLT - MAJOR REPAIR - RON - NR 6095204, CRACKED FUSELAGE SKIN AT BS 727E, S24L. REPAIRED FUSELAGE SKIN AT BS 727E, S24L I AW B737 SRM 53-00-01-2R-31. 2 L 7 2 4F RT A16WE 20090106 EU 2009 1 6 USAA2008123192370 1 20081221 A 2560 BATTERY AIRBUS 320 A320232 3930326 EU FLASHLIGHT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 647AW 762 SAL - EES - C8 CHECK - NR 6142565 INOPERATIVE BATTERY IN FLASHLIGHT AT AFT SWIVEL FLIGHT ATTENDANTS SEAT. REMOVED AND REPLACED FLASHLIGHT BATTERY AT THE AFT SWIVEL FLIGHT ATTENDANTS SEAT. 2 L 7 2 4F RT A28NM 20090106 EU 2009 1 6 USAA2008123192371 1 20081215 A 5320 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - MAJOR REPAIR - C8 CHECK - NR 6138912, CORROSION ON THE L2 DOOR CUT OUT LOWER SILL AT FR 67+12". REPAIRED THE L2 D OOR CUT OUT LOWER SILL AT FR 67+12" IAW A320 SRM 53-41-14 FIGURE 201 REPAIR PRINCIPLE 5. 2 L 7 2 4F RT A28NM 20081126 NM 2008 11 26 ASAA0873855 1 20081118 A 5320 141A85119 WEB BOEING 737 737790 13844CN NM BS 338 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 E/E BAY DOOR CUTOUT RT WEB DAMAGED. REMOVED AND REPLACED WEB. 2 L 7 2 4F RT A16WE 20081126 NM 2008 11 26 SWAA086558 1 20081120 A 2560 P4010021 BATTERY BOEING 737 737317 138447P NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 693SW 23174 FOUND AFT FLASHLIGHT INOP. R&R BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081126 EU 2008 11 26 F3LA2008111900719 1 20081117 A 5270 2LA00546901 WARNING LIGHT AIRBUS A318 A318111 3940019 EU OVERWING SLIDE FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 806FR 13 2218 PILOT REPORTED THAT THE LEFT OVERWING EXIT SLIDE ARMED LIGHT IS ILLUMINATED WHEN ON MAINTENANCE BUS. EMERGENCY EXIT OPE N ECAM INDICATION. MAINTENANCE REMOVED AND REPLACED LEFT OVERWING SLIDE ARMED INDICATOR LIGHT AND PERFORMED OPERATIONAL TEST IN ACCORDANCE WITH A318 AMM 52-73-21-000-003. 2 L 7 2 4F RT 20081211 EA 2008 12 11 ASOA200801607 1 20081202 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 FS 559 BULKHEAD WEB AND CAP ANGLE HAS INDICATIONS NOTED. RT WEB WL 58.70 HAS INDICATION NOTED APPROX .2 INCH IN LENGTH 70 PERCENT FSH AND LT CAD ANGLE AT LBL 18 HAS INDICATION NOTED APPROX .3 INCH IN LENGTH 70 PERCENT FSH, FAILED NDT INSPE CTION. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW BOMBARDIER REO 601R-53-41-260, REV C. C/W EC/TC REO 601R-53-41-827 & MET ALL THE REQUIREMENTS OF REO 601R-53-41-827. 2 L 7 2 4F RT A21EA 20081211 EA 2008 12 11 SWIA200820604 1 20081203 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 802SK 15061 FLT 4596 - FLIGHT ATTENDANT EMERGENCY EXIT SIGN INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 QXEA2008121001234 1 20081206 A 5270 WARNING SYSTEM BOMBDR DHC8 DHC8402 1390042 NM DOOR MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 19 417QX 4086 ALW - ON LIFT OFF FUSELAGE DOOR WARNING LIGHT/AFT SERV DOOR UNSECURE INDICATION. DOOR APPEARED SECURE. AIRCRAFT PRESSU RIZATION NORMAL. CHECKED DOOR SENSOR VALUES PER AMM 32-61-00 PG 602. VALUES IN NORMAL RANGE. DOOR WARNING SYSTEM OPS CHECKED GOOD PER AMM 52-41-00-710-801 STEP 3.B. NO DEFECTS, NOTED RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081211 EA 2008 12 11 ASOA200801671 1 20081206 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 FLOOR SUPPORT CAP HAS CORROSION AT LBL 9 BETWEEN FS 485.00 AND FS 501.00. BLENDED FLOORBEAM CAP LBL 9 BETWEEN FS485.00 & FS501.00 IAW CRJ 700 SRM 51-21-06. REQUIRES THICKNESS CHECK. LBL 9 FLOORBEAM REPLACED DUE TO OUT OF LIMIT CORROSION. REFER TO W/O 105591 N/R-00391 FOR BEAM REPLACEMENT. 2 L 7 2 4F RT A21EA 20081211 WP 2008 12 11 AALA200802378S 1 20081021 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT INCORRECT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 955U 49427 LGA - EMERGENCY LIGHT AT OVERHEAD FORWARD OF RIGHT LAVATORY HAS INCORRECT LENS. REPLACED LENS FOR EMERGENCY LIGHT AT OV ERHEAD FORWARD OF RIGHT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081211 NM 2008 12 11 AALA200802379S 1 20081022 A 3350 LIGHT BOEING 777 777223 1385213 NM ZONE 200 BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 784AN 29588 NRT - EMERGENCY LIGHT LEFT OF FORWARD CLOSET IS BROKEN. REPLACED EMERGENCY LIGHT LEFT OF FORWARD CLOSET. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081211 CE 2008 12 11 GUUA91252120708A 1 20081207 A 5220 DOOR BEECH 1900 1900D 1154162 CE EMERGENCY EXIT STUCK A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 45AR UE12 REPORT:DURING SCHEDULED ROUTINE MAINTANANCE DISCOVERED RIGHT FORWARD EXIT HARD TO OPEN. LUBRICATED RIGHT FORWARD EMERGE NCY EXIT DOOR HANDLE. 2 L 7 2 4T RT A24CE 20081211 EU 2008 12 11 AALA200802381S 1 20081022 A 3260 PROXIMITY SENSOR AIRBUS 300 A300B4605R 3930308 EU MLG FAULTED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 14077 612 BOG INFLIGHT - NOSE LANDING GEAR DOOR INDICATION ILLUMINATED ON BOTH GEAR INDICATION PANELS. RETURNED TO BOG AND LANDED WITHOUT INCIDENT. ACCOMPLISHED BITE CHECK OF GROUND PROXIMITY DETECTION UNIT AND FOUND NUMBER TEN SENSOR FAULTED. RES ET FAULT AND CLEARED. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081211 WP 2008 12 11 AALA200802371V 1 20081021 A 3397 CONNECTOR DOUG DC9 DC982 3022082 WP ZONE 200 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 955U 49427 LGA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. RESET CONNECTOR AT SEAT 29D FOR INOPERATIVE EMERGENCY LIGHT . SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081211 WP 2008 12 11 AALA200802373V 1 20081021 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 955U 49427 LGA - SEAT MOUNTED FORWARD EMERGENCY LIGHT MISSING LAMPS AT SEAT 4E. REPLACED LAMPS FOR EMERGENCY LIGHT AT SEAT 4E. SY STEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081211 WP 2008 12 11 AALA200802374S 1 20081021 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 955U 49427 LGA - SEAT MOUNTED FORWARD EMERGENCY LIGHT MISSING SHROUD AT SEAT 4E. REPLACED SHROUD FOR EMERGENCY LIGHT AT SEAT 4E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081211 WP 2008 12 11 AALA200802375S 1 20081021 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 955U 49427 LGA - SEAT MOUNTED FORWARD EMERGENCY LIGHT MISSING LENS AT SEAT 4E. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 4E. SYST EM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081211 NM 2008 12 11 DU4R2008266 1 20081207 A 5730 SKIN BOEING 757 75723APF 1384966 NM LT WING CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 868AN 24868 DURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND CORROSION ON LT WING AT NUMEROUS FASTENERS IN UPPER SKIN I N PREVIOUSLY WORKED SKIN AND UNWORKED SKIN. 2 L 7 2 4F RT A2NM 20081211 SO 2008 12 11 C2XA08IA248 1 20081208 A 2120 UNKNOWN EMB 145 EMB145XR 3260214 SO CABIN & COCKPIT ODOR A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 24103 145645 IAH - FLIGHT 2608 THE CREW REPORTED A FUEL SMELL ON TAKEOFF IN THE CABIN AND COCKPIT THAT LASTED 30-60 SECONDS. THE AIR CRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, OPERATIONALLY CHECKED THE B LEED SYSTEM ALL WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081211 2008 12 11 DL76G081668 4 20081130 A 3421 INDICATOR BOEING 767 7673P6 1385105 NM STDBY ATTITUDE INOPERATIVE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 155DL 6005 25269 STANDBY ATTITUDE INDICATOR INOP. REPLACED INDICATOR. 2 L 7 2 4F RT A1NM 20081212 NM 2008 12 12 HNAA2008120800341 1 20081208 A 2910 82900001001 HYDRAULIC SYSTEM DHAV DHC8 DHC8102 2809003 NM NR 2 CONTAMINATED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 908HA 59617 59617 015 JUST AFTER TAKEOFF, THE 'RUDDER PRESSURE' AND 'RUDDER FULL PRESSURE' CAUTION LIGHTS ILLUMINATED. THE CREW ELECTED TO RE TURN TO THE ORIGINATING AIRFIELD. AFTER THE LANDING GEAR AND FLAPS WERE EXTENDED, THE CAUTION LIGHTS EXTINGUISHED. BOT H HYDRAULIC SYSTEMS QUANTITIES REMAINED NORMAL. MAINTENANCE DISCOVERED THE NR 2 HYDRAULIC SYSTEM HAD AIR IN THE SYSTEM. SYSTEM WAS BLED AND REPLENISHED. AIRCRAFT WAS RUN ON THE GROUND AND RUDDER ACTUATED SEVERAL TIME WITHOUT ANY CAUTION LIGHTS ILLUMINATING. AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 20081212 NM 2008 12 12 HNAA2008120700340 1 20081207 A 2917 2379003001 REGULATOR DHAV DHC8 DHC8102 2809003 NM HYDRAULIC SYS FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 846EX 2622 88 326 JUST AFTER TAKEOFF, THE 'RUDDER FULL PRESSURE', 'RUDDER PRESSURE', AND 'NR 2 RUDDER HYDRAULIC' CAUTION LIGHTS CAME ON. HYDRAULIC QUANTITIES WERE NORMAL. THE AIRCRAFT WAS RETURNED TO THE FIELD. MAINTENANCE REPLACED THE DUAL PRESSURE REGUL ATOR. LEAK AND OPS CHECKS WERE GOOD AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2 H 7 2 4T RT A13NM 20081212 NE 2008 12 12 UPS08554083 2 20081201 A 7200 ENGINE BOEING 757 75724APF 1384969 NM RROYCE RB211 RB211* 54555 NE NR 2 FAULTY A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 438UP 25469 INSPECTION TYPE:N/A RT PACK EXTREME ODOR/FUMES WHEN OPERATING SHUT DOWN RT PACK & FUMES EXTINGUISHED. ACCOMPLISHED NR 2 ENG PWR RUN PER MM 71-00-00-5. OIL FUMES EMITTED FROM NR 2 ENG WITH EITHER PACK L OR R SELECTED AND ENG ABOVE GRD IDLE . FUMES DISSIPATED WITH NR 2 ENG BLEED OFF. REF L/P 160663 I3 NR 2 ENG REMOVED AND REPLACED, NO FUMES NOTED DURING ENG RUN AFTER INSTALLATION. 2 L 7 2 4F 4 F RT A2NM A12EU 20081212 WP 2008 12 12 UPS08854074 1 20081118 A 5730 SKIN DOUG DC8 DC871F 302199D WP WING MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:SV SURVEY SEQ 729-W4-10 DOES NOT MEET SRM CRITERIA. PREVIOUSLY REPAIRED, FOUND NO DEFECTS 51-40-02. 2 L 7 4 4F RT 4A25 20081212 SO 2008 12 12 LR7A08125 1 20081205 A 5220 SKIN LKHEED 382 382G 526414U SO ESCAPE HATCH CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 406LC 128 4676 DURING A-CHECK INSPECTION, FOUND FWD ESCAPE HATCH LEADING EDGE SKIN CRACKED AT FS 212, WL 285. REPAIRED ESCAPE HATCH SK IN IAW SMP583 52-40. 2 H 7 4 4T A1SO 20081212 NM 2008 12 12 USAA2008120992210 1 20081123 A 5320 D5361018300240 STIFFENER AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 808AW 1088 SAL - C7 - MAJOR REPAIR - CORROSION ALONG PLATE STIFFENER ASSEMBLY AT FR12 +6, -Y1292. REPLACED PLATE STIFFENER ASSEMBL Y AT FR12 +6, -Y1292 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081212 NM 2008 12 12 USAA2008120992211 1 20081126 A 5320 D5348004800104 FITTING AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 808AW 1088 SAL - C7 - MAJOR REPAIR - CORROSION ON CENTER FITTING OF LOWER SILL AT FR66 TO FR68, S23R. REPLACED CENTER FITTING OF L OWER SILL AT FR67 +15, S23R IAW A319 SRM 57-72-11. 2 L 7 2 4F RT A28NM 20081212 NM 2008 12 12 USAA2008121092214 1 20081209 A 5311 D531122240005 BRACKET AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 806AW 1056 PIT - C7-C3 BRIDGE - MAJOR REPAIR - GALVANIC CORROSION ON FRAME BRACKET AT FR 365, -Z240. REPLACED FRAME BRACKET AT FR 365, -Z240 IAW SRM 53-11-14. UPON FURTHER EVALUATION, FOUND DISCREPANCY TO BE LEVEL 2 CORROSION. 2 L 7 2 4F RT A28NM 20081212 NM 2008 12 12 USAA2008121092215 1 20081209 A 5315 D5311281400200 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 806AW 1056 PIT - C6 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT FR20, -Y765. REPLACED FLOORBEAM AT FR20, -Y765 IAW A319 SR M 51-72-11. 2 L 7 2 4F RT A28NM 20081212 NM 2008 12 12 SWAA086921 1 20081209 A 2913 849589 PUMP BOEING 737 7377H4 1384404 NM NR 2 ENGINE FAULTY A SWAA K NONE J WARNING INDICATION CR CRUISE 1 SW 29 261WN 32517 DECLARED EMERGENCY, NR 2 ENG DRIVEN HYDRAULIC PRESSURE LOW PRESSURE LIGHT EN ROUTE SUBSEQUENT SLOW LOSS OF QUANTITY. RE MOVED AND REPLACED NR 2 ENGINE HYDRAULIC PUMP PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086922 1 20081207 A 5330 6545772 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 697, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086920 1 20081209 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 23R. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086927 1 20081209 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 16R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086884 1 20081206 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 477WN 33988 FOUND LT TRACK LIGHT COVER MISSING. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086885 1 20081206 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 477WN 33988 FOUND RT TRACK LIGHT COVER MISSING. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086886 1 20081205 A 5610 5893543140 WINDOW BOEING 737 7375H4 138449D NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED MV2 CHECK, FOUND R1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086928 1 20081208 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 363SW 26574 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STR 10L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086929 1 20081207 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 373SW 26581 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, STR 2R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081212 2008 12 12 SWAA086930 4 20081207 A 2565 61620468 SLIDE BOEING 737 7375H4 138449D NM L1 DOOR UNWANTED DEPLOY A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 515SW 25154 L1 EMERGENCY EXIT DOOR SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086931 1 20081208 A 5753 6546434369 FLAP BOEING 737 7375H4 138449D NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 525SW 26567 DURING SCHEDULED MV2 CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED. REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086932 1 20081208 A 3350 8210248801 LENS BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 428WN 29844 LT OVERWING EEPLS LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086933 1 20081207 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 455WN 32462 FWD EEPLS LIGHT COVER MISSING. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086938 1 20081207 A 3350 417A56014 COVER BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 636WN 27709 FOUND R1 DOOR EMERGENCY EXIT SIGN COVER LOOSE. REMOVED AND REPLACED SIGN PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086939 1 20081206 A 5230 6546921230 DOOR BOEING 737 7373H4 1384600 NM FWD CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 653SW 28398 DURING SCHEDULED MV3 CHECK, FOUND FWD CARGO DOOR LOWER AFT CORNER CRACKED. REMOVED AND REPLACED DOOR PER MM. 2 L 7 2 4F RT A16WE 20081212 2008 12 12 SWAA086894 4 20081204 A 2565 D31354 SLIDE BOEING 737 7373Q8 1384670 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 687SW 23388 R1 DOOR SLIDE OUT OF POSITION. POSITIONED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086883 1 20081206 A 3350 417A56014 SIGN BOEING 737 7377H4 1384404 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 472WN 33831 AFT GALLEY EMERGENCY EXIT SIGN FELL OFF. REMOVED AND REPLACED SIGN PER MM. 2 L 7 2 4F RT A16WE 20081212 2008 12 12 SWAA086895 4 20081206 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 710SW 27844 R1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086896 1 20081205 A 3350 284A01216 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 765SW 29805 DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086897 1 20081206 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 790SW 30604 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, RBL 1. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086900 1 20081205 A 3350 81000 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 920WN 32460 FOUND EEPLS COVER MISSING AT ROW 1. REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086901 1 20081208 A 3350 767 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 201LV 29854 DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EMERGENCY EXIT HATCH LIGHT INOP. REMOVED AND REPLACED BULB PER MM. 2 L 7 2 4F RT A16WE 20081230 NM 2008 12 30 UALA2008122406988 1 20081223 A 2560 P20700031 FLASHLIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 777UA 26916 EMERGENCY FLASHLIGHT AT 3R INOP. REPLACED FLASHLIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081230 NM 2008 12 30 UALA2008122406989 1 20081222 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 174UA 24381 SEAT EMERGENCY LIGHT 21ABC INOP. REPLACED EMERGENCY LIGHT INOP AT SEAT 21ABC. OPS CHECKED OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20081230 2008 12 30 UALA2008122406990 4 20081223 A 2565 101630302 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE R1 DOOR LOW PRESSURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 644UA 25094 DOOR 1R PRESSURE GAUGE IS BELOW THE GREEN BAND. REPLACED SLIDE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081230 EU 2008 12 30 UALA2008122406991 1 20081223 A 5320 SUPPORT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE R2 DOOR SILL CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 406UA 454 R2 DOOR SILL HAS CORROSION AT AFT GIRT SUPPORT BLOCK. MAJOR REPAIR. INSTALLED REPAIR ANGLE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081230 NM 2008 12 30 UALA2008122406996 1 20081224 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHT DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY EXIT LIGHTS INOP, DOOR 1L, 2L, 2R, 4L CEILING ARE A, & UPPER DECK LT DOORWAY. REPLACED BATTERY PACKS AT ALL L OCATIONS. LIGHTS CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081230 NM 2008 12 30 UALA2008122406997 1 20081224 A 3350 362624 LIGHT BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 105UA 26473 EMERGENCY LIGHT BROKEN, ROW 48LT & 58RT. REPLACED LIGHTS, OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081230 NM 2008 12 30 UALA2008122406998 1 20081224 A 3350 9F19948501 LAMP BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 105UA 26473 ESCAPE SLIDE INDICATOR LIGHTS INOP, DOOR 4R & 5L. RELAMPED, OPS CHECK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081230 NM 2008 12 30 UALA2008122406999 1 20081224 A 3510 MF20003 OXYGEN MASK BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE COCKPIT FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 786UA 26938 OBSERVER O2 MASK EMERGENCY BUTTON STICKING. CREW O2 HAS A HISTORY OF BEING LOW. SUSPECT MASK. REPLACED O2 MASK. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081230 2008 12 30 UALA2008122407000 4 20081224 A 2565 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L1 DOOR LOW PRESSURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 474UA 1475 THE 1L SLIDE PRESSURE LOW. COLD SOAKED DOOR WAS OPEN FOR OVER 1 HR. OP PER MM 25-62-00 PG 603 (NOTE A). 2 L 7 2 4F 4 F RT A28NM E40NE 20081230 NM 2008 12 30 UALA2008122407001 1 20081224 A 3350 78941 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 677UA 30029 EMERGENCY LIGHT AT 1H BROKEN PREVIOUSLY DEFERRED. SECURED LIGHT IN SEAT. INSTALLED MISSING EMERGENCY LIGHT STRIP. 2 L 7 2 4F 4 F RT A1NM E24NE 20081230 2008 12 30 UALA2008122407002 4 20081224 A 2565 B14056008 O-RING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE LEAKING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 560UA 0868 26660 LOW PRESSURE PULLEY STEM LEAKING. REMOVED & REPLACED SHAFT O-RING AND BACK-UP RING. 2 L 7 2 4F 4 F RT A2NM E17NE 20081230 2008 12 30 UPS08154225 4 20081221 A 2565 SM129353312 WARNING LIGHT AIRBUS A300 A300F4622R 3930360 EU EVAC SLIDE INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 154UP 0840 EVAC SLIDE WARNING LIGHTS INOP. DEFERRED PER 52-73-01-1. ACCOMPLISHED ASPSU BATTERY CAPACITY TEST FROM BUILT IN TEST P ANEL PER MM 52-73-00-05. BATTERY 1&2 FAULTED. REPLACED NR 1 BATTERY OPS NORMAL. NR 2 STILL FAULTED. FOUND BATTERY NOT SEATED. RESEATED BATTERY OPS CHECK GOOD. PLACARD REMOVED. 2 L 7 2 4F RT A35EU 20081230 NM 2008 12 30 AALA200802416A 1 20081027 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LGIHT BURNED OUT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 771AN 29579 DFW - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 24G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 26G. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081230 NM 2008 12 30 AALA200802420A 1 20081027 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 610AA 24486 DFW - EMERGENCY LIGHT AT SEAT ROW 31ABC MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 31ABC. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081230 NM 2008 12 30 AALA200802421A 1 20081028 A 2400 POWER SUPPLY BOEING 757 757223 1384957 NM POWER PANEL SHORTED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 698AN 26980 SJU INFLIGHT MIA TO BGI - PASSENGERS REPORTED SEEING SPARKS AT FLOOR VENTS BY RIGHT WING EXIT ROWS. PASSENGERS AND FLIG HT ATTENDANTS IN AREA SMELLED SMOKE. LANDED SJU WITHOUT INCIDENT. FOUND ROW 20DEF LOWER VENT PANEL POWERPORT POWER SUP PLY BOX SMELLED BURNED. REPLACED ROW 20DEF LOWER VENT PANEL POWERPORT POWER SUPPLY. SYSTEM GROUND CHECKED NORMAL OPER ATION. 2 L 7 2 4F RT A2NM 20081230 NM 2008 12 30 AALA200802424A 1 20081028 A 3350 BPS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 195AN 32389 LAX - EMERGENCY LIGHTS AT CENTER CABIN INOPERATIVE. REPLACED BATTERY PACK AT CENTER CABIN. SYSTEM GROUND CHECKED NORMA L OPERATION. 2 L 7 2 4F RT A2NM 20081230 NM 2008 12 30 AALA200802425A 1 20081028 A 3397 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 680AN 29590 DFW - EMERGENCY LIGHT AT SEAT 9DEF INOPERATIVE. INSTALLED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 9DEF. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081230 2008 12 30 UPS08154226 4 20081209 A 2565 WARNING LIGHT AIRBUS A300 A300F4622R 3930360 EU EVAC SLIDE INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 152UP 0835 INSPECTION TYPE:N/A EVACUATION SLIDE WARNING LIGHT INOP. BUZZER OPERATES NORMAL. RESET C/B AS PER MM 52-73-11-04, OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 20081230 WP 2008 12 30 UPS08854229 1 20081219 A 5753 5642970324 SKIN DOUG DC8 DC871F 302199D WP TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:SV SEQ 729-W4-05 RT WING O/B FLAP UPPER SURFACE STA XF 252 2 X 2 INCH DOUBLER GOUGED. ALL WORK ACCOMPLI SHED IAW UPS EO DC8-5720-31671A. 2 L 7 4 4F RT 4A25 20081230 WP 2008 12 30 UPS08854237 1 20081212 A 5720 FUEL TANK DOUG DC8 DC873F 302199F WP RIGHT AUX DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQ 803-W4-24 RT WING L/E AUX TANK LWR SURFACE XFS 60 HAS NO SRM REF PER APPX G AND REQUIRES E NGINEERING. REMOVED EXISTING REPAIR, FABBED AND INSTALLED REPAIR DOUBLER IAW EA 00 8-5730-01-A1576 AND EO DC8-5730-3157 6-A. 2 L 7 4 4F RT 4A25 20081230 WP 2008 12 30 UPS08854239 1 20081224 A 2421 EADI DOUG DC8 DC871F 302199D WP COCKPIT FAILED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:N/A CAPTAIN'S EADI FAILED AND BURNT/SMOKE IN COCKPIT. ***SDR FILED OPEN*** 2 L 7 4 4F RT 4A25 20081230 WP 2008 12 30 UPS08854241 1 20081226 A 5753 5642960510 SKIN DOUG DC8 DC871F 302199D WP TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:N/A CRACK AND DENT RT I/B FLAP LWR SKIN AND INNER STRUCTURE. REPAIRED PER EO DC8-5750-31712 DOUBLER AND COLDWORK REPAIR. 2 L 7 4 4F RT 4A25 20081230 WP 2008 12 30 UPS08854230 1 20081221 A 5320 STRUCTURE DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:SV REPAIR DOUBLER (FEN 729RA1019) HAS NO SUPPORTING DOCUMENTATION, (LOCATE D AT STA 1600, L30R). INSTAL LED REPAIR IAW DC8 SRM 53-02-01-0 TR 53-203 FIGURE 7 SHEET 13. 2 L 7 4 4F RT 4A25 20081230 2008 12 30 UPS08M54232 4 20081222 A 2565 60289115 BOTTLE DOUG MD11 MD11F 3023600 NM EVAC SLIDE LOW PRESSURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 296UP 48474 INSPECTION TYPE:N/A L1 DOOR SLIDE'S BOTTLE PRESSURE IS LOW PER TEMPERATURE COMPENSATED GREEN BAND ON GAUGE PRESSURE SWIT CH IS CLOSED DUE TO LOW PSI. REPLACED L1 DOOR SLIDE ASSY IAW MD-11 MM 25-61-01-4. THIS CLEARS M-391314. PLACARD REMOV ED. 2 L 7 3 4F RT A22WE 20081230 WP 2008 12 30 UPS08854219 1 20081013 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR 803-F1-24, STA 270-278 L23R-L25R, HAS SRM 53-02-01 FIG 7 SHT 11, IS CAT B, AND REQUIRES ENGINE ERING DISPOSITION. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED NEW REPAIR REF UPS EO DC8-5330-31561-A. 2 L 7 4 4F RT 4A25 20090115 2009 1 15 UALA2008121906920 4 20081218 A 2210 COMPUTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FLT CONTROLS FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 592UA 28143 AUTOPILOT FAILURE. FLT DIVERTED. SUPPLEMENTAL DATA UPDATE FOUND MULTIPLE INFC FAULTS AND CENTER FCC FAILED. CTR FCC PULL ED DOWN INTERCONNECT BUS. REPLACED CENTER FLIGHT CONTROL COMPUTER AND CHECKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081224 WP 2008 12 24 NWAA085629993 1 20081216 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8986E 47402 DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OP CONDITION. 2 L 7 2 4F A6WE 20081224 NM 2008 12 24 ASAA0874043 1 20081210 A 5320 FLOOR SUPPORT BOEING 737 737790 13844CN NM BS 800-829 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION AROUND NUTPLATE HOLES ON FLOOR SUPPORT. R&R AFT CARGO TRACK FROM BS 727 TO BS 849 RBL 14 IAW SRM 51 40 02. 2 L 7 2 4F RT A16WE 20081224 NE 2008 12 24 NWAA085583270 2 20081214 A 7321 ECU AIRBUS 320 A320212 3930322 EU CFMINT CFM56 CFM565A3 NE NR 1 ENGINE FAILED A NWAA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 GL 01 370NW 1037 DURING CLIMB AT 27,000 FT ENGINE NR 2 ECAM MSG FADEC FAULT. C/B A-4 TRIPPED AND ENGINE NR 1 FLAMED OUT. RELIGHT WAS SU CCESSFUL. DURING DESCENT FOR LANDING AT 12,000 FT ENGINE NR 1 FLAMED OUT AGAIN. FLIGHT CREW PERFORMED A SINGLE ENGINE LANDING. MX REPLACED THE ECU, PMA STATOR AND ROTOR. 2 L 7 2 4F 4 F RT A28NM E29NE 20081224 NM 2008 12 24 ASAA0874058 1 20081217 A 5320 141A83107 ANGLE BOEING 737 737790 13844CN NM BS 310-344 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION ON THRESHOLD SUPPORT ANGLE BS 310 TO BS 344 WL 208 RBL 50. 2 L 7 2 4F RT A16WE 20090106 2009 1 6 USAABB08178 4 20081228 A 2565 101630306 SLIDE BOEING 767 7672B7 1385107 NM RT OVERWING UNSERVICEABLE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AY 40081 2146 24764 CLT - THE RIGHT WING ESCAPE SLIDE LACING CORD OPENED WHEN THE SLIDE DOOR WAS OPENED. MAINTENANCE REPLACED THE RIGHT WIN G ESCAPE SLIDE. OK FOR SERVICE. 2 L 7 2 4F RT A1NM 20090106 NM 2009 1 6 USAABB0179 1 20081231 A 3350 BATTERY PACK BOEING 767 7672B7 1385107 NM CABIN DISCONNECTED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 251AY 24764 BRU - THE CEILING EMERGENCY LIGHTS FROM ROW 11 TO 19, LEFT AISLE, WERE FOUND INOPERATIVE DURING TEST. MAINTENANCE FOUND BATTERY PACK ON LEFT HAND LOWER SIDEWALL, NEXT TO SEAT 13A/B, DISCONNECTED. THE BATTERY PACK WAS RECONNECTED. SYSTEM OPERATIONALLY CHECKS OK. 2 L 7 2 4F RT A1NM 20090107 NM 2009 1 7 FDEA200812265295 1 20081226 A 5310 AFA71321 SUPPORT FITTING DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JA MB, NR 4 SUPPORT FITTING AT HOLES A, B, C AND D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090107 EA 2009 1 7 2009F00005 2 20081230 A 8500 ENGINE PIPER PA23 PA23250 7102308 SO LYC O540 IO540C4B5 41532 EA LEFT POWER LOSS E ECLA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 09 63790 27775411 L176948A AFTER APPROX 30 MINUTES OF IFR FLIGHT AT 8000 FT WITH NO OUTSIDE EVIDENCE OF AIRFRAME ICING THE PILOT NOTICED LT ENG LOO SING FUEL PRESSURE AND MANIFOLD PRESSURE, PILOT FOLLOWED ENG FAILURE CHECKLIST AND ALTERNATE AIR, BOOST PUMPS AND FULL M IXTURE WERE APPLIED ON THAT ENG WITH NO EFFECT, ENGINE AT IDLE POWER SETTING ONLY, PILOT THEN CROSS FEED FROM RT WING TA NK TO LT ENG AND SHORTLY AFTER BEGAN LOOSING FUEL PRESSURE AND MANIFOLD PRESSURE ON THE RT ENG THE PILOT THEN SWITCHED T HE CROSS FEED OFF AND ADVANCED MIXTURE, BOOST PUMP AND ALTERNATE AIR WERE APPLIED TO THE RT ENGINE WITH NO EFFECT. AFTER MANEUVERING TOWARD AN ALTERNATE AIRPORT THE LT ENGINE CAME BACK UP ON POWER FOLLOWED SHORTLY AFTER BY THE RT ENGINE. TH 1 L 7 2 3O 3 O 1A10 1E4 20090107 NM 2009 1 7 UALA2008122907015 1 20081227 A 3350 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN NOT SEATED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EXIT LIGHT INOP AT SEAT 5J AFT LIGHT ASSY. RESEATED CONNECTOR. CHECKS OK 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008122907016 1 20081227 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EXIT LIGHT INOP AT ROW 37 RT CEILING LIGHT. RELAMPED. CHECKS OK 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008122907017 1 20081227 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EXIT LIGHT INOP UPPER DECK CEILING AT ROW 12. RELAMPED, CHECKS OK 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008122907026 1 20081228 A 2421 727810B GENERATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU DAMAGED A UALA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 29 595UA 28748 AFTER APU START UP, OIL RUNNING FROM UNDERNEATH OF GEN TERMINAL BLOCK. CTR 2 FIELD STUDS APPEAR TO BE BROKEN. REPLACED APU GENERATOR AND FEEDER CABLES. NO LEAKS DURING APU OPS CHECK. 2 L 7 2 4F 4 F RT A2NM E17NE 20090107 NM 2009 1 7 UALA2008122907028 1 20081228 A 3040 6240665 CONTROLLER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE WINDOW HEAT OUT OF TOLERANCE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 REPLACE NR 1 RT WINDOW HEAT CONTROLLER ACCT SHATTERED WINDOW. R&R CRACKED WINDOW. REPLACED NR 1 RT WINDOW HEAT CONTROL LER. 2 L 7 2 4F 4 F RT A2NM E17NE 20090107 NM 2009 1 7 UALA2008122907029 1 20081229 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 UPPER DECK EMERGENCY CEILING LIGHT INOP ROW 13. RELAMPED, OPS CK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008123007038 1 20081229 A 2432 20131A CHARGER BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE MAIN BATTERY FAULTY A UALA K NONE J WARNING INDICATION IN INSP/MAINT 1 WP 29 665UA 29237 EICAS MSG MAIN BATTERY CHARGER. REPLACED MAIN BATTERY CHARGER. 2 L 7 2 4F 4 F RT A1NM E24NE 20090107 NM 2009 1 7 UALA2008123007040 1 20081230 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT LIGHT INOP AT DOOR 5 LT FWD SILL LIGHT. REPLACED LAMP. OPS CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008123007043 1 20081230 A 3350 78671 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT LIGHT INOP AT SEAT ROW 46 LT. RELAMPED. CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008123007047 1 20081229 A 7330 PRESSURE SWITCH BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FUEL SYSTEM FAULTY A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 795UA 26927 LT ENG FUEL FILTER INDICATION. REPLACED DIFFERENTIAL PRESSURE SWITCH 2 L 7 2 4F 4 F RT T0001SE E46NE 20090107 EU 2009 1 7 UALA2008123007049 1 20081230 A 5313 STRINGER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 455UA 1105 STRINGER 38 LT BETWEEN FRAMES 32 & 31 HAS IMPACT DAMAGE. MFG NEW CLEAT. HFEC REVEALED NO CRACKS AT THIS TIME. ACCOMPLI SHED STRINGER REPAIRS TO 37L AND 38L. 2 L 7 2 4F 4 F RT A28NM E40NE 20090107 CE 2009 1 7 CIEA200800009 1 20081216 A 5610 5042006936 WINDSHIELD BEECH 90 E90 1152914 CE COCKPIT CRACKED E CIEA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 63BV 3251 LW256 DURING CRUISE AT FL240 APPROX 80 TO 90 MILES FROM KCPR, THE RT SIDE FRONT WINDSHIELD CRACKED. AT THE TIME, THE TEMPERAT URE OUTSIDE WAS -38 DEGREES CELSIUS AND THE WINDSHIELD HEAT WAS OFF WITH CLEAR SKIES OBSERVED. THE PILOT CONTACTED ATC AND LET THEM KNOW THE WINDOW WAS BROKEN AND THE PRESSURIZATION WAS HOLDING. AFTER LOOKING AT THE CHECKLIST FOR THIS PRO BLEM, THE PILOT ASCERTAINED THE INNER PANEL WAS BROKEN AND REQUESTED A DESCENT. THE PILOT WAS GIVEN DISCRETION TO 15,00 0 FEET. THE PILOT CALLED INTO FLIGHT CONTROL AND WAS ADVISED TO RETURN TO DEPARTURE. THE PILOT RETURNED AND NO FURTHER ISSUES WERE OBSERVED WITH THE FLIGHT. THE PILOT COORDINATED WITH THE PASSENGERS AND ATC WITH NO ISSUES. 1 L 7 2 3T 3A20 20090107 NM 2009 1 7 UALA2008120506760 1 20081204 A 5210 FITTING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R2 DOOR MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 579UA 26697 MED 2 RT EMER TRIGGER MECH. MISSING ADJUSTMENT SAFETY CLIP. REPLACED SAFETY CLIP. 2 L 7 2 4F 4 F RT A2NM E17NE 20090107 NM 2009 1 7 UALA2008123107059 1 20081230 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 128UA 30023 SEAT 35 HJK SEAT EMERGENCY LIGHT INOP BROKEN. REPLACED LIGHT ASSEMBLY. OPS CHECK IS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008111305606 1 20080902 A 2930 SENSOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE HYDRAULIC SYS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 175UA 24382 NR 4 HYD OVERHEAT, TEMP WOULD RISE TO 96 DGR WITH ADP RUNNING, TEMP WOULD RISE TO 88 DEGREES WITH AUX PUMP RUNNING. DPI INDICATORS ARE IN ON CASE DRAIN MODULE AND RETURN FILTER MODULE. MEASURED TEMPERATURE AT RETURNED MODULE MATCHES FLIGH T DECK INDICATION AND HYD QTY IS NORMAL. REPLACED NR 4 ENG HYD TEMP SENSOR, RETURN FILTER, AND CASE DRAIN FILTERS. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 USAA2009010590022 1 20081224 A 5320 65458562F4 INTERCOSTAL BOEING 737 7374B7 138449C NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT Q5 MAJOR REPAIR NR 03C10853057/004 LEVEL 2 INTERGRANULAR CORROSION ON INTERCOSTAL BETWEEN BS947 TO BS967, S21R. REP AIRED INTERCOSTAL BETWEEN BS947 TO BS967, S21R IAW BOEING DRAWING NR 65-458562. 2 L 7 2 4F RT A16WE 20090107 NM 2009 1 7 USAA2009010590023 1 20081229 A 5311 65C22908 FRAME BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT Q5 MAJOR REPAIR NR 03C20853011/001 CRACK ON FUSELAGE FRAME AT BS500B BELOW S20L. REPAIRED FUSELAGE FRAME AT BS500B BELOW S20L IAW B737 SRM 53-00-07 & US AIRWAYS EA NR 100790. 2 L 7 2 4F RT A16WE 20090107 EU 2009 1 7 FDEA200812185198 1 20081218 A 5321 FXSRZ25005251FG FLOORBEAM AIRBUS 310 A310 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 3668 248 FLOORBOARD 251FG BROKE AT CORNER FROM FRAME 69 TO FRAME 71 LT SIDE. REPAIRED FLOORBOARD BY FABRICATING A NEW FLOORBOARD FROM STOCK MATERIAL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ20-005; REV " G ". 2 L 7 2 4F RT A35EU 20090107 EU 2009 1 7 FDEA200812195239 1 20081219 A 5347 A5327400500000 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 CABIN SEAT TRACK BETWEEN RBL 28 & RBL 38 IS GOUGED AT FR 37. REMOVED DAMAGE AND CHECKED LIMITS REF SRM 53-10-16. ALODI NED REF SRM 51-21-10. PRINED & PAINTED REF SRM 51-23-10. 2 L 7 2 4F RT A35EU 20090107 EU 2009 1 7 FDEA200812185199 1 20081218 A 5321 FXSRZ25005242SK FLOOR PANEL AIRBUS 310 A310 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 38333 248 FLOOR PANEL BETWEEN FR 45 - 46 & BETWEEN RBL 71 - 91 IS BROKEN ON THE EDGE. 242SK REPAIRED FLOOR PANEL BY FABRICATING A NEW FLOOR PANEL FROM STOCK MATERIAL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ20-005; REV " G ". 2 L 7 2 4F RT A35EU 20090107 NM 2009 1 7 QXEA2008121901253 1 20081218 A 2711 TRIM SYSTEM BOMBDR DHC8 DHC8402 1390042 NM AILERONS OUT OF ADJUST A QXEA O OTHER F FLT CONT AFFECTED CL CLIMB 1 NM 19 402QX 4032 DURING CLIMB AND CRUISE MORE THAN HALF AILERON TRIM IS REQUIRED TO MAINTAIN WINGS LEVEL. DURING SLOW SPEEDS AND FLAPS A T 35 TRIM IS NORMAL. AIRCRAFT IS CONTROLLABLE DURING ALL PHASES OF FLIGHT. LT WING IS HEAVY WING. FERRY TO PDX FOR REP AIRS. INSPECTED AILERON SYSTEM, NO DEFECTS NOTED. C/W ADJUSTMENT OF THE GROUND ADJUSTABLE TAB IAW AMM TASK 27-13-11-83 0-803 STEPS 3A (2) AND (6). PERFORMED CHECK FLIGHT, NO DEFECTS NOTED. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20090107 NM 2009 1 7 QXEA2008122401256 1 20081220 A 5210 BOLT BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR LOOSE A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 19 422QX 4150 BOI - FRONT PAX DOOR IS UNLATCHED, BUT WILL NOT OPEN. FOUND DOOR RAIL BOLT LOOSE CAUSING DOOR TO HANG UP. TIGHTENED FA STENER SECURELY. DOOR OPENS AND CLOSES NORMALLY. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20090107 NM 2009 1 7 ASAA0944143 1 20081214 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU NR 2 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 NR 2 SPOILER UPPER SKIN IS DENTED. PREPPED DAMAGED AREA FABRICATED DOUBLER AND BONDED REPAIR IAW SRM 51 70 10 REPAIR 2. 2 L 7 2 4F 4 F RT A16WE E21EU 20090107 NM 2009 1 7 ASAA0944148 1 20081214 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM NR 3 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 LT NR 3 SPOILER UPPER SKIN DENTED .45 INCH DIAMETER AND .004 DEEP A/Y=112. REMOVED DAMAGED AREA FABRICATED AND INSTALLE D DOUBLER IAW SRM 51 70 10. 2 L 7 2 4F RT A16WE 20090107 NM 2009 1 7 ASAA0944149 1 20081214 A 5753 6546430167 DOUBLER BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU MIDFLAP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 LT INBD MID FLAP LOWER SURFACE PREVIOUS REPAIR DOUBLER PUNCTURED. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER INS TALLED IAW SRM 51 70 10. 2 L 7 2 4F 4 F RT A16WE E21EU 20090107 NM 2009 1 7 ASAA0944150 1 20081229 A 5753 6546430167 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FOREFLAP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 LT INBD FORE FLAP LOWER SURFACE PUNCTURED. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER INSTALLED IAW SRM 51 70 10 . 2 L 7 2 4F 4 F RT A16WE E21EU 20090107 NM 2009 1 7 ASAA0944152 1 20081213 A 5512 6573783 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 RT HORIZ STAB AT STA 92.7 HAS 2 DENTS ON THE LEADING EDGE. REMOVED PREVIOUS REPAIR FABRICATED FILLER AND DOUBLER INSTALL ED IAW SRM 55 10 01. 2 L 7 2 4F 4 F RT A16WE E21EU 20090107 NM 2009 1 7 ASAA0944153 1 20081213 A 5512 657378336 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU HORIZ STAB DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 RT HORIZ STAB AT STA101 HAS A DENTS ON THE LEADING EDGE. REMOVED PREVIOUS REPAIR FABRICATED FILLER AND DOUBLER INSTALLED IAW SRM 55 10 01. 2 L 7 2 4F 4 F RT A16WE E21EU 20090107 NM 2009 1 7 ASAA0944151 1 20081217 A 5200 5007945279 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 LT DOOR UPPER AFT CORNER CURLED BACK. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER INSTALLED IAW SRM 52-00-01. 2 L 7 2 4F 4 F RT A16WE E21EU 20090107 EU 2009 1 7 USAA2009010690042 1 20081226 A 3320 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN MALFUNCTIONED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 620AW 052 LOG PAGE 8316197 - FLT 231 PHX-DTW - ELECTRICAL SMELL - FLIGHT ATTENDANT REPORTED ELECTRICAL SMELL BETWEEN ROWS 3 AND 4 AIRCRAFT LEFT. READING LIGHTS AT ROW 3 WOULD NOT TURN OFF. HOWEVER WHEN ENGINES WERE SHUT DOWN AND ELECTRICAL POWER RE MOVED, LIGHTS WENT OUT. MX R&R THE POWER SUPPLY AND CONNECTOR DUE TO EXCESSIVE HEAT DAMAGE. 2 L 7 2 4F RT A28NM 20090108 EA 2009 1 8 DATA200800010 2 20081219 A 7200 PT6A45R ENGINE STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA HARTZL HCB5M HCB5MP3 GL LEFT SURGES E DATA F A ACTIVATE FIRE EXT. UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 GL 13 336MV 16883 2641 SH3018 PCE84060 EVA2279 PILOT DECLARED A LT ENGINE FIRE WITH NO FIRE SYS ALARM DURING INITIAL CLIMB. FIRE BOTTLES DISCHARGED. FIRE EXTINGUISHED BY ITSELF WHEN ON APPROACH. NO SIGN OF FIRE DAMAGE IN OR AROUND ENGINE. SUSPECT COMPRESSOR SURGE NOTED BY VISIBLE FLAMES FROM EXHAUST STACKS. 2 H 7 2 4T 4 T A41EU E4EA 6 C P44GL 20090108 EA 2009 1 8 SWIA200820746 1 20081225 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 936SW 7726 FLT 6018 - EMERGENCY LIGHT OVER ROW 10 INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 SWIA200820747 1 20081227 A 5210 HANDLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR BINDING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 903SW 7425 FLT 5827 - MAIN DOOR OUTER HANDLE DIFFICULT TO STOW AND OPERATES ABNORMAL. REPLACED PAX DOOR HANDLE. 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 SWIA200820748 1 20081223 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 960SW 7853 FLT 5984 - 3RD AFT OVERHEAD EMERGENCY EXIT LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090108 NM 2009 1 8 QXEA2008123101271 1 20081226 A 3230 LANDING GEAR BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 19 406QX 4048 SEA - SELECTED GEAR UP, NOTHING HAPPENED, GOT 3 RED UNSAFE LIGHTS AND HANDLE AND 3 GEAR DOWN LIGHTS (GREEN), RAN ALTERNA TE EXTENSION EMERGENCY CHECKLIST. NOSE WHEEL CENTERING PROX SENSOR WAS RIGGED AND ACFT WAS JACKED PER TASK CARD THE LAN DING GEAR WAS RETRACTED AND EXTENDED THROUGH FOUR CYCLES WITH NO DEFECTS NOTED OR FAULTS LOGGED IN PSEU A/C OK FOR CONTI NUED SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20090108 NM 2009 1 8 QXEA2008123101272 1 20081227 A 3080 4100S01907 DETECTOR BOMBDR DHC8 DHC8402 1390042 NM ZONE 200 FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 19 401QX 2177 4031 SEA - FLIGHT 2218 (BOI-LWS) DIVERTED TO SEA FOR MAINTENANCE DUE TO "ICE DETECT FAIL" CAUTION LIGHT ILLUMINATED IN CRUISE AFTER EXITING ICING CONDITIONS. REMOVED AND REPLACED NR 2 ICE DETECTOR PROBE IAW AMM TASKS 30-80-01-000-801 AND 30-80- 00-400-801. PERFORMED OPERATIONAL TEST OF THE ICE DETECTION SYSTEM IAW 30-80-00-710-801. OPS TEST CHECKED GOOD. NO OT HER DEFECTS NOTED. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20090108 EU 2009 1 8 FDEA200811144882 1 20081114 A 3260 GA558614 HOUSING AIRBUS 310 A310203 3930313 EU SWITCH BROKEN A FDEA O OTHER N FALSE WARNING LD LANDING 1 CE 21 411FE 7927 7318 359 ON ARRIVAL INTO MEM, THE NOSE GEAR INDICATED UNSAFE ON BOTH SYSTEM 1 AND 2. COMPLIED WITH QRH AND USED THE MLG GRAVITY EXTEND CHECKLIST. WHEN THAT WAS COMPLETED THE UNSAFE WARNING REMAINED. THEN WENT DOWNSTAIRS TO VISUALLY CHECK. IT IND ICATED DOWN AND LOCKED SO WE LANDED WITH THAT INDICATION FOUND SWITCH 40 GB HOUSING BROKEN. REMOVED REPLACED HOUSING AN D SWITCH IAW MM 32-00-00-4. NEEDS GEAR SWING AND OPS CHECK. COMPLIED WITH NOSE GEAR SWING IAW MM 32-31-00-5. ALL INDI CATIONS NORMAL ON FLIGHT DECK. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 20090108 SO 2009 1 8 SWIA200820749 1 20081207 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS FRACTURED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 232SW 120306 FLT 7816 - LIGHT "EXIT" SIGN NEXT TO MAIN DOOR FIXTURE IS BROKEN. REPLACED MAIN DOOR LIGHTED "EXIT" SIGN. 2 L 7 2 4T RT A31SO 20090108 NM 2009 1 8 DHLA2008743525 1 20081109 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 D-CHECK, WO NR 5350 NR 5350-2-98, UPPER FUSELAGE PAX CABIN AT BS 700 STR 16R AND 17R FRAME WITH DENT. REPAIRED FUSELAGE FRAME SECTION AT BS 700, BETWEEN STR 16R AND STR 17R DUE TO DENT IAW SRM 51-40-3 FIG.1. 2 L 7 3 4F A3WE 20090108 EA 2009 1 8 SWIA200820763 1 20081216 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 979SW 7954 DURING C-CHECK, FS 280 RBL 11-13 LOWER FLOORBEAM FLANGE CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090108 WP 2009 1 8 FDEA200812185214 1 20081218 A 5320 NCA624627 WEB DOUG DC10 DC1030F 3023504 WP ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 317FE 46835 DURING INSPECTION NLG FOUND CRACK ON VERTICAL WEB. 2 L 7 3 4F RT A22WE 20090108 WP 2009 1 8 FDEA200812185215 1 20081218 A 5320 NCA624625 WEB DOUG DC10 DC1030F 3023504 WP NLG WW CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 317FE 46835 DURING INSPECTION NLG WW FOUND CRACK ON VERTICAL WEB. 2 L 7 3 4F RT A22WE 20090107 NM 2009 1 7 UALA2008122907027 1 20081228 A 3350 767 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 660UA 27115 RT EXTERIOR EMERG LIGHT INOP RT SLIDE LIGHT. RELAMPED, OPS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20090107 NM 2009 1 7 UALA2008122907030 1 20081229 A 3350 10681 POWERPACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT SEAT 4A INOP. REPLACED PWR PACK OPS CK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008122907036 1 20081228 A 2810 300710303 RELAY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUEL SYSTEM FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 651UA 25389 UNABLE TO FUEL ACFT, FUELING VALVES (ALL) DO NOT OPEN AUTOMATICALLY. RPL RELAYS K357 FUELING PWR TRANS ON THE P36 AND K181 OVERFILL CONT ON THE P36. ALSO RPL THE ASSY FUEL LEVEL SENSOR CARD. RPL RELAY K180. REPLACED FUEL QTY PROCESSOR. F UELER WAS ABLE TO PRESSURE FUEL ALL 3 TANKS. 2 L 7 2 4F 4 F RT A1NM E24NE 20090107 NM 2009 1 7 UALA2008123007042 1 20081229 A 3350 78671 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT LIGHT INOP AT SEAT 57 RT. RELAMPED, CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 CE 2009 1 7 DJFA2008087 1 20081224 A 2150 73838433 ACM CESSNA 750 750 2076810 CE FORWARD SMOKE E DJFA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 23 709LX 7500145 ON GROUND CREW REPORTED SMOKE IN THE COCKPIT WHEN MAX COOL SELECTED IN COCKPIT. MX FOUND THE FWD ACM FAILED; THE ACM WA S REPLACED. 2 L 7 2 4J RT T00007WI 20090107 NM 2009 1 7 UALA2008123007048 1 20081228 A 2710 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT AILERON LEAKING A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 548UA 25396 RT AILERON HAS EXCESSIVE FLUID RUNNING OUT OF IT. REPLACED RT INBD AILERON PCA. OPS AND LEAK CHKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20090107 NM 2009 1 7 UALA2008123007050 1 20081226 A 2432 893003 CHARGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU BATTERY FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 656UA 25394 APU SHUTS DOWN WITH ELEC OR PNEUMATIC LOAD. REPLACED BATTERY CHARGER AS PER SERVICE TIP. CLEARED APU CONTROLLER OF ALL FAULTS. RAN ENG 3 TIMES TO PUT LOAD ON APU, AT MAX HAD 40 P.S.I. ALSO SERVICED APU OIL. 2 L 7 2 4F 4 F RT A1NM E24NE 20090107 EU 2009 1 7 UALA2008123007051 1 20081226 A 5210 SKIN AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE L2 DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 406UA 454 DOOR 2L HAS DENT 16.0" AFT OF FWD EDGE AND 13.5" FROM BOTTOM. EVALUATED DENT & FOUND OUT OF LIMITS. CUT OUT DAMAGE. F ABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR. RESTORED THE PROTECTIVE COATING. 2 L 7 2 4F 4 F RT A28NM E40NE 20090107 NM 2009 1 7 UALA2008123007052 1 20081229 A 3610 79027013 SHUTOFF VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE BLEED AIR SYS FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 668UA 30024 LT ENG BLEED LGT & L ENG HPSOV EICAS MSG, ENG BLEED SW OFF, ANTI-ICE SW OFF, & ENG SHUTDOWN. REPLACED HPSOV. 2 L 7 2 4F 4 F RT A1NM E24NE 20090107 NE 2009 1 7 UALA2008123107053 2 20081230 A 7321 7911004111 EEC BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE FAULTY A UALA K NONE J WARNING INDICATION LD LANDING 1 WP 29 654UA 25392 LT ENG CONTROL EICAS MSG DISPLAYED ON LANDING. REPLACED NR 1 ENG EEC. 2 L 7 2 4F 4 F RT A1NM E24NE 20090107 NM 2009 1 7 UALA2008123107054 1 20081231 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY LIGHTS (2) ON AFT GALLEY WALL LT SIDE INOP. REPLACED FEEDER. OP CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 SO 2009 1 7 C2XA08SH164 1 20081219 A 7160 14575001401 INLET EMB 145 EMB145LR 3260212 SO ZONE 400 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 48901 145501 VARIOUS BOLTHOLES ON THE LT ENG AIR INLET CORRODED. REPAIRED BOLT HOLE ON LT ENG AIR INLET IAW EC 5420-01179. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20090107 2009 1 7 CLCA-1008-2 4 20081026 A 2565 SLIDE DOUG DC10 DC1030F 3023504 WP R1 DOOR UNWANTED DEPLOY A CLCA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 29 614GC 46931 1R EMERGENCY SLIDE ACCIDENTALLY BLOWN. 1R EMERGENCY SLIDE ORDERED AND REPLACED. 2 L 7 3 4F RT A22WE 20090107 NM 2009 1 7 USAA2009010290009 1 20081221 A 5754 65C26601197A SKIN BOEING 737 7374B7 138449C NM LE SLAT DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT Q5 MAJOR REPAIR NR 03C30257009/005 NR 1 SLAT DISBONDED ON UPPER SURFACE AT WEDGE AREA. REPAIRED NR 1 SLAT IAW B737 SRM 57-43-02 & 51-70-10. 2 L 7 2 4F RT A16WE 20081230 WP 2008 12 30 UPS08854220 1 20081117 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:SV EXTERNAL REPAIR AT BS 70 AND L34L TO L34R DOES NOT MEET SRM CRITERIA REF SURVEY SEQ 729-F1-06. REPAI RED IAW DC8-SRM 53-02-05 FIG 8C2 SH 1-5. 2 L 7 4 4F RT 4A25 20081230 WP 2008 12 30 UPS08854221 1 20081214 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:SV EVAL REPAIR DOUBLER INSTALLED AT STATION 161 UPPER SURFACE OF FUSELAGE SKIN JUST AFT OF NOSE RADOME S URVEY SEQUENCE 894-F1-43. REPAIRED IAW DC8 SRM 53-02-0 FIG 001 D SHEET 3. 2 L 7 4 4F RT 4A25 20081230 WP 2008 12 30 UPS08854222 1 20081118 A 5330 5779934 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:SV REPAIR AT BS 400 TO 420 LONG 36 TO 35R NEEDS ENGINEER APPROVAL FOR PRESSURIZED AREA. INSTALLED DOUBL ER AND FINGER DOUBLERS IAW DC8 SRM 53-2-1 FIG 7 TR 53-2 03 SHT 3 AND 4. 2 L 7 4 4F RT 4A25 20081230 WP 2008 12 30 UPS08854228 1 20081117 A 5230 STRUCTURE DOUG DC8 DC871F 302199D WP CARGO DOOR MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:SV REPAIR ON A PIT DOOR DOES NOT MEET SRM SURVEY SEQ 729-F1-59. REPLACED REPAIR IAW DC8 SRM 52-2-0 FIG 4 REV 78. 2 L 7 4 4F RT 4A25 20081230 NM 2008 12 30 HNAA2008121000345 1 20081214 A 3350 6013211X BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 940HA 30401 390 156 LEFT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT ROW 3AC LOCATION IN ACCORDANCE WITH 33-51-00. 2 H 7 2 4T RT A13NM 20081230 EA 2008 12 30 COMA2008122970008 1 20081229 A 5320 INTERCOSTAL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 371CA 10082 INTERCOSTAL CHAFED FROM RIGHT ACM WATER LINE. BLENDED OUT DAMAGED AREA AND PERFORMED REPAIR IN ACCORDANCE WITH EA 70-53 61-02470. 2 L 7 2 4F RT A21EA 20081230 EA 2008 12 30 COMA2008122850052 1 20081228 A 5330 SKIN CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 27 591CA 7079 RT FUSELAGE SKIN IS CRACKED AT FS 235.00 IN THE RT AFT RADIUS OF THE NOSE LANDING GEAR CUTOUT. INSTALLED PERMANENT REP AIR PARTS PER BOMBARDIER AEROSPACE REO 601R-53-11-048 REV (B). 2 L 7 2 4F RT A21EA 20081230 EA 2008 12 30 COMA2008122750047 1 20081227 A 3030 CONTROLLER CNDAIR CL600 CL6002B19 1900309 EA ANTI-ICE SYSTEM MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 443CA 7539 EN ROUTE JFK-YUL RECEIVED MULTIPLE ANTI-ICE CAUTION MESSAGES, FLIGHT RETURNED TO JFK. PERFORMED RESET OF THE AIR DATA S YSTEM (ADS) CONTROLLER NR 2. 2 L 7 2 4F RT A21EA 20081230 SO 2008 12 30 RAIA2008122900003 1 20081226 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145EP 3260221 SO CABIN DISCHARGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 807HK 145119 DURING THE PRE FLIGHT INSPECTION, IT WAS DISCOVERED THAT THE EMERGENCY LIGHTS IN THE BACK HALF OF THE AIRCRAFT WERE INOP ERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY. LIGHTS OPS CHECKED GOOD. 2 L 7 2 4F RT T00011AT 20081230 SO 2008 12 30 RAIA2008122900001 1 20081223 A 3610 THERMOSTAT EMB 145 EMB145LR 3260212 SO BLEED AIR SYS INOPERATIVE A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 838HK 145321 CREW RECEIVED A BLEED 2 OVERTEMP MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 2 THERMOSTAT. SYSTEM OP S CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20081230 EU 2008 12 30 USAA2008122392301 1 20081218 A 3397 WIRE HARNESS AIRBUS 330 A330323 3940030 EU CABIN DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AY 375 BFM - C2 - EEL - NR 6056406 - EMERGENCY EXIT LIGHTING WIRE HARNESS AT SEAT 16HG DAMAGED. REPLACED EMERGENCY EXIT LIGHTI NG WIRE HARNESS AT SEAT 16HG IAW A320 AMM 33-51-12. 2 L 7 2 4F RT A46NM 20081230 NM 2008 12 30 NOCA09108 1 20081216 A 2621 FIRE BOTTLE BOEING 767 76736N 1385152 NM APU DISCHARGED A NOCA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 15 768NA 29898 APU FIRE EXTINGUISHING SYSTEM INOP. DISCHARGED THE BOTTLE INADVERTENTLY BY THE GROUND CREW FROM THE NOSE GEAR POSITION. ITEM REMAINS OPEN. 2 L 7 2 4F RT A1NM 20081230 NM 2008 12 30 NOCA08808 1 20081215 A 3350 20121 CHARGER BOEING 757 75728A 1384976 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 FLOOR EMERGENCY LIGHTS AT SEATS 7 AND 8 ABC ARE INOP. REPLACED BATTERY AND CHARGER AS PER MM 33-51-07, OPS CHECK OK. 2 L 7 2 4F RT A2NM 20081231 WP 2008 12 31 AALA200802475A 1 20081108 A 3242 BRAKE ASSY DOUG DC9 DC982 3022082 WP MLG OVERHEATED A AALA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SW 21 559AA 53089 DFW - DURING TAKEOFF ROLL BRAKE TEMPERATURE LIGHT FLASHED AT 100 KNOTS FOLLOWED BY A STEADY LIGHT AND TEMPERATURE HIGH I NDICATION. ABORTED TAKEOFF AT 110 KNOTS. AIRCRAFT TOWED TO HANGAR FOR EVALUATION. REPLACED NUMBER ONE MAIN LANDING GE AR BRAKE ASSEMBLY AND TIRE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081231 NM 2008 12 31 AALA200802491A 1 20081108 A 2612 644501 LOGIC CARD BOEING 767 767323 1385205 NM FIRE DETECTION FAULTED A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 368AA 25195 REC INFLIGHT - NUMBER ONE ENGINE FIRE DETECTION LOOP ONE FAULTED WITH LEFT ENGINE LOOP TWO PLACARDED. RETURNED TO REC A ND LANDED WITHOUT INCIDENT. REPLACED FIRE DETECTION SYSTEM LOGIC CARD AND TIGHTENED LOOSE LEFT ENGINE LOOP ONE LOWER AF T CONNECTOR AND REPLACED FAULTY LT ENGINE LOOP UPPER AFT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081231 EU 2008 12 31 AALA200802499A 1 20081110 A 3230 UPLOCK ACTUATOR AIRBUS 300 A300B4605R 3930308 EU MLG FAULTED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 14077 612 JFK INFLIGHT - AFTER GEAR RETRACTION NOSE GEAR DOOR INDICATION ILLUMINATED FOR SYSTEM ONE AND TWO. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED LEFT NOSE GEAR DOOR UPLOCK ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20081231 NM 2008 12 31 AALA200802495A 1 20081010 A 3350 PBS73 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 607AM 27058 MCO INFLIGHT - EMERGENCY FLOOR LIGHTING FLICKERED ON AND OFF DURING FLIGHT. REPLACED BATTERY PACK AT STATION 1095. SYS TEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 WP 2008 12 31 AALA200802497A 1 20081109 A 2560 P4010021 BATTERY DOUG DC9 DC983 3022083 WP FLASHLIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 970TW 53620 SFO - EMERGENCY FLASHLIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY FOR EMERGENCY FLASHLIGHT AT LEFT NUBME R ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081231 SO 2008 12 31 C2XA08CL137 1 20081226 A 2740 3621001013 CONTROL UNIT EMB 145 EMB145LR 3260212 SO HORIZ STAB FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 14916 14092 145415 CLE FLT 2345 - THE CREW REPORTED A PITCH TRIM MAIN INOP MESSAGE IN FLIGHT. THE CREW RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE HORIZONTAL STAB CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20081231 SO 2008 12 31 C2XA08IA261 1 20081221 A 2120 UNKNOWN EMB 145 EMB145EP 3260221 SO CABIN ODOR A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 27 14945 145049 FLIGHT 2195 MOB - IAH. THE CREW REPORTED A BURNING PLASTIC SMELL AT PASSENGER SEAT ROWS 9 THROUGH 11. THE AIRCRAFT LAN DED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE PASSENGER CABIN. ALL CONDITIONS WERE FOUND TO BE NORMAL AND THERE WERE NOT ANY INDICATIONS OF BURNING, SMOKE OR COMPONENT OVERHEATING. 2 L 7 2 4F RT T00011AT 20081231 SO 2008 12 31 C2XA08CL136 1 20081224 A 3030 MS332020 CIRCUIT BREAKER EMB 145 EMB145LR 3260212 SO COCKPIT BURNED A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 27 14977 145175 CLE FLT 2031 - THE CREW REPORTED A HOT ELECTRONICS’ SMELL COMING FROM THE CLOSET AREA. MAINTENANCE INSPECTED AND REPLAC ED CB0059. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20081231 SO 2008 12 31 C2XA08IA262 1 20081218 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO CABIN FAULTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 12921 145354 DURING SCHEDULED MAINTENANCE THE FORWARD OVERWING EXIT LOCATOR SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AN D REPLACED THE NR 6 INVERTER, OPERATIONALLY TESTED THE LIGHTING SYSTEM AND CLEARED THE DISCREPANCY. 2 L 7 2 4T RT T00011AT 20081231 NM 2008 12 31 AALA200802510A 1 20081106 A 5330 SKIN BOEING 767 767323 1385205 NM BS 440 S36 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 366AA 25193 AFW - FUSELAGE SKIN AT STATION 440 AT STRINGER 36 JUST AFT OF THE SECTION 41/43 BUTT SPLICE AND ABOVE A SKIN LAP JOINT H AS CORROSION BLENDED. MATERIAL REMAINING IS BEYOND SRM LIMITS. REPAIRED IN ACCORDANCE WITH MRB 767 3337. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 AALA200802514A 1 20081104 A 5330 146T3261 SKIN BOEING 767 767323 1385205 NM BS 1087 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 366AA 25193 AFW - CORROSION WAS FOUND AT THREE LOCATIONS JUST AFT OF STATION 1087 ON THE INTERIOR SURFACE OF FUSELAGE SKIN. BLENDIN G IS BEYOND SRM LIMITS. REPAIRED IN ACCORDANCE WITH MRB 767-3333. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 AALA200802521A 1 20081113 A 3350 0201720101 LIGHT BOEING 777 777223 1385213 NM SEAT 12D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 797AN 30012 JFK - SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 12D INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 12D. SYSTEM GROUND CHECKE D NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 CALA2008122301165 1 20081223 A 5311 6546555 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24633 27901 FRAME CRACKED AT STATION 867 BETWEEN STRINGER 8 AND 9 LEFT. REPAIRED CRACKED FRAME PER EA 5310-04498, OP 2. 2 L 7 2 4F RT A16WE 20081231 NM 2008 12 31 CALA2008121901154 1 20081219 A 5512 182A4002 SKIN BOEING 737 737924 13848A1 NM HORIZONTAL STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 79402 30119 LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 129.5, APPROXIMATELY 18 INCHES AFT OF FRONT SPAR INBOARD SIDE O F RIB. INSTALLED INTERIM REPAIR ON LEFT HORIZONTAL STAB LOWER INBOARD SPAR SKIN STATION 129.5. REF ECRA 5510-01955, LO G 9702589 FOR DIP (55-DIP) CNTL NR 91773 WHICH READS: ACCOMPLISH A PERMANENT REPAIR WITHIN 24 MONTHS FROM 17DEC08 PER E CRA 5510-01955 PART3, PLANNING TO CONTACT ENGINEERING AFTER 17OCT10 BUT BEFORE 17NOV10 FOR A PERMANENT REPAIR. 2 L 7 2 4F RT A16WE 20081231 WP 2008 12 31 AALA200802524A 1 20081113 A 1100 PLACARD DOUG DC9 DC982 3022082 WP SEAT 21A MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 475AA 49650 DFW - EMERGENCY LIGHT PLACARD IN FRONT OF SEAT 21A MISSING. REPLACED PLACARD IN FRONT OF SEAT 21A. SYSTEM GROUND CHECK ED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081231 2008 12 31 AALA200802525A 4 20081115 A 3417 ADC DOUG DC9 DC983 3022083 WP NR 1 FAILED A AALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SW 21 9302B 49528 TUL INFLIGHT ORD TO SJD - NUMBER ONE AIR DATA COMPUTER FAILED WITH MULTIPLE CAPTAINS INSTRUMENTS INOPERATIVE. LANDED TU L WITHOUT INCIDENT. REPLACED NUMBER 1 AIR DATA COMPUTER. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081231 WP 2008 12 31 AALA200802442A 1 20081030 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DISLODGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 16545 53027 LGA - EMERGENCY LIGHTS AT AFT LAVATORY INOPERATIVE. REPOSITIONED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20081231 NM 2008 12 31 AALA200802437A 1 20081030 A 3510 NUT BOEING 757 757223 1384957 NM OXYGEN MASK LOOSE A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 656AA 24614 MCI INFLIGHT SFO TO STL - CREW REPORTED OXYGEN BOTTLE PRESSURE LOW. LANDED MCI WITHOUT INCIDENT. FOUND CAPTAINS MASK C OMPARTMENT LEAKING. TIGHTEN B NUT AT CAPTAINS MASK COMPARTMENT. REPLACED CREW OXYGEN BOTTLE. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 2008 12 31 AALA200802493A 4 20081109 A 2220 285T0015117MODD MODULE BOEING 757 757223 1384957 NM STAB TRIM FAULTED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 187AN 32381 LAX INFLIGHT - MACH SPEED TRIM INDICATIONS AT 16000 FEET. AUTOPILOT WAS OFF AIRSPEED ABOUT 270 KNOTS INDICATED AIR SPE ED. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. REPLACED RIGHT STABILIZER TRIM ASYMMETRY MODULE AND RIGHT STABILIZER TRIM CONTROL MODULE BRAKE PRESSURE SWITCH (MPN 10605525). SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802439A 1 20081030 A 3350 6011779 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9413T 53188 SFO - AFT EMERGENCY LIGHTS ABOVE LEFT AND RIGHT AFT OVERWING ESCAPE HATCH INOPERATIVE. REPLACED BATTERY PACK FOR AFT EM ERGENCY LIGHTS OVERHEAD RIGHT AND LEFT AFT OVERWING DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT 20081231 WP 2008 12 31 AALA200802440A 1 20081030 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 439AA 49457 SFO - EMERGENCY LIGHT AT SEAT 18D INOPERATIVE. REPINNED CONNECTOR AT SEAT 18D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20081231 NM 2008 12 31 AALA200802462A 1 20081103 A 3350 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 681AA 25338 DFW - EMERGENCY LIGHT AT SEAT 1E INOPERATIVE. SECURED CONNECTOR AT SEAT 1E. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 RYNA2008121800045 1 20081216 A 2751 WARNING SYSTEM BOEING 757 7572G5 1384912 NM TE FLAP FALSE ACTIVATION A RYNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 151GX 24451 AFTER TAKEOFF FLIGHT CREW REPORTED A TRAILING EDGE FLAP DISAGREEMENT MESSAGE. AIRCRAFT RETURNED TO RFD MAINTENANCE TROU BLESHOT PERFORMED OPERATIONAL CHECKS PER AMM 27-51-00, NO DEFECTS NOTED. AIRCRAFT DEICED AND DISPATCHED. SYSTEM FAULT HAS NOT REPEATED IN FOUR FLIGHT LEGS. 2 L 7 2 4F RT A2NM 20081231 SO 2008 12 31 C2XA08IA269 1 20081228 A 2120 BWT1268143345A2A MUFFLER EMB 145 EMB145LR 3260212 SO AC PACK LOOSE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15973 145159 IAH - FLIGHT 2434, THE CREW REPORTED THAT THE PACK 2 VALVE CLOSED IN FLIGHT, AND WERE UNABLE TO RESET. THE AIRCRAFT RE TURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-SECURED THE PACK 2 DISTRIBUTI ON MUFFLER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081231 2008 12 31 C2XA08IA272 4 20081229 A 3140 C16221GD04 COMPUTER EMB 145 EMB145XR 3260214 SO ISIS MALFUNCTIONED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 27 16112 5416 5416 145660 IAH - FLIGHT 2133, THE CREW REPORTED THAT THE ISIS ALTITUDE AND SPEED BLANKED OUT DURING CLIMB. THE AIRCRAFT RETURNED T O IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE ISIS COMPUTER, OPERATIONALLY TESTED WITHOU T DEFECT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081231 NM 2008 12 31 AALA200802494A 1 20081109 A 7330 QA07995 SWITCH BOEING 737 737823 13844CB NM FUEL FILTER BPAS FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 951AA 29538 MSP INFLIGHT YYZ TO LAX - LEFT FUEL FILTER BYPASS INDICATION ILLUMINATED IN FLIGHT. LANDED MSP WITHOUT INCIDENT. REPLA CED LEFT FUEL FILTER AND FUEL DIFFERENTIAL PRESSURE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A16WE 20081231 SO 2008 12 31 C2XA08IA273 1 20081223 A 2611 FDS765A2 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY MALFUNCTIONED A C2XA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 27 48901 4361 4361 145501 IAH - FLIGHT 2406, THE CREW REPORTED A LAV SMOKE INDICATION ON T/O FROM DAL. THE SYSTEM WAS RESET SUCCESSFULLY PER THE QRH, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR, OPERATIO NALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081231 NE 2008 12 31 AALA200802527A 2 20081117 A 7230 FAN BLADE AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE NR 2 ENGINE BIRD INGESTION A AALA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 21 80058 6244 466 690261 INFLIGHT - AT ROTATION CREW REPORTED LOUD BANG AND VIBRATION FROM NUMBER TWO ENGINE DUE TO BIRDSTRIKE. RETURNED TO SJU AND LANDED WITHOUT INCIDENT. REPLACED NUMBER TWO ENGINE ON 21NOV AT JFK DUE TO BLADE AND FAN CASE DAMAGE. SYSTEM GROUN D CHECKED NORMAL OPERATION. 2 L 7 2 4F 4 F RT A35EU E13NE 20081231 SO 2008 12 31 C2XA08IA271 1 20081229 A 2612 3601133500230C90 FIRE LOOP EMB 145 EMB145LR 3260212 SO NR 1 ENGINE CHAFED A C2XA O OTHER J WARNING INDICATION UK UNKNOWN 1 SW 27 16541 18490 18490 145542 IAH - FLIGHT 2386, THE CREW REPORTED A NUMBER ONE ENGINE FIRE DETECTOR FAIL IN FLIGHT. THE AIRCRAFT LANDED AT IAH WITHO UT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE FIRE LOOP. OPERATIONAL TESTS WERE SATISFACTORY , AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081231 NM 2008 12 31 DLM88081704 1 20081119 A 5330 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 972DL 53215 CRACK ON FUSELAGE SKIN AT STY Y=1437, LONGERON 2 RT. FUSELAGE SKIN WAS REPAIRED PER SRM 53-04D FIG 27. 2 L 7 2 4F RT A6WE 20081231 NM 2008 12 31 DLM88081705 1 20081204 A 5330 5911401211 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 972DL 53215 FUSELAGE SKIN AT FS 125, BETWEEN L-29L AND L-30 WAS FOUND WITH A LIGHTNING STRIKE BEYOND SRM 53-04 FIG 38 LIMITS. THE D AMAGE WAS CUT OUT AND AN EXTERNAL REPAIR DOUBLER INSTALLED. REPAIR IS TIME-LIMITED FOR DTA PURPOSES. 2 L 7 2 4F RT A6WE 20081231 NM 2008 12 31 AALA200802529A 1 20081118 A 2780 PSEU BOEING 767 767323 1385205 NM SLATS FAULTED A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 366AA 25193 INFLIGHT - CREW REPORTED INTERMITTENT SLAT ASYMMETRY INDICATION ON FINAL APPROACH. LANDED BOS WITHOUT INCIDENT. FOUND PROXIMITY SENSOR ELECTRONIC UNIT FAULT ON CARD 13 AND FAULT ON FLAP HANDLE. ADJUSTED FLAP HANDLE AND REPLACED PROXIMIT Y SENSOR ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 AALA200802536A 1 20081120 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 781AN 29586 DFW - EMERGENCY LIGHT AT SEAT 30G MISSING LENS. REPLACED LENS AT SEAT 30G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 DL76L081739 1 20081215 A 2120 UNKNOWN BOEING 767 767332 1382001 NM CABIN ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 187DN 27582 070908 HI FLOW INHIBIT MESSAGE ON EICAS DURING DESCENT. PAX REPORTED BURNING RUBBER SMELL SHORT TIME LATER AROUND ROW 20-22. T/S PER FIM 21-51-00-101. NO FAULTS INDICATED. SYS OPS OK. RAN PACKS. RECRIC FANS. READING LIGHTS AND ENT SYS. NO ODORS DETECTED. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 DL757081769 1 20081218 A 2121 COOLING FAN BOEING 757 757232 1384965 NM E&E BAY SEIZED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 640DL 23994 BURNING SMELL IN COCKPIT AT CRUISE. RAN CHECKLIST, DIVERTED TO SJU. MTC FOUND THE FWD EQUIP COOLING SUPPLY FAN NR 1 SE IZED AND CAUSING THE SMELL. REPLACED THE FAN PER THE MM, ALL CHECKS OK. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 AALA200802539A 1 20081120 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 781AN 29586 DFW - EMERGENCY LIGHT AT OVERHEAD L3 DOOR INOPERATIVE. REPLACED LAMP AT OVERHEAD L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 DLM88081732 1 20081114 A 5320 BEAM DOUG MD88 MD88 3023688 NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 972DL 53215 EXFOLIATION CORROSION ON LWR BEAM OF MID CARGO COMPARTMENT LWR DOOR JAMB BETWEEN STA Y=636-693. CORROSION REMOVED IAW S RM 51-10-3, FOUND OUT OF LIMITS. INSTALLED NEW LOWER BEAM IAW SRM 51-30-1, -2, AND -5. 2 L 7 2 4F RT A6WE 20081231 NM 2008 12 31 AALA200802543A 1 20081120 A 3397 CONNECTOR BOEING 777 777223 1385213 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 781AN 29586 DFW - EMERGENCY LIGHTS AT SEAT ROWS 41G TO 45G FAILED TEST. SECECURED CONNECTOR AT SEAT ROW 40G FOR EMERGENCY LIGHTS AT SEAT ROWS 41G TO 45G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20081231 NM 2008 12 31 DL76L081710 1 20081210 A 2730 162000105 COMPUTER BOEING 767 767332 1382001 NM ELEVATOR MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 173DN 24800 AFTER PUSHBACK GOT STATUS MSG ELEV FEEL, IT CLEARED AFTER STARTING BOTH ENGINES READ NEEDED HYD PRESSURE IN MDM. AFTER A COUPLE OF MINUTES IT RETURNED AND WOULD NOT CLEAR. MSG FIRST APPEARED AFTER STARTING FIRST ENGINE. REMOVED AND INSTA LLED ELEV FEEL COMPUTER PER AMM. LEAK TEST AND GROUND TEST OK. 2 L 7 2 4F RT A1NM 20081231 NM 2008 12 31 AALA200802490A 1 20081108 A 3350 CONNECTOR BOEING 757 757223 1384957 NM EMERGENCY LIGHT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 181AN 29591 DFW - EMERGENCY LIGHT AT SEAT ROW 35DEF INOPERATIVE. SECURED LOOSE CONNECTOR AT SEAT ROW 35DEF SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20081231 NM 2008 12 31 DL764081711 1 20081209 A 3620 WARNING SYSTEM BOEING 767 767432ER 1385134 NM BLEEED AIR SYS MALFUNCTIONED A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 837MH 29710 RT PACK INOP AFTER START OF SECOND ENG. RAN QRH TO NO AVAIL. SEVERAL MINUTES LATER EICAS MSG R BLEED HPSOV CAME UP. R ESET CTC C/BS AC AND DC PACKS OP CK NORMAL. ALSO RESET ASCUTU FAULTS SHOWN WERE R HPSOV 36-10370 FAULT NR. PERFORMED R T HPSOV TEST FAULTS CLEARED. 2 L 7 2 4F RT A1NM 20081231 EU 2008 12 31 AALA200802492A 1 20081109 A 3260 DSB11021 SENSOR AIRBUS 300 A300B4605R 3930308 EU NR 1 MLG FAULTED A AALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 40064 507 INFLIGHT - CAPTAIN PITOT OVERHEAT, CAPTAIN TOTAL AIR TEMPERATURE FAULT AND NR 1 PRESSURE REGULATOR OVERHEAT INDICATIONS. RETURNED AND LANDED WITHOUT INCIDENT. REPLACED LT SYSTEM NR 1 MAIN LANDING GEAR PROXIMITY SENSOR. SYSTEM GROUND CHEC KED NORMAL OPERATION. 2 L 7 2 4F RT A35EU 20090105 EA 2009 1 5 SWIA200820716 1 20081121 A 5320 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 468CA 7649 C-CHECK, FLOOR SUPPORT CLIP AT FS 280 RBL9 INBOARD CRACKED. REPLACED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820725 1 20081230 A 5610 601R3303311 WINDOW CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 951SW 15 15 7795 FLT 6617 - CAPTIAN SIDE WINDOW CRACKED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820728 1 20081228 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 980SW 7955 EFLT 6242 - EMERGENCY LIGHT IN GALLEY INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820730 1 20081227 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 970SW 7881 FLT 6014 - OVERHEAD EMERGENCY DOME LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820731 1 20081226 A 3234 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A SWIA K NONE J WARNING INDICATION AP APPROACH 1 NM 07 472CA 378 378 7667 FLT 2641 - GEAR DISAGREE WARNING. REPLACED NLG SELECTOR VALVE PN 750006000 SN ON 0272T SN OFF 1032T. 2 L 7 2 4F RT A21EA 20090105 EA 2009 1 5 SWIA200820732 1 20081220 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 755SK 10220 FLT 6769 - EMERGENCY LIGHT ON CABIN CEILING INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 NM 2009 1 6 HALA2008122600902 1 20081226 A 7700 7302143 CIRCUIT CARD BOEING 767 7673CB 1385187 NM RT ENGINE MALFUNCTIONED A HALA O OTHER O OTHER NR NOT REPORTED 1 WP 13 592HA 33468 ETOPS SIGNIFICANT SYSTEM, RT ENG SPEED CARD DISPLAYED EICAS MSG R ENG EPR INDICATOR BLANKED LT ENG EPR INDICATOR BLANKED . LT ENG EPR INDICATOR CAME BACK. REMOVED AND REPLACED RT ENG SPEED CSRD PER AMM 77-12-01. SYSTEM CHECKS NORMAL. EPR L/R BACK TO NORMAL SPEED CARD MSG NO LONGER ON EICAS. 2 L 7 2 4F RT A1NM 20090106 NM 2009 1 6 K11A2009010272303 1 20080514 A 5313 STRINGER BOEING 727 7272H3 138368N NM FUSELAGE CORRODED A K11A K NONE O OTHER UK UNKNOWN 1 GL 23 723CK 20545 STRINGER CORROSION. 2 L 7 3 4F RT A3WE 20090106 NM 2009 1 6 FDEA200812015020 1 20081201 A 5320 AJC705070 STIFFENER DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 AFT FUSELAGE COMPARTMENT AFT PRESSURE BULKHEAD STATION 2007 AFT SURFACE QUANTITY 01 STIFFENER AT X = -15.250 FOUND CRA CKED APPROXIMATELY 0.5 INCH. EMPENNAGE, AFT FUSELAGE COMPARTMENT AFT PRESSURE BULKHEAD STATION 2007 AFT SURFACE STIFFEN ER AT X = -15.250 REPAIRED AS PER EA 1-5310-122645 PART 1. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090106 SO 2009 1 6 SWIA200820688 1 20081217 A 3260 DOWNLOCK SENSOR EMB 120 EMB120ER 3260203 SO MLG INOPERATIVE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 271YV 120271 FLT 5752 - GEAR DID NOT EXTEND WHEN COMMANDED. REPLACED RIGHT MLG DOWN LOCK SENSORS AND SWUNG GEAR. 2 L 7 2 4T RT A31SO 20090106 SO 2009 1 6 SWIA200820689 1 20081215 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA K NONE L NO TEST IN INSP/MAINT 1 NM 07 296SW 120325 FLT 7813 - AFT SECTION EMERGENCY LIGHTS INOP. OPS CHECKED GOOD. 2 L 7 2 4T RT A31SO 20090106 EA 2009 1 6 SWIA200820690 1 20081218 A 3350 LAMP CNDAIR CL600 CL6002D24 1390016 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 820SK 15108 FLT 4774 - NR 2 AND NR 6 EMERGENCY CEILING FLOODLIGHTS INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820691 1 20081215 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 604SK 10249 FLT 4687 - CABIN EMERGENCY CELIING LIGHTS NR 3 AND NR 4 INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820649 1 20081215 A 5610 601R3303317 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 507CA 7796 FLT 2599 - CAPTAIN WINDSHIELD SHATTERED. REPLACED CAPTAIN'S WINDSHIELD P/N ON, 601R33033-21 S/N ON, 08264H2884, P/N OF F: 601R33033-17, S/N OFF: 03034H5615. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820654 1 20081212 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 916SW 7634 FLT 6403 - NR 3 CEILING EMERGENCY FLOOD LIGHT IN CABIN INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820655 1 20081213 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG DISCHARGED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 495CA 7774 FLT 2522 - NOSE GEAR DID NOT RETRACT AFTER TAKEOFF. SERVICED NLG STRUT. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820703 1 20081220 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 944SW 7764 FLT 5866 - CEILING LEVEL EMERGENCY FLOODLIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 NM 2009 1 6 WX0A070248 1 20081108 A 3350 AD4002 BATTERY PACK DOUG MD80 MD83 3023681 NM EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 884GA 49401 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETUR NED TO SERVICE. 2 L 7 2 4F RT 20090106 EU 2009 1 6 FDEA200811285033 1 20081128 A 5730 A5796000720000 SKIN AIRBUS 300 A300B4622 3930401 EU ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 RT INBD FLAP INBD UPPER SKIN NR A57960007000 IS CRACKED. FABRICATED NEW SKIN IAW EA 6-5750-123529 AND DWG A57960007. A LODINED AND PRIMED IAW SRM 51-21-10. INSTALLATION OF SKIN TO BE ACCOMPLISHED ON J/C NR 6-5750-7-5003 PT 1. 2 L 7 2 4F RT A35EU 20090106 EA 2009 1 6 SWIA200820660 1 20081029 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 479CA 7675 C-CHECK, RIGHT ENGINE AFT THRUST FITTING CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820661 1 20081029 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 479CA 7675 DURING C-CHECK, LEFT ENGINE AFT THRUST FITTING CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820666 1 20081212 A 3397 WIRE CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT SHORTED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 932SW 7714 FLT 6660 - EMERGENCY LIGHT INOP AT MAIN CABIN DOOR. REPAIRED WIRE. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820667 1 20081216 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 443SW 7638 FLT 4507 - THIRD AFT CEILING EMERGENCY FLOOD LIGHTS INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820668 1 20081216 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN SMOKE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 912SW 7595 FLT 5857 - 'SMOKE TOILET' WARNING ON TAKEOFF. ACCOMPLISHED COMPRESSOR WASH ON LEFT ENGINE, REPLACED BOTH ACM'S AND COAL ESCER SOCKS, AND HIGH POWER ENGINE RUNS. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820718 1 20081121 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 468CA 7649 C-CHECK, LEFT ENGINE THRUST FITTING CORRODED. REPLACED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820719 1 20081121 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 709BR 7850 C-CHECK, LEFT ENGINE AFT THRUST MOUNT FITTING CORRODED. REPLACED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820720 1 20081121 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 709BR 7850 C-CHECK, RIGHT ENGINE AFT THRUST MOUNT FITTING CORRODED. REPLACED. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820721 1 20081121 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 709BR 7850 C-CHECK, LBL 9 FS 280 UPPER FLOOR SUPPORT CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820722 1 20081121 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 709BR 7850 C-CHECK, FS 280 RBL9 LOWER FLOOR SUPPORT CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820723 1 20081121 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 709BR 7850 C-CHECK, FS 280 LBL9 LOWER FLOOR SUPPORT CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090106 EA 2009 1 6 SWIA200820693 1 20081218 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 773SK 10236 FLT 6335 - CABIN CEILING EMERGENCY FLOOD LIGHT NR 6 INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090106 2009 1 6 YENA200812300133 4 20081227 A 2330 ENTERTAIN SYS AIRBUS 320 A320232 3930326 EU CABIN OBSTRUCTED A YENA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 649JB 2977 FLT NR 718, SJU-JFK, ENROUTE AT FL360 FA'S SMELLED A BURNING RUBBER SMELL BETWEEN ROWS 11-16 NEAR TOP OF AC. SMELL WAS EVIDENT FOR APPROX 15 MINUTES, THEN DISSIPATED. INSPECTED CABIN FOUND THAT PASSENGER ITEMS BLOCKING LIVE TV BOX UNDER R OW 12 PRODUCED EXCESSIVE HEAT AS SOURCE OF SMELL. ALL VISUAL CHECK OK AT THIS TIME. 2 L 7 2 4F RT A28NM 20090106 CE 2009 1 6 GUUA91253042508A 1 20080425 A 5330 SKIN BEECH 1900 1900D 1154162 CE BS 288 CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 45AR UE12 DURING SCHEDULED ROUTINE MX DISCOVERED 2.0 INCH CRACK IN FUSELAGE BELLY SKIN AT RBL 30.62. STOP DRILLED CRACK AND INSTA LLED REINFORCEMENT DOUBLER. 2 L 7 2 4T RT A24CE 20090106 SO 2009 1 6 2009F00000 1 20081223 A 2120 UNKNOWN GULSTM G1159 GIV 3980115 SO CABIN ODOR E N93A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 13 489QS 1389 AT FL 380 CREW HAD SMELLED SMOKE IN CABIN, SMELL WENT AWAY AFTER GALLEY AND CABIN POWER WAS TURNED OFF. 2 L 7 2 4F RT A12EA 20090106 NM 2009 1 6 DHLA2008743519 1 20081113 A 5753 FLAP TRACK BOEING 727 727200 138407E NM ZONE 500 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 REF N/R 5-222, LT WING NR3 T/E FLAP TACK AFT AND FWD SURFACES WITH CORROSION. REPAIRED LT WING NR 3 T/E FLAP TRACK AFT AND FWD MOUNTING PADS IAW OHM 57-40-01 PAR 2 B PAGE 403 AND PARA 2.E PAGE 411. 2 L 7 3 4F RT A3WE 20090106 NM 2009 1 6 USAA2008123092351 1 20081210 A 5530 D5537131800000 HINGE FITTING AIRBUS A319 A319132 3930340 NM VERTICAL STAB WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL - MAJOR REPAIR - C7 CHECK - NR 6141112, NR 5 RUDDER HINGE FITTING AT VERTICAL STABILIZER STATION 2985 / RIB7 HAS EX CESSIVE PLAY. REPLACED NR 5 RUDDER HINGE FITTING AT VERTICAL STABILIZER STATION 2985 / RIB7 IAW A319 AMM 55-36-41. 2 L 7 2 4F RT A28NM 20090106 NM 2009 1 6 USAA2008123092341 1 20081211 A 5315 D53472189202 FLOORBEAM AIRBUS A319 A319132 3930340 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL - MAJOR REPAIR - C7 CHECK - NR 6142381, CORROSION ON CABIN BEAM AT FR 67 - FR 69, -Y1165. REPLACED BEAM AT FR 67 FR 69, -Y1165 IAW A319 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20090106 EU 2009 1 6 USAA2009010590019 1 20081231 A 5315 D53472133200 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656AW 1079 SAL - C7 - MAJOR REPAIR - NR 6129698 - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66 +5 INCHES, -Y1292. REPAIRED FLOORBEAM BETWEEN FR64 TO FR66 +5 INCHES, -Y1292 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20090106 EA 2009 1 6 A6WA200840646 1 20081216 A 3020 ANTI-ICE VALVE CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE FAULTY A A6WA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 421ZW 7346 LOG 186570/2 RT COWL ANTI-ICE MSG IN FLIGHT WITH ANTI-ICE SELECTED ON. COMPLIED WITH QRH, MST PERSISTED, DIVERTED. RE MOVED AND REPLACED RT COWL ANTI-ICE VALVE REF AMM 30-20. OPS AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 20090106 WP 2009 1 6 AALA200810552 1 20081206 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7508 49802 CORROSION ON AFT END OF FLOORBOARD SUPPORT ON RT SIDE.(AFT CARGO) INSTALLED A SERVICEABLE SUPPORT IAW SRM 51-10-1. 2 L 7 2 4F A6WE 20090106 WP 2009 1 6 ABXA200812200272 1 20081229 A 2460 CIRCUIT BREAKER DOUG DC9 DC932 3022066 WP COCKPIT DEFECTIVE A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 986AX 47543 AT 4000 FT DC EMERGENCY BUS OFF LIGHT ILLUMINATED WITH ASSOCIATED MASTER WARNING. SHORTLY THEREAFTER THE NR 1 ADDU FAIL ED. WHEN THIS HAPPENED THE DC EMERGENCY BUS OFF ANNUNCIATOR EXTINGUISHED. PERFORMED ADJUST/TEST DC GENERATION. PERFOR MED ADJUSTMENT AND TEST OF EMERGENCY POWER SWITCH IAW AMM 24-23-02-2. DURING TROUBLESHOOTING, NOTICED THE LT WINDSHIELD WIPER CIRCUIT BREAKER HAD A CORNER CRACKED OUT OF IT AND WIRE WAS BROKEN ON A TERMINAL LUG. REPLACED TERMINAL LUG AND LT WINDSHIELD WIPER C/B. OPS CHECKED GOOD. REPLACED EMERGENCY DC BUS FEED C/B. REPLACED MASTER CAUTION LIGHT ASSY. ALL TESTS GOOD. 2 L 7 2 4F A6WE 20090107 NM 2009 1 7 FDEA200812265292 1 20081226 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11 3023602 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JA MB NR 1 SUPPORT FITTING AT HOLES NR A, NR C AND NR D. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I . REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090107 WP 2009 1 7 AALA200810554 1 20081219 A 5322 SHEAR TIE DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 259AA 49289 SHEAR TIE CRACKED AT FRAME STA 1418 BETWEEN LONGERON 1 AND 2 RT. INSTALLED REPAIR ANGLE IAW ESO 80559 DATED 12-18-08 AN D AARD 53-10-00-20. 2 L 7 2 4F A6WE 20090107 CE 2009 1 7 2009F00001 1 20081212 A 2750 FLAP SYSTEM BEECH 99 99 1154002 CE TE FLAPS MALFUNCTIONED E AXSA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 65 193WA U17 DURING FINAL APPROACH, BEFORE REACHING ANEYE INTERSECTION TO RWY 11 PILOT LOWERED FLAPS AND AS THE ACFT REACHED 140KTS L OWERED THE GEAR. WHEN THE GEAR WAS DOWN AND LOCKED THE PILOT NOTED AN ELECTRICAL BURNING SMELL AND, A FEW SECONDS LATER, NOTICED A LITTLE SMOKE IN THE COCKPIT WHICH DISAPPEARED AFTER A FEW SECONDS. THE PILOT DID NOT DECLARE AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINT WAS DISPATCHED TO THE ACFT. MX INSPECTED THE WIRING AND ELECTICAL COMPONENTS ON THE LAND ING GEAR AND FLAPS SYS AND NOTED NO DISCREPANCIES. THE ACFT WAS JACKED AND THE GEAR AND FLAPS WERE CYCLED WITH ELECTRICA L LOADS AND COULD NOT DUPLICATE THE DISCREPANCY. THE ACFT WAS RETURNED TO SERVICE WITHOUT ANY FURTHER INCIDENT. 1 L 7 2 3T A14CE 20090107 NM 2009 1 7 DHLA2008743522 1 20081110 A 5311 FRAME BOEING 727 727225 1384077 NM BS 440 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 D-CHECK, WO NR 5740, NR 5740-2-136, UPPER FUSELAGE PAX CABIN AT BS 440 BETWEEN STR16R AND 17R FRAME INBD FLANGE WITH CRA CK. REPAIRED FRAME AT BS 440 BETWEEN STR 15R AND 17R. DUE TO CRACK IAW SRM 51-40-3 FIG.1. 2 L 7 3 4F A3WE 20090107 NM 2009 1 7 DHLA2008743523 1 20081109 A 5311 FRAME BOEING 727 727225 1384077 NM BS 620 S16-17R DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 D-CHECK AT WO NR 5740, NR 5740-2-115, UPPER FUSELAGE PAX CABIN BS 620 BETWEEN STR 16R AND 17R FRAME WITH DOUBLE HOLE. R EPAIRED FUSELAGE FRAME SECTION AT BS 620 BETWEEN STR 15R AND 17R DUE TO DOUBLE HOLE. 2 L 7 3 4F A3WE 20090106 EA 2009 1 6 A6WA200840641 1 20081208 A 5220 HANDLE CNDAIR CL600 CL6002B19 1900309 EA ENERGENCY EXIT CORRODED A A6WA O OTHER O OTHER UK UNKNOWN 1 GL 31 5220 7586 MX WORK CARD 129777-29 ON HEAVY MX C-CHECK HANDLE OF EMERGENCY ESCAPE HATCH FOUND STUCK DUE TO STEM CORRODED. HANDLE RE PLACED IAW AMM 52-22-03-400-801 AND AMM 52-22-03. 2 L 7 2 4F RT A21EA 20090107 NM 2009 1 7 UALA2008122907022 1 20081227 A 3350 794640 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EXIT LIGHT INOP BETWEEN LAVS 111 AND 112 LOWER WALL. REPAIRED EMERGENCY LIGHT POWER STRIP. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008122907031 1 20081229 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT SEAT 47ABC INOP. REPAIRED SUPPLY WIRE OPS CK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008122907032 1 20081229 A 3350 582240 POWERPACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY SILL LITE DR 1L INOP FWD AND AFT. REPLACED POWER PACK. OPS CK OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008123007037 1 20081229 A 5522 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ELEVATOR DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 501UA 24622 RT ELEVATOR LOWER CENTER EXT SURFACE HAS DELAMINATED BROKEN AREA AT ELEV STA 220. REMOVED DAMAGE AND ACCOMPLISHED CARBO N FIBER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20090107 EU 2009 1 7 DHLA200800138 1 20081228 A 7160 NSL6051533 NOSE COWL AIRBUS 300 A300B42C 3930106 EU NR 1 ENGINE DAMAGED A DLLA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 05 365DH 149 RAMP DAMAGE TO INB D TOP SIDE OF NR 1 ENGINE NOSE COWL. ACFT STRUCK BY PORTABLE AIRSTAIRS WHILE PARKED ON RAMP. NR1 ENG COWL P/N NSL6051-533 REQUIRING REPLACEMENT. 2 L 7 2 4F RT A35EU 20090107 WP 2009 1 7 DBCA20081219605SA 2 20081218 A 7261 S9413117 O-RING CESSNA 650 650 2076802 CE GARRTT TPE731 TFE7313C WP OIL CAP CUT E DBCA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 13 605SA 6500152 87420 DURING CRUISE FLIGHT, CREW NOTICED NR 1 ENG OIL PRESSURE DECREASING FROM 42 PSI TO 35 PSI. CREW REDUCED POWER ON NR 1 EN GINE AND CONTINUED TO MONITOR OIL PRESSURE. WHEN OIL PRESSURE DROPPED TO 30 PSI CREW SHUTDOWN NR 1 ENGINE AND DIVERTED TO NEAREST AIRPORT. INSPECTED NR 1 ENG. FOUND O-RING ON OIL FILLER TUBE CUT RESULTING IN A LOSS OF OIL. CONTACTED TEC H SUPPORT FOR ENGINE INSP REQUIREMENTS DUE TO LOW OIL PRESSURE AND OIL LOSS. LOCAL MX INSPECTED OIL FILTER FOR METAL IA W TECH SUPPORT. NO DEFECTS NOTED. REPLACED DAMAGED O-RING AND LEAK CHECKED ENGINE. 2 L 7 2 4F 4 F A9NM E6WE 20090107 CE 2009 1 7 DJFA2008089 1 20081230 A 5610 45AS31001023 WINDSHIELD BEECH MU300 400A 1155402 CE ZONE 200 CRACKED E DJFA O OTHER O OTHER LD LANDING 1 EA 23 898TA 1423 RK295 ON FINAL APPROACH PILOTS WINDSCREEN GLASS OUTER PLY CRACKED IN MULTIPLE LOCATIONS. CREW DECLARED AN EMERGENCY AND LANDE D SAFELY. 45 MINUTES AFTER LANDING, THE COPILOTS WINDSHIELD ALSO CRACKED. OPEN 2 H 7 2 4F RT A16SW 20090107 NM 2009 1 7 UALA2008123007046 1 20081230 A 2421 GENERATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 575UA 26689 LOST LT GENERATOR. 2 L 7 2 4F 4 F RT A2NM E17NE 20090107 NM 2009 1 7 UALA2008123107055 1 20081231 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 EMERGENCY LIGHT ON DIVIDER BETWEEN SEATS 9 AND 10 LT INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 WP 2009 1 7 CLCA20080805001 1 20080805 A 2611 3023117 SMOKE DETECTOR DOUG DC10 DC1030F 3023504 WP CARGO BAY FAILED A CLCA F J A ACTIVATE FIRE EXT. DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 29 614GC 46931 AFTER TAKEOFF, LWR FWD CARGO SMOKE DETECTOR POS. 1 LT ON, FOLLOWED BY FWD FIRE LT ON. CREW FOLLOWED PROCEDURES AND DISCH ARGED NR1 FIRE BOTTLE CYLINDER. REPLACED NR1 FIRE BOTTLE AND 2 EA SQUIBS AND NR 1 FWD SMOKE DETECTOR. NO EVIDENCE OF FI RE AFTER POST FLIGHT INSP. PASS OPS CHECK OF SYS. 2 L 7 3 4F RT A22WE 20090107 NM 2009 1 7 UALA2008123107056 1 20081231 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 UPPER DECK EMERGENCY LIGHT CEILING LIGHT INOP NEAR SEAT 17K. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008123107057 1 20081231 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE AFT CREW REST INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 AFT CREW REST CEILING LIGHT INOP. REPLACED EMERGENCY LIGHT ASSY. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008123107058 1 20081231 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 DR 5 RT FWD SILL EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008123107060 1 20081230 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 128UA 30023 SEAT 46 HJK EMERGENCY LIGHT INOP. REPLACED LIGHT ASSEMBLY. OPS CHECK IS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008123107063 1 20081231 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 597UA 28750 NR 3 RT MED EXTERIOR EMERGENCY LIGHT INOP. RELAMPED. OPS CHECKED OK 2 L 7 2 4F 4 F RT A2NM E17NE 20090107 EU 2009 1 7 FDEA200812185197 1 20081218 A 5321 FXSRZ25005252WG FLOORBEAM AIRBUS 310 A310 EU ZONE 200 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 38333 248 FLOORBOARD 252WG IS DELAMINATED ON THE LWR SURFACE FROM FRAME 62 TO FRAME 65 R/H. REPAIRED FLOOR PANEL 252 WG BY FABRI CATING A NEW FLOOR PANEL FROM STOCK MATERIAL USING THE OLD PANEL AS A TEMPLATE IAW FEDEX DWG SRZ20-005; REV " G ". 2 L 7 2 4F RT A35EU 20090107 CE 2009 1 7 J7SA452022081221 1 20081221 A 2421 6608458005 GENERATOR LEAR 45 45LEAR 5170805 CE GARRTT TFE731 TFE7312 01518 WP RIGHT FAILED E J7SA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 05 609FX 452022 P116572C R/H ENGINE VIBRATION NECESSITATED IN-FLIGHT SHUTDOWN. DURING VIBRATION THE 'EMER BATT' AND EMER SWITCH LIGHTS WOULD BLIN K. AIRCRAFT DIVERTED TO KFLL. MAINTENANCE RAN ENGINE AND FOUND THE RT GENERATOR FAULTY. GENERATOR REPLACED AND GROUND R UNS PERFORMES SATISFACTORILY 2 L 7 2 4F 4 F RT T00008WI E6WE 20090107 2009 1 7 J7SA45371081227 4 20081227 A 2310 4523558501003 CONTROL PANEL LEAR 45 45LEAR 5170805 CE HF SYSTEM MALFUNCTIONED E J7SA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 05 443FX 45371 UNBEARABLE STATIC OVER BOTH RADIOS & SPEAKERS AFTER ROTATION WITH GEAR RETRACTION. CONTINUED THROUGH LANDING AND TAXI & DUPLICATED AFTER ENGINE SHUT DOWN & RESTART ON RT SIDE. TX CHECK LEFT SIDE WAS NORMAL. NO TX RIGHT SIDE. MIC OR HEADSET SEEMS WORSE WITH RAD MASTER ON OR ENGINE START.MX FOUND STATIC TIED TO WHETHER THE R INST PANEL BACKLIGHTING IS ON OR NOT. FURTHER T/S FOUND AN OPEN RESISTOR ON THE COPILOT'S SWITCH PANEL THAT REGULATES THE VOLTAGE TO THE PANEL (DB80). W IRING TO THE RESISTOR WAS REPAIRED IAW LEAR MM CHAP 33-10-01. NR 1 AND 2 AUDIO CONTROL PANELS REPLACED AS A PRECAUTION. ALL OPERATIONAL CHECKS NORMAL 2 L 7 2 4F RT T00008WI 20090107 NM 2009 1 7 QXEA2008122401255 1 20081220 A 3350 6138001 BATTERY PACK BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY LIGHTS FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 19 406QX 5512 718 4048 SEA - DURING A CHECK OF CABIN LIGHTING WHILE DOING A LINE CHECK, FOUND THAT THE FORWARD CEILING EMERGENCY LIGHT AND THE TWO FORWARD EMERGENCY EXIT SIGNS DID NOT ILLUMINATE. REMOVED AND REPLACED THE TWO FORWARD EMERGENCY BATTERY PACKS LOCAT ED AT POSITIONS R1 AND L1. PERFORMED OP CHECK IAW AMM TASK 33-51-00-710-801. OP CHECK GOOD. NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 20090107 NM 2009 1 7 ASAA0944145 1 20081214 A 5753 6546430167 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FOREFLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 LT IB FORE FLAP UPPER SURFACE DENTED. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER BONDED REPAIR IAW SRM 51 70 10 . 2 L 7 2 4F 4 F RT A16WE E21EU 20090107 NM 2009 1 7 ASAA0944146 1 20081218 A 5753 6546486149 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU MIDFLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 LT INBD MID FLAP T/E WEDGE LOWER SURFACE HAS MULTIPLE SHARP DENTS AT INBD CORNER AT PREVIOUS REPAIR. REMOVED PREVIOUS RE PAIR FABBED REPAIR PARTS AND BONDED IAW SRM51 70 10. 2 L 7 2 4F 4 F RT A16WE E21EU 20090107 NM 2009 1 7 ASAA0944147 1 20081214 A 5755 654645170A SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU NR 3 SPOILER DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 NR 3 SPOILER UPPER SKIN HAS A CLUSTER OF DENTS 1.8 IN FWD OF T/E. REMOVED DAMAGED AREA FABRICATED FILLER AND DOUBLER BON DED REPAIR IAW SRM 51 70 10. 2 L 7 2 4F 4 F RT A16WE E21EU 20090107 NM 2009 1 7 QXEA2008122601262 1 20081226 A 4920 APU BOMBDR DHC8 DHC8402 1390042 NM SMOKE A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 19 411QX 4055 WHITE SMOKE COMING FROM AROUND APU ACCESS DOORS AND THE OUTSIDE OF THE APU EXHAUST PIPE CONTINUED FOR SEVERAL MINUTES AF TER APU SHUT DOWN. INSPECTED APU AREA FOR ANY FUEL OR OIL LEAKS, NONE FOUND. RAN APU TO VERIFY NO LEAKS. UPON FURTHER INVESTIGATION, FOUND DEICE FLUID ON APU COMPARTMENT. CLEANED DEICE FLUID AND RAN APU AGAIN. NO SMOKE NOTED. NO FURTH ER DEFECTS. ACFT OK FOR SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20090107 NM 2009 1 7 ASAA0944126 1 20081211 A 5322 69407124 SHEAR TIE BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON SHEAR TIE AT BS 927-947 RBL 17. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F RT A16WE 20090107 NM 2009 1 7 ASAA0944154 1 20081215 A 5330 65E3477832 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 FUSELAGE SKIN CRACKED AFT OF STA 303 BELOW LT DOOR UPPER HINGE REMOVED DAMAGED SKIN. FABRICATED INSTALLED REPLACEMENT G AP COVER IAW SRM 51 40 02. 2 L 7 2 4F 4 F RT A16WE E21EU 20090107 NM 2009 1 7 QXEA2008123001261 1 20081226 A 3260 465007 UPLOCK BOMBDR DHC8 DHC8402 1390042 NM ZONE 700 MALFUNCTIONED A QXEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 NM 19 409QX 12252 4051 SEA- ON APPROACH RM GEAR FAILED TO EXTEND DOOR UNSAFE LIGHT ILLUMINATED AFTER COMMENCING MISSED APPROACH GREEN LIGHT ILL UMINATED LEFT GEAR EXTENDED. LANDED NORMALLY. FERRIED THE AIRCRAFT TO PDX FOR REPAIRS. REMOVED AND REPLACED RT MLG UP LOCK ASSY IAW Q400 AMM 32-31-21-400-801. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20090108 NM 2009 1 8 QXEA2009010601274 1 20081230 A 5320 FLOOR SUPPORT BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 415QX 4081 PDX - C3 - LIGHT CORROSION ON HORIZONTAL SURFACE OF CARGO BAY FLOOR ANGLE AT STA X783 FROM STA Y0 TO Y22L. REMOVED CORR OSION REF SRM 51-21-00 PG 2 PARA A(1,2&9). UT THICKNESS IAW NDTM PART 1 51-00-04. LOW .049 CORRODED ANGLE TO BE REPLAC ED. REMOVED CORRODED ANGLE, TEMP, INSTALLED ANGLE, DRILLED AND COUNTERSUNK ALL HOLES. ALODINED NEW ANGLE REF SRM 51-21 -00, PRIMED REF SRM 51-25-10. PERFORMED VISUAL SURVEY OF AREA OK TO INSTALL. INSTALLED VERTICAL FLANGE OF ANGLE USING MS20470AD5 RIVETS REF SRM 51-42-05. COMPLETED INSTALLATION OF NEW ANGLE BY INSTALLING ALL REMAINING FASTENERS REF Q400 SRM 51-42-05. 2 H 7 2 4T RT A13NM 20090108 NM 2009 1 8 QXEA2009010601275 1 20081230 A 5321 FLOOR PANEL BOMBDR DHC8 DHC8402 1390042 NM CARGO BAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 415QX 4081 PDX - C3 - LIGHT CORROSION ON STRUCTURE AT THE MATING SURFACE OF CARGO BAY PANEL 144JZ. REMOVED CORROSION REF SRM 51-21 -00 PAGE 2, PARA A(1), (2)(A). UT THICKNESS IAW NDTM PART 1, 51-00-04 HIGH .050 LOW .046. HFEC AT BLENDED AREA FOR CRA CK IAW NDTM PART 6 51-00-01, NO CRACKS NOTED. REMOVED .004 INCH AND FOUND TO BE WITHIN LIMITS REF SRM 51-14-00 PG 204 P ARA 7 (A) THRU 3. APPLIED ALODINE TO MATING SURFACE OF CARGO BAY PANEL 144JZ REF SRM 51-21-10-02-01 PARA 5D. PRIMED AR EA REF SRM 51-25-10-02-01 PARA 5D. 2 H 7 2 4T RT A13NM 20090108 EA 2009 1 8 SWIA200820743 1 20081231 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 948SW 7789 FLT 5934 - CEILING EMERGENCY LIGHT INOP ABOVE ROW 5. RELAMPED. 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 SWIA200820744 1 20081229 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 FLT 6621 - EMERGENCY LIGHT, LEFT WING ROOT AREA NEAR LEADING EDGE INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090108 SO 2009 1 8 SWIA200820745 1 20081228 A 3350 SIGN EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT MISSING A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 294SW 120321 FLT 5566 - EMERGENCY EXIT SIGN UNDER FLIGHT ATTENDANT SEAT MISSING AND LIGHT INOPERATIVE. INSTALLED COVER, SIGN TESTS N ORMAL. 2 L 7 2 4T RT A31SO 20090108 EU 2009 1 8 FDEA200811014671 1 20081101 A 2611 CG7G0 SMOKE DETECTOR AIRBUS 300 A300B4622R 3930312 EU FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 721FD 13225 10357 477 AT 8000 AFTER TAKEOFF FROM EGSS GOT SMOKE/FUME ALERT FROM MAIN DECK SMOKE DETECTOR MID 2A. STAYED ON FOR ABOUT 8 MINS, WENT OFF JUST BEFORE LANDING. MID 1B, MID 2B, AND AFT A WERE ALL READY DEFERRED. ACN RELEASED FOR SERVICE PER MEL/CDL: 26-17-01-B CATEGORY: C EXPIRATION: 11NOV08 "MEL 26-17-01-B: MAIN DECK (IDENTIFY MID 1, MID 2 AN D/OR AFT), 2A SMOKE DE TECTOR(S) INOP. NO CARGO INSTEAD OF 12-13 SECONDS FOR ALL THE OTHER ONES, AMM REF:26-19-00 PAGE 504, ACTION NR 1. REM OVED AND REPLACED SMOKE DETECTOR 10 WU AS PER AMM:26-19-12 P401. PERFORMED TEST AS PER PREVIOUS AMM REF: TEST PASSED. 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812185211 1 20081218 A 5312 A5381109320000 FITTING AIRBUS 310 A310203 3930313 EU S39L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 AFT PIT FWD BULKHEAD AT S39L CORROSION ON END FITTING. REMOVED CORROSION; FOUND TO BE OUT OF LIMITS IAW SRM 53-15-14; F IG 7; SHEET 2. REMOVED FITTING IAW SRM 51-40-21. RECEIVED NEW FITTING, LOCATED & DRILLED NEW FITTING IAW DWG A53811093 . INSTALLED FITTING IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812185212 1 20081218 A 5312 A5381109320000 FITTING AIRBUS 310 A310203 3930313 EU S40L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 AFT PIT FWD BULKHEAD AT S40L, CORROSION ON END FITTING. REMOVED CORROSION; FOUND TO BE OUT OF LIMITS IAW SRM 53-15-14; FIG 7; SHEET 2. REMOVED FITTING IAW SRM 51-40-21. RECEIVED NEW FITTING, LOCATED & DRILLED NEW FITTING IAW DWG A5381109 3. INSTALLED FITTING IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812185213 1 20081218 A 5312 A5381109320000 FITTING AIRBUS 310 A310203 3930313 EU S43L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 AFT PIT FWD BULKHEAD AT S43L, CORROSION ON END FITTING. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-15-14; FIG 7; SHEET 2. REMOVED FITTING IAW SRM 51-40-21. RECEIVED NEW FITTING, LOCATED & DRILLED NEW FITTING IAW DWG A5381109 3. INSTALLED FITTING IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20090108 NM 2009 1 8 FDEA200812185195 1 20081218 A 2750 6519268 CONTROL LEVER BOEING 727 7272D4 138407U NM TE FLAPS LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 FLIGHT TEST OUTBOARD FLAP GAUGE INDICATED BETWEEN 20 DEGREES AND 25 DEGREES AT FLAPS 25 DEGREES AND BETWEEN 25 INCH AND 30 INCH AT FLAPS 30 INCH ALL OTHER POSITIONS OK (REPEAT) PERFORMED ADJUSTMENT AND TEST ON OTBD T/E FLAP POSITION TRANSMI TTER REF MM 27-52-013-5. OPS CK GOOD POINTERS IN TOLERANCE THIS IS CLASSIFIED AS A MINOR REPAIR CHECKED T/E FLAP DRIVE SYSTEM FOUND PLAY IN FLAP CONTROL LEVER DRUM FLAP CONTROL LEVER DRUM. REMOVED REPAIRED AND REINSTALLED ON EA NR 7-2750- 123828 CHECKED ADJUSTED AND TESTED T/E FLAP DRIVE SYSTEM REF MM 27-51-000-5 PAGES 2 THRU 5 AND 9 THRU 11 T/E FLAP DRIVE SYSTEM. OPS CHECKED GOOD. 2 L 7 3 4F A3WE 20090108 NM 2009 1 8 QXEA2008010501282 1 20081231 A 3260 6007047 TRANSDUCER BOMBDR DHC8 DHC8402 1390042 NM WHEEL SPEED FAILED A QXEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 19 401QX 4031 PDX - MAIN BRAKES APPEARED SLOW TO ENGAGE DURING LANDING. A GREAT AMOUNT OF BRAKE PEDAL FORCE WAS REQUIRED BEFORE A/C B EGAN TO SLOW BRAKE RESPONDED WAS BETTER WHEN ANTI-SKID WAS TURNED OFF. REPLACED LT OUTBOARD WHEEL SPEED TRANSDUCER, AND REPAIRED CHAFED WIRES. PERFORMED TAXI CHECK, CHECKS OK. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20090107 EU 2009 1 7 FDEA200812305320 1 20081230 A 5321 FXA532727980080 FLOOR PANEL AIRBUS 310 A310 EU ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 810FD 452 FWD CARGO COMPARTMENT FLOOR PANELS, ZONE 131, FLOOR PANEL 131 HG HAS STRUCTURAL DAMAGES FABRICATED NEW FWD CARGO COMPA RTMENT FLOOR PANEL, IAW SAMPLE,PANEL 131 HG, IAW SRZ-25-005,ON TRAVELER, NR T8/773384. 2 L 7 2 4F RT A35EU 20090107 NM 2009 1 7 FDEA200812305321 1 20081230 A 5347 SEAT TRACK BOEING 757 75728A 1384976 NM BS1080-1180 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 912FD 24260 SEAT TRACK, BS 1080-1180, RBL 45, HAS LUG DAMAGE. REMOVED AND REPLACED SEAT TRACK ASSY, IAW SRM 51-40-02. REPLACEMENT S EAT TRACK ASSY FABRICATED ON MAE TRAVELER T8/771189 IAW SRM 53-00- 52. LUG REWORK DIMENSIONS, ON DAMAGED SEAT TRACK, WE RE AS FOLLOWS: L=.250 INCH, W=.100 INCH, D=.035 INCH. THIS IS CLASSIFIED AS A CAT. "A" MAJOR REPAIR. 2 L 7 2 4F RT A2NM 20090107 NM 2009 1 7 ABXA200901060001 1 20081229 A 5270 WARNING LIGHT BOEING 767 767232 1385132 NM CARGO DOOR ILLUMINATED A ABXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 746AX 22223 MAIN CARGO DOOR LIGHT ON AFTER TAKEOFF, RETURNED TO DEPARTURE.ACCOMPLISHED MX PRACTICES ON DOOR OPERATION AND CHECKED ALL EXTERIOR DOOR LOCK INDICATOR'S ARE WHITE. DOOR LIGHTS OUT AND OPS CHECK GOOD IAW AMM 52-32-00-2. 2 L 7 2 4F RT A1NM 20090107 CE 2009 1 7 GUUA94732121908A 1 20081219 A 3260 DOWNLOCK SWITCH BEECH 1900 1900D 1154162 CE MLG OUT OF ADJUST A GUUA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 29 69547 UE189 FLIGHT 9294 CLE/FKL AFTER TAKEOFF LANDING GEAR BROUGHT TO THE UP POSITION, RED INTRANSIT LIGHTS REMAINED ILLUMINATED AND ALL GREEN LIGHTS WERE EXTINGUISHED. CYCLED THE LANDING GEAR THE CONDITION REMAINED THE SAME. RETURNED TO CLE LANDED WIT HOUT INCIDENT. ADJUSTED ALL THREE GEAR DOWNLOCK SWITCHES AND CLEANED ALL THREE UPLOCK SWITCHES. OPERATIONAL CHECK GOOD. 2 L 7 2 4T RT A24CE 20090107 NM 2009 1 7 QXEA2008121901250 1 20081216 A 3233 4655013 ACTUATOR BOMBDR DHC8 DHC8402 1390042 NM ZONE 700 FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 19 413QX 15227 2001 4060 SEA - UPON GEAR UP SELECTION LEFT DOOR AMBER AND LT GEAR RED UNSAFE LIGHTS LAG 7 SECONDS AFTER ALL OTHER GEAR LIGHT GEA R LIGHT EXTINGUISH THIS TIME LAG HAS INCREASED FROM 4 SECONDS TO 7 SECONDS OVER LAST THREE GEAR UP SELECTIONS. RETURNE D TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. FERRY TO PDX FOR REPAIR. REMOVED AND INSTALLED SERVICEABLE LT ML G RETRACT/EXTEND ACTUATOR IAW TASK 32-31-11-000-801 AND 32-31-11-400-801. OPERATIONAL CHECK IAW 32-31-00-710-801 TR32-2 40. CHECKS GOOD. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20090107 NM 2009 1 7 C8GA20080080 1 20081027 A 5322 SHEAR TIE BOEING 727 727223 1384074 NM PWA JT8 JT8D NE FUSELAGE CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 NA WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT SHEAR TIE LOCATED AT STATION 580 STRINGER 26R-27R WA S CORRODED. REMOVED DAMAGED SHEAR TIE. FABRICATED NEW SHEAR TIE FROM 7075-O .071 INCH (8 INCHES X 2 INCHES) HEAT TREATED TO T6. INSTALLED NEW SHEAR TIE IAW 51-40-2, 53-10-2. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 20090107 EA 2009 1 7 COMA2009010550053 1 20081231 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 1900309 EA TE FLAP FAILED A COMA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 27 720SW 16524 7297 DURING APPROACH INTO AIRPORT, RECEIVED FLAPS FAIL CAUTION MSG. EMERGENCY DECLARED, ACFT DIVERTED LANDED SAFELY. REMOVE D AND REPLACED LT BPSU. 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 SWIA200820751 1 20081229 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 743SK 10199 FLT 6599 - NR 2 OVERHEAD EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 SWIA200820754 1 20081229 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 816SK 15105 FLT 4679 - OVERHEAD EMERGENCY EXIT LIGHT AT ROW 14 INOP. OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 SWIA200820756 1 20081230 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002B19 1900309 EA MLG OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 506CA 7793 FLT 2825 - "GEAR DISAGREE" AND "NOSE DOOR OPEN" WARNINGS DISPLAYED. ADJUSTED THE NLG OLEO CENTRAL EXTENDED PROXIMITY SE NSOR. 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 SWIA200820757 1 20081229 A 2150 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN SMOKE A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 506CA 7793 FLT 2716 - AFTER TAKEOFF ODOR OF SMOKE IN CABIN AND COCKPIT. INSPECTED BOTH PACKS, RAN ENGINES AND BLEED AIR, RAN APU B LEED AIR FOR SEVERAL MINUTES COULD NOT DUPLICATE ANY UNUSUAL ODORS. 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 SWIA200820759 1 20081129 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 423SW 7456 DURING C-CHECK, LEFT FS 484 FLOORBEAM CRACKED. REPLACED. 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 SWIA200820760 1 20081129 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 423SW 7456 DURING C-CHECK, RIGHT FS 484 FLOORBEAM CRACKED. REPLACED. 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 SWIA200820761 1 20081206 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 DURING C-CHECK, RIGHT ENGINE AFT THRUST MOUNT CORRODED. REPLACED. 2 L 7 2 4F RT A21EA 20090108 2009 1 8 FDEA200811154892 4 20081115 A 3417 4045053914 ADC AIRBUS 310 A310203 3930313 EU NR 2 FAILED A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 21 813FD 12 12 500 ON TAKEOFF ROLL, F/O HAD NO AIRSPEED INDICATION, PERFORMED REJECT (70KTS). PERFORMED ALL OTHER PARAMETERS THAT COME FRO M ADC ARE NORMAL. THE ON ISSUE IS THE SEED. PER FLIGHT CREW THE SPEED STOP AND THERE WAS DIFFERENCE FROM THE CAPTAIN'S AND THE FO'S. DURING FLIGHT FROM OAK TO BUR, FLIGHT CREW DID MENTIONED THAT THEY SWITCHED OVER FROM NR 2 SGU TO NR 3 AND THE RESULTS WERE NO JOY. BAGGED FO'S PITOT PROBE AND BACK PRESSURED PITOT LINE, NO DEBRIS FOUND, RECONNECTED ALL LI NES. REMOVED AND REPLACED NR 2 AIR DATA COMPUTER. PERFORMED FO'S PITOT LEAK CHECK WITH BARFIELD TESTER, LEAK CHECKS N ORMAL. SYSTEM OPS CHECKS NORMAL PER MM 34-11-34-4. 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812185205 1 20081218 A 5320 A5381109320000 FITTING AIRBUS 310 A310203 3930313 EU S33L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 AFT PIT FWD BULKHEAD AT S33L, END FITTING CORRODED. REMOVED CORROSION; FOUND TO BE OUT OF LIMITS IAW SRM 53-15-14; FIG 7; SHEET 2. REMOVED FITTING IAW SRM 51-40-21. LOCATED & DRILLED NEW FITTING IAW DWG A53811093. INSTALLED FITTING IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812185207 1 20081218 A 5313 A5381109320000 FITTING AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 AFT PIT FWD BULKHEAD AT S35L END FITTING CORRODED. REMOVED CORROSION; FOUND TO BE OUT OF LIMITS IAW SRM 53-15-14; FIG 7 ; SHEET 2. REMOVED FITTING IAW SRM 51-40-21. RECEIVED NEW FITTING, LOCATED & DRILLED NEW FITTING IAW DWG A53811093. I NSTALLED FITTING IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20090108 NM 2009 1 8 DHLA2008743526 1 20081109 A 5311 FRAME BOEING 727 727225 1384077 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 D-CHECK, WO NR 5740, NR 5740-2-85, UPPER FUSELAGE PAX CABIN STA 1090 BETWEEN STRINGERS 10 AND 11, 13 AND 14 RT FRAME INB D FLANGE WITH ENLONGATED HOLES. REPAIRED FUSELAGE FRAME SECTION AT BS1090 BETWEEN STR 10R AND STR 14R DO TO ELONGATED H OLES IAW SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 20090108 EU 2009 1 8 FDEA200812185224 1 20081218 A 5347 A5383202020400 SEAT TRACK AIRBUS 310 A310324 3930206 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 810FD 452 MAIN CARGO DECK SEAT TRACK AT RBL 18 HAS EXFOLIATION FROM FR 19 TO FR 14B. REMOVED SEAT TRACK IAW SRM 51-40-21, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-44, P/N A538320202400 BATCH 0001549861. INSTALLED SEAT TRACK IAW SRM 51-40-21 . 2 L 7 2 4F RT A35EU 20090108 WP 2009 1 8 FDEA200812195230 1 20081219 A 5311 ABA722113 FRAME DOUG DC10 DC1030F 3023504 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 317FE 46835 DURING INSPECTION ON AVIONIC COMPT FOUND CRACK ON FRAME. 2 L 7 3 4F RT A22WE 20090108 EU 2009 1 8 FDEA200812185226 1 20081218 A 3260 DOWNLOCK SWITCH AIRBUS 300 A300F4605R 3930327 EU NLG OUT OF ADJUST A FDEA B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 CE 21 650FE 726 UNSAFE NOSE GEAR INDICATION ON INITIAL LOWERING OF THE GEAR HANDLE. COMPLIED WITH QRH PROCEDURES AND HAND CRANKED THE GEAR. STILL HAD AN UNSAFE INDICATION AFTER ALL STEPS WERE COMPLETED. EXECUTED HIGH "G" MANEUVER AND NOSE GEAR CAME DO WN SHORTLY THEREAFTER. JACKED ACFT AND ACCOMPLISHED SEVERAL GEAR RETRACTION/EXTEND CYCLES WITH NO FAULTS NOTED. REF T SM 32-61-00 VERIFIED TELESCOPIC DRAG STRUT DOWNLOCK SWITCHES ADJUSTED PER MM 32-31-24-4. ACCOMPLISHED SEVERAL MORE FULL EXTEND AND RETRACT CYCLES WITH NO FAULTS, ACFT OK FOR SERVICE AT THIS TIME. 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812195241 1 20081219 A 5320 A5327400500000 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 CABIN SEAT TRACK AT RBL 38 HAS GOUGES BETWEEN FR 38.1 & FR 38.2. BLENDED & REMOVED GOUGES ON THE SEAT TRACK AT FRAMES 38 .1 & 38.2; RBL 38 REF SRM 51-73-10. ALODINED REF SRM 51-21-10. PRIMED & PAINTED REF SRM 51-23-10. 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812205248 1 20081220 A 5321 FXSRZ25005132QR FLOOR PANEL AIRBUS 310 A310203 3930313 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 FWD CARGO PIT FLOOR PANEL NR 132 QF IS DAMAGED. FABBED NEW PANEL USING THE OLD PANEL AS A TEMPLATE. MATERIAL ID; LOCAT ED HOLES USING THE THE OLD PANEL; COUNTERBORED HOLES; POTTED & SANDED EDGE; INSTALLED INSERTS; APPLIED ANTI-SKID & PART MARKED IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812195240 1 20081219 A 5347 A5327400500000 SEAT TRACK AIRBUS 310 A310203 3930313 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 CABIN SEAT TRACK AT RBL 38 GOUGED IN AREAS BETWEEN FR 36 AND FR 37. BLENDED & REMOVED GOUGE ON THE SEAT TRACK FRAMES 36 & 37; RBL 38 REF 51-73-10. ALODINED REF SRM 51-21-10. PRIMED & PAINTED REF SRM 51-23-10. 2 L 7 2 4F RT A35EU 20090108 NM 2009 1 8 FDEA200812265303 1 20081226 A 5310 7075T6080C DOOR FRAME BOEING 757 75728A 1384976 NM FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 912FD 24260 NR2 PASS DOOR LT LWR CUT OUT FRAME WEB AND ANGLE SUPPORT HAVE SEVERAL SPOT OF CORROSION AT STA 690-730. REMOVED ANGLE SU PPORT AND FABBED ON MAE TRAVELER NR T8/767744, LOCATED, DRILLED,TREATED, PRIMED AND INSTALLED NEW ANGLE SUPPORT IAW SRM5 1-40-02, 51-40-05, 51-40-06 AND 51-20-01. REMOVED WEB ON STA 680-700 AND FABBED NEW WEB ON MAE TRAVELER NR T8/767742, L OCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW WEB IAW SRM 51-40-02, 51-40-05, 51-40-06, 51-20-01. THIS IS A MAJOR A ND CATEGORY "A" REPAIR ON STA 690- 730. 2 L 7 2 4F RT A2NM 20090108 SO 2009 1 8 GLBA200812223 1 20081221 A 5330 SKIN EMB 120 EMB120ER 3260203 SO FUSELAGE GOUGED A GLBA K NONE O OTHER UK UNKNOWN 1 NM 21 299UX 120299 RT FUSELAGE DENTED FWD OF FRAME 20 AT F.S. 6462.6 AND STRINGER 13R GOUGE APPROX .049 DEEP BY APPROX .70 IN DIAMETER. MX REPAIRED DENT AT THE RT SIDE FUSELAGE FWD OF FRAME 20 AT FS 6462.6 BELOW STRINGER 13R. REPAIR APPROX 3.5 INCH BY 3.5 I NCH OUT OF 2024 T3, .063 DOUBLER, 2024 T3 .063 FILLER, BRFZ-5AD RIVETS. AC-665 C-12 SEALANT, AC240 B 1/4 SEALANT. 2 L 7 2 4T RT A31SO 20090108 SO 2009 1 8 GLBA200812222 1 20081220 A 3230 SPRING ASSY EMB 120 EMB120ER 3260203 SO RT MLG DIRTY A GLBA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 21 299UX 120299 PILOTS REPORTED THE RT MLG WOULD NOT RETRACT AT TAKEOFF. MX CLEANED AND LUBED THE RT MAIN GEAR SPRING BOX ASSY. MX PERF ORMED AND OPS CHECK OF THE SYS WHICH WAS GOOD IAW MM 32-10. 2 L 7 2 4T RT A31SO 20090108 NM 2009 1 8 SWAA090006 1 20081231 A 3350 PL2230LH0 LIGHT BOEING 737 7373H4 1384600 NM CABIN DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 608SW 27928 EMERGENCY LIGHT STRIP DELAMINATED AT ROW 8. REMOVED AND REPLACED EMERGENCY LIGHT PER MM. 2 L 7 2 4F RT A16WE 20090108 EU 2009 1 8 M7KA20081219#4173 1 20081219 A 5610 350A25902500 WINDSHIELD UROCOP EC130 EC130B4 8680989 EU COCKPIT CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 824MH 1772 4173 WINDSCREEN FOUND CRACKED DURING PREFLIGHT INSPECTION. A NEW WINDSCREEN WAS INSTALLED. SUGGEST THAT A FORM OF REINFORCEME NT BE ADDED TO THE WINDSCREEN EDGES OR AN ALTERNATE AND MORE FLEXIBLE ADHESIVE SYSTEM BE DEVELOPED TO ALLOW FOR PLEXIGLA SS EXPANSION AND CONTRACTION WITH SEASONAL TEMPERATURE CHANGES. COLD WEATHER SEEMS TO BE A CONTRIBUTING FACTOR AS MOST C RACKS DEVELOP BELOW 40 DEGREES FAHRENHEIT. EXTRA CARE IN TRIMMING AND FINISHING OF THE WINDOWS EDGES BEFORE INSTALLATION IS ENCOURAGED. 1 G 7 2 3U H9EU 20090108 NM 2009 1 8 MYWA081512 1 20081215 A 2130 PRESSURE SYSTEM BOEING 737 73781Q 13844GE NM CABIN MALFUNCTIONED A MYWA B G A EMER. DESCENT O2 MASK DEPLOYED UNSCHED LANDING O OTHER CR CRUISE 1 SO 29 733MA 30619 ACFT WAS ON A FERRY FLIGHT WITH ONLY CREW AND NO PASSENGERS THAT DEPARTED AND EXPERIENCED A RAPID DECOMPRESSION. AT FL41 0 CRUISE, THE RT ENGINE BLEED TRIP LIGHT ILLUMINATED. WHEN RESET LIGHT WENT OUT FOR APPROX 20 SECONDS AND LIGHT ILLUMINA TED AGAIN. ACFT COULD NOT MAINTAIN CABIN PRESSURE FOR SAFE OPERATION. CREW COMPLIED WITH NON-NORMAL PROCEDURES AND DID A RAPID DECENT TO 10,000 FEET. OXYGEN MASKS WERE DEPLOYED. FLIGHT LANDED SAFELY WITH NO ACFT DAMAGE OR PERSONNEL INJURY. 2 L 7 2 4F RT A16WE 20090108 EA 2009 1 8 N6WA200812213 1 20081221 A 3350 BATTERY CNDAIR CL600 CL6002C10 1390015 EA CABIN DISCHARGED A N6WA K NONE O OTHER IN INSP/MAINT 1 CE 03 152GJ 10224 ON PREFLIGHT TEST OF EMERGENCY LIGHTS INDICATED POSSIBLE DRAINED BATTERIES. OPS CHECK EMERGENCY LIGHTS IAW AMM 33-51-00 . 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 N6WA20081201 1 20081217 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A N6WA K NONE L NO TEST IN INSP/MAINT 1 CE 03 163GJ 10255 EMERGENCY LIGHTS INOP, FERRIED. 2 L 7 2 4F RT A21EA 20090108 NE 2009 1 8 P4Y2008F00004 2 20080908 A 7250 31081251 TURBINE BLADES CASA C212 C212200 2410304 EU GARRTT TPE331 TPE33110R 29064 NE ENGINE FAILED E P4YA K NONE O OTHER IN INSP/MAINT 1 EA 39 962BW 1871 000322901020 290 HAVE RECEIVED AN ENGINE THAT HAS SUFFERED AN INFLIGHT FAILURE AND SHUTDOWN. UPON INITIAL INVESTIGATION WE HAVE IDENTIFI ED THAT A 1ST STAGE TURBINE WHEEL BLADE APPEARS TO HAVE FAILED IN THE ROOT AREA. THIS BLADE HAS CAUSED SUBSTANTIAL DAMA GE TO THE REMAINDER OF THE 1ST STAGE WHEEL AND ALL COMPONENTS DOWNSTREAT OF IT. THE ENGINE WAS LAST IN OUT SHOP ON 15TH MAY, 2006 WHEN A CAM INSP WAS PERFORMED AT 8894.3 TSN, 10114 CSN. THE SUSPECT 1ST STAGE WHEEL WAS REPLACED AT THAT TIM E WITH AN OVERHAULED ITEM FROM MFG WHICH HAD NEW BLADES. (K) 2 H 7 2 4T 4 T RT A43EU E4WE 20090107 NM 2009 1 7 UALA2008122907020 1 20081227 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EXIT LIGHT INOP JUST AFT OF ROW 2 CEILING LIGHT. RELAMPED, CHECKS OK 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008122907021 1 20081227 A 3350 794640 WIRE HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EXIT LIGHT INOP ACROSS DOOR 3 LT LOWER WALL. REPAIRED FEED HARNESS. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008123007039 1 20081230 A 3350 1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT LIGHT INOP AT DOOR 5 RT BUSTLE LIGHT. REPLACED LIGHT ASSY. OPS CKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008120506759 1 20081204 A 5210 UNKNOWN MECHANISM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR WORN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 579UA 26697 MED 1 RT EMER. TRIGGER MECH. WORN. REPLACED EMERGENCY TRIGGER. 2 L 7 2 4F 4 F RT A2NM E17NE 20090107 NM 2009 1 7 ASAA0944140 1 20081215 A 5753 6546486149 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU MIDFLAP DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 LT IB MID FLAP T/E WEDGE IS DELAMINATED UPPER SURFACE CENTER. REMOVED DAMAGED AREA FABRICATED REPAIR PARTS BONDED REPAIR IAW SRM 51 70 10 REP 4. 2 L 7 2 4F 4 F RT A16WE E21EU 20090107 NM 2009 1 7 ASAA0944141 1 20081214 A 5753 65C357051 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FOREFLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 LT OB FORE FLAP IB LEADING EDGE IS CHAFED. REMOVED DAMAGED AREA FABRICATED HEAT TREATED AND INSTALLED REPLACEMENT SKIN I AW SOPM 20 50 01. 2 L 7 2 4F 4 F RT A16WE E21EU 20090107 NM 2009 1 7 ASAA0944142 1 20081214 A 5753 65C2632018 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU MIDFLAP CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 RT OTBD MID FLAP CHAFED ABOVE NR 7 FLAP TRACK FAIRING. REMOVED DAMAGED AREA FABRICATED REPAIR PARTS AND BONDED REPAIR IA W SRM 51 70 10. 2 L 7 2 4F 4 F RT A16WE E21EU 20090107 NM 2009 1 7 FDEA200812175194 1 20081217 A 5313 7075T6040C STRINGER BOEING 757 75723A 1384967 NM BS 395-436 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 918FD 24290 MAIN EQUIPMENT CENTER, ZONE 119, STA 420, S23L HAS CORROSION. REMOVED AND FABRICATED NEW STRINGER SECTION ON MAE TRAVEL ER NR T8/759394, DRILLED, TREATED, PRIMED AND INSTALLED NEW STRINGER SECTION ON S23L BETWEEN STA 395 TO 436 IAW SRM 51-4 0-02, SRM 53-00-03, FIG 101, DETAIL 2. THIS IS A MAJOR REPAIR NR 2 AND CATEGORY "A". 2 L 7 2 4F RT A2NM 20090107 NM 2009 1 7 QXEA2008122601257 1 20081224 A 3297 471515 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM NLG WOW FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 19 406QX 4048 SEA - UPON SELECTION OF GEAR UP, AFTER TAKEOFF, GEAR 3 GREEN LIGHTS REMAINED ILLUMINATED, 3 RED INDICATORS ILLUMINATED A ND GEAR HANDLE ILLUMINATED. RAN 'GEAR WOULD NOT RETRACT' AND 'ALT GEAR EXTENSION' CHECKLIST. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. REMOVED AND REPLACED NLG WOW HARNESS. ALL CHECKS GOOD. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20090107 EA 2009 1 7 QXEA2008122601260 1 20081224 A 3260 895303 PSEU CNDAIR CL600 CL6002C10 1390015 EA ZONE 200 MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 19 603QX 14151 10011 "PROX SYSTEM" CAUTION MSG AFTER GEAR RETRACTION, REMAINED ON FOR 10-15 MIN. THEN EXTINGUISHED DURING CRUISE. TOWED TO GATE AFTER LANDING. INTERROGATED MDC AND FOUND 'LDG SEL VLV - EXTEND SOL D043/63 FAILED/WIRING' AND 'LDG GEAR HANDLE, RE TRACT SWITCH D102/06 FAILED/WIRING. HISTORY SHOWS THAT BOTH FAULTS HAVE APPEARED NUMEROUS TIMES TOGETHER. BOTH LANDING GEAR SELECTOR VALVE AND LANDING GEAR HANDLE HAVE BEEN CHANGED WITH FAULTS RETURNING. CHECKED WIRING BETWEEN LDG GEAR HANDLE AND PSEU WITH MULTIMETER AND MEGGER. CHECKED WIRING BETWEEN PSEU TO LANDING GEAR SELECTOR VALVE WITH MULTIMETER AND MEGGER. CHECKED WIRING BETWEEN SELECTOR VALVE AND LANDING GEAR HANDLE WITH MULTIMETER. NO WIRING DEFECTS FOUND. R 2 L 7 2 4F RT A21EA 20090107 NM 2009 1 7 QXEA2008122601264 1 20081224 A 3240 BRAKE SYS BOMBDR DHC8 DHC8402 1390042 NM MLG MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 19 401QX 4031 ON LANDING BRAKES INEFFECTIVE. C/W FUNCTIONAL TEST OF THE ANTI-SKID SYS IAW AMM TASK 32-46-00-720-802. FUNCTIONAL TEST GOOD. INTEGRATED CDS FOR ANTI-SKID FAULTS. NO FAULTS NOTED. PERFORMED BLEED AND REMOVED AIR FROM THE MAIN BRAKE SYS TEM (NR 1) IAW AMM TASK 32-42-00-870-801. PERFORMED FUNCTIONAL TEST OF THE MAIN LANDING GEAR BRAKE SYSTEM IAW 32-42-00- 720-801. ALL BRAKE PRESSURES FOUND WITHIN LIMITS. NO DEFECTS NOTED. PERFORMED TAXI CHECK OF ACFT AT VARIOUS SPEEDS AN D BRAKING FORCES. COULD NOT DUPLICATE DISCREPANCY. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20090107 NM 2009 1 7 C8GA20080074 1 20081027 A 5320 SUPPORT ANGLE BOEING 727 727223 1384074 NM PWA JT8 JT8D NE FUSELAGE CORRODED A C8GA O OTHER O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE SUPPORT ANGLE LOCATED ABOVE STRINGER 26R AT BS 558 HAS SURFACE C ORROSION. REMOVED CORRODED SUPPORT ANGLE AND FABRICATED SUPPORT ANGLE FROM 7075 O -.040 INCH (9 INCHES X 4.5 INCHES) HEA T TREATED TO T6. INSTALLED SUPPORT ANGLE. IAW SRM 53-10-2, 51-30-2. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE . 2 L 7 3 4F 4 F A3WE E2EA 20090107 NM 2009 1 7 C8GA20080075 1 20081020 A 5320 70750 ANGLE BOEING 727 727223 1384074 NM PWA JT8 JT8D NE FUSELAGE CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE L-ANGLE LOCATED BETWEEN STRINGER 27L - 28L IS CORRODED AT STA 74 0. REMOVED CORRODED L-ANGLE AND FABRICATED NEW FROM 7075 O -.090" (10.6250 INCH X 7.6258 INCH)HEAT TREATED TO T6. INSTAL LED (L) ANGLE. IAW DRAWING NR 65-15940 AND SRM 51-30-2. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 20090107 NM 2009 1 7 C8GA20080076 1 20081020 A 5320 ANGLE BOEING 727 727223 1384074 NM PWA JT8 JT8D NE FUSELAGE CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 WHILE IN HEAVY MX, PERFORMING INSP IT WAS NOTED THAT AN L-ANGLE LOCATED AT STA 740 STR 27R-28R WAS CORRODED. REMOVED DAM AGED ANGLE AND FABRICATED NEW ANGLE FROM 7075-O .190 INCH (12 INCH X 10.5 INCH) HEAT TREATED TO T6. INSTALLED L-ANGLE IA W 727 DRAWING NR 65-15940 AND 51-30-2. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 20090107 NM 2009 1 7 C8GA20080077 1 20081010 A 5322 SHEAR TIE BOEING 727 727223 1384074 NM PWA JT8 JT8D NE FUSELAGE CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 NA WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT SHEAR TIE LOCATED AT STA 620 STRINGER 26L-27L WAS CORRODED. REMOVED DAMAGED SHEAR TIE. FABRICATED NEW SHEAR TIE FROM BAC 1506-1630 7075-T6 (6.75 INCHES) INSTALLED SHEAR TIE IAW 51-30-2, 53 -10-2. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 20090108 NM 2009 1 8 QXEA2000901060128 1 20081230 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 415QX 4081 PDX - C3 - RT INBD CABIN SEAT TRACK IS CORRODED AT STA X0.0 ON TOP OF SURFACE OF OTBD SUPPORT FLANGE AND ADJACENT OTBD SIDE SURFACE OF TRACKING LUG. REMOVED CORROSION FROM TOP SURFACES OF OTBD SUPPORT FLANGE BY BLENDING IAW RD 8/4-53-884 PAGE 6 GENERAL NOTES 1 AND 3. MAX MATERIAL REMOVED WAS .022 INCH BLEND IS OUT OF LIMITS IAW RD 8/4-53-884. HFEC INSPEC TED BLENDED AREA FOR CRACK IAWS D-8 400 NDTM PART 6, 51-00-01, NO CRACKS NOTED. RE PROTECTED REPAIR AREA W/ALODINE PRIM ER AND PAINT REF RD 8/4-53-2592. 2 H 7 2 4T RT A13NM 20090108 EU 2009 1 8 FDEA200812205252 1 20081220 A 3230 PIN AIRBUS 300 A300F4605R 3930327 EU LT BOGIE BINDING A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 679FE 793 LANDING GEAR LEVER WOULD NOT GO UP PAST THE OFF POSITION IN SYS 1 OR SYS 2. CHECKED PSEU ON ARRIVAL FOUND FAULT LIGHT ON WITH FAULT CODE "BL" BOGIE LT FAIL. VERIFIED FAULT ON PROX BOX "BL",GREASED LT BOGIE AND JACKED ACFT (NITROGEN DESE RVICE OF L/R BOGIE TRIM CYL. UNDER SEP. WRI) AND PLACED FLOOR JACK UNDER FWD JACK PAD OF LT BOGIE. BOGIE WOULD NOT PIVOT VERY EASILY, REMOVED LOWER TRAY ON THE LT BOGIE AND REMOVED PROX SENSOR HSG ASSY. BOGIE PIVOTS BY HAND NOW. THE BOGIE PIN IS DRAGGING/TIGHT ON THE LEG BRGS. REMOVED BOGIE PIN CLEANED ALL OLD AND DRIED UP GREASE NO DAMAGE FOUND ON PIN O R BUSHINGS. REINSTALLED PIN GEAR PIVOT IS GOOD. PERFORMED GEAR RETRACT AND INHIBIT TEST IAW MM 32-31-00 CHECKS OK. PIN 2 L 7 2 4F RT A35EU 20090107 NM 2009 1 7 DHLA2008743528 1 20081109 A 5311 FRAME BOEING 727 727225 1384077 NM BS 970 S26L DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 D-CHECK, WO NR 5740, NR 5740-1-137 LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 970 STR 26L FRAME WITH DENT. REPAIRED FU SELAGE SECTION AT BS970 BETWEEN STR.25L AND 27L DUE TO DENT IAW SRM 51-40-3 FIG.1 2 L 7 3 4F A3WE 20090107 NM 2009 1 7 DHLA2008743520 1 20081112 A 5311 FRAME BOEING 727 727225 1384077 NM BS 1010 S16-17R DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 D-CHECK, WO NR 5740 NR 5740-2-299, UPPER FUSELAGE PAX CABIN AT BS 1010 BETWEEN STR 16R AND 17R FRAME WEB WITH DOUBLE HOL E. REPAIRED FUSELAGE FRAME SECTION AT BS 1010 BETWEEN STR 16R AND 17R DUE TO DOUBLE HOLE IAW SRM 51-40-3 FIG.1. 2 L 7 3 4F A3WE 20090107 NM 2009 1 7 UALA2008122907019 1 20081227 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EXIT LIGHT INOP UPPER DECK ROW 17 LT AFT LIGHT ASSY. RELAMPED, CHECKS OK 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008122907024 1 20081227 A 2820 7G1018600U PRESSURE SWITCH BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE FUEL SYSTEM FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 670UA 29240 BEFORE PUSHBACK CREW NOTICED LT CTR FUEL OVRD PUMP LOW PRESSURE LIGHT NOT ILLUMINATED ON THE GROUND. NEEDS LOW PRESSURE FUEL BOOST PUMP PRESSURE SWITCH. OPS CHECKED OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20090107 EU 2009 1 7 UALA2008122907034 1 20081226 A 2611 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E&E BAY FALSE ACTIVATION A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 467UA 1359 AVIONICS MSG RCV'D. SUSPECT HUMIDITY SET OFF THE ALARM. MSG WAS NOT PRESENT WHEN MECH ARRIVED. PERFORMED AEVC TEST AN D SDCU TEST AND TESTED OK. CHECKED AVIONICS BAYS FOR SMOKE AND NONE FOUND. NO BURNING ODOR EITHER. 2 L 7 2 4F 4 F RT A28NM E40NE 20090107 NM 2009 1 7 UALA2008123007044 1 20081229 A 2530 OVEN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY CONTAMINATED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 644UA 25094 ELECTRICAL ODOR IN CABIN. FLIGHT DIVERTED. DOOR AREA HEATER CB PULLED R12 ON OVERHEAD P11 PANEL TO SEE IF ODOR GOES A WAY. THERE IS NO SIGN OF ANY SMOKE. REPLACED RT AFT DOOR HEATER. WARMING OVEN DIRECTLY BELOW W51 HAD MELTED PLASTIC INS IDE CAUSING BURNED ODOR IN AFT GALLEY. CLEANED OUT OVEN AND RAN FOR SEVERAL HOURS. CHECKS OK. REPLACED OVEN. 2 L 7 2 4F 4 F RT A1NM E24NE 20090107 WP 2009 1 7 DJFA2008088 2 20081229 A 7261 OIL CAP RAYTHN DH125 HAWKER800XP 7150012 CE GARRTT TFE731 TFE7315BR WP ENGINE MISSING E DJFA E ENGINE SHUTDOWN W K J INADEQUATE Q C FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 23 829LX 258466 P107476 DURING FLIGHT NR1 ENGINE LOW OIL PRESSURE WARNING ILLUMINATED. CREW SHUT DOWN THE NR 1 ENGINE AND DIVERTED. ACFT LANDE D SAFELY. MX FOUND THE OIL SERVICING CAP NOT INSTALLED. THE OIL RESERVOIR WAS EMPTY AND OIL WAS FOUND COVERING THE EXTE RIOR OF THE ENGINE. MX SERVICED THE OIL AND IS PERFORMING AN OIL "SOAP" ANALYSIS USING RESIDUAL OIL FROM INSIDE THE ENG INE. ACFT WILL BE RELEASED PENDING THE OUTCOME OF THE "SOAP" ANALYSIS. 2 L 7 2 4F 4 F RT A3EU E6WE 20090107 NM 2009 1 7 UALA2008123107061 1 20081231 A 3350 767 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 526UA 24994 RT FWD OVER WING SLIDE EMERGENCY EXIT LIGHT INOP. RELAMPED, OPS CK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20090107 NM 2009 1 7 UALA2008123107062 1 20081231 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 597UA 28750 NR 1 RT FWD DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED, OPS CHECK OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20090107 NM 2009 1 7 USAA2009010290006 1 20081219 A 5752 654645522C TAB BOEING 737 7374B7 138449C NM RT AILERON DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT Q5 MAJOR REPAIR NR 03C40627011/002 RT AILERON TAB SEPARATED AT OTBD END. REPLACED RT AILERON TAB & INSTALLED ON US A IRWAYS TASK CARD NR 03C40627010. 2 L 7 2 4F RT A16WE 20090107 NM 2009 1 7 USAA2009010290007 1 20081228 A 5754 65C26603101 SKIN BOEING 737 7374B7 138449C NM LE SLAT CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT Q5 MAJOR REPAIR NR 03C30257005/001 CRACKS IN NR 3 SLAT LOWER SKIN AT OTBD AUXILIARY TRACK. REPAIRED NR 3 SLAT LOWER SKIN IAW B737 SRM 57-43-01. 2 L 7 2 4F RT A16WE 20090107 NM 2009 1 7 USAA2009010290008 1 20081226 A 5313 65516989 STRINGER SPLICE BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT Q5 MAJOR REPAIR NR 03C10725040/001 STRINGER SPLICE CRACKED AT BS907, S4R. REPLACED STRINGER SPLICE AT BS907, S4R IAW B737 SRM 51-10-2. 2 L 7 2 4F RT A16WE 20090107 NM 2009 1 7 USAA2009010590021 1 20081223 A 5315 6546811 FLOORBEAM BOEING 737 7374B7 138449C NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT Q5 MAJOR REPAIR NR 03C10853057/002 LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT BS986.5, LBL11.5 TO LBL26.5. REP LACED FLOORBEAM AT BS986.5, LBL11.5 TO LBL26.5 IAW B737 SRM 51-40-02, 53-60-01 REV A & US AIRWAYS TYPICAL REPAIR NR 53-6 0-01. 2 L 7 2 4F RT A16WE 20090107 WP 2009 1 7 FDEA200812175190 1 20081217 A 7830 34H40600 CLAMP DOUG MD10 MD1010F 3022112 WP THRUST REVERSER FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 550FE 46521 AFTER TAKEOFF AT 500 FT, FELT A LOUD "THUMP" LIKE A BIRDSTRIKE. THIS WAS FOLLOWED BY AN INDICATION OF NR 3 BLEED CLOSED (VALVE WAS SELECTED OPEN). THIS WAS FOLLOWED BY A "REV 3 PRESS FAULT". T/R WAS 'NOT' UNLOCKED. ALL OTHER ENGINE INDICA TIONS WERE NORMAL. THRUST REVERSER OPERATED NORMALLY ON LANDING. REV 3 PRESS FAULT REMAINED AFTER T/R WAS STOWED. WHIL E PARKING ACFT, NOTICED BLOWOUT DOOR ON THE BOTTOM OF THE NR 3 ENGINE OPEN. FOUND BAND CLAMP FAILED BETWEEN PRESSURE R EGULATOR VALVE AND HSV. NR 3 LT THRUST REVERSER DAMAGED BY PRESSURE REGULATOR VALVE. NEEDS THRUST REVERSER, HSV, PRV, D UCTS AND SENSE LINES. REMOVED AND REPLACED NR 3 ENG. HP BLEED CONTROL VALVE PER MM 36-11-02-4, AND REG PNEU PRESS VALVE 2 L 7 3 4F RT A22WE 20090107 NM 2009 1 7 QXEA2008122401254 1 20081220 A 6123 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM PROPELLER MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 19 412QX 4059 SEA - AUTOFEATHER SELECT DID NOT INDICATE ON EICAS DISPLY DURING T/O ROLL. ABORTED AT 60 KIAS, AND RETURNED TO THE GATE . INTERROGATED CDS, FOUND CODES 64 AND 70. PERFORMED AUTOFEATHER TEST IAW AMM TASK 61-20-00-710-801. FAULTS CLEARED I N CDS. NO FURTHER MTX ACTION REQUIRED PER FIM TASKS 61-20-02-810-834 AND 61-20-02-810-835. OPS CHECK OF AUTOFEATHER GO OD. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20090107 EU 2009 1 7 FDEA200812175191 1 20081217 A 3230 224TS05Y CONTROL MODULE AIRBUS 310 A310222 3930315 EU MLG MALFUNCTIONED A FDEA F ACTIVATE FIRE EXT. J WARNING INDICATION CL CLIMB 1 CE 21 453FE 267 AFTER T/O LANDING GEAR WOULD NOT RETRACT. THIS WAS CONFIRMED ON OVHD PANEL AS WELL. INTERROGATED MTP AND GOT 28V GEAR PWR SUPPLY 1 LOSS LOGGED AND LIKEWISE FOUND RELAYS AND RETRACT CTL CB OF LDG PROX DETECTOR POPPED OUT. FOLLOWED T/S PE R TSM 32-30-00 FIG 109 AND RESET SAID CB, NO POPPING OUT AND UNABLE TO DUPLICATE THIS TIME. PERFORMED NORMAL EXTENSION AND RETRACTION ADJ/TEST USING LDG SAFETY RELAY SIMULATOR TEST SET AND DUPLICATED POPPING OF CB IN FLIGHT CONFIGURATION. FURTHER T/S FOUND LDG GEAR CTL MODULE DEFECTIVE. REMOVED AND REPLACED LDG GEAR CTL MODULE PER MM 32-31-11. PERFORMED OPS TEST PER MM 32-31-00-5, SATISFACTORY AND NO CB POPPING OUT NOTICED ON BOTH SYSTEM 1 AND 2. 2 L 7 2 4F RT A35EU 20090107 EU 2009 1 7 FDEA200812175192 1 20081217 A 3260 BDM3003 PROXIMITY SENSOR AIRBUS 300 A300F4605R 3930327 EU MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 674FE 781 LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF IN POSITION DET SYS 1 OR SYS 2. REPLACED RELAY 20ES FOUND BAD ON PREVIOUS T/S. SWUNG GEAR IN SYSTEM 1 AND 2 REF AMM 32-61-00-5. BOTH SYSTEMS CHECK GOOD. DOWN JACKED ACFT , NEEDS PROX BOX DET BITE TEST WHEN POWER RESTORED. REPLACED AND TESTED GEAR PROX BOX PER AMM 32-31-71-4. TESTS OK. JACKED ACFT AGAIN AND SWUNG GEAR 2 TIMES ON EACH CHANNEL WITH NORMAL INDICATION AND NO FAULTS NOTED. 2 L 7 2 4F RT A35EU 20090107 NM 2009 1 7 QXEA2008122601258 1 20081221 A 2130 CABIN PRESSURE BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 19 402QX 4032 DURING CLIMB OUT OF BOI CABIN INDICATOR WENT OFF THE SCALE UP THEN REVERSED AND WENT FULL SCALE DOWN THE PRESSURIZED NOR MALLY FOR A FEW MINUTES. IT STARTED CLIMBING RAPIDLY UPWARD AGAIN AT WHICH TIME WE RAN THE PRESSURIZATION FAIL CHECKLIS T, WENT TO MANUAL CONTROL AND IT STARTED TO WORK NORMALLY AGAIN. INTERROGATED CDS ECS AND CPCS. NO FAULTS NOTED. PERF ORMED OPERATIONAL CHECK OF THE AUTO PRESSURIZATION CONTROL FAULT INDICATION. REF AMM TASK NR 21-31-00-710-802. NO FAU LT NOTED. INSPECTED ACFT DOOR SEALS NO DEFECTS NOTED AT THIS TIME. PERFORMED FUNCTIONAL TEST OF THE PRESSURIZATION CON TROL. REF AMM TASK 21-31-00-720-801. OPS TEST GOOD. NO FLUCTUATIONS NOTED DURING CHECK. ACFT OK FOR SERVICE. NO PART 2 H 7 2 4T RT A13NM 20090107 NM 2009 1 7 C8GA20080078 1 20081010 A 5322 SHEAR TIE BOEING 727 727223 1384074 NM PWA JT8 JT8D NE FUSELAGE CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT SHEAR TIE LOCATED AT STA 640 STRINGER 26L-27L WAS CORRODED. REMOVED DAMAGED SHEAR TIE. FABRICATED NEW SHEAR TIE FROM BAC 1506-1630 7075-T6 (6.75 INCH) INSTALLED SHEAR TIE IAW 51-30-2, 53-1 0-2. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 20090107 NM 2009 1 7 C8GA20080079 1 20081010 A 5322 SHEAR TIE BOEING 727 727223 1384074 NM PWA JT8 JT8D NE FUSELAGE CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT SHEAR TIE LOCATED AT STA 660 STRINGER 26R-27R WAS CORRODED. REMOVED DAMAGED SHEAR TIE. FABRICATED NEW SHEAR TIE FROM BAC 1506-1630 7075-T6 (6.5 INCH) INSTALLED SHEAR TIE IAW 51-30-2, 51-10 -2. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 20090108 EA 2009 1 8 SWIA200820750 1 20081228 A 3350 COVER CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 771SK 10244 FLT 6669 - GALLEY FLOOR LEVEL FLOOD LIGHT COVER BROKE MISSING. REPLACED GALLEY FLOOR EMERGENCY FLOODLIGHT. 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 SWIA200820752 1 20081229 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 748SK 10203 FLT 6929 - NR 2 EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 SWIA200820753 1 20081230 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 716SK 10180 FLT 6265 - EXIT ROW LIGHT AT MAIN CABIN DOOR AND RIGHT SIDE EMERGENCY EXIT ROW 12 INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 SWIA200820755 1 20081229 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 932SW 7714 FLT 6038 - VARIOUS EMERGENCY CEILING LIGHTS INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 SWIA200820758 1 20081224 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 742SK 10197 FLT 5889 - BOTH "EXIT" SIGNS AT THE FLOOR LEVEL HAVE AN INOP BULB. RELAMPED. 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 SWIA200820762 1 20081206 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA LT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 925SW 7682 DURING C-CHECK, LEFT ENGINE AFT THRUST MOUNT CORRODED. REPLACED. 2 L 7 2 4F RT A21EA 20090108 2009 1 8 QXEA2008010201273 4 20081231 A 6122 697072003 GOVERNOR BOMBDR DHC8 DHC8402 1390042 NM DOWTY R4086 R4086123F17 EU PROPELLER FAILED A QXEA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 19 416QX 2775 4083 SEA - NR 2 PROP SLOW TO UNFEATHER. REMOVED AND REPLACED NR 2 OVERSPEED GOVERNOR IAW AMM TASKS 61-20-26-000-801 AND 61-2 0-26-400-801. PERFORMED OPS TEST OF THE OVERSPEED GOVERNOR IAW TASK 61-20-00-710-803 AND FUNCTIONAL TEST OF PROP TIME T O UNFEATHER IAW TASK 61-20-00-720-801. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 6 C P17BO 20090108 EU 2009 1 8 FDEA200812185206 1 20081218 A 5312 A5381109320000 FITTING AIRBUS 310 A310203 3930313 EU S34L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 AFT PIT FWD BULKHEAD AT S34L, END FITTING CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-15-14 FIG 7 SHEET 2. REMOVED FITTING IAW SRM 51-40-21. RECEIVED NEW FITTING LOCATED & DRILLED NEW FITTING IAW DWG A53811093. IN STALLED FITTING IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812185208 1 20081218 A 5312 A5381109320000 FITTING AIRBUS 310 A310203 3930313 EU S36L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 38333 248 AFT PIT FWD BULKHEAD AT S36L, END FITTING CORRODED. REMOVED CORROSION; FOUND TO BE OUT OF LIMITS IAW SRM 53-15-14; FIG 7; SHEET 2. REMOVED FITTING IAW SRM 51-40-21. RECEIVED NEW FITTING, LOCATED & DRILLED NEW FITTING IAW DWG A53811093. INSTALLED FITTING IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812185209 1 20081218 A 5312 BULKHEAD AIRBUS 310 A310203 3930313 EU S37L CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 AFT PIT FWD BULKHEAD AT S37L, END FITTING CORRODED. REMOVED CORROSION; FOUND TO BE OUT OF LIMITS IAW SRM 53-15-14; FIG 7; SHEET 2. REMOVED FITTING IAW SRM 51-40-21. RECEIVED NEW FITTING, LOCATED & DRILLED IAW DWG A53811093. INSTALLE D FITTING IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20090108 NM 2009 1 8 FDEA200812265298 1 20081226 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 7 SUPPORT FITTING AT HOLES NR B, NR C AND NR D. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIE D AS MAJOR AS PER GMM 6-2- 100. 2 L 7 3 4F RT A22WE 20090108 WP 2009 1 8 FDEA200812185222 1 20081218 A 5311 ABA73483 FRAME DOUG DC10 DC1030F 3023504 WP ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 317FE 46835 DURING INSPECTION ON AVIONIC COMPT FOUND CRACK ON FRAME. 2 L 7 3 4F RT A22WE 20090108 WP 2009 1 8 FDEA200812185223 1 20081218 A 5311 ABA73483 FRAME DOUG DC10 DC1030F 3023504 WP ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 317FE 46835 DURING INSPECTION ON AVIONIC COMPT FOUND DEEP WEAR ON FRAME. 2 L 7 3 4F RT A22WE 20090108 EA 2009 1 8 SWIA200820764 1 20081216 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 979SW 7682 C-CHECK, FS 280 LBL 11-13 LOWER FLOORBEAM FLANGE CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 SWIA200820765 1 20081216 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 979SW 7954 C-CHECK, FS 280 RBL 9 INBOARD FLOORBEAM CRACKED. REPLACED. 2 L 7 2 4F RT A21EA 20090130 EA 2009 1 30 HNAA2009012500018 1 20081016 A 5347 85331409 SEAT TRACK DHAV DHC3 DHC3 2800202 EA ZONE 100 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 327EN 30485 30485 261 RT INBD SEAT RAIL CORRODED FROM STATION X 423 TO X 588. FABRICATED LT HAND AND RT IAW DRAWING 85331406. USED ON ALODIN E SURFACE IAW ESR 07-07-3003. 1 H 7 1 3R A815 20090108 EU 2009 1 8 FDEA200812185200 1 20081218 A 5321 FXSRZ25005252YS FLOOR PANEL AIRBUS 310 A310 EU ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 38333 248 FLOORBOARD 252YG IS CRACKED. FR 62 - 65 RT. REPAIRED FLOORBOARD BY FABRICATING A NEW FLOORBOARD FROM STOCK MATERIAL US ING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ20-005; REV " G ". 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812205247 1 20081220 A 5321 FXSRZ25005131ZF FLOOR PANEL AIRBUS 310 A310 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 FWD CARGO PIT FLOOR PANEL 131 ZF IS DAMAGED. FABBED NEW PANEL USING THE OLD PANEL AS A TEMPLATE. MATERIAL ID; LOCATED H OLES USING THE THE OLS PANEL; COUNTERBORED HOLES; POTTED & SANDED EDGE; INSTALLED INSERTS; APPLIED ANTI-SKID & PA RT MARKED IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812185201 1 20081218 A 5321 FXSRZ25005232HG FLOOR PANEL AIRBUS 310 A310 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 38333 248 FLOOR PANEL BROKEN ON THE END ( 232HG ). REPAIRED FLOOR PANEL 232 HG BY FABRICATING A NEW FLOOR PANEL FROM STOCK MATER IAL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ20-005; REV " G ". 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812185202 1 20081218 A 5321 FXSRZ25005252BG FLOOR PANEL AIRBUS 310 A310203 3930313 EU ZONE 200 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 38333 248 FLOORBOARD 252BG DELAMED LWR. SURFACE FR 65 - 69 R/H. REPAIRED FLOOR PANEL 252 BG BY FABRICATING A NEW FLOOR PANEL FROM STOCK MATERIAL USING THE OLD PANEL AS A TEMPLATE IAW FEDEX DWG SRZ20-005; REV " G ". 2 L 7 2 4F RT A35EU 20090108 NM 2009 1 8 FDEA200812195243 1 20081219 A 5330 651842018 SKIN BOEING 727 727233 138408A NM BS 185 BULGED A FDEA O OTHER O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 EXTERIOR FUSELAGE SKIN BULGE SAT 185, STR 24L CUTOUT DAMAGED AREA IAW SRM 53-30-3 FIG 14. FABRICATED REPAIR PART AND DOU BLER IAW SRM 53-30-3 FIG 14. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-30-3 AND 51-30-2. 2 L 7 3 4F RT A3WE 20090108 EU 2009 1 8 FDEA200812175231 1 20081217 A 2897 WIRE AIRBUS 300 A300F4605R 3930327 EU FUEL QTY DISCONNECTED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 668FE 772 DURING CLIMB-OUT, ABOUT 10,000, LT OUTER FUEL QTY BEGAN TO DECREASE. CENTER TANKS (BOTH) FAULTED EVEN THOUGH 400 LBS PR ESENT OR INDICATED. LT OUTER DECREASED TO BELOW 1,000 LBS. DURING DESCENT, LT OUTER FUEL QTY INDICATION BEGAN TO INCR EASE RISING TO 3,400 LBS BY 10,000 FT. LT OUTER TANKS INDICATED NEAR FULL BY SHORT APPROACH. TOTAL FUEL QTY REFLECTED FLUCTUATING LT OUTER INDICATIONS. BOTH ECAM & OVHD PANEL PRODUCED ACCOMPLISHED FQIC BITE TEST. AFTER BITE TEST, RESET FQIC. PERFORMED LT OUTER INDIVIDUAL PROBE CAPACITANCE & RESISTANCE CHECK IN REF TO AMM28-42-00-5. ALL PROBE CAP AND RE SISTANCES WITHIN LIMITS. MEGGED WIRING FROM 563VCA TO FQIC ALL WIRING CHECKED GOOD. CONDUCTOR (-W OF 563VCA). DEPINNE 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812195234 1 20081219 A 5415 A5461175400300 FITTING AIRBUS 310 A310 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 NR 2 PYLON TO WING ATTACHMENT FITTING LUG INNER RACE BEARING AT RIB 18 RUSTED. R & R AFT ATTACH FITTING IAW AMM 54-51-7 5-4-02 TW - T8312G. 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812205246 1 20081220 A 5321 FXSRZ25005312BF FLOOR PANEL AIRBUS 310 A310 EU ZONE 100 DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 L/H TAIL COMPARTMENT FLOORBOARD IS DELAMINATED AT THE AFT CORNER ACCESS THRU 312 AR. FABBED A NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. MATERIAL ID; LOCATED HOLES; COUNTERBORED HOLES; POTTED & SANDED EDGE; INSTALLED INSERTS; A PPLIED ANTI-SKID & PART MARKED IAW DWG SRZ25-005: REV "G". INSTALLED FLOOR PANEL IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200811195300 1 20081119 A 5754 A5786325116300 SKIN AIRBUS 300 A300B4622R 3930312 EU LE SLAT DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 723FD 543 RT WING - (2) DENTS ON NOSE SKIN OF SLAT NR1 BETWEEN RIB 20 AND JACK RIB 2. THE SLAT NR1 WAS REPAIRED IAW EA 6-5750-1270 34. 2 L 7 2 4F RT A35EU 20090108 WP 2009 1 8 FDEA200812175189 1 20081217 A 5330 SM105300015 SKIN DOUG MD10 MD1010F 3022112 WP FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 75122 46631 RT FUSELAGE AT STA 1776 BETWEEN LONGERONS 39R AND 40R THE SKIN IS DENTED. REPAIR SKIN IAW E.A. 8-5330-123532 TITLE (FUSE LAGE DENT IN GROSS WEIGHT MOD DOUBLER AT STA 1816, L39R - L40R ). REMOVED AND REINSTALLED ACCESS PANELS IN THE PIT IAW SRM 57-31-01; VOL II. 2 L 7 3 4F RT A22WE 20090108 SO 2009 1 8 GAJ2008F00001 1 20081215 A 7810 LW16697 EXHAUST PIPE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA ENGINE CRACKED E GAJA K NONE O OTHER IN INSP/MAINT 1 NM 11 8006U 412 752003 FOUND EXHAUST FLANGE UNDER V-CLAMP CRACKED. FIRST SIGN OF PROBLEM WAS EXHAUST STAINS IN AREA. AFTER THE CLAMP WAS REMO VED THE FLANGE WAS FOUND CRACKED APPROXIMATELY 70 PERCENT OF TH4E CIRCUMFERENCE OF THE FLANGE. (K) 1 L 7 2 3O 3 O A20SO E14EA 20090108 NM 2009 1 8 FDEA200812185225 1 20081218 A 5330 65545755 SKIN BOEING 727 727233 138408A NM ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 DENT STA 720D, STR 18L. CUT OUT DAMAGED AREA DIM (1 7/8" X 7/8") IAW SRM 53-10-3 FIG 2. REMOVED FLOORBOARDS ROW "A" STA 720A TO 740 IAW SRM 51-30-2. FABRICATE REPAIR PARTS DOUBLER AND FILLER IAW SRM 53-30-2 FIG 2 AND 53-30-3 FIG 2. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2. INSTALLE 2 L 7 3 4F RT A3WE 20090108 SO 2009 1 8 GLBA200812221 1 20081219 A 3233 ACTUATOR EMB 120 EMB120ER 3260203 SO NLG OUT OF ADJUST A GLBA O OTHER J WARNING INDICATION LD LANDING 1 NM 21 293UX 120293 PILOTS REPORTED THAT THE NLG WAS SHOWING (2) RED, WHEN EXTENDING NORMALLY, THEY PERFORMED THE CHECKLIST FOR ELECTRICAL O VERRIDE AND IT DID NOT WORK. THEY THEN RAN THE CHECKLIST FOR GEAR EXTENSION BY FREEFALL. THIS STILL DID NOT WORK. THE W HOLE TIME (2) RED NO GREEN FOR NLG. IT THEN SHOWED 6 GREEN WHEN NLG TOUCHED. MX ADJUSTED NOSE GEAR ACTUATOR IAW EMB-120 MM 32-32-11. PERFORMED 30 GEAR EXTENSIONS AND RETRACTIONSWITH NO DEFECTS NOTED. OPS CHECK WAS GOOD. RII INSP COMPLIED W ITH OF THE NOSE GEAR ACTUATOR ADJUSTMENT IAW TASKCARD 4.3.7. OPS CHECK FLIGHT WAS SATISFACTORY. 2 L 7 2 4T RT A31SO 20090108 CE 2009 1 8 GLBA200812224 1 20081220 A 3234 CONTROL HANDLE BEECH 1900 1900D 1154162 CE COCKPIT DEFECTIVE A GLBA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 21 92SK UE92 SMELL/SMOKE/FUMES/SPARKS - PILOTS REPORTED THAT DURING PRE-FLIGHT CHECKS THEY NOTICED SPARKS BETWEEN THE GEAR HANDLE AND THE DOWN LOCK ARM. MX REMOVED AND REPLACED THE GEAR HANDLE ASSY PN 101-384137-7. PERFORMED GEAR SWINGS AND OPS CHECKS W ERE GOOD IAW MM 32-60. 2 L 7 2 4T RT A24CE 20090108 NM 2009 1 8 Q2SA783002 1 20081215 A 3411 PITOT LINE BOEING 747 747281F 13848AB NM GE CF6 CF650E2 30018 NE BROKEN A Q2SA A UNSCHED LANDING G S MULTIPLE FAILURE AFFECT SYSTEMS CL CLIMB 1 EA 63 783SA 23919 ON DEPARTURE FROM KJFK, CAPTAIN'S POSITION LOST ALL PRIMARY INSTRUMENTS (AIRSPEED, ALTITUDE, IVSI INDICATORS). AIR TURN BACK TO KFJK, NO FUEL DUMP PERFORMED. CADC REPLACED AND BROKEN PITOT LINE FOUND BEHIND CAPTAIN'S ALTIMETER. 2 L 7 4 4F 4 F RT A20WE E23EA 20090108 2009 1 8 FDEA200812195245 2 20081219 A 7397 8062127 WIRE DOUG MD10 MD1010F 3022112 WP NR 3 MEC BROKEN A FDEA E H ENGINE SHUTDOWN DEACTIVATE SYST/CIRCUITS J WARNING INDICATION DE DESCENT 1 CE 21 397FE 46631 NR 3 ENGINE HUNG START AT FL 25.0 AND DESCENDED TO 10000 FT STILL WOULD NOT ACCELERATE; SHUT DOWN ENGINE. IDLE READINGS : ENGINE 1 N1 38 PERCENT; EGT 362; N2 71.1 PERCENT, ENGINE 2 N1 39 PERCENT; EGT 362; N2 72.6 - ENGINE 3 N1 29 PERCENT; EGT 372; N2 50.5 PERCENT. REMOVED AND REPLACED THE NR 3 ENGINE MEC REF AMM 73-20-01-2. REPAIRED A BROKEN WIRE ON PL UG PL-8079 REF AMM 20-30-02-2. PERFORMED FLT IDLE ADJUSTMENT REF AMM 71-00-00-5. PERFORMED ENGINE RUN; LEAK AND BOPS CHECK GOOD. 2 L 7 3 4F RT A22WE 20090108 NM 2009 1 8 FDEA200812235267 1 20081223 A 5230 AFA3805505 SKIN DOUG MD11 MD11F 3023600 NM CARGO DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 CENTER CARGO DOOR LOWER FORWARD CORNER FOUND DOOR SKIN DAMAGED. CENTER CARGO DOOR LOWER FORWARD CORNER, DOOR SKIN DAMAG ED AREA REPAIR CARRIED OUT AS PER EA 1-5230-127702. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090108 NM 2009 1 8 FDEA200812245268 1 20081224 A 2751 18129942F1 INDICATOR BOEING 727 727233 138408A NM TE FLAPS FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 222FE 20933 ASSYMETRIC OUTBOARD TRAILING EDGE FLAPS DURING FLAP RETRACTION FROM FLAPS 2 TO FLAPS 0. REMOVED AND REPLACED OUTBOARD FLAP POSITION INDICATOR AND PERFORMED OPERATIONAL CHECK IAW AMM 27-52-021-2 ALL CHECK GOOD. OK FOR SERVICE. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG 18-1299-4-2F1. 2 L 7 3 4F RT A3WE 20090108 NE 2009 1 8 Q2SA753005 2 20081225 A 7320 665038901224 SENSOR BOEING 747 747228F 1384895 NM GE CF6 CF650E2 30018 NE NR 2 ENGINE FAILED A Q2SA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 EA 63 753SA 21787 517351 ON TAKE-OFF FROM LEIGE, BELGIUM (EBLG), NR 2 ENGINE FLAMED OUT. LOUD NOISE HEARD AND AIRCRAFT YAWED LEFT. IGNITION AND ENGINE ANTI-ICE IN USE. ENGINE RELIGHT AT 3000' AGL, ALL PARAMETERS NORMAL. AIRCRAFT CONTINUED TO DESTINATION AT DOHA , QATAR (OTBD). NO FUEL WAS DUMPED. ON INSPECTION, REMOVED/REPLACED COMPRESSOR INLET TEMPERATURE (CIT) SENSOR IN ACCOR DANCE WITH AMM, SYSTEM CHECKED GOOD. 2 L 7 4 4F 4 F RT A20WE E23EA 20090108 NM 2009 1 8 Q2SA758004 1 20081221 A 7830 THRUST REVERSER BOEING 747 747281F 13848AB NM GE CF6 CF650E2 30018 NE ZONE 400 DEPLOYED A Q2SA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 63 758SA 23138 517231 ON CLIMB-OUT FROM ADDIS ABABA, ETHIOPIA (HAAB), AIRCRAFT PERFORMED AN AIR TURN BACK DUE TO INDICATION OF NR 4 ENGINE THR UST REVERSER TRYING TO DEPLOY IN FLIGHT. CREW WAS ALERTED BY THRUST REVERSER VALVE LIGHT AND TRANSIT LIGHT ILLUMINATING . CREW RETURNED TO HAAB WITH REVERSER PARTIALLY DEPLOYED. NO FUEL WAS DUMPED. MAINTENANCE TOOK ACTION TO LOCK OUT THR UST REVERSER AND SCHEDULE FOR APPROVED DEFERRED MAINTENANCE ACTION. 2 L 7 4 4F 4 F RT A20WE E23EA 20090108 CE 2009 1 8 GUUA93532120808A 1 20081208 A 3230 1013880073 HAND PUMP BEECH 1900 1900D 1154162 CE LANDING GEAR BYPASSING A GUUA O OTHER J WARNING INDICATION AP APPROACH 1 SO 29 81535 UE147 DURING APPROACH SELECTED LANDING GEAR DOWN, NO GEAR INDICATION. RETURNED TO DEPARTURE AIRPORT, MANUALLY PUMPED LANDING GEAR DOWN GOT TWO GREEN MAIN GEAR LOCKED ANNUNCIATOR. NO NOSE GEAR ILLUMINATED ON LANDING SHUTDOWN AND FEATHERED BOTH EN GINES. TROUBLESHOT LANDING GEAR SYS AND FOUND EMERGENCY EXTENSION HAND PUMP TO NOT BUILD PRESSURE. REPLACED HAND PUMP AS SY. LANDING GEAR OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 20090108 SO 2009 1 8 JIK2008F00007 1 20081204 A 7810 LW16620AWL EXHAUST PIPE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540* 41532 EA ENGINE CRACKED E JIKA K NONE O OTHER IN INSP/MAINT 1 WP 01 59973 241 317552079 ON 11/24/2008 DURING COMPLETION (FCD) 31-78-2008-02. INSP OF EXHAUST SYS, IT WAS NOTED THAT THE FLANGE OF THE EXHAUST PI PE AS IT GOES INTO THE TRANSITION HSG WAS CRACKED APPROX .5 THE WAY AROUND THE CIRCUMFERENCE OF THE FLANGE. THE EXHAUST MANIFOLD WAS REPLACED WITH A NEW MANIFOLD FROM A DIFFERENT MFG. THE FCD WAS WRITTEN IN RESPONSE TO A NEAR CATASTROPHIC FAILURE OF AN EXHAUST PIPE IN THIS SAME AREA THAT CAUSED AN IN-FLIGHT FIRE ON ANOTHER ACFT. IT IS HIGHLY RECOMMENDED T O PAY CLOSE ATTENTION TO THE FLANGES AND WELDED AREAS ON THESE EXHAUST ASSEMBLIES, AS FAILURE OF THE EXHAUST PIPES COULD CAUSE CONSIDERABLE DAMAGE, AND POSSIBLE LOSS OF THE ACFT AND LIFE. (K) 1 L 7 2 3O 3 O A20SO E14EA 20090108 EA 2009 1 8 N6WA200812215 1 20081228 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A N6WA K NONE L NO TEST IN INSP/MAINT 1 CE 03 153GJ 10219 ROW 15 EMERGENCY FLOOD LIGHT INOP. DEFERRED IAW MEL 33-51-01-2A, DMI 9355 CAT C. 2 L 7 2 4F RT A21EA 20090108 EA 2009 1 8 N6WA200812214 1 20081226 A 3230 LANDING GEAR CNDAIR CL600 CL6002C10 1390015 EA MALFUNCTIONED A N6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 159GJ 10238 GEAR DIDN'T RETRACT AFTER TAKEOFF, GEAR DISAGREE WARNING MESSAGE. DEFERRED LG RETRACT SYS IAW MEL 32-30-01-2 CAT A, DMI NR 8653. 2 L 7 2 4F RT A21EA 20090107 NM 2009 1 7 UALA2008122907018 1 20081227 A 3350 GE1317 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EXIT LIGHT INOP UPPER DECK FWD. CEILING LIGHT BETWEEN DOORS. RELAMPED, CHECKS OK 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 EU 2009 1 7 DATA200800012 1 20081231 A 2840 FUEL SYS STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA HARTZL HCB5M HCB5MP3 GL LT ENGINE OUT OF ADJUST E DATA B EMER. DESCENT X J ENGINE FLAMEOUT WARNING INDICATION DE DESCENT 1 GL 13 390GA 20692 SH3077 PCE84087 EVA2338 DURING DESCENT TO DESTINATION AROUND 200AGL LT SIDE FUEL PRESSURE LOW LIGHT ILLUMINATED FOLLOWED BY LT ENG FLAMEOUT. 2 H 7 2 4T 4 T A41EU E4EA 6 C P44GL 20090107 NM 2009 1 7 UALA2008122907023 1 20081227 A 3350 794640 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 177UA 24384 EMERGENCY EXIT LIGHT INOP ACROSS DOOR 3 RT LOWER WALL. REPAIRED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 UALA2008122907025 1 20081227 A 3350 767 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R1 DOOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 534UA 25129 DOOR 1R SLIDE LIGHT INOP. RELAMPED, OPS CKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20090107 NM 2009 1 7 UALA2008122907033 1 20081228 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 122UA 29168 EMERGENCY LIGHT SEAT 21RH INOP. REPLACED EMERGENCY LIGHT. LIGHT CHECKS OKAY. 2 L 7 4 4F 4 F RT A20WE E24NE 20090107 NM 2009 1 7 USAA2009010290005 1 20081229 A 5542 65C2584151M SKIN BOEING 737 7374B7 138449C NM RUDDER DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT Q5 MAJOR REPAIR NR 03C70827010/001 DELAMINATION ON RUDDER 3 INCHES ABOVE NR 4 HINGE ON RT SIDE. REPAIRED RUDDER ABO VE NR 4 HINGE ON RT SIDE IAW US AIRWAYS EA NR 100793. 2 L 7 2 4F RT A16WE 20090107 NM 2009 1 7 ASAA0944139 1 20081214 A 5753 6546430167 SKIN BOEING 737 7374Q8 138447Q NM CFMINT CFM56 CFM563C1 13802 EU FOREFLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 LT IB FORE FLAP LOWER SURFACE HAS A CLUSTER OF 20 DENTS BEHIND NR 2 TIRE. REMOVED DAMAGED AREA FABRICATED FILLER AND DOU BLER BONDED REPAIR IAW SRM 51 70 10. 2 L 7 2 4F 4 F RT A16WE E21EU 20090107 NM 2009 1 7 QXEA2008122601259 1 20081223 A 5270 PROXIMITY SENSOR BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR FROZEN A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 19 433QX 4210 "CABIN DOORS" WARNING LIGHT ILLUMINATED CLIMBING THROUGH 5000'. DOORS PAGE REVEALED AFT PASSENGER DOOR AJAR. PRESSURIZ ATION SEEMED TO BE NORMAL. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. INSPECTED AFT PASSENGER DOOR HANDL ES, ALL ARE FLUSH WITH DOOR. INSPECTED PROX SENSORS AND FOUND ICE ON DOOR PROX. CLEANED AND LUBED AND REMOVED ICE. SE NSOR OPS CK GOOD. ACFT OK FOR CONTINUED SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20090107 NM 2009 1 7 QXEA2008122601263 1 20081225 A 5210 SEAL BOMBDR DHC8 DHC8402 1390042 NM PAX DOOR FROZEN A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 19 422QX 4150 AIRCRAFT DID NOT PRESSURIZE UNTIL 5 MINUTES AFTER TAKEOFF. F/A REPORTS DELAY IN MAIN CABIN DOOR SEAL INFLATION. FOUND ICE IN AND AROUND MCD SEAL- LWR/ AFT CORNER. REMOVED ICE USING HEAT, PERFORMED FUNCTIONAL TEST OF THE PRESS SYS IAW AMM 21-31-00-720-801 PRESS CHECKS NORMAL. NO LEAKS NOTED AT MCD OK FOR SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20090107 NM 2009 1 7 QXEA2008122601265 1 20081225 A 3240 FE279001 CONTROL MODULE BOMBDR DHC8 DHC8402 1390042 NM BRAKES FAILED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 19 404QX 4046 PDX - PRIOR TO TAXI OUT, DID THE T/O WARN TEST TWICE AND GOT THE T/O HORN. THEN DID IT TWICE AND DID NOT GET THE HORN. THEN ON TAKEOFF APPLIED POWER AND GOT THE T/O HORN. SPEED WAS MORE THAN 60 KTS BUT LESS THAN 80 KTS. ABORTED TAKEOFF AND RETURNED TO THE GATE. FOUND PARK BRAKE SWITCH INTERMITTENT. REMOVED AND REPLACED PARK BRAKE CONTROL MODULE IAW Q40 0 AMM 32-44-21-000-801 AND 32-44-21-400-801. T/O WARNING OPS CHECKED GOOD. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20090107 NM 2009 1 7 C8GA20080081 1 20081015 A 5322 7075TO SHEAR TIE BOEING 727 727223 1384074 NM PWA JT8 JT8D NE FUSELAGE CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 NA WHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT SHEAR TIE LOCATED AT STA 990 STRINGER 29R WAS CRACKED. REMOVED DAMAG ED SHEAR TIE. FABRICATED NEW SHEAR TIE FROM 7075-O .063 INCH (4.380 INCH X 2 INCH) HEAT TREATED TO T6. INSTALLED NEW SHE AR TIE IAW 53-10-4, 51-10-2. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 20090108 NE 2009 1 8 CVG2008F00003 2 20081202 A 7321 1240KDC03005 EEC LEAR 60 60LEAR 5170707 CE PWA 305 PW305A 52128 NE NR 1 ENGINE FAILED E CVGA K NONE R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 05 95AG 4989 079 305280 LT ENGINE FAILED ABOUT 10-15 MINUTES INTO FLIGHT AT FL190. THE CREW REPORTED HEARING A BOOM AND THE 1ST OFFICER NOTICED THE LT ENGINE ROLL BACK. AN AIR START WAS NOT ATTEMPTED AND THE ACFT DIVERTED. REPLACED EEC WITH REPAIRED UNIT. PERF ORMED GROUND RUNS AND THE TEST FLIGHT. ACFT RETURNED TO SERVICE. MFG SUSPECTS ONE CHANNEL OF THE EEC DEVELOPED A FAULT AND ATTEMPTED TO CHANGE CHANNEL. THE EEC HAS A LANE-CHANGE RELAY, WHICH IS AN ELECTROMECHANICAL RELAY (AND NOT A SOLID STATE RELAY AS IN THE NEWER EEC`S) WHICH HAS A TENDENCY TO STICK OR TOO SLOW TO SWITCH CONTACTS. WHEN THIS TYPE OF FAI LURE OCCURS NEITHER CHANNEL IS IN CONTROL OF THE FUEL FLOW AND FLAMEOUT WILL OCCUR. THIS TYPE OF FAILURE WILL GENERATE 2 L 7 2 4F 4 F RT A10CE E35NE 20090108 NM 2009 1 8 QXEA2009010601280 1 20081230 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 415QX 4081 PDX - C3 - PITTING CORROSION ON UPPER SURFACE OF SEAT TRACK STA X779-X782 Y9.25L. BLENDED UPPER SURFACE OF SEAT TRACK C LAW IAW RD 8/4-53-884 AND REMOVED .018 INCH MATERIAL DETERMINED TRACK TO BE OUT OF LIMITS IAW RD 8/4-53-884. REMOVED SE AT TRACK. TEMP INSTALLED NEW TRACK AND MATCH DRILLED TO STRUCTURE, CLEANED DEBURRED AND ALODINED HOLES. INSTALLED TRAC K BY INSTALLING FWD SPLICE RIVETS THROUGH WEB, RIVETS THROUGH DECK SKIN AND BOLTS AT FRAME CROSSINGS. REF DHC-8 400 SRM 51-40-15 AND 51-42-05. 2 H 7 2 4T RT A13NM 20090108 NM 2009 1 8 FDEA200812305317 1 20081230 A 5330 SKIN BOEING 727 727233 138408A NM BS 390 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 257FE 20939 DENT STA 390 STR 8L. DENT FOUND TO BE OUT OF LIMITS, REWORKED DENT TO ORIGINAL CONTOUR IAW SRM 51-40- 1 HFEC INSPECTED IAW NDTM 51-00-00 WITH NO DEFECTS NOTED. 2 L 7 3 4F RT A3WE 20090108 EU 2009 1 8 FDEA200812115232 1 20081211 A 5330 A53612608200 SKIN AIRBUS 300 A300B4622R 3930312 EU FUSELAGE DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 723FD 543 FWD FUSELAGE - DENT FOUND ON LOWER FWD FUSELAGE BETWEEN FR 12-12A STR 46-47. THE DENTED SKIN WAS REPAIRED IAW EA 6-5330- 125500. 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812195235 1 20081219 A 5347 A5381192320601 SEAT TRACK AIRBUS 310 A310 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 SEAT TRACK AT RBL 35 AND FR47/48 HAS CORROSION ON OTBD FLANGE AT FASTENER HOLE, LOWER SURFACE. BLENDED CORROSION ON SEA T TRACK. ORIGINAL THICKNESS 0.078. THICKNESS REMAINING 0.054. MATERIAL LOSS 0.024. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16; FIG 101. REPLACED TRACK WITH NEW. DRILLED AND LOCATED TRACK IAW SRM 51-40-21; PG 24; PARA 7: SRM 53-10-16; FIG 201; PG 206, PO NR 644456.7, SRM 51-40-21, PG 7, PARA 6 AND DWG A538112.8. 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812195237 1 20081219 A 5347 A5381192220251 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 SEAT TRACK AT BL " 0 " APPROX 5" FWD OF FR 53, GOUGED. REMOVED AND REPLACED SEAT TRACK AS REQUIRED IAW SRM 51-40-21; P ARA 5 AND 6. 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812245287 1 20081224 A 5321 FXSRZ25005132QF FLOOR PANEL AIRBUS 310 A310203 3930313 EU FWD CARGO BAY DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 FWD CARGO PIT FLOOR PANEL NR 132QF IS DAMAGED. THIS SDR WAS GENERATED TO CORRECT THE P/N IN SECTION 5 OF SDR TRACKING NR 08-5248. FABBED NEW PANEL USING THE OLD PANEL AS A TEMPLATE. MATERIAL ID; LOCATED HOLES USING THE THE OLD PANEL; COUN TERBORED HOLES; POTTED AND SANDED EDGE; INSTALLED INSERTS; APPLIED ANTI-SKID AND PART MARKED IAW DWG SRZ 25-005; RE V "G". 2 L 7 2 4F RT A35EU 20090108 2009 1 8 SWAA090014 4 20081230 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 729SW 27861 R1 DOOR EMERGENCY EVACUATION SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20090108 CE 2009 1 8 GUUA94357061208A 1 20080612 A 5730 SKIN BEECH 1900 1900D 1154162 CE RT WING CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 49543 UE181 DURING SCHEDULED ROUTINE MX DISCOVERED RT OTBD WING, UPPER SKIN, T/E HAD CORROSION AND DEBOND BETWEEN WS 121 THROUGH 194 .85. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AND EXTERNAL REPAIR DOUBLER 2 L 7 2 4T RT A24CE 20090108 EA 2009 1 8 HNAA2009010700379 1 20081126 A 5720 85712012101 PLATE DHAV DHC8 DHC8311 1386006 EA RT WING CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 326EN 33224 33224 234 DURING C-CHECK INSP, A CRACK WAS FOUND IN THE FWD, INBD CORNER OF THE WING BOX LADDER PLATE UNDER STRESS PANEL 622AT. AN ENGINEERING ORDER WAS ISSUED REFERENCING RD8-57-4107 TO INCORPORATE RD8-57-2387 TO REPAIR THE LADDER PLATE. REPAIR WORK WAS THEN COMPLETED. 2 H 7 2 4T RT A13NM 20090108 NM 2009 1 8 HNAA2009010300365 1 20081229 A 2910 82910009149 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM NLG LEAKING A HNAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 07 938HA 51465 51465 152 AFTER ROTATION, SELECTED GEAR UP, NOSE GEAR CAME UP, NOSE DOORS STAYED OPEN, MAIN GEAR STAYED UNSAFE, GEAR CAME UP NORMA LLY WITH 3 GREENS AFTER APPOX 10 SECONDS AND GRINDING SOUND QUIT. INSPECTED AND FOUND NOSE GEAR DOWN LINE LEAKING AT STA X107.00. REMOVED AND REPLACE LINE IAW 29-20-00, OPS AND LEAK CHECKS GOOD IAW MM 12-10-29, CYCLED GEAR SEVERAL TIMES, OK FOR SERVICE. 2 H 7 2 4T RT A13NM 20090108 NM 2009 1 8 PIDA08038 1 20081223 A 3350 6104789 BATTERY BOEING 737 737228 13844AG NM CABIN DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 252TR 1 1 23001 L1 AND R1 EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY ASSY AT LT FWD CARGO-FWD SIDEWAL L. OPS CHECK IS GOOD. MM 33-51-71. 2 L 7 2 4F RT A16WE 20090108 EU 2009 1 8 U30A2008122300007 1 20081222 A 2120 UNKNOWN AIRBUS 320 A320214 3930316 EU AFT GALLEY ODOR A U30A K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 17 270AV 2325 FLT 820, MKE-PUJ WAS DESCENDING AT 10,000' ON APPROACH INTO PUJ. THE CABIN CREW SMELLED SMOKE IN THE AFT GALLEY AREA THA T LASTED FOR ABOUT 3 MINUTES. THERE WAS NO VISIBLE SMOKE, JUST AN ODOR. THE FLIGHT CREW WAS NOTIFIED, AND THEY DID NOT D ECLARE AN EMERGENCY. THE ACFT LANDED WITHOUT INCIDENT. MX INSPECTED THE AFT GALLEY AREA, THE AFT COFFE MAKERS, WASTE DIS POSAL CONTAINERS AND AFT LAVS, AND FOUND NO DEFECTS. MX ALSO CHECKED FOR ANY CIRCUIT BREAKERS THAT MAY HAVE POPPED, AND FOUND NONE. MX DID NOT SMELL ANY ODORS. THE ACFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A28NM 20090108 NM 2009 1 8 UALA2008111301566 1 20080318 A 2697 WIRE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FIRE LOOP SHORTED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 824UA 965 ENG NR2 LOOP A FIRE DETECTOR. HUNG NEW LOOP, NO HELP. SUSPECT FDU BENCH PLUG, SHAKING FDU CLEARS FAULT. SUPPLEMENTAL DA TA UPDATE WIRING SHORT IN FAN LOOP HARNESS. REMOVED CONNECTOR PLUG FROM NR2 FDU, WIRE 'A' FROM 450VT PULLED FROM BLOCK. SECURED CONNECTOR PLUG ON NR2 FDU. CONNECTION 458VC 'J' PLUG, INSIDE BOX WIRES, HAS CHAFED COATING ON BOTH WIRES 276, 27 7, WIRES MARKED WITH TAPE. WIRES REPAIRED. WIRE 2612-276-CF20 PIN A AT 450VT2 DEPINNED FOR TROUBLESHOOTING. INSTALLED PI N. SECURED INSTALLATION. ACCOMPLISHED NR 2 ENG FIRE LOOP TEST IAW 26-12-00. TEST OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20090109 NM 2009 1 9 UIEA200800349 1 20081215 A 2612 30326 AMPLIFIER BOEING 747 747243B 1384830 NM FIRE DETECTION FAILED A UIEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 540MC 22508 HIGH SPEED REJECTED TAKEOFF FOR CARGO FIRE INDICATION, NR 1 MAIN DECK WARNING ON TAKEOFF ROLL. REJECTED SPEED 146KTS. PERFORMED HIGH ENERGY STOP INSPECTION PER 5-31-10, ALL CHECKED OKAY. REMOVED AND REPLACED NR 1 SMOKE DETECTOR AMPLIFIER , ALL OPS CHECKED OK. 2 L 7 4 4F RT A20WE 20090109 NM 2009 1 9 FDEA200812245284 1 20081224 A 5330 6554583138 SKIN BOEING 727 727233 138408A NM 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 GOUGE AND DENT ON FUSELAGE SKIN STA 1030, STR 28L. FOUND GOUGE OUT OF LIMIT IAW B727 SRM 53-30-1 FIG 1 AND 2. CUTOUT D AMAGED AREA IAW B727 SRM 53-30-3 FIG 3. FABRICATED DOUBLER FROM 2024T3, 0.071 AND A FILLER FROM 2024T3, 0.063 INCH IAW B727 SRM 53-30-3 FIG 3 AND 53-30-2 FIG 3. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-30-3 FIG 1 AND 51-30-2. 2 L 7 3 4F RT A3WE 20090109 2009 1 9 SWAA090023 4 20081231 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 318SW 23339 R1 DOOR EMERGENCY EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20090109 NM 2009 1 9 HNAA2009010300364 1 20081226 A 3350 0L3071BPEGPL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 07 826EX 32967 32967 389 EMERGENCY LIGHT OFF CENTER LIGHT INOPERATIVE. DID NOT TEST. RELAMPED BULBS. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 20090109 EU 2009 1 9 FDEA200812245285 1 20081224 A 5321 FXSRZ25005132ZF FLOOR PANEL AIRBUS 310 A310203 3930313 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 FWD CARGO PIT FLOOR PANEL NR 132 ZF IS DAMAGED. FABRICATED NEW PANEL USING THE OLD PANEL AS A TEMPLATE. MATERIAL ID; L OCATED HOLES USING THE OLD PANEL; COUNTERBORED HOLES; POTTED AND SANDED EDGE; INSTALLED INSERTS; APPLIED ANTI-SKID AND P ART MARKED IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20090109 NE 2009 1 9 FDEA200812265299 2 20081226 A 7300 WARNING LIGHT AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE FALSE INDICATION A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 686FE 804 705256 LEVEL CRUISE AT FL 250, ENG 2 FUEL CLOG LIGHT CAME ON WITH ASSOCIATED ECAM ALERT. REDUCED ENG 2 POWER TO IDLE IAW ECAM. STARTED RETURN TO MEM. AFTER 7-8 MINS AT IDLE, LIGHT WENT OUT AND STAYED OUT THROUGHOUT APPROACH AND LANDING USING NO RMAL POWER. REPEAT WRITE UP, ORIGINAL FUEL FILTER FOUND TO HAVE NO CONTAMINATION. REPLACED FUEL FILTER REF AMM 73-12- 0 2-4, LEAK CHECK OK. REMOVED AND REPLACED NR 2 ENG FUEL PRESS SWITCH IAW AMM 73-34-11-4 05 OPS NORMAL NO LEAKS NOTED. 2 L 7 2 4F 4 F RT A35EU E13NE 20090108 NM 2009 1 8 QXEA2008122601268 1 20081225 A 3241 6007047 TRANSDUCER BOMBDR DHC8 DHC8402 1390042 NM ANTI SKID SYS FAILED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 19 407QX 4049 SEA - ON T/O ROLL APPROX. 50KTS, "INBD ANTISKID" CAUTION LT REMOVED AND REPLACED RT INBOARD ANTI-SKID TRANSDUCER IAW AMM 32-46-11 PAGES 401-THRU 407. FUNCTIONAL CK GOOD NO NEW FAULTS RECORDED IN CDS. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20090108 NM 2009 1 8 Q2SA751007 1 20081216 A 3233 ROD END BOEING 747 747228F 1384895 NM GE CF6 CF650E2 30018 NE MLG ACTUATOR SHEARED A Q2SA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 63 751SA 22678 AFTER DEPARTURE FROM LAGOS, NIGERIA (DNMM), RIGHT BODY GEAR DOOR WOULD NOT INDICATE CLOSED WITH GEAR RETRACTED. FLIGHT CREW FOLLOWED QRH. UNABLE TO CONTINUE TO DESTINATION DUE TO INCREASE FUEL BURN. AIR TURN BACK. NO FUEL DUMP PERFORMED . INSPECTION CONFIRMED RIGHT BODY GEAR RETRACTION ACTUATOR ROD END SHEARED OFF. NO OTHER DAMAGE TO AIRCRAFT OR LANDING GEAR. 2 L 7 4 4F 4 F RT A20WE E23EA 20090108 EU 2009 1 8 FDEA200812205249 1 20081220 A 5321 FXSRZ25005162HF FLOOR PANEL AIRBUS 310 A310 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 BULK CARGO PIT FLOOR PANEL 162 HF HAS SEVERAL DENTS. FABBED NEW PANEL USING THE OLD PANEL AS A TEMPLATE. MATERIAL ID; L OCATED HOLES USING THE THE OLD PANEL; COUNTERBORED HOLES; POTTED & SANDED EDGE; INSTALLED INSERTS; APPLIED ANTI-S KID & PART MARKED IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812205250 1 20081220 A 5321 FXSRZ25005162HF FLOOR PANEL AIRBUS 310 A310 EU ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 FWD CARGO PIT FLOOR PANEL 132 ZF IS DAMAGED. FABBED NEW PANEL USING THE OLD PANEL AS A TEMPLATE. MATERIAL ID; LOCATED HOLES USING THE THE OLD PANEL; COUNTERBORED HOLES; POTTED & SANDED EDGE; INSTALLED INSERTS; APPLIED ANTI-SKID & PART MARKED IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812205251 1 20081220 A 5321 FXSRZ25005242RJ FLOOR PANEL AIRBUS 310 A310 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 MAIN CABIN FLOOR PANEL 242 RJ IS DAMAGED. FABBED NEW PANEL USING THE OLD PANEL AS A TEMPLATE. MATERIAL ID; LOCATED HO LES USING THE THE OLD PANEL; COUNTERBORED HOLES; POTTED & SANDED EDGE; INSTALLED INSERTS; APPLIED ANTI-SKID & PART MARKED IAW DWG SRZ 25-005; REV "G". 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812185203 1 20081218 A 5330 A5377863120000 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 38333 248 FWD PIT BILGE 6 INCH FWD OF FR 38, BL 0 INTERNAL SKIN HAS CORROSION. REMOVED DAMAGED AREA IAW SRM 53-10-12; FIG 225. FABRICATED THE DOUBLER IAW SRM 53-10-12; FIG 225. ALODINED DOUBLER IAW SRM 51-21-10. PRIMED DOUBLER IAW SRM 51-23-10. INSTALLED DOUBLER IAW A310-200 SRM 53-10-12; FIG 225. TOPCOATED DOUBLER IAW SRM 51-23-10. 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812185210 1 20081218 A 5312 BULKHEAD AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 38333 248 AFT PIT FWD BULKHEAD AT STGR 38L END FITTING CORRODED. REPLACED THE FITTING AT THE AFT PIT FWD BULKHEAD LT SIDE IF STRI NGER 38L IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20090108 SO 2009 1 8 GLBA200812181 1 20081217 A 3233 2060500005 ACTUATOR EMB 120 EMB120ER 3260203 SO NLG DEFECTIVE A GLBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 21 293UX 120293 PILOTS REPORTED THAT THE NOSE GEAR WOULD NOT COME UP AFTER TAKEOFF. THEY RECYCLED THE GEAR 5 TIMES WITH NO EFFECT. GEAR INDICATIONS WERE ALL CORRECT. ACFT WAS FERRIED FOR REPAIRS. MX REMOVED AND REPLACED THE NLG ACTUATOR IAW MM 32-32-11. O PS CHECK WAS GOOD. 2 L 7 2 4T RT A31SO 20090108 NM 2009 1 8 SWAA090003 1 20081231 A 3350 COVER BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 425LV 29829 R2 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20090108 NM 2009 1 8 SWAA090004 1 20081230 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM EMERGENCY LIGHT MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 427WN 29831 EGRESS LIGHT AT ROW 2 MISSING LENS. REMOVED AND REPLACED LENS PER MM. 2 L 7 2 4F RT A16WE 20090108 NM 2009 1 8 FDEA200812235261 1 20081223 A 5310 STRUCTURE DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 CENTER LANDING GEAR WHEEL WELL, FOUND RIGHT FORWARD MOST CORNER CUTOUT DOUBLER CRACKED. CENTER MLG WW, RIGHT FORWARD MOST CORNER CUTOUT CRACKED. DOUBLER REMOVED AS PER SRM 51-33-01 VOLUME II. FASTENER HOLES PICKED UP ON NEW DOUBLER AND INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090108 CE 2009 1 8 BSYA2009003 1 20081209 A 3240 FLUID BEECH 58 58 1152740 CE BRAKE RESERVOIR LOW E BSYA O OTHER K FLUID LOSS AP APPROACH 1 GL 07 62500 TH1347 GETTING READY TO LAND, PILOT DID A BRAKE CHECK AND THE BRAKES FELT WEAK, BUT HE LANDED NO PROBLEMS. MX FILLED BRAKE RES ERVOIR, BLED BRAKES BUT COULD NOT FIND ANY LEAKS. 1 L 7 2 3O 3A16 20090108 NM 2009 1 8 P5CA2008121801584 1 20081218 A 2520 PANEL BOEING 747 74746NF 13848BT NM MAIN DECK DAMAGED A P5CA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 15 454PA 30812 DURING LOADING OF MAIN DECK DAMAGE WAS FOUND ON THE CEILING PANEL BETWEEN STA 620 AND 720 AT RBL 17.0. DAMAGE WAS FOUND TO BE OVER LIMIT EO 4425A100 WAS ISSUED CONSISITING OF A TEMPORARY REPAIR AND DVI EACH A-CHECK ACFT DEPARTED. 2 L 7 4 4F RT A20WE 20090108 EU 2009 1 8 YENA20090106002 1 20081228 A 5310 D53475529208 STRUCTURE AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A YENA K NONE O OTHER IN INSP/MAINT 1 EA 15 517JB 33024 1327 ON WEEKLY INSP, AFT CARGO DOOR PROFILE SEAL BETWEEN FR 52 TO FR 56 HAS CORROSION AT WITH THE 5 FOLLOWING SIZE OF DEFECT LENGTH AND DEPTH. PERMANENT REPAIR FUSELAGE/AFT CARGO DOOR SEALING SECTION/CORROSION WAS ACCOMPLISHED IAW EC A08-690-02 REPLACED AFFECTED DOOR SEAL. REFERENCES SRM 53-41-49-101, SRM 53-41-49-201M. PARA 5D, FIG 204, SRM 51-74-00 AND RAS/DAHA M/4026841/2008 ISSUE A. 2 L 7 2 4F RT A28NM 20090108 NM 2009 1 8 UALA2009010200002 1 20081231 A 2697 WIRE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE FIRE LOOP CHAFED A UALA O OTHER N FALSE WARNING CL CLIMB 1 WP 29 843UA 1573 NR1 ENG FIRE LOOP MESSAGE ON CLIMB. FOUND CHAFED WIRE AT 12 O'CLOCK POSITION BY PRSOV. LOOP WIRE WAS REPLACED AND SEC URED. REINSTALLED AND OPS NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20090109 CE 2009 1 9 HYIA660CA 1 20081217 A 5410 56541097 BEAM CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO ZONE 400 CRACKED E HYIA O OTHER O OTHER NR NOT REPORTED 1 NE 01 660CA 402C0406 RIGHT ENGINE'S INBOARD ENGINE BEAM CRACKED AT AFT UPPER WEB . REMOVAL AND REPLACEMENT OF ENGINE BEAM. 1 L 7 2 3O 3 O A7CE E8CE 20090109 CE 2009 1 9 HYIA3292M 1 20081222 A 5410 56541097 BEAM CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO RT ENGINE CRACKED E HYIA O OTHER O OTHER NR NOT REPORTED 1 NE 01 3292M 402C0304 RIGHT ENGINE'S INBOARD ENGINE BEAM IS CRACKED AT THE AFT UPPER WEB 0NE HALF OF AN INCH. REMOVAL AND REPLACEMENT OF THE ENGINE BEAM. 1 L 7 2 3O 3 O A7CE E8CE 20090109 NM 2009 1 9 FDEA200812265304 1 20081226 A 5311 70750071 FRAME BOEING 757 75728A 1384976 NM BS 760 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 912FD 24260 FUSELAGE FRAME STA.760 INNER CHORD BET S23L AND S24L HAS DENT. REPAIRED FRAME IAW SRM 53-00-07 FIG 201 REPAIR 5. INSPE CTION REQUIREMENT 25,000 FLIGHT CYCLES AFTER REPAIR INSTALLATION OR 50,000 AIRFRAME FLIGHT CYCLES, WHICHEVER COMES FIRST , REPEAT INSPECTION, HFEC AND DETAILED INSPECTION AT EVERY 11,000 FLIGHT CYCLES IAW NDT, PART 6, 51-00-01. THIS IS A MA JOR AND CATEGORY "B" REPAIR ON STA 760. 2 L 7 2 4F RT A2NM 20090108 EU 2009 1 8 FDEA200811205233 1 20081120 A 5540 A55471500000 RUDDER AIRBUS 300 A300B4622R 3930312 EU DEBONDED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 723FD 543 RUDDER T/E W/DEBONS BETWEEN RIB 10 AND RIB 12 REPAIR WAS DONE IAW EA 6-5510-125493. 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 QMLA122520087154 1 20081225 A 2120 UNKNOWN BOLKMS 117 BK117B2 5626013 EU COCKPIT ODOR E QMLA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 03 154AM 7154 PILOT EXPERIENCED SMELL OF BURNED ELECTRICAL DURING APPROACH; ACFT LANDED WITHOUT INCIDENT. ACFT WAS VISUALLY INSPECTED FOR DEFECTS, NONE NOTED. ADDITIONALLY, NO ABNORMAL SMELLS OR BURNED ELECTRICAL COMPONENTS FOUND. ACFT WAS GROUND RUN W /ALL ACCESSORIES OPERATING. NO EVIDENCE OF MALFUNCTION OF ANY COMPONENTS. ACFT RELEASED FOR MX OPS CHECK FLT. ACFT FLOW N WITHOUT INCIDENT. ACFT RETURNED TO SERVICE. SUBSEQUENT FLIGHTS ALSO GOOD. 1 G 7 2 3U NC H13EU 20090108 SW 2009 1 8 QMLA1218200808056 1 20081218 A 2120 UNKNOWN BELL 222 222U 1182140 SW COCKPIT ODOR E QMLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS AA AIR AMBULANCE 1 NM 03 224LN 47552 ACFT DEPARTED HOSPITAL FOR RETURN TO BASE ON THIRD LEG OF SECOND MISSION OF THE DAY. APPROX 5 MIN INTO FLIGHT, A CREWMEM BER STATED THAT HE SMELLED AN ELECTRICAL ODOR EMITTING IN THE AFT AREA OF THE CABIN. PILOT CHECKED GAUGES, WHICH ALL WER E IN NORMAL OPERATING RANGES, AND PROCEEDED TO NEAREST AIRPORT TO HAVE A MECHANIC INVESTIGATE POTENTIAL ACFT PROBLEM. ME CHANIC WENT TO ACFT AND COULD NOT SMELL AN ODOR. MECHANIC REQUESTED PILOT TO RUN THE ACFT AND RECONFIGURED MEDICAL AND I NTERIOR TO MATCH WHEN THE ODOR WAS ENCOUNTERED. RAN THE AIRCRAFT FOR 20 MINUTES, INSPECTED WALL AND OUTLETS BUT COULD NO T DETECT THE ODOR. 1 G 7 2 3U H9SW 20090108 EU 2009 1 8 QMLA1222200808057 1 20081222 A 2820 O-RING SNIAS 350 AS350B2 8680813 EU FUEL SYSTEM DEFECTIVE E QMLA C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS AA AIR AMBULANCE 1 NM 03 779LF 3474 SMELL OF JET FUEL EMITTED FROM HEATER AFTER TAKEOFF. IMMEDIATELY RETURNED TO PLACE OF TAKEOFF. SMELL SEEMED TO GO AWAY A FTER HEATER TURNED OFF. PILOT NOTIFIED MECHANIC OF THE FUEL SMELL IN THE COCKPIT. MECHANIC REMOVED THE DRAIN PLUG FROM THE FUEL INLET LINE TO MOD 3. PILOT GROUND RUNS THE HELICOPTER TO SEE IF FUEL WAS DRAINING FROM THE PLUG. THERE WAS NO NE. MECHANIC REINSTALLED THE PLUG IAW TEC SPECS AND REPLACED THE START DRAIN VALVE. THE FUEL SMELL WAS STILL PRESENT D URING RUN UP PROCEDURES. REMOVED THE P2 AIRLINE FROM THE FCU. VERIFIED NO FUEL EXISTED IN THE P2 CHAMBER. THERE WAS EV IDENCE OF FUEL IN THE P2 PORT. DETERMINED THE FCU WAS INDEED SERVICEABLE. MECHANIC REPLACED THE 2 O-RINGS AT THE MOD 3 1 G 7 1 3U H9EU 20090108 NM 2009 1 8 SWAA090009 1 20081228 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM BS 947 S21R CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20090108 EU 2009 1 8 RMXA0329121708 1 20081217 A 5350 L535A4001101 FAIRING UROCOP UROCOP EC135 EC135P2 5620027 EU TAILBOOM DELAMINATED E RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 135WL 3980 FLV328 0329 DURING A SCHEDULED INSP, FOUND THE TAIL ROTOR DRIVESHAFT FAIRING HAS A DELAMINATED AREA ON THE TOP SURFACE. THE DELAMINA TED AREA WAS 8 INCHES L X 2.25 INCHES W. REPAIR SCHEME WAS PROVIDED FROM THE MFG AND THE FAIRING WAS REPAIRED. 1 G 7 2 3U H88EU 20090108 NM 2009 1 8 SWAA090010 1 20081228 A 5330 6545767 SKIN BOEING 737 7373A4 1384585 NM BS 444-446 S17L CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 678AA 23290 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BETWEEN BS 444 TO BS. 446, STR 17L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20090108 NM 2009 1 8 SWAA090018 1 20081228 A 2121 2125201 GASPER FAN BOEING 737 7373H4 1384600 NM A/C COMPT FAULTY A SWAA O OTHER O OTHER AP APPROACH 1 SW 29 605SW 27956 UPON APPROACH INTO STL (APPROX 1000') FA'S CALLED, INFORMING CAPT OF ELECTRICAL SMELL. PILOT'S BEGAN SMELLING FAINT ELE CTRICAL SMELL AT THAT TIME. NO LIGHTS OF INSTRUMENT FAILURES NOTED NOR POPPED CB'S. REMOVED AND REPLACED GASPER FAN PE R MM. 2 L 7 2 4F RT A16WE 20090108 CE 2009 1 8 GUUA93653080208A 1 20080802 A 2800 FUEL SYS BEECH 1900 1900D 1154162 CE LEAKING A GUUA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 29 81536 UE152 DURING ROUTINE MX, CUT OUT A SMALL ACCESS SECTION OF LT FUSELAGE BETWEEN FS 288 AND FS 318 FOR FUEL LEAK REPAIR. FABRIC ATED AND INSTALLED EXTERNAL REPAIR DOUBLER. 2 L 7 2 4T RT A24CE 20090108 CE 2009 1 8 GUUA93653092908A 1 20080929 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81536 UE152 DURING SCHEDULED ROUTINE MX DISCOVERED EXFOLIATION AT THE LOWER FUSELAGE SKIN AT FS 438.250 STRINGER 16. REMOVED DAMAGE D SKIN FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER. 2 L 7 2 4T RT A24CE 20090108 CE 2009 1 8 GUUA93654102008A 1 20081020 A 5410 KEEL BEECH 1900 1900D 1154162 CE LT NACELLE CHAFED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 81536 UE152 DURING SCHEDULED ROUTINE MX DISCOVERED LT NACELLE KEEL CHAFING AT THE INBD SIDE FENDER ATTACHMENT FLANGE. REMOVED DAMAG ED AREA AND INSTALLED FILLER AND CAP REPAIR DOUBLER. 2 L 7 2 4T RT A24CE 20090108 CE 2009 1 8 GUUA94053042208A 1 20080422 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 16540 UE172 DURING SCHEDULED ROUTINE MX DISCOVERED EXFOLIATION AT THE LWR FUSELAGE SKIN AT FS 438.250. REMOVED DAMAGED SKIN FABRICA TED AND INSTALLED AN EXTERNAL DOUBLER REPAIR. 2 L 7 2 4T RT A24CE 20090108 CE 2009 1 8 GUUA95557073008A 1 20080730 A 5730 SKIN BEECH 1900 1900D 1154162 CE RT WING CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 87555 UE234 DURING SCHEDULED ROUTINE MX DISCOVERED RT OTBD WING, UPPER SKIN, T/E HAD CORROSION AND DEBOND BETWEEN WS 121 THROUGH 194 .85. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER. 2 L 7 2 4T RT A24CE 20090108 CE 2009 1 8 GUUA94753081308A 1 20080813 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 69547 UE189 DURING SCHEDULED ROUTINE MX DISCOVERED 1.875 INCH CRACK IN FUSELAGE BELLY SKIN SPAR AREA AT RBL 30.62. STOP DRILLED CRA CK AND INSTALLED REINFORCEMENT DOUBLER REPAIR. 2 L 7 2 4T RT A24CE 20090108 EA 2009 1 8 HNAA2009010700380 1 20081126 A 5720 85712012101 PLATE DHAV DHC8 DHC8311 1386006 EA LT WING CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 326EN 33224 33224 234 DURING C-CHECK INSP, A CRACK WAS FOUND IN THE AFT OTBD CORNER OF THE WING BOX LADDER PLATE UNDER STRESS PANEL 522AT. AN EO WAS ISSUED REFERENCING RD8-57-4106 TO INCORPORATE RD8-57-2375 TO REPAIR THE LADDER PLATE. REPAIR WORK WAS THEN COMPLE TED. 2 H 7 2 4T RT A13NM 20090108 NM 2009 1 8 QXEA2009010701283 1 20081230 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 415QX 4081 PDX - C3 - LT SEAT TRACK HAS CORROSION AT APPROX 449.50 AND A GOUGE ACROSS THE FACE ON TRACK AT APPROX 547.00. BLENDED CORROSION FROM NR2 SEAT TRACK. MAX MATERIAL REMOVED IS .068 INCH BLEND IS OUT OF LIMITS IAW RD8/4-53-884. REMOVED NR2 SEAT TRACK AT FWD AND AFT SPLICES, WEBS AND FRAMES. PICKED UP ALL HOLES ON NEW SEAT TRACK AND DEBURRED. INSTALLED NEW NR2 SEAT TRACK IN FWD SPLICE, WEBS AND FRAMES. REF SRM 51-40-15, 51-42-05 AND 51-42-15. CONTINUED INSTALLATION REF SR M 51-40-07, 51-42-05 AND 51-42-45. 2 H 7 2 4T RT A13NM 20090108 CE 2009 1 8 YADA122908 1 20081229 A 2822 1333890311 PUMP BEECH 1900 1900C 1154161 CE FUEL SYSTEM DAMAGED E YADA O OTHER J WARNING INDICATION NR NOT REPORTED 1 AL 03 113AX UC41 ON AN OPS CHECK FLIGHT, PILOT REPORTED LOW PRESSURE FUEL LIGHT ON THE NR 1 ENG, LIGHT WENT OUT WITH AUX PUMP ON. REPLAC ED PUMP. TEARDOWN OF REMOVED PUMP REVEALED THAT THE PRESSURE CONTROL DIAPHRAGM HAD FAILED POSSIBLY DUE TO AN IMPROPERLY MFG PN RA5361 SPRING PLATE WITH EDGE RADIUS NOT IN CONFORMANCE WITH MFG DRAWING. 2 L 7 2 4T RT A24CE 20090108 CE 2009 1 8 YYE2008F00000 1 20081201 A 2913 PUMP CESSNA 337 T337G 2075726 CE CONT O360 TSIO360CB 17025 SO MCAULY 2A34C D2A34C* GL HYDRAULIC SYS FAILED E YYEA O OTHER O OTHER NR NOT REPORTED 1 NM 11 5CS P3370087 236205R 7830087 THE PRIMARY ELECTRIC/ HYD LANDING GEAR PUMP FAILED. THE ATTEMPT TO LWR THE GEAR WITH THE MANUAL GEAR LEVER ALSO FAILED, RESULTING IN A GEAR UP LANDING. THE PRIMARY PUMP FAILURE MAY HAVE CAUSED THE MANUAL PUMP FAILURE. (K) 1 H 7 2 3O 3 O A6CE E9CE 5 C P3EA 20090108 2009 1 8 YYFA20080004 4 20081222 A 2340 6224096002 AMPLIFIER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE PA SYSTEM INOPERATIVE A YYFA O OTHER O OTHER UK UNKNOWN 1 SO 29 905TA 49905 PA SYS INTERMITTENT. 2 L 7 2 4F 4 F A6WE E9NE 20090108 NM 2009 1 8 UALA2008123007041 1 20081230 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DEFECTIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 178UA 24385 EMERGENCY EXIT EEL LIGHTS INOP AT DOOR 4 RT AFT. EXIT EEL SIGN, DOOR 4 LT FWD EXIT EEL SIGN, SEATS 45 THRU 53 LT, LOWER WALL EEL LIGHT ACROSS DOOR 4 LT, AND LOWER WALL EEL LIGHT AT DOOR 4 GALLEY AREA. REPLACED POWER FEEDER. ALL EEL LIGHT S OPS CK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20090108 NM 2009 1 8 UALA2009010200001 1 20081231 A 3397 58791 FEEDER CABLE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU CABIN DIRTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 339UA 24243 ROW 15 TO BACK OF ACFT EEL LIGHTS ARE VERY DIM. CLEANED AND SECURED WALL FEEDER CABLE. OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E21EU 20090109 EA 2009 1 9 MALA080214 1 20081216 A 3211 BRACKET CNDAIR CL600 CL6002B19 1900309 EA PROX SENSOR BENT A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 831AY 8031 SHORTLY AFTER TAKEOFF, CREW OBSERVED GEAR DISAGREE WARNING LIGHT. NOSE DOOR OPEN WARNING MESSAGE INDICATION AFTER GEAR HANDLE TRAVELED UP AFTER CLIMB-OUT, ALSO GEAR DOOR DISAGREE WARNING ASSOCIATED. FOLLOWED POM, PUT GEAR HANDLE DOWN RECE IVED ALL THREE DOWN AND GREEN INDICATION. RETURNED MSP AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NLG OLEO CENT ER AND EXTENDED PROX SWITCH BRACKET AND ADJUSTED SWITCH IAW 32-61-05 OPS CHECKS NORMAL P/N 16215-105 ACT EXT AND RET TES T IAW 32-30-00 OPS CHECKS GOOD. 2 L 7 2 4F RT A21EA 20090109 NM 2009 1 9 HNAA2009010300368 1 20081229 A 3350 OL3071BPEGPL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 941HA 50299 50299 161 EMERGENCY FLOOR PATH LIGHT INOPERATIVE AT ROW 4 AFT. R&R EMERGENCY FLOOR PATH LIGHT AT ROW 4 AFT. 2 H 7 2 4T RT A13NM 20090109 NM 2009 1 9 FDEA200812265302 1 20081226 A 5320 7075T6080B SUPPORT ANGLE BOEING 757 75728A 1384976 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 912FD 24260 NR 2 PASS DOOR RT SIDE LOWER CUT-OUT FRAME WEB SUPPORT ANGLE HAS SURFACE CORROSION. REMOVED AND REPLACED NR 2 PASS DOOR RT SIDE LOWER SUPPORT ANGLE IAW SRM 51-40-02 USING FABBED NEW INBD CREASE BEAM CHORD ON MAE TRAVELER NR T8/769356. THI S IS A MAJOR AND CATEGORY "A" REPAIR AT STA 690 TO 730. 2 L 7 2 4F RT A2NM 20090108 NM 2009 1 8 QXEA2008122601266 1 20081225 A 3260 DOWNLOCK SENSOR BOMBDR DHC8 DHC8402 1390042 NM LEFT OUT OF RIG A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 19 434MK 4227 SEA -L GEAR DOOR AMBER LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION F/A REPORTED BOTH REAR DOORS OPEN. RIGGED LEFT GEAR DOWNLOCK NR 2 SENSOR. PERFORMED GEAR RETRACTION CHECK OPS CHECK GOOD A/C OK FOR CONT SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20090108 NM 2009 1 8 QXEA2008122601267 1 20081226 A 3297 471515 WIRE HARNESS BOMBDR DHC8 DHC8402 1390042 NM NLG WOW FAILED A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 19 406QX 4048 SEA - UPON SELECTION OF GEAR UP, AFTER TAKEOFF, GEAR 3 GREEN REMAINED ILLUMINATED, 3 RED INDICATORS ILLUMINATED AND GEAR HANDLE ILLUMINATED. RAN 'GEAR WOULD NOT RETRACT' AND 'ALT GEAR EXTENSION' CHECKLIST. RETURNED TO THE FIELD AND ACCOMP LISHED A UNEVENTFUL LANDING. REMOVED AND REPLACED NLG WOW HARNESS. ALL CHECKS GOOD. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20090108 NM 2009 1 8 FDEA200812245288 1 20081224 A 5330 53FX1301 SKIN BOEING 727 727233 138408A NM FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 FUSELAGE, FASTENER INSTALLED AT SEAM AT STA 550, STR 21L REMOVED SUBJECT FASTENER AND TRIMMED OUT DAMAGED AREA IAW EA NR 7-5330-126879. REPAIRED IAW EA NR 7-5330-126879, FUSELAGE, PLATES AND SKIN AD 98-11-03 R1 MCD CUTOUT PLATING REPAIR AT STA 554. 2 L 7 3 4F RT A3WE 20090108 NM 2009 1 8 FDEA200812265294 1 20081226 A 5230 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON 0.460 INCH HOLES AT MAIN CARGO DOOR LWR JAMB NR 3 SUPPORT FITTING AT HOLE NR A. BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIE D AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090108 EU 2009 1 8 FDEA200812195238 1 20081219 A 5347 A5327400500000 SEAT TRACK AIRBUS 310 A310 EU ZONE 200 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 38333 248 CABIN SEAT TRACK GOUGED BETWEEN FR 18 & FR 19 AT RBL 63. REMOVED DAMAGE AND CHECKED LIMITS REF SRM 53-10-16. ALODINED R EF SRM 51-21-10. PRIMED & PAINTED REF SRM 51-23-10. 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812185196 1 20081218 A 5321 FXSRZ25005252GF FLOOR PANEL AIRBUS 310 A310203 3930313 EU ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 38333 248 CABIN FLOOR PANEL 252GF DENTED IN 2 PLACES. REPAIRED FLOOR PANEL 252 GF BY FABRICATING A NEW FLOOR PANEL FROM STOCK M ATERIAL USING THE OLD PANEL AS A TEMPLATE IAW DWG SRZ20-005; REV " G ". 2 L 7 2 4F RT A35EU 20090108 EU 2009 1 8 FDEA200812235265 1 20081223 A 7120 BEARING AIRBUS 310 A310203 3930313 EU ZONE 400 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 NR 1 PYLON THRUST SIDE LOAD FITTING BEARING IS EMITTING RUST ON THE TOP AND BOTTOM SIDES. CLEANED AREA IAW AMM 51-78-00 -7. REMOVED AND REPLACED NR 1 PYLON SPIGOT P/N IAW DWG 22A57150065. 2 L 7 2 4F RT A35EU 20090108 2009 1 8 J7SA5723081216 4 20081216 A 3160 8221917202822157 DISPLAY CNDAIR CL600 CL6002B16 1900305 EA COCKPIT MALFUNCTIONED E J7SA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 05 340FX 5723 NR1 AND NR2 COMM RADIOS CHANGED FREQUENCIES ALL BY THEMSELVES. ACFT DIVERTED WITH LANDING AND TAXI UNEVENTFUL. MX CHANG ED THE NR2 PRIMARY FLIGHT DISPLAY AND THE NR2 MULTI-FUNCTION DISPLAY. OPS CHECKS AND MX CHECK FLIGHT PERFORMED SATISFACT ORILY. 2 L 7 2 4F RT A21EA 20090108 NM 2009 1 8 Q2SA749003 1 20081229 A 5330 SKIN PANEL BOEING 747 7473B5 1384920 NM PWA JT9 JT9D7R4G2 52054 NE BS 2690-2701 DEPARTED A Q2SA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 EA 63 749SA 24194 DURING FLIGHT, FUSELAGE SKIN PANEL SECTION BROKEN OFF (APPROXIMATELY 10 INCH BY 20 INCH BETWEEN STA 2690.85 AND 2701.5 A T WL 310). VEERED AFTER LANDING DURING MAINTENANCE INSPECTION ACTIVITY. REPAIR IN PROGRESS, TO BE PERFORMED IN ACCORDA NCE WITH BOEING STRUCTURAL REPAIR MANUAL. 2 L 7 4 4F 4 F RT A20WE E3NE 20090108 NM 2009 1 8 FDEA200812225258 1 20081222 A 5730 ARB2888502 SKIN DOUG MD11 MD11F 3023600 NM RT WING CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 RIGHT WING FIXED LEADING EDGE SLAT TRACK 12 SKIN FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090108 NM 2009 1 8 FDEA200812225259 1 20081222 A 5730 ARB2887504 SKIN DOUG MD11 MD11F 3023600 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 RIGHT WING FIXED LEADING EDGE ACCESS PANEL NR 619CB CUTOUT FOUND CRACKED. RIGHT WING FIXED LEADING EDGE ACCESS PANEL 619CB CUTOUT CRACKED. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER G MM 6-2-100. 2 L 7 3 4F RT A22WE 20090108 NM 2009 1 8 FDEA200812225260 1 20081222 A 3230 AYG70505507 SELECTOR VALVE DOUG MD11 MD11F 3023600 NM MLG MALFUNCTIONED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 CE 21 607FE 45411 45411 48547 LEFT MAIN GEAR FAILED TO RETRACT ON TAKEOFF. AFT CYCLING GEAR IAW QRH GEAR AGAIN REMAINED EXTENDED APPROXIMATELY 3-4 MI NUTES LATER WITH NO CREW ACTION GEAR RETRACTED ON ITS OWN. HYD NORMAL. ALTITUDE APPROX 26000 AND 230 KTS WHEN RETRACT ION FINALLY OCCURED. R/I LANDING GEAR SELECTOR VALVE AND LEAK CK'D OK PER MM 32-31-20-4. 2 L 7 3 4F RT A22WE 20090108 NM 2009 1 8 FDEA200812235262 1 20081223 A 5230 AFA3805505 SKIN DOUG MD11 MD11F 3023600 NM CARGO DOOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 CENTER CARGO DOOR LOWER FORWARD CORNER FOUND DOOR SKIN DAMAGED. REPAIR CARRIED OUT AS PER E.A. NO. 1-5230-127702 REPAI R CLASSIFIED AS MINOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090108 NM 2009 1 8 SWAA090007 1 20081230 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 647SW 27717 DURING SCHEDULED MV2 CHECK, FOUND FLOORBEAM SUPPORT CORRODED AT BS 270, RBL 12. REMOVED AND REPLACED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20090108 NM 2009 1 8 KCSA081618 1 20081221 A 5210 DOOR FRAME BOEING 747 747212B 1384886 NM L2 DOOR CRACKED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 L2 MAIN ENTRY DOOR FWD LWR CORNER HORZ FRAME CRACKED IN RADIUS, BS 809, WL-208. 2 L 7 4 4F RT A20WE 20090108 NM 2009 1 8 KCSA081619 1 20081224 A 3350 LIGHT BOEING 747 747259B 1384804 NM CABIN INOPERATIVE A KCSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 701CK 21730 UPPER DECK EXIT DOOR EMERGENCY SILL LIGHTS ARE INOP. 2 L 7 4 4F RT A20WE 20090108 NM 2009 1 8 PCSA2008121801 1 20081218 A 2611 SMOKE DETECTOR BOEING 727 7272J7 138400E NM CABIN DIRTY A PCSA O OTHER N FALSE WARNING DE DESCENT 1 SO 17 128NA 20879 ON DESCENT, MAIN CABIN SMOKE DETECTOR LIGHT ILLUMINATED. NO EVIDENCE OF SMOKE DISCOVERED. MX DISCOVERED NR 1 SMOKE DETE CTOR DIRTY. THE DETECTOR WAS CLEANED AND THE SYS TESTED NORMAL. 2 L 7 3 4F A3WE 20090108 NM 2009 1 8 WX0A070251 1 20081230 A 2520 INSULATION DOUG MD88 MD88 3023688 NM CABIN CONTAMINATED A WX0A D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 19 404NV 49765 DURING TAXI, ACFT FILLED WITH SMOKE, PERFORMED PASSENGER EVACUATION OUT THE AFT AIRSTAIRS. F/A SAW SMOKE FROM OVERHEAD A T ROW 16 F AND 15 DEF AROUND LIGHT FIXTURE. AIR CONDITIONING PACKS WHERE NOT IN OPERATION. MX INSPECTED THE PSU'S AT RO W 15 AND 16 AND FOUND NO WATER OR MOISTURE, SHORTED OR BURNED WIRES. REMOVED OVERHEAD PANEL AND FOUND INSULATION SOAKED WITH WATER. REPLACED INSULATION AND PERFORMED NUMEROUS OPS CHECK OF THE AIR CONDITIONING SYS. ACFT OK FOR RETURN TO SE RVICE. 2 L 7 2 4F RT A6WE 20090108 2009 1 8 XV6A20081212 4 20081211 A 2565 LIGHT AIRCRUISERS BOEING 737 737400 138449A NM LYC O320 O320* 41508 EA EVAC SLIDE INOPERATIVE A XV6A K NONE L NO TEST IN INSP/MAINT 1 WP 19 742 0173 188146 DURING EVACUATION EXERCISES THE FWD SERVICE DOOR (RT) EMERGENCY SLIDE DEPLOYED NORMALLY BUT THE INTEGRAL SLIDE ILLUMINAT ION LIGHTS DID NOT ILLUMINATE. 2 L 7 2 4F 3 O RT A16WE E274 20090109 CE 2009 1 9 HYIA401TJ 1 20081225 A 8097 9910397 RELAY CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO ZONE 500 BURNED E HYIA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NE 01 401TJ 402C0109 SMOKE COMING OUT OFF THE COCKPIT. MAINTENANCE INSPECTED FOUND RIGHT ENGINE'S STARTER RELAY HAD FAILED. MAINTENANCE REM OVED AND REPLACED RELAY RETURNED AIRCRAFT TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 20090109 EA 2009 1 9 ASOA20090018 1 20081230 A 5320 INTERCOSTAL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE DAMAGED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 RESOLVED ON W/O 107153 TASKCARD: NR-00005 REMOVED CARGO LINERS FROM AFT PRESSURE BULKHEAD, INSTALLED DOUBLER ON LINTEL I NTERCOSTAL, APPLIED CPC TO AFT BULKHEAD, REINSTALLED FIREBLOCK, REINSTALLED AND SEALED AFT PRESSURE BULKHEAD CARGO LINER S. ALL WORK DONE IAW REO 601R-53-61-1230, CRJ 200 AMM 25-52-01, CRJ 200 SRM 51-22-00, REO 601R-53-61-1230, PER CRJ 200 NDTM 51-20-06. 2 L 7 2 4F RT A21EA 20090109 CE 2009 1 9 HYIA26632 1 20081215 A 3240 BRAKE SYS CESSNA 402 402C 207590R CE CONT O520 TSIO520VB 17040 SO LEFT FAILED E HYIA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NE 01 26632 402C0404 LEFT BRAKE FAILED DURING TAXI. MAINTENANCE INSPECTED BLED AND SERVICED LEFT BRAKE SYSTEM. 1 L 7 2 3O 3 O A7CE E8CE 20090109 EU 2009 1 9 FDEA200812245283 1 20081224 A 5330 A5731002920000 SKIN AIRBUS 310 A310203 3930313 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 MAIN CABIN, CENTER FUEL TANK UPPER SKIN AT FRAME 44, RBL 77 - 96 HAS CORROSION RUNNING FROM BELOW THE TRACK WEB OTBD UND ER THE FRAME ATTACH FITTING TO UNDER THE OTBD ATTACH FITTING. REMOVED AND RE-INSTALLED 2 ANGLES IAW SRM 51-40-21, PG 7 . REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 57-10-12, FIG 101. ALODINED AND PRIMED AREA IAW SRM 51-21- 10; PG 2. 2 L 7 2 4F RT A35EU 20090109 NM 2009 1 9 FDEA200812265307 1 20081226 A 5744 ARC050311 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 LEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE LOWER ATTACH INBOARD HOLE FOUND WITH CORROSION. REWORKED AS PER EA 1-5 750-127701. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090109 NM 2009 1 9 FDEA200812265309 1 20081226 A 5512 AJC70602 SKIN DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 EMPENNAGE, RIGHT AFT FUSELAGE SKIN COMMON TO AFT BODY FAIRING NR 347DF LOWER MATING SURFACE FOUND WITH SURFACE CORROSI ON. SURFACE CORROSION ON EMPENNAGE RT AFT FUSELAGE SKIN COMMON TO AFT BODY FAIRING 347DF LOWER MATING SURFACE REMOVED A S PER SRM 51-21-01 VOLUME II. FOUND EXCEEDED LIMIT AS PER SRM 53-20-00 FIGURE 13 VOLUME I. REPAIR CLASSIFIED AS MAJOR A S PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090109 EA 2009 1 9 MALA080217 1 20081217 A 2120 UNKNOWN CNDAIR CL600 CL6002B19 1900309 EA CABIN ODOR A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 836AY 8036 AFTER DEPARTURE FROM MSP THE CREW EXPERIENCED A LAVATORY SMOKE WARNING. AT APPROX 500 FT SMOKE TOILET CAUTION MESSAGE A PPEARED. DURING THE NON NORMAL CHECKLIST MESSAGE DISAPPEARED. FA SAID NO SMOKE, BUT DID DETECT DE-ICE FLUID FROM DEICI NG. FLIGHT RETURNED TO MSP. THE CAPTAIN DID DECLARE AN EMERGENCY TO ATC AND RETURNED TO MSP LANDING WITHOUT FURTHER IN CIDENT. COMPLIED WITH EO NR C25025: INSTALLATION OF COVER ON LAV AIR VENT. 2 L 7 2 4F RT A21EA 20090109 NM 2009 1 9 FDEA200811054728 1 20081105 A 5754 40173 SWITCH BOEING 727 727225 1384077 NM LE FLAP MISALIGNED A FDEA C ABORTED TAKEOFF J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 CE 21 464FE 21288 NR 2 LED/FLAP DID NOT RETRACT. FOUND SWITCH INTERNALLY BINDING. REPLACED SWITCH PER 27-82-001-4, OP CHECKS NORMAL, GOO D FOR SERVICE. REMOVED AND REPLACED NR 2 LEADING EDGE FLAP SWITCH AMM 27-82-001-4. 2 L 7 3 4F A3WE 20090109 EU 2009 1 9 FDEA200812295314 1 20081229 A 5321 FXSRZ25005242VF FLOOR PANEL AIRBUS 310 A310203 3930313 EU ZONE 200 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 38333 248 MAIN CABIN FLOOR PANEL IS PUNCTURED 8 INCHES FROM FRAME 52, RBL 64 INCHES. REPAIRED THE PUNCTURED AREA IAW SRM 53-10-20 , PG 202, PARA 9-C. 2 L 7 2 4F RT A35EU 20090109 NM 2009 1 9 NWAA085693141 1 20081219 A 2100 CONVERTER AIRBUS A319 A319114 3930350 NM CABIN INOPERATIVE A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 01 341NB 01738 BAD SMELL IN AC SYS. IT IS NOTICEABLE WITH APU BLEED AND ENGINE BLEED. IT IS WORSE AT LOW ALTITUDES, WHETHER ON CLIMB OR DESCENT. AT CRUISE SMELL SEEMS WORSE IN BACK. ON FINAL APPROACH PASSENGER AND F/A IN BACK OF ACFT WERE COUGHING AND COMPLAINING OF SMELL. REPLACED LT AND RT CATALYTIC CONVERTERS, NO SMELL NOTED. 2 L 7 2 4F RT A28NM 20090109 WP 2009 1 9 NWAA085709866 1 20081223 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 775NC 47785 DURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE CABIN HAD FAILED. MX REPLACED THE BATTERY PACK AN D THE LIGHTS WERE RETURNED TO AN OP CONDITION. 2 L 7 2 4F RT A6WE 20090109 NM 2009 1 9 R5KB15936 1 20081220 A 5320 FLOOR SUPPORT BOEING 727 727212 138407G NM FUSELAGE CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 FLOOR SUPPORT CORRODED. 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 R5KB15791 1 20081219 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21845 SEAT TRACK CORRODED. 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 R5KB15803 1 20081219 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 SEAT TRACK CORRODED. 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 R5KB15774 1 20081220 A 5320 CHANNEL BOEING 727 727212 138407G NM FUSELAGE CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 HAT CHANNEL CORRODED 2 L 7 3 4F A3WE 20090109 SO 2009 1 9 RAIA2009010500001 1 20081231 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 811HK 145256 DURING PRE-FLIGHT INSPECTION, THE CREW FOUND THE EMERGENCY LIGHT AT THE GALLEY TO BE INOPERATIVE. MX PERFORMED A TEST O F THE EMERGENCY LIGHT. THE SYSTEM CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20090109 SO 2009 1 9 RAIA2008123000001 1 20081229 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN LOOSE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 813HK 145044 DURING THE PRE FLIGHT INSPECTION, MX FOUND THAT THE EMERGENCY LIGHT AT ROW 12 WAS INOPERATIVE. MX RESECURED WIRING TO T HE INOPERATIVE LIGHT. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT T00011AT 20090108 NM 2009 1 8 KPVA 2008-06 1 20081228 A 2611 8006221 CONTROL UNIT DHAV DHC8 DHC8103 1386005 NM SMOKE WARNING INTERMITTENT A KPVA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 13 806WP 357 ON TAXI, RECEIVED MASTER WARNING AND SMOKE WARNING LIGHT INTERMITTENT ON AND OFF 6 TIMES. MX REMOVE AND REPLACED CAUTIO N CONTROL BOX IAW MM CHAP 33-18-00 PAR 2A PG 203. OPS CHECK OF SMOKE DETECTOR SYS IAW MM CHAP 26-12-00 PG 201. 2 H 7 2 4T RT A13NM 20090108 NM 2009 1 8 UALA2009010200003 1 20081231 A 2697 W038001TRW20 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FIRE LOOP CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 643UA 25093 NR 1 ENGINE UPPER PYLON POSSIBLE FIRE LOOP HARNESS RED 01TR-W-20 CHAFED 2 PLACES. FOUND WIRE IN QUESTION TO BE W0380-01 TR (W)-20 USED FOR EVB WIRE TYPE RQ. REPAIRED SHIELD WIRE. RESECURED WIRES, CLAMPS AND PROTECTED WITH TEFLON & FIBERGL ASS TAPE. REPAIRED OTHER LESS DAMAGED SHIELD WIRES IN THE SAME PYLON BUNDLE THE SAME WAY. ACCOMPLISHED CAT III CHECK. TEST GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20090109 EA 2009 1 9 HNAA2009010300366 1 20081230 A 7922 45E041 REGULATOR DHAV DHC8 DHC8311 1386006 EA NR 1 ENGINE FAILED A HNAA D RETURN TO BLOCK M OVER TEMP TX TAXI/GRND HDL 1 EA 07 330EN 35175 35175 274 NR 1 ENGINE TEMPERATURE WENT TO MAX PERMISSIBLE LIMIT OF 125 DEGREES, IMMEDIATELY PULLED POWER BACK TO BRING TEMPERATURE TO 115 DEGREE WITH IN LIMITS. R&R THERMO VALVE ON NR 1 ENGINE OIL COOLER IAW 79-20-11, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 20090109 NE 2009 1 9 UIEA200900002 2 20081230 A 7250 CF650E2 BLADES BOEING 747 747228F 1384895 NM GE CF6 CF650E2 30018 NE NR 1 ENGINE MISSING A UIEA O OTHER E VIBRATION/BUFFET CL CLIMB 1 EA 15 809MC * 20887 517612 DURING DESCENT CREW REPORTED SIGNIFICANT VIBRATION FROM NR 1 ENGINE. INSPECTION FOUND MISSING BLADES IN THE LPT AREA. ENGINE CHANGE IS IN PROGRESS. 2 L 7 4 4F 4 F RT A20WE E23EA 20090109 NM 2009 1 9 FDEA200812285312 1 20081228 A 2810 FUEL TANK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 MAIN DECK CARGO, CENTER AUXILIARY TANK UPPER SURFACE FOUND CORROSION AT STA 1229 X = 6. CORROSION REMOVED AS PER SRM 51 -21-01 VOLUME II. FOUND TO EXCEED LIMIT AS PER SRM 57-20-00 FIGURE 13 VOLUME I. REPAIR CARRIED OUT AS PER EA 1-5710-122 666. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090109 NM 2009 1 9 R5KB15945 1 20081220 A 3270 BEAM BOEING 727 727212 138407G NM TAIL SKID CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 TAIL SKID TRANSVERSE BEAM FWD ATTACH ANGLE CORRODED. 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 R5KB15779 1 20081218 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 SEAT TRACK CROWN CORRODED. 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 R5KB15804 1 20081219 A 5320 FLOOR SUPPORT BOEING 727 727212 138407G NM FUSELAGE CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 FLOOR SUPPORT EXTRUSION CORRODED. 2 L 7 3 4F A3WE 20090109 SO 2009 1 9 RAIA2009010500002 1 20081231 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 811HK 145256 DURING PRE FLIGHT INSPECTION, THE CREW FOUND THAT THE EMERGENCY LIGHT AT THE AFT CEILING EXIT LOCATOR WAS INOPERATIVE. MX PERFORMED AN OPS CHECK OF THE EMERGENCY LIGHTING SYSTEM WITH NO DEFECTS NOTED. 2 L 7 2 4T RT T00011AT 20090109 SO 2009 1 9 RAIA2008123100001 1 20081230 A 3397 WIRE EMB 145 EMB145LR 3260212 SO CABIN DAMAGED A RAIA K NONE L NO TEST IN INSP/MAINT 1 CE 03 811HK 145256 DURING PREFLIGHT INSPECTION EMERGENCY LIGHT INOPERATIVE AFT OF CEILING LOCATOR. MX DISCOVERED A LOOSE WIRING CONNECTION . MX REPAIRED DISCREPANT WIRE CONNECTION. OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 20090109 CE 2009 1 9 Z5FA121808N507CS1 1 20081218 A 2740 TRIM SYSTEM CESSNA 560 560XL 2076702 CE STABILIZER MALFUNCTIONED E Z5FA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 63 507CS 5605282 AFTER TAKEOFF, PITCH TRIM WAS INTERMITTENT. FLIGHT CREW DECLARED AN EMERGENCY AND DIVERTED TO DEPARTURE. MX PERFORMED A FULL PITCH TRIM AND AUTOPILOT SYS CHECK. NO DEFECTS NOTED. AN OPS CHECK FLIGHT WAS PERFORMED AND NO DEFECTS WERE NOTED . ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT A22CE 20090112 NM 2009 1 12 UALA2009010500052 1 20080103 A 2421 745329F IDG BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE NR 1 FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 675UA 29243 L GEN DRIVE LT CYCLING ON-OFF WITH THROTTLE MOVEMENT. ALSO HAD TO RECYCLE L GEN. REPLACED NR1 IDG & NR1 GCU. ACCOMPLIS HED ENG RUN, OPS CK AND BITE CK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20090112 NM 2009 1 12 FDEA200812245278 1 20081224 A 5320 65751724 CHANNEL BOEING 727 727233 138408A NM 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 FWD CARGO CORROSION AT STR 27R AND STA 680 ON STRINGER CHANNEL REMOVED CORRODED CHANNEL IAW SRM 51-30-2. FABRICATED NEW CHANNEL IAW SRM 51-10-2. INSTALLED NEW CHANNEL AT FWD CARGO STRINGER 27R, STA 680 IAW SRM 51-30-2 2 L 7 3 4F RT A3WE 20090112 NM 2009 1 12 FDEA200812245279 1 20081224 A 5330 65545753 SKIN BOEING 727 727233 138408A NM 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 EXT FUSELAGE, SKIN DENTED AT STA 700 STR 24L FOUND DENT OUT OF LIMITS IAW SRM 53-30-1 FIG 1. CUTOUT DAMAGED AREA AND FA BRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-10-2 FIG. 1 AND 53-30-2 FIG 2. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 20090112 EU 2009 1 12 NSVA2008048 1 20081221 A 3610 VALVE SAAB SF340 340B 7860101 EU BLEED AIR SYS STICKING A NSVA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 204CJ 204 SMOKE IN CABIN. VERIFIED NO SMOKE IN THE CABIN. FOUND LT HP VALVE STICKING AND NOT SHUTTING OFF AS IT SHOULD AT 64 DEG SWITCH. REMOVED AND REPLACED LT HP VALVE IAW AMM 36-11-10-02. PERFORMED OPS CHECKS IAW AMM 36-11-00. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 20090112 SO 2009 1 12 LR7A08126 1 20081218 A 5730 SKIN LKHEED 382 382G 526414U SO LT WING DAMAGED A LR7A K NONE O OTHER CL CLIMB 1 AL 03 401LC 1 4606 DURING CLIMB, ACFT SUSTAINED A BIRD STRIKE TO LT WING L/E AT FS480, WL284, OWS421. REPAIRS IN WORK. WILL UP DATE SDR A S FURTHER INFORMATION BECOMES AVALIABLE. LOG PAGE 26549. 2 H 7 4 4T A1SO 20090112 NM 2009 1 12 UHLA2009010900016 1 20081228 A 2751 WARNING SYSTEM EMB ERJ170 ERJ170100SE 3260406 NM COCKPIT MALFUNCTIONED A UHLA O OTHER N FALSE WARNING AP APPROACH 1 GL 11 858RW 17000080 WHEN SELECTING SLAT/FLAP 5 THE CREW RECEIVED A MASTER CAUTION AND ASSOCIATED EICAS MESSAGE STATING SLAT/FLAP LEVER DISAG REE. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MX REPOWERED THE ACFT AND TROUBLESHOT IAW FIM AND WAS U NABLE TO DUPLICATE THE FAULT. 2 L 7 2 4F RT A56NM 20090112 NM 2009 1 12 UHLA2009010900015 1 20081230 A 2751 59128437 SENSOR EMB ERJ170 ERJ170100SE 3260406 NM TE FLAP DEFECTIVE A UHLA O OTHER N FALSE WARNING AP APPROACH 1 GL 11 648RW 10514 17000068 ON APPROACH CREW RECEIVED A FLAP LO RATE MESSAGE FOLLOWED BY FLAP FAIL MESSAGE. THE CREW DECLARED EMERGENCY AND LANDED W ITHOUT INCIDENT. MAINTENANCE REPLACED THE RT T4 SKEW SENSOR. 2 L 7 2 4F RT A56NM 20090112 NM 2009 1 12 USAA2009010590027 1 20081224 A 5330 BEAR STRAP BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - NR 03-0553-8-0550/002 & 5031233 - 3 CRACKS ON FUSELAGE SKIN AT L1 DOOR LOWER HINGE CUTOUT IN S ECOND LAYER AT BS303, WL236.68, .125, .250, & .400 INCHES LENGTH. REPAIRED FUSELAGE SKIN AT L1 DOOR LOWER HINGE CUTOUT AT BS303, WL236.68 IAW US AIRWAYS EA 100773. 2 L 7 2 4F RT A16WE 20090112 NM 2009 1 12 USAA2009010590028 1 20081218 A 5315 6545810 FLOORBEAM BOEING 737 7374B7 138449C NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - NR 03C10753060/011 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT BS312, RBL13 & RBL30. REPA IRED FLOORBEAM AT BS312, RBL13 & RBL30 IAW B737 SRM 53-10-51. 2 L 7 2 4F RT A16WE 20090112 NM 2009 1 12 USAA2009010590026 1 20081223 A 5330 6545800 SKIN BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT Q5 MAJOR REPAIR NR 03-0553-8-0550/001 & 5031231 CRACK ON FUSELAGE SKIN AT L1 DOOR UPPER HINGE CUTOUT IN SECOND LAYER AT BS312, BETWEEN S8L & S12L. REPAIRED L1 DOOR UPPER HINGE CUTOUT SKIN IAW B737 US AIRWAYS EA NR100772. 2 L 7 2 4F RT A16WE 20090112 EU 2009 1 12 USAA2009010690040 1 20081229 A 5320 D53112827202 DUMMY RAIL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656AW 1079 SAL C7 MAJOR REPAIR NR 6131298 GALVANIC CORROSION ON DUMMY RAIL FLOOR STRUCTURE BETWEEN FR12 TO FR16, Y503. REPLACED DU MMY RAIL FLOOR STRUCTURE BETWEEN FR12 TO FR16, Y503 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20090112 EU 2009 1 12 USAA2009010690041 1 20081221 A 5320 D53480043203 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656AW 1079 SAL C7 MAJOR REPAIR NR 6129699 GALVANIC CORROSION ON LOWER SILL AT R2 DOOR AT FR66, -Y1292. REPAIRED LOWER SILL AT R2 D OOR AT FR66, -Y1292 IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 20090109 NM 2009 1 9 R5KB15950 1 20081220 A 5320 BEAM BOEING 727 727212 138407G NM FUSELAGE CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21845 LOWER BEAM CORRODED. 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 R5KB15781 1 20081218 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 SEAT TRACK FLANGE CORRODED. 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 ASAA0944162 1 20081218 A 5330 65C277994 SKIN BOEING 737 7374Q8 138447Q NM FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 RT EXTERNAL FUSELAGE DENTED AT STA 236 BELOW AND AFT OF EXTERNAL POWER DOOR. REMOVED DAMAGED AREA FABBED REPAIR PARTS I NSTALLED THE REPAIR IAW AAR EA 13108 AND ASA EA 400 53 EA 00454. 2 L 7 2 4F RT A16WE 20090109 EA 2009 1 9 ASOA200900034 1 20081231 A 2750 FLAP CNDAIR CL600 CL6002B19 1900309 EA WING FAILED A ASOA K NONE J WARNING INDICATION AP APPROACH 1 SO 27 903EV 7621 FLAP FAIL MSG WHEN SELECTING 0-8 ON APPROACH, SPEED 200 KNOTS, EMERGENCY DECLARED. 2 L 7 2 4F RT A21EA 20090112 NM 2009 1 12 UALA2008111302843 1 20080517 A 2741 SWITCH BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT STABILIZER FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 210UA 30216 "STAB AUTO SHUTDOWN" STATUS MSG IS DISPLAYED ON EICAS. STAB SYSTEM GND TEST FAILS. EXISTING FAULTS MAINT MSG 27-10007, 27-10010. UNABLE TO CONTROL STAB TRIM USING RIGHT STAB TRIM CUTOUT SWITCH, STAB CONTINUES TO MOVE WITH SWITCH IN CUTOU T. REPLACED STCM SHUTOFF VALVE. PERFORMED OPS CHECK. OPS CHECKED NORMAL. FAILED STABILIZER SYSTEM GROUND TEST. REPL ACED RELAY K27008, REF WD27-41-13, NO HELP. ORDERED ACE FROM LAX. NO "STAB AUTO SHUTDOWN" MSG ON EICAS. RIGHT NOW ACF T FAILED STABILIZER TEST RIGHT AFTER RT STAB CUTOUT TEST. REMOVED AND REPLACED RT ACE NO HELP. REINSTALLED ORIGINAL UN IT, ACP FIM 27-1008 AND REPLACED STAB CUTOUT SWITCH. PASSED STABILIZER TEST. NO STATUS MESSAGES OR EXISTING FAULTS. S 2 L 7 2 4F 4 F RT T0001SE E46NE 20090112 EU 2009 1 12 MALA080218 1 20081211 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 340B430 DURING N4K, 2Y INSPECTIONS IN CWA, FOUND FRAME AT STA 363 AT SL1505 CHAFED. REPAIRED CHAFE IAW EO NR S53644 AND S53152. 2 L 7 2 4T RT A52EU 20090112 NM 2009 1 12 USAA2009010590036 1 20081218 A 5320 907822 STRAP BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - NR 03C10753006/007 - CRACK ON L1 DOOR FRAME STRAP AT UPPER HINGE CUTOUT AT BS294.5, S9L. REPL ACED L1 DOOR FRAME STRAP AT UPPER HINGE CUTOUT AT BS294.5, S9L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20090112 EU 2009 1 12 USAA2009010790044 1 20081223 A 5320 D53480043202 SILL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656AW 1079 SAL - C7 - MAJOR REPAIR - NR 6129688 - GALVANIC CORROSION ON LOWER SILL AT L2 DOOR BETWEEN FR66 TO FR68, Y1732. REPAIRE D LOWER SILL AT L2 DOOR BETWEEN FR66 TO FR68, Y1732 IAW A320 SRM 53-41-14. 2 L 7 2 4F RT A28NM 20090112 EU 2009 1 12 USAA2009010790045 1 20081230 A 5321 D5361060500100 FLOOR PANEL AIRBUS 320 A320232 3930326 EU CABIN CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656AW 1079 SAL - C7 - MAJOR REPAIR - NR 6129498 - CORROSION ON FLOORBOARD PANEL NR 222FF, (R1 DOOR ENTRY). REPLACED FLOORBOARD PA NEL NR 222FF, (R1 DOOR ENTRY). 2 L 7 2 4F RT A28NM 20090109 EU 2009 1 9 FDEA200812245272 1 20081224 A 5310 STRUCTURE AIRBUS 310 A310324 3930206 EU ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 810FD 452 AIR CONDITIONING COMPT BETWEEN FR44 AND FR45, STR 38R AND 39R HAS SURFACE CORROSION. REMOVED LIGHT SURFACE CORROSION IAW SRM 51-74-10, MATERIAL LOSS .001 IN. TREATED AND PRIMED IAW SRM 51-21-10, PAINTED IAW MM 75-10-08. 2 L 7 2 4F RT A35EU 20090109 2009 1 9 UIEA200900004 4 20081229 A 3442 DRIVE ASSY BOEING 747 74747UF 1384812 NM WX RADAR SYS FAILED A UIEA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 EA 15 412MC 30559 AIR TURN BACK, CREW PHONE PATCHED THAT THEY LOST NR 1 WX RADAR SYSTEM. NR 2 WX RADAR SYSTEM WAS ALREADY ON DEFERRAL. C REW RETURNED TO BKK. MAINTENANCE REMOVED AND REPLACED RADAR DRIVE ALL SYSTEMS, OPS CHECKED OK. 2 L 7 4 4F RT A20WE 20090109 NM 2009 1 9 FDEA200812265306 1 20081226 A 5744 ARC050213 HINGE BRACKET DOUG MD11 MD11F 3023600 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 LEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE ACTUATOR ATTACH OUTBOARD HOLE FOUND WITH CORROSION. REPAIRED AS PER EA 1- 5750-122667. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090109 NM 2009 1 9 R5KB15782 1 20081218 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 SEAT TRACK CORRODED. 2 L 7 3 4F A3WE 20090113 SO 2009 1 13 SIMA200900904 1 20081229 A 2611 SMOKE DETECTOR EMB 145 EMB145LR 3260212 SO LAVATORY MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 909AE 14500899 ON FLIGHT 3862, CREW REPORTED JUST AFTER TAKE OFF, AS THE LANDING GEAR RETRACTED, LAV SMOKE ALARM ON EICAS AND ALARM IN THE LAV SOUNDED. BOTH WENT AWAY WHEN LANDING GEAR WAS RETRACTED. ACFT REMOVED FROM SERVICE . PERFORMED OPS CHECK OF LAV SMOKE DETECTION SYS. IAW AMM 26-14-00 NO DEFECTS NOTED AT THIS TIME, NO OIL OR SMOKE SMELL DETECTED. ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20090113 EA 2009 1 13 SWIA200820767 1 20081203 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 608SK 10252 DURING C-CHECK, FS 280 FLOORBEAM CRACKED AT LBL13. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090114 NM 2009 1 14 AALA200802602A 1 20081129 A 3350 LAMP BOEING 737 737823 13844CB NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 946AN 30600 MIA EMERGENCY LIGHT AT LT FORWARD DOOR INOPERATIVE. REPLACED LAMP AT FORWARD LEFT HAND DOOR. SYSTEM GROUND CHECKED NOR MAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 20090114 NM 2009 1 14 AALA200802603A 1 20081129 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 EMERGENCY LIGHT AT SEAT 21G MISSING LENS. REPLACED LENS AT SEAT 21G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20090114 NM 2009 1 14 AALA200802604A 1 20081129 A 3350 LENS BOEING 777 777223 1385213 NM ZONE 200 MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 DFW EMERGENCY LIGHT AT SEAT 26G MISSING LENS. REPLACED LENS AT SEAT 26G. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOS ED) 2 L 7 2 4F RT T00001SE 20090114 NM 2009 1 14 AALA200802606A 1 20081129 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 DFW EMERGENCY LIGHT AT SEAT 38G MISSING LENS. REPLACED LENS AT SEAT 28G. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOS ED) 2 L 7 2 4F RT T00001SE 20090114 EA 2009 1 14 A6WA200840649 1 20081217 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 416AW 7603 MWC 15 FS 621 PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING IS CRACKED. PERFORMED A REPAIR BY CUTT ING OUT SECTION OF WEB, FABRICATING AND INSTALLING REPAIR PARTS IAW BOMBARDIER REO 601R-53-61-1230 REV D. 2 L 7 2 4F RT A21EA 20090114 NM 2009 1 14 HNAA2009010900385 1 20080616 A 5320 85320686101 THRESHOLD DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 980HA 32623 32623 376 DURING C-CHECK INSP, THE PAX DOOR THRESHOLD WAS FOUND TO BE CORRODED. THIS ITEM WAS R&R IAW SRM PROCEDURES. A BRACKET U NDERNEATH THE THRESHOLD, P/N 85321069-101, WAS ALSO FOUND CORRODED. A REPLACEMENT WAS FABRICATED AND THE BRACKET REPLAC ED. ADDITIONALLY, THE FWD INBD LT SEAT RAIL P/N 85320490-133, WAS ALSO FOUND TO BE DEEPLY CORRODED. THIS ITEM WAS ALSO R&R. 2 H 7 2 4T RT A13NM 20090114 NM 2009 1 14 AALA200802618 1 20081130 A 3350 SHROUD BOEING 757 757223 1384957 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 682AA 25339 DFW - EMERGENCY LIGHT AT SEAT 17D SHROUD BROKEN. REPLACED SHROUD AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20090114 NM 2009 1 14 AALA200802573A 1 20081123 A 3350 CONNECTOR BOEING 737 737823 13844CB NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 934AN 29531 MIA EMERGENCY LIGHT AT SEAT ROW 19 INOPERATIVE. SECURED CONNECTOR ON SIDE WALL AT SEAT ROW 19DEF. SYSTEM GROUND CHECKE D NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A16WE 20090114 NM 2009 1 14 DHLA2009770AT508 1 20081219 A 5311 FRAME BOEING 727 7272B7 138407L NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 770AT 21953 UPPER FUSELAGE CARGO CABIN FRAME WITH DENT AT BS 580 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME SECTION BS 580 BT WN S-16R AND S-17R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20090114 2009 1 14 AALA200802575A 4 20081124 A 3442 6225132109 TRANSCEIVER BOEING 767 767323 1385205 NM WX RADAR SYS FAILED A AALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 SW 21 381AN 25450 GIG INFLIGHT. CREW REPORTED WEATHER RADAR WENT INOPERATIVE DURING FLIGHT. RETURNED TO GIG AND LANDED WITHOUT INCIDENT. REPLACED WEATHER RADAR TRANSCEIVER. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A1NM 20090114 NM 2009 1 14 DHLA2009770AT509 1 20081211 A 5320 STRAP BOEING 727 7272B7 138407L NM FUSELAGE CRACKED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 770AT 21953 LOWER FUSELAGE STABILIZER STRAP WITH CRACK AT BS 344 LBL 23 WL 201. REPAIRED STABILIZER STRAP FROM BS 324.5 TO BS 347.5 AT LBL 23 IAW B727 SRM 53-10-8 FIG 6. 2 L 7 3 4F A3WE 20090114 NM 2009 1 14 DHLA2009770AT510 1 20081218 A 5311 FRAME BOEING 727 7272B7 138407L NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 770AT 21953 UPPER FUSELAGE CARGO CABIN FRAME WITH DENT AT BS 640 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME SECTION BS 640 BE TWEEN S-16R AND S-17R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20090114 NM 2009 1 14 DHLA2009770AT511 1 20081205 A 5330 SKIN PANEL BOEING 727 7272B7 138407L NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 770AT 21953 LOWER FUSELAGE AT BS 316 BETWEEN S-22R AND S-23R SKIN WITH DENT. REPAIRED FUSELAGE SKIN SECTION FROM BS 309.25 TO BS 32 3 BETWEEN S-21R AND S-24R IAW B727 SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 20090114 NM 2009 1 14 DHLA2009770AT512 1 20081211 A 5322 SHEAR TIE BOEING 727 7272B7 138407L NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 770AT 21953 LOWER FUSELAGE AFT CARGO COMPARTMENT BS 1050 BETWEEN S-26L AND S-27L SHEARTIE WITH CORROSION. REPLACED FUSELAGE SHEARTI E SECTION AT BS 1050 BETWEEN S-26L AND S-27L. 2 L 7 3 4F A3WE 20090114 WP 2009 1 14 AALA200802577A 1 20081124 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 567AM 53293 ORD RIGHT HAND SEAT MOUNTED EMERGENCY LIGHTS AT FORWARD HALF OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNT ED EMERGENCY LIGHTS AT FORWARD HALF OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A6WE 20090114 WP 2009 1 14 IXXA08SMN205S 1 20081025 A 5315 FLOORBEAM DOUG DC8 DC862F 3021972 WP FUSELAGE CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE CENTER SECTION FLOORBEAM LOWER HORIZONTAL FLANGES AND FLOOR PRESS P ANEL CORRODED AT STATION 902.000 LBL 51. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING DAMAGED SPLICE ANGL E. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED MODIFIED SPLICE ANGLE S, FILLERS, PANEL SEGMENT, EXTERNAL REPAIR DOUBLERS, STRAPS, TAPERED STRAPS, INTERNAL FINGER DOUBLER. PERFORMED HEAT TR EATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED IAW FAA FORM 8110-3 NUMBER 08543 DATED 11/18/08, SE MAN DRAWING ED-4871 DATED 11/06/08, DC8 SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 53-2- 2 L 7 4 4F 4A25 20090114 WP 2009 1 14 AALA200802590A 1 20081126 A 2842 5D03271 RELAY DOUG DC9 DC982 3022082 WP FUEL QTY FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 223AA 49173 INFLIGHT ORD TO LAX. CREW REPORTED ALL FUEL QUANTITY INDICATIONS INOPERATIVE. CIRCUIT BREAKER POPPED. LANDED ABQ WITHOU T INCIDENT. REPLACED RELAY FROM AFT GALLEY DRAIN MAST HEAT POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20090114 NM 2009 1 14 AALA200802592A 1 20081126 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 790AN 30251 EMERGENCY LIGHT AT SEAT 32G MISSING LENS. REPLACED LENS AT SEAT 32G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20090114 NM 2009 1 14 AALA200802593A 1 20081126 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 790AN 30251 EMERGENCY LIGHT AT SEAT 32G MISSING LAMP. REPLACED LAMP AT SEAT 32G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20090114 NM 2009 1 14 AALA200802594A 1 20081126 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 790AN 30251 EMERGENCY LIGHT AT SEAT 33G MISSING LENS. REPLACED LENS AT SEAT 33G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20090114 NM 2009 1 14 AALA200802596A 1 20081127 A 2910 B-NUT BOEING 757 757223 1384957 NM HYD LINE LOOSE A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 199AN 32393 INFLIGHT LEFT HAND HYDRAULIC SYSTEM QUANTITY DROPPED TO .18. LANDED MCO WITHOUT INCIDENT. TIGHTENED LOOSE B-NUT ON LEF T HAND PRESSURE LINE TO ALT SHUTTLE VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20090114 WP 2009 1 14 IXXA08SMN211S 1 20081028 A 5320 4753360U502 FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 834.000 LONGERON 22 RIGHT. R EMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-1, AND DC8 SRM 51-1-8B. 2 L 7 4 4F 4A25 20090114 NM 2009 1 14 AALA200802597A 1 20081127 A 3350 CHARGER BOEING 757 757223 1384957 NM EMERGENCY LIGHTS FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 672AA 25337 EMERGENCY LIGHT FROM SEAT ROWS 14 TO 36 INOPERATIVE. REPLACED BATTERY CHARGER FOR SEAT ROWS 14 TO 36. SYSTEM GROUND CHE CKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20090114 NM 2009 1 14 AALA200802607A 1 20081129 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 EMERGENCY LIGHT AT SEAT 45G INOPERATIVE. REPLACED LAMP AT SEAT 45G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20090114 NM 2009 1 14 AALA200802608A 1 20081129 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 EMERGENCY LIGHT AT SEAT 45G MISSING LENS. REPLACED LENS AT SEAT 45G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20090114 EU 2009 1 14 MALA080224 1 20081229 A 3350 LIGHT SAAB SF340 340B 7860101 EU EXTERIOR INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 423XJ 340B423 LT OUTSIDE EMERGENCY OVERWING EXIT LIGHT WAS BURNT OUT. REPLACED BULB. 2 L 7 2 4T RT A52EU 20090114 EA 2009 1 14 MALA080221 1 20081222 A 3260 BRACKET CNDAIR CL600 CL6002B19 1900309 EA NLG DEFECTIVE A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 602XJ 8044 DURING CLIMB-OUT AT MSP, RECEIVED A GEAR DISAGREE WARNING MESSAGE ALONG WITH NOSE DOOR WARNING MESSAGE. BOTH MAIN GEAR INDICATED UP AND LOCKED AND NOSE GEAR DOWN AND LOCKED. COMPLETED GEAR DISAGREE NON-NORMAL CHECKLIST. RETURNED TO MSP F OR A PRECAUTIONARY LANDING. LANDING UNEVENTFUL. NOSE WHEEL STEERING WORKED FINE. REMOVED AND REPLACED NLG CENTERING/E XTENDED BRACKET FOR PROXIMITY SENSOR P/N ON/OFF 16215-105 NSN PER AMM 32-61-05. PERFORMED GEAR SWING SEVERAL TIMES. OP S NORMAL PER AMM 32-30-00. 2 L 7 2 4F RT A21EA 20090114 CE 2009 1 14 MALA080223 1 20081214 A 2910 PDU CESSNA 177 177B 2073708 CE LEFT MALFUNCTIONED H MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 410 17702536 "AFTER T/O SELECTED GEAR UP AND HYDRAULIC CAUTION LIGHT ILLUMINATED. COMPLETED MEMORY ITEMS THEN COMPLETED AFTER T/O CH ECK. COMPLETED EMERGENCY/NON-NORMAL CHECKLIST HYDRAULIC PROC 2. RETURNED TO TRI. DECLARED EMERGENCY AND RETURNED TO G ATE. FLAPS REMAINED ZERO. REMOVED AND REPLACED LT PDU IAW SAAB AMM 24-31-20. OPS CHECK GOOD AT THIS TIME, P/N ON AND OFF A2042C, S/N ON CL-86429, S/N OFF CG-81553. REMOVED AND REPLACED RELAY 7ML IAW SAAB AMM 20-20-00 OPS CHECK GOOD, P/N ON AND OFF MS24142D1. 1 H 7 1 3O A13CE 20090114 NE 2009 1 14 FDEA200812235266 2 20081223 A 7261 21SN04334 PRESSURE SWITCH DOUG MD11 MD11F 3023600 NM GE CF6 CF680 30025 NE NR 3 ENGINE FROZEN A FDEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 21 617FE 48748 702294 LOW SPEED REJECTED T/O AT 75KT DUE TO LEVEL 2 ENGINE OIL FILTER 3 ALERT. COMPLETED RTO AND OIL FILTER CHECK LISTS. OIL TEMPS WERE ALL AT 65 DEGREES. ACFT COLD SOAKED FROM SITTING IN VERY COLD AIR FOR 2 DAYS. CONTACTED MX AND AGREED THAT P ROBLEM WAS MOST LIKELY DUE TO COLD SOAK. SECOND T/O SUCCESSFUL. R&R SCAVENGE OIL FILTER ELEMENT PER MM 79-22-05-4-1 & O IL FILTER DIFFERENTIAL PRESSURE SWITCH PER MM 7 9-35-01-4 1 ON NR 3 ENGINE. NR 3 ENGINE RAN PER 340709 IAW JRH. LEAK CHECK OK 2 L 7 3 4F 4 F RT A22WE E13NE 20090114 WP 2009 1 14 IXXA08SMN216S 1 20081028 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 420.00 0 LONGERON 17-18 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABR ICATED ANGLE DOUBLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08549, SEMAN DRAWING ED-4877, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-1 PAGES 1, 13, AND 17, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D, AND SRM 51-3-1. 2 L 7 4 4F 4A25 20090114 WP 2009 1 14 IXXA08SMN217S 1 20081028 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 1040.0 00 LONGERON 19-20 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FAB RICATED ANGLE DOUBLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PAR TS IAW FAA FORM 8110-3 NUMBER 08549, SEMAN DRAWING ED-4877, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-1 PAGES 1, 13, A ND 17, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D, AND SRM 51-3-1. 2 L 7 4 4F 4A25 20090114 EU 2009 1 14 MALA080219 1 20081210 A 5311 FRAME SAAB SF340 340B 7860101 EU FUSELAGE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 340B430 DURING N4K, 2Y INSPECTIONS IN CWA, FOUND FRAME AT STA363 AT SL1605 CHAFED. REMOVED AND REPLACED INNER FLANGE REINFORCEM ENT ANGLE P/N 7253742-111, IAW SAAB 51-40-21 AND EO NR S53644. 2 L 7 2 4T RT A52EU 20090114 EU 2009 1 14 MALA080222 1 20081216 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED H MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 417XJ 340B417 FLOOR PROXIMITY ESCAPE PATH LIGHTS 46LN 47LN 48LN ARE INOP. REPLACED EMERGENCY POWER SUPPLY 24LN IAW AMM 33-50-10. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 20090114 WP 2009 1 14 IXXA08SMN204S 1 20081025 A 5753 SKIN DOUG DC8 DC862F 3021972 WP TE FLAP CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP LEADING EDGE CORRODED AT STATION XW 2.000-91.000. REMOVED CO RROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INS PECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED NEW SKIN, AND FILLER. CLEANED, TREATED, PRIMED AREA, AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08543 DATED 11/18/08, SEMAN DRAWING ED-4878 DATED 11/11/08, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 57-2-0 PAGE 16, DC8 SRM 51-1-21, SRM 51-3-0, DC8 NDT SPM PART 06-10- 01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND SRM 51-3-1. 2 L 7 4 4F 4A25 20090115 NM 2009 1 15 C8GA20080068 1 20081024 A 5313 BAC1498143 STRINGER BOEING 727 727223 1384074 NM ZONE 100 CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 22470 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT STRINGER 22L WAS CORRODED AT B.S. 1177. DAMAGE WAS OU T OF LIMITS. CUT OUT DAMAGED AREA AT STR. 22L AT B.S 1177, FABRICATED 2 EA STR. REPAIR MATERIALS FROM BAC 1498-143 7075T 6 (14 3/8" & 9 1/4"). FABRICATED 2 EA SPLICES FROM BAC 1498-132. INSTALLED REPAIR IAW SRM 53-10-2, 53-10-3 AT STR. 22L S TATION 1165-1189. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20090115 NM 2009 1 15 C8GA20080073 1 20081219 A 7930 OIL SYSTEM BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE READS HIGH A C8GA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 29 713AA 55651 22469 708910 FLT 706 FROM TOL TO MSP. DURING CRUISE OPERATION THE NR 2 ENGINE LOW OIL PSI LIGHT ILLUMINATED. APPROPRIATE CHECKLIST W AS FOLLOWED AND THE ENGINE WAS SHUT DOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT IN MSP. POST FLIGHT INSPECTION WAS PERFOR MED, FOUND NR 2 ENGINE OIL BREATHER PRESSURE TO BE 14 PSI. ENGINE SCHEDULED FOR REMOVAL AND REPLACEMENT. 2 L 7 3 4F 4 F A3WE E2EA 20090115 NM 2009 1 15 FDEA200812275310 1 20081227 A 5311 AFA00183 FRAME DOUG MD11 MD11F 3023600 NM ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 MAIN DECK CARGO - LT FRAME STATION 1741 AT LONGERON 11 FOUND DENT. REPAIR CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOLU ME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. DAMAGE TOLERANCE INSPECTION REQUIRED AT INITIAL FLIGHT CYCLE 14,500 AS PER SRM 53-30-00 FIGURE 1 VOLUME I. 2 L 7 3 4F RT A22WE 20090115 NM 2009 1 15 FDEA200812275311 1 20081227 A 5311 AFA00183 FRAME DOUG MD11 MD11F 3023600 NM BS 1741 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 MAIN DECK CARGO RT FRAME STATION 1741 AT LONGERON 11 FOUND DENTED. REPAIR CARRIED OUT AS PER SRM 53-30-00 FIGURE 1 VOL UME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. DAMAGE TOLERANCE INSPECTION REQUIRED AT INITIAL FLIGHT CYCLE 14,50 0 AS PER SRM 53-30-00 FIGURE 1 VOLUME I. 2 L 7 3 4F RT A22WE 20090115 EU 2009 1 15 FDEA200812315322 1 20081231 A 3230 DSB11021 SENSOR AIRBUS 310 A310 EU MLG MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 804FD 549 AFTER T/O LANDING GEAR FAILED TO RETRACT. ECAM DISPLAYED L/G RETRACTION INOP. ACFT LOST AUTO-THROTTLES. FOUND TARGET SENSORS 9GA AND 11GA LOS SE AND OUT OF "C" DIMENSIONS OUT OF LIMITS; REMOVED AND REPLACED SENSORS 9GA AND 11GA ON LT BO GIE REF. MM 32-00-00-4. JACKED ACFT AND PERFORMED GEAR SWING REF MM 32-31-00 IN BOTH SYSTEMS 1 AND 2, OPS CHECK NORMAL, NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F RT A35EU 20090115 EU 2009 1 15 AJAA20090113 1 20081218 A 3060 SMR2360 LEAD PILATS PC12 PC1245 7090551 EU PWA PT6 PT6A67D NE PROP DE-ICE BROKEN E AJAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 AL 05 933SP 240 ACFT HAD PROP DE-ICE FAILURE LIGHT. FLIGHT RETURNED TO MX BASE FOR REPAIRS. TROUBLESHOOTING INDICATED DE-ICE TIMER FAI LURE. REPLACED AND GROUND RUN AND FUNCTION CHECKED CORRECT. NEXT DAY LEFT ON FLIGHT AND WITHIN 20-30 MINUTES SAME FAIL URE INDICATION. DUE TO NO MX AT FWD LOCATION RETURN TO DEPARTURE BASE FOR REPAIR. AFTER MUCH MORE INTENSE SCRUTINY FOU ND DE-ICE BLADE LEADS BAD AND REPLACED ALL 4 ITEMS. RUN/FUNCTION AND FLIGHT CHECKED GOOD. NO FURTHER PROBLEMS. SYS NO T MECHANIC FRIENDLY TO TROUBLESHOOTING. LEADS ALMOST NEED TO BE REMOVED FROM BLADE TO THOROUGHLY OHM OUT AND FIND POTEN TIAL PROBLEMS. 1 L 7 1 3T 4 T RT A78EU E26NE 20090115 EA 2009 1 15 SWIA200820816 1 20081217 A 5320 STRUCTURE CNDAIR CL600 CL6002D24 1390016 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 803SK 15062 DURING C-CHECK FOUND, FS 280 CRACKED AT RBL9. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090116 EA 2009 1 16 A6WA200840651 1 20081218 A 3246 WHEEL CNDAIR CL600 CL6002B19 1900309 EA NLG & MLG LOOSE A A6WA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 GL 31 469AW 7917 LOG 193468/1 EXTREME VIBRATION ON TAKEOFF ROLL. ABORTED TAKEOFF AT 85 KNOTS. BRAKE TEMPS WERE 3,3,2,3. INSPECTED AND RETORQUED NR 1 NLG TIRE, NR 1 MLG TIRE AND NR 4 MLG TIRE IAW CRJ AMM 32-42-01, 32-41-01 AND AMM SUP 08056. NO DEFECTS N OTED. 2 L 7 2 4F RT A21EA 20090112 NM 2009 1 12 DHLA2008743527 1 20081108 A 5311 FRAME BOEING 727 727225 1384077 NM BS 1090 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 "D" CHECK, UPPER FUSELAGE PAX CABIN BS 1090 BETWEEN 13L & 14L FRAME I/B FLANGE WITH DOUBLE HOLES & DENT. REPAIRED FUSEL AGE FRAME SECTION AT BS 1090 BETWEEN STR. 11L & STR.14L DUE TO DOUBLE HOLES & DENT IAW SRM 53-10-4 FIG.1 2 L 7 3 4F A3WE 20090112 EU 2009 1 12 FDEA200812295316 1 20081229 A 5420 SUPPORT AIRBUS 310 A310203 3930313 EU PRECOOLER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 436FE 40324 454 NR 1 PRECOOLER SUPPORT IS CRACKED. MATERIAL ID PER ASTME-1476-01 & WELD PER P.S. 01-04-21. 2 L 7 2 4F RT A35EU 20090112 NM 2009 1 12 UALA2008111306132 1 20081016 A 3260 835109 CIRCUIT CARD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE PSEU FAULTY A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 641UA 25091 AFTER TAKEOFF AIR-GND DISAGREE STATUS MSG. RTFL. REPLACED ENTIRE PROXIMITY SWITCH ELEC UNIT WITH ALL CARDS AND NLG SWG OPS OK. REF SCHEMATIC:32-09-03 AND 32-09-02. REPLACED RELAYS K203, K293, K219 AND K209. AIR-GND RELAY TEST FAILS STE P I(3) AND I(7) FOR SYSTEM 1, PG 507-508 OF MM 32-09-02. SYSTEM 2 OPERATES OKAY. ACCOMPLISHED FIM 32-09-00 FIG103A. F IM SUGGESTS ADJUSTING SENSOR CLEARANCE (BLOCK 43, PG 116). HOWEVER, SENSORS ARE SLUGGED PER BLOCK 8 SO THERE IS NO ADJU STMENT. ACP TEST REF MM32-09- 02, NO FAULTS. CHRONIC AIR-GRD MSG, SUGGEST REPLACED DRIVE R CARD IN PSEU REF MM32-09-06 . REPLACED DRIVE R CARDS PER MM 32-09-06. OP CKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20090109 EA 2009 1 9 HNAA2009010600376 1 20081122 A 5320 85333844101 SILL DHAV DHC8 DHC8311 1386006 EA FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 326EN 33224 33224 234 DURING C-CHECK INSPECTIONS, CORROSION WAS FOUND ON THE LOWER DOOR SILL FOR THE AFT RT SERVICE DOOR. AREA OF CORROSION W AS CLEANED, ALODINE AND PRIMER APPLIED IAW DEHAVILLAND STRUCTURAL REPAIR MANUAL. 2 H 7 2 4T RT A13NM 20090109 WP 2009 1 9 FDEA200811285002 1 20081128 A 5512 ALC70821 SKIN DOUG MD10 MD1010F 3022112 WP HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 387FE 46621 RT HORIZONTAL STAB FRONT SPAR CAP AND UPPER PORTION OF THE SKIN CRACKED AT STA XF 88.834, (N/R 513 GENERATED WO 43105). INSTALLED RT HORIZONTAL STAB FRONT SPAR CAP REPAIR IN REF TO SRM 55-20-00 PG 42 FIGURE 8 CAT A REPAIR. 2 L 7 3 4F RT A22WE 20090109 NM 2009 1 9 FDEA200812245286 1 20081224 A 5311 FRAME BOEING 757 75728A 1384976 NM BS 780 S24-25R DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 912FD 24260 FWD PIT, FUSELAGE FRAME BS 780, INNER CHORD, (SLOPING), BETWEEN S24R AND S25R, HAS A DENT. REMOVED DAMAGED SECTION OF B S 780 FRAME, BETWEEN S24R AND S25R, PER SRM 53-00- 07, REPAIR NR 5. RECEIVED FABRICATED FRAME REPAIR PARTS ON MAE TRAV ELER NR T8/772747. LOCATED, DRILLED, TREATED AND PRIMED REPAIR PARTS PER SRM 51-20-01, 51-21-00 AND 51-40-02. INSTALLE D BS 780 FRAME REPAIR, BETWEEN S24R AND S25R, PER SRM 51-40-02, 51- 20-05, AND 53-00-07, REPAIR NR 5. THIS REPAIR IS CL ASSIFIED AS A CAT "B" MAJOR REPAIR WITH THE FOLLOWING TRACKING REQUIREMENTS: INITIAL AT 37,500 FC AT TIME OF REPAIR OR 5 0,000 FC WHICHEVER OCCURS FIRST, THEREAFTER EVERY 12,000 FC. 2 L 7 2 4F RT A2NM 20090109 WP 2009 1 9 NWAA085659928 1 20081217 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8921E 45836 DURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION OF THE CABIN HAD FAILED. MX R EPLACED THE ASSOCIATED FUSE AND THE POWER SUPPLY. OPS CHECK WAS GOOD. 2 L 7 2 4F A6WE 20090109 EA 2009 1 9 MALA080215 1 20081216 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 1900309 EA UNKNOWN A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 8943A 7943 AFTER TAKEOFF "SMOKE TOILET" CAUTION ILLUMINATED. FLIGHT ATTENDANT REPORTED SMOKE ALARM SOUNDING. COMPLETED POM CHECKL IST, PRECAUTIONARY LANDING. COMPLETED MM 409 NR 352872 REPLACEMENT OF L AND R COALESCER BAGS, INSPECTION FOR OIL LEAKS, REPLACEMENT OF LAV SMOKE DETECTOR. REF WORK CARD FOR DETAILS. FROM 409 352872 REPLACED LEFT AND RIGHT COALESCER BAGS PN 783689-3 IAW CRJ200 AMM 21-51-13 COMPLETED GROUND RUN AT PWR SETTINGS OPERATING NR 1 LT AND NR 2 RT A/C PACKS NO FAUL T NOTED INSPECTED RT ACM INLET AND NO SIGN OF OIL NOTED REPLACED LAV SMOKE DETECTOR IAW AMM 26-16-00. OPS CK GOOD. 2 L 7 2 4F RT A21EA 20090109 NM 2009 1 9 NWAA085665503 1 20081218 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM CABIN FAULTY A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 503US 23192 DURING AN OVERNIGHT LINE CHECK THE EMERGENCY ESCAPE PATH LIGHTING FAILED TO OPERATE FROM ROW 14 TO ROW 22. MX FOUND POW ER SUPPLY M735 TO BE FAULTY AND REPLACED IT. SYSTEM OP WAS NORMAL AFTER THE POWER SUPPLY WAS REPLACED. 2 L 7 2 4F RT A2NM 20090109 NM 2009 1 9 UIEA200900001 1 20081230 A 4990 APU BOEING 747 747341 13848AM NM ZONE 200 LEAKING A UIEA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 15 355MC 23395 ON TAXI IN APU OIL CONSUMPTION WAS HIGH AND THERE WAS A STRONG ODOR OF OIL WHEN USING THE APU. THE APU WAS PLACED ON ME L DEACTIVATED PER 49-01. 2 L 7 4 4F RT A20WE 20090109 2009 1 9 UIEA200900003 4 20081224 A 3441 46300161300413 INU BOEING 747 747228F 1384895 NM NR 1 FAILED A UIEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 809MC 20887 AIR TURN BACK DUE TO NR 1 INS RED WARNING LIGHT ON WITH HDG AND FLIGHT DIRECTOR FLAGS IN VIEW. FOUND NR 1 INU FAILED. REPLACED INU, OPS CHECKED OK. 2 L 7 4 4F RT A20WE 20090109 NM 2009 1 9 FDEA200812265305 1 20081226 A 5744 HINGE DOUG MD11 MD11F 3023600 NM LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 LEFT WING OUTBOARD FLAP INBOARD FORWARD HINGE ACTUATOR ATTACH INBOARD HOLE FOUND WITH CORROSION. REPAIRED AS PER EA 1 -5750-122667. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090109 NM 2009 1 9 FDEA200812265308 1 20081226 A 5744 ARC050311 HINGE BRACKET DOUG MD11 MD11F 3023600 NM ZONE 500 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 LEFT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE LOWER ATTACH INBOARD HOLE FORWARD AND AFT SURFACE FOUND WITH CORROSION. REWORKED AS PER EA 1-5750-127701. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090109 EA 2009 1 9 MALA080216 1 20081217 A 3220 BRACKET CNDAIR CL600 CL6002B19 1900309 EA NLG PROX SENSOR DAMAGED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 832AY 8032 NOSE WHEEL DID NOT RETRACT AFTER TAKEOFF WHEN GEAR WAS SELECTED UP GEAR DISAGREE AND NOSEWHEEL DOOR OPEN WARNINGS ANNUNC IATED. GEAR DID NOT RETRACT. RAN EMERGENCY CK LIST, EXTENDED GEAR MANUALLY. DECLARED EMERGENCY BACK INTO MSP LANDED B ELOW 47,000 DESCENT RATE BELOW 600 FT PER MIN. AIRSPEED REMAINED AT 200 IAS NO OVERWEIGHT LANDING. COMPLETED MM409 NR 352863. REPLACED NLG OLEA CENTER/EXTENDED PROX SENSOR BRACKET PN 16215-105 AND ADJUSTED SENSOR GAP. OPS CHECK GOOD. 2 L 7 2 4F RT A21EA 20090109 WP 2009 1 9 NWAA085689993 1 20081220 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8966E 47402 DURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK WAS INOPERATIVE. MX REPLACED THE POWER S UPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 2 L 7 2 4F A6WE 20090109 NM 2009 1 9 R5KB15795 1 20081218 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 SEAT TRACK CORRODED. 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 R5KB15808 1 20081219 A 5320 WEB BOEING 727 727212 138407G NM FUSELAGE CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 UNDER FLOOR WEB CORRODED. 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 R5KB15825 1 20081219 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 SEAT TRACK FLANGE CORRODED. 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 R5KB15776 1 20081220 A 5320 WEB BOEING 727 727212 138407G NM FUSELAGE CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 SUB FLOOR CORRODED 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 R5KB15785 1 20081218 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 SEAT TRACK CROWN AND FLANGE CORRODED 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 R5KB15546 1 20081218 A 5330 SKIN BOEING 727 727212 138407G NM FUSELAGE DENTED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 DENT IN SKIN STA 328 ABOVE FWD ENTRY DOOR 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 R5KB15750 1 20081218 A 5520 HINGE FITTING BOEING 727 727212 138407G NM ELEVATOR CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 ELEVATOR UPPER HINGE CORD CORRODED. 2 L 7 3 4F A3WE 20090108 WP 2009 1 8 WRLA2008108 1 20081227 A 2910 HYDRAULIC SYSTEM DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 1 MALFUNCTIONED A WRLA K NONE K FLUID LOSS DE DESCENT 1 SO 11 137 48282 WHILE EXTENDING SLATS, FELT A BUMP; NR 1 HYD SYS LOST FLUID AND PRESSURE, COMPLETED CHECKLIST AND PROCEEDED WITH UNEVENT FUL LANDING AND PARKING. C/A: OPEN 2 L 7 3 4F 4 F A22WE E23EA 20090108 NM 2009 1 8 KPVA2008-05 1 20081220 A 7997 2D20 WIRE DHAV DHC8 DHC8103 1386005 NM PWA PW121 PW121 52124 NE OIL PRESSURE INTERMITTENT A KPVA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 WP 13 809WP 032 PCEAC0043 IN CRUISE, NR1 OIL PRESSURE 50 TO 55 PSI. MX NR1 OIL PRESSURE TRANSMITTER CONNECTOR P1 WIRE 2D20 REPAIRED IAW WD 79-32- 00 SHEET 1 OF 2. PERFORMED OPS CHECK GOOD. C/W NR1 AND NR2 ENGINE RUN-UP IAW MM 71-00-00 PG. 529-531. NO DEFECTS NOTED. 2 H 7 2 4T 4 T RT A13NM E20NE 20090108 NM 2009 1 8 UALA2009010200004 1 20081231 A 3030 893301 SENSOR AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE PITOT HEAT SHORTED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 851UA 1664 ECAM ANTI-ICE CAPT PITOT. FLIGHT DIVERTED. FOUND SENSOR 21GA SHORTED. REPLACED SENSOR AND ACCOMPLISHED GEAR SWING AN D CFDS TEST AND SYS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20090109 NM 2009 1 9 HNAA2009010300369 1 20081230 A 3350 1317 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA L ABORTED APPROACH L NO TEST IN INSP/MAINT 1 EA 07 911HA 58778 58778 034 AFT OVER HEAD EMERGENCY LIGHT INOPERATIVE. REMOVED CEILING PANEL BEFORE REMOVING BULB, REINSTALL NEW BULB AND CEILING P ANEL. OPS CHECK GOOD 2 H 7 2 4T RT A13NM 20090109 EU 2009 1 9 NWAA085643264 1 20081217 A 3230 SAFETY VALVE AIRBUS 320 A320212 3930322 EU LANDING GEAR LEAKING A NWAA O OTHER K FLUID LOSS CR CRUISE 1 GL 01 364NW 0962 IN CRUISE ECAM MSG HYD G RSVR LO LVL. COM FOLLOWED WITH GRAVITY GEAR EXTENSION PRIOR TO LANDING. UNEVENTFUL LANDING WI TH ACFT TOWED TO GATE. REPLACED LANDING GEAR SAFETY VALVE 49GA, CHECKS OK. 2 L 7 2 4F RT A28NM 20090109 NM 2009 1 9 R5KB15838 1 20081219 A 5260 WEB BOEING 727 727212 138407G NM STAIRS CRACKED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 VERTICAL WEB CRACK AT LIGHTNING HOLE. 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 R5KB15914 1 20081220 A 3270 BEAM BOEING 727 727212 138407G NM TAIL SKID CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 TRANSVERSE BEAM AT TAIL SKID CORRODED. 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 R5KB15678 1 20081218 A 5315 FLOORBEAM BOEING 727 727212 138407G NM FUSELAGE DAMAGED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 FLOORBEAM WEB DAMAGED BELOW UPPER CHORD, STA 460, RBL-25. 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 ASAA0944170 1 20081223 A 5311 654795978 FRAME BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON FRAME BS 794. REPLACED BS 794 IN AFT CARGO BAY. 2 L 7 2 4F RT A16WE 20090109 EA 2009 1 9 VNAA2009010700014 1 20081231 A 5610 601R3303317 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A VNAA A UNSCHED LANDING O OTHER UK UNKNOWN 1 GL 05 246PS 11229 7920 CREW REPORTED THE LT WINDSHIELD CRACKED. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX REMOVED AND REPLA CED THE WINDSHIELD IAW THE ACFT MM. ACFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 20090109 EA 2009 1 9 VNAA2009010700015 1 20081231 A 5610 NP13932112 WINDSHIELD CNDAIR CL600 CL6002C10 1390015 EA COCKPIT CRACKED A VNAA O OTHER O OTHER CR CRUISE 1 GL 05 708PS 11199 10160 CREW REPORTED RT WINDSHIELD SHATTERED WHILE AT CRUISE. CREW DECENDED TO 10,000 FEET AND THEN LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE WINDSHIELD IAW THE ACFT MM. ACFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 20090109 NM 2009 1 9 UALA2009010200008 1 20081231 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY LIGHT INOP AT 36 ABC. NO LIGHT BULBS IN SYS. REPLACED EEL AT 36ABC 2 L 7 4 4F 4 F RT A20WE E24NE 20090109 NM 2009 1 9 UALA2009010200009 1 20081231 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 173UA 24380 EMERGENCY LIGHT INOP AT 20 ABC. REPLACED EEL LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 20090114 NM 2009 1 14 HNAA2009010900386 1 20080618 A 5523 85520215102 SPAR DHAV DHC8 DHC8102 2809003 NM LT ELEVATOR TAB CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 980HA 32623 32623 376 DURING C-CHECK INSP, THE REAR SPAR OF THE LT ELEVATOR SPRING TAB WAS FOUND TO BE CRACKED AT THE OTBD EDGE. THE SPAR WAS REPAIRED IAW RD8-55-068. 2 H 7 2 4T RT A13NM 20090114 NM 2009 1 14 AALA200802574A 1 20081123 A 3397 WIRE BOEING 777 777223 1385213 NM EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 753AN 30261 DFW EMERGENCY LIGHT AT SEAT 12D INOPERATIVE. SECURED LOOSE CONNECTION AT SEAT 12D. SYSTEM GROUND CHECKED NORMAL OPERAT ION. (CLOSED) 2 L 7 2 4F RT T00001SE 20090114 EU 2009 1 14 FDEA200812235264 1 20081223 A 5320 A5327267100000 PANEL AIRBUS 310 A310203 3930313 EU CARGO BAY DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 38333 248 FWD CARGO PIT; BETWEEN FRAMES 23 & 24 AT STRINGER 44L; THE TRANS PANEL HAS A DENT ON THE TOP & BARE METAL ON THE LOWE R SURFACE. REPAIRED DENT IAW SRM 51-73-10; PG 202. ALODINED BARE METAL IAW SRM 51-21-10. PRIMED & APPLIED TOPCOAT IAW SRM 51-23-10. 2 L 7 2 4F RT A35EU 20090114 NM 2009 1 14 ASAA0944185 1 20081205 A 5347 655384414 CARGO TRACK BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 AFT CARGO COMPARTMENT CORROSION FOUND ON STRUCTURE BENEATH FLOOR PANEL AT CARGO DOOR LOWER THRESHOLD SILL AREA. R&R CAR GO TIEDOWN TRACK BS 777 877 RBL 13 SRM 53 00 53. 2 L 7 2 4F RT A16WE 20090114 WP 2009 1 14 IXXA08SMN210S 1 20081028 A 5320 3754220U501 FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT SPLICE FITTING CRACKED AT STATION 600.000-620.000 LON GERON 31 LEFT. REMOVED CRACKED SPLICE FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW SPLICE FITTING IAW DC 8 SRM 51-1-20D, SRM 51-3-1, AND DC8 SRM 51-1-8B. 2 L 7 4 4F 4A25 20090115 EA 2009 1 15 ASOA200900045 1 20081229 A 5755 PANEL CNDAIR CL600 CL6002C10 1390015 EA SPOILER CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 LT WING MULTI-FUNCTION SPOILER CLOSEOUT PANEL CRACKED AT INBD AFT CORNER. OPEN 2 L 7 2 4F RT A21EA 20090116 NE 2009 1 16 FDEA200811084795 2 20081108 A 7200 ENGINE DOUG MD10 MD1030F 3024020 NM GE CF6 CF650C2 30018 NE OVERTEMP A FDEA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 CE 21 304FE 46992 517630 AFTER 2 HOURS INTO FLT GOT EGT FLUCTUATING UP TO 1065 DEGREES CELSIUS TO VALUES AT OR BELOW NORMAL. RETARDED THROTTLE T O IDLE AND RAN CKLIST. EGT STILL FLUCTUATING WILDLY SO PERFORMED ENG SHUTDOWN. NO OTHER INDICATIONS OF SEVERE DAMAGE, BUT WITH EGT STILL CYCLING ABOVE RED LINE TREATED IT AS SEVERE DAMAGE AND RAN THAT CKLIST AS WELL, TO INCLUDE FIRING FI RE BOTTLE. AFTER 1 MIN, STILL SHOWED HI EGT, SO FIRED 2ND BOTTLE AND DIVERTED TO KFLL. SHORTLY AFTER FIRING 2ND BOTTLE EGT SETTLED DOWN TO 25C. INSPECTED INLET AND EXHAUST NO DAMAGE NOTICED. SPUN FAN AND EXHAUST TURNED FREE. REF JRH FO R EGT EXCEEDENCE REQUIREMENTS, AS DIRECTED, BOROSCOPE HPT1 AND HPT 2. NO DAMAGE NOTED. AS PRECAUTION BOROSCOPE HPC 1, 2 L 7 3 4F 4 F RT A22WE E23EA 20090116 NM 2009 1 16 USAA2009011390068 1 20081226 A 5347 65468156 SEAT TRACK BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - NR 6142261 - GALVANIC CORROSION ON SEAT TRACK AT BS919, RBL45. REPAIRED SEAT TRACK AT BS919, RBL45 IAW B737 SRM 53-00-52. 2 L 7 2 4F RT A16WE 20090120 SO 2009 1 20 FFKA20081217001 2 20081217 A 7314 LW15473 PUMP PIPER PA32 PA32R300 7103213 SO LYC 0540 IO540K1G5D 41532 SO FUEL SYS INOPERATIVE E FFKA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 05 8954C 1923 89 32R7680146 L419348A ABOUT 40 OR SO MILES FROM AIRPORT, THE ENGINE DRIVEN FUEL PUMP DIED. WHEN THE FUEL PRESSURE STARTED DROPPING THE PILOT WENT THROUGH THE "HAIL MARY" MANEUVER (SWITCH TANKS, MIXTURE RICH, CHECK THE MAGNETOS, ELECTRICAL FUEL PUMP ON). AS SOO N AS HE HIT THE ELECTRICAL FUEL PUMP THE ENGINE PICKED RIGHT UP. PILOT MONITORED THE FUEL PRESSURE, BUT IT WAS SITTING RIGHT AT ZERO. PILOT TURNED THE ELECTRICAL FUEL PUMP OFF AFTER THINGS SETTLED DOWN JUST TO MAKE SURE THIS WAS THE PROBL EM, BUT THE FUEL FLOW GAUGE ALSO STARTED TO DROP AND THE ENGINE BEGAN TO LOOSE POWER, SO HE TURNED IT BACK ON. MX REPLA CED FUEL PUMP AND NO FURTHER PROBLEMS WERE NOTED. 1 L 7 1 3O 3 O A3SO 1E4 20090113 NM 2009 1 13 USAA2009010590030 1 20081222 A 5320 6546812Y169 FLOOR SUPPORT BOEING 737 7374B7 138449C NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - NR 03C10853029/007 - LEVEL 2 EXFOLIATION CORROSION ON FLOOR SUPPORT ANGLE BETWEEN BS967 TO BS9 87, RBL18. REPLACED FLOOR SUPPORT ANGLE BETWEEN BS967 TO BS987, RBL18 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20090114 NM 2009 1 14 HNAA2009010900387 1 20080618 A 5542 85545031101 SKIN PANEL DHAV DHAV DHC8 DHC8102 2809003 NM RUDDER DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 980HA 32623 32623 CAP0070 376 DURING C-CHECK INSP, THE TRAIL RUDDER SKIN WAS FOUND TO BE DAMAGED ON THE LT SIDE NEAR THE LOWER HINGE POINT. THE DAMAG E WAS REPAIRED IAW SRM PROCEDURES AND EO8-55-08-3203. 2 H 7 2 4T RT A13NM 20090114 NM 2009 1 14 DHLA2009770AT501 1 20081211 A 5311 FAILSAFE BOEING 727 7272B7 138407L NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 770AT 21953 UPPER FUSELAGE CARGO CABIN FRAME FAIL SAFE CHORD WITH CORROSION AT BS 1166 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE F RAME FAIL SAFE CHORD SECTION AT BS 1166 BETWEEN S-16R AND S-18R DUE TO CORROSION IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20090114 WP 2009 1 14 AALA200802598A 1 20081127 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 593AA 53256 SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 3EF TO 20EF EXTINGUISHED AFTER 10 TO 25 SECONDS. CHARGED EMERGENCY LIGHTS FROM SEAT ROWS 3EF TO 20EF. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20090114 NM 2009 1 14 AALA200802599A 1 20081128 A 3350 P4010049 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 335AA 22333 EMERGENCY LIGHTS FROM LEFT HAND SEAT ROWS 20AB TO AFT CABIN INOPERTIVE. REPLACED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20090114 NM 2009 1 14 AALA200802600A 1 20081128 A 3350 P4010049 BATTERY PACK BOEING 767 767223 1385123 NM EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 335AA 22333 EMERGENCY LIGHTS FROM LEFT HAND SEAT ROWS 20AB TO AFT CABIN INOPERTIVE. REPLACED BATTERY PACK FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A1NM 20090112 SO 2009 1 12 SIMA200900901 1 20080126 A 3230 429513 ECU EMB 135 EMB135KL 3260302 SO LANDING GEAR MALFUNCTIONED A SIMA O OTHER O OTHER CL CLIMB 1 SW 21 833AE 18056 639 145629 ON FLIGHT 4533 CREW REPORTED NLG DOORS DID NOT RETRACT/CLOSE UPON GEAR RETRACTION. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED LANDING GEAR ELECTRONIC CONTROL UNIT IAW AMM 32-32-01. OPS CHECK GOOD, ACFT PASSED FCF. ACFT RETURNED TO S ERVICE. 2 L 7 2 4F RT T00011AT 20090112 NM 2009 1 12 USAA2009010590024 1 20081229 A 5311 65C22910 FRAME BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT Q5 MAJOR REPAIR NR 03C20853011/002 & 03C20853011/003 CRACK ON FUSELAGE FRAME AT BS500D BELOW S20L & S20R. REPAIRED FUSELAGE FRAME AT BS500D BELOW S20L & S20R IAW B737 SRM 53-00-07, US AIRWAYS EA NR 100790, & EA NR 100792. 2 L 7 2 4F RT A16WE 20090112 NM 2009 1 12 USAA2009010590025 1 20081230 A 5311 65C32351 FRAME BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT Q5 MAJOR REPAIR NR 03C20853011/009 & 03C20853011/010 CRACK ON FUSELAGE FRAME AT BS500E BETWEEN S20R & S21R, ALSO BET WEEN S20L & S21L. REPAIRED FUSELAGE FRAME AT BS500E BETWEEN S20R & S21R, ALSO BETWEEN S20L & S21L IAW B737 SRM 53-00-07 & US AIRWAY EA NR 100790. 2 L 7 2 4F RT A16WE 20090112 NM 2009 1 12 USAA2009010690039 1 20081212 A 5743 D57259162001 ANCHOR FITTING AIRBUS A319 A319132 3930340 NM RT MLG CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805AW 1049 SAL C7 MAJOR REPAIR NR 6142519 CORROSION ON LOWER SURFACE OF RT MLG ANCHORAGE FITTING. REPAIRED RT MLG ANCHORAGE FITTIN G IAW US AIRWAYS EA NR 132186. 2 L 7 2 4F RT A28NM 20090112 NM 2009 1 12 UALA2008111302571 1 20080501 A 2830 S343T00339 ACTUATOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FUEL SYSTEM FAULTY A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 793UA 26946 RT TANK QTY INCREASES 300 LBS EVERY 10 MINUTES WITH CENTER TANK PUMPS ON. OCCURS IN NORMAL CONFIGURATION, JUST CENTER TA NK RT AND LT PUMPS ON. REPLACED FWD RT MAIN DISCHARGE CHECK VALVE. PROBLEM REOCCURRED. RPL'D L-H JETTISON ISO VALVE A CTUATOR. OP'S CHK OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20090112 NM 2009 1 12 UALA2008111304281 1 20080813 A 2820 568131509000 CHECK VALVE BOEING 777 777222 1385219 NM PWA 4090 PW4090 52119 NE FUEL SYSTEM FAULTY A UALA O OTHER K FLUID LOSS CR CRUISE 1 WP 29 209UA 30215 FUEL APPEARS TO XFR TO THE RT TANK AT 600-HR OR MORE. SUPPLEMENTAL DATA UPDATE REMOVED AND REPLACED LT AND RT WING BOOS T PUMP DISCHARGE CHECK VALVES. OPS CHECK AND LEAK CHECK GOOD. LT FWD SERIAL NR RMV 172231-15 INST 1072645-42, AFT RMV 172231-18 INST 1066737-32, RT FWD RMV NR 133888-2 INST 1072645-47, RT AFT RMV 172231-18 INST 1066737-28. 2 L 7 2 4F 4 F RT T0001SE E46NE 20090109 NM 2009 1 9 R5KB15807 1 20081219 A 5320 WEB BOEING 727 727212 138407G NM FUSELAGE CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 SUBFLOOR WEB CORRODED AFT LAV. 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 R5KB15784 1 20081218 A 5347 SEAT TRACK BOEING 727 727212 138407G NM FUSELAGE CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 SEAT TRACK CROWN CORRODED. 2 L 7 3 4F A3WE 20090109 NM 2009 1 9 ASAA0944166 1 20081227 A 5344 65C346701 HINGE FITTING BOEING 737 737490 1384715 NM CFMINT CFM56 CFM563C1 13802 EU L1 DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 708AS 28895 L1 DOOR UPPER HINGE CUTOUT FASTENER HOLE HAS CRACK INDICATION IN THE FITTING AT BS 304 WL 259. R&R L1 DOOR UPPER HINGE FITTING AT BS 304 WL 259. 2 L 7 2 4F 4 F RT A16WE E21EU 20090109 NM 2009 1 9 ASAA0944160 1 20081215 A 5542 65C2584151 SKIN BOEING 737 7374Q8 138447Q NM RUDDER PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 RUDDER PUNCTURED RT SIDE APPROX. 16" FROM 88" FROM LOWER EDGE. PREPPED PUNCTURED AREA AND REPAIRED AREA IAW B737 400 SR M 51 70 03 REP 2. 2 L 7 2 4F RT A16WE 20090112 NM 2009 1 12 USAA2009010590031 1 20081220 A 5320 6549815 ANGLE BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - NR 03C20353004/002 - CRACK ON ANGLE AT FORWARD GALLEY BULKHEAD AT BS277, S17R. REPAIRED ANGLE AT FORWARD GALLEY BULKHEAD AT BS277, S17R IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20090112 NM 2009 1 12 USAA2009010590032 1 20081219 A 5340 654688210 STRINGER CLIP BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - NR 03C10753006/001 - STRINGER TIE CLIP CRACKED AT BS344, S11R. REPLACED STRINGER TIE CLIP AT BS344, S11R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20090112 NM 2009 1 12 USAA2009010590033 1 20081219 A 5320 69374024 ANGLE BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - NR 03C10753006/002 - ANGLE CRACKED FORWARD OF R1 DOOR AT BS294.5, S17L. REPLACED ANGLE FORWAR D OF R1 DOOR AT BS294.5, S17L IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20090112 NM 2009 1 12 USAA2009010590034 1 20081219 A 5311 6545805 FRAME BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - NR 03C10753006/004 - FUSELAGE FRAME CRACKED AT BS277, S16L. REPAIRED FUSELAGE FRAME AT BS277, S16L IAW B737 SRM 53-00-07. 2 L 7 2 4F RT A16WE 20090112 NM 2009 1 12 USAA2009010590035 1 20081218 A 5310 6545808 DOOR FRAME BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - NR 03C10753006/006 - CRACK IN R1 DOOR FRAME AT BS294.5, BETWEEN S6R & S7R. REPAIRED R1 DOOR F RAME AT BS294.5, BETWEEN S6R & S7R IAW B737 SRM 51-70-11. 2 L 7 2 4F RT A16WE 20090113 EU 2009 1 13 USAA2009010890047 1 20081221 A 5320 D53112610000 BRACKET AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656AW 1079 SAL - C7 - MAJOR REPAIR - NR 6131306 - CORROSION ON PLATE ASSEMBLY BRACKET OF FLOOR STRUCTURE AT FR16, -Y1387. REPLACED PLATE ASSEMBLY BRACKET OF FLOOR STRUCTURE AT FR16, -Y1387 IAW A320 SRM 51-42-11 & 51-21-11. 2 L 7 2 4F RT A28NM 20090114 NM 2009 1 14 AALA200802609A 1 20081129 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 EMERGENCY LIGHT AT SEAT 20C INOPERATIVE. REPLACED LAMP AT SEAT 20C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20090114 WP 2009 1 14 IXXA08SMN220S 1 20081028 A 5320 37538771 FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT SPLICE FITTING CRACKED AT STATION 902.000 LONGERON 1. R EMOVED CRACKED SPLICE FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-20D AN D SRM 51-3-1 TABLE II PAGE 2A, DC8 SRM 51-1-21, AND DC8 SRM 51-1-8B. 2 L 7 4 4F 4A25 20090114 WP 2009 1 14 IXXA08SMN207S 1 20081028 A 5542 SKIN DOUG DC8 DC862F 3021972 WP RUDDER CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND EMPENNAGE RUDDER RIGHT SKIN CRACKED AT STATION ZR 253.00. REMOVED DAMAGED SKIN . FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. PERFORMED BALANCE. FOUND WITHIN LIMITS WITH A MOMENT: 2532.0 IN-POUND. INSTALLED REPAIR PARTS IAW DC8 SRM 55-6 -1 FIGURE 1 ITEM "A", DC8 SRM 55-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-9 TR 51-142, SRM 51-1-9A TR 51-141, DC8 SRM 51-1- 8B, DC8 SRM 51-1-11, DC8 SRM 51-4-6 PAGES 1-5, 2 L 7 4 4F 4A25 20090114 WP 2009 1 14 IXXA08SMN212S 1 20081028 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME SHOWS MISDRILLED HOLE AT STATION 1400 .000 LONGERON 16 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABR ICATED INTERNAL DOUBLER ANGLE, AND FILLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FAA FORM 81103 NUMBER 08549 DATED 11/24/08, SEMAN DRAWING ED-4877 DATED 11/10/08, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-1 PAGE 1, 13, AND 17, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D, AND SRM 51-3-1. 2 L 7 4 4F 4A25 20090114 NM 2009 1 14 FDEA200812245269 1 20081224 A 5320 6517510117 WEB BOEING 727 727233 138408A NM BS 1218-1230 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 AFT AIRSTAIRS, LT TORQUE BOX I/B VERTICAL WEB IS CRACKED AT BS.1225, WB 190 APROX REMOVED AFT AIRSTAIRS FLOOR PANEL AND ANGLE FOR ACCESS IAW SRM 51-30-2. CUTOUT DAMAGED AREA IAW SRM 51-40-2 FIG 1. FABRICATED REPAIR PART AND FILLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PART AND FILLER IAW SRM 51-30-2. INSTALLED AFT AIRSTAIRS AND ANGLE IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 20090114 NM 2009 1 14 FDEA200812245270 1 20081224 A 5320 6517510120 WEB BOEING 727 727233 138408A NM BS 1203-1223 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 AFT AIRSTAIRS, RH LOWER TORQUE BOX I/B VERTICAL WEB IS CRACKED AT UPPER ROW OF RIVETS BETWEEN STA. 1203 AND STA 1223 R EMOVED PANEL AT AFT AIRSTAIRS RH VERTICAL WEB FOR ACCESS IAW SRM 51-30-2 CUTOUT DAMAGED AREA IAW SRM 51-40-2 FIG 1. FABR ICATED REPAIR PART AND FILLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. TERATED AND PRIMED PARTS IAW B727-200 51-10-2. INSTALLED REPAIR PART AND FILLER IAW SRM 51-30-2 AT AFT AIRSTAIRS RH LWR TORQUE I/B VERTICAL WEB AND ACCESS PANEL IAW S RM 51-30-2. 2 L 7 3 4F RT A3WE 20090114 NM 2009 1 14 FDEA200812245273 1 20081224 A 5320 6517510119 WEB BOEING 727 727233 138408A NM BS 1203-1223 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 AFT AIRSTAIRS LT LOWER TORQUE BOX I/B VERTICAL WEB IS CRACKED AT UPPER ROW OF RIVETS BETWEEN STA 1203 AND STA. 1223 RE MOVED PANEL AT AFT AIRSTAIRS LT VERTICAL WEB FOR ACCESS IAW SRM 51-30- 2. CUTOUT DAMAGED AREA IAW SRM 51-40-2 FIG 1. FA BRICATED REPAIR PART AND FILLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INS TALLED REPAIR PART AND FILLER AND ACCESS PANEL IAW SRM 51-30-2 AT AFT AIRSTAIRS LT TORQUE I/B VERTICAL WEB AREA. 2 L 7 3 4F RT A3WE 20090114 NM 2009 1 14 R5KB081218001 1 20081218 A 5315 SEAT TRACK BOEING 727 727212 138407G NM BS 1130 CORRODED I R5KB K NONE O OTHER IN INSP/MAINT 1 SO 33 727NK 21945 SEAT TRACK CORRODED BS 1130. 2 L 7 3 4F A3WE 20090115 CE 2009 1 15 Z5FA122408N541CS1 1 20081224 A 3233 99125373 ACTUATOR CESSNA 560 560XL 2076702 CE ZONE 500 DEFECTIVE E Z5FA O OTHER J WARNING INDICATION DE DESCENT 1 EA 63 541CS 4016 5605521 UPON DECENT, CREW EXTENDED LANDING GEAR BUT DIDN'T GET GEAR LOCK LIGHT FOR THE LEFT MAIN. CREW DISCONTINUED THEIR APPROA CH AND PICKED UP A NEW IFR CLEARANCE FROM ATC AND WAS PUT INTO HOLD TO DO THEIR EMERGENCY CHECK LIST. AFTER BLOWING THE GEAR BOTTLE, THERE WAS STILL NO GREEN LIGHT FOR THE LEFT MAIN. AIRCRAFT DECLARED AN EMERGENCYAND DIVERTED TO MTJ, LANDI NG WAS UNEVENTFUL. AIRCRAFT WAS FERRIED TO GJT WITH GEAR DOWN AND LOCKED TO FACILITATE MAINTENANCE. MX REPLACED LT MAIN GEAR ACTUATOR IAW MM 32-30-04 AND PERFORMED SATISFACTORY GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A22CE 20090115 NM 2009 1 15 FDEA200812305318 1 20081230 A 5313 STRINGER BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 257FE 20939 FWD CARGO COMPT STRINGER 28L IS CORRODED FROM BS 600-620. CUTOUT DAMAGED STRINGER. FABRICATED STRINGER REPAIR FILLER, R EPAIR SPLICE. CUTOUT DAMAGED SKIN & FABRICATED REPAIR DOUBLER. INSTALLED REPAIR PARTS IAW SRM 53-10-3, 53-10-2, 53-30-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 20090115 EA 2009 1 15 ASOA200900044 1 20081229 A 5755 PANEL CNDAIR CL600 CL6002C10 1390015 EA SPOILER CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 659CA 10153 RT MULTI-FUNCTION SPOILER CLOSEOUT PANEL CRACKED AT INBD AFT CORNER. OPEN 2 L 7 2 4F RT A21EA 20090116 EU 2009 1 16 NWAA085763360 1 20081226 A 2120 FILTER ELEMENT AIRBUS A330 A330223 3930374 EU CABIN DIRTY A NWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 860NW 00778 SMOKE IN THE CABIN AFTER TAKE OFF, MOST CONCENTRATED IN AREA OF ROW 5, FOLLOWED COM AND ISOLATED THE SOURCE TO BE PACK 2 AIR SUPPLY. DECLARED AN EMERGENCY AND RETURNED TO PEK AND LANDING WAS UNEVENTFUL. INSPECTED CABIN OVERHEAD CEILING AR EA, LIGHTING BALLAST, IN FLIGHT ENTERTAINMENT SYSTEM, PACK VALVES, APU AND ENGINE FOR OIL LEAK AND THE HP VALVE AND HYDR AULIC LINE THAT HAD JUST BEEN REPLACED, NO DISCREPANCIES FOUND. THE 4 FORWARD RECIRCULATION FILTERS WERE REPLACED AND R AN THE ENGINES AND COULD NOT DUPLICATE DISCREPANCY. SUBSEQUENT MX REPLACED THE OZONE CONVERTER. 2 L 7 2 4F RT A46NM 20090113 NM 2009 1 13 USAA2009010590029 1 20081223 A 5320 6552878U97 ANGLE BOEING 737 7374B7 138449C NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - NR 03C10853029/004 - LEVEL 2 EXFOLIATION CORROSION ON Z ANGLE UPPER FLANGE AT L2 DOOR FROM BS9 67 TO BS987, LBL50. REPLACED Z ANGLE UPPER FLANGE AT L2 DOOR FROM BS967 TO BS987, LBL50 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20090113 EU 2009 1 13 USAA2009010790046 1 20081222 A 5321 D5367180500400 FLOOR PANEL AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 656AW 1079 SAL - C7 - MAJOR REPAIR - NR 6129499 - CORROSION ON FLOORBOARD PANEL NR 261FF, (L2 DOOR ENTRY). REPLACED FLOORBOARD PAN EL NR 261FF, (L2 DOOR ENTRY). 2 L 7 2 4F RT A28NM 20090113 EA 2009 1 13 SWIA200820777 1 20081231 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 430SW 7523 FLT 4810 - CABIN CEILING EMERGENCY LIGHT NR 4 INOP. RELAMPED 2 L 7 2 4F RT A21EA 20090114 NM 2009 1 14 AALA200820097 1 20081205 A 5543 178W00615 TAB BOEING 777 777223 1385213 NM RUDDER DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 761AJ 27651 31478 LT SIDE OF RUDDER TAB HAS DAMAGE 14 INCHES FROM LEADING EDGE AND 5 INCHES ABOVE BOTTOM OF TAB, DIAMETER .5 INCHES; REPAI R NR AALA20820097 ENTERED IN ERROR SHOULD READ, AALA200820097. 2 L 7 2 4F RT T00001SE 20090114 NM 2009 1 14 DHLA2009770AT507 1 20081212 A 5313 STRINGER BOEING 727 7272B7 138407L NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 770AT 21953 LOWER FUSELAGE FWD CARGO COMPARTMENT BS 727E STRINGER END S-27R CORRODED. REPAIRED FUSELAGE S-27R SECTION FROM BS 727E TO BS 740 IAW B727 SRM 53-10-3 FIG 1 DETAIL 1. 2 L 7 3 4F A3WE 20090114 WP 2009 1 14 AALA200802580A 1 20081124 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 434AA 49452 EMERGENCY LIGHTS AT MID CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 20 FOR EMERGENCY LIGHTS AT MID CABIN. SYST EM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A6WE 20090114 WP 2009 1 14 AALA200802581A 1 20081124 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 434AA 49452 EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR EXTERNAL EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A6WE 20090114 WP 2009 1 14 AALA200802584A 1 20081124 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 967TW 53617 EMERGENCY LIGHT AT SEAT 25D INOPERATIVE. SECURED CONNECTOR AT SEAT 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20090114 NM 2009 1 14 AALA200802585A 1 20081124 A 3350 0201922001 LIGHT BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 385AM 27059 EMERGENCY LIGHT AT SEAT 27H DAMAGED. REPLACED LIGHT ASSEMBLY AT SEAT 27H. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLO SED) 2 L 7 2 4F RT A1NM 20090114 WP 2009 1 14 IXXA08SMN206S 1 20081025 A 5320 4641324U501 FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND AFT ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 1530.000 LONGERON 36. REM OVED DAMAGED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, DC8 SRM 51-1-8B, S RM 51-1-20D, AND SRM 51-3-1. 2 L 7 4 4F 4A25 20090115 NM 2009 1 15 FDEA200812265293 1 20081226 A 5230 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 615FE 48767 CRACK INDICATION FOUND DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON 0.460 INCH HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES A, B, C AND D. AT MAIN CARGO DOOR LOWER JAMB, CRACKED NR 2 SUPPORT FITTIN G REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20090115 WP 2009 1 15 IXXA080039O 1 20081229 A 2121 X702256D FAN DOUG DC8 DC862F 3021972 WP CABIN BURNED OUT A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 11 71CX 72936 89 45961 ON TOP OF DESCENT FLIGHT ATTENDANT'S DETECTED SMOKE IN CABIN. AFTER TURNING OFF THE RT RECIRCULATION FAN THE ODOR DISSI PATED. THE CREW LANDED IN PHIK WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND LT RECIRCULATION FAN EMMITTING BURNING ODOR. MAINTENANCE REPLACED LT RECIRCULATION FAN. OPERATIONAL CHECK GOOD IAW MM 21-21-1. ACFT RETURNED TO SERVICE . 2 L 7 4 4F 4A25 20090114 WP 2009 1 14 IXXA08SMN213S 1 20081028 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 1320.0 00 LONGERON 16 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICA TED ANGLE DOUBLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS I AW FAA FORM 8110-3 NUMBER 08549, SEMAN DRAWING ED-4877, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-1 PAGES 1, 13, AND 1 7, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D, AND SRM 51-3-1. 2 L 7 4 4F 4A25 20090114 NM 2009 1 14 DHLA2008743521 1 20081110 A 5311 FRAME BOEING 727 727225 1384077 NM BS 360 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 "D" CHECK, UPPER FUSELAGE PAX CABIN AT BS 680 BETWEEN STR.16R & 17R FRAME WITH HOLE. REPAIRED FUSELAGE FRAME SECTION AT BS 680 BETWEEN S15 & 17R DUE TO DOUBLE HOLE IAW SRM 51-40-3 FIG.1. 2 L 7 3 4F A3WE 20090115 SO 2009 1 15 SWIA200820796 1 20081230 A 3350 FUSE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHTS BLOWN A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 226SW 120296 FLT 5433 - FLT 5433 - FORWARD MOST OVERHEAD EMERGENCY LIGHT INOP. REPLACED FUSE. 2 L 7 2 4T RT A31SO 20090116 NM 2009 1 16 USAA2009011390067 1 20081224 A 5320 65479573 SILL BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - NR 6142731 - CORROSION ON LOWER SILL WEB BETWEEN BS807 TO BS827, LBL25. REPAIRED LOWER SILL WEB BETWEEN BS807 TO BS827, LBL25 IAW B737 SRM 51-70-13. 2 L 7 2 4F RT A16WE 20090120 EU 2009 1 20 UPS09154295 1 20081230 A 5753 DOUBLER AIRBUS A300 A300F4622R 3930360 EU TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 141UP 0824 INSPECTION TYPE:1/3C SURVEY SEQ NR 141-W3-001 LT CTR FLAP UPPER SKIN REPAIR EFN NR 141200610 07 HAS GOUGE DAMAGE REFEREN CE APPX. C PARAGRAPH C ITEM C. REMOVED EXSITING REPAIR AND FABBED AND INSTALLED NEW REPAIR IAW SRM. REF. 57-50-00 FIG 2 05 ,51-21-10,AND 51-23-10. 2 L 7 2 4F RT A35EU 20090120 WP 2009 1 20 UPS09854282 1 20081226 A 5544 56550776 DOUBLER DOUG DC8 DC871F 302199D WP RUDDER MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE: SV RUDDER RT SIDE APPROX STA ZR 259.9 HAS A DOUBLER THAT IS 2.5 X 1.7 THA T DOES NOT CORRELATE TO THE S RM SURVEY SEQUENCE NR715-54-06. REPAIRED IAW UPS EO DC8-5570-31778-A. 2 L 7 4 4F RT 4A25 20090120 NM 2009 1 20 DHLA2009770AT518 1 20081208 A 5330 SKIN PANEL BOEING 727 7272B7 138407L NM ZONE 100 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 770AT 21953 LWR FUSELAGE AT BS 509.5 BTWN S-20R AND S-21R WITH DENTS. REPAIRED FUSELAGE SKIN FROM BS 501 TO BS 512 BTWN S-19R AND S -21R IAW SRM 53-30-3 FIG 2. 2 L 7 3 4F A3WE 20090120 2009 1 20 CALA2009011300030 4 20081231 A 2565 65C1990115 CABLE BOEING 737 7373T0 1384582 NM R2 DOOR SLIDE FRAYED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 63305 23356 R-2 DOOR EMERGENCY ESCAPE SLIDE CABLE HAS BROKEN STRANDS. REMOVED AND REPLACED R2 DOOR EMERGENCY ESCAPE SLIDE CABLE IAW AMM 25-61-35. 2 L 7 2 4F RT A16WE 20090120 EU 2009 1 20 F3LA2009010800004 1 20080702 A 5755 D57745013016 WEB AIRBUS A318 A318111 3940019 EU ZONE 500 GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 805FR 40 1660 DURING C-3 C-CHECK INSP, NOTED THAT THE LT NR 4 SPOILER ANTI-ROTATION LUG HAS A GOUGE. MX REPAIRED DAMAGED AREA IAW EA A 8-57R-30431. 2 L 7 2 4F RT 20090120 NM 2009 1 20 DHLA2009743530 1 20081202 A 5320 STIFFENER BOEING 727 727225 1384077 NM ZONE 100 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 REF NR 1-267: VERTICAL STIFFENER ON BS 1183 BULKHEAD, AT RBL 8, CRACKED. ACCOMPLISHED REPAIR TO STIFFENER IAW SB 727-5 3-0175 R3, SECT III, PART III, FIG 3, DATED 01/25/96. 2 L 7 3 4F A3WE 20090120 NM 2009 1 20 DHLA2009770AT517 1 20081219 A 5320 SUPPORT CHANNEL BOEING 727 7272B7 138407L NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 770AT 21953 REF N/R 1-306 LOWER FUSELAGE INTERIOR FWD NOSE COMPARTMENT, LOWER CHORD AND SUPPORT CHANNEL WITH CORROSION AT BS 227.8 L BL2. REPAIRED FUSELAGE FWD NOSE COMPT LOWER CHORD SECTION AT BS 227.8 BTWN LBL 5.5 AND RBL 6 IAW SRM 51-40-4 FIG 1. 2 L 7 3 4F A3WE 20090120 NM 2009 1 20 UPS09554330 1 20081230 A 5340 NUT PLATE BOEING 757 75724APF 1384969 NM ZONE 166 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 461UP 28265 INSPECTION TYPE: C2 CORROSION, NUTPLATE RETAINER ON THE BOTTOM OF THE FLOOR WEB BS 1715 RBL 4.5 WL 208, REMOVED, FABRICA TED AND INSTALLED PLATE IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 20090120 WP 2009 1 20 UPS09854297 1 20081215 A 5340 4641324U501 FITTING DOUG DC8 DC873F 302199F WP BS 1690 L26L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE: SP WHILE WORKING REPAIR SEQ: NR 803-F1-126 FOUND CRACK FITTING AT STA. 1690- L26L. REMOVED AND INSTALL ED REPAIR FITTING IAW SRM 51-1-20D, 51-1-24,51-1-8. 2 L 7 4 4F RT 4A25 20090120 EA 2009 1 20 ASOA200900060 1 20081231 A 5320 POST CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 JOB 8733515 OPERATION 174 F.S. 409+128 VERTICAL POST HAS INDICATION NOTED APPROX .3" IN LENGTH AT RBL 18.0 WL 69.0 I/B AND O/B FLANGES 90% FULL SCREEN HEIGHT FAILED NDT INSP. 2 L 7 2 4F RT A21EA 20090120 WP 2009 1 20 AALA200910578 1 20081218 A 5755 CASTING DOUG DC9 DC982 3022082 WP RT WING SPOILER CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 465A 49595 GROUND SPOILER CASTING CRACKED ON OUTBOARD SIDE ABOVE GROUND SPOILER ACTUATOR FORWARD ATTACH BOLT. REPLACED CASTING. 2 L 7 2 4F A6WE 20090120 WP 2009 1 20 AALA200910559 1 20081215 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 290 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 90511 49805 CORROSION ON NUMBER 4 SEAT TRACK STATION 290. INSTALLED SEAT TRACK PLUG AT STATION 290. 2 L 7 2 4F A6WE 20090120 EU 2009 1 20 M7KA0908084266 1 20081117 A 5210 677130400 MOUNT FLANGE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE PILOT DOOR CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 847MH 1007 4266 23416 DURING ROUTINE INSPECTION THE MOST AFT OTBD CORNER OF THE MOUNTING FLANGE ASSEMBLY WHICH INCLUDES THE UPPER LOCKING PIN MECHANISM WAS CRACKED. A NEW ASSEMBLY WAS INSTALLED. 1 G 7 2 3U 3 U H9EU E00054EN 20090120 EU 2009 1 20 M7KA1031083949 1 20081117 A 5302 350A24422020 SPAR UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE HORIZ STAB CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 810MH 3949 23318 DURING ROUTINE 500 HOUR INSPECTION A CRACK WAS FOUND RADIATING FROM AN ATTACHMENT FITTING SCREW BORE TO THE EDGE OF THE SPAR. A NEW SPAR WAS MATCH DRILLED AND INSTALLED IAW EUROCOPTER REPAIR SCHEME. 1 G 7 2 3U 3 U H9EU E00054EN 20090120 EU 2009 1 20 FDEA200812020105 1 20081202 A 5420 A5461102420 FITTING AIRBUS 300 A300B4622R 3930312 EU PYLONS CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 723FD 543 PYLONS, PYLON STRUCTURE, NR 1 AND NR 2 PYLON AFT FITTING BORES AND BOLTS HOLES CORROSION REPAIR. 2 L 7 2 4F RT A35EU 20090121 NM 2009 1 21 DL764090009 1 20080102 A 8012 7997001 START VALVE BOEING 767 767432ER 1385134 NM GE CF6 CF680C2* GL NR 2 ENGINE INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 839MH 29712 704952 EICAS MSG RT STARTER CUTOUT ILLUMINATED IN FLIGHT. DUE TO QRH PROCEDURES AND ICING CONDITIONS IN ATL HAD TO DIVERT TO M IA FOR REPAIR. REMOVED AND REPLACED RT ENG START VALVE PER AMM. SPUN ENG AT GATE. START VALVE CKS GOOD. 2 L 7 2 4F 4 F RT A1NM E23EA 20090121 EU 2009 1 21 UPS09154314 1 20081228 A 7830 22141261147 THRUST REVERSER AIRBUS A300 A300F4622R 3930360 EU NR 2 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 141UP 0824 INSPECTION TYPE:1C NR 2 ENGINE OUTBOARD T/R DOOR UPPER EDGE JUST OUTBOARD OF FWD SPRING SEAL HAS A CRACK ON UPPER LONGER ON OUTER SKIN. REPAIRED NR 2 OUTBOARD T/R DOOR UPPER EDGE REF EA 300-7830-01-A1592 AND EO C-7830-31824-A. 2 L 7 2 4F RT A35EU 20090121 NM 2009 1 21 DHLA2009743535 1 20081229 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 FUSELAGE FRAME HAS DOUBLE DRILLED HOLES AT BS 560, STR 14R TO 17R. REMOVED FRAME SECTION. FABRICATED, AND INSTALLED FR AME SECTION PER SRM 53-10-2 FIG 2, 51-30-2, AND 51-10-1. 2 L 7 3 4F A3WE 20090121 NM 2009 1 21 DHLA2009743536 1 20081203 A 5753 FLAP TRACK BOEING 727 727225 1384077 NM ZONE 500 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 NR 3 FLAP TRACK, FWD AND AFT ATTACH SURFACES CORRODED. ACCOMPLISHED REPAIR TO FLAP TRACK SURFACES IAW OHM 57-40-01 PAGE 403-411. 2 L 7 3 4F A3WE 20090121 NM 2009 1 21 DHLA2009743537 1 20081125 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 100 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 FUSELAGE FRAME AT BS 1050 DENTED AT STR 26L. REPAIRED FRAME SECTION IAW SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20090121 NM 2009 1 21 UPS09654315 1 20081231 A 5753 SKIN PANEL BOEING 767 76734AF 1385212 NM TE FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE:C RT WING I/B MAIN FLAP T/E UPPER SURFACE DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PARA 5A (1) FIG 5. 2 L 7 2 4F RT A1NM 20090121 NM 2009 1 21 UPS09654318 1 20081230 A 5532 PANEL BOEING 767 76734AF 1385212 NM VERTICAL STAB DEBONDED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE:C EMP VERTICAL STABILIZER RT LOWER SURFACE PREVIOUS REPAIR AREA DEBOND. METAL HOT BOND REPAIR CARRIED O UT AS PER SRM 51-70-10 REPAIR 4. 2 L 7 2 4F RT A1NM 20090121 NM 2009 1 21 DHLA2009770AT519 1 20081205 A 5330 SKIN PANEL BOEING 727 7272B7 138407L NM ZONE 100 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 770AT 21953 LOWER FUSELAGE AT BS 1218.5 RBL 10.25 SKIN CRACKED. REPLACED SKIN SECTION FROM BS 1204.25 TO BS 1232.25 BTWN BL 0 AND R BL 21 IAW SRM 51-10-01 PAR 7A. 2 L 7 3 4F A3WE 20090121 NM 2009 1 21 DLM88090034 1 20081210 A 5523 TAB DOUG MD88 MD88 3023688 NM LT ELEVATOR DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 974DL 53242 DELAMINATED LT ELEVATOR ANTI-FLOAT TAB SKIN. LEFT ELEVATOR ANTI-FLOAT TAB WAS REPAIRED IAW SRM 55-04 FIG 3 AND OPN 1031 CARD 1343 AND 1351. 2 L 7 2 4F RT A6WE 20090121 NE 2009 1 21 DL738081814 2 20081229 A 7261 INDICATOR BOEING 737 737832 13844CF NM GE CFM56 CFM56* 13802 NE NR 1 OIL FILTER TRIPPED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 3769L 30822 888790 LEFT OIL FILTER BYPASS VALVE ILLUMINATED ON CLIMB. FOLLOW QRH AND LIGHT EXTINGUISHED AFTER THROTTLE RETARD. REMOVED AN D REPLACED SCV OIL FILTER. CHECKED FOR METAL PER M/M. FOUND LUBE FILTER DPI POPPED. REPLACED LUBE FILTER. CHECKED FOR DEBRIS. RAN ENG. MSG DID NOT APPEAR. DRAINED AND REPLENISHED OIL FROM NR 1 ENG PER M/M. INSPECTED CHIP DETECTORS. RAN ENG AT TAKEOFF PWR FOR 5 MIN, NO MSG. NO MSG DISPLAYED. ALL NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 20090121 NM 2009 1 21 DL757081815 1 20081230 A 5345 MOUNT BOEING 757 757232 1384965 NM RT MLG DOOR WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 DURING HMV, THE RT MLG DOOR CENTER MOUNT FITTING, HINGE SUPPORT AND BRACKET ATTACHMENT HOLES WERE FOUND TO BE WORN AND E LONGATED. THE HOLES WERE CLEANED UP TO ROUND DIAMETERS AND OVERSIZE BOLTS WERE INSTALLED IN SOME OF THE HOLES. 2 L 7 2 4F RT A2NM 20090121 NM 2009 1 21 DL738081816 1 20081230 A 2530 2281 CHILLER BOEING 737 737832 13844CF NM FWD GALLEY ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 3766 30820 FLT ATTENDANT REPORTED SMALL AMOUNT WHITE SMOKE AND ELEC ODOR COMING FROM BETWEEN F/C CHILLER AND BUN WARMER. C/B`S PUL LED AND NO MORE SMOKE. GALLEY POWER TURNED OFF. PULLED F/C CHILLER AND BUN WARMER AND INSPECTED AREA AND WIRING CKS OK . FOUND F/C CHILLER TO BE THE FAULT. CB FOR F/C CHILLER PULLED AND COLLARED AND NOW ALL CHECKS OK. FWD F/C CHILLER TO NEF 253.07. 2 L 7 2 4F RT A16WE 20090121 NM 2009 1 21 UPS09654325 1 20081231 A 5340 146T56515 ATTACH ANGLE BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE:C AFT OF BULK CARGO STA 1580 LBL 80 MAIN DECK SEAT TRACK ATTACH ANGLE CRACK. AFT OF BULK CARGO BS 1580 LBL 80 MAIN DECK SEAT TRACK ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20090121 NM 2009 1 21 UPS09654328 1 20081230 A 5330 SKIN BOEING 767 76734AF 1385212 NM FUSELAGE DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE:C SURVEY SEQUENCE 305-F1-05 FX BS 444-458.5 STR 23R-24R EXISTING REPAIR DOUBLER TOP SURFACE PREVIOUS BLE NDING FOUND WITH SLIGHTLY DENT. SURVEY SEQUENCE 305-F1-05 FUSELAGE BS 444-458.5 BETWEEN STR 23R-24R SKIN REPAIRED WITH ZERO TIMING AS PER SRM 53-00-01-2R14 FIG 201. UPS MPI P20223 ISSUED FOR SUBSEQUENT INSP AS PER SRM 53-00-01-2R14 FIG 20 1 SHT 9 TABLE V. 2 L 7 2 4F RT A1NM 20090120 WP 2009 1 20 AALA200910560 1 20081218 A 5342 ATTACH ANGLE DOUG DC9 DC982 3022082 WP VERTICAL STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 90511 49805 RIGHT ATTACH ANGLE, VERTICAL STABILIZER IS CRACKED. INSTALLED REPAIR ANGLE DOUBLER PER AARD 53-10-00-2, REFERENCE ECO K 2221CC. 2 L 7 2 4F A6WE 20090120 WP 2009 1 20 AALA200910561 1 20081216 A 5322 MOUNT DOUG DC9 DC982 3022082 WP NR 2 GALLEY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 90511 49805 CORROSION ON NUMBER 2 GALLEY TIE DOWN MOUNT. INSTALLED A SERVICEABLE GALLEY MOUNT PER SRM 51-01-51-30. 2 L 7 2 4F A6WE 20090120 WP 2009 1 20 AALA200910562 1 20081217 A 2560 MOUNT DOUG DC9 DC982 3022082 WP GIRT BAR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 90511 49805 CORROSION ON AFT SERVICE DOOR, FORWARD GIRT BAR MOUNT. INSTALLED A SERVICEABLE GIRT BAR MOUNT PER SRM 51-01. 2 L 7 2 4F A6WE 20090120 WP 2009 1 20 AALA200910563 1 20081217 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 90511 49805 CUSP MEMBRANE CRACKED AT STATION 218 OUTBOARD OF NUMBER 2 SEAT TRACK. INSTALLED REPAIR PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20090120 WP 2009 1 20 AALA200910556 1 20081215 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 90511 49805 CORROSION ON DIAMOND DOUBLER (DELTA PLATE) STATION 1338 AT LONGERON 30. REMOVED DIAMOND DOUBLER AND INSTALLED A SERVICE ABLE DOUBLER PER SRM 51-01. 2 L 7 2 4F A6WE 20090120 WP 2009 1 20 AALA200910576 1 20081217 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN FAULTY A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 465A 49595 CABIN EMERGENCY LIGHTS TEST DIM. 2 L 7 2 4F A6WE 20090120 WP 2009 1 20 AALA200910558 1 20081216 A 2560 MOUNT DOUG DC9 DC982 3022082 WP GIRT BAR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 90511 49805 CORROSION ON FORWARD GIRT BAR MOUNT STATION 1145. INSTALLED A SERVICEABLE GIRT BAR MOUNT. 2 L 7 2 4F A6WE 20090121 NM 2009 1 21 DHLA2009770AT520 1 20081218 A 5347 SEAT TRACK BOEING 727 7272B7 138407L NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 770AT 21953 UPPER FUSELAGE MAIN CARGO CABIN SEAT TRACK WITH CORROSION FROM BS 480 TO BS 620 RBL 45.5 OTBD FLANGE. REPLACED SEAT TRA CK FROM BS 480 TO BS 690 RBL 45.5 IAW SRM 51-10-1 PARA 7A AND IAW RIGID BARRIER INSTALLATION PARA 5.4. 2 L 7 3 4F A3WE 20090121 NM 2009 1 21 DL76G090028 1 20080107 A 2910 HOSE BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B6 30025 NE HYD SYSTEM LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 153DL 24985 695307 RIGHT HYD QTY EICAS MESSAGE WITH RT HYD QTY LIGHT. RT SYSTEM QTY INDICATING 0.47 WITH RF AND DECREASING SLOWLY 5 HOURS AND 20 MIN INTO FLIGHT. REPLACED LINE WITH BORROW PART FROM AIR FRANCE. FOUND RT ENG EDP HYDRAULIC PRESS HOSE ASSEMBLY LEAKING. REPLACED HOSE ASSEMBLY RAN ENG LEAK CHECK PERFORMED FOUND NML PART PROVIDED BY AIR FRANCE, MPN AE1010744M0174 . 2 L 7 2 4F 4 F RT A1NM E13NE 20090121 NM 2009 1 21 UPS09M54381 1 20081227 A 5280 SE105200124 DOOR FRAME DOUG MD11 MD11F 3023600 NM LANDING GEAR GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:1C CENTER LANDING GEAR RT FWD DOOR HAS DEEP GOUGE ON FWD SIDE. REPLACED CENTER LANDING GEAR RT FWD DOOR FRAME REF MD11 SRM 51-35-01 VOL 2 PG 1 AND MD11 SRM 51-35-02 VOL 2 PG 2. 2 L 7 3 4F RT A22WE 20090121 WP 2009 1 21 UPS08854242 1 20081024 A 5514 DOUBLER DOUG DC8 DC873F 302199F WP HORIZ STAB DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQ 803-S2-01 RT HORIZONTAL STAB XE 25.312 - XE 29.812, HAS NO SRM REF. REMOVED, FABBED AND I NSTALLED REPAIR DOUBLER IAW EA 008-5500-01-A1585, AND EO DC8-5530-31694-A. 2 L 7 4 4F RT 4A25 20090121 NM 2009 1 21 UPS09M54379 1 20081230 A 5720 ARB2890502 DOUBLER DOUG MD11 MD11F 3023600 NM RT WING GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:1C REPAIR SURVEY SEQ 289-W4-04 FOUND GOUGE ON REPAIR DOUBLER ON RT WING FIXED L/E STA XOS 740-729. REMO VED, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-01-00 VOL 2 AND 51-31-01 VOL PG 2. 2 L 7 3 4F RT A22WE 20090121 NM 2009 1 21 UPS09M54371 1 20081230 A 5330 NDA6313507 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE F1-289-2 HAS DEEP BLEND OUT ON CORNER APPROX 4 X .2 INCH. REPLACED REPAIR BY FABRICATION REF REPAIR SURVEY SEQ F1-289-2 AT AFT SIDE OF FWD LOWER CARGO DOOR, STA 1002 AND LONGERON L-40R TO L-42R REF EA 011-5330-01-A1595 AND EO MD11-5330-31865-A. 2 L 7 3 4F RT A22WE 20090122 NM 2009 1 22 AALA200802628A 1 20081202 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 604AA 27055 MIA - EMERGENCY LIGHTS AT SEAT ROWS 9 TO 15 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER AT SEAT ROW 9E. SYSTEM GROU ND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20090122 NM 2009 1 22 AALA200802629A 1 20081202 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 604AA 27055 MIA - EMERGENCY LIGHTS AT SEAT ROWS 9 TO 15 INOPERATIVE. REPLACED BATTERY PACK AND CHARGER AT SEAT ROW 19E. SYSTEM GRO UND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20090120 NM 2009 1 20 DLM88090036 1 20081230 A 5230 PAN DOUG MD88 MD88 3023688 NM C1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 974DL 53242 CRACK ON C1 DOOR FWD PAN BEHIND DOOR STOP NR 2. REF NRC T0118022. CRACK WAS STOP DRILLED IAW SRM 52-05D FIG 50. REPAI R DOUBLER WAS INSTALLED IAW SRM 52-05D FIG 50 AND IDENTIFIED IAW PS 900-5-1 NR 4. 2 L 7 2 4F RT A6WE 20090120 NM 2009 1 20 DLM88090040 1 20081202 A 5330 PANEL DOUG MD88 MD88 3023688 NM AFT FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 974DL 53242 EXFOLIATION CORROSION ON AFT LAVATORY SERVICE PANEL. REMOVE CORROSION IAW SRM 51-10-3 PAR 35, FOUND OUT OF LIMITS. REP AIR PARTS FABRICATED IAW ERA 472127-14 REV ORIG. REPAIR PARTS INSTALLED IAW ERA 472127-14 REV ORIG AND IDENTIFIED IAW P S 900-5-1 NR 4. 2 L 7 2 4F RT A6WE 20090120 WP 2009 1 20 UPS09854271 1 20081209 A 5330 561537869 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE: SV VALIDATE APPENDIX G FOR REPAIR SURVEY SEQUENCE NR 715-F1-41, STA 1438 T O 1454 AT L29R TO L31R. REP AIRED IAW UPS EO DC8-5330-31569A. 2 L 7 4 4F RT 4A25 20090120 WP 2009 1 20 UPS09854272 1 20081223 A 5753 DOUBLER DOUG DC8 DC871F 302199D WP TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE: SV RT WING OTBD FLAP INBD HINGE COVER DOUBLER GOUGES. REPAIRED IAW EO 5720 31754A. 2 L 7 4 4F RT 4A25 20090120 WP 2009 1 20 UPS09854273 1 20081223 A 5753 DOUBLER DOUG DC8 DC871F 302199D WP TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE: SV STA 340 LT WING OTBD FLAP STA 340 OTBD SIDE OF FLAP HINGE COVER EXISTING DOUBLER GOUGED. REPAIRED I AW UPS EO 5720 31755A. 2 L 7 4 4F RT 4A25 20090121 NM 2009 1 21 DHLA2009743538 1 20081126 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 FUSELAGE FRAME AT BS 600 HAS DOUBLE DRILLED HOLES BETWEEN STR 13R AND 17R. REMOVED FRAME SECTION BETWEEN STR 13R AND 18 R. FABRICATED FRAME SECTION, AND INSTALLED PER B727 SRM 53-10-2 FIG 2, AND 51-10-1. ALSO, ACCOMPLISHED FRAME REPAIR BE TWEEN STR 11R AND 14R PER B727 SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 20090121 NM 2009 1 21 UPS09654317 1 20081230 A 5711 114T02212 BRACKET BOEING 767 76734AF 1385212 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE:C RT WING LES 675 L/E SUPPORT AFT UPPER FRONT SPAR BRACKET FOUND CRACKED. RT WING LES 675 L/E SUPPORT A FT UPPER FRONT SPAR BRACKET REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20090121 NM 2009 1 21 AALA200910598 1 20081212 A 5310 BEAM BOEING 737 737823 13844CB NM BS 294.5 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CORROSION ON BEAM STATION 294.5 RBL 30. REPAIRED PER ESO 61000. 2 L 7 2 4F RT A16WE 20090113 EU 2009 1 13 UALA2008120506768 1 20081205 A 3260 PROXIMITY SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LANDING GEAR DIRTY A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 454UA 1104 L-G SYS DISAGREE ECAM. RTFL. RECURRED ON NEXT FLT OUT. PROX SENSOR S24GA AND 25GA, DIRTY. CLEANED -OK. 2 L 7 2 4F 4 F RT A28NM E40NE 20090109 NM 2009 1 9 NWAA085676316 1 20081219 A 3350 POWER SUPPLY BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 676NW 33002 DURING OVERNIGHT CHECK FOUND DOOR 3 RT EMERGENCY EXIT SIGN INOP. MX R&R POWER SUPPLY. OPS CHECKED GOOD AND ACFT WAS RE TURNED TO SERVICE. 2 L 7 4 4F RT A20WE 20090109 WP 2009 1 9 IXXA08SMN215S 1 20081028 A 5311 FRAME DOUG DC8 DC862F 3021972 WP BS 420 L19R DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 420.00 0 LONGERON 19 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICA TED ANGLE DOUBLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS I AW FAA FORM 8110-3 NR 08549, DRAWING ED-4877, DC8 NDT SPM PART 06-10-01-001, SRM 51-1-1 PAGES 1, 13, AND 17, SRM 51-1-8B , SRM 51-1-20D, AND SRM 51-3-1. 2 L 7 4 4F 4A25 20090109 NM 2009 1 9 ASAA0944161 1 20081218 A 5753 6546486150 SKIN BOEING 737 7374Q8 138447Q NM MIDFLAP PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 779AS 25111 RT IB MID FLAP TRAILING EDGE WEDGE HAS A PUNCTURE IB OF 2ND TRACK. REMOVED EXISTING DOUBLER FABBED REPAIR PARTS AND BON DED REPAIR IAW B737 400 SRM 51 70 10. 2 L 7 2 4F RT A16WE 20090113 NM 2009 1 13 USAA2009011290065 1 20081216 A 5712 6545445 RIB BOEING 737 7374B7 138449C NM RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 NR 03-0528-8-0176/001 AND 6099288 - CRACK ON RT WING RIB LOWER CHORD WEB AT WBL 135.5. REPAIRED RT WING RIB LOWER CHORD WEB AT WBL 135.5 IAW EA NR 100777. 2 L 7 2 4F RT A16WE 20090113 SO 2009 1 13 SIMA200900902 1 20081225 A 3240 429513 CONTROL UNIT EMB 145 EMB145LR 3260212 SO BRAKE SYSTEM MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION LD LANDING 1 SW 21 625AE 18056 639 145115 ON FLIGHT 4345, CREW REPORTED UPON GEAR EXTENSION THEY RECEIVED 2 EICAS MESSAGES 1 FOR INBD BRAKES INOPERATIVE AND 1 FOR OTBD BRAKES INOPERATIVE. THEY RECYCLED GEAR WITH NO HELP. CREW DECLARED EMERGENCY AND LANDED USING THRUST REVERSERS. BRAKES APPEARED TO WORK NORMALLY. ACFT TAXIED TO GATE SAFELY WITH NO FURTHER INCIDENTS. CREW INSP SHOWED NO APPARENT P HYSICAL DEFECTS. REMOVED AND REPLACED BRAKE CONTROL UNIT. OPS CHECK GOOD. ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20090113 SO 2009 1 13 SIMA200900903 1 20081228 A 5610 NP15131111 WINDSHIELD EMB 145 EMB145LR 3260212 SO COCKPIT CRACKED A SIMA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 21 689EC 14500853 ON FLIGHT 4122, CREW REPORTED BOTH WINDSHIELDS SHATTERED ON TAKEOFF AT 125KTS. ACFT REMOVED FROM SERVICE. REMOVED AND REPLACED BOTH COCKPIT WINDSHIELDS. OPS CHECK GOOD. NO LEAKS NOTED. ACFT RETURNED TO SERVICE.LT WINDSHIELD P/N OFF NP15 131112 S/N OFF 08071H7424 2 L 7 2 4T RT T00011AT 20090113 NE 2009 1 13 QMLA122320080805 2 20081223 A 7200 400100025 ENGINE BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE NR 2 MALFUNCTIONED E QMLA F A ACTIVATE FIRE EXT. UNSCHED LANDING J B A WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE AA AIR AMBULANCE 1 NM 03 601EH 6346 31 7181 LE45599 APPROACHING THE AIRPORT LANDING PAD AND STILL ATTEMPTING TO MATCH THE TORQUES, THE NR 2 ENG TORQUE NEEDLE WAS HIGH AND N R 1 ENG TORQUE NEEDLE WAS LOW. THE TRIMMING AND ATTEMPTING TO MATCH THE TORQUES WERE COMPLETELY UNSUCCESSFUL. ALL COLLEC TIVE MOVEMENTS MADE THINGS WORSE. LANDED AND OBSERVED THE (2) TORQUE NEEDLE REACH 125-130 PERCENT. IMMEDIATELY AFTER LAN DING OBSERVED SMOKE COMING FROM THE RT SIDE OF THE HELICOPTER, LOOKED OUT THE RT SIDE AND TO THE REAR HE SAW FIRE COMING FROM THE (2) ENGINE EXHAUST. PILOT ARMED THE NR 2 ENGINE FIRE EXT AND ACTIVATED THE NR1 BOTTLE OF AGENT DISCHARGE. LEAD PILOT AND MX PERSONNEL WERE CALLED. PILOT REPORTED TO MECHANIC TORQUE SPLIT AND HIGH TOT. FIRE LIGHT DID NOT COME ON. 1 G 7 2 3U 3 U H13EU E5NE10 20090113 EU 2009 1 13 MALA080226 1 20081228 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 456XJ 456 FOUND EMERGENCY LIGHTING FLOOR PROXIMITY LIGHT 42LN INOP. REMOVED AND REPLACED LIGHT ASSY PN 6636-2 IAW AMM 33-50-20. O PS CHECK GOOD. 2 L 7 2 4T RT A52EU 20090113 EA 2009 1 13 MALA080227 1 20081229 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY INTERMITTENT A MALA K NONE N FALSE WARNING CR CRUISE 1 GL 15 836AY 8036 DURING CLIMB THROUGH 3500 FT, AMBER TOILET SMOKE CAUTION EICAS MESSAGE. MESSAGE WENT AWAY AFTER APPROX 20 SECONDS, VERIF IED ALL OK IN THE LAV. SYS OPS CHECK GOOD IAW FIM 26-00-00. 2 L 7 2 4F RT A21EA 20090113 EA 2009 1 13 SWIA200820785 1 20081230 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 507CA 7796 FLT 2740 - CEILING AFT EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090113 SO 2009 1 13 SWIA200820771 1 20081230 A 3350 LIGHT EMB 120 EMB120ER 3260203 SO CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 576SW 120345 FLT 7796 - ENTRY EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4T RT A31SO 20090113 EA 2009 1 13 SWIA200820773 1 20081229 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 710BR 7852 FLT 6162 - 2ND TO AFT EMERGENCY LIGHT AND EXIT SIGN INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090113 EA 2009 1 13 SWIA200820766 1 20081215 A 5320 SILL CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 743SK 10199 DURING C-CHECK, RIGHT OUTBOARD FLOOR SILL AT FS280 CORRODED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090113 EA 2009 1 13 SWIA200820768 1 20081202 A 5312 STIFFENER CNDAIR CL600 CL6002C10 1390015 EA BULKHEAD CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 740SK 10196 DURING C-CHECK, FS 280 BULKHEAD WEB STIFFENER AT RBL 25.5 CRACKED. REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20090113 EA 2009 1 13 SWIA200820769 1 20081202 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 740SK 10196 DURING C-CHECK, FS280 FLOORBEAM CRACKED RIGHT SIDE. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090113 SO 2009 1 13 SWIA200820770 1 20081229 A 5210 DOOR EMB 120 EMB120ER 3260203 SO PAX DOOR LACK OF LUBE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 579SW 120347 FLT 5408 - MAIN CABIN DOOR HARD TO OPEN. CLEANED AND LUBED CABIN DOOR. 2 L 7 2 4T RT A31SO 20090114 WP 2009 1 14 AALA200802601A 1 20081129 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP ZONE 200 DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 442AA 49468 LGA EMERGENCY LIGHT AFT FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT FORWARD GALLEY. SYSTE M GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 20090114 NM 2009 1 14 AALA200802605A 1 20081129 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 759AN 32638 DFW EMERGENCY LIGHT AT SEAT 26G INOPERATIVE. REPLACED LAMP AT SEAT 26G. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSE D) 2 L 7 2 4F RT T00001SE 20090114 WP 2009 1 14 AALA200802572A 1 20081123 A 4900 CSD DOUG DC9 DC982 3022082 WP APU FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 7508 49802 MSY INFLIGHT DFW TO TPA. CREW REPORTED RIGHT HAND CONSTANT SPEED DRIVE LOW PRESSURE INDICATION. APU WOULD NOT START. D IVERTED TO MSY AND LANDED WITHOUT INCIDENT. REPLACED CONSTANT SPEED DRIVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLO SED) 2 L 7 2 4F A6WE 20090114 EA 2009 1 14 A6WA200840638 1 20081214 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA LT MLG MALFUNCTIONED A A6WA O OTHER O OTHER LD LANDING 1 GL 31 407AW 7424 LT MLG DID NOT EXTEND ON LANDING. 2 L 7 2 4F RT A21EA 20090114 NM 2009 1 14 HNAA2009010900383 1 20080913 A 5730 85711802005 PANEL DHAV DHC8 DHC8102 2809003 NM LT WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 980HA 36674 36674 380 DURING C-CHECK INSP, THE LT WING STRESS PANEL, 522AT, WAS FOUND TO HAVE CORROSION IN SOME OF THE SCREW COUNTER SINKS THA T WAS BEYOND ACCEPTABLE LIMITS. THE PANEL WAS REPLACED. 2 H 7 2 4T RT A13NM 20090114 NM 2009 1 14 DHLA2009770502 1 20081218 A 5311 FRAME BOEING 727 7272B7 138407L NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 770AT 21953 UPPER FUSELAGE CARGO CABIN FRAME WITH DENT BS 600 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME SECTION BS 600 BETWE EN S-16R AND S-17R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20090114 NM 2009 1 14 DHLA2009770503 1 20081218 A 5311 FRAME BOEING 727 7272B7 138407L NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 770AT 21953 UPPER FUSELAGE CARGO CABIN FRAME WITH DENT AT BS 540 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME SECTION BS 540 BE TWEEN S-16R AND S-17R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20090114 WP 2009 1 14 AALA200802576A 1 20081124 A 2120 5953625521 DUCT DOUG DC9 DC982 3022082 WP AIR CONDITIONING LEAKING A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 21 446AA 49472 DFW INFLIGHT. CREW REPORTED TAIL COMPARTMENT OVERTEMP INDICATION DURING CLIMB. RETURNED TO DFW AND LANDED WITHOUT INC IDENT. FOUND DUCT BLOWN IN TAIL COMPARTMENT. AIRCRAFT OUT OF SERVICE FOR REPAIRS. REPLACED RIGHT HAND AIR CONDITIONIN G WATER SEPARATOR DUCT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F A6WE 20090114 WP 2009 1 14 AALA200802589A 1 20081126 A 8097 CONNECTOR DOUG DC9 DC982 3022082 WP NR 2 START VALVE LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 426AA 49338 INFLIGHT, RIGHT ENGINE START VALVE INDICATION. RETURNED TO TUL AND LANDED WITHOUT INCIDENT. RESEATED VALVE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20090114 WP 2009 1 14 AALA200802591A 1 20081126 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 9405T 53141 EMERGENCY LIGHT EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK AT AFT GALLEY FOR INOPERATIVE EMERGENCY LIGHT EXIT SIGN. S YSTM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20090114 WP 2009 1 14 IXXA08SMN202S 1 20081024 A 5730 SKIN DOUG DC8 DC862F 3021972 WP RT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XRS 74.869 STRINGER 9. REMOVED FASTEN ERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, AND FILLER PLUG. PERFORMED NDT INSPECTION . NO CRACK AND NO CORROSION. TAPERED EXTERNAL DOUBLER FROM 0.160 INCH TO 0.080 INCH. CLEANED, TREATED, PRIMED AREA A ND EXTERNAL DOUBLER. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-2-1 FIGURE 17, DC8 SRM 51-1-20D, SRM 57-3- 2 FIGURE 13, DC8 NDT SPM PART 08, DC8 SRM 51-10-0 FIGURE 1 SHEET 20, DC8 SRM 51-1-8B, IAW DC8 SRM 51-1-12, AND SRM 51-3- 1. 2 L 7 4 4F 4A25 20090114 NM 2009 1 14 AALA200802595A 1 20081126 A 3350 LAMP BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 790AN 30251 EMERGENCY LIGHT AT SEAT 33G MISSING LAMP. REPLACED LAMP AT SEAT 33G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20090114 WP 2009 1 14 IXXA08SMN209S 1 20081028 A 5320 3750257505N FITTING DOUG DC8 DC862F 3021972 WP FUSELAGE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT SPLICE FITTING CRACKED AT STATION 600.000 - 620.000 L ONGERON 31 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, AND SRM 51-3-1. 2 L 7 4 4F 4A25 20090114 WP 2009 1 14 AALA200802620A 1 20081201 A 2120 DUCT DOUG DC9 DC982 3022082 WP ACM CRACKED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 431AA 49343 INFLIGHT CREW REPORTED UNABLE TO PRESSURIZE CABIN. RETURNED TO STL AND LANDED WITHOUT INCIDENT. FOUND BROKEN DUCT ON R IGHT HAND AIR CYCLE MACHING. REPLACED RIGHT HAND AIR CYCLE MACHINE DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20090114 WP 2009 1 14 IXXA08SMN201S 1 20081024 A 5751 SKIN DOUG DC8 DC862F 3021972 WP RT AILERON MISREPAIRED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD AILERON LOWER HAS IMPROPER REPAIR AT STATION XW 698.000. REMOVE D EXISTING REPAIR. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. PERFORMED BALANCE. FOUND WITHIN LIMITS WITH A MOMENT: 3322.9 IN-POUNDS. INSTALLED REPAIR PARTS AT S TATION XA 724.000 - XW 698.000 IAW DC8 SRM 57-8-1 FIGURE 4 ITEMS "E" AND "L", DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DOUGLA S DRAWING NUMBER 5763133, DC8 SRM 51-1-9 TR NUMBER 51-142, SRM 51-1-9A TR 51-141, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-1-21A, AND DC8 SRM 51-4-3 PAGES 1-4. 2 L 7 4 4F 4A25 20090114 EU 2009 1 14 MALA080225 1 20081231 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 435XJ 340B435 EMERGENCY COVE LIGHT AT 15LN DAMAGED. REPLACED LIGHT ASSY. 2 L 7 2 4T RT A52EU 20090114 NM 2009 1 14 DHLA2009770AT513 1 20081209 A 5315 FLOORBEAM BOEING 727 7272B7 138407L NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 770AT 21953 UPPER FUSELAGE CARGO CABIN AT BS 1130 BETWEEN RBL 25 AND RBL 45 FLOORBEAM UPPER AND LOWER FACE WITH CORROSION. REPAIRED FUSELAGE FLOORBEAM UPPER CHORD SECTION AT BS 1130 BETWEEN RBL 37 AND RBL 47.5 IAW B727 SRM 53-10-8 FIG 10. 2 L 7 3 4F A3WE 20090114 NM 2009 1 14 FDEA200812245277 1 20081224 A 5330 65562385 STRAP BOEING 727 727233 138408A NM BS 680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 FWD CARGO BAY CORROSION AT AFT OF STA 680, STR 26R TO STR 26L REPAIRED (REMOVED & REPLACED) TEAR STRAP AT FWD PIT STA 68 0 BETWEEN STR 26R AND 26L IAW DRAWING 65-56238 REV. B AND SRM 51-30-2. 2 L 7 3 4F RT A3WE 20090109 CE 2009 1 9 Z5FA122008N550CS1 1 20081220 A 3230 99125373 ACTUATOR CESSNA 560 560XL 2076702 CE LT MLG MALFUNCTIONED E Z5FA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 63 550CS 3665 5605551 ON APPROACH, CREW OBSERVED NO GEAR DOWN AND LOCK INDICATION FOR LT MLG. CREW ABORTED APPROACH TO WORK AFM ABNORMAL/EMER GENCY CHECK LIST. CREW DECLARED EMERGENCY AND SHORTLY AFTER ATTEMPTS TO BLOW GEAR DOWN, CREW RECEIVED DOWN AND LOCK INDI CATION. ACFT LANDED WITHOUT INCIDENT. NO RESOURCES AVAILABLE TO PERFORM GEAR SWING AT MX FACILITY AND ACFT WAS FERRIED T O MFG FACILITY. MX REPLACED THE LT MLG ACTUATOR IAW 32-30-04. GEAR SWINGS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A22CE 20090114 NM 2009 1 14 DHLA2009770AT515 1 20081208 A 5230 SKIN BOEING 727 7272B7 138407L NM FWD CARGO DOOR DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 770AT 21953 LOWER FUSELAGE FWD CARGO COMPARTMENT DOOR OUTER SKIN WITH DENT AT BS 617.5 BETWEEN BEAM 2 AND BEAM 3. REPAIRED FWD CARG O COMPARTMENT DOOR OUTER SKIN SECTION AT BS 615.5 TO620 BETWEEN BEAMS 2 AND 3 IAW B727 SRM 52-00-3 FIG 3. 2 L 7 3 4F A3WE 20090114 NM 2009 1 14 ASAA0944178 1 20081223 A 5311 65C312403 DOUBLER BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON INTERNAL DOUBLER ON FRAME STA 794 RBL 30 WL 160. R&R INTERNAL DOUBLER PER SRM 51 40 02. 2 L 7 2 4F RT A16WE 20090114 WP 2009 1 14 IXXA08SMN218S 1 20081028 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 1080.0 00 LONGERON 19-20 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FAB RICATED ANGLE DOUBLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PAR TS IAW FAA FORM 8110-3 NUMBER 08549, SEMAN DRAWING ED-4877, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-1 PAGES 1, 13, A ND 17, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D, AND SRM 51-3-1. 2 L 7 4 4F 4A25 20090114 WP 2009 1 14 IXXA08SMN219S 1 20081028 A 5730 SKIN DOUG DC8 DC862F 3021972 WP LT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD CENTER LEADING EDGE LOWER SKIN CRACKED AT STATION XS 520.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP HOLE. PERFORMED NDT INSPECTION. NO CRACK AND NO CORRO SION FOUND. FABRICATED EXTERNAL DOUBLER, INTERNAL DOUBLER, AND SPACER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08543 DATED 11-18-08, SEMAN DRAWING ED-4876 DATED 11-08-08, DC8 SRM 51-1-21, SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, SRM 51-1-11, SRM 51-1-20D, AND SR M 51-3-1. 2 L 7 4 4F 4A25 20090114 NM 2009 1 14 ASAA0944181 1 20081223 A 5311 654795967 STRAP BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON FAILSAFE STRAP. REPLACED FAILSAFE STRAP. 2 L 7 2 4F RT A16WE 20090115 NM 2009 1 15 FDEA200812295313 1 20081229 A 5322 65163491 SHEAR TIE BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 276FE 22041 AFT CARGO COMPARTMENT - CORROSION ON SHEAR TIE AT BS 1166 AFT SIDE BETWEEN STRINGERS 29L AND 28L. CORROSION ON SHEAR T IE 100% MATERIAL LOSS & OUT OF LIMITS IAW SRM 53-10-1 FIG 1. REMOVED SHEAR TIE IAW SRM 51-30-2 AND FABRICATED NEW PART IAW SRM 51-20-1 FIG 7 & 53-10-2 FIG 5. TREATED AND PRIMED NEW PART IAW SRM 51-10-2 AND INSTALLED PART IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 20090115 NM 2009 1 15 FDEA200812245274 1 20081224 A 5522 65256372 SKIN BOEING 727 727233 138408A NM LT ELEVATOR DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 GOUGE AND DENT IN UPPER SURFACE SKIN OF LT ELEVATOR, O/B END OF CONTROL TAB CUTOUT, AT JOINT OF ELEVATOR T/E WEDGES. B LENDED AND SMOOTHED GOUGE AREA IAW SRM 51-10-1. FABRICATED REPAIR DOUBLERS IAW SRM 55-20-3. TREATED AND PRIMED PART IA W SRM 51-10-2. INSTALLED REPAIR DOUBLRES IAW 55-20-3 FIG 2. REBALANCE NOT REQUIRED IAW SRM 51-80-00 PAG 1 & 2. PAR 3D. 2 L 7 3 4F RT A3WE 20090116 EA 2009 1 16 A6WA200840621 1 20081130 A 2612 FIRE LOOP CNDAIR CL600 CL6002B19 1900309 EA LT FUSELAGE MALFUNCTIONED A A6WA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 455AW 7848 ANTI ICE DUCT WARNING MSG ON TAKEOFF. TAKEOFF ABORTED AT 80 KNOTS, BRAKE TEMPS WERE 5,6,3,3 SYNOPTIC PAGE SHOWS LT FUSE LAGE RED. R&R LT FUSELAGE FIRE DETECTION LOOP AS PER AMM 36-21-04, OPS CHECK GOOD AT THIS TIME. 2 L 7 2 4F RT A21EA 20090116 EA 2009 1 16 A6WA200840653 1 20081229 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 1900309 EA COCKPIT CRACKED A A6WA A UNSCHED LANDING D INFLIGHT SEPARATION CR CRUISE 1 GL 31 427ZW 7685 LOG 198420/2 CAPTAINS SIDE WINDSHIELD SHATTERED INFLIGHT COMPLIED WITH QRH. R&R CAPTS SIDE WINDSHIELD IAW CRJ AMM 56-11 -01. REF W/O 130800 W/C NR 1 FOR LEAK CHECK AND OPS CHECK. 2 L 7 2 4F RT A21EA 20090112 NM 2009 1 12 FDEA200812245276 1 20081224 A 5344 5212874 HINGE BOEING 727 727233 138408A NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 EXTERIOR FUSELAGE AFT SEGMENT OF MCD HINGE, FUE SIDE, HAS A LOBE CRACKED STA. 680-720 REMOVED AFT SECTION MAIN CARGO DOO R HINGE IAW SRM 51-30-2. FABRICATED NEW HINGE IAW SRM 51-30-5 AND 51-10-1. TREATED AND PRIMED NEW HINGE IAW SRM 51-1 0-2. INSTALLED NEW MCD HINGE SECTION IAW SRM 51-30-2. OPS CHECK GOOD. 2 L 7 3 4F RT A3WE 20090112 NE 2009 1 12 U2RA872LP2993 2 20081225 A 7320 CABLE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C 13802 NE NR 1 ENGINE OUT OF RIG A U2RA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 GL 23 872SJ 46040 693372 NR 1 ENGINE FLAMED OUT AT IDLE AT 30,000 FT. BEGAN PERFORMING ENGINE FLAMEOUT ABNORMAL CK LIST. ENGINE RELITE AND PERF ORMED NORMALLY AFTER IGNITION TURNED ON. FINISHED ABNORMAL CK LIST. WEATHER VMC. PERFORMED PULL, TRAVEL AND RIGGING CH ECKS OF VBV AND VSV FEEDBACK CABLES IAW MM 73-20-1, PULL AND TRAVEL CHECKS OF VBV AND VSV CABLES NO DEFECTS. RIGGED VBV AND VSV CABLES IAW MM 73-20-1. 2 L 7 4 4F 4 F RT 4A25 E2GL 20090114 NM 2009 1 14 HNAA2009010900382 1 20080911 A 5310 85320807101 DOOR FRAME DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 982HA 36674 36673 380 DURING C-CHECK INSP, THE LAVATORY SERVICE DOOR FRAME WAS FOUND TO HAVE CORROSION ON IT. THE DOOR FRAME WAS REPLACED IAW SRM PROCEDURES. ADDITIONALLY, THE PAX DOOR THRESHOLD WAS FOUND TO BE CORRODED. THAT ITEM, P/N 85320686-101, WAS ALSO R EPLACED. 2 H 7 2 4T RT A13NM 20090121 NM 2009 1 21 DHLA2009770AT521 1 20081219 A 5313 STRINGER BOEING 727 7272B7 138407L NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 770AT 21953 LWR FUSELAGE FWD CARGO COMPARTMENT S-28R WITH CORROSION AT BS 488. REPAIRED S-28R SECTION BETWEEN BS 480 TO BS 516.5 IA W SRM 53-10-3 FIG 1. REPLACED S-28R SECTION FROM BS 450 TO BS 480 IAW SRM 51-10-1 PARA 7A AND 53-10-3 FIG 1. 2 L 7 3 4F A3WE 20090121 NM 2009 1 21 DHLA2009770AT522 1 20081212 A 5311 FRAME BOEING 727 7272B7 138407L NM ZONE 100 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 770AT 21953 LWR FUSELAGE FWD CARGO COMPARTMENT DOOR CUTOUT BS 620 AT STOP FITTING NR 1 WEB WITH CRACK. REPAIRED FUSELAGE FRAME WEB SECTION AT BS 620 BETWEEN S-18R AND S-22R IAW B727 SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 20090121 NM 2009 1 21 DHLA2009770AT523 1 20081212 A 5311 FRAME BOEING 727 7272B7 138407L NM ZONE 100 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 770AT 21953 LWR FUSELAGE FWD CARGO COMPARTMENT DOOR CUTOUT BS 560 AT STOP FITTING NR 1 WEB WITH CRACK. REPAIRED FRAME WEB SECTION A T BS 560 BETWEEN S-17R AND S-22R IAW SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 20090121 NM 2009 1 21 UPS09554377 1 20081230 A 4930 SUPPORT CHANNEL BOEING 757 75724APF 1384969 NM APU CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 461UP 28265 INSPECTION TYPE:C2 APU FIRE WIRE SUPPORT BRACKET RT APU ACCESS DOOR IS CHAFING ON APU FUEL LINE AT 4TH LATCH FROM THE FR ONT. REMOVED SUPPORT CHANNEL, FABRICATED AND INSTALLED REPLACEMENT CHANNEL PER SRM 51-40-02 2 L 7 2 4F RT A2NM 20090121 NM 2009 1 21 UPS09M54359 1 20081228 A 5713 ARB293347 ANGLE DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:1C LT WING L/E STRINGER ANGLE FOUND CRACKED APPROX 1 INCH IN LENGTH AT STA XORS 456. REPAIRED LT WING L /E STRINGER ANGLE AT XORS 456 BY FABRICATION REF DWG ARB2933 AND MD11 SRM 51-31-01 VOL II PAGE 1. 2 L 7 3 4F RT A22WE 20090121 NM 2009 1 21 UPS09M54360 1 20081227 A 5320 ANB718036 ANGLE DOUG MD11 MD11F 3023600 NM RT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:1C LOWER FUSELAGE STA 1381 RT MLG WHEEL WELL DOOR CUTOUT FWD ANGLE CRACKED AS MARKED. REPAIRED RT MLG W HEEL WELL DOOR CUTOUT FWD CLIP AT STA 1381 BY FABRICATION REF DWG ANB7180 AND MD11 SRM 51-35-01 VOL II PG 10. 2 L 7 3 4F RT A22WE 20090122 WP 2009 1 22 AALA200910612 1 20081223 A 5230 FITTING DOUG DC9 DC983 3022083 WP CARGO DOOR WRONG PART A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 CARGO DOOR UPPER AFT FITTING WRONG TYPE. REMOVED AND REPLACED FITTING PER S/B DC9-52-189. 2 L 7 2 4F RT A6WE 20090122 EA 2009 1 22 SWIA200820835 1 20081211 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 DURING C-CHECK, RIGHT INBOARD CLIP AT FS 280 RBL 9 CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20090122 WP 2009 1 22 AALA200910614 1 20081229 A 5230 FITTING DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 CARGO DOOR STOP FITTING ON FORWARD SIDE CRACKED. REPLACED FITTING PER ESO 80174. 2 L 7 2 4F RT A6WE 20090122 WP 2009 1 22 AALA200910615 1 20081223 A 5320 FITTING DOUG DC9 DC983 3022083 WP CARGO DOOR WRONG PART A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 434AA 49452 LOWER FORWARD CLIP WRONG TYPE ON CARGO DOOR. REMOVED AND REPLACED FITTING (CLIP) PER S/B DC 9 - 52- 189. 2 L 7 2 4F RT A6WE 20090122 WP 2009 1 22 WX0A070253 1 20081213 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 878GA 53487 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE POWER SUPPLY BAT TERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 20090122 WP 2009 1 22 WX0A070254 1 20081218 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 878GA 53487 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETUR NED TO SERVICE. 2 L 7 2 4F RT A6WE 20090122 WP 2009 1 22 WX0A070255 1 20081220 A 3350 6111779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 879GA 53486 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION, MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENC Y EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN TH E POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETU RNED TO SERVICE. 2 L 7 2 4F RT A6WE 20090122 WP 2009 1 22 UPS08854248 1 20081024 A 5751 SKIN DOUG DC8 DC871F 302199D WP AILERON MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:SV APPENDIX G SURVEY SEQ 715-W4-01 EXTERNAL DOUBLER DOES NOT MATCH SRM 57-02-01-0 FIG 002Y UPPER SURFA CE RW OUTBOARD AILERON. REPLACED DOUBLER IAW SRM 57-02-01 FIG 002Y REV 78. 2 L 7 4 4F RT 4A25 20090120 NE 2009 1 20 M7KA1006084142 2 20081117 A 7320 130062 ACTUATOR UROCOP UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE FUEL CONTROL INTERMITTENT E M7KA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 19 822MH 4142 23179 GOVENOR LIGHT ILLUMINATES INTERMITTENTLY WITH THIS EMERGENCY BACKUP CONTROL. ACTUATOR INSTALLED. 1 G 7 2 3U 3 U H9EU E00054EN 20090121 NM 2009 1 21 UPS09654319 1 20081228 A 5315 SUPPORT ANGLE BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE:C MEC BS246 LBL 40 FLOORBEAM FRONT FACE SUPPORT ANGLE FWD CRACK. MEC BS 246 LBL 40 FLOORBEAM FRONT FACE SUPPORT ANGLE REPAIRED AS PER SRM 53-10-51-2R4 FIG 201. REPEAT INSP IS REQUIRED AS PER SRM 53-10-51-2R4 FIG 201 SHT 2 TABLE II UPS MPI P20220 ISSUED FOR REPEAT INSP. 2 L 7 2 4F RT A1NM 20090122 EU 2009 1 22 UPS08154244 1 20081227 A 5321 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 169UP 0005 INSPECTION TYPE:N/A DAMAGE TO FLOORBOARD. FABRICATED NEW FLOOR. INSTALLED NEW FLOORBOARD PER AIRBUS AMM 53-10-35. 2 L 7 2 4F RT A35EU 20090122 EU 2009 1 22 UPS08154245 1 20081228 A 5321 GILFAB4123 FLOORBOARD AIRBUS A300 A300F4622R 3930360 EU MAIN CARGO DECK PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 136UP 0819 INSPECTION TYPE:N/A FLOORBOARD DAMAGED MAIN CARGO DECK POS 1 RT SIDE. FABRICATED NEW PANEL IAW EO A300-5320-16409-C. 2 L 7 2 4F RT A35EU 20090122 NM 2009 1 22 UPS09654393 1 20081231 A 5755 SKIN BOEING 767 76734AF 1385212 NM NR 5 SPOILER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE:C LT WING NR 5 SPOILER LOWER SURFACE DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER HX RS R57-70-36252 REV B AND UPS EO B767-5750-31918-A. 2 L 7 2 4F RT A1NM 20090122 NM 2009 1 22 UPS09554374 1 20081230 A 5230 SEAL DEPRESSOR BOEING 757 75724APF 1384969 NM FWD CARGO DOOR DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 461UP 28265 INSPECTION TYPE:C2 DENT ON FWD CARGO DOOR AFT SEAL DEPRESSOR 20 INCHES FROM DOOR BOTTOM. REPAIRED PER ATS ENGINEERING R EPAIR 09-1025. 2 L 7 2 4F RT A2NM 20090122 NM 2009 1 22 DL757081804 1 20081229 A 5347 SEAT TRACK BOEING 757 757232 1384965 NM BS 1435 LBL48 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 CABIN COMPARTMENT FLOOR SEAT TRACK FOUND WITH CORRSION ON TOP SURFACE INBD FLANGE AT SAT, 1435 LBL48 AS MARKED W/L 208-1 0/COMPLIED WITH AT SAA -SAT ON NON- ROUTINE 81720150001. 2 L 7 2 4F RT A2NM 20090122 NM 2009 1 22 DL757081805 1 20081229 A 5313 STRINGER BOEING 757 757232 1384965 NM STA 1520 S29R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 AFT CARGO BETWEEN STA, 1500 AND STA, 1520 STRINGER S-29R FOUND WITH CORROSION AS MARKED. COMPLIED WITH AT SAA, SAT ON N ON-ROUTINE 8172105000. 2 L 7 2 4F RT A2NM 20090122 EA 2009 1 22 SWIA200820830 1 20081216 A 7120 MOUNT CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 DURING C-CHECK, RIGHT ENGINE AFT THRUST MOUNT CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20090122 WP 2009 1 22 AALA200910635 1 20081230 A 5320 ANGLE DOUG DC9 DC983 3022083 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 FORWARD SIDE OF STATION 1338 BULKHEAD VERTICAL ANGLE BETWEEN AIR CONDITIONING DUCTS CRACKED AT TOP FASTENERS. INSTALLED REPAIR PER AARD 53-10-00-15. 2 L 7 2 4F RT A6WE 20090123 WP 2009 1 23 AALA200802630A 1 20081203 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP ZONE 200 DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424AA 49336 LGA - EMERGENCY LIGHTS AT FORWARD COACH CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 8. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20090123 NM 2009 1 23 USAA2009012190114 1 20081226 A 5320 6546812170 SUPPORT BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON INTERCOSTAL SUPPORT BETWEEN BS 947 TO BS 967, LBL 18. REPAIRED INTERCO STAL SUPPORT BETWEEN BS 947 TO BS 967, LBL 18 IAW B737 SRM 51-10-02-06. 2 L 7 2 4F RT A16WE 20090121 NM 2009 1 21 UPS09M54400 1 20081230 A 5720 DOUBLER DOUG MD11 MD11F 3023600 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:1C RIGHT WING TELESCOPING DUCT CUTOUT CRACK ON UPPER I/B CORNER. REMOVED CRACK, FABRICATED AND INSTALLE D DOUBLER IAW MD11 SRM 57-10-00 VOL 1 FIG 42. 2 L 7 3 4F RT A22WE 20090122 WP 2009 1 22 AALA200910613 1 20081223 A 5300 FITTING DOUG DC9 DC983 3022083 WP UNKNOWN WRONG PART A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 UPPER FORWARD CLIP (FITTING) WRONG TYPE. REMOVED AND REPLACED FITTING PER S/B DC9-52-189. 2 L 7 2 4F RT A6WE 20090122 NM 2009 1 22 UPS09554376 1 20081230 A 7830 FITTING BOEING 757 75724APF 1384969 NM THRUST REVERSER GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 461UP 28265 INSPECTION TYPE:C2 NR 1 ENGINE O/B T/R INNER SURFACE AFT LWR CORNER FITTING IS GOUGED. REMOVED AND REPLACED FITTING PER RR EM 70-42-28-300-05. 2 L 7 2 4F RT A2NM 20090122 NE 2009 1 22 UALA2008111306096 2 20081014 A 7250 TURBINE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 ENGINE VIBRATES A UALA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 217UA 42689 10365 30550 222042 ENG VIB MONITOR R RIGHT ENGINE AIRBORNE VIBRATION MONITORING (AVM) SYSTEM IS INOPERATIVE, OR LOSS OF TACHOMETER DATA. S TATUS MSG01- NOT ACTIVE DESCENT INTERMITTENT; 'E' FLANGE ACCELEROMETER (CIRCUIT 1 RIGHT) SIGNAL IS OUT OF RANGE. DB- S IGNAL CONDITIONER UNIT (RIGHT) MSG02- NOT ACTIVE DESCENT INTERMITTENT; 'E' FLANGE ACCELEROMETER (CIRCUIT 1 RIGHT) SIGNAL IS OUT OF RANGE. REPLACED NR 2 ENGINE. SHOP FINDINGS: ENGINE WAS GIVEN A FULL REFURBISHMENT DUE TO POOR PERFORMANCE. LP TURBINE WAS SUSPECT AS CAUSE FOR ON-WING VIBRATION. 2 L 7 2 4F 4 F RT T0001SE E46NE 20090123 NM 2009 1 23 USAA2009012190115 1 20081224 A 5315 6546811 FLOORBEAM BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM UPPER FLANGE AT BS 986.5, BL 0 TO RBL 54. REPAIRED FLOORBEAM UPPER FLANGE AT BS 986.5, BL 0 TO RBL 54 IAW B737 SRM 53-00-51. 2 L 7 2 4F RT A16WE 20090126 NM 2009 1 26 DL757081784 1 20081223 A 5330 146N37505 SKIN BOEING 757 757232 1384965 NM BS 1701 S15L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 DURING HMV, FUSELAGE SKIN DENTS AND OIL CANNING WERE FOUND AT BETWEEN STA 1701 TO 1720 AND S-15L AND S-17L. THE DENTS W ERE APPROVED AS IS AND THE OIL CANNING SKIN WAS CUT OUT AND REPAIRED PER BOEING REPAIR INSTRUCTIONS. 2 L 7 2 4F RT A2NM 20090126 NM 2009 1 26 DL757081786 1 20081223 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1763 S27-28R DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 AFT FUSE SKIN DENT RT STA 1763 S-27R TO S 28R. REPAIR PER SRM 53-00-01 FIG 201 REP 2. 2 L 7 2 4F RT A2NM 20090122 NM 2009 1 22 UALA2008111305641 1 20080908 A 3412 PROBE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE TAT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 127UA 28813 THE "HEAT L TAT" DISPLAYED. RTFL. *S/D* REPLACED LT TAT PROBE. REPLACED TAT SENSOR. REPLACED GROUND SAFETY RELAY R7 334, ALTN NLG SQUAT RELAY R854, LT TAT PWR RELAY & LT TAT CURRENT SENSING RELAY R7429. 2 L 7 4 4F 4 F RT A20WE E24NE 20090122 NM 2009 1 22 UPS09554375 1 20081231 A 5420 STRUT BOEING 757 75724APF 1384969 NM NR 2 NACELLE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 461UP 28265 INSPECTION TYPE:C2 CORROSION ON THE NR 2 ENGINE CNA LWR STRUT 6 O'CLOCK POSITION PPS205. REPAIRED PER ATS ER 09-1052 DA TED 12JAN09 AND UPS EO 757-7810-31855A. 2 L 7 2 4F RT A2NM 20090123 NM 2009 1 23 USAA2009012190105 1 20081227 A 5754 WEDGE BOEING 737 7374B7 138449C NM LE SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - NR 2 SLAT DELAMINATED AT THE INBOARD END OF THE TRAILING EDGE WEDGE UPPER SURFACE. REPAIRED N R 2 SLAT AT THE INBOARD END OF THE TRAILING EDGE WEDGE UPPER SURFACE IAW B737 SRM 51-70-10. 2 L 7 2 4F RT A16WE 20090123 NM 2009 1 23 USAA2009012190113 1 20081227 A 5311 65465752 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - CRACK ON FRAME AT BS 380 BETWEEN S8R & S9R. REPAIRED FRAME AT BS 380 BETWEEN S8R & S9R IAW U S AIRWAYS TASK CARD M1C53002. 2 L 7 2 4F RT A16WE 20090126 NM 2009 1 26 USAA2009012190106 1 20081229 A 5753 6546435340 SKIN BOEING 737 7373G7 138447J NM TE FLAP DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - DELAMINATION ON UPPER SKIN OF RIGHT OUTBOARD AFT FLAP WBL 350 TO WBL 368. REPAIRED UPPER SKI N OF RIGHT OUTBOARD AFT FLAP WBL 350 TO WBL 36 IAW B737 SRM 51-70-10. 2 L 7 2 4F RT A16WE 20090126 NM 2009 1 26 DLM88081808 1 20081210 A 5523 TAB DOUG MD88 MD88 3023688 NM LT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 974DL 53242 CRACK ON OTBD END T/E SKIN OF LT ELEVATOR GEARED TAB. THIS NRC WAS ACCOMPLISHED IAW OPN 1031 CARD 1254-1262 AND SRM 55- 04D PAR 3A. THIS REPAIR WAS IDENTIFIED IAW PS 900-5-1 NR 4. WEIGHT AND BALANCE IN LIMITS IAW SRM 55-20-2D. 2 L 7 2 4F RT A6WE 20090126 NM 2009 1 26 DL757081810 1 20081229 A 5320 146N5391U24 SILL BOEING 757 757232 1384965 NM BS 1380-1440 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 AFT CARGO COMP BETWEEN BS 1380 TO 1440 RBL 21 HAS THE LOWER SILL OF NR 2 CARGO DOOR WITH SEVERAL CORRODED AREAS AT UPPER SURFACE, CP53-156-021/COMPLIED WITH AT SAA, SAT ON NON ROUTINE 81719980001. 2 L 7 2 4F RT A2NM 20090126 NM 2009 1 26 DL76G081812 1 20081229 A 5343 141T992124 TRUNNION BOEING 767 767332 1382001 NM NLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1602 29694 FOUND RT NLG TRUNNION FITTING WITH LOOSE BUSHING AND CORRODED IN BRE. OVERESIZED BORE AND INSTALLED OVERSIZED BUSHING. 2 L 7 2 4F RT A1NM 20090126 NM 2009 1 26 USAA2009012190103 1 20081224 A 5320 6546812 INTERCOSTAL BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19- MAJOR REPAIR - GALVANIC CORROSION ON INTERCOSTAL BETWEEN BS 967 TO BS 986.3, LBL 18. REPLACED INTERCOSTAL BE TWEEN BS 967 TO BS 986.3, LBL 18 IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20090126 EA 2009 1 26 SWIA200820866 1 20081211 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 494CA 7765 C-CHECK, OUTBOARD ATTACH CLIP AT FS280 LBL9 CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090126 EA 2009 1 26 SWIA200820867 1 20081211 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 621 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 494CA 7765 C-CHECK, RIGHT OUTBOARD FLOOR SUPPORT ANGLE AT FS 621 CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090126 WP 2009 1 26 NWAA085739863 1 20081224 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 772NC 47774 DURING LINE CHECK, MX FOUND THAT THE EMERGENCY ESCAPE PATH LIGHTS FOR THE TAIL COMPARTMENT WERE INOPERATIVE. MX REPLACE D THE TAIL COMPARTMENT BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (K) 2 L 7 2 4F RT A6WE 20090126 NM 2009 1 26 FDEA200807293130 1 20080729 A 3260 859803 PROXIMITY SWITCH DOUG MD11 MD11F 3023600 NM RT MLG FAILED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 CE 21 598FE 49139 49139 48597 PDIS: AFTER T/O DEL, RT MAIN GEAR UNSAFE INDICATION AFTER RETRACTION ON BOTH PRIMARY AND SECONDARY. CYCLE GEAR PER CK L IST, NO HELP. FELT VIBRATION AT 230KTS WHILE WORKING CK LIST AFTER APPROX 10 MIN VIBRATION STOPPED, INDICATION WENT TO SAFE, LIGHT OUT. CHECK ADJ OF RT MLG UPLATCH. RT MLG DOOR LINK AND BRACKET ASSY PER MM FOUND ON THE LIMITS. ADJUSTMEN T MADE AS PRECAUTIONARY MEASURE ONE NOTCH O/B. WIRING, CONNECTORS CHECKED ALL FOUND NORMAL. PSEU FAIL TEST 31-71-04-00 ITEM 4. TEST FAIL. REMOVED AND REPLACED PSEU PER MM 31-71-01, ALL TEST PASS. RETURN TO SERVICE. 2 L 7 3 4F RT A22WE 20090126 NM 2009 1 26 DL76G090001 1 20081231 A 2750 FLAP SYSTEM BOEING 767 767332 1382001 NM TE FLAPS MALFUNCTIONED A DALA O OTHER O OTHER DE DESCENT 1 SO 27 171DZ 29690 TRAILING EDGE FLAP DISAGREE EICAS AFTER MOVING FLAP LEVER FROM 1 T0 5 POSITION. ALT FLAP POWER C/B FOUND POPPED OUT AND RESET. FLAP SLAT ELEC UNIT BITE TEST C/OUT WITH NO FINDINGS. OPS TEST FLAPS MANY TIMES. NO FINDINGS. 2 L 7 2 4F RT A1NM 20090126 NM 2009 1 26 UALA2008111303520 1 20080623 A 2760 10613378 VALVE BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU SPOILER INTERLOC STUCK A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 364UA 24533 LOSS OF AIR MODE INFLIGHT. RTFL. *S/D* FOUND LANDING GEAR SAFETY SWITCH TELEFLEX CABLE CLEVIS BOLT LOOSE AND CABLE GU IDE BENT AT RT MLG CONNECTION. DISCONNECTED TELEFLEX CABLE AT GEAR AND CABLE IS EXTREMELY HARD TO OPERATE MANUALLY, FE ELS LIKE IT IS BIRDCAGED OR DAMAGED INTERNALLY. CABLE STICKS IN GROUND POSITION AND IS VERY HARD TO ACTUATE. TELEFLEX REQUIRES REPLACEMENT. REMOVED TELEFLEX CABLE. REMOVED GND SPOILER INTERLOCK VALVE. REPLACED CABLE & GROUND SPEED INTE RLOCK VALVE CONTROL ASSY. 2 L 7 2 4F 4 F RT A16WE E21EU 20090114 NM 2009 1 14 DHLA2009770AT506 1 20081212 A 5320 WEB BOEING 727 7272B7 138407L NM NLG WW DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 770AT 21953 LOWER FUSELAGE NOSE W/W WEB DENTED AT BS 323 WL 181 BL 0. REPAIRED NOSE W/W WEB FROM BS 320 TO BS 325.5 BETWEEN LBL4 AN D RBL 5 IAW B727 SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 20090115 EA 2009 1 15 SWIA200820817 1 20081217 A 5312 BULKHEAD CNDAIR CL600 CL6002D24 1390016 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 803SK 15062 DURING C-CHECK, RIGHT LOWER FS 280 BULKHEAD WEB CORRODED AT RBL11. REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20090116 NM 2009 1 16 AALA200802622A 1 20081201 A 2780 FSEU BOEING 757 757223 1384957 NM ZONE 100 FAILED A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 685AA 25342 LAX INFLIGHT. CREW REPORTED LEADING EDGE SLAT DISAGREE INDICATION. EXECUTED A GO AROUND. LANDED LAX WITHOUT INCIDENT W ITH FLAPS AT 20 DEGREES. REPLACED NUMBER 2 FLAP SLAT ELECTRONICS UNIT. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20090116 WP 2009 1 16 AALA200802623A 1 20081202 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 972TW 53622 LGA EMERGENCY LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED BATTERY PACK IN FIRST CLASS OVERHEAD ELECTRONICS BAY FOR INO PERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A6WE 20090116 NM 2009 1 16 AALA200802624A 1 20081201 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHT MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 777AN 29585 DFW EMERGENCY LIGHT AT SEAT 22C MISSING LENS AND INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 22C. SYSTEM GROUND CHECK ED NORMAL OPS. 2 L 7 2 4F RT T00001SE 20090116 NM 2009 1 16 NWAA085806311 1 20081231 A 5320 WEB BOEING 747 747451 1384940 NM FUSELAGE MISMANUFACTURED A NWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 01 671US 26477 DURING L CHECK AND WHILE ACCOMPLISHING BOEING SB 747-53-2481 CREW REST MODIFICATION FOUND SHORT EDGE MARGIN AT 4 LOCATIO NS ON THE MOD WEB. 3 OF THE 4 LOCATIONS ARE COMMON TO THE WEB AND MOD STIFFENER. REPAIRED PER EA 63-214837. 2 L 7 4 4F RT A20WE 20090120 NM 2009 1 20 KCSA08085 1 20081218 A 2120 UNKNOWN BOEING 747 747132 1384882 NM COCKPIT ODOR A KCSA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 23 709CK 20247 ON DESCENT THROUGH 12.0 FT. CREW DETECTED A SMELL LIKE ELECTRICAL SMOKE ACCOMPANIED BY A HUMMING SOUND. SOUND APPEARED T O BE COMING FROM CAPT INSTRUMENT PANEL. AFTER SEVERAL SECONDS SOUND STOPPED AND SMELL DISSIPATED. PERFORMED DETAILED V ISUAL INSP OF COCKPIT FOR CAUSE OF ODOR. INSPECTED WIRING IAW SWPM 20-60-03. INSPECTED BEHIND PILOTS INSTRUMENT PANEL IA W MM 31-10-00. INSPECTED BEHIND F/E DESK IAW MM 24-58-00. RAN ENGINES IAW 71-00-00. ALL INSTRUMENTS AND GAUGES POWERED F OR APROX 2.5 HRS. NO ODORS NOTED OR SUSPECT CAUSE OF ODOR FOUND. 2 L 7 4 4F RT A20WE 20090120 NM 2009 1 20 JJBA200953036 1 20081112 A 5330 85320007 SKIN DHAV DHC8 DHC8202 2809007 NM FUSELAGE GOUGED A JBBA K NONE O OTHER IN INSP/MAINT 1 EA 01 351PH 490 DURING C-CHECK FOUND GOUGE IN FUSELAGE (JUST FWD OF STA X531.5 BETWEEN STRINGERS 21S AND 22S). REPAIRED IAW REPAIR DOCU MENT 08-53-08 REV.1, DAMAGE TOLERANCE ANALYSIS BY MFG WITHIN ONE YEAR. 2 H 7 2 4T RT A13NM 20090114 NM 2009 1 14 DHLA2009770AT504 1 20081218 A 5311 FRAME BOEING 727 7272B7 138407L NM FUSELAGE DENTED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 770AT 21953 UPPER FUSELAGE CARGO CABIN FRAME WITH DENT AT BS 520 BETWEEN S-16R AND S-17R. REPAIRED FUSELAGE FRAME SECTION AT BS 520 BTWN S-16R AND S-17R IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20090114 NM 2009 1 14 DHLA2009770AT505 1 20081211 A 5311 FRAME BOEING 727 7272B7 138407L NM FUSELAGE DAMAGED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 770AT 21953 UPPER FUSELAGE CARGO CABIN FRAME WITH DOUBLE HOLE AT BS 1090 BETWEEN S-16L AND S-17L. REPAIRED FUSELAGE FRAME SECTION A T BS 1090 BETWEEN S-16L AND S-17L IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20090114 NM 2009 1 14 AALA200802610A 1 20081129 A 3350 LENS BOEING 777 777223 1385213 NM EMERGENCY LIGHTS MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 759AN 32638 EMERGENCY LIGHT AT SEAT 26C MISSING LENS. REPLACED LENS AT SEAT 26C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT T00001SE 20090114 WP 2009 1 14 AALA200802611A 1 20081130 A 3222 SEAL DOUG DC9 DC983 3022083 WP NLG STRUT LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 9402W 53138 INFLIGHT CREW REPORTED NOSE LANDING GEAR RED INDICATION WITH AIR NOISE. SUSPECTED GEAR NOT FULLY RETRACTED. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR STRUT SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A6WE 20090114 WP 2009 1 14 AALA200802612A 1 20081130 A 3260 833704 PROXIMITY SENSOR DOUG DC9 DC982 3022082 WP LANDING GEAR FAILED A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 492AA 49730 INFLIGHT. CREW REPORTED GEAR UNSAFE INDICATION FOLLOWING GEAR EXTENSION. ACCOMPLISHED ALTERNALE GEAR EXTENSION PROCEDU RE. LANDED ABQ WITHOUT INCIDENT. REPLACED LEFT HAND MAIN LANDING GEAR PROXIMITY SENSOR. SYSTEM GROUND CHECKED NORMAL O PERATION. 2 L 7 2 4F A6WE 20090114 EU 2009 1 14 AALA200802613A 1 20081130 A 3397 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 3075A 606 EMERGENCY LIGHT NEAR LAVATORY INOPERATIVE. RESEATED CONNECTOR IN LAVATORY FOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NO RMAL OPERATION. 2 L 7 2 4F RT A35EU 20090114 NM 2009 1 14 AALA200802614A 1 20081130 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 682AA 25339 EMERGENCY LIGHT AT RIGHT HAND OVERWING INOPERATIVE. REPLACED LAMP FOR INOPERATIVE LIGHT AT RIGHT HAND OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20090114 NM 2009 1 14 AALA200802615A 1 20081130 A 3350 LENS BOEING 757 757223 1384957 NM EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 682AA 25339 EMERGENCY LIGHT EXIT IDENTIFER AT RIGHT NUMBER FOUR DOOR DAMAGED. REPLACED LENS FOR DAMAGED LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20090126 EU 2009 1 26 UALA2008111303887 2 20080714 A 7200 ENGINE BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU NR 1 LEAKING A UALA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 936UA 26667 724334 STRONG PUNGENT ODOR IN FLIGHT DECK. CAUSE: NR 1 ENGINE BOROSCOPE DISCOVERED OIL IN COMPRESSOR. OIL WETTING AND STREAK S AT STAGES 1, 2 AND 3 HPC BLADES AND VANES. REPLACED NR 1 ENGINE. 2 L 7 2 4F 4 F RT A16WE E21EU 20090128 NE 2009 1 28 DL777090004 2 20080102 A 7200 ENGINE BOEING 777 777232 1385232 NM RROYCE RB211 RB211TRENT89 NE NR 2 DAMAGED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 864DA 35206 051191 29736 051191 RTO FOR ENG EXCEEDENCE, ACFT QUARANTINED PENDING NTSB INVESTIGATION FOR POSSIBLE UNCONTAINED FAN SEPERATION NR 2 ENGINE REPLACED. 2 L 7 2 4F 4 F RT T00001SE E00050EN 20090128 2009 1 28 DL76G081794 4 20081222 A 3442 343002067 TRANSCEIVER BOEING 767 767332 1382001 NM WX RADAR SYS MALFUNCTIONED A DALA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 SO 27 16065 30199 WX RADAR FAILED IN FLIGHT. WOULD NOT WORK IN ANY MODE APPROX 1 HOUR LATER WORKED NORMAL IN ALL MODES. REPLACED WEATHER RADAR TRANSCEIVER AND INDICATOR PER AMM 34-43-01-004-001 AND 34-43-06-002-005 RESPECTIVELY. PERFORMED OPERATIONAL AND SYSTEM TEST. ALL PASSED GOOD. 2 L 7 2 4F RT A1NM 20090128 NM 2009 1 28 DL757081796 1 20081227 A 3520 11700314 O2 GENERATOR BOEING 757 757232 1384965 NM CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 FOUND ONE BLOWN OXYGEN CHEMICAL GENERATOR SN ARYD-F010-510 ON INSPECTION OF OXYGEN GENERATORS. COMPLIED WITH AT SAA- SA T ON N/R 81698450001 AND N/R 81707610001. 2 L 7 2 4F RT A2NM 20090128 NM 2009 1 28 DL757081797 1 20081227 A 5347 SEAT TRACK BOEING 757 757232 1384965 NM BS 1435 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 CABIN COMPT FLOOR SEAT TRACK FOUND WITH CORROSION ON TOP SURFACE INBOARD FLANGE AT BS 1435 LBL 48 AS MARKEDW/L08-10. CO MPLIED WITH AT SAA- SAT ON NON ROUTINE 81720150001. 2 L 7 2 4F RT A2NM 20090128 EU 2009 1 28 M7KA1110084173 1 20081117 A 5320 LATCH UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENG BAY DOOR LOOSE E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 824MH 1678 4173 23209 DURING ROUTINE INSPECTION LATCH APPEARED LOOSE AND CLOSER INSPECTION REVEALED LOCKING LATCH HINGE PINS SOCKETS AND HOOK CATCH WORN EXCESSIVELY. INSTALLED NEW LATCHES AS REQUIRED. 1 G 7 2 3U 3 U H9EU E00054EN 20090128 EU 2009 1 28 M7KA1109084125 1 20081117 A 5344 350A58004523 HINGE UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENG BAY DOOR CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 846MH 295 4248 23292 HINGE ATTACHMENT BORE HAD A 1` LONG CRACK RADIATING. 1 G 7 2 3U 3 U H9EU E00054EN 20090123 NM 2009 1 23 USAA2009012190112 1 20081226 A 5320 6547957 COVER BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - CORROSION ON COVER SHEET BETWEEN BS 767 TO BS 787, S26R. REPLACED COVER SHEET BETWEEN BS 767 TO BS 787, S26R IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20090126 2009 1 26 DL75E081813 4 20081229 A 3417 4040800912 ADC BOEING 757 7572Q8 1384972 NM RIGHT INOPERATIVE A DALA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 SO 27 706TW 28165 AIR TURN BACK, AFTER TAKEOFF MACH SPEED TRIM AND RUDDER RATIO EICAS MSG F/O AIRSPEED IND VERY SLOW TO INCREASE ABOVE 100 KTS, LAGGED BEHIND CAPT AIRSPEED INDICATOR BY 30+ KNOTS. REMOVED AND REPLACED RT ADC AND FCC IAW MM. 2 L 7 2 4F RT A2NM 20090126 EA 2009 1 26 SWIA200820872 1 20081220 A 5310 WINDOW POST CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 869AS 7479 C-CHECK, RIGHT WINDSHIELD SIDE POST OUTBOARD CLIP CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20090126 NE 2009 1 26 NWAA085719935 2 20081223 A 7200 JT8D9 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE NR 2 STALLED A NWAA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 01 1332U 47404 49412 DURING TAKEOFF, ENGINE NR 2 EXPERIENCED MULTIPLE COMPRESSOR STALLS. TAKEOFF ABORTED AT 120 KNOTS. MX PERFORMED POST STA LL INSPECTIONS. NTF. ENGINE NR 2 GROUND RUN TO TAKEOFF POWER WITH NO STALL OR SURGE. (K) 2 L 7 2 4F 4 F A6WE E2EA 20090126 EA 2009 1 26 SWIA200820874 1 20081220 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 869AS 7479 C-CHECK, 4 CLIPS AT RBL9 AND LBL9 FS280 CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090126 EA 2009 1 26 SWIA200820875 1 20081220 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 473 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 869AS 7479 DURING C-CHECK, LEFT FLOOR SUPPORT INTERCOSTAL AT FS 473 ATTACH BRACKET CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090126 EA 2009 1 26 SWIA200820876 1 20081220 A 5320 FLOOR SUPPORT CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 869AS 7479 C-CHECK, RIGHT FLOOR SUPPORT INTERCOSTAL AT FS484, INBOARD BRACKET TO FLOOR BEAM RBL27 CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20090126 EA 2009 1 26 SWIA200820877 1 20081229 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 863AS 7487 DURING C-CHECK, FS 280 FLOORBEAM LBL9 UPPER FLANGE CRACKED. REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20090126 NM 2009 1 26 NWAA09125655 1 20081213 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM EMERGENCY LIGHTS DEFECTIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 555NW 33391 DURING AN OVERNIGHT LINE CHECK THE EMERGENCY ESCAPE PATH LIGHTING IN ROWS 1 THROUGH 4 WERE INOPERATIVE ALONG WITH THE EM ERGENCY LIGHTS ON THE FWD CLOSET. MX FOUND POWER SUPPLY M732 TO BE DEFECTIVE AND REPLACED IT. SYS OPERATION WAS NORMAL AFTER THE POWER SUPPLY WAS REPLACED. (K) 2 L 7 2 4F RT A2NM 20090126 NM 2009 1 26 DL757081785 1 20081223 A 5330 SKIN BOEING 757 757232 1384965 NM BS 600-640 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 LT FUSELAGE SKIN AT STA 600-640 BETWEEN S 16L TO 18L HAS SEVERAL DENTS AS MARKED. REPAIRED PER ERA 471873-14 REV O. 2 L 7 2 4F RT A2NM 20090126 NM 2009 1 26 DL757081787 1 20081223 A 5330 SKIN BOEING 757 757232 1384965 NM BS 420 S22R GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 PERM REPAIR ON ERA 384204-14 STA 420 BELOW STR 22R. REPAIR PER ERA. 2 L 7 2 4F RT A2NM 20090126 NM 2009 1 26 DL757081790 1 20081224 A 4910 353N40141 BELLMOUTH BOEING 757 757232 1384965 NM APU INLET CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 DURING HMV, CRACKS WERE FOUND IN THE APU AIR INTAKE PLENUM BELLMOUTH. THE CRACKING WAS ADDRESSED IN BOEING SERVICE BULL ETIN 757-49-0011 AND THE CRACKED BELLMOUTH WAS REPLACED WITH A MODIFIED BELLMOUTH ASSEMBLY AS DIRECTED BY THE SERVICE BU LLETIN. 2 L 7 2 4F RT A2NM 20090126 NM 2009 1 26 DLM88081791 1 20081224 A 3260 DOWNLOCK SENSOR DOUG MD88 MD88 3023688 NM RT MLG MALFUNCTIONED A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 943DL 49816 RIGHT MAIN GEAR UNSAFE LIGHT ALONG WITH LANDING GEAR AURAL WARNING. REPLACED RT DOWNLOCK PROX SENSOR-CONDUIT AND CONNEC TOR PROX TEST NOW GOOD. 2 L 7 2 4F RT A6WE 20090126 NM 2009 1 26 UALA2008111302447 1 20080426 A 2120 UNKNOWN BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 902UA 25002 CREW REPORTS FAINT ELECTRICAL BURNING SMELL FROM FORWARD CABIN NEAR DOOR 1 POSSIBLY FROM FWD CABIN SPEAKER, CAPT ADVISED TO OPEN THE PA AMP CB P6-1 D5 IF NECESSARY TO REMOVE POWER FROM THE CABIN SPEAKERS AND WILL LOSE THE CHIME SYS IF IT'S PULLED. F/A REPORTS SLIGHT SMELL OF BURNING OIL ONLY IN FWD GALLEY AREA. SMELL OCCURS EVERY FEW MINUTE INOPED FWD GALL EY COFFEEMAKER. RESET C/B BREWED TWO POTS OF COFFEE AND LEFT ON FOR TWO HOURS AND CHECKED FOR SMELL, NONE NOTED. 2 L 7 2 4F 4 F RT A16WE E21EU 20090128 EU 2009 1 28 M7KA1017084173 1 20081117 A 5350 ASNA2154C02 LATCH UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENG BAY DOOR WORN E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 824MH 4173 23209 DURING ROUTINE INSP, LATCH APPEARED LOOSE AND CLOSER INSPECTION REVEALED LOCKING LATCH HINGE PINS SOCKETS AND HOOK CATCH WORN EXCESSIVELY. INSTALLED NEW LATCHES AS REQUIRED. 1 G 7 2 3U 3 U H9EU E00054EN 20090128 NM 2009 1 28 ASAA0944234 1 20081230 A 5541 65C2584151 SPAR BOEING 737 737490 1384715 NM RUDDER DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 708AS 28895 RUDDER LE SPAR DELAMINATED. REPAIRED RUDDER LE SPAR. 2 L 7 2 4F RT A16WE 20090126 EA 2009 1 26 SWIA200820831 1 20081216 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 DURING C-CHECK, UPPER RIGHT FS 625 CLIP CRACKED ON PRESSURE BULKHEAD. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20090126 EA 2009 1 26 SWIA200820832 1 20081216 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 C-CHECK, UPPER LEFT FS 625 CLIP CRACKED ON PRESSURE BULKHEAD. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20090126 EA 2009 1 26 SWIA200820833 1 20081216 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 446SW 7666 C-CHECK, FS 280 INBOARD AND OUTBOARD CLIPS CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20090128 NM 2009 1 28 DL757081795 1 20081227 A 5311 FAILSAFE BOEING 757 757232 1384965 NM BS 900 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 FAIL/SAFE STRAP CORRODED AT STA 900 SKIN BUTT JOINT BELOW WINDOW BELT RT SIDE OF FUSELAGE. COMPLIED WITH AT SAA SAT ON NON ROUTINE 81716550001. 2 L 7 2 4F RT A2NM 20090128 NM 2009 1 28 USAA2009012190104 1 20081227 A 5320 6553594501 SEAL BOEING 737 7374B7 138449C NM ZONE 200 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - CRACK AT FORWARD SERVICE DOOR RAMP SEAL AT UPPER FORWARD CORNER. REPAIRED FORWARD SERVICE DOO R RAMP SEAL AT UPPER FORWARD CORNER IAW B737 SRM 53-10-15. 2 L 7 2 4F RT A16WE 20090129 SO 2009 1 29 SWIA200820899 1 20081025 A 5330 SHEAR TIE EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 229SW 120305 C-CHECK, FRAME 32 CENTER BELLY OF AIRCRAFT HAS ONE SKIN SUPPORT CORRODED. REPLACED SUPPORT PER SRM. 2 L 7 2 4T RT A31SO 20090129 SO 2009 1 29 SWIA200820901 1 20081020 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 229SW 120305 C-CHECK, RIGHT SIDE FLOOR SEAT TRACK MOST FORWARD SECTION CORRODED AND FLAKING UP. REPLACED PER EMB EST-186/96. 2 L 7 2 4T RT A31SO 20090129 NM 2009 1 29 C8GA20080083A 1 20081029 A 5320 7075T6 INTERCOSTAL BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE ZONE 100 CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 62202 22470 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS SURFACE CORROSION WAS NOTED ON INTERCOSTAL BS 695 STR 27R. DAMAGED IN TERCOSTAL WAS REMOVED, A NEW INTERCOSTAL WAS FABRICATED. INSTALLED REPAIR IAW SRM 53-10-2 AND 51-10-3. NO OTHER DEFECT S NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 20090129 NM 2009 1 29 DHLA2009743552 1 20081129 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 BS 825 MAIN FRAME HAS DOUBLE DRILLED HOLES BETWEEN STR 3L AND 5L. ACCOMPLISHED FRAME REPAIR IAW SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 20090129 NM 2009 1 29 DHLA2009743546 1 20081126 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 BS 1110 FRAME HAS DOUBLE DRILLED HOLES BETWEEN STR 4L AND 5L. ACCOMPLISHED FRAME REPAIR AS REQUIRED PER B727 SRM 51-40- 3 FIG 1. 2 L 7 3 4F A3WE 20090129 NM 2009 1 29 DHLA2009743547 1 20081125 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 BS 400 FRAME HAS DOUBLE DRILLED HOLES BETWEEN STR 2L AND 3L. ACCOMPLISHED FRAME REPAIR AS REQUIRED PER B727 SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 20090129 NM 2009 1 29 DHLA2009743548 1 20081222 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 100 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 BS 1030 FRAME DENTED AT STR 26L. ACCOMPLISHED FRAME REPAIR AS REQUIRED PER B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20090129 NM 2009 1 29 DHLA2009743549 1 20081125 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 BS 848 FRAME HAS DOUBLE DRILLED AND ELONGATED HOLES BETWEEN STR 2L AND 5L. ACCOMPLISHED FRAME REPAIR AS REQUIRED PER B7 27 SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 20090129 NM 2009 1 29 DHLA2009743550 1 20081123 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 100 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 BS 1170 FRAME HAS DOUBLE DRILLED HOLES ON INBD FLANGE BETWEEN STR 16L AND 17L. ACCOMPLISHED FRAME REPAIR AS REQUIRED PE R B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20090129 NM 2009 1 29 DHLA2009770AT528 1 20081208 A 5531 FRAME BOEING 727 7272B7 138407L NM ZONE 300 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 770AT 21953 EMPENNAGE VERTICAL STABILIZER ACTUATOR LT ACCESS PANEL FRAME "T" SHAPE SUPPORT WORN AND LOOSE. REPAIRED VERTICAL STABIL IZER MID SPAR CHORD SECTION FROM FIN STA 222 TO FIN STA 241 IAW COOPESA EO COO-2-55-499-08 DTD 12/22/08 DOCUMENTED ON FA A FORM 8110-3. 2 L 7 3 4F A3WE 20090129 NM 2009 1 29 DHLA2009770AT529 1 20081208 A 5311 FRAME BOEING 727 7272B7 138407L NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 770AT 21953 LOWER FUSELAGE AT BS 740 BTWN S-27L AND S-28L FRAME WITH CORROSION. REPLACED FUSELAGE CHORD SECTION AT BS 740 BTWN S-27 L AND S-28L IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20090129 NM 2009 1 29 DHLA2009743540 1 20081126 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 BS 720 FRAME HAS DOUBLE DRILLED HOLES BETWEEN STR 16L AND 17L. ACCOMPLISHED FRAME REPAIR AS REQ PER SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20090129 SO 2009 1 29 SWIA200820904 1 20081020 A 5310 BUTTSTRAP EMB 120 EMB120ER 3260203 SO CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 229SW 120305 C-CHECK, BUTT STRAPS BETWEEN LAV AND GALLEY CORRODED. REPLACED PER SRM. 2 L 7 2 4T RT A31SO 20090130 NM 2009 1 30 UPS09654286 1 20081228 A 5315 140T013038 FLOORBEAM BOEING 767 76734AF 1385212 NM BS 1087 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE: C, AFT CARGO COMPT BS 1087 RBL 26 INCHES BELOW FLOOR ANGLE SUPPORT FOUND CRACK. AFT CARGO COMPT BS 108 7 RBL 26 INCHES BELOW FLOOR SUPPORT ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20090130 WP 2009 1 30 UPS09854259 1 20081219 A 5520 ATTACH ANGLE DOUG DC8 DC873F 302199F WP LT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE: SV LT ELEVATOR STA 200.238 DOUBLER ATTACHED ANGLE IS CRACKED AND DENTED, REPAIRED IAW DWG 5700911 AND S RM 51-01-21. 2 L 7 4 4F RT 4A25 20090130 NM 2009 1 30 FDEA200804121389 1 20080412 A 2611 1226M255481830 SMOKE DETECTOR DOUG MD10 MD1030F 3024020 NM FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 21 311FE 5548 5548 46871 CABIN SMOKE WARNING, TWO TIMES. FIRST TIME IN CLIMB PASSING FL310. BRIEF FLASH OF MASTER WARNING THEN WENT AWAY, 4-5 M IN LATER LEVEL AT FL330 GOT 2ND MASTER WARNING AND CABIN SMOKE FOR ABOUT 10 SECS. LANDED AT KPDX. FIRE DEPARTMENT INSP ECTION NO INDICATION OF HEAT. PER MX TURNOVER CREW REPORTED AREA 2 OF UPPER DECK WAS AREA CAUSING INPUT DURING FLIGHT. REMOVED AND REPLACED ALL NR 2 AREA DETECTOR UNITS PER MM 26-15-00. REMOVED AND REPLACED MSC PER MM 26-15-00. ALL OPS CKS C/W SYSTEM CKS NORMAL. ALSO CHECKED EACH VIA IN COMMAND MODE PER MM 26-15-01. OPS CK NORMAL. 2 L 7 3 4F RT A22WE 20090128 EU 2009 1 28 M7KA1026083949 1 20081117 A 6220 704A33640088 FREQ ADAPTER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE MAIN ROTOR HUB CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 810MH 1749 3949 23318 DURING ROUTINE INSPECTION 1 OF 3 FREQUENCY ADAPTERS FOUND TO HAVE A CRACK IN THE ELASTOMER NEARING ITS MAXIMUM ALLOWABLE LIMITATION OF 10MM. A NEW KIT OF 3 MATCHED ADAPTERS WERE INSTALLED. 1 G 7 2 3U 3 U H9EU E00054EN 20090129 NM 2009 1 29 DHLA2009743551 1 20081125 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 200 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 BS 680 MAIN FRAME DENTED/DOUBLE DRILLED HOLES BETWEEN STR 13L AND 17L. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3 F IG 1. 2 L 7 3 4F A3WE 20090130 WP 2009 1 30 FDEA200805011723 1 20080501 A 2150 350082 CONTROLLER DOUG MD10 MD1010F 3022112 WP A/C PACK FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 21 568FE 47827 FL 370 LEVEL 1 AIR SYS 2 FAIL. AIR SYS AUTO CONTROLLER SHUTDOWN NR 2 AIR SYSTEM 2 MINUTES LATER. LEVEL 3 AIR SYS FAIL FOLLOWED QRH. LAND AT NEAREST SUITABLE EVENTUALLY 10 MINUTES LATER APPROX AIR SYS 2 INDICATED NORMAL. SYSTEM DECAY CH ECK PER MD10 AMM 36-00-01-5 AND ALL PARAMETERS WERE WITHIN LIMITS. CHECKED NR 2 PACK BAY, FWD, CTR AND CAC COMPTS FOR LEAKS AND NONE FOUND. REMOVED AND REPLACED MANIFOLD FAILURE DETECTION CONTROLLER AS PRECAUTIONARY PER MD10 AMM 36-23-01 -4 AND SYSTEM CHECKS GOOD. RAN NR 2 ENG AT IDLE AND OP`S CHECK THE NR 2 PNEUMATIC SYSTEM AND NO DEFECTS NOTED PER MD10 FDX JRH. OK TO CONTINUE. 2 L 7 3 4F RT A22WE 20090130 WP 2009 1 30 FDEA200804271738 1 20080427 A 2150 9273184 TRANSMITTER DOUG MD10 MD1010F 3022112 WP A/C PACK FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 21 384FE 13958 3595 46617 RECEIVED A LEVEL 1 PACK 2 FLOW DISAG ALERT IN FLIGHT 6 TIMES. REMOVED AND REPLACED PACK 2 FLOW CONT VLV, REF MD10 MM 2 1-51-02-4. REMOVED AND REPLACED PACK 2 FLOW XMITER, REF MM 21-52-01-4. OPS AND LK CK OK. 2 L 7 3 4F RT A22WE 20090130 NM 2009 1 30 UPS09M54254 1 20081231 A 3260 PROXIMITY SWITCH DOUG MD11 MD11F 3023600 NM RT MLG BROKEN A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 292UP RT MLG WILL NOT RETRACT AFTER TAKEOFF ACFT FERRIED FOR REPAIR. D391954 RT MLG PROX SWITCH BROKEN. PROX SWITCH REPLACE D, MLG SWING C/W. ALL OPS NORMAL, THIS CLEARS D391954. 2 L 7 3 4F RT A22WE 20090130 EU 2009 1 30 FDEA200807152906 1 20080715 A 2913 571191 PUMP AIRBUS 310 A310222 3930315 EU HYD SYSTEM LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 21 450FE 3484 3484 162 WHILE EN ROUTE AT FL370 GOT ECAM WARNING FOR GREEN HYD RESV LOW. RESV QUANTITY ECAM WAS IN THE RED. PRESSURE INDICATED ZERO. DIVERTED TO KPHX. GEAR EXTENDED BY GRAVITY. REMOVED AND REPLACED GREEN YELLOW POWER TRANSFER UNIT PER MM 29-23 -11-4. REQUIRES BLEEDING, OPS AND LK CHECK PER STEP D.10. REMOVED AND REPLACED NR 1 ENG GREEN SYSTEM HYDRAULIC PUMP PE R M/M 29-11-32-4 AND PUMP CASE DRAIN FILTER PER M/M 29-11-36-4 LEAK AND OP'S CHECK GOOD. 2 L 7 2 4F RT A35EU 20090130 EU 2009 1 30 FDEA200808263602 1 20080826 A 2780 516A000002 LIMITER AIRBUS 310 A310324 3930206 EU SLAT TORQUE FAILED A FDEA L ABORTED APPROACH S AFFECT SYSTEMS AP APPROACH 1 CE 21 805FD 3783 3783 456 DURING APPROACH WITH LANDING GEAR DOWN AND FLAPS 20/20, F/O GOT UNRELIABLE AIRSPEED ON PFD FOLLOWED BY SLATS/FLAPS SYS 1 AND 2 FAULT O/H. SLATS/FLAPS CYCLED PER QRH, THE LIGHT/FAULTS CLEARED CONFIGURED AGAIN THE SLATS STUCK AT 15 DEGREES . FOLLOWED QRH FOR SLATS STUCK LANDING. ON FINAL AP FLAP HANDLE AT 40 DEGREES SLATS BROKE FREE AND WENT TO 30 DEGREES SLATS WITH 40 DEG FLAPS. THE LANDING WAS UNEVENTFUL. SLAT/FLAP RETRACT ON THE GND WAS NORMAL. CKD SLAT 0 POSITION AND INDEX OF LT APPU, W/W IPPU AND FPPU, CHK OK. REMOVED AND REPLACED RT APPU ALL AMM 27-81-19-4. REMOVED AND REPLACED RT SLAT TORQUE LIMITER PER AMM 27-84-12-4 OPS CHK NORMAL PER AMM 27-84-00-5 OFF MFG 516A0000-02, SRL K1142, ON MFG 516A000 2 L 7 2 4F RT A35EU 20090130 EU 2009 1 30 FDEA200809063752 1 20080906 A 3244 Z3200203 TIRE AIRBUS 310 A310324 3930206 EU MLG FAILED A FDEA O OTHER O OTHER TO TAKEOFF 1 CE 21 801FD 539 ON DEPT TLV, ATC ADVISED COMPANY THAT RUBBER WAS FOUND ON RWY AFTER TAKEOFF. FRA CONFIRMED THAT A STARBOARD SIDE WAS DA MAGED. FOUND NR 8 TIRE LOST COMPLETE REINFORCED PLY, NO DAMAGE ON FLAPS OR GEAR FOUND. REMOVED AND REPLACED NR 7 TIRE FOR OVERLOAD. 2 L 7 2 4F RT A35EU 20090130 NM 2009 1 30 FDEA200809073757 1 20080907 A 3200 UNKNOWN DOUG MD11 MD11F 3023600 NM MLG UNKNOWN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 598FE 48597 AFTER TAKEOFF R MAIN GEAR SHOWED UNSAFE RAN LIST RECYCLED GEAR NO HELP, INCREASE SPEED AFTER FLAP RETRACT AND AT 225 LIG HT WENT OUT. 2 L 7 3 4F RT A22WE 20090130 NM 2009 1 30 ASAA0944308 1 20081231 A 5311 65C229103 FAILSAFE BOEING 737 7374Q8 138447Q NM BS 500G CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 FAIL SAFE ANGLE HAS CORROSION AT STR 28R. REMOVED CORRODED FAIL SAFE ANGLE IAW SRM 51-40-02 FIG 8. INSTALLED NEW FAIL SAFE ANGLE IAW B737 400 SRM 51 40 02. 2 L 7 2 4F RT A16WE 20090202 NM 2009 2 2 UPS09M54412 1 20081230 A 5754 ARB2886503 DOUBLER DOUG MD11 MD11F 3023600 NM LE SLAT GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:N/A REPAIR SURVEY SEQUENCE NUMBER 289-W3-04 GOUGE FOUND AT THE CENTER OF THE REPAIR DOUBLER ON LT WING I NBOARD LEADING EDGE STA XOS 455-567. REMOVED DOUBLER, REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW U PS EO MD11-5750-31916-B. 2 L 7 3 4F RT A22WE 20090203 NM 2009 2 3 UALA2008111304043 1 20080730 A 2133 VALVE AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN PRESSURE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 827UA 1022 VENT SKIN VALVE FAULT. RTFL. ALTHOUGH NO LONGER CHRONIC, THIS APPEARS TO BE AN ISOLATED EVENT RELATED TO THE VALVE FAI LURE. 2 L 7 2 4F 4 F RT A28NM E40NE 20090203 WP 2009 2 3 FDEA200810294607 1 20081029 A 3234 HANDLE DOUG DC10 DC1030F 3023504 WP MLG STUCK A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CE 21 310FE 48299 ON DEPARTURE FROM MEM GEAR HANDLE WOULD NOT MOVE TO UP POSITION RAN QRH PROCEDURE FOR GEAR HANDLE, WILL NOT MOVE TO UP P OSITION UNABLE TO RAISE GEAR HANDLE RETURNED TO MEM. 2 L 7 3 4F RT A22WE 20090202 NM 2009 2 2 FDEA200809163906 1 20080916 A 7830 W460FIA RELAY BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE MALFUNCTIONED A FDEA L ABORTED APPROACH J WARNING INDICATION CR CRUISE 1 CE 21 903FD 30545 30545 27124 30898 L REV AMBER LIGHT ON RAN QRH NO YAW OR ADVERSE CONDITIONS. ACFT RELEASED FOR SERVICE PER MEL/CDL: 78-36-01 CATEGORY: C EXPIRATION: 26SEP08 MEL 78-36-01: LEFT ENGINE REVERSER UNLOCK INDICATION INOP. REVERSER DEACTIVATED IN FORWARD THRUST POSITION. "A/C CAT IIIA" C/0374246. REMOVED AND REPLACED RELAYS K26 AND K10108, REF WRI 78-30/0496. 2 L 7 2 4F 4 F RT A2NM E12EU 20090203 NM 2009 2 3 ASAA0944259 1 20081231 A 5210 6552870503 FITTING BOEING 737 7374Q8 138447Q NM R2 DOOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 774AS 25107 R2 DOOR CORROSION ON DOOR SURROUND FWD LIP FROM UPPER LATCH FITTING TOO UPPER HINGE. R2 PRESSURE SEAL LANDING AT DOOR C UTOUT. R&R R2 DOOR FWD LIP UPPER LATCH FITTING IAW 737 400 SRM 51 40 02. ACCOMPLISHED DOORSILL LAND AREA BUILD UP RESE AL ON UPPER LATCH FITTING IAW EA 5210 01133. 2 L 7 2 4F RT A16WE 20090203 EA 2009 2 3 SWIA200820909 1 20081231 A 5315 FLOORBEAM CNDAIR CL600 CL6002D24 1390016 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 805SK 15069 DURING C-CHECK, RIGHT SIDE FLOORBEAM FORWARD OF FS 280 CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090203 SO 2009 2 3 SWIA200820914 1 20081117 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO CORRODED CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 567SW 120342 DURING C-CHECK, LEFT SIDE FLOOR CROSS MEMBER AT FRAME 39 CORRODED. REPLACED PER SRM. 2 L 7 2 4T RT A31SO 20090203 SO 2009 2 3 SWIA200820915 1 20081028 A 5712 RIB EMB 120 EMB120ER 3260203 SO LT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 569SW 120344 C-CHECK, LEFT OUTBOARD WING OUTBOARD OF NACELLE, RIB NR 16 LOWER CLIP CRACKED. REPLACED PER SRM. 2 L 7 2 4T RT A31SO 20090203 SO 2009 2 3 SWIA200820916 1 20081028 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 569SW 120344 C-CHECK, RIGHT INBOARD WING OUTBOARD PANEL STRINGER NR 8 CRACKED. REPAIRED PER SRM. 2 L 7 2 4T RT A31SO 20090203 SO 2009 2 3 SWIA200820917 1 20081030 A 5311 FRAME EMB 120 EMB120ER 3260203 SO CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 569SW 120344 C-CHECK, CABIN FRAME AFT TOP SIDE OF GASPER IS CRACKED. REPAIRED PER SRM. 2 L 7 2 4T RT A31SO 20090204 NM 2009 2 4 HNAA2009012500021 1 20080812 A 5347 85330469001 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 931HA 51108 51108 132 SEVERAL SPOT OF MINOR CORROSION FOUND ON RT INBD SEAT TRACK FROM STA X259 TO 597. R&R SEAT TRACK IAW STRUCTURAL REPAIR MANUAL 51-40-00. 2 H 7 2 4T RT A13NM 20090204 EA 2009 2 4 HNAA2009012300014 1 20081022 A 5330 85322487115 SKIN DHAV DHC8 DHC8311 1386006 EA FUSELAGE DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 327EN 30034 30034 261 DURING 'C' CHECK INSPECTIONS, A REPAIR WITH NO DOCUMENTATION WAS FOUND ON THE FUSELAGE BELLY SKIN AT X210 TO X221 BETWEE N STRINGERS 29P TO 32P. DOCUMENTATION WAS FOUND FOR THIS REPAIR UNDER DHC RD8-53-10353. 2 H 7 2 4T RT A13NM 20090204 EA 2009 2 4 HNAA2009020100037 1 20081022 A 5330 85322487115 SKIN PANEL DHAV DHC8 DHC8311 1386006 EA FUSELAGE DENTED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 327EN 30034 261 2 PROTRUDING DENTS BETWEEN STATION X179-X199 STRINGER 29P-30P. REPAIRED DAMAGE IAW RD8-53-2181. 2 H 7 2 4T RT A13NM 20090204 NM 2009 2 4 HNAA2009012500019 1 20080909 A 5730 857110898007 PANEL DHAV DHC8 DHC8102 2809003 NM WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 984HA 33035 33035 377 STRESS PANEL 623 AT, 522AT, 521AT, 523AT CORROSION FOUND COUNTER SINK HOLES. STRESS PANEL 623AT, 523AT CORROSION REMOVED AND RETREATED 622AT,522 AT OUT OFF LIMITS. R&R PANEL. 512 AT NEED BUSHING INSTALLATION. 2 H 7 2 4T RT A13NM 20090204 NM 2009 2 4 HNAA2009012700031 1 20080902 A 5315 85320342113 FLOORBEAM DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 931HA 51109 51109 132 DURING 'C' CHECK INSPECTIONS, AN UNRECORDED REPAIR AND CORROSION WAS DISCOVERED ON THE LT SIDE OF THE FLOOR BEAM LOCATED AT X270.5 AND Y9.25 UNDER THE SEAT RAIL. THE CORRODED FLOOR BEAM SECTION WAS REMOVED, REPAIR ANGLES AND A PACKER FABRI CATED AND INSTALLED IAW EO8-53-3278. 2 H 7 2 4T RT A13NM 20090204 NM 2009 2 4 HNAA2009020100042 1 20080613 A 5500 85520003009 TAB DHAV DHC8 DHC8102 2809003 NM STABILIZER DENTED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 980HA 32622 376 DENT ON TRAILING ARM OF LT STRING TAB 3.3" FROM INBD EDGE. REPAIR DAMAGE IAW WITH RD8-55-037. 2 H 7 2 4T RT A13NM 20090204 EA 2009 2 4 HNAA2009020100036 1 20081015 A 5330 SKIN DHAV DHC8 DHC8311 1386006 EA FUSELAGE DENTED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 327EN 261 PROTRUDING DENT ON BELLY SECTION OF FORWARD FUSELAGE AT STATION X223 BETWEEN STRINGER 32S-33S. REPAIR SKIN IAW RD8-53-2 181. 2 H 7 2 4T RT A13NM 20090204 EA 2009 2 4 HNAA2009012500023 1 20081022 A 5315 85320379117 FLOORBEAM DHAV DHC3 DHC3 2800202 EA FUSELAGE DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 327EN 30034 30034 261 FLOOR BEAM DAMAGE AT STA X129 BENEATH RT INBD SEAT RAIL ATTACHMENT. PERFORM LIQUID PENETRANT INSPECTION PER EO8-53-08-33 7 NO DEFECT FOUND. REPAIR DAMAGE PART PER EO8-53-08-337 1 H 7 1 3R A815 20090204 EA 2009 2 4 HNAA2009012500024 1 20081015 A 5330 85330022011 SKIN PANEL DHAV DHC8 DHC8311 1386006 EA FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 327EN 30034 30034 261 PROTRUDING DENT ON LT FUSE STA X444.8, STR 30P - STR 31P. REPAIR DAMAGE IAW EO8-53-08-3363 EDDY CURRENT AND BONT TEST. 2 H 7 2 4T RT A13NM 20090205 EA 2009 2 5 S9BA2008024 2 20080620 A 7250 BLADE DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA NR 2 ENGINE WORN A S9BA K NONE O OTHER IN INSP/MAINT 1 SO 29 562CP 562 PGO266 UNUSUAL NOISE NOTED IN COMPRESSOR SECTION (NR 2 ENG) UPON START UP. REMOVED ENGINE FROM SERVICE, ENGINE RETURNED TO ENG INE SHOP, FOUND 1ST STAGE BLADE RUB. ENGINE PENDING REPAIR. (K) 1 H 7 2 3T 4 T RT A9EA E4EA 20090205 NM 2009 2 5 UPS09654431 1 20080124 A 3350 BPS73 BATTERY BOEING 767 76734AF 1385212 NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 308UP 27761 INSPECTION TYPE:N/A COCKPIT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY ASSY IAW 33 -57-07-2. ALL OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 20090205 WP 2009 2 5 UPS09854453 1 20080128 A 2560 SLIDE DOUG DC8 DC873F 302199F WP CREW DOOR OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 851UP 46051 INSPECTION TYPE:N/A ESCAPE SLIDE FELL OUT OF HOLDER. DEFERRED SLIDE PER MEL M393690 ASSIGNED. INSTALLED EVACUATION SLI DE IAW M/M 25 60 01 2. THIS CLEARS M393690. 2 L 7 4 4F RT 4A25 20090204 NM 2009 2 4 HNAA2009012500022 1 20080910 A 5347 85320490 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 984HA 33035 33035 337 FORWARD LT INBD SEAT TRACK HAVE SURFACE CORROSION FROM STA X182 TO STA X424.124. FROM STA 182 TO STA 260 FOUND TO BE PR EVIOUSLY BLENDED, R&R SEAT TRACK IAW RD8-53-1932. REMOVED CORROSION FROM STA 260 TO STA 424 IAW RD8-53-1339. 2 H 7 2 4T RT A13NM 20090205 NM 2009 2 5 PCSA2009012701 1 20081231 A 2611 SMOKE WARNING BOEING 727 7272J7 138400E NM CARGO BAY FALSE ACTIVATION A PCSA O OTHER N FALSE WARNING CR CRUISE 1 SO 17 128NA 20879 CARGO SMOKE LIGHT ILLUMINATED IN FLIGHT, RAN ALL APPROPRIATE CHECKS, FALSE INDICATION, CONTINUED FLIGHT. MX PERFORMED A N OPS TEST OF THE SMOKE DETECTION SYS AND FOUND GOOD IAW THE MM. 2 L 7 3 4F A3WE 20090205 WP 2009 2 5 AALA200803045 1 20081205 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 278AA 49294 MSP EMERGENCY LIGHT AT SEAT 22D HAS BROKEN SHROUD. REPLACED SHROUD. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20090114 NM 2009 1 14 AALA200802616A 1 20081130 A 3350 SIGN BOEING 757 757223 1384957 NM EMERGENCY LIGHT DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 682AA 25339 EMERGENCY LIGHT EXIT IDENTIFER AT LEFT NUMBER FOUR DOOR DAMAGED. REPLACED PLACARD FOR LIGHT AT LEFT NUMBER FOUR DOOR. S YSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20090114 NM 2009 1 14 AALA200802617A 1 20081130 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 682AA 25339 EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. REPLACED LAMP AT SEAT 29D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20090114 NM 2009 1 14 AALA200802619A 1 20081130 A 3350 LAMP BOEING 757 757223 1384957 NM EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 682AA 25339 EMERGENCY LIGHT AT SEAT 34D INOPERATIVE. REPLACED LAMP AT SEAT 34D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F RT A2NM 20090114 NM 2009 1 14 ASAA0944177 1 20081220 A 5320 65C33973337 INTERCOSTAL BOEING 737 737490 1384715 NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 708AS 28895 INTERCOSTAL CRACKED. R&R INTERCOSTAL. 2 L 7 2 4F RT A16WE 20090114 WP 2009 1 14 IXXA08SMN200S 1 20081024 A 5711 SPAR CAP DOUG DC8 DC862F 3021972 WP RT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER REAR SPAR CAP VERTICAL FLANGE CRACKED AT STATION XRS 554.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP HOLE. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROS ION FOUND AFTER DRILLING STOP HOLE. FABRICATED REPAIR ANGLE, STIFFENER, SPACERS. CLEANED, TREATED, PRIMED AREA AND REP AIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08543 DATED 11/18/08, SEMAN DRAWING ED-4 879 DATED 11/07/08, DC8 SRM 51-1-20D, SRM 51-1-21, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-12, DC8 SRM 51-1-11, AND SRM 51-3-1. 2 L 7 4 4F 4A25 20090114 WP 2009 1 14 IXXA08SMN214S 1 20081028 A 5311 FRAME DOUG DC8 DC862F 3021972 WP FUSELAGE DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 280.00 0 LONGERON 19-20 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABR ICATED ANGLE DOUBLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PART S IAW FAA FORM 8110-3 NUMBER 08549, SEMAN DRAWING ED-4877, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-1 PAGES 1, 13, AN D 17, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D, AND SRM 51-3-1. 2 L 7 4 4F 4A25 20090114 NE 2009 1 14 ZZDA2008188 2 20081220 A 7230 PLUG BOEING 717 717200 1383700 NM RROYCE BR700 BR700715A130 NE NR 1 ENGINE LOOSE A ZZDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 37 899AT 55049 ON DEPARTURE, FIRE DETECTOR LEFT ENGINE FAIL ILLUMINATED AT 12,000 FEET, WENT OUT AT ABOUT 13,000 FEET FOLLOWED BY A LEF T ENGINE FIRE INDICATION. INDICATION WENT OUT WHEN THROTTLE WAS MOVED TO IDLE. OVERWEIGHT LANDING APPROX 106,500 LBS. FOUND BORESCOPE PLUG 'F' ON NR 1 ENGINE LOOSE. RESECURED PLUG PER MM 72-33. PERFORMED FIM 26-11, TASK 807. NO DEFECT S NOTED. A/C LANDED BELOW OVERWEIGHT LANDING LIMIT OF 110,000 LBS. A/C OK FOR SERVICE REF MM 05-51-04, 1B. 2 L 7 2 4F 4 F TR A6WE E00061EN 20090114 NM 2009 1 14 FDEA200812235263 1 20081223 A 2840 2300071 INDICATOR BOEING 727 727225 1384077 NM FUEL QTY FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 469FE 21581 NUMBER 2 FUEL GAUGE INDICATED ZERO DURING CRUISE THEN PASSING THROUGH APPROX 12000 FT GAUGE STARTED TO COME UP TO READ F UEL QUANTITY. SUMPED NR 3 TANK. NO WATER FOUND. NO FAULT CODES ON INDICATOR. CLEANED CANNON PLUG ON NR 3 VTO ON FWD S PAR. R&RD NR 3 FUEL QUANTITY GAGE INDICATOR AS A PRECAUTION PER AMM 28-41-040-4 AND OPS CHECKED PER 28-41-000-5 AND I. N O FAULTS . TRANSFERED ALL FUEL FROM TANK TO 0 READING. TRANSFERED FUEL BACK INTO NR 3 TO READING OF 11.1 WITH NO BLANKIN G OUT OF GAGE. ACFT OK FOR SERVICE. 2 L 7 3 4F A3WE 20090115 NM 2009 1 15 FDEA200812245275 1 20081224 A 5340 65561521 STRINGER CLIP BOEING 727 727233 138408A NM BS 344 DAMAGED A FDEA O OTHER O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 MISDRILLED STRINGER CLIP AT 9G BULKEAD, STR 4R REMOVED STRINGER CLIP ON 9G BULKHEAD STR 4R IAW SRM 51-30-2. CUTOUT DAMA GED AREA IAW SRM 53-10-4. FABRICATED PARTS OF STRINGER CLIP IAW SRM 51-20-1 AND 51-10-3. FABRICATED FRAME REPAIR PARTS AND HEAT TREATED IAW SRM 53-10-4 FIG 2 AND 53-10-2 FIG 3. TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REP AIR PARTS IAW SRM 51-30-2 AND 53- 10-4, FIG 2. 2 L 7 3 4F RT A3WE 20090113 NM 2009 1 13 NWAA08736302 1 20080225 A 2460 ELECTRICAL SYS BOEING 747 747451 1384940 NM COCKPIT MALFUNCTIONED A NWAA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 01 662US 23720 AFTER TAKE OFF NR 2 MAIN TANK FORWARD PUMP MSG AND LIGHT CAME ON FOLLOWED BY RT UTILITY BUS LIGHT AND MSG. PERFORMED FU EL PUMP PROCEDURE AS PER COM FIRST AND COMPLIED. THEN PERFORMED RT UTILITY PROCEDURE AS PER COM AND COORDINATED WITH PU RSER. HER REPORT WAS ACRID ODOR AND FUZZY VISIBILITY BUT NO FIRE WAS VISIBLE. ODOR WAS REPORTED AT BOTH ENDS OF THE CA BIN. AN EMERGENCY WAS DECLARED AND AN IMMEDIATE UNEVENTFUL LANDING WAS MADE BACK AT NRT. MX R&R CONTROL UNIT BUS, BOOS T FUEL PUMP, LOAD CONTROL UNIT, EPESC ENHANCED PASSENGER ENTERTAINMENT SYSTEM, RELAY R50 AND CB C401, OVEN CONTROLLER AN D NEED TO REPLACE 2 OVEN RELAYS AND OVEN. ALSO INSPECTED OVEN AND COFFEE CONNECTORS, FEEDER LINES AND CONNECTORS, UTILI 2 L 7 4 4F RT A20WE 20090113 EA 2009 1 13 SWIA200820793 1 20081231 A 3350 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A SWIA K NONE O OTHER UK UNKNOWN 1 NM 07 816SK 15105 FLT 4519 - THIRD FROM AFT EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090114 NM 2009 1 14 HNAA2009010900384 1 20080925 A 5347 85320701123 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 828EX 33568 33568 392 DURING C-CHECK, SEVERAL AREAS OF CORROSION WERE FOUND ON THE LT OTBD SEAT RAIL. THE SEAT RAIL WAS R&R. 2 H 7 2 4T RT A13NM 20090114 WP 2009 1 14 AALA200802578A 1 20081124 A 3350 P4010049 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 567AM 53293 LT HAND SEAT MOUNTED EMERGENCY LIGHTS AT FORWARD HALF OF CABIN INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERG ENCY LIGHTS AT FORWARD HALF OF CABIN. S YSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A6WE 20090114 NM 2009 1 14 AALA200802579A 1 20081124 A 2751 TRANSMITTER BOEING 757 757223 1384957 NM TE FLAPS FAILED A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 677AN 29427 STL INFLIGHT. TRAILING EDGE FLAP DISAGREE INDICATION ON APPROACH. LANDED STL WITHOUT INCIDENT WITH FLAPS AT 20 DEGREES . REPLACED RIGHT HAND FLAP TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A2NM 20090114 WP 2009 1 14 AALA200802582A 1 20081124 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 967TW 53617 EMERGENCY LIGHT AT SEAT 17D INOPERATIVE. SECURED CONNECTOR AT SEAT 17D. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSE D) 2 L 7 2 4F RT A6WE 20090114 WP 2009 1 14 AALA200802583A 1 20081124 A 3397 CONNECTOR DOUG DC9 DC983 3022083 WP EMERGENCY LIGHTS LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 967TW 53617 LGA EMERGENCY LIGHT AT SEAT 22D INOPERATIVE. SECURED CONNECTOR AT SEAT 22D. SYSTEM GROUND CHECKED NORMAL OPERATION. ( CLOSED) 2 L 7 2 4F RT A6WE 20090114 WP 2009 1 14 AALA200802586A 1 20081125 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7544A 53026 EMERGENCY LIGHT AT SEAT ROW 6EF INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 6EF. SYSTEM GROUND CHECKED NORMAL OPERA TION. 2 L 7 2 4F A6WE 20090114 WP 2009 1 14 AALA200802587A 1 20081125 A 3350 P4010051111 CHARGER DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 3507A 49801 EMERGENCY LIGHTS AT RIGHT HAND FROM SEAT ROWS 3 TO 21 INOPERATIVE. REPLACED BATTERY CHARGER AT FIRST CLASS FOR EMERGENC Y LIGHTS AT RIGHT HAND FROM SEAT ROWS 3 TO 21. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20090114 WP 2009 1 14 AALA200802588A 1 20081124 A 3350 P4010049 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 3507A 49801 EMERGENCY LIGHT AT LEFT HAND AFT CABIN AT AIR STAIR INOPERATIVE. REPLACED BATTERY PACK AT AFT GALLEY. SYSTEM GROUND CH ECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20090114 WP 2009 1 14 IXXA08SMN203S 1 20081025 A 5720 FITTING DOUG DC8 DC862F 3021972 WP RT WING CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 STUB WING INNER FITTING CRACKED AT STATION XS 526.000. REM OVED CRACKED FITTING. FABRICATED NEW FITTING. CLEANED, TREATED, AND PRIMED AREA AND FITTING. INSTALLED FITTING IAW DC 8 SRM 51-1-20D, ATI REPAIR SPECIFICATION NUMBER 2003-05, SEMAN FORM IPI NUMBER 2009017, DOUGLAS DRAWING NUMBER 5754705, DC8 SRM 51-1-8B, AND SRM 51-3-1. 2 L 7 4 4F 4A25 20090114 EU 2009 1 14 MALA080220 1 20081211 A 5753 SKIN PANEL SAAB SF340 340B 7860101 EU TE FLAP DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 430XJ 340B430 DURING N4K, 2Y INSPECTIONS IN CWA, FOUND F1 DENT IN LT FLAP UPPER SURFACE PANEL 541AT AND 1 DENT INBOARD BOTTOM SURFACE 6 FROM INBD EDGE AND 18 FWD OF T/E. DENT WAS EVALUATED AND REPAIRED IAW EO NR S57060. 2 L 7 2 4T RT A52EU 20090114 NM 2009 1 14 DHLA2009770AT514 1 20081213 A 5315 FLOORBEAM BOEING 727 7272B7 138407L NM FUSELAGE CORRODED A DHLA K NONE O OTHER UK UNKNOWN 1 GL 05 770AT 21953 LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 1130 RBL 45 FLOORBEAM LOWER FWD FLANGE WITH CORROSION. REPAIRED FUSELAGE FLO ORBEAM LOWER CHORD SECTION BS 1130 BETWEEN RBL 20 AND RBL 56.5 IAW B727 SRM 53-10-8 FIG 10 DETAIL V. 2 L 7 3 4F A3WE 20090114 WP 2009 1 14 AALA200802621A 1 20080925 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 570AA 49352 CORROSION FOUND ON NR 5 SEAT TRACK. AREA OF DISCREPANCY WAS 3 INCHES BY 2 INCHES. INSTALLED SEAT TRACK PLUG IAW SRM 53 -05-00 FIGURE 4A. 2 L 7 2 4F RT A6WE 20090114 NM 2009 1 14 ASAA0944179 1 20081212 A 5347 65538441 CARGO TRACK BOEING 737 7374Q8 138447Q NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON AFT CARGO TRACK BS 945 LBL 13. R&R CARGO TRACK. 2 L 7 2 4F RT A16WE 20090114 WP 2009 1 14 IXXA08SMN208S 1 20081028 A 3210 364956U502 FITTING DOUG DC8 DC862F 3021972 WP RT MLG WW CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR WHEEL WELL FITTING CRACKED AT STATION 940.000 LONGERON 24 RIGHT. REMOVED DAMAGED FITTING FRAME. FABRICATED SPLICES, DOUBLER, AND FILLERS. PERFORMED HEAT TREATMENT. INSTALL NEW FITTING AND REPAIR PARTS IAW DC8 SRM 53-2-0 FIGURE 8 SHEETS 2, 5, AND 6, DC8 SRM 53-1-0 PAGE 1, SRM 51-1-20D, DC8 S RM 51-1-1 PAGES 1, 13, AND 17, SRM 51-1-11, AND SRM 51-3-1. 2 L 7 4 4F 4A25 20090116 EA 2009 1 16 A6WA200840645 1 20081215 A 4930 600970249 RETAINING CLIP CNDAIR CL600 CL6002B19 1900309 EA APU OUT OF POSITION A A6WA K NONE K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 433AW 7289 WHILE SERVICING APU SMELL NOTICED OPENED PANEL RAN APU. FOUND APU INLET BELLOWS RETAINING CLIP RT SIDE SLID AFT AND CHA FED HOLE IN METERED FUEL LINE TO NOZZLES. DRIPS ON IGNITER BOX. R&R FUEL LINE, REPOSITIONED RETAINING CLIP AND PLACED SPIRAL WRAP ON FUEL LINE BEHIND CLIP. 2 L 7 2 4F RT A21EA 20090116 EU 2009 1 16 M7KA1030084134 1 20081117 A 6220 704A33640088 FREQ ADAPTER UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE MAIN ROTOR CRACKED E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 821MH 906 4134 23319 DURING ROUTINE MX INSPECTION 1 OF THE 3 FRQUENCY ADAPTERS FOUND TO HAVE A CRACK IN THE ELASTOMER NEARING ITS MAXIMUM ALL OWABLE LIMITATION OF 10MM. A NEW KIT OF 3 MATCHED ADAPTERS WERE INSTALLED. 1 G 7 2 3U 3 U H9EU E00054EN 20090116 EU 2009 1 16 WRN2009F00000 1 20081219 A 2612 ASG08388501 FIRE LOOP AIRBUS 300 A300B4203 3930306 EU NR 1 ENGINE DEFECTIVE A WRNA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 SO 05 510TA 100 ENGINE NR 1 SHUT DOWN IN FLIGHT DUE TO A FIRE INDICATION DURING FLIGHT FROM BDL TO BQN. BOTH FIRE BOTTLES WERE DISCHARG ED. WARNING LIGHT EXTINGUISHED. ACFT LANDED NORMALLY. NO FUEL DUMPED. MX REPLACED 3 FIRE LOOPS AND AN AMPLIFIER. RU N UP CHECK OK. ACFT RETURNED TO SERVICE. 2 L 7 2 4F RT A35EU 20090116 NM 2009 1 16 UALA2008111305837 1 20080921 A 7921 15622000 OIL COOLER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 ENGINE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 781UA 26945 777052 L ENG OIL QTY INDICATION DROPPING INDICATED 2QTS WITH TEMP RISING. CREW REPORT. RPLD AIR COOLED OIL COOLER. RUN, OPS LEAK CK OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 20090116 EU 2009 1 16 FDEA200812170082 1 20081217 A 5311 A57110531207 FRAME AIRBUS 300 A300B4622R 3930312 EU ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 723FD 543 INSPECTION OF HOLES AT FRAME 47 RT SPLICE FITTING BETWEEN STR 24 AND 26 INDICATED DAMAGE ON HOLE "M". COMPLIED WITH EA 6-5310-125501 PART 1. 2 L 7 2 4F RT A35EU 20090120 NM 2009 1 20 HALA2008122600916 1 20081226 A 2497 745329E CIRCUIT CARD BOEING 767 767300 1385204 NM LT GENERATOR MALFUNCTIONED A HALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 593HA 33424 SUP-ETOPS SIGNIFICANT SYS - ATB - LT GEN DRIVE LIGHT ILLUM IN FLT. LT GEN CONT LIGHT ILLUM DISCONNECTED DRIVE IAW CHECK LIST (QR4). R&R LT IDG ASSY IAW TASK CARD 767-3-405001. 2 L 7 2 4F RT A1NM 20090120 NM 2009 1 20 DHLA2009770AT516 1 20081212 A 5313 STRINGER BOEING 727 7272B7 138407L NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 770AT 21953 REF N/R 1-279 LWR FUSELAGE AFT CARGO COMPARTMENT AT BS 1010 S-29R WITH CORROSION. REPAIRED FUSELAGE S-29R SECTION FROM BS 1010 TO BS 1045 IAW SRM 53-10-3 FIG 1 DETAIL 1. 2 L 7 3 4F A3WE 20090120 NM 2009 1 20 UPS09M54278 1 20081228 A 5343 FITTING DOUG MD11 MD11F 3023600 NM NLG TRUNNION CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 270UP 48576 INSPECTION TYPE: S.V. NOSE LANDING GEAR LT TRUNNION FITTING CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER , REPAIR DOUBLER AND STRAP IAW SRM 53-40-00 FIG 23 NOTE 9. 2 L 7 3 4F RT A22WE 20090120 NM 2009 1 20 ABXA200901160005 1 20081231 A 3350 BPS73 POWER SUPPLY BOEING 767 767281 1385109 NM CABIN DISCHARGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 788AX 23021 EMERGENCY LIGHTS WERE DIM AND THEN WENT OUT AFTER 2 SECONDS. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW B767 AMM 33-50-0 0. OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 20090120 EU 2009 1 20 F3LA2009010800003 1 20080702 A 5755 D57745013015 WEB AIRBUS A318 A318111 3940019 EU ZONE 600 GOUGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 805FR 40 1660 DURING C-3 C-CHECK INSP, NOTED THAT THE RT NR 3 SPOILER ANTI-ROTATION FLAT HAS A GOUGE. MX REPAIRED DAMAGED AREA IAW EA A8-57R-30430. 2 L 7 2 4F RT 20090120 NM 2009 1 20 DXTA200803079 1 20080523 A 2435 23291006 STARTER GEN GULSTM 200 200 4500308 NM LEFT FAILED E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 727QS 1121 1121 113 UPON ATTEMPT TO START THE LT ENG, THERE WAS NO ROTATION. HIT THE STOP SWITCH, SAW SMOKE COMING OUT OF LWR ALTERNATOR VEN T. 2 L 7 2 4F RT A53NM 20090120 CE 2009 1 20 DXTA200803080 1 20080527 A 7710 3074135 COMPENSATOR RAYTHN DH125 HAWKER800XP 7150012 CE N1 MALFUNCTIONED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 811QS 5764 258614 ON TAKEOFF, IMMEDIATELY AFTER APR WAS ARMED, BOTH N1 SPEEDS WENT TO 100.5 BUT LT CLIMBED TO 100.7, ABORTED TAKE OFF. 2 L 7 2 4F RT A3EU 20090120 NM 2009 1 20 DHLA2009743531 1 20081229 A 5330 SKIN BOEING 727 727225 1384077 NM ZONE 100 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 745DH 22438 SKIN DENTED AT BS 1000, BETWEEN STR 28R AND 30. ACCOMPLISHED SKIN REPAIR AS REQUIRED IAW SRM 53-30-1 FIG 1. 2 L 7 3 4F A3WE 20090120 NM 2009 1 20 DHLA2009743532 1 20081205 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 FLOORBEAM UPPER CHORD CORRODED AT BS 328, WL 208, AT RBL 44. REMOVED, FABRICATED, AND REPLACED FLOORBEAM UPPER CHORD IA W SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 20090120 NM 2009 1 20 ASAA0944228 1 20081210 A 5320 65479514 INTERCOSTAL BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON INTERCOSTAL UPPER FLANGE BETWEEN FRAME AT BS 767 TO 787 RBL 24. R&R INTERCOSTAL BS 767 787 RBL 24. 2 L 7 2 4F RT A16WE 20090120 NM 2009 1 20 UPS09654342 1 20081228 A 5320 141T514616 ANGLE BOEING 767 76734AF 1385212 NM BS 246 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE: C FX MEC COMPT BS 246 LBL 50 INCH FLOORBEAM, AFT FACE ANGLE SUPPORT FWD CRACK. REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20090120 WP 2009 1 20 UPS09854294 1 20081226 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1450 L34R MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE: SV REFERENCE UPS NRC 105041-EFN NR715RA1018 DOES NOT MATCH THE REPAIR CURRENTLY INSTALLED ON THE ACFT ( 715-F1-43). REPAIR LOCATED AT L34R STA 1458-1489). REPAIRED IAW UPS EO DC8-5330-31779A. 2 L 7 4 4F RT 4A25 20090120 WP 2009 1 20 AALA200910566 1 20081230 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 90511 49805 CORROSION ON LEFT CUSP BS 503. INSTALLED REPAIR PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20090120 EU 2009 1 20 FDEA200811285034 1 20081128 A 5531 A55177703020400 SPAR CAP AIRBUS 300 A300B4622 3930401 EU ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 33428 358 R/H THS REAR SPAR UPPER TEE CAP HAS CORROSION AT RIB 3. REMOVED PANELS & NECESSARY SUB STRUCTURE TO FACILITATE MANTENANC E IAW SRM 51-40-21; ( RE-INSTALLED IAW SRM 51-40-21). REMOVED & RE-INSTALLED THE ELEVATOR PRESSURE & RETURN LINES & ELEVATOR CONTROL RODS TO FACILITATE MANTENANCE IAW AMM 27-31-23-4 & 20-23-12-0. FABRICARED & INSTALLED NEW TEE CAP P ROFILE IAW DWG A55177703 & SRM 55-11-21; FIG 226; PAGES 377-384. 2 L 7 2 4F RT A35EU 20090120 NM 2009 1 20 DLM88090023 1 20081226 A 5520 TAB DOUG MD88 MD88 3023688 NM LT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 974DL 53242 CRACK ON TRAILING EDGE SKIN OF LT ELEVATOR ANTI-FLOAT TAB AT OTBD END. TRAILING EDGE SKIN OF LT ELEVATOR ANTI-FLOAT TAB WAS REPAIRED IAW SRM 55-09 FIG 3 AND OPN 1031 CARD 1361 AND 1369. PERFORMED WEIGHT AND BALANCE IAW SRM 55-20-2D. 2 L 7 2 4F RT A6WE 20090120 NM 2009 1 20 USAA2009011590078 1 20081227 A 5311 90526911 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - NR 6192125 - FRAME CRACKED AT BS480, BETWEEN S-8L & S9L. REPAIRED FRAME AT BS480, BETWEEN S- 8L & S9L IAW AMERICA WEST AIRLINES TASK CARD M1C53002. 2 L 7 2 4F RT A16WE 20090121 NM 2009 1 21 DHLA2009743539 1 20081125 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 100 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 FUSELAGE FRAME AT BS 1070 DENTED BETWEEN STR 25R AND 27R. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20090121 EU 2009 1 21 UPS09154311 1 20081228 A 7830 22141261147 SUPPORT ANGLE AIRBUS A300 A300F4622R 3930360 EU THRUST REVERSER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 141UP 0824 INSPECTION TYPE:1C NR 2 OUTBOARD T/R SLEEVE LOWER WEDGE SUPPORT ANGLE T-CHORD CRACKED AT BEND RADIUS (LOCATED JUST BELO W SLIDER TRACK). REPAIRED NR 2 OUTBOARD T/R SLEEVE LOWER WEDGE SUPPORT ANGLE REF EA 300-5430-01-A1589 AND EO C-7830-318 10. 2 L 7 2 4F RT A35EU 20090121 NM 2009 1 21 DHLA2009743533 1 20081229 A 5330 SKIN BOEING 727 727225 1384077 NM ZONE 100 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 FUSELAGE SKIN DENTED AT BS 950F +14 INCH, BETWEEN STR 28R AND 29R. ACCOMPLISHED DOUBLER REPAIR TO FUSE SKIN PER SRM 53- 30-3 FIG 1. 2 L 7 3 4F A3WE 20090121 NM 2009 1 21 UPS09554300 1 20081230 A 5320 RETAINER BOEING 757 75724APF 1384969 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 461UP 28265 INSPECTION TYPE:C2 CORROSION ON NUT PLATE RETAINER ON THE BOTTOM OF THE FLOOR WEB BS 1715 RBL 4.5 WL 208. REMOVED, FABR ICATED AND INSTALLED PLATE PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 20090121 NM 2009 1 21 DHLA2009743534 1 20081205 A 5320 WEB BOEING 727 727225 1384077 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 VERTICAL FLOOR WEB IN AFT CARGO COMPT CORRODED, BS 1165 TO 1170, WL 208, RBL 25. ACCOMPLISHED WEB REPAIR PER SRM 51-40- 2 FIG 2. 2 L 7 3 4F A3WE 20090121 WP 2009 1 21 UPS09854255 1 20081230 A 5310 575514956 ANGLE DOUG DC8 DC871F 302199D WP COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:N/A F/O WINDOW CRACKED AND FOUND CORROSION ON F/O'S WINDOW FRAME. A/C WILL FERRY TO SDF - SAT. REMOVED AND REPLACED LT AND RT COCKPIT WINDOW FRAME Z-ANGLES. REF EA 008-5310-A1588 & EO DC8-5310-31796-A. 2 L 7 4 4F RT 4A25 20090121 NM 2009 1 21 DLM88090035 1 20081230 A 5320 PAN DOUG MD88 MD88 3023688 NM C1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 974DL 53242 CRACK ON C1 DOOR FWD PAN BEHIND DOOR STOP NR 4, REF NRC T0116928. CRACK WAS STOP DRILLED IAW SRM 52-05D FIG 50. INSTAL LED REPAIR DOUBLER IAW SRM 52-05D FIG 50 AND IDENTIFIED IAW PS 900-5-1 NR4. 2 L 7 2 4F RT A6WE 20090121 NM 2009 1 21 DL76S081817 1 20081224 A 5753 SKIN BOEING 767 767332 1382001 NM RT WING TE FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 121DE 23435 DURING SHOP VISIT, SERVICE DAMAGE WAS FOUND ON THE LOWER SKIN OF THE RT WING OUTBOARD MAIN FLAP. THE DAMAGE RESULTED IN A LOWER SKIN CUTOUT OF 33.5 INCH BY 5.8 INCH. REPAIRED PER ERA HAS BEEN IN SHOP FOR SEVERAL YEARS, ONLY REMAINING A/C IN THE FLEET EFFECTIVE FOR THIS FLAP. 2 L 7 2 4F RT A1NM 20090121 NM 2009 1 21 DL764081818 1 20081231 A 3150 WARNING MESSAGE BOEING 767 767432ER 1385134 NM ILLUMINATED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 825MH 29696 ACFT RTB AFTER CREW REPORTED YSM AND F/O DISPLAY TRU STATUS MESSAGES. CREW LEFT RUNWAY AND RETURNED TO GATE IN ORDER TO ATTEMPT RESET AND THEN PLACE ITEMS ON FLIGHT CREW PLACARD AS PER MCC TLX. THIS MSG COULD APPEAR IF ACFT ON BATTERY POW ER ONLY FOR 1 MIN. ACFT DOWN POWERED MCDP MSG CLEARED AND STS M CLEARED. MCO AND PLACARD REMOVED. 2 L 7 2 4F RT A1NM 20090121 NM 2009 1 21 UPS09654321 1 20081231 A 5532 SKIN PANEL BOEING 767 76734AF 1385212 NM VERTICAL STAB DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE:C EMP - VERTICAL STABILIZER PANEL 322CR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A (1) FIG 9. 2 L 7 2 4F RT A1NM 20090121 NM 2009 1 21 UPS09654323 1 20081228 A 5320 INTERCOSTAL BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE:C FX MEC COMPT BS 246 LBL 50 FLOORBEAM AFT FACE INTERCOSTAL UPPER AREA FOUND CRACK. MEC COMPT BS 246 LB L 50 FLOORBEAM AFT FACE INTERCOSTAL UPPER AREA REPAIRED AS PER SRM 51-70-11-0G FIG 1. 2 L 7 2 4F RT A1NM 20090121 NM 2009 1 21 UPS09654324 1 20081231 A 5315 141T514622 STIFFENER BOEING 767 76734AF 1385212 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE:C FX MEC COMPT BS 246 RBL 10 MAIN DECK FLOOR SUPPORT BEAM ATTACH STIFFENER CRACK. MEC BS 246 RBL 10 FLO OR SUPPORT BEAM ATTACH STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20090120 WP 2009 1 20 AALA200910597 1 20081217 A 3350 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7543A 53025 FAILED OPERATIONAL TEST. REPLACED BATTERY POWER SUPPLY. OPERATIONAL CHECK OK, PER AMM 33-53-00-5. 2 L 7 2 4F A6WE 20090120 NM 2009 1 20 UPS09654343 1 20081228 A 5320 141T52822 ANGLE BOEING 767 76734AF 1385212 NM BS 246 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE: C FX MEC COMPT BS 246 LBL 25 INCH FLOORBEAM FRONT FACE SUPPORT ANGLE FOUND CRACKED. REPLACED AND INST ALLED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20090120 NM 2009 1 20 UPS09654292 1 20081231 A 5753 FITTING BOEING 767 76734AF 1385212 NM LT WING TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE: C LT WING INBD MAIN FLAP INBD AFT FLAP SUPPORT FTG UPPR AREA FLANGE FOUND CRACKED. REPAIRED IAW SRM 57 -53-02-2R1 FIG 201. 2 L 7 2 4F RT A1NM 20090120 WP 2009 1 20 AALA200910599 1 20081208 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7550 53032 EMERGENCY LIGHTS AT AFT LAVS INOPERATIVE. REPLACED BATTERY PACK, OPERATION CHECK GOOD. 2 L 7 2 4F A6WE 20090120 NM 2009 1 20 UPS09654293 1 20081228 A 5315 140T013039 FLOORBEAM BOEING 767 76734AF 1385212 NM BS 1087 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE: C AFT CARGO COMPT BS 1087 LBL 26 INBD BELOW FLOOR ANGLE SUPPORT FOUND CRACKED. AFT CARGO COMPT BS 1087 LBL 26 INCH BELOW FLOOR SUPPORT ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02. 2 L 7 2 4F RT A1NM 20090120 WP 2009 1 20 AALA200910564 1 20081217 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 90511 49805 CORROSION ON CUSP STATION 697 TO 702, LEFT SIDE. INSTALLED REPAIR PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20090120 WP 2009 1 20 AALA200910565 1 20081230 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 90511 49805 CORROSION ON RIGHT CUSP STATION 1287. INSTALLED REPAIR PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20090120 WP 2009 1 20 AALA200819463 1 20081202 A 5320 BRACKET DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 BRACKET CORRODED, BETWEEN LONGERON 27 AND 28 RIGHT AT AFT CARGO DOOR CUTOUT STATION 1210. REMOVED BRACKET AND INSTALLED SERVICEABLE BRACKET PER SRM 51-01-00. 2 L 7 2 4F RT A6WE 20090120 WP 2009 1 20 AALA200910575 1 20081212 A 5311 FORMER DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 90511 49805 CRACKED FORMER. 2 L 7 2 4F A6WE 20090120 WP 2009 1 20 AALA200910577 1 20081218 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 465A 49595 BATTERY PACKS TESTED DIM. 2 L 7 2 4F A6WE 20090120 NM 2009 1 20 ASAA0944223 1 20081223 A 5730 SKIN BOEING 737 7374Q8 138447Q NM LT WING DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 LT WING FIXED LE HAS FIBER DAMAGE AT NR 1 SLAT IB AUX TRACK CUTOUT. REPAIRED LT WING FIXED LEADING FIBER DAMAGE AT NR 1 SLAT IB AUX TRACK CUTOUT. 2 L 7 2 4F RT A16WE 20090120 EA 2009 1 20 ASOA200900058 1 20081231 A 5320 POST CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 JOB 8733515 OPERATION 172 F.S. 409+128 VERTICAL POST LBL 18.0 HAS INDICATION NOTED APPROX .3" IN LENGTH 90% FULL SCREEN HEIGHT OTBD SIDE WL 64 FLANGE FAILED NDT INSP. 2 L 7 2 4F RT A21EA 20090120 EA 2009 1 20 ASOA200900059 1 20081231 A 5320 POST CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 847AS 7335 JOB 8733515 OPERATION 173 F.S. 409+128 VERTICAL POST BL 0.0 HAS INDICATION NOTED APPROX .3" IN LENGTH 905 FULL SCREEN H EIGHT RT WL 69.0 FLANGE FAILED NDT INSP. 2 L 7 2 4F RT A21EA 20090121 EU 2009 1 21 UPS08154251 1 20081229 A 5753 A5796030000751 SKIN AIRBUS A300 A300F4622R 3930360 EU TE FLAP DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 159UP 0848 INSPECTION TYPE:N/A CENTER FLAP LOWER SKIN DAMAGED 3.4 INCH T/E BETWEEN RIB 16 AND RIB 16A DENT MEASURES 3 X 3 X .050 IN CH. PERMANENT REPAIR REF: EO A300-5750-31446-C APPENDIX A. 2 L 7 2 4F RT A35EU 20090121 NM 2009 1 21 UPS08554253 1 20081228 A 5532 175N20014 SKIN PANEL BOEING 757 75724APF 1384969 NM VERTICAL STAB DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 410UP 23732 INSPECTION TYPE:C D385560 LOWER VERTICAL STAB PANEL SKIN 175N2001-4 RT HAS SKIN DENT. REMOVED VERTICAL L/E PANEL 321BL TO FOM IAW MM 55-25-01-4. REMOVED DOUBLERS IAW SRM 51-70-10 PG 202 REPAIR 4 VERTICAL STA 172. SANDED AREA IAW SRM 51-7 0-10 PG 202 REPAIR 4. CUT OUT DAMAGED AREA IAW SRM 51-70-10 PG 202 REPAIR 4. MIXED POTTING RESIN IAW SRM 51-70-10 PG 2 02 REPAINT MST 0026587. 2 L 7 2 4F RT A2NM 20090121 NM 2009 1 21 UALA2008111303707 1 20080705 A 2120 UNKNOWN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY SMOKE A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 118UA 28811 SMOKE IN GALLEY. FLIGHT DIVERTED. NO FAULT FOUND. 2 L 7 4 4F 4 F RT A20WE E24NE 20090122 WP 2009 1 22 AALA20090121TUL01 1 20081202 A 3350 LENS DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 473AA 49648 EMERGENCY LIGHT AT SEAT ROW 19 RIGHT HAS BROKEN LENS. REPLACED LENS AT SEAT ROW 19 RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20090122 WP 2009 1 22 AALA200802627A 1 20081202 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 473AA 49648 EMERGENCY LIGHT AT SEAT ROW 19 RIGHT INOPERATIVE. REPLACED LAMP AT SEAT ROW 19 RIGHT. SYSTEM GROUND CHECKED NORMAL OPE RATION. 2 L 7 2 4F A6WE 20090122 NM 2009 1 22 USAA2009011690083 1 20081227 A 5311 90526911 FRAME BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - CRACK ON FRAME AT BS 500C, BETWEEN S8L TO S9L. REPAIRED FRAME AT BS 500C, BETWEEN S8L TO S9L IAW AMERICA WEST AIRLINES TASK CARD M1C53002. 2 L 7 2 4F RT A16WE 20090120 WP 2009 1 20 UPS09854274 1 20081223 A 5753 564297022 DOUBLER DOUG DC8 DC871F 302199D WP TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE: SV RT WING OTBD FLAP INBD HINGE COVER OTBD SIDE DOUBLER GOUGED (ALSO INVESTIGAT E CAUSE). REPAIRED IAW UPS EO DC8-572031745A. 2 L 7 4 4F RT 4A25 20090121 EU 2009 1 21 UPS09154312 1 20081229 A 7830 22141261151 SUPPORT ANGLE AIRBUS A300 A300F4622R 3930360 EU THRUST REVERSER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 141UP 0824 INSPECTION TYPE:1C NR 2 ENG INBOARD T/R SLEEVE LOWER WEDGE SUPPORT ANGLE IS CRACKED JUST NEXT TO SLIDER TRACK. REPAIRED NR 2 INBOARD T/R SLEEVE LOWER WEDGE SUPPORT ANGLE REF EA300-5430- 01-A1591 AND EO C-7830-31801-A. 2 L 7 2 4F RT A35EU 20090121 NM 2009 1 21 DHLA2008743524 1 20081118 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 FUSELAGE FRAME HAS DOUBLE DRILLED HOLES AT BS 680, STR 16R TO 17R. REPAIRED FUSE FRAME SECTION PER SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 20090121 NM 2009 1 21 DL75E090014 1 20081231 A 2760 276002127 PCA BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE NR 3 MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 703TW 27620 716383 SPOILER MSG AND LIGHT FOUND FUSE LIGHT ON SCM 2R FAULT POWER CONTROL ACTUATOR (PCA) NR 3. INSTALLED KNOWN GOOD SAM AT 2 R. NO HELP. REPLACED FUSE. REMOVED C/P FROM NR 3 PCA. NO FUSE LIGHT ON SCM 2R NOW. INSTALLED C/P AT PCA NR 3.50608 0. REMOVED PCA NR 3 PER AMM. OK TO INSTALLED PER A NARINE611731 250/JFK RII. INSTALLED NR 3 PCA PER AMM. DID NOT ADJ UST ROD END NUT OR LVDT DUE TO NO FUSE IN BOX. REPLACED FUSE. 2 L 7 2 4F 4 F RT A2NM E17NE 20090122 WP 2009 1 22 AALA200910608 1 20081224 A 5300 FITTING DOUG DC9 DC983 3022083 WP UNKNOWN WRONG PART A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 FITTING WRONG TYPE. REMOVED AND REPLACED FITTING, PER S/B DC9-52-189. 2 L 7 2 4F RT A6WE 20090122 WP 2009 1 22 WX0A070256 1 20081222 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 879GA 53486 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETUR NED TO SERVICE. 2 L 7 2 4F RT A6WE 20090122 WP 2009 1 22 AALA200910609 1 20081224 A 5300 FITTING DOUG DC9 DC983 3022083 WP UNKNOWN WRONG PART A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 FITTING WRONG TYPE. REMOVED AND REPLACED FITTING PER S/B DC9-52-189. 2 L 7 2 4F RT A6WE 20090122 WP 2009 1 22 AALA200910610 1 20081224 A 5300 FITTING DOUG DC9 DC983 3022083 WP UNKNOWN WRONG PART A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 FITTING WRONG TYPE. REMOVED AND REPLACED UPPER FORWARD FITTING PER S/B DC9-52-189. 2 L 7 2 4F RT A6WE 20090122 NM 2009 1 22 DL76L081799 1 20081228 A 2780 SLAT SYSTEM BOEING 767 767332 1382001 NM MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 195DN 28452 RTB - L/E SLAT ASYMMETRY ON TAXI OUT. FLAP SLAT CONTROL UNIT TESTED M548 READ OUT AND THEN PSEU TESTED 294-301 BITE REA DOUT. RESET PROCEDURE PERFORMED SUCCESSFULY. NO FAULTS EXIST. TEST OK. 2 L 7 2 4F RT A1NM 20090122 NM 2009 1 22 DL76L081800 1 20081228 A 2822 PUMP BOEING 767 767332 1382001 NM FUEL BOOST FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 189DN 25990 RTB - TAXI OUT LT FWD FUEL BOOST PUMP FAILED. FOUND PUMP OPERATING NORMAL. FOUND C/P PINS GREEN AND SWITCH PINS CONTAM INATED AT LOW PRESS SWITCH S71. REPINNED CONNECT AND REPLACED LOW PRESSURE SWITCH S71. WITH SWITCH OUT AND P ON FOUND NO FLOW FROM LOW PRESS LINE-AFTER SEVERAL MINUTES BLOCKAGE CLEARED-PURGED LINE FOR SEVERAL MORE MINUTES UNTIL ALL FLOW C LEAR. REINSTALLED SWITCH ALL, OPS NORMAL NO FURTHER CONTAMINATION FOUND IN TANK. 2 L 7 2 4F RT A1NM 20090122 NM 2009 1 22 DL76L081801 1 20081228 A 2897 CONNECTOR BOEING 767 767332 1382001 NM CONTAMINATED A DALA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 SO 27 189DN 25990 JUST CLEARING MAIN AIRSPACE GOT LEFT FUEL SYSTEM PRESS MSG DIV TO JFK FOR REPAIRS. FOUND PUMP OPERATING NORMAL. FOUND C/P PINS GREEN AND SWITCH PINS CONTAMINATED AT LOW PRESS SWITCH S71. REPINNED CONNECT AND REPLACED LOW PRESSURE SWITCH S71. WITH SWITCH OUT AND P ON FOUND NO FLOW FROM LOW PRESS LINE-AFTER SEVERAL MINUTES BLOCKAGE CLEARED-PURGED LINE FOR SEVERAL MORE MINUTES UNTIL ALL FLOW CLEAR. REINSTALLED SWITCH ALL OPS NORMAL. NO FURTHER CONTAMINATION FOUND IN TANK. 2 L 7 2 4F RT A1NM 20090122 NM 2009 1 22 DL757081803 1 20081229 A 5320 INTERCOSTAL BOEING 757 757232 1384965 NM BS 1540-1560 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 AFT CARGO BETWEEN SAT, 1540 - SAT: 1560 BETWEEN STRINGERS S-26R AND S-27R FOUND SUPPORT WEB (INTERCOSTAL) WITH CORROSION AS MARKED C53-162-01L, COMPLIED WITH AT SAA-SAT ON NON ROUTINE 81721150001. 2 L 7 2 4F RT A2NM 20090122 WP 2009 1 22 AALA200910611 1 20081224 A 5300 FITTING DOUG DC9 DC983 3022083 WP WRONG PART A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 FITTING WRONG TYPE. REMOVED AND REPLACED UPPER AFT FITTING PER S/B DC9-52-189. 2 L 7 2 4F RT A6WE 20090122 WP 2009 1 22 WX0A070257 1 20081231 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT INOPERATIVE A WX0A K NONE L NO TEST IN INSP/MAINT 1 WP 19 862GA 49556 DURING A ROUTINE OVERNIGHT SERVICE CHECK INSPECTION MAINTENANCE DEPARTMENT PERSONNEL REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYSTEM WOULD NOT TEST. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 33-50-00. THE AIRCRAFT HAS RETUR NED TO SERVICE. 2 L 7 2 4F RT A6WE 20090122 WP 2009 1 22 AALA200910616 1 20081223 A 5230 FITTING DOUG DC9 DC983 3022083 WP CARGO DOOR WRONG PART A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 21 434AA 49452 CARGO DOOR LOWER AFT CLIP WRONG TYPE. REMOVED AND REPLACED FITTING (CLIP) PER S/B DC-9-52-189. 2 L 7 2 4F RT A6WE 20090122 WP 2009 1 22 AALA200910617 1 20081229 A 5230 FITTING DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AA 49452 CARGO DOOR FORWARD BOTTOM STOP PAD FITTING CRACKED. REMOVED AND REPLACED FITTING. 2 L 7 2 4F RT A6WE 20090122 NM 2009 1 22 DLM88081806 1 20081210 A 5523 TAB DOUG MD88 MD88 3023688 NM LT ELEVATOR DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 974DL 53242 DENTS ON LT ELEVATOR GEARED TAB SKIN. THIS NRC WAS ACCOMPLISHED IAW OPN 1031 CARD 1245-1253 AND SRM 55-04D PAR 3A FIG 2 . THIS REPAIR WAS IDENTIFIED IAW PS 900-5-1 NO 4. WEIGHT AND BALANCE WITHIN LIMITS IAW SRM 55-20-2D. 2 L 7 2 4F RT A6WE 20090122 NM 2009 1 22 DLM88081807 1 20081210 A 5532 SKIN DOUG MD88 MD88 3023688 NM VERTICAL STAB DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 974DL 53242 DAMAGED METALIZED COAT ON RUDDER. SURFACE SANDED IAW SRM 51-70-1AD PARA 23 A. (1). PLY OF GLASS FABRIC AND LAMINATE AST ROSTRIKE WERE INSTALLED IAW SRM 51-70-1AD PARA 23 A. (2)(3). RUDDER PAINTED IAW SRM 51-10-3B. 2 L 7 2 4F RT A6WE 20090123 NM 2009 1 23 USAA2009012190117 1 20081226 A 5315 6546810 FLOORBEAM BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT BS 967, BETWEEN LBL 18 TO LBL 44. REPAIRED FLOORBEAM AT B S 967, BETWEEN LBL 18 TO LBL 44 IAW B737 SRM 53-00-51. 2 L 7 2 4F RT A16WE 20090121 NM 2009 1 21 UPS09M54384 1 20081230 A 5730 ARB2888502 SKIN DOUG MD11 MD11F 3023600 NM RT WING MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:1C REPAIR SURVEY SEQ 289-W4-03 SOME HI-LOKS NOT FLUSHED AND SOME FASTENERS OUT OF EDGE DISTANCE ON RT WI NG L/E STA XOS 708-729. REMOVED EXISTING REPAIR ON RT WING L/E STA XOS 708 TO 729 REF REPAIR SURVEY SEQ 289-W4-03 AND R EPAIRED L/E SKIN REF MD11 SRM VOL 1 57-10-00 FIG 21 SHT 1, 3 AND ALL NOTES APPLICABLE TO THIS SECTION. 2 L 7 3 4F RT A22WE 20090121 NM 2009 1 21 UPS09M54399 1 20081228 A 5713 STRINGER DOUG MD11 MD11F 3023600 NM LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:1C LT WING LEADING EDGE STRINGER ANGLE AT STA XORS 455 FOUND CRACKED APPROX 1 INCH LENGTH. REMOVED STRI NGER ANGLE, FABRICATED AND INSTALLED DOUBLER ANGLE IAW ARB2933 AND MD-11 SRM 51-31-01 VOL 1 PG 1. 2 L 7 3 4F RT A22WE 20090121 NM 2009 1 21 UALA2008111300951 1 20080220 A 2820 40885 CONTROLLER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CENTER TANK FAULTY A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 773UA 26929 FUEL LEAK DETECTED FROM DRAIN MAST BETWEEN MLG DOORS. REPLACED SEALS ON ALL FIVE GAMMA COUPLINGS ON FWD TRANSFER TUBE I N CENTER TANK DRY BAY. REPLACED FUEL VALVE CONTROLLER, OPS AND LEAK CHECKED OK. REPLACED APU FUEL FEED LINE GAMMA COUP LING O-RINGS. 2 L 7 2 4F 4 F RT T0001SE E46NE 20090122 NM 2009 1 22 USAA2009011690085 1 20081224 A 5320 SUPPORT BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON SUPPORT DECK BETWEEN BS 500C TO BS 500D, & BETWEEN S26R TO S27R IN FORW ARD CARGO COMPARTMENT. REPAIRED SUPPORT DECK BETWEEN BS 500C TO BS 500D, & BETWEEN S26R TO S27R IN FORWARD CARGO COMPA RTMENT IAW B737 SRM 53-00-53. 2 L 7 2 4F RT A16WE 20090122 EA 2009 1 22 SWIA200820836 1 20081211 A 5320 SILL CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 FLOOR STRUCTURE FORWARD OF SERVICE DOOR SILL HAS EXFOLIATION CORROSION. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20090122 NM 2009 1 22 UPS08M54243 1 20081227 A 5712 ARB7770506 RIB DOUG MD11 MD11F 3023600 NM RT WINGLET MISMANUFACTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 274UP 48575 INSPECTION TYPE:N/A MAJOR REPAIR- RT LWR WINGLET, RIB MISSING LIGHTENING. REPAIRED RIB AS PER MD11-5720-31667. 2 L 7 3 4F RT A22WE 20090122 NE 2009 1 22 UALA2008111305595 2 20080905 A 7250 50L936 DUCT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 ENGINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 781UA 42586 290 26945 777034 NR 1 ENGINE HPT DAMAGE. REPLACED NR 1 ENGINE. SHOP TEARDOWN FOUND A MISSING HP TURBINE STAGE-2 DUCT SEGMENT. ADJACENT SEGMENTS HAD FOREIGN MATERIAL LODGED IN THE INTERNAL COOLING PASSAGES THAT CHOKED OFF COOLING AIR. THIS CAUSED BOWING, WHICH LEAD TO HEAVY BLADE RUB AND EVENTUAL SEGMENT LIBERATION. 2 L 7 2 4F 4 F RT T0001SE E46NE 20090122 NE 2009 1 22 UALA2008111306196 2 20081020 A 7260 GEARBOX BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 46724 12578 27115 727366 NR 1 ENG ANGLE GEAR BOX (AGB) AFT END HAS LOOSE BOLTS AT 12:00 AND FLANGE EAR IS BROKEN AT 1:00. REPLACED NR 1 ENGINE. ENGINE WAS SUBSEQUENTLY FIELD REPAIRED. THE ANGLE GEARBOX (AGB), HORIZONTAL DRIVESHAFT, AND CP07 FUEL TUBE WERE REPLAC ED. 2 L 7 2 4F 4 F RT A1NM E24NE 20090123 NM 2009 1 23 UALA2009011900187 1 20080115 A 2150 285T007816 CIRCUIT CARD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT AC PACK FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 643UA 25093 RT PACK OFF LIGHT. REPLACED RT FLOW CONTROL VALVE, NO HELP. REPLACED AC PACK FLOW PC CARD. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20090123 NM 2009 1 23 DL757081782 1 20081223 A 5315 143N50174 FLOORBEAM BOEING 757 757232 1384965 NM BS 760, LBL36 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 DURING HMV, DAMAGE WAS FOUND ON AN UNDOCUMENTED REPAIR TO THE STA 760 FLOORBEAM WEB AND UPPER CHORD. THE UNAPPROVED REP AIR WAS REMOVED AND A NEW UPPER CHORD SPLICE WAS INSTALLED PER SRM AND BOEING REPAIR INSTRUCTIONS. 2 L 7 2 4F RT A2NM 20090123 NM 2009 1 23 DL757081783 1 20081223 A 5330 144N321011 SKIN BOEING 757 757232 1384965 NM BS 1640 S23L CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 DURING HMV, A CRACK WAS FOUND ON THE FUSELAGE SKIN AT STA 1640 AT THE UPPER FWD CORNER OF THE OUTFLOW VALVE CUTOUT. THE DAMAGE WAS REPAIRED WITH A REPAIR DOUBLER PER BOEING REPAIR INSTRUCTIONS. 2 L 7 2 4F RT A2NM 20090126 NM 2009 1 26 USAA2009012190108 1 20081224 A 5523 65C25746131A TAB BOEING 737 7373G7 138447J NM RT ELEVATOR DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - RIGHT ELEVATOR TAB DELAMINATED AT NR 1 HINGE BRACKET, ELEV STA 39.22. REPAIRED RIGHT ELEVATO R TAB AT NR 1 HINGE BRACKET, ELEV STA 39.22 IAW B737 SRM 51-70-17. 2 L 7 2 4F RT A16WE 20090126 NM 2009 1 26 DHLA 2009770AT527 1 20081209 A 5730 SKIN PANEL BOEING 727 7272B7 138407L NM ZONE 600 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 770AT 21953 RIGHT WING FRONT SPAR SECTION LEADING EDGE SKIN CRACKED AT WS 491. REPAIRED RIGHT WING FIXED LEADING EDGE SKIN SECTION FROM LE STA 151.40 TO LE STA 195.65 IAW COOPESA EO COO-2-57-461-08 DTD 12/19/08. 2 L 7 3 4F A3WE 20090126 NM 2009 1 26 USAA2009012190110 1 20081229 A 5312 651758350 BULKHEAD BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - CRACK AT BS 178 BULKHEAD ON WEB SURFACE OF VERTICAL BEAM, RBL 5.7, BETWEEN WL 180 & WL 190. REPAIRED BS 178 BULKHEAD ON WEB SURFACE OF VERTICAL BEAM, RBL 5.7, BETWEEN WL 180 & WL 190 IAW US AIRWAYS EA 132193. 2 L 7 2 4F RT A16WE 20090123 NM 2009 1 23 USAA2009012190116 1 20081224 A 5320 SUPPORT BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON STRAP ANGLE SUPPORT AT BS 1006, RBL 41. REPAIRED STRAP ANGLE SUPPORT A T BS 1006, RBL 41 IAW B737 SRM 51-40-02 & 51-10-02. 2 L 7 2 4F RT A16WE 20090204 EU 2009 2 4 FDEA200808263600 1 20080826 A 7700 154DN3 SENSOR AIRBUS 300 A300F4605R 3930327 EU NR 1 ENGINE FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 661FE 760 NR 1 ENGINE N1 INDICATION BECAME UNSTABLE DURING CLIMB. REPEAT WRITE-UP, THEN EGT EXCEEDED LIMITS AT 952 DEG THEN FUEL FLOW INDICATION BECAME UNSTABLE WITH SURGING AND YAW. REMOVED AND REPLACED THE FUEL FILTER AND THE TEMP INLET SENSOR (T 1.2). REF AMM A300-600 73-12-02-4 AND 73-23-06-4. COMPLETED HIGH PWR RUN PER JRH ALL PARAMETERS WERE WITHIN LIMITS 2 L 7 2 4F RT A35EU 20090206 WP 2009 2 6 AALA200803044 1 20081205 A 3350 SHROUD DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 278AA 49294 MSP EMERGENCY LIGHT AT SEAT 30D HAS BROKEN SHROUD. REPLACED SHROUD. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20090206 EU 2009 2 6 FDEA200811244963 1 20081124 A 5270 A5237424900600 HOUSING AIRBUS 310 A310222 3930315 EU WARNING SWITCH DAMAGED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 455FE 331 AFT CARGO DOOR OPEN LIGHT IN FLIGHT. RETURNED TO KUL. VISUALLY CHECKED CLOSED AND LOCKED. VERIFIED INTEGRITY OF AFT C ARGO DOOR CLOSING AND LOCKING MECHANISM, ALL SATISFACTORY. SUSPECT FAULTY SWITCH CAUSING ERRONEOUS DOOR INDICATION. A PPLIED MEL 52-71-01. FOUND AFT CARGO DOOR LIMIT SW 32WS HOUSING BROKEN. REMOVED AND REPLACED AFT CARGO DOOR LIMIT SW 3 2WS AND HOUSING. 2 L 7 2 4F RT A35EU 20090206 NM 2009 2 6 AALA200803032 1 20081203 A 3350 P4010049 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 638AA 24596 JFK EMERGENCY LIGHTS AFT OF SEAT ROW 28 INOPERATIVE. REPLACED BATTERY PACK IN AFT GALLEY CEILING. SYSTEM GROUND CHECKE D NORMAL OPS. 2 L 7 2 4F RT A2NM 20081212 NM 2008 12 12 SWAA086902 1 20081208 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 201LV 29854 DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086903 1 20081208 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 201LV 29854 DURING SCHEDULED HC2 CHECK, FOUND RT EEPLS COVER CRACKED. REMOVED AND REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086943 1 20081206 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 747SA 29799 DURING SCHEDULED MV3 CHECK, FOUND LT MLG FWD TRUNNION BEARING O/B LOWER LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086908 1 20081208 A 5753 6546431 SKIN BOEING 737 7373H4 1384600 NM FORE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND RT WING O/B FORE FLAP SKIN CRACKED AT O/B TRACK ATTACH FITTING CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086944 1 20081206 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 747SA 29799 DURING SCHEDULED MV3 CHECK, FOUND RT MLG FWD TRUNNION BEARING FITTING I/B UPPER LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086909 1 20081206 A 3350 300432 LIGHT BOEING 737 7373Y0 1384671 NM EXTERIOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 308SA 23498 DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086911 1 20081209 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767+6, LBL 3. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086912 1 20081209 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767+6, LBL 9. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086913 1 20081209 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767+6, LBL 17. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086914 1 20081209 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767+6, LBL 12. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086919 1 20081209 A 5330 6562212 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086945 1 20081206 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 747SA 29799 DURING SCHEDULED MV3 CHECK, FOUND LT MLG FWD TRUNNION BEARING UPPER I/B LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086946 1 20081206 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 747SA 29799 DURING SCHEDULED MV3 CHECK, FOUND RT MLG FWD TRUNNION BEARING FITTING I/B LOWER LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 AALA200810406 1 20081114 A 5311 FRAME BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 STATION 480 RIGHT, FRAME CRACKED AT AIRCONDITIONING RAIL ATTACH POINT. REPAIRED PER ECO J1159AA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 AALA200810397 1 20081122 A 5340 BRACKET BOEING 737 737823 13844CB NM ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 BRACKET CRACKED IN RADIUS UNDER RIGHT TRANSITION PANEL IN FORWARD CARGO AT STATION 500H FORWARD SIDE OF BELLFRAME CONNEC TED TO INTERCOSTAL. REMOVED AND REPLACED BRACKET PER SRM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 AALA200810398 1 20081122 A 5320 BRACKET BOEING 737 737823 13844CB NM ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 BRACKET CRACKED IN RADIUS UNDER RIGHT TRANSITION PANEL IN FORWARD CARGO AT STATION 500F AFT SIDE OF BELLFRAME CONNECTED TO INTERCOSTAL. REMOVED AND REPLACED BRACKET PER SRM. 2 L 7 2 4F RT A16WE 20081212 WP 2008 12 12 IXXA08SMN191S 1 20081021 A 5330 SKIN DOUG DC8 DC862F 3021972 WP ZONE 100 MISREPAIRED A IXXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND DOUBLER BELOW MAIN CARGO DOOR OPENING HAS IMPROPER REPAIR AT STATION FS 400 LON GERON 25 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORM ED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. CLEANED, TRE ATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08548 DATED 11/ 18/08, SEMAN DRAWING ED-4868 DATED 10/23/08, DC8 SRM 51-1-21, SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1- 8B, DC8 SRM 51-1-11, AND SRM 51-3-1. 2 L 7 4 4F 4A25 20081212 NM 2008 12 12 AALA200810388 1 20081121 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 TOP OF FLOORBEAM CORRODED AT STATION 986 BETWEEN BUTT LINE 29 LEFT AND BUTT LINE 31 LEFT. INSTALLED REPAIR ANGLE PER AA RD 53-00-00-7. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 CALA2008121101142 1 20081211 A 5315 65C33970 STRAP BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 46625 27529 BOTTOM OF FLOORBEAM STABILIZER STRAP CRACKED AT BODY STATION 312 RBL-36. REPAIRED DAMAGED STABILIZER STRAP ON BOTTOM OF FLOORBEAM AT BODY STATION 312 RBL-36 PER B737-500 SRM 53-10-51, REPAIR 4. 2 L 7 2 4F RT A16WE 20081211 NM 2008 12 11 DU4R2008271 1 20081207 A 5314 KEELBEAM BOEING 757 75723APF 1384966 NM FUSELAGE CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 868AN 24868 DURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND KEEL BEAM AREA PANEL SUPPORT FRAME HAS CORROSION ON BOTH S IDES TOP AND BOTTOM SURFACES. 2 L 7 2 4F RT A2NM 20081211 WP 2008 12 11 UPS08854084 1 20081009 A 5754 VANE DOUG DC8 DC873F 302199F WP LE SLOT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQUENCE 803-W4-30, NR 4 STUB WING, 2 LOOSE BLIND FASTENERS, 8 OVERSIZED HOLES WITH DIMPLE WAS HERS, NEAR XFS 511, O/B END OF SLOT VANE. REMOVED SLOT VANE, REMOVED AND REPLACED 1 DAMAGED EXT & 1 DAMAGED INT REPAIR DOUBLER, RE-ASSEMBLED AS REQUIRED REF SRM 57-2-1 FIG 2H, 57-3-3 FIG 11, 51-1-8, 51-1-21, 57-20-05-2, DWG 5769933. 2 L 7 4 4F RT 4A25 20081211 WP 2008 12 11 UPS08854085 1 20081102 A 5313 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP AFTER REMOVAL OF DOUBLER AT STA 492 L24L (803-F1-18) FOUND BLENDOUT ON ON LOWER RADIUS OF L24L. NOT ALLOWED PER SRM. PERFORMED LONGERON SECTION SPLICE REPAIR PER SRM 53-2-2, DWG4613495. 2 L 7 4 4F RT 4A25 20081211 WP 2008 12 11 UPS08854094 1 20081013 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR 803-F1-108, STA 1566-1573, L31L-L32L, WAS REPAIRED PER SRM 53-2-1 FIG 7, IS CAT B, AND REQUIRE S ENGINEERING DISPOSITION. REMOVED EXISTING REPAIR. INSTALLED NEW REPAIR PER DC8 SRM 53-04-01-0 FIG 16 SHT 2. 2 L 7 4 4F RT 4A25 20081212 NM 2008 12 12 AALA200810386 1 20081124 A 5320 FLOOR SUPPORT BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 TOP OF FLOOR SUPPORT CORRODED AT STATION 929 AND BUTT LINE 46 RIGHT. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-0 2-0G STATION 929 BUTT LINE 46 RIGHT. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 CALA2008121001134 1 20081209 A 5312 651758243 BULKHEAD BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14652 28913 VERTICAL WEB AT STATION 178 BULKHEAD STRUCTURE HAS A CRACK RBL 17.1 WL-119.5. REPAIRED VERTICAL WEB STATION 178 BULKHEA D RBL 17.1 WL-119.5 PER ECRA 5311-01438. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 CALA2008121001135 1 20081210 A 5311 6546550 FRAME BOEING 737 737524 1384721 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14652 28913 AIR CONDITIONING SUPPORT BRACKET ATTACHED TO THE FRAME BETWEEN STRINGERS 8 AND 9 IS CRACKED AROUND RIVET AT STA 787L. T RIMMED OUT CRACKED AREA OF FRAME AND INSTALLED REPAIR DOUBLERS AND FILLERS PER ECRA 5311-01439. INITIATED DIP 91636 TO READ AS FOLLOWS, BEFORE THE ACCUMULATION OF 71598 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM AN INSPECTION PER PART 2 OF ECRA 5311-014 39. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 CALA2008121001136 1 20081210 A 5532 65C3579238 SKIN BOEING 737 737524 1384721 NM VERTICAL STAB WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14652 28913 FUSELAGE UPPER SURFACE WHERE DORSAL FIN SEAL BLADE TOUCHES THE SKIN IS WORN. REPAIRED THE UPPER SKIN OF THE DORSAL PER ECRA 5331-01433. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 DL757081690 1 20081203 A 8012 7755386 START VALVE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE INTERMITTENT A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 646DL 24217 716574 PUSHED UP THROTTLES FOR TAKEOFF AND BEFORE REACHING 60 KTS THE "R STARTER CUTOUT" LIGHT CAME ON. WHEN PULLED POWER BACK FOR ABORT, LIGHT WENT OUT. REPLACED RT START VALVE PER MM CKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081212 NM 2008 12 12 DLM88081677 1 20081028 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM BS 636-693 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 EXFOLIATION CORROSION ON LOWER DOOR JAMB FRAME BTW STA 636-693 WITHIN C2. REMOVED CORROSION IAW SRM 51-10-3, FOUND OUT OF LIMITS. FABRICATED REPAIR PARTS WERE INSTALLED IAW SRM 53-05 FIG 123. 2 L 7 2 4F RT A6WE 20081212 NE 2008 12 12 ASAA0854011 2 20081207 A 7310 FA00631C FUEL FILTER BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE NR 2 ENGINE UNKNOWN A ASAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 NM 02 559AS 35178 876334 DURING TAXI OUT NUMBER 2 ENG "FILTER BYPASS" LIGHT ILLUMINATED IT REMAINED ON CONTINUOUSLY UNTIL ENG WAS SHUT DOWN ALL E NG INDICATIONS APPEARED NORMAL. GROUNDED YES. PERFORMED EEC BITE PROCEDURE REF 73 00 TASK 801 WITH 73 31072 MAINT MESS AGE BEGAN FIM TASK 73 05 00 810 801 F00 UP THROUGH STEP E (5)(B) PG 9 OF 21 STARTED STEP E (5)(E) IMPENDING BYPASS "PG 1 0 REMOVED NR 2 ENG FUEL FILTER TEMP REINSTALLED FILTER COVER IDLE LEAK CHECK (NO CONTAMINATION FOUND ON FILTER) NR 2 ENG FILTER BYPASS DID NOT COME ON DURING SEVERAL STARTS COULD NOT DUPLICATE. THIS COMPLETES FIM TASK 73 05 00 STEP E AND S TEP H IMPENDING BYPASS. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081212 NM 2008 12 12 DL764081654 1 20081127 A 2750 PSEU BOEING 767 767432ER 1385134 NM GE CF6 CF680 30025 NE TE FLAPS DAMAGED A DALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 27 832MH 29704 P80464 LOW SPEED ABORT FOR TAKEOFF WARNING EICAS FLAPS FOUND DURING TROUBLESHOOTING WENT TO RERACK PSEU AND FOUND ALIGNMENT KEY BROKEN. REMOVED KEY RESEATED PSEU. FAULT REMOVED BITE CHECK OF FSEU AND PSEU, NO FAULTS NOTED. 2 L 7 2 4F 4 F RT A1NM E13NE 20081212 NM 2008 12 12 ASAA0874004 1 20081209 A 5320 147A5710Y1 SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON LT GALLEY SUPPORT. REMOVED AND REPLACED LT GALLEY SUPPORT. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 ASAA0874005 1 20081209 A 5320 147A5710Y2 CIRCUIT BREAKER BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 RT GALLEY SUPPORT HAS CORROSION. REMOVED AND REPLACED RT GALLEY SUPPORT. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 ASAA0874020 1 20081130 A 5321 453A261015 FLOORBOARD BOEING 737 737790 13844CN NM CARGO BAY CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON AFT CARGO BAY FLOORBOARD. FABRICATED NEW FLOOR PANEL. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 ASAA0874018 1 20081121 A 5755 113A4001 SKIN PANEL BOEING 737 737790 13844CN NM NR 6 SPOILER PUNCTURED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 NR 6 SPOILER LOWER SURFACE PUNCTURED. REPAIRED LOWER SURFACE PER SRM 57 70 10 REPAIR 2. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 CALA2008121101140 1 20081211 A 5310 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14336 23574 FLOORBOARD ATTACH ANGLE AT RIGHT SIDEWALL STATION 486 NEEDS TO BE CUT AND DISPLACED TO FACILITATE REPAIR OF FORWARD CARG O DOOR AFT FRAME. CUT ANGLE TO FORM FRAME MAT ID 7075 T6 .063" PER SRM B737 53-30-13. FABRICATED REPAIR ANGLE PER SRM B737 53-30-13. ALODINED AND PRIMED PER SRM 51-20-01. INSTALLED ANGLE PER SRM 53-30-13. 2 L 7 2 4F RT A16WE 20081212 EA 2008 12 12 MASA2008120700738 1 20081207 A 3350 1317 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 7291Z 7291 ASH FLT 2843 PHX. EMERGENCY CEILING LIGHT AT ROW 10 INOP. MX RELAMPED EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 20081212 EA 2008 12 12 MASA2008120900739 1 20081209 A 2560 BATTERY CNDAIR CL600 CL6002B19 1900309 EA FLASHLIGHT DISCHARGED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 27191 7191 ASH FLT 7148 ORD-TVC - CREW REPORTED F/O EMERGENCY FLASHLIGHT LED WAS NOT FLASHING. MX REPLACED THE BATTERY. 2 L 7 2 4F RT A21EA 20081212 EA 2008 12 12 MASA2008120900740 1 20081209 A 3350 1317 LIGHT CNDAIR CL600 CL6002D24 1390016 EA CABIN INOPERATIVE A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 942LR 15042 ASH FLT 2790 PHX-OAK. OVERHEAD CABIN EMERGENCY LIGHT ROW 10 INOP. MX REPLACED BULB. 2 L 7 2 4F RT A21EA 20081212 SO 2008 12 12 RAIA2008121000001 1 20081208 A 2120 DUCT EMB 145 EMB145EP 3260221 SO NR 2 AC PACK LOOSE A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 807HK 145119 CREW RECEIVED A WING 2 ANTI-ICE LEAK MESSAGE ON THE EICAS. MAINTENANCE INSPECTED AND FOUND THE NR 2 PACK HAD A LOOSE EX HAUST DUCT. THE DUCT WAS RE-SECURED AND THE SYSTEM TESTED WITH NO DEFECTS. 2 L 7 2 4F RT T00011AT 20081212 NM 2008 12 12 WRLA2008107 1 20081120 A 5320 WEB BOEING 747 7474H6 13848BE NM FUSELAGE CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 SO 11 740WA 25700 DURING FWD CARGO COMPARTMENT INSPECTION FOUND AT STA 860 BELOW CENTER GUIDE WEB CRACKED (BUTT LINE 0). PERMANENT REPAIR PERFORMED BY BEAGLE AIRCRAFT REPAIR SERVICE, FAA XBKY891X, JOB CARD REF BAR50750.ORDER NUMBER 65B06236-2 REPAIRS CARRIE D OUT PER BOEING SERVICE REQUEST ID NO 1-1080401394 11/21/08. 2 L 7 4 4F RT A20WE 20081212 SO 2008 12 12 SIMA200834306 1 20081204 A 5320 CHANNEL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 918AE 14500902 DURING A IMBV INSPECTION, THE BAGGAGE DOOR LOWER SILL WAS FOUND TO BE CORRODED. REMOVED CORRODED DOOR SILL. POSITIONED NEW SILL AND DRILLED, CLEANED, ALODINED AND PRIMED NEW SILL AND SILL AREA. REPAIR DONE IAW EMBRAER SRM (SRM EMB 145/11 42 REV 40) CHAPTER 51-40-02. 2 L 7 2 4T RT T00011AT 20081212 NM 2008 12 12 AALA200820086 1 20081124 A 5320 146N5246 FLOOR SUPPORT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 56842 24599 FLOOR SUPPORT CORRODED, REPAIRED FLOOR SUPPORT IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20081212 NM 2008 12 12 DLM88081657 1 20081028 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 206 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 DENT ON FUSELAGE SKIN STA 206 BTW LONG 16 AND 17. DENT FOUND WITHIN LIMITS IAW SRM 53-04 FIG 38 TABLE COND 1B. PER NDT SPM 06.10.001 HFEC ACCOMPLISHED, NO CRACKS FOUND. NEW FILLER AND DOUBLER FABRICATED IAW ERA 362959-14 REV B. NEW DOUB LER AND FILLER INSTALLED IAW ERA 362959-14REVB. 2 L 7 2 4F RT A6WE 20090123 NM 2009 1 23 USAA2009012190111 1 20081224 A 5320 65C326779 INTERCOSTAL BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON INTERCOSTAL AT BS 993.5, RBL 26. REPAIRED INTERCOSTAL AT BS 993.5, RBL 26 IAW B737 SRM 51-70-11. 2 L 7 2 4F RT A16WE 20090126 NM 2009 1 26 DL757081809 1 20081229 A 5313 STRINGER BOEING 757 757232 1384965 NM BS 1506 S28L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 AFT CARGO FUSELAGE S28L BS 1506 HAS EXFOLIATION CORROSION C/W AT SAA - SAT ON NON ROUTINE 81720380001. 2 L 7 2 4F RT A2NM 20090126 NM 2009 1 26 DL757081811 1 20081229 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1510-1520 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 EXTERNAL SKIN AT BS 1510-1520 UNDER RT AIRPHONE ANTENNA HAS CORROSION. COMPLIED WITH AT SAA, SAT ON NON ROUTINE 8172352 0001. 2 L 7 2 4F RT A2NM 20090126 NM 2009 1 26 DHLA2009770AT524 1 20081218 A 5330 SKIN PANEL BOEING 727 7272B7 138407L NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 770AT 21953 LOWER FUSELAGE FWD CARGO COMPARTMENT SKIN WITH CORROSION FROM BS 486 TO BS 494 BETWEEN S-27R AND S28R. REPAIRED FUSELAG E SKIN SECTION FROM BS 481 TO BS 496.5 BETWEEN BL 0 AND S27R IAW EO-COO-2-53-500-08 DTD 12/23/08 DOCUMENTED OF FAA FORM 8110-3. DTA WITHIN 12 MONTHS AFTER COMPLETION OF REPAIR 2 L 7 3 4F A3WE 20090126 NM 2009 1 26 DHLA2009770AT525 1 20081208 A 5330 SKIN PANEL BOEING 727 7272B7 138407L NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 770AT 21953 LOWER FUSELAGE FWD CARGO COMPARTMENT FROM BS 560 TO BS 570 RBL 11 WL 148 SKIN WITH CORROSION. REPAIRED FUSELAGE SKIN SE CTION FROM BS 557 TO BS 579 BTWN S-26R AND S-28L IAW EO COO-2-53-474-08 DTD 12/18/08. 2 L 7 3 4F A3WE 20090126 EA 2009 1 26 SWIA200820868 1 20081211 A 7120 BEAM CNDAIR CL600 CL6002B19 1900309 EA ENGINE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 494CA 7765 C-CHECK, ENGINE BEAM UPPER RIGHT CLOSEOUT ANGLE CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20090126 NM 2009 1 26 UALA2008111306318 1 20081030 A 2751 TRANSMITTER BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE TE FLAP UNRELIABLE A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 173UA 24380 EICAS "FLAPS DRIVE" WITH INBOARD T/E FLAP ASYMMETRY CMC FAULT. FOUND LT INBOARD INDICATION WAS 2.0 DEGREES WHILE OTHER FLAP INDICATIONS WERE 0.0 DEGREES. ON ARRIVAL WHILE LOWERING FLAPS THE INDICATION BECAME BLANK. REPLACED LT INBOARD RT VDT TRANSMITTER. OPS CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20090128 NM 2009 1 28 DL76G081798 1 20081227 A 2751 TRANSMITTER BOEING 767 767332 1382001 NM NR 8 FLAP MALFUNCTIONED A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 1609 30574 FLAP/SLAT ELEC STATUS MESSAGE DISPLAYED DURING TAXI. HARD FAULT NR 8 RES 12/28/08 JFK 271703321. REMOVED AND REPLACED NR 8 FLAP POSITION TRANSMITTER PER AMM. OPS NORMAL. 2 L 7 2 4F RT A1NM 20090128 NM 2009 1 28 DL757081802 1 20081229 A 5330 146N35318 SKIN BOEING 757 757232 1384965 NM BS 1510, S28R CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 DURING HMV, CORROSION WAS FOUND UNDER THE AIRFONE ANTENNA BLANKING DOUBLER AT STA 1510, RT. THE CORRODED SKIN SECTION W AS CUT OUT AND AN SRM SKIN REPAIR WAS INSTALLED. A 12 MONTH DTA RESTRICTION WAS IMPOSED DUE TO CLOSE PROXIMITY OF ANOTH ER EXISTING REPAIR DOUBLER. 2 L 7 2 4F RT A2NM 20090123 WP 2009 1 23 AALA200802625A 1 20081202 A 2910 HOSE DOUG DC9 DC982 3022082 WP HYD SYSTEM LEAKING A AALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 419AA 49331 FLL INFLIGHT - CREW REPORTED RIGHT HYDRAULIC QUANTITY AND PRESSURE LOSS. EXTENDED LANDING GEAR MANUALLY. LANDED FLL WI THOUT INCIDENT AND AIRCRAFT WAS TOWED OFF RUNWAY. REPLACED RIGHT HYDRAULIC SYSTEM HOSE AND SERVICED HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. 2 L 7 2 4F A6WE 20090126 NM 2009 1 26 NWAA085756316 1 20081227 A 3350 FUSE BOEING 747 747451 1384940 NM PWA 4168 PW4168A NE EMERGENCY LIGHT FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 676NW 33002 DURING OVERNIGHT CHECK, FOUND LEFT SIDE, 3RD OVERWING EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED FUSE ON POWE R SUPPLY. OPS CHECKED GOOD, ACFT WAS RETURNED TO SERVICE. (K) 2 L 7 4 4F 4 F RT A20WE 20090126 NM 2009 1 26 NWAA085746316 1 20081227 A 3350 FUSE BOEING 747 747451 1384940 NM POWER SUPPLY FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 676NW 33002 DURING OVERNIGHT CHECK, FOUND RT SIDE OVERWING EMERGENCY LIGHT INOPERATIVE AT STA 1503. REMOVED AND REPLACED FUSE ON PO WER SUPPLY. OPS CHECKED GOOD, AND ACFT WAS RETURNED TO SERVICE. (K) 2 L 7 4 4F RT A20WE 20090126 EA 2009 1 26 SWIA200820869 1 20081211 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT NACELLE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 494CA 7765 DURING C-CHECK, RIGHT ENGINE AFT THRUST FITTING CORRODED. REPLACED PER AMM 2 L 7 2 4F RT A21EA 20090126 EA 2009 1 26 SWIA200820870 1 20081211 A 7120 BEARING CNDAIR CL600 CL6002B19 1900309 EA THRUST FITTING CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 494CA 7765 DURING C-CHECK, LEFT ENGINE THRUST SHAFT FITTING SPHERICAL BEARING CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20090126 EA 2009 1 26 SWIA200820871 1 20081220 A 5310 WINDOW POST CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 869AS 7479 DURING C-CHECK, LEFT WINDSHIELD SIDE POST OUTBOARD CLIP CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20090126 EA 2009 1 26 SWIA200820873 1 20081220 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 869AS 7479 C-CHECK, CRACK ON AFT PRESSURE BULKHEAD AT LOWER BOTTOM LINTEL FITTING. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081212 NM 2008 12 12 DLM88081659 1 20081028 A 5540 RUDDER DOUG MD88 MD88 3023688 NM DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 DAMAGED METALIZED PROTECTION COAT ON RUDDER ASSY. DAMAGED METALIZED WAS SANDED IAW SRM 51-70-1AD PAR 23 FIG 58. ONE PL Y OF STYLEROGLASS FIBER FABRIC AND ASTRO STRIKE LAMINATE IMPREGNATE WITH EA956 AB WERE INSTALLED IAW SRM 51-70-1AD PAR 2 3. ASSEMBLY WAS CURED IAW SRM 51-70-1AD. 2 L 7 2 4F RT A6WE 20081212 NE 2008 12 12 DLM88081664 2 20081024 A 7200 JT8D219 BOLT DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RT ENGINE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 48907 43173 718224 WEAR ON AFT CONE BOLT FLANGES (BOTH SIDES) ON RT ENGINE. WEAR REWORKED IAW EA 49-469467-14 REV ORIG. WITHIN LIMITS AND NO CRACKS NOTED IAW EA 49-469467-14 REV ORIGINAL. 2 L 7 2 4F 4 F RT A6WE E9NE 20081212 NM 2008 12 12 DLM88081665 1 20081028 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 229-245 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 DENTS ON REPAIR DOUBLER STA 229-245 BTW LONG 16 AND 18 LT. DENT OUT OF LIMITS. REMOVED DOUBLER AND FILLER IAW SRM 51-3 0-2 AND 51-30-5. REPAIR PARTS INSTALLED IAW ERA 330121-14 REV E. 2 L 7 2 4F RT A6WE 20081212 NM 2008 12 12 DL76P081666 1 20081128 A 2910 V643602 VALVE BOEING 767 767332 1382001 NM HYD SYSTEM LEAKING A DALA O OTHER K FLUID LOSS CR CRUISE 1 SO 27 143DA 25991 INFLIGHT LEVEL 340, R HYD QTY EICAS MSG WARNING WITH ASSOCIATED LOSS TO 0.45 ON ARRIVAL AT GATE. RIGHT HYD QTY WENT TO 0.01.\D MODULE SHOWS NO FAULTS. REPLACED SELF RESETTING FUSE VALVE AT LEFT ANTI-SKID VALVE MODULE NR 5 LK CHECK OPS CK OK. 2 L 7 2 4F RT A1NM 20081212 SO 2008 12 12 CHQA200800235 1 20081202 A 3350 RPS1B BATTERY PACK EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL EMERGENCY LIGHT DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 564RP 16667 16667 145524 CAE312502 THE OVERWING EMERGENCY LIGHTS DO NOT OPERATE WHEN TESTED. THE EMERGENCY BATTERY WAS REPLACED IAW EMB 145 AMM 33-50-04 A ND THE EMERGENCY LIGHTS OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081212 WP 2008 12 12 IXXA08SMN187S 1 20081021 A 5330 SKIN DOUG DC8 DC862F 3021972 WP ZONE 100 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE EXTERNAL SKIN CORRODED AT STATION 1530.000 LONGERON 35 RIGHT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN SEGMENT, SPLICE, INTERNAL DOUBLERS, INTERNAL DOUBLERS, INTERNAL FINGER DOUBLERS, LONGERON STRAPS. CLEANED, TREATED, PRIMED AREA AND REP AIR PARTS. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIGURE 8 SHEET 1, SRM 51-1-8B PAGES 17-18, SRM 53-2-0 PAGE 2P, SRM 51- 1-21, SRM 51-1-20D, SRM 53-2-1 FIGURE 8 SHEET 3 TR 53-173, SRM 53-5-2 FIGURE 1, SRM 51-1-8B. SRM 51-1-11, AND SRM 51-3-1 . 2 L 7 4 4F 4A25 20081212 NM 2008 12 12 AALA200810411 1 20081114 A 5311 FRAME BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 STATION 500A LEFT, FRAME CRACKED AT AIR CONDITIONING RAIL ATTACH POINT. REPAIRED PER ECO J1159AA. 2 L 7 2 4F RT A16WE 20081212 SO 2008 12 12 SIMA200834308 1 20081203 A 5320 14530643401 CHANNEL EMB 145 EMB145LR 3260212 SO FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 646AE 145213 DURING CPCP INSPECTION, FOUND RIGHT OMEGA BEAM CORRODED BETWEEN FRAMES 24 AND 25. REPAIRED OMEGA BEAM IAW EMB SRM 53-00 -10. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081212 NM 2008 12 12 DL757081645 1 20081119 A 5320 146N852257 THRESHOLD BOEING 757 757232 1384965 NM BS 1436-1438 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 AFT CARGO BAY DOORWAY THRESHOLD INNER T-CHORD CORRODED AT VERTICAL LEG FASTENER HOLES BS 1436 AND 1438, OUT OF LIMITS RE MOVED AND REPLACED PART. 2 L 7 2 4F RT A2NM 20081212 NM 2008 12 12 DL76G081647 1 20081126 A 2822 PUMP BOEING 767 767332 1382001 NM FUEL BOOST MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 1604R 30180 RTB - R FWD FUEL BOOST PUMP LOW PRESSURE LIGHT ON. FLT CREW PLACARD WAS ISSUED BUT A/C NEEDED FUEL ADDED DUE 120 RTE PE R MEL. 2 L 7 2 4F RT A1NM 20081212 NM 2008 12 12 DL76L081700 1 20081207 A 3810 COMPRESSOR BOEING 767 767332 1382001 NM POTABLE WATER ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 192DN 28449 POTABLE WATER COMPRESSOR INOP AND EMITTING ELEC SMELL. FOUND COMPRESSOR WITH BURNT SMELL. DISCONNECTED AND STOWED CONN ECTOR. PULLED/SECURED C/B H6 ON P33. FWD TO MCO PLAC REF MEL 38-10-01A SMELL OCCURRED AT GATE WITH PAX ONBOARD. REMOV ED AND REPLACED POTABLE WATER COMPRESSER PER M/M. OPS CHK OK. MCO/PLA REMOVED. 2 L 7 2 4F RT A1NM 20081212 NM 2008 12 12 AALA200810394 1 20081121 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 FLOORBEAM STATION 328 ALL MOUNT HOLES FROM BUTT LINE 10 RIGHT TO OUTBOARD FUSELAGE HAS CORROSION AFT LIP. INSTALLED FLO OR BEAM REPAIR STATION 328 PER ESO 61000 DATED 11/21/08. 2 L 7 2 4F RT A16WE 20081215 EA 2008 12 15 ASOA200801695 1 20081208 A 5312 BULKHEAD CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 848AS 7339 FS 202 FWD BULKHEAD CRACKED AT PARKING BRAKE CABLE AREA. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 ASOA200801698 1 20081208 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 CARGO SEAT TRACK AT RBL 9 FS 559 + 80 IS CORRODED. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 ASOA200801702 1 20081208 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 LIGHT SURFACE CORROSION UNDER 281LLF AT CARGO DOOR ENTRANCE. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 ASOA200801703 1 20081208 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 FS 484 ANGLE LBL 27 IS CRACKED IN RADIUS. REMOVED CLIP AND RIVETS AND INSTALLED NEW CLIP AND RIVETS IAW CRJ 200 SRM 51- 42-06, 51-42-20, AND REO 601R-53-41-059. REQUIRES PAINT AND DYNATROL. PAINTED REPAIR AREA IAW CRJ SRM 51-25-01 AND APP LIED DINITROL IAW CRJ SRM 51-21-11. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 A6WA200840617 1 20081125 A 3230 LANDING GEAR CNDAIR CL600 CL6002B19 1900309 EA NLG MALFUNCTIONED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 436AW 7734 LOG 193016/2 NOSE GEAR FAILED TO RETRACT ON TAKEOFF RESULTING WITH A GEAR DISAGREE MSG. COMPLIED WITH QRH RETURNED LGA. INSPECTED NLG AND FOUND DURING RETRACTION NLG DOES NOT CENTER. FLUSHED AND SERVICED NLG IAW AMM 32-12-32. JACKED NLG AND FOUND CENTERING TO OP CHECK GOOD C/W EXTENSION / RETRACTION CHECK IAW AMM 32-30 OP CHECKS GOOD. 2 L 7 2 4F RT A21EA 20081215 NM 2008 12 15 ASMF 20081201 1 20081201 A 3244 294W5110362 TIRE BOEING 777 7772Q8 1385238 NM LT MLG SEPARATED W ASMF K NONE C E F.O.D. VIBRATION/BUFFET TO TAKEOFF 1 SW 23 776AM 4491 4491 28692 DURING TAKE OFF, CAPTAIN REPORTED STRONG VIBRATION IN MLG. MX PERSONNEL DETECTED TREAD LOSS IN THE WHEEL POSITION NR 1 IN THE LT MLG, CRACK IN THE LT FLAP LOWER SKIN AT STA 261 AND A DENT OF 8 IN LONG X 4 IN WIDTH 0.200” DEPTH IN THE LOWER ACCESS PANEL 511JB OF LEADING EDGE OF SLAT N7. THE WHEEL WAS REPLACED IAW AMM 32-45-01. 2 L 7 2 4F RT T00001SE 20081215 CE 2008 12 15 GUUA91252120708B 1 20081207 A 5220 HANDLE BEECH 1900 1900D 1154162 CE EMERGENCY EXIT LACK OF LUBE A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 45AR UE12 DURING SCHEDULED ROUTINE MX DISCOVERED RT AFT EMERGENCY EXIT HARD TO OPEN. LUBRICATED RT AFT EMERGENCY EXIT DOOR HANDLE . 2 L 7 2 4T RT A24CE 20081215 2008 12 15 AJC2008F00003 4 20081127 A 3160 DISPLAY LEAR 35 31A 5170531 CE COCKPIT MALFUNCTIONED A AJCA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 65 864KB 048 DURING CLIMB OUT COPILOT EADI WENT BLACK. EADI CIRCUIT BREAKER WAS FOUND POPPED. AFTER SOME CONSIDERATION, CREW ELECTE D TO RESET CIRCUIT BREAKER ONCE. NEARLY IMMEDIATELY SMELL OF HOT ELECTRICAL COMPONENT. CREW PULLED CIRCUIT BREAKER AND CONTINUED FLIGHT WITH COPILOT INSTRUMENTS IN COMPOSITE MODE. 2 L 7 2 4F RT A10CE 20081215 CE 2008 12 15 GUUA94732120608A 1 20081206 A 3260 UPLOCK SWITCH BEECH 1900 1900D 1154162 CE RIGHT DIRTY A GUUA O OTHER N FALSE WARNING CL CLIMB 1 SO 29 69547 UE189 FLIGHT NR 9291 DUJ/DUJ AFTER TAKEOFF LANDING GEAR INTRANSIT LIGHT REMAINS ILLUMINATED WITH THE HANDLE IN THE UP POSITION . CLEANED RT UPLOCK SWITCH. OPS CHECK NORMAL. 2 L 7 2 4T RT A24CE 20081215 CE 2008 12 15 GLBA20081208A 1 20081207 A 3297 G15C22 WIRE BEECH 1900 1900D 1154162 CE LANDING GEAR CHAFED A GLBA O OTHER O OTHER LD LANDING 1 NM 21 251GL UE251 SIGNIFICANT EVENT - ACFT. 251GL FLIGHT NR 5145 ENROUTE FROM WRL TO LWT. THE PILOTS REPORTED THAT THE LANDING GEAR CIRCU IT BREAKER TRIPPED WHEN EXTENDING THE LANDING GEAR. PILOTS MANUALLY EXTENDED THE GEAR. MX REPAIRED CHAFED G15C22 WIRE IN THE FUSELAGE IAW. GLA GENERAL MX MANUAL VOLUME 6 CHAPTER 9 SECTION 9.3.0. OPS CHECKS OF THE LANDING GEAR SYSTEM WERE GOOD. 2 L 7 2 4T RT A24CE 20081215 CE 2008 12 15 GUUA94157120908A 1 20081209 A 5730 SKIN BEECH 1900 1900D 1154162 CE RT WING CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 17541 UE203 DURING SCHEDULED ROUTINE MX DISCOVERED RT OTBD WING UPPER SKIN TRAILING EDGE HAD CORROSION AND DEBOND BETWEEN WS 139 THR OUGH 158. REMOVED DAMAGED SKIN AND FABRICATED AND INSTALLED AN EXTERNAL REPAIR DOUBLER. 2 L 7 2 4T RT A24CE 20081215 CE 2008 12 15 GUUA937120908A 1 20081209 A 3233 1143800417 ACTUATOR BEECH 1900 1900D 1154162 CE LT MLG BYPASSING A GUUA O OTHER O OTHER CR CRUISE 1 SO 29 38537 966 UE158 FLIGHT NR 9191 PNS/TPA DURING FLIGHT LANDING GEAR RELAY CIRCUIT BREAKER POPPED. REPLACED LT MLG ACTUATOR. OPS CHECK NO RMAL. 2 L 7 2 4T RT A24CE 20081215 EA 2008 12 15 ASOA200801690 1 20081207 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 CORROSION ON FS 501 TO FS 517 ON LBL FLOORBEAM. BLENDED OUT CORROSION ON FLOORBEAM CAP FS 501 - FS517 LBL9 PER CRJ 700 SRM 51-21-06. LBL9 FLOORBEAM REPLACED DUE TO OUT OF LIMIT CORROSION. REFER TO W/O 105591 N/R-00391 FOR THE REMOVAL AND REPLACEMENT OF LBL9 FLOORBEAM FS485-565. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 ASOA200801691 1 20081207 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 716EV 10084 CORROSION FOUND FS 517 TO FS 533 LBL 9 FLOOR BEAM CAP. BLENDED CORROSION ON FLOORBEAM CAP FS517 - FS533 LBL9 PERCRJ 700 SRM 51-21-06. LBL9 FLOORBEAM REPLACED DUE TO OUT OF LIMIT CORROSION. REFER TO W/O 105591 N/R-00391 FOR THE REMOVAL AN D REPLACEMENT OF LBL9 FLOORBEAM FS485-565. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 ASOA200801692 1 20081207 A 2560 BATTERY CNDAIR CL600 CL6002B19 1900309 EA FLASHLIGHT DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 832AS 7243 F/O FLASHLIGHT NEEDS BATTERIES. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 ASOA200801705 1 20081210 A 3350 LIGHT CNDAIR CL600 CL6002C10 1390015 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 719EV 10099 RIGHT FUSELAGE CENTER EMERGENCY LIGHT INOP. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 AWKA7741211 2 20081208 A 7261 SEAL CESSNA 750 750 2076810 CE RROYCE AE3007 AE3007C1 54168 EA LT ENGINE LEAKING E AWKA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 25 774XJ 1456 7500274 CAE330569 DEPARTING TEB, FLT CREW REPORTED AT 40K FT SMOKE IN THE CABIN AT TAKEOFF POWER ENROUTE TO LAS. AFTER CLIMB-OUT AND POWE R REDUCED, CREW WAS ABLE TO CLEAR THE SMOKE. DIVERTED TO CMH. MX WAS CONTACTED AND A ROLLS ROYCE REP WAS ALSO ON SITE. THE DECISION WAS MADE TO FERRY THE ACFT TO WICHITA CITATION SERVICE CENTER (ICT) FOR FURTHER EVALUATION. WHILE PERFOR MING THE FERRY FLIGHT INSP, SMALL AMOUNTS OF ENGINE OIL WERE FOUND ON THE LT ENGINE CASE SPLIT LINE. WHILE AT ICT, THE LT ENGINE WAS BORESCOPED AND IT WAS DETERMINED THE NR 0 AND THE NR 4 BEARING SEALS WERE LEAKING INTRODUCING SMALL AMOUNT S OF OIL TO THE LOW PRESSURE BLEED LINE. THE ENGINE WAS SUBSEQUENTLY REMOVED FOR REPAIR AND A LOANER ENGINE INSTALLED. 2 L 7 2 4J 4 F RT T00007WI TE6CH 20081215 CE 2008 12 15 GSPA36365 1 20081130 A 2121 EM6039 BLOWER MOTOR ELECTROMECH BEECH 90 F90 1152909 CE CABIN BURNED OUT E GSPA B G H A EMER. DESCENT O2 MASK DEPLOYED DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 05 16WG 414 LA226 DURING CRUISE A STRONG SMELL OF SMOKE FOLLOWED BY SMOKE IN THE COCKPIT AND THE CABIN. PAX AND CREW OXYGEN MASKS WERE DO NNED, EMERGENCY PROCEDURES WERE TAKEN AND AN EMERGENCY WAS DECLARED. EMERGENCY LANDING WAS MADE WITHOUT INCIDENT. INVE STIGATION BY THE MX ON THE FIELD REVEALED THE CABIN BLOWER MOTOR WAS OVERHEATED, BURNED AND DISCOLORED AND THE CURRENT L IMITER IN THE LT NACELLE WAS BLOWN. MX INSP ASSOCIATED WIRING AND REMOVED THE BURNED OUT FUSE TO ENSURE NO POWER WAS GO ING TO THE MOTOR. THE FAILED BLOWER MOTOR ASSEMBLY WAS REMOVED AN OVERHAUL MOTOR ASSEMBLY WAS INSTALLED ALONG WITH A NE W CURRENT LIMITER. A SATISFACTORY OPS CHECK WAS PERFORMED. 1 L 7 2 4T A31CE 20081215 NM 2008 12 15 USAA2008121292219 1 20081211 A 5753 6546481150USA SPINDLE BOEING 737 7374B7 138449C NM FLAP CARRIAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 PHL - RON - MAJOR REPAIR - LOG NR 4385223 - CORROSION FOUND ON RT OTBD FLAP CARRIAGE SPINDLE. REPLACED RT OTBD FLAP SPI NDLE IAW B737 AMM 27-51-44-4. 2 L 7 2 4F RT A16WE 20081215 EA 2008 12 15 SWIA200820612 1 20081207 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 447SW 7677 FLT 4755 - REAR CEILING EMERGENCY FLOODLIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20090126 EA 2009 1 26 SWIA200820878 1 20081229 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 863AS 7487 C-CHECK, 2 CLIPS AT FS 280 BELOW FLOOR LINE RBL9 CRACKED. REPAIRED PER SRM. 2 L 7 2 4F RT A21EA 20090126 EA 2009 1 26 SWIA200820879 1 20081229 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA BS 625 S14R CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 863AS 7487 DURING C-CHECK, FS 625 RIGHT SIDE ANGLE AT STR14 CRACKED. REPLACED PER REO. 2 L 7 2 4F RT A21EA 20090126 NM 2009 1 26 DL757081781 1 20081223 A 5330 144N321011 DOUBLER BOEING 757 757232 1384965 NM BS 960 S15L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 DURING HMV, CORROSION WAS FOUND ON THE OVERWING ESCAPE HATCH CUTOUT REINFORCING STRAP AT STA 960 AND S-15L. THE CORROSI ON WAS BLENDED AND A REPAIR DOUBLER WAS INSTALLED PER BOEING REPAIR INSTRUCTIONS. 2 L 7 2 4F RT A2NM 20090126 NM 2009 1 26 DL757081788 1 20081223 A 5320 CUSP WEB BOEING 757 757232 1384965 NM BS 968 S17L CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 649DL 24389 STA 968 AT STR 17L CUSP WEB HAS AREA OF HEAVY CORROSION. REPLACE CUSP WEB. 2 L 7 2 4F RT A2NM 20090126 NM 2009 1 26 DL764081789 1 20081223 A 5270 849704 PSEU BOEING 767 767432ER 1385134 NM CARGO DOOR MALFUNCTIONED A DALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 27 825MH 29696 NUMEROUS ABNORMAL CAUTION MSGS ON TAXI OUT. DOOR MSG BULK CARGO. CLEARED ALL MSG. REPLACED PSEU, BIT CK OK. NO ABNOR MAL CAUTION MSG OK FOR SVC. 2 L 7 2 4F RT A1NM 20090126 NM 2009 1 26 DL76L081792 1 20081225 A 3610 ISOLATION VALVE BOEING 767 767332 1382001 NM RIGHT INOPERATIVE A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 188DN 1229 27583 RIGHT ISOLATION VALVE LIGHT WOULD NOT EXTINGUISH WHEN ISOLATION VALVE SELECTOR CLOSE AFTER ENGINES START. REMOVED AND R EPLACED RT ISOLATION VALVE PER M/M. OPS CHK NORMAL. 2 L 7 2 4F RT A1NM 20090126 NM 2009 1 26 DL757081793 1 20081227 A 5230 694557929 FITTING BOEING 757 757232 1384965 NM AFT CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 610DL 22817 FITTING AT BOTTOM OF AFT CARGO DOOR OPENING CORRODED ON BOTTOM STA 1400, NEW DOOR FITTING EXISTING PLATE AND NEW TIE DOW N FITTING INSTALLED IAW SRM 51-40-02 PG 39 FIG 12. 2 L 7 2 4F RT A2NM 20090128 NM 2009 1 28 USAA2009012190102 1 20081213 A 5315 6545815 FLOORBEAM BOEING 737 7374B7 138449C NM ZONE 100 - FUSEL CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 438US 24560 CLT - Q5 - MAJOR REPAIR - NR 03C10753060/005 - CORROSION ON FLOOR BEAM TEE CAP AT BS344, LBL12 TO RBL12. REPAIRED FLOOR BEAM TEE CAP AT BS 344, LBL12 TO RBL12 IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 20090128 EU 2009 1 28 M7KA1028084248 1 20081117 A 5350 ASNA2154C02 LATCH UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE ENG BAY DOOR WORN E M7KA K NONE O OTHER IN INSP/MAINT 1 WP 19 846MH 4248 23399 DURING ROUTINE INSPECTION LATCH APPEARED LOOSE AND CLOSER INSPECTION REVEALED LOCKING LATCH HINGE PINS SOCKETS AND HOOK CATCH WORN EXCESSIVELY. HINGE ATTACHMENT BORE HAD A 1` LONG CRACK RADIATING. INSTALLED NEW LATCHES AS REQUIRED. 1 G 7 2 3U 3 U H9EU E00054EN 20090128 EA 2009 1 28 A6WA200940003 1 20081222 A 4940 27044581 STARTER CNDAIR CL600 CL6002B19 1900309 EA APU MALFUNCTIONED A A6WA O OTHER A FLAME/FIRE NR NOT REPORTED 1 GL 31 404AW 7675 7294 DURING APU START EGT 715, RPM 6 FLAMES REPORTED SHOOTING OUT OF THE EXHAUST CM ACTION C/W PLACED ON MEL. R&R APU STARTE R PER AMM 49-41-07. OPS CHECK GOOD. APU PARAMETERS NORMAL. REMOVED FROM MEL. PLACARD REMOVED. 2 L 7 2 4F RT A21EA 20090126 EA 2009 1 26 SWIA200820834 1 20081211 A 5340 FITTING CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 406SW 7030 C-CHECK, CRACKED FOUND ON PRESSURE BULKHEAD AT FS 621. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090128 EA 2009 1 28 HNA2009F00000 1 20081126 A 5714 85712012101 PLATE DHAV DHC8 DHC8311 1386006 EA WING BOX CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 326EN 33233 33223 234 DURING C-CHECK INSPECTIONS, A CRACK WAS FOUND IN THE AFT OTBD CORNER OF THE WING BOX LADDER PLATE UNDER STRESS PANEL. A N EO WAS ISSUED REF RD8-57-4106 TO INCORPORATE RD8-57-2375 TO REPAIR THE LADDER PLATE. REPAIR WORK WAS THEN COMPLETED. (K) 2 H 7 2 4T RT A13NM 20090128 SO 2009 1 28 VOX2009F00000 2 20081226 A 8530 BOLT PIPER PA34 PA34200T 7103406 SO CONT O360 LTSIO360EB 17025 SO HARTZL HCC2Y HCC2YF1 GL NR 3 CYLINDER BROKEN E VOXA K NONE O OTHER IN INSP/MAINT 1 NM 03 2883Q 347970326 266173R JS87B NR 3 CYL INTAKE ROCKER ARM RETAIN BOLTS BROKEN. 1 L 7 2 3O 3 O A7SO E9CE 5 C P920 20090129 SO 2009 1 29 SWIA200820902 1 20081022 A 5315 FLOORBEAM EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 229SW 120305 C-CHECK, 2 CROSS MEMBERS AT FRAME 37 HAVE CRACKS AND CORROSION. REPLACED CROSSMEMBERS PER SRM. 2 L 7 2 4T RT A31SO 20090129 NM 2009 1 29 C8GA20080083 1 20081029 A 5311 FRAME BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE ZONE 100 CORRODED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 715AA 62202 22470 WHILE IN HEAVY PERFORMING INSPECTIONS IT WAS NOTED THAT THE FRAME WAS DENTED AT BS 1110 JUST ABOVE STR 26R CUT OUT DAMAG ED FRAME AND FABRICATED NEW FRAME FROM 7075-O .063 INCH 23 INCH BY 4.5 INCH. HEAT TREATED FRAME TO T6. INSTALLED REPAI R IAW SRM 53-10-2 AND 51-40-3. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 20090129 NM 2009 1 29 DHLA2009743545 1 20081124 A 5531 STRINGER BOEING 727 727225 1384077 NM ZONE 300 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 VERTICAL STABILIZER, LT SIDE, AT FIN STA 133, STR 9 CRACKED AT WL 359. ACCOMPLISHED REPAIR TO STRINGER PER B727 SRM 55- 30-3 FIG 2. 2 L 7 3 4F A3WE 20090129 NM 2009 1 29 DHLA2009743553 1 20081127 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 BS 783 MAIN FRAME HAS DOUBLE DRILLED HOLES BETWEEN STR 7L AND 8L. ACCOMPLISHED FRAME REPAIR IAW SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 20081212 NM 2008 12 12 SWAA086937 1 20081206 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 477WN 33988 FOUND EEPLS LIGHT COVER MISSING. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086890 1 20081205 A 5330 6552988 SKIN BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED HC1 CHECK, FOUND SKIN CRACKED AT AFT CARGO DOOR HANDLE, AFT UPPER CORNER CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081212 2008 12 12 SWAA086891 4 20081205 A 2565 D31354 SLIDE BOEING 737 7373G7 138447J NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086892 1 20081205 A 5753 6546431286 FLAP BOEING 737 7373G7 138447J NM RT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED HC1 CHECK, FOUND RT WING O/B FORE FLAP DELAMINATED. REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086893 1 20081205 A 5330 6545774 SKIN BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 683SW 24008 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 798, STR 17L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086881 1 20081204 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 415WN 29836 FOUND FWD CABIN EEPLS TRACK OUT OF POSITION. POSITIONED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086882 1 20081204 A 3350 207377 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 415WN 29836 FOUND FWD CABIN EEPLS LENS BROKEN. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086898 1 20081206 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN UNSECURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 904WN 36616 FOUND EGRESS LIGHT UNSECURED AT ROW 1 SEAT A. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086940 1 20081208 A 2560 P4010021 BATTERY BOEING 737 7373G7 138447J NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST UK UNKNOWN 1 SW 29 670SW 23784 FOUND FWD I/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086899 1 20081205 A 3350 417A56014 SIGN BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 910WN 36618 FOUND R2 EMERGENCY EXIT DOOR SIGN LOOSE. INSTALLED SIGN PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086904 1 20081208 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 201LV 29854 DURING SCHEDULED HC2 CHECK, LT BATTERY PACK FAILED CAPACITY TEST. REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086905 1 20081208 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 201LV 29854 DURING SCHEDULED HC2 CHECK, RT BATTERY PACK FAILED CAPACITY TEST. REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086906 1 20081204 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 213WN 34217 FOUND EMERGENCY EXIT LIGHT COVER LOOSE AT R2 DOOR. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086907 1 20081208 A 5310 654797321 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 638, LBL 61. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081212 2008 12 12 SWAA086941 4 20081207 A 2565 63550101 SLIDE BOEING 737 7377H4 1384404 NM R1 DOOR LOW PRESSURE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 723SW 27855 FOUND R1 DOOR SLIDE PRESSURE LOW. REPLACED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086942 1 20081206 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 747SA 29799 DURING SCHEDULED MV3 CHECK, FOUND LT MLG FWD TRUNNION BEARING O/B UPPER LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086910 1 20081209 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 767+6, RBL 12. REPAIRED BEAM PER SWA EA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086915 1 20081209 A 5313 BAC1498 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND STRINGER CORRODED AT BS 967, STR 27L, LBL 3. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086916 1 20081209 A 5330 6545776 BEAR STRAP BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND BEAR STRAP SKIN CORRODED AT BS 967, STR 27L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086917 1 20081209 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CHORD CRACKED BETWEEN BS 666 TO BS 663, RBL 24. REPAIRED CHORD PER PAE ER. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086918 1 20081209 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER PAE ER. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 AALA200810385 1 20081124 A 5320 INTERCOSTAL BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 INTERCOSTAL CORRODED BETWEEN STATION 986.5 AND STATION 1006 BUTT LINE 32 LEFT. INSTALLED INTERCOSTAL PER SRM 53-10-51. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 AALA200810405 1 20081114 A 5311 FRAME BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 STATION 440 RIGHT, FRAME CRACKED AT AIRCONDITIONING RAIL ATTACH POINT. REPAIRED PER ECO J1159AA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086947 1 20081206 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 747SA 29799 DURING SCHEDULED MV3 CHECK, FOUND LT MLG FWD TRUNNION BEARING LOWER I/B LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086948 1 20081206 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 747SA 29799 DURING SCHEDULED MV3 CHECK, FOUND RT MLG FWD TRUNNION BEARING FITTING O/B UPPER LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086949 1 20081206 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 747SA 29799 DURING SCHEDULED MV3 CHECK, FOUND RT MLG FWD TRUNNION BEARING FITTING O/B LOWER LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086950 1 20081207 A 3350 81000 SIGN BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 776WN 30591 FOUND R1 DOOR EGRESS SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 SWAA086951 1 20081210 A 2913 849589 PUMP BOEING 737 7377H4 1384404 NM NR 2 ENGINE FAULTY A SWAA K NONE O OTHER DE DESCENT 1 SW 29 261WN 32517 DECLARED EMERGENCY. NR 2 ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. DURING DESCENT, B-SYST EM HYDRAULIC FLUID QUANTITY DECREASED FLUID QUANTITY DECREASED TO ZERO WITH SUBSEQUENT LOSS OF B-SYSTEM PRESSURE. REMOV ED AND REPLACED HYDRAULIC PUMP PER MM. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 CALA2008121101141 1 20081211 A 5320 6545812 FASTENER BOEING 737 7373T0 1384582 NM CABIN FLOOR LOOSE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14336 23574 TWO EACH FASTENERS FOUND UNSECURED ON FORWARD END OF FLOOR SUPPORT INTERCOSTAL BETWEEN STATIONS 328 - 344 LBL-12. ACCOM PLISHED FLOORBEAM REPAIR PER B737 SRM 53-10-51 AT STATION 328 AT RBL-5 TO LBL-25. 2 L 7 2 4F RT A16WE 20081211 NM 2008 12 11 UHLA2008110700006 1 20081204 A 2780 SLAT EMB ERJ170 ERJ170100SE 3260406 NM WING MALFUNCTIONED A UHLA O OTHER J WARNING INDICATION DE DESCENT 1 GL 11 865RW 17000122 FLIGHT 5941 MTY TO ATL ON DESCENT THE CREW RECEIVED A SLAT FAIL MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED THE AIRCRAFT WITHOUT INCIDENT. MAINTENANCE TROUBLE SHOT PER FIM, CLEARED INHIBITS AND CYCLED THE SLATS SEVERAL TIMES; OPS C HECKED GOOD. THIS DISCREPANCY HAS NOT REPEATED THIS DATE 12/08/2008. 2 L 7 2 4F RT A56NM 20081211 NM 2008 12 11 ZZDA2008180 1 20081204 A 3350 8039251 POWER SUPPLY BOEING 717 717200 1383700 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 991AT 55135 EMERGENCY EXIT LIGHTS ON SEATS ROWS 1-2-3 & 10 INOP. REMOVED AND REPLACED BATTERY PACK POWER SUPPLY FOR SEAT ROWS 1-2-3 & 10 PER MM 33-51-03. 2 L 7 2 4F TR A6WE 20081211 NM 2008 12 11 MWEA080134 1 20081206 A 5753 5910040 SKIN BOEING 717 717200 1383700 NM TE FLAP VANE DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 13 909ME 55173 THE LEFT WING MOVABLE FLAP VANE IS DENTED ON THE LOWER SURFACE SKIN REQUIRING A REPAIR DOUBLER. 2 L 7 2 4F TR A6WE 20081211 NM 2008 12 11 UPS08M54079 1 20081130 A 5753 WEDGE DOUG MD11 MD11F 3023600 NM TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 283UP 48484 INSPECTION TYPE:N/A LEFT I/B TRAILING EDGE FLAP WEDGE CRACKED 9.5 INCHES. REPAIRED PER EO MD11-5750-31369-B. 2 L 7 3 4F RT A22WE 20081212 NM 2008 12 12 AALA200810403 1 20081113 A 5320 INTERCOSTAL BOEING 737 737823 13844CB NM ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 FLOORBOARD STRINGER CRACKED AT CENTER MOUNT HOLE BETWEEN STATION 259 AND 295. REPAIRED PER SRM 53-10-04. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 AALA200820083 1 20081120 A 5320 FLOOR SUPPORT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 56842 24599 LEFT NR 4 PASSENGER/SERVICE DOOR AFT FLOOR SUPPORT CORRODED, REPAIRED SUPPORT IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20081212 NM 2008 12 12 AALA200820084 1 20081120 A 5320 146N52465 FLOOR SUPPORT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 56842 24599 FLOOR SUPPORT CORRODED, REPAIRED SUPPORT IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20081212 SO 2008 12 12 CHQA200800241 1 20081208 A 3350 78241 INVERTER EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL EMERGENCY LIGHTS INOPERATIVE A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 287SK 145460 CAE312670 EMERGENCY FLOOR STRIP LIGHTS 2 AND 3 WERE INOPERATIVE DURING TEST. THE NR 3 INVERTER WAS REPLACED IAW EMB 145 AMM 33-50 -11 AND THE SYSTEMS CHECKED OPERATIONAL. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081212 2008 12 12 IXXA080036O 4 20081210 A 2210 COMPUTER DOUG DC8 DC871F 302199D WP AUTO PILOT DEFECTIVE A IXXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 11 830BX 150 45973 DURING CLIMB-OUT OF KTOL WITH RUDDER POWER ON, YAW DAMPER ON AND AUTO PILOT ON THE RUDDER HAD A LEFT RUDDER INPUT. THE CREW TURNED THE AUTO PILOT OFF AND THE CONDITION REMAINED, TURNED THE YAW DAMPER OFF AND NO CHANGE. THE LEFT INPUT WENT AWAY ONLY WHEN RUDDER POWER WAS TURNED OFF. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBL ESHOT THE SYSTEM AND FOUND A DEFECTIVE YAW CHANNEL COMPUTER. THE YAW CHANNEL COMPUTER WAS DEFERRED AND THE ACFT WAS RET URNED TO SERVICE. 2 L 7 4 4F RT 4A25 20081212 NM 2008 12 12 CALA2008121101137 1 20081211 A 5313 6545772263 STRINGER BOEING 737 737524 1384721 NM FUSELAGE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14652 28913 STRINGER DAMAGED AT STATION 867 S-1 BL-0. CUT OUT DAMAGED SECTION OF STRINGER AND INSTALLED STRINGER SPLICE REPAIR PER ECRA 5310-04876. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 DL76L081685 1 20081202 A 2530 828450407MODA FAN BOEING 767 767332 1382001 NM NR 3 OVEN SEIZED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 195DN 28452 ELECTRICAL SMELL FROM NR 3 OVEN IN REAR GALLEY. NO LOG YET OVEN NR 4 - NOT 3 - HAS PROBLEM WITH FAN SEIZED. FWD TO NEF 253-30. C/B PULLED AND COLLARED. NEEDS OVEN ASSY. 2 L 7 2 4F RT A1NM 20081212 NM 2008 12 12 CALA2008121101138 1 20081211 A 5310 6520722U70 DOOR FRAME BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 69348 23586 FORWARD CARGO DOOR CUTOUT FORWARD FRAME CRACKED AT LOWER DOOR STOP FITTING AT STR 24R. REMOVED AND REPLACED FORWARD CAR GO DOOR CUTOUT FORWARD FRAME PER SRM 51-10-2, PAGE 8, MAT ID 65-20722U70, PAC 59980. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 DL75E081691 1 20081203 A 3097 TERMINAL BOEING 757 7572Q8 1384972 NM PWA 2037 PW2037 NE WINDOW MELTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 706TW 28165 716574 FLT CREW REPORTED SMOKE AND FUMES IN THE FLT DECK. DAL MTC DETERMINED R1 WINDOW HEAT TERMINAL MELTED. CONFIRMED SMELL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081212 NM 2008 12 12 DL76S081692 1 20081203 A 3213 STRUT BOEING 767 767332 1382001 NM MLG UNKNOWN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 MLG SHOCK STRUT CYLINDER REPAIR IAW ERA 01-471561-14 REV A C/W ERA 01-471561-14. 2 L 7 2 4F RT A1NM 20081212 NM 2008 12 12 DL757081676 1 20080605 A 5754 STRUCTURE BOEING 757 757232 1384965 NM NR 7 SLAT UNKNOWN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 616DL 22823 SUPPLEMENTAL SDR RT WING NR 7 SLAT TRAILING EDGE WEDGE REPAIR IAW ERA 468804-14, C/W ERA 468804-14. 2 L 7 2 4F RT A2NM 20081212 NM 2008 12 12 CALA2008121101139 1 20081211 A 5311 BAC1493577 STRAP BOEING 737 7373T0 1384582 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 14336 23574 STRAP ON BOTTOM OF FRAME CRACKED AT STATION 328 BL-0. FABRICATED REPAIR PARTS AND LOCATED HOLES PER SRM 53-10-51, ALODI NED AND PRIMED REPAIR PARTS PER SRM 51-20-01. INSTALLED REPAIR PARTS PER SRM 53-10-51 AND SRM 51-40-02. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 ASAA0844017 1 20081210 A 5320 SUPPORT BOEING 737 7374Q8 138447Q NM BS 727B CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE. REPLACED SUPPORT PLATE PERRM 53-60-53 FIG 201. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 ASAA0874019 1 20081120 A 5320 BAC1509100146 FLOOR SUPPORT BOEING 737 737790 13844CN NM BS 772 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 CORROSION ON FLOOR SUPPORT AFT CARGO BAY BS 772 RBL 2 WATERLINE 153. REMOVED CORROSION ON FLOOR SUPPORT. 2 L 7 2 4F RT A16WE 20081212 NE 2008 12 12 ASAA0854010 2 20081208 A 7420 CIRCUIT BREAKER BOEING 737 737890 1384527 NM CFMINT CFM56 CFM567B27 13046 NE IGNITION SYS POPPED A ASAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NM 02 570AS 7189 35185 NR 1 ENG FAILED TO START AFTER LEVER RAISED TO IDLE N1 4.5 EGT22 N2 30 PERCENT FUEL FLOWS .50. GROUNDED YES. ENG NR 1 SHOWS MAINTENANCE MESSAGE 74 30981 RT IGNITION OUT OF RANGE. FOUND ENG NR 1 RT C/B OUT. CHECKED BEHIND P18 2 PANEL FO R CONTAMINATION OR DEFECTS NONE NOTED. RESET C/B REF MM 20 60 01. ACCOMPLISHED FIM 74 21 00 810 802. VERIFIED RESOLUT ION OF PROBLEM ENG NR 1 RT IGNITION, OPS NORMAL. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081212 NM 2008 12 12 ASAA0874007 1 20081209 A 5320 143A940521 FLOOR SUPPORT BOEING 737 737790 13844CN NM FUSELAGE DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 FLOOR SUPPORT HAS ELONGATED HOLES (SUPPORT BRACKET PAYLOADS). REMOVED FLOOR SUPPORT, FABRICATED NEW SUPPORT AND INSTALL ED. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 ASAA0874008 1 20081209 A 5320 141A5410U3 INTERCOSTAL BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CRACK ON INTERCOSTAL. REPLACED INTERCOSTAL. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 ASAA0874006 1 20081209 A 5320 147A571235 WEB BOEING 737 737790 13844CN NM FUSELAGE CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 625AS 30792 RIGHT WEB CRACKED. REMOVED AND REPLACED WEB. 2 L 7 2 4F RT A16WE 20081212 WP 2008 12 12 WRLA2008106 1 20080906 A 5350 FAIRING DOUG DC10 DC1030 3023501 WP FUSELAGE PUNCTURED A WRLA K NONE C F.O.D. CR CRUISE 1 SO 11 14075 46922 FLIGHT 8010 09/06/08 KBWI/ETAR - DURING FLIGHT A THUMP WAS HEARD AND FELT 5 HOURS INTO FLIGHT AT FL310, NO ABNORMAL INDI CATIONS OR HANDLING FOLLOWED. DURING POST FLIGHT INSPECTION, MAINTENANCE FOUND LT WING LDG EDGE WING/BODY FAIRING PUNCT URED AND CRACKED. REMOVED FAIRING PER MM 57-31, REPAIRED IAW DAC DWG PL ANS7100, SPEC DPS 1.44. & REINSTALLED FAIRING. 2 L 7 3 4F A22WE 20081212 SO 2008 12 12 SIMA200834304 1 20081201 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 918AE 5000 14500902 DURING A IMBV INSPECTION, THE BAGGAGE DOOR LOWER SILL WAS FOUND TO BE CORRODED. REMOVED CORRODED DOOR SILL. POSITIONED NEW SILL AND DRILLED. CLEANED, ALODINED AND PRIMED NEW SILL AND SILL AREA. REPAIR DONE IAW EMBRAER SRM (SRM EMB 145/1 142 REV 40) CHAPTER 51-40-02. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081212 SO 2008 12 12 SIMA200834305 1 20081203 A 5320 CHANNEL EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 907AE 5000 14500895 DURING A IMBV INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. CUTOUT A SECTION OF BEAM TO REMOVE THE CORROSION. FABRICATED FILLER AND TWO SHIMS. DRILLED PARTS, CLEANED, ALODINED AND PRIMED REPAIR PARTS. REPAIR DON E IAW EMB SRM (SRM EMB 145/1142 REV 40) CHAPTERS 53-00-10 AND 51-40-02. 2 L 7 2 4T RT T00011AT 20081212 SO 2008 12 12 SIMA200834307 1 20081203 A 5310 14525480603 BEAM EMB 145 EMB145LR 3260212 SO CARGO BAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 646AE 145213 DURING INSPECTION, FOUND CARGO DOOR SILL CORRODED. REPLACED SILL IAW EMBRAER SRM 51-40-02. AIRCRAFT WAS RETURNED TO SE RVICE. 2 L 7 2 4T RT T00011AT 20081212 NM 2008 12 12 DLM88081658 1 20081125 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 360-427 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 DEEP GOUGES ON EXTERNAL FUSELAGE SKIN FROM STA 360-427 BTW LONG 27 RT-30. GOUGES WERE BLENDED OUT IAW SRM 53-04D FIG 38 , SOME FOUND OUT OF LIMITS. DAMAGED SKIN REMOVED IAW SRM 53-04 FIG 12C. NEW SKIN INSTALLED IAW SRM 53-04D FIG 12C VIEW T AND H. REPAIR IDENTIFIED IAW PS 900-5-1 NR 4. 2 L 7 2 4F RT A6WE 20081212 NM 2008 12 12 DLM88081660 1 20081111 A 5523 TAB DOUG MD88 MD88 3023688 NM ELEVATOR UNKNOWN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 LIGHTNING STRIKES ON T/E OF RT ELEVATOR CONTROL TAB. THIS N/R CARD WAS ACCOMPLISHED IAW OPN 1031 CARD NO 1242. RT ELEV ATOR CONTROL TAB WAS BALANCED IAW SRM 55-20-2D. 2 L 7 2 4F RT A6WE 20081212 NM 2008 12 12 DLM88081662 1 20081026 A 7120 JT8D219 MOUNT DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE SCRATCHED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 48091 43173 718150 SCRATCHED INNER WALL ON FLANGE OF AFT MOUNT BOLTS FOR LT ENGINE. SCRATCHES REWORKED IAW EA 49-469467-14. WITHIN LIMITS AND NO CRACKS NOTED IAW EA 49-469467-14 REV ORIGINAL. 2 L 7 2 4F 4 F RT A6WE E9NE 20081212 SO 2008 12 12 CHQA200800236 1 20081202 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CABIN MALFUNCTIONED A CHQA K NONE O OTHER IN INSP/MAINT 1 GL 11 576RP 14500856 CAE312178 THE FLIGHT ATTENDANT STATES THAT THE EMERGENCY EXIT ROW ILLUMINATION LIGHT IS INOPERATIVE. THE LIGHT OPERATIONALLY CHEC KS GOOD IAW AMM 33-50-00. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081212 WP 2008 12 12 IXXA08SMN188S 1 20081021 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING OUTBOARD OUTER LEADING EDGE UPPER EXTERNAL SKIN CORRODED AT STATION X W 762.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INS PECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, AND FILLERS. CLEANED, TREATED, PRIMED AREA AND R EPAIR PARTS. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08548, DRAWING ED-4874 DATED 11/06/08, SRM 51-1-8 PAGES 17-18, SRM 57-2-0 PAGE 16, SRM 51-1-21, SRM 51-1-20D, NDT SPM PARTS 06-10-01-001, SRM 51-1-8B, SRM 51-1-11, SRM 51-3-0, AND SRM 51-3-1. 2 L 7 4 4F 4A25 20081212 WP 2008 12 12 IXXA08SMN189S 1 20081021 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND LT WING LOWER CENTER OUTER LEADING EDGE SKIN CORRODED AT STATION XFS 280.250.RE MOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED NEW SKIN, FILLER. CLEANED, TREATED, PRIMED AREA, AND REP AIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08548 DATED 11/18/08, DRAWING ED-4872 DA TED 11/03/08, SRM 51-1-21, SRM 51-1-20D, SRM 51-1-8 PAGES 17-18, SRM 57-2-0 PAGE 16, NDT SPM PART 06-10-01-001, SRM 51-1 -8B, SRM 51-1-11, SRM 51-3-0, AND SRM 51-3-1. 2 L 7 4 4F 4A25 20081212 SO 2008 12 12 CHQA200800237 1 20081202 A 3297 CONNECTOR EMB 145 EMB145 3260210 SO ALLSN AE3007 AE3007A 03030 GL MLG LOOSE A CHQA O OTHER J WARNING INDICATION AP APPROACH 1 GL 11 260SK 145128 CAE311802 ON THE APPROACH, THE CREW RECEIVED A LG AIR/GRND FAIL MESSAGE WHEN THE LANDING GEAR WAS SELECTED DOWN. THE INDICATION C LEARED WHEN ALL GEAR SHOWED GREEN. A NORMAL LANDING WAS MADE WITH NO INCIDENT. A LOOSE CONNECTOR WAS FOUND ON THE RIGH T MAIN LANDING GEAR PROXIMITY SWITCH. ALL CONNECTORS FOR THE AIR/GROUND PROXIMITY SWITCHES WERE CLEANED AND THE LOOSE C ONNECTOR WAS SECURED. OPERATIONAL CHECKS ARE GOOD IAW EMB 145 AMM 32-63-00. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081212 NM 2008 12 12 DL757081646 1 20081114 A 5320 SUPPORT BOEING 757 757232 1384965 NM BS 1510-1530 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 651DL 24391 CORROSION ON OTBD LOWER SURFACE OF FLOOR TO SIDEWALL SUPPORT COMMON TO NUTPLATE LOCATIONS, BS 1510-1530 RT, OUT OF LIMIT S REPLACED PART. 2 L 7 2 4F RT A2NM 20081212 NM 2008 12 12 DL76L081667 1 20081129 A 2910 290087500 LINE BOEING 767 767332 1382001 NM HYD SYSTEM LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 180DN 25985 INFLIGHT L HYD QUANTITY BLED TO ZERO WITH ASSOCIATED L HYD QTY EICAS MESSAGE. FOUND RIDGED PIPE FROM LT HYD SYS RESERVO IR SUPPLY, HOLEDSIGN(?) OF CHAFING ON HOLD OPEN STAY. REPAIRED PIPE IAW AMM 20-10-09-358-151. RAN LT HYD PUMP. NO LE AKS. LT SYSTEM FILLED. 2 L 7 2 4F RT A1NM 20081212 NM 2008 12 12 DLM88081681 1 20081115 A 5523 TAB DOUG MD88 MD88 3023688 NM RT ELEVATOR DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 DELAMINATED UPPER SKIN ON RT ELEVATOR CONTROL TAB. THIS NR WAS ACCOMPLISHED IAW OPN 1031. WEIGHT AND BALANCE CHECK TO BE ACCOMPLISHED PER NR T0111759. 2 L 7 2 4F RT A6WE 20081212 NM 2008 12 12 DL76P081701 1 20081207 A 3610 SHUTOFF VALVE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 143DA 25991 727738 LEFT ENG HPSOV ANNUNCIATED MSG ON TAXI OUT-QRH FOLLOWED, LIGHT EXTINGUISHED. FWD LEFT ENG HPSOV TO MCO/PLAC MEL 36-11-0 2 VALVE LOCKED OUT JUMPER INSTALLED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081212 NM 2008 12 12 NWAA085375644 1 20081109 A 5210 SKIN BOEING 757 757251 1384970 NM L4 DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 544US 26491 DURING L CHECK FOUND CRACK IN DOOR 4L SKIN AT STA 1658 AT THE UPPER HINGE ARM EXTERNAL CUTOUT. REPAIRED PER EA 56-21420 0. 2 L 7 2 4F RT A2NM 20081212 NM 2008 12 12 DLM88081663 1 20081030 A 5523 TAB DOUG MD88 MD88 3023688 NM LT ELEVATOR NICKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 NICKS ON LOWER SURFACE OF LT ANTI-FLOAT TAB. NICK ON LOWER SURFACE OF LT ANTI FLOAT TAB WAS REPAIRED IAW OPN 1031 CARD 1187. 2 L 7 2 4F RT A6WE 20081212 NM 2008 12 12 AALA200810412 1 20081118 A 5320 FLOOR SUPPORT BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 CORROSION ON FLOOR SUPPORT AT STATION 967 TO 987. INSTALLED SERVICEABLE FLOOR SUPPORT PER SRM 51-10-02G. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 AALA200810413 1 20081118 A 5320 STRAP BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 WEB STRAP CORRODED AT STATION 1019 TO 1022 AFT CABIN GALLEY FLOOR AREA. INSTALLED A SERVICEABLE STRAP PER SRM 53-70-51- 2R. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 AALA200810414 1 20081118 A 5320 STRAP BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 WEB STRAP CORRODED AT STATION 1018 TO 1026 AFT CABIN GALLEY FLOOR AREA. INSTALLED A SERVICEABLE STRAP PER SRM 53-70-51- 2R. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 AALA200810393 1 20081120 A 5320 ANGLE BOEING 737 737823 13844CB NM ZONE 100 PUNCTURED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 AFT CARGO LEFT TRANSITION ANGLE HAS HOLE BETWEEN STATION 727H AND STATION 727I HOLE IS THROUGH PANEL. REMOVED DAMAGED A REA AND FABRICATED NEW ANGLE, INSTALLED PER SRM 53-00-53-2R5. 2 L 7 2 4F RT A16WE 20081212 2008 12 12 QXEA2008121001233 4 20081205 A 6122 697072004 GOVERNOR BOMBDR DHC8 DHC8402 1390042 NM DOWTY R4086 R4086123F17 EU PROPELLER MALFUNCTIONED A QXEA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 19 425QX 4039 FCA- NR 1 PROPELLER WILL NOT COME OUT OF FEATHER ON ENGINE START. REPLACED NR 1 OVERSPEED GOVERNOR PER Q400 MM 61-20-26 -000-801 + 61-20-26-400-801. TESTS GOOD. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 6 C P17BO 20081212 NM 2008 12 12 AALA200810415 1 20081201 A 5320 ANGLE BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 AFT SERVICE DOOR CREASE ANGLE CORRODED STATION 945 TO 993. INSTALLED A SERVICEABLE CREASE ANGLE PER SRM 53-70-51. 2 L 7 2 4F RT A16WE 20081215 EA 2008 12 15 ASOA2008011590 1 20081201 A 5210 ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED THE PAX DOOR INNER HANDLE STRUCTURAL ANGLE. LOCATED, SEALED, AND INSTALLED A NEW ANGLE IAW CRJ 200 SRM 51-40-11 AND 51-42-06. SUPPLEMENTAL-SDR CLOSED 12/11/08. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 ASOA200801696 1 20081208 A 5320 POST CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 FS 409+128 LBL 18 LT INBOARD POST WL 69 HAS INDICATION NOTED APPROX .3 INCH LENGTH. FAILS NDT. WORK DONE IAW CRJ 200 S RM 51-42-06, CRJ 200 SRM 51-24-21 AND BOBARDIER DWG 601R32208, CRJ 200 NDTM PT 1 51-20-08, ASA CRJ 200 SRM 51-25-00, ASA CRJ 200 SRM 51-42-22. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 ASOA200801697 1 20081208 A 5320 STRUCTURE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 THE 281ELW IS CRACKED ALONG VERTICAL CORNERS. REMOVED COMPOSITE DAMAGE ALONG VERTICAL CORNER, FABBED REPAIR DOUBLER. I NSTALLED REPAIR DOUBLER USING RTV106 AND CR3523-4-4 FASTENERS PO 100782 IAW BOMBARDIER REO 601R-25-53-005. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 ASOA200801701 1 20081208 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 CARGO SEAT TRACK AT LBL 27 AT FS 559+80 IS CORRODED. 2 L 7 2 4F RT A21EA 20081215 NE 2008 12 15 CNMA20080010 2 20081102 A 7200 ENGINE DOUG DC10 DC1030 3023501 WP GE CF6 CF650E2 30018 NE NR 2 MALFUNCTIONED A CNMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 270AX 48318 455500 NR 2 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED AT TOP OF CLIMB (29,000) INTERMITTENTLY. LIGHT BECAME SOLID AFTER 3 MIN UTES. ENGINE SHUTDOWN IN FLIGHT IAW QRH PROCEDURE 4-1-2-19 AND CORRESPONDING CHECKLISTS. COMPLETED WORTAN 08-0368 R&R NR 2 ENGINE OIL STRAINER CLOGGING SWITCH PER MM 79-35 R&R SCAVENGE OIL FILTER ASSY IAW MM 79-20 R&R CLOGSWITCH CANNON PL UG & PINS PER WORTAN IAW MM 20-30 NEED LEAK CHECKED. R&R REPLACED MASTAR SYSTEM WARNING CONTROL IAW 33-15. MEGGED WIRES BETWEEN NR 2 ENG SWITCH P1-8065 & ANNUN PANEL PLUG P1-12L/3 IAW WDM 79-34-01 CHECKS NORMAL, COMPLETED VISUAL INSP OF CO MPONENTS & WIRING AS REQUIRED WORTAN 08-0368 COMPLETED AS WRITTEN. REPLACED ENGINE REMOVED SERIAL NUMBER 455-500. 2 L 7 3 4F 4 F A22WE E23EA 20081215 NM 2008 12 15 CNMA20080011 1 20081202 A 3610 CIRCUIT CARD BOEING 757 757200 1384950 NM BLEED AIR SYS FAULTY A CNMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 549AX 24528 EICAS L ENG BLEED OFF. T/S PER FIM 36-10. VISUALLY CHECK PRSOV, NO LEAK NOTED. RESEATED ECS BLEED LT CONFIG CARD. RA N ENGINE. OPS CHECK NORMAL. LT PACK OPERATION NORMAL. REPLACED LT ENG BLEED CARD IAW MM REF 36-10 GRND OPS OF BLEED S YSTEM GOOD AT THIS TIME. R&R LT ENG REVERSE FLOW CONTROL VALVE IAW MM REF 36-11, GROUND OPS CK GOOD. 2 L 7 2 4F RT A2NM 20081215 WP 2008 12 15 NWAA085369763 1 20081203 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 763NW 47396 DURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 12-15 OF THE CABIN GO OUT AFTER ABOUT 10 SECONDS. MX CHARGED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 2 L 7 2 4F A6WE 20081215 NM 2008 12 15 QXEA2008121001231 1 20081208 A 6123 AUTOFEATHER SYS BOMBDR DHC8 DHC8402 1390042 NM DOWTY R4086 R4086123F17 EU PROPELLER MALFUNCTIONED A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 19 415QX 4081 MSO - AUTO FEATHER FAILED TO ARM ABORTED TAKEOFF AT 65 KTS. RETURN TO THE GATE. PERFORMED Q400 AMM TASK 61-20-00-710-8 01 AND TASK 61-20-00-710-802 CW STATIC AND ENGINE'S RUNNING, NO DEFECTS NOTED. PERFORMED SIM TAKEOFF ON TAXIWAY, AUTOFE ATHER ARMED NORMALLY. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 6 C P17BO 20081215 WP 2008 12 15 IXXA08SMN190S 1 20081021 A 5730 SKIN DOUG DC8 DC862F 3021972 WP ZONE 500 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C-CHECK INSPECTION, FOUND LT WING INBOARD OUTER L/E UPPER EXTERNAL SKIN CORRODED AT STATION XFS 560.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFOR MED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED DOUBLER, FILLER. CLEANED, TREATED, PRIMED AREA, AND R EPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NR 08549 DATED 11/24/08, DRAWING ED-4873 DATE D 11/03/08, SRM 51-1-21, SRM 51-3-0, SRM 51-1-8 PAGES 17-18, SRM 57-2-0 PAGE 16, NDT SPM PART 06-10-01-001, SRM 51-1-8B, SRM 51-1-11, AND SRM 51-3-1. 2 L 7 4 4F 4A25 20081215 2008 12 15 QMLA1127200808055 4 20081127 A 2210 41800876800 ACTUATOR UROCOP EC135 EC135T2 5620028 SW T/R CONTROL INOPERATIVE E QMLA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AA AIR AMBULANCE 1 NM 03 235UW 837 0548 ON SHORT FINAL AT STOUGHTON HOSPITAL HELIPAD CAUTION LIGHT ILLUM AND CAD INDICATED YAW SAS AND ACTUATION LIGHTS WITH A C ORRESPONDING AMBER "Y" ON THE PFD. INITIATED A GO AROUND. AS POWER WAS APPLIED THE MASTER WARNING PANEL ILLUMINATED AND THE AP A. TRIM LIGHT ILLUMINATED ALONG WITH THE DISCONNECT OF THE AUTOPILOT, P SAS, P/R SAS CAD LIGHTS. GO AROUND WAS CO NTINUED AND PILOT WAS ABLE TO RESET P SAS, P/R SAS AND THE AUTOPILOT, CLIMB TO SAFE ALTITUDE AND AIRSPEED AND FM WAS CHE CKED FOR PROPER PROCEDURE. YAW SAS AND ACTUATION LIGHTS WOULD NOT RESET. FLIGHT RETURNED TO BASE AND MAINT WAS ALERTED. 1 G 7 2 3U H88EU 20081215 NE 2008 12 15 A6WA200840619 2 20081127 A 7261 SCAVENGE PUMP CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE LT ENGINE MALFUNCTIONED A A6WA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 31 406AW 7402 24040 LOG 192858/1&2 LOSS OF LT OIL PRESSURE INFLIGHT AT FLIGHT LEVEL 340. COMPLIED QRH SHUTDOWN LT ENGINE. R&R LT ENG SCAVA NGE PUMP IAW AWAC 70-21-01. PERFORMED OIL CONSUMPTION CHECK AND OK LEAK CHECK. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 20081215 EA 2008 12 15 A6WA200840618 1 20081126 A 2750 ECU CNDAIR CL600 CL6002B19 1900309 EA TE FLAP MALFUNCTIONED A A6WA O OTHER J WARNING INDICATION AP APPROACH 1 GL 31 452AW 7835 LOG 192018/1 ON APPROACH HAD FLAPS FAIL MSG. WHEN FLAPS SELECTED TO 8 FLAP INOPERATIVE CAUTION MSG DISPLAYED. COMPLIED WITH FIM 27-50-00. FAULTS FOUND LEAD TO INTERNAL FECU/BPSU MISS RIG. R&R FECU IAW AMM 27-51-05. OPS CHECK GOOD. RIG CHECK GOOD AT THIS TIME REF AMM 27-51-10. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 ASOA200801290 1 20081201 A 5210 ANGLE CNDAIR CL600 CL6002B19 1900309 EA PAX DOOR UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED THE PAX DOOR INNER HANDLE STRUCTURAL ANGLE. LOCATED, SEALED AND INSTALLED A NEW ANGLE IAW CRJ 200 SRM 51-40-11 AND 51-42-06. SUPPLEMENTAL - SDR CLOSED 12/11/08. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 ASOA208801595 1 20081201 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE UNKNOWN A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 REMOVED AND REPLACED LT/RT OBLIQUE ANGLES AT FS 625 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. SUPPLEMENTAL - SDR CLOSED 12 /11/08. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 ASOA200801689 1 20081202 A 5320 SUPPORT BEAM CNDAIR CL600 CL6002B19 1900309 EA CARGO BAY CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 925EV 7831 CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX 1.3 INCH IN LENGTH. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 ASOA200801694 1 20081207 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX .2 INCHES IN LENGTH. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 ASOA200801704 1 20081208 A 5320 ANGLE CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 FS 484 ANGLE RBL 27 IS CRACKED IN RADIUS. REMOVED CLIP AND RIVETS AND INSTALLED NEW CLIP AND RIVETS IAW CRJ 200 SRM 51- 42-06, 51-42-20, AND REO 601R-53-41-059. REQUIRES PAINT AND DYNATROL. PAINTED REPAIRED AREAS AT FS 484 ANGLE RBL 27 IA W CRJ SRM 51-25-01. ALSO APPLIED DYNATROL TO REPAIRED AREAS IAW CRJ SRM 51-21-11. 2 L 7 2 4F RT A21EA 20081215 CE 2008 12 15 HAEA20000206 1 20081212 A 5730 SKIN LEAR 24 24E 5170316 CE LT WING TIP TANK DAMAGED E HAEA K NONE O OTHER UK UNKNOWN 1 SW 05 330TW 13762 91 24330 LT TIP TANK DAMAGED AND DENTED ON AFT LOWER SURFACE. TIP TANK REMOVED AND AFT CONE REMOVED TO EVALUATE DAMAGE. DISCOVE RED AFT CENTER BULKHEAD DEFORMED, INNER ATTACH DOUBLER DEFORMED AND LOWER SEAM RIVETS SHEARED. TIP TANK REQUIRES REPAIR FOR RETURN TO SERVICE. 2 L 7 2 4J A10CE 20081215 NM 2008 12 15 AALA200810395 1 20081122 A 5340 BRACKET BOEING 737 737823 13844CB NM ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 BRACKET CRACKED IN RADIUS UNDER RIGHT TRANSITION PANEL IN AFT CARGO, STATION 500E FORWARD SIDE BETWEEN BELLFRAME AND INT ERCOSTAL. REMOVED AND REPLACED BRACKET PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 AALA200820082 1 20081111 A 5320 146N5391142 PANEL BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 666A 52891 25300 TRANSITION PANEL CORRODED, REPAIRED TRANSITION PANEL IAW SRM 51-10-02. 2 L 7 2 4F RT A2NM 20081215 EA 2008 12 15 SWIA200820615 1 20081207 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 926SW 7687 FLT 5998 - OVERHEAD EMERGENCY LIGHT AT LAV DOOR INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 DU4R2008269 1 20081207 A 5730 SKIN BOEING 757 75723APF 1384966 NM LT WING CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 868AN 24868 DURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND CORROSION ON LT WING AFT SPAR UPPER CHANNEL, SKIN FROM FUS ELAGE TO WING TIP. 2 L 7 2 4F RT A2NM 20081211 NM 2008 12 11 DU4R2008270 1 20081207 A 5320 SUPPORT BOEING 757 75723APF 1384966 NM FUSELAGE CORRODED B DU4R K NONE O OTHER IN INSP/MAINT 1 SO 15 868AN 24868 DURING SCHEDULED INSPECTION AT TIMCO-LCQ, LAKE CITY, FL FOUND LT WHEEL WELL (MLG) WTB FAIRING SUPPORT ARE CORRODED THROU GHOUT AT BS 1040 - 1060 LBL 40 - 651. 2 L 7 2 4F RT A2NM 20081211 NM 2008 12 11 QXEA2008121001204 1 20081125 A 5330 SKIN BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 412QX 4059 PDX - C4 - SCRATCH ON RT FUSELAGE SKIN PANEL AT APPROX STA X151.00 AND Z99.00. REMOVED PAINT, BLENDED OUT SCRATCH REF R D8/4-53-666 PAGE 2,3,4. AND REF SRM 51-26-10. HFEC INSPECTED AREA FOR CRACKS IAW NDTM PART 6 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECKED AREA IAW NDTM PART 1, 51-00-04. FOUND TO BE WITH LIMITS REF RD8/4-53-505 PAGE 2. ALODINED, PRIM ED AND PAINTED REF SRM 51-26-10, 51-25-10 AND 51-25-15. 2 H 7 2 4T RT A13NM 20081211 NM 2008 12 11 QXEA2008121001205 1 20081125 A 5310 STRUCTURE BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 412QX 4059 PDX - C4 - SUSPECT CORROSION AROUND STRAKE UPPER BOLT HOLE AT APPROX X624.5 AND Z97.500. INSPECTED STRAKE UPPER BOLT HO LE AND FOUND MINOR CORROSION, BLENDED OUT IAW RD8/4-53-666 PG 5 NOTE 1. HFEC INSPECTED AREA FOR CRACKS IAW NDTM PART 6 51-00-01. NO CRACKS NOTED. UT THICKNESS CHECKED AREA IAW NDTM PART 1, 51-00-04 HIGH .060 LOW .058. COMPLETED REPAIR I AW RD8/4-53-666 PG 5 NOTES 3-5. 2 H 7 2 4T RT A13NM 20081211 NM 2008 12 11 UPS08B54086 1 20081203 A 5330 SKIN BOEING 747 74745E 1384947 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 578UP 27154 INSPECTION TYPE:N/A HOLE IN FUSELAGE 40 INCHES FWD OF LWR AFT CARGO DOOR BS 1770, BETWEEN STRINGERS 28R & 29R. FABRICAT ED PATCH PER EO B747-5330-31394A, AND SRM 53-00-01 OUT OF 2024 -T-3 .125 CLEANED DAMAGE ON A/C REPAIRS MATERIAL AND A/C ETCHED, ALODINE & PRIMED PER SRM 51. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 REPAIR 1 DETAIL III USING HI-LOC HL111VA Z8-6 HL11VAZ8-6. SEALANT 870 BY 1/2 IAW EO B747-5330-31394A, M5100-21238B2, M-5100-19877-D. RCD C/W. 2 L 7 4 4F RT A20WE 20081211 NM 2008 12 11 UPS08554091 1 20081207 A 5321 144N531636 FLOOR PANEL BOEING 757 75724APF 1384969 NM MAIN DECK DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 467UP 25483 INSPECTION TYPE:N/A MAIN DECK FLOOR PANEL POS 8 HAS HOLE. REPAIRED PER SRM 53-00-50-2R. 2 L 7 2 4F RT A2NM 20081211 WP 2008 12 11 UPS08854093 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR 803-F1-11, STA 40-45, L28L-L29L HAS NO SRM REFERENCE AND REQUIRES EO APPX F. REMOVED EXISTING REPAIR. REPAIRED AREA PER TR 53-205 OF DC8 SRM 53-2- 00-0 PARA 22A. 2 L 7 4 4F RT 4A25 20081212 SO 2008 12 12 C2XA08IA250 1 20081130 A 3610 40303920SD O-RING EMB 145 EMB145LR 3260212 SO BLEED AIR SYS FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 12900 145511 CVG - FLIGHT 2770, DURING CLIMBOUT THE CREW REPORTED A NR 1 BLEED LEAK. THE AIRCRAFT RETURNED TO CVG WHERE IT LANDED WI THOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BLEED O-RINGS IN THE AFT CABIN AND FORWARD CARGO, OPERATIONALLY CH ECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081212 NM 2008 12 12 HNAA2008121000342 1 20081210 A 3350 1619 LIGHT DHAV DHC8 DHC8102 2809003 NM EXTERIOR DEFECTIVE A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 942HA 50425 50425 163 DURING RON MAINTENANCE, THE LEFT FORWARD EMERGENCY EGRESS LIGHT WAS FOUND TO BE DIM. THE BULB WAS REPLACED AND LIGHTING , OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 20081212 NM 2008 12 12 HNAA2008121000343 1 20081210 A 3350 1619 LIGHT DHAV DHC8 DHC8102 2809003 NM EXTERIOR DEFECTIVE A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 56314 56314 053 DURING ROM MAINTENANCE, THE LEFT FORWARD EMERGENCY EGRESS LIGHT WAS FOUND TO BE DIM. THE BULB WAS REPLACED AND LIGHTING , OPS CHECKED GOOD. 2 H 7 2 4T RT A13NM 20081212 NM 2008 12 12 AALA200810389 1 20081121 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM ZONE 100 CORRUPTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 TOP OF FLOORBEAM CORRODED AT STATION 986 AND BUTT LINE 42 LEFT. INSTALLED REPAIR ANGLE PER AARD 53-00-00-7. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 AALA200820077 1 20081111 A 5320 146N5391142 PANEL BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 666A 52891 25300 TRANSITION PANEL CORRODED. REPLACED TRANSITION PANEL IAW SRM 51-10-02. 2 L 7 2 4F RT A2NM 20081212 NM 2008 12 12 FDEA200811144879 1 20081114 A 5330 6518220 SKIN BOEING 727 7272S2F 1384O81 NM ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 LT EXTERIOR FUSELAGE BS 720D, 12 STR 19L SKIN LAP JUST FWD OF WING LE, SKIN HAS WEAR REPAIRED FUSE SKIN AT STA 720D 12 S TR 19L REF SRM 53-30-3 FIG 5. DISPLACED LEFT INBD LEADING EDGE FOR REPAIR AND REINSTALLED REF SRM 51-30-2 PG 1-5. DISC ONNECTED LEADING EDGE PNEUMATIC DUCT AND REINSTALLED AND LEAK CHECKED REF MM 36-13-00-4 PG4. THIS IS CLASSIFIED AS A MA JOR REPAIR. 2 L 7 3 4F A3WE 20081212 EU 2008 12 12 AALA200820079 1 20081113 A 5710 STRUCTURE AIRBUS 300 A300B4605R 3930308 EU ZONE 600 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 70073 53863 0516 RT WING ROOT LEADING EDGE HAS DAMAGE. REPAIRED IAW SRM 51-70-00-2. 2 L 7 2 4F RT A35EU 20081212 EU 2008 12 12 AALA200820080 1 20081111 A 5340 A5361068859301 FITTING AIRBUS 300 A300B4605R 3930308 EU ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 19059 53486 0469 FOUND UPPER FUSELAGE FITTING CRACKED. REPLACED FITTING IAW SRM 53-12-81-0 ITEM NR 180A. 2 L 7 2 4F RT A35EU 20081215 2008 12 15 SWIA200820609 2 20081204 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO RIGHT OVERSPEED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 584SW 120352 FLT 5700 - RIGHT NP WENT TO 103 PERCENT DURING TAKE OFF. ACCOMPLISHED ENGINE RUNS, UNABLE TO DUPLICATE. 2 L 7 2 4T RT A31SO 20081215 EA 2008 12 15 SWIA200820614 1 20081208 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 963SW 7865 FLT 6274 - NR 1 EMERGENCY FLOOD LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081215 NE 2008 12 15 DLM88081703 2 20081208 A 7261 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 INTERNAL LEAKING A DALA O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 937DL 44379 49810 725820 CREW REPORTS OILY SMELL/ODOR IN CABIN AFTER TAKEOFF. DISSIPATED. FOUND NR 1 ENG CREATING SMOKE AND ODOR WHILE PERFORMI NG OPN 5088. ENGINE CHANGE. 2 L 7 2 4F 4 F RT A6WE E9NE 20081215 NM 2008 12 15 QXEA2008121001232 1 20081206 A 2721 82410608007 CONTROL PANEL BOMBDR DHC8 DHC8402 1390042 NM RUDDER TRIM MALFUNCTIONED A QXEA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 NM 19 411QX 4055 PDX - RUDDER TRIM DOES NOT ENGAGE, WHEN TURNING KNOB RIGHT KNOB IS TURNED WELL PAST THE 1/2 WAY POINT WORKS CORRECTLY LE FT. REMOVED AND REPLACED RUDDER/AILERON TRIM CONTROL PANEL. C/W AILERON TRIM OPERATIONAL TEST REF DH-8 400 MM 27-13-00 -710-802. C/W RUDDER TRIM OPERATIONAL TEST REF DH-8 400 MM 27-22-00-710-801. NO FURTHER DEFECTS NOTED. RETURNED TO SE RVICE. 2 H 7 2 4T RT A13NM 20081211 EA 2008 12 11 SWIA200820606 1 20081203 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHTS BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 506CA 7793 FLT 2682 - OVERHEAD EMERGENCY LIGHT SECOND FROM AFT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081211 NM 2008 12 11 QXEA2008121001208 1 20081125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 412QX 4059 PDX - C4 - NR 9 SEAT TRACK HAS CORROSION AT FUSELAGE STATION APPROX 708 TO 714. BLENDED AREA ON NR 9 SEAT TRACK AT APPR OX STA X709 ON UPPER SURFACE IAW RD 8/4-53-884 MATERIAL REMOVED .032, BLENDED AREA OUT OF LIMITS IAW ABOVE. REMOVED NR 9 SEAT TRACK INSTALLED NEW NR 9 SEAT TRACK REF SRM 51-42-05 AND 51-40-15. 2 H 7 2 4T RT A13NM 20081211 2008 12 11 UPS08M54103 4 20081205 A 2565 COVER DOUG MD11 MD11F 3023600 NM EVAC SLIDE OUT OF POSITION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 286UP 48453 INSPECTION TYPE:N/A SLIDE CASING ON L1 DOOR IS ASKEW AND INTERFERES WITH DOOR OPENING. INSTALLED SLIDE CASING DOOR L1 C ORRECTLY REF MM 25-61-05. OK FOR SERVICE. 2 L 7 3 4F RT A22WE 20081212 NM 2008 12 12 AALA200810402 1 20081125 A 5312 BULKHEAD BOEING 737 737823 13844CB NM ZONE 200 CANNING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 AFT PRESSURE BULKHEAD OIL CANNING BETWEEN 10 O'CLOCK AND 12 O'CLOCK POSITION. REPAIRED PER ESO 61000 DATED 11-24-08. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 AALA200810384 1 20081124 A 5320 SUPPORT BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 GALLEY WALL SUPPORT AT STATION 991 BETWEEN BUTT LINE 34 LEFT AND BUTT LINE 45 LEFT CORRODED. INSTALLED NEW GALLEY WALL SUPPORT PER SRM 53-10-51. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 AALA200810390 1 20081117 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 TOP OF FLOORBEAM CORRODED STATION 948 AND BUTT LINE 40 RIGHT. INSTALLED REPAIR DOUBLER PER SRM 53-00-51. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 AALA200820078 1 20081111 A 5320 146N54512 BRACKET BOEING 757 757223 1384957 NM ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 666A 52891 25300 FORWARD CARGO VERTICAL CHANNEL ON FORWARD SIDE OF FLOORBEAM CRACKED. REPLACED BRACKET IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20081212 SO 2008 12 12 CHQA200800239 1 20081203 A 3620 8166248 THERMOSTAT EMB 135 EMB135KL 3260302 SO ALLSN AE3007 AE3007A 03030 GL BLEED SYSTEM FAULTY A CHQA O OTHER J WARNING INDICATION CL CLIMB 1 GL 11 372SK 1667 145538 CAE311903 THE CREW RECEIVED A BLEED 2 OVERTEMP MESSAGE DURING CLIMB THROUGH ICING CONDITIONS WITH AN ASSOCIATED ARROW IN THE RED O N THE MFD. THE NR 2 THERMOSTAT WAS REPLACED IAW EMB AMM 36-20-01 AND OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081212 NM 2008 12 12 DLM88081655 1 20081021 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 674 STR 21L DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 DUE ERA 093410-14 REV A FUSELAGE SKIN STA 674 STR 21L REPAIR OF DENT. ACCOMPLISH PERM REPAIR AT NEXT HMV. DAMAGED AREA WAS CUT OUT IAW SRM 53-04 FIG 12C. REPAIR PARTS WERE FABRICATED IAW 53-04D FIG 12C. REPAIR PARTS WERE INSTALLED IAW S RM 53-04D FIG 12C AND IDENTIFIED IAW PS 900-1-4 NO 04. 2 L 7 2 4F RT A6WE 20081212 NM 2008 12 12 AALA200810382 1 20081124 A 5320 FLOOR SUPPORT BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 FLOOR SUPPORT CORRODED AT STATION 958 AND BUTT LINE 49 RIGHT. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-70-51. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 AALA200810392 1 20081119 A 5330 SKIN BOEING 737 737823 13844CB NM ZONE 200 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 DENT IN FUSELAGE SKIN JUST BELOW STRINGER 3 LEFT AT STATION 328. INSTALLED REPAIR AS PER SRM 53-00-01. 2 L 7 2 4F RT A16WE 20081212 SO 2008 12 12 SIMA200834302 1 20081204 A 3260 8005701 PROXIMITY SWITCH EMB 135 EMB135LR 3260305 SO NLG MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 716AE 145264 ON FLIGHT 4728, CREW REPORTED THAT AT APPROX 7700 FEET THEIR NOSE DOORS HAD COME DOWN UNCOMMENTED AFTER GEAR RETRACTED. THEY HAD NO OTHER ABNORMAL INDICATIONS OTHER THAN A LOT OF NOISE AND SLIGHT DRAG. CREW RETURNED TO RDU. AIRCRAFT REMO VED FROM SERVICE. REMOVED AND REPLACED NOSE LAND GEAR UP PROX SWITCH AND NOSE LANDING GEAR DOOR RELAY. OPERATIONAL CHE CKED GOOD. AIRCRAFT RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 20081215 NM 2008 12 15 NOCA08708 1 20081210 A 3350 20121 CHARGER BOEING 767 767324 1385203 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 767NA 27569 DURING DAILY CHECK FOUND EMERGENCY FLOOR PATH LIGHTING INOP ROWS 11-27 LT OF A/C. REPLACED EMERGENCY FLOOR PATH LIGHTIN G CHARGER ASSY PER MM 33-51-07, OPS CHECK OK. 2 L 7 2 4F RT A1NM 20081215 NM 2008 12 15 SWAA086967 1 20081209 A 5610 571761 WINDOW BOEING 737 7373H4 1384600 NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 29 602SW 27953 R1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086953 1 20081208 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 455WN 32462 DURING SCHEDULED MV1 CHECK, FOUND FWD EEPLS LIGHT COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087028 1 20081210 A 5312 6517582 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 DURING SCHEDULED SPV CHECK, FOUND BS 178 BULKHEAD VERTICAL WEB CRACKED, LBL 17, WL 228. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087029 1 20081210 A 5311 6963820 FRAME BOEING 737 7373H4 1384600 NM BULKHEAD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 DURING SCHEDULED SPV CHECK, FOUND BS 178 BULKHEAD CHORD CRACKED, LBL 17, WL 218. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087030 1 20081211 A 3350 417N5120 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 631SW 27706 DURING SCHEDULED MV4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 22. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081215 2008 12 15 SWAA087032 4 20081211 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 913WN 29840 FOUND L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086968 1 20081210 A 5311 65C22909 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086960 1 20081208 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727, RBL 24. REPAIRED CHORD PER ER. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086961 1 20081209 A 5754 65C26602 SKIN BOEING 737 7373H4 1384600 NM LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 L/E SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED SLAT PER MM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087001 1 20081210 A 5322 6546546 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087002 1 20081210 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 932, STR 21R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087038 1 20081211 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20090129 NM 2009 1 29 DHLA2009743554 1 20081127 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 BS 700 MAIN FRAME HAS DOUBLE DRILLED HOLES BETWEEN STR 13L AND 17L. ACCOMPLISHED FRAME REPAIR IAW B727 SRM 51-40-3 FIG 1 AND 53-10-4 FIG 1 BETWEEN STR 11L AND 17L. 2 L 7 3 4F A3WE 20090129 NM 2009 1 29 DHLA2009743555 1 20081125 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 BS 460 MAIN FRAME INBD FLANGE HAS ELONGATED HOLES BETWEEN STR 6R AND 7R. ACCOMPLISHED FRAME REPAIR IAW SRM 53-10-4 FIG 1. 2 L 7 3 4F A3WE 20090129 SO 2009 1 29 SWIA200820903 1 20081024 A 5320 BUTTSTRAP EMB 120 EMB120ER 3260203 SO CARGO BAY CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 229SW 120305 C-CHECK, CARGO COMPARTMENT LEFT OUTBOARD FLOOR BUTT STRAP CORRODED. REPLACED PER SRM. 2 L 7 2 4T RT A31SO 20090130 EU 2009 1 30 NWAA09133211 1 20081213 A 2913 PUMP AIRBUS 320 A320211 3930320 EU HYD SYSTEM MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 01 311US 125 OUT OF AIRPORT, AT APPROX 20,000 FT, RECEIVED "HYD GREEN RSVR LO LVL" CAUTION. FOLLOWED COM, LANDING GEAR GRAVITY EXTEN DED AND LANDED UNEVENTFULLY. CORRECTION WAS TO REPLACE HYD LINE IN LT WHEEL WELL AND NR 1 ENG DRIVEN PUMP IAW LOG PAGES 4568789 AND 0011489. (K) 2 L 7 2 4F RT A28NM 20090130 NM 2009 1 30 UPS09654409 1 20081229 A 5321 141T585613 FLOOR PANEL BOEING 767 76734AF 1385212 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE:C M/D STA 410 WL 200 RBL 83 FLOOR PANEL FOUND REPAIR PATCH. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R . 2 L 7 2 4F RT A1NM 20090130 WP 2009 1 30 FDEA200804271611 1 20080427 A 2150 3966361 FLOW VALVE DOUG MD10 MD1010F 3022112 WP NR 2 A/C PACK FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 21 384FE 21471 649 46617 RECEIVED A LEVEL 1 PACK 2 FLOW DISAG ALERT IN FLIGHT 6 TIMES. REMOVED AND REPLACED PACK 2 FLOW CONT VALVE, REF MM 21-51 -02-4. REMOVED AND REPLACED PACK 2 FLOW TRANSMITTER, REF MM 21-52-01-4. OPS AND LEAK CHECK OK. 2 L 7 3 4F RT A22WE 20090128 WP 2009 1 28 NWAA085729858 1 20081226 A 3350 RELAY DOUG DC9 DC951 3022051 WP EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 767NC 47724 DURING LINE CHECK, MX FOUND THAT THE RT EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MX REPLACED THE PERTINENT POWER RELAY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. (K) 2 L 7 2 4F RT A6WE 20090129 SO 2009 1 29 SWIA200820900 1 20081026 A 5310 DOOR FRAME EMB 120 EMB120ER 3260203 SO FUSELAGE CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 229SW 120305 C-CHECK, PASSENGER DOOR ENTRANCE THRESHOLD LOWER FRAME CORRODED. REPLACED PER SRM. 2 L 7 2 4T RT A31SO 20090129 NM 2009 1 29 DHLA2009770AT530 1 20081210 A 5314 KEELBEAM BOEING 727 7272B7 138407L NM ZONE 100 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 770AT 21953 LOWER FUSELAGE AIR CONDITIONING BAY AT BS 740 KEEL BEAM LOWER LEFT CHORD WITH CRACK. REPAIRED FUSELAGE LEFT SIDE KEEL B EAM LOWER CHORD AT HORIZONTAL FLANGE SECTION FROM BS 740 TO BS 748 LBL 7 IAW COOPESA EO-COO-2-53-503-08 DTD 12/24/08 AND BOEING MESSAGE 1-1127202504-3 DTD 12/23/08 DOCUMENTED ON FAA FORM 8100-9. 2 L 7 3 4F A3WE 20090130 NM 2009 1 30 UPS09M54257 1 20081231 A 5297 CONNECTOR DOUG MD11 MD11F 3023600 NM R1 DOOR INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 259UP R1 DOOR INOP ELEC AND PNEUMATIC. DEFERRED IAW MEL 391975. REF WDM 52-11-01 FOUND UP LIMIT SWITCH 51-588 TO HAVE INTERMI TTENT HIGH RESISTANCE FROM PINS E TO D. REPLACED 51-588. DOOR CHECKS GOOD. 2 L 7 3 4F RT A22WE 20090130 NM 2009 1 30 UPS09654402 1 20080119 A 5321 141T585647 FLOOR PANEL BOEING 767 76734AF 1385212 NM CABIN PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 320UP 27747 INSPECTION TYPE:N/A FLOOR PANEL 3 PUNCTURES. REPAIRED PER EO B767-5320-31943-A. 2 L 7 2 4F RT A1NM 20090130 NM 2009 1 30 UPS09654408 1 20081230 A 5321 141T585612 FLOOR PANEL BOEING 767 76734AF 1385212 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE:C M/D STA 363 WL 200 RBL 71 FLOOR PANEL FOUND REPAIR PATCH. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R . 2 L 7 2 4F RT A1NM 20090130 EU 2009 1 30 HCM2009F00000 1 20081225 A 5610 WINDSHIELD UROCOP EC130 EC130B4 8680989 EU TMECA ARRIEL ARRIEL2B1 60056 NE COCKPIT BROKEN E HCMA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 11QL 3738 3738 ACFT DEPARTED AIRPORT ON A TOUR FLIGHT AT APPROX 3:20 PM, WHILE FLYING AT 2500 FT, APPROX 100 KNOTS IAS A BIRD STRUCK TH E CENTER WINDSHIELD OF THE ACFT, SHATTERING THE UPPER SECTION OF THE WINDSHIELD, THE DEAD BIRD CAME INTO THE CABIN. THE PILOT IMMEDIATELY SLOWED DOWN AND PROCEDED TO THE AIRPORT AND MADE A PRECAUTIONARY LANDING. NO SERIOUS INJURIES OCCURR ED. MX PERFORMED A DETAILED CHECK OFTHE ACFT, CABIN STRUCTURE AND OTHER WINDSHIELDS, NO FURTHER DEFECTS FOUND. THE DAM AGED WINDOW WAS REMOVED AND REPLACED IAW MFG MM. (K) 1 G 7 2 3U 3 U H9EU E00054EN 20090130 WP 2009 1 30 FDEA200806102213 1 20080610 A 3260 39140165501 CYLINDER DOUG MD10 MD1010F 3022112 WP RT MLG DAMAGED A FDEA O OTHER J WARNING INDICATION TO TAKEOFF 1 CE 21 363FE 48263 UPON GEAR RETRACTION HAD RED LIGHT IN PRIMARY RT MAIN INDICATOR. CONFIRMED IN SECONDARY. RAN GEAR PRIMARY OR SECONDAR Y LT(S) ILLUMINATE WITH GEAR HANDLE UP CHECKLIST. RETURN TO KMEM. NO PROBLEMS ON ROLLOUT. REMOVED AND REPLACED RT ML G BUNGEE CYLINDER, ROD END BROKE IN HALF. 2 L 7 3 4F RT A22WE 20090203 EA 2009 2 3 SWIA200820908 1 20081231 A 5315 FLOORBEAM CNDAIR CL600 CL6002D24 1390016 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 805SK 15069 DURING C-CHECK, FS 280 BEAM CRACKED AT LBL11.25. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20090130 WP 2009 1 30 FDEA200807012615 1 20080701 A 2611 SMOKE DETECTOR DOUG MD10 MD1010F 3022112 WP CARGO BAY FAILED A FDEA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 CE 21 554FE 46708 AT FL 350 GOT LEVEL 3 LOWER FWD CARGO FIRE FLASHING DISCHARGE SWITCH/FIRE WARNING. DISCHARGED AGENT AND LANDED FIRE CRE W FOUND NO FIRE EVIDENCE ON A/C. REMOVED AND REPLACED 4 SMOKE DETECTORS IN LOWER FORWARD CARGO COMPARTMENT. 2 L 7 3 4F RT A22WE 20090130 WP 2009 1 30 FDEA200807012617 1 20080701 A 5610 ABA73181 SEAL BOEING DOUG MD10 MD1010F 3022112 WP WINDOW WORN A FDEA O OTHER O OTHER CR CRUISE 1 CE 21 68057 AA30 48264 LOUD NOISE THAT APPEARED TO COME FROM THE CAPT'S SLIDING WINDOW AREA. A VIBRATION COULD BE FELT ON THE POST IN THE WIN DOW ARM. BUT COMMUNICATION WAS NEARLY IMPOSSIBLE WITH ATC. EVENTUALLY AN EMERGENCY WAS DECLARED. LOWER ALTITUDE AND L OWER AIRSPEED HELPED. NOISE REMAINED UNTIL DESCENT BELOW 19,000 FT AND FL 270. REMOVED AND REPLACED CAPTS SLIDING WIND OW FRAME INNER SEAL. 2 L 7 3 4F RT A22WE 20090130 EU 2009 1 30 FDEA200807122844 1 20080712 A 2780 518B000001 JACKSCREW AIRBUS 310 A310324 3930206 EU SLATS LEAKING A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 CE 21 805FD 3676 3676 456 SLATS STUCK AT 0 DEG, C/W QRH. EMERGENCY DECLARED, LANDED UNEVENTFULLY AT SYR. REMOVED AND REPLACED RIGHT NR 2 JACKSCR EW ASSY PER A310-300MM ATA 27-84-22-4. 2 L 7 2 4F RT A35EU 20090130 WP 2009 1 30 FDEA200809053747 1 20080905 A 7797 J0112292062 WIRE DOUG MD10 MD1010F 3022112 WP ENGINE CHAFED A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 399FE 50742 48262 NR 2 ENGINE SHUTDOWN IN FLIGHT. ON CLIMB-OUT PASSING FL 250 HAD A LEVEL 1 NR 2 ENGINE EGT EXCEEDANCE. PER CHECK LIST B ROUGHT POWER BACK. TEMP CAME DOWN WITHIN LIMITS BUT SHORTLY CLIMBED BACK ABOVE REDLINE AND HAD A NR 2 EGT HIGH LEVEL 2. SHUT ENGINE DOWN AND RETURNED TO LAND PER CHECKLIST. FOUND WIRES J011-229-20GR AND J011-229-20WH CHAFED THRU SHIELDIN G AND INTO CONDUCTORS INSIDE OF J BOX, APPROX 6 INCHES BACK FROM PLUG R5-8216. AFTER EA 8-7720-123490, RETERMINATED NR 2 ENG EGT WIRES PER MD10-10 WDM 77-21-01. CONTINUITY CHECK 'OK'. ENG AT MAX ASSURANCE POWER PER MD10-10 JRH ALL PERIME TERS GOOD. OPS CK GOOD. 2 L 7 3 4F RT A22WE 20090130 WP 2009 1 30 FDEA200809093782 1 20080909 A 2913 3508806 PUMP DOUG MD10 MD1010F 3022112 WP HYD SYSTEM LEAKING A FDEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 21 366FE 3009 46602 35 MINUTES INTO FLT, ENG NR 2 OIL QTY DROPPED TO ZERO, TEMP 7 PRESSURE NORMAL. PRESSURE FLUCTUATED CONSTANTLY DECREASI NG TO APPROX (15 PSI) FLUCTUATING /- 5 PSI WHEN ENGINE WAS SHUT DOWN IN ACCORDANCE W/QRH. WINDMILLING PRESSURE GREATER THAN 2 PSI. REPLACED NR 2 ENGINE UPPER HYDRAULIC PUMP. 2 L 7 3 4F RT A22WE 20090202 NM 2009 2 2 UPS09M54413 1 20081229 A 5753 ARC73611 VANE DOUG MD11 MD11F 3023600 NM TE FLAP CHAFED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:1C LT WING OUTBOARD FLAP VANE OUTBOARD EDGE FOUND CHAFE MARK. REPAIRED LT WING OUTBOARD FLAP OUTBOARD E DGE REF MD11 SRM 51-62-01 VOL II PARA 8F. 2 L 7 3 4F RT A22WE 20090202 NM 2009 2 2 UPS09M54415 1 20081230 A 5330 SKIN DOUG MD11 MD11F 3023600 NM FUSELAGE WRINKLED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:1C REPAIR SURVEY SEQUENCE F1-289-07 HAS WRINKLING ON FUSELAGE SKIN ON FWD END OF FLUSH REPAIR. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW UPS EO MD11-5330-31957-A. 2 L 7 3 4F RT A22WE 20090202 NM 2009 2 2 USAA2009012390131 1 20081224 A 5320 65C3267723 WEB BOEING 737 7373G7 138447J NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - CRACK ON WEB AT BS 987.5, RBL 40. REPAIRED WEB AT BS 987.5, RBL 40 IAW B737 SRM 51-10-02-0G. 2 L 7 2 4F RT A16WE 20090202 NM 2009 2 2 USAA2009012390132 1 20081227 A 5320 654659211 CHANNEL BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - CORROSION ON CHANNEL BETWEEN BS 787 TO BS 947, LBL 12.5. REPAIRED CHANNEL BETWEEN BS 787 TO BS 947, LBL 12.5 IAW B737 SRM 53-00-53. 2 L 7 2 4F RT A16WE 20090202 NM 2009 2 2 UPS09M54405 1 20081230 A 7110 2210503515 SKIN DOUG MD11 MD11F 3023600 NM NR 1 COWLING DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 289UP 48455 INSPECTION TYPE:1C NR 1 ENG OUTBOARD FAN COWL HAS DELAMINATED SKIN AT TOP SIDE CENTER SECTION UNDER CENTER HINGE. REPAI RED NR 1 OUTBOARD FAN COWL UPPER CENTER AREA REF MD11 VOL IV SRM 54-20-00 PARA 11 REPAIR 8. 2 L 7 3 4F RT A22WE 20090202 NM 2009 2 2 USAA2009012190107 1 20081226 A 5320 69434961 WEB BOEING 737 7373G7 138447J NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 305AW 24012 SAL - C19 - MAJOR REPAIR - GALVANIC CORROSION ON UPPER WEB AT S26R BETWEEN BS 847 TO BS 867. REPAIRED UPPER WEB AT S26R BETWEEN BS 847 TO BS 867 IAW B737 SRM 51-40-02. 2 L 7 2 4F RT A16WE 20090203 WP 2009 2 3 CVG2009F00000 2 20081224 A 7321 21195761011 ECU BOMBDR BD100 BD1001A10 1390044 GL HNYWL AS907 AS90711A 33908 WP LT ENGINE MALFUNCTIONED E CVGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 885TW 20037 P118187 DURING INITIAL CLIMB-OUT, AT 2000 FT AGL, LT ENGINE BEGAN HAVEING FLUCTUATIONS OF +/- 2 PERCENT N1 AND A "L ENG MINOR FA ULT" CYAN CAS MESSAGE WAS NOTED. CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. THE ENGINE WAS NOT SHUTDOWN. C REW PERFORMED STATIC TAKEOFF PWR GROUND RUN AND NO DISCREPANCIES WERE NOTED. DEFERRED ENGINE MINOR FAULT IAW MEL 73-00- 01 CAT A, EXPIRES IN 125 FLIGHT HOURS. ACFT RETURNED TO SERVICE. NO DISCREPANCY NOTED ON SUBSEQUENT FLIGHT. MX REPLAC ED ENGINE 1 ECU, CHANNEL A. (K) 2 L 7 2 4F 4 F RT T00005NY E00010LA 20090202 WP 2009 2 2 FDEA200810204445 1 20081020 A 2913 1489951 PUMP DOUG DC10 DC1030F 3023504 WP HYD SYSTEM FAILED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 21 317FE 25352 21046 46835 AT CRUISE FLT, NR 2 HYDRAULIC QTY AND PRESSURE WENT TO ZER0. NO HIGH TEMP INDICATED. COMPLIED WITH QRH AND RETURNED TO MEMPHIS. REMOVED AND REPLACED 2/1 NON-REV MOTOR PUMP SHUTOFF VALVE. 2 L 7 3 4F RT A22WE 20090203 EA 2009 2 3 SWIA200820910 1 20081231 A 5320 WEB CNDAIR CL600 CL6002D24 1390016 EA BS 280 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 805SK 15069 FS 280 LEFT LOWER WEB CORRODED AT LBL12.5. REMOVED CORROSION PER SRM. 2 L 7 2 4F RT A21EA 20090203 EA 2009 2 3 SWIA200820911 1 20081231 A 2150 CHECK VALVE CNDAIR CL600 CL6002D24 1390016 EA CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 805SK 15069 C-CHECK, RIGHT PRESSURE BULKHEAD CHECK VALVE CRACKED ON DUCT. REPLACED VALVE PER AMM. 2 L 7 2 4F RT A21EA 20090203 SO 2009 2 3 SWIA200820912 1 20081106 A 5713 STRINGER EMB 120 EMB120ER 3260203 SO CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 567SW 120342 C-CHECK, STRINGER NEAR NR 2 FUEL ACCESS PANEL CRACKED. REPLACED PER SRM. 2 L 7 2 4T RT A31SO 20090203 SO 2009 2 3 SWIA200820913 1 20081109 A 5320 FLOOR SUPPORT EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 567SW 120342 C-CHECK, RIGHT SIDE BELOW COCKPIT FLOOR, SUPPORT ANGLE CRACKED. REPLACED PER SRM. 2 L 7 2 4T RT A31SO 20090203 SO 2009 2 3 SWIA200820918 1 20081024 A 3397 WIRE EMB 120 EMB120ER 3260203 SO EMERGENCY LIGHT BROKEN A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 569SW 120344 C-CHECK, FLOOR EMERGENCY LIGHTS LOOSE AND INOP AT 2A. REPAIRED BROKEN WIRES AND REINSTALLED FLOOR EMERGENCY LIGHTS AT 2 A. 2 L 7 2 4T RT A31SO 20090204 NM 2009 2 4 HNAA2009012500026 1 20080814 A 5210 85210301102 BRACKET DHAV DHC8 DHC8102 2809003 NM PAX DOOR CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 931HA 51108 51108 132 UPPER AFT ANGLE OF INSIDE AIRSTAIR DOOR FOUND CORRODED. R&R PAX DOOR AFT ANGLE AND SHIMS IAW 52-10-00. 2 H 7 2 4T RT A13NM 20090204 EA 2009 2 4 HNAA2009012500027 1 20081017 A 5730 85730018011 SKIN DHAV DHC8 DHC8311 1386006 EA RT WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 327EN 30034 261 CORROSION FOUND ON LOWER SKIN OF THE RT WING BETWEEN STA 130.0 TO 145 AT REAR ON RT WING AT REAR SPAR, LOWER FLAP SHROUD . P/N 85730018-011 R&R IAW STRUCTURAL REPAIR MANUAL 51-40-00. 2 H 7 2 4T RT A13NM 20090204 NM 2009 2 4 HNAA2009020100038 1 20080812 A 5330 85310046101 SKIN PANEL DHAV DHC8 DHC8102 2809003 NM FUSELAGE DENTED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 931HA 51108 132 PROTRUDING DENT FOUND AT STATION 183.350 BETWEEN 24P-25P. REPAIRED DAMAGE IAW RD8-53-2181. 2 H 7 2 4T RT A13NM 20090204 NM 2009 2 4 HNAA2009012500025 1 20080812 A 5320 85330934103 SUPPORT ANGLE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 931HA 51108 51108 132 FORWARD CARGO FLOOR AFT SUPPORT ANGLE CORRODED ON RT. R&R FORWARD CARGO FLOOR AFT SUPPORT ANGLE WITH SOLID RIVET AS PER STRUCTURAL REPAIR MANUAL 51-40-00. 2 H 7 2 4T RT A13NM 20090204 EA 2009 2 4 HNAA2009012500020 1 20081015 A 5711 85711334101 SPAR DHAV DHC8 DHC8311 1386006 EA LT WING CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 327EN 30034 30034 261 SUPECTED CRACK ON LT WING FRONT SPAR AT INBD NACELLE ATTACHMENT TOP CORNER. R&R ANGLE IAW STRUCTURAL REPAIR MANUAL 51-4 0-00. 2 H 7 2 4T RT A13NM 20090204 EA 2009 2 4 HNAA2009012300011 1 20081022 A 5330 85322487115 SKIN DHAV DHC8 DHC8311 1386006 EA FUSELAGE DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 327EN 30034 30034 261 DURING 'C' CHECK INSPECTIONS, A REPAIR WITH NO DOCUMENTATION WAS FOUND ON THE FUSELAGE SKIN ON THE FORWARD BELLY AREA, L OCATED AT X231 TO X238 BETWEEN STRINGERS 30P TO 32P. THIS PATCH WAS REPLACED AND NEW DOCUMENTATION ISSUED FOR THE ACFT. 2 H 7 2 4T RT A13NM 20090204 NM 2009 2 4 HNAA2009020100041 1 20080913 A 5730 85711802005 ACCESS PANEL DHAV DHC8 DHC8102 2809003 NM RT WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 982HA 36673 380 RT WING ACCESS PANEL 622 AT (STRESS PANEL) HAS 2 HOLES CORRODED. CORROSION FOUND TO BE IN LIMIT PER RD8-57-1715. REPAI R HOLES IAW RD8-57-1715. 2 H 7 2 4T RT A13NM 20090204 EA 2009 2 4 HNAA2009012300012 1 20081022 A 5330 85322498101 SKIN DHAV DHC8 DHC8311 1386006 EA FUSELAGE DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 327EN 30034 30034 261 DURING 'C' CHECK INSPECTIONS, A REPAIR WITH NO DOCUMENTATION WAS FOUND ON THE FORWARD FUSELAGE BELLY SKIN AT X225 TO X23 0 BETWEEN STRINGERS 28P AND 29P. THE PATCH WAS R&R AND NEW DOCUMENTATION WAS ISSUED FOR THE ACFT. 2 H 7 2 4T RT A13NM 20090204 EA 2009 2 4 HNAA2009012500028 1 20081015 A 5415 8541078007 ATTACH FITTING DHAV DHC8 DHC8311 1386006 EA NACELLE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 327EN 30034 261 CORROSION AROUND 1 FASTENER ON THE REAR SPAR ATTACHMENT TO OTBD NACELLE. REPAIR ATTACHMENT TO OTBD NACELLE WITH HI LOCK S IAW STRUCTURAL REPAIR MANUAL 51-40-00. 2 H 7 2 4T RT A13NM 20090204 EA 2009 2 4 HNAA2009012300013 1 20081022 A 5330 85322487115 SKIN DHAV DHC8 DHC8311 1386006 EA FUSELAGE DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 327EN 30034 30034 261 DURING 'C' CHECK INSPECTIONS, A REPAIR WITH NO DOCUMENTATION WAS FOUND ON THE FUSELAGE BELLY SKIN AT X198 BETWEEN STRING ERS 30P AND 32P. THIS PATCH WAS R&R AND NEW DOCUMENTATION ISSUED FOR THIS REPAIR. 2 H 7 2 4T RT A13NM 20090204 NM 2009 2 4 HNAA2009020100040 1 20080908 A 5330 85311825101 SKIN PANEL DHAV DHC8 DHC8102 2809003 NM FUSELAGE DENTED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 931HA 51108 132 PROTRUDING DENT ON LT FUSELAGE AT STATION X195 BETWEEN STRINGER 23P AND 24P. REPAIRED DAMAGED IAW RD8-53-2181. 2 H 7 2 4T RT A13NM 20090205 CE 2009 2 5 YYE2009F00000 1 20081030 A 2910 15800252 POWERPACK CESSNA 337 T337G 2075726 CE CONT O360 TSIO360C 17025 SO HYD SYSTEM FAILED E YYEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 NM 11 5CS P3370087 HYDR PUMP FAILED TO EXTEND LANDING GEAR. HAND PUMP FAILED TO EXTEND LANDING GEAR. HAND PUMP FAILURE PROBABLY CAUSED BY DEBRIS FROM PRIMARY PUMP - YET TO BE DETERMINED. WILL SEND FOLLOW UP REPORT. LATE REPORT IS BEING DELT WITH BY FSDO. (K) 1 H 7 2 3O 3 O A6CE E9CE 20090205 NM 2009 2 5 UALA2008111300878 1 20080215 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 382UA 24657 FUSELAGE SKIN CRACKED ABOVE AND BELOW FWD ENTRY DOOR UPPER HINGE CUTOUT. MAJOR REPAIR ACP'D, FABRICATED AND INSTALLED S INGLE EXTERNAL DOUBLER. 2 L 7 2 4F 4 F RT A16WE E21EU 20090205 NM 2009 2 5 UALA2008111303323 1 20080611 A 2730 654450310 ACTUATOR BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU ELEVATOR FAULTY A UALA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 914UA 25381 CREW REPORTS EXCESSIVE CONTROL COLUMN FORCE REQUIRED FOR PITCH. REMOVED AND REPLACED ELEV FEEL ACTUATOR & ELEVATOR FEEL COMPUTER. ALSO REPLACED LT OUTBOARD AND INBOARD FLAP CARRIAGE ASSEMBLIES. 2 L 7 2 4F 4 F RT A16WE E21EU 20090205 NM 2009 2 5 AALA200803036 1 20081204 A 3350 BATTERY PACK BOEING 757 757223 1384957 NM EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 678AN 29428 MIA EMERGENCY LIGHT FROM SEAT ROW 16 TO 25 DIM. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A2NM 20090205 EU 2009 2 5 AALA200803037 1 20081205 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHTS DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 SJU LEFT HAND EMERGENCY LIGHTS FOR LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR LEFT NUMBER ONE DOOR. S YSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) 2 L 7 2 4F RT A35EU 20090205 EU 2009 2 5 AALA200803038 1 20081205 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 SJU LT EMERGENCY LIGHTS FOR LT NR 2 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR LT NR 2 DOOR. SYSTEM GROUND CHECKED NOR MAL OPS. 2 L 7 2 4F RT A35EU 20090205 EU 2009 2 5 AALA200803039 1 20081205 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 SJU EMERGENCY LIGHT AT RT SEAT 19G TO AFT CABIN INOPERATIVE. REPLACED BATTERY PACK AT RT NR 3 DOOR. SYSTEM GROUND CHEC KED NORMAL OPS. 2 L 7 2 4F RT A35EU 20090205 EU 2009 2 5 AALA200803040 1 20081205 A 3350 BATTERY PACK AIRBUS 300 A300B4605R 3930308 EU EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 40064 507 SJU RT EMERGENCY LIGHTS FROM RT NR 4 DOOR TO SEAT ROW 28G INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NO RMAL OPS. 2 L 7 2 4F RT A35EU 20090204 EU 2009 2 4 FDEA200810094290 1 20081009 A 2420 764067A GCU AIRBUS 300 A300F4605R 3930327 EU NR 2 FAILED A FDEA C ABORTED TAKEOFF J H WARNING INDICATION ELECT. POWER LOSS-50 PC TO TAKEOFF 1 CE 21 656FE 16999 16999 745 REJECTED TAKEOFF AT 30 KTS DUE TO LOSS OF ALL ELECTRICAL POWER EXCEPT EMERGENCY POWER. MULTIPLE PROBLEMS RELATED TO RAI N DRIPPING INTO AVIONICS BAY. REMOVED AND REPLACED NR 2 GCU AND ALL ASSOCIATED SYSTEMS OPERATE NORMAL ON ACFT, A300-6 00 MM 24-41-11-4 AND 24-41-00-0. 2 L 7 2 4F RT A35EU 20090204 NM 2009 2 4 FDEA200810254550 1 20081025 A 2620 8956831 SWITCH DOUG MD11 MD11F 3023600 NM FIRE BOTTLE MALFUNCTIONED A FDEA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 21 605FE 82791EK 48514 "CRG FIRE LWR AFT" LEVEL 3 ALERT AND AURAL WARNING ON TAKEOFF ROLL. ABORTED T/O AND DISCHARGED BOTH FIRE BOTTLES. PER FORMED AFT AND FWD CARGO COMPT INSPECTION, NO DAMAGE OR FIRE CONDITION FOUND. VERIFY WITH FLT CREW THAT THEY DISCHARGED AGENT 1 (THE BIG BOTTLE) ONLY. REMOVED AND REPLACED LOWER CARGO FIRE EXTINGUISHER CONTAINER NR 1 PER MM 26-22-01-4. F OUND FWD AND AFT AGENT 1 LOW PRESS LIGHT ON. T/S FIM 26-22-01 FOUND LOW PRESS SWITCH AT FAULT, PRESSURE SWITCH PIN "A" AND "B" IN CLOSED. SWITCH IS PART OF THE FIRE BOTTLE SAME P/N. 2 L 7 3 4F RT A22WE 20090204 NM 2009 2 4 FDEA200810284587 1 20081028 A 3040 2315 CONTROLLER BOEING 727 7272D4 138407U NM WINDOW HEAT MALFUNCTIONED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 21 288FE 21850 L1 WINDOW HEAT FAILED EN ROUTE. TURNED OFF AND BACK ON SEVERAL TIMES BUT WINDOW HEAT CONTINUED TO FAIL. CHECKED/RESET BOTH L1 AC AND DC CONTROL PER MOCC. NO HELP. WINDOW VERY COLD. ACN RELEASED FOR SERVICE PER MEL/CDL: 30-15-A CATEGORY : C. REPLACED BROKEN C/B C665. AFTER LAST ENTRY, FOUND CONTROL UNIT SERIAL NUMBERS FOR POS L1 AND L2 DID NOT MATCH MAX I. CONFIRMED BAD CONTROL UNIT TO HAVE MSN 7002. REMOVED AND REPLACED L1 CONTROL UNIT AND INSTALLED CONTROL UNIT WITH M SN 8892 IN L2 POSITION TO MATCH MAXI REF MM 30-41-033-4, WDM 30-41-11 AND SMP CH 20. OP CKS ARE GOOD AT THIS TIME. 2 L 7 3 4F A3WE 20090204 NE 2009 2 4 FDEA200811104881 2 20081010 A 7200 7110812 ENGINE AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4E1 52054 NE NR 2 INOPERATIVE A FDEA F A ACTIVATE FIRE EXT. UNSCHED LANDING E Y VIBRATION/BUFFET ENGINE STOPPAGE CL CLIMB 1 CE 21 453FE 47009 267 715410 ENG NR 2 FAILURE DURING CLIMB-OUT. CLIMB POWER PASSING 1800 FT, FELT SHUDDER, HEARD A BANG, HAD YAW. COMPLETED SINGLE ENGINE LANDING. NO SMOKE OR FIRE PULLED NR 2 ENG FIRE HANDLE AND AGENT 1 DISCHARGED. EGT SPIKE TO 780. R AND I NR 2 E NGINE AND PERFORMED ADJUSTMENT AND TEST PER MM 71-00-00-4 FOUND SATISFACTORY. R AND I NR 2 ENG FIREX AGENT 1 BOTTLE PER MM 26-21-15-4 AND TEST OK. PERFORMED ENG RUN PER A310 JRH ALL PARAMETERS NML. OLD CONTROL NUMBER: 08FDEA04881. 2 L 7 2 4F 4 F RT A35EU E3NE 20090206 WP 2009 2 6 AALA200803042 1 20081205 A 3350 LAMP DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT BURNED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 7509 49803 LGA LT COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP. SYSTEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F A6WE 20090206 WP 2009 2 6 AALA200803043 1 20081205 A 3350 CHARGER DOUG DC9 DC982 3022082 WP EMERGENCY LIGHTS INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 278AA 49294 MSP EMERGENCY LIGHT AT OVERHEAD SEAT ROW 29 INOPERATIVE. REPLACED CHARGER FOR SEAT ROW 29C. SYSTEM GROUND CHECKED NORM AL OPS. 2 L 7 2 4F A6WE 20090206 WP 2009 2 6 AALA200803030 1 20081203 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP EMERGENCY LIGHT DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424AA 49336 LGA EMERGENCY LIGHTS AT FORWARD CABIN INOPERATIVE. REPLACED BATTERY PACK AT SEAT ROW 8 FOR EMERGENCY LIGHTS AT FORWARD CABIN. 2 L 7 2 4F A6WE 20090206 NM 2009 2 6 AALA200803031 1 20081203 A 3397 CONNECTOR BOEING 757 757223 1384957 NM ZONE 200 LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 21 690AA 25696 DFW EMERGENCY LIGHT AT SEAT 34D INOPERATIVE. FOUND LOOSE CONNECTION. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 34D . 2 L 7 2 4F RT A2NM 20090205 2009 2 5 AALA200803041 4 20081205 A 2565 5A33075 SLIDE BOEING 737 737823 13844CB NM L1 DOOR FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 920AN 29521 MIA SLIDE FELL OUT OF FORWARD LT NR 1 DOOR AS DOOR WAS OPENED. SLIDE DID NOT DEPLOY. REPLACED LT NR 1 DOOR SLIDE. SYS TEM GROUND CHECKED NORMAL OPS. 2 L 7 2 4F RT A16WE 20090206 EU 2009 2 6 FDEA200809274073 1 20080927 A 2611 CG7G011 SMOKE DETECTOR AIRBUS 300 A300B4622 3930401 EU E/E BAY FAILED A FDEA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 21 716FD 31422 358 AV SMOKE ALARM ON TAXI OUT. ACFT SUFFERED RAIN INGRESSION DRIED OUT COURIER AREA AND AVIONICS BAY AREA. VERIFIED THAT FLOOR AND DRIP PAN DRAINS ARE CLEAR AND DRAIN NORMALLY. REMOVED AND REPLACED AVIONICS DUCT SMOKE DETECTOR 13WA PER AMM 26-15-12-4. PERFORMED SATISFACTORY, OPS CHECK PER AMM 26-15-00. 2 L 7 2 4F RT A35EU 20081215 NM 2008 12 15 SWAA086983 1 20081210 A 5322 6546546 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086993 1 20081210 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086994 1 20081210 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 23R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081215 2008 12 15 SWAA086971 4 20081210 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L1 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 744SW 29490 DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086978 1 20081210 A 5330 6562212 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086982 1 20081210 A 3230 6552235 SUPPORT FITTING BOEING 737 737317 138447P NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND RT MLG UPLOCK ASSEMBLY FWD SUPPORT FITTING CORRODED. REPAIRED FITTING PER SB. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087019 1 20081211 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 15L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087020 1 20081211 A 5754 65C26686 SKIN BOEING 737 7373H4 1384600 NM LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 22Y CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED AT O/B CORNER. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087021 1 20081211 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 583, STR 10R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086977 1 20081210 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 420, LBL 3. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081215 WP 2008 12 15 AALA200810434 1 20081121 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 CORROSION TOP LEFT CUSP FROM STATION 1136 TO STATION 1174. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081215 NM 2008 12 15 SWAA087004 1 20081210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 270, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087008 1 20081210 A 5322 6546536 SHEAR TIE BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 40. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087009 1 20081210 A 5322 6546536 SHEAR TIE BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 32. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087013 1 20081210 A 5322 6546536 SHEAR TIE BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 6. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086952 1 20081208 A 3350 8210248801 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST UK UNKNOWN 1 SW 29 914WN 36622 FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081215 WP 2008 12 15 AALA200810435 1 20081121 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 CORROSION ON CUSP FROM STATION 1164 TO STATION 1178. INSTALLED DOUBLER PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081215 EA 2008 12 15 SWIA200820623 1 20081208 A 3230 PRIORITY VALVE CNDAIR CL600 CL6002B19 1900309 EA NLG FAILED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 437SW 7564 FLT 4699 - NOSE GEAR FAILED TO EXTEND. REPLACED NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 20081215 WP 2008 12 15 AALA200810437 1 20081121 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 NR 6 SEAT TRACK CORROSION OUT OF LIMITS STATION 855 TO STATION 857. REMOVED CORROSION ROUTED AND INSTALLED SEAT TRACK P LUG. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810426 1 20081120 A 5311 FRAME DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 WINDOW FRAME, CRACK IN FRAME TOP CORNER LEFT SIDE STATION 1060. REPAIRED PER AARD 53-10-00-25. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810427 1 20081120 A 5311 FRAME DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 WINDOW FRAME, CRACK IN FRAME TOP CORNER LEFT SIDE STATION 1098. REPAIRED PER AARD 53-10-00-25. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810491 1 20081208 A 5322 SHEAR TIE DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7542A 49996 SHEAR TIE CRACKED AFT SIDE OF STATION 1451 FRAME AT LONGERON 2R. REPLACED WITH SERVICEABLE SHEAR TIE PER SRM 53 01. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810446 1 20081126 A 5310 BEAM DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 CARGO DOOR BEAM CORRODED/PITTED IN SEVERAL AREAS FROM STATION 1155 TO STATION 1211. BLENDED CORROSION, REMOVED CORROSIO N, WITHIN LIMITS PER ESO 80559 DATED 11/21/08. 2 L 7 2 4F A6WE 20081215 EA 2008 12 15 SWIA200820616 1 20081102 A 5420 CHANNEL CNDAIR CL600 CL6002C10 1390015 EA NACELLE CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 732SK 10194 C-CHECK, LEFT LOWER OUTBOARD 'U' CHANNEL CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081215 WP 2008 12 15 AALA200810490 1 20081209 A 5320 STIFFENER DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7542A 49996 STIFFENER ON AFT SIDE OF FRAME STATION 1418 AT LONGERON 2R IS CRACKED AT ATTACH POINTS. REPAIRED PER SRM 53-01-00. 2 L 7 2 4F A6WE 20081215 NM 2008 12 15 UALA2008121106851 1 20081211 A 3397 7945243 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT ROW 38 LT INOP. RE-SECURED EEL CONNECTOR. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081216 WP 2008 12 16 AALA200810457 1 20081202 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 CORROSION ON LOWER SIDE OF RIGHT CUSP STATION 1200. INSTALLED REPAIR PER AARD 53-20-00-16. 2 L 7 2 4F RT A6WE 20081216 WP 2008 12 16 AALA200810459 1 20081128 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 NUMBER 4 SEAT TRACK TANG BROKEN FROM STATION 928 TO 930. INSTALLED REPAIR PLUG. 2 L 7 2 4F RT A6WE 20081212 NM 2008 12 12 AALA200810404 1 20081114 A 5311 FRAME BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 STATION 400 RIGHT, FRAME CRACKED AT AIRCONDITIONING RAIL ATTACH POINT. REPAIRED PER ECO J1159AA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 DLM88081679 1 20081003 A 2731 TAB DOUG MD88 MD88 3023688 NM TRIM SYSTEM BENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 BENT LT ANTI-FLOAT TAB AT OUTBOARD AFT CORNER. BENT LT ANTI-FLOAT TAB AT OTBD AFT CORNER WAS REPAIRED IAW OPN 1031 CARD 1196. WEIGHT AND BALANCE WILL BE ACCOMPLISHED PER NR T0111845. 2 L 7 2 4F RT A6WE 20081212 NM 2008 12 12 DLM88081680 1 20081111 A 2731 SKIN DOUG MD88 MD88 3023688 NM TRIM TAB DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 SWOLLEN UPPER SKIN OF RT GEARED TAB OTBD SECTION. RT GEARED TAB OTBD SECTION WAS REPAIRED IAW SRM 55-04 PAR 3 FIG 2 AND OPN 1031 CARD 1260. 2 L 7 2 4F RT A6WE 20081212 NM 2008 12 12 ASAA0874014 1 20081206 A 5315 147A55067 FLOORBEAM BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION ON FLOORBEAM BS 986.5 RBL 30 TO LBL 30 WL 208. FLOORBEAM WAS BLENDED OUT OF LIMITS RBL 30 LBL 30 AND SO UPPER CHORD WAS R&R BS 986.5 WL 208. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 ASAA0844015 1 20081211 A 5320 SUPPORT BOEING 737 7374Q8 138447Q NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE. REPLACE FLOOR TO SIDEWALL SUPPORT PER SRM 53-60-53 FIG 201. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 DLM88081683 1 20081117 A 5523 TAB DOUG MD88 MD88 3023688 NM LT ELEVATOR CONTAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 REPAIR LT ELEVATOR ANTI-FLOAT TAB DUE TO PRESENCE OF WATER IN HONEYCOMB STRUCTURE. WATER REMOVED IAW SRM 51-70-2 PAR 6C . TAB WAS BALANCED IAW SRM 55-20-2D. 2 L 7 2 4F RT A6WE 20081215 EA 2008 12 15 ASOA200801699 1 20081208 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 CARGO SEAT TRACK AT RBL 27 FS 559+80 IS CORRODED. 2 L 7 2 4F RT A21EA 20081215 CE 2008 12 15 GUUA94532120908A 1 20081209 A 2916 RESERVOIR BEECH 1900 1900D 1154162 CE MLG LOW A GUUA O OTHER O OTHER AP APPROACH 1 SO 29 53545 UE185 FLIGHT NR 9168 PNS/MCO DURING APPROACH, UPON LANDING GEAR EXTENSION LANDING GEAR CIRCUIT BREAKER POPPED. CLEANED, INSPE CTED AND SERVICED THE MLG RESERVIOR. LANDING GEAR OPS CHECK NORMAL. NO DEFECTS NOTED. 2 L 7 2 4T RT A24CE 20081215 NM 2008 12 15 USAA2008121292220 1 20081211 A 5753 6546481111 SPINDLE BOEING 737 7374B7 138449C NM FLAP CARRIAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 434US 24556 PHL - RON - MAJOR REPAIR - LOG NR 4205761 - AFT SECTION OF LT OTBD SPINDLE AT WBL355 HAS CORROSION. REPLACED LT OTBD SP INDLE AT WBL355 IAW B737 AMM 27-51-44-4. 2 L 7 2 4F RT A16WE 20081215 EA 2008 12 15 SWIA200820607 1 20081204 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 754SK 10215 FLT 6181 - EMERGENCY LIGHT AT 12A HAS INOP BULB. RELAMPED. 2 L 7 2 4F RT A21EA 20081215 NM 2008 12 15 SWAA087031 1 20081211 A 3350 10107451 SIGN BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 639SW 27712 FOUND R1 DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED SIGN PER MM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086958 1 20081209 A 3350 411A2212 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 921WN 36626 R1 DOOR EMERGENCY EXIT LIGHT COVER MISSING. REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087012 1 20081210 A 5322 6546536 SHEAR TIE BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 15. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087014 1 20081210 A 5322 6546536 SHEAR TIE BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 6. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081215 WP 2008 12 15 AALA200810441 1 20081126 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 CORROSION ON CUSP FROM STATION 598 TO STATION 617 LEFT HAND. REMOVED AND INSTALLED SERVICEABLE CUSP SHEET FROM STATION 598 TO STATION 712 PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810424 1 20081122 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 CORROSION ON CUSP STATION 560 TO 579, LEFT SIDE. REPAIRED PER AARD 53-20-00 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810489 1 20081209 A 5311 FRAME DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7542A 49996 FRAME CRACKED AT STATION 1418 LONGERON 2L. REPAIRED PER SRM 53-01-00 FIGURE 2. 2 L 7 2 4F A6WE 20081216 2008 12 16 UALA2008111301038 4 20080226 A 3160 DISPLAY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE COCKPIT DEFECTIVE A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 536UA 25156 AFTER AIRCRAFT ARRIVED, RAMP PLUGGED GROUND POWER IN AND CREW NOTICED AN ACRID ODOR, FOUND UPPER CENTER EICAS CRT SCREEN BURNED UP AND RECEPTACLE ON AIRCRAFT BURNED PINS AND RUBBER INSULATION BURNED. BPCU BITE SHOWS EXT PWR OVR VOLT TRIP. REPLACED CRT AND REPT PINS. ALL CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081216 WP 2008 12 16 AALA200810460 1 20081128 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP FUSELAGE BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 NUMBER 4 SEAT TRACK TANG BROKEN FROM STATION 916 TO 919. INSTALLED REPAIR PLUG. 2 L 7 2 4F RT A6WE 20081217 NM 2008 12 17 UALA2008120906803 1 20081209 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1395 S39L CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 BULK CARGO COMPARTMENT UNDERFLOOR, CORROSION ON SHEAR TIE AT BS 1395, STR 39L TO STR 39R. MAJOR REPAIR ACCOMPLISHED. R EMOVED DAMAGED SHEAR TIE. FAB NEW SHEAR TIE AND INSTALLED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081217 NM 2008 12 17 UALA2008120906805 1 20081209 A 5320 STIFFENER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NLG WW CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 NOSE LANDING GEAR WHEEL WELL, RT VERTICAL STIFFENER HAS A .125 INCH CRACK FOUND 7.5 INCHES ABOVE TOP OF ELECTRICAL BOX. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF VERTICAL STIFFENER. INSTALLED FILLER AND 3 EA ANGLE REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081217 NM 2008 12 17 UALA2008111302091 1 20080410 A 2150 3987505 CONTROL VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE AC PACK FAULTY A UALA O OTHER O OTHER CR CRUISE 1 WP 29 668UA 30024 LEFT PACK "OFF" LIGHT WITH ASSOCIATED "L PACK OFF" DISPLAYED IN CRUISE WITH PACK SELECTED TO "STBY" (REF DF583) DUCT PRE SSURE AND PRESSURIZATION NORMAL. RECURRED ON FLT 9834-13. REPLACED LT PACK FLOW CONTROL AND SHUTOFF VALVE. OPS CHECK GOOD. LEFT PACK DOES NOT SUPPLY SUFFICIENT AIR FOR CABIN PRESSURE WHEN LEFT WING ANTI-ICE IS SWITCHED ON. PACK AIR SUP PLY IS SUFFICIENT WITH ANTI-ICE OFF. SAME CONDITION WITH RIGHT BLEED SUPPLYING LEFT SIDE. FOR TROUBLESHOOTING LT AND R T FLOW CONTROL VALVE WERE SWAPPED. FOUND PROBLEM FOLLOWED TO RIGHT FLOW CONTROL VALVE. REPLACED RT FLOW CONTROL VALVE . BOTH PACKS OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081217 NE 2008 12 17 UALA2008121006839 2 20081209 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 659UA 27114 724347 NR 1 ENG FAULTY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081212 NM 2008 12 12 UIEA200800341 1 20081123 A 5330 SKIN BOEING 747 74747UF 1384812 NM ZONE 100 PUNCTURED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 492MC 29253 AT DEPARTURE FOUND TAIL PUNCTURED THRU FUSELAGE EXTERNAL SKIN JUST FORWARD OF STA 2598 AT 6 O`CLOCK POSITION APPROX 11.5 " BY 16". CUT OUT FUSELAGE SKIN DAMAGE AND LOWER CHORD AT STA 2598 AS PER SRM 53-00-01 AND 51-70-12. PERFORMED REPAIR IAW ATLAS EO NR 4453A221. 2 L 7 4 4F RT A20WE 20081212 EU 2008 12 12 AALA200820081 1 20081111 A 5320 A53970870200 STRUCTURE AIRBUS 300 A300B4605R 3930308 EU ZONE 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 19059 53486 0469 SEALING SECTION CORRODED, REPAIRED SEALING SECTION IAW SRM 53-16-18-01 ITEM NR 360. 2 L 7 2 4F RT A35EU 20081212 SO 2008 12 12 CHQA200800242 1 20081209 A 3260 8005701 PROXIMITY SWITCH EMB 135 EMB135KL 3260302 SO ALLSN AE3007 AE3007A 03030 GL NLG FAULTY A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 377SK 145579 CAE311350 FLIGHT 5315, MSP TO STL - AFTER TAKEOFF THE FLIGHT CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL EICAS MESSAGE AND THE LA NDING GEAR WOULD NOT RETRACT. THE QRH WAS FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT BACK AT MSP. THE MESSAGE D ISAPPEARED AFTER LANDING. MAINTENANCE PERFORMED A WOW TEST PER THE EMB AMM 32-63-00 AND THE SYSTEM OPS CHECKED GOOD. T HE AIRCRAFT THEN CONTINUED ON TO STL WHERE THE FAULT WAS TROUBLESHOT FURTHER. STL MAINTENANCE FOUND THE NOSE LANDING GE AR WOW PROX SWITCH TO BE AT FAULT. THE PROX SWITCH WAS THEN REPLACED. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081212 NM 2008 12 12 AALA200810399 1 20081122 A 5320 BRACKET BOEING 737 737823 13844CB NM ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 FORWARD CARGO, BRACKET CRACKED IN RADIUS UNDER LEFT HAND TRANSITION PANEL STATION 500H FORWARD SIDE OF BELTFRAME CONNECT ED TO INTERCOSTAL. REMOVED AND REPLACED WITH SERVICEABLE BRACKET. 2 L 7 2 4F RT A16WE 20081212 EA 2008 12 12 MALA080209 1 20081207 A 4920 APU CNDAIR CL600 CL6002B19 1900309 EA ODOR A MALA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 15 834AY 8034 FIRST ATTEMPT AT TURNING ON THE APU DURING APPROACH WAS UNSUCCESSFUL, SECOND ATTEMPT TO START THE APU WAS SUCCESSFUL BUT AFTER ONE MINUTE OF USE A VERY STRONG JET FUEL ODOR AS DETECTED IN THE CABIN AND FLIGHT DECK. FLIGHT CREW DONNED OXYGE N MASK AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. MX COMPLETE PACK BURN AND DEFERRED PER MEL 49-10-1C, PULLED AND COLLARED CB N12 AND S3 TRANSFERRED TO MM02, MXC 17754 NOTIFIED PERFORMED OPS CK 3 TIMES. APU START NORMALLY, NO DE FECTS THIS TIME. 2 L 7 2 4F RT A21EA 20081212 NM 2008 12 12 DLM88081656 1 20081029 A 5310 DOOR FRAME DOUG MD88 MD88 3023688 NM BS 370-408 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 EXFOLIATION CORROSION ON LOWER C1 DOOR JAMB FROM STA 370-408. DAMAGED SECTION OF JAMB PAN WAS REMOVED IAW SRM 53-08D. NEW JAMB SECTION DRILLED AND TRIMMED IAW 53-05D FIG 804D. REPAIR ANGLES FABRICATED IAW SRM 53-05D FIG 804D. NEW SECTIO N OF JAMB PAN AND REPAIR PARTS INSTALLED IAW SRM 53-05D FIG 804D. REPAIR IDENTIFIED PER PS 900-5-1 NO 04. 2 L 7 2 4F RT A6WE 20081212 2008 12 12 GTIA0800085 4 20081130 A 2565 D30665309 SLIDE AIRBUS A321 A321231 3940032 NM ZONE 100 LOW PRESSURE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 588NK 2590 L1 DOOR SLIDE HAD ZERO PRESSURE. 2 L 7 2 4F RT A28NM 20081212 NM 2008 12 12 AALA200810391 1 20081117 A 5320 FLOOR SUPPORT BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 RIGHT FLOOR SUPPORT TRANSITION PANEL IN AFT CARGO HAS CORROSION BETWEEN STATION 767 AND STATION 787. REMOVED CORRODED S UPPORT AND INSTALLED NEW PART PER ESO 61000 DATED 11/17/08. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 AALA200810408 1 20081114 A 5311 FRAME BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 STATION 500A RIGHT, FRAME CRACKED AT AIRCONDITIONING RAIL ATTACH POINT. REPAIRED PER ECO J1159AA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 AALA200810409 1 20081114 A 5311 FRAME BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 STATION 500C LEFT, FRAME CRACKED AT AIRCONDITIONING RAIL ATTACH POINT. REPAIRED PER ECO J1159AA. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 AALA200810410 1 20081114 A 5311 FRAME BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 STATION 480 LEFT, FRAME CRACKED AT AIR CONDITIONING RAIL ATTACH POINT. REPAIRED PER ECO J1159AA. 2 L 7 2 4F RT A16WE 20081212 SO 2008 12 12 SIMA200834303 1 20081128 A 5320 14525480603 SILL EMB 145 EMB145LR 3260212 SO ZONE 100 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 907AE 5000 14500895 DURING A IMBV INSPECTION, THE BAGGAGE DOOR LOWER SILL WAS FOUND TO BE CORRODED. REMOVED CORRODED DOOR SILL. POSITIONED NEW SILL AND DRILLED FOR FASTENERS. CLEANED ALODINED AND PRIMED NEW SILL AND INSTALLED. REPAIR DONE IAW EMB SRM (SRM EMB 145/1142 REV 40) CHAPTERS 51-20-01, 51-20-03, 51-40-02, 51-40-04 AND 51-40-06. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081215 SW 2008 12 15 QMLA1124200808054 1 20081124 A 2560 107CDC1824B PUMP BELL 230 230 1182149 SW CARGO BAY OVERHEATED E QMLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AA AIR AMBULANCE 1 NM 03 904CM 23013 APPROX 2-3 MILES FROM HOSPITAL FUMES IN COCKPIT AND CABIN. NO INDICATION IN THE COCKPIT, OTHER THAN THE SMELL THAT ANYT HING WAS ABNORMAL. ELECTED TO CONTINUE TO THE DESTINATION. REDUCED THE ELECTRICAL LOAD AS MUCH AS POSSIBLE AND RELAYED TO THE CREW TO TURN OFF UNNECESSARY EQUIPMENT AND SWITCH TO PORTABLE O2 SO THAT HE COULD TURN OFF THE MED BUS. UPON LA NDING, PILOT PERFORMED A RAPID SHUTDOWN. POST FLIGHT REVEALED NOTHING OBVIOUS OTHER THAN THE SMELL. MX FOUND 1 OF THE MEDICAL AIR PUMPS UNDER THE BAGGAGE COMPT FLOOR HAD OVERHEATED CAUSING THE ODOR. THE PUMP HAD BEEN INADVERTENTLY TURNED ON AND ALLOWED TO RUN FOR AN EXTENDED PERIOD OF TIME. THE AIR PUMP HAS SINCE BEEN REPLACED AND IS FUNCTIONING NORMALLY 1 G 7 2 3U NC H9SW 20081215 CE 2008 12 15 GLBA200812112 1 20081210 A 2697 WIRE BEECH 1900 1900D 1154162 CE LT FIRE BOTTLE LOOSE A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 21 219GL UE219 FALSE WARNING - IN FLIGHT THE PILOTS REPORTED A LT ENGINE DISCHARGE LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT. MX FOUN D AND REPAIRED LOOSE WIRE AT TERMINAL OF THE LT FIRE BOTTLE IAW GMM 9.3.0. OPS CHECKS WERE GOOD IAW BEECH 1900D MM 26-2 0-01. 2 L 7 2 4T RT A24CE 20081215 NM 2008 12 15 AALA200810400 1 20081122 A 5340 BRACKET BOEING 737 737823 13844CB NM ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 FORWARD CARGO, BRACKET CRACKED IN RADIUS UNDER RIGHT TRANSITION PANEL STATION 500G FORWARD SIDE OF BELTFRAME CONNECTED T O INTERCOSTAL. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 AALA200810401 1 20081122 A 5340 BRACKET BOEING 737 737823 13844CB NM ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 FORWARD CARGO, BRACKET CRACKED IN RADIUS UNDER RIGHT TRANSITION PANEL STATION 500H FORWARD SIDE OF BELTFRAME CONNECTED T O INTERCOSTAL. REMOVED AND REPLACED WITH SERVICEABLE BRACKET. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 UALA2008120806774 1 20081205 A 5230 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FWD CARGO DOOR GOUGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 552UA 26641 FWD CARGO DOOR LOWER FWD FRAME CORNER GOUGED. MAJOR REPAIR ACCOMPLISHED. REMOVED CORNER SECTION OF FRAME AND INSTALLED NEW CORNER FRAME P/N 143N6618-6. 2 L 7 2 4F 4 F RT A2NM E17NE 20081217 NM 2008 12 17 UALA2008120906813 1 20081209 A 5322 SHEAR TIE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1197 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 MAJOR REPAIR: SHEAR TIES CORRODED AT BS 1197+44, AFT FACE AREA BETWEEN STRINGERS 38L & 37R. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR TIE AT 39R-38R. 2 L 7 2 4F 4 F RT A1NM E24NE 20081217 NM 2008 12 17 UALA2008120806776 1 20081205 A 5320 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 552UA 26641 G4B GALLEY PRESSURE DECK STA 1682-1720, RBL 53 UNDER WATER DRAIN CHANNEL HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REM OVED CORROSION, TRIMMED OUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081217 2008 12 17 UALA2008121106840 4 20081209 A 2565 7A147913 SLIDE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE L2 DOOR UNSERVICEABLE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 173UA 24380 LOW PSI. GAUGE TEMPERATURE COMPENSATION. LET BOTTLE COOL AND ADJUSTED PRESSURE. 2 L 7 4 4F 4 F RT A20WE E24NE 20081217 NM 2008 12 17 UALA2008121106847 1 20081211 A 2822 568129115004 PUMP BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE RIGHT DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 799UA 26926 FOUND FWD RIGHT MAIN BOOST PUMP HANDLER BROKEN. REPLACED PUMP. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081217 NM 2008 12 17 UALA2008121106852 1 20081211 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT SEAT 2J AFT INOP. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081217 NM 2008 12 17 UALA2008120806777 1 20081206 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 198UA 28716 SEAT 3A AFT EEL STRIP LIGHT FOUND BROKEN AWAY FROM SEAT. REPLACED EEL STRIP AND OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081217 NM 2008 12 17 UIEA200800345 1 20081204 A 5751 SKIN BOEING 747 747230B 1384889 NM LT WING AILERON DELAMINATED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 512MC 21220 LT WING OUTBOARD AILERON UPPER SURFACE HAS 3 AREAS WITH PREVIOUS REPAIRS DELAMINATING. DELAMINATION AT WBL 883.0 AREA I S 3.5 BY 2.0 INCHES, LOCATED 9.5 INCHES FROM T/E, WBL 991.0 AREA IS 4.0 BY 2.0 INCHES, LOCATED 8.5 INCHES FROM T/E AND A T WBL 1033 AREA IS 7.5 BY 2.0 INCHES, LOCATED 7.5 INCHES FROM T/E OF AILERON. PERMANENT REPAIR ACCOMPLISHED AS PER SRM 51-40-09, FIG 7, SHEETS 1, 3 AND 4 PREPREG LAYUP 250 DEGREES CURE PER SRM 51-40-12. WEIGHT AND BALANCE NEGLIGIBLE, PREV IOUS REPAIRS REMOVED, SAME MATERIAL AMOUNT OF WEIGHT MATERIAL INSTALLED PER SRM 51-80-01. ALSO, REFERENCE ATLAS AIR EO NR 4757A470. 2 L 7 4 4F RT A20WE 20081217 NM 2008 12 17 UALA2008120806780 1 20081207 A 5753 BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAP MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 515UA 24840 RT WING T/E FLAP AFT FLAP INBOARD SUPPORT TRACK LOWER AFT BEARINGS ATTACHED ON T/E FLAP REAR SPAR ARE MISSING AND THRU B OLT IS SHEARED OFF. REPLACED ROLLER SUPPORT ASSY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081217 NM 2008 12 17 UALA2008120806786 1 20081207 A 4950 PRESSURE SENSOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU DEFECTIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 768UA 26919 APU FAILED DURING STARTING, AUTO SHUTDOWN (TWICE). REPLACED DELTA PRESSURE SENSOR, TOTAL PRESSURE SENSOR AND SURGE CON TROL VALVE. RAN APU AND DRY MOTORED ENGINE, OPS OK. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081217 NM 2008 12 17 UALA2008120906790 1 20081209 A 3610 32907706 ISOLATION VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE BLEED AIR SYS SEIZED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 776UA 26937 RIGHT BLEED ISOLATION VALVE SEIZED IN OPEN POSITION. REPLACED ISOLATION VALVE. OPS OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081217 NM 2008 12 17 UALA2008121006828 1 20081210 A 3397 794640 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN LOOSE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT EEL LIGHT INOP BY DOOR 5 RIGHT AFT LOWER WALL EEL. SECURED CONNECTOR, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081217 NM 2008 12 17 DHLA2008743518 1 20081112 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 UPPER FUSELAGE CARGO CABIN FROM BS 460 TO BS 720D RBL 25 SEAT TRACK WITH CORROSION. REPAIRED MAIN CARGO CABIN SEAT TRAC K SECTION FROM BS 583.75 TO BS 596.125 RBL 25 IAW SRM 53-10-5 FIG 9, FROM BS 460 TO 583.75 AND BS 596.125 TO BS 720D RBL 25. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW SRM 53-10-1 FIG 3. 2 L 7 3 4F A3WE 20081217 WP 2008 12 17 AALA200810469 1 20081204 A 5320 BRACKET DOUG DC9 DC983 3022083 WP CARGO DOOR FRAME CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 CORROSION IN MID CARGO DOOR JAMB FORWARD LOWER CORNER FITTING. OLD BRACKET WAS REMOVED AND NEW BRACKET INSTALLED. 2 L 7 2 4F RT A6WE 20081217 WP 2008 12 17 AALA200810470 1 20081205 A 5347 CARGO TRACK DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 LEFT TIE DOWN TRACK IN AFT CARGO HAS CORROSION SEVERAL PLACES FROM STATION 1212 TO STATION 1117. REPLACED LEFT FORWARD TRACK FROM STATION 1212 TO STATION 1117. 2 L 7 2 4F RT A6WE 20081215 NM 2008 12 15 AALA200810396 1 20081122 A 5340 BRACKET BOEING 737 737823 13844CB NM ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 BRACKET CRACKED IN RADIUS UNDER RIGHT TRANSITION PANEL IN FORWARD CARGO AT STATION 500F FORWARD SIDE BETWEEN BELLFRAME A ND INTERCOSTAL. REMOVED AND REPLACED BRACKET PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086964 1 20081210 A 5240 6545871 SKIN BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 383SW 26589 DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT R1 DOOR LOWER AFT FASTENER HOLE STOP FITTING. REMOVED AND REPLACED DO OR PER MM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086965 1 20081210 A 5330 6545800 SKIN BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 415WN 29836 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR AT UPPER RT CORNER CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087034 1 20081211 A 5311 6546545 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND FRAME STUB BEAM WEB CRACKED AT BS 685, RBL 45, WL 208. REPAIRED WEB PER ER. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086956 1 20081205 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086974 1 20081210 A 2560 6557463 BRACKET BOEING 737 7377H4 1384404 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED 8Y CHECK, FOUND L1 DOOR FWD GIRT BAR BRACKET CORRODED AT BS 312, LBL 42. REMOVED AND REPLACED BRACKET PER MM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086975 1 20081210 A 2560 6557463 BRACKET BOEING 737 7377H4 1384404 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED 8Y CHECK, FOUND L1 DOOR AFT GIRT BAR BRACKET CORRODED AT BS 344, LBL 58. REMOVED AND REPLACED BRACKET PER MM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086980 1 20081210 A 5330 6545800 SKIN BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 227, BETWEEN RBL 0 TO RBL 3. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087035 1 20081211 A 5753 65C26714 SKIN BOEING 737 7373H4 1384600 NM FORE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND RT WING O/B FORE FLAP SKIN DELAMINATED AT 100" O/B OF I/B END. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087037 1 20081211 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081215 2008 12 15 SWAA086969 4 20081210 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 744SW 29490 DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086955 1 20081205 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086981 1 20081210 A 5322 69353656 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 360, BETWEEN STR 28R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086988 1 20081210 A 5311 6546545 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND STUB BEAM WEB CRACKED AT BS 685, RBL 45. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086989 1 20081210 A 5311 6546526 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086990 1 20081210 A 5311 6546532 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086991 1 20081210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 4R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086992 1 20081210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086996 1 20081210 A 5330 6562212 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, AT BS 304 ABOVE CUTOUT CENTER LIN E. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087017 1 20081210 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25L TO STR 27L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087018 1 20081210 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL CHORD CRACKED AT BS 666, RBL 24. REPAIRED CHORD PER ER. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087024 1 20081211 A 5330 6552988 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT L2 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087010 1 20081210 A 5322 6546536 SHEAR TIE BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, RBL 32. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087015 1 20081210 A 5311 6546540 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND MID CABIN LT FRAME WEB CRACKED AT BS 639, WL 215. REMOVED AND REPLACED WEB PER DWG. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086962 1 20081210 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 399WN 27693 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 AALA200820088 1 20081129 A 5315 146N5092 FLOORBEAM BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AA 57228 24591 CORROSION ON FORWARD EDGE AND BETWEEN TEE CAP OF BEAM, REPAIRED FLOORBEAM TEE CAP IAW SRM 53-60-51-2R2 AND AARD 53-60-51 -5 2 L 7 2 4F RT A2NM 20081215 NM 2008 12 15 AALA200820089 1 20081126 A 5320 146N52468 SUPPORT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 56842 24599 CORROSION UNDER R NR 4 PASSENGER/SERVICE DOOR, REPAIRED R 4 DOOR DRAIN SUPPORT IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20081215 NM 2008 12 15 AALA200820090 1 20081202 A 5315 146N508919 FLOORBEAM BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 56842 24599 FLOORBEAM CORRODED, REPAIRED FLOORBEAM IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20081215 WP 2008 12 15 AALA200810418 1 20081124 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 CORROSION AROUND TIE DOWN TRACK FASTENERS LEFT SIDE STATION 1210 TO 1322 (AFT CARGO). REMOVED AND REPLACED WITH SERVICE ABLE TRACK PER SRM 51-10-01. 2 L 7 2 4F A6WE 20081215 EA 2008 12 15 SWIA200820625 1 20081208 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 472CA 7667 FLT 2676 - ONE BULB ON ENTRY WAY EMERGENCY LIGHT BURNED OUT. RELAMPED. 2 L 7 2 4F RT A21EA 20081215 WP 2008 12 15 AALA200820421 1 20081122 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 CORROSION ON CUSP STATION 1022, LEFT SIDE. REPAIRED PER SRM 53-20-00-16. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810422 1 20081122 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 CORROSION ON CUSP STATION 579 TO 598 LEFT SIDE. REPAIRED PER AARD 53-20-00-16. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810442 1 20081125 A 5522 SKIN DOUG DC9 DC982 3022082 WP ZONE 300 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 CRACK IN RIGHT ELEVATOR UPPER SKIN ALONG TOE, OUTBOARD OF GEAR TAB. INSTALL DOUBLER REPAIR PER ESO 80559 DATED 11/25/08 . 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810443 1 20081126 A 5320 GUSSET DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 GUSSET IS CRACKED AT LEFT STATION 207 WHERE IT ATTACHES TO INTERCOSTAL AT LONGERON 15 LEFT. INSTALLED "T" DOUBLER AT ST ATION 207 AND LONGERON 15 LEFT PER SRM 53-10-00-11. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810486 1 20081208 A 5755 CASTING DOUG DC9 DC982 3022082 WP RT SPOILER CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 RIGHT GROUND SPOILER CASTING CRACKED. INSTALLED DOUBLER OF 17-7 PH 0.100 THICK, (FULL LENGTH), AARD 57-20-00-15. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810439 1 20081125 A 5313 LONGERON DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 LONGERON 4 LEFT CRACKED AT STATION 160 AND STATION 200. REMOVED LONGERON FROM END CAP AT STATION 148 TO PRODUCTION SPLIC E AT STATION 234. INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810420 1 20081202 A 5340 BRACKET DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 NUMBER 4 SEAT TRACK SUPPORT BRACKET CRACKED STATION 864. REMOVED AND REPLACED WITH SERVICEABLE SUPPORT BRACKET. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810428 1 20081120 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 WINDOW FRAME, CRACK IN FRAME TOP CORNER RIGHT SIDE STATION 886. REPAIRED PER AARD 53-10-00-25. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810429 1 20081120 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 WINDOW FRAME, CRACK IN FRAME TOP AFT CORNER RIGHT SIDE STATION 1079. REPAIRED PER AARD 53-10-00-25. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810445 1 20081126 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 CRACK IN CUSP AT LIGHTENING HOLE STATION 222 LEFT AT NR 2 SEAT TRACK. REPAIRED CUSP PER AARD 53-20-00-16 USING NEW CUSP MATERIAL FROM STATION 218 TO STATION 237. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810430 1 20081120 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 WINDOW FRAME, CRACK IN FRAME TOP CORNER RIGHT SIDE STATION 927. REPAIRED PER AARD 53-10-00-25. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810431 1 20081120 A 5310 WINDOW FRAME DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 WINDOW FRAME, CRACK IN FRAME AFT TOP CORNER RIGHT SIDE STATION 1060. REPAIRED PER AARD 53-10-00-25. 2 L 7 2 4F A6WE 20081215 NM 2008 12 15 UALA2008121106846 1 20081210 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 174UA 24381 THE 24C EMERGENCY LIGHT STRIP DAMAGED, REPLACED SEAT 24C EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 20081215 NM 2008 12 15 YENA200812110127 1 20081211 A 2781 1702286A SENSOR EMB ERJ190 ERJ190100IGW 3260408 NM SLATS FAILED A YENA O OTHER F FLT CONT AFFECTED AP APPROACH 1 EA 15 284JB 437 190000144 FLT NR 1219, BOS-BUF, SLAT FAIL IN FLIGHT WHEN FLAPS SELECTED TO POSITION ON APPROACH. R&R LT OTBD SKEW SENSOR IAW 27-8 3-01. OPS CHECK OK. 2 L 7 2 4F RT A57NM 20081216 NM 2008 12 16 UALA2008111305420 1 20080822 A 5210 F1314 SPRING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE L2 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 L-2 DOOR MANUAL DEPLOY GAS CYLINDER INOP. REPLACED GAS SPRING. 2 L 7 2 4F 4 F RT A1NM E24NE 20081216 NM 2008 12 16 UALA2008111305554 1 20080831 A 2120 113882 SENSOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE E&E BAY FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 EQUIP COOLING CTRL R RIGHT ECC REPORTS FAILED FOR 10 SECONDS AND POWER IS AVAILABLE FOR THE ECC. STATUS MSG-2117112 INA CTV ER MODE MSG-2117112 LATCHED ER MODE MSG-2117132 LATCHED ER HARD. SUSPECT LOW FLOW SENSOR. REPLACED LOW FLOW SENSOR , OP CHECK GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081216 NE 2008 12 16 UALA2008111306270 2 20081026 A 7230 FAN BLADE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ENGINE DENTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 648UA 25285 NUMEROUS FAN BLADES HAVE SMALL NICKS & DENTS ON BOTH NR 1 & NR 2 ENGINES. ALL DAMAGED FAN BLADES BLENDED ON BOTH NR 1 & NR 2 ENGINES. 2 L 7 2 4F 4 F RT A1NM E24NE 20081216 NM 2008 12 16 UALA2008111406510 1 20081113 A 3397 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN BROKEN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 551UA 25399 TWO EEL EXIT IDENTIFIERS HAVE BROKEN WIRES. REPLACED 2 EA EEL IDENTIFIERS, 1 EA SEAT ROW 15 LT AND RT. OPS CHECKS GOOD . 2 L 7 2 4F 4 F RT A2NM E17NE 20081216 WP 2008 12 16 AALA200810475 1 20081215 A 5230 STOP FITTING DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7541A 49995 FORWARD SIDE OF AFT CARGO DOOR, LOWER STOP PAD FITTING CRACKED. FITTING WAS REMOVED AND REPLACED WITH NEW FITTING SRM 5 3-01. 2 L 7 2 4F A6WE 20081212 NM 2008 12 12 UIEA200800346 1 20081204 A 5720 STRUCTURE BOEING 747 74747UF 1384812 NM ZONE 600 DAMAGED A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 408MC 29261 WHILE AIRCRAFT WAS TAXING, THE AIRCRAFT STRUCK ANOTHER AIRCRAFT THAT WAS PARKED CAUSING DAMAGE TO RIGHT WINGLET. RIGHT WINGLET REMOVED PER CDL, AREA VISUALLY INSPECTED AND AIRCRAFT RELEASED. ACFT AWAITING PERMANENT REPAIRS. OPEN 2 L 7 4 4F RT A20WE 20081212 NM 2008 12 12 ASAA0854009 1 20081208 A 2697 WIRE BOEING 737 737890 1384527 NM CABIN CHAFED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 02 570AS 7189 AC00570 35185 MAIN FIRE WARNING INOP. GROUNDED YES. FOUND WIRE CHAFED AT REMOTE APU CONTROL PANEL & FIRE PROTECTION MASTER WARNING & CONTROL C/B POPPED. REPLACED REMOTE APU CONTROL PANEL REF MM 26 22 03 000 801. MAIN FIRE WARNING OPS NORMAL REF MM 26 15 00 & MM 26 11 00. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 ASAA0874012 1 20081207 A 5312 SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION ON FLOOR TO BULKHEAD SUPPORT BS 500D RBL 17 LBL 13. REMOVED AND REPLACED BULKHEAD SUPPORT. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 ASAA0874013 1 20081206 A 5320 146A750224 SUPPORT BOEING 737 737790 13844CN NM FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 626AS 30793 CORROSION ON FLOOR TO SIDEWALL SUPOPORT. R&R FLOOR TO SIDEWALL SUPPORT PER SRM 53-00-53-51-40-05 & 51-20-01. 2 L 7 2 4F RT A16WE 20090105 NM 2009 1 5 ASAA0844016 1 20081210 A 5320 SUPPORT BOEING 737 7374Q8 138447Q NM BS 727E-837 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 02 773AS 25106 CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE. REPLACE SUPPORT PLATE PER SRM 53-60-53. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 DLM88081682 1 20081117 A 5523 TAB DOUG MD88 MD88 3023688 NM RT ELEVATOR CONTAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 REPAIR RT ELEVATOR ANTI-FLOAT TAB DUE TO PRESENCE OF WATER IN HONEYCOMB STRUCTURE. WATER IN HONEYCOMB STRUCTURE REMOVED IAW SRM 51-70-2 PAR 6C. TAB WAS BALANCED IAW SRM 55-20-2D. 2 L 7 2 4F RT A6WE 20081212 NM 2008 12 12 DLM88081661 1 20081030 A 5523 TAB DOUG MD88 MD88 3023688 NM LT ELEVATOR PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 PUNCTURE UPPER SURFACE OF LT ANTI-FLOAT TAB. PUNCTURE REPAIRED IAW OPN 1031 CARD 1178. WEIGHT AND BALANCE WILL BE ACCO MPLISHED PER N/R T0111845. 2 L 7 2 4F RT A6WE 20081215 EU 2008 12 15 U30A2008121100006 1 20081208 A 5330 SKIN AIRBUS 320 A320214 3930316 EU FUSELAGE DAMAGED A U30A K NONE O OTHER IN INSP/MAINT 1 EA 17 264AV 20046 1867 AFTER FLT 599, ACFT PARKED ON GATE IN ORD FOR OVERNIGHT. ACFT WAS STRUCK BY GROUND EQUIPMENT (ASIG) TUG, CAUSING DAMAGE TO THE FWD EXTERNAL GROUND POWER RECEPTACLE DOOR, THE FWD DME ATC ANTENNA & LOWER FUSELAGE SKIN ADJACENT TO THE DME ANT ENNA INSTALLATION. THE DAMAGED AREA IS COMMON TO THE FWD DME ANTENNA LOCATED BETWEEN FR5-FR6 & STRG 43L-43R. THE REPAIR WAS ACCOMPLISHED IAW AIRBUS STRUCTURAL REPAIR MANUAL (SRM) 53-11-11/201, PAR.5.J & FIG. 212 EXTERNAL DOUBLER REPAIR, AN D GENERAL REPAIR REQUIREMENTS FOUND IN SRM 51-70-20. SUPPORTING SUB PLATE P/N D53230940001 (REF SRM 53-11-29, FIG. 4, I TEM 365) WAS REPLACED & DME ANTENNA REPLACED PER AMM 34-51-11PB401. REPLACED THE FWD EXTERNAL POWER RECEPTACLE DOOR PER 2 L 7 2 4F RT A28NM 20081215 CE 2008 12 15 GLBA200812113 1 20081209 A 5511 SPAR BEECH 1900 1900D 1154162 CE HORIZ STAB CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 21 231YV UE231 MAJOR REPAIR HORIZONTAL STABILIZER SPAR WEB CRACKED APPROXIMATELY .250" IN LENGTH. MAINTENANCE REPAIRED HORIZONTAL STA BILIZER MAIN SPAR WEB IAW BEECH 1900D SRM 55-91. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1. 2 L 7 2 4T RT A24CE 20081215 NE 2008 12 15 USAA2008121292218 2 20081209 A 7261 OIL SYSTEM AIRBUS A321 A321211 3930370 EU CFMINT CFM56 CFM565B3P 13006 NE NR 2 ENGINE LOW A USAA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 19 193UW 3584 LOG PAGE 8292519 - FLT NR 1192 PHX-PHL - EMERGENCY LANDING - WHILE ENROUTE, CAPTAIN SENT AN ACARS MSG ADVISING NR 2 ENGI NE OIL WAS AT 6 QUARTS. JUST EAST OF PIT, CREW SAID OIL WAS NOW AT 4 QUARTS AND WERE ADVISED TO SHUT DOWN ENGINE AT 3 Q UARTS. ENGINE OIL WENT FROM 4 TO 2 QUARTS WITHIN A MATTER OF MINUTES. CREW SHUT DOWN THE NR 2 ENGINE AND DECLARED AN E MERGENCY. ACFT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F 4 F RT A28NM E37NE 20081215 NM 2008 12 15 SWAA087000 1 20081210 A 5322 6546546 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 27L TO STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086987 1 20081210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 460, STR 15L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086957 1 20081208 A 5610 2315MODB WINDOW BOEING 737 7377H4 1384404 NM COCKPIT ARCED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 29 756SA 27872 R1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 20081215 WP 2008 12 15 AALA200810451 1 20081203 A 5311 FRAME DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 0.250 CRACK AT RIGHT CANT FRAME STATION 1474, AFT OF ELEVATOR ACCUMULATOR ACCESS. 5.5 INCH BY 3.5 INCH, .040 7075 T6 DOU BLER INSTALLED AFTER END OF CRACK STOP DRILLED. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810448 1 20081130 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 CORROSION ON SEAT TRACK BLENDED BEYOND LIMITS. REPLACED SEAT TRACK. 2 L 7 2 4F A6WE 20081215 NM 2008 12 15 SWAA086963 1 20081209 A 3350 65C3330484 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 329SW 23693 DURING SCHEDULED MV3 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081215 WP 2008 12 15 AALA200810423 1 20081122 A 5320 STIFFENER DOUG DC9 DC982 3022082 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 STIFFENER CRACKED ABOVE VAULT DOOR JAMB O TOP FORWARD SIDE STATION 1338. REPAIRED PER AARD 53-10-00-15. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810485 1 20081204 A 5310 BEAM DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7539A 49993 NOSE WHEEL WELL, LEFT J BEAM REPAIR DOUBLER CRACKED AT LOCK FASTENER AT UPPER AFT SIDE. REMOVED AND REPLACED DOUBLER PE R AARD 53-10-00-4. 2 L 7 2 4F A6WE 20081216 WP 2008 12 16 AALA200810458 1 20081128 A 5320 ANGLE DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 PLOW ANGLE CORRODED IN AFT CARGO STATION 1338. INSTALLED A SERVICEABLE ANGLE PER SRM 53-01. 2 L 7 2 4F RT A6WE 20081217 2008 12 17 UALA2008120906800 4 20081209 A 2565 D31516313 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT CABIN DOOR DISCONNECTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 474UA 1475 FWD RT CABIN DOOR SLIDE PACK ASSY CONNECTOR BETWEEN CABLE LOOP ASSY AND COVER RELEASE CABLE WAS FOUND DISCONNECTED. SLI DE REPLACED DUE TO CRACKED MOUNTING LUG. 2 L 7 2 4F 4 F RT A28NM E40NE 20081217 NM 2008 12 17 UALA2008111302275 1 20080418 A 4920 380029817 APU BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE FAULTY A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 WP 29 668UA 30024 APU FAULT CAUTION LT AND EICAS MSG. TEMP SPIKED TO +600 ON SHUTDOWN IN FLIGHT. REPLACED APU. 2 L 7 2 4F 4 F RT A1NM E24NE 20081217 NE 2008 12 17 UALA2008120506766 2 20081204 A 7530 8136642 ACTUATOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 1 ENGINE LEAKING A UALA O OTHER K FLUID LOSS IN INSP/MAINT 1 WP 29 796UA 26931 NR 1 ENGINE HAS FUEL LEAKING FROM NR 2 DRAIN. REPLACED TCC ACTUATOR, NO HELP. LINE STILL LEAKING. FOUND STATOR VANE A CTUATOR LEAK BEYOND LIMITS. REPLACED SVA. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081217 NM 2008 12 17 UALA2008120806771 1 20081208 A 8012 TUBE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 2 STARTER CRACKED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 781UA 26945 RIGHT START VALVE WILL NOT OPEN IN AUTO START. REPLACED NR 2 START VALVE AND STARTER, NO HELP. T/S IN PROGRESS. SWAPP ED ENG START MODULE, SWAPPED ENG RELAY BOX. NO HELP. NO AIR COMING OUT OF ENG START SOLENOID WITH START SWITCH ACTIVAT ED AND AIR ON. START VALVE TUBE CRACKED. REPLACED LINE. ENGINE START GOOD IN AUTO AND MANUAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081217 NM 2008 12 17 UALA2008120806772 1 20081205 A 3350 D71702001 POWER SUPPLY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN DISCHARGED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 777UA 26916 AISLE SEAT EMERGENCY EXIT LIGHTS INOP BOTH LEFT AND RIGHT AISLES SEAT ROWS 31 TO 43. REPLACED EMERGENCY LIGHTS POWER SU PPLY M33401, OP'S CHECK GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081217 NM 2008 12 17 UALA2008120806773 1 20081205 A 3350 78941 LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 777UA 26916 EMERGENCY EXIT LIGHTS INOP ON AISLE SEATS 1F AND 3E. REPLACED AFT LIGHT ON SEAT 1F AND FWD LIGHT ON SEAT 3E. OP'S CHEC K GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081217 NM 2008 12 17 UALA2008120906808 1 20081209 A 5315 FLOORBEAM BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE BS 1197 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 FLOORBEAM TEE CAP AT BS 1197, LBL 3 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED & INSTALLED NEW TEE FROM STR 32L TO STR 32R. 2 L 7 2 4F 4 F RT A1NM E24NE 20081217 NM 2008 12 17 UALA2008120906811 1 20081209 A 3397 ELECWC528 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 DOOR L1 LIGHT BAR (EMERGENCY LIGHT BAR) IS INOP. REPAIRED BROKEN WIRE. OPS CHECKS GOOD. WIRE REPAIRED IS EI E-CWC528 . 2 L 7 2 4F 4 F RT A1NM E24NE 20081217 NM 2008 12 17 UALA2008120906816 1 20081209 A 3350 767 LAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 DOOR 2R UPPER EMERGENCY EXIT LIGHT DOOR HANDLE ILLUMINATION PORTION IS INOP. RELAMPED AT DOOR R2 UPPER EMERGENCY EXIT L IGHT DOOR HANDLE AND ILLUMINATION PORTION. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081217 NM 2008 12 17 UALA2008111303687 1 20080702 A 2997 SOCKET BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 PYLON DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 57UA 27112 NR 1 ENG PYLON HYD BAY CONNECTOR D02118 HAS DAMAGED SOCKET. REPLACED SOCKET AT CONNECTOR D02118P PER BSWPM 20-60-09 AND WDM 78-34-11. OPS CHECKS GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081217 NM 2008 12 17 UALA2008121006824 1 20081210 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE LAVATORY UNSECURE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 181UA 25278 DOOR 1R LAV EMERGENCY LIGHT NEEDS TO BE SECURED. FOUND SCREW MISSING, SECURED WITH SCREW, OPS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081217 NM 2008 12 17 UALA2008121006825 1 20081210 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT LIGHTS INOP AT DOOR 5 RIGHT FWD AND AFT SILL LIGHTS. REPLACED BATTERY. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081217 NM 2008 12 17 UALA2008121006826 1 20081210 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT LIGHT INOP AT DOOR 5 RIGHT CEILING ENTRY. REPLACED BATTERY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081217 EU 2008 12 17 UALA2008120806778 1 20081206 A 5320 SHEAR PLATE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 405UA 452 AFT RT SIDE TRIANGULAR SHEAR PLATE HAS CORROSION AT FASTENER HOLES. REMOVED 4EA LOCK FASTENERS AT SHEAR PLATE AND BEAM 205. REMOVED PLATE, DRILLED NEW PLATE, NEEDS INSTALL. INSTALLED 5 EA LOCK AND BLIND FASTENERS. COMPLETED INSTALLATION OF FRAME AND SHEAR PLATE. 2 L 7 2 4F 4 F RT A28NM E40NE 20081217 NM 2008 12 17 UALA2008120806779 1 20081206 A 3350 767 LAMP BOEING 767 767222 1385122 NM PWA 2037 PW2037 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 598UA 28751 DOOR 4 RT EMERGENCY EXIT LIGHT INOP (EXT). RELAMPED EMERGENCY LIGHT, OPERATES NORMAL. 2 L 7 2 4F 4 F RT A1NM E17NE 20081217 NE 2008 12 17 UALA2008120806782 2 20081207 A 7321 FUEL CONTROL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE MALFUNCTIONED A UALA D RETURN TO BLOCK X ENGINE FLAMEOUT IN INSP/MAINT 1 WP 29 536UA 25156 726521 LEFT ENGINE SHUTDOWN BY ITSELF AFTER START. REPLACED FUEL CONTROL UNIT. 2 L 7 2 4F 4 F RT A2NM E17NE 20081217 NM 2008 12 17 UALA2008120806785 1 20081206 A 2432 263BA1011 BATTERY BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE APU FAULTY A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 229UA 30557 APU BATTERY STATUS MESSAGE. REPLACED APU BATTERY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081217 WP 2008 12 17 AALA200810452 1 20081206 A 5230 BRACKET DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 MID CARGO DOOR UPPER FORWARD STOP BRACKET CRACKED. INSTALLED A SERVICEABLE BRACKET PER ESO 80174. 2 L 7 2 4F RT A6WE 20081217 NM 2008 12 17 DHLA2008743514 1 20081113 A 5320 SUPPORT ANGLE BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 UPPER FUSELAGE CARGO CABIN BS 848 LBL62 OVERWING STUB BEAM AND SUPPORT ANGLES WITH DOUBLE HOLES. REPLACED UPPER CHORD O N STUB BEAM AT BS 848 BETWEEN LBL 45 TO LBL 62 IAW B727 SRM 51-10-1 PARA 7. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 DHLA200800133 1 20081204 A 5330 SKIN BOEING 727 727214 138407R NM BS 212 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 786AT 21692 ACFT SKIN DAMAGE 2 IN HOLE LOWER RT SIDE BELOW PITOT TUBE. ACFT DAMAGED BY CARGO CONTAINER. INSTALLED REPAIR IAW SRM 5 3-30-3 AT STA 212 RT STR 25R. 2 L 7 3 4F A3WE 20081217 EU 2008 12 17 FDEA200810084278 1 20081008 A 2750 532A000003 LIMITER AIRBUS 300 A300F4605R 3930327 EU FLAP TORQUE MALFUNCTIONED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CE 21 650FE 726 FLAPS STUCK AT 20 DEG WOULD NOT RETRACT. FOLLOWED RED TABS FLAPS DID EXTEND TO 30/40 ON LANDING FLAPS RETRACTED AFTER L ANDING. BOTH SYS 1 AND SYS 2 FLAP FAULT LIGHT ON IN FLIGHT. PERFORMED SERVICING OF RT WING JACKSCREWS AND TORQUE LIMI TER PER AMM 12-13-27-0. ALL FLUIDS CLEAN WITH MINIMAL SERVICING REQUIRED. REMOVED AND REPLACED FLAP TORQUE LIMITER IAW MM 27-54-12-4. PERFORMED OPERATIONAL TEST OF FLAP SYSTEM AND NO DEFECTS FOUND. REINSTALLED INBD NR 1 JACKSCREW ACCES S PANEL. PER VERBAL, MTSI STEP 4 FLAP SYSTEM LUBE ACCOMPLISHED BY EMP NR 175004. PER STEP 1 PERFORMED VISUAL INSPECTIO N OF ALL CARRIAGES, BEARINGS, ROLLERS, JACKSCREWS, TRACKS, NO DEFECTS FOUND. 2 L 7 2 4F RT A35EU 20081217 EU 2008 12 17 FDEA200810154372 1 20081015 A 2750 CHA1478004H JACKSCREW AIRBUS 300 A300F4605R 3930327 EU TE FLAPS DAMAGED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 650FE 726 AFTER TAKEOFF, UPON ATTEMPTING TO RAISE THE FLAPS, FLAPS FAULTED. COMPLIED WITH ECAM AND RED TABS AND RETURNED TO KATL . UPON CONFIG FOR LANDING FLAPS DID GO TO 40 FOR A NORMAL LANDING. FLAPS THEN RETRACTED TO 0 UPON LANDING. REMOVED A ND REPLACED NR 6 RT FLAP JACKSCREW IAW FDX A 300-600 MM 27-54-24-4. REPLACED NR 5 FLAP JACKSCREW IAW A300-600 AMM 27-5 4-24 -4. SERVICED NR 5 JACKSCREW WITH OIL IAW A300-600 AMM. REMOVED AND REPLACED NR 4 RT FLAP JACKSCREW IAW FDX A 300 -600 MM 27-54-24. OPS CHECKED GOOD IAW FDX A300-6 00 MM 27-54-24-4. NR 4 MPN-CHA1478-004H, S/N G053, NR 5 MPN-CHA1484- 002J S/N R1270 NR 6 MPN CHA1485-004F, S/N N1198. 2 L 7 2 4F RT A35EU 20081217 WP 2008 12 17 FDEA200811044709 1 20081104 A 5414 AJC741537 SKIN DOUG MD10 MD1010F 3022112 WP ZONE 400 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 75122 46631 AFT NACELLE, FIREWALL SEAL PLANE AT FS Y2166 AND LEFT SIDE OF THE TRAILING EDGE OF THE DIVERTER, HAS WORN SKIN. REPAIR WORN SKIN AREA IAW SRM 51-31-01; VOL II; PG 1; SRM 55-35-04; VOL III AND DWG AJC7415, REV "BK". ALODINED AND PRIMED I AW SRM 51-21-01; VOL II; PG 1. PART MARKED IAW GMM 7-0-1000. REMOVED AND RE-INSTALLED THE NR 2 STARTER DUCT; FLANGE AN D LOWER ADAPTER RING REF AMM 80-11-01-2 AND 71-10-01-2. NO LEAKS NOTED. 2 L 7 3 4F RT A22WE 20081217 WP 2008 12 17 FDEA200811124864 1 20081112 A 5754 ARB16191 SKIN DOUG MD10 MD1010F 3022112 WP LT WING SLAT GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 46631 LT WING INBD SLAT GOUGED OTBD TOP CORNER. REMOVED AND RE-INSTALLED THE LEFT NR 2 SLAT. BLENDED AREA IAW SRM 57-00-01; FIG 1-A; SHEET 3; PG 5; VOL I AND 57-55-01. FABRICATED SKIN AND SPLICE PLATES THEN INSTALLED RTEF SRM 57-10-00; VOL I; FIG 3-1. GAP CHECKS GOOD REF MD10-10 AMM 27-80-01-4. 2 L 7 3 4F RT A22WE 20081217 NM 2008 12 17 DHLA2008743513 1 20081113 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 UPPER FUSELAGE CARGO CABIN FROM BS 950 TO BS 1166 LBL25 SEAT TRACK WITH CORROSION AND BARE METAL. REPLACED SEAT TRACK S ECTION FROM BS 950 TO BS 1166 LBL25 IAW SRM 51-10-1 PARA 7A 2 L 7 3 4F A3WE 20081217 WP 2008 12 17 AALA200810467 1 20081203 A 5320 ANGLE DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 CORROSION IN LOWER "J" ANGLE AT STATION 1322 BETWEEN LONGERON 29 LEFT AND LONGERON 29 RIGHT. REPAIR DOUBLER INSTALLED P ER AARD 53-10-00-17. 2 L 7 2 4F RT A6WE 20081217 WP 2008 12 17 AALA200810453 1 20081206 A 5230 BRACKET DOUG DC9 DC983 3022083 WP CARGO DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 MID CARGO DOOR UPPER AFT STOP BRACKET CRACKED. INSTALLED SERVICEABLE BRACKET PER ESO80174. 2 L 7 2 4F RT A6WE 20081217 WP 2008 12 17 AALA200810464 1 20081128 A 5210 FITTING DOUG DC9 DC983 3022083 WP AFT PAX DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 VAULT DOOR BELL CRANK FITTING CRACKED.INSTALLED A SERVICEABLE FITTING. 2 L 7 2 4F RT A6WE 20081217 WP 2008 12 17 AALA200810465 1 20081203 A 5230 BEAM DOUG DC9 DC983 3022083 WP CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 MID CARGO DOOR BEAM VERTICAL LEG CORRODED. INSTALLED 2 DOUBLERS PER AARD 53-10-00-3. 2 L 7 2 4F RT A6WE 20081217 NM 2008 12 17 FDEA200812125128 1 20081212 A 5711 65249661 SPAR BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 276FE 22041 CRACKED CHORD FALSE SPAR UNDER NR 7 SPOILER FITTING. REMOVED LOWER SECTION OF CHORD IAW DRWG SR27-57-038 REV C AND FABR ICATED NEW LOWER SECTION, 2 REPAIR ANGLES, 1 REPAIR STRAP, AND WEB IAW DWG SR27-57-038 REV C. TREATED AND PRIMED REPAI R PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND DWG SR27-57-038 REV C. 2 L 7 3 4F RT A3WE 20081217 NM 2008 12 17 SWAA087053 1 20081211 A 5330 6562212 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 291, WL 259 RT SIDE. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 FDEA200812015016 1 20081201 A 5310 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPOR T FITTING NR 2 FOUND WITH CRACK INDICATION AT HOLE NR A. MAIN CARGO DOOR LOWER JAMB, CRACKED NR 2 SUPPORT FITTING REMOV ED AND REPLACED AS PER SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081217 NM 2008 12 17 FDEA200812015017 1 20081201 A 5310 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON 0.460 INCH DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPO RT FITTING NR 3 FOUND WITH CRACK INDICATIONS AT HOLES NR B AND NR C. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 3 FO R CRACKED BOLT HOLES NR B AND NR C, BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIE D AS MAJOR AS PER GMM 6-2-10. 2 L 7 3 4F RT A22WE 20081217 NM 2008 12 17 FDEA200812015021 1 20081201 A 5330 AJC70601 SKIN DOUG MD11 MD11F 3023600 NM ZONE 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 EMPENNAGE, RIGHT AFT FUSELAGE EXTERNAL SKIN COMMON TO BODY FAIRING NR 347DF MATING SURFACE FOUND WITH CORROSION. CORROD ED SKIN AT EMPENNAGE RIGHT AFT FUSELAGE EXTERNAL SKIN COMMON TO BODY FAIRING NR 347DF. REPAIRED AS PER SRM 53-20-00 FIG URE 13 VOLUME I. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100. CORROSION FOUND EXCEEDED LIMITS, ORIGINAL THICKNESS: 0.10 0 INCH, MATERIAL REMOVED: 0.044 INCH, MATERIAL REMAIN: 0.056 INCH AS PER SRM 53-20-00 FIGURE 13 VOLUME I. 2 L 7 3 4F RT A22WE 20081217 NM 2008 12 17 DHLA2008743512 1 20081112 A 5320 BEAM BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 UPPER FUSELAGE CARGO CABIN BS 825.95 RBL 62 OVERWING STUB BEAM WITH DOUBLE HOLES. REPLACED STUB BEAM BS 825.95 BETWEEN RBL 45 TO RBL 62 IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081217 EA 2008 12 17 SWIA200820627 1 20081019 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 965SW 7871 C-CHECK, FS 280 FLOOR SUPPORT BEAM RBL9 LOWER INBOARD AND OUTBOARD CLIPS CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081217 NM 2008 12 17 SWAA087058 1 20081211 A 5730 6546419 SKIN BOEING 737 7377H4 1384404 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED 10Y CHECK, FOUND LT WING L/E SKIN CRACKED AT I/B END. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087066 1 20081213 A 3350 81000 LENS BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 298WN 32543 FWD LT EEPLS LIGHT LENS BROKEN. REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081217 SO 2008 12 17 DJF2008F00017 1 20081126 A 2530 940236900675 DRAIN MAST EMB 135 EMB135BJ 3260306 SO ALLSN AE3007 AE3007A 03030 GL FWD GALLEY FROZEN E DJFA O OTHER O OTHER NR NOT REPORTED 1 EA 23 905LX 648 145775 FWD GALLEY ICE DRAWER DRAIN FROZEN, INSPECTED AND FOUND FWD GALLEY HEATED DRAIN MAST OVERHEATED AND WIRES BURNED OFF. T HIS UNIT WAS REPLACED DUE TO AD2007-17-10 IAW SB145LEG-38-0013, 648.8 HRS PRIOR TO FAILURE. RECOMMEND THAT MFG TEST PAR TS FOR POSSIBLE SHORTING OR OVERHEAT PROBLEMS. 2 L 7 2 4F 4 F RT TE6CH 20081217 SO 2008 12 17 C2XA08TY138 1 20081209 A 3350 66361 LIGHT EMB 145 EMB145 3260210 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 14916 145415 EMERGENCY LIGHT FLOOR PROXIMITY STRIP INOP. R&R LIGHT STRIP IAW EMB 145 AMM 33-50-12. OPS CK GOOD. ACFT RELEASED AND RETURNED TO SERVICE 2 L 7 2 4F RT T00011AT 20081217 NM 2008 12 17 SWAA087069 1 20081212 A 3350 417A5900 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 428WN 29844 DURING SCHEDULED HC2 CHECK, AFT LT BATTERY PACK FAILED FUNCTION CHECK. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087070 1 20081212 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 473WN 33832 EEPLS LIGHT STRIP LOOSE AT ROW 1. SECURED EEPLS PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087059 1 20081211 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 790SW 30604 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, RBL 1. REPAIRED FLOORBEAM PER SRM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087083 1 20081213 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 731SA 27863 DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION BEARING I/B LOWER ATTACH LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087050 1 20081211 A 5311 65C25228 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 727C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087040 1 20081211 A 5311 6546596 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND FRAME CORRODED AT BS 727B, STR 18R. REPAIRED FRAME PER SRM. 2 L 7 2 4F RT A16WE 20081212 WP 2008 12 12 IXXA08SMN192S 1 20081024 A 5512 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 77. 000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, AND STIFFENER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AT STATION XE 29.000 - 77.000 IAW FAA FORM 8110-3 NUMBER 08548 DATED 11/18/08, SEMAN DRAWING ED-4875 DATED 11/05/08, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 55-2-0 PAGE 12, DC8 SRM 55-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, AND DC8 SRM 51-1-11. 2 L 7 4 4F 4A25 20081212 NM 2008 12 12 AALA200810387 1 20081121 A 5320 FLOOR SUPPORT BOEING 737 737823 13844CB NM ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 INTERCOSTAL FLOOR BOARD SUPPORT CRACKED AT MOUNT HOLES BUTT LINE 30 RIGHT BETWEEN STATIONS 312 AND STATION 328. INSTAL LED NEW FLOOR SUPPORT BRACKET. 2 L 7 2 4F RT A16WE 20081212 NM 2008 12 12 DLM88081651 1 20081126 A 5330 SKIN DOUG MD88 MD88 3023688 NM FS 313-427 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 970DL 43173 FUSELAGE BELLY SKIN FROM FS 313 TO FS 427, AND L26L TO L26R WAS SPLICED DUE TO NUMEROUS GOUGES, TWO PREVIOUS SKIN REPAIR S, AND REMNANTS OF AN ANTENNA MODIFICATION THAT IS NO LONGER USED. THE SKIN SPLICE WAS PER THE SRM, AND INCLUDED PLUGGI NG PREVIOUS REPAIR FASTENER HOLES IN THE PRODUCTION DOUBLER (BEAR STRAP). 2 L 7 2 4F RT A6WE 20081212 NM 2008 12 12 DL76G081652 1 20081126 A 2160 3987865 VALVE BOEING 767 767332 1382001 NM LT ECS BAY MALFUNCTIONED A DALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 178DZ 30596 FLIGHT DECK TEMP CONTROL INOP IN AUTO AND MANUAL. FWD TO MCO PLACARD PER MEL 21-61-02A. VERIFIED FLT DECK TRIM AIR VAL VE. DISCONNECTED AND STOWED CONNECTOR. 2 L 7 2 4F RT A1NM 20081212 EA 2008 12 12 MALA080210 1 20081129 A 3230 533407 SELECTOR VALVE CNDAIR CL600 CL6002D24 1390016 EA NLG MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 909XJ 15141 AFTER TAKEOFF FROM KIND, 3596 EXPERIENCED A NOSE GEAR CAUTION EICAS MESSAGE, FOLLOWING THE POM, THE CREW RETURNED TO AND LANDED AT IND. I DID NOT RECEIVE INFORMATION AS TO THE EXACT EICAS MESSAGE, BUT IT WAS A FLASHING AMBER CAUTION MESSAG E. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW CRJ900 M/M 32-32-10 PN NR 53340-7/SN NR NGL/1681/08-OFF PN NR 5 3340-7/SN NR NGL/1558/06. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F RT A21EA 20081212 NM 2008 12 12 DL76G081698 1 20081205 A 2822 PUMP BOEING 767 767324 1385203 NM PWA 4060 PW4060 52119 NE FUEL BOOST INOPERATIVE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 394DL 27394 724164 CTR FUEL PUMPS DID NOT COME ON WHEN BOTH ENGS ON LINE FWD TO MCO/PLAC MEL 28-22-02A, RT CTR C/B PULLED AND COLLARED, LT CTR WORKS OK. ACFT RETURNED A SECOND TIME FOR INOP CTR BOOST PUMP. REPLACED RELAY K330. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081212 SO 2008 12 12 CHQA200800238 1 20081203 A 2421 30086011 GENERATOR EMB 135 EMB135KL 3260302 SO ALLSN AE3007 AE3007A 03030 GL NR 4 FAILED A CHQA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 11 375SK 24428 720 145569 CAE312296 AFTER LANDING THE FLIGHT CREW RECEIVED A GENERATOR NR 4 BEARING FAIL MESSAGE ON EICAS. THE MESSAGE WAS DEFERRED PER MEL 24-31-02-1 CAT A. THE NR 4 GENERATOR WAS THEN REPLACED AND OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081215 EA 2008 12 15 ASOA200801700 1 20081208 A 5347 SEAT TRACK CNDAIR CL600 CL6002B19 1900309 EA FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 27 868AS 7474 CARGO SEAT TRACK AT LBL 9 FS 559+80 IS CORRODED. 2 L 7 2 4F RT A21EA 20081215 CE 2008 12 15 GLBA200812111 1 20081210 A 3040 TERMINAL BEECH 1900 1900D 1154162 CE WINDSHIELD ARCED A GLBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 21 184UX UE184 SMOKE SMELL - FLIGHT NR 7195 - UPON DEPARTURE FROM MKE IN FLIGHT - PILOTS REPORTED SPARKS NEAR THE BOTTOM OF THE RT CORN ER OF THE FIRST OFFICERS WINDSHIELD INSIDE OF COCKPIT AND SMELLED A SLIGHT BURNING SCENT. MX REMOVED PAPER CLIP FROM FI RST OFFICERS WINDSHIELD TERMINAL LUGS. INSPECTED TERMINAL LUG AND SURROUNDING WINDSHIELD AREA. NO DEFECTS NOTED. FIRS T OFFICERS WINDSHIELD OPS CHECKED GOOD IAW BMM 56-10-00-201. 2 L 7 2 4T RT A24CE 20081215 EA 2008 12 15 ASOA200801693 1 20081207 A 3350 LIGHT CNDAIR CL600 CL6002B19 1900309 EA CABIN INOPERATIVE A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 27 847AS 7335 EMERGENCY LIGHT ON BY PREVIOUS CREW OR CLEANING CREW. FLIGHT ATTENDANTS REPORTS LIGHT INOP. FLT 5034 DEL 92 MINS. 2 L 7 2 4F RT A21EA 20081215 SW 2008 12 15 DUFA20080003 1 20081126 A 2613 434422122 OVERHEAT SENSOR SWRNGN SA227 SA227AC 8780603 SW RT WING FALSE ACTIVATION E DUFA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 27 158MC AC726B WHILE ON CLIMB OUT, THE PILOT NOTICED THAT THE RT WING OVERHEAT LIGHT ILLUMINATED. THE RT GENERATOR WAS SHUT DOWN, BLEE D AIR TURNED OFF AND THE LANDING GEAR EXTENDED. AFTER 3 MINUTES THE LIGHT WAS STILL ILLUMINATED AND PROCEDURES CALL OUT FOR ENGINE SHUT DOWN. SHORTLY AFTER ENGINE SHUT DOWN THE LIGHT EXTINGUISHED. THE PILOT INFORMED THE TOWER OF HIS SITU ATION AND WAS CLEARED TO RETURN TO THE AIRPORT WHERE HE MADE AN UNEVENTFUL LANDING. UPON INVESTIGATION, NO EVIDENCE OF FIRE OR OVERHEATING COULD BE FOUND IN THE WING AND GEAR WELL AREAS. A NEW DUCT SENSOR WAS INSTALLED AS A PRECAUTION. 2 L 7 2 4T RT A8SW 20081215 EA 2008 12 15 SWIA200820610 1 20081205 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 907SW 7511 FLT 5838 - MAIN CABIN DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 SWIA200820613 1 20081207 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG DISCHARGED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 454SW 7749 FLT 4529 - NOSE GEAR DIDN'T RETRACT ON TAKEOFF AND NOSE STEERING INOP ON LANDING. ACCOMPLISHED FULL SERVICE OF NOSE STR UT. 2 L 7 2 4F RT A21EA 20081215 NM 2008 12 15 SWAA086954 1 20081209 A 2560 P4010021 BATTERY BOEING 737 7373G7 138447J NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST UK UNKNOWN 1 SW 29 670SW 23784 FOUND FWD I/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086997 1 20081210 A 5330 6562212 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT, AT BS 304 BELOW CUTOUT CENTER LIN E. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081215 WP 2008 12 15 AALA200810433 1 20081121 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 CENTER WING, INTERCOSTAL LOWER SUPPORT ANGLE CRACKED STATION 825. REPAIRED PER ESO 80559 DATED 11-21-08. 2 L 7 2 4F A6WE 20081215 NM 2008 12 15 SWAA087005 1 20081210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 7R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087006 1 20081210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 887, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087007 1 20081210 A 5322 6546536 SHEAR TIE BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 40. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087011 1 20081210 A 5322 6546536 SHEAR TIE BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED 10Y CHECK, FOUND SHEAR TIE CRACKED AT BS 540, LBL 15. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087016 1 20081210 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM INNER CHORD CRACKED AT BS 639, LBL 64. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086973 1 20081210 A 5753 6573732 FLAP BOEING 737 7377H4 1384404 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 789SW 29816 DURING SCHEDULED 8Y CHECK, FOUND LTR WING O/B AFT FLAP DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20081215 WP 2008 12 15 AALA200810417 1 20081124 A 5340 BRACKET DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 NUMBER 3 SEAT TRACK LOWER SUPPORT BRACKET CRACKED AT STATION 864. REMOVED AND REPLACED WITH SERVICEABLE BRACKET. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810438 1 20081121 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 NR 3 SEAT TRACK HAS CORROSION OUT OF LIMITS. REMOVED CORROSION, ROUTED AND INSTALLED SEAT TRACK PLUG. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810440 1 20081125 A 5320 ANGLE DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 CRACK IN TEE ANGLE OUTBOARD AND AFT OF VENTRAL STAIRS ACTUATOR RIGHT SIDE, 1497 TO 1510 CANT FRAME. INSTALLED NEW TEE A NGLE PER SRM 51-30-05. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810419 1 20081124 A 5347 CARGO TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 TIE DOWN TRACK SPLICE PLATE CORRODED STATION 1212 TO 1225 (AFT CARGO, LEFT SIDE). REMOVED AND REPLACED WITH SERVICEABLE TRACK SPLICE PLATE. 2 L 7 2 4F A6WE 20081215 EA 2008 12 15 SWIA200820622 1 20081207 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 710SK 10170 FLT 6145 - LAST AISLE OVERHEAD EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081215 WP 2008 12 15 AALA200810450 1 20081125 A 5320 STOP FITTING DOUG DC9 DC982 3022082 WP ZONE 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 AFT DOOR FRAME STOP FITTING CORROSION. REMOVED AND REPLACED FITTING. 2 L 7 2 4F A6WE 20081217 WP 2008 12 17 AALA2008104 1 20081206 A 5320 BRACKET DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 LOWER CORNER BRACKET IN AFT CARGO AT STATION 1211 AND LONGERON 27 RIGHT CORRODED BEYOND LIMITS. REMOVED AND REPLACED BR ACKET PER SRM 51-30-00. 2 L 7 2 4F RT A6WE 20081217 NM 2008 12 17 DHLA2008743507 1 20081111 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 UPPER FUSELAGE CARGO CABIN BS 328 BTWN S-13R AND S-14R FRAME INBD FLANGE AND SUPPORT ANGLE WITH DOUBLE HOLE AND BTWN S-1 6R AND 17R ELONGATED HOLES. REPAIRED FRAME AT BS 328 BTWN S-13R AND 18R IAW B727SRM 51-40-4 FIG 1. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 DHLA2008743508 1 20081111 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 UPPER FUSELAGE CARGO CABIN BS 380 AT LBL 38 AND BETWEEN RBL 53 AND 64 FLOORBEAM CORRODED BETWEEN RBL 53 AND RBL 64. REM OVED CORROSION AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW SRM 53-10-1 FIG 5. REPAIRED FLOORBEAM SECTION AT BS 380 BTWN LBL 29.5 AND LBL 48 IAW SRM 53-10-8 FIG 8. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 UALA2008121106841 1 20081208 A 2613 8242 DETECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE FAULTY A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 653UA 25391 STATUS MSG R ENG OH LP2 DISPLAYED. REPLACED SUSPECT HEAT DETECTOR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081217 NM 2008 12 17 UALA2008121106848 1 20081211 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT SEAT 4J AFT INOP. RELAMPED, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081217 NE 2008 12 17 FDEA200810154371 2 20081015 A 7200 ENGINE AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4E1 52054 NE NR 2 FAILED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 421FE 342 715842 NUMBER TWO ENGINE HUNG START AT 36 PERCENT N2, EGT 506'. ABORTED START FOLLOWED QRH PROCEDURES. SECOND START ATTEMPT NU MBER TWO ENGINE HUNG AT 38 PERCENT N2. START AIR PRESSURE 30 PSI. REJECTED START AT 529'. OBSERVED PEAK EGT 538'. E NGINE REMOVAL APPROVED. DUE TO HIGH DRAG OF THE N2 SPOOL. MOCC/POWERPLANT/MARC. REPLACED NR 2 ENGINE IAW W/C 44T0704- 2 REV 14. OPERATIONAL AND LEAK CHECKS GOOD PER JRM AND AMM 72-00 TEST 13. OK FOR SERVICE. 2 L 7 2 4F 4 F RT A35EU E3NE 20081217 WP 2008 12 17 FDEA200810274845 1 20081027 A 5320 AEA04722 STRUCTURE DOUG MD10 MD1010F 3022112 WP ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 46631 RT MLG W/W BS 1381 RBL 116 OTBD LOWER CORNER OF SLANT PANEL VERTICAL TEE CAP HAS CORROSION. DISPLACED SLANT PANEL IAW S RM 51-31-01; VOL I. REMOVED 7, REPLACED ANGLE IAW SRM 51-33-01; VOL II AND DWG NR AEA0471; REV "A". FABBED AND INSTALL ED NEW ANGLE IAW DAC DWG NR AEA0471, REV "A". RE-INSTALLED SLANT PANEL IAW SRM 51-31-01; VOL I. 2 L 7 3 4F RT A22WE 20081217 WP 2008 12 17 AALA200810454 1 20081125 A 5320 CUSP WEB DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 RIGHT CUSP CORRODED STATION 845. REPAIRED PER AARD 53-20-00-10. 2 L 7 2 4F RT A6WE 20081217 WP 2008 12 17 AALA200810455 1 20081126 A 5320 FITTING DOUG DC9 DC983 3022083 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 DOOR STOP BACK UP FITTING IS CRACKED AT LOWER FASTENER ON LEFT SIDE OF VAULT DOOR OPENING, LOWER FITTING. INSTALLED SER VICEABLE DOOR STOP FITTING PER SRM 51-01. 2 L 7 2 4F RT A6WE 20081217 NM 2008 12 17 FDEA200810034182 1 20081003 A 5310 7075T6511 CREASE BEAM BOEING 757 75723A 1384967 NM BS 1390-1630 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 920FD 24289 MAIN CABIN, STA 1620-1640, RT SIDE INBD CREASE BEAM CHORD HAS CORROSION. REMOVED CORROSION AND CHECK LIMITS, FOUND TO B E OUT OF LIMITS IAW SRM 53-60-03 FIG 101 DETAIL III. REMOVED CREASE BEAM INBD CHORD, FABRICATED CREASE BEAM INBD CHORD IAW SRM 51-10-02 SECTION 8. LOCATED AND DRILLED CREASE BEAM INBD CHORD, TREATED AND PRIMED INBD CHORD AND INSTALLED INB D CHORD IAW 51-40-02. 2 L 7 2 4F RT A2NM 20081217 NM 2008 12 17 FDEA200811154884 1 20081115 A 5320 6523638 STRAP BOEING 727 7272S2F 1384O81 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 216FE 22937 AREAS OF CORROSION ON FWD CARGO PIT UPPER FLOORBEAM STABILITY STRAP AS MARKED. REMOVED CORROSION FOUND OUT OF LIMITS RE F SRM 53-10-01. FABRICATED STRAP AND SPLICE PLATE REF DWG 65-23638 AND 66-14865. TREATED, PRIMED AND INSTALLED STABILI TY STRAP AND SPLICE BS 620-720C RBL 48 REF SRM 51-10-2 AND MM 51-20-151-7 AND 51-30-2. THIS IS CLASSIFIED AS A MINOR RE PAIR. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 DHLA2008743506 1 20081117 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 LOWER FUSELAGE E/E COMPARTMENT BS 328 WL 208 RBL 44 FLOORBEAM WITH CORROSION. REPLACED FUSELAGE FLOORBEAM SECTION AT BS 328 BETWEEN LBL 63 AND RBL 63 IAW SRM 51-10-1 PARA 7. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 UALA2008121106842 1 20081208 A 3610 7732887810 SHUTOFF VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT ENGINE FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 664UA 29236 LEFT ENGINE HIGH STG SYSTEM FLUCTUATES WILDLY FROM 15-40 PSI AT 75-77 PCT N2. ABOVE 80 PCT N2, PNEU STEADY AT ALL POWER SETTINGS. REPLACED HI STAGE VALVE AND CONTROLLER. FAILED TEST AFTER VALVE REPLACEMENT. ACP'D PNEUMATIC HEALTH CK ON PRV & PRC, HPSOV & HPC, FAMV, AND PRSOV. PRSOV FAILED HEALTH CK. REPLACED PRSOV BLEED SHIFT & OPS CHECK PERFORMED, ALL NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081217 WP 2008 12 17 AALA200810468 1 20081202 A 5313 LONGERON DOUG DC9 DC983 3022083 WP BS 160 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 STATION 160 AT LONGERON LEFT 3 IS CRACKED AT FASTENER. INSTALLED REPLACEMENT SPLICE LONGERON AT STATION 160 AT LEFT 3 P ER SRM 53-02. 2 L 7 2 4F RT A6WE 20081217 NM 2008 12 17 UALA2008121006829 1 20081210 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT EEL LIGHT INOP AT SEAT ROW 52 LEFT. REPAIRED WIRES, OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081215 NM 2008 12 15 UALA2008111305393 1 20080822 A 2611 2156556HS SMOKE DETECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CREW REST AREA FALSE ACTIVATION A UALA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 WP 29 107UA 26900 SMOKE ALARM IN FLT ATT CREW REST AREA WENT OFF 2X ON TAXI IN. ALSO LOUD NOISE HEARD BENEATH 5L. DOOR 5 SMOKE DETECT CB CYCLED, SYS RESET, ALL OPS NORMAL. UNABLE TO REPRODUCE LOUD NOISE UNDER 5L. NO FAULT FOUND. 2 L 7 4 4F 4 F RT A20WE E24NE 20081216 NM 2008 12 16 UALA2008111306169 1 20081017 A 3350 3071BPEGPL LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 781UA 26945 SEAT 24G EMERGENCY LIGHT IS OUT. RELAMPED, TESTED GOOD. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081217 NM 2008 12 17 UALA2008120806784 1 20081207 A 8012 7755386 START VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 547UA 25368 L ENG STARTER EICAS WHEN START SELECTOR SWITCH PLACED INTO GND. REPLACED START VALVE AND CHECK OKAY. 2 L 7 2 4F 4 F RT A2NM E17NE 20081217 NM 2008 12 17 UALA2008111303688 1 20080702 A 2997 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 PYLON CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NR 1 ENG PYLON HYD BAY WIRE W390-082-18 IS CHAFED. REPLACED WIRE. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081217 NM 2008 12 17 SWAA087082 1 20081213 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 731SA 27863 DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION BEARING O/B UPPER ATTACH LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087067 1 20081211 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 313SW 23335 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 583, STR 10R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087041 1 20081211 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 967, STR 21L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 C8GA20080038 1 20080905 A 5330 SKIN BOEING 727 727200 138407E NM BS 684 MISREPAIRED A C8GA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING VISUAL INSP. FOR DTA FOUND EXISTING EXTERNAL FUSELAGE REPAIR AT STA. 684 STR. 27L TO BE NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR,CUT OUT DAMAGE AND VERIFIED CRACK CONTAINMENT. FABRICATED FILLER AND FABRICATED DOUBLER. INSTALLED REPAIR PER SRM 53-30-03. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F RT A3WE 20081217 NM 2008 12 17 C8GA20080039 1 20080905 A 5330 SKIN BOEING 727 727200 138407E NM BS 684 MISREPAIRED A C8GA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING VISUAL INSP. FOR DTA FOUND EXISTING EXTERNAL FUSELAGE REPAIR AT STA. 684 STR. 27R TO BE NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR,CUT OUT DAMAGE AND VERIFIED CRACK CONTAINMENT. FABRICATED FILLER A ND FABRICATED DOUBLER. INSTALLED REPAIR PER SRM 53-30-03. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F RT A3WE 20081217 EU 2008 12 17 FDEA200812115133 1 20081211 A 3230 BDM3003 ELECTRONIC UNIT AIRBUS 300 A300B4605R 3930308 EU MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 21 683FE 2555 2555 801 LANDING GEAR FAILED TO RETRACT, TRIED BOTH SYS 1 2. RETURN TO AIRPORT. FOLLOWED TSM 32-30-00, BITE CHECKED PROX DET, FAULT CODE: BR.(RT.BOGIE FAIL).INSP RT LDG GEAR BOGIE BEAM SENSOR 12GA. WHILE REMOVING POX DETECTOR SUPPORT BOLT FOUND WATER IN HOUSING. REMOVED AND DRIED SAME AND LUBED IAW MM 32-11-14-6. CLEANED AND INSPECTED C/P 1930C REF AWM 32-31 -02. INSP PITCH DAMPER IAW MM 12-12-32-0 BITE TEST PROX DET PROCESSING UNIT (54GB) FAULT HAS CLEARED. RESET/TESTED AGAIN WITH NO FAULTS RECORDED. IAW MM 32-31-71-4. ORDERED PROX. UNIT AS PRECAUTION. REF WRI: 32-30-7268. REMOVED AND RE PLACED PROXIMITY DETECTOR PROCESSING UNIT PER MM 32-31-71-4. PERFORMED OPS CHECK. PASSED. LUBRICATED PIVOT PIN AIW MM 1 2 L 7 2 4F RT A35EU 20081217 NM 2008 12 17 SWAA087043 1 20081211 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 947, STR 23R. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087048 1 20081211 A 5311 65C22909 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087049 1 20081211 A 5311 6546529 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087052 1 20081211 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 294, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087077 1 20081213 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED MV2 CHECK, FOUND STRINGER CRACKED AT BS 500C, STR 16R. REPAIRED STRINGER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087079 1 20081213 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 731SA 27863 DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION BEARING I/B LOWER ATTACH LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087085 1 20081213 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 731SA 27863 DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION BEARING O/B UPPER ATTACH LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087095 1 20081214 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 430 AT RADIO ALTIMETER ANTENNA CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087101 1 20081215 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087102 1 20081215 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087103 1 20081215 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 UALA2008120906817 1 20081209 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CEILING UPPER DE INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 116UA 26908 EMERGENCY CEILING LIGHT UPPER DECK ABOVE STAIRS INOP. RELAMPED EMERGENCY LIGHT. 2 L 7 4 4F 4 F RT A20WE E24NE 20081217 NM 2008 12 17 SWAA087138 1 20081215 A 5330 6545800 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED BETWEEN BS 265 TO BS 275, STR 15R. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087109 1 20081214 A 3350 8210248801 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 287WN 32537 FOUND FWD ENTRY FLOOR LEVEL EMERGENCY EXT SIGN LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087111 1 20081215 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 402WN 29814 LT EEPLS LIGHT STRIP COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087118 1 20081215 A 5312 6517582 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED SPV CHECK, FOUND BULKHEAD VERTICAL BEAM WEB CHORD CRACKED AT BS 178, RBL 17, WL 230. REPAIRED CHORD PE R SRM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087119 1 20081215 A 5312 6517853 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED SPV CHECK, FOUND BULKHEAD VERTICAL BEAM WEB CHORD CRACKED AT BS 178, RBL 5.7, BETWEEN WL 198 TO WL 199. REPAIRED CHORD PER SRM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087121 1 20081215 A 3350 65C27095 BATTERY BOEING 737 737317 138447P NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND AFT CABIN EMERGNECY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087128 1 20081215 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 UALA2008120906815 1 20081209 A 3397 58791 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHTS BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 RIGHT AFT GALLEY EMERGENCY LIGHT BAR IS INOP. REPAIRED BROKEN CABLE ON LIGHT BAR. CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 UALA2008120906818 1 20081209 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 116UA 26908 MAIN GALLEY EMERGENCY LIGHT LT AND FWD WALL INOP. REPLACED EMERGENCY LIGHT FEEDER CABLE. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081218 NM 2008 12 18 UALA2008120906820 1 20081209 A 3397 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 116UA 26908 EMERGENCY LIGHT ON SEATS 1A, 2A, 3A&E, 4A, 5A&E INOP. REPLACED EMERGENCY LIGHT FEEDER CABLE. OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081218 NM 2008 12 18 UALA2008120906821 1 20081209 A 3397 7945243 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 116UA 26908 EMERGENCY LIGHT ON SEAT 4E&F AND 5F INOP. REPLACED EMERGENCY LIGHT FEEDER CABLE. OPS CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081218 NM 2008 12 18 UALA2008120906822 1 20081209 A 3397 794640 FEEDER CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 116UA 26908 EMERGENCY LIGHT ALONG FWD GALLEY WALL LT AND RT SIDE INOP. REPLACED EMERGENCY LIGHTS FEEDER CABLE. OPS CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081218 NM 2008 12 18 UALA2008120906823 1 20081209 A 5330 SKIN BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU FUSELAGE DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 381UA 24656 DAMAGE TO ACFT BELOW & AFT OF DOOR 1L. DIMENSIONS 2.6 FT BY 4 INCHES WIDE RUNNING ALONG STRINGER, 15 INCHES BELOW LAP J OINT. MAJOR REPAIR ACCOMPLISHED. NO STRINGER DAMAGE. CUT OUT DAMAGED SKIN. DOUBLERS DRILLED, TRIMMING COUNTER SINK H OLES & PRIME. ALL PARTS PRIMED AND READY TO INSTALL. INSTALLED REPAIR PARTS. 2 L 7 2 4F 4 F RT A16WE E21EU 20081215 NM 2008 12 15 QXEA2008121001235 1 20081208 A 2435 400SG163Q STARTER GEN BOMBDR DHC8 DHC8402 1390042 NM NR 1 FAILED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 19 422QX 235 4150 BLI - NR 1 ENGINE APPEARED TO HANG START DURING START ATTEMPT. RAMP PERSONNEL SAID SPARKS WERE COMING OUT OF THE DC GEN ERATOR VENT PORTS. REMOVED AND REPLACED NR 1 ENG DC STARTER GEN IAW MTC 6243101. OPS CKS GOOD, NO FURTHER DEFECTS NOTE D. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081215 NM 2008 12 15 SWAA086998 1 20081210 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND STRINGER CORRODED AT BS 908 TO BS 927, STR 24R. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086999 1 20081210 A 5322 6546546 SHEAR TIE BOEING 737 7373A4 1384585 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087036 1 20081211 A 5753 65C26714 SKIN BOEING 737 7373H4 1384600 NM FORE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND RT WING O/B FORE FLAP SKIN CRACKED AT ATTACH FITTING CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086986 1 20081210 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 25L TO 26L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087025 1 20081211 A 5330 6545772 SKIN PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 361SW 26572 DURING SCHEDULED HC1 CHECK, FOUND KEEL BEAM LOWER SKIN PANEL CRACKED AT LT BS 680. REPAIRED SKIN SWA EA. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087026 1 20081211 A 3350 81000 TRACK BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 409WN 27896 FOUND EEPLS TRACK LOOSE AT ROW 11. SECURED STRIP PER MM. 2 L 7 2 4F RT A16WE 20081215 WP 2008 12 15 AALA200810416 1 20081202 A 5320 STRAP DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 STRAP CORRODED IN LONGERON 23L FROM 1287 TO 1306. REMOVED AND REPLACED WITH SERVICEABLE STRAP. 2 L 7 2 4F A6WE 20081215 NM 2008 12 15 AALA200820091 1 20081202 A 5315 146N508919 FLOORBEAM BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 56842 24599 FLOORBEAM CORRODED, REPAIRED FLOORBEAM IAW SRM 53-0-51. 2 L 7 2 4F RT A2NM 20081215 WP 2008 12 15 AALA200810436 1 20081121 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 NR 6 SEAT TRACK CORROSION OUT OF LIMITS STATION 933 TO STATION 936. REPAIRED DAMAGE BY INSTALLING PLUG PER AARD 53-20-0 0-10. 2 L 7 2 4F A6WE 20081215 EA 2008 12 15 SWIA200820624 1 20081207 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 431SW 7536 FLT 4757 - FORWARD EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081215 WP 2008 12 15 AALA20081094 1 20081208 A 5740 FITTING DOUG DC9 DC982 3022082 WP ZONE 500 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7542A 49996 CRACK IN GROUND SPOILER ACTUATOR FITTING LEFT WING. REPAIRED PER AARD 57-20-00-15 AND ESO 80559 DATED 12-05-08. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810487 1 20081202 A 5340 FITTING DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 982TW 53632 LEFT MAIN LANDING GEAR WHEEL WELL, TRAPEZOID FITTING TOP ATTACH ANGLE CORRODED. REPLACED TRAPEZOID FITTING ATTACH ANGLE PER SRM 57-09-00. 2 L 7 2 4F RT A6WE 20081215 NM 2008 12 15 AALAL200820087 1 20081129 A 5320 146N5318 PLATE BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AA 57228 24591 AFT MAIN DECK PLATE CORRODED, REPAIRED AFT DECK PLATE IAW SRM 53-60-51-2R2 AND EA B757-53-00-4996. 2 L 7 2 4F RT A2NM 20081216 NM 2008 12 16 UALA2008111306195 1 20081020 A 5754 SLAT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 AND 2 DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 512UA 24809 NR 1 AND NR 2 LEADING EDGE SLAT AND UNDER WING PANEL 521MB DAMAGED BY AIR STAIR. SLATS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081216 NM 2008 12 16 UALA2008111406508 1 20081113 A 3610 REGULATOR VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE BLEED AIR SYS FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 598UA 28751 WHILE RE-ACTIVATING NR 2 ENG HS-PILOT FOUND OVERPRESSURE INDICATOR POPPED. RESET, RAN ENG AT IDLE. PRESSURE INDICATING 18 PSI. REF MEL 3611D BY- 118169: ACP'D PNEUMATIC HEALTH CK ON NR 2 ENG ON H-S PILOT, HPSOV, PRC, AND PRSOV. PRSOV C ONTROLLER FAILED REF PRESSURE, PRESS EXCEEDED LIMIT. REPLACED PRSOV REGULATOR AND HIGH STAGE PILOT. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081217 NE 2008 12 17 UALA2008120806770 2 20081207 A 7230 6A7614 FAN BLADE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE DAMAGED A UALA A UNSCHED LANDING W C INADEQUATE Q C F.O.D. CL CLIMB 1 WP 29 415UA 475 V10789 BIRD INJESTION NR 2 ENGINE. RTFL. CREW REPORTS 4EA FAN BLADES FOUND DAMAGED UPON ARRIVAL. INSPECTION COMPLETED, BLADE S REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081217 EA 2008 12 17 SWIA200820626 1 20081019 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 965SW 7871 C-CHECK, STATION 280 FLOOR SUPPORT BEAM RBL9/LBL9 CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081217 NM 2008 12 17 DHLA2008743501 1 20081112 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 LOWER FUSELAGE AFT CARGO COMPARTMENT AT BS 950D RBL13 AND RBL 30 FLOORBEAM LOWER FLANGE WITH CORROSION. REPAIRED FLOORB EAM LOWER CHORD FWD FLANGE AT BS 950D BETWEEN RBL 2 TO RBL 20 WL 200 IAW B727 SRM 53-10-8 FIG 8. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 DHLA2008743502 1 20081112 A 5320 STRAP BOEING 727 727225 1384077 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 LOWER FUSELAGE CARGO COMPARTMENT FROM BS 1070 TO BS 1130 LBL 25 FLOOR BEAM STABILIZER STRAP WITH CORROSION. REPLACED FL OORBEAM STABILIZER STRAP FROM BS 1046.5 TO BS 1130 LBL 25 IAW B727SRM 53-10-8 FIG 6. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 DHLA2008743503 1 20081113 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 UPPER FUSELAGE CARGO CABIN FROM BS 950 TO BS 1166 BL 0 SEAT TRACK WITH CORROSION AND BARE METAL. REPLACED CARGO SEAT TR ACK FROM BS 950C TO 1010 BL 0 IAW SRM 51-10-1 PARA 7D. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 DHLA2008743504 1 20081110 A 5753 SKIN BOEING 727 727225 1384077 NM LT WING TE FLAP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 LT WING OTBD FORE FLAP L/E LOWER SURFACE WITH WEAR AT WBL 492. REPAIRED L/E SKIN SECTION AT OTBD FORE FLAP LT WING FROM WBL 492.5 TO WBL 482.5 IAW SRM 57-50-4 FIG 4. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 FDEA200812125134 1 20081212 A 5720 SUPPORT BRACKET BOEING 727 727225 1384077 NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 469FE 21581 LT WING L/E SLAT ACTUATOR SUPPORT BRACKET CRACKED INBD SIDE AT NR 1 SLAT. REMOVED AND REPLACED NR 1 SLAT STA 390.9 RIB, WEB, AND DOUBLER IAW EA 7-5750-126863. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 DHLA2008743509 1 20081120 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 UPPER FUSELAGE CARGO CABIN BS 328 BTWN LBL 45 AND RBL 45 FLOORBEAM UPPER CHORD CORRODED. REPLACED FLOORBEAM SECTION AT BS 328 WL 208 BTWN RBL 63 AND LBL 63 DUE TO CORROSION IAW SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081217 GL 2008 12 17 FDEA200810024173 2 20081002 A 7323 ENGINE DOUG MD10 MD1010F 3022112 WP GE CF6 CF66D 30020 GL NR 3 FLAMED OUT A FDEA C ABORTED TAKEOFF R X J PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 CE 21 384FE 46617 451125 NR 3 ENGINE FLAMED OUT ON TAKEOFF ROLL. ENGINE ROLLED BACK TO ABOUT 8 PERCENT N1; FF INTERMITTENT FROM 0-500. EGT LO WER THAN OTHER 2 AT IDLE. REPLACED THE FUEL CONTROL AND FUEL PUMP. 2 L 7 3 4F 4 F RT A22WE E23EA 20081217 WP 2008 12 17 FDEA200811054721 1 20081105 A 5755 NRC6050507 SKIN DOUG DC10 DC1030F 3023504 WP NR 4 SPOILER CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 319FE 47820 LT WING NR 4 SPOILER FOUND CRACK ON UPPER SURFACE SPOILER. SDR WRITTEN IN ERROR, SPOILER WAS REMOVED AND REPLACED WITH OVERHAULED UNIT. 2 L 7 3 4F RT A22WE 20081217 WP 2008 12 17 FDEA200811124865 1 20081112 A 5711 ARB0007502 SPAR CAP DOUG MD10 MD1010F 3022112 WP ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 397FE 46631 APPROX 2.75 INCH CRACK EXISTS IN RT WING LOWER SPAR CAP (PSE 57.10.008) AT XORS = 411. CRACK RUNS FROM AFT EDGE OF SPAR CAP AFT TANG, FWD APPROX 1.625 INCH TO RADIUS, THEN UPWARDS AND INBOARD APPROX 1.125 INCH AND TERMINATES AT VERTICAL LE G FASTENER AT APPROX = 410. REPAIRED SPAR CAP AT XORS 411 IAW EA 8-5710-123520. 2 L 7 3 4F RT A22WE 20081217 EU 2008 12 17 FDEA200812115123 1 20081211 A 5753 A5794253300060 SKIN AIRBUS 300 A300F4605R 3930327 EU LT WING TE FLAP DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 687FE 873 LT WING INBD FLAP BOTTOM SURFACE IS DENTED AT 67 INCH FROM THE INBD EDGE AND 22 INCH FROM THE TRAILING EDGE. DENT WAS F OUND TO BE OUT OF LIMITS IAW SRM 57-50-00, PG 120, FIG 105. REMOVED DAMAGE IAW SRM 57-55-00, PG 225, FIG 6. FABBED DOU BLER AND 1 FILLER IAW SRM 57-50-00 PGS 215-220. INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 57-50-00 PGS 215-220. ALOD INED IAW SRM 51-21-10. PRIMED IAW SRM 51-23-10. APPLIED TOP COAT IAW SRM 57-50-00 PG 219. 2 L 7 2 4F RT A35EU 20081217 EU 2008 12 17 FDEA200811244962 1 20081124 A 5270 A5237424900600 SWITCH AIRBUS 310 A310222 3930315 EU CARGO DOOR DAMAGED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 21 455FE 331 AFT CARGO DOOR OPEN LIGHT IN FLIGHT. ACN RELEASED FOR SERVICE PER MEL/CDL, 52-71-01 CARRIED OUT OVERWEIGHT LANDING INSP ECTION PER AMM 05-51-11-0, NO ABNORMALITIES NOTED. OLD CONTROL NUMBER: , REMOVED AND REPLACED AFT CARGO DOOR LIMIT SWIT CH 32WS AND HOUSING AS PER MM 52-71-11-4. PERFORMED SWITCH ADJUSTMENT/TEST AS PER MM 52-71-11-5, NORMAL. REMOVED PLACA RD AND CLEARED MEL. 2 L 7 2 4F RT A35EU 20081217 NM 2008 12 17 SWAA087068 1 20081212 A 3350 101114 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 337SW 23959 RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087060 1 20081211 A 5311 6546540 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND MID CABIN FRAME CRACKED AT BS 639, WL 216 LT SIDE. REPAIRED FRAME PER DWG. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087061 1 20081211 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND KEEL BEAM CORRODED AT BS 787, STR 27L. REPAIRED BEAM PER ER. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087071 1 20081211 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 487WN 33854 DURING SCHEDULED MV3 CHECK, FOUND EEPLS LIGHT LENS COVER MISSING AT ROW 1. REPLACED COVER PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087047 1 20081211 A 5311 6546558 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087072 1 20081213 A 3350 101114 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 611SW 27697 FWD EMERGENCY EXIT SIGN LENS COVER MISSING. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087084 1 20081213 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 731SA 27863 DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION BEARING I/B UPPER ATTACH LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087096 1 20081214 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 450 AT RADIO ALTIMETER ANTENNA CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087137 1 20081215 A 5210 6562212 SKIN BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR SKIN CRACKED BELOW UPPER HINGE CUTOUT. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087139 1 20081215 A 5330 6545776 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED BS 980, STR 21L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081217 NE 2008 12 17 SWAA087108 2 20081216 A 7200 CFM567B24G22 ENGINE BOEING 737 7377H4 1384404 NM CFMINT CFM567 CFM567B22 13802 NE NR 1 FAILED A SWAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 29 904WN 36616 896213 ABORTED TAKEOFF DUE TO LOUD BANG HEARD AND AIRPLANE STARTED TO TURN LEFT. NR 1 ENGINE SHOWED ENGINE FAILED ON EGT N1'S WAS APPROX 84 PERCENT AND LOW GROUND SPEED. REMOVED AND REPLACED NR 1 ENGINE PER MM. 2 L 7 2 4F 4 F RT A16WE E00055EN 20081217 NM 2008 12 17 SWAA087110 1 20081214 A 3350 101114 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 337SW 23959 DURING SCHEDULED MV1 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087112 1 20081215 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 402WN 29814 RT EEPLS LIGHT STRIP COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087120 1 20081215 A 5754 65C26002 SLAT BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT I/B END DELAMINATED AT EDGE. REPAIRED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20081217 2008 12 17 SWAA087129 4 20081215 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087130 1 20081215 A 5311 6554892 SUPPORT BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND FRAME SUPPORT WEB CRACKED AT BS 348, STR 15L. REMOVED AND REPLACED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 UALA2008120806783 1 20081207 A 8011 35054367 STARTER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 655UA 25393 724465 NR 2 ENGINE NO START. REPLACED STARTER. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 SWAA087143 1 20081215 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM . 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 SWAA087144 1 20081215 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 316SW 23338 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 440, STR 16L. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 SWAA087145 1 20081215 A 5330 6545768 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED 24Y CHECK, FOUND E & E COMPARTMENT SKIN CRACKED BETWEEN BS 360 TO BS 380, STR 28R. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 20081218 EU 2008 12 18 UALA2008120906796 1 20081208 A 2597 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE PAX DOOR DISCONNECTED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 474UA 1475 AFT RT CABIN DOOR SLIDE ASSY CONNECTOR BETWEEN CABLE LOOP ASSY AND COVER RELEASE CABLE WAS FOUND DISCONNECTED. CABLE LO OP ASSY AND COVER RELEASE CABLE CONNECTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081218 NM 2008 12 18 UALA2008111304095 1 20080804 A 2842 1835KTU01 PROBE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE RT WING FAULTY A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 782UA 26948 FUEL QTY SHOWS ERRATIC. RT WING QTY IND FLT DIVERTED. CREW COMMENT: AFTER LANDING ALL FUEL QTY IND WORK NORMAL. CHEC KED FUEL QTY BY STICK GAUGE. FOUND CMC MSG 28-20123, 28-20127 & 28-20145 CAME ON. TANK UNIT 17, 19 & 9 FAULT. REPLACE D RT FUEL PROBES NR 9, 17 & 19. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 NM 2008 12 18 UALA2008111306173 1 20081017 A 3350 20121 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 548UA 25396 DURING EMERG LITE TEST, FOLLOWING BULLNOSE LIGHTS INOP, 4AB, 6AB, 10CD, 13 CD, 14 AB, 15 AB, 20 CD, 21 AB, 23 CD, 27 CD, AND 29 AB. LAMPED ALL LISTED LOCATIONS. ALSO REPLACED BATTERY PACK M10568, OPS CHECKS GOOD. INSTALLED JIFFY SPLICES ALL LOCATIONS. FOUND SWITCH S10219 BAD. REPLACED AND TEST GOOD. FOUND MID CABIN EMERGENCY TEST SWITCH BAD, REPLACED A ND OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081218 NM 2008 12 18 UALA2008111306184 1 20081019 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR SHORTED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 569UA 26677 DOOR 2R AND PARTS OF AFT CABIN EMER EXIT LIGHTS ARE ON. REPLACED SHORTED BULB FOR DOOR 2 RIGHT EXTERNAL EMERGENCY LIGHT AND REPLACED INOP BATTERY PACK AT STA LOC 1240 ITEM M10699 REF WDM 33-51-14 PG 1 AND MM 33- 51-06 AND MM 33-51-07. SYS CHECKD NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 20081218 NM 2008 12 18 UALA2008111306230 1 20081021 A 3320 RECEPTACLE BOEING 767 767222 1385122 NM PWA 2037 PW2037 NE MID LAVATORY DAMAGED A UALA A UNSCHED LANDING W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 556UA 26650 BURNING ODOR REPORTED. MID LAV FLOW LIGHT AFT LAMP RECEPTACLES ARE CHARRED. NEED REPLACEMENT. REMOVED LAMPS FROM MIRR OR LAMP. DOME LAMP WORKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E17NE 20081218 2008 12 18 UALA2008120906806 4 20081209 A 2565 69B528083 HOUSING BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 LT OVERWING ESCAPE SLIDE DISCONNECT HOUSING CRACKED. INSTALLED NEW DISCONNECT HOUSING. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 UALA2008120906809 1 20081209 A 5210 HANDLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE PAX DOOR OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 LT FWD ENTRY DOOR EXTERIOR HANDLE FAILS FREEPLAY CHECK (EXCEEDS 0.35 INCH). ADJUSTED EXTERIOR HANDLE. FREE PLAY CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 UALA2008111306413 1 20081106 A 2997 BMS1360T11C02G18 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE HYDRAULIC SYS FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 543UA 25698 LT HYD QTY "LOW" PRESSURE DISPLAYED ON HYDRAULIC PAGE ALONG WITH OVERHEAD "RSVR" LIGHT ILLUMINATED. FOUND LEAKING CAP A T PRESSURIZATION MODULE. REPLACED CAP, LEAK CHECK GOOD WITH APU BLEED AND ENG BLEED. REPLACED LEFT SIDE HYDRAULIC RESE RVOIR. OPS OKAY. FOUND WIRE WITH HIGH RESISTANCE. REMOVED & REPLACED WIRE. WILL NEED TO PRESSURIZE RESERVOIR TO CONF IRM FIX. 2 L 7 2 4F 4 F RT A2NM E17NE 20081218 NM 2008 12 18 UALA2008111303985 1 20080725 A 2750 654W00382 FSEU BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE TE FLAP FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 210UA 30216 STATUS MESSAGES PFCS INTERFACE & FLAP-SLAT CONTROL 1 WILL NOT ERASE. REPLACED FSEU 1. REPLACED SFCU 1. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 NM 2008 12 18 UALA2008111304150 1 20080806 A 2822 32C171 VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FUEL SYSTEM FAULTY A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 216UA 30549 UNWANTED FUEL TRANSFER. REPLACED BOTH RT FWD AND AFT BOOST PUMP DISCHARGE VALVES. PERFORMED ITEMS 1 AND 4 REF MT28-008 R2, AND DISCHARGE CK VLV FUNCTIONAL TEST. REPLACED NR 2 FUEL FLOW TRANSMITTER. NO FURTHER DEFECTS NOTED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 NM 2008 12 18 UALA2008111304171 1 20080808 A 5610 58935733 WINDOW BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT CRACKED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 914UA 25381 CREW REPORTS THE CAPTAIN'S NR 4 WINDOW PANE IS CRACKED. AWAITING SHOP FINDINGS. REPLACED WINDOW. 2 L 7 2 4F 4 F RT A16WE E21EU 20081218 NE 2008 12 18 UALA2008111304351 2 20080820 A 7421 50U984 IGNITER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT ENGINE FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 214UA 30220 ENG IGNITER L1 LEFT ENGINE FAILED TO IGNITE USING IGNITER 1. REPLACED IGNITER L1 ON LEFT ENGINE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 NM 2008 12 18 UALA2008120506764 1 20081205 A 2560 MECHANISM BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE GIRT BAR LACK OF LUBE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 795UA 26927 THE 3R IS ARMED AND FROZEN, PACK COVER REMOVED AND PINNED. CLEANED AND LUBED GIRT BAR MECHANISM SYSTEM CHECKS OK. PINS REMOVED AND STOWED IN POUCH; ACFT RETURNED TO NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 NM 2008 12 18 UALA2008121106854 1 20081211 A 5330 SKIN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 585UA 26709 EXTERNAL FUSELAGE STA 1680 BETWEEN STR 27L AND 28L DENTED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN AND INSTALL ED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081218 NM 2008 12 18 FDEA200812115121 1 20081211 A 5740 651724024 BRACKET BOEING 727 727225 1384077 NM ZONE 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 469FE 21581 RT WING NR 7 SLAT ACTUATOR MOUNTING BRACKETS BOTH INBD AND OTBD ON WING SIDE ARE CRACKED AT WS 635. REMOVED AND REPLACE D INBD AND OTBD NR 7 SLAT ACTUATOR MOUNTING BRACKETS AND STEEL DOUBLERS IAW FEDEX EA 7-5750-126869, WINGS, RT NR 7 SLAT STA 281.4 AND 288.6 ACTUATOR SUPPORT RIB, REPAIR OF STIFFENER AND DOUBLER CRACKS PER SB 727-57-130. 2 L 7 3 4F A3WE 20081218 NM 2008 12 18 UALA2008111306257 1 20081024 A 2710 2828001011 CONTROL UNIT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE AILERON FAULTY A UALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 WP 29 663UA 27160 RUDDER AND AILERON TRIM EXCESSIVE WITH AILERON DEFLECTED. SUSPECT LEFT INBD AILERON STUCK IN UP POSITION, AS IND ON EIC AS FLT CONT, IS DEFLECTED APPX HALF UP AND NOT RESPONDING TO INPUT. RUDDER AND AIL TRIM IS EXCESSIVE. AILERON FOR 6 HR S WAS ABOUT HALF DEFLECTED AND THEN WORKED ITS WAY TO ABOUT 1-4 DEFLECTION AS SEEN IN YOKE AND TRIM USED. FOUND LT INBO ARD AIL, BOTH LT & CNTR SYS PCA'S HAVE QUICK DROOP & ARE BYPASSING (BOTH PCA'S MANUAL MANIPULATION WITH SYS PRESS APPLIE D). REPLACED CTR SYS PCA. REPLACED LT INBOARD & OUTBOARD AILERON LEFT SYSTEM PCA. REPLACED RT NR 7 OVERRIDE SPOILER A CTUATOR & LT SPOILER OVERRIDE ACTUATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 UALA2008111304370 1 20080820 A 5753 113W30034 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE TE FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 RT WING O/B FLAP 12 INCHES FROM I/B END AND 48 INCHES FROM AFT END, SKIN IS WORN. ACP REPAIR PER 777 EN-57-00 46-01, TH E REPAIR IS APPROVED BY BAC, FORM 8100-9. THE REPAIR IS PERMANENT REPAIR. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 NM 2008 12 18 UALA2008111304371 1 20080820 A 5753 113W30033 SKIN BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE TE FLAP WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 771UA 26932 LT WING O/B FLAP 12 INCHES FROM I/B END AND 48 INCHES FROM AFT END, SKIN IS WORN. ACP REPAIR PER 777EN57-004 7-01. THE REPAIR IS APPROVED BY BAC FORM 8100-9. THE REPAIR IS PERMANENT REPAIR. NO RE-INSPECTION IS REQUIRED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 NM 2008 12 18 UALA2008111306194 1 20081020 A 3320 RELAY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE P-19 PANEL DAMAGED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 644UA 25094 RELAYS K417 AND K383 IN P-19 PANEL SHOW SIGNS OF OVERHEATING. REMOVED AND REPLACED RELAYS. PERFORMED A GOOD OPS CHECK OF THE NS-FSB SIGNS AND OPS CHECK OF L-1 DOOR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 UALA2008111305489 1 20080827 A 2822 5006286C PUMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUEL SYSTEM FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 651UA 25389 BOTH MAIN TANKS FED WHILE THERE WAS 12000LBS IN CENTER TANKS. RIGHT MAIN TANK FED FASTER, IMBALANCE OF 2000LBS. SUSPEC T BAD OVERRIDE PUMPS. FOUND PUMP LEAKING DURING OPS CHECK. REMOVED PUMP TO REPLACE O-RINGS. DURING INSTALLATION SHOUL DER SCREW BROKE. NEEDS NEW SHOULDER SCREW AND REINSTALL PUMP. CHANGED BOTH RT AND LT OJ PUMPS. OP CHECKS & LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 UALA2008121006834 1 20081209 A 3020 2790583108 ANTI-ICE VALVE BOEING 767 767322 1385200 NM PWA 4052 PW4052 52119 NE NR 2 ENGINE FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 673UA 29241 EICAS MSG ENG ANTI-ICE DISPLAYED AND ENG ANTI-ICE VALVE LIGHT REMAINED ILLUM WITH SW OFF, POSITION 2. REPLACED NR 2 ENG INE ANTI-ICE VALVE. OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 UALA2008121006835 1 20081210 A 4920 CHARGER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE APU BATTERY FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 644UA 25094 APU AUTO SHUT DOWN. TAXI CREW TRIED STARTING IT SEVERAL TIMES WITH NO START, BIT OF APU CONTROLLER SHOWED NO ACCEL IN P OSITION 1 AND OVERTEMP IN POSITION 4 THRU 5. REPLACE APU BATTERY CHARGER. APU SLOW TO GET TO SPEED AND DUCT PRESSURE 1 0 PSI. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 AALA200810497 1 20081216 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM BS 986 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CORROSION ON FLOORBEAM STATION 986.5 AT LEFT BUTT LINE 36. REPAIRED PER SRM 53-00-21-2R. 2 L 7 2 4F RT A16WE 20081218 EU 2008 12 18 FDEA200812125135 1 20081212 A 3230 A252791 RESTRICTOR VALVE AIRBUS 300 A300F4605R 3930327 EU MLG DIRTY A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 CE 21 671FE 778 ON APPROACH, LOWERED LANDING GEAR, LT MAIN GEAR SHOWED UNSAFE IN BOTH SYS 1 AND SYS 2 AND NR 3 GEAR SYS. ON GO AROUND, GEAR CAME DOWN. CREW AND STATED LIGHTS WENT SAFE AFTER GO AROUND, RAISED GEAR AND TRIED AGAIN. RECEIVED UNSAFE LIGHTS AGAIN FOR LT MLG. FOUND LT GEAR WOULD TAKE APPROX 90-120 SECONDS TO START TO EXTEND AFTER RT GEAR, THEN WOULD OPERATE NORMALLY REF TSM 32-30-00. REMOVED MLG RESTRICTOR VALVE & FOUND IT CONTAMINATED. REPLACED VALVE, REMOVED MLG DOOR RES TRICTOR VALVE, NO CONTAMINATION FOUND. REPLACED AS A PRECAUTION. PERFORMED NUMEROUS GEAR SWINGS. OPS CHECKS NORMAL. R & R GREEN SYSTEM LOW PRESSURE & HIGH PRESSURE FILTERS. FOUND SMALL AMOUNT OF PARTICLES IN GREEN SYSTEM HIGH PRESSUR 2 L 7 2 4F RT A35EU 20081218 EU 2008 12 18 FDEA200812135137 1 20081213 A 5310 A53611658204 DOOR FRAME AIRBUS 310 A310203 3930313 EU ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 429FE 364 L1 DOOR LT UPPER FWD FAIL/SAFE RING RADIUS BOTH LAYERS SHOW EXFOLIATION CORROSION INDICATIONS AFTER EDDY CURRENT INSPE CTION, UNABLE TO VERIFY ULTRASONICALLY 1 SQ INCH AREA. REMOVED LEVEL 1 CORROSION AND REPAIRED DAMAGED AREA AT L-1 DOO R UPPER FWD CORNER FAIL/SAFE RING IAW FEDEX EA 6-5310-124179, RELEASE DATE 20 NOVEMBER, 2008. 2 L 7 2 4F RT A35EU 20081218 NM 2008 12 18 FDEA200812145139 1 20081214 A 5311 FRAME SPLICE BOEING 757 75728A 1384976 NM ZONE 100 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 912FD 24260 AFT CARGO PIT STA 1560 STR 24-25R, FRAME AND FRAME SPLICE ARE GOUGED. BLENDED AND SMOOTHED FRAME FOUND WITHIN LIMITS IA W SRM 53-60-07 AND SRM 53-00-07 FIG 101 DETAIL 2. REMOVED AND FABRICATED NEW SPLICE FRAME WITH MAE TRAVELER NR T8/77100 3, LOCATED, DRILLED HOLES, TREATED, PRIMED, PAINTED AND INSTALLED SPLICE FRAME IAW SRM 51-40-02. THIS IS MAJOR AND CATE GORY "A" REPAIR. 2 L 7 2 4F RT A2NM 20081218 EU 2008 12 18 FDEA200812155146 1 20081215 A 5321 FXSRZ25005242LK FLOOR PANEL AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 MAIN CABIN FLOOR PANEL NR 242 LK IS DAMAGED. FABBED A NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED HOLE S; COUNTERBORED HOLES; POTTED & SANDED EDGE; INSTALLED INSERTS; APPLIED ANTI-SKID & PART MARKED IAW FEDEX DWG SRZ25 -005: REV "G". 2 L 7 2 4F RT A35EU 20081218 EU 2008 12 18 FDEA200812155156 1 20081215 A 5321 FXSRZ25005242SF FLOOR PANEL AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 MAIN CABIN FLOOR PANEL NR 242 SF IS DAMAGED. FABBED A NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED, COU NTERBORED HOLES; POTTED & SANDED EDGE; INSTALLED INSERTS; APPLIED ANTI-SKID & PART MARKED IAW FEDEX DWG SRZ25-005: REV "G". 2 L 7 2 4F RT A35EU 20081217 NM 2008 12 17 UALA2008111301963 1 20080405 A 2150 3964622 SHUTOFF VALVE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE AC BAY FAILED A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION IN INSP/MAINT 1 WP 29 668UA 30024 PACK "OFF" LIGHT & "PACK OFF" EICAS MESSAGE DISPLAYED WITH PACK SELECTED TO AUTO. NO "PACK TEMP" OR "INOP" LIGHT DISPLA YED. RECURRED ON FLT 0059-07. REPLACED FLOW CONTROL SHUT OFF VALVE. OPERATIONAL CHECK WAS GOOD. REPLACED FLOW CONTRO L CARD ASSY, CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081217 NM 2008 12 17 UALA2008111303291 1 20080610 A 2612 8244 FIRE LOOP BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT ENGINE FAULTY A UALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 29 668UA 30024 LEFT ENGINE FIRE LOOP 2 STATUS MESSAGE WOULD NOT RESET. FOUND TOP REAR AND BOTTOM FWD LOOPS BAD. REPLACED TOP AFT AND FWD LOWER LOOPS 1 AND 2 OP CHECKED GOOD. AC OK FOR SERVICE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081217 2008 12 17 C2XA08TY140 4 20081215 A 3160 C16221GD04 ISIS UNIT EMB 145 EMB145XR 3260214 SO COCKPIT INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 27 10156 14209 786 FLT 2276 DIVERTED INTO TYS FROM IAH FOR ISIS "OUT OF ORDER". R&R ISIS UNIT IAW EMB 145XR AMM 34-01-01. OPS CK GOOD. A CFT RELEASED AND RETURNED TO SERVICE. 2 L 7 2 4F RT 20081217 EA 2008 12 17 C2XA08CL129 2 20081211 A 7200 ENGINE EMB 145 EMB145XR 3260214 SO RROYCE AE3007 AE3007A1E 54169 EA NR 2 SMOKE A C2XA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 27 14204 14500968 CAE312923 IAH FLIGHT NR 2249 THE CREW REPORTED A LAV SMOKE WARNING IN FLIGHT. THE CABIN FILLED WITH SMOKE MINUTES AFTER TAKEOFF. THE ACFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MX REPLACED THE NR 2 ENGINE AND OPS CHECKS WERE GOOD. SUPPLEMEN T TO FOLLOW. 2 L 7 2 4F 4 F RT TE6CH 20081217 SO 2008 12 17 C2XA08CL130 1 20081212 A 3350 78241 INVERTER EMB 145 EMB145XR 3260214 SO EMERGENCY LIGHT INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 13161 14500805 CLE FLIGHT NR 2375 THE CREW REPORTED ROW 12 EMERGENCY LIGHT WAS INOPERATIVE. MX INSPECTED AND REPLACED THE NR 6 EMERGEN CY LIGHT INVERTER. OPS CHECKS WERE GOOD. 2 L 7 2 4F RT 20081217 CE 2008 12 17 YADA120108 1 20081201 A 5610 10138402523 WINDSHIELD BEECH 1900 1900C 1154161 CE ZONE 200 CRACKED E YADA O OTHER O OTHER CR CRUISE 1 AL 03 111AX 5400 UC81 LT WINDSHIELD BROKE IN CRUISE - RED GLOW FROM HEATER ELEMENTS UNTIL WINDSHIELD HEAT TURNED OFF. UNEVENTFUL LANDING MADE AT ORIGINAL DESTINATION. MX REPLACED THE LT WINDSHIELD DUE TO OUTER PANE FAILURE. 2 L 7 2 4T RT A24CE 20081217 SO 2008 12 17 C2XA08CL131 1 20081215 A 3610 8166101 VALVE EMB 145 EMB145LR 3260212 SO BLEED SYSTEM FAULTY A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 15980 26237 145202 CLE FLIGHT NR 2344 THE CREW REPORTED A BLEED 2 OVERTEMP WARNING WITH THE ANTI-ICE SYSTEM TURNED ON. MSG CLEARED WITH AN TI-ICE OFF. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. 2 L 7 2 4T RT T00011AT 20081217 NM 2008 12 17 SWAA087078 1 20081213 A 5330 6545765 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 676SW 23288 DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 500C, STR 14R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087093 1 20081214 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 390 AT RADIO ALTIMETER ANTENNA CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087094 1 20081214 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 410 AT RADIO ALTIMETER ANTENNA CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087131 1 20081215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087132 1 20081215 A 5330 6545768 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED 24Y CHECK, FOUND E & E COMPARTMENT SKIN CRACKED BETWEEN BS 360 TO BS 380, STR 28L. REPAIRED SKIN PER S RM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 FDEA200812125127 1 20081212 A 5711 65249662 SPAR BOEING 727 727233 138408A NM ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 276FE 22041 FALSE SPAR CHORD CRACKED UNDER NR 8 SPOILER . TRIMMED INBRD WEB SECTION IAW DRAWING SR 27-57-038 REV C. TRIMMED LOWER STRUCTURE IAW DRAWING SR 27-57-038. LOCATED, DRILLED, DEBURRED LOWER ANGLE IAW 51-30-5 & DWG SR 27-57-038 REV C. FABR ICATED 2 EA ANGLES AND FABRICATED STRAP IAW DWG SR 27-57-038 AND SRM 51-30-5. FABRICATED DOULBLER AND HEAT TREATED ANG LES AND DOUBLER TO 7075-T6 AND 7075-T4 IAW WITH ENG REPORT 2-37153-801 REV A. TREATED AND PRIMED REPAIR PARTS IAW SRM 5 1-10-2 AND INSTALLED REPAIR PARTS IAW FX DWG SR27-57-038. 2 L 7 3 4F RT A3WE 20081217 NM 2008 12 17 SWAA087065 1 20081213 A 2560 65C16820 HOOK BOEING 737 7377H4 1384404 NM GIRT BAR LOOSE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 250WN 34972 R1 DOOR AFT GIRT BAR HOOK LOOSE. REPLACED HOOK PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 FDEA200812015018 1 20081201 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON 0.460 INCH DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPO RT FITTING NR 6 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B, NR C AND NR D. MAIN CARGO DOOR LOWER JAMB SUPPORT FIT TING NR 6 FOR CRACKED BOLT HOLES NR A, NR B, NR C AND NR D, BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOL UME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081217 NM 2008 12 17 DHLA2008743510 1 20081111 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 UPPER FUSELAGE CARGO CABIN BS 312 BETWEEN RBL 41 TO LBL 45 FLOORBEAM UPPER CHORD WITH CORROSION AT BOTH SECTIONS. REPAI RED FLOORBEAM SECTION AT BS 312 BETWEEN LBL 9 TO RBL 63 IAW B 727 SRM 53-10-8 FIG 9. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 DHLA2008743511 1 20081125 A 5313 STRINGER BOEING 727 727225 1384077 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 LOWER FUSELAGE FROM BS 720F TO BS 740 S27L WITH CORROSION. REPAIRED FUSELAGE STRINGER SECTION FROM BS 720F+17.25 INCH T O BS 740 S27L IAW SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 20081217 EU 2008 12 17 FDEA200812105118 1 20081210 A 5415 A5725000420100 ATTACH FITTING AIRBUS 310 A310203 3930313 EU RT NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 RIGHT WING AFT OTBD PYLON FAIRING SUPPORT ATTACH FITTING ON THE WING, RIB 9, STRINGERS 8 - 9, IS CRACKED. REMOVED AND R EPLACED FITTING IAW DWG 3 A57250004, ISSUE "E" AND SRM 51-40-21, PARA 7 AND PART 5. 2 L 7 2 4F RT A35EU 20081217 EU 2008 12 17 FDEA200812105119 1 20081210 A 5510 A5517805820600 WEB AIRBUS 310 A310203 3930313 EU HORIZONTAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 RIGHT HORIZONTAL STAB L/E 341 CB WEB IS CRACKED, APPROX 5' FROM OTBD END. STOP DRILLED CRACK IAW SRM 51-73-10. ACCOMPL ISHED HFEC IAW NTM 51-10-08 AND NO FURTHER DAMAGE WAS FOUND. FABRICATED REPAIR IAW SRM 51-71-40. ALODINED IAW SRM 51-2 1-10 PRIMED IAW SRM 51-23-10. INSTALLED REPAIR IAW SRM 51-40-21. 2 L 7 2 4F RT A35EU 20081217 EA 2008 12 17 SWIA200820628 1 20081019 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 625 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 965SW 7871 C-CHECK, RIGHT AND LEFT FS 625 TIE CLIPS ON FRAME TO BULKHEAD INTERCOSTAL ARE CRACKED. REPLACED PER SRM. 2 L 7 2 4F RT A21EA 20081217 NM 2008 12 17 SWAA087081 1 20081213 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 731SA 27863 DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION BEARING O/B LOWER ATTACH LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 EA 2008 12 17 SWIA200820629 1 20081019 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 1900309 EA BS 280 CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 965SW 7871 C-CHECK, FS 280 FLOOR SUPPORT BEAM LBL9 LOWER INBOARD AND OUTBOARD CLIPS CRACKED. REPAIRED PER REO. 2 L 7 2 4F RT A21EA 20081217 EA 2008 12 17 SWIA200820630 1 20081019 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF34* 30015 NE LT ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 965SW 7871 C-CHECK, LEFT ENGINE THRUST FITTING CORRODED. REPLACED PER AMM. 2 L 7 2 4F 4 F RT A21EA 20081217 EA 2008 12 17 SWIA200820631 1 20081019 A 7120 FITTING CNDAIR CL600 CL6002B19 1900309 EA RT ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 965SW 7871 C-CHECK, RIGHT ENGINE THRUST FITTING CORRODED. REPLACED PER AMM. 2 L 7 2 4F RT A21EA 20081217 NM 2008 12 17 DHLA2008743505 1 20081109 A 5311 FRAME BOEING 727 727225 1384077 NM ZONE 200 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 UPPER FUSELAGE CARGO CABIN AT BS 580 BETWEEN S-14R AND S-17R FRAME WITH DENT AND DOUBLE HOLE. REPLACED FRAME SECTION AT BS 580 BETWEEN S-12R AND S-18R DUE TO DOUBLE HOLES IAW B727SRM 51-10-1 PARA 7D. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 SWAA087055 1 20081211 A 5313 BAC1498 STRINGER BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 950, STR 27R. REMOVED AND REPLACED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087056 1 20081211 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM TEE CAP CRACKED AT BS 540, RBL 1. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081217 CE 2008 12 17 DXTA2008120803389 1 20081204 A 3150 WARNING LIGHT RAYTHN DH125 HAWKER800XP 7150012 CE ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 882QS 258482 THE AMBER "ELE/AIL TRIM" ANNUNCIATOR (ON MWS) ILLUMINATES DURING FLIGHT OUTSIDE OF GREEN NORMAL BAND FOR TAKE OFF. 2 L 7 2 4F RT A3EU 20081217 EU 2008 12 17 FDEA200812115122 1 20081211 A 3230 BDM3003 PSEU AIRBUS 300 A300F4605R 3930327 EU MLG FAILED A FDEA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 CE 21 683FE 801 LANDING GEAR FAILED TO RETRACT, TRIED BOTH SYS 1 & 2. RETURNED TO AIRPORT. ACFT DOWN FOR WORK. REMOVED AND REPLACED P ROXIMITY DETECTOR PROCESSING UNIT PER MM REFERENCE 32-31-71-4. BDL/11, LUBRICATED PIVOT PIN AIW MM 12-22-32-0 - BDL/11, ACN RELEASED FOR SERVICE PER MEL/CDL: 32-30-01. JACKED ACFT AND SWUNG GEAR SEVERAL TIMES. ALL THREE LANDING GEARS RET RACT AND EXTEND NORMALLY IN 1&2. DISCONNECTED PITCH DAMPERS ON BOTH MAINS TO CHECK FOR MOVEMENT OF BOGIES. NO BINDING NOTED. MM 32-11-15-4. RECONNECTED PITCH DAMPERS AND CHARGED SYSTEM PER MM 12-12-32-0. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 20081212 SO 2008 12 12 SIMA200834501 1 20081208 A 5330 SKIN EMB 145 EMB145LR 3260212 SO FUSELAGE GOUGED A SIMA O OTHER O OTHER IN INSP/MAINT 1 SW 21 922AE 5000 14500906 ON A IMBV INSPECTION REPAIRED A DEFERRED DISCREPANCY. A GOUGE AND DENT ON FUSELAGE SKIN BETWEEN FRAMES 21 AND 22 AND BE TWEEN STRINGERS 17L AND 18L. PERFORMED A CUT OUT OF THE FUSELAGE SKIN TO REMOVE THE DAMAGE. FABRICATED. A FILLER AND R EPAIR DOUBLER. MARKED, DRILLED, CLEANED AND TREATED REPAIR PARTS. REPAIR DONE IAW EMB 145 SRM (SRM-145/1142 REV 40) CH APTERS 53-21-01 AND 51-75-04. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081212 NM 2008 12 12 AALA200810407 1 20081114 A 5340 ATTACH FITTING BOEING 737 737823 13844CB NM ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 STATION 727B LEFT, FRAME CRACKED AT AIR CONDITIONING RAIL ATTACH POINT. REPAIRED PER ECO J1159AA. 2 L 7 2 4F RT A16WE 20081212 2008 12 12 CHQA200800240 4 20081205 A 3100 S8406F011 KNOB EMB 135 EMB135KL 3260302 SO ALLSN AE3007 AE3007A 03030 GL CONTROL PANEL LOOSE A CHQA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 11 297SK 145522 CAE311245 FLIGHT 5300, IND TO STL - THE FLIGHT CREW REPORTED THAT THE PRESSURIZATION SYSTEM WOULD NOT OPERATE IN EITHER AUTO OR MA NUAL MODES AND RETURNED TO IND AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE MANUAL CONTROL KNOB LOOSE. THE KNOB WAS SECURED AND THE SYSTEM OPERATED NORMALLY. 2 L 7 2 4F 4 F RT T00011AT TE6CH 20081212 NM 2008 12 12 DLM88081653 1 20081126 A 4990 36280 LINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE APU OIL SYS LOOSE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 919DL 16975 49584 P80464 ON DEPARTURE WITH TAKEOFF POWER SELECTED CREW NOTICED SLIGHT ODOR IN COCKPIT SMELLED LIKE OVERHEATED DUCTS NOT ELECTRICA L, BRAKE OR TIRES. AFTER LANDING PASSENGERS TOLD F/A THAT THEY SAW HAZE AND ODOR IN AFT CABIN. AFTER TAKEOFF ODOR DISS IPATED AFTER 1 MINUTE FROM INITIAL OBSERVATION. FOUND LOOSE UNION ON APU OIL PRESSURE SWITCH THAT CONTAMINATED APU INLE T WITH OIL-TIGHTENED LINE AND CLEANED APU INLET IN WASH RACK. PERFORMED OPN 5089 DUCT BURNOUT AND CHANGED COALESCER BAG S. LEAK AND OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A6WE E9NE 20081212 NE 2008 12 12 DL75E081675 2 20081130 A 7320 EEC BOEING 757 757231 1384950 NM PWA 2037 PW2037 NE NR 1 ENGINE MALFUNCTIONED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 718TW 41583 28486 727156 L ENG SEC CONT STATUS MESSAGE DISPLAYED, UNABLE TO CLEAR OUT RAN NR 1 ENG SEVERAL TIMES AND SELECT EEC TO ALTN POSITION NO MSG ARE NOTED. PERFORMED VISUAL INSPECTION ALL WIRING CHECK OK FOUND LOOSE CONNECTOR AT TCA AND J1 CONNECTOR ON EEC, AS PRECAUTION AND DUE TO HISTORY. REMOVED AND REPLACED EEC PER MM. RAN ENG FOR ABOUT 15 MIN. NO MSG ARE NOTED. CHEC K OK. 2 L 7 2 4F 4 F RT A2NM E17NE 20081212 SO 2008 12 12 SIMA200834502 1 20081205 A 5320 SILL EMB 145 EMB145LR 3260212 SO SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 918AE 5000 14500902 DURING A IMBV INSPECTION A PREVIOUS REWORKED AREA ON THE SERVICE DOOR CUT OUT LOWER CENTER SILL WAS FOUND CORRODED. BLE NDED THE CORRODED AREAS, CLEANED AND PERFORMED NDT INSPECTIONS. APPLIED EPOXY PRIMER TO BLENDED AREAS. FABRICATED FORW ARD DOUBLER, CLEANED AND TREATED THE DOUBLER. REPAIR DONE IAW EMBRAER 145 SRM (SRM EMB-145/1142 REV 40) CHAPTER 53-21-0 2. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT T00011AT 20081212 NM 2008 12 12 DL738081694 1 20081111 A 5510 UNKNOWN BOEING 737 737832 13844CF NM HORIZONTAL STAB DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3767 30821 RIGHT HORIZONTAL STABILIZER DENT REPAIR IAW SRM 55-10-01, C/W SRM 55-10-01. 2 L 7 2 4F RT A16WE 20081212 NE 2008 12 12 DL76L081696 2 20081205 A 7200 PW4060 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 MAKING METAL A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1201P 61802 28458 724164 LARGE PIECE OF FERROUS METAL FOUND IN ANGLE GEAR BOX CHIP DETECTOR. FOUND LARGE METAL CHIP OBSTRUCTING VALVE. REPLACED ANGLE GEAR MCD AND HOUSING WILL NEED LEAK CK PER MM. REMOVED AND REPLACED NR 1 ENG PER TRANSMITTAL 1T148AD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081212 NM 2008 12 12 DL76P081697 1 20081205 A 2131 CONTROLLER BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE CABIN PRESSURE MALFUNCTIONED A DALA D RETURN TO BLOCK G MULTIPLE FAILURE TX TAXI/GRND HDL 1 SO 27 143DA 25991 724164 AUTO INOP LIGHT ON WITH STATUS MESSAGE CABIN ALT AUTO 2 AND 1. BITE CHECK OF CPC1 AND 2 SHOWED AC MOTOR. RESET CONTROL LERS NOW MSGS CLEARED AND SYSTEM OPS NML. 2 L 7 2 4F 4 F RT A1NM E24NE 20081212 NM 2008 12 12 DL76S081699 1 20081207 A 2761 ACTUATOR BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 6 SPOILER MALFUNCTIONED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 136DL 23146 724164 ON DEPARTURE FROM LAS CREW REPORTED TO DISPATCH THAT L HYD QTY READ ZERO. DISPATCH NOTIFIED MCC THAT ACFT WAS RETURNING TO LAS. REMOVED AND REPLACED NR 6 SPOILER PCA PER AMM. PERFORMED REQUIRED INSPECTION. 2 L 7 2 4F 4 F RT A1NM E24NE 20081212 2008 12 12 DL764081684 2 20081202 A 7314 PUMP BOEING 767 767432ER 1385134 NM FUEL SYSTEM FAILED A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 831MH 29702 RTB - TAXI OUT LT FWD FUEL PUMP FAILED. RETURNED FOR ADDITIONAL FUEL. 2 L 7 2 4F RT A1NM 20081212 NM 2008 12 12 AALA200820085 1 20081120 A 5320 146N52467 FLOOR SUPPORT BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 641AA 56842 24599 FLOOR SUPPORT CORRODED, REPAIRED FLOOR SUPPORT IAW SRM 53-00-51. 2 L 7 2 4F RT A2NM 20081212 WP 2008 12 12 IXXA080035O 1 20081208 A 7997 CONNECTOR DOUG DC8 DC871F 302199D WP ENGINE OIL SYS DEFECTIVE A IXXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 11 828BX 88019 1535 45993 DURING CRUISE FROM KTOL NUMBER THREE ENGINE OIL PRESSURE STABILIZED AT 50 PSI THEN FLUCTUATED BETWEEN 20-60 PSI FOR A SH ORT TIME, THEN STABILIZED AGAIN AT 50 PSI. THE CREW RETURNED TO KTOL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED OIL PRESSURE ELECTRICAL CONNECTOR. OPERATIONAL CHECK GOOD IAW DACO MAINTENANCE MANUAL 20-50-1, AND ERH 70.01. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 20081212 NM 2008 12 12 DLM90081702 1 20081208 A 2150 210017014 BOOT DOUG MD90 MD9030 3023690 NM PWA 4060 PW4060 52119 NE RT A/C PACK WORN A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 901DA 53381 727738 LEVELING AT 33000 ALT FLOW LIGHT ILLUMINATED RT PACK FLOW DROPPED TO ZERO DESCENDED TO 24000 RAN QRH PROCEDURES FOR FLO W LIGHT AND LOSS OF PACK DID NOT RESTORE PRESSURIZATION CABIN ALT REACHED 13500 DESCENDED TO 10000 ALT CABIN DOOR LIGHT ILLUM OUT OF 24000. REPLACED RT A/C WATER SEPARATOR BAG AND CLAMP ASSY. 2 L 7 2 4F 4 F RT A6WE E24NE 20081215 CE 2008 12 15 FCP2008F00001 1 20081114 A 5720 1011100841 ATTACH FITTING BEECH 300 300BEECH 1152930 CE LT WING CRACKED B FCPR K NONE O OTHER IN INSP/MAINT 1 NM 09 898RJ 8875 FA90 WHILE COMPLYING WITH AD AD 91-12-10 AMENDMENT 39-7021, FOUND THE LT WING PANEL LOWER FORWARD ATTACH POINT HAD A .1250 IN CH CRACK. 2 L 7 2 4T A24CE 20081215 EA 2008 12 15 SWIA200820611 1 20081205 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 907SW 7511 FLT 5838 - LEFT WING AFT EMERGENCY EXIT LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081215 NM 2008 12 15 AALA200810383 1 20081124 A 5320 ANGLE BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 905AN 29507 AFT ENTRY DOOR OPENING CREASE ANGLE CORRODED. INSTALLED NEW CREASE ANGLE PER SRM 51-10-02-05. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086966 1 20081210 A 5330 6545774 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 512SW 24189 DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 764, BETWEEN STR 21L TO STR 22L. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086979 1 20081210 A 5330 6562212 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 661SW 23173 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE. REPAIRED SKIN PER AAR EA. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087033 1 20081211 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1006, LBL 2. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086985 1 20081210 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND CREASE BEAM CHORD CRACKED AT BS 639, LBL 64. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087022 1 20081211 A 5730 6546419 SKIN BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED HC2 CHECK, FOUND LT WING SKIN CRACKED AT FIXED L/E ABOVE SPRING DOOR. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087023 1 20081211 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 333SW 23697 DURING SCHEDULED HC2 CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR UPPER FWD CUTOUT REVEAL. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087027 1 20081210 A 3350 417N5120 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 FOUND RT FWD EMERGENCY EXIT BULL NOSE LIGHT LOOSE. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA087003 1 20081210 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 270, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081215 WP 2008 12 15 AALA200810449 1 20081125 A 5320 STOP FITTING DOUG DC9 DC982 3022082 WP ZONE 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 AFT DOOR FRAME STOP FITTING CORROSION. REMOVED AND REPLACED FITTING. 2 L 7 2 4F A6WE 20081215 NM 2008 12 15 SWAA086972 1 20081210 A 3350 417N5120 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 522SW 26564 RT FWD EMERGENCY EXIT BULLNOSE LIGHT LOOSE. SECURED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081215 WP 2008 12 15 AALA200810488 1 20081202 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY LIGHT WEAK A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 982TW 53632 EMERGENCY BATTERY PACK ABS-1 WEAK. REPLACED BATTERY PACK WITH SERVICEABLE UNIT AND OPERATIONAL CHECKED. PART NUMBER BA T5016/SERIAL NUMBER 18858 AMM 33-60-98-4. 2 L 7 2 4F RT A6WE 20081215 WP 2008 12 15 AALA200810493 1 20081208 A 5311 FRAME DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7542A 49996 CANT FRAME CRACKED STATION 1510 BELOW MAIN LIGHT SWITCH LEFT SIDE AT TAIL CONE ALIGNMENT PIN. INSTALLED DOUBLER PER EA MD80 53-005083. 2 L 7 2 4F A6WE 20081215 EA 2008 12 15 SWIA200820617 1 20081210 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 935SW 7725 FLT 6351 - OVERHEAD CABIN EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081217 NM 2008 12 17 SWAA087113 1 20081212 A 3350 417A5701 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 409WN 27896 RT AFT EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087127 1 20081215 A 5322 69353656 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CRACKED AT BS 380, LBL 3, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PE R SRM. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 UALA2008111303689 1 20080702 A 5754 SLAT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 3 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NR 3 SLAT REMOVED FROM A-C 6352. SLAT DENTED 56 INCHES FROM INBOARD END. DAMAGED CAUSE IN WIND STORM. INSTALLED REPAI RED SLAT. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 UALA2008121006832 1 20081210 A 3397 17512201 WIRE HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT EEL LIGHT INOP AT SEAT ROW 59 LEFT. SECURED WIRING HARNESS. 2 L 7 4 4F 4 F RT A20WE E24NE 20081218 NE 2008 12 18 UALA2008111305396 2 20080822 A 7520 16P944 VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 ENGINE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 223UA 30224 NR 2 ENGINE LT LOWER TURBINE VANE AND BLADE COOLING AIR VALVE WAS FOUND IN THE CLOSED POSITION. BEGAN REMOVAL OF NR 2 E NGINE LT LOWER TVBC VALVE. VALVE IN POSITION ON ENG WITH NEW FLANGE AND LARGE DUCT GASKET INSTALLED. THREE BOLTS LOOSE LY INSTALLED ON FLANGE, AWAITING BOLTS TO CONTINUE INSTALLATION. COMPLETED INSTALLATION OF LOWER LT TVBC VALVE ON THE N R 2 ENGINE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 NM 2008 12 18 UALA2008111305459 1 20080825 A 2597 CONNECTOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GALLEY CHAFED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 104UA 26902 ELECTRICAL ODOR MAIN DECK GALLEY. RTFL. FOUND PIGTAIL CONNECTOR WIRE BUNDLE FOR P56 AND P57 LOCATED ON BACK WALL WHERE GALLEY OVEN CARTS GO TO BE CHAFED IN TWO PLACES. REPLACED THE WIRE BUNDLE FOR P56 TO P57. OVERHEAD GALLEY LIGHT IN MI D GALLEY INOP. REPLACED THE THE BALLAST AND BULBS, SYSTEM CHECKS OKAY. OPERATED PACKS USING EACH ENGINE NO SMOKE NOTED . PER FLT CREW, NO SMOKE SMELL IN AFT GALLEY AREA AND NO SMOKE EICAS INDICATION DURING OPERATIONAL CONFIRMATION FLT. A /C DETERMINED OK FOR SERVICE. 2 L 7 4 4F 4 F RT A20WE E24NE 20081218 NM 2008 12 18 UALA2008121106856 1 20081211 A 5753 FLAP BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU LT WING DELAMINATED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 329UA 24149 LT WING OUTBOARD AFT FLAP TRAILING EDGE HAS 6 INCH AREA OF DELAMINATION AND DISBONDING ON INBOARD SIDE. OUTSIDE OF SRM LIMITS. FLAP IS REPAIRED. 2 L 7 2 4F 4 F RT A16WE E21EU 20081218 NM 2008 12 18 UALA2008121006833 1 20081210 A 2820 S343T00339 ACTUATOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT ENGINE FAILED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 780UA 26944 LEFT ENG FUEL SPAR VALVE STATUS MSG. ENG SPAR VLV WOULD NOT OPEN. MSG NUMBER 28-14001. REPLACED RELAY K76102. NO HELP . REPLACED LEFT ENG SPAR VALVE ACTUATOR. SPAR VALVE, OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 WP 2008 12 18 IXXA080038O 1 20081215 A 7930 PRESSURE SWITCH DOUG DC8 DC871F 302199D WP ENGINE OIL DEFECTIVE A IXXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 11 820BX 90945 1866 46065 DURING TAKEOFF FROM KTOL AT APPROXIMATELY NINTY KNOTS THE CREW HAD A NUMBER TWO LOW OIL PRESSURE LIGHT FLICKER FOR ABOUT 1/2 SECOND WHILE SETTING MAX POWER OF EIGHTY-SEVEN PERCENT N1. POWER WAS AT ABOUT EIGHTY-SIX PERCENT AT THE TIME THEN LIGHT CAME ON STEADY FOR ABOUT 1 SECOND AND THE CAPTAIN ABORTED THE TAKEOFF. AS POWER WAS RETARDED LOW OIL PRESSURE LIG HT WENT OUT IMMEDIATELY. MAINTENANCE REPLACED THE LOW OIL PRESSURE SWITCH. THE OPERATIONAL CHECK WAS GOOD AND THE AIRC RAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 20081218 EU 2008 12 18 FDEA200812155147 1 20081215 A 5321 FLOOR PANEL AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 MAIN CABIN FLOOR PANEL NR 242 KJ IS DAMAGED. FABBED A NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED, COUNT ERBORED HOLES, POTTED & SANDED EDGE; INSTALLED INSERTS. APPLIED ANTI-SKID & PART MARKED IAW DWG SRZ25-005: REV "G" . 2 L 7 2 4F RT A35EU 20081218 EU 2008 12 18 FDEA200812155148 1 20081215 A 5321 FLOOR PANEL AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 MAIN CABIN FLOOR PANEL NR 241 LK IS DAMAGED. FABBED A NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED, COUN TERBORED HOLES; POTTED & SANDED EDGE; INSTALLED INSERTS; APPLIED ANTI-SKID & PART MARKED IAW DWG SRZ25-005: REV "G ". 2 L 7 2 4F RT A35EU 20081218 EU 2008 12 18 FDEA200812155149 1 20081215 A 5321 FLOOR PANEL AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 MAIN CABIN FLOOR PANEL NR 242 BF IS DAMAGED. FABBED A NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED & C OUNTERBORED HOLES; POTTED & SANDED EDGE; INSTALLED INSERTS; APPLIED ANTI-SKID & PART MARKED IAW DWG SRZ25-005: REV " G". 2 L 7 2 4F RT A35EU 20081218 EU 2008 12 18 FDEA200812155150 1 20081215 A 5321 FLOOR PANEL AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 MAIN CABIN FLOOR PANEL NR 251 WG IS DAMAGED. FABBED A NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED & CO UNTERBORED HOLES; POTTED & SANDED EDGE; INSTALLED INSERTS; APPLIED ANTI-SKID & PART MARKED IAW DWG SRZ25-005: REV "G ". 2 L 7 2 4F RT A35EU 20081218 EU 2008 12 18 FDEA200812155151 1 20081215 A 5321 FLOOR PANEL AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 MAIN CABIN FLOOR PANEL NR 262 AH IS DAMAGED. FABBED A NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED & COU NTERBORED HOLES; POTTED & SANDED EDGE; INSTALLED INSERTS; APPLIED ANTI-SKID & PART MARKED IAW FEDEX DWG SRZ25-005: R EV "G". 2 L 7 2 4F RT A35EU 20081218 EU 2008 12 18 FDEA200812155153 1 20081215 A 5321 FLOOR PANEL AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 MAIN CABIN FLOOR PANEL NR 242 BF IS DAMAGED. FABBED A NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED HOLE S, COUNTERBORED HOLES, POTTED & SANDED EDGE, INSTALLED INSERTS; APPLIED ANTI-SKID & PART MARKED IAW DWG SRZ25-005: REV "G". 2 L 7 2 4F RT A35EU 20081218 EU 2008 12 18 FDEA200812155160 1 20081215 A 2810 SEAL AIRBUS 310 A310203 3930313 EU CENTER TANK TORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 VERTICAL VAPOR SEAL IS TORN AT THE CENTER WING BOX AT FRAME 40/41 AT LBL 58. REPAIRED VAPOR SEAL SEAM IAW AMM 28-13-12- 8; PG 1; FIG 802 AND PARA 2-B. 2 L 7 2 4F RT A35EU 20081218 EU 2008 12 18 FDEA200812155161 1 20081215 A 2810 A28110280000 VAPOR BARRIER AIRBUS 310 A310203 3930313 EU ZONE 100 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 A/C BAY HORZONTAL VAPOR BARRIER NR 7 IS WORN THROUGH. FABRICATED DOUBLER IAW SRM 51-71-31; PG 201. ALODINED & PRIMED IAW SRM 51-21-10; PG 3 & SRM 51-23-10; PG 24. INSTALLED DOUBLERS IAW SRM 51-40- 21; PG 3 & SRM 51-71-31; PG 201. ROUTED OUT DAMAGE IAW SRM 51-71-30; PG 201. 2 L 7 2 4F RT A35EU 20081218 EU 2008 12 18 FDEA200812155162 1 20081215 A 2810 VAPOR BARRIER AIRBUS 310 A310203 3930313 EU FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 ACFT HORIZONTAL VAPOR BARRIER NR 1 AFT IS CRACKED. RECEIVED NEW A2811028300500 SHEET METAL ASSY (PO 643383.1) TO BE INS TALLED ON WIC 41X5087ALI. 2 L 7 2 4F RT A35EU 20081218 EU 2008 12 18 FDEA200812155163 1 20081215 A 5714 STRUCTURE AIRBUS 310 A310203 3930313 EU WING BOX CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 CENTER WING BOX LOWER SURFACE HAS LIGHT CORROSION BETWEEN FRAMES 40/41- 43, ADJACENT TO RIB 1 LEFT. CLEANED AREA IAW AM M 12-21-11-0; PG 3. CORROSION FOUND TO BE A PAINT CHIPPED OFF. NO MATERIAL LOSS. ALODINED AND PRIMED BARE AREA IAW S RM 51-21-10. PAINTED AREA IAW SRM 51-23-10; PG 7 AND 8. 2 L 7 2 4F RT A35EU 20081218 NM 2008 12 18 P5CA2008121101582 1 20081208 A 2750 FLAP SYSTEM BOEING 747 74746NF 13848BT NM TE FLAPS MALFUNCTIONED A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 452PA 30810 L/E SINGLE DRIVE FLAPS PRIMARY MESSAGE ON FLAP EXTENSION. LEADING EDGE HAD A DELAYED EXTENSION. "PERFORMED GROUND OPER ATIONAL CHECK OF THE FLAPS IAW MM 27-81-00. FOUND SYSTEM OPERATES NORMALLY. THE MESSAGE CLEARED AND AIRCRAFT DEPARTED. " 2 L 7 4 4F RT A20WE 20081218 WP 2008 12 18 AALA200810376 1 20081125 A 5230 ANGLE DOUG DC9 DC983 3022083 WP ZONE 800 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 572AA 49458 CARGO DOOR LOWER STOP ANGLE CRACKED. INSTALLED SERVICEABLE ANGLE. 2 L 7 2 4F RT A6WE 20081218 WP 2008 12 18 AALA200810472 1 20081204 A 5320 INTERCOSTAL DOUG DC9 DC983 3022083 WP ZONE 200 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 FORWARD ENTRY DOOR THIRD FROM BOTTOM INTERCOSTAL CRACKED. REPAIRED PER AARD 52-10-00-3. 2 L 7 2 4F RT A6WE 20081218 WP 2008 12 18 AALA200810473 1 20081204 A 5210 BEAM DOUG DC9 DC983 3022083 WP ZONE 800 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 FORWARD ENTRY DOOR, NUMBER 6 DOOR BEAM CRACKED. REPAIRED PER SRM 52-05-00 FIGURE 3. 2 L 7 2 4F RT A6WE 20081218 WP 2008 12 18 AALA200810474 1 20081206 A 5311 FRAME DOUG DC9 DC983 3022083 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 CRACK IN DOUBLER REPAIR AT BASE OF ACTUATOR CRADLE AT FRAME STATION 1485. INSTALLED SERVICEABLE DOUBLER PER AARD 53-10- 00-33. 2 L 7 2 4F RT A6WE 20081218 NM 2008 12 18 AALA200810505 1 20081215 A 5320 FLOOR SUPPORT BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CORROSION ON FLOOR SUPPORT STATION 312 TO 328. INSTALLED A SERVICEABLE FLOOR SUPPORT. 2 L 7 2 4F RT A16WE 20081218 WP 2008 12 18 IXXA08SMN198S 1 20081024 A 5512 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 52. 825-75.672. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN, STIFFENER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AT STA XE 29.000 - 77. 000 IAW FAA FORM 8110-3 NUMBER 08 548 DATED 11/18/08, DRAWING ED-4875 DATED 11/05/08, SRM 51-1-8 PAGES 17-18, SRM 55-2-0 PAGE 12, SRM 55-1-0 PAGE 1, SRM 5 1-1-21, SRM 51-1-8B, AND SRM 51-1-11. 2 L 7 4 4F 4A25 20081218 NM 2008 12 18 F3LA2008121600723 1 20081212 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319111 3930336 NM ZONE 200 FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 923FR 60 2019 PILOT REPORTED THE EMERGENCY LIGHTS WERE ON IN ROWS 14 AND AFT. MAINTENANCE REMOVED MOISTURE FROM THE AFT LEFT HAND EXI T SIGN CONNECTOR 7245VC AND REPLACED THE EMERGENCY POWER SUPPLY UNIT IN POSITION 13WL IN ACCORDANCE WITH A319 AMM 33-51- 38 PB401 AND PERFORMED OPERATIONAL TEST. 2 L 7 2 4F RT A28NM 20081218 WP 2008 12 18 IXXA08SMN193S 1 20081024 A 5522 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 55.062. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDE D. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. PERFORMED BALANCE FOUND WITHIN LIMITS MOMENT 1526.000 IN-POUND. INS TALLED REPAIR PARTS IAW SRM 55-4-1 FIGURE 1 SHEETS 1-2 ITEMS "E" AND "F", SRM 51-1-8 PAGES 17-18, SRM 55-2-0 PAGE 12, SR M 55-1-0 PAGE 1, SRM 51-1-21, SRM 51-1-9 TR NUMBER 51-142, SRM 51-1-9A TR NUMBER 51-141, SRM 51-1-8B, SRM 51-1-11, AND S RM 51-4-4 PAGES 1-4 TR NUMBER 51-116. 2 L 7 4 4F 4A25 20081218 2008 12 18 P5CA2008121101581 4 20081211 A 3460 4052508952 FMC BOEING 747 74746NF 13848BT NM RIGHT UNSERVICEABLE A P5CA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 452PA 30810 DURING PUSHBACK RIGHT FMC FAILED. "FMC WAS REPLACED AND AIRCRAFT DEPARTED NO FURTHER ISSUES." 2 L 7 4 4F RT A20WE 20081218 WP 2008 12 18 IXXA08SMN199S 1 20081024 A 5522 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 147.188A - XE 15 6.168. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED P ARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. PERFORMED BALANCE. FOUND WITHIN LIMITS, MOM ENT: 1526.0 IN-POUND. INSTALLED REPAIR PARTS IAW SRM 55-4-1 FIGURE 1 SHEETS 1-2 ITEMS "E" AND "F", SRM 51-1-8 PAGES 17- 18, SRM 55-2-0 PAGE 12, SRM 55-1-0 PAGE 1, SRM 51-1-21, SRM 51-1-9 TR 51-142, SRM 51-1-9A TR 51-141, SRM 51-1-8B, SRM 51 -1-11, AND SRM 51-4-4 PAGES 1-4. 2 L 7 4 4F 4A25 20081218 NM 2008 12 18 AALA200810502 1 20081215 A 5320 INTERCOSTAL BOEING 737 737823 13844CB NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 INTERCOSTAL CRACKED BETWEEN STATION 312 AND 328 RIGHT BUTT LINE 31. INSTALLED A SERVICEABLE INTERCOSTAL. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 AALA200810503 1 20081212 A 5320 PANEL BOEING 737 737823 13844CB NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CORROSION ON LEFT TRANSITION PANEL STATION 470. INSTALLED DOUBLER PER SRM 53-00-53-2R. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 AALA200810484 1 20081216 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CORROSION ON FLOORBEAM AT STATION 986.5 LEFT BUTT LINE 4. REPAIRED PER SRM 53-00-2R. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 AALA200810495 1 20081216 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CORROSION ON FLOORBEAM STATION 986.5 AT LEFT BUTT LINE 12. REPAIRED PER SRM 53-00-51-2R. 2 L 7 2 4F RT A16WE 20081219 EU 2008 12 19 UALA2008121206861 1 20081212 A 3350 32145410 POWER SUPPLY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN FAILED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 448UA 842 FWD LT ESPU FAILED TEST. REPLACED FWD LT EPSU. OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 20081219 NM 2008 12 19 FDEA200812015019 1 20081201 A 5320 AFA71321 SUPPORT FITTING DOUG MD11 MD11F 3023600 NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON 0.460 INCH DIAMETER HOLES, MAIN CARGO DOOR LOWER JAMB SUPPO RT FITTING NR 7 FOUND WITH CRACK INDICATIONS AT HOLES NR A, NR B AND NR D. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING N R 7, FOR CRACKED BOLT HOLES NR A, NR B AND NR D, BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REP AIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081219 EU 2008 12 19 FDEA200812155166 1 20081215 A 5347 A5381192220251 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 THE MAIN CABIN SEAT TRACK IS WORN BEWTEEN FRAME 50 AND FRAME 51 RBL 18. REMOVED & REPLACED SEAT TRACK SECTION DUE TO BE ING OUT OF LIMITS IAW SRM 53-10-6. INSTALLED NEW SEAT TRACK RAIL P/N A5381192220251; PO 644457.1 IAW SRM 51-72-10; PG 1. 2 L 7 2 4F RT A35EU 20081219 NM 2008 12 19 UALA2008111306088 1 20081013 A 2150 62594610 CONTROLLER BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT AC PACK FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 654UA 25392 THE 'R PACK INOP 'LIGHT ON. EICAS MSG 'R PACK TEMP' DISPLAYED. REPLACED OUTLET DOOR ACTUATOR, PACK CONTROLLER AND FLOW CONTROL CARD (P/N 285T0093-1). OPERATED SYSTEM, NO FAULTS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081219 NM 2008 12 19 UALA2008111306412 1 20081106 A 2780 7321870019 MODULE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LE SLAT FAULTY A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 671UA 30026 LEADING EDGE SLAT DISAGREE GOING FROM FLAPS 20 TO 25. REPLACED FLAP-SLAT SHUTOFF VALVE MODULE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081219 NM 2008 12 19 CALA2008121401144 1 20081213 A 5240 146N61001 SERVICE DOOR BOEING 757 757224 1384958 NM L4 DOOR OUT OF ADJUST A CALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 27 14107 27297 L4 DOOR WILL NOT CLOSE. PERFORMED ADJUSTMENT OF L-4 DOOR LOWER GUIDE ARM SUPPORT BRACKET SERRATED SHIMS AND GUIDE ARM A DJUSTER ARM ASSY IAW AMM 52-11-04 PG 216. DOOR LEAK AND OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A2NM 20081219 NM 2008 12 19 CALA2008121401146 1 20081214 A 5313 58530030020 STRINGER BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24224 28933 STRINGER 27-R BETWEEN STATION 500 F AND 500G HAS CORROSION AROUND RIVETS. STRINGER 27-R REPAIRED PER SRM 53-00-03 BETWE EN STA 500F AND 500G. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 CALA2008121701150 1 20081217 A 3260 3186301001035 INDICATOR BOEING 737 737524 1384721 NM COCKPIT INOPERATIVE A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 27 37615 27328 UPON ARRIVAL ON APPROACH CAPTAIN DECLARED EMERGENCY FOR A LEFT MAIN GEAR INDICATION PROBLEM, AIRCRAFT LANDED SAFELY. TR OUBLESHOT AND FOUND LEFT MAIN LANDING GEAR GREEN INDICATOR SWITCH BAD. REMOVED AND REPLACED LEFT MLG (GREEN) INDICATOR SWITCH PER AMM 33-11-81, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 CALA2008121701151 1 20081216 A 5315 141T5108 FLOORBEAM BOEING 767 767424ER 1385270 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 66056 29451 STATION 325 LBL 25 TO LBL 36 FLOOR SUPPORT FOUND CORRODED. STATION 325 LBL 25 TO LBL 36 FLOOR SUPPORT REPAIRED PER SRM 53-00-51, FIG 201 REPAIR 1, AND HFEC NO CRACK FOUND. 2 L 7 2 4F RT A1NM 20081219 NM 2008 12 19 SWAA087162 1 20081216 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087164 1 20081216 A 5322 6546529 SHEAR TIE BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500C, LBL 3. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087169 1 20081216 A 5313 BAC1498 STRINGER BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087155 1 20081216 A 5754 65C26602312A SKIN BOEING 737 7373H4 1384600 NM LE SLAT DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 SLAT O/B LEADING EDGE SKIN DELAMINATED. INSTALLED SLAT PER MM. 2 L 7 2 4F RT A16WE 20081217 EU 2008 12 17 FDEA200812125132 1 20081212 A 7710 E0066Z01W00A RELAY AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680 30025 NE ENGINE FAILED A FDEA F ACTIVATE FIRE EXT. O OTHER TO TAKEOFF 1 CE 21 689FE 875 705309 DURING T.O. ROLL NR 1 ENG N1 AND N2 SURGED AFTER TOGA, DROPPED 2 % 3 TIMES. NOTED EGT AND F.F. GAGES MIRRORED N1 AND N 2. REJECTED TO AT 85 KTS. FOLLOWED QRH PROCEDURE. RETRIEVED FAULT CODE 351-18, 28 VDC POWER DISCONNECT FAULT. PER TSM REMOVED AND REPLACED RELAY 33KS. PERFORMED POWER ASSURANCE RUN. RAN ENG'S AT T/O PWER FOR 5 MIN. NO FAULTS NOTED, NO FL UCTUATIONS NOTED FOR ANY OF THE PARAMETERS. IAW TSM 73-21-30 & JRH. 2 L 7 2 4F 4 F RT A35EU E13NE 20081217 NM 2008 12 17 SWAA087051 1 20081211 A 5311 6546593 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087100 1 20081215 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087126 1 20081215 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND SKIN CRACKED AT BS 727D, STR 4L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081217 NE 2008 12 17 RMXA2008121600575 2 20081215 A 7260 CHIP DETECTOR BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE NR 1 ENGINE ACTIVATED E RMXA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 05 171M 7138 LE45311 NR 1 ENGINE CHIP LIGHT ILLUMINATED AND COULD NOT BE EXTINGUISHED WITH ZAPPER. PILOT SECURED NR 1 ENGINE AND PERFORMED N IGHT SINGLE ENGINE RUN-ON LANDING TO JZI AIRPORT. THE TECHNICIAN INSPECTED THE CHIP DETECTOR. FOUND 2 APPROX 1/2MM FLAK ES CLASSIFIED AS "MINOR" AS PER LTS 101 650B MM. CLEANED DETECTOR. PERFORMED GROUND RUN. CHIP LIGHT REMAINS EXTINGUIS HED. 1 G 7 2 3U 3 U H13EU E5NE 20081218 NM 2008 12 18 UALA2008111306298 1 20081027 A 3397 60444 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN EXPOSED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 649UA 25286 WIRES EXPOSED ON EMERGENCY FLOOR LIGHTS. REPLACED EEL LIGHT STRIP AND COVER. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 EU 2008 12 18 UALA2008120906801 1 20081209 A 3397 WIRE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE EMERGENCY LIGHTS PINCHED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 474UA 1475 BOTH OVERWING EXIT LIGHTS WILL NOT ILLUMINATE AND RT EPSU FAILED BITE TEST. FOUND EMERGENCY LIGHT WIRE PINCH UNDER SEAT TRACK ROW 10 LEFT. REMOVED WIRE AND REPAIRED DAMAGE WIRE, OPERATIONAL CHECKS OF LEFT AND RIGHT OVERWING LIGHTS CHECKS OK, ALSO NO FURTHER FAULTS AT FLAP PANEL. CHECKED SEAT FOR SECURITY AND OP-CHECK. CHECKED WIRE REPAIR AND OP CHECKS OF LEFT AND RIGHT OVERWING LIGHTS. 2 L 7 2 4F 4 F RT A28NM E40NE 20081218 NE 2008 12 18 UALA2008111306485 2 20081110 A 7261 MAIN BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 598UA 28751 727116 STRONG ODOR OIL SMELL ON TAKEOFF DISSIPATED ON CLIMBOUT. REPLACED NR 2 ENGINE. MAIN BEARING FAILURE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081218 2008 12 18 UALA2008111305931 4 20080929 A 3414 INDICATOR BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU COCKPIT UNKNOWN A UALA C ABORTED TAKEOFF W INADEQUATE Q C TO TAKEOFF 1 WP 29 336UA 24240 ABORTED T/O AT 100 KNOTS. ACCOUNT OF FLAG IN VIEW ON F/O'S AIRSPEED INDICATOR. CHECKED PER AMM05-51-07. BRAKE TEMP CO OLED 54 MINUTES PER FIG 201. BRAKE TEMP RETURNED TO NORMAL, NO DAMAGE TO BRAKES. 2 L 7 2 4F 4 F RT A16WE E21EU 20081219 NM 2008 12 19 UALA2008121206860 1 20081211 A 5420 STRUCTURE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 PYLON CRACKED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 NR 2 PYLON INBOARD SIDE IS CRACKED AT PNL LANDING. MAJOR REPAIR ACCOMPLISHED. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081219 NM 2008 12 19 FDEA200811295008 1 20081129 A 5340 ACA7017501 FITTING DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 LEFT NOSE LANDING GEAR WHEEL WELL TRUNNION WEB FITTING FOUND CRACKED, CRACK LENGTH APPROXIMATELY: 3/4 INCH. LEFT NOSE L ANDING GEAR WHEEL WELL TRUNNION WEB FITTING REPAIRED AS PER SRM 53-40-00 FIGURE 23 VOLUME I. REPAIR CLASSIFIED MAJOR A S PER GMM 6-2-100. REPETITIVE INSPECTION REQUIRED FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS. 2 L 7 3 4F RT A22WE 20081219 NM 2008 12 19 UALA2008111306281 1 20081027 A 2421 745329C GENERATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE FAILED A UALA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CR CRUISE 1 WP 29 662UA 27159 LOST RT GENERATOR AND APU. FLIGHT DIVERTED. NR 2 ENGINE GENERATOR REPLACED. APU REPLACED (P/N 3800298-1-7). AFTER AP U REPLACEMENT FAULT LIGHT AND MSG FUEL SEL VLV. REPLACED FUEL CONTROL UNIT (P/N 3882500-17), NO HELP. REPLACED APU CON TROLLER (P/N 2117342-19). APU OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081219 2008 12 19 UALA2008111303919 4 20080723 A 3425 6227998003 ADI BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT FAULTY A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 658UA 27113 CAPTAINS ADI BLANKING INTERMITTENTLY. RTFL. LOSS OF ATTITUDE DEVIATION INDICATOR. REPLACED CAPTAIN'S ADI. OPS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081219 NM 2008 12 19 CALA2008121601148 1 20081215 A 5313 143A324141 STRINGER BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24224 28933 FORWARD PIT STR 28L HAS CORROSION THAT IS OUT OF LIMITS. NEEDS TO BE REPLACED FROM STATION 500B TO STATION 500I. INSTA LLED NEW STRINGER AND REPAIR SPLICES IN ACCORDANCE WITH SRM 53-00-03. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087185 1 20081216 A 5313 6551698 STRINGER SPLICE BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 22R. REMOVED AND REPLACED SPLICE PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087190 1 20081216 A 5311 65C22910 FRAME BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND FRAME CORRODED AT BS 500D, BETWEEN STR 25R TO STR 26R. REPAIRED FRAME PER ER. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087220 1 20081217 A 5311 6546593 FRAME BOEING 737 7373L9 1384470 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087172 1 20081216 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087173 1 20081216 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087174 1 20081216 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087199 1 20081216 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087186 1 20081216 A 5330 6562212 SKIN BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087227 1 20081217 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087153 1 20081216 A 5753 6546435333 FLAP BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 612SW 27930 DURING SCHEDULED HC2 CHECK, FOUND, LT WING O/B AFT FLAP I/B CORNER DELAMINATED. REMOVED AND REPLACED FLAP PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087154 1 20081216 A 3350 101073 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 614SW 28033 DURING SCHEDULED HC2 CHECK, FOUND FWD ENTRY LOWER EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087179 1 20081216 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087219 1 20081216 A 2121 210501 GASPER FAN BOEING 737 7373H4 1384600 NM CABIN FAULTY A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SW 29 636WN 27709 ELECTRICAL ODOR FROM RT PACK, APU BLEED SOURCE BOTH GASPER AND RECIRC FAN WERE ON. REMOVED AND REPLACED GASPER FAN PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087226 1 20081216 A 2560 6557463 ATTACH FITTING BOEING 737 7373H4 1384600 NM GIRT BAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED 16Y CHECK, FOUND L1 DOOR AFT GIRT BAR MOUNT ATTACH FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM. 2 L 7 2 4F RT A16WE 20081219 EU 2008 12 19 NSVA2008046 1 20081214 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHT DISCHARGED A NSVA K NONE L NO TEST IN INSP/MAINT 1 EA 27 338CJ 338 DURING OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM ON A LINE CHECK EMERGENCY LIGHTS 37LN, 38LN, 40LN, 54LN, 56LN, 57 LN WERE NOT ILLUMINATING. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY 22LN IAW WORK CARD NR 33-50-02S AND SYSTEM CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A52EU 20081219 NM 2008 12 19 QXEA2008121201238 1 20081211 A 3610 69494J905 SWITCH BOMBDR DHC8 DHC8402 1390042 NM BLEED OVERTEMP MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION DE DESCENT 1 NM 19 410QX 4053 SEA - NR 1 BLEED HOT CAUTION LIGHT ILLUMINATED AT APPROXIMATELY 13,000 FEET TURNED OFF BLEED NR 1 IAW CHECKLIST AND LIGH T EXTINGUISHED. RESET BLEED NR 1 IAW CHECKLIST, AND BLEED HOT CAUTION ILLUMINATED AGAIN. TURNED NR 1 BLEED OFF AGAIN A ND NR 1 BLEED HOT CAUTION CAME ON AGAIN AND REMAINED ON FOR ALMOST 2 MINUTES BEFORE EXTINGUISHING, 3 MINUTES LATER, THE NR 1 BLEED HOT ILLUMINATED ON APPROACH FOR 40 SECONDS AND THEN EXTINGUISHED. FOUND "LT BLD ANA OT" FAULT MESSAGE IN CDS . REMOVED AND REPLACED NR 1 BLEED AIR OVERTEMP SWITCH IAW AMM TASK NR'S 36-11-16-000-801, AND 36-11-16-400-801. RAN EN GINES BLD HOT CAUTION DID NOT RE-OCCUR. NO FURTHER DEFECTS. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081219 NM 2008 12 19 QXEA2008121601243 1 20081214 A 3230 858601 PSEU DHAV DHC8 DHC8202 2809007 NM ZONE 200 MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 19 346PH 15093 477 SEA - DURING CLIMB-OUT AT 185 KNOTS, 8000 FEET MSL, PROPS AT 1050 THE NOSE GEAR DOORS RAPIDLY CYCLED OPEN THEN SHUT, NOS E DOOR AMBER LIGHT BLINKED ON, AND CREW FELT THE EVENT VIBRATE THROUGH FLOORBOARDS. HYDRAULICS ALL NORMAL. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. FERRY TO PDX FOR REPAIRS. COULD NOT DUPLICATE THE DISCREPANCY. REMO VED AND REPLACED THE PSEU AS A PRECAUTIONARY MEASURE IAW AMM TASK 32-61-00-000-801/400-801. RETRACTED AND EXTENDED MLG, NOSE GEAR DOORS OPERATE NORMALLY. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081219 NM 2008 12 19 SWAA087188 1 20081216 A 5322 6546546 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26L TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087202 1 20081216 A 5322 6546529 SHEAR TIE BOEING 737 7373L9 1384470 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500B, BBL 0. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087225 1 20081217 A 5312 6517853 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT WL 180, RBL 5.7, BS 178. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087211 1 20081217 A 3350 284A01216 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 417WN 29822 DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087218 1 20081214 A 2560 P2070001 FLASHLIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND FLASHLIGHT IN AFT LT WINDSCREEN BROKEN. REMOVED AND REPLACED FLASHLIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087207 1 20081217 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT, BS 290, WL 234. REPAIRED SKIN PE R SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087208 1 20081217 A 5330 6545800 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT R1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087209 1 20081216 A 5330 6545765 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 330SW 23694 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500D, STR 16L. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087221 1 20081217 A 5753 65C26714 SKIN BOEING 737 7373L9 1384470 NM FORE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 657SW 23331 DURING SCHEDULED 24Y CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED SKIN PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087230 1 20081217 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087231 1 20081217 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087191 1 20081216 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER ER. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 UALA2008121506873 1 20081212 A 2421 GENERATOR BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LT ENGINE FAILED A UALA C ABORTED TAKEOFF W INADEQUATE Q C TO TAKEOFF 1 WP 29 668UA 30024 LEFT ENGINE GENERATOR FAILURE. ABORTED TAKEOFF. 2 L 7 2 4F 4 F RT A1NM E24NE 20081219 NM 2008 12 19 UALA2008121506874 1 20081213 A 3350 362624 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROW 15A INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 557UA 26653 EMERGENCY EGRESS LIGHT AT ROW 15A IS INOP. REPLACED LIGHT AND OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081219 NE 2008 12 19 UALA2008121506875 2 20081213 A 7532 BLEED VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE EXCESS PLAY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 655UA 25393 724666 NR 1 ENGINE 2.5 BLEED VALVE HAS EXCESSIVE PLY ON THE RIGHT SIDE OF THE RING. ALSO FOUND METAL SHAVINGS IN RING AREA ARO UND 3 O`CLOCK POS. REPLACED ESN 724666 WITH ESN 727987 IN POS 01. 2 L 7 2 4F 4 F RT A1NM E24NE 20081219 NM 2008 12 19 UALA2008121506876 1 20081213 A 3350 1060091102 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 660UA 27115 COCKPIT EMERGENCY EXIT LIGHT DOES NOT COME ON IN ARM WITH BATT AND STBY POWER OFF. REPLACED LIGHT ASSY AND OPS CHECKS G OOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081219 EA 2008 12 19 QXEA2008121801251 1 20081211 A 5330 SKIN CNDAIR CL600 CL6002C10 1390015 EA FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 616QX 10128 PDX - C4 - UPPER TCAS ANTENNA HAS MINOR SURFACE CORROSION ON FUSELAGE SKIN AROUND NUTPLATE. BLENDED MINOR CORROSION ON FUSELAGE SKIN IAW SRM 51-12-00. BLENDED AREAS ARE WITHIN LIMITS IAW SRM 53-00-01 PG 101. SKIN IS .061", MAX REWORKED M ATERIAL LOSS IS .003". FPI BLENDED AREAS FOR CRACKS IAW CRJ 700 NDTM PART 1, 51-20-008, NO CRACKS NOTED. MAPPED FOR EN GINEERING. BLEND WAS FOUND TO BE IN A "NO CHANGE ALLOWED" AREA, AS STATED IN SRM 53-21-01-101-003-AAI. BLEND WAS FOUND TO COMPLY WITH REO 670-53-21-418 STEP 1. REPLACED 2 FASTENERS AS PER STEP 2, AND FINISHED REWORKED AREA IAW STEP 4. 2 L 7 2 4F RT A21EA 20081219 NM 2008 12 19 QXEA2008121701249 1 20081215 A 5270 SHAFT BOMBDR DHC8 DHC8402 1390042 NM PROX SENSOR FROZEN A QXEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 19 428QX 4160 YLW - AFTER LIFTOFF RIGHT FORWARD EMERGENCY EXIT SHOWED UNSAFE INDICATION. RETURNED TO THE FIELD AND ACCOMPLISHED A UNE VENTFUL LANDING. FOUND THE FWD RT EMERGENCY DOOR PROX SENSOR TARGET SPRING LOADED FOLLOWING SHAFT FROZEN WITH WATER. H EATED AND DRIED WATER FROM FOLLOWING SHAFT. LUBRICATED FOLLOWING SHAFT TO ALLOW TARGET TO FOLLOW SENSOR. NO FURTHER D EFECTS NOTED. OPS CHECK GOOD. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081219 NM 2008 12 19 HALA2008121500892 1 20081215 A 2612 FIRE WARNING BOEING 767 76733A 1385209 NM LT NACELLE FALSE INDICATION A HALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, "L ENG FIRE LP 1" ON LOWER STATUS PAGE. PERFORMED ENG FIRE TEST. TEST OK. MESSAGE CLEARED. 2 L 7 2 4F RT A1NM 20081219 NM 2008 12 19 UALA2008121506885 1 20081213 A 5210 141N622022 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L4 DOOR CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 554UA 26644 L-4 DOOR LOWER GATE CORRODED. DAMAGE EXCEEDS LIMITS. INSTALLED NEW GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081219 NM 2008 12 19 UALA2008121506886 1 20081213 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 554UA 26644 FWD PIT BILGE, FRAME AT STA 660 RT SIDE HAS A DENT BETWEEN STR 24R-25R. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SEC TION OF FRAME AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081219 SO 2008 12 19 SWIA200820637 1 20081214 A 5610 WINDOW EMB 120 EMB120ER 3260203 SO COCKPIT CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 216SW 120285 FLT 5783 - FO`S DV WINDOW HAS A CRACK INSIDE AT THE LOWER FORWARD CORNER. REPLACED FO DV WINDOW. 2 L 7 2 4T RT A31SO 20081219 NE 2008 12 19 UALA2008121506887 2 20081213 A 7310 5903150 FUEL FILTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE DIRTY A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 553UA 25277 L ENG FUEL FILTER LIGHT ILLUMINATED. RTFL. REPLACED NR 1 FUEL FILTER. RAN ENGINE, NO LEAKS FOUND AT THIS TIME. OP CH ECKS GOOD. NO FAULTS. ACFT OK FOR SERVICE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081219 EA 2008 12 19 SWIA200820641 1 20081207 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 466SW 7856 FLT 6750 - CEILING EMERGENCY LIGHT BEHIND EXIT ROW SIGN INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081219 NM 2008 12 19 UALA2008120506765 1 20081205 A 3010 2780537104 ANTI-ICE VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT WING FAULTY A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION NR NOT REPORTED 1 WP 29 597UA 28750 EICAS MSG WING ANTI-ICE DISPLAYED. REPLACED ANTI-ICE VALVE RIGHT WING. ANTI-ICE VALVE SENSE LINE FITTING AND B-NUT STR IPPED AT LINE TO VALVE. NEEDS NEW LINE AND FITTING. BOTH ENDS OF SENSE LINE STRIPPED NEED NEW LINE AND BOTH UNIONS REP LACED. REPLACED LINE AND FITTINGS. 2 L 7 2 4F 4 F RT A2NM E17NE 20081219 NM 2008 12 19 UALA2008121506865 1 20081212 A 3810 2920016101 VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE POTABLE WATER UNSTABLE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 777UA 26916 WATER PRESSURE FAILURE. FLIGHT DIVERTED. DEFERRED DUE TIME, PRESELECT FILL VALVE FOUND SOLID, MECHANICAL LINKAGE WILL NOT MAKE SOLENOID. TRIED TO REWORK NO HELP. PREVIOUS HISTORY AND CHRONIC ITEM. REPLACED PRESELECT OVERFLOW VALVE. WA TER SYSTEM SERVICEABLE. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081219 NM 2008 12 19 UALA2008121506867 1 20081212 A 5511 SPAR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE HORIZONTAL STAB CRACKED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 RT OUTBOARD HORIZ SPAR FASTENER HOLES OUTBOARD END CRACKED. REMOVED DAMAGE AND INSTALLED COMPOSITE REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081219 NM 2008 12 19 KCSA081617 1 20081216 A 5340 FITTING BOEING 747 747212B 1384886 NM BS 1480 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 LT DRAG FITTING AT STA-1480 LBL-13 CORRODED 2 L 7 4 4F RT A20WE 20081219 2008 12 19 DXTA2008121203397 4 20081211 A 3420 INDICATOR CESSNA 500 560CESSNA 2076750 CE HSI MALFUNCTIONED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 360QS 5600460 DURING TAKEOFF ROLL AT 50 KIAS, RED "HDG" FLAGS APPEARED ON CAPTAIN PFD, MFD, AND SIMULTANEOUSLY ON STBY HSI. 2 L 7 2 4F RT A22CE 20081219 CE 2008 12 19 DXTA2008120503387 1 20081203 A 3150 WARNING MESSAGE CESSNA 750 750 2076810 CE ILLUMINATED E DXTA O OTHER J WARNING INDICATION CL CLIMB 1 GL 07 962QS 7500126 WHILE ACCELERATING BETWEEN 200 AND 250 PITCH FEEL FAIL CAS MSG ILLUMINATED. 2 L 7 2 4J RT T00007WI 20081219 CE 2008 12 19 DXTA2008120803392 1 20081207 A 4920 APU CESSNA 560 560XL 2076702 CE SMOKE E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 640QS 5605260 FOUL ODOR COMING OUT OF ENVIRONMENTAL SYSTEM. ITS A MUSTY ODOR AND ITS MOST NOTICEABLE AT A RELATIVELY WARM OUTSIDE TEM P WITH CABIN SET TO COOL. WITH THE APU BLEED ON THERE WAS BLUE SMOKE COMING OUT OF THE WEMACS. KBNA-KSAT. 2 L 7 2 4F RT A22CE 20081219 EA 2008 12 19 C2XA08IA251 2 20081211 A 7200 ENGINE EMB 145 EMB145XR 3260214 SO RROYCE AE3007 AE3007A1 54165 EA ZONE 400 SMOKE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 27 41104 145646 CAE312690 IAH - FLIGHT 2160, THE FLIGHT ATTENDANT REPORTED THAT A HAZE DEVELOPED IN THE CABIN FOLLOWED BY A MOMENTARY LAV SMOKE IN DICATION. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX R&R THE NR 2 ENGINE, OPS CHECKED WITH NO DEFEC TS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT TE6CH 20081218 NM 2008 12 18 UALA2008111303690 1 20080702 A 2997 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 1 PYLON DETERIORATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 57UA 27112 NR 1 ENG HYD BAY (PYLON) CONNECTOR D00916 HAS DETERIORATED INSULATOR. REPLACED CONNECTOR D00916. OPS CHECKED AND NO DE FECTS NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 UALA2008120906795 1 20081206 A 3350 78671 LAMP BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 670UA 29240 SEAT 13HJ EMERGENCY LIGHT IS INOPERATIVE. REPLACED EMERGENCY LIGHT STRIP AT 13 HJ. CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 2008 12 18 UALA2008111306174 4 20081017 A 2565 CABLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 548UA 25396 LT OVERWING MANUAL BACKUP CABLE FAILS OPS CHECK. REPLACED BACK-UP CABLE. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081218 EU 2008 12 18 UALA2008111306354 1 20081101 A 4990 LINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE APU LEAKING A UALA O OTHER W K B INADEQUATE Q C FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 447UA 836 ACRID SMELL RETURNED ON TAKEOFF AND CLIMB GOT BETTER AT ALTITUDE NOW JUST MILD. SMELL GETS BETTER WITH CABIN FANS OFF A ND PACK IN HIGH FLOW. FOUND BRAIDED OIL LUBE LINE AFT SIDE OF GEARBOX ON APU LEAKING OIL INTO AREA OF APU INLET, AND CA USING OIL SMELL. ACCOMPLISHED PACK BURN OUT ENG RUN, SMELL GONE. CLEANED APU INLET. RESIDUAL OIL SMELL IS STILL REMAI NING IN A-C. SMELL HAS NOT DISSIPATED ENTIRE FLIGHT. REPLACED RECIRCULATION FILTERS. 2 L 7 2 4F 4 F RT A28NM E40NE 20081218 NE 2008 12 18 UALA2008111303521 2 20080622 A 7200 ENGINE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 OIL CONSUMPTION A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 219UA 30551 222053 NR 2 ENGINE OIL CONSUMPTION EXCEEDS LIMIT. BOROSCOPED NR 3 WEEP. FOUND NO LEAKS AND NO HISTORY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 NE 2008 12 18 UALA2008121206857 2 20081211 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE LEFT VIBRATION A UALA O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 29 668UA 30024 727985 CREW REPORT: L ENG VIB INDICTOR READS 3.2 IN CRUISE FL380 M.80 NO SIGNIFICANT VIBRATION NOTED. AT TOP OF DESCENT AS TH ROTTLES CAME BACK TO IDLE AIRFRAME VIBRATION NOTED FOR ABOUT 5 SEC. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 UALA2008111306183 1 20081019 A 3397 80172424 CONNECTOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 797UA 26924 SEATS 1E AND 3F 1EA SEAT EEL LIGHTS INOP. SECURED CONNECTOR ON SEAT 1, REPLACED LAMP ASSY ON SEAT 3, OPS CHECK. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 NM 2008 12 18 UALA2008120906810 1 20081209 A 3397 58791 FEEDER CABLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 LEFT FWD GALLEY EMERGENCY LIGHT BAR IS INOP. REPAIRED BROKEN CABLE ON LIGHT BAR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 CE 2008 12 18 DXTA200812163401 1 20081215 A 2750 FLAP SYSTEM CESSNA 750 750 2076810 CE TE FLAPS FAILED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED DE DESCENT 1 GL 07 936QS 7500036 WHEN FLAPS SELECTED TO 5 DEGREES FOR LANDING THEY FAILED. 2 L 7 2 4J RT T00007WI 20081218 CE 2008 12 18 DXTA2008121603401 1 20081215 A 2750 FLAP SYSTEM CESSNA 750 750 2076810 CE TE FLAPS FAILED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED DE DESCENT 1 GL 07 936QS 7500036 WHEN FLAPS SELECTED TO 5 DEGREES FOR LANDING THEY FAILED. 2 L 7 2 4J RT T00007WI 20081218 NM 2008 12 18 UALA2008111305534 1 20080828 A 2842 0320KPU01 PROCESSING UNIT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FUEL SYSTEM FAULTY A UALA O OTHER W INADEQUATE Q C CR CRUISE 1 WP 29 787UA 26939 FUEL QTY INDICATION STATUS MSG PER CREW. L MAIN TANK QTY INTERMITTENT, CTR READS NORMAL AND RIGHT MAIN TANK WAS BLANK F OR ABOUT 1.5 HOURS AND THEN ALL TANK READINGS RETURNED TO NORMAL. WITH ALL TANK READINGS NORMAL THE TTL QTY IND WAS STI LL BLANK. FOUND FAULTY FUEL QUANTITY PROCESSOR UNIT. REPLACED FUEL QUANTITY PROCESSOR UNIT. ALSO REPLACED FOUR FUEL Q T PROBES. ALL INDICATIONS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081219 NM 2008 12 19 FDEA200811295006 1 20081129 A 5347 ADA7321519 SEAT TRACK DOUG MD11 MD11F 3023600 NM ZONE 200 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 CABIN SEAT TRACK STATION 959 RIGHT X =-8.5 FOUND CORRODED. CABIN: CORRODED SEAT TRACK AT STATION 959, X =-8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 949 TO STATION 969, X = -8.5 AS PER SRM 53-70-00 FIGURE 1 VOLUME I. R EPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081219 NM 2008 12 19 SWAA087161 1 20081216 A 5311 6546550 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087180 1 20081216 A 5311 6546532 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087196 1 20081216 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 24R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087198 1 20081216 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED 14Y CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 HALA2008121100882 1 20081211 A 3150 WARNING LIGHT BOEING 717 717200 1383700 NM FALSE ACTIVATION A HALA O OTHER N FALSE WARNING CR CRUISE 1 WP 13 478HA 55123 WING MANIFOLD FAIL ALERT INFLIGHT AFTER THE QRH PROCEDURES WERE FOLLOWED LIGHT EXTINGUISHED IN 2 MIN. PERFORMED FIM 36- 23-814. RETURN TO SERVICE TEST PASSED, OK FOR SERVICE. 2 L 7 2 4F TR A6WE 20081219 EU 2008 12 19 FDEA200812155170 1 20081215 A 5347 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 THE MAIN CABIN SEAT TRACK IS WORN BETWEEN FRAME 54.2 AND FRAME 54.3 RBL 77. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 . REMOVED & REPLACED THE SEAT TRACK IAW SRM 53-10-16; FIG 208 & SRM 51-40-21. 2 L 7 2 4F RT A35EU 20081219 2008 12 19 HALA2008121400884 4 20081214 A 2310 9640452012 TRANSCEIVER BOEING 767 76733A 1385209 NM HF SYSTEM MALFUNCTIONED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 583HA 25531 ETOPS SIGNIFICANT SYSTEM, TRANSMISSIONS ON RT HF INTERMITTENT AT ALL STATIONS. REMOVED AND REPLACED NR 2 HF TRANSCIEVER GROUND CHECKED OK PER AMM 23-11-03. 2 L 7 2 4F RT A1NM 20081219 SO 2008 12 19 FDKA2008121300314 1 20081213 A 2750 FLAP EMB 145 EMB145LR 3260212 SO WING FAILED A FDKA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 836MJ 145359 FRL FLT 6254 IND-JFK - FLAPS FAIL IN FLIGHT, EMERGENCY DECLARED. AC REQUIRED ADDITIONAL RIGGING, OPS CHECK GOOD. 2 L 7 2 4T RT T00011AT 20081219 CE 2008 12 19 DXTA2008120303383 1 20081202 A 3260 INDICATOR CESSNA 500 560CESSNA 2076750 CE MLG MALFUNCTIONED E DXTA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 825QS 5600655 GEAR UNLOCKED LIGHT REMAINED ON AFTER GEAR RETRACTION. 2 L 7 2 4F RT A22CE 20081219 CE 2008 12 19 DXTA2008120303384 1 20081202 A 3260 INDICATOR CESSNA 500 560CESSNA 2076750 CE LT MLG INOPERATIVE E DXTA O OTHER P NO WARNING INDICATION LD LANDING 1 GL 07 304QS 5600408 LT MLG INDICATOR LIGHT INOP. USED NITROGEN TO BLOW GEAR DOWN. 2 L 7 2 4F RT A22CE 20081219 CE 2008 12 19 DXTA2008120303385 1 20081202 A 3240 BRAKE ASSY CESSNA 500 560CESSNA 2076750 CE MLG WEAK E DXTA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 319QS 5600519 BRAKES ARE SPONGY ON BOTH SIDES. COPILOTS SIDE BRAKES ARE WORSE. 2 L 7 2 4F RT A22CE 20081222 NE 2008 12 22 UALA2008121606901 2 20081214 A 7200 70R077600U MODULE BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE NR 2 ENGINE CRACKED A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 671UA 30026 717695 NR 2 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT. NR 2 ENG PLATE WHERE STARTER MOUNTS ON GEARBOX IS CRACKED AT LEAST 8 INCH ES AND LEAKING OIL. REPLACED STARTER DRIVE MODULE AND HOUSING. ALSO REPLACED ACCELEROMETER (P/N 144-151-000-101). OPE RATIONS AND INDICATIONS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081222 NM 2008 12 22 UALA2008121606902 1 20081216 A 3350 78671 LIGHT BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE SEAT 39H MISSING A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 671UA 30026 SEAT 39H IS MISSING SEAT MOUNTED EMERGENCY EXIT PATH LIGHT. INSTALLED NEW PATH LIGHT. OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081222 NM 2008 12 22 UALA2008121606909 1 20081215 A 2150 2780539107 ISOLATION VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT AC PACK FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 643UA 25093 RIGHT "PACK OFF" EICAS ON APU AIR. REPLACED CENTER ISOLATION VALVE. EICAS MSG RETURNED AT DEPT TIME. REPLACED RIGHT P ACK ISOLATION VALVE. 2 L 7 2 4F 4 F RT A1NM E24NE 20081222 NM 2008 12 22 UALA2008121606910 1 20081216 A 2150 3964622 CONTROL VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT AC PACK INOPERATIVE A UALA D RETURN TO BLOCK J WARNING INDICATION IN INSP/MAINT 1 WP 29 662UA 27159 RIGHT PACK OFF LIGHT NOT ILLUMINATED WITH PACK OFF. REPLACED FLOW CONTROL CARD, NO HELP. FOUND FLOW CONTROL VALVE INOP . REPLACED RT PACK FLOW CONTROL VALVE. OP CHECK GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081222 NM 2008 12 22 UALA2008121506896 1 20081212 A 2497 CTB9000 TERMINAL BLOCK BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 IDG LOOSE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 219UA 30551 NR 2 ENG IDG MAIN FEED WIRES AT TERMINAL BLOCK ON TOP OF ENGINE ARE LOOSE. REPLACED TERMINAL BLOCK AT TOP OF ENGINE AND RECONNECTED WIRES. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081222 NE 2008 12 22 UALA2008121506900 2 20081215 A 7321 7791005 FUEL CONTROL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALA D RETURN TO BLOCK W INADEQUATE Q C IN INSP/MAINT 1 WP 29 552UA 26641 L ENG SEC CONT MSG DISPLAYED. REPLACED FCU. ACCMP TEST 2A IAW MM 71-00-59 ON NR 1 ENG FCU, NO LEAKS NOTED. ACCOMPLISHE D ENGINE RUN PER JRH 2-95-1 AND 71-00-59, NO FAULTS NOTED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081222 EU 2008 12 22 USAA2008121592228 1 20081204 A 5315 D5347219020300 FLOORBEAM AIRBUS 320 A320232 3930326 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647AW 762 SAL - C8 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66 +4.5 INCHES, -Y765. REPLACED FLOORBEAM B ETWEEN FR64 TO FR66 +4.5 INCHES, -Y765 IAW A320 SRM 51-72-11. 2 L 7 2 4F RT A28NM 20081222 NM 2008 12 22 USAA2008121692238 1 20081206 A 5322 6545810517 SHEAR TIE BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - SHEAR TIE CRACKED AT BS 312, S18R. REPLACED SHEAR TIE AT BS 312, S18R IAW B737 SRM 51-40-05 & BOEING DRAWING 65-45810. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 USAA2008121692240 1 20081205 A 5315 6546810 FLOORBEAM BOEING 737 7374B7 138449C NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM T-CAP AT BS 967, RBL 4. REPAIRED FLOORBEAM T-CAP A T BS 967, RBL 4 IAW US AIRWAYS TYPICAL REPAIR 53-10-05B. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 USAA2008121692241 1 20081206 A 5315 6546811 FLOORBEAM BOEING 737 7374B7 138449C NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM T-CAP AT BS 986.5, LBL 45 TO RBL 45. REPAIRED FLOO RBEAM T-CAP AT BS 986.5, LBL 45 TO RBL 45 IAW US AIRWAYS TYPICAL REPAIR 53-60-01. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 USAA2008121692243 1 20081209 A 5754 65C26602224 SKIN BOEING 737 7374B7 138449C NM LE SLAT DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - NR 5 SLAT SKIN TRAILING EDGE DELAMINATED ON UPPER INBOARD SIDE. REPAIRED NR 5 SLAT SKIN TRAIL ING EDGE IAW B737 SRM 51-70-10. 2 L 7 2 4F RT A16WE 20081222 NE 2008 12 22 VNAA2008121500005 2 20081209 A 7532 BLEED VALVE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE ENGINE MALFUNCTIONED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 251PS 7931 ON CLIMB THE CREW REPORTED THE 10TH STAGE BLEED AIR ISOLATION VALVE WOULD NOT CLOSE, DURING AFTER T/O CHECKS. THE CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE 10TH STAGE BLEED VALVE. NO OTHER DEFECTS WERE NOTED AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 20081222 NM 2008 12 22 ZZDA2008185 1 20081216 A 3397 WIRE BOEING 717 717200 1383700 NM CABIN BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 930AT 55072 SEAT ROW 22DEF E-PATH LIGHTS INOP (BROKEN WIRE). RE-TERMINATED 1 EA PIN SOCKET ON THE FLOOR SIDE ELECTRICAL CONNECTOR P ER SWPM 20-20, WDM 33-51-14, OPS CHECK GOOD IAW AMM 33-51-00 SEAT ROW 22DEF. 2 L 7 2 4F TR A6WE 20081222 2008 12 22 DXTA2008120503386 2 20081204 A 7200 ENGINE CESSNA 500 560CESSNA 2076750 CE RIGHT STOPPED E DXTA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 398QS 5600522 RT ENGINE QUIT WHEN THROTTLE WAS BROUGHT TO IDLE. 2 L 7 2 4F RT A22CE 20081222 WP 2008 12 22 UPS08854204 1 20081114 A 5330 57549923 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:SV BS LONG 35R TO 35L SEQ 729-F1-22 CANNOT FIND SRM REPAIR OR EO TO MAT CH AREA. REPAIRED IAW UPS EO DC 8-5330-31570-A. 2 L 7 4 4F RT 4A25 20081222 NE 2008 12 22 UPS08854209 2 20081216 A 7310 FUEL DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C 13802 NE TANK CONTAMINATED A IPXA K NONE X ENGINE FLAMEOUT DE DESCENT 1 SO 01 874UP 46074 INSPECTION TYPE:N/A IFSD - NR 1 ENGINE FLAMED OUT AS POWER WAS BROUGHT TO IDLE FOR DESCENT OUT OF 380. PERFORMED FLAME OUT CK LIST AT FL 240 ENGINE STARTED AND INDICATED NORMAL OPERATION. PERFORMED STEPS IAW T/S TREE REF MM 71-00-00-1 FIG 139. REMOVED AND REPLACED FUEL FILTER AS PRECAUTIONARY REF MM 73-10-02-4. FOUND UNUSUAL AMOUNT OF WATER. DRAINED WAT ER FROM TANK AND GROUND RUN OPS NORMAL. 2 L 7 4 4F 4 F RT 4A25 E2GL 20081222 WP 2008 12 22 UPS08854152 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-85 AT STA 1718-1720 L19R-L20R HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILL ER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11. 2 L 7 4 4F RT 4A25 20081222 NM 2008 12 22 NWAA085456623 1 20081209 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM EMERGENCY LIGHTS INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 623US 21705 DURING AN OVERNIGHT LINE CHECK THE EMERGENCY LIGHTS IN THE UPPER DECK WERE FOUND TO BE INOPERATIVE. MX FOUND THE ASSOCI ATED BATTERY PACK TO BE DEFECTIVE AND REPLACED IT. SYSTEM OPS WERE NORMAL AFTER THE BATTERY PACK WAS REPLACED. 2 L 7 4 4F RT A20WE 20081222 WP 2008 12 22 UPS08854159 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-98 AT STA 1535 L14L HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER, FABRIC ATED AND INSTALLED REPAIR DOUBLERS AND FILLERS IAW UPS EO DC8-5330-31413-A AND FVCI DWG 53-08540-11. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854161 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-35 AT STA 8-4 L32-34R HAS NO SRM REF. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854163 1 20081019 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-73 AT FS 1393.5 L17-18L HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTAL LED REPAIR PARTS IAW UPS EO DC8-5330-31417-A AND FVCI DWG 53-08540-15. 2 L 7 4 4F RT 4A25 20081222 CE 2008 12 22 A6WA200840624 1 20081201 A 5340 SUPPORT CESSNA 414 414 2075908 CE BS 718 CRACKED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 414AW 4140520 AFT COMPARTMENT RT HYDRAULIC SUPPORT AT FS 718 FOUND CRACKED IN AFT LOWER CORNER. AFT COMPARTMENT RT HYDRAULIC SUPPORT AT FS 718 ON AFT LOWER CORNER REPAIRED IAW CRJ200 REO 601R-53-62-031 REV A. 1 L 7 2 3O RT A7CE 20081222 CE 2008 12 22 DXTA2008121503398 1 20081212 A 3200 LANDING GEAR CESSNA 680 680CE 2076811 CE UNKNOWN E DXTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 307QS 6800130 UPON LANDING GEAR RETRACTION, NOSE GEAR MADE LOUD "CLUNKING" NOISE. LT MAIN GEAR LIGHT REMAINED ON. THE RED UNSAFE LIG HT REMAINED ON. 2 L 7 2 4F RC T00012WI 20081218 NM 2008 12 18 AALA200810510 1 20081212 A 5320 INTERCOSTAL BOEING 737 737823 13844CB NM ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CABIN FLOOR INTERCOSTAL CRACKED STATION 284. INSTALLED A SERVICEABLE INTERCOSTAL. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 AALA200810500 1 20081216 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 TOP OF FLOORBEAM STATION 986.5 CORRODED AT RIGHT BUTT LINE 25. REPAIRED PER SRM 51-00-53-2R. 2 L 7 2 4F RT A16WE 20081218 2008 12 18 P5CA2008121601583 4 20081216 A 3400 TRANSPONDER BOEING 747 74746NF 13848BT NM MALFUNCTIONED A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 15 450PA 30808 DURING TAXI OUT CREW WAS UNABLE TO SELECT THE FIRST DIGIT ON TRANSPONDER. MAINTENANCE CONFIRMED THE OPERATION OF THE LE FT AND RIGHT TRANSPONDERS IAW AMM 34-53-00. THE AIRCRAFT DEPARTED WITH NO FURTHER ISSUES. 2 L 7 4 4F RT A20WE 20081218 NM 2008 12 18 F3LA2008121000721 1 20081209 A 3610 6774E010000 PRESSURE VALVE AIRBUS A319 A319111 3930336 NM NR 2 ENGINE FAILED A F3LA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 21 927FR 21 2209 PILOT MADE AN AIR TURN BACK TO DEN DUE TO ENGINE NR 2 AIR BLEED FAULT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE PRESSURE REGULATOR VALVE ASSEMBLY IN ACCORDANCE WITH A319 AMM 36-11-52-400-042. 2 L 7 2 4F RT A28NM 20081219 NE 2008 12 19 UALA2008111306192 2 20081020 A 7200 ENGINE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 STALLED A UALA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 651UA 25389 724651 TWO ENGINES STALLED AT FL380. DFDR INVESTIGATION REVEALED THAT ONLY THE NUMBER 2 ENGINE STALLED. AIRPLANE ENCOUNTERED AN ATMOSPHERIC WAVE AT .80 MACH CAUSING AUDIBLE COMPRESSOR STALLS AND A FLUCTUATION IN THE MACH METER FROM .75 TO .84 RE TURNING TO .80. CREW REPORTS ALL ENGINE PARAMETERS NORMAL. ALL AMM CHECKS WERE WITHIN LIMITS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081219 NM 2008 12 19 UALA2008111306387 1 20081106 A 2120 CD01109F2 FILTER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE FWD CARGO BAY DIRTY A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 784UA 26951 ALL FLIGHT ATTENDANTS FROM BUSS CLASS AFT REPORT STALE STUFFY AIR QUALITY SAMC TEXT: FLT CREW REPORTED MORE THAN 10 F/A' S FELL ILL WITH EFFECTS OF DIZZINESS AND LIGHTHEADED. ONE FLT CREW FELT SAME EFFECTS WHEN TRAVELED TO BACK OF CABIN. F/A'S FROM MID CABIN FELT ILL FIRST AND THEN AFT CABIN F/A'S. ALL FELT BETTER AFTER USING PORTABLE O2. REPLACED 4 EA RE CIRC FAN FILTERS IN FWD PIT. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081219 NM 2008 12 19 SWAA087200 1 20081216 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087156 1 20081216 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087163 1 20081216 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087175 1 20081216 A 5311 6546552 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 827, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087201 1 20081216 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 667 TO BS 671, RBL 24. REPAIRED CHORD PER ER. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087228 1 20081217 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 2008 12 19 SWAA087212 4 20081216 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM L2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 425LV 29829 DURING SCHEDULED RON CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087236 1 20081217 A 5312 6545402 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 22Y CHECK, FOUND BULKHEAD HORIZONTAL FLANGE CRACKED AT BS 663, RBL 6. REPAIRED BULKHEAD PER DWG. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 QXEA2008121701248 1 20081215 A 2720 RUDDER PEDAL BOMBDR DHC8 DHC8402 1390042 NM STUCK A QXEA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 19 418QX 4143 STS - AT TOP OF DESCENT CREW ATTEMPTED TO APPLY A SLIGHT AMOUNT OF RUDDER PRESSURE TO THE RIGHT RUDDER PEDAL AND ENCOUNT ERED WHAT FELT LIKE A JAMMED RUDDER. A/P WAS ON AND AIRSPEED WAS 275 KIAS. BOTH DIRECTIONS AND PILOTS SAME FEEL AND RE SULT. AFTER PUSHING WITH GREAT FORCE, THE PEDALS "BROKE LOOSE" AND RUDDER WAS CONTROLLABLE. AS AIR SPEED REDUCED FOR L ANDING JAM WAS LESS. UNEVENTFUL LANDING. PERFORMED GVI OF RUDDER CABLES FROM RUDDER PEDALS TO RUDDER PCV'S NO DEFECTS NOTED. INSPECTED FEEL/SUMMING UNIT, NO DEFECT NOTED. PERFORMED OPS TEST OF RUDDER SYSTEM IAW TASK NR 27-20-00-710-802, OPS GOOD. REMOVED FLOORBOARD AND ACCESS PANEL AS REQUIRED. PERFORMED GVI OF RUDDER CABLES FROM RUDDER PCV. NO DEFECT 2 H 7 2 4T RT A13NM 20081219 EA 2008 12 19 MALA080212 1 20081211 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE INDICATION A MALA B EMER. DESCENT N FALSE WARNING CL CLIMB 1 GL 15 8943A 7943 ON CLIMB-OUT THE SMOKE TOILET MSG ILLUMINATED AND LAVATORY SMOKE ALARM SOUNDED FOR APPROX 5 MIN AND THEN EXTINGUISHED AF TER 5 MIN. THE CREW FOLLOWED THE AIRCRAFT NON-NORMAL PROCEDURES. THE CREW CONTACTED ATC AND DECLARED AN EMERGENCY AND REQUESTED PRIORITY BACK TO DTW, FLIGHT LANDED IN DTW WITHOUT FURTHER INCIDENT. THE FA AND PAX SMELLED AN ODOR THAT WAS VERY FOUL. THE FOUL SMELL DIDN'T APPEAR TO BE ELECTRICAL, RUBBER OR PETROLEUM. PERFORMED OP CHK LAV SMOKE DETECTION SY STEM IAW AMM 26-16. OP CHECK GOOD NO EVIDENCE OF SMOKE OR FOUL SMELL IN THE LAV OR PAX COMPARTMENT. RAN PACKS OF BOTH ENGINES AND ALSO APU FOR 10 MINUTES. 2 L 7 2 4F RT A21EA 20081219 NM 2008 12 19 NSVA2008047 1 20081217 A 5240 DOOR BOMBDR DHC8 DHC8402 1390042 NM AFT SERVICE UNSECURE A NSVA O OTHER N FALSE WARNING CR CRUISE 1 EA 27 199WQ 4199 RIGHT SERVICE DOOR ILLUMINATED INFLIGHT AT 12000 FT. NO LOSS OF CABIN PRESSURE. EMERGENCY WAS DECLARED. RESECURED AFT SERVICE DOOR IAW AMM 52-41-00. NO DISCREPANCIES NOTED. 2 H 7 2 4T RT A13NM 20081219 NM 2008 12 19 HALA2008121100881 1 20081211 A 2120 UNKNOWN BOEING 717 717200 1383700 NM CABIN ODOR A HALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 484HA 55129 ELECTRICAL SMOKE DETECTED LIGHTLY ON FLT 120, BUT ON FLT 119 THE CABIN AND PAX INQUIRED. ALSO, ICE. RAN LT AND RT PAC KS GASPER FANS ENG TURNED GALLEY PWR ON. NO DEFECTS, ALL INT LTS TURNED ON, NO DEFECTS. ALSO, COCKPIT INTERIOR LIGHTS CHECK OK. 2 L 7 2 4F TR A6WE 20081219 EU 2008 12 19 MALA080211 1 20081205 A 3350 POWER SUPPLY SAAB SF340 340B 7860101 EU EMERGENCY LIGHTS INOPERATIVE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 438XJ 340B438 DURING OPERATIONAL CHECK OF EMERGENCY LIGHTS FOUND OVERWING DOOR EXIT LIGHTS INOP. FOUND POWER SUPPLY AT 23LN INOPERATI VE. REMOVED AND REPLACE EMERGENCY POWER SUPPLY, OPS CHECKS WERE GOOD. 2 L 7 2 4T RT A52EU 20081219 NM 2008 12 19 HALA2008120500888 1 20081205 A 5314 KEELBEAM BOEING 767 76733A 1385209 NM BS 785-950 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 593HA 33424 LEVEL "2" CORROSION AT FASTENER HOLES ON KEEL LOWER CHORDS FROM STA 785.9 - 950 AND LBL 9.5 - RBL 9.5. CORROSION BLENDE D OUT ON KEEL CHORDS LOWER SURFACE AROUND FASTENER HOLES IAW SRM 58-50-12/1AO1 REV 77. 2 L 7 2 4F RT A1NM 20081219 SO 2008 12 19 SWIA200820632 1 20081210 A 5712 RIB EMB 120 EMB120ER 3260203 SO RT WING CRACKED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 217SW 120286 SVC CHECK, RIGHT WING LEADING EDGE, INBOARD RIB ASSEMBLY IS CRACKED IN TWO PLACES. REPLACED PER SRM. 2 L 7 2 4T RT A31SO 20081219 SO 2008 12 19 SWIA200820634 1 20081209 A 2497 WIRE EMB 120 EMB120ER 3260203 SO C/B PANEL BURNED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 560SW 120334 SVC CHECK, FOUND WIRE W138-0001-2 BURNED ABOVE OVERHEAD CB PANEL. REPLACED FULL LENGTH OF WIRE W138-0001-2. 2 L 7 2 4T RT A31SO 20081219 SO 2008 12 19 SWIA200820635 1 20081211 A 3233 1959500007 ACTUATOR EMB 120 EMB120ER 3260203 SO RT MLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 565SW 7592 1901 120340 FLT 5791 - RIGHT MAIN GEAR WOULD NOT FULLY RETRACT. REPLACED RIGHT MAIN GEAR ACTUATOR PER AMM, PN 19595-000-07, SN ON 9 1, SN OFF B161. 2 L 7 2 4T RT A31SO 20081219 NM 2008 12 19 UALA2008121506888 1 20081214 A 2560 140N2576218 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR UNSECURE A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 572UA 26682 GIRT BAR AT DOOR 4R HAS FALLEN ON FLOOR. SECURED DOOR 4R GIRT BAR INSTALLATION. 2 L 7 2 4F 4 F RT A2NM E17NE 20081219 NM 2008 12 19 UALA2008121506866 1 20081212 A 5720 ANGLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT WING CRACKED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 RT WING I/B CAVITY, LES 160 MOST I/B LEADING EDGE FAIRING SUPPORT UPPER ATTACH TO FRONT SPAR CRACK BETWEEN 2 EA FASTENER S INTO FRONT SPAR ON ANGLE. MAJOR REPAIR ACCOMPLISHED. INSTALLED FREEZE PLUGS AND NEW ANGLE REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081219 NM 2008 12 19 ABXA200812160270 1 20081210 A 3397 CONNECTOR BOEING 767 767232 1385132 NM CABIN DEFECTIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 750AX 22227 L1 ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RE-PINNED CONNECTOR D9084P, PIN NR 9 RELOCATED TO PIN SLOT NR 13. REFE RENCE WIRE NR WT84-8020-16 IAW B767 WDM 33-51-14. 2 L 7 2 4F RT A1NM 20081222 EU 2008 12 22 USAA2008121592230 1 20081212 A 5347 F53332210200 SEAT TRACK AIRBUS 330 A330323 3940030 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AY 375 BFM - C2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR53.9 TO FR55, -Y450. REPAIRED SEAT TRACK BETWEEN FR53.9 TO FR55, -Y450 IAW A330 SRM 53-31-15. 2 L 7 2 4F RT A46NM 20081222 EU 2008 12 22 USAA2008121592231 1 20081212 A 5347 A53275187203 SEAT TRACK AIRBUS 330 A330323 3940030 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AY 375 BFM - C2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR58 TO FR68, -Y450. REPAIRED SEAT TRACK BETWEEN FR58 TO FR68 , -Y450 IAW A330 SRM 51-42-11. 2 L 7 2 4F RT A46NM 20081222 NM 2008 12 22 USAA2008121592223 1 20081211 A 5347 141T5121 SEAT TRACK BOEING 767 7672B7ER 1385107 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 253AY 24894 BFM - C4 - MAJOR REPAIR - LEVEL 2 CORROSION ON SEAT TRACK CROWN & INBOARD FLANGE AT BS 347, LBL 54.75. REPAIRED SEAT TR ACK AT BS 347, LBL 54.75 IAW B767 SRM 51-10-02. 2 L 7 2 4F RT A1NM 20081222 NM 2008 12 22 USAA2008121692239 1 20081206 A 5320 65C333701 INTERCOSTAL BOEING 737 7374B7 138449C NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - EXFOLIATION CORROSION ON INTERCOSTAL BETWEEN BS 947 & BS 967, RBL 25. REPLACED INTERCOSTAL BE TWEEN BS 947 & BS 967, RBL 25 IAW SRM 53-60-51 & 51-10-02. 2 L 7 2 4F RT A16WE 20081222 CE 2008 12 22 GUUA94732121208A 1 20081212 A 3260 RECEPTACLE BEECH 1900 1900D 1154162 CE MLG INDICATOR DIRTY A GUUA O OTHER N FALSE WARNING AP APPROACH 1 SO 29 69547 UE189 FLIGHT: 9294 FKL/DUJ DURING APPROACH GREEN "H" LANDING GEAR INDICATOR LIGHTS DO NOT ALWAYS STAY ILLUMINATED. CLEANED LI GHT RECEPTACLE TO RESTORE CONDUCTIVITY. OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 20081215 EA 2008 12 15 SWIA200820618 1 20081210 A 3350 LAMP CNDAIR CL600 CL6002B19 1900309 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 929SW 7703 FLT 5849 - AFT EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 SWIA200820619 1 20081207 A 2910 O-RING CNDAIR CL600 CL6002B19 1900309 EA HYD SYSTEM LEAKING A SWIA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 699BR 7801 FLT 6562 - GEAR DISAGREE WARNING ON GEAR EXTENSION WITH HYDRAULIC SYSTEM 3 SHOWING ZERO. REPLACED DAMAGED O-RING AND SW UNG GEAR. 2 L 7 2 4F RT A21EA 20081215 WP 2008 12 15 AALA200810425 1 20081121 A 5340 ATTACH ANGLE DOUG DC9 DC982 3022082 WP ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 FORWARD CARGO, RIGHT SIDE STATION 237 INTERCOSTAL ATTACH ANGLE AT FRAME BELOW TIE DOWN TRACK IS CRACKED. REMOVED AND RE PLACED WITH SERVICEABLE ANGLE PER SRM 51-01-00. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810444 1 20081126 A 5310 DOOR FRAME DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 CORROSION ON AFT CARGO DOOR CUT-OUT BOX FRAME FORWARD SIDE OF DOOR, STATION 1148 TO STATION 1155 BETWEEN LONGERON 26 RIG HT AND LONGERON 27 RIGHT. BLENDED OUT DAMAGE, FOUND TO BE OUT OF LIMITS. INSTALLED WEB REPAIR PER ESO 80559 DATED 11/2 6/08. 2 L 7 2 4F A6WE 20081215 WP 2008 12 15 AALA200810447 1 20081121 A 5340 BRACKET DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 CORROSION ON TOP OF GIRT BAR BRACKET, AFT SERVICE DOOR, FORWARD BRACKET. REPLACED GIRT BAR BRACKET. 2 L 7 2 4F A6WE 20081215 EA 2008 12 15 SWIA200820620 1 20081205 A 3350 LAMP CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHT BURNED OUT A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 766SK 10232 FLT 6550 - AFT EXIT SIGN EMERGENCY CALL LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A21EA 20081215 EA 2008 12 15 SWIA200820621 1 20081210 A 7120 BUSHING CNDAIR CL600 CL6002C10 1390015 EA ENGINE MOUNT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 709SK 10159 SVC CHK, RIGHT ENGINE LEFT THRUST LINK AND BUSHING CORRODED. REPLACED LINK AND BUSHING PER AMM. 2 L 7 2 4F RT A21EA 20081217 NM 2008 12 17 UALA2008121006827 1 20081210 A 3350 582233 BATTERY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT LIGHT SIGN INOP AT AFT CREW STAIRS. REPLACED BATTERY, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081217 NM 2008 12 17 SWAA087057 1 20081211 A 5315 6546804 FLOORBEAM BOEING 737 7377H4 1384404 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 707SA 27841 DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM TEE CAP CRACKED AT BS 540, LBL 1. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087088 1 20081214 A 3350 8100022608 LIGHT BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 790SW 30604 DURING SCHEDULED 8Y CHECK, FOUND FWD LAV EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 C8GA20080040 1 20080824 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720-720A DAMAGED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING MFEC INSPECTION OF # 4 RIGHT LAP SEAM BS 720-720A NOTED 7 EA FASTENER HOLES CRACKE D. CUT OUT DAMAGED HOLES AND VERIFIED CRACK CONTAINMENT. FABRICATED FILLER FROM 2024 T3 .071" AND FABRICATED DOUBLER FRO M 2024 T3 .080". INSTALLED REPAIR PER B727 SRM 53-30-03. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 C8GA20080034 1 20080904 A 5414 NOSE COWL BOEING 727 727223 1384074 NM NR 1 ENGINE DENTED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING VISUAL INSPECTION ON THE NR 1 ENGINE NOSE COWL A DENT WAS NOTED AT THE 1 O'CLOCK P OSITION. EVALUATED DENT AND FOUND A/Y RATIO OUT OF LIMITS. CUT OUT DAMAGED AREA AND FABRICATED INTERNAL DOUBLER OF 2024 T3 .040, FABRACATED FILLER OF 2024 T3 .032, FABRICATED DOOR DOUBLER OF 2024 T3 .050. INSTALLED DOUBLER REPAIRS IAW SRM 5 4-30-02, 54-30-03. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 C8GA20080035 1 20080903 A 5330 SKIN BOEING 727 727223 1384074 NM BS 254 DAMAGED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION A CRACK WAS NOTED ON THE EXTERIOR OF THE FUSELAGE BS 254 STRINGER 10 LE FT. CUT OUT DAMAGED SKIN, VERFIED CRACK CONTAINEMENT WITH NDT. FABRICATED FILLE AND FABRICATED DOUBLER. INSTALLED FILLER AND DOUBLER IAW SRM 53-30-03. NO OTHER DEFECTES WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 C8GA20080041 1 20080913 A 5330 SKIN BOEING 727 727223 1384074 NM BS 950E-990 MISREPAIRED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING VISUAL INSPECTION FOR DTA. EXISTING EXTERNAL DOUBLER/TRIPLER REPAIR AT BS 950E TO 990 29R IS NON-COMPLIANT. REMOVED EXISTING REPAIR CLEANED AND VERIFIED CRACK CONTAINMENT. FABRICATED TRIPLER AND FABRICA TED DOUBLER. FABRICATED 2 EA STRAPS. INSTALLED REPAIR PER EA EAAG38-1 . NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 C8GA20080037 1 20080906 A 5330 SKIN BOEING 727 727223 1384074 NM BS 481-681 CRACKED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING MFEC INSPECTION MULTIPLE FASTENER HOLES WERE NOTED AS CRACKED AT UPPER FUSELADGE S KIN LAP SEAM 4R BETWEEN BS 481-681. CUT OUT UPPER AND LOWER SKINS, VERIFIED CRACK CONTAINMENT. FABRICATED LAP SEAM FILLE R, REPAIR DOUBLER AND REPAIR TRIPPLER, INSTALLED DOUBLER/ TRIPLER REPAIR AT STR. 4R BETWEEN BS 481-681 IAW BOEING MESSAG E 1-947016492-14 AND SKETCH 1-947016492-1 W/ 8100-9 DATED 09-05-08. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SE RVICE. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 SWAA087044 1 20081211 A 5330 6545768 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 304, UPPER HINGE CUTOUT. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087045 1 20081211 A 5330 6562212 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT, BS 304 ABOVE CUTOUT CENTER LINE. REPAIRE D SKIN PER ER. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087046 1 20081211 A 5330 6562212 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER HINGE CUTOUT, BS 304 BELOW CUTOUT CENTER LINE. REPAIRE D SKIN PER ER. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087062 1 20081211 A 5313 6546546 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 769 TO BS 770, STR 25L. REPAIRED STRINGER PER SRM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087063 1 20081211 A 5322 6546546 SHEAR TIE BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 847, BETWEEN STR 25L TO STR 26L. REPAIRED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087073 1 20081214 A 5312 6517853 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 5.7. REPAIRED WEB PER ER. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087074 1 20081214 A 5312 6517853 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 613SW 27931 DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 5.7. REPAIRED WEB PER ER. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087075 1 20081213 A 3233 65448105 ACTUATOR BOEING 737 7373H4 1384600 NM RT MLG FAULTY A SWAA K NONE J WARNING INDICATION LD LANDING 1 SW 29 653SW 28398 RT MLG EXTENSION SHOWED UNSAFE INDICATION. CYCLED GEAR AND GOT THREE GREEN AND LANDED WITHOUT INCIDENT. REMOVED AND RE PLACED UPLOCK ACTUATOR PER MM. 2 L 7 2 4F RT A16WE 20081217 2008 12 17 SWAA087076 4 20081212 A 2565 D31354 SLIDE BOEING 737 7373G7 138447J NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 671SW 23785 R2 EMERGENCY EVAC DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087080 1 20081213 A 5743 115A5211 LUG BOEING 737 7377H4 1384404 NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 731SA 27863 DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION BEARING I/B UPPER ATTACH LUG CORRODED. REPAIRED LUG PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087090 1 20081212 A 3260 189929 SENSOR BOEING 737 7373H4 1384600 NM RT MLG LOOSE A SWAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 29 653SW 28398 RED RIGHT GEAR LIGHT ILLUMINATED DURING CONFIGURATING A/C ON FINAL APPROACH, GO-AROUND INITIATED, GEAR HANDLE BROUGHT UP . DURING NEXT GEAR EXTENSION THE GREEN RIGHT GEAR LIGHT ILLUMINATED, 3 GREEN - NORMAL LANDING. FOUND SENSOR LOOSE. SE CURED SENSOR PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087091 1 20081214 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 38, STR 21L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087098 1 20081215 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087099 1 20081215 A 5311 6546536 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 559, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087105 1 20081215 A 2560 P4010021 BATTERY BOEING 737 7373H4 1384600 NM FLASHLIGHT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED OTS CHECK, FOUND FWD EMERGENCY FLASHLIGHT I/B BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087106 1 20081215 A 5754 65C26602 SLAT BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED OTS CHECK, FOUND LT WING 2 SLAT OUTBOARD T/E DELAMINATED. REMOVED AND REPLACED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087107 1 20081214 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 491WN 33867 DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS LIGHT COVER BROKEN. REPAIRED COVER PER MM. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 ZZDA2008184 1 20081211 A 2897 WIRE BOEING 717 717200 1383700 NM LT WING DAMAGED A ZZDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 37 989AT 55152 DEPARTED TPA CLIMBING ABOVE 10,000 FEET ENGINE LEFT FUEL PRESSURE AND TANK LEFT PUMP LOW LIGHTS CAME ON. CONFIRMED LEFT TANK NOT FEEDING. OPENED CROSSFEED VALVE AND DIVERTED TO KMOC. REPAIRED DAMAGED WIRES TO LEFT FUEL BOOST PUMP IN LEFT WING IAW EA 17-28-1412A; ALL SYSTEMS OPS CHECK NORMAL IAW 28-20-01; LEAK CHECK GOOD FOR LEFT WING ANTI-ICE DUCT IAW 30- 10-07. AIRCRAFT RETURNED TO NORMAL. 2 L 7 2 4F TR A6WE 20081222 WP 2008 12 22 UPS08854151 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-86 AT STA 1743 L16R - L17R HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW UPS EO DC8-5330-31415-A AND FVCI DWG 53-08540-13. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854162 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-02 AT STA 13 L15-16L HAS NO SRM REF. REMOVED REPAIR DOUBLER, FABRICATED AND I NSTALLED REPLACEMENT REPAIR DOUBLER IAW UPS EO DC8-5330-31402-A AND FVCI DWG 53-08540-1. 2 L 7 4 4F RT 4A25 20081222 NM 2008 12 22 KCSA081616 1 20081215 A 5320 WEB BOEING 747 747212B 1384886 NM ZONE 100 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 AFT EDGE OF PRESSURE DECK WEB CRACKED AND CORRODED AT B.S.1480, WL-187, BL-0 TO RBL-9 2 L 7 4 4F RT A20WE 20081222 CE 2008 12 22 GUUA94152120908A 1 20081209 A 5220 DOOR BEECH 1900 1900D 1154162 CE EMERGENCY EXIT OUT OF RIG A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 17541 UE203 DURING SCHEDULED ROUTINE MX DISCOVERED RT AFT EMERGENCY EXIT HARD TO OPEN. RERIGGED RT AFT EMERGENCY EXIT. OPS CHECK G OOD. 2 L 7 2 4T RT A24CE 20081222 NM 2008 12 22 KCSA081614 1 20081214 A 5320 STIFFENER BOEING 747 747212B 1384886 NM ZONE 100 CORRODED A KCSA K NONE O OTHER IN INSP/MAINT 1 GL 23 708CK 21937 B.S.1335 FRAME STIFFENER CORRODED IN LT WING LANDING GEAR WW AT LBL-130, WL-160 TO 188 2 L 7 4 4F RT A20WE 20081222 2008 12 22 DXTA2008121603404 4 20081216 A 2210 AUTOPILOT SYS AMD FALC50 FALCON2000 2730170 NM INOPERATIVE E DXTA A UNSCHED LANDING S AFFECT SYSTEMS CL CLIMB 1 GL 07 204QS 104 AUTOPILOT INOP. 2 L 7 2 4F RT A50NM 20081222 WP 2008 12 22 UPS08854168 1 20081012 A 5230 SKIN DOUG DC8 DC873F 302199F WP MAIN CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-08 STA 160-167 L15-17L AT MCD EXTERIOR WINDOW PLUG HAS NO SRM REF. REMOVED RE PAIR DOUBLER AND TRIPLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-02-00 FIG 22A. 2 L 7 4 4F RT 4A25 20081222 EA 2008 12 22 QXEA2008121601242 1 20081211 A 5315 FLOORBEAM CNDAIR CL600 CL6002C10 1390015 EA BS 280 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 616QX 10128 PDX - C4 - CRACK ON BEAM AT FS 280 ABOVE TEE FITTING IN THE UPPER RADIUS AT LBL 9.0. REMOVED LT 280 BEAM, LOCATED AND D RILLED NEW LT SECTION OF BEAM. INSTALLED BEAM IAW SRM 51-42-06 AND REO 670-53-11-265. INSTALLED DRIP TRAY AND INTERCOS TALS IAW SRM 51-42-06. 2 L 7 2 4F RT A21EA 20081222 NM 2008 12 22 F3LA2008121600722 1 20081212 A 3350 32145410 POWER SUPPLY AIRBUS A319 A319111 3930336 NM EMERGENCY LIGHTS FAILED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 923FR 60 2019 PILOT REPORTED THE EMERGENCY LIGHTS WERE ON IN ROWS 14 AND AFT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SU PPLY UNIT AT POSITION 10WL IN ACCORDANCE WITH AMM 33-51-38PB401 AND PERFORMED AN OPERATIONAL TEST. 2 L 7 2 4F RT A28NM 20081222 WP 2008 12 22 UPS08854134 1 20081022 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-W3-11 LT WING O/B LEADING EDGE SKIN PLATING XFS 534.1 EO DC8-5100-30418-C APPX H IS MARKED NOT VISIBLE ON STEP 6&7. REMOVED REPAIR DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 57-02-01 FIG 2H. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854142 1 20081027 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-W3-19 LT STUB WING PLATING XFS 516.5 EO DC8 -5100-30418-C APPX H STEP 6 & 7 ARE M ARKED NOT VISIBLE. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW DC-8 SRM 57-02-01A F IG 1 SHEET 1 AND 57-03-00 FIG 12 SHEET 1. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854144 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-45 AT STA 1418 L25R - L26R HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER. FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11. 2 L 7 4 4F RT 4A25 20081222 NM 2008 12 22 UPS08554190 1 20081214 A 5753 113N200949H SKIN BOEING 757 75724APF 1384969 NM TE FLAP DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 467UP 25483 INSPECTION TYPE:N/A DENT IN LWR FLAP SKIN LT INBOARD MAIN FLAP. REPAIRED IAW B757-5750-31130-B. 2 L 7 2 4F RT A2NM 20081222 NM 2008 12 22 UPS08554197 1 20081213 A 5610 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT BINDING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 468UP 25484 INSPECTION TYPE:N/A UNABLE TO OPEN CAPTAINS COCKPIT WINDOW. HANDLE MOVES AFT BUT WINDOW WILL NOT OPEN. CHECKED CAPTAIN S C/P WINDOW WINDOW IAW MM 56-11-02-215-089. TESTS OK. 2 L 7 2 4F RT A2NM 20081222 WP 2008 12 22 UPS08854187 1 20081015 A 5330 DOUBLER DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR SEQUENCE 803-F1-92 AT STA 1430 L16L HAS NO SRM REF AND REQUIRES APPX F OF EO DC8-5100-30418C. REPAIRED PER FVC DRAWING 53-08540-12, EO DC8-5330-31414-A SA PER SAA EAR 81426850001. 2 L 7 4 4F RT 4A25 20081217 NM 2008 12 17 SWAA087134 1 20081215 A 5754 6573714 SLAT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 327SW 23691 DURING SCHEDULED 22Y CHECK, FOUND RT WING 6 SLAT CRACKED O/B OF ACTUATOR. REMOVED AND REPLACED SLAT PER SRM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087135 1 20081215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 847, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087115 1 20081214 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 491WN 33867 DURING SCHEDULED MV2 CHECK, FOUND RT EEPLS LIGHT COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087116 1 20081215 A 3350 101331 LENS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 614SW 28033 LT FWD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2 L 7 2 4F RT A16WE 20081217 2008 12 17 SWAA087122 4 20081215 A 2565 D31354 SLIDE BOEING 737 737317 138447P NM R2 DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EXIT SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087123 1 20081215 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 790SW 30604 DURING SCHEDULED 8Y CHECK, FOUND LT EEPLS STRIP DAMAGED. REPLACED EEPLS PER SWA DWG. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087124 1 20081215 A 3350 81000 LIGHT BOEING 737 7377H4 1384404 NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 790SW 30604 DURING SCHEDULED 8Y CHECK, FOUND RT EEPLS STRIP DAMAGED. REPLACED EEPLS PER SWA DWG. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087140 1 20081215 A 5340 65C27314 STRINGER CLIP BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED 24Y CHECK, FOUND LT STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 UALA2008120906819 1 20081209 A 3350 GE1317 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 116UA 26908 MAIN GALLEY EMERGENCY CEILING LIGHT INOP. RELAMPED EMERGENCY LIGHT, OP CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081215 NM 2008 12 15 SWAA086959 1 20081210 A 5754 65C26002 SLAT BOEING 737 7373H4 1384600 NM LT WING DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT O/B T/E DELAMINATED. REPAIRED SLAT PER SWA EA. 2 L 7 2 4F RT A16WE 20081215 2008 12 15 SWAA086970 4 20081210 A 2565 63550 SLIDE BOEING 737 7377H4 1384404 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 744SW 29490 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2 L 7 2 4F RT A16WE 20081215 2008 12 15 SWAA087039 4 20081211 A 2565 D31354 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR OUT OF ADJUST A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086976 1 20081210 A 5330 6545767 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 430, RBL 2. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086984 1 20081210 A 5314 6545866 KEELBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND RT KEEL BEAM CORRODED BETWEEN BS 520 TO BS 530. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 SWAA086995 1 20081210 A 5330 6562212 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 675AA 23253 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT, AT BS 304. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081215 NM 2008 12 15 AALA200820093 1 20081201 A 5320 146N56511 INTERCOSTAL BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AA 57228 24591 INTERCOSTAL CORRODED, REPAIRED INTERCOSTAL IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 20081215 NM 2008 12 15 AALA200820092 1 20081201 A 5315 146N508919 FLOORBEAM BOEING 757 757223 1384957 NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 633AA 57228 24591 FLOORBEAM CORRODED, REPAIRED FLOORBEAM IAW SRM 53-0-51-2R3. 2 L 7 2 4F RT A2NM 20081215 EU 2008 12 15 UALA2008121006838 1 20081209 A 5320 BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 405UA 452 BEAM 205 HAS 1EA HOLE CORRODED. MAJOR REPAIR ACCOMPLISHED. CONNECTED NEW BEAM 205 TO NEW BEAM 200 AND INSTALLED GALLEY HOLD DOWN NUTS IN RETAINERS. INSTALLED BEAM 205. 2 L 7 2 4F 4 F RT A28NM E40NE 20081215 WP 2008 12 15 AALA200810432 1 20081121 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 501AA 49738 CORROSION ON NUMBER 1 SEAT TRACK STATION 470. INSTALLED REPAIR PLUG AARD 53-20-00-10. 2 L 7 2 4F A6WE 20081216 WP 2008 12 16 AALA200810476 1 20081211 A 5320 ANGLE DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 7541A 49995 ANGLE CRACKED AT STATION 1474 AND LONGERON 19 LEFT. REMOVED AND REPLACED ANGLE PER SRM 53-01. 2 L 7 2 4F A6WE 20081217 NM 2008 12 17 UALA2008120806775 1 20081205 A 5230 DOOR FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FWD CARGO DOOR DENTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 552UA 26641 FWD CARGO DOOR DENTED, LOWER AFT INSIDE CORNER. MAJOR REPAIR ACCOMPLISHED. REPLACED LWR AFT CORNER FRAME P/N 143N6618- 5. 2 L 7 2 4F 4 F RT A2NM E17NE 20081217 WP 2008 12 17 DHLA200800134 1 20081210 A 2612 FIRE WARNING DOUG DC8 DC873 302199C WP NR 1 NACELLE ILLUMINATED A DHLA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 GL 05 802DH 46076 FIRE INDICATION NR 1 ENG DURING APPROACH. FIRED BOTTLES INBOARD. NR 1 ENG FIRE LOOP B DEFERRED PER MEL 26-2-3 CT C DMI 34247. INSTALL PLACARD INST SPEC PROC C/W. MX NOTIFIED. 2 L 7 4 4F RT 4A25 20081217 NM 2008 12 17 DHLA2008743515 1 20081110 A 5320 STRAP BOEING 727 727225 1384077 NM ZONE 100 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 LOWER FUSELAGE FWD CARGO COMPARTMENT FROM BS 700 TO BS 720A WL 200 LBL47 STABILIZER STRAP WITH CORROSION OUT OF LIMITS. REPLACED STABILIZER STRAP FROM BS 680 TO BS 720C WL 200 LBL 47 IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081217 WP 2008 12 17 AALA200810480 1 20081214 A 5230 3926046510 TEE FITTING BOEING DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 248AA 49259 LOWER FORWARD TEE FITTING CRACKED. REMOVED AND REPLACED CRACKED TEE FITTING. 2 L 7 2 4F A6WE 20081217 EU 2008 12 17 DHLA200800137 1 20081215 A 3350 BATTERY PACK AIRBUS 300 A300B4203 3930306 EU EMERGENCY LIGHTS DISCHARGED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 366DH 249 EMERGENCY LIGHTS BATTERIES 0 VOLTS. 2 L 7 2 4F RT A35EU 20081217 WP 2008 12 17 AALA200810466 1 20081203 A 5320 ANGLE DOUG DC9 DC983 3022083 WP ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 436AA 49454 CORROSION ON ANGLE FRAME 9 INCHES TO THE RIGHT OF AIRCRAFT CENTER LINE AT STATION 1380, LOWER AFT SIDE OF APU ENCLOSURE. REPAIR DOUBLER INSTALLED PER ESO 80559 DATED 12/01/08. 2 L 7 2 4F RT A6WE 20081217 NM 2008 12 17 DHLA2008743516 1 20081105 A 5320 STRAP BOEING 727 727225 1384077 NM ZONE 200 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 UPPER FUSELAGE CARGO CABIN BS 720C+3 INCH AT LBL 2 AND LBL 25 FLOORBEAM STABILIZER STRAPS CORRODED. REPLACED STABILIZER STRAP LBL2 FROM BS 720C TO BS 720F IAW B727 SRM 51-10-1 PARA 7A. REMOVED CORROSION AND FOUND WITHIN LIMITS ON STABILIZ ER STRAP BS 720C+3 INCH LBL 25 IAW B727 SRM 53-10-1FIG 1. 2 L 7 3 4F A3WE 20081217 WP 2008 12 17 FDEA200812125124 1 20081212 A 5720 ARB2917 ANGLE DOUG DC10 DC1030F 3023504 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 317FE 46835 LT WING LEADING EDGE, FOUND CRACK AND RIVETS U/S ON ANGLE SUPPORT REFUEL PANEL. 2 L 7 3 4F RT A22WE 20081217 2008 12 17 FDEA200812125130 2 20081212 A 7200 ENGINE AIRBUS 300 A300F4605R 3930327 EU NR 1 SURGES A FDEA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CE 21 689FE 875 DURING TAKEOFF ROLL NR 1 ENG N1 AND N2 SURGED AFTER TOGA, DROPPED 2 3 PERCENT TIMES. NOTED EGT AND FF GAGES MIRRORED N1 AND N2. REJECTED TAKEOFF AT 85 KTS. FOLLOWED QRH PROCEDURE. 2 L 7 2 4F RT A35EU 20081217 NM 2008 12 17 FDEA200812125131 1 20081212 A 5315 FLOORBEAM BOEING 727 7272D4 138407U NM ZONE 200 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 287FE 21849 ANGLE FOR FLOOR JUST FWD OF FLIGHT DECK DOOR CUT OUT IS CRACKED REMOVED FLOOR SUPPORT AND ATTACH BRACKET, FABRICATED DRI LLED, TRIMMED, TREATED AND PRIMED NEW ATTACH ANGLE. INSTALLED FLOOR SUPPORT AND NEW ANGLE. REFERENCE BOEING DWG NR 6 5-17593/ITEM NR -239 AND SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 DHLA2008743517 1 20081123 A 5320 STRAP BOEING 727 727225 1384077 NM ZONE 100 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 GL 05 743DH 22438 LOWER FUSELAGE E/E COMPARTMENT FROM BS 294.5 TO BS 360 WL 199 BL 0 STABILIZER CRACKED. REPLACED STABILIZER STRAP SECTIO N FROM BS 294.5 TO BS 360 WL 199 BL 0 IAW B727 SRM 51-10-1 PARA 7A. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 FDEA200812015015 1 20081201 A 5310 AFA71321 FITTING DOUG MD11 MD11F 3023600 NM DOOR FRAME CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ON 0.460 INCH DIAMETER HOLE, MAIN CARGO DOOR LOWER JAMB SUPPOR T FITTING NR 1 FOUND WITH CRACK INDICATION AT HOLE NR C. MAIN CARGO DOOR LOWER JAMB SUPPORT FITTING NR 1 FOR CRACKED BO LT HOLE NR C, BUSHING REPAIR CARRIED OUT AS PER SRM 53-50-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100. 2 L 7 3 4F RT A22WE 20081217 NM 2008 12 17 SWAA087054 1 20081211 A 5340 65C27314 STRINGER CLIP BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 1006, STR 25R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087087 1 20081213 A 3350 6574550 LIGHT BOEING 737 7377H4 1384404 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 779SW 27884 DURING SCHEDULED MV3 CHECK, FOUND OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 16. RELAMPED LIGHT PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087117 1 20081215 A 5312 6545409 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 323SW 23344 DURING SCHEDULED 22Y CHECK, FOUND LT MLG WHEEL WELL CEILING PRESSURE DECK, FWD BULKHEAD, CRACKED AT BS 665, LBL 40. REP AIRED BULKHEAD PER AAR EA. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 SWAA087141 1 20081215 A 5753 6573731 SKIN BOEING 737 7373Y0 1384671 NM FORE FLAP DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 682SW 23496 DURING SCHEDULED 24Y CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM. 2 L 7 2 4F RT A16WE 20081218 2008 12 18 UALA2008120806781 4 20081207 A 2565 D31564101 LANYARD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R3 DOOR SLIDE UNSECURE A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 549UA 25397 THE R3 DOOR SLIDE PACK HAS LANYARD STICKING OUT OF THE BOTTOM OF THE SLIDE PACK DOOR. SLIDE PACK UNDISTURBED. DOOR ARM S AND DISARMS NORMALLY. SECURED D-RING STRAP. 2 L 7 2 4F 4 F RT A2NM E17NE 20081218 NM 2008 12 18 SWAA087142 1 20081215 A 5210 6545800 SKIN BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 304SW 22944 DURING SCHEDULED 24Y CHECK, FOUND R1 DOOR SKIN CRACKED AT UPPER HINGE CUTOUT, BS 290, BETWEEN WL 256 TO WL 259. REPAIRE D SKIN PER ER. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 UALA2008111303691 1 20080702 A 2997 CLAMP BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CONNECTOR MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 NR 1 ENG PYLON HYD BAY CONNECTOR D02134 SADDLE CLAMP IS MISSING. REPLACED CONNECTOR DO2134P SADDLE CLAMP. OPS CHECKS O F NR 1 ENG HYD PRESSURE INDICATION CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 UALA2008111304201 1 20080809 A 2820 7G1103600U PRESSURE SWITCH BOEING 767 767322 1385200 NM PWA 4056 PW4056 NE FUEL SYSTEM FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 668UA 30024 LEFT AFT FUEL BOOST LOW PRESS LIGHT INOP WITH PUMP OFF. REPLACED PRESSURE SWITCH, CHECKS OKAY. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 2008 12 18 UALA2008111306178 4 20081017 A 2565 SENSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EVAC SLIDE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 548UA 25396 DOOR 2R SLIDE ANNUNCIATOR ALWAYS ON EVEN WHEN DOOR NOT ARMED. REPLACED DOOR 2R GIRT BAR SENSOR S10220. OPS CHECKS GOOD . 2 L 7 2 4F 4 F RT A2NM E17NE 20081218 NM 2008 12 18 UALA2008120906797 1 20081208 A 3350 78671 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SEAT 58H MISSING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 198UA 28716 FLOOR PATH EMERGENCY LIGHT AT 58H MISSING. REPLACED LIGHT ASSY AT SEAT 58H. OPS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081218 NM 2008 12 18 UALA2008111306181 1 20081019 A 3320 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN IMPROPER PART A UALA O OTHER W B INADEQUATE Q C SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 555UA 26647 OVERHEAD READING LIGHT OVER ROW 26ABC OVERHEATED CAUSING BURNING SMELL IN CABIN. DEADHEADING FLT CREW REMOVED BULB AND SMELL DISSIPATED. REMOVED BULB IS IN COCKPIT. FLT ATTENDANT REPORTED AFT CABIN FWD LAV DOME LIGHT, THAT CAUSED OVERHEA D SMELL AT 26ABC. THE 26ABC READING LIGHTS NEVER REMOVED. REPLACED LAV DOME LIGHT 1591 REF IPC33-26-52-010, TESTED GOO D. INFO ONLY, FOUND WRONG BULB WAS INSTALLED, AND FLT CREWS REMOVED A BAD ELECTRICAL SMELL HEADSET AT 26ABC SEAT. 2 L 7 2 4F 4 F RT A2NM E17NE 20081218 NM 2008 12 18 UALA2008111306360 1 20081104 A 2913 65057 PUMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 ENGINE LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 547UA 25368 LOSS OF HYDRAULICS. FLIGHT DIVERTED. INBD CREW REPORTS PTU FAILED TO ENGAGE UPON FLUID LOSS VIA NR1 ENG EDP. NEED TO PERFORM HYDRAULIC PTU OPERATIONAL TEST. ACCOMPLISHED OPERATIONAL TEST PER MM 29-22-00 PTU CHECKS OK. ENGINE DRIVEN PUM P (EDP) - HYDRAULIC LOW PRESS LIGHT ILLUMINATED. EICAS MESSAGE 'HYD ENG PUMP' DISPLAYED BUT EICAS MESSAGE 'HYD SYS MAIN T' NOT DISPLAYED-LEFT SYSTEM. HYD FLUID RUNNING FROM NR 1 ENG HYD PUMP DRIVE PAD CAVITY DRAIN TUBE. REPLACED NR 1 CASE DRAIN FILTER & LEAK CHECKED DUE TO ENG DRIVEN PUMP LEAKING. REPLACED NR 1 ENG EDP AND APPLICABLE FILTERS. PER SFOLM L EFT ELECTRIC AC PUMP WILL NEED PRESSURE AND CASE DRAIN FILTERS REPLACED. REPLACED FILTER PER IPC 29 -11-18 AND LEAK CHE 2 L 7 2 4F 4 F RT A2NM E17NE 20081218 NM 2008 12 18 UALA2008120906804 1 20081209 A 5522 SKIN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ELEVATOR DELAMINATED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 LT OUTBOARD ELEVATOR, OUTBOARD FWD EDGE IS DELAMINATED. REMOVED DAMAGED PLY AND INSTALLED CARBON FIBER REPAIR. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 UALA2008111306362 1 20081102 A 2751 18196918 TRANSMITTER BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAP INACCURATE A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 550UA 25398 IN ALTERNATE FLAPS - INDICATORS SPLIT AT FLAPS 1. LT INDICATION MOVES TO 1 NORMALLY, RT INDICATOR JUMPS TO ABOUT 15 THE N NEEDLES STAY SPLIT UNTIL LEADING EDGES AND TRAILING EDGES GET TO POSITION 1, THEN INDICATIONS ARE WITHIN LIMITS. RT F LAP AND RT SLAT O/B XMITTERS WERE BOTH SLAVED IN. T/S WIRES FROM FSEU 2 TO FLIGHT DECK ROTARY SWITCH AND ARMING SWITCHE S, CKS GOOD. RELAY K10244 CHANGED. REMOVED ALL 3 FSEU 'S AT SAME TIME AND SLAVED IN KNOWN GOOD UNITS. SLAVED IN KNOWN GOOD FLAP. WIRING HAS BEEN RUNG FROM FSEU'S TO RT FLAP & SLAT, LT FLAP & SLAT AND PDU FLAP & SLAT XMITTERS. ALL ARE GOOD & COMPARABLE TO OPPOSITE SIDE. RELAY K10244 CHANGED. 2 L 7 2 4F 4 F RT A2NM E17NE 20081218 NM 2008 12 18 UALA2008111306427 1 20081108 A 2750 TRANSMISSION BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAP FAULTY A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 29 550UA 25398 FLAP DISAGREE ON APPROACH. FLAPS STUCK ON 20 UNITS. TROUBLESHOOT T/E FLAP DISAGREE. FOUND NR 6 FLAP TRANSMISSION OIL IS BLACK AS VIEWED THROUGH SIGHT GLASS. DRAINED AND REPLACED WITH NEW OIL. LAB ANALYSIS INDICATED ACCEPTABLE LEVELS OF CARBON COMPOUND, OK. REMOVED NR 8 TRANSMISSION BALL SCREW ASSY. INSTALLED NEW NR 8 T/E FLAP TRANS. 2 L 7 2 4F 4 F RT A2NM E17NE 20081218 NM 2008 12 18 UALA2008111304268 1 20080813 A 2730 4885501002 CONTROL UNIT BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE ELEVATOR FAULTY A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 791UA 26933 FLIGHT CONTROL SYSTEM STATUS MESSAGE. REPLACED CENTER ACE AND B27143 COUPLER IN P312-E01 PANEL. FAULT CLEARED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 NM 2008 12 18 UALA2008121006830 1 20081210 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT EEL LIGHT INOP AT SEAT ROW 44 LEFT. REPAIRED WIRING. OP CHECKS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081218 NM 2008 12 18 UALA2008121006831 1 20081210 A 3397 WIRE HARNESS BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE EMERGENCY LIGHT UNSECURE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 198UA 28716 EMERGENCY EXIT LIGHT INOP AT SEAT ROW 60 RIGHT. SECURED WIRING HARNESS. 2 L 7 4 4F 4 F RT A20WE E24NE 20081218 NM 2008 12 18 UALA2008111306144 1 20081016 A 3040 7858972 CONTROLLER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE WINDOW HEAT FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 215UA 30221 WINDOW HEAT L FWD LOSS OF LEFT FORWARD WINDOW HEAT ADVISORY. REPLACED LT WINDOW HEAT CONTROLLER. TEST OK, MSG CLEARED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 2008 12 18 UALA2008121206858 4 20081212 A 3421 S231T1106 INDICATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE ATTITUDE FAILED A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 656UA 25394 SAI PROBLEM. RTFL. REPLACED STANDBY ATTITUDE IND AND STATIC INVERTER-ILS PROCESSOR. OPS NORMAL ON GROUND. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 UALA2008121006836 1 20081209 A 2820 7G1103600U PRESSURE SENSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT BOOST PUMP INOPERATIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 644UA 25094 LEFT AFT BOOST PUMP PRESSURE LIGHT INOP. REPLACED LEFT AFT BOOST PUMP PRESSURE SWITCH. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 WP 2008 12 18 IXXA080037O 1 20081214 A 2910 ELBOW DOUG DC8 DC862F 3021972 WP HYD LINE BROKEN A IXXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 11 799AL 82623 3234 45922 DURING CLIMB FROM KMCC, THE CREW NOTICED A LOSS OF HYDRAULIC QUANTITY TO THE FIVE GALLON LEVEL. THE CREW RETURNED TO KM CC AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE HYDRAULIC SYSTEM AND FOUND THE RIGHT MAIN LANDING GEAR ACTUAT ING CYLINDER, UPPER LINE ELBOW BROKEN. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR ACTUATING CYLINDER, SERVICED TH E HYDRAULIC SYSTEM. THE OPERATIONAL CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 20081218 NM 2008 12 18 UALA2008111305605 1 20080831 A 2197 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CARGO BAY DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 659UA 27114 FWD CARGO COMP BELOW FLOOR-EQUIP COOLING SUPPLY AIR OVERHEAT SWITCH CONNECTOR WIRE HAS INSULATOR DAMAGE AND BARE CONDUCT OR EXPOSED 19 INCHES UPSTREAM OF CONNECTOR D00644. REPAIRED WIRE IAW BSWPM 20 -30-12 AND OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 UALA2008111305631 1 20080907 A 3350 78961 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 118UA 28811 THE 4F FWD PEEP LIGHT STRIP BROKEN OFF. REPLACED PEEPS LIGHT STRIP AND OPS CHECK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081218 EU 2008 12 18 FDEA200812125136 1 20081212 A 3230 A254210012 UPLOCK AIRBUS 300 A300F4605R 3930327 EU NLG FAILED A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 CE 21 650FE 726 ON FINAL NLG BOTH SYSTEMS SHOWED UNSAFE, GO AROUND TO HOLDING TO USE GRAVITY EXTEND PROCEDURES. THREE GREEN SAFE LIGHTS AFTER PROCEDURE WITH NORMAL LANDING, AND TOW IN CREW STATED GOT 3 UNLOCK (AMBER) RED LIGHT AND 2 GREEN LOCK LIGHTS ON M LG`S ON BOTH SYSTEMS BEFORE INITIATING GO-AROUND ADDED MPN A25421001-2, CPN 3211274 QTY 1 UPLOCK MSN 1114661. T/S PER T SM 32-30-00 PG112 FIG 117, AND DETERMINED THAT NLG UPLOCK ASSY NEEDS TO BE REPLACED. R & R NLG UPLOCK ASSY IAW AMM 32-3 1-21-4, & CYCLED NOSE GEAR 8 TIMES WITH NO FAULTS OR LEAKS DURING RETRACTION OR EXTENSION OF NLG INTERROGATED PROX BOX A S A PRECAUTION, BUT NO FAULTS FOUND. ACFT OKAY FOR SERVICE. 2 L 7 2 4F RT A35EU 20081218 NM 2008 12 18 FDEA200812145140 1 20081214 A 5311 FRAME BOEING 757 75728A 1384976 NM ZONE 100 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 912FD 24260 AFT CARGO PIT STA.1540 STR 25R FRAME HAS A MISDRILLED HOLE. REPAIRED AFT CARGO PIT STA 1540 STR 25R FRAME IAW SRM 53-00 -07 FIG 201 REPAIR 5 ZONE 1.I INSPECTION THRESHOLD 37500 FLIGHT CYCLES AFTER REPAIR INSTALLATION OR 50000 AIRFRAME FL IGHT CYCLES, WHICHEVER COMES FIRST. REPEAT INSPECTIONS , HIGH FREQUENCY EDDY CURRENT AND DETAILED INSPECTION AT 12000 FLIGHT CYCLES PER NDT, PART 6, 51-00-01. THIS IS A MAJOR AND CATEGORY "B" REPAIR. 2 L 7 2 4F RT A2NM 20081218 WP 2008 12 18 FDEA200812155142 1 20081215 A 5330 NGA6213505 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 100 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 317FE 46835 EXT FUSELAGE LWR SURFACE FOUND DEEP DENT ON SKIN 1 INCH BY 1 INCH DEEP .078 INCH. 2 L 7 3 4F RT A22WE 20081218 WP 2008 12 18 FDEA200812155143 1 20081215 A 5330 ADA74461 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 200 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 317FE 46835 DURING INSPECTION EXT FUSELAGE UPPER SURFACE FOUND DEEP DENT ON SKIN 1.50 INCH BY 1 INCH DEEP .074". 2 L 7 3 4F RT A22WE 20081218 WP 2008 12 18 FDEA200812155144 1 20081215 A 5730 NRB6225501 SKIN DOUG DC10 DC1030F 3023504 WP ZONE 500 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 317FE 46835 LT WING SLATS, FOUND CRACK AND NR 10 FASTENERS U/S ON CORNER SKIN INTERNAL SIDE SLAT NR 2. 2 L 7 3 4F RT A22WE 20081218 EU 2008 12 18 FDEA200812155145 1 20081215 A 5330 SKIN AIRBUS 300 A300B4622 3930401 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 716FD 358 EXTERNAL FUSELAGE HAS STATIC DISCHARGE AT FRAME 10, LEFT SIDE APPROX 18 INCH ABOVE THE WINDOW. BLENDED AREA IAW SRM 53- 10-12 FIG. 220 SHT 1 REMOVED DAMAGE IAW SRM 53-11-12. FABRICATED FILLER AND DOUBLER IAW SRM 53-11-12 FIG. 202 SHT 1. ALODINED IAW SRM 51-21-10 PG2. PRIMED IAW SRM 51-23-10. INSTALLED FILLER AND DOUBLER IAW SRM 53-11-12 FIG. 202 SHT 1. 2 L 7 2 4F RT A35EU 20081218 EU 2008 12 18 FDEA200812155154 1 20081215 A 5321 FXSRZ25005242GF FLOOR PANEL AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 MAIN CABIN FLOOR PANEL NR 242 GF IS DAMAGED. FABRICATED A NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED & COUNTERBORED HOLES; POTTED & SANDED EDGE; INSTALLED INSERTS; APPLIED ANTI-SKID & PART MARKED IAW DWG SRZ25-005: RE V "G". 2 L 7 2 4F RT A35EU 20081218 EU 2008 12 18 FDEA200812155155 1 20081215 A 5321 FXSRZ25005242MF FLOOR PANEL AIRBUS 310 A310203 3930313 EU FUSELAGE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 248 MAIN CABIN FLOOR PANEL NR 242 MF IS DAMAGED. FABRICATED A NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. LOCATED & COUNTERBORED HOLES; POTTED & SANDED EDGE; INSTALLED INSERTS; APPLIED ANTI-SKID & PART MARKED IAW DWG SRZ25-005: REV "G". 2 L 7 2 4F RT A35EU 20081217 NM 2008 12 17 UALA2008111303487 1 20080619 A 5320 GUARD BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 657UA 27112 MAIN CABIN FLOOR SUPPORT ANGLE SPLASH GUARD HAS CORROSION AT BS 285 AND RBL 83. REMOVED & REPLACED SPLASH GUARD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081217 2008 12 17 UALA2008121106843 4 20081211 A 2300 RADIO BOEING 737 737322 1384676 NM CFMINT CFM56 CFM563C1 13802 EU MALFUNCTIONED A UALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 WP 29 386UA 24661 RADIO PROBLEM. RTFL. 2 L 7 2 4F 4 F RT A16WE E21EU 20081217 NM 2008 12 17 UALA2008120906793 1 20081209 A 5210 2603830004 CABLE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE L3 DOOR FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 795UA 26927 DOOR 3L WOULD NOT DISARM ON ARRIVAL. DOOR DISARMED & ARMED NORMALLY AFTER 10 MINUTES. DOOR HAS HISTORY & AREA WAS LIBE RALLY COATED IN INC RELEASE & DOOR HEATER TEST NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081217 CE 2008 12 17 DXTA2008120503388 1 20081204 A 3150 WARNING LIGHT RAYTHN DH125 HAWKER800XP 7150012 CE ILLUMINATED E DXTA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 882QS 258482 YELLOW ELE"AIL" TRIM ON MAIN MASTER WARNING PANEL ILLUMINATED IN FLIGHT WHEN ELEVATOR TRIM WHEEL POSITION OUTSIDE OF TAK E OFF RANGE. 2 L 7 2 4F RT A3EU 20081217 NM 2008 12 17 DXTA2008121103396 1 20081210 A 2780 WARNING LIGHT AMD FALC50 FALCON2000 2730170 NM AUTO SLATS ILLUMINATED E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 275QS 075 ON TAKE OFF APPROX 2 SECONDS AFTER BRINGING THE THROTTLES TO TAKE OFF THE "AUTO SLATS" LIGHT ILLUMINATED. ABORTED TAKEO FF. 2 L 7 2 4F RT A50NM 20081217 CE 2008 12 17 GLBA200812151 1 20081212 A 5330 SKIN BEECH 1900 1900D 1154162 CE ZONE 100 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 21 231YV UE231 MAJOR REPAIR - DURING CONFORMITY INSPECTIONS MX DISCOVERED THE FUSELAGE SKIN ON THE LT SIDE OF THE NR 2 COMM ANTENNA TO BE CRACKED APPROXIMATELY 2.5 " IN LENGTH AT F.S. 393.25. MAINTENANCE REPAIRED CRACK ON FUSELAGE SKIN UNDER NR 2 COMM AN TENNA IAW E.O. 03-17 REV. 1. 2 L 7 2 4T RT A24CE 20081217 SO 2008 12 17 GLBA200812161 1 20081214 A 3210 LANDING GEAR EMB 120 EMB120ER 3260203 SO MALFUNCTIONED A GLBA O OTHER S AFFECT SYSTEMS LD LANDING 1 NM 21 299UX 120299 FLT NR 5148 PILOTS REPORTED THE RT MLG WOULD NOT RETRACT UPON TAKEOFF CLIMB. UPON GEAR RETRACTION THE PILOTS REPORTED THE RIGHT MAIN RED LIGHTS ON SYSTEMS A & B STAYED ILLUMINATED. PILOTS TRIED CYCLING THE GEAR A COUPLE OF TIMES WITH THE SAME RESULT. MX SERVICED HYD FLUID IAW MM 12-13. SWUNG GEAR NINE TIMES, HEATED HYDROPACKS, REMOVED DE-ICE FLUID, CLEANE D GEAR, CLEANED GEAR DOORS. ALL OPS CHECKED GOOD AND SUBSEQUENT OPS CHECK FLT SATISFACTORY. MX R & R RT MLG ACTUATOR PER EMB-120 MM 32-52. OPS CHECK GOOD. 2 L 7 2 4T RT A31SO 20081217 NM 2008 12 17 C8GA20080036 1 20080823 A 5330 SKIN BOEING 727 727223 1384074 NM BS 435 CRACKED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 29 713AA 22469 WHILE IN HEAVY MAINTENANCE PERFORMING MFEC INSPECTION OF THE LEFT #4 LAP SEAM, 2 EA CRACKS WERE NOTED AT FASTENER LOCATI ONS BS 435. THE DAMAGE WAS CUT OUT AND REMOVED. VERIFIED CRACK CONTAINMENT, FABRICATED FILLER FROM 2024 T3 .040", FABRIC ATED DOUBLER FROM 2024 T3 .050". INSTALLED REPAIR IAW B727 SRM 53-30-03. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETUR NED TO SERVICE. 2 L 7 3 4F A3WE 20081217 NM 2008 12 17 SWAA087064 1 20081211 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 231WN 32499 DURING SCHEDULED MV1 CHECK, FOUND EEPLS LIGHT LENS COVER MISSING BETWEEN ROW 1 TO ROW 5. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087092 1 20081214 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087097 1 20081214 A 5330 6545774 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED BETWEEN BS 727D TO BS 727E, STR 4L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087136 1 20081215 A 5210 6562212 SKIN BOEING 737 7373H4 1384600 NM R1 DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 380SW 26587 DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR SKIN CRACKED ABOVE UPPER HINGE CUTOUT. REPAIRED SKIN PER EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087114 1 20081214 A 3350 417N5213 COVER BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 491WN 33867 DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS LIGHT COVER LOOSE. SECURED COVER PER MM. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 UALA2008111302332 1 20080421 A 2612 473760 FIRE LOOP BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 ENGINE FAULTY A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 795UA 26927 FIRE LOOP 2 ENG R RIGHT ENGINE FIRE DETECTION SYSTEM LOOP 2 FAILURE. STATUS MSG01- ACTIVE CLIMB INTERMITTENT; FIRE LOO P 2 (RIGHT ENGINE) IS SHORTED. DB- ENGINE FIRE DETECTION CARD (RIGHT) MSG02- ACTIVE CLIMB HARD; ENGINE FIRE DETECTION C ARD (RIGHT) HAS AN INTERNAL FAILURE. DB- ENGINE FIRE DETECTION CARD (RIGHT) MSG03- ACTIVE CLIMB HARD; ENGINE FIRE DETEC TION CARD (RIGHT) HAS AN INTERNAL FAILURE. ITEM CNX PER PLF SHOWS NOT ACTIVE. MSG-2610232 ACTIVE CL INTER, MSG-2610012 ACTIVE CL HARD, MSG-2610012 ACTIVE CL HARD. FIRE LOOP FAILURE. REPLACED RIGHT ENGINE FIRE LOOP. FIRE TEST PASSED. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 NM 2008 12 18 UALA2008121106850 1 20081211 A 3350 362624 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT SEAT 56 RT INOP. RELAMPED EMERGENCY LIGHT, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081218 NM 2008 12 18 AALA200810498 1 20081216 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM BS 986 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CORROSION ON FLOORBEAM STATION 986.5 AT LEFT BUTT LINE 28. REPAIRED PER SRM 53-00-51-2R. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 AALA200810504 1 20081212 A 5320 WEB BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CORROSION AROUND RIGHT GALLEY COMPLEX MOUNT STATION 987. INSTALLED WEB REPAIR PER SRM 51-70-13. 2 L 7 2 4F RT A16WE 20081218 WP 2008 12 18 IXXA08SMN197S 1 20081024 A 5512 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C-CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER SKIN CORRODED AT STA XE 29.812 - 52.825. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN, AND STIFFENER. CLEANE D, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AT STATION XE 29.000 - 77.000 IAW FAA FORM 8110-3 NUMB ER 08548 DATED 11/18/08, DRAWING ED-4875 DATED 11/05/08, SRM 51-1-8 PAGES 17-18, SRM 55-2-0 PAGE 12, SRM 55-1-0 PAGE 1, SRM 51-1-21, SRM 51-1-8B, AND SRM 51-1-11. 2 L 7 4 4F 4A25 20081218 NM 2008 12 18 AALA200810506 1 20081215 A 5320 FLOOR SUPPORT BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CORROSION ON FLOOR SUPPORT AT STATION 310. INSTALLED A SERVICEABLE SUPPORT. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 AALA200810507 1 20081215 A 5320 ANGLE BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CORROSION ON RIGHT Z ANGLE STATION 727I TO 727J. INSTALLED A SERVICEABLE Z ANGLE PER SRM 53-00-53-2R. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 AALA200810508 1 20081215 A 5320 ANGLE BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CORROSION ON LEFT Z ANGLE STATION 787 TO 827. REPAIRED PER SRM 53-00-53-2R5. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 AALA200810499 1 20081216 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM ZONE 100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CORROSION ON FLOORBEAM STATION 986.5 AT LEFT BUTT LINE 22. REPAIRED PER SRM 53-00-51-2R. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 AALA200810509 1 20081212 A 5320 INTERCOSTAL BOEING 737 737823 13844CB NM ZONE 100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CABIN FLOOR INTERCOSTAL CRACKED STATION 321. INSTALLED A SERVICEABLE INTERCOSTAL PER SRM 51-10-2. 2 L 7 2 4F RT A16WE 20081218 WP 2008 12 18 IXXA08SMN194S 1 20081024 A 5522 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 89.719. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED EXISTING REPAIR. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE FOUND WITHIN LIMITS. MOMENT 1526.000 IN -POUND. INSTALLED REPAIR PARTS IAW SRM 55-4-1 FIGURE 1 SHEETS 1-2 ITEMS "E" AND "F", SRM 51-1-8 PAGES 17-18, SRM 55-2-0 PAGE 12, SRM 55-1-0 PAGE 1, SRM 51-1-21, SRM 51-1-9 TR NUMBER 51-142, SRM 51-1-9A TR NUMBER 51-141, SRM 51-1-8B, SRM 51 -1-11, AND SRM 51-4-4 PAGES 1-4 TR NUMBER 51-116. 2 L 7 4 4F 4A25 20081218 NM 2008 12 18 F3LA2008121600724 1 20081213 A 2611 37200101 FIRE DETECTOR AIRBUS A319 A319111 3930336 NM ZONE 200 NO TEST A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 21 904FR 9 1579 PILOT REPORTED THE NR 2 ENGINE FIRE PUSHBUTTON SWITCH LIGHT, CONTINUOUS REPETITIVE CHIME, BOTH MASTER WARNINGS AND ENGIN E CONTROL PANEL FIRE LIGHT FAIL TO TEST. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FIRE DETECTION UNIT IN ACCORD ANCE WITH AMM 26-12-34 PB401 AND PERFORMED AN OPERATIONAL CHECK. 2 L 7 2 4F RT A28NM 20081218 WP 2008 12 18 IXXA08SMN195S 1 20081024 A 5522 SKIN DOUG DC8 DC862F 3021972 WP ZONE 300 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 74.469. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDE D WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE. FOUND WITHIN LIMITS. MOMENT 1526.000 IN-POUND. INSTALLED REPAIR PARTS IAW SRM 55-4-1 FIGURE 1 SHEETS 1-2 ITEMS "E" AND "F", SRM 51-1-8 PAGES 17-18, SRM 55- 2-0 PAGE 12, SRM 55-1-0 PAGE 1, SRM 51-1-21, SRM 51-1-9 TR NUMBER 51-142, SRM 51-1-9A TR NUMBER 51-141, SRM 51-1-8B, SRM 51-1-11, AND SRM 51-4-4 PAGES 1-4 TR NUMBER 51-116. 2 L 7 4 4F 4A25 20081218 NM 2008 12 18 AALA200810501 1 20081216 A 5320 ANGLE BOEING 737 737823 13844CB NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 RIGHT TRANSITION ANGLE CORRODED STATION 767 TO 793 RIGHT BUTT LINE 21. INSTALLED A SERVICEABLE SUPPORT ANGLE PER ESO 61 000 DATED 12-12-08. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 AALA200810496 1 20081216 A 5315 FLOORBEAM BOEING 737 737823 13844CB NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CORROSION ON FLOORBEAM STATION 986.5 AT LEFT BUTT LINE 16. REPAIRED PER SRM 53-00-51-2R. 2 L 7 2 4F RT A16WE 20081218 NM 2008 12 18 AALA200810482 1 20081211 A 5320 WEB BOEING 737 737823 13844CB NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 CORROSION ON AFT GALLEY WEB STATION 1016. REPAIRED PER SRM 51-70-13. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 UALA2008121206862 1 20081212 A 7334 42D395 SWITCH BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE NR 2 ENGINE WORN A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 219UA 30551 NR 2 ENG FUEL DIFFERENTIAL SWITCH HAS WORN CONNECTOR THREADS. FOUND CONNECTOR LOOSE AND FLOATING ON WORN THREADS. INST ALLED NEW DIFFERENTIAL PRESSURE SWITCH UP TO, BUT NOT INCLUDING ITEM 3, H, (6) OF MM 73-34-01. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081219 WP 2008 12 19 FDEA200807052716 1 20080705 A 3240 BRAKE DOUG MD10 MD1010F 3022112 WP MLG FIRE A FDEA O OTHER A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 21 363FE 8178 4 48263 NR 3 BRAKE CAUGHT ON FIRE AT GATE. REMOVE AND REPLACE NR 3 BRAKE IAW MM 32-43-01-4, ALSO INSPECTED ADJACENT AREA FOR DA MAGE AND NO DAMAGE NOTED. 2 L 7 3 4F RT A22WE 20081219 NM 2008 12 19 FDEA200811295007 1 20081129 A 5343 ACA7017502 FITTING DOUG MD11 MD11F 3023600 NM ZONE 700 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 575FE 48500 RIGHT NOSE LANDING GEAR WHEEL WELL TRUNNION WEB FITTING FOUND CRACKED, CRACK LENGTH APPROXIMATELY : 1 INCH. RT NOSE LAN DING GEAR WHEEL WELL TRUNNION WEB FITTING REPAIRED AS PER SRM 53-40-00 FIGURE 23 (SHEET 1 OF 6). REPAIR CLASSIFIED MAJO R AS PER GMM 6-2-100. REPETITIVE INSPECTION REQUIRE FOR CRACK GROWTH AT NOT TO EXCEED 1500 LANDING INTERVALS. 2 L 7 3 4F RT A22WE 20081219 NM 2008 12 19 UALA2008121206864 1 20081211 A 4940 27044425 STARTER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE APU DEFECTIVE A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 782UA 26948 APU INOP, NO START ON GATE. ATTEMPTED START ON ARRIVAL. NO VOLTAGE DROP ON START, APU DOOR OPEN NORMALLY. WITH APU MA INT SWITCH IN TEST NO FAULTS ON APUC. ACPD FIM 49-40 TASK 812, CONFIRMED RELAY K24494 WORKING PROPERLY AND 28VDC ON TER MINAL E2 AT ELEC STARTER. NEED TO REPLACE ELEC STARTER. REPLACED STARTER. OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081219 NM 2008 12 19 HALA2008121700893 1 20081217 A 2697 WIRE BOEING 767 76733A 1385209 NM FIRE DETECTOR DAMAGED A HALA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 13 589HA 33422 ETOPS SIGNIFICANT SYSTEM, STATUS MSG L ENG FIRE LP1 INTERMITTENTLY COME ON. REPAIRED WIRING AT LEFT ENG UPPER AFT DETEC TOR ASSY. OPS CK OK PER FIM 26-11-00. 2 L 7 2 4F RT A1NM 20081219 NM 2008 12 19 CALA2008121401143 1 20081213 A 5610 5893543139 WINDOW BOEING 737 7373T0 1384582 NM COCKPIT FAULTY A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 27 14336 1744 1147 23574 CAPT FOUND WINDOW ARCING AND SMOKING AT POWER ATTACH POINT, TURNED OFF POWER SWITCH, POWER AND ARCING STOPPED. REMOVED AND REPLACED CAPT''S L1 WINDOW PER M/M 56-11-11. OPS CHECKS GOOD. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 CALA2008121601147 1 20081215 A 5313 143A3241 STRINGER BOEING 737 737824 13844BZ NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 24224 28933 FORWARD PIT STR 28R HAS CORROSION AROUND RIVETS FROM STATION 500C TO 500I. INSTALLED NEW STRINGER AND REPAIR SPLICES IN ACCORDANCE WITH SRM 53-00-03. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 CALA2008121601149 1 20081216 A 5320 141T5107 FLOOR SUPPORT BOEING 767 767424ER 1385270 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 66056 29451 CABIN - STATION 303 LBL 28 TO 38 FLOOR SUPPORT FOUND CORRODED. CABIN - STATION 303 LBL 28 TO LBL 38 FLOOR SUPPORT REPAI RED PER SRM 53-00-51 FIG 201, REPAIR 1 (UPR SPLICE STRAP ONLY). 2 L 7 2 4F RT A1NM 20081219 NM 2008 12 19 SWAA087148 1 20081216 A 5340 65C27314 STRINGER CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 827, STR 16R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087177 1 20081216 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087160 1 20081216 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087165 1 20081216 A 5311 6558280 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087168 1 20081216 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087147 1 20081216 A 5310 6547978 CREASE BEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 16Y CHECK, FOUND CREASE BEAM CORRODED AT L2 DOOR, BETWEEN BS 950 TO BS 990. REMOVED AND REPLACED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087158 1 20081216 A 5311 6546555 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087159 1 20081216 A 5311 6546558 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087216 1 20081215 A 5610 141A481014 WINDOW BOEING 737 73776Q 13845AA NM COCKPIT ARCED A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 550WN 30279 L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087181 1 20081216 A 5315 6546804 FLOORBEAM BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 685, RBL .07. REPAIRED BEAM PER EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087193 1 20081216 A 5330 6545768 SKIN BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED AT BS 360, STR 26L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087195 1 20081216 A 5322 6546546 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 727B, BETWEEN STR 20R TO STR 21R. REMOVED AND REPLACED SHEAR TIE PER SRM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 FDEA200812125129 1 20081212 A 5330 6554583138 SKIN BOEING 727 727233 138408A NM ZONE 100 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 276FE 22041 SKIN BULGING AND CRACKED STA 1010 STR 27L CUT DAMAGE AREA IAW SRM 53-30-3 , FIG 3A. FABRICATED FILLER AND DOUBLER IAW SRM 53-30-3 FIG 3A. TREATED & PRIMED REPAIR PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 20081217 NM 2008 12 17 SWAA087089 1 20081213 A 3350 417A56014 SIGN BOEING 737 7377H4 1384404 NM CABIN LOOSE A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 902WN 36615 EMERGENCY EXIT SIGN LOOSE AT L1 DOOR. REMOVED AND REPLACED SIGN PER MM. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087104 1 20081215 A 5311 6546596 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087133 1 20081215 A 5330 6545768 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 317WN 24068 DURING SCHEDULED SPV CHECK, FOUND SKIN CRACKED AT BS 693, STR 4L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081217 NM 2008 12 17 SWAA087125 1 20081215 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 378SW 26585 DURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727A, RBL 24, WL 208. REPAIRED BEAM PER ER. 2 L 7 2 4F RT A16WE 20081218 EU 2008 12 18 UALA2008120906799 1 20081208 A 2597 CONNECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE PAX DOOR DISCONNECTED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 474UA 1475 LT AFT CABIN DOOR SLIDE CONNECTOR BETWEEN CABLE LOOP ASSY AND COVER RELEASE CABLE WAS FOUND DISCONNECTED. CABLE LOOP AS SY & COVER RELEASE CABLE CONNECTED. 2 L 7 2 4F 4 F RT A28NM E40NE 20081218 NM 2008 12 18 UALA2008111306188 1 20081020 A 3350 POWER SUPPLY BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 569UA 26677 EMERGENCY LIGHT PROBLEM DISCOVERED ON 1SV. REPLACED POWER SUPPLY M10818, M10817 AND BATTERY PACKS FOR BOTH POWER SUPPLI ES. 2 L 7 2 4F 4 F RT A2NM E17NE 20081218 NM 2008 12 18 UALA2008111303920 1 20080722 A 2161 8102003 CONTROLLER BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CABIN FAILED A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 216UA 30549 TRIM AIR PRSOV R RIGHT TRIM AIR PRESSURE RELIEF SHUTOFF VALVE (PRSOV) FAILED. STATUS MSG-2124202 ACTIVE CL MODE. REPLA CED CTC-R AND OP CHK'D. ALSO REPLACED COND TEMP SENSOR R AND OPERATED PACK. ALL INDICATIONS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 NM 2008 12 18 UALA2008111305786 1 20080916 A 2842 1833KTU01 PROBE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE CENTER TANK FAULTY A UALA O OTHER W J INADEQUATE Q C WARNING INDICATION CR CRUISE 1 WP 29 785UA 26954 RECEIVED UNBALANCED FUEL EICAS TWICE WITH FAULTY R FUEL QUANTITY. REPLACED LEFT CTR TANK PROBE NR 2. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 NM 2008 12 18 UALA2008111305487 1 20080826 A 2120 UNKNOWN BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE AFT GALLEY SMOKE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 29 171UA 24322 SMOKE APPEARED IN AFT GALLEY. PER FLIGHT ATTENDANT, SAW A SLIGHT AMOUNT OF SMOKE COMING FROM AREA NEAR AFT LEFT COFFEE WARMER. OPERATED ALL AFT GALLEY EQUIPMENT. CHECKED AREA. NO SMOKE DETECTED. GALLEY 428 NR 181 GETS TOO HOT. OPS OK. NO OTHERS DEFECTS NOTED. 2 L 7 4 4F 4 F RT A20WE E24NE 20081218 NM 2008 12 18 UALA2008121206859 1 20081211 A 3350 767 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 660UA 27115 DOOR L1 AND R1 UPPER EMERGENCY EXIT DOOR HANDLE ILLUMINATION PORTION IS INOP. REPLACED EMERGENCY EXIT LIGHT ASSY FOR DO OR R1 AND RELAMPED DOOR L1, TESTED GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 EU 2008 12 18 UALA2008121006837 1 20081209 A 5320 PLATE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 405UA 452 ONE EA FLOORBOARD CONNECTOR PLATE CORRODED AT FRAME 68. MAJOR REPAIR ACCOMPLISHED. REPLACED PLATE AT FRAME 68. 2 L 7 2 4F 4 F RT A28NM E40NE 20081219 NM 2008 12 19 FDEA200811184926 1 20081118 A 2750 AYG70305511 VALVE DOUG MD11 MD11F 3023600 NM TE FLAPS FAILED A FDEA J A DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 CE 21 579FE 48470 ACFT HAD AN ATB FOR FLAPS SLOW TO RETRACT AND ON GROUND FLAPS ARE STUCK AT 28 DEG. REMOVED AND REPLACED FLAP LIMITER DU PLEX ACTUATOR, IAW AMM 27-56-01-4. REMOVED AND REPLACED INBOARD FLAP CONTROL VALVE IAW AMM 27-52-03-4. REMOVED AND REP LACED SYS 2 INLINE RESTRICTOR VALVE IAW AMM 27-52-09-4. 2 L 7 3 4F RT A22WE 20081219 NM 2008 12 19 CALA2008121401145 1 20081213 A 5315 BAC14902887T6 FLOORBEAM BOEING 737 737924 13848A1 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 27 79402 30119 FLOORBEAM CORROSION AT NUT PLATE HOLE, STA 986.5 RBL 29, FOUND OUT OF LIMITS. INSTALLED REPAIR PER ECRA 5321-0129. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087166 1 20081216 A 5311 6546555 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087150 1 20081216 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 465WN 33829 DURING SCHEDULED HC1 CHECK, LT AFT EMERGENCY BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER M M. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087194 1 20081216 A 3350 300432 LENS BOEING 737 737317 138447P NM EXTERIOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND EXTERNAL EMERGENCY EXIT LIGHT LENS CRACKED AT BS 727D, BETWEEN STR 22L TO STR 23L. RE MOVED AND REPLACED LIGHT ASSY PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087151 1 20081216 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 465WN 33829 DURING SCHEDULED HC1 CHECK, RT AFT EMERGENCY BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER M M. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 HALA2008121400890 1 20081214 A 2421 IDG BOEING 767 76733A 1385209 NM LEFT UNDERSERVICED A HALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 581HA 28141 ETOPS SIGNIFICANT SYSTEM, EICAS MX LEVEL MSG L IDG OUT TEMP DISPLAYED AT TOP OF CLIMB. IDG OUT 86, 115 IDG RISE 10,11. FOUND LEFT IDG UNDERSERVICED. SERVICED IDG, TO INSP IDG NO LEAKS NOTED. T/S PER FIM 24-20-00. NO FAULTS ON BPCU BITE . 2 L 7 2 4F RT A1NM 20081219 NM 2008 12 19 HALA2008120700879 1 20081207 A 2841 INDICATOR BOEING 767 767332 1382001 NM FUEL QTY INOPERATIVE A HALA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 WP 13 594HA 23275 OPEN - ETOPS SIGNIFICANT SYSTEM, ATB RT FUEL TANK AND TOTAL FUEL QTY INDICATORS BLANK, EICAS MSG FUEL QTY IND NOT DISPL AYED. AIR TURN BACK TO LAX. REPAIR IN WORK. 2 L 7 2 4F RT A1NM 20081219 NM 2008 12 19 QXEA2008121201237 1 20081211 A 3350 6138001 BATTERY BOMBDR DHC8 DHC8402 1390042 NM EMERGENCY LIGHTS FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 405QX 4047 PDX - AFT EMERGENCY CEILING LIGHT IS INOP. REPLACED THE POWER SUPPLY UNITS IAW AMM 33-51-301-000-801 AND 33-51-01-400-8 01. CHECKS GOOD. 2 H 7 2 4T RT A13NM 20081219 NM 2008 12 19 SWAA087189 1 20081216 A 5322 6546529 SHEAR TIE BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 500D, BETWEEN STR 25R TO STR 26R. REMOVED AND REPLACED SHEAR TIE PER ER. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087205 1 20081217 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087223 1 20081216 A 3350 D71701100 BATTERY PACK BOEING 737 7377H4 1384404 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 29 790SW 30604 DURING SCHEDULED 8Y CHECK, FOUND FWD RT EMERGENCY BATTERY PACK INOP. REPLACED BATTERY PACK PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 QXEA2008121701247 1 20081215 A 3110 DSC5431 LIGHT BOMBDR DHC8 DHC8402 1390042 NM INSTRUMENT PANEL FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 402QX 4032 PDX - BETA LIGHT REQUIRES REPLACEMENT DUE TO LOW INTENSITY LEVEL, TASK CARD 335000204-60368. REPLACED BETA LIGHT. CHEC KS GOOD. 2 H 7 2 4T RT A13NM 20081219 NM 2008 12 19 SWAA087224 1 20081217 A 5312 6517853 BULKHEAD BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 368SW 26579 DURING SCHEDULED SPV CHECK, FOUND VERTICAL BEAM WEB CRACKED AT WL 180, LBL 5.7, BS 178. REPAIRED WEB PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087235 1 20081217 A 5330 6562212 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED 14Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087192 1 20081216 A 5330 6545765 SKIN BOEING 737 737317 138447P NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 686SW 23175 DURING SCHEDULED SPV CHECK, FOUND SKIN CORRODED AT BS 540, STR 26L. REPAIRED SKIN PER ER. 2 L 7 2 4F RT A16WE 20081219 SO 2008 12 19 CHQA200800246 1 20081212 A 3240 9067404 VALVE EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL MLG BRAKE ASSY FALSE INDICATION A CHQA O OTHER J WARNING INDICATION CR CRUISE 1 GL 11 273SK 21353 21353 145331 CAE311926 IN FLIGHT THE CREW RECEIVED THE BRAKE ON INDICATION LIGHT. THEY PROCEEDED TO THE FINAL DESTINATION AND LANDED WITHOUT I NCIDENT. THE PARKING BRAKE VALVE WAS REMOVED AND REPLACED IAW AMM 32-44-01 AND OPERATIONALLY CHECKED OK. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081219 EA 2008 12 19 CHQA200800243 1 20081210 A 2750 FLAP SYSTEM CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE TE FLAPS MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 11 467CA 7637 GEE873361 FLIGHT 5637, IAH TO ELP - DURING FINAL SEGMENT OF CLIMB THE FLIGHT CREW RECEIVED A FLAP FAIL MESSAGE ON EICAS. THE FLAP S WERE AT ZERO AND WERE INDICATING ZERO AT THE TIME. THE QRH WAS FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MA INTENANCE CHECKED THE FECU FOR FAULT CODES AND FOUND CODES FOR RT BPSU, FECU, AND WIRING FOR THE RT BPSU. THE SYSTEM WA S RESET AND THE FLAPS OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 20081219 NM 2008 12 19 UALA2008121506877 1 20081213 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 554UA 26644 AFT CARGO COMPARTMENT, FRAME DENTED BS 1380, STR 25L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081219 NM 2008 12 19 UALA2008121506878 1 20081213 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 554UA 26644 AFT PIT FRAME DENTED BS 1400, STR 26L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBL ER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081219 SO 2008 12 19 CHQA200800249 1 20081215 A 2611 FIRE DETECTOR EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL CARGO BAY MALFUNCTIONED A CHQA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 11 296SK 145514 CAE311697 FLIGHT 5938, STL TO CLE - THE FLIGHT CREW RECEIVED A BAGGAGE SMOKE MESSAGE DURING CRUISE. THE QRH WAS FOLLOWED AND BOTH CARGO COMPARTMENT FIRE BOTTLES WERE DISCHARGED. THE ACFT LANDED WITHOUT INCIDENT IN IND. THE CARGO COMPARTMENT WAS IN SPECTED WITH NO SIGNS OF SMOKE OR FIRE. THE SMOKE DETECTION SYSTEM WAS TESTED WITH NO DEFECTS NOTED AND THE CARGO FIRE BOTTLES WERE PLACED ON MEL. BOTH BOTTLES WERE REPLACED LATER ON THE 15TH IN CLE. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081219 SO 2008 12 19 CHQA200800250 1 20081216 A 3350 RPS1B BATTERY PACK EMB 145 EMB145LR 3260212 SO ALLSN AE3007 AE3007A 03030 GL BATTERY PACK DISCHARGED A CHQA K NONE L NO TEST IN INSP/MAINT 1 GL 11 570RP 13752 170 145821 CAE312340 DURING INSPECTION BOTH THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS WERE INOP. THE NR 4 EMERGENCY LIGHT BATTERY PACK WA S REPLACED AND THE SYSTEM OPERATED NORMALLY. 2 L 7 2 4T 4 F RT T00011AT TE6CH 20081219 NM 2008 12 19 HALA2008121200886 1 20081212 A 2120 UNKNOWN BOEING 717 717200 1383700 NM CABIN ODOR A HALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 486HA 55130 BTB - UPON TAXI OUT F/A REPORT SMOKE IN CABIN WITH ODOR. POSSIBLE ELECTRIC. ACCOMPLISHED INSPECTION PER AMM 21-00-00-7 10-805, 803 AND 801 NO SMOKE IN CABIN OR ODOR. NO ELECTRICAL ODOR NOTED, CABIN ELECTRICAL SYS CHECK OK. APU AND ENG RU N FOR AIR CONDITION CHECK, OK FOR SERVICE. 2 L 7 2 4F TR A6WE 20081219 NM 2008 12 19 UALA2008121506884 1 20081213 A 2611 69B635871 TUBE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SMOKE DETECTOR DAMAGED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 554UA 26644 FWD PIT SMOKE DETECTOR TUBE CUT AND DETERIORATED STA 640, RBL 20. LOCATION LWR PART OF UPPER FLOORBEAM. INSTALLED NEW SMOKE DETECTOR TEE TUBE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081219 SO 2008 12 19 SWIA200820638 1 20081214 A 3210 LANDING GEAR EMB 120 EMB120ER 3260203 SO HUNG UP A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 569SW 120344 FLT 7779 - LANDING GEAR WOULD NOT COME UP ON FIRST ATTEMPT. OPERATION CHECKS NORMAL. 2 L 7 2 4T RT A31SO 20081219 EA 2008 12 19 SWIA200820639 1 20081211 A 5730 SKIN CNDAIR CL600 CL6002B19 1900309 EA RT WING DENTED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 405SW 7029 FLT 1010 - TWO DENTS ON RIGHT LEADING EDGE AT WS 201.0 EXCEED LIMITS OF SRM. REPLACED LEADING EDGE SKIN PER SRM. 2 L 7 2 4F RT A21EA 20081219 EA 2008 12 19 SWIA200820640 1 20081211 A 5210 ROLLER CNDAIR CL600 CL6002B19 1900309 EA DOOR HANDLE DIRTY A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 952SW 7805 FLT 59009 - BOTH MAIN CABIN AND SERVICE DOORS DIFFICULT TO OPEN. CLEANED FOD FROM SERVICE DOOR SEAL, CLEANED AND LUBED MCD HANDLE ROLLER. 2 L 7 2 4F RT A21EA 20081219 WP 2008 12 19 IXXA08SMN196S 1 20081024 A 5512 565174758 SKIN DOUG DC8 DC862F 3021972 WP HORIZONTAL STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 SW 11 71CX 72846 2844 45961 DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE UPPER SKIN CORRODED AT STATION XE 29. 812. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. CLEANED, TREATED, PRIMED AREA. INSTALLED NEW SKI N IAW SRM 55-3-1 FIGURE 1 SHEETS 1-2, SRM 51-1-8 PAGES 17-18, SRM 55-2-0 PAGE 12, SRM 55-1-0 PAGE 1, SRM 51-1-21, AND SR M 51-1-8B. 2 L 7 4 4F 4A25 20081219 NM 2008 12 19 UALA2008121506891 1 20081213 A 4950 32908145 VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU MALFUNCTIONED A UALA O OTHER J WARNING INDICATION UK UNKNOWN 1 WP 29 773UA 26929 APU STATUS MSG. REPLACED APU SURGE VALVE. APU OPS NORMAL. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081219 CE 2008 12 19 DXTA2008121703405 1 20081216 A 3150 WARNING LIGHT CESSNA 500 550 2076604 CE INTERMITTENT E DXTA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 07 843QS 5600790 DURING TAKEOFF ROLL WINDSHIELD OVERHEAT MOMENTARILY ILLUMINATED. 1 L 7 2 4F A22CE 20081219 CE 2008 12 19 GLBA200812171 1 20081216 A 5347 SEAT TRACK BEECH 1900 1900D 1154162 CE BS 160-164 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 21 231YV UE231 MAJOR REPAIR - LT CENTER SEAT TRACK SUPPORT TAB IS BROKEN OFF FROM SEAT TRACK AT F.S.160 TO F.S. 164. MAINTENANCE REPAI RED THE LEFT HAND CENTER SEAT TRACK SUPPORT TAB AT F.S. 162 TO F.S. 164 IAW SRM 53-90. RII INSPECTION COMPLIED WITH PE R TASKCARD 8.2.1. 2 L 7 2 4T RT A24CE 20081222 WP 2008 12 22 UPS08854189 1 20081205 A 5313 DC853B0097 LONGERON DOUG DC8 DC873F 302199F WP FUSELAGE CUT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP AFTER REMOVAL OF REPAIR DOUBLER SEQ 803-F1-15, FOUND L26L WITH DEEP CUT AT FS 398. CUT OUT DAMAGED L ONGERON AND INSTALLED REPAIR SPLICE IAW SRM 53-2-2 FIG 10, 51-1-24, 51-1-20D. 2 L 7 4 4F RT 4A25 20081222 2008 12 22 UPS08154192 4 20081209 A 2565 WARNING SYSTEM AIRBUS A300 A300F4622R 3930360 EU EVAC SLIDE INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 148UP 0831 INSPECTION TYPE:N/A EVACUATION SLIDE RELEASE WARNING INOP (BUZZER IS OPERATIVE). PERFORMED TSM - RESET CONNECT TO AUTON OMOUS POWER SUPPLY. ACCOMPLISHED EVAC SLIDE WARNING TEST WITH REFERENCE TO A300 MM 52-73-00-05. REF LP 163490. 2 L 7 2 4F RT A35EU 20081222 EU 2008 12 22 UPS08154194 1 20081212 A 3350 LIGHT AIRBUS A300 A300F4622R 3930360 EU COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 160UP 0005 INSPECTION TYPE:N/A LAMP INOP IN GLARESHIELD EMERGENCY LIGHT. RELAMPED EMERGENCY, OPS CHECK GOOD. 2 L 7 2 4F RT A35EU 20081222 WP 2008 12 22 UPS08854170 1 20081014 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-40 AT FS 1200-1218 L1-4R HAS SRM REF 53-02-01 FIG 7 SHEET 11 IS A CAT B REPAIR . REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854171 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-70 AT FS 1376.5-1379.5 L19-20L HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854173 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-72 AT FS 1406 L20-21L HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTALLE D REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11. 2 L 7 4 4F RT 4A25 20081222 2008 12 22 DXTA2008120903394 1 20081208 A 5100 UNKNOWN CESSNA UNKNOWN E DXTA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 07 369QS 6800081 AFTER LANDING GEAR RETRACTION 8-10 LOUD BANGS WERE HEARD & VIBRATIONS WERE FELT IN THE COCKPIT FLOOR. 20081219 CE 2008 12 19 GLBA200812172 1 20081216 A 5347 SEAT TRACK BEECH 1900 1900D 1154162 CE BS 187-190 CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 NM 21 231YV UE231 MAJOR REPAIR - LT CENTER SEAT TRACK SUPPORT TAB IS BROKEN OFF FROM SEAT TRACK AT F.S. 187.5 TO 190.5. MAINTENANCE REPAI RED LEFT CENTER SEAT TRACK SUPPORT TAB AT APPROXIMATELY F.S. 189 TO 191 IAW SRM 53-90. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1. 2 L 7 2 4T RT A24CE 20081219 NM 2008 12 19 UALA2008121506868 1 20081212 A 3350 767 LAMP BOEING 767 76731B 1385190 NM PWA 4060 PW4060 52119 NE EMERGENCY LIGHT INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 660UA 27115 AFT LT EXTERIOR EMERGENCY LIGHT AT DOOR 4L IS INOP. RELAMPED AND RESEALED AND OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081219 NM 2008 12 19 UALA2008121506869 1 20081212 A 3350 8200009007 SIGN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 LT FWD AISLE EXIT SIGN FAILS LIGHT COMPARATOR TEST. INSTALLED NEW EXIT SIGN. 2 L 7 2 4F 4 F RT A1NM E24NE 20081219 NM 2008 12 19 UALA2008121506870 1 20081212 A 3350 8200009007 SIGN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 LT AFT AISLE EXIT SIGN FAILS COMPARATOR TEST. INSTALLED NEW EXIT SIGN AND OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081219 NE 2008 12 19 22AA20081202 2 20081211 A 7200 CF650C2 ENGINE DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 1 FAILED A 22AA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 29 524MD 92266 15136 46999 455468 ON TAKEOFF AT 800FT NR 1 ENGINE FAILED. ENGINE REPLACEMENT IN PROGRESS. ACCOMPLISHED RED BORDER 025093. REMOVED AND R EPLACED NR 1 ENGINE IAW WORK CARD 141R7101M, PERFORMED ENGINE RUN UP IAW MM 71-00-00, 71-06-00; OPERATION NORMAL, NO LEA KS NOTED. 2 L 7 3 4F 4 F RT A22WE E23EA 20081219 EU 2008 12 19 RMXA2008121518093 1 20081215 A 2697 CONNECTOR BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE FIRE DETECTION DIRTY E RMXA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 05 117NG 7083 LE45032 THE NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED. ENGINES WERE OPERATING NORMALLY. FLIGHT NURSE AND PILOT NOTICED A SLIG HT BURNING SMELL. DISCHARGED THE NR 2 ENGINE FIRE BOTTLE INTO THE NR 2 ENGINE. THE NR 2 ENGINE FIRE WARNING LIGHT REMAI NED ILLUMINATED. DISCHARGED THE NR 1 ENGINE FIRE BOTTLE INTO THE NR 2 ENGINE. THE PILOT TURNED TO THE NEAREST AIRPORT K SFQ, DECLARED AN EMERGENCY WITH APPROACH AND LANDED UNEVENTFUL. EMERGENCY SHUTDOWN AND EVACUATION WAS UNEVENTFUL. POST FLIGHT INSPECTION DID NOT INDICATE ANY FIRE DAMAGE TO THE ENGINE COMPARTMENT. INSPECTION OF ENGINE DID NOT REVEAL SIGNS OF FIRE OR OVERHEATING. PERFORMED FIRE INDICATING FUNCTIONAL CHECKS IAW MM 706-3. REPLACED FIRE EXTINGUSHER BOTTLES AN 1 G 7 2 3U 3 U H13EU E5NE 20081219 CE 2008 12 19 DXTA2008120803390 1 20081206 A 2731 TRIM SYSTEM CESSNA 560 560XL 2076702 CE ELEVATOR STUCK E DXTA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 07 692QS 5605092 THE ELEVATOR TRIM JAMMED AFTER TAKE OFF. 2 L 7 2 4F RT A22CE 20081219 CE 2008 12 19 DXTA2008120803391 1 20081207 A 2120 UNKNOWN CESSNA 750 750 2076810 CE CABIN ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 918QS 7500223 WHEN COCKPIT PAC SUPPLY TEMP INCREASED ABOVE 130 DEGREES THERE WAS A STRONG PETROLEUM TYPE ODOR. 2 L 7 2 4J RT T00007WI 20081219 SO 2008 12 19 FDKA2008121600315 1 20081216 A 3397 CONNECTOR EMB 145 EMB145LR 3260212 SO CABIN LOOSE A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 838MJ 145384 FRL FLT 6215 JFK-ORF - ROW 12 CEILING AFT EMERGENCY LIGHT INOP. MX RE-SECURED LIGHT ASSY CONNECTORS AND RESET SYSTEM, O PS CHECK GOOD. 2 L 7 2 4T RT T00011AT 20081219 SO 2008 12 19 FDKA2008121400312 1 20081214 A 3350 20131A BATTERY EMB 145 EMB145LR 3260212 SO CABIN DISCHARGED A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 857MJ 145765 FRL FLT 6260 PIT - AC EMERGENCY LIGHTS WILL NOT ILLUMINATE. MX REMOVED AND REPLACED EMERGENCY BATTERIES. 2 L 7 2 4T RT T00011AT 20081219 SO 2008 12 19 FDKA2008121400313 1 20081214 A 3350 1317 LIGHT EMB 145 EMB145LR 3260212 SO CABIN INOPERATIVE A FDKA K NONE O OTHER NR NOT REPORTED 1 SW 07 845MJ 145502 FRL FLT 6274 JFK - RT EMERGENCY EXIT MARKER NOT ILLUMINATING. MX RELAMPED, OPS GOOD. 2 L 7 2 4T RT T00011AT 20081218 NM 2008 12 18 UALA2008120906789 1 20081208 A 3350 15AT48 SWITCH BOEING 737 737522 138449F NM CFMINT CFM56 CFM563C1 13802 EU EMERGENCY LIGHTS FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 929UA 26652 EMER EXIT LIGHTS ARE ILLUMINATED GATE WITH GROUND POWER. EMERGENCY LIGHTS WORK NORMAL IN THE ARM AND ON POSITION, LIGHTS REMAIN ON IN THE OFF POSITION, SUSPECT BAD SWITCH. REPLACED S7 EMERGENCY LIGHT SWITCH. 2 L 7 2 4F 4 F RT A16WE E21EU 20081218 NM 2008 12 18 UALA2008120906791 1 20081209 A 3350 3071BPEGPL LAMP BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 218UA 30222 SEAT 32G AISLE EMERGENCY LIGHT INOP. REPLACED LAMP. OPS CHECKED OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 NM 2008 12 18 UALA2008120906792 1 20081209 A 3350 3071BPEGPL LAMP BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE EMERGENCY LIGHTS INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 218UA 30222 SEAT 36G AISLE EMERGENCY LIGHT INOP. REPLACED LAMP. OPS CHECKED OKAY. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 2008 12 18 UALA2008111303704 4 20080703 A 3417 S242T210211 ADC BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE COCKPIT FAULTY A UALA A UNSCHED LANDING W INADEQUATE Q C CR CRUISE 1 WP 29 662UA 27159 CAPT AIR SPEED ALTIMETER & VSI FAILED. RTFL. FOUND FAULTY ADC. REPLACED CAPTAIN'S AIR DATA COMPUTER & REPLACED CABIN PRESSURE CONTROLLER 1. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 UALA2008111306209 1 20081019 A 3350 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXTERIOR INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 548UA 25396 DOOR 4R EMERGENCY LIGHT OUT - OUTSIDE. RELAMPED EMERGENCY EXIT LIGHT AT R4 DOOR AND OPS CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081218 EU 2008 12 18 UALA2008120906802 1 20081209 A 5320 BEAM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 405UA 452 BEAM 200 HAS SEVERAL PLACES CORRODED. MAJOR REPAIR ACCOMPLISHED. CONNECTED NEW BEAM 200 TO NEW BEAM 205. INSTALLED BE AM 200 IN ACFT. 2 L 7 2 4F 4 F RT A28NM E40NE 20081218 2008 12 18 UALA2008120906814 4 20081209 A 2565 C17638109 BOTTLE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EVAC SLIDE FAULTY A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 660UA 27115 LT OVERWING SLIDE BOTTLE CABLE BALL IS BELOW RETAINING CLIP. REPLACED SLIDE BOTTLE, PRESSURE CHECKED GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 20081218 NM 2008 12 18 UALA2008121106849 1 20081211 A 3350 362624 LAMP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 197UA 26901 EMERGENCY LIGHT SEAT 5F FWD INOP. RELAMPED EMERGENCY LIGHT, CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 20081218 NM 2008 12 18 UALA2008111305578 1 20080903 A 2611 SMOKE DETECTOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE E&E BAY FAULTY A UALA O OTHER W N INADEQUATE Q C FALSE WARNING IN INSP/MAINT 1 WP 29 771UA 26932 CHANNEL 1 E-E SMOKE DETECTOR EICAS MESSAGE. REPLACED E-E COOLING SMOKE DETECTOR. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081218 NM 2008 12 18 AALA200810483 1 20081211 A 5320 FLOOR SUPPORT BOEING 737 737823 13844CB NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 FLOORBOARD SUPPORT CORRODED FORWARD RIGHT AFT GALLEY DOOR CUTOUT STATION 947.5 TO 976 RIGHT BUTT LINE 52. INSTALLED A S ERVICEABLE AFT GALLEY DOOR CREASE ANGLE PER SRM 51-10-02-0G. 2 L 7 2 4F RT A16WE 20081219 EU 2008 12 19 FDEA200812155167 1 20081215 A 5347 A5381192320601 SEAT TRACK AIRBUS 310 A310203 3930313 EU FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 428FE 38333 248 THE MAIN CABIN SEAT TRACK IS CORRODED BETWEEN FRAME 46 AND FRAME 47/48 RBL 37. SEAT TRACK REPLACED ON NON-ROUTINE CARD N01243. 2 L 7 2 4F RT A35EU 20081219 NM 2008 12 19 SWAA087167 1 20081216 A 5311 6546557 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 887, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087170 1 20081216 A 5315 6546804 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 371SW 26598 DURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 18. REPAIRED BEAM PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087182 1 20081216 A 5311 6546554 FRAME BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND FRAME CRACKED AT BS 847, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087206 1 20081217 A 5311 6546593 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 604SW 27955 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087152 1 20081215 A 5610 141A481014 WINDOW BOEING 737 73776Q 13845AA NM COCKPIT ARCED A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 550WN 30279 L2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087234 1 20081217 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, STR 26L. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087149 1 20081216 A 5311 65C25229 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 642WN 27715 DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 727D, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 EA 2008 12 19 CHQA200800248 1 20081213 A 3260 TARGET CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343B1 30070 NE PROX SENSOR OUT OF ADJUST A CHQA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 11 458CA 7613 GEE873283 ON TAKEOFF FROM BRO WHEN THE LANDING GEAR WAS SELECTED "UP" THE EICAS DISPLAYED "LNDG GEAR DISAGREE" MESSAGE FOLLOWED BY "NOSE GEAR DOOR" MESSAGE. THE QRH WAS FOLLOWED AND THE GEAR WAS LOWERED AND THE MESSAGES CLEARED. THEY THEN RETURNED TO BRO AND PERFORMED A LOW PASS SO THE TOWER COULD VERIFY ALL GEAR DOWN. PROCEEDED TO LAND NORMALLY. THE ACFT WAS FERR IED TO IAH AND MAINTENANCE TROUBLESHOT THE SYSTEM. THEY READJUSTED THE PROX SWITCH TARGET FOR PROX SWITCH 14GA AND THE SYSTEM CHECKED NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 20090108 NM 2009 1 8 FDEA200812195244 1 20081219 A 5311 FRAME BOEING 727 727233 138408A NM ZONE 100 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 CE 21 277FE 22042 CORROSION ON FRAME REPAIR 1070 AND 27L REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATE REPAIR PART, IAW SRM 53-10-2 FIG 5, AND 54-40-3 FIG 1. HEAT TREATED IAW ER 2-37153-801 REV A. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW FR AME REPAIR IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 20081219 NM 2008 12 19 QXEA2008121501240 1 20081210 A 2720 3995001007 FEEL UNIT BOMBDR DHC8 DHC8402 1390042 NM RUDDER MALFUNCTIONED A QXEA O OTHER F FLT CONT AFFECTED AP APPROACH 1 NM 19 405QX 18524 4047 PDX - CAPTAINS AND FO'S RIGHT RUDDER PEDAL'S STICKY. REMOVED AND INSTALLED SERVICEABLE RUDDER FEEL SUMMING UNIT IAW AMM TASK 27-22-06-000-801 AND 27-22-06-400-801. PERFORMED RUDDER CONTROL SYS RIG CK IAW Q400 AMM TASK 27-21-00-830-810/ 27 -21-00-830-811/ 27-21-00-830-812/ AND OKS CK 27-20-00-710-802, RIG AND OP CK GOOD. COMPLETED FREEDOM OF MOVEMENT CHECK, ENSURED FULL TRAVEL AND VERIFIED PROPER DIRECTION OF MOVEMENT, NO DEFECTS NOTED. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081219 NM 2008 12 19 QXEA2008121501239 1 20081212 A 5230 502213 SEAL BOMBDR DHC8 DHC8402 1390042 NM CARGO DOOR FAILED A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 19 403QX 4037 BOI - CABIN RATE WENT FROM 500 FPM TO 3000 FPM WHILE CLIMBING THRU 13,000 SELECTED MANUAL INCR RATE WENT TO 3000 FPM DOW N FOR A FEW SECONDS THEN BACK TO 3000 FPM CLIMB KEPT OSCILLATING UP AND DOWN THEN WENT BACK TO AUTO AND SYSTEM STABILIZE D. RETURNED TO BOI FOR MTX. REMOVED AND REPLACED CARGO DOOR SEAL IAW AMM 52-31-26-001-400-801. NO FURTHER DEFECTS NOT ED CHECKS GOOD. RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 20081219 NM 2008 12 19 UALA2008121506879 1 20081213 A 5210 STRUCTURE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L2 DOOR DAMAGED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 554UA 26644 DOOR L2 REQUIRES REPAIR DOUBLER AT UPPER HINGE CUTOUT. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR AT UPPER HI NGE CUTOUT. 2 L 7 2 4F 4 F RT A2NM E17NE 20081219 NM 2008 12 19 UALA2008121506882 1 20081213 A 5311 FRAME BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 554UA 26644 AFT PIT FRAME DENTED BS 1460, STR 26L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBL ER REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 20081219 NM 2008 12 19 UALA2008121506893 1 20081214 A 3220 65B825854 ACTUATOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NLG ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 121UA 29167 A 'GEAR DISAGREE' MSG WITH ASSOCIATED 'GEAR DOOR' EICAS. DURING GEAR SWING WITH WLG & BDG PINNED. NLG UP & LOCKED NORMA LLY BUT WHEN SWINGING ALL GEARS (NOT PINNED) THE NLG WILL NOT RETRACT FULLY. SUSPECT NOSE-BODY LANDING GEAR SELECTOR VL V AT FAULT. REPLACED NLG RETRACT ACTUATOR AND NLG LOCK. OPS CHK NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 20081219 NM 2008 12 19 UALA2008121506871 1 20081212 A 3350 8200009007 SIGN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN FAULTY A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 660UA 27115 RT AISLE EXIT SIGN FAILS LIGHT COMPARATOR TEST. INSTALLED NEW SIGN. 2 L 7 2 4F 4 F RT A1NM E24NE 20081219 NM 2008 12 19 ABXA200812120269 1 20081210 A 3230 AS46246026455 HOSE BOEING 767 767281 1385109 NM RT DRAG BRACE DEFECTIVE A ABXA A UNSCHED LANDING O OTHER TO TAKEOFF 1 GL 23 783AX 23016 AFTER TAKEOFF, LEFT GEAR WOULD NOT RAISE WITH ASSOCIATED EICAS "DISAGREE" MSG 2 UP-TO-OFF CYCLES WITH NO CHANGE. REPLAC ED DRAG BRACE ACTUATOR HOSES. PERFORMED GEAR SWING OF ALL GEAR. LEAK & OPS CHECK GOOD. LEFT GEAR CYCLES UP & DOWN, IN DICATION NORMAL. RESET LEFT MAIN GEAR TRACK POSITION FUSES, GEAR UP & GEAR DOWN FUSES. 2 L 7 2 4F RT A1NM 20081219 SO 2008 12 19 C2XA08SH156 1 20081218 A 5320 14521700007 FLOOR SUPPORT EMB 145 EMB145XR 3260214 SO ZONE 100 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27190 14500934 SHV DURING C-CHECK LT OMEGA BEAM FRM 20 SIDE WALL CORRODED. MX REPAIRED LT OMEGA BEAM FRM 20 SIDE WALL IAW SRM 53-10-00 . THE ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081219 SO 2008 12 19 C2XA08SH157 1 20081218 A 5720 C510 PLATE EMB 145 EMB145XR 3260214 SO ZONE 600 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 27 27190 979 14500934 SHV DURING C-CHECK RT LOWER AILERON SHROUD HAD CORRODED BONDING PLATE. MX REPAIRED RT LOWER AILERON SHROUD IAW EC5750-0 1315(E). THE ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4F RT 20081222 EA 2008 12 22 MASA2008121500744 1 20081215 A 5210 PANEL CNDAIR CL600 CL6002C10 1390015 EA PAX DOOR BUCKLED A MASA K NONE O OTHER NR NOT REPORTED 1 SW 07 515MJ 10117 PASSENGER DOOR FWD AND AFT SIDE PANEL BUCKLING. REPAIRED PASSENGER DOOR FWD AND AFT SIDE PANEL. 2 L 7 2 4F RT A21EA 20081222 EA 2008 12 22 MASA2008121000741 1 20081210 A 3222 STRUT CNDAIR CL600 CL6002B19 1900309 EA NLG DEFECTIVE A MASA B EMER. DESCENT O OTHER AP APPROACH 1 SW 07 77181 7181 ASH FLT 7042 IAD-BUF. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD DUE TO A LOUD THUMP DURING GEAR RETRACTION. MX REPACKED THE NLG STRUT. 2 L 7 2 4F RT A21EA 20081222 2008 12 22 UALA2008121606904 4 20081214 A 2297 D5715P CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE E&E BAY LOOSE A UALA O OTHER W INADEQUATE Q C NR NOT REPORTED 1 WP 29 658UA 27113 A-T FAILED TO ENGAGE. A-T MODE NOT DISPLAYED ON ADI. REPLACED EEC (P/N 791100-4-108, S/N 209), NO HELP. ALSO TRIED NE W ADC AND SWAPPED PIMUS, NO HELP. REPLACED AUTO THROTTLE SERVO MOTOR (S253T409-4, S/N 4), NO HELP MR 22324 OFF-4 ON-112 . STILL HAVE NO INFC TMC EEC R PRIM AND SEC ON MCDP GRND TEST 30. RECHECKED WIRING FROM TMC TO EEC, CKS OK. TRIED NEW MCP, NO HELP. REPLACED K1040, NO HELP. FOUND OUTPUT BUSS FROM RT PIMU TO TMC INOP ON BOTH CHANNELS. SECURED CONNECTO R D5715P IN BACK OF E2-3 SHELF. ACP'D CAT III TEST. ALL TESTS PASSED. ACFT RETURNED TO CAT III STATUS. 2 L 7 2 4F 4 F RT A1NM E24NE 20081222 NM 2008 12 22 UALA2008121606905 1 20081213 A 7933 10300080 SENSOR BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE RT ENGINE FAILED A UALA O OTHER N FALSE WARNING IN INSP/MAINT 1 WP 29 788UA 26942 ENG EEC C1 R RIGHT ENGINE CONTROL IS IN A TIME LIMITED DISPATCH CONDITION. ENGINE CONTROL SYSTEM IS OPERATING WITH REDU CED REDUNDANCY. STATUS FOUND MSG NR 79-60842. REPLACED R ENG OIL TEMP SENSOR. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081222 NM 2008 12 22 UALA2008121606906 1 20081215 A 2421 745329F IDG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LEFT MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 647UA 25284 CREW REPORT LEFT GENERATOR DRIVE LIGHT ILLUMINATED. GENERATOR DRIVE DISCONNECTED AND APU NOW POWERING BUSS. LEFT IDG R EPLACED. LEAK CHECK CARRIED OUT OK. TEST CARRIED OUT. 2 L 7 2 4F 4 F RT A1NM E24NE 20081222 NM 2008 12 22 UALA2008121606907 1 20081216 A 5347 SEAT TRACK BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE FUSELAGE BROKEN A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 105UA 26473 SEAT TRACK SCALLOP FLANGE BROKEN, BS 1152 LBL 98.58. SPLICED IN NEW SECTION OF TRACK FROM BS 1128.5 TO 1170.5. 2 L 7 4 4F 4 F RT A20WE E24NE 20081222 NM 2008 12 22 UALA2008121606908 1 20081216 A 3350 20131A BATTERY AIRBUS A319 A319131 3930317 NM IAE V2522 V2522A5 NE CABIN DISCHARGED A UALA K NONE W L INADEQUATE Q C NO TEST IN INSP/MAINT 1 WP 29 843UA 1573 THREE SVC EMER LIGHTS TEST FAILS. REPLACED EMERGENCY LIGHTS BATTERIES AT DOOR 1L AND L OVERWING POSITIONS. EMERGENCY L IGHTS TEST NOW PASSES. 2 L 7 2 4F 4 F RT A28NM E40NE 20081222 NE 2008 12 22 UALA2008121506898 2 20081213 A 7321 7911004111 EEC BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE FAULTY A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 654UA 25392 MULTI MESSAGES FOR BOTH ENGINES, RELATED TO P2T2 AND EECS. REPLACED EEC'S AND CONTROL ALTERNATOR. NO FAULTS NOTED. 2 L 7 2 4F 4 F RT A1NM E24NE 20081222 NM 2008 12 22 UALA2008121506899 1 20081213 A 2913 35059208 PUMP BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE HYDRAULIC SYS OVERHEATED A UALA O OTHER W M INADEQUATE Q C OVER TEMP NR NOT REPORTED 1 WP 29 776UA 26937 HYD PUMP DEM C2 LOW CENTER HYDRAULIC DEMAND PUMP NR 2 PRESSURE WHEN COMMANDED ON, OR CENTER DEMAND PUMP NR 2 OVERHEATED. STATUS MSG-2910460 ACTIVE DC MODE MSG-2911110 INACTV DC MODE. REPLACED ADP. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081222 NM 2008 12 22 USAA2008121592225 1 20081202 A 5320 ANGLE BOEING 757 7572B7 1384964 NM FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 200UU 27809 CLT - C1 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON TRANSITION ANGLE AT BS 783, RBL 25. REPAIRED TRANSITION AN GLE AT BS 783, RBL 25 IAW B757 SRM 51-70-13. 2 L 7 2 4F RT A2NM 20081222 NM 2008 12 22 USAA2008121292221 1 20081111 A 5753 113N200348SP FLAP BOEING 757 7572B7 1384964 NM TE FLAP DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 941UW 27806 MCN - C1 - MAJOR REPAIR - RIGHT INBOARD FLAP DISBONDED AT WS 233 TO WS 235. REPAIRED RIGHT INBOARD FLAP AT WS 233 TO WS 235 IAW B757 SRM 51-70-10. 2 L 7 2 4F RT A2NM 20081222 NM 2008 12 22 USAA2008121692237 1 20081214 A 5330 6518420 SKIN BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - CRACK IN CAPTAINS WINDSHIELD CUTOUT, UPPER AFT IN RADIUS, BS 231.25, S9L. REPAIRED CAPTAINS W INDSHIELD CUTOUT, UPPER AFT IN RADIUS, BS 231.25, S9L IAW B737 SRM 53-10-01 REPAIR 10. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 USAA2008121692244 1 20081207 A 5322 6935352Y1 SHEAR TIE BOEING 737 7374B7 138449C NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - SHEAR TIE CRACKED AT BS 767, S25L. REPLACED SHEAR TIE AT BS 767, S25L IAW B737 SRM 51-10-02. 2 L 7 2 4F RT A16WE 20081222 NM 2008 12 22 USAA2008121692245 1 20081208 A 5754 65C26603102 SKIN BOEING 737 7374B7 138449C NM LE SLAT DEBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 435US 24557 CLT - Q2 - MAJOR REPAIR - DISBONDED DOUBLER ON NR 4 SLAT INBOARD TRAILING EDGE WEDGE UPPER SURFACE. REPAIRED NR 4 SLAT INBOARD TRAILING EDGE WEDGE UPPER SURFACE IAW US AIRWAYS TYPICAL REPAIR 57-42-03. 2 L 7 2 4F RT A16WE 20081222 SO 2008 12 22 C2XA08IA254 1 20081214 A 3610 32158861 VALVE EMB 145 EMB145XR 3260214 SO ZONE 400 INOPERATIVE A C2XA O OTHER J WARNING INDICATION DE DESCENT 1 SW 27 13118 17319 17319 145675 IAH- FLIGHT 2632, THE CREW REPORTED A LOSS OF PRESSURIZATION AT THE TOP OF DESCENT. THE ACFT LANDED AT IAH WITHOUT INCI DENT WHERE MX R&R THE HIGH STAGE BLEED VALVE. OPS TESTED WITH NO DEFECTS FOUND, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE 2 L 7 2 4F RT 20081222 CE 2008 12 22 GUUA93952121108A 1 20081211 A 5220 DOOR BEECH 1900 1900D 1154162 CE EMERGENCY EXIT STIFF A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 82539 UE168 DURING SCHEDULED ROUTINE MX DISCOVERED LT EMERGENCY EXIT INTERIOR AND EXTERIOR HANDLES HARD TO OPERATE. LUBRICATED LT E MERGENCY EXIT LATCH PINS AND GUIDES. OPS CHECK OK. 2 L 7 2 4T RT A24CE 20081222 NM 2008 12 22 USAA2008121692246 1 20081213 A 3350 20137A BATTERY PACK BOEING 737 7373G7 138447J NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 307AW 24634 SAL - C17 - EEL - EMERGENCY EXIT LIGHT UPPER AND LOWER POSITIONS INOP AT RIGHT EMERGENCY EXIT DOOR. REPLACED EMERGENCY BATTERY PACK AT RIGHT CENTER POSITION IAW B737 AMM 33-51-51. 2 L 7 2 4F RT A16WE 20081222 EU 2008 12 22 USAA2008120992196 1 20081208 A 2120 UNKNOWN AIRBUS 320 A320214 3930316 EU CABIN FUMES A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 103US 861 FLT 873 LAS-SAN - FUMES - PASSENGERS SEATED AFT OF THE WING COMPLAINED OF FUMES IN THE CABIN, EYE IRRITATION AND SNEEZIN G. MAINTENANCE INSPECTED THE APU FOR LEAKS - NONE NOTED. RAN THE APU AND BOTH ENGINES INDEPENDENTLY WITH NO ODORS NOTE D. AIRCRAFT IS OK FOR SERVICE. 2 L 7 2 4F RT A28NM 20081222 EU 2008 12 22 USAA2008121292217 1 20081211 A 3350 POWER SUPPLY AIRBUS 320 A320232 3930326 EU CABIN MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 668AW 1764 FLT 252 PHL-PHX - EEL - FOUR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE, TWO LEFT WING AND TWO RIGHT WING. MAINTENANCE RESET THE EMERGENCY POWER SUPPLY UNIT. OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F RT A28NM 20081222 EA 2008 12 22 VNAA2008121700007 1 20081212 A 3260 PROXIMITY SENSOR CNDAIR CL600 CL6002C10 1390015 EA LANDING GEAR OUT OF ADJUST A VNAA A UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 GL 05 705PS 10144 CREW REPORTED A GEAR DISAGREE RED MSG (UP POSITION SELECTED), PROX SYS FAULT 1. AIRCRAFT RETURNED TO CLT AND LANDED WIT HOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND ADJUSTED THE PROX 3 SENSOR. OPERATIONAL CHECKS WERE ACCOMPLISHED PER THE MAINTENANCE MANUAL WITH NO DEFECTS NOTED. NO OTHER DEFECTS WERE NOTED AND AIRCRAFT WAS RELEASED FOR SERVICE. 2 L 7 2 4F RT A21EA 20081222 EA 2008 12 22 VNAA2008121900008 1 20081214 A 3260 PSEU CNDAIR CL600 CL6002C10 1390015 EA LANDING GEAR MALFUNCTIONED A VNAA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 GL 05 705PS 10144 CREW REPORTED WHEN LANDING GEAR WAS SELECTED UP, RECEIVED A GEAR DISAGREE, PROX SYS FAULT 1. AIRCRAFT RETURNED TO CLT A ND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND ADJUSTED THE PROX 3 AND PX37 SENSORS, AND REMOVED AND RE PLACED PSEU PER MAINTENANCE MANUAL UNDER DIRECTION OF THE MANUFACTURER. ALL OTHER PROX SENSORS WERE CHECKED FOR ADJUSTM ENT. OPERATIONAL CHECKS WERE ACCOMPLISHED PER THE MAINTENANCE MANUAL WITH NO OTHER DEFECTS NOTED. AIRCRAFT WAS RELEASE D FOR SERVICE. 2 L 7 2 4F RT A21EA 20081222 2008 12 22 ZZDA2008169R1 4 20081104 A 2565 3964899501 LANYARD BOEING 717 717200 1383700 NM EVAC SLIDE BROKEN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 915AT 55073 ESCAPE SLIDE AT L-1 DOOR WIRE LANYARD BROKEN. REMOVED AND REPLACED WIRE LANYARD IAW REF MM 25-61. 2 L 7 2 4F TR A6WE 20081222 2008 12 22 C2XA08RI179 2 20081215 A 7532 32158861 BLEED VALVE EMB 145 EMB145LR 3260212 SO NR 2 INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 14952 11644 9627 145067 FLIGHT 2306 EWR DURING CLIMBING FLIGHT CREW REPORTED THE FOLLOWING MSGS ON EICAS: PACK 2 CLSD AND BLD 2 CLSD. CREW RESE T THE SYSTEM BUT FAILED AGAIN AND WHEN TRIED AN ANTI ICE TEST GOT BLD 2 FAIL MSG. CREW PERFORMED AIR RETURN AND LANDED U NEVENTFULLY. EWR MX R&R NR 2 BLEED VALVE AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2 L 7 2 4T RT T00011AT 20081222 NM 2008 12 22 ZZDA2008182 1 20081209 A 2120 UNKNOWN BOEING 737 7377BD 1384511 NM CABIN ODOR A ZZDA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 37 316AT 33928 UPON T/O FLIGHT ATTENDANT`S REPORTED SMELL OF SMOKE IN CABIN. DECLARE EMERGENCY AND RETURN TO AIRPORT. UPON INITIAL EN TRY INTO AIRCRAFT NO FUMES OR SMOKE SMELL PRESENT. INSPECTED CABIN, BAG BINS, E&E, COMPT AND A/C BAYS, NO EVIDENCE OF B URNING PRESENT. FOUND NO POPPED C/B`S. COULD NOT DUPLICATE DISCREPANCY PER FIM 21-00 TASK 806. OK FOR SERVICE. 2 L 7 2 4F RT A16WE 20081222 EA 2008 12 22 A6WA200840632 1 20081207 A 5200 STOP CNDAIR CL600 CL6002B19 1900309 EA DOOR CRACKED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 414ZW 7586 BUTE DOOR HINGE PANEL 694KB STOP ASSY CRACKED. .550" L X .300 W X .090 D STOP ASSY ON BUTE DOOR HINGE PANEL 694KB R&R I AW CRJ200 SRM 51-42-06 AND 51-23-00. 2 L 7 2 4F RT A21EA 20081222 CE 2008 12 22 DXTA2008120903393 1 20081208 A 3260 WARNING LIGHT CESSNA 560 560XL 2076702 CE MLG ILLUMINATED E DXTA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 07 579QS 5605773 THE LANDING GEAR UNLOCK LIGHT REMAINED ILLUMINATED IN FLIGHT AFTER EXTENDING THE GEAR HANDLE. 2 L 7 2 4F RT A22CE 20081222 NM 2008 12 22 UPS08554135 1 20081209 A 5610 WINDOW BOEING 757 75724APF 1384969 NM COCKPIT OUT OF ADJUST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 455UP 25476 INSPECTION TYPE:N/A L2 WINDOW HARD TO OPERATE. ADJUSTED L2 WINDOW PER MM 56-11-02-5. 2 L 7 2 4F RT A2NM 20081222 NM 2008 12 22 UPS08654180 1 20081211 A 3350 LIGHT BOEING 767 76734AF 1385212 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 313UP 27764 INSPECTION TYPE:N/A DURING AS-E FOUND EMERGENCY LIGHTS NOT ILLUMINATED AT COCKPIT ENTRANCE. RELAMPED AND OPS CHECKED SA TISFACTORY PER AMM 33-51-11-2. 2 L 7 2 4F RT A1NM 20081222 SO 2008 12 22 C2XA08IA255 1 20081215 A 3350 LIGHT EMB 145 EMB145LR 3260212 SO CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 27 26549 145571 IAH - DURING A-CK INSPECTION THE EMERGENCY LIGHT STRIPS BETWEEN ROWS 8 & 9 WERE FOUND TO BE INOPERATIVE. MX INSPECTED T HE LIGHTING SYSTEM, OPS TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE 2 L 7 2 4T RT T00011AT 20081222 EU 2008 12 22 UPS08154133 1 20081210 A 7897 WIRE AIRBUS 300 A300B4622R 3930312 EU THRUST REVERSER CHAFED A IPXA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 163UP 0852 INSPECTION TYPE:N/A AT 11,000 FT, GOT AN ECAM "ENG 1 ENG REV UNLOCK". ALSO HAD A GREEN NR 1 "REV" LIGHT ON. DEFERRED 3 90408. REPAIRED CHAFED WIRING SEE LP 906735. REVERSER OPS CHECKS GOOD THIS CLEARS M390408. 2 L 7 2 4F RT A35EU 20081222 CE 2008 12 22 DXTA2008120903395 1 20081208 A 2750 FLAP SYSTEM CESSNA 560 560XL 2076702 CE TE FLAPS MALFUNCTIONED E DXTA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 GL 07 579QS 5605773 FLAPS WOULD NOT EXTEND PAST 15 (DEG) ON FINAL APPROACH. 2 L 7 2 4F RT A22CE 20081222 WP 2008 12 22 UPS08854205 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR 803-F1-82, STA 1670 L8R HAS NO SRM REFERENCE AND REQUIRES EO APPX F. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED REPAIR REF SRM 53-02-01 FIG10 SHT 1. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854145 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-66 FS 1385 L27L - L28L HAS NO SRM REF. REMOVED INTERNAL REPAIR DOUBLER AND FI LLER. FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-0201 FIG 7 SHEET 10. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854146 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-67 FS 1407.5 L26L - L27L HAS NO SRM REF. REMOVED INTERNAL REPAIR DOUBLER AND FILLER. FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854147 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-68 FS 1381 L24L - L25L HAS NO SRM REF. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 10. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854148 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-95 AT STA 1446 L12L HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER, FABRIC ATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 10 TR 53-204. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854149 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-89 AT STA -153/-156 L21R HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER, F ABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 10. 2 L 7 4 4F RT 4A25 20081222 CE 2008 12 22 GUUA93952121108B 1 20081211 A 5220 DOOR BEECH 1900 1900D 1154162 CE EMERGENCY EXIT STIFF A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 29 82539 UE168 DURING SCHEDULED ROUTINE MX DISCOVERED RT AFT EMERGENCY EXIT INTERIOR AND EXTERIOR HANDLES HARD TO OPERATE. LUBRICATED RT AFT EMERGENCY EXIT HANDLES. OPS CHECK GOOD. 2 L 7 2 4T RT A24CE 20081222 WP 2008 12 22 UPS08854150 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-87 AT STA 1748 L20R - L21R HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854155 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-103 AT STA 1472 L29-30L HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER, FA BRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 10. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854156 1 20081003 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR DOUBLER AT STA 53-65 L31R-L34R INSTALLED WITH BLIND RIVETS 803-F1-32. REMOVED EXISTING DOUBLE R. FABRICATED & INSTALLED REPLACEMENT DOUBLER REF DC8 SRM 53-02-01 FIG 7 SHT 11. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854160 1 20081018 A 5320 WEB DOUG DC8 DC873F 302199F WP FS-81 LBL37.5 MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F3-06 AT FS -75/-83 LBL 37-42 HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW UPS EO DC8-5330-31487-A ANG FVCI DWG 53-08540-21. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854165 1 20081119 A 5720 DWG5771181 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP LT WING O/B LEADING EDGE, I/B SEGMENT LOWER INTERNAL BEADED DOUBLER CRACKED NEAR PANEL 520A, XFS 452. FABRICATED AND INSTALLED REPAIR PER EO DC8-5730-31521-A AND EA 008-5720-01-A1569. 2 L 7 4 4F RT 4A25 20081218 EU 2008 12 18 F3LA2008121600725 1 20081213 A 2611 UNKNOWN AIRBUS A319 A319112 3930323 EU COCKPIT SMOKE A F3LA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 21 910FR 10 1781 PILOT REPORTED THAT THE DEICING CREW STARTED DEICING THE AIRCRAFT BEFORE CONTACT WITH THE COCKPIT CREW. SMOKE FILLED CO CKPIT AND MID-CABIN. AN ALARM WAS RECEIVED FROM THE PARTICLE SENSORS IN THE AFT AND FORWARD CARGO AREA. PILOT TURNED O FF THE APU BLEED AND ALL PROBLEMS WENT AWAY. MAINTENANCE WAS CALLED TO INSPECT THE AIRCRAFT. MAINTENANCE OPERATED THE PACK SYSTEM AND SMOKE ODOR DISSIPATED. MAINTENANCE RESET CIRCUIT BREAKERS C7 AND S22 FOR CARGO SMOKE DETECTION SYSTEM A ND PERFORMED OPERATIONAL TEST OF THE SAME. NO FAULTS NOTED IN ACCORDANCE WITH AMM 26-16-710-003. 2 L 7 2 4F RT A28NM 20081218 NM 2008 12 18 AALA200810481 1 20081211 A 5320 STIFFENER BOEING 737 737823 13844CB NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 21 906AN 29508 FLOOR STIFFENER STATION 1016 AT 3 INCHES LEFT BUTT LINE, HAS CORROSION. INSTALLED A SERVICEABLE STRAP (STIFFENER) PER S RM 51-00-02G. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 UALA2008121206863 1 20081212 A 2150 8102044 VALVE BOEING 777 777222 1385219 NM PWA PW4090 PW40903 51538 NE AC PACK MALFUNCTIONED A UALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 29 225UA 30554 PACK FCV L ON STATUS PAGE. REPLACED UPPER LT FCV. RETURNED AIRCRAFT TO NORMAL CONFIGURATION, OPS CHECKED, VERIFIED NO EICAS MSG. 2 L 7 2 4F 4 F RT T0001SE E46NE 20081219 NM 2008 12 19 SWAA087184 1 20081216 A 5340 65C27314 STRINGER CLIP BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 680AA 23505 DURING SCHEDULED 22Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 22R. REMOVED AND REPLACED CLIP PER SRM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087176 1 20081216 A 5311 6546526 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087229 1 20081217 A 5311 6546548 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 386SW 26601 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 2008 12 19 HALA2008121300889 4 20081213 A 2210 4052506955 COMPUTER BOEING 767 76733A 1385209 NM MALFUNCTIONED A HALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM - ATB - VNAV/LNAV WOULD NOT ENGAGE WITH CENTER AUTOPILOT ENGAGED. CAPTAIN SPEED LIMIT INOP DIS PLAYED ON CAPTAINS ADI. REPLACED NR 1 FMC. GND OPS CHK OK AMM 34-61-02. ACCOMPLISHED MCDP TEST 30 TEST PASS A/C OK TO REMAIN AT LMP STATUS "LAND 3". 2 L 7 2 4F RT A1NM 20081219 NM 2008 12 19 SWAA087178 1 20081216 A 5311 6546534 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 520, STR 8R. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087215 1 20081214 A 3350 101114 COVER BOEING 737 7375H4 138449D NM CABIN OUT OF POSITION A SWAA K NONE O OTHER UK UNKNOWN 1 SW 29 512SW 24189 FWD LT EMERGENCY EXIT LIGHT COVER FELL OFF. INSTALLED COVER PER MM. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 QXEA2008121201236 1 20081210 A 6123 UNKNOWN BOMBDR DHC8 DHC8402 1390042 NM AUTOFEATHER SYS UNKNOWN A QXEA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 NM 19 434MK 4227 SEA - ABORTED TAKEOFF AT 90 KNOTS DUE TO FAILURE OF AUTOFEATHER TO ARM (THERE WAS NO ANNUNCIATION ON ED). RETURNED TO T HE GATE. COMPLIED WITH OPS TEST OF PROP AUTOFEATHER AND UPTRIM SYSTEM IAW AMM TASK 61-20-00-710-801. TEST IS GOOD. GR OUND RAN ACFT AT RATING, AUTOFEATHER ARMED AS REQUIRED. PERFORMED HIGH SPEED TAXI WITH NO DEFECTS NOTED. ARMED AT 45 K NOTS. COULD NOT DUPLICATE. RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081219 NM 2008 12 19 QXEA2008121601244 1 20081214 A 2130 CABIN PRESSURE BOMBDR DHC8 DHC8402 1390042 NM MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 19 401QX 4031 RDM - ACFT FAILED TO PRESSURIZE. FA REPORTS LOUD SOUND AT DOOR L2. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. INSPECTED MCD SEAL, AFT ENTRY DOOR SEAL, AFT CARGO DOOR SEAL, NO DEFECT NOTED. PRESSURIZED AIRCRAFT IAW AMM TASK 21-00-00-863-80, TASK 21-00-00-863-802, NO DEFECT NOTED, ACFT OK FOR CONTINUED SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 20081219 NM 2008 12 19 SWAA087203 1 20081217 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 986, STR 24R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087204 1 20081217 A 5330 6545776 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 312SW 23334 DURING SCHEDULED OTS CHECK, FOUND FUSELAGE SKIN CORRODED AT BS 987, STR 27R. REPAIRED SKIN PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 SWAA087157 1 20081216 A 5311 6546529 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 29 384SW 26590 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME PER SWA EA. 2 L 7 2 4F RT A16WE 20081219 NM 2008 12 19 QXEA2008121801252 1 20081125 A 5347 SEAT TRACK BOMBDR DHC8 DHC8402 1390042 NM FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 19 412QX 4059 PDX - C4 - SEAT TRACK NR 11 HAS BLENDED AREAS AT FWD END AT SPLICE FASTENER HOLES THAT ARE OUT OF LIMITS PER RD 8/4-53-8 84. REMOVED NR 11 SEAT TRACK. LOCATED FASTENER HOLES IN NR 11 SEAT TRACK. INSTALLED MIDDLE SPLICE BETWEEN SEAT TRACK NR 10 AND NR11 IAW SRM 51-40-07, 51-40-15. INSTALLED AFT SPLICE IAW SRM 51-42-05. INSTALLED SEAT TRACKS NR 10 AND NR 11 IAW SRM 51-40-07, 51-40-15. 2 H 7 2 4T RT A13NM 20081219 EA 2008 12 19 MALA080213 1 20081215 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 1900309 EA LAVATORY FALSE INDICATION A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 8943A 7943 AFTER TAKEOFF SMOKE TOILET EICAS MSG ILLUMINATED POM PROCEDURE COMPLETED. LANDED AT NEAREST SUITABLE AIRPORT. FLT ATTE NDANT REPORTED ODOR IN LAV AND SMOKE ALARM. AIRCRAFT WAS DE-ICED PRIOR TO DEPARTURE. RAN ENGINES IAW CRJ 200 AMM 71-00 -00 FOR 30 MIN. MESSAGE EXTINGUISHED, UPON INITIAL RUN UP NOTED FAINT SMELL, BUT AFTER RUNNING ENGINES AND PACKS FOR 3 0 MIN. SMELL DISSIPATED AND DID NOT RETURN. NO SMOKE OR VAPOR NOTED. NO FURTHER ACTIONS REQUIRED. 2 L 7 2 4F RT A21EA 20081219 NM 2008 12 19 NSVA2008045 1 20081212 A 4920 APU BOMBDR DHC8 DHC8402 1390042 NM APU BAY CONTAMINATED A NSVA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 196WQ 4196 APU ON SMOKE FILLED ENTIRE AIRPLANE, EVACUATED. IN PROCESS OF DE-ICING. FOUND CAUSE OF SMOKE TO BE GLYCOL INDUCTION FR OM RUNNING APU. APU DEFERRED IAW MEL 49-00-1. CAT D ID NR 33748. 2 H 7 2 4T RT A13NM 20081219 NM 2008 12 19 HALA2008120700880 1 20081207 A 8012 9798585 CONTROL VALVE BOEING 767 76733A 1385209 NM ENGINE STARTER MALFUNCTIONED A HALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 13 587HA 33421 ETOPS SIGNIFICANT SYSTEM - LEFT ENGINE FAILED TO START. NO ROTATION. R & R LT ENGINE STARTER CONTROL VALVE PER AMM 80- 11-02 OPS AND LEAK CHK GOOD. 2 L 7 2 4F RT A1NM 20081219 EU 2008 12 19 F3LA2008121600726 1 20081213 A 7830 ISOLATION VALVE AIRBUS A318 A318111 3940019 EU THRUST REVERSER CRACKED A F3LA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 NM 21 807FR 15 2276 ENROUTE AT FL330, PILOT REPORTED INDICATION OF HYDRAULIC RESERVOIR LOW LEVEL FOLLOWED BY ENGINE NR 2 PUMP LOW LEVEL AND NOTED THE YELLOW SYSTEM FLUID QUANTITY DEPLETED. MAINTENANCE INSPECTED THE NR 2 ENGINE AND FOUND THE THRUST REVERSER IS OLATION VALVE HYDRAULIC LINE CRACKED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE THRUST REVERSER ISOLATION VALVE HYDRAULIC LINE AND PERFORMED OPERATIONAL AND LEAK CHECKS IAW AMM 78-37-51-400-001 AND 78-21-00-710-042. 2 L 7 2 4F RT 20081219 EU 2008 12 19 F3LA2008121600727 1 20081215 A 3397 EN3646A62039DN CONNECTOR AIRBUS A318 A318111 3940019 EU EMERGENCY LIGHTS LOOSE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 21 802FR 42 1991 DURING C4 C-CHECK, INSPECTION NOTED THE EMERGENCY PATH LIGHTING AT SEAT 7 ABC INOPERATIVE. MAINTENANCE FOUND PUSHED BAC K PIN ON ROW 7 SEAT CONNECTOR, LOCKED PIN IN PLACE AND PERFORMED OPERATIONAL CHECK IN ACCORDANCE WITH AMM 33-51-00-710-0 09. 2 L 7 2 4F RT 20081219 2008 12 19 HALA2008121500887 4 20081215 A 3460 4052506955 FMC BOEING 767 76733A 1385209 NM LEFT INOPERATIVE A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 587HA 24006 24006 33421 ETOPS SIGNIFICANT SYSTEM, AFTER FMC INITIALIZATION AT GATE. LEFT FMC BLANKED THEN DISPLAYED "FMC L OUTPUT LOSS". REPLA CED RIGHT FMC, LOADED NEW SOFTWARE FROM BINDER AND CROSSLOADED TO LEFT FMC MONITORED FOR MSG. NO MSG DISPLAYED AMM 34-6 1-01. PERFORMED FMC OPS TEST PER AMM 34-61-00. "PER HAL ENGINEERING RIGHT FMC REPLACED". 2 L 7 2 4F RT A1NM 20081219 SO 2008 12 19 SWIA200820633 1 20081213 A 2721 55298 ACTUATOR EMB 120 EMB120ER 3260203 SO RUDDER TRIM JAMMED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 295SW 120322 FLT 5522 - RUDDER TRIM JAMMED. REPLACED RUDDER TRIM ACTUATOR PER MM, P/N: 5-5298, S/N ON: 40, SN OFF: 399. 2 L 7 2 4T RT A31SO 20081219 EA 2008 12 19 SWIA200820636 1 20081216 A 3350 BATTERY PACK CNDAIR CL600 CL6002C10 1390015 EA EMERGENCY LIGHTS DISCHARGED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 368CA 10075 FLT 4399 - TWO EMERGENCY LIGHTS AND EXIT LIGHT IN AFT CABIN INOP. REPLACED BATTERY PACK. 2 L 7 2 4F RT A21EA 20081219 NM 2008 12 19 UALA2008121506883 1 20081213 A 5210 141N622022 GATE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE R4 DOOR CORRODED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 554UA 26644 R-4 DOOR LOWER GATE CORRODED. INSTALLED NEW GATE. 2 L 7 2 4F 4 F RT A2NM E17NE 20081219 NM 2008 12 19 UALA2008121506892 1 20081213 A 2620 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE P40 PANEL SHORTED A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 659UA 27114 APU FIRE PROTECTION SYSTEM INOP. REPLACED APU FIRE BOTTLE. FOUND FIRE BOTTLE ARM LIGHT ASSY SHORTED ON P40 PANEL. REP LACED LIGHT ASSY L542, CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 20081219 NM 2008 12 19 UALA2008121506872 1 20081212 A 5210 140N264023 MECHANISM BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE L1 DOOR OUT OF ADJUST A UALA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 WP 29 554UA 26644 DOOR 1L EMERGENCY POWER TRIGGER MECHANISM OUT OF ADJUSTMENT. ACCOMP ADJUSTMENT AND OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 20081219 EU 2008 12 19 YENA200812180128 1 20081217 A 2910 D2901055400000 DRAIN LINE AIRBUS 320 A320232 3930326 EU NR 1 PYLON LEAKING A YENA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 EA 15 646JB 8844 2945 FLT NR 300, LGB-IAD, GREEN HYD SYS FAIL IN FLIGHT. FOUND CASE DRAIN LINE NR 1 ENG PYLON LEAKING. REPLACED CASE DRAIN L INE, OPS AND LEAK CHECK GOOD. REPLACED NR 1 ENG DRIVEN PUMP AS PER AMM 29-11-40 PRECAUTIONARY, OPS CHECK OK. 2 L 7 2 4F RT A28NM 20081219 SO 2008 12 19 C2XA08IA252 1 20081212 A 2530 500064001 COFFEEMAKER EMB 145 EMB145XR 3260214 SO GALLEY DIRTY A C2XA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 27 14143 14424 33 145739 IAH - FLIGHT 2924, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL FROM BOTH COFFEEMAKERS. MX PLACED THE COFFEEMAKERS ON NEF NR GL01 D CTL NR 160100, AND THE ACFT WAS RETURNED TO SERVICE. ON 12/14/08 THE DISCREPANCY REPEATED AND MX INSPECTED THE COFFEEMAKERS, FOUND THEM TO BE DIRTY ON THE HEATERS, CLEANED THE HEATERS, OPS CHECKED WITH NO DEFE CTS, REMOVED THE NEF, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. 2 L 7 2 4F RT 20081222 EU 2008 12 22 USAA2008121592232 1 20081212 A 5347 F53477210204 SEAT TRACK AIRBUS 330 A330323 3940030 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AY 375 BFM - C2 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR70 TO FR71, -Y2462. REPAIRED SEAT TRACK BETWEEN FR70 TO FR7 1, -Y2462 IAW A330 SRM 51-42-00. 2 L 7 2 4F RT A46NM 20081222 2008 12 22 USAA2008121592234 4 20081213 A 2565 D30664109 SLIDE AIRBUS 320 A320231 3930325 EU R1 DOOR LOW PRESSURE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 629AW 23295 8412 76 FLT 180 PHX - EMERGENCY EQUIPMENT - R1 PASSENGER ENTRY DOOR SLIDE PRESSURE LOW (NOT IN THE GREEN BAND). MAINTENANCE REM OVED AND REPLACED THE R1 DOOR SLIDE ASSEMBLY. 2 L 7 2 4F RT A28NM 20081222 NM 2008 12 22 USAA2008121592227 1 20081204 A 3397 55A0821109296 WIRE BOEING 737 7373G7 138447J NM CABIN UNKNOWN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 307AW 24634 SAL - C17 - EEL - EMERGENCY EXIT LIGHT IN THE FOLLOWING POSITION IN SEAT ROW 17 LT SIDE UPPER POSITION AND EXIT UPPER PO SITION AND LITTLE EXIT L2 DOOR. PERFORMED RE-CONFIGURATION OF WIRES ON CONNECTOR D2966 IAW B737 TROUBLESHOOTING MANUAL 33-51-02-1, WDM 33-51-15, & AMM 33-51-02-5. 2 L 7 2 4F RT A16WE 20081222 SO 2008 12 22 C2XA08CL132 1 20081210 A 3097 WIRE EMB 145 EMB145LR 3260212 SO ANTI ICE T SWITC FRAYED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 27 19966 145131 CLE FLIGHT NR 2118 THE CREW REPORTED A STAB A/I FAIL MSG IN CLIMBOUT FROM CLE. THE CREW COMPLETED THE QRH INSTRUCTIONS A ND MSG WAS STILL THERE. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE STAB ANTI/I CE VALVE AND REPAIRED THE WIRE TO THE ANTI-ICE LEAK THERMAL SWITCH. OPS CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20081222 NM 2008 12 22 ZZDA2008186 1 20081216 A 3397 WIRE BOEING 717 717200 1383700 NM CABIN BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 37 930AT 55072 SEAT ROW 25DEF E PATH LIGHTS INOP (BROKEN WIRE). RE-TERMINATED 1 EA PIN SOCKET ON THE FLOOR SIDE ELECTRICAL CONNECTOR P ER SWPM 20-20, WDM 33-51-14 OPS CHECK GOOD IAW AMM 33-51-00 SEAT ROW 25DEF. 2 L 7 2 4F TR A6WE 20081222 NM 2008 12 22 ZZDA2008181 1 20081211 A 5320 PAN BOEING 717 717200 1383700 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 37 894AT 55046 AFT CARGO COMPARTMENT DOOR LOWER PAN CORRODED BEYOND LIMITS. REMOVED AND REPLACED LOWER DOOR PAN SPLICE SECTION PER SRM 53-20-15. 2 L 7 2 4F TR A6WE 20081222 WP 2008 12 22 UPS08854206 1 20081105 A 5753 564296016 SKIN DOUG DC8 DC871F 302199D WP TE FLAP MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:SV SURVEY SEQ 729-W4-06 RT INBOARD FLAP DOUBLER FASTENER SPACING LESS THAN 4D REF APPENDIX D/C1 UPPER SU RFACE STA XW 88. REPAIRED IAW UPS EODC8-5720-31610A. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854164 1 20081018 A 5312 PRESSURE PANEL DOUG DC8 DC873F 302199F WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F3-02 AT FS -9 TO -15 LBL 5 TO RBL 23 HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR PARTS IAW UPS EO DC8-5330-31508-A AND SAA EA 008-5320-01-A1574. 2 L 7 4 4F RT 4A25 20081222 CE 2008 12 22 DXTA2008121503399 1 20081213 A 2120 UNKNOWN CESSNA 750 750 2076810 CE COCKPIT ODOR E DXTA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 07 949QS 7500049 AS WE WERE DESCENDING THRU FL350 WE HEARD A VERY LOUD BANG IN THE COCKPIT FOLLOWED BY A STRANGE ODOR. THE ODOR WAS STRO NG IN THE ENTIRE COCKPIT AND CABIN. 2 L 7 2 4J RT T00007WI 20081222 WP 2008 12 22 UPS08854166 1 20081027 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-W3-06 AT LT STUB WING SKIN XFS 249.5 - 258.9 EO DC8-5100-30418-C APPX H STEP 4 IS MARKED NO AND STEP 6&7 ARE MARKED NOT VISIBLE. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO DC8- 5730-31485-A AND FVCI DWG 57-08540-19. 2 L 7 4 4F RT 4A25 20081222 CE 2008 12 22 DXTA2008121603402 1 20081215 A 3230 LANDING GEAR CESSNA 680 680CE 2076811 CE MALFUNCTIONED E DXTA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 07 338QS 6800011 UPON LOWERING GEAR HANDLE, NOSE GEAR DID NOT LOCK DOWN. RECYCLED GEAR WITH SAME RESULTS. ON GO-AROUND, NOSE GEAR LOCKE D DOWN ON ITS OWN. 2 L 7 2 4F RC T00012WI 20081222 EA 2008 12 22 A6WA200840633 1 20081203 A 5340 ATTACH FITTING CNDAIR CL600 CL6002B19 1900309 EA BS 484 CRACKED A A6WA O OTHER O OTHER NR NOT REPORTED 1 GL 31 414ZW 7586 CRACK FOUND ON INTERCOSTAL CLIP AT FS 484 RBL 27. CRACK LENGTH IS .400. INTERCOSTAL CLIP AT FS 484 RBL 27 R&R. 2 L 7 2 4F RT A21EA 20081222 CE 2008 12 22 Z5FA121308N547CS1 1 20081213 A 7500 30J320401 SERVO VALVE CESSNA 560 560XL 2076702 CE PWC 545 PW545B NE BLEED SYSTEM DEFECTIVE E Z5FA O OTHER J E WARNING INDICATION VIBRATION/BUFFET DE DESCENT 1 EA 63 547CS 34 DD0102 DD0102 DURING DESCENT, RT ENGINE EEC FAULT LIGHT ILLUMINATED FOLLOWED BY ENGINE VIBRATION, ALL PARAMETERS OK. RAN FAULT CHECKL IST USING AFM ABNORMAL CHECK LIST AND PULLED RT ENGINE TO IDLE POSITION. DECLARED EMERGENCY AND FOLLOWED SINGLE ENGINE LANDING PROCEDURES. ACFT LANDED WITHOUT INCIDENT AND RT ENGINE WAS SHUT DOWN AFTER LANDING, TAXIED TO FBO TO OFF-LOAD P ASSENGERS. ON SITE MX PERSONNEL FOUND BOV TORQUE MOTOR TO BE AT FAULT, REPLACED BOV TORQUE MOTOR GROUND PERFORMANCE RUN SATISFACTORY, ACFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A22CE E00059EN 20081222 2008 12 22 C2XA08CL128 4 20081209 A 3420 HG2010AC02 COMPUTER EMB 145 EMB145LR 3260212 SO AHRS FAULTY A C2XA O OTHER O OTHER CR CRUISE 1 SW 27 16999 22986 145307 CLE FLIGHT NR 2475 THE CREW REPORTED THEY LOST THE NR 1 ATTITUDE AND HEADING COMPUTER (AHRS) IN FLIGHT. MX INSPECTED AN D REPLACED THE CAPTAINS AHRS COMPUTER AND OPS CHECKS WERE GOOD. 2 L 7 2 4T RT T00011AT 20081222 CE 2008 12 22 BXS2008F00000 1 20081209 A 3230 LANDING GEAR CESSNA 421 421C 2076016 CE CONT O520 GTSIO520* 17032 SO MALFUNCTIONED E BXSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 09 60RR 421C0885 MLG WOULD NOT RETRACT AFTER TAKEOFF. VISUALLY INSPECTED MLG SYS & FOUND NO DAMAGE. JACKED ACFT. PILOT CONFIRMED THAT 3 GREEN LIGHTS REMAINED ON, TRANSIT/WARMING LIGHT DID NOT ILLUMINATE & MLG HORN SOUNDED. EXPOSED SQUAT SWITCH WIRING SP LICES & TESTED SWITCH OPERATION. SWITCH FUNCTIONED NORMALLY. FOUND GROUND WIRE 1-20 MOUNTING HARDWARE LOOSE. TIGHTENE D HARDWARE. CONNECTED HYD POWER SUPPLY TO ACFT & ATTEMPTED GEAR SWING. MLG WOULD NOT RETRACT. PUT MLG HANDLE IN DOWN POSITION & MANUALLY CYCLED MLG SWITCH. PUT MLG HANDLE IN UP POSITION & APPLIED HYD POWER, MLG RETRACTED NORMALLY. EXTE NDED MLG & REMOVED SQUAT SWITCH FROM STRUT. CONNECTED MULTIMETER TO SWITCH & CYCLED BOTH SIDES OF SWITCH SEVERAL TIMES 1 L 7 2 3O 3 O A7CE E7CE 20081222 WP 2008 12 22 UPS08854167 1 20081020 A 5720 STRUCTURE DOUG DC8 DC873F 302199F WP RT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SP REPAIR 803-W4-10, RT WING L/E STA XFS650-662 REQUIRES ENGINEERING EVALUATION DUE TO APPX H STEP A6 & A7 MARKED NV. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED REPAIR REF SRM DC8 SRM 57-02-01 FIG 2H SHT 1. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854130 1 20081109 A 5522 56549708 SKIN DOUG DC8 DC871F 302199D WP RT ELEVATOR BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:SV REF SURVEY SEQ 729-S2-05 DOUBLER HAS SHARP BULGE TOP OF RT ELEVATOR T/E XE 200.218. REPAIRED IAW UPS EO DC8-5510-31614A. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854131 1 20081117 A 5330 5615368 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:SV REPAIR AT BS 822-834 LONG 1 TO LONG 3L NOT PER SRM STANDARD REF SURVEY SEQUENCE 729-F1-38. REPAIRED IAW DC8 SRM 53-2-1 FIG 7 SHT 1 REV 78. 2 L 7 4 4F RT 4A25 20081222 EA 2008 12 22 MASA2008121300742 1 20081213 A 2740 TRIM SYSTEM CNDAIR CL600 CL6002B19 1900309 EA STAB FAILED A MASA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 75993 7372 ASH 7304 IAD-JAX - CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD DUE TO BOTH STAB TRIMS FAILED. MX CLEANED STAB TRIM, DISCONNECT AND ENGAGE SWITCHES. 2 L 7 2 4F RT A21EA 20081222 WP 2008 12 22 UPS08854132 1 20081020 A 5720 STRUCTURE DOUG DC8 DC873F 302199F WP LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-W3-15 LT INBOARD STUB WING AT STA XFS 239 - XFS 246 EO DC8-5100-30418-C APPENDIX H STEP A (6)&(7) MARKED AS NOT VISIBLE. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW DC-8 SRM 57-02-01A FIG 001 SHEET 1 AND 57-03-00 FIG 12 SHEET 1. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854140 1 20081024 A 5754 STRUCTURE DOUG DC8 DC873F 302199F WP SLOT VANE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-W3-05 LT SLOT VANE XFS 239.0 EO DC8-5100-30418 -C APPX H STEP 6&7 ARE MARKED NOT VISIBLE. REMOVED REPAIR DOUBLER, FABRICATED REPLACEMENT REPAIR DOUBLER, FILLER AND INTERNAL DOUBLER IAW DC-8 SRM 57-03- 03 FIG 10 SHEET 1 AND 57-02-01-FIG 2H SHEET 1. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854141 1 20081027 A 5754 SKIN DOUG DC8 DC873F 302199F WP LT SLOT VANE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-W3-08 LT OUTBOARD VANE SKIN PLATING EO DC8-5100 -30418-C APPX H STEPS 4, 5, 6 & 7 ARE MARKED NOT VISIBLE. REMOVED REPAIR DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 57-02-01 FIG 2H SHEET 1. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854185 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-57 AT STA 1217 L18L HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO DC8-5330-31420-A AND DWG 53-08540-18. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854186 1 20081120 A 5730 SKIN DOUG DC8 DC873F 302199F WP LLT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV LT WING O/B LEADING EDGE I/B SECTION LOWER EXTERIOR SKIN CRACKED AT DRAIN HOLE. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO DC8-5730-31529-A AND SAA EA 008-5720-01-A1571. 2 L 7 4 4F RT 4A25 20081222 NM 2008 12 22 UPS08554200 1 20081215 A 5321 143N545796 FLOORBOARD BOEING 757 75724APF 1384969 NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 466UP 25482 INSPECTION TYPE:N/A LT MOST O/B FLOORBOARD 17 INCHES FROM AFT END OF PANEL POS 4 STA 440 SEC 4 43 DAMAGE 3 BY 1 INCHES T OP OF SKIN AND CORE. REPLACED PANEL. 2 L 7 2 4F RT A2NM 20081222 NM 2008 12 22 UPS08554207 1 20081215 A 5610 ROLLER BOEING 757 75724APF 1384969 NM L2 WINDOW OUT OF ADJUST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 455UP 25476 INSPECTION TYPE:N/A L2 WINDOW WILL NOT OPEN. ADJUSTED LOWER AFT ROLLER. ACCOMPLISHED NR 2 WINDOW LATCHING SYS HANDLE A LL WORK PER MM 56-11-02-5. OK FOR SERVICE. 2 L 7 2 4F RT A2NM 20081222 NM 2008 12 22 UPS08654212 1 20081216 A 3620 3500833 CIRCUIT CARD BOEING 767 76734AF 1385212 NM E&E BAY FAULTY A IPXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 325UP 27751 INSPECTION TYPE:ETOP L DUCT LIGHT ILLUMINATED. L BLEED DUCT LEAK DISPLAYED. LIGHT EXTINGUISHED AFTER ENGINE BLEED AIR SUPPLY AND ISOLATION VALVE CLOSED. T/S IAW FIM 26-18-00 FIG 104. WING AND BODY DUCT LEAK BITE CHK FOUND OK. REMOVED W ING ACCESS PANELS. NO LEAKS FOUND AND REINSTALLED. RAN LENG FT ENG FOR 10 MINUTES AT 38 PSI DUCT PRESSURE NO DUCT LEAK MSG APPEARED. REMOVED AND REPLACED DUCT LEAK FIRE CARD M691 FOR PRECAUTIONARY OPS CK GOOD PER MM 26-10-01. 2 L 7 2 4F RT A1NM 20081222 WP 2008 12 22 UPS08854127 1 20081009 A 5753 SKIN DOUG DC8 DC873F 302199F WP TE FLAP GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-W4-33 RT OUTBOARD FLAP UPPER SKIN REPAIR DOUBLER GOUGED JUST O/B OF FLAP STA 219 HINGE. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW DC-8 SRM 57-02-00 FIG 2A AND 57- 07-01 FIG 4. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854128 1 20081020 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING MISREPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-W4-02 RT WING STA XFS 265 - XFS 527 REPAIR DOUBLER THINNER THAN BASE STRUCTURE. REMOVED REPAIR DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 57-02-01 FIG 38 SHEET 1. 2 L 7 4 4F RT 4A25 20081222 WP 2008 12 22 UPS08854174 1 20081015 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-74 AT FS 1427 L19-20L HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTALLE D REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 10. 2 L 7 4 4F RT 4A25 20080520 2008 5 20 V2J2008F00000 1 20080104 A 2120 UNKNOWN PIAGIO PWA PT6 PT6A66 52043 NE HARTZL HCE5N HCE5N3 GL CABIN ODOR E V2JA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 15 163SL 6334 634 1131 PCERK0210 KU86 AT FL280, CREW CALLED INTO THE OPERATION CONTROL CENTER TO ADVISE OF AN UNKNOWN ODOR IN THE AC, AND SLIGHT VISIBLE SMOKE . THE CREW PULLED BACK ON THE THROTTLES AND THE SMOKE DISSIPATED. THEY THEN POWERED BACK UP AND THE SMOKE WENT AWAY. THE ODOR REMAINED AND AT THAT POINT THE SIC CONTACTED ATC TO DECLARE AN EMERGENCY FOR SMOKE IN THE COCKPIT. THEY CHANGE D THEIR FLIGHT DESTINATION IN THE PROCESS. THE PIC, NOT WANTING TO DOWN-GRADE THE EMERGENCY STATUS, GOT ON THE RADIOS A ND ADVISED THAT ALL IS WELL AND THAT THE ROLLING OF EMERGENCY VEHICLES WAS NOT NECESSARY. (K) 4 T E26NE 5 C PZONE 20081008 2008 10 8 UIE2008F00036 4 20080921 A 2200 NONE GE CF6 CF650* 30018 NE NONE NONE A UIEA O OTHER O OTHER NR NOT REPORTED 1 EA 15 523MC 21782 ATB. BOTH AUTOPILOTS A AND B WILL NOT ENGAGE (BOTH TESTED OK ON GROUND). A/P A AND B PITCH AND ROLL COMPUTERS, ASTU AND M AND LU BITE CHECK ALL OK. FLT CTL HYD POWER SHUT OFF SWITCHES ALL CHECKED IN ON POSITION. A/P ACCESS BOXES INSTALLATI ON SECURED. MSP ELECT CONNECTORS INSPECTION, NO FAULTS (SEE LOG PAGES). (K) 4 F E23EA 2008021200036 20080212 00036 EA 2008 2 12 5AM2008F00000 2 20080116 A 8520 LW19332S CONNECTING ROD LYC LYC O540 TIO540J2BD 41532 EA MCAULY 3DF36C B3DF36C526 GL NR 5 CYLINDER BROKEN E 5AMA E ENGINE SHUTDOWN O OTHER LD LANDING 1 WP 15 830SA LW754061A 318052045 LW754061A 982842 CONNECTING ROD ON NR5 PISTON BROKE APART, PUNCTURING A HOLE IN THE LT ENGINE CASE HALF. PILOT SECURED THE ENGINE AND MA DE A SINGLE ENGINE LANDING AT THE AIRPORT WITHOUT INCIDENT. NO INJURIES TO PASSENGERS OR CREW. ENGINE WAS WITHIN TBO A ND IN COMPLIANCE WITH ALL AD`S. ENGINE WAS IN COMPLIANCE WITH COMPANY INSPECTION SCHEDULE. (K) 3 O E14EA 5 C